From fc124714c3901df07d324e5d7bce02db92f9bb64 Mon Sep 17 00:00:00 2001
From: aa-g <aa.gastaldi@pm.me>
Date: Wed, 19 May 2021 18:54:41 +0200
Subject: [PATCH 001/656] [WIP] Add CDeformationDriver

---
 .../include/drivers/CDeformationDriver.hpp    |  63 +++
 SU2_DEF/src/drivers/CDeformationDriver.cpp    | 501 ++++++++++++++++++
 SU2_PY/pySU2/Makefile.am                      |  21 +-
 SU2_PY/pySU2/pySU2.i                          |  10 +-
 SU2_PY/pySU2/pySU2ad.i                        |   8 +-
 5 files changed, 585 insertions(+), 18 deletions(-)
 create mode 100644 SU2_DEF/include/drivers/CDeformationDriver.hpp
 create mode 100644 SU2_DEF/src/drivers/CDeformationDriver.cpp

diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
new file mode 100644
index 00000000000..afd9a5abb8d
--- /dev/null
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -0,0 +1,63 @@
+/*!
+ * \file CDeformationDriver.hpp
+ * \brief Headers of the main subroutines for driving single or multi-zone problems.
+ *        The subroutines and functions are in the <i>driver_structure.cpp</i> file.
+ * \author T. Economon, H. Kline, R. Sanchez
+ * \version 7.1.1 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2021, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+
+#pragma once
+#include "../../../SU2_CFD/include/drivers/CDriver.hpp"
+
+/*!
+ * \class CDeformationDriver
+ * \brief Class for driving single-zone solvers.
+ * \author R. Sanchez
+ * \version 7.1.1 "Blackbird"
+ */
+class CDeformationDriver : public CDriver {
+protected:
+
+  unsigned long TimeIter;
+
+public:
+
+  /*!
+   * \brief Constructor of the class.
+   * \param[in] confFile - Configuration file name.
+   * \param[in] MPICommunicator - MPI communicator for SU2.
+   */
+  CDeformationDriver(char* confFile,
+             SU2_Comm MPICommunicator);
+
+  /*!
+   * \brief Destructor of the class.
+   */
+  ~CDeformationDriver(void) override;
+
+  /*!
+   * \brief [Overload] Launch the computation for single-zone problems.
+   */
+  void RunSolver();
+
+};
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
new file mode 100644
index 00000000000..0aa20dff8a8
--- /dev/null
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -0,0 +1,501 @@
+/*!
+ * \file SU2_DEF.cpp
+ * \brief Main file of Mesh Deformation Code (SU2_DEF).
+ * \author F. Palacios, T. Economon
+ * \version 7.1.1 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2021, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+
+
+#include "../../include/drivers/CDeformationDriver.hpp"
+#include "../../../Common/include/geometry/CPhysicalGeometry.hpp"
+#include "../../../SU2_CFD/include/output/COutput.hpp"
+#include "../../../SU2_CFD/include/output/CMeshOutput.hpp"
+using namespace std;
+
+CDeformationDriver::CDeformationDriver(char* confFile,
+                       SU2_Comm MPICommunicator) : CDriver(confFile,
+                                                          1,
+                                                          MPICommunicator,
+                                                          false) {
+
+  /*--- Initialize the counter for TimeIter ---*/
+  TimeIter = 0;
+}
+
+CDeformationDriver::~CDeformationDriver(void) {
+
+}
+
+void CDeformationDriver::RunSolver() {
+
+
+  unsigned short iZone, nZone = SINGLE_ZONE;
+    su2double StartTime = 0.0, StopTime = 0.0, UsedTime = 0.0;
+    char config_file_name[MAX_STRING_SIZE];
+    int rank, size;
+    string str;
+
+    rank = SU2_MPI::GetRank();
+    size = SU2_MPI::GetSize();
+
+    /*--- Pointer to different structures that will be used throughout
+     the entire code ---*/
+
+    CConfig **config_container          = nullptr;
+    CGeometry **geometry_container      = nullptr;
+    CSurfaceMovement **surface_movement = nullptr;
+    CVolumetricMovement **grid_movement = nullptr;
+    COutput **output                    = nullptr;
+    CConfig *driver_config              = nullptr;
+
+    /*--- Read the name and format of the input mesh file to get from the mesh
+     file the number of zones and dimensions from the numerical grid (required
+     for variables allocation)  ---*/
+
+    CConfig *config = nullptr;
+    config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DEF);
+
+    nZone    = config->GetnZone();
+
+    /*--- Definition of the containers per zones ---*/
+
+    config_container = new CConfig*[nZone];
+    geometry_container = new CGeometry*[nZone];
+    surface_movement   = new CSurfaceMovement*[nZone];
+    grid_movement      = new CVolumetricMovement*[nZone];
+    output             = new COutput*[nZone];
+
+    driver_config       = nullptr;
+
+    for (iZone = 0; iZone < nZone; iZone++) {
+      config_container[iZone]       = nullptr;
+      geometry_container[iZone]     = nullptr;
+      surface_movement[iZone]       = nullptr;
+      grid_movement[iZone]          = nullptr;
+      output[iZone]                 = nullptr;
+    }
+
+    /*--- Initialize the configuration of the driver ---*/
+    driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DEF, false);
+
+    /*--- Initialize a char to store the zone filename ---*/
+    char zone_file_name[MAX_STRING_SIZE];
+
+    /*--- Loop over all zones to initialize the various classes. In most
+     cases, nZone is equal to one. This represents the solution of a partial
+     differential equation on a single block, unstructured mesh. ---*/
+
+    for (iZone = 0; iZone < nZone; iZone++) {
+
+      /*--- Definition of the configuration option class for all zones. In this
+       constructor, the input configuration file is parsed and all options are
+       read and stored. ---*/
+
+      if (driver_config->GetnConfigFiles() > 0){
+        strcpy(zone_file_name, driver_config->GetConfigFilename(iZone).c_str());
+        config_container[iZone] = new CConfig(driver_config, zone_file_name, SU2_COMPONENT::SU2_DEF, iZone, nZone, true);
+      }
+      else{
+        config_container[iZone] = new CConfig(driver_config, config_file_name, SU2_COMPONENT::SU2_DEF, iZone, nZone, true);
+      }
+      config_container[iZone]->SetMPICommunicator(SU2_MPI::GetComm());
+    }
+
+    /*--- Set the multizone part of the problem. ---*/
+    if (driver_config->GetMultizone_Problem()){
+      for (iZone = 0; iZone < nZone; iZone++) {
+        /*--- Set the interface markers for multizone ---*/
+        config_container[iZone]->SetMultizone(driver_config, config_container);
+      }
+    }
+
+    for (iZone = 0; iZone < nZone; iZone++) {
+
+      /*--- Definition of the geometry class to store the primal grid in the partitioning process. ---*/
+
+      CGeometry *geometry_aux = nullptr;
+
+      /*--- All ranks process the grid and call ParMETIS for partitioning ---*/
+
+      geometry_aux = new CPhysicalGeometry(config_container[iZone], iZone, nZone);
+
+      /*--- Color the initial grid and set the send-receive domains (ParMETIS) ---*/
+
+      geometry_aux->SetColorGrid_Parallel(config_container[iZone]);
+
+      /*--- Build the grid data structures using the ParMETIS coloring. ---*/
+
+      geometry_container[iZone] = new CPhysicalGeometry(geometry_aux, config_container[iZone]);
+
+      /*--- Deallocate the memory of geometry_aux ---*/
+
+      delete geometry_aux;
+
+      /*--- Add the Send/Receive boundaries ---*/
+
+      geometry_container[iZone]->SetSendReceive(config_container[iZone]);
+
+      /*--- Add the Send/Receive boundaries ---*/
+
+      geometry_container[iZone]->SetBoundaries(config_container[iZone]);
+
+    }
+
+    /*--- Set up a timer for performance benchmarking (preprocessing time is included) ---*/
+
+    StartTime = SU2_MPI::Wtime();
+
+    for (iZone = 0; iZone < nZone; iZone++) {
+
+      /*--- Computational grid preprocesing ---*/
+
+      if (rank == MASTER_NODE) cout << endl << "----------------------- Preprocessing computations ----------------------" << endl;
+
+      /*--- Compute elements surrounding points, points surrounding points ---*/
+
+      if (rank == MASTER_NODE) cout << "Setting local point connectivity." <<endl;
+      geometry_container[iZone]->SetPoint_Connectivity();
+
+      /*--- Check the orientation before computing geometrical quantities ---*/
+
+      geometry_container[iZone]->SetBoundVolume();
+      if (config_container[iZone]->GetReorientElements()) {
+        if (rank == MASTER_NODE) cout << "Checking the numerical grid orientation of the interior elements." <<endl;
+        geometry_container[iZone]->Check_IntElem_Orientation(config_container[iZone]);
+        geometry_container[iZone]->Check_BoundElem_Orientation(config_container[iZone]);
+      }
+
+      /*--- Create the edge structure ---*/
+
+      if (rank == MASTER_NODE) cout << "Identify edges and vertices." <<endl;
+      geometry_container[iZone]->SetEdges();
+      geometry_container[iZone]->SetVertex(config_container[iZone]);
+
+      if (config_container[iZone]->GetDesign_Variable(0) != NO_DEFORMATION) {
+
+        /*--- Create the dual control volume structures ---*/
+
+        if (rank == MASTER_NODE) cout << "Setting the bound control volume structure." << endl;
+        geometry_container[iZone]->SetControlVolume(config_container[iZone], ALLOCATE);
+        geometry_container[iZone]->SetBoundControlVolume(config_container[iZone], ALLOCATE);
+
+      }
+      /*--- Create the point-to-point MPI communication structures. ---*/
+
+      geometry_container[iZone]->PreprocessP2PComms(geometry_container[iZone], config_container[iZone]);
+
+      /*--- Allocate the mesh output ---*/
+
+      output[iZone] = new CMeshOutput(config_container[iZone], geometry_container[iZone]->GetnDim());
+
+      /*--- Preprocess the volume output ---*/
+
+      output[iZone]->PreprocessVolumeOutput(config_container[iZone]);
+
+      /*--- Preprocess history --- */
+
+      output[iZone]->PreprocessHistoryOutput(config_container[iZone], false);
+
+    }
+
+
+    /*--- Surface grid deformation using design variables ---*/
+
+    for (iZone = 0; iZone < nZone; iZone++){
+
+      if (config_container[iZone]->GetDesign_Variable(0) != NO_DEFORMATION) {
+
+        /*--- Definition of the Class for grid movement ---*/
+        grid_movement[iZone] = new CVolumetricMovement(geometry_container[iZone], config_container[iZone]);
+
+        /*--- Save original coordinates to be reused in convexity checking procedure ---*/
+        auto OriginalCoordinates = geometry_container[iZone]->nodes->GetCoord();
+
+        /*--- First check for volumetric grid deformation/transformations ---*/
+
+        if (config_container[iZone]->GetDesign_Variable(0) == SCALE_GRID) {
+
+          if (rank == MASTER_NODE)
+            cout << endl << "--------------------- Volumetric grid scaling (ZONE " << iZone <<") ------------------" << endl;
+          grid_movement[iZone]->SetVolume_Scaling(geometry_container[iZone], config_container[iZone], false);
+
+        } else if (config_container[iZone]->GetDesign_Variable(0) == TRANSLATE_GRID) {
+
+          if (rank == MASTER_NODE)
+            cout << endl << "------------------- Volumetric grid translation (ZONE " << iZone <<") ----------------" << endl;
+          grid_movement[iZone]->SetVolume_Translation(geometry_container[iZone], config_container[iZone], false);
+
+        } else if (config_container[iZone]->GetDesign_Variable(0) == ROTATE_GRID) {
+
+          if (rank == MASTER_NODE)
+            cout << endl << "--------------------- Volumetric grid rotation (ZONE " << iZone <<") -----------------" << endl;
+          grid_movement[iZone]->SetVolume_Rotation(geometry_container[iZone], config_container[iZone], false);
+
+        } else {
+
+          /*--- If no volume-type deformations are requested, then this is a
+           surface-based deformation or FFD set up. ---*/
+
+          if (rank == MASTER_NODE)
+            cout << endl << "--------------------- Surface grid deformation (ZONE " << iZone <<") -----------------" << endl;
+
+          /*--- Definition and initialization of the surface deformation class ---*/
+
+          surface_movement[iZone] = new CSurfaceMovement();
+
+          /*--- Copy coordinates to the surface structure ---*/
+
+          surface_movement[iZone]->CopyBoundary(geometry_container[iZone], config_container[iZone]);
+
+          /*--- Surface grid deformation ---*/
+
+          if (rank == MASTER_NODE) cout << "Performing the deformation of the surface grid." << endl;
+          auto TotalDeformation = surface_movement[iZone]->SetSurface_Deformation(geometry_container[iZone], config_container[iZone]);
+
+          if (config_container[iZone]->GetDesign_Variable(0) != FFD_SETTING) {
+
+            if (rank == MASTER_NODE)
+              cout << endl << "------------------- Volumetric grid deformation (ZONE " << iZone <<") ----------------" << endl;
+
+            if (rank == MASTER_NODE)
+              cout << "Performing the deformation of the volumetric grid." << endl;
+            grid_movement[iZone]->SetVolume_Deformation(geometry_container[iZone], config_container[iZone], false);
+
+            /*--- Get parameters for convexity check ---*/
+            bool ConvexityCheck;
+            unsigned short ConvexityCheck_MaxIter, ConvexityCheck_MaxDepth;
+
+            tie(ConvexityCheck, ConvexityCheck_MaxIter, ConvexityCheck_MaxDepth) = config_container[iZone]->GetConvexityCheck();
+
+            /*--- Recursively change deformations if there are nonconvex elements. ---*/
+
+            if (ConvexityCheck && geometry_container[iZone]->GetnNonconvexElements() > 0) {
+              if (rank == MASTER_NODE) {
+                cout << "Nonconvex elements present after deformation. " << endl;
+                cout << "Recursively lowering deformation magnitude." << endl;
+              }
+
+              /*--- Load initial deformation values ---*/
+              auto InitialDeformation = TotalDeformation;
+
+              unsigned short ConvexityCheckIter, RecursionDepth = 0;
+              su2double DeformationFactor = 1.0, DeformationDifference = 1.0;
+              for (ConvexityCheckIter = 1; ConvexityCheckIter <= ConvexityCheck_MaxIter; ConvexityCheckIter++) {
+
+                /*--- Recursively change deformation magnitude:
+                decrease if there are nonconvex elements, increase otherwise ---*/
+                DeformationDifference /= 2.0;
+
+                if (geometry_container[iZone]->GetnNonconvexElements() > 0) {
+                  DeformationFactor -= DeformationDifference;
+                } else {
+                  RecursionDepth += 1;
+
+                  if (RecursionDepth == ConvexityCheck_MaxDepth) {
+                    if (rank == MASTER_NODE) {
+                      cout << "Maximum recursion depth reached." << endl;
+                      cout << "Remaining amount of original deformation: ";
+                      cout << DeformationFactor*100.0 << " percent. " << endl;
+                    }
+                    break;
+                  }
+
+                  DeformationFactor += DeformationDifference;
+                }
+
+                /*--- Load mesh to start every iteration with an undeformed grid ---*/
+                for (auto iPoint = 0ul; iPoint < OriginalCoordinates.rows(); iPoint++) {
+                  for (auto iDim = 0ul; iDim < OriginalCoordinates.cols(); iDim++) {
+                    geometry_container[iZone]->nodes->SetCoord(iPoint, iDim, OriginalCoordinates(iPoint,iDim));
+                  }
+                }
+
+                /*--- Set deformation magnitude as percentage of initial deformation ---*/
+                for (auto iDV = 0u; iDV < config->GetnDV(); iDV++) {
+                  for (auto iDV_Value = 0u; iDV_Value < config->GetnDV_Value(iDV); iDV_Value++) {
+                    config_container[iZone]->SetDV_Value(iDV, iDV_Value, InitialDeformation[iDV][iDV_Value]*DeformationFactor);
+                  }
+                }
+
+                /*--- Surface grid deformation ---*/
+                if (rank == MASTER_NODE) cout << "Performing the deformation of the surface grid." << endl;
+
+                TotalDeformation = surface_movement[iZone]->SetSurface_Deformation(geometry_container[iZone], config_container[iZone]);
+
+                if (rank == MASTER_NODE)
+                  cout << endl << "------------------- Volumetric grid deformation (ZONE " << iZone <<") ----------------" << endl;
+
+                if (rank == MASTER_NODE)
+                  cout << "Performing the deformation of the volumetric grid." << endl;
+                grid_movement[iZone]->SetVolume_Deformation(geometry_container[iZone], config_container[iZone], false);
+
+                if (rank == MASTER_NODE) {
+                  cout << "Number of nonconvex elements for iteration " << ConvexityCheckIter << ": ";
+                  cout << geometry_container[iZone]->GetnNonconvexElements() << endl;
+                  cout << "Remaining amount of original deformation: ";
+                  cout << DeformationFactor*100.0 << " percent. " << endl;
+                }
+
+              }
+
+            }
+
+          }
+
+        }
+
+      }
+
+    }
+
+    /*--- Computational grid preprocesing ---*/
+
+    if (rank == MASTER_NODE) cout << endl << "----------------------- Write deformed grid files -----------------------" << endl;
+
+    /*--- Output deformed grid for visualization, if requested (surface and volumetric), in parallel
+     requires to move all the data to the master node---*/
+
+    for (iZone = 0; iZone < nZone; iZone++){
+
+      /*--- Compute Mesh Quality if requested. Necessary geometry preprocessing re-done beforehand. ---*/
+
+      if (config_container[iZone]->GetWrt_MeshQuality() && !config->GetStructuralProblem()) {
+
+        if (rank == MASTER_NODE) cout << "Recompute geometry properties necessary to evaluate mesh quality statistics.\n";
+
+        geometry_container[iZone]->SetPoint_Connectivity();
+        geometry_container[iZone]->SetBoundVolume();
+        geometry_container[iZone]->SetEdges();
+        geometry_container[iZone]->SetVertex(config_container[iZone]);
+        geometry_container[iZone]->SetControlVolume(config_container[iZone], ALLOCATE);
+        geometry_container[iZone]->SetBoundControlVolume(config_container[iZone], ALLOCATE);
+
+        if (rank == MASTER_NODE) cout << "Computing mesh quality statistics for the dual control volumes.\n";
+        geometry_container[iZone]->ComputeMeshQualityStatistics(config_container[iZone]);
+      }// Mesh Quality Output
+
+      /*--- Load the data --- */
+
+      output[iZone]->Load_Data(geometry_container[iZone], config_container[iZone], nullptr);
+
+      output[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone], MESH, config->GetMesh_Out_FileName());
+
+      /*--- Set the file names for the visualization files ---*/
+
+      output[iZone]->SetVolume_Filename("volume_deformed");
+      output[iZone]->SetSurface_Filename("surface_deformed");
+
+      for (unsigned short iFile = 0; iFile < config_container[iZone]->GetnVolumeOutputFiles(); iFile++){
+        auto FileFormat = config_container[iZone]->GetVolumeOutputFiles();
+        if (FileFormat[iFile] != RESTART_ASCII && FileFormat[iFile] != RESTART_BINARY)
+          output[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone], FileFormat[iFile]);
+      }
+    }
+
+
+    if ((config_container[ZONE_0]->GetDesign_Variable(0) != NO_DEFORMATION) &&
+        (config_container[ZONE_0]->GetDesign_Variable(0) != SCALE_GRID)     &&
+        (config_container[ZONE_0]->GetDesign_Variable(0) != TRANSLATE_GRID) &&
+        (config_container[ZONE_0]->GetDesign_Variable(0) != ROTATE_GRID)) {
+
+      /*--- Write the the free-form deformation boxes after deformation. ---*/
+
+      if (rank == MASTER_NODE) cout << "Adding any FFD information to the SU2 file." << endl;
+
+      surface_movement[ZONE_0]->WriteFFDInfo(surface_movement, geometry_container, config_container);
+
+    }
+
+    delete config;
+    config = nullptr;
+    if (rank == MASTER_NODE)
+      cout << endl <<"------------------------- Solver Postprocessing -------------------------" << endl;
+
+    if (geometry_container != nullptr) {
+      for (iZone = 0; iZone < nZone; iZone++) {
+        if (geometry_container[iZone] != nullptr) {
+          delete geometry_container[iZone];
+        }
+      }
+      delete [] geometry_container;
+    }
+    if (rank == MASTER_NODE) cout << "Deleted CGeometry container." << endl;
+
+    if (surface_movement != nullptr) {
+      for (iZone = 0; iZone < nZone; iZone++) {
+        if (surface_movement[iZone] != nullptr) {
+          delete surface_movement[iZone];
+        }
+      }
+      delete [] surface_movement;
+    }
+    if (rank == MASTER_NODE) cout << "Deleted CSurfaceMovement class." << endl;
+
+    if (grid_movement != nullptr) {
+      for (iZone = 0; iZone < nZone; iZone++) {
+        if (grid_movement[iZone] != nullptr) {
+          delete grid_movement[iZone];
+        }
+      }
+      delete [] grid_movement;
+    }
+    if (rank == MASTER_NODE) cout << "Deleted CVolumetricMovement class." << endl;
+
+    if (config_container != nullptr) {
+      for (iZone = 0; iZone < nZone; iZone++) {
+        if (config_container[iZone] != nullptr) {
+          delete config_container[iZone];
+        }
+      }
+      delete [] config_container;
+    }
+    if (output != nullptr) {
+      for (iZone = 0; iZone < nZone; iZone++) {
+        if (output[iZone] != nullptr) {
+          delete output[iZone];
+        }
+      }
+      delete [] output;
+    }
+    if (rank == MASTER_NODE) cout << "Deleted CConfig container." << endl;
+
+    if (rank == MASTER_NODE) cout << "Deleted COutput class." << endl;
+
+    /*--- Synchronization point after a single solver iteration. Compute the
+     wall clock time required. ---*/
+
+    StopTime = SU2_MPI::Wtime();
+
+    /*--- Compute/print the total time for performance benchmarking. ---*/
+
+    UsedTime = StopTime-StartTime;
+    if (rank == MASTER_NODE) {
+      cout << "\nCompleted in " << fixed << UsedTime << " seconds on "<< size;
+      if (size == 1) cout << " core." << endl; else cout << " cores." << endl;
+    }
+
+    /*--- Exit the solver cleanly ---*/
+
+    if (rank == MASTER_NODE)
+      cout << endl << "------------------------- Exit Success (SU2_DEF) ------------------------" << endl << endl;
+  }
diff --git a/SU2_PY/pySU2/Makefile.am b/SU2_PY/pySU2/Makefile.am
index 29c7ef1833b..631400db6bd 100644
--- a/SU2_PY/pySU2/Makefile.am
+++ b/SU2_PY/pySU2/Makefile.am
@@ -6,8 +6,8 @@
 # \version 7.1.1 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
-# 
-# The SU2 Project is maintained by the SU2 Foundation 
+#
+# The SU2 Project is maintained by the SU2 Foundation
 # (http://su2foundation.org)
 #
 # Copyright 2012-2021, SU2 Contributors (cf. AUTHORS.md)
@@ -16,7 +16,7 @@
 # modify it under the terms of the GNU Lesser General Public
 # License as published by the Free Software Foundation; either
 # version 2.1 of the License, or (at your option) any later version.
-# 
+#
 # SU2 is distributed in the hope that it will be useful,
 # but WITHOUT ANY WARRANTY; without even the implied warranty of
 # MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
@@ -61,15 +61,15 @@ PY_LIB = ${PYTHON_LIBS} \
          -L${PYTHON_EXEC_PREFIX}/lib \
          -L/usr/lib \
          -L/usr/lib/x86_64-linux-gnu
-         
+
 
 SWIG_INCLUDE = ${PY_INCLUDE}
 
 SUBDIR_EXEC = ${bindir}
 
-all:	
-	${MAKE} real; 
-	
+all:
+	${MAKE} real;
+
 # List the dependencies
 real: ${SWIG_SO_REAL}
 
@@ -104,11 +104,11 @@ pySU2_LD_FLAGS = ${SU2SOLVER_LIB} @su2_externals_LIBS@ ${PY_LIB}
 # Set the command line flags to use for compilation
 pySU2_CC_FLAGS = ${CPPFLAGS} ${EXTRA_CC_FLAGS} @su2_externals_INCLUDES@ ${pySU2_INCLUDE}
 
-SO_LINK_FLAGS= -fPIC -shared 
+SO_LINK_FLAGS= -fPIC -shared
 
 # Default rule for creating the _wrap.cxx file from the .i file
 ${SWIG_WRAP_REAL}.cxx: ${SU2SOLVER_LIB} ${SWIG_SRC}
-	${SWIG} ${CPPFLAGS} -Wall ${SWIG_INCLUDE} -outdir ./ -o ${SWIG_WRAP_REAL}.cxx -c++ -python ${SWIG_SRC} 
+	${SWIG} ${CPPFLAGS} -Wall ${SWIG_INCLUDE} -outdir ./ -o ${SWIG_WRAP_REAL}.cxx -c++ -python ${SWIG_SRC}
 
 #Default rule for compiling the .o files
 ${SWIG_WRAP_REAL}.o: ${SWIG_WRAP_REAL}.cxx
@@ -122,7 +122,7 @@ ${SWIG_SO_REAL}: ${SWIG_WRAP_REAL}.o
 
 .SECONDARY:
 
-clean: 
+clean:
 	rm -f ${CURRENT_DIR}/*.cxx
 	rm -f ${CURRENT_DIR}/*.${SO_EXT}
 	rm -f ${CURRENT_DIR}/*.o
@@ -132,4 +132,3 @@ clean:
 install: all
 	${INSTALL} ${PYLIB} ${bindir}
 	${INSTALL} ${SOLIB} ${bindir}
-
diff --git a/SU2_PY/pySU2/pySU2.i b/SU2_PY/pySU2/pySU2.i
index e783ac8b48b..c042919a506 100644
--- a/SU2_PY/pySU2/pySU2.i
+++ b/SU2_PY/pySU2/pySU2.i
@@ -7,8 +7,8 @@
 #  \version 7.1.1 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
-# 
-# The SU2 Project is maintained by the SU2 Foundation 
+#
+# The SU2 Project is maintained by the SU2 Foundation
 # (http://su2foundation.org)
 #
 # Copyright 2012-2021, SU2 Contributors (cf. AUTHORS.md)
@@ -17,7 +17,7 @@
 # modify it under the terms of the GNU Lesser General Public
 # License as published by the Free Software Foundation; either
 # version 2.1 of the License, or (at your option) any later version.
-# 
+#
 # SU2 is distributed in the hope that it will be useful,
 # but WITHOUT ANY WARRANTY; without even the implied warranty of
 # MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
@@ -42,7 +42,8 @@ threads="1"
 #include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CMultizoneDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp"
-  
+#include "../../SU2_DEF/include/drivers/CDeformationDriver.hpp"
+
 %}
 
 // ----------- USED MODULES ------------
@@ -91,3 +92,4 @@ const unsigned int ZONE_1 = 1; /*!< \brief Definition of the first grid domain.
 %include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CMultizoneDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp"
+%include "../../SU2_DEF/include/drivers/CDeformationDriver.hpp"
diff --git a/SU2_PY/pySU2/pySU2ad.i b/SU2_PY/pySU2/pySU2ad.i
index aaf37844c90..910202a138e 100644
--- a/SU2_PY/pySU2/pySU2ad.i
+++ b/SU2_PY/pySU2/pySU2ad.i
@@ -7,8 +7,8 @@
 # \version 7.1.1 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
-# 
-# The SU2 Project is maintained by the SU2 Foundation 
+#
+# The SU2 Project is maintained by the SU2 Foundation
 # (http://su2foundation.org)
 #
 # Copyright 2012-2021, SU2 Contributors (cf. AUTHORS.md)
@@ -17,7 +17,7 @@
 # modify it under the terms of the GNU Lesser General Public
 # License as published by the Free Software Foundation; either
 # version 2.1 of the License, or (at your option) any later version.
-# 
+#
 # SU2 is distributed in the hope that it will be useful,
 # but WITHOUT ANY WARRANTY; without even the implied warranty of
 # MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
@@ -42,6 +42,7 @@ threads="1"
 #include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CMultizoneDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp"
+#include "../../SU2_DEF/include/drivers/CDeformationDriver.hpp"
 
 %}
 
@@ -91,3 +92,4 @@ const unsigned int ZONE_1 = 1; /*!< \brief Definition of the first grid domain.
 %include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CMultizoneDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp"
+%include "../../SU2_DEF/include/drivers/CDeformationDriver.hpp"

From 2643405946420bf47459c7961fafa2c4c80eb08b Mon Sep 17 00:00:00 2001
From: aa-g <aa.gastaldi@pm.me>
Date: Fri, 21 May 2021 18:48:51 +0200
Subject: [PATCH 002/656] Implement RunSolver()

---
 .../include/drivers/CDeformationDriver.hpp    | 22 ++++--
 SU2_DEF/src/drivers/CDeformationDriver.cpp    | 36 ++++-----
 SU2_DEF/src/meson.build                       | 73 +++++++++++--------
 SU2_PY/pySU2/meson.build                      |  2 +-
 SU2_PY/pySU2/pySU2ad.i                        |  2 -
 5 files changed, 79 insertions(+), 56 deletions(-)

diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index afd9a5abb8d..e2fd22f748f 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -27,7 +27,8 @@
  */
 
 #pragma once
-#include "../../../SU2_CFD/include/drivers/CDriver.hpp"
+#include "../../../Common/include/parallelization/mpi_structure.hpp"
+#include "../../../Common/include/geometry/CGeometry.hpp"
 
 /*!
  * \class CDeformationDriver
@@ -35,13 +36,11 @@
  * \author R. Sanchez
  * \version 7.1.1 "Blackbird"
  */
-class CDeformationDriver : public CDriver {
+class CDeformationDriver {
 protected:
-
-  unsigned long TimeIter;
+  char config_file_name[MAX_STRING_SIZE];
 
 public:
-
   /*!
    * \brief Constructor of the class.
    * \param[in] confFile - Configuration file name.
@@ -53,11 +52,22 @@ class CDeformationDriver : public CDriver {
   /*!
    * \brief Destructor of the class.
    */
-  ~CDeformationDriver(void) override;
+  ~CDeformationDriver(void);
 
   /*!
    * \brief [Overload] Launch the computation for single-zone problems.
    */
   void RunSolver();
 
+protected:
+    /*!
+     * \brief Init_Containers
+     */
+    void SetContainers_Null();
+
+    /*!
+     * \brief Read in the config and mesh files.
+     */
+    void Input_Preprocessing(CConfig **&config, CConfig *&driver_config);
+
 };
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 0aa20dff8a8..529085f87e6 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -12,7 +12,7 @@
  * Copyright 2012-2021, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
+ * modify it under the terms of the GNU Lesser/ General Public
  * License as published by the Free Software Foundation; either
  * version 2.1 of the License, or (at your option) any later version.
  *
@@ -28,18 +28,25 @@
 
 #include "../../include/drivers/CDeformationDriver.hpp"
 #include "../../../Common/include/geometry/CPhysicalGeometry.hpp"
+#include "../../../Common/include/grid_movement/CSurfaceMovement.hpp"
+#include "../../../Common/include/grid_movement/CVolumetricMovement.hpp"
 #include "../../../SU2_CFD/include/output/COutput.hpp"
 #include "../../../SU2_CFD/include/output/CMeshOutput.hpp"
 using namespace std;
 
-CDeformationDriver::CDeformationDriver(char* confFile,
-                       SU2_Comm MPICommunicator) : CDriver(confFile,
-                                                          1,
-                                                          MPICommunicator,
-                                                          false) {
+CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator) {
 
-  /*--- Initialize the counter for TimeIter ---*/
-  TimeIter = 0;
+  /*--- Initialize Medipack (must also be here so it is initialized from python) ---*/
+  #ifdef HAVE_MPI
+    #if defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)
+      SU2_MPI::Init_AMPI();
+    #endif
+  #endif
+
+    SU2_MPI::SetComm(MPICommunicator);
+
+  /*--- Copy the config filename ---*/
+  strcpy(config_file_name, confFile);
 }
 
 CDeformationDriver::~CDeformationDriver(void) {
@@ -48,15 +55,12 @@ CDeformationDriver::~CDeformationDriver(void) {
 
 void CDeformationDriver::RunSolver() {
 
-
-  unsigned short iZone, nZone = SINGLE_ZONE;
+    unsigned short iZone, nZone = SINGLE_ZONE;
     su2double StartTime = 0.0, StopTime = 0.0, UsedTime = 0.0;
-    char config_file_name[MAX_STRING_SIZE];
-    int rank, size;
     string str;
 
-    rank = SU2_MPI::GetRank();
-    size = SU2_MPI::GetSize();
+    int rank = SU2_MPI::GetRank();
+    int size = SU2_MPI::GetSize();
 
     /*--- Pointer to different structures that will be used throughout
      the entire code ---*/
@@ -79,7 +83,7 @@ void CDeformationDriver::RunSolver() {
 
     /*--- Definition of the containers per zones ---*/
 
-    config_container = new CConfig*[nZone];
+    config_container   = new CConfig*[nZone];
     geometry_container = new CGeometry*[nZone];
     surface_movement   = new CSurfaceMovement*[nZone];
     grid_movement      = new CVolumetricMovement*[nZone];
@@ -215,10 +219,8 @@ void CDeformationDriver::RunSolver() {
       /*--- Preprocess history --- */
 
       output[iZone]->PreprocessHistoryOutput(config_container[iZone], false);
-
     }
 
-
     /*--- Surface grid deformation using design variables ---*/
 
     for (iZone = 0; iZone < nZone; iZone++){
diff --git a/SU2_DEF/src/meson.build b/SU2_DEF/src/meson.build
index d18ed7a46b0..a6681c5c88d 100644
--- a/SU2_DEF/src/meson.build
+++ b/SU2_DEF/src/meson.build
@@ -1,38 +1,51 @@
-su2_def_src = ['SU2_DEF.cpp']
+su2_def_include = include_directories('./')
+su2_def_src = files([
+  'SU2_DEF.cpp',
+  'drivers/CDeformationDriver.cpp'
+])
 if get_option('enable-normal')
 
-  su2_cfd_obj = su2_cfd_lib.extract_objects(['solvers/CSolver.cpp',
-                                        'solvers/CBaselineSolver.cpp',
-                                        'CMarkerProfileReaderFVM.cpp',
-                                        'output/COutput.cpp',
-                                        'output/tools/CWindowingTools.cpp',
-                                        'output/CMeshOutput.cpp',
-                                        'output/output_structure_legacy.cpp',
-                                        'variables/CBaselineVariable.cpp',
-                                        'variables/CVariable.cpp',
-                                        'output/filewriter/CParallelDataSorter.cpp',
-                                        'output/filewriter/CFVMDataSorter.cpp',
-                                        'output/filewriter/CFEMDataSorter.cpp',
-                                        'output/filewriter/CSurfaceFEMDataSorter.cpp',
-                                        'output/filewriter/CSurfaceFVMDataSorter.cpp',
-                                        'output/filewriter/CParallelFileWriter.cpp',
-                                        'output/filewriter/CParaviewFileWriter.cpp',
-                                        'output/filewriter/CParaviewBinaryFileWriter.cpp',
-                                        'output/filewriter/CTecplotFileWriter.cpp',
-                                        'output/filewriter/CTecplotBinaryFileWriter.cpp',
-                                        'output/filewriter/CCSVFileWriter.cpp',
-                                        'output/filewriter/CSTLFileWriter.cpp',
-                                        'output/filewriter/CSU2FileWriter.cpp',
-                                        'output/filewriter/CSU2BinaryFileWriter.cpp',
-                                        'output/filewriter/CParaviewXMLFileWriter.cpp',
-                                        'output/filewriter/CParaviewVTMFileWriter.cpp',
-                                        'output/filewriter/CSU2MeshFileWriter.cpp',
-                                        'limiters/CLimiterDetails.cpp'])
+su2_cfd_obj = su2_cfd_lib.extract_objects(['solvers/CSolver.cpp',
+                                      'solvers/CBaselineSolver.cpp',
+                                      'CMarkerProfileReaderFVM.cpp',
+                                      'output/COutput.cpp',
+                                      'output/tools/CWindowingTools.cpp',
+                                      'output/CMeshOutput.cpp',
+                                      'output/output_structure_legacy.cpp',
+                                      'variables/CBaselineVariable.cpp',
+                                      'variables/CVariable.cpp',
+                                      'output/filewriter/CParallelDataSorter.cpp',
+                                      'output/filewriter/CFVMDataSorter.cpp',
+                                      'output/filewriter/CFEMDataSorter.cpp',
+                                      'output/filewriter/CSurfaceFEMDataSorter.cpp',
+                                      'output/filewriter/CSurfaceFVMDataSorter.cpp',
+                                      'output/filewriter/CParallelFileWriter.cpp',
+                                      'output/filewriter/CParaviewFileWriter.cpp',
+                                      'output/filewriter/CParaviewBinaryFileWriter.cpp',
+                                      'output/filewriter/CTecplotFileWriter.cpp',
+                                      'output/filewriter/CTecplotBinaryFileWriter.cpp',
+                                      'output/filewriter/CCSVFileWriter.cpp',
+                                      'output/filewriter/CSTLFileWriter.cpp',
+                                      'output/filewriter/CSU2FileWriter.cpp',
+                                      'output/filewriter/CSU2BinaryFileWriter.cpp',
+                                      'output/filewriter/CParaviewXMLFileWriter.cpp',
+                                      'output/filewriter/CParaviewVTMFileWriter.cpp',
+                                      'output/filewriter/CSU2MeshFileWriter.cpp',
+                                      'limiters/CLimiterDetails.cpp'])
+
+  su2_def_lib = static_library('SU2core_DEF',
+                               su2_def_src,
+                               install : false,
+                               dependencies : [su2_deps, common_dep],
+                               cpp_args:  [default_warning_flags, su2_cpp_args])
+
+  su2_def_dep = declare_dependency(link_with: su2_def_lib,
+                                   include_directories: su2_def_include)
 
   su2_def = executable('SU2_DEF',
-                        su2_def_src, 
+                        su2_def_src,
                         install: true,
-                        dependencies: [su2_deps, common_dep], 
+                        dependencies: [su2_deps, common_dep],
                         objects : su2_cfd_obj,
                         cpp_args :[default_warning_flags, su2_cpp_args])
 endif
diff --git a/SU2_PY/pySU2/meson.build b/SU2_PY/pySU2/meson.build
index 1404f7fe10a..1aab2e53b50 100644
--- a/SU2_PY/pySU2/meson.build
+++ b/SU2_PY/pySU2/meson.build
@@ -28,7 +28,7 @@ if get_option('enable-normal')
       '_pysu2',
       cpp_source,
       dependencies: [wrapper_deps, common_dep, su2_deps],
-      objects: su2_cfd_lib.extract_all_objects(),
+      objects: [su2_cfd_lib.extract_all_objects(), su2_def_lib.extract_objects('drivers/CDeformationDriver.cpp')],
       install: true,
       include_directories : mpi4py_include,
       cpp_args : [default_warning_flags,su2_cpp_args],
diff --git a/SU2_PY/pySU2/pySU2ad.i b/SU2_PY/pySU2/pySU2ad.i
index 910202a138e..4409fd93fcb 100644
--- a/SU2_PY/pySU2/pySU2ad.i
+++ b/SU2_PY/pySU2/pySU2ad.i
@@ -42,7 +42,6 @@ threads="1"
 #include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CMultizoneDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp"
-#include "../../SU2_DEF/include/drivers/CDeformationDriver.hpp"
 
 %}
 
@@ -92,4 +91,3 @@ const unsigned int ZONE_1 = 1; /*!< \brief Definition of the first grid domain.
 %include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CMultizoneDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp"
-%include "../../SU2_DEF/include/drivers/CDeformationDriver.hpp"

From 907b5bfd4fae3f6db7ec141f9de9c3f002bd220f Mon Sep 17 00:00:00 2001
From: aa-g <aa.gastaldi@pm.me>
Date: Tue, 25 May 2021 19:06:39 +0200
Subject: [PATCH 003/656] Clean up CDeformationDriver implementation.

Refactor some pre-processing operations in constructor to Geometrical_Preprocessing() and Output_Preprocessing().
Refactor SU2_DEF main function to use the new CDeformationDriver class.
---
 SU2_DEF/include/SU2_DEF.hpp                   |   7 +-
 .../include/drivers/CDeformationDriver.hpp    |  53 +-
 SU2_DEF/src/SU2_DEF.cpp                       | 456 +-----------------
 SU2_DEF/src/drivers/CDeformationDriver.cpp    | 265 +++++-----
 4 files changed, 200 insertions(+), 581 deletions(-)

diff --git a/SU2_DEF/include/SU2_DEF.hpp b/SU2_DEF/include/SU2_DEF.hpp
index 462599f36df..505e72a73d0 100644
--- a/SU2_DEF/include/SU2_DEF.hpp
+++ b/SU2_DEF/include/SU2_DEF.hpp
@@ -32,14 +32,11 @@
 #include "../../Common/include/parallelization/mpi_structure.hpp"
 #include "../../Common/include/parallelization/omp_structure.hpp"
 
+#include "drivers/CDeformationDriver.hpp"
+
 #include <cstdlib>
 #include <iostream>
 #include <iomanip>
 #include <cmath>
 
-#include "../../SU2_CFD/include/solvers/CSolver.hpp"
-#include "../../SU2_CFD/include/output/CMeshOutput.hpp"
-#include "../../Common/include/geometry/CPhysicalGeometry.hpp"
-#include "../../Common/include/CConfig.hpp"
-
 using namespace std;
diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index e2fd22f748f..b76a2919976 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -27,7 +27,12 @@
  */
 
 #pragma once
+
 #include "../../../Common/include/parallelization/mpi_structure.hpp"
+
+#include "../../../Common/include/grid_movement/CSurfaceMovement.hpp"
+#include "../../../Common/include/grid_movement/CVolumetricMovement.hpp"
+#include "../../../SU2_CFD/include/output/COutput.hpp"
 #include "../../../Common/include/geometry/CGeometry.hpp"
 
 /*!
@@ -39,6 +44,21 @@
 class CDeformationDriver {
 protected:
   char config_file_name[MAX_STRING_SIZE];
+  int rank,
+      size;
+  su2double StartTime,                          /*!< \brief Start point of the timer for performance benchmarking.*/
+            StopTime,                           /*!< \brief Stop point of the timer for performance benchmarking.*/
+            UsedTimePreproc,                    /*!< \brief Elapsed time between Start and Stop point of the timer for tracking preprocessing phase.*/
+            UsedTimeCompute,                    /*!< \brief Elapsed time between Start and Stop point of the timer for tracking compute phase.*/
+            UsedTime;                           /*!< \brief Elapsed time between Start and Stop point of the timer.*/
+  unsigned short iZone, nZone = SINGLE_ZONE;
+  CConfig *driver_config;                       /*!< \brief Definition of the driver configuration. */
+  CConfig **config_container;                   /*!< \brief Definition of the particular problem. */
+  CGeometry **geometry_container;             /*!< \brief Geometrical definition of the problem. */
+  CSurfaceMovement **surface_movement;          /*!< \brief Surface movement classes of the problem. */
+  CVolumetricMovement **grid_movement;         /*!< \brief Volume grid movement classes of the problem. */
+  COutput **output_container;                   /*!< \brief Pointer to the COutput class. */
+                   /*!< \brief FFD FFDBoxes of the problem. */
 
 public:
   /*!
@@ -57,17 +77,32 @@ class CDeformationDriver {
   /*!
    * \brief [Overload] Launch the computation for single-zone problems.
    */
-  void RunSolver();
+  void Run();
+
+  /*!
+   * \brief Deallocation routine
+   */
+  void Postprocessing();
 
 protected:
-    /*!
-     * \brief Init_Containers
-     */
-    void SetContainers_Null();
+  /*!
+   * \brief Init_Containers
+   */
+  void SetContainers_Null();
 
-    /*!
-     * \brief Read in the config and mesh files.
-     */
-    void Input_Preprocessing(CConfig **&config, CConfig *&driver_config);
+  /*!
+   * \brief Read in the config and mesh files.
+   */
+  void Input_Preprocessing();
+
+  /*!
+   * \brief Construction of the edge-based data structure.
+   */
+  void Geometrical_Preprocessing(CConfig *config, CGeometry *&geometry);
+
+  /*!
+   * \brief Preprocess the output container.
+   */
+  void Output_Preprocessing(CConfig *config, CGeometry *geometry, COutput *&output);
 
 };
diff --git a/SU2_DEF/src/SU2_DEF.cpp b/SU2_DEF/src/SU2_DEF.cpp
index adb078ae4a1..ea0ce32bcb2 100644
--- a/SU2_DEF/src/SU2_DEF.cpp
+++ b/SU2_DEF/src/SU2_DEF.cpp
@@ -27,15 +27,16 @@
 
 
 #include "../include/SU2_DEF.hpp"
+
 using namespace std;
 
 int main(int argc, char *argv[]) {
 
-  unsigned short iZone, nZone = SINGLE_ZONE;
-  su2double StartTime = 0.0, StopTime = 0.0, UsedTime = 0.0;
   char config_file_name[MAX_STRING_SIZE];
-  int rank, size;
-  string str;
+
+  /*--- Create a pointer to the main SU2_DEF Driver ---*/
+
+  CDeformationDriver* driver = nullptr;
 
   /*--- MPI initialization ---*/
 
@@ -45,20 +46,7 @@ int main(int argc, char *argv[]) {
 #else
   SU2_MPI::Init(&argc, &argv);
 #endif
-  SU2_MPI::Comm MPICommunicator = SU2_MPI::GetComm();
-
-  rank = SU2_MPI::GetRank();
-  size = SU2_MPI::GetSize();
-
-  /*--- Pointer to different structures that will be used throughout
-   the entire code ---*/
-
-  CConfig **config_container          = nullptr;
-  CGeometry **geometry_container      = nullptr;
-  CSurfaceMovement **surface_movement = nullptr;
-  CVolumetricMovement **grid_movement = nullptr;
-  COutput **output                     = nullptr;
-  CConfig *driver_config                = nullptr;
+  SU2_MPI::Comm comm = SU2_MPI::GetComm();
 
   /*--- Load in the number of zones and spatial dimensions in the mesh file
    (if no config file is specified, default.cfg is used) ---*/
@@ -66,436 +54,18 @@ int main(int argc, char *argv[]) {
   if (argc == 2) { strcpy(config_file_name, argv[1]); }
   else { strcpy(config_file_name, "default.cfg"); }
 
-  /*--- Read the name and format of the input mesh file to get from the mesh
-   file the number of zones and dimensions from the numerical grid (required
-   for variables allocation)  ---*/
-
-  CConfig *config = nullptr;
-  config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DEF);
-
-  nZone    = config->GetnZone();
-
-  /*--- Definition of the containers per zones ---*/
-
-  config_container = new CConfig*[nZone];
-  geometry_container = new CGeometry*[nZone];
-  surface_movement   = new CSurfaceMovement*[nZone];
-  grid_movement      = new CVolumetricMovement*[nZone];
-  output             = new COutput*[nZone];
-
-  driver_config       = nullptr;
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    config_container[iZone]       = nullptr;
-    geometry_container[iZone]     = nullptr;
-    surface_movement[iZone]       = nullptr;
-    grid_movement[iZone]          = nullptr;
-    output[iZone]                 = nullptr;
-  }
-
-  /*--- Initialize the configuration of the driver ---*/
-  driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DEF, false);
-
-  /*--- Initialize a char to store the zone filename ---*/
-  char zone_file_name[MAX_STRING_SIZE];
-
-  /*--- Loop over all zones to initialize the various classes. In most
-   cases, nZone is equal to one. This represents the solution of a partial
-   differential equation on a single block, unstructured mesh. ---*/
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-
-    /*--- Definition of the configuration option class for all zones. In this
-     constructor, the input configuration file is parsed and all options are
-     read and stored. ---*/
-
-    if (driver_config->GetnConfigFiles() > 0){
-      strcpy(zone_file_name, driver_config->GetConfigFilename(iZone).c_str());
-      config_container[iZone] = new CConfig(driver_config, zone_file_name, SU2_COMPONENT::SU2_DEF, iZone, nZone, true);
-    }
-    else{
-      config_container[iZone] = new CConfig(driver_config, config_file_name, SU2_COMPONENT::SU2_DEF, iZone, nZone, true);
-    }
-    config_container[iZone]->SetMPICommunicator(MPICommunicator);
-  }
-
-  /*--- Set the multizone part of the problem. ---*/
-  if (driver_config->GetMultizone_Problem()){
-    for (iZone = 0; iZone < nZone; iZone++) {
-      /*--- Set the interface markers for multizone ---*/
-      config_container[iZone]->SetMultizone(driver_config, config_container);
-    }
-  }
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-
-    /*--- Definition of the geometry class to store the primal grid in the partitioning process. ---*/
-
-    CGeometry *geometry_aux = nullptr;
-
-    /*--- All ranks process the grid and call ParMETIS for partitioning ---*/
-
-    geometry_aux = new CPhysicalGeometry(config_container[iZone], iZone, nZone);
-
-    /*--- Color the initial grid and set the send-receive domains (ParMETIS) ---*/
-
-    geometry_aux->SetColorGrid_Parallel(config_container[iZone]);
-
-    /*--- Build the grid data structures using the ParMETIS coloring. ---*/
-
-    geometry_container[iZone] = new CPhysicalGeometry(geometry_aux, config_container[iZone]);
-
-    /*--- Deallocate the memory of geometry_aux ---*/
-
-    delete geometry_aux;
-
-    /*--- Add the Send/Receive boundaries ---*/
-
-    geometry_container[iZone]->SetSendReceive(config_container[iZone]);
-
-    /*--- Add the Send/Receive boundaries ---*/
-
-    geometry_container[iZone]->SetBoundaries(config_container[iZone]);
-
-  }
-
-  /*--- Set up a timer for performance benchmarking (preprocessing time is included) ---*/
-
-  StartTime = SU2_MPI::Wtime();
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-
-    /*--- Computational grid preprocesing ---*/
-
-    if (rank == MASTER_NODE) cout << endl << "----------------------- Preprocessing computations ----------------------" << endl;
-
-    /*--- Compute elements surrounding points, points surrounding points ---*/
-
-    if (rank == MASTER_NODE) cout << "Setting local point connectivity." <<endl;
-    geometry_container[iZone]->SetPoint_Connectivity();
-
-    /*--- Check the orientation before computing geometrical quantities ---*/
-
-    geometry_container[iZone]->SetBoundVolume();
-    if (config_container[iZone]->GetReorientElements()) {
-      if (rank == MASTER_NODE) cout << "Checking the numerical grid orientation of the interior elements." <<endl;
-      geometry_container[iZone]->Check_IntElem_Orientation(config_container[iZone]);
-      geometry_container[iZone]->Check_BoundElem_Orientation(config_container[iZone]);
-    }
-
-    /*--- Create the edge structure ---*/
-
-    if (rank == MASTER_NODE) cout << "Identify edges and vertices." <<endl;
-    geometry_container[iZone]->SetEdges();
-    geometry_container[iZone]->SetVertex(config_container[iZone]);
-
-    if (config_container[iZone]->GetDesign_Variable(0) != NO_DEFORMATION) {
-
-      /*--- Create the dual control volume structures ---*/
-
-      if (rank == MASTER_NODE) cout << "Setting the bound control volume structure." << endl;
-      geometry_container[iZone]->SetControlVolume(config_container[iZone], ALLOCATE);
-      geometry_container[iZone]->SetBoundControlVolume(config_container[iZone], ALLOCATE);
-
-    }
-    /*--- Create the point-to-point MPI communication structures. ---*/
-
-    geometry_container[iZone]->PreprocessP2PComms(geometry_container[iZone], config_container[iZone]);
-
-    /*--- Allocate the mesh output ---*/
-
-    output[iZone] = new CMeshOutput(config_container[iZone], geometry_container[iZone]->GetnDim());
-
-    /*--- Preprocess the volume output ---*/
-
-    output[iZone]->PreprocessVolumeOutput(config_container[iZone]);
-
-    /*--- Preprocess history --- */
-
-    output[iZone]->PreprocessHistoryOutput(config_container[iZone], false);
-
-  }
-
-
-  /*--- Surface grid deformation using design variables ---*/
-
-  for (iZone = 0; iZone < nZone; iZone++){
-
-    if (config_container[iZone]->GetDesign_Variable(0) != NO_DEFORMATION) {
-
-      /*--- Definition of the Class for grid movement ---*/
-      grid_movement[iZone] = new CVolumetricMovement(geometry_container[iZone], config_container[iZone]);
-
-      /*--- Save original coordinates to be reused in convexity checking procedure ---*/
-      auto OriginalCoordinates = geometry_container[iZone]->nodes->GetCoord();
-
-      /*--- First check for volumetric grid deformation/transformations ---*/
-
-      if (config_container[iZone]->GetDesign_Variable(0) == SCALE_GRID) {
-
-        if (rank == MASTER_NODE)
-          cout << endl << "--------------------- Volumetric grid scaling (ZONE " << iZone <<") ------------------" << endl;
-        grid_movement[iZone]->SetVolume_Scaling(geometry_container[iZone], config_container[iZone], false);
-
-      } else if (config_container[iZone]->GetDesign_Variable(0) == TRANSLATE_GRID) {
-
-        if (rank == MASTER_NODE)
-          cout << endl << "------------------- Volumetric grid translation (ZONE " << iZone <<") ----------------" << endl;
-        grid_movement[iZone]->SetVolume_Translation(geometry_container[iZone], config_container[iZone], false);
-
-      } else if (config_container[iZone]->GetDesign_Variable(0) == ROTATE_GRID) {
-
-        if (rank == MASTER_NODE)
-          cout << endl << "--------------------- Volumetric grid rotation (ZONE " << iZone <<") -----------------" << endl;
-        grid_movement[iZone]->SetVolume_Rotation(geometry_container[iZone], config_container[iZone], false);
-
-      } else {
-
-        /*--- If no volume-type deformations are requested, then this is a
-         surface-based deformation or FFD set up. ---*/
-
-        if (rank == MASTER_NODE)
-          cout << endl << "--------------------- Surface grid deformation (ZONE " << iZone <<") -----------------" << endl;
-
-        /*--- Definition and initialization of the surface deformation class ---*/
-
-        surface_movement[iZone] = new CSurfaceMovement();
-
-        /*--- Copy coordinates to the surface structure ---*/
-
-        surface_movement[iZone]->CopyBoundary(geometry_container[iZone], config_container[iZone]);
-
-        /*--- Surface grid deformation ---*/
-
-        if (rank == MASTER_NODE) cout << "Performing the deformation of the surface grid." << endl;
-        auto TotalDeformation = surface_movement[iZone]->SetSurface_Deformation(geometry_container[iZone], config_container[iZone]);
-
-        if (config_container[iZone]->GetDesign_Variable(0) != FFD_SETTING) {
-
-          if (rank == MASTER_NODE)
-            cout << endl << "------------------- Volumetric grid deformation (ZONE " << iZone <<") ----------------" << endl;
-
-          if (rank == MASTER_NODE)
-            cout << "Performing the deformation of the volumetric grid." << endl;
-          grid_movement[iZone]->SetVolume_Deformation(geometry_container[iZone], config_container[iZone], false);
-
-          /*--- Get parameters for convexity check ---*/
-          bool ConvexityCheck;
-          unsigned short ConvexityCheck_MaxIter, ConvexityCheck_MaxDepth;
-
-          tie(ConvexityCheck, ConvexityCheck_MaxIter, ConvexityCheck_MaxDepth) = config_container[iZone]->GetConvexityCheck();
-
-          /*--- Recursively change deformations if there are nonconvex elements. ---*/
-
-          if (ConvexityCheck && geometry_container[iZone]->GetnNonconvexElements() > 0) {
-            if (rank == MASTER_NODE) {
-              cout << "Nonconvex elements present after deformation. " << endl;
-              cout << "Recursively lowering deformation magnitude." << endl;
-            }
-
-            /*--- Load initial deformation values ---*/
-            auto InitialDeformation = TotalDeformation;
-
-            unsigned short ConvexityCheckIter, RecursionDepth = 0;
-            su2double DeformationFactor = 1.0, DeformationDifference = 1.0;
-            for (ConvexityCheckIter = 1; ConvexityCheckIter <= ConvexityCheck_MaxIter; ConvexityCheckIter++) {
-
-              /*--- Recursively change deformation magnitude:
-              decrease if there are nonconvex elements, increase otherwise ---*/
-              DeformationDifference /= 2.0;
-
-              if (geometry_container[iZone]->GetnNonconvexElements() > 0) {
-                DeformationFactor -= DeformationDifference;
-              } else {
-                RecursionDepth += 1;
-
-                if (RecursionDepth == ConvexityCheck_MaxDepth) {
-                  if (rank == MASTER_NODE) {
-                    cout << "Maximum recursion depth reached." << endl;
-                    cout << "Remaining amount of original deformation: ";
-                    cout << DeformationFactor*100.0 << " percent. " << endl;
-                  }
-                  break;
-                }
-
-                DeformationFactor += DeformationDifference;
-              }
-
-              /*--- Load mesh to start every iteration with an undeformed grid ---*/
-              for (auto iPoint = 0ul; iPoint < OriginalCoordinates.rows(); iPoint++) {
-                for (auto iDim = 0ul; iDim < OriginalCoordinates.cols(); iDim++) {
-                  geometry_container[iZone]->nodes->SetCoord(iPoint, iDim, OriginalCoordinates(iPoint,iDim));
-                }
-              }
-
-              /*--- Set deformation magnitude as percentage of initial deformation ---*/
-              for (auto iDV = 0u; iDV < config->GetnDV(); iDV++) {
-                for (auto iDV_Value = 0u; iDV_Value < config->GetnDV_Value(iDV); iDV_Value++) {
-                  config_container[iZone]->SetDV_Value(iDV, iDV_Value, InitialDeformation[iDV][iDV_Value]*DeformationFactor);
-                }
-              }
-
-              /*--- Surface grid deformation ---*/
-              if (rank == MASTER_NODE) cout << "Performing the deformation of the surface grid." << endl;
-
-              TotalDeformation = surface_movement[iZone]->SetSurface_Deformation(geometry_container[iZone], config_container[iZone]);
-
-              if (rank == MASTER_NODE)
-                cout << endl << "------------------- Volumetric grid deformation (ZONE " << iZone <<") ----------------" << endl;
-
-              if (rank == MASTER_NODE)
-                cout << "Performing the deformation of the volumetric grid." << endl;
-              grid_movement[iZone]->SetVolume_Deformation(geometry_container[iZone], config_container[iZone], false);
-
-              if (rank == MASTER_NODE) {
-                cout << "Number of nonconvex elements for iteration " << ConvexityCheckIter << ": ";
-                cout << geometry_container[iZone]->GetnNonconvexElements() << endl;
-                cout << "Remaining amount of original deformation: ";
-                cout << DeformationFactor*100.0 << " percent. " << endl;
-              }
-
-            }
-
-          }
-
-        }
-
-      }
-
-    }
-
-  }
-
-  /*--- Computational grid preprocesing ---*/
-
-  if (rank == MASTER_NODE) cout << endl << "----------------------- Write deformed grid files -----------------------" << endl;
-
-  /*--- Output deformed grid for visualization, if requested (surface and volumetric), in parallel
-   requires to move all the data to the master node---*/
-
-  for (iZone = 0; iZone < nZone; iZone++){
-
-    /*--- Compute Mesh Quality if requested. Necessary geometry preprocessing re-done beforehand. ---*/
-
-    if (config_container[iZone]->GetWrt_MeshQuality() && !config->GetStructuralProblem()) {
-
-      if (rank == MASTER_NODE) cout << "Recompute geometry properties necessary to evaluate mesh quality statistics.\n";
-
-      geometry_container[iZone]->SetPoint_Connectivity();
-      geometry_container[iZone]->SetBoundVolume();
-      geometry_container[iZone]->SetEdges();
-      geometry_container[iZone]->SetVertex(config_container[iZone]);
-      geometry_container[iZone]->SetControlVolume(config_container[iZone], ALLOCATE);
-      geometry_container[iZone]->SetBoundControlVolume(config_container[iZone], ALLOCATE);
-
-      if (rank == MASTER_NODE) cout << "Computing mesh quality statistics for the dual control volumes.\n";
-      geometry_container[iZone]->ComputeMeshQualityStatistics(config_container[iZone]);
-    }// Mesh Quality Output
-
-    /*--- Load the data --- */
-
-    output[iZone]->Load_Data(geometry_container[iZone], config_container[iZone], nullptr);
-
-    output[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone], MESH, config->GetMesh_Out_FileName());
-
-    /*--- Set the file names for the visualization files ---*/
-
-    output[iZone]->SetVolume_Filename("volume_deformed");
-    output[iZone]->SetSurface_Filename("surface_deformed");
-
-    for (unsigned short iFile = 0; iFile < config_container[iZone]->GetnVolumeOutputFiles(); iFile++){
-      auto FileFormat = config_container[iZone]->GetVolumeOutputFiles();
-      if (FileFormat[iFile] != RESTART_ASCII && FileFormat[iFile] != RESTART_BINARY)
-        output[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone], FileFormat[iFile]);
-    }
-  }
-
-
-  if ((config_container[ZONE_0]->GetDesign_Variable(0) != NO_DEFORMATION) &&
-      (config_container[ZONE_0]->GetDesign_Variable(0) != SCALE_GRID)     &&
-      (config_container[ZONE_0]->GetDesign_Variable(0) != TRANSLATE_GRID) &&
-      (config_container[ZONE_0]->GetDesign_Variable(0) != ROTATE_GRID)) {
-
-    /*--- Write the the free-form deformation boxes after deformation. ---*/
-
-    if (rank == MASTER_NODE) cout << "Adding any FFD information to the SU2 file." << endl;
-
-    surface_movement[ZONE_0]->WriteFFDInfo(surface_movement, geometry_container, config_container);
-
-  }
-
-  delete config;
-  config = nullptr;
-  if (rank == MASTER_NODE)
-    cout << endl <<"------------------------- Solver Postprocessing -------------------------" << endl;
-
-  if (geometry_container != nullptr) {
-    for (iZone = 0; iZone < nZone; iZone++) {
-      if (geometry_container[iZone] != nullptr) {
-        delete geometry_container[iZone];
-      }
-    }
-    delete [] geometry_container;
-  }
-  if (rank == MASTER_NODE) cout << "Deleted CGeometry container." << endl;
-
-  if (surface_movement != nullptr) {
-    for (iZone = 0; iZone < nZone; iZone++) {
-      if (surface_movement[iZone] != nullptr) {
-        delete surface_movement[iZone];
-      }
-    }
-    delete [] surface_movement;
-  }
-  if (rank == MASTER_NODE) cout << "Deleted CSurfaceMovement class." << endl;
-
-  if (grid_movement != nullptr) {
-    for (iZone = 0; iZone < nZone; iZone++) {
-      if (grid_movement[iZone] != nullptr) {
-        delete grid_movement[iZone];
-      }
-    }
-    delete [] grid_movement;
-  }
-  if (rank == MASTER_NODE) cout << "Deleted CVolumetricMovement class." << endl;
-
-  if (config_container != nullptr) {
-    for (iZone = 0; iZone < nZone; iZone++) {
-      if (config_container[iZone] != nullptr) {
-        delete config_container[iZone];
-      }
-    }
-    delete [] config_container;
-  }
-  if (output != nullptr) {
-    for (iZone = 0; iZone < nZone; iZone++) {
-      if (output[iZone] != nullptr) {
-        delete output[iZone];
-      }
-    }
-    delete [] output;
-  }
-  if (rank == MASTER_NODE) cout << "Deleted CConfig container." << endl;
-
-  if (rank == MASTER_NODE) cout << "Deleted COutput class." << endl;
-
-  /*--- Synchronization point after a single solver iteration. Compute the
-   wall clock time required. ---*/
+  /*--- Initialize the mesh deformation driver ---*/
+  driver = new CDeformationDriver(config_file_name, comm);
 
-  StopTime = SU2_MPI::Wtime();
+  /*--- Launch the main external loop of the solver. ---*/
 
-  /*--- Compute/print the total time for performance benchmarking. ---*/
+  driver->Run();
 
-  UsedTime = StopTime-StartTime;
-  if (rank == MASTER_NODE) {
-    cout << "\nCompleted in " << fixed << UsedTime << " seconds on "<< size;
-    if (size == 1) cout << " core." << endl; else cout << " cores." << endl;
-  }
+  /*--- Postprocess all the containers, close history file, exit SU2. ---*/
 
-  /*--- Exit the solver cleanly ---*/
+  driver->Postprocessing();
 
-  if (rank == MASTER_NODE)
-    cout << endl << "------------------------- Exit Success (SU2_DEF) ------------------------" << endl << endl;
+  delete driver;
 
   /*--- Finalize MPI parallelization ---*/
   SU2_MPI::Finalize();
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 529085f87e6..9ceb6b65fc5 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -28,9 +28,6 @@
 
 #include "../../include/drivers/CDeformationDriver.hpp"
 #include "../../../Common/include/geometry/CPhysicalGeometry.hpp"
-#include "../../../Common/include/grid_movement/CSurfaceMovement.hpp"
-#include "../../../Common/include/grid_movement/CVolumetricMovement.hpp"
-#include "../../../SU2_CFD/include/output/COutput.hpp"
 #include "../../../SU2_CFD/include/output/CMeshOutput.hpp"
 using namespace std;
 
@@ -43,183 +40,202 @@ CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
     #endif
   #endif
 
-    SU2_MPI::SetComm(MPICommunicator);
+  SU2_MPI::SetComm(MPICommunicator);
+
+  rank = SU2_MPI::GetRank();
+  size = SU2_MPI::GetSize();
 
   /*--- Copy the config filename ---*/
   strcpy(config_file_name, confFile);
-}
 
-CDeformationDriver::~CDeformationDriver(void) {
+  /*--- Initialize the configuration of the driver ---*/
+  driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DEF, false);
 
-}
+  nZone    = driver_config->GetnZone();
+
+  /*--- Initialize containers --- */
+
+  SetContainers_Null();
+
+  /*--- Preprocessing of the config files. ---*/
 
-void CDeformationDriver::RunSolver() {
+  Input_Preprocessing();
 
-    unsigned short iZone, nZone = SINGLE_ZONE;
-    su2double StartTime = 0.0, StopTime = 0.0, UsedTime = 0.0;
-    string str;
+  /*--- Set up a timer for performance benchmarking ---*/
 
-    int rank = SU2_MPI::GetRank();
-    int size = SU2_MPI::GetSize();
+  StartTime = SU2_MPI::Wtime();
 
-    /*--- Pointer to different structures that will be used throughout
-     the entire code ---*/
+  for (iZone = 0; iZone < nZone; iZone++) {
 
-    CConfig **config_container          = nullptr;
-    CGeometry **geometry_container      = nullptr;
-    CSurfaceMovement **surface_movement = nullptr;
-    CVolumetricMovement **grid_movement = nullptr;
-    COutput **output                    = nullptr;
-    CConfig *driver_config              = nullptr;
+    /*--- Preprocessing of the geometry for all zones. ---*/
 
-    /*--- Read the name and format of the input mesh file to get from the mesh
-     file the number of zones and dimensions from the numerical grid (required
-     for variables allocation)  ---*/
+    Geometrical_Preprocessing(config_container[iZone], geometry_container[iZone]);
 
-    CConfig *config = nullptr;
-    config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DEF);
+    /*--- Preprocessing of the output for all zones. ---*/
 
-    nZone    = config->GetnZone();
+    Output_Preprocessing(config_container[iZone], geometry_container[iZone], output_container[iZone]);
 
-    /*--- Definition of the containers per zones ---*/
+  }
+
+  /*--- Preprocessing time is reported now, but not included in the next compute portion. ---*/
+
+  StopTime = SU2_MPI::Wtime();
+
+  /*--- Compute/print the total time for performance benchmarking. ---*/
+
+  UsedTime = StopTime-StartTime;
+  UsedTimePreproc    = UsedTime;
+  UsedTimeCompute    = 0.0;
+
+}
 
+CDeformationDriver::~CDeformationDriver(void) {
+
+}
+
+void CDeformationDriver::SetContainers_Null() {
+
+    /*--- Create pointers to all of the classes that may be used throughout
+        the SU2_DEF code. In general, the pointers are instantiated down a
+        hierarchy over all zones as described in the comments below. ---*/
     config_container   = new CConfig*[nZone];
     geometry_container = new CGeometry*[nZone];
     surface_movement   = new CSurfaceMovement*[nZone];
     grid_movement      = new CVolumetricMovement*[nZone];
-    output             = new COutput*[nZone];
-
-    driver_config       = nullptr;
+    output_container   = new COutput*[nZone];
 
     for (iZone = 0; iZone < nZone; iZone++) {
-      config_container[iZone]       = nullptr;
-      geometry_container[iZone]     = nullptr;
-      surface_movement[iZone]       = nullptr;
-      grid_movement[iZone]          = nullptr;
-      output[iZone]                 = nullptr;
+        config_container[iZone]       = nullptr;
+        geometry_container[iZone]     = nullptr;
+        surface_movement[iZone]       = nullptr;
+        grid_movement[iZone]          = nullptr;
+        output_container[iZone]       = nullptr;
     }
+}
 
-    /*--- Initialize the configuration of the driver ---*/
-    driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DEF, false);
+void CDeformationDriver::Input_Preprocessing() {
 
     /*--- Initialize a char to store the zone filename ---*/
     char zone_file_name[MAX_STRING_SIZE];
 
     /*--- Loop over all zones to initialize the various classes. In most
-     cases, nZone is equal to one. This represents the solution of a partial
-     differential equation on a single block, unstructured mesh. ---*/
+       cases, nZone is equal to one. This represents the solution of a partial
+       differential equation on a single block, unstructured mesh. ---*/
 
     for (iZone = 0; iZone < nZone; iZone++) {
 
-      /*--- Definition of the configuration option class for all zones. In this
-       constructor, the input configuration file is parsed and all options are
-       read and stored. ---*/
+    /*--- Definition of the configuration option class for all zones. In this
+          constructor, the input configuration file is parsed and all options are
+          read and stored. ---*/
 
-      if (driver_config->GetnConfigFiles() > 0){
-        strcpy(zone_file_name, driver_config->GetConfigFilename(iZone).c_str());
-        config_container[iZone] = new CConfig(driver_config, zone_file_name, SU2_COMPONENT::SU2_DEF, iZone, nZone, true);
-      }
-      else{
-        config_container[iZone] = new CConfig(driver_config, config_file_name, SU2_COMPONENT::SU2_DEF, iZone, nZone, true);
-      }
-      config_container[iZone]->SetMPICommunicator(SU2_MPI::GetComm());
+        if (driver_config->GetnConfigFiles() > 0){
+            strcpy(zone_file_name, driver_config->GetConfigFilename(iZone).c_str());
+            config_container[iZone] = new CConfig(driver_config, zone_file_name, SU2_COMPONENT::SU2_DEF, iZone, nZone, true);
+        } else {
+            config_container[iZone] = new CConfig(driver_config, config_file_name, SU2_COMPONENT::SU2_DEF, iZone, nZone, true);
+        }
+
+        config_container[iZone]->SetMPICommunicator(SU2_MPI::GetComm());
     }
 
-    /*--- Set the multizone part of the problem. ---*/
+      /*--- Set the multizone part of the problem. ---*/
     if (driver_config->GetMultizone_Problem()){
-      for (iZone = 0; iZone < nZone; iZone++) {
-        /*--- Set the interface markers for multizone ---*/
-        config_container[iZone]->SetMultizone(driver_config, config_container);
-      }
+        for (iZone = 0; iZone < nZone; iZone++) {
+            /*--- Set the interface markers for multizone ---*/
+            config_container[iZone]->SetMultizone(driver_config, config_container);
+        }
     }
+}
 
-    for (iZone = 0; iZone < nZone; iZone++) {
+void CDeformationDriver::Geometrical_Preprocessing(CConfig *config, CGeometry *&geometry) {
 
-      /*--- Definition of the geometry class to store the primal grid in the partitioning process. ---*/
+    /*--- Definition of the geometry class to store the primal grid in the partitioning process. ---*/
 
-      CGeometry *geometry_aux = nullptr;
+    CGeometry *geometry_aux = nullptr;
 
-      /*--- All ranks process the grid and call ParMETIS for partitioning ---*/
+    /*--- All ranks process the grid and call ParMETIS for partitioning ---*/
 
-      geometry_aux = new CPhysicalGeometry(config_container[iZone], iZone, nZone);
+    geometry_aux = new CPhysicalGeometry(config, iZone, nZone);
 
-      /*--- Color the initial grid and set the send-receive domains (ParMETIS) ---*/
+    /*--- Color the initial grid and set the send-receive domains (ParMETIS) ---*/
 
-      geometry_aux->SetColorGrid_Parallel(config_container[iZone]);
+    geometry_aux->SetColorGrid_Parallel(config);
 
-      /*--- Build the grid data structures using the ParMETIS coloring. ---*/
+    /*--- Build the grid data structures using the ParMETIS coloring. ---*/
 
-      geometry_container[iZone] = new CPhysicalGeometry(geometry_aux, config_container[iZone]);
+    geometry = new CPhysicalGeometry(geometry_aux, config);
 
-      /*--- Deallocate the memory of geometry_aux ---*/
+    /*--- Deallocate the memory of geometry_aux ---*/
 
-      delete geometry_aux;
+    delete geometry_aux;
 
-      /*--- Add the Send/Receive boundaries ---*/
+    /*--- Add the Send/Receive boundaries ---*/
 
-      geometry_container[iZone]->SetSendReceive(config_container[iZone]);
+    geometry->SetSendReceive(config);
 
-      /*--- Add the Send/Receive boundaries ---*/
+    /*--- Add the Send/Receive boundaries ---*/
 
-      geometry_container[iZone]->SetBoundaries(config_container[iZone]);
+    geometry->SetBoundaries(config);
 
-    }
+    /*--- Computational grid preprocesing ---*/
 
-    /*--- Set up a timer for performance benchmarking (preprocessing time is included) ---*/
+    if (rank == MASTER_NODE) cout << endl << "----------------------- Preprocessing computations ----------------------" << endl;
 
-    StartTime = SU2_MPI::Wtime();
+    /*--- Compute elements surrounding points, points surrounding points ---*/
 
-    for (iZone = 0; iZone < nZone; iZone++) {
+    if (rank == MASTER_NODE) cout << "Setting local point connectivity." <<endl;
+    geometry->SetPoint_Connectivity();
 
-      /*--- Computational grid preprocesing ---*/
+    /*--- Check the orientation before computing geometrical quantities ---*/
 
-      if (rank == MASTER_NODE) cout << endl << "----------------------- Preprocessing computations ----------------------" << endl;
+    geometry->SetBoundVolume();
+    if (config->GetReorientElements()) {
+    if (rank == MASTER_NODE) cout << "Checking the numerical grid orientation of the interior elements." <<endl;
+        geometry->Check_IntElem_Orientation(config);
+        geometry->Check_BoundElem_Orientation(config);
+    }
 
-      /*--- Compute elements surrounding points, points surrounding points ---*/
+    /*--- Create the edge structure ---*/
 
-      if (rank == MASTER_NODE) cout << "Setting local point connectivity." <<endl;
-      geometry_container[iZone]->SetPoint_Connectivity();
+    if (rank == MASTER_NODE) cout << "Identify edges and vertices." <<endl;
+    geometry->SetEdges();
+    geometry->SetVertex(config);
 
-      /*--- Check the orientation before computing geometrical quantities ---*/
+    if (config->GetDesign_Variable(0) != NO_DEFORMATION) {
 
-      geometry_container[iZone]->SetBoundVolume();
-      if (config_container[iZone]->GetReorientElements()) {
-        if (rank == MASTER_NODE) cout << "Checking the numerical grid orientation of the interior elements." <<endl;
-        geometry_container[iZone]->Check_IntElem_Orientation(config_container[iZone]);
-        geometry_container[iZone]->Check_BoundElem_Orientation(config_container[iZone]);
-      }
+        /*--- Create the dual control volume structures ---*/
 
-      /*--- Create the edge structure ---*/
+        if (rank == MASTER_NODE) cout << "Setting the bound control volume structure." << endl;
+        geometry->SetControlVolume(config, ALLOCATE);
+        geometry->SetBoundControlVolume(config, ALLOCATE);
+    }
 
-      if (rank == MASTER_NODE) cout << "Identify edges and vertices." <<endl;
-      geometry_container[iZone]->SetEdges();
-      geometry_container[iZone]->SetVertex(config_container[iZone]);
+    /*--- Create the point-to-point MPI communication structures. ---*/
 
-      if (config_container[iZone]->GetDesign_Variable(0) != NO_DEFORMATION) {
+    geometry->PreprocessP2PComms(geometry, config);
 
-        /*--- Create the dual control volume structures ---*/
+}
 
-        if (rank == MASTER_NODE) cout << "Setting the bound control volume structure." << endl;
-        geometry_container[iZone]->SetControlVolume(config_container[iZone], ALLOCATE);
-        geometry_container[iZone]->SetBoundControlVolume(config_container[iZone], ALLOCATE);
+void CDeformationDriver::Output_Preprocessing(CConfig *config, CGeometry *geometry, COutput *&output) {
 
-      }
-      /*--- Create the point-to-point MPI communication structures. ---*/
+        /*--- Allocate the mesh output ---*/
 
-      geometry_container[iZone]->PreprocessP2PComms(geometry_container[iZone], config_container[iZone]);
+        output = new CMeshOutput(config, geometry->GetnDim());
 
-      /*--- Allocate the mesh output ---*/
+        /*--- Preprocess the volume output ---*/
 
-      output[iZone] = new CMeshOutput(config_container[iZone], geometry_container[iZone]->GetnDim());
+        output->PreprocessVolumeOutput(config);
 
-      /*--- Preprocess the volume output ---*/
+        /*--- Preprocess history --- */
 
-      output[iZone]->PreprocessVolumeOutput(config_container[iZone]);
+        output->PreprocessHistoryOutput(config, false);
+}
 
-      /*--- Preprocess history --- */
+void CDeformationDriver::Run() {
 
-      output[iZone]->PreprocessHistoryOutput(config_container[iZone], false);
-    }
+    /* --- Start measuring computation time ---*/
+
+    StartTime = SU2_MPI::Wtime();
 
     /*--- Surface grid deformation using design variables ---*/
 
@@ -333,8 +349,8 @@ void CDeformationDriver::RunSolver() {
                 }
 
                 /*--- Set deformation magnitude as percentage of initial deformation ---*/
-                for (auto iDV = 0u; iDV < config->GetnDV(); iDV++) {
-                  for (auto iDV_Value = 0u; iDV_Value < config->GetnDV_Value(iDV); iDV_Value++) {
+                for (auto iDV = 0u; iDV < driver_config->GetnDV(); iDV++) {
+                  for (auto iDV_Value = 0u; iDV_Value < driver_config->GetnDV_Value(iDV); iDV_Value++) {
                     config_container[iZone]->SetDV_Value(iDV, iDV_Value, InitialDeformation[iDV][iDV_Value]*DeformationFactor);
                   }
                 }
@@ -381,7 +397,7 @@ void CDeformationDriver::RunSolver() {
 
       /*--- Compute Mesh Quality if requested. Necessary geometry preprocessing re-done beforehand. ---*/
 
-      if (config_container[iZone]->GetWrt_MeshQuality() && !config->GetStructuralProblem()) {
+      if (config_container[iZone]->GetWrt_MeshQuality() && !driver_config->GetStructuralProblem()) {
 
         if (rank == MASTER_NODE) cout << "Recompute geometry properties necessary to evaluate mesh quality statistics.\n";
 
@@ -398,19 +414,19 @@ void CDeformationDriver::RunSolver() {
 
       /*--- Load the data --- */
 
-      output[iZone]->Load_Data(geometry_container[iZone], config_container[iZone], nullptr);
+      output_container[iZone]->Load_Data(geometry_container[iZone], config_container[iZone], nullptr);
 
-      output[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone], MESH, config->GetMesh_Out_FileName());
+      output_container[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone], MESH, driver_config->GetMesh_Out_FileName());
 
       /*--- Set the file names for the visualization files ---*/
 
-      output[iZone]->SetVolume_Filename("volume_deformed");
-      output[iZone]->SetSurface_Filename("surface_deformed");
+      output_container[iZone]->SetVolume_Filename("volume_deformed");
+      output_container[iZone]->SetSurface_Filename("surface_deformed");
 
       for (unsigned short iFile = 0; iFile < config_container[iZone]->GetnVolumeOutputFiles(); iFile++){
         auto FileFormat = config_container[iZone]->GetVolumeOutputFiles();
         if (FileFormat[iFile] != RESTART_ASCII && FileFormat[iFile] != RESTART_BINARY)
-          output[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone], FileFormat[iFile]);
+          output_container[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone], FileFormat[iFile]);
       }
     }
 
@@ -427,12 +443,15 @@ void CDeformationDriver::RunSolver() {
       surface_movement[ZONE_0]->WriteFFDInfo(surface_movement, geometry_container, config_container);
 
     }
+}
 
-    delete config;
-    config = nullptr;
+void CDeformationDriver::Postprocessing() {
     if (rank == MASTER_NODE)
       cout << endl <<"------------------------- Solver Postprocessing -------------------------" << endl;
 
+    delete driver_config;
+    driver_config = nullptr;
+
     if (geometry_container != nullptr) {
       for (iZone = 0; iZone < nZone; iZone++) {
         if (geometry_container[iZone] != nullptr) {
@@ -471,13 +490,13 @@ void CDeformationDriver::RunSolver() {
       }
       delete [] config_container;
     }
-    if (output != nullptr) {
+    if (output_container != nullptr) {
       for (iZone = 0; iZone < nZone; iZone++) {
-        if (output[iZone] != nullptr) {
-          delete output[iZone];
+        if (output_container[iZone] != nullptr) {
+          delete output_container[iZone];
         }
       }
-      delete [] output;
+      delete [] output_container;
     }
     if (rank == MASTER_NODE) cout << "Deleted CConfig container." << endl;
 
@@ -488,11 +507,9 @@ void CDeformationDriver::RunSolver() {
 
     StopTime = SU2_MPI::Wtime();
 
-    /*--- Compute/print the total time for performance benchmarking. ---*/
-
-    UsedTime = StopTime-StartTime;
+    UsedTimeCompute = StopTime-StartTime;
     if (rank == MASTER_NODE) {
-      cout << "\nCompleted in " << fixed << UsedTime << " seconds on "<< size;
+      cout << "\nCompleted in " << fixed << UsedTimeCompute << " seconds on "<< size;
       if (size == 1) cout << " core." << endl; else cout << " cores." << endl;
     }
 

From b9838977be491aa8b529b69b6d7839f5db980a83 Mon Sep 17 00:00:00 2001
From: aa-g <aa.gastaldi@pm.me>
Date: Wed, 26 May 2021 01:17:28 +0200
Subject: [PATCH 004/656] Minor fixes in CDeformationDriver

---
 .../include/drivers/CDeformationDriver.hpp    | 11 ++----
 SU2_DEF/src/drivers/CDeformationDriver.cpp    | 38 ++++++++++---------
 2 files changed, 24 insertions(+), 25 deletions(-)

diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index b76a2919976..905cdf106c6 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -1,7 +1,6 @@
 /*!
  * \file CDeformationDriver.hpp
- * \brief Headers of the main subroutines for driving single or multi-zone problems.
- *        The subroutines and functions are in the <i>driver_structure.cpp</i> file.
+ * \brief Headers of the main subroutines for driving the mesh deformation.
  * \author T. Economon, H. Kline, R. Sanchez
  * \version 7.1.1 "Blackbird"
  *
@@ -37,8 +36,8 @@
 
 /*!
  * \class CDeformationDriver
- * \brief Class for driving single-zone solvers.
- * \author R. Sanchez
+ * \brief Class for driving mesh deformation solvers.
+ * \author A. Gastaldi, H. Patel
  * \version 7.1.1 "Blackbird"
  */
 class CDeformationDriver {
@@ -58,7 +57,6 @@ class CDeformationDriver {
   CSurfaceMovement **surface_movement;          /*!< \brief Surface movement classes of the problem. */
   CVolumetricMovement **grid_movement;         /*!< \brief Volume grid movement classes of the problem. */
   COutput **output_container;                   /*!< \brief Pointer to the COutput class. */
-                   /*!< \brief FFD FFDBoxes of the problem. */
 
 public:
   /*!
@@ -66,8 +64,7 @@ class CDeformationDriver {
    * \param[in] confFile - Configuration file name.
    * \param[in] MPICommunicator - MPI communicator for SU2.
    */
-  CDeformationDriver(char* confFile,
-             SU2_Comm MPICommunicator);
+  CDeformationDriver(char* confFile, SU2_Comm MPICommunicator);
 
   /*!
    * \brief Destructor of the class.
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 9ceb6b65fc5..eb4524c6376 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -1,7 +1,7 @@
 /*!
- * \file SU2_DEF.cpp
- * \brief Main file of Mesh Deformation Code (SU2_DEF).
- * \author F. Palacios, T. Economon
+ * \file CDeformationDriver.hpp
+ * \brief Main subroutines for driving the mesh deformation.
+ * \author T. Economon, H. Kline, R. Sanchez
  * \version 7.1.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
@@ -27,8 +27,10 @@
 
 
 #include "../../include/drivers/CDeformationDriver.hpp"
+
 #include "../../../Common/include/geometry/CPhysicalGeometry.hpp"
 #include "../../../SU2_CFD/include/output/CMeshOutput.hpp"
+
 using namespace std;
 
 CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator) {
@@ -49,9 +51,10 @@ CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
   strcpy(config_file_name, confFile);
 
   /*--- Initialize the configuration of the driver ---*/
-  driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DEF, false);
+  driver_config = nullptr;
+  driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DEF);
 
-  nZone    = driver_config->GetnZone();
+  nZone = driver_config->GetnZone();
 
   /*--- Initialize containers --- */
 
@@ -430,7 +433,6 @@ void CDeformationDriver::Run() {
       }
     }
 
-
     if ((config_container[ZONE_0]->GetDesign_Variable(0) != NO_DEFORMATION) &&
         (config_container[ZONE_0]->GetDesign_Variable(0) != SCALE_GRID)     &&
         (config_container[ZONE_0]->GetDesign_Variable(0) != TRANSLATE_GRID) &&
@@ -443,6 +445,17 @@ void CDeformationDriver::Run() {
       surface_movement[ZONE_0]->WriteFFDInfo(surface_movement, geometry_container, config_container);
 
     }
+
+    /*--- Synchronization point after a single solver iteration. Compute the
+      wall clock time required. ---*/
+
+    StopTime = SU2_MPI::Wtime();
+
+    UsedTimeCompute = StopTime-StartTime;
+    if (rank == MASTER_NODE) {
+      cout << "\nCompleted in " << fixed << UsedTimeCompute << " seconds on "<< size;
+      if (size == 1) cout << " core." << endl; else cout << " cores." << endl;
+    }
 }
 
 void CDeformationDriver::Postprocessing() {
@@ -502,19 +515,8 @@ void CDeformationDriver::Postprocessing() {
 
     if (rank == MASTER_NODE) cout << "Deleted COutput class." << endl;
 
-    /*--- Synchronization point after a single solver iteration. Compute the
-     wall clock time required. ---*/
-
-    StopTime = SU2_MPI::Wtime();
-
-    UsedTimeCompute = StopTime-StartTime;
-    if (rank == MASTER_NODE) {
-      cout << "\nCompleted in " << fixed << UsedTimeCompute << " seconds on "<< size;
-      if (size == 1) cout << " core." << endl; else cout << " cores." << endl;
-    }
-
     /*--- Exit the solver cleanly ---*/
 
     if (rank == MASTER_NODE)
       cout << endl << "------------------------- Exit Success (SU2_DEF) ------------------------" << endl << endl;
-  }
+}

From 6facf5b1fe5b49b9f97430ee1f46f3ed978d4cd4 Mon Sep 17 00:00:00 2001
From: aa-g <aa.gastaldi@pm.me>
Date: Tue, 1 Jun 2021 21:36:01 +0200
Subject: [PATCH 005/656] Add CDiscAdjDeformationDriver

---
 .../include/drivers/CDeformationDriver.hpp    |   4 +-
 .../drivers/CDiscAdjDeformationDriver.hpp     | 155 +++
 SU2_DEF/src/drivers/CDeformationDriver.cpp    |  61 +-
 .../src/drivers/CDiscAdjDeformationDriver.cpp | 945 ++++++++++++++++++
 SU2_DEF/src/meson.build                       |  44 +-
 SU2_DOT/src/meson.build                       |   9 +-
 SU2_PY/pySU2/meson.build                      |  10 +-
 SU2_PY/pySU2/pySU2ad.i                        |   2 +
 8 files changed, 1192 insertions(+), 38 deletions(-)
 create mode 100644 SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
 create mode 100644 SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp

diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index 905cdf106c6..8a424ff32fd 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -95,11 +95,11 @@ class CDeformationDriver {
   /*!
    * \brief Construction of the edge-based data structure.
    */
-  void Geometrical_Preprocessing(CConfig *config, CGeometry *&geometry);
+  void Geometrical_Preprocessing();
 
   /*!
    * \brief Preprocess the output container.
    */
-  void Output_Preprocessing(CConfig *config, CGeometry *geometry, COutput *&output);
+  void Output_Preprocessing();
 
 };
diff --git a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
new file mode 100644
index 00000000000..f3635ab694b
--- /dev/null
+++ b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
@@ -0,0 +1,155 @@
+/*!
+* \file CDiscAdjDeformationDriver.cpp
+* \brief Main subroutines for driving the projection of sensitivities.
+ * \author T. Economon, H. Kline, R. Sanchez
+ * \version 7.1.1 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2021, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+
+#pragma once
+
+#define ENABLE_MAPS
+#include "../../../Common/include/CConfig.hpp"
+#undef ENABLE_MAPS
+
+#include "../../../Common/include/parallelization/mpi_structure.hpp"
+
+#include "../../../Common/include/geometry/CGeometry.hpp"
+#include "../../../Common/include/fem/fem_geometry_structure.hpp"
+#include "../../../Common/include/grid_movement/CSurfaceMovement.hpp"
+#include "../../../Common/include/grid_movement/CVolumetricMovement.hpp"
+#include "../../../SU2_CFD/include/output/COutput.hpp"
+#include "../../../SU2_CFD/include/output/CBaselineOutput.hpp"
+#include "../../../SU2_CFD/include/solvers/CBaselineSolver.hpp"
+
+/*!
+ * \class CDiscAdjDeformationDriver
+ * \brief Class for driving sensitivity DiscAdjDeformations.
+ * \author A. Gastaldi, H. Patel
+ * \version 7.1.1 "Blackbird"
+ */
+class CDiscAdjDeformationDriver {
+protected:
+  char config_file_name[MAX_STRING_SIZE];
+  int rank,
+      size;
+  unsigned short iZone, nZone = SINGLE_ZONE;
+  unsigned short iInst;
+  unsigned short* nInst;
+  su2double StartTime,                          /*!< \brief Start point of the timer for performance benchmarking.*/
+            StopTime,                           /*!< \brief Stop point of the timer for performance benchmarking.*/
+            UsedTimePreproc,                    /*!< \brief Elapsed time between Start and Stop point of the timer for tracking preprocessing phase.*/
+            UsedTimeCompute,                    /*!< \brief Elapsed time between Start and Stop point of the timer for tracking compute phase.*/
+            UsedTime;                           /*!< \brief Elapsed time between Start and Stop point of the timer.*/
+  su2double** Gradient;
+  ofstream Gradient_file;
+  CConfig *driver_config;                       /*!< \brief Definition of the driver configuration. */
+  CConfig **config_container;                   /*!< \brief Definition of the particular problem. */
+  CGeometry ***geometry_container;             /*!< \brief Geometrical definition of the problem. */
+  CSurfaceMovement **surface_movement;
+  CVolumetricMovement **grid_movement;
+  COutput **output_container;                   /*!< \brief Pointer to the COutput class. */
+
+public:
+  /*!
+   * \brief Constructor of the class.
+   * \param[in] confFile - Configuration file name.
+   * \param[in] MPICommunicator - MPI communicator for SU2.
+   */
+  CDiscAdjDeformationDriver(char* confFile, SU2_Comm MPICommunicator);
+
+  /*!
+   * \brief Destructor of the class.
+   */
+  ~CDiscAdjDeformationDriver(void);
+
+  /*!
+   * \brief [Overload] Launch the computation for single-zone problems.
+   */
+  void Run();
+
+  /*!
+   * \brief Deallocation routine
+   */
+  void Postprocessing();
+
+protected:
+  /*!
+   * \brief Init_Containers
+   */
+  void SetContainers_Null();
+
+  /*!
+   * \brief Read in the config and mesh files.
+   */
+  void Input_Preprocessing();
+
+  /*!
+   * \brief Construction of the edge-based data structure.
+   */
+  void Geometrical_Preprocessing();
+
+  /*!
+   * \brief Preprocess the output container.
+   */
+  void Output_Preprocessing();
+
+  /*!
+   * \brief DiscAdjDeformation of the surface sensitivity using finite differences (FD).
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] surface_movement - Surface movement class of the problem.
+   * \param[in] Gradient_file - Output file to store the gradient data.
+   */
+
+  void SetDiscAdjDeformation_FD(CGeometry *geometry, CConfig *config, CSurfaceMovement *surface_movement, su2double **Gradient);
+
+  /*!
+   * \brief DiscAdjDeformation of the surface sensitivity using algorithmic differentiation (AD).
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] surface_movement - Surface movement class of the problem.
+   * \param[in] Gradient_file - Output file to store the gradient data.
+   */
+
+  void SetDiscAdjDeformation_AD(CGeometry *geometry, CConfig *config, CSurfaceMovement *surface_movement, su2double **Gradient);
+
+  /*!
+   * \brief Prints the gradient information to a file.
+   * \param[in] Gradient - The gradient data.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] Gradient_file - Output file to store the gradient data.
+   */
+
+  void OutputGradient(su2double** Gradient, CConfig* config, ofstream& Gradient_file);
+
+  /*!
+   * \brief Write the sensitivity (including mesh sensitivity) computed with the discrete adjoint method
+   *  on the surface and in the volume to a file.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] val_nZone - Number of Zones.
+   */
+
+  void SetSensitivity_Files(CGeometry ***geometry, CConfig **config, unsigned short val_nZone);
+
+};
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index eb4524c6376..b12d24154a9 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -68,17 +68,13 @@ CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
 
   StartTime = SU2_MPI::Wtime();
 
-  for (iZone = 0; iZone < nZone; iZone++) {
+  /*--- Preprocessing of the geometry for all zones. ---*/
 
-    /*--- Preprocessing of the geometry for all zones. ---*/
+  Geometrical_Preprocessing();
 
-    Geometrical_Preprocessing(config_container[iZone], geometry_container[iZone]);
+  /*--- Preprocessing of the output for all zones. ---*/
 
-    /*--- Preprocessing of the output for all zones. ---*/
-
-    Output_Preprocessing(config_container[iZone], geometry_container[iZone], output_container[iZone]);
-
-  }
+  Output_Preprocessing();
 
   /*--- Preprocessing time is reported now, but not included in the next compute portion. ---*/
 
@@ -150,7 +146,9 @@ void CDeformationDriver::Input_Preprocessing() {
     }
 }
 
-void CDeformationDriver::Geometrical_Preprocessing(CConfig *config, CGeometry *&geometry) {
+void CDeformationDriver::Geometrical_Preprocessing() {
+
+    for (iZone = 0; iZone < nZone; iZone++) {
 
     /*--- Definition of the geometry class to store the primal grid in the partitioning process. ---*/
 
@@ -158,15 +156,15 @@ void CDeformationDriver::Geometrical_Preprocessing(CConfig *config, CGeometry *&
 
     /*--- All ranks process the grid and call ParMETIS for partitioning ---*/
 
-    geometry_aux = new CPhysicalGeometry(config, iZone, nZone);
+    geometry_aux = new CPhysicalGeometry(config_container[iZone], iZone, nZone);
 
     /*--- Color the initial grid and set the send-receive domains (ParMETIS) ---*/
 
-    geometry_aux->SetColorGrid_Parallel(config);
+    geometry_aux->SetColorGrid_Parallel(config_container[iZone]);
 
     /*--- Build the grid data structures using the ParMETIS coloring. ---*/
 
-    geometry = new CPhysicalGeometry(geometry_aux, config);
+    geometry_container[iZone] = new CPhysicalGeometry(geometry_aux, config_container[iZone]);
 
     /*--- Deallocate the memory of geometry_aux ---*/
 
@@ -174,11 +172,11 @@ void CDeformationDriver::Geometrical_Preprocessing(CConfig *config, CGeometry *&
 
     /*--- Add the Send/Receive boundaries ---*/
 
-    geometry->SetSendReceive(config);
+    geometry_container[iZone]->SetSendReceive(config_container[iZone]);
 
     /*--- Add the Send/Receive boundaries ---*/
 
-    geometry->SetBoundaries(config);
+    geometry_container[iZone]->SetBoundaries(config_container[iZone]);
 
     /*--- Computational grid preprocesing ---*/
 
@@ -187,51 +185,56 @@ void CDeformationDriver::Geometrical_Preprocessing(CConfig *config, CGeometry *&
     /*--- Compute elements surrounding points, points surrounding points ---*/
 
     if (rank == MASTER_NODE) cout << "Setting local point connectivity." <<endl;
-    geometry->SetPoint_Connectivity();
+    geometry_container[iZone]->SetPoint_Connectivity();
 
     /*--- Check the orientation before computing geometrical quantities ---*/
 
-    geometry->SetBoundVolume();
-    if (config->GetReorientElements()) {
+    geometry_container[iZone]->SetBoundVolume();
+    if (config_container[iZone]->GetReorientElements()) {
     if (rank == MASTER_NODE) cout << "Checking the numerical grid orientation of the interior elements." <<endl;
-        geometry->Check_IntElem_Orientation(config);
-        geometry->Check_BoundElem_Orientation(config);
+        geometry_container[iZone]->Check_IntElem_Orientation(config_container[iZone]);
+        geometry_container[iZone]->Check_BoundElem_Orientation(config_container[iZone]);
     }
 
     /*--- Create the edge structure ---*/
 
     if (rank == MASTER_NODE) cout << "Identify edges and vertices." <<endl;
-    geometry->SetEdges();
-    geometry->SetVertex(config);
+    geometry_container[iZone]->SetEdges();
+    geometry_container[iZone]->SetVertex(config_container[iZone]);
 
-    if (config->GetDesign_Variable(0) != NO_DEFORMATION) {
+    if (config_container[iZone]->GetDesign_Variable(0) != NO_DEFORMATION) {
 
         /*--- Create the dual control volume structures ---*/
 
         if (rank == MASTER_NODE) cout << "Setting the bound control volume structure." << endl;
-        geometry->SetControlVolume(config, ALLOCATE);
-        geometry->SetBoundControlVolume(config, ALLOCATE);
+        geometry_container[iZone]->SetControlVolume(config_container[iZone], ALLOCATE);
+        geometry_container[iZone]->SetBoundControlVolume(config_container[iZone], ALLOCATE);
     }
 
     /*--- Create the point-to-point MPI communication structures. ---*/
 
-    geometry->PreprocessP2PComms(geometry, config);
+    geometry_container[iZone]->PreprocessP2PComms(geometry_container[iZone], config_container[iZone]);
 
+    }
 }
 
-void CDeformationDriver::Output_Preprocessing(CConfig *config, CGeometry *geometry, COutput *&output) {
+void CDeformationDriver::Output_Preprocessing() {
+
+      for (iZone = 0; iZone < nZone; iZone++) {
 
         /*--- Allocate the mesh output ---*/
 
-        output = new CMeshOutput(config, geometry->GetnDim());
+        output_container[iZone] = new CMeshOutput(config_container[iZone], geometry_container[iZone]->GetnDim());
 
         /*--- Preprocess the volume output ---*/
 
-        output->PreprocessVolumeOutput(config);
+        output_container[iZone]->PreprocessVolumeOutput(config_container[iZone]);
 
         /*--- Preprocess history --- */
 
-        output->PreprocessHistoryOutput(config, false);
+        output_container[iZone]->PreprocessHistoryOutput(config_container[iZone], false);
+
+    }
 }
 
 void CDeformationDriver::Run() {
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
new file mode 100644
index 00000000000..923901fee8b
--- /dev/null
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -0,0 +1,945 @@
+/*!
+ * \file CDiscAdjDeformationDriver.cpp
+ * \brief Main subroutines for driving the projection of sensitivities.
+ * \author T. Economon, H. Kline, R. Sanchez
+ * \version 7.1.1 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2021, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+
+#include "../../include/drivers/CDiscAdjDeformationDriver.hpp"
+
+#include "../../../Common/include/geometry/CPhysicalGeometry.hpp"
+
+using namespace std;
+
+CDiscAdjDeformationDriver::CDiscAdjDeformationDriver(char* confFile, SU2_Comm MPICommunicator) {
+
+    /*--- Initialize Medipack (must also be here so it is initialized from python) ---*/
+    #ifdef HAVE_MPI
+      #if defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)
+        SU2_MPI::Init_AMPI();
+      #endif
+    #endif
+
+    SU2_MPI::SetComm(MPICommunicator);
+
+    rank = SU2_MPI::GetRank();
+    size = SU2_MPI::GetSize();
+
+    /*--- Copy the config filename ---*/
+    strcpy(config_file_name, confFile);
+
+    /*--- Read the name and format of the input mesh file to get from the mesh
+      file the number of zones and dimensions from the numerical grid (required
+      for variables allocation)  ---*/
+
+    driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DOT);
+
+    nZone = driver_config->GetnZone();
+
+    /*--- Initialize containers --- */
+
+    SetContainers_Null();
+
+    /*--- Preprocessing of the config files. ---*/
+
+    Input_Preprocessing();
+
+    /*--- Set up a timer for performance benchmarking ---*/
+
+    StartTime = SU2_MPI::Wtime();
+
+    /*--- Preprocessing of the geometry for all zones. ---*/
+
+    Geometrical_Preprocessing();
+
+    /*--- Preprocessing of the outputs for all zones. ---*/
+
+    Output_Preprocessing();
+
+    /*--- Preprocessing time is reported now, but not included in the next compute portion. ---*/
+
+    StopTime = SU2_MPI::Wtime();
+
+    /*--- Compute/print the total time for performance benchmarking. ---*/
+
+    UsedTime = StopTime-StartTime;
+    UsedTimePreproc    = UsedTime;
+    UsedTimeCompute    = 0.0;
+
+}
+
+CDiscAdjDeformationDriver::~CDiscAdjDeformationDriver(void) {
+
+}
+
+void CDiscAdjDeformationDriver::SetContainers_Null() {
+
+    /*--- Definition of the containers per zones ---*/
+
+    config_container    = new CConfig*[nZone] ();
+    geometry_container  = new CGeometry**[nZone] ();
+    surface_movement    = new CSurfaceMovement*[nZone] ();
+    grid_movement       = new CVolumetricMovement*[nZone] ();
+
+    nInst               = new unsigned short[nZone];
+    for (iZone = 0; iZone < nZone; iZone++) {
+        nInst[iZone] = 1;
+    }
+}
+
+void CDiscAdjDeformationDriver::Input_Preprocessing() {
+
+    // TODO Check that config is for Discrete Adjoint !
+
+    /*--- Initialize a char to store the zone filename ---*/
+    char zone_file_name[MAX_STRING_SIZE];
+
+    /*--- Loop over all zones to initialize the various classes. In most
+      cases, nZone is equal to one. This represents the solution of a partial
+      differential equation on a single block, unstructured mesh. ---*/
+
+    for (iZone = 0; iZone < nZone; iZone++) {
+
+         /*--- Definition of the configuration option class for all zones. In this
+          constructor, the input configuration file is parsed and all options are
+          read and stored. ---*/
+
+        if (driver_config->GetnConfigFiles() > 0){
+            strcpy(zone_file_name, driver_config->GetConfigFilename(iZone).c_str());
+            config_container[iZone] = new CConfig(driver_config, zone_file_name, SU2_COMPONENT::SU2_DOT, iZone, nZone, true);
+        } else {
+            config_container[iZone] = new CConfig(driver_config, config_file_name, SU2_COMPONENT::SU2_DOT, iZone, nZone, true);
+        }
+
+        config_container[iZone]->SetMPICommunicator(SU2_MPI::GetComm());
+    }
+
+    /*--- Set the multizone part of the problem. ---*/
+    if (driver_config->GetMultizone_Problem()){
+        for (iZone = 0; iZone < nZone; iZone++) {
+            /*--- Set the interface markers for multizone ---*/
+            config_container[iZone]->SetMultizone(driver_config, config_container);
+        }
+    }
+}
+
+void CDiscAdjDeformationDriver::Geometrical_Preprocessing() {
+
+    /*--- Loop over all zones to initialize the various classes. In most
+     cases, nZone is equal to one. This represents the solution of a partial
+     differential equation on a single block, unstructured mesh. ---*/
+
+     for (iZone = 0; iZone < nZone; iZone++) {
+
+        /*--- Determine whether or not the FEM solver is used, which decides the
+         type of geometry classes that are instantiated. ---*/
+        const bool fem_solver = config_container[iZone]->GetFEMSolver();
+
+        /*--- Read the number of instances for each zone ---*/
+
+        nInst[iZone] = config_container[iZone]->GetnTimeInstances();
+
+        geometry_container[iZone] = new CGeometry*[nInst[iZone]];
+
+        for (iInst = 0; iInst < nInst[iZone]; iInst++){
+
+            /*--- Definition of the geometry class to store the primal grid in the partitioning process. ---*/
+
+            CGeometry *geometry_aux = nullptr;
+
+            /*--- All ranks process the grid and call ParMETIS for partitioning ---*/
+
+            geometry_aux = new CPhysicalGeometry(config_container[iZone], iZone, nZone);
+
+            /*--- Color the initial grid and set the send-receive domains (ParMETIS) ---*/
+
+            if ( fem_solver ) geometry_aux->SetColorFEMGrid_Parallel(config_container[iZone]);
+            else              geometry_aux->SetColorGrid_Parallel(config_container[iZone]);
+
+            /*--- Build the grid data structures using the ParMETIS coloring. ---*/
+
+            if( fem_solver ) {
+                switch( config_container[iZone]->GetKind_FEM_Flow() ) {
+                case DG: {
+                    geometry_container[iZone][iInst] = new CMeshFEM_DG(geometry_aux, config_container[iZone]);
+                    break;
+                }
+                }
+            }
+            else {
+                geometry_container[iZone][iInst] = new CPhysicalGeometry(geometry_aux, config_container[iZone]);
+            }
+
+            /*--- Deallocate the memory of geometry_aux ---*/
+
+            delete geometry_aux;
+
+            /*--- Add the Send/Receive boundaries ---*/
+
+            geometry_container[iZone][iInst]->SetSendReceive(config_container[iZone]);
+
+            /*--- Add the Send/Receive boundaries ---*/
+
+            geometry_container[iZone][iInst]->SetBoundaries(config_container[iZone]);
+
+            /*--- Create the vertex structure (required for MPI) ---*/
+
+            if (rank == MASTER_NODE) cout << "Identify vertices." << endl;
+            geometry_container[iZone][iInst]->SetVertex(config_container[iZone]);
+
+            /*--- Store the global to local mapping after preprocessing. ---*/
+
+            if (rank == MASTER_NODE) cout << "Storing a mapping from global to local point index." << endl;
+            geometry_container[iZone][iInst]->SetGlobal_to_Local_Point();
+
+            /* Test for a fem solver, because some more work must be done. */
+
+            if (fem_solver) {
+
+                /*--- Carry out a dynamic cast to CMeshFEM_DG, such that it is not needed to
+                 define all virtual functions in the base class CGeometry. ---*/
+                CMeshFEM_DG *DGMesh = dynamic_cast<CMeshFEM_DG *>(geometry_container[iZone][iInst]);
+
+                /*--- Determine the standard elements for the volume elements. ---*/
+                if (rank == MASTER_NODE) cout << "Creating standard volume elements." << endl;
+                DGMesh->CreateStandardVolumeElements(config_container[iZone]);
+
+                /*--- Create the face information needed to compute the contour integral
+                 for the elements in the Discontinuous Galerkin formulation. ---*/
+                if (rank == MASTER_NODE) cout << "Creating face information." << endl;
+                DGMesh->CreateFaces(config_container[iZone]);
+            }
+        }
+
+        if (rank == MASTER_NODE)
+        cout << "\n----------------------- Preprocessing computations ----------------------" << endl;
+
+        /*--- Compute elements surrounding points, points surrounding points ---*/
+
+        if (rank == MASTER_NODE) cout << "Setting local point connectivity." << endl;
+        geometry_container[iZone][INST_0]->SetPoint_Connectivity();
+
+        /*--- Check the orientation before computing geometrical quantities ---*/
+
+        geometry_container[iZone][INST_0]->SetBoundVolume();
+        if (config_container[iZone]->GetReorientElements()) {
+            if (rank == MASTER_NODE) cout << "Checking the numerical grid orientation of the elements." << endl;
+            geometry_container[iZone][INST_0]->Check_IntElem_Orientation(config_container[iZone]);
+            geometry_container[iZone][INST_0]->Check_BoundElem_Orientation(config_container[iZone]);
+        }
+
+        /*--- Create the edge structure ---*/
+
+        if (rank == MASTER_NODE) cout << "Identify edges and vertices." << endl;
+        geometry_container[iZone][INST_0]->SetEdges(); geometry_container[iZone][INST_0]->SetVertex(config_container[iZone]);
+
+        /*--- Create the dual control volume structures ---*/
+
+        if (rank == MASTER_NODE) cout << "Setting the bound control volume structure." << endl;
+        geometry_container[iZone][INST_0]->SetBoundControlVolume(config_container[ZONE_0], ALLOCATE);
+
+        /*--- Store the global to local mapping after preprocessing. ---*/
+
+        if (rank == MASTER_NODE) cout << "Storing a mapping from global to local point index." << endl;
+        geometry_container[iZone][INST_0]->SetGlobal_to_Local_Point();
+
+        /*--- Create the point-to-point MPI communication structures. ---*/
+
+        geometry_container[iZone][INST_0]->PreprocessP2PComms(geometry_container[iZone][INST_0], config_container[iZone]);
+
+    }
+}
+
+void CDiscAdjDeformationDriver::Output_Preprocessing() {
+
+}
+
+void CDiscAdjDeformationDriver::Run() {
+
+    for (iZone = 0; iZone < nZone; iZone++) {
+            if (rank == MASTER_NODE) cout << "Reading volume sensitivities at each node from file." << endl;
+            grid_movement[iZone] = new CVolumetricMovement(geometry_container[iZone][INST_0], config_container[iZone]);
+
+            /*--- Read in sensitivities from file. ---*/
+            if (config_container[ZONE_0]->GetSensitivity_Format() == UNORDERED_ASCII)
+                geometry_container[iZone][INST_0]->ReadUnorderedSensitivity(config_container[iZone]);
+            else
+                geometry_container[iZone][INST_0]->SetSensitivity(config_container[iZone]);
+
+            if (rank == MASTER_NODE) cout << "\n---------------------- Mesh sensitivity computation ---------------------" << endl;
+            grid_movement[iZone]->SetVolume_Deformation(geometry_container[iZone][INST_0], config_container[iZone], false, true);
+    }
+
+    if (rank == MASTER_NODE) cout << "\n------------------------ Mesh sensitivity Output ------------------------" << endl;
+    SetSensitivity_Files(geometry_container, config_container, nZone);
+
+    /*--- Initialize structure to store the gradient ---*/
+    Gradient = new su2double*[config_container[ZONE_0]->GetnDV()];
+
+    for (auto iDV = 0u; iDV  < config_container[ZONE_0]->GetnDV(); iDV++) {
+        /*--- Initialize to zero ---*/
+        Gradient[iDV] = new su2double[config_container[ZONE_0]->GetnDV_Value(iDV)]();
+    }
+
+    Gradient_file.precision(driver_config->OptionIsSet("OUTPUT_PRECISION") ? driver_config->GetOutput_Precision() : 6);
+
+    /*--- For multizone computations the gradient contributions are summed up and written into one file. ---*/
+    for (iZone = 0; iZone < nZone; iZone++){
+        if ((config_container[iZone]->GetDesign_Variable(0) != NONE) &&
+            (config_container[iZone]->GetDesign_Variable(0) != SURFACE_FILE)) {
+
+        if (rank == MASTER_NODE)
+            cout << "\n---------- Start gradient evaluation using sensitivity information ----------" << endl;
+
+        /*--- Definition of the Class for surface deformation ---*/
+
+        surface_movement[iZone] = new CSurfaceMovement();
+
+        /*--- Copy coordinates to the surface structure ---*/
+
+        surface_movement[iZone]->CopyBoundary(geometry_container[iZone][INST_0], config_container[iZone]);
+
+        /*--- If AD mode is enabled we can use it to compute the projection,
+         *    otherwise we use finite differences. ---*/
+
+        if (config_container[iZone]->GetAD_Mode())
+            SetDiscAdjDeformation_AD(geometry_container[iZone][INST_0], config_container[iZone], surface_movement[iZone] , Gradient);
+        else
+            SetDiscAdjDeformation_FD(geometry_container[iZone][INST_0], config_container[iZone], surface_movement[iZone] , Gradient);
+
+        }
+    } // for iZone
+
+    /*--- Write the gradient to a file ---*/
+
+    if (rank == MASTER_NODE)
+        Gradient_file.open(config_container[ZONE_0]->GetObjFunc_Grad_FileName().c_str(), ios::out);
+
+    /*--- Print gradients to screen and writes to file ---*/
+
+    OutputGradient(Gradient, config_container[ZONE_0], Gradient_file);
+
+}
+
+void CDiscAdjDeformationDriver::Postprocessing() {
+
+    for (auto iDV = 0u; iDV  < config_container[ZONE_0]->GetnDV(); iDV++){
+          delete [] Gradient[iDV];
+    }
+    delete [] Gradient;
+
+    delete driver_config;
+    driver_config = nullptr;
+
+    if (rank == MASTER_NODE)
+        cout << "\n------------------------- Solver Postprocessing -------------------------" << endl;
+
+    if (geometry_container != nullptr) {
+        for (iZone = 0; iZone < nZone; iZone++) {
+            if (geometry_container[iZone] != nullptr) {
+                for (iInst = 0; iInst < nInst[iZone]; iInst++){
+                    if (geometry_container[iZone][iInst] != nullptr) {
+                        delete geometry_container[iZone][iInst];
+                    }
+                }
+                delete geometry_container[iZone];
+            }
+        }
+        delete [] geometry_container;
+    }
+    if (rank == MASTER_NODE) cout << "Deleted CGeometry container." << endl;
+
+    if (surface_movement != nullptr) {
+        for (iZone = 0; iZone < nZone; iZone++) {
+            if (surface_movement[iZone] != nullptr) {
+                delete surface_movement[iZone];
+            }
+        }
+        delete [] surface_movement;
+    }
+    if (rank == MASTER_NODE) cout << "Deleted CSurfaceMovement class." << endl;
+
+    if (grid_movement != nullptr) {
+        for (iZone = 0; iZone < nZone; iZone++) {
+            if (grid_movement[iZone] != nullptr) {
+                delete grid_movement[iZone];
+            }
+        }
+        delete [] grid_movement;
+    }
+    if (rank == MASTER_NODE) cout << "Deleted CVolumetricMovement class." << endl;
+
+    if (config_container != nullptr) {
+        for (iZone = 0; iZone < nZone; iZone++) {
+            if (config_container[iZone] != nullptr) {
+                delete config_container[iZone];
+            }
+        }
+        delete [] config_container;
+    }
+    if (rank == MASTER_NODE) cout << "Deleted CConfig container." << endl;
+
+}
+
+void CDiscAdjDeformationDriver::SetDiscAdjDeformation_FD(CGeometry *geometry, CConfig *config, CSurfaceMovement *surface_movement, su2double** Gradient){
+
+  unsigned short iDV, nDV, iFFDBox, nDV_Value, iMarker, iDim;
+  unsigned long iVertex, iPoint;
+  su2double delta_eps, my_Gradient, localGradient, *Normal, dS, *VarCoord, Sensitivity,
+  dalpha[3], deps[3], dalpha_deps;
+  bool *UpdatePoint, MoveSurface, Local_MoveSurface;
+  CFreeFormDefBox **FFDBox;
+
+  int rank = SU2_MPI::GetRank();
+
+  nDV = config->GetnDV();
+
+  /*--- Boolean controlling points to be updated ---*/
+
+  UpdatePoint = new bool[geometry->GetnPoint()];
+
+  /*--- Definition of the FFD deformation class ---*/
+
+  unsigned short nFFDBox = MAX_NUMBER_FFD;
+  FFDBox = new CFreeFormDefBox*[nFFDBox];
+  for (iFFDBox = 0; iFFDBox < MAX_NUMBER_FFD; iFFDBox++) FFDBox[iFFDBox] = nullptr;
+
+  for (iDV = 0; iDV  < nDV; iDV++){
+    nDV_Value = config->GetnDV_Value(iDV);
+    if (nDV_Value != 1){
+      SU2_MPI::Error("The DiscAdjDeformation using finite differences currently only supports a fixed direction of movement for FFD points.", CURRENT_FUNCTION);
+    }
+  }
+
+  /*--- Continuous adjoint gradient computation ---*/
+
+  if (rank == MASTER_NODE)
+    cout << "Evaluate functional gradient using Finite Differences." << endl;
+
+  for (iDV = 0; iDV < nDV; iDV++) {
+
+    MoveSurface = true;
+    Local_MoveSurface = true;
+
+    /*--- Free Form deformation based ---*/
+
+    if ((config->GetDesign_Variable(iDV) == FFD_CONTROL_POINT_2D) ||
+        (config->GetDesign_Variable(iDV) == FFD_CAMBER_2D) ||
+        (config->GetDesign_Variable(iDV) == FFD_THICKNESS_2D) ||
+        (config->GetDesign_Variable(iDV) == FFD_TWIST_2D) ||
+        (config->GetDesign_Variable(iDV) == FFD_CONTROL_POINT) ||
+        (config->GetDesign_Variable(iDV) == FFD_NACELLE) ||
+        (config->GetDesign_Variable(iDV) == FFD_GULL) ||
+        (config->GetDesign_Variable(iDV) == FFD_TWIST) ||
+        (config->GetDesign_Variable(iDV) == FFD_ROTATION) ||
+        (config->GetDesign_Variable(iDV) == FFD_CAMBER) ||
+        (config->GetDesign_Variable(iDV) == FFD_THICKNESS) ||
+        (config->GetDesign_Variable(iDV) == FFD_ANGLE_OF_ATTACK)) {
+
+      /*--- Read the FFD information in the first iteration ---*/
+
+      if (iDV == 0) {
+
+        if (rank == MASTER_NODE)
+          cout << "Read the FFD information from mesh file." << endl;
+
+        /*--- Read the FFD information from the grid file ---*/
+
+        surface_movement->ReadFFDInfo(geometry, config, FFDBox, config->GetMesh_FileName());
+
+        /*--- If the FFDBox was not defined in the input file ---*/
+        if (!surface_movement->GetFFDBoxDefinition()) {
+          SU2_MPI::Error("The input grid doesn't have the entire FFD information!", CURRENT_FUNCTION);
+        }
+
+        for (iFFDBox = 0; iFFDBox < surface_movement->GetnFFDBox(); iFFDBox++) {
+
+          if (rank == MASTER_NODE) cout << "Checking FFD box dimension." << endl;
+          surface_movement->CheckFFDDimension(geometry, config, FFDBox[iFFDBox], iFFDBox);
+
+          if (rank == MASTER_NODE) cout << "Check the FFD box intersections with the solid surfaces." << endl;
+          surface_movement->CheckFFDIntersections(geometry, config, FFDBox[iFFDBox], iFFDBox);
+
+        }
+
+        if (rank == MASTER_NODE)
+          cout <<"-------------------------------------------------------------------------" << endl;
+
+      }
+
+      if (rank == MASTER_NODE) {
+        cout << endl << "Design variable number "<< iDV <<"." << endl;
+        cout << "Performing 3D deformation of the surface." << endl;
+      }
+
+      /*--- Apply the control point change ---*/
+
+      MoveSurface = false;
+
+      for (iFFDBox = 0; iFFDBox < surface_movement->GetnFFDBox(); iFFDBox++) {
+
+        /*--- Reset FFD box ---*/
+
+        switch (config->GetDesign_Variable(iDV) ) {
+          case FFD_CONTROL_POINT_2D : Local_MoveSurface = surface_movement->SetFFDCPChange_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+          case FFD_CAMBER_2D :        Local_MoveSurface = surface_movement->SetFFDCamber_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+          case FFD_THICKNESS_2D :     Local_MoveSurface = surface_movement->SetFFDThickness_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+          case FFD_TWIST_2D :         Local_MoveSurface = surface_movement->SetFFDTwist_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+          case FFD_CONTROL_POINT :    Local_MoveSurface = surface_movement->SetFFDCPChange(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+          case FFD_NACELLE :          Local_MoveSurface = surface_movement->SetFFDNacelle(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+          case FFD_GULL :             Local_MoveSurface = surface_movement->SetFFDGull(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+          case FFD_TWIST :            Local_MoveSurface = surface_movement->SetFFDTwist(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+          case FFD_ROTATION :         Local_MoveSurface = surface_movement->SetFFDRotation(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+          case FFD_CAMBER :           Local_MoveSurface = surface_movement->SetFFDCamber(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+          case FFD_THICKNESS :        Local_MoveSurface = surface_movement->SetFFDThickness(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+          case FFD_CONTROL_SURFACE :  Local_MoveSurface = surface_movement->SetFFDControl_Surface(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+          case FFD_ANGLE_OF_ATTACK :  Gradient[iDV][0] = config->GetAoA_Sens(); break;
+        }
+
+        /*--- Recompute cartesian coordinates using the new control points position ---*/
+
+        if (Local_MoveSurface) {
+          MoveSurface = true;
+          surface_movement->SetCartesianCoord(geometry, config, FFDBox[iFFDBox], iFFDBox, true);
+        }
+
+      }
+
+    }
+
+    /*--- Hicks Henne design variable ---*/
+
+    else if (config->GetDesign_Variable(iDV) == HICKS_HENNE) {
+      surface_movement->SetHicksHenne(geometry, config, iDV, true);
+    }
+
+    /*--- Surface bump design variable ---*/
+
+    else if (config->GetDesign_Variable(iDV) == SURFACE_BUMP) {
+      surface_movement->SetSurface_Bump(geometry, config, iDV, true);
+    }
+
+    /*--- Kulfan (CST) design variable ---*/
+
+    else if (config->GetDesign_Variable(iDV) == CST) {
+      surface_movement->SetCST(geometry, config, iDV, true);
+    }
+
+    /*--- Displacement design variable ---*/
+
+    else if (config->GetDesign_Variable(iDV) == TRANSLATION) {
+      surface_movement->SetTranslation(geometry, config, iDV, true);
+    }
+
+    /*--- Angle of Attack design variable ---*/
+
+    else if (config->GetDesign_Variable(iDV) == ANGLE_OF_ATTACK) {
+      Gradient[iDV][0] = config->GetAoA_Sens();
+    }
+
+    /*--- Scale design variable ---*/
+
+    else if (config->GetDesign_Variable(iDV) == SCALE) {
+      surface_movement->SetScale(geometry, config, iDV, true);
+    }
+
+    /*--- Rotation design variable ---*/
+
+    else if (config->GetDesign_Variable(iDV) == ROTATION) {
+      surface_movement->SetRotation(geometry, config, iDV, true);
+    }
+
+    /*--- NACA_4Digits design variable ---*/
+
+    else if (config->GetDesign_Variable(iDV) == NACA_4DIGITS) {
+      surface_movement->SetNACA_4Digits(geometry, config);
+    }
+
+    /*--- Parabolic design variable ---*/
+
+    else if (config->GetDesign_Variable(iDV) == PARABOLIC) {
+      surface_movement->SetParabolic(geometry, config);
+    }
+
+    /*--- Design variable not implement ---*/
+
+    else {
+      if (rank == MASTER_NODE)
+        cout << "Design Variable not implement yet" << endl;
+    }
+
+    /*--- Load the delta change in the design variable (finite difference step). ---*/
+
+    if ((config->GetDesign_Variable(iDV) != ANGLE_OF_ATTACK) &&
+        (config->GetDesign_Variable(iDV) != FFD_ANGLE_OF_ATTACK)) {
+
+      /*--- If the Angle of attack is not involved, reset the value of the gradient ---*/
+
+      my_Gradient = 0.0; Gradient[iDV][0] = 0.0;
+
+      if (MoveSurface) {
+
+        delta_eps = config->GetDV_Value(iDV);
+
+        for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++)
+          UpdatePoint[iPoint] = true;
+
+        for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
+          if (config->GetMarker_All_DV(iMarker) == YES) {
+            for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
+
+              iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+              if ((iPoint < geometry->GetnPointDomain()) && UpdatePoint[iPoint]) {
+
+                Normal = geometry->vertex[iMarker][iVertex]->GetNormal();
+                VarCoord = geometry->vertex[iMarker][iVertex]->GetVarCoord();
+                Sensitivity = geometry->vertex[iMarker][iVertex]->GetAuxVar();
+
+                dS = 0.0;
+                for (iDim = 0; iDim < geometry->GetnDim(); iDim++) {
+                  dS += Normal[iDim]*Normal[iDim];
+                  deps[iDim] = VarCoord[iDim] / delta_eps;
+                }
+                dS = sqrt(dS);
+
+                dalpha_deps = 0.0;
+                for (iDim = 0; iDim < geometry->GetnDim(); iDim++) {
+                  dalpha[iDim] = Normal[iDim] / dS;
+                  dalpha_deps -= dalpha[iDim]*deps[iDim];
+                }
+
+                my_Gradient += Sensitivity*dalpha_deps;
+                UpdatePoint[iPoint] = false;
+              }
+            }
+          }
+        }
+      }
+
+      SU2_MPI::Allreduce(&my_Gradient, &localGradient, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
+      Gradient[iDV][0] += localGradient;
+    }
+  }
+
+  /*--- Delete memory for parameterization. ---*/
+
+  if (FFDBox != nullptr) {
+    for (iFFDBox = 0; iFFDBox < MAX_NUMBER_FFD; iFFDBox++) {
+      if (FFDBox[iFFDBox] != nullptr) {
+        delete FFDBox[iFFDBox];
+      }
+    }
+    delete [] FFDBox;
+  }
+
+  delete [] UpdatePoint;
+
+}
+
+
+void CDiscAdjDeformationDriver::SetDiscAdjDeformation_AD(CGeometry *geometry, CConfig *config, CSurfaceMovement *surface_movement, su2double** Gradient){
+
+  su2double DV_Value, *VarCoord, Sensitivity, my_Gradient, localGradient, *Normal, Area = 0.0;
+  unsigned short iDV_Value = 0, iMarker, nMarker, iDim, nDim, iDV, nDV, nDV_Value;
+  unsigned long iVertex, nVertex, iPoint;
+
+  int rank = SU2_MPI::GetRank();
+
+  nMarker = config->GetnMarker_All();
+  nDim    = geometry->GetnDim();
+  nDV     = config->GetnDV();
+
+  VarCoord = nullptr;
+
+  /*--- Discrete adjoint gradient computation ---*/
+
+  if (rank == MASTER_NODE)
+    cout  << endl << "Evaluate functional gradient using Algorithmic Differentiation (ZONE " << config->GetiZone() << ")." << endl;
+
+  /*--- Start recording of operations ---*/
+
+  AD::StartRecording();
+
+  /*--- Register design variables as input and set them to zero
+   * (since we want to have the derivative at alpha = 0, i.e. for the current design) ---*/
+
+
+
+  for (iDV = 0; iDV < nDV; iDV++){
+
+    nDV_Value =  config->GetnDV_Value(iDV);
+
+    for (iDV_Value = 0; iDV_Value < nDV_Value; iDV_Value++){
+
+      /*--- Initilization with su2double resets the index ---*/
+
+      DV_Value = 0.0;
+
+      AD::RegisterInput(DV_Value);
+
+      config->SetDV_Value(iDV, iDV_Value, DV_Value);
+    }
+  }
+
+  /*--- Call the surface deformation routine ---*/
+
+  surface_movement->SetSurface_Deformation(geometry, config);
+
+  /*--- Stop the recording --- */
+
+  AD::StopRecording();
+
+  /*--- Create a structure to identify points that have been already visited.
+   * We need that to make sure to set the sensitivity of surface points only once
+   *  (Markers share points, so we would visit them more than once in the loop over the markers below) ---*/
+
+  bool* visited = new bool[geometry->GetnPoint()];
+  for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++){
+    visited[iPoint] = false;
+  }
+
+  /*--- Initialize the derivatives of the output of the surface deformation routine
+   * with the discrete adjoints from the CFD solution ---*/
+
+  for (iMarker = 0; iMarker < nMarker; iMarker++) {
+    if (config->GetMarker_All_DV(iMarker) == YES) {
+      nVertex = geometry->nVertex[iMarker];
+      for (iVertex = 0; iVertex <nVertex; iVertex++) {
+        iPoint      = geometry->vertex[iMarker][iVertex]->GetNode();
+        if (!visited[iPoint]){
+          VarCoord    = geometry->vertex[iMarker][iVertex]->GetVarCoord();
+          Normal      = geometry->vertex[iMarker][iVertex]->GetNormal();
+
+          Area = 0.0;
+          for (iDim = 0; iDim < nDim; iDim++){
+            Area += Normal[iDim]*Normal[iDim];
+          }
+          Area = sqrt(Area);
+
+          for (iDim = 0; iDim < nDim; iDim++){
+            if (config->GetDiscrete_Adjoint()){
+              Sensitivity = geometry->GetSensitivity(iPoint, iDim);
+            } else {
+              Sensitivity = -Normal[iDim]*geometry->vertex[iMarker][iVertex]->GetAuxVar()/Area;
+            }
+            SU2_TYPE::SetDerivative(VarCoord[iDim], SU2_TYPE::GetValue(Sensitivity));
+          }
+          visited[iPoint] = true;
+        }
+      }
+    }
+  }
+
+  delete [] visited;
+
+  /*--- Compute derivatives and extract gradient ---*/
+
+  AD::ComputeAdjoint();
+
+  for (iDV = 0; iDV  < nDV; iDV++){
+    nDV_Value =  config->GetnDV_Value(iDV);
+
+    for (iDV_Value = 0; iDV_Value < nDV_Value; iDV_Value++){
+      DV_Value = config->GetDV_Value(iDV, iDV_Value);
+      my_Gradient = SU2_TYPE::GetDerivative(DV_Value);
+      SU2_MPI::Allreduce(&my_Gradient, &localGradient, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
+
+      /*--- Angle of Attack design variable (this is different,
+       the value comes form the input file) ---*/
+
+      if ((config->GetDesign_Variable(iDV) == ANGLE_OF_ATTACK) ||
+          (config->GetDesign_Variable(iDV) == FFD_ANGLE_OF_ATTACK))  {
+        Gradient[iDV][iDV_Value] = config->GetAoA_Sens();
+      }
+
+      Gradient[iDV][iDV_Value] += localGradient;
+    }
+  }
+
+  AD::Reset();
+
+}
+
+void CDiscAdjDeformationDriver::OutputGradient(su2double** Gradient, CConfig* config, ofstream& Gradient_file){
+
+  unsigned short nDV, iDV, iDV_Value, nDV_Value;
+
+  int rank = SU2_MPI::GetRank();
+
+  nDV = config->GetnDV();
+
+  /*--- Loop through all design variables and their gradients ---*/
+
+  for (iDV = 0; iDV  < nDV; iDV++){
+    nDV_Value = config->GetnDV_Value(iDV);
+    if (rank == MASTER_NODE){
+
+      /*--- Print the kind of design variable on screen ---*/
+
+      cout << endl << "Design variable (";
+      for (std::map<string, ENUM_PARAM>::const_iterator it = Param_Map.begin(); it != Param_Map.end(); ++it ){
+        if (it->second == config->GetDesign_Variable(iDV)){
+          cout << it->first << ") number "<< iDV << "." << endl;
+        }
+      }
+
+      /*--- Print the kind of objective function to screen ---*/
+
+      for (std::map<string, ENUM_OBJECTIVE>::const_iterator it = Objective_Map.begin(); it != Objective_Map.end(); ++it ){
+        if (it->second == config->GetKind_ObjFunc()){
+          cout << it->first << " gradient : ";
+          if (iDV == 0) Gradient_file << it->first << " gradient " << endl;
+        }
+      }
+
+      /*--- Print the gradient to file and screen ---*/
+
+      for (iDV_Value = 0; iDV_Value < nDV_Value; iDV_Value++){
+        cout << Gradient[iDV][iDV_Value];
+        if (iDV_Value != nDV_Value-1 ){
+          cout << ", ";
+        }
+        Gradient_file << Gradient[iDV][iDV_Value] << endl;
+      }
+      cout << endl;
+      cout <<"-------------------------------------------------------------------------" << endl;
+    }
+  }
+}
+
+
+void CDiscAdjDeformationDriver::SetSensitivity_Files(CGeometry ***geometry, CConfig **config, unsigned short val_nZone) {
+
+  unsigned short iMarker,iDim, nDim, nMarker, nVar;
+  unsigned long iVertex, iPoint, nPoint, nVertex;
+  su2double *Normal, Prod, Sens = 0.0, SensDim, Area;
+
+  unsigned short iZone;
+
+  CSolver *solver  = nullptr;
+  COutput *output  = nullptr;
+
+  for (iZone = 0; iZone < val_nZone; iZone++) {
+
+    nPoint = geometry[iZone][INST_0]->GetnPoint();
+    nDim   = geometry[iZone][INST_0]->GetnDim();
+    nMarker = config[iZone]->GetnMarker_All();
+    nVar = nDim + 1;
+
+    /*--- We create a baseline solver to easily merge the sensitivity information ---*/
+
+    vector<string> fieldnames;
+    fieldnames.push_back("\"Point\"");
+    fieldnames.push_back("\"x\"");
+    fieldnames.push_back("\"y\"");
+    if (nDim == 3) {
+      fieldnames.push_back("\"z\"");
+    }
+    fieldnames.push_back("\"Sensitivity_x\"");
+    fieldnames.push_back("\"Sensitivity_y\"");
+    if (nDim == 3) {
+      fieldnames.push_back("\"Sensitivity_z\"");
+    }
+    fieldnames.push_back("\"Surface_Sensitivity\"");
+
+    solver = new CBaselineSolver(geometry[iZone][INST_0], config[iZone], nVar+nDim, fieldnames);
+
+    for (iPoint = 0; iPoint < nPoint; iPoint++) {
+      for (iDim = 0; iDim < nDim; iDim++) {
+        solver->GetNodes()->SetSolution(iPoint, iDim,      geometry[iZone][INST_0]->nodes->GetCoord(iPoint, iDim));
+        solver->GetNodes()->SetSolution(iPoint, iDim+nDim, geometry[iZone][INST_0]->GetSensitivity(iPoint, iDim));
+      }
+    }
+
+    /*--- Compute the sensitivity in normal direction ---*/
+
+    for (iMarker = 0; iMarker < nMarker; iMarker++) {
+
+      if(config[iZone]->GetSolid_Wall(iMarker) || (config[iZone]->GetMarker_All_DV(iMarker) == YES )) {
+
+        nVertex = geometry[iZone][INST_0]->GetnVertex(iMarker);
+
+        for (iVertex = 0; iVertex < nVertex; iVertex++) {
+          iPoint = geometry[iZone][INST_0]->vertex[iMarker][iVertex]->GetNode();
+          Normal = geometry[iZone][INST_0]->vertex[iMarker][iVertex]->GetNormal();
+          Prod = 0.0;
+          Area = 0.0;
+          for (iDim = 0; iDim < nDim; iDim++) {
+
+            /*--- Retrieve the gradient calculated with discrete adjoint method ---*/
+
+            SensDim = geometry[iZone][INST_0]->GetSensitivity(iPoint, iDim);
+
+            /*--- Calculate scalar product for DiscAdjDeformation onto the normal vector ---*/
+
+            Prod += Normal[iDim]*SensDim;
+
+            Area += Normal[iDim]*Normal[iDim];
+          }
+
+          Area = sqrt(Area);
+
+          /*--- DiscAdjDeformation of the gradient onto the normal vector of the surface ---*/
+
+          Sens = Prod/Area;
+
+          solver->GetNodes()->SetSolution(iPoint, 2*nDim, Sens);
+
+        }
+      }
+    }
+
+    output = new CBaselineOutput(config[iZone], nDim, solver);
+    output->PreprocessVolumeOutput(config[iZone]);
+    output->PreprocessHistoryOutput(config[iZone], false);
+
+    /*--- Load the data --- */
+
+    output->Load_Data(geometry[iZone][INST_0], config[iZone], &solver);
+
+    /*--- Set the surface filename ---*/
+
+    output->SetSurface_Filename(config[iZone]->GetSurfSens_FileName());
+
+    /*--- Set the volume filename ---*/
+
+    output->SetVolume_Filename(config[iZone]->GetVolSens_FileName());
+
+    /*--- Write to file ---*/
+
+    for (unsigned short iFile = 0; iFile < config[iZone]->GetnVolumeOutputFiles(); iFile++){
+      auto FileFormat = config[iZone]->GetVolumeOutputFiles();
+      if (FileFormat[iFile] != RESTART_ASCII &&
+          FileFormat[iFile] != RESTART_BINARY &&
+          FileFormat[iFile] != CSV)
+        output->WriteToFile(config[iZone], geometry[iZone][INST_0], FileFormat[iFile]);
+    }
+
+    /*--- Free memory ---*/
+
+    delete output;
+    delete solver;
+
+  }
+
+}
diff --git a/SU2_DEF/src/meson.build b/SU2_DEF/src/meson.build
index a6681c5c88d..0f19687b7bc 100644
--- a/SU2_DEF/src/meson.build
+++ b/SU2_DEF/src/meson.build
@@ -1,7 +1,8 @@
 su2_def_include = include_directories('./')
 su2_def_src = files([
   'SU2_DEF.cpp',
-  'drivers/CDeformationDriver.cpp'
+  'drivers/CDeformationDriver.cpp',
+  'drivers/CDiscAdjDeformationDriver.cpp'
 ])
 if get_option('enable-normal')
 
@@ -12,6 +13,7 @@ su2_cfd_obj = su2_cfd_lib.extract_objects(['solvers/CSolver.cpp',
                                       'output/tools/CWindowingTools.cpp',
                                       'output/CMeshOutput.cpp',
                                       'output/output_structure_legacy.cpp',
+                                      'output/CBaselineOutput.cpp',
                                       'variables/CBaselineVariable.cpp',
                                       'variables/CVariable.cpp',
                                       'output/filewriter/CParallelDataSorter.cpp',
@@ -49,3 +51,43 @@ su2_cfd_obj = su2_cfd_lib.extract_objects(['solvers/CSolver.cpp',
                         objects : su2_cfd_obj,
                         cpp_args :[default_warning_flags, su2_cpp_args])
 endif
+
+if get_option('enable-autodiff')
+su2_cfd_obj_ad = su2_cfd_lib_ad.extract_objects(['solvers/CSolver.cpp',
+                                                 'solvers/CBaselineSolver.cpp',
+                                                 'CMarkerProfileReaderFVM.cpp',
+                                                 'output/COutput.cpp',
+                                                 'output/tools/CWindowingTools.cpp',
+                                                 'output/output_structure_legacy.cpp',
+                                                 'output/CBaselineOutput.cpp',
+                                                 'output/filewriter/CParallelDataSorter.cpp',
+                                                 'output/filewriter/CParallelFileWriter.cpp',
+                                                 'output/filewriter/CFEMDataSorter.cpp',
+                                                 'output/filewriter/CSurfaceFEMDataSorter.cpp',
+                                                 'output/filewriter/CFVMDataSorter.cpp',
+                                                 'output/filewriter/CSurfaceFVMDataSorter.cpp',
+                                                 'output/filewriter/CCSVFileWriter.cpp',
+                                                 'output/filewriter/CSTLFileWriter.cpp',
+                                                 'output/filewriter/CTecplotFileWriter.cpp',
+                                                 'output/filewriter/CTecplotBinaryFileWriter.cpp',
+                                                 'output/filewriter/CParaviewFileWriter.cpp',
+                                                 'output/filewriter/CParaviewBinaryFileWriter.cpp',
+                                                 'output/filewriter/CSU2FileWriter.cpp',
+                                                 'output/filewriter/CSU2BinaryFileWriter.cpp',
+                                                 'output/filewriter/CSU2MeshFileWriter.cpp',
+                                                 'output/filewriter/CParaviewXMLFileWriter.cpp',
+                                                 'output/filewriter/CParaviewVTMFileWriter.cpp',
+                                                 'variables/CBaselineVariable.cpp',
+                                                 'variables/CVariable.cpp',
+                                                 'limiters/CLimiterDetails.cpp'])
+
+  su2_def_lib_ad = static_library('SU2core_DEF_AD',
+                                  su2_def_src,
+                                  install : false,
+                                  dependencies : [su2_deps, codi_dep, commonAD_dep],
+                                  cpp_args:  [default_warning_flags, su2_cpp_args, codi_rev_args])
+
+  su2_def_dep_ad = declare_dependency(link_with: su2_def_lib_ad,
+                                     include_directories: su2_def_include)
+
+endif
diff --git a/SU2_DOT/src/meson.build b/SU2_DOT/src/meson.build
index 4b01f4f3547..8fd80741329 100644
--- a/SU2_DOT/src/meson.build
+++ b/SU2_DOT/src/meson.build
@@ -1,4 +1,4 @@
-su2_dot_src = ['SU2_DOT.cpp']
+su2_dot_src = 'SU2_DOT.cpp'
 
 if get_option('enable-normal')
   su2_cfd_obj = su2_cfd_lib.extract_objects(['solvers/CSolver.cpp',
@@ -28,10 +28,11 @@ if get_option('enable-normal')
                                              'variables/CBaselineVariable.cpp',
                                              'variables/CVariable.cpp',
                                              'limiters/CLimiterDetails.cpp'])
+
   su2_dot = executable('SU2_DOT',
-                      su2_dot_src, 
+                      su2_dot_src,
                       install: true,
-                      dependencies: [su2_deps, common_dep], 
+                      dependencies: [su2_deps, common_dep],
                       objects : su2_cfd_obj,
                       cpp_args :[default_warning_flags, su2_cpp_args])
 
@@ -69,7 +70,7 @@ if get_option('enable-autodiff')
   su2_dot_ad = executable('SU2_DOT_AD',
                           su2_dot_src,
                           install: true,
-                          dependencies: [su2_deps, codi_dep, commonAD_dep], 
+                          dependencies: [su2_deps, codi_dep, commonAD_dep],
 		                      objects : su2_cfd_obj_ad,
 		                      cpp_args : [default_warning_flags, su2_cpp_args, codi_rev_args])
 
diff --git a/SU2_PY/pySU2/meson.build b/SU2_PY/pySU2/meson.build
index 1aab2e53b50..59b6a063347 100644
--- a/SU2_PY/pySU2/meson.build
+++ b/SU2_PY/pySU2/meson.build
@@ -28,7 +28,10 @@ if get_option('enable-normal')
       '_pysu2',
       cpp_source,
       dependencies: [wrapper_deps, common_dep, su2_deps],
-      objects: [su2_cfd_lib.extract_all_objects(), su2_def_lib.extract_objects('drivers/CDeformationDriver.cpp')],
+      objects: [
+        su2_cfd_lib.extract_all_objects(),
+        su2_def_lib.extract_objects('drivers/CDeformationDriver.cpp')
+      ],
       install: true,
       include_directories : mpi4py_include,
       cpp_args : [default_warning_flags,su2_cpp_args],
@@ -44,7 +47,10 @@ if get_option('enable-autodiff')
       '_pysu2ad',
       cpp_source,
       dependencies: [wrapper_deps, commonAD_dep, su2_deps, codi_dep],
-      objects: su2_cfd_lib_ad.extract_all_objects(),
+      objects: [
+        su2_cfd_lib_ad.extract_all_objects(),
+        su2_def_lib_ad.extract_objects('drivers/CDiscAdjDeformationDriver.cpp')
+      ],
       install: true,
       include_directories : mpi4py_include,
       cpp_args : [default_warning_flags, su2_cpp_args, codi_rev_args],
diff --git a/SU2_PY/pySU2/pySU2ad.i b/SU2_PY/pySU2/pySU2ad.i
index 4409fd93fcb..ff7eaf6cb51 100644
--- a/SU2_PY/pySU2/pySU2ad.i
+++ b/SU2_PY/pySU2/pySU2ad.i
@@ -42,6 +42,7 @@ threads="1"
 #include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CMultizoneDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp"
+#include "../../SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp"
 
 %}
 
@@ -91,3 +92,4 @@ const unsigned int ZONE_1 = 1; /*!< \brief Definition of the first grid domain.
 %include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CMultizoneDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp"
+%include "../../SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp"

From bb2c03044cf60e4106eb7041f5152477052b2a71 Mon Sep 17 00:00:00 2001
From: aa-g <aa.gastaldi@pm.me>
Date: Tue, 22 Jun 2021 19:34:31 +0200
Subject: [PATCH 006/656] Integrate CMeshSolver for mesh deformation based on
 linear elasticity solver

---
 .../geometry/primal_grid/CPrimalGrid.hpp      |   1 +
 SU2_CFD/include/solvers/CMeshSolver.hpp       |  15 +-
 SU2_CFD/include/solvers/CSolver.hpp           |  12 +-
 SU2_CFD/src/iteration/CIteration.cpp          |   2 +-
 SU2_CFD/src/solvers/CMeshSolver.cpp           |  58 ++++++-
 .../include/drivers/CDeformationDriver.hpp    |  30 +++-
 SU2_DEF/src/drivers/CDeformationDriver.cpp    | 152 ++++++++++++++----
 SU2_DEF/src/meson.build                       |  10 ++
 8 files changed, 245 insertions(+), 35 deletions(-)

diff --git a/Common/include/geometry/primal_grid/CPrimalGrid.hpp b/Common/include/geometry/primal_grid/CPrimalGrid.hpp
index 5697b6fbf07..e5b7f19ca50 100644
--- a/Common/include/geometry/primal_grid/CPrimalGrid.hpp
+++ b/Common/include/geometry/primal_grid/CPrimalGrid.hpp
@@ -32,6 +32,7 @@
 
 #include <iostream>
 #include <vector>
+#include <limits>
 #include <cstdlib>
 
 #include "../../CConfig.hpp"
diff --git a/SU2_CFD/include/solvers/CMeshSolver.hpp b/SU2_CFD/include/solvers/CMeshSolver.hpp
index 5a4a6d927f0..2b8cdb04b9e 100644
--- a/SU2_CFD/include/solvers/CMeshSolver.hpp
+++ b/SU2_CFD/include/solvers/CMeshSolver.hpp
@@ -129,6 +129,7 @@ class CMeshSolver final : public CFEASolver {
   /*!
    * \brief Grid deformation using the linear elasticity equations.
    * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] numerics - Numerics used in the solution.
    * \param[in] config - Definition of the particular problem.
    */
   void DeformMesh(CGeometry **geometry,
@@ -136,12 +137,20 @@ class CMeshSolver final : public CFEASolver {
                   CConfig *config) override;
 
   /*!
-   * \brief Set the stiffness of the mesh.
+   * \brief Grid deformation using the linear elasticity equations (no multigrid).
    * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] numerics - Numerics used in the solution.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void DeformMesh(CGeometry *geometry,
+                  CNumerics **numerics,
+                  CConfig *config) override;
+  /*!
+   * \brief Set the stiffness of the mesh.
+   * \param[in] numerics - Numerics used in the solution.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetMesh_Stiffness(CGeometry **geometry,
-                         CNumerics **numerics,
+  void SetMesh_Stiffness(CNumerics **numerics,
                          CConfig *config) override;
 
   /*!
diff --git a/SU2_CFD/include/solvers/CSolver.hpp b/SU2_CFD/include/solvers/CSolver.hpp
index ad1889ce9f4..8263a8ae064 100644
--- a/SU2_CFD/include/solvers/CSolver.hpp
+++ b/SU2_CFD/include/solvers/CSolver.hpp
@@ -4205,8 +4205,16 @@ class CSolver {
    * \param[in] config - Definition of the particular problem.
    * \param[in] referenceCoord - Determine if the mesh is deformed from the reference or from the current coordinates.
    */
-  inline virtual void SetMesh_Stiffness(CGeometry **geometry,
-                                        CNumerics **numerics,
+  inline virtual void DeformMesh(CGeometry *geometry,
+                                 CNumerics **numerics,
+                                 CConfig *config) { }
+
+  /*!
+   * \brief A virtual member.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] referenceCoord - Determine if the mesh is deformed from the reference or from the current coordinates.
+   */
+  inline virtual void SetMesh_Stiffness(CNumerics **numerics,
                                         CConfig *config) { }
 
   /*!
diff --git a/SU2_CFD/src/iteration/CIteration.cpp b/SU2_CFD/src/iteration/CIteration.cpp
index 3fbe23c695c..fe27147992a 100644
--- a/SU2_CFD/src/iteration/CIteration.cpp
+++ b/SU2_CFD/src/iteration/CIteration.cpp
@@ -163,7 +163,7 @@ void CIteration::SetMesh_Deformation(CGeometry** geometry, CSolver** solver, CNu
 
   /*--- Set the stiffness of each element mesh into the mesh numerics ---*/
 
-  solver[MESH_SOL]->SetMesh_Stiffness(geometry, numerics[MESH_SOL], config);
+  solver[MESH_SOL]->SetMesh_Stiffness(numerics[MESH_SOL], config);
 
   /*--- Deform the volume grid around the new boundary locations ---*/
 
diff --git a/SU2_CFD/src/solvers/CMeshSolver.cpp b/SU2_CFD/src/solvers/CMeshSolver.cpp
index 06af9b8408c..ab0446da994 100644
--- a/SU2_CFD/src/solvers/CMeshSolver.cpp
+++ b/SU2_CFD/src/solvers/CMeshSolver.cpp
@@ -420,7 +420,7 @@ void CMeshSolver::SetWallDistance(CGeometry *geometry, CConfig *config) {
   END_SU2_OMP_PARALLEL
 }
 
-void CMeshSolver::SetMesh_Stiffness(CGeometry **geometry, CNumerics **numerics, CConfig *config){
+void CMeshSolver::SetMesh_Stiffness(CNumerics **numerics, CConfig *config){
 
   if (stiffness_set) return;
 
@@ -542,6 +542,62 @@ void CMeshSolver::DeformMesh(CGeometry **geometry, CNumerics **numerics, CConfig
 
 }
 
+void CMeshSolver::DeformMesh(CGeometry *geometry, CNumerics **numerics, CConfig *config){
+
+  if (multizone) nodes->Set_BGSSolution_k();
+
+  /*--- Capture a few MPI dependencies for AD. ---*/
+  geometry->InitiateComms(geometry, config, COORDINATES);
+  geometry->CompleteComms(geometry, config, COORDINATES);
+
+  InitiateComms(geometry, config, SOLUTION);
+  CompleteComms(geometry, config, SOLUTION);
+
+  InitiateComms(geometry, config, MESH_DISPLACEMENTS);
+  CompleteComms(geometry, config, MESH_DISPLACEMENTS);
+
+  /*--- Compute the stiffness matrix, no point recording because we clear the residual. ---*/
+
+  const bool wasActive = AD::BeginPassive();
+
+  Compute_StiffMatrix(geometry, numerics, config);
+
+  AD::EndPassive(wasActive);
+
+  /*--- Clear residual (loses AD info), we do not want an incremental solution. ---*/
+  SU2_OMP_PARALLEL {
+    LinSysRes.SetValZero();
+    if (time_domain && config->GetFSI_Simulation()) LinSysSol.SetValZero();
+  }
+  END_SU2_OMP_PARALLEL
+
+  /*--- Impose boundary conditions (all of them are ESSENTIAL BC's - displacements). ---*/
+  SetBoundaryDisplacements(geometry, config, false);
+
+  /*--- Solve the linear system. ---*/
+  Solve_System(geometry, config);
+
+  SU2_OMP_PARALLEL {
+
+  /*--- Update the grid coordinates and cell volumes using the solution
+     of the linear system (usol contains the x, y, z displacements). ---*/
+  UpdateGridCoord(geometry, config);
+
+  /*--- Update the dual grid. ---*/
+  UpdateDualGrid(geometry, config);
+
+  /*--- Check for failed deformation (negative volumes). ---*/
+  SetMinMaxVolume(geometry, config, true);
+
+  /*--- The Grid Velocity is only computed if the problem is time domain ---*/
+  if (time_domain && !config->GetFSI_Simulation())
+    ComputeGridVelocity(geometry, config);
+
+  }
+  END_SU2_OMP_PARALLEL
+
+}
+
 void CMeshSolver::UpdateGridCoord(CGeometry *geometry, CConfig *config){
 
   /*--- Update the grid coordinates using the solution of the linear system ---*/
diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index 8a424ff32fd..2601f378ad8 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -1,4 +1,4 @@
-/*!
+ /*!
  * \file CDeformationDriver.hpp
  * \brief Headers of the main subroutines for driving the mesh deformation.
  * \author T. Economon, H. Kline, R. Sanchez
@@ -32,6 +32,7 @@
 #include "../../../Common/include/grid_movement/CSurfaceMovement.hpp"
 #include "../../../Common/include/grid_movement/CVolumetricMovement.hpp"
 #include "../../../SU2_CFD/include/output/COutput.hpp"
+#include "../../../SU2_CFD/include/numerics/CNumerics.hpp"
 #include "../../../Common/include/geometry/CGeometry.hpp"
 
 /*!
@@ -56,6 +57,8 @@ class CDeformationDriver {
   CGeometry **geometry_container;             /*!< \brief Geometrical definition of the problem. */
   CSurfaceMovement **surface_movement;          /*!< \brief Surface movement classes of the problem. */
   CVolumetricMovement **grid_movement;         /*!< \brief Volume grid movement classes of the problem. */
+  CSolver **solver_container;
+  CNumerics ***numerics_container;
   COutput **output_container;                   /*!< \brief Pointer to the COutput class. */
 
 public:
@@ -76,6 +79,11 @@ class CDeformationDriver {
    */
   void Run();
 
+  /*!
+   * \brief Output the mesh.
+   */
+  void Output();
+
   /*!
    * \brief Deallocation routine
    */
@@ -102,4 +110,24 @@ class CDeformationDriver {
    */
   void Output_Preprocessing();
 
+  /*!
+   * \brief Preprocess the mesh solver container.
+   */
+  void Solver_Preprocessing();
+
+  /*!
+   * \brief Preprocess the numerics container.
+   */
+  void Numerics_Preprocessing();
+
+  /*!
+   * \brief Mesh deformation based on linear elasticity solver (CMeshSolver).
+   */
+  void Update();
+
+  /*!
+   * \brief Mesh deformation based on legacy implementation.
+   */
+  void Update_Legacy();
+
 };
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index b12d24154a9..b330c7fc343 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -29,7 +29,9 @@
 #include "../../include/drivers/CDeformationDriver.hpp"
 
 #include "../../../Common/include/geometry/CPhysicalGeometry.hpp"
+#include "../../../SU2_CFD/include/solvers/CMeshSolver.hpp"
 #include "../../../SU2_CFD/include/output/CMeshOutput.hpp"
+#include "../../../SU2_CFD/include/numerics/elasticity/CFEALinearElasticity.hpp"
 
 using namespace std;
 
@@ -76,6 +78,18 @@ CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
 
   Output_Preprocessing();
 
+  if (driver_config->GetDeform_Mesh()){
+
+    /*--- Preprocessing of the mesh solver for all zones. ---*/
+
+    Solver_Preprocessing();
+
+    /*--- Preprocessing of the mesh solver for all zones. ---*/
+
+    Numerics_Preprocessing();
+
+  }
+
   /*--- Preprocessing time is reported now, but not included in the next compute portion. ---*/
 
   StopTime = SU2_MPI::Wtime();
@@ -98,17 +112,22 @@ void CDeformationDriver::SetContainers_Null() {
         the SU2_DEF code. In general, the pointers are instantiated down a
         hierarchy over all zones as described in the comments below. ---*/
     config_container   = new CConfig*[nZone];
+    output_container   = new COutput*[nZone];
     geometry_container = new CGeometry*[nZone];
     surface_movement   = new CSurfaceMovement*[nZone];
     grid_movement      = new CVolumetricMovement*[nZone];
-    output_container   = new COutput*[nZone];
+
+    solver_container   = new CSolver*[nZone];
+    numerics_container = new CNumerics**[nZone];
 
     for (iZone = 0; iZone < nZone; iZone++) {
         config_container[iZone]       = nullptr;
+        output_container[iZone]       = nullptr;
         geometry_container[iZone]     = nullptr;
         surface_movement[iZone]       = nullptr;
         grid_movement[iZone]          = nullptr;
-        output_container[iZone]       = nullptr;
+        solver_container[iZone]       = nullptr;
+        numerics_container[iZone]     = nullptr;
     }
 }
 
@@ -137,10 +156,13 @@ void CDeformationDriver::Input_Preprocessing() {
         config_container[iZone]->SetMPICommunicator(SU2_MPI::GetComm());
     }
 
-      /*--- Set the multizone part of the problem. ---*/
+    /*--- Set the multizone part of the problem. ---*/
+
     if (driver_config->GetMultizone_Problem()){
         for (iZone = 0; iZone < nZone; iZone++) {
+
             /*--- Set the interface markers for multizone ---*/
+
             config_container[iZone]->SetMultizone(driver_config, config_container);
         }
     }
@@ -237,6 +259,30 @@ void CDeformationDriver::Output_Preprocessing() {
     }
 }
 
+void CDeformationDriver::Solver_Preprocessing() {
+
+  for (iZone = 0; iZone < nZone; iZone++) {
+    solver_container[iZone] = new CMeshSolver(geometry_container[iZone], config_container[iZone]);
+  }
+
+}
+
+void CDeformationDriver::Numerics_Preprocessing() {
+
+  for (iZone = 0; iZone < nZone; iZone++) {
+    numerics_container[iZone] = new CNumerics* [omp_get_num_threads() * MAX_TERMS]();
+
+    for (int thread = 0; thread < omp_get_max_threads(); ++thread) {
+        const int iTerm = FEA_TERM + thread * MAX_TERMS;
+        const int nDim = geometry_container[iZone]->GetnDim();
+
+        numerics_container[iZone][iTerm] = new CFEAMeshElasticity(nDim, nDim, geometry_container[iZone]->GetnElem(), config_container[iZone]);
+    }
+
+  }
+
+}
+
 void CDeformationDriver::Run() {
 
     /* --- Start measuring computation time ---*/
@@ -245,6 +291,47 @@ void CDeformationDriver::Run() {
 
     /*--- Surface grid deformation using design variables ---*/
 
+    if (driver_config->GetDeform_Mesh()) {
+        Update();
+    }
+    else {
+        Update_Legacy();
+    }
+
+    /*--- Synchronization point after a single solver iteration. Compute the
+      wall clock time required. ---*/
+
+    StopTime = SU2_MPI::Wtime();
+
+    UsedTimeCompute = StopTime-StartTime;
+    if (rank == MASTER_NODE) {
+      cout << "\nCompleted in " << fixed << UsedTimeCompute << " seconds on "<< size;
+
+      if (size == 1) cout << " core." << endl; else cout << " cores." << endl;
+    }
+
+    /*--- Output the deformed mesh ---*/
+    Output();
+
+}
+
+void CDeformationDriver::Update() {
+
+    for (iZone = 0; iZone < nZone; iZone++){
+
+    /*--- Set the stiffness of each element mesh into the mesh numerics ---*/
+
+    solver_container[iZone]->SetMesh_Stiffness(numerics_container[iZone], config_container[iZone]);
+
+    /*--- Deform the volume grid around the new boundary locations ---*/
+
+    solver_container[iZone]->DeformMesh(geometry_container[iZone], numerics_container[iZone], config_container[iZone]);
+
+    }
+}
+
+void CDeformationDriver::Update_Legacy() {
+
     for (iZone = 0; iZone < nZone; iZone++){
 
       if (config_container[iZone]->GetDesign_Variable(0) != NO_DEFORMATION) {
@@ -392,12 +479,14 @@ void CDeformationDriver::Run() {
 
     }
 
-    /*--- Computational grid preprocesing ---*/
+}
 
-    if (rank == MASTER_NODE) cout << endl << "----------------------- Write deformed grid files -----------------------" << endl;
+void CDeformationDriver::Output() {
 
     /*--- Output deformed grid for visualization, if requested (surface and volumetric), in parallel
-     requires to move all the data to the master node---*/
+          requires to move all the data to the master node---*/
+
+    if (rank == MASTER_NODE) cout << endl << "----------------------- Write deformed grid files -----------------------" << endl;
 
     for (iZone = 0; iZone < nZone; iZone++){
 
@@ -427,7 +516,7 @@ void CDeformationDriver::Run() {
       /*--- Set the file names for the visualization files ---*/
 
       output_container[iZone]->SetVolume_Filename("volume_deformed");
-      output_container[iZone]->SetSurface_Filename("surface_deformed");
+      output_container[iZone]->SetSurface_Filename("surfac  e_deformed");
 
       for (unsigned short iFile = 0; iFile < config_container[iZone]->GetnVolumeOutputFiles(); iFile++){
         auto FileFormat = config_container[iZone]->GetVolumeOutputFiles();
@@ -436,38 +525,47 @@ void CDeformationDriver::Run() {
       }
     }
 
-    if ((config_container[ZONE_0]->GetDesign_Variable(0) != NO_DEFORMATION) &&
-        (config_container[ZONE_0]->GetDesign_Variable(0) != SCALE_GRID)     &&
-        (config_container[ZONE_0]->GetDesign_Variable(0) != TRANSLATE_GRID) &&
-        (config_container[ZONE_0]->GetDesign_Variable(0) != ROTATE_GRID)) {
-
-      /*--- Write the the free-form deformation boxes after deformation. ---*/
-
-      if (rank == MASTER_NODE) cout << "Adding any FFD information to the SU2 file." << endl;
-
-      surface_movement[ZONE_0]->WriteFFDInfo(surface_movement, geometry_container, config_container);
+    if (!driver_config->GetDeform_Mesh()) {
+      if ((config_container[ZONE_0]->GetDesign_Variable(0) != NO_DEFORMATION) &&
+          (config_container[ZONE_0]->GetDesign_Variable(0) != SCALE_GRID)     &&
+          (config_container[ZONE_0]->GetDesign_Variable(0) != TRANSLATE_GRID) &&
+          (config_container[ZONE_0]->GetDesign_Variable(0) != ROTATE_GRID)) {
 
-    }
+          /*--- Write the the free-form deformation boxes after deformation. ---*/
 
-    /*--- Synchronization point after a single solver iteration. Compute the
-      wall clock time required. ---*/
+          if (rank == MASTER_NODE) cout << "Adding any FFD information to the SU2 file." << endl;
 
-    StopTime = SU2_MPI::Wtime();
+          surface_movement[ZONE_0]->WriteFFDInfo(surface_movement, geometry_container, config_container);
 
-    UsedTimeCompute = StopTime-StartTime;
-    if (rank == MASTER_NODE) {
-      cout << "\nCompleted in " << fixed << UsedTimeCompute << " seconds on "<< size;
-      if (size == 1) cout << " core." << endl; else cout << " cores." << endl;
     }
+  }
 }
 
 void CDeformationDriver::Postprocessing() {
+
     if (rank == MASTER_NODE)
       cout << endl <<"------------------------- Solver Postprocessing -------------------------" << endl;
 
     delete driver_config;
     driver_config = nullptr;
 
+    for (iZone = 0; iZone < nZone; iZone++) {
+      if (numerics_container[iZone] != nullptr) {
+        for (unsigned int iTerm = 0; iTerm < MAX_TERMS*omp_get_max_threads(); iTerm++) {
+          delete numerics_container[iZone][iTerm];
+        }
+        delete [] numerics_container[iZone];
+      }
+    }
+    delete [] numerics_container;
+    if (rank == MASTER_NODE) cout << "Deleted CNumerics container." << endl;
+
+    for (iZone = 0; iZone < nZone; iZone++) {
+      delete solver_container[iZone];
+    }
+    delete [] solver_container;
+    if (rank == MASTER_NODE) cout << "Deleted CSolver container." << endl;
+
     if (geometry_container != nullptr) {
       for (iZone = 0; iZone < nZone; iZone++) {
         if (geometry_container[iZone] != nullptr) {
@@ -506,6 +604,8 @@ void CDeformationDriver::Postprocessing() {
       }
       delete [] config_container;
     }
+    if (rank == MASTER_NODE) cout << "Deleted CConfig container." << endl;
+
     if (output_container != nullptr) {
       for (iZone = 0; iZone < nZone; iZone++) {
         if (output_container[iZone] != nullptr) {
@@ -514,8 +614,6 @@ void CDeformationDriver::Postprocessing() {
       }
       delete [] output_container;
     }
-    if (rank == MASTER_NODE) cout << "Deleted CConfig container." << endl;
-
     if (rank == MASTER_NODE) cout << "Deleted COutput class." << endl;
 
     /*--- Exit the solver cleanly ---*/
diff --git a/SU2_DEF/src/meson.build b/SU2_DEF/src/meson.build
index 0f19687b7bc..ecd2c2faf86 100644
--- a/SU2_DEF/src/meson.build
+++ b/SU2_DEF/src/meson.build
@@ -8,6 +8,11 @@ if get_option('enable-normal')
 
 su2_cfd_obj = su2_cfd_lib.extract_objects(['solvers/CSolver.cpp',
                                       'solvers/CBaselineSolver.cpp',
+                                      'solvers/CMeshSolver.cpp',
+                                      'solvers/CFEASolver.cpp',
+                                      'numerics/CNumerics.cpp',
+                                      'numerics/elasticity/CFEAElasticity.cpp',
+                                      'numerics/elasticity/CFEALinearElasticity.cpp',
                                       'CMarkerProfileReaderFVM.cpp',
                                       'output/COutput.cpp',
                                       'output/tools/CWindowingTools.cpp',
@@ -16,6 +21,11 @@ su2_cfd_obj = su2_cfd_lib.extract_objects(['solvers/CSolver.cpp',
                                       'output/CBaselineOutput.cpp',
                                       'variables/CBaselineVariable.cpp',
                                       'variables/CVariable.cpp',
+                                      'variables/CFEAVariable.cpp',
+                                      'variables/CFEABoundVariable.cpp',
+                                      'variables/CMeshElement.cpp',
+                                      'variables/CMeshVariable.cpp',
+                                      'variables/CMeshBoundVariable.cpp',
                                       'output/filewriter/CParallelDataSorter.cpp',
                                       'output/filewriter/CFVMDataSorter.cpp',
                                       'output/filewriter/CFEMDataSorter.cpp',

From c44014888000d625489c28fd0e04dec85b518a86 Mon Sep 17 00:00:00 2001
From: aa-g <aa.gastaldi@pm.me>
Date: Tue, 22 Jun 2021 20:53:48 +0200
Subject: [PATCH 007/656] Fix merge 29e45213f1c5c27db241da16665bebad41d20d4f

---
 SU2_CFD/src/solvers/CMeshSolver.cpp | 13 +++++++------
 1 file changed, 7 insertions(+), 6 deletions(-)

diff --git a/SU2_CFD/src/solvers/CMeshSolver.cpp b/SU2_CFD/src/solvers/CMeshSolver.cpp
index f51bda27186..b3605563473 100644
--- a/SU2_CFD/src/solvers/CMeshSolver.cpp
+++ b/SU2_CFD/src/solvers/CMeshSolver.cpp
@@ -586,16 +586,17 @@ void CMeshSolver::DeformMesh(CGeometry *geometry, CNumerics **numerics, CConfig
      of the linear system (usol contains the x, y, z displacements). ---*/
   UpdateGridCoord(geometry, config);
 
-  /*--- Update the dual grid. ---*/
-  UpdateDualGrid(geometry, config);
+  /*--- Update the dual grid (without multigrid). ---*/
+  geometry->InitiateComms(geometry, config, COORDINATES);
+  geometry->CompleteComms(geometry, config, COORDINATES);
+
+  geometry->SetControlVolume(config, UPDATE);
+  geometry->SetBoundControlVolume(config, UPDATE);
+  geometry->SetMaxLength(config);
 
   /*--- Check for failed deformation (negative volumes). ---*/
   SetMinMaxVolume(geometry, config, true);
 
-  /*--- The Grid Velocity is only computed if the problem is time domain ---*/
-  if (time_domain && !config->GetFSI_Simulation())
-    ComputeGridVelocity(geometry, config);
-
   }
   END_SU2_OMP_PARALLEL
 

From 169be9a4067cebc7495485069a72e21ce1930087 Mon Sep 17 00:00:00 2001
From: aa-g <aa.gastaldi@pm.me>
Date: Wed, 23 Jun 2021 00:43:00 +0200
Subject: [PATCH 008/656] Add marker- and vertex-data getters and setters (+
 minor fixes)

---
 .../include/drivers/CDeformationDriver.hpp    |  83 ++++++++
 SU2_DEF/src/SU2_DEF.cpp                       |   1 +
 SU2_DEF/src/drivers/CDeformationDriver.cpp    | 193 +++++++++++++++++-
 3 files changed, 276 insertions(+), 1 deletion(-)

diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index 2601f378ad8..cfb92560262 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -89,6 +89,89 @@ class CDeformationDriver {
    */
   void Postprocessing();
 
+  /*!
+   * \brief Get all the deformable boundary marker tags.
+   * \return List of deformable boundary markers tags.
+   */
+  vector<string> GetAllDeformMeshMarkersTag() const;
+
+  /*!
+   * \brief Get all the boundary markers tags with their associated indices.
+   * \return List of boundary markers tags with their indices.
+   */
+  map<string, int> GetAllBoundaryMarkers() const;
+
+  /*!
+   * \brief Get all the boundary markers tags with their associated types.
+   * \return List of boundary markers tags with their types.
+   */
+  map<string, string> GetAllBoundaryMarkersType() const;
+
+  /*!
+   * \brief Get the number of vertices (halo nodes included) from a specified marker.
+   * \param[in] iMarker -  Marker identifier.
+   * \return Number of vertices.
+   */
+  unsigned long GetNumberVertices(unsigned short iMarker) const;
+
+  /*!
+   * \brief Get the number of halo vertices from a specified marker.
+   * \param[in] iMarker - Marker identifier.
+   * \return Number of vertices.
+   */
+  unsigned long GetNumberHaloVertices(unsigned short iMarker) const;
+
+  /*!
+   * \brief Check if a vertex is physical or not (halo node) on a specified marker.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \return True if the specified vertex is a halo node.
+   */
+  bool IsAHaloNode(unsigned short iMarker, unsigned long iVertex) const;
+
+  /*!
+   * \brief Get the global index of a vertex on a specified marker.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \return Vertex global index.
+   */
+  unsigned long GetVertexGlobalIndex(unsigned short iMarker, unsigned long iVertex) const;
+
+  /*!
+   * \brief Get undeformed coordinates from the mesh solver.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \return x,y,z coordinates of the vertex.
+   */
+  vector<passivedouble> GetInitialMeshCoord(unsigned short iMarker, unsigned long iVertex) const;
+
+  /*!
+   * \brief Get the unit normal (vector) at a vertex on a specified marker.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \return Unit normal (vector) at the vertex.
+   */
+  vector<passivedouble> GetVertexNormal(unsigned short iMarker, unsigned long iVertex, bool unitNormal = false) const;
+
+  inline vector<passivedouble> GetVertexUnitNormal(unsigned short iMarker, unsigned long iVertex) const {
+    return GetVertexNormal(iMarker, iVertex, true);
+  }
+  
+  /*!
+   * \brief Set the mesh displacement for the elasticity mesh solver.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \param[in] DispX - Value of the mesh displacement in the direction X.
+   * \param[in] DispY - Value of the mesh displacement in the direction Y.
+   * \param[in] DispZ - Value of the mesh displacement in the direction Z.
+   */
+  void SetMeshDisplacement(unsigned short iMarker, unsigned long iVertex, passivedouble DispX, passivedouble DispY, passivedouble DispZ);
+
+  /*!
+   * \brief Communicate the boundary mesh displacements in a python call
+   */
+  void CommunicateMeshDisplacement(void);
+
 protected:
   /*!
    * \brief Init_Containers
diff --git a/SU2_DEF/src/SU2_DEF.cpp b/SU2_DEF/src/SU2_DEF.cpp
index ea0ce32bcb2..f383f2f7746 100644
--- a/SU2_DEF/src/SU2_DEF.cpp
+++ b/SU2_DEF/src/SU2_DEF.cpp
@@ -55,6 +55,7 @@ int main(int argc, char *argv[]) {
   else { strcpy(config_file_name, "default.cfg"); }
 
   /*--- Initialize the mesh deformation driver ---*/
+
   driver = new CDeformationDriver(config_file_name, comm);
 
   /*--- Launch the main external loop of the solver. ---*/
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index b330c7fc343..3f8d5ce71ac 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -29,6 +29,7 @@
 #include "../../include/drivers/CDeformationDriver.hpp"
 
 #include "../../../Common/include/geometry/CPhysicalGeometry.hpp"
+#include "../../../Common/include/toolboxes/geometry_toolbox.hpp"
 #include "../../../SU2_CFD/include/solvers/CMeshSolver.hpp"
 #include "../../../SU2_CFD/include/output/CMeshOutput.hpp"
 #include "../../../SU2_CFD/include/numerics/elasticity/CFEALinearElasticity.hpp"
@@ -516,7 +517,7 @@ void CDeformationDriver::Output() {
       /*--- Set the file names for the visualization files ---*/
 
       output_container[iZone]->SetVolume_Filename("volume_deformed");
-      output_container[iZone]->SetSurface_Filename("surfac  e_deformed");
+      output_container[iZone]->SetSurface_Filename("surface_deformed");
 
       for (unsigned short iFile = 0; iFile < config_container[iZone]->GetnVolumeOutputFiles(); iFile++){
         auto FileFormat = config_container[iZone]->GetVolumeOutputFiles();
@@ -621,3 +622,193 @@ void CDeformationDriver::Postprocessing() {
     if (rank == MASTER_NODE)
       cout << endl << "------------------------- Exit Success (SU2_DEF) ------------------------" << endl << endl;
 }
+
+vector<string> CDeformationDriver::GetAllDeformMeshMarkersTag() const {
+
+  vector<string> interfaceBoundariesTagList;
+  unsigned short iMarker, nBoundariesMarker;
+  string Marker_Tag;
+
+  nBoundariesMarker = config_container[ZONE_0]->GetnMarker_Deform_Mesh();
+  interfaceBoundariesTagList.resize(nBoundariesMarker);
+
+  for(iMarker=0; iMarker < nBoundariesMarker; iMarker++){
+    Marker_Tag = config_container[ZONE_0]->GetMarker_Deform_Mesh_TagBound(iMarker);
+    interfaceBoundariesTagList[iMarker] = Marker_Tag;
+  }
+
+  return interfaceBoundariesTagList;
+}
+
+map<string, int> CDeformationDriver::GetAllBoundaryMarkers() const {
+
+  map<string, int>  allBoundariesMap;
+  unsigned short iMarker, nBoundaryMarkers;
+  string Marker_Tag;
+
+  nBoundaryMarkers = config_container[ZONE_0]->GetnMarker_All();
+
+  for(iMarker=0; iMarker < nBoundaryMarkers; iMarker++){
+    Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
+    allBoundariesMap[Marker_Tag] = iMarker;
+  }
+
+  return allBoundariesMap;
+}
+
+map<string, string> CDeformationDriver::GetAllBoundaryMarkersType() const {
+
+  map<string, string> allBoundariesTypeMap;
+  unsigned short iMarker, KindBC;
+  string Marker_Tag, Marker_Type;
+
+  for(iMarker=0; iMarker < config_container[ZONE_0]->GetnMarker_All(); iMarker++){
+    Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
+    KindBC = config_container[ZONE_0]->GetMarker_All_KindBC(iMarker);
+    switch(KindBC){
+      case EULER_WALL:
+        Marker_Type = "EULER_WALL";
+        break;
+      case FAR_FIELD:
+        Marker_Type = "FARFIELD";
+        break;
+      case ISOTHERMAL:
+        Marker_Type = "ISOTHERMAL";
+        break;
+      case HEAT_FLUX:
+        Marker_Type = "HEATFLUX";
+        break;
+      case INLET_FLOW:
+        Marker_Type = "INLET_FLOW";
+        break;
+      case OUTLET_FLOW:
+        Marker_Type = "OUTLET_FLOW";
+        break;
+      case SYMMETRY_PLANE:
+        Marker_Type = "SYMMETRY";
+        break;
+      case SEND_RECEIVE:
+        Marker_Type = "SEND_RECEIVE";
+        break;
+      default:
+        Marker_Type = "UNKNOWN_TYPE";
+    }
+    allBoundariesTypeMap[Marker_Tag] = Marker_Type;
+  }
+
+  return allBoundariesTypeMap;
+}
+
+unsigned long CDeformationDriver::GetNumberVertices(unsigned short iMarker) const {
+
+  return geometry_container[ZONE_0]->nVertex[iMarker];
+
+}
+
+unsigned long CDeformationDriver::GetNumberHaloVertices(unsigned short iMarker) const {
+
+  unsigned long nHaloVertices, iVertex, iPoint;
+
+  nHaloVertices = 0;
+  for(iVertex = 0; iVertex < geometry_container[ZONE_0]->nVertex[iMarker]; iVertex++){
+    iPoint = geometry_container[ZONE_0]->vertex[iMarker][iVertex]->GetNode();
+    if(!(geometry_container[ZONE_0]->nodes->GetDomain(iPoint))) nHaloVertices += 1;
+  }
+
+  return nHaloVertices;
+
+}
+
+unsigned long CDeformationDriver::GetVertexGlobalIndex(unsigned short iMarker, unsigned long iVertex) const {
+
+  unsigned long iPoint, GlobalIndex;
+
+  iPoint = geometry_container[ZONE_0]->vertex[iMarker][iVertex]->GetNode();
+  GlobalIndex = geometry_container[ZONE_0]->nodes->GetGlobalIndex(iPoint);
+
+  return GlobalIndex;
+
+}
+
+bool CDeformationDriver::IsAHaloNode(unsigned short iMarker, unsigned long iVertex) const {
+
+  unsigned long iPoint;
+
+  iPoint = geometry_container[ZONE_0]->vertex[iMarker][iVertex]->GetNode();
+  if(geometry_container[ZONE_0]->nodes->GetDomain(iPoint)) return false;
+  else return true;
+
+}
+
+vector<passivedouble> CDeformationDriver::GetInitialMeshCoord(unsigned short iMarker, unsigned long iVertex) const {
+
+  vector<su2double> coord(3,0.0);
+  vector<passivedouble> coord_passive(3, 0.0);
+
+  auto iPoint = geometry_container[ZONE_0]->vertex[iMarker][iVertex]->GetNode();
+
+  for (auto iDim = 0 ; iDim < geometry_container[ZONE_0]->GetnDim(); iDim++){
+   coord[iDim] = solver_container[ZONE_0]->GetNodes()->GetMesh_Coord(iPoint,iDim);
+  }
+
+  coord_passive[0] = SU2_TYPE::GetValue(coord[0]);
+  coord_passive[1] = SU2_TYPE::GetValue(coord[1]);
+  coord_passive[2] = SU2_TYPE::GetValue(coord[2]);
+
+  return coord_passive;
+}
+
+vector<passivedouble> CDeformationDriver::GetVertexNormal(unsigned short iMarker, unsigned long iVertex, bool unitNormal) const {
+
+  int nDim = geometry_container[ZONE_0]->GetnDim();
+
+  su2double *Normal;
+  su2double Area;
+  vector<su2double> ret_Normal(3, 0.0);
+  vector<passivedouble> ret_Normal_passive(3, 0.0);
+
+  Normal = geometry_container[ZONE_0]->vertex[iMarker][iVertex]->GetNormal();
+
+  if (!unitNormal) {
+
+    ret_Normal_passive[0] = SU2_TYPE::GetValue(Normal[0]);
+    ret_Normal_passive[1] = SU2_TYPE::GetValue(Normal[1]);
+    if(nDim>2) ret_Normal_passive[2] = SU2_TYPE::GetValue(Normal[2]);
+
+    return ret_Normal_passive;
+  }
+
+  Area = GeometryToolbox::Norm(nDim, Normal);
+
+  ret_Normal[0] = Normal[0]/Area;
+  ret_Normal[1] = Normal[1]/Area;
+  if(nDim>2) ret_Normal[2] = Normal[2]/Area;
+
+  ret_Normal_passive[0] = SU2_TYPE::GetValue(ret_Normal[0]);
+  ret_Normal_passive[1] = SU2_TYPE::GetValue(ret_Normal[1]);
+  ret_Normal_passive[2] = SU2_TYPE::GetValue(ret_Normal[2]);
+
+  return ret_Normal_passive;
+}
+
+void CDeformationDriver::SetMeshDisplacement(unsigned short iMarker, unsigned long iVertex, passivedouble DispX, passivedouble DispY, passivedouble DispZ) {
+
+  unsigned long iPoint;
+  su2double MeshDispl[3] =  {0.0,0.0,0.0};
+
+  MeshDispl[0] = DispX;
+  MeshDispl[1] = DispY;
+  MeshDispl[2] = DispZ;
+
+  iPoint = geometry_container[ZONE_0]->vertex[iMarker][iVertex]->GetNode();
+
+  solver_container[ZONE_0]->GetNodes()->SetBound_Disp(iPoint, MeshDispl);
+
+}
+
+void CDeformationDriver::CommunicateMeshDisplacement(void) {
+
+  solver_container[ZONE_0]->InitiateComms(geometry_container[ZONE_0], config_container[ZONE_0], MESH_DISPLACEMENTS);
+  solver_container[ZONE_0]->CompleteComms(geometry_container[ZONE_0], config_container[ZONE_0], MESH_DISPLACEMENTS);
+
+}

From e818703eaa73ae9cc5bfe78bcf20a19b69b57aa7 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Tue, 22 Jun 2021 17:20:16 -0400
Subject: [PATCH 009/656] Remove nullptr checks, update AD register input code,
 minor code fixes

---
 .../drivers/CDiscAdjDeformationDriver.hpp     |  4 -
 SU2_DEF/src/drivers/CDeformationDriver.cpp    | 96 +++++++++----------
 .../src/drivers/CDiscAdjDeformationDriver.cpp | 30 ++----
 3 files changed, 50 insertions(+), 80 deletions(-)

diff --git a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
index f3635ab694b..7901776a9f1 100644
--- a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
@@ -27,12 +27,8 @@
 
 #pragma once
 
-#define ENABLE_MAPS
 #include "../../../Common/include/CConfig.hpp"
-#undef ENABLE_MAPS
-
 #include "../../../Common/include/parallelization/mpi_structure.hpp"
-
 #include "../../../Common/include/geometry/CGeometry.hpp"
 #include "../../../Common/include/fem/fem_geometry_structure.hpp"
 #include "../../../Common/include/grid_movement/CSurfaceMovement.hpp"
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 3f8d5ce71ac..8c8155dfaa5 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -173,70 +173,70 @@ void CDeformationDriver::Geometrical_Preprocessing() {
 
     for (iZone = 0; iZone < nZone; iZone++) {
 
-    /*--- Definition of the geometry class to store the primal grid in the partitioning process. ---*/
+      /*--- Definition of the geometry class to store the primal grid in the partitioning process. ---*/
 
-    CGeometry *geometry_aux = nullptr;
+      CGeometry *geometry_aux = nullptr;
 
-    /*--- All ranks process the grid and call ParMETIS for partitioning ---*/
+      /*--- All ranks process the grid and call ParMETIS for partitioning ---*/
 
-    geometry_aux = new CPhysicalGeometry(config_container[iZone], iZone, nZone);
+      geometry_aux = new CPhysicalGeometry(config_container[iZone], iZone, nZone);
 
-    /*--- Color the initial grid and set the send-receive domains (ParMETIS) ---*/
+      /*--- Color the initial grid and set the send-receive domains (ParMETIS) ---*/
 
-    geometry_aux->SetColorGrid_Parallel(config_container[iZone]);
+      geometry_aux->SetColorGrid_Parallel(config_container[iZone]);
 
-    /*--- Build the grid data structures using the ParMETIS coloring. ---*/
+      /*--- Build the grid data structures using the ParMETIS coloring. ---*/
 
-    geometry_container[iZone] = new CPhysicalGeometry(geometry_aux, config_container[iZone]);
+      geometry_container[iZone] = new CPhysicalGeometry(geometry_aux, config_container[iZone]);
 
-    /*--- Deallocate the memory of geometry_aux ---*/
+      /*--- Deallocate the memory of geometry_aux ---*/
 
-    delete geometry_aux;
+      delete geometry_aux;
 
-    /*--- Add the Send/Receive boundaries ---*/
+      /*--- Add the Send/Receive boundaries ---*/
 
-    geometry_container[iZone]->SetSendReceive(config_container[iZone]);
+      geometry_container[iZone]->SetSendReceive(config_container[iZone]);
 
-    /*--- Add the Send/Receive boundaries ---*/
+      /*--- Add the Send/Receive boundaries ---*/
 
-    geometry_container[iZone]->SetBoundaries(config_container[iZone]);
+      geometry_container[iZone]->SetBoundaries(config_container[iZone]);
 
-    /*--- Computational grid preprocesing ---*/
+      /*--- Computational grid preprocesing ---*/
 
-    if (rank == MASTER_NODE) cout << endl << "----------------------- Preprocessing computations ----------------------" << endl;
+      if (rank == MASTER_NODE) cout << endl << "----------------------- Preprocessing computations ----------------------" << endl;
 
-    /*--- Compute elements surrounding points, points surrounding points ---*/
+      /*--- Compute elements surrounding points, points surrounding points ---*/
 
-    if (rank == MASTER_NODE) cout << "Setting local point connectivity." <<endl;
-    geometry_container[iZone]->SetPoint_Connectivity();
+      if (rank == MASTER_NODE) cout << "Setting local point connectivity." <<endl;
+      geometry_container[iZone]->SetPoint_Connectivity();
 
-    /*--- Check the orientation before computing geometrical quantities ---*/
+      /*--- Check the orientation before computing geometrical quantities ---*/
 
-    geometry_container[iZone]->SetBoundVolume();
-    if (config_container[iZone]->GetReorientElements()) {
-    if (rank == MASTER_NODE) cout << "Checking the numerical grid orientation of the interior elements." <<endl;
-        geometry_container[iZone]->Check_IntElem_Orientation(config_container[iZone]);
-        geometry_container[iZone]->Check_BoundElem_Orientation(config_container[iZone]);
-    }
+      geometry_container[iZone]->SetBoundVolume();
+      if (config_container[iZone]->GetReorientElements()) {
+      if (rank == MASTER_NODE) cout << "Checking the numerical grid orientation of the interior elements." <<endl;
+          geometry_container[iZone]->Check_IntElem_Orientation(config_container[iZone]);
+          geometry_container[iZone]->Check_BoundElem_Orientation(config_container[iZone]);
+      }
 
-    /*--- Create the edge structure ---*/
+      /*--- Create the edge structure ---*/
 
-    if (rank == MASTER_NODE) cout << "Identify edges and vertices." <<endl;
-    geometry_container[iZone]->SetEdges();
-    geometry_container[iZone]->SetVertex(config_container[iZone]);
+      if (rank == MASTER_NODE) cout << "Identify edges and vertices." <<endl;
+      geometry_container[iZone]->SetEdges();
+      geometry_container[iZone]->SetVertex(config_container[iZone]);
 
-    if (config_container[iZone]->GetDesign_Variable(0) != NO_DEFORMATION) {
+      if (config_container[iZone]->GetDesign_Variable(0) != NO_DEFORMATION) {
 
-        /*--- Create the dual control volume structures ---*/
+          /*--- Create the dual control volume structures ---*/
 
-        if (rank == MASTER_NODE) cout << "Setting the bound control volume structure." << endl;
-        geometry_container[iZone]->SetControlVolume(config_container[iZone], ALLOCATE);
-        geometry_container[iZone]->SetBoundControlVolume(config_container[iZone], ALLOCATE);
-    }
+          if (rank == MASTER_NODE) cout << "Setting the bound control volume structure." << endl;
+          geometry_container[iZone]->SetControlVolume(config_container[iZone], ALLOCATE);
+          geometry_container[iZone]->SetBoundControlVolume(config_container[iZone], ALLOCATE);
+      }
 
-    /*--- Create the point-to-point MPI communication structures. ---*/
+      /*--- Create the point-to-point MPI communication structures. ---*/
 
-    geometry_container[iZone]->PreprocessP2PComms(geometry_container[iZone], config_container[iZone]);
+      geometry_container[iZone]->PreprocessP2PComms(geometry_container[iZone], config_container[iZone]);
 
     }
 }
@@ -569,9 +569,7 @@ void CDeformationDriver::Postprocessing() {
 
     if (geometry_container != nullptr) {
       for (iZone = 0; iZone < nZone; iZone++) {
-        if (geometry_container[iZone] != nullptr) {
-          delete geometry_container[iZone];
-        }
+        delete geometry_container[iZone];
       }
       delete [] geometry_container;
     }
@@ -579,9 +577,7 @@ void CDeformationDriver::Postprocessing() {
 
     if (surface_movement != nullptr) {
       for (iZone = 0; iZone < nZone; iZone++) {
-        if (surface_movement[iZone] != nullptr) {
-          delete surface_movement[iZone];
-        }
+        delete surface_movement[iZone];
       }
       delete [] surface_movement;
     }
@@ -589,9 +585,7 @@ void CDeformationDriver::Postprocessing() {
 
     if (grid_movement != nullptr) {
       for (iZone = 0; iZone < nZone; iZone++) {
-        if (grid_movement[iZone] != nullptr) {
-          delete grid_movement[iZone];
-        }
+        delete grid_movement[iZone];
       }
       delete [] grid_movement;
     }
@@ -599,9 +593,7 @@ void CDeformationDriver::Postprocessing() {
 
     if (config_container != nullptr) {
       for (iZone = 0; iZone < nZone; iZone++) {
-        if (config_container[iZone] != nullptr) {
-          delete config_container[iZone];
-        }
+        delete config_container[iZone];
       }
       delete [] config_container;
     }
@@ -609,9 +601,7 @@ void CDeformationDriver::Postprocessing() {
 
     if (output_container != nullptr) {
       for (iZone = 0; iZone < nZone; iZone++) {
-        if (output_container[iZone] != nullptr) {
-          delete output_container[iZone];
-        }
+        delete output_container[iZone];
       }
       delete [] output_container;
     }
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index 923901fee8b..f95c9f36455 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -358,9 +358,7 @@ void CDiscAdjDeformationDriver::Postprocessing() {
         for (iZone = 0; iZone < nZone; iZone++) {
             if (geometry_container[iZone] != nullptr) {
                 for (iInst = 0; iInst < nInst[iZone]; iInst++){
-                    if (geometry_container[iZone][iInst] != nullptr) {
-                        delete geometry_container[iZone][iInst];
-                    }
+                    delete geometry_container[iZone][iInst];
                 }
                 delete geometry_container[iZone];
             }
@@ -371,9 +369,7 @@ void CDiscAdjDeformationDriver::Postprocessing() {
 
     if (surface_movement != nullptr) {
         for (iZone = 0; iZone < nZone; iZone++) {
-            if (surface_movement[iZone] != nullptr) {
-                delete surface_movement[iZone];
-            }
+            delete surface_movement[iZone];
         }
         delete [] surface_movement;
     }
@@ -381,9 +377,7 @@ void CDiscAdjDeformationDriver::Postprocessing() {
 
     if (grid_movement != nullptr) {
         for (iZone = 0; iZone < nZone; iZone++) {
-            if (grid_movement[iZone] != nullptr) {
-                delete grid_movement[iZone];
-            }
+            delete grid_movement[iZone];
         }
         delete [] grid_movement;
     }
@@ -391,9 +385,7 @@ void CDiscAdjDeformationDriver::Postprocessing() {
 
     if (config_container != nullptr) {
         for (iZone = 0; iZone < nZone; iZone++) {
-            if (config_container[iZone] != nullptr) {
-                delete config_container[iZone];
-            }
+            delete config_container[iZone];
         }
         delete [] config_container;
     }
@@ -683,21 +675,13 @@ void CDiscAdjDeformationDriver::SetDiscAdjDeformation_AD(CGeometry *geometry, CC
   /*--- Register design variables as input and set them to zero
    * (since we want to have the derivative at alpha = 0, i.e. for the current design) ---*/
 
-
-
   for (iDV = 0; iDV < nDV; iDV++){
 
-    nDV_Value =  config->GetnDV_Value(iDV);
-
-    for (iDV_Value = 0; iDV_Value < nDV_Value; iDV_Value++){
-
-      /*--- Initilization with su2double resets the index ---*/
-
-      DV_Value = 0.0;
+    for (iDV_Value = 0; iDV_Value < config->GetnDV_Value(iDV); iDV_Value++){
 
-      AD::RegisterInput(DV_Value);
+      config->SetDV_Value(iDV, iDV_Value, 0.0);
 
-      config->SetDV_Value(iDV, iDV_Value, DV_Value);
+      AD::RegisterInput(config->GetDV_Value(iDV, iDV_Value));
     }
   }
 

From 31c969e16507ae80d69105ea8c9190071d54a08d Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Tue, 22 Jun 2021 17:40:55 -0400
Subject: [PATCH 010/656] Simplify cfd and cfd_ad library links

---
 SU2_DEF/src/meson.build | 67 ++---------------------------------------
 1 file changed, 2 insertions(+), 65 deletions(-)

diff --git a/SU2_DEF/src/meson.build b/SU2_DEF/src/meson.build
index ecd2c2faf86..f7edd9f0a19 100644
--- a/SU2_DEF/src/meson.build
+++ b/SU2_DEF/src/meson.build
@@ -6,44 +6,7 @@ su2_def_src = files([
 ])
 if get_option('enable-normal')
 
-su2_cfd_obj = su2_cfd_lib.extract_objects(['solvers/CSolver.cpp',
-                                      'solvers/CBaselineSolver.cpp',
-                                      'solvers/CMeshSolver.cpp',
-                                      'solvers/CFEASolver.cpp',
-                                      'numerics/CNumerics.cpp',
-                                      'numerics/elasticity/CFEAElasticity.cpp',
-                                      'numerics/elasticity/CFEALinearElasticity.cpp',
-                                      'CMarkerProfileReaderFVM.cpp',
-                                      'output/COutput.cpp',
-                                      'output/tools/CWindowingTools.cpp',
-                                      'output/CMeshOutput.cpp',
-                                      'output/output_structure_legacy.cpp',
-                                      'output/CBaselineOutput.cpp',
-                                      'variables/CBaselineVariable.cpp',
-                                      'variables/CVariable.cpp',
-                                      'variables/CFEAVariable.cpp',
-                                      'variables/CFEABoundVariable.cpp',
-                                      'variables/CMeshElement.cpp',
-                                      'variables/CMeshVariable.cpp',
-                                      'variables/CMeshBoundVariable.cpp',
-                                      'output/filewriter/CParallelDataSorter.cpp',
-                                      'output/filewriter/CFVMDataSorter.cpp',
-                                      'output/filewriter/CFEMDataSorter.cpp',
-                                      'output/filewriter/CSurfaceFEMDataSorter.cpp',
-                                      'output/filewriter/CSurfaceFVMDataSorter.cpp',
-                                      'output/filewriter/CParallelFileWriter.cpp',
-                                      'output/filewriter/CParaviewFileWriter.cpp',
-                                      'output/filewriter/CParaviewBinaryFileWriter.cpp',
-                                      'output/filewriter/CTecplotFileWriter.cpp',
-                                      'output/filewriter/CTecplotBinaryFileWriter.cpp',
-                                      'output/filewriter/CCSVFileWriter.cpp',
-                                      'output/filewriter/CSTLFileWriter.cpp',
-                                      'output/filewriter/CSU2FileWriter.cpp',
-                                      'output/filewriter/CSU2BinaryFileWriter.cpp',
-                                      'output/filewriter/CParaviewXMLFileWriter.cpp',
-                                      'output/filewriter/CParaviewVTMFileWriter.cpp',
-                                      'output/filewriter/CSU2MeshFileWriter.cpp',
-                                      'limiters/CLimiterDetails.cpp'])
+su2_cfd_obj = su2_cfd_lib.extract_all_objects()
 
   su2_def_lib = static_library('SU2core_DEF',
                                su2_def_src,
@@ -63,33 +26,7 @@ su2_cfd_obj = su2_cfd_lib.extract_objects(['solvers/CSolver.cpp',
 endif
 
 if get_option('enable-autodiff')
-su2_cfd_obj_ad = su2_cfd_lib_ad.extract_objects(['solvers/CSolver.cpp',
-                                                 'solvers/CBaselineSolver.cpp',
-                                                 'CMarkerProfileReaderFVM.cpp',
-                                                 'output/COutput.cpp',
-                                                 'output/tools/CWindowingTools.cpp',
-                                                 'output/output_structure_legacy.cpp',
-                                                 'output/CBaselineOutput.cpp',
-                                                 'output/filewriter/CParallelDataSorter.cpp',
-                                                 'output/filewriter/CParallelFileWriter.cpp',
-                                                 'output/filewriter/CFEMDataSorter.cpp',
-                                                 'output/filewriter/CSurfaceFEMDataSorter.cpp',
-                                                 'output/filewriter/CFVMDataSorter.cpp',
-                                                 'output/filewriter/CSurfaceFVMDataSorter.cpp',
-                                                 'output/filewriter/CCSVFileWriter.cpp',
-                                                 'output/filewriter/CSTLFileWriter.cpp',
-                                                 'output/filewriter/CTecplotFileWriter.cpp',
-                                                 'output/filewriter/CTecplotBinaryFileWriter.cpp',
-                                                 'output/filewriter/CParaviewFileWriter.cpp',
-                                                 'output/filewriter/CParaviewBinaryFileWriter.cpp',
-                                                 'output/filewriter/CSU2FileWriter.cpp',
-                                                 'output/filewriter/CSU2BinaryFileWriter.cpp',
-                                                 'output/filewriter/CSU2MeshFileWriter.cpp',
-                                                 'output/filewriter/CParaviewXMLFileWriter.cpp',
-                                                 'output/filewriter/CParaviewVTMFileWriter.cpp',
-                                                 'variables/CBaselineVariable.cpp',
-                                                 'variables/CVariable.cpp',
-                                                 'limiters/CLimiterDetails.cpp'])
+su2_cfd_obj_ad = su2_cfd_lib_ad.extract_all_objects()
 
   su2_def_lib_ad = static_library('SU2core_DEF_AD',
                                   su2_def_src,

From fd959313969af95c06b6057f003bcdd9869ed447 Mon Sep 17 00:00:00 2001
From: Harsh Patel <51417692+patelha57@users.noreply.github.com>
Date: Mon, 28 Jun 2021 10:55:13 -0400
Subject: [PATCH 011/656] Remove redundant nullptr in CDeformationDriver

Co-authored-by: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
---
 SU2_DEF/src/drivers/CDeformationDriver.cpp | 1 -
 1 file changed, 1 deletion(-)

diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 8c8155dfaa5..c95c45493be 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -54,7 +54,6 @@ CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
   strcpy(config_file_name, confFile);
 
   /*--- Initialize the configuration of the driver ---*/
-  driver_config = nullptr;
   driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DEF);
 
   nZone = driver_config->GetnZone();

From 90dbc0da26f37b22be01723b9cc4e96e5ad10da4 Mon Sep 17 00:00:00 2001
From: aa-g <aa.gastaldi@pm.me>
Date: Tue, 25 Jan 2022 17:55:31 +0100
Subject: [PATCH 012/656] Merge develop

---
 externals/meson | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/externals/meson b/externals/meson
index 41c650a040d..29ef4478df6 160000
--- a/externals/meson
+++ b/externals/meson
@@ -1 +1 @@
-Subproject commit 41c650a040d50e0912d268af7a903a9ce1456dfa
+Subproject commit 29ef4478df6d3aaca40c7993f125b29409be1de2

From 1e2b91fe7c099a9587bf2df958d4702d83ce76ef Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Sun, 13 Feb 2022 23:34:48 -0800
Subject: [PATCH 013/656] Updates for PR1300

---
 Common/include/drivers/CDriverBase.hpp        |  343 ++++
 Common/src/drivers/CDriverBase.cpp            |  547 ++++++
 Common/src/drivers/meson.build                |    1 +
 Common/src/meson.build                        |    1 +
 SU2_CFD/include/drivers/CDriver.hpp           | 1661 ++++++++---------
 SU2_CFD/src/drivers/CDriver.cpp               |    3 +-
 SU2_CFD/src/python_wrapper_structure.cpp      |  197 --
 .../include/drivers/CDeformationDriver.hpp    |  115 +-
 .../drivers/CDiscAdjDeformationDriver.hpp     |  225 +--
 SU2_DEF/src/drivers/CDeformationDriver.cpp    | 1092 +++++------
 .../src/drivers/CDiscAdjDeformationDriver.cpp | 1395 +++++++-------
 SU2_DOT/include/SU2_DOT.hpp                   |   69 +-
 SU2_DOT/src/SU2_DOT.cpp                       | 1060 +----------
 SU2_PY/pySU2/pySU2.i                          |    1 +
 SU2_PY/pySU2/pySU2ad.i                        |    1 +
 15 files changed, 3035 insertions(+), 3676 deletions(-)
 create mode 100644 Common/include/drivers/CDriverBase.hpp
 create mode 100644 Common/src/drivers/CDriverBase.cpp
 create mode 100644 Common/src/drivers/meson.build

diff --git a/Common/include/drivers/CDriverBase.hpp b/Common/include/drivers/CDriverBase.hpp
new file mode 100644
index 00000000000..7291411e397
--- /dev/null
+++ b/Common/include/drivers/CDriverBase.hpp
@@ -0,0 +1,343 @@
+/*!
+ * \file CDriverBase.hpp
+ * \brief Base class template for all drivers.
+ * \author H. Patel, A. Gastaldi
+ * \version 7.3.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2021, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+
+#pragma once
+
+#include "../CConfig.hpp"
+#include "../../../SU2_CFD/include/numerics/CNumerics.hpp"
+#include "../../../SU2_CFD/include/solvers/CSolver.hpp"
+#include "../../../SU2_CFD/include/output/COutput.hpp"
+
+class CDriverBase {
+    
+protected:
+    
+    int rank,                                       /*!< \brief MPI Rank. */
+    size;                                           /*!< \brief MPI Size. */
+    char* config_file_name;                         /*!< \brief Configuration file name of the problem.*/
+    
+    su2double StartTime,                            /*!< \brief Start point of the timer for performance benchmarking.*/
+    StopTime,                                       /*!< \brief Stop point of the timer for performance benchmarking.*/
+    UsedTimePreproc,                                /*!< \brief Elapsed time between Start and Stop point of the timer for tracking preprocessing phase.*/
+    UsedTimeCompute,                                /*!< \brief Elapsed time between Start and Stop point of the timer for tracking compute phase.*/
+    UsedTime;                                       /*!< \brief Elapsed time between Start and Stop point of the timer.*/
+    
+    unsigned long TimeIter;
+    
+    unsigned short iMesh,                           /*!< \brief Iterator on mesh levels.*/
+    iZone,                                          /*!< \brief Iterator on zones.*/
+    nZone,                                          /*!< \brief Total number of zones in the problem. */
+    nDim,                                           /*!< \brief Number of dimensions.*/
+    iInst,                                          /*!< \brief Iterator on instance levels.*/
+    *nInst,                                         /*!< \brief Total number of instances in the problem (per zone). */
+    **interface_types;                              /*!< \brief Type of coupling between the distinct (physical) zones.*/
+    
+    CConfig **config_container;                     /*!< \brief Definition of the particular problem. */
+    CConfig *driver_config;                         /*!< \brief Definition of the driver configuration. */
+    COutput **output_container;                     /*!< \brief Pointer to the COutput class. */
+    COutput *driver_output;                         /*!< \brief Definition of the driver output. */
+    CGeometry ****geometry_container;               /*!< \brief Geometrical definition of the problem. */
+    CSolver *****solver_container;                  /*!< \brief Container vector with all the solutions. */
+    CNumerics ******numerics_container;             /*!< \brief Description of the numerical method (the way in which the equations are solved). */
+    CSurfaceMovement **surface_movement;            /*!< \brief Surface movement classes of the problem. */
+    CVolumetricMovement ***grid_movement;           /*!< \brief Volume grid movement classes of the problem. */
+    CFreeFormDefBox*** FFDBox;                      /*!< \brief FFD FFDBoxes of the problem. */
+    
+public:
+    
+    /*!
+     * \brief Constructor of the class.
+     * \param[in] confFile - Configuration file name.
+     * \param[in] val_nZone - Total number of zones.
+     * \param[in] MPICommunicator - MPI communicator for SU2.
+     */
+    CDriverBase(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator);
+    
+    /*!
+     * \brief Destructor of the class.
+     */
+    ~CDriverBase(void);
+    
+    /*!
+     * \brief A virtual member.
+     */
+    virtual void Preprocessing() {};
+    
+    /*!
+     * \brief A virtual member.
+     */
+    virtual void Run() {};
+    
+    /*!
+     * \brief A virtual member.
+     */
+    virtual void Update() {};
+    
+    /*!
+     * \brief A virtual member.
+     */
+    virtual void Update_Legacy() {};
+    
+    /*!
+     * \brief A virtual member.
+     */
+    virtual void Output() {};
+    
+    /*!
+     * \brief A virtual member.
+     */
+    virtual void Postprocessing() {};
+    
+    /*!
+     * \brief Get all the boundary markers tags with their associated indices.
+     * \return List of boundary markers tags with their indices.
+     */
+    map<string, int> GetBoundaryMarkerIndices() const;
+    
+    /*!
+     * \brief Get all the boundary markers tags with their associated types.
+     * \return List of boundary markers tags with their types.
+     */
+    map<string, string> GetBoundaryMarkerTypes() const;
+    
+    /*!
+     * \brief Get all the deformable boundary marker tags.
+     * \return List of deformable boundary markers tags.
+     */
+    vector<string> GetDeformableMarkerTags() const;
+    
+    /*!
+     * \brief Get the number of mesh dimensions.
+     * \return Number of dimensions.
+     */
+    unsigned long GetNumberDimensions() const;
+    
+    /*!
+     * \brief Get the number of mesh elements.
+     * \return Number of elements.
+     */
+    unsigned long GetNumberElements() const;
+    
+    /*!
+     * \brief Get the number of mesh elements from a specified marker.
+     * \param[in] iMarker - Marker identifier.
+     * \return Number of elements.
+     */
+    unsigned long GetNumberElementsMarker(unsigned short iMarker) const;
+    
+    /*!
+     * \brief Get the number of mesh vertices.
+     * \return Number of vertices.
+     */
+    unsigned long GetNumberVertices() const;
+    
+    /*!
+     * \brief Get the number of mesh vertices from a specified marker.
+     * \param[in] iMarker - Marker identifier.
+     * \return Number of vertices.
+     */
+    unsigned long GetNumberVerticesMarker(unsigned short iMarker) const;
+    
+    /*!
+     * \brief Get the number of halo mesh vertices.
+     * \return Number of vertices.
+     */
+    unsigned long GetNumberHaloVertices() const;
+    
+    /*!
+     * \brief Get the number of halo mesh vertices from a specified marker.
+     * \param[in] iMarker - Marker identifier.
+     * \return Number of vertices.
+     */
+    unsigned long GetNumberHaloVerticesMarker(unsigned short iMarker) const;
+    
+    /*!
+     * \brief Get global IDs of mesh vertices.
+     * \return Global vertex IDs.
+     */
+    vector<unsigned long> GetVertexIDs() const;
+    
+    /*!
+     * \brief Get global IDs of mesh vertices.
+     * \param[in] iMarker - Marker identifier.
+     * \return Global vertex IDs.
+     */
+    vector<unsigned long> GetVertexIDsMarker(unsigned short iMarker) const;
+    
+    /*!
+     * \brief Get global IDs of mesh elements.
+     * \return Global element IDs.
+     */
+    vector<unsigned long> GetElementIDs() const;
+    
+    /*!
+     * \brief Get global IDs of mesh elements.
+     * \param[in] iMarker - Marker identifier.
+     * \return Global element IDs.
+     */
+    vector<unsigned long> GetElementIDsMarker(unsigned short iMarker) const;
+    
+    /*!
+     * \brief Get the connected point IDs of mesh elements.
+     * \return Element connectivities (nElem, nNode)
+     */
+    vector<vector<unsigned long>> GetConnectivity() const;
+    
+    /*!
+     * \brief Get the connected point IDs of mesh elements on a specified marker.
+     * \param[in] iMarker - Marker identifier.
+     * \return Element connectivities (nBound, nNode).
+     */
+    vector<vector<unsigned long>> GetConnectivityMarker(unsigned short iMarker) const;
+    
+    /*!
+     * \brief Get halo node stauts of mesh vertices.
+     * \return Point domain status.
+     */
+    vector<bool> GetDomain() const;
+    
+    /*!
+     * \brief Get halo node stauts of mesh marker vertices.
+     * \param[in] iMarker - Marker identifier.
+     * \return Point domain status.
+     */
+    vector<bool> GetDomainMarker(unsigned short iMarker) const;
+    
+    /*!
+     * \brief Get the coordinates of the mesh points.
+     * \return Point coordinates (nPoint*nDim).
+     */
+    vector<passivedouble> GetCoordinates() const;
+    
+    /*!
+     * \brief Get the coordinates of the mesh points on the specified marker.
+     * \param[in] iMarker - Marker identifier.
+     * \return Point coordinates (nVertex*nDim).
+     */
+    vector<passivedouble> GetCoordinatesMarker(unsigned short iMarker) const;
+    
+    /*!
+     * \brief Set the coordinates of the mesh points.
+     * \param[in] values - Point coordinates (nPoint*nDim).
+     */
+    void SetCoordinates(vector<passivedouble> values);
+    
+    /*!
+     * \brief Set the coordinates of the mesh points on the specified marker.
+     * \param[in] iMarker - Marker identifier.
+     * \param[in] values - Point coordinates (nVertex*nDim).
+     */
+    void SetCoordinatesMarker(unsigned short iMarker, vector<passivedouble> values);
+    
+    /*!
+     * \brief Get the vertex displacements on the specified marker.
+     * \param[in] iMarker - Marker identifier.
+     * \return Vertex displacements (nVertex*nDim).
+     */
+    vector<passivedouble> GetDisplacementsMarker(unsigned short iMarker) const;
+    
+    /*!
+     * \brief Set the vertex displacements on the specified marker.
+     * \param[in] iMarker - Marker identifier.
+     * \param[in] values - Vertex displacements (nVertex*nDim).
+     */
+    void SetDisplacementsMarker(unsigned short iMarker, vector<passivedouble> values);
+    
+    /*!
+     * \brief Get the vertex velocities on the specified marker.
+     * \param[in] iMarker - Marker identifier.
+     * \return Vertex velocities (nVertex*nDim).
+     */
+    vector<passivedouble> GetVelocitiesMarker(unsigned short iMarker) const;
+    
+    /*!
+     * \brief Set the vertex velocities on the specified marker.
+     * \param[in] iMarker - Marker identifier.
+     * \param[in] values - Vertex velocities (nVertex*nDim).
+     */
+    void SetVelocitiesMarker(unsigned short iMarker, vector<passivedouble> values);
+    
+    /*!
+     * \brief Get undeformed coordinates from mesh solver on the specified marker.
+     * \param[in] iMarker - Marker identifier.
+     * \return Initial point coordinates (nVertex*nDim).
+     */
+    vector<passivedouble> GetInitialCoordinatesMarker(unsigned short iMarker) const;
+    
+    /*!
+     * \brief Get the vertex normal vectors on the specified marker.
+     * \param[in] iMarker - Marker identifier.
+     * \param[in] UnitNormal - Boolean to indicate if unit normal vector should be returned.
+     * \return Normal vector at the vertex (nVertex*nDim).
+     */
+    vector<passivedouble> GetVertexNormalsMarker(unsigned short iMarker, bool UnitNormal = false) const;
+    
+    /*!
+     * \brief Communicate the boundary mesh displacements in a python call
+     */
+    void CommunicateMeshDisplacements(void);
+    
+protected:
+    
+    /*!
+     * \brief Initialize Containers
+     */
+    void SetContainers_Null();
+    
+    /*!
+     * \brief Read in the config and mesh files.
+     */
+    void Input_Preprocessing(CConfig **&config, CConfig *&driver_config);
+    
+    /*!
+     * \brief Construction of the edge-based data structure and the multigrid structure.
+     */
+    void Geometrical_Preprocessing(CConfig *config, CGeometry **&geometry, bool dummy);
+    
+    /*!
+     * \brief Definition and allocation of all solution classes.
+     * \param[in] solver_container - Container vector with all the solutions.
+     * \param[in] geometry - Geometrical definition of the problem.
+     * \param[in] config - Definition of the particular problem.
+     */
+    void Solver_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***&solver);
+    
+    /*!
+     * \brief Definition and allocation of all solver classes.
+     * \param[in] numerics_container - Description of the numerical method (the way in which the equations are solved).
+     * \param[in] geometry - Geometrical definition of the problem.
+     * \param[in] solver_container - Container vector with all the solutions.
+     * \param[in] config - Definition of the particular problem.
+     */
+    void Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***solver, CNumerics ****&numerics) const;
+    
+    /*!
+     * \brief Preprocess the output container.
+     */
+    void Output_Preprocessing(CConfig **config, CConfig *driver_config, COutput **&output_container, COutput *&driver_output);
+    
+};
diff --git a/Common/src/drivers/CDriverBase.cpp b/Common/src/drivers/CDriverBase.cpp
new file mode 100644
index 00000000000..094113173ec
--- /dev/null
+++ b/Common/src/drivers/CDriverBase.cpp
@@ -0,0 +1,547 @@
+/*!
+ * \file CDriverBase.hpp
+ * \brief Base class template for all drivers.
+ * \author H. Patel, A. Gastaldi
+ * \version 7.3.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2021, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser/ General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+
+#include "../../include/drivers/CDriverBase.hpp"
+
+#include "../../include/geometry/CPhysicalGeometry.hpp"
+#include "../../include/toolboxes/geometry_toolbox.hpp"
+
+using namespace std;
+
+CDriverBase::CDriverBase(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator): 
+    config_file_name(confFile),
+    StartTime(0.0),
+    StopTime(0.0),
+    UsedTime(0.0),
+    TimeIter(0),
+    nZone()
+{
+    
+}
+
+CDriverBase::~CDriverBase(void) {
+    
+}
+
+void CDriverBase::SetContainers_Null() {
+    
+    /*--- Create pointers to all of the classes that may be used by drivers. In general, the pointers are instantiated down a
+     hierarchy over all zones, multigrid levels, equation sets, and equation
+     terms as described in the comments below. ---*/
+    
+    nInst                 = nullptr;
+    
+    config_container      = nullptr;
+    output_container      = nullptr;
+    geometry_container    = nullptr;
+    solver_container      = nullptr;
+    numerics_container    = nullptr;
+    
+    surface_movement      = nullptr;
+    grid_movement         = nullptr;
+    FFDBox                = nullptr;
+    
+    nInst                 = new unsigned short[nZone] ();
+    
+    config_container      = new CConfig*[nZone] ();
+    output_container      = new COutput*[nZone] ();
+    geometry_container    = new CGeometry***[nZone] ();
+    solver_container      = new CSolver****[nZone] ();
+    numerics_container    = new CNumerics*****[nZone] ();
+    
+    surface_movement      = new CSurfaceMovement*[nZone] ();
+    grid_movement         = new CVolumetricMovement**[nZone] ();
+    FFDBox                = new CFreeFormDefBox**[nZone] ();
+    
+    driver_config         = nullptr;
+    driver_output         = nullptr;
+    
+    for (iZone = 0; iZone < nZone; iZone++) {
+        nInst[iZone] = 1;
+    }
+}
+
+map<string, int> CDriverBase::GetBoundaryMarkerIndices() const {
+    CConfig* config = config_container[ZONE_0];
+    
+    const auto nBoundaryMarkers = config->GetnMarker_All();
+    map<string, int>  allBoundariesMap;
+    
+    for (auto iMarker = 0u; iMarker < nBoundaryMarkers; iMarker++) {
+        auto Marker_Tag = config->GetMarker_All_TagBound(iMarker);
+        allBoundariesMap[Marker_Tag] = iMarker;
+    }
+    
+    return allBoundariesMap;
+}
+
+map<string, string> CDriverBase::GetBoundaryMarkerTypes() const {
+    CConfig* config = config_container[ZONE_0];
+    
+    map<string, string> allBoundariesTypeMap;
+    string Marker_Type;
+    
+    for (auto iMarker = 0u; iMarker < config->GetnMarker_All(); iMarker++) {
+        auto Marker_Tag = config->GetMarker_All_TagBound(iMarker);
+        auto KindBC = config->GetMarker_All_KindBC(iMarker);
+        
+        switch(KindBC) {
+            case EULER_WALL:
+                Marker_Type = "EULER_WALL";
+                break;
+            case FAR_FIELD:
+                Marker_Type = "FARFIELD";
+                break;
+            case ISOTHERMAL:
+                Marker_Type = "ISOTHERMAL";
+                break;
+            case HEAT_FLUX:
+                Marker_Type = "HEATFLUX";
+                break;
+            case INLET_FLOW:
+                Marker_Type = "INLET_FLOW";
+                break;
+            case OUTLET_FLOW:
+                Marker_Type = "OUTLET_FLOW";
+                break;
+            case SYMMETRY_PLANE:
+                Marker_Type = "SYMMETRY";
+                break;
+            case SEND_RECEIVE:
+                Marker_Type = "SEND_RECEIVE";
+                break;
+            default:
+                Marker_Type = "UNKNOWN_TYPE";
+        }
+        allBoundariesTypeMap[Marker_Tag] = Marker_Type;
+    }
+    
+    return allBoundariesTypeMap;
+}
+
+vector<string> CDriverBase::GetDeformableMarkerTags() const {
+    CConfig* config = config_container[ZONE_0];
+    
+    const auto nBoundariesMarker = config->GetnMarker_Deform_Mesh();
+    vector<string> interfaceBoundariesTagList;
+    
+    interfaceBoundariesTagList.resize(nBoundariesMarker);
+    
+    for (auto iMarker = 0u; iMarker < nBoundariesMarker; iMarker++) {
+        auto Marker_Tag = config->GetMarker_Deform_Mesh_TagBound(iMarker);
+        interfaceBoundariesTagList[iMarker] = Marker_Tag;
+    }
+    
+    return interfaceBoundariesTagList;
+}
+
+unsigned long CDriverBase::GetNumberDimensions() const {
+    return geometry_container[ZONE_0][INST_0][MESH_0]->GetnDim();
+}
+
+unsigned long CDriverBase::GetNumberElements() const {
+    return geometry_container[ZONE_0][INST_0][MESH_0]->GetnElem();
+}
+
+unsigned long CDriverBase::GetNumberElementsMarker(unsigned short iMarker) const {
+    return geometry_container[ZONE_0][INST_0][MESH_0]->GetnElem_Bound(iMarker);
+}
+
+unsigned long CDriverBase::GetNumberVertices() const {
+    return geometry_container[ZONE_0][INST_0][MESH_0]->GetnPoint();
+}
+
+unsigned long CDriverBase::GetNumberVerticesMarker(unsigned short iMarker) const {
+    return geometry_container[ZONE_0][INST_0][MESH_0]->GetnVertex(iMarker);
+}
+
+unsigned long CDriverBase::GetNumberHaloVertices() const {
+    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    
+    const auto nPoint = geometry->GetnPoint();
+    unsigned long nHaloVertices = 0;
+    
+    for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
+        if (!(geometry->nodes->GetDomain(iPoint))) {
+            nHaloVertices += 1;
+        }
+    }
+    
+    return nHaloVertices;
+}
+
+unsigned long CDriverBase::GetNumberHaloVerticesMarker(unsigned short iMarker) const {
+    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    
+    const auto nVertex = geometry->GetnVertex(iMarker);
+    unsigned long nHaloVertices = 0;
+    
+    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+        auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+        if (!(geometry->nodes->GetDomain(iPoint))) {
+            nHaloVertices += 1;
+        }
+    }
+    
+    return nHaloVertices;
+}
+
+vector<unsigned long> CDriverBase::GetVertexIDs() const {
+    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    
+    const auto nPoint = geometry->GetnPoint();
+    vector<unsigned long> values;
+    
+    for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
+        values.push_back(geometry->nodes->GetGlobalIndex(iPoint));
+    }
+    
+    return values;
+}
+
+vector<unsigned long> CDriverBase::GetVertexIDsMarker(unsigned short iMarker) const {
+    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    
+    const auto nVertex = geometry->GetnVertex(iMarker);
+    vector<unsigned long> values;
+    
+    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+        auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+        
+        values.push_back(geometry->nodes->GetGlobalIndex(iPoint));
+    }
+    
+    return values;
+}
+
+vector<unsigned long> CDriverBase::GetElementIDs() const {
+    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    
+    const auto nElem = geometry->GetnElem();
+    vector<unsigned long> values;
+    
+    for (auto iElem = 0ul; iElem < nElem; iElem++) {
+        values.push_back(geometry->elem[iElem]->GetGlobalIndex());
+    }
+    
+    return values;
+}
+
+vector<unsigned long> CDriverBase::GetElementIDsMarker(unsigned short iMarker) const {
+    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    
+    const auto nBound = geometry->GetnElem_Bound(iMarker);
+    vector<unsigned long> values;
+    
+    for (auto iBound = 0ul; iBound < nBound; iBound++) {
+        values.push_back(geometry->bound[iMarker][iBound]->GetGlobalIndex());
+    }
+    
+    return values;
+}
+
+vector<vector<unsigned long>> CDriverBase::GetConnectivity() const {
+    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    
+    const auto nElem = geometry->GetnElem();
+    vector<vector<unsigned long>> values(nElem);
+    
+    for (auto iElem = 0ul; iElem < nElem; iElem++) {
+        unsigned short nNode = geometry->elem[iElem]->GetnNodes();
+        
+        for (auto iNode = 0u; iNode < nNode; iNode++) {
+            values[iElem].push_back(geometry->elem[iElem]->GetNode(iNode));
+        }
+    }
+    
+    return values;
+}
+
+vector<vector<unsigned long>> CDriverBase::GetConnectivityMarker(unsigned short iMarker) const {
+    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    
+    const auto nBound = geometry->GetnElem_Bound(iMarker);
+    vector<vector<unsigned long>> values(nBound);
+    
+    for (auto iBound = 0ul; iBound < nBound; iBound++) {
+        unsigned short nNode = geometry->bound[iMarker][iBound]->GetnNodes();
+        
+        for (auto iNode = 0u; iNode < nNode; iNode++) {
+            values[iBound].push_back(geometry->bound[iMarker][iBound]->GetNode(iNode));
+        }
+    }
+    
+    return values;
+}
+
+vector<bool> CDriverBase::GetDomain() const {
+    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    
+    const auto nPoint = geometry->GetnPoint();
+    vector<bool> values(nPoint);
+    
+    for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
+        values.push_back(geometry->nodes->GetDomain(iPoint));
+    }
+    
+    return values;
+}
+
+vector<bool> CDriverBase::GetDomainMarker(unsigned short iMarker) const {
+    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    
+    const auto nVertex = geometry->GetnVertex(iMarker);
+    vector<bool> values(nVertex);
+    
+    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+        auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+        
+        values.push_back(geometry->nodes->GetDomain(iPoint));
+    }
+    
+    return values;
+}
+
+vector<passivedouble> CDriverBase::GetCoordinates() const {
+    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    
+    const auto nPoint = geometry->GetnPoint();
+    vector<passivedouble> values(nPoint*nDim, 0.0);
+    su2double value;
+    
+    for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
+        for (auto iDim = 0u; iDim < nDim; iDim++) {
+            value = geometry->nodes->GetCoord(iPoint, iDim);
+            values[iPoint*nDim + iDim] = SU2_TYPE::GetValue(value);
+        }
+    }
+    
+    return values;
+}
+
+vector<passivedouble> CDriverBase::GetCoordinatesMarker(unsigned short iMarker) const {
+    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    
+    const auto nVertex = geometry->GetnVertex(iMarker);
+    vector<passivedouble> values(nVertex*nDim, 0.0);
+    su2double value;
+    
+    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+        auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+        
+        for (auto iDim = 0u; iDim < nDim; iDim++) {
+            value = geometry->nodes->GetCoord(iPoint, iDim);
+            values[iVertex*nDim + iDim] = SU2_TYPE::GetValue(value);
+        }
+    }
+    
+    return values;
+}
+
+void CDriverBase::SetCoordinates(vector<passivedouble> values) {
+    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    
+    const auto nPoint = geometry->GetnPoint();
+    if (values.size() != nPoint*nDim) {
+        SU2_MPI::Error("Size does not match nPoint * nDim!", CURRENT_FUNCTION);
+    }
+    
+    for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
+        for (auto iDim = 0u; iDim < nDim; iDim++) {
+            geometry->nodes->SetCoord(iPoint, iDim, values[iPoint*nDim + iDim]);
+        }
+    }
+}
+
+void CDriverBase::SetCoordinatesMarker(unsigned short iMarker, vector<passivedouble> values) {
+    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    
+    const auto nVertex = geometry->GetnVertex(iMarker);
+    if (values.size() != nVertex*nDim) {
+        SU2_MPI::Error("Size does not match nVertex * nDim!", CURRENT_FUNCTION);
+    }
+    
+    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+        auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+        
+        for (auto iDim = 0u; iDim < nDim; iDim++) {
+            geometry->nodes->SetCoord(iPoint, iDim, values[iVertex*nDim + iDim]);
+        }
+    }
+}
+
+vector<passivedouble> CDriverBase::GetDisplacementsMarker(unsigned short iMarker) const {
+    CConfig* config     = config_container[ZONE_0];
+    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    CSolver* solver     = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL];
+    
+    if (!config->GetDeform_Mesh()) {
+        return {};
+    }
+    
+    const auto nVertex = geometry->GetnVertex(iMarker);
+    vector<passivedouble> values(nVertex*nDim, 0.0);
+    su2double value;
+    
+    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+        auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+        
+        for (auto iDim = 0u; iDim < nDim; iDim++) {
+            value = solver->GetNodes()->GetBound_Disp(iPoint, iDim);
+            values[iVertex*nDim + iDim] = SU2_TYPE::GetValue(value);
+        }
+    }
+    
+    return values;
+}
+
+void CDriverBase::SetDisplacementsMarker(unsigned short iMarker, vector<passivedouble> values) {
+    CConfig* config     = config_container[ZONE_0];
+    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    CSolver* solver     = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL];
+    
+    if (!config->GetDeform_Mesh()) {
+        SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
+    }
+    
+    const auto nVertex = geometry->GetnVertex(iMarker);
+    if (values.size() != nVertex*nDim) {
+        SU2_MPI::Error("Size does not match nVertex * nDim!", CURRENT_FUNCTION);
+    }
+    
+    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+        auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+        
+        for (auto iDim = 0u; iDim < nDim; iDim++) {
+            solver->GetNodes()->SetBound_Disp(iPoint, iDim, values[iVertex*nDim + iDim]);
+        }
+    }
+}
+
+vector<passivedouble> CDriverBase::GetVelocitiesMarker(unsigned short iMarker) const {
+    CConfig* config     = config_container[ZONE_0];
+    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    CSolver* solver     = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL];
+    
+    if (!config->GetDeform_Mesh()) {
+        return {};
+    }
+    
+    const auto nVertex = geometry->GetnVertex(iMarker);
+    vector<passivedouble> values(nVertex*nDim, 0.0);
+    su2double value;
+    
+    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+        auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+        
+        for (auto iDim = 0u; iDim < nDim; iDim++) {
+            value = solver->GetNodes()->GetBound_Vel(iPoint, iDim);
+            values[iVertex*nDim + iDim] = SU2_TYPE::GetValue(value);
+        }
+    }
+    
+    return values;
+}
+
+void CDriverBase::SetVelocitiesMarker(unsigned short iMarker, vector<passivedouble> values) {
+    CConfig* config     = config_container[ZONE_0];
+    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    CSolver* solver     = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL];
+    
+    if (!config->GetDeform_Mesh()) {
+        SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
+    }
+    
+    const auto nVertex = geometry->GetnVertex(iMarker);
+    if (values.size() != nVertex*nDim) {
+        SU2_MPI::Error("Size does not match nVertex * nDim!", CURRENT_FUNCTION);
+    }
+    
+    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+        auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+        
+        for (auto iDim = 0u; iDim < nDim; iDim++) {
+            solver->GetNodes()->SetBound_Vel(iPoint, iDim, values[iVertex*nDim + iDim]);
+        }
+    }
+}
+
+vector<passivedouble> CDriverBase::GetInitialCoordinatesMarker(unsigned short iMarker) const {
+    CConfig* config     = config_container[ZONE_0];
+    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    CSolver* solver     = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL];
+    
+    if (!config->GetDeform_Mesh()) {
+        return {};
+    }
+    
+    const auto nVertex = geometry->GetnVertex(iMarker);
+    vector<passivedouble> values(nVertex*nDim, 0.0);
+    su2double value;
+    
+    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+        auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+        
+        for (auto iDim = 0u; iDim < nDim; iDim++) {
+            value = solver->GetNodes()->GetMesh_Coord(iPoint, iDim);
+            values[iVertex*nDim + iDim] = SU2_TYPE::GetValue(value);
+        }
+    }
+    
+    return values;
+}
+
+vector<passivedouble> CDriverBase::GetVertexNormalsMarker(unsigned short iMarker, bool UnitNormal) const {
+    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    
+    const auto nVertex = geometry->GetnVertex(iMarker);
+    vector<passivedouble> values(nVertex*nDim, 0.0);
+    
+    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+        auto Normal = geometry->vertex[iMarker][iVertex]->GetNormal();
+        auto Area   = GeometryToolbox::Norm(nDim, Normal);
+        
+        for (auto iDim = 0u; iDim < nDim; iDim++) {
+            if (!UnitNormal) {
+                values[iVertex*nDim + iDim] = SU2_TYPE::GetValue(Normal[iDim]);
+            } else {
+                values[iVertex*nDim + iDim] = SU2_TYPE::GetValue(Normal[iDim]/Area);
+            }
+        }
+    }
+    
+    return values;
+}
+
+void CDriverBase::CommunicateMeshDisplacements(void) {
+    CConfig* config     = config_container[ZONE_0];
+    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    CSolver* solver     = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL];
+    
+    solver->InitiateComms(geometry, config, MESH_DISPLACEMENTS);
+    solver->CompleteComms(geometry, config, MESH_DISPLACEMENTS);
+}
diff --git a/Common/src/drivers/meson.build b/Common/src/drivers/meson.build
new file mode 100644
index 00000000000..bcee2ba35cb
--- /dev/null
+++ b/Common/src/drivers/meson.build
@@ -0,0 +1 @@
+common_src += files(['CDriverBase.cpp'])
diff --git a/Common/src/meson.build b/Common/src/meson.build
index b3e0726e70c..4902f8bf9ab 100644
--- a/Common/src/meson.build
+++ b/Common/src/meson.build
@@ -13,6 +13,7 @@ subdir('geometry/elements')
 subdir('geometry/dual_grid')
 subdir('geometry/primal_grid')
 subdir('geometry/meshreader')
+subdir('drivers')
 subdir('interface_interpolation')
 subdir('fem')
 subdir('grid_movement')
diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index 7f27dab3bbe..32843db8c50 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -1,4 +1,4 @@
-/*!
+/*!
  * \file driver_structure.hpp
  * \brief Headers of the main subroutines for driving single or multi-zone problems.
  *        The subroutines and functions are in the <i>driver_structure.cpp</i> file.
@@ -35,6 +35,7 @@
 #include "../interfaces/CInterface.hpp"
 
 #include "../../../Common/include/geometry/CGeometry.hpp"
+#include "../../../Common/include/drivers/CDriverBase.hpp"
 
 using namespace std;
 
@@ -48,739 +49,629 @@ class COutput;
  * \brief Parent class for driving an iteration of a single or multi-zone problem.
  * \author T. Economon
  */
-class CDriver {
-protected:
-  int rank,   /*!< \brief MPI Rank. */
-  size;         /*!< \brief MPI Size. */
-  char* config_file_name;                       /*!< \brief Configuration file name of the problem.*/
-  char runtime_file_name[MAX_STRING_SIZE];
-  su2double StartTime,                          /*!< \brief Start point of the timer for performance benchmarking.*/
-            StopTime,                           /*!< \brief Stop point of the timer for performance benchmarking.*/
-            UsedTimePreproc,                    /*!< \brief Elapsed time between Start and Stop point of the timer for tracking preprocessing phase.*/
-            UsedTimeCompute,                    /*!< \brief Elapsed time between Start and Stop point of the timer for tracking compute phase.*/
-            UsedTimeOutput,                     /*!< \brief Elapsed time between Start and Stop point of the timer for tracking output phase.*/
-            UsedTime;                           /*!< \brief Elapsed time between Start and Stop point of the timer.*/
-  su2double BandwidthSum = 0.0;                 /*!< \brief Aggregate value of the bandwidth for writing restarts (to be average later).*/
-  unsigned long IterCount,                      /*!< \brief Iteration count stored for performance benchmarking.*/
-  OutputCount;                                  /*!< \brief Output count stored for performance benchmarking.*/
-  unsigned long DOFsPerPoint;                   /*!< \brief Number of unknowns at each vertex, i.e., number of equations solved. */
-  su2double Mpoints;                            /*!< \brief Total number of grid points in millions in the calculation (including ghost points).*/
-  su2double MpointsDomain;                      /*!< \brief Total number of grid points in millions in the calculation (excluding ghost points).*/
-  su2double MDOFs;                              /*!< \brief Total number of DOFs in millions in the calculation (including ghost points).*/
-  su2double MDOFsDomain;                        /*!< \brief Total number of DOFs in millions in the calculation (excluding ghost points).*/
-  unsigned long TimeIter;                       /*!< \brief External iteration.*/
-  ofstream **ConvHist_file;                     /*!< \brief Convergence history file.*/
-  ofstream FSIHist_file;                        /*!< \brief FSI convergence history file.*/
-  unsigned short iMesh,                         /*!< \brief Iterator on mesh levels.*/
-                iZone,                          /*!< \brief Iterator on zones.*/
-                nZone,                          /*!< \brief Total number of zones in the problem. */
-                nDim,                           /*!< \brief Number of dimensions.*/
-                iInst,                          /*!< \brief Iterator on instance levels.*/
-                *nInst,                         /*!< \brief Total number of instances in the problem (per zone). */
-                **interface_types;              /*!< \brief Type of coupling between the distinct (physical) zones.*/
-  bool StopCalc,                                /*!< \brief Stop computation flag.*/
-       mixingplane,                             /*!< \brief mixing-plane simulation flag.*/
-       fsi,                                     /*!< \brief FSI simulation flag.*/
-       fem_solver;                              /*!< \brief FEM fluid solver simulation flag. */
-  CIteration ***iteration_container;            /*!< \brief Container vector with all the iteration methods. */
-  COutput **output_container;                   /*!< \brief Pointer to the COutput class. */
-  CIntegration ****integration_container;       /*!< \brief Container vector with all the integration methods. */
-  CGeometry ****geometry_container;             /*!< \brief Geometrical definition of the problem. */
-  CSolver *****solver_container;                /*!< \brief Container vector with all the solutions. */
-  CNumerics ******numerics_container;           /*!< \brief Description of the numerical method (the way in which the equations are solved). */
-  CConfig **config_container;                   /*!< \brief Definition of the particular problem. */
-  CConfig *driver_config;                       /*!< \brief Definition of the driver configuration. */
-  COutput *driver_output;                       /*!< \brief Definition of the driver output. */
-  CSurfaceMovement **surface_movement;          /*!< \brief Surface movement classes of the problem. */
-  CVolumetricMovement ***grid_movement;         /*!< \brief Volume grid movement classes of the problem. */
-  CFreeFormDefBox*** FFDBox;                    /*!< \brief FFD FFDBoxes of the problem. */
-  vector<vector<unique_ptr<CInterpolator> > >
-  interpolator_container;                       /*!< \brief Definition of the interpolation method between non-matching discretizations of the interface. */
-  CInterface ***interface_container;            /*!< \brief Definition of the interface of information and physics. */
-  bool dry_run;                                 /*!< \brief Flag if SU2_CFD was started as dry-run via "SU2_CFD -d <config>.cfg" */
 
+class CDriver : public CDriverBase {
+    
+protected:
+    
+    char runtime_file_name[MAX_STRING_SIZE];
+    su2double UsedTimeOutput;                     /*!< \brief Elapsed time between Start and Stop point of the timer for tracking output phase.*/
+    
+    su2double BandwidthSum = 0.0;                 /*!< \brief Aggregate value of the bandwidth for writing restarts (to be average later).*/
+    unsigned long IterCount,                       /*!< \brief Iteration count stored for performance benchmarking.*/
+    OutputCount;                                  /*!< \brief Output count stored for performance benchmarking.*/
+    unsigned long DOFsPerPoint;                    /*!< \brief Number of unknowns at each vertex, i.e., number of equations solved. */
+    su2double Mpoints;                            /*!< \brief Total number of grid points in millions in the calculation (including ghost points).*/
+    su2double MpointsDomain;                      /*!< \brief Total number of grid points in millions in the calculation (excluding ghost points).*/
+    su2double MDOFs;                              /*!< \brief Total number of DOFs in millions in the calculation (including ghost points).*/
+    su2double MDOFsDomain;                        /*!< \brief Total number of DOFs in millions in the calculation (excluding ghost points).*/
+    
+    ofstream **ConvHist_file;                     /*!< \brief Convergence history file.*/
+    ofstream FSIHist_file;                        /*!< \brief FSI convergence history file.*/
+    
+    bool StopCalc,                                /*!< \brief Stop computation flag.*/
+    mixingplane,                                  /*!< \brief mixing-plane simulation flag.*/
+    fsi,                                          /*!< \brief FSI simulation flag.*/
+    fem_solver;                                   /*!< \brief FEM fluid solver simulation flag. */
+    
+    CIteration ***iteration_container;            /*!< \brief Container vector with all the iteration methods. */
+    CIntegration ****integration_container;       /*!< \brief Container vector with all the integration methods. */
+    vector<vector<unique_ptr<CInterpolator> > >
+    interpolator_container;                       /*!< \brief Definition of the interpolation method between non-matching discretizations of the interface. */
+    CInterface ***interface_container;            /*!< \brief Definition of the interface of information and physics. */
+    bool dry_run;                                 /*!< \brief Flag if SU2_CFD was started as dry-run via "SU2_CFD -d <config>.cfg" */
+    
 public:
-
-  /*!
-   * \brief Constructor of the class.
-   * \param[in] confFile - Configuration file name.
-   * \param[in] val_nZone - Total number of zones.
-   * \param[in] val_nDim - Number of dimensions.
-   * \param[in] MPICommunicator - MPI communicator for SU2.
-   */
-  CDriver(char* confFile,
-          unsigned short val_nZone,
-          SU2_Comm MPICommunicator, bool dummy_geo);
-
-  /*!
-   * \brief Destructor of the class.
-   */
-  virtual ~CDriver(void);
-
-  /*!
-   * \brief A virtual member.
-   */
-  virtual void Run() { };
-
+    
+    /*!
+     * \brief Constructor of the class.
+     * \param[in] confFile - Configuration file name.
+     * \param[in] val_nZone - Total number of zones.
+     * \param[in] val_nDim - Number of dimensions.
+     * \param[in] MPICommunicator - MPI communicator for SU2.
+     */
+    CDriver(char* confFile,
+            unsigned short val_nZone,
+            SU2_Comm MPICommunicator, bool dummy_geo);
+    
+    /*!
+     * \brief Destructor of the class.
+     */
+    virtual ~CDriver(void);
+    
+    /*!
+     * \brief A virtual member.
+     */
+    virtual void Run() { };
+    
 protected:
-
-  /*!
-   * \brief Init_Containers
-   */
-  void SetContainers_Null();
-
-  /*!
-   * \brief Read in the config and mesh files.
-   */
-  void Input_Preprocessing(CConfig **&config, CConfig *&driver_config);
-
-  /*!
-   * \brief Construction of the edge-based data structure and the multigrid structure.
-   */
-  void Geometrical_Preprocessing(CConfig *config, CGeometry **&geometry, bool dummy);
-
-  /*!
-   * \brief Do the geometrical preprocessing for the DG FEM solver.
-   */
-  void Geometrical_Preprocessing_DGFEM(CConfig *config, CGeometry **&geometry);
-
-  /*!
-   * \brief Geometrical_Preprocessing_FVM
-   */
-  void Geometrical_Preprocessing_FVM(CConfig *config, CGeometry **&geometry);
-
-  /*!
-   * \brief Definition of the physics iteration class or within a single zone.
-   * \param[in] iteration_container - Pointer to the iteration container to be instantiated.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] iZone - Index of the zone.
-   */
-  void Iteration_Preprocessing(CConfig *config, CIteration *&iteration) const;
-
-  /*!
-   * \brief Definition and allocation of all solution classes.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] config - Definition of the particular problem.
-   */
-  void Solver_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***&solver);
-
-  /*!
-   * \brief Restart of the solvers from the restart files.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] config - Definition of the particular problem.
-   */
-  void Solver_Restart(CSolver ***solver, CGeometry **geometry, CConfig *config, bool update_geo);
-
-  /*!
-   * \brief Definition and allocation of all solution classes.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] config - Definition of the particular problem.
-   */
-  void Solver_Postprocessing(CSolver ****solver, CGeometry **geometry, CConfig *config, unsigned short val_iInst);
-
-  /*!
-   * \brief Definition and allocation of all integration classes.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] solver - Container vector with all the solutions.
-   * \param[out] integration - Container vector with all the integration methods.
-   */
-  void Integration_Preprocessing(CConfig *config, CSolver **solver, CIntegration **&integration) const;
-
-  /*!
-   * \brief Definition and allocation of all integration classes.
-   * \param[in] integration_container - Container vector with all the integration methods.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] config - Definition of the particular problem.
-   */
-  void Integration_Postprocessing(CIntegration ***integration, CGeometry **geometry, CConfig *config, unsigned short val_iInst);
-
-  /*!
-   * \brief Definition and allocation of all interface classes.
-   */
-  void Interface_Preprocessing(CConfig **config, CSolver *****solver, CGeometry ****geometry,
-                               unsigned short **interface_types, CInterface ***interface,
-                               vector<vector<unique_ptr<CInterpolator> > > &interpolation);
-
-  /*!
-   * \brief Definition and allocation of all solver classes.
-   * \param[in] numerics_container - Description of the numerical method (the way in which the equations are solved).
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] config - Definition of the particular problem.
-   */
-  void Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***solver, CNumerics ****&numerics) const;
-
-  /*!
-   * \brief Helper to instantiate turbulence numerics specialized for different flow solvers.
-   */
-  template <class FlowIndices>
-  void InstantiateTurbulentNumerics(unsigned short nVar_Turb, int offset, const CConfig *config,
-                                    const CSolver* turb_solver, CNumerics ****&numerics) const;
-
-  /*!
-   * \brief Helper to instantiate species transport numerics specialized for different flow solvers.
-   */
-  template <class FlowIndices>
-  void InstantiateSpeciesNumerics(unsigned short nVar_Species, int offset, const CConfig *config,
-                                  const CSolver* species_solver, CNumerics ****&numerics) const;
-
-  /*!
-   * \brief Definition and allocation of all solver classes.
-   * \param[in] numerics_container - Description of the numerical method (the way in which the equations are solved).
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] config - Definition of the particular problem.
-   */
-  void Numerics_Postprocessing(CNumerics *****numerics, CSolver ***solver, CGeometry **geometry, CConfig *config, unsigned short val_iInst);
-
-  /*!
-   * \brief GridMovement_Preprocessing
-   * \param config
-   * \param geometry
-   * \param solver
-   * \param iteration
-   * \param grid_movement
-   * \param surface_movement
-   */
-  void DynamicMesh_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***solver, CIteration *iteration, CVolumetricMovement *&grid_movement, CSurfaceMovement *&surface_movement) const;
-
-  /*!
-   * \brief Initialize Python interface functionalities
-   */
-  void PythonInterface_Preprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver);
-
-  /*!
-   * \brief Preprocess the output container.
-   */
-  void Output_Preprocessing(CConfig **config, CConfig *driver_config, COutput **&output_container, COutput *&driver_output);
-
-  /*!
-   * \brief Initiate value for static mesh movement such as the gridVel for the ROTATING frame.
-   */
-  void StaticMesh_Preprocessing(const CConfig *config, CGeometry **geometry);
-
-  /*!
-   * \brief Initiate value for static mesh movement such as the gridVel for the ROTATING frame.
-   */
-  void Turbomachinery_Preprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver,
-                                    CInterface*** interface);
-
-  /*!
-   * \brief A virtual member.
-   * \param[in] donorZone - zone in which the displacements will be predicted.
-   * \param[in] targetZone - zone which receives the predicted displacements.
-   */
-  virtual void Predict_Displacements(unsigned short donorZone, unsigned short targetZone) {}
-
-  /*!
-   * \brief A virtual member.
-   * \param[in] donorZone - zone in which the tractions will be predicted.
-   * \param[in] targetZone - zone which receives the predicted traction.
-   */
-  virtual void Predict_Tractions(unsigned short donorZone, unsigned short targetZone) {}
-
-  /*!
-   * \brief A virtual member.
-   * \param[in] donorZone - zone in which the displacements will be transferred.
-   * \param[in] targetZone - zone which receives the tractions transferred.
-   */
-  virtual void Transfer_Displacements(unsigned short donorZone, unsigned short targetZone) {}
-
-  /*!
-   * \brief A virtual member.
-   * \param[in] donorZone - zone from which the tractions will be transferred.
-   * \param[in] targetZone - zone which receives the tractions transferred.
-   */
-  virtual void Transfer_Tractions(unsigned short donorZone, unsigned short targetZone) {}
-
-  /*!
-   * \brief A virtual member.
-   * \param[in] donorZone - origin of the information.
-   * \param[in] targetZone - destination of the information.
-   * \param[in] iOuterIter - Fluid-Structure Interaction subiteration.
-   */
-  virtual void Relaxation_Displacements(unsigned short donorZone, unsigned short targetZone, unsigned long iOuterIter) {}
-
-  /*!
-   * \brief A virtual member.
-   * \param[in] donorZone - origin of the information.
-   * \param[in] targetZone - destination of the information.
-   * \param[in] iOuterIter - Fluid-Structure Interaction subiteration.
-   */
-  virtual void Relaxation_Tractions(unsigned short donorZone, unsigned short targetZone, unsigned long iOuterIter) {}
-
-  /*!
-   * \brief A virtual member to run a Block Gauss-Seidel iteration in multizone problems.
-   */
-  virtual void Run_GaussSeidel(){}
-
-  /*!
-   * \brief A virtual member to run a Block-Jacobi iteration in multizone problems.
-   */
-  virtual void Run_Jacobi(){}
-
-  /*!
-   * \brief A virtual member.
-   */
-  virtual void Update() {}
-
-  /*!
-   * \brief Print out the direct residuals.
-   * \param[in] kind_recording - Type of recording (full list in ENUM_RECORDING, option_structure.hpp)
-   */
-  void Print_DirectResidual(RECORDING kind_recording);
-
+    
+    /*!
+     * \brief Init_Containers
+     */
+    void SetContainers_Null();
+    
+    /*!
+     * \brief Read in the config and mesh files.
+     */
+    void Input_Preprocessing(CConfig **&config, CConfig *&driver_config);
+    
+    /*!
+     * \brief Construction of the edge-based data structure and the multigrid structure.
+     */
+    void Geometrical_Preprocessing(CConfig *config, CGeometry **&geometry, bool dummy);
+    
+    /*!
+     * \brief Do the geometrical preprocessing for the DG FEM solver.
+     */
+    void Geometrical_Preprocessing_DGFEM(CConfig *config, CGeometry **&geometry);
+    
+    /*!
+     * \brief Geometrical_Preprocessing_FVM
+     */
+    void Geometrical_Preprocessing_FVM(CConfig *config, CGeometry **&geometry);
+    
+    /*!
+     * \brief Definition of the physics iteration class or within a single zone.
+     * \param[in] iteration_container - Pointer to the iteration container to be instantiated.
+     * \param[in] config - Definition of the particular problem.
+     * \param[in] iZone - Index of the zone.
+     */
+    void Iteration_Preprocessing(CConfig *config, CIteration *&iteration) const;
+    
+    /*!
+     * \brief Definition and allocation of all solution classes.
+     * \param[in] solver_container - Container vector with all the solutions.
+     * \param[in] geometry - Geometrical definition of the problem.
+     * \param[in] config - Definition of the particular problem.
+     */
+    void Solver_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***&solver);
+    
+    /*!
+     * \brief Restart of the solvers from the restart files.
+     * \param[in] solver_container - Container vector with all the solutions.
+     * \param[in] geometry - Geometrical definition of the problem.
+     * \param[in] config - Definition of the particular problem.
+     */
+    void Solver_Restart(CSolver ***solver, CGeometry **geometry, CConfig *config, bool update_geo);
+    
+    /*!
+     * \brief Definition and allocation of all solution classes.
+     * \param[in] solver_container - Container vector with all the solutions.
+     * \param[in] geometry - Geometrical definition of the problem.
+     * \param[in] config - Definition of the particular problem.
+     */
+    void Solver_Postprocessing(CSolver ****solver, CGeometry **geometry, CConfig *config, unsigned short val_iInst);
+    
+    /*!
+     * \brief Definition and allocation of all integration classes.
+     * \param[in] config - Definition of the particular problem.
+     * \param[in] solver - Container vector with all the solutions.
+     * \param[out] integration - Container vector with all the integration methods.
+     */
+    void Integration_Preprocessing(CConfig *config, CSolver **solver, CIntegration **&integration) const;
+    
+    /*!
+     * \brief Definition and allocation of all integration classes.
+     * \param[in] integration_container - Container vector with all the integration methods.
+     * \param[in] geometry - Geometrical definition of the problem.
+     * \param[in] config - Definition of the particular problem.
+     */
+    void Integration_Postprocessing(CIntegration ***integration, CGeometry **geometry, CConfig *config, unsigned short val_iInst);
+    
+    /*!
+     * \brief Definition and allocation of all interface classes.
+     */
+    void Interface_Preprocessing(CConfig **config, CSolver *****solver, CGeometry ****geometry,
+                                 unsigned short **interface_types, CInterface ***interface,
+                                 vector<vector<unique_ptr<CInterpolator> > > &interpolation);
+    
+    /*!
+     * \brief Definition and allocation of all solver classes.
+     * \param[in] numerics_container - Description of the numerical method (the way in which the equations are solved).
+     * \param[in] geometry - Geometrical definition of the problem.
+     * \param[in] solver_container - Container vector with all the solutions.
+     * \param[in] config - Definition of the particular problem.
+     */
+    void Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***solver, CNumerics ****&numerics) const;
+    
+    /*!
+     * \brief Helper to instantiate turbulence numerics specialized for different flow solvers.
+     */
+    template <class FlowIndices>
+    void InstantiateTurbulentNumerics(unsigned short nVar_Turb, int offset, const CConfig *config,
+                                      const CSolver* turb_solver, CNumerics ****&numerics) const;
+    
+    /*!
+     * \brief Helper to instantiate species transport numerics specialized for different flow solvers.
+     */
+    template <class FlowIndices>
+    void InstantiateSpeciesNumerics(unsigned short nVar_Species, int offset, const CConfig *config,
+                                    const CSolver* species_solver, CNumerics ****&numerics) const;
+    
+    /*!
+     * \brief Definition and allocation of all solver classes.
+     * \param[in] numerics_container - Description of the numerical method (the way in which the equations are solved).
+     * \param[in] solver_container - Container vector with all the solutions.
+     * \param[in] geometry - Geometrical definition of the problem.
+     * \param[in] config - Definition of the particular problem.
+     */
+    void Numerics_Postprocessing(CNumerics *****numerics, CSolver ***solver, CGeometry **geometry, CConfig *config, unsigned short val_iInst);
+    
+    /*!
+     * \brief GridMovement_Preprocessing
+     * \param config
+     * \param geometry
+     * \param solver
+     * \param iteration
+     * \param grid_movement
+     * \param surface_movement
+     */
+    void DynamicMesh_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***solver, CIteration *iteration, CVolumetricMovement *&grid_movement, CSurfaceMovement *&surface_movement) const;
+    
+    /*!
+     * \brief Initialize Python interface functionalities
+     */
+    void PythonInterface_Preprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver);
+    
+    /*!
+     * \brief Preprocess the output container.
+     */
+    void Output_Preprocessing(CConfig **config, CConfig *driver_config, COutput **&output_container, COutput *&driver_output);
+    
+    /*!
+     * \brief Initiate value for static mesh movement such as the gridVel for the ROTATING frame.
+     */
+    void StaticMesh_Preprocessing(const CConfig *config, CGeometry **geometry);
+    
+    /*!
+     * \brief Initiate value for static mesh movement such as the gridVel for the ROTATING frame.
+     */
+    void Turbomachinery_Preprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver,
+                                      CInterface*** interface);
+    
+    /*!
+     * \brief A virtual member.
+     * \param[in] donorZone - zone in which the displacements will be predicted.
+     * \param[in] targetZone - zone which receives the predicted displacements.
+     */
+    virtual void Predict_Displacements(unsigned short donorZone, unsigned short targetZone) {}
+    
+    /*!
+     * \brief A virtual member.
+     * \param[in] donorZone - zone in which the tractions will be predicted.
+     * \param[in] targetZone - zone which receives the predicted traction.
+     */
+    virtual void Predict_Tractions(unsigned short donorZone, unsigned short targetZone) {}
+    
+    /*!
+     * \brief A virtual member.
+     * \param[in] donorZone - zone in which the displacements will be transferred.
+     * \param[in] targetZone - zone which receives the tractions transferred.
+     */
+    virtual void Transfer_Displacements(unsigned short donorZone, unsigned short targetZone) {}
+    
+    /*!
+     * \brief A virtual member.
+     * \param[in] donorZone - zone from which the tractions will be transferred.
+     * \param[in] targetZone - zone which receives the tractions transferred.
+     */
+    virtual void Transfer_Tractions(unsigned short donorZone, unsigned short targetZone) {}
+    
+    /*!
+     * \brief A virtual member.
+     * \param[in] donorZone - origin of the information.
+     * \param[in] targetZone - destination of the information.
+     * \param[in] iOuterIter - Fluid-Structure Interaction subiteration.
+     */
+    virtual void Relaxation_Displacements(unsigned short donorZone, unsigned short targetZone, unsigned long iOuterIter) {}
+    
+    /*!
+     * \brief A virtual member.
+     * \param[in] donorZone - origin of the information.
+     * \param[in] targetZone - destination of the information.
+     * \param[in] iOuterIter - Fluid-Structure Interaction subiteration.
+     */
+    virtual void Relaxation_Tractions(unsigned short donorZone, unsigned short targetZone, unsigned long iOuterIter) {}
+    
+    /*!
+     * \brief A virtual member to run a Block Gauss-Seidel iteration in multizone problems.
+     */
+    virtual void Run_GaussSeidel(){}
+    
+    /*!
+     * \brief A virtual member to run a Block-Jacobi iteration in multizone problems.
+     */
+    virtual void Run_Jacobi(){}
+    
+    /*!
+     * \brief A virtual member.
+     */
+    virtual void Update() {}
+    
+    /*!
+     * \brief Print out the direct residuals.
+     * \param[in] kind_recording - Type of recording (full list in ENUM_RECORDING, option_structure.hpp)
+     */
+    void Print_DirectResidual(RECORDING kind_recording);
+    
 public:
-
-  /*!
-   * \brief Launch the computation for all zones and all physics.
-   */
-  virtual void StartSolver() {}
-
-  /*!
-   * \brief Deallocation routine
-   */
-  void Postprocessing();
-
-  /*!
-   * \brief A virtual member.
-   */
-  virtual void ResetConvergence();
-
-  /*!
-   * \brief Perform some pre-processing before an iteration of the physics.
-   */
-  virtual void Preprocess(unsigned long TimeIter){ }
-
-  /*!
-   * \brief Monitor the computation.
-   */
-  virtual bool Monitor(unsigned long TimeIter){ return false; }
-
-  /*!
-   * \brief Output the solution in solution file.
-   */
-  virtual void Output(unsigned long TimeIter){ }
-
-  /*!
-   * \brief Perform a dynamic mesh deformation, including grid velocity computation and update of the multigrid structure.
-   */
-  virtual void DynamicMeshUpdate(unsigned long TimeIter) { }
-
-  /*!
-   * \brief Perform a dynamic mesh deformation, including grid velocity computation and update of the multigrid structure.
-   */
-  virtual void DynamicMeshUpdate(unsigned short val_iZone, unsigned long TimeIter) { }
-
-  /*!
-   * \brief Perform a mesh deformation as initial condition.
-   */
-  virtual void SetInitialMesh() { }
-
-  /*!
-   * \brief Process the boundary conditions and update the multigrid structure.
-   */
-  void BoundaryConditionsUpdate();
-
-  /*!
-   * \brief Get the total drag.
-   * \return Total drag.
-   */
-  passivedouble Get_Drag() const;
-
-  /*!
-   * \brief Get the total lift.
-   * \return Total lift.
-   */
-  passivedouble Get_Lift() const;
-
-  /*!
-   * \brief Get the total x moment.
-   * \return Total x moment.
-   */
-  passivedouble Get_Mx() const;
-
-  /*!
-   * \brief Get the total y moment.
-   * \return Total y moment.
-   */
-  passivedouble Get_My() const;
-
-  /*!
-   * \brief Get the total z moment.
-   * \return Total z moment.
-   */
-  passivedouble Get_Mz() const;
-
-  /*!
-   * \brief Get the total drag coefficient.
-   * \return Total drag coefficient.
-   */
-  passivedouble Get_DragCoeff() const;
-
-  /*!
-   * \brief Get the total lift coefficient.
-   * \return Total lift coefficient.
-   */
-  passivedouble Get_LiftCoeff() const;
-
-  /*!
-   * \brief Get the number of vertices (halo nodes included) from a specified marker.
-   * \param[in] iMarker -  Marker identifier.
-   * \return Number of vertices.
-   */
-  unsigned long GetNumberVertices(unsigned short iMarker) const;
-
-  /*!
-   * \brief Get the number of halo vertices from a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \return Number of vertices.
-   */
-  unsigned long GetNumberHaloVertices(unsigned short iMarker) const;
-
-  /*!
-   * \brief Check if a vertex is physical or not (halo node) on a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return True if the specified vertex is a halo node.
-   */
-  bool IsAHaloNode(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Get the number of external iterations.
-   * \return Number of external iterations.
-   */
-  unsigned long GetnTimeIter() const;
-
-  /*!
-   * \brief Get the current external iteration.
-   * \return Current external iteration.
-   */
-  unsigned long GetTime_Iter() const;
-
-  /*!
-   * \brief Get the unsteady time step.
-   * \return Unsteady time step.
-   */
-  passivedouble GetUnsteady_TimeStep() const;
-
-  /*!
-   * \brief Get the name of the output file for the surface.
-   * \return File name for the surface output.
-   */
-  string GetSurfaceFileName() const;
-
-  /*!
-   * \brief Get the global index of a vertex on a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Vertex global index.
-   */
-  unsigned long GetVertexGlobalIndex(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Get undeformed coordinates from the mesh solver.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return x,y,z coordinates of the vertex.
-   */
-  vector<passivedouble> GetInitialMeshCoord(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Get the temperature at a vertex on a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Temperature of the vertex.
-   */
-  passivedouble GetVertexTemperature(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Set the temperature of a vertex on a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \param[in] val_WallTemp - Value of the temperature.
-   */
-  void SetVertexTemperature(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallTemp);
-
-  /*!
-   * \brief Get the heat flux at a vertex on a specified marker (3 components).
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return True if the vertex is a halo node.
-   */
-  vector<passivedouble> GetVertexHeatFluxes(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Get the wall normal component of the heat flux at a vertex on a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Wall normal component of the heat flux at the vertex.
-   */
-  passivedouble GetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Set the wall normal component of the heat flux at a vertex on a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \param[in] val_WallHeatFlux - Value of the normal heat flux.
-   */
-  void SetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallHeatFlux);
-
-  /*!
-   * \brief Get the thermal conductivity at a vertex on a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Thermal conductivity at the vertex.
-   */
-  passivedouble GetThermalConductivity(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Preprocess the inlets via file input for all solvers.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] config - Definition of the particular problem.
-   */
-  void Inlet_Preprocessing(CSolver ***solver, CGeometry **geometry, CConfig *config) const;
-
-  /*!
-   * \brief Get the normal (vector) at a vertex on a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \param[in] unitNormal - Bool to normalise the vector.
-   * \return Normal (vector) at the vertex.
-   */
-  vector<passivedouble> GetVertexNormal(unsigned short iMarker, unsigned long iVertex, bool unitNormal = false) const;
-
-  /*!
-   * \brief Get the unit normal (vector) at a vertex on a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Unit normal (vector) at the vertex.
-   */
-  inline vector<passivedouble> GetVertexUnitNormal(unsigned short iMarker, unsigned long iVertex) const {
-    return GetVertexNormal(iMarker, iVertex, true);
-  }
-
-  /*!
-   * \brief Get all the boundary markers tags.
-   * \return List of boundary markers tags.
-   */
-  vector<string> GetAllBoundaryMarkersTag() const;
-
-  /*!
-   * \brief Get all the deformable boundary marker tags.
-   * \return List of deformable boundary markers tags.
-   */
-  vector<string> GetAllDeformMeshMarkersTag() const;
-
-  /*!
-   * \brief Get all the heat transfer boundary markers tags.
-   * \return List of heat transfer boundary markers tags.
-   */
-  vector<string> GetAllCHTMarkersTag() const;
-
-  /*!
-   * \brief Get all the (subsonic) inlet boundary markers tags.
-   * \return List of inlet boundary markers tags.
-   */
-  vector<string> GetAllInletMarkersTag() const;
-
-  /*!
-   * \brief Get all the boundary markers tags with their associated indices.
-   * \return List of boundary markers tags with their indices.
-   */
-  map<string, int> GetAllBoundaryMarkers() const;
-
-  /*!
-   * \brief Get all the boundary markers tags with their associated types.
-   * \return List of boundary markers tags with their types.
-   */
-  map<string, string> GetAllBoundaryMarkersType() const;
-
-  /*!
-   * \brief Set the mesh displacement for the elasticity mesh solver.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \param[in] DispX - Value of the mesh displacement in the direction X.
-   * \param[in] DispY - Value of the mesh displacement in the direction Y.
-   * \param[in] DispZ - Value of the mesh displacement in the direction Z.
-   */
-  void SetMeshDisplacement(unsigned short iMarker, unsigned long iVertex, passivedouble DispX, passivedouble DispY, passivedouble DispZ);
-
-  /*!
-   * \brief Communicate the boundary mesh displacements in a python call
-   */
-  void CommunicateMeshDisplacement(void);
-
-  /*!
-   * \brief Return the sensitivities of the mesh boundary vertices.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Vector of sensitivities.
-   */
-  vector<passivedouble> GetMeshDisp_Sensitivity(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Set the load in X direction for the structural solver.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \param[in] LoadX - Value of the load in the direction X.
-   * \param[in] LoadX - Value of the load in the direction Y.
-   * \param[in] LoadX - Value of the load in the direction Z.
-   */
-  void SetFEA_Loads(unsigned short iMarker, unsigned long iVertex, passivedouble LoadX,
-                    passivedouble LoadY, passivedouble LoadZ);
-
-  /*!
-   * \brief Return the displacements from the FEA solver.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Vector of displacements.
-   */
-  vector<passivedouble> GetFEA_Displacements(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Return the velocities from the FEA Solver.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Vector of velocities.
-   */
-  vector<passivedouble> GetFEA_Velocity(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Return the velocities from the FEA Solver.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Vector of velocities at time n.
-   */
-  vector<passivedouble> GetFEA_Velocity_n(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Get the sensitivity of the flow loads for the structural solver.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \param[in] LoadX - Value of the load in the direction X.
-   * \param[in] LoadX - Value of the load in the direction Y.
-   * \param[in] LoadX - Value of the load in the direction Z.
-   */
-  vector<passivedouble> GetFlowLoad_Sensitivity(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Get the flow load (from the extra step - the repeated methods should be unified once the postprocessing
-   * strategy is in place).
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   */
-  vector<passivedouble> GetFlowLoad(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Set the adjoint of the flow tractions (from the extra step -
-   * the repeated methods should be unified once the postprocessing strategy is in place).
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \param[in] val_AdjointX - Value of the adjoint in the direction X.
-   * \param[in] val_AdjointY - Value of the adjoint in the direction Y.
-   * \param[in] val_AdjointZ - Value of the adjoint in the direction Z.
-   */
-  void SetFlowLoad_Adjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
-                                    passivedouble val_AdjointY, passivedouble val_AdjointZ);
-
-  /*!
-   * \brief Set the adjoint of the structural displacements (from an outside source)
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \param[in] val_AdjointX - Value of the adjoint in the direction X.
-   * \param[in] val_AdjointY - Value of the adjoint in the direction Y.
-   * \param[in] val_AdjointZ - Value of the adjoint in the direction Z.
-   */
-  void SetSourceTerm_DispAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
-                                 passivedouble val_AdjointY, passivedouble val_AdjointZ);
-  void SetSourceTerm_VelAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
-                                 passivedouble val_AdjointY, passivedouble val_AdjointZ);
-
-  /*!
-   * \brief Set the position of the heat source.
-   * \param[in] alpha - Angle of rotation respect to Z axis.
-   * \param[in] pos_x - Position X.
-   * \param[in] pos_y - Position Y.
-   * \param[in] pos_z - Position Z.
-   */
-  void SetHeatSource_Position(passivedouble alpha, passivedouble pos_x, passivedouble pos_y, passivedouble pos_z);
-
-  /*!
-   * \brief Set the direction of the inlet.
-   * \param[in] iMarker - Marker index.
-   * \param[in] alpha - Angle (Zpos).
-   */
-  void SetInlet_Angle(unsigned short iMarker, passivedouble alpha);
-
-  /*!
-   * \brief Sum the number of primal or adjoint variables for all solvers in a given zone.
-   * \param[in] iZone - Index of the zone.
-   * \param[in] adjoint - True to consider adjoint solvers instead of primal.
-   * \return Total number of solution variables.
-   */
-  unsigned short GetTotalNumberOfVariables(unsigned short iZone, bool adjoint) const {
-    unsigned short nVar = 0;
-    for (auto iSol = 0u; iSol < MAX_SOLS; iSol++) {
-      auto solver = solver_container[iZone][INST_0][MESH_0][iSol];
-      if (solver && (solver->GetAdjoint() == adjoint)) nVar += solver->GetnVar();
+    
+    /*!
+     * \brief Launch the computation for all zones and all physics.
+     */
+    virtual void StartSolver() {}
+    
+    /*!
+     * \brief Deallocation routine
+     */
+    void Postprocessing();
+    
+    /*!
+     * \brief A virtual member.
+     */
+    virtual void ResetConvergence();
+    
+    /*!
+     * \brief Perform some pre-processing before an iteration of the physics.
+     */
+    virtual void Preprocess(unsigned long TimeIter){ }
+    
+    /*!
+     * \brief Monitor the computation.
+     */
+    virtual bool Monitor(unsigned long TimeIter){ return false; }
+    
+    /*!
+     * \brief Output the solution in solution file.
+     */
+    virtual void Output(unsigned long TimeIter){ }
+    
+    /*!
+     * \brief Perform a dynamic mesh deformation, including grid velocity computation and update of the multigrid structure.
+     */
+    virtual void DynamicMeshUpdate(unsigned long TimeIter) { }
+    
+    /*!
+     * \brief Perform a dynamic mesh deformation, including grid velocity computation and update of the multigrid structure.
+     */
+    virtual void DynamicMeshUpdate(unsigned short val_iZone, unsigned long TimeIter) { }
+    
+    /*!
+     * \brief Perform a mesh deformation as initial condition.
+     */
+    virtual void SetInitialMesh() { }
+    
+    /*!
+     * \brief Process the boundary conditions and update the multigrid structure.
+     */
+    void BoundaryConditionsUpdate();
+    
+    /*!
+     * \brief Get the total drag.
+     * \return Total drag.
+     */
+    passivedouble Get_Drag() const;
+    
+    /*!
+     * \brief Get the total lift.
+     * \return Total lift.
+     */
+    passivedouble Get_Lift() const;
+    
+    /*!
+     * \brief Get the total x moment.
+     * \return Total x moment.
+     */
+    passivedouble Get_Mx() const;
+    
+    /*!
+     * \brief Get the total y moment.
+     * \return Total y moment.
+     */
+    passivedouble Get_My() const;
+    
+    /*!
+     * \brief Get the total z moment.
+     * \return Total z moment.
+     */
+    passivedouble Get_Mz() const;
+    
+    /*!
+     * \brief Get the total drag coefficient.
+     * \return Total drag coefficient.
+     */
+    passivedouble Get_DragCoeff() const;
+    
+    /*!
+     * \brief Get the total lift coefficient.
+     * \return Total lift coefficient.
+     */
+    passivedouble Get_LiftCoeff() const;
+    
+    /*!
+     * \brief Get the number of external iterations.
+     * \return Number of external iterations.
+     */
+    unsigned long GetnTimeIter() const;
+    
+    /*!
+     * \brief Get the current external iteration.
+     * \return Current external iteration.
+     */
+    unsigned long GetTime_Iter() const;
+    
+    /*!
+     * \brief Get the unsteady time step.
+     * \return Unsteady time step.
+     */
+    passivedouble GetUnsteady_TimeStep() const;
+    
+    /*!
+     * \brief Get the name of the output file for the surface.
+     * \return File name for the surface output.
+     */
+    string GetSurfaceFileName() const;
+    
+    /*!
+     * \brief Get the temperature at a vertex on a specified marker.
+     * \param[in] iMarker - Marker identifier.
+     * \param[in] iVertex - Vertex identifier.
+     * \return Temperature of the vertex.
+     */
+    passivedouble GetVertexTemperature(unsigned short iMarker, unsigned long iVertex) const;
+    
+    /*!
+     * \brief Set the temperature of a vertex on a specified marker.
+     * \param[in] iMarker - Marker identifier.
+     * \param[in] iVertex - Vertex identifier.
+     * \param[in] val_WallTemp - Value of the temperature.
+     */
+    void SetVertexTemperature(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallTemp);
+    
+    /*!
+     * \brief Get the heat flux at a vertex on a specified marker (3 components).
+     * \param[in] iMarker - Marker identifier.
+     * \param[in] iVertex - Vertex identifier.
+     * \return True if the vertex is a halo node.
+     */
+    vector<passivedouble> GetVertexHeatFluxes(unsigned short iMarker, unsigned long iVertex) const;
+    
+    /*!
+     * \brief Get the wall normal component of the heat flux at a vertex on a specified marker.
+     * \param[in] iMarker - Marker identifier.
+     * \param[in] iVertex - Vertex identifier.
+     * \return Wall normal component of the heat flux at the vertex.
+     */
+    passivedouble GetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex) const;
+    
+    /*!
+     * \brief Set the wall normal component of the heat flux at a vertex on a specified marker.
+     * \param[in] iMarker - Marker identifier.
+     * \param[in] iVertex - Vertex identifier.
+     * \param[in] val_WallHeatFlux - Value of the normal heat flux.
+     */
+    void SetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallHeatFlux);
+    
+    /*!
+     * \brief Get the thermal conductivity at a vertex on a specified marker.
+     * \param[in] iMarker - Marker identifier.
+     * \param[in] iVertex - Vertex identifier.
+     * \return Thermal conductivity at the vertex.
+     */
+    passivedouble GetThermalConductivity(unsigned short iMarker, unsigned long iVertex) const;
+    
+    /*!
+     * \brief Preprocess the inlets via file input for all solvers.
+     * \param[in] solver_container - Container vector with all the solutions.
+     * \param[in] geometry - Geometrical definition of the problem.
+     * \param[in] config - Definition of the particular problem.
+     */
+    void Inlet_Preprocessing(CSolver ***solver, CGeometry **geometry, CConfig *config) const;
+    
+    /*!
+     * \brief Get all the boundary markers tags.
+     * \return List of boundary markers tags.
+     */
+    vector<string> GetAllBoundaryMarkersTag() const;
+    
+    /*!
+     * \brief Get all the heat transfer boundary markers tags.
+     * \return List of heat transfer boundary markers tags.
+     */
+    vector<string> GetAllCHTMarkersTag() const;
+    
+    /*!
+     * \brief Get all the (subsonic) inlet boundary markers tags.
+     * \return List of inlet boundary markers tags.
+     */
+    vector<string> GetAllInletMarkersTag() const;
+    
+    /*!
+     * \brief Return the sensitivities of the mesh boundary vertices.
+     * \param[in] iMarker - Marker identifier.
+     * \param[in] iVertex - Vertex identifier.
+     * \return Vector of sensitivities.
+     */
+    vector<passivedouble> GetMeshDisp_Sensitivity(unsigned short iMarker, unsigned long iVertex) const;
+    
+    /*!
+     * \brief Set the load in X direction for the structural solver.
+     * \param[in] iMarker - Marker identifier.
+     * \param[in] iVertex - Vertex identifier.
+     * \param[in] LoadX - Value of the load in the direction X.
+     * \param[in] LoadX - Value of the load in the direction Y.
+     * \param[in] LoadX - Value of the load in the direction Z.
+     */
+    void SetFEA_Loads(unsigned short iMarker, unsigned long iVertex, passivedouble LoadX, passivedouble LoadY, passivedouble LoadZ);
+    
+    /*!
+     * \brief Return the displacements from the FEA solver.
+     * \param[in] iMarker - Marker identifier.
+     * \param[in] iVertex - Vertex identifier.
+     * \return Vector of displacements.
+     */
+    vector<passivedouble> GetFEA_Displacements(unsigned short iMarker, unsigned long iVertex) const;
+    
+    /*!
+     * \brief Return the velocities from the FEA Solver.
+     * \param[in] iMarker - Marker identifier.
+     * \param[in] iVertex - Vertex identifier.
+     * \return Vector of velocities.
+     */
+    vector<passivedouble> GetFEA_Velocity(unsigned short iMarker, unsigned long iVertex) const;
+    
+    /*!
+     * \brief Return the velocities from the FEA Solver.
+     * \param[in] iMarker - Marker identifier.
+     * \param[in] iVertex - Vertex identifier.
+     * \return Vector of velocities at time n.
+     */
+    vector<passivedouble> GetFEA_Velocity_n(unsigned short iMarker, unsigned long iVertex) const;
+    
+    /*!
+     * \brief Get the sensitivity of the flow loads for the structural solver.
+     * \param[in] iMarker - Marker identifier.
+     * \param[in] iVertex - Vertex identifier.
+     * \param[in] LoadX - Value of the load in the direction X.
+     * \param[in] LoadX - Value of the load in the direction Y.
+     * \param[in] LoadX - Value of the load in the direction Z.
+     */
+    vector<passivedouble> GetFlowLoad_Sensitivity(unsigned short iMarker, unsigned long iVertex) const;
+    
+    /*!
+     * \brief Get the flow load (from the extra step - the repeated methods should be unified once the postprocessing
+     * strategy is in place).
+     * \param[in] iMarker - Marker identifier.
+     * \param[in] iVertex - Vertex identifier.
+     */
+    vector<passivedouble> GetFlowLoad(unsigned short iMarker, unsigned long iVertex) const;
+    
+    /*!
+     * \brief Set the adjoint of the flow tractions (from the extra step -
+     * the repeated methods should be unified once the postprocessing strategy is in place).
+     * \param[in] iMarker - Marker identifier.
+     * \param[in] iVertex - Vertex identifier.
+     * \param[in] val_AdjointX - Value of the adjoint in the direction X.
+     * \param[in] val_AdjointY - Value of the adjoint in the direction Y.
+     * \param[in] val_AdjointZ - Value of the adjoint in the direction Z.
+     */
+    void SetFlowLoad_Adjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
+                             passivedouble val_AdjointY, passivedouble val_AdjointZ);
+    
+    /*!
+     * \brief Set the adjoint of the structural displacements (from an outside source)
+     * \param[in] iMarker - Marker identifier.
+     * \param[in] iVertex - Vertex identifier.
+     * \param[in] val_AdjointX - Value of the adjoint in the direction X.
+     * \param[in] val_AdjointY - Value of the adjoint in the direction Y.
+     * \param[in] val_AdjointZ - Value of the adjoint in the direction Z.
+     */
+    void SetSourceTerm_DispAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
+                                   passivedouble val_AdjointY, passivedouble val_AdjointZ);
+    void SetSourceTerm_VelAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
+                                  passivedouble val_AdjointY, passivedouble val_AdjointZ);
+    
+    /*!
+     * \brief Set the position of the heat source.
+     * \param[in] alpha - Angle of rotation respect to Z axis.
+     * \param[in] pos_x - Position X.
+     * \param[in] pos_y - Position Y.
+     * \param[in] pos_z - Position Z.
+     */
+    void SetHeatSource_Position(passivedouble alpha, passivedouble pos_x, passivedouble pos_y, passivedouble pos_z);
+    
+    /*!
+     * \brief Set the direction of the inlet.
+     * \param[in] iMarker - Marker index.
+     * \param[in] alpha - Angle (Zpos).
+     */
+    void SetInlet_Angle(unsigned short iMarker, passivedouble alpha);
+    
+    /*!
+     * \brief Sum the number of primal or adjoint variables for all solvers in a given zone.
+     * \param[in] iZone - Index of the zone.
+     * \param[in] adjoint - True to consider adjoint solvers instead of primal.
+     * \return Total number of solution variables.
+     */
+    unsigned short GetTotalNumberOfVariables(unsigned short iZone, bool adjoint) const {
+        unsigned short nVar = 0;
+        for (auto iSol = 0u; iSol < MAX_SOLS; iSol++) {
+            auto solver = solver_container[iZone][INST_0][MESH_0][iSol];
+            if (solver && (solver->GetAdjoint() == adjoint)) nVar += solver->GetnVar();
+        }
+        return nVar;
     }
-    return nVar;
-  }
-
-  /*!
-   * \brief Set the solution of all solvers (adjoint or primal) in a zone.
-   * \param[in] iZone - Index of the zone.
-   * \param[in] adjoint - True to consider adjoint solvers instead of primal.
-   * \param[in] solution - Solution object with interface (iPoint,iVar).
-   * \tparam Old - If true set "old solutions" instead.
-   */
-  template<class Container, bool Old = false>
-  void SetAllSolutions(unsigned short iZone, bool adjoint, const Container& solution) {
-    const auto nPoint = geometry_container[iZone][INST_0][MESH_0]->GetnPoint();
-    for (auto iSol = 0u, offset = 0u; iSol < MAX_SOLS; ++iSol) {
-      auto solver = solver_container[iZone][INST_0][MESH_0][iSol];
-      if (!(solver && (solver->GetAdjoint() == adjoint))) continue;
-      for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint)
-        for (auto iVar = 0ul; iVar < solver->GetnVar(); ++iVar)
-          if (!Old) solver->GetNodes()->SetSolution(iPoint, iVar, solution(iPoint,offset+iVar));
-          else solver->GetNodes()->SetSolution_Old(iPoint, iVar, solution(iPoint,offset+iVar));
-      offset += solver->GetnVar();
+    
+    /*!
+     * \brief Set the solution of all solvers (adjoint or primal) in a zone.
+     * \param[in] iZone - Index of the zone.
+     * \param[in] adjoint - True to consider adjoint solvers instead of primal.
+     * \param[in] solution - Solution object with interface (iPoint,iVar).
+     * \tparam Old - If true set "old solutions" instead.
+     */
+    template<class Container, bool Old = false>
+    void SetAllSolutions(unsigned short iZone, bool adjoint, const Container& solution) {
+        const auto nPoint = geometry_container[iZone][INST_0][MESH_0]->GetnPoint();
+        for (auto iSol = 0u, offset = 0u; iSol < MAX_SOLS; ++iSol) {
+            auto solver = solver_container[iZone][INST_0][MESH_0][iSol];
+            if (!(solver && (solver->GetAdjoint() == adjoint))) continue;
+            for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint)
+                for (auto iVar = 0ul; iVar < solver->GetnVar(); ++iVar)
+                    if (!Old) solver->GetNodes()->SetSolution(iPoint, iVar, solution(iPoint,offset+iVar));
+                    else solver->GetNodes()->SetSolution_Old(iPoint, iVar, solution(iPoint,offset+iVar));
+            offset += solver->GetnVar();
+        }
     }
-  }
-
-  /*!
-   * \brief Set the "old solution" of all solvers (adjoint or primal) in a zone.
-   */
-  template<class Container>
-  void SetAllSolutionsOld(unsigned short iZone, bool adjoint, const Container& solution) {
-    SetAllSolutions<Container,true>(iZone, adjoint, solution);
-  }
-
-  /*!
-   * \brief Get the solution of all solvers (adjoint or primal) in a zone.
-   * \param[in] iZone - Index of the zone.
-   * \param[in] adjoint - True to consider adjoint solvers instead of primal.
-   * \param[out] solution - Solution object with interface (iPoint,iVar).
-   */
-  template<class Container>
-  void GetAllSolutions(unsigned short iZone, bool adjoint, Container& solution) const {
-    const auto nPoint = geometry_container[iZone][INST_0][MESH_0]->GetnPoint();
-    for (auto iSol = 0u, offset = 0u; iSol < MAX_SOLS; ++iSol) {
-      auto solver = solver_container[iZone][INST_0][MESH_0][iSol];
-      if (!(solver && (solver->GetAdjoint() == adjoint))) continue;
-      const auto& sol = solver->GetNodes()->GetSolution();
-      for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint)
-        for (auto iVar = 0ul; iVar < solver->GetnVar(); ++iVar)
-          solution(iPoint,offset+iVar) = SU2_TYPE::GetValue(sol(iPoint,iVar));
-      offset += solver->GetnVar();
+    
+    /*!
+     * \brief Set the "old solution" of all solvers (adjoint or primal) in a zone.
+     */
+    template<class Container>
+    void SetAllSolutionsOld(unsigned short iZone, bool adjoint, const Container& solution) {
+        SetAllSolutions<Container,true>(iZone, adjoint, solution);
     }
-  }
-
+    
+    /*!
+     * \brief Get the solution of all solvers (adjoint or primal) in a zone.
+     * \param[in] iZone - Index of the zone.
+     * \param[in] adjoint - True to consider adjoint solvers instead of primal.
+     * \param[out] solution - Solution object with interface (iPoint,iVar).
+     */
+    template<class Container>
+    void GetAllSolutions(unsigned short iZone, bool adjoint, Container& solution) const {
+        const auto nPoint = geometry_container[iZone][INST_0][MESH_0]->GetnPoint();
+        for (auto iSol = 0u, offset = 0u; iSol < MAX_SOLS; ++iSol) {
+            auto solver = solver_container[iZone][INST_0][MESH_0][iSol];
+            if (!(solver && (solver->GetAdjoint() == adjoint))) continue;
+            const auto& sol = solver->GetNodes()->GetSolution();
+            for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint)
+                for (auto iVar = 0ul; iVar < solver->GetnVar(); ++iVar)
+                    solution(iPoint,offset+iVar) = SU2_TYPE::GetValue(sol(iPoint,iVar));
+            offset += solver->GetnVar();
+        }
+    }
+    
 };
 
 /*!
@@ -789,69 +680,69 @@ class CDriver {
  * \author T. Economon, G. Gori
  */
 class CFluidDriver : public CDriver {
-
+    
 protected:
-   unsigned long Max_Iter;
-
+    unsigned long Max_Iter;
+    
 protected:
-
-  /*!
-   * \brief Constructor of the class.
-   * \param[in] confFile - Configuration file name.
-   * \param[in] val_nZone - Total number of zones.
-   * \param[in] val_nDim - Number of dimensions.
-   * \param[in] MPICommunicator - MPI communicator for SU2.
-   */
-  CFluidDriver(char* confFile,
-               unsigned short val_nZone,
-               SU2_Comm MPICommunicator);
-
+    
+    /*!
+     * \brief Constructor of the class.
+     * \param[in] confFile - Configuration file name.
+     * \param[in] val_nZone - Total number of zones.
+     * \param[in] val_nDim - Number of dimensions.
+     * \param[in] MPICommunicator - MPI communicator for SU2.
+     */
+    CFluidDriver(char* confFile,
+                 unsigned short val_nZone,
+                 SU2_Comm MPICommunicator);
+    
 public:
-  /*!
-   * \brief Destructor of the class.
-   */
-  ~CFluidDriver(void) override;
-
-  /*!
-   * \brief Launch the computation for all zones and all physics.
-   */
-  void StartSolver() override;
-
-  /*!
-   * \brief Run a single iteration of the physics within multiple zones.
-   */
-  void Run() override;
-
-  /*!
-   * \brief Update the dual-time solution within multiple zones.
-   */
-  void Update() override;
-
-  /*!
-   * \brief Output the solution in solution file.
-   */
-  void Output(unsigned long InnerIter) override;
-
-  /*!
-   * \brief Monitor the computation.
-   */
-  bool Monitor(unsigned long ExtIter) override;
-
-  /*!
-   * \brief Perform some pre-processing before an iteration of the physics.
-   */
-  void Preprocess(unsigned long Iter) override;
-
-  /*!
-   * \brief Perform a dynamic mesh deformation, included grid velocity computation and the update of the multigrid structure (multiple zone).
-   */
-  void DynamicMeshUpdate(unsigned long TimeIter) override;
-
-  /*!
-   * \brief Transfer data among different zones (multiple zone).
-   */
-  void Transfer_Data(unsigned short donorZone, unsigned short targetZone);
-
+    /*!
+     * \brief Destructor of the class.
+     */
+    ~CFluidDriver(void) override;
+    
+    /*!
+     * \brief Launch the computation for all zones and all physics.
+     */
+    void StartSolver() override;
+    
+    /*!
+     * \brief Run a single iteration of the physics within multiple zones.
+     */
+    void Run() override;
+    
+    /*!
+     * \brief Update the dual-time solution within multiple zones.
+     */
+    void Update() override;
+    
+    /*!
+     * \brief Output the solution in solution file.
+     */
+    void Output(unsigned long InnerIter) override;
+    
+    /*!
+     * \brief Monitor the computation.
+     */
+    bool Monitor(unsigned long ExtIter) override;
+    
+    /*!
+     * \brief Perform some pre-processing before an iteration of the physics.
+     */
+    void Preprocess(unsigned long Iter) override;
+    
+    /*!
+     * \brief Perform a dynamic mesh deformation, included grid velocity computation and the update of the multigrid structure (multiple zone).
+     */
+    void DynamicMeshUpdate(unsigned long TimeIter) override;
+    
+    /*!
+     * \brief Transfer data among different zones (multiple zone).
+     */
+    void Transfer_Data(unsigned short donorZone, unsigned short targetZone);
+    
 };
 
 
@@ -862,50 +753,50 @@ class CFluidDriver : public CDriver {
  */
 class CTurbomachineryDriver : public CFluidDriver {
 private:
-  COutputLegacy* output_legacy;
-
+    COutputLegacy* output_legacy;
+    
 public:
-
-  /*!
-   * \brief Constructor of the class.
-   * \param[in] confFile - Configuration file name.
-   * \param[in] val_nZone - Total number of zones.
-   * \param[in] val_nDim - Number of dimensions.
-   * \param[in] val_periodic - Bool for periodic BCs.
-   * \param[in] MPICommunicator - MPI communicator for SU2.
-   */
-  CTurbomachineryDriver(char* confFile,
-                        unsigned short val_nZone,
-                        SU2_Comm MPICommunicator);
-
-  /*!
-   * \brief Destructor of the class.
-   */
-  ~CTurbomachineryDriver(void) override;
-
-  /*!
-   * \brief Run a single iteration of the physics within multiple zones.
-   */
-
-  void Run() override;
-
-  /*!
-   * \brief Set Mixing Plane interface within multiple zones.
-   */
-  void SetMixingPlane(unsigned short iZone);
-
-  /*!
-   * \brief Set Mixing Plane interface within multiple zones.
-   */
-  void SetTurboPerformance(unsigned short targetZone);
-
-  /*!
-   * \brief Monitor the computation.
-   */
-  bool Monitor(unsigned long TimeIter) override;
-
-
-
+    
+    /*!
+     * \brief Constructor of the class.
+     * \param[in] confFile - Configuration file name.
+     * \param[in] val_nZone - Total number of zones.
+     * \param[in] val_nDim - Number of dimensions.
+     * \param[in] val_periodic - Bool for periodic BCs.
+     * \param[in] MPICommunicator - MPI communicator for SU2.
+     */
+    CTurbomachineryDriver(char* confFile,
+                          unsigned short val_nZone,
+                          SU2_Comm MPICommunicator);
+    
+    /*!
+     * \brief Destructor of the class.
+     */
+    ~CTurbomachineryDriver(void) override;
+    
+    /*!
+     * \brief Run a single iteration of the physics within multiple zones.
+     */
+    
+    void Run() override;
+    
+    /*!
+     * \brief Set Mixing Plane interface within multiple zones.
+     */
+    void SetMixingPlane(unsigned short iZone);
+    
+    /*!
+     * \brief Set Mixing Plane interface within multiple zones.
+     */
+    void SetTurboPerformance(unsigned short targetZone);
+    
+    /*!
+     * \brief Monitor the computation.
+     */
+    bool Monitor(unsigned long TimeIter) override;
+    
+    
+    
 };
 
 /*!
@@ -914,61 +805,61 @@ class CTurbomachineryDriver : public CFluidDriver {
  * \author T. Economon
  */
 class CHBDriver : public CFluidDriver {
-
+    
 private:
-  COutputLegacy* output_legacy;
-  unsigned short nInstHB;
-  su2double **D; /*!< \brief Harmonic Balance operator. */
-
+    COutputLegacy* output_legacy;
+    unsigned short nInstHB;
+    su2double **D; /*!< \brief Harmonic Balance operator. */
+    
 public:
-
-  /*!
-   * \brief Constructor of the class.
-   * \param[in] confFile - Configuration file name.
-   * \param[in] val_nZone - Total number of zones.
-   * \param[in] val_nDim - Number of dimensions.
-   * \param[in] MPICommunicator - MPI communicator for SU2.
-   */
-  CHBDriver(char* confFile,
-            unsigned short val_nZone,
-            SU2_Comm MPICommunicator);
-
-  /*!
-   * \brief Destructor of the class.
-   */
-  ~CHBDriver(void) override;
-
-  /*!
-   * \brief Run a single iteration of a Harmonic Balance problem.
-   */
-  void Run() override;
-
-  /*!
-   * \brief Computation and storage of the Harmonic Balance method source terms.
-   * \author T. Economon, K. Naik
-   * \param[in] iZone - Current zone number.
-   */
-  void SetHarmonicBalance(unsigned short iZone);
-
-  /*!
-   * \brief Precondition Harmonic Balance source term for stability
-   * \author J. Howison
-   */
-  void StabilizeHarmonicBalance();
-
-  /*!
-   * \brief Computation of the Harmonic Balance operator matrix for harmonic balance.
-   * \author A. Rubino, S. Nimmagadda
-   */
-  void ComputeHB_Operator();
-
-  /*!
-   * \brief Update the solution for the Harmonic Balance.
-   */
-  void Update() override;
-
-  /*!
-   * \brief Reset the convergence flag (set to false) of the solver for the Harmonic Balance.
-   */
-  void ResetConvergence() override;
+    
+    /*!
+     * \brief Constructor of the class.
+     * \param[in] confFile - Configuration file name.
+     * \param[in] val_nZone - Total number of zones.
+     * \param[in] val_nDim - Number of dimensions.
+     * \param[in] MPICommunicator - MPI communicator for SU2.
+     */
+    CHBDriver(char* confFile,
+              unsigned short val_nZone,
+              SU2_Comm MPICommunicator);
+    
+    /*!
+     * \brief Destructor of the class.
+     */
+    ~CHBDriver(void) override;
+    
+    /*!
+     * \brief Run a single iteration of a Harmonic Balance problem.
+     */
+    void Run() override;
+    
+    /*!
+     * \brief Computation and storage of the Harmonic Balance method source terms.
+     * \author T. Economon, K. Naik
+     * \param[in] iZone - Current zone number.
+     */
+    void SetHarmonicBalance(unsigned short iZone);
+    
+    /*!
+     * \brief Precondition Harmonic Balance source term for stability
+     * \author J. Howison
+     */
+    void StabilizeHarmonicBalance();
+    
+    /*!
+     * \brief Computation of the Harmonic Balance operator matrix for harmonic balance.
+     * \author A. Rubino, S. Nimmagadda
+     */
+    void ComputeHB_Operator();
+    
+    /*!
+     * \brief Update the solution for the Harmonic Balance.
+     */
+    void Update() override;
+    
+    /*!
+     * \brief Reset the convergence flag (set to false) of the solver for the Harmonic Balance.
+     */
+    void ResetConvergence() override;
 };
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index fa14d73fe34..dcb8447d591 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -107,8 +107,7 @@
 #include <fenv.h>
 
 CDriver::CDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator, bool dummy_geo) :
-  config_file_name(confFile), StartTime(0.0), StopTime(0.0), UsedTime(0.0),
-  TimeIter(0), nZone(val_nZone), StopCalc(false), fsi(false), fem_solver(false), dry_run(dummy_geo) {
+  CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false), fem_solver(false), dry_run(dummy_geo) {
 
   /*--- Initialize Medipack (must also be here so it is initialized from python) ---*/
 #ifdef HAVE_MPI
diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index 206c81492d1..2f85546f4d3 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -166,99 +166,6 @@ passivedouble CDriver::Get_LiftCoeff() const {
   return SU2_TYPE::GetValue(CLift);
 }
 
-/////////////////////////////////////////////////////////////////////////////
-/* Functions to obtain information from the geometry/mesh                  */
-/////////////////////////////////////////////////////////////////////////////
-
-unsigned long CDriver::GetNumberVertices(unsigned short iMarker) const {
-
-  return geometry_container[ZONE_0][INST_0][MESH_0]->nVertex[iMarker];
-
-}
-
-unsigned long CDriver::GetNumberHaloVertices(unsigned short iMarker) const {
-
-  unsigned long nHaloVertices, iVertex, iPoint;
-
-  nHaloVertices = 0;
-  for(iVertex = 0; iVertex < geometry_container[ZONE_0][INST_0][MESH_0]->nVertex[iMarker]; iVertex++){
-    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-    if(!(geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint))) nHaloVertices += 1;
-  }
-
-  return nHaloVertices;
-
-}
-
-unsigned long CDriver::GetVertexGlobalIndex(unsigned short iMarker, unsigned long iVertex) const {
-
-  unsigned long iPoint, GlobalIndex;
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  GlobalIndex = geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetGlobalIndex(iPoint);
-
-  return GlobalIndex;
-
-}
-
-bool CDriver::IsAHaloNode(unsigned short iMarker, unsigned long iVertex) const {
-
-  unsigned long iPoint;
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  if(geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint)) return false;
-  else return true;
-
-}
-
-vector<passivedouble> CDriver::GetInitialMeshCoord(unsigned short iMarker, unsigned long iVertex) const {
-
-  vector<su2double> coord(3,0.0);
-  vector<passivedouble> coord_passive(3, 0.0);
-
-  auto iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  for (auto iDim = 0 ; iDim < nDim ; iDim++){
-   coord[iDim] = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord(iPoint,iDim);
-  }
-
-  coord_passive[0] = SU2_TYPE::GetValue(coord[0]);
-  coord_passive[1] = SU2_TYPE::GetValue(coord[1]);
-  coord_passive[2] = SU2_TYPE::GetValue(coord[2]);
-
-  return coord_passive;
-}
-
-vector<passivedouble> CDriver::GetVertexNormal(unsigned short iMarker, unsigned long iVertex, bool unitNormal) const {
-
-  su2double *Normal;
-  su2double Area;
-  vector<su2double> ret_Normal(3, 0.0);
-  vector<passivedouble> ret_Normal_passive(3, 0.0);
-
-  Normal = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNormal();
-
-  if (!unitNormal) {
-
-    ret_Normal_passive[0] = SU2_TYPE::GetValue(Normal[0]);
-    ret_Normal_passive[1] = SU2_TYPE::GetValue(Normal[1]);
-    if(nDim>2) ret_Normal_passive[2] = SU2_TYPE::GetValue(Normal[2]);
-
-    return ret_Normal_passive;
-  }
-
-  Area = GeometryToolbox::Norm(nDim, Normal);
-
-  ret_Normal[0] = Normal[0]/Area;
-  ret_Normal[1] = Normal[1]/Area;
-  if(nDim>2) ret_Normal[2] = Normal[2]/Area;
-
-  ret_Normal_passive[0] = SU2_TYPE::GetValue(ret_Normal[0]);
-  ret_Normal_passive[1] = SU2_TYPE::GetValue(ret_Normal[1]);
-  ret_Normal_passive[2] = SU2_TYPE::GetValue(ret_Normal[2]);
-
-  return ret_Normal_passive;
-}
-
 //////////////////////////////////////////////////////////////////////////////////
 /* Functions to obtain global parameters from SU2 (time steps, delta t, ecc...) */
 //////////////////////////////////////////////////////////////////////////////////
@@ -430,23 +337,6 @@ vector<string> CDriver::GetAllBoundaryMarkersTag() const {
   return boundariesTagList;
 }
 
-vector<string> CDriver::GetAllDeformMeshMarkersTag() const {
-
-  vector<string> interfaceBoundariesTagList;
-  unsigned short iMarker, nBoundariesMarker;
-  string Marker_Tag;
-
-  nBoundariesMarker = config_container[ZONE_0]->GetnMarker_Deform_Mesh();
-  interfaceBoundariesTagList.resize(nBoundariesMarker);
-
-  for(iMarker=0; iMarker < nBoundariesMarker; iMarker++){
-    Marker_Tag = config_container[ZONE_0]->GetMarker_Deform_Mesh_TagBound(iMarker);
-    interfaceBoundariesTagList[iMarker] = Marker_Tag;
-  }
-
-  return interfaceBoundariesTagList;
-}
-
 vector<string> CDriver::GetAllCHTMarkersTag() const {
 
   vector<string> CHTBoundariesTagList;
@@ -486,65 +376,6 @@ vector<string> CDriver::GetAllInletMarkersTag() const {
   return BoundariesTagList;
 }
 
-map<string, int> CDriver::GetAllBoundaryMarkers() const {
-
-  map<string, int>  allBoundariesMap;
-  unsigned short iMarker, nBoundaryMarkers;
-  string Marker_Tag;
-
-  nBoundaryMarkers = config_container[ZONE_0]->GetnMarker_All();
-
-  for(iMarker=0; iMarker < nBoundaryMarkers; iMarker++){
-    Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
-    allBoundariesMap[Marker_Tag] = iMarker;
-  }
-
-  return allBoundariesMap;
-}
-
-map<string, string> CDriver::GetAllBoundaryMarkersType() const {
-
-  map<string, string> allBoundariesTypeMap;
-  unsigned short iMarker, KindBC;
-  string Marker_Tag, Marker_Type;
-
-  for(iMarker=0; iMarker < config_container[ZONE_0]->GetnMarker_All(); iMarker++){
-    Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
-    KindBC = config_container[ZONE_0]->GetMarker_All_KindBC(iMarker);
-    switch(KindBC){
-      case EULER_WALL:
-        Marker_Type = "EULER_WALL";
-        break;
-      case FAR_FIELD:
-        Marker_Type = "FARFIELD";
-        break;
-      case ISOTHERMAL:
-        Marker_Type = "ISOTHERMAL";
-        break;
-      case HEAT_FLUX:
-        Marker_Type = "HEATFLUX";
-        break;
-      case INLET_FLOW:
-        Marker_Type = "INLET_FLOW";
-        break;
-      case OUTLET_FLOW:
-        Marker_Type = "OUTLET_FLOW";
-        break;
-      case SYMMETRY_PLANE:
-        Marker_Type = "SYMMETRY";
-        break;
-      case SEND_RECEIVE:
-        Marker_Type = "SEND_RECEIVE";
-        break;
-      default:
-        Marker_Type = "UNKNOWN_TYPE";
-    }
-    allBoundariesTypeMap[Marker_Tag] = Marker_Type;
-  }
-
-  return allBoundariesTypeMap;
-}
-
 void CDriver::SetHeatSource_Position(passivedouble alpha, passivedouble pos_x, passivedouble pos_y, passivedouble pos_z){
 
   CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][RAD_SOL];
@@ -837,34 +668,6 @@ void CDriver::SetSourceTerm_VelAdjoint(unsigned short iMarker, unsigned long iVe
 
 }
 
-////////////////////////////////////////////////////////////////////////////////
-/* Functions related to mesh deformation */
-////////////////////////////////////////////////////////////////////////////////
-
-void CDriver::SetMeshDisplacement(unsigned short iMarker, unsigned long iVertex, passivedouble DispX, passivedouble DispY, passivedouble DispZ) {
-
-  unsigned long iPoint;
-  su2double MeshDispl[3] =  {0.0,0.0,0.0};
-
-  MeshDispl[0] = DispX;
-  MeshDispl[1] = DispY;
-  MeshDispl[2] = DispZ;
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-
-  solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->SetBound_Disp(iPoint,MeshDispl);
-
-}
-
-void CDriver::CommunicateMeshDisplacement(void) {
-
-  solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->InitiateComms(geometry_container[ZONE_0][INST_0][MESH_0],
-                                                                    config_container[ZONE_0], MESH_DISPLACEMENTS);
-  solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->CompleteComms(geometry_container[ZONE_0][INST_0][MESH_0],
-                                                                    config_container[ZONE_0], MESH_DISPLACEMENTS);
-
-}
-
 ////////////////////////////////////////////////////////////////////////////////
 /* Functions related to flow loads */
 ////////////////////////////////////////////////////////////////////////////////
diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index 8196faeda5a..5c1d7c0da4e 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -1,8 +1,8 @@
- /*!
+/*!
  * \file CDeformationDriver.hpp
  * \brief Headers of the main subroutines for driving the mesh deformation.
- * \author T. Economon, H. Kline, R. Sanchez
- * \version 7.1.1 "Blackbird"
+ * \author A. Gastaldi, H. Patel
+ * \version 7.3.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -38,32 +38,12 @@
 #include "../../../SU2_CFD/include/output/COutput.hpp"
 #include "../../../SU2_CFD/include/numerics/CNumerics.hpp"
 #include "../../../Common/include/geometry/CGeometry.hpp"
+#include "../../../Common/include/drivers/CDriverBase.hpp"
+
+class CDeformationDriver : public CDriverBase {
 
-/*!
- * \class CDeformationDriver
- * \brief Class for driving mesh deformation solvers.
- * \author A. Gastaldi, H. Patel
- * \version 7.1.1 "Blackbird"
- */
-class CDeformationDriver {
 protected:
-  char config_file_name[MAX_STRING_SIZE];
-  int rank,
-      size;
-  su2double StartTime,                          /*!< \brief Start point of the timer for performance benchmarking.*/
-            StopTime,                           /*!< \brief Stop point of the timer for performance benchmarking.*/
-            UsedTimePreproc,                    /*!< \brief Elapsed time between Start and Stop point of the timer for tracking preprocessing phase.*/
-            UsedTimeCompute,                    /*!< \brief Elapsed time between Start and Stop point of the timer for tracking compute phase.*/
-            UsedTime;                           /*!< \brief Elapsed time between Start and Stop point of the timer.*/
-  unsigned short iZone, nZone = SINGLE_ZONE;
-  CConfig *driver_config;                       /*!< \brief Definition of the driver configuration. */
-  CConfig **config_container;                   /*!< \brief Definition of the particular problem. */
-  CGeometry **geometry_container;             /*!< \brief Geometrical definition of the problem. */
-  CSurfaceMovement **surface_movement;          /*!< \brief Surface movement classes of the problem. */
-  CVolumetricMovement **grid_movement;         /*!< \brief Volume grid movement classes of the problem. */
-  CSolver **solver_container;
   CNumerics ***numerics_container;
-  COutput **output_container;                   /*!< \brief Pointer to the COutput class. */
 
 public:
   /*!
@@ -93,88 +73,7 @@ class CDeformationDriver {
    */
   void Postprocessing();
 
-  /*!
-   * \brief Get all the deformable boundary marker tags.
-   * \return List of deformable boundary markers tags.
-   */
-  vector<string> GetAllDeformMeshMarkersTag() const;
-
-  /*!
-   * \brief Get all the boundary markers tags with their associated indices.
-   * \return List of boundary markers tags with their indices.
-   */
-  map<string, int> GetAllBoundaryMarkers() const;
-
-  /*!
-   * \brief Get all the boundary markers tags with their associated types.
-   * \return List of boundary markers tags with their types.
-   */
-  map<string, string> GetAllBoundaryMarkersType() const;
-
-  /*!
-   * \brief Get the number of vertices (halo nodes included) from a specified marker.
-   * \param[in] iMarker -  Marker identifier.
-   * \return Number of vertices.
-   */
-  unsigned long GetNumberVertices(unsigned short iMarker) const;
-
-  /*!
-   * \brief Get the number of halo vertices from a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \return Number of vertices.
-   */
-  unsigned long GetNumberHaloVertices(unsigned short iMarker) const;
-
-  /*!
-   * \brief Check if a vertex is physical or not (halo node) on a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return True if the specified vertex is a halo node.
-   */
-  bool IsAHaloNode(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Get the global index of a vertex on a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Vertex global index.
-   */
-  unsigned long GetVertexGlobalIndex(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Get undeformed coordinates from the mesh solver.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return x,y,z coordinates of the vertex.
-   */
-  vector<passivedouble> GetInitialMeshCoord(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Get the unit normal (vector) at a vertex on a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Unit normal (vector) at the vertex.
-   */
-  vector<passivedouble> GetVertexNormal(unsigned short iMarker, unsigned long iVertex, bool unitNormal = false) const;
-
-  inline vector<passivedouble> GetVertexUnitNormal(unsigned short iMarker, unsigned long iVertex) const {
-    return GetVertexNormal(iMarker, iVertex, true);
-  }
-  
-  /*!
-   * \brief Set the mesh displacement for the elasticity mesh solver.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \param[in] DispX - Value of the mesh displacement in the direction X.
-   * \param[in] DispY - Value of the mesh displacement in the direction Y.
-   * \param[in] DispZ - Value of the mesh displacement in the direction Z.
-   */
-  void SetMeshDisplacement(unsigned short iMarker, unsigned long iVertex, passivedouble DispX, passivedouble DispY, passivedouble DispZ);
-
-  /*!
-   * \brief Communicate the boundary mesh displacements in a python call
-   */
-  void CommunicateMeshDisplacement(void);
+  void CommunicateMeshDisplacements(void);
 
 protected:
   /*!
diff --git a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
index 36cf9daab8f..41a1df49b2c 100644
--- a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
@@ -1,8 +1,8 @@
 /*!
-* \file CDiscAdjDeformationDriver.cpp
-* \brief Main subroutines for driving the projection of sensitivities.
+ * \file CDiscAdjDeformationDriver.cpp
+ * \brief Headers of the main subroutines for driving the projection of sensitivities.
  * \author T. Economon, H. Kline, R. Sanchez
- * \version 7.1.1 "Blackbird"
+ * \version 7.3.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -40,115 +40,126 @@
 #include "../../../SU2_CFD/include/output/CBaselineOutput.hpp"
 #include "../../../SU2_CFD/include/solvers/CBaselineSolver.hpp"
 
+#include "../../../Common/include/drivers/CDriverBase.hpp"
+#include "../../../SU2_CFD/include/solvers/CGradientSmoothingSolver.hpp"
+#include "../../../SU2_CFD/include/numerics/CGradSmoothing.hpp"
+
 /*!
  * \class CDiscAdjDeformationDriver
- * \brief Class for driving sensitivity DiscAdjDeformations.
+ * \brief Class for driving sensitivity projections.
  * \author A. Gastaldi, H. Patel
- * \version 7.1.1 "Blackbird"
+ * \version 7.3.0 "Blackbird"
  */
-class CDiscAdjDeformationDriver {
-protected:
-  char config_file_name[MAX_STRING_SIZE];
-  int rank,
-      size;
-  unsigned short iZone, nZone = SINGLE_ZONE;
-  unsigned short iInst;
-  unsigned short* nInst;
-  su2double StartTime,                          /*!< \brief Start point of the timer for performance benchmarking.*/
-            StopTime,                           /*!< \brief Stop point of the timer for performance benchmarking.*/
-            UsedTimePreproc,                    /*!< \brief Elapsed time between Start and Stop point of the timer for tracking preprocessing phase.*/
-            UsedTimeCompute,                    /*!< \brief Elapsed time between Start and Stop point of the timer for tracking compute phase.*/
-            UsedTime;                           /*!< \brief Elapsed time between Start and Stop point of the timer.*/
-  su2double** Gradient;
-  ofstream Gradient_file;
-  CConfig *driver_config;                       /*!< \brief Definition of the driver configuration. */
-  CConfig **config_container;                   /*!< \brief Definition of the particular problem. */
-  CGeometry ***geometry_container;             /*!< \brief Geometrical definition of the problem. */
-  CSurfaceMovement **surface_movement;
-  CVolumetricMovement **grid_movement;
-  COutput **output_container;                   /*!< \brief Pointer to the COutput class. */
+class CDiscAdjDeformationDriver : public CDriverBase {
 
+protected:
+    su2double** Gradient;
+    ofstream Gradient_file;
+    CGeometry ***geometry_container;              /*!< \brief Geometrical definition of the problem. */
+    CSurfaceMovement **surface_movement;
+    CVolumetricMovement **grid_movement;
+    
 public:
-  /*!
-   * \brief Constructor of the class.
-   * \param[in] confFile - Configuration file name.
-   * \param[in] MPICommunicator - MPI communicator for SU2.
-   */
-  CDiscAdjDeformationDriver(char* confFile, SU2_Comm MPICommunicator);
-
-  /*!
-   * \brief Destructor of the class.
-   */
-  ~CDiscAdjDeformationDriver(void);
-
-  /*!
-   * \brief [Overload] Launch the computation for single-zone problems.
-   */
-  void Run();
-
-  /*!
-   * \brief Deallocation routine
-   */
-  void Postprocessing();
-
+    /*!
+     * \brief Constructor of the class.
+     * \param[in] confFile - Configuration file name.
+     * \param[in] MPICommunicator - MPI communicator for SU2.
+     */
+    CDiscAdjDeformationDriver(char* confFile, SU2_Comm MPICommunicator);
+    
+    /*!
+     * \brief Destructor of the class.
+     */
+    ~CDiscAdjDeformationDriver(void);
+    
+    /*!
+     * \brief [Overload] Launch the computation for single-zone problems.
+     */
+    void Run();
+    
+    /*!
+     * \brief Deallocation routine
+     */
+    void Postprocessing();
+    
 protected:
-  /*!
-   * \brief Init_Containers
-   */
-  void SetContainers_Null();
-
-  /*!
-   * \brief Read in the config and mesh files.
-   */
-  void Input_Preprocessing();
-
-  /*!
-   * \brief Construction of the edge-based data structure.
-   */
-  void Geometrical_Preprocessing();
-
-  /*!
-   * \brief Preprocess the output container.
-   */
-  void Output_Preprocessing();
-
-  /*!
-   * \brief DiscAdjDeformation of the surface sensitivity using finite differences (FD).
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] surface_movement - Surface movement class of the problem.
-   * \param[in] Gradient_file - Output file to store the gradient data.
-   */
-
-  void SetDiscAdjDeformation_FD(CGeometry *geometry, CConfig *config, CSurfaceMovement *surface_movement, su2double **Gradient);
-
-  /*!
-   * \brief DiscAdjDeformation of the surface sensitivity using algorithmic differentiation (AD).
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] surface_movement - Surface movement class of the problem.
-   * \param[in] Gradient_file - Output file to store the gradient data.
-   */
-
-  void SetDiscAdjDeformation_AD(CGeometry *geometry, CConfig *config, CSurfaceMovement *surface_movement, su2double **Gradient);
-
-  /*!
-   * \brief Prints the gradient information to a file.
-   * \param[in] Gradient - The gradient data.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] Gradient_file - Output file to store the gradient data.
-   */
-
-  void OutputGradient(su2double** Gradient, CConfig* config, ofstream& Gradient_file);
-
-  /*!
-   * \brief Write the sensitivity (including mesh sensitivity) computed with the discrete adjoint method
-   *  on the surface and in the volume to a file.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] val_nZone - Number of Zones.
-   */
-
-  void SetSensitivity_Files(CGeometry ***geometry, CConfig **config, unsigned short val_nZone);
-
+    /*!
+     * \brief Init_Containers
+     */
+    void SetContainers_Null();
+    
+    /*!
+     * \brief Read in the config and mesh files.
+     */
+    void Input_Preprocessing();
+    
+    /*!
+     * \brief Construction of the edge-based data structure.
+     */
+    void Geometrical_Preprocessing();
+    
+    /*!
+     * \brief Preprocess the output container.
+     */
+    void Output_Preprocessing();
+    
+    /*!
+     * \brief Projection of the surface sensitivity using finite differences (FD).
+     * \param[in] geometry - Geometrical definition of the problem.
+     * \param[in] config - Definition of the particular problem.
+     * \param[in] surface_movement - Surface movement class of the problem.
+     * \param[in] Gradient_file - Output file to store the gradient data.
+     */
+    
+    void SetProjection_FD(CGeometry *geometry, CConfig *config, CSurfaceMovement *surface_movement, su2double **Gradient);
+    
+    /*!
+     * \brief Projection of the surface sensitivity using algorithmic differentiation (AD).
+     * \param[in] geometry - Geometrical definition of the problem.
+     * \param[in] config - Definition of the particular problem.
+     * \param[in] surface_movement - Surface movement class of the problem.
+     * \param[in] Gradient_file - Output file to store the gradient data.
+     */
+    
+    void SetProjection_AD(CGeometry *geometry, CConfig *config, CSurfaceMovement *surface_movement, su2double **Gradient);
+    
+    /*!
+     * \brief Prints the gradient information to a file.
+     * \param[in] Gradient - The gradient data.
+     * \param[in] config - Definition of the particular problem.
+     * \param[in] Gradient_file - Output file to store the gradient data.
+     */
+    
+    void OutputGradient(su2double** Gradient, CConfig* config, ofstream& Gradient_file);
+    
+    /*!
+     * \brief Write the sensitivity (including mesh sensitivity) computed with the discrete adjoint method
+     *  on the surface and in the volume to a file.
+     * \param[in] geometry - Geometrical definition of the problem.
+     * \param[in] config - Definition of the particular problem.
+     * \param[in] val_nZone - Number of Zones.
+     */
+    
+    void SetSensitivity_Files(CGeometry ***geometry, CConfig **config, unsigned short val_nZone);
+    
+    /*!
+     * \brief Treatment of derivatives with the Sobolev smoothing solver.
+     * \param[in] geometry - Geometrical definition of the problem.
+     * \param[in] config - Definition of the particular problem.
+     * \param[in] grid_movement - Volumetric movement class of the problem.
+     */
+    
+    void DerivativeTreatment_MeshSensitivity(CGeometry *geometry, CConfig *config, CVolumetricMovement *grid_movement);
+    
+    /*!
+     * \brief Treatment of derivatives with the Sobolev smoothing solver.
+     * \param[in] geometry - Geometrical definition of the problem.
+     * \param[in] config - Definition of the particular problem.
+     * \param[in] grid_movement - Volumetric movement class of the problem.
+     * \param[in] surface_movement - Surface movement class of the problem.
+     * \param[in] Gradient - Output array to store the gradient data.
+     */
+    
+    void DerivativeTreatment_Gradient(CGeometry *geometry, CConfig *config, CVolumetricMovement *grid_movement, CSurfaceMovement *surface_movement, su2double **Gradient);
+    
 };
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 81973fc7608..90563e93f2f 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -1,8 +1,8 @@
 /*!
- * \file CDeformationDriver.hpp
+ * \file CDeformationDriver.cpp
  * \brief Main subroutines for driving the mesh deformation.
- * \author T. Economon, H. Kline, R. Sanchez
- * \version 7.1.1 "Blackbird"
+ * \author A. Gastaldi, H. Patel
+ * \version 7.3.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -25,7 +25,6 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #include "../../include/drivers/CDeformationDriver.hpp"
 
 #include "../../../Common/include/geometry/CPhysicalGeometry.hpp"
@@ -36,770 +35,589 @@
 
 using namespace std;
 
-CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator) {
-
-  /*--- Initialize Medipack (must also be here so it is initialized from python) ---*/
-  #ifdef HAVE_MPI
-    #if defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)
-      SU2_MPI::Init_AMPI();
-    #endif
-  #endif
-
-  SU2_MPI::SetComm(MPICommunicator);
-
-  rank = SU2_MPI::GetRank();
-  size = SU2_MPI::GetSize();
-
-  /*--- Copy the config filename ---*/
-  strcpy(config_file_name, confFile);
-
-  /*--- Initialize the configuration of the driver ---*/
-  driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DEF);
-
-  nZone = driver_config->GetnZone();
-
-  /*--- Initialize containers --- */
-
-  SetContainers_Null();
-
-  /*--- Preprocessing of the config files. ---*/
-
-  Input_Preprocessing();
-
-  /*--- Set up a timer for performance benchmarking ---*/
-
-  StartTime = SU2_MPI::Wtime();
-
-  /*--- Preprocessing of the geometry for all zones. ---*/
-
-  Geometrical_Preprocessing();
-
-  /*--- Preprocessing of the output for all zones. ---*/
-
-  Output_Preprocessing();
-
-  if (driver_config->GetDeform_Mesh()){
-
-    /*--- Preprocessing of the mesh solver for all zones. ---*/
-
-    Solver_Preprocessing();
-
-    /*--- Preprocessing of the mesh solver for all zones. ---*/
-
-    Numerics_Preprocessing();
-
-  }
-
-  /*--- Preprocessing time is reported now, but not included in the next compute portion. ---*/
-
-  StopTime = SU2_MPI::Wtime();
-
-  /*--- Compute/print the total time for performance benchmarking. ---*/
-
-  UsedTime = StopTime-StartTime;
-  UsedTimePreproc    = UsedTime;
-  UsedTimeCompute    = 0.0;
-
+CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator):
+    CDriverBase(confFile, 1, MPICommunicator) 
+{
+    
+    /*--- Initialize Medipack (must also be here so it is initialized from python) ---*/
+#ifdef HAVE_MPI
+#if defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)
+    SU2_MPI::Init_AMPI();
+#endif
+#endif
+    
+    SU2_MPI::SetComm(MPICommunicator);
+    
+    rank = SU2_MPI::GetRank();
+    size = SU2_MPI::GetSize();
+    
+    /*--- Copy the config filename ---*/
+    strcpy(config_file_name, confFile);
+    
+    /*--- Initialize the configuration of the driver ---*/
+    driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DEF);
+    
+    nZone = driver_config->GetnZone();
+    
+    /*--- Initialize containers --- */
+    
+    SetContainers_Null();
+    
+    /*--- Preprocessing of the config files. ---*/
+    
+    Input_Preprocessing();
+    
+    /*--- Set up a timer for performance benchmarking ---*/
+    
+    StartTime = SU2_MPI::Wtime();
+    
+    /*--- Preprocessing of the geometry for all zones. ---*/
+    
+    Geometrical_Preprocessing();
+    
+    /*--- Preprocessing of the output for all zones. ---*/
+    
+    Output_Preprocessing();
+    
+    if (driver_config->GetDeform_Mesh()){
+        
+        /*--- Preprocessing of the mesh solver for all zones. ---*/
+        
+        Solver_Preprocessing();
+        
+        /*--- Preprocessing of the mesh solver for all zones. ---*/
+        
+        Numerics_Preprocessing();
+        
+    }
+    
+    /*--- Preprocessing time is reported now, but not included in the next compute portion. ---*/
+    
+    StopTime = SU2_MPI::Wtime();
+    
+    /*--- Compute/print the total time for performance benchmarking. ---*/
+    
+    UsedTime = StopTime-StartTime;
+    UsedTimePreproc    = UsedTime;
+    UsedTimeCompute    = 0.0;
+    
 }
 
 CDeformationDriver::~CDeformationDriver(void) {
-
+    
 }
 
 void CDeformationDriver::SetContainers_Null() {
-
+    
     /*--- Create pointers to all of the classes that may be used throughout
-        the SU2_DEF code. In general, the pointers are instantiated down a
-        hierarchy over all zones as described in the comments below. ---*/
+     the SU2_DEF code. In general, the pointers are instantiated down a
+     hierarchy over all zones as described in the comments below. ---*/
     config_container   = new CConfig*[nZone];
     output_container   = new COutput*[nZone];
-    geometry_container = new CGeometry*[nZone];
+    geometry_container = new CGeometry***[nZone];
     surface_movement   = new CSurfaceMovement*[nZone];
-    grid_movement      = new CVolumetricMovement*[nZone];
-
-    solver_container   = new CSolver*[nZone];
+    grid_movement      = new CVolumetricMovement**[nZone];
+    
+    solver_container   = new CSolver****[nZone];
     numerics_container = new CNumerics**[nZone];
-
+    
     for (iZone = 0; iZone < nZone; iZone++) {
-        config_container[iZone]       = nullptr;
-        output_container[iZone]       = nullptr;
-        geometry_container[iZone]     = nullptr;
-        surface_movement[iZone]       = nullptr;
-        grid_movement[iZone]          = nullptr;
-        solver_container[iZone]       = nullptr;
-        numerics_container[iZone]     = nullptr;
+        config_container[iZone]   = nullptr;
+        output_container[iZone]   = nullptr;
+        geometry_container[iZone] = nullptr;
+        surface_movement[iZone]   = nullptr;
+        grid_movement[iZone]      = nullptr;
+        solver_container[iZone]   = nullptr;
+        numerics_container[iZone] = nullptr;
     }
 }
 
 void CDeformationDriver::Input_Preprocessing() {
-
+    
     /*--- Initialize a char to store the zone filename ---*/
     char zone_file_name[MAX_STRING_SIZE];
-
+    
     /*--- Loop over all zones to initialize the various classes. In most
-       cases, nZone is equal to one. This represents the solution of a partial
-       differential equation on a single block, unstructured mesh. ---*/
-
+     cases, nZone is equal to one. This represents the solution of a partial
+     differential equation on a single block, unstructured mesh. ---*/
+    
     for (iZone = 0; iZone < nZone; iZone++) {
-
-    /*--- Definition of the configuration option class for all zones. In this
-          constructor, the input configuration file is parsed and all options are
-          read and stored. ---*/
-
+        
+        /*--- Definition of the configuration option class for all zones. In this
+         constructor, the input configuration file is parsed and all options are
+         read and stored. ---*/
+        
         if (driver_config->GetnConfigFiles() > 0){
             strcpy(zone_file_name, driver_config->GetConfigFilename(iZone).c_str());
             config_container[iZone] = new CConfig(driver_config, zone_file_name, SU2_COMPONENT::SU2_DEF, iZone, nZone, true);
         } else {
             config_container[iZone] = new CConfig(driver_config, config_file_name, SU2_COMPONENT::SU2_DEF, iZone, nZone, true);
         }
-
+        
         config_container[iZone]->SetMPICommunicator(SU2_MPI::GetComm());
     }
-
+    
     /*--- Set the multizone part of the problem. ---*/
-
+    
     if (driver_config->GetMultizone_Problem()){
         for (iZone = 0; iZone < nZone; iZone++) {
-
+            
             /*--- Set the interface markers for multizone ---*/
-
+            
             config_container[iZone]->SetMultizone(driver_config, config_container);
         }
     }
 }
 
 void CDeformationDriver::Geometrical_Preprocessing() {
-
+    
     for (iZone = 0; iZone < nZone; iZone++) {
-
-      /*--- Definition of the geometry class to store the primal grid in the partitioning process. ---*/
-
-      CGeometry *geometry_aux = nullptr;
-
-      /*--- All ranks process the grid and call ParMETIS for partitioning ---*/
-
-      geometry_aux = new CPhysicalGeometry(config_container[iZone], iZone, nZone);
-
-      /*--- Color the initial grid and set the send-receive domains (ParMETIS) ---*/
-
-      geometry_aux->SetColorGrid_Parallel(config_container[iZone]);
-
-      /*--- Build the grid data structures using the ParMETIS coloring. ---*/
-
-      geometry_container[iZone] = new CPhysicalGeometry(geometry_aux, config_container[iZone]);
-
-      /*--- Deallocate the memory of geometry_aux ---*/
-
-      delete geometry_aux;
-
-      /*--- Add the Send/Receive boundaries ---*/
-
-      geometry_container[iZone]->SetSendReceive(config_container[iZone]);
-
-      /*--- Add the Send/Receive boundaries ---*/
-
-      geometry_container[iZone]->SetBoundaries(config_container[iZone]);
-
-      /*--- Computational grid preprocesing ---*/
-
-      if (rank == MASTER_NODE) cout << endl << "----------------------- Preprocessing computations ----------------------" << endl;
-
-      /*--- Compute elements surrounding points, points surrounding points ---*/
-
-      if (rank == MASTER_NODE) cout << "Setting local point connectivity." <<endl;
-      geometry_container[iZone]->SetPoint_Connectivity();
-
-      /*--- Check the orientation before computing geometrical quantities ---*/
-
-      geometry_container[iZone]->SetBoundVolume();
-      if (config_container[iZone]->GetReorientElements()) {
-      if (rank == MASTER_NODE) cout << "Checking the numerical grid orientation of the interior elements." <<endl;
-          geometry_container[iZone]->Check_IntElem_Orientation(config_container[iZone]);
-          geometry_container[iZone]->Check_BoundElem_Orientation(config_container[iZone]);
-      }
-
-      /*--- Create the edge structure ---*/
-
-      if (rank == MASTER_NODE) cout << "Identify edges and vertices." <<endl;
-      geometry_container[iZone]->SetEdges();
-      geometry_container[iZone]->SetVertex(config_container[iZone]);
-
-      if (config_container[iZone]->GetDesign_Variable(0) != NO_DEFORMATION) {
-
-          /*--- Create the dual control volume structures ---*/
-
-          if (rank == MASTER_NODE) cout << "Setting the bound control volume structure." << endl;
-          geometry_container[iZone]->SetControlVolume(config_container[iZone], ALLOCATE);
-          geometry_container[iZone]->SetBoundControlVolume(config_container[iZone], ALLOCATE);
-      }
-
-      /*--- Create the point-to-point MPI communication structures. ---*/
-
-      geometry_container[iZone]->PreprocessP2PComms(geometry_container[iZone], config_container[iZone]);
-
+        
+        /*--- Definition of the geometry class to store the primal grid in the partitioning process. ---*/
+        
+        CGeometry *geometry_aux = nullptr;
+        
+        /*--- All ranks process the grid and call ParMETIS for partitioning ---*/
+        
+        geometry_aux = new CPhysicalGeometry(config_container[iZone], iZone, nZone);
+        
+        /*--- Color the initial grid and set the send-receive domains (ParMETIS) ---*/
+        
+        geometry_aux->SetColorGrid_Parallel(config_container[iZone]);
+        
+        /*--- Build the grid data structures using the ParMETIS coloring. ---*/
+        
+        geometry_container[iZone][INST_0][MESH_0] = new CPhysicalGeometry(geometry_aux, config_container[iZone]);
+        
+        /*--- Deallocate the memory of geometry_aux ---*/
+        
+        delete geometry_aux;
+        
+        /*--- Add the Send/Receive boundaries ---*/
+        
+        geometry_container[iZone][INST_0][MESH_0]->SetSendReceive(config_container[iZone]);
+        
+        /*--- Add the Send/Receive boundaries ---*/
+        
+        geometry_container[iZone][INST_0][MESH_0]->SetBoundaries(config_container[iZone]);
+        
+        /*--- Computational grid preprocesing ---*/
+        
+        if (rank == MASTER_NODE) cout << endl << "----------------------- Preprocessing computations ----------------------" << endl;
+        
+        /*--- Compute elements surrounding points, points surrounding points ---*/
+        
+        if (rank == MASTER_NODE) cout << "Setting local point connectivity." <<endl;
+        geometry_container[iZone][INST_0][MESH_0]->SetPoint_Connectivity();
+        
+        /*--- Check the orientation before computing geometrical quantities ---*/
+        
+        geometry_container[iZone][INST_0][MESH_0]->SetBoundVolume();
+        if (config_container[iZone]->GetReorientElements()) {
+            if (rank == MASTER_NODE) cout << "Checking the numerical grid orientation of the interior elements." <<endl;
+            geometry_container[iZone][INST_0][MESH_0]->Check_IntElem_Orientation(config_container[iZone]);
+            geometry_container[iZone][INST_0][MESH_0]->Check_BoundElem_Orientation(config_container[iZone]);
+        }
+        
+        /*--- Create the edge structure ---*/
+        
+        if (rank == MASTER_NODE) cout << "Identify edges and vertices." <<endl;
+        geometry_container[iZone][INST_0][MESH_0]->SetEdges();
+        geometry_container[iZone][INST_0][MESH_0]->SetVertex(config_container[iZone]);
+        
+        if (config_container[iZone]->GetDesign_Variable(0) != NO_DEFORMATION) {
+            
+            /*--- Create the dual control volume structures ---*/
+            
+            if (rank == MASTER_NODE) cout << "Setting the bound control volume structure." << endl;
+            geometry_container[iZone][INST_0][MESH_0]->SetControlVolume(config_container[iZone], ALLOCATE);
+            geometry_container[iZone][INST_0][MESH_0]->SetBoundControlVolume(config_container[iZone], ALLOCATE);
+        }
+        
+        /*--- Create the point-to-point MPI communication structures. ---*/
+        
+        geometry_container[iZone][INST_0][MESH_0]->PreprocessP2PComms(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
+        
     }
 }
 
 void CDeformationDriver::Output_Preprocessing() {
-
-      for (iZone = 0; iZone < nZone; iZone++) {
-
+    
+    for (iZone = 0; iZone < nZone; iZone++) {
+        
         /*--- Allocate the mesh output ---*/
-
-        output_container[iZone] = new CMeshOutput(config_container[iZone], geometry_container[iZone]->GetnDim());
-
+        
+        output_container[iZone] = new CMeshOutput(config_container[iZone], geometry_container[iZone][INST_0][MESH_0]->GetnDim());
+        
         /*--- Preprocess the volume output ---*/
-
+        
         output_container[iZone]->PreprocessVolumeOutput(config_container[iZone]);
-
+        
         /*--- Preprocess history --- */
-
+        
         output_container[iZone]->PreprocessHistoryOutput(config_container[iZone], false);
-
+        
     }
 }
 
 void CDeformationDriver::Solver_Preprocessing() {
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    solver_container[iZone] = new CMeshSolver(geometry_container[iZone], config_container[iZone]);
-  }
-
+    
+    for (iZone = 0; iZone < nZone; iZone++) {
+        solver_container[iZone][INST_0][MESH_0][MESH_SOL] = new CMeshSolver(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
+    }
+    
 }
 
 void CDeformationDriver::Numerics_Preprocessing() {
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    numerics_container[iZone] = new CNumerics* [omp_get_num_threads() * MAX_TERMS]();
-
-    for (int thread = 0; thread < omp_get_max_threads(); ++thread) {
-        const int iTerm = FEA_TERM + thread * MAX_TERMS;
-        const int nDim = geometry_container[iZone]->GetnDim();
-
-        numerics_container[iZone][iTerm] = new CFEAMeshElasticity(nDim, nDim, geometry_container[iZone]->GetnElem(), config_container[iZone]);
+    
+    for (iZone = 0; iZone < nZone; iZone++) {
+        numerics_container[iZone] = new CNumerics* [omp_get_num_threads() * MAX_TERMS]();
+        
+        for (int thread = 0; thread < omp_get_max_threads(); ++thread) {
+            const int iTerm = FEA_TERM + thread * MAX_TERMS;
+            const int nDim = geometry_container[iZone][INST_0][MESH_0]->GetnDim();
+            
+            numerics_container[iZone][iTerm] = new CFEAMeshElasticity(nDim, nDim, geometry_container[iZone][INST_0][MESH_0]->GetnElem(), config_container[iZone]);
+        }
+        
     }
-
-  }
-
+    
 }
 
 void CDeformationDriver::Run() {
-
+    
     /* --- Start measuring computation time ---*/
-
+    
     StartTime = SU2_MPI::Wtime();
-
+    
     /*--- Surface grid deformation using design variables ---*/
-
+    
     if (driver_config->GetDeform_Mesh()) {
         Update();
     }
     else {
         Update_Legacy();
     }
-
+    
     /*--- Synchronization point after a single solver iteration. Compute the
-      wall clock time required. ---*/
-
+     wall clock time required. ---*/
+    
     StopTime = SU2_MPI::Wtime();
-
+    
     UsedTimeCompute = StopTime-StartTime;
     if (rank == MASTER_NODE) {
-      cout << "\nCompleted in " << fixed << UsedTimeCompute << " seconds on "<< size;
-
-      if (size == 1) cout << " core." << endl; else cout << " cores." << endl;
+        cout << "\nCompleted in " << fixed << UsedTimeCompute << " seconds on "<< size;
+        
+        if (size == 1) cout << " core." << endl; else cout << " cores." << endl;
     }
-
+    
     /*--- Output the deformed mesh ---*/
     Output();
-
+    
 }
 
 void CDeformationDriver::Update() {
-
+    
     for (iZone = 0; iZone < nZone; iZone++){
-
-    /*--- Set the stiffness of each element mesh into the mesh numerics ---*/
-
-    solver_container[iZone]->SetMesh_Stiffness(numerics_container[iZone], config_container[iZone]);
-
-    /*--- Deform the volume grid around the new boundary locations ---*/
-
-    solver_container[iZone]->DeformMesh(geometry_container[iZone], numerics_container[iZone], config_container[iZone]);
-
+        
+        /*--- Set the stiffness of each element mesh into the mesh numerics ---*/
+        
+        solver_container[iZone][INST_0][MESH_0][MESH_SOL]->SetMesh_Stiffness(numerics_container[iZone], config_container[iZone]);
+        
+        /*--- Deform the volume grid around the new boundary locations ---*/
+        
+        solver_container[iZone][INST_0][MESH_0][MESH_SOL]->DeformMesh(geometry_container[iZone][INST_0][MESH_0], numerics_container[iZone], config_container[iZone]);
+        
     }
 }
 
 void CDeformationDriver::Update_Legacy() {
-
+    
     for (iZone = 0; iZone < nZone; iZone++){
-
-      if (config_container[iZone]->GetDesign_Variable(0) != NO_DEFORMATION) {
-
-        /*--- Definition of the Class for grid movement ---*/
-        grid_movement[iZone] = new CVolumetricMovement(geometry_container[iZone], config_container[iZone]);
-
-        /*--- Save original coordinates to be reused in convexity checking procedure ---*/
-        auto OriginalCoordinates = geometry_container[iZone]->nodes->GetCoord();
-
-        /*--- First check for volumetric grid deformation/transformations ---*/
-
-        if (config_container[iZone]->GetDesign_Variable(0) == SCALE_GRID) {
-
-          if (rank == MASTER_NODE)
-            cout << endl << "--------------------- Volumetric grid scaling (ZONE " << iZone <<") ------------------" << endl;
-          grid_movement[iZone]->SetVolume_Scaling(geometry_container[iZone], config_container[iZone], false);
-
-        } else if (config_container[iZone]->GetDesign_Variable(0) == TRANSLATE_GRID) {
-
-          if (rank == MASTER_NODE)
-            cout << endl << "------------------- Volumetric grid translation (ZONE " << iZone <<") ----------------" << endl;
-          grid_movement[iZone]->SetVolume_Translation(geometry_container[iZone], config_container[iZone], false);
-
-        } else if (config_container[iZone]->GetDesign_Variable(0) == ROTATE_GRID) {
-
-          if (rank == MASTER_NODE)
-            cout << endl << "--------------------- Volumetric grid rotation (ZONE " << iZone <<") -----------------" << endl;
-          grid_movement[iZone]->SetVolume_Rotation(geometry_container[iZone], config_container[iZone], false);
-
-        } else {
-
-          /*--- If no volume-type deformations are requested, then this is a
-           surface-based deformation or FFD set up. ---*/
-
-          if (rank == MASTER_NODE)
-            cout << endl << "--------------------- Surface grid deformation (ZONE " << iZone <<") -----------------" << endl;
-
-          /*--- Definition and initialization of the surface deformation class ---*/
-
-          surface_movement[iZone] = new CSurfaceMovement();
-
-          /*--- Copy coordinates to the surface structure ---*/
-
-          surface_movement[iZone]->CopyBoundary(geometry_container[iZone], config_container[iZone]);
-
-          /*--- Surface grid deformation ---*/
-
-          if (rank == MASTER_NODE) cout << "Performing the deformation of the surface grid." << endl;
-          auto TotalDeformation = surface_movement[iZone]->SetSurface_Deformation(geometry_container[iZone], config_container[iZone]);
-
-          if (config_container[iZone]->GetDesign_Variable(0) != FFD_SETTING) {
-
-            if (rank == MASTER_NODE)
-              cout << endl << "------------------- Volumetric grid deformation (ZONE " << iZone <<") ----------------" << endl;
-
-            if (rank == MASTER_NODE)
-              cout << "Performing the deformation of the volumetric grid." << endl;
-            grid_movement[iZone]->SetVolume_Deformation(geometry_container[iZone], config_container[iZone], false);
-
-            /*--- Get parameters for convexity check ---*/
-            bool ConvexityCheck;
-            unsigned short ConvexityCheck_MaxIter, ConvexityCheck_MaxDepth;
-
-            tie(ConvexityCheck, ConvexityCheck_MaxIter, ConvexityCheck_MaxDepth) = config_container[iZone]->GetConvexityCheck();
-
-            /*--- Recursively change deformations if there are nonconvex elements. ---*/
-
-            if (ConvexityCheck && geometry_container[iZone]->GetnNonconvexElements() > 0) {
-              if (rank == MASTER_NODE) {
-                cout << "Nonconvex elements present after deformation. " << endl;
-                cout << "Recursively lowering deformation magnitude." << endl;
-              }
-
-              /*--- Load initial deformation values ---*/
-              auto InitialDeformation = TotalDeformation;
-
-              unsigned short ConvexityCheckIter, RecursionDepth = 0;
-              su2double DeformationFactor = 1.0, DeformationDifference = 1.0;
-              for (ConvexityCheckIter = 1; ConvexityCheckIter <= ConvexityCheck_MaxIter; ConvexityCheckIter++) {
-
-                /*--- Recursively change deformation magnitude:
-                decrease if there are nonconvex elements, increase otherwise ---*/
-                DeformationDifference /= 2.0;
-
-                if (geometry_container[iZone]->GetnNonconvexElements() > 0) {
-                  DeformationFactor -= DeformationDifference;
-                } else {
-                  RecursionDepth += 1;
-
-                  if (RecursionDepth == ConvexityCheck_MaxDepth) {
-                    if (rank == MASTER_NODE) {
-                      cout << "Maximum recursion depth reached." << endl;
-                      cout << "Remaining amount of original deformation: ";
-                      cout << DeformationFactor*100.0 << " percent. " << endl;
-                    }
-                    break;
-                  }
-
-                  DeformationFactor += DeformationDifference;
-                }
-
-                /*--- Load mesh to start every iteration with an undeformed grid ---*/
-                for (auto iPoint = 0ul; iPoint < OriginalCoordinates.rows(); iPoint++) {
-                  for (auto iDim = 0ul; iDim < OriginalCoordinates.cols(); iDim++) {
-                    geometry_container[iZone]->nodes->SetCoord(iPoint, iDim, OriginalCoordinates(iPoint,iDim));
-                  }
-                }
-
-                /*--- Set deformation magnitude as percentage of initial deformation ---*/
-                for (auto iDV = 0u; iDV < driver_config->GetnDV(); iDV++) {
-                  for (auto iDV_Value = 0u; iDV_Value < driver_config->GetnDV_Value(iDV); iDV_Value++) {
-                    config_container[iZone]->SetDV_Value(iDV, iDV_Value, InitialDeformation[iDV][iDV_Value]*DeformationFactor);
-                  }
-                }
-
-                /*--- Surface grid deformation ---*/
-                if (rank == MASTER_NODE) cout << "Performing the deformation of the surface grid." << endl;
-
-                TotalDeformation = surface_movement[iZone]->SetSurface_Deformation(geometry_container[iZone], config_container[iZone]);
-
+        
+        if (config_container[iZone]->GetDesign_Variable(0) != NO_DEFORMATION) {
+            
+            /*--- Definition of the Class for grid movement ---*/
+            grid_movement[iZone][INST_0] = new CVolumetricMovement(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
+            
+            /*--- Save original coordinates to be reused in convexity checking procedure ---*/
+            auto OriginalCoordinates = geometry_container[iZone][INST_0][MESH_0]->nodes->GetCoord();
+            
+            /*--- First check for volumetric grid deformation/transformations ---*/
+            
+            if (config_container[iZone]->GetDesign_Variable(0) == SCALE_GRID) {
+                
                 if (rank == MASTER_NODE)
-                  cout << endl << "------------------- Volumetric grid deformation (ZONE " << iZone <<") ----------------" << endl;
-
+                    cout << endl << "--------------------- Volumetric grid scaling (ZONE " << iZone <<") ------------------" << endl;
+                grid_movement[iZone][INST_0]->SetVolume_Scaling(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], false);
+                
+            } else if (config_container[iZone]->GetDesign_Variable(0) == TRANSLATE_GRID) {
+                
                 if (rank == MASTER_NODE)
-                  cout << "Performing the deformation of the volumetric grid." << endl;
-                grid_movement[iZone]->SetVolume_Deformation(geometry_container[iZone], config_container[iZone], false);
-
-                if (rank == MASTER_NODE) {
-                  cout << "Number of nonconvex elements for iteration " << ConvexityCheckIter << ": ";
-                  cout << geometry_container[iZone]->GetnNonconvexElements() << endl;
-                  cout << "Remaining amount of original deformation: ";
-                  cout << DeformationFactor*100.0 << " percent. " << endl;
+                    cout << endl << "------------------- Volumetric grid translation (ZONE " << iZone <<") ----------------" << endl;
+                grid_movement[iZone][INST_0]->SetVolume_Translation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], false);
+                
+            } else if (config_container[iZone]->GetDesign_Variable(0) == ROTATE_GRID) {
+                
+                if (rank == MASTER_NODE)
+                    cout << endl << "--------------------- Volumetric grid rotation (ZONE " << iZone <<") -----------------" << endl;
+                grid_movement[iZone][INST_0]->SetVolume_Rotation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], false);
+                
+            } else {
+                
+                /*--- If no volume-type deformations are requested, then this is a
+                 surface-based deformation or FFD set up. ---*/
+                
+                if (rank == MASTER_NODE)
+                    cout << endl << "--------------------- Surface grid deformation (ZONE " << iZone <<") -----------------" << endl;
+                
+                /*--- Definition and initialization of the surface deformation class ---*/
+                
+                surface_movement[iZone] = new CSurfaceMovement();
+                
+                /*--- Copy coordinates to the surface structure ---*/
+                
+                surface_movement[iZone]->CopyBoundary(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
+                
+                /*--- Surface grid deformation ---*/
+                
+                if (rank == MASTER_NODE) cout << "Performing the deformation of the surface grid." << endl;
+                auto TotalDeformation = surface_movement[iZone]->SetSurface_Deformation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
+                
+                if (config_container[iZone]->GetDesign_Variable(0) != FFD_SETTING) {
+                    
+                    if (rank == MASTER_NODE)
+                        cout << endl << "------------------- Volumetric grid deformation (ZONE " << iZone <<") ----------------" << endl;
+                    
+                    if (rank == MASTER_NODE)
+                        cout << "Performing the deformation of the volumetric grid." << endl;
+                    grid_movement[iZone][INST_0]->SetVolume_Deformation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], false);
+                    
+                    /*--- Get parameters for convexity check ---*/
+                    bool ConvexityCheck;
+                    unsigned short ConvexityCheck_MaxIter, ConvexityCheck_MaxDepth;
+                    
+                    tie(ConvexityCheck, ConvexityCheck_MaxIter, ConvexityCheck_MaxDepth) = config_container[iZone]->GetConvexityCheck();
+                    
+                    /*--- Recursively change deformations if there are nonconvex elements. ---*/
+                    
+                    if (ConvexityCheck && geometry_container[iZone][INST_0][MESH_0]->GetnNonconvexElements() > 0) {
+                        if (rank == MASTER_NODE) {
+                            cout << "Nonconvex elements present after deformation. " << endl;
+                            cout << "Recursively lowering deformation magnitude." << endl;
+                        }
+                        
+                        /*--- Load initial deformation values ---*/
+                        auto InitialDeformation = TotalDeformation;
+                        
+                        unsigned short ConvexityCheckIter, RecursionDepth = 0;
+                        su2double DeformationFactor = 1.0, DeformationDifference = 1.0;
+                        for (ConvexityCheckIter = 1; ConvexityCheckIter <= ConvexityCheck_MaxIter; ConvexityCheckIter++) {
+                            
+                            /*--- Recursively change deformation magnitude:
+                             decrease if there are nonconvex elements, increase otherwise ---*/
+                            DeformationDifference /= 2.0;
+                            
+                            if (geometry_container[iZone][INST_0][MESH_0]->GetnNonconvexElements() > 0) {
+                                DeformationFactor -= DeformationDifference;
+                            } else {
+                                RecursionDepth += 1;
+                                
+                                if (RecursionDepth == ConvexityCheck_MaxDepth) {
+                                    if (rank == MASTER_NODE) {
+                                        cout << "Maximum recursion depth reached." << endl;
+                                        cout << "Remaining amount of original deformation: ";
+                                        cout << DeformationFactor*100.0 << " percent. " << endl;
+                                    }
+                                    break;
+                                }
+                                
+                                DeformationFactor += DeformationDifference;
+                            }
+                            
+                            /*--- Load mesh to start every iteration with an undeformed grid ---*/
+                            for (auto iPoint = 0ul; iPoint < OriginalCoordinates.rows(); iPoint++) {
+                                for (auto iDim = 0ul; iDim < OriginalCoordinates.cols(); iDim++) {
+                                    geometry_container[iZone][INST_0][MESH_0]->nodes->SetCoord(iPoint, iDim, OriginalCoordinates(iPoint,iDim));
+                                }
+                            }
+                            
+                            /*--- Set deformation magnitude as percentage of initial deformation ---*/
+                            for (auto iDV = 0u; iDV < driver_config->GetnDV(); iDV++) {
+                                for (auto iDV_Value = 0u; iDV_Value < driver_config->GetnDV_Value(iDV); iDV_Value++) {
+                                    config_container[iZone]->SetDV_Value(iDV, iDV_Value, InitialDeformation[iDV][iDV_Value]*DeformationFactor);
+                                }
+                            }
+                            
+                            /*--- Surface grid deformation ---*/
+                            if (rank == MASTER_NODE) cout << "Performing the deformation of the surface grid." << endl;
+                            
+                            TotalDeformation = surface_movement[iZone]->SetSurface_Deformation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
+                            
+                            if (rank == MASTER_NODE)
+                                cout << endl << "------------------- Volumetric grid deformation (ZONE " << iZone <<") ----------------" << endl;
+                            
+                            if (rank == MASTER_NODE)
+                                cout << "Performing the deformation of the volumetric grid." << endl;
+                            grid_movement[iZone][INST_0]->SetVolume_Deformation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], false);
+                            
+                            if (rank == MASTER_NODE) {
+                                cout << "Number of nonconvex elements for iteration " << ConvexityCheckIter << ": ";
+                                cout << geometry_container[iZone][INST_0][MESH_0]->GetnNonconvexElements() << endl;
+                                cout << "Remaining amount of original deformation: ";
+                                cout << DeformationFactor*100.0 << " percent. " << endl;
+                            }
+                            
+                        }
+                        
+                    }
+                    
                 }
-
-              }
-
+                
             }
-
-          }
-
+            
         }
-
-      }
-
+        
     }
-
+    
 }
 
 void CDeformationDriver::Output() {
-
+    
     /*--- Output deformed grid for visualization, if requested (surface and volumetric), in parallel
-          requires to move all the data to the master node---*/
-
+     requires to move all the data to the master node---*/
+    
     if (rank == MASTER_NODE) cout << endl << "----------------------- Write deformed grid files -----------------------" << endl;
-
+    
     for (iZone = 0; iZone < nZone; iZone++){
-
-      /*--- Compute Mesh Quality if requested. Necessary geometry preprocessing re-done beforehand. ---*/
-
-      if (config_container[iZone]->GetWrt_MeshQuality() && !driver_config->GetStructuralProblem()) {
-
-        if (rank == MASTER_NODE) cout << "Recompute geometry properties necessary to evaluate mesh quality statistics.\n";
-
-        geometry_container[iZone]->SetPoint_Connectivity();
-        geometry_container[iZone]->SetBoundVolume();
-        geometry_container[iZone]->SetEdges();
-        geometry_container[iZone]->SetVertex(config_container[iZone]);
-        geometry_container[iZone]->SetControlVolume(config_container[iZone], ALLOCATE);
-        geometry_container[iZone]->SetBoundControlVolume(config_container[iZone], ALLOCATE);
-
-        if (rank == MASTER_NODE) cout << "Computing mesh quality statistics for the dual control volumes.\n";
-        geometry_container[iZone]->ComputeMeshQualityStatistics(config_container[iZone]);
-      }// Mesh Quality Output
-
-      /*--- Load the data --- */
-
-      output_container[iZone]->Load_Data(geometry_container[iZone], config_container[iZone], nullptr);
-
-      output_container[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone], OUTPUT_TYPE::MESH, driver_config->GetMesh_Out_FileName());
-
-      /*--- Set the file names for the visualization files ---*/
-
-      output_container[iZone]->SetVolume_Filename("volume_deformed");
-      output_container[iZone]->SetSurface_Filename("surface_deformed");
-
-      for (unsigned short iFile = 0; iFile < config_container[iZone]->GetnVolumeOutputFiles(); iFile++){
-        auto FileFormat = config_container[iZone]->GetVolumeOutputFiles();
-        if (FileFormat[iFile] != OUTPUT_TYPE::RESTART_ASCII && 
-            FileFormat[iFile] != OUTPUT_TYPE::RESTART_BINARY &&
-            FileFormat[iFile] != OUTPUT_TYPE::CSV)
-          output_container[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone], FileFormat[iFile]);
-      }
+        
+        /*--- Compute Mesh Quality if requested. Necessary geometry preprocessing re-done beforehand. ---*/
+        
+        if (config_container[iZone]->GetWrt_MeshQuality() && !driver_config->GetStructuralProblem()) {
+            
+            if (rank == MASTER_NODE) cout << "Recompute geometry properties necessary to evaluate mesh quality statistics.\n";
+            
+            geometry_container[iZone][INST_0][MESH_0]->SetPoint_Connectivity();
+            geometry_container[iZone][INST_0][MESH_0]->SetBoundVolume();
+            geometry_container[iZone][INST_0][MESH_0]->SetEdges();
+            geometry_container[iZone][INST_0][MESH_0]->SetVertex(config_container[iZone]);
+            geometry_container[iZone][INST_0][MESH_0]->SetControlVolume(config_container[iZone], ALLOCATE);
+            geometry_container[iZone][INST_0][MESH_0]->SetBoundControlVolume(config_container[iZone], ALLOCATE);
+            
+            if (rank == MASTER_NODE) cout << "Computing mesh quality statistics for the dual control volumes.\n";
+            geometry_container[iZone][INST_0][MESH_0]->ComputeMeshQualityStatistics(config_container[iZone]);
+        }// Mesh Quality Output
+        
+        /*--- Load the data --- */
+        
+        output_container[iZone]->Load_Data(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], nullptr);
+        
+        output_container[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone][INST_0][MESH_0], OUTPUT_TYPE::MESH, driver_config->GetMesh_Out_FileName());
+        
+        /*--- Set the file names for the visualization files ---*/
+        
+        output_container[iZone]->SetVolume_Filename("volume_deformed");
+        output_container[iZone]->SetSurface_Filename("surface_deformed");
+        
+        for (unsigned short iFile = 0; iFile < config_container[iZone]->GetnVolumeOutputFiles(); iFile++){
+            auto FileFormat = config_container[iZone]->GetVolumeOutputFiles();
+            if (FileFormat[iFile] != OUTPUT_TYPE::RESTART_ASCII &&
+                FileFormat[iFile] != OUTPUT_TYPE::RESTART_BINARY &&
+                FileFormat[iFile] != OUTPUT_TYPE::CSV)
+                output_container[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone][INST_0][MESH_0], FileFormat[iFile]);
+        }
     }
-
+    
     if (!driver_config->GetDeform_Mesh()) {
-      if ((config_container[ZONE_0]->GetDesign_Variable(0) != NO_DEFORMATION) &&
-          (config_container[ZONE_0]->GetDesign_Variable(0) != SCALE_GRID)     &&
-          (config_container[ZONE_0]->GetDesign_Variable(0) != TRANSLATE_GRID) &&
-          (config_container[ZONE_0]->GetDesign_Variable(0) != ROTATE_GRID)) {
-
-          /*--- Write the the free-form deformation boxes after deformation. ---*/
-
-          if (rank == MASTER_NODE) cout << "Adding any FFD information to the SU2 file." << endl;
-
-          surface_movement[ZONE_0]->WriteFFDInfo(surface_movement, geometry_container, config_container);
-
+        if ((config_container[ZONE_0]->GetDesign_Variable(0) != NO_DEFORMATION) &&
+            (config_container[ZONE_0]->GetDesign_Variable(0) != SCALE_GRID)     &&
+            (config_container[ZONE_0]->GetDesign_Variable(0) != TRANSLATE_GRID) &&
+            (config_container[ZONE_0]->GetDesign_Variable(0) != ROTATE_GRID)) {
+            
+            /*--- Write the the free-form deformation boxes after deformation. ---*/
+            
+            if (rank == MASTER_NODE) cout << "Adding any FFD information to the SU2 file." << endl;
+            
+            surface_movement[ZONE_0]->WriteFFDInfo(surface_movement, geometry_container[INST_0][MESH_0], config_container);
+            
+        }
     }
-  }
 }
 
 void CDeformationDriver::Postprocessing() {
-
+    
     if (rank == MASTER_NODE)
-      cout << endl <<"------------------------- Solver Postprocessing -------------------------" << endl;
-
+        cout << endl <<"------------------------- Solver Postprocessing -------------------------" << endl;
+    
     delete driver_config;
     driver_config = nullptr;
-
+    
     for (iZone = 0; iZone < nZone; iZone++) {
-      if (numerics_container[iZone] != nullptr) {
-        for (unsigned int iTerm = 0; iTerm < MAX_TERMS*omp_get_max_threads(); iTerm++) {
-          delete numerics_container[iZone][iTerm];
+        if (numerics_container[iZone] != nullptr) {
+            for (unsigned int iTerm = 0; iTerm < MAX_TERMS*omp_get_max_threads(); iTerm++) {
+                delete numerics_container[iZone][iTerm];
+            }
+            delete [] numerics_container[iZone];
         }
-        delete [] numerics_container[iZone];
-      }
     }
     delete [] numerics_container;
     if (rank == MASTER_NODE) cout << "Deleted CNumerics container." << endl;
-
+    
     for (iZone = 0; iZone < nZone; iZone++) {
-      delete solver_container[iZone];
+        delete solver_container[iZone][INST_0][MESH_0][MESH_SOL];
     }
     delete [] solver_container;
     if (rank == MASTER_NODE) cout << "Deleted CSolver container." << endl;
-
+    
     if (geometry_container != nullptr) {
-      for (iZone = 0; iZone < nZone; iZone++) {
-        delete geometry_container[iZone];
-      }
-      delete [] geometry_container;
+        for (iZone = 0; iZone < nZone; iZone++) {
+            delete geometry_container[iZone][INST_0][MESH_0];
+        }
+        delete [] geometry_container;
     }
     if (rank == MASTER_NODE) cout << "Deleted CGeometry container." << endl;
-
+    
     if (surface_movement != nullptr) {
-      for (iZone = 0; iZone < nZone; iZone++) {
-        delete surface_movement[iZone];
-      }
-      delete [] surface_movement;
+        for (iZone = 0; iZone < nZone; iZone++) {
+            delete surface_movement[iZone];
+        }
+        delete [] surface_movement;
     }
     if (rank == MASTER_NODE) cout << "Deleted CSurfaceMovement class." << endl;
-
+    
     if (grid_movement != nullptr) {
-      for (iZone = 0; iZone < nZone; iZone++) {
-        delete grid_movement[iZone];
-      }
-      delete [] grid_movement;
+        for (iZone = 0; iZone < nZone; iZone++) {
+            delete grid_movement[iZone][INST_0];
+        }
+        delete [] grid_movement;
     }
     if (rank == MASTER_NODE) cout << "Deleted CVolumetricMovement class." << endl;
-
+    
     if (config_container != nullptr) {
-      for (iZone = 0; iZone < nZone; iZone++) {
-        delete config_container[iZone];
-      }
-      delete [] config_container;
+        for (iZone = 0; iZone < nZone; iZone++) {
+            delete config_container[iZone];
+        }
+        delete [] config_container;
     }
     if (rank == MASTER_NODE) cout << "Deleted CConfig container." << endl;
-
+    
     if (output_container != nullptr) {
-      for (iZone = 0; iZone < nZone; iZone++) {
-        delete output_container[iZone];
-      }
-      delete [] output_container;
+        for (iZone = 0; iZone < nZone; iZone++) {
+            delete output_container[iZone];
+        }
+        delete [] output_container;
     }
     if (rank == MASTER_NODE) cout << "Deleted COutput class." << endl;
-
+    
     /*--- Exit the solver cleanly ---*/
-
+    
     if (rank == MASTER_NODE)
-      cout << endl << "------------------------- Exit Success (SU2_DEF) ------------------------" << endl << endl;
-}
-
-vector<string> CDeformationDriver::GetAllDeformMeshMarkersTag() const {
-
-  vector<string> interfaceBoundariesTagList;
-  unsigned short iMarker, nBoundariesMarker;
-  string Marker_Tag;
-
-  nBoundariesMarker = config_container[ZONE_0]->GetnMarker_Deform_Mesh();
-  interfaceBoundariesTagList.resize(nBoundariesMarker);
-
-  for(iMarker=0; iMarker < nBoundariesMarker; iMarker++){
-    Marker_Tag = config_container[ZONE_0]->GetMarker_Deform_Mesh_TagBound(iMarker);
-    interfaceBoundariesTagList[iMarker] = Marker_Tag;
-  }
-
-  return interfaceBoundariesTagList;
-}
-
-map<string, int> CDeformationDriver::GetAllBoundaryMarkers() const {
-
-  map<string, int>  allBoundariesMap;
-  unsigned short iMarker, nBoundaryMarkers;
-  string Marker_Tag;
-
-  nBoundaryMarkers = config_container[ZONE_0]->GetnMarker_All();
-
-  for(iMarker=0; iMarker < nBoundaryMarkers; iMarker++){
-    Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
-    allBoundariesMap[Marker_Tag] = iMarker;
-  }
-
-  return allBoundariesMap;
-}
-
-map<string, string> CDeformationDriver::GetAllBoundaryMarkersType() const {
-
-  map<string, string> allBoundariesTypeMap;
-  unsigned short iMarker, KindBC;
-  string Marker_Tag, Marker_Type;
-
-  for(iMarker=0; iMarker < config_container[ZONE_0]->GetnMarker_All(); iMarker++){
-    Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
-    KindBC = config_container[ZONE_0]->GetMarker_All_KindBC(iMarker);
-    switch(KindBC){
-      case EULER_WALL:
-        Marker_Type = "EULER_WALL";
-        break;
-      case FAR_FIELD:
-        Marker_Type = "FARFIELD";
-        break;
-      case ISOTHERMAL:
-        Marker_Type = "ISOTHERMAL";
-        break;
-      case HEAT_FLUX:
-        Marker_Type = "HEATFLUX";
-        break;
-      case INLET_FLOW:
-        Marker_Type = "INLET_FLOW";
-        break;
-      case OUTLET_FLOW:
-        Marker_Type = "OUTLET_FLOW";
-        break;
-      case SYMMETRY_PLANE:
-        Marker_Type = "SYMMETRY";
-        break;
-      case SEND_RECEIVE:
-        Marker_Type = "SEND_RECEIVE";
-        break;
-      default:
-        Marker_Type = "UNKNOWN_TYPE";
-    }
-    allBoundariesTypeMap[Marker_Tag] = Marker_Type;
-  }
-
-  return allBoundariesTypeMap;
-}
-
-unsigned long CDeformationDriver::GetNumberVertices(unsigned short iMarker) const {
-
-  return geometry_container[ZONE_0]->nVertex[iMarker];
-
-}
-
-unsigned long CDeformationDriver::GetNumberHaloVertices(unsigned short iMarker) const {
-
-  unsigned long nHaloVertices, iVertex, iPoint;
-
-  nHaloVertices = 0;
-  for(iVertex = 0; iVertex < geometry_container[ZONE_0]->nVertex[iMarker]; iVertex++){
-    iPoint = geometry_container[ZONE_0]->vertex[iMarker][iVertex]->GetNode();
-    if(!(geometry_container[ZONE_0]->nodes->GetDomain(iPoint))) nHaloVertices += 1;
-  }
-
-  return nHaloVertices;
-
-}
-
-unsigned long CDeformationDriver::GetVertexGlobalIndex(unsigned short iMarker, unsigned long iVertex) const {
-
-  unsigned long iPoint, GlobalIndex;
-
-  iPoint = geometry_container[ZONE_0]->vertex[iMarker][iVertex]->GetNode();
-  GlobalIndex = geometry_container[ZONE_0]->nodes->GetGlobalIndex(iPoint);
-
-  return GlobalIndex;
-
-}
-
-bool CDeformationDriver::IsAHaloNode(unsigned short iMarker, unsigned long iVertex) const {
-
-  unsigned long iPoint;
-
-  iPoint = geometry_container[ZONE_0]->vertex[iMarker][iVertex]->GetNode();
-  if(geometry_container[ZONE_0]->nodes->GetDomain(iPoint)) return false;
-  else return true;
-
-}
-
-vector<passivedouble> CDeformationDriver::GetInitialMeshCoord(unsigned short iMarker, unsigned long iVertex) const {
-
-  vector<su2double> coord(3,0.0);
-  vector<passivedouble> coord_passive(3, 0.0);
-
-  auto iPoint = geometry_container[ZONE_0]->vertex[iMarker][iVertex]->GetNode();
-
-  for (auto iDim = 0 ; iDim < geometry_container[ZONE_0]->GetnDim(); iDim++){
-   coord[iDim] = solver_container[ZONE_0]->GetNodes()->GetMesh_Coord(iPoint,iDim);
-  }
-
-  coord_passive[0] = SU2_TYPE::GetValue(coord[0]);
-  coord_passive[1] = SU2_TYPE::GetValue(coord[1]);
-  coord_passive[2] = SU2_TYPE::GetValue(coord[2]);
-
-  return coord_passive;
+        cout << endl << "------------------------- Exit Success (SU2_DEF) ------------------------" << endl << endl;
 }
 
-vector<passivedouble> CDeformationDriver::GetVertexNormal(unsigned short iMarker, unsigned long iVertex, bool unitNormal) const {
-
-  int nDim = geometry_container[ZONE_0]->GetnDim();
-
-  su2double *Normal;
-  su2double Area;
-  vector<su2double> ret_Normal(3, 0.0);
-  vector<passivedouble> ret_Normal_passive(3, 0.0);
-
-  Normal = geometry_container[ZONE_0]->vertex[iMarker][iVertex]->GetNormal();
-
-  if (!unitNormal) {
-
-    ret_Normal_passive[0] = SU2_TYPE::GetValue(Normal[0]);
-    ret_Normal_passive[1] = SU2_TYPE::GetValue(Normal[1]);
-    if(nDim>2) ret_Normal_passive[2] = SU2_TYPE::GetValue(Normal[2]);
-
-    return ret_Normal_passive;
-  }
-
-  Area = GeometryToolbox::Norm(nDim, Normal);
-
-  ret_Normal[0] = Normal[0]/Area;
-  ret_Normal[1] = Normal[1]/Area;
-  if(nDim>2) ret_Normal[2] = Normal[2]/Area;
-
-  ret_Normal_passive[0] = SU2_TYPE::GetValue(ret_Normal[0]);
-  ret_Normal_passive[1] = SU2_TYPE::GetValue(ret_Normal[1]);
-  ret_Normal_passive[2] = SU2_TYPE::GetValue(ret_Normal[2]);
-
-  return ret_Normal_passive;
-}
-
-void CDeformationDriver::SetMeshDisplacement(unsigned short iMarker, unsigned long iVertex, passivedouble DispX, passivedouble DispY, passivedouble DispZ) {
-
-  unsigned long iPoint;
-  su2double MeshDispl[3] =  {0.0,0.0,0.0};
-
-  MeshDispl[0] = DispX;
-  MeshDispl[1] = DispY;
-  MeshDispl[2] = DispZ;
-
-  iPoint = geometry_container[ZONE_0]->vertex[iMarker][iVertex]->GetNode();
-
-  solver_container[ZONE_0]->GetNodes()->SetBound_Disp(iPoint, MeshDispl);
-
-}
-
-void CDeformationDriver::CommunicateMeshDisplacement(void) {
-
-  solver_container[ZONE_0]->InitiateComms(geometry_container[ZONE_0], config_container[ZONE_0], MESH_DISPLACEMENTS);
-  solver_container[ZONE_0]->CompleteComms(geometry_container[ZONE_0], config_container[ZONE_0], MESH_DISPLACEMENTS);
-
+void CDeformationDriver::CommunicateMeshDisplacements(void) {
+    
+    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->InitiateComms(geometry_container[ZONE_0][INST_0][MESH_0], config_container[ZONE_0], MESH_DISPLACEMENTS);
+    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->CompleteComms(geometry_container[ZONE_0][INST_0][MESH_0], config_container[ZONE_0], MESH_DISPLACEMENTS);
+    
 }
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index 195dbf59aa6..63555b249c2 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -1,8 +1,8 @@
 /*!
  * \file CDiscAdjDeformationDriver.cpp
  * \brief Main subroutines for driving the projection of sensitivities.
- * \author T. Economon, H. Kline, R. Sanchez
- * \version 7.1.1 "Blackbird"
+ * \author T. Economon, H. Kline, R. Sanchez, A. Gastaldi, H. Patel
+ * \version 7.3.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -31,76 +31,77 @@
 
 using namespace std;
 
-CDiscAdjDeformationDriver::CDiscAdjDeformationDriver(char* confFile, SU2_Comm MPICommunicator) {
-
+CDiscAdjDeformationDriver::CDiscAdjDeformationDriver(char* confFile, SU2_Comm MPICommunicator):
+    CDriverBase(confFile, 1, MPICommunicator) 
+{
     /*--- Initialize Medipack (must also be here so it is initialized from python) ---*/
-    #ifdef HAVE_MPI
-      #if defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)
-        SU2_MPI::Init_AMPI();
-      #endif
-    #endif
-
+#ifdef HAVE_MPI
+#if defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)
+    SU2_MPI::Init_AMPI();
+#endif
+#endif
+    
     SU2_MPI::SetComm(MPICommunicator);
-
+    
     rank = SU2_MPI::GetRank();
     size = SU2_MPI::GetSize();
-
+    
     /*--- Copy the config filename ---*/
     strcpy(config_file_name, confFile);
-
+    
     /*--- Read the name and format of the input mesh file to get from the mesh
-      file the number of zones and dimensions from the numerical grid (required
-      for variables allocation)  ---*/
-
+     file the number of zones and dimensions from the numerical grid (required
+     for variables allocation)  ---*/
+    
     driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DOT);
-
+    
     nZone = driver_config->GetnZone();
-
+    
     /*--- Initialize containers --- */
-
+    
     SetContainers_Null();
-
+    
     /*--- Preprocessing of the config files. ---*/
-
+    
     Input_Preprocessing();
-
+    
     /*--- Set up a timer for performance benchmarking ---*/
-
+    
     StartTime = SU2_MPI::Wtime();
-
+    
     /*--- Preprocessing of the geometry for all zones. ---*/
-
+    
     Geometrical_Preprocessing();
-
+    
     /*--- Preprocessing of the outputs for all zones. ---*/
-
+    
     Output_Preprocessing();
-
+    
     /*--- Preprocessing time is reported now, but not included in the next compute portion. ---*/
-
+    
     StopTime = SU2_MPI::Wtime();
-
+    
     /*--- Compute/print the total time for performance benchmarking. ---*/
-
+    
     UsedTime = StopTime-StartTime;
     UsedTimePreproc    = UsedTime;
     UsedTimeCompute    = 0.0;
-
+    
 }
 
 CDiscAdjDeformationDriver::~CDiscAdjDeformationDriver(void) {
-
+    
 }
 
 void CDiscAdjDeformationDriver::SetContainers_Null() {
-
+    
     /*--- Definition of the containers per zones ---*/
-
+    
     config_container    = new CConfig*[nZone] ();
     geometry_container  = new CGeometry**[nZone] ();
     surface_movement    = new CSurfaceMovement*[nZone] ();
     grid_movement       = new CVolumetricMovement*[nZone] ();
-
+    
     nInst               = new unsigned short[nZone];
     for (iZone = 0; iZone < nZone; iZone++) {
         nInst[iZone] = 1;
@@ -108,32 +109,34 @@ void CDiscAdjDeformationDriver::SetContainers_Null() {
 }
 
 void CDiscAdjDeformationDriver::Input_Preprocessing() {
-
-    // TODO Check that config is for Discrete Adjoint !
+    
+    if (!config_container[iZone]->GetDiscrete_Adjoint()) {
+         SU2_MPI::Error("The discrete adjoint solver was not specified in the configuration file.", CURRENT_FUNCTION);
+    }
 
     /*--- Initialize a char to store the zone filename ---*/
     char zone_file_name[MAX_STRING_SIZE];
-
+    
     /*--- Loop over all zones to initialize the various classes. In most
-      cases, nZone is equal to one. This represents the solution of a partial
-      differential equation on a single block, unstructured mesh. ---*/
-
+     cases, nZone is equal to one. This represents the solution of a partial
+     differential equation on a single block, unstructured mesh. ---*/
+    
     for (iZone = 0; iZone < nZone; iZone++) {
-
-         /*--- Definition of the configuration option class for all zones. In this
-          constructor, the input configuration file is parsed and all options are
-          read and stored. ---*/
-
+        
+        /*--- Definition of the configuration option class for all zones. In this
+         constructor, the input configuration file is parsed and all options are
+         read and stored. ---*/
+        
         if (driver_config->GetnConfigFiles() > 0){
             strcpy(zone_file_name, driver_config->GetConfigFilename(iZone).c_str());
             config_container[iZone] = new CConfig(driver_config, zone_file_name, SU2_COMPONENT::SU2_DOT, iZone, nZone, true);
         } else {
             config_container[iZone] = new CConfig(driver_config, config_file_name, SU2_COMPONENT::SU2_DOT, iZone, nZone, true);
         }
-
+        
         config_container[iZone]->SetMPICommunicator(SU2_MPI::GetComm());
     }
-
+    
     /*--- Set the multizone part of the problem. ---*/
     if (driver_config->GetMultizone_Problem()){
         for (iZone = 0; iZone < nZone; iZone++) {
@@ -144,216 +147,224 @@ void CDiscAdjDeformationDriver::Input_Preprocessing() {
 }
 
 void CDiscAdjDeformationDriver::Geometrical_Preprocessing() {
-
+    
     /*--- Loop over all zones to initialize the various classes. In most
      cases, nZone is equal to one. This represents the solution of a partial
      differential equation on a single block, unstructured mesh. ---*/
-
-     for (iZone = 0; iZone < nZone; iZone++) {
-
+    
+    for (iZone = 0; iZone < nZone; iZone++) {
+        
         /*--- Determine whether or not the FEM solver is used, which decides the
          type of geometry classes that are instantiated. ---*/
         const bool fem_solver = config_container[iZone]->GetFEMSolver();
-
+        
         /*--- Read the number of instances for each zone ---*/
-
+        
         nInst[iZone] = config_container[iZone]->GetnTimeInstances();
-
+        
         geometry_container[iZone] = new CGeometry*[nInst[iZone]];
-
+        
         for (iInst = 0; iInst < nInst[iZone]; iInst++){
-
+            
             /*--- Definition of the geometry class to store the primal grid in the partitioning process. ---*/
-
+            
             CGeometry *geometry_aux = nullptr;
-
+            
             /*--- All ranks process the grid and call ParMETIS for partitioning ---*/
-
+            
             geometry_aux = new CPhysicalGeometry(config_container[iZone], iZone, nZone);
-
+            
             /*--- Color the initial grid and set the send-receive domains (ParMETIS) ---*/
-
+            
             if ( fem_solver ) geometry_aux->SetColorFEMGrid_Parallel(config_container[iZone]);
             else              geometry_aux->SetColorGrid_Parallel(config_container[iZone]);
-
+            
             /*--- Build the grid data structures using the ParMETIS coloring. ---*/
-
+            
             if( fem_solver ) {
                 switch( config_container[iZone]->GetKind_FEM_Flow() ) {
-                case DG: {
-                    geometry_container[iZone][iInst] = new CMeshFEM_DG(geometry_aux, config_container[iZone]);
-                    break;
-                }
+                    case DG: {
+                        geometry_container[iZone][iInst] = new CMeshFEM_DG(geometry_aux, config_container[iZone]);
+                        break;
+                    }
                 }
             }
             else {
                 geometry_container[iZone][iInst] = new CPhysicalGeometry(geometry_aux, config_container[iZone]);
             }
-
+            
             /*--- Deallocate the memory of geometry_aux ---*/
-
+            
             delete geometry_aux;
-
+            
             /*--- Add the Send/Receive boundaries ---*/
-
+            
             geometry_container[iZone][iInst]->SetSendReceive(config_container[iZone]);
-
+            
             /*--- Add the Send/Receive boundaries ---*/
-
+            
             geometry_container[iZone][iInst]->SetBoundaries(config_container[iZone]);
-
+            
             /*--- Create the vertex structure (required for MPI) ---*/
-
+            
             if (rank == MASTER_NODE) cout << "Identify vertices." << endl;
             geometry_container[iZone][iInst]->SetVertex(config_container[iZone]);
-
+            
             /*--- Store the global to local mapping after preprocessing. ---*/
-
+            
             if (rank == MASTER_NODE) cout << "Storing a mapping from global to local point index." << endl;
             geometry_container[iZone][iInst]->SetGlobal_to_Local_Point();
-
+            
             /* Test for a fem solver, because some more work must be done. */
-
+            
             if (fem_solver) {
-
+                
                 /*--- Carry out a dynamic cast to CMeshFEM_DG, such that it is not needed to
                  define all virtual functions in the base class CGeometry. ---*/
                 CMeshFEM_DG *DGMesh = dynamic_cast<CMeshFEM_DG *>(geometry_container[iZone][iInst]);
-
+                
                 /*--- Determine the standard elements for the volume elements. ---*/
                 if (rank == MASTER_NODE) cout << "Creating standard volume elements." << endl;
                 DGMesh->CreateStandardVolumeElements(config_container[iZone]);
-
+                
                 /*--- Create the face information needed to compute the contour integral
                  for the elements in the Discontinuous Galerkin formulation. ---*/
                 if (rank == MASTER_NODE) cout << "Creating face information." << endl;
                 DGMesh->CreateFaces(config_container[iZone]);
             }
         }
-
+        
         if (rank == MASTER_NODE)
-        cout << "\n----------------------- Preprocessing computations ----------------------" << endl;
-
+            cout << "\n----------------------- Preprocessing computations ----------------------" << endl;
+        
         /*--- Compute elements surrounding points, points surrounding points ---*/
-
+        
         if (rank == MASTER_NODE) cout << "Setting local point connectivity." << endl;
         geometry_container[iZone][INST_0]->SetPoint_Connectivity();
-
+        
         /*--- Check the orientation before computing geometrical quantities ---*/
-
+        
         geometry_container[iZone][INST_0]->SetBoundVolume();
         if (config_container[iZone]->GetReorientElements()) {
             if (rank == MASTER_NODE) cout << "Checking the numerical grid orientation of the elements." << endl;
             geometry_container[iZone][INST_0]->Check_IntElem_Orientation(config_container[iZone]);
             geometry_container[iZone][INST_0]->Check_BoundElem_Orientation(config_container[iZone]);
         }
-
+        
         /*--- Create the edge structure ---*/
-
+        
         if (rank == MASTER_NODE) cout << "Identify edges and vertices." << endl;
         geometry_container[iZone][INST_0]->SetEdges(); geometry_container[iZone][INST_0]->SetVertex(config_container[iZone]);
-
+        
         /*--- Create the dual control volume structures ---*/
-
+        
         if (rank == MASTER_NODE) cout << "Setting the bound control volume structure." << endl;
         geometry_container[iZone][INST_0]->SetBoundControlVolume(config_container[ZONE_0], ALLOCATE);
-
+        
         /*--- Store the global to local mapping after preprocessing. ---*/
-
+        
         if (rank == MASTER_NODE) cout << "Storing a mapping from global to local point index." << endl;
         geometry_container[iZone][INST_0]->SetGlobal_to_Local_Point();
-
+        
         /*--- Create the point-to-point MPI communication structures. ---*/
-
+        
         geometry_container[iZone][INST_0]->PreprocessP2PComms(geometry_container[iZone][INST_0], config_container[iZone]);
-
+        
     }
 }
 
 void CDiscAdjDeformationDriver::Output_Preprocessing() {
-
+    
 }
 
 void CDiscAdjDeformationDriver::Run() {
-
+    
     for (iZone = 0; iZone < nZone; iZone++) {
-            if (rank == MASTER_NODE) cout << "Reading volume sensitivities at each node from file." << endl;
-            grid_movement[iZone] = new CVolumetricMovement(geometry_container[iZone][INST_0], config_container[iZone]);
-
-            /*--- Read in sensitivities from file. ---*/
-            if (config_container[ZONE_0]->GetSensitivity_Format() == UNORDERED_ASCII)
-                geometry_container[iZone][INST_0]->ReadUnorderedSensitivity(config_container[iZone]);
-            else
-                geometry_container[iZone][INST_0]->SetSensitivity(config_container[iZone]);
-
-            if (rank == MASTER_NODE) cout << "\n---------------------- Mesh sensitivity computation ---------------------" << endl;
+        if (rank == MASTER_NODE) cout << "Reading volume sensitivities at each node from file." << endl;
+        grid_movement[iZone] = new CVolumetricMovement(geometry_container[iZone][INST_0], config_container[iZone]);
+        
+        /*--- Read in sensitivities from file. ---*/
+        if (config_container[ZONE_0]->GetSensitivity_Format() == UNORDERED_ASCII)
+            geometry_container[iZone][INST_0]->ReadUnorderedSensitivity(config_container[iZone]);
+        else
+            geometry_container[iZone][INST_0]->SetSensitivity(config_container[iZone]);
+        
+        if (rank == MASTER_NODE) cout << "\n---------------------- Mesh sensitivity computation ---------------------" << endl;
+        if (config_container[iZone]->GetDiscrete_Adjoint() && config_container[iZone]->GetSmoothGradient() &&
+            config_container[iZone]->GetSobMode() == ENUM_SOBOLEV_MODUS::MESH_LEVEL) {
+            DerivativeTreatment_MeshSensitivity(geometry_container[iZone][INST_0], config_container[iZone], grid_movement[iZone]);
+        } else {
             grid_movement[iZone]->SetVolume_Deformation(geometry_container[iZone][INST_0], config_container[iZone], false, true);
+        }
     }
-
+    
     if (rank == MASTER_NODE) cout << "\n------------------------ Mesh sensitivity Output ------------------------" << endl;
     SetSensitivity_Files(geometry_container, config_container, nZone);
-
+    
     /*--- Initialize structure to store the gradient ---*/
     Gradient = new su2double*[config_container[ZONE_0]->GetnDV()];
-
+    
     for (auto iDV = 0u; iDV  < config_container[ZONE_0]->GetnDV(); iDV++) {
         /*--- Initialize to zero ---*/
         Gradient[iDV] = new su2double[config_container[ZONE_0]->GetnDV_Value(iDV)]();
     }
-
+    
     Gradient_file.precision(driver_config->OptionIsSet("OUTPUT_PRECISION") ? driver_config->GetOutput_Precision() : 6);
-
+    
     /*--- For multizone computations the gradient contributions are summed up and written into one file. ---*/
     for (iZone = 0; iZone < nZone; iZone++){
         if ((config_container[iZone]->GetDesign_Variable(0) != NONE) &&
             (config_container[iZone]->GetDesign_Variable(0) != SURFACE_FILE)) {
-
-        if (rank == MASTER_NODE)
-            cout << "\n---------- Start gradient evaluation using sensitivity information ----------" << endl;
-
-        /*--- Definition of the Class for surface deformation ---*/
-
-        surface_movement[iZone] = new CSurfaceMovement();
-
-        /*--- Copy coordinates to the surface structure ---*/
-
-        surface_movement[iZone]->CopyBoundary(geometry_container[iZone][INST_0], config_container[iZone]);
-
-        /*--- If AD mode is enabled we can use it to compute the projection,
-         *    otherwise we use finite differences. ---*/
-
-        if (config_container[iZone]->GetAD_Mode())
-            SetDiscAdjDeformation_AD(geometry_container[iZone][INST_0], config_container[iZone], surface_movement[iZone] , Gradient);
-        else
-            SetDiscAdjDeformation_FD(geometry_container[iZone][INST_0], config_container[iZone], surface_movement[iZone] , Gradient);
-
+            
+            if (rank == MASTER_NODE)
+                cout << "\n---------- Start gradient evaluation using sensitivity information ----------" << endl;
+            
+            /*--- Definition of the Class for surface deformation ---*/
+            
+            surface_movement[iZone] = new CSurfaceMovement();
+            
+            /*--- Copy coordinates to the surface structure ---*/
+            
+            surface_movement[iZone]->CopyBoundary(geometry_container[iZone][INST_0], config_container[iZone]);
+            
+            /*--- If AD mode is enabled we can use it to compute the projection,
+             *    otherwise we use finite differences. ---*/
+            
+            if (config_container[iZone]->GetAD_Mode())
+                if (config_container[iZone]->GetSmoothGradient()) {
+                    DerivativeTreatment_Gradient(geometry_container[iZone][INST_0], config_container[iZone], grid_movement[iZone], surface_movement[iZone] , Gradient);
+                } else {
+                    SetProjection_AD(geometry_container[iZone][INST_0], config_container[iZone], surface_movement[iZone] , Gradient);
+                }
+        } else {
+            SetProjection_FD(geometry_container[iZone][INST_0], config_container[iZone], surface_movement[iZone] , Gradient);
         }
     } // for iZone
-
+    
     /*--- Write the gradient to a file ---*/
-
+    
     if (rank == MASTER_NODE)
         Gradient_file.open(config_container[ZONE_0]->GetObjFunc_Grad_FileName().c_str(), ios::out);
-
+    
     /*--- Print gradients to screen and writes to file ---*/
-
+    
     OutputGradient(Gradient, config_container[ZONE_0], Gradient_file);
-
+    
 }
 
 void CDiscAdjDeformationDriver::Postprocessing() {
-
+    
     for (auto iDV = 0u; iDV  < config_container[ZONE_0]->GetnDV(); iDV++){
-          delete [] Gradient[iDV];
+        delete [] Gradient[iDV];
     }
     delete [] Gradient;
-
+    
     delete driver_config;
     driver_config = nullptr;
-
+    
     if (rank == MASTER_NODE)
         cout << "\n------------------------- Solver Postprocessing -------------------------" << endl;
-
+    
     if (geometry_container != nullptr) {
         for (iZone = 0; iZone < nZone; iZone++) {
             if (geometry_container[iZone] != nullptr) {
@@ -366,7 +377,7 @@ void CDiscAdjDeformationDriver::Postprocessing() {
         delete [] geometry_container;
     }
     if (rank == MASTER_NODE) cout << "Deleted CGeometry container." << endl;
-
+    
     if (surface_movement != nullptr) {
         for (iZone = 0; iZone < nZone; iZone++) {
             delete surface_movement[iZone];
@@ -374,7 +385,7 @@ void CDiscAdjDeformationDriver::Postprocessing() {
         delete [] surface_movement;
     }
     if (rank == MASTER_NODE) cout << "Deleted CSurfaceMovement class." << endl;
-
+    
     if (grid_movement != nullptr) {
         for (iZone = 0; iZone < nZone; iZone++) {
             delete grid_movement[iZone];
@@ -382,7 +393,7 @@ void CDiscAdjDeformationDriver::Postprocessing() {
         delete [] grid_movement;
     }
     if (rank == MASTER_NODE) cout << "Deleted CVolumetricMovement class." << endl;
-
+    
     if (config_container != nullptr) {
         for (iZone = 0; iZone < nZone; iZone++) {
             delete config_container[iZone];
@@ -390,540 +401,620 @@ void CDiscAdjDeformationDriver::Postprocessing() {
         delete [] config_container;
     }
     if (rank == MASTER_NODE) cout << "Deleted CConfig container." << endl;
-
+    
 }
 
-void CDiscAdjDeformationDriver::SetDiscAdjDeformation_FD(CGeometry *geometry, CConfig *config, CSurfaceMovement *surface_movement, su2double** Gradient){
-
-  unsigned short iDV, nDV, iFFDBox, nDV_Value, iMarker, iDim;
-  unsigned long iVertex, iPoint;
-  su2double delta_eps, my_Gradient, localGradient, *Normal, dS, *VarCoord, Sensitivity,
-  dalpha[3], deps[3], dalpha_deps;
-  bool *UpdatePoint, MoveSurface, Local_MoveSurface;
-  CFreeFormDefBox **FFDBox;
-
-  int rank = SU2_MPI::GetRank();
-
-  nDV = config->GetnDV();
-
-  /*--- Boolean controlling points to be updated ---*/
-
-  UpdatePoint = new bool[geometry->GetnPoint()];
-
-  /*--- Definition of the FFD deformation class ---*/
-
-  unsigned short nFFDBox = MAX_NUMBER_FFD;
-  FFDBox = new CFreeFormDefBox*[nFFDBox];
-  for (iFFDBox = 0; iFFDBox < MAX_NUMBER_FFD; iFFDBox++) FFDBox[iFFDBox] = nullptr;
-
-  for (iDV = 0; iDV  < nDV; iDV++){
-    nDV_Value = config->GetnDV_Value(iDV);
-    if (nDV_Value != 1){
-      SU2_MPI::Error("The DiscAdjDeformation using finite differences currently only supports a fixed direction of movement for FFD points.", CURRENT_FUNCTION);
+void CDiscAdjDeformationDriver::SetProjection_FD(CGeometry *geometry, CConfig *config, CSurfaceMovement *surface_movement, su2double** Gradient){
+    
+    unsigned short iDV, nDV, iFFDBox, nDV_Value, iMarker, iDim;
+    unsigned long iVertex, iPoint;
+    su2double delta_eps, my_Gradient, localGradient, *Normal, dS, *VarCoord, Sensitivity,
+    dalpha[3], deps[3], dalpha_deps;
+    bool *UpdatePoint, MoveSurface, Local_MoveSurface;
+    CFreeFormDefBox **FFDBox;
+    
+    int rank = SU2_MPI::GetRank();
+    
+    nDV = config->GetnDV();
+    
+    /*--- Boolean controlling points to be updated ---*/
+    
+    UpdatePoint = new bool[geometry->GetnPoint()];
+    
+    /*--- Definition of the FFD deformation class ---*/
+    
+    unsigned short nFFDBox = MAX_NUMBER_FFD;
+    FFDBox = new CFreeFormDefBox*[nFFDBox];
+    for (iFFDBox = 0; iFFDBox < MAX_NUMBER_FFD; iFFDBox++) FFDBox[iFFDBox] = nullptr;
+    
+    for (iDV = 0; iDV  < nDV; iDV++){
+        nDV_Value = config->GetnDV_Value(iDV);
+        if (nDV_Value != 1){
+            SU2_MPI::Error("The projection using finite differences currently only supports a fixed direction of movement for FFD points.", CURRENT_FUNCTION);
+        }
     }
-  }
-
-  /*--- Continuous adjoint gradient computation ---*/
-
-  if (rank == MASTER_NODE)
-    cout << "Evaluate functional gradient using Finite Differences." << endl;
-
-  for (iDV = 0; iDV < nDV; iDV++) {
-
-    MoveSurface = true;
-    Local_MoveSurface = true;
-
-    /*--- Free Form deformation based ---*/
-
-    if ((config->GetDesign_Variable(iDV) == FFD_CONTROL_POINT_2D) ||
-        (config->GetDesign_Variable(iDV) == FFD_CAMBER_2D) ||
-        (config->GetDesign_Variable(iDV) == FFD_THICKNESS_2D) ||
-        (config->GetDesign_Variable(iDV) == FFD_TWIST_2D) ||
-        (config->GetDesign_Variable(iDV) == FFD_CONTROL_POINT) ||
-        (config->GetDesign_Variable(iDV) == FFD_NACELLE) ||
-        (config->GetDesign_Variable(iDV) == FFD_GULL) ||
-        (config->GetDesign_Variable(iDV) == FFD_TWIST) ||
-        (config->GetDesign_Variable(iDV) == FFD_ROTATION) ||
-        (config->GetDesign_Variable(iDV) == FFD_CAMBER) ||
-        (config->GetDesign_Variable(iDV) == FFD_THICKNESS) ||
-        (config->GetDesign_Variable(iDV) == FFD_ANGLE_OF_ATTACK)) {
-
-      /*--- Read the FFD information in the first iteration ---*/
-
-      if (iDV == 0) {
-
-        if (rank == MASTER_NODE)
-          cout << "Read the FFD information from mesh file." << endl;
-
-        /*--- Read the FFD information from the grid file ---*/
-
-        surface_movement->ReadFFDInfo(geometry, config, FFDBox, config->GetMesh_FileName());
-
-        /*--- If the FFDBox was not defined in the input file ---*/
-        if (!surface_movement->GetFFDBoxDefinition()) {
-          SU2_MPI::Error("The input grid doesn't have the entire FFD information!", CURRENT_FUNCTION);
+    
+    /*--- Continuous adjoint gradient computation ---*/
+    
+    if (rank == MASTER_NODE)
+        cout << "Evaluate functional gradient using Finite Differences." << endl;
+    
+    for (iDV = 0; iDV < nDV; iDV++) {
+        
+        MoveSurface = true;
+        Local_MoveSurface = true;
+        
+        /*--- Free Form deformation based ---*/
+        
+        if ((config->GetDesign_Variable(iDV) == FFD_CONTROL_POINT_2D) ||
+            (config->GetDesign_Variable(iDV) == FFD_CAMBER_2D) ||
+            (config->GetDesign_Variable(iDV) == FFD_THICKNESS_2D) ||
+            (config->GetDesign_Variable(iDV) == FFD_TWIST_2D) ||
+            (config->GetDesign_Variable(iDV) == FFD_CONTROL_POINT) ||
+            (config->GetDesign_Variable(iDV) == FFD_NACELLE) ||
+            (config->GetDesign_Variable(iDV) == FFD_GULL) ||
+            (config->GetDesign_Variable(iDV) == FFD_TWIST) ||
+            (config->GetDesign_Variable(iDV) == FFD_ROTATION) ||
+            (config->GetDesign_Variable(iDV) == FFD_CAMBER) ||
+            (config->GetDesign_Variable(iDV) == FFD_THICKNESS) ||
+            (config->GetDesign_Variable(iDV) == FFD_ANGLE_OF_ATTACK)) {
+            
+            /*--- Read the FFD information in the first iteration ---*/
+            
+            if (iDV == 0) {
+                
+                if (rank == MASTER_NODE)
+                    cout << "Read the FFD information from mesh file." << endl;
+                
+                /*--- Read the FFD information from the grid file ---*/
+                
+                surface_movement->ReadFFDInfo(geometry, config, FFDBox, config->GetMesh_FileName());
+                
+                /*--- If the FFDBox was not defined in the input file ---*/
+                if (!surface_movement->GetFFDBoxDefinition()) {
+                    SU2_MPI::Error("The input grid doesn't have the entire FFD information!", CURRENT_FUNCTION);
+                }
+                
+                for (iFFDBox = 0; iFFDBox < surface_movement->GetnFFDBox(); iFFDBox++) {
+                    
+                    if (rank == MASTER_NODE) cout << "Checking FFD box dimension." << endl;
+                    surface_movement->CheckFFDDimension(geometry, config, FFDBox[iFFDBox], iFFDBox);
+                    
+                    if (rank == MASTER_NODE) cout << "Check the FFD box intersections with the solid surfaces." << endl;
+                    surface_movement->CheckFFDIntersections(geometry, config, FFDBox[iFFDBox], iFFDBox);
+                    
+                }
+                
+                if (rank == MASTER_NODE)
+                    cout <<"-------------------------------------------------------------------------" << endl;
+                
+            }
+            
+            if (rank == MASTER_NODE) {
+                cout << endl << "Design variable number "<< iDV <<"." << endl;
+                cout << "Performing 3D deformation of the surface." << endl;
+            }
+            
+            /*--- Apply the control point change ---*/
+            
+            MoveSurface = false;
+            
+            for (iFFDBox = 0; iFFDBox < surface_movement->GetnFFDBox(); iFFDBox++) {
+                
+                /*--- Reset FFD box ---*/
+                
+                switch (config->GetDesign_Variable(iDV) ) {
+                    case FFD_CONTROL_POINT_2D : Local_MoveSurface = surface_movement->SetFFDCPChange_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+                    case FFD_CAMBER_2D :        Local_MoveSurface = surface_movement->SetFFDCamber_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+                    case FFD_THICKNESS_2D :     Local_MoveSurface = surface_movement->SetFFDThickness_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+                    case FFD_TWIST_2D :         Local_MoveSurface = surface_movement->SetFFDTwist_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+                    case FFD_CONTROL_POINT :    Local_MoveSurface = surface_movement->SetFFDCPChange(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+                    case FFD_NACELLE :          Local_MoveSurface = surface_movement->SetFFDNacelle(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+                    case FFD_GULL :             Local_MoveSurface = surface_movement->SetFFDGull(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+                    case FFD_TWIST :            Local_MoveSurface = surface_movement->SetFFDTwist(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+                    case FFD_ROTATION :         Local_MoveSurface = surface_movement->SetFFDRotation(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+                    case FFD_CAMBER :           Local_MoveSurface = surface_movement->SetFFDCamber(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+                    case FFD_THICKNESS :        Local_MoveSurface = surface_movement->SetFFDThickness(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+                    case FFD_CONTROL_SURFACE :  Local_MoveSurface = surface_movement->SetFFDControl_Surface(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
+                    case FFD_ANGLE_OF_ATTACK :  Gradient[iDV][0] = config->GetAoA_Sens(); break;
+                }
+                
+                /*--- Recompute cartesian coordinates using the new control points position ---*/
+                
+                if (Local_MoveSurface) {
+                    MoveSurface = true;
+                    surface_movement->SetCartesianCoord(geometry, config, FFDBox[iFFDBox], iFFDBox, true);
+                }
+                
+            }
+            
         }
-
-        for (iFFDBox = 0; iFFDBox < surface_movement->GetnFFDBox(); iFFDBox++) {
-
-          if (rank == MASTER_NODE) cout << "Checking FFD box dimension." << endl;
-          surface_movement->CheckFFDDimension(geometry, config, FFDBox[iFFDBox], iFFDBox);
-
-          if (rank == MASTER_NODE) cout << "Check the FFD box intersections with the solid surfaces." << endl;
-          surface_movement->CheckFFDIntersections(geometry, config, FFDBox[iFFDBox], iFFDBox);
-
+        
+        /*--- Hicks Henne design variable ---*/
+        
+        else if (config->GetDesign_Variable(iDV) == HICKS_HENNE) {
+            surface_movement->SetHicksHenne(geometry, config, iDV, true);
         }
-
-        if (rank == MASTER_NODE)
-          cout <<"-------------------------------------------------------------------------" << endl;
-
-      }
-
-      if (rank == MASTER_NODE) {
-        cout << endl << "Design variable number "<< iDV <<"." << endl;
-        cout << "Performing 3D deformation of the surface." << endl;
-      }
-
-      /*--- Apply the control point change ---*/
-
-      MoveSurface = false;
-
-      for (iFFDBox = 0; iFFDBox < surface_movement->GetnFFDBox(); iFFDBox++) {
-
-        /*--- Reset FFD box ---*/
-
-        switch (config->GetDesign_Variable(iDV) ) {
-          case FFD_CONTROL_POINT_2D : Local_MoveSurface = surface_movement->SetFFDCPChange_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_CAMBER_2D :        Local_MoveSurface = surface_movement->SetFFDCamber_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_THICKNESS_2D :     Local_MoveSurface = surface_movement->SetFFDThickness_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_TWIST_2D :         Local_MoveSurface = surface_movement->SetFFDTwist_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_CONTROL_POINT :    Local_MoveSurface = surface_movement->SetFFDCPChange(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_NACELLE :          Local_MoveSurface = surface_movement->SetFFDNacelle(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_GULL :             Local_MoveSurface = surface_movement->SetFFDGull(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_TWIST :            Local_MoveSurface = surface_movement->SetFFDTwist(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_ROTATION :         Local_MoveSurface = surface_movement->SetFFDRotation(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_CAMBER :           Local_MoveSurface = surface_movement->SetFFDCamber(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_THICKNESS :        Local_MoveSurface = surface_movement->SetFFDThickness(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_CONTROL_SURFACE :  Local_MoveSurface = surface_movement->SetFFDControl_Surface(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_ANGLE_OF_ATTACK :  Gradient[iDV][0] = config->GetAoA_Sens(); break;
+        
+        /*--- Surface bump design variable ---*/
+        
+        else if (config->GetDesign_Variable(iDV) == SURFACE_BUMP) {
+            surface_movement->SetSurface_Bump(geometry, config, iDV, true);
         }
-
-        /*--- Recompute cartesian coordinates using the new control points position ---*/
-
-        if (Local_MoveSurface) {
-          MoveSurface = true;
-          surface_movement->SetCartesianCoord(geometry, config, FFDBox[iFFDBox], iFFDBox, true);
+        
+        /*--- Kulfan (CST) design variable ---*/
+        
+        else if (config->GetDesign_Variable(iDV) == CST) {
+            surface_movement->SetCST(geometry, config, iDV, true);
         }
-
-      }
-
-    }
-
-    /*--- Hicks Henne design variable ---*/
-
-    else if (config->GetDesign_Variable(iDV) == HICKS_HENNE) {
-      surface_movement->SetHicksHenne(geometry, config, iDV, true);
-    }
-
-    /*--- Surface bump design variable ---*/
-
-    else if (config->GetDesign_Variable(iDV) == SURFACE_BUMP) {
-      surface_movement->SetSurface_Bump(geometry, config, iDV, true);
-    }
-
-    /*--- Kulfan (CST) design variable ---*/
-
-    else if (config->GetDesign_Variable(iDV) == CST) {
-      surface_movement->SetCST(geometry, config, iDV, true);
-    }
-
-    /*--- Displacement design variable ---*/
-
-    else if (config->GetDesign_Variable(iDV) == TRANSLATION) {
-      surface_movement->SetTranslation(geometry, config, iDV, true);
-    }
-
-    /*--- Angle of Attack design variable ---*/
-
-    else if (config->GetDesign_Variable(iDV) == ANGLE_OF_ATTACK) {
-      Gradient[iDV][0] = config->GetAoA_Sens();
-    }
-
-    /*--- Scale design variable ---*/
-
-    else if (config->GetDesign_Variable(iDV) == SCALE) {
-      surface_movement->SetScale(geometry, config, iDV, true);
-    }
-
-    /*--- Rotation design variable ---*/
-
-    else if (config->GetDesign_Variable(iDV) == ROTATION) {
-      surface_movement->SetRotation(geometry, config, iDV, true);
-    }
-
-    /*--- NACA_4Digits design variable ---*/
-
-    else if (config->GetDesign_Variable(iDV) == NACA_4DIGITS) {
-      surface_movement->SetNACA_4Digits(geometry, config);
-    }
-
-    /*--- Parabolic design variable ---*/
-
-    else if (config->GetDesign_Variable(iDV) == PARABOLIC) {
-      surface_movement->SetParabolic(geometry, config);
-    }
-
-    /*--- Design variable not implement ---*/
-
-    else {
-      if (rank == MASTER_NODE)
-        cout << "Design Variable not implement yet" << endl;
-    }
-
-    /*--- Load the delta change in the design variable (finite difference step). ---*/
-
-    if ((config->GetDesign_Variable(iDV) != ANGLE_OF_ATTACK) &&
-        (config->GetDesign_Variable(iDV) != FFD_ANGLE_OF_ATTACK)) {
-
-      /*--- If the Angle of attack is not involved, reset the value of the gradient ---*/
-
-      my_Gradient = 0.0; Gradient[iDV][0] = 0.0;
-
-      if (MoveSurface) {
-
-        delta_eps = config->GetDV_Value(iDV);
-
-        for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++)
-          UpdatePoint[iPoint] = true;
-
-        for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-          if (config->GetMarker_All_DV(iMarker) == YES) {
-            for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
-
-              iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
-              if ((iPoint < geometry->GetnPointDomain()) && UpdatePoint[iPoint]) {
-
-                Normal = geometry->vertex[iMarker][iVertex]->GetNormal();
-                VarCoord = geometry->vertex[iMarker][iVertex]->GetVarCoord();
-                Sensitivity = geometry->vertex[iMarker][iVertex]->GetAuxVar();
-
-                dS = 0.0;
-                for (iDim = 0; iDim < geometry->GetnDim(); iDim++) {
-                  dS += Normal[iDim]*Normal[iDim];
-                  deps[iDim] = VarCoord[iDim] / delta_eps;
-                }
-                dS = sqrt(dS);
-
-                dalpha_deps = 0.0;
-                for (iDim = 0; iDim < geometry->GetnDim(); iDim++) {
-                  dalpha[iDim] = Normal[iDim] / dS;
-                  dalpha_deps -= dalpha[iDim]*deps[iDim];
+        
+        /*--- Displacement design variable ---*/
+        
+        else if (config->GetDesign_Variable(iDV) == TRANSLATION) {
+            surface_movement->SetTranslation(geometry, config, iDV, true);
+        }
+        
+        /*--- Angle of Attack design variable ---*/
+        
+        else if (config->GetDesign_Variable(iDV) == ANGLE_OF_ATTACK) {
+            Gradient[iDV][0] = config->GetAoA_Sens();
+        }
+        
+        /*--- Scale design variable ---*/
+        
+        else if (config->GetDesign_Variable(iDV) == SCALE) {
+            surface_movement->SetScale(geometry, config, iDV, true);
+        }
+        
+        /*--- Rotation design variable ---*/
+        
+        else if (config->GetDesign_Variable(iDV) == ROTATION) {
+            surface_movement->SetRotation(geometry, config, iDV, true);
+        }
+        
+        /*--- NACA_4Digits design variable ---*/
+        
+        else if (config->GetDesign_Variable(iDV) == NACA_4DIGITS) {
+            surface_movement->SetNACA_4Digits(geometry, config);
+        }
+        
+        /*--- Parabolic design variable ---*/
+        
+        else if (config->GetDesign_Variable(iDV) == PARABOLIC) {
+            surface_movement->SetParabolic(geometry, config);
+        }
+        
+        /*--- Design variable not implemented ---*/
+        
+        else {
+            if (rank == MASTER_NODE)
+                cout << "Design Variable not implemented yet" << endl;
+        }
+        
+        /*--- Load the delta change in the design variable (finite difference step). ---*/
+        
+        if ((config->GetDesign_Variable(iDV) != ANGLE_OF_ATTACK) &&
+            (config->GetDesign_Variable(iDV) != FFD_ANGLE_OF_ATTACK)) {
+            
+            /*--- If the Angle of attack is not involved, reset the value of the gradient ---*/
+            
+            my_Gradient = 0.0; Gradient[iDV][0] = 0.0;
+            
+            if (MoveSurface) {
+                
+                delta_eps = config->GetDV_Value(iDV);
+                
+                for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++)
+                    UpdatePoint[iPoint] = true;
+                
+                for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
+                    if (config->GetMarker_All_DV(iMarker) == YES) {
+                        for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
+                            
+                            iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+                            if ((iPoint < geometry->GetnPointDomain()) && UpdatePoint[iPoint]) {
+                                
+                                Normal = geometry->vertex[iMarker][iVertex]->GetNormal();
+                                VarCoord = geometry->vertex[iMarker][iVertex]->GetVarCoord();
+                                Sensitivity = geometry->vertex[iMarker][iVertex]->GetAuxVar();
+                                
+                                dS = 0.0;
+                                for (iDim = 0; iDim < geometry->GetnDim(); iDim++) {
+                                    dS += Normal[iDim]*Normal[iDim];
+                                    deps[iDim] = VarCoord[iDim] / delta_eps;
+                                }
+                                dS = sqrt(dS);
+                                
+                                dalpha_deps = 0.0;
+                                for (iDim = 0; iDim < geometry->GetnDim(); iDim++) {
+                                    dalpha[iDim] = Normal[iDim] / dS;
+                                    dalpha_deps -= dalpha[iDim]*deps[iDim];
+                                }
+                                
+                                my_Gradient += Sensitivity*dalpha_deps;
+                                UpdatePoint[iPoint] = false;
+                            }
+                        }
+                    }
                 }
-
-                my_Gradient += Sensitivity*dalpha_deps;
-                UpdatePoint[iPoint] = false;
-              }
             }
-          }
+            
+            SU2_MPI::Allreduce(&my_Gradient, &localGradient, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
+            Gradient[iDV][0] += localGradient;
         }
-      }
-
-      SU2_MPI::Allreduce(&my_Gradient, &localGradient, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-      Gradient[iDV][0] += localGradient;
     }
-  }
-
-  /*--- Delete memory for parameterization. ---*/
-
-  if (FFDBox != nullptr) {
-    for (iFFDBox = 0; iFFDBox < MAX_NUMBER_FFD; iFFDBox++) {
-      if (FFDBox[iFFDBox] != nullptr) {
-        delete FFDBox[iFFDBox];
-      }
+    
+    /*--- Delete memory for parameterization. ---*/
+    
+    if (FFDBox != nullptr) {
+        for (iFFDBox = 0; iFFDBox < MAX_NUMBER_FFD; iFFDBox++) {
+            if (FFDBox[iFFDBox] != nullptr) {
+                delete FFDBox[iFFDBox];
+            }
+        }
+        delete [] FFDBox;
     }
-    delete [] FFDBox;
-  }
-
-  delete [] UpdatePoint;
-
+    
+    delete [] UpdatePoint;
+    
 }
 
 
-void CDiscAdjDeformationDriver::SetDiscAdjDeformation_AD(CGeometry *geometry, CConfig *config, CSurfaceMovement *surface_movement, su2double** Gradient){
-
-  su2double DV_Value, *VarCoord, Sensitivity, my_Gradient, localGradient, *Normal, Area = 0.0;
-  unsigned short iDV_Value = 0, iMarker, nMarker, iDim, nDim, iDV, nDV, nDV_Value;
-  unsigned long iVertex, nVertex, iPoint;
-
-  int rank = SU2_MPI::GetRank();
-
-  nMarker = config->GetnMarker_All();
-  nDim    = geometry->GetnDim();
-  nDV     = config->GetnDV();
-
-  VarCoord = nullptr;
-
-  /*--- Discrete adjoint gradient computation ---*/
-
-  if (rank == MASTER_NODE)
-    cout  << endl << "Evaluate functional gradient using Algorithmic Differentiation (ZONE " << config->GetiZone() << ")." << endl;
-
-  /*--- Start recording of operations ---*/
-
-  AD::StartRecording();
-
-  /*--- Register design variables as input and set them to zero
-   * (since we want to have the derivative at alpha = 0, i.e. for the current design) ---*/
-
-  for (iDV = 0; iDV < nDV; iDV++){
-
-    for (iDV_Value = 0; iDV_Value < config->GetnDV_Value(iDV); iDV_Value++){
-
-      config->SetDV_Value(iDV, iDV_Value, 0.0);
-
-      AD::RegisterInput(config->GetDV_Value(iDV, iDV_Value));
+void CDiscAdjDeformationDriver::SetProjection_AD(CGeometry *geometry, CConfig *config, CSurfaceMovement *surface_movement, su2double** Gradient){
+    
+    su2double *VarCoord = nullptr, Sensitivity, my_Gradient, localGradient, *Normal, Area = 0.0;
+    unsigned short iDV_Value = 0, iMarker, nMarker, iDim, nDim, iDV, nDV;
+    unsigned long iVertex, nVertex, iPoint;
+    
+    const int rank = SU2_MPI::GetRank();
+    
+    nMarker = config->GetnMarker_All();
+    nDim    = geometry->GetnDim();
+    nDV     = config->GetnDV();
+    
+    /*--- Discrete adjoint gradient computation ---*/
+    
+    if (rank == MASTER_NODE)
+        cout  << endl << "Evaluate functional gradient using Algorithmic Differentiation (ZONE " << config->GetiZone() << ")." << endl;
+    
+    /*--- Start recording of operations ---*/
+    
+    AD::StartRecording();
+    
+    /*--- Register design variables as input and set them to zero
+     * (since we want to have the derivative at alpha = 0, i.e. for the current design) ---*/
+    
+    for (iDV = 0; iDV < nDV; iDV++){
+        
+        for (iDV_Value = 0; iDV_Value < config->GetnDV_Value(iDV); iDV_Value++){
+            
+            config->SetDV_Value(iDV, iDV_Value, 0.0);
+            
+            AD::RegisterInput(config->GetDV_Value(iDV, iDV_Value));
+        }
     }
-  }
-
-  /*--- Call the surface deformation routine ---*/
-
-  surface_movement->SetSurface_Deformation(geometry, config);
-
-  /*--- Stop the recording --- */
-
-  AD::StopRecording();
-
-  /*--- Create a structure to identify points that have been already visited.
-   * We need that to make sure to set the sensitivity of surface points only once
-   *  (Markers share points, so we would visit them more than once in the loop over the markers below) ---*/
-
-  bool* visited = new bool[geometry->GetnPoint()];
-  for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++){
-    visited[iPoint] = false;
-  }
-
-  /*--- Initialize the derivatives of the output of the surface deformation routine
-   * with the discrete adjoints from the CFD solution ---*/
-
-  for (iMarker = 0; iMarker < nMarker; iMarker++) {
-    if (config->GetMarker_All_DV(iMarker) == YES) {
-      nVertex = geometry->nVertex[iMarker];
-      for (iVertex = 0; iVertex <nVertex; iVertex++) {
-        iPoint      = geometry->vertex[iMarker][iVertex]->GetNode();
-        if (!visited[iPoint]){
-          VarCoord    = geometry->vertex[iMarker][iVertex]->GetVarCoord();
-          Normal      = geometry->vertex[iMarker][iVertex]->GetNormal();
-
-          Area = 0.0;
-          for (iDim = 0; iDim < nDim; iDim++){
-            Area += Normal[iDim]*Normal[iDim];
-          }
-          Area = sqrt(Area);
-
-          for (iDim = 0; iDim < nDim; iDim++){
-            if (config->GetDiscrete_Adjoint()){
-              Sensitivity = geometry->GetSensitivity(iPoint, iDim);
-            } else {
-              Sensitivity = -Normal[iDim]*geometry->vertex[iMarker][iVertex]->GetAuxVar()/Area;
+    
+    /*--- Call the surface deformation routine ---*/
+    
+    surface_movement->SetSurface_Deformation(geometry, config);
+    
+    /*--- Stop the recording --- */
+    
+    AD::StopRecording();
+    
+    /*--- Create a structure to identify points that have been already visited.
+     * We need that to make sure to set the sensitivity of surface points only once
+     *  (Markers share points, so we would visit them more than once in the loop over the markers below) ---*/
+    
+    vector<bool> visited(geometry->GetnPoint(), false);
+    
+    /*--- Initialize the derivatives of the output of the surface deformation routine
+     * with the discrete adjoints from the CFD solution ---*/
+    
+    for (iMarker = 0; iMarker < nMarker; iMarker++) {
+        if (config->GetMarker_All_DV(iMarker) == YES) {
+            nVertex = geometry->nVertex[iMarker];
+            for (iVertex = 0; iVertex <nVertex; iVertex++) {
+                iPoint      = geometry->vertex[iMarker][iVertex]->GetNode();
+                if (!visited[iPoint]){
+                    VarCoord    = geometry->vertex[iMarker][iVertex]->GetVarCoord();
+                    Normal      = geometry->vertex[iMarker][iVertex]->GetNormal();
+                    
+                    Area = 0.0;
+                    for (iDim = 0; iDim < nDim; iDim++){
+                        Area += Normal[iDim]*Normal[iDim];
+                    }
+                    Area = sqrt(Area);
+                    
+                    for (iDim = 0; iDim < nDim; iDim++){
+                        if (config->GetDiscrete_Adjoint()){
+                            Sensitivity = geometry->GetSensitivity(iPoint, iDim);
+                        } else {
+                            Sensitivity = -Normal[iDim]*geometry->vertex[iMarker][iVertex]->GetAuxVar()/Area;
+                        }
+                        SU2_TYPE::SetDerivative(VarCoord[iDim], SU2_TYPE::GetValue(Sensitivity));
+                    }
+                    visited[iPoint] = true;
+                }
             }
-            SU2_TYPE::SetDerivative(VarCoord[iDim], SU2_TYPE::GetValue(Sensitivity));
-          }
-          visited[iPoint] = true;
         }
-      }
     }
-  }
-
-  delete [] visited;
-
-  /*--- Compute derivatives and extract gradient ---*/
-
-  AD::ComputeAdjoint();
-
-  for (iDV = 0; iDV  < nDV; iDV++){
-    nDV_Value =  config->GetnDV_Value(iDV);
-
-    for (iDV_Value = 0; iDV_Value < nDV_Value; iDV_Value++){
-      DV_Value = config->GetDV_Value(iDV, iDV_Value);
-      my_Gradient = SU2_TYPE::GetDerivative(DV_Value);
-      SU2_MPI::Allreduce(&my_Gradient, &localGradient, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-
-      /*--- Angle of Attack design variable (this is different,
-       the value comes form the input file) ---*/
-
-      if ((config->GetDesign_Variable(iDV) == ANGLE_OF_ATTACK) ||
-          (config->GetDesign_Variable(iDV) == FFD_ANGLE_OF_ATTACK))  {
-        Gradient[iDV][iDV_Value] = config->GetAoA_Sens();
-      }
-
-      Gradient[iDV][iDV_Value] += localGradient;
+    
+    /*--- Compute derivatives and extract gradient ---*/
+    
+    AD::ComputeAdjoint();
+    
+    for (iDV = 0; iDV  < nDV; iDV++){
+        
+        for (iDV_Value = 0; iDV_Value < config->GetnDV_Value(iDV); iDV_Value++) {
+            
+            my_Gradient = SU2_TYPE::GetDerivative(config->GetDV_Value(iDV, iDV_Value));
+            
+            SU2_MPI::Allreduce(&my_Gradient, &localGradient, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
+            
+            /*--- Angle of Attack design variable (this is different,
+             the value comes form the input file) ---*/
+            
+            if ((config->GetDesign_Variable(iDV) == ANGLE_OF_ATTACK) ||
+                (config->GetDesign_Variable(iDV) == FFD_ANGLE_OF_ATTACK))  {
+                Gradient[iDV][iDV_Value] = config->GetAoA_Sens();
+            }
+            
+            Gradient[iDV][iDV_Value] += localGradient;
+        }
     }
-  }
-
-  AD::Reset();
-
+    
+    AD::Reset();
+    
 }
 
 void CDiscAdjDeformationDriver::OutputGradient(su2double** Gradient, CConfig* config, ofstream& Gradient_file){
-
-  unsigned short nDV, iDV, iDV_Value, nDV_Value;
-
-  int rank = SU2_MPI::GetRank();
-
-  nDV = config->GetnDV();
-
-  /*--- Loop through all design variables and their gradients ---*/
-
-  for (iDV = 0; iDV  < nDV; iDV++){
-    nDV_Value = config->GetnDV_Value(iDV);
-    if (rank == MASTER_NODE){
-
-      /*--- Print the kind of design variable on screen ---*/
-
-      cout << endl << "Design variable (";
-      for (std::map<string, ENUM_PARAM>::const_iterator it = Param_Map.begin(); it != Param_Map.end(); ++it ){
-        if (it->second == config->GetDesign_Variable(iDV)){
-          cout << it->first << ") number "<< iDV << "." << endl;
-        }
-      }
-
-      /*--- Print the kind of objective function to screen ---*/
-
-      for (std::map<string, ENUM_OBJECTIVE>::const_iterator it = Objective_Map.begin(); it != Objective_Map.end(); ++it ){
-        if (it->second == config->GetKind_ObjFunc()){
-          cout << it->first << " gradient : ";
-          if (iDV == 0) Gradient_file << it->first << " gradient " << endl;
+    
+    unsigned short nDV, iDV, iDV_Value, nDV_Value;
+    
+    int rank = SU2_MPI::GetRank();
+    
+    nDV = config->GetnDV();
+    
+    /*--- Loop through all design variables and their gradients ---*/
+    
+    for (iDV = 0; iDV  < nDV; iDV++){
+        nDV_Value = config->GetnDV_Value(iDV);
+        if (rank == MASTER_NODE){
+            
+            /*--- Print the kind of design variable on screen ---*/
+            
+            cout << endl << "Design variable (";
+            for (std::map<string, ENUM_PARAM>::const_iterator it = Param_Map.begin(); it != Param_Map.end(); ++it ){
+                if (it->second == config->GetDesign_Variable(iDV)){
+                    cout << it->first << ") number "<< iDV << "." << endl;
+                }
+            }
+            
+            /*--- Print the kind of objective function to screen ---*/
+            
+            for (std::map<string, ENUM_OBJECTIVE>::const_iterator it = Objective_Map.begin(); it != Objective_Map.end(); ++it ){
+                if (it->second == config->GetKind_ObjFunc()){
+                    cout << it->first << " gradient : ";
+                    if (iDV == 0) Gradient_file << it->first << " gradient " << endl;
+                }
+            }
+            
+            /*--- Print the gradient to file and screen ---*/
+            
+            for (iDV_Value = 0; iDV_Value < nDV_Value; iDV_Value++){
+                cout << Gradient[iDV][iDV_Value];
+                if (iDV_Value != nDV_Value-1 ){
+                    cout << ", ";
+                }
+                Gradient_file << Gradient[iDV][iDV_Value] << endl;
+            }
+            cout << endl;
+            cout <<"-------------------------------------------------------------------------" << endl;
         }
-      }
-
-      /*--- Print the gradient to file and screen ---*/
-
-      for (iDV_Value = 0; iDV_Value < nDV_Value; iDV_Value++){
-        cout << Gradient[iDV][iDV_Value];
-        if (iDV_Value != nDV_Value-1 ){
-          cout << ", ";
-        }
-        Gradient_file << Gradient[iDV][iDV_Value] << endl;
-      }
-      cout << endl;
-      cout <<"-------------------------------------------------------------------------" << endl;
     }
-  }
 }
 
 
 void CDiscAdjDeformationDriver::SetSensitivity_Files(CGeometry ***geometry, CConfig **config, unsigned short val_nZone) {
-
-  unsigned short iMarker,iDim, nDim, nMarker, nVar;
-  unsigned long iVertex, iPoint, nPoint, nVertex;
-  su2double *Normal, Prod, Sens = 0.0, SensDim, Area;
-
-  unsigned short iZone;
-
-  CSolver *solver  = nullptr;
-  COutput *output  = nullptr;
-
-  for (iZone = 0; iZone < val_nZone; iZone++) {
-
-    nPoint = geometry[iZone][INST_0]->GetnPoint();
-    nDim   = geometry[iZone][INST_0]->GetnDim();
-    nMarker = config[iZone]->GetnMarker_All();
-    nVar = nDim + 1;
-
-    /*--- We create a baseline solver to easily merge the sensitivity information ---*/
-
-    vector<string> fieldnames;
-    fieldnames.push_back("\"Point\"");
-    fieldnames.push_back("\"x\"");
-    fieldnames.push_back("\"y\"");
-    if (nDim == 3) {
-      fieldnames.push_back("\"z\"");
-    }
-    fieldnames.push_back("\"Sensitivity_x\"");
-    fieldnames.push_back("\"Sensitivity_y\"");
-    if (nDim == 3) {
-      fieldnames.push_back("\"Sensitivity_z\"");
-    }
-    fieldnames.push_back("\"Surface_Sensitivity\"");
-
-    solver = new CBaselineSolver(geometry[iZone][INST_0], config[iZone], nVar+nDim, fieldnames);
-
-    for (iPoint = 0; iPoint < nPoint; iPoint++) {
-      for (iDim = 0; iDim < nDim; iDim++) {
-        solver->GetNodes()->SetSolution(iPoint, iDim,      geometry[iZone][INST_0]->nodes->GetCoord(iPoint, iDim));
-        solver->GetNodes()->SetSolution(iPoint, iDim+nDim, geometry[iZone][INST_0]->GetSensitivity(iPoint, iDim));
-      }
-    }
-
-    /*--- Compute the sensitivity in normal direction ---*/
-
-    for (iMarker = 0; iMarker < nMarker; iMarker++) {
-
-      if(config[iZone]->GetSolid_Wall(iMarker) || (config[iZone]->GetMarker_All_DV(iMarker) == YES )) {
-
-        nVertex = geometry[iZone][INST_0]->GetnVertex(iMarker);
-
-        for (iVertex = 0; iVertex < nVertex; iVertex++) {
-          iPoint = geometry[iZone][INST_0]->vertex[iMarker][iVertex]->GetNode();
-          Normal = geometry[iZone][INST_0]->vertex[iMarker][iVertex]->GetNormal();
-          Prod = 0.0;
-          Area = 0.0;
-          for (iDim = 0; iDim < nDim; iDim++) {
-
-            /*--- Retrieve the gradient calculated with discrete adjoint method ---*/
-
-            SensDim = geometry[iZone][INST_0]->GetSensitivity(iPoint, iDim);
-
-            /*--- Calculate scalar product for DiscAdjDeformation onto the normal vector ---*/
-
-            Prod += Normal[iDim]*SensDim;
-
-            Area += Normal[iDim]*Normal[iDim];
-          }
-
-          Area = sqrt(Area);
-
-          /*--- DiscAdjDeformation of the gradient onto the normal vector of the surface ---*/
-
-          Sens = Prod/Area;
-
-          solver->GetNodes()->SetSolution(iPoint, 2*nDim, Sens);
-
+    
+    unsigned short iMarker,iDim, nDim, nMarker, nVar;
+    unsigned long iVertex, iPoint, nPoint, nVertex;
+    su2double *Normal, Prod, Sens = 0.0, SensDim, Area;
+    
+    unsigned short iZone;
+    
+    CSolver *solver  = nullptr;
+    COutput *output  = nullptr;
+    
+    for (iZone = 0; iZone < val_nZone; iZone++) {
+        
+        nPoint = geometry[iZone][INST_0]->GetnPoint();
+        nDim   = geometry[iZone][INST_0]->GetnDim();
+        nMarker = config[iZone]->GetnMarker_All();
+        nVar = nDim + 1;
+        
+        /*--- We create a baseline solver to easily merge the sensitivity information ---*/
+        
+        vector<string> fieldnames;
+        fieldnames.push_back("\"Point\"");
+        fieldnames.push_back("\"x\"");
+        fieldnames.push_back("\"y\"");
+        if (nDim == 3) {
+            fieldnames.push_back("\"z\"");
         }
-      }
-    }
-
-    output = new CBaselineOutput(config[iZone], nDim, solver);
-    output->PreprocessVolumeOutput(config[iZone]);
-    output->PreprocessHistoryOutput(config[iZone], false);
-
-    /*--- Load the data --- */
-
-    output->Load_Data(geometry[iZone][INST_0], config[iZone], &solver);
-
-    /*--- Set the surface filename ---*/
-
-    output->SetSurface_Filename(config[iZone]->GetSurfSens_FileName());
-
-    /*--- Set the volume filename ---*/
-
-    output->SetVolume_Filename(config[iZone]->GetVolSens_FileName());
-
-    /*--- Write to file ---*/
+        fieldnames.push_back("\"Sensitivity_x\"");
+        fieldnames.push_back("\"Sensitivity_y\"");
+        if (nDim == 3) {
+            fieldnames.push_back("\"Sensitivity_z\"");
+        }
+        fieldnames.push_back("\"Surface_Sensitivity\"");
+        
+        solver = new CBaselineSolver(geometry[iZone][INST_0], config[iZone], nVar+nDim, fieldnames);
+        
+        for (iPoint = 0; iPoint < nPoint; iPoint++) {
+            for (iDim = 0; iDim < nDim; iDim++) {
+                solver->GetNodes()->SetSolution(iPoint, iDim,      geometry[iZone][INST_0]->nodes->GetCoord(iPoint, iDim));
+                solver->GetNodes()->SetSolution(iPoint, iDim+nDim, geometry[iZone][INST_0]->GetSensitivity(iPoint, iDim));
+            }
+        }
+        
+        /*--- Compute the sensitivity in normal direction ---*/
+        
+        for (iMarker = 0; iMarker < nMarker; iMarker++) {
+            
+            if(config[iZone]->GetSolid_Wall(iMarker) || (config[iZone]->GetMarker_All_DV(iMarker) == YES )) {
+                
+                nVertex = geometry[iZone][INST_0]->GetnVertex(iMarker);
+                
+                for (iVertex = 0; iVertex < nVertex; iVertex++) {
+                    iPoint = geometry[iZone][INST_0]->vertex[iMarker][iVertex]->GetNode();
+                    Normal = geometry[iZone][INST_0]->vertex[iMarker][iVertex]->GetNormal();
+                    Prod = 0.0;
+                    Area = 0.0;
+                    for (iDim = 0; iDim < nDim; iDim++) {
+                        
+                        /*--- Retrieve the gradient calculated with discrete adjoint method ---*/
+                        
+                        SensDim = geometry[iZone][INST_0]->GetSensitivity(iPoint, iDim);
+                        
+                        /*--- Calculate scalar product for projection onto the normal vector ---*/
+                        
+                        Prod += Normal[iDim]*SensDim;
+                        
+                        Area += Normal[iDim]*Normal[iDim];
+                    }
+                    
+                    Area = sqrt(Area);
+                    
+                    /*--- Projection of the gradient onto the normal vector of the surface ---*/
+                    
+                    Sens = Prod/Area;
+                    
+                    solver->GetNodes()->SetSolution(iPoint, 2*nDim, Sens);
+                    
+                }
+            }
+        }
+        
+        output = new CBaselineOutput(config[iZone], nDim, solver);
+        output->PreprocessVolumeOutput(config[iZone]);
+        output->PreprocessHistoryOutput(config[iZone], false);
+        
+        /*--- Load the data --- */
+        
+        output->Load_Data(geometry[iZone][INST_0], config[iZone], &solver);
+        
+        /*--- Set the surface filename ---*/
+        
+        output->SetSurface_Filename(config[iZone]->GetSurfSens_FileName());
+        
+        /*--- Set the volume filename ---*/
+        
+        output->SetVolume_Filename(config[iZone]->GetVolSens_FileName());
+        
+        /*--- Write to file ---*/
+        
+        for (unsigned short iFile = 0; iFile < config[iZone]->GetnVolumeOutputFiles(); iFile++){
+            auto FileFormat = config[iZone]->GetVolumeOutputFiles();
+            if (FileFormat[iFile] != OUTPUT_TYPE::RESTART_ASCII &&
+                FileFormat[iFile] != OUTPUT_TYPE::RESTART_BINARY &&
+                FileFormat[iFile] != OUTPUT_TYPE::CSV)
+                output->WriteToFile(config[iZone], geometry[iZone][INST_0], FileFormat[iFile]);
+        }
+        
+        /*--- Free memory ---*/
+        
+        delete output;
+        delete solver;
+        
+    }
+    
+}
 
-    for (unsigned short iFile = 0; iFile < config[iZone]->GetnVolumeOutputFiles(); iFile++){
-      auto FileFormat = config[iZone]->GetVolumeOutputFiles();
-      if (FileFormat[iFile] != OUTPUT_TYPE::RESTART_ASCII &&
-          FileFormat[iFile] != OUTPUT_TYPE::RESTART_BINARY &&
-          FileFormat[iFile] != OUTPUT_TYPE::CSV)
-        output->WriteToFile(config[iZone], geometry[iZone][INST_0], FileFormat[iFile]);
+void CDiscAdjDeformationDriver::DerivativeTreatment_MeshSensitivity(CGeometry *geometry, CConfig *config, CVolumetricMovement *grid_movement) {
+    
+    int rank = SU2_MPI::GetRank();
+    
+    /*--- Warning if choosen smoothing mode is unsupported.
+     * This is the default option if the user has not specified a mode in the config file. ---*/
+    if (config->GetSobMode() == ENUM_SOBOLEV_MODUS::NONE) {
+        SU2_MPI::Error("Unsupported operation modus for the Sobolev Smoothing Solver.", CURRENT_FUNCTION);
+    }
+    
+    /*-- Construct the smoothing solver and numerics ---*/
+    std::unique_ptr<CSolver> solver(new CGradientSmoothingSolver(geometry, config));
+    unsigned dim = (config->GetSmoothOnSurface() ? geometry->GetnDim() - 1 : geometry->GetnDim());
+    std::unique_ptr<CNumerics> numerics(new CGradSmoothing(dim, config));
+    
+    if (rank == MASTER_NODE)  cout << "Sobolev Smoothing of derivatives is active." << endl;
+    
+    /*--- Apply the smoothing procedure on the mesh level. ---*/
+    if (config->GetSobMode() == ENUM_SOBOLEV_MODUS::MESH_LEVEL) {
+        if (rank == MASTER_NODE) cout << "  working on mesh level" << endl;
+        
+        /*--- Work with the surface derivatives. ---*/
+        if (config->GetSmoothOnSurface()) {
+            
+            /*--- Project to surface and then smooth on surface. ---*/
+            grid_movement->SetVolume_Deformation(geometry, config, false, true);
+            
+            /*--- Get the sensitivities from the geometry class to work with. ---*/
+            solver->ReadSensFromGeometry(geometry);
+            
+            /*--- Perform the smoothing procedure on all boundaries marked as DV marker. ---*/
+            solver->ApplyGradientSmoothingSurface(geometry, numerics.get(), config);
+            
+            /*--- After appling the solver write the results back ---*/
+            solver->WriteSensToGeometry(geometry);
+            
+        /*--- Work with the volume derivatives. ---*/
+        } else {
+            
+            /*--- Get the sensitivities from the geometry class to work with. ---*/
+            solver->ReadSensFromGeometry(geometry);
+            
+            solver->ApplyGradientSmoothingVolume(geometry, numerics.get(), config);
+            
+            /*--- After appling the solver write the results back ---*/
+            solver->WriteSensToGeometry(geometry);
+            
+            /*--- Projection is applied after smoothing. ---*/
+            grid_movement->SetVolume_Deformation(geometry, config, false, true);
+        }
+        
     }
+    
+}
 
-    /*--- Free memory ---*/
-
-    delete output;
-    delete solver;
-
-  }
-
+void CDiscAdjDeformationDriver::DerivativeTreatment_Gradient(CGeometry *geometry, CConfig *config, CVolumetricMovement* grid_movement, CSurfaceMovement *surface_movement, su2double** Gradient) {
+    
+    int rank = SU2_MPI::GetRank();
+    
+    /*--- Error if choosen smoothing mode is unsupported.
+     * This is the default option if the user has not specified a mode in the config file. ---*/
+    if (config->GetSobMode() == ENUM_SOBOLEV_MODUS::NONE) {
+        SU2_MPI::Error("Unsupported operation modus for the Sobolev Smoothing Solver.", CURRENT_FUNCTION);
+    }
+    
+    /*-- Construct the smoothing solver and numerics ---*/
+    std::unique_ptr<CSolver> solver(new CGradientSmoothingSolver(geometry, config));
+    unsigned dim = (config->GetSmoothOnSurface() ? geometry->GetnDim() - 1 : geometry->GetnDim());
+    std::unique_ptr<CNumerics> numerics(new CGradSmoothing(dim, config));
+    
+    if (rank == MASTER_NODE)  cout << "Sobolev Smoothing of derivatives is active." << endl;
+    
+    /*--- Get the sensitivities from the geometry class to work with. ---*/
+    solver->ReadSensFromGeometry(geometry);
+    
+    /*--- Apply the smoothing procedure on the DV level. ---*/
+    if (config->GetSobMode() == ENUM_SOBOLEV_MODUS::PARAM_LEVEL_COMPLETE) {
+        solver->ApplyGradientSmoothingDV(geometry, numerics.get(), surface_movement, grid_movement, config, Gradient);
+        
+    /*--- If smoothing already took place on the mesh level, or none is requested, just do standard projection. ---*/
+    } else if (config->GetSobMode() == ENUM_SOBOLEV_MODUS::ONLY_GRAD ||
+               config->GetSobMode() == ENUM_SOBOLEV_MODUS::MESH_LEVEL) {
+        solver->RecordTapeAndCalculateOriginalGradient(geometry, surface_movement, grid_movement, config, Gradient);
+    }
+    
 }
diff --git a/SU2_DOT/include/SU2_DOT.hpp b/SU2_DOT/include/SU2_DOT.hpp
index 857b1e18376..5fa74b3a533 100644
--- a/SU2_DOT/include/SU2_DOT.hpp
+++ b/SU2_DOT/include/SU2_DOT.hpp
@@ -26,7 +26,6 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #pragma once
 
 #define ENABLE_MAPS
@@ -41,72 +40,6 @@
 #include <iomanip>
 #include <cmath>
 
-#include "../../Common/include/geometry/CPhysicalGeometry.hpp"
-#include "../../Common/include/fem/fem_geometry_structure.hpp"
-#include "../../SU2_CFD/include/output/CBaselineOutput.hpp"
-#include "../../SU2_CFD/include/solvers/CBaselineSolver.hpp"
-
-#include "../../SU2_CFD/include/solvers/CGradientSmoothingSolver.hpp"
-#include "../../SU2_CFD/include/numerics/CGradSmoothing.hpp"
+#include "../../SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp"
 
 using namespace std;
-
-
-/*!
- * \brief Projection of the surface sensitivity using finite differences (FD).
- * \param[in] geometry - Geometrical definition of the problem.
- * \param[in] config - Definition of the particular problem.
- * \param[in] surface_movement - Surface movement class of the problem.
- * \param[in] Gradient_file - Output file to store the gradient data.
- */
-
-void SetProjection_FD(CGeometry *geometry, CConfig *config, CSurfaceMovement *surface_movement, su2double **Gradient);
-
-/*!
- * \brief Projection of the surface sensitivity using algorithmic differentiation (AD).
- * \param[in] geometry - Geometrical definition of the problem.
- * \param[in] config - Definition of the particular problem.
- * \param[in] surface_movement - Surface movement class of the problem.
- * \param[in] Gradient_file - Output file to store the gradient data.
- */
-
-void SetProjection_AD(CGeometry *geometry, CConfig *config, CSurfaceMovement *surface_movement, su2double **Gradient);
-
-/*!
- * \brief Prints the gradient information to a file.
- * \param[in] Gradient - The gradient data.
- * \param[in] config - Definition of the particular problem.
- * \param[in] Gradient_file - Output file to store the gradient data.
- */
-
-void OutputGradient(su2double** Gradient, CConfig* config, ofstream& Gradient_file);
-
-/*!
- * \brief Write the sensitivity (including mesh sensitivity) computed with the discrete adjoint method
- *  on the surface and in the volume to a file.
- * \param[in] geometry - Geometrical definition of the problem.
- * \param[in] config - Definition of the particular problem.
- * \param[in] val_nZone - Number of Zones.
- */
-
-void SetSensitivity_Files(CGeometry ***geometry, CConfig **config, unsigned short val_nZone);
-
-/*!
- * \brief Treatment of derivatives with the Sobolev smoothing solver.
- * \param[in] geometry - Geometrical definition of the problem.
- * \param[in] config - Definition of the particular problem.
- * \param[in] grid_movement - Volumetric movement class of the problem.
- */
-
-void DerivativeTreatment_MeshSensitivity(CGeometry *geometry, CConfig *config, CVolumetricMovement *grid_movement);
-
-/*!
- * \brief Treatment of derivatives with the Sobolev smoothing solver.
- * \param[in] geometry - Geometrical definition of the problem.
- * \param[in] config - Definition of the particular problem.
- * \param[in] grid_movement - Volumetric movement class of the problem.
- * \param[in] surface_movement - Surface movement class of the problem.
- * \param[in] Gradient - Output array to store the gradient data.
- */
-
-void DerivativeTreatment_Gradient(CGeometry *geometry, CConfig *config, CVolumetricMovement *grid_movement, CSurfaceMovement *surface_movement, su2double **Gradient);
diff --git a/SU2_DOT/src/SU2_DOT.cpp b/SU2_DOT/src/SU2_DOT.cpp
index 077923ea359..c4632a3eac1 100644
--- a/SU2_DOT/src/SU2_DOT.cpp
+++ b/SU2_DOT/src/SU2_DOT.cpp
@@ -27,1030 +27,50 @@
 
 
 #include "../include/SU2_DOT.hpp"
+
 using namespace std;
 
 int main(int argc, char *argv[]) {
-
-  unsigned short iZone, iInst;
-  su2double StartTime = 0.0, StopTime = 0.0, UsedTime = 0.0;
-
-  char config_file_name[MAX_STRING_SIZE];
-
-  /*--- OpenMP initialization ---*/
-
-  omp_initialize();
-
-  /*--- MPI initialization, and buffer setting ---*/
-
+    
+    char config_file_name[MAX_STRING_SIZE];
+    
+    /*--- Create a pointer to the main SU2_DEF Driver ---*/
+    
+    CDiscAdjDeformationDriver* driver = nullptr;
+    
+    /*--- MPI initialization ---*/
+    
 #if defined(HAVE_OMP) && defined(HAVE_MPI)
-  int provided;
-  SU2_MPI::Init_thread(&argc, &argv, MPI_THREAD_FUNNELED, &provided);
+    int provided;
+    SU2_MPI::Init_thread(&argc, &argv, MPI_THREAD_FUNNELED, &provided);
 #else
-  SU2_MPI::Init(&argc, &argv);
-#endif
-  SU2_MPI::Comm MPICommunicator = SU2_MPI::GetComm();
-
-  const int rank = SU2_MPI::GetRank();
-  const int size = SU2_MPI::GetSize();
-
-  /*--- AD initialization ---*/
-#ifdef HAVE_OPDI
-  AD::getGlobalTape().initialize();
-#endif
-
-  /*--- Pointer to different structures that will be used throughout the entire code ---*/
-
-  CConfig **config_container            = nullptr;
-  CConfig *driver_config                = nullptr;
-  CGeometry ***geometry_container       = nullptr;
-  CSurfaceMovement **surface_movement   = nullptr;
-  CVolumetricMovement **grid_movement   = nullptr;
-  unsigned short *nInst                 = nullptr;
-
-  /*--- Load in the number of zones and spatial dimensions in the mesh file (if no config
-   file is specified, default.cfg is used) ---*/
-
-  if (argc == 2) { strcpy(config_file_name,argv[1]); }
-  else { strcpy(config_file_name, "default.cfg"); }
-
-  /*--- Read the name and format of the input mesh file to get from the mesh
-   file the number of zones and dimensions from the numerical grid (required
-   for variables allocation)  ---*/
-
-  CConfig *config = nullptr;
-  config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DOT);
-
-  const auto nZone = config->GetnZone();
-
-  /*--- Definition of the containers per zones ---*/
-
-  config_container    = new CConfig*[nZone] ();
-  geometry_container  = new CGeometry**[nZone] ();
-  surface_movement    = new CSurfaceMovement*[nZone] ();
-  grid_movement       = new CVolumetricMovement*[nZone] ();
-
-  nInst               = new unsigned short[nZone];
-  driver_config       = nullptr;
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    nInst[iZone] = 1;
-  }
-
-  /*--- Initialize the configuration of the driver ---*/
-  driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DOT, false);
-
-  /*--- Initialize a char to store the zone filename ---*/
-  char zone_file_name[MAX_STRING_SIZE];
-
-  /*--- Loop over all zones to initialize the various classes. In most
-   cases, nZone is equal to one. This represents the solution of a partial
-   differential equation on a single block, unstructured mesh. ---*/
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-
-    /*--- Definition of the configuration option class for all zones. In this
-     constructor, the input configuration file is parsed and all options are
-     read and stored. ---*/
-
-    if (driver_config->GetnConfigFiles() > 0){
-      strcpy(zone_file_name, driver_config->GetConfigFilename(iZone).c_str());
-      config_container[iZone] = new CConfig(driver_config, zone_file_name, SU2_COMPONENT::SU2_DOT, iZone, nZone, true);
-    }
-    else{
-      config_container[iZone] = new CConfig(driver_config, config_file_name, SU2_COMPONENT::SU2_DOT, iZone, nZone, true);
-    }
-    config_container[iZone]->SetMPICommunicator(MPICommunicator);
-
-  }
-
-  /*--- Set the multizone part of the problem. ---*/
-  if (driver_config->GetMultizone_Problem()){
-    for (iZone = 0; iZone < nZone; iZone++) {
-      /*--- Set the interface markers for multizone ---*/
-      config_container[iZone]->SetMultizone(driver_config, config_container);
-    }
-  }
-
-  /*--- Loop over all zones to initialize the various classes. In most
-   cases, nZone is equal to one. This represents the solution of a partial
-   differential equation on a single block, unstructured mesh. ---*/
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-
-    /*--- Determine whether or not the FEM solver is used, which decides the
-     type of geometry classes that are instantiated. ---*/
-    const bool fem_solver = config_container[iZone]->GetFEMSolver();
-
-    /*--- Read the number of instances for each zone ---*/
-
-    nInst[iZone] = config_container[iZone]->GetnTimeInstances();
-
-    geometry_container[iZone] = new CGeometry*[nInst[iZone]];
-
-    for (iInst = 0; iInst < nInst[iZone]; iInst++){
-
-      /*--- Definition of the geometry class to store the primal grid in the partitioning process. ---*/
-
-      CGeometry *geometry_aux = nullptr;
-
-      /*--- All ranks process the grid and call ParMETIS for partitioning ---*/
-
-      geometry_aux = new CPhysicalGeometry(config_container[iZone], iZone, nZone);
-
-      /*--- Color the initial grid and set the send-receive domains (ParMETIS) ---*/
-
-      if ( fem_solver ) geometry_aux->SetColorFEMGrid_Parallel(config_container[iZone]);
-      else              geometry_aux->SetColorGrid_Parallel(config_container[iZone]);
-
-      /*--- Build the grid data structures using the ParMETIS coloring. ---*/
-
-      if( fem_solver ) {
-        switch( config_container[iZone]->GetKind_FEM_Flow() ) {
-          case DG: {
-            geometry_container[iZone][iInst] = new CMeshFEM_DG(geometry_aux, config_container[iZone]);
-            break;
-          }
-        }
-      }
-      else {
-        geometry_container[iZone][iInst] = new CPhysicalGeometry(geometry_aux, config_container[iZone]);
-      }
-
-      /*--- Deallocate the memory of geometry_aux ---*/
-
-      delete geometry_aux;
-
-      /*--- Add the Send/Receive boundaries ---*/
-
-      geometry_container[iZone][iInst]->SetSendReceive(config_container[iZone]);
-
-      /*--- Add the Send/Receive boundaries ---*/
-
-      geometry_container[iZone][iInst]->SetBoundaries(config_container[iZone]);
-
-      /*--- Create the vertex structure (required for MPI) ---*/
-
-      if (rank == MASTER_NODE) cout << "Identify vertices." << endl;
-      geometry_container[iZone][iInst]->SetVertex(config_container[iZone]);
-
-      /*--- Store the global to local mapping after preprocessing. ---*/
-
-      if (rank == MASTER_NODE) cout << "Storing a mapping from global to local point index." << endl;
-      geometry_container[iZone][iInst]->SetGlobal_to_Local_Point();
-
-      /* Test for a fem solver, because some more work must be done. */
-
-      if (fem_solver) {
-
-        /*--- Carry out a dynamic cast to CMeshFEM_DG, such that it is not needed to
-         define all virtual functions in the base class CGeometry. ---*/
-        CMeshFEM_DG *DGMesh = dynamic_cast<CMeshFEM_DG *>(geometry_container[iZone][iInst]);
-
-        /*--- Determine the standard elements for the volume elements. ---*/
-        if (rank == MASTER_NODE) cout << "Creating standard volume elements." << endl;
-        DGMesh->CreateStandardVolumeElements(config_container[iZone]);
-
-        /*--- Create the face information needed to compute the contour integral
-         for the elements in the Discontinuous Galerkin formulation. ---*/
-        if (rank == MASTER_NODE) cout << "Creating face information." << endl;
-        DGMesh->CreateFaces(config_container[iZone]);
-      }
-    }
-  }
-
-  /*--- Set up a timer for performance benchmarking (preprocessing time is included) ---*/
-
-  StartTime = SU2_MPI::Wtime();
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-
-    if (rank == MASTER_NODE)
-      cout << "\n----------------------- Preprocessing computations ----------------------" << endl;
-
-    /*--- Compute elements surrounding points, points surrounding points ---*/
-
-    if (rank == MASTER_NODE) cout << "Setting local point connectivity." << endl;
-      geometry_container[iZone][INST_0]->SetPoint_Connectivity();
-
-    /*--- Check the orientation before computing geometrical quantities ---*/
-
-    geometry_container[iZone][INST_0]->SetBoundVolume();
-    if (config_container[iZone]->GetReorientElements()) {
-      if (rank == MASTER_NODE) cout << "Checking the numerical grid orientation of the elements." << endl;
-      geometry_container[iZone][INST_0]->Check_IntElem_Orientation(config_container[iZone]);
-      geometry_container[iZone][INST_0]->Check_BoundElem_Orientation(config_container[iZone]);
-    }
-
-    /*--- Create the edge structure ---*/
-
-    if (rank == MASTER_NODE) cout << "Identify edges and vertices." << endl;
-      geometry_container[iZone][INST_0]->SetEdges(); geometry_container[iZone][INST_0]->SetVertex(config_container[iZone]);
-
-    /*--- Create the dual control volume structures ---*/
-
-    if (rank == MASTER_NODE) cout << "Setting the bound control volume structure." << endl;
-    geometry_container[iZone][INST_0]->SetBoundControlVolume(config_container[ZONE_0], ALLOCATE);
-
-    /*--- Store the global to local mapping after preprocessing. ---*/
-
-    if (rank == MASTER_NODE) cout << "Storing a mapping from global to local point index." << endl;
-    geometry_container[iZone][INST_0]->SetGlobal_to_Local_Point();
-
-    /*--- Create the point-to-point MPI communication structures. ---*/
-
-    geometry_container[iZone][INST_0]->PreprocessP2PComms(geometry_container[iZone][INST_0], config_container[iZone]);
-
-    /*--- Load the surface sensitivities from file. This is done only
-     once: if this is an unsteady problem, a time-average of the surface
-     sensitivities at each node is taken within this routine. ---*/
-
-    if (!config_container[iZone]->GetDiscrete_Adjoint()) {
-      if (rank == MASTER_NODE) cout << "Reading surface sensitivities at each node from file." << endl;
-      geometry_container[iZone][INST_0]->SetBoundSensitivity(config_container[iZone]);
-    }
-    else {
-      if (rank == MASTER_NODE) cout << "Reading volume sensitivities at each node from file." << endl;
-      grid_movement[iZone] = new CVolumetricMovement(geometry_container[iZone][INST_0], config_container[iZone]);
-
-      /*--- Read in sensitivities from file. ---*/
-      if (config_container[ZONE_0]->GetSensitivity_Format() == UNORDERED_ASCII)
-        geometry_container[iZone][INST_0]->ReadUnorderedSensitivity(config_container[iZone]);
-      else
-        geometry_container[iZone][INST_0]->SetSensitivity(config_container[iZone]);
-
-      if (rank == MASTER_NODE)
-        cout << "\n---------------------- Mesh sensitivity computation ---------------------" << endl;
-
-      if(config_container[iZone]->GetDiscrete_Adjoint() && config_container[iZone]->GetSmoothGradient() &&
-         config_container[iZone]->GetSobMode() == ENUM_SOBOLEV_MODUS::MESH_LEVEL) {
-        DerivativeTreatment_MeshSensitivity(geometry_container[iZone][INST_0], config_container[iZone], grid_movement[iZone]);
-      } else {
-        grid_movement[iZone]->SetVolume_Deformation(geometry_container[iZone][INST_0], config_container[iZone], false, true);
-      }
-
-    }
-  }
-
-
-  if (config_container[ZONE_0]->GetDiscrete_Adjoint()) {
-    if (rank == MASTER_NODE)
-      cout << "\n------------------------ Mesh sensitivity Output ------------------------" << endl;
-    SetSensitivity_Files(geometry_container, config_container, nZone);
-  }
-
-  /*--- Initialize structure to store the gradient ---*/
-  su2double** Gradient = new su2double*[config_container[ZONE_0]->GetnDV()];
-
-  for (auto iDV = 0u; iDV  < config_container[ZONE_0]->GetnDV(); iDV++) {
-    /*--- Initialize to zero ---*/
-    Gradient[iDV] = new su2double[config_container[ZONE_0]->GetnDV_Value(iDV)]();
-  }
-
-  ofstream Gradient_file;
-  Gradient_file.precision(config->OptionIsSet("OUTPUT_PRECISION") ? config->GetOutput_Precision() : 6);
-
-  /*--- For multizone computations the gradient contributions are summed up and written into one file. ---*/
-  for (iZone = 0; iZone < nZone; iZone++){
-    if ((config_container[iZone]->GetDesign_Variable(0) != NONE) &&
-        (config_container[iZone]->GetDesign_Variable(0) != SURFACE_FILE)) {
-
-      if (rank == MASTER_NODE)
-        cout << "\n---------- Start gradient evaluation using sensitivity information ----------" << endl;
-
-      /*--- Definition of the Class for surface deformation ---*/
-
-      surface_movement[iZone] = new CSurfaceMovement();
-
-      /*--- Copy coordinates to the surface structure ---*/
-
-      surface_movement[iZone]->CopyBoundary(geometry_container[iZone][INST_0], config_container[iZone]);
-
-      /*--- If AD mode is enabled we can use it to compute the projection,
-       *    otherwise we use finite differences. ---*/
-
-      if (config_container[iZone]->GetAD_Mode()) {
-        if (config_container[iZone]->GetSmoothGradient()) {
-          DerivativeTreatment_Gradient(geometry_container[iZone][INST_0], config_container[iZone], grid_movement[iZone], surface_movement[iZone] , Gradient);
-        } else {
-          SetProjection_AD(geometry_container[iZone][INST_0], config_container[iZone], surface_movement[iZone] , Gradient);
-        }
-      } else {
-        SetProjection_FD(geometry_container[iZone][INST_0], config_container[iZone], surface_movement[iZone] , Gradient);
-      }
-    }
-  } // for iZone
-
-  /*--- Write the gradient to a file ---*/
-
-  if (rank == MASTER_NODE)
-    Gradient_file.open(config_container[ZONE_0]->GetObjFunc_Grad_FileName().c_str(), ios::out);
-
-  /*--- Print gradients to screen and writes to file ---*/
-
-  OutputGradient(Gradient, config_container[ZONE_0], Gradient_file);
-
-  for (auto iDV = 0u; iDV  < config_container[ZONE_0]->GetnDV(); iDV++){
-    delete [] Gradient[iDV];
-  }
-  delete [] Gradient;
-
-  delete config;
-  config = nullptr;
-
-  if (rank == MASTER_NODE)
-    cout << "\n------------------------- Solver Postprocessing -------------------------" << endl;
-
-  if (geometry_container != nullptr) {
-    for (iZone = 0; iZone < nZone; iZone++) {
-      if (geometry_container[iZone] != nullptr) {
-        for (iInst = 0; iInst < nInst[iZone]; iInst++){
-          if (geometry_container[iZone][iInst] != nullptr) {
-            delete geometry_container[iZone][iInst];
-          }
-        }
-        delete geometry_container[iZone];
-      }
-    }
-    delete [] geometry_container;
-  }
-  if (rank == MASTER_NODE) cout << "Deleted CGeometry container." << endl;
-
-  if (surface_movement != nullptr) {
-    for (iZone = 0; iZone < nZone; iZone++) {
-      if (surface_movement[iZone] != nullptr) {
-        delete surface_movement[iZone];
-      }
-    }
-    delete [] surface_movement;
-  }
-  if (rank == MASTER_NODE) cout << "Deleted CSurfaceMovement class." << endl;
-
-  if (grid_movement != nullptr) {
-    for (iZone = 0; iZone < nZone; iZone++) {
-      if (grid_movement[iZone] != nullptr) {
-        delete grid_movement[iZone];
-      }
-    }
-    delete [] grid_movement;
-  }
-  if (rank == MASTER_NODE) cout << "Deleted CVolumetricMovement class." << endl;
-
-  delete config;
-  config = nullptr;
-  if (config_container != nullptr) {
-    for (iZone = 0; iZone < nZone; iZone++) {
-      if (config_container[iZone] != nullptr) {
-        delete config_container[iZone];
-      }
-    }
-    delete [] config_container;
-  }
-  if (rank == MASTER_NODE) cout << "Deleted CConfig container." << endl;
-
-  /*--- Synchronization point after a single solver iteration. Compute the
-   wall clock time required. ---*/
-
-  StopTime = SU2_MPI::Wtime();
-
-  /*--- Compute/print the total time for performance benchmarking. ---*/
-
-  UsedTime = StopTime-StartTime;
-  if (rank == MASTER_NODE) {
-    cout << "\nCompleted in " << fixed << UsedTime << " seconds on "<< size;
-    if (size == 1) cout << " core." << endl; else cout << " cores." << endl;
-  }
-
-  /*--- Exit the solver cleanly ---*/
-
-  if (rank == MASTER_NODE)
-    cout << "\n------------------------- Exit Success (SU2_DOT) ------------------------\n" << endl;
-
-  /*--- Finalize AD, if necessary. ---*/
-#ifdef HAVE_OPDI
-  AD::getGlobalTape().finalize();
+    SU2_MPI::Init(&argc, &argv);
 #endif
-
-  /*--- Finalize MPI parallelization. ---*/
-  SU2_MPI::Finalize();
-
-  /*--- Finalize OpenMP. ---*/
-  omp_finalize();
-
-  return EXIT_SUCCESS;
-
-}
-
-void SetProjection_FD(CGeometry *geometry, CConfig *config, CSurfaceMovement *surface_movement, su2double** Gradient){
-
-  unsigned short iDV, nDV, iFFDBox, nDV_Value, iMarker, iDim;
-  unsigned long iVertex, iPoint;
-  su2double delta_eps, my_Gradient, localGradient, *Normal, dS, *VarCoord, Sensitivity,
-  dalpha[3], deps[3], dalpha_deps;
-  bool *UpdatePoint, MoveSurface, Local_MoveSurface;
-  CFreeFormDefBox **FFDBox;
-
-  int rank = SU2_MPI::GetRank();
-
-  nDV = config->GetnDV();
-
-  /*--- Boolean controlling points to be updated ---*/
-
-  UpdatePoint = new bool[geometry->GetnPoint()];
-
-  /*--- Definition of the FFD deformation class ---*/
-
-  unsigned short nFFDBox = MAX_NUMBER_FFD;
-  FFDBox = new CFreeFormDefBox*[nFFDBox];
-  for (iFFDBox = 0; iFFDBox < MAX_NUMBER_FFD; iFFDBox++) FFDBox[iFFDBox] = nullptr;
-
-  for (iDV = 0; iDV  < nDV; iDV++){
-    nDV_Value = config->GetnDV_Value(iDV);
-    if (nDV_Value != 1){
-      SU2_MPI::Error("The projection using finite differences currently only supports a fixed direction of movement for FFD points.", CURRENT_FUNCTION);
-    }
-  }
-
-  /*--- Continuous adjoint gradient computation ---*/
-
-  if (rank == MASTER_NODE)
-    cout << "Evaluate functional gradient using Finite Differences." << endl;
-
-  for (iDV = 0; iDV < nDV; iDV++) {
-
-    MoveSurface = true;
-    Local_MoveSurface = true;
-
-    /*--- Free Form deformation based ---*/
-
-    if ((config->GetDesign_Variable(iDV) == FFD_CONTROL_POINT_2D) ||
-        (config->GetDesign_Variable(iDV) == FFD_CAMBER_2D) ||
-        (config->GetDesign_Variable(iDV) == FFD_THICKNESS_2D) ||
-        (config->GetDesign_Variable(iDV) == FFD_TWIST_2D) ||
-        (config->GetDesign_Variable(iDV) == FFD_CONTROL_POINT) ||
-        (config->GetDesign_Variable(iDV) == FFD_NACELLE) ||
-        (config->GetDesign_Variable(iDV) == FFD_GULL) ||
-        (config->GetDesign_Variable(iDV) == FFD_TWIST) ||
-        (config->GetDesign_Variable(iDV) == FFD_ROTATION) ||
-        (config->GetDesign_Variable(iDV) == FFD_CAMBER) ||
-        (config->GetDesign_Variable(iDV) == FFD_THICKNESS) ||
-        (config->GetDesign_Variable(iDV) == FFD_ANGLE_OF_ATTACK)) {
-
-      /*--- Read the FFD information in the first iteration ---*/
-
-      if (iDV == 0) {
-
-        if (rank == MASTER_NODE)
-          cout << "Read the FFD information from mesh file." << endl;
-
-        /*--- Read the FFD information from the grid file ---*/
-
-        surface_movement->ReadFFDInfo(geometry, config, FFDBox, config->GetMesh_FileName());
-
-        /*--- If the FFDBox was not defined in the input file ---*/
-        if (!surface_movement->GetFFDBoxDefinition()) {
-          SU2_MPI::Error("The input grid doesn't have the entire FFD information!", CURRENT_FUNCTION);
-        }
-
-        for (iFFDBox = 0; iFFDBox < surface_movement->GetnFFDBox(); iFFDBox++) {
-
-          if (rank == MASTER_NODE) cout << "Checking FFD box dimension." << endl;
-          surface_movement->CheckFFDDimension(geometry, config, FFDBox[iFFDBox], iFFDBox);
-
-          if (rank == MASTER_NODE) cout << "Check the FFD box intersections with the solid surfaces." << endl;
-          surface_movement->CheckFFDIntersections(geometry, config, FFDBox[iFFDBox], iFFDBox);
-
-        }
-
-        if (rank == MASTER_NODE)
-          cout <<"-------------------------------------------------------------------------" << endl;
-
-      }
-
-      if (rank == MASTER_NODE) {
-        cout << endl << "Design variable number "<< iDV <<"." << endl;
-        cout << "Performing 3D deformation of the surface." << endl;
-      }
-
-      /*--- Apply the control point change ---*/
-
-      MoveSurface = false;
-
-      for (iFFDBox = 0; iFFDBox < surface_movement->GetnFFDBox(); iFFDBox++) {
-
-        /*--- Reset FFD box ---*/
-
-        switch (config->GetDesign_Variable(iDV) ) {
-          case FFD_CONTROL_POINT_2D : Local_MoveSurface = surface_movement->SetFFDCPChange_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_CAMBER_2D :        Local_MoveSurface = surface_movement->SetFFDCamber_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_THICKNESS_2D :     Local_MoveSurface = surface_movement->SetFFDThickness_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_TWIST_2D :         Local_MoveSurface = surface_movement->SetFFDTwist_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_CONTROL_POINT :    Local_MoveSurface = surface_movement->SetFFDCPChange(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_NACELLE :          Local_MoveSurface = surface_movement->SetFFDNacelle(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_GULL :             Local_MoveSurface = surface_movement->SetFFDGull(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_TWIST :            Local_MoveSurface = surface_movement->SetFFDTwist(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_ROTATION :         Local_MoveSurface = surface_movement->SetFFDRotation(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_CAMBER :           Local_MoveSurface = surface_movement->SetFFDCamber(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_THICKNESS :        Local_MoveSurface = surface_movement->SetFFDThickness(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_CONTROL_SURFACE :  Local_MoveSurface = surface_movement->SetFFDControl_Surface(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-          case FFD_ANGLE_OF_ATTACK :  Gradient[iDV][0] = config->GetAoA_Sens(); break;
-        }
-
-        /*--- Recompute cartesian coordinates using the new control points position ---*/
-
-        if (Local_MoveSurface) {
-          MoveSurface = true;
-          surface_movement->SetCartesianCoord(geometry, config, FFDBox[iFFDBox], iFFDBox, true);
-        }
-
-      }
-
-    }
-
-    /*--- Hicks Henne design variable ---*/
-
-    else if (config->GetDesign_Variable(iDV) == HICKS_HENNE) {
-      surface_movement->SetHicksHenne(geometry, config, iDV, true);
-    }
-
-    /*--- Surface bump design variable ---*/
-
-    else if (config->GetDesign_Variable(iDV) == SURFACE_BUMP) {
-      surface_movement->SetSurface_Bump(geometry, config, iDV, true);
-    }
-
-    /*--- Kulfan (CST) design variable ---*/
-
-    else if (config->GetDesign_Variable(iDV) == CST) {
-      surface_movement->SetCST(geometry, config, iDV, true);
-    }
-
-    /*--- Displacement design variable ---*/
-
-    else if (config->GetDesign_Variable(iDV) == TRANSLATION) {
-      surface_movement->SetTranslation(geometry, config, iDV, true);
-    }
-
-    /*--- Angle of Attack design variable ---*/
-
-    else if (config->GetDesign_Variable(iDV) == ANGLE_OF_ATTACK) {
-      Gradient[iDV][0] = config->GetAoA_Sens();
-    }
-
-    /*--- Scale design variable ---*/
-
-    else if (config->GetDesign_Variable(iDV) == SCALE) {
-      surface_movement->SetScale(geometry, config, iDV, true);
-    }
-
-    /*--- Rotation design variable ---*/
-
-    else if (config->GetDesign_Variable(iDV) == ROTATION) {
-      surface_movement->SetRotation(geometry, config, iDV, true);
-    }
-
-    /*--- NACA_4Digits design variable ---*/
-
-    else if (config->GetDesign_Variable(iDV) == NACA_4DIGITS) {
-      surface_movement->SetNACA_4Digits(geometry, config);
-    }
-
-    /*--- Parabolic design variable ---*/
-
-    else if (config->GetDesign_Variable(iDV) == PARABOLIC) {
-      surface_movement->SetParabolic(geometry, config);
-    }
-
-    /*--- Design variable not implemented ---*/
-
-    else {
-      if (rank == MASTER_NODE)
-        cout << "Design Variable not implemented yet" << endl;
-    }
-
-    /*--- Load the delta change in the design variable (finite difference step). ---*/
-
-    if ((config->GetDesign_Variable(iDV) != ANGLE_OF_ATTACK) &&
-        (config->GetDesign_Variable(iDV) != FFD_ANGLE_OF_ATTACK)) {
-
-      /*--- If the Angle of attack is not involved, reset the value of the gradient ---*/
-
-      my_Gradient = 0.0; Gradient[iDV][0] = 0.0;
-
-      if (MoveSurface) {
-
-        delta_eps = config->GetDV_Value(iDV);
-
-        for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++)
-          UpdatePoint[iPoint] = true;
-
-        for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-          if (config->GetMarker_All_DV(iMarker) == YES) {
-            for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
-
-              iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
-              if ((iPoint < geometry->GetnPointDomain()) && UpdatePoint[iPoint]) {
-
-                Normal = geometry->vertex[iMarker][iVertex]->GetNormal();
-                VarCoord = geometry->vertex[iMarker][iVertex]->GetVarCoord();
-                Sensitivity = geometry->vertex[iMarker][iVertex]->GetAuxVar();
-
-                dS = 0.0;
-                for (iDim = 0; iDim < geometry->GetnDim(); iDim++) {
-                  dS += Normal[iDim]*Normal[iDim];
-                  deps[iDim] = VarCoord[iDim] / delta_eps;
-                }
-                dS = sqrt(dS);
-
-                dalpha_deps = 0.0;
-                for (iDim = 0; iDim < geometry->GetnDim(); iDim++) {
-                  dalpha[iDim] = Normal[iDim] / dS;
-                  dalpha_deps -= dalpha[iDim]*deps[iDim];
-                }
-
-                my_Gradient += Sensitivity*dalpha_deps;
-                UpdatePoint[iPoint] = false;
-              }
-            }
-          }
-        }
-      }
-
-      SU2_MPI::Allreduce(&my_Gradient, &localGradient, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-      Gradient[iDV][0] += localGradient;
-    }
-  }
-
-  /*--- Delete memory for parameterization. ---*/
-
-  if (FFDBox != nullptr) {
-    for (iFFDBox = 0; iFFDBox < MAX_NUMBER_FFD; iFFDBox++) {
-      if (FFDBox[iFFDBox] != nullptr) {
-        delete FFDBox[iFFDBox];
-      }
-    }
-    delete [] FFDBox;
-  }
-
-  delete [] UpdatePoint;
-
-}
-
-
-void SetProjection_AD(CGeometry *geometry, CConfig *config, CSurfaceMovement *surface_movement, su2double** Gradient){
-
-  su2double *VarCoord = nullptr, Sensitivity, my_Gradient, localGradient, *Normal, Area = 0.0;
-  unsigned short iDV_Value = 0, iMarker, nMarker, iDim, nDim, iDV, nDV;
-  unsigned long iVertex, nVertex, iPoint;
-
-  const int rank = SU2_MPI::GetRank();
-
-  nMarker = config->GetnMarker_All();
-  nDim    = geometry->GetnDim();
-  nDV     = config->GetnDV();
-
-  /*--- Discrete adjoint gradient computation ---*/
-
-  if (rank == MASTER_NODE)
-    cout  << endl << "Evaluate functional gradient using Algorithmic Differentiation (ZONE " << config->GetiZone() << ")." << endl;
-
-  /*--- Start recording of operations ---*/
-
-  AD::StartRecording();
-
-  /*--- Register design variables as input and set them to zero
-   * (since we want to have the derivative at alpha = 0, i.e. for the current design) ---*/
-
-  for (iDV = 0; iDV < nDV; iDV++){
-
-    for (iDV_Value = 0; iDV_Value < config->GetnDV_Value(iDV); iDV_Value++){
-
-      config->SetDV_Value(iDV, iDV_Value, 0.0);
-
-      AD::RegisterInput(config->GetDV_Value(iDV, iDV_Value));
-    }
-  }
-
-  /*--- Call the surface deformation routine ---*/
-
-  surface_movement->SetSurface_Deformation(geometry, config);
-
-  /*--- Stop the recording --- */
-
-  AD::StopRecording();
-
-  /*--- Create a structure to identify points that have been already visited.
-   * We need that to make sure to set the sensitivity of surface points only once
-   *  (Markers share points, so we would visit them more than once in the loop over the markers below) ---*/
-
-  vector<bool> visited(geometry->GetnPoint(), false);
-
-  /*--- Initialize the derivatives of the output of the surface deformation routine
-   * with the discrete adjoints from the CFD solution ---*/
-
-  for (iMarker = 0; iMarker < nMarker; iMarker++) {
-    if (config->GetMarker_All_DV(iMarker) == YES) {
-      nVertex = geometry->nVertex[iMarker];
-      for (iVertex = 0; iVertex <nVertex; iVertex++) {
-        iPoint      = geometry->vertex[iMarker][iVertex]->GetNode();
-        if (!visited[iPoint]){
-          VarCoord    = geometry->vertex[iMarker][iVertex]->GetVarCoord();
-          Normal      = geometry->vertex[iMarker][iVertex]->GetNormal();
-
-          Area = 0.0;
-          for (iDim = 0; iDim < nDim; iDim++){
-            Area += Normal[iDim]*Normal[iDim];
-          }
-          Area = sqrt(Area);
-
-          for (iDim = 0; iDim < nDim; iDim++){
-            if (config->GetDiscrete_Adjoint()){
-              Sensitivity = geometry->GetSensitivity(iPoint, iDim);
-            } else {
-              Sensitivity = -Normal[iDim]*geometry->vertex[iMarker][iVertex]->GetAuxVar()/Area;
-            }
-            SU2_TYPE::SetDerivative(VarCoord[iDim], SU2_TYPE::GetValue(Sensitivity));
-          }
-          visited[iPoint] = true;
-        }
-      }
-    }
-  }
-
-  /*--- Compute derivatives and extract gradient ---*/
-
-  AD::ComputeAdjoint();
-
-  for (iDV = 0; iDV  < nDV; iDV++){
-
-    for (iDV_Value = 0; iDV_Value < config->GetnDV_Value(iDV); iDV_Value++){
-
-      my_Gradient = SU2_TYPE::GetDerivative(config->GetDV_Value(iDV, iDV_Value));
-
-      SU2_MPI::Allreduce(&my_Gradient, &localGradient, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-
-      /*--- Angle of Attack design variable (this is different,
-       the value comes form the input file) ---*/
-
-      if ((config->GetDesign_Variable(iDV) == ANGLE_OF_ATTACK) ||
-          (config->GetDesign_Variable(iDV) == FFD_ANGLE_OF_ATTACK))  {
-        Gradient[iDV][iDV_Value] = config->GetAoA_Sens();
-      }
-
-      Gradient[iDV][iDV_Value] += localGradient;
-    }
-  }
-
-  AD::Reset();
-
-}
-
-void OutputGradient(su2double** Gradient, CConfig* config, ofstream& Gradient_file){
-
-  unsigned short nDV, iDV, iDV_Value, nDV_Value;
-
-  int rank = SU2_MPI::GetRank();
-
-  nDV = config->GetnDV();
-
-  /*--- Loop through all design variables and their gradients ---*/
-
-  for (iDV = 0; iDV  < nDV; iDV++){
-    nDV_Value = config->GetnDV_Value(iDV);
-    if (rank == MASTER_NODE){
-
-      /*--- Print the kind of design variable on screen ---*/
-
-      cout << endl << "Design variable (";
-      for (std::map<string, ENUM_PARAM>::const_iterator it = Param_Map.begin(); it != Param_Map.end(); ++it ){
-        if (it->second == config->GetDesign_Variable(iDV)){
-          cout << it->first << ") number "<< iDV << "." << endl;
-        }
-      }
-
-      /*--- Print the kind of objective function to screen ---*/
-
-      for (std::map<string, ENUM_OBJECTIVE>::const_iterator it = Objective_Map.begin(); it != Objective_Map.end(); ++it ){
-        if (it->second == config->GetKind_ObjFunc()){
-          cout << it->first << " gradient : ";
-          if (iDV == 0) Gradient_file << it->first << " gradient " << endl;
-        }
-      }
-
-      /*--- Print the gradient to file and screen ---*/
-
-      for (iDV_Value = 0; iDV_Value < nDV_Value; iDV_Value++){
-        cout << Gradient[iDV][iDV_Value];
-        if (iDV_Value != nDV_Value-1 ){
-          cout << ", ";
-        }
-        Gradient_file << Gradient[iDV][iDV_Value] << endl;
-      }
-      cout << endl;
-      cout <<"-------------------------------------------------------------------------" << endl;
-    }
-  }
-}
-
-
-void SetSensitivity_Files(CGeometry ***geometry, CConfig **config, unsigned short val_nZone) {
-
-  unsigned short iMarker,iDim, nDim, nMarker, nVar;
-  unsigned long iVertex, iPoint, nPoint, nVertex;
-  su2double *Normal, Prod, Sens = 0.0, SensDim, Area;
-
-  unsigned short iZone;
-
-  CSolver *solver  = nullptr;
-  COutput *output  = nullptr;
-
-  for (iZone = 0; iZone < val_nZone; iZone++) {
-
-    nPoint = geometry[iZone][INST_0]->GetnPoint();
-    nDim   = geometry[iZone][INST_0]->GetnDim();
-    nMarker = config[iZone]->GetnMarker_All();
-    nVar = nDim + 1;
-
-    /*--- We create a baseline solver to easily merge the sensitivity information ---*/
-
-    vector<string> fieldnames;
-    fieldnames.push_back("\"Point\"");
-    fieldnames.push_back("\"x\"");
-    fieldnames.push_back("\"y\"");
-    if (nDim == 3) {
-      fieldnames.push_back("\"z\"");
-    }
-    fieldnames.push_back("\"Sensitivity_x\"");
-    fieldnames.push_back("\"Sensitivity_y\"");
-    if (nDim == 3) {
-      fieldnames.push_back("\"Sensitivity_z\"");
-    }
-    fieldnames.push_back("\"Surface_Sensitivity\"");
-
-    solver = new CBaselineSolver(geometry[iZone][INST_0], config[iZone], nVar+nDim, fieldnames);
-
-    for (iPoint = 0; iPoint < nPoint; iPoint++) {
-      for (iDim = 0; iDim < nDim; iDim++) {
-        solver->GetNodes()->SetSolution(iPoint, iDim,      geometry[iZone][INST_0]->nodes->GetCoord(iPoint, iDim));
-        solver->GetNodes()->SetSolution(iPoint, iDim+nDim, geometry[iZone][INST_0]->GetSensitivity(iPoint, iDim));
-      }
-    }
-
-    /*--- Compute the sensitivity in normal direction ---*/
-
-    for (iMarker = 0; iMarker < nMarker; iMarker++) {
-
-      if(config[iZone]->GetSolid_Wall(iMarker) || (config[iZone]->GetMarker_All_DV(iMarker) == YES )) {
-
-        nVertex = geometry[iZone][INST_0]->GetnVertex(iMarker);
-
-        for (iVertex = 0; iVertex < nVertex; iVertex++) {
-          iPoint = geometry[iZone][INST_0]->vertex[iMarker][iVertex]->GetNode();
-          Normal = geometry[iZone][INST_0]->vertex[iMarker][iVertex]->GetNormal();
-          Prod = 0.0;
-          Area = 0.0;
-          for (iDim = 0; iDim < nDim; iDim++) {
-
-            /*--- Retrieve the gradient calculated with discrete adjoint method ---*/
-
-            SensDim = geometry[iZone][INST_0]->GetSensitivity(iPoint, iDim);
-
-            /*--- Calculate scalar product for projection onto the normal vector ---*/
-
-            Prod += Normal[iDim]*SensDim;
-
-            Area += Normal[iDim]*Normal[iDim];
-          }
-
-          Area = sqrt(Area);
-
-          /*--- Projection of the gradient onto the normal vector of the surface ---*/
-
-          Sens = Prod/Area;
-
-          solver->GetNodes()->SetSolution(iPoint, 2*nDim, Sens);
-
-        }
-      }
-    }
-
-    output = new CBaselineOutput(config[iZone], nDim, solver);
-    output->PreprocessVolumeOutput(config[iZone]);
-    output->PreprocessHistoryOutput(config[iZone], false);
-
-    /*--- Load the data --- */
-
-    output->Load_Data(geometry[iZone][INST_0], config[iZone], &solver);
-
-    /*--- Set the surface filename ---*/
-
-    output->SetSurface_Filename(config[iZone]->GetSurfSens_FileName());
-
-    /*--- Set the volume filename ---*/
-
-    output->SetVolume_Filename(config[iZone]->GetVolSens_FileName());
-
-    /*--- Write to file ---*/
-
-    for (unsigned short iFile = 0; iFile < config[iZone]->GetnVolumeOutputFiles(); iFile++){
-      auto FileFormat = config[iZone]->GetVolumeOutputFiles();
-      if (FileFormat[iFile] != OUTPUT_TYPE::RESTART_ASCII &&
-          FileFormat[iFile] != OUTPUT_TYPE::RESTART_BINARY &&
-          FileFormat[iFile] != OUTPUT_TYPE::CSV)
-        output->WriteToFile(config[iZone], geometry[iZone][INST_0], FileFormat[iFile]);
-    }
-
-    /*--- Free memory ---*/
-
-    delete output;
-    delete solver;
-
-  }
-
-}
-
-void DerivativeTreatment_MeshSensitivity(CGeometry *geometry, CConfig *config, CVolumetricMovement *grid_movement) {
-
-  int rank = SU2_MPI::GetRank();
-
-  /*--- Warning if choosen smoothing mode is unsupported.
-   * This is the default option if the user has not specified a mode in the config file. ---*/
-  if (config->GetSobMode() == ENUM_SOBOLEV_MODUS::NONE) {
-    SU2_MPI::Error("Unsupported operation modus for the Sobolev Smoothing Solver.", CURRENT_FUNCTION);
-  }
-
-  /*-- Construct the smoothing solver and numerics ---*/
-  std::unique_ptr<CSolver> solver(new CGradientSmoothingSolver(geometry, config));
-  unsigned dim = (config->GetSmoothOnSurface() ? geometry->GetnDim() - 1 : geometry->GetnDim());
-  std::unique_ptr<CNumerics> numerics(new CGradSmoothing(dim, config));
-
-  if (rank == MASTER_NODE)  cout << "Sobolev Smoothing of derivatives is active." << endl;
-
-  /*--- Apply the smoothing procedure on the mesh level. ---*/
-  if (config->GetSobMode() == ENUM_SOBOLEV_MODUS::MESH_LEVEL) {
-    if (rank == MASTER_NODE) cout << "  working on mesh level" << endl;
-
-    /*--- Work with the surface derivatives. ---*/
-    if (config->GetSmoothOnSurface()) {
-
-      /*--- Project to surface and then smooth on surface. ---*/
-      grid_movement->SetVolume_Deformation(geometry, config, false, true);
-
-      /*--- Get the sensitivities from the geometry class to work with. ---*/
-      solver->ReadSensFromGeometry(geometry);
-
-      /*--- Perform the smoothing procedure on all boundaries marked as DV marker. ---*/
-      solver->ApplyGradientSmoothingSurface(geometry, numerics.get(), config);
-
-      /*--- After appling the solver write the results back ---*/
-      solver->WriteSensToGeometry(geometry);
-
-    /*--- Work with the volume derivatives. ---*/
-    } else {
-
-      /*--- Get the sensitivities from the geometry class to work with. ---*/
-      solver->ReadSensFromGeometry(geometry);
-
-      solver->ApplyGradientSmoothingVolume(geometry, numerics.get(), config);
-
-      /*--- After appling the solver write the results back ---*/
-      solver->WriteSensToGeometry(geometry);
-
-      /*--- Projection is applied after smoothing. ---*/
-      grid_movement->SetVolume_Deformation(geometry, config, false, true);
-    }
-
-  }
-
-}
-
-void DerivativeTreatment_Gradient(CGeometry *geometry, CConfig *config, CVolumetricMovement* grid_movement, CSurfaceMovement *surface_movement, su2double** Gradient) {
-
-  int rank = SU2_MPI::GetRank();
-
-  /*--- Error if choosen smoothing mode is unsupported.
-   * This is the default option if the user has not specified a mode in the config file. ---*/
-  if (config->GetSobMode() == ENUM_SOBOLEV_MODUS::NONE) {
-    SU2_MPI::Error("Unsupported operation modus for the Sobolev Smoothing Solver.", CURRENT_FUNCTION);
-  }
-
-  /*-- Construct the smoothing solver and numerics ---*/
-  std::unique_ptr<CSolver> solver(new CGradientSmoothingSolver(geometry, config));
-  unsigned dim = (config->GetSmoothOnSurface() ? geometry->GetnDim() - 1 : geometry->GetnDim());
-  std::unique_ptr<CNumerics> numerics(new CGradSmoothing(dim, config));
-
-  if (rank == MASTER_NODE)  cout << "Sobolev Smoothing of derivatives is active." << endl;
-
-  /*--- Get the sensitivities from the geometry class to work with. ---*/
-  solver->ReadSensFromGeometry(geometry);
-
-  /*--- Apply the smoothing procedure on the DV level. ---*/
-  if (config->GetSobMode() == ENUM_SOBOLEV_MODUS::PARAM_LEVEL_COMPLETE) {
-    solver->ApplyGradientSmoothingDV(geometry, numerics.get(), surface_movement, grid_movement, config, Gradient);
-
-    /*--- If smoothing already took place on the mesh level, or none is requested, just do standard projection. ---*/
-  } else if (config->GetSobMode() == ENUM_SOBOLEV_MODUS::ONLY_GRAD ||
-             config->GetSobMode() == ENUM_SOBOLEV_MODUS::MESH_LEVEL) {
-    solver->RecordTapeAndCalculateOriginalGradient(geometry, surface_movement, grid_movement, config, Gradient);
-  }
-
+    SU2_MPI::Comm comm = SU2_MPI::GetComm();
+    
+    /*--- Load in the number of zones and spatial dimensions in the mesh file
+     (if no config file is specified, default.cfg is used) ---*/
+    
+    if (argc == 2) { strcpy(config_file_name, argv[1]); }
+    else { strcpy(config_file_name, "default.cfg"); }
+    
+    /*--- Initialize the mesh deformation driver ---*/
+    
+    driver = new CDiscAdjDeformationDriver(config_file_name, comm);
+    
+    /*--- Launch the main external loop of the solver. ---*/
+    
+    driver->Run();
+    
+    /*--- Postprocess all the containers, close history file, exit SU2. ---*/
+    
+    driver->Postprocessing();
+    
+    delete driver;
+    
+    /*--- Finalize MPI parallelization ---*/
+    SU2_MPI::Finalize();
+    
+    return EXIT_SUCCESS;
+    
 }
diff --git a/SU2_PY/pySU2/pySU2.i b/SU2_PY/pySU2/pySU2.i
index 4cbb9afc3bd..e5cdf388fe0 100644
--- a/SU2_PY/pySU2/pySU2.i
+++ b/SU2_PY/pySU2/pySU2.i
@@ -50,6 +50,7 @@ threads="1"
 %import "../../Common/include/code_config.hpp"
 %import "../../Common/include/basic_types/datatype_structure.hpp"
 %import "../../Common/include/parallelization/mpi_structure.hpp"
+%import "../../Common/include/drivers/CDriverBase.hpp"
 %include "std_string.i"
 %include "std_vector.i"
 %include "std_map.i"
diff --git a/SU2_PY/pySU2/pySU2ad.i b/SU2_PY/pySU2/pySU2ad.i
index e2e3bfbc54c..f0c6702a940 100644
--- a/SU2_PY/pySU2/pySU2ad.i
+++ b/SU2_PY/pySU2/pySU2ad.i
@@ -50,6 +50,7 @@ threads="1"
 %import "../../Common/include/code_config.hpp"
 %import "../../Common/include/basic_types/datatype_structure.hpp"
 %import "../../Common/include/parallelization/mpi_structure.hpp"
+%import "../../Common/include/drivers/CDriverBase.hpp"
 %include "std_string.i"
 %include "std_vector.i"
 %include "std_map.i"

From de94b6dc8057b1f67efe393b13149d6ad53c7f2f Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Mon, 14 Feb 2022 10:54:30 -0800
Subject: [PATCH 014/656] Introduce dependency of SU2_DOT on SU2_DEF

---
 SU2_DOT/src/meson.build | 4 ++--
 meson.build             | 4 ++--
 2 files changed, 4 insertions(+), 4 deletions(-)

diff --git a/SU2_DOT/src/meson.build b/SU2_DOT/src/meson.build
index 0f0b5234dcd..3cda6c961ed 100644
--- a/SU2_DOT/src/meson.build
+++ b/SU2_DOT/src/meson.build
@@ -5,7 +5,7 @@ if get_option('enable-normal')
   su2_dot = executable('SU2_DOT',
                       su2_dot_src,
                       install: true,
-                      dependencies: [su2_deps, common_dep, su2_cfd_dep],
+                      dependencies: [su2_deps, common_dep, su2_cfd_dep, su2_def_dep],
                       cpp_args :[default_warning_flags, su2_cpp_args])
 
 endif
@@ -15,7 +15,7 @@ if get_option('enable-autodiff')
   su2_dot_ad = executable('SU2_DOT_AD',
                           su2_dot_src,
                           install: true,
-                          dependencies: [su2_deps, codi_dep, commonAD_dep, su2_cfd_dep_ad],
+                          dependencies: [su2_deps, codi_dep, commonAD_dep, su2_cfd_dep_ad, su2_def_dep_ad],
 		                      cpp_args : [default_warning_flags, su2_cpp_args, codi_rev_args])
 
 endif
diff --git a/meson.build b/meson.build
index ebb7be89255..597fc38ab7a 100644
--- a/meson.build
+++ b/meson.build
@@ -230,10 +230,10 @@ endif
 subdir('Common/src')
 # compile SU2_CFD executable
 subdir('SU2_CFD/src')
-# compile SU2_DOT executable
-subdir('SU2_DOT/src')
 # compile SU2_DEF executable
 subdir('SU2_DEF/src')
+# compile SU2_DOT executable
+subdir('SU2_DOT/src')
 # compile SU2_GEO executable
 subdir('SU2_GEO/src')
 # compile SU2_SOL executable

From 1c57ad34350a4c8bba680fd56b8ef51c29e965d9 Mon Sep 17 00:00:00 2001
From: aa-g <aa.gastaldi@pm.me>
Date: Mon, 14 Feb 2022 23:01:35 +0100
Subject: [PATCH 015/656] [WIP] Small fixes

---
 .../grid_movement/CSurfaceMovement.hpp        |   2 +-
 Common/src/grid_movement/CSurfaceMovement.cpp |   6 +-
 SU2_CFD/src/drivers/CDriver.cpp               |   2 +-
 .../include/drivers/CDeformationDriver.hpp    |  11 +-
 SU2_DEF/src/drivers/CDeformationDriver.cpp    | 105 +++++++++++-------
 5 files changed, 75 insertions(+), 51 deletions(-)

diff --git a/Common/include/grid_movement/CSurfaceMovement.hpp b/Common/include/grid_movement/CSurfaceMovement.hpp
index 45acfd2aa74..700fa6dbe32 100644
--- a/Common/include/grid_movement/CSurfaceMovement.hpp
+++ b/Common/include/grid_movement/CSurfaceMovement.hpp
@@ -443,7 +443,7 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] val_mesh_filename - Name of the grid output file.
    */
-  void WriteFFDInfo(CSurfaceMovement **surface_movement, CGeometry **geometry, CConfig **config);
+  void WriteFFDInfo(CSurfaceMovement **surface_movement, CGeometry ****geometry, CConfig **config);
 
   /*!
    * \brief Get information about if there is a complete FFDBox definition, or it is necessary to
diff --git a/Common/src/grid_movement/CSurfaceMovement.cpp b/Common/src/grid_movement/CSurfaceMovement.cpp
index 3d346c13950..8c57008d9ea 100644
--- a/Common/src/grid_movement/CSurfaceMovement.cpp
+++ b/Common/src/grid_movement/CSurfaceMovement.cpp
@@ -4674,7 +4674,7 @@ void CSurfaceMovement::MergeFFDInfo(CGeometry *geometry, CConfig *config) {
 
 }
 
-void CSurfaceMovement::WriteFFDInfo(CSurfaceMovement** surface_movement, CGeometry **geometry, CConfig **config) {
+void CSurfaceMovement::WriteFFDInfo(CSurfaceMovement** surface_movement, CGeometry ****geometry, CConfig **config) {
 
 
   unsigned short iOrder, jOrder, kOrder, iFFDBox, iCornerPoints, iParentFFDBox, iChildFFDBox, iZone;
@@ -4685,13 +4685,13 @@ void CSurfaceMovement::WriteFFDInfo(CSurfaceMovement** surface_movement, CGeomet
 
   bool polar = (config[ZONE_0]->GetFFD_CoordSystem() == POLAR);
 
-  unsigned short nDim = geometry[ZONE_0]->GetnDim();
+  unsigned short nDim = geometry[ZONE_0][INST_0][MESH_0]->GetnDim();
 
   for (iZone = 0; iZone < config[ZONE_0]->GetnZone(); iZone++){
 
     /*--- Merge the parallel FFD info ---*/
 
-    surface_movement[iZone]->MergeFFDInfo(geometry[iZone], config[iZone]);
+    surface_movement[iZone]->MergeFFDInfo(geometry[iZone][INST_0][MESH_0], config[iZone]);
 
     if (iZone > 0){
 
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index dcb8447d591..53ec9afc51a 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -343,7 +343,7 @@ void CDriver::SetContainers_Null(){
   interface_container            = new CInterface**[nZone] ();
   interface_types                = new unsigned short*[nZone] ();
   output_container               = new COutput*[nZone] ();
-  nInst                          = new unsigned short[nZone] ();
+  nInst                          = new unsigned short[nZone] ();  // TODO: remove (moved to base class)
   driver_config                  = nullptr;
   driver_output                  = nullptr;
 
diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index 5c1d7c0da4e..20b260f6eff 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -42,9 +42,6 @@
 
 class CDeformationDriver : public CDriverBase {
 
-protected:
-  CNumerics ***numerics_container;
-
 public:
   /*!
    * \brief Constructor of the class.
@@ -76,10 +73,10 @@ class CDeformationDriver : public CDriverBase {
   void CommunicateMeshDisplacements(void);
 
 protected:
-  /*!
-   * \brief Init_Containers
-   */
-  void SetContainers_Null();
+  // /*!
+  //  * \brief Init_Containers
+  //  */
+  // void SetContainer_Null();
 
   /*!
    * \brief Read in the config and mesh files.
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 90563e93f2f..22f58ebb574 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -54,11 +54,6 @@ CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
     /*--- Copy the config filename ---*/
     strcpy(config_file_name, confFile);
     
-    /*--- Initialize the configuration of the driver ---*/
-    driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DEF);
-    
-    nZone = driver_config->GetnZone();
-    
     /*--- Initialize containers --- */
     
     SetContainers_Null();
@@ -107,36 +102,41 @@ CDeformationDriver::~CDeformationDriver(void) {
     
 }
 
-void CDeformationDriver::SetContainers_Null() {
-    
-    /*--- Create pointers to all of the classes that may be used throughout
-     the SU2_DEF code. In general, the pointers are instantiated down a
-     hierarchy over all zones as described in the comments below. ---*/
-    config_container   = new CConfig*[nZone];
-    output_container   = new COutput*[nZone];
-    geometry_container = new CGeometry***[nZone];
-    surface_movement   = new CSurfaceMovement*[nZone];
-    grid_movement      = new CVolumetricMovement**[nZone];
-    
-    solver_container   = new CSolver****[nZone];
-    numerics_container = new CNumerics**[nZone];
-    
-    for (iZone = 0; iZone < nZone; iZone++) {
-        config_container[iZone]   = nullptr;
-        output_container[iZone]   = nullptr;
-        geometry_container[iZone] = nullptr;
-        surface_movement[iZone]   = nullptr;
-        grid_movement[iZone]      = nullptr;
-        solver_container[iZone]   = nullptr;
-        numerics_container[iZone] = nullptr;
-    }
-}
+// void CDeformationDriver::SetContainers_Null() {
+//     
+//     /*--- Create pointers to all of the classes that may be used throughout
+//      the SU2_DEF code. In general, the pointers are instantiated down a
+//      hierarchy over all zones as described in the comments below. ---*/
+//     config_container   = new CConfig*[nZone];
+//     output_container   = new COutput*[nZone];
+//     geometry_container = new CGeometry***[nZone];
+//     surface_movement   = new CSurfaceMovement*[nZone];
+//     grid_movement      = new CVolumetricMovement**[nZone];
+//     
+//     solver_container   = new CSolver****[nZone];
+//     numerics_container = new CNumerics**[nZone];
+//     
+//     for (iZone = 0; iZone < nZone; iZone++) {
+//         config_container[iZone]   = nullptr;
+//         output_container[iZone]   = nullptr;
+//         geometry_container[iZone] = nullptr;
+//         surface_movement[iZone]   = nullptr;
+//         grid_movement[iZone]      = nullptr;
+//         solver_container[iZone]   = nullptr;
+//         numerics_container[iZone] = nullptr;
+//     }
+// }
 
 void CDeformationDriver::Input_Preprocessing() {
     
     /*--- Initialize a char to store the zone filename ---*/
     char zone_file_name[MAX_STRING_SIZE];
     
+    /*--- Initialize the configuration of the driver ---*/
+    driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DEF);
+    
+    nZone = driver_config->GetnZone();  
+    
     /*--- Loop over all zones to initialize the various classes. In most
      cases, nZone is equal to one. This represents the solution of a partial
      differential equation on a single block, unstructured mesh. ---*/
@@ -186,7 +186,11 @@ void CDeformationDriver::Geometrical_Preprocessing() {
         geometry_aux->SetColorGrid_Parallel(config_container[iZone]);
         
         /*--- Build the grid data structures using the ParMETIS coloring. ---*/
-        
+        unsigned short nInst_Zone = nInst[iZone];
+        unsigned short nMesh = 1;
+
+        geometry_container[iZone] = new CGeometry**[nInst_Zone] ();
+        geometry_container[iZone][INST_0] = new CGeometry*[nMesh] ();
         geometry_container[iZone][INST_0][MESH_0] = new CPhysicalGeometry(geometry_aux, config_container[iZone]);
         
         /*--- Deallocate the memory of geometry_aux ---*/
@@ -263,21 +267,36 @@ void CDeformationDriver::Output_Preprocessing() {
 void CDeformationDriver::Solver_Preprocessing() {
     
     for (iZone = 0; iZone < nZone; iZone++) {
+        unsigned short nInst_Zone = nInst[iZone];
+        unsigned short nMesh = 1;
+        unsigned short nSols = MAX_SOLS;
+
+
+        solver_container[iZone] = new CSolver*** [nInst_Zone] ();
+        solver_container[iZone][INST_0] = new CSolver** [nMesh] ();
+        solver_container[iZone][INST_0][MESH_0] = new CSolver* [nSols] ();
         solver_container[iZone][INST_0][MESH_0][MESH_SOL] = new CMeshSolver(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
-    }
-    
+    } 
 }
 
 void CDeformationDriver::Numerics_Preprocessing() {
     
     for (iZone = 0; iZone < nZone; iZone++) {
-        numerics_container[iZone] = new CNumerics* [omp_get_num_threads() * MAX_TERMS]();
+        unsigned short nInst_Zone = nInst[iZone];
+        unsigned short nMesh = 1;
+        unsigned short nSols = MAX_SOLS;
+        unsigned int nTerm = omp_get_num_threads() * MAX_TERMS;
+
+        numerics_container[iZone] = new CNumerics**** [nInst_Zone] ();
+        numerics_container[iZone][INST_0] = new CNumerics*** [nMesh] ();
+        numerics_container[iZone][INST_0][MESH_0] = new CNumerics** [nSols] ();
+        numerics_container[iZone][INST_0][MESH_0][MESH_SOL] = new CNumerics* [nTerm] ();
         
         for (int thread = 0; thread < omp_get_max_threads(); ++thread) {
             const int iTerm = FEA_TERM + thread * MAX_TERMS;
             const int nDim = geometry_container[iZone][INST_0][MESH_0]->GetnDim();
             
-            numerics_container[iZone][iTerm] = new CFEAMeshElasticity(nDim, nDim, geometry_container[iZone][INST_0][MESH_0]->GetnElem(), config_container[iZone]);
+            numerics_container[iZone][INST_0][MESH_0][MESH_SOL][iTerm] = new CFEAMeshElasticity(nDim, nDim, geometry_container[iZone][INST_0][MESH_0]->GetnElem(), config_container[iZone]);
         }
         
     }
@@ -322,11 +341,11 @@ void CDeformationDriver::Update() {
         
         /*--- Set the stiffness of each element mesh into the mesh numerics ---*/
         
-        solver_container[iZone][INST_0][MESH_0][MESH_SOL]->SetMesh_Stiffness(numerics_container[iZone], config_container[iZone]);
+        solver_container[iZone][INST_0][MESH_0][MESH_SOL]->SetMesh_Stiffness(numerics_container[iZone][INST_0][MESH_0][MESH_SOL], config_container[iZone]);
         
         /*--- Deform the volume grid around the new boundary locations ---*/
         
-        solver_container[iZone][INST_0][MESH_0][MESH_SOL]->DeformMesh(geometry_container[iZone][INST_0][MESH_0], numerics_container[iZone], config_container[iZone]);
+        solver_container[iZone][INST_0][MESH_0][MESH_SOL]->DeformMesh(geometry_container[iZone][INST_0][MESH_0], numerics_container[iZone][INST_0][MESH_0][MESH_SOL], config_container[iZone]);
         
     }
 }
@@ -511,7 +530,7 @@ void CDeformationDriver::Output() {
         /*--- Load the data --- */
         
         output_container[iZone]->Load_Data(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], nullptr);
-        
+
         output_container[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone][INST_0][MESH_0], OUTPUT_TYPE::MESH, driver_config->GetMesh_Out_FileName());
         
         /*--- Set the file names for the visualization files ---*/
@@ -538,7 +557,7 @@ void CDeformationDriver::Output() {
             
             if (rank == MASTER_NODE) cout << "Adding any FFD information to the SU2 file." << endl;
             
-            surface_movement[ZONE_0]->WriteFFDInfo(surface_movement, geometry_container[INST_0][MESH_0], config_container);
+            surface_movement[ZONE_0]->WriteFFDInfo(surface_movement, geometry_container, config_container);
             
         }
     }
@@ -555,7 +574,10 @@ void CDeformationDriver::Postprocessing() {
     for (iZone = 0; iZone < nZone; iZone++) {
         if (numerics_container[iZone] != nullptr) {
             for (unsigned int iTerm = 0; iTerm < MAX_TERMS*omp_get_max_threads(); iTerm++) {
-                delete numerics_container[iZone][iTerm];
+                delete numerics_container[iZone][INST_0][MESH_0][MESH_SOL][iTerm];
+                delete [] numerics_container[iZone][INST_0][MESH_0][MESH_SOL];
+                delete [] numerics_container[iZone][INST_0][MESH_0];
+                delete [] numerics_container[iZone][INST_0];
             }
             delete [] numerics_container[iZone];
         }
@@ -565,6 +587,9 @@ void CDeformationDriver::Postprocessing() {
     
     for (iZone = 0; iZone < nZone; iZone++) {
         delete solver_container[iZone][INST_0][MESH_0][MESH_SOL];
+        delete [] solver_container[iZone][INST_0][MESH_0];
+        delete [] solver_container[iZone][INST_0];
+        delete [] solver_container[iZone];
     }
     delete [] solver_container;
     if (rank == MASTER_NODE) cout << "Deleted CSolver container." << endl;
@@ -572,6 +597,8 @@ void CDeformationDriver::Postprocessing() {
     if (geometry_container != nullptr) {
         for (iZone = 0; iZone < nZone; iZone++) {
             delete geometry_container[iZone][INST_0][MESH_0];
+            delete [] geometry_container[iZone][INST_0];
+            delete [] geometry_container[iZone];
         }
         delete [] geometry_container;
     }

From 342d3a204c36f1affc49d8e4b443e6684c7d097b Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Tue, 15 Feb 2022 15:21:07 -0800
Subject: [PATCH 016/656] Fix 'unknown module' SWIG warning for CDriverBase

---
 SU2_PY/pySU2/pySU2.i   | 5 +++--
 SU2_PY/pySU2/pySU2ad.i | 5 +++--
 2 files changed, 6 insertions(+), 4 deletions(-)

diff --git a/SU2_PY/pySU2/pySU2.i b/SU2_PY/pySU2/pySU2.i
index e5cdf388fe0..02ba990a514 100644
--- a/SU2_PY/pySU2/pySU2.i
+++ b/SU2_PY/pySU2/pySU2.i
@@ -38,6 +38,7 @@ threads="1"
 ) pysu2
 %{
 
+#include "../../Common/include/drivers/CDriverBase.hpp"
 #include "../../SU2_CFD/include/drivers/CDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CMultizoneDriver.hpp"
@@ -50,7 +51,7 @@ threads="1"
 %import "../../Common/include/code_config.hpp"
 %import "../../Common/include/basic_types/datatype_structure.hpp"
 %import "../../Common/include/parallelization/mpi_structure.hpp"
-%import "../../Common/include/drivers/CDriverBase.hpp"
+
 %include "std_string.i"
 %include "std_vector.i"
 %include "std_map.i"
@@ -88,7 +89,7 @@ const unsigned int MESH_1 = 1; /*!< \brief Definition of the finest grid level.
 const unsigned int ZONE_0 = 0; /*!< \brief Definition of the first grid domain. */
 const unsigned int ZONE_1 = 1; /*!< \brief Definition of the first grid domain. */
 
-// CDriver class
+%include "../../Common/include/drivers/CDriverBase.hpp"
 %include "../../SU2_CFD/include/drivers/CDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CMultizoneDriver.hpp"
diff --git a/SU2_PY/pySU2/pySU2ad.i b/SU2_PY/pySU2/pySU2ad.i
index f0c6702a940..27a2dfe6cd1 100644
--- a/SU2_PY/pySU2/pySU2ad.i
+++ b/SU2_PY/pySU2/pySU2ad.i
@@ -38,6 +38,7 @@ threads="1"
 ) pysu2ad
 %{
 
+#include "../../Common/include/drivers/CDriverBase.hpp"
 #include "../../SU2_CFD/include/drivers/CDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CMultizoneDriver.hpp"
@@ -50,7 +51,7 @@ threads="1"
 %import "../../Common/include/code_config.hpp"
 %import "../../Common/include/basic_types/datatype_structure.hpp"
 %import "../../Common/include/parallelization/mpi_structure.hpp"
-%import "../../Common/include/drivers/CDriverBase.hpp"
+
 %include "std_string.i"
 %include "std_vector.i"
 %include "std_map.i"
@@ -88,7 +89,7 @@ const unsigned int MESH_1 = 1; /*!< \brief Definition of the finest grid level.
 const unsigned int ZONE_0 = 0; /*!< \brief Definition of the first grid domain. */
 const unsigned int ZONE_1 = 1; /*!< \brief Definition of the first grid domain. */
 
-// CDriver class
+%include "../../Common/include/drivers/CDriverBase.hpp"
 %include "../../SU2_CFD/include/drivers/CDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CMultizoneDriver.hpp"

From bfb175c15a5086847a69507869b2071a90a87232 Mon Sep 17 00:00:00 2001
From: aa-g <aa.gastaldi@pm.me>
Date: Wed, 16 Feb 2022 20:43:05 +0100
Subject: [PATCH 017/656] Fix small issues in getters, skip FFD output if not
 defined

---
 Common/src/drivers/CDriverBase.cpp            | 13 ++++----
 .../include/drivers/CDeformationDriver.hpp    |  3 ++
 SU2_DEF/src/drivers/CDeformationDriver.cpp    | 30 ++++++++++---------
 SU2_PY/pySU2/pySU2.i                          |  3 ++
 SU2_PY/pySU2/pySU2ad.i                        |  3 ++
 5 files changed, 31 insertions(+), 21 deletions(-)

diff --git a/Common/src/drivers/CDriverBase.cpp b/Common/src/drivers/CDriverBase.cpp
index 094113173ec..7d7de27aabd 100644
--- a/Common/src/drivers/CDriverBase.cpp
+++ b/Common/src/drivers/CDriverBase.cpp
@@ -65,24 +65,23 @@ void CDriverBase::SetContainers_Null() {
     grid_movement         = nullptr;
     FFDBox                = nullptr;
     
-    nInst                 = new unsigned short[nZone] ();
-    
     config_container      = new CConfig*[nZone] ();
     output_container      = new COutput*[nZone] ();
     geometry_container    = new CGeometry***[nZone] ();
     solver_container      = new CSolver****[nZone] ();
     numerics_container    = new CNumerics*****[nZone] ();
-    
     surface_movement      = new CSurfaceMovement*[nZone] ();
     grid_movement         = new CVolumetricMovement**[nZone] ();
     FFDBox                = new CFreeFormDefBox**[nZone] ();
     
-    driver_config         = nullptr;
-    driver_output         = nullptr;
+    nInst                 = new unsigned short[nZone] ();
     
     for (iZone = 0; iZone < nZone; iZone++) {
         nInst[iZone] = 1;
     }
+
+    driver_config         = nullptr;
+    driver_output         = nullptr;
 }
 
 map<string, int> CDriverBase::GetBoundaryMarkerIndices() const {
@@ -302,7 +301,7 @@ vector<bool> CDriverBase::GetDomain() const {
     CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
     
     const auto nPoint = geometry->GetnPoint();
-    vector<bool> values(nPoint);
+    vector<bool> values;
     
     for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
         values.push_back(geometry->nodes->GetDomain(iPoint));
@@ -315,7 +314,7 @@ vector<bool> CDriverBase::GetDomainMarker(unsigned short iMarker) const {
     CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
     
     const auto nVertex = geometry->GetnVertex(iMarker);
-    vector<bool> values(nVertex);
+    vector<bool> values;
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
         auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index 20b260f6eff..6d64c4b6f2f 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -42,6 +42,9 @@
 
 class CDeformationDriver : public CDriverBase {
 
+protected:
+  bool haveSurfaceDeformation = false;  // flag used to determine whether surface deformation is available for output
+
 public:
   /*!
    * \brief Constructor of the class.
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 22f58ebb574..c1e6136b970 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -116,14 +116,7 @@ CDeformationDriver::~CDeformationDriver(void) {
 //     solver_container   = new CSolver****[nZone];
 //     numerics_container = new CNumerics**[nZone];
 //     
-//     for (iZone = 0; iZone < nZone; iZone++) {
-//         config_container[iZone]   = nullptr;
-//         output_container[iZone]   = nullptr;
-//         geometry_container[iZone] = nullptr;
-//         surface_movement[iZone]   = nullptr;
-//         grid_movement[iZone]      = nullptr;
-//         solver_container[iZone]   = nullptr;
-//         numerics_container[iZone] = nullptr;
+
 //     }
 // }
 
@@ -243,6 +236,9 @@ void CDeformationDriver::Geometrical_Preprocessing() {
         geometry_container[iZone][INST_0][MESH_0]->PreprocessP2PComms(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
         
     }
+        
+    /*--- Get the number of dimensions ---*/
+    nDim = geometry_container[ZONE_0][INST_0][MESH_0]->GetnDim();
 }
 
 void CDeformationDriver::Output_Preprocessing() {
@@ -351,6 +347,8 @@ void CDeformationDriver::Update() {
 }
 
 void CDeformationDriver::Update_Legacy() {
+
+    std::cout << "UPDATE LEGACY CALLED" << std::endl; 
     
     for (iZone = 0; iZone < nZone; iZone++){
         
@@ -393,6 +391,7 @@ void CDeformationDriver::Update_Legacy() {
                 /*--- Definition and initialization of the surface deformation class ---*/
                 
                 surface_movement[iZone] = new CSurfaceMovement();
+                haveSurfaceDeformation = true;
                 
                 /*--- Copy coordinates to the surface structure ---*/
                 
@@ -553,12 +552,15 @@ void CDeformationDriver::Output() {
             (config_container[ZONE_0]->GetDesign_Variable(0) != TRANSLATE_GRID) &&
             (config_container[ZONE_0]->GetDesign_Variable(0) != ROTATE_GRID)) {
             
-            /*--- Write the the free-form deformation boxes after deformation. ---*/
-            
-            if (rank == MASTER_NODE) cout << "Adding any FFD information to the SU2 file." << endl;
-            
-            surface_movement[ZONE_0]->WriteFFDInfo(surface_movement, geometry_container, config_container);
-            
+            /*--- Write the the free-form deformation boxes after deformation (if defined). ---*/
+            if (true) {
+                if (rank == MASTER_NODE) cout << "No FFD information available." << endl;
+            }
+            else {
+                if (rank == MASTER_NODE) cout << "Adding any FFD information to the SU2 file." << endl;
+
+                surface_movement[ZONE_0]->WriteFFDInfo(surface_movement, geometry_container, config_container);
+            }  
         }
     }
 }
diff --git a/SU2_PY/pySU2/pySU2.i b/SU2_PY/pySU2/pySU2.i
index 02ba990a514..0125ffd1e6b 100644
--- a/SU2_PY/pySU2/pySU2.i
+++ b/SU2_PY/pySU2/pySU2.i
@@ -63,6 +63,9 @@ threads="1"
 #endif
 
 namespace std {
+   %template() vector<bool>;
+   %template() vector<unsigned long>;
+   %template() vector<vector<unsigned long>>;
    %template() vector<int>;
    %template() vector<double>;
    %template() vector<string>;
diff --git a/SU2_PY/pySU2/pySU2ad.i b/SU2_PY/pySU2/pySU2ad.i
index 27a2dfe6cd1..a1f47b6bf2b 100644
--- a/SU2_PY/pySU2/pySU2ad.i
+++ b/SU2_PY/pySU2/pySU2ad.i
@@ -63,6 +63,9 @@ threads="1"
 #endif
 
 namespace std {
+   %template() vector<bool>;
+   %template() vector<unsigned long>;
+   %template() vector<vector<unsigned long>>;
    %template() vector<int>;
    %template() vector<double>;
    %template() vector<string>;

From 1fdb8374e38a89972b4e81c81c786661083f79dc Mon Sep 17 00:00:00 2001
From: aa-g <aa.gastaldi@pm.me>
Date: Fri, 18 Feb 2022 20:54:24 +0100
Subject: [PATCH 018/656] Remove some code duplication and fix memory leaks

---
 Common/include/drivers/CDriverBase.hpp        |   2 +-
 Common/src/drivers/CDriverBase.cpp            |   6 +-
 .../include/drivers/CDeformationDriver.hpp    |   5 -
 .../drivers/CDiscAdjDeformationDriver.hpp     |  11 +-
 SU2_DEF/src/drivers/CDeformationDriver.cpp    |  46 ++---
 .../src/drivers/CDiscAdjDeformationDriver.cpp | 169 ++++++++++--------
 6 files changed, 123 insertions(+), 116 deletions(-)

diff --git a/Common/include/drivers/CDriverBase.hpp b/Common/include/drivers/CDriverBase.hpp
index 7291411e397..28619eab44e 100644
--- a/Common/include/drivers/CDriverBase.hpp
+++ b/Common/include/drivers/CDriverBase.hpp
@@ -80,7 +80,7 @@ class CDriverBase {
     /*!
      * \brief Destructor of the class.
      */
-    ~CDriverBase(void);
+    virtual ~CDriverBase(void);
     
     /*!
      * \brief A virtual member.
diff --git a/Common/src/drivers/CDriverBase.cpp b/Common/src/drivers/CDriverBase.cpp
index 7d7de27aabd..4ec2d3b1a27 100644
--- a/Common/src/drivers/CDriverBase.cpp
+++ b/Common/src/drivers/CDriverBase.cpp
@@ -38,7 +38,7 @@ CDriverBase::CDriverBase(char* confFile, unsigned short val_nZone, SU2_Comm MPIC
     StopTime(0.0),
     UsedTime(0.0),
     TimeIter(0),
-    nZone()
+    nZone(val_nZone)
 {
     
 }
@@ -53,8 +53,6 @@ void CDriverBase::SetContainers_Null() {
      hierarchy over all zones, multigrid levels, equation sets, and equation
      terms as described in the comments below. ---*/
     
-    nInst                 = nullptr;
-    
     config_container      = nullptr;
     output_container      = nullptr;
     geometry_container    = nullptr;
@@ -74,7 +72,7 @@ void CDriverBase::SetContainers_Null() {
     grid_movement         = new CVolumetricMovement**[nZone] ();
     FFDBox                = new CFreeFormDefBox**[nZone] ();
     
-    nInst                 = new unsigned short[nZone] ();
+    nInst                 = new unsigned short[nZone];
     
     for (iZone = 0; iZone < nZone; iZone++) {
         nInst[iZone] = 1;
diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index 6d64c4b6f2f..329c660bb4c 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -76,11 +76,6 @@ class CDeformationDriver : public CDriverBase {
   void CommunicateMeshDisplacements(void);
 
 protected:
-  // /*!
-  //  * \brief Init_Containers
-  //  */
-  // void SetContainer_Null();
-
   /*!
    * \brief Read in the config and mesh files.
    */
diff --git a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
index 41a1df49b2c..1f1f79b76c1 100644
--- a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
@@ -54,10 +54,7 @@ class CDiscAdjDeformationDriver : public CDriverBase {
 
 protected:
     su2double** Gradient;
-    ofstream Gradient_file;
-    CGeometry ***geometry_container;              /*!< \brief Geometrical definition of the problem. */
-    CSurfaceMovement **surface_movement;
-    CVolumetricMovement **grid_movement;
+    ofstream Gradient_file; 
     
 public:
     /*!
@@ -83,10 +80,6 @@ class CDiscAdjDeformationDriver : public CDriverBase {
     void Postprocessing();
     
 protected:
-    /*!
-     * \brief Init_Containers
-     */
-    void SetContainers_Null();
     
     /*!
      * \brief Read in the config and mesh files.
@@ -140,7 +133,7 @@ class CDiscAdjDeformationDriver : public CDriverBase {
      * \param[in] val_nZone - Number of Zones.
      */
     
-    void SetSensitivity_Files(CGeometry ***geometry, CConfig **config, unsigned short val_nZone);
+    void SetSensitivity_Files(CGeometry ****geometry, CConfig **config, unsigned short val_nZone);
     
     /*!
      * \brief Treatment of derivatives with the Sobolev smoothing solver.
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index c1e6136b970..8bf4b8b9e98 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -51,9 +51,6 @@ CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
     rank = SU2_MPI::GetRank();
     size = SU2_MPI::GetSize();
     
-    /*--- Copy the config filename ---*/
-    strcpy(config_file_name, confFile);
-    
     /*--- Initialize containers --- */
     
     SetContainers_Null();
@@ -102,24 +99,6 @@ CDeformationDriver::~CDeformationDriver(void) {
     
 }
 
-// void CDeformationDriver::SetContainers_Null() {
-//     
-//     /*--- Create pointers to all of the classes that may be used throughout
-//      the SU2_DEF code. In general, the pointers are instantiated down a
-//      hierarchy over all zones as described in the comments below. ---*/
-//     config_container   = new CConfig*[nZone];
-//     output_container   = new COutput*[nZone];
-//     geometry_container = new CGeometry***[nZone];
-//     surface_movement   = new CSurfaceMovement*[nZone];
-//     grid_movement      = new CVolumetricMovement**[nZone];
-//     
-//     solver_container   = new CSolver****[nZone];
-//     numerics_container = new CNumerics**[nZone];
-//     
-
-//     }
-// }
-
 void CDeformationDriver::Input_Preprocessing() {
     
     /*--- Initialize a char to store the zone filename ---*/
@@ -142,6 +121,7 @@ void CDeformationDriver::Input_Preprocessing() {
         
         if (driver_config->GetnConfigFiles() > 0){
             strcpy(zone_file_name, driver_config->GetConfigFilename(iZone).c_str());
+            
             config_container[iZone] = new CConfig(driver_config, zone_file_name, SU2_COMPONENT::SU2_DEF, iZone, nZone, true);
         } else {
             config_container[iZone] = new CConfig(driver_config, config_file_name, SU2_COMPONENT::SU2_DEF, iZone, nZone, true);
@@ -179,6 +159,7 @@ void CDeformationDriver::Geometrical_Preprocessing() {
         geometry_aux->SetColorGrid_Parallel(config_container[iZone]);
         
         /*--- Build the grid data structures using the ParMETIS coloring. ---*/
+        
         unsigned short nInst_Zone = nInst[iZone];
         unsigned short nMesh = 1;
 
@@ -348,13 +329,13 @@ void CDeformationDriver::Update() {
 
 void CDeformationDriver::Update_Legacy() {
 
-    std::cout << "UPDATE LEGACY CALLED" << std::endl; 
-    
     for (iZone = 0; iZone < nZone; iZone++){
         
         if (config_container[iZone]->GetDesign_Variable(0) != NO_DEFORMATION) {
+            unsigned short nInst_Zone = nInst[iZone];
             
             /*--- Definition of the Class for grid movement ---*/
+            grid_movement[iZone] = new CVolumetricMovement* [nInst_Zone] ();
             grid_movement[iZone][INST_0] = new CVolumetricMovement(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
             
             /*--- Save original coordinates to be reused in convexity checking procedure ---*/
@@ -588,10 +569,12 @@ void CDeformationDriver::Postprocessing() {
     if (rank == MASTER_NODE) cout << "Deleted CNumerics container." << endl;
     
     for (iZone = 0; iZone < nZone; iZone++) {
-        delete solver_container[iZone][INST_0][MESH_0][MESH_SOL];
-        delete [] solver_container[iZone][INST_0][MESH_0];
-        delete [] solver_container[iZone][INST_0];
-        delete [] solver_container[iZone];
+        if (solver_container[iZone] != nullptr) {
+            delete solver_container[iZone][INST_0][MESH_0][MESH_SOL];
+            delete [] solver_container[iZone][INST_0][MESH_0];
+            delete [] solver_container[iZone][INST_0];
+            delete [] solver_container[iZone];
+        }
     }
     delete [] solver_container;
     if (rank == MASTER_NODE) cout << "Deleted CSolver container." << endl;
@@ -606,6 +589,12 @@ void CDeformationDriver::Postprocessing() {
     }
     if (rank == MASTER_NODE) cout << "Deleted CGeometry container." << endl;
     
+    for (iZone = 0; iZone < nZone; iZone++) {
+        delete [] FFDBox[iZone];
+    }
+    delete [] FFDBox;
+    if (rank == MASTER_NODE) cout << "Deleted CFreeFormDefBox class." << endl;
+    
     if (surface_movement != nullptr) {
         for (iZone = 0; iZone < nZone; iZone++) {
             delete surface_movement[iZone];
@@ -617,6 +606,7 @@ void CDeformationDriver::Postprocessing() {
     if (grid_movement != nullptr) {
         for (iZone = 0; iZone < nZone; iZone++) {
             delete grid_movement[iZone][INST_0];
+            delete [] grid_movement[iZone];
         }
         delete [] grid_movement;
     }
@@ -638,6 +628,8 @@ void CDeformationDriver::Postprocessing() {
     }
     if (rank == MASTER_NODE) cout << "Deleted COutput class." << endl;
     
+    if (nInst != nullptr) delete [] nInst;
+    
     /*--- Exit the solver cleanly ---*/
     
     if (rank == MASTER_NODE)
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index 63555b249c2..fea679b6f55 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -46,17 +46,6 @@ CDiscAdjDeformationDriver::CDiscAdjDeformationDriver(char* confFile, SU2_Comm MP
     rank = SU2_MPI::GetRank();
     size = SU2_MPI::GetSize();
     
-    /*--- Copy the config filename ---*/
-    strcpy(config_file_name, confFile);
-    
-    /*--- Read the name and format of the input mesh file to get from the mesh
-     file the number of zones and dimensions from the numerical grid (required
-     for variables allocation)  ---*/
-    
-    driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DOT);
-    
-    nZone = driver_config->GetnZone();
-    
     /*--- Initialize containers --- */
     
     SetContainers_Null();
@@ -93,30 +82,16 @@ CDiscAdjDeformationDriver::~CDiscAdjDeformationDriver(void) {
     
 }
 
-void CDiscAdjDeformationDriver::SetContainers_Null() {
-    
-    /*--- Definition of the containers per zones ---*/
-    
-    config_container    = new CConfig*[nZone] ();
-    geometry_container  = new CGeometry**[nZone] ();
-    surface_movement    = new CSurfaceMovement*[nZone] ();
-    grid_movement       = new CVolumetricMovement*[nZone] ();
-    
-    nInst               = new unsigned short[nZone];
-    for (iZone = 0; iZone < nZone; iZone++) {
-        nInst[iZone] = 1;
-    }
-}
-
 void CDiscAdjDeformationDriver::Input_Preprocessing() {
-    
-    if (!config_container[iZone]->GetDiscrete_Adjoint()) {
-         SU2_MPI::Error("The discrete adjoint solver was not specified in the configuration file.", CURRENT_FUNCTION);
-    }
 
     /*--- Initialize a char to store the zone filename ---*/
     char zone_file_name[MAX_STRING_SIZE];
     
+    /*--- Initialize the configuration of the driver ---*/
+    driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DEF);
+    
+    nZone = driver_config->GetnZone();  
+    
     /*--- Loop over all zones to initialize the various classes. In most
      cases, nZone is equal to one. This represents the solution of a partial
      differential equation on a single block, unstructured mesh. ---*/
@@ -135,6 +110,11 @@ void CDiscAdjDeformationDriver::Input_Preprocessing() {
         }
         
         config_container[iZone]->SetMPICommunicator(SU2_MPI::GetComm());
+    
+        if (!config_container[iZone]->GetDiscrete_Adjoint()) {
+            SU2_MPI::Error("The discrete adjoint solver was not specified in the configuration file.", CURRENT_FUNCTION);
+        }
+
     }
     
     /*--- Set the multizone part of the problem. ---*/
@@ -151,6 +131,7 @@ void CDiscAdjDeformationDriver::Geometrical_Preprocessing() {
     /*--- Loop over all zones to initialize the various classes. In most
      cases, nZone is equal to one. This represents the solution of a partial
      differential equation on a single block, unstructured mesh. ---*/
+    unsigned short nMesh = 1;
     
     for (iZone = 0; iZone < nZone; iZone++) {
         
@@ -162,7 +143,7 @@ void CDiscAdjDeformationDriver::Geometrical_Preprocessing() {
         
         nInst[iZone] = config_container[iZone]->GetnTimeInstances();
         
-        geometry_container[iZone] = new CGeometry*[nInst[iZone]];
+        geometry_container[iZone] = new CGeometry**[nInst[iZone]];
         
         for (iInst = 0; iInst < nInst[iZone]; iInst++){
             
@@ -184,13 +165,15 @@ void CDiscAdjDeformationDriver::Geometrical_Preprocessing() {
             if( fem_solver ) {
                 switch( config_container[iZone]->GetKind_FEM_Flow() ) {
                     case DG: {
-                        geometry_container[iZone][iInst] = new CMeshFEM_DG(geometry_aux, config_container[iZone]);
+                        geometry_container[iZone][iInst] = new CGeometry*[nMesh];
+                        geometry_container[iZone][iInst][MESH_0] = new CMeshFEM_DG(geometry_aux, config_container[iZone]);
                         break;
                     }
                 }
             }
             else {
-                geometry_container[iZone][iInst] = new CPhysicalGeometry(geometry_aux, config_container[iZone]);
+                geometry_container[iZone][iInst] = new CGeometry*[nMesh];
+                geometry_container[iZone][iInst][MESH_0] = new CPhysicalGeometry(geometry_aux, config_container[iZone]);
             }
             
             /*--- Deallocate the memory of geometry_aux ---*/
@@ -199,21 +182,21 @@ void CDiscAdjDeformationDriver::Geometrical_Preprocessing() {
             
             /*--- Add the Send/Receive boundaries ---*/
             
-            geometry_container[iZone][iInst]->SetSendReceive(config_container[iZone]);
+            geometry_container[iZone][iInst][MESH_0]->SetSendReceive(config_container[iZone]);
             
             /*--- Add the Send/Receive boundaries ---*/
             
-            geometry_container[iZone][iInst]->SetBoundaries(config_container[iZone]);
+            geometry_container[iZone][iInst][MESH_0]->SetBoundaries(config_container[iZone]);
             
             /*--- Create the vertex structure (required for MPI) ---*/
             
             if (rank == MASTER_NODE) cout << "Identify vertices." << endl;
-            geometry_container[iZone][iInst]->SetVertex(config_container[iZone]);
+            geometry_container[iZone][iInst][MESH_0]->SetVertex(config_container[iZone]);
             
             /*--- Store the global to local mapping after preprocessing. ---*/
             
             if (rank == MASTER_NODE) cout << "Storing a mapping from global to local point index." << endl;
-            geometry_container[iZone][iInst]->SetGlobal_to_Local_Point();
+            geometry_container[iZone][iInst][MESH_0]->SetGlobal_to_Local_Point();
             
             /* Test for a fem solver, because some more work must be done. */
             
@@ -221,7 +204,7 @@ void CDiscAdjDeformationDriver::Geometrical_Preprocessing() {
                 
                 /*--- Carry out a dynamic cast to CMeshFEM_DG, such that it is not needed to
                  define all virtual functions in the base class CGeometry. ---*/
-                CMeshFEM_DG *DGMesh = dynamic_cast<CMeshFEM_DG *>(geometry_container[iZone][iInst]);
+                CMeshFEM_DG *DGMesh = dynamic_cast<CMeshFEM_DG *>(geometry_container[iZone][iInst][MESH_0]);
                 
                 /*--- Determine the standard elements for the volume elements. ---*/
                 if (rank == MASTER_NODE) cout << "Creating standard volume elements." << endl;
@@ -240,35 +223,35 @@ void CDiscAdjDeformationDriver::Geometrical_Preprocessing() {
         /*--- Compute elements surrounding points, points surrounding points ---*/
         
         if (rank == MASTER_NODE) cout << "Setting local point connectivity." << endl;
-        geometry_container[iZone][INST_0]->SetPoint_Connectivity();
+        geometry_container[iZone][INST_0][MESH_0]->SetPoint_Connectivity();
         
         /*--- Check the orientation before computing geometrical quantities ---*/
         
-        geometry_container[iZone][INST_0]->SetBoundVolume();
+        geometry_container[iZone][INST_0][MESH_0]->SetBoundVolume();
         if (config_container[iZone]->GetReorientElements()) {
             if (rank == MASTER_NODE) cout << "Checking the numerical grid orientation of the elements." << endl;
-            geometry_container[iZone][INST_0]->Check_IntElem_Orientation(config_container[iZone]);
-            geometry_container[iZone][INST_0]->Check_BoundElem_Orientation(config_container[iZone]);
+            geometry_container[iZone][INST_0][MESH_0]->Check_IntElem_Orientation(config_container[iZone]);
+            geometry_container[iZone][INST_0][MESH_0]->Check_BoundElem_Orientation(config_container[iZone]);
         }
         
         /*--- Create the edge structure ---*/
         
         if (rank == MASTER_NODE) cout << "Identify edges and vertices." << endl;
-        geometry_container[iZone][INST_0]->SetEdges(); geometry_container[iZone][INST_0]->SetVertex(config_container[iZone]);
+        geometry_container[iZone][INST_0][MESH_0]->SetEdges(); geometry_container[iZone][INST_0][MESH_0]->SetVertex(config_container[iZone]);
         
         /*--- Create the dual control volume structures ---*/
         
         if (rank == MASTER_NODE) cout << "Setting the bound control volume structure." << endl;
-        geometry_container[iZone][INST_0]->SetBoundControlVolume(config_container[ZONE_0], ALLOCATE);
+        geometry_container[iZone][INST_0][MESH_0]->SetBoundControlVolume(config_container[ZONE_0], ALLOCATE);
         
         /*--- Store the global to local mapping after preprocessing. ---*/
         
         if (rank == MASTER_NODE) cout << "Storing a mapping from global to local point index." << endl;
-        geometry_container[iZone][INST_0]->SetGlobal_to_Local_Point();
+        geometry_container[iZone][INST_0][MESH_0]->SetGlobal_to_Local_Point();
         
         /*--- Create the point-to-point MPI communication structures. ---*/
         
-        geometry_container[iZone][INST_0]->PreprocessP2PComms(geometry_container[iZone][INST_0], config_container[iZone]);
+        geometry_container[iZone][INST_0][MESH_0]->PreprocessP2PComms(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
         
     }
 }
@@ -281,20 +264,23 @@ void CDiscAdjDeformationDriver::Run() {
     
     for (iZone = 0; iZone < nZone; iZone++) {
         if (rank == MASTER_NODE) cout << "Reading volume sensitivities at each node from file." << endl;
-        grid_movement[iZone] = new CVolumetricMovement(geometry_container[iZone][INST_0], config_container[iZone]);
+        unsigned short nInst_Zone = nInst[iZone];
+
+        grid_movement[iZone] = new CVolumetricMovement* [nInst_Zone] ();
+        grid_movement[iZone][INST_0] = new CVolumetricMovement(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
         
         /*--- Read in sensitivities from file. ---*/
         if (config_container[ZONE_0]->GetSensitivity_Format() == UNORDERED_ASCII)
-            geometry_container[iZone][INST_0]->ReadUnorderedSensitivity(config_container[iZone]);
+            geometry_container[iZone][INST_0][MESH_0]->ReadUnorderedSensitivity(config_container[iZone]);
         else
-            geometry_container[iZone][INST_0]->SetSensitivity(config_container[iZone]);
+            geometry_container[iZone][INST_0][MESH_0]->SetSensitivity(config_container[iZone]);
         
         if (rank == MASTER_NODE) cout << "\n---------------------- Mesh sensitivity computation ---------------------" << endl;
         if (config_container[iZone]->GetDiscrete_Adjoint() && config_container[iZone]->GetSmoothGradient() &&
             config_container[iZone]->GetSobMode() == ENUM_SOBOLEV_MODUS::MESH_LEVEL) {
-            DerivativeTreatment_MeshSensitivity(geometry_container[iZone][INST_0], config_container[iZone], grid_movement[iZone]);
+            DerivativeTreatment_MeshSensitivity(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], grid_movement[iZone][INST_0]);
         } else {
-            grid_movement[iZone]->SetVolume_Deformation(geometry_container[iZone][INST_0], config_container[iZone], false, true);
+            grid_movement[iZone][INST_0]->SetVolume_Deformation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], false, true);
         }
     }
     
@@ -325,19 +311,19 @@ void CDiscAdjDeformationDriver::Run() {
             
             /*--- Copy coordinates to the surface structure ---*/
             
-            surface_movement[iZone]->CopyBoundary(geometry_container[iZone][INST_0], config_container[iZone]);
+            surface_movement[iZone]->CopyBoundary(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
             
             /*--- If AD mode is enabled we can use it to compute the projection,
              *    otherwise we use finite differences. ---*/
             
             if (config_container[iZone]->GetAD_Mode())
                 if (config_container[iZone]->GetSmoothGradient()) {
-                    DerivativeTreatment_Gradient(geometry_container[iZone][INST_0], config_container[iZone], grid_movement[iZone], surface_movement[iZone] , Gradient);
+                    DerivativeTreatment_Gradient(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], grid_movement[iZone][INST_0], surface_movement[iZone] , Gradient);
                 } else {
-                    SetProjection_AD(geometry_container[iZone][INST_0], config_container[iZone], surface_movement[iZone] , Gradient);
+                    SetProjection_AD(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], surface_movement[iZone] , Gradient);
                 }
         } else {
-            SetProjection_FD(geometry_container[iZone][INST_0], config_container[iZone], surface_movement[iZone] , Gradient);
+            SetProjection_FD(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], surface_movement[iZone] , Gradient);
         }
     } // for iZone
     
@@ -365,19 +351,42 @@ void CDiscAdjDeformationDriver::Postprocessing() {
     if (rank == MASTER_NODE)
         cout << "\n------------------------- Solver Postprocessing -------------------------" << endl;
     
+    for (iZone = 0; iZone < nZone; iZone++) {
+        if (numerics_container[iZone] != nullptr) {
+            delete [] numerics_container[iZone];
+        }
+    }
+    delete [] numerics_container;
+    if (rank == MASTER_NODE) cout << "Deleted CNumerics container." << endl;
+    
+    for (iZone = 0; iZone < nZone; iZone++) {
+        if (solver_container[iZone] != nullptr) {
+            delete [] solver_container[iZone];
+        }
+    }
+    delete [] solver_container;
+    if (rank == MASTER_NODE) cout << "Deleted CSolver container." << endl;
+        
     if (geometry_container != nullptr) {
         for (iZone = 0; iZone < nZone; iZone++) {
             if (geometry_container[iZone] != nullptr) {
                 for (iInst = 0; iInst < nInst[iZone]; iInst++){
-                    delete geometry_container[iZone][iInst];
+                    delete geometry_container[iZone][iInst][MESH_0];
+                    delete [] geometry_container[iZone][iInst];
                 }
-                delete geometry_container[iZone];
+                delete [] geometry_container[iZone];
             }
         }
         delete [] geometry_container;
     }
     if (rank == MASTER_NODE) cout << "Deleted CGeometry container." << endl;
     
+    for (iZone = 0; iZone < nZone; iZone++) {
+        delete [] FFDBox[iZone];
+    }
+    delete [] FFDBox;
+    if (rank == MASTER_NODE) cout << "Deleted CFreeFormDefBox class." << endl;
+    
     if (surface_movement != nullptr) {
         for (iZone = 0; iZone < nZone; iZone++) {
             delete surface_movement[iZone];
@@ -388,7 +397,12 @@ void CDiscAdjDeformationDriver::Postprocessing() {
     
     if (grid_movement != nullptr) {
         for (iZone = 0; iZone < nZone; iZone++) {
-            delete grid_movement[iZone];
+            if (grid_movement[iZone] != nullptr) {
+                for (iInst = 0; iInst < nInst[iZone]; iInst++){
+                    delete grid_movement[iZone][iInst];
+                }
+                delete [] grid_movement[iZone];
+            }
         }
         delete [] grid_movement;
     }
@@ -402,6 +416,21 @@ void CDiscAdjDeformationDriver::Postprocessing() {
     }
     if (rank == MASTER_NODE) cout << "Deleted CConfig container." << endl;
     
+    if (output_container != nullptr) {
+        for (iZone = 0; iZone < nZone; iZone++) {
+            delete output_container[iZone];
+        }
+        delete [] output_container;
+    }
+    if (rank == MASTER_NODE) cout << "Deleted COutput class." << endl;
+    
+    if (nInst != nullptr) delete [] nInst;
+
+    /*--- Exit the solver cleanly ---*/
+    
+    if (rank == MASTER_NODE)
+        cout << endl << "------------------------- Exit Success (SU2_DEF_AD) ------------------------" << endl << endl;
+    
 }
 
 void CDiscAdjDeformationDriver::SetProjection_FD(CGeometry *geometry, CConfig *config, CSurfaceMovement *surface_movement, su2double** Gradient){
@@ -816,7 +845,7 @@ void CDiscAdjDeformationDriver::OutputGradient(su2double** Gradient, CConfig* co
 }
 
 
-void CDiscAdjDeformationDriver::SetSensitivity_Files(CGeometry ***geometry, CConfig **config, unsigned short val_nZone) {
+void CDiscAdjDeformationDriver::SetSensitivity_Files(CGeometry ****geometry, CConfig **config, unsigned short val_nZone) {
     
     unsigned short iMarker,iDim, nDim, nMarker, nVar;
     unsigned long iVertex, iPoint, nPoint, nVertex;
@@ -829,8 +858,8 @@ void CDiscAdjDeformationDriver::SetSensitivity_Files(CGeometry ***geometry, CCon
     
     for (iZone = 0; iZone < val_nZone; iZone++) {
         
-        nPoint = geometry[iZone][INST_0]->GetnPoint();
-        nDim   = geometry[iZone][INST_0]->GetnDim();
+        nPoint = geometry[iZone][INST_0][MESH_0]->GetnPoint();
+        nDim   = geometry[iZone][INST_0][MESH_0]->GetnDim();
         nMarker = config[iZone]->GetnMarker_All();
         nVar = nDim + 1;
         
@@ -850,12 +879,12 @@ void CDiscAdjDeformationDriver::SetSensitivity_Files(CGeometry ***geometry, CCon
         }
         fieldnames.push_back("\"Surface_Sensitivity\"");
         
-        solver = new CBaselineSolver(geometry[iZone][INST_0], config[iZone], nVar+nDim, fieldnames);
+        solver = new CBaselineSolver(geometry[iZone][INST_0][MESH_0], config[iZone], nVar+nDim, fieldnames);
         
         for (iPoint = 0; iPoint < nPoint; iPoint++) {
             for (iDim = 0; iDim < nDim; iDim++) {
-                solver->GetNodes()->SetSolution(iPoint, iDim,      geometry[iZone][INST_0]->nodes->GetCoord(iPoint, iDim));
-                solver->GetNodes()->SetSolution(iPoint, iDim+nDim, geometry[iZone][INST_0]->GetSensitivity(iPoint, iDim));
+                solver->GetNodes()->SetSolution(iPoint, iDim,      geometry[iZone][INST_0][MESH_0]->nodes->GetCoord(iPoint, iDim));
+                solver->GetNodes()->SetSolution(iPoint, iDim+nDim, geometry[iZone][INST_0][MESH_0]->GetSensitivity(iPoint, iDim));
             }
         }
         
@@ -865,18 +894,18 @@ void CDiscAdjDeformationDriver::SetSensitivity_Files(CGeometry ***geometry, CCon
             
             if(config[iZone]->GetSolid_Wall(iMarker) || (config[iZone]->GetMarker_All_DV(iMarker) == YES )) {
                 
-                nVertex = geometry[iZone][INST_0]->GetnVertex(iMarker);
+                nVertex = geometry[iZone][INST_0][MESH_0]->GetnVertex(iMarker);
                 
                 for (iVertex = 0; iVertex < nVertex; iVertex++) {
-                    iPoint = geometry[iZone][INST_0]->vertex[iMarker][iVertex]->GetNode();
-                    Normal = geometry[iZone][INST_0]->vertex[iMarker][iVertex]->GetNormal();
+                    iPoint = geometry[iZone][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+                    Normal = geometry[iZone][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNormal();
                     Prod = 0.0;
                     Area = 0.0;
                     for (iDim = 0; iDim < nDim; iDim++) {
                         
                         /*--- Retrieve the gradient calculated with discrete adjoint method ---*/
                         
-                        SensDim = geometry[iZone][INST_0]->GetSensitivity(iPoint, iDim);
+                        SensDim = geometry[iZone][INST_0][MESH_0]->GetSensitivity(iPoint, iDim);
                         
                         /*--- Calculate scalar product for projection onto the normal vector ---*/
                         
@@ -903,7 +932,7 @@ void CDiscAdjDeformationDriver::SetSensitivity_Files(CGeometry ***geometry, CCon
         
         /*--- Load the data --- */
         
-        output->Load_Data(geometry[iZone][INST_0], config[iZone], &solver);
+        output->Load_Data(geometry[iZone][INST_0][MESH_0], config[iZone], &solver);
         
         /*--- Set the surface filename ---*/
         
@@ -920,7 +949,7 @@ void CDiscAdjDeformationDriver::SetSensitivity_Files(CGeometry ***geometry, CCon
             if (FileFormat[iFile] != OUTPUT_TYPE::RESTART_ASCII &&
                 FileFormat[iFile] != OUTPUT_TYPE::RESTART_BINARY &&
                 FileFormat[iFile] != OUTPUT_TYPE::CSV)
-                output->WriteToFile(config[iZone], geometry[iZone][INST_0], FileFormat[iFile]);
+                output->WriteToFile(config[iZone], geometry[iZone][INST_0][MESH_0], FileFormat[iFile]);
         }
         
         /*--- Free memory ---*/

From 58dd9716b427dcdda705eddd5dea8f1519ac8858 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Sun, 20 Feb 2022 14:37:30 -0800
Subject: [PATCH 019/656] Run clang-format on files

---
 Common/src/drivers/CDriverBase.cpp            |   14 +-
 SU2_CFD/src/drivers/CDriver.cpp               | 7264 ++++++++---------
 SU2_CFD/src/python_wrapper_structure.cpp      | 1034 +--
 SU2_DEF/include/SU2_DEF.hpp                   |    1 -
 .../include/drivers/CDeformationDriver.hpp    |  134 +-
 .../drivers/CDiscAdjDeformationDriver.hpp     |    2 +-
 SU2_DEF/src/SU2_DEF.cpp                       |   79 +-
 SU2_DEF/src/drivers/CDeformationDriver.cpp    |   24 +-
 .../src/drivers/CDiscAdjDeformationDriver.cpp |   16 +-
 9 files changed, 4283 insertions(+), 4285 deletions(-)

diff --git a/Common/src/drivers/CDriverBase.cpp b/Common/src/drivers/CDriverBase.cpp
index 4ec2d3b1a27..98d05d65305 100644
--- a/Common/src/drivers/CDriverBase.cpp
+++ b/Common/src/drivers/CDriverBase.cpp
@@ -33,12 +33,12 @@
 using namespace std;
 
 CDriverBase::CDriverBase(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator): 
-    config_file_name(confFile),
-    StartTime(0.0),
-    StopTime(0.0),
-    UsedTime(0.0),
-    TimeIter(0),
-    nZone(val_nZone)
+config_file_name(confFile),
+StartTime(0.0),
+StopTime(0.0),
+UsedTime(0.0),
+TimeIter(0),
+nZone(val_nZone)
 {
     
 }
@@ -77,7 +77,7 @@ void CDriverBase::SetContainers_Null() {
     for (iZone = 0; iZone < nZone; iZone++) {
         nInst[iZone] = 1;
     }
-
+    
     driver_config         = nullptr;
     driver_output         = nullptr;
 }
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index 53ec9afc51a..082a777d36c 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -107,3889 +107,3889 @@
 #include <fenv.h>
 
 CDriver::CDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator, bool dummy_geo) :
-  CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false), fem_solver(false), dry_run(dummy_geo) {
-
-  /*--- Initialize Medipack (must also be here so it is initialized from python) ---*/
+CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false), fem_solver(false), dry_run(dummy_geo) {
+    
+    /*--- Initialize Medipack (must also be here so it is initialized from python) ---*/
 #ifdef HAVE_MPI
-  #if defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)
+#if defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)
     SU2_MPI::Init_AMPI();
-  #endif
 #endif
-
-  SU2_MPI::SetComm(MPICommunicator);
-
-  rank = SU2_MPI::GetRank();
-  size = SU2_MPI::GetSize();
-
-  /*--- Start timer to track preprocessing for benchmarking. ---*/
-
-  StartTime = SU2_MPI::Wtime();
-
-  /*--- Initialize containers with null --- */
-
-  SetContainers_Null();
-
-  /*--- Preprocessing of the config files. ---*/
-
-  Input_Preprocessing(config_container, driver_config);
-
-  /*--- Retrieve dimension from mesh file ---*/
-
-  nDim = CConfig::GetnDim(config_container[ZONE_0]->GetMesh_FileName(),
-                          config_container[ZONE_0]->GetMesh_FileFormat());
-
-  /*--- Output preprocessing ---*/
-
-  Output_Preprocessing(config_container, driver_config, output_container, driver_output);
-
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-
-    /*--- Read the number of instances for each zone ---*/
-
-    nInst[iZone] = config_container[iZone]->GetnTimeInstances();
-
-    geometry_container[iZone]    = new CGeometry**    [nInst[iZone]] ();
-    iteration_container[iZone]   = new CIteration*    [nInst[iZone]] ();
-    solver_container[iZone]      = new CSolver***     [nInst[iZone]] ();
-    integration_container[iZone] = new CIntegration** [nInst[iZone]] ();
-    numerics_container[iZone]    = new CNumerics****  [nInst[iZone]] ();
-    grid_movement[iZone]         = new CVolumetricMovement* [nInst[iZone]] ();
-
-    /*--- Allocate transfer and interpolation container --- */
-
-    interface_container[iZone]    = new CInterface*[nZone] ();
-    interpolator_container[iZone].resize(nZone);
-
-    for (iInst = 0; iInst < nInst[iZone]; iInst++) {
-
-      config_container[iZone]->SetiInst(iInst);
-
-      /*--- Preprocessing of the geometry for all zones. In this routine, the edge-
-       based data structure is constructed, i.e. node and cell neighbors are
-       identified and linked, face areas and volumes of the dual mesh cells are
-       computed, and the multigrid levels are created using an agglomeration procedure. ---*/
-
-      Geometrical_Preprocessing(config_container[iZone], geometry_container[iZone][iInst], dry_run);
-
+#endif
+    
+    SU2_MPI::SetComm(MPICommunicator);
+    
+    rank = SU2_MPI::GetRank();
+    size = SU2_MPI::GetSize();
+    
+    /*--- Start timer to track preprocessing for benchmarking. ---*/
+    
+    StartTime = SU2_MPI::Wtime();
+    
+    /*--- Initialize containers with null --- */
+    
+    SetContainers_Null();
+    
+    /*--- Preprocessing of the config files. ---*/
+    
+    Input_Preprocessing(config_container, driver_config);
+    
+    /*--- Retrieve dimension from mesh file ---*/
+    
+    nDim = CConfig::GetnDim(config_container[ZONE_0]->GetMesh_FileName(),
+                            config_container[ZONE_0]->GetMesh_FileFormat());
+    
+    /*--- Output preprocessing ---*/
+    
+    Output_Preprocessing(config_container, driver_config, output_container, driver_output);
+    
+    
+    for (iZone = 0; iZone < nZone; iZone++) {
+        
+        /*--- Read the number of instances for each zone ---*/
+        
+        nInst[iZone] = config_container[iZone]->GetnTimeInstances();
+        
+        geometry_container[iZone]    = new CGeometry**    [nInst[iZone]] ();
+        iteration_container[iZone]   = new CIteration*    [nInst[iZone]] ();
+        solver_container[iZone]      = new CSolver***     [nInst[iZone]] ();
+        integration_container[iZone] = new CIntegration** [nInst[iZone]] ();
+        numerics_container[iZone]    = new CNumerics****  [nInst[iZone]] ();
+        grid_movement[iZone]         = new CVolumetricMovement* [nInst[iZone]] ();
+        
+        /*--- Allocate transfer and interpolation container --- */
+        
+        interface_container[iZone]    = new CInterface*[nZone] ();
+        interpolator_container[iZone].resize(nZone);
+        
+        for (iInst = 0; iInst < nInst[iZone]; iInst++) {
+            
+            config_container[iZone]->SetiInst(iInst);
+            
+            /*--- Preprocessing of the geometry for all zones. In this routine, the edge-
+             based data structure is constructed, i.e. node and cell neighbors are
+             identified and linked, face areas and volumes of the dual mesh cells are
+             computed, and the multigrid levels are created using an agglomeration procedure. ---*/
+            
+            Geometrical_Preprocessing(config_container[iZone], geometry_container[iZone][iInst], dry_run);
+            
+        }
     }
-  }
-
-  /*--- Before we proceed with the zone loop we have to compute the wall distances.
+    
+    /*--- Before we proceed with the zone loop we have to compute the wall distances.
      * This computation depends on all zones at once. ---*/
-  if (rank == MASTER_NODE)
-    cout << "Computing wall distances." << endl;
-
-  CGeometry::ComputeWallDistance(config_container, geometry_container);
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-
-    for (iInst = 0; iInst < nInst[iZone]; iInst++){
-
-      /*--- Definition of the solver class: solver_container[#ZONES][#INSTANCES][#MG_GRIDS][#EQ_SYSTEMS].
-       The solver classes are specific to a particular set of governing equations,
-       and they contain the subroutines with instructions for computing each spatial
-       term of the PDE, i.e. loops over the edges to compute convective and viscous
-       fluxes, loops over the nodes to compute source terms, and routines for
-       imposing various boundary condition type for the PDE. ---*/
-
-      Solver_Preprocessing(config_container[iZone], geometry_container[iZone][iInst], solver_container[iZone][iInst]);
-
-      /*--- Definition of the numerical method class:
-       numerics_container[#ZONES][#INSTANCES][#MG_GRIDS][#EQ_SYSTEMS][#EQ_TERMS].
-       The numerics class contains the implementation of the numerical methods for
-       evaluating convective or viscous fluxes between any two nodes in the edge-based
-       data structure (centered, upwind, galerkin), as well as any source terms
-       (piecewise constant reconstruction) evaluated in each dual mesh volume. ---*/
-
-      Numerics_Preprocessing(config_container[iZone], geometry_container[iZone][iInst],
-                             solver_container[iZone][iInst], numerics_container[iZone][iInst]);
-
-      /*--- Definition of the integration class: integration_container[#ZONES][#INSTANCES][#EQ_SYSTEMS].
-       The integration class orchestrates the execution of the spatial integration
-       subroutines contained in the solver class (including multigrid) for computing
-       the residual at each node, R(U) and then integrates the equations to a
-       steady state or time-accurately. ---*/
-
-      Integration_Preprocessing(config_container[iZone], solver_container[iZone][iInst][MESH_0],
-                                integration_container[iZone][iInst]);
-
-      /*--- Instantiate the type of physics iteration to be executed within each zone. For
-       example, one can execute the same physics across multiple zones (mixing plane),
-       different physics in different zones (fluid-structure interaction), or couple multiple
-       systems tightly within a single zone by creating a new iteration class (e.g., RANS). ---*/
-
-      Iteration_Preprocessing(config_container[iZone], iteration_container[iZone][iInst]);
-
-      /*--- Dynamic mesh processing.  ---*/
-
-      DynamicMesh_Preprocessing(config_container[iZone], geometry_container[iZone][iInst], solver_container[iZone][iInst],
-                                iteration_container[iZone][iInst], grid_movement[iZone][iInst], surface_movement[iZone]);
-      /*--- Static mesh processing.  ---*/
-
-      StaticMesh_Preprocessing(config_container[iZone], geometry_container[iZone][iInst]);
-
-    }
-
-  }
-
-  /*! --- Compute the wall distance again to correctly compute the derivatives if we are running direct diff mode --- */
-  if (driver_config->GetDirectDiff() == D_DESIGN){
-    CGeometry::ComputeWallDistance(config_container, geometry_container);
-  }
-
-  /*--- Definition of the interface and transfer conditions between different zones. ---*/
-
-  if (nZone > 1) {
     if (rank == MASTER_NODE)
-      cout << endl <<"------------------- Multizone Interface Preprocessing -------------------" << endl;
-
-    Interface_Preprocessing(config_container, solver_container, geometry_container,
-                            interface_types, interface_container, interpolator_container);
-  }
-
-  if (fsi) {
+        cout << "Computing wall distances." << endl;
+    
+    CGeometry::ComputeWallDistance(config_container, geometry_container);
+    
     for (iZone = 0; iZone < nZone; iZone++) {
-      for (iInst = 0; iInst < nInst[iZone]; iInst++){
-        Solver_Restart(solver_container[iZone][iInst], geometry_container[iZone][iInst],
-                       config_container[iZone], true);
-      }
+        
+        for (iInst = 0; iInst < nInst[iZone]; iInst++){
+            
+            /*--- Definition of the solver class: solver_container[#ZONES][#INSTANCES][#MG_GRIDS][#EQ_SYSTEMS].
+             The solver classes are specific to a particular set of governing equations,
+             and they contain the subroutines with instructions for computing each spatial
+             term of the PDE, i.e. loops over the edges to compute convective and viscous
+             fluxes, loops over the nodes to compute source terms, and routines for
+             imposing various boundary condition type for the PDE. ---*/
+            
+            Solver_Preprocessing(config_container[iZone], geometry_container[iZone][iInst], solver_container[iZone][iInst]);
+            
+            /*--- Definition of the numerical method class:
+             numerics_container[#ZONES][#INSTANCES][#MG_GRIDS][#EQ_SYSTEMS][#EQ_TERMS].
+             The numerics class contains the implementation of the numerical methods for
+             evaluating convective or viscous fluxes between any two nodes in the edge-based
+             data structure (centered, upwind, galerkin), as well as any source terms
+             (piecewise constant reconstruction) evaluated in each dual mesh volume. ---*/
+            
+            Numerics_Preprocessing(config_container[iZone], geometry_container[iZone][iInst],
+                                   solver_container[iZone][iInst], numerics_container[iZone][iInst]);
+            
+            /*--- Definition of the integration class: integration_container[#ZONES][#INSTANCES][#EQ_SYSTEMS].
+             The integration class orchestrates the execution of the spatial integration
+             subroutines contained in the solver class (including multigrid) for computing
+             the residual at each node, R(U) and then integrates the equations to a
+             steady state or time-accurately. ---*/
+            
+            Integration_Preprocessing(config_container[iZone], solver_container[iZone][iInst][MESH_0],
+                                      integration_container[iZone][iInst]);
+            
+            /*--- Instantiate the type of physics iteration to be executed within each zone. For
+             example, one can execute the same physics across multiple zones (mixing plane),
+             different physics in different zones (fluid-structure interaction), or couple multiple
+             systems tightly within a single zone by creating a new iteration class (e.g., RANS). ---*/
+            
+            Iteration_Preprocessing(config_container[iZone], iteration_container[iZone][iInst]);
+            
+            /*--- Dynamic mesh processing.  ---*/
+            
+            DynamicMesh_Preprocessing(config_container[iZone], geometry_container[iZone][iInst], solver_container[iZone][iInst],
+                                      iteration_container[iZone][iInst], grid_movement[iZone][iInst], surface_movement[iZone]);
+            /*--- Static mesh processing.  ---*/
+            
+            StaticMesh_Preprocessing(config_container[iZone], geometry_container[iZone][iInst]);
+            
+        }
+        
     }
-  }
-
-  if (config_container[ZONE_0]->GetBoolTurbomachinery()){
-    if (rank == MASTER_NODE)
-      cout << endl <<"---------------------- Turbomachinery Preprocessing ---------------------" << endl;
-
-    Turbomachinery_Preprocessing(config_container, geometry_container, solver_container, interface_container);
-  }
-
-
-  PythonInterface_Preprocessing(config_container, geometry_container, solver_container);
-
-
-  /*--- Preprocessing time is reported now, but not included in the next compute portion. ---*/
-
-  StopTime = SU2_MPI::Wtime();
-
-  /*--- Compute/print the total time for performance benchmarking. ---*/
-
-  UsedTime = StopTime-StartTime;
-  UsedTimePreproc    = UsedTime;
-  UsedTimeCompute    = 0.0;
-  UsedTimeOutput     = 0.0;
-  IterCount          = 0;
-  OutputCount        = 0;
-  MDOFs              = 0.0;
-  MDOFsDomain        = 0.0;
-  Mpoints            = 0.0;
-  MpointsDomain      = 0.0;
-  for (iZone = 0; iZone < nZone; iZone++) {
-    Mpoints       += geometry_container[iZone][INST_0][MESH_0]->GetGlobal_nPoint()/(1.0e6);
-    MpointsDomain += geometry_container[iZone][INST_0][MESH_0]->GetGlobal_nPointDomain()/(1.0e6);
-    MDOFs         += DOFsPerPoint*geometry_container[iZone][INST_0][MESH_0]->GetGlobal_nPoint()/(1.0e6);
-    MDOFsDomain   += DOFsPerPoint*geometry_container[iZone][INST_0][MESH_0]->GetGlobal_nPointDomain()/(1.0e6);
-  }
-
-  /*--- Reset timer for compute/output performance benchmarking. ---*/
-
-  StopTime = SU2_MPI::Wtime();
-
-  /*--- Compute/print the total time for performance benchmarking. ---*/
-
-  UsedTime = StopTime-StartTime;
-  UsedTimePreproc = UsedTime;
-
-  /*--- Reset timer for compute performance benchmarking. ---*/
-
-  StartTime = SU2_MPI::Wtime();
-
+    
+    /*! --- Compute the wall distance again to correctly compute the derivatives if we are running direct diff mode --- */
+    if (driver_config->GetDirectDiff() == D_DESIGN){
+        CGeometry::ComputeWallDistance(config_container, geometry_container);
+    }
+    
+    /*--- Definition of the interface and transfer conditions between different zones. ---*/
+    
+    if (nZone > 1) {
+        if (rank == MASTER_NODE)
+            cout << endl <<"------------------- Multizone Interface Preprocessing -------------------" << endl;
+        
+        Interface_Preprocessing(config_container, solver_container, geometry_container,
+                                interface_types, interface_container, interpolator_container);
+    }
+    
+    if (fsi) {
+        for (iZone = 0; iZone < nZone; iZone++) {
+            for (iInst = 0; iInst < nInst[iZone]; iInst++){
+                Solver_Restart(solver_container[iZone][iInst], geometry_container[iZone][iInst],
+                               config_container[iZone], true);
+            }
+        }
+    }
+    
+    if (config_container[ZONE_0]->GetBoolTurbomachinery()){
+        if (rank == MASTER_NODE)
+            cout << endl <<"---------------------- Turbomachinery Preprocessing ---------------------" << endl;
+        
+        Turbomachinery_Preprocessing(config_container, geometry_container, solver_container, interface_container);
+    }
+    
+    
+    PythonInterface_Preprocessing(config_container, geometry_container, solver_container);
+    
+    
+    /*--- Preprocessing time is reported now, but not included in the next compute portion. ---*/
+    
+    StopTime = SU2_MPI::Wtime();
+    
+    /*--- Compute/print the total time for performance benchmarking. ---*/
+    
+    UsedTime = StopTime-StartTime;
+    UsedTimePreproc    = UsedTime;
+    UsedTimeCompute    = 0.0;
+    UsedTimeOutput     = 0.0;
+    IterCount          = 0;
+    OutputCount        = 0;
+    MDOFs              = 0.0;
+    MDOFsDomain        = 0.0;
+    Mpoints            = 0.0;
+    MpointsDomain      = 0.0;
+    for (iZone = 0; iZone < nZone; iZone++) {
+        Mpoints       += geometry_container[iZone][INST_0][MESH_0]->GetGlobal_nPoint()/(1.0e6);
+        MpointsDomain += geometry_container[iZone][INST_0][MESH_0]->GetGlobal_nPointDomain()/(1.0e6);
+        MDOFs         += DOFsPerPoint*geometry_container[iZone][INST_0][MESH_0]->GetGlobal_nPoint()/(1.0e6);
+        MDOFsDomain   += DOFsPerPoint*geometry_container[iZone][INST_0][MESH_0]->GetGlobal_nPointDomain()/(1.0e6);
+    }
+    
+    /*--- Reset timer for compute/output performance benchmarking. ---*/
+    
+    StopTime = SU2_MPI::Wtime();
+    
+    /*--- Compute/print the total time for performance benchmarking. ---*/
+    
+    UsedTime = StopTime-StartTime;
+    UsedTimePreproc = UsedTime;
+    
+    /*--- Reset timer for compute performance benchmarking. ---*/
+    
+    StartTime = SU2_MPI::Wtime();
+    
 }
 
 void CDriver::SetContainers_Null(){
-
-  /*--- Create pointers to all of the classes that may be used throughout
-   the SU2_CFD code. In general, the pointers are instantiated down a
-   hierarchy over all zones, multigrid levels, equation sets, and equation
-   terms as described in the comments below. ---*/
-
-  ConvHist_file                  = nullptr;
-  iteration_container            = nullptr;
-  output_container               = nullptr;
-  integration_container          = nullptr;
-  geometry_container             = nullptr;
-  solver_container               = nullptr;
-  numerics_container             = nullptr;
-  config_container               = nullptr;
-  surface_movement               = nullptr;
-  grid_movement                  = nullptr;
-  FFDBox                         = nullptr;
-  interface_container            = nullptr;
-  interface_types                = nullptr;
-  nInst                          = nullptr;
-
-  /*--- Definition and of the containers for all possible zones. ---*/
-
-  iteration_container            = new CIteration**[nZone] ();
-  solver_container               = new CSolver****[nZone] ();
-  integration_container          = new CIntegration***[nZone] ();
-  numerics_container             = new CNumerics*****[nZone] ();
-  config_container               = new CConfig*[nZone] ();
-  geometry_container             = new CGeometry***[nZone] ();
-  surface_movement               = new CSurfaceMovement*[nZone] ();
-  grid_movement                  = new CVolumetricMovement**[nZone] ();
-  FFDBox                         = new CFreeFormDefBox**[nZone] ();
-  interpolator_container.resize(nZone);
-  interface_container            = new CInterface**[nZone] ();
-  interface_types                = new unsigned short*[nZone] ();
-  output_container               = new COutput*[nZone] ();
-  nInst                          = new unsigned short[nZone] ();  // TODO: remove (moved to base class)
-  driver_config                  = nullptr;
-  driver_output                  = nullptr;
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    interface_types[iZone] = new unsigned short[nZone];
-    nInst[iZone] = 1;
-  }
-
-  strcpy(runtime_file_name, "runtime.dat");
-
+    
+    /*--- Create pointers to all of the classes that may be used throughout
+     the SU2_CFD code. In general, the pointers are instantiated down a
+     hierarchy over all zones, multigrid levels, equation sets, and equation
+     terms as described in the comments below. ---*/
+    
+    ConvHist_file                  = nullptr;
+    iteration_container            = nullptr;
+    output_container               = nullptr;
+    integration_container          = nullptr;
+    geometry_container             = nullptr;
+    solver_container               = nullptr;
+    numerics_container             = nullptr;
+    config_container               = nullptr;
+    surface_movement               = nullptr;
+    grid_movement                  = nullptr;
+    FFDBox                         = nullptr;
+    interface_container            = nullptr;
+    interface_types                = nullptr;
+    nInst                          = nullptr;
+    
+    /*--- Definition and of the containers for all possible zones. ---*/
+    
+    iteration_container            = new CIteration**[nZone] ();
+    solver_container               = new CSolver****[nZone] ();
+    integration_container          = new CIntegration***[nZone] ();
+    numerics_container             = new CNumerics*****[nZone] ();
+    config_container               = new CConfig*[nZone] ();
+    geometry_container             = new CGeometry***[nZone] ();
+    surface_movement               = new CSurfaceMovement*[nZone] ();
+    grid_movement                  = new CVolumetricMovement**[nZone] ();
+    FFDBox                         = new CFreeFormDefBox**[nZone] ();
+    interpolator_container.resize(nZone);
+    interface_container            = new CInterface**[nZone] ();
+    interface_types                = new unsigned short*[nZone] ();
+    output_container               = new COutput*[nZone] ();
+    nInst                          = new unsigned short[nZone] ();  // TODO: remove (moved to base class)
+    driver_config                  = nullptr;
+    driver_output                  = nullptr;
+    
+    for (iZone = 0; iZone < nZone; iZone++) {
+        interface_types[iZone] = new unsigned short[nZone];
+        nInst[iZone] = 1;
+    }
+    
+    strcpy(runtime_file_name, "runtime.dat");
+    
 }
 
 
 void CDriver::Postprocessing() {
-
-  const bool wrt_perf = config_container[ZONE_0]->GetWrt_Performance();
-
+    
+    const bool wrt_perf = config_container[ZONE_0]->GetWrt_Performance();
+    
     /*--- Output some information to the console. ---*/
-
-  if (rank == MASTER_NODE) {
-
-    /*--- Print out the number of non-physical points and reconstructions ---*/
-
-    if (config_container[ZONE_0]->GetNonphysical_Points() > 0)
-      cout << "Warning: there are " << config_container[ZONE_0]->GetNonphysical_Points() << " non-physical points in the solution." << endl;
-    if (config_container[ZONE_0]->GetNonphysical_Reconstr() > 0)
-      cout << "Warning: " << config_container[ZONE_0]->GetNonphysical_Reconstr() << " reconstructed states for upwinding are non-physical." << endl;
-  }
-
-  if (rank == MASTER_NODE)
-    cout << endl <<"------------------------- Solver Postprocessing -------------------------" << endl;
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    for (iInst = 0; iInst < nInst[iZone]; iInst++){
-      Numerics_Postprocessing(numerics_container[iZone], solver_container[iZone][iInst],
-          geometry_container[iZone][iInst], config_container[iZone], iInst);
-    }
-    delete [] numerics_container[iZone];
-  }
-  delete [] numerics_container;
-  if (rank == MASTER_NODE) cout << "Deleted CNumerics container." << endl;
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    for (iInst = 0; iInst < nInst[iZone]; iInst++){
-      Integration_Postprocessing(integration_container[iZone],
-          geometry_container[iZone][iInst],
-          config_container[iZone],
-          iInst);
-    }
-    delete [] integration_container[iZone];
-  }
-  delete [] integration_container;
-  if (rank == MASTER_NODE) cout << "Deleted CIntegration container." << endl;
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    for (iInst = 0; iInst < nInst[iZone]; iInst++){
-      Solver_Postprocessing(solver_container[iZone],
-          geometry_container[iZone][iInst],
-          config_container[iZone],
-          iInst);
-    }
-    delete [] solver_container[iZone];
-  }
-  delete [] solver_container;
-  if (rank == MASTER_NODE) cout << "Deleted CSolver container." << endl;
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    for (iInst = 0; iInst < nInst[iZone]; iInst++)
-      delete iteration_container[iZone][iInst];
-    delete [] iteration_container[iZone];
-  }
-  delete [] iteration_container;
-  if (rank == MASTER_NODE) cout << "Deleted CIteration container." << endl;
-
-  if (interface_container != nullptr) {
+    
+    if (rank == MASTER_NODE) {
+        
+        /*--- Print out the number of non-physical points and reconstructions ---*/
+        
+        if (config_container[ZONE_0]->GetNonphysical_Points() > 0)
+            cout << "Warning: there are " << config_container[ZONE_0]->GetNonphysical_Points() << " non-physical points in the solution." << endl;
+        if (config_container[ZONE_0]->GetNonphysical_Reconstr() > 0)
+            cout << "Warning: " << config_container[ZONE_0]->GetNonphysical_Reconstr() << " reconstructed states for upwinding are non-physical." << endl;
+    }
+    
+    if (rank == MASTER_NODE)
+        cout << endl <<"------------------------- Solver Postprocessing -------------------------" << endl;
+    
     for (iZone = 0; iZone < nZone; iZone++) {
-      if (interface_container[iZone] != nullptr) {
-        for (unsigned short jZone = 0; jZone < nZone; jZone++)
-          delete interface_container[iZone][jZone];
-        delete [] interface_container[iZone];
-      }
+        for (iInst = 0; iInst < nInst[iZone]; iInst++){
+            Numerics_Postprocessing(numerics_container[iZone], solver_container[iZone][iInst],
+                                    geometry_container[iZone][iInst], config_container[iZone], iInst);
+        }
+        delete [] numerics_container[iZone];
     }
-    delete [] interface_container;
-    if (rank == MASTER_NODE) cout << "Deleted CInterface container." << endl;
-  }
-
-  if (interface_types != nullptr) {
-    for (iZone = 0; iZone < nZone; iZone++)
-      delete [] interface_types[iZone];
-    delete [] interface_types;
-  }
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    if (geometry_container[iZone] != nullptr) {
-      for (iInst = 0; iInst < nInst[iZone]; iInst++){
-        for (unsigned short iMGlevel = 0; iMGlevel < config_container[iZone]->GetnMGLevels()+1; iMGlevel++)
-          delete geometry_container[iZone][iInst][iMGlevel];
-        delete [] geometry_container[iZone][iInst];
-      }
-      delete [] geometry_container[iZone];
-    }
-  }
-  delete [] geometry_container;
-  if (rank == MASTER_NODE) cout << "Deleted CGeometry container." << endl;
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    delete [] FFDBox[iZone];
-  }
-  delete [] FFDBox;
-  if (rank == MASTER_NODE) cout << "Deleted CFreeFormDefBox class." << endl;
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    delete surface_movement[iZone];
-  }
-  delete [] surface_movement;
-  if (rank == MASTER_NODE) cout << "Deleted CSurfaceMovement class." << endl;
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    for (iInst = 0; iInst < nInst[iZone]; iInst++)
-      delete grid_movement[iZone][iInst];
-    delete [] grid_movement[iZone];
-  }
-  delete [] grid_movement;
-  if (rank == MASTER_NODE) cout << "Deleted CVolumetricMovement class." << endl;
-
-  /*--- Output profiling information ---*/
-  // Note that for now this is called only by a single thread, but all
-  // necessary variables have been made thread private for safety (tick/tock)!!
-
-  config_container[ZONE_0]->SetProfilingCSV();
-  config_container[ZONE_0]->GEMMProfilingCSV();
-
-  /*--- Deallocate config container ---*/
-  if (config_container!= nullptr) {
-    for (iZone = 0; iZone < nZone; iZone++)
-      delete config_container[iZone];
-    delete [] config_container;
-  }
-  delete driver_config;
-  if (rank == MASTER_NODE) cout << "Deleted CConfig container." << endl;
-
-  delete [] nInst;
-  if (rank == MASTER_NODE) cout << "Deleted nInst container." << endl;
-
-  /*--- Deallocate output container ---*/
-
-  if (output_container!= nullptr) {
-    for (iZone = 0; iZone < nZone; iZone++)
-      delete output_container[iZone];
-    delete [] output_container;
-  }
-
-  delete driver_output;
-
-  if (rank == MASTER_NODE) cout << "Deleted COutput class." << endl;
-
-  if (rank == MASTER_NODE) cout << "-------------------------------------------------------------------------" << endl;
-
-
-  /*--- Stop the timer and output the final performance summary. ---*/
-
-  StopTime = SU2_MPI::Wtime();
-
-  UsedTime = StopTime-StartTime;
-  UsedTimeCompute += UsedTime;
-
-  if ((rank == MASTER_NODE) && (wrt_perf)) {
-    su2double TotalTime = UsedTimePreproc + UsedTimeCompute + UsedTimeOutput;
-    cout.precision(6);
-    cout << endl << endl <<"-------------------------- Performance Summary --------------------------" << endl;
-    cout << "Simulation totals:" << endl;
-    cout << setw(25) << "Wall-clock time (hrs):" << setw(12) << (TotalTime)/(60.0*60.0) << " | ";
-    cout << setw(20) << "Core-hrs:" << setw(12) << size*TotalTime/(60.0*60.0) << endl;
-    cout << setw(25) << "Cores:" << setw(12) << size << " | ";
-    cout << setw(20) << "DOFs/point:" << setw(12) << DOFsPerPoint << endl;
-    cout << setw(25) << "Points/core:" << setw(12) << 1.0e6*MpointsDomain/size << " | ";
-    cout << setw(20) << "Ghost points/core:" << setw(12) << 1.0e6*(Mpoints-MpointsDomain)/size << endl;
-    cout << setw(25) << "Ghost/Owned Point Ratio:" << setw(12) << (Mpoints-MpointsDomain)/MpointsDomain << " | " << endl;
-    cout << endl;
-    cout << "Preprocessing phase:" << endl;
-    cout << setw(25) << "Preproc. Time (s):"  << setw(12)<< UsedTimePreproc << " | ";
-    cout << setw(20) << "Preproc. Time (%):" << setw(12)<< ((UsedTimePreproc * 100.0) / (TotalTime)) << endl;
-    cout << endl;
-    cout << "Compute phase:" << endl;
-    cout << setw(25) << "Compute Time (s):"  << setw(12)<< UsedTimeCompute << " | ";
-    cout << setw(20) << "Compute Time (%):" << setw(12)<< ((UsedTimeCompute * 100.0) / (TotalTime)) << endl;
-    cout << setw(25) << "Iteration count:"  << setw(12)<< IterCount << " | ";
-    if (IterCount != 0) {
-      cout << setw(20) << "Avg. s/iter:" << setw(12)<< UsedTimeCompute/IterCount << endl;
-      cout << setw(25) << "Core-s/iter/Mpoints:" << setw(12)<< size*UsedTimeCompute/IterCount/Mpoints << " | ";
-      cout << setw(20) << "Mpoints/s:" << setw(12)<< Mpoints*IterCount/UsedTimeCompute << endl;
-    } else cout << endl;
-    cout << endl;
-    cout << "Output phase:" << endl;
-    cout << setw(25) << "Output Time (s):"  << setw(12)<< UsedTimeOutput << " | ";
-    cout << setw(20) << "Output Time (%):" << setw(12)<< ((UsedTimeOutput * 100.0) / (TotalTime)) << endl;
-    cout << setw(25) << "Output count:" << setw(12)<< OutputCount << " | ";
-    if (OutputCount != 0) {
-      cout << setw(20)<< "Avg. s/output:" << setw(12)<< UsedTimeOutput/OutputCount << endl;
-      if (BandwidthSum > 0) {
-        cout << setw(25)<< "Restart Aggr. BW (MB/s):" << setw(12)<< BandwidthSum/OutputCount << " | ";
-        cout << setw(20)<< "MB/s/core:" << setw(12)<< BandwidthSum/OutputCount/size << endl;
-      }
-    } else cout << endl;
-    cout << "-------------------------------------------------------------------------" << endl;
-    cout << endl;
-  }
-
-  /*--- Exit the solver cleanly ---*/
-
-  if (rank == MASTER_NODE)
-    cout << endl <<"------------------------- Exit Success (SU2_CFD) ------------------------" << endl << endl;
-
-}
-
-
-void CDriver::Input_Preprocessing(CConfig **&config, CConfig *&driver_config) {
-
-  char zone_file_name[MAX_STRING_SIZE];
-
-  /*--- Initialize the configuration of the driver ---*/
-
-  driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_CFD, false);
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-
-    if (rank == MASTER_NODE){
-      cout  << endl << "Parsing config file for zone " << iZone << endl;
+    delete [] numerics_container;
+    if (rank == MASTER_NODE) cout << "Deleted CNumerics container." << endl;
+    
+    for (iZone = 0; iZone < nZone; iZone++) {
+        for (iInst = 0; iInst < nInst[iZone]; iInst++){
+            Integration_Postprocessing(integration_container[iZone],
+                                       geometry_container[iZone][iInst],
+                                       config_container[iZone],
+                                       iInst);
+        }
+        delete [] integration_container[iZone];
     }
-    /*--- Definition of the configuration option class for all zones. In this
-     constructor, the input configuration file is parsed and all options are
-     read and stored. ---*/
-
-    if (driver_config->GetnConfigFiles() > 0){
-
-      strcpy(zone_file_name, driver_config->GetConfigFilename(iZone).c_str());
-      config[iZone] = new CConfig(driver_config, zone_file_name, SU2_COMPONENT::SU2_CFD, iZone, nZone, true);
+    delete [] integration_container;
+    if (rank == MASTER_NODE) cout << "Deleted CIntegration container." << endl;
+    
+    for (iZone = 0; iZone < nZone; iZone++) {
+        for (iInst = 0; iInst < nInst[iZone]; iInst++){
+            Solver_Postprocessing(solver_container[iZone],
+                                  geometry_container[iZone][iInst],
+                                  config_container[iZone],
+                                  iInst);
+        }
+        delete [] solver_container[iZone];
     }
-    else{
-      config[iZone] = new CConfig(driver_config, config_file_name, SU2_COMPONENT::SU2_CFD, iZone, nZone, true);
+    delete [] solver_container;
+    if (rank == MASTER_NODE) cout << "Deleted CSolver container." << endl;
+    
+    for (iZone = 0; iZone < nZone; iZone++) {
+        for (iInst = 0; iInst < nInst[iZone]; iInst++)
+            delete iteration_container[iZone][iInst];
+        delete [] iteration_container[iZone];
+    }
+    delete [] iteration_container;
+    if (rank == MASTER_NODE) cout << "Deleted CIteration container." << endl;
+    
+    if (interface_container != nullptr) {
+        for (iZone = 0; iZone < nZone; iZone++) {
+            if (interface_container[iZone] != nullptr) {
+                for (unsigned short jZone = 0; jZone < nZone; jZone++)
+                    delete interface_container[iZone][jZone];
+                delete [] interface_container[iZone];
+            }
+        }
+        delete [] interface_container;
+        if (rank == MASTER_NODE) cout << "Deleted CInterface container." << endl;
     }
-
-    /*--- Set the MPI communicator ---*/
-
-    config[iZone]->SetMPICommunicator(SU2_MPI::GetComm());
-  }
-
-
-  /*--- Set the multizone part of the problem. ---*/
-  if (driver_config->GetMultizone_Problem()){
+    
+    if (interface_types != nullptr) {
+        for (iZone = 0; iZone < nZone; iZone++)
+            delete [] interface_types[iZone];
+        delete [] interface_types;
+    }
+    
     for (iZone = 0; iZone < nZone; iZone++) {
-      /*--- Set the interface markers for multizone ---*/
-      config_container[iZone]->SetMultizone(driver_config, config_container);
+        if (geometry_container[iZone] != nullptr) {
+            for (iInst = 0; iInst < nInst[iZone]; iInst++){
+                for (unsigned short iMGlevel = 0; iMGlevel < config_container[iZone]->GetnMGLevels()+1; iMGlevel++)
+                    delete geometry_container[iZone][iInst][iMGlevel];
+                delete [] geometry_container[iZone][iInst];
+            }
+            delete [] geometry_container[iZone];
+        }
     }
-  }
-
-  /*--- Determine whether or not the FEM solver is used, which decides the type of
-   *    geometry classes that are instantiated. Only adapted for single-zone problems ---*/
-
-  fem_solver = config_container[ZONE_0]->GetFEMSolver();
-
-  fsi = config_container[ZONE_0]->GetFSI_Simulation();
-}
-
-void CDriver::Geometrical_Preprocessing(CConfig* config, CGeometry **&geometry, bool dummy){
-
-  if (!dummy){
-    if (rank == MASTER_NODE)
-      cout << endl <<"------------------- Geometry Preprocessing ( Zone " << config->GetiZone() <<" ) -------------------" << endl;
-
-    if( fem_solver ) {
-      switch( config->GetKind_FEM_Flow() ) {
-        case DG: {
-            Geometrical_Preprocessing_DGFEM(config, geometry);
-            break;
-          }
-      }
+    delete [] geometry_container;
+    if (rank == MASTER_NODE) cout << "Deleted CGeometry container." << endl;
+    
+    for (iZone = 0; iZone < nZone; iZone++) {
+        delete [] FFDBox[iZone];
+    }
+    delete [] FFDBox;
+    if (rank == MASTER_NODE) cout << "Deleted CFreeFormDefBox class." << endl;
+    
+    for (iZone = 0; iZone < nZone; iZone++) {
+        delete surface_movement[iZone];
     }
-    else {
-      Geometrical_Preprocessing_FVM(config, geometry);
+    delete [] surface_movement;
+    if (rank == MASTER_NODE) cout << "Deleted CSurfaceMovement class." << endl;
+    
+    for (iZone = 0; iZone < nZone; iZone++) {
+        for (iInst = 0; iInst < nInst[iZone]; iInst++)
+            delete grid_movement[iZone][iInst];
+        delete [] grid_movement[iZone];
+    }
+    delete [] grid_movement;
+    if (rank == MASTER_NODE) cout << "Deleted CVolumetricMovement class." << endl;
+    
+    /*--- Output profiling information ---*/
+    // Note that for now this is called only by a single thread, but all
+    // necessary variables have been made thread private for safety (tick/tock)!!
+    
+    config_container[ZONE_0]->SetProfilingCSV();
+    config_container[ZONE_0]->GEMMProfilingCSV();
+    
+    /*--- Deallocate config container ---*/
+    if (config_container!= nullptr) {
+        for (iZone = 0; iZone < nZone; iZone++)
+            delete config_container[iZone];
+        delete [] config_container;
+    }
+    delete driver_config;
+    if (rank == MASTER_NODE) cout << "Deleted CConfig container." << endl;
+    
+    delete [] nInst;
+    if (rank == MASTER_NODE) cout << "Deleted nInst container." << endl;
+    
+    /*--- Deallocate output container ---*/
+    
+    if (output_container!= nullptr) {
+        for (iZone = 0; iZone < nZone; iZone++)
+            delete output_container[iZone];
+        delete [] output_container;
+    }
+    
+    delete driver_output;
+    
+    if (rank == MASTER_NODE) cout << "Deleted COutput class." << endl;
+    
+    if (rank == MASTER_NODE) cout << "-------------------------------------------------------------------------" << endl;
+    
+    
+    /*--- Stop the timer and output the final performance summary. ---*/
+    
+    StopTime = SU2_MPI::Wtime();
+    
+    UsedTime = StopTime-StartTime;
+    UsedTimeCompute += UsedTime;
+    
+    if ((rank == MASTER_NODE) && (wrt_perf)) {
+        su2double TotalTime = UsedTimePreproc + UsedTimeCompute + UsedTimeOutput;
+        cout.precision(6);
+        cout << endl << endl <<"-------------------------- Performance Summary --------------------------" << endl;
+        cout << "Simulation totals:" << endl;
+        cout << setw(25) << "Wall-clock time (hrs):" << setw(12) << (TotalTime)/(60.0*60.0) << " | ";
+        cout << setw(20) << "Core-hrs:" << setw(12) << size*TotalTime/(60.0*60.0) << endl;
+        cout << setw(25) << "Cores:" << setw(12) << size << " | ";
+        cout << setw(20) << "DOFs/point:" << setw(12) << DOFsPerPoint << endl;
+        cout << setw(25) << "Points/core:" << setw(12) << 1.0e6*MpointsDomain/size << " | ";
+        cout << setw(20) << "Ghost points/core:" << setw(12) << 1.0e6*(Mpoints-MpointsDomain)/size << endl;
+        cout << setw(25) << "Ghost/Owned Point Ratio:" << setw(12) << (Mpoints-MpointsDomain)/MpointsDomain << " | " << endl;
+        cout << endl;
+        cout << "Preprocessing phase:" << endl;
+        cout << setw(25) << "Preproc. Time (s):"  << setw(12)<< UsedTimePreproc << " | ";
+        cout << setw(20) << "Preproc. Time (%):" << setw(12)<< ((UsedTimePreproc * 100.0) / (TotalTime)) << endl;
+        cout << endl;
+        cout << "Compute phase:" << endl;
+        cout << setw(25) << "Compute Time (s):"  << setw(12)<< UsedTimeCompute << " | ";
+        cout << setw(20) << "Compute Time (%):" << setw(12)<< ((UsedTimeCompute * 100.0) / (TotalTime)) << endl;
+        cout << setw(25) << "Iteration count:"  << setw(12)<< IterCount << " | ";
+        if (IterCount != 0) {
+            cout << setw(20) << "Avg. s/iter:" << setw(12)<< UsedTimeCompute/IterCount << endl;
+            cout << setw(25) << "Core-s/iter/Mpoints:" << setw(12)<< size*UsedTimeCompute/IterCount/Mpoints << " | ";
+            cout << setw(20) << "Mpoints/s:" << setw(12)<< Mpoints*IterCount/UsedTimeCompute << endl;
+        } else cout << endl;
+        cout << endl;
+        cout << "Output phase:" << endl;
+        cout << setw(25) << "Output Time (s):"  << setw(12)<< UsedTimeOutput << " | ";
+        cout << setw(20) << "Output Time (%):" << setw(12)<< ((UsedTimeOutput * 100.0) / (TotalTime)) << endl;
+        cout << setw(25) << "Output count:" << setw(12)<< OutputCount << " | ";
+        if (OutputCount != 0) {
+            cout << setw(20)<< "Avg. s/output:" << setw(12)<< UsedTimeOutput/OutputCount << endl;
+            if (BandwidthSum > 0) {
+                cout << setw(25)<< "Restart Aggr. BW (MB/s):" << setw(12)<< BandwidthSum/OutputCount << " | ";
+                cout << setw(20)<< "MB/s/core:" << setw(12)<< BandwidthSum/OutputCount/size << endl;
+            }
+        } else cout << endl;
+        cout << "-------------------------------------------------------------------------" << endl;
+        cout << endl;
     }
-  } else {
+    
+    /*--- Exit the solver cleanly ---*/
+    
     if (rank == MASTER_NODE)
-      cout << endl <<"-------------------------- Using Dummy Geometry -------------------------" << endl;
+        cout << endl <<"------------------------- Exit Success (SU2_CFD) ------------------------" << endl << endl;
+    
+}
 
-    unsigned short iMGlevel;
 
-    geometry = new CGeometry*[config->GetnMGLevels()+1] ();
+void CDriver::Input_Preprocessing(CConfig **&config, CConfig *&driver_config) {
+    
+    char zone_file_name[MAX_STRING_SIZE];
+    
+    /*--- Initialize the configuration of the driver ---*/
+    
+    driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_CFD, false);
+    
+    for (iZone = 0; iZone < nZone; iZone++) {
+        
+        if (rank == MASTER_NODE){
+            cout  << endl << "Parsing config file for zone " << iZone << endl;
+        }
+        /*--- Definition of the configuration option class for all zones. In this
+         constructor, the input configuration file is parsed and all options are
+         read and stored. ---*/
+        
+        if (driver_config->GetnConfigFiles() > 0){
+            
+            strcpy(zone_file_name, driver_config->GetConfigFilename(iZone).c_str());
+            config[iZone] = new CConfig(driver_config, zone_file_name, SU2_COMPONENT::SU2_CFD, iZone, nZone, true);
+        }
+        else{
+            config[iZone] = new CConfig(driver_config, config_file_name, SU2_COMPONENT::SU2_CFD, iZone, nZone, true);
+        }
+        
+        /*--- Set the MPI communicator ---*/
+        
+        config[iZone]->SetMPICommunicator(SU2_MPI::GetComm());
+    }
+    
+    
+    /*--- Set the multizone part of the problem. ---*/
+    if (driver_config->GetMultizone_Problem()){
+        for (iZone = 0; iZone < nZone; iZone++) {
+            /*--- Set the interface markers for multizone ---*/
+            config_container[iZone]->SetMultizone(driver_config, config_container);
+        }
+    }
+    
+    /*--- Determine whether or not the FEM solver is used, which decides the type of
+     *    geometry classes that are instantiated. Only adapted for single-zone problems ---*/
+    
+    fem_solver = config_container[ZONE_0]->GetFEMSolver();
+    
+    fsi = config_container[ZONE_0]->GetFSI_Simulation();
+}
 
-    if (!fem_solver){
-      for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-        geometry[iMGlevel] = new CDummyGeometry(config);
-      }
+void CDriver::Geometrical_Preprocessing(CConfig* config, CGeometry **&geometry, bool dummy){
+    
+    if (!dummy){
+        if (rank == MASTER_NODE)
+            cout << endl <<"------------------- Geometry Preprocessing ( Zone " << config->GetiZone() <<" ) -------------------" << endl;
+        
+        if( fem_solver ) {
+            switch( config->GetKind_FEM_Flow() ) {
+                case DG: {
+                    Geometrical_Preprocessing_DGFEM(config, geometry);
+                    break;
+                }
+            }
+        }
+        else {
+            Geometrical_Preprocessing_FVM(config, geometry);
+        }
     } else {
-      geometry[MESH_0] = new CDummyMeshFEM_DG(config);
+        if (rank == MASTER_NODE)
+            cout << endl <<"-------------------------- Using Dummy Geometry -------------------------" << endl;
+        
+        unsigned short iMGlevel;
+        
+        geometry = new CGeometry*[config->GetnMGLevels()+1] ();
+        
+        if (!fem_solver){
+            for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                geometry[iMGlevel] = new CDummyGeometry(config);
+            }
+        } else {
+            geometry[MESH_0] = new CDummyMeshFEM_DG(config);
+        }
+        
+        nDim = geometry[MESH_0]->GetnDim();
     }
-
-    nDim = geometry[MESH_0]->GetnDim();
-  }
-
-  /*--- Computation of positive surface area in the z-plane which is used for
+    
+    /*--- Computation of positive surface area in the z-plane which is used for
      the calculation of force coefficient (non-dimensionalization). ---*/
-
-  geometry[MESH_0]->SetPositive_ZArea(config);
-
-  /*--- Set the actuator disk boundary conditions, if necessary. ---*/
-
-  for (iMesh = 0; iMesh <= config->GetnMGLevels(); iMesh++) {
-    geometry[iMesh]->MatchActuator_Disk(config);
-  }
-
-  /*--- If we have any periodic markers in this calculation, we must
-       match the periodic points found on both sides of the periodic BC.
-       Note that the current implementation requires a 1-to-1 matching of
-       periodic points on the pair of periodic faces after the translation
-       or rotation is taken into account. ---*/
-
-  if ((config->GetnMarker_Periodic() != 0) && !fem_solver) {
+    
+    geometry[MESH_0]->SetPositive_ZArea(config);
+    
+    /*--- Set the actuator disk boundary conditions, if necessary. ---*/
+    
     for (iMesh = 0; iMesh <= config->GetnMGLevels(); iMesh++) {
-
-      /*--- Note that we loop over pairs of periodic markers individually
-           so that repeated nodes on adjacent periodic faces are properly
-           accounted for in multiple places. ---*/
-
-      for (unsigned short iPeriodic = 1; iPeriodic <= config->GetnMarker_Periodic()/2; iPeriodic++) {
-        geometry[iMesh]->MatchPeriodic(config, iPeriodic);
-      }
-
-      /*--- For Streamwise Periodic flow, find a unique reference node on the dedicated inlet marker. ---*/
-      if (config->GetKind_Streamwise_Periodic() != ENUM_STREAMWISE_PERIODIC::NONE)
-        geometry[iMesh]->FindUniqueNode_PeriodicBound(config);
-
-      /*--- Initialize the communication framework for the periodic BCs. ---*/
-      geometry[iMesh]->PreprocessPeriodicComms(geometry[iMesh], config);
-
-    }
-  }
-
-  /*--- If activated by the compile directive, perform a partition analysis. ---*/
-#if PARTITION
-  if (!dummy){
-    if( fem_solver ) Partition_Analysis_FEM(geometry[MESH_0], config);
-    else Partition_Analysis(geometry[MESH_0], config);
-  }
-#endif
-
-  /*--- Check if Euler & Symmetry markers are straight/plane. This information
-        is used in the Euler & Symmetry boundary routines. ---*/
-  if((config_container[iZone]->GetnMarker_Euler() != 0 ||
-     config_container[iZone]->GetnMarker_SymWall() != 0) &&
-     !fem_solver) {
-
-    if (rank == MASTER_NODE)
-      cout << "Checking if Euler & Symmetry markers are straight/plane:" << endl;
-
-    for (iMesh = 0; iMesh <= config_container[iZone]->GetnMGLevels(); iMesh++)
-      geometry_container[iZone][iInst][iMesh]->ComputeSurf_Straightness(config_container[iZone], (iMesh==MESH_0) );
-
-  }
-
-}
-
-void CDriver::Geometrical_Preprocessing_FVM(CConfig *config, CGeometry **&geometry) {
-
-  unsigned short iZone = config->GetiZone(), iMGlevel;
-  unsigned short requestedMGlevels = config->GetnMGLevels();
-  const bool fea = config->GetStructuralProblem();
-
-  /*--- Definition of the geometry class to store the primal grid in the partitioning process.
-   *    All ranks process the grid and call ParMETIS for partitioning ---*/
-
-  CGeometry *geometry_aux = new CPhysicalGeometry(config, iZone, nZone);
-
-  /*--- Set the dimension --- */
-
-  nDim = geometry_aux->GetnDim();
-
-  /*--- Color the initial grid and set the send-receive domains (ParMETIS) ---*/
-
-  geometry_aux->SetColorGrid_Parallel(config);
-
-  /*--- Allocate the memory of the current domain, and divide the grid
-     between the ranks. ---*/
-
-  geometry = new CGeometry *[config->GetnMGLevels()+1] ();
-
-  /*--- Build the grid data structures using the ParMETIS coloring. ---*/
-
-  geometry[MESH_0] = new CPhysicalGeometry(geometry_aux, config);
-
-  /*--- Deallocate the memory of geometry_aux and solver_aux ---*/
-
-  delete geometry_aux;
-
-  /*--- Add the Send/Receive boundaries ---*/
-  geometry[MESH_0]->SetSendReceive(config);
-
-  /*--- Add the Send/Receive boundaries ---*/
-  geometry[MESH_0]->SetBoundaries(config);
-
-  /*--- Compute elements surrounding points, points surrounding points ---*/
-
-  if (rank == MASTER_NODE) cout << "Setting point connectivity." << endl;
-  geometry[MESH_0]->SetPoint_Connectivity();
-
-  /*--- Renumbering points using Reverse Cuthill McKee ordering ---*/
-
-  if (rank == MASTER_NODE) cout << "Renumbering points (Reverse Cuthill McKee Ordering)." << endl;
-  geometry[MESH_0]->SetRCM_Ordering(config);
-
-  /*--- recompute elements surrounding points, points surrounding points ---*/
-
-  if (rank == MASTER_NODE) cout << "Recomputing point connectivity." << endl;
-  geometry[MESH_0]->SetPoint_Connectivity();
-
-  /*--- Compute elements surrounding elements ---*/
-
-  if (rank == MASTER_NODE) cout << "Setting element connectivity." << endl;
-  geometry[MESH_0]->SetElement_Connectivity();
-
-  /*--- Check the orientation before computing geometrical quantities ---*/
-
-  geometry[MESH_0]->SetBoundVolume();
-  if (config->GetReorientElements()) {
-    if (rank == MASTER_NODE) cout << "Checking the numerical grid orientation." << endl;
-    geometry[MESH_0]->Check_IntElem_Orientation(config);
-    geometry[MESH_0]->Check_BoundElem_Orientation(config);
-  }
-
-  /*--- Create the edge structure ---*/
-
-  if (rank == MASTER_NODE) cout << "Identifying edges and vertices." << endl;
-  geometry[MESH_0]->SetEdges();
-  geometry[MESH_0]->SetVertex(config);
-
-  /*--- Create the control volume structures ---*/
-
-  if (rank == MASTER_NODE) cout << "Setting the control volume structure." << endl;
-  SU2_OMP_PARALLEL {
-    geometry[MESH_0]->SetControlVolume(config, ALLOCATE);
-    geometry[MESH_0]->SetBoundControlVolume(config, ALLOCATE);
-  }
-  END_SU2_OMP_PARALLEL
-
-  /*--- Visualize a dual control volume if requested ---*/
-
-  if ((config->GetVisualize_CV() >= 0) &&
-      (config->GetVisualize_CV() < (long)geometry[MESH_0]->GetGlobal_nPointDomain()))
-    geometry[MESH_0]->VisualizeControlVolume(config);
-
-  /*--- Identify closest normal neighbor ---*/
-
-  if (rank == MASTER_NODE) cout << "Searching for the closest normal neighbors to the surfaces." << endl;
-  geometry[MESH_0]->FindNormal_Neighbor(config);
-
-  /*--- Store the global to local mapping. ---*/
-
-  if (rank == MASTER_NODE) cout << "Storing a mapping from global to local point index." << endl;
-  geometry[MESH_0]->SetGlobal_to_Local_Point();
-
-  /*--- Compute the surface curvature ---*/
-
-  if (!fea) {
-    if (rank == MASTER_NODE) cout << "Compute the surface curvature." << endl;
-    geometry[MESH_0]->ComputeSurf_Curvature(config);
-  }
-
-  /*--- Check for periodicity and disable MG if necessary. ---*/
-
-  if (rank == MASTER_NODE) cout << "Checking for periodicity." << endl;
-  geometry[MESH_0]->Check_Periodicity(config);
-
-  /*--- Compute mesh quality statistics on the fine grid. ---*/
-
-  if (!fea) {
-    if (rank == MASTER_NODE)
-      cout << "Computing mesh quality statistics for the dual control volumes." << endl;
-    geometry[MESH_0]->ComputeMeshQualityStatistics(config);
-  }
-
-  geometry[MESH_0]->SetMGLevel(MESH_0);
-  if ((config->GetnMGLevels() != 0) && (rank == MASTER_NODE))
-    cout << "Setting the multigrid structure." << endl;
-
-  /*--- Loop over all the new grid ---*/
-
-  for (iMGlevel = 1; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-
-    /*--- Create main agglomeration structure ---*/
-
-    geometry[iMGlevel] = new CMultiGridGeometry(geometry[iMGlevel-1], config, iMGlevel);
-
-    /*--- Compute points surrounding points. ---*/
-
-    geometry[iMGlevel]->SetPoint_Connectivity(geometry[iMGlevel-1]);
-
-    /*--- Create the edge structure ---*/
-
-    geometry[iMGlevel]->SetEdges();
-    geometry[iMGlevel]->SetVertex(geometry[iMGlevel-1], config);
-
-    /*--- Create the control volume structures ---*/
-
-    geometry[iMGlevel]->SetControlVolume(geometry[iMGlevel-1], ALLOCATE);
-    geometry[iMGlevel]->SetBoundControlVolume(geometry[iMGlevel-1], ALLOCATE);
-    geometry[iMGlevel]->SetCoord(geometry[iMGlevel-1]);
-
-    /*--- Find closest neighbor to a surface point ---*/
-
-    geometry[iMGlevel]->FindNormal_Neighbor(config);
-
-    /*--- Store our multigrid index. ---*/
-
-    geometry[iMGlevel]->SetMGLevel(iMGlevel);
-
-    /*--- Protect against the situation that we were not able to complete
-       the agglomeration for this level, i.e., there weren't enough points.
-       We need to check if we changed the total number of levels and delete
-       the incomplete CMultiGridGeometry object. ---*/
-
-    if (config->GetnMGLevels() != requestedMGlevels) {
-      delete geometry[iMGlevel];
-      geometry[iMGlevel] = nullptr;
-      break;
-    }
-
-  }
-
-  if (config->GetWrt_MultiGrid()) geometry[MESH_0]->ColorMGLevels(config->GetnMGLevels(), geometry);
-
-  /*--- For unsteady simulations, initialize the grid volumes
-   and coordinates for previous solutions. Loop over all zones/grids ---*/
-
-  if ((config->GetTime_Marching() != TIME_MARCHING::STEADY) && config->GetDynamic_Grid()) {
-    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-
-      /*--- Update cell volume ---*/
-      geometry[iMGlevel]->nodes->SetVolume_n();
-      geometry[iMGlevel]->nodes->SetVolume_nM1();
-
-      if (config->GetGrid_Movement()) {
-        /*--- Update point coordinates ---*/
-        geometry[iMGlevel]->nodes->SetCoord_n();
-        geometry[iMGlevel]->nodes->SetCoord_n1();
-      }
+        geometry[iMesh]->MatchActuator_Disk(config);
+    }
+    
+    /*--- If we have any periodic markers in this calculation, we must
+     match the periodic points found on both sides of the periodic BC.
+     Note that the current implementation requires a 1-to-1 matching of
+     periodic points on the pair of periodic faces after the translation
+     or rotation is taken into account. ---*/
+    
+    if ((config->GetnMarker_Periodic() != 0) && !fem_solver) {
+        for (iMesh = 0; iMesh <= config->GetnMGLevels(); iMesh++) {
+            
+            /*--- Note that we loop over pairs of periodic markers individually
+             so that repeated nodes on adjacent periodic faces are properly
+             accounted for in multiple places. ---*/
+            
+            for (unsigned short iPeriodic = 1; iPeriodic <= config->GetnMarker_Periodic()/2; iPeriodic++) {
+                geometry[iMesh]->MatchPeriodic(config, iPeriodic);
+            }
+            
+            /*--- For Streamwise Periodic flow, find a unique reference node on the dedicated inlet marker. ---*/
+            if (config->GetKind_Streamwise_Periodic() != ENUM_STREAMWISE_PERIODIC::NONE)
+                geometry[iMesh]->FindUniqueNode_PeriodicBound(config);
+            
+            /*--- Initialize the communication framework for the periodic BCs. ---*/
+            geometry[iMesh]->PreprocessPeriodicComms(geometry[iMesh], config);
+            
+        }
     }
-  }
-
-
-  /*--- Create the data structure for MPI point-to-point communications. ---*/
-
-  for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-    geometry[iMGlevel]->PreprocessP2PComms(geometry[iMGlevel], config);
-
-
-  /*--- Perform a few preprocessing routines and communications. ---*/
-
-  for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-
-    /*--- Compute the max length. ---*/
-
-    if (!fea) {
-      if ((rank == MASTER_NODE) && (iMGlevel == MESH_0))
-        cout << "Finding max control volume width." << endl;
-      geometry[iMGlevel]->SetMaxLength(config);
-    }
-
-    /*--- Communicate the number of neighbors. This is needed for
-         some centered schemes and for multigrid in parallel. ---*/
-
-    if ((rank == MASTER_NODE) && (size > SINGLE_NODE) && (iMGlevel == MESH_0))
-      cout << "Communicating number of neighbors." << endl;
-    geometry[iMGlevel]->InitiateComms(geometry[iMGlevel], config, NEIGHBORS);
-    geometry[iMGlevel]->CompleteComms(geometry[iMGlevel], config, NEIGHBORS);
-  }
-
-}
-
-void CDriver::Geometrical_Preprocessing_DGFEM(CConfig* config, CGeometry **&geometry) {
-
-  /*--- Definition of the geometry class to store the primal grid in the partitioning process. ---*/
-  /*--- All ranks process the grid and call ParMETIS for partitioning ---*/
-
-  CGeometry *geometry_aux = new CPhysicalGeometry(config, iZone, nZone);
-
-  /*--- Set the dimension --- */
-
-  nDim = geometry_aux->GetnDim();
-
-  /*--- For the FEM solver with time-accurate local time-stepping, use
-       a dummy solver class to retrieve the initial flow state. ---*/
-
-  CSolver *solver_aux = new CFEM_DG_EulerSolver(config, nDim, MESH_0);
-
-  /*--- Color the initial grid and set the send-receive domains (ParMETIS) ---*/
-
-  geometry_aux->SetColorFEMGrid_Parallel(config);
-
-  /*--- Allocate the memory of the current domain, and divide the grid
-     between the ranks. ---*/
-
-  geometry = new CGeometry *[config->GetnMGLevels()+1] ();
-
-  geometry[MESH_0] = new CMeshFEM_DG(geometry_aux, config);
-
-  /*--- Deallocate the memory of geometry_aux and solver_aux ---*/
-
-  delete geometry_aux;
-  delete solver_aux;
-
-  /*--- Add the Send/Receive boundaries ---*/
-  geometry[MESH_0]->SetSendReceive(config);
-
-  /*--- Add the Send/Receive boundaries ---*/
-  geometry[MESH_0]->SetBoundaries(config);
-
-  /*--- Carry out a dynamic cast to CMeshFEM_DG, such that it is not needed to
-       define all virtual functions in the base class CGeometry. ---*/
-  CMeshFEM_DG *DGMesh = dynamic_cast<CMeshFEM_DG *>(geometry[MESH_0]);
-
-  /*--- Determine the standard elements for the volume elements. ---*/
-  if (rank == MASTER_NODE) cout << "Creating standard volume elements." << endl;
-  DGMesh->CreateStandardVolumeElements(config);
-
-  /*--- Create the face information needed to compute the contour integral
-       for the elements in the Discontinuous Galerkin formulation. ---*/
-  if (rank == MASTER_NODE) cout << "Creating face information." << endl;
-  DGMesh->CreateFaces(config);
-
-  /*--- Compute the metric terms of the volume elements. ---*/
-  if (rank == MASTER_NODE) cout << "Computing metric terms volume elements." << endl;
-  DGMesh->MetricTermsVolumeElements(config);
-
-  /*--- Compute the metric terms of the surface elements. ---*/
-  if (rank == MASTER_NODE) cout << "Computing metric terms surface elements." << endl;
-  DGMesh->MetricTermsSurfaceElements(config);
-
-  /*--- Compute a length scale of the volume elements. ---*/
-  if (rank == MASTER_NODE) cout << "Computing length scale volume elements." << endl;
-  DGMesh->LengthScaleVolumeElements();
-
-  /*--- Compute the coordinates of the integration points. ---*/
-  if (rank == MASTER_NODE) cout << "Computing coordinates of the integration points." << endl;
-  DGMesh->CoordinatesIntegrationPoints();
-
-  /*--- Compute the coordinates of the location of the solution DOFs. This is different
-            from the grid points when a different polynomial degree is used to represent the
-            geometry and solution. ---*/
-  if (rank == MASTER_NODE) cout << "Computing coordinates of the solution DOFs." << endl;
-  DGMesh->CoordinatesSolDOFs();
-
-  /*--- Perform the preprocessing tasks when wall functions are used. ---*/
-  if (rank == MASTER_NODE) cout << "Preprocessing for the wall functions. " << endl;
-  DGMesh->WallFunctionPreprocessing(config);
-
-  /*--- Store the global to local mapping. ---*/
-  if (rank == MASTER_NODE) cout << "Storing a mapping from global to local DOF index." << endl;
-  geometry[MESH_0]->SetGlobal_to_Local_Point();
-
-
-  /*--- Loop to create the coarser grid levels. ---*/
-
-  for(unsigned short iMGlevel=1; iMGlevel<=config->GetnMGLevels(); iMGlevel++) {
-
-    SU2_MPI::Error("Geometrical_Preprocessing_DGFEM: Coarse grid levels not implemented yet.",
-                   CURRENT_FUNCTION);
-  }
-
-}
-
-void CDriver::Solver_Preprocessing(CConfig* config, CGeometry** geometry, CSolver ***&solver) {
-
-  MAIN_SOLVER kindSolver = config->GetKind_Solver();
-
-  if (rank == MASTER_NODE)
-    cout << endl <<"-------------------- Solver Preprocessing ( Zone " << config->GetiZone() <<" ) --------------------" << endl;
-
-  solver = new CSolver**[config->GetnMGLevels()+1] ();
-
-  for (iMesh = 0; iMesh <= config->GetnMGLevels(); iMesh++){
-    solver[iMesh] = CSolverFactory::CreateSolverContainer(kindSolver, config, geometry[iMesh], iMesh);
-  }
-
-  /*--- Count the number of DOFs per solution point. ---*/
-
-  DOFsPerPoint = 0;
-
-  for (unsigned int iSol = 0; iSol < MAX_SOLS; iSol++)
-    if (solver[MESH_0][iSol]) DOFsPerPoint += solver[MESH_0][iSol]->GetnVar();
-
-  /*--- Restart solvers, for FSI the geometry cannot be updated because the interpolation classes
-   * should always use the undeformed mesh (otherwise the results would not be repeatable). ---*/
-
-  if (!fsi) Solver_Restart(solver, geometry, config, true);
-
-  /*--- Set up any necessary inlet profiles ---*/
-
-  Inlet_Preprocessing(solver, geometry, config);
-
-}
-
-void CDriver::Inlet_Preprocessing(CSolver ***solver, CGeometry **geometry,
-                                  CConfig *config) const {
-
-  /*--- Adjust iteration number for unsteady restarts. ---*/
-
-  const bool adjoint = config->GetDiscrete_Adjoint() || config->GetContinuous_Adjoint();
-
-  int val_iter = 0;
-
-  if (config->GetTime_Domain()) {
-    val_iter = adjoint? config->GetUnst_AdjointIter() : config->GetRestart_Iter();
-    val_iter -= 1;
-    if (!adjoint && config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND)
-      val_iter -= 1;
-    if (!adjoint && !config->GetRestart()) val_iter = 0;
-  }
-
-  /*--- Load inlet profile files for any of the active solver containers.
-   Note that these routines fill the fine grid data structures for the markers
-   and restrict values down to all coarser MG levels. ---*/
-
-  if (config->GetInlet_Profile_From_File()) {
-
-    /*--- Use LoadInletProfile() routines for the particular solver. ---*/
-
-    if (rank == MASTER_NODE) {
-      cout << endl;
-      cout << "Reading inlet profile from file: ";
-      cout << config->GetInlet_FileName() << endl;
-    }
-
-    if (solver[MESH_0][FLOW_SOL]) {
-      solver[MESH_0][FLOW_SOL]->LoadInletProfile(geometry, solver, config, val_iter, FLOW_SOL, INLET_FLOW);
-    }
-    if (solver[MESH_0][TURB_SOL]) {
-      solver[MESH_0][TURB_SOL]->LoadInletProfile(geometry, solver, config, val_iter, TURB_SOL, INLET_FLOW);
-    }
-    if (solver[MESH_0][SPECIES_SOL]) {
-      solver[MESH_0][SPECIES_SOL]->LoadInletProfile(geometry, solver, config, val_iter, SPECIES_SOL, INLET_FLOW);
-    }
-
-    /*--- Exit if profiles were requested for a solver that is not available. ---*/
-
-    if (!config->GetFluidProblem()) {
-      SU2_MPI::Error(string("Inlet profile specification via file (C++) has not been \n") +
-                     string("implemented yet for this solver.\n") +
-                     string("Please set SPECIFIED_INLET_PROFILE= NO and try again."), CURRENT_FUNCTION);
-    }
-
-  } else {
-
-    /*--- Uniform inlets or python-customized inlets ---*/
-
-    /* --- Initialize quantities for inlet boundary
-     * This routine does not check if they python wrapper is being used to
-     * set custom boundary conditions.  This is intentional; the
-     * default values for python custom BCs are initialized with the default
-     * values specified in the config (avoiding non physical values) --- */
-
-    for (unsigned short iMesh = 0; iMesh <= config->GetnMGLevels(); iMesh++) {
-      for(unsigned short iMarker=0; iMarker < config->GetnMarker_All(); iMarker++) {
-        if (solver[iMesh][FLOW_SOL]) solver[iMesh][FLOW_SOL]->SetUniformInlet(config, iMarker);
-        if (solver[iMesh][TURB_SOL]) solver[iMesh][TURB_SOL]->SetUniformInlet(config, iMarker);
-        if (solver[iMesh][SPECIES_SOL]) solver[iMesh][SPECIES_SOL]->SetUniformInlet(config, iMarker);
-      }
-    }
-
-  }
-
-}
-
-void CDriver::Solver_Restart(CSolver ***solver, CGeometry **geometry,
-                             CConfig *config, bool update_geo) {
-
-  /*--- Check for restarts and use the LoadRestart() routines. ---*/
-
-  const bool restart = config->GetRestart();
-  const bool restart_flow = config->GetRestart_Flow();
-
-  /*--- Adjust iteration number for unsteady restarts. ---*/
-
-  int val_iter = 0;
-
-  const bool adjoint = (config->GetDiscrete_Adjoint() || config->GetContinuous_Adjoint());
-  const bool time_domain = config->GetTime_Domain();
-  const bool dt_step_2nd = (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND) &&
-                           !config->GetStructuralProblem() && !config->GetFEMSolver() &&
-                           !adjoint && time_domain;
-
-  if (time_domain) {
-    if (adjoint) val_iter = config->GetUnst_AdjointIter() - 1;
-    else val_iter = config->GetRestart_Iter() - 1 - dt_step_2nd;
-  }
-
-  /*--- Restart direct solvers. ---*/
-
-  if (restart || restart_flow) {
-    for (auto iSol = 0u; iSol < MAX_SOLS; ++iSol) {
-      auto sol = solver[MESH_0][iSol];
-      if (sol && !sol->GetAdjoint()) {
-        /*--- Note that the mesh solver always loads the most recent file (and not -2). ---*/
-        SU2_OMP_PARALLEL_(if(sol->GetHasHybridParallel()))
-        sol->LoadRestart(geometry, solver, config, val_iter + (iSol==MESH_SOL && dt_step_2nd), update_geo);
-        END_SU2_OMP_PARALLEL
-      }
-    }
-  }
-
-  /*--- Restart adjoint solvers. ---*/
-
-  if (restart) {
-    if ((config->GetKind_Solver() == MAIN_SOLVER::TEMPLATE_SOLVER) ||
-        (config->GetKind_Solver() == MAIN_SOLVER::ADJ_RANS && !config->GetFrozen_Visc_Cont())) {
-      SU2_MPI::Error("A restart capability has not been implemented yet for this solver.\n"
-                     "Please set RESTART_SOL= NO and try again.", CURRENT_FUNCTION);
-    }
-
-    for (auto iSol = 0u; iSol < MAX_SOLS; ++iSol) {
-      auto sol = solver[MESH_0][iSol];
-      if (sol && sol->GetAdjoint())
-        sol->LoadRestart(geometry, solver, config, val_iter, update_geo);
-    }
-  }
-
-}
-
-void CDriver::Solver_Postprocessing(CSolver ****solver, CGeometry **geometry,
-                                    CConfig *config, unsigned short val_iInst) {
-
-  for (int iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-    for (unsigned int iSol = 0; iSol < MAX_SOLS; iSol++){
-      delete solver[val_iInst][iMGlevel][iSol];
-    }
-    delete [] solver[val_iInst][iMGlevel];
-  }
-  delete [] solver[val_iInst];
-
-  CSolverFactory::ClearSolverMeta();
-
-}
-
-void CDriver::Integration_Preprocessing(CConfig *config, CSolver **solver, CIntegration **&integration) const {
-
-  if (rank == MASTER_NODE)
-    cout << endl <<"----------------- Integration Preprocessing ( Zone " << config->GetiZone() <<" ) ------------------" << endl;
-
-  MAIN_SOLVER kindMainSolver = config->GetKind_Solver();
-
-  integration = CIntegrationFactory::CreateIntegrationContainer(kindMainSolver, solver);
-
-}
-
-void CDriver::Integration_Postprocessing(CIntegration ***integration, CGeometry **geometry, CConfig *config, unsigned short val_iInst) {
-
-  for (unsigned int iSol = 0; iSol < MAX_SOLS; iSol++){
-    delete integration[val_iInst][iSol];
-  }
-
-  delete [] integration[val_iInst];
-
-}
-
-template <class Indices>
-void CDriver::InstantiateTurbulentNumerics(unsigned short nVar_Turb, int offset, const CConfig *config,
-                                           const CSolver* turb_solver, CNumerics ****&numerics) const {
-  const int conv_term = CONV_TERM + offset;
-  const int visc_term = VISC_TERM + offset;
-
-  const int source_first_term = SOURCE_FIRST_TERM + offset;
-  const int source_second_term = SOURCE_SECOND_TERM + offset;
-
-  const int conv_bound_term = CONV_BOUND_TERM + offset;
-  const int visc_bound_term = VISC_BOUND_TERM + offset;
-
-  bool spalart_allmaras, neg_spalart_allmaras, e_spalart_allmaras, comp_spalart_allmaras, e_comp_spalart_allmaras, menter_sst;
-  spalart_allmaras = neg_spalart_allmaras = e_spalart_allmaras = comp_spalart_allmaras = e_comp_spalart_allmaras = menter_sst = false;
-
-  /*--- Assign turbulence model booleans ---*/
-
-  switch (config->GetKind_Turb_Model()) {
-    case TURB_MODEL::NONE:
-      SU2_MPI::Error("No turbulence model selected.", CURRENT_FUNCTION);
-      break;
-    case TURB_MODEL::SA:        spalart_allmaras = true;        break;
-    case TURB_MODEL::SA_NEG:    neg_spalart_allmaras = true;    break;
-    case TURB_MODEL::SA_E:      e_spalart_allmaras = true;      break;
-    case TURB_MODEL::SA_COMP:   comp_spalart_allmaras = true;   break;
-    case TURB_MODEL::SA_E_COMP: e_comp_spalart_allmaras = true; break;
-    case TURB_MODEL::SST:       menter_sst = true;              break;
-    case TURB_MODEL::SST_SUST:  menter_sst = true;              break;
-  }
-
-  /*--- If the Menter SST model is used, store the constants of the model and determine the
-        free stream values of the turbulent kinetic energy and dissipation rate. ---*/
-
-  const su2double *constants = nullptr;
-  su2double kine_Inf = 0.0, omega_Inf = 0.0;
-
-  if (menter_sst) {
-    constants = turb_solver->GetConstants();
-    kine_Inf  = turb_solver->GetTke_Inf();
-    omega_Inf = turb_solver->GetOmega_Inf();
-  }
-
-  /*--- Definition of the convective scheme for each equation and mesh level ---*/
-
-  switch (config->GetKind_ConvNumScheme_Turb()) {
-    case NO_UPWIND:
-      SU2_MPI::Error("Config file is missing the CONV_NUM_METHOD_TURB option.", CURRENT_FUNCTION);
-      break;
-    case SPACE_UPWIND :
-      for (auto iMGlevel = 0u; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-        if (spalart_allmaras || neg_spalart_allmaras || e_spalart_allmaras || comp_spalart_allmaras || e_comp_spalart_allmaras) {
-          numerics[iMGlevel][TURB_SOL][conv_term] = new CUpwSca_TurbSA<Indices>(nDim, nVar_Turb, config);
-        }
-        else if (menter_sst) numerics[iMGlevel][TURB_SOL][conv_term] = new CUpwSca_TurbSST<Indices>(nDim, nVar_Turb, config);
-      }
-      break;
-    default:
-      SU2_MPI::Error("Invalid convective scheme for the turbulence equations.", CURRENT_FUNCTION);
-      break;
-  }
-
-  /*--- Definition of the viscous scheme for each equation and mesh level ---*/
-
-  for (auto iMGlevel = 0u; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-    if (spalart_allmaras || e_spalart_allmaras || comp_spalart_allmaras || e_comp_spalart_allmaras) {
-      numerics[iMGlevel][TURB_SOL][visc_term] = new CAvgGrad_TurbSA<Indices>(nDim, nVar_Turb, true, config);
-    }
-    else if (neg_spalart_allmaras)
-      numerics[iMGlevel][TURB_SOL][visc_term] = new CAvgGrad_TurbSA_Neg<Indices>(nDim, nVar_Turb, true, config);
-    else if (menter_sst)
-      numerics[iMGlevel][TURB_SOL][visc_term] = new CAvgGrad_TurbSST<Indices>(nDim, nVar_Turb, constants, true, config);
-  }
-
-  /*--- Definition of the source term integration scheme for each equation and mesh level ---*/
-
-  for (auto iMGlevel = 0u; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-    auto& turb_source_first_term = numerics[iMGlevel][TURB_SOL][source_first_term];
-
-    if (spalart_allmaras)
-      turb_source_first_term = new CSourcePieceWise_TurbSA<Indices>(nDim, nVar_Turb, config);
-    else if (e_spalart_allmaras)
-      turb_source_first_term = new CSourcePieceWise_TurbSA_E<Indices>(nDim, nVar_Turb, config);
-    else if (comp_spalart_allmaras)
-      turb_source_first_term = new CSourcePieceWise_TurbSA_COMP<Indices>(nDim, nVar_Turb, config);
-    else if (e_comp_spalart_allmaras)
-      turb_source_first_term = new CSourcePieceWise_TurbSA_E_COMP<Indices>(nDim, nVar_Turb, config);
-    else if (neg_spalart_allmaras)
-      turb_source_first_term = new CSourcePieceWise_TurbSA_Neg<Indices>(nDim, nVar_Turb, config);
-    else if (menter_sst)
-      turb_source_first_term = new CSourcePieceWise_TurbSST<Indices>(nDim, nVar_Turb, constants, kine_Inf, omega_Inf,
-                                                                     config);
-
-    numerics[iMGlevel][TURB_SOL][source_second_term] = new CSourceNothing(nDim, nVar_Turb, config);
-  }
-
-  /*--- Definition of the boundary condition method ---*/
-
-  for (auto iMGlevel = 0u; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-    if (spalart_allmaras || e_spalart_allmaras || comp_spalart_allmaras || e_comp_spalart_allmaras) {
-      numerics[iMGlevel][TURB_SOL][conv_bound_term] = new CUpwSca_TurbSA<Indices>(nDim, nVar_Turb, config);
-      numerics[iMGlevel][TURB_SOL][visc_bound_term] = new CAvgGrad_TurbSA<Indices>(nDim, nVar_Turb, false, config);
-    }
-    else if (neg_spalart_allmaras) {
-      numerics[iMGlevel][TURB_SOL][conv_bound_term] = new CUpwSca_TurbSA<Indices>(nDim, nVar_Turb, config);
-      numerics[iMGlevel][TURB_SOL][visc_bound_term] = new CAvgGrad_TurbSA_Neg<Indices>(nDim, nVar_Turb, false, config);
-    }
-    else if (menter_sst) {
-      numerics[iMGlevel][TURB_SOL][conv_bound_term] = new CUpwSca_TurbSST<Indices>(nDim, nVar_Turb, config);
-      numerics[iMGlevel][TURB_SOL][visc_bound_term] = new CAvgGrad_TurbSST<Indices>(nDim, nVar_Turb, constants, false,
-                                                                                    config);
-    }
-  }
-}
-/*--- Explicit instantiation of the template above, needed because it is defined in a cpp file, instead of hpp. ---*/
-template void CDriver::InstantiateTurbulentNumerics<CEulerVariable::CIndices<unsigned short>>(
-    unsigned short, int, const CConfig*, const CSolver*, CNumerics****&) const;
-
-template void CDriver::InstantiateTurbulentNumerics<CIncEulerVariable::CIndices<unsigned short>>(
-    unsigned short, int, const CConfig*, const CSolver*, CNumerics****&) const;
-
-template void CDriver::InstantiateTurbulentNumerics<CNEMOEulerVariable::CIndices<unsigned short>>(
-    unsigned short, int, const CConfig*, const CSolver*, CNumerics****&) const;
-
-template <class Indices>
-void CDriver::InstantiateSpeciesNumerics(unsigned short nVar_Species, int offset, const CConfig *config,
-                                         const CSolver* species_solver, CNumerics ****&numerics) const {
-  const int conv_term = CONV_TERM + offset;
-  const int visc_term = VISC_TERM + offset;
-
-  const int source_first_term = SOURCE_FIRST_TERM + offset;
-  const int source_second_term = SOURCE_SECOND_TERM + offset;
-
-  const int conv_bound_term = CONV_BOUND_TERM + offset;
-  const int visc_bound_term = VISC_BOUND_TERM + offset;
-
-  /*--- Definition of the convective scheme for each equation and mesh level. Also for boundary conditions. ---*/
-
-  switch (config->GetKind_ConvNumScheme_Species()) {
-    case NONE :
-      break;
-    case SPACE_UPWIND :
-      for (auto iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-        numerics[iMGlevel][SPECIES_SOL][conv_term] = new CUpwSca_Species<Indices>(nDim, nVar_Species, config);
-        numerics[iMGlevel][SPECIES_SOL][conv_bound_term] = new CUpwSca_Species<Indices>(nDim, nVar_Species, config);
-      }
-      break;
-    default :
-      SU2_MPI::Error("Invalid convective scheme for the species transport equations. Use SCALAR_UPWIND.", CURRENT_FUNCTION);
-      break;
-  }
-
-  /*--- Definition of the viscous scheme for each equation and mesh level ---*/
-
-  for (auto iMGlevel = 0u; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-    numerics[iMGlevel][SPECIES_SOL][visc_term] = new CAvgGrad_Species<Indices>(nDim, nVar_Species, true, config);
-    numerics[iMGlevel][SPECIES_SOL][visc_bound_term] = new CAvgGrad_Species<Indices>(nDim, nVar_Species, false, config);
-  }
-
-  /*--- Definition of the source term integration scheme for each equation and mesh level ---*/
-
-  for (auto iMGlevel = 0u; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-    if (config->GetAxisymmetric() == YES) {
-      numerics[iMGlevel][SPECIES_SOL][source_first_term] = new CSourceAxisymmetric_Species<Indices>(nDim, nVar_Species, config);
-    }
-    else {
-      numerics[iMGlevel][SPECIES_SOL][source_first_term] = new CSourceNothing(nDim, nVar_Species, config);
-    }
-    numerics[iMGlevel][SPECIES_SOL][source_second_term] = new CSourceNothing(nDim, nVar_Species, config);
-  }
-}
-/*--- Explicit instantiation of the template above, needed because it is defined in a cpp file, instead of hpp. ---*/
-template void CDriver::InstantiateSpeciesNumerics<CEulerVariable::CIndices<unsigned short>>(
-    unsigned short, int, const CConfig*, const CSolver*, CNumerics****&) const;
-
-template void CDriver::InstantiateSpeciesNumerics<CIncEulerVariable::CIndices<unsigned short>>(
-    unsigned short, int, const CConfig*, const CSolver*, CNumerics****&) const;
-
-template void CDriver::InstantiateSpeciesNumerics<CNEMOEulerVariable::CIndices<unsigned short>>(
-    unsigned short, int, const CConfig*, const CSolver*, CNumerics****&) const;
-
-void CDriver::Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***solver, CNumerics ****&numerics) const {
-
-  if (rank == MASTER_NODE)
-    cout << endl <<"------------------- Numerics Preprocessing ( Zone " << config->GetiZone() <<" ) -------------------" << endl;
-
-  unsigned short iMGlevel, iSol,
-
-  nVar_Template         = 0,
-  nVar_Flow             = 0,
-  nVar_NEMO             = 0,
-  nPrimVar_NEMO         = 0,
-  nPrimVarGrad_NEMO     = 0,
-  nVar_Trans            = 0,
-  nVar_Turb             = 0,
-  nVar_Species          = 0,
-  nVar_Adj_Flow         = 0,
-  nVar_Adj_Turb         = 0,
-  nVar_FEM              = 0,
-  nVar_Rad              = 0,
-  nVar_Heat             = 0;
-
-  numerics = new CNumerics***[config->GetnMGLevels()+1] ();
-
-  bool compressible = false;
-  bool incompressible = false;
-  bool ideal_gas = (config->GetKind_FluidModel() == STANDARD_AIR) || (config->GetKind_FluidModel() == IDEAL_GAS);
-  bool roe_low_dissipation = (config->GetKind_RoeLowDiss() != NO_ROELOWDISS);
-
-  /*--- Initialize some useful booleans ---*/
-  bool euler, ns, NEMO_euler, NEMO_ns, turbulent, adj_euler, adj_ns, adj_turb, fem_euler, fem_ns;
-  bool fem, heat, transition, template_solver;
-
-  euler = ns = NEMO_euler = NEMO_ns = turbulent = adj_euler = adj_ns = adj_turb = fem_euler = fem_ns = false;
-  fem = heat = transition = template_solver = false;
-  bool species = false;
-
-  /*--- Assign booleans ---*/
-  switch (config->GetKind_Solver()) {
-    case MAIN_SOLVER::TEMPLATE_SOLVER:
-      template_solver = true; break;
-
-    case MAIN_SOLVER::EULER:
-    case MAIN_SOLVER::DISC_ADJ_EULER:
-      euler = compressible = true; break;
-
-    case MAIN_SOLVER::NAVIER_STOKES:
-    case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES:
-      ns = compressible = true;
-      species = (config->GetKind_Species_Model() != SPECIES_MODEL::NONE); break;
-
-    case MAIN_SOLVER::NEMO_EULER:
-      NEMO_euler = compressible = true; break;
-
-    case MAIN_SOLVER::NEMO_NAVIER_STOKES:
-      NEMO_ns = compressible = true; break;
-
-    case MAIN_SOLVER::RANS:
-    case MAIN_SOLVER::DISC_ADJ_RANS:
-      ns = compressible = turbulent = true;
-      transition = (config->GetKind_Trans_Model() == TURB_TRANS_MODEL::LM);
-      species = config->GetKind_Species_Model() != SPECIES_MODEL::NONE; break;
-
-    case MAIN_SOLVER::INC_EULER:
-    case MAIN_SOLVER::DISC_ADJ_INC_EULER:
-      euler = incompressible = true; break;
-
-    case MAIN_SOLVER::INC_NAVIER_STOKES:
-    case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES:
-      ns = incompressible = true;
-      heat = config->GetWeakly_Coupled_Heat();
-      species = (config->GetKind_Species_Model() != SPECIES_MODEL::NONE); break;
-
-    case MAIN_SOLVER::INC_RANS:
-    case MAIN_SOLVER::DISC_ADJ_INC_RANS:
-      ns = incompressible = turbulent = true;
-      heat = config->GetWeakly_Coupled_Heat();
-      transition = (config->GetKind_Trans_Model() == TURB_TRANS_MODEL::LM);
-      species = (config->GetKind_Species_Model() != SPECIES_MODEL::NONE); break;
-
-    case MAIN_SOLVER::FEM_EULER:
-    case MAIN_SOLVER::DISC_ADJ_FEM_EULER:
-      fem_euler = compressible = true; break;
-
-    case MAIN_SOLVER::FEM_NAVIER_STOKES:
-    case MAIN_SOLVER::DISC_ADJ_FEM_NS:
-      fem_ns = compressible = true; break;
-
-    case MAIN_SOLVER::FEM_RANS:
-    case MAIN_SOLVER::DISC_ADJ_FEM_RANS:
-      fem_ns = compressible = true; break;
-
-    case MAIN_SOLVER::FEM_LES:
-      fem_ns = compressible = true; break;
-
-    case MAIN_SOLVER::HEAT_EQUATION:
-    case MAIN_SOLVER::DISC_ADJ_HEAT:
-      heat = true; break;
-
-    case MAIN_SOLVER::FEM_ELASTICITY:
-    case MAIN_SOLVER::DISC_ADJ_FEM:
-      fem = true; break;
-
-    case MAIN_SOLVER::ADJ_EULER:
-      adj_euler = euler = compressible = true; break;
-
-    case MAIN_SOLVER::ADJ_NAVIER_STOKES:
-      adj_ns = ns = compressible = true;
-      turbulent = (config->GetKind_Turb_Model() != TURB_MODEL::NONE); break;
-
-    case MAIN_SOLVER::ADJ_RANS:
-      adj_ns = ns = compressible = turbulent = true;
-      adj_turb = !config->GetFrozen_Visc_Cont(); break;
-
-    default:
-      break;
-
-  }
-
-  /*--- Number of variables for the template ---*/
-
-  if (template_solver) nVar_Flow = solver[MESH_0][FLOW_SOL]->GetnVar();
-
-  /*--- Number of variables for direct problem ---*/
-
-  if (euler)        nVar_Flow = solver[MESH_0][FLOW_SOL]->GetnVar();
-  if (ns)           nVar_Flow = solver[MESH_0][FLOW_SOL]->GetnVar();
-  if (NEMO_euler)   nVar_NEMO = solver[MESH_0][FLOW_SOL]->GetnVar();
-  if (NEMO_ns)      nVar_NEMO = solver[MESH_0][FLOW_SOL]->GetnVar();
-  if (turbulent)    nVar_Turb = solver[MESH_0][TURB_SOL]->GetnVar();
-  if (transition)   nVar_Trans = solver[MESH_0][TRANS_SOL]->GetnVar();
-  if (species)      nVar_Species = solver[MESH_0][SPECIES_SOL]->GetnVar();
-
-  if (fem_euler)    nVar_Flow = solver[MESH_0][FLOW_SOL]->GetnVar();
-  if (fem_ns)       nVar_Flow = solver[MESH_0][FLOW_SOL]->GetnVar();
-
-  if (fem)          nVar_FEM = solver[MESH_0][FEA_SOL]->GetnVar();
-  if (heat)         nVar_Heat = solver[MESH_0][HEAT_SOL]->GetnVar();
-
-  if (config->AddRadiation()) nVar_Rad = solver[MESH_0][RAD_SOL]->GetnVar();
-
-  /*--- Number of variables for adjoint problem ---*/
-
-  if (adj_euler)    nVar_Adj_Flow = solver[MESH_0][ADJFLOW_SOL]->GetnVar();
-  if (adj_ns)       nVar_Adj_Flow = solver[MESH_0][ADJFLOW_SOL]->GetnVar();
-  if (adj_turb)     nVar_Adj_Turb = solver[MESH_0][ADJTURB_SOL]->GetnVar();
-
-  /*--- Additional Variables required for NEMO solver ---*/
-
-  if (NEMO_euler || NEMO_ns) nPrimVar_NEMO     = solver[MESH_0][FLOW_SOL]->GetnPrimVar();
-  if (NEMO_euler || NEMO_ns) nPrimVarGrad_NEMO = solver[MESH_0][FLOW_SOL]->GetnPrimVarGrad();
-
-  /*--- Definition of the Class for the numerical method:
-    numerics_container[INSTANCE_LEVEL][MESH_LEVEL][EQUATION][EQ_TERM] ---*/
-
-  for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-    numerics[iMGlevel] = new CNumerics** [MAX_SOLS];
-    for (iSol = 0; iSol < MAX_SOLS; iSol++)
-      numerics[iMGlevel][iSol] = new CNumerics* [MAX_TERMS*omp_get_max_threads()]();
-  }
-
-  /*--- Instantiate one numerics object per thread for each required term. ---*/
-
-  for (int thread = 0; thread < omp_get_max_threads(); ++thread)
-  {
-  const int offset = thread * MAX_TERMS;
-
-  const int conv_term = CONV_TERM + offset;
-  const int visc_term = VISC_TERM + offset;
-
-  const int source_first_term = SOURCE_FIRST_TERM + offset;
-  const int source_second_term = SOURCE_SECOND_TERM + offset;
-
-  const int conv_bound_term = CONV_BOUND_TERM + offset;
-  const int visc_bound_term = VISC_BOUND_TERM + offset;
-
-  const int fea_term = FEA_TERM + offset;
-
-  /*--- Solver definition for the template problem ---*/
-  if (template_solver) {
-
-    /*--- Definition of the convective scheme for each equation and mesh level ---*/
-    switch (config->GetKind_ConvNumScheme_Template()) {
-      case SPACE_CENTERED : case SPACE_UPWIND :
-        for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-          numerics[iMGlevel][TEMPLATE_SOL][conv_term] = new CConvective_Template(nDim, nVar_Template, config);
-        break;
-      default:
-        SU2_MPI::Error("Convective scheme not implemented (template_solver).", CURRENT_FUNCTION);
-        break;
-    }
-
-    /*--- Definition of the viscous scheme for each equation and mesh level ---*/
-    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-      numerics[iMGlevel][TEMPLATE_SOL][visc_term] = new CViscous_Template(nDim, nVar_Template, config);
-
-    /*--- Definition of the source term integration scheme for each equation and mesh level ---*/
-    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-      numerics[iMGlevel][TEMPLATE_SOL][source_first_term] = new CSource_Template(nDim, nVar_Template, config);
-
-    /*--- Definition of the boundary condition method ---*/
-    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-      numerics[iMGlevel][TEMPLATE_SOL][conv_bound_term] = new CConvective_Template(nDim, nVar_Template, config);
-    }
-
-  }
-
-  /*--- Solver definition for the Potential, Euler, Navier-Stokes problems ---*/
-  if ((euler) || (ns)) {
-
-    /*--- Definition of the convective scheme for each equation and mesh level ---*/
-    switch (config->GetKind_ConvNumScheme_Flow()) {
-      case NO_CONVECTIVE :
-        SU2_MPI::Error("Config file is missing the CONV_NUM_METHOD_FLOW option.", CURRENT_FUNCTION);
-        break;
-
-      case SPACE_CENTERED :
-        if (compressible) {
-          /*--- "conv_term" is not instantiated as all compressible centered schemes are vectorized. ---*/
-
-          /*--- Definition of the boundary condition method ---*/
-          for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-            numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwRoe_Flow(nDim, nVar_Flow, config, false);
-
-        }
-        if (incompressible) {
-          /*--- Incompressible flow, use preconditioning method ---*/
-          switch (config->GetKind_Centered_Flow()) {
-            case LAX : numerics[MESH_0][FLOW_SOL][conv_term] = new CCentLaxInc_Flow(nDim, nVar_Flow, config); break;
-            case JST : numerics[MESH_0][FLOW_SOL][conv_term] = new CCentJSTInc_Flow(nDim, nVar_Flow, config); break;
-            default:
-              SU2_MPI::Error("Invalid centered scheme or not implemented.\n Currently, only JST and LAX-FRIEDRICH are available for incompressible flows.", CURRENT_FUNCTION);
-              break;
-          }
-          for (iMGlevel = 1; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-            numerics[iMGlevel][FLOW_SOL][conv_term] = new CCentLaxInc_Flow(nDim, nVar_Flow, config);
-
-          /*--- Definition of the boundary condition method ---*/
-          for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-            numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwFDSInc_Flow(nDim, nVar_Flow, config);
-
-        }
-        break;
-      case SPACE_UPWIND :
-        if (compressible) {
-          /*--- Compressible flow ---*/
-          switch (config->GetKind_Upwind_Flow()) {
-            case ROE:
-              if (ideal_gas) {
-
-                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-                  numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwRoe_Flow(nDim, nVar_Flow, config, roe_low_dissipation);
-                  numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwRoe_Flow(nDim, nVar_Flow, config, false);
-                }
-              } else {
-
-                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-                  numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwGeneralRoe_Flow(nDim, nVar_Flow, config);
-                  numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwGeneralRoe_Flow(nDim, nVar_Flow, config);
-                }
-              }
-              break;
-
-            case AUSM:
-              for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-                numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwAUSM_Flow(nDim, nVar_Flow, config);
-                numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwAUSM_Flow(nDim, nVar_Flow, config);
-              }
-              break;
-
-            case AUSMPLUSUP:
-              for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-                numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwAUSMPLUSUP_Flow(nDim, nVar_Flow, config);
-                numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwAUSMPLUSUP_Flow(nDim, nVar_Flow, config);
-              }
-              break;
-
-            case AUSMPLUSUP2:
-              for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-                numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwAUSMPLUSUP2_Flow(nDim, nVar_Flow, config);
-                numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwAUSMPLUSUP2_Flow(nDim, nVar_Flow, config);
-              }
-              break;
-
-            case TURKEL:
-              for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-                numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwTurkel_Flow(nDim, nVar_Flow, config);
-                numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwTurkel_Flow(nDim, nVar_Flow, config);
-              }
-              break;
-
-            case L2ROE:
-              for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-                numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwL2Roe_Flow(nDim, nVar_Flow, config);
-                numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwL2Roe_Flow(nDim, nVar_Flow, config);
-              }
-              break;
-            case LMROE:
-              for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-                numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwLMRoe_Flow(nDim, nVar_Flow, config);
-                numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwLMRoe_Flow(nDim, nVar_Flow, config);
-              }
-              break;
-
-            case SLAU:
-              for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-                numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwSLAU_Flow(nDim, nVar_Flow, config, roe_low_dissipation);
-                numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwSLAU_Flow(nDim, nVar_Flow, config, false);
-              }
-              break;
-
-            case SLAU2:
-              for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-                numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwSLAU2_Flow(nDim, nVar_Flow, config, roe_low_dissipation);
-                numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwSLAU2_Flow(nDim, nVar_Flow, config, false);
-              }
-              break;
-
-            case HLLC:
-              if (ideal_gas) {
-                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-                  numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwHLLC_Flow(nDim, nVar_Flow, config);
-                  numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwHLLC_Flow(nDim, nVar_Flow, config);
-                }
-              }
-              else {
-                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-                  numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwGeneralHLLC_Flow(nDim, nVar_Flow, config);
-                  numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwGeneralHLLC_Flow(nDim, nVar_Flow, config);
-                }
-              }
-              break;
-
-            case MSW:
-              for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-                numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwMSW_Flow(nDim, nVar_Flow, config);
-                numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwMSW_Flow(nDim, nVar_Flow, config);
-              }
-              break;
-
-            case CUSP:
-              for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-                numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwCUSP_Flow(nDim, nVar_Flow, config);
-                numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwCUSP_Flow(nDim, nVar_Flow, config);
-              }
-              break;
-
-            default:
-              SU2_MPI::Error("Invalid upwind scheme or not implemented.", CURRENT_FUNCTION);
-              break;
-          }
-
-        }
-        if (incompressible) {
-          /*--- Incompressible flow, use artificial compressibility method ---*/
-          switch (config->GetKind_Upwind_Flow()) {
-            case FDS:
-              for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-                numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwFDSInc_Flow(nDim, nVar_Flow, config);
-                numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwFDSInc_Flow(nDim, nVar_Flow, config);
-              }
-              break;
-            default:
-              SU2_MPI::Error("Invalid upwind scheme or not implemented.\n Currently, only FDS is available for incompressible flows.", CURRENT_FUNCTION);
-              break;
-          }
-        }
-        break;
-
-      default:
-        SU2_MPI::Error("Invalid convective scheme for the Euler / Navier-Stokes equations.", CURRENT_FUNCTION);
-        break;
-    }
-
-    /*--- Definition of the viscous scheme for each equation and mesh level ---*/
-    if (compressible) {
-      if (ideal_gas) {
-
-        /*--- Compressible flow Ideal gas ---*/
-        numerics[MESH_0][FLOW_SOL][visc_term] = new CAvgGrad_Flow(nDim, nVar_Flow, true, config);
-        for (iMGlevel = 1; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-          numerics[iMGlevel][FLOW_SOL][visc_term] = new CAvgGrad_Flow(nDim, nVar_Flow, false, config);
-
-        /*--- Definition of the boundary condition method ---*/
-        for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-          numerics[iMGlevel][FLOW_SOL][visc_bound_term] = new CAvgGrad_Flow(nDim, nVar_Flow, false, config);
-
-      } else {
-
-        /*--- Compressible flow Real gas ---*/
-        numerics[MESH_0][FLOW_SOL][visc_term] = new CGeneralAvgGrad_Flow(nDim, nVar_Flow, true, config);
-        for (iMGlevel = 1; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-          numerics[iMGlevel][FLOW_SOL][visc_term] = new CGeneralAvgGrad_Flow(nDim, nVar_Flow, false, config);
-
-        /*--- Definition of the boundary condition method ---*/
-        for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-          numerics[iMGlevel][FLOW_SOL][visc_bound_term] = new CGeneralAvgGrad_Flow(nDim, nVar_Flow, false, config);
-
-      }
-    }
-    if (incompressible) {
-      /*--- Incompressible flow, use preconditioning method ---*/
-      numerics[MESH_0][FLOW_SOL][visc_term] = new CAvgGradInc_Flow(nDim, nVar_Flow, true, config);
-      for (iMGlevel = 1; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-        numerics[iMGlevel][FLOW_SOL][visc_term] = new CAvgGradInc_Flow(nDim, nVar_Flow, false, config);
-
-      /*--- Definition of the boundary condition method ---*/
-      for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-        numerics[iMGlevel][FLOW_SOL][visc_bound_term] = new CAvgGradInc_Flow(nDim, nVar_Flow, false, config);
-    }
-
-    /*--- Definition of the source term integration scheme for each equation and mesh level ---*/
-    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-
-      if (config->GetBody_Force() == YES) {
-        if (incompressible)
-          numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceIncBodyForce(nDim, nVar_Flow, config);
-        else
-          numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceBodyForce(nDim, nVar_Flow, config);
-      }
-      else if (incompressible && (config->GetKind_Streamwise_Periodic() != ENUM_STREAMWISE_PERIODIC::NONE)) {
-        numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceIncStreamwise_Periodic(nDim, nVar_Flow, config);
-      }
-      else if (incompressible && (config->GetKind_DensityModel() == INC_DENSITYMODEL::BOUSSINESQ)) {
-        numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceBoussinesq(nDim, nVar_Flow, config);
-      }
-      else if (config->GetRotating_Frame() == YES) {
-        if (incompressible)
-          numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceIncRotatingFrame_Flow(nDim, nVar_Flow, config);
-        else
-        numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceRotatingFrame_Flow(nDim, nVar_Flow, config);
-      }
-      else if (config->GetAxisymmetric() == YES) {
-        if (incompressible)
-          numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceIncAxisymmetric_Flow(nDim, nVar_Flow, config);
-        else if (ideal_gas)
-          numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceAxisymmetric_Flow(nDim, nVar_Flow, config);
-        else
-          numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceGeneralAxisymmetric_Flow(nDim, nVar_Flow, config);
-      }
-      else if (config->GetGravityForce() == YES) {
-        numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceGravity(nDim, nVar_Flow, config);
-      }
-      else if (config->GetWind_Gust() == YES) {
-        numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceWindGust(nDim, nVar_Flow, config);
-      }
-      else {
-        numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceNothing(nDim, nVar_Flow, config);
-      }
-
-      /*--- At the moment it is necessary to have the RHT equation in order to have a volumetric heat source. ---*/
-      if (config->AddRadiation())
-        numerics[iMGlevel][FLOW_SOL][source_second_term] = new CSourceRadiation(nDim, nVar_Flow, config);
-      else if ((incompressible && (config->GetKind_Streamwise_Periodic() != ENUM_STREAMWISE_PERIODIC::NONE)) &&
-               (config->GetEnergy_Equation() && !config->GetStreamwise_Periodic_Temperature()))
-        numerics[iMGlevel][FLOW_SOL][source_second_term] = new CSourceIncStreamwisePeriodic_Outlet(nDim, nVar_Flow, config);
-      else
-        numerics[iMGlevel][FLOW_SOL][source_second_term] = new CSourceNothing(nDim, nVar_Flow, config);
-    }
-
-  }
-
-   /*--- Solver definition for the Potential, Euler, Navier-Stokes NEMO problems ---*/
-
-  if (NEMO_euler || NEMO_ns) {
-
-    /*--- Definition of the convective scheme for each equation and mesh level ---*/
-    switch (config->GetKind_ConvNumScheme_Flow()) {
-      case NO_CONVECTIVE :
-        SU2_MPI::Error("Config file is missing the CONV_NUM_METHOD_FLOW option.", CURRENT_FUNCTION);
-        break;
-
-      case SPACE_CENTERED :
-        if (compressible) {
-          /*--- Compressible flow ---*/
-          switch (config->GetKind_Centered_Flow()) {
-            case LAX : numerics[MESH_0][FLOW_SOL][conv_term] = new CCentLax_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config); break;
-            default:
-            SU2_MPI::Error("Invalid centered scheme or not implemented.", CURRENT_FUNCTION);
-            break;
-          }
-
-          for (iMGlevel = 1; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-            numerics[iMGlevel][FLOW_SOL][conv_term] = new CCentLax_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
-
-          /*--- Definition of the boundary condition method ---*/
-          for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-            numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwRoe_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
-        }
-        break;
-      case SPACE_UPWIND :
-        if (compressible) {
-          /*--- Compressible flow ---*/
-          switch (config->GetKind_Upwind_Flow()) {
-            case ROE:
-              for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-                numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwRoe_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
-                numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwRoe_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
-              }
-              break;
-
-            case AUSM:
-              for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-                numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwAUSM_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
-                numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwAUSM_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
-              }
-              break;
-
-            case AUSMPLUSUP2:
-              for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-                numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwAUSMPLUSUP2_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
-                numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwAUSMPLUSUP2_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
-              }
-              break;
-
-            case MSW:
-              for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-                numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwMSW_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
-                numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwMSW_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
-              }
-              break;
-
-            case AUSMPWPLUS:
-              for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-                numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwAUSMPWplus_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
-                numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwAUSMPWplus_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
-              }
-              break;
-
-            default:
-              SU2_MPI::Error("Invalid upwind scheme or not implemented.", CURRENT_FUNCTION);
-              break;
-          }
-
-        }
-        break;
-
-      default:
-        SU2_MPI::Error("Invalid convective scheme for the NEMO Euler / Navier-Stokes equations.", CURRENT_FUNCTION);
-        break;
+    
+    /*--- If activated by the compile directive, perform a partition analysis. ---*/
+#if PARTITION
+    if (!dummy){
+        if( fem_solver ) Partition_Analysis_FEM(geometry[MESH_0], config);
+        else Partition_Analysis(geometry[MESH_0], config);
     }
-
-    /*--- Definition of the viscous scheme for each equation and mesh level ---*/
-    if (compressible) {
-
-      numerics[MESH_0][FLOW_SOL][visc_term] = new CAvgGradCorrected_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
-      for (iMGlevel = 1; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-        numerics[iMGlevel][FLOW_SOL][visc_term] = new CAvgGrad_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
-
-      /*--- Definition of the boundary condition method ---*/
-      for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-        numerics[iMGlevel][FLOW_SOL][visc_bound_term] = new CAvgGrad_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
+#endif
+    
+    /*--- Check if Euler & Symmetry markers are straight/plane. This information
+     is used in the Euler & Symmetry boundary routines. ---*/
+    if((config_container[iZone]->GetnMarker_Euler() != 0 ||
+        config_container[iZone]->GetnMarker_SymWall() != 0) &&
+       !fem_solver) {
+        
+        if (rank == MASTER_NODE)
+            cout << "Checking if Euler & Symmetry markers are straight/plane:" << endl;
+        
+        for (iMesh = 0; iMesh <= config_container[iZone]->GetnMGLevels(); iMesh++)
+            geometry_container[iZone][iInst][iMesh]->ComputeSurf_Straightness(config_container[iZone], (iMesh==MESH_0) );
+        
     }
+    
+}
 
-    /*--- Definition of the source term integration scheme for each equation and mesh level ---*/
+void CDriver::Geometrical_Preprocessing_FVM(CConfig *config, CGeometry **&geometry) {
+    
+    unsigned short iZone = config->GetiZone(), iMGlevel;
+    unsigned short requestedMGlevels = config->GetnMGLevels();
+    const bool fea = config->GetStructuralProblem();
+    
+    /*--- Definition of the geometry class to store the primal grid in the partitioning process.
+     *    All ranks process the grid and call ParMETIS for partitioning ---*/
+    
+    CGeometry *geometry_aux = new CPhysicalGeometry(config, iZone, nZone);
+    
+    /*--- Set the dimension --- */
+    
+    nDim = geometry_aux->GetnDim();
+    
+    /*--- Color the initial grid and set the send-receive domains (ParMETIS) ---*/
+    
+    geometry_aux->SetColorGrid_Parallel(config);
+    
+    /*--- Allocate the memory of the current domain, and divide the grid
+     between the ranks. ---*/
+    
+    geometry = new CGeometry *[config->GetnMGLevels()+1] ();
+    
+    /*--- Build the grid data structures using the ParMETIS coloring. ---*/
+    
+    geometry[MESH_0] = new CPhysicalGeometry(geometry_aux, config);
+    
+    /*--- Deallocate the memory of geometry_aux and solver_aux ---*/
+    
+    delete geometry_aux;
+    
+    /*--- Add the Send/Receive boundaries ---*/
+    geometry[MESH_0]->SetSendReceive(config);
+    
+    /*--- Add the Send/Receive boundaries ---*/
+    geometry[MESH_0]->SetBoundaries(config);
+    
+    /*--- Compute elements surrounding points, points surrounding points ---*/
+    
+    if (rank == MASTER_NODE) cout << "Setting point connectivity." << endl;
+    geometry[MESH_0]->SetPoint_Connectivity();
+    
+    /*--- Renumbering points using Reverse Cuthill McKee ordering ---*/
+    
+    if (rank == MASTER_NODE) cout << "Renumbering points (Reverse Cuthill McKee Ordering)." << endl;
+    geometry[MESH_0]->SetRCM_Ordering(config);
+    
+    /*--- recompute elements surrounding points, points surrounding points ---*/
+    
+    if (rank == MASTER_NODE) cout << "Recomputing point connectivity." << endl;
+    geometry[MESH_0]->SetPoint_Connectivity();
+    
+    /*--- Compute elements surrounding elements ---*/
+    
+    if (rank == MASTER_NODE) cout << "Setting element connectivity." << endl;
+    geometry[MESH_0]->SetElement_Connectivity();
+    
+    /*--- Check the orientation before computing geometrical quantities ---*/
+    
+    geometry[MESH_0]->SetBoundVolume();
+    if (config->GetReorientElements()) {
+        if (rank == MASTER_NODE) cout << "Checking the numerical grid orientation." << endl;
+        geometry[MESH_0]->Check_IntElem_Orientation(config);
+        geometry[MESH_0]->Check_BoundElem_Orientation(config);
+    }
+    
+    /*--- Create the edge structure ---*/
+    
+    if (rank == MASTER_NODE) cout << "Identifying edges and vertices." << endl;
+    geometry[MESH_0]->SetEdges();
+    geometry[MESH_0]->SetVertex(config);
+    
+    /*--- Create the control volume structures ---*/
+    
+    if (rank == MASTER_NODE) cout << "Setting the control volume structure." << endl;
+    SU2_OMP_PARALLEL {
+        geometry[MESH_0]->SetControlVolume(config, ALLOCATE);
+        geometry[MESH_0]->SetBoundControlVolume(config, ALLOCATE);
+    }
+    END_SU2_OMP_PARALLEL
+    
+    /*--- Visualize a dual control volume if requested ---*/
+    
+    if ((config->GetVisualize_CV() >= 0) &&
+        (config->GetVisualize_CV() < (long)geometry[MESH_0]->GetGlobal_nPointDomain()))
+        geometry[MESH_0]->VisualizeControlVolume(config);
+    
+    /*--- Identify closest normal neighbor ---*/
+    
+    if (rank == MASTER_NODE) cout << "Searching for the closest normal neighbors to the surfaces." << endl;
+    geometry[MESH_0]->FindNormal_Neighbor(config);
+    
+    /*--- Store the global to local mapping. ---*/
+    
+    if (rank == MASTER_NODE) cout << "Storing a mapping from global to local point index." << endl;
+    geometry[MESH_0]->SetGlobal_to_Local_Point();
+    
+    /*--- Compute the surface curvature ---*/
+    
+    if (!fea) {
+        if (rank == MASTER_NODE) cout << "Compute the surface curvature." << endl;
+        geometry[MESH_0]->ComputeSurf_Curvature(config);
+    }
+    
+    /*--- Check for periodicity and disable MG if necessary. ---*/
+    
+    if (rank == MASTER_NODE) cout << "Checking for periodicity." << endl;
+    geometry[MESH_0]->Check_Periodicity(config);
+    
+    /*--- Compute mesh quality statistics on the fine grid. ---*/
+    
+    if (!fea) {
+        if (rank == MASTER_NODE)
+            cout << "Computing mesh quality statistics for the dual control volumes." << endl;
+        geometry[MESH_0]->ComputeMeshQualityStatistics(config);
+    }
+    
+    geometry[MESH_0]->SetMGLevel(MESH_0);
+    if ((config->GetnMGLevels() != 0) && (rank == MASTER_NODE))
+        cout << "Setting the multigrid structure." << endl;
+    
+    /*--- Loop over all the new grid ---*/
+    
+    for (iMGlevel = 1; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+        
+        /*--- Create main agglomeration structure ---*/
+        
+        geometry[iMGlevel] = new CMultiGridGeometry(geometry[iMGlevel-1], config, iMGlevel);
+        
+        /*--- Compute points surrounding points. ---*/
+        
+        geometry[iMGlevel]->SetPoint_Connectivity(geometry[iMGlevel-1]);
+        
+        /*--- Create the edge structure ---*/
+        
+        geometry[iMGlevel]->SetEdges();
+        geometry[iMGlevel]->SetVertex(geometry[iMGlevel-1], config);
+        
+        /*--- Create the control volume structures ---*/
+        
+        geometry[iMGlevel]->SetControlVolume(geometry[iMGlevel-1], ALLOCATE);
+        geometry[iMGlevel]->SetBoundControlVolume(geometry[iMGlevel-1], ALLOCATE);
+        geometry[iMGlevel]->SetCoord(geometry[iMGlevel-1]);
+        
+        /*--- Find closest neighbor to a surface point ---*/
+        
+        geometry[iMGlevel]->FindNormal_Neighbor(config);
+        
+        /*--- Store our multigrid index. ---*/
+        
+        geometry[iMGlevel]->SetMGLevel(iMGlevel);
+        
+        /*--- Protect against the situation that we were not able to complete
+         the agglomeration for this level, i.e., there weren't enough points.
+         We need to check if we changed the total number of levels and delete
+         the incomplete CMultiGridGeometry object. ---*/
+        
+        if (config->GetnMGLevels() != requestedMGlevels) {
+            delete geometry[iMGlevel];
+            geometry[iMGlevel] = nullptr;
+            break;
+        }
+        
+    }
+    
+    if (config->GetWrt_MultiGrid()) geometry[MESH_0]->ColorMGLevels(config->GetnMGLevels(), geometry);
+    
+    /*--- For unsteady simulations, initialize the grid volumes
+     and coordinates for previous solutions. Loop over all zones/grids ---*/
+    
+    if ((config->GetTime_Marching() != TIME_MARCHING::STEADY) && config->GetDynamic_Grid()) {
+        for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+            
+            /*--- Update cell volume ---*/
+            geometry[iMGlevel]->nodes->SetVolume_n();
+            geometry[iMGlevel]->nodes->SetVolume_nM1();
+            
+            if (config->GetGrid_Movement()) {
+                /*--- Update point coordinates ---*/
+                geometry[iMGlevel]->nodes->SetCoord_n();
+                geometry[iMGlevel]->nodes->SetCoord_n1();
+            }
+        }
+    }
+    
+    
+    /*--- Create the data structure for MPI point-to-point communications. ---*/
+    
+    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+        geometry[iMGlevel]->PreprocessP2PComms(geometry[iMGlevel], config);
+    
+    
+    /*--- Perform a few preprocessing routines and communications. ---*/
+    
     for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-
-      numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSource_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
-      numerics[iMGlevel][FLOW_SOL][source_second_term] = new CSourceNothing(nDim, nVar_NEMO, config);
+        
+        /*--- Compute the max length. ---*/
+        
+        if (!fea) {
+            if ((rank == MASTER_NODE) && (iMGlevel == MESH_0))
+                cout << "Finding max control volume width." << endl;
+            geometry[iMGlevel]->SetMaxLength(config);
+        }
+        
+        /*--- Communicate the number of neighbors. This is needed for
+         some centered schemes and for multigrid in parallel. ---*/
+        
+        if ((rank == MASTER_NODE) && (size > SINGLE_NODE) && (iMGlevel == MESH_0))
+            cout << "Communicating number of neighbors." << endl;
+        geometry[iMGlevel]->InitiateComms(geometry[iMGlevel], config, NEIGHBORS);
+        geometry[iMGlevel]->CompleteComms(geometry[iMGlevel], config, NEIGHBORS);
     }
-  }
+    
+}
 
-  /*--- Riemann solver definition for the Euler, Navier-Stokes problems for the FEM discretization. ---*/
-  if ((fem_euler) || (fem_ns)) {
+void CDriver::Geometrical_Preprocessing_DGFEM(CConfig* config, CGeometry **&geometry) {
+    
+    /*--- Definition of the geometry class to store the primal grid in the partitioning process. ---*/
+    /*--- All ranks process the grid and call ParMETIS for partitioning ---*/
+    
+    CGeometry *geometry_aux = new CPhysicalGeometry(config, iZone, nZone);
+    
+    /*--- Set the dimension --- */
+    
+    nDim = geometry_aux->GetnDim();
+    
+    /*--- For the FEM solver with time-accurate local time-stepping, use
+     a dummy solver class to retrieve the initial flow state. ---*/
+    
+    CSolver *solver_aux = new CFEM_DG_EulerSolver(config, nDim, MESH_0);
+    
+    /*--- Color the initial grid and set the send-receive domains (ParMETIS) ---*/
+    
+    geometry_aux->SetColorFEMGrid_Parallel(config);
+    
+    /*--- Allocate the memory of the current domain, and divide the grid
+     between the ranks. ---*/
+    
+    geometry = new CGeometry *[config->GetnMGLevels()+1] ();
+    
+    geometry[MESH_0] = new CMeshFEM_DG(geometry_aux, config);
+    
+    /*--- Deallocate the memory of geometry_aux and solver_aux ---*/
+    
+    delete geometry_aux;
+    delete solver_aux;
+    
+    /*--- Add the Send/Receive boundaries ---*/
+    geometry[MESH_0]->SetSendReceive(config);
+    
+    /*--- Add the Send/Receive boundaries ---*/
+    geometry[MESH_0]->SetBoundaries(config);
+    
+    /*--- Carry out a dynamic cast to CMeshFEM_DG, such that it is not needed to
+     define all virtual functions in the base class CGeometry. ---*/
+    CMeshFEM_DG *DGMesh = dynamic_cast<CMeshFEM_DG *>(geometry[MESH_0]);
+    
+    /*--- Determine the standard elements for the volume elements. ---*/
+    if (rank == MASTER_NODE) cout << "Creating standard volume elements." << endl;
+    DGMesh->CreateStandardVolumeElements(config);
+    
+    /*--- Create the face information needed to compute the contour integral
+     for the elements in the Discontinuous Galerkin formulation. ---*/
+    if (rank == MASTER_NODE) cout << "Creating face information." << endl;
+    DGMesh->CreateFaces(config);
+    
+    /*--- Compute the metric terms of the volume elements. ---*/
+    if (rank == MASTER_NODE) cout << "Computing metric terms volume elements." << endl;
+    DGMesh->MetricTermsVolumeElements(config);
+    
+    /*--- Compute the metric terms of the surface elements. ---*/
+    if (rank == MASTER_NODE) cout << "Computing metric terms surface elements." << endl;
+    DGMesh->MetricTermsSurfaceElements(config);
+    
+    /*--- Compute a length scale of the volume elements. ---*/
+    if (rank == MASTER_NODE) cout << "Computing length scale volume elements." << endl;
+    DGMesh->LengthScaleVolumeElements();
+    
+    /*--- Compute the coordinates of the integration points. ---*/
+    if (rank == MASTER_NODE) cout << "Computing coordinates of the integration points." << endl;
+    DGMesh->CoordinatesIntegrationPoints();
+    
+    /*--- Compute the coordinates of the location of the solution DOFs. This is different
+     from the grid points when a different polynomial degree is used to represent the
+     geometry and solution. ---*/
+    if (rank == MASTER_NODE) cout << "Computing coordinates of the solution DOFs." << endl;
+    DGMesh->CoordinatesSolDOFs();
+    
+    /*--- Perform the preprocessing tasks when wall functions are used. ---*/
+    if (rank == MASTER_NODE) cout << "Preprocessing for the wall functions. " << endl;
+    DGMesh->WallFunctionPreprocessing(config);
+    
+    /*--- Store the global to local mapping. ---*/
+    if (rank == MASTER_NODE) cout << "Storing a mapping from global to local DOF index." << endl;
+    geometry[MESH_0]->SetGlobal_to_Local_Point();
+    
+    
+    /*--- Loop to create the coarser grid levels. ---*/
+    
+    for(unsigned short iMGlevel=1; iMGlevel<=config->GetnMGLevels(); iMGlevel++) {
+        
+        SU2_MPI::Error("Geometrical_Preprocessing_DGFEM: Coarse grid levels not implemented yet.",
+                       CURRENT_FUNCTION);
+    }
+    
+}
 
-    switch (config->GetRiemann_Solver_FEM()) {
-      case ROE:
-      case LAX_FRIEDRICH:
-        /* Hard coded optimized implementation is used in the DG solver. No need to allocate the
-           corresponding entry in numerics. */
-        break;
+void CDriver::Solver_Preprocessing(CConfig* config, CGeometry** geometry, CSolver ***&solver) {
+    
+    MAIN_SOLVER kindSolver = config->GetKind_Solver();
+    
+    if (rank == MASTER_NODE)
+        cout << endl <<"-------------------- Solver Preprocessing ( Zone " << config->GetiZone() <<" ) --------------------" << endl;
+    
+    solver = new CSolver**[config->GetnMGLevels()+1] ();
+    
+    for (iMesh = 0; iMesh <= config->GetnMGLevels(); iMesh++){
+        solver[iMesh] = CSolverFactory::CreateSolverContainer(kindSolver, config, geometry[iMesh], iMesh);
+    }
+    
+    /*--- Count the number of DOFs per solution point. ---*/
+    
+    DOFsPerPoint = 0;
+    
+    for (unsigned int iSol = 0; iSol < MAX_SOLS; iSol++)
+        if (solver[MESH_0][iSol]) DOFsPerPoint += solver[MESH_0][iSol]->GetnVar();
+    
+    /*--- Restart solvers, for FSI the geometry cannot be updated because the interpolation classes
+     * should always use the undeformed mesh (otherwise the results would not be repeatable). ---*/
+    
+    if (!fsi) Solver_Restart(solver, geometry, config, true);
+    
+    /*--- Set up any necessary inlet profiles ---*/
+    
+    Inlet_Preprocessing(solver, geometry, config);
+    
+}
 
-      case AUSM:
-        for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-          numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwAUSM_Flow(nDim, nVar_Flow, config);
-          numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwAUSM_Flow(nDim, nVar_Flow, config);
+void CDriver::Inlet_Preprocessing(CSolver ***solver, CGeometry **geometry,
+                                  CConfig *config) const {
+    
+    /*--- Adjust iteration number for unsteady restarts. ---*/
+    
+    const bool adjoint = config->GetDiscrete_Adjoint() || config->GetContinuous_Adjoint();
+    
+    int val_iter = 0;
+    
+    if (config->GetTime_Domain()) {
+        val_iter = adjoint? config->GetUnst_AdjointIter() : config->GetRestart_Iter();
+        val_iter -= 1;
+        if (!adjoint && config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND)
+            val_iter -= 1;
+        if (!adjoint && !config->GetRestart()) val_iter = 0;
+    }
+    
+    /*--- Load inlet profile files for any of the active solver containers.
+     Note that these routines fill the fine grid data structures for the markers
+     and restrict values down to all coarser MG levels. ---*/
+    
+    if (config->GetInlet_Profile_From_File()) {
+        
+        /*--- Use LoadInletProfile() routines for the particular solver. ---*/
+        
+        if (rank == MASTER_NODE) {
+            cout << endl;
+            cout << "Reading inlet profile from file: ";
+            cout << config->GetInlet_FileName() << endl;
         }
-        break;
-
-      case TURKEL:
-        for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-          numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwTurkel_Flow(nDim, nVar_Flow, config);
-          numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwTurkel_Flow(nDim, nVar_Flow, config);
+        
+        if (solver[MESH_0][FLOW_SOL]) {
+            solver[MESH_0][FLOW_SOL]->LoadInletProfile(geometry, solver, config, val_iter, FLOW_SOL, INLET_FLOW);
         }
-        break;
-
-      case HLLC:
-          for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-            numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwHLLC_Flow(nDim, nVar_Flow, config);
-            numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwHLLC_Flow(nDim, nVar_Flow, config);
-          }
-        break;
-
-      case MSW:
-        for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-          numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwMSW_Flow(nDim, nVar_Flow, config);
-          numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwMSW_Flow(nDim, nVar_Flow, config);
+        if (solver[MESH_0][TURB_SOL]) {
+            solver[MESH_0][TURB_SOL]->LoadInletProfile(geometry, solver, config, val_iter, TURB_SOL, INLET_FLOW);
         }
-        break;
-
-      case CUSP:
-        for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-          numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwCUSP_Flow(nDim, nVar_Flow, config);
-          numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwCUSP_Flow(nDim, nVar_Flow, config);
+        if (solver[MESH_0][SPECIES_SOL]) {
+            solver[MESH_0][SPECIES_SOL]->LoadInletProfile(geometry, solver, config, val_iter, SPECIES_SOL, INLET_FLOW);
         }
-        break;
-
-      default:
-        SU2_MPI::Error("Riemann solver not implemented.", CURRENT_FUNCTION);
-        break;
-    }
-
-  }
-
-  /*--- Solver definition for the turbulent model problem ---*/
-
-  if (turbulent) {
-    if (incompressible)
-      InstantiateTurbulentNumerics<CIncEulerVariable::CIndices<unsigned short> >(nVar_Turb, offset, config,
-                                                                                 solver[MESH_0][TURB_SOL], numerics);
-    else if (NEMO_ns)
-      InstantiateTurbulentNumerics<CNEMOEulerVariable::CIndices<unsigned short> >(nVar_Turb, offset, config,
-                                                                                  solver[MESH_0][TURB_SOL], numerics);
-    else
-      InstantiateTurbulentNumerics<CEulerVariable::CIndices<unsigned short> >(nVar_Turb, offset, config,
-                                                                              solver[MESH_0][TURB_SOL], numerics);
-  }
-
-  /*--- Solver definition for the transition model problem ---*/
-  if (transition) {
-
-    /*--- Definition of the convective scheme for each equation and mesh level ---*/
-    switch (config->GetKind_ConvNumScheme_Turb()) {
-      case NO_UPWIND:
-        SU2_MPI::Error("Config file is missing the CONV_NUM_METHOD_TURB option.", CURRENT_FUNCTION);
-        break;
-      case SPACE_UPWIND:
-        for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-          numerics[iMGlevel][TRANS_SOL][conv_term] = new CUpwSca_TransLM(nDim, nVar_Trans, config);
+        
+        /*--- Exit if profiles were requested for a solver that is not available. ---*/
+        
+        if (!config->GetFluidProblem()) {
+            SU2_MPI::Error(string("Inlet profile specification via file (C++) has not been \n") +
+                           string("implemented yet for this solver.\n") +
+                           string("Please set SPECIFIED_INLET_PROFILE= NO and try again."), CURRENT_FUNCTION);
+        }
+        
+    } else {
+        
+        /*--- Uniform inlets or python-customized inlets ---*/
+        
+        /* --- Initialize quantities for inlet boundary
+         * This routine does not check if they python wrapper is being used to
+         * set custom boundary conditions.  This is intentional; the
+         * default values for python custom BCs are initialized with the default
+         * values specified in the config (avoiding non physical values) --- */
+        
+        for (unsigned short iMesh = 0; iMesh <= config->GetnMGLevels(); iMesh++) {
+            for(unsigned short iMarker=0; iMarker < config->GetnMarker_All(); iMarker++) {
+                if (solver[iMesh][FLOW_SOL]) solver[iMesh][FLOW_SOL]->SetUniformInlet(config, iMarker);
+                if (solver[iMesh][TURB_SOL]) solver[iMesh][TURB_SOL]->SetUniformInlet(config, iMarker);
+                if (solver[iMesh][SPECIES_SOL]) solver[iMesh][SPECIES_SOL]->SetUniformInlet(config, iMarker);
+            }
         }
-        break;
-      default:
-        SU2_MPI::Error("Invalid convective scheme for the transition equations.", CURRENT_FUNCTION);
-        break;
+        
     }
+    
+}
 
-    /*--- Definition of the viscous scheme for each equation and mesh level ---*/
-    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-      numerics[iMGlevel][TRANS_SOL][visc_term] = new CAvgGradCorrected_TransLM(nDim, nVar_Trans, config);
+void CDriver::Solver_Restart(CSolver ***solver, CGeometry **geometry,
+                             CConfig *config, bool update_geo) {
+    
+    /*--- Check for restarts and use the LoadRestart() routines. ---*/
+    
+    const bool restart = config->GetRestart();
+    const bool restart_flow = config->GetRestart_Flow();
+    
+    /*--- Adjust iteration number for unsteady restarts. ---*/
+    
+    int val_iter = 0;
+    
+    const bool adjoint = (config->GetDiscrete_Adjoint() || config->GetContinuous_Adjoint());
+    const bool time_domain = config->GetTime_Domain();
+    const bool dt_step_2nd = (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND) &&
+    !config->GetStructuralProblem() && !config->GetFEMSolver() &&
+    !adjoint && time_domain;
+    
+    if (time_domain) {
+        if (adjoint) val_iter = config->GetUnst_AdjointIter() - 1;
+        else val_iter = config->GetRestart_Iter() - 1 - dt_step_2nd;
+    }
+    
+    /*--- Restart direct solvers. ---*/
+    
+    if (restart || restart_flow) {
+        for (auto iSol = 0u; iSol < MAX_SOLS; ++iSol) {
+            auto sol = solver[MESH_0][iSol];
+            if (sol && !sol->GetAdjoint()) {
+                /*--- Note that the mesh solver always loads the most recent file (and not -2). ---*/
+                SU2_OMP_PARALLEL_(if(sol->GetHasHybridParallel()))
+                sol->LoadRestart(geometry, solver, config, val_iter + (iSol==MESH_SOL && dt_step_2nd), update_geo);
+                END_SU2_OMP_PARALLEL
+            }
+        }
     }
-
-    /*--- Definition of the source term integration scheme for each equation and mesh level ---*/
-    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-      numerics[iMGlevel][TRANS_SOL][source_first_term] = new CSourcePieceWise_TransLM(nDim, nVar_Trans, config);
-      numerics[iMGlevel][TRANS_SOL][source_second_term] = new CSourceNothing(nDim, nVar_Trans, config);
+    
+    /*--- Restart adjoint solvers. ---*/
+    
+    if (restart) {
+        if ((config->GetKind_Solver() == MAIN_SOLVER::TEMPLATE_SOLVER) ||
+            (config->GetKind_Solver() == MAIN_SOLVER::ADJ_RANS && !config->GetFrozen_Visc_Cont())) {
+            SU2_MPI::Error("A restart capability has not been implemented yet for this solver.\n"
+                           "Please set RESTART_SOL= NO and try again.", CURRENT_FUNCTION);
+        }
+        
+        for (auto iSol = 0u; iSol < MAX_SOLS; ++iSol) {
+            auto sol = solver[MESH_0][iSol];
+            if (sol && sol->GetAdjoint())
+                sol->LoadRestart(geometry, solver, config, val_iter, update_geo);
+        }
     }
+    
+}
 
-    /*--- Definition of the boundary condition method ---*/
-    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-      numerics[iMGlevel][TRANS_SOL][conv_bound_term] = new CUpwLin_TransLM(nDim, nVar_Trans, config);
+void CDriver::Solver_Postprocessing(CSolver ****solver, CGeometry **geometry,
+                                    CConfig *config, unsigned short val_iInst) {
+    
+    for (int iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+        for (unsigned int iSol = 0; iSol < MAX_SOLS; iSol++){
+            delete solver[val_iInst][iMGlevel][iSol];
+        }
+        delete [] solver[val_iInst][iMGlevel];
     }
-  }
-
-  /*--- Solver definition for the species transport problem ---*/
-
-  if (species) {
-    if (incompressible)
-      InstantiateSpeciesNumerics<CIncEulerVariable::CIndices<unsigned short> >(nVar_Species, offset, config,
-                                                                               solver[MESH_0][SPECIES_SOL], numerics);
-    else if (compressible)
-      InstantiateSpeciesNumerics<CEulerVariable::CIndices<unsigned short> >(nVar_Species, offset, config,
-                                                                            solver[MESH_0][SPECIES_SOL], numerics);
-    else
-      SU2_MPI::Error("Species transport only available for standard compressible and incompressible flow.", CURRENT_FUNCTION);
-  }
-
-  /*--- Solver definition of the finite volume heat solver  ---*/
-  if (heat) {
-
-    /*--- Definition of the viscous scheme for each equation and mesh level ---*/
-    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+    delete [] solver[val_iInst];
+    
+    CSolverFactory::ClearSolverMeta();
+    
+}
 
-      numerics[iMGlevel][HEAT_SOL][visc_term] = new CAvgGrad_Heat(nDim, nVar_Heat, config, true);
-      numerics[iMGlevel][HEAT_SOL][visc_bound_term] = new CAvgGrad_Heat(nDim, nVar_Heat, config, false);
+void CDriver::Integration_Preprocessing(CConfig *config, CSolver **solver, CIntegration **&integration) const {
+    
+    if (rank == MASTER_NODE)
+        cout << endl <<"----------------- Integration Preprocessing ( Zone " << config->GetiZone() <<" ) ------------------" << endl;
+    
+    MAIN_SOLVER kindMainSolver = config->GetKind_Solver();
+    
+    integration = CIntegrationFactory::CreateIntegrationContainer(kindMainSolver, solver);
+    
+}
 
-      switch (config->GetKind_ConvNumScheme_Heat()) {
+void CDriver::Integration_Postprocessing(CIntegration ***integration, CGeometry **geometry, CConfig *config, unsigned short val_iInst) {
+    
+    for (unsigned int iSol = 0; iSol < MAX_SOLS; iSol++){
+        delete integration[val_iInst][iSol];
+    }
+    
+    delete [] integration[val_iInst];
+    
+}
 
+template <class Indices>
+void CDriver::InstantiateTurbulentNumerics(unsigned short nVar_Turb, int offset, const CConfig *config,
+                                           const CSolver* turb_solver, CNumerics ****&numerics) const {
+    const int conv_term = CONV_TERM + offset;
+    const int visc_term = VISC_TERM + offset;
+    
+    const int source_first_term = SOURCE_FIRST_TERM + offset;
+    const int source_second_term = SOURCE_SECOND_TERM + offset;
+    
+    const int conv_bound_term = CONV_BOUND_TERM + offset;
+    const int visc_bound_term = VISC_BOUND_TERM + offset;
+    
+    bool spalart_allmaras, neg_spalart_allmaras, e_spalart_allmaras, comp_spalart_allmaras, e_comp_spalart_allmaras, menter_sst;
+    spalart_allmaras = neg_spalart_allmaras = e_spalart_allmaras = comp_spalart_allmaras = e_comp_spalart_allmaras = menter_sst = false;
+    
+    /*--- Assign turbulence model booleans ---*/
+    
+    switch (config->GetKind_Turb_Model()) {
+        case TURB_MODEL::NONE:
+            SU2_MPI::Error("No turbulence model selected.", CURRENT_FUNCTION);
+            break;
+        case TURB_MODEL::SA:        spalart_allmaras = true;        break;
+        case TURB_MODEL::SA_NEG:    neg_spalart_allmaras = true;    break;
+        case TURB_MODEL::SA_E:      e_spalart_allmaras = true;      break;
+        case TURB_MODEL::SA_COMP:   comp_spalart_allmaras = true;   break;
+        case TURB_MODEL::SA_E_COMP: e_comp_spalart_allmaras = true; break;
+        case TURB_MODEL::SST:       menter_sst = true;              break;
+        case TURB_MODEL::SST_SUST:  menter_sst = true;              break;
+    }
+    
+    /*--- If the Menter SST model is used, store the constants of the model and determine the
+     free stream values of the turbulent kinetic energy and dissipation rate. ---*/
+    
+    const su2double *constants = nullptr;
+    su2double kine_Inf = 0.0, omega_Inf = 0.0;
+    
+    if (menter_sst) {
+        constants = turb_solver->GetConstants();
+        kine_Inf  = turb_solver->GetTke_Inf();
+        omega_Inf = turb_solver->GetOmega_Inf();
+    }
+    
+    /*--- Definition of the convective scheme for each equation and mesh level ---*/
+    
+    switch (config->GetKind_ConvNumScheme_Turb()) {
+        case NO_UPWIND:
+            SU2_MPI::Error("Config file is missing the CONV_NUM_METHOD_TURB option.", CURRENT_FUNCTION);
+            break;
         case SPACE_UPWIND :
-          numerics[iMGlevel][HEAT_SOL][conv_term] = new CUpwSca_Heat(nDim, nVar_Heat, config);
-          numerics[iMGlevel][HEAT_SOL][conv_bound_term] = new CUpwSca_Heat(nDim, nVar_Heat, config);
-          break;
-
-        case SPACE_CENTERED :
-          numerics[iMGlevel][HEAT_SOL][conv_term] = new CCentSca_Heat(nDim, nVar_Heat, config);
-          numerics[iMGlevel][HEAT_SOL][conv_bound_term] = new CUpwSca_Heat(nDim, nVar_Heat, config);
-          break;
-
+            for (auto iMGlevel = 0u; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                if (spalart_allmaras || neg_spalart_allmaras || e_spalart_allmaras || comp_spalart_allmaras || e_comp_spalart_allmaras) {
+                    numerics[iMGlevel][TURB_SOL][conv_term] = new CUpwSca_TurbSA<Indices>(nDim, nVar_Turb, config);
+                }
+                else if (menter_sst) numerics[iMGlevel][TURB_SOL][conv_term] = new CUpwSca_TurbSST<Indices>(nDim, nVar_Turb, config);
+            }
+            break;
         default:
-          SU2_MPI::Error("Invalid convective scheme for the heat transfer equations.", CURRENT_FUNCTION);
-          break;
-      }
+            SU2_MPI::Error("Invalid convective scheme for the turbulence equations.", CURRENT_FUNCTION);
+            break;
     }
-  }
-
-  /*--- Solver definition for the radiation model problem ---*/
-
-  if (config->AddRadiation()) {
+    
     /*--- Definition of the viscous scheme for each equation and mesh level ---*/
-    numerics[MESH_0][RAD_SOL][VISC_TERM] = new CAvgGradCorrected_P1(nDim, nVar_Rad, config);
-
+    
+    for (auto iMGlevel = 0u; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+        if (spalart_allmaras || e_spalart_allmaras || comp_spalart_allmaras || e_comp_spalart_allmaras) {
+            numerics[iMGlevel][TURB_SOL][visc_term] = new CAvgGrad_TurbSA<Indices>(nDim, nVar_Turb, true, config);
+        }
+        else if (neg_spalart_allmaras)
+            numerics[iMGlevel][TURB_SOL][visc_term] = new CAvgGrad_TurbSA_Neg<Indices>(nDim, nVar_Turb, true, config);
+        else if (menter_sst)
+            numerics[iMGlevel][TURB_SOL][visc_term] = new CAvgGrad_TurbSST<Indices>(nDim, nVar_Turb, constants, true, config);
+    }
+    
     /*--- Definition of the source term integration scheme for each equation and mesh level ---*/
-    numerics[MESH_0][RAD_SOL][SOURCE_FIRST_TERM] = new CSourceP1(nDim, nVar_Rad, config);
-
+    
+    for (auto iMGlevel = 0u; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+        auto& turb_source_first_term = numerics[iMGlevel][TURB_SOL][source_first_term];
+        
+        if (spalart_allmaras)
+            turb_source_first_term = new CSourcePieceWise_TurbSA<Indices>(nDim, nVar_Turb, config);
+        else if (e_spalart_allmaras)
+            turb_source_first_term = new CSourcePieceWise_TurbSA_E<Indices>(nDim, nVar_Turb, config);
+        else if (comp_spalart_allmaras)
+            turb_source_first_term = new CSourcePieceWise_TurbSA_COMP<Indices>(nDim, nVar_Turb, config);
+        else if (e_comp_spalart_allmaras)
+            turb_source_first_term = new CSourcePieceWise_TurbSA_E_COMP<Indices>(nDim, nVar_Turb, config);
+        else if (neg_spalart_allmaras)
+            turb_source_first_term = new CSourcePieceWise_TurbSA_Neg<Indices>(nDim, nVar_Turb, config);
+        else if (menter_sst)
+            turb_source_first_term = new CSourcePieceWise_TurbSST<Indices>(nDim, nVar_Turb, constants, kine_Inf, omega_Inf,
+                                                                           config);
+        
+        numerics[iMGlevel][TURB_SOL][source_second_term] = new CSourceNothing(nDim, nVar_Turb, config);
+    }
+    
     /*--- Definition of the boundary condition method ---*/
-    numerics[MESH_0][RAD_SOL][VISC_BOUND_TERM] = new CAvgGradCorrected_P1(nDim, nVar_Rad, config);
-  }
-
-  /*--- Solver definition for the flow adjoint problem ---*/
-
-  if (adj_euler || adj_ns) {
-
-    if (incompressible)
-      SU2_MPI::Error("Convective schemes not implemented for incompressible continuous adjoint.", CURRENT_FUNCTION);
-
-    /*--- Definition of the convective scheme for each equation and mesh level ---*/
-
-    switch (config->GetKind_ConvNumScheme_AdjFlow()) {
-      case NO_CONVECTIVE:
-        SU2_MPI::Error("Config file is missing the CONV_NUM_METHOD_ADJFLOW option.", CURRENT_FUNCTION);
-        break;
-
-      case SPACE_CENTERED :
-
-        if (compressible) {
-
-          /*--- Compressible flow ---*/
-
-          switch (config->GetKind_Centered_AdjFlow()) {
-            case LAX : numerics[MESH_0][ADJFLOW_SOL][conv_term] = new CCentLax_AdjFlow(nDim, nVar_Adj_Flow, config); break;
-            case JST : numerics[MESH_0][ADJFLOW_SOL][conv_term] = new CCentJST_AdjFlow(nDim, nVar_Adj_Flow, config); break;
-            default:
-              SU2_MPI::Error("Centered scheme not implemented.", CURRENT_FUNCTION);
-              break;
-          }
-
-          for (iMGlevel = 1; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-            numerics[iMGlevel][ADJFLOW_SOL][conv_term] = new CCentLax_AdjFlow(nDim, nVar_Adj_Flow, config);
-
-          for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-            numerics[iMGlevel][ADJFLOW_SOL][conv_bound_term] = new CUpwRoe_AdjFlow(nDim, nVar_Adj_Flow, config);
-
+    
+    for (auto iMGlevel = 0u; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+        if (spalart_allmaras || e_spalart_allmaras || comp_spalart_allmaras || e_comp_spalart_allmaras) {
+            numerics[iMGlevel][TURB_SOL][conv_bound_term] = new CUpwSca_TurbSA<Indices>(nDim, nVar_Turb, config);
+            numerics[iMGlevel][TURB_SOL][visc_bound_term] = new CAvgGrad_TurbSA<Indices>(nDim, nVar_Turb, false, config);
         }
-        break;
-
-      case SPACE_UPWIND :
-
-        if (compressible) {
-
-          /*--- Compressible flow ---*/
-
-          switch (config->GetKind_Upwind_AdjFlow()) {
-            case ROE:
-              for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-                numerics[iMGlevel][ADJFLOW_SOL][conv_term] = new CUpwRoe_AdjFlow(nDim, nVar_Adj_Flow, config);
-                numerics[iMGlevel][ADJFLOW_SOL][conv_bound_term] = new CUpwRoe_AdjFlow(nDim, nVar_Adj_Flow, config);
-              }
-              break;
-            default:
-              SU2_MPI::Error("Upwind scheme not implemented.", CURRENT_FUNCTION);
-              break;
-          }
+        else if (neg_spalart_allmaras) {
+            numerics[iMGlevel][TURB_SOL][conv_bound_term] = new CUpwSca_TurbSA<Indices>(nDim, nVar_Turb, config);
+            numerics[iMGlevel][TURB_SOL][visc_bound_term] = new CAvgGrad_TurbSA_Neg<Indices>(nDim, nVar_Turb, false, config);
+        }
+        else if (menter_sst) {
+            numerics[iMGlevel][TURB_SOL][conv_bound_term] = new CUpwSca_TurbSST<Indices>(nDim, nVar_Turb, config);
+            numerics[iMGlevel][TURB_SOL][visc_bound_term] = new CAvgGrad_TurbSST<Indices>(nDim, nVar_Turb, constants, false,
+                                                                                          config);
         }
-        break;
-
-      default:
-        SU2_MPI::Error("Invalid convective scheme for the continuous adjoint Euler / Navier-Stokes equations.", CURRENT_FUNCTION);
-        break;
     }
+}
+/*--- Explicit instantiation of the template above, needed because it is defined in a cpp file, instead of hpp. ---*/
+template void CDriver::InstantiateTurbulentNumerics<CEulerVariable::CIndices<unsigned short>>(
+                                                                                              unsigned short, int, const CConfig*, const CSolver*, CNumerics****&) const;
 
-    /*--- Definition of the viscous scheme for each equation and mesh level ---*/
-
-    if (compressible) {
-
-      /*--- Compressible flow ---*/
-
-      numerics[MESH_0][ADJFLOW_SOL][visc_term] = new CAvgGradCorrected_AdjFlow(nDim, nVar_Adj_Flow, config);
-      numerics[MESH_0][ADJFLOW_SOL][visc_bound_term] = new CAvgGrad_AdjFlow(nDim, nVar_Adj_Flow, config);
+template void CDriver::InstantiateTurbulentNumerics<CIncEulerVariable::CIndices<unsigned short>>(
+                                                                                                 unsigned short, int, const CConfig*, const CSolver*, CNumerics****&) const;
 
-      for (iMGlevel = 1; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-        numerics[iMGlevel][ADJFLOW_SOL][visc_term] = new CAvgGrad_AdjFlow(nDim, nVar_Adj_Flow, config);
-        numerics[iMGlevel][ADJFLOW_SOL][visc_bound_term] = new CAvgGrad_AdjFlow(nDim, nVar_Adj_Flow, config);
-      }
+template void CDriver::InstantiateTurbulentNumerics<CNEMOEulerVariable::CIndices<unsigned short>>(
+                                                                                                  unsigned short, int, const CConfig*, const CSolver*, CNumerics****&) const;
 
+template <class Indices>
+void CDriver::InstantiateSpeciesNumerics(unsigned short nVar_Species, int offset, const CConfig *config,
+                                         const CSolver* species_solver, CNumerics ****&numerics) const {
+    const int conv_term = CONV_TERM + offset;
+    const int visc_term = VISC_TERM + offset;
+    
+    const int source_first_term = SOURCE_FIRST_TERM + offset;
+    const int source_second_term = SOURCE_SECOND_TERM + offset;
+    
+    const int conv_bound_term = CONV_BOUND_TERM + offset;
+    const int visc_bound_term = VISC_BOUND_TERM + offset;
+    
+    /*--- Definition of the convective scheme for each equation and mesh level. Also for boundary conditions. ---*/
+    
+    switch (config->GetKind_ConvNumScheme_Species()) {
+        case NONE :
+            break;
+        case SPACE_UPWIND :
+            for (auto iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                numerics[iMGlevel][SPECIES_SOL][conv_term] = new CUpwSca_Species<Indices>(nDim, nVar_Species, config);
+                numerics[iMGlevel][SPECIES_SOL][conv_bound_term] = new CUpwSca_Species<Indices>(nDim, nVar_Species, config);
+            }
+            break;
+        default :
+            SU2_MPI::Error("Invalid convective scheme for the species transport equations. Use SCALAR_UPWIND.", CURRENT_FUNCTION);
+            break;
     }
-
+    
+    /*--- Definition of the viscous scheme for each equation and mesh level ---*/
+    
+    for (auto iMGlevel = 0u; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+        numerics[iMGlevel][SPECIES_SOL][visc_term] = new CAvgGrad_Species<Indices>(nDim, nVar_Species, true, config);
+        numerics[iMGlevel][SPECIES_SOL][visc_bound_term] = new CAvgGrad_Species<Indices>(nDim, nVar_Species, false, config);
+    }
+    
     /*--- Definition of the source term integration scheme for each equation and mesh level ---*/
-
-    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-
-      /*--- Note that RANS is incompatible with Axisymmetric or Rotational (Fix it!) ---*/
-
-      if (compressible) {
-
-        if (adj_ns) {
-
-          numerics[iMGlevel][ADJFLOW_SOL][source_first_term] = new CSourceViscous_AdjFlow(nDim, nVar_Adj_Flow, config);
-
-          if (config->GetRotating_Frame() == YES)
-            numerics[iMGlevel][ADJFLOW_SOL][source_second_term] = new CSourceRotatingFrame_AdjFlow(nDim, nVar_Adj_Flow, config);
-          else
-            numerics[iMGlevel][ADJFLOW_SOL][source_second_term] = new CSourceConservative_AdjFlow(nDim, nVar_Adj_Flow, config);
-
+    
+    for (auto iMGlevel = 0u; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+        if (config->GetAxisymmetric() == YES) {
+            numerics[iMGlevel][SPECIES_SOL][source_first_term] = new CSourceAxisymmetric_Species<Indices>(nDim, nVar_Species, config);
         }
-
         else {
-
-          if (config->GetRotating_Frame() == YES)
-            numerics[iMGlevel][ADJFLOW_SOL][source_first_term] = new CSourceRotatingFrame_AdjFlow(nDim, nVar_Adj_Flow, config);
-          else if (config->GetAxisymmetric() == YES)
-            numerics[iMGlevel][ADJFLOW_SOL][source_first_term] = new CSourceAxisymmetric_AdjFlow(nDim, nVar_Adj_Flow, config);
-          else
-            numerics[iMGlevel][ADJFLOW_SOL][source_first_term] = new CSourceNothing(nDim, nVar_Adj_Flow, config);
-
-          numerics[iMGlevel][ADJFLOW_SOL][source_second_term] = new CSourceNothing(nDim, nVar_Adj_Flow, config);
-
+            numerics[iMGlevel][SPECIES_SOL][source_first_term] = new CSourceNothing(nDim, nVar_Species, config);
         }
-
-      }
-
-    }
-
-  }
-
-  /*--- Solver definition for the turbulent adjoint problem ---*/
-  if (adj_turb) {
-
-    if (config->GetKind_Turb_Model() != TURB_MODEL::SA)
-      SU2_MPI::Error("Only the SA turbulence model can be used with the continuous adjoint solver.", CURRENT_FUNCTION);
-
-    /*--- Definition of the convective scheme for each equation and mesh level ---*/
-    switch (config->GetKind_ConvNumScheme_AdjTurb()) {
-      case NO_CONVECTIVE:
-        SU2_MPI::Error("Config file is missing the CONV_NUM_METHOD_ADJTURB option.", CURRENT_FUNCTION);
-        break;
-      case SPACE_UPWIND :
-        for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-          numerics[iMGlevel][ADJTURB_SOL][conv_term] = new CUpwSca_AdjTurb(nDim, nVar_Adj_Turb, config);
-        break;
-      default:
-        SU2_MPI::Error("Convective scheme not implemented (adjoint turbulence).", CURRENT_FUNCTION);
-        break;
-    }
-
-    /*--- Definition of the viscous scheme for each equation and mesh level ---*/
-    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-      numerics[iMGlevel][ADJTURB_SOL][visc_term] = new CAvgGradCorrected_AdjTurb(nDim, nVar_Adj_Turb, config);
-
-    /*--- Definition of the source term integration scheme for each equation and mesh level ---*/
-    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-      numerics[iMGlevel][ADJTURB_SOL][source_first_term] = new CSourcePieceWise_AdjTurb(nDim, nVar_Adj_Turb, config);
-      numerics[iMGlevel][ADJTURB_SOL][source_second_term] = new CSourceConservative_AdjTurb(nDim, nVar_Adj_Turb, config);
+        numerics[iMGlevel][SPECIES_SOL][source_second_term] = new CSourceNothing(nDim, nVar_Species, config);
     }
+}
+/*--- Explicit instantiation of the template above, needed because it is defined in a cpp file, instead of hpp. ---*/
+template void CDriver::InstantiateSpeciesNumerics<CEulerVariable::CIndices<unsigned short>>(
+                                                                                            unsigned short, int, const CConfig*, const CSolver*, CNumerics****&) const;
 
-    /*--- Definition of the boundary condition method ---*/
-    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-      numerics[iMGlevel][ADJTURB_SOL][conv_bound_term] = new CUpwLin_AdjTurb(nDim, nVar_Adj_Turb, config);
-
-  }
+template void CDriver::InstantiateSpeciesNumerics<CIncEulerVariable::CIndices<unsigned short>>(
+                                                                                               unsigned short, int, const CConfig*, const CSolver*, CNumerics****&) const;
 
-  /*--- Numerics definition for FEM-like problems. ---*/
+template void CDriver::InstantiateSpeciesNumerics<CNEMOEulerVariable::CIndices<unsigned short>>(
+                                                                                                unsigned short, int, const CConfig*, const CSolver*, CNumerics****&) const;
 
-  if (fem) {
-    /*--- Initialize the container for FEA_TERM. This will be the only one for most of the cases. ---*/
-    switch (config->GetGeometricConditions()) {
-      case STRUCT_DEFORMATION::SMALL:
-        switch (config->GetMaterialModel()) {
-          case STRUCT_MODEL::LINEAR_ELASTIC:
-            numerics[MESH_0][FEA_SOL][fea_term] = new CFEALinearElasticity(nDim, nVar_FEM, config);
-            break;
-          default:
-            SU2_MPI::Error("Material model does not correspond to geometric conditions.", CURRENT_FUNCTION);
+void CDriver::Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***solver, CNumerics ****&numerics) const {
+    
+    if (rank == MASTER_NODE)
+        cout << endl <<"------------------- Numerics Preprocessing ( Zone " << config->GetiZone() <<" ) -------------------" << endl;
+    
+    unsigned short iMGlevel, iSol,
+    
+    nVar_Template         = 0,
+    nVar_Flow             = 0,
+    nVar_NEMO             = 0,
+    nPrimVar_NEMO         = 0,
+    nPrimVarGrad_NEMO     = 0,
+    nVar_Trans            = 0,
+    nVar_Turb             = 0,
+    nVar_Species          = 0,
+    nVar_Adj_Flow         = 0,
+    nVar_Adj_Turb         = 0,
+    nVar_FEM              = 0,
+    nVar_Rad              = 0,
+    nVar_Heat             = 0;
+    
+    numerics = new CNumerics***[config->GetnMGLevels()+1] ();
+    
+    bool compressible = false;
+    bool incompressible = false;
+    bool ideal_gas = (config->GetKind_FluidModel() == STANDARD_AIR) || (config->GetKind_FluidModel() == IDEAL_GAS);
+    bool roe_low_dissipation = (config->GetKind_RoeLowDiss() != NO_ROELOWDISS);
+    
+    /*--- Initialize some useful booleans ---*/
+    bool euler, ns, NEMO_euler, NEMO_ns, turbulent, adj_euler, adj_ns, adj_turb, fem_euler, fem_ns;
+    bool fem, heat, transition, template_solver;
+    
+    euler = ns = NEMO_euler = NEMO_ns = turbulent = adj_euler = adj_ns = adj_turb = fem_euler = fem_ns = false;
+    fem = heat = transition = template_solver = false;
+    bool species = false;
+    
+    /*--- Assign booleans ---*/
+    switch (config->GetKind_Solver()) {
+        case MAIN_SOLVER::TEMPLATE_SOLVER:
+            template_solver = true; break;
+            
+        case MAIN_SOLVER::EULER:
+        case MAIN_SOLVER::DISC_ADJ_EULER:
+            euler = compressible = true; break;
+            
+        case MAIN_SOLVER::NAVIER_STOKES:
+        case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES:
+            ns = compressible = true;
+            species = (config->GetKind_Species_Model() != SPECIES_MODEL::NONE); break;
+            
+        case MAIN_SOLVER::NEMO_EULER:
+            NEMO_euler = compressible = true; break;
+            
+        case MAIN_SOLVER::NEMO_NAVIER_STOKES:
+            NEMO_ns = compressible = true; break;
+            
+        case MAIN_SOLVER::RANS:
+        case MAIN_SOLVER::DISC_ADJ_RANS:
+            ns = compressible = turbulent = true;
+            transition = (config->GetKind_Trans_Model() == TURB_TRANS_MODEL::LM);
+            species = config->GetKind_Species_Model() != SPECIES_MODEL::NONE; break;
+            
+        case MAIN_SOLVER::INC_EULER:
+        case MAIN_SOLVER::DISC_ADJ_INC_EULER:
+            euler = incompressible = true; break;
+            
+        case MAIN_SOLVER::INC_NAVIER_STOKES:
+        case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES:
+            ns = incompressible = true;
+            heat = config->GetWeakly_Coupled_Heat();
+            species = (config->GetKind_Species_Model() != SPECIES_MODEL::NONE); break;
+            
+        case MAIN_SOLVER::INC_RANS:
+        case MAIN_SOLVER::DISC_ADJ_INC_RANS:
+            ns = incompressible = turbulent = true;
+            heat = config->GetWeakly_Coupled_Heat();
+            transition = (config->GetKind_Trans_Model() == TURB_TRANS_MODEL::LM);
+            species = (config->GetKind_Species_Model() != SPECIES_MODEL::NONE); break;
+            
+        case MAIN_SOLVER::FEM_EULER:
+        case MAIN_SOLVER::DISC_ADJ_FEM_EULER:
+            fem_euler = compressible = true; break;
+            
+        case MAIN_SOLVER::FEM_NAVIER_STOKES:
+        case MAIN_SOLVER::DISC_ADJ_FEM_NS:
+            fem_ns = compressible = true; break;
+            
+        case MAIN_SOLVER::FEM_RANS:
+        case MAIN_SOLVER::DISC_ADJ_FEM_RANS:
+            fem_ns = compressible = true; break;
+            
+        case MAIN_SOLVER::FEM_LES:
+            fem_ns = compressible = true; break;
+            
+        case MAIN_SOLVER::HEAT_EQUATION:
+        case MAIN_SOLVER::DISC_ADJ_HEAT:
+            heat = true; break;
+            
+        case MAIN_SOLVER::FEM_ELASTICITY:
+        case MAIN_SOLVER::DISC_ADJ_FEM:
+            fem = true; break;
+            
+        case MAIN_SOLVER::ADJ_EULER:
+            adj_euler = euler = compressible = true; break;
+            
+        case MAIN_SOLVER::ADJ_NAVIER_STOKES:
+            adj_ns = ns = compressible = true;
+            turbulent = (config->GetKind_Turb_Model() != TURB_MODEL::NONE); break;
+            
+        case MAIN_SOLVER::ADJ_RANS:
+            adj_ns = ns = compressible = turbulent = true;
+            adj_turb = !config->GetFrozen_Visc_Cont(); break;
+            
+        default:
             break;
+            
+    }
+    
+    /*--- Number of variables for the template ---*/
+    
+    if (template_solver) nVar_Flow = solver[MESH_0][FLOW_SOL]->GetnVar();
+    
+    /*--- Number of variables for direct problem ---*/
+    
+    if (euler)        nVar_Flow = solver[MESH_0][FLOW_SOL]->GetnVar();
+    if (ns)           nVar_Flow = solver[MESH_0][FLOW_SOL]->GetnVar();
+    if (NEMO_euler)   nVar_NEMO = solver[MESH_0][FLOW_SOL]->GetnVar();
+    if (NEMO_ns)      nVar_NEMO = solver[MESH_0][FLOW_SOL]->GetnVar();
+    if (turbulent)    nVar_Turb = solver[MESH_0][TURB_SOL]->GetnVar();
+    if (transition)   nVar_Trans = solver[MESH_0][TRANS_SOL]->GetnVar();
+    if (species)      nVar_Species = solver[MESH_0][SPECIES_SOL]->GetnVar();
+    
+    if (fem_euler)    nVar_Flow = solver[MESH_0][FLOW_SOL]->GetnVar();
+    if (fem_ns)       nVar_Flow = solver[MESH_0][FLOW_SOL]->GetnVar();
+    
+    if (fem)          nVar_FEM = solver[MESH_0][FEA_SOL]->GetnVar();
+    if (heat)         nVar_Heat = solver[MESH_0][HEAT_SOL]->GetnVar();
+    
+    if (config->AddRadiation()) nVar_Rad = solver[MESH_0][RAD_SOL]->GetnVar();
+    
+    /*--- Number of variables for adjoint problem ---*/
+    
+    if (adj_euler)    nVar_Adj_Flow = solver[MESH_0][ADJFLOW_SOL]->GetnVar();
+    if (adj_ns)       nVar_Adj_Flow = solver[MESH_0][ADJFLOW_SOL]->GetnVar();
+    if (adj_turb)     nVar_Adj_Turb = solver[MESH_0][ADJTURB_SOL]->GetnVar();
+    
+    /*--- Additional Variables required for NEMO solver ---*/
+    
+    if (NEMO_euler || NEMO_ns) nPrimVar_NEMO     = solver[MESH_0][FLOW_SOL]->GetnPrimVar();
+    if (NEMO_euler || NEMO_ns) nPrimVarGrad_NEMO = solver[MESH_0][FLOW_SOL]->GetnPrimVarGrad();
+    
+    /*--- Definition of the Class for the numerical method:
+     numerics_container[INSTANCE_LEVEL][MESH_LEVEL][EQUATION][EQ_TERM] ---*/
+    
+    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+        numerics[iMGlevel] = new CNumerics** [MAX_SOLS];
+        for (iSol = 0; iSol < MAX_SOLS; iSol++)
+            numerics[iMGlevel][iSol] = new CNumerics* [MAX_TERMS*omp_get_max_threads()]();
+    }
+    
+    /*--- Instantiate one numerics object per thread for each required term. ---*/
+    
+    for (int thread = 0; thread < omp_get_max_threads(); ++thread)
+    {
+        const int offset = thread * MAX_TERMS;
+        
+        const int conv_term = CONV_TERM + offset;
+        const int visc_term = VISC_TERM + offset;
+        
+        const int source_first_term = SOURCE_FIRST_TERM + offset;
+        const int source_second_term = SOURCE_SECOND_TERM + offset;
+        
+        const int conv_bound_term = CONV_BOUND_TERM + offset;
+        const int visc_bound_term = VISC_BOUND_TERM + offset;
+        
+        const int fea_term = FEA_TERM + offset;
+        
+        /*--- Solver definition for the template problem ---*/
+        if (template_solver) {
+            
+            /*--- Definition of the convective scheme for each equation and mesh level ---*/
+            switch (config->GetKind_ConvNumScheme_Template()) {
+                case SPACE_CENTERED : case SPACE_UPWIND :
+                    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+                        numerics[iMGlevel][TEMPLATE_SOL][conv_term] = new CConvective_Template(nDim, nVar_Template, config);
+                    break;
+                default:
+                    SU2_MPI::Error("Convective scheme not implemented (template_solver).", CURRENT_FUNCTION);
+                    break;
+            }
+            
+            /*--- Definition of the viscous scheme for each equation and mesh level ---*/
+            for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+                numerics[iMGlevel][TEMPLATE_SOL][visc_term] = new CViscous_Template(nDim, nVar_Template, config);
+            
+            /*--- Definition of the source term integration scheme for each equation and mesh level ---*/
+            for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+                numerics[iMGlevel][TEMPLATE_SOL][source_first_term] = new CSource_Template(nDim, nVar_Template, config);
+            
+            /*--- Definition of the boundary condition method ---*/
+            for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                numerics[iMGlevel][TEMPLATE_SOL][conv_bound_term] = new CConvective_Template(nDim, nVar_Template, config);
+            }
+            
         }
-        break;
-      case STRUCT_DEFORMATION::LARGE:
-        switch (config->GetMaterialModel()) {
-          case STRUCT_MODEL::LINEAR_ELASTIC:
-            SU2_MPI::Error("Material model does not correspond to geometric conditions.", CURRENT_FUNCTION);
-            break;
-          case STRUCT_MODEL::NEO_HOOKEAN:
-            if (config->GetMaterialCompressibility() == STRUCT_COMPRESS::COMPRESSIBLE) {
-              numerics[MESH_0][FEA_SOL][fea_term] = new CFEM_NeoHookean_Comp(nDim, nVar_FEM, config);
-            } else {
-              SU2_MPI::Error("Material model not implemented.", CURRENT_FUNCTION);
+        
+        /*--- Solver definition for the Potential, Euler, Navier-Stokes problems ---*/
+        if ((euler) || (ns)) {
+            
+            /*--- Definition of the convective scheme for each equation and mesh level ---*/
+            switch (config->GetKind_ConvNumScheme_Flow()) {
+                case NO_CONVECTIVE :
+                    SU2_MPI::Error("Config file is missing the CONV_NUM_METHOD_FLOW option.", CURRENT_FUNCTION);
+                    break;
+                    
+                case SPACE_CENTERED :
+                    if (compressible) {
+                        /*--- "conv_term" is not instantiated as all compressible centered schemes are vectorized. ---*/
+                        
+                        /*--- Definition of the boundary condition method ---*/
+                        for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+                            numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwRoe_Flow(nDim, nVar_Flow, config, false);
+                        
+                    }
+                    if (incompressible) {
+                        /*--- Incompressible flow, use preconditioning method ---*/
+                        switch (config->GetKind_Centered_Flow()) {
+                            case LAX : numerics[MESH_0][FLOW_SOL][conv_term] = new CCentLaxInc_Flow(nDim, nVar_Flow, config); break;
+                            case JST : numerics[MESH_0][FLOW_SOL][conv_term] = new CCentJSTInc_Flow(nDim, nVar_Flow, config); break;
+                            default:
+                                SU2_MPI::Error("Invalid centered scheme or not implemented.\n Currently, only JST and LAX-FRIEDRICH are available for incompressible flows.", CURRENT_FUNCTION);
+                                break;
+                        }
+                        for (iMGlevel = 1; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+                            numerics[iMGlevel][FLOW_SOL][conv_term] = new CCentLaxInc_Flow(nDim, nVar_Flow, config);
+                        
+                        /*--- Definition of the boundary condition method ---*/
+                        for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+                            numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwFDSInc_Flow(nDim, nVar_Flow, config);
+                        
+                    }
+                    break;
+                case SPACE_UPWIND :
+                    if (compressible) {
+                        /*--- Compressible flow ---*/
+                        switch (config->GetKind_Upwind_Flow()) {
+                            case ROE:
+                                if (ideal_gas) {
+                                    
+                                    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                                        numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwRoe_Flow(nDim, nVar_Flow, config, roe_low_dissipation);
+                                        numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwRoe_Flow(nDim, nVar_Flow, config, false);
+                                    }
+                                } else {
+                                    
+                                    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                                        numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwGeneralRoe_Flow(nDim, nVar_Flow, config);
+                                        numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwGeneralRoe_Flow(nDim, nVar_Flow, config);
+                                    }
+                                }
+                                break;
+                                
+                            case AUSM:
+                                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                                    numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwAUSM_Flow(nDim, nVar_Flow, config);
+                                    numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwAUSM_Flow(nDim, nVar_Flow, config);
+                                }
+                                break;
+                                
+                            case AUSMPLUSUP:
+                                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                                    numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwAUSMPLUSUP_Flow(nDim, nVar_Flow, config);
+                                    numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwAUSMPLUSUP_Flow(nDim, nVar_Flow, config);
+                                }
+                                break;
+                                
+                            case AUSMPLUSUP2:
+                                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                                    numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwAUSMPLUSUP2_Flow(nDim, nVar_Flow, config);
+                                    numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwAUSMPLUSUP2_Flow(nDim, nVar_Flow, config);
+                                }
+                                break;
+                                
+                            case TURKEL:
+                                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                                    numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwTurkel_Flow(nDim, nVar_Flow, config);
+                                    numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwTurkel_Flow(nDim, nVar_Flow, config);
+                                }
+                                break;
+                                
+                            case L2ROE:
+                                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                                    numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwL2Roe_Flow(nDim, nVar_Flow, config);
+                                    numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwL2Roe_Flow(nDim, nVar_Flow, config);
+                                }
+                                break;
+                            case LMROE:
+                                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                                    numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwLMRoe_Flow(nDim, nVar_Flow, config);
+                                    numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwLMRoe_Flow(nDim, nVar_Flow, config);
+                                }
+                                break;
+                                
+                            case SLAU:
+                                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                                    numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwSLAU_Flow(nDim, nVar_Flow, config, roe_low_dissipation);
+                                    numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwSLAU_Flow(nDim, nVar_Flow, config, false);
+                                }
+                                break;
+                                
+                            case SLAU2:
+                                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                                    numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwSLAU2_Flow(nDim, nVar_Flow, config, roe_low_dissipation);
+                                    numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwSLAU2_Flow(nDim, nVar_Flow, config, false);
+                                }
+                                break;
+                                
+                            case HLLC:
+                                if (ideal_gas) {
+                                    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                                        numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwHLLC_Flow(nDim, nVar_Flow, config);
+                                        numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwHLLC_Flow(nDim, nVar_Flow, config);
+                                    }
+                                }
+                                else {
+                                    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                                        numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwGeneralHLLC_Flow(nDim, nVar_Flow, config);
+                                        numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwGeneralHLLC_Flow(nDim, nVar_Flow, config);
+                                    }
+                                }
+                                break;
+                                
+                            case MSW:
+                                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                                    numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwMSW_Flow(nDim, nVar_Flow, config);
+                                    numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwMSW_Flow(nDim, nVar_Flow, config);
+                                }
+                                break;
+                                
+                            case CUSP:
+                                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                                    numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwCUSP_Flow(nDim, nVar_Flow, config);
+                                    numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwCUSP_Flow(nDim, nVar_Flow, config);
+                                }
+                                break;
+                                
+                            default:
+                                SU2_MPI::Error("Invalid upwind scheme or not implemented.", CURRENT_FUNCTION);
+                                break;
+                        }
+                        
+                    }
+                    if (incompressible) {
+                        /*--- Incompressible flow, use artificial compressibility method ---*/
+                        switch (config->GetKind_Upwind_Flow()) {
+                            case FDS:
+                                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                                    numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwFDSInc_Flow(nDim, nVar_Flow, config);
+                                    numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwFDSInc_Flow(nDim, nVar_Flow, config);
+                                }
+                                break;
+                            default:
+                                SU2_MPI::Error("Invalid upwind scheme or not implemented.\n Currently, only FDS is available for incompressible flows.", CURRENT_FUNCTION);
+                                break;
+                        }
+                    }
+                    break;
+                    
+                default:
+                    SU2_MPI::Error("Invalid convective scheme for the Euler / Navier-Stokes equations.", CURRENT_FUNCTION);
+                    break;
             }
-            break;
-          case STRUCT_MODEL::KNOWLES:
-            if (config->GetMaterialCompressibility() == STRUCT_COMPRESS::NEARLY_INCOMP) {
-              numerics[MESH_0][FEA_SOL][fea_term] = new CFEM_Knowles_NearInc(nDim, nVar_FEM, config);
-            } else {
-              SU2_MPI::Error("Material model not implemented.", CURRENT_FUNCTION);
+            
+            /*--- Definition of the viscous scheme for each equation and mesh level ---*/
+            if (compressible) {
+                if (ideal_gas) {
+                    
+                    /*--- Compressible flow Ideal gas ---*/
+                    numerics[MESH_0][FLOW_SOL][visc_term] = new CAvgGrad_Flow(nDim, nVar_Flow, true, config);
+                    for (iMGlevel = 1; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+                        numerics[iMGlevel][FLOW_SOL][visc_term] = new CAvgGrad_Flow(nDim, nVar_Flow, false, config);
+                    
+                    /*--- Definition of the boundary condition method ---*/
+                    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+                        numerics[iMGlevel][FLOW_SOL][visc_bound_term] = new CAvgGrad_Flow(nDim, nVar_Flow, false, config);
+                    
+                } else {
+                    
+                    /*--- Compressible flow Real gas ---*/
+                    numerics[MESH_0][FLOW_SOL][visc_term] = new CGeneralAvgGrad_Flow(nDim, nVar_Flow, true, config);
+                    for (iMGlevel = 1; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+                        numerics[iMGlevel][FLOW_SOL][visc_term] = new CGeneralAvgGrad_Flow(nDim, nVar_Flow, false, config);
+                    
+                    /*--- Definition of the boundary condition method ---*/
+                    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+                        numerics[iMGlevel][FLOW_SOL][visc_bound_term] = new CGeneralAvgGrad_Flow(nDim, nVar_Flow, false, config);
+                    
+                }
             }
-            break;
-          case STRUCT_MODEL::IDEAL_DE:
-            if (config->GetMaterialCompressibility() == STRUCT_COMPRESS::NEARLY_INCOMP) {
-              numerics[MESH_0][FEA_SOL][fea_term] = new CFEM_IdealDE(nDim, nVar_FEM, config);
-            } else {
-              SU2_MPI::Error("Material model not implemented.", CURRENT_FUNCTION);
+            if (incompressible) {
+                /*--- Incompressible flow, use preconditioning method ---*/
+                numerics[MESH_0][FLOW_SOL][visc_term] = new CAvgGradInc_Flow(nDim, nVar_Flow, true, config);
+                for (iMGlevel = 1; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+                    numerics[iMGlevel][FLOW_SOL][visc_term] = new CAvgGradInc_Flow(nDim, nVar_Flow, false, config);
+                
+                /*--- Definition of the boundary condition method ---*/
+                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+                    numerics[iMGlevel][FLOW_SOL][visc_bound_term] = new CAvgGradInc_Flow(nDim, nVar_Flow, false, config);
             }
-            break;
+            
+            /*--- Definition of the source term integration scheme for each equation and mesh level ---*/
+            for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                
+                if (config->GetBody_Force() == YES) {
+                    if (incompressible)
+                        numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceIncBodyForce(nDim, nVar_Flow, config);
+                    else
+                        numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceBodyForce(nDim, nVar_Flow, config);
+                }
+                else if (incompressible && (config->GetKind_Streamwise_Periodic() != ENUM_STREAMWISE_PERIODIC::NONE)) {
+                    numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceIncStreamwise_Periodic(nDim, nVar_Flow, config);
+                }
+                else if (incompressible && (config->GetKind_DensityModel() == INC_DENSITYMODEL::BOUSSINESQ)) {
+                    numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceBoussinesq(nDim, nVar_Flow, config);
+                }
+                else if (config->GetRotating_Frame() == YES) {
+                    if (incompressible)
+                        numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceIncRotatingFrame_Flow(nDim, nVar_Flow, config);
+                    else
+                        numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceRotatingFrame_Flow(nDim, nVar_Flow, config);
+                }
+                else if (config->GetAxisymmetric() == YES) {
+                    if (incompressible)
+                        numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceIncAxisymmetric_Flow(nDim, nVar_Flow, config);
+                    else if (ideal_gas)
+                        numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceAxisymmetric_Flow(nDim, nVar_Flow, config);
+                    else
+                        numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceGeneralAxisymmetric_Flow(nDim, nVar_Flow, config);
+                }
+                else if (config->GetGravityForce() == YES) {
+                    numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceGravity(nDim, nVar_Flow, config);
+                }
+                else if (config->GetWind_Gust() == YES) {
+                    numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceWindGust(nDim, nVar_Flow, config);
+                }
+                else {
+                    numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceNothing(nDim, nVar_Flow, config);
+                }
+                
+                /*--- At the moment it is necessary to have the RHT equation in order to have a volumetric heat source. ---*/
+                if (config->AddRadiation())
+                    numerics[iMGlevel][FLOW_SOL][source_second_term] = new CSourceRadiation(nDim, nVar_Flow, config);
+                else if ((incompressible && (config->GetKind_Streamwise_Periodic() != ENUM_STREAMWISE_PERIODIC::NONE)) &&
+                         (config->GetEnergy_Equation() && !config->GetStreamwise_Periodic_Temperature()))
+                    numerics[iMGlevel][FLOW_SOL][source_second_term] = new CSourceIncStreamwisePeriodic_Outlet(nDim, nVar_Flow, config);
+                else
+                    numerics[iMGlevel][FLOW_SOL][source_second_term] = new CSourceNothing(nDim, nVar_Flow, config);
+            }
+            
         }
-        break;
-    }
-
-    /*--- The following definitions only make sense if we have a non-linear solution. ---*/
-    if (config->GetGeometricConditions() == STRUCT_DEFORMATION::LARGE) {
-
-      /*--- This allocates a container for electromechanical effects. ---*/
-
-      bool de_effects = config->GetDE_Effects();
-      if (de_effects)
-        numerics[MESH_0][FEA_SOL][DE_TERM+offset] = new CFEM_DielectricElastomer(nDim, nVar_FEM, config);
-
-      ifstream properties_file;
-
-      string filename = config->GetFEA_FileName();
-      if (nZone > 1)
-        filename = config->GetMultizone_FileName(filename, iZone, ".dat");
-
-      properties_file.open(filename.data(), ios::in);
-
-      /*--- In case there is a properties file, containers are allocated for a number of material models. ---*/
-
-      if (!(properties_file.fail())) {
-        numerics[MESH_0][FEA_SOL][MAT_NHCOMP+offset]  = new CFEM_NeoHookean_Comp(nDim, nVar_FEM, config);
-        numerics[MESH_0][FEA_SOL][MAT_IDEALDE+offset] = new CFEM_IdealDE(nDim, nVar_FEM, config);
-        numerics[MESH_0][FEA_SOL][MAT_KNOWLES+offset] = new CFEM_Knowles_NearInc(nDim, nVar_FEM, config);
-      }
-    }
-  }
-
-  /*--- Instantiate the numerics for the mesh solver. ---*/
-  if (config->GetDeform_Mesh())
-    numerics[MESH_0][MESH_SOL][fea_term] = new CFEAMeshElasticity(nDim, nDim, geometry[MESH_0]->GetnElem(), config);
-
-  } // end "per-thread" allocation loop
-
+        
+        /*--- Solver definition for the Potential, Euler, Navier-Stokes NEMO problems ---*/
+        
+        if (NEMO_euler || NEMO_ns) {
+            
+            /*--- Definition of the convective scheme for each equation and mesh level ---*/
+            switch (config->GetKind_ConvNumScheme_Flow()) {
+                case NO_CONVECTIVE :
+                    SU2_MPI::Error("Config file is missing the CONV_NUM_METHOD_FLOW option.", CURRENT_FUNCTION);
+                    break;
+                    
+                case SPACE_CENTERED :
+                    if (compressible) {
+                        /*--- Compressible flow ---*/
+                        switch (config->GetKind_Centered_Flow()) {
+                            case LAX : numerics[MESH_0][FLOW_SOL][conv_term] = new CCentLax_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config); break;
+                            default:
+                                SU2_MPI::Error("Invalid centered scheme or not implemented.", CURRENT_FUNCTION);
+                                break;
+                        }
+                        
+                        for (iMGlevel = 1; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+                            numerics[iMGlevel][FLOW_SOL][conv_term] = new CCentLax_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
+                        
+                        /*--- Definition of the boundary condition method ---*/
+                        for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+                            numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwRoe_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
+                    }
+                    break;
+                case SPACE_UPWIND :
+                    if (compressible) {
+                        /*--- Compressible flow ---*/
+                        switch (config->GetKind_Upwind_Flow()) {
+                            case ROE:
+                                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                                    numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwRoe_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
+                                    numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwRoe_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
+                                }
+                                break;
+                                
+                            case AUSM:
+                                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                                    numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwAUSM_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
+                                    numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwAUSM_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
+                                }
+                                break;
+                                
+                            case AUSMPLUSUP2:
+                                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                                    numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwAUSMPLUSUP2_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
+                                    numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwAUSMPLUSUP2_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
+                                }
+                                break;
+                                
+                            case MSW:
+                                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                                    numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwMSW_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
+                                    numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwMSW_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
+                                }
+                                break;
+                                
+                            case AUSMPWPLUS:
+                                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                                    numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwAUSMPWplus_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
+                                    numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwAUSMPWplus_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
+                                }
+                                break;
+                                
+                            default:
+                                SU2_MPI::Error("Invalid upwind scheme or not implemented.", CURRENT_FUNCTION);
+                                break;
+                        }
+                        
+                    }
+                    break;
+                    
+                default:
+                    SU2_MPI::Error("Invalid convective scheme for the NEMO Euler / Navier-Stokes equations.", CURRENT_FUNCTION);
+                    break;
+            }
+            
+            /*--- Definition of the viscous scheme for each equation and mesh level ---*/
+            if (compressible) {
+                
+                numerics[MESH_0][FLOW_SOL][visc_term] = new CAvgGradCorrected_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
+                for (iMGlevel = 1; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+                    numerics[iMGlevel][FLOW_SOL][visc_term] = new CAvgGrad_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
+                
+                /*--- Definition of the boundary condition method ---*/
+                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+                    numerics[iMGlevel][FLOW_SOL][visc_bound_term] = new CAvgGrad_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
+            }
+            
+            /*--- Definition of the source term integration scheme for each equation and mesh level ---*/
+            for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                
+                numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSource_NEMO(nDim, nVar_NEMO, nPrimVar_NEMO, nPrimVarGrad_NEMO, config);
+                numerics[iMGlevel][FLOW_SOL][source_second_term] = new CSourceNothing(nDim, nVar_NEMO, config);
+            }
+        }
+        
+        /*--- Riemann solver definition for the Euler, Navier-Stokes problems for the FEM discretization. ---*/
+        if ((fem_euler) || (fem_ns)) {
+            
+            switch (config->GetRiemann_Solver_FEM()) {
+                case ROE:
+                case LAX_FRIEDRICH:
+                    /* Hard coded optimized implementation is used in the DG solver. No need to allocate the
+                     corresponding entry in numerics. */
+                    break;
+                    
+                case AUSM:
+                    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                        numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwAUSM_Flow(nDim, nVar_Flow, config);
+                        numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwAUSM_Flow(nDim, nVar_Flow, config);
+                    }
+                    break;
+                    
+                case TURKEL:
+                    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                        numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwTurkel_Flow(nDim, nVar_Flow, config);
+                        numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwTurkel_Flow(nDim, nVar_Flow, config);
+                    }
+                    break;
+                    
+                case HLLC:
+                    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                        numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwHLLC_Flow(nDim, nVar_Flow, config);
+                        numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwHLLC_Flow(nDim, nVar_Flow, config);
+                    }
+                    break;
+                    
+                case MSW:
+                    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                        numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwMSW_Flow(nDim, nVar_Flow, config);
+                        numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwMSW_Flow(nDim, nVar_Flow, config);
+                    }
+                    break;
+                    
+                case CUSP:
+                    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                        numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwCUSP_Flow(nDim, nVar_Flow, config);
+                        numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwCUSP_Flow(nDim, nVar_Flow, config);
+                    }
+                    break;
+                    
+                default:
+                    SU2_MPI::Error("Riemann solver not implemented.", CURRENT_FUNCTION);
+                    break;
+            }
+            
+        }
+        
+        /*--- Solver definition for the turbulent model problem ---*/
+        
+        if (turbulent) {
+            if (incompressible)
+                InstantiateTurbulentNumerics<CIncEulerVariable::CIndices<unsigned short> >(nVar_Turb, offset, config,
+                                                                                           solver[MESH_0][TURB_SOL], numerics);
+            else if (NEMO_ns)
+                InstantiateTurbulentNumerics<CNEMOEulerVariable::CIndices<unsigned short> >(nVar_Turb, offset, config,
+                                                                                            solver[MESH_0][TURB_SOL], numerics);
+            else
+                InstantiateTurbulentNumerics<CEulerVariable::CIndices<unsigned short> >(nVar_Turb, offset, config,
+                                                                                        solver[MESH_0][TURB_SOL], numerics);
+        }
+        
+        /*--- Solver definition for the transition model problem ---*/
+        if (transition) {
+            
+            /*--- Definition of the convective scheme for each equation and mesh level ---*/
+            switch (config->GetKind_ConvNumScheme_Turb()) {
+                case NO_UPWIND:
+                    SU2_MPI::Error("Config file is missing the CONV_NUM_METHOD_TURB option.", CURRENT_FUNCTION);
+                    break;
+                case SPACE_UPWIND:
+                    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                        numerics[iMGlevel][TRANS_SOL][conv_term] = new CUpwSca_TransLM(nDim, nVar_Trans, config);
+                    }
+                    break;
+                default:
+                    SU2_MPI::Error("Invalid convective scheme for the transition equations.", CURRENT_FUNCTION);
+                    break;
+            }
+            
+            /*--- Definition of the viscous scheme for each equation and mesh level ---*/
+            for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                numerics[iMGlevel][TRANS_SOL][visc_term] = new CAvgGradCorrected_TransLM(nDim, nVar_Trans, config);
+            }
+            
+            /*--- Definition of the source term integration scheme for each equation and mesh level ---*/
+            for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                numerics[iMGlevel][TRANS_SOL][source_first_term] = new CSourcePieceWise_TransLM(nDim, nVar_Trans, config);
+                numerics[iMGlevel][TRANS_SOL][source_second_term] = new CSourceNothing(nDim, nVar_Trans, config);
+            }
+            
+            /*--- Definition of the boundary condition method ---*/
+            for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                numerics[iMGlevel][TRANS_SOL][conv_bound_term] = new CUpwLin_TransLM(nDim, nVar_Trans, config);
+            }
+        }
+        
+        /*--- Solver definition for the species transport problem ---*/
+        
+        if (species) {
+            if (incompressible)
+                InstantiateSpeciesNumerics<CIncEulerVariable::CIndices<unsigned short> >(nVar_Species, offset, config,
+                                                                                         solver[MESH_0][SPECIES_SOL], numerics);
+            else if (compressible)
+                InstantiateSpeciesNumerics<CEulerVariable::CIndices<unsigned short> >(nVar_Species, offset, config,
+                                                                                      solver[MESH_0][SPECIES_SOL], numerics);
+            else
+                SU2_MPI::Error("Species transport only available for standard compressible and incompressible flow.", CURRENT_FUNCTION);
+        }
+        
+        /*--- Solver definition of the finite volume heat solver  ---*/
+        if (heat) {
+            
+            /*--- Definition of the viscous scheme for each equation and mesh level ---*/
+            for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                
+                numerics[iMGlevel][HEAT_SOL][visc_term] = new CAvgGrad_Heat(nDim, nVar_Heat, config, true);
+                numerics[iMGlevel][HEAT_SOL][visc_bound_term] = new CAvgGrad_Heat(nDim, nVar_Heat, config, false);
+                
+                switch (config->GetKind_ConvNumScheme_Heat()) {
+                        
+                    case SPACE_UPWIND :
+                        numerics[iMGlevel][HEAT_SOL][conv_term] = new CUpwSca_Heat(nDim, nVar_Heat, config);
+                        numerics[iMGlevel][HEAT_SOL][conv_bound_term] = new CUpwSca_Heat(nDim, nVar_Heat, config);
+                        break;
+                        
+                    case SPACE_CENTERED :
+                        numerics[iMGlevel][HEAT_SOL][conv_term] = new CCentSca_Heat(nDim, nVar_Heat, config);
+                        numerics[iMGlevel][HEAT_SOL][conv_bound_term] = new CUpwSca_Heat(nDim, nVar_Heat, config);
+                        break;
+                        
+                    default:
+                        SU2_MPI::Error("Invalid convective scheme for the heat transfer equations.", CURRENT_FUNCTION);
+                        break;
+                }
+            }
+        }
+        
+        /*--- Solver definition for the radiation model problem ---*/
+        
+        if (config->AddRadiation()) {
+            /*--- Definition of the viscous scheme for each equation and mesh level ---*/
+            numerics[MESH_0][RAD_SOL][VISC_TERM] = new CAvgGradCorrected_P1(nDim, nVar_Rad, config);
+            
+            /*--- Definition of the source term integration scheme for each equation and mesh level ---*/
+            numerics[MESH_0][RAD_SOL][SOURCE_FIRST_TERM] = new CSourceP1(nDim, nVar_Rad, config);
+            
+            /*--- Definition of the boundary condition method ---*/
+            numerics[MESH_0][RAD_SOL][VISC_BOUND_TERM] = new CAvgGradCorrected_P1(nDim, nVar_Rad, config);
+        }
+        
+        /*--- Solver definition for the flow adjoint problem ---*/
+        
+        if (adj_euler || adj_ns) {
+            
+            if (incompressible)
+                SU2_MPI::Error("Convective schemes not implemented for incompressible continuous adjoint.", CURRENT_FUNCTION);
+            
+            /*--- Definition of the convective scheme for each equation and mesh level ---*/
+            
+            switch (config->GetKind_ConvNumScheme_AdjFlow()) {
+                case NO_CONVECTIVE:
+                    SU2_MPI::Error("Config file is missing the CONV_NUM_METHOD_ADJFLOW option.", CURRENT_FUNCTION);
+                    break;
+                    
+                case SPACE_CENTERED :
+                    
+                    if (compressible) {
+                        
+                        /*--- Compressible flow ---*/
+                        
+                        switch (config->GetKind_Centered_AdjFlow()) {
+                            case LAX : numerics[MESH_0][ADJFLOW_SOL][conv_term] = new CCentLax_AdjFlow(nDim, nVar_Adj_Flow, config); break;
+                            case JST : numerics[MESH_0][ADJFLOW_SOL][conv_term] = new CCentJST_AdjFlow(nDim, nVar_Adj_Flow, config); break;
+                            default:
+                                SU2_MPI::Error("Centered scheme not implemented.", CURRENT_FUNCTION);
+                                break;
+                        }
+                        
+                        for (iMGlevel = 1; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+                            numerics[iMGlevel][ADJFLOW_SOL][conv_term] = new CCentLax_AdjFlow(nDim, nVar_Adj_Flow, config);
+                        
+                        for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+                            numerics[iMGlevel][ADJFLOW_SOL][conv_bound_term] = new CUpwRoe_AdjFlow(nDim, nVar_Adj_Flow, config);
+                        
+                    }
+                    break;
+                    
+                case SPACE_UPWIND :
+                    
+                    if (compressible) {
+                        
+                        /*--- Compressible flow ---*/
+                        
+                        switch (config->GetKind_Upwind_AdjFlow()) {
+                            case ROE:
+                                for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                                    numerics[iMGlevel][ADJFLOW_SOL][conv_term] = new CUpwRoe_AdjFlow(nDim, nVar_Adj_Flow, config);
+                                    numerics[iMGlevel][ADJFLOW_SOL][conv_bound_term] = new CUpwRoe_AdjFlow(nDim, nVar_Adj_Flow, config);
+                                }
+                                break;
+                            default:
+                                SU2_MPI::Error("Upwind scheme not implemented.", CURRENT_FUNCTION);
+                                break;
+                        }
+                    }
+                    break;
+                    
+                default:
+                    SU2_MPI::Error("Invalid convective scheme for the continuous adjoint Euler / Navier-Stokes equations.", CURRENT_FUNCTION);
+                    break;
+            }
+            
+            /*--- Definition of the viscous scheme for each equation and mesh level ---*/
+            
+            if (compressible) {
+                
+                /*--- Compressible flow ---*/
+                
+                numerics[MESH_0][ADJFLOW_SOL][visc_term] = new CAvgGradCorrected_AdjFlow(nDim, nVar_Adj_Flow, config);
+                numerics[MESH_0][ADJFLOW_SOL][visc_bound_term] = new CAvgGrad_AdjFlow(nDim, nVar_Adj_Flow, config);
+                
+                for (iMGlevel = 1; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                    numerics[iMGlevel][ADJFLOW_SOL][visc_term] = new CAvgGrad_AdjFlow(nDim, nVar_Adj_Flow, config);
+                    numerics[iMGlevel][ADJFLOW_SOL][visc_bound_term] = new CAvgGrad_AdjFlow(nDim, nVar_Adj_Flow, config);
+                }
+                
+            }
+            
+            /*--- Definition of the source term integration scheme for each equation and mesh level ---*/
+            
+            for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                
+                /*--- Note that RANS is incompatible with Axisymmetric or Rotational (Fix it!) ---*/
+                
+                if (compressible) {
+                    
+                    if (adj_ns) {
+                        
+                        numerics[iMGlevel][ADJFLOW_SOL][source_first_term] = new CSourceViscous_AdjFlow(nDim, nVar_Adj_Flow, config);
+                        
+                        if (config->GetRotating_Frame() == YES)
+                            numerics[iMGlevel][ADJFLOW_SOL][source_second_term] = new CSourceRotatingFrame_AdjFlow(nDim, nVar_Adj_Flow, config);
+                        else
+                            numerics[iMGlevel][ADJFLOW_SOL][source_second_term] = new CSourceConservative_AdjFlow(nDim, nVar_Adj_Flow, config);
+                        
+                    }
+                    
+                    else {
+                        
+                        if (config->GetRotating_Frame() == YES)
+                            numerics[iMGlevel][ADJFLOW_SOL][source_first_term] = new CSourceRotatingFrame_AdjFlow(nDim, nVar_Adj_Flow, config);
+                        else if (config->GetAxisymmetric() == YES)
+                            numerics[iMGlevel][ADJFLOW_SOL][source_first_term] = new CSourceAxisymmetric_AdjFlow(nDim, nVar_Adj_Flow, config);
+                        else
+                            numerics[iMGlevel][ADJFLOW_SOL][source_first_term] = new CSourceNothing(nDim, nVar_Adj_Flow, config);
+                        
+                        numerics[iMGlevel][ADJFLOW_SOL][source_second_term] = new CSourceNothing(nDim, nVar_Adj_Flow, config);
+                        
+                    }
+                    
+                }
+                
+            }
+            
+        }
+        
+        /*--- Solver definition for the turbulent adjoint problem ---*/
+        if (adj_turb) {
+            
+            if (config->GetKind_Turb_Model() != TURB_MODEL::SA)
+                SU2_MPI::Error("Only the SA turbulence model can be used with the continuous adjoint solver.", CURRENT_FUNCTION);
+            
+            /*--- Definition of the convective scheme for each equation and mesh level ---*/
+            switch (config->GetKind_ConvNumScheme_AdjTurb()) {
+                case NO_CONVECTIVE:
+                    SU2_MPI::Error("Config file is missing the CONV_NUM_METHOD_ADJTURB option.", CURRENT_FUNCTION);
+                    break;
+                case SPACE_UPWIND :
+                    for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+                        numerics[iMGlevel][ADJTURB_SOL][conv_term] = new CUpwSca_AdjTurb(nDim, nVar_Adj_Turb, config);
+                    break;
+                default:
+                    SU2_MPI::Error("Convective scheme not implemented (adjoint turbulence).", CURRENT_FUNCTION);
+                    break;
+            }
+            
+            /*--- Definition of the viscous scheme for each equation and mesh level ---*/
+            for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+                numerics[iMGlevel][ADJTURB_SOL][visc_term] = new CAvgGradCorrected_AdjTurb(nDim, nVar_Adj_Turb, config);
+            
+            /*--- Definition of the source term integration scheme for each equation and mesh level ---*/
+            for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+                numerics[iMGlevel][ADJTURB_SOL][source_first_term] = new CSourcePieceWise_AdjTurb(nDim, nVar_Adj_Turb, config);
+                numerics[iMGlevel][ADJTURB_SOL][source_second_term] = new CSourceConservative_AdjTurb(nDim, nVar_Adj_Turb, config);
+            }
+            
+            /*--- Definition of the boundary condition method ---*/
+            for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+                numerics[iMGlevel][ADJTURB_SOL][conv_bound_term] = new CUpwLin_AdjTurb(nDim, nVar_Adj_Turb, config);
+            
+        }
+        
+        /*--- Numerics definition for FEM-like problems. ---*/
+        
+        if (fem) {
+            /*--- Initialize the container for FEA_TERM. This will be the only one for most of the cases. ---*/
+            switch (config->GetGeometricConditions()) {
+                case STRUCT_DEFORMATION::SMALL:
+                    switch (config->GetMaterialModel()) {
+                        case STRUCT_MODEL::LINEAR_ELASTIC:
+                            numerics[MESH_0][FEA_SOL][fea_term] = new CFEALinearElasticity(nDim, nVar_FEM, config);
+                            break;
+                        default:
+                            SU2_MPI::Error("Material model does not correspond to geometric conditions.", CURRENT_FUNCTION);
+                            break;
+                    }
+                    break;
+                case STRUCT_DEFORMATION::LARGE:
+                    switch (config->GetMaterialModel()) {
+                        case STRUCT_MODEL::LINEAR_ELASTIC:
+                            SU2_MPI::Error("Material model does not correspond to geometric conditions.", CURRENT_FUNCTION);
+                            break;
+                        case STRUCT_MODEL::NEO_HOOKEAN:
+                            if (config->GetMaterialCompressibility() == STRUCT_COMPRESS::COMPRESSIBLE) {
+                                numerics[MESH_0][FEA_SOL][fea_term] = new CFEM_NeoHookean_Comp(nDim, nVar_FEM, config);
+                            } else {
+                                SU2_MPI::Error("Material model not implemented.", CURRENT_FUNCTION);
+                            }
+                            break;
+                        case STRUCT_MODEL::KNOWLES:
+                            if (config->GetMaterialCompressibility() == STRUCT_COMPRESS::NEARLY_INCOMP) {
+                                numerics[MESH_0][FEA_SOL][fea_term] = new CFEM_Knowles_NearInc(nDim, nVar_FEM, config);
+                            } else {
+                                SU2_MPI::Error("Material model not implemented.", CURRENT_FUNCTION);
+                            }
+                            break;
+                        case STRUCT_MODEL::IDEAL_DE:
+                            if (config->GetMaterialCompressibility() == STRUCT_COMPRESS::NEARLY_INCOMP) {
+                                numerics[MESH_0][FEA_SOL][fea_term] = new CFEM_IdealDE(nDim, nVar_FEM, config);
+                            } else {
+                                SU2_MPI::Error("Material model not implemented.", CURRENT_FUNCTION);
+                            }
+                            break;
+                    }
+                    break;
+            }
+            
+            /*--- The following definitions only make sense if we have a non-linear solution. ---*/
+            if (config->GetGeometricConditions() == STRUCT_DEFORMATION::LARGE) {
+                
+                /*--- This allocates a container for electromechanical effects. ---*/
+                
+                bool de_effects = config->GetDE_Effects();
+                if (de_effects)
+                    numerics[MESH_0][FEA_SOL][DE_TERM+offset] = new CFEM_DielectricElastomer(nDim, nVar_FEM, config);
+                
+                ifstream properties_file;
+                
+                string filename = config->GetFEA_FileName();
+                if (nZone > 1)
+                    filename = config->GetMultizone_FileName(filename, iZone, ".dat");
+                
+                properties_file.open(filename.data(), ios::in);
+                
+                /*--- In case there is a properties file, containers are allocated for a number of material models. ---*/
+                
+                if (!(properties_file.fail())) {
+                    numerics[MESH_0][FEA_SOL][MAT_NHCOMP+offset]  = new CFEM_NeoHookean_Comp(nDim, nVar_FEM, config);
+                    numerics[MESH_0][FEA_SOL][MAT_IDEALDE+offset] = new CFEM_IdealDE(nDim, nVar_FEM, config);
+                    numerics[MESH_0][FEA_SOL][MAT_KNOWLES+offset] = new CFEM_Knowles_NearInc(nDim, nVar_FEM, config);
+                }
+            }
+        }
+        
+        /*--- Instantiate the numerics for the mesh solver. ---*/
+        if (config->GetDeform_Mesh())
+            numerics[MESH_0][MESH_SOL][fea_term] = new CFEAMeshElasticity(nDim, nDim, geometry[MESH_0]->GetnElem(), config);
+        
+    } // end "per-thread" allocation loop
+    
 }
 
 void CDriver::Numerics_Postprocessing(CNumerics *****numerics, CSolver***, CGeometry**,
                                       CConfig *config, unsigned short val_iInst) {
-
-  for (unsigned short iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-
-    for (unsigned int iSol = 0; iSol < MAX_SOLS; iSol++) {
-
-      for (unsigned int iTerm = 0; iTerm < MAX_TERMS*omp_get_max_threads(); iTerm++) {
-
-        delete numerics[val_iInst][iMGlevel][iSol][iTerm];
-      }
-      delete [] numerics[val_iInst][iMGlevel][iSol];
+    
+    for (unsigned short iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
+        
+        for (unsigned int iSol = 0; iSol < MAX_SOLS; iSol++) {
+            
+            for (unsigned int iTerm = 0; iTerm < MAX_TERMS*omp_get_max_threads(); iTerm++) {
+                
+                delete numerics[val_iInst][iMGlevel][iSol][iTerm];
+            }
+            delete [] numerics[val_iInst][iMGlevel][iSol];
+        }
+        delete[] numerics[val_iInst][iMGlevel];
     }
-    delete[] numerics[val_iInst][iMGlevel];
-  }
-  delete[] numerics[val_iInst];
-
+    delete[] numerics[val_iInst];
+    
 }
 
 void CDriver::Iteration_Preprocessing(CConfig* config, CIteration *&iteration) const {
-
-  if (rank == MASTER_NODE)
-    cout << endl <<"------------------- Iteration Preprocessing ( Zone " << config->GetiZone() <<" ) ------------------" << endl;
-
-  iteration = CIterationFactory::CreateIteration(config->GetKind_Solver(), config);
-
+    
+    if (rank == MASTER_NODE)
+        cout << endl <<"------------------- Iteration Preprocessing ( Zone " << config->GetiZone() <<" ) ------------------" << endl;
+    
+    iteration = CIterationFactory::CreateIteration(config->GetKind_Solver(), config);
+    
 }
 
 void CDriver::DynamicMesh_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***solver, CIteration* iteration,
                                         CVolumetricMovement *&grid_movement, CSurfaceMovement *&surface_movement) const{
-
-  /*--- Instantiate the geometry movement classes for the solution of unsteady
-   flows on dynamic meshes, including rigid mesh transformations, dynamically
-   deforming meshes, and preprocessing of harmonic balance. ---*/
-
-  if (!fem_solver && (config->GetGrid_Movement() || (config->GetDirectDiff() == D_DESIGN))) {
-    if (rank == MASTER_NODE)
-      cout << "Setting dynamic mesh structure for zone "<< iZone + 1<<"." << endl;
-    grid_movement = new CVolumetricMovement(geometry[MESH_0], config);
-
-    surface_movement = new CSurfaceMovement();
-    surface_movement->CopyBoundary(geometry[MESH_0], config);
-    if (config->GetTime_Marching() == TIME_MARCHING::HARMONIC_BALANCE){
-      if (rank == MASTER_NODE) cout << endl <<  "Instance "<< iInst + 1 <<":" << endl;
-      iteration->SetGrid_Movement(geometry, surface_movement, grid_movement,  solver, config, 0, iInst);
+    
+    /*--- Instantiate the geometry movement classes for the solution of unsteady
+     flows on dynamic meshes, including rigid mesh transformations, dynamically
+     deforming meshes, and preprocessing of harmonic balance. ---*/
+    
+    if (!fem_solver && (config->GetGrid_Movement() || (config->GetDirectDiff() == D_DESIGN))) {
+        if (rank == MASTER_NODE)
+            cout << "Setting dynamic mesh structure for zone "<< iZone + 1<<"." << endl;
+        grid_movement = new CVolumetricMovement(geometry[MESH_0], config);
+        
+        surface_movement = new CSurfaceMovement();
+        surface_movement->CopyBoundary(geometry[MESH_0], config);
+        if (config->GetTime_Marching() == TIME_MARCHING::HARMONIC_BALANCE){
+            if (rank == MASTER_NODE) cout << endl <<  "Instance "<< iInst + 1 <<":" << endl;
+            iteration->SetGrid_Movement(geometry, surface_movement, grid_movement,  solver, config, 0, iInst);
+        }
     }
-  }
-
-  if (config->GetDirectDiff() == D_DESIGN) {
-    if (rank == MASTER_NODE)
-      cout << "Setting surface/volume derivatives." << endl;
-
-    /*--- Set the surface derivatives, i.e. the derivative of the surface mesh nodes with respect to the design variables ---*/
-
-    surface_movement->SetSurface_Derivative(geometry[MESH_0],config);
-
-    /*--- Call the volume deformation routine with derivative mode enabled.
-       This computes the derivative of the volume mesh with respect to the surface nodes ---*/
-
-    grid_movement->SetVolume_Deformation(geometry[MESH_0],config, true, true);
-
-    /*--- Update the multi-grid structure to propagate the derivative information to the coarser levels ---*/
-
-    CGeometry::UpdateGeometry(geometry,config);
-
-  }
-
+    
+    if (config->GetDirectDiff() == D_DESIGN) {
+        if (rank == MASTER_NODE)
+            cout << "Setting surface/volume derivatives." << endl;
+        
+        /*--- Set the surface derivatives, i.e. the derivative of the surface mesh nodes with respect to the design variables ---*/
+        
+        surface_movement->SetSurface_Derivative(geometry[MESH_0],config);
+        
+        /*--- Call the volume deformation routine with derivative mode enabled.
+         This computes the derivative of the volume mesh with respect to the surface nodes ---*/
+        
+        grid_movement->SetVolume_Deformation(geometry[MESH_0],config, true, true);
+        
+        /*--- Update the multi-grid structure to propagate the derivative information to the coarser levels ---*/
+        
+        CGeometry::UpdateGeometry(geometry,config);
+        
+    }
+    
 }
 
 void CDriver::Interface_Preprocessing(CConfig **config, CSolver***** solver, CGeometry**** geometry,
                                       unsigned short** interface_types, CInterface ***interface,
                                       vector<vector<unique_ptr<CInterpolator> > >& interpolation) {
-
-  /*--- Setup interpolation and transfer for all possible donor/target pairs. ---*/
-
-  for (auto target = 0u; target < nZone; target++) {
-
-    for (auto donor = 0u; donor < nZone; donor++) {
-
-      /*--- Aliases to make code less verbose. ---*/
-      auto& interface_type = interface_types[donor][target];
-
-      if (donor == target) {
-        interface_type = ZONES_ARE_EQUAL;
-        continue;
-      }
-      interface_type = NO_TRANSFER;
-
-      /*--- If there is a common interface setup the interpolation and transfer. ---*/
-
-      if (!CInterpolator::CheckZonesInterface(config[donor], config[target])) {
-        interface_type = NO_COMMON_INTERFACE;
-      }
-      else {
-        /*--- Begin the creation of the communication pattern among zones. ---*/
-
-        if (rank == MASTER_NODE) cout << "From zone " << donor << " to zone " << target << ":" << endl;
-
-        /*--- Setup the interpolation. ---*/
-
-        interpolation[donor][target] = unique_ptr<CInterpolator>(CInterpolatorFactory::CreateInterpolator(
-                                       geometry, config, interpolation[target][donor].get(), donor, target));
-
-        /*--- The type of variables transferred depends on the donor/target physics. ---*/
-
-        const bool heat_target = config[target]->GetHeatProblem();
-        const bool fluid_target = config[target]->GetFluidProblem();
-        const bool structural_target = config[target]->GetStructuralProblem();
-
-        const bool heat_donor = config[donor]->GetHeatProblem();
-        const bool fluid_donor = config[donor]->GetFluidProblem();
-        const bool structural_donor = config[donor]->GetStructuralProblem();
-
-        /*--- Initialize the appropriate transfer strategy. ---*/
-
-        if (rank == MASTER_NODE) cout << " Transferring ";
-
-        if (fluid_donor && structural_target) {
-          interface_type = FLOW_TRACTION;
-          auto nConst = 2;
-          bool conservative = config[target]->GetConservativeInterpolation();
-          if(!config[ZONE_0]->GetDiscrete_Adjoint()) {
-            interface[donor][target] = new CFlowTractionInterface(nDim, nConst, config[donor], conservative);
-          } else {
-            interface[donor][target] = new CDiscAdjFlowTractionInterface(nDim, nConst, config[donor], conservative);
-          }
-          if (rank == MASTER_NODE) cout << "fluid " << (conservative? "forces." : "tractions.") << endl;
-        }
-        else if (structural_donor && (fluid_target || heat_target)) {
-          if (solver_container[target][INST_0][MESH_0][MESH_SOL] == nullptr) {
-            SU2_MPI::Error("Mesh deformation was not correctly specified for the fluid/heat zone.\n"
-                           "Use DEFORM_MESH=YES, and setup MARKER_DEFORM_MESH=(...)", CURRENT_FUNCTION);
-          }
-          interface_type = BOUNDARY_DISPLACEMENTS;
-          if (!config[donor]->GetTime_Domain()) interface[donor][target] = new CDisplacementsInterface(nDim, 0);
-          else interface[donor][target] = new CDisplacementsInterface(2*nDim, 0);
-          if (rank == MASTER_NODE) cout << "boundary displacements from the structural solver." << endl;
-        }
-        else if (fluid_donor && fluid_target) {
-          interface_type = SLIDING_INTERFACE;
-          auto nVar = solver[donor][INST_0][MESH_0][FLOW_SOL]->GetnPrimVar();
-          interface[donor][target] = new CSlidingInterface(nVar, 0);
-          if (rank == MASTER_NODE) cout << "sliding interface." << endl;
-        }
-        else if (heat_donor || heat_target) {
-          if (heat_donor && heat_target)
-            SU2_MPI::Error("Conjugate heat transfer between solids is not implemented.", CURRENT_FUNCTION);
-
-          const auto fluidZone = heat_target? donor : target;
-
-          if (config[fluidZone]->GetEnergy_Equation() || (config[fluidZone]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE))
-            interface_type = heat_target? CONJUGATE_HEAT_FS : CONJUGATE_HEAT_SF;
-          else if (config[fluidZone]->GetWeakly_Coupled_Heat())
-            interface_type = heat_target? CONJUGATE_HEAT_WEAKLY_FS : CONJUGATE_HEAT_WEAKLY_SF;
-          else
+    
+    /*--- Setup interpolation and transfer for all possible donor/target pairs. ---*/
+    
+    for (auto target = 0u; target < nZone; target++) {
+        
+        for (auto donor = 0u; donor < nZone; donor++) {
+            
+            /*--- Aliases to make code less verbose. ---*/
+            auto& interface_type = interface_types[donor][target];
+            
+            if (donor == target) {
+                interface_type = ZONES_ARE_EQUAL;
+                continue;
+            }
             interface_type = NO_TRANSFER;
-
-          if (interface_type != NO_TRANSFER) {
-            auto nVar = 4;
-            interface[donor][target] = new CConjugateHeatInterface(nVar, 0);
-            if (rank == MASTER_NODE) cout << "conjugate heat variables." << endl;
-          }
-          else {
-            if (rank == MASTER_NODE) cout << "NO heat variables." << endl;
-          }
-        }
-        else {
-          if (solver[donor][INST_0][MESH_0][FLOW_SOL] == nullptr)
-            SU2_MPI::Error("Could not determine the number of variables for transfer.", CURRENT_FUNCTION);
-
-          auto nVar = solver[donor][INST_0][MESH_0][FLOW_SOL]->GetnVar();
-          interface_type = CONSERVATIVE_VARIABLES;
-          interface[donor][target] = new CConservativeVarsInterface(nVar, 0);
-          if (rank == MASTER_NODE) cout << "generic conservative variables." << endl;
-        }
-      }
-
-      /*--- Mixing plane for turbo machinery applications. ---*/
-
-      if (config[donor]->GetBoolMixingPlaneInterface()) {
-        interface_type = MIXING_PLANE;
-        auto nVar = solver[donor][INST_0][MESH_0][FLOW_SOL]->GetnVar();
-        interface[donor][target] = new CMixingPlaneInterface(nVar, 0);
-        if (rank == MASTER_NODE) {
-          cout << "Set mixing-plane interface from donor zone "
-               << donor << " to target zone " << target << "." << endl;
+            
+            /*--- If there is a common interface setup the interpolation and transfer. ---*/
+            
+            if (!CInterpolator::CheckZonesInterface(config[donor], config[target])) {
+                interface_type = NO_COMMON_INTERFACE;
+            }
+            else {
+                /*--- Begin the creation of the communication pattern among zones. ---*/
+                
+                if (rank == MASTER_NODE) cout << "From zone " << donor << " to zone " << target << ":" << endl;
+                
+                /*--- Setup the interpolation. ---*/
+                
+                interpolation[donor][target] = unique_ptr<CInterpolator>(CInterpolatorFactory::CreateInterpolator(
+                                                                                                                  geometry, config, interpolation[target][donor].get(), donor, target));
+                
+                /*--- The type of variables transferred depends on the donor/target physics. ---*/
+                
+                const bool heat_target = config[target]->GetHeatProblem();
+                const bool fluid_target = config[target]->GetFluidProblem();
+                const bool structural_target = config[target]->GetStructuralProblem();
+                
+                const bool heat_donor = config[donor]->GetHeatProblem();
+                const bool fluid_donor = config[donor]->GetFluidProblem();
+                const bool structural_donor = config[donor]->GetStructuralProblem();
+                
+                /*--- Initialize the appropriate transfer strategy. ---*/
+                
+                if (rank == MASTER_NODE) cout << " Transferring ";
+                
+                if (fluid_donor && structural_target) {
+                    interface_type = FLOW_TRACTION;
+                    auto nConst = 2;
+                    bool conservative = config[target]->GetConservativeInterpolation();
+                    if(!config[ZONE_0]->GetDiscrete_Adjoint()) {
+                        interface[donor][target] = new CFlowTractionInterface(nDim, nConst, config[donor], conservative);
+                    } else {
+                        interface[donor][target] = new CDiscAdjFlowTractionInterface(nDim, nConst, config[donor], conservative);
+                    }
+                    if (rank == MASTER_NODE) cout << "fluid " << (conservative? "forces." : "tractions.") << endl;
+                }
+                else if (structural_donor && (fluid_target || heat_target)) {
+                    if (solver_container[target][INST_0][MESH_0][MESH_SOL] == nullptr) {
+                        SU2_MPI::Error("Mesh deformation was not correctly specified for the fluid/heat zone.\n"
+                                       "Use DEFORM_MESH=YES, and setup MARKER_DEFORM_MESH=(...)", CURRENT_FUNCTION);
+                    }
+                    interface_type = BOUNDARY_DISPLACEMENTS;
+                    if (!config[donor]->GetTime_Domain()) interface[donor][target] = new CDisplacementsInterface(nDim, 0);
+                    else interface[donor][target] = new CDisplacementsInterface(2*nDim, 0);
+                    if (rank == MASTER_NODE) cout << "boundary displacements from the structural solver." << endl;
+                }
+                else if (fluid_donor && fluid_target) {
+                    interface_type = SLIDING_INTERFACE;
+                    auto nVar = solver[donor][INST_0][MESH_0][FLOW_SOL]->GetnPrimVar();
+                    interface[donor][target] = new CSlidingInterface(nVar, 0);
+                    if (rank == MASTER_NODE) cout << "sliding interface." << endl;
+                }
+                else if (heat_donor || heat_target) {
+                    if (heat_donor && heat_target)
+                        SU2_MPI::Error("Conjugate heat transfer between solids is not implemented.", CURRENT_FUNCTION);
+                    
+                    const auto fluidZone = heat_target? donor : target;
+                    
+                    if (config[fluidZone]->GetEnergy_Equation() || (config[fluidZone]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE))
+                        interface_type = heat_target? CONJUGATE_HEAT_FS : CONJUGATE_HEAT_SF;
+                    else if (config[fluidZone]->GetWeakly_Coupled_Heat())
+                        interface_type = heat_target? CONJUGATE_HEAT_WEAKLY_FS : CONJUGATE_HEAT_WEAKLY_SF;
+                    else
+                        interface_type = NO_TRANSFER;
+                    
+                    if (interface_type != NO_TRANSFER) {
+                        auto nVar = 4;
+                        interface[donor][target] = new CConjugateHeatInterface(nVar, 0);
+                        if (rank == MASTER_NODE) cout << "conjugate heat variables." << endl;
+                    }
+                    else {
+                        if (rank == MASTER_NODE) cout << "NO heat variables." << endl;
+                    }
+                }
+                else {
+                    if (solver[donor][INST_0][MESH_0][FLOW_SOL] == nullptr)
+                        SU2_MPI::Error("Could not determine the number of variables for transfer.", CURRENT_FUNCTION);
+                    
+                    auto nVar = solver[donor][INST_0][MESH_0][FLOW_SOL]->GetnVar();
+                    interface_type = CONSERVATIVE_VARIABLES;
+                    interface[donor][target] = new CConservativeVarsInterface(nVar, 0);
+                    if (rank == MASTER_NODE) cout << "generic conservative variables." << endl;
+                }
+            }
+            
+            /*--- Mixing plane for turbo machinery applications. ---*/
+            
+            if (config[donor]->GetBoolMixingPlaneInterface()) {
+                interface_type = MIXING_PLANE;
+                auto nVar = solver[donor][INST_0][MESH_0][FLOW_SOL]->GetnVar();
+                interface[donor][target] = new CMixingPlaneInterface(nVar, 0);
+                if (rank == MASTER_NODE) {
+                    cout << "Set mixing-plane interface from donor zone "
+                    << donor << " to target zone " << target << "." << endl;
+                }
+            }
+            
         }
-      }
-
+        
     }
-
-  }
-
+    
 }
 
 void CDriver::StaticMesh_Preprocessing(const CConfig *config, CGeometry** geometry){
-
-  unsigned short iMGlevel, iMGfine;
-  unsigned short Kind_Grid_Movement;
-
-  unsigned short iZone = config->GetiZone();
-
-  Kind_Grid_Movement = config->GetKind_GridMovement();
-
-  if (!fem_solver) {
-
-    switch (Kind_Grid_Movement) {
-
-      case ROTATING_FRAME:
-
-        /*--- Steadily rotating frame: set the grid velocities just once
-         before the first iteration flow solver. ---*/
-
-        if (rank == MASTER_NODE) {
-          cout << endl << " Setting rotating frame grid velocities";
-          cout << " for zone " << iZone << "." << endl;
+    
+    unsigned short iMGlevel, iMGfine;
+    unsigned short Kind_Grid_Movement;
+    
+    unsigned short iZone = config->GetiZone();
+    
+    Kind_Grid_Movement = config->GetKind_GridMovement();
+    
+    if (!fem_solver) {
+        
+        switch (Kind_Grid_Movement) {
+                
+            case ROTATING_FRAME:
+                
+                /*--- Steadily rotating frame: set the grid velocities just once
+                 before the first iteration flow solver. ---*/
+                
+                if (rank == MASTER_NODE) {
+                    cout << endl << " Setting rotating frame grid velocities";
+                    cout << " for zone " << iZone << "." << endl;
+                }
+                
+                /*--- Set the grid velocities on all multigrid levels for a steadily
+                 rotating reference frame. ---*/
+                
+                for (iMGlevel = 0; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++){
+                    geometry[iMGlevel]->SetRotationalVelocity(config, true);
+                    geometry[iMGlevel]->SetShroudVelocity(config);
+                }
+                
+                break;
+                
+            case STEADY_TRANSLATION:
+                
+                /*--- Set the translational velocity and hold the grid fixed during
+                 the calculation (similar to rotating frame, but there is no extra
+                 source term for translation). ---*/
+                
+                if (rank == MASTER_NODE)
+                    cout << endl << " Setting translational grid velocities." << endl;
+                
+                /*--- Set the translational velocity on all grid levels. ---*/
+                
+                for (iMGlevel = 0; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++)
+                    geometry_container[iZone][INST_0][iMGlevel]->SetTranslationalVelocity(config, true);
+                
+                break;
+                
+            default:
+                break;
         }
-
-        /*--- Set the grid velocities on all multigrid levels for a steadily
-           rotating reference frame. ---*/
-
-        for (iMGlevel = 0; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++){
-          geometry[iMGlevel]->SetRotationalVelocity(config, true);
-          geometry[iMGlevel]->SetShroudVelocity(config);
+        
+        if (config->GetnMarker_Moving() > 0) {
+            
+            /*--- Fixed wall velocities: set the grid velocities only one time
+             before the first iteration flow solver. ---*/
+            if (rank == MASTER_NODE)
+                cout << endl << " Setting the moving wall velocities." << endl;
+            
+            geometry[MESH_0]->SetWallVelocity(config, true);
+            
+            /*--- Update the grid velocities on the coarser multigrid levels after
+             setting the moving wall velocities for the finest mesh. ---*/
+            for (iMGlevel = 1; iMGlevel <= config->GetnMGLevels(); iMGlevel++){
+                iMGfine = iMGlevel-1;
+                geometry[iMGlevel]->SetRestricted_GridVelocity(geometry[iMGfine]);
+            }
         }
-
-        break;
-
-      case STEADY_TRANSLATION:
-
-        /*--- Set the translational velocity and hold the grid fixed during
-         the calculation (similar to rotating frame, but there is no extra
-         source term for translation). ---*/
-
-        if (rank == MASTER_NODE)
-          cout << endl << " Setting translational grid velocities." << endl;
-
-        /*--- Set the translational velocity on all grid levels. ---*/
-
-        for (iMGlevel = 0; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++)
-          geometry_container[iZone][INST_0][iMGlevel]->SetTranslationalVelocity(config, true);
-
-        break;
-
-      default:
-        break;
-    }
-
-    if (config->GetnMarker_Moving() > 0) {
-
-      /*--- Fixed wall velocities: set the grid velocities only one time
-       before the first iteration flow solver. ---*/
-      if (rank == MASTER_NODE)
-        cout << endl << " Setting the moving wall velocities." << endl;
-
-      geometry[MESH_0]->SetWallVelocity(config, true);
-
-      /*--- Update the grid velocities on the coarser multigrid levels after
-        setting the moving wall velocities for the finest mesh. ---*/
-      for (iMGlevel = 1; iMGlevel <= config->GetnMGLevels(); iMGlevel++){
-        iMGfine = iMGlevel-1;
-        geometry[iMGlevel]->SetRestricted_GridVelocity(geometry[iMGfine]);
-      }
-    }
-  } else {
-
-    /*--- Carry out a dynamic cast to CMeshFEM_DG, such that it is not needed to
+    } else {
+        
+        /*--- Carry out a dynamic cast to CMeshFEM_DG, such that it is not needed to
          define all virtual functions in the base class CGeometry. ---*/
-    CMeshFEM_DG *DGMesh = dynamic_cast<CMeshFEM_DG *>(geometry[MESH_0]);
-
-    /*--- Initialize the static mesh movement, if necessary. ---*/
-    const unsigned short Kind_Grid_Movement = config->GetKind_GridMovement();
-    const bool initStaticMovement = (config->GetGrid_Movement() &&
-                                     (Kind_Grid_Movement == MOVING_WALL    ||
-                                      Kind_Grid_Movement == ROTATING_FRAME ||
-                                      Kind_Grid_Movement == STEADY_TRANSLATION));
-
-    if(initStaticMovement){
-      if (rank == MASTER_NODE) cout << "Initialize Static Mesh Movement" << endl;
-      DGMesh->InitStaticMeshMovement(config, Kind_Grid_Movement, iZone);
+        CMeshFEM_DG *DGMesh = dynamic_cast<CMeshFEM_DG *>(geometry[MESH_0]);
+        
+        /*--- Initialize the static mesh movement, if necessary. ---*/
+        const unsigned short Kind_Grid_Movement = config->GetKind_GridMovement();
+        const bool initStaticMovement = (config->GetGrid_Movement() &&
+                                         (Kind_Grid_Movement == MOVING_WALL    ||
+                                          Kind_Grid_Movement == ROTATING_FRAME ||
+                                          Kind_Grid_Movement == STEADY_TRANSLATION));
+        
+        if(initStaticMovement){
+            if (rank == MASTER_NODE) cout << "Initialize Static Mesh Movement" << endl;
+            DGMesh->InitStaticMeshMovement(config, Kind_Grid_Movement, iZone);
+        }
     }
-  }
-
+    
 }
 
 void CDriver::Output_Preprocessing(CConfig **config, CConfig *driver_config, COutput **&output, COutput *&driver_output){
-
-  /*--- Definition of the output class (one for each zone). The output class
-   manages the writing of all restart, volume solution, surface solution,
-   surface comma-separated value, and convergence history files (both in serial
-   and in parallel). ---*/
-
-  for (iZone = 0; iZone < nZone; iZone++){
-
-    if (rank == MASTER_NODE)
-      cout << endl <<"-------------------- Output Preprocessing ( Zone " << iZone <<" ) --------------------" << endl;
-
-    MAIN_SOLVER kindSolver = config[iZone]->GetKind_Solver();
-
-    output[iZone] = COutputFactory::CreateOutput(kindSolver, config[iZone], nDim);
-
-    /*--- If dry-run is used, do not open/overwrite history file. ---*/
-    output[iZone]->PreprocessHistoryOutput(config[iZone], !dry_run);
-
-    output[iZone]->PreprocessVolumeOutput(config[iZone]);
-
-  }
-
-  if (driver_config->GetMultizone_Problem()){
-    if (rank == MASTER_NODE)
-      cout << endl <<"------------------- Output Preprocessing ( Multizone ) ------------------" << endl;
-
-    driver_output = COutputFactory::CreateMultizoneOutput(driver_config, config, nDim);
-
-    driver_output->PreprocessMultizoneHistoryOutput(output, config, driver_config, !dry_run);
-  }
-
-  /*--- Check for an unsteady restart. Update ExtIter if necessary. ---*/
-  if (config_container[ZONE_0]->GetTime_Domain() && config_container[ZONE_0]->GetRestart())
-    TimeIter = config_container[ZONE_0]->GetRestart_Iter();
-
+    
+    /*--- Definition of the output class (one for each zone). The output class
+     manages the writing of all restart, volume solution, surface solution,
+     surface comma-separated value, and convergence history files (both in serial
+     and in parallel). ---*/
+    
+    for (iZone = 0; iZone < nZone; iZone++){
+        
+        if (rank == MASTER_NODE)
+            cout << endl <<"-------------------- Output Preprocessing ( Zone " << iZone <<" ) --------------------" << endl;
+        
+        MAIN_SOLVER kindSolver = config[iZone]->GetKind_Solver();
+        
+        output[iZone] = COutputFactory::CreateOutput(kindSolver, config[iZone], nDim);
+        
+        /*--- If dry-run is used, do not open/overwrite history file. ---*/
+        output[iZone]->PreprocessHistoryOutput(config[iZone], !dry_run);
+        
+        output[iZone]->PreprocessVolumeOutput(config[iZone]);
+        
+    }
+    
+    if (driver_config->GetMultizone_Problem()){
+        if (rank == MASTER_NODE)
+            cout << endl <<"------------------- Output Preprocessing ( Multizone ) ------------------" << endl;
+        
+        driver_output = COutputFactory::CreateMultizoneOutput(driver_config, config, nDim);
+        
+        driver_output->PreprocessMultizoneHistoryOutput(output, config, driver_config, !dry_run);
+    }
+    
+    /*--- Check for an unsteady restart. Update ExtIter if necessary. ---*/
+    if (config_container[ZONE_0]->GetTime_Domain() && config_container[ZONE_0]->GetRestart())
+        TimeIter = config_container[ZONE_0]->GetRestart_Iter();
+    
 }
 
 
 void CDriver::Turbomachinery_Preprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver,
                                            CInterface*** interface){
-
-  unsigned short donorZone,targetZone, nMarkerInt, iMarkerInt;
-  unsigned short nSpanMax = 0;
-  bool restart   = (config[ZONE_0]->GetRestart() || config[ZONE_0]->GetRestart_Flow());
-  mixingplane = config[ZONE_0]->GetBoolMixingPlaneInterface();
-  bool discrete_adjoint = config[ZONE_0]->GetDiscrete_Adjoint();
-  su2double areaIn, areaOut, nBlades, flowAngleIn, flowAngleOut;
-
-  /*--- Create turbovertex structure ---*/
-  if (rank == MASTER_NODE) cout<<endl<<"Initialize Turbo Vertex Structure." << endl;
-  for (iZone = 0; iZone < nZone; iZone++) {
-    if (config[iZone]->GetBoolTurbomachinery()){
-      geometry[iZone][INST_0][MESH_0]->ComputeNSpan(config[iZone], iZone, INFLOW, true);
-      geometry[iZone][INST_0][MESH_0]->ComputeNSpan(config[iZone], iZone, OUTFLOW, true);
-      if (rank == MASTER_NODE) cout <<"Number of span-wise sections in Zone "<< iZone<<": "<< config[iZone]->GetnSpanWiseSections() <<"."<< endl;
-      if (config[iZone]->GetnSpanWiseSections() > nSpanMax){
-        nSpanMax = config[iZone]->GetnSpanWiseSections();
-      }
-
-      config[ZONE_0]->SetnSpan_iZones(config[iZone]->GetnSpanWiseSections(), iZone);
-
-      geometry[iZone][INST_0][MESH_0]->SetTurboVertex(config[iZone], iZone, INFLOW, true);
-      geometry[iZone][INST_0][MESH_0]->SetTurboVertex(config[iZone], iZone, OUTFLOW, true);
-    }
-  }
-
-  /*--- Set maximum number of Span among all zones ---*/
-  for (iZone = 0; iZone < nZone; iZone++) {
-    if (config[iZone]->GetBoolTurbomachinery()){
-      config[iZone]->SetnSpanMaxAllZones(nSpanMax);
-    }
-  }
-  if (rank == MASTER_NODE) cout<<"Max number of span-wise sections among all zones: "<< nSpanMax<<"."<< endl;
-
-
-  if (rank == MASTER_NODE) cout<<"Initialize solver containers for average and performance quantities." << endl;
-  for (iZone = 0; iZone < nZone; iZone++) {
-    solver[iZone][INST_0][MESH_0][FLOW_SOL]->InitTurboContainers(geometry[iZone][INST_0][MESH_0],config[iZone]);
-  }
-
-//TODO(turbo) make it general for turbo HB
-  if (rank == MASTER_NODE) cout<<"Compute inflow and outflow average geometric quantities." << endl;
-  for (iZone = 0; iZone < nZone; iZone++) {
-    geometry[iZone][INST_0][MESH_0]->SetAvgTurboValue(config[iZone], iZone, INFLOW, true);
-    geometry[iZone][INST_0][MESH_0]->SetAvgTurboValue(config[iZone],iZone, OUTFLOW, true);
-    geometry[iZone][INST_0][MESH_0]->GatherInOutAverageValues(config[iZone], true);
-  }
-
-
-  if(mixingplane){
-    if (rank == MASTER_NODE) cout << "Set span-wise sections between zones on Mixing-Plane interface." << endl;
-    for (donorZone = 0; donorZone < nZone; donorZone++) {
-      for (targetZone = 0; targetZone < nZone; targetZone++) {
-        if (targetZone != donorZone){
-          interface[donorZone][targetZone]->SetSpanWiseLevels(config[donorZone], config[targetZone]);
-        }
-      }
-    }
-  }
-
-  if (rank == MASTER_NODE) cout << "Transfer average geometric quantities to zone 0." << endl;
-  for (iZone = 1; iZone < nZone; iZone++) {
-    interface[iZone][ZONE_0]->GatherAverageTurboGeoValues(geometry[iZone][INST_0][MESH_0],geometry[ZONE_0][INST_0][MESH_0], iZone);
-  }
-
-  /*--- Transfer number of blade to ZONE_0 to correctly compute turbo performance---*/
-  for (iZone = 1; iZone < nZone; iZone++) {
-    nBlades = config[iZone]->GetnBlades(iZone);
-    config[ZONE_0]->SetnBlades(iZone, nBlades);
-  }
-
-  if (rank == MASTER_NODE){
+    
+    unsigned short donorZone,targetZone, nMarkerInt, iMarkerInt;
+    unsigned short nSpanMax = 0;
+    bool restart   = (config[ZONE_0]->GetRestart() || config[ZONE_0]->GetRestart_Flow());
+    mixingplane = config[ZONE_0]->GetBoolMixingPlaneInterface();
+    bool discrete_adjoint = config[ZONE_0]->GetDiscrete_Adjoint();
+    su2double areaIn, areaOut, nBlades, flowAngleIn, flowAngleOut;
+    
+    /*--- Create turbovertex structure ---*/
+    if (rank == MASTER_NODE) cout<<endl<<"Initialize Turbo Vertex Structure." << endl;
     for (iZone = 0; iZone < nZone; iZone++) {
-    areaIn  = geometry[iZone][INST_0][MESH_0]->GetSpanAreaIn(iZone, config[iZone]->GetnSpanWiseSections());
-    areaOut = geometry[iZone][INST_0][MESH_0]->GetSpanAreaOut(iZone, config[iZone]->GetnSpanWiseSections());
-    nBlades = config[iZone]->GetnBlades(iZone);
-    cout << "Inlet area for Row "<< iZone + 1<< ": " << areaIn*10000.0 <<" cm^2."  <<endl;
-    cout << "Oulet area for Row "<< iZone + 1<< ": " << areaOut*10000.0 <<" cm^2."  <<endl;
-    cout << "Recomputed number of blades for Row "<< iZone + 1 << ": " << nBlades<<"."  <<endl;
-    }
-  }
-
-
-  if(mixingplane){
-    if (rank == MASTER_NODE) cout<<"Preprocessing of the Mixing-Plane Interface." << endl;
-    for (donorZone = 0; donorZone < nZone; donorZone++) {
-      nMarkerInt     = config_container[donorZone]->GetnMarker_MixingPlaneInterface()/2;
-      for (iMarkerInt = 1; iMarkerInt <= nMarkerInt; iMarkerInt++){
-        for (targetZone = 0; targetZone < nZone; targetZone++) {
-          if (targetZone != donorZone){
-            interface[donorZone][targetZone]->PreprocessAverage(geometry[donorZone][INST_0][MESH_0], geometry[targetZone][INST_0][MESH_0],
-                config[donorZone], config[targetZone],
-                iMarkerInt);
-          }
+        if (config[iZone]->GetBoolTurbomachinery()){
+            geometry[iZone][INST_0][MESH_0]->ComputeNSpan(config[iZone], iZone, INFLOW, true);
+            geometry[iZone][INST_0][MESH_0]->ComputeNSpan(config[iZone], iZone, OUTFLOW, true);
+            if (rank == MASTER_NODE) cout <<"Number of span-wise sections in Zone "<< iZone<<": "<< config[iZone]->GetnSpanWiseSections() <<"."<< endl;
+            if (config[iZone]->GetnSpanWiseSections() > nSpanMax){
+                nSpanMax = config[iZone]->GetnSpanWiseSections();
+            }
+            
+            config[ZONE_0]->SetnSpan_iZones(config[iZone]->GetnSpanWiseSections(), iZone);
+            
+            geometry[iZone][INST_0][MESH_0]->SetTurboVertex(config[iZone], iZone, INFLOW, true);
+            geometry[iZone][INST_0][MESH_0]->SetTurboVertex(config[iZone], iZone, OUTFLOW, true);
         }
-      }
     }
-  }
-
-  if(!restart && !discrete_adjoint){
-    if (rank == MASTER_NODE) cout<<"Initialize turbomachinery solution quantities." << endl;
-    for(iZone = 0; iZone < nZone; iZone++) {
-      solver[iZone][INST_0][MESH_0][FLOW_SOL]->SetFreeStream_TurboSolution(config[iZone]);
+    
+    /*--- Set maximum number of Span among all zones ---*/
+    for (iZone = 0; iZone < nZone; iZone++) {
+        if (config[iZone]->GetBoolTurbomachinery()){
+            config[iZone]->SetnSpanMaxAllZones(nSpanMax);
+        }
     }
-  }
-
-  if (rank == MASTER_NODE) cout<<"Initialize inflow and outflow average solution quantities." << endl;
-  for(iZone = 0; iZone < nZone; iZone++) {
-    solver[iZone][INST_0][MESH_0][FLOW_SOL]->PreprocessAverage(solver[iZone][INST_0][MESH_0], geometry[iZone][INST_0][MESH_0],config[iZone],INFLOW);
-    solver[iZone][INST_0][MESH_0][FLOW_SOL]->PreprocessAverage(solver[iZone][INST_0][MESH_0], geometry[iZone][INST_0][MESH_0],config[iZone],OUTFLOW);
-    solver[iZone][INST_0][MESH_0][FLOW_SOL]->TurboAverageProcess(solver[iZone][INST_0][MESH_0], geometry[iZone][INST_0][MESH_0],config[iZone],INFLOW);
-    solver[iZone][INST_0][MESH_0][FLOW_SOL]->TurboAverageProcess(solver[iZone][INST_0][MESH_0], geometry[iZone][INST_0][MESH_0],config[iZone],OUTFLOW);
-    solver[iZone][INST_0][MESH_0][FLOW_SOL]->GatherInOutAverageValues(config[iZone], geometry[iZone][INST_0][MESH_0]);
-    if (rank == MASTER_NODE){
-      flowAngleIn = solver[iZone][INST_0][MESH_0][FLOW_SOL]->GetTurboVelocityIn(iZone, config[iZone]->GetnSpanWiseSections())[1];
-      flowAngleIn /= solver[iZone][INST_0][MESH_0][FLOW_SOL]->GetTurboVelocityIn(iZone, config[iZone]->GetnSpanWiseSections())[0];
-      flowAngleIn = atan(flowAngleIn)*180.0/PI_NUMBER;
-      cout << "Inlet flow angle for Row "<< iZone + 1<< ": "<< flowAngleIn <<"°."  <<endl;
-      flowAngleOut = solver[iZone][INST_0][MESH_0][FLOW_SOL]->GetTurboVelocityOut(iZone, config[iZone]->GetnSpanWiseSections())[1];
-      flowAngleOut /= solver[iZone][INST_0][MESH_0][FLOW_SOL]->GetTurboVelocityOut(iZone, config[iZone]->GetnSpanWiseSections())[0];
-      flowAngleOut = atan(flowAngleOut)*180.0/PI_NUMBER;
-      cout << "Outlet flow angle for Row "<< iZone + 1<< ": "<< flowAngleOut <<"°."  <<endl;
-
+    if (rank == MASTER_NODE) cout<<"Max number of span-wise sections among all zones: "<< nSpanMax<<"."<< endl;
+    
+    
+    if (rank == MASTER_NODE) cout<<"Initialize solver containers for average and performance quantities." << endl;
+    for (iZone = 0; iZone < nZone; iZone++) {
+        solver[iZone][INST_0][MESH_0][FLOW_SOL]->InitTurboContainers(geometry[iZone][INST_0][MESH_0],config[iZone]);
     }
-  }
-
-}
-
-CDriver::~CDriver(void) {}
-
-void CDriver::Print_DirectResidual(RECORDING kind_recording) {
-
-  if (!(rank == MASTER_NODE && kind_recording == RECORDING::SOLUTION_VARIABLES)) return;
-
-  const bool multizone = config_container[ZONE_0]->GetMultizone_Problem();
-
-  /*--- Helper lambda func to return lenghty [iVar][iZone] string.  ---*/
-  auto iVar_iZone2string = [&](unsigned short ivar, unsigned short izone) {
-    if (multizone)
-      return "[" + std::to_string(ivar) + "][" + std::to_string(izone) + "]";
-    else
-      return "[" + std::to_string(ivar) + "]";
-  };
-
-  /*--- Print residuals in the first iteration ---*/
-
-  const unsigned short fieldWidth = 15;
-  PrintingToolbox::CTablePrinter RMSTable(&std::cout);
-  RMSTable.SetPrecision(config_container[ZONE_0]->GetOutput_Precision());
-
-  /*--- The CTablePrinter requires two sweeps:
-    *--- 0. Add the colum names (addVals=0=false) plus CTablePrinter.PrintHeader()
-    *--- 1. Add the RMS-residual values (addVals=1=true) plus CTablePrinter.PrintFooter() ---*/
-  for (int addVals = 0; addVals < 2; addVals++) {
-
-    for (unsigned short iZone = 0; iZone < nZone; iZone++) {
-
-      auto solvers = solver_container[iZone][INST_0][MESH_0];
-      auto configs = config_container[iZone];
-
-      /*--- Note: the FEM-Flow solvers are availalbe for disc. adjoint runs only for SingleZone. ---*/
-      if (configs->GetFluidProblem() || configs->GetFEMSolver()) {
-
-        for (unsigned short iVar = 0; iVar < solvers[FLOW_SOL]->GetnVar(); iVar++) {
-          if (!addVals)
-            RMSTable.AddColumn("rms_Flow" + iVar_iZone2string(iVar, iZone), fieldWidth);
-          else
-            RMSTable << log10(solvers[FLOW_SOL]->GetRes_RMS(iVar));
-        }
-
-        if (configs->GetKind_Turb_Model() != TURB_MODEL::NONE && !configs->GetFrozen_Visc_Disc()) {
-          for (unsigned short iVar = 0; iVar < solvers[TURB_SOL]->GetnVar(); iVar++) {
-            if (!addVals)
-              RMSTable.AddColumn("rms_Turb" + iVar_iZone2string(iVar, iZone), fieldWidth);
-            else
-              RMSTable << log10(solvers[TURB_SOL]->GetRes_RMS(iVar));
-          }
-        }
-
-        if (configs->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
-          for (unsigned short iVar = 0; iVar < solvers[SPECIES_SOL]->GetnVar(); iVar++) {
-            if (!addVals)
-              RMSTable.AddColumn("rms_Spec" + iVar_iZone2string(iVar, iZone), fieldWidth);
-            else
-              RMSTable << log10(solvers[SPECIES_SOL]->GetRes_RMS(iVar));
-          }
+    
+    //TODO(turbo) make it general for turbo HB
+    if (rank == MASTER_NODE) cout<<"Compute inflow and outflow average geometric quantities." << endl;
+    for (iZone = 0; iZone < nZone; iZone++) {
+        geometry[iZone][INST_0][MESH_0]->SetAvgTurboValue(config[iZone], iZone, INFLOW, true);
+        geometry[iZone][INST_0][MESH_0]->SetAvgTurboValue(config[iZone],iZone, OUTFLOW, true);
+        geometry[iZone][INST_0][MESH_0]->GatherInOutAverageValues(config[iZone], true);
+    }
+    
+    
+    if(mixingplane){
+        if (rank == MASTER_NODE) cout << "Set span-wise sections between zones on Mixing-Plane interface." << endl;
+        for (donorZone = 0; donorZone < nZone; donorZone++) {
+            for (targetZone = 0; targetZone < nZone; targetZone++) {
+                if (targetZone != donorZone){
+                    interface[donorZone][targetZone]->SetSpanWiseLevels(config[donorZone], config[targetZone]);
+                }
+            }
         }
-
-        if (!multizone && configs->GetWeakly_Coupled_Heat()){
-          if (!addVals) RMSTable.AddColumn("rms_Heat" + iVar_iZone2string(0, iZone), fieldWidth);
-          else RMSTable << log10(solvers[HEAT_SOL]->GetRes_RMS(0));
+    }
+    
+    if (rank == MASTER_NODE) cout << "Transfer average geometric quantities to zone 0." << endl;
+    for (iZone = 1; iZone < nZone; iZone++) {
+        interface[iZone][ZONE_0]->GatherAverageTurboGeoValues(geometry[iZone][INST_0][MESH_0],geometry[ZONE_0][INST_0][MESH_0], iZone);
+    }
+    
+    /*--- Transfer number of blade to ZONE_0 to correctly compute turbo performance---*/
+    for (iZone = 1; iZone < nZone; iZone++) {
+        nBlades = config[iZone]->GetnBlades(iZone);
+        config[ZONE_0]->SetnBlades(iZone, nBlades);
+    }
+    
+    if (rank == MASTER_NODE){
+        for (iZone = 0; iZone < nZone; iZone++) {
+            areaIn  = geometry[iZone][INST_0][MESH_0]->GetSpanAreaIn(iZone, config[iZone]->GetnSpanWiseSections());
+            areaOut = geometry[iZone][INST_0][MESH_0]->GetSpanAreaOut(iZone, config[iZone]->GetnSpanWiseSections());
+            nBlades = config[iZone]->GetnBlades(iZone);
+            cout << "Inlet area for Row "<< iZone + 1<< ": " << areaIn*10000.0 <<" cm^2."  <<endl;
+            cout << "Oulet area for Row "<< iZone + 1<< ": " << areaOut*10000.0 <<" cm^2."  <<endl;
+            cout << "Recomputed number of blades for Row "<< iZone + 1 << ": " << nBlades<<"."  <<endl;
         }
-
-        if (configs->AddRadiation()) {
-          if (!addVals) RMSTable.AddColumn("rms_Rad" + iVar_iZone2string(0, iZone), fieldWidth);
-          else RMSTable << log10(solvers[RAD_SOL]->GetRes_RMS(0));
+    }
+    
+    
+    if(mixingplane){
+        if (rank == MASTER_NODE) cout<<"Preprocessing of the Mixing-Plane Interface." << endl;
+        for (donorZone = 0; donorZone < nZone; donorZone++) {
+            nMarkerInt     = config_container[donorZone]->GetnMarker_MixingPlaneInterface()/2;
+            for (iMarkerInt = 1; iMarkerInt <= nMarkerInt; iMarkerInt++){
+                for (targetZone = 0; targetZone < nZone; targetZone++) {
+                    if (targetZone != donorZone){
+                        interface[donorZone][targetZone]->PreprocessAverage(geometry[donorZone][INST_0][MESH_0], geometry[targetZone][INST_0][MESH_0],
+                                                                            config[donorZone], config[targetZone],
+                                                                            iMarkerInt);
+                    }
+                }
+            }
         }
-
-      }
-      else if (configs->GetStructuralProblem()) {
-
-        if (configs->GetGeometricConditions() == STRUCT_DEFORMATION::LARGE){
-          if (!addVals) {
-            RMSTable.AddColumn("UTOL-A", fieldWidth);
-            RMSTable.AddColumn("RTOL-A", fieldWidth);
-            RMSTable.AddColumn("ETOL-A", fieldWidth);
-          }
-          else {
-            RMSTable << log10(solvers[FEA_SOL]->GetRes_FEM(0))
-                     << log10(solvers[FEA_SOL]->GetRes_FEM(1))
-                     << log10(solvers[FEA_SOL]->GetRes_FEM(2));
-          }
+    }
+    
+    if(!restart && !discrete_adjoint){
+        if (rank == MASTER_NODE) cout<<"Initialize turbomachinery solution quantities." << endl;
+        for(iZone = 0; iZone < nZone; iZone++) {
+            solver[iZone][INST_0][MESH_0][FLOW_SOL]->SetFreeStream_TurboSolution(config[iZone]);
         }
-        else{
-          if (!addVals) {
-            RMSTable.AddColumn("log10[RMS Ux]", fieldWidth);
-            RMSTable.AddColumn("log10[RMS Uy]", fieldWidth);
-            if (nDim == 3) RMSTable.AddColumn("log10[RMS Uz]", fieldWidth);
-          }
-          else {
-            RMSTable << log10(solvers[FEA_SOL]->GetRes_FEM(0))
-                     << log10(solvers[FEA_SOL]->GetRes_FEM(1));
-            if (nDim == 3) RMSTable << log10(solvers[FEA_SOL]->GetRes_FEM(2));
-          }
+    }
+    
+    if (rank == MASTER_NODE) cout<<"Initialize inflow and outflow average solution quantities." << endl;
+    for(iZone = 0; iZone < nZone; iZone++) {
+        solver[iZone][INST_0][MESH_0][FLOW_SOL]->PreprocessAverage(solver[iZone][INST_0][MESH_0], geometry[iZone][INST_0][MESH_0],config[iZone],INFLOW);
+        solver[iZone][INST_0][MESH_0][FLOW_SOL]->PreprocessAverage(solver[iZone][INST_0][MESH_0], geometry[iZone][INST_0][MESH_0],config[iZone],OUTFLOW);
+        solver[iZone][INST_0][MESH_0][FLOW_SOL]->TurboAverageProcess(solver[iZone][INST_0][MESH_0], geometry[iZone][INST_0][MESH_0],config[iZone],INFLOW);
+        solver[iZone][INST_0][MESH_0][FLOW_SOL]->TurboAverageProcess(solver[iZone][INST_0][MESH_0], geometry[iZone][INST_0][MESH_0],config[iZone],OUTFLOW);
+        solver[iZone][INST_0][MESH_0][FLOW_SOL]->GatherInOutAverageValues(config[iZone], geometry[iZone][INST_0][MESH_0]);
+        if (rank == MASTER_NODE){
+            flowAngleIn = solver[iZone][INST_0][MESH_0][FLOW_SOL]->GetTurboVelocityIn(iZone, config[iZone]->GetnSpanWiseSections())[1];
+            flowAngleIn /= solver[iZone][INST_0][MESH_0][FLOW_SOL]->GetTurboVelocityIn(iZone, config[iZone]->GetnSpanWiseSections())[0];
+            flowAngleIn = atan(flowAngleIn)*180.0/PI_NUMBER;
+            cout << "Inlet flow angle for Row "<< iZone + 1<< ": "<< flowAngleIn <<"°."  <<endl;
+            flowAngleOut = solver[iZone][INST_0][MESH_0][FLOW_SOL]->GetTurboVelocityOut(iZone, config[iZone]->GetnSpanWiseSections())[1];
+            flowAngleOut /= solver[iZone][INST_0][MESH_0][FLOW_SOL]->GetTurboVelocityOut(iZone, config[iZone]->GetnSpanWiseSections())[0];
+            flowAngleOut = atan(flowAngleOut)*180.0/PI_NUMBER;
+            cout << "Outlet flow angle for Row "<< iZone + 1<< ": "<< flowAngleOut <<"°."  <<endl;
+            
         }
+    }
+    
+}
 
-      }
-      else if (configs->GetHeatProblem()) {
-
-        if (!addVals) RMSTable.AddColumn("rms_Heat" + iVar_iZone2string(0, iZone), fieldWidth);
-        else RMSTable << log10(solvers[HEAT_SOL]->GetRes_RMS(0));
-      } else {
-        SU2_MPI::Error("Invalid KindSolver for CDiscAdj-MultiZone/SingleZone-Driver.", CURRENT_FUNCTION);
-      }
-    } // loop iZone
-
-    if (!addVals) RMSTable.PrintHeader();
-    else RMSTable.PrintFooter();
-
-  } // for addVals
-
-  cout << "\n-------------------------------------------------------------------------\n" << endl;
+CDriver::~CDriver(void) {}
 
+void CDriver::Print_DirectResidual(RECORDING kind_recording) {
+    
+    if (!(rank == MASTER_NODE && kind_recording == RECORDING::SOLUTION_VARIABLES)) return;
+    
+    const bool multizone = config_container[ZONE_0]->GetMultizone_Problem();
+    
+    /*--- Helper lambda func to return lenghty [iVar][iZone] string.  ---*/
+    auto iVar_iZone2string = [&](unsigned short ivar, unsigned short izone) {
+        if (multizone)
+            return "[" + std::to_string(ivar) + "][" + std::to_string(izone) + "]";
+        else
+            return "[" + std::to_string(ivar) + "]";
+    };
+    
+    /*--- Print residuals in the first iteration ---*/
+    
+    const unsigned short fieldWidth = 15;
+    PrintingToolbox::CTablePrinter RMSTable(&std::cout);
+    RMSTable.SetPrecision(config_container[ZONE_0]->GetOutput_Precision());
+    
+    /*--- The CTablePrinter requires two sweeps:
+     *--- 0. Add the colum names (addVals=0=false) plus CTablePrinter.PrintHeader()
+     *--- 1. Add the RMS-residual values (addVals=1=true) plus CTablePrinter.PrintFooter() ---*/
+    for (int addVals = 0; addVals < 2; addVals++) {
+        
+        for (unsigned short iZone = 0; iZone < nZone; iZone++) {
+            
+            auto solvers = solver_container[iZone][INST_0][MESH_0];
+            auto configs = config_container[iZone];
+            
+            /*--- Note: the FEM-Flow solvers are availalbe for disc. adjoint runs only for SingleZone. ---*/
+            if (configs->GetFluidProblem() || configs->GetFEMSolver()) {
+                
+                for (unsigned short iVar = 0; iVar < solvers[FLOW_SOL]->GetnVar(); iVar++) {
+                    if (!addVals)
+                        RMSTable.AddColumn("rms_Flow" + iVar_iZone2string(iVar, iZone), fieldWidth);
+                    else
+                        RMSTable << log10(solvers[FLOW_SOL]->GetRes_RMS(iVar));
+                }
+                
+                if (configs->GetKind_Turb_Model() != TURB_MODEL::NONE && !configs->GetFrozen_Visc_Disc()) {
+                    for (unsigned short iVar = 0; iVar < solvers[TURB_SOL]->GetnVar(); iVar++) {
+                        if (!addVals)
+                            RMSTable.AddColumn("rms_Turb" + iVar_iZone2string(iVar, iZone), fieldWidth);
+                        else
+                            RMSTable << log10(solvers[TURB_SOL]->GetRes_RMS(iVar));
+                    }
+                }
+                
+                if (configs->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
+                    for (unsigned short iVar = 0; iVar < solvers[SPECIES_SOL]->GetnVar(); iVar++) {
+                        if (!addVals)
+                            RMSTable.AddColumn("rms_Spec" + iVar_iZone2string(iVar, iZone), fieldWidth);
+                        else
+                            RMSTable << log10(solvers[SPECIES_SOL]->GetRes_RMS(iVar));
+                    }
+                }
+                
+                if (!multizone && configs->GetWeakly_Coupled_Heat()){
+                    if (!addVals) RMSTable.AddColumn("rms_Heat" + iVar_iZone2string(0, iZone), fieldWidth);
+                    else RMSTable << log10(solvers[HEAT_SOL]->GetRes_RMS(0));
+                }
+                
+                if (configs->AddRadiation()) {
+                    if (!addVals) RMSTable.AddColumn("rms_Rad" + iVar_iZone2string(0, iZone), fieldWidth);
+                    else RMSTable << log10(solvers[RAD_SOL]->GetRes_RMS(0));
+                }
+                
+            }
+            else if (configs->GetStructuralProblem()) {
+                
+                if (configs->GetGeometricConditions() == STRUCT_DEFORMATION::LARGE){
+                    if (!addVals) {
+                        RMSTable.AddColumn("UTOL-A", fieldWidth);
+                        RMSTable.AddColumn("RTOL-A", fieldWidth);
+                        RMSTable.AddColumn("ETOL-A", fieldWidth);
+                    }
+                    else {
+                        RMSTable << log10(solvers[FEA_SOL]->GetRes_FEM(0))
+                        << log10(solvers[FEA_SOL]->GetRes_FEM(1))
+                        << log10(solvers[FEA_SOL]->GetRes_FEM(2));
+                    }
+                }
+                else{
+                    if (!addVals) {
+                        RMSTable.AddColumn("log10[RMS Ux]", fieldWidth);
+                        RMSTable.AddColumn("log10[RMS Uy]", fieldWidth);
+                        if (nDim == 3) RMSTable.AddColumn("log10[RMS Uz]", fieldWidth);
+                    }
+                    else {
+                        RMSTable << log10(solvers[FEA_SOL]->GetRes_FEM(0))
+                        << log10(solvers[FEA_SOL]->GetRes_FEM(1));
+                        if (nDim == 3) RMSTable << log10(solvers[FEA_SOL]->GetRes_FEM(2));
+                    }
+                }
+                
+            }
+            else if (configs->GetHeatProblem()) {
+                
+                if (!addVals) RMSTable.AddColumn("rms_Heat" + iVar_iZone2string(0, iZone), fieldWidth);
+                else RMSTable << log10(solvers[HEAT_SOL]->GetRes_RMS(0));
+            } else {
+                SU2_MPI::Error("Invalid KindSolver for CDiscAdj-MultiZone/SingleZone-Driver.", CURRENT_FUNCTION);
+            }
+        } // loop iZone
+        
+        if (!addVals) RMSTable.PrintHeader();
+        else RMSTable.PrintFooter();
+        
+    } // for addVals
+    
+    cout << "\n-------------------------------------------------------------------------\n" << endl;
+    
 }
 
 CFluidDriver::CFluidDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator) : CDriver(confFile, val_nZone, MPICommunicator, false) {
-  Max_Iter = config_container[ZONE_0]->GetnInner_Iter();
+    Max_Iter = config_container[ZONE_0]->GetnInner_Iter();
 }
 
 CFluidDriver::~CFluidDriver(void) { }
 
 void CFluidDriver::StartSolver(){
-
+    
 #ifdef VTUNEPROF
-  __itt_resume();
+    __itt_resume();
 #endif
-
-  /*--- Main external loop of the solver. Within this loop, each iteration ---*/
-
-  if (rank == MASTER_NODE){
-    cout << endl <<"------------------------------ Begin Solver -----------------------------" << endl;
-  }
-
-  unsigned long Iter = 0;
-  while ( Iter < Max_Iter ) {
-
-    /*--- Perform some external iteration preprocessing. ---*/
-
-    Preprocess(Iter);
-
-    /*--- Perform a dynamic mesh update if required. ---*/
-    /*--- For the Disc.Adj. of a case with (rigidly) moving grid, the appropriate
-          mesh cordinates are read from the restart files. ---*/
-    if (!fem_solver &&
-        !(config_container[ZONE_0]->GetGrid_Movement() && config_container[ZONE_0]->GetDiscrete_Adjoint())) {
-      DynamicMeshUpdate(Iter);
+    
+    /*--- Main external loop of the solver. Within this loop, each iteration ---*/
+    
+    if (rank == MASTER_NODE){
+        cout << endl <<"------------------------------ Begin Solver -----------------------------" << endl;
+    }
+    
+    unsigned long Iter = 0;
+    while ( Iter < Max_Iter ) {
+        
+        /*--- Perform some external iteration preprocessing. ---*/
+        
+        Preprocess(Iter);
+        
+        /*--- Perform a dynamic mesh update if required. ---*/
+        /*--- For the Disc.Adj. of a case with (rigidly) moving grid, the appropriate
+         mesh cordinates are read from the restart files. ---*/
+        if (!fem_solver &&
+            !(config_container[ZONE_0]->GetGrid_Movement() && config_container[ZONE_0]->GetDiscrete_Adjoint())) {
+            DynamicMeshUpdate(Iter);
+        }
+        
+        /*--- Run a single iteration of the problem (fluid, elasticity, heat, ...). ---*/
+        
+        Run();
+        
+        /*--- Update the solution for dual time stepping strategy ---*/
+        
+        Update();
+        
+        /*--- Terminate the simulation if only the Jacobian must be computed. ---*/
+        if (config_container[ZONE_0]->GetJacobian_Spatial_Discretization_Only()) break;
+        
+        /*--- Monitor the computations after each iteration. ---*/
+        
+        Monitor(Iter);
+        
+        /*--- Output the solution in files. ---*/
+        
+        Output(Iter);
+        
+        /*--- If the convergence criteria has been met, terminate the simulation. ---*/
+        
+        if (StopCalc) break;
+        
+        Iter++;
+        
     }
-
-    /*--- Run a single iteration of the problem (fluid, elasticity, heat, ...). ---*/
-
-    Run();
-
-    /*--- Update the solution for dual time stepping strategy ---*/
-
-    Update();
-
-    /*--- Terminate the simulation if only the Jacobian must be computed. ---*/
-    if (config_container[ZONE_0]->GetJacobian_Spatial_Discretization_Only()) break;
-
-    /*--- Monitor the computations after each iteration. ---*/
-
-    Monitor(Iter);
-
-    /*--- Output the solution in files. ---*/
-
-    Output(Iter);
-
-    /*--- If the convergence criteria has been met, terminate the simulation. ---*/
-
-    if (StopCalc) break;
-
-    Iter++;
-
-  }
 #ifdef VTUNEPROF
-  __itt_pause();
+    __itt_pause();
 #endif
 }
 
 
 void CFluidDriver::Preprocess(unsigned long Iter) {
-
-  /*--- Set the value of the external iteration and physical time. ---*/
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    config_container[iZone]->SetInnerIter(Iter);
-    if (config_container[iZone]->GetTime_Marching() != TIME_MARCHING::STEADY)
-      config_container[iZone]->SetPhysicalTime(static_cast<su2double>(Iter)*config_container[iZone]->GetDelta_UnstTimeND());
-    else
-      config_container[iZone]->SetPhysicalTime(0.0);
-  }
-
-  /*--- Set the initial condition for EULER/N-S/RANS and for a non FSI simulation ---*/
-
-  if(!fsi) {
+    
+    /*--- Set the value of the external iteration and physical time. ---*/
+    
     for (iZone = 0; iZone < nZone; iZone++) {
-      if (config_container[iZone]->GetFluidProblem()) {
-        for (iInst = 0; iInst < nInst[iZone]; iInst++) {
-          solver_container[iZone][iInst][MESH_0][FLOW_SOL]->SetInitialCondition(geometry_container[iZone][INST_0], solver_container[iZone][iInst], config_container[iZone], Iter);
+        config_container[iZone]->SetInnerIter(Iter);
+        if (config_container[iZone]->GetTime_Marching() != TIME_MARCHING::STEADY)
+            config_container[iZone]->SetPhysicalTime(static_cast<su2double>(Iter)*config_container[iZone]->GetDelta_UnstTimeND());
+        else
+            config_container[iZone]->SetPhysicalTime(0.0);
+    }
+    
+    /*--- Set the initial condition for EULER/N-S/RANS and for a non FSI simulation ---*/
+    
+    if(!fsi) {
+        for (iZone = 0; iZone < nZone; iZone++) {
+            if (config_container[iZone]->GetFluidProblem()) {
+                for (iInst = 0; iInst < nInst[iZone]; iInst++) {
+                    solver_container[iZone][iInst][MESH_0][FLOW_SOL]->SetInitialCondition(geometry_container[iZone][INST_0], solver_container[iZone][iInst], config_container[iZone], Iter);
+                }
+            }
         }
-      }
     }
-  }
 }
 
 void CFluidDriver::Run() {
-
-  unsigned short iZone, jZone, checkConvergence;
-  unsigned long IntIter, nIntIter;
-  bool unsteady;
-
-  /*--- Run a single iteration of a multi-zone problem by looping over all
-   zones and executing the iterations. Note that data transers between zones
-   and other intermediate procedures may be required. ---*/
-
-  unsteady = (config_container[MESH_0]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
-             (config_container[MESH_0]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND);
-
-  /*--- Zone preprocessing ---*/
-
-  for (iZone = 0; iZone < nZone; iZone++)
-    iteration_container[iZone][INST_0]->Preprocess(output_container[iZone], integration_container, geometry_container, solver_container, numerics_container, config_container, surface_movement, grid_movement, FFDBox, iZone, INST_0);
-
-  /*--- Updating zone interface communication patterns,
-   needed only for unsteady simulation since for steady problems
-   this is done once in the interpolator_container constructor
-   at the beginning of the computation ---*/
-
-  if ( unsteady ) {
-    for (iZone = 0; iZone < nZone; iZone++) {
-      for (jZone = 0; jZone < nZone; jZone++)
-        if(jZone != iZone && interpolator_container[iZone][jZone] != nullptr)
-        interpolator_container[iZone][jZone]->SetTransferCoeff(config_container);
-    }
-  }
-
-  /*--- Begin Unsteady pseudo-time stepping internal loop, if not unsteady it does only one step --*/
-
-  if (unsteady)
-    nIntIter = config_container[MESH_0]->GetnInner_Iter();
-  else
-    nIntIter = 1;
-
-  for (IntIter = 0; IntIter < nIntIter; IntIter++) {
-
-    /*--- At each pseudo time-step updates transfer data ---*/
-    for (iZone = 0; iZone < nZone; iZone++)
-      for (jZone = 0; jZone < nZone; jZone++)
-        if(jZone != iZone && interface_container[iZone][jZone] != nullptr)
-          Transfer_Data(iZone, jZone);
-
-    /*--- For each zone runs one single iteration ---*/
-
-    for (iZone = 0; iZone < nZone; iZone++) {
-      config_container[iZone]->SetInnerIter(IntIter);
-      iteration_container[iZone][INST_0]->Iterate(output_container[iZone], integration_container, geometry_container, solver_container, numerics_container,
-                                                  config_container, surface_movement, grid_movement, FFDBox, iZone, INST_0);
-    }
-
-    /*--- Check convergence in each zone --*/
-
-    checkConvergence = 0;
-    for (iZone = 0; iZone < nZone; iZone++)
-    checkConvergence += (int) integration_container[iZone][INST_0][FLOW_SOL]->GetConvergence();
-
-    /*--- If convergence was reached in every zone --*/
-
-  if (checkConvergence == nZone) break;
-  }
-
+    
+    unsigned short iZone, jZone, checkConvergence;
+    unsigned long IntIter, nIntIter;
+    bool unsteady;
+    
+    /*--- Run a single iteration of a multi-zone problem by looping over all
+     zones and executing the iterations. Note that data transers between zones
+     and other intermediate procedures may be required. ---*/
+    
+    unsteady = (config_container[MESH_0]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
+    (config_container[MESH_0]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND);
+    
+    /*--- Zone preprocessing ---*/
+    
+    for (iZone = 0; iZone < nZone; iZone++)
+        iteration_container[iZone][INST_0]->Preprocess(output_container[iZone], integration_container, geometry_container, solver_container, numerics_container, config_container, surface_movement, grid_movement, FFDBox, iZone, INST_0);
+    
+    /*--- Updating zone interface communication patterns,
+     needed only for unsteady simulation since for steady problems
+     this is done once in the interpolator_container constructor
+     at the beginning of the computation ---*/
+    
+    if ( unsteady ) {
+        for (iZone = 0; iZone < nZone; iZone++) {
+            for (jZone = 0; jZone < nZone; jZone++)
+                if(jZone != iZone && interpolator_container[iZone][jZone] != nullptr)
+                    interpolator_container[iZone][jZone]->SetTransferCoeff(config_container);
+        }
+    }
+    
+    /*--- Begin Unsteady pseudo-time stepping internal loop, if not unsteady it does only one step --*/
+    
+    if (unsteady)
+        nIntIter = config_container[MESH_0]->GetnInner_Iter();
+    else
+        nIntIter = 1;
+    
+    for (IntIter = 0; IntIter < nIntIter; IntIter++) {
+        
+        /*--- At each pseudo time-step updates transfer data ---*/
+        for (iZone = 0; iZone < nZone; iZone++)
+            for (jZone = 0; jZone < nZone; jZone++)
+                if(jZone != iZone && interface_container[iZone][jZone] != nullptr)
+                    Transfer_Data(iZone, jZone);
+        
+        /*--- For each zone runs one single iteration ---*/
+        
+        for (iZone = 0; iZone < nZone; iZone++) {
+            config_container[iZone]->SetInnerIter(IntIter);
+            iteration_container[iZone][INST_0]->Iterate(output_container[iZone], integration_container, geometry_container, solver_container, numerics_container,
+                                                        config_container, surface_movement, grid_movement, FFDBox, iZone, INST_0);
+        }
+        
+        /*--- Check convergence in each zone --*/
+        
+        checkConvergence = 0;
+        for (iZone = 0; iZone < nZone; iZone++)
+            checkConvergence += (int) integration_container[iZone][INST_0][FLOW_SOL]->GetConvergence();
+        
+        /*--- If convergence was reached in every zone --*/
+        
+        if (checkConvergence == nZone) break;
+    }
+    
 }
 
 void CFluidDriver::Transfer_Data(unsigned short donorZone, unsigned short targetZone) {
-
-  interface_container[donorZone][targetZone]->BroadcastData(*interpolator_container[donorZone][targetZone].get(),
-    solver_container[donorZone][INST_0][MESH_0][FLOW_SOL], solver_container[targetZone][INST_0][MESH_0][FLOW_SOL],
-    geometry_container[donorZone][INST_0][MESH_0], geometry_container[targetZone][INST_0][MESH_0],
-    config_container[donorZone], config_container[targetZone]);
-
-  if (config_container[targetZone]->GetKind_Solver() == MAIN_SOLVER::RANS) {
+    
     interface_container[donorZone][targetZone]->BroadcastData(*interpolator_container[donorZone][targetZone].get(),
-      solver_container[donorZone][INST_0][MESH_0][TURB_SOL], solver_container[targetZone][INST_0][MESH_0][TURB_SOL],
-      geometry_container[donorZone][INST_0][MESH_0], geometry_container[targetZone][INST_0][MESH_0],
-      config_container[donorZone], config_container[targetZone]);
-  }
+                                                              solver_container[donorZone][INST_0][MESH_0][FLOW_SOL], solver_container[targetZone][INST_0][MESH_0][FLOW_SOL],
+                                                              geometry_container[donorZone][INST_0][MESH_0], geometry_container[targetZone][INST_0][MESH_0],
+                                                              config_container[donorZone], config_container[targetZone]);
+    
+    if (config_container[targetZone]->GetKind_Solver() == MAIN_SOLVER::RANS) {
+        interface_container[donorZone][targetZone]->BroadcastData(*interpolator_container[donorZone][targetZone].get(),
+                                                                  solver_container[donorZone][INST_0][MESH_0][TURB_SOL], solver_container[targetZone][INST_0][MESH_0][TURB_SOL],
+                                                                  geometry_container[donorZone][INST_0][MESH_0], geometry_container[targetZone][INST_0][MESH_0],
+                                                                  config_container[donorZone], config_container[targetZone]);
+    }
 }
 
 void CFluidDriver::Update() {
-
-  for(iZone = 0; iZone < nZone; iZone++)
-    iteration_container[iZone][INST_0]->Update(output_container[iZone], integration_container, geometry_container,
-         solver_container, numerics_container, config_container,
-         surface_movement, grid_movement, FFDBox, iZone, INST_0);
+    
+    for(iZone = 0; iZone < nZone; iZone++)
+        iteration_container[iZone][INST_0]->Update(output_container[iZone], integration_container, geometry_container,
+                                                   solver_container, numerics_container, config_container,
+                                                   surface_movement, grid_movement, FFDBox, iZone, INST_0);
 }
 
 void CFluidDriver::DynamicMeshUpdate(unsigned long TimeIter) {
-
-  bool harmonic_balance;
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-   harmonic_balance = (config_container[iZone]->GetTime_Marching() == TIME_MARCHING::HARMONIC_BALANCE);
-    /*--- Dynamic mesh update ---*/
-    if ((config_container[iZone]->GetGrid_Movement()) && (!harmonic_balance)) {
-      iteration_container[iZone][INST_0]->SetGrid_Movement(geometry_container[iZone][INST_0], surface_movement[iZone], grid_movement[iZone][INST_0], solver_container[iZone][INST_0], config_container[iZone], 0, TimeIter );
+    
+    bool harmonic_balance;
+    
+    for (iZone = 0; iZone < nZone; iZone++) {
+        harmonic_balance = (config_container[iZone]->GetTime_Marching() == TIME_MARCHING::HARMONIC_BALANCE);
+        /*--- Dynamic mesh update ---*/
+        if ((config_container[iZone]->GetGrid_Movement()) && (!harmonic_balance)) {
+            iteration_container[iZone][INST_0]->SetGrid_Movement(geometry_container[iZone][INST_0], surface_movement[iZone], grid_movement[iZone][INST_0], solver_container[iZone][INST_0], config_container[iZone], 0, TimeIter );
+        }
     }
-  }
-
+    
 }
 bool CFluidDriver::Monitor(unsigned long ExtIter) {
-
-  /*--- Synchronization point after a single solver iteration. Compute the
-   wall clock time required. ---*/
-
-  StopTime = SU2_MPI::Wtime();
-
-  IterCount++;
-  UsedTime = (StopTime - StartTime) + UsedTimeCompute;
-
-  /*--- Check if there is any change in the runtime parameters ---*/
-
-  CConfig *runtime = nullptr;
-  strcpy(runtime_file_name, "runtime.dat");
-  runtime = new CConfig(runtime_file_name, config_container[ZONE_0]);
-  runtime->SetTimeIter(ExtIter);
-  delete runtime;
-
-  /*--- Check whether the current simulation has reached the specified
-   convergence criteria, and set StopCalc to true, if so. ---*/
-
-  switch (config_container[ZONE_0]->GetKind_Solver()) {
-    case MAIN_SOLVER::EULER: case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::RANS:
-    case MAIN_SOLVER::NEMO_EULER: case MAIN_SOLVER::NEMO_NAVIER_STOKES:
-      StopCalc = integration_container[ZONE_0][INST_0][FLOW_SOL]->GetConvergence(); break;
-    case MAIN_SOLVER::HEAT_EQUATION:
-      StopCalc = integration_container[ZONE_0][INST_0][HEAT_SOL]->GetConvergence(); break;
-    case MAIN_SOLVER::FEM_ELASTICITY:
-      StopCalc = integration_container[ZONE_0][INST_0][FEA_SOL]->GetConvergence(); break;
-    case MAIN_SOLVER::ADJ_EULER: case MAIN_SOLVER::ADJ_NAVIER_STOKES: case MAIN_SOLVER::ADJ_RANS:
-    case MAIN_SOLVER::DISC_ADJ_EULER: case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_RANS:
-    case MAIN_SOLVER::DISC_ADJ_INC_EULER: case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_INC_RANS:
-    case MAIN_SOLVER::DISC_ADJ_FEM_EULER: case MAIN_SOLVER::DISC_ADJ_FEM_NS: case MAIN_SOLVER::DISC_ADJ_FEM_RANS:
-      StopCalc = integration_container[ZONE_0][INST_0][ADJFLOW_SOL]->GetConvergence(); break;
-    default:
-      break;
-  }
-
-  /*--- Set StopCalc to true if max. number of iterations has been reached ---*/
-
-  StopCalc = StopCalc || (ExtIter == Max_Iter - 1);
-
-  return StopCalc;
-
+    
+    /*--- Synchronization point after a single solver iteration. Compute the
+     wall clock time required. ---*/
+    
+    StopTime = SU2_MPI::Wtime();
+    
+    IterCount++;
+    UsedTime = (StopTime - StartTime) + UsedTimeCompute;
+    
+    /*--- Check if there is any change in the runtime parameters ---*/
+    
+    CConfig *runtime = nullptr;
+    strcpy(runtime_file_name, "runtime.dat");
+    runtime = new CConfig(runtime_file_name, config_container[ZONE_0]);
+    runtime->SetTimeIter(ExtIter);
+    delete runtime;
+    
+    /*--- Check whether the current simulation has reached the specified
+     convergence criteria, and set StopCalc to true, if so. ---*/
+    
+    switch (config_container[ZONE_0]->GetKind_Solver()) {
+        case MAIN_SOLVER::EULER: case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::RANS:
+        case MAIN_SOLVER::NEMO_EULER: case MAIN_SOLVER::NEMO_NAVIER_STOKES:
+            StopCalc = integration_container[ZONE_0][INST_0][FLOW_SOL]->GetConvergence(); break;
+        case MAIN_SOLVER::HEAT_EQUATION:
+            StopCalc = integration_container[ZONE_0][INST_0][HEAT_SOL]->GetConvergence(); break;
+        case MAIN_SOLVER::FEM_ELASTICITY:
+            StopCalc = integration_container[ZONE_0][INST_0][FEA_SOL]->GetConvergence(); break;
+        case MAIN_SOLVER::ADJ_EULER: case MAIN_SOLVER::ADJ_NAVIER_STOKES: case MAIN_SOLVER::ADJ_RANS:
+        case MAIN_SOLVER::DISC_ADJ_EULER: case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_RANS:
+        case MAIN_SOLVER::DISC_ADJ_INC_EULER: case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_INC_RANS:
+        case MAIN_SOLVER::DISC_ADJ_FEM_EULER: case MAIN_SOLVER::DISC_ADJ_FEM_NS: case MAIN_SOLVER::DISC_ADJ_FEM_RANS:
+            StopCalc = integration_container[ZONE_0][INST_0][ADJFLOW_SOL]->GetConvergence(); break;
+        default:
+            break;
+    }
+    
+    /*--- Set StopCalc to true if max. number of iterations has been reached ---*/
+    
+    StopCalc = StopCalc || (ExtIter == Max_Iter - 1);
+    
+    return StopCalc;
+    
 }
 
 
 void CFluidDriver::Output(unsigned long InnerIter) {
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    const auto inst = config_container[iZone]->GetiInst();
-
-    for (iInst = 0; iInst < nInst[iZone]; ++iInst) {
-      config_container[iZone]->SetiInst(iInst);
-      output_container[iZone]->SetResult_Files(geometry_container[iZone][iInst][MESH_0],
-                                               config_container[iZone],
-                                               solver_container[iZone][iInst][MESH_0],
-                                               InnerIter, StopCalc);
+    
+    for (iZone = 0; iZone < nZone; iZone++) {
+        const auto inst = config_container[iZone]->GetiInst();
+        
+        for (iInst = 0; iInst < nInst[iZone]; ++iInst) {
+            config_container[iZone]->SetiInst(iInst);
+            output_container[iZone]->SetResult_Files(geometry_container[iZone][iInst][MESH_0],
+                                                     config_container[iZone],
+                                                     solver_container[iZone][iInst][MESH_0],
+                                                     InnerIter, StopCalc);
+        }
+        config_container[iZone]->SetiInst(inst);
     }
-    config_container[iZone]->SetiInst(inst);
-  }
-
+    
 }
 
 
 CTurbomachineryDriver::CTurbomachineryDriver(char* confFile, unsigned short val_nZone,
                                              SU2_Comm MPICommunicator):
-                                             CFluidDriver(confFile, val_nZone, MPICommunicator) {
-
-  output_legacy = COutputFactory::CreateLegacyOutput(config_container[ZONE_0]);
-
-  /*--- LEGACY OUTPUT (going to be removed soon) --- */
-
-  /*--- Open the convergence history file ---*/
-  ConvHist_file = nullptr;
-  ConvHist_file = new ofstream*[nZone];
-  for (iZone = 0; iZone < nZone; iZone++) {
-    ConvHist_file[iZone] = nullptr;
-    if (rank == MASTER_NODE){
-      ConvHist_file[iZone] = new ofstream[nInst[iZone]];
-      for (iInst = 0; iInst < nInst[iZone]; iInst++) {
-        output_legacy->SetConvHistory_Header(&ConvHist_file[iZone][iInst], config_container[iZone], iZone, iInst);
-      }
+CFluidDriver(confFile, val_nZone, MPICommunicator) {
+    
+    output_legacy = COutputFactory::CreateLegacyOutput(config_container[ZONE_0]);
+    
+    /*--- LEGACY OUTPUT (going to be removed soon) --- */
+    
+    /*--- Open the convergence history file ---*/
+    ConvHist_file = nullptr;
+    ConvHist_file = new ofstream*[nZone];
+    for (iZone = 0; iZone < nZone; iZone++) {
+        ConvHist_file[iZone] = nullptr;
+        if (rank == MASTER_NODE){
+            ConvHist_file[iZone] = new ofstream[nInst[iZone]];
+            for (iInst = 0; iInst < nInst[iZone]; iInst++) {
+                output_legacy->SetConvHistory_Header(&ConvHist_file[iZone][iInst], config_container[iZone], iZone, iInst);
+            }
+        }
+    }
+    
+    if (nZone > 1){
+        Max_Iter = config_container[ZONE_0]->GetnOuter_Iter();
     }
-  }
-
-  if (nZone > 1){
-    Max_Iter = config_container[ZONE_0]->GetnOuter_Iter();
-  }
 }
 
 CTurbomachineryDriver::~CTurbomachineryDriver(void) {
-  if (rank == MASTER_NODE){
-    /*--- Close the convergence history file. ---*/
-    for (iZone = 0; iZone < nZone; iZone++) {
-      for (iInst = 0; iInst < 1; iInst++) {
-        ConvHist_file[iZone][iInst].close();
-      }
-      delete [] ConvHist_file[iZone];
+    if (rank == MASTER_NODE){
+        /*--- Close the convergence history file. ---*/
+        for (iZone = 0; iZone < nZone; iZone++) {
+            for (iInst = 0; iInst < 1; iInst++) {
+                ConvHist_file[iZone][iInst].close();
+            }
+            delete [] ConvHist_file[iZone];
+        }
+        delete [] ConvHist_file;
     }
-    delete [] ConvHist_file;
-  }
 }
 
 void CTurbomachineryDriver::Run() {
-
-  /*--- Run a single iteration of a multi-zone problem by looping over all
-   zones and executing the iterations. Note that data transers between zones
-   and other intermediate procedures may be required. ---*/
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    iteration_container[iZone][INST_0]->Preprocess(output_container[iZone], integration_container, geometry_container,
-                                           solver_container, numerics_container, config_container,
-                                           surface_movement, grid_movement, FFDBox, iZone, INST_0);
-  }
-
-  /* --- Update the mixing-plane interface ---*/
-  for (iZone = 0; iZone < nZone; iZone++) {
-    if(mixingplane)SetMixingPlane(iZone);
-  }
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    iteration_container[iZone][INST_0]->Iterate(output_container[iZone], integration_container, geometry_container,
-                                        solver_container, numerics_container, config_container,
-                                        surface_movement, grid_movement, FFDBox, iZone, INST_0);
-  }
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    iteration_container[iZone][INST_0]->Postprocess(output_container[iZone], integration_container, geometry_container,
-                                      solver_container, numerics_container, config_container,
-                                      surface_movement, grid_movement, FFDBox, iZone, INST_0);
-  }
-
-  if (rank == MASTER_NODE){
-    SetTurboPerformance(ZONE_0);
-  }
-
-
+    
+    /*--- Run a single iteration of a multi-zone problem by looping over all
+     zones and executing the iterations. Note that data transers between zones
+     and other intermediate procedures may be required. ---*/
+    
+    for (iZone = 0; iZone < nZone; iZone++) {
+        iteration_container[iZone][INST_0]->Preprocess(output_container[iZone], integration_container, geometry_container,
+                                                       solver_container, numerics_container, config_container,
+                                                       surface_movement, grid_movement, FFDBox, iZone, INST_0);
+    }
+    
+    /* --- Update the mixing-plane interface ---*/
+    for (iZone = 0; iZone < nZone; iZone++) {
+        if(mixingplane)SetMixingPlane(iZone);
+    }
+    
+    for (iZone = 0; iZone < nZone; iZone++) {
+        iteration_container[iZone][INST_0]->Iterate(output_container[iZone], integration_container, geometry_container,
+                                                    solver_container, numerics_container, config_container,
+                                                    surface_movement, grid_movement, FFDBox, iZone, INST_0);
+    }
+    
+    for (iZone = 0; iZone < nZone; iZone++) {
+        iteration_container[iZone][INST_0]->Postprocess(output_container[iZone], integration_container, geometry_container,
+                                                        solver_container, numerics_container, config_container,
+                                                        surface_movement, grid_movement, FFDBox, iZone, INST_0);
+    }
+    
+    if (rank == MASTER_NODE){
+        SetTurboPerformance(ZONE_0);
+    }
+    
+    
 }
 
 void CTurbomachineryDriver::SetMixingPlane(unsigned short donorZone){
-
-  unsigned short targetZone, nMarkerInt, iMarkerInt ;
-  nMarkerInt     = config_container[donorZone]->GetnMarker_MixingPlaneInterface()/2;
-
-  /* --- transfer the average value from the donorZone to the targetZone*/
-  for (iMarkerInt = 1; iMarkerInt <= nMarkerInt; iMarkerInt++){
-    for (targetZone = 0; targetZone < nZone; targetZone++) {
-      if (targetZone != donorZone){
-        interface_container[donorZone][targetZone]->AllgatherAverage(solver_container[donorZone][INST_0][MESH_0][FLOW_SOL],solver_container[targetZone][INST_0][MESH_0][FLOW_SOL],
-            geometry_container[donorZone][INST_0][MESH_0],geometry_container[targetZone][INST_0][MESH_0],
-            config_container[donorZone], config_container[targetZone], iMarkerInt );
-      }
+    
+    unsigned short targetZone, nMarkerInt, iMarkerInt ;
+    nMarkerInt     = config_container[donorZone]->GetnMarker_MixingPlaneInterface()/2;
+    
+    /* --- transfer the average value from the donorZone to the targetZone*/
+    for (iMarkerInt = 1; iMarkerInt <= nMarkerInt; iMarkerInt++){
+        for (targetZone = 0; targetZone < nZone; targetZone++) {
+            if (targetZone != donorZone){
+                interface_container[donorZone][targetZone]->AllgatherAverage(solver_container[donorZone][INST_0][MESH_0][FLOW_SOL],solver_container[targetZone][INST_0][MESH_0][FLOW_SOL],
+                                                                             geometry_container[donorZone][INST_0][MESH_0],geometry_container[targetZone][INST_0][MESH_0],
+                                                                             config_container[donorZone], config_container[targetZone], iMarkerInt );
+            }
+        }
     }
-  }
 }
 
 void CTurbomachineryDriver::SetTurboPerformance(unsigned short targetZone){
-
-  unsigned short donorZone;
-  //IMPORTANT this approach of multi-zone performances rely upon the fact that turbomachinery markers follow the natural (stator-rotor) development of the real machine.
-  /* --- transfer the local turboperfomance quantities (for each blade)  from all the donorZones to the targetZone (ZONE_0) ---*/
-  for (donorZone = 1; donorZone < nZone; donorZone++) {
-    interface_container[donorZone][targetZone]->GatherAverageValues(solver_container[donorZone][INST_0][MESH_0][FLOW_SOL],solver_container[targetZone][INST_0][MESH_0][FLOW_SOL], donorZone);
-  }
-
-  /* --- compute turboperformance for each stage and the global machine ---*/
-
- output_legacy->ComputeTurboPerformance(solver_container[targetZone][INST_0][MESH_0][FLOW_SOL], geometry_container[targetZone][INST_0][MESH_0], config_container[targetZone]);
-
+    
+    unsigned short donorZone;
+    //IMPORTANT this approach of multi-zone performances rely upon the fact that turbomachinery markers follow the natural (stator-rotor) development of the real machine.
+    /* --- transfer the local turboperfomance quantities (for each blade)  from all the donorZones to the targetZone (ZONE_0) ---*/
+    for (donorZone = 1; donorZone < nZone; donorZone++) {
+        interface_container[donorZone][targetZone]->GatherAverageValues(solver_container[donorZone][INST_0][MESH_0][FLOW_SOL],solver_container[targetZone][INST_0][MESH_0][FLOW_SOL], donorZone);
+    }
+    
+    /* --- compute turboperformance for each stage and the global machine ---*/
+    
+    output_legacy->ComputeTurboPerformance(solver_container[targetZone][INST_0][MESH_0][FLOW_SOL], geometry_container[targetZone][INST_0][MESH_0], config_container[targetZone]);
+    
 }
 
 
 bool CTurbomachineryDriver::Monitor(unsigned long ExtIter) {
-
-  su2double rot_z_ini, rot_z_final ,rot_z;
-  su2double outPres_ini, outPres_final, outPres;
-  unsigned long rampFreq, finalRamp_Iter;
-  unsigned short iMarker, KindBC, KindBCOption;
-  string Marker_Tag;
-
-  bool print;
-
-  /*--- Synchronization point after a single solver iteration. Compute the
-   wall clock time required. ---*/
-
-  StopTime = SU2_MPI::Wtime();
-
-  IterCount++;
-  UsedTime = (StopTime - StartTime);
-
-
-  /*--- Check if there is any change in the runtime parameters ---*/
-  CConfig *runtime = nullptr;
-  strcpy(runtime_file_name, "runtime.dat");
-  runtime = new CConfig(runtime_file_name, config_container[ZONE_0]);
-  runtime->SetInnerIter(ExtIter);
-  delete runtime;
-
-  /*--- Update the convergence history file (serial and parallel computations). ---*/
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    for (iInst = 0; iInst < nInst[iZone]; iInst++)
-      output_legacy->SetConvHistory_Body(&ConvHist_file[iZone][iInst], geometry_container, solver_container,
-          config_container, integration_container, false, UsedTime, iZone, iInst);
-  }
-
-  /*--- ROTATING FRAME Ramp: Compute the updated rotational velocity. ---*/
-  if (config_container[ZONE_0]->GetGrid_Movement() && config_container[ZONE_0]->GetRampRotatingFrame()) {
-    rampFreq       = SU2_TYPE::Int(config_container[ZONE_0]->GetRampRotatingFrame_Coeff(1));
-    finalRamp_Iter = SU2_TYPE::Int(config_container[ZONE_0]->GetRampRotatingFrame_Coeff(2));
-    rot_z_ini = config_container[ZONE_0]->GetRampRotatingFrame_Coeff(0);
-    print = false;
-    if(ExtIter % rampFreq == 0 &&  ExtIter <= finalRamp_Iter){
-
-      for (iZone = 0; iZone < nZone; iZone++) {
-        rot_z_final = config_container[iZone]->GetFinalRotation_Rate_Z();
-        if(abs(rot_z_final) > 0.0){
-          rot_z = rot_z_ini + ExtIter*( rot_z_final - rot_z_ini)/finalRamp_Iter;
-          config_container[iZone]->SetRotation_Rate(2, rot_z);
-          if(rank == MASTER_NODE && print && ExtIter > 0) {
-            cout << endl << " Updated rotating frame grid velocities";
-            cout << " for zone " << iZone << "." << endl;
-          }
-          geometry_container[iZone][INST_0][MESH_0]->SetRotationalVelocity(config_container[iZone], print);
-          geometry_container[iZone][INST_0][MESH_0]->SetShroudVelocity(config_container[iZone]);
+    
+    su2double rot_z_ini, rot_z_final ,rot_z;
+    su2double outPres_ini, outPres_final, outPres;
+    unsigned long rampFreq, finalRamp_Iter;
+    unsigned short iMarker, KindBC, KindBCOption;
+    string Marker_Tag;
+    
+    bool print;
+    
+    /*--- Synchronization point after a single solver iteration. Compute the
+     wall clock time required. ---*/
+    
+    StopTime = SU2_MPI::Wtime();
+    
+    IterCount++;
+    UsedTime = (StopTime - StartTime);
+    
+    
+    /*--- Check if there is any change in the runtime parameters ---*/
+    CConfig *runtime = nullptr;
+    strcpy(runtime_file_name, "runtime.dat");
+    runtime = new CConfig(runtime_file_name, config_container[ZONE_0]);
+    runtime->SetInnerIter(ExtIter);
+    delete runtime;
+    
+    /*--- Update the convergence history file (serial and parallel computations). ---*/
+    
+    for (iZone = 0; iZone < nZone; iZone++) {
+        for (iInst = 0; iInst < nInst[iZone]; iInst++)
+            output_legacy->SetConvHistory_Body(&ConvHist_file[iZone][iInst], geometry_container, solver_container,
+                                               config_container, integration_container, false, UsedTime, iZone, iInst);
+    }
+    
+    /*--- ROTATING FRAME Ramp: Compute the updated rotational velocity. ---*/
+    if (config_container[ZONE_0]->GetGrid_Movement() && config_container[ZONE_0]->GetRampRotatingFrame()) {
+        rampFreq       = SU2_TYPE::Int(config_container[ZONE_0]->GetRampRotatingFrame_Coeff(1));
+        finalRamp_Iter = SU2_TYPE::Int(config_container[ZONE_0]->GetRampRotatingFrame_Coeff(2));
+        rot_z_ini = config_container[ZONE_0]->GetRampRotatingFrame_Coeff(0);
+        print = false;
+        if(ExtIter % rampFreq == 0 &&  ExtIter <= finalRamp_Iter){
+            
+            for (iZone = 0; iZone < nZone; iZone++) {
+                rot_z_final = config_container[iZone]->GetFinalRotation_Rate_Z();
+                if(abs(rot_z_final) > 0.0){
+                    rot_z = rot_z_ini + ExtIter*( rot_z_final - rot_z_ini)/finalRamp_Iter;
+                    config_container[iZone]->SetRotation_Rate(2, rot_z);
+                    if(rank == MASTER_NODE && print && ExtIter > 0) {
+                        cout << endl << " Updated rotating frame grid velocities";
+                        cout << " for zone " << iZone << "." << endl;
+                    }
+                    geometry_container[iZone][INST_0][MESH_0]->SetRotationalVelocity(config_container[iZone], print);
+                    geometry_container[iZone][INST_0][MESH_0]->SetShroudVelocity(config_container[iZone]);
+                }
+            }
+            
+            for (iZone = 0; iZone < nZone; iZone++) {
+                geometry_container[iZone][INST_0][MESH_0]->SetAvgTurboValue(config_container[iZone], iZone, INFLOW, false);
+                geometry_container[iZone][INST_0][MESH_0]->SetAvgTurboValue(config_container[iZone],iZone, OUTFLOW, false);
+                geometry_container[iZone][INST_0][MESH_0]->GatherInOutAverageValues(config_container[iZone], false);
+                
+            }
+            
+            for (iZone = 1; iZone < nZone; iZone++) {
+                interface_container[iZone][ZONE_0]->GatherAverageTurboGeoValues(geometry_container[iZone][INST_0][MESH_0],geometry_container[ZONE_0][INST_0][MESH_0], iZone);
+            }
+            
         }
-      }
-
-      for (iZone = 0; iZone < nZone; iZone++) {
-        geometry_container[iZone][INST_0][MESH_0]->SetAvgTurboValue(config_container[iZone], iZone, INFLOW, false);
-        geometry_container[iZone][INST_0][MESH_0]->SetAvgTurboValue(config_container[iZone],iZone, OUTFLOW, false);
-        geometry_container[iZone][INST_0][MESH_0]->GatherInOutAverageValues(config_container[iZone], false);
-
-      }
-
-      for (iZone = 1; iZone < nZone; iZone++) {
-        interface_container[iZone][ZONE_0]->GatherAverageTurboGeoValues(geometry_container[iZone][INST_0][MESH_0],geometry_container[ZONE_0][INST_0][MESH_0], iZone);
-      }
-
     }
-  }
-
-
-  /*--- Outlet Pressure Ramp: Compute the updated rotational velocity. ---*/
-  if (config_container[ZONE_0]->GetRampOutletPressure()) {
-    rampFreq       = SU2_TYPE::Int(config_container[ZONE_0]->GetRampOutletPressure_Coeff(1));
-    finalRamp_Iter = SU2_TYPE::Int(config_container[ZONE_0]->GetRampOutletPressure_Coeff(2));
-    outPres_ini    = config_container[ZONE_0]->GetRampOutletPressure_Coeff(0);
-    outPres_final  = config_container[ZONE_0]->GetFinalOutletPressure();
-
-    if(ExtIter % rampFreq == 0 &&  ExtIter <= finalRamp_Iter){
-      outPres = outPres_ini + ExtIter*(outPres_final - outPres_ini)/finalRamp_Iter;
-      if(rank == MASTER_NODE) config_container[ZONE_0]->SetMonitotOutletPressure(outPres);
-
-      for (iZone = 0; iZone < nZone; iZone++) {
-        for (iMarker = 0; iMarker < config_container[iZone]->GetnMarker_All(); iMarker++) {
-          KindBC = config_container[iZone]->GetMarker_All_KindBC(iMarker);
-          switch (KindBC) {
-          case RIEMANN_BOUNDARY:
-            Marker_Tag         = config_container[iZone]->GetMarker_All_TagBound(iMarker);
-            KindBCOption       = config_container[iZone]->GetKind_Data_Riemann(Marker_Tag);
-            if(KindBCOption == STATIC_PRESSURE || KindBCOption == RADIAL_EQUILIBRIUM ){
-              SU2_MPI::Error("Outlet pressure ramp only implemented for NRBC", CURRENT_FUNCTION);
-            }
-            break;
-          case GILES_BOUNDARY:
-            Marker_Tag         = config_container[iZone]->GetMarker_All_TagBound(iMarker);
-            KindBCOption       = config_container[iZone]->GetKind_Data_Giles(Marker_Tag);
-            if(KindBCOption == STATIC_PRESSURE || KindBCOption == STATIC_PRESSURE_1D || KindBCOption == RADIAL_EQUILIBRIUM ){
-              config_container[iZone]->SetGiles_Var1(outPres, Marker_Tag);
+    
+    
+    /*--- Outlet Pressure Ramp: Compute the updated rotational velocity. ---*/
+    if (config_container[ZONE_0]->GetRampOutletPressure()) {
+        rampFreq       = SU2_TYPE::Int(config_container[ZONE_0]->GetRampOutletPressure_Coeff(1));
+        finalRamp_Iter = SU2_TYPE::Int(config_container[ZONE_0]->GetRampOutletPressure_Coeff(2));
+        outPres_ini    = config_container[ZONE_0]->GetRampOutletPressure_Coeff(0);
+        outPres_final  = config_container[ZONE_0]->GetFinalOutletPressure();
+        
+        if(ExtIter % rampFreq == 0 &&  ExtIter <= finalRamp_Iter){
+            outPres = outPres_ini + ExtIter*(outPres_final - outPres_ini)/finalRamp_Iter;
+            if(rank == MASTER_NODE) config_container[ZONE_0]->SetMonitotOutletPressure(outPres);
+            
+            for (iZone = 0; iZone < nZone; iZone++) {
+                for (iMarker = 0; iMarker < config_container[iZone]->GetnMarker_All(); iMarker++) {
+                    KindBC = config_container[iZone]->GetMarker_All_KindBC(iMarker);
+                    switch (KindBC) {
+                        case RIEMANN_BOUNDARY:
+                            Marker_Tag         = config_container[iZone]->GetMarker_All_TagBound(iMarker);
+                            KindBCOption       = config_container[iZone]->GetKind_Data_Riemann(Marker_Tag);
+                            if(KindBCOption == STATIC_PRESSURE || KindBCOption == RADIAL_EQUILIBRIUM ){
+                                SU2_MPI::Error("Outlet pressure ramp only implemented for NRBC", CURRENT_FUNCTION);
+                            }
+                            break;
+                        case GILES_BOUNDARY:
+                            Marker_Tag         = config_container[iZone]->GetMarker_All_TagBound(iMarker);
+                            KindBCOption       = config_container[iZone]->GetKind_Data_Giles(Marker_Tag);
+                            if(KindBCOption == STATIC_PRESSURE || KindBCOption == STATIC_PRESSURE_1D || KindBCOption == RADIAL_EQUILIBRIUM ){
+                                config_container[iZone]->SetGiles_Var1(outPres, Marker_Tag);
+                            }
+                            break;
+                    }
+                }
             }
-            break;
-          }
         }
-      }
     }
-  }
-
-
-  /*--- Check whether the current simulation has reached the specified
-   convergence criteria, and set StopCalc to true, if so. ---*/
-
-  switch (config_container[ZONE_0]->GetKind_Solver()) {
-  case MAIN_SOLVER::EULER: case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::RANS:
-  case MAIN_SOLVER::INC_EULER: case MAIN_SOLVER::INC_NAVIER_STOKES: case MAIN_SOLVER::INC_RANS:
-  case MAIN_SOLVER::NEMO_EULER: case MAIN_SOLVER::NEMO_NAVIER_STOKES:
-    StopCalc = integration_container[ZONE_0][INST_0][FLOW_SOL]->GetConvergence();
-    break;
-  case MAIN_SOLVER::DISC_ADJ_EULER: case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_RANS:
-  case MAIN_SOLVER::DISC_ADJ_INC_EULER: case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_INC_RANS:
-  case MAIN_SOLVER::DISC_ADJ_FEM_EULER: case MAIN_SOLVER::DISC_ADJ_FEM_NS: case MAIN_SOLVER::DISC_ADJ_FEM_RANS:
-    StopCalc = integration_container[ZONE_0][INST_0][ADJFLOW_SOL]->GetConvergence();
-    break;
-  default:
-    break;
-
-  }
-
-  /*--- Set StopCalc to true if max. number of iterations has been reached ---*/
-
-  StopCalc = StopCalc || (ExtIter == Max_Iter - 1);
-
-  return StopCalc;
-
+    
+    
+    /*--- Check whether the current simulation has reached the specified
+     convergence criteria, and set StopCalc to true, if so. ---*/
+    
+    switch (config_container[ZONE_0]->GetKind_Solver()) {
+        case MAIN_SOLVER::EULER: case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::RANS:
+        case MAIN_SOLVER::INC_EULER: case MAIN_SOLVER::INC_NAVIER_STOKES: case MAIN_SOLVER::INC_RANS:
+        case MAIN_SOLVER::NEMO_EULER: case MAIN_SOLVER::NEMO_NAVIER_STOKES:
+            StopCalc = integration_container[ZONE_0][INST_0][FLOW_SOL]->GetConvergence();
+            break;
+        case MAIN_SOLVER::DISC_ADJ_EULER: case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_RANS:
+        case MAIN_SOLVER::DISC_ADJ_INC_EULER: case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_INC_RANS:
+        case MAIN_SOLVER::DISC_ADJ_FEM_EULER: case MAIN_SOLVER::DISC_ADJ_FEM_NS: case MAIN_SOLVER::DISC_ADJ_FEM_RANS:
+            StopCalc = integration_container[ZONE_0][INST_0][ADJFLOW_SOL]->GetConvergence();
+            break;
+        default:
+            break;
+            
+    }
+    
+    /*--- Set StopCalc to true if max. number of iterations has been reached ---*/
+    
+    StopCalc = StopCalc || (ExtIter == Max_Iter - 1);
+    
+    return StopCalc;
+    
 }
 
 CHBDriver::CHBDriver(char* confFile,
-    unsigned short val_nZone,
-    SU2_Comm MPICommunicator) : CFluidDriver(confFile,
-        val_nZone,
-        MPICommunicator) {
-  unsigned short kInst;
-
-  nInstHB = nInst[ZONE_0];
-
-  D = nullptr;
-  /*--- allocate dynamic memory for the Harmonic Balance operator ---*/
-  D = new su2double*[nInstHB]; for (kInst = 0; kInst < nInstHB; kInst++) D[kInst] = new su2double[nInstHB];
-
-  output_legacy = COutputFactory::CreateLegacyOutput(config_container[ZONE_0]);
-
-  /*--- Open the convergence history file ---*/
-  ConvHist_file = nullptr;
-  ConvHist_file = new ofstream*[nZone];
-  for (iZone = 0; iZone < nZone; iZone++) {
-    ConvHist_file[iZone] = nullptr;
-    if (rank == MASTER_NODE){
-      ConvHist_file[iZone] = new ofstream[nInst[iZone]];
-      for (iInst = 0; iInst < nInst[iZone]; iInst++) {
-        output_legacy->SetConvHistory_Header(&ConvHist_file[iZone][iInst], config_container[iZone], iZone, iInst);
-      }
-    }
-  }
-
-
-}
+                     unsigned short val_nZone,
+                     SU2_Comm MPICommunicator) : CFluidDriver(confFile,
+                                                              val_nZone,
+                                                              MPICommunicator) {
+                         unsigned short kInst;
+                         
+                         nInstHB = nInst[ZONE_0];
+                         
+                         D = nullptr;
+                         /*--- allocate dynamic memory for the Harmonic Balance operator ---*/
+                         D = new su2double*[nInstHB]; for (kInst = 0; kInst < nInstHB; kInst++) D[kInst] = new su2double[nInstHB];
+                         
+                         output_legacy = COutputFactory::CreateLegacyOutput(config_container[ZONE_0]);
+                         
+                         /*--- Open the convergence history file ---*/
+                         ConvHist_file = nullptr;
+                         ConvHist_file = new ofstream*[nZone];
+                         for (iZone = 0; iZone < nZone; iZone++) {
+                             ConvHist_file[iZone] = nullptr;
+                             if (rank == MASTER_NODE){
+                                 ConvHist_file[iZone] = new ofstream[nInst[iZone]];
+                                 for (iInst = 0; iInst < nInst[iZone]; iInst++) {
+                                     output_legacy->SetConvHistory_Header(&ConvHist_file[iZone][iInst], config_container[iZone], iZone, iInst);
+                                 }
+                             }
+                         }
+                         
+                         
+                     }
 
 CHBDriver::~CHBDriver(void) {
-
-  unsigned short kInst;
-
-  /*--- delete dynamic memory for the Harmonic Balance operator ---*/
-  for (kInst = 0; kInst < nInstHB; kInst++) delete [] D[kInst];
-  delete [] D;
-
-  if (rank == MASTER_NODE){
-  /*--- Close the convergence history file. ---*/
-  for (iZone = 0; iZone < nZone; iZone++) {
-    for (iInst = 0; iInst < nInstHB; iInst++) {
-      ConvHist_file[iZone][iInst].close();
+    
+    unsigned short kInst;
+    
+    /*--- delete dynamic memory for the Harmonic Balance operator ---*/
+    for (kInst = 0; kInst < nInstHB; kInst++) delete [] D[kInst];
+    delete [] D;
+    
+    if (rank == MASTER_NODE){
+        /*--- Close the convergence history file. ---*/
+        for (iZone = 0; iZone < nZone; iZone++) {
+            for (iInst = 0; iInst < nInstHB; iInst++) {
+                ConvHist_file[iZone][iInst].close();
+            }
+            delete [] ConvHist_file[iZone];
+        }
+        delete [] ConvHist_file;
     }
-    delete [] ConvHist_file[iZone];
-  }
-  delete [] ConvHist_file;
-  }
 }
 
 
 void CHBDriver::Run() {
-
-  /*--- Run a single iteration of a Harmonic Balance problem. Preprocess all
-   all zones before beginning the iteration. ---*/
-
-  for (iInst = 0; iInst < nInstHB; iInst++)
-    iteration_container[ZONE_0][iInst]->Preprocess(output_container[ZONE_0], integration_container, geometry_container,
-        solver_container, numerics_container, config_container,
-        surface_movement, grid_movement, FFDBox, ZONE_0, iInst);
-
-  for (iInst = 0; iInst < nInstHB; iInst++)
-    iteration_container[ZONE_0][iInst]->Iterate(output_container[ZONE_0], integration_container, geometry_container,
-        solver_container, numerics_container, config_container,
-        surface_movement, grid_movement, FFDBox, ZONE_0, iInst);
-
-  /*--- Update the convergence history file (serial and parallel computations). ---*/
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    for (iInst = 0; iInst < nInst[iZone]; iInst++)
-      output_legacy->SetConvHistory_Body(&ConvHist_file[iZone][iInst], geometry_container, solver_container,
-          config_container, integration_container, false, UsedTime, iZone, iInst);
-  }
-
+    
+    /*--- Run a single iteration of a Harmonic Balance problem. Preprocess all
+     all zones before beginning the iteration. ---*/
+    
+    for (iInst = 0; iInst < nInstHB; iInst++)
+        iteration_container[ZONE_0][iInst]->Preprocess(output_container[ZONE_0], integration_container, geometry_container,
+                                                       solver_container, numerics_container, config_container,
+                                                       surface_movement, grid_movement, FFDBox, ZONE_0, iInst);
+    
+    for (iInst = 0; iInst < nInstHB; iInst++)
+        iteration_container[ZONE_0][iInst]->Iterate(output_container[ZONE_0], integration_container, geometry_container,
+                                                    solver_container, numerics_container, config_container,
+                                                    surface_movement, grid_movement, FFDBox, ZONE_0, iInst);
+    
+    /*--- Update the convergence history file (serial and parallel computations). ---*/
+    
+    for (iZone = 0; iZone < nZone; iZone++) {
+        for (iInst = 0; iInst < nInst[iZone]; iInst++)
+            output_legacy->SetConvHistory_Body(&ConvHist_file[iZone][iInst], geometry_container, solver_container,
+                                               config_container, integration_container, false, UsedTime, iZone, iInst);
+    }
+    
 }
 
 void CHBDriver::Update() {
-
-  for (iInst = 0; iInst < nInstHB; iInst++) {
-    /*--- Compute the harmonic balance terms across all zones ---*/
-    SetHarmonicBalance(iInst);
-
-  }
-
-  /*--- Precondition the harmonic balance source terms ---*/
-  if (config_container[ZONE_0]->GetHB_Precondition() == YES) {
-    StabilizeHarmonicBalance();
-
-  }
-
-  for (iInst = 0; iInst < nInstHB; iInst++) {
-
-    /*--- Update the harmonic balance terms across all zones ---*/
-    iteration_container[ZONE_0][iInst]->Update(output_container[ZONE_0], integration_container, geometry_container,
-        solver_container, numerics_container, config_container,
-        surface_movement, grid_movement, FFDBox, ZONE_0, iInst);
-
-  }
-
+    
+    for (iInst = 0; iInst < nInstHB; iInst++) {
+        /*--- Compute the harmonic balance terms across all zones ---*/
+        SetHarmonicBalance(iInst);
+        
+    }
+    
+    /*--- Precondition the harmonic balance source terms ---*/
+    if (config_container[ZONE_0]->GetHB_Precondition() == YES) {
+        StabilizeHarmonicBalance();
+        
+    }
+    
+    for (iInst = 0; iInst < nInstHB; iInst++) {
+        
+        /*--- Update the harmonic balance terms across all zones ---*/
+        iteration_container[ZONE_0][iInst]->Update(output_container[ZONE_0], integration_container, geometry_container,
+                                                   solver_container, numerics_container, config_container,
+                                                   surface_movement, grid_movement, FFDBox, ZONE_0, iInst);
+        
+    }
+    
 }
 
 void CHBDriver::ResetConvergence() {
-
-  for(iInst = 0; iInst < nZone; iInst++) {
-    switch (config_container[ZONE_0]->GetKind_Solver()) {
-
-    case MAIN_SOLVER::EULER: case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::RANS:
-      integration_container[ZONE_0][iInst][FLOW_SOL]->SetConvergence(false);
-      if (config_container[ZONE_0]->GetKind_Solver() == MAIN_SOLVER::RANS) integration_container[ZONE_0][iInst][TURB_SOL]->SetConvergence(false);
-      if(config_container[ZONE_0]->GetKind_Trans_Model() == TURB_TRANS_MODEL::LM) integration_container[ZONE_0][iInst][TRANS_SOL]->SetConvergence(false);
-      break;
-
-    case MAIN_SOLVER::FEM_ELASTICITY:
-      integration_container[ZONE_0][iInst][FEA_SOL]->SetConvergence(false);
-      break;
-
-    case MAIN_SOLVER::ADJ_EULER: case MAIN_SOLVER::ADJ_NAVIER_STOKES: case MAIN_SOLVER::ADJ_RANS: case MAIN_SOLVER::DISC_ADJ_EULER: case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_RANS:
-      integration_container[ZONE_0][iInst][ADJFLOW_SOL]->SetConvergence(false);
-      if( (config_container[ZONE_0]->GetKind_Solver() == MAIN_SOLVER::ADJ_RANS) || (config_container[ZONE_0]->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_RANS) )
-        integration_container[ZONE_0][iInst][ADJTURB_SOL]->SetConvergence(false);
-      break;
-
-    default:
-      SU2_MPI::Error("Harmonic Balance has not been set up for this solver.", CURRENT_FUNCTION);
+    
+    for(iInst = 0; iInst < nZone; iInst++) {
+        switch (config_container[ZONE_0]->GetKind_Solver()) {
+                
+            case MAIN_SOLVER::EULER: case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::RANS:
+                integration_container[ZONE_0][iInst][FLOW_SOL]->SetConvergence(false);
+                if (config_container[ZONE_0]->GetKind_Solver() == MAIN_SOLVER::RANS) integration_container[ZONE_0][iInst][TURB_SOL]->SetConvergence(false);
+                if(config_container[ZONE_0]->GetKind_Trans_Model() == TURB_TRANS_MODEL::LM) integration_container[ZONE_0][iInst][TRANS_SOL]->SetConvergence(false);
+                break;
+                
+            case MAIN_SOLVER::FEM_ELASTICITY:
+                integration_container[ZONE_0][iInst][FEA_SOL]->SetConvergence(false);
+                break;
+                
+            case MAIN_SOLVER::ADJ_EULER: case MAIN_SOLVER::ADJ_NAVIER_STOKES: case MAIN_SOLVER::ADJ_RANS: case MAIN_SOLVER::DISC_ADJ_EULER: case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_RANS:
+                integration_container[ZONE_0][iInst][ADJFLOW_SOL]->SetConvergence(false);
+                if( (config_container[ZONE_0]->GetKind_Solver() == MAIN_SOLVER::ADJ_RANS) || (config_container[ZONE_0]->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_RANS) )
+                    integration_container[ZONE_0][iInst][ADJTURB_SOL]->SetConvergence(false);
+                break;
+                
+            default:
+                SU2_MPI::Error("Harmonic Balance has not been set up for this solver.", CURRENT_FUNCTION);
+        }
     }
-  }
-
+    
 }
 
 void CHBDriver::SetHarmonicBalance(unsigned short iInst) {
-
-  unsigned short iVar, jInst, iMGlevel;
-  unsigned short nVar = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetnVar();
-  unsigned long iPoint;
-  bool implicit = (config_container[ZONE_0]->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
-  bool adjoint = (config_container[ZONE_0]->GetContinuous_Adjoint());
-  if (adjoint) {
-    implicit = (config_container[ZONE_0]->GetKind_TimeIntScheme_AdjFlow() == EULER_IMPLICIT);
-  }
-
-  unsigned long InnerIter = config_container[ZONE_0]->GetInnerIter();
-
-  /*--- Retrieve values from the config file ---*/
-  su2double *U = new su2double[nVar];
-  su2double *U_old = new su2double[nVar];
-  su2double *Psi = new su2double[nVar];
-  su2double *Psi_old = new su2double[nVar];
-  su2double *Source = new su2double[nVar];
-  su2double deltaU, deltaPsi;
-
-  /*--- Compute period of oscillation ---*/
-  su2double period = config_container[ZONE_0]->GetHarmonicBalance_Period();
-
-  /*--- Non-dimensionalize the input period, if necessary.  */
-  period /= config_container[ZONE_0]->GetTime_Ref();
-
-  if (InnerIter == 0)
-    ComputeHB_Operator();
-
-  /*--- Compute various source terms for explicit direct, implicit direct, and adjoint problems ---*/
-  /*--- Loop over all grid levels ---*/
-  for (iMGlevel = 0; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++) {
-
-    /*--- Loop over each node in the volume mesh ---*/
-    for (iPoint = 0; iPoint < geometry_container[ZONE_0][iInst][iMGlevel]->GetnPoint(); iPoint++) {
-
-      for (iVar = 0; iVar < nVar; iVar++) {
-        Source[iVar] = 0.0;
-      }
-
-      /*--- Step across the columns ---*/
-      for (jInst = 0; jInst < nInstHB; jInst++) {
-
-        /*--- Retrieve solution at this node in current zone ---*/
-        for (iVar = 0; iVar < nVar; iVar++) {
-
-          if (!adjoint) {
-            U[iVar] = solver_container[ZONE_0][jInst][iMGlevel][FLOW_SOL]->GetNodes()->GetSolution(iPoint, iVar);
-            Source[iVar] += U[iVar]*D[iInst][jInst];
-
-            if (implicit) {
-              U_old[iVar] = solver_container[ZONE_0][jInst][iMGlevel][FLOW_SOL]->GetNodes()->GetSolution_Old(iPoint, iVar);
-              deltaU = U[iVar] - U_old[iVar];
-              Source[iVar] += deltaU*D[iInst][jInst];
+    
+    unsigned short iVar, jInst, iMGlevel;
+    unsigned short nVar = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetnVar();
+    unsigned long iPoint;
+    bool implicit = (config_container[ZONE_0]->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
+    bool adjoint = (config_container[ZONE_0]->GetContinuous_Adjoint());
+    if (adjoint) {
+        implicit = (config_container[ZONE_0]->GetKind_TimeIntScheme_AdjFlow() == EULER_IMPLICIT);
+    }
+    
+    unsigned long InnerIter = config_container[ZONE_0]->GetInnerIter();
+    
+    /*--- Retrieve values from the config file ---*/
+    su2double *U = new su2double[nVar];
+    su2double *U_old = new su2double[nVar];
+    su2double *Psi = new su2double[nVar];
+    su2double *Psi_old = new su2double[nVar];
+    su2double *Source = new su2double[nVar];
+    su2double deltaU, deltaPsi;
+    
+    /*--- Compute period of oscillation ---*/
+    su2double period = config_container[ZONE_0]->GetHarmonicBalance_Period();
+    
+    /*--- Non-dimensionalize the input period, if necessary.  */
+    period /= config_container[ZONE_0]->GetTime_Ref();
+    
+    if (InnerIter == 0)
+        ComputeHB_Operator();
+    
+    /*--- Compute various source terms for explicit direct, implicit direct, and adjoint problems ---*/
+    /*--- Loop over all grid levels ---*/
+    for (iMGlevel = 0; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++) {
+        
+        /*--- Loop over each node in the volume mesh ---*/
+        for (iPoint = 0; iPoint < geometry_container[ZONE_0][iInst][iMGlevel]->GetnPoint(); iPoint++) {
+            
+            for (iVar = 0; iVar < nVar; iVar++) {
+                Source[iVar] = 0.0;
             }
-
-          }
-
-          else {
-            Psi[iVar] = solver_container[ZONE_0][jInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->GetSolution(iPoint, iVar);
-            Source[iVar] += Psi[iVar]*D[jInst][iInst];
-
-            if (implicit) {
-              Psi_old[iVar] = solver_container[ZONE_0][jInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->GetSolution_Old(iPoint, iVar);
-              deltaPsi = Psi[iVar] - Psi_old[iVar];
-              Source[iVar] += deltaPsi*D[jInst][iInst];
+            
+            /*--- Step across the columns ---*/
+            for (jInst = 0; jInst < nInstHB; jInst++) {
+                
+                /*--- Retrieve solution at this node in current zone ---*/
+                for (iVar = 0; iVar < nVar; iVar++) {
+                    
+                    if (!adjoint) {
+                        U[iVar] = solver_container[ZONE_0][jInst][iMGlevel][FLOW_SOL]->GetNodes()->GetSolution(iPoint, iVar);
+                        Source[iVar] += U[iVar]*D[iInst][jInst];
+                        
+                        if (implicit) {
+                            U_old[iVar] = solver_container[ZONE_0][jInst][iMGlevel][FLOW_SOL]->GetNodes()->GetSolution_Old(iPoint, iVar);
+                            deltaU = U[iVar] - U_old[iVar];
+                            Source[iVar] += deltaU*D[iInst][jInst];
+                        }
+                        
+                    }
+                    
+                    else {
+                        Psi[iVar] = solver_container[ZONE_0][jInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->GetSolution(iPoint, iVar);
+                        Source[iVar] += Psi[iVar]*D[jInst][iInst];
+                        
+                        if (implicit) {
+                            Psi_old[iVar] = solver_container[ZONE_0][jInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->GetSolution_Old(iPoint, iVar);
+                            deltaPsi = Psi[iVar] - Psi_old[iVar];
+                            Source[iVar] += deltaPsi*D[jInst][iInst];
+                        }
+                    }
+                }
+                
+                /*--- Store sources for current row ---*/
+                for (iVar = 0; iVar < nVar; iVar++) {
+                    if (!adjoint) {
+                        solver_container[ZONE_0][iInst][iMGlevel][FLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iVar]);
+                    }
+                    else {
+                        solver_container[ZONE_0][iInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iVar]);
+                    }
+                }
+                
             }
-          }
-        }
-
-        /*--- Store sources for current row ---*/
-        for (iVar = 0; iVar < nVar; iVar++) {
-          if (!adjoint) {
-            solver_container[ZONE_0][iInst][iMGlevel][FLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iVar]);
-          }
-          else {
-            solver_container[ZONE_0][iInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iVar]);
-          }
         }
-
-      }
     }
-  }
-
-  /*--- Source term for a turbulence model ---*/
-  if (config_container[ZONE_0]->GetKind_Solver() == MAIN_SOLVER::RANS) {
-
-    /*--- Extra variables needed if we have a turbulence model. ---*/
-    unsigned short nVar_Turb = solver_container[ZONE_0][INST_0][MESH_0][TURB_SOL]->GetnVar();
-    su2double *U_Turb = new su2double[nVar_Turb];
-    su2double *Source_Turb = new su2double[nVar_Turb];
-
-    /*--- Loop over only the finest mesh level (turbulence is always solved
-     on the original grid only). ---*/
-    for (iPoint = 0; iPoint < geometry_container[ZONE_0][INST_0][MESH_0]->GetnPoint(); iPoint++) {
-      for (iVar = 0; iVar < nVar_Turb; iVar++) Source_Turb[iVar] = 0.0;
-      for (jInst = 0; jInst < nInstHB; jInst++) {
-
-        /*--- Retrieve solution at this node in current zone ---*/
-        for (iVar = 0; iVar < nVar_Turb; iVar++) {
-          U_Turb[iVar] = solver_container[ZONE_0][jInst][MESH_0][TURB_SOL]->GetNodes()->GetSolution(iPoint, iVar);
-          Source_Turb[iVar] += U_Turb[iVar]*D[iInst][jInst];
+    
+    /*--- Source term for a turbulence model ---*/
+    if (config_container[ZONE_0]->GetKind_Solver() == MAIN_SOLVER::RANS) {
+        
+        /*--- Extra variables needed if we have a turbulence model. ---*/
+        unsigned short nVar_Turb = solver_container[ZONE_0][INST_0][MESH_0][TURB_SOL]->GetnVar();
+        su2double *U_Turb = new su2double[nVar_Turb];
+        su2double *Source_Turb = new su2double[nVar_Turb];
+        
+        /*--- Loop over only the finest mesh level (turbulence is always solved
+         on the original grid only). ---*/
+        for (iPoint = 0; iPoint < geometry_container[ZONE_0][INST_0][MESH_0]->GetnPoint(); iPoint++) {
+            for (iVar = 0; iVar < nVar_Turb; iVar++) Source_Turb[iVar] = 0.0;
+            for (jInst = 0; jInst < nInstHB; jInst++) {
+                
+                /*--- Retrieve solution at this node in current zone ---*/
+                for (iVar = 0; iVar < nVar_Turb; iVar++) {
+                    U_Turb[iVar] = solver_container[ZONE_0][jInst][MESH_0][TURB_SOL]->GetNodes()->GetSolution(iPoint, iVar);
+                    Source_Turb[iVar] += U_Turb[iVar]*D[iInst][jInst];
+                }
+            }
+            
+            /*--- Store sources for current iZone ---*/
+            for (iVar = 0; iVar < nVar_Turb; iVar++)
+                solver_container[ZONE_0][iInst][MESH_0][TURB_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source_Turb[iVar]);
         }
-      }
-
-      /*--- Store sources for current iZone ---*/
-      for (iVar = 0; iVar < nVar_Turb; iVar++)
-        solver_container[ZONE_0][iInst][MESH_0][TURB_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source_Turb[iVar]);
-    }
-
-    delete [] U_Turb;
-    delete [] Source_Turb;
-  }
-
-  delete [] Source;
-  delete [] U;
-  delete [] U_old;
-  delete [] Psi;
-  delete [] Psi_old;
-
+        
+        delete [] U_Turb;
+        delete [] Source_Turb;
+    }
+    
+    delete [] Source;
+    delete [] U;
+    delete [] U_old;
+    delete [] Psi;
+    delete [] Psi_old;
+    
 }
 
 void CHBDriver::StabilizeHarmonicBalance() {
+    
+    unsigned short i, j, k, iVar, iInst, jInst, iMGlevel;
+    unsigned short nVar = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetnVar();
+    unsigned long iPoint;
+    bool adjoint = (config_container[ZONE_0]->GetContinuous_Adjoint());
+    
+    /*--- Retrieve values from the config file ---*/
+    su2double *Source     = new su2double[nInstHB];
+    su2double *Source_old = new su2double[nInstHB];
+    su2double Delta;
+    
+    su2double **Pinv     = new su2double*[nInstHB];
+    su2double **P        = new su2double*[nInstHB];
+    for (iInst = 0; iInst < nInstHB; iInst++) {
+        Pinv[iInst]       = new su2double[nInstHB];
+        P[iInst]          = new su2double[nInstHB];
+    }
+    
+    /*--- Loop over all grid levels ---*/
+    for (iMGlevel = 0; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++) {
+        
+        /*--- Loop over each node in the volume mesh ---*/
+        for (iPoint = 0; iPoint < geometry_container[ZONE_0][INST_0][iMGlevel]->GetnPoint(); iPoint++) {
+            
+            /*--- Get time step for current node ---*/
+            Delta = solver_container[ZONE_0][INST_0][iMGlevel][FLOW_SOL]->GetNodes()->GetDelta_Time(iPoint);
+            
+            /*--- Setup stabilization matrix for this node ---*/
+            for (iInst = 0; iInst < nInstHB; iInst++) {
+                for (jInst = 0; jInst < nInstHB; jInst++) {
+                    if (jInst == iInst ) {
+                        Pinv[iInst][jInst] = 1.0 + Delta*D[iInst][jInst];
+                    }
+                    else {
+                        Pinv[iInst][jInst] = Delta*D[iInst][jInst];
+                    }
+                }
+            }
+            
+            /*--- Invert stabilization matrix Pinv with Gauss elimination---*/
+            
+            /*--  A temporary matrix to hold the inverse, dynamically allocated ---*/
+            su2double **temp = new su2double*[nInstHB];
+            for (i = 0; i < nInstHB; i++) {
+                temp[i] = new su2double[2 * nInstHB];
+            }
+            
+            /*---  Copy the desired matrix into the temporary matrix ---*/
+            for (i = 0; i < nInstHB; i++) {
+                for (j = 0; j < nInstHB; j++) {
+                    temp[i][j] = Pinv[i][j];
+                    temp[i][nInstHB + j] = 0;
+                }
+                temp[i][nInstHB + i] = 1;
+            }
+            
+            su2double max_val;
+            unsigned short max_idx;
+            
+            /*---  Pivot each column such that the largest number possible divides the other rows  ---*/
+            for (k = 0; k < nInstHB - 1; k++) {
+                max_idx = k;
+                max_val = abs(temp[k][k]);
+                /*---  Find the largest value (pivot) in the column  ---*/
+                for (j = k; j < nInstHB; j++) {
+                    if (abs(temp[j][k]) > max_val) {
+                        max_idx = j;
+                        max_val = abs(temp[j][k]);
+                    }
+                }
+                
+                /*---  Move the row with the highest value up  ---*/
+                for (j = 0; j < (nInstHB * 2); j++) {
+                    su2double d = temp[k][j];
+                    temp[k][j] = temp[max_idx][j];
+                    temp[max_idx][j] = d;
+                }
+                /*---  Subtract the moved row from all other rows ---*/
+                for (i = k + 1; i < nInstHB; i++) {
+                    su2double c = temp[i][k] / temp[k][k];
+                    for (j = 0; j < (nInstHB * 2); j++) {
+                        temp[i][j] = temp[i][j] - temp[k][j] * c;
+                    }
+                }
+            }
+            
+            /*---  Back-substitution  ---*/
+            for (k = nInstHB - 1; k > 0; k--) {
+                if (temp[k][k] != su2double(0.0)) {
+                    for (int i = k - 1; i > -1; i--) {
+                        su2double c = temp[i][k] / temp[k][k];
+                        for (j = 0; j < (nInstHB * 2); j++) {
+                            temp[i][j] = temp[i][j] - temp[k][j] * c;
+                        }
+                    }
+                }
+            }
+            
+            /*---  Normalize the inverse  ---*/
+            for (i = 0; i < nInstHB; i++) {
+                su2double c = temp[i][i];
+                for (j = 0; j < nInstHB; j++) {
+                    temp[i][j + nInstHB] = temp[i][j + nInstHB] / c;
+                }
+            }
+            
+            /*---  Copy the inverse back to the main program flow ---*/
+            for (i = 0; i < nInstHB; i++) {
+                for (j = 0; j < nInstHB; j++) {
+                    P[i][j] = temp[i][j + nInstHB];
+                }
+            }
+            
+            /*---  Delete dynamic template  ---*/
+            for (iInst = 0; iInst < nInstHB; iInst++) {
+                delete[] temp[iInst];
+            }
+            delete[] temp;
+            
+            /*--- Loop through variables to precondition ---*/
+            for (iVar = 0; iVar < nVar; iVar++) {
+                
+                /*--- Get current source terms (not yet preconditioned) and zero source array to prepare preconditioning ---*/
+                for (iInst = 0; iInst < nInstHB; iInst++) {
+                    Source_old[iInst] = solver_container[ZONE_0][iInst][iMGlevel][FLOW_SOL]->GetNodes()->GetHarmonicBalance_Source(iPoint, iVar);
+                    Source[iInst] = 0;
+                }
+                
+                /*--- Step through columns ---*/
+                for (iInst = 0; iInst < nInstHB; iInst++) {
+                    for (jInst = 0; jInst < nInstHB; jInst++) {
+                        Source[iInst] += P[iInst][jInst]*Source_old[jInst];
+                    }
+                    
+                    /*--- Store updated source terms for current node ---*/
+                    if (!adjoint) {
+                        solver_container[ZONE_0][iInst][iMGlevel][FLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iInst]);
+                    }
+                    else {
+                        solver_container[ZONE_0][iInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iInst]);
+                    }
+                }
+                
+            }
+        }
+    }
+    
+    /*--- Deallocate dynamic memory ---*/
+    for (iInst = 0; iInst < nInstHB; iInst++){
+        delete [] P[iInst];
+        delete [] Pinv[iInst];
+    }
+    delete [] P;
+    delete [] Pinv;
+    delete [] Source;
+    delete [] Source_old;
+    
+}
 
-  unsigned short i, j, k, iVar, iInst, jInst, iMGlevel;
-  unsigned short nVar = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetnVar();
-  unsigned long iPoint;
-  bool adjoint = (config_container[ZONE_0]->GetContinuous_Adjoint());
-
-  /*--- Retrieve values from the config file ---*/
-  su2double *Source     = new su2double[nInstHB];
-  su2double *Source_old = new su2double[nInstHB];
-  su2double Delta;
-
-  su2double **Pinv     = new su2double*[nInstHB];
-  su2double **P        = new su2double*[nInstHB];
-  for (iInst = 0; iInst < nInstHB; iInst++) {
-    Pinv[iInst]       = new su2double[nInstHB];
-    P[iInst]          = new su2double[nInstHB];
-  }
-
-  /*--- Loop over all grid levels ---*/
-  for (iMGlevel = 0; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++) {
-
-    /*--- Loop over each node in the volume mesh ---*/
-    for (iPoint = 0; iPoint < geometry_container[ZONE_0][INST_0][iMGlevel]->GetnPoint(); iPoint++) {
-
-      /*--- Get time step for current node ---*/
-      Delta = solver_container[ZONE_0][INST_0][iMGlevel][FLOW_SOL]->GetNodes()->GetDelta_Time(iPoint);
-
-      /*--- Setup stabilization matrix for this node ---*/
-      for (iInst = 0; iInst < nInstHB; iInst++) {
-        for (jInst = 0; jInst < nInstHB; jInst++) {
-          if (jInst == iInst ) {
-            Pinv[iInst][jInst] = 1.0 + Delta*D[iInst][jInst];
-          }
-          else {
-            Pinv[iInst][jInst] = Delta*D[iInst][jInst];
-          }
-        }
-      }
-
-      /*--- Invert stabilization matrix Pinv with Gauss elimination---*/
-
-      /*--  A temporary matrix to hold the inverse, dynamically allocated ---*/
-      su2double **temp = new su2double*[nInstHB];
-      for (i = 0; i < nInstHB; i++) {
-        temp[i] = new su2double[2 * nInstHB];
-      }
-
-      /*---  Copy the desired matrix into the temporary matrix ---*/
-      for (i = 0; i < nInstHB; i++) {
+void CHBDriver::ComputeHB_Operator() {
+    
+    const   complex<su2double> J(0.0,1.0);
+    unsigned short i, j, k, iInst;
+    
+    su2double *Omega_HB       = new su2double[nInstHB];
+    complex<su2double> **E    = new complex<su2double>*[nInstHB];
+    complex<su2double> **Einv = new complex<su2double>*[nInstHB];
+    complex<su2double> **DD   = new complex<su2double>*[nInstHB];
+    for (iInst = 0; iInst < nInstHB; iInst++) {
+        E[iInst]    = new complex<su2double>[nInstHB];
+        Einv[iInst] = new complex<su2double>[nInstHB];
+        DD[iInst]   = new complex<su2double>[nInstHB];
+    }
+    
+    /*--- Get simualation period from config file ---*/
+    su2double Period = config_container[ZONE_0]->GetHarmonicBalance_Period();
+    
+    /*--- Non-dimensionalize the input period, if necessary.      */
+    Period /= config_container[ZONE_0]->GetTime_Ref();
+    
+    /*--- Build the array containing the selected frequencies to solve ---*/
+    for (iInst = 0; iInst < nInstHB; iInst++) {
+        Omega_HB[iInst]  = config_container[ZONE_0]->GetOmega_HB()[iInst];
+        Omega_HB[iInst] /= config_container[ZONE_0]->GetOmega_Ref(); //TODO: check
+    }
+    
+    /*--- Build the diagonal matrix of the frequencies DD ---*/
+    for (i = 0; i < nInstHB; i++) {
+        for (k = 0; k < nInstHB; k++) {
+            if (k == i ) {
+                DD[i][k] = J*Omega_HB[k];
+            }
+        }
+    }
+    
+    
+    /*--- Build the harmonic balance inverse matrix ---*/
+    for (i = 0; i < nInstHB; i++) {
+        for (k = 0; k < nInstHB; k++) {
+            Einv[i][k] = complex<su2double>(cos(Omega_HB[k]*(i*Period/nInstHB))) + J*complex<su2double>(sin(Omega_HB[k]*(i*Period/nInstHB)));
+        }
+    }
+    
+    /*---  Invert inverse harmonic balance Einv with Gauss elimination ---*/
+    
+    /*--  A temporary matrix to hold the inverse, dynamically allocated ---*/
+    complex<su2double> **temp = new complex<su2double>*[nInstHB];
+    for (i = 0; i < nInstHB; i++) {
+        temp[i] = new complex<su2double>[2 * nInstHB];
+    }
+    
+    /*---  Copy the desired matrix into the temporary matrix ---*/
+    for (i = 0; i < nInstHB; i++) {
         for (j = 0; j < nInstHB; j++) {
-          temp[i][j] = Pinv[i][j];
-          temp[i][nInstHB + j] = 0;
+            temp[i][j] = Einv[i][j];
+            temp[i][nInstHB + j] = 0;
         }
         temp[i][nInstHB + i] = 1;
-      }
-
-      su2double max_val;
-      unsigned short max_idx;
-
-      /*---  Pivot each column such that the largest number possible divides the other rows  ---*/
-      for (k = 0; k < nInstHB - 1; k++) {
+    }
+    
+    su2double max_val;
+    unsigned short max_idx;
+    
+    /*---  Pivot each column such that the largest number possible divides the other rows  ---*/
+    for (k = 0; k < nInstHB - 1; k++) {
         max_idx = k;
         max_val = abs(temp[k][k]);
         /*---  Find the largest value (pivot) in the column  ---*/
         for (j = k; j < nInstHB; j++) {
-          if (abs(temp[j][k]) > max_val) {
-            max_idx = j;
-            max_val = abs(temp[j][k]);
-          }
+            if (abs(temp[j][k]) > max_val) {
+                max_idx = j;
+                max_val = abs(temp[j][k]);
+            }
         }
-
         /*---  Move the row with the highest value up  ---*/
         for (j = 0; j < (nInstHB * 2); j++) {
-          su2double d = temp[k][j];
-          temp[k][j] = temp[max_idx][j];
-          temp[max_idx][j] = d;
+            complex<su2double> d = temp[k][j];
+            temp[k][j] = temp[max_idx][j];
+            temp[max_idx][j] = d;
         }
         /*---  Subtract the moved row from all other rows ---*/
         for (i = k + 1; i < nInstHB; i++) {
-          su2double c = temp[i][k] / temp[k][k];
-          for (j = 0; j < (nInstHB * 2); j++) {
-            temp[i][j] = temp[i][j] - temp[k][j] * c;
-          }
-        }
-      }
-
-      /*---  Back-substitution  ---*/
-      for (k = nInstHB - 1; k > 0; k--) {
-        if (temp[k][k] != su2double(0.0)) {
-          for (int i = k - 1; i > -1; i--) {
-            su2double c = temp[i][k] / temp[k][k];
+            complex<su2double> c = temp[i][k] / temp[k][k];
             for (j = 0; j < (nInstHB * 2); j++) {
-              temp[i][j] = temp[i][j] - temp[k][j] * c;
+                temp[i][j] = temp[i][j] - temp[k][j] * c;
             }
-          }
         }
-      }
-
-      /*---  Normalize the inverse  ---*/
-      for (i = 0; i < nInstHB; i++) {
-        su2double c = temp[i][i];
+    }
+    /*---  Back-substitution  ---*/
+    for (k = nInstHB - 1; k > 0; k--) {
+        if (temp[k][k] != complex<su2double>(0.0)) {
+            for (int i = k - 1; i > -1; i--) {
+                complex<su2double> c = temp[i][k] / temp[k][k];
+                for (j = 0; j < (nInstHB * 2); j++) {
+                    temp[i][j] = temp[i][j] - temp[k][j] * c;
+                }
+            }
+        }
+    }
+    /*---  Normalize the inverse  ---*/
+    for (i = 0; i < nInstHB; i++) {
+        complex<su2double> c = temp[i][i];
         for (j = 0; j < nInstHB; j++) {
-          temp[i][j + nInstHB] = temp[i][j + nInstHB] / c;
+            temp[i][j + nInstHB] = temp[i][j + nInstHB] / c;
         }
-      }
-
-      /*---  Copy the inverse back to the main program flow ---*/
-      for (i = 0; i < nInstHB; i++) {
+    }
+    /*---  Copy the inverse back to the main program flow ---*/
+    for (i = 0; i < nInstHB; i++) {
         for (j = 0; j < nInstHB; j++) {
-          P[i][j] = temp[i][j + nInstHB];
+            E[i][j] = temp[i][j + nInstHB];
         }
-      }
-
-      /*---  Delete dynamic template  ---*/
-      for (iInst = 0; iInst < nInstHB; iInst++) {
-        delete[] temp[iInst];
-      }
-      delete[] temp;
-
-      /*--- Loop through variables to precondition ---*/
-      for (iVar = 0; iVar < nVar; iVar++) {
-
-        /*--- Get current source terms (not yet preconditioned) and zero source array to prepare preconditioning ---*/
-        for (iInst = 0; iInst < nInstHB; iInst++) {
-          Source_old[iInst] = solver_container[ZONE_0][iInst][iMGlevel][FLOW_SOL]->GetNodes()->GetHarmonicBalance_Source(iPoint, iVar);
-          Source[iInst] = 0;
+    }
+    /*---  Delete dynamic template  ---*/
+    for (i = 0; i < nInstHB; i++) {
+        delete[] temp[i];
+    }
+    delete[] temp;
+    
+    
+    /*---  Temporary matrix for performing product  ---*/
+    complex<su2double> **Temp    = new complex<su2double>*[nInstHB];
+    
+    /*---  Temporary complex HB operator  ---*/
+    complex<su2double> **Dcpx    = new complex<su2double>*[nInstHB];
+    
+    for (iInst = 0; iInst < nInstHB; iInst++){
+        Temp[iInst]    = new complex<su2double>[nInstHB];
+        Dcpx[iInst]   = new complex<su2double>[nInstHB];
+    }
+    
+    
+    /*---  Calculation of the HB operator matrix ---*/
+    for (int row = 0; row < nInstHB; row++) {
+        for (int col = 0; col < nInstHB; col++) {
+            for (int inner = 0; inner < nInstHB; inner++) {
+                Temp[row][col] += Einv[row][inner] * DD[inner][col];
+            }
         }
-
-        /*--- Step through columns ---*/
-        for (iInst = 0; iInst < nInstHB; iInst++) {
-          for (jInst = 0; jInst < nInstHB; jInst++) {
-            Source[iInst] += P[iInst][jInst]*Source_old[jInst];
-          }
-
-          /*--- Store updated source terms for current node ---*/
-          if (!adjoint) {
-            solver_container[ZONE_0][iInst][iMGlevel][FLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iInst]);
-          }
-          else {
-            solver_container[ZONE_0][iInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iInst]);
-          }
+    }
+    
+    unsigned short row, col, inner;
+    
+    for (row = 0; row < nInstHB; row++) {
+        for (col = 0; col < nInstHB; col++) {
+            for (inner = 0; inner < nInstHB; inner++) {
+                Dcpx[row][col] += Temp[row][inner] * E[inner][col];
+            }
         }
-
-      }
     }
-  }
-
-  /*--- Deallocate dynamic memory ---*/
-  for (iInst = 0; iInst < nInstHB; iInst++){
-    delete [] P[iInst];
-    delete [] Pinv[iInst];
-  }
-  delete [] P;
-  delete [] Pinv;
-  delete [] Source;
-  delete [] Source_old;
-
-}
-
-void CHBDriver::ComputeHB_Operator() {
-
-  const   complex<su2double> J(0.0,1.0);
-  unsigned short i, j, k, iInst;
-
-  su2double *Omega_HB       = new su2double[nInstHB];
-  complex<su2double> **E    = new complex<su2double>*[nInstHB];
-  complex<su2double> **Einv = new complex<su2double>*[nInstHB];
-  complex<su2double> **DD   = new complex<su2double>*[nInstHB];
-  for (iInst = 0; iInst < nInstHB; iInst++) {
-    E[iInst]    = new complex<su2double>[nInstHB];
-    Einv[iInst] = new complex<su2double>[nInstHB];
-    DD[iInst]   = new complex<su2double>[nInstHB];
-  }
-
-  /*--- Get simualation period from config file ---*/
-  su2double Period = config_container[ZONE_0]->GetHarmonicBalance_Period();
-
-  /*--- Non-dimensionalize the input period, if necessary.      */
-  Period /= config_container[ZONE_0]->GetTime_Ref();
-
-  /*--- Build the array containing the selected frequencies to solve ---*/
-  for (iInst = 0; iInst < nInstHB; iInst++) {
-    Omega_HB[iInst]  = config_container[ZONE_0]->GetOmega_HB()[iInst];
-    Omega_HB[iInst] /= config_container[ZONE_0]->GetOmega_Ref(); //TODO: check
-  }
-
-  /*--- Build the diagonal matrix of the frequencies DD ---*/
-  for (i = 0; i < nInstHB; i++) {
-    for (k = 0; k < nInstHB; k++) {
-      if (k == i ) {
-        DD[i][k] = J*Omega_HB[k];
-      }
-    }
-  }
-
-
-  /*--- Build the harmonic balance inverse matrix ---*/
-  for (i = 0; i < nInstHB; i++) {
-    for (k = 0; k < nInstHB; k++) {
-      Einv[i][k] = complex<su2double>(cos(Omega_HB[k]*(i*Period/nInstHB))) + J*complex<su2double>(sin(Omega_HB[k]*(i*Period/nInstHB)));
-    }
-  }
-
-  /*---  Invert inverse harmonic balance Einv with Gauss elimination ---*/
-
-  /*--  A temporary matrix to hold the inverse, dynamically allocated ---*/
-  complex<su2double> **temp = new complex<su2double>*[nInstHB];
-  for (i = 0; i < nInstHB; i++) {
-    temp[i] = new complex<su2double>[2 * nInstHB];
-  }
-
-  /*---  Copy the desired matrix into the temporary matrix ---*/
-  for (i = 0; i < nInstHB; i++) {
-    for (j = 0; j < nInstHB; j++) {
-      temp[i][j] = Einv[i][j];
-      temp[i][nInstHB + j] = 0;
-    }
-    temp[i][nInstHB + i] = 1;
-  }
-
-  su2double max_val;
-  unsigned short max_idx;
-
-  /*---  Pivot each column such that the largest number possible divides the other rows  ---*/
-  for (k = 0; k < nInstHB - 1; k++) {
-    max_idx = k;
-    max_val = abs(temp[k][k]);
-    /*---  Find the largest value (pivot) in the column  ---*/
-    for (j = k; j < nInstHB; j++) {
-      if (abs(temp[j][k]) > max_val) {
-        max_idx = j;
-        max_val = abs(temp[j][k]);
-      }
-    }
-    /*---  Move the row with the highest value up  ---*/
-    for (j = 0; j < (nInstHB * 2); j++) {
-      complex<su2double> d = temp[k][j];
-      temp[k][j] = temp[max_idx][j];
-      temp[max_idx][j] = d;
-    }
-    /*---  Subtract the moved row from all other rows ---*/
-    for (i = k + 1; i < nInstHB; i++) {
-      complex<su2double> c = temp[i][k] / temp[k][k];
-      for (j = 0; j < (nInstHB * 2); j++) {
-        temp[i][j] = temp[i][j] - temp[k][j] * c;
-      }
-    }
-  }
-  /*---  Back-substitution  ---*/
-  for (k = nInstHB - 1; k > 0; k--) {
-    if (temp[k][k] != complex<su2double>(0.0)) {
-      for (int i = k - 1; i > -1; i--) {
-        complex<su2double> c = temp[i][k] / temp[k][k];
-        for (j = 0; j < (nInstHB * 2); j++) {
-          temp[i][j] = temp[i][j] - temp[k][j] * c;
-        }
-      }
-    }
-  }
-  /*---  Normalize the inverse  ---*/
-  for (i = 0; i < nInstHB; i++) {
-    complex<su2double> c = temp[i][i];
-    for (j = 0; j < nInstHB; j++) {
-      temp[i][j + nInstHB] = temp[i][j + nInstHB] / c;
-    }
-  }
-  /*---  Copy the inverse back to the main program flow ---*/
-  for (i = 0; i < nInstHB; i++) {
-    for (j = 0; j < nInstHB; j++) {
-      E[i][j] = temp[i][j + nInstHB];
-    }
-  }
-  /*---  Delete dynamic template  ---*/
-  for (i = 0; i < nInstHB; i++) {
-    delete[] temp[i];
-  }
-  delete[] temp;
-
-
-  /*---  Temporary matrix for performing product  ---*/
-  complex<su2double> **Temp    = new complex<su2double>*[nInstHB];
-
-  /*---  Temporary complex HB operator  ---*/
-  complex<su2double> **Dcpx    = new complex<su2double>*[nInstHB];
-
-  for (iInst = 0; iInst < nInstHB; iInst++){
-    Temp[iInst]    = new complex<su2double>[nInstHB];
-    Dcpx[iInst]   = new complex<su2double>[nInstHB];
-  }
-
-
-  /*---  Calculation of the HB operator matrix ---*/
-  for (int row = 0; row < nInstHB; row++) {
-    for (int col = 0; col < nInstHB; col++) {
-      for (int inner = 0; inner < nInstHB; inner++) {
-        Temp[row][col] += Einv[row][inner] * DD[inner][col];
-      }
-    }
-  }
-
-  unsigned short row, col, inner;
-
-  for (row = 0; row < nInstHB; row++) {
-    for (col = 0; col < nInstHB; col++) {
-      for (inner = 0; inner < nInstHB; inner++) {
-        Dcpx[row][col] += Temp[row][inner] * E[inner][col];
-      }
-    }
-  }
-
-  /*---  Take just the real part of the HB operator matrix ---*/
-  for (i = 0; i < nInstHB; i++) {
-    for (k = 0; k < nInstHB; k++) {
-      D[i][k] = real(Dcpx[i][k]);
-    }
-  }
-
-  /*--- Deallocate dynamic memory ---*/
-  for (iInst = 0; iInst < nInstHB; iInst++){
-    delete [] E[iInst];
-    delete [] Einv[iInst];
-    delete [] DD[iInst];
-    delete [] Temp[iInst];
-    delete [] Dcpx[iInst];
-  }
-  delete [] E;
-  delete [] Einv;
-  delete [] DD;
-  delete [] Temp;
-  delete [] Dcpx;
-  delete [] Omega_HB;
-
+    
+    /*---  Take just the real part of the HB operator matrix ---*/
+    for (i = 0; i < nInstHB; i++) {
+        for (k = 0; k < nInstHB; k++) {
+            D[i][k] = real(Dcpx[i][k]);
+        }
+    }
+    
+    /*--- Deallocate dynamic memory ---*/
+    for (iInst = 0; iInst < nInstHB; iInst++){
+        delete [] E[iInst];
+        delete [] Einv[iInst];
+        delete [] DD[iInst];
+        delete [] Temp[iInst];
+        delete [] Dcpx[iInst];
+    }
+    delete [] E;
+    delete [] Einv;
+    delete [] DD;
+    delete [] Temp;
+    delete [] Dcpx;
+    delete [] Omega_HB;
+    
 }
diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index 2f85546f4d3..ba6a563c5b0 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -31,32 +31,32 @@
 #include "../../Common/include/toolboxes/geometry_toolbox.hpp"
 
 void CDriver::PythonInterface_Preprocessing(CConfig **config, CGeometry ****geometry, CSolver *****solver){
-
-  int rank = MASTER_NODE;
-  SU2_MPI::Comm_rank(SU2_MPI::GetComm(), &rank);
-
-  /* --- Initialize boundary conditions customization, this is achieve through the Python wrapper --- */
-  for(iZone=0; iZone < nZone; iZone++){
-
-    if (config[iZone]->GetnMarker_PyCustom() > 0){
-
-      if (rank == MASTER_NODE) cout << endl << "----------------- Python Interface Preprocessing ( Zone "<< iZone <<" ) -----------------" << endl;
-
-      if (rank == MASTER_NODE) cout << "Setting customized boundary conditions for zone " << iZone << endl;
-      for (iMesh = 0; iMesh <= config[iZone]->GetnMGLevels(); iMesh++) {
-        geometry[iZone][INST_0][iMesh]->SetCustomBoundary(config[iZone]);
-      }
-      geometry[iZone][INST_0][MESH_0]->UpdateCustomBoundaryConditions(geometry[iZone][INST_0], config[iZone]);
-
-      if ((config[iZone]->GetKind_Solver() == MAIN_SOLVER::EULER) ||
-          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::NAVIER_STOKES) ||
-          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::RANS)) {
-
-        solver[iZone][INST_0][MESH_0][FLOW_SOL]->UpdateCustomBoundaryConditions(geometry[iZone][INST_0], config[iZone]);
-      }
+    
+    int rank = MASTER_NODE;
+    SU2_MPI::Comm_rank(SU2_MPI::GetComm(), &rank);
+    
+    /* --- Initialize boundary conditions customization, this is achieve through the Python wrapper --- */
+    for(iZone=0; iZone < nZone; iZone++){
+        
+        if (config[iZone]->GetnMarker_PyCustom() > 0){
+            
+            if (rank == MASTER_NODE) cout << endl << "----------------- Python Interface Preprocessing ( Zone "<< iZone <<" ) -----------------" << endl;
+            
+            if (rank == MASTER_NODE) cout << "Setting customized boundary conditions for zone " << iZone << endl;
+            for (iMesh = 0; iMesh <= config[iZone]->GetnMGLevels(); iMesh++) {
+                geometry[iZone][INST_0][iMesh]->SetCustomBoundary(config[iZone]);
+            }
+            geometry[iZone][INST_0][MESH_0]->UpdateCustomBoundaryConditions(geometry[iZone][INST_0], config[iZone]);
+            
+            if ((config[iZone]->GetKind_Solver() == MAIN_SOLVER::EULER) ||
+                (config[iZone]->GetKind_Solver() == MAIN_SOLVER::NAVIER_STOKES) ||
+                (config[iZone]->GetKind_Solver() == MAIN_SOLVER::RANS)) {
+                
+                solver[iZone][INST_0][MESH_0][FLOW_SOL]->UpdateCustomBoundaryConditions(geometry[iZone][INST_0], config[iZone]);
+            }
+        }
     }
-  }
-
+    
 }
 
 /////////////////////////////////////////////////////////////////////////////
@@ -64,106 +64,106 @@ void CDriver::PythonInterface_Preprocessing(CConfig **config, CGeometry ****geom
 /////////////////////////////////////////////////////////////////////////////
 
 passivedouble CDriver::Get_Drag() const {
-
-  unsigned short val_iZone = ZONE_0;
-  unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
-  su2double CDrag, factor, val_Drag;
-
-  /*--- Calculate drag force based on drag coefficient ---*/
-  factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
-  CDrag = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CD();
-
-  val_Drag = CDrag*factor;
-
-  return SU2_TYPE::GetValue(val_Drag);
+    
+    unsigned short val_iZone = ZONE_0;
+    unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
+    su2double CDrag, factor, val_Drag;
+    
+    /*--- Calculate drag force based on drag coefficient ---*/
+    factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
+    CDrag = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CD();
+    
+    val_Drag = CDrag*factor;
+    
+    return SU2_TYPE::GetValue(val_Drag);
 }
 
 passivedouble CDriver::Get_Lift() const {
-
-  unsigned short val_iZone = ZONE_0;
-  unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
-  su2double CLift, factor, val_Lift;
-
-  /*--- Calculate drag force based on drag coefficient ---*/
-  factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
-  CLift = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CL();
-
-  val_Lift = CLift*factor;
-
-  return SU2_TYPE::GetValue(val_Lift);
+    
+    unsigned short val_iZone = ZONE_0;
+    unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
+    su2double CLift, factor, val_Lift;
+    
+    /*--- Calculate drag force based on drag coefficient ---*/
+    factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
+    CLift = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CL();
+    
+    val_Lift = CLift*factor;
+    
+    return SU2_TYPE::GetValue(val_Lift);
 }
 
 passivedouble CDriver::Get_Mx() const {
-
-  unsigned short val_iZone = ZONE_0;
-  unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
-  su2double CMx, RefLengthCoeff, factor, val_Mx;
-
-  RefLengthCoeff = config_container[val_iZone]->GetRefLength();
-
-  /*--- Calculate moment around x-axis based on coefficients ---*/
-  factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
-  CMx = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMx();
-
-  val_Mx = CMx*factor*RefLengthCoeff;
-
-  return SU2_TYPE::GetValue(val_Mx);
+    
+    unsigned short val_iZone = ZONE_0;
+    unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
+    su2double CMx, RefLengthCoeff, factor, val_Mx;
+    
+    RefLengthCoeff = config_container[val_iZone]->GetRefLength();
+    
+    /*--- Calculate moment around x-axis based on coefficients ---*/
+    factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
+    CMx = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMx();
+    
+    val_Mx = CMx*factor*RefLengthCoeff;
+    
+    return SU2_TYPE::GetValue(val_Mx);
 }
 
 passivedouble CDriver::Get_My() const {
-
-  unsigned short val_iZone = ZONE_0;
-  unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
-  su2double CMy, RefLengthCoeff, factor, val_My;
-
-  RefLengthCoeff = config_container[val_iZone]->GetRefLength();
-
-  /*--- Calculate moment around x-axis based on coefficients ---*/
-  factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
-  CMy = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMy();
-
-  val_My = CMy*factor*RefLengthCoeff;
-
-  return SU2_TYPE::GetValue(val_My);
+    
+    unsigned short val_iZone = ZONE_0;
+    unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
+    su2double CMy, RefLengthCoeff, factor, val_My;
+    
+    RefLengthCoeff = config_container[val_iZone]->GetRefLength();
+    
+    /*--- Calculate moment around x-axis based on coefficients ---*/
+    factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
+    CMy = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMy();
+    
+    val_My = CMy*factor*RefLengthCoeff;
+    
+    return SU2_TYPE::GetValue(val_My);
 }
 
 passivedouble CDriver::Get_Mz() const {
-
-  unsigned short val_iZone = ZONE_0;
-  unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
-  su2double CMz, RefLengthCoeff, factor, val_Mz;
-
-  RefLengthCoeff = config_container[val_iZone]->GetRefLength();
-
-  /*--- Calculate moment around z-axis based on coefficients ---*/
-  factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
-  CMz = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMz();
-
-  val_Mz = CMz*factor*RefLengthCoeff;
-
-  return SU2_TYPE::GetValue(val_Mz);
+    
+    unsigned short val_iZone = ZONE_0;
+    unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
+    su2double CMz, RefLengthCoeff, factor, val_Mz;
+    
+    RefLengthCoeff = config_container[val_iZone]->GetRefLength();
+    
+    /*--- Calculate moment around z-axis based on coefficients ---*/
+    factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
+    CMz = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMz();
+    
+    val_Mz = CMz*factor*RefLengthCoeff;
+    
+    return SU2_TYPE::GetValue(val_Mz);
 }
 
 passivedouble CDriver::Get_DragCoeff() const {
-
-  unsigned short val_iZone = ZONE_0;
-  unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
-  su2double CDrag;
-
-  CDrag = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CD();
-
-  return SU2_TYPE::GetValue(CDrag);
+    
+    unsigned short val_iZone = ZONE_0;
+    unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
+    su2double CDrag;
+    
+    CDrag = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CD();
+    
+    return SU2_TYPE::GetValue(CDrag);
 }
 
 passivedouble CDriver::Get_LiftCoeff() const {
-
-  unsigned short val_iZone = ZONE_0;
-  unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
-  su2double CLift;
-
-  CLift = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CL();
-
-  return SU2_TYPE::GetValue(CLift);
+    
+    unsigned short val_iZone = ZONE_0;
+    unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
+    su2double CLift;
+    
+    CLift = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CL();
+    
+    return SU2_TYPE::GetValue(CLift);
 }
 
 //////////////////////////////////////////////////////////////////////////////////
@@ -171,23 +171,23 @@ passivedouble CDriver::Get_LiftCoeff() const {
 //////////////////////////////////////////////////////////////////////////////////
 
 unsigned long CDriver::GetnTimeIter() const {
-
-  return config_container[ZONE_0]->GetnTime_Iter();
+    
+    return config_container[ZONE_0]->GetnTime_Iter();
 }
 
 unsigned long CDriver::GetTime_Iter() const{
-
-  return TimeIter;
+    
+    return TimeIter;
 }
 
 passivedouble CDriver::GetUnsteady_TimeStep() const {
-
-  return SU2_TYPE::GetValue(config_container[ZONE_0]->GetTime_Step());
+    
+    return SU2_TYPE::GetValue(config_container[ZONE_0]->GetTime_Step());
 }
 
 string CDriver::GetSurfaceFileName() const {
-
-  return config_container[ZONE_0]->GetSurfCoeff_FileName();
+    
+    return config_container[ZONE_0]->GetSurfCoeff_FileName();
 }
 
 ///////////////////////////////////////////////////////////////////////////////
@@ -195,125 +195,125 @@ string CDriver::GetSurfaceFileName() const {
 ///////////////////////////////////////////////////////////////////////////////
 
 passivedouble CDriver::GetVertexTemperature(unsigned short iMarker, unsigned long iVertex) const {
-
-  unsigned long iPoint;
-  su2double vertexWallTemp(0.0);
-
-  bool compressible = (config_container[ZONE_0]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-
-  if(geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint) && compressible){
-    vertexWallTemp = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetTemperature(iPoint);
-  }
-
-  return SU2_TYPE::GetValue(vertexWallTemp);
-
+    
+    unsigned long iPoint;
+    su2double vertexWallTemp(0.0);
+    
+    bool compressible = (config_container[ZONE_0]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
+    
+    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+    
+    if(geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint) && compressible){
+        vertexWallTemp = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetTemperature(iPoint);
+    }
+    
+    return SU2_TYPE::GetValue(vertexWallTemp);
+    
 }
 
 void CDriver::SetVertexTemperature(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallTemp){
-
-  geometry_container[ZONE_0][INST_0][MESH_0]->SetCustomBoundaryTemperature(iMarker, iVertex, val_WallTemp);
+    
+    geometry_container[ZONE_0][INST_0][MESH_0]->SetCustomBoundaryTemperature(iMarker, iVertex, val_WallTemp);
 }
 
 vector<passivedouble> CDriver::GetVertexHeatFluxes(unsigned short iMarker, unsigned long iVertex) const {
-
-  unsigned long iPoint;
-  unsigned short iDim;
-  su2double Prandtl_Lam  = config_container[ZONE_0]->GetPrandtl_Lam();
-  su2double Gas_Constant = config_container[ZONE_0]->GetGas_ConstantND();
-  su2double Gamma = config_container[ZONE_0]->GetGamma();
-  su2double Gamma_Minus_One = Gamma - 1.0;
-  su2double Cp = (Gamma / Gamma_Minus_One) * Gas_Constant;
-  su2double laminar_viscosity, thermal_conductivity;
-  vector<su2double> GradT (3,0.0);
-  vector<su2double> HeatFlux (3,0.0);
-  vector<passivedouble> HeatFluxPassive (3,0.0);
-
-  bool compressible = (config_container[ZONE_0]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-
-  if(compressible){
-    laminar_viscosity    = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
-    thermal_conductivity = Cp * (laminar_viscosity/Prandtl_Lam);
-    for(iDim=0; iDim < nDim; iDim++){
-      GradT[iDim] = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetGradient_Primitive(iPoint, 0, iDim);
-      HeatFlux[iDim] = -thermal_conductivity*GradT[iDim];
+    
+    unsigned long iPoint;
+    unsigned short iDim;
+    su2double Prandtl_Lam  = config_container[ZONE_0]->GetPrandtl_Lam();
+    su2double Gas_Constant = config_container[ZONE_0]->GetGas_ConstantND();
+    su2double Gamma = config_container[ZONE_0]->GetGamma();
+    su2double Gamma_Minus_One = Gamma - 1.0;
+    su2double Cp = (Gamma / Gamma_Minus_One) * Gas_Constant;
+    su2double laminar_viscosity, thermal_conductivity;
+    vector<su2double> GradT (3,0.0);
+    vector<su2double> HeatFlux (3,0.0);
+    vector<passivedouble> HeatFluxPassive (3,0.0);
+    
+    bool compressible = (config_container[ZONE_0]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
+    
+    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+    
+    if(compressible){
+        laminar_viscosity    = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
+        thermal_conductivity = Cp * (laminar_viscosity/Prandtl_Lam);
+        for(iDim=0; iDim < nDim; iDim++){
+            GradT[iDim] = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetGradient_Primitive(iPoint, 0, iDim);
+            HeatFlux[iDim] = -thermal_conductivity*GradT[iDim];
+        }
     }
-  }
-
-  HeatFluxPassive[0] = SU2_TYPE::GetValue(HeatFlux[0]);
-  HeatFluxPassive[1] = SU2_TYPE::GetValue(HeatFlux[1]);
-  HeatFluxPassive[2] = SU2_TYPE::GetValue(HeatFlux[2]);
-
-  return HeatFluxPassive;
+    
+    HeatFluxPassive[0] = SU2_TYPE::GetValue(HeatFlux[0]);
+    HeatFluxPassive[1] = SU2_TYPE::GetValue(HeatFlux[1]);
+    HeatFluxPassive[2] = SU2_TYPE::GetValue(HeatFlux[2]);
+    
+    return HeatFluxPassive;
 }
 
 passivedouble CDriver::GetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex) const{
-
-  unsigned long iPoint;
-  unsigned short iDim;
-  su2double vertexWallHeatFlux;
-  su2double Prandtl_Lam  = config_container[ZONE_0]->GetPrandtl_Lam();
-  su2double Gas_Constant = config_container[ZONE_0]->GetGas_ConstantND();
-  su2double Gamma = config_container[ZONE_0]->GetGamma();
-  su2double Gamma_Minus_One = Gamma - 1.0;
-  su2double Cp = (Gamma / Gamma_Minus_One) * Gas_Constant;
-  su2double Area;
-  su2double laminar_viscosity, thermal_conductivity, dTdn;
-  su2double *Normal, GradT[3] = {0.0,0.0,0.0}, UnitNormal[3] = {0.0,0.0,0.0};
-
-  bool compressible = (config_container[ZONE_0]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
-
-  vertexWallHeatFlux = 0.0;
-  dTdn = 0.0;
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-
-  if(geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint) && compressible){
-    Normal = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNormal();
-
-    Area = GeometryToolbox::Norm(nDim, Normal);
-
-    for (iDim = 0; iDim < nDim; iDim++)
-      UnitNormal[iDim] = Normal[iDim]/Area;
-
-    laminar_viscosity    = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
-    thermal_conductivity = Cp * (laminar_viscosity/Prandtl_Lam);
-    /*Compute wall heat flux (normal to the wall) based on computed temperature gradient*/
-    for(iDim=0; iDim < nDim; iDim++){
-      GradT[iDim] = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetGradient_Primitive(iPoint, 0, iDim);
-      dTdn += GradT[iDim]*UnitNormal[iDim];
+    
+    unsigned long iPoint;
+    unsigned short iDim;
+    su2double vertexWallHeatFlux;
+    su2double Prandtl_Lam  = config_container[ZONE_0]->GetPrandtl_Lam();
+    su2double Gas_Constant = config_container[ZONE_0]->GetGas_ConstantND();
+    su2double Gamma = config_container[ZONE_0]->GetGamma();
+    su2double Gamma_Minus_One = Gamma - 1.0;
+    su2double Cp = (Gamma / Gamma_Minus_One) * Gas_Constant;
+    su2double Area;
+    su2double laminar_viscosity, thermal_conductivity, dTdn;
+    su2double *Normal, GradT[3] = {0.0,0.0,0.0}, UnitNormal[3] = {0.0,0.0,0.0};
+    
+    bool compressible = (config_container[ZONE_0]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
+    
+    vertexWallHeatFlux = 0.0;
+    dTdn = 0.0;
+    
+    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+    
+    if(geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint) && compressible){
+        Normal = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNormal();
+        
+        Area = GeometryToolbox::Norm(nDim, Normal);
+        
+        for (iDim = 0; iDim < nDim; iDim++)
+            UnitNormal[iDim] = Normal[iDim]/Area;
+        
+        laminar_viscosity    = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
+        thermal_conductivity = Cp * (laminar_viscosity/Prandtl_Lam);
+        /*Compute wall heat flux (normal to the wall) based on computed temperature gradient*/
+        for(iDim=0; iDim < nDim; iDim++){
+            GradT[iDim] = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetGradient_Primitive(iPoint, 0, iDim);
+            dTdn += GradT[iDim]*UnitNormal[iDim];
+        }
+        
+        vertexWallHeatFlux = -thermal_conductivity*dTdn;
     }
-
-    vertexWallHeatFlux = -thermal_conductivity*dTdn;
-  }
-
-  return SU2_TYPE::GetValue(vertexWallHeatFlux);
+    
+    return SU2_TYPE::GetValue(vertexWallHeatFlux);
 }
 
 void CDriver::SetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallHeatFlux){
-
-  geometry_container[ZONE_0][INST_0][MESH_0]->SetCustomBoundaryHeatFlux(iMarker, iVertex, val_WallHeatFlux);
+    
+    geometry_container[ZONE_0][INST_0][MESH_0]->SetCustomBoundaryHeatFlux(iMarker, iVertex, val_WallHeatFlux);
 }
 
 passivedouble CDriver::GetThermalConductivity(unsigned short iMarker, unsigned long iVertex) const {
-
-  unsigned long iPoint;
-  su2double Prandtl_Lam  = config_container[ZONE_0]->GetPrandtl_Lam();
-  su2double Gas_Constant = config_container[ZONE_0]->GetGas_ConstantND();
-  su2double Gamma = config_container[ZONE_0]->GetGamma();
-  su2double Gamma_Minus_One = Gamma - 1.0;
-  su2double Cp = (Gamma / Gamma_Minus_One) * Gas_Constant;
-  su2double laminar_viscosity, thermal_conductivity;
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  laminar_viscosity    = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
-  thermal_conductivity = Cp * (laminar_viscosity/Prandtl_Lam);
-
-  return SU2_TYPE::GetValue(thermal_conductivity);
-
+    
+    unsigned long iPoint;
+    su2double Prandtl_Lam  = config_container[ZONE_0]->GetPrandtl_Lam();
+    su2double Gas_Constant = config_container[ZONE_0]->GetGas_ConstantND();
+    su2double Gamma = config_container[ZONE_0]->GetGamma();
+    su2double Gamma_Minus_One = Gamma - 1.0;
+    su2double Cp = (Gamma / Gamma_Minus_One) * Gas_Constant;
+    su2double laminar_viscosity, thermal_conductivity;
+    
+    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+    laminar_viscosity    = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
+    thermal_conductivity = Cp * (laminar_viscosity/Prandtl_Lam);
+    
+    return SU2_TYPE::GetValue(thermal_conductivity);
+    
 }
 
 ////////////////////////////////////////////////////////////////////////////////
@@ -321,83 +321,83 @@ passivedouble CDriver::GetThermalConductivity(unsigned short iMarker, unsigned l
 ////////////////////////////////////////////////////////////////////////////////
 
 vector<string> CDriver::GetAllBoundaryMarkersTag() const {
-
-  vector<string> boundariesTagList;
-  unsigned short iMarker,nBoundariesMarkers;
-  string Marker_Tag;
-
-  nBoundariesMarkers = config_container[ZONE_0]->GetnMarker_All();
-  boundariesTagList.resize(nBoundariesMarkers);
-
-  for(iMarker=0; iMarker < nBoundariesMarkers; iMarker++){
-    Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
-    boundariesTagList[iMarker] = Marker_Tag;
-  }
-
-  return boundariesTagList;
+    
+    vector<string> boundariesTagList;
+    unsigned short iMarker,nBoundariesMarkers;
+    string Marker_Tag;
+    
+    nBoundariesMarkers = config_container[ZONE_0]->GetnMarker_All();
+    boundariesTagList.resize(nBoundariesMarkers);
+    
+    for(iMarker=0; iMarker < nBoundariesMarkers; iMarker++){
+        Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
+        boundariesTagList[iMarker] = Marker_Tag;
+    }
+    
+    return boundariesTagList;
 }
 
 vector<string> CDriver::GetAllCHTMarkersTag() const {
-
-  vector<string> CHTBoundariesTagList;
-  unsigned short iMarker, nBoundariesMarker;
-  string Marker_Tag;
-
-  nBoundariesMarker = config_container[ZONE_0]->GetnMarker_All();
-
-  //The CHT markers can be identified as the markers that are customizable with a BC type HEAT_FLUX or ISOTHERMAL.
-  for(iMarker=0; iMarker<nBoundariesMarker; iMarker++){
-    if((config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == HEAT_FLUX || config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == ISOTHERMAL) && config_container[ZONE_0]->GetMarker_All_PyCustom(iMarker)){
-      Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
-      CHTBoundariesTagList.push_back(Marker_Tag);
+    
+    vector<string> CHTBoundariesTagList;
+    unsigned short iMarker, nBoundariesMarker;
+    string Marker_Tag;
+    
+    nBoundariesMarker = config_container[ZONE_0]->GetnMarker_All();
+    
+    //The CHT markers can be identified as the markers that are customizable with a BC type HEAT_FLUX or ISOTHERMAL.
+    for(iMarker=0; iMarker<nBoundariesMarker; iMarker++){
+        if((config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == HEAT_FLUX || config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == ISOTHERMAL) && config_container[ZONE_0]->GetMarker_All_PyCustom(iMarker)){
+            Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
+            CHTBoundariesTagList.push_back(Marker_Tag);
+        }
     }
-  }
-
-  return CHTBoundariesTagList;
+    
+    return CHTBoundariesTagList;
 }
 
 vector<string> CDriver::GetAllInletMarkersTag() const {
-
-  vector<string> BoundariesTagList;
-  unsigned short iMarker, nBoundariesMarker;
-  string Marker_Tag;
-
-  nBoundariesMarker = config_container[ZONE_0]->GetnMarker_All();
-
-  for(iMarker=0; iMarker<nBoundariesMarker; iMarker++){
-    bool isCustomizable = config_container[ZONE_0]->GetMarker_All_PyCustom(iMarker);
-    bool isInlet = (config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == INLET_FLOW);
-    if(isCustomizable && isInlet) {
-      Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
-      BoundariesTagList.push_back(Marker_Tag);
+    
+    vector<string> BoundariesTagList;
+    unsigned short iMarker, nBoundariesMarker;
+    string Marker_Tag;
+    
+    nBoundariesMarker = config_container[ZONE_0]->GetnMarker_All();
+    
+    for(iMarker=0; iMarker<nBoundariesMarker; iMarker++){
+        bool isCustomizable = config_container[ZONE_0]->GetMarker_All_PyCustom(iMarker);
+        bool isInlet = (config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == INLET_FLOW);
+        if(isCustomizable && isInlet) {
+            Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
+            BoundariesTagList.push_back(Marker_Tag);
+        }
     }
-  }
-
-  return BoundariesTagList;
+    
+    return BoundariesTagList;
 }
 
 void CDriver::SetHeatSource_Position(passivedouble alpha, passivedouble pos_x, passivedouble pos_y, passivedouble pos_z){
-
-  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][RAD_SOL];
-
-  config_container[ZONE_0]->SetHeatSource_Rot_Z(alpha);
-  config_container[ZONE_0]->SetHeatSource_Center(pos_x, pos_y, pos_z);
-
-  solver->SetVolumetricHeatSource(geometry_container[ZONE_0][INST_0][MESH_0], config_container[ZONE_0]);
-
+    
+    CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][RAD_SOL];
+    
+    config_container[ZONE_0]->SetHeatSource_Rot_Z(alpha);
+    config_container[ZONE_0]->SetHeatSource_Center(pos_x, pos_y, pos_z);
+    
+    solver->SetVolumetricHeatSource(geometry_container[ZONE_0][INST_0][MESH_0], config_container[ZONE_0]);
+    
 }
 
 void CDriver::SetInlet_Angle(unsigned short iMarker, passivedouble alpha){
-
-  su2double alpha_rad = alpha * PI_NUMBER/180.0;
-
-  unsigned long iVertex;
-
-  for (iVertex = 0; iVertex < geometry_container[ZONE_0][INST_0][MESH_0]->nVertex[iMarker]; iVertex++){
-    solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->SetInlet_FlowDir(iMarker, iVertex, 0, cos(alpha_rad));
-    solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->SetInlet_FlowDir(iMarker, iVertex, 1, sin(alpha_rad));
-  }
-
+    
+    su2double alpha_rad = alpha * PI_NUMBER/180.0;
+    
+    unsigned long iVertex;
+    
+    for (iVertex = 0; iVertex < geometry_container[ZONE_0][INST_0][MESH_0]->nVertex[iMarker]; iVertex++){
+        solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->SetInlet_FlowDir(iMarker, iVertex, 0, cos(alpha_rad));
+        solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->SetInlet_FlowDir(iMarker, iVertex, 1, sin(alpha_rad));
+    }
+    
 }
 
 /////////////////////////////////////////////////////////////////////////////////////////////////////////////////
@@ -405,74 +405,74 @@ void CDriver::SetInlet_Angle(unsigned short iMarker, passivedouble alpha){
 /////////////////////////////////////////////////////////////////////////////////////////////////////////////////
 
 void CDriver::ResetConvergence() {
-
-  for(iZone = 0; iZone < nZone; iZone++) {
-    switch (config_container[iZone]->GetKind_Solver()) {
-
-    case MAIN_SOLVER::EULER: case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::RANS:
-    case MAIN_SOLVER::INC_EULER: case MAIN_SOLVER::INC_NAVIER_STOKES: case MAIN_SOLVER::INC_RANS:
-      integration_container[iZone][INST_0][FLOW_SOL]->SetConvergence(false);
-      if (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::RANS) integration_container[iZone][INST_0][TURB_SOL]->SetConvergence(false);
-      if(config_container[iZone]->GetKind_Trans_Model() == TURB_TRANS_MODEL::LM) integration_container[iZone][INST_0][TRANS_SOL]->SetConvergence(false);
-      break;
-
-    case MAIN_SOLVER::FEM_ELASTICITY:
-      integration_container[iZone][INST_0][FEA_SOL]->SetConvergence(false);
-      break;
-
-    case MAIN_SOLVER::ADJ_EULER: case MAIN_SOLVER::ADJ_NAVIER_STOKES: case MAIN_SOLVER::ADJ_RANS: case MAIN_SOLVER::DISC_ADJ_EULER: case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_RANS:
-    case MAIN_SOLVER::DISC_ADJ_INC_EULER: case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_INC_RANS:
-      integration_container[iZone][INST_0][ADJFLOW_SOL]->SetConvergence(false);
-      if( (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::ADJ_RANS) || (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_RANS) )
-        integration_container[iZone][INST_0][ADJTURB_SOL]->SetConvergence(false);
-      break;
-
-    default:
-      break;
+    
+    for(iZone = 0; iZone < nZone; iZone++) {
+        switch (config_container[iZone]->GetKind_Solver()) {
+                
+            case MAIN_SOLVER::EULER: case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::RANS:
+            case MAIN_SOLVER::INC_EULER: case MAIN_SOLVER::INC_NAVIER_STOKES: case MAIN_SOLVER::INC_RANS:
+                integration_container[iZone][INST_0][FLOW_SOL]->SetConvergence(false);
+                if (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::RANS) integration_container[iZone][INST_0][TURB_SOL]->SetConvergence(false);
+                if(config_container[iZone]->GetKind_Trans_Model() == TURB_TRANS_MODEL::LM) integration_container[iZone][INST_0][TRANS_SOL]->SetConvergence(false);
+                break;
+                
+            case MAIN_SOLVER::FEM_ELASTICITY:
+                integration_container[iZone][INST_0][FEA_SOL]->SetConvergence(false);
+                break;
+                
+            case MAIN_SOLVER::ADJ_EULER: case MAIN_SOLVER::ADJ_NAVIER_STOKES: case MAIN_SOLVER::ADJ_RANS: case MAIN_SOLVER::DISC_ADJ_EULER: case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_RANS:
+            case MAIN_SOLVER::DISC_ADJ_INC_EULER: case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_INC_RANS:
+                integration_container[iZone][INST_0][ADJFLOW_SOL]->SetConvergence(false);
+                if( (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::ADJ_RANS) || (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_RANS) )
+                    integration_container[iZone][INST_0][ADJTURB_SOL]->SetConvergence(false);
+                break;
+                
+            default:
+                break;
+        }
     }
-  }
-
+    
 }
 
 void CSinglezoneDriver::SetInitialMesh() {
-
-  DynamicMeshUpdate(0);
-
-  SU2_OMP_PARALLEL {
-    // Overwrite fictious velocities
-    for (iMesh = 0u; iMesh <= config_container[ZONE_0]->GetnMGLevels(); iMesh++) {
-      SU2_OMP_FOR_STAT(roundUpDiv(geometry_container[ZONE_0][INST_0][iMesh]->GetnPoint(),omp_get_max_threads()))
-      for (unsigned long iPoint = 0; iPoint < geometry_container[ZONE_0][INST_0][iMesh]->GetnPoint(); iPoint++) {
-
-        /*--- Overwrite fictitious velocities ---*/
-        su2double Grid_Vel[3] = {0.0, 0.0, 0.0};
-
-        /*--- Set the grid velocity for this coarse node. ---*/
-        geometry_container[ZONE_0][INST_0][iMesh]->nodes->SetGridVel(iPoint, Grid_Vel);
-      }
-      END_SU2_OMP_FOR
-      /*--- Push back the volume. ---*/
-      geometry_container[ZONE_0][INST_0][iMesh]->nodes->SetVolume_n();
-      geometry_container[ZONE_0][INST_0][iMesh]->nodes->SetVolume_nM1();
+    
+    DynamicMeshUpdate(0);
+    
+    SU2_OMP_PARALLEL {
+        // Overwrite fictious velocities
+        for (iMesh = 0u; iMesh <= config_container[ZONE_0]->GetnMGLevels(); iMesh++) {
+            SU2_OMP_FOR_STAT(roundUpDiv(geometry_container[ZONE_0][INST_0][iMesh]->GetnPoint(),omp_get_max_threads()))
+            for (unsigned long iPoint = 0; iPoint < geometry_container[ZONE_0][INST_0][iMesh]->GetnPoint(); iPoint++) {
+                
+                /*--- Overwrite fictitious velocities ---*/
+                su2double Grid_Vel[3] = {0.0, 0.0, 0.0};
+                
+                /*--- Set the grid velocity for this coarse node. ---*/
+                geometry_container[ZONE_0][INST_0][iMesh]->nodes->SetGridVel(iPoint, Grid_Vel);
+            }
+            END_SU2_OMP_FOR
+            /*--- Push back the volume. ---*/
+            geometry_container[ZONE_0][INST_0][iMesh]->nodes->SetVolume_n();
+            geometry_container[ZONE_0][INST_0][iMesh]->nodes->SetVolume_nM1();
+        }
+        /*--- Push back the solution so that there is no fictious velocity at the next step. ---*/
+        solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->Set_Solution_time_n();
+        solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->Set_Solution_time_n1();
     }
-    /*--- Push back the solution so that there is no fictious velocity at the next step. ---*/
-    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->Set_Solution_time_n();
-    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->Set_Solution_time_n1();
-  }
-  END_SU2_OMP_PARALLEL
+    END_SU2_OMP_PARALLEL
 }
 
 void CDriver::BoundaryConditionsUpdate(){
-
-  int rank = MASTER_NODE;
-  unsigned short iZone;
-
-  SU2_MPI::Comm_rank(SU2_MPI::GetComm(), &rank);
-
-  if(rank == MASTER_NODE) cout << "Updating boundary conditions." << endl;
-  for(iZone = 0; iZone < nZone; iZone++){
-    geometry_container[iZone][INST_0][MESH_0]->UpdateCustomBoundaryConditions(geometry_container[iZone][INST_0], config_container[iZone]);
-  }
+    
+    int rank = MASTER_NODE;
+    unsigned short iZone;
+    
+    SU2_MPI::Comm_rank(SU2_MPI::GetComm(), &rank);
+    
+    if(rank == MASTER_NODE) cout << "Updating boundary conditions." << endl;
+    for(iZone = 0; iZone < nZone; iZone++){
+        geometry_container[iZone][INST_0][MESH_0]->UpdateCustomBoundaryConditions(geometry_container[iZone][INST_0], config_container[iZone]);
+    }
 }
 
 ////////////////////////////////////////////////////////////////////////////////
@@ -480,95 +480,95 @@ void CDriver::BoundaryConditionsUpdate(){
 ////////////////////////////////////////////////////////////////////////////////
 
 void CDriver::SetFEA_Loads(unsigned short iMarker, unsigned long iVertex, passivedouble LoadX,
-                       passivedouble LoadY, passivedouble LoadZ) {
-
-  unsigned long iPoint;
-  su2double NodalForce[3] = {0.0,0.0,0.0};
-  NodalForce[0] = LoadX;
-  NodalForce[1] = LoadY;
-  NodalForce[2] = LoadZ;
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL]->GetNodes()->Set_FlowTraction(iPoint,NodalForce);
-
+                           passivedouble LoadY, passivedouble LoadZ) {
+    
+    unsigned long iPoint;
+    su2double NodalForce[3] = {0.0,0.0,0.0};
+    NodalForce[0] = LoadX;
+    NodalForce[1] = LoadY;
+    NodalForce[2] = LoadZ;
+    
+    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+    solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL]->GetNodes()->Set_FlowTraction(iPoint,NodalForce);
+    
 }
 
 vector<passivedouble> CDriver::GetFEA_Displacements(unsigned short iMarker, unsigned long iVertex) const {
-
-  unsigned long iPoint;
-  vector<su2double> Displacements(3, 0.0);
-  vector<passivedouble> Displacements_passive(3, 0.0);
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
-  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-
-  Displacements[0] = solver->GetNodes()->GetSolution(iPoint, 0);
-  Displacements[1] = solver->GetNodes()->GetSolution(iPoint, 1);
-  if (geometry->GetnDim() == 3)
-    Displacements[2] = solver->GetNodes()->GetSolution(iPoint, 2);
-  else
-    Displacements[2] = 0.0;
-
-  Displacements_passive[0] = SU2_TYPE::GetValue(Displacements[0]);
-  Displacements_passive[1] = SU2_TYPE::GetValue(Displacements[1]);
-  Displacements_passive[2] = SU2_TYPE::GetValue(Displacements[2]);
-
-  return Displacements_passive;
-}
-
-
-vector<passivedouble> CDriver::GetFEA_Velocity(unsigned short iMarker, unsigned long iVertex) const {
-
-  unsigned long iPoint;
-  vector<su2double> Velocity(3, 0.0);
-  vector<passivedouble> Velocity_passive(3,0.0);
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
-  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-
-  if (config_container[ZONE_0]->GetDynamic_Analysis() == DYNAMIC){
-    Velocity[0] = solver->GetNodes()->GetSolution_Vel(iPoint, 0);
-    Velocity[1] = solver->GetNodes()->GetSolution_Vel(iPoint, 1);
+    
+    unsigned long iPoint;
+    vector<su2double> Displacements(3, 0.0);
+    vector<passivedouble> Displacements_passive(3, 0.0);
+    
+    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+    CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
+    CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    
+    Displacements[0] = solver->GetNodes()->GetSolution(iPoint, 0);
+    Displacements[1] = solver->GetNodes()->GetSolution(iPoint, 1);
     if (geometry->GetnDim() == 3)
-      Velocity[2] = solver->GetNodes()->GetSolution_Vel(iPoint, 2);
+        Displacements[2] = solver->GetNodes()->GetSolution(iPoint, 2);
     else
-      Velocity[2] = 0.0;
-  }
+        Displacements[2] = 0.0;
+    
+    Displacements_passive[0] = SU2_TYPE::GetValue(Displacements[0]);
+    Displacements_passive[1] = SU2_TYPE::GetValue(Displacements[1]);
+    Displacements_passive[2] = SU2_TYPE::GetValue(Displacements[2]);
+    
+    return Displacements_passive;
+}
 
-  Velocity_passive[0] = SU2_TYPE::GetValue(Velocity[0]);
-  Velocity_passive[1] = SU2_TYPE::GetValue(Velocity[1]);
-  Velocity_passive[2] = SU2_TYPE::GetValue(Velocity[2]);
 
-  return Velocity_passive;
+vector<passivedouble> CDriver::GetFEA_Velocity(unsigned short iMarker, unsigned long iVertex) const {
+    
+    unsigned long iPoint;
+    vector<su2double> Velocity(3, 0.0);
+    vector<passivedouble> Velocity_passive(3,0.0);
+    
+    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+    CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
+    CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    
+    if (config_container[ZONE_0]->GetDynamic_Analysis() == DYNAMIC){
+        Velocity[0] = solver->GetNodes()->GetSolution_Vel(iPoint, 0);
+        Velocity[1] = solver->GetNodes()->GetSolution_Vel(iPoint, 1);
+        if (geometry->GetnDim() == 3)
+            Velocity[2] = solver->GetNodes()->GetSolution_Vel(iPoint, 2);
+        else
+            Velocity[2] = 0.0;
+    }
+    
+    Velocity_passive[0] = SU2_TYPE::GetValue(Velocity[0]);
+    Velocity_passive[1] = SU2_TYPE::GetValue(Velocity[1]);
+    Velocity_passive[2] = SU2_TYPE::GetValue(Velocity[2]);
+    
+    return Velocity_passive;
 }
 
 vector<passivedouble> CDriver::GetFEA_Velocity_n(unsigned short iMarker, unsigned long iVertex) const {
-
-  unsigned long iPoint;
-  vector<su2double> Velocity_n(3, 0.0);
-  vector<passivedouble> Velocity_n_passive(3, 0.0);
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
-  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-
-  if (config_container[ZONE_0]->GetDynamic_Analysis() == DYNAMIC){
-    Velocity_n[0] = solver->GetNodes()->GetSolution_Vel_time_n(iPoint, 0);
-    Velocity_n[1] = solver->GetNodes()->GetSolution_Vel_time_n(iPoint, 1);
-    if (geometry->GetnDim() == 3)
-      Velocity_n[2] = solver->GetNodes()->GetSolution_Vel_time_n(iPoint, 2);
-    else
-      Velocity_n[2] = 0.0;
-  }
-
-  Velocity_n_passive[0] = SU2_TYPE::GetValue(Velocity_n[0]);
-  Velocity_n_passive[1] = SU2_TYPE::GetValue(Velocity_n[1]);
-  Velocity_n_passive[2] = SU2_TYPE::GetValue(Velocity_n[2]);
-
-  return Velocity_n_passive;
-
+    
+    unsigned long iPoint;
+    vector<su2double> Velocity_n(3, 0.0);
+    vector<passivedouble> Velocity_n_passive(3, 0.0);
+    
+    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+    CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
+    CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    
+    if (config_container[ZONE_0]->GetDynamic_Analysis() == DYNAMIC){
+        Velocity_n[0] = solver->GetNodes()->GetSolution_Vel_time_n(iPoint, 0);
+        Velocity_n[1] = solver->GetNodes()->GetSolution_Vel_time_n(iPoint, 1);
+        if (geometry->GetnDim() == 3)
+            Velocity_n[2] = solver->GetNodes()->GetSolution_Vel_time_n(iPoint, 2);
+        else
+            Velocity_n[2] = 0.0;
+    }
+    
+    Velocity_n_passive[0] = SU2_TYPE::GetValue(Velocity_n[0]);
+    Velocity_n_passive[1] = SU2_TYPE::GetValue(Velocity_n[1]);
+    Velocity_n_passive[2] = SU2_TYPE::GetValue(Velocity_n[2]);
+    
+    return Velocity_n_passive;
+    
 }
 
 ////////////////////////////////////////////////////////////////////////////////
@@ -576,96 +576,96 @@ vector<passivedouble> CDriver::GetFEA_Velocity_n(unsigned short iMarker, unsigne
 ////////////////////////////////////////////////////////////////////////////////
 
 vector<passivedouble> CDriver::GetMeshDisp_Sensitivity(unsigned short iMarker, unsigned long iVertex) const {
-
-  unsigned long iPoint;
-  vector<su2double> Disp_Sens(3, 0.0);
-  vector<passivedouble> Disp_Sens_passive(3, 0.0);
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver *solver =  solver_container[ZONE_0][INST_0][MESH_0][ADJMESH_SOL];
-  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-
-  Disp_Sens[0] = solver->GetNodes()->GetBoundDisp_Sens(iPoint, 0);
-  Disp_Sens[1] = solver->GetNodes()->GetBoundDisp_Sens(iPoint, 1);
-  if (geometry->GetnDim() == 3)
-    Disp_Sens[2] = solver->GetNodes()->GetBoundDisp_Sens(iPoint, 2);
-  else
-    Disp_Sens[2] = 0.0;
-
-  Disp_Sens_passive[0] = SU2_TYPE::GetValue(Disp_Sens[0]);
-  Disp_Sens_passive[1] = SU2_TYPE::GetValue(Disp_Sens[1]);
-  Disp_Sens_passive[2] = SU2_TYPE::GetValue(Disp_Sens[2]);
-
-  return Disp_Sens_passive;
-
+    
+    unsigned long iPoint;
+    vector<su2double> Disp_Sens(3, 0.0);
+    vector<passivedouble> Disp_Sens_passive(3, 0.0);
+    
+    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+    CSolver *solver =  solver_container[ZONE_0][INST_0][MESH_0][ADJMESH_SOL];
+    CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    
+    Disp_Sens[0] = solver->GetNodes()->GetBoundDisp_Sens(iPoint, 0);
+    Disp_Sens[1] = solver->GetNodes()->GetBoundDisp_Sens(iPoint, 1);
+    if (geometry->GetnDim() == 3)
+        Disp_Sens[2] = solver->GetNodes()->GetBoundDisp_Sens(iPoint, 2);
+    else
+        Disp_Sens[2] = 0.0;
+    
+    Disp_Sens_passive[0] = SU2_TYPE::GetValue(Disp_Sens[0]);
+    Disp_Sens_passive[1] = SU2_TYPE::GetValue(Disp_Sens[1]);
+    Disp_Sens_passive[2] = SU2_TYPE::GetValue(Disp_Sens[2]);
+    
+    return Disp_Sens_passive;
+    
 }
 
 vector<passivedouble> CDriver::GetFlowLoad_Sensitivity(unsigned short iMarker, unsigned long iVertex) const {
-
-  unsigned long iPoint;
-  vector<su2double> FlowLoad_Sens(3, 0.0);
-  vector<passivedouble> FlowLoad_Sens_passive(3, 0.0);
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
-  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-
-  FlowLoad_Sens[0] = solver->GetNodes()->GetFlowTractionSensitivity(iPoint, 0);
-  FlowLoad_Sens[1] = solver->GetNodes()->GetFlowTractionSensitivity(iPoint, 1);
-  if (geometry->GetnDim() == 3)
-    FlowLoad_Sens[2] = solver->GetNodes()->GetFlowTractionSensitivity(iPoint, 2);
-  else
-    FlowLoad_Sens[2] = 0.0;
-
-  FlowLoad_Sens_passive[0] = SU2_TYPE::GetValue(FlowLoad_Sens[0]);
-  FlowLoad_Sens_passive[1] = SU2_TYPE::GetValue(FlowLoad_Sens[1]);
-  FlowLoad_Sens_passive[2] = SU2_TYPE::GetValue(FlowLoad_Sens[2]);
-
-  return FlowLoad_Sens_passive;
-
+    
+    unsigned long iPoint;
+    vector<su2double> FlowLoad_Sens(3, 0.0);
+    vector<passivedouble> FlowLoad_Sens_passive(3, 0.0);
+    
+    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+    CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
+    CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    
+    FlowLoad_Sens[0] = solver->GetNodes()->GetFlowTractionSensitivity(iPoint, 0);
+    FlowLoad_Sens[1] = solver->GetNodes()->GetFlowTractionSensitivity(iPoint, 1);
+    if (geometry->GetnDim() == 3)
+        FlowLoad_Sens[2] = solver->GetNodes()->GetFlowTractionSensitivity(iPoint, 2);
+    else
+        FlowLoad_Sens[2] = 0.0;
+    
+    FlowLoad_Sens_passive[0] = SU2_TYPE::GetValue(FlowLoad_Sens[0]);
+    FlowLoad_Sens_passive[1] = SU2_TYPE::GetValue(FlowLoad_Sens[1]);
+    FlowLoad_Sens_passive[2] = SU2_TYPE::GetValue(FlowLoad_Sens[2]);
+    
+    return FlowLoad_Sens_passive;
+    
 }
 
 void CDriver::SetFlowLoad_Adjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
                                   passivedouble val_AdjointY, passivedouble val_AdjointZ) {
-
-  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL];
-  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-
-  solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 0, val_AdjointX);
-  solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 1, val_AdjointY);
-  if (geometry->GetnDim() == 3)
-    solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 2, val_AdjointZ);
-
+    
+    CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL];
+    CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    
+    solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 0, val_AdjointX);
+    solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 1, val_AdjointY);
+    if (geometry->GetnDim() == 3)
+        solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 2, val_AdjointZ);
+    
 }
 
 void CDriver::SetSourceTerm_DispAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
                                         passivedouble val_AdjointY, passivedouble val_AdjointZ) {
-
-  unsigned long iPoint;
-
-  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
-  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-
-  solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 0, val_AdjointX);
-  solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 1, val_AdjointY);
-  if (geometry->GetnDim() == 3)
-    solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 2, val_AdjointZ);
-
+    
+    unsigned long iPoint;
+    
+    CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
+    CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+    
+    solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 0, val_AdjointX);
+    solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 1, val_AdjointY);
+    if (geometry->GetnDim() == 3)
+        solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 2, val_AdjointZ);
+    
 }
 
 void CDriver::SetSourceTerm_VelAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
-                                        passivedouble val_AdjointY, passivedouble val_AdjointZ) {
-
-  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
-  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-  const auto iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-
-  solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 0, val_AdjointX);
-  solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 1, val_AdjointY);
-  if (geometry->GetnDim() == 3)
-    solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 2, val_AdjointZ);
-
+                                       passivedouble val_AdjointY, passivedouble val_AdjointZ) {
+    
+    CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
+    CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    const auto iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+    
+    solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 0, val_AdjointX);
+    solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 1, val_AdjointY);
+    if (geometry->GetnDim() == 3)
+        solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 2, val_AdjointZ);
+    
 }
 
 ////////////////////////////////////////////////////////////////////////////////
@@ -673,26 +673,26 @@ void CDriver::SetSourceTerm_VelAdjoint(unsigned short iMarker, unsigned long iVe
 ////////////////////////////////////////////////////////////////////////////////
 
 vector<passivedouble> CDriver::GetFlowLoad(unsigned short iMarker, unsigned long iVertex) const {
-
-  vector<su2double> FlowLoad(3, 0.0);
-  vector<passivedouble> FlowLoad_passive(3, 0.0);
-
-  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL];
-  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-
-  if (config_container[ZONE_0]->GetSolid_Wall(iMarker)) {
-    FlowLoad[0] = solver->GetVertexTractions(iMarker, iVertex, 0);
-    FlowLoad[1] = solver->GetVertexTractions(iMarker, iVertex, 1);
-    if (geometry->GetnDim() == 3)
-      FlowLoad[2] = solver->GetVertexTractions(iMarker, iVertex, 2);
-    else
-      FlowLoad[2] = 0.0;
-  }
-
-  FlowLoad_passive[0] = SU2_TYPE::GetValue(FlowLoad[0]);
-  FlowLoad_passive[1] = SU2_TYPE::GetValue(FlowLoad[1]);
-  FlowLoad_passive[2] = SU2_TYPE::GetValue(FlowLoad[2]);
-
-  return FlowLoad_passive;
-
+    
+    vector<su2double> FlowLoad(3, 0.0);
+    vector<passivedouble> FlowLoad_passive(3, 0.0);
+    
+    CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL];
+    CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    
+    if (config_container[ZONE_0]->GetSolid_Wall(iMarker)) {
+        FlowLoad[0] = solver->GetVertexTractions(iMarker, iVertex, 0);
+        FlowLoad[1] = solver->GetVertexTractions(iMarker, iVertex, 1);
+        if (geometry->GetnDim() == 3)
+            FlowLoad[2] = solver->GetVertexTractions(iMarker, iVertex, 2);
+        else
+            FlowLoad[2] = 0.0;
+    }
+    
+    FlowLoad_passive[0] = SU2_TYPE::GetValue(FlowLoad[0]);
+    FlowLoad_passive[1] = SU2_TYPE::GetValue(FlowLoad[1]);
+    FlowLoad_passive[2] = SU2_TYPE::GetValue(FlowLoad[2]);
+    
+    return FlowLoad_passive;
+    
 }
diff --git a/SU2_DEF/include/SU2_DEF.hpp b/SU2_DEF/include/SU2_DEF.hpp
index b0f7ab26fc2..ea076540340 100644
--- a/SU2_DEF/include/SU2_DEF.hpp
+++ b/SU2_DEF/include/SU2_DEF.hpp
@@ -26,7 +26,6 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #pragma once
 
 #include "../../Common/include/parallelization/mpi_structure.hpp"
diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index 329c660bb4c..507978d77e7 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -41,74 +41,74 @@
 #include "../../../Common/include/drivers/CDriverBase.hpp"
 
 class CDeformationDriver : public CDriverBase {
-
+    
 protected:
-  bool haveSurfaceDeformation = false;  // flag used to determine whether surface deformation is available for output
-
+    bool haveSurfaceDeformation = false;  // flag used to determine whether surface deformation is available for output
+    
 public:
-  /*!
-   * \brief Constructor of the class.
-   * \param[in] confFile - Configuration file name.
-   * \param[in] MPICommunicator - MPI communicator for SU2.
-   */
-  CDeformationDriver(char* confFile, SU2_Comm MPICommunicator);
-
-  /*!
-   * \brief Destructor of the class.
-   */
-  ~CDeformationDriver(void);
-
-  /*!
-   * \brief [Overload] Launch the computation for single-zone problems.
-   */
-  void Run();
-
-  /*!
-   * \brief Output the mesh.
-   */
-  void Output();
-
-  /*!
-   * \brief Deallocation routine
-   */
-  void Postprocessing();
-
-  void CommunicateMeshDisplacements(void);
-
+    /*!
+     * \brief Constructor of the class.
+     * \param[in] confFile - Configuration file name.
+     * \param[in] MPICommunicator - MPI communicator for SU2.
+     */
+    CDeformationDriver(char* confFile, SU2_Comm MPICommunicator);
+    
+    /*!
+     * \brief Destructor of the class.
+     */
+    ~CDeformationDriver(void);
+    
+    /*!
+     * \brief [Overload] Launch the computation for single-zone problems.
+     */
+    void Run();
+    
+    /*!
+     * \brief Output the mesh.
+     */
+    void Output();
+    
+    /*!
+     * \brief Deallocation routine
+     */
+    void Postprocessing();
+    
+    void CommunicateMeshDisplacements(void);
+    
 protected:
-  /*!
-   * \brief Read in the config and mesh files.
-   */
-  void Input_Preprocessing();
-
-  /*!
-   * \brief Construction of the edge-based data structure.
-   */
-  void Geometrical_Preprocessing();
-
-  /*!
-   * \brief Preprocess the output container.
-   */
-  void Output_Preprocessing();
-
-  /*!
-   * \brief Preprocess the mesh solver container.
-   */
-  void Solver_Preprocessing();
-
-  /*!
-   * \brief Preprocess the numerics container.
-   */
-  void Numerics_Preprocessing();
-
-  /*!
-   * \brief Mesh deformation based on linear elasticity solver (CMeshSolver).
-   */
-  void Update();
-
-  /*!
-   * \brief Mesh deformation based on legacy implementation.
-   */
-  void Update_Legacy();
-
+    /*!
+     * \brief Read in the config and mesh files.
+     */
+    void Input_Preprocessing();
+    
+    /*!
+     * \brief Construction of the edge-based data structure.
+     */
+    void Geometrical_Preprocessing();
+    
+    /*!
+     * \brief Preprocess the output container.
+     */
+    void Output_Preprocessing();
+    
+    /*!
+     * \brief Preprocess the mesh solver container.
+     */
+    void Solver_Preprocessing();
+    
+    /*!
+     * \brief Preprocess the numerics container.
+     */
+    void Numerics_Preprocessing();
+    
+    /*!
+     * \brief Mesh deformation based on linear elasticity solver (CMeshSolver).
+     */
+    void Update();
+    
+    /*!
+     * \brief Mesh deformation based on legacy implementation.
+     */
+    void Update_Legacy();
+    
 };
diff --git a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
index 1f1f79b76c1..176f89b93f9 100644
--- a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
@@ -51,7 +51,7 @@
  * \version 7.3.0 "Blackbird"
  */
 class CDiscAdjDeformationDriver : public CDriverBase {
-
+    
 protected:
     su2double** Gradient;
     ofstream Gradient_file; 
diff --git a/SU2_DEF/src/SU2_DEF.cpp b/SU2_DEF/src/SU2_DEF.cpp
index 4cf24b8b5d1..3c5d4db9273 100644
--- a/SU2_DEF/src/SU2_DEF.cpp
+++ b/SU2_DEF/src/SU2_DEF.cpp
@@ -25,52 +25,51 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #include "../include/SU2_DEF.hpp"
 
 using namespace std;
 
 int main(int argc, char *argv[]) {
-
-  char config_file_name[MAX_STRING_SIZE];
-
-  /*--- Create a pointer to the main SU2_DEF Driver ---*/
-
-  CDeformationDriver* driver = nullptr;
-
-  /*--- MPI initialization ---*/
-
+    
+    char config_file_name[MAX_STRING_SIZE];
+    
+    /*--- Create a pointer to the main SU2_DEF Driver ---*/
+    
+    CDeformationDriver* driver = nullptr;
+    
+    /*--- MPI initialization ---*/
+    
 #if defined(HAVE_OMP) && defined(HAVE_MPI)
-  int provided;
-  SU2_MPI::Init_thread(&argc, &argv, MPI_THREAD_FUNNELED, &provided);
+    int provided;
+    SU2_MPI::Init_thread(&argc, &argv, MPI_THREAD_FUNNELED, &provided);
 #else
-  SU2_MPI::Init(&argc, &argv);
+    SU2_MPI::Init(&argc, &argv);
 #endif
-  SU2_MPI::Comm comm = SU2_MPI::GetComm();
-
-  /*--- Load in the number of zones and spatial dimensions in the mesh file
-   (if no config file is specified, default.cfg is used) ---*/
-
-  if (argc == 2) { strcpy(config_file_name, argv[1]); }
-  else { strcpy(config_file_name, "default.cfg"); }
-
-  /*--- Initialize the mesh deformation driver ---*/
-
-  driver = new CDeformationDriver(config_file_name, comm);
-
-  /*--- Launch the main external loop of the solver. ---*/
-
-  driver->Run();
-
-  /*--- Postprocess all the containers, close history file, exit SU2. ---*/
-
-  driver->Postprocessing();
-
-  delete driver;
-
-  /*--- Finalize MPI parallelization ---*/
-  SU2_MPI::Finalize();
-
-  return EXIT_SUCCESS;
-
+    SU2_MPI::Comm comm = SU2_MPI::GetComm();
+    
+    /*--- Load in the number of zones and spatial dimensions in the mesh file
+     (if no config file is specified, default.cfg is used) ---*/
+    
+    if (argc == 2) { strcpy(config_file_name, argv[1]); }
+    else { strcpy(config_file_name, "default.cfg"); }
+    
+    /*--- Initialize the mesh deformation driver ---*/
+    
+    driver = new CDeformationDriver(config_file_name, comm);
+    
+    /*--- Launch the main external loop of the solver. ---*/
+    
+    driver->Run();
+    
+    /*--- Postprocess all the containers, close history file, exit SU2. ---*/
+    
+    driver->Postprocessing();
+    
+    delete driver;
+    
+    /*--- Finalize MPI parallelization ---*/
+    SU2_MPI::Finalize();
+    
+    return EXIT_SUCCESS;
+    
 }
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 8bf4b8b9e98..ecca754838a 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -36,7 +36,7 @@
 using namespace std;
 
 CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator):
-    CDriverBase(confFile, 1, MPICommunicator) 
+CDriverBase(confFile, 1, MPICommunicator)
 {
     
     /*--- Initialize Medipack (must also be here so it is initialized from python) ---*/
@@ -107,7 +107,7 @@ void CDeformationDriver::Input_Preprocessing() {
     /*--- Initialize the configuration of the driver ---*/
     driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DEF);
     
-    nZone = driver_config->GetnZone();  
+    nZone = driver_config->GetnZone();
     
     /*--- Loop over all zones to initialize the various classes. In most
      cases, nZone is equal to one. This represents the solution of a partial
@@ -162,7 +162,7 @@ void CDeformationDriver::Geometrical_Preprocessing() {
         
         unsigned short nInst_Zone = nInst[iZone];
         unsigned short nMesh = 1;
-
+        
         geometry_container[iZone] = new CGeometry**[nInst_Zone] ();
         geometry_container[iZone][INST_0] = new CGeometry*[nMesh] ();
         geometry_container[iZone][INST_0][MESH_0] = new CPhysicalGeometry(geometry_aux, config_container[iZone]);
@@ -217,7 +217,7 @@ void CDeformationDriver::Geometrical_Preprocessing() {
         geometry_container[iZone][INST_0][MESH_0]->PreprocessP2PComms(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
         
     }
-        
+    
     /*--- Get the number of dimensions ---*/
     nDim = geometry_container[ZONE_0][INST_0][MESH_0]->GetnDim();
 }
@@ -247,13 +247,13 @@ void CDeformationDriver::Solver_Preprocessing() {
         unsigned short nInst_Zone = nInst[iZone];
         unsigned short nMesh = 1;
         unsigned short nSols = MAX_SOLS;
-
-
+        
+        
         solver_container[iZone] = new CSolver*** [nInst_Zone] ();
         solver_container[iZone][INST_0] = new CSolver** [nMesh] ();
         solver_container[iZone][INST_0][MESH_0] = new CSolver* [nSols] ();
         solver_container[iZone][INST_0][MESH_0][MESH_SOL] = new CMeshSolver(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
-    } 
+    }
 }
 
 void CDeformationDriver::Numerics_Preprocessing() {
@@ -263,7 +263,7 @@ void CDeformationDriver::Numerics_Preprocessing() {
         unsigned short nMesh = 1;
         unsigned short nSols = MAX_SOLS;
         unsigned int nTerm = omp_get_num_threads() * MAX_TERMS;
-
+        
         numerics_container[iZone] = new CNumerics**** [nInst_Zone] ();
         numerics_container[iZone][INST_0] = new CNumerics*** [nMesh] ();
         numerics_container[iZone][INST_0][MESH_0] = new CNumerics** [nSols] ();
@@ -328,7 +328,7 @@ void CDeformationDriver::Update() {
 }
 
 void CDeformationDriver::Update_Legacy() {
-
+    
     for (iZone = 0; iZone < nZone; iZone++){
         
         if (config_container[iZone]->GetDesign_Variable(0) != NO_DEFORMATION) {
@@ -510,7 +510,7 @@ void CDeformationDriver::Output() {
         /*--- Load the data --- */
         
         output_container[iZone]->Load_Data(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], nullptr);
-
+        
         output_container[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone][INST_0][MESH_0], OUTPUT_TYPE::MESH, driver_config->GetMesh_Out_FileName());
         
         /*--- Set the file names for the visualization files ---*/
@@ -539,9 +539,9 @@ void CDeformationDriver::Output() {
             }
             else {
                 if (rank == MASTER_NODE) cout << "Adding any FFD information to the SU2 file." << endl;
-
+                
                 surface_movement[ZONE_0]->WriteFFDInfo(surface_movement, geometry_container, config_container);
-            }  
+            }
         }
     }
 }
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index fea679b6f55..bab02b385ca 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -32,7 +32,7 @@
 using namespace std;
 
 CDiscAdjDeformationDriver::CDiscAdjDeformationDriver(char* confFile, SU2_Comm MPICommunicator):
-    CDriverBase(confFile, 1, MPICommunicator) 
+CDriverBase(confFile, 1, MPICommunicator)
 {
     /*--- Initialize Medipack (must also be here so it is initialized from python) ---*/
 #ifdef HAVE_MPI
@@ -83,14 +83,14 @@ CDiscAdjDeformationDriver::~CDiscAdjDeformationDriver(void) {
 }
 
 void CDiscAdjDeformationDriver::Input_Preprocessing() {
-
+    
     /*--- Initialize a char to store the zone filename ---*/
     char zone_file_name[MAX_STRING_SIZE];
     
     /*--- Initialize the configuration of the driver ---*/
     driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DEF);
     
-    nZone = driver_config->GetnZone();  
+    nZone = driver_config->GetnZone();
     
     /*--- Loop over all zones to initialize the various classes. In most
      cases, nZone is equal to one. This represents the solution of a partial
@@ -110,11 +110,11 @@ void CDiscAdjDeformationDriver::Input_Preprocessing() {
         }
         
         config_container[iZone]->SetMPICommunicator(SU2_MPI::GetComm());
-    
+        
         if (!config_container[iZone]->GetDiscrete_Adjoint()) {
             SU2_MPI::Error("The discrete adjoint solver was not specified in the configuration file.", CURRENT_FUNCTION);
         }
-
+        
     }
     
     /*--- Set the multizone part of the problem. ---*/
@@ -265,7 +265,7 @@ void CDiscAdjDeformationDriver::Run() {
     for (iZone = 0; iZone < nZone; iZone++) {
         if (rank == MASTER_NODE) cout << "Reading volume sensitivities at each node from file." << endl;
         unsigned short nInst_Zone = nInst[iZone];
-
+        
         grid_movement[iZone] = new CVolumetricMovement* [nInst_Zone] ();
         grid_movement[iZone][INST_0] = new CVolumetricMovement(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
         
@@ -366,7 +366,7 @@ void CDiscAdjDeformationDriver::Postprocessing() {
     }
     delete [] solver_container;
     if (rank == MASTER_NODE) cout << "Deleted CSolver container." << endl;
-        
+    
     if (geometry_container != nullptr) {
         for (iZone = 0; iZone < nZone; iZone++) {
             if (geometry_container[iZone] != nullptr) {
@@ -425,7 +425,7 @@ void CDiscAdjDeformationDriver::Postprocessing() {
     if (rank == MASTER_NODE) cout << "Deleted COutput class." << endl;
     
     if (nInst != nullptr) delete [] nInst;
-
+    
     /*--- Exit the solver cleanly ---*/
     
     if (rank == MASTER_NODE)

From 976408cfbc3a97e4a43a0954f5add106028a4157 Mon Sep 17 00:00:00 2001
From: aa-g <aa.gastaldi@pm.me>
Date: Mon, 21 Feb 2022 16:23:49 +0100
Subject: [PATCH 020/656] Fix dangling if statement in
 CDiscAdjDeformationDriver

---
 SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp | 9 +++++----
 1 file changed, 5 insertions(+), 4 deletions(-)

diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index bab02b385ca..a91ade80097 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -312,18 +312,19 @@ void CDiscAdjDeformationDriver::Run() {
             /*--- Copy coordinates to the surface structure ---*/
             
             surface_movement[iZone]->CopyBoundary(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
-            
+
             /*--- If AD mode is enabled we can use it to compute the projection,
              *    otherwise we use finite differences. ---*/
             
-            if (config_container[iZone]->GetAD_Mode())
+            if (config_container[iZone]->GetAD_Mode()) {
                 if (config_container[iZone]->GetSmoothGradient()) {
                     DerivativeTreatment_Gradient(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], grid_movement[iZone][INST_0], surface_movement[iZone] , Gradient);
                 } else {
                     SetProjection_AD(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], surface_movement[iZone] , Gradient);
                 }
-        } else {
-            SetProjection_FD(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], surface_movement[iZone] , Gradient);
+            } else {
+                SetProjection_FD(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], surface_movement[iZone] , Gradient);
+            }
         }
     } // for iZone
     

From 1b4ba30126576d9141d7b76c4ed72115d8ca2250 Mon Sep 17 00:00:00 2001
From: aa-g <aa.gastaldi@pm.me>
Date: Thu, 3 Mar 2022 22:58:57 +0100
Subject: [PATCH 021/656] Fix py_wrapper tests broken by new Python interface

---
 .../py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py     | 2 +-
 .../py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py    | 4 ++--
 2 files changed, 3 insertions(+), 3 deletions(-)

diff --git a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
index 1f994db4118..89006b9a53a 100755
--- a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
@@ -71,7 +71,7 @@ def main():
   MarkerList = SU2Driver.GetAllBoundaryMarkersTag()
 
   # Get all the markers defined on this rank and their associated indices.
-  allMarkerIDs = SU2Driver.GetAllBoundaryMarkers()
+  allMarkerIDs = SU2Driver.GetBoundaryMarkerIndices()
 
   #Check if the specified marker exists and if it belongs to this rank.
   if MarkerName in MarkerList and MarkerName in allMarkerIDs.keys():
diff --git a/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
index f4ee6ed5b68..2229ad8ce5c 100755
--- a/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
@@ -70,7 +70,7 @@ def main():
   MarkerList = SU2Driver.GetAllBoundaryMarkersTag()
 
   # Get all the markers defined on this rank and their associated indices.
-  allMarkerIDs = SU2Driver.GetAllBoundaryMarkers()
+  allMarkerIDs = SU2Driver.GetBoundaryMarkerIndices()
 
   #Check if the specified marker exists and if it belongs to this rank.
   if MarkerName in MarkerList and MarkerName in allMarkerIDs.keys():
@@ -80,7 +80,7 @@ def main():
   nVertex_Marker = 0         #total number of vertices (physical + halo)
 
   if MarkerID != None:
-    nVertex_Marker = SU2Driver.GetNumberVertices(MarkerID)
+    nVertex_Marker = SU2Driver.GetNumberVerticesMarker(MarkerID)
 
   # Time loop is defined in Python so that we have acces to SU2 functionalities at each time step
   if rank == 0:

From 4a79c133f4fe29405961451de71c7e4a5fe9dbfd Mon Sep 17 00:00:00 2001
From: aa-g <aa.gastaldi@pm.me>
Date: Mon, 7 Mar 2022 20:12:46 +0100
Subject: [PATCH 022/656] Implement overleaded getters/setter

---
 Common/include/drivers/CDriverBase.hpp        | 376 ++++++++--
 Common/src/drivers/CDriverBase.cpp            | 688 ++++++++++++------
 SU2_CFD/include/drivers/CDriver.hpp           |  16 +-
 SU2_CFD/src/python_wrapper_structure.cpp      |  58 +-
 .../flow_load_sens/run_adjoint.py             |   4 +-
 .../mesh_disp_sens/run_adjoint.py             |   8 +-
 .../launch_flatPlate_rigidMotion.py           |  17 +-
 .../launch_unsteady_CHT_FlatPlate.py          |  15 +-
 8 files changed, 832 insertions(+), 350 deletions(-)

diff --git a/Common/include/drivers/CDriverBase.hpp b/Common/include/drivers/CDriverBase.hpp
index 28619eab44e..6b9590fdd22 100644
--- a/Common/include/drivers/CDriverBase.hpp
+++ b/Common/include/drivers/CDriverBase.hpp
@@ -111,19 +111,30 @@ class CDriverBase {
      * \brief A virtual member.
      */
     virtual void Postprocessing() {};
+    /*!
+     * \brief Get the number of markers in the mesh.
+     * \return Number of markers.
+     */
+    unsigned short GetNumberMarkers() const;
     
     /*!
      * \brief Get all the boundary markers tags with their associated indices.
      * \return List of boundary markers tags with their indices.
      */
-    map<string, int> GetBoundaryMarkerIndices() const;
+    map<string, int> GetMarkerIndices() const;
     
     /*!
      * \brief Get all the boundary markers tags with their associated types.
      * \return List of boundary markers tags with their types.
      */
-    map<string, string> GetBoundaryMarkerTypes() const;
+    map<string, string> GetMarkerTypes() const;
     
+    /*!
+     * \brief Get all the boundary marker tags.
+     * \return List of boundary markers tags.
+     */
+    vector<string> GetMarkerTags() const;
+
     /*!
      * \brief Get all the deformable boundary marker tags.
      * \return List of deformable boundary markers tags.
@@ -131,170 +142,393 @@ class CDriverBase {
     vector<string> GetDeformableMarkerTags() const;
     
     /*!
-     * \brief Get the number of mesh dimensions.
+     * \brief Get the number of dimensions of the mesh.
      * \return Number of dimensions.
      */
     unsigned long GetNumberDimensions() const;
     
     /*!
-     * \brief Get the number of mesh elements.
+     * \brief Get the number of elements in the mesh.
      * \return Number of elements.
      */
     unsigned long GetNumberElements() const;
     
     /*!
-     * \brief Get the number of mesh elements from a specified marker.
-     * \param[in] iMarker - Marker identifier.
+     * \brief Get the number of elements in the marker.
+     * \param[in] iMarker - Marker index.
      * \return Number of elements.
      */
-    unsigned long GetNumberElementsMarker(unsigned short iMarker) const;
+    unsigned long GetNumberMarkerElements(unsigned short iMarker) const;
+    
+    /*!
+     * \brief Get the global IDs of the mesh elements.
+     * \return Global element IDs.
+     */
+    vector<unsigned long> GetElementIDs() const;
     
     /*!
-     * \brief Get the number of mesh vertices.
+     * \brief Get the global ID of a mesh element.
+     * \param[in] iElem - Mesh element index.
+     * \return Global element ID.
+     */
+    unsigned long GetElementIDs(unsigned long iElem) const;
+    
+    /*!
+     * \brief Get the global IDs of the marker elements.
+     * \param[in] iMarker - Marker index.
+     * \return Global element IDs.
+     */
+    vector<unsigned long> GetMarkerElementIDs(unsigned short iMarker) const;
+    
+    /*!
+     * \brief Get the global IDs of a marker element.
+     * \param[in] iMarker - Marker index.
+     * \param[in] iBound - Marker element index.
+     * \return Global element ID.
+     */
+    unsigned long GetMarkerElementIDs(unsigned short iMarker, unsigned long iBound) const;
+    
+    /*!
+     * \brief Get the MPI colors for mesh elements.
+     * \return Element colors.
+     */
+    vector<unsigned long> GetElementColors() const;
+    
+    /*!
+     * \brief Get the MPI color for a mesh element.
+     * \param[in] iElem - Mesh element index.
+     * \return Element color.
+     */
+    unsigned long GetElementColors(unsigned long iElem) const;
+    
+    /*!
+     * \brief Get the MPI colors for marker elements.
+     * \param[in] iMarker - Marker index.
+     * \return Element colors.
+     */
+    vector<unsigned long> GetMarkerElementColors(unsigned short iMarker) const;
+     
+    /*!
+     * \brief Get the MPI color for a marker element.
+     * \param[in] iMarker - Marker index.
+     * \param[in] iBound - Marker element index.
+     * \return Element color.
+     */
+    unsigned long GetMarkerElementColors(unsigned short iMarker, unsigned long iBound) const;
+
+    /*!
+     * \brief Get the table of vertex IDs belonging to the mesh elements.
+     * \return Element connectivities (nElem, nNode)
+     */
+    vector<vector<unsigned long>> GetElementConnectivities() const;
+    
+    /*!
+     * \brief Get the row of vertex IDs belonging to a mesh element.
+     * \param[in] iElem - Mesh element index.
+     * \return Element connectivity (nNode)
+     */
+    vector<unsigned long> GetElementConnectivities(unsigned long iElem) const;
+    
+    /*!
+     * \brief Get the table of vertex IDs belonging to the marker elements.
+     * \param[in] iMarker - Marker index.
+     * \return Element connectivities (nBound, nNode).
+     */
+    vector<vector<unsigned long>> GetMarkerElementConnectivities(unsigned short iMarker) const;
+    
+    /*!
+     * \brief Get the row of vertex IDs belonging to a marker element.
+     * \param[in] iMarker - Marker index.
+     * \param[in] iBound - Marker element index.
+     * \return Element connectivity (nNode).
+     */
+    vector<unsigned long> GetMarkerElementConnectivities(unsigned short iMarker, unsigned long iBound) const;
+    
+    /*!
+     * \brief Get the number of vertices in the mesh.
      * \return Number of vertices.
      */
     unsigned long GetNumberVertices() const;
     
     /*!
-     * \brief Get the number of mesh vertices from a specified marker.
-     * \param[in] iMarker - Marker identifier.
+     * \brief Get the number of vertices in the marker.
+     * \param[in] iMarker - Marker index.
      * \return Number of vertices.
      */
-    unsigned long GetNumberVerticesMarker(unsigned short iMarker) const;
+    unsigned long GetNumberMarkerVertices(unsigned short iMarker) const;
     
     /*!
-     * \brief Get the number of halo mesh vertices.
+     * \brief Get the number of halo vertices in the mesh.
      * \return Number of vertices.
      */
     unsigned long GetNumberHaloVertices() const;
     
     /*!
-     * \brief Get the number of halo mesh vertices from a specified marker.
-     * \param[in] iMarker - Marker identifier.
+     * \brief Get the number of halo vertices in the marker.
+     * \param[in] iMarker - Marker index.
      * \return Number of vertices.
      */
-    unsigned long GetNumberHaloVerticesMarker(unsigned short iMarker) const;
+    unsigned long GetNumberMarkerHaloVertices(unsigned short iMarker) const;
     
     /*!
-     * \brief Get global IDs of mesh vertices.
+     * \brief Get the mesh vertex indices of the marker vertices.
+     * \param[in] iMarker - Marker index.
+     * \return Mesh vertex indices.
+     */
+    vector<unsigned long> GetMarkerVertexIndex(unsigned short iMarker) const;
+    
+    /*!
+     * \brief Get the mesh vertex index of a marker vertex.
+     * \param[in] iMarker - Marker index.
+     * \param[in] iVertex - Marker vertex index.
+     * \return Mesh vertex index.
+     */
+    unsigned long GetMarkerVertexIndex(unsigned short iMarker, unsigned long iVertex) const;
+    
+    /*!
+     * \brief Get the global IDs of the mesh vertices.
      * \return Global vertex IDs.
      */
     vector<unsigned long> GetVertexIDs() const;
+
+    /*!
+     * \brief Get the global ID of a mesh vertex.
+     * \param[in] iPoint - Mesh vertex index.
+     * \return Global vertex ID.
+     */
+    unsigned long GetVertexIDs(unsigned long iPoint) const;
     
     /*!
-     * \brief Get global IDs of mesh vertices.
-     * \param[in] iMarker - Marker identifier.
+     * \brief Get the global IDs of the marker vertices.
+     * \param[in] iMarker - Marker index.
      * \return Global vertex IDs.
      */
-    vector<unsigned long> GetVertexIDsMarker(unsigned short iMarker) const;
+    vector<unsigned long> GetMarkerVertexIDs(unsigned short iMarker) const;
     
     /*!
-     * \brief Get global IDs of mesh elements.
-     * \return Global element IDs.
+     * \brief Get the global ID of a marker vertex.
+     * \param[in] iMarker - Marker index.
+     * \param[in] iVertex - Marker vertex index.
+     * \return Global vertex ID.
      */
-    vector<unsigned long> GetElementIDs() const;
+    unsigned long GetMarkerVertexIDs(unsigned short iMarker, unsigned long iVertex) const;
     
     /*!
-     * \brief Get global IDs of mesh elements.
-     * \param[in] iMarker - Marker identifier.
-     * \return Global element IDs.
+     * \brief Get the MPI colors of the mesh vertices.
+     * \return Vertex colors.
      */
-    vector<unsigned long> GetElementIDsMarker(unsigned short iMarker) const;
+    vector<unsigned long> GetVertexColors() const;
     
     /*!
-     * \brief Get the connected point IDs of mesh elements.
-     * \return Element connectivities (nElem, nNode)
+     * \brief Get the MPI color of a mesh vertex.
+     * \param[in] iPoint - Mesh vertex index.
+     * \return Vertex color.
      */
-    vector<vector<unsigned long>> GetConnectivity() const;
+    unsigned long GetVertexColors(unsigned long iPoint) const;
     
     /*!
-     * \brief Get the connected point IDs of mesh elements on a specified marker.
-     * \param[in] iMarker - Marker identifier.
-     * \return Element connectivities (nBound, nNode).
+     * \brief Get the MPI colors of the marker vertices.
+     * \param[in] iMarker - Marker index.
+     * \return Vertex colors.
      */
-    vector<vector<unsigned long>> GetConnectivityMarker(unsigned short iMarker) const;
+    vector<unsigned long> GetMarkerVertexColors(unsigned short iMarker) const;
     
     /*!
-     * \brief Get halo node stauts of mesh vertices.
-     * \return Point domain status.
+     * \brief Get the MPI color of a marker vertex.
+     * \param[in] iMarker - Marker index.
+     * \param[in] iVertex - Marker vertex index.
+     * \return Vertex color.
+     */
+    unsigned long GetMarkerVertexColors(unsigned short iMarker, unsigned long iVertex) const;
+    
+    /*!
+     * \brief Get the halo flags of the mesh vertices.
+     * \return Vertex domain flags.
      */
     vector<bool> GetDomain() const;
     
     /*!
-     * \brief Get halo node stauts of mesh marker vertices.
-     * \param[in] iMarker - Marker identifier.
-     * \return Point domain status.
+     * \brief Get the halo flag of a mesh vertex.
+     * \param[in] iPoint - Mesh vertex index.
+     * \return Vertex domain flag.
+     */
+    bool GetDomain(unsigned long iPoint) const;
+    
+    /*!
+     * \brief Get the halo flags of the marker vertices.
+     * \param[in] iMarker - Marker index.
+     * \return Vertex domain flags.
+     */
+    vector<bool> GetMarkerDomain(unsigned short iMarker) const;
+    
+    /*!
+     * \brief Get the halo flag of a marker vertex.
+     * \param[in] iMarker - Marker index.
+     * \param[in] iVertex - Marker vertex index.
+     * \return Vertex domain flag.
+     */
+    bool GetMarkerDomain(unsigned short iMarker, unsigned long iVertex) const;
+    
+    /*!
+     * \brief Get the initial (un-deformed) coordinates of the mesh vertices.
+     * \return Initial vertex coordinates (nPoint*nDim).
+     */
+    vector<passivedouble> GetInitialCoordinates() const;
+
+    /*!
+     * \brief Get the initial (un-deformed) coordinates of a mesh vertex.
+     * \param[in] iPoint - Mesh vertex index.
+     * \return Initial vertex coordinates (nDim).
+     */
+    vector<passivedouble> GetInitialCoordinates(unsigned long iPoint) const;
+    
+    /*!
+     * \brief Get the initial (un-deformed) coordinates of the marker vertices.
+     * \param[in] iMarker - Marker index.
+     * \return Initial vertex coordinates (nVertex*nDim).
+     */
+    vector<passivedouble> GetMarkerInitialCoordinates(unsigned short iMarker) const;
+    
+    /*!
+     * \brief Get the initial (un-deformed) coordinates of a marker vertex.
+     * \param[in] iMarker - Marker index.
+     * \param[in] iVertex - Marker vertex index.
+     * \return Initial vertex coordinates (nDim).
      */
-    vector<bool> GetDomainMarker(unsigned short iMarker) const;
+    vector<passivedouble> GetMarkerInitialCoordinates(unsigned short iMarker, unsigned long iVertex) const;
     
     /*!
-     * \brief Get the coordinates of the mesh points.
-     * \return Point coordinates (nPoint*nDim).
+     * \brief Get the coordinates of the mesh vertices.
+     * \return Vertex coordinates (nPoint*nDim).
      */
     vector<passivedouble> GetCoordinates() const;
+
+    /*!
+     * \brief Get the coordinates of a mesh vertex.
+     * \param[in] iPoint - Mesh vertex index.
+     * \return Vertex coordinates (nDim).
+     */
+    vector<passivedouble> GetCoordinates(unsigned long iPoint) const;
+    
+    /*!
+     * \brief Get the coordinates of the marker vertices.
+     * \param[in] iMarker - Marker index.
+     * \return Vertex coordinates (nVertex*nDim).
+     */
+    vector<passivedouble> GetMarkerCoordinates(unsigned short iMarker) const;
     
     /*!
-     * \brief Get the coordinates of the mesh points on the specified marker.
-     * \param[in] iMarker - Marker identifier.
-     * \return Point coordinates (nVertex*nDim).
+     * \brief Get the coordinates of a marker vertex.
+     * \param[in] iMarker - Marker index.
+     * \param[in] iVertex - Marker vertex index.
+     * \return Vertex coordinates (nDim).
      */
-    vector<passivedouble> GetCoordinatesMarker(unsigned short iMarker) const;
+    vector<passivedouble> GetMarkerCoordinates(unsigned short iMarker, unsigned long iVertex) const;
     
     /*!
-     * \brief Set the coordinates of the mesh points.
-     * \param[in] values - Point coordinates (nPoint*nDim).
+     * \brief Set the coordinates of the mesh vertices.
+     * \param[in] values - Vertex coordinates (nPoint*nDim).
      */
     void SetCoordinates(vector<passivedouble> values);
     
     /*!
-     * \brief Set the coordinates of the mesh points on the specified marker.
-     * \param[in] iMarker - Marker identifier.
-     * \param[in] values - Point coordinates (nVertex*nDim).
+     * \brief Set the coordinates of a mesh vertex.
+     * \param[in] iPoint - Mesh vertex index.
+     * \param[in] values - Vertex coordinates (nDim).
+     */
+    void SetCoordinates(unsigned long iPoint, vector<passivedouble> values);
+    
+    /*!
+     * \brief Set the coordinates of the marker vertices.
+     * \param[in] iMarker - Marker index.
+     * \param[in] values - Vertex coordinates (nVertex*nDim).
+     */
+    void SetMarkerCoordinates(unsigned short iMarker, vector<passivedouble> values);
+    
+    /*!
+     * \brief Set the coordinates of a marker vertex.
+     * \param[in] iMarker - Marker index.
+     * \param[in] iVertex - Marker vertex index.
+     * \param[in] values - Vertex coordinates (nDim).
      */
-    void SetCoordinatesMarker(unsigned short iMarker, vector<passivedouble> values);
+    void SetMarkerCoordinates(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values);
     
     /*!
-     * \brief Get the vertex displacements on the specified marker.
-     * \param[in] iMarker - Marker identifier.
+     * \brief Get the displacements of the marker vertices.
+     * \param[in] iMarker - Marker index.
      * \return Vertex displacements (nVertex*nDim).
      */
-    vector<passivedouble> GetDisplacementsMarker(unsigned short iMarker) const;
+    vector<passivedouble> GetMarkerDisplacements(unsigned short iMarker) const;
     
     /*!
-     * \brief Set the vertex displacements on the specified marker.
-     * \param[in] iMarker - Marker identifier.
+     * \brief Get the displacements of a marker vertex.
+     * \param[in] iMarker - Marker index.
+     * \param[in] iVertex - Marker vertex index.
+     * \return Vertex displacements (nDim).
+     */
+    vector<passivedouble> GetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex) const;
+    
+    /*!
+     * \brief Set the displacements of the marker vertices.
+     * \param[in] iMarker - Marker index.
      * \param[in] values - Vertex displacements (nVertex*nDim).
      */
-    void SetDisplacementsMarker(unsigned short iMarker, vector<passivedouble> values);
+    void SetMarkerDisplacements(unsigned short iMarker, vector<passivedouble> values);
     
     /*!
-     * \brief Get the vertex velocities on the specified marker.
-     * \param[in] iMarker - Marker identifier.
+     * \brief Set the displacements of a marker vertex.
+     * \param[in] iMarker - Marker index.
+     * \param[in] iVertex - Marker vertex index.
+     * \param[in] values - Vertex displacements (nDim).
+     */
+    void SetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values);
+    
+    /*!
+     * \brief Get the velocities of the marker vertices.
+     * \param[in] iMarker - Marker index.
      * \return Vertex velocities (nVertex*nDim).
      */
-    vector<passivedouble> GetVelocitiesMarker(unsigned short iMarker) const;
+    vector<passivedouble> GetMarkerVelocities(unsigned short iMarker) const;
+
+    /*!
+     * \brief Get the velocities of a marker vertex.
+     * \param[in] iMarker - Marker index.
+     * \param[in] iVertex - Marker vertex index.
+     * \return Vertex velocities (nVertex*nDim).
+     */
+    vector<passivedouble> GetMarkerVelocities(unsigned short iMarker, unsigned long iVertex) const;
     
     /*!
-     * \brief Set the vertex velocities on the specified marker.
-     * \param[in] iMarker - Marker identifier.
+     * \brief Set the velocities of the marker vertices.
+     * \param[in] iMarker - Marker index.
      * \param[in] values - Vertex velocities (nVertex*nDim).
      */
-    void SetVelocitiesMarker(unsigned short iMarker, vector<passivedouble> values);
+    void SetMarkerVelocities(unsigned short iMarker, vector<passivedouble> values);
     
     /*!
-     * \brief Get undeformed coordinates from mesh solver on the specified marker.
-     * \param[in] iMarker - Marker identifier.
-     * \return Initial point coordinates (nVertex*nDim).
+     * \brief Set the velocities of a marker vertex.
+     * \param[in] iMarker - Marker index.
+     * \param[in] iVertex - Marker vertex index.
+     * \param[in] values - Vertex velocities (nDim).
      */
-    vector<passivedouble> GetInitialCoordinatesMarker(unsigned short iMarker) const;
+    void SetMarkerVelocities(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values);
     
     /*!
-     * \brief Get the vertex normal vectors on the specified marker.
-     * \param[in] iMarker - Marker identifier.
-     * \param[in] UnitNormal - Boolean to indicate if unit normal vector should be returned.
+     * \brief Get the normal vectors at the marker vertices.
+     * \param[in] iMarker - Marker index.
+     * \param[in] normalize - If true, the unit (i.e. normalized) normal vector is returned.
      * \return Normal vector at the vertex (nVertex*nDim).
      */
-    vector<passivedouble> GetVertexNormalsMarker(unsigned short iMarker, bool UnitNormal = false) const;
+    vector<passivedouble> GetMarkerVertexNormals(unsigned short iMarker, bool normalize = false) const;
+    
+    /*!
+     * \brief Get the normal vectors at a marker vertex.
+     * \param[in] iMarker - Marker index.
+     * \param[in] iVertex - Marker vertex index.
+     * \param[in] normalize - If true, the unit (i.e. normalized) normal vector is returned.
+     * \return Normal vector at the vertex (nDim).
+     */
+    vector<passivedouble> GetMarkerVertexNormals(unsigned short iMarker, unsigned long iVertex, bool normalize = false) const;
     
     /*!
      * \brief Communicate the boundary mesh displacements in a python call
diff --git a/Common/src/drivers/CDriverBase.cpp b/Common/src/drivers/CDriverBase.cpp
index 98d05d65305..9a3ee6ba686 100644
--- a/Common/src/drivers/CDriverBase.cpp
+++ b/Common/src/drivers/CDriverBase.cpp
@@ -82,78 +82,85 @@ void CDriverBase::SetContainers_Null() {
     driver_output         = nullptr;
 }
 
-map<string, int> CDriverBase::GetBoundaryMarkerIndices() const {
-    CConfig* config = config_container[ZONE_0];
-    
-    const auto nBoundaryMarkers = config->GetnMarker_All();
-    map<string, int>  allBoundariesMap;
+unsigned short CDriverBase::GetNumberMarkers() const {
+    return config_container[ZONE_0]->GetnMarker_All();
+}
+
+map<string, int> CDriverBase::GetMarkerIndices() const {
+    const auto nMarker = config_container[ZONE_0]->GetnMarker_All();
+    map<string, int> indexMap;
     
-    for (auto iMarker = 0u; iMarker < nBoundaryMarkers; iMarker++) {
-        auto Marker_Tag = config->GetMarker_All_TagBound(iMarker);
-        allBoundariesMap[Marker_Tag] = iMarker;
+    for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
+        auto tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
+
+        indexMap[tag] = iMarker;
     }
     
-    return allBoundariesMap;
+    return indexMap;
 }
 
-map<string, string> CDriverBase::GetBoundaryMarkerTypes() const {
-    CConfig* config = config_container[ZONE_0];
+map<string, string> CDriverBase::GetMarkerTypes() const {
+    map<string, string> typeMap;
+    string type;
     
-    map<string, string> allBoundariesTypeMap;
-    string Marker_Type;
-    
-    for (auto iMarker = 0u; iMarker < config->GetnMarker_All(); iMarker++) {
-        auto Marker_Tag = config->GetMarker_All_TagBound(iMarker);
-        auto KindBC = config->GetMarker_All_KindBC(iMarker);
+    for (auto iMarker = 0u; iMarker < config_container[ZONE_0]->GetnMarker_All(); iMarker++) {
+        auto tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
+        auto kindBC = config_container[ZONE_0]->GetMarker_All_KindBC(iMarker);
         
-        switch(KindBC) {
+        switch(kindBC) {
             case EULER_WALL:
-                Marker_Type = "EULER_WALL";
+                type = "EULER_WALL";
                 break;
             case FAR_FIELD:
-                Marker_Type = "FARFIELD";
+                type = "FARFIELD";
                 break;
             case ISOTHERMAL:
-                Marker_Type = "ISOTHERMAL";
+                type = "ISOTHERMAL";
                 break;
             case HEAT_FLUX:
-                Marker_Type = "HEATFLUX";
+                type = "HEATFLUX";
                 break;
             case INLET_FLOW:
-                Marker_Type = "INLET_FLOW";
+                type = "INLET_FLOW";
                 break;
             case OUTLET_FLOW:
-                Marker_Type = "OUTLET_FLOW";
+                type = "OUTLET_FLOW";
                 break;
             case SYMMETRY_PLANE:
-                Marker_Type = "SYMMETRY";
+                type = "SYMMETRY";
                 break;
             case SEND_RECEIVE:
-                Marker_Type = "SEND_RECEIVE";
+                type = "SEND_RECEIVE";
                 break;
             default:
-                Marker_Type = "UNKNOWN_TYPE";
+                type = "UNKNOWN_TYPE";
         }
-        allBoundariesTypeMap[Marker_Tag] = Marker_Type;
+        typeMap[tag] = type;
     }
     
-    return allBoundariesTypeMap;
+    return typeMap;
 }
 
-vector<string> CDriverBase::GetDeformableMarkerTags() const {
-    CConfig* config = config_container[ZONE_0];
+vector<string> CDriverBase::GetMarkerTags() const {
+    vector<string> tags;
+    const auto nMarker = config_container[ZONE_0]->GetnMarker_All();
     
-    const auto nBoundariesMarker = config->GetnMarker_Deform_Mesh();
-    vector<string> interfaceBoundariesTagList;
+    for(auto iMarker = 0u; iMarker < nMarker; iMarker++){
+        tags.push_back(config_container[ZONE_0]->GetMarker_All_TagBound(iMarker));
+    }
     
-    interfaceBoundariesTagList.resize(nBoundariesMarker);
+    return tags;
+}
+
+vector<string> CDriverBase::GetDeformableMarkerTags() const {
+    vector<string> tags;
+    const auto nMarker = config_container[ZONE_0]->GetnMarker_All();
     
-    for (auto iMarker = 0u; iMarker < nBoundariesMarker; iMarker++) {
-        auto Marker_Tag = config->GetMarker_Deform_Mesh_TagBound(iMarker);
-        interfaceBoundariesTagList[iMarker] = Marker_Tag;
+    for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
+        tags.push_back(config_container[ZONE_0]->GetMarker_Deform_Mesh_TagBound(iMarker));
     }
     
-    return interfaceBoundariesTagList;
+    return tags;
 }
 
 unsigned long CDriverBase::GetNumberDimensions() const {
@@ -164,26 +171,160 @@ unsigned long CDriverBase::GetNumberElements() const {
     return geometry_container[ZONE_0][INST_0][MESH_0]->GetnElem();
 }
 
-unsigned long CDriverBase::GetNumberElementsMarker(unsigned short iMarker) const {
+unsigned long CDriverBase::GetNumberMarkerElements(unsigned short iMarker) const {
+    if (iMarker >= GetNumberMarkers()) {
+        SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
+    }
+
     return geometry_container[ZONE_0][INST_0][MESH_0]->GetnElem_Bound(iMarker);
 }
 
+vector<unsigned long> CDriverBase::GetElementIDs() const {
+    vector<unsigned long> values;
+    const auto nElem = GetNumberElements();
+
+    for (auto iElem = 0ul; iElem < nElem; iElem++) {
+        values.push_back(GetElementIDs(iElem));
+    }
+    
+    return values;
+}
+
+unsigned long CDriverBase::GetElementIDs(unsigned long iElem) const {
+    if (iElem >= GetNumberElements()) {
+        SU2_MPI::Error("Element index exceeds size.", CURRENT_FUNCTION);
+    }
+
+    return geometry_container[ZONE_0][INST_0][MESH_0]->elem[iElem]->GetGlobalIndex();
+}
+
+vector<unsigned long> CDriverBase::GetMarkerElementIDs(unsigned short iMarker) const { 
+    vector<unsigned long> values;
+    const auto nBound = GetNumberMarkerElements(iMarker);
+
+    for (auto iBound = 0ul; iBound < nBound; iBound++) {
+        values.push_back(GetMarkerElementIDs(iMarker, iBound));
+    }
+    
+    return values;
+}
+
+unsigned long CDriverBase::GetMarkerElementIDs(unsigned short iMarker, unsigned long iBound) const {
+    if (iBound >= GetNumberMarkerElements(iMarker)) {
+        SU2_MPI::Error("Marker element index exceeds size.", CURRENT_FUNCTION);
+    }
+
+    return geometry_container[ZONE_0][INST_0][MESH_0]->bound[iMarker][iBound]->GetGlobalIndex();
+}
+
+vector<unsigned long> CDriverBase::GetElementColors() const {
+    vector<unsigned long> values;
+    const auto nElem = GetNumberElements();
+
+    for (auto iElem = 0ul; iElem < nElem; iElem++) {
+        values.push_back(GetElementColors(iElem));
+    }
+    
+    return values;
+}
+
+unsigned long CDriverBase::GetElementColors(unsigned long iElem) const {
+    if (iElem >= GetNumberElements()) {
+        SU2_MPI::Error("Element index exceeds size.", CURRENT_FUNCTION);
+    }
+    
+    return geometry_container[ZONE_0][INST_0][MESH_0]->elem[iElem]->GetColor();
+}
+
+vector<unsigned long> CDriverBase::GetMarkerElementColors(unsigned short iMarker) const {
+    vector<unsigned long> values;
+    const auto nBound = GetNumberMarkerElements(iMarker);
+
+    for (auto iBound = 0ul; iBound < nBound; iBound++) {
+        values.push_back(GetMarkerElementColors(iMarker, iBound));
+    }
+    
+    return values;
+}
+
+unsigned long CDriverBase::GetMarkerElementColors(unsigned short iMarker, unsigned long iBound) const {
+    if (iBound >= GetNumberMarkerElements(iMarker)) {
+        SU2_MPI::Error("Marker element index exceeds size.", CURRENT_FUNCTION);
+    }
+
+    return geometry_container[ZONE_0][INST_0][MESH_0]->bound[iMarker][iBound]->GetColor();
+}
+
+vector<vector<unsigned long>> CDriverBase::GetElementConnectivities() const {
+    vector<vector<unsigned long>> values;
+    const auto nElem = GetNumberElements();
+    
+    for (auto iElem = 0ul; iElem < nElem; iElem++) {
+        values.push_back(GetElementConnectivities(iElem));
+    }
+    
+    return values;
+}
+
+vector<unsigned long> CDriverBase::GetElementConnectivities(unsigned long iElem) const {
+    if (iElem >= GetNumberElements()) {
+        SU2_MPI::Error("Element index exceeds size.", CURRENT_FUNCTION);
+    }
+    
+    vector<unsigned long> values; 
+    unsigned short nNode = geometry_container[ZONE_0][INST_0][MESH_0]->elem[iElem]->GetnNodes();
+    
+    for (auto iNode = 0u; iNode < nNode; iNode++) {
+        values.push_back(geometry_container[ZONE_0][INST_0][MESH_0]->elem[iElem]->GetNode(iNode));
+    }
+    
+    return values;
+}
+
+vector<vector<unsigned long>> CDriverBase::GetMarkerElementConnectivities(unsigned short iMarker) const {
+    vector<vector<unsigned long>> values;
+    const auto nBound = GetNumberMarkerElements(iMarker);
+    
+    for (auto iBound = 0ul; iBound < nBound; iBound++) {
+        values.push_back(GetMarkerElementConnectivities(iMarker, iBound));
+    }
+    
+    return values;
+}
+
+vector<unsigned long> CDriverBase::GetMarkerElementConnectivities(unsigned short iMarker, unsigned long iBound) const {
+    if (iBound >= GetNumberMarkerElements(iMarker)) {
+        SU2_MPI::Error("Marker element index exceeds size.", CURRENT_FUNCTION);
+    }
+    
+    vector<unsigned long> values; 
+    unsigned short nNode = geometry_container[ZONE_0][INST_0][MESH_0]->bound[iMarker][iBound]->GetnNodes();
+    
+    for (auto iNode = 0u; iNode < nNode; iNode++) {
+        values.push_back(geometry_container[ZONE_0][INST_0][MESH_0]->bound[iMarker][iBound]->GetNode(iNode));
+    }
+    
+    return values;
+}
+
 unsigned long CDriverBase::GetNumberVertices() const {
     return geometry_container[ZONE_0][INST_0][MESH_0]->GetnPoint();
 }
 
-unsigned long CDriverBase::GetNumberVerticesMarker(unsigned short iMarker) const {
+unsigned long CDriverBase::GetNumberMarkerVertices(unsigned short iMarker) const {
+    if (iMarker >= GetNumberMarkers()) {
+        SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
+    }
+
     return geometry_container[ZONE_0][INST_0][MESH_0]->GetnVertex(iMarker);
 }
 
 unsigned long CDriverBase::GetNumberHaloVertices() const {
-    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-    
-    const auto nPoint = geometry->GetnPoint();
+    const auto nPoint = GetNumberVertices();
     unsigned long nHaloVertices = 0;
     
     for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
-        if (!(geometry->nodes->GetDomain(iPoint))) {
+        if (!(geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint))) {
             nHaloVertices += 1;
         }
     }
@@ -191,15 +332,14 @@ unsigned long CDriverBase::GetNumberHaloVertices() const {
     return nHaloVertices;
 }
 
-unsigned long CDriverBase::GetNumberHaloVerticesMarker(unsigned short iMarker) const {
-    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-    
-    const auto nVertex = geometry->GetnVertex(iMarker);
+unsigned long CDriverBase::GetNumberMarkerHaloVertices(unsigned short iMarker) const {
+    const auto nVertex = GetNumberMarkerVertices(iMarker);  // error-checking included
     unsigned long nHaloVertices = 0;
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
-        if (!(geometry->nodes->GetDomain(iPoint))) {
+        auto iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+        
+        if (!(geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint))) {
             nHaloVertices += 1;
         }
     }
@@ -207,338 +347,474 @@ unsigned long CDriverBase::GetNumberHaloVerticesMarker(unsigned short iMarker) c
     return nHaloVertices;
 }
 
-vector<unsigned long> CDriverBase::GetVertexIDs() const {
-    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+vector<unsigned long> CDriverBase::GetMarkerVertexIndex(unsigned short iMarker) const {
+    vector<unsigned long> values;
+    const auto nVertex = GetNumberMarkerVertices(iMarker);
+    
+    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+        values.push_back(GetMarkerVertexIndex(iMarker, iVertex));
+    }
+    
+    return values;
+}
+
+unsigned long CDriverBase::GetMarkerVertexIndex(unsigned short iMarker, unsigned long iVertex) const {
+    if (iVertex >= GetNumberMarkerVertices(iMarker)) {
+        SU2_MPI::Error("Marker vertex index exceeds size.", CURRENT_FUNCTION);
+    }
     
-    const auto nPoint = geometry->GetnPoint();
+    return geometry_container[MESH_0][INST_0][ZONE_0]->vertex[iMarker][iVertex]->GetNode();
+}
+
+vector<unsigned long> CDriverBase::GetVertexIDs() const {
     vector<unsigned long> values;
+    const auto nPoint = GetNumberVertices();
     
     for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
-        values.push_back(geometry->nodes->GetGlobalIndex(iPoint));
+        values.push_back(GetVertexIDs(iPoint));
     }
     
     return values;
 }
 
-vector<unsigned long> CDriverBase::GetVertexIDsMarker(unsigned short iMarker) const {
-    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-    
-    const auto nVertex = geometry->GetnVertex(iMarker);
+unsigned long CDriverBase::GetVertexIDs(unsigned long iPoint) const {
+    if (iPoint >= GetNumberVertices()) {
+        SU2_MPI::Error("Vertex index exceeds size.", CURRENT_FUNCTION);
+    }
+
+    return geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetGlobalIndex(iPoint);
+}
+
+vector<unsigned long> CDriverBase::GetMarkerVertexIDs(unsigned short iMarker) const {
     vector<unsigned long> values;
+    const auto nVertex = GetNumberMarkerVertices(iMarker); 
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
-        
-        values.push_back(geometry->nodes->GetGlobalIndex(iPoint));
+        values.push_back(GetMarkerVertexIDs(iMarker, iVertex));
     }
     
     return values;
 }
 
-vector<unsigned long> CDriverBase::GetElementIDs() const {
-    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-    
-    const auto nElem = geometry->GetnElem();
+unsigned long CDriverBase::GetMarkerVertexIDs(unsigned short iMarker, unsigned long iVertex) const {
+    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);  // includes error-checking
+
+    return geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetGlobalIndex(iPoint);
+}
+
+vector<unsigned long> CDriverBase::GetVertexColors() const {
     vector<unsigned long> values;
+    const auto nPoint = GetNumberVertices();
     
-    for (auto iElem = 0ul; iElem < nElem; iElem++) {
-        values.push_back(geometry->elem[iElem]->GetGlobalIndex());
+    for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
+        values.push_back(GetVertexColors(iPoint));
     }
     
     return values;
 }
 
-vector<unsigned long> CDriverBase::GetElementIDsMarker(unsigned short iMarker) const {
-    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-    
-    const auto nBound = geometry->GetnElem_Bound(iMarker);
+unsigned long CDriverBase::GetVertexColors(unsigned long iPoint) const {
+    if (iPoint >= GetNumberVertices()) {
+        SU2_MPI::Error("Vertex index exceeds size.", CURRENT_FUNCTION);
+    }
+
+    return geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetColor(iPoint);
+}
+
+vector<unsigned long> CDriverBase::GetMarkerVertexColors(unsigned short iMarker) const {
     vector<unsigned long> values;
+    const auto nVertex = GetNumberMarkerVertices(iMarker);
     
-    for (auto iBound = 0ul; iBound < nBound; iBound++) {
-        values.push_back(geometry->bound[iMarker][iBound]->GetGlobalIndex());
+    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+        values.push_back(GetMarkerVertexColors(iMarker, iVertex));
     }
     
     return values;
 }
 
-vector<vector<unsigned long>> CDriverBase::GetConnectivity() const {
-    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+unsigned long CDriverBase::GetMarkerVertexColors(unsigned short iMarker, unsigned long iVertex) const {
+    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);  // includes error-checking
     
-    const auto nElem = geometry->GetnElem();
-    vector<vector<unsigned long>> values(nElem);
+    return geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetColor(iPoint);
+}
+
+vector<bool> CDriverBase::GetDomain() const {
+    vector<bool> values;
+    const auto nPoint = GetNumberVertices();
     
-    for (auto iElem = 0ul; iElem < nElem; iElem++) {
-        unsigned short nNode = geometry->elem[iElem]->GetnNodes();
-        
-        for (auto iNode = 0u; iNode < nNode; iNode++) {
-            values[iElem].push_back(geometry->elem[iElem]->GetNode(iNode));
-        }
+    for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
+        values.push_back(GetDomain(iPoint));
     }
     
     return values;
 }
 
-vector<vector<unsigned long>> CDriverBase::GetConnectivityMarker(unsigned short iMarker) const {
-    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+bool CDriverBase::GetDomain(unsigned long iPoint) const {
+    if (iPoint >= GetNumberVertices()) {
+        SU2_MPI::Error("Vertex index exceeds size.", CURRENT_FUNCTION);
+    }
     
-    const auto nBound = geometry->GetnElem_Bound(iMarker);
-    vector<vector<unsigned long>> values(nBound);
+    return geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint);
+}
+
+vector<bool> CDriverBase::GetMarkerDomain(unsigned short iMarker) const {
+    vector<bool> values;
+    const auto nVertex = GetNumberMarkerVertices(iMarker);
     
-    for (auto iBound = 0ul; iBound < nBound; iBound++) {
-        unsigned short nNode = geometry->bound[iMarker][iBound]->GetnNodes();
-        
-        for (auto iNode = 0u; iNode < nNode; iNode++) {
-            values[iBound].push_back(geometry->bound[iMarker][iBound]->GetNode(iNode));
-        }
+    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+        values.push_back(GetMarkerDomain(iMarker, iVertex));
     }
     
     return values;
 }
 
-vector<bool> CDriverBase::GetDomain() const {
-    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+bool CDriverBase::GetMarkerDomain(unsigned short iMarker, unsigned long iVertex) const {
+    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
     
-    const auto nPoint = geometry->GetnPoint();
-    vector<bool> values;
+    return geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint);
+}
+
+vector<passivedouble> CDriverBase::GetInitialCoordinates() const {
+    const auto nPoint = GetNumberVertices();
+    vector<passivedouble> values;
     
     for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
-        values.push_back(geometry->nodes->GetDomain(iPoint));
+        const auto value = GetInitialCoordinates(iPoint);
+        
+        for (auto iDim = 0u; iDim < nDim; iDim++) {
+            values.push_back(value[iDim]);
+        }
     }
     
     return values;
 }
 
-vector<bool> CDriverBase::GetDomainMarker(unsigned short iMarker) const {
-    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+vector<passivedouble> CDriverBase::GetInitialCoordinates(unsigned long iPoint) const {
+    if (iPoint >= GetNumberVertices()) {
+        SU2_MPI::Error("Vertex index exceeds size.", CURRENT_FUNCTION);
+    }
+
+    vector<passivedouble> values;
+
+    for (auto iDim = 0u; iDim < nDim; iDim++) {
+        const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord(iPoint, iDim);
+
+        if (!config_container[ZONE_0]->GetDeform_Mesh()) {
+            values.push_back(0.0);  // mesh solver is not defined !
+        }
+        else {
+            values.push_back(SU2_TYPE::GetValue(value));
+        }
+    }
     
-    const auto nVertex = geometry->GetnVertex(iMarker);
-    vector<bool> values;
+    return values;
+}
+
+vector<passivedouble> CDriverBase::GetMarkerInitialCoordinates(unsigned short iMarker) const {
+    const auto nVertex = GetNumberMarkerVertices(iMarker);
+    vector<passivedouble> values;
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+        const auto value = GetMarkerInitialCoordinates(iVertex);
         
-        values.push_back(geometry->nodes->GetDomain(iPoint));
+        for (auto iDim = 0u; iDim < nDim; iDim++) {
+            values.push_back(value[iDim]);
+        }
     }
     
     return values;
 }
 
-vector<passivedouble> CDriverBase::GetCoordinates() const {
-    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+vector<passivedouble> CDriverBase::GetMarkerInitialCoordinates(unsigned short iMarker, unsigned long iVertex) const {
+    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+    vector<passivedouble> values;
+
+    for (auto iDim = 0u; iDim < nDim; iDim++) {
+        const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord(iPoint, iDim);
+
+        if (!config_container[ZONE_0]->GetDeform_Mesh()) {
+            values.push_back(0.0);  // mesh solver is not defined !
+        }
+        else {
+            values.push_back(SU2_TYPE::GetValue(value));
+        }
+    }
     
-    const auto nPoint = geometry->GetnPoint();
-    vector<passivedouble> values(nPoint*nDim, 0.0);
-    su2double value;
+    return values;
+}
+
+vector<passivedouble> CDriverBase::GetCoordinates() const {
+    const auto nPoint = GetNumberVertices();
+    vector<passivedouble> values;
     
     for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
+        const auto value = GetCoordinates(iPoint);
+        
         for (auto iDim = 0u; iDim < nDim; iDim++) {
-            value = geometry->nodes->GetCoord(iPoint, iDim);
-            values[iPoint*nDim + iDim] = SU2_TYPE::GetValue(value);
+            values.push_back(value[iDim]);
         }
     }
     
     return values;
 }
 
-vector<passivedouble> CDriverBase::GetCoordinatesMarker(unsigned short iMarker) const {
-    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+vector<passivedouble> CDriverBase::GetCoordinates(unsigned long iPoint) const {
+    const auto nPoint = GetNumberVertices();
+    vector<passivedouble> values;
+    
+    for (auto iDim = 0u; iDim < nDim; iDim++) {
+        const su2double value = geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetCoord(iPoint, iDim);
+        
+        values.push_back(SU2_TYPE::GetValue(value));
+    }
     
-    const auto nVertex = geometry->GetnVertex(iMarker);
-    vector<passivedouble> values(nVertex*nDim, 0.0);
-    su2double value;
+    return values;
+}
+
+vector<passivedouble> CDriverBase::GetMarkerCoordinates(unsigned short iMarker) const {
+    const auto nVertex = GetNumberMarkerVertices(iMarker);
+    vector<passivedouble> values;
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+        const auto value = GetMarkerCoordinates(iVertex);
         
         for (auto iDim = 0u; iDim < nDim; iDim++) {
-            value = geometry->nodes->GetCoord(iPoint, iDim);
-            values[iVertex*nDim + iDim] = SU2_TYPE::GetValue(value);
+            values.push_back(value[iDim]);
         }
     }
     
     return values;
 }
 
+vector<passivedouble> CDriverBase::GetMarkerCoordinates(unsigned short iMarker, unsigned long iVertex) const {
+    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+    vector<passivedouble> values;
+    
+    for (auto iDim = 0u; iDim < nDim; iDim++) {
+        const su2double value = geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetCoord(iPoint, iDim);
+        
+        values.push_back(SU2_TYPE::GetValue(value));
+    }
+    
+    return values;
+}
+
 void CDriverBase::SetCoordinates(vector<passivedouble> values) {
-    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    const auto nPoint = GetNumberVertices();
     
-    const auto nPoint = geometry->GetnPoint();
     if (values.size() != nPoint*nDim) {
         SU2_MPI::Error("Size does not match nPoint * nDim!", CURRENT_FUNCTION);
     }
     
     for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
         for (auto iDim = 0u; iDim < nDim; iDim++) {
-            geometry->nodes->SetCoord(iPoint, iDim, values[iPoint*nDim + iDim]);
+            geometry_container[ZONE_0][INST_0][MESH_0]->nodes->SetCoord(iPoint, iDim, values[iPoint*nDim + iDim]);
         }
     }
 }
 
-void CDriverBase::SetCoordinatesMarker(unsigned short iMarker, vector<passivedouble> values) {
-    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+void CDriverBase::SetCoordinates(unsigned long iPoint, vector<passivedouble> values) {
+    if (values.size() != nDim) {
+        SU2_MPI::Error("Size does not match nDim!", CURRENT_FUNCTION);
+    }
     
-    const auto nVertex = geometry->GetnVertex(iMarker);
+    for (auto iDim = 0u; iDim < nDim; iDim++) {
+        geometry_container[ZONE_0][INST_0][MESH_0]->nodes->SetCoord(iPoint, iDim, values[iDim]);
+    }
+}
+
+void CDriverBase::SetMarkerCoordinates(unsigned short iMarker, vector<passivedouble> values) {
+    const auto nVertex = GetNumberMarkerVertices(iMarker);
+
     if (values.size() != nVertex*nDim) {
         SU2_MPI::Error("Size does not match nVertex * nDim!", CURRENT_FUNCTION);
     }
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+        auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
         
         for (auto iDim = 0u; iDim < nDim; iDim++) {
-            geometry->nodes->SetCoord(iPoint, iDim, values[iVertex*nDim + iDim]);
+            geometry_container[ZONE_0][INST_0][MESH_0]->nodes->SetCoord(iPoint, iDim, values[iVertex*nDim + iDim]);
         }
     }
 }
 
-vector<passivedouble> CDriverBase::GetDisplacementsMarker(unsigned short iMarker) const {
-    CConfig* config     = config_container[ZONE_0];
-    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-    CSolver* solver     = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL];
-    
-    if (!config->GetDeform_Mesh()) {
-        return {};
+void CDriverBase::SetMarkerCoordinates(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
+    if (values.size() != nDim) {
+        SU2_MPI::Error("Size does not match nDim!", CURRENT_FUNCTION);
     }
     
-    const auto nVertex = geometry->GetnVertex(iMarker);
-    vector<passivedouble> values(nVertex*nDim, 0.0);
-    su2double value;
+    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+    
+    for (auto iDim = 0u; iDim < nDim; iDim++) {
+        geometry_container[ZONE_0][INST_0][MESH_0]->nodes->SetCoord(iPoint, iDim, values[iDim]);
+    }
+}
+
+vector<passivedouble> CDriverBase::GetMarkerDisplacements(unsigned short iMarker) const {
+    const auto nVertex = GetNumberMarkerVertices(iMarker);
+    vector<passivedouble> values;
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+        const auto value = GetMarkerDisplacements(iMarker, iVertex);
         
         for (auto iDim = 0u; iDim < nDim; iDim++) {
-            value = solver->GetNodes()->GetBound_Disp(iPoint, iDim);
-            values[iVertex*nDim + iDim] = SU2_TYPE::GetValue(value);
+            values.push_back(values[iDim]);
         }
     }
     
     return values;
 }
 
-void CDriverBase::SetDisplacementsMarker(unsigned short iMarker, vector<passivedouble> values) {
-    CConfig* config     = config_container[ZONE_0];
-    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-    CSolver* solver     = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL];
+vector<passivedouble> CDriverBase::GetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex) const {
+    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+    vector<passivedouble> values;
     
-    if (!config->GetDeform_Mesh()) {
-        SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
+    for (auto iDim = 0u; iDim < nDim; iDim++) {
+        const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetBound_Disp(iPoint, iDim);
+
+        values.push_back(SU2_TYPE::GetValue(value));
     }
     
-    const auto nVertex = geometry->GetnVertex(iMarker);
+    return values;
+}
+
+void CDriverBase::SetMarkerDisplacements(unsigned short iMarker, vector<passivedouble> values) {
+    if (!config_container[ZONE_0]->GetDeform_Mesh()) {
+        SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
+    }
+
+    const auto nVertex = GetNumberMarkerVertices(iMarker);
+
     if (values.size() != nVertex*nDim) {
         SU2_MPI::Error("Size does not match nVertex * nDim!", CURRENT_FUNCTION);
     }
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+        auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
         
         for (auto iDim = 0u; iDim < nDim; iDim++) {
-            solver->GetNodes()->SetBound_Disp(iPoint, iDim, values[iVertex*nDim + iDim]);
+            solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->SetBound_Disp(iPoint, iDim, values[iVertex*nDim + iDim]);
         }
     }
 }
 
-vector<passivedouble> CDriverBase::GetVelocitiesMarker(unsigned short iMarker) const {
-    CConfig* config     = config_container[ZONE_0];
-    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-    CSolver* solver     = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL];
-    
-    if (!config->GetDeform_Mesh()) {
-        return {};
+void CDriverBase::SetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
+    if (!config_container[ZONE_0]->GetDeform_Mesh()) {
+        SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
+    }
+    if (values.size() != nDim) {
+        SU2_MPI::Error("Size does not match nDim!", CURRENT_FUNCTION);
     }
     
-    const auto nVertex = geometry->GetnVertex(iMarker);
-    vector<passivedouble> values(nVertex*nDim, 0.0);
-    su2double value;
+    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+    
+    for (auto iDim = 0u; iDim < nDim; iDim++) {
+        solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->SetBound_Disp(iPoint, iDim, values[iDim]);
+    }
+}
+
+vector<passivedouble> CDriverBase::GetMarkerVelocities(unsigned short iMarker) const {
+    const auto nVertex = GetNumberMarkerVertices(iMarker);
+    vector<passivedouble> values;
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+        const auto value = GetMarkerVelocities(iMarker, iVertex);
         
         for (auto iDim = 0u; iDim < nDim; iDim++) {
-            value = solver->GetNodes()->GetBound_Vel(iPoint, iDim);
-            values[iVertex*nDim + iDim] = SU2_TYPE::GetValue(value);
+            values.push_back(values[iDim]);
         }
     }
     
     return values;
 }
 
-void CDriverBase::SetVelocitiesMarker(unsigned short iMarker, vector<passivedouble> values) {
-    CConfig* config     = config_container[ZONE_0];
-    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-    CSolver* solver     = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL];
+vector<passivedouble> CDriverBase::GetMarkerVelocities(unsigned short iMarker, unsigned long iVertex) const {
+    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+    vector<passivedouble> values;
     
-    if (!config->GetDeform_Mesh()) {
-        SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
+    for (auto iDim = 0u; iDim < nDim; iDim++) {
+        const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetBound_Vel(iPoint, iDim);
+
+        values.push_back(SU2_TYPE::GetValue(value));
     }
     
-    const auto nVertex = geometry->GetnVertex(iMarker);
+    return values;
+}
+
+void CDriverBase::SetMarkerVelocities(unsigned short iMarker, vector<passivedouble> values) {
+    if (!config_container[ZONE_0]->GetDeform_Mesh()) {
+        SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
+    }
+
+    const auto nVertex = GetNumberMarkerVertices(iMarker);
+
     if (values.size() != nVertex*nDim) {
         SU2_MPI::Error("Size does not match nVertex * nDim!", CURRENT_FUNCTION);
     }
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+        auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
         
         for (auto iDim = 0u; iDim < nDim; iDim++) {
-            solver->GetNodes()->SetBound_Vel(iPoint, iDim, values[iVertex*nDim + iDim]);
+            solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->SetBound_Disp(iPoint, iDim, values[iVertex*nDim + iDim]);
         }
     }
 }
 
-vector<passivedouble> CDriverBase::GetInitialCoordinatesMarker(unsigned short iMarker) const {
-    CConfig* config     = config_container[ZONE_0];
-    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-    CSolver* solver     = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL];
-    
-    if (!config->GetDeform_Mesh()) {
-        return {};
+void CDriverBase::SetMarkerVelocities(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
+    if (!config_container[ZONE_0]->GetDeform_Mesh()) {
+        SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
+    }
+    if (values.size() != nDim) {
+        SU2_MPI::Error("Size does not match nDim!", CURRENT_FUNCTION);
     }
     
-    const auto nVertex = geometry->GetnVertex(iMarker);
-    vector<passivedouble> values(nVertex*nDim, 0.0);
-    su2double value;
+    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+    
+    for (auto iDim = 0u; iDim < nDim; iDim++) {
+        solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->SetBound_Disp(iPoint, iDim, values[iDim]);
+    }
+}
+
+vector<passivedouble> CDriverBase::GetMarkerVertexNormals(unsigned short iMarker, bool normalize) const {
+    const auto nVertex = GetNumberMarkerVertices(iMarker);
+    vector<passivedouble> values;
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+        const auto value = GetMarkerVertexNormals(iMarker, normalize=normalize);
         
         for (auto iDim = 0u; iDim < nDim; iDim++) {
-            value = solver->GetNodes()->GetMesh_Coord(iPoint, iDim);
-            values[iVertex*nDim + iDim] = SU2_TYPE::GetValue(value);
+            values.push_back(value[iDim]);
         }
     }
     
     return values;
 }
 
-vector<passivedouble> CDriverBase::GetVertexNormalsMarker(unsigned short iMarker, bool UnitNormal) const {
-    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-    
-    const auto nVertex = geometry->GetnVertex(iMarker);
-    vector<passivedouble> values(nVertex*nDim, 0.0);
+vector<passivedouble> CDriverBase::GetMarkerVertexNormals(unsigned short iMarker, unsigned long iVertex, bool normalize) const {
+    if (iVertex >= GetNumberMarkerVertices(iMarker)) {
+        SU2_MPI::Error("Marker vertex index exceeds size.", CURRENT_FUNCTION);
+    }
+
+    vector<passivedouble> values;
+
+    auto normal = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNormal();
+    auto area   = GeometryToolbox::Norm(nDim, normal);
     
-    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        auto Normal = geometry->vertex[iMarker][iVertex]->GetNormal();
-        auto Area   = GeometryToolbox::Norm(nDim, Normal);
-        
-        for (auto iDim = 0u; iDim < nDim; iDim++) {
-            if (!UnitNormal) {
-                values[iVertex*nDim + iDim] = SU2_TYPE::GetValue(Normal[iDim]);
-            } else {
-                values[iVertex*nDim + iDim] = SU2_TYPE::GetValue(Normal[iDim]/Area);
-            }
+    for (auto iDim = 0u; iDim < nDim; iDim++) {
+        if (normalize) {
+            values[iDim] = SU2_TYPE::GetValue(normal[iDim]/area);
+        } else {
+            values[iDim] = SU2_TYPE::GetValue(normal[iDim]);
         }
     }
-    
+
     return values;
 }
 
+
 void CDriverBase::CommunicateMeshDisplacements(void) {
-    CConfig* config     = config_container[ZONE_0];
-    CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-    CSolver* solver     = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL];
-    
-    solver->InitiateComms(geometry, config, MESH_DISPLACEMENTS);
-    solver->CompleteComms(geometry, config, MESH_DISPLACEMENTS);
+    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->InitiateComms(geometry_container[ZONE_0][INST_0][MESH_0], config_container[ZONE_0], MESH_DISPLACEMENTS);
+    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->CompleteComms(geometry_container[ZONE_0][INST_0][MESH_0], config_container[ZONE_0], MESH_DISPLACEMENTS);
 }
diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index 32843db8c50..d15a510cae4 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -490,22 +490,16 @@ class CDriver : public CDriverBase {
     void Inlet_Preprocessing(CSolver ***solver, CGeometry **geometry, CConfig *config) const;
     
     /*!
-     * \brief Get all the boundary markers tags.
-     * \return List of boundary markers tags.
+     * \brief Get all the CHT boundary marker tags.
+     * \return List of CHT boundary markers tags.
      */
-    vector<string> GetAllBoundaryMarkersTag() const;
+    vector<string> GetCHTMarkerTags() const;
     
     /*!
-     * \brief Get all the heat transfer boundary markers tags.
-     * \return List of heat transfer boundary markers tags.
-     */
-    vector<string> GetAllCHTMarkersTag() const;
-    
-    /*!
-     * \brief Get all the (subsonic) inlet boundary markers tags.
+     * \brief Get all the inlet boundary marker tags.
      * \return List of inlet boundary markers tags.
      */
-    vector<string> GetAllInletMarkersTag() const;
+    vector<string> GetInletMarkerTags() const;
     
     /*!
      * \brief Return the sensitivities of the mesh boundary vertices.
diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index ba6a563c5b0..2f7e35a1247 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -320,60 +320,36 @@ passivedouble CDriver::GetThermalConductivity(unsigned short iMarker, unsigned l
 /* Functions related to the management of markers                             */
 ////////////////////////////////////////////////////////////////////////////////
 
-vector<string> CDriver::GetAllBoundaryMarkersTag() const {
-    
-    vector<string> boundariesTagList;
-    unsigned short iMarker,nBoundariesMarkers;
-    string Marker_Tag;
-    
-    nBoundariesMarkers = config_container[ZONE_0]->GetnMarker_All();
-    boundariesTagList.resize(nBoundariesMarkers);
-    
-    for(iMarker=0; iMarker < nBoundariesMarkers; iMarker++){
-        Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
-        boundariesTagList[iMarker] = Marker_Tag;
-    }
-    
-    return boundariesTagList;
-}
-
-vector<string> CDriver::GetAllCHTMarkersTag() const {
-    
-    vector<string> CHTBoundariesTagList;
-    unsigned short iMarker, nBoundariesMarker;
-    string Marker_Tag;
-    
-    nBoundariesMarker = config_container[ZONE_0]->GetnMarker_All();
+vector<string> CDriver::GetCHTMarkerTags() const {
+    vector<string> tags;
+    const auto nMarker = config_container[ZONE_0]->GetnMarker_All();
     
     //The CHT markers can be identified as the markers that are customizable with a BC type HEAT_FLUX or ISOTHERMAL.
-    for(iMarker=0; iMarker<nBoundariesMarker; iMarker++){
-        if((config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == HEAT_FLUX || config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == ISOTHERMAL) && config_container[ZONE_0]->GetMarker_All_PyCustom(iMarker)){
-            Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
-            CHTBoundariesTagList.push_back(Marker_Tag);
+    for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
+        if ((config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == HEAT_FLUX || 
+             config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == ISOTHERMAL) && config_container[ZONE_0]->GetMarker_All_PyCustom(iMarker)){
+            
+            tags.push_back(config_container[ZONE_0]->GetMarker_All_TagBound(iMarker));
         }
     }
     
-    return CHTBoundariesTagList;
+    return tags;
 }
 
-vector<string> CDriver::GetAllInletMarkersTag() const {
+vector<string> CDriver::GetInletMarkerTags() const {
+    vector<string> tags;
+    const auto nMarker = config_container[ZONE_0]->GetnMarker_All();
     
-    vector<string> BoundariesTagList;
-    unsigned short iMarker, nBoundariesMarker;
-    string Marker_Tag;
-    
-    nBoundariesMarker = config_container[ZONE_0]->GetnMarker_All();
-    
-    for(iMarker=0; iMarker<nBoundariesMarker; iMarker++){
+    for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
         bool isCustomizable = config_container[ZONE_0]->GetMarker_All_PyCustom(iMarker);
         bool isInlet = (config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == INLET_FLOW);
-        if(isCustomizable && isInlet) {
-            Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
-            BoundariesTagList.push_back(Marker_Tag);
+        
+        if (isCustomizable && isInlet) {
+            tags.push_back(config_container[ZONE_0]->GetMarker_All_TagBound(iMarker));
         }
     }
     
-    return BoundariesTagList;
+    return tags;
 }
 
 void CDriver::SetHeatSource_Position(passivedouble alpha, passivedouble pos_x, passivedouble pos_y, passivedouble pos_z){
diff --git a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
index 89006b9a53a..a962558d0d6 100755
--- a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
@@ -68,10 +68,10 @@ def main():
   MarkerName = 'RightBeamS'       # Specified by the user
 
   # Get all the boundary tags
-  MarkerList = SU2Driver.GetAllBoundaryMarkersTag()
+  MarkerList = SU2Driver.GetMarkerTags()
 
   # Get all the markers defined on this rank and their associated indices.
-  allMarkerIDs = SU2Driver.GetBoundaryMarkerIndices()
+  allMarkerIDs = SU2Driver.GetMarkerIndices()
 
   #Check if the specified marker exists and if it belongs to this rank.
   if MarkerName in MarkerList and MarkerName in allMarkerIDs.keys():
diff --git a/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
index 2229ad8ce5c..d174d13da12 100755
--- a/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
@@ -67,12 +67,12 @@ def main():
   MarkerName = 'wallF'       # Specified by the user
 
   # Get all the boundary tags
-  MarkerList = SU2Driver.GetAllBoundaryMarkersTag()
+  MarkerList = SU2Driver.GetMarkerTags()
 
   # Get all the markers defined on this rank and their associated indices.
-  allMarkerIDs = SU2Driver.GetBoundaryMarkerIndices()
+  allMarkerIDs = SU2Driver.GetMarkerIndices()
 
-  #Check if the specified marker exists and if it belongs to this rank.
+  # Check if the specified marker exists and if it belongs to this rank.
   if MarkerName in MarkerList and MarkerName in allMarkerIDs.keys():
     MarkerID = allMarkerIDs[MarkerName]
 
@@ -80,7 +80,7 @@ def main():
   nVertex_Marker = 0         #total number of vertices (physical + halo)
 
   if MarkerID != None:
-    nVertex_Marker = SU2Driver.GetNumberVerticesMarker(MarkerID)
+    nVertex_Marker = SU2Driver.GetNumberMarkerVertices(MarkerID)
 
   # Time loop is defined in Python so that we have acces to SU2 functionalities at each time step
   if rank == 0:
diff --git a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
index ea7983e2156..691f5b134c5 100755
--- a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
+++ b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
@@ -76,10 +76,10 @@ def main():
   MovingMarker = 'plate'       #specified by the user
 
   # Get all the tags with the moving option
-  MovingMarkerList =  SU2Driver.GetAllDeformMeshMarkersTag()
+  MovingMarkerList =  SU2Driver.GetMarkerTags()
 
   # Get all the markers defined on this rank and their associated indices.
-  allMarkerIDs = SU2Driver.GetAllBoundaryMarkers()
+  allMarkerIDs = SU2Driver.GetMarkerIndices()
 
   # Check if the specified marker has a moving option and if it exists on this rank.
   if MovingMarker in MovingMarkerList and MovingMarker in allMarkerIDs.keys():
@@ -91,8 +91,8 @@ def main():
   nVertex_MovingMarker_PHYS = 0    #number of physical vertices
 
   if MovingMarkerID != None:
-    nVertex_MovingMarker = SU2Driver.GetNumberVertices(MovingMarkerID)
-    nVertex_MovingMarker_HALO = SU2Driver.GetNumberHaloVertices(MovingMarkerID)
+    nVertex_MovingMarker = SU2Driver.GetNumberMarkerVertices(MovingMarkerID)
+    nVertex_MovingMarker_HALO = SU2Driver.GetNumberMarkerHaloVertices(MovingMarkerID)
     nVertex_MovingMarker_PHYS = nVertex_MovingMarker - nVertex_MovingMarker_HALO
 
   # Retrieve some control parameters from the driver
@@ -104,9 +104,8 @@ def main():
   # Extract the initial position of each node on the moving marker
   CoordX = np.zeros(nVertex_MovingMarker)
   CoordY = np.zeros(nVertex_MovingMarker)
-  CoordZ = np.zeros(nVertex_MovingMarker)
   for iVertex in range(nVertex_MovingMarker):
-    CoordX[iVertex], CoordY[iVertex], CoordZ[iVertex] = SU2Driver.GetInitialMeshCoord(MovingMarkerID, iVertex)
+    CoordX[iVertex], CoordY[iVertex] = SU2Driver.GetMarkerInitialCoordinates(MovingMarkerID, iVertex)
 
   # Time loop is defined in Python so that we have acces to SU2 functionalities at each time step
   if rank == 0:
@@ -117,9 +116,11 @@ def main():
 
   while (TimeIter < nTimeIter):
     # Define the rigid body displacement and set the new coords of each node on the marker
-    d_y = 0.0175*sin(2*pi*time)
+    value = 0.0, 0.0175*sin(2*pi*time)
+
     for iVertex in range(nVertex_MovingMarker):
-      SU2Driver.SetMeshDisplacement(MovingMarkerID, int(iVertex), 0.0, d_y, 0.0)
+      SU2Driver.SetMarkerDisplacements(MovingMarkerID, int(iVertex), value)
+
     # Time iteration preprocessing
     SU2Driver.Preprocess(TimeIter)
     # Run one time iteration (e.g. dual-time)
diff --git a/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py b/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
index dfde1d6b2c8..d63bb335442 100755
--- a/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
+++ b/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
@@ -75,23 +75,23 @@ def main():
   CHTMarker = 'plate'       # Specified by the user
 
   # Get all the tags with the CHT option
-  CHTMarkerList =  SU2Driver.GetAllCHTMarkersTag()
+  CHTMarkerList =  SU2Driver.GetCHTMarkerTags()
 
   # Get all the markers defined on this rank and their associated indices.
-  allMarkerIDs = SU2Driver.GetAllBoundaryMarkers()
+  allMarkerIDs = SU2Driver.GetMarkerIndices()
 
   #Check if the specified marker has a CHT option and if it exists on this rank.
   if CHTMarker in CHTMarkerList and CHTMarker in allMarkerIDs.keys():
     CHTMarkerID = allMarkerIDs[CHTMarker]
 
   # Number of vertices on the specified marker (per rank)
-  nVertex_CHTMarker = 0         #total number of vertices (physical + halo)
-  nVertex_CHTMarker_HALO = 0    #number of halo vertices
-  nVertex_CHTMarker_PHYS = 0    #number of physical vertices
+  nVertex_CHTMarker = 0         # total number of vertices (physical + halo)
+  nVertex_CHTMarker_HALO = 0    # number of halo vertices
+  nVertex_CHTMarker_PHYS = 0    # number of physical vertices
 
   if CHTMarkerID != None:
-    nVertex_CHTMarker = SU2Driver.GetNumberVertices(CHTMarkerID)
-    nVertex_CHTMarker_HALO = SU2Driver.GetNumberHaloVertices(CHTMarkerID)
+    nVertex_CHTMarker = SU2Driver.GetNumberMarkerVertices(CHTMarkerID)
+    nVertex_CHTMarker_HALO = SU2Driver.GetNumberMarkerHaloVertices(CHTMarkerID)
     nVertex_CHTMarker_PHYS = nVertex_CHTMarker - nVertex_CHTMarker_HALO
 
   # Retrieve some control parameters from the driver
@@ -115,6 +115,7 @@ def main():
     # Set this temperature to all the vertices on the specified CHT marker
     for iVertex in range(nVertex_CHTMarker):
       SU2Driver.SetVertexTemperature(CHTMarkerID, iVertex, WallTemp)
+
     # Tell the SU2 drive to update the boundary conditions
     SU2Driver.BoundaryConditionsUpdate()
     # Run one time iteration (e.g. dual-time)

From fad776d390fea1ef7f6e3f28ca7c9c3eeb462885 Mon Sep 17 00:00:00 2001
From: aa-g <aa.gastaldi@pm.me>
Date: Mon, 7 Mar 2022 21:20:05 +0100
Subject: [PATCH 023/656] Adapt Python API to get/set from multi-dimensional
 arrays

---
 Common/include/drivers/CDriverBase.hpp |  48 +++---
 Common/src/drivers/CDriverBase.cpp     | 229 +++++++++++++------------
 SU2_PY/pySU2/pySU2.i                   |   4 +-
 SU2_PY/pySU2/pySU2ad.i                 |   4 +-
 4 files changed, 144 insertions(+), 141 deletions(-)

diff --git a/Common/include/drivers/CDriverBase.hpp b/Common/include/drivers/CDriverBase.hpp
index 6b9590fdd22..68aa0bd5956 100644
--- a/Common/include/drivers/CDriverBase.hpp
+++ b/Common/include/drivers/CDriverBase.hpp
@@ -121,7 +121,7 @@ class CDriverBase {
      * \brief Get all the boundary markers tags with their associated indices.
      * \return List of boundary markers tags with their indices.
      */
-    map<string, int> GetMarkerIndices() const;
+    map<string, unsigned short> GetMarkerIndices() const;
     
     /*!
      * \brief Get all the boundary markers tags with their associated types.
@@ -371,9 +371,9 @@ class CDriverBase {
     
     /*!
      * \brief Get the initial (un-deformed) coordinates of the mesh vertices.
-     * \return Initial vertex coordinates (nPoint*nDim).
+     * \return Initial vertex coordinates (nPoint, nDim).
      */
-    vector<passivedouble> GetInitialCoordinates() const;
+    vector<vector<passivedouble>> GetInitialCoordinates() const;
 
     /*!
      * \brief Get the initial (un-deformed) coordinates of a mesh vertex.
@@ -385,9 +385,9 @@ class CDriverBase {
     /*!
      * \brief Get the initial (un-deformed) coordinates of the marker vertices.
      * \param[in] iMarker - Marker index.
-     * \return Initial vertex coordinates (nVertex*nDim).
+     * \return Initial vertex coordinates (nVertex, nDim).
      */
-    vector<passivedouble> GetMarkerInitialCoordinates(unsigned short iMarker) const;
+    vector<vector<passivedouble>> GetMarkerInitialCoordinates(unsigned short iMarker) const;
     
     /*!
      * \brief Get the initial (un-deformed) coordinates of a marker vertex.
@@ -399,9 +399,9 @@ class CDriverBase {
     
     /*!
      * \brief Get the coordinates of the mesh vertices.
-     * \return Vertex coordinates (nPoint*nDim).
+     * \return Vertex coordinates (nPoint, nDim).
      */
-    vector<passivedouble> GetCoordinates() const;
+    vector<vector<passivedouble>> GetCoordinates() const;
 
     /*!
      * \brief Get the coordinates of a mesh vertex.
@@ -413,9 +413,9 @@ class CDriverBase {
     /*!
      * \brief Get the coordinates of the marker vertices.
      * \param[in] iMarker - Marker index.
-     * \return Vertex coordinates (nVertex*nDim).
+     * \return Vertex coordinates (nVertex, nDim).
      */
-    vector<passivedouble> GetMarkerCoordinates(unsigned short iMarker) const;
+    vector<vector<passivedouble>> GetMarkerCoordinates(unsigned short iMarker) const;
     
     /*!
      * \brief Get the coordinates of a marker vertex.
@@ -427,9 +427,9 @@ class CDriverBase {
     
     /*!
      * \brief Set the coordinates of the mesh vertices.
-     * \param[in] values - Vertex coordinates (nPoint*nDim).
+     * \param[in] values - Vertex coordinates (nPoint, nDim).
      */
-    void SetCoordinates(vector<passivedouble> values);
+    void SetCoordinates(vector<vector<passivedouble>> values);
     
     /*!
      * \brief Set the coordinates of a mesh vertex.
@@ -441,9 +441,9 @@ class CDriverBase {
     /*!
      * \brief Set the coordinates of the marker vertices.
      * \param[in] iMarker - Marker index.
-     * \param[in] values - Vertex coordinates (nVertex*nDim).
+     * \param[in] values - Vertex coordinates (nVertex, nDim).
      */
-    void SetMarkerCoordinates(unsigned short iMarker, vector<passivedouble> values);
+    void SetMarkerCoordinates(unsigned short iMarker, vector<vector<passivedouble>> values);
     
     /*!
      * \brief Set the coordinates of a marker vertex.
@@ -456,9 +456,9 @@ class CDriverBase {
     /*!
      * \brief Get the displacements of the marker vertices.
      * \param[in] iMarker - Marker index.
-     * \return Vertex displacements (nVertex*nDim).
+     * \return Vertex displacements (nVertex, nDim).
      */
-    vector<passivedouble> GetMarkerDisplacements(unsigned short iMarker) const;
+    vector<vector<passivedouble>> GetMarkerDisplacements(unsigned short iMarker) const;
     
     /*!
      * \brief Get the displacements of a marker vertex.
@@ -471,9 +471,9 @@ class CDriverBase {
     /*!
      * \brief Set the displacements of the marker vertices.
      * \param[in] iMarker - Marker index.
-     * \param[in] values - Vertex displacements (nVertex*nDim).
+     * \param[in] values - Vertex displacements (nVertex, nDim).
      */
-    void SetMarkerDisplacements(unsigned short iMarker, vector<passivedouble> values);
+    void SetMarkerDisplacements(unsigned short iMarker, vector<vector<passivedouble>> values);
     
     /*!
      * \brief Set the displacements of a marker vertex.
@@ -486,24 +486,24 @@ class CDriverBase {
     /*!
      * \brief Get the velocities of the marker vertices.
      * \param[in] iMarker - Marker index.
-     * \return Vertex velocities (nVertex*nDim).
+     * \return Vertex velocities (nVertex, nDim).
      */
-    vector<passivedouble> GetMarkerVelocities(unsigned short iMarker) const;
+    vector<vector<passivedouble>> GetMarkerVelocities(unsigned short iMarker) const;
 
     /*!
      * \brief Get the velocities of a marker vertex.
      * \param[in] iMarker - Marker index.
      * \param[in] iVertex - Marker vertex index.
-     * \return Vertex velocities (nVertex*nDim).
+     * \return Vertex velocities (nDim).
      */
     vector<passivedouble> GetMarkerVelocities(unsigned short iMarker, unsigned long iVertex) const;
     
     /*!
      * \brief Set the velocities of the marker vertices.
      * \param[in] iMarker - Marker index.
-     * \param[in] values - Vertex velocities (nVertex*nDim).
+     * \param[in] values - Vertex velocities (nVertex, nDim).
      */
-    void SetMarkerVelocities(unsigned short iMarker, vector<passivedouble> values);
+    void SetMarkerVelocities(unsigned short iMarker, vector<vector<passivedouble>> values);
     
     /*!
      * \brief Set the velocities of a marker vertex.
@@ -517,9 +517,9 @@ class CDriverBase {
      * \brief Get the normal vectors at the marker vertices.
      * \param[in] iMarker - Marker index.
      * \param[in] normalize - If true, the unit (i.e. normalized) normal vector is returned.
-     * \return Normal vector at the vertex (nVertex*nDim).
+     * \return Normal vector at the vertex (nVertex, nDim).
      */
-    vector<passivedouble> GetMarkerVertexNormals(unsigned short iMarker, bool normalize = false) const;
+    vector<vector<passivedouble>> GetMarkerVertexNormals(unsigned short iMarker, bool normalize = false) const;
     
     /*!
      * \brief Get the normal vectors at a marker vertex.
diff --git a/Common/src/drivers/CDriverBase.cpp b/Common/src/drivers/CDriverBase.cpp
index 9a3ee6ba686..8f2f74d0a99 100644
--- a/Common/src/drivers/CDriverBase.cpp
+++ b/Common/src/drivers/CDriverBase.cpp
@@ -86,9 +86,9 @@ unsigned short CDriverBase::GetNumberMarkers() const {
     return config_container[ZONE_0]->GetnMarker_All();
 }
 
-map<string, int> CDriverBase::GetMarkerIndices() const {
+map<string, unsigned short> CDriverBase::GetMarkerIndices() const {
     const auto nMarker = config_container[ZONE_0]->GetnMarker_All();
-    map<string, int> indexMap;
+    map<string, unsigned short> indexMap;
     
     for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
         auto tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
@@ -154,7 +154,7 @@ vector<string> CDriverBase::GetMarkerTags() const {
 
 vector<string> CDriverBase::GetDeformableMarkerTags() const {
     vector<string> tags;
-    const auto nMarker = config_container[ZONE_0]->GetnMarker_All();
+    const auto nMarker = config_container[ZONE_0]->GetnMarker_Deform_Mesh();
     
     for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
         tags.push_back(config_container[ZONE_0]->GetMarker_Deform_Mesh_TagBound(iMarker));
@@ -180,9 +180,10 @@ unsigned long CDriverBase::GetNumberMarkerElements(unsigned short iMarker) const
 }
 
 vector<unsigned long> CDriverBase::GetElementIDs() const {
-    vector<unsigned long> values;
     const auto nElem = GetNumberElements();
 
+    vector<unsigned long> values;
+
     for (auto iElem = 0ul; iElem < nElem; iElem++) {
         values.push_back(GetElementIDs(iElem));
     }
@@ -199,9 +200,10 @@ unsigned long CDriverBase::GetElementIDs(unsigned long iElem) const {
 }
 
 vector<unsigned long> CDriverBase::GetMarkerElementIDs(unsigned short iMarker) const { 
-    vector<unsigned long> values;
     const auto nBound = GetNumberMarkerElements(iMarker);
 
+    vector<unsigned long> values;
+     
     for (auto iBound = 0ul; iBound < nBound; iBound++) {
         values.push_back(GetMarkerElementIDs(iMarker, iBound));
     }
@@ -218,9 +220,10 @@ unsigned long CDriverBase::GetMarkerElementIDs(unsigned short iMarker, unsigned
 }
 
 vector<unsigned long> CDriverBase::GetElementColors() const {
-    vector<unsigned long> values;
     const auto nElem = GetNumberElements();
 
+    vector<unsigned long> values;
+
     for (auto iElem = 0ul; iElem < nElem; iElem++) {
         values.push_back(GetElementColors(iElem));
     }
@@ -237,9 +240,10 @@ unsigned long CDriverBase::GetElementColors(unsigned long iElem) const {
 }
 
 vector<unsigned long> CDriverBase::GetMarkerElementColors(unsigned short iMarker) const {
-    vector<unsigned long> values;
     const auto nBound = GetNumberMarkerElements(iMarker);
 
+    vector<unsigned long> values;
+    
     for (auto iBound = 0ul; iBound < nBound; iBound++) {
         values.push_back(GetMarkerElementColors(iMarker, iBound));
     }
@@ -256,9 +260,10 @@ unsigned long CDriverBase::GetMarkerElementColors(unsigned short iMarker, unsign
 }
 
 vector<vector<unsigned long>> CDriverBase::GetElementConnectivities() const {
-    vector<vector<unsigned long>> values;
     const auto nElem = GetNumberElements();
     
+    vector<vector<unsigned long>> values;
+    
     for (auto iElem = 0ul; iElem < nElem; iElem++) {
         values.push_back(GetElementConnectivities(iElem));
     }
@@ -271,9 +276,10 @@ vector<unsigned long> CDriverBase::GetElementConnectivities(unsigned long iElem)
         SU2_MPI::Error("Element index exceeds size.", CURRENT_FUNCTION);
     }
     
-    vector<unsigned long> values; 
     unsigned short nNode = geometry_container[ZONE_0][INST_0][MESH_0]->elem[iElem]->GetnNodes();
     
+    vector<unsigned long> values; 
+
     for (auto iNode = 0u; iNode < nNode; iNode++) {
         values.push_back(geometry_container[ZONE_0][INST_0][MESH_0]->elem[iElem]->GetNode(iNode));
     }
@@ -282,9 +288,10 @@ vector<unsigned long> CDriverBase::GetElementConnectivities(unsigned long iElem)
 }
 
 vector<vector<unsigned long>> CDriverBase::GetMarkerElementConnectivities(unsigned short iMarker) const {
-    vector<vector<unsigned long>> values;
     const auto nBound = GetNumberMarkerElements(iMarker);
     
+    vector<vector<unsigned long>> values;
+
     for (auto iBound = 0ul; iBound < nBound; iBound++) {
         values.push_back(GetMarkerElementConnectivities(iMarker, iBound));
     }
@@ -297,9 +304,10 @@ vector<unsigned long> CDriverBase::GetMarkerElementConnectivities(unsigned short
         SU2_MPI::Error("Marker element index exceeds size.", CURRENT_FUNCTION);
     }
     
-    vector<unsigned long> values; 
     unsigned short nNode = geometry_container[ZONE_0][INST_0][MESH_0]->bound[iMarker][iBound]->GetnNodes();
     
+    vector<unsigned long> values; 
+
     for (auto iNode = 0u; iNode < nNode; iNode++) {
         values.push_back(geometry_container[ZONE_0][INST_0][MESH_0]->bound[iMarker][iBound]->GetNode(iNode));
     }
@@ -348,9 +356,10 @@ unsigned long CDriverBase::GetNumberMarkerHaloVertices(unsigned short iMarker) c
 }
 
 vector<unsigned long> CDriverBase::GetMarkerVertexIndex(unsigned short iMarker) const {
-    vector<unsigned long> values;
     const auto nVertex = GetNumberMarkerVertices(iMarker);
     
+    vector<unsigned long> values;
+
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
         values.push_back(GetMarkerVertexIndex(iMarker, iVertex));
     }
@@ -367,9 +376,10 @@ unsigned long CDriverBase::GetMarkerVertexIndex(unsigned short iMarker, unsigned
 }
 
 vector<unsigned long> CDriverBase::GetVertexIDs() const {
-    vector<unsigned long> values;
     const auto nPoint = GetNumberVertices();
     
+    vector<unsigned long> values;
+
     for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
         values.push_back(GetVertexIDs(iPoint));
     }
@@ -386,9 +396,10 @@ unsigned long CDriverBase::GetVertexIDs(unsigned long iPoint) const {
 }
 
 vector<unsigned long> CDriverBase::GetMarkerVertexIDs(unsigned short iMarker) const {
-    vector<unsigned long> values;
     const auto nVertex = GetNumberMarkerVertices(iMarker); 
     
+    vector<unsigned long> values;
+
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
         values.push_back(GetMarkerVertexIDs(iMarker, iVertex));
     }
@@ -403,9 +414,10 @@ unsigned long CDriverBase::GetMarkerVertexIDs(unsigned short iMarker, unsigned l
 }
 
 vector<unsigned long> CDriverBase::GetVertexColors() const {
-    vector<unsigned long> values;
     const auto nPoint = GetNumberVertices();
     
+    vector<unsigned long> values;
+    
     for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
         values.push_back(GetVertexColors(iPoint));
     }
@@ -422,9 +434,10 @@ unsigned long CDriverBase::GetVertexColors(unsigned long iPoint) const {
 }
 
 vector<unsigned long> CDriverBase::GetMarkerVertexColors(unsigned short iMarker) const {
-    vector<unsigned long> values;
     const auto nVertex = GetNumberMarkerVertices(iMarker);
     
+    vector<unsigned long> values;
+    
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
         values.push_back(GetMarkerVertexColors(iMarker, iVertex));
     }
@@ -439,8 +452,9 @@ unsigned long CDriverBase::GetMarkerVertexColors(unsigned short iMarker, unsigne
 }
 
 vector<bool> CDriverBase::GetDomain() const {
-    vector<bool> values;
     const auto nPoint = GetNumberVertices();
+
+    vector<bool> values;
     
     for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
         values.push_back(GetDomain(iPoint));
@@ -458,8 +472,9 @@ bool CDriverBase::GetDomain(unsigned long iPoint) const {
 }
 
 vector<bool> CDriverBase::GetMarkerDomain(unsigned short iMarker) const {
-    vector<bool> values;
     const auto nVertex = GetNumberMarkerVertices(iMarker);
+
+    vector<bool> values;
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
         values.push_back(GetMarkerDomain(iMarker, iVertex));
@@ -474,16 +489,13 @@ bool CDriverBase::GetMarkerDomain(unsigned short iMarker, unsigned long iVertex)
     return geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint);
 }
 
-vector<passivedouble> CDriverBase::GetInitialCoordinates() const {
+vector<vector<passivedouble>> CDriverBase::GetInitialCoordinates() const {
     const auto nPoint = GetNumberVertices();
-    vector<passivedouble> values;
+
+    vector<vector<passivedouble>> values;
     
     for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
-        const auto value = GetInitialCoordinates(iPoint);
-        
-        for (auto iDim = 0u; iDim < nDim; iDim++) {
-            values.push_back(value[iDim]);
-        }
+        values.push_back(GetInitialCoordinates(iPoint));
     }
     
     return values;
@@ -510,9 +522,10 @@ vector<passivedouble> CDriverBase::GetInitialCoordinates(unsigned long iPoint) c
     return values;
 }
 
-vector<passivedouble> CDriverBase::GetMarkerInitialCoordinates(unsigned short iMarker) const {
+vector<vector<passivedouble>> CDriverBase::GetMarkerInitialCoordinates(unsigned short iMarker) const {
     const auto nVertex = GetNumberMarkerVertices(iMarker);
-    vector<passivedouble> values;
+
+    vector<vector<passivedouble>> values;
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
         const auto value = GetMarkerInitialCoordinates(iVertex);
@@ -527,6 +540,7 @@ vector<passivedouble> CDriverBase::GetMarkerInitialCoordinates(unsigned short iM
 
 vector<passivedouble> CDriverBase::GetMarkerInitialCoordinates(unsigned short iMarker, unsigned long iVertex) const {
     auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+
     vector<passivedouble> values;
 
     for (auto iDim = 0u; iDim < nDim; iDim++) {
@@ -543,23 +557,23 @@ vector<passivedouble> CDriverBase::GetMarkerInitialCoordinates(unsigned short iM
     return values;
 }
 
-vector<passivedouble> CDriverBase::GetCoordinates() const {
+vector<vector<passivedouble>> CDriverBase::GetCoordinates() const {
     const auto nPoint = GetNumberVertices();
-    vector<passivedouble> values;
+
+    vector<vector<passivedouble>> values;
     
     for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
-        const auto value = GetCoordinates(iPoint);
-        
-        for (auto iDim = 0u; iDim < nDim; iDim++) {
-            values.push_back(value[iDim]);
-        }
+        values.push_back(GetCoordinates(iPoint));
     }
     
     return values;
 }
 
 vector<passivedouble> CDriverBase::GetCoordinates(unsigned long iPoint) const {
-    const auto nPoint = GetNumberVertices();
+    if (iPoint >= GetNumberVertices()) {
+        SU2_MPI::Error("Vertex index exceeds size.", CURRENT_FUNCTION);
+    }
+
     vector<passivedouble> values;
     
     for (auto iDim = 0u; iDim < nDim; iDim++) {
@@ -571,16 +585,13 @@ vector<passivedouble> CDriverBase::GetCoordinates(unsigned long iPoint) const {
     return values;
 }
 
-vector<passivedouble> CDriverBase::GetMarkerCoordinates(unsigned short iMarker) const {
+vector<vector<passivedouble>> CDriverBase::GetMarkerCoordinates(unsigned short iMarker) const {
     const auto nVertex = GetNumberMarkerVertices(iMarker);
-    vector<passivedouble> values;
+
+    vector<vector<passivedouble>> values;
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        const auto value = GetMarkerCoordinates(iVertex);
-        
-        for (auto iDim = 0u; iDim < nDim; iDim++) {
-            values.push_back(value[iDim]);
-        }
+        values.push_back(GetMarkerCoordinates(iMarker, iVertex));
     }
     
     return values;
@@ -588,6 +599,7 @@ vector<passivedouble> CDriverBase::GetMarkerCoordinates(unsigned short iMarker)
 
 vector<passivedouble> CDriverBase::GetMarkerCoordinates(unsigned short iMarker, unsigned long iVertex) const {
     auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+
     vector<passivedouble> values;
     
     for (auto iDim = 0u; iDim < nDim; iDim++) {
@@ -599,23 +611,25 @@ vector<passivedouble> CDriverBase::GetMarkerCoordinates(unsigned short iMarker,
     return values;
 }
 
-void CDriverBase::SetCoordinates(vector<passivedouble> values) {
+void CDriverBase::SetCoordinates(vector<vector<passivedouble>> values) {
     const auto nPoint = GetNumberVertices();
     
-    if (values.size() != nPoint*nDim) {
-        SU2_MPI::Error("Size does not match nPoint * nDim!", CURRENT_FUNCTION);
+    if (values.size() != nPoint) {
+        SU2_MPI::Error("Invalid number of vertices !", CURRENT_FUNCTION);
     }
     
     for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
-        for (auto iDim = 0u; iDim < nDim; iDim++) {
-            geometry_container[ZONE_0][INST_0][MESH_0]->nodes->SetCoord(iPoint, iDim, values[iPoint*nDim + iDim]);
-        }
+        SetCoordinates(iPoint, values[iPoint]);
     }
 }
 
 void CDriverBase::SetCoordinates(unsigned long iPoint, vector<passivedouble> values) {
+    if (iPoint >= GetNumberVertices()) {
+        SU2_MPI::Error("Vertex index exceeds size.", CURRENT_FUNCTION);
+    }
+
     if (values.size() != nDim) {
-        SU2_MPI::Error("Size does not match nDim!", CURRENT_FUNCTION);
+        SU2_MPI::Error("Invalid number of dimensions !", CURRENT_FUNCTION);
     }
     
     for (auto iDim = 0u; iDim < nDim; iDim++) {
@@ -623,44 +637,37 @@ void CDriverBase::SetCoordinates(unsigned long iPoint, vector<passivedouble> val
     }
 }
 
-void CDriverBase::SetMarkerCoordinates(unsigned short iMarker, vector<passivedouble> values) {
+void CDriverBase::SetMarkerCoordinates(unsigned short iMarker, vector<vector<passivedouble>> values) {
     const auto nVertex = GetNumberMarkerVertices(iMarker);
 
-    if (values.size() != nVertex*nDim) {
-        SU2_MPI::Error("Size does not match nVertex * nDim!", CURRENT_FUNCTION);
+    if (values.size() != nVertex) {
+        SU2_MPI::Error("Invalid number of marker vertices !", CURRENT_FUNCTION);
     }
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
-        
-        for (auto iDim = 0u; iDim < nDim; iDim++) {
-            geometry_container[ZONE_0][INST_0][MESH_0]->nodes->SetCoord(iPoint, iDim, values[iVertex*nDim + iDim]);
-        }
+        SetMarkerCoordinates(iMarker, iVertex, values[iVertex]);
     }
 }
 
 void CDriverBase::SetMarkerCoordinates(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
+    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+
     if (values.size() != nDim) {
-        SU2_MPI::Error("Size does not match nDim!", CURRENT_FUNCTION);
+        SU2_MPI::Error("Invalid number of dimensions !", CURRENT_FUNCTION);
     }
     
-    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
-    
     for (auto iDim = 0u; iDim < nDim; iDim++) {
         geometry_container[ZONE_0][INST_0][MESH_0]->nodes->SetCoord(iPoint, iDim, values[iDim]);
     }
 }
 
-vector<passivedouble> CDriverBase::GetMarkerDisplacements(unsigned short iMarker) const {
+vector<vector<passivedouble>> CDriverBase::GetMarkerDisplacements(unsigned short iMarker) const {
     const auto nVertex = GetNumberMarkerVertices(iMarker);
-    vector<passivedouble> values;
+
+    vector<vector<passivedouble>> values;
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        const auto value = GetMarkerDisplacements(iMarker, iVertex);
-        
-        for (auto iDim = 0u; iDim < nDim; iDim++) {
-            values.push_back(values[iDim]);
-        }
+        values.push_back(GetMarkerDisplacements(iMarker, iVertex));
     }
     
     return values;
@@ -668,62 +675,60 @@ vector<passivedouble> CDriverBase::GetMarkerDisplacements(unsigned short iMarker
 
 vector<passivedouble> CDriverBase::GetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex) const {
     auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+
     vector<passivedouble> values;
     
     for (auto iDim = 0u; iDim < nDim; iDim++) {
-        const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetBound_Disp(iPoint, iDim);
-
-        values.push_back(SU2_TYPE::GetValue(value));
+        if (config_container[ZONE_0]->GetDeform_Mesh()) {
+            values.push_back(SU2_TYPE::GetValue(solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetBound_Disp(iPoint, iDim)));
+        }
+        else {
+            values.push_back(0.0);
+        }
     }
     
     return values;
 }
 
-void CDriverBase::SetMarkerDisplacements(unsigned short iMarker, vector<passivedouble> values) {
+void CDriverBase::SetMarkerDisplacements(unsigned short iMarker, vector<vector<passivedouble>> values) {
     if (!config_container[ZONE_0]->GetDeform_Mesh()) {
-        SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
+        SU2_MPI::Error("Mesh solver is not defined !", CURRENT_FUNCTION);
     }
 
     const auto nVertex = GetNumberMarkerVertices(iMarker);
 
-    if (values.size() != nVertex*nDim) {
-        SU2_MPI::Error("Size does not match nVertex * nDim!", CURRENT_FUNCTION);
+    if (values.size() != nVertex) {
+        SU2_MPI::Error("Invalid number of marker vertices !", CURRENT_FUNCTION);
     }
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
-        
-        for (auto iDim = 0u; iDim < nDim; iDim++) {
-            solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->SetBound_Disp(iPoint, iDim, values[iVertex*nDim + iDim]);
-        }
+        SetMarkerDisplacements(iMarker, iVertex, values[iVertex]);
     }
 }
 
 void CDriverBase::SetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
     if (!config_container[ZONE_0]->GetDeform_Mesh()) {
-        SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
+        SU2_MPI::Error("Mesh solver is not defined !", CURRENT_FUNCTION);
     }
+
+    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+
     if (values.size() != nDim) {
-        SU2_MPI::Error("Size does not match nDim!", CURRENT_FUNCTION);
+        SU2_MPI::Error("Invalid number of dimensions !", CURRENT_FUNCTION);
     }
     
-    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
-    
     for (auto iDim = 0u; iDim < nDim; iDim++) {
         solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->SetBound_Disp(iPoint, iDim, values[iDim]);
     }
 }
 
-vector<passivedouble> CDriverBase::GetMarkerVelocities(unsigned short iMarker) const {
+vector<vector<passivedouble>> CDriverBase::GetMarkerVelocities(unsigned short iMarker) const {
     const auto nVertex = GetNumberMarkerVertices(iMarker);
-    vector<passivedouble> values;
+
+    vector<vector<passivedouble>> values;
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        const auto value = GetMarkerVelocities(iMarker, iVertex);
-        
-        for (auto iDim = 0u; iDim < nDim; iDim++) {
-            values.push_back(values[iDim]);
-        }
+        values.push_back(GetMarkerVelocities(iMarker, iVertex));
     }
     
     return values;
@@ -731,62 +736,60 @@ vector<passivedouble> CDriverBase::GetMarkerVelocities(unsigned short iMarker) c
 
 vector<passivedouble> CDriverBase::GetMarkerVelocities(unsigned short iMarker, unsigned long iVertex) const {
     auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+
     vector<passivedouble> values;
     
     for (auto iDim = 0u; iDim < nDim; iDim++) {
-        const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetBound_Vel(iPoint, iDim);
-
-        values.push_back(SU2_TYPE::GetValue(value));
+        if (config_container[ZONE_0]->GetDeform_Mesh()) {
+            values.push_back(SU2_TYPE::GetValue(solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetBound_Vel(iPoint, iDim)));
+        }
+        else {
+            values.push_back(0.0);
+        }
     }
     
     return values;
 }
 
-void CDriverBase::SetMarkerVelocities(unsigned short iMarker, vector<passivedouble> values) {
+void CDriverBase::SetMarkerVelocities(unsigned short iMarker, vector<vector<passivedouble>> values) {
     if (!config_container[ZONE_0]->GetDeform_Mesh()) {
-        SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
+        SU2_MPI::Error("Mesh solver is not defined !", CURRENT_FUNCTION);
     }
 
     const auto nVertex = GetNumberMarkerVertices(iMarker);
 
-    if (values.size() != nVertex*nDim) {
-        SU2_MPI::Error("Size does not match nVertex * nDim!", CURRENT_FUNCTION);
+    if (values.size() != nVertex) {
+        SU2_MPI::Error("Invalid number of marker vertices !", CURRENT_FUNCTION);
     }
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
-        
-        for (auto iDim = 0u; iDim < nDim; iDim++) {
-            solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->SetBound_Disp(iPoint, iDim, values[iVertex*nDim + iDim]);
-        }
+        SetMarkerVelocities(iMarker, iVertex, values[iVertex]);
     }
 }
 
 void CDriverBase::SetMarkerVelocities(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
     if (!config_container[ZONE_0]->GetDeform_Mesh()) {
-        SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
+        SU2_MPI::Error("Mesh solver is not defined !", CURRENT_FUNCTION);
     }
+
+    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+
     if (values.size() != nDim) {
-        SU2_MPI::Error("Size does not match nDim!", CURRENT_FUNCTION);
+        SU2_MPI::Error("Invalid number of dimensions !", CURRENT_FUNCTION);
     }
     
-    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
-    
     for (auto iDim = 0u; iDim < nDim; iDim++) {
         solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->SetBound_Disp(iPoint, iDim, values[iDim]);
     }
 }
 
-vector<passivedouble> CDriverBase::GetMarkerVertexNormals(unsigned short iMarker, bool normalize) const {
+vector<vector<passivedouble>> CDriverBase::GetMarkerVertexNormals(unsigned short iMarker, bool normalize) const {
     const auto nVertex = GetNumberMarkerVertices(iMarker);
-    vector<passivedouble> values;
+
+    vector<vector<passivedouble>> values;
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        const auto value = GetMarkerVertexNormals(iMarker, normalize=normalize);
-        
-        for (auto iDim = 0u; iDim < nDim; iDim++) {
-            values.push_back(value[iDim]);
-        }
+        values.push_back(GetMarkerVertexNormals(iMarker, iVertex, normalize=normalize));
     }
     
     return values;
diff --git a/SU2_PY/pySU2/pySU2.i b/SU2_PY/pySU2/pySU2.i
index 0125ffd1e6b..08cf47042fb 100644
--- a/SU2_PY/pySU2/pySU2.i
+++ b/SU2_PY/pySU2/pySU2.i
@@ -66,10 +66,10 @@ namespace std {
    %template() vector<bool>;
    %template() vector<unsigned long>;
    %template() vector<vector<unsigned long>>;
-   %template() vector<int>;
    %template() vector<double>;
+   %template() vector<vector<double>>;
    %template() vector<string>;
-   %template() map<string, int>;
+   %template() map<string, unsigned short>;
    %template() map<string, string>;
 }
 
diff --git a/SU2_PY/pySU2/pySU2ad.i b/SU2_PY/pySU2/pySU2ad.i
index a1f47b6bf2b..5f0ce8412eb 100644
--- a/SU2_PY/pySU2/pySU2ad.i
+++ b/SU2_PY/pySU2/pySU2ad.i
@@ -66,10 +66,10 @@ namespace std {
    %template() vector<bool>;
    %template() vector<unsigned long>;
    %template() vector<vector<unsigned long>>;
-   %template() vector<int>;
    %template() vector<double>;
+   %template() vector<vector<double>>;
    %template() vector<string>;
-   %template() map<string, int>;
+   %template() map<string, unsigned short>;
    %template() map<string, string>;
 }
 

From 5891d3e16e15bac721051788c3e069941f7fbd6a Mon Sep 17 00:00:00 2001
From: aa-g <aa.gastaldi@pm.me>
Date: Mon, 7 Mar 2022 21:43:26 +0100
Subject: [PATCH 024/656] Fix small inconsistencies in previous commit

---
 Common/src/drivers/CDriverBase.cpp | 84 ++++++++++++++----------------
 1 file changed, 40 insertions(+), 44 deletions(-)

diff --git a/Common/src/drivers/CDriverBase.cpp b/Common/src/drivers/CDriverBase.cpp
index 8f2f74d0a99..e07a40652a9 100644
--- a/Common/src/drivers/CDriverBase.cpp
+++ b/Common/src/drivers/CDriverBase.cpp
@@ -329,30 +329,30 @@ unsigned long CDriverBase::GetNumberMarkerVertices(unsigned short iMarker) const
 
 unsigned long CDriverBase::GetNumberHaloVertices() const {
     const auto nPoint = GetNumberVertices();
-    unsigned long nHaloVertices = 0;
+    unsigned long nHalo = 0;
     
     for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
         if (!(geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint))) {
-            nHaloVertices += 1;
+            nHalo += 1;
         }
     }
     
-    return nHaloVertices;
+    return nHalo;
 }
 
 unsigned long CDriverBase::GetNumberMarkerHaloVertices(unsigned short iMarker) const {
-    const auto nVertex = GetNumberMarkerVertices(iMarker);  // error-checking included
-    unsigned long nHaloVertices = 0;
+    const auto nVertex = GetNumberMarkerVertices(iMarker);
+    unsigned long nHalo = 0;
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        auto iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+        auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
         
         if (!(geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint))) {
-            nHaloVertices += 1;
+            nHalo += 1;
         }
     }
     
-    return nHaloVertices;
+    return nHalo;
 }
 
 vector<unsigned long> CDriverBase::GetMarkerVertexIndex(unsigned short iMarker) const {
@@ -408,7 +408,7 @@ vector<unsigned long> CDriverBase::GetMarkerVertexIDs(unsigned short iMarker) co
 }
 
 unsigned long CDriverBase::GetMarkerVertexIDs(unsigned short iMarker, unsigned long iVertex) const {
-    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);  // includes error-checking
+    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
 
     return geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetGlobalIndex(iPoint);
 }
@@ -446,7 +446,7 @@ vector<unsigned long> CDriverBase::GetMarkerVertexColors(unsigned short iMarker)
 }
 
 unsigned long CDriverBase::GetMarkerVertexColors(unsigned short iMarker, unsigned long iVertex) const {
-    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);  // includes error-checking
+    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
     
     return geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetColor(iPoint);
 }
@@ -506,17 +506,16 @@ vector<passivedouble> CDriverBase::GetInitialCoordinates(unsigned long iPoint) c
         SU2_MPI::Error("Vertex index exceeds size.", CURRENT_FUNCTION);
     }
 
-    vector<passivedouble> values;
+    vector<passivedouble> values (nDim, 0.0);
+    
+    if (!config_container[ZONE_0]->GetDeform_Mesh()) {
+        return values;
+    }
 
     for (auto iDim = 0u; iDim < nDim; iDim++) {
         const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord(iPoint, iDim);
-
-        if (!config_container[ZONE_0]->GetDeform_Mesh()) {
-            values.push_back(0.0);  // mesh solver is not defined !
-        }
-        else {
-            values.push_back(SU2_TYPE::GetValue(value));
-        }
+        
+        values[iDim] = SU2_TYPE::GetValue(value);
     }
     
     return values;
@@ -528,11 +527,7 @@ vector<vector<passivedouble>> CDriverBase::GetMarkerInitialCoordinates(unsigned
     vector<vector<passivedouble>> values;
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        const auto value = GetMarkerInitialCoordinates(iVertex);
-        
-        for (auto iDim = 0u; iDim < nDim; iDim++) {
-            values.push_back(value[iDim]);
-        }
+        values.push_back(GetMarkerInitialCoordinates(iMarker, iVertex));
     }
     
     return values;
@@ -541,17 +536,16 @@ vector<vector<passivedouble>> CDriverBase::GetMarkerInitialCoordinates(unsigned
 vector<passivedouble> CDriverBase::GetMarkerInitialCoordinates(unsigned short iMarker, unsigned long iVertex) const {
     auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
 
-    vector<passivedouble> values;
+    vector<passivedouble> values(nDim, 0.0);
+
+    if (!config_container[ZONE_0]->GetDeform_Mesh()) {
+        return values;
+    }
 
     for (auto iDim = 0u; iDim < nDim; iDim++) {
         const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord(iPoint, iDim);
 
-        if (!config_container[ZONE_0]->GetDeform_Mesh()) {
-            values.push_back(0.0);  // mesh solver is not defined !
-        }
-        else {
-            values.push_back(SU2_TYPE::GetValue(value));
-        }
+        values[iDim] = SU2_TYPE::GetValue(value);
     }
     
     return values;
@@ -676,15 +670,16 @@ vector<vector<passivedouble>> CDriverBase::GetMarkerDisplacements(unsigned short
 vector<passivedouble> CDriverBase::GetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex) const {
     auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
 
-    vector<passivedouble> values;
+    vector<passivedouble> values (nDim, 0.0);
+    
+    if (!config_container[ZONE_0]->GetDeform_Mesh()) {
+        return values;
+    }
     
     for (auto iDim = 0u; iDim < nDim; iDim++) {
-        if (config_container[ZONE_0]->GetDeform_Mesh()) {
-            values.push_back(SU2_TYPE::GetValue(solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetBound_Disp(iPoint, iDim)));
-        }
-        else {
-            values.push_back(0.0);
-        }
+        const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetBound_Disp(iPoint, iDim);
+        
+        values[iDim] = SU2_TYPE::GetValue(value);
     }
     
     return values;
@@ -737,15 +732,16 @@ vector<vector<passivedouble>> CDriverBase::GetMarkerVelocities(unsigned short iM
 vector<passivedouble> CDriverBase::GetMarkerVelocities(unsigned short iMarker, unsigned long iVertex) const {
     auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
 
-    vector<passivedouble> values;
+    vector<passivedouble> values (nDim, 0.0);
+    
+    if (!config_container[ZONE_0]->GetDeform_Mesh()) {
+        return values;
+    }
     
     for (auto iDim = 0u; iDim < nDim; iDim++) {
-        if (config_container[ZONE_0]->GetDeform_Mesh()) {
-            values.push_back(SU2_TYPE::GetValue(solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetBound_Vel(iPoint, iDim)));
-        }
-        else {
-            values.push_back(0.0);
-        }
+        const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetBound_Vel(iPoint, iDim);
+        
+        values[iDim] = SU2_TYPE::GetValue(value);
     }
     
     return values;

From 59fdd2e86d14f264d92d6b610ee3331a0fe82140 Mon Sep 17 00:00:00 2001
From: aa-g <aa.gastaldi@pm.me>
Date: Mon, 7 Mar 2022 22:22:25 +0100
Subject: [PATCH 025/656] Fix conditional output of FFD information

---
 SU2_DEF/src/drivers/CDeformationDriver.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index ecca754838a..309e65377d2 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -534,7 +534,7 @@ void CDeformationDriver::Output() {
             (config_container[ZONE_0]->GetDesign_Variable(0) != ROTATE_GRID)) {
             
             /*--- Write the the free-form deformation boxes after deformation (if defined). ---*/
-            if (true) {
+            if (!haveSurfaceDeformation) {
                 if (rank == MASTER_NODE) cout << "No FFD information available." << endl;
             }
             else {

From 4873aa2f46c76e744c482c3c0e655addc6fc608f Mon Sep 17 00:00:00 2001
From: aa-g <aa.gastaldi@pm.me>
Date: Mon, 7 Mar 2022 23:25:20 +0100
Subject: [PATCH 026/656] Introduce 'main' Config and Geometry for Python API

---
 Common/include/drivers/CDriverBase.hpp        |  8 +-
 Common/src/drivers/CDriverBase.cpp            | 99 ++++++++++---------
 SU2_CFD/src/drivers/CDriver.cpp               | 10 +-
 SU2_DEF/src/drivers/CDeformationDriver.cpp    |  7 ++
 .../src/drivers/CDiscAdjDeformationDriver.cpp |  7 ++
 5 files changed, 79 insertions(+), 52 deletions(-)

diff --git a/Common/include/drivers/CDriverBase.hpp b/Common/include/drivers/CDriverBase.hpp
index 68aa0bd5956..19f0923e4b2 100644
--- a/Common/include/drivers/CDriverBase.hpp
+++ b/Common/include/drivers/CDriverBase.hpp
@@ -56,10 +56,11 @@ class CDriverBase {
     *nInst,                                         /*!< \brief Total number of instances in the problem (per zone). */
     **interface_types;                              /*!< \brief Type of coupling between the distinct (physical) zones.*/
     
-    CConfig **config_container;                     /*!< \brief Definition of the particular problem. */
     CConfig *driver_config;                         /*!< \brief Definition of the driver configuration. */
-    COutput **output_container;                     /*!< \brief Pointer to the COutput class. */
     COutput *driver_output;                         /*!< \brief Definition of the driver output. */
+
+    CConfig **config_container;                     /*!< \brief Definition of the particular problem. */
+    COutput **output_container;                     /*!< \brief Pointer to the COutput class. */
     CGeometry ****geometry_container;               /*!< \brief Geometrical definition of the problem. */
     CSolver *****solver_container;                  /*!< \brief Container vector with all the solutions. */
     CNumerics ******numerics_container;             /*!< \brief Description of the numerical method (the way in which the equations are solved). */
@@ -67,6 +68,9 @@ class CDriverBase {
     CVolumetricMovement ***grid_movement;           /*!< \brief Volume grid movement classes of the problem. */
     CFreeFormDefBox*** FFDBox;                      /*!< \brief FFD FFDBoxes of the problem. */
     
+    CConfig *main_config;                           /*!< \brief Reference to the base (i.e. ZONE 0) configuration (used in the driver API). */
+    CGeometry *main_geometry;                       /*!< \brief Reference to the base (i.E. ZONE, INST, MESH 0) geometry (used in the driver API). */
+    
 public:
     
     /*!
diff --git a/Common/src/drivers/CDriverBase.cpp b/Common/src/drivers/CDriverBase.cpp
index e07a40652a9..01eccb23448 100644
--- a/Common/src/drivers/CDriverBase.cpp
+++ b/Common/src/drivers/CDriverBase.cpp
@@ -78,20 +78,23 @@ void CDriverBase::SetContainers_Null() {
         nInst[iZone] = 1;
     }
     
-    driver_config         = nullptr;
-    driver_output         = nullptr;
+    driver_config = nullptr;
+    driver_output = nullptr;
+
+    main_config = nullptr;
+    main_geometry = nullptr;
 }
 
 unsigned short CDriverBase::GetNumberMarkers() const {
-    return config_container[ZONE_0]->GetnMarker_All();
+    return main_config->GetnMarker_All();
 }
 
 map<string, unsigned short> CDriverBase::GetMarkerIndices() const {
-    const auto nMarker = config_container[ZONE_0]->GetnMarker_All();
+    const auto nMarker = main_config->GetnMarker_All();
     map<string, unsigned short> indexMap;
     
     for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
-        auto tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
+        auto tag = main_config->GetMarker_All_TagBound(iMarker);
 
         indexMap[tag] = iMarker;
     }
@@ -103,9 +106,9 @@ map<string, string> CDriverBase::GetMarkerTypes() const {
     map<string, string> typeMap;
     string type;
     
-    for (auto iMarker = 0u; iMarker < config_container[ZONE_0]->GetnMarker_All(); iMarker++) {
-        auto tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
-        auto kindBC = config_container[ZONE_0]->GetMarker_All_KindBC(iMarker);
+    for (auto iMarker = 0u; iMarker < main_config->GetnMarker_All(); iMarker++) {
+        auto tag = main_config->GetMarker_All_TagBound(iMarker);
+        auto kindBC = main_config->GetMarker_All_KindBC(iMarker);
         
         switch(kindBC) {
             case EULER_WALL:
@@ -143,10 +146,10 @@ map<string, string> CDriverBase::GetMarkerTypes() const {
 
 vector<string> CDriverBase::GetMarkerTags() const {
     vector<string> tags;
-    const auto nMarker = config_container[ZONE_0]->GetnMarker_All();
+    const auto nMarker = main_config->GetnMarker_All();
     
     for(auto iMarker = 0u; iMarker < nMarker; iMarker++){
-        tags.push_back(config_container[ZONE_0]->GetMarker_All_TagBound(iMarker));
+        tags.push_back(main_config->GetMarker_All_TagBound(iMarker));
     }
     
     return tags;
@@ -154,21 +157,21 @@ vector<string> CDriverBase::GetMarkerTags() const {
 
 vector<string> CDriverBase::GetDeformableMarkerTags() const {
     vector<string> tags;
-    const auto nMarker = config_container[ZONE_0]->GetnMarker_Deform_Mesh();
+    const auto nMarker = main_config->GetnMarker_Deform_Mesh();
     
     for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
-        tags.push_back(config_container[ZONE_0]->GetMarker_Deform_Mesh_TagBound(iMarker));
+        tags.push_back(main_config->GetMarker_Deform_Mesh_TagBound(iMarker));
     }
     
     return tags;
 }
 
 unsigned long CDriverBase::GetNumberDimensions() const {
-    return geometry_container[ZONE_0][INST_0][MESH_0]->GetnDim();
+    return main_geometry->GetnDim();
 }
 
 unsigned long CDriverBase::GetNumberElements() const {
-    return geometry_container[ZONE_0][INST_0][MESH_0]->GetnElem();
+    return main_geometry->GetnElem();
 }
 
 unsigned long CDriverBase::GetNumberMarkerElements(unsigned short iMarker) const {
@@ -176,7 +179,7 @@ unsigned long CDriverBase::GetNumberMarkerElements(unsigned short iMarker) const
         SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
     }
 
-    return geometry_container[ZONE_0][INST_0][MESH_0]->GetnElem_Bound(iMarker);
+    return main_geometry->GetnElem_Bound(iMarker);
 }
 
 vector<unsigned long> CDriverBase::GetElementIDs() const {
@@ -196,7 +199,7 @@ unsigned long CDriverBase::GetElementIDs(unsigned long iElem) const {
         SU2_MPI::Error("Element index exceeds size.", CURRENT_FUNCTION);
     }
 
-    return geometry_container[ZONE_0][INST_0][MESH_0]->elem[iElem]->GetGlobalIndex();
+    return main_geometry->elem[iElem]->GetGlobalIndex();
 }
 
 vector<unsigned long> CDriverBase::GetMarkerElementIDs(unsigned short iMarker) const { 
@@ -216,7 +219,7 @@ unsigned long CDriverBase::GetMarkerElementIDs(unsigned short iMarker, unsigned
         SU2_MPI::Error("Marker element index exceeds size.", CURRENT_FUNCTION);
     }
 
-    return geometry_container[ZONE_0][INST_0][MESH_0]->bound[iMarker][iBound]->GetGlobalIndex();
+    return main_geometry->bound[iMarker][iBound]->GetGlobalIndex();
 }
 
 vector<unsigned long> CDriverBase::GetElementColors() const {
@@ -236,7 +239,7 @@ unsigned long CDriverBase::GetElementColors(unsigned long iElem) const {
         SU2_MPI::Error("Element index exceeds size.", CURRENT_FUNCTION);
     }
     
-    return geometry_container[ZONE_0][INST_0][MESH_0]->elem[iElem]->GetColor();
+    return main_geometry->elem[iElem]->GetColor();
 }
 
 vector<unsigned long> CDriverBase::GetMarkerElementColors(unsigned short iMarker) const {
@@ -256,7 +259,7 @@ unsigned long CDriverBase::GetMarkerElementColors(unsigned short iMarker, unsign
         SU2_MPI::Error("Marker element index exceeds size.", CURRENT_FUNCTION);
     }
 
-    return geometry_container[ZONE_0][INST_0][MESH_0]->bound[iMarker][iBound]->GetColor();
+    return main_geometry->bound[iMarker][iBound]->GetColor();
 }
 
 vector<vector<unsigned long>> CDriverBase::GetElementConnectivities() const {
@@ -276,12 +279,12 @@ vector<unsigned long> CDriverBase::GetElementConnectivities(unsigned long iElem)
         SU2_MPI::Error("Element index exceeds size.", CURRENT_FUNCTION);
     }
     
-    unsigned short nNode = geometry_container[ZONE_0][INST_0][MESH_0]->elem[iElem]->GetnNodes();
+    unsigned short nNode = main_geometry->elem[iElem]->GetnNodes();
     
     vector<unsigned long> values; 
 
     for (auto iNode = 0u; iNode < nNode; iNode++) {
-        values.push_back(geometry_container[ZONE_0][INST_0][MESH_0]->elem[iElem]->GetNode(iNode));
+        values.push_back(main_geometry->elem[iElem]->GetNode(iNode));
     }
     
     return values;
@@ -304,19 +307,19 @@ vector<unsigned long> CDriverBase::GetMarkerElementConnectivities(unsigned short
         SU2_MPI::Error("Marker element index exceeds size.", CURRENT_FUNCTION);
     }
     
-    unsigned short nNode = geometry_container[ZONE_0][INST_0][MESH_0]->bound[iMarker][iBound]->GetnNodes();
+    unsigned short nNode = main_geometry->bound[iMarker][iBound]->GetnNodes();
     
     vector<unsigned long> values; 
 
     for (auto iNode = 0u; iNode < nNode; iNode++) {
-        values.push_back(geometry_container[ZONE_0][INST_0][MESH_0]->bound[iMarker][iBound]->GetNode(iNode));
+        values.push_back(main_geometry->bound[iMarker][iBound]->GetNode(iNode));
     }
     
     return values;
 }
 
 unsigned long CDriverBase::GetNumberVertices() const {
-    return geometry_container[ZONE_0][INST_0][MESH_0]->GetnPoint();
+    return main_geometry->GetnPoint();
 }
 
 unsigned long CDriverBase::GetNumberMarkerVertices(unsigned short iMarker) const {
@@ -324,7 +327,7 @@ unsigned long CDriverBase::GetNumberMarkerVertices(unsigned short iMarker) const
         SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
     }
 
-    return geometry_container[ZONE_0][INST_0][MESH_0]->GetnVertex(iMarker);
+    return main_geometry->GetnVertex(iMarker);
 }
 
 unsigned long CDriverBase::GetNumberHaloVertices() const {
@@ -332,7 +335,7 @@ unsigned long CDriverBase::GetNumberHaloVertices() const {
     unsigned long nHalo = 0;
     
     for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
-        if (!(geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint))) {
+        if (!(main_geometry->nodes->GetDomain(iPoint))) {
             nHalo += 1;
         }
     }
@@ -347,7 +350,7 @@ unsigned long CDriverBase::GetNumberMarkerHaloVertices(unsigned short iMarker) c
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
         auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
         
-        if (!(geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint))) {
+        if (!(main_geometry->nodes->GetDomain(iPoint))) {
             nHalo += 1;
         }
     }
@@ -392,7 +395,7 @@ unsigned long CDriverBase::GetVertexIDs(unsigned long iPoint) const {
         SU2_MPI::Error("Vertex index exceeds size.", CURRENT_FUNCTION);
     }
 
-    return geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetGlobalIndex(iPoint);
+    return main_geometry->nodes->GetGlobalIndex(iPoint);
 }
 
 vector<unsigned long> CDriverBase::GetMarkerVertexIDs(unsigned short iMarker) const {
@@ -410,7 +413,7 @@ vector<unsigned long> CDriverBase::GetMarkerVertexIDs(unsigned short iMarker) co
 unsigned long CDriverBase::GetMarkerVertexIDs(unsigned short iMarker, unsigned long iVertex) const {
     auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
 
-    return geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetGlobalIndex(iPoint);
+    return main_geometry->nodes->GetGlobalIndex(iPoint);
 }
 
 vector<unsigned long> CDriverBase::GetVertexColors() const {
@@ -430,7 +433,7 @@ unsigned long CDriverBase::GetVertexColors(unsigned long iPoint) const {
         SU2_MPI::Error("Vertex index exceeds size.", CURRENT_FUNCTION);
     }
 
-    return geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetColor(iPoint);
+    return main_geometry->nodes->GetColor(iPoint);
 }
 
 vector<unsigned long> CDriverBase::GetMarkerVertexColors(unsigned short iMarker) const {
@@ -448,7 +451,7 @@ vector<unsigned long> CDriverBase::GetMarkerVertexColors(unsigned short iMarker)
 unsigned long CDriverBase::GetMarkerVertexColors(unsigned short iMarker, unsigned long iVertex) const {
     auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
     
-    return geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetColor(iPoint);
+    return main_geometry->nodes->GetColor(iPoint);
 }
 
 vector<bool> CDriverBase::GetDomain() const {
@@ -468,7 +471,7 @@ bool CDriverBase::GetDomain(unsigned long iPoint) const {
         SU2_MPI::Error("Vertex index exceeds size.", CURRENT_FUNCTION);
     }
     
-    return geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint);
+    return main_geometry->nodes->GetDomain(iPoint);
 }
 
 vector<bool> CDriverBase::GetMarkerDomain(unsigned short iMarker) const {
@@ -486,7 +489,7 @@ vector<bool> CDriverBase::GetMarkerDomain(unsigned short iMarker) const {
 bool CDriverBase::GetMarkerDomain(unsigned short iMarker, unsigned long iVertex) const {
     auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
     
-    return geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint);
+    return main_geometry->nodes->GetDomain(iPoint);
 }
 
 vector<vector<passivedouble>> CDriverBase::GetInitialCoordinates() const {
@@ -508,7 +511,7 @@ vector<passivedouble> CDriverBase::GetInitialCoordinates(unsigned long iPoint) c
 
     vector<passivedouble> values (nDim, 0.0);
     
-    if (!config_container[ZONE_0]->GetDeform_Mesh()) {
+    if (!main_config->GetDeform_Mesh()) {
         return values;
     }
 
@@ -538,7 +541,7 @@ vector<passivedouble> CDriverBase::GetMarkerInitialCoordinates(unsigned short iM
 
     vector<passivedouble> values(nDim, 0.0);
 
-    if (!config_container[ZONE_0]->GetDeform_Mesh()) {
+    if (!main_config->GetDeform_Mesh()) {
         return values;
     }
 
@@ -571,7 +574,7 @@ vector<passivedouble> CDriverBase::GetCoordinates(unsigned long iPoint) const {
     vector<passivedouble> values;
     
     for (auto iDim = 0u; iDim < nDim; iDim++) {
-        const su2double value = geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetCoord(iPoint, iDim);
+        const su2double value = main_geometry->nodes->GetCoord(iPoint, iDim);
         
         values.push_back(SU2_TYPE::GetValue(value));
     }
@@ -597,7 +600,7 @@ vector<passivedouble> CDriverBase::GetMarkerCoordinates(unsigned short iMarker,
     vector<passivedouble> values;
     
     for (auto iDim = 0u; iDim < nDim; iDim++) {
-        const su2double value = geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetCoord(iPoint, iDim);
+        const su2double value = main_geometry->nodes->GetCoord(iPoint, iDim);
         
         values.push_back(SU2_TYPE::GetValue(value));
     }
@@ -627,7 +630,7 @@ void CDriverBase::SetCoordinates(unsigned long iPoint, vector<passivedouble> val
     }
     
     for (auto iDim = 0u; iDim < nDim; iDim++) {
-        geometry_container[ZONE_0][INST_0][MESH_0]->nodes->SetCoord(iPoint, iDim, values[iDim]);
+        main_geometry->nodes->SetCoord(iPoint, iDim, values[iDim]);
     }
 }
 
@@ -651,7 +654,7 @@ void CDriverBase::SetMarkerCoordinates(unsigned short iMarker, unsigned long iVe
     }
     
     for (auto iDim = 0u; iDim < nDim; iDim++) {
-        geometry_container[ZONE_0][INST_0][MESH_0]->nodes->SetCoord(iPoint, iDim, values[iDim]);
+        main_geometry->nodes->SetCoord(iPoint, iDim, values[iDim]);
     }
 }
 
@@ -672,7 +675,7 @@ vector<passivedouble> CDriverBase::GetMarkerDisplacements(unsigned short iMarker
 
     vector<passivedouble> values (nDim, 0.0);
     
-    if (!config_container[ZONE_0]->GetDeform_Mesh()) {
+    if (!main_config->GetDeform_Mesh()) {
         return values;
     }
     
@@ -686,7 +689,7 @@ vector<passivedouble> CDriverBase::GetMarkerDisplacements(unsigned short iMarker
 }
 
 void CDriverBase::SetMarkerDisplacements(unsigned short iMarker, vector<vector<passivedouble>> values) {
-    if (!config_container[ZONE_0]->GetDeform_Mesh()) {
+    if (!main_config->GetDeform_Mesh()) {
         SU2_MPI::Error("Mesh solver is not defined !", CURRENT_FUNCTION);
     }
 
@@ -702,7 +705,7 @@ void CDriverBase::SetMarkerDisplacements(unsigned short iMarker, vector<vector<p
 }
 
 void CDriverBase::SetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
-    if (!config_container[ZONE_0]->GetDeform_Mesh()) {
+    if (!main_config->GetDeform_Mesh()) {
         SU2_MPI::Error("Mesh solver is not defined !", CURRENT_FUNCTION);
     }
 
@@ -734,7 +737,7 @@ vector<passivedouble> CDriverBase::GetMarkerVelocities(unsigned short iMarker, u
 
     vector<passivedouble> values (nDim, 0.0);
     
-    if (!config_container[ZONE_0]->GetDeform_Mesh()) {
+    if (!main_config->GetDeform_Mesh()) {
         return values;
     }
     
@@ -748,7 +751,7 @@ vector<passivedouble> CDriverBase::GetMarkerVelocities(unsigned short iMarker, u
 }
 
 void CDriverBase::SetMarkerVelocities(unsigned short iMarker, vector<vector<passivedouble>> values) {
-    if (!config_container[ZONE_0]->GetDeform_Mesh()) {
+    if (!main_config->GetDeform_Mesh()) {
         SU2_MPI::Error("Mesh solver is not defined !", CURRENT_FUNCTION);
     }
 
@@ -764,7 +767,7 @@ void CDriverBase::SetMarkerVelocities(unsigned short iMarker, vector<vector<pass
 }
 
 void CDriverBase::SetMarkerVelocities(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
-    if (!config_container[ZONE_0]->GetDeform_Mesh()) {
+    if (!main_config->GetDeform_Mesh()) {
         SU2_MPI::Error("Mesh solver is not defined !", CURRENT_FUNCTION);
     }
 
@@ -798,7 +801,7 @@ vector<passivedouble> CDriverBase::GetMarkerVertexNormals(unsigned short iMarker
 
     vector<passivedouble> values;
 
-    auto normal = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNormal();
+    auto normal = main_geometry->vertex[iMarker][iVertex]->GetNormal();
     auto area   = GeometryToolbox::Norm(nDim, normal);
     
     for (auto iDim = 0u; iDim < nDim; iDim++) {
@@ -814,6 +817,6 @@ vector<passivedouble> CDriverBase::GetMarkerVertexNormals(unsigned short iMarker
 
 
 void CDriverBase::CommunicateMeshDisplacements(void) {
-    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->InitiateComms(geometry_container[ZONE_0][INST_0][MESH_0], config_container[ZONE_0], MESH_DISPLACEMENTS);
-    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->CompleteComms(geometry_container[ZONE_0][INST_0][MESH_0], config_container[ZONE_0], MESH_DISPLACEMENTS);
+    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->InitiateComms(main_geometry, main_config, MESH_DISPLACEMENTS);
+    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->CompleteComms(main_geometry, main_config, MESH_DISPLACEMENTS);
 }
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index 4bb2a8a7071..b649ddc751d 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -589,6 +589,7 @@ void CDriver::Input_Preprocessing(CConfig **&config, CConfig *&driver_config) {
         /*--- Set the MPI communicator ---*/
         
         config[iZone]->SetMPICommunicator(SU2_MPI::GetComm());
+        
     }
     
     
@@ -599,7 +600,10 @@ void CDriver::Input_Preprocessing(CConfig **&config, CConfig *&driver_config) {
             config_container[iZone]->SetMultizone(driver_config, config_container);
         }
     }
-    
+
+    /*--- Keep a reference to the main (ZONE 0) config ---*/
+    main_config = config_container[ZONE_0];
+
     /*--- Determine whether or not the FEM solver is used, which decides the type of
      *    geometry classes that are instantiated. Only adapted for single-zone problems ---*/
     
@@ -703,7 +707,9 @@ void CDriver::Geometrical_Preprocessing(CConfig* config, CGeometry **&geometry,
             geometry_container[iZone][iInst][iMesh]->ComputeSurf_Straightness(config_container[iZone], (iMesh==MESH_0) );
         
     }
-    
+
+    /*--- Keep a reference to the main (ZONE_0, INST_0, MESH_0) geometry ---*/
+    main_geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 }
 
 void CDriver::Geometrical_Preprocessing_FVM(CConfig *config, CGeometry **&geometry) {
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 309e65377d2..2c577ed2c7f 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -140,6 +140,9 @@ void CDeformationDriver::Input_Preprocessing() {
             config_container[iZone]->SetMultizone(driver_config, config_container);
         }
     }
+
+    /*--- Keep a reference to the main (ZONE 0) config ---*/
+    main_config = config_container[ZONE_0];
 }
 
 void CDeformationDriver::Geometrical_Preprocessing() {
@@ -220,6 +223,10 @@ void CDeformationDriver::Geometrical_Preprocessing() {
     
     /*--- Get the number of dimensions ---*/
     nDim = geometry_container[ZONE_0][INST_0][MESH_0]->GetnDim();
+
+    /*--- Keep a reference to the main (ZONE_0, INST_0, MESH_0) geometry ---*/
+    main_geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+
 }
 
 void CDeformationDriver::Output_Preprocessing() {
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index a91ade80097..94768b3c0e4 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -124,6 +124,9 @@ void CDiscAdjDeformationDriver::Input_Preprocessing() {
             config_container[iZone]->SetMultizone(driver_config, config_container);
         }
     }
+
+    /*--- Keep a reference to the main (ZONE 0) config ---*/
+    main_config = config_container[ZONE_0];
 }
 
 void CDiscAdjDeformationDriver::Geometrical_Preprocessing() {
@@ -254,6 +257,10 @@ void CDiscAdjDeformationDriver::Geometrical_Preprocessing() {
         geometry_container[iZone][INST_0][MESH_0]->PreprocessP2PComms(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
         
     }
+
+    /*--- Keep a reference to the main (ZONE_0, INST_0, MESH_0) geometry ---*/
+    main_geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+
 }
 
 void CDiscAdjDeformationDriver::Output_Preprocessing() {

From 6aa8018695d37f754cbcd435685263855d334d69 Mon Sep 17 00:00:00 2001
From: aa-g <aa.gastaldi@pm.me>
Date: Mon, 4 Apr 2022 22:23:32 +0200
Subject: [PATCH 027/656] Remove some functions and fix IDs in
 Get(Marker)?ElementConnectivities

---
 Common/include/drivers/CDriverBase.hpp | 56 ---------------
 Common/src/drivers/CDriverBase.cpp     | 98 ++------------------------
 SU2_CFD/src/drivers/CDriver.cpp        | 20 ------
 3 files changed, 6 insertions(+), 168 deletions(-)

diff --git a/Common/include/drivers/CDriverBase.hpp b/Common/include/drivers/CDriverBase.hpp
index 19f0923e4b2..5a78918ec67 100644
--- a/Common/include/drivers/CDriverBase.hpp
+++ b/Common/include/drivers/CDriverBase.hpp
@@ -192,34 +192,6 @@ class CDriverBase {
      */
     unsigned long GetMarkerElementIDs(unsigned short iMarker, unsigned long iBound) const;
     
-    /*!
-     * \brief Get the MPI colors for mesh elements.
-     * \return Element colors.
-     */
-    vector<unsigned long> GetElementColors() const;
-    
-    /*!
-     * \brief Get the MPI color for a mesh element.
-     * \param[in] iElem - Mesh element index.
-     * \return Element color.
-     */
-    unsigned long GetElementColors(unsigned long iElem) const;
-    
-    /*!
-     * \brief Get the MPI colors for marker elements.
-     * \param[in] iMarker - Marker index.
-     * \return Element colors.
-     */
-    vector<unsigned long> GetMarkerElementColors(unsigned short iMarker) const;
-     
-    /*!
-     * \brief Get the MPI color for a marker element.
-     * \param[in] iMarker - Marker index.
-     * \param[in] iBound - Marker element index.
-     * \return Element color.
-     */
-    unsigned long GetMarkerElementColors(unsigned short iMarker, unsigned long iBound) const;
-
     /*!
      * \brief Get the table of vertex IDs belonging to the mesh elements.
      * \return Element connectivities (nElem, nNode)
@@ -317,34 +289,6 @@ class CDriverBase {
      */
     unsigned long GetMarkerVertexIDs(unsigned short iMarker, unsigned long iVertex) const;
     
-    /*!
-     * \brief Get the MPI colors of the mesh vertices.
-     * \return Vertex colors.
-     */
-    vector<unsigned long> GetVertexColors() const;
-    
-    /*!
-     * \brief Get the MPI color of a mesh vertex.
-     * \param[in] iPoint - Mesh vertex index.
-     * \return Vertex color.
-     */
-    unsigned long GetVertexColors(unsigned long iPoint) const;
-    
-    /*!
-     * \brief Get the MPI colors of the marker vertices.
-     * \param[in] iMarker - Marker index.
-     * \return Vertex colors.
-     */
-    vector<unsigned long> GetMarkerVertexColors(unsigned short iMarker) const;
-    
-    /*!
-     * \brief Get the MPI color of a marker vertex.
-     * \param[in] iMarker - Marker index.
-     * \param[in] iVertex - Marker vertex index.
-     * \return Vertex color.
-     */
-    unsigned long GetMarkerVertexColors(unsigned short iMarker, unsigned long iVertex) const;
-    
     /*!
      * \brief Get the halo flags of the mesh vertices.
      * \return Vertex domain flags.
diff --git a/Common/src/drivers/CDriverBase.cpp b/Common/src/drivers/CDriverBase.cpp
index 01eccb23448..5702cf51513 100644
--- a/Common/src/drivers/CDriverBase.cpp
+++ b/Common/src/drivers/CDriverBase.cpp
@@ -222,58 +222,6 @@ unsigned long CDriverBase::GetMarkerElementIDs(unsigned short iMarker, unsigned
     return main_geometry->bound[iMarker][iBound]->GetGlobalIndex();
 }
 
-vector<unsigned long> CDriverBase::GetElementColors() const {
-    const auto nElem = GetNumberElements();
-
-    vector<unsigned long> values;
-
-    for (auto iElem = 0ul; iElem < nElem; iElem++) {
-        values.push_back(GetElementColors(iElem));
-    }
-    
-    return values;
-}
-
-unsigned long CDriverBase::GetElementColors(unsigned long iElem) const {
-    if (iElem >= GetNumberElements()) {
-        SU2_MPI::Error("Element index exceeds size.", CURRENT_FUNCTION);
-    }
-    
-    return main_geometry->elem[iElem]->GetColor();
-}
-
-vector<unsigned long> CDriverBase::GetMarkerElementColors(unsigned short iMarker) const {
-    const auto nBound = GetNumberMarkerElements(iMarker);
-
-    vector<unsigned long> values;
-    
-    for (auto iBound = 0ul; iBound < nBound; iBound++) {
-        values.push_back(GetMarkerElementColors(iMarker, iBound));
-    }
-    
-    return values;
-}
-
-unsigned long CDriverBase::GetMarkerElementColors(unsigned short iMarker, unsigned long iBound) const {
-    if (iBound >= GetNumberMarkerElements(iMarker)) {
-        SU2_MPI::Error("Marker element index exceeds size.", CURRENT_FUNCTION);
-    }
-
-    return main_geometry->bound[iMarker][iBound]->GetColor();
-}
-
-vector<vector<unsigned long>> CDriverBase::GetElementConnectivities() const {
-    const auto nElem = GetNumberElements();
-    
-    vector<vector<unsigned long>> values;
-    
-    for (auto iElem = 0ul; iElem < nElem; iElem++) {
-        values.push_back(GetElementConnectivities(iElem));
-    }
-    
-    return values;
-}
-
 vector<unsigned long> CDriverBase::GetElementConnectivities(unsigned long iElem) const {
     if (iElem >= GetNumberElements()) {
         SU2_MPI::Error("Element index exceeds size.", CURRENT_FUNCTION);
@@ -284,7 +232,9 @@ vector<unsigned long> CDriverBase::GetElementConnectivities(unsigned long iElem)
     vector<unsigned long> values; 
 
     for (auto iNode = 0u; iNode < nNode; iNode++) {
-        values.push_back(main_geometry->elem[iElem]->GetNode(iNode));
+        unsigned long iPoint = main_geometry->elem[iElem]->GetNode(iNode);
+
+        values.push_back(main_geometry->nodes->GetGlobalIndex(iPoint));
     }
     
     return values;
@@ -312,7 +262,9 @@ vector<unsigned long> CDriverBase::GetMarkerElementConnectivities(unsigned short
     vector<unsigned long> values; 
 
     for (auto iNode = 0u; iNode < nNode; iNode++) {
-        values.push_back(main_geometry->bound[iMarker][iBound]->GetNode(iNode));
+        unsigned long iPoint = main_geometry->bound[iMarker][iBound]->GetNode(iNode);
+
+        values.push_back(main_geometry->nodes->GetGlobalIndex(iPoint));
     }
     
     return values;
@@ -416,44 +368,6 @@ unsigned long CDriverBase::GetMarkerVertexIDs(unsigned short iMarker, unsigned l
     return main_geometry->nodes->GetGlobalIndex(iPoint);
 }
 
-vector<unsigned long> CDriverBase::GetVertexColors() const {
-    const auto nPoint = GetNumberVertices();
-    
-    vector<unsigned long> values;
-    
-    for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
-        values.push_back(GetVertexColors(iPoint));
-    }
-    
-    return values;
-}
-
-unsigned long CDriverBase::GetVertexColors(unsigned long iPoint) const {
-    if (iPoint >= GetNumberVertices()) {
-        SU2_MPI::Error("Vertex index exceeds size.", CURRENT_FUNCTION);
-    }
-
-    return main_geometry->nodes->GetColor(iPoint);
-}
-
-vector<unsigned long> CDriverBase::GetMarkerVertexColors(unsigned short iMarker) const {
-    const auto nVertex = GetNumberMarkerVertices(iMarker);
-    
-    vector<unsigned long> values;
-    
-    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        values.push_back(GetMarkerVertexColors(iMarker, iVertex));
-    }
-    
-    return values;
-}
-
-unsigned long CDriverBase::GetMarkerVertexColors(unsigned short iMarker, unsigned long iVertex) const {
-    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
-    
-    return main_geometry->nodes->GetColor(iPoint);
-}
-
 vector<bool> CDriverBase::GetDomain() const {
     const auto nPoint = GetNumberVertices();
 
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index e44a0e6781b..279470e0fcf 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -1139,26 +1139,6 @@ void CDriver::Inlet_Preprocessing(CSolver ***solver, CGeometry **geometry,
                      string("Please set SPECIFIED_INLET_PROFILE= NO and try again."), CURRENT_FUNCTION);
     }
 
-  } else {
-
-    /*--- Uniform inlets or python-customized inlets ---*/
-
-    /* --- Initialize quantities for inlet boundary
-     * This routine does not check if the python wrapper is being used to
-     * set custom boundary conditions.  This is intentional; the
-     * default values for python custom BCs are initialized with the default
-     * values specified in the config (avoiding non physical values) --- */
-
-    for (unsigned short iMesh = 0; iMesh <= config->GetnMGLevels(); iMesh++) {
-      for(unsigned short iMarker=0; iMarker < config->GetnMarker_All(); iMarker++) {
-        if (solver[iMesh][FLOW_SOL]) solver[iMesh][FLOW_SOL]->SetUniformInlet(config, iMarker);
-        if (solver[iMesh][TURB_SOL]) solver[iMesh][TURB_SOL]->SetUniformInlet(config, iMarker);
-        if (solver[iMesh][SPECIES_SOL]) solver[iMesh][SPECIES_SOL]->SetUniformInlet(config, iMarker);
-      }
-    }
-
-  }
-
 }
 
 void CDriver::Solver_Restart(CSolver ***solver, CGeometry **geometry,

From 3f0247625a9510232edf439297d7295888c6a3ed Mon Sep 17 00:00:00 2001
From: aa-g <aa.gastaldi@pm.me>
Date: Mon, 11 Apr 2022 20:15:52 +0200
Subject: [PATCH 028/656] Fix small inconsistency in naming of Getters/Setters

---
 Common/include/drivers/CDriverBase.hpp |  4 +--
 Common/src/drivers/CDriverBase.cpp     | 38 +++++++++++++++++---------
 2 files changed, 27 insertions(+), 15 deletions(-)

diff --git a/Common/include/drivers/CDriverBase.hpp b/Common/include/drivers/CDriverBase.hpp
index 5a78918ec67..1fa0d011ca2 100644
--- a/Common/include/drivers/CDriverBase.hpp
+++ b/Common/include/drivers/CDriverBase.hpp
@@ -251,7 +251,7 @@ class CDriverBase {
      * \param[in] iMarker - Marker index.
      * \return Mesh vertex indices.
      */
-    vector<unsigned long> GetMarkerVertexIndex(unsigned short iMarker) const;
+    vector<unsigned long> GetMarkerVertexIndices(unsigned short iMarker) const;
     
     /*!
      * \brief Get the mesh vertex index of a marker vertex.
@@ -259,7 +259,7 @@ class CDriverBase {
      * \param[in] iVertex - Marker vertex index.
      * \return Mesh vertex index.
      */
-    unsigned long GetMarkerVertexIndex(unsigned short iMarker, unsigned long iVertex) const;
+    unsigned long GetMarkerVertexIndices(unsigned short iMarker, unsigned long iVertex) const;
     
     /*!
      * \brief Get the global IDs of the mesh vertices.
diff --git a/Common/src/drivers/CDriverBase.cpp b/Common/src/drivers/CDriverBase.cpp
index 5702cf51513..b778a6ab99b 100644
--- a/Common/src/drivers/CDriverBase.cpp
+++ b/Common/src/drivers/CDriverBase.cpp
@@ -222,6 +222,18 @@ unsigned long CDriverBase::GetMarkerElementIDs(unsigned short iMarker, unsigned
     return main_geometry->bound[iMarker][iBound]->GetGlobalIndex();
 }
 
+vector<vector<unsigned long>> CDriverBase::GetElementConnectivities() const {
+    const auto nElem = GetNumberElements();
+    
+    vector<vector<unsigned long>> values;
+
+    for (auto iElem = 0ul; iElem < nElem; iElem++) {
+        values.push_back(GetElementConnectivities(iElem));
+    }
+    
+    return values;
+}
+
 vector<unsigned long> CDriverBase::GetElementConnectivities(unsigned long iElem) const {
     if (iElem >= GetNumberElements()) {
         SU2_MPI::Error("Element index exceeds size.", CURRENT_FUNCTION);
@@ -300,7 +312,7 @@ unsigned long CDriverBase::GetNumberMarkerHaloVertices(unsigned short iMarker) c
     unsigned long nHalo = 0;
     
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+        auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
         
         if (!(main_geometry->nodes->GetDomain(iPoint))) {
             nHalo += 1;
@@ -310,19 +322,19 @@ unsigned long CDriverBase::GetNumberMarkerHaloVertices(unsigned short iMarker) c
     return nHalo;
 }
 
-vector<unsigned long> CDriverBase::GetMarkerVertexIndex(unsigned short iMarker) const {
+vector<unsigned long> CDriverBase::GetMarkerVertexIndices(unsigned short iMarker) const {
     const auto nVertex = GetNumberMarkerVertices(iMarker);
     
     vector<unsigned long> values;
 
     for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        values.push_back(GetMarkerVertexIndex(iMarker, iVertex));
+        values.push_back(GetMarkerVertexIndices(iMarker, iVertex));
     }
     
     return values;
 }
 
-unsigned long CDriverBase::GetMarkerVertexIndex(unsigned short iMarker, unsigned long iVertex) const {
+unsigned long CDriverBase::GetMarkerVertexIndices(unsigned short iMarker, unsigned long iVertex) const {
     if (iVertex >= GetNumberMarkerVertices(iMarker)) {
         SU2_MPI::Error("Marker vertex index exceeds size.", CURRENT_FUNCTION);
     }
@@ -363,7 +375,7 @@ vector<unsigned long> CDriverBase::GetMarkerVertexIDs(unsigned short iMarker) co
 }
 
 unsigned long CDriverBase::GetMarkerVertexIDs(unsigned short iMarker, unsigned long iVertex) const {
-    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+    auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
 
     return main_geometry->nodes->GetGlobalIndex(iPoint);
 }
@@ -401,7 +413,7 @@ vector<bool> CDriverBase::GetMarkerDomain(unsigned short iMarker) const {
 }
 
 bool CDriverBase::GetMarkerDomain(unsigned short iMarker, unsigned long iVertex) const {
-    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+    auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
     
     return main_geometry->nodes->GetDomain(iPoint);
 }
@@ -451,7 +463,7 @@ vector<vector<passivedouble>> CDriverBase::GetMarkerInitialCoordinates(unsigned
 }
 
 vector<passivedouble> CDriverBase::GetMarkerInitialCoordinates(unsigned short iMarker, unsigned long iVertex) const {
-    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+    auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
 
     vector<passivedouble> values(nDim, 0.0);
 
@@ -509,7 +521,7 @@ vector<vector<passivedouble>> CDriverBase::GetMarkerCoordinates(unsigned short i
 }
 
 vector<passivedouble> CDriverBase::GetMarkerCoordinates(unsigned short iMarker, unsigned long iVertex) const {
-    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+    auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
 
     vector<passivedouble> values;
     
@@ -561,7 +573,7 @@ void CDriverBase::SetMarkerCoordinates(unsigned short iMarker, vector<vector<pas
 }
 
 void CDriverBase::SetMarkerCoordinates(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
-    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+    auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
 
     if (values.size() != nDim) {
         SU2_MPI::Error("Invalid number of dimensions !", CURRENT_FUNCTION);
@@ -585,7 +597,7 @@ vector<vector<passivedouble>> CDriverBase::GetMarkerDisplacements(unsigned short
 }
 
 vector<passivedouble> CDriverBase::GetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex) const {
-    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+    auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
 
     vector<passivedouble> values (nDim, 0.0);
     
@@ -623,7 +635,7 @@ void CDriverBase::SetMarkerDisplacements(unsigned short iMarker, unsigned long i
         SU2_MPI::Error("Mesh solver is not defined !", CURRENT_FUNCTION);
     }
 
-    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+    auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
 
     if (values.size() != nDim) {
         SU2_MPI::Error("Invalid number of dimensions !", CURRENT_FUNCTION);
@@ -647,7 +659,7 @@ vector<vector<passivedouble>> CDriverBase::GetMarkerVelocities(unsigned short iM
 }
 
 vector<passivedouble> CDriverBase::GetMarkerVelocities(unsigned short iMarker, unsigned long iVertex) const {
-    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+    auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
 
     vector<passivedouble> values (nDim, 0.0);
     
@@ -685,7 +697,7 @@ void CDriverBase::SetMarkerVelocities(unsigned short iMarker, unsigned long iVer
         SU2_MPI::Error("Mesh solver is not defined !", CURRENT_FUNCTION);
     }
 
-    auto iPoint = GetMarkerVertexIndex(iMarker, iVertex);
+    auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
 
     if (values.size() != nDim) {
         SU2_MPI::Error("Invalid number of dimensions !", CURRENT_FUNCTION);

From 01bb85b8f9ef6f76e0a7a2757e87ebdde8a814cc Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 12 Sep 2022 16:03:56 +0200
Subject: [PATCH 029/656] Added MLP classes to numerics folder

---
 .../numerics/multilayer_perceptron/IOMap.hpp  |  80 +++++
 .../numerics/multilayer_perceptron/Layer.hpp  |  63 ++++
 .../multilayer_perceptron/LookUp_ANN.hpp      | 131 +++++++
 .../multilayer_perceptron/NeuralNetwork.hpp   | 174 +++++++++
 .../numerics/multilayer_perceptron/Neuron.hpp |  74 ++++
 .../ReadNeuralNetwork.hpp                     |  74 ++++
 SU2_CFD/obj/Makefile.am                       |   6 +
 SU2_CFD/src/meson.build                       |   8 +-
 .../numerics/multilayer_perceptron/IOMap.cpp  |  60 ++++
 .../numerics/multilayer_perceptron/Layer.cpp  |  62 ++++
 .../multilayer_perceptron/LookUp_ANN.cpp      | 268 ++++++++++++++
 .../multilayer_perceptron/NeuralNetwork.cpp   | 332 ++++++++++++++++++
 .../numerics/multilayer_perceptron/Neuron.cpp | 114 ++++++
 .../ReadNeuralNetwork.cpp                     | 151 ++++++++
 14 files changed, 1596 insertions(+), 1 deletion(-)
 create mode 100644 SU2_CFD/include/numerics/multilayer_perceptron/IOMap.hpp
 create mode 100644 SU2_CFD/include/numerics/multilayer_perceptron/Layer.hpp
 create mode 100644 SU2_CFD/include/numerics/multilayer_perceptron/LookUp_ANN.hpp
 create mode 100644 SU2_CFD/include/numerics/multilayer_perceptron/NeuralNetwork.hpp
 create mode 100644 SU2_CFD/include/numerics/multilayer_perceptron/Neuron.hpp
 create mode 100644 SU2_CFD/include/numerics/multilayer_perceptron/ReadNeuralNetwork.hpp
 create mode 100644 SU2_CFD/src/numerics/multilayer_perceptron/IOMap.cpp
 create mode 100644 SU2_CFD/src/numerics/multilayer_perceptron/Layer.cpp
 create mode 100644 SU2_CFD/src/numerics/multilayer_perceptron/LookUp_ANN.cpp
 create mode 100644 SU2_CFD/src/numerics/multilayer_perceptron/NeuralNetwork.cpp
 create mode 100644 SU2_CFD/src/numerics/multilayer_perceptron/Neuron.cpp
 create mode 100644 SU2_CFD/src/numerics/multilayer_perceptron/ReadNeuralNetwork.cpp

diff --git a/SU2_CFD/include/numerics/multilayer_perceptron/IOMap.hpp b/SU2_CFD/include/numerics/multilayer_perceptron/IOMap.hpp
new file mode 100644
index 00000000000..66878762edb
--- /dev/null
+++ b/SU2_CFD/include/numerics/multilayer_perceptron/IOMap.hpp
@@ -0,0 +1,80 @@
+/*!
+ * \file IOMap.hpp
+ * \brief Declaration of input-to-output mapping class for artifical neural networks
+ * \author E. Bunschoten
+ * \version 7.4.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+#pragma once
+
+#include <cmath>
+#include <string>
+#include <iostream>
+#include <limits>
+#include <cstdlib>
+#include <vector>
+#include "../../../../Common/include/CConfig.hpp"
+#include "../../../../Common/include/linear_algebra/blas_structure.hpp"
+#include "LookUp_ANN.hpp"
+
+using namespace std;
+class LookUp_ANN;
+
+class IOMap
+{
+    private:
+    vector<size_t> ANN_indices;
+    vector<vector<pair<size_t, size_t>>> Input_Map;
+    vector<vector<pair<size_t, size_t>>> Output_Map;
+    vector<vector<su2double>> input_indices;
+    public:
+    IOMap(){};
+    IOMap(LookUp_ANN*ANN_collection, vector<string> &inputs, vector<string> &outputs);
+    ~IOMap(){};
+    void Push_ANN_index(size_t i_ANN){ANN_indices.push_back(i_ANN);};
+    void PairVariableswithANNs(LookUp_ANN * ANN_collection, vector<string> &inputs, vector<string> &outputs);
+    size_t GetNANNs(){return ANN_indices.size();}
+    size_t GetANNIndex(size_t i_Map){return ANN_indices[i_Map];}
+    size_t GetInputIndex(size_t i_Map, size_t iInput){return Input_Map[i_Map][iInput].first;}
+    size_t GetOutputIndex(size_t i_Map, size_t iOutput){return Output_Map[i_Map][iOutput].first;}
+    vector<pair<size_t, size_t>> GetOutputMapping(size_t i_map){return Output_Map[i_map];}
+    vector<pair<size_t, size_t>> GetInputMapping(size_t i_map){return Input_Map[i_map];}
+    
+    vector<su2double> GetANN_Inputs(size_t i_Map, vector<su2double>&inputs){
+        vector<su2double> ANN_input;
+        ANN_input.resize(Input_Map[i_Map].size());
+
+        for(size_t iInput=0; iInput<Input_Map[i_Map].size(); iInput++){
+            ANN_input.at(iInput) = inputs[GetInputIndex(i_Map, iInput)];
+        }
+        return ANN_input;
+    }
+    vector<su2double*> GetANN_Outputs(size_t i_Map, vector<su2double*>&outputs){
+        vector<su2double*> ANN_output;
+        ANN_output.resize(Output_Map[i_Map].size());
+
+        for(size_t iOutput=0; iOutput<Output_Map[i_Map].size(); iOutput++){
+            ANN_output.at(iOutput) = outputs[GetOutputIndex(i_Map, iOutput)];
+        }
+        return ANN_output;
+    }
+};
\ No newline at end of file
diff --git a/SU2_CFD/include/numerics/multilayer_perceptron/Layer.hpp b/SU2_CFD/include/numerics/multilayer_perceptron/Layer.hpp
new file mode 100644
index 00000000000..892654901e9
--- /dev/null
+++ b/SU2_CFD/include/numerics/multilayer_perceptron/Layer.hpp
@@ -0,0 +1,63 @@
+/*!
+ * \file Layer.hpp
+ * \brief Declaration of artificial neural network interpolation class
+ * \author E. Bunschoten
+ * \version 7.4.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+#pragma once
+
+#include <cmath>
+#include <iostream>
+#include <limits>
+#include <cstdlib>
+
+#include "../../../../Common/include/CConfig.hpp"
+#include "Neuron.hpp"
+#include "../../../../Common/include/linear_algebra/blas_structure.hpp"
+using namespace std;
+
+class Layer
+{
+private:
+    unsigned long number_of_neurons;
+    Neuron * neurons;
+    bool input;
+    string activation_type;
+public:
+    Layer();
+    Layer(unsigned long n_neurons);
+    void setNNeurons(unsigned long n_neurons);
+    unsigned long getNNeurons(){return number_of_neurons;};
+    void sayhi();
+    void setInput(bool def){input = def;};
+    bool isInput(){return input;};
+    void setValue(size_t i_neuron, su2double value){neurons[i_neuron].setValue(value);}
+    su2double getValue(size_t i_neuron){return neurons[i_neuron].getValue();}
+    void setBias(size_t i_neuron, su2double value){neurons[i_neuron].setBias(value);}
+    su2double getBias(size_t i_neuron){return neurons[i_neuron].getBias();}
+    su2double getdYdX(size_t i_neuron){return neurons[i_neuron].getGradient();}
+    string getActivationType(){return activation_type;}
+    ~Layer(){
+        delete [] neurons;
+    };
+};
diff --git a/SU2_CFD/include/numerics/multilayer_perceptron/LookUp_ANN.hpp b/SU2_CFD/include/numerics/multilayer_perceptron/LookUp_ANN.hpp
new file mode 100644
index 00000000000..9cab1a9204c
--- /dev/null
+++ b/SU2_CFD/include/numerics/multilayer_perceptron/LookUp_ANN.hpp
@@ -0,0 +1,131 @@
+/*!
+ * \file LookUp_ANN.hpp
+ * \brief Declaration of artificial neural network interpolation class
+ * \author E. Bunschoten
+ * \version 7.4.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+
+#pragma once
+
+#include <cmath>
+#include <string>
+#include <iostream>
+#include <limits>
+#include <cstdlib>
+#include <vector>
+#include "../../../../Common/include/CConfig.hpp"
+#include "../../../../Common/include/linear_algebra/blas_structure.hpp"
+#include "NeuralNetwork.hpp"
+#include "IOMap.hpp"
+
+using namespace std;
+class IOMap;
+
+class LookUp_ANN
+{
+    private:
+    int rank{0};
+    vector<NeuralNetwork*> NeuralNetworks;  /*!< Vector containing all loaded neural networks. */
+
+    vector<string> ANN_filenames;       /*!< Filenames containing ANN architecture information. */
+
+    unsigned long number_of_variables;  /*!< Number of loaded ANNs. */
+
+    /*!
+   * \brief Skip to certain flag in file.
+   * \param[in] file_stream - input stream of file
+   * \param[in] flag - line to search for
+   * \return line in file.
+   */
+    string SkipToFlag(ifstream *file_stream, string flag); 
+
+    /*!
+    * \brief Load ANN architecture
+    * \param[in] ANN - pointer to target NeuralNetwork class
+    * \param[in] filename - filename containing ANN architecture information
+    */
+    void GenerateANN(NeuralNetwork*ANN, string filename);
+
+    /*!
+    * \brief Read ANN architecture input file
+    * \param[in] filename - filename containing ANN architecture information
+    */
+    void ReadANNInputFile(string fileName); 
+    
+    public: 
+    
+    /*!
+    * \brief ANN collection class constructor
+    * \param[in] filename - filename containing list of ANN input files
+    */
+    LookUp_ANN(string fileName);
+    
+    /*!
+    * \brief Evaluate loaded ANNs for given inputs and outputs
+    * \param[in] input_output_map - input-output map coupling desired inputs and outputs to loaded ANNs
+    * \param[in] inputs - input values
+    * \param[in] outputs - pointers to output variables
+    */
+    void Predict_ANN(IOMap *input_output_map, vector<su2double> &inputs, vector<su2double*> &outputs);
+
+    ~LookUp_ANN(){for(size_t i_ANN=0; i_ANN<number_of_variables; i_ANN++)
+        delete NeuralNetworks.at(i_ANN);
+    };
+
+    /*!
+    * \brief Get number of loaded ANNs
+    * \return number of loaded ANNs
+    */
+    const size_t GetNANNs() const {return NeuralNetworks.size();}
+
+    /*!
+    * \brief Check if variables occur more than once in ANN outputs
+    * \param[in] output_names - output variable names to check
+    * \param[in] input_output_map - pointer to input-output map to be checked
+    */
+    bool Check_Duplicate_Outputs(vector<string> &output_names, IOMap *input_output_map) const;
+
+    /*!
+    * \brief Check if all output variables are present in the loaded ANNs
+    * \param[in] output_names - output variable names to check
+    * \param[in] input_output_map - pointer to input-output map to be checked
+    */
+    bool Check_Use_of_Outputs(vector<string> &output_names, IOMap *input_output_map) const;
+
+    /*!
+    * \brief Check if all input variables are present in the loaded ANNs
+    * \param[in] input_names - input variable names to check
+    * \param[in] input_output_map - pointer to input-output map to be checked
+    */
+    bool Check_Use_of_Inputs(vector<string> &input_names, IOMap *input_output_map) const;
+
+    /*!
+    * \brief Map variable names to ANN inputs or outputs
+    * \param[in] i_ANN - loaded ANN index
+    * \param[in] variable_names - variable names to map to ANN inputs or outputs
+    * \param[in] input - map to inputs (true) or outputs (false)
+    */
+    vector<pair<size_t, size_t>> FindVariable_Indices(size_t i_ANN, vector<string> variable_names, bool input) const;
+    
+};  
+
diff --git a/SU2_CFD/include/numerics/multilayer_perceptron/NeuralNetwork.hpp b/SU2_CFD/include/numerics/multilayer_perceptron/NeuralNetwork.hpp
new file mode 100644
index 00000000000..682d673f5a6
--- /dev/null
+++ b/SU2_CFD/include/numerics/multilayer_perceptron/NeuralNetwork.hpp
@@ -0,0 +1,174 @@
+/*!
+ * \file NeuralNetwork.hpp
+ * \brief Declaration of the neural network class
+ * \author E. Bunschoten
+ * \version 7.4.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+
+#pragma once
+
+#include <cmath>
+#include <cstring>
+#include <iostream>
+#include <limits>
+#include <cstdlib>
+
+#include "../../../../Common/include/CConfig.hpp"
+#include "../../../../Common/include/linear_algebra/blas_structure.hpp"
+#include "Layer.hpp"
+
+using namespace std;
+class Activation_Function {
+    private:
+    public:
+    Activation_Function(){};
+    ~Activation_Function(){};
+    inline virtual su2double run_activation_function(su2double x) {return 0.0;}
+};
+
+class Linear : public Activation_Function {
+    private:
+    public:
+    Linear() : Activation_Function() {};
+    ~Linear(){};
+    su2double run_activation_function(su2double x) final {return x;}
+};
+
+class Relu : public Activation_Function {
+    private:
+    public:
+    Relu() : Activation_Function() {};
+    ~Relu(){};
+    su2double run_activation_function(su2double x) final {return max(0.0, x);}
+};
+
+class SmoothSlope : public Activation_Function {
+    private:
+    su2double tanhx;
+    public:
+    SmoothSlope() : Activation_Function() {};
+    ~SmoothSlope(){};
+    su2double run_activation_function(su2double x) final {tanhx = tanh(x); return max(tanhx, x);}
+};
+
+class None : public Activation_Function {
+    private:
+    public:
+    None() : Activation_Function() {};
+    ~None(){};
+    su2double run_activation_function(su2double x) final {return 0.0;}
+};
+
+class NeuralNetwork
+{
+private:
+    vector<string> input_names;
+    vector<string> output_names;
+
+    unsigned long n_hidden_layers;
+    Layer *inputLayer;
+    Layer *outputLayer;
+    vector< Layer *> hiddenLayers; 
+    vector<Layer *>total_layers;
+
+    vector<vector<vector<su2double>>> weights;
+    vector<su2activematrix> weights_mat;
+    vector<vector<su2double>> values;
+
+    vector<pair<su2double, su2double>> input_norm;
+    vector<pair<su2double, su2double>> output_norm;
+    vector<su2double> last_inputs;
+
+    enum ENUM_ACTIVATION_FUNCTION {
+        NONE=0,
+        LINEAR=1,
+        RELU=2,
+        SMOOTH_SLOPE=3,
+        ELU = 4
+    };
+    ENUM_ACTIVATION_FUNCTION * activation_function_types;
+    vector<Activation_Function*> activation_functions;
+    Activation_Function* current_activation_function;
+    //Activation_Function *activation_functions;
+public:
+    NeuralNetwork();
+    ~NeuralNetwork(){
+        for(size_t i=0; i<total_layers.size(); i++){
+            delete total_layers.at(i);
+        }
+    };
+    void defineInputLayer(unsigned long n_neurons);
+    void defineOutputLayer(unsigned long n_neurons);
+    void push_hidden_layer(unsigned long n_neurons);
+    void setWeight(unsigned long i_layer, unsigned long i_neuron, unsigned long j_neuron, su2double value);
+    void setBias(unsigned long i_layer, unsigned long i_neuron, su2double value){total_layers.at(i_layer)->setBias(i_neuron, value);}
+    void setActivationFunction(unsigned long i_layer, string input);
+    void displayNetwork();
+    void sizeWeights();
+    void sizeInputs(unsigned long n_inputs){last_inputs.resize(n_inputs); for(unsigned long iInput=0; iInput<n_inputs; iInput++) last_inputs.at(iInput) = 0.0;}
+    unsigned long getNWeightLayers(){return weights.size();}
+    unsigned long getNLayers(){return total_layers.size();}
+
+    unsigned long getNNeurons(unsigned long iLayer){;
+    return total_layers.at(iLayer)->getNNeurons();}
+    unsigned long getNNeurons(unsigned long iLayer, unsigned long iNeuron){return weights.at(iLayer).at(iNeuron).size();}
+
+    // su2double predict(su2double * X, size_t i_output);
+    // void predict(vector<su2double> &inputs, vector<su2double*> &outputs);
+    void predict(vector<su2double> &inputs, vector<su2double*> &outputs, su2double**doutputs_dinputs=nullptr);
+
+    //void predict_new(vector<su2double> &inputs, vector<su2double*> &outputs, su2double**doutputs_dinputs=nullptr);
+
+    void SetInputNorm(unsigned long iInput, su2double input_min, su2double input_max){input_norm.at(iInput) = make_pair(input_min, input_max);}
+    void SetOutputNorm(unsigned long iOutput, su2double output_min, su2double output_max){output_norm.at(iOutput) = make_pair(output_min, output_max);}
+    
+    void PushOutputName(string input){output_names.push_back(input);}
+    void PushInputName(string input){input_names.push_back(input);}
+   
+    string GetInputName(size_t iInput){return input_names[iInput];}
+    string GetOutputName(size_t iOutput){return output_names[iOutput];}
+
+    size_t GetnInputs(){return input_names.size();}
+    size_t GetnOutputs(){return output_names.size();}
+
+    void SizeActivationFunctions(unsigned long n_layers){activation_function_types = new ENUM_ACTIVATION_FUNCTION[n_layers]; activation_functions.resize(4); 
+    activation_functions[ENUM_ACTIVATION_FUNCTION::LINEAR] = new Linear(); 
+    activation_functions[ENUM_ACTIVATION_FUNCTION::RELU] = new Relu();
+    activation_functions[ENUM_ACTIVATION_FUNCTION::SMOOTH_SLOPE] = new SmoothSlope();
+    }
+
+    su2double ComputeX(size_t iLayer, size_t iNeuron){
+        su2double x;
+        x = total_layers[iLayer]->getBias(iNeuron);
+        size_t nNeurons_previous = total_layers[iLayer - 1]->getNNeurons();
+        for(size_t jNeuron=0; jNeuron<nNeurons_previous; jNeuron++){
+            x += weights_mat[iLayer - 1][iNeuron][jNeuron] * total_layers[iLayer-1]->getValue(jNeuron);
+        }
+        return x;
+    }
+    // su2double run_activation_function(unsigned long iLayer, su2double x){return activation_functions[iLayer]->run_activation_function(x);}
+    //void SetActivationFunction(size_t iLayer, unsigned long function_index){activation_functions[iLayer] = ENUM_ACTIVATION_FUNCTION(function_index);}
+};
+
+
+
diff --git a/SU2_CFD/include/numerics/multilayer_perceptron/Neuron.hpp b/SU2_CFD/include/numerics/multilayer_perceptron/Neuron.hpp
new file mode 100644
index 00000000000..12e1012b09a
--- /dev/null
+++ b/SU2_CFD/include/numerics/multilayer_perceptron/Neuron.hpp
@@ -0,0 +1,74 @@
+/*!
+ * \file LookUp_ANN.hpp
+ * \brief Declaration of artificial neural network perceptron class
+ * \author E. Bunschoten
+ * \version 7.4.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+#pragma once
+
+#include <cmath>
+#include <iostream>
+#include <limits>
+#include <cstdlib>
+
+#include "../../../../Common/include/CConfig.hpp"
+#include "../../../../Common/include/linear_algebra/blas_structure.hpp"
+
+using namespace std;
+class Neuron
+{
+private:
+    string activation_type="SmoothSlope";
+    unsigned long ActivationFunction{ENUM_ACTIVATION_FUNCTION::LINEAR};
+    unsigned long i_neuron;
+    double value;
+    su2double dy_dx;
+    double bias{0};
+    enum ENUM_ACTIVATION_FUNCTION {
+        NONE=0,
+        LINEAR=1,
+        RELU=2,
+        SMOOTH_SLOPE=3
+    };
+
+public:
+    Neuron(){};
+    void setNumber(unsigned long input){i_neuron = input;}
+    unsigned long getNumber(){return i_neuron;}
+    //void setFunctionType(string input);
+
+    //string getFunctionType(){return activation_type;}
+    //su2double activation_function(su2double x);
+    void setValue(su2double input){value = input;}
+    su2double getValue(){return value;}
+
+    void setBias(su2double input){bias = input;}
+    su2double getBias(){return bias;}
+
+    su2double getGradient(){return dy_dx;}
+    void setGradient(su2double input){dy_dx = input;}
+    //void SetActivationFunction(unsigned long input){ActivationFunction = input;}
+
+    ~Neuron(){};
+};
+
diff --git a/SU2_CFD/include/numerics/multilayer_perceptron/ReadNeuralNetwork.hpp b/SU2_CFD/include/numerics/multilayer_perceptron/ReadNeuralNetwork.hpp
new file mode 100644
index 00000000000..e33d267cbe2
--- /dev/null
+++ b/SU2_CFD/include/numerics/multilayer_perceptron/ReadNeuralNetwork.hpp
@@ -0,0 +1,74 @@
+/*!
+ * \file ReadNeuralNetwork.hpp
+ * \brief Declaration of MLP input file reader class
+ * \author E. Bunschoten
+ * \version 7.4.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+#pragma once
+
+#include <cmath>
+#include <iostream>
+#include <limits>
+#include <cstdlib>
+
+#include "../../../../Common/include/CConfig.hpp"
+#include "../../../../Common/include/linear_algebra/blas_structure.hpp"
+
+using namespace std;
+class ReadNeuralNetwork {
+    private:
+    vector<string> input_names;
+    vector<string> output_names;
+
+    string filename;
+    unsigned long n_layers;
+    vector<unsigned long> n_neurons;
+    vector<vector<vector<double long>>> weights;
+    vector<vector<double long>> biases;
+    vector<string> activation_functions;
+
+    vector<pair<double long, double long>> input_norm;
+    vector<pair<double long, double long>> output_norm;
+    public:
+
+    ReadNeuralNetwork(string filename_in);
+    void ReadMLPFile();
+
+    string SkipToFlag(ifstream *file_stream, string flag);
+    
+    unsigned long GetNInputs(){return n_neurons.at(0);}
+    unsigned long GetNOutputs(){return n_neurons.at(n_layers - 1);}
+
+    unsigned long GetNlayers(){return n_layers;}
+    unsigned long GetNneurons(size_t iLayer){return n_neurons.at(iLayer);}
+    double long GetWeight(size_t iLayer, size_t iNeuron, size_t jNeuron){return weights.at(iLayer).at(iNeuron).at(jNeuron);}
+    double long GetBias(size_t iLayer, size_t iNeuron){return biases.at(iLayer).at(iNeuron);}
+    pair<double long, double long> GetInputNorm(size_t iInput){return input_norm.at(iInput);}
+    pair<double long, double long> GetOutputNorm(size_t iOutput){return output_norm.at(iOutput);}
+    string GetActivationFunction(size_t iLayer){return activation_functions.at(iLayer);}
+
+    string GetInputName(size_t iInput){return input_names.at(iInput);}
+    string GetOutputName(size_t iOutput){return output_names.at(iOutput);}
+    
+    ~ReadNeuralNetwork(){};
+};
\ No newline at end of file
diff --git a/SU2_CFD/obj/Makefile.am b/SU2_CFD/obj/Makefile.am
index 8d1e64e48cd..140433ec93a 100644
--- a/SU2_CFD/obj/Makefile.am
+++ b/SU2_CFD/obj/Makefile.am
@@ -116,6 +116,12 @@ libSU2Core_sources = ../src/definition_structure.cpp \
   ../src/numerics/elasticity/CFEALinearElasticity.cpp \
   ../src/numerics/elasticity/CFEANonlinearElasticity.cpp \
   ../src/numerics/elasticity/nonlinear_models.cpp \
+  ../src/numerics/multilayer_perceptron/LookUp_ANN.cpp \
+  ../src/numerics/multilayer_perceptron/IOMap.cpp \
+  ../src/numerics/multilayer_perceptron/NeuralNetwork.cpp \
+  ../src/numerics/multilayer_perceptron/Neuron.cpp \
+  ../src/numerics/multilayer_perceptron/Layer.cpp \
+  ../src/numerics/multilayer_perceptron/ReadNeuralNetwork.cpp \
   ../include/numerics_simd/CNumericsSIMD.cpp \
   ../src/output/filewriter/CCSVFileWriter.cpp \
   ../src/output/filewriter/CSTLFileWriter.cpp \
diff --git a/SU2_CFD/src/meson.build b/SU2_CFD/src/meson.build
index 691db4e5b2d..6e730d80ffc 100644
--- a/SU2_CFD/src/meson.build
+++ b/SU2_CFD/src/meson.build
@@ -147,7 +147,13 @@ su2_cfd_src += files(['numerics/CNumerics.cpp',
                       'numerics/elasticity/CFEALinearElasticity.cpp',
                       'numerics/elasticity/CFEANonlinearElasticity.cpp',
                       'numerics/elasticity/nonlinear_models.cpp',
-                      'numerics/CGradSmoothing.cpp'])
+                      'numerics/CGradSmoothing.cpp',
+                      'numerics/multilayer_perceptron/LookUp_ANN.cpp',
+                      'numerics/multilayer_perceptron/IOMap.cpp',
+                      'numerics/multilayer_perceptron/NeuralNetwork.cpp',
+                      'numerics/multilayer_perceptron/Layer.cpp',
+                      'numerics/multilayer_perceptron/Neuron.cpp',
+                      'numerics/multilayer_perceptron/ReadNeuralNetwork.cpp'])
 
 su2_cfd_src += files(['../include/numerics_simd/CNumericsSIMD.cpp'])
 
diff --git a/SU2_CFD/src/numerics/multilayer_perceptron/IOMap.cpp b/SU2_CFD/src/numerics/multilayer_perceptron/IOMap.cpp
new file mode 100644
index 00000000000..82d2faf1965
--- /dev/null
+++ b/SU2_CFD/src/numerics/multilayer_perceptron/IOMap.cpp
@@ -0,0 +1,60 @@
+/*!
+ * \file IOMap.cpp
+ * \brief Implementation of the input-output mapping class for the 
+ *      use of multi-layer perceptrons in SU2
+ * \author E. Bunschoten
+ * \version 7.4.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+#include "../../../include/numerics/multilayer_perceptron/LookUp_ANN.hpp"
+#include "../../../include/numerics/multilayer_perceptron/IOMap.hpp"
+#include <iostream>
+#include <string>
+#include <cmath>
+#include <fstream>
+
+IOMap::IOMap(LookUp_ANN*ANN_collection, vector<string> &inputs, vector<string> &outputs){
+    PairVariableswithANNs(ANN_collection, inputs, outputs);
+    if(outputs.size() > 0){
+        ANN_collection->Check_Use_of_Inputs(inputs, this);
+        ANN_collection->Check_Use_of_Outputs(outputs, this);
+        ANN_collection->Check_Duplicate_Outputs(outputs, this);
+    }
+}
+void IOMap::PairVariableswithANNs(LookUp_ANN*ANN_collection, vector<string> &inputs, vector<string> &outputs){
+
+    bool isInput, isOutput,input_match;
+    for(size_t i_ANN=0; i_ANN<ANN_collection->GetNANNs(); i_ANN++){
+        vector<pair<size_t, size_t>> Input_Indices = ANN_collection->FindVariable_Indices(i_ANN, inputs, true);
+        isInput = Input_Indices.size() > 0;
+        if(isInput){
+            input_match = true;
+            vector<pair<size_t, size_t>> Output_Indices = ANN_collection->FindVariable_Indices(i_ANN, outputs, false);
+            isOutput = Output_Indices.size() > 0;
+            if(isOutput){
+                ANN_indices.push_back(i_ANN);
+                Input_Map.push_back(Input_Indices);
+                Output_Map.push_back(Output_Indices);
+            }
+        }
+    }
+}
\ No newline at end of file
diff --git a/SU2_CFD/src/numerics/multilayer_perceptron/Layer.cpp b/SU2_CFD/src/numerics/multilayer_perceptron/Layer.cpp
new file mode 100644
index 00000000000..b666e4547d3
--- /dev/null
+++ b/SU2_CFD/src/numerics/multilayer_perceptron/Layer.cpp
@@ -0,0 +1,62 @@
+/*!
+ * \file Layer.cpp
+ * \brief Implementation of the Layer class to be used in the NeuralNetwork
+ *      class
+ * \author E. Bunschoten
+ * \version 7.4.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+#include "../../../include/numerics/multilayer_perceptron/Layer.hpp"
+#include <cstring>
+using namespace std;
+
+Layer::Layer() : Layer(1) {};
+
+Layer::Layer(unsigned long n_neurons) : number_of_neurons{n_neurons}, input{false}
+{
+    neurons = new Neuron[n_neurons];
+    for(size_t i=0; i<number_of_neurons; i++){
+        neurons[i].setNumber(i+1);
+    }
+}
+
+void Layer::setNNeurons(unsigned long n_neurons){
+    if(number_of_neurons != n_neurons){
+        delete [] neurons;
+        neurons = new Neuron[n_neurons];
+        for(size_t i=0; i<number_of_neurons; i++){
+            neurons[i].setNumber(i+1);
+        }
+    }
+}
+
+// void Layer::setActivationFunction(string input){
+//     activation_type = input;
+//     for(size_t i=0; i<number_of_neurons; i++){
+//         neurons[i].setFunctionType(input);
+//     }
+// }
+// void Layer::sayhi(){
+//     for(size_t i=0; i<number_of_neurons; i++){
+//         neurons[i].sayhi();
+//     }
+// }
diff --git a/SU2_CFD/src/numerics/multilayer_perceptron/LookUp_ANN.cpp b/SU2_CFD/src/numerics/multilayer_perceptron/LookUp_ANN.cpp
new file mode 100644
index 00000000000..26c4c02e645
--- /dev/null
+++ b/SU2_CFD/src/numerics/multilayer_perceptron/LookUp_ANN.cpp
@@ -0,0 +1,268 @@
+/*!
+ * \file LookUp_ANN.cpp
+ * \brief Implementation of the multi-layer perceptron class to be 
+ *      used for look-up operations.
+ * \author E. Bunschoten
+ * \version 7.4.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+#include "../../../include/numerics/multilayer_perceptron/LookUp_ANN.hpp"
+#include "../../../include/numerics/multilayer_perceptron/IOMap.hpp"
+#include "../../../include/numerics/multilayer_perceptron/ReadNeuralNetwork.hpp"
+#include <iostream>
+#include <string>
+#include <cmath>
+#include <fstream>
+
+using namespace std;
+
+LookUp_ANN::LookUp_ANN(string inputFileName)
+{
+    
+    #ifdef HAVE_MPI
+    MPI_Comm_rank(MPI_COMM_WORLD, &rank);
+    #endif
+    if(rank == MASTER_NODE)
+        cout << "Generating ANN collection" << endl;
+
+    ReadANNInputFile(inputFileName);
+    for(size_t i_ANN=0; i_ANN<number_of_variables; i_ANN++){
+        
+        NeuralNetworks.at(i_ANN) = new NeuralNetwork;
+        if(rank == MASTER_NODE)
+            cout << "Generating neural network for " << ANN_filenames.at(i_ANN) << endl;
+        GenerateANN(NeuralNetworks.at(i_ANN), ANN_filenames.at(i_ANN));
+    }
+}
+
+
+vector<pair<size_t, size_t>> LookUp_ANN::FindVariable_Indices(size_t i_ANN, vector<string> variable_names, bool input) const {
+    vector<pair<size_t, size_t>> variable_indices;
+    size_t nVar = input ? NeuralNetworks[i_ANN]->GetnInputs() : NeuralNetworks[i_ANN]->GetnOutputs();
+
+    for(size_t iVar=0; iVar<nVar; iVar++){
+        for(size_t jVar=0; jVar<variable_names.size(); jVar++){
+            string ANN_varname = input ? NeuralNetworks[i_ANN]->GetInputName(iVar) : NeuralNetworks[i_ANN]->GetOutputName(iVar);
+            
+            if(variable_names.at(jVar).compare(ANN_varname) == 0){
+                variable_indices.push_back(make_pair(jVar, iVar));
+                //cout << variable_names[jVar] << " : " << jVar << " | " << ANN_varname << " : " << iVar << endl;
+            }
+        }
+    }
+    return variable_indices;
+}
+
+void LookUp_ANN::Predict_ANN(IOMap *input_output_map, vector<su2double>& inputs, vector<su2double*>& outputs){
+    for(size_t i_map=0; i_map<input_output_map->GetNANNs(); i_map++){
+        size_t i_ANN = input_output_map->GetANNIndex(i_map);
+        vector<su2double> ANN_inputs = input_output_map->GetANN_Inputs(i_map, inputs);
+        vector<su2double*> ANN_outputs = input_output_map->GetANN_Outputs(i_map, outputs);
+        NeuralNetworks[i_ANN]->predict(ANN_inputs, ANN_outputs);
+    }
+}
+void LookUp_ANN::GenerateANN(NeuralNetwork * ANN, string fileName)
+{
+    ReadNeuralNetwork Reader = ReadNeuralNetwork(fileName);
+    
+    // Read MLP input file
+    Reader.ReadMLPFile();
+
+    // Generate basic layer architectures
+    ANN->defineInputLayer(Reader.GetNInputs());
+    ANN->sizeInputs(Reader.GetNInputs());
+    for(size_t iInput=0; iInput<Reader.GetNInputs(); iInput++){
+        ANN->PushInputName(Reader.GetInputName(iInput));
+    }
+    for(size_t iLayer=1; iLayer<Reader.GetNlayers()-1; iLayer++){
+        ANN->push_hidden_layer(Reader.GetNneurons(iLayer));
+    }
+    ANN->defineOutputLayer(Reader.GetNOutputs());
+    for(size_t iOutput=0; iOutput<Reader.GetNOutputs(); iOutput++){
+        ANN->PushOutputName(Reader.GetOutputName(iOutput));
+    }
+
+    // Size weights of each layer
+    ANN->sizeWeights();
+
+    // Define weights and activation functions
+    ANN->SizeActivationFunctions(ANN->getNWeightLayers()+1);
+    for(size_t i_layer = 0; i_layer < ANN->getNWeightLayers(); i_layer++){
+        ANN->setActivationFunction(i_layer, Reader.GetActivationFunction(i_layer));
+        for(size_t i_neuron=0; i_neuron < ANN->getNNeurons(i_layer); i_neuron++){
+            for(size_t j_neuron=0; j_neuron<ANN->getNNeurons(i_layer, i_neuron); j_neuron++){
+                ANN->setWeight(i_layer, i_neuron, j_neuron, Reader.GetWeight(i_layer, i_neuron, j_neuron));
+            }
+        }
+
+        
+    }
+    ANN->setActivationFunction(ANN->getNWeightLayers(), Reader.GetActivationFunction(ANN->getNWeightLayers()));
+    
+    // Set neuron biases
+    for(size_t i_layer=0; i_layer<ANN->getNWeightLayers()+1; i_layer++){
+        for(size_t i_neuron=0; i_neuron<ANN->getNNeurons(i_layer); i_neuron++){
+            ANN->setBias(i_layer, i_neuron, Reader.GetBias(i_layer, i_neuron));
+        }
+    }
+    
+    // Define input and output layer normalization values
+    for(unsigned long iInput=0; iInput<Reader.GetNInputs(); iInput++){
+        ANN->SetInputNorm(iInput, Reader.GetInputNorm(iInput).first, Reader.GetInputNorm(iInput).second);
+    }
+    for(unsigned long iOutput=0; iOutput<Reader.GetNOutputs(); iOutput++){
+        ANN->SetOutputNorm(iOutput, Reader.GetOutputNorm(iOutput).first, Reader.GetOutputNorm(iOutput).second);
+    }
+    
+}
+void LookUp_ANN::ReadANNInputFile(string inputFileName)
+{
+    ifstream file_stream;
+    istringstream stream_names_var;
+    istringstream stream_filenames;
+    file_stream.open(inputFileName.c_str(), ifstream::in);
+
+    if (!file_stream.is_open()) {
+      SU2_MPI::Error(string("There is no MLP collection file file called ") + inputFileName,
+                    CURRENT_FUNCTION);
+    }
+
+    string line;
+    string word;
+
+    line = SkipToFlag(&file_stream, "[number of MLP files]");
+    getline(file_stream, line);
+    number_of_variables = stoul(line);
+    NeuralNetworks.resize(number_of_variables);
+
+    line = SkipToFlag(&file_stream, "[MLP file names]");
+    getline(file_stream, line);
+    stream_filenames.str(line);
+    while(stream_filenames){
+        stream_filenames >> word;
+        ANN_filenames.push_back(word);
+    }
+    ANN_filenames.pop_back();
+}
+string LookUp_ANN::SkipToFlag(ifstream *file_stream, string flag) {
+  string line;
+  getline(*file_stream, line);
+
+  while (line.compare(flag) != 0 && !(*file_stream).eof()) {
+    getline(*file_stream, line);
+  }
+
+  if ((*file_stream).eof())
+    SU2_MPI::Error("Flag not found in file", CURRENT_FUNCTION);
+
+  return line;
+}
+
+
+bool LookUp_ANN::Check_Duplicate_Outputs(vector<string> &output_names, IOMap *input_output_map) const {
+    unsigned short n_occurances;
+    bool duplicate{false};
+    vector<string> duplicate_variables;
+    for(size_t i_Output =0; i_Output < output_names.size(); i_Output++){
+        n_occurances = 0;
+        for(size_t i_map=0; i_map<input_output_map->GetNANNs(); i_map++){
+            size_t i_ANN =  input_output_map->GetANNIndex(i_map);
+            vector<pair<size_t, size_t>> output_map = input_output_map->GetOutputMapping(i_map);
+            for(size_t j_Output=0; j_Output<output_map.size(); j_Output++){
+                if(output_map[j_Output].first == i_Output) n_occurances++;
+            }
+        }
+        if(n_occurances > 1){
+            duplicate_variables.push_back(output_names[i_Output]);
+            duplicate = true;
+        }
+    }
+    if(duplicate){
+        string message{"Variables "};
+        for(size_t iVar=0; iVar<duplicate_variables.size(); iVar++) message += duplicate_variables[iVar] + " ";
+        SU2_MPI::Error(message + "occur more than once in the loaded ANN outputs.", CURRENT_FUNCTION);
+    }
+    
+    return duplicate;
+}
+
+
+bool LookUp_ANN::Check_Use_of_Inputs(vector<string> &input_names, IOMap *input_output_map) const {
+unsigned short n_inputs = input_names.size();
+vector<string> missing_inputs;
+bool inputs_are_present{true};
+for(size_t iInput=0; iInput<input_names.size(); iInput ++){
+    bool found_input = false;
+    for(size_t i_map=0; i_map < input_output_map->GetNANNs(); i_map++){
+        size_t i_ANN = input_output_map->GetANNIndex(i_map);
+        vector<pair<size_t, size_t>> input_map = input_output_map->GetInputMapping(i_map);
+        for(size_t jInput=0; jInput<input_map.size(); jInput++){
+            if(input_map[jInput].first == iInput){
+                found_input = true;
+            }
+        }
+    }
+    if(!found_input){
+        missing_inputs.push_back(input_names[iInput]);
+        inputs_are_present = false;
+    };
+}
+if(missing_inputs.size() > 0){
+    string message{"Inputs "};
+    for(size_t iVar=0; iVar<missing_inputs.size(); iVar++) message += missing_inputs[iVar] + " ";
+    SU2_MPI::Error(message + "are not present in any loaded ANN.", CURRENT_FUNCTION);
+}
+return inputs_are_present;
+}
+
+bool LookUp_ANN::Check_Use_of_Outputs(vector<string> &output_names, IOMap * input_output_map) const {
+    /* Check wether all output variables are in the loaded MLPs */
+    
+    vector<string> missing_outputs;     
+    bool outputs_are_present{true};
+    /* Looping over the target outputs */
+    for(size_t iOutput=0; iOutput<output_names.size(); iOutput ++){
+
+        bool found_output{false};
+
+        /* Looping over all the selected ANNs */
+        for(size_t i_map=0; i_map < input_output_map->GetNANNs(); i_map++){
+            size_t i_ANN = input_output_map->GetANNIndex(i_map);
+            vector<pair<size_t, size_t>> output_map = input_output_map->GetOutputMapping(i_map);
+
+            /* Looping over the outputs of the output map of the current ANN */
+            for(size_t jOutput=0; jOutput<output_map.size(); jOutput++){
+                if(output_map[jOutput].first == iOutput) found_output = true;
+            }
+        }
+        if(!found_output){
+            missing_outputs.push_back(output_names[iOutput]);
+            outputs_are_present = false;
+        };
+    }
+    if(missing_outputs.size() > 0){
+        string message{"Outputs "};
+        for(size_t iVar=0; iVar<missing_outputs.size(); iVar++) message += missing_outputs[iVar] + " ";
+        SU2_MPI::Error(message + "are not present in any loaded ANN.", CURRENT_FUNCTION);
+    }
+    return outputs_are_present;
+}
\ No newline at end of file
diff --git a/SU2_CFD/src/numerics/multilayer_perceptron/NeuralNetwork.cpp b/SU2_CFD/src/numerics/multilayer_perceptron/NeuralNetwork.cpp
new file mode 100644
index 00000000000..2cfa5a165d6
--- /dev/null
+++ b/SU2_CFD/src/numerics/multilayer_perceptron/NeuralNetwork.cpp
@@ -0,0 +1,332 @@
+/*!
+ * \file NeuralNetwork.cpp
+ * \brief Implementation of the NeuralNetwork class to be used
+ *      for evaluation of multi-layer perceptrons.
+ * \author E. Bunschoten
+ * \version 7.4.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+#include "../../../include/numerics/multilayer_perceptron/NeuralNetwork.hpp"
+#include "../../../include/numerics/multilayer_perceptron/Layer.hpp"
+#include <iostream>
+#include "../../../include/numerics/multilayer_perceptron/ReadNeuralNetwork.hpp"
+#include "../../../Common/include/toolboxes/geometry_toolbox.hpp"
+using namespace std;
+
+
+void NeuralNetwork::predict(vector<su2double> &inputs, vector<su2double*>&outputs, su2double**doutputs_dinputs){
+    su2double x, x_norm, y, y_norm, tanx;
+    size_t iNeuron, jNeuron, iLayer, nNeurons_current, nNeurons_previous;
+    bool same_point{true};
+    for(iNeuron=0; iNeuron<inputLayer->getNNeurons(); iNeuron++){
+        x_norm = (inputs[iNeuron] - input_norm[iNeuron].first)/(input_norm[iNeuron].second - input_norm[iNeuron].first);
+        if(abs(x_norm - inputLayer->getValue(iNeuron)) > 0) same_point = false;
+        inputLayer->setValue(iNeuron, x_norm);
+    }
+    if(!same_point){
+        for(iLayer=1; iLayer<n_hidden_layers + 2; iLayer++){
+            nNeurons_current = total_layers[iLayer]->getNNeurons();
+            nNeurons_previous = total_layers[iLayer - 1]->getNNeurons();
+
+            
+            switch (activation_function_types[iLayer])
+                {
+                case ENUM_ACTIVATION_FUNCTION::SMOOTH_SLOPE:
+                    for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
+                        x = ComputeX(iLayer, iNeuron);
+                        y = x > 0 ? x : tanh(x);
+                        total_layers[iLayer]->setValue(iNeuron, y);
+                    }
+                    break;
+                case ENUM_ACTIVATION_FUNCTION::ELU:
+                    for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
+                        x = ComputeX(iLayer, iNeuron);
+                        y = x > 0 ? x : (exp(x) - 1);
+                        total_layers[iLayer]->setValue(iNeuron, y);
+                    }
+                    break;
+                case ENUM_ACTIVATION_FUNCTION::LINEAR:
+                    for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
+                        x = ComputeX(iLayer, iNeuron);
+                        y = x;
+                        total_layers[iLayer]->setValue(iNeuron, y);
+                    }
+                    break;
+                case ENUM_ACTIVATION_FUNCTION::RELU:
+                    for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
+                        x = ComputeX(iLayer, iNeuron);
+                        y = x > 0.0 ? x : 0.0;
+                        total_layers[iLayer]->setValue(iNeuron, y);
+                    }
+                    break;
+                case ENUM_ACTIVATION_FUNCTION::NONE:
+                    for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
+                        y = 0.0;
+                        total_layers[iLayer]->setValue(iNeuron, y);
+                    }
+                    break;
+                default:
+                    break;
+                }
+                
+        }
+    }
+    for(iNeuron=0; iNeuron<outputLayer->getNNeurons(); iNeuron++){
+        y_norm = outputLayer->getValue(iNeuron);
+        y = y_norm*(output_norm[iNeuron].second - output_norm[iNeuron].first) + output_norm[iNeuron].first;
+        
+        // Setting output value
+        *outputs[iNeuron] = y;
+    }
+}
+// void NeuralNetwork::predict(vector<su2double> &inputs, vector<su2double*>&outputs, su2double**doutputs_dinputs){
+//     // Evaluate the MLP based on the inputs. In case a pointer to the output gradient is provided, the partial
+//     // derivatives of the outputs with respect to the inputs are evaluated as well.
+
+//     su2double *y_values_old, // Perceptron values of the previous layer
+//               *y_values_new, // Perceptron values of the current layer
+//               **dy_dx_old,   // Derivatives of the previous layer
+//               **dy_dx_new;   // Derivatives of the current layer
+
+//     su2double x,    // Perceptron input
+//             x_norm, // Normalized MLP input
+//             y,      // Perceptron output
+//             y_norm; // Normalized MLP output
+
+//     size_t n_inputs{inputLayer->getNNeurons()}; // Number of inputs
+
+//     bool compute_gradient = (doutputs_dinputs != nullptr); // Gradient computation option
+
+//     // Stepping though the MLP layers, communicating the output from the previous layer to the next.
+//     // TODO: make this recursive to increase performance and code simplification
+//     for(size_t iLayer=0; iLayer < total_layers.size(); iLayer++){
+
+//         // In case the input layer is called, input normalization is applied.
+//         if(total_layers.at(iLayer)->isInput()){
+//             // Generating an array for the input layer preceptron values.
+//             y_values_old = new su2double[total_layers.at(iLayer)->getNNeurons()];
+
+//             if(compute_gradient)
+//                 dy_dx_old = new su2double*[total_layers.at(iLayer)->getNNeurons()];
+
+//             for(size_t iNeuron=0; iNeuron<total_layers.at(iLayer)->getNNeurons(); iNeuron++){
+//                 // Normalizing the inputs
+//                 x_norm = (inputs[iNeuron] - input_norm.at(iNeuron).first)/(input_norm.at(iNeuron).second - input_norm.at(iNeuron).first);
+
+//                 // Set perceptron values of input layer.
+//                 total_layers.at(iLayer)->setValue(iNeuron, x_norm);
+//                 y_values_old[iNeuron] = x_norm;
+
+//                 if(compute_gradient){
+//                     dy_dx_old[iNeuron] = new su2double[n_inputs];
+//                     for(size_t jInput=0; jInput<n_inputs; jInput++){
+//                         if(iNeuron == jInput) dy_dx_old[iNeuron][jInput] = 1.0/(input_norm.at(iNeuron).second - input_norm.at(iNeuron).first);
+//                         else dy_dx_old[iNeuron][jInput] = 0.0;
+//                     }
+//                 }
+//             }
+//         }else{
+//             // For the layers after the input layer, activation functions of each layer are called.
+//             y_values_new = new su2double[total_layers.at(iLayer)->getNNeurons()];
+
+//             if(compute_gradient)
+//                 dy_dx_new = new su2double*[total_layers.at(iLayer)->getNNeurons()];
+
+//             for(size_t iNeuron=0; iNeuron<total_layers.at(iLayer)->getNNeurons(); iNeuron++){
+//                 // Multiplying the weights and output values of the previous layer to generate the current perceptron input
+//                 x = GeometryToolbox::DotProduct(total_layers.at(iLayer-1)->getNNeurons(), y_values_old, weights_mat[iLayer-1][iNeuron]);
+
+//                 // Generating the perceptron output
+//                 y = total_layers.at(iLayer)->activation_function(iNeuron, x);
+
+//                 // Storing perceptron output
+//                 total_layers.at(iLayer)->setValue(iNeuron, y);
+//                 y_values_new[iNeuron] = y;
+
+//                 if(compute_gradient){
+//                     dy_dx_new[iNeuron] = new su2double[n_inputs];
+//                     for(size_t jInput=0; jInput < n_inputs; jInput++) dy_dx_new[iNeuron][jInput] = 0.0;
+
+//                     for(size_t jNeuron=0; jNeuron<total_layers.at(iLayer-1)->getNNeurons(); jNeuron++){
+//                         for(size_t jInput=0; jInput<inputLayer->getNNeurons(); jInput++){
+//                             dy_dx_new[iNeuron][jInput] += total_layers.at(iLayer)->getdYdX(iNeuron) * weights_mat[iLayer-1][iNeuron][jNeuron] * dy_dx_old[jNeuron][jInput]; 
+//                         }
+//                     }
+//                 }
+                
+//             }
+//             // Resetting pointer to previous layer outputs
+//             delete y_values_old;
+//             y_values_old = y_values_new;
+
+//             if(compute_gradient){
+//                 for(size_t jNeuron=0; jNeuron<total_layers.at(iLayer-1)->getNNeurons(); jNeuron++){
+//                     delete [] dy_dx_old[jNeuron];
+//                 }
+//                 delete [] dy_dx_old;
+//                 dy_dx_old = dy_dx_new;
+//             }
+//         }
+//     }
+//     delete y_values_old;
+
+//     // Dimensionalize the MLP outputs and gradients
+//     for(size_t iOutput=0; iOutput<outputLayer->getNNeurons(); iOutput++){
+
+//         // Dimensionalize the outputs
+//         y_norm = outputLayer->getValue(iOutput);
+//         y = y_norm*(output_norm.at(iOutput).second - output_norm.at(iOutput).first) + output_norm.at(iOutput).first;
+        
+//         // Setting output value
+//         *outputs.at(iOutput) = y;
+
+//         if(compute_gradient){
+//             for(size_t iInput=0; iInput<n_inputs; iInput++){
+//                 doutputs_dinputs[iOutput][iInput] = (output_norm.at(iOutput).second - output_norm.at(iOutput).first) * dy_dx_old[iOutput][iInput];
+//             }
+//             delete [] dy_dx_old[iOutput];
+//         }
+//     }
+
+//     if(compute_gradient)
+//         delete [] dy_dx_old;
+// }
+
+NeuralNetwork::NeuralNetwork(){
+    inputLayer = nullptr;
+    outputLayer = nullptr;
+    n_hidden_layers = 0;
+}
+
+
+void NeuralNetwork::defineInputLayer(unsigned long n_neurons){
+    //cout << "Creating an input layer with " << n_neurons << " neurons. "<< endl;
+    inputLayer = new Layer(n_neurons);
+    inputLayer->setInput(true);
+    input_norm.resize(n_neurons);
+}
+
+void NeuralNetwork::defineOutputLayer(unsigned long n_neurons){
+    //cout << "Creating an output layer with " << n_neurons << " neurons. "<< endl;
+    outputLayer = new Layer(n_neurons);
+    output_norm.resize(n_neurons);
+}
+
+void NeuralNetwork::push_hidden_layer(unsigned long n_neurons){
+    Layer *newLayer = new Layer(n_neurons);
+    //cout << "Creating a hidden layer with " << n_neurons << " neurons. "<< endl;
+    hiddenLayers.push_back(newLayer);
+    n_hidden_layers ++;
+}
+
+void NeuralNetwork::sizeWeights(){
+    unsigned long i_layer{0};
+    weights.resize(n_hidden_layers + 1);
+    weights.at(i_layer).resize(inputLayer->getNNeurons());
+    Layer * previouslayer = inputLayer;
+
+    if(n_hidden_layers != 0){
+        for(size_t i_hidden_layer=0; i_hidden_layer < n_hidden_layers; i_hidden_layer++){
+            for(size_t i_neuron=0; i_neuron < previouslayer->getNNeurons(); i_neuron++){
+                weights.at(i_layer).at(i_neuron).resize(hiddenLayers.at(i_hidden_layer)->getNNeurons());
+            }
+            previouslayer = hiddenLayers.at(i_hidden_layer);
+            i_layer ++;
+            weights.at(i_layer).resize(previouslayer->getNNeurons());
+        }
+    }
+    for(size_t i_neuron=0; i_neuron < previouslayer->getNNeurons(); i_neuron++){
+        weights.at(i_layer).at(i_neuron).resize(outputLayer->getNNeurons());
+    }
+
+    total_layers.resize(n_hidden_layers + 2);
+    total_layers.at(0) = inputLayer;
+    for(size_t iLayer=0; iLayer<n_hidden_layers; iLayer++){
+        total_layers.at(iLayer + 1) = hiddenLayers.at(iLayer);
+    }
+    total_layers.at(total_layers.size()-1) = outputLayer;
+
+    weights_mat.resize(n_hidden_layers+1);
+    weights_mat[0].resize(hiddenLayers[0]->getNNeurons(), inputLayer->getNNeurons());
+    for(size_t iLayer=1; iLayer<n_hidden_layers; iLayer++){
+        weights_mat[iLayer].resize(hiddenLayers[iLayer]->getNNeurons(), hiddenLayers[iLayer-1]->getNNeurons());
+    }
+    weights_mat[n_hidden_layers].resize(outputLayer->getNNeurons(), hiddenLayers[n_hidden_layers-1]->getNNeurons());
+
+}
+
+void NeuralNetwork::setWeight(unsigned long i_layer, unsigned long i_neuron, unsigned long j_neuron, su2double value){
+    //weights.at(i_layer).at(i_neuron).at(j_neuron) = value;
+    weights_mat[i_layer][j_neuron][i_neuron] = value;
+}
+void NeuralNetwork::displayNetwork(){
+    cout << "Input layer: " << inputLayer->getNNeurons() << " neurons, Activation Function: " <<  inputLayer->getActivationType() << endl;
+    for(size_t i=0; i<total_layers[1]->getNNeurons(); i++){
+        for(size_t j=0; j<inputLayer->getNNeurons(); j++){
+            cout << weights_mat[0][i][j] << " ";
+        }
+        su2double thingy[] = {1, 1, 1};
+        cout << GeometryToolbox::DotProduct(inputLayer->getNNeurons(), weights_mat[0][i], thingy) << endl;
+        cout << endl;
+    }
+    for(size_t i_layer=0; i_layer < hiddenLayers.size(); i_layer++){
+        cout << "Hidden layer " << i_layer + 1 << ": " << hiddenLayers.at(i_layer)->getNNeurons() << " neurons, Activation Function: " <<  hiddenLayers.at(i_layer) ->getActivationType() << endl;
+        for(size_t i=0; i<weights.at(i_layer+1).size(); i++){
+            for(size_t j=0; j<weights.at(i_layer+1).at(i).size(); j++){
+                cout << weights_mat[i_layer][i][j] << " ";
+            }
+            cout << endl;
+    }
+    }
+    cout << "Output layer: "<<outputLayer->getNNeurons() <<" neurons, Activation Function: " << outputLayer->getActivationType() << endl;
+}
+
+void NeuralNetwork::setActivationFunction(unsigned long i_layer, string input)
+{
+    if(input.compare("linear") == 0){
+        //activation_functions[i_layer] = new Linear();
+        activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::LINEAR;
+        return;
+    }
+    if(input.compare("relu") == 0){
+        //activation_functions[i_layer] = new Relu();
+        activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::RELU;
+        return;
+    }
+    if((input.compare("smooth_slope") == 0)){
+        //activation_functions[i_layer] = new SmoothSlope();
+        activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::SMOOTH_SLOPE;
+        return;
+    }
+    if((input.compare("elu") == 0)){
+        //activation_functions[i_layer] = new SmoothSlope();
+        activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::ELU;
+        return;
+    }
+    if(input.compare("none") == 0){
+        //activation_functions[i_layer] = new None();
+        activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::NONE;
+        return;
+    }
+    //total_layers.at(i_layer)->setActivationFunction(input);
+    return;
+}
diff --git a/SU2_CFD/src/numerics/multilayer_perceptron/Neuron.cpp b/SU2_CFD/src/numerics/multilayer_perceptron/Neuron.cpp
new file mode 100644
index 00000000000..4fbef6a462e
--- /dev/null
+++ b/SU2_CFD/src/numerics/multilayer_perceptron/Neuron.cpp
@@ -0,0 +1,114 @@
+/*!
+ * \file Neuron.cpp
+ * \brief Implementation of the neuron class to be used within the 
+ *      Layer class as a part of the NeuralNetwork class.
+ * \author E. Bunschoten
+ * \version 7.4.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+#include "../../../include/numerics/multilayer_perceptron/Neuron.hpp"
+#include <iostream>
+#include <cstring>
+#include <cmath>
+
+using namespace std;
+// Neuron::Neuron()
+// {
+// }
+
+// su2double Neuron::activation_function(su2double x)
+// {
+//     x += bias;
+//     su2double tanx;
+//     switch(ActivationFunction){
+//         case ENUM_ACTIVATION_FUNCTION::LINEAR:
+//             dy_dx = 1;
+//             return x;
+//             break;
+//         case ENUM_ACTIVATION_FUNCTION::RELU:
+//             if(x > 0.0){
+//                 dy_dx = 1.0;
+//                 return x;
+//             }else{
+//                 dy_dx = 0.0;
+//                 return 0.0;
+//             }
+//             break;
+//         case ENUM_ACTIVATION_FUNCTION::SMOOTH_SLOPE:
+//             tanx = tanh(x);
+//             if(tanx > x){
+//                 dy_dx = 4.0 / pow((exp(-x) + exp(x)), 2); 
+//                 return tanx;
+//             }else{
+//                 dy_dx = 1.0;
+//                 return x;
+//             }
+//             break;
+//         default:
+//             SU2_MPI::Error(string("Unknown activation function type: ")+activation_type,
+//                     CURRENT_FUNCTION);
+//             return 0.0;
+//         break;
+//     }
+//     // if(activation_type.compare("smooth_slope") == 0){
+//     //     su2double tanx = tanh(x);
+//     //     if(tanx > x){
+//     //         dy_dx = 4.0 / pow((exp(-x) + exp(x)), 2); 
+//     //         return tanx;
+//     //     }else{
+//     //         dy_dx = 1.0;
+//     //         return x;
+//     //     }
+
+//     // }
+//     // if(activation_type.compare("linear") == 0){
+//     //     dy_dx = 1.0;
+//     //     return x;
+//     // }
+//     // if(activation_type.compare("relu") == 0){
+//     //     su2double zero{0.0};
+//     //     if(x > zero){
+//     //         dy_dx = 1.0;
+//     //         return x;
+//     //     }else{
+//     //         dy_dx = 0.0;
+//     //         return zero;
+//     //     }
+//     // }
+    
+//     // SU2_MPI::Error(string("Unknown activation function type: ")+activation_type,
+//     //                CURRENT_FUNCTION);   
+    
+//     // return x;
+// }
+
+// void Neuron::setFunctionType(string input){
+//     activation_type = input;
+
+//     if(input.compare("smooth_slope") == 0) ActivationFunction = ENUM_ACTIVATION_FUNCTION::SMOOTH_SLOPE; return;
+    
+//     if(input.compare("linear") == 0) ActivationFunction = ENUM_ACTIVATION_FUNCTION::LINEAR; return;
+
+//     if(input.compare("relu") == 0) ActivationFunction = ENUM_ACTIVATION_FUNCTION::RELU; return;
+
+//     if(input.compare("none") == 0) ActivationFunction = ENUM_ACTIVATION_FUNCTION::NONE; return;
+// }
\ No newline at end of file
diff --git a/SU2_CFD/src/numerics/multilayer_perceptron/ReadNeuralNetwork.cpp b/SU2_CFD/src/numerics/multilayer_perceptron/ReadNeuralNetwork.cpp
new file mode 100644
index 00000000000..5c137397bb8
--- /dev/null
+++ b/SU2_CFD/src/numerics/multilayer_perceptron/ReadNeuralNetwork.cpp
@@ -0,0 +1,151 @@
+/*!
+ * \file ReadNeuralNetwork.cpp
+ * \brief Implementation of the reader class to read .mlp input files
+ *      used to set up multi-layer perceptrons.
+ * \author E. Bunschoten
+ * \version 7.4.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+#include "../../../include/numerics/multilayer_perceptron/ReadNeuralNetwork.hpp"
+using namespace std;
+
+ReadNeuralNetwork::ReadNeuralNetwork(string filename_in){
+    filename = filename_in;
+};
+
+void ReadNeuralNetwork::ReadMLPFile(){
+    ifstream file_stream;
+    file_stream.open(filename.c_str(), ifstream::in);
+    if (!file_stream.is_open()) {
+      SU2_MPI::Error(string("There is no MLP file file called ") + filename,
+                    CURRENT_FUNCTION);
+    }
+
+    string line, word;
+    double input_min, input_max, output_min, output_max;
+
+    line = SkipToFlag(&file_stream, "[number of layers]");
+    getline(file_stream, line);
+    n_layers = stoul(line);
+    n_neurons.resize(n_layers);
+    biases.resize(n_layers);
+    weights.resize(n_layers-1);
+    activation_functions.resize(n_layers);
+    line = SkipToFlag(&file_stream, "[neurons per layer]");
+    for(size_t iLayer=0; iLayer<n_layers; iLayer++){
+      getline(file_stream, line);
+      n_neurons.at(iLayer) = stoul(line);
+      biases.at(iLayer).resize(n_neurons.at(iLayer));
+    }
+    for(size_t iLayer=0; iLayer<n_layers-1; iLayer++){
+      weights.at(iLayer).resize(n_neurons.at(iLayer));
+      for(size_t iNeuron=0; iNeuron<n_neurons.at(iLayer); iNeuron++){
+        weights.at(iLayer).at(iNeuron).resize(n_neurons.at(iLayer+1));
+      }
+    }
+
+    input_norm.resize(n_neurons.at(0));
+    output_norm.resize(n_neurons.at(n_neurons.size()-1));
+
+    line = SkipToFlag(&file_stream, "[activation function]");
+    for(size_t iLayer=0; iLayer<n_layers; iLayer++){
+      getline(file_stream, line);
+      istringstream activation_stream(line);
+      activation_stream >> word;
+      activation_functions.at(iLayer) = word;
+    }    
+
+    line = SkipToFlag(&file_stream, "[input names]");
+    for(size_t iInput=0; iInput < n_neurons.at(0); iInput++){
+      getline(file_stream, line);
+      input_names.push_back(line);
+    }
+
+    line = SkipToFlag(&file_stream, "[input normalization]");
+    for(size_t iInput=0; iInput<input_norm.size(); iInput++){
+      getline(file_stream, line);
+      istringstream input_norm_stream(line);
+      input_norm_stream >> word;
+      input_min = stold(word);
+      input_norm_stream >> word;
+      input_max = stold(word);
+      input_norm.at(iInput) = make_pair(input_min, input_max);
+    }
+
+    line = SkipToFlag(&file_stream, "[output names]");
+    for(size_t iOutput=0; iOutput < n_neurons.at(n_neurons.size()-1); iOutput++){
+      getline(file_stream, line);
+      output_names.push_back(line);
+    }
+
+    line = SkipToFlag(&file_stream, "[output normalization]");
+    for(size_t iOutput=0; iOutput<output_norm.size(); iOutput++){
+      getline(file_stream, line);
+      istringstream output_norm_stream(line);
+      output_norm_stream >> word;
+      output_min = stold(word);
+      output_norm_stream >> word;
+      output_max = stold(word);
+      output_norm.at(iOutput) = make_pair(output_min, output_max);
+    }
+
+    line = SkipToFlag(&file_stream, "[weights per layer]");
+    for(size_t iLayer=0; iLayer<n_layers-1; iLayer++){
+      getline(file_stream, line);
+      for(size_t iNeuron=0; iNeuron<n_neurons.at(iLayer); iNeuron++){
+        getline(file_stream, line);
+        istringstream weight_stream(line);
+        for(size_t jNeuron=0; jNeuron<n_neurons.at(iLayer+1); jNeuron++){
+          weight_stream >> word;
+          weights.at(iLayer).at(iNeuron).at(jNeuron) = stold(word);
+        }
+      }
+      getline(file_stream, line);
+    }
+    
+    line = SkipToFlag(&file_stream, "[biases per layer]");
+    for(size_t iLayer=0; iLayer<n_layers; iLayer++){
+      getline(file_stream, line);
+      istringstream bias_stream(line);
+      for(size_t iNeuron=0; iNeuron<n_neurons.at(iLayer); iNeuron++){
+        bias_stream >> word;
+        biases.at(iLayer).at(iNeuron) = stold(word);
+      }
+    }
+
+
+
+}
+
+string ReadNeuralNetwork::SkipToFlag(ifstream *file_stream, string flag) {
+  string line;
+  getline(*file_stream, line);
+
+  while (line.compare(flag) != 0 && !(*file_stream).eof()) {
+    getline(*file_stream, line);
+  }
+
+  if ((*file_stream).eof())
+    cout << "line not in file!" << endl;
+
+  return line;
+}
\ No newline at end of file

From f5d0267d47a8a235c4e3e026ca6faba0806507e2 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 13 Sep 2022 11:58:30 +0200
Subject: [PATCH 030/656] Added error checking in MLP file reader and fixed bug
 with input-output mapping preventing single, specific outputs from MLP's to
 be evaluated

---
 .../numerics/multilayer_perceptron/IOMap.hpp  |   3 +
 .../multilayer_perceptron/NeuralNetwork.hpp   |   4 +-
 .../multilayer_perceptron/LookUp_ANN.cpp      |   6 +-
 .../multilayer_perceptron/NeuralNetwork.cpp   | 119 +--------
 .../ReadNeuralNetwork.cpp                     | 234 +++++++++++++-----
 5 files changed, 192 insertions(+), 174 deletions(-)

diff --git a/SU2_CFD/include/numerics/multilayer_perceptron/IOMap.hpp b/SU2_CFD/include/numerics/multilayer_perceptron/IOMap.hpp
index 66878762edb..2e2f14b1d75 100644
--- a/SU2_CFD/include/numerics/multilayer_perceptron/IOMap.hpp
+++ b/SU2_CFD/include/numerics/multilayer_perceptron/IOMap.hpp
@@ -56,6 +56,9 @@ class IOMap
     size_t GetANNIndex(size_t i_Map){return ANN_indices[i_Map];}
     size_t GetInputIndex(size_t i_Map, size_t iInput){return Input_Map[i_Map][iInput].first;}
     size_t GetOutputIndex(size_t i_Map, size_t iOutput){return Output_Map[i_Map][iOutput].first;}
+    size_t GetANNOutputIndex(size_t i_Map, size_t iOutput){return Output_Map[i_Map][iOutput].second;}
+    size_t GetNMappedOutputs(size_t i_Map){return Output_Map[i_Map].size();}
+
     vector<pair<size_t, size_t>> GetOutputMapping(size_t i_map){return Output_Map[i_map];}
     vector<pair<size_t, size_t>> GetInputMapping(size_t i_map){return Input_Map[i_map];}
     
diff --git a/SU2_CFD/include/numerics/multilayer_perceptron/NeuralNetwork.hpp b/SU2_CFD/include/numerics/multilayer_perceptron/NeuralNetwork.hpp
index 682d673f5a6..a5cb8beeffa 100644
--- a/SU2_CFD/include/numerics/multilayer_perceptron/NeuralNetwork.hpp
+++ b/SU2_CFD/include/numerics/multilayer_perceptron/NeuralNetwork.hpp
@@ -98,6 +98,7 @@ class NeuralNetwork
     vector<pair<su2double, su2double>> input_norm;
     vector<pair<su2double, su2double>> output_norm;
     vector<su2double> last_inputs;
+    su2double* ANN_outputs;
 
     enum ENUM_ACTIVATION_FUNCTION {
         NONE=0,
@@ -135,7 +136,7 @@ class NeuralNetwork
 
     // su2double predict(su2double * X, size_t i_output);
     // void predict(vector<su2double> &inputs, vector<su2double*> &outputs);
-    void predict(vector<su2double> &inputs, vector<su2double*> &outputs, su2double**doutputs_dinputs=nullptr);
+    void predict(vector<su2double> &inputs);
 
     //void predict_new(vector<su2double> &inputs, vector<su2double*> &outputs, su2double**doutputs_dinputs=nullptr);
 
@@ -151,6 +152,7 @@ class NeuralNetwork
     size_t GetnInputs(){return input_names.size();}
     size_t GetnOutputs(){return output_names.size();}
 
+    su2double GetANN_Output(size_t iOutput){return ANN_outputs[iOutput];}
     void SizeActivationFunctions(unsigned long n_layers){activation_function_types = new ENUM_ACTIVATION_FUNCTION[n_layers]; activation_functions.resize(4); 
     activation_functions[ENUM_ACTIVATION_FUNCTION::LINEAR] = new Linear(); 
     activation_functions[ENUM_ACTIVATION_FUNCTION::RELU] = new Relu();
diff --git a/SU2_CFD/src/numerics/multilayer_perceptron/LookUp_ANN.cpp b/SU2_CFD/src/numerics/multilayer_perceptron/LookUp_ANN.cpp
index 26c4c02e645..3999cf47ba7 100644
--- a/SU2_CFD/src/numerics/multilayer_perceptron/LookUp_ANN.cpp
+++ b/SU2_CFD/src/numerics/multilayer_perceptron/LookUp_ANN.cpp
@@ -76,8 +76,10 @@ void LookUp_ANN::Predict_ANN(IOMap *input_output_map, vector<su2double>& inputs,
     for(size_t i_map=0; i_map<input_output_map->GetNANNs(); i_map++){
         size_t i_ANN = input_output_map->GetANNIndex(i_map);
         vector<su2double> ANN_inputs = input_output_map->GetANN_Inputs(i_map, inputs);
-        vector<su2double*> ANN_outputs = input_output_map->GetANN_Outputs(i_map, outputs);
-        NeuralNetworks[i_ANN]->predict(ANN_inputs, ANN_outputs);
+        NeuralNetworks[i_ANN]->predict(ANN_inputs);
+        for(size_t i=0; i < input_output_map->GetNMappedOutputs(i_map); i++){
+            *outputs[input_output_map->GetOutputIndex(i_map, i)] = NeuralNetworks[i_ANN]->GetANN_Output(input_output_map->GetANNOutputIndex(i_map, i));
+        }
     }
 }
 void LookUp_ANN::GenerateANN(NeuralNetwork * ANN, string fileName)
diff --git a/SU2_CFD/src/numerics/multilayer_perceptron/NeuralNetwork.cpp b/SU2_CFD/src/numerics/multilayer_perceptron/NeuralNetwork.cpp
index 2cfa5a165d6..2ece6768c59 100644
--- a/SU2_CFD/src/numerics/multilayer_perceptron/NeuralNetwork.cpp
+++ b/SU2_CFD/src/numerics/multilayer_perceptron/NeuralNetwork.cpp
@@ -33,7 +33,7 @@
 using namespace std;
 
 
-void NeuralNetwork::predict(vector<su2double> &inputs, vector<su2double*>&outputs, su2double**doutputs_dinputs){
+void NeuralNetwork::predict(vector<su2double> &inputs){
     su2double x, x_norm, y, y_norm, tanx;
     size_t iNeuron, jNeuron, iLayer, nNeurons_current, nNeurons_previous;
     bool same_point{true};
@@ -95,121 +95,9 @@ void NeuralNetwork::predict(vector<su2double> &inputs, vector<su2double*>&output
         y = y_norm*(output_norm[iNeuron].second - output_norm[iNeuron].first) + output_norm[iNeuron].first;
         
         // Setting output value
-        *outputs[iNeuron] = y;
+        ANN_outputs[iNeuron] = y;
     }
 }
-// void NeuralNetwork::predict(vector<su2double> &inputs, vector<su2double*>&outputs, su2double**doutputs_dinputs){
-//     // Evaluate the MLP based on the inputs. In case a pointer to the output gradient is provided, the partial
-//     // derivatives of the outputs with respect to the inputs are evaluated as well.
-
-//     su2double *y_values_old, // Perceptron values of the previous layer
-//               *y_values_new, // Perceptron values of the current layer
-//               **dy_dx_old,   // Derivatives of the previous layer
-//               **dy_dx_new;   // Derivatives of the current layer
-
-//     su2double x,    // Perceptron input
-//             x_norm, // Normalized MLP input
-//             y,      // Perceptron output
-//             y_norm; // Normalized MLP output
-
-//     size_t n_inputs{inputLayer->getNNeurons()}; // Number of inputs
-
-//     bool compute_gradient = (doutputs_dinputs != nullptr); // Gradient computation option
-
-//     // Stepping though the MLP layers, communicating the output from the previous layer to the next.
-//     // TODO: make this recursive to increase performance and code simplification
-//     for(size_t iLayer=0; iLayer < total_layers.size(); iLayer++){
-
-//         // In case the input layer is called, input normalization is applied.
-//         if(total_layers.at(iLayer)->isInput()){
-//             // Generating an array for the input layer preceptron values.
-//             y_values_old = new su2double[total_layers.at(iLayer)->getNNeurons()];
-
-//             if(compute_gradient)
-//                 dy_dx_old = new su2double*[total_layers.at(iLayer)->getNNeurons()];
-
-//             for(size_t iNeuron=0; iNeuron<total_layers.at(iLayer)->getNNeurons(); iNeuron++){
-//                 // Normalizing the inputs
-//                 x_norm = (inputs[iNeuron] - input_norm.at(iNeuron).first)/(input_norm.at(iNeuron).second - input_norm.at(iNeuron).first);
-
-//                 // Set perceptron values of input layer.
-//                 total_layers.at(iLayer)->setValue(iNeuron, x_norm);
-//                 y_values_old[iNeuron] = x_norm;
-
-//                 if(compute_gradient){
-//                     dy_dx_old[iNeuron] = new su2double[n_inputs];
-//                     for(size_t jInput=0; jInput<n_inputs; jInput++){
-//                         if(iNeuron == jInput) dy_dx_old[iNeuron][jInput] = 1.0/(input_norm.at(iNeuron).second - input_norm.at(iNeuron).first);
-//                         else dy_dx_old[iNeuron][jInput] = 0.0;
-//                     }
-//                 }
-//             }
-//         }else{
-//             // For the layers after the input layer, activation functions of each layer are called.
-//             y_values_new = new su2double[total_layers.at(iLayer)->getNNeurons()];
-
-//             if(compute_gradient)
-//                 dy_dx_new = new su2double*[total_layers.at(iLayer)->getNNeurons()];
-
-//             for(size_t iNeuron=0; iNeuron<total_layers.at(iLayer)->getNNeurons(); iNeuron++){
-//                 // Multiplying the weights and output values of the previous layer to generate the current perceptron input
-//                 x = GeometryToolbox::DotProduct(total_layers.at(iLayer-1)->getNNeurons(), y_values_old, weights_mat[iLayer-1][iNeuron]);
-
-//                 // Generating the perceptron output
-//                 y = total_layers.at(iLayer)->activation_function(iNeuron, x);
-
-//                 // Storing perceptron output
-//                 total_layers.at(iLayer)->setValue(iNeuron, y);
-//                 y_values_new[iNeuron] = y;
-
-//                 if(compute_gradient){
-//                     dy_dx_new[iNeuron] = new su2double[n_inputs];
-//                     for(size_t jInput=0; jInput < n_inputs; jInput++) dy_dx_new[iNeuron][jInput] = 0.0;
-
-//                     for(size_t jNeuron=0; jNeuron<total_layers.at(iLayer-1)->getNNeurons(); jNeuron++){
-//                         for(size_t jInput=0; jInput<inputLayer->getNNeurons(); jInput++){
-//                             dy_dx_new[iNeuron][jInput] += total_layers.at(iLayer)->getdYdX(iNeuron) * weights_mat[iLayer-1][iNeuron][jNeuron] * dy_dx_old[jNeuron][jInput]; 
-//                         }
-//                     }
-//                 }
-                
-//             }
-//             // Resetting pointer to previous layer outputs
-//             delete y_values_old;
-//             y_values_old = y_values_new;
-
-//             if(compute_gradient){
-//                 for(size_t jNeuron=0; jNeuron<total_layers.at(iLayer-1)->getNNeurons(); jNeuron++){
-//                     delete [] dy_dx_old[jNeuron];
-//                 }
-//                 delete [] dy_dx_old;
-//                 dy_dx_old = dy_dx_new;
-//             }
-//         }
-//     }
-//     delete y_values_old;
-
-//     // Dimensionalize the MLP outputs and gradients
-//     for(size_t iOutput=0; iOutput<outputLayer->getNNeurons(); iOutput++){
-
-//         // Dimensionalize the outputs
-//         y_norm = outputLayer->getValue(iOutput);
-//         y = y_norm*(output_norm.at(iOutput).second - output_norm.at(iOutput).first) + output_norm.at(iOutput).first;
-        
-//         // Setting output value
-//         *outputs.at(iOutput) = y;
-
-//         if(compute_gradient){
-//             for(size_t iInput=0; iInput<n_inputs; iInput++){
-//                 doutputs_dinputs[iOutput][iInput] = (output_norm.at(iOutput).second - output_norm.at(iOutput).first) * dy_dx_old[iOutput][iInput];
-//             }
-//             delete [] dy_dx_old[iOutput];
-//         }
-//     }
-
-//     if(compute_gradient)
-//         delete [] dy_dx_old;
-// }
 
 NeuralNetwork::NeuralNetwork(){
     inputLayer = nullptr;
@@ -272,7 +160,8 @@ void NeuralNetwork::sizeWeights(){
     }
     weights_mat[n_hidden_layers].resize(outputLayer->getNNeurons(), hiddenLayers[n_hidden_layers-1]->getNNeurons());
 
-}
+    ANN_outputs = new su2double[outputLayer->getNNeurons()];
+}   
 
 void NeuralNetwork::setWeight(unsigned long i_layer, unsigned long i_neuron, unsigned long j_neuron, su2double value){
     //weights.at(i_layer).at(i_neuron).at(j_neuron) = value;
diff --git a/SU2_CFD/src/numerics/multilayer_perceptron/ReadNeuralNetwork.cpp b/SU2_CFD/src/numerics/multilayer_perceptron/ReadNeuralNetwork.cpp
index 5c137397bb8..13d0b64a14f 100644
--- a/SU2_CFD/src/numerics/multilayer_perceptron/ReadNeuralNetwork.cpp
+++ b/SU2_CFD/src/numerics/multilayer_perceptron/ReadNeuralNetwork.cpp
@@ -42,71 +42,193 @@ void ReadNeuralNetwork::ReadMLPFile(){
 
     string line, word;
     double input_min, input_max, output_min, output_max;
+    bool eoHeader{false}, found_layercount{false}, found_input_names{false}, found_output_names{false};
 
-    line = SkipToFlag(&file_stream, "[number of layers]");
-    getline(file_stream, line);
-    n_layers = stoul(line);
-    n_neurons.resize(n_layers);
-    biases.resize(n_layers);
-    weights.resize(n_layers-1);
-    activation_functions.resize(n_layers);
-    line = SkipToFlag(&file_stream, "[neurons per layer]");
-    for(size_t iLayer=0; iLayer<n_layers; iLayer++){
-      getline(file_stream, line);
-      n_neurons.at(iLayer) = stoul(line);
-      biases.at(iLayer).resize(n_neurons.at(iLayer));
-    }
-    for(size_t iLayer=0; iLayer<n_layers-1; iLayer++){
-      weights.at(iLayer).resize(n_neurons.at(iLayer));
-      for(size_t iNeuron=0; iNeuron<n_neurons.at(iLayer); iNeuron++){
-        weights.at(iLayer).at(iNeuron).resize(n_neurons.at(iLayer+1));
+    line = SkipToFlag(&file_stream, "<header>");
+
+    while(getline(file_stream, line) && !eoHeader){
+      if(line.compare("[number of layers]") == 0){
+        getline(file_stream, line);
+        n_layers = stoul(line);
+        n_neurons.resize(n_layers);
+        biases.resize(n_layers);
+        weights.resize(n_layers-1);
+        activation_functions.resize(n_layers);
+
+        found_layercount = true;
       }
-    }
 
-    input_norm.resize(n_neurons.at(0));
-    output_norm.resize(n_neurons.at(n_neurons.size()-1));
+      if(line.compare("[neurons per layer]") == 0){
+        if(!found_layercount){
+          SU2_MPI::Error("No layer count provided before defining neuron count per layer", CURRENT_FUNCTION);
+        }
+        // Loop over layer count and size neuron count and bias count per layer accordingly
+        for(size_t iLayer=0; iLayer<n_layers; iLayer++){
+          getline(file_stream, line);
+          n_neurons.at(iLayer) = stoul(line);
+          biases.at(iLayer).resize(n_neurons.at(iLayer));
+        }
+        // Loop over spaces between layers and size the weight matrices accordingly
+        for(size_t iLayer=0; iLayer<n_layers-1; iLayer++){
+          weights.at(iLayer).resize(n_neurons.at(iLayer));
+          for(size_t iNeuron=0; iNeuron<n_neurons.at(iLayer); iNeuron++){
+            weights.at(iLayer).at(iNeuron).resize(n_neurons.at(iLayer+1));
+          }
+        }
+        // Size input normalization according to number of inputs
+        input_norm.resize(n_neurons.at(0));
+        // Set default input normalization
+        for(size_t iNeuron=0; iNeuron<n_neurons.at(0); iNeuron++) input_norm.at(iNeuron) = make_pair(0, 1);
 
-    line = SkipToFlag(&file_stream, "[activation function]");
-    for(size_t iLayer=0; iLayer<n_layers; iLayer++){
-      getline(file_stream, line);
-      istringstream activation_stream(line);
-      activation_stream >> word;
-      activation_functions.at(iLayer) = word;
-    }    
+        // Size output normalization according to number of outputs
+        output_norm.resize(n_neurons.at(n_neurons.size()-1));
+        // Set default output normalization
+        for(size_t iNeuron=0; iNeuron<n_neurons.at(n_neurons.size()-1); iNeuron++) output_norm.at(iNeuron) = make_pair(0, 1);
+      }
 
-    line = SkipToFlag(&file_stream, "[input names]");
-    for(size_t iInput=0; iInput < n_neurons.at(0); iInput++){
-      getline(file_stream, line);
-      input_names.push_back(line);
-    }
+      if(line.compare("[activation function]") == 0){
+        if(!found_layercount){
+          SU2_MPI::Error("No layer count provided before providing layer activation functions", CURRENT_FUNCTION);
+        }
+        for(size_t iLayer=0; iLayer<n_layers; iLayer++){
+          getline(file_stream, line);
+          istringstream activation_stream(line);
+          activation_stream >> word;
+          activation_functions.at(iLayer) = word;
+        }    
+      }
 
-    line = SkipToFlag(&file_stream, "[input normalization]");
-    for(size_t iInput=0; iInput<input_norm.size(); iInput++){
-      getline(file_stream, line);
-      istringstream input_norm_stream(line);
-      input_norm_stream >> word;
-      input_min = stold(word);
-      input_norm_stream >> word;
-      input_max = stold(word);
-      input_norm.at(iInput) = make_pair(input_min, input_max);
-    }
+      if(line.compare("[input names]") == 0){
+        found_input_names = true;
+        unsigned short j{1};
+        getline(file_stream, line);
+        while(line.compare("") != 0){
+          input_names.push_back(line);
+          getline(file_stream, line);
+        }
 
-    line = SkipToFlag(&file_stream, "[output names]");
-    for(size_t iOutput=0; iOutput < n_neurons.at(n_neurons.size()-1); iOutput++){
-      getline(file_stream, line);
-      output_names.push_back(line);
-    }
+        if(input_names.size() != n_neurons.at(0)){
+          SU2_MPI::Error("Number of input variable names inconsistent with number of MLP inputs", CURRENT_FUNCTION);
+        }
+      }
 
-    line = SkipToFlag(&file_stream, "[output normalization]");
-    for(size_t iOutput=0; iOutput<output_norm.size(); iOutput++){
-      getline(file_stream, line);
-      istringstream output_norm_stream(line);
-      output_norm_stream >> word;
-      output_min = stold(word);
-      output_norm_stream >> word;
-      output_max = stold(word);
-      output_norm.at(iOutput) = make_pair(output_min, output_max);
+      if(line.compare("[input normalization]") == 0){
+        for(size_t iInput=0; iInput<input_norm.size(); iInput++){
+          getline(file_stream, line);
+          if(line.compare("") != 0){
+            istringstream input_norm_stream(line);
+            input_norm_stream >> word;
+            input_min = stold(word);
+            input_norm_stream >> word;
+            input_max = stold(word);
+            input_norm.at(iInput) = make_pair(input_min, input_max);
+          }
+        }
+      }
+
+      if(line.compare("[output names]") == 0){
+        found_output_names = true;
+        getline(file_stream, line);
+        while(line.compare("") != 0){
+          output_names.push_back(line);
+          getline(file_stream, line);
+        }
+
+        if(output_names.size() != (n_neurons.at(n_neurons.size()-1))){
+          SU2_MPI::Error("Number of output variable names inconsistent with number of MLP outputs", CURRENT_FUNCTION);
+        }
+      }
+
+      if(line.compare("[output normalization]") == 0){
+        for(size_t iOutput=0; iOutput<output_norm.size(); iOutput++){
+          getline(file_stream, line);
+          if(line.compare("") != 0){
+            istringstream output_norm_stream(line);
+            output_norm_stream >> word;
+            output_min = stold(word);
+            output_norm_stream >> word;
+            output_max = stold(word);
+            output_norm.at(iOutput) = make_pair(output_min, output_max);
+          }
+        }
+      }
+
+      if(line.compare("</header>") == 0){
+        eoHeader = true;
+      }
+    }
+    if(!found_input_names){
+      SU2_MPI::Error("No MLP input variable names provided", CURRENT_FUNCTION);
     }
+    if(!found_output_names){
+      SU2_MPI::Error("No MLP output variable names provided", CURRENT_FUNCTION);
+    }
+
+
+    // line = SkipToFlag(&file_stream, "[number of layers]");
+    // getline(file_stream, line);
+    // n_layers = stoul(line);
+    // n_neurons.resize(n_layers);
+    // biases.resize(n_layers);
+    // weights.resize(n_layers-1);
+    // activation_functions.resize(n_layers);
+    // line = SkipToFlag(&file_stream, "[neurons per layer]");
+    // for(size_t iLayer=0; iLayer<n_layers; iLayer++){
+    //   getline(file_stream, line);
+    //   n_neurons.at(iLayer) = stoul(line);
+    //   biases.at(iLayer).resize(n_neurons.at(iLayer));
+    // }
+    // for(size_t iLayer=0; iLayer<n_layers-1; iLayer++){
+    //   weights.at(iLayer).resize(n_neurons.at(iLayer));
+    //   for(size_t iNeuron=0; iNeuron<n_neurons.at(iLayer); iNeuron++){
+    //     weights.at(iLayer).at(iNeuron).resize(n_neurons.at(iLayer+1));
+    //   }
+    // }
+
+    // input_norm.resize(n_neurons.at(0));
+    // output_norm.resize(n_neurons.at(n_neurons.size()-1));
+
+    // line = SkipToFlag(&file_stream, "[activation function]");
+    // for(size_t iLayer=0; iLayer<n_layers; iLayer++){
+    //   getline(file_stream, line);
+    //   istringstream activation_stream(line);
+    //   activation_stream >> word;
+    //   activation_functions.at(iLayer) = word;
+    // }    
+
+    // line = SkipToFlag(&file_stream, "[input names]");
+    // for(size_t iInput=0; iInput < n_neurons.at(0); iInput++){
+    //   getline(file_stream, line);
+    //   input_names.push_back(line);
+    // }
+
+    // line = SkipToFlag(&file_stream, "[input normalization]");
+    // for(size_t iInput=0; iInput<input_norm.size(); iInput++){
+    //   getline(file_stream, line);
+    //   istringstream input_norm_stream(line);
+    //   input_norm_stream >> word;
+    //   input_min = stold(word);
+    //   input_norm_stream >> word;
+    //   input_max = stold(word);
+    //   input_norm.at(iInput) = make_pair(input_min, input_max);
+    // }
+
+    // line = SkipToFlag(&file_stream, "[output names]");
+    // for(size_t iOutput=0; iOutput < n_neurons.at(n_neurons.size()-1); iOutput++){
+    //   getline(file_stream, line);
+    //   output_names.push_back(line);
+    // }
+
+    // line = SkipToFlag(&file_stream, "[output normalization]");
+    // for(size_t iOutput=0; iOutput<output_norm.size(); iOutput++){
+    //   getline(file_stream, line);
+    //   istringstream output_norm_stream(line);
+    //   output_norm_stream >> word;
+    //   output_min = stold(word);
+    //   output_norm_stream >> word;
+    //   output_max = stold(word);
+    //   output_norm.at(iOutput) = make_pair(output_min, output_max);
+    // }
 
     line = SkipToFlag(&file_stream, "[weights per layer]");
     for(size_t iLayer=0; iLayer<n_layers-1; iLayer++){

From 438e8c6c46194053cb7859ffe51ab71cc82f931a Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Thu, 15 Sep 2022 14:07:14 +0200
Subject: [PATCH 031/656] Moved MLP classes to separate library in its own
 namespace. Added a template CFluidModel class using MLPs for lookups as well

---
 .../multilayer_perceptron/CIOMap.hpp          |  87 +++++++++++
 .../multilayer_perceptron/CLayer.hpp          | 135 ++++++++++++++++++
 .../multilayer_perceptron/CLookUp_ANN.hpp     |  36 ++---
 .../multilayer_perceptron/CNeuralNetwork.hpp  |  94 ++++--------
 .../multilayer_perceptron/CNeuron.hpp         | 113 +++++++++++++++
 .../CReadNeuralNetwork.hpp                    |  16 ++-
 Common/lib/Makefile.am                        |   6 +
 Common/src/toolboxes/meson.build              |   8 ++
 .../multilayer_perceptron/CIOMap.cpp          |  13 +-
 .../multilayer_perceptron/CLayer.cpp          |  26 +---
 .../multilayer_perceptron/CLookUp_ANN.cpp     |  34 +++--
 .../multilayer_perceptron/CNeuralNetwork.cpp  |  67 +++++----
 .../multilayer_perceptron/CNeuron.cpp         |  33 +++++
 .../CReadNeuralNetwork.cpp                    |  90 +++---------
 SU2_CFD/include/fluid/CMLPGas_Template.hpp    | 102 +++++++++++++
 .../numerics/multilayer_perceptron/IOMap.hpp  |  83 -----------
 .../numerics/multilayer_perceptron/Layer.hpp  |  63 --------
 .../numerics/multilayer_perceptron/Neuron.hpp |  74 ----------
 SU2_CFD/obj/Makefile.am                       |   7 +-
 SU2_CFD/src/fluid/CMLPGas_Template.cpp        | 125 ++++++++++++++++
 SU2_CFD/src/meson.build                       |  11 +-
 .../numerics/multilayer_perceptron/Neuron.cpp | 114 ---------------
 22 files changed, 748 insertions(+), 589 deletions(-)
 create mode 100644 Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
 create mode 100644 Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
 rename SU2_CFD/include/numerics/multilayer_perceptron/LookUp_ANN.hpp => Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp (79%)
 rename SU2_CFD/include/numerics/multilayer_perceptron/NeuralNetwork.hpp => Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp (59%)
 create mode 100644 Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
 rename SU2_CFD/include/numerics/multilayer_perceptron/ReadNeuralNetwork.hpp => Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp (90%)
 rename SU2_CFD/src/numerics/multilayer_perceptron/IOMap.cpp => Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp (82%)
 rename SU2_CFD/src/numerics/multilayer_perceptron/Layer.cpp => Common/src/toolboxes/multilayer_perceptron/CLayer.cpp (67%)
 rename SU2_CFD/src/numerics/multilayer_perceptron/LookUp_ANN.cpp => Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp (87%)
 rename SU2_CFD/src/numerics/multilayer_perceptron/NeuralNetwork.cpp => Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp (77%)
 create mode 100644 Common/src/toolboxes/multilayer_perceptron/CNeuron.cpp
 rename SU2_CFD/src/numerics/multilayer_perceptron/ReadNeuralNetwork.cpp => Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp (71%)
 create mode 100644 SU2_CFD/include/fluid/CMLPGas_Template.hpp
 delete mode 100644 SU2_CFD/include/numerics/multilayer_perceptron/IOMap.hpp
 delete mode 100644 SU2_CFD/include/numerics/multilayer_perceptron/Layer.hpp
 delete mode 100644 SU2_CFD/include/numerics/multilayer_perceptron/Neuron.hpp
 create mode 100644 SU2_CFD/src/fluid/CMLPGas_Template.cpp
 delete mode 100644 SU2_CFD/src/numerics/multilayer_perceptron/Neuron.cpp

diff --git a/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp b/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
new file mode 100644
index 00000000000..f0ef33fefed
--- /dev/null
+++ b/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
@@ -0,0 +1,87 @@
+/*!
+ * \file CIOMap.hpp
+ * \brief Declaration of input-to-output mapping class for artifical neural networks
+ * \author E. Bunschoten
+ * \version 7.4.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+#pragma once
+
+#include <cmath>
+#include <string>
+#include <iostream>
+#include <limits>
+#include <cstdlib>
+#include <vector>
+#include "../../CConfig.hpp"
+#include "../../linear_algebra/blas_structure.hpp"
+#include "CLookUp_ANN.hpp"
+
+using namespace std;
+namespace MLPToolbox
+{
+        
+    class CLookUp_ANN;
+
+    class CIOMap
+    {
+        private:
+        vector<size_t> ANN_indices;
+        vector<vector<pair<size_t, size_t>>> Input_Map;
+        vector<vector<pair<size_t, size_t>>> Output_Map;
+        vector<vector<su2double>> input_indices;
+        public:
+        CIOMap(){};
+        CIOMap(CLookUp_ANN*ANN_collection, vector<string> &inputs, vector<string> &outputs);
+        ~CIOMap(){};
+        void Push_ANN_index(size_t i_ANN){ANN_indices.push_back(i_ANN);};
+        void PairVariableswithANNs(CLookUp_ANN * ANN_collection, vector<string> &inputs, vector<string> &outputs);
+        size_t GetNANNs(){return ANN_indices.size();}
+        size_t GetANNIndex(size_t i_Map){return ANN_indices[i_Map];}
+        size_t GetInputIndex(size_t i_Map, size_t iInput){return Input_Map[i_Map][iInput].first;}
+        size_t GetOutputIndex(size_t i_Map, size_t iOutput){return Output_Map[i_Map][iOutput].first;}
+        size_t GetANNOutputIndex(size_t i_Map, size_t iOutput){return Output_Map[i_Map][iOutput].second;}
+        size_t GetNMappedOutputs(size_t i_Map){return Output_Map[i_Map].size();}
+
+        vector<pair<size_t, size_t>> GetOutputMapping(size_t i_map){return Output_Map[i_map];}
+        vector<pair<size_t, size_t>> GetInputMapping(size_t i_map){return Input_Map[i_map];}
+        
+        vector<su2double> GetANN_Inputs(size_t i_Map, vector<su2double>&inputs){
+            vector<su2double> ANN_input;
+            ANN_input.resize(Input_Map[i_Map].size());
+
+            for(size_t iInput=0; iInput<Input_Map[i_Map].size(); iInput++){
+                ANN_input.at(iInput) = inputs[GetInputIndex(i_Map, iInput)];
+            }
+            return ANN_input;
+        }
+        vector<su2double*> GetANN_Outputs(size_t i_Map, vector<su2double*>&outputs){
+            vector<su2double*> ANN_output;
+            ANN_output.resize(Output_Map[i_Map].size());
+
+            for(size_t iOutput=0; iOutput<Output_Map[i_Map].size(); iOutput++){
+                ANN_output.at(iOutput) = outputs[GetOutputIndex(i_Map, iOutput)];
+            }
+            return ANN_output;
+        }
+    };
+}
diff --git a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
new file mode 100644
index 00000000000..ee8aac9bd74
--- /dev/null
+++ b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
@@ -0,0 +1,135 @@
+/*!
+ * \file CLayer.hpp
+ * \brief Declaration of artificial neural network interpolation class
+ * \author E. Bunschoten
+ * \version 7.4.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+#pragma once
+
+#include <cmath>
+#include <iostream>
+#include <limits>
+#include <cstdlib>
+
+#include "../../CConfig.hpp"
+#include "CNeuron.hpp"
+#include "../../linear_algebra/blas_structure.hpp"
+using namespace std;
+
+namespace MLPToolbox{
+class CLayer
+{
+private:
+    unsigned long number_of_neurons;    /*!< Neuron count in current layer */
+    CNeuron * neurons;                   /*!< Array of neurons in current layer */
+    bool is_input;                      /*!< Input layer identifyer */
+    string activation_type;             /*!< Activation function type applied to the current layer*/
+public:
+    CLayer();
+    CLayer(unsigned long n_neurons);
+
+    /*!
+    * \brief Set current layer neuron count
+    * \param[in] n_neurons - Number of neurons in this layer
+    */
+    void setNNeurons(unsigned long n_neurons);
+
+    /*!
+    * \brief Get the current layer neuron count
+    * \return Neuron count
+    */
+    unsigned long getNNeurons() const {return number_of_neurons;};
+
+    /*!
+    * \brief Define current layer as input layer
+    * \param[in] input - input layer identifyer
+    */
+    void setInput(bool def){is_input = def;};
+
+    /*!
+    * \brief Get input layer identifyer
+    * \return input layer identifyer
+    */
+    bool isInput() const {return is_input;};
+
+    /*!
+    * \brief Set the output value of a neuron in the layer
+    * \param[in] i_neuron - Neuron index
+    * \param[in] output_value - Activation function output
+    */
+    void setOutput(size_t i_neuron, su2double value){neurons[i_neuron].setOutput(value);}
+
+    /*!
+    * \brief Get the output value of a neuron in the layer
+    * \param[in] i_neuron - Neuron index
+    * \return Neuron output value
+    */
+    su2double getOutput(size_t i_neuron) const {return neurons[i_neuron].getOutput();}
+
+    /*!
+    * \brief Set the input value of a neuron in the layer
+    * \param[in] i_neuron - Neuron index
+    * \param[in] input_value - Activation function input
+    */
+    void setInput(size_t i_neuron, su2double value){neurons[i_neuron].setInput(value);}
+
+    /*!
+    * \brief Get the input value of a neuron in the layer
+    * \param[in] i_neuron - Neuron index
+    * \return Neuron input value
+    */
+    su2double getInput(size_t i_neuron) const {return neurons[i_neuron].getInput();}
+
+    /*!
+    * \brief Set the bias value of a neuron in the layer
+    * \param[in] i_neuron - Neuron index
+    * \param[in] bias_value - Bias value
+    */
+    void setBias(size_t i_neuron, su2double value){neurons[i_neuron].setBias(value);}
+
+    /*!
+    * \brief Get the bias value of a neuron in the layer
+    * \param[in] i_neuron - Neuron index
+    * \return Neuron bias value
+    */
+    su2double getBias(size_t i_neuron){return neurons[i_neuron].getBias();}
+
+    /*!
+    * \brief Get the output-input gradient of a neuron in the layer
+    * \param[in] i_neuron - Neuron index
+    * \return Gradient of neuron output wrt input
+    */
+    su2double getdYdX(size_t i_neuron){return neurons[i_neuron].getGradient();}
+
+    /*!
+    * \brief Get the activation function name applied to this layer
+    * \return name of the activation function
+    */
+    string getActivationType(){return activation_type;}
+    
+    ~CLayer(){
+        delete [] neurons;
+    };
+};
+
+}
diff --git a/SU2_CFD/include/numerics/multilayer_perceptron/LookUp_ANN.hpp b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
similarity index 79%
rename from SU2_CFD/include/numerics/multilayer_perceptron/LookUp_ANN.hpp
rename to Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
index 9cab1a9204c..3b7a0baaf02 100644
--- a/SU2_CFD/include/numerics/multilayer_perceptron/LookUp_ANN.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
@@ -1,5 +1,5 @@
 /*!
- * \file LookUp_ANN.hpp
+ * \file CLookUp_ANN.hpp
  * \brief Declaration of artificial neural network interpolation class
  * \author E. Bunschoten
  * \version 7.4.0 "Blackbird"
@@ -33,19 +33,21 @@
 #include <limits>
 #include <cstdlib>
 #include <vector>
-#include "../../../../Common/include/CConfig.hpp"
-#include "../../../../Common/include/linear_algebra/blas_structure.hpp"
-#include "NeuralNetwork.hpp"
-#include "IOMap.hpp"
+#include "../../CConfig.hpp"
+#include "../../linear_algebra/blas_structure.hpp"
+#include "CNeuralNetwork.hpp"
+#include "CIOMap.hpp"
 
 using namespace std;
-class IOMap;
 
-class LookUp_ANN
+namespace MLPToolbox{
+class CIOMap;
+
+class CLookUp_ANN
 {
     private:
     int rank{0};
-    vector<NeuralNetwork*> NeuralNetworks;  /*!< Vector containing all loaded neural networks. */
+    vector<CNeuralNetwork*> NeuralNetworks;  /*!< Vector containing all loaded neural networks. */
 
     vector<string> ANN_filenames;       /*!< Filenames containing ANN architecture information. */
 
@@ -64,7 +66,7 @@ class LookUp_ANN
     * \param[in] ANN - pointer to target NeuralNetwork class
     * \param[in] filename - filename containing ANN architecture information
     */
-    void GenerateANN(NeuralNetwork*ANN, string filename);
+    void GenerateANN(CNeuralNetwork*ANN, string filename);
 
     /*!
     * \brief Read ANN architecture input file
@@ -78,7 +80,7 @@ class LookUp_ANN
     * \brief ANN collection class constructor
     * \param[in] filename - filename containing list of ANN input files
     */
-    LookUp_ANN(string fileName);
+    CLookUp_ANN(string fileName);
     
     /*!
     * \brief Evaluate loaded ANNs for given inputs and outputs
@@ -86,9 +88,9 @@ class LookUp_ANN
     * \param[in] inputs - input values
     * \param[in] outputs - pointers to output variables
     */
-    void Predict_ANN(IOMap *input_output_map, vector<su2double> &inputs, vector<su2double*> &outputs);
+    void Predict_ANN(CIOMap *input_output_map, vector<su2double> &inputs, vector<su2double*> &outputs);
 
-    ~LookUp_ANN(){for(size_t i_ANN=0; i_ANN<number_of_variables; i_ANN++)
+    ~CLookUp_ANN(){for(size_t i_ANN=0; i_ANN<number_of_variables; i_ANN++)
         delete NeuralNetworks.at(i_ANN);
     };
 
@@ -96,28 +98,28 @@ class LookUp_ANN
     * \brief Get number of loaded ANNs
     * \return number of loaded ANNs
     */
-    const size_t GetNANNs() const {return NeuralNetworks.size();}
+    size_t GetNANNs() const {return NeuralNetworks.size();}
 
     /*!
     * \brief Check if variables occur more than once in ANN outputs
     * \param[in] output_names - output variable names to check
     * \param[in] input_output_map - pointer to input-output map to be checked
     */
-    bool Check_Duplicate_Outputs(vector<string> &output_names, IOMap *input_output_map) const;
+    bool Check_Duplicate_Outputs(vector<string> &output_names, CIOMap *input_output_map) const;
 
     /*!
     * \brief Check if all output variables are present in the loaded ANNs
     * \param[in] output_names - output variable names to check
     * \param[in] input_output_map - pointer to input-output map to be checked
     */
-    bool Check_Use_of_Outputs(vector<string> &output_names, IOMap *input_output_map) const;
+    bool Check_Use_of_Outputs(vector<string> &output_names, CIOMap *input_output_map) const;
 
     /*!
     * \brief Check if all input variables are present in the loaded ANNs
     * \param[in] input_names - input variable names to check
     * \param[in] input_output_map - pointer to input-output map to be checked
     */
-    bool Check_Use_of_Inputs(vector<string> &input_names, IOMap *input_output_map) const;
+    bool Check_Use_of_Inputs(vector<string> &input_names, CIOMap *input_output_map) const;
 
     /*!
     * \brief Map variable names to ANN inputs or outputs
@@ -129,3 +131,5 @@ class LookUp_ANN
     
 };  
 
+}
+
diff --git a/SU2_CFD/include/numerics/multilayer_perceptron/NeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
similarity index 59%
rename from SU2_CFD/include/numerics/multilayer_perceptron/NeuralNetwork.hpp
rename to Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
index a5cb8beeffa..6e54cd363a8 100644
--- a/SU2_CFD/include/numerics/multilayer_perceptron/NeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
@@ -1,5 +1,5 @@
 /*!
- * \file NeuralNetwork.hpp
+ * \file CNeuralNetwork.hpp
  * \brief Declaration of the neural network class
  * \author E. Bunschoten
  * \version 7.4.0 "Blackbird"
@@ -33,71 +33,34 @@
 #include <limits>
 #include <cstdlib>
 
-#include "../../../../Common/include/CConfig.hpp"
-#include "../../../../Common/include/linear_algebra/blas_structure.hpp"
-#include "Layer.hpp"
+#include "../../CConfig.hpp"
+#include "../../linear_algebra/blas_structure.hpp"
+#include "CLayer.hpp"
 
 using namespace std;
-class Activation_Function {
-    private:
-    public:
-    Activation_Function(){};
-    ~Activation_Function(){};
-    inline virtual su2double run_activation_function(su2double x) {return 0.0;}
-};
-
-class Linear : public Activation_Function {
-    private:
-    public:
-    Linear() : Activation_Function() {};
-    ~Linear(){};
-    su2double run_activation_function(su2double x) final {return x;}
-};
-
-class Relu : public Activation_Function {
-    private:
-    public:
-    Relu() : Activation_Function() {};
-    ~Relu(){};
-    su2double run_activation_function(su2double x) final {return max(0.0, x);}
-};
-
-class SmoothSlope : public Activation_Function {
-    private:
-    su2double tanhx;
-    public:
-    SmoothSlope() : Activation_Function() {};
-    ~SmoothSlope(){};
-    su2double run_activation_function(su2double x) final {tanhx = tanh(x); return max(tanhx, x);}
-};
-
-class None : public Activation_Function {
-    private:
-    public:
-    None() : Activation_Function() {};
-    ~None(){};
-    su2double run_activation_function(su2double x) final {return 0.0;}
-};
-
-class NeuralNetwork
+namespace MLPToolbox{
+class CNeuralNetwork
 {
 private:
-    vector<string> input_names;
-    vector<string> output_names;
+    vector<string> input_names,
+                   output_names;
 
     unsigned long n_hidden_layers;
-    Layer *inputLayer;
-    Layer *outputLayer;
-    vector< Layer *> hiddenLayers; 
-    vector<Layer *>total_layers;
+
+    CLayer *inputLayer,
+           *outputLayer;
+
+    vector<CLayer*> hiddenLayers,
+                    total_layers;
 
     vector<vector<vector<su2double>>> weights;
     vector<su2activematrix> weights_mat;
     vector<vector<su2double>> values;
 
-    vector<pair<su2double, su2double>> input_norm;
-    vector<pair<su2double, su2double>> output_norm;
+    vector<pair<su2double, su2double>> input_norm,
+                                       output_norm;
     vector<su2double> last_inputs;
+
     su2double* ANN_outputs;
 
     enum ENUM_ACTIVATION_FUNCTION {
@@ -108,15 +71,14 @@ class NeuralNetwork
         ELU = 4
     };
     ENUM_ACTIVATION_FUNCTION * activation_function_types;
-    vector<Activation_Function*> activation_functions;
-    Activation_Function* current_activation_function;
-    //Activation_Function *activation_functions;
+
 public:
-    NeuralNetwork();
-    ~NeuralNetwork(){
+    CNeuralNetwork();
+    ~CNeuralNetwork(){
         for(size_t i=0; i<total_layers.size(); i++){
             delete total_layers.at(i);
         }
+        delete [] ANN_outputs;
     };
     void defineInputLayer(unsigned long n_neurons);
     void defineOutputLayer(unsigned long n_neurons);
@@ -134,11 +96,8 @@ class NeuralNetwork
     return total_layers.at(iLayer)->getNNeurons();}
     unsigned long getNNeurons(unsigned long iLayer, unsigned long iNeuron){return weights.at(iLayer).at(iNeuron).size();}
 
-    // su2double predict(su2double * X, size_t i_output);
-    // void predict(vector<su2double> &inputs, vector<su2double*> &outputs);
     void predict(vector<su2double> &inputs);
 
-    //void predict_new(vector<su2double> &inputs, vector<su2double*> &outputs, su2double**doutputs_dinputs=nullptr);
 
     void SetInputNorm(unsigned long iInput, su2double input_min, su2double input_max){input_norm.at(iInput) = make_pair(input_min, input_max);}
     void SetOutputNorm(unsigned long iOutput, su2double output_min, su2double output_max){output_norm.at(iOutput) = make_pair(output_min, output_max);}
@@ -153,10 +112,7 @@ class NeuralNetwork
     size_t GetnOutputs(){return output_names.size();}
 
     su2double GetANN_Output(size_t iOutput){return ANN_outputs[iOutput];}
-    void SizeActivationFunctions(unsigned long n_layers){activation_function_types = new ENUM_ACTIVATION_FUNCTION[n_layers]; activation_functions.resize(4); 
-    activation_functions[ENUM_ACTIVATION_FUNCTION::LINEAR] = new Linear(); 
-    activation_functions[ENUM_ACTIVATION_FUNCTION::RELU] = new Relu();
-    activation_functions[ENUM_ACTIVATION_FUNCTION::SMOOTH_SLOPE] = new SmoothSlope();
+    void SizeActivationFunctions(unsigned long n_layers){activation_function_types = new ENUM_ACTIVATION_FUNCTION[n_layers]; 
     }
 
     su2double ComputeX(size_t iLayer, size_t iNeuron){
@@ -164,13 +120,13 @@ class NeuralNetwork
         x = total_layers[iLayer]->getBias(iNeuron);
         size_t nNeurons_previous = total_layers[iLayer - 1]->getNNeurons();
         for(size_t jNeuron=0; jNeuron<nNeurons_previous; jNeuron++){
-            x += weights_mat[iLayer - 1][iNeuron][jNeuron] * total_layers[iLayer-1]->getValue(jNeuron);
+            x += weights_mat[iLayer - 1][iNeuron][jNeuron] * total_layers[iLayer-1]->getOutput(jNeuron);
         }
         return x;
     }
-    // su2double run_activation_function(unsigned long iLayer, su2double x){return activation_functions[iLayer]->run_activation_function(x);}
-    //void SetActivationFunction(size_t iLayer, unsigned long function_index){activation_functions[iLayer] = ENUM_ACTIVATION_FUNCTION(function_index);}
 };
 
 
+}
+
 
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
new file mode 100644
index 00000000000..fed140d4457
--- /dev/null
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
@@ -0,0 +1,113 @@
+/*!
+ * \file CNeuron.hpp
+ * \brief Declaration of artificial neural network perceptron class
+ * \author E. Bunschoten
+ * \version 7.4.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+#pragma once
+
+#include <cmath>
+#include <iostream>
+#include <limits>
+#include <cstdlib>
+
+#include "../../CConfig.hpp"
+#include "../../linear_algebra/blas_structure.hpp"
+
+using namespace std;
+namespace MLPToolbox{
+class CNeuron
+{
+private:
+    unsigned long i_neuron;         /*!< Neuron identification number */
+    su2double output{0},            /*!< Output value of the current neuron */
+              input{0},             /*!< Input value of the current neuron */
+              doutput_dinput{0},    /*!< Gradient of output with respect to input */
+              bias{0};              /*!< Bias value at current neuron */
+
+public:
+    CNeuron(){};
+
+    /*!
+    * \brief Set neuron identification number
+    * \param[in] input - Identification number
+    */
+    void setNumber(unsigned long input){i_neuron = input;}
+
+    /*!
+    * \brief Get neuron identification number
+    * \return Identification number
+    */
+    unsigned long getNumber() const {return i_neuron;}
+
+    /*!
+    * \brief Set neuron output value
+    * \param[in] input - activation function output value
+    */
+    void setOutput(su2double input){output = input;}
+
+    /*!
+    * \brief Get neuron output value
+    * \return Output value
+    */
+    su2double getOutput() const {return output;}
+
+    /*!
+    * \brief Set neuron input value
+    * \param[in] input - activation function input value
+    */
+    void setInput(su2double x){input = x;}
+
+    /*!
+    * \brief Get neuron input value
+    * \return input value
+    */
+    su2double getInput() const {return input;}
+
+    /*!
+    * \brief Set neuron bias
+    * \param[in] input - bias value
+    */
+    void setBias(su2double input){bias = input;}
+
+    /*!
+    * \brief Get neuron bias value
+    * \return bias value
+    */
+    su2double getBias() const {return bias;}
+
+    /*!
+    * \brief Set neuron output gradient with respect to its input value
+    * \param[in] input - Derivative of activation function with respect to input
+    */
+    void setGradient(su2double input){doutput_dinput = input;}
+
+    /*!
+    * \brief Get neuron output gradient with respect to input value
+    * \return output gradient wrt input value
+    */
+    su2double getGradient() const {return doutput_dinput;}
+};
+
+}
+
diff --git a/SU2_CFD/include/numerics/multilayer_perceptron/ReadNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
similarity index 90%
rename from SU2_CFD/include/numerics/multilayer_perceptron/ReadNeuralNetwork.hpp
rename to Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
index e33d267cbe2..d471e42d939 100644
--- a/SU2_CFD/include/numerics/multilayer_perceptron/ReadNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
@@ -1,5 +1,5 @@
 /*!
- * \file ReadNeuralNetwork.hpp
+ * \file CReadNeuralNetwork.hpp
  * \brief Declaration of MLP input file reader class
  * \author E. Bunschoten
  * \version 7.4.0 "Blackbird"
@@ -31,11 +31,12 @@
 #include <limits>
 #include <cstdlib>
 
-#include "../../../../Common/include/CConfig.hpp"
-#include "../../../../Common/include/linear_algebra/blas_structure.hpp"
+#include "../../CConfig.hpp"
+#include "../../linear_algebra/blas_structure.hpp"
 
 using namespace std;
-class ReadNeuralNetwork {
+namespace MLPToolbox{
+class CReadNeuralNetwork {
     private:
     vector<string> input_names;
     vector<string> output_names;
@@ -51,7 +52,7 @@ class ReadNeuralNetwork {
     vector<pair<double long, double long>> output_norm;
     public:
 
-    ReadNeuralNetwork(string filename_in);
+    CReadNeuralNetwork(string filename_in);
     void ReadMLPFile();
 
     string SkipToFlag(ifstream *file_stream, string flag);
@@ -70,5 +71,6 @@ class ReadNeuralNetwork {
     string GetInputName(size_t iInput){return input_names.at(iInput);}
     string GetOutputName(size_t iOutput){return output_names.at(iOutput);}
     
-    ~ReadNeuralNetwork(){};
-};
\ No newline at end of file
+    ~CReadNeuralNetwork(){};
+};
+}
diff --git a/Common/lib/Makefile.am b/Common/lib/Makefile.am
index af2046cf826..c938e931966 100644
--- a/Common/lib/Makefile.am
+++ b/Common/lib/Makefile.am
@@ -128,6 +128,12 @@ lib_sources = \
   ../src/toolboxes/MMS/CRinglebSolution.cpp \
   ../src/toolboxes/MMS/CTGVSolution.cpp \
   ../src/toolboxes/MMS/CUserDefinedSolution.cpp \
+  ../src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp\
+  ../src/toolboxes/multilayer_perceptron/CIOMap.cpp\
+  ../src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp\
+  ../src/toolboxes/multilayer_perceptron/CLayer.cpp\
+  ../src/toolboxes/multilayer_perceptron/CNeuron.cpp\
+  ../src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp\
   ../src/linear_algebra/CSysVector.cpp \
   ../src/linear_algebra/CSysMatrix.cpp \
   ../src/linear_algebra/CSysSolve.cpp \
diff --git a/Common/src/toolboxes/meson.build b/Common/src/toolboxes/meson.build
index d95ffad5992..d6441390a57 100644
--- a/Common/src/toolboxes/meson.build
+++ b/Common/src/toolboxes/meson.build
@@ -5,3 +5,11 @@ common_src += files(['CLinearPartitioner.cpp',
                      'CSymmetricMatrix.cpp'])
 
 subdir('MMS')
+
+common_src += files(['multilayer_perceptron/CLookUp_ANN.cpp',
+                     'multilayer_perceptron/CIOMap.cpp',
+                     'multilayer_perceptron/CNeuralNetwork.cpp',
+                     'multilayer_perceptron/CLayer.cpp',
+                     'multilayer_perceptron/CNeuron.cpp',
+                     'multilayer_perceptron/CReadNeuralNetwork.cpp'])
+
diff --git a/SU2_CFD/src/numerics/multilayer_perceptron/IOMap.cpp b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
similarity index 82%
rename from SU2_CFD/src/numerics/multilayer_perceptron/IOMap.cpp
rename to Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
index 82d2faf1965..d6bba0ce8b2 100644
--- a/SU2_CFD/src/numerics/multilayer_perceptron/IOMap.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
@@ -1,5 +1,5 @@
 /*!
- * \file IOMap.cpp
+ * \file CIOMap.cpp
  * \brief Implementation of the input-output mapping class for the 
  *      use of multi-layer perceptrons in SU2
  * \author E. Bunschoten
@@ -25,14 +25,14 @@
  * You should have received a copy of the GNU Lesser General Public
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
-#include "../../../include/numerics/multilayer_perceptron/LookUp_ANN.hpp"
-#include "../../../include/numerics/multilayer_perceptron/IOMap.hpp"
+#include "../../../include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp"
+#include "../../../include/toolboxes/multilayer_perceptron/CIOMap.hpp"
 #include <iostream>
 #include <string>
 #include <cmath>
 #include <fstream>
 
-IOMap::IOMap(LookUp_ANN*ANN_collection, vector<string> &inputs, vector<string> &outputs){
+MLPToolbox::CIOMap::CIOMap(CLookUp_ANN*ANN_collection, vector<string> &inputs, vector<string> &outputs){
     PairVariableswithANNs(ANN_collection, inputs, outputs);
     if(outputs.size() > 0){
         ANN_collection->Check_Use_of_Inputs(inputs, this);
@@ -40,14 +40,13 @@ IOMap::IOMap(LookUp_ANN*ANN_collection, vector<string> &inputs, vector<string> &
         ANN_collection->Check_Duplicate_Outputs(outputs, this);
     }
 }
-void IOMap::PairVariableswithANNs(LookUp_ANN*ANN_collection, vector<string> &inputs, vector<string> &outputs){
+void MLPToolbox::CIOMap::PairVariableswithANNs(CLookUp_ANN*ANN_collection, vector<string> &inputs, vector<string> &outputs){
 
-    bool isInput, isOutput,input_match;
+    bool isInput, isOutput;
     for(size_t i_ANN=0; i_ANN<ANN_collection->GetNANNs(); i_ANN++){
         vector<pair<size_t, size_t>> Input_Indices = ANN_collection->FindVariable_Indices(i_ANN, inputs, true);
         isInput = Input_Indices.size() > 0;
         if(isInput){
-            input_match = true;
             vector<pair<size_t, size_t>> Output_Indices = ANN_collection->FindVariable_Indices(i_ANN, outputs, false);
             isOutput = Output_Indices.size() > 0;
             if(isOutput){
diff --git a/SU2_CFD/src/numerics/multilayer_perceptron/Layer.cpp b/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp
similarity index 67%
rename from SU2_CFD/src/numerics/multilayer_perceptron/Layer.cpp
rename to Common/src/toolboxes/multilayer_perceptron/CLayer.cpp
index b666e4547d3..74f1e702063 100644
--- a/SU2_CFD/src/numerics/multilayer_perceptron/Layer.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp
@@ -1,5 +1,5 @@
 /*!
- * \file Layer.cpp
+ * \file CLayer.cpp
  * \brief Implementation of the Layer class to be used in the NeuralNetwork
  *      class
  * \author E. Bunschoten
@@ -25,38 +25,26 @@
  * You should have received a copy of the GNU Lesser General Public
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
-#include "../../../include/numerics/multilayer_perceptron/Layer.hpp"
+#include "../../../include/toolboxes/multilayer_perceptron/CLayer.hpp"
 #include <cstring>
 using namespace std;
 
-Layer::Layer() : Layer(1) {};
+MLPToolbox::CLayer::CLayer() : CLayer(1) {};
 
-Layer::Layer(unsigned long n_neurons) : number_of_neurons{n_neurons}, input{false}
+MLPToolbox::CLayer::CLayer(unsigned long n_neurons) : number_of_neurons{n_neurons}, is_input{false}
 {
-    neurons = new Neuron[n_neurons];
+    neurons = new CNeuron[n_neurons];
     for(size_t i=0; i<number_of_neurons; i++){
         neurons[i].setNumber(i+1);
     }
 }
 
-void Layer::setNNeurons(unsigned long n_neurons){
+void MLPToolbox::CLayer::setNNeurons(unsigned long n_neurons){
     if(number_of_neurons != n_neurons){
         delete [] neurons;
-        neurons = new Neuron[n_neurons];
+        neurons = new CNeuron[n_neurons];
         for(size_t i=0; i<number_of_neurons; i++){
             neurons[i].setNumber(i+1);
         }
     }
 }
-
-// void Layer::setActivationFunction(string input){
-//     activation_type = input;
-//     for(size_t i=0; i<number_of_neurons; i++){
-//         neurons[i].setFunctionType(input);
-//     }
-// }
-// void Layer::sayhi(){
-//     for(size_t i=0; i<number_of_neurons; i++){
-//         neurons[i].sayhi();
-//     }
-// }
diff --git a/SU2_CFD/src/numerics/multilayer_perceptron/LookUp_ANN.cpp b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
similarity index 87%
rename from SU2_CFD/src/numerics/multilayer_perceptron/LookUp_ANN.cpp
rename to Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
index 3999cf47ba7..331e08c11c7 100644
--- a/SU2_CFD/src/numerics/multilayer_perceptron/LookUp_ANN.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
@@ -1,5 +1,5 @@
 /*!
- * \file LookUp_ANN.cpp
+ * \file CLookUp_ANN.cpp
  * \brief Implementation of the multi-layer perceptron class to be 
  *      used for look-up operations.
  * \author E. Bunschoten
@@ -25,9 +25,9 @@
  * You should have received a copy of the GNU Lesser General Public
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
-#include "../../../include/numerics/multilayer_perceptron/LookUp_ANN.hpp"
-#include "../../../include/numerics/multilayer_perceptron/IOMap.hpp"
-#include "../../../include/numerics/multilayer_perceptron/ReadNeuralNetwork.hpp"
+#include "../../../include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp"
+#include "../../../include/toolboxes/multilayer_perceptron/CIOMap.hpp"
+#include "../../../include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp"
 #include <iostream>
 #include <string>
 #include <cmath>
@@ -35,7 +35,7 @@
 
 using namespace std;
 
-LookUp_ANN::LookUp_ANN(string inputFileName)
+MLPToolbox::CLookUp_ANN::CLookUp_ANN(string inputFileName)
 {
     
     #ifdef HAVE_MPI
@@ -47,7 +47,7 @@ LookUp_ANN::LookUp_ANN(string inputFileName)
     ReadANNInputFile(inputFileName);
     for(size_t i_ANN=0; i_ANN<number_of_variables; i_ANN++){
         
-        NeuralNetworks.at(i_ANN) = new NeuralNetwork;
+        NeuralNetworks.at(i_ANN) = new CNeuralNetwork;
         if(rank == MASTER_NODE)
             cout << "Generating neural network for " << ANN_filenames.at(i_ANN) << endl;
         GenerateANN(NeuralNetworks.at(i_ANN), ANN_filenames.at(i_ANN));
@@ -55,7 +55,7 @@ LookUp_ANN::LookUp_ANN(string inputFileName)
 }
 
 
-vector<pair<size_t, size_t>> LookUp_ANN::FindVariable_Indices(size_t i_ANN, vector<string> variable_names, bool input) const {
+vector<pair<size_t, size_t>> MLPToolbox::CLookUp_ANN::FindVariable_Indices(size_t i_ANN, vector<string> variable_names, bool input) const {
     vector<pair<size_t, size_t>> variable_indices;
     size_t nVar = input ? NeuralNetworks[i_ANN]->GetnInputs() : NeuralNetworks[i_ANN]->GetnOutputs();
 
@@ -72,7 +72,7 @@ vector<pair<size_t, size_t>> LookUp_ANN::FindVariable_Indices(size_t i_ANN, vect
     return variable_indices;
 }
 
-void LookUp_ANN::Predict_ANN(IOMap *input_output_map, vector<su2double>& inputs, vector<su2double*>& outputs){
+void MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap *input_output_map, vector<su2double>& inputs, vector<su2double*>& outputs){
     for(size_t i_map=0; i_map<input_output_map->GetNANNs(); i_map++){
         size_t i_ANN = input_output_map->GetANNIndex(i_map);
         vector<su2double> ANN_inputs = input_output_map->GetANN_Inputs(i_map, inputs);
@@ -82,9 +82,9 @@ void LookUp_ANN::Predict_ANN(IOMap *input_output_map, vector<su2double>& inputs,
         }
     }
 }
-void LookUp_ANN::GenerateANN(NeuralNetwork * ANN, string fileName)
+void MLPToolbox::CLookUp_ANN::GenerateANN(CNeuralNetwork * ANN, string fileName)
 {
-    ReadNeuralNetwork Reader = ReadNeuralNetwork(fileName);
+    CReadNeuralNetwork Reader = CReadNeuralNetwork(fileName);
     
     // Read MLP input file
     Reader.ReadMLPFile();
@@ -136,7 +136,8 @@ void LookUp_ANN::GenerateANN(NeuralNetwork * ANN, string fileName)
     }
     
 }
-void LookUp_ANN::ReadANNInputFile(string inputFileName)
+
+void MLPToolbox::CLookUp_ANN::ReadANNInputFile(string inputFileName)
 {
     ifstream file_stream;
     istringstream stream_names_var;
@@ -165,7 +166,7 @@ void LookUp_ANN::ReadANNInputFile(string inputFileName)
     }
     ANN_filenames.pop_back();
 }
-string LookUp_ANN::SkipToFlag(ifstream *file_stream, string flag) {
+string MLPToolbox::CLookUp_ANN::SkipToFlag(ifstream *file_stream, string flag) {
   string line;
   getline(*file_stream, line);
 
@@ -180,7 +181,7 @@ string LookUp_ANN::SkipToFlag(ifstream *file_stream, string flag) {
 }
 
 
-bool LookUp_ANN::Check_Duplicate_Outputs(vector<string> &output_names, IOMap *input_output_map) const {
+bool MLPToolbox::CLookUp_ANN::Check_Duplicate_Outputs(vector<string> &output_names, CIOMap *input_output_map) const {
     unsigned short n_occurances;
     bool duplicate{false};
     vector<string> duplicate_variables;
@@ -208,14 +209,12 @@ bool LookUp_ANN::Check_Duplicate_Outputs(vector<string> &output_names, IOMap *in
 }
 
 
-bool LookUp_ANN::Check_Use_of_Inputs(vector<string> &input_names, IOMap *input_output_map) const {
-unsigned short n_inputs = input_names.size();
+bool MLPToolbox::CLookUp_ANN::Check_Use_of_Inputs(vector<string> &input_names, CIOMap *input_output_map) const {
 vector<string> missing_inputs;
 bool inputs_are_present{true};
 for(size_t iInput=0; iInput<input_names.size(); iInput ++){
     bool found_input = false;
     for(size_t i_map=0; i_map < input_output_map->GetNANNs(); i_map++){
-        size_t i_ANN = input_output_map->GetANNIndex(i_map);
         vector<pair<size_t, size_t>> input_map = input_output_map->GetInputMapping(i_map);
         for(size_t jInput=0; jInput<input_map.size(); jInput++){
             if(input_map[jInput].first == iInput){
@@ -236,7 +235,7 @@ if(missing_inputs.size() > 0){
 return inputs_are_present;
 }
 
-bool LookUp_ANN::Check_Use_of_Outputs(vector<string> &output_names, IOMap * input_output_map) const {
+bool MLPToolbox::CLookUp_ANN::Check_Use_of_Outputs(vector<string> &output_names, CIOMap * input_output_map) const {
     /* Check wether all output variables are in the loaded MLPs */
     
     vector<string> missing_outputs;     
@@ -248,7 +247,6 @@ bool LookUp_ANN::Check_Use_of_Outputs(vector<string> &output_names, IOMap * inpu
 
         /* Looping over all the selected ANNs */
         for(size_t i_map=0; i_map < input_output_map->GetNANNs(); i_map++){
-            size_t i_ANN = input_output_map->GetANNIndex(i_map);
             vector<pair<size_t, size_t>> output_map = input_output_map->GetOutputMapping(i_map);
 
             /* Looping over the outputs of the output map of the current ANN */
diff --git a/SU2_CFD/src/numerics/multilayer_perceptron/NeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
similarity index 77%
rename from SU2_CFD/src/numerics/multilayer_perceptron/NeuralNetwork.cpp
rename to Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
index 2ece6768c59..b4344662613 100644
--- a/SU2_CFD/src/numerics/multilayer_perceptron/NeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
@@ -1,5 +1,5 @@
 /*!
- * \file NeuralNetwork.cpp
+ * \file CNeuralNetwork.cpp
  * \brief Implementation of the NeuralNetwork class to be used
  *      for evaluation of multi-layer perceptrons.
  * \author E. Bunschoten
@@ -25,63 +25,65 @@
  * You should have received a copy of the GNU Lesser General Public
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
-#include "../../../include/numerics/multilayer_perceptron/NeuralNetwork.hpp"
-#include "../../../include/numerics/multilayer_perceptron/Layer.hpp"
+#include "../../../include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp"
+#include "../../../include/toolboxes/multilayer_perceptron/CLayer.hpp"
 #include <iostream>
-#include "../../../include/numerics/multilayer_perceptron/ReadNeuralNetwork.hpp"
-#include "../../../Common/include/toolboxes/geometry_toolbox.hpp"
+#include "../../../include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp"
 using namespace std;
 
 
-void NeuralNetwork::predict(vector<su2double> &inputs){
+void MLPToolbox::CNeuralNetwork::predict(vector<su2double> &inputs){
     su2double x, x_norm, y, y_norm, tanx;
     size_t iNeuron, jNeuron, iLayer, nNeurons_current, nNeurons_previous;
     bool same_point{true};
     for(iNeuron=0; iNeuron<inputLayer->getNNeurons(); iNeuron++){
         x_norm = (inputs[iNeuron] - input_norm[iNeuron].first)/(input_norm[iNeuron].second - input_norm[iNeuron].first);
-        if(abs(x_norm - inputLayer->getValue(iNeuron)) > 0) same_point = false;
-        inputLayer->setValue(iNeuron, x_norm);
+        if(abs(x_norm - inputLayer->getOutput(iNeuron)) > 0) same_point = false;
+        inputLayer->setOutput(iNeuron, x_norm);
     }
     if(!same_point){
         for(iLayer=1; iLayer<n_hidden_layers + 2; iLayer++){
             nNeurons_current = total_layers[iLayer]->getNNeurons();
             nNeurons_previous = total_layers[iLayer - 1]->getNNeurons();
 
-            
+            for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
+                x = ComputeX(iLayer, iNeuron);
+                total_layers[iLayer]->setInput(iNeuron, x);
+            }
             switch (activation_function_types[iLayer])
                 {
                 case ENUM_ACTIVATION_FUNCTION::SMOOTH_SLOPE:
                     for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
-                        x = ComputeX(iLayer, iNeuron);
+                        x = total_layers[iLayer]->getInput(iNeuron);
                         y = x > 0 ? x : tanh(x);
-                        total_layers[iLayer]->setValue(iNeuron, y);
+                        total_layers[iLayer]->setOutput(iNeuron, y);
                     }
                     break;
                 case ENUM_ACTIVATION_FUNCTION::ELU:
                     for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
-                        x = ComputeX(iLayer, iNeuron);
+                        x = total_layers[iLayer]->getInput(iNeuron);
                         y = x > 0 ? x : (exp(x) - 1);
-                        total_layers[iLayer]->setValue(iNeuron, y);
+                        total_layers[iLayer]->setOutput(iNeuron, y);
                     }
                     break;
                 case ENUM_ACTIVATION_FUNCTION::LINEAR:
                     for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
-                        x = ComputeX(iLayer, iNeuron);
+                        x = total_layers[iLayer]->getInput(iNeuron);
                         y = x;
-                        total_layers[iLayer]->setValue(iNeuron, y);
+                        total_layers[iLayer]->setOutput(iNeuron, y);
                     }
                     break;
                 case ENUM_ACTIVATION_FUNCTION::RELU:
                     for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
-                        x = ComputeX(iLayer, iNeuron);
+                        x = total_layers[iLayer]->getInput(iNeuron);
                         y = x > 0.0 ? x : 0.0;
-                        total_layers[iLayer]->setValue(iNeuron, y);
+                        total_layers[iLayer]->setOutput(iNeuron, y);
                     }
                     break;
                 case ENUM_ACTIVATION_FUNCTION::NONE:
                     for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
                         y = 0.0;
-                        total_layers[iLayer]->setValue(iNeuron, y);
+                        total_layers[iLayer]->setOutput(iNeuron, y);
                     }
                     break;
                 default:
@@ -91,7 +93,7 @@ void NeuralNetwork::predict(vector<su2double> &inputs){
         }
     }
     for(iNeuron=0; iNeuron<outputLayer->getNNeurons(); iNeuron++){
-        y_norm = outputLayer->getValue(iNeuron);
+        y_norm = outputLayer->getOutput(iNeuron);
         y = y_norm*(output_norm[iNeuron].second - output_norm[iNeuron].first) + output_norm[iNeuron].first;
         
         // Setting output value
@@ -99,38 +101,38 @@ void NeuralNetwork::predict(vector<su2double> &inputs){
     }
 }
 
-NeuralNetwork::NeuralNetwork(){
+MLPToolbox::CNeuralNetwork::CNeuralNetwork(){
     inputLayer = nullptr;
     outputLayer = nullptr;
     n_hidden_layers = 0;
 }
 
 
-void NeuralNetwork::defineInputLayer(unsigned long n_neurons){
+void MLPToolbox::CNeuralNetwork::defineInputLayer(unsigned long n_neurons){
     //cout << "Creating an input layer with " << n_neurons << " neurons. "<< endl;
-    inputLayer = new Layer(n_neurons);
+    inputLayer = new CLayer(n_neurons);
     inputLayer->setInput(true);
     input_norm.resize(n_neurons);
 }
 
-void NeuralNetwork::defineOutputLayer(unsigned long n_neurons){
+void MLPToolbox::CNeuralNetwork::defineOutputLayer(unsigned long n_neurons){
     //cout << "Creating an output layer with " << n_neurons << " neurons. "<< endl;
-    outputLayer = new Layer(n_neurons);
+    outputLayer = new CLayer(n_neurons);
     output_norm.resize(n_neurons);
 }
 
-void NeuralNetwork::push_hidden_layer(unsigned long n_neurons){
-    Layer *newLayer = new Layer(n_neurons);
+void MLPToolbox::CNeuralNetwork::push_hidden_layer(unsigned long n_neurons){
+    CLayer *newLayer = new CLayer(n_neurons);
     //cout << "Creating a hidden layer with " << n_neurons << " neurons. "<< endl;
     hiddenLayers.push_back(newLayer);
     n_hidden_layers ++;
 }
 
-void NeuralNetwork::sizeWeights(){
+void MLPToolbox::CNeuralNetwork::sizeWeights(){
     unsigned long i_layer{0};
     weights.resize(n_hidden_layers + 1);
     weights.at(i_layer).resize(inputLayer->getNNeurons());
-    Layer * previouslayer = inputLayer;
+    CLayer * previouslayer = inputLayer;
 
     if(n_hidden_layers != 0){
         for(size_t i_hidden_layer=0; i_hidden_layer < n_hidden_layers; i_hidden_layer++){
@@ -163,19 +165,16 @@ void NeuralNetwork::sizeWeights(){
     ANN_outputs = new su2double[outputLayer->getNNeurons()];
 }   
 
-void NeuralNetwork::setWeight(unsigned long i_layer, unsigned long i_neuron, unsigned long j_neuron, su2double value){
+void MLPToolbox::CNeuralNetwork::setWeight(unsigned long i_layer, unsigned long i_neuron, unsigned long j_neuron, su2double value){
     //weights.at(i_layer).at(i_neuron).at(j_neuron) = value;
     weights_mat[i_layer][j_neuron][i_neuron] = value;
 }
-void NeuralNetwork::displayNetwork(){
+void MLPToolbox::CNeuralNetwork::displayNetwork(){
     cout << "Input layer: " << inputLayer->getNNeurons() << " neurons, Activation Function: " <<  inputLayer->getActivationType() << endl;
     for(size_t i=0; i<total_layers[1]->getNNeurons(); i++){
         for(size_t j=0; j<inputLayer->getNNeurons(); j++){
             cout << weights_mat[0][i][j] << " ";
         }
-        su2double thingy[] = {1, 1, 1};
-        cout << GeometryToolbox::DotProduct(inputLayer->getNNeurons(), weights_mat[0][i], thingy) << endl;
-        cout << endl;
     }
     for(size_t i_layer=0; i_layer < hiddenLayers.size(); i_layer++){
         cout << "Hidden layer " << i_layer + 1 << ": " << hiddenLayers.at(i_layer)->getNNeurons() << " neurons, Activation Function: " <<  hiddenLayers.at(i_layer) ->getActivationType() << endl;
@@ -189,7 +188,7 @@ void NeuralNetwork::displayNetwork(){
     cout << "Output layer: "<<outputLayer->getNNeurons() <<" neurons, Activation Function: " << outputLayer->getActivationType() << endl;
 }
 
-void NeuralNetwork::setActivationFunction(unsigned long i_layer, string input)
+void MLPToolbox::CNeuralNetwork::setActivationFunction(unsigned long i_layer, string input)
 {
     if(input.compare("linear") == 0){
         //activation_functions[i_layer] = new Linear();
diff --git a/Common/src/toolboxes/multilayer_perceptron/CNeuron.cpp b/Common/src/toolboxes/multilayer_perceptron/CNeuron.cpp
new file mode 100644
index 00000000000..f52bdb007f2
--- /dev/null
+++ b/Common/src/toolboxes/multilayer_perceptron/CNeuron.cpp
@@ -0,0 +1,33 @@
+/*!
+ * \file CNeuron.cpp
+ * \brief Implementation of the neuron class to be used within the 
+ *      Layer class as a part of the NeuralNetwork class.
+ * \author E. Bunschoten
+ * \version 7.4.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+#include "../../../include/toolboxes/multilayer_perceptron/CNeuron.hpp"
+#include <iostream>
+#include <cstring>
+#include <cmath>
+
+using namespace std;
\ No newline at end of file
diff --git a/SU2_CFD/src/numerics/multilayer_perceptron/ReadNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
similarity index 71%
rename from SU2_CFD/src/numerics/multilayer_perceptron/ReadNeuralNetwork.cpp
rename to Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
index 13d0b64a14f..8c34674e260 100644
--- a/SU2_CFD/src/numerics/multilayer_perceptron/ReadNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
@@ -25,18 +25,18 @@
  * You should have received a copy of the GNU Lesser General Public
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
-#include "../../../include/numerics/multilayer_perceptron/ReadNeuralNetwork.hpp"
+#include "../../../include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp"
 using namespace std;
 
-ReadNeuralNetwork::ReadNeuralNetwork(string filename_in){
+MLPToolbox::CReadNeuralNetwork::CReadNeuralNetwork(string filename_in){
     filename = filename_in;
 };
 
-void ReadNeuralNetwork::ReadMLPFile(){
+void MLPToolbox::CReadNeuralNetwork::ReadMLPFile(){
     ifstream file_stream;
     file_stream.open(filename.c_str(), ifstream::in);
     if (!file_stream.is_open()) {
-      SU2_MPI::Error(string("There is no MLP file file called ") + filename,
+      SU2_MPI::Error(string("There is no MLP file called ") + filename,
                     CURRENT_FUNCTION);
     }
 
@@ -44,9 +44,13 @@ void ReadNeuralNetwork::ReadMLPFile(){
     double input_min, input_max, output_min, output_max;
     bool eoHeader{false}, found_layercount{false}, found_input_names{false}, found_output_names{false};
 
+    /* Read general architecture information from file header */
+
     line = SkipToFlag(&file_stream, "<header>");
 
     while(getline(file_stream, line) && !eoHeader){
+
+      /* Read layer count */
       if(line.compare("[number of layers]") == 0){
         getline(file_stream, line);
         n_layers = stoul(line);
@@ -58,7 +62,10 @@ void ReadNeuralNetwork::ReadMLPFile(){
         found_layercount = true;
       }
 
+      /* Set number of neurons for each layer */
       if(line.compare("[neurons per layer]") == 0){
+
+        /* In case layer count was not yet provided, return an error */
         if(!found_layercount){
           SU2_MPI::Error("No layer count provided before defining neuron count per layer", CURRENT_FUNCTION);
         }
@@ -86,6 +93,7 @@ void ReadNeuralNetwork::ReadMLPFile(){
         for(size_t iNeuron=0; iNeuron<n_neurons.at(n_neurons.size()-1); iNeuron++) output_norm.at(iNeuron) = make_pair(0, 1);
       }
 
+      /* Read layer activation function types */
       if(line.compare("[activation function]") == 0){
         if(!found_layercount){
           SU2_MPI::Error("No layer count provided before providing layer activation functions", CURRENT_FUNCTION);
@@ -98,6 +106,7 @@ void ReadNeuralNetwork::ReadMLPFile(){
         }    
       }
 
+      /* Read MLP input variable names */
       if(line.compare("[input names]") == 0){
         found_input_names = true;
         unsigned short j{1};
@@ -112,6 +121,7 @@ void ReadNeuralNetwork::ReadMLPFile(){
         }
       }
 
+      /* In case input normalization is applied, read upper and lower input bounds */
       if(line.compare("[input normalization]") == 0){
         for(size_t iInput=0; iInput<input_norm.size(); iInput++){
           getline(file_stream, line);
@@ -126,6 +136,7 @@ void ReadNeuralNetwork::ReadMLPFile(){
         }
       }
 
+      /* Read MLP output variable names */
       if(line.compare("[output names]") == 0){
         found_output_names = true;
         getline(file_stream, line);
@@ -139,6 +150,7 @@ void ReadNeuralNetwork::ReadMLPFile(){
         }
       }
 
+      /* In case output normalization is applied, read upper and lower output bounds */
       if(line.compare("[output normalization]") == 0){
         for(size_t iOutput=0; iOutput<output_norm.size(); iOutput++){
           getline(file_stream, line);
@@ -164,72 +176,7 @@ void ReadNeuralNetwork::ReadMLPFile(){
       SU2_MPI::Error("No MLP output variable names provided", CURRENT_FUNCTION);
     }
 
-
-    // line = SkipToFlag(&file_stream, "[number of layers]");
-    // getline(file_stream, line);
-    // n_layers = stoul(line);
-    // n_neurons.resize(n_layers);
-    // biases.resize(n_layers);
-    // weights.resize(n_layers-1);
-    // activation_functions.resize(n_layers);
-    // line = SkipToFlag(&file_stream, "[neurons per layer]");
-    // for(size_t iLayer=0; iLayer<n_layers; iLayer++){
-    //   getline(file_stream, line);
-    //   n_neurons.at(iLayer) = stoul(line);
-    //   biases.at(iLayer).resize(n_neurons.at(iLayer));
-    // }
-    // for(size_t iLayer=0; iLayer<n_layers-1; iLayer++){
-    //   weights.at(iLayer).resize(n_neurons.at(iLayer));
-    //   for(size_t iNeuron=0; iNeuron<n_neurons.at(iLayer); iNeuron++){
-    //     weights.at(iLayer).at(iNeuron).resize(n_neurons.at(iLayer+1));
-    //   }
-    // }
-
-    // input_norm.resize(n_neurons.at(0));
-    // output_norm.resize(n_neurons.at(n_neurons.size()-1));
-
-    // line = SkipToFlag(&file_stream, "[activation function]");
-    // for(size_t iLayer=0; iLayer<n_layers; iLayer++){
-    //   getline(file_stream, line);
-    //   istringstream activation_stream(line);
-    //   activation_stream >> word;
-    //   activation_functions.at(iLayer) = word;
-    // }    
-
-    // line = SkipToFlag(&file_stream, "[input names]");
-    // for(size_t iInput=0; iInput < n_neurons.at(0); iInput++){
-    //   getline(file_stream, line);
-    //   input_names.push_back(line);
-    // }
-
-    // line = SkipToFlag(&file_stream, "[input normalization]");
-    // for(size_t iInput=0; iInput<input_norm.size(); iInput++){
-    //   getline(file_stream, line);
-    //   istringstream input_norm_stream(line);
-    //   input_norm_stream >> word;
-    //   input_min = stold(word);
-    //   input_norm_stream >> word;
-    //   input_max = stold(word);
-    //   input_norm.at(iInput) = make_pair(input_min, input_max);
-    // }
-
-    // line = SkipToFlag(&file_stream, "[output names]");
-    // for(size_t iOutput=0; iOutput < n_neurons.at(n_neurons.size()-1); iOutput++){
-    //   getline(file_stream, line);
-    //   output_names.push_back(line);
-    // }
-
-    // line = SkipToFlag(&file_stream, "[output normalization]");
-    // for(size_t iOutput=0; iOutput<output_norm.size(); iOutput++){
-    //   getline(file_stream, line);
-    //   istringstream output_norm_stream(line);
-    //   output_norm_stream >> word;
-    //   output_min = stold(word);
-    //   output_norm_stream >> word;
-    //   output_max = stold(word);
-    //   output_norm.at(iOutput) = make_pair(output_min, output_max);
-    // }
-
+    /* Read weights for each layer */
     line = SkipToFlag(&file_stream, "[weights per layer]");
     for(size_t iLayer=0; iLayer<n_layers-1; iLayer++){
       getline(file_stream, line);
@@ -244,6 +191,7 @@ void ReadNeuralNetwork::ReadMLPFile(){
       getline(file_stream, line);
     }
     
+    /* Read biases for each neuron */
     line = SkipToFlag(&file_stream, "[biases per layer]");
     for(size_t iLayer=0; iLayer<n_layers; iLayer++){
       getline(file_stream, line);
@@ -258,7 +206,7 @@ void ReadNeuralNetwork::ReadMLPFile(){
 
 }
 
-string ReadNeuralNetwork::SkipToFlag(ifstream *file_stream, string flag) {
+string MLPToolbox::CReadNeuralNetwork::SkipToFlag(ifstream *file_stream, string flag) {
   string line;
   getline(*file_stream, line);
 
diff --git a/SU2_CFD/include/fluid/CMLPGas_Template.hpp b/SU2_CFD/include/fluid/CMLPGas_Template.hpp
new file mode 100644
index 00000000000..db3207c3313
--- /dev/null
+++ b/SU2_CFD/include/fluid/CMLPGas_Template.hpp
@@ -0,0 +1,102 @@
+/*!
+ * \file CMLPGas_Template.hpp
+ * \brief Defines a template fluid model class using multilayer perceptrons
+ *  for theromodynamic state definition
+ * \author E.Bunschoten
+ * \version 7.4.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+
+#pragma once
+
+#include "CFluidModel.hpp"
+#include "../../../Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp"
+/*!
+ * \class CMLPGas_Template
+ * \brief Template class for fluid model definition using multi-layer perceptrons for 
+ * fluid dynamic state definition.
+ * \author: E.Bunschoten.
+ */
+class CMLPGas_Template : public CFluidModel {
+ protected:
+  su2double Gamma{0.0};           /*!< \brief Ratio of Specific Heats. */
+  su2double Gamma_Minus_One{0.0}; /*!< \brief Ratio of Specific Heats Minus One. */
+  su2double Gas_Constant{0.0};    /*!< \brief Gas Constant. */
+  bool ComputeEntropy{true};      /*!< \brief Whether or not to compute entropy. */
+
+  string ann_input_filename;
+  MLPToolbox::CLookUp_ANN * lookup_ann;
+  vector<string> mlp_input_names, lookup_names;
+  vector<su2double*> lookup_data;
+
+  MLPToolbox::CIOMap * iomap_rhoe;
+  vector<string> input_names_rhoe, 
+                 output_names_rhoe;
+  vector<su2double*> outputs_rhoe;
+  
+  MLPToolbox::CIOMap * iomap_PT;
+  vector<string> input_names_PT, 
+                 output_names_PT;
+  vector<su2double*> outputs_PT;
+
+  MLPToolbox::CIOMap * iomap_Prho;
+  vector<string> input_names_Prho, 
+                 output_names_Prho;
+  vector<su2double*> outputs_Prho;
+
+  void MapInputs_to_Outputs();
+
+ public:
+  /*!
+   * \brief Constructor of the class.
+   */
+  CMLPGas_Template(su2double gamma, su2double R, bool CompEntropy = true);
+
+  ~CMLPGas_Template();
+  /*!
+   * \brief Set the Dimensionless State using Density and Internal Energy
+   * \param[in] rho - first thermodynamic variable.
+   * \param[in] e - second thermodynamic variable.
+   */
+  void SetTDState_rhoe(su2double rho, su2double e) override;
+
+  /*!
+   * \brief Set the Dimensionless State using Pressure  and Temperature
+   * \param[in] P - first thermodynamic variable.
+   * \param[in] T - second thermodynamic variable.
+   */
+  void SetTDState_PT(su2double P, su2double T) override;
+
+  /*!
+   * \brief Set the Dimensionless State using Pressure and Density
+   * \param[in] P - first thermodynamic variable.
+   * \param[in] rho - second thermodynamic variable.
+   */
+  void SetTDState_Prho(su2double P, su2double rho) override;
+
+  /*!
+   * \brief Set the Dimensionless Internal Energy using Pressure and Density
+   * \param[in] P - first thermodynamic variable.
+   * \param[in] rho - second thermodynamic variable.
+   */
+  void SetEnergy_Prho(su2double P, su2double rho) override;
+};
diff --git a/SU2_CFD/include/numerics/multilayer_perceptron/IOMap.hpp b/SU2_CFD/include/numerics/multilayer_perceptron/IOMap.hpp
deleted file mode 100644
index 2e2f14b1d75..00000000000
--- a/SU2_CFD/include/numerics/multilayer_perceptron/IOMap.hpp
+++ /dev/null
@@ -1,83 +0,0 @@
-/*!
- * \file IOMap.hpp
- * \brief Declaration of input-to-output mapping class for artifical neural networks
- * \author E. Bunschoten
- * \version 7.4.0 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-#pragma once
-
-#include <cmath>
-#include <string>
-#include <iostream>
-#include <limits>
-#include <cstdlib>
-#include <vector>
-#include "../../../../Common/include/CConfig.hpp"
-#include "../../../../Common/include/linear_algebra/blas_structure.hpp"
-#include "LookUp_ANN.hpp"
-
-using namespace std;
-class LookUp_ANN;
-
-class IOMap
-{
-    private:
-    vector<size_t> ANN_indices;
-    vector<vector<pair<size_t, size_t>>> Input_Map;
-    vector<vector<pair<size_t, size_t>>> Output_Map;
-    vector<vector<su2double>> input_indices;
-    public:
-    IOMap(){};
-    IOMap(LookUp_ANN*ANN_collection, vector<string> &inputs, vector<string> &outputs);
-    ~IOMap(){};
-    void Push_ANN_index(size_t i_ANN){ANN_indices.push_back(i_ANN);};
-    void PairVariableswithANNs(LookUp_ANN * ANN_collection, vector<string> &inputs, vector<string> &outputs);
-    size_t GetNANNs(){return ANN_indices.size();}
-    size_t GetANNIndex(size_t i_Map){return ANN_indices[i_Map];}
-    size_t GetInputIndex(size_t i_Map, size_t iInput){return Input_Map[i_Map][iInput].first;}
-    size_t GetOutputIndex(size_t i_Map, size_t iOutput){return Output_Map[i_Map][iOutput].first;}
-    size_t GetANNOutputIndex(size_t i_Map, size_t iOutput){return Output_Map[i_Map][iOutput].second;}
-    size_t GetNMappedOutputs(size_t i_Map){return Output_Map[i_Map].size();}
-
-    vector<pair<size_t, size_t>> GetOutputMapping(size_t i_map){return Output_Map[i_map];}
-    vector<pair<size_t, size_t>> GetInputMapping(size_t i_map){return Input_Map[i_map];}
-    
-    vector<su2double> GetANN_Inputs(size_t i_Map, vector<su2double>&inputs){
-        vector<su2double> ANN_input;
-        ANN_input.resize(Input_Map[i_Map].size());
-
-        for(size_t iInput=0; iInput<Input_Map[i_Map].size(); iInput++){
-            ANN_input.at(iInput) = inputs[GetInputIndex(i_Map, iInput)];
-        }
-        return ANN_input;
-    }
-    vector<su2double*> GetANN_Outputs(size_t i_Map, vector<su2double*>&outputs){
-        vector<su2double*> ANN_output;
-        ANN_output.resize(Output_Map[i_Map].size());
-
-        for(size_t iOutput=0; iOutput<Output_Map[i_Map].size(); iOutput++){
-            ANN_output.at(iOutput) = outputs[GetOutputIndex(i_Map, iOutput)];
-        }
-        return ANN_output;
-    }
-};
\ No newline at end of file
diff --git a/SU2_CFD/include/numerics/multilayer_perceptron/Layer.hpp b/SU2_CFD/include/numerics/multilayer_perceptron/Layer.hpp
deleted file mode 100644
index 892654901e9..00000000000
--- a/SU2_CFD/include/numerics/multilayer_perceptron/Layer.hpp
+++ /dev/null
@@ -1,63 +0,0 @@
-/*!
- * \file Layer.hpp
- * \brief Declaration of artificial neural network interpolation class
- * \author E. Bunschoten
- * \version 7.4.0 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-#pragma once
-
-#include <cmath>
-#include <iostream>
-#include <limits>
-#include <cstdlib>
-
-#include "../../../../Common/include/CConfig.hpp"
-#include "Neuron.hpp"
-#include "../../../../Common/include/linear_algebra/blas_structure.hpp"
-using namespace std;
-
-class Layer
-{
-private:
-    unsigned long number_of_neurons;
-    Neuron * neurons;
-    bool input;
-    string activation_type;
-public:
-    Layer();
-    Layer(unsigned long n_neurons);
-    void setNNeurons(unsigned long n_neurons);
-    unsigned long getNNeurons(){return number_of_neurons;};
-    void sayhi();
-    void setInput(bool def){input = def;};
-    bool isInput(){return input;};
-    void setValue(size_t i_neuron, su2double value){neurons[i_neuron].setValue(value);}
-    su2double getValue(size_t i_neuron){return neurons[i_neuron].getValue();}
-    void setBias(size_t i_neuron, su2double value){neurons[i_neuron].setBias(value);}
-    su2double getBias(size_t i_neuron){return neurons[i_neuron].getBias();}
-    su2double getdYdX(size_t i_neuron){return neurons[i_neuron].getGradient();}
-    string getActivationType(){return activation_type;}
-    ~Layer(){
-        delete [] neurons;
-    };
-};
diff --git a/SU2_CFD/include/numerics/multilayer_perceptron/Neuron.hpp b/SU2_CFD/include/numerics/multilayer_perceptron/Neuron.hpp
deleted file mode 100644
index 12e1012b09a..00000000000
--- a/SU2_CFD/include/numerics/multilayer_perceptron/Neuron.hpp
+++ /dev/null
@@ -1,74 +0,0 @@
-/*!
- * \file LookUp_ANN.hpp
- * \brief Declaration of artificial neural network perceptron class
- * \author E. Bunschoten
- * \version 7.4.0 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-#pragma once
-
-#include <cmath>
-#include <iostream>
-#include <limits>
-#include <cstdlib>
-
-#include "../../../../Common/include/CConfig.hpp"
-#include "../../../../Common/include/linear_algebra/blas_structure.hpp"
-
-using namespace std;
-class Neuron
-{
-private:
-    string activation_type="SmoothSlope";
-    unsigned long ActivationFunction{ENUM_ACTIVATION_FUNCTION::LINEAR};
-    unsigned long i_neuron;
-    double value;
-    su2double dy_dx;
-    double bias{0};
-    enum ENUM_ACTIVATION_FUNCTION {
-        NONE=0,
-        LINEAR=1,
-        RELU=2,
-        SMOOTH_SLOPE=3
-    };
-
-public:
-    Neuron(){};
-    void setNumber(unsigned long input){i_neuron = input;}
-    unsigned long getNumber(){return i_neuron;}
-    //void setFunctionType(string input);
-
-    //string getFunctionType(){return activation_type;}
-    //su2double activation_function(su2double x);
-    void setValue(su2double input){value = input;}
-    su2double getValue(){return value;}
-
-    void setBias(su2double input){bias = input;}
-    su2double getBias(){return bias;}
-
-    su2double getGradient(){return dy_dx;}
-    void setGradient(su2double input){dy_dx = input;}
-    //void SetActivationFunction(unsigned long input){ActivationFunction = input;}
-
-    ~Neuron(){};
-};
-
diff --git a/SU2_CFD/obj/Makefile.am b/SU2_CFD/obj/Makefile.am
index 140433ec93a..361d69d5af9 100644
--- a/SU2_CFD/obj/Makefile.am
+++ b/SU2_CFD/obj/Makefile.am
@@ -57,6 +57,7 @@ libSU2Core_sources = ../src/definition_structure.cpp \
   ../src/fluid/CNEMOGas.cpp \
   ../src/fluid/CSU2TCLib.cpp \
   ../src/fluid/CMutationTCLib.cpp \
+  ../src/fluid/CMLPGas.cpp \
   ../src/integration/CIntegration.cpp \
   ../src/integration/CSingleGridIntegration.cpp \
   ../src/integration/CMultiGridIntegration.cpp \
@@ -116,12 +117,6 @@ libSU2Core_sources = ../src/definition_structure.cpp \
   ../src/numerics/elasticity/CFEALinearElasticity.cpp \
   ../src/numerics/elasticity/CFEANonlinearElasticity.cpp \
   ../src/numerics/elasticity/nonlinear_models.cpp \
-  ../src/numerics/multilayer_perceptron/LookUp_ANN.cpp \
-  ../src/numerics/multilayer_perceptron/IOMap.cpp \
-  ../src/numerics/multilayer_perceptron/NeuralNetwork.cpp \
-  ../src/numerics/multilayer_perceptron/Neuron.cpp \
-  ../src/numerics/multilayer_perceptron/Layer.cpp \
-  ../src/numerics/multilayer_perceptron/ReadNeuralNetwork.cpp \
   ../include/numerics_simd/CNumericsSIMD.cpp \
   ../src/output/filewriter/CCSVFileWriter.cpp \
   ../src/output/filewriter/CSTLFileWriter.cpp \
diff --git a/SU2_CFD/src/fluid/CMLPGas_Template.cpp b/SU2_CFD/src/fluid/CMLPGas_Template.cpp
new file mode 100644
index 00000000000..44e00c5ec8d
--- /dev/null
+++ b/SU2_CFD/src/fluid/CMLPGas_Template.cpp
@@ -0,0 +1,125 @@
+/*!
+ * \file CMLPGas_Template.cpp
+ * \brief Source of the data-driven fluid model class using 
+ *  multilayer perceptrons for data regression
+ * \author E.Bunschoten
+ * \version 7.4.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+
+#include "../../include/fluid/CMLPGas_Template.hpp"
+
+CMLPGas_Template::CMLPGas_Template(su2double gamma, su2double R, bool CompEntropy) : CFluidModel() {
+  Gamma = gamma;
+  Gamma_Minus_One = Gamma - 1.0;
+  Gas_Constant = R;
+  Cp = Gamma / Gamma_Minus_One * Gas_Constant;
+  Cv = Cp - R;
+
+  ComputeEntropy = CompEntropy;
+
+  /* Define a CLookUp_ANN object to allow for data regression */
+  ann_input_filename = "MLP_collection.mlp";
+  lookup_ann = new MLPToolbox::CLookUp_ANN(ann_input_filename);
+
+  /* Map MLP inputs to outputs for each look-up operation*/
+  MapInputs_to_Outputs();
+}
+
+CMLPGas_Template::~CMLPGas_Template(){
+  delete iomap_rhoe;
+  delete iomap_PT;
+  delete iomap_Prho;
+  delete lookup_ann;
+}
+void CMLPGas_Template::MapInputs_to_Outputs(){
+
+  input_names_rhoe.push_back("rho");
+  input_names_rhoe.push_back("e");
+
+  output_names_rhoe.push_back("Temperature");
+  outputs_rhoe.push_back(&Temperature);
+  output_names_rhoe.push_back("Pressure");
+  outputs_rhoe.push_back(&Pressure);
+  output_names_rhoe.push_back("SoundSpeed2");
+  outputs_rhoe.push_back(&SoundSpeed2);
+  output_names_rhoe.push_back("dPdrho_e");
+  outputs_rhoe.push_back(&dPdrho_e);
+  output_names_rhoe.push_back("dPde_rho");
+  outputs_rhoe.push_back(&dPde_rho);
+  output_names_rhoe.push_back("dTdrho_e");
+  outputs_rhoe.push_back(&dTdrho_e);
+  output_names_rhoe.push_back("dTde_rho");
+  outputs_rhoe.push_back(&dTde_rho);
+  output_names_rhoe.push_back("Entropy");
+  outputs_rhoe.push_back(&Entropy);
+
+  iomap_rhoe = new MLPToolbox::CIOMap(lookup_ann, input_names_rhoe, output_names_rhoe);
+
+  input_names_PT.push_back("P");
+  input_names_PT.push_back("T");
+
+  output_names_PT.push_back("rho");
+  outputs_PT.push_back(&Density);
+  output_names_PT.push_back("e");
+  outputs_PT.push_back(&StaticEnergy);
+
+  iomap_PT = new MLPToolbox::CIOMap(lookup_ann, input_names_PT, output_names_PT);
+
+  input_names_Prho.push_back("P");
+  input_names_Prho.push_back("rho");
+
+  output_names_Prho.push_back("e");
+  outputs_Prho.push_back(&StaticEnergy);
+  iomap_Prho = new MLPToolbox::CIOMap(lookup_ann, input_names_Prho, output_names_Prho);
+}
+
+void CMLPGas_Template::SetTDState_rhoe(su2double rho, su2double e) {
+  vector<su2double> ann_inputs;
+  ann_inputs.push_back(rho);
+  ann_inputs.push_back(e);
+  lookup_ann->Predict_ANN(iomap_rhoe, ann_inputs, outputs_rhoe);
+}
+
+void CMLPGas_Template::SetTDState_PT(su2double P, su2double T) {
+  vector<su2double> ann_inputs;
+  ann_inputs.push_back(P);
+  ann_inputs.push_back(T);
+  lookup_ann->Predict_ANN(iomap_PT, ann_inputs, outputs_PT);
+
+  SetTDState_rhoe(Density, StaticEnergy);
+}
+
+void CMLPGas_Template::SetTDState_Prho(su2double P, su2double rho) {
+  vector<su2double> ann_inputs;
+  ann_inputs.push_back(P);
+  ann_inputs.push_back(rho);
+  lookup_ann->Predict_ANN(iomap_Prho, ann_inputs, outputs_Prho);
+  SetTDState_rhoe(rho, StaticEnergy);
+}
+
+void CMLPGas_Template::SetEnergy_Prho(su2double P, su2double rho) { 
+  vector<su2double> ann_inputs;
+  ann_inputs.push_back(P);
+  ann_inputs.push_back(rho);
+  lookup_ann->Predict_ANN(iomap_Prho, ann_inputs, outputs_Prho);
+}
diff --git a/SU2_CFD/src/meson.build b/SU2_CFD/src/meson.build
index 6e730d80ffc..e477f80b2b6 100644
--- a/SU2_CFD/src/meson.build
+++ b/SU2_CFD/src/meson.build
@@ -10,7 +10,8 @@ su2_cfd_src += files(['fluid/CFluidModel.cpp',
                       'fluid/CVanDerWaalsGas.cpp',
                       'fluid/CNEMOGas.cpp',
                       'fluid/CMutationTCLib.cpp',
-                      'fluid/CSU2TCLib.cpp'])
+                      'fluid/CSU2TCLib.cpp',
+                      'fluid/CMLPGas.cpp'])
 
 su2_cfd_src += files(['output/COutputFactory.cpp',
                       'output/CAdjElasticityOutput.cpp',
@@ -147,13 +148,7 @@ su2_cfd_src += files(['numerics/CNumerics.cpp',
                       'numerics/elasticity/CFEALinearElasticity.cpp',
                       'numerics/elasticity/CFEANonlinearElasticity.cpp',
                       'numerics/elasticity/nonlinear_models.cpp',
-                      'numerics/CGradSmoothing.cpp',
-                      'numerics/multilayer_perceptron/LookUp_ANN.cpp',
-                      'numerics/multilayer_perceptron/IOMap.cpp',
-                      'numerics/multilayer_perceptron/NeuralNetwork.cpp',
-                      'numerics/multilayer_perceptron/Layer.cpp',
-                      'numerics/multilayer_perceptron/Neuron.cpp',
-                      'numerics/multilayer_perceptron/ReadNeuralNetwork.cpp'])
+                      'numerics/CGradSmoothing.cpp'])
 
 su2_cfd_src += files(['../include/numerics_simd/CNumericsSIMD.cpp'])
 
diff --git a/SU2_CFD/src/numerics/multilayer_perceptron/Neuron.cpp b/SU2_CFD/src/numerics/multilayer_perceptron/Neuron.cpp
deleted file mode 100644
index 4fbef6a462e..00000000000
--- a/SU2_CFD/src/numerics/multilayer_perceptron/Neuron.cpp
+++ /dev/null
@@ -1,114 +0,0 @@
-/*!
- * \file Neuron.cpp
- * \brief Implementation of the neuron class to be used within the 
- *      Layer class as a part of the NeuralNetwork class.
- * \author E. Bunschoten
- * \version 7.4.0 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-#include "../../../include/numerics/multilayer_perceptron/Neuron.hpp"
-#include <iostream>
-#include <cstring>
-#include <cmath>
-
-using namespace std;
-// Neuron::Neuron()
-// {
-// }
-
-// su2double Neuron::activation_function(su2double x)
-// {
-//     x += bias;
-//     su2double tanx;
-//     switch(ActivationFunction){
-//         case ENUM_ACTIVATION_FUNCTION::LINEAR:
-//             dy_dx = 1;
-//             return x;
-//             break;
-//         case ENUM_ACTIVATION_FUNCTION::RELU:
-//             if(x > 0.0){
-//                 dy_dx = 1.0;
-//                 return x;
-//             }else{
-//                 dy_dx = 0.0;
-//                 return 0.0;
-//             }
-//             break;
-//         case ENUM_ACTIVATION_FUNCTION::SMOOTH_SLOPE:
-//             tanx = tanh(x);
-//             if(tanx > x){
-//                 dy_dx = 4.0 / pow((exp(-x) + exp(x)), 2); 
-//                 return tanx;
-//             }else{
-//                 dy_dx = 1.0;
-//                 return x;
-//             }
-//             break;
-//         default:
-//             SU2_MPI::Error(string("Unknown activation function type: ")+activation_type,
-//                     CURRENT_FUNCTION);
-//             return 0.0;
-//         break;
-//     }
-//     // if(activation_type.compare("smooth_slope") == 0){
-//     //     su2double tanx = tanh(x);
-//     //     if(tanx > x){
-//     //         dy_dx = 4.0 / pow((exp(-x) + exp(x)), 2); 
-//     //         return tanx;
-//     //     }else{
-//     //         dy_dx = 1.0;
-//     //         return x;
-//     //     }
-
-//     // }
-//     // if(activation_type.compare("linear") == 0){
-//     //     dy_dx = 1.0;
-//     //     return x;
-//     // }
-//     // if(activation_type.compare("relu") == 0){
-//     //     su2double zero{0.0};
-//     //     if(x > zero){
-//     //         dy_dx = 1.0;
-//     //         return x;
-//     //     }else{
-//     //         dy_dx = 0.0;
-//     //         return zero;
-//     //     }
-//     // }
-    
-//     // SU2_MPI::Error(string("Unknown activation function type: ")+activation_type,
-//     //                CURRENT_FUNCTION);   
-    
-//     // return x;
-// }
-
-// void Neuron::setFunctionType(string input){
-//     activation_type = input;
-
-//     if(input.compare("smooth_slope") == 0) ActivationFunction = ENUM_ACTIVATION_FUNCTION::SMOOTH_SLOPE; return;
-    
-//     if(input.compare("linear") == 0) ActivationFunction = ENUM_ACTIVATION_FUNCTION::LINEAR; return;
-
-//     if(input.compare("relu") == 0) ActivationFunction = ENUM_ACTIVATION_FUNCTION::RELU; return;
-
-//     if(input.compare("none") == 0) ActivationFunction = ENUM_ACTIVATION_FUNCTION::NONE; return;
-// }
\ No newline at end of file

From 9e32ee0672289517ad7a3172b75e025b255eae44 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Thu, 15 Sep 2022 14:14:51 +0200
Subject: [PATCH 032/656] fixed build bug

---
 SU2_CFD/obj/Makefile.am | 2 +-
 SU2_CFD/src/meson.build | 2 +-
 2 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/SU2_CFD/obj/Makefile.am b/SU2_CFD/obj/Makefile.am
index 361d69d5af9..5ba91fd0d4e 100644
--- a/SU2_CFD/obj/Makefile.am
+++ b/SU2_CFD/obj/Makefile.am
@@ -57,7 +57,7 @@ libSU2Core_sources = ../src/definition_structure.cpp \
   ../src/fluid/CNEMOGas.cpp \
   ../src/fluid/CSU2TCLib.cpp \
   ../src/fluid/CMutationTCLib.cpp \
-  ../src/fluid/CMLPGas.cpp \
+  ../src/fluid/CMLPGas_Template.cpp \
   ../src/integration/CIntegration.cpp \
   ../src/integration/CSingleGridIntegration.cpp \
   ../src/integration/CMultiGridIntegration.cpp \
diff --git a/SU2_CFD/src/meson.build b/SU2_CFD/src/meson.build
index e477f80b2b6..9d81ec13f71 100644
--- a/SU2_CFD/src/meson.build
+++ b/SU2_CFD/src/meson.build
@@ -11,7 +11,7 @@ su2_cfd_src += files(['fluid/CFluidModel.cpp',
                       'fluid/CNEMOGas.cpp',
                       'fluid/CMutationTCLib.cpp',
                       'fluid/CSU2TCLib.cpp',
-                      'fluid/CMLPGas.cpp'])
+                      'fluid/CMLPGas_Template.cpp'])
 
 su2_cfd_src += files(['output/COutputFactory.cpp',
                       'output/CAdjElasticityOutput.cpp',

From b233278084092bf9fe26077b6f829cc763e7d981 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Thu, 15 Sep 2022 14:27:38 +0200
Subject: [PATCH 033/656] Fixed unused-variable error

---
 Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp | 1 -
 1 file changed, 1 deletion(-)

diff --git a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
index 331e08c11c7..f63e57038a7 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
@@ -188,7 +188,6 @@ bool MLPToolbox::CLookUp_ANN::Check_Duplicate_Outputs(vector<string> &output_nam
     for(size_t i_Output =0; i_Output < output_names.size(); i_Output++){
         n_occurances = 0;
         for(size_t i_map=0; i_map<input_output_map->GetNANNs(); i_map++){
-            size_t i_ANN =  input_output_map->GetANNIndex(i_map);
             vector<pair<size_t, size_t>> output_map = input_output_map->GetOutputMapping(i_map);
             for(size_t j_Output=0; j_Output<output_map.size(); j_Output++){
                 if(output_map[j_Output].first == i_Output) n_occurances++;

From 47b456cb3d65ce3f29a6521e947caec819eb8335 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Thu, 15 Sep 2022 14:44:28 +0200
Subject: [PATCH 034/656] Fixed unused-variable error

---
 Common/src/toolboxes/multilayer_perceptron/CLayer.cpp        | 2 +-
 .../src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp   | 5 ++---
 2 files changed, 3 insertions(+), 4 deletions(-)

diff --git a/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp b/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp
index 74f1e702063..b53a397fbd5 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp
@@ -29,7 +29,7 @@
 #include <cstring>
 using namespace std;
 
-MLPToolbox::CLayer::CLayer() : CLayer(1) {};
+MLPToolbox::CLayer::CLayer() : CLayer(1) {}
 
 MLPToolbox::CLayer::CLayer(unsigned long n_neurons) : number_of_neurons{n_neurons}, is_input{false}
 {
diff --git a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
index b4344662613..496ac851048 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
@@ -33,8 +33,8 @@ using namespace std;
 
 
 void MLPToolbox::CNeuralNetwork::predict(vector<su2double> &inputs){
-    su2double x, x_norm, y, y_norm, tanx;
-    size_t iNeuron, jNeuron, iLayer, nNeurons_current, nNeurons_previous;
+    su2double x, x_norm, y, y_norm;
+    size_t iNeuron, iLayer, nNeurons_current;
     bool same_point{true};
     for(iNeuron=0; iNeuron<inputLayer->getNNeurons(); iNeuron++){
         x_norm = (inputs[iNeuron] - input_norm[iNeuron].first)/(input_norm[iNeuron].second - input_norm[iNeuron].first);
@@ -44,7 +44,6 @@ void MLPToolbox::CNeuralNetwork::predict(vector<su2double> &inputs){
     if(!same_point){
         for(iLayer=1; iLayer<n_hidden_layers + 2; iLayer++){
             nNeurons_current = total_layers[iLayer]->getNNeurons();
-            nNeurons_previous = total_layers[iLayer - 1]->getNNeurons();
 
             for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
                 x = ComputeX(iLayer, iNeuron);

From 88f0012afd0ac8f2b10778faadd0c0af4e8507d9 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 26 Sep 2022 10:59:15 +0200
Subject: [PATCH 035/656] Added more comments to CIOMap and CLookUp_ANN classes

---
 .../multilayer_perceptron/CIOMap.hpp          | 171 ++++++++++++++----
 .../multilayer_perceptron/CLayer.hpp          |  17 +-
 .../multilayer_perceptron/CLookUp_ANN.hpp     |  38 ++--
 .../multilayer_perceptron/CNeuralNetwork.hpp  |  52 +++---
 .../multilayer_perceptron/CNeuron.hpp         |   3 +-
 .../CReadNeuralNetwork.hpp                    |  43 +++--
 .../multilayer_perceptron/CIOMap.cpp          |  45 +++--
 .../multilayer_perceptron/CLookUp_ANN.cpp     |  18 +-
 .../multilayer_perceptron/CNeuralNetwork.cpp  | 132 +++++++++-----
 SU2_CFD/src/fluid/CPengRobinson.cpp           |  51 ++++++
 10 files changed, 395 insertions(+), 175 deletions(-)

diff --git a/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp b/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
index f0ef33fefed..8d0c97aa696 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
@@ -32,56 +32,157 @@
 #include <limits>
 #include <cstdlib>
 #include <vector>
-#include "../../CConfig.hpp"
 #include "../../linear_algebra/blas_structure.hpp"
 #include "CLookUp_ANN.hpp"
 
-using namespace std;
 namespace MLPToolbox
 {
         
     class CLookUp_ANN;
 
     class CIOMap
+    /*! 
+    *\class CIOMap
+    *\brief This class is used by the CLookUp_ANN class to assign user-defined inputs 
+    * and outputs to loaded multi-layer perceptrons. When a look-up operation is called
+    * with a specific CIOMap, the multi-layer perceptrons are evaluated with input and
+    * output variables coinciding with the desired input and output variable names.
+    * 
+    *
+    * For example, in a custom, data-driven fluid model, MLP's are used for thermodynamic state
+    * definition. There are three MLP's loaded. MLP_1 predicts temperature and specific heat 
+    * based on density and energy. MLP_2 predicts pressure and speed of sound based on density and
+    * energy as well. MLP_3 predicts density and energy based on pressure and temperature.
+    * During a certain look-up operation in the CFluidModel, temperature, speed of sound and pressure 
+    * are needed for a given density and energy. What the CIOMap does is to point to MLP_1 for 
+    * temperature evalutation, and to MLP_2 for pressure and speed of sound evaluation. MLP_3 is 
+    * not considered, as the respective inputs and outputs don't match with the function call
+    * inputs and outputs.
+    * 
+    *  call variables:      MLP inputs:                     MLP outputs:           call outputs:
+    *   
+    *                        2--> energy --|            |--> temperature --> 1       
+    *                                      |--> MLP_1 --|       
+    *  1:density            1--> density --|            |--> c_p                   1:temperature
+    *  2:energy                                                                    2:speed of sound
+    *                       1--> density --|            |--> pressure --> 3        3:pressure
+    *                                      |--> MLP_2 --|
+    *                        2--> energy --|            |--> speed of sound --> 2
+    * 
+    *                           pressure --|            |--> density
+    *                                      |--> MLP_3 --|
+    *                        temperature --|            |--> energy
+    * 
+    * 
+    * \author E.Bunschoten
+    */
+
     {
         private:
-        vector<size_t> ANN_indices;
-        vector<vector<pair<size_t, size_t>>> Input_Map;
-        vector<vector<pair<size_t, size_t>>> Output_Map;
-        vector<vector<su2double>> input_indices;
-        public:
-        CIOMap(){};
-        CIOMap(CLookUp_ANN*ANN_collection, vector<string> &inputs, vector<string> &outputs);
-        ~CIOMap(){};
-        void Push_ANN_index(size_t i_ANN){ANN_indices.push_back(i_ANN);};
-        void PairVariableswithANNs(CLookUp_ANN * ANN_collection, vector<string> &inputs, vector<string> &outputs);
-        size_t GetNANNs(){return ANN_indices.size();}
-        size_t GetANNIndex(size_t i_Map){return ANN_indices[i_Map];}
-        size_t GetInputIndex(size_t i_Map, size_t iInput){return Input_Map[i_Map][iInput].first;}
-        size_t GetOutputIndex(size_t i_Map, size_t iOutput){return Output_Map[i_Map][iOutput].first;}
-        size_t GetANNOutputIndex(size_t i_Map, size_t iOutput){return Output_Map[i_Map][iOutput].second;}
-        size_t GetNMappedOutputs(size_t i_Map){return Output_Map[i_Map].size();}
-
-        vector<pair<size_t, size_t>> GetOutputMapping(size_t i_map){return Output_Map[i_map];}
-        vector<pair<size_t, size_t>> GetInputMapping(size_t i_map){return Input_Map[i_map];}
+        std::vector<std::size_t> MLP_indices;       /*!< Loaded MLP index */
+
+        std::vector<std::vector<std::pair<std::size_t, std::size_t>>> 
+            Input_Map,      /*!< Mapping of call variable inputs to matching MLP inputs */
+            Output_Map;     /*!< Mapping of call variable outputs to matching MLP outputs */
+
+        std::vector<std::vector<su2double>> input_indices;  /*!< */
         
-        vector<su2double> GetANN_Inputs(size_t i_Map, vector<su2double>&inputs){
-            vector<su2double> ANN_input;
-            ANN_input.resize(Input_Map[i_Map].size());
+        public:
 
-            for(size_t iInput=0; iInput<Input_Map[i_Map].size(); iInput++){
-                ANN_input.at(iInput) = inputs[GetInputIndex(i_Map, iInput)];
-            }
-            return ANN_input;
-        }
-        vector<su2double*> GetANN_Outputs(size_t i_Map, vector<su2double*>&outputs){
-            vector<su2double*> ANN_output;
-            ANN_output.resize(Output_Map[i_Map].size());
+        /*!
+        * \brief CIOMap class constructor;
+        * \param[in] MLP_collection - Pointer to CLookUp_ANN class for which the input-output amap is to be created
+        * \param[in] inputs - Input names for the call function. These should match with at least one of the MLP inputs.
+        * \param[in] outputs - Output names for the call function. These should match with at least one of the MLP outputs.
+        */
+        CIOMap(CLookUp_ANN*MLP_collection, std::vector<std::string> &inputs, std::vector<std::string> &outputs);
+
+        /*!
+        * \brief Set MLP index in IO map
+        * \param[in] i_MLP - loaded MLP index
+        */
+        void Push_MLP_index(std::size_t i_MLP){MLP_indices.push_back(i_MLP);};
+
+        /*!
+        * \brief Pair call inputs and outputs with the inputs and outputs of 
+                the loaded MLPs
+        * \param[in] MLP_collection - pointer to MLP collection class
+        * \param[in] inputs - vector with call input variable names
+        * \param[in] outputs - vector with call output variable names
+        */
+        void PairVariableswithMLPs(CLookUp_ANN * MLP_collection, std::vector<std::string> &inputs, std::vector<std::string> &outputs);
+
+        /*!
+        * \brief Get the number of MLPs in the current IO map
+        * \return number of MLPs with matching inputs and output(s)
+        */
+        std::size_t GetNMLPs() const {return MLP_indices.size();}
+
+        /*!
+        * \brief Get the loaded MLP index
+        * \return MLP index
+        */
+        std::size_t GetMLPIndex(std::size_t i_Map) const {return MLP_indices[i_Map];}
+
+        /*!
+        * \brief Get the call input variable index 
+        * \param[in] i_Map - input-output mapping index of the IO map
+        * \param[in] i_Input - input index of the call input variable
+        * \return MLP input variable index
+        */
+        std::size_t GetInputIndex(std::size_t i_Map, std::size_t i_Input) const {return Input_Map[i_Map][i_Input].first;}
+
+        /*!
+        * \brief Get the call output variable index 
+        * \param[in] i_Map - input-output mapping index of the IO map
+        * \param[in] i_Output - output index of the call input variable
+        * \return call variable output index
+        */
+        std::size_t GetOutputIndex(std::size_t i_Map, std::size_t i_Output) const {return Output_Map[i_Map][i_Output].first;}
+
+        /*!
+        * \brief Get the MLP output variable index 
+        * \param[in] i_Map - input-output mapping index of the IO map
+        * \param[in] i_Output - output index of the call input variable
+        * \return MLP output variable index
+        */
+        std::size_t GetMLPOutputIndex(std::size_t i_Map, std::size_t i_Output) const {return Output_Map[i_Map][i_Output].second;}
+
+        /*!
+        * \brief Get the number of matching output variables between the call and MLP outputs
+        * \param[in] i_Map - input-output mapping index of the IO map
+        * \return Number of matching variables between the loaded MLP and call variables
+        */
+        std::size_t GetNMappedOutputs(std::size_t i_Map) const {return Output_Map[i_Map].size();}
+
+        /*!
+        * \brief Get the mapping of MLP outputs matching to call outputs
+        * \param[in] i_Map - input-output mapping index of the IO map
+        * \return Mapping of MLP output variables to call variables
+        */
+        std::vector<std::pair<std::size_t, std::size_t>> GetOutputMapping(std::size_t i_map) const {return Output_Map[i_map];}
+
+        /*!
+        * \brief Get the mapping of MLP inputs to call inputs
+        * \param[in] i_Map - input-output mapping index of the IO map
+        * \return Mapping of MLP input variables to call inputs
+        */
+        std::vector<std::pair<std::size_t, std::size_t>> GetInputMapping(std::size_t i_map) const{return Input_Map[i_map];}
+        
+        /*!
+        * \brief Get the mapped inputs for the MLP at i_Map
+        * \param[in] i_Map - input-output mapping index of the IO map
+        * \param[in] inputs - call inputs
+        * \return Vector with call inputs in the correct order of the loaded MLP
+        */
+        std::vector<su2double> GetMLP_Inputs(std::size_t i_Map, std::vector<su2double>&inputs) const {
+            std::vector<su2double> MLP_input;
+            MLP_input.resize(Input_Map[i_Map].size());
 
-            for(size_t iOutput=0; iOutput<Output_Map[i_Map].size(); iOutput++){
-                ANN_output.at(iOutput) = outputs[GetOutputIndex(i_Map, iOutput)];
+            for(std::size_t i_Input=0; i_Input<Input_Map[i_Map].size(); i_Input++){
+                MLP_input[i_Input] = inputs[GetInputIndex(i_Map, i_Input)];
             }
-            return ANN_output;
+            return MLP_input;
         }
     };
 }
diff --git a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
index ee8aac9bd74..c72709fe52e 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
@@ -34,7 +34,6 @@
 #include "../../CConfig.hpp"
 #include "CNeuron.hpp"
 #include "../../linear_algebra/blas_structure.hpp"
-using namespace std;
 
 namespace MLPToolbox{
 class CLayer
@@ -43,7 +42,7 @@ class CLayer
     unsigned long number_of_neurons;    /*!< Neuron count in current layer */
     CNeuron * neurons;                   /*!< Array of neurons in current layer */
     bool is_input;                      /*!< Input layer identifyer */
-    string activation_type;             /*!< Activation function type applied to the current layer*/
+    std::string activation_type;             /*!< Activation function type applied to the current layer*/
 public:
     CLayer();
     CLayer(unsigned long n_neurons);
@@ -77,49 +76,49 @@ class CLayer
     * \param[in] i_neuron - Neuron index
     * \param[in] output_value - Activation function output
     */
-    void setOutput(size_t i_neuron, su2double value){neurons[i_neuron].setOutput(value);}
+    void setOutput(std::size_t i_neuron, su2double value){neurons[i_neuron].setOutput(value);}
 
     /*!
     * \brief Get the output value of a neuron in the layer
     * \param[in] i_neuron - Neuron index
     * \return Neuron output value
     */
-    su2double getOutput(size_t i_neuron) const {return neurons[i_neuron].getOutput();}
+    su2double getOutput(std::size_t i_neuron) const {return neurons[i_neuron].getOutput();}
 
     /*!
     * \brief Set the input value of a neuron in the layer
     * \param[in] i_neuron - Neuron index
     * \param[in] input_value - Activation function input
     */
-    void setInput(size_t i_neuron, su2double value){neurons[i_neuron].setInput(value);}
+    void setInput(std::size_t i_neuron, su2double value){neurons[i_neuron].setInput(value);}
 
     /*!
     * \brief Get the input value of a neuron in the layer
     * \param[in] i_neuron - Neuron index
     * \return Neuron input value
     */
-    su2double getInput(size_t i_neuron) const {return neurons[i_neuron].getInput();}
+    su2double getInput(std::size_t i_neuron) const {return neurons[i_neuron].getInput();}
 
     /*!
     * \brief Set the bias value of a neuron in the layer
     * \param[in] i_neuron - Neuron index
     * \param[in] bias_value - Bias value
     */
-    void setBias(size_t i_neuron, su2double value){neurons[i_neuron].setBias(value);}
+    void setBias(std::size_t i_neuron, su2double value){neurons[i_neuron].setBias(value);}
 
     /*!
     * \brief Get the bias value of a neuron in the layer
     * \param[in] i_neuron - Neuron index
     * \return Neuron bias value
     */
-    su2double getBias(size_t i_neuron){return neurons[i_neuron].getBias();}
+    su2double getBias(std::size_t i_neuron){return neurons[i_neuron].getBias();}
 
     /*!
     * \brief Get the output-input gradient of a neuron in the layer
     * \param[in] i_neuron - Neuron index
     * \return Gradient of neuron output wrt input
     */
-    su2double getdYdX(size_t i_neuron){return neurons[i_neuron].getGradient();}
+    su2double getdYdX(std::size_t i_neuron){return neurons[i_neuron].getGradient();}
 
     /*!
     * \brief Get the activation function name applied to this layer
diff --git a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
index 3b7a0baaf02..f2306470a98 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
@@ -38,18 +38,26 @@
 #include "CNeuralNetwork.hpp"
 #include "CIOMap.hpp"
 
-using namespace std;
 
 namespace MLPToolbox{
-class CIOMap;
 
 class CLookUp_ANN
 {
+    /*! 
+    *\class CLookUp_ANN
+    *\brief This class allows for the evaluation of one or more multi-layer perceptrons in for example
+    * thermodynamic state look-up operations. The multi-layer perceptrons are loaded in the order listed
+    * in the MLP collection file. Each multi-layer perceptron is generated based on the 
+    * architecture described in its respective input file. When evaluating the MLP collection, an
+    * input-output map is used to find the correct MLP corresponding to the call function inputs and 
+    * outputs.  
+    */
+
     private:
     int rank{0};
-    vector<CNeuralNetwork*> NeuralNetworks;  /*!< Vector containing all loaded neural networks. */
+    std::vector<CNeuralNetwork*> NeuralNetworks;  /*!< std::vector containing all loaded neural networks. */
 
-    vector<string> ANN_filenames;       /*!< Filenames containing ANN architecture information. */
+    std::vector<std::string> ANN_filenames;       /*!< Filenames containing ANN architecture information. */
 
     unsigned long number_of_variables;  /*!< Number of loaded ANNs. */
 
@@ -59,20 +67,20 @@ class CLookUp_ANN
    * \param[in] flag - line to search for
    * \return line in file.
    */
-    string SkipToFlag(ifstream *file_stream, string flag); 
+    std::string SkipToFlag(ifstream *file_stream, std::string flag); 
 
     /*!
     * \brief Load ANN architecture
     * \param[in] ANN - pointer to target NeuralNetwork class
     * \param[in] filename - filename containing ANN architecture information
     */
-    void GenerateANN(CNeuralNetwork*ANN, string filename);
+    void GenerateANN(CNeuralNetwork*ANN, std::string filename);
 
     /*!
     * \brief Read ANN architecture input file
     * \param[in] filename - filename containing ANN architecture information
     */
-    void ReadANNInputFile(string fileName); 
+    void ReadANNInputFile(std::string fileName); 
     
     public: 
     
@@ -80,7 +88,7 @@ class CLookUp_ANN
     * \brief ANN collection class constructor
     * \param[in] filename - filename containing list of ANN input files
     */
-    CLookUp_ANN(string fileName);
+    CLookUp_ANN(std::string fileName);
     
     /*!
     * \brief Evaluate loaded ANNs for given inputs and outputs
@@ -88,9 +96,9 @@ class CLookUp_ANN
     * \param[in] inputs - input values
     * \param[in] outputs - pointers to output variables
     */
-    void Predict_ANN(CIOMap *input_output_map, vector<su2double> &inputs, vector<su2double*> &outputs);
+    void Predict_ANN(CIOMap *input_output_map, std::vector<su2double> &inputs, std::vector<su2double*> &outputs);
 
-    ~CLookUp_ANN(){for(size_t i_ANN=0; i_ANN<number_of_variables; i_ANN++)
+    ~CLookUp_ANN(){for(std::size_t i_ANN=0; i_ANN<number_of_variables; i_ANN++)
         delete NeuralNetworks.at(i_ANN);
     };
 
@@ -98,28 +106,28 @@ class CLookUp_ANN
     * \brief Get number of loaded ANNs
     * \return number of loaded ANNs
     */
-    size_t GetNANNs() const {return NeuralNetworks.size();}
+    std::size_t GetNANNs() const {return NeuralNetworks.size();}
 
     /*!
     * \brief Check if variables occur more than once in ANN outputs
     * \param[in] output_names - output variable names to check
     * \param[in] input_output_map - pointer to input-output map to be checked
     */
-    bool Check_Duplicate_Outputs(vector<string> &output_names, CIOMap *input_output_map) const;
+    bool Check_Duplicate_Outputs(std::vector<std::string> &output_names, CIOMap *input_output_map) const;
 
     /*!
     * \brief Check if all output variables are present in the loaded ANNs
     * \param[in] output_names - output variable names to check
     * \param[in] input_output_map - pointer to input-output map to be checked
     */
-    bool Check_Use_of_Outputs(vector<string> &output_names, CIOMap *input_output_map) const;
+    bool Check_Use_of_Outputs(std::vector<std::string> &output_names, CIOMap *input_output_map) const;
 
     /*!
     * \brief Check if all input variables are present in the loaded ANNs
     * \param[in] input_names - input variable names to check
     * \param[in] input_output_map - pointer to input-output map to be checked
     */
-    bool Check_Use_of_Inputs(vector<string> &input_names, CIOMap *input_output_map) const;
+    bool Check_Use_of_Inputs(std::vector<std::string> &input_names, CIOMap *input_output_map) const;
 
     /*!
     * \brief Map variable names to ANN inputs or outputs
@@ -127,7 +135,7 @@ class CLookUp_ANN
     * \param[in] variable_names - variable names to map to ANN inputs or outputs
     * \param[in] input - map to inputs (true) or outputs (false)
     */
-    vector<pair<size_t, size_t>> FindVariable_Indices(size_t i_ANN, vector<string> variable_names, bool input) const;
+    std::vector<pair<std::size_t, std::size_t>> FindVariable_Indices(std::size_t i_ANN, std::vector<std::string> variable_names, bool input) const;
     
 };  
 
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
index 6e54cd363a8..a7d1cfba5e4 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
@@ -37,12 +37,11 @@
 #include "../../linear_algebra/blas_structure.hpp"
 #include "CLayer.hpp"
 
-using namespace std;
 namespace MLPToolbox{
 class CNeuralNetwork
 {
 private:
-    vector<string> input_names,
+    std::vector<std::string> input_names,
                    output_names;
 
     unsigned long n_hidden_layers;
@@ -50,16 +49,16 @@ class CNeuralNetwork
     CLayer *inputLayer,
            *outputLayer;
 
-    vector<CLayer*> hiddenLayers,
+    std::vector<CLayer*> hiddenLayers,
                     total_layers;
 
-    vector<vector<vector<su2double>>> weights;
-    vector<su2activematrix> weights_mat;
-    vector<vector<su2double>> values;
+    //std::vector<std::vector<std::vector<su2double>>> weights;
+    std::vector<su2activematrix> weights_mat;
+    std::vector<std::vector<su2double>> values;
 
-    vector<pair<su2double, su2double>> input_norm,
+    std::vector<std::pair<su2double, su2double>> input_norm,
                                        output_norm;
-    vector<su2double> last_inputs;
+    std::vector<su2double> last_inputs;
 
     su2double* ANN_outputs;
 
@@ -68,14 +67,19 @@ class CNeuralNetwork
         LINEAR=1,
         RELU=2,
         SMOOTH_SLOPE=3,
-        ELU = 4
+        ELU = 4,
+        GELU = 5,
+        SELU = 6,
+        SIGMOID = 7,
+        SWISH = 8,
+        TANH = 9
     };
     ENUM_ACTIVATION_FUNCTION * activation_function_types;
 
 public:
     CNeuralNetwork();
     ~CNeuralNetwork(){
-        for(size_t i=0; i<total_layers.size(); i++){
+        for(std::size_t i=0; i<total_layers.size(); i++){
             delete total_layers.at(i);
         }
         delete [] ANN_outputs;
@@ -85,41 +89,41 @@ class CNeuralNetwork
     void push_hidden_layer(unsigned long n_neurons);
     void setWeight(unsigned long i_layer, unsigned long i_neuron, unsigned long j_neuron, su2double value);
     void setBias(unsigned long i_layer, unsigned long i_neuron, su2double value){total_layers.at(i_layer)->setBias(i_neuron, value);}
-    void setActivationFunction(unsigned long i_layer, string input);
+    void setActivationFunction(unsigned long i_layer, std::string input);
     void displayNetwork();
     void sizeWeights();
     void sizeInputs(unsigned long n_inputs){last_inputs.resize(n_inputs); for(unsigned long iInput=0; iInput<n_inputs; iInput++) last_inputs.at(iInput) = 0.0;}
-    unsigned long getNWeightLayers(){return weights.size();}
+    unsigned long getNWeightLayers(){return total_layers.size()-1;}
     unsigned long getNLayers(){return total_layers.size();}
 
     unsigned long getNNeurons(unsigned long iLayer){;
     return total_layers.at(iLayer)->getNNeurons();}
-    unsigned long getNNeurons(unsigned long iLayer, unsigned long iNeuron){return weights.at(iLayer).at(iNeuron).size();}
+    //unsigned long getNNeurons(unsigned long iLayer, unsigned long iNeuron){return weights.at(iLayer).at(iNeuron).size();}
 
-    void predict(vector<su2double> &inputs);
+    void predict(std::vector<su2double> &inputs);
 
 
     void SetInputNorm(unsigned long iInput, su2double input_min, su2double input_max){input_norm.at(iInput) = make_pair(input_min, input_max);}
     void SetOutputNorm(unsigned long iOutput, su2double output_min, su2double output_max){output_norm.at(iOutput) = make_pair(output_min, output_max);}
     
-    void PushOutputName(string input){output_names.push_back(input);}
-    void PushInputName(string input){input_names.push_back(input);}
+    void PushOutputName(std::string input){output_names.push_back(input);}
+    void PushInputName(std::string input){input_names.push_back(input);}
    
-    string GetInputName(size_t iInput){return input_names[iInput];}
-    string GetOutputName(size_t iOutput){return output_names[iOutput];}
+    std::string GetInputName(std::size_t iInput){return input_names[iInput];}
+    std::string GetOutputName(std::size_t iOutput){return output_names[iOutput];}
 
-    size_t GetnInputs(){return input_names.size();}
-    size_t GetnOutputs(){return output_names.size();}
+    std::size_t GetnInputs(){return input_names.size();}
+    std::size_t GetnOutputs(){return output_names.size();}
 
-    su2double GetANN_Output(size_t iOutput){return ANN_outputs[iOutput];}
+    su2double GetANN_Output(std::size_t iOutput){return ANN_outputs[iOutput];}
     void SizeActivationFunctions(unsigned long n_layers){activation_function_types = new ENUM_ACTIVATION_FUNCTION[n_layers]; 
     }
 
-    su2double ComputeX(size_t iLayer, size_t iNeuron){
+    su2double ComputeX(std::size_t iLayer, std::size_t iNeuron){
         su2double x;
         x = total_layers[iLayer]->getBias(iNeuron);
-        size_t nNeurons_previous = total_layers[iLayer - 1]->getNNeurons();
-        for(size_t jNeuron=0; jNeuron<nNeurons_previous; jNeuron++){
+        std::size_t nNeurons_previous = total_layers[iLayer - 1]->getNNeurons();
+        for(std::size_t jNeuron=0; jNeuron<nNeurons_previous; jNeuron++){
             x += weights_mat[iLayer - 1][iNeuron][jNeuron] * total_layers[iLayer-1]->getOutput(jNeuron);
         }
         return x;
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
index fed140d4457..3e1cefd1d6f 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
@@ -32,9 +32,8 @@
 #include <cstdlib>
 
 #include "../../CConfig.hpp"
-#include "../../linear_algebra/blas_structure.hpp"
+//#include "../../linear_algebra/blas_structure.hpp"
 
-using namespace std;
 namespace MLPToolbox{
 class CNeuron
 {
diff --git a/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
index d471e42d939..7921023762b 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
@@ -30,46 +30,45 @@
 #include <iostream>
 #include <limits>
 #include <cstdlib>
-
+#include <vector>
 #include "../../CConfig.hpp"
-#include "../../linear_algebra/blas_structure.hpp"
 
-using namespace std;
 namespace MLPToolbox{
+
 class CReadNeuralNetwork {
     private:
-    vector<string> input_names;
-    vector<string> output_names;
+    std::vector<std::string> input_names;
+    std::vector<std::string> output_names;
 
-    string filename;
+    std::string filename;
     unsigned long n_layers;
-    vector<unsigned long> n_neurons;
-    vector<vector<vector<double long>>> weights;
-    vector<vector<double long>> biases;
-    vector<string> activation_functions;
+    std::vector<unsigned long> n_neurons;
+    std::vector<std::vector<std::vector<su2double>>> weights;
+    std::vector<std::vector<su2double>> biases;
+    std::vector<std::string> activation_functions;
 
-    vector<pair<double long, double long>> input_norm;
-    vector<pair<double long, double long>> output_norm;
+    std::vector<std::pair<su2double, su2double>> input_norm;
+    std::vector<std::pair<su2double, su2double>> output_norm;
     public:
 
-    CReadNeuralNetwork(string filename_in);
+    CReadNeuralNetwork(std::string filename_in);
     void ReadMLPFile();
 
-    string SkipToFlag(ifstream *file_stream, string flag);
+    std::string SkipToFlag(std::ifstream *file_stream, std::string flag);
     
     unsigned long GetNInputs(){return n_neurons.at(0);}
     unsigned long GetNOutputs(){return n_neurons.at(n_layers - 1);}
 
     unsigned long GetNlayers(){return n_layers;}
-    unsigned long GetNneurons(size_t iLayer){return n_neurons.at(iLayer);}
-    double long GetWeight(size_t iLayer, size_t iNeuron, size_t jNeuron){return weights.at(iLayer).at(iNeuron).at(jNeuron);}
-    double long GetBias(size_t iLayer, size_t iNeuron){return biases.at(iLayer).at(iNeuron);}
-    pair<double long, double long> GetInputNorm(size_t iInput){return input_norm.at(iInput);}
-    pair<double long, double long> GetOutputNorm(size_t iOutput){return output_norm.at(iOutput);}
-    string GetActivationFunction(size_t iLayer){return activation_functions.at(iLayer);}
+    unsigned long GetNneurons(std::size_t iLayer){return n_neurons.at(iLayer);}
+    su2double GetWeight(std::size_t iLayer, std::size_t iNeuron, std::size_t jNeuron){return weights.at(iLayer).at(iNeuron).at(jNeuron);}
+    su2double GetBias(std::size_t iLayer, std::size_t iNeuron){return biases.at(iLayer).at(iNeuron);}
+    std::pair<su2double, su2double> GetInputNorm(std::size_t iInput){return input_norm.at(iInput);}
+    std::pair<su2double, su2double> GetOutputNorm(std::size_t iOutput){return output_norm.at(iOutput);}
+    std::string GetActivationFunction(std::size_t iLayer){return activation_functions.at(iLayer);}
 
-    string GetInputName(size_t iInput){return input_names.at(iInput);}
-    string GetOutputName(size_t iOutput){return output_names.at(iOutput);}
+    std::string GetInputName(std::size_t iInput){return input_names.at(iInput);}
+    std::string GetOutputName(std::size_t iOutput){return output_names.at(iOutput);}
     
     ~CReadNeuralNetwork(){};
 };
diff --git a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
index d6bba0ce8b2..789988af101 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
@@ -32,25 +32,48 @@
 #include <cmath>
 #include <fstream>
 
-MLPToolbox::CIOMap::CIOMap(CLookUp_ANN*ANN_collection, vector<string> &inputs, vector<string> &outputs){
-    PairVariableswithANNs(ANN_collection, inputs, outputs);
+MLPToolbox::CIOMap::CIOMap(CLookUp_ANN*MLP_collection, vector<string> &inputs, vector<string> &outputs){
+    /* Generate an input-output map given a set of call inputs and call outputs. These inputs are 
+    mapped to the inputs of the loaded MLPs in the MLP_collection object. The call outputs are 
+    then matched to the MLPs with matching inputs.
+    */
+    PairVariableswithMLPs(MLP_collection, inputs, outputs);
+
+    // Perform checks on input-output validity
     if(outputs.size() > 0){
-        ANN_collection->Check_Use_of_Inputs(inputs, this);
-        ANN_collection->Check_Use_of_Outputs(outputs, this);
-        ANN_collection->Check_Duplicate_Outputs(outputs, this);
+        // Check wether all call inputs are used
+        MLP_collection->Check_Use_of_Inputs(inputs, this);
+
+        // Check wether all call outputs are present in the MLP collection
+        MLP_collection->Check_Use_of_Outputs(outputs, this);
+
+        // Check wether there are any duplicates in the MLP outputs
+        MLP_collection->Check_Duplicate_Outputs(outputs, this);
     }
 }
-void MLPToolbox::CIOMap::PairVariableswithANNs(CLookUp_ANN*ANN_collection, vector<string> &inputs, vector<string> &outputs){
-
+void MLPToolbox::CIOMap::PairVariableswithMLPs(CLookUp_ANN*MLP_collection, vector<string> &inputs, vector<string> &outputs){
+    /*
+    In this function, the call inputs and outputs are matched to those within the MLP collection. 
+    */
     bool isInput, isOutput;
-    for(size_t i_ANN=0; i_ANN<ANN_collection->GetNANNs(); i_ANN++){
-        vector<pair<size_t, size_t>> Input_Indices = ANN_collection->FindVariable_Indices(i_ANN, inputs, true);
+
+    // Looping over the loaded MLPs to check wether the MLP inputs match with the call inputs
+    for(size_t i_MLP=0; i_MLP<MLP_collection->GetNANNs(); i_MLP++){
+
+        // Mapped call inputs to MLP inputs
+        vector<pair<size_t, size_t>> Input_Indices = MLP_collection->FindVariable_Indices(i_MLP, inputs, true);
         isInput = Input_Indices.size() > 0;
+
         if(isInput){
-            vector<pair<size_t, size_t>> Output_Indices = ANN_collection->FindVariable_Indices(i_ANN, outputs, false);
+            // Only when the MLP inputs match with a portion of the call inputs are the output variable checks performed
+
+            vector<pair<size_t, size_t>> Output_Indices = MLP_collection->FindVariable_Indices(i_MLP, outputs, false);
             isOutput = Output_Indices.size() > 0;
+
             if(isOutput){
-                ANN_indices.push_back(i_ANN);
+
+                // Update input and output mapping if both inputs and outputs match
+                MLP_indices.push_back(i_MLP);
                 Input_Map.push_back(Input_Indices);
                 Output_Map.push_back(Output_Indices);
             }
diff --git a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
index f63e57038a7..4642a8a9bd4 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
@@ -73,12 +73,12 @@ vector<pair<size_t, size_t>> MLPToolbox::CLookUp_ANN::FindVariable_Indices(size_
 }
 
 void MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap *input_output_map, vector<su2double>& inputs, vector<su2double*>& outputs){
-    for(size_t i_map=0; i_map<input_output_map->GetNANNs(); i_map++){
-        size_t i_ANN = input_output_map->GetANNIndex(i_map);
-        vector<su2double> ANN_inputs = input_output_map->GetANN_Inputs(i_map, inputs);
+    for(size_t i_map=0; i_map<input_output_map->GetNMLPs(); i_map++){
+        size_t i_ANN = input_output_map->GetMLPIndex(i_map);
+        vector<su2double> ANN_inputs = input_output_map->GetMLP_Inputs(i_map, inputs);
         NeuralNetworks[i_ANN]->predict(ANN_inputs);
         for(size_t i=0; i < input_output_map->GetNMappedOutputs(i_map); i++){
-            *outputs[input_output_map->GetOutputIndex(i_map, i)] = NeuralNetworks[i_ANN]->GetANN_Output(input_output_map->GetANNOutputIndex(i_map, i));
+            *outputs[input_output_map->GetOutputIndex(i_map, i)] = NeuralNetworks[i_ANN]->GetANN_Output(input_output_map->GetMLPOutputIndex(i_map, i));
         }
     }
 }
@@ -111,7 +111,7 @@ void MLPToolbox::CLookUp_ANN::GenerateANN(CNeuralNetwork * ANN, string fileName)
     for(size_t i_layer = 0; i_layer < ANN->getNWeightLayers(); i_layer++){
         ANN->setActivationFunction(i_layer, Reader.GetActivationFunction(i_layer));
         for(size_t i_neuron=0; i_neuron < ANN->getNNeurons(i_layer); i_neuron++){
-            for(size_t j_neuron=0; j_neuron<ANN->getNNeurons(i_layer, i_neuron); j_neuron++){
+            for(size_t j_neuron=0; j_neuron<ANN->getNNeurons(i_layer+1); j_neuron++){
                 ANN->setWeight(i_layer, i_neuron, j_neuron, Reader.GetWeight(i_layer, i_neuron, j_neuron));
             }
         }
@@ -175,7 +175,7 @@ string MLPToolbox::CLookUp_ANN::SkipToFlag(ifstream *file_stream, string flag) {
   }
 
   if ((*file_stream).eof())
-    SU2_MPI::Error("Flag not found in file", CURRENT_FUNCTION);
+    SU2_MPI::Error("Flag " + flag + " not found in file", CURRENT_FUNCTION);
 
   return line;
 }
@@ -187,7 +187,7 @@ bool MLPToolbox::CLookUp_ANN::Check_Duplicate_Outputs(vector<string> &output_nam
     vector<string> duplicate_variables;
     for(size_t i_Output =0; i_Output < output_names.size(); i_Output++){
         n_occurances = 0;
-        for(size_t i_map=0; i_map<input_output_map->GetNANNs(); i_map++){
+        for(size_t i_map=0; i_map<input_output_map->GetNMLPs(); i_map++){
             vector<pair<size_t, size_t>> output_map = input_output_map->GetOutputMapping(i_map);
             for(size_t j_Output=0; j_Output<output_map.size(); j_Output++){
                 if(output_map[j_Output].first == i_Output) n_occurances++;
@@ -213,7 +213,7 @@ vector<string> missing_inputs;
 bool inputs_are_present{true};
 for(size_t iInput=0; iInput<input_names.size(); iInput ++){
     bool found_input = false;
-    for(size_t i_map=0; i_map < input_output_map->GetNANNs(); i_map++){
+    for(size_t i_map=0; i_map < input_output_map->GetNMLPs(); i_map++){
         vector<pair<size_t, size_t>> input_map = input_output_map->GetInputMapping(i_map);
         for(size_t jInput=0; jInput<input_map.size(); jInput++){
             if(input_map[jInput].first == iInput){
@@ -245,7 +245,7 @@ bool MLPToolbox::CLookUp_ANN::Check_Use_of_Outputs(vector<string> &output_names,
         bool found_output{false};
 
         /* Looping over all the selected ANNs */
-        for(size_t i_map=0; i_map < input_output_map->GetNANNs(); i_map++){
+        for(size_t i_map=0; i_map < input_output_map->GetNMLPs(); i_map++){
             vector<pair<size_t, size_t>> output_map = input_output_map->GetOutputMapping(i_map);
 
             /* Looping over the outputs of the output map of the current ANN */
diff --git a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
index 496ac851048..ebc712e15e5 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
@@ -42,6 +42,8 @@ void MLPToolbox::CNeuralNetwork::predict(vector<su2double> &inputs){
         inputLayer->setOutput(iNeuron, x_norm);
     }
     if(!same_point){
+        su2double alpha=1.67326324;
+        su2double lambda=1.05070098;
         for(iLayer=1; iLayer<n_hidden_layers + 2; iLayer++){
             nNeurons_current = total_layers[iLayer]->getNNeurons();
 
@@ -54,14 +56,22 @@ void MLPToolbox::CNeuralNetwork::predict(vector<su2double> &inputs){
                 case ENUM_ACTIVATION_FUNCTION::SMOOTH_SLOPE:
                     for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
                         x = total_layers[iLayer]->getInput(iNeuron);
-                        y = x > 0 ? x : tanh(x);
+                        if(x > 0){
+                            y = x;
+                        }else{
+                            y = tanh(x);
+                        }
                         total_layers[iLayer]->setOutput(iNeuron, y);
                     }
                     break;
                 case ENUM_ACTIVATION_FUNCTION::ELU:
                     for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
                         x = total_layers[iLayer]->getInput(iNeuron);
-                        y = x > 0 ? x : (exp(x) - 1);
+                        if(x > 0){
+                            y = x;
+                        }else{
+                            y = exp(x) - 1;
+                        }
                         total_layers[iLayer]->setOutput(iNeuron, y);
                     }
                     break;
@@ -75,7 +85,52 @@ void MLPToolbox::CNeuralNetwork::predict(vector<su2double> &inputs){
                 case ENUM_ACTIVATION_FUNCTION::RELU:
                     for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
                         x = total_layers[iLayer]->getInput(iNeuron);
-                        y = x > 0.0 ? x : 0.0;
+                        if(x > 0){
+                            y = x;
+                        }else{
+                            y = 0.0;
+                        }
+                        total_layers[iLayer]->setOutput(iNeuron, y);
+                    }
+                    break;
+                case ENUM_ACTIVATION_FUNCTION::SWISH:
+                    for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
+                        x = total_layers[iLayer]->getInput(iNeuron);
+                        y = x / (1 + exp(-x));
+                        total_layers[iLayer]->setOutput(iNeuron, y);
+                    }
+                    break;
+                case ENUM_ACTIVATION_FUNCTION::TANH:
+                    for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
+                        x = total_layers[iLayer]->getInput(iNeuron);
+                        y = tanh(x);
+                        total_layers[iLayer]->setOutput(iNeuron, y);
+                    }
+                    break;
+                case ENUM_ACTIVATION_FUNCTION::SIGMOID:
+                    for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
+                        x = total_layers[iLayer]->getInput(iNeuron);
+                        y = 1.0/(1 + exp(-x));
+                        total_layers[iLayer]->setOutput(iNeuron, y);
+                    }
+                    break;
+                case ENUM_ACTIVATION_FUNCTION::SELU:
+                    for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
+                        x = total_layers[iLayer]->getInput(iNeuron);
+                        if(x > 0.0){
+                            y = lambda * x;
+                        }else{
+                            y = lambda * alpha * (exp(x) - 1);
+                        }
+                        total_layers[iLayer]->setOutput(iNeuron, y);
+                    }
+                    break;
+                case ENUM_ACTIVATION_FUNCTION::GELU:
+                    
+                    for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
+                        x = total_layers[iLayer]->getInput(iNeuron);
+
+                        y = 0.5 * x * (1 + tanh(sqrt(2 / PI_NUMBER) * (x + 0.044715 * pow(x, 3))));
                         total_layers[iLayer]->setOutput(iNeuron, y);
                     }
                     break;
@@ -108,45 +163,24 @@ MLPToolbox::CNeuralNetwork::CNeuralNetwork(){
 
 
 void MLPToolbox::CNeuralNetwork::defineInputLayer(unsigned long n_neurons){
-    //cout << "Creating an input layer with " << n_neurons << " neurons. "<< endl;
     inputLayer = new CLayer(n_neurons);
     inputLayer->setInput(true);
     input_norm.resize(n_neurons);
 }
 
 void MLPToolbox::CNeuralNetwork::defineOutputLayer(unsigned long n_neurons){
-    //cout << "Creating an output layer with " << n_neurons << " neurons. "<< endl;
     outputLayer = new CLayer(n_neurons);
     output_norm.resize(n_neurons);
 }
 
 void MLPToolbox::CNeuralNetwork::push_hidden_layer(unsigned long n_neurons){
     CLayer *newLayer = new CLayer(n_neurons);
-    //cout << "Creating a hidden layer with " << n_neurons << " neurons. "<< endl;
     hiddenLayers.push_back(newLayer);
     n_hidden_layers ++;
 }
 
 void MLPToolbox::CNeuralNetwork::sizeWeights(){
-    unsigned long i_layer{0};
-    weights.resize(n_hidden_layers + 1);
-    weights.at(i_layer).resize(inputLayer->getNNeurons());
-    CLayer * previouslayer = inputLayer;
-
-    if(n_hidden_layers != 0){
-        for(size_t i_hidden_layer=0; i_hidden_layer < n_hidden_layers; i_hidden_layer++){
-            for(size_t i_neuron=0; i_neuron < previouslayer->getNNeurons(); i_neuron++){
-                weights.at(i_layer).at(i_neuron).resize(hiddenLayers.at(i_hidden_layer)->getNNeurons());
-            }
-            previouslayer = hiddenLayers.at(i_hidden_layer);
-            i_layer ++;
-            weights.at(i_layer).resize(previouslayer->getNNeurons());
-        }
-    }
-    for(size_t i_neuron=0; i_neuron < previouslayer->getNNeurons(); i_neuron++){
-        weights.at(i_layer).at(i_neuron).resize(outputLayer->getNNeurons());
-    }
-
+    
     total_layers.resize(n_hidden_layers + 2);
     total_layers.at(0) = inputLayer;
     for(size_t iLayer=0; iLayer<n_hidden_layers; iLayer++){
@@ -165,55 +199,57 @@ void MLPToolbox::CNeuralNetwork::sizeWeights(){
 }   
 
 void MLPToolbox::CNeuralNetwork::setWeight(unsigned long i_layer, unsigned long i_neuron, unsigned long j_neuron, su2double value){
-    //weights.at(i_layer).at(i_neuron).at(j_neuron) = value;
     weights_mat[i_layer][j_neuron][i_neuron] = value;
 }
 void MLPToolbox::CNeuralNetwork::displayNetwork(){
-    cout << "Input layer: " << inputLayer->getNNeurons() << " neurons, Activation Function: " <<  inputLayer->getActivationType() << endl;
-    for(size_t i=0; i<total_layers[1]->getNNeurons(); i++){
-        for(size_t j=0; j<inputLayer->getNNeurons(); j++){
-            cout << weights_mat[0][i][j] << " ";
-        }
-    }
-    for(size_t i_layer=0; i_layer < hiddenLayers.size(); i_layer++){
-        cout << "Hidden layer " << i_layer + 1 << ": " << hiddenLayers.at(i_layer)->getNNeurons() << " neurons, Activation Function: " <<  hiddenLayers.at(i_layer) ->getActivationType() << endl;
-        for(size_t i=0; i<weights.at(i_layer+1).size(); i++){
-            for(size_t j=0; j<weights.at(i_layer+1).at(i).size(); j++){
-                cout << weights_mat[i_layer][i][j] << " ";
-            }
-            cout << endl;
-    }
-    }
-    cout << "Output layer: "<<outputLayer->getNNeurons() <<" neurons, Activation Function: " << outputLayer->getActivationType() << endl;
+    /*!
+    TODO:
+    find way of displaying network architectures
+    */
 }
 
 void MLPToolbox::CNeuralNetwork::setActivationFunction(unsigned long i_layer, string input)
 {
     if(input.compare("linear") == 0){
-        //activation_functions[i_layer] = new Linear();
         activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::LINEAR;
         return;
     }
     if(input.compare("relu") == 0){
-        //activation_functions[i_layer] = new Relu();
         activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::RELU;
         return;
     }
     if((input.compare("smooth_slope") == 0)){
-        //activation_functions[i_layer] = new SmoothSlope();
         activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::SMOOTH_SLOPE;
         return;
     }
     if((input.compare("elu") == 0)){
-        //activation_functions[i_layer] = new SmoothSlope();
         activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::ELU;
         return;
     }
+    if(input.compare("swish") == 0){
+        activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::SWISH;
+        return;
+    }
+    if(input.compare("sigmoid") == 0){
+        activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::SIGMOID;
+        return;
+    }
+    if(input.compare("tanh") == 0){
+        activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::TANH;
+        return;
+    }
+    if(input.compare("selu") == 0){
+        activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::SELU;
+        return;
+    }
+    if(input.compare("gelu") == 0){
+        activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::GELU;
+        return;
+    }
     if(input.compare("none") == 0){
-        //activation_functions[i_layer] = new None();
         activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::NONE;
         return;
     }
-    //total_layers.at(i_layer)->setActivationFunction(input);
+    SU2_MPI::Error("Unknown activation function type: " + input, CURRENT_FUNCTION);
     return;
 }
diff --git a/SU2_CFD/src/fluid/CPengRobinson.cpp b/SU2_CFD/src/fluid/CPengRobinson.cpp
index 66abe62f4f4..962e8a60ea1 100644
--- a/SU2_CFD/src/fluid/CPengRobinson.cpp
+++ b/SU2_CFD/src/fluid/CPengRobinson.cpp
@@ -26,6 +26,7 @@
  */
 
 #include "../../include/fluid/CPengRobinson.hpp"
+#include "../../../Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp"
 
 CPengRobinson::CPengRobinson(su2double gamma, su2double R, su2double Pstar, su2double Tstar, su2double w)
     : CIdealGas(gamma, R) {
@@ -38,6 +39,56 @@ CPengRobinson::CPengRobinson(su2double gamma, su2double R, su2double Pstar, su2d
     k = 0.37464 + 1.54226 * w - 0.26992 * w * w;
   else
     k = 0.379642 + 1.48503 * w - 0.164423 * w * w + 0.016666 * w * w * w;
+
+  vector<string> call_input_variables;
+  vector<string> call_output_variables;
+  vector<su2double> call_inputs;
+  vector<su2double*> call_outputs;
+  call_input_variables.push_back("Progress_Variable");
+  call_inputs.push_back(-5.74934292655689e-01);
+  call_input_variables.push_back("Enthalpy");
+  call_inputs.push_back(+2.22692201641688e+03);
+  call_input_variables.push_back("Mixture_Fraction");
+  call_inputs.push_back(0.0144045);
+
+  call_output_variables.push_back("Temperature");
+  call_outputs.push_back(&Temperature);
+  call_output_variables.push_back("Density");
+  call_outputs.push_back(&Density);
+
+  vector<string> call_inputvars_lean;
+  call_inputvars_lean.push_back("Progress_Variable_lean");
+  call_inputvars_lean.push_back("Enthalpy_lean");
+  call_inputvars_lean.push_back("Mixture_Fraction_lean");
+
+  vector<string> call_inputvars_rich;
+  call_inputvars_rich.push_back("Progress_Variable_rich");
+  call_inputvars_rich.push_back("Enthalpy_rich");
+  call_inputvars_rich.push_back("Mixture_Fraction_rich");
+
+  MLPToolbox::CLookUp_ANN * test_mlp = new MLPToolbox::CLookUp_ANN("MLP_collection.mlp");
+  MLPToolbox::CIOMap * test_map = new MLPToolbox::CIOMap(test_mlp, call_input_variables, call_output_variables);
+  MLPToolbox::CIOMap * lean_map = new MLPToolbox::CIOMap(test_mlp, call_inputvars_lean, call_output_variables);
+  MLPToolbox::CIOMap * rich_map = new MLPToolbox::CIOMap(test_mlp, call_inputvars_rich, call_output_variables);
+
+
+  test_mlp->Predict_ANN(test_map, call_inputs, call_outputs);
+  cout << "in flame zone: " << Density << " " << Temperature << endl;
+  call_inputs[0] = -7.36;
+  call_inputs[1] = 26468.5;
+  call_inputs[2] = 1.0;
+  test_mlp->Predict_ANN(rich_map, call_inputs, call_outputs);
+  cout << "rich: " << Density << " " << Temperature << endl;
+  call_inputs[0] = -0.4753;
+  call_inputs[1] = 3144.6;
+  call_inputs[2] = 0.0;
+  test_mlp->Predict_ANN(lean_map, call_inputs, call_outputs);
+  cout << "lean: " << Density << " " << Temperature << endl;
+
+  delete test_mlp;
+  delete test_map;
+  delete rich_map;
+  delete lean_map;
 }
 
 su2double CPengRobinson::alpha2(su2double T) const {

From 04813b107392ff542fc4fb7577e30bd2a54bf7e5 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Wed, 19 Oct 2022 14:43:54 +0200
Subject: [PATCH 036/656] Added a MLP fluid model template class

---
 Common/include/CConfig.hpp                    |  7 ++
 Common/include/option_structure.hpp           |  2 +
 Common/src/CConfig.cpp                        |  3 +
 .../multilayer_perceptron/CIOMap.cpp          |  2 +-
 .../CReadNeuralNetwork.cpp                    |  3 +-
 .../{CMLPGas_Template.hpp => CMLPGas.hpp}     | 13 +--
 SU2_CFD/obj/Makefile.am                       |  2 +-
 .../{CMLPGas_Template.cpp => CMLPGas.cpp}     | 95 ++++++++++++-------
 SU2_CFD/src/meson.build                       |  2 +-
 SU2_CFD/src/solvers/CEulerSolver.cpp          | 12 +++
 SU2_CFD/src/solvers/CIncEulerSolver.cpp       | 13 +++
 11 files changed, 111 insertions(+), 43 deletions(-)
 rename SU2_CFD/include/fluid/{CMLPGas_Template.hpp => CMLPGas.hpp} (91%)
 rename SU2_CFD/src/fluid/{CMLPGas_Template.cpp => CMLPGas.cpp} (54%)

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index 9e47dc85e56..db4410287a8 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -223,6 +223,7 @@ class CConfig {
   string Inlet_Filename;        /*!< \brief Filename specifying an inlet profile. */
   su2double Inlet_Matching_Tol; /*!< \brief Tolerance used when matching a point to a point from the inlet file. */
   string ActDisk_FileName;      /*!< \brief Filename specifying an actuator disk. */
+  string MLP_filename;          /*!< \brief Filename specifying an MLP-driven fluid model. */
 
   string *Marker_Euler,           /*!< \brief Euler wall markers. */
   *Marker_FarField,               /*!< \brief Far field markers. */
@@ -4842,6 +4843,12 @@ class CConfig {
    */
   string GetActDisk_FileName(void) const { return ActDisk_FileName; }
 
+  /*!
+   * \brief Get name of the input file for the fluid model multi-layer perceptron collection.
+   * \return Name of the input file for the specified MLP collection file.
+   */
+  string GetMLP_FileName(void) const { return MLP_filename; }
+
   /*!
    * \brief Get the tolerance used for matching two points on a specified inlet
    * \return Tolerance used for matching a point to a specified inlet
diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index 0b97712612a..45d475fbbe4 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -569,6 +569,7 @@ enum ENUM_FLUIDMODEL {
   MUTATIONPP = 7,         /*!< \brief Mutation++ gas model for nonequilibrium flow. */
   SU2_NONEQ = 8,          /*!< \brief User defined gas model for nonequilibrium flow. */
   FLUID_MIXTURE = 9,      /*!< \brief Species mixture model. */
+  MLP_GAS = 10,           /*!< \brief multi-layer perceptron driven fluid model. */
 };
 static const MapType<std::string, ENUM_FLUIDMODEL> FluidModel_Map = {
   MakePair("STANDARD_AIR", STANDARD_AIR)
@@ -581,6 +582,7 @@ static const MapType<std::string, ENUM_FLUIDMODEL> FluidModel_Map = {
   MakePair("MUTATIONPP", MUTATIONPP)
   MakePair("SU2_NONEQ", SU2_NONEQ)
   MakePair("FLUID_MIXTURE", FLUID_MIXTURE)
+  MakePair("MLP_GAS", MLP_GAS)
 };
 
 /*!
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index cc9ea692c76..e6375f1a78d 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -1482,6 +1482,9 @@ void CConfig::SetConfig_Options() {
   /*!\brief ACTDISK_FILENAME \n DESCRIPTION: Input file for a specified actuator disk (w/ extension) \n DEFAULT: actdiskinput.dat \ingroup Config*/
   addStringOption("ACTDISK_FILENAME", ActDisk_FileName, string("actdiskinput.dat"));
 
+  /*!\brief MLP_FILENAME \n DESCRIPTION: Input file for a multi-layer perceptron input file for fluid model definition. w/ extension) \n DEFAULT: MLP_collection.mlp \ingroup Config*/
+  addStringOption("MLP_FILENAME", MLP_filename, string("MLP_collection.mlp"));
+
   /*!\brief INLET_TYPE  \n DESCRIPTION: Inlet boundary type \n OPTIONS: see \link Inlet_Map \endlink \n DEFAULT: TOTAL_CONDITIONS \ingroup Config*/
   addEnumOption("INLET_TYPE", Kind_Inlet, Inlet_Map, INLET_TYPE::TOTAL_CONDITIONS);
   /*!\brief INC_INLET_TYPE \n DESCRIPTION: List of inlet types for incompressible flows. List length must match number of inlet markers. Options: VELOCITY_INLET, PRESSURE_INLET, INPUT_FILE. \ingroup Config*/
diff --git a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
index 789988af101..36d08a081db 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
@@ -48,7 +48,7 @@ MLPToolbox::CIOMap::CIOMap(CLookUp_ANN*MLP_collection, vector<string> &inputs, v
         MLP_collection->Check_Use_of_Outputs(outputs, this);
 
         // Check wether there are any duplicates in the MLP outputs
-        MLP_collection->Check_Duplicate_Outputs(outputs, this);
+        //MLP_collection->Check_Duplicate_Outputs(outputs, this);
     }
 }
 void MLPToolbox::CIOMap::PairVariableswithMLPs(CLookUp_ANN*MLP_collection, vector<string> &inputs, vector<string> &outputs){
diff --git a/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
index 8c34674e260..73e49fda1e1 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
@@ -30,7 +30,7 @@ using namespace std;
 
 MLPToolbox::CReadNeuralNetwork::CReadNeuralNetwork(string filename_in){
     filename = filename_in;
-};
+}
 
 void MLPToolbox::CReadNeuralNetwork::ReadMLPFile(){
     ifstream file_stream;
@@ -109,7 +109,6 @@ void MLPToolbox::CReadNeuralNetwork::ReadMLPFile(){
       /* Read MLP input variable names */
       if(line.compare("[input names]") == 0){
         found_input_names = true;
-        unsigned short j{1};
         getline(file_stream, line);
         while(line.compare("") != 0){
           input_names.push_back(line);
diff --git a/SU2_CFD/include/fluid/CMLPGas_Template.hpp b/SU2_CFD/include/fluid/CMLPGas.hpp
similarity index 91%
rename from SU2_CFD/include/fluid/CMLPGas_Template.hpp
rename to SU2_CFD/include/fluid/CMLPGas.hpp
index db3207c3313..0da131105b4 100644
--- a/SU2_CFD/include/fluid/CMLPGas_Template.hpp
+++ b/SU2_CFD/include/fluid/CMLPGas.hpp
@@ -1,5 +1,5 @@
 /*!
- * \file CMLPGas_Template.hpp
+ * \file CMLPGas.hpp
  * \brief Defines a template fluid model class using multilayer perceptrons
  *  for theromodynamic state definition
  * \author E.Bunschoten
@@ -31,17 +31,18 @@
 #include "CFluidModel.hpp"
 #include "../../../Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp"
 /*!
- * \class CMLPGas_Template
+ * \class CMLPGas
  * \brief Template class for fluid model definition using multi-layer perceptrons for 
  * fluid dynamic state definition.
  * \author: E.Bunschoten.
  */
-class CMLPGas_Template : public CFluidModel {
+class CMLPGas : public CFluidModel {
  protected:
   su2double Gamma{0.0};           /*!< \brief Ratio of Specific Heats. */
   su2double Gamma_Minus_One{0.0}; /*!< \brief Ratio of Specific Heats Minus One. */
   su2double Gas_Constant{0.0};    /*!< \brief Gas Constant. */
-  bool ComputeEntropy{true};      /*!< \brief Whether or not to compute entropy. */
+
+  su2double R_u = 8.31451;
 
   string ann_input_filename;
   MLPToolbox::CLookUp_ANN * lookup_ann;
@@ -69,9 +70,9 @@ class CMLPGas_Template : public CFluidModel {
   /*!
    * \brief Constructor of the class.
    */
-  CMLPGas_Template(su2double gamma, su2double R, bool CompEntropy = true);
+  CMLPGas(const CConfig* config);
 
-  ~CMLPGas_Template();
+  ~CMLPGas();
   /*!
    * \brief Set the Dimensionless State using Density and Internal Energy
    * \param[in] rho - first thermodynamic variable.
diff --git a/SU2_CFD/obj/Makefile.am b/SU2_CFD/obj/Makefile.am
index 5ba91fd0d4e..361d69d5af9 100644
--- a/SU2_CFD/obj/Makefile.am
+++ b/SU2_CFD/obj/Makefile.am
@@ -57,7 +57,7 @@ libSU2Core_sources = ../src/definition_structure.cpp \
   ../src/fluid/CNEMOGas.cpp \
   ../src/fluid/CSU2TCLib.cpp \
   ../src/fluid/CMutationTCLib.cpp \
-  ../src/fluid/CMLPGas_Template.cpp \
+  ../src/fluid/CMLPGas.cpp \
   ../src/integration/CIntegration.cpp \
   ../src/integration/CSingleGridIntegration.cpp \
   ../src/integration/CMultiGridIntegration.cpp \
diff --git a/SU2_CFD/src/fluid/CMLPGas_Template.cpp b/SU2_CFD/src/fluid/CMLPGas.cpp
similarity index 54%
rename from SU2_CFD/src/fluid/CMLPGas_Template.cpp
rename to SU2_CFD/src/fluid/CMLPGas.cpp
index 44e00c5ec8d..219dc2351e3 100644
--- a/SU2_CFD/src/fluid/CMLPGas_Template.cpp
+++ b/SU2_CFD/src/fluid/CMLPGas.cpp
@@ -1,5 +1,5 @@
 /*!
- * \file CMLPGas_Template.cpp
+ * \file CMLPGas.cpp
  * \brief Source of the data-driven fluid model class using 
  *  multilayer perceptrons for data regression
  * \author E.Bunschoten
@@ -26,35 +26,28 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-#include "../../include/fluid/CMLPGas_Template.hpp"
+#include "../../include/fluid/CMLPGas.hpp"
 
-CMLPGas_Template::CMLPGas_Template(su2double gamma, su2double R, bool CompEntropy) : CFluidModel() {
-  Gamma = gamma;
-  Gamma_Minus_One = Gamma - 1.0;
-  Gas_Constant = R;
-  Cp = Gamma / Gamma_Minus_One * Gas_Constant;
-  Cv = Cp - R;
-
-  ComputeEntropy = CompEntropy;
+CMLPGas::CMLPGas(const CConfig* config) : CFluidModel() {
 
   /* Define a CLookUp_ANN object to allow for data regression */
-  ann_input_filename = "MLP_collection.mlp";
+  ann_input_filename = config->GetMLP_FileName();
   lookup_ann = new MLPToolbox::CLookUp_ANN(ann_input_filename);
 
   /* Map MLP inputs to outputs for each look-up operation*/
   MapInputs_to_Outputs();
 }
 
-CMLPGas_Template::~CMLPGas_Template(){
+CMLPGas::~CMLPGas(){
   delete iomap_rhoe;
   delete iomap_PT;
   delete iomap_Prho;
   delete lookup_ann;
 }
-void CMLPGas_Template::MapInputs_to_Outputs(){
+void CMLPGas::MapInputs_to_Outputs(){
 
-  input_names_rhoe.push_back("rho");
-  input_names_rhoe.push_back("e");
+  input_names_rhoe.push_back("Density");
+  input_names_rhoe.push_back("Energy");
 
   output_names_rhoe.push_back("Temperature");
   outputs_rhoe.push_back(&Temperature);
@@ -75,41 +68,79 @@ void CMLPGas_Template::MapInputs_to_Outputs(){
 
   iomap_rhoe = new MLPToolbox::CIOMap(lookup_ann, input_names_rhoe, output_names_rhoe);
 
-  input_names_PT.push_back("P");
-  input_names_PT.push_back("T");
+  input_names_PT.push_back("Pressure");
+  input_names_PT.push_back("Temperature");
 
-  output_names_PT.push_back("rho");
+  output_names_PT.push_back("Density");
   outputs_PT.push_back(&Density);
-  output_names_PT.push_back("e");
+  output_names_PT.push_back("Energy");
   outputs_PT.push_back(&StaticEnergy);
 
   iomap_PT = new MLPToolbox::CIOMap(lookup_ann, input_names_PT, output_names_PT);
 
-  input_names_Prho.push_back("P");
-  input_names_Prho.push_back("rho");
+  input_names_Prho.push_back("Pressure");
+  input_names_Prho.push_back("Density");
 
-  output_names_Prho.push_back("e");
+  output_names_Prho.push_back("Energy");
   outputs_Prho.push_back(&StaticEnergy);
   iomap_Prho = new MLPToolbox::CIOMap(lookup_ann, input_names_Prho, output_names_Prho);
 }
 
-void CMLPGas_Template::SetTDState_rhoe(su2double rho, su2double e) {
+void CMLPGas::SetTDState_rhoe(su2double rho, su2double e) {
+  Density = rho;
+  StaticEnergy = e;
   vector<su2double> ann_inputs;
   ann_inputs.push_back(rho);
   ann_inputs.push_back(e);
   lookup_ann->Predict_ANN(iomap_rhoe, ann_inputs, outputs_rhoe);
-}
+  Cp = (Pressure / (R_u * Density * Temperature)) * 1 / (dTde_rho);
+  Cv = (1/dTde_rho);
+  Gamma = Cp / Cv;
+  Gamma_Minus_One = Gamma - 1;
+  Gas_Constant = Cp * Gamma_Minus_One;
 
-void CMLPGas_Template::SetTDState_PT(su2double P, su2double T) {
-  vector<su2double> ann_inputs;
-  ann_inputs.push_back(P);
-  ann_inputs.push_back(T);
-  lookup_ann->Predict_ANN(iomap_PT, ann_inputs, outputs_PT);
+}
 
-  SetTDState_rhoe(Density, StaticEnergy);
+void CMLPGas::SetTDState_PT(su2double P, su2double T) {
+  // vector<su2double> ann_inputs;
+  // ann_inputs.push_back(P);
+  // ann_inputs.push_back(T);
+  // lookup_ann->Predict_ANN(iomap_PT, ann_inputs, outputs_PT);
+
+  su2double rho = 0.5*(6.9682399336300005e-01 + 2.4896548789900002e+00);
+  su2double e = 0.5*(3.2562734877400001e+05	+4.8566089128400001e+05);
+  rho = 1.0;
+  e = 3.2562734877400001e+05;
+  su2double delta_P, delta_T, delta_rho, delta_e, tolerance_P = 10, tolerance_T = 1.0;
+  su2double determinant, relaxation = 0.1;
+  unsigned long iter = 0, iter_max = 1000;
+  bool converged= false;
+  cout << "Target PT: " << P << " " << T << endl;
+  while(!converged && (iter < iter_max)){
+    SetTDState_rhoe(rho, e);
+    delta_P = (P - Pressure);
+    delta_T = (T - Temperature);
+    cout << delta_P << " " << delta_T << endl;
+    if((abs(delta_P)<tolerance_P) && (abs(delta_T) < tolerance_T)){
+      converged = true;
+      cout << "Converged PT: " << Pressure << " " << Temperature << endl;
+      return;
+    }else{
+      determinant = dPdrho_e * dTde_rho - dPde_rho * dTdrho_e;
+      delta_rho = (dTde_rho * delta_P - dPde_rho * delta_T) / determinant;
+      delta_T = (-dTdrho_e * delta_P + dPdrho_e * delta_T) / determinant;
+
+      rho -= relaxation * delta_rho;
+      e -= relaxation * delta_e;    
+    }
+    iter++;
+  }
+
+  SetTDState_rhoe(rho, e);
+  cout << "Final(nonconverged) PT: " << Pressure << " " << Temperature << endl;
 }
 
-void CMLPGas_Template::SetTDState_Prho(su2double P, su2double rho) {
+void CMLPGas::SetTDState_Prho(su2double P, su2double rho) {
   vector<su2double> ann_inputs;
   ann_inputs.push_back(P);
   ann_inputs.push_back(rho);
@@ -117,7 +148,7 @@ void CMLPGas_Template::SetTDState_Prho(su2double P, su2double rho) {
   SetTDState_rhoe(rho, StaticEnergy);
 }
 
-void CMLPGas_Template::SetEnergy_Prho(su2double P, su2double rho) { 
+void CMLPGas::SetEnergy_Prho(su2double P, su2double rho) { 
   vector<su2double> ann_inputs;
   ann_inputs.push_back(P);
   ann_inputs.push_back(rho);
diff --git a/SU2_CFD/src/meson.build b/SU2_CFD/src/meson.build
index 9d81ec13f71..e477f80b2b6 100644
--- a/SU2_CFD/src/meson.build
+++ b/SU2_CFD/src/meson.build
@@ -11,7 +11,7 @@ su2_cfd_src += files(['fluid/CFluidModel.cpp',
                       'fluid/CNEMOGas.cpp',
                       'fluid/CMutationTCLib.cpp',
                       'fluid/CSU2TCLib.cpp',
-                      'fluid/CMLPGas_Template.cpp'])
+                      'fluid/CMLPGas.cpp'])
 
 su2_cfd_src += files(['output/COutputFactory.cpp',
                       'output/CAdjElasticityOutput.cpp',
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index 43dcd3de27c..35338ebbfda 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -32,6 +32,7 @@
 #include "../../include/fluid/CIdealGas.hpp"
 #include "../../include/fluid/CVanDerWaalsGas.hpp"
 #include "../../include/fluid/CPengRobinson.hpp"
+#include "../../include/fluid/CMLPGas.hpp"
 #include "../../include/numerics_simd/CNumericsSIMD.hpp"
 #include "../../include/limiters/CLimiterDetails.hpp"
 
@@ -857,6 +858,12 @@ void CEulerSolver::SetNondimensionalization(CConfig *config, unsigned short iMes
       auxFluidModel = new CPengRobinson(Gamma, config->GetGas_Constant(), config->GetPressure_Critical(),
                                         config->GetTemperature_Critical(), config->GetAcentric_Factor());
       break;
+    
+    case MLP_GAS:
+
+      auxFluidModel = new CMLPGas(config);
+
+      break;
 
     default:
       SU2_MPI::Error("Unknown fluid model.", CURRENT_FUNCTION);
@@ -1070,6 +1077,11 @@ void CEulerSolver::SetNondimensionalization(CConfig *config, unsigned short iMes
                                                config->GetTemperature_Critical() / config->GetTemperature_Ref(),
                                                config->GetAcentric_Factor());
         break;
+
+      case MLP_GAS:
+        FluidModel[thread] = new CMLPGas(config);
+
+        break;
     }
 
     GetFluidModel()->SetEnergy_Prho(Pressure_FreeStreamND, Density_FreeStreamND);
diff --git a/SU2_CFD/src/solvers/CIncEulerSolver.cpp b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
index 371055f31bb..796144f085f 100644
--- a/SU2_CFD/src/solvers/CIncEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
@@ -30,6 +30,7 @@
 #include "../../include/fluid/CConstantDensity.hpp"
 #include "../../include/fluid/CIncIdealGas.hpp"
 #include "../../include/fluid/CIncIdealGasPolynomial.hpp"
+#include "../../include/fluid/CMLPGas.hpp"
 #include "../../include/variables/CIncNSVariable.hpp"
 #include "../../include/limiters/CLimiterDetails.hpp"
 #include "../../../Common/include/toolboxes/geometry_toolbox.hpp"
@@ -330,6 +331,13 @@ void CIncEulerSolver::SetNondimensionalization(CConfig *config, unsigned short i
       config->SetPressure_Thermodynamic(Pressure_Thermodynamic);
       break;
 
+    case MLP_GAS:
+      auxFluidModel = new CMLPGas(config);
+      auxFluidModel->SetTDState_T(Temperature_FreeStream);
+      Pressure_Thermodynamic = auxFluidModel->GetPressure();
+      config->SetPressure_Thermodynamic(Pressure_Thermodynamic);
+      break;
+
     default:
 
       SU2_MPI::Error("Fluid model not implemented for incompressible solver.", CURRENT_FUNCTION);
@@ -492,6 +500,11 @@ void CIncEulerSolver::SetNondimensionalization(CConfig *config, unsigned short i
         fluidModel->SetTDState_T(Temperature_FreeStreamND);
         break;
 
+      case MLP_GAS:
+        fluidModel = new CMLPGas(config);
+        fluidModel->SetTDState_T(Temperature_FreeStreamND);
+        break;
+
     }
 
     if (viscous) {

From 167e5d29bdaba5e0a60c9b656b265a2ca010957f Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 9 Nov 2022 17:01:40 +0100
Subject: [PATCH 037/656] CoDiPack update.

---
 externals/codi | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/externals/codi b/externals/codi
index 96ac78ec5bc..82e80e953d3 160000
--- a/externals/codi
+++ b/externals/codi
@@ -1 +1 @@
-Subproject commit 96ac78ec5bcc5ac25b785e79b16ed76fca22d736
+Subproject commit 82e80e953d3aa1486d9879909308af51ed8159dc

From 6a95f5a4e7967b0ef2518edaa75fcee6a4cd9384 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 9 Nov 2022 17:03:14 +0100
Subject: [PATCH 038/656] OpDiLib update.

---
 externals/opdi | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/externals/opdi b/externals/opdi
index 1aabf5bd1ed..13350bc3b57 160000
--- a/externals/opdi
+++ b/externals/opdi
@@ -1 +1 @@
-Subproject commit 1aabf5bd1ed77611742eb655002f2ac7a3dddef9
+Subproject commit 13350bc3b57d27e1845af0e8998eafee22b29593

From c1940410d8a1c08aa40967cf9ffea0a32bde7229 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 9 Nov 2022 17:06:03 +0100
Subject: [PATCH 039/656] Adapt AD names and syntax to CoDiPack 2.

---
 Common/include/basic_types/ad_structure.hpp   | 91 ++++++++++---------
 Common/include/code_config.hpp                |  2 +-
 Common/include/linear_algebra/CSysSolve_b.hpp |  2 +-
 .../include/parallelization/mpi_structure.hpp |  4 +-
 .../include/parallelization/omp_structure.cpp |  2 -
 Common/src/basic_types/ad_structure.cpp       |  2 +-
 Common/src/linear_algebra/CSysSolve.cpp       | 16 ++--
 Common/src/linear_algebra/CSysSolve_b.cpp     |  2 +-
 SU2_CFD/src/SU2_CFD.cpp                       |  5 -
 .../src/drivers/CDiscAdjMultizoneDriver.cpp   |  2 +-
 .../src/drivers/CDiscAdjSinglezoneDriver.cpp  |  2 +-
 SU2_DOT/src/SU2_DOT.cpp                       | 10 --
 12 files changed, 63 insertions(+), 77 deletions(-)

diff --git a/Common/include/basic_types/ad_structure.hpp b/Common/include/basic_types/ad_structure.hpp
index 27e7946a622..0dfcbddf380 100644
--- a/Common/include/basic_types/ad_structure.hpp
+++ b/Common/include/basic_types/ad_structure.hpp
@@ -290,13 +290,13 @@ namespace AD{
   inline void EndNoSharedReading() {}
 
 #else
-  using CheckpointHandler = codi::DataStore;
+  using CheckpointHandler = codi::ExternalFunctionUserData;
 
-  using Tape = su2double::TapeType;
+  using Tape = su2double::Tape;
 
   using ExtFuncHelper = codi::ExternalFunctionHelper<su2double>;
 
-  extern ExtFuncHelper* FuncHelper;
+  extern ExtFuncHelper FuncHelper;
 
   extern bool PreaccActive;
 #ifdef HAVE_OPDI
@@ -306,11 +306,11 @@ namespace AD{
   extern bool PreaccEnabled;
 
 #ifdef HAVE_OPDI
-  using CoDiTapePosition = su2double::TapeType::Position;
+  using CoDiTapePosition = Tape::Position;
   using OpDiState = void*;
   using TapePosition = std::pair<CoDiTapePosition, OpDiState>;
 #else
-  using TapePosition = su2double::TapeType::Position;
+  using TapePosition = Tape::Position;
 #endif
 
   extern TapePosition StartPosition, EndPosition;
@@ -324,45 +324,45 @@ namespace AD{
 
   /*--- Reference to the tape. ---*/
 
-  FORCEINLINE su2double::TapeType& getGlobalTape() {return su2double::getGlobalTape();}
+  FORCEINLINE Tape& getTape() {return su2double::getTape();}
 
-  FORCEINLINE void RegisterInput(su2double &data) {AD::getGlobalTape().registerInput(data);}
+  FORCEINLINE void RegisterInput(su2double &data) {AD::getTape().registerInput(data);}
 
-  FORCEINLINE void RegisterOutput(su2double& data) {AD::getGlobalTape().registerOutput(data);}
+  FORCEINLINE void RegisterOutput(su2double& data) {AD::getTape().registerOutput(data);}
 
   FORCEINLINE void ResetInput(su2double &data) {data = data.getValue();}
 
-  FORCEINLINE void StartRecording() {AD::getGlobalTape().setActive();}
+  FORCEINLINE void StartRecording() {AD::getTape().setActive();}
 
-  FORCEINLINE void StopRecording() {AD::getGlobalTape().setPassive();}
+  FORCEINLINE void StopRecording() {AD::getTape().setPassive();}
 
-  FORCEINLINE bool TapeActive() { return AD::getGlobalTape().isActive(); }
+  FORCEINLINE bool TapeActive() { return AD::getTape().isActive(); }
 
-  FORCEINLINE void PrintStatistics() {AD::getGlobalTape().printStatistics();}
+  FORCEINLINE void PrintStatistics() {AD::getTape().printStatistics();}
 
-  FORCEINLINE void ClearAdjoints() {AD::getGlobalTape().clearAdjoints(); }
+  FORCEINLINE void ClearAdjoints() {AD::getTape().clearAdjoints(); }
 
   FORCEINLINE void ComputeAdjoint() {
   #if defined(HAVE_OPDI)
     opdi::logic->prepareEvaluate();
   #endif
-    AD::getGlobalTape().evaluate();
+    AD::getTape().evaluate();
   }
 
   FORCEINLINE void ComputeAdjoint(unsigned short enter, unsigned short leave) {
   #if defined(HAVE_OPDI)
     opdi::logic->recoverState(TapePositions[enter].second);
     opdi::logic->prepareEvaluate();
-    AD::getGlobalTape().evaluate(TapePositions[enter].first, TapePositions[leave].first);
+    AD::getTape().evaluate(TapePositions[enter].first, TapePositions[leave].first);
   #else
-    AD::getGlobalTape().evaluate(TapePositions[enter], TapePositions[leave]);
+    AD::getTape().evaluate(TapePositions[enter], TapePositions[leave]);
   #endif
   }
 
-  FORCEINLINE void ComputeAdjointForward() {AD::getGlobalTape().evaluateForward();}
+  FORCEINLINE void ComputeAdjointForward() {AD::getTape().evaluateForward();}
 
   FORCEINLINE void Reset() {
-    AD::getGlobalTape().reset();
+    AD::getTape().reset();
   #if defined(HAVE_OPDI)
     opdi::logic->reset();
   #endif
@@ -377,15 +377,19 @@ namespace AD{
   }
 
   FORCEINLINE void SetIndex(int &index, const su2double &data) {
-    index = data.getGradientData();
+    index = data.getIdentifier();
   }
 
   FORCEINLINE void SetDerivative(int index, const double val) {
-    AD::getGlobalTape().setGradient(index, val);
+    AD::getTape().setGradient(index, val);
   }
 
   FORCEINLINE double GetDerivative(int index) {
-    return AD::getGlobalTape().getGradient(index);
+    return AD::getTape().getGradient(index);
+  }
+
+  FORCEINLINE bool IsIdentifierActive(su2double const& value) {
+    return getTape().isIdentifierActive(value.getIdentifier());
   }
 
   /*--- Base case for parameter pack expansion. ---*/
@@ -394,7 +398,7 @@ namespace AD{
   template<class T, class... Ts, su2enable_if<std::is_same<T,su2double>::value> = 0>
   FORCEINLINE void SetPreaccIn(const T& data, Ts&&... moreData) {
     if (!PreaccActive) return;
-    if (data.isActive())
+    if (IsIdentifierActive(data))
       PreaccHelper.addInput(data);
     SetPreaccIn(moreData...);
   }
@@ -408,7 +412,7 @@ namespace AD{
   FORCEINLINE void SetPreaccIn(const T& data, const int size) {
     if (PreaccActive) {
       for (int i = 0; i < size; i++) {
-        if (data[i].isActive()) {
+        if (IsIdentifierActive(data[i])) {
           PreaccHelper.addInput(data[i]);
         }
       }
@@ -420,7 +424,7 @@ namespace AD{
     if (!PreaccActive) return;
     for (int i = 0; i < size_x; i++) {
       for (int j = 0; j < size_y; j++) {
-        if (data[i][j].isActive()) {
+        if (IsIdentifierActive(data[i][j])) {
           PreaccHelper.addInput(data[i][j]);
         }
       }
@@ -428,7 +432,7 @@ namespace AD{
   }
 
   FORCEINLINE void StartPreacc() {
-    if (AD::getGlobalTape().isActive() && PreaccEnabled) {
+    if (AD::getTape().isActive() && PreaccEnabled) {
       PreaccHelper.start();
       PreaccActive = true;
     }
@@ -440,7 +444,7 @@ namespace AD{
   template<class T, class... Ts, su2enable_if<std::is_same<T,su2double>::value> = 0>
   FORCEINLINE void SetPreaccOut(T& data, Ts&&... moreData) {
     if (!PreaccActive) return;
-    if (data.isActive())
+    if (IsIdentifierActive(data))
       PreaccHelper.addOutput(data);
     SetPreaccOut(moreData...);
   }
@@ -449,7 +453,7 @@ namespace AD{
   FORCEINLINE void SetPreaccOut(T&& data, const int size) {
     if (PreaccActive) {
       for (int i = 0; i < size; i++) {
-        if (data[i].isActive()) {
+        if (IsIdentifierActive(data[i])) {
           PreaccHelper.addOutput(data[i]);
         }
       }
@@ -461,7 +465,7 @@ namespace AD{
     if (!PreaccActive) return;
     for (int i = 0; i < size_x; i++) {
       for (int j = 0; j < size_y; j++) {
-        if (data[i][j].isActive()) {
+        if (IsIdentifierActive(data[i][j])) {
           PreaccHelper.addOutput(data[i][j]);
         }
       }
@@ -470,9 +474,9 @@ namespace AD{
 
   FORCEINLINE void Push_TapePosition() {
   #if defined(HAVE_OPDI)
-    TapePositions.push_back({AD::getGlobalTape().getPosition(), opdi::logic->exportState()});
+    TapePositions.push_back({AD::getTape().getPosition(), opdi::logic->exportState()});
   #else
-    TapePositions.push_back(AD::getGlobalTape().getPosition());
+    TapePositions.push_back(AD::getTape().getPosition());
   #endif
   }
 
@@ -484,23 +488,22 @@ namespace AD{
   }
 
   FORCEINLINE void StartExtFunc(bool storePrimalInput, bool storePrimalOutput){
-    FuncHelper = new ExtFuncHelper(true);
     if (!storePrimalInput){
-      FuncHelper->disableInputPrimalStore();
+      FuncHelper.disableInputPrimalStore();
     }
     if (!storePrimalOutput){
-      FuncHelper->disableOutputPrimalStore();
+      FuncHelper.disableOutputPrimalStore();
     }
   }
 
   FORCEINLINE void SetExtFuncIn(const su2double &data) {
-    FuncHelper->addInput(data);
+    FuncHelper.addInput(data);
   }
 
   template<class T>
   FORCEINLINE void SetExtFuncIn(const T& data, const int size) {
     for (int i = 0; i < size; i++) {
-      FuncHelper->addInput(data[i]);
+      FuncHelper.addInput(data[i]);
     }
   }
 
@@ -508,22 +511,22 @@ namespace AD{
   FORCEINLINE void SetExtFuncIn(const T& data, const int size_x, const int size_y) {
     for (int i = 0; i < size_x; i++) {
       for (int j = 0; j < size_y; j++) {
-        FuncHelper->addInput(data[i][j]);
+        FuncHelper.addInput(data[i][j]);
       }
     }
   }
 
   FORCEINLINE void SetExtFuncOut(su2double& data) {
-    if (AD::getGlobalTape().isActive()) {
-      FuncHelper->addOutput(data);
+    if (AD::getTape().isActive()) {
+      FuncHelper.addOutput(data);
     }
   }
 
   template<class T>
   FORCEINLINE void SetExtFuncOut(T&& data, const int size) {
     for (int i = 0; i < size; i++) {
-      if (AD::getGlobalTape().isActive()) {
-        FuncHelper->addOutput(data[i]);
+      if (AD::getTape().isActive()) {
+        FuncHelper.addOutput(data[i]);
       }
     }
   }
@@ -532,8 +535,8 @@ namespace AD{
   FORCEINLINE void SetExtFuncOut(T&& data, const int size_x, const int size_y) {
     for (int i = 0; i < size_x; i++) {
       for (int j = 0; j < size_y; j++) {
-        if (AD::getGlobalTape().isActive()) {
-          FuncHelper->addOutput(data[i][j]);
+        if (AD::getTape().isActive()) {
+          FuncHelper.addOutput(data[i][j]);
         }
       }
     }
@@ -544,10 +547,10 @@ namespace AD{
     checkpoint->clear();
   }
 
-  FORCEINLINE void EndExtFunc() { delete FuncHelper; }
+  FORCEINLINE void EndExtFunc() { }
 
   FORCEINLINE bool BeginPassive() {
-    if(AD::getGlobalTape().isActive()) {
+    if(AD::getTape().isActive()) {
       StopRecording();
       return true;
     }
diff --git a/Common/include/code_config.hpp b/Common/include/code_config.hpp
index 7bb34cffbdb..4547054f800 100644
--- a/Common/include/code_config.hpp
+++ b/Common/include/code_config.hpp
@@ -87,7 +87,7 @@ FORCEINLINE Out su2staticcast_p(In ptr) {
 
 #if defined(CODI_REVERSE_TYPE) // reverse mode AD
 #include "codi.hpp"
-#include "codi/tools/dataStore.hpp"
+#include "codi/tools/data/externalFunctionUserData.hpp"
 
 #if defined(HAVE_OMP)
 using su2double = codi::RealReverseIndexParallel;
diff --git a/Common/include/linear_algebra/CSysSolve_b.hpp b/Common/include/linear_algebra/CSysSolve_b.hpp
index eae9de62ad4..006a5e09583 100644
--- a/Common/include/linear_algebra/CSysSolve_b.hpp
+++ b/Common/include/linear_algebra/CSysSolve_b.hpp
@@ -34,6 +34,6 @@ template<class ScalarType>
 struct CSysSolve_b {
   static void Solve_b(const su2double::Real* x, su2double::Real* x_b, size_t m,
                       const su2double::Real* y, const su2double::Real* y_b, size_t n,
-                      codi::DataStore* d);
+                      codi::ExternalFunctionUserData* d);
 };
 #endif
diff --git a/Common/include/parallelization/mpi_structure.hpp b/Common/include/parallelization/mpi_structure.hpp
index 06a65a6fef7..980572dc7eb 100644
--- a/Common/include/parallelization/mpi_structure.hpp
+++ b/Common/include/parallelization/mpi_structure.hpp
@@ -68,12 +68,12 @@
 #include <medi/medi.hpp>
 using namespace medi;
 
-#include <codi/externals/codiMpiTypes.hpp>
+#include <codi/tools/mpi/codiMpiTypes.hpp>
 
 class CMediMPIWrapper;
 typedef CMediMPIWrapper SU2_MPI;
 
-typedef CoDiMpiTypes<su2double> MediTypes;
+typedef codi::CoDiMpiTypes<su2double> MediTypes;
 typedef MediTypes::Tool MediTool;
 
 extern MediTypes* mediTypes;
diff --git a/Common/include/parallelization/omp_structure.cpp b/Common/include/parallelization/omp_structure.cpp
index 09a50c3ba72..ed690b78f6b 100644
--- a/Common/include/parallelization/omp_structure.cpp
+++ b/Common/include/parallelization/omp_structure.cpp
@@ -36,7 +36,6 @@ void omp_initialize() {
 #endif
   opdi::logic = new opdi::OmpLogic;
   opdi::logic->init();
-  su2double::getGlobalTape().initialize();
   opdi::tool = new CoDiOpDiTool<su2double>;
   opdi::tool->init();
 #endif
@@ -45,7 +44,6 @@ void omp_initialize() {
 void omp_finalize() {
 #ifdef HAVE_OPDI
   opdi::tool->finalize();
-  su2double::getGlobalTape().finalize();
   opdi::logic->finalize();
   opdi::backend->finalize();
   delete opdi::tool;
diff --git a/Common/src/basic_types/ad_structure.cpp b/Common/src/basic_types/ad_structure.cpp
index d67bd486a8b..77b09675efd 100644
--- a/Common/src/basic_types/ad_structure.cpp
+++ b/Common/src/basic_types/ad_structure.cpp
@@ -46,7 +46,7 @@ namespace AD {
   SU2_OMP(threadprivate(PreaccHelper))
 #endif
 
-  ExtFuncHelper* FuncHelper;
+  ExtFuncHelper FuncHelper;
 
 #endif
 }
diff --git a/Common/src/linear_algebra/CSysSolve.cpp b/Common/src/linear_algebra/CSysSolve.cpp
index 54406fdfc8c..3d7659d4441 100644
--- a/Common/src/linear_algebra/CSysSolve.cpp
+++ b/Common/src/linear_algebra/CSysSolve.cpp
@@ -864,7 +864,7 @@ unsigned long CSysSolve<ScalarType>::Solve(CSysMatrix<ScalarType> & Jacobian, co
   if (config->GetDiscrete_Adjoint()) {
 #ifdef CODI_REVERSE_TYPE
 
-    TapeActive = AD::getGlobalTape().isActive();
+    TapeActive = AD::TapeActive();
 
     BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
       AD::StartExtFunc(false, false);
@@ -971,16 +971,16 @@ unsigned long CSysSolve<ScalarType>::Solve(CSysMatrix<ScalarType> & Jacobian, co
     BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS
     {
       AD::SetExtFuncOut(&LinSysSol[0], LinSysSol.GetLocSize());
-      AD::FuncHelper->addUserData(&LinSysRes);
-      AD::FuncHelper->addUserData(&LinSysSol);
-      AD::FuncHelper->addUserData(&Jacobian);
-      AD::FuncHelper->addUserData(geometry);
-      AD::FuncHelper->addUserData(config);
-      AD::FuncHelper->addUserData(this);
+      AD::FuncHelper.addUserData(&LinSysRes);
+      AD::FuncHelper.addUserData(&LinSysSol);
+      AD::FuncHelper.addUserData(&Jacobian);
+      AD::FuncHelper.addUserData(geometry);
+      AD::FuncHelper.addUserData(config);
+      AD::FuncHelper.addUserData(this);
     }
     END_SU2_OMP_SAFE_GLOBAL_ACCESS
 
-    AD::FuncHelper->addToTape(CSysSolve_b<ScalarType>::Solve_b);
+    AD::FuncHelper.addToTape(CSysSolve_b<ScalarType>::Solve_b);
 
     SU2_OMP_SAFE_GLOBAL_ACCESS(AD::EndExtFunc();)
 #endif
diff --git a/Common/src/linear_algebra/CSysSolve_b.cpp b/Common/src/linear_algebra/CSysSolve_b.cpp
index c381eb26d39..3db62e67fa2 100644
--- a/Common/src/linear_algebra/CSysSolve_b.cpp
+++ b/Common/src/linear_algebra/CSysSolve_b.cpp
@@ -34,7 +34,7 @@
 template<class ScalarType>
 void CSysSolve_b<ScalarType>::Solve_b(const su2double::Real* x, su2double::Real* x_b, size_t m,
                                       const su2double::Real* y, const su2double::Real* y_b, size_t n,
-                                      codi::DataStore* d) {
+                                      codi::ExternalFunctionUserData* d) {
 
   CSysVector<su2double>* LinSysRes_b = nullptr;
   d->getDataByIndex(LinSysRes_b, 0);
diff --git a/SU2_CFD/src/SU2_CFD.cpp b/SU2_CFD/src/SU2_CFD.cpp
index d5197f8c4dc..f342a4157e7 100644
--- a/SU2_CFD/src/SU2_CFD.cpp
+++ b/SU2_CFD/src/SU2_CFD.cpp
@@ -164,11 +164,6 @@ int main(int argc, char *argv[]) {
   libxsmm_finalize();
 #endif
 
-  /*--- Finalize AD, if necessary. ---*/
-#ifdef HAVE_OPDI
-  AD::getGlobalTape().finalize();
-#endif
-
   /*--- Finalize MPI parallelization. ---*/
   SU2_MPI::Finalize();
 
diff --git a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
index 960a2a8ef4a..34312717cc4 100644
--- a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
@@ -673,7 +673,7 @@ void CDiscAdjMultizoneDriver::SetRecording(RECORDING kind_recording, Kind_Tape t
     if (rank == MASTER_NODE) AD::PrintStatistics();
 #ifdef CODI_REVERSE_TYPE
     if (size > SINGLE_NODE) {
-      su2double myMem = AD::getGlobalTape().getTapeValues().getUsedMemorySize(), totMem = 0.0;
+      su2double myMem = AD::getTape().getTapeValues().getUsedMemorySize(), totMem = 0.0;
       SU2_MPI::Allreduce(&myMem, &totMem, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
       if (rank == MASTER_NODE) {
         cout << "MPI\n";
diff --git a/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
index 2d943c5351e..c866133edaa 100644
--- a/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
@@ -304,7 +304,7 @@ void CDiscAdjSinglezoneDriver::SetRecording(RECORDING kind_recording){
     if (rank == MASTER_NODE) AD::PrintStatistics();
 #ifdef CODI_REVERSE_TYPE
     if (size > SINGLE_NODE) {
-      su2double myMem = AD::getGlobalTape().getTapeValues().getUsedMemorySize(), totMem = 0.0;
+      su2double myMem = AD::getTape().getTapeValues().getUsedMemorySize(), totMem = 0.0;
       SU2_MPI::Allreduce(&myMem, &totMem, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
       if (rank == MASTER_NODE) {
         cout << "MPI\n";
diff --git a/SU2_DOT/src/SU2_DOT.cpp b/SU2_DOT/src/SU2_DOT.cpp
index e15bd2af8ee..05dea2fa5ee 100644
--- a/SU2_DOT/src/SU2_DOT.cpp
+++ b/SU2_DOT/src/SU2_DOT.cpp
@@ -53,11 +53,6 @@ int main(int argc, char *argv[]) {
   const int rank = SU2_MPI::GetRank();
   const int size = SU2_MPI::GetSize();
 
-  /*--- AD initialization ---*/
-#ifdef HAVE_OPDI
-  AD::getGlobalTape().initialize();
-#endif
-
   /*--- Pointer to different structures that will be used throughout the entire code ---*/
 
   CConfig **config_container            = nullptr;
@@ -425,11 +420,6 @@ int main(int argc, char *argv[]) {
   if (rank == MASTER_NODE)
     cout << "\n------------------------- Exit Success (SU2_DOT) ------------------------\n" << endl;
 
-  /*--- Finalize AD, if necessary. ---*/
-#ifdef HAVE_OPDI
-  AD::getGlobalTape().finalize();
-#endif
-
   /*--- Finalize MPI parallelization. ---*/
   SU2_MPI::Finalize();
 

From e8a3a93e987c38e54e98b86c9f35d4830d3c90c9 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 21 Nov 2022 11:34:58 +0100
Subject: [PATCH 040/656] Bug fix

---
 SU2_CFD/src/fluid/CPengRobinson.cpp | 50 -----------------------------
 1 file changed, 50 deletions(-)

diff --git a/SU2_CFD/src/fluid/CPengRobinson.cpp b/SU2_CFD/src/fluid/CPengRobinson.cpp
index 962e8a60ea1..2b5b09d611d 100644
--- a/SU2_CFD/src/fluid/CPengRobinson.cpp
+++ b/SU2_CFD/src/fluid/CPengRobinson.cpp
@@ -39,56 +39,6 @@ CPengRobinson::CPengRobinson(su2double gamma, su2double R, su2double Pstar, su2d
     k = 0.37464 + 1.54226 * w - 0.26992 * w * w;
   else
     k = 0.379642 + 1.48503 * w - 0.164423 * w * w + 0.016666 * w * w * w;
-
-  vector<string> call_input_variables;
-  vector<string> call_output_variables;
-  vector<su2double> call_inputs;
-  vector<su2double*> call_outputs;
-  call_input_variables.push_back("Progress_Variable");
-  call_inputs.push_back(-5.74934292655689e-01);
-  call_input_variables.push_back("Enthalpy");
-  call_inputs.push_back(+2.22692201641688e+03);
-  call_input_variables.push_back("Mixture_Fraction");
-  call_inputs.push_back(0.0144045);
-
-  call_output_variables.push_back("Temperature");
-  call_outputs.push_back(&Temperature);
-  call_output_variables.push_back("Density");
-  call_outputs.push_back(&Density);
-
-  vector<string> call_inputvars_lean;
-  call_inputvars_lean.push_back("Progress_Variable_lean");
-  call_inputvars_lean.push_back("Enthalpy_lean");
-  call_inputvars_lean.push_back("Mixture_Fraction_lean");
-
-  vector<string> call_inputvars_rich;
-  call_inputvars_rich.push_back("Progress_Variable_rich");
-  call_inputvars_rich.push_back("Enthalpy_rich");
-  call_inputvars_rich.push_back("Mixture_Fraction_rich");
-
-  MLPToolbox::CLookUp_ANN * test_mlp = new MLPToolbox::CLookUp_ANN("MLP_collection.mlp");
-  MLPToolbox::CIOMap * test_map = new MLPToolbox::CIOMap(test_mlp, call_input_variables, call_output_variables);
-  MLPToolbox::CIOMap * lean_map = new MLPToolbox::CIOMap(test_mlp, call_inputvars_lean, call_output_variables);
-  MLPToolbox::CIOMap * rich_map = new MLPToolbox::CIOMap(test_mlp, call_inputvars_rich, call_output_variables);
-
-
-  test_mlp->Predict_ANN(test_map, call_inputs, call_outputs);
-  cout << "in flame zone: " << Density << " " << Temperature << endl;
-  call_inputs[0] = -7.36;
-  call_inputs[1] = 26468.5;
-  call_inputs[2] = 1.0;
-  test_mlp->Predict_ANN(rich_map, call_inputs, call_outputs);
-  cout << "rich: " << Density << " " << Temperature << endl;
-  call_inputs[0] = -0.4753;
-  call_inputs[1] = 3144.6;
-  call_inputs[2] = 0.0;
-  test_mlp->Predict_ANN(lean_map, call_inputs, call_outputs);
-  cout << "lean: " << Density << " " << Temperature << endl;
-
-  delete test_mlp;
-  delete test_map;
-  delete rich_map;
-  delete lean_map;
 }
 
 su2double CPengRobinson::alpha2(su2double T) const {

From 0a565343307aa6a5a7f012f2779cf5c02ad4e8b7 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 21 Nov 2022 16:57:25 +0100
Subject: [PATCH 041/656] Allowed for LUT alongside MLP evaluation in
 datadriven fluid model

---
 .../multilayer_perceptron/CNeuralNetwork.hpp  |   3 +
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp    |  75 +++++--
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        | 211 ++++++++++++++++--
 3 files changed, 246 insertions(+), 43 deletions(-)

diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
index a7d1cfba5e4..b58528069d8 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
@@ -83,6 +83,9 @@ class CNeuralNetwork
             delete total_layers.at(i);
         }
         delete [] ANN_outputs;
+        delete [] inputLayer;
+        delete [] outputLayer;
+        delete [] activation_function_types;
     };
     void defineInputLayer(unsigned long n_neurons);
     void defineOutputLayer(unsigned long n_neurons);
diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index 2866bcbebf8..79e423d6215 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -30,6 +30,8 @@
 
 #include "CFluidModel.hpp"
 #include "../../../Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp"
+#include "../../../Common/include/containers/CLookUpTable.hpp"
+
 /*!
  * \class CDataDrivenFluid
  * \brief Template class for fluid model definition using multi-layer perceptrons for 
@@ -39,26 +41,35 @@
 class CDataDrivenFluid : public CFluidModel {
  protected:
 
-  unsigned short Kind_DataDriven_Method = ENUM_DATADRIVEN_METHOD::LUT;
-  size_t idx_rho,
-         idx_e;
+  unsigned short Kind_DataDriven_Method = ENUM_DATADRIVEN_METHOD::LUT;       // Interpolation method for data set evaluation
 
-  su2double Newton_Relaxation,
-            rho_start,
-            e_start;
+  size_t idx_rho,    // Interpolator index for density input
+         idx_e;      // Interpolator index for energy input
 
-  string input_filename;
+  su2double Newton_Relaxation,     // Relaxation factor for Newton solvers.
+            rho_start,             // Initial value for the density in Newton solver processes.
+            e_start;               // Initial value for the energy in Newton solver processes.
 
-  vector<string> input_names_rhoe,
-                 output_names_rhoe;
+  string input_filename;    // Data-driven method input file name.
+  
+  su2double dsde_rho, dsdrho_e, d2sde2, d2sdedrho, d2sdrho2;
+  
+  su2double Gamma{0.0};           /*!< \brief Ratio of Specific Heats. */
+  su2double Gamma_Minus_One{0.0}; /*!< \brief Ratio of Specific Heats Minus One. */
+  su2double Gas_Constant{0.0};    /*!< \brief Gas Constant. */
+  
+  vector<string> input_names_rhoe,        // Data-driven method input variable names of the independent variables (density, energy).
+                 output_names_rhoe;       // Output variable names listed in the data-driven method input file name.
 
-  vector<su2double*> outputs_rhoe;
+  vector<su2double*> outputs_rhoe;        // Pointers to output variables.
 
-  MLPToolbox::CLookUp_ANN * lookup_mlp;
-  MLPToolbox::CIOMap * iomap_rhoe;
-  vector<su2double> MLP_inputs;
+  /*--- Class variables for the multi-layer perceptron method ---*/
+  MLPToolbox::CLookUp_ANN * lookup_mlp;   // multi-layer perceptron collection.
+  MLPToolbox::CIOMap * iomap_rhoe;        // input-output map.
+  vector<su2double> MLP_inputs;           // inputs for the multi-layer perceptron look-up operation.
 
-  
+  /*--- Class variables for the look-up table method ---*/
+  CLookUpTable *lookup_table;
 
   void MapInputs_to_Outputs();
 
@@ -71,29 +82,49 @@ class CDataDrivenFluid : public CFluidModel {
   ~CDataDrivenFluid();
   /*!
    * \brief Set the Dimensionless State using Density and Internal Energy
-   * \param[in] rho - first thermodynamic variable.
-   * \param[in] e - second thermodynamic variable.
+   * \param[in] rho - first thermodynamic variable (density).
+   * \param[in] e - second thermodynamic variable (static energy).
    */
   void SetTDState_rhoe(su2double rho, su2double e) override;
 
   /*!
    * \brief Set the Dimensionless State using Pressure  and Temperature
-   * \param[in] P - first thermodynamic variable.
-   * \param[in] T - second thermodynamic variable.
+   * \param[in] P - first thermodynamic variable (pressure).
+   * \param[in] T - second thermodynamic variable (temperature).
    */
   void SetTDState_PT(su2double P, su2double T) override;
 
   /*!
    * \brief Set the Dimensionless State using Pressure and Density
-   * \param[in] P - first thermodynamic variable.
-   * \param[in] rho - second thermodynamic variable.
+   * \param[in] P - first thermodynamic variable (pressure).
+   * \param[in] rho - second thermodynamic variable (density).
    */
   void SetTDState_Prho(su2double P, su2double rho) override;
 
   /*!
    * \brief Set the Dimensionless Internal Energy using Pressure and Density
-   * \param[in] P - first thermodynamic variable.
-   * \param[in] rho - second thermodynamic variable.
+   * \param[in] P - first thermodynamic variable (pressure).
+   * \param[in] rho - second thermodynamic variable (density).
    */
   void SetEnergy_Prho(su2double P, su2double rho) override;
+
+  /*!
+   * \brief Set the Dimensionless Internal Energy using Pressure and Density
+   * \param[in] rho - second thermodynamic variable (density).
+   */
+  void SetTDState_rhoT(su2double rho, su2double T) override;
+
+  /*!
+   * \brief Set the Dimensionless State using Enthalpy and Entropy
+   * \param[in] h - first thermodynamic variable (h).
+   * \param[in] s - second thermodynamic variable (s).
+   */
+  void SetTDState_hs(su2double h, su2double s) override;
+
+  /*!
+   * \brief Set the Dimensionless State using Pressure and Entropy
+   * \param[in] P - first thermodynamic variable (P).
+   * \param[in] s - second thermodynamic variable (s).
+   */
+  void SetTDState_Ps(su2double P, su2double s) override;
 };
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 4f4b7e95790..7dafd4bf5e6 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -44,6 +44,9 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
   case ENUM_DATADRIVEN_METHOD::MLP:
     lookup_mlp = new MLPToolbox::CLookUp_ANN(input_filename);
     break;
+  case ENUM_DATADRIVEN_METHOD::LUT:
+    lookup_table = new CLookUpTable(input_filename, "Density", "Energy");
+    break;
   default:
     break;
   }
@@ -66,7 +69,9 @@ CDataDrivenFluid::~CDataDrivenFluid(){
     delete iomap_rhoe;
     delete lookup_mlp;
     break;
-  
+  case ENUM_DATADRIVEN_METHOD::LUT:
+    delete lookup_table;
+    break;
   default:
     break;
   }
@@ -80,23 +85,19 @@ void CDataDrivenFluid::MapInputs_to_Outputs(){
   input_names_rhoe.push_back("Energy");
   idx_e = 1;
 
-  /*--- Required outputs for the interpolation method are primary and secondary thermodynamic variables. ---*/
-  output_names_rhoe.push_back("Temperature");
-  outputs_rhoe.push_back(&Temperature);
-  output_names_rhoe.push_back("Pressure");
-  outputs_rhoe.push_back(&Pressure);
-  output_names_rhoe.push_back("SoundSpeed2");
-  outputs_rhoe.push_back(&SoundSpeed2);
-  output_names_rhoe.push_back("dPdrho_e");
-  outputs_rhoe.push_back(&dPdrho_e);
-  output_names_rhoe.push_back("dPde_rho");
-  outputs_rhoe.push_back(&dPde_rho);
-  output_names_rhoe.push_back("dTdrho_e");
-  outputs_rhoe.push_back(&dTdrho_e);
-  output_names_rhoe.push_back("dTde_rho");
-  outputs_rhoe.push_back(&dTde_rho);
-  output_names_rhoe.push_back("Entropy");
+  /*--- Required outputs for the interpolation method are entropy and its partial derivatives with respect to energy and density ---*/
+  output_names_rhoe.push_back("s");
   outputs_rhoe.push_back(&Entropy);
+  output_names_rhoe.push_back("dsde_rho");
+  outputs_rhoe.push_back(&dsde_rho);
+  output_names_rhoe.push_back("dsdrho_e");
+  outputs_rhoe.push_back(&dsdrho_e);
+  output_names_rhoe.push_back("d2sde2");
+  outputs_rhoe.push_back(&d2sde2);
+  output_names_rhoe.push_back("d2sdedrho");
+  outputs_rhoe.push_back(&d2sdedrho);
+  output_names_rhoe.push_back("d2sdrho2");
+  outputs_rhoe.push_back(&d2sdrho2);
 
   /*--- Further preprocessing of input and output variables ---*/
   switch (Kind_DataDriven_Method)
@@ -125,15 +126,37 @@ void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
     /* --- Evaluate MLP --- */
     lookup_mlp->Predict_ANN(iomap_rhoe, MLP_inputs, outputs_rhoe);
     break;
-  
+  case ENUM_DATADRIVEN_METHOD::LUT:
+    lookup_table->LookUp_ProgEnth(output_names_rhoe, outputs_rhoe, rho, e, "Density", "Energy");
   default:
     break;
   }
 
+  su2double blue_term = (dsdrho_e * (2 - rho * pow(dsde_rho, -1) * d2sdedrho) + rho * d2sdrho2);
+  su2double green_term = (- pow(dsde_rho, -1) * d2sde2 * dsdrho_e + d2sdedrho);
+  
+  SoundSpeed2 = - rho * pow(dsde_rho, -1) * (blue_term - rho * green_term * (dsdrho_e / dsde_rho));
+
+  Temperature = 1.0 / dsde_rho;
+  Pressure = -pow(rho, 2) * Temperature * dsdrho_e;
+  Density = rho;
+  StaticEnergy = e;
+  
+  dTde_rho = -pow(dsde_rho, -2)*d2sde2;
+  dTdrho_e = 0.0;
+
+  dPde_rho = -pow(rho, 2) * dTde_rho * dsdrho_e;
+  dPdrho_e = -2*rho*Temperature*dsdrho_e - pow(rho, 2)*Temperature*d2sdrho2;
+
+  Cp = (1 / dTde_rho) * ( 1 + (1 / Density)*dPde_rho) + (1/Density)*(1/dTdrho_e)*(dPdrho_e - Pressure / Density);
+  Cv = 1 / dTde_rho;
+  Gamma = Cp / Cv;
+  Gamma_Minus_One = Gamma - 1;
+  Gas_Constant = Cp - Cv;
+  
 }
 
 void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
-  /*--- Newton solver for */
 
   /*--- Setting initial values for density and energy ---*/
   su2double rho = rho_start, 
@@ -152,6 +175,7 @@ void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
             delta_e,      // Energy step size
             determinant;  // Jacobian determinant
 
+  /*--- Initiating Newton solver ---*/
   while(!converged && (Iter < iter_max)){
 
     /*--- Determine thermodynamic state based on current density and energy*/
@@ -220,8 +244,8 @@ void CDataDrivenFluid::SetEnergy_Prho(su2double P, su2double rho) {
       /*--- Compute step size for energy ---*/
       delta_e = delta_P / dPde_rho;
 
-      /*--- Update density and energy values ---*/
-      e -= Newton_Relaxation * delta_e;
+      /*--- energy value ---*/
+      e += Newton_Relaxation * delta_e;
     }
     Iter ++;
   }
@@ -229,3 +253,148 @@ void CDataDrivenFluid::SetEnergy_Prho(su2double P, su2double rho) {
   /*--- Setting static energy as the converged value ---*/
   StaticEnergy = e;
 }
+
+void CDataDrivenFluid::SetTDState_rhoT(su2double rho, su2double T) {
+
+  /*--- Setting initial values for density and energy ---*/
+  su2double e = e_start;
+
+  su2double tolerance_T = 1;  // Tolerance for temperature solution
+
+  bool converged = false;         // Convergence flag
+  unsigned long iter_max = 1000,  // Maximum number of iterations
+                Iter = 0;       
+
+  su2double delta_T,      // Temperature residual
+            delta_e;  // Energy increment
+
+  /*--- Initiating Newton solver ---*/
+  while(!converged && (Iter < iter_max)){
+
+    /*--- Determine thermodynamic state based on current density and energy*/
+    SetTDState_rhoe(rho ,e);
+
+    /*--- Determine temperature residual ---*/
+    delta_T = Temperature - T;
+
+    /*--- Continue iterative process if residuals are outside tolerances ---*/
+    if((abs(delta_T) < tolerance_T)){
+      converged = true;
+    }else{
+      
+
+      delta_e = delta_T / dTde_rho;
+
+      /*--- Update energy value ---*/
+      e += Newton_Relaxation * delta_e;
+    }
+    Iter ++;
+  }
+
+  /*--- Calculate thermodynamic state based on converged values for density and energy ---*/
+  SetTDState_rhoe(rho, e);
+}
+
+void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
+
+  /*--- Setting initial values for density and energy ---*/
+  su2double rho = rho_start, 
+            e = e_start;
+
+  su2double tolerance_h = 10, // Tolerance for enthalpy solution
+            tolerance_s = 1;  // Tolerance for entropy solution
+
+  bool converged = false;         // Convergence flag
+  unsigned long iter_max = 1000,  // Maximum number of iterations
+                Iter = 0;       
+
+  su2double delta_h,      // Enthalpy
+            delta_s,      // Entropy residual
+            delta_rho,    // Density step size
+            delta_e,      // Energy step size
+            determinant;  // Jacobian determinant
+
+  /*--- Initiating Newton solver ---*/
+  while(!converged && (Iter < iter_max)){
+
+    /*--- Determine thermodynamic state based on current density and energy*/
+    SetTDState_rhoe(rho ,e);
+
+    su2double Enthalpy = e + Pressure / rho;
+    /*--- Determine pressure and temperature residuals ---*/
+    delta_h = Enthalpy - h;
+    delta_s = Entropy - s;
+
+    /*--- Continue iterative process if residuals are outside tolerances ---*/
+    if((abs(delta_h) < tolerance_h) && (abs(delta_s) < tolerance_s)){
+      converged = true;
+    }else{
+      
+      su2double dh_de = 1 + dPde_rho / rho;
+      su2double dh_drho = -Pressure*pow(rho, -2) + dPdrho_e / rho;
+
+      determinant = dh_drho * dsde_rho - dh_de * dsdrho_e;
+      delta_rho = (dsde_rho * delta_h - dh_de * delta_s) / determinant;
+      delta_e = (-dsdrho_e * delta_h + dh_drho * delta_s) / determinant;
+
+      /*--- Update density and energy values ---*/
+      rho -= Newton_Relaxation * delta_rho;
+      e -= Newton_Relaxation * delta_e;
+    }
+    Iter ++;
+  }
+
+  /*--- Calculate thermodynamic state based on converged values for density and energy ---*/
+  SetTDState_rhoe(rho, e);
+}
+
+void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
+  
+  /*--- Setting initial values for density and energy ---*/
+  su2double rho = rho_start, 
+            e = e_start;
+
+  su2double tolerance_P = 10, // Tolerance for pressure solution
+            tolerance_s = 1;  // Tolerance for entropy solution
+
+  bool converged = false;         // Convergence flag
+  unsigned long iter_max = 1000,  // Maximum number of iterations
+                Iter = 0;       
+
+  su2double delta_P,      // Enthalpy
+            delta_s,      // Entropy residual
+            delta_rho,    // Density step size
+            delta_e,      // Energy step size
+            determinant;  // Jacobian determinant
+
+  /*--- Initiating Newton solver ---*/
+  while(!converged && (Iter < iter_max)){
+
+    /*--- Determine thermodynamic state based on current density and energy*/
+    SetTDState_rhoe(rho ,e);
+
+    /*--- Determine pressure and temperature residuals ---*/
+    delta_P = Pressure - P;
+    delta_s = Entropy - s;
+
+    /*--- Continue iterative process if residuals are outside tolerances ---*/
+    if((abs(delta_P) < tolerance_P) && (abs(delta_s) < tolerance_s)){
+      converged = true;
+    }else{
+
+       /*--- Compute step size for density and energy ---*/
+      determinant = dPdrho_e * dsde_rho - dPde_rho * dsdrho_e;
+
+      delta_rho = (dsde_rho * delta_P - dPde_rho * delta_s) / determinant;
+      delta_e = (-dsdrho_e * delta_P + dPdrho_e * delta_s) / determinant;
+
+      /*--- Update density and energy values ---*/
+      rho -= Newton_Relaxation * delta_rho;
+      e -= Newton_Relaxation * delta_e;
+    }
+    Iter ++;
+  }
+
+  /*--- Calculate thermodynamic state based on converged values for density and energy ---*/
+  SetTDState_rhoe(rho, e);
+}
\ No newline at end of file

From 8ce5a260cec8fefcbd240081d2153de5ec8e321c Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 21 Nov 2022 17:15:11 +0100
Subject: [PATCH 042/656] Replaced progress variable and enthalpy variables in
 the CLookUpTable class with x and y

---
 Common/include/containers/CLookUpTable.hpp | 102 +++++++-------
 Common/src/containers/CLookUpTable.cpp     | 154 ++++++++++-----------
 2 files changed, 128 insertions(+), 128 deletions(-)

diff --git a/Common/include/containers/CLookUpTable.hpp b/Common/include/containers/CLookUpTable.hpp
index ecb59c97aa1..1d93cdea516 100644
--- a/Common/include/containers/CLookUpTable.hpp
+++ b/Common/include/containers/CLookUpTable.hpp
@@ -53,10 +53,10 @@ class CLookUpTable {
   unsigned long n_hull_points;
 
   /*! 
-   * \brief the lower and upper limits of the enthalpy and progress variable.
+   * \brief the lower and upper limits of the y and x.
    */
-  su2double limits_table_enth[2];
-  su2double limits_table_prog[2];
+  su2double limits_table_y[2];
+  su2double limits_table_x[2];
 
   /*! \brief Holds the variable names stored in the table file.
    * Order is in sync with data
@@ -80,12 +80,12 @@ class CLookUpTable {
    */
   std::vector<unsigned long> hull;
 
-  CTrapezoidalMap trap_map_prog_enth;
+  CTrapezoidalMap trap_map_x_y;
 
   /*! \brief 
    * vector of all the weight factors for the interpolation.
    */
-  std::vector<su2activematrix> interp_mat_inv_prog_enth;
+  std::vector<su2activematrix> interp_mat_inv_x_y;
 
   /*! \brief 
    * returns the index to the variable in the lookup table.
@@ -112,12 +112,12 @@ class CLookUpTable {
 
   /*!
    * \brief find the table limits, i.e. the minimum and maximum values of the 2 independent.
-   * controlling variables (progress variable and enthalpy). We put the values in the variables.
-   * limits_table_prog[2] and limit_table_enth[2].
-   * \param[in] name_prog - the string name for the first controlling variable.
-   * \param[in] name_enth - the string name of the second controlling variable.
+   * controlling variables (x and y). We put the values in the variables.
+   * limits_table_x[2] and limit_table_y[2].
+   * \param[in] name_x - the string name for the first controlling variable.
+   * \param[in] name_y - the string name of the second controlling variable.
    */
-  void FindTableLimits(const std::string& name_prog, const std::string& name_enth);
+  void FindTableLimits(const std::string& name_x, const std::string& name_y);
 
   /*!
    * \brief construct a list of all the edges and a list of the pair of elements left and right of the edge.
@@ -132,15 +132,15 @@ class CLookUpTable {
 
   /*!
    * \brief compute vector of all (inverse) interpolation coefficients "interp_mat_inv_prog_enth" of all triangles.
-   * \param[in] name_prog - the string name of the first controlling variable (progress variable).
-   * \param[in] name_enth - the string name of the second controlling variable (enthalpy).
+   * \param[in] name_prog - the string name of the first controlling variable (x).
+   * \param[in] name_enth - the string name of the second controlling variable (y).
   */
-  void ComputeInterpCoeffs(const std::string& name_prog, const std::string& name_enth);
+  void ComputeInterpCoeffs(const std::string& name_x, const std::string& name_y);
 
   /*!
    * \brief compute the inverse matrix for interpolation.
-   * \param[in] vec_x - pointer to first coordinate (progress variable).
-   * \param[in] vec_y - pointer to second coordinate (enthalpy).
+   * \param[in] vec_x - pointer to first coordinate (x).
+   * \param[in] vec_y - pointer to second coordinate (y).
    * \param[in] point_ids - single triangle data.
    * \param[out] interp_mat_inv - inverse matrix for interpolation.
   */
@@ -149,8 +149,8 @@ class CLookUpTable {
 
   /*!
    * \brief compute the interpolation coefficients for the triangular interpolation.
-   * \param[in] val_x - value of first coordinate (progress variable).
-   * \param[in] val_y - value of second coordinate (enthalpy).
+   * \param[in] val_x - value of first coordinate (x).
+   * \param[in] val_y - value of second coordinate (y).
    * \param[in] interp_mat_inv - inverse matrix for interpolation.
    * \param[out] interp_coeffs - interpolation coefficients.
   */
@@ -168,14 +168,14 @@ class CLookUpTable {
                         std::array<su2double,3>& val_interp_coeffs);
 
   /*!
-   * \brief find the point on the hull (boundary of the table) that is closest to the point P(val_prog,val_enth).
+   * \brief find the point on the hull (boundary of the table) that is closest to the point P(val_x,val_y).
    * \param[in] val_x - first coordinate of point P(val_x,val_y) to check.
    * \param[in] val_y - second coordinate of point P(val_x,val_y) to check.
    * \param[in] name_prog - string name of the first controlling variable.
    * \param[in] name_enth - string name of the second controlling variable.
    * \returns point id of the nearest neighbor on the hull.
    */
-  unsigned long FindNearestNeighborOnHull(su2double val_prog, su2double val_enth, const std::string& name_prog, const std::string& name_enth);
+  unsigned long FindNearestNeighborOnHull(su2double val_x, su2double val_y, const std::string& name_x, const std::string& name_y);
 
   /*!
    * \brief determine if a point P(val_x,val_y) is inside the triangle val_id_triangle.
@@ -186,8 +186,8 @@ class CLookUpTable {
    * \param[in] name_enth - string name of the second controlling variable.
    * \returns true if the point is in the triangle, false if it is outside.
    */
-  bool IsInTriangle(su2double val_x, su2double val_y, unsigned long val_id_triangle, const std::string& name_prog,
-                    const std::string& name_enth);
+  bool IsInTriangle(su2double val_x, su2double val_y, unsigned long val_id_triangle, const std::string& name_x,
+                    const std::string& name_y);
 
   /*!
    * \brief compute the area of a triangle given the 3 points of the triangle.
@@ -204,7 +204,7 @@ class CLookUpTable {
   }
 
  public:
-  CLookUpTable(const std::string& file_name_lut, const std::string& name_prog, const std::string& name_enth);
+  CLookUpTable(const std::string& file_name_lut, const std::string& name_x, const std::string& name_y);
 
 
   /*!
@@ -214,59 +214,59 @@ class CLookUpTable {
 
   /*!
    * \brief lookup 1 value of the single variable "val_name_var" using controlling variable values(val_prog,val_enth)
-   *  whose controlling variable names are "name_prog" and "name_enth".
+   *  whose controlling variable names are "name_x" and "name_y".
    * \param[in] val_name_var - string name of the variable to look up.
    * \param[out] val_var - the stored value of the variable to look up.
-   * \param[in] val_prog - value of controlling variable 1 (progress variable).
-   * \param[in] val_enth - value of controlling variable 2 (enthalpy).
-   * \param[in] name_prog - string name of controlling variable 1 (progress variable).
-   * \param[in] name_enth - string name of controlling variable 2 (enthalpy).
+   * \param[in] val_x - value of controlling variable 1 (x).
+   * \param[in] val_y - value of controlling variable 2 (y).
+   * \param[in] name_x - string name of controlling variable 1 (x).
+   * \param[in] name_y - string name of controlling variable 2 (y).
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
-  unsigned long LookUp_ProgEnth(const std::string& val_name_var, su2double* val_var, su2double val_prog, su2double val_enth,
-                                const std::string& name_prog, const std::string& name_enth);
+  unsigned long LookUp_XY(const std::string& val_name_var, su2double* val_var, su2double val_x, su2double val_y,
+                                const std::string& name_x, const std::string& name_y);
 
   /*!
-   * \brief lookup 1 value for each of the variables in "val_name_var" using controlling variable values(val_prog,val_enth)
-   *  whose controlling variable names are "name_prog" and "name_enth".
+   * \brief lookup 1 value for each of the variables in "val_name_var" using controlling variable values(val_x,val_y)
+   *  whose controlling variable names are "name_x" and "name_y".
    * \param[in] val_names_var - vector of string names of the variables to look up.
    * \param[out] val_vars - pointer to the vector of stored values of the variables to look up.
-   * \param[in] val_prog - value of controlling variable 1 (progress variable).
-   * \param[in] val_enth - value of controlling variable 2 (enthalpy).
-   * \param[in] name_prog - string name of controlling variable 1 (progress variable).
-   * \param[in] name_enth - string name of controlling variable 2 (enthalpy).
+   * \param[in] val_x - value of controlling variable 1 (x).
+   * \param[in] val_y - value of controlling variable 2 (y).
+   * \param[in] name_x - string name of controlling variable 1 (x).
+   * \param[in] name_y - string name of controlling variable 2 (y).
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
-  unsigned long LookUp_ProgEnth(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars, su2double val_prog,
-                                su2double val_enth, const std::string& name_prog, const std::string& name_enth);
+  unsigned long LookUp_XY(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars, su2double val_x,
+                                su2double val_y, const std::string& name_x, const std::string& name_y);
 
   /*!
-   * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_prog,val_enth)
-   *  whose controlling variable names are "name_prog" and "name_enth".
+   * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_x,val_y)
+   *  whose controlling variable names are "name_x" and "name_y".
    * \param[in] val_name_var - string name of the variable to look up.
    * \param[out] val_var - the stored value of the variable to look up.
-   * \param[in] val_prog - value of controlling variable 1 (progress variable).
-   * \param[in] val_enth - value of controlling variable 2 (enthalpy).
-   * \param[in] name_prog - string name of controlling variable 1 (progress variable).
-   * \param[in] name_enth - string name of controlling variable 2 (enthalpy).
+   * \param[in] val_x - value of controlling variable 1 (x).
+   * \param[in] val_y - value of controlling variable 2 (y).
+   * \param[in] name_x - string name of controlling variable 1 (x).
+   * \param[in] name_y - string name of controlling variable 2 (y).
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
-  unsigned long LookUp_ProgEnth(const std::vector<std::string>& val_names_var, std::vector<su2double>& val_vars, su2double val_prog,
-                                su2double val_enth, const std::string& name_prog, const std::string& name_enth);
+  unsigned long LookUp_XY(const std::vector<std::string>& val_names_var, std::vector<su2double>& val_vars, su2double val_x,
+                                su2double val_y, const std::string& name_x, const std::string& name_y);
 
   /*!
-   * \brief determine the minimum and maximum value of the enthalpy (controlling variable 2).
+   * \brief determine the minimum and maximum value of the y (controlling variable 2).
    * \returns pair of minimum and maximum value of controlling variable 2.
    */
-  inline std::pair<su2double, su2double> GetTableLimitsEnth() const {
-    return std::make_pair(limits_table_enth[0], limits_table_enth[1]);
+  inline std::pair<su2double, su2double> GetTableLimitsY() const {
+    return std::make_pair(limits_table_y[0], limits_table_y[1]);
   }
 
   /*!
-   * \brief determine the minimum and maximum value of the progress variable (controlling variable 1).
+   * \brief determine the minimum and maximum value of the x (controlling variable 1).
    * \returns pair of minimum and maximum value of controlling variable 1.
    */
-  inline std::pair<su2double, su2double> GetTableLimitsProg() const {
-    return std::make_pair(limits_table_prog[0], limits_table_prog[1]);
+  inline std::pair<su2double, su2double> GetTableLimitsX() const {
+    return std::make_pair(limits_table_x[0], limits_table_x[1]);
   }
 };
diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index a0e84c2926e..2f450268d9a 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -31,14 +31,14 @@
 
 using namespace std;
 
-CLookUpTable::CLookUpTable(const string& var_file_name_lut, const string& name_prog, const string& name_enth) {
+CLookUpTable::CLookUpTable(const string& var_file_name_lut, const string& name_x, const string& name_y) {
   file_name_lut = var_file_name_lut;
 
   rank = SU2_MPI::GetRank();
 
   LoadTableRaw(var_file_name_lut);
 
-  FindTableLimits(name_prog, name_enth);
+  FindTableLimits(name_x, name_y);
 
   if (rank == MASTER_NODE)
     cout << "Detecting all unique edges and setting edge to triangle connectivity "
@@ -53,11 +53,11 @@ CLookUpTable::CLookUpTable(const string& var_file_name_lut, const string& name_p
   PrintTableInfo();
 
   if (rank == MASTER_NODE)
-    cout << "Building a trapezoidal map for the (progress variable, enthalpy) "
+    cout << "Building a trapezoidal map for the (x, y) "
             "space ..."
          << endl;
 
-  trap_map_prog_enth = CTrapezoidalMap(GetDataP(name_prog), GetDataP(name_enth), table_data.cols(), edges, edge_to_triangle);
+  trap_map_x_y = CTrapezoidalMap(GetDataP(name_x), GetDataP(name_y), table_data.cols(), edges, edge_to_triangle);
 
   if (rank == MASTER_NODE) 
     cout << " done." << endl;
@@ -66,7 +66,7 @@ CLookUpTable::CLookUpTable(const string& var_file_name_lut, const string& name_p
     cout << "Precomputing interpolation coefficients..." << endl;
   
 
-  ComputeInterpCoeffs(name_prog, name_enth);
+  ComputeInterpCoeffs(name_x, name_y);
 
   if (rank == MASTER_NODE) 
     cout << "LUT fluid model ready for use" << endl;
@@ -95,15 +95,15 @@ void CLookUpTable::LoadTableRaw(const string& var_file_name_lut) {
     cout << " done." << endl;
 }
 
-void CLookUpTable::FindTableLimits(const string& name_prog, const string& name_enth) {
-  int ixEnth = GetIndexOfVar(name_enth);
-  int ixProg = GetIndexOfVar(name_prog);
+void CLookUpTable::FindTableLimits(const string& name_x, const string& name_y) {
+  int ixy = GetIndexOfVar(name_y);
+  int ixx = GetIndexOfVar(name_x);
 
-  /* we find the lowest and highest value of enthalpy and progress variable in the table */
-  limits_table_enth[0] = *min_element(&table_data[ixEnth][0], &table_data[ixEnth][0]+table_data.cols());
-  limits_table_enth[1] = *max_element(&table_data[ixEnth][0], &table_data[ixEnth][0]+table_data.cols());
-  limits_table_prog[0] = *min_element(&table_data[ixProg][0], &table_data[ixProg][0]+table_data.cols());
-  limits_table_prog[1] = *max_element(&table_data[ixProg][0], &table_data[ixProg][0]+table_data.cols());
+  /* we find the lowest and highest value of y and x in the table */
+  limits_table_y[0] = *min_element(&table_data[ixy][0], &table_data[ixy][0]+table_data.cols());
+  limits_table_y[1] = *max_element(&table_data[ixy][0], &table_data[ixy][0]+table_data.cols());
+  limits_table_x[0] = *min_element(&table_data[ixx][0], &table_data[ixx][0]+table_data.cols());
+  limits_table_x[1] = *max_element(&table_data[ixx][0], &table_data[ixx][0]+table_data.cols());
 
 }
 
@@ -122,10 +122,10 @@ void CLookUpTable::PrintTableInfo() {
     cout << "| Number of triangles:" << setw(44) << right << n_triangles << " |" << endl;
     cout << "| Number of edges:" << setw(48) << right << edges.size() << " |" << endl;
     cout << "+------------------------------------------------------------------+" << endl;
-    cout << "| Minimum enthalpy:" << setw(47) << right << limits_table_enth[0] << " |" << endl;
-    cout << "| Maximum enthalpy:" << setw(47) << right << limits_table_enth[1] << " |" << endl;
-    cout << "| Minimum progress variable:" << setw(38) << right << limits_table_prog[0] << " |" << endl;
-    cout << "| Maximum progress variable:" << setw(38) << right << limits_table_prog[1] << " |" << endl;
+    cout << "| Minimum y:" << setw(47) << right << limits_table_y[0] << " |" << endl;
+    cout << "| Maximum y:" << setw(47) << right << limits_table_y[1] << " |" << endl;
+    cout << "| Minimum x:" << setw(38) << right << limits_table_x[0] << " |" << endl;
+    cout << "| Maximum x:" << setw(38) << right << limits_table_x[1] << " |" << endl;
     cout << "+------------------------------------------------------------------+" << endl;
     cout << "| Variable names:                                                  |" << endl;
     cout << "|                                                                  |" << endl;
@@ -243,13 +243,13 @@ void CLookUpTable::IdentifyUniqueEdges() {
   }
 }
 
-void CLookUpTable::ComputeInterpCoeffs(const string& name_prog, const string& name_enth) {
-  /* build KD tree for enthalpy, progress variable space */
+void CLookUpTable::ComputeInterpCoeffs(const string& name_x, const string& name_y) {
+  /* build KD tree for y, x space */
 
   std::array<unsigned long, 3> next_triangle;
 
-  const su2double* prog = GetDataP(name_prog);
-  const su2double* enth = GetDataP(name_enth);
+  const su2double* x = GetDataP(name_x);
+  const su2double* y = GetDataP(name_y);
 
   /* calculate weights for each triangle (basically a distance function) and
    * build inverse interpolation matrices */
@@ -259,9 +259,9 @@ void CLookUpTable::ComputeInterpCoeffs(const string& name_prog, const string& na
       next_triangle[p] = triangles[i_triangle][p];
     }
 
-    su2activematrix prog_interp_mat_inv(3, 3);
-    GetInterpMatInv(prog, enth, next_triangle, prog_interp_mat_inv);
-    interp_mat_inv_prog_enth.push_back(prog_interp_mat_inv);
+    su2activematrix x_interp_mat_inv(3, 3);
+    GetInterpMatInv(x, y, next_triangle, x_interp_mat_inv);
+    interp_mat_inv_x_y.push_back(x_interp_mat_inv);
   }
 }
 
@@ -291,8 +291,8 @@ void CLookUpTable::GetInterpMatInv(const su2double* vec_x, const su2double* vec_
 
 }
 
-unsigned long CLookUpTable::LookUp_ProgEnth(const string& val_name_var, su2double *val_var, su2double val_prog,
-                                            su2double val_enth, const string& name_prog, const string& name_enth) {
+unsigned long CLookUpTable::LookUp_XY(const string& val_name_var, su2double *val_var, su2double val_x,
+                                            su2double val_y, const string& name_x, const string& name_y) {
   unsigned long exit_code = 0;
 
   if (val_name_var.compare("NULL") == 0) {
@@ -301,17 +301,17 @@ unsigned long CLookUpTable::LookUp_ProgEnth(const string& val_name_var, su2doubl
     return exit_code;
   }
 
-  /* check if progress variable and enthalpy value is in table range */
-  if ((val_prog >= limits_table_prog[0] && val_prog <= limits_table_prog[1]) &&
-      (val_enth >= limits_table_enth[0] && val_enth <= limits_table_enth[1])){
+  /* check if x and y value is in table range */
+  if ((val_x >= limits_table_x[0] && val_x <= limits_table_x[1]) &&
+      (val_y >= limits_table_y[0] && val_y <= limits_table_y[1])){
 
-    /* find the triangle that holds the (prog, enth) point */
-    unsigned long id_triangle = trap_map_prog_enth.GetTriangle(val_prog, val_enth);
+    /* find the triangle that holds the (x, y) point */
+    unsigned long id_triangle = trap_map_x_y.GetTriangle(val_x, val_y);
 
-    if (IsInTriangle(val_prog, val_enth, id_triangle, name_prog, name_enth)) {
+    if (IsInTriangle(val_x, val_y, id_triangle, name_x, name_y)) {
       /* get interpolation coefficients for point on triangle */
       std::array<su2double,3> interp_coeffs{0};
-      GetInterpCoeffs(val_prog, val_enth, interp_mat_inv_prog_enth[id_triangle], interp_coeffs);
+      GetInterpCoeffs(val_x, val_y, interp_mat_inv_x_y[id_triangle], interp_coeffs);
 
       /* first, copy the single triangle from the large triangle list*/
       std::array<unsigned long,3> triangle{0};
@@ -322,67 +322,67 @@ unsigned long CLookUpTable::LookUp_ProgEnth(const string& val_name_var, su2doubl
       exit_code = 0;
     } else {
       /* in bounding box but outside of table */
-      unsigned long nearest_neighbor = FindNearestNeighborOnHull(val_prog, val_enth, name_prog, name_enth);
+      unsigned long nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, name_x, name_y);
       *val_var = GetDataP(val_name_var)[nearest_neighbor];
       exit_code = 1;
     }
   } else {
     /* lookup is outside of table bounding box */
-    unsigned long nearest_neighbor = FindNearestNeighborOnHull(val_prog, val_enth, name_prog, name_enth);
+    unsigned long nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, name_x, name_y);
     *val_var = GetDataP(val_name_var)[nearest_neighbor];
     exit_code = 1;
   }
   return exit_code;
 }
 
-unsigned long CLookUpTable::LookUp_ProgEnth(const vector<string>& val_names_var, vector<su2double>& val_vars,
-                                            su2double val_prog, su2double val_enth, const string& name_prog,
-                                            const string& name_enth) {
+unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vector<su2double>& val_vars,
+                                            su2double val_x, su2double val_y, const string& name_x,
+                                            const string& name_y) {
   vector<su2double*> look_up_data;
 
   for (long unsigned int i_var = 0; i_var < val_vars.size(); ++i_var) {
     look_up_data.push_back(&val_vars[i_var]);
   }
 
-  unsigned long exit_code = LookUp_ProgEnth(val_names_var, look_up_data, val_prog, val_enth, name_prog, name_enth);
+  unsigned long exit_code = LookUp_XY(val_names_var, look_up_data, val_x, val_y, name_x, name_y);
 
   return exit_code;
 }
 
-unsigned long CLookUpTable::LookUp_ProgEnth(const vector<string>& val_names_var, vector<su2double*>& val_vars,
-                                            su2double val_prog, su2double val_enth, const string& name_prog,
-                                            const string& name_enth) {
+unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vector<su2double*>& val_vars,
+                                            su2double val_x, su2double val_y, const string& name_x,
+                                            const string& name_y) {
   unsigned long exit_code = 0;
   unsigned long nearest_neighbor = 0;
   unsigned long id_triangle;
   std::array<su2double,3> interp_coeffs{0};
   std::array<unsigned long,3> triangle{0};
 
-  /* check if progress variable value is in progress variable table range
-   * and if enthalpy is in enthalpy table range */
-  if (val_prog >= limits_table_prog[0] && val_prog <= limits_table_prog[1] && val_enth >= limits_table_enth[0] &&
-      val_enth <= limits_table_enth[1]) {
-    /* if so, try to find the triangle that holds the (prog, enth) point */
-    id_triangle = trap_map_prog_enth.GetTriangle(val_prog, val_enth);
+  /* check if x value is in x table range
+   * and if y is in y table range */
+  if (val_x >= limits_table_x[0] && val_x <= limits_table_x[1] && val_y >= limits_table_y[0] &&
+      val_y <= limits_table_y[1]) {
+    /* if so, try to find the triangle that holds the (x, y) point */
+    id_triangle = trap_map_x_y.GetTriangle(val_x, val_y);
 
     /* check if point is inside a triangle (if table domain is non-rectangular,
      * the previous range check might be true but the point could still be outside of the domain) */
-    if (IsInTriangle(val_prog, val_enth, id_triangle, name_prog, name_enth)) {
+    if (IsInTriangle(val_x, val_y, id_triangle, name_x, name_y)) {
       /* if so, get interpolation coefficients for point in  the triangle */
-      GetInterpCoeffs(val_prog, val_enth, interp_mat_inv_prog_enth[id_triangle], interp_coeffs);
+      GetInterpCoeffs(val_x, val_y, interp_mat_inv_x_y[id_triangle], interp_coeffs);
 
       /* exit_code 0 means point was in triangle */
       exit_code = 0;
 
     } else {
       /* if point is not inside a triangle (outside table domain) search nearest neighbor */
-      nearest_neighbor = FindNearestNeighborOnHull(val_prog, val_enth, name_prog, name_enth);
+      nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, name_x, name_y);
       exit_code = 1;
     }
 
   } else {
     /* if point is outside of table ranges, find nearest neighbor */
-    nearest_neighbor = FindNearestNeighborOnHull(val_prog, val_enth, name_prog, name_enth);
+    nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, name_x, name_y);
     exit_code = 1;
   }
 
@@ -433,27 +433,27 @@ su2double CLookUpTable::Interpolate(const su2double* val_samples, std::array<uns
   return result;
 }
 
-unsigned long CLookUpTable::FindNearestNeighborOnHull(su2double val_prog, su2double val_enth, const string& name_prog,
-                                                      const string& name_enth) {
+unsigned long CLookUpTable::FindNearestNeighborOnHull(su2double val_x, su2double val_y, const string& name_x,
+                                                      const string& name_y) {
   su2double min_distance = 1.e99;
   su2double next_distance = 1.e99;
-  su2double next_prog_norm;
-  su2double next_enth_norm;
+  su2double next_x_norm;
+  su2double next_y_norm;
   unsigned long neighbor_id = 0;
 
-  const su2double* prog_table = GetDataP(name_prog);
-  const su2double* enth_table = GetDataP(name_enth);
+  const su2double* x_table = GetDataP(name_x);
+  const su2double* y_table = GetDataP(name_y);
 
-  su2double norm_coeff_prog = 1. / (limits_table_prog[1] - limits_table_prog[0]);
-  su2double norm_coeff_enth = 1. / (limits_table_enth[1] - limits_table_enth[0]);
-  su2double val_prog_norm = val_prog / (limits_table_prog[1] - limits_table_prog[0]);
-  su2double val_enth_norm = val_enth / (limits_table_enth[1] - limits_table_enth[0]);
+  su2double norm_coeff_x = 1. / (limits_table_x[1] - limits_table_x[0]);
+  su2double norm_coeff_y = 1. / (limits_table_y[1] - limits_table_y[0]);
+  su2double val_x_norm = val_x / (limits_table_x[1] - limits_table_x[0]);
+  su2double val_y_norm = val_y / (limits_table_y[1] - limits_table_y[0]);
 
   for (unsigned long i_point = 0; i_point < n_hull_points; ++i_point) {
-    next_prog_norm = prog_table[hull[i_point]] * norm_coeff_prog;
-    next_enth_norm = enth_table[hull[i_point]] * norm_coeff_enth;
+    next_x_norm = x_table[hull[i_point]] * norm_coeff_x;
+    next_y_norm = y_table[hull[i_point]] * norm_coeff_y;
 
-    next_distance = sqrt(pow(val_prog_norm - next_prog_norm, 2) + pow(val_enth_norm - next_enth_norm, 2));
+    next_distance = sqrt(pow(val_x_norm - next_x_norm, 2) + pow(val_y_norm - next_y_norm, 2));
 
     if (next_distance < min_distance) {
       min_distance = next_distance;
@@ -463,22 +463,22 @@ unsigned long CLookUpTable::FindNearestNeighborOnHull(su2double val_prog, su2dou
   return neighbor_id;
 }
 
-bool CLookUpTable::IsInTriangle(su2double val_prog, su2double val_enth, unsigned long val_id_triangle, const string& name_prog,
-                                const string& name_enth) {
-  su2double tri_prog_0 = GetDataP(name_prog)[triangles[val_id_triangle][0]];
-  su2double tri_enth_0 = GetDataP(name_enth)[triangles[val_id_triangle][0]];
+bool CLookUpTable::IsInTriangle(su2double val_x, su2double val_y, unsigned long val_id_triangle, const string& name_x,
+                                const string& name_y) {
+  su2double tri_x_0 = GetDataP(name_x)[triangles[val_id_triangle][0]];
+  su2double tri_y_0 = GetDataP(name_y)[triangles[val_id_triangle][0]];
 
-  su2double tri_prog_1 = GetDataP(name_prog)[triangles[val_id_triangle][1]];
-  su2double tri_enth_1 = GetDataP(name_enth)[triangles[val_id_triangle][1]];
+  su2double tri_x_1 = GetDataP(name_x)[triangles[val_id_triangle][1]];
+  su2double tri_y_1 = GetDataP(name_y)[triangles[val_id_triangle][1]];
   
-  su2double tri_prog_2 = GetDataP(name_prog)[triangles[val_id_triangle][2]];
-  su2double tri_enth_2 = GetDataP(name_enth)[triangles[val_id_triangle][2]];
+  su2double tri_x_2 = GetDataP(name_x)[triangles[val_id_triangle][2]];
+  su2double tri_y_2 = GetDataP(name_y)[triangles[val_id_triangle][2]];
 
-  su2double area_tri = TriArea(tri_prog_0, tri_enth_0, tri_prog_1, tri_enth_1, tri_prog_2, tri_enth_2);
+  su2double area_tri = TriArea(tri_x_0, tri_y_0, tri_x_1, tri_y_1, tri_x_2, tri_y_2);
 
-  su2double area_0 = TriArea(val_prog, val_enth, tri_prog_1, tri_enth_1, tri_prog_2, tri_enth_2);
-  su2double area_1 = TriArea(tri_prog_0, tri_enth_0, val_prog, val_enth, tri_prog_2, tri_enth_2);
-  su2double area_2 = TriArea(tri_prog_0, tri_enth_0, tri_prog_1, tri_enth_1, val_prog, val_enth);
+  su2double area_0 = TriArea(val_x, val_y, tri_x_1, tri_y_1, tri_x_2, tri_y_2);
+  su2double area_1 = TriArea(tri_x_0, tri_y_0, val_x, val_y, tri_x_2, tri_y_2);
+  su2double area_2 = TriArea(tri_x_0, tri_y_0, tri_x_1, tri_y_1, val_x, val_y);
 
   return (abs(area_tri - (area_0 + area_1 + area_2)) < area_tri * 1e-10);
 }

From 73895efb50aa72fe6b92c821f53cb340d044ef54 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 21 Nov 2022 19:28:45 +0100
Subject: [PATCH 043/656] Added third dimension to CLookUpTable class, changed
 method names in CLookupTable_tests

---
 Common/include/containers/CFileReaderLUT.hpp  |  29 +-
 Common/include/containers/CLookUpTable.hpp    | 132 +++++---
 Common/src/containers/CFileReaderLUT.cpp      | 120 +++++--
 Common/src/containers/CLookUpTable.cpp        | 313 ++++++++++++------
 .../Common/containers/CLookupTable_tests.cpp  |  10 +-
 5 files changed, 403 insertions(+), 201 deletions(-)

diff --git a/Common/include/containers/CFileReaderLUT.hpp b/Common/include/containers/CFileReaderLUT.hpp
index a000b2ddc60..37b6f7a4aaa 100644
--- a/Common/include/containers/CFileReaderLUT.hpp
+++ b/Common/include/containers/CFileReaderLUT.hpp
@@ -42,11 +42,13 @@ class CFileReaderLUT {
  protected:
   int rank;
 
+  unsigned short table_dim = 2;
   std::string version_lut;
   std::string version_reader;
-  unsigned long n_points;
-  unsigned long n_triangles;
-  unsigned long n_hull_points;
+  unsigned long n_levels = 1;
+  unsigned long *n_points;
+  unsigned long *n_triangles;
+  unsigned long *n_hull_points;
   unsigned long n_variables;
 
   /*! \brief Holds the variable names stored in the table file. 
@@ -57,11 +59,11 @@ class CFileReaderLUT {
   /*! \brief Holds all data stored in the table. 
    * First index addresses the variable while second index addresses the point.
    */
-  su2activematrix table_data;
+  su2activematrix *table_data;
 
-  su2matrix<unsigned long> triangles;
+  su2matrix<unsigned long> *triangles;
 
-  std::vector<unsigned long> hull;
+  std::vector<unsigned long> *hull;
 
   /*! \brief Searches for the position of flag in file_stream and 
    *         sets the stream position of file_stream to that position.
@@ -82,18 +84,21 @@ class CFileReaderLUT {
   
   inline const std::string& GetVersionLUT() const { return version_lut; }
   inline const std::string& GetVersionReader() const { return version_reader; }
-  inline unsigned long GetNPoints() const { return n_points; }
-  inline unsigned long GetNTriangles() const { return n_triangles; }
-  inline unsigned long GetNHullPoints() const { return n_hull_points; }
+  inline unsigned long GetNPoints(std::size_t i_level=0) const { return n_points[i_level]; }
+  inline unsigned long GetNTriangles(std::size_t i_level=0) const { return n_triangles[i_level]; }
+  inline unsigned long GetNHullPoints(std::size_t i_level=0) const { return n_hull_points[i_level]; }
   inline unsigned long GetNVariables() const { return n_variables; }
+  inline unsigned long GetNLevels() const { return n_levels; }
 
   inline const std::vector<std::string>& GetNamesVar() const { return names_var; }
 
-  inline const su2activematrix& GetTableData() const { return table_data; }
+  inline const su2activematrix& GetTableData(std::size_t i_level=0) const { return table_data[i_level]; }
 
-  inline const su2matrix<unsigned long>& GetTriangles() const { return triangles; };
+  inline const su2matrix<unsigned long>& GetTriangles(std::size_t i_level=0) const { return triangles[i_level]; }
 
-  inline const std::vector<unsigned long>& GetHull() const { return hull; };
+  inline const std::vector<unsigned long>& GetHull(std::size_t i_level=0) const { return hull[i_level]; }
+
+  inline const unsigned short GetTableDim() const { return table_dim; }
 
   void ReadRawLUT(const std::string& file_name);
 };
diff --git a/Common/include/containers/CLookUpTable.hpp b/Common/include/containers/CLookUpTable.hpp
index 1d93cdea516..3dcfceb0d51 100644
--- a/Common/include/containers/CLookUpTable.hpp
+++ b/Common/include/containers/CLookUpTable.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file CLookupTable.hpp
  * \brief tabulation of fluid properties
- * \author D. Mayer, T. Economon
+ * \author D. Mayer, T. Economon, E.C.Bunschoten
  * \version 7.4.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
@@ -47,16 +47,19 @@ class CLookUpTable {
   std::string file_name_lut;
   std::string version_lut;
   std::string version_reader;
-  unsigned long n_points;
-  unsigned long n_triangles;
+  unsigned long *n_points;
+  unsigned long *n_triangles;
   unsigned long n_variables;
-  unsigned long n_hull_points;
+  unsigned long *n_hull_points;
+  unsigned long n_table_levels = 1;
+  su2double *z_values_levels;
 
   /*! 
-   * \brief the lower and upper limits of the y and x.
+   * \brief the lower and upper limits of the z, y and x variable.
    */
-  su2double limits_table_y[2];
-  su2double limits_table_x[2];
+  std::pair<su2double, su2double> limits_table_z;
+  std::pair<su2double, su2double> *limits_table_y;
+  std::pair<su2double, su2double> *limits_table_x;
 
   /*! \brief Holds the variable names stored in the table file.
    * Order is in sync with data
@@ -67,25 +70,25 @@ class CLookUpTable {
    * Holds all data stored in the table. First index addresses the variable
    * while second index addresses the point.
    */
-  su2activematrix table_data;
+  su2activematrix *table_data;
 
-  su2matrix<unsigned long> triangles;
+  su2matrix<unsigned long> *triangles;
 
   /* we do not know this size in advance until we go through the entire lookup table */
-  std::vector<std::vector<unsigned long> > edges;
-  std::vector<std::vector<unsigned long> > edge_to_triangle;
+  std::vector<std::vector<unsigned long> > *edges;
+  std::vector<std::vector<unsigned long> > *edge_to_triangle;
 
   /*! \brief 
    * The hull contains the boundary of the lookup table.
    */
-  std::vector<unsigned long> hull;
+  std::vector<unsigned long> *hull;
 
-  CTrapezoidalMap trap_map_x_y;
+  CTrapezoidalMap *trap_map_x_y;
 
   /*! \brief 
    * vector of all the weight factors for the interpolation.
    */
-  std::vector<su2activematrix> interp_mat_inv_x_y;
+  std::vector<su2activematrix> *interp_mat_inv_x_y;
 
   /*! \brief 
    * returns the index to the variable in the lookup table.
@@ -106,13 +109,13 @@ class CLookUpTable {
    * \brief Get the pointer to the column data of the table (density, temperature, source terms, ...).
    * \returns pointer to the column data.
    */
-  inline const su2double* GetDataP(const std::string& name_var) const {
-    return table_data[GetIndexOfVar(name_var)];
+  inline const su2double* GetDataP(const std::string& name_var, unsigned long i_level=0) const {
+    return table_data[i_level][GetIndexOfVar(name_var)];
   }
 
   /*!
    * \brief find the table limits, i.e. the minimum and maximum values of the 2 independent.
-   * controlling variables (x and y). We put the values in the variables.
+   * controlling variables. We put the values in the variables.
    * limits_table_x[2] and limit_table_y[2].
    * \param[in] name_x - the string name for the first controlling variable.
    * \param[in] name_y - the string name of the second controlling variable.
@@ -131,16 +134,16 @@ class CLookUpTable {
   void LoadTableRaw(const std::string& file_name_lut);
 
   /*!
-   * \brief compute vector of all (inverse) interpolation coefficients "interp_mat_inv_prog_enth" of all triangles.
-   * \param[in] name_prog - the string name of the first controlling variable (x).
-   * \param[in] name_enth - the string name of the second controlling variable (y).
+   * \brief compute vector of all (inverse) interpolation coefficients "interp_mat_inv_x_y" of all triangles.
+   * \param[in] name_x - the string name of the first controlling variable.
+   * \param[in] name_y - the string name of the second controlling variable.
   */
   void ComputeInterpCoeffs(const std::string& name_x, const std::string& name_y);
 
   /*!
    * \brief compute the inverse matrix for interpolation.
-   * \param[in] vec_x - pointer to first coordinate (x).
-   * \param[in] vec_y - pointer to second coordinate (y).
+   * \param[in] vec_x - pointer to first coordinate (progress variable).
+   * \param[in] vec_y - pointer to second coordinate (enthalpy).
    * \param[in] point_ids - single triangle data.
    * \param[out] interp_mat_inv - inverse matrix for interpolation.
   */
@@ -149,8 +152,8 @@ class CLookUpTable {
 
   /*!
    * \brief compute the interpolation coefficients for the triangular interpolation.
-   * \param[in] val_x - value of first coordinate (x).
-   * \param[in] val_y - value of second coordinate (y).
+   * \param[in] val_x - value of first coordinate (progress variable).
+   * \param[in] val_y - value of second coordinate (enthalpy).
    * \param[in] interp_mat_inv - inverse matrix for interpolation.
    * \param[out] interp_coeffs - interpolation coefficients.
   */
@@ -167,27 +170,29 @@ class CLookUpTable {
   su2double Interpolate(const su2double* val_samples, std::array<unsigned long,3>& val_triangle,
                         std::array<su2double,3>& val_interp_coeffs);
 
+  void Linear_Interpolation(su2double val_z, std::pair<unsigned long, unsigned long> &inclusion_levels, std::vector<su2double>&lower_values,std::vector<su2double>&upper_values, std::vector<su2double*>&var_vals);
+
   /*!
    * \brief find the point on the hull (boundary of the table) that is closest to the point P(val_x,val_y).
    * \param[in] val_x - first coordinate of point P(val_x,val_y) to check.
    * \param[in] val_y - second coordinate of point P(val_x,val_y) to check.
-   * \param[in] name_prog - string name of the first controlling variable.
-   * \param[in] name_enth - string name of the second controlling variable.
+   * \param[in] name_x - string name of the first controlling variable.
+   * \param[in] name_y - string name of the second controlling variable.
    * \returns point id of the nearest neighbor on the hull.
    */
-  unsigned long FindNearestNeighborOnHull(su2double val_x, su2double val_y, const std::string& name_x, const std::string& name_y);
+  unsigned long FindNearestNeighborOnHull(su2double val_x, su2double val_y, const std::string& name_x, const std::string& name_y, unsigned long i_level=0);
 
   /*!
    * \brief determine if a point P(val_x,val_y) is inside the triangle val_id_triangle.
    * \param[in] val_x - first coordinate of point P(val_x,val_y) to check.
    * \param[in] val_y - second coordinate of point P(val_x,val_y) to check.
    * \param[in] val_id_triangle - ID of the triangle to check.
-   * \param[in] name_prog - string name of the first controlling variable.
-   * \param[in] name_enth - string name of the second controlling variable.
+   * \param[in] name_x - string name of the first controlling variable.
+   * \param[in] name_y - string name of the second controlling variable.
    * \returns true if the point is in the triangle, false if it is outside.
    */
   bool IsInTriangle(su2double val_x, su2double val_y, unsigned long val_id_triangle, const std::string& name_x,
-                    const std::string& name_y);
+                    const std::string& name_y, unsigned long i_level=0);
 
   /*!
    * \brief compute the area of a triangle given the 3 points of the triangle.
@@ -205,7 +210,7 @@ class CLookUpTable {
 
  public:
   CLookUpTable(const std::string& file_name_lut, const std::string& name_x, const std::string& name_y);
-
+  ~CLookUpTable();
 
   /*!
    * \brief print information to screen.
@@ -213,60 +218,79 @@ class CLookUpTable {
   void PrintTableInfo();
 
   /*!
-   * \brief lookup 1 value of the single variable "val_name_var" using controlling variable values(val_prog,val_enth)
-   *  whose controlling variable names are "name_x" and "name_y".
+   * \brief lookup 1 value of the single variable "val_name_var" using controlling variable values(val_x,val_y)
+   *  whose controlling variable names are "name_prog" and "name_enth".
    * \param[in] val_name_var - string name of the variable to look up.
    * \param[out] val_var - the stored value of the variable to look up.
-   * \param[in] val_x - value of controlling variable 1 (x).
-   * \param[in] val_y - value of controlling variable 2 (y).
-   * \param[in] name_x - string name of controlling variable 1 (x).
-   * \param[in] name_y - string name of controlling variable 2 (y).
+   * \param[in] val_x - value of controlling variable 1.
+   * \param[in] val_y - value of controlling variable 2.
+   * \param[in] name_x - string name of controlling variable 1.
+   * \param[in] name_y - string name of controlling variable 2.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
   unsigned long LookUp_XY(const std::string& val_name_var, su2double* val_var, su2double val_x, su2double val_y,
-                                const std::string& name_x, const std::string& name_y);
+                                const std::string& name_x, const std::string& name_y, unsigned long i_level=0);
 
   /*!
    * \brief lookup 1 value for each of the variables in "val_name_var" using controlling variable values(val_x,val_y)
    *  whose controlling variable names are "name_x" and "name_y".
    * \param[in] val_names_var - vector of string names of the variables to look up.
    * \param[out] val_vars - pointer to the vector of stored values of the variables to look up.
-   * \param[in] val_x - value of controlling variable 1 (x).
-   * \param[in] val_y - value of controlling variable 2 (y).
-   * \param[in] name_x - string name of controlling variable 1 (x).
-   * \param[in] name_y - string name of controlling variable 2 (y).
+   * \param[in] val_x - value of controlling variable 1.
+   * \param[in] val_y - value of controlling variable 2.
+   * \param[in] name_x - string name of controlling variable 1.
+   * \param[in] name_y - string name of controlling variable 2.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
   unsigned long LookUp_XY(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars, su2double val_x,
-                                su2double val_y, const std::string& name_x, const std::string& name_y);
+                                su2double val_y, const std::string& name_x, const std::string& name_y, unsigned long i_level=0);
 
   /*!
    * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_x,val_y)
    *  whose controlling variable names are "name_x" and "name_y".
    * \param[in] val_name_var - string name of the variable to look up.
    * \param[out] val_var - the stored value of the variable to look up.
-   * \param[in] val_x - value of controlling variable 1 (x).
-   * \param[in] val_y - value of controlling variable 2 (y).
-   * \param[in] name_x - string name of controlling variable 1 (x).
-   * \param[in] name_y - string name of controlling variable 2 (y).
+   * \param[in] val_x - value of controlling variable 1.
+   * \param[in] val_y - value of controlling variable 2.
+   * \param[in] name_x - string name of controlling variable 1.
+   * \param[in] name_y - string name of controlling variable 2.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
   unsigned long LookUp_XY(const std::vector<std::string>& val_names_var, std::vector<su2double>& val_vars, su2double val_x,
-                                su2double val_y, const std::string& name_x, const std::string& name_y);
+                                su2double val_y, const std::string& name_x, const std::string& name_y, unsigned long i_level=0);
+
+  /*!
+   * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_x,val_y,val_z)
+   *  whose controlling variable names are "name_x" and "name_y".
+   * \param[in] val_name_var - string name of the variable to look up.
+   * \param[out] val_var - the stored value of the variable to look up.
+   * \param[in] val_x - value of controlling variable 1.
+   * \param[in] val_y - value of controlling variable 2.
+   * \param[in] name_x - string name of controlling variable 1.
+   * \param[in] name_y - string name of controlling variable 2.
+   * \param[in] val_z - value of controlling variable 3.
+   * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
+   */
+  unsigned long LookUp_XYZ(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars, su2double val_x,
+                                su2double val_y, const std::string& name_x, const std::string& name_y, su2double val_z=0);
+  
+  std::pair<unsigned long, unsigned long> FindInclusionLevels(su2double val_z, bool *within_limits);
 
   /*!
-   * \brief determine the minimum and maximum value of the y (controlling variable 2).
+   * \brief determine the minimum and maximum value of the second controlling variable.
    * \returns pair of minimum and maximum value of controlling variable 2.
    */
-  inline std::pair<su2double, su2double> GetTableLimitsY() const {
-    return std::make_pair(limits_table_y[0], limits_table_y[1]);
+  inline std::pair<su2double, su2double> GetTableLimitsY(unsigned long i_level = 0) const {
+    return limits_table_y[i_level];
   }
 
   /*!
-   * \brief determine the minimum and maximum value of the x (controlling variable 1).
+   * \brief determine the minimum and maximum value of the first controlling variable.
    * \returns pair of minimum and maximum value of controlling variable 1.
    */
-  inline std::pair<su2double, su2double> GetTableLimitsX() const {
-    return std::make_pair(limits_table_x[0], limits_table_x[1]);
+  inline std::pair<su2double, su2double> GetTableLimitsX(unsigned long i_level = 0) const {
+    return limits_table_x[i_level];
   }
+
+  
 };
diff --git a/Common/src/containers/CFileReaderLUT.cpp b/Common/src/containers/CFileReaderLUT.cpp
index 081293eded1..4e9e6b013d2 100644
--- a/Common/src/containers/CFileReaderLUT.cpp
+++ b/Common/src/containers/CFileReaderLUT.cpp
@@ -59,31 +59,64 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
 
   /*--- Read header ---*/
   SkipToFlag(file_stream, line, "<Header>");
-
+  table_dim = 2;
+  bool found_level_count = false;
   while (GetNextNonEmptyLine(file_stream, line) && !eoHeader) {
 
     /*--- number of points in LUT ---*/
     if (line.compare("[Version]") == 0) {
       GetNextNonEmptyLine(file_stream, line);
       version_lut = line;
+
+      if(version_lut.compare("1.0.0") == 0){
+        table_dim = 2;
+        n_levels = 1;
+        found_level_count = true;
+      }
+      if(version_lut.compare("1.1.0") == 0){
+        table_dim = 3;
+      }
+    }
+
+    if (line.compare("[Number of table levels]") == 0)
+    {
+      found_level_count = true;
+      GetNextNonEmptyLine(file_stream, line);
+      n_levels = stoul(line);
+      
+      n_points      = new unsigned long[n_levels];
+      n_triangles   = new unsigned long[n_levels];
+      n_hull_points = new unsigned long[n_levels];
     }
 
     /*--- number of points in LUT ---*/
     if (line.compare("[Number of points]") == 0) {
-      GetNextNonEmptyLine(file_stream, line);
-      n_points = stoi(line);
+      if(!found_level_count)
+        SU2_MPI::Error("Number of points provided before specifying level count.", CURRENT_FUNCTION);
+      for(unsigned long i_level=0; i_level<n_levels; i_level){
+        GetNextNonEmptyLine(file_stream, line);
+        n_points[i_level] = stoi(line);
+      }
     }
 
     /*--- number of triangles in LUT ---*/
     if (line.compare("[Number of triangles]") == 0) {
-      GetNextNonEmptyLine(file_stream, line);
-      n_triangles = stoi(line);
+      if(!found_level_count)
+        SU2_MPI::Error("Number of triangles provided before specifying level count.", CURRENT_FUNCTION);
+      for(unsigned long i_level=0; i_level<n_levels; i_level){
+        GetNextNonEmptyLine(file_stream, line);
+        n_triangles[i_level] = stoi(line);
+      }
     }
 
     /*--- number of points on the hull ---*/
     if (line.compare("[Number of hull points]") == 0) {
-      GetNextNonEmptyLine(file_stream, line);
-      n_hull_points = stoi(line);
+      if(!found_level_count)
+        SU2_MPI::Error("Number of hull points provided before specifying level count.", CURRENT_FUNCTION);
+      for(unsigned long i_level=0; i_level<n_levels; i_level){
+        GetNextNonEmptyLine(file_stream, line);
+        n_hull_points[i_level] = stoi(line);
+      }
     }
 
     /*--- number of variables in LUT ---*/
@@ -112,11 +145,14 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
     SU2_MPI::Error("Version conflict between LUT reader and LUT library file.", CURRENT_FUNCTION);
 
   /*--- check header quantities ---*/
-  if (n_points == 0 || n_triangles == 0 || n_variables == 0 || n_hull_points == 0)
+  for(unsigned long i_level=0; i_level < n_levels; i_level++){
+    if (n_points[i_level] == 0 || n_triangles[i_level] == 0 || n_variables == 0 || n_hull_points[i_level] == 0)
     SU2_MPI::Error(
         "Number of points, triangles, hull points, or variables in lookup table "
         "library header is zero.",
         CURRENT_FUNCTION);
+  }
+  
 
   /*--- check if number of variables is consistent ---*/
   if (n_variables != names_var.size())
@@ -128,13 +164,19 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
 
   /*--- now that n_variables, n_points, n_hull_points and n_variables are available, allocate memory ---*/
   if (rank == MASTER_NODE) cout << "allocating memory for the data, size = ( " << GetNVariables() << " , " << GetNPoints() << " )" << endl;
-  table_data.resize(GetNVariables(), GetNPoints());
+  table_data = new su2activematrix[n_levels];
+  for(unsigned long i_level=0; i_level<n_levels; i_level++)
+    table_data[i_level].resize(GetNVariables(), GetNPoints(i_level));
 
   if (rank == MASTER_NODE) cout << "allocating memory for the triangles, size = "<< GetNTriangles() << endl;
-  triangles.resize(GetNTriangles(), 3);
+  triangles = new su2matrix<unsigned long>[n_levels];
+  for(unsigned long i_level=0; i_level<n_levels; i_level++)
+    triangles[i_level].resize(GetNTriangles(i_level), 3);
 
   if (rank == MASTER_NODE) cout << "allocating memory for the hull points, size = " << GetNHullPoints() << endl;
-  hull.resize(GetNHullPoints());
+  hull = new vector<unsigned long>[n_levels];
+  for(unsigned long i_level=0; i_level<n_levels; i_level++)
+    hull[i_level].resize(GetNHullPoints(i_level));
 
   /*--- flush any cout ---*/
   if (rank == MASTER_NODE) cout << endl;
@@ -143,38 +185,52 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
   if (rank == MASTER_NODE) cout << "loading data block" << endl;
 
   SkipToFlag(file_stream, line, "<Data>");
-
+  unsigned long i_level = 0;
+  bool eoLevel = false;
   unsigned long pointCounter = 0;
+  unsigned long levelCounter = 0;
   while (GetNextNonEmptyLine(file_stream, line) && !eoData) {
 
     /*--- check if end of data is reached ---*/
     if (line.compare("</Data>") == 0) eoData = true;
 
     if (!eoData) {
-      /*--- one line contains values for one point for all variables ---*/
-      istringstream streamDataLine(line);
-
-      /*--- add next line to table array ---*/
-      for (unsigned long iVar = 0; iVar < n_variables; iVar++) {
-        streamDataLine >> word;
-        passivedouble tmp = stod(word);
-        table_data[iVar][pointCounter] = (su2double)tmp;
+      if(line.compare("<Level>") == 0){
+        eoLevel = false;
+        pointCounter = 0;
+        GetNextNonEmptyLine(file_stream, line);
+      }
+      if(line.compare("</Level>") == 0){
+        eoLevel = true;
+        if (n_points[levelCounter] != pointCounter - 1)
+        SU2_MPI::Error(
+            "Number of read points on level " + std::to_string(levelCounter) + " does not match number of points "
+            "specified in lookup table library header.",
+            CURRENT_FUNCTION);
+        levelCounter++;
+      }
+      if(!eoLevel || (table_dim == 2)){
+        /*--- one line contains values for one point for all variables ---*/
+        istringstream streamDataLine(line);
+
+        /*--- add next line to table array ---*/
+        for (unsigned long iVar = 0; iVar < n_variables; iVar++) {
+          streamDataLine >> word;
+          passivedouble tmp = stod(word);
+          table_data[levelCounter][iVar][pointCounter] = (su2double)tmp;
+        }
+        pointCounter++;
       }
     }
-    pointCounter++;
   }
 
-  if (n_points != pointCounter - 1)
-    SU2_MPI::Error(
-        "Number of read points does not match number of points "
-        "specified in lookup table library header.",
-        CURRENT_FUNCTION);
+  
 
   /*--- read connectivity ---*/
   if (rank == MASTER_NODE) cout << "loading connectivity block" << endl;
 
   SkipToFlag(file_stream, line, "<Connectivity>");
-
+  i_level = 0;
   unsigned long triCounter = 0;
   while (GetNextNonEmptyLine(file_stream, line) && !eoConnectivity) {
     if (!line.empty() && (line[line.length()-1] == '\n' || line[line.length()-1] == '\r' )) {
@@ -193,13 +249,13 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
         streamTriLine >> word;
 
         /*--- lookup table index starts with 1, convert to c++ indexing starting with 0: ---*/
-        triangles[triCounter][iPoint] = stol(word) - 1;
+        triangles[i_level][triCounter][iPoint] = stol(word) - 1;
       }
     }
     triCounter++;
   }
 
-  if (n_triangles != triCounter - 1)
+  if (n_triangles[i_level] != triCounter - 1)
     SU2_MPI::Error(
         "Number of read triangles does not match number of points "
         "specified in lookup table library header.",
@@ -209,7 +265,7 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
   if (rank == MASTER_NODE) cout << "loading hull block" << endl;
 
   SkipToFlag(file_stream, line, "<Hull>");
-
+  i_level = 0;
   unsigned long hullCounter = 0;
   while (GetNextNonEmptyLine(file_stream, line) && !eoHull) {
     if (!line.empty() && (line[line.length()-1] == '\n' || line[line.length()-1] == '\r' )) {
@@ -225,12 +281,12 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
       streamHullLine >> word;
 
       /*--- Lookup table indices start with 1, convert to c++ indexing starting with 0: ---*/
-      hull[hullCounter] = stol(word) - 1;
+      hull[i_level][hullCounter] = stol(word) - 1;
     }
     hullCounter++;
   }
 
-  if (n_hull_points != hullCounter - 1)
+  if (n_hull_points[i_level] != hullCounter - 1)
     SU2_MPI::Error(
         "Number of read hull points does not match number of points "
         "specified in lookup table library header.",
diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index 2f450268d9a..a64ebcfa7ab 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -1,7 +1,7 @@
 /*!
  * \file CLookupTable.cpp
  * \brief tabulation of fluid properties
- * \author D. Mayer, T. Economon
+ * \author D. Mayer, T. Economon, E.C.Bunschoten
  * \version 7.4.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
@@ -53,11 +53,12 @@ CLookUpTable::CLookUpTable(const string& var_file_name_lut, const string& name_x
   PrintTableInfo();
 
   if (rank == MASTER_NODE)
-    cout << "Building a trapezoidal map for the (x, y) "
+    cout << "Building a trapezoidal map for the (" + name_x + ", " + name_y + ") "
             "space ..."
          << endl;
-
-  trap_map_x_y = CTrapezoidalMap(GetDataP(name_x), GetDataP(name_y), table_data.cols(), edges, edge_to_triangle);
+  trap_map_x_y = new CTrapezoidalMap[n_table_levels];
+  for(auto i_level = 0ul; i_level<n_table_levels; i_level++)
+    trap_map_x_y[i_level] = CTrapezoidalMap(GetDataP(name_x, i_level), GetDataP(name_y, i_level), table_data[i_level].cols(), edges[i_level], edge_to_triangle[i_level]);
 
   if (rank == MASTER_NODE) 
     cout << " done." << endl;
@@ -72,6 +73,20 @@ CLookUpTable::CLookUpTable(const string& var_file_name_lut, const string& name_x
     cout << "LUT fluid model ready for use" << endl;
 }
 
+CLookUpTable::~CLookUpTable()
+{
+  delete [] trap_map_x_y;
+  delete [] n_points;
+  delete [] n_triangles;
+  delete [] n_hull_points;
+  delete [] table_data;
+  delete [] hull;
+  delete [] triangles;
+  delete [] interp_mat_inv_x_y;
+  delete [] edges;
+  delete [] edge_to_triangle;
+}
+
 void CLookUpTable::LoadTableRaw(const string& var_file_name_lut) {
   CFileReaderLUT file_reader;
 
@@ -79,35 +94,63 @@ void CLookUpTable::LoadTableRaw(const string& var_file_name_lut) {
     cout << "Loading lookup table, filename = " << var_file_name_lut << " ..." << endl;
 
   file_reader.ReadRawLUT(var_file_name_lut);
-
-  n_points = file_reader.GetNPoints();
-  n_triangles = file_reader.GetNTriangles();
+  unsigned short table_dim = file_reader.GetTableDim();
+  n_table_levels = file_reader.GetNLevels();
+
+  n_points            = new unsigned long[n_table_levels];
+  n_triangles         = new unsigned long[n_table_levels];
+  n_hull_points       = new unsigned long[n_table_levels];
+  table_data          = new su2activematrix[n_table_levels];
+  hull                = new std::vector<unsigned long>[n_table_levels];
+  triangles           = new su2matrix<unsigned long>[n_table_levels];
+  interp_mat_inv_x_y  = new std::vector<su2activematrix>[n_table_levels];
+  edges               = new std::vector<std::vector<unsigned long> >[n_table_levels];
+  edge_to_triangle    = new std::vector<std::vector<unsigned long> >[n_table_levels];
+
+  for(unsigned long i_level=0; i_level<n_table_levels; i_level++){
+    n_points[i_level] = file_reader.GetNPoints(i_level);
+    n_triangles[i_level] = file_reader.GetNTriangles(i_level);
+    n_hull_points[i_level] = file_reader.GetNHullPoints(i_level);
+    table_data[i_level] = file_reader.GetTableData(i_level);
+    triangles[i_level] = file_reader.GetTriangles(i_level);
+    hull[i_level] = file_reader.GetHull(i_level);
+  }
+  
   n_variables = file_reader.GetNVariables();
-  n_hull_points = file_reader.GetNHullPoints();
   version_lut = file_reader.GetVersionLUT();
   version_reader = file_reader.GetVersionReader();
   names_var = file_reader.GetNamesVar();
-  table_data = file_reader.GetTableData();
-  triangles = file_reader.GetTriangles();
-  hull = file_reader.GetHull();
 
+  if(table_dim == 3){
+    z_values_levels = new su2double[n_table_levels];
+    //TODO: fill in z-values from table reader.
+    //TODO: get minimum and maximum z-values from table reader.
+  }
   if (rank == MASTER_NODE) 
     cout << " done." << endl;
 }
 
 void CLookUpTable::FindTableLimits(const string& name_x, const string& name_y) {
-  int ixy = GetIndexOfVar(name_y);
-  int ixx = GetIndexOfVar(name_x);
+  int idx_X = GetIndexOfVar(name_x);
+  int idx_Y = GetIndexOfVar(name_y);
+  limits_table_x = new pair<su2double, su2double>[n_table_levels];
+  limits_table_y = new pair<su2double, su2double>[n_table_levels];
 
   /* we find the lowest and highest value of y and x in the table */
-  limits_table_y[0] = *min_element(&table_data[ixy][0], &table_data[ixy][0]+table_data.cols());
-  limits_table_y[1] = *max_element(&table_data[ixy][0], &table_data[ixy][0]+table_data.cols());
-  limits_table_x[0] = *min_element(&table_data[ixx][0], &table_data[ixx][0]+table_data.cols());
-  limits_table_x[1] = *max_element(&table_data[ixx][0], &table_data[ixx][0]+table_data.cols());
-
+  for(auto i_level=0u; i_level<n_table_levels; i_level++)
+  {
+    su2double min_x, max_x, min_y, max_y;
+    min_y = *min_element(&table_data[i_level][idx_Y][0], &table_data[i_level][idx_Y][0]+table_data[i_level].cols());
+    min_x = *min_element(&table_data[i_level][idx_X][0], &table_data[i_level][idx_X][0]+table_data[i_level].cols());
+    max_y = *max_element(&table_data[i_level][idx_Y][0], &table_data[i_level][idx_Y][0]+table_data[i_level].cols());
+    max_x = *max_element(&table_data[i_level][idx_X][0], &table_data[i_level][idx_X][0]+table_data[i_level].cols());
+    limits_table_x[i_level] = make_pair(min_x, max_x);
+    limits_table_y[i_level] = make_pair(min_y, max_y);
+  }
 }
 
 void CLookUpTable::PrintTableInfo() {
+  //TODO: make compatible with 3D table
   if (rank == MASTER_NODE) {
     cout << setfill(' ');
     cout << endl;
@@ -118,14 +161,14 @@ void CLookUpTable::PrintTableInfo() {
     cout << "| Table version:" << setw(50) << right << version_lut << " |" << endl;
     cout << "| Table reader version:" << setw(43) << right << version_reader << " |" << endl;
     cout << "| Number of variables:" << setw(44) << right << n_variables << " |" << endl;
-    cout << "| Number of points:" << setw(47) << right << n_points << " |" << endl;
-    cout << "| Number of triangles:" << setw(44) << right << n_triangles << " |" << endl;
-    cout << "| Number of edges:" << setw(48) << right << edges.size() << " |" << endl;
+    cout << "| Number of points:" << setw(47) << right << n_points[0] << " |" << endl;
+    cout << "| Number of triangles:" << setw(44) << right << n_triangles[0] << " |" << endl;
+    cout << "| Number of edges:" << setw(48) << right << edges[0].size() << " |" << endl;
     cout << "+------------------------------------------------------------------+" << endl;
-    cout << "| Minimum y:" << setw(47) << right << limits_table_y[0] << " |" << endl;
-    cout << "| Maximum y:" << setw(47) << right << limits_table_y[1] << " |" << endl;
-    cout << "| Minimum x:" << setw(38) << right << limits_table_x[0] << " |" << endl;
-    cout << "| Maximum x:" << setw(38) << right << limits_table_x[1] << " |" << endl;
+    cout << "| Minimum Y:" << setw(47) << right << limits_table_y[0].first << " |" << endl;
+    cout << "| Maximum Y:" << setw(47) << right << limits_table_y[0].second << " |" << endl;
+    cout << "| Minimum X:" << setw(38) << right << limits_table_x[0].first << " |" << endl;
+    cout << "| Maximum X:" << setw(38) << right << limits_table_x[0].second << " |" << endl;
     cout << "+------------------------------------------------------------------+" << endl;
     cout << "| Variable names:                                                  |" << endl;
     cout << "|                                                                  |" << endl;
@@ -141,17 +184,19 @@ void CLookUpTable::PrintTableInfo() {
 
 void CLookUpTable::IdentifyUniqueEdges() {
 
+  for(auto i_level=0u; i_level<n_table_levels; i_level++){
+
   /* loop through elements and store the vector of element IDs (neighbors)
      for each of the points in the table */
 
   vector<vector<unsigned long> > neighborElemsOfPoint;
   
-  neighborElemsOfPoint.resize(n_points);
-  for (unsigned long iElem = 0; iElem < n_triangles; iElem++) {
+  neighborElemsOfPoint.resize(n_points[i_level]);
+  for (unsigned long iElem = 0; iElem < n_triangles[i_level]; iElem++) {
     /* loop over 3 points per triangle */
     for (unsigned long iPoint = 0; iPoint < N_POINTS_TRIANGLE; iPoint++) {
       /* get the global ID of the current point */
-      const unsigned long GlobalIndex = triangles[iElem][iPoint];
+      const unsigned long GlobalIndex = triangles[i_level][iElem][iPoint];
 
       /* add the current element ID to the neighbor list for this point */
       neighborElemsOfPoint[GlobalIndex].push_back(iElem);
@@ -160,7 +205,7 @@ void CLookUpTable::IdentifyUniqueEdges() {
 
   /* remove duplicates from the neighboring element lists*/
   vector<unsigned long>::iterator vecIt;
-  for (unsigned long iPoint = 0; iPoint < n_points; iPoint++) {
+  for (unsigned long iPoint = 0; iPoint < n_points[i_level]; iPoint++) {
     /* sort neighboring elements for each point */
     sort(neighborElemsOfPoint[iPoint].begin(), neighborElemsOfPoint[iPoint].end());
 
@@ -174,13 +219,13 @@ void CLookUpTable::IdentifyUniqueEdges() {
   /* loop through all neighboring elements of each point and store
      the point IDs that are neighboring points */
   vector<vector<unsigned long> > neighborPointsOfPoint;
-  neighborPointsOfPoint.resize(n_points);
-  for (unsigned long iPoint = 0; iPoint < n_points; iPoint++) {
+  neighborPointsOfPoint.resize(n_points[i_level]);
+  for (unsigned long iPoint = 0; iPoint < n_points[i_level]; iPoint++) {
     for (unsigned long iElem = 0; iElem < neighborElemsOfPoint[iPoint].size(); iElem++) {
       /* loop over element points */
       for (unsigned long jPoint = 0; jPoint < N_POINTS_TRIANGLE; jPoint++) {
         /* get the global ID of the current point */
-        const unsigned long GlobalIndex = triangles[neighborElemsOfPoint[iPoint][iElem]][jPoint];
+        const unsigned long GlobalIndex = triangles[i_level][neighborElemsOfPoint[iPoint][iElem]][jPoint];
 
         /* add the current element ID to the neighbor list for this point */
         if (GlobalIndex != iPoint) neighborPointsOfPoint[iPoint].push_back(GlobalIndex);
@@ -189,7 +234,7 @@ void CLookUpTable::IdentifyUniqueEdges() {
   }
 
   /* remove duplicates from the neighboring points lists */
-  for (unsigned long iPoint = 0; iPoint < n_points; iPoint++) {
+  for (unsigned long iPoint = 0; iPoint < n_points[i_level]; iPoint++) {
     /* sort neighboring points for each point */
     sort(neighborPointsOfPoint[iPoint].begin(), neighborPointsOfPoint[iPoint].end());
 
@@ -205,7 +250,7 @@ void CLookUpTable::IdentifyUniqueEdges() {
      that the smaller global index is in the first position and the larger
      is in the second to make for a unique set, so there's no need to
      remove duplicates. */
-  for (unsigned long iPoint = 0; iPoint < n_points; iPoint++) {
+  for (unsigned long iPoint = 0; iPoint < n_points[i_level]; iPoint++) {
     for (unsigned long jPoint = 0; jPoint < neighborPointsOfPoint[iPoint].size(); jPoint++) {
       /* Store the neighbor index more clearly. */
       const unsigned long GlobalIndex = neighborPointsOfPoint[iPoint][jPoint];
@@ -215,53 +260,57 @@ void CLookUpTable::IdentifyUniqueEdges() {
         vector<unsigned long> edge(2);
         edge[0] = iPoint;
         edge[1] = GlobalIndex;
-        edges.push_back(edge);
+        edges[i_level].push_back(edge);
       }
     }
   }
 
+
   /* Loop over our edges data structure. For the first point in each
    pair, loop through the neighboring elements and store the two
    elements that contain the second point in the edge ('left' and 'right' of the edge). */
-  edge_to_triangle.resize(edges.size());
-  for (unsigned long iEdge = 0; iEdge < edges.size(); iEdge++) {
+  edge_to_triangle[i_level].resize(edges[i_level].size());
+  for (unsigned long iEdge = 0; iEdge < edges[i_level].size(); iEdge++) {
     /* Store the two points of the edge more clearly. */
-    const unsigned long iPoint = edges[iEdge][0];
-    const unsigned long jPoint = edges[iEdge][1];
+    const unsigned long iPoint = edges[i_level][iEdge][0];
+    const unsigned long jPoint = edges[i_level][iEdge][1];
 
     /* Loop over all neighboring elements to iPoint. */
     for (unsigned long iElem = 0; iElem < neighborElemsOfPoint[iPoint].size(); iElem++) {
       /* loop over 3 points per triangle */
       for (unsigned long kPoint = 0; kPoint < N_POINTS_TRIANGLE; kPoint++) {
         /* Get the global ID of the current point. */
-        const unsigned long GlobalIndex = triangles[neighborElemsOfPoint[iPoint][iElem]][kPoint];
+        const unsigned long GlobalIndex = triangles[i_level][neighborElemsOfPoint[iPoint][iElem]][kPoint];
 
         /* Add the current element ID to the neighbor list for this point. */
-        if (GlobalIndex == jPoint) edge_to_triangle[iEdge].push_back(neighborElemsOfPoint[iPoint][iElem]);
+        if (GlobalIndex == jPoint) edge_to_triangle[i_level][iEdge].push_back(neighborElemsOfPoint[iPoint][iElem]);
       }
     }
   }
+  }
 }
 
 void CLookUpTable::ComputeInterpCoeffs(const string& name_x, const string& name_y) {
-  /* build KD tree for y, x space */
+  for(auto i_level=0ul; i_level<n_table_levels; i_level++){
+    /* build KD tree for y, x space */
 
-  std::array<unsigned long, 3> next_triangle;
+    std::array<unsigned long, 3> next_triangle;
 
-  const su2double* x = GetDataP(name_x);
-  const su2double* y = GetDataP(name_y);
+    const su2double* val_x = GetDataP(name_x, i_level);
+    const su2double* val_y = GetDataP(name_y, i_level);
 
-  /* calculate weights for each triangle (basically a distance function) and
-   * build inverse interpolation matrices */
-  for (unsigned long i_triangle = 0; i_triangle < n_triangles; i_triangle++) {
+    /* calculate weights for each triangle (basically a distance function) and
+    * build inverse interpolation matrices */
+    for (unsigned long i_triangle = 0; i_triangle < n_triangles[i_level]; i_triangle++) {
 
-    for (int p = 0; p < 3; p++) {
-      next_triangle[p] = triangles[i_triangle][p];
-    }
+      for (int p = 0; p < 3; p++) {
+        next_triangle[p] = triangles[i_level][i_triangle][p];
+      }
 
-    su2activematrix x_interp_mat_inv(3, 3);
-    GetInterpMatInv(x, y, next_triangle, x_interp_mat_inv);
-    interp_mat_inv_x_y.push_back(x_interp_mat_inv);
+      su2activematrix x_interp_mat_inv(3, 3);
+      GetInterpMatInv(val_x, val_y, next_triangle, x_interp_mat_inv);
+      interp_mat_inv_x_y[i_level].push_back(x_interp_mat_inv);
+    }
   }
 }
 
@@ -291,8 +340,76 @@ void CLookUpTable::GetInterpMatInv(const su2double* vec_x, const su2double* vec_
 
 }
 
+std::pair<unsigned long, unsigned long> CLookUpTable::FindInclusionLevels(su2double val_z, bool*within_table_limits)
+{
+  std::pair<unsigned long, unsigned long> inclusion_levels;
+  if(val_z >= limits_table_z.second){
+    *within_table_limits = false;
+    inclusion_levels = std::make_pair(n_table_levels-1, n_table_levels-1);
+  }else if(val_z <= limits_table_z.first){
+    *within_table_limits = false;
+    inclusion_levels = std::make_pair(0, 0);
+  }else{
+    for(auto i_level = 0ul; i_level < n_table_levels-1; i_level++){
+      if((val_z >= z_values_levels[i_level]) && (val_z < z_values_levels[i_level+1])){
+        *within_table_limits = true;
+        inclusion_levels = std::make_pair(i_level, i_level+1);
+      }
+    }
+  }
+  return inclusion_levels;
+}
+
+unsigned long CLookUpTable::LookUp_XYZ(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars, su2double val_x,
+                                su2double val_y, const std::string& name_x, const std::string& name_y, su2double val_z)
+{
+  bool within_z_limits, exit_code;
+  unsigned long lower_level, upper_level;
+  std::pair<unsigned long, unsigned long> inclusion_levels;
+  if(val_z == 0){
+    inclusion_levels = std::make_pair(0, 0);
+    within_z_limits = false;
+  }else{
+    inclusion_levels = FindInclusionLevels(val_z, &within_z_limits);
+  }
+  
+  if(within_z_limits){
+    lower_level = inclusion_levels.first;
+    upper_level = inclusion_levels.second;
+    std::vector<su2double> val_vars_lower, val_vars_upper;
+    val_vars_lower.resize(val_vars.size());
+    val_vars_upper.resize(val_vars.size());
+    unsigned long exit_code_lower = LookUp_XY(val_names_var, val_vars_lower, val_x, val_y, name_x, name_y, lower_level);
+    unsigned long exit_code_upper = LookUp_XY(val_names_var, val_vars_upper, val_x, val_y, name_x, name_y, upper_level);
+
+    Linear_Interpolation(val_z, inclusion_levels, val_vars_lower, val_vars_upper, val_vars);
+
+    return max(exit_code_lower, exit_code_upper);
+  }else{
+    lower_level = inclusion_levels.first;
+    exit_code = LookUp_XY(val_names_var, val_vars, val_x, val_y, name_x, name_y, lower_level);
+    if( val_z == 0 ){
+      return exit_code;
+    }else{
+      return 1;
+    }
+  }
+}
+
+void CLookUpTable::Linear_Interpolation(su2double val_z, std::pair<unsigned long, unsigned long> &inclusion_levels, std::vector<su2double>&lower_values,std::vector<su2double>&upper_values, std::vector<su2double*>&var_vals)
+{
+  su2double val_z_lower = z_values_levels[inclusion_levels.first];
+  su2double val_z_upper = z_values_levels[inclusion_levels.second];
+  su2double factor_upper = (val_z - val_z_lower) / (val_z_upper - val_z_lower);
+  su2double factor_lower = (val_z_upper - val_z) / (val_z_upper - val_z_lower);
+
+  for(unsigned short iVar=0; iVar<var_vals.size(); iVar++){
+    *var_vals[iVar] = lower_values[iVar] * factor_lower + upper_values[iVar] * factor_upper;
+  }
+}
+
 unsigned long CLookUpTable::LookUp_XY(const string& val_name_var, su2double *val_var, su2double val_x,
-                                            su2double val_y, const string& name_x, const string& name_y) {
+                                            su2double val_y, const string& name_x, const string& name_y, unsigned long i_level) {
   unsigned long exit_code = 0;
 
   if (val_name_var.compare("NULL") == 0) {
@@ -302,34 +419,34 @@ unsigned long CLookUpTable::LookUp_XY(const string& val_name_var, su2double *val
   }
 
   /* check if x and y value is in table range */
-  if ((val_x >= limits_table_x[0] && val_x <= limits_table_x[1]) &&
-      (val_y >= limits_table_y[0] && val_y <= limits_table_y[1])){
+  if ((val_x >= limits_table_x[i_level].first && val_x <= limits_table_x[i_level].second) &&
+      (val_y >= limits_table_y[i_level].first && val_y <= limits_table_y[i_level].second)){
 
     /* find the triangle that holds the (x, y) point */
-    unsigned long id_triangle = trap_map_x_y.GetTriangle(val_x, val_y);
+    unsigned long id_triangle = trap_map_x_y[i_level].GetTriangle(val_x, val_y);
 
-    if (IsInTriangle(val_x, val_y, id_triangle, name_x, name_y)) {
+    if (IsInTriangle(val_x, val_y, id_triangle, name_x, name_y, i_level)) {
       /* get interpolation coefficients for point on triangle */
       std::array<su2double,3> interp_coeffs{0};
-      GetInterpCoeffs(val_x, val_y, interp_mat_inv_x_y[id_triangle], interp_coeffs);
+      GetInterpCoeffs(val_x, val_y, interp_mat_inv_x_y[i_level][id_triangle], interp_coeffs);
 
       /* first, copy the single triangle from the large triangle list*/
       std::array<unsigned long,3> triangle{0};
       for (int p = 0; p < 3; p++) 
-        triangle[p] = triangles[id_triangle][p]; 
+        triangle[p] = triangles[i_level][id_triangle][p]; 
 
       *val_var = Interpolate(GetDataP(val_name_var), triangle, interp_coeffs);
       exit_code = 0;
     } else {
       /* in bounding box but outside of table */
-      unsigned long nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, name_x, name_y);
-      *val_var = GetDataP(val_name_var)[nearest_neighbor];
+      unsigned long nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, name_x, name_y, i_level);
+      *val_var = GetDataP(val_name_var, i_level)[nearest_neighbor];
       exit_code = 1;
     }
   } else {
     /* lookup is outside of table bounding box */
-    unsigned long nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, name_x, name_y);
-    *val_var = GetDataP(val_name_var)[nearest_neighbor];
+    unsigned long nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, name_x, name_y, i_level);
+    *val_var = GetDataP(val_name_var, i_level)[nearest_neighbor];
     exit_code = 1;
   }
   return exit_code;
@@ -337,52 +454,52 @@ unsigned long CLookUpTable::LookUp_XY(const string& val_name_var, su2double *val
 
 unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vector<su2double>& val_vars,
                                             su2double val_x, su2double val_y, const string& name_x,
-                                            const string& name_y) {
+                                            const string& name_y, unsigned long i_level) {
   vector<su2double*> look_up_data;
 
   for (long unsigned int i_var = 0; i_var < val_vars.size(); ++i_var) {
     look_up_data.push_back(&val_vars[i_var]);
   }
 
-  unsigned long exit_code = LookUp_XY(val_names_var, look_up_data, val_x, val_y, name_x, name_y);
+  unsigned long exit_code = LookUp_XY(val_names_var, look_up_data, val_x, val_y, name_x, name_y, i_level);
 
   return exit_code;
 }
 
 unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vector<su2double*>& val_vars,
                                             su2double val_x, su2double val_y, const string& name_x,
-                                            const string& name_y) {
+                                            const string& name_y, unsigned long i_level) {
   unsigned long exit_code = 0;
   unsigned long nearest_neighbor = 0;
   unsigned long id_triangle;
   std::array<su2double,3> interp_coeffs{0};
   std::array<unsigned long,3> triangle{0};
 
-  /* check if x value is in x table range
-   * and if y is in y table range */
-  if (val_x >= limits_table_x[0] && val_x <= limits_table_x[1] && val_y >= limits_table_y[0] &&
-      val_y <= limits_table_y[1]) {
-    /* if so, try to find the triangle that holds the (x, y) point */
-    id_triangle = trap_map_x_y.GetTriangle(val_x, val_y);
+  /* check if x value is in table x-dimension range
+   * and if y is in table y-dimension table range */
+  if ((val_x >= limits_table_x[i_level].first && val_x <= limits_table_x[i_level].second) &&
+      (val_y >= limits_table_y[i_level].first && val_y <= limits_table_y[i_level].second)){
+    /* if so, try to find the triangle that holds the (prog, enth) point */
+    id_triangle = trap_map_x_y[i_level].GetTriangle(val_x, val_y);
 
     /* check if point is inside a triangle (if table domain is non-rectangular,
      * the previous range check might be true but the point could still be outside of the domain) */
-    if (IsInTriangle(val_x, val_y, id_triangle, name_x, name_y)) {
+    if (IsInTriangle(val_x, val_y, id_triangle, name_x, name_y, i_level)) {
       /* if so, get interpolation coefficients for point in  the triangle */
-      GetInterpCoeffs(val_x, val_y, interp_mat_inv_x_y[id_triangle], interp_coeffs);
+      GetInterpCoeffs(val_x, val_y, interp_mat_inv_x_y[i_level][id_triangle], interp_coeffs);
 
       /* exit_code 0 means point was in triangle */
       exit_code = 0;
 
     } else {
       /* if point is not inside a triangle (outside table domain) search nearest neighbor */
-      nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, name_x, name_y);
+      nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, name_x, name_y, i_level);
       exit_code = 1;
     }
 
   } else {
     /* if point is outside of table ranges, find nearest neighbor */
-    nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, name_x, name_y);
+    nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, name_x, name_y, i_level);
     exit_code = 1;
   }
 
@@ -395,11 +512,11 @@ unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vecto
 
         /* first, copy the single triangle from the large triangle list*/
         for (int p = 0; p < 3; p++) 
-          triangle[p] = triangles[id_triangle][p]; 
+          triangle[p] = triangles[i_level][id_triangle][p]; 
         *val_vars[i_var] = Interpolate(GetDataP(val_names_var[i_var]), triangle, interp_coeffs);
       }
       else
-        *val_vars[i_var] = GetDataP(val_names_var[i_var])[nearest_neighbor];
+        *val_vars[i_var] = GetDataP(val_names_var[i_var], i_level)[nearest_neighbor];
     }
   }
   return exit_code;
@@ -434,45 +551,45 @@ su2double CLookUpTable::Interpolate(const su2double* val_samples, std::array<uns
 }
 
 unsigned long CLookUpTable::FindNearestNeighborOnHull(su2double val_x, su2double val_y, const string& name_x,
-                                                      const string& name_y) {
+                                                      const string& name_y, unsigned long i_level) {
   su2double min_distance = 1.e99;
   su2double next_distance = 1.e99;
   su2double next_x_norm;
   su2double next_y_norm;
   unsigned long neighbor_id = 0;
 
-  const su2double* x_table = GetDataP(name_x);
-  const su2double* y_table = GetDataP(name_y);
+  const su2double* x_table = GetDataP(name_x, i_level);
+  const su2double* y_table = GetDataP(name_y, i_level);
 
-  su2double norm_coeff_x = 1. / (limits_table_x[1] - limits_table_x[0]);
-  su2double norm_coeff_y = 1. / (limits_table_y[1] - limits_table_y[0]);
-  su2double val_x_norm = val_x / (limits_table_x[1] - limits_table_x[0]);
-  su2double val_y_norm = val_y / (limits_table_y[1] - limits_table_y[0]);
+  su2double norm_coeff_x = 1. / (limits_table_x[i_level].second - limits_table_x[i_level].first);
+  su2double norm_coeff_y = 1. / (limits_table_y[i_level].second - limits_table_y[i_level].first);
+  su2double val_x_norm = val_x / (limits_table_x[i_level].second - limits_table_x[i_level].first);
+  su2double val_y_norm = val_y / (limits_table_y[i_level].second - limits_table_y[i_level].first);
 
-  for (unsigned long i_point = 0; i_point < n_hull_points; ++i_point) {
-    next_x_norm = x_table[hull[i_point]] * norm_coeff_x;
-    next_y_norm = y_table[hull[i_point]] * norm_coeff_y;
+  for (unsigned long i_point = 0; i_point < n_hull_points[i_level]; ++i_point) {
+    next_x_norm = x_table[hull[i_level][i_point]] * norm_coeff_x;
+    next_y_norm = y_table[hull[i_level][i_point]] * norm_coeff_y;
 
     next_distance = sqrt(pow(val_x_norm - next_x_norm, 2) + pow(val_y_norm - next_y_norm, 2));
 
     if (next_distance < min_distance) {
       min_distance = next_distance;
-      neighbor_id = hull[i_point];
+      neighbor_id = hull[i_level][i_point];
     }
   }
   return neighbor_id;
 }
 
 bool CLookUpTable::IsInTriangle(su2double val_x, su2double val_y, unsigned long val_id_triangle, const string& name_x,
-                                const string& name_y) {
-  su2double tri_x_0 = GetDataP(name_x)[triangles[val_id_triangle][0]];
-  su2double tri_y_0 = GetDataP(name_y)[triangles[val_id_triangle][0]];
+                                const string& name_y, unsigned long i_level) {
+  su2double tri_x_0 = GetDataP(name_x, i_level)[triangles[i_level][val_id_triangle][0]];
+  su2double tri_y_0 = GetDataP(name_y, i_level)[triangles[i_level][val_id_triangle][0]];
 
-  su2double tri_x_1 = GetDataP(name_x)[triangles[val_id_triangle][1]];
-  su2double tri_y_1 = GetDataP(name_y)[triangles[val_id_triangle][1]];
+  su2double tri_x_1 = GetDataP(name_x, i_level)[triangles[i_level][val_id_triangle][1]];
+  su2double tri_y_1 = GetDataP(name_y, i_level)[triangles[i_level][val_id_triangle][1]];
   
-  su2double tri_x_2 = GetDataP(name_x)[triangles[val_id_triangle][2]];
-  su2double tri_y_2 = GetDataP(name_y)[triangles[val_id_triangle][2]];
+  su2double tri_x_2 = GetDataP(name_x, i_level)[triangles[i_level][val_id_triangle][2]];
+  su2double tri_y_2 = GetDataP(name_y, i_level)[triangles[i_level][val_id_triangle][2]];
 
   su2double area_tri = TriArea(tri_x_0, tri_y_0, tri_x_1, tri_y_1, tri_x_2, tri_y_2);
 
diff --git a/UnitTests/Common/containers/CLookupTable_tests.cpp b/UnitTests/Common/containers/CLookupTable_tests.cpp
index d19d1800fc0..1d607584e4b 100644
--- a/UnitTests/Common/containers/CLookupTable_tests.cpp
+++ b/UnitTests/Common/containers/CLookupTable_tests.cpp
@@ -53,7 +53,7 @@ TEST_CASE("LUTreader", "[tabulated chemistry]") {
   su2double enth = -0.5; 
   string look_up_tag = "Density";
   su2double look_up_dat;
-  look_up_table.LookUp_ProgEnth(look_up_tag, &look_up_dat, prog, enth, name_CV1, name_CV2); 
+  look_up_table.LookUp_XY(look_up_tag, &look_up_dat, prog, enth, name_CV1, name_CV2); 
   CHECK(look_up_dat == Approx(1.02));
 
   /*--- look up a single value for viscosity ---*/
@@ -61,16 +61,16 @@ TEST_CASE("LUTreader", "[tabulated chemistry]") {
   prog = 0.6;
   enth = 0.9; 
   look_up_tag = "Viscosity";
-  look_up_table.LookUp_ProgEnth(look_up_tag, &look_up_dat, prog, enth, name_CV1, name_CV2); 
+  look_up_table.LookUp_XY(look_up_tag, &look_up_dat, prog, enth, name_CV1, name_CV2); 
   CHECK(look_up_dat == Approx(0.0000674286));
 
   /* find the table limits */
   
-  auto limitsEnth = look_up_table.GetTableLimitsEnth();
+  auto limitsEnth = look_up_table.GetTableLimitsY();
   CHECK(limitsEnth.first == Approx(-1.0));
   CHECK(limitsEnth.second == Approx(1.0));
 
-  auto limitsProgvar = look_up_table.GetTableLimitsProg();
+  auto limitsProgvar = look_up_table.GetTableLimitsX();
   CHECK(limitsProgvar.first == Approx(0.0));
   CHECK(limitsProgvar.second == Approx(1.0));
 
@@ -79,7 +79,7 @@ TEST_CASE("LUTreader", "[tabulated chemistry]") {
   prog = 1.10;
   enth = 1.1;
   look_up_tag = "Density";
-  look_up_table.LookUp_ProgEnth(look_up_tag, &look_up_dat, prog, enth, name_CV1, name_CV2); 
+  look_up_table.LookUp_XY(look_up_tag, &look_up_dat, prog, enth, name_CV1, name_CV2); 
   CHECK(look_up_dat == Approx(1.2));
  
 }

From 76194ecc4154ee6569a3420178c5af801478bfc9 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 22 Nov 2022 14:30:22 +0100
Subject: [PATCH 044/656] Improved Newton solver behavior in data driven fluid
 model

---
 .../multilayer_perceptron/CLayer.hpp          |  3 --
 .../multilayer_perceptron/CNeuralNetwork.hpp  |  3 --
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp    | 12 ++++++++
 SU2_CFD/include/fluid/CFluidModel.hpp         | 12 ++++++++
 SU2_CFD/src/fluid/CCoolProp.cpp               | 28 +++++++++++++++++++
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        | 12 ++++----
 SU2_CFD/src/solvers/CEulerSolver.cpp          |  5 +++-
 7 files changed, 62 insertions(+), 13 deletions(-)

diff --git a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
index c72709fe52e..92566312809 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
@@ -126,9 +126,6 @@ class CLayer
     */
     string getActivationType(){return activation_type;}
     
-    ~CLayer(){
-        delete [] neurons;
-    };
 };
 
 }
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
index b58528069d8..54eb19f3238 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
@@ -83,8 +83,6 @@ class CNeuralNetwork
             delete total_layers.at(i);
         }
         delete [] ANN_outputs;
-        delete [] inputLayer;
-        delete [] outputLayer;
         delete [] activation_function_types;
     };
     void defineInputLayer(unsigned long n_neurons);
@@ -101,7 +99,6 @@ class CNeuralNetwork
 
     unsigned long getNNeurons(unsigned long iLayer){;
     return total_layers.at(iLayer)->getNNeurons();}
-    //unsigned long getNNeurons(unsigned long iLayer, unsigned long iNeuron){return weights.at(iLayer).at(iNeuron).size();}
 
     void predict(std::vector<su2double> &inputs);
 
diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index 79e423d6215..deb893edd6b 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -127,4 +127,16 @@ class CDataDrivenFluid : public CFluidModel {
    * \param[in] s - second thermodynamic variable (s).
    */
   void SetTDState_Ps(su2double P, su2double s) override;
+
+  /*!
+  * \brief Set the initial guess for the density in Newton solvers
+  * \param[in] rho - Initial value for density.
+  */
+  void SetDensity(su2double rho) override {rho_start = rho;}
+
+  /*!
+  * \brief Set the initial guess for the static energy in Newton solvers
+  * \param[in] e - Initial value for static energy.
+  */
+  void SetEnergy(su2double e) override {e_start = e;}
 };
diff --git a/SU2_CFD/include/fluid/CFluidModel.hpp b/SU2_CFD/include/fluid/CFluidModel.hpp
index b57badc99c9..4a1bc47e403 100644
--- a/SU2_CFD/include/fluid/CFluidModel.hpp
+++ b/SU2_CFD/include/fluid/CFluidModel.hpp
@@ -325,4 +325,16 @@ class CFluidModel {
    * \brief Set fluid eddy viscosity provided by a turbulence model needed for computing effective thermal conductivity.
    */
   void SetEddyViscosity(su2double val_Mu_Turb) { Mu_Turb = val_Mu_Turb; }
+
+  /*!
+  * \brief Set the initial guess for the density in Newton solvers
+  * \param[in] rho - Initial value for density.
+  */
+  virtual void SetDensity(su2double rho) {}
+
+  /*!
+  * \brief Set the initial guess for the static energy in Newton solvers
+  * \param[in] e - Initial value for static energy.
+  */
+  virtual void SetEnergy(su2double e) {}
 };
diff --git a/SU2_CFD/src/fluid/CCoolProp.cpp b/SU2_CFD/src/fluid/CCoolProp.cpp
index 61dfb5840cb..9121c8164ed 100644
--- a/SU2_CFD/src/fluid/CCoolProp.cpp
+++ b/SU2_CFD/src/fluid/CCoolProp.cpp
@@ -37,6 +37,34 @@ CCoolProp::CCoolProp(string fluidname) : CFluidModel() {
   Pressure_Critical = fluid_entity->p_critical();
   Temperature_Critical = fluid_entity->T_critical();
   acentric_factor = fluid_entity->acentric_factor();
+
+  su2double p = 5e4;
+  su2double T = 250;
+  su2double p_max = 2e6;
+  su2double T_max = 600;
+  su2double delta_p = (p_max - p)/500;
+  su2double delta_T = (T_max - T)/500;
+  cout << "rho, e, s, dsde_rho, dsdrho_e, d2sde2, d2sdedrho, d2sdrho2, pressure, temperature, soundspeed2" << endl;
+  for(unsigned long i=0;i<500;i++){
+    p = 5e4;
+    for(unsigned long j=0; j<500;j++){
+      fluid_entity->update(CoolProp::PT_INPUTS, p, T);
+      cout << fluid_entity->rhomass() << ", "
+           << fluid_entity->umass() << ", "
+           << fluid_entity->smass() << ", "
+           << fluid_entity->first_partial_deriv(CoolProp::iSmass, CoolProp::iUmass, CoolProp::iDmass) << ", "
+           << fluid_entity->first_partial_deriv(CoolProp::iSmass, CoolProp::iDmass, CoolProp::iUmass) << ", "
+           << fluid_entity->second_partial_deriv(CoolProp::iSmass, CoolProp::iUmass, CoolProp::iDmass, CoolProp::iUmass, CoolProp::iDmass) << ", "
+           << fluid_entity->second_partial_deriv(CoolProp::iSmass, CoolProp::iUmass, CoolProp::iDmass, CoolProp::iDmass, CoolProp::iUmass) << ", "
+           << fluid_entity->second_partial_deriv(CoolProp::iSmass, CoolProp::iDmass, CoolProp::iUmass, CoolProp::iDmass, CoolProp::iUmass) << ", "
+           << p << ", "
+           << T << ", "
+           << pow(fluid_entity->speed_sound(), 2) << endl;
+      p += delta_p;
+    }
+    T += delta_T;
+
+  }
 }
 
 CCoolProp::~CCoolProp() {}
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 7dafd4bf5e6..b95f7c81986 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -60,6 +60,7 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
   /*--- Set initial values for density and energy based on config options ---*/
   rho_start = config->GetDensity_Init_DataDriven();
   e_start   = config->GetEnergy_Init_DataDriven();
+  
 }
 
 CDataDrivenFluid::~CDataDrivenFluid(){
@@ -148,7 +149,7 @@ void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
   dPde_rho = -pow(rho, 2) * dTde_rho * dsdrho_e;
   dPdrho_e = -2*rho*Temperature*dsdrho_e - pow(rho, 2)*Temperature*d2sdrho2;
 
-  Cp = (1 / dTde_rho) * ( 1 + (1 / Density)*dPde_rho) + (1/Density)*(1/dTdrho_e)*(dPdrho_e - Pressure / Density);
+  Cp = (1 / dTde_rho) * ( 1 + (1 / Density)*dPde_rho);
   Cv = 1 / dTde_rho;
   Gamma = Cp / Cv;
   Gamma_Minus_One = Gamma - 1;
@@ -174,7 +175,6 @@ void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
             delta_rho,    // Density step size
             delta_e,      // Energy step size
             determinant;  // Jacobian determinant
-
   /*--- Initiating Newton solver ---*/
   while(!converged && (Iter < iter_max)){
 
@@ -184,7 +184,6 @@ void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
     /*--- Determine pressure and temperature residuals ---*/
     delta_P = Pressure - P;
     delta_T = Temperature - T;
-
     /*--- Continue iterative process if residuals are outside tolerances ---*/
     if((abs(delta_P) < tolerance_P) && (abs(delta_T) < tolerance_T)){
       converged = true;
@@ -199,6 +198,7 @@ void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
       /*--- Update density and energy values ---*/
       rho -= Newton_Relaxation * delta_rho;
       e -= Newton_Relaxation * delta_e;
+      
     }
     Iter ++;
   }
@@ -210,6 +210,7 @@ void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
 void CDataDrivenFluid::SetTDState_Prho(su2double P, su2double rho) {
   /*--- Computing static energy according to pressure and density ---*/
   SetEnergy_Prho(P, rho);
+  
 
   /*--- Calculate thermodynamic state based on converged value for energy ---*/
   SetTDState_rhoe(rho, StaticEnergy);
@@ -245,7 +246,7 @@ void CDataDrivenFluid::SetEnergy_Prho(su2double P, su2double rho) {
       delta_e = delta_P / dPde_rho;
 
       /*--- energy value ---*/
-      e += Newton_Relaxation * delta_e;
+      e -= Newton_Relaxation * delta_e;
     }
     Iter ++;
   }
@@ -286,7 +287,7 @@ void CDataDrivenFluid::SetTDState_rhoT(su2double rho, su2double T) {
       delta_e = delta_T / dTde_rho;
 
       /*--- Update energy value ---*/
-      e += Newton_Relaxation * delta_e;
+      e -= Newton_Relaxation * delta_e;
     }
     Iter ++;
   }
@@ -343,7 +344,6 @@ void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
     }
     Iter ++;
   }
-
   /*--- Calculate thermodynamic state based on converged values for density and energy ---*/
   SetTDState_rhoe(rho, e);
 }
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index d2f07539d29..1850649063e 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -4658,11 +4658,14 @@ void CEulerSolver::BC_Riemann(CGeometry *geometry, CSolver **solver_container,
         P_Total /= config->GetPressure_Ref();
         T_Total /= config->GetTemperature_Ref();
 
+        /*--- Set initial values for density and energy for Newton solvers in fluid model ---*/
+        GetFluidModel()->SetDensity(Density_i);
+        GetFluidModel()->SetEnergy(StaticEnergy_i);
+
         /* --- Computes the total state --- */
         GetFluidModel()->SetTDState_PT(P_Total, T_Total);
         Enthalpy_e = GetFluidModel()->GetStaticEnergy()+ GetFluidModel()->GetPressure()/GetFluidModel()->GetDensity();
         Entropy_e = GetFluidModel()->GetEntropy();
-
         /* --- Compute the boundary state u_e --- */
         Velocity2_e = Velocity2_i;
         if (nDim == 2){

From 32366c44e07f11e3628581a6fe7ca45ef93b4136 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 22 Nov 2022 16:34:29 +0100
Subject: [PATCH 045/656] Removed controlling variable names from inputs to
 lookup operations, as they're redundant. Added a 3D table unit test case

---
 Common/include/containers/CFileReaderLUT.hpp  |   5 +-
 Common/include/containers/CLookUpTable.hpp    |  59 ++++----
 Common/src/containers/CFileReaderLUT.cpp      | 115 +++++++++++----
 Common/src/containers/CLookUpTable.cpp        | 112 ++++++++++-----
 .../Common/containers/CLookupTable_tests.cpp  |  56 +++++++-
 .../Common/containers/lookuptable_3D.drg      | 135 ++++++++++++++++++
 6 files changed, 383 insertions(+), 99 deletions(-)
 create mode 100644 UnitTests/Common/containers/lookuptable_3D.drg

diff --git a/Common/include/containers/CFileReaderLUT.hpp b/Common/include/containers/CFileReaderLUT.hpp
index 37b6f7a4aaa..fbd31bc84fb 100644
--- a/Common/include/containers/CFileReaderLUT.hpp
+++ b/Common/include/containers/CFileReaderLUT.hpp
@@ -50,6 +50,7 @@ class CFileReaderLUT {
   unsigned long *n_triangles;
   unsigned long *n_hull_points;
   unsigned long n_variables;
+  su2double *table_levels = nullptr;
 
   /*! \brief Holds the variable names stored in the table file. 
    * Order is in sync with tableFlamelet.
@@ -81,7 +82,7 @@ class CFileReaderLUT {
 
  public:
   CFileReaderLUT(){};
-  
+  ~CFileReaderLUT();
   inline const std::string& GetVersionLUT() const { return version_lut; }
   inline const std::string& GetVersionReader() const { return version_reader; }
   inline unsigned long GetNPoints(std::size_t i_level=0) const { return n_points[i_level]; }
@@ -98,6 +99,8 @@ class CFileReaderLUT {
 
   inline const std::vector<unsigned long>& GetHull(std::size_t i_level=0) const { return hull[i_level]; }
 
+  inline const su2double GetTableLevel(std::size_t i_level) const { return table_levels[i_level]; }
+  
   inline const unsigned short GetTableDim() const { return table_dim; }
 
   void ReadRawLUT(const std::string& file_name);
diff --git a/Common/include/containers/CLookUpTable.hpp b/Common/include/containers/CLookUpTable.hpp
index 3dcfceb0d51..b92f0903aef 100644
--- a/Common/include/containers/CLookUpTable.hpp
+++ b/Common/include/containers/CLookUpTable.hpp
@@ -47,6 +47,9 @@ class CLookUpTable {
   std::string file_name_lut;
   std::string version_lut;
   std::string version_reader;
+  std::string name_CV1,   // Name of controlling variable 1 
+              name_CV2;   // Name of xontrolling variable 2
+
   unsigned long *n_points;
   unsigned long *n_triangles;
   unsigned long n_variables;
@@ -135,10 +138,8 @@ class CLookUpTable {
 
   /*!
    * \brief compute vector of all (inverse) interpolation coefficients "interp_mat_inv_x_y" of all triangles.
-   * \param[in] name_x - the string name of the first controlling variable.
-   * \param[in] name_y - the string name of the second controlling variable.
   */
-  void ComputeInterpCoeffs(const std::string& name_x, const std::string& name_y);
+  void ComputeInterpCoeffs();
 
   /*!
    * \brief compute the inverse matrix for interpolation.
@@ -170,29 +171,27 @@ class CLookUpTable {
   su2double Interpolate(const su2double* val_samples, std::array<unsigned long,3>& val_triangle,
                         std::array<su2double,3>& val_interp_coeffs);
 
+  void Linear_Interpolation(su2double val_z, std::pair<unsigned long, unsigned long> &inclusion_levels, su2double&lower_value,su2double&upper_value, su2double*&var_vals);
+
+
   void Linear_Interpolation(su2double val_z, std::pair<unsigned long, unsigned long> &inclusion_levels, std::vector<su2double>&lower_values,std::vector<su2double>&upper_values, std::vector<su2double*>&var_vals);
 
   /*!
    * \brief find the point on the hull (boundary of the table) that is closest to the point P(val_x,val_y).
    * \param[in] val_x - first coordinate of point P(val_x,val_y) to check.
    * \param[in] val_y - second coordinate of point P(val_x,val_y) to check.
-   * \param[in] name_x - string name of the first controlling variable.
-   * \param[in] name_y - string name of the second controlling variable.
    * \returns point id of the nearest neighbor on the hull.
    */
-  unsigned long FindNearestNeighborOnHull(su2double val_x, su2double val_y, const std::string& name_x, const std::string& name_y, unsigned long i_level=0);
+  unsigned long FindNearestNeighborOnHull(su2double val_x, su2double val_y, unsigned long i_level=0);
 
   /*!
    * \brief determine if a point P(val_x,val_y) is inside the triangle val_id_triangle.
    * \param[in] val_x - first coordinate of point P(val_x,val_y) to check.
    * \param[in] val_y - second coordinate of point P(val_x,val_y) to check.
    * \param[in] val_id_triangle - ID of the triangle to check.
-   * \param[in] name_x - string name of the first controlling variable.
-   * \param[in] name_y - string name of the second controlling variable.
    * \returns true if the point is in the triangle, false if it is outside.
    */
-  bool IsInTriangle(su2double val_x, su2double val_y, unsigned long val_id_triangle, const std::string& name_x,
-                    const std::string& name_y, unsigned long i_level=0);
+  bool IsInTriangle(su2double val_x, su2double val_y, unsigned long val_id_triangle, unsigned long i_level=0);
 
   /*!
    * \brief compute the area of a triangle given the 3 points of the triangle.
@@ -218,61 +217,59 @@ class CLookUpTable {
   void PrintTableInfo();
 
   /*!
-   * \brief lookup 1 value of the single variable "val_name_var" using controlling variable values(val_x,val_y)
-   *  whose controlling variable names are "name_prog" and "name_enth".
+   * \brief lookup 1 value of the single variable "val_name_var" using controlling variable values(val_x,val_y).
    * \param[in] val_name_var - string name of the variable to look up.
    * \param[out] val_var - the stored value of the variable to look up.
    * \param[in] val_x - value of controlling variable 1.
    * \param[in] val_y - value of controlling variable 2.
-   * \param[in] name_x - string name of controlling variable 1.
-   * \param[in] name_y - string name of controlling variable 2.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
-  unsigned long LookUp_XY(const std::string& val_name_var, su2double* val_var, su2double val_x, su2double val_y,
-                                const std::string& name_x, const std::string& name_y, unsigned long i_level=0);
+  unsigned long LookUp_XY(const std::string& val_name_var, su2double* val_var, su2double val_x, su2double val_y, unsigned long i_level=0);
 
   /*!
-   * \brief lookup 1 value for each of the variables in "val_name_var" using controlling variable values(val_x,val_y)
-   *  whose controlling variable names are "name_x" and "name_y".
+   * \brief lookup 1 value for each of the variables in "val_name_var" using controlling variable values(val_x,val_y).
    * \param[in] val_names_var - vector of string names of the variables to look up.
    * \param[out] val_vars - pointer to the vector of stored values of the variables to look up.
    * \param[in] val_x - value of controlling variable 1.
    * \param[in] val_y - value of controlling variable 2.
-   * \param[in] name_x - string name of controlling variable 1.
-   * \param[in] name_y - string name of controlling variable 2.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
   unsigned long LookUp_XY(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars, su2double val_x,
-                                su2double val_y, const std::string& name_x, const std::string& name_y, unsigned long i_level=0);
+                                su2double val_y, unsigned long i_level=0);
 
   /*!
-   * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_x,val_y)
-   *  whose controlling variable names are "name_x" and "name_y".
+   * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_x,val_y).
    * \param[in] val_name_var - string name of the variable to look up.
    * \param[out] val_var - the stored value of the variable to look up.
    * \param[in] val_x - value of controlling variable 1.
    * \param[in] val_y - value of controlling variable 2.
-   * \param[in] name_x - string name of controlling variable 1.
-   * \param[in] name_y - string name of controlling variable 2.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
   unsigned long LookUp_XY(const std::vector<std::string>& val_names_var, std::vector<su2double>& val_vars, su2double val_x,
-                                su2double val_y, const std::string& name_x, const std::string& name_y, unsigned long i_level=0);
+                                su2double val_y, unsigned long i_level=0);
+
+  /*!
+   * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_x,val_y,val_z).
+   * \param[in] val_name_var - string name of the variable to look up.
+   * \param[out] val_var - the stored value of the variable to look up.
+   * \param[in] val_x - value of controlling variable 1.
+   * \param[in] val_y - value of controlling variable 2.
+   * \param[in] val_z - value of controlling variable 3.
+   * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
+   */
+  unsigned long LookUp_XYZ(const std::string& val_name_var, su2double* val_var, su2double val_x, su2double val_y, su2double val_z);
 
   /*!
-   * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_x,val_y,val_z)
-   *  whose controlling variable names are "name_x" and "name_y".
+   * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_x,val_y,val_z).
    * \param[in] val_name_var - string name of the variable to look up.
    * \param[out] val_var - the stored value of the variable to look up.
    * \param[in] val_x - value of controlling variable 1.
    * \param[in] val_y - value of controlling variable 2.
-   * \param[in] name_x - string name of controlling variable 1.
-   * \param[in] name_y - string name of controlling variable 2.
    * \param[in] val_z - value of controlling variable 3.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
   unsigned long LookUp_XYZ(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars, su2double val_x,
-                                su2double val_y, const std::string& name_x, const std::string& name_y, su2double val_z=0);
+                                su2double val_y, su2double val_z=0);
   
   std::pair<unsigned long, unsigned long> FindInclusionLevels(su2double val_z, bool *within_limits);
 
diff --git a/Common/src/containers/CFileReaderLUT.cpp b/Common/src/containers/CFileReaderLUT.cpp
index 4e9e6b013d2..d18ab05f7f8 100644
--- a/Common/src/containers/CFileReaderLUT.cpp
+++ b/Common/src/containers/CFileReaderLUT.cpp
@@ -63,18 +63,22 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
   bool found_level_count = false;
   while (GetNextNonEmptyLine(file_stream, line) && !eoHeader) {
 
-    /*--- number of points in LUT ---*/
+    /*--- check version_lut ---*/
     if (line.compare("[Version]") == 0) {
       GetNextNonEmptyLine(file_stream, line);
       version_lut = line;
 
-      if(version_lut.compare("1.0.0") == 0){
+      if(version_lut.compare("1.0.1") == 0){
         table_dim = 2;
         n_levels = 1;
         found_level_count = true;
-      }
-      if(version_lut.compare("1.1.0") == 0){
+        n_points      = new unsigned long[n_levels];
+        n_triangles   = new unsigned long[n_levels];
+        n_hull_points = new unsigned long[n_levels];
+      }else if(version_lut.compare("1.1.0") == 0){
         table_dim = 3;
+      }else{
+        SU2_MPI::Error("Version conflict between LUT reader and LUT library file.", CURRENT_FUNCTION);
       }
     }
 
@@ -87,13 +91,14 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
       n_points      = new unsigned long[n_levels];
       n_triangles   = new unsigned long[n_levels];
       n_hull_points = new unsigned long[n_levels];
+      table_levels  = new su2double[n_levels];
     }
 
     /*--- number of points in LUT ---*/
     if (line.compare("[Number of points]") == 0) {
       if(!found_level_count)
         SU2_MPI::Error("Number of points provided before specifying level count.", CURRENT_FUNCTION);
-      for(unsigned long i_level=0; i_level<n_levels; i_level){
+      for(unsigned long i_level=0; i_level<n_levels; i_level++){
         GetNextNonEmptyLine(file_stream, line);
         n_points[i_level] = stoi(line);
       }
@@ -103,7 +108,7 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
     if (line.compare("[Number of triangles]") == 0) {
       if(!found_level_count)
         SU2_MPI::Error("Number of triangles provided before specifying level count.", CURRENT_FUNCTION);
-      for(unsigned long i_level=0; i_level<n_levels; i_level){
+      for(unsigned long i_level=0; i_level<n_levels; i_level++){
         GetNextNonEmptyLine(file_stream, line);
         n_triangles[i_level] = stoi(line);
       }
@@ -113,12 +118,18 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
     if (line.compare("[Number of hull points]") == 0) {
       if(!found_level_count)
         SU2_MPI::Error("Number of hull points provided before specifying level count.", CURRENT_FUNCTION);
-      for(unsigned long i_level=0; i_level<n_levels; i_level){
+      for(unsigned long i_level=0; i_level<n_levels; i_level++){
         GetNextNonEmptyLine(file_stream, line);
         n_hull_points[i_level] = stoi(line);
       }
     }
 
+    if (line.compare("[Table levels]") == 0) {
+      for(unsigned long i_level=0; i_level<n_levels; i_level++){
+        GetNextNonEmptyLine(file_stream, line);
+        table_levels[i_level] = stod(line);
+      }
+    }
     /*--- number of variables in LUT ---*/
     if (line.compare("[Number of variables]") == 0) {
       GetNextNonEmptyLine(file_stream, line);
@@ -139,10 +150,7 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
     /*--- check if end of header is reached ---*/
     if (line.compare("</Header>") == 0) eoHeader = true;
   }
-
-  /*--- check version_lut ---*/
-  if (version_lut.compare(version_reader) != 0)
-    SU2_MPI::Error("Version conflict between LUT reader and LUT library file.", CURRENT_FUNCTION);
+    
 
   /*--- check header quantities ---*/
   for(unsigned long i_level=0; i_level < n_levels; i_level++){
@@ -186,7 +194,7 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
 
   SkipToFlag(file_stream, line, "<Data>");
   unsigned long i_level = 0;
-  bool eoLevel = false;
+  bool eoLevel = true;
   unsigned long pointCounter = 0;
   unsigned long levelCounter = 0;
   while (GetNextNonEmptyLine(file_stream, line) && !eoData) {
@@ -202,7 +210,7 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
       }
       if(line.compare("</Level>") == 0){
         eoLevel = true;
-        if (n_points[levelCounter] != pointCounter - 1)
+        if (n_points[levelCounter] != pointCounter)
         SU2_MPI::Error(
             "Number of read points on level " + std::to_string(levelCounter) + " does not match number of points "
             "specified in lookup table library header.",
@@ -232,6 +240,8 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
   SkipToFlag(file_stream, line, "<Connectivity>");
   i_level = 0;
   unsigned long triCounter = 0;
+  eoLevel = true;
+  levelCounter = 0;
   while (GetNextNonEmptyLine(file_stream, line) && !eoConnectivity) {
     if (!line.empty() && (line[line.length()-1] == '\n' || line[line.length()-1] == '\r' )) {
       line.erase(line.length()-1);
@@ -240,22 +250,39 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
     if (line.compare("</Connectivity>") == 0) eoConnectivity = true;
 
     if (!eoConnectivity) {
-      /*--- one line contains values for one triangle (3 points) ---*/
-      istringstream streamTriLine(line);
+      if(line.compare("<Level>") == 0){
+        eoLevel = false;
+        triCounter = 0;
+        GetNextNonEmptyLine(file_stream, line);
+      }
+      if(line.compare("</Level>") == 0){
+        eoLevel = true;
+        if (n_triangles[levelCounter] != triCounter)
+        SU2_MPI::Error(
+            "Number of read points on level " + std::to_string(levelCounter) + " does not match number of points "
+            "specified in lookup table library header.",
+            CURRENT_FUNCTION);
+        levelCounter++;
+      }
+      if(!eoLevel || (table_dim == 2)){
+        /*--- one line contains values for one triangle (3 points) ---*/
+        istringstream streamTriLine(line);
 
-      /*--- add next line to triangles ---*/
-      for (int iPoint = 0; iPoint < 3; iPoint++) {
+        /*--- add next line to triangles ---*/
+        for (int iPoint = 0; iPoint < 3; iPoint++) {
 
-        streamTriLine >> word;
+          streamTriLine >> word;
 
-        /*--- lookup table index starts with 1, convert to c++ indexing starting with 0: ---*/
-        triangles[i_level][triCounter][iPoint] = stol(word) - 1;
+          /*--- lookup table index starts with 1, convert to c++ indexing starting with 0: ---*/
+          triangles[levelCounter][triCounter][iPoint] = stol(word) - 1;
+        }
+        triCounter++;
       }
     }
-    triCounter++;
+    
   }
 
-  if (n_triangles[i_level] != triCounter - 1)
+  if (n_triangles[0] != triCounter)
     SU2_MPI::Error(
         "Number of read triangles does not match number of points "
         "specified in lookup table library header.",
@@ -267,6 +294,8 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
   SkipToFlag(file_stream, line, "<Hull>");
   i_level = 0;
   unsigned long hullCounter = 0;
+  eoLevel = true;
+  levelCounter = 0;
   while (GetNextNonEmptyLine(file_stream, line) && !eoHull) {
     if (!line.empty() && (line[line.length()-1] == '\n' || line[line.length()-1] == '\r' )) {
       line.erase(line.length()-1);
@@ -275,18 +304,34 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
     if (line.compare("</Hull>") == 0) eoHull = true;
 
     if (!eoHull) {
-      /*--- one line contains one point ID for one point on the hull  ---*/
-      istringstream streamHullLine(line);
+      if(line.compare("<Level>") == 0){
+        eoLevel = false;
+        hullCounter = 0;
+        GetNextNonEmptyLine(file_stream, line);
+      }
+      if(line.compare("</Level>") == 0){
+        eoLevel = true;
+        if (n_hull_points[levelCounter] != hullCounter)
+        SU2_MPI::Error(
+            "Number of read points on level " + std::to_string(levelCounter) + " does not match number of points "
+            "specified in lookup table library header.",
+            CURRENT_FUNCTION);
+        levelCounter++;
+      }
+      if(!eoLevel || (table_dim == 2)){
+        /*--- one line contains one point ID for one point on the hull  ---*/
+        istringstream streamHullLine(line);
 
-      streamHullLine >> word;
+        streamHullLine >> word;
 
-      /*--- Lookup table indices start with 1, convert to c++ indexing starting with 0: ---*/
-      hull[i_level][hullCounter] = stol(word) - 1;
-    }
-    hullCounter++;
+        /*--- Lookup table indices start with 1, convert to c++ indexing starting with 0: ---*/
+        hull[levelCounter][hullCounter] = stol(word) - 1;
+        hullCounter++;
+      }
+      }
   }
 
-  if (n_hull_points[i_level] != hullCounter - 1)
+  if (n_hull_points[0] != hullCounter)
     SU2_MPI::Error(
         "Number of read hull points does not match number of points "
         "specified in lookup table library header.",
@@ -296,6 +341,16 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
 
 }
 
+CFileReaderLUT::~CFileReaderLUT(){
+  delete [] n_triangles;
+  delete [] n_hull_points;
+  delete [] n_points;
+  delete [] table_data;
+  delete [] hull;
+  delete [] triangles;
+  if(table_levels != nullptr) delete [] table_levels;
+}
+
 void CFileReaderLUT::SkipToFlag(ifstream& file_stream, const string& current_line, const string& flag) const {
   string next_line = "";
 
diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index a64ebcfa7ab..f3e455a1418 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -36,6 +36,9 @@ CLookUpTable::CLookUpTable(const string& var_file_name_lut, const string& name_x
 
   rank = SU2_MPI::GetRank();
 
+  name_CV1 = name_x;
+  name_CV2 = name_y;
+
   LoadTableRaw(var_file_name_lut);
 
   FindTableLimits(name_x, name_y);
@@ -67,7 +70,7 @@ CLookUpTable::CLookUpTable(const string& var_file_name_lut, const string& name_x
     cout << "Precomputing interpolation coefficients..." << endl;
   
 
-  ComputeInterpCoeffs(name_x, name_y);
+  ComputeInterpCoeffs();
 
   if (rank == MASTER_NODE) 
     cout << "LUT fluid model ready for use" << endl;
@@ -123,8 +126,9 @@ void CLookUpTable::LoadTableRaw(const string& var_file_name_lut) {
 
   if(table_dim == 3){
     z_values_levels = new su2double[n_table_levels];
-    //TODO: fill in z-values from table reader.
-    //TODO: get minimum and maximum z-values from table reader.
+    for(unsigned long i_level=0; i_level<n_table_levels; i_level++){
+      z_values_levels[i_level] = file_reader.GetTableLevel(i_level);
+    }
   }
   if (rank == MASTER_NODE) 
     cout << " done." << endl;
@@ -290,14 +294,14 @@ void CLookUpTable::IdentifyUniqueEdges() {
   }
 }
 
-void CLookUpTable::ComputeInterpCoeffs(const string& name_x, const string& name_y) {
+void CLookUpTable::ComputeInterpCoeffs() {
   for(auto i_level=0ul; i_level<n_table_levels; i_level++){
     /* build KD tree for y, x space */
 
     std::array<unsigned long, 3> next_triangle;
 
-    const su2double* val_x = GetDataP(name_x, i_level);
-    const su2double* val_y = GetDataP(name_y, i_level);
+    const su2double* val_x = GetDataP(name_CV1, i_level);
+    const su2double* val_y = GetDataP(name_CV2, i_level);
 
     /* calculate weights for each triangle (basically a distance function) and
     * build inverse interpolation matrices */
@@ -360,8 +364,41 @@ std::pair<unsigned long, unsigned long> CLookUpTable::FindInclusionLevels(su2dou
   return inclusion_levels;
 }
 
+unsigned long CLookUpTable::LookUp_XYZ(const std::string& val_name_var, su2double* val_var, su2double val_x,
+                                su2double val_y, su2double val_z)
+{
+  bool within_z_limits, exit_code;
+  unsigned long lower_level, upper_level;
+  std::pair<unsigned long, unsigned long> inclusion_levels;
+  if(val_z == 0){
+    inclusion_levels = std::make_pair(0, 0);
+    within_z_limits = false;
+  }else{
+    inclusion_levels = FindInclusionLevels(val_z, &within_z_limits);
+  }
+  
+  if(within_z_limits){
+    lower_level = inclusion_levels.first;
+    upper_level = inclusion_levels.second;
+    su2double val_var_lower, val_var_upper;
+    unsigned long exit_code_lower = LookUp_XY(val_name_var, &val_var_lower, val_x, val_y, lower_level);
+    unsigned long exit_code_upper = LookUp_XY(val_name_var, &val_var_upper, val_x, val_y, upper_level);
+
+    Linear_Interpolation(val_z, inclusion_levels, val_var_lower, val_var_upper, val_var);
+
+    return max(exit_code_lower, exit_code_upper);
+  }else{
+    lower_level = inclusion_levels.first;
+    exit_code = LookUp_XY(val_name_var, val_var, val_x, val_y, lower_level);
+    if( val_z == 0 ){
+      return exit_code;
+    }else{
+      return 1;
+    }
+  }
+}
 unsigned long CLookUpTable::LookUp_XYZ(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars, su2double val_x,
-                                su2double val_y, const std::string& name_x, const std::string& name_y, su2double val_z)
+                                su2double val_y, su2double val_z)
 {
   bool within_z_limits, exit_code;
   unsigned long lower_level, upper_level;
@@ -379,15 +416,15 @@ unsigned long CLookUpTable::LookUp_XYZ(const std::vector<std::string>& val_names
     std::vector<su2double> val_vars_lower, val_vars_upper;
     val_vars_lower.resize(val_vars.size());
     val_vars_upper.resize(val_vars.size());
-    unsigned long exit_code_lower = LookUp_XY(val_names_var, val_vars_lower, val_x, val_y, name_x, name_y, lower_level);
-    unsigned long exit_code_upper = LookUp_XY(val_names_var, val_vars_upper, val_x, val_y, name_x, name_y, upper_level);
+    unsigned long exit_code_lower = LookUp_XY(val_names_var, val_vars_lower, val_x, val_y, lower_level);
+    unsigned long exit_code_upper = LookUp_XY(val_names_var, val_vars_upper, val_x, val_y, upper_level);
 
     Linear_Interpolation(val_z, inclusion_levels, val_vars_lower, val_vars_upper, val_vars);
 
     return max(exit_code_lower, exit_code_upper);
   }else{
     lower_level = inclusion_levels.first;
-    exit_code = LookUp_XY(val_names_var, val_vars, val_x, val_y, name_x, name_y, lower_level);
+    exit_code = LookUp_XY(val_names_var, val_vars, val_x, val_y, lower_level);
     if( val_z == 0 ){
       return exit_code;
     }else{
@@ -396,6 +433,17 @@ unsigned long CLookUpTable::LookUp_XYZ(const std::vector<std::string>& val_names
   }
 }
 
+void CLookUpTable::Linear_Interpolation(su2double val_z, std::pair<unsigned long, unsigned long> &inclusion_levels, su2double&lower_value,su2double&upper_value, su2double*&var_val)
+{
+  su2double val_z_lower = z_values_levels[inclusion_levels.first];
+  su2double val_z_upper = z_values_levels[inclusion_levels.second];
+  su2double factor_upper = (val_z - val_z_lower) / (val_z_upper - val_z_lower);
+  su2double factor_lower = (val_z_upper - val_z) / (val_z_upper - val_z_lower);
+
+  *var_val = lower_value * factor_lower + upper_value * factor_upper;
+  
+}
+
 void CLookUpTable::Linear_Interpolation(su2double val_z, std::pair<unsigned long, unsigned long> &inclusion_levels, std::vector<su2double>&lower_values,std::vector<su2double>&upper_values, std::vector<su2double*>&var_vals)
 {
   su2double val_z_lower = z_values_levels[inclusion_levels.first];
@@ -409,7 +457,7 @@ void CLookUpTable::Linear_Interpolation(su2double val_z, std::pair<unsigned long
 }
 
 unsigned long CLookUpTable::LookUp_XY(const string& val_name_var, su2double *val_var, su2double val_x,
-                                            su2double val_y, const string& name_x, const string& name_y, unsigned long i_level) {
+                                            su2double val_y, unsigned long i_level) {
   unsigned long exit_code = 0;
 
   if (val_name_var.compare("NULL") == 0) {
@@ -425,7 +473,7 @@ unsigned long CLookUpTable::LookUp_XY(const string& val_name_var, su2double *val
     /* find the triangle that holds the (x, y) point */
     unsigned long id_triangle = trap_map_x_y[i_level].GetTriangle(val_x, val_y);
 
-    if (IsInTriangle(val_x, val_y, id_triangle, name_x, name_y, i_level)) {
+    if (IsInTriangle(val_x, val_y, id_triangle, i_level)) {
       /* get interpolation coefficients for point on triangle */
       std::array<su2double,3> interp_coeffs{0};
       GetInterpCoeffs(val_x, val_y, interp_mat_inv_x_y[i_level][id_triangle], interp_coeffs);
@@ -439,13 +487,13 @@ unsigned long CLookUpTable::LookUp_XY(const string& val_name_var, su2double *val
       exit_code = 0;
     } else {
       /* in bounding box but outside of table */
-      unsigned long nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, name_x, name_y, i_level);
+      unsigned long nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, i_level);
       *val_var = GetDataP(val_name_var, i_level)[nearest_neighbor];
       exit_code = 1;
     }
   } else {
     /* lookup is outside of table bounding box */
-    unsigned long nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, name_x, name_y, i_level);
+    unsigned long nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, i_level);
     *val_var = GetDataP(val_name_var, i_level)[nearest_neighbor];
     exit_code = 1;
   }
@@ -453,22 +501,20 @@ unsigned long CLookUpTable::LookUp_XY(const string& val_name_var, su2double *val
 }
 
 unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vector<su2double>& val_vars,
-                                            su2double val_x, su2double val_y, const string& name_x,
-                                            const string& name_y, unsigned long i_level) {
+                                            su2double val_x, su2double val_y, unsigned long i_level) {
   vector<su2double*> look_up_data;
 
   for (long unsigned int i_var = 0; i_var < val_vars.size(); ++i_var) {
     look_up_data.push_back(&val_vars[i_var]);
   }
 
-  unsigned long exit_code = LookUp_XY(val_names_var, look_up_data, val_x, val_y, name_x, name_y, i_level);
+  unsigned long exit_code = LookUp_XY(val_names_var, look_up_data, val_x, val_y, i_level);
 
   return exit_code;
 }
 
 unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vector<su2double*>& val_vars,
-                                            su2double val_x, su2double val_y, const string& name_x,
-                                            const string& name_y, unsigned long i_level) {
+                                            su2double val_x, su2double val_y, unsigned long i_level) {
   unsigned long exit_code = 0;
   unsigned long nearest_neighbor = 0;
   unsigned long id_triangle;
@@ -484,7 +530,7 @@ unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vecto
 
     /* check if point is inside a triangle (if table domain is non-rectangular,
      * the previous range check might be true but the point could still be outside of the domain) */
-    if (IsInTriangle(val_x, val_y, id_triangle, name_x, name_y, i_level)) {
+    if (IsInTriangle(val_x, val_y, id_triangle, i_level)) {
       /* if so, get interpolation coefficients for point in  the triangle */
       GetInterpCoeffs(val_x, val_y, interp_mat_inv_x_y[i_level][id_triangle], interp_coeffs);
 
@@ -493,13 +539,13 @@ unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vecto
 
     } else {
       /* if point is not inside a triangle (outside table domain) search nearest neighbor */
-      nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, name_x, name_y, i_level);
+      nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, i_level);
       exit_code = 1;
     }
 
   } else {
     /* if point is outside of table ranges, find nearest neighbor */
-    nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, name_x, name_y, i_level);
+    nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, i_level);
     exit_code = 1;
   }
 
@@ -550,16 +596,15 @@ su2double CLookUpTable::Interpolate(const su2double* val_samples, std::array<uns
   return result;
 }
 
-unsigned long CLookUpTable::FindNearestNeighborOnHull(su2double val_x, su2double val_y, const string& name_x,
-                                                      const string& name_y, unsigned long i_level) {
+unsigned long CLookUpTable::FindNearestNeighborOnHull(su2double val_x, su2double val_y, unsigned long i_level) {
   su2double min_distance = 1.e99;
   su2double next_distance = 1.e99;
   su2double next_x_norm;
   su2double next_y_norm;
   unsigned long neighbor_id = 0;
 
-  const su2double* x_table = GetDataP(name_x, i_level);
-  const su2double* y_table = GetDataP(name_y, i_level);
+  const su2double* x_table = GetDataP(name_CV1, i_level);
+  const su2double* y_table = GetDataP(name_CV2, i_level);
 
   su2double norm_coeff_x = 1. / (limits_table_x[i_level].second - limits_table_x[i_level].first);
   su2double norm_coeff_y = 1. / (limits_table_y[i_level].second - limits_table_y[i_level].first);
@@ -580,16 +625,15 @@ unsigned long CLookUpTable::FindNearestNeighborOnHull(su2double val_x, su2double
   return neighbor_id;
 }
 
-bool CLookUpTable::IsInTriangle(su2double val_x, su2double val_y, unsigned long val_id_triangle, const string& name_x,
-                                const string& name_y, unsigned long i_level) {
-  su2double tri_x_0 = GetDataP(name_x, i_level)[triangles[i_level][val_id_triangle][0]];
-  su2double tri_y_0 = GetDataP(name_y, i_level)[triangles[i_level][val_id_triangle][0]];
+bool CLookUpTable::IsInTriangle(su2double val_x, su2double val_y, unsigned long val_id_triangle, unsigned long i_level) {
+  su2double tri_x_0 = GetDataP(name_CV1, i_level)[triangles[i_level][val_id_triangle][0]];
+  su2double tri_y_0 = GetDataP(name_CV2, i_level)[triangles[i_level][val_id_triangle][0]];
 
-  su2double tri_x_1 = GetDataP(name_x, i_level)[triangles[i_level][val_id_triangle][1]];
-  su2double tri_y_1 = GetDataP(name_y, i_level)[triangles[i_level][val_id_triangle][1]];
+  su2double tri_x_1 = GetDataP(name_CV1, i_level)[triangles[i_level][val_id_triangle][1]];
+  su2double tri_y_1 = GetDataP(name_CV2, i_level)[triangles[i_level][val_id_triangle][1]];
   
-  su2double tri_x_2 = GetDataP(name_x, i_level)[triangles[i_level][val_id_triangle][2]];
-  su2double tri_y_2 = GetDataP(name_y, i_level)[triangles[i_level][val_id_triangle][2]];
+  su2double tri_x_2 = GetDataP(name_CV1, i_level)[triangles[i_level][val_id_triangle][2]];
+  su2double tri_y_2 = GetDataP(name_CV2, i_level)[triangles[i_level][val_id_triangle][2]];
 
   su2double area_tri = TriArea(tri_x_0, tri_y_0, tri_x_1, tri_y_1, tri_x_2, tri_y_2);
 
diff --git a/UnitTests/Common/containers/CLookupTable_tests.cpp b/UnitTests/Common/containers/CLookupTable_tests.cpp
index 1d607584e4b..e80c4285f20 100644
--- a/UnitTests/Common/containers/CLookupTable_tests.cpp
+++ b/UnitTests/Common/containers/CLookupTable_tests.cpp
@@ -53,7 +53,7 @@ TEST_CASE("LUTreader", "[tabulated chemistry]") {
   su2double enth = -0.5; 
   string look_up_tag = "Density";
   su2double look_up_dat;
-  look_up_table.LookUp_XY(look_up_tag, &look_up_dat, prog, enth, name_CV1, name_CV2); 
+  look_up_table.LookUp_XY(look_up_tag, &look_up_dat, prog, enth); 
   CHECK(look_up_dat == Approx(1.02));
 
   /*--- look up a single value for viscosity ---*/
@@ -61,7 +61,7 @@ TEST_CASE("LUTreader", "[tabulated chemistry]") {
   prog = 0.6;
   enth = 0.9; 
   look_up_tag = "Viscosity";
-  look_up_table.LookUp_XY(look_up_tag, &look_up_dat, prog, enth, name_CV1, name_CV2); 
+  look_up_table.LookUp_XY(look_up_tag, &look_up_dat, prog, enth); 
   CHECK(look_up_dat == Approx(0.0000674286));
 
   /* find the table limits */
@@ -79,8 +79,58 @@ TEST_CASE("LUTreader", "[tabulated chemistry]") {
   prog = 1.10;
   enth = 1.1;
   look_up_tag = "Density";
-  look_up_table.LookUp_XY(look_up_tag, &look_up_dat, prog, enth, name_CV1, name_CV2); 
+  look_up_table.LookUp_XY(look_up_tag, &look_up_dat, prog, enth); 
   CHECK(look_up_dat == Approx(1.2));
  
 }
 
+TEST_CASE("LUTreader_3D", "[tabulated chemistry]") {
+
+  /*--- smaller and trivial lookup table ---*/
+  
+  CLookUpTable look_up_table("src/SU2/UnitTests/Common/containers/lookuptable_3D.drg","ProgressVariable","EnthalpyTot");
+
+  /*--- string names of the controlling variables ---*/
+
+  string name_CV1 = "ProgressVariable";
+  string name_CV2 = "EnthalpyTot";
+
+ /*--- look up a single value for density ---*/
+
+  su2double prog = 0.55;
+  su2double enth = -0.5; 
+  su2double mfrac = 0.5;
+  string look_up_tag = "Density";
+  su2double look_up_dat;
+  look_up_table.LookUp_XYZ(look_up_tag, &look_up_dat, prog, enth, mfrac); 
+  CHECK(look_up_dat == Approx(1.02));
+
+  /*--- look up a single value for viscosity ---*/
+
+  prog = 0.6;
+  enth = 0.9; 
+  mfrac = 0.8;
+  look_up_tag = "Viscosity";
+  look_up_table.LookUp_XYZ(look_up_tag, &look_up_dat, prog, enth, mfrac); 
+  CHECK(look_up_dat == Approx(0.0000674286));
+
+  /* find the table limits */
+  
+  auto limitsEnth = look_up_table.GetTableLimitsY();
+  CHECK(limitsEnth.first == Approx(-1.0));
+  CHECK(limitsEnth.second == Approx(1.0));
+
+  auto limitsProgvar = look_up_table.GetTableLimitsX();
+  CHECK(limitsProgvar.first == Approx(0.0));
+  CHECK(limitsProgvar.second == Approx(1.0));
+
+  /* lookup value outside of lookup table */
+
+  prog = 1.10;
+  enth = 1.1;
+  mfrac = 2.0;
+  look_up_tag = "Density";
+  look_up_table.LookUp_XYZ(look_up_tag, &look_up_dat, prog, enth, mfrac); 
+  CHECK(look_up_dat == Approx(1.2));
+ 
+}
\ No newline at end of file
diff --git a/UnitTests/Common/containers/lookuptable_3D.drg b/UnitTests/Common/containers/lookuptable_3D.drg
new file mode 100644
index 00000000000..2bfb4e3cc93
--- /dev/null
+++ b/UnitTests/Common/containers/lookuptable_3D.drg
@@ -0,0 +1,135 @@
+Dragon library
+
+<Header>
+[Version]
+1.1.0
+
+[Number of table levels]
+2
+
+[Number of points]
+12
+12
+
+[Number of triangles]
+14
+14
+
+[Number of hull points]
+8
+8
+
+[Progress variable definition]
+prog var = 1*Y-CH4
+
+[Progress variable range]
+0.0 | 1.0
+0.0 | 1.0
+
+[Enthalpy range]
+-1.0 | 1.0
+-1.0 | 1.0
+
+[Table levels]
+0.0
+1.0
+
+[Number of variables]
+4
+
+[Variable names]
+1:ProgressVariable
+2:EnthalpyTot
+3:Density
+4:Viscosity
+
+</Header>
+
+<Data>
+<Level>
+0.0 -1.0 1.0 1.0e-5
+0.3 -1.0 1.0 1.2e-5
+0.6 -1.0 1.0 1.4e-5
+1.0 -1.0 1.0 1.6e-5
+0.5 0.25 1.05 2.0e-5
+0.75 0.25 1.05 3.0e-5
+0.3 0.5 1.1 3.0e-5
+0.6 0.5 1.1 4.0e-5
+1.0 0.5 1.1 5.0e-5
+0.0 1.0 1.2 6.0e-5
+0.3 1.0 1.2 7.0e-5
+1.0 1.0 1.2 8.0e-5
+</Level>
+<Level>
+0.0 -1.0 1.0 1.0e-5
+0.3 -1.0 1.0 1.2e-5
+0.6 -1.0 1.0 1.4e-5
+1.0 -1.0 1.0 1.6e-5
+0.5 0.25 1.05 2.0e-5
+0.75 0.25 1.05 3.0e-5
+0.3 0.5 1.1 3.0e-5
+0.6 0.5 1.1 4.0e-5
+1.0 0.5 1.1 5.0e-5
+0.0 1.0 1.2 6.0e-5
+0.3 1.0 1.2 7.0e-5
+1.0 1.0 1.2 8.0e-5
+</Level>
+</Data>
+
+<Connectivity>
+<Level>
+1 2 7
+1 7 11
+1 11 10
+2 5 7
+2 3 5
+3 8 5
+5 8 7
+7 8 11
+3 6 8
+3 4 6
+4 9 6
+6 9 8
+8 9 12
+8 12 11
+</Level>
+<Level>
+1 2 7
+1 7 11
+1 11 10
+2 5 7
+2 3 5
+3 8 5
+5 8 7
+7 8 11
+3 6 8
+3 4 6
+4 9 6
+6 9 8
+8 9 12
+8 12 11
+</Level>
+</Connectivity>
+
+<Hull>
+<Level>
+1
+2
+3
+4
+9
+12
+11
+10
+</Level>
+<Level>
+1
+2
+3
+4
+9
+12
+11
+10
+</Level>
+</Hull>

From 68d02ae7036ef8fa5d93cfb6a6bc47aa9a280d4d Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Wed, 23 Nov 2022 12:17:38 +0100
Subject: [PATCH 046/656] Added unit test for multi-layer perceptron

---
 .../CLookUp_ANN_tests.cpp                     | 35 ++++++++++++++
 .../multilayer_perceptron/mlp_collection.mlp  |  5 ++
 .../multilayer_perceptron/simple_mlp.mlp      | 47 +++++++++++++++++++
 3 files changed, 87 insertions(+)
 create mode 100644 UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
 create mode 100644 UnitTests/Common/toolboxes/multilayer_perceptron/mlp_collection.mlp
 create mode 100644 UnitTests/Common/toolboxes/multilayer_perceptron/simple_mlp.mlp

diff --git a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
new file mode 100644
index 00000000000..13e3709f3f8
--- /dev/null
+++ b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
@@ -0,0 +1,35 @@
+/*!
+ * \file CLookUp_ANN_tests.cpp
+ * \brief Unit tests for NdFlattener template classes.
+ * \author M. Aehle
+ * \version 7.4.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+
+#include "catch.hpp"
+#include "../../../../Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp"
+#include "../../../../Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp"
+
+TEST_CASE("LookUp ANN test", "[LookUpANN]"){
+  CLookUp_ANN ANN("mlp_collection.mlp");
+
+}
diff --git a/UnitTests/Common/toolboxes/multilayer_perceptron/mlp_collection.mlp b/UnitTests/Common/toolboxes/multilayer_perceptron/mlp_collection.mlp
new file mode 100644
index 00000000000..620e796825e
--- /dev/null
+++ b/UnitTests/Common/toolboxes/multilayer_perceptron/mlp_collection.mlp
@@ -0,0 +1,5 @@
+[number of MLP files]
+1
+
+[MLP file names]
+simple_mlp.mlp 
diff --git a/UnitTests/Common/toolboxes/multilayer_perceptron/simple_mlp.mlp b/UnitTests/Common/toolboxes/multilayer_perceptron/simple_mlp.mlp
new file mode 100644
index 00000000000..01fb20bd102
--- /dev/null
+++ b/UnitTests/Common/toolboxes/multilayer_perceptron/simple_mlp.mlp
@@ -0,0 +1,47 @@
+<header>
+
+[number of layers]
+3
+
+[neurons per layer]
+2
+4
+1
+
+[activation function]
+linear
+elu
+linear
+
+[input names]
+x
+y
+
+[input normalization]
++0.0000000000000000e+00	+2.0000000000000000e+00
+-1.0000000000000000e+00	+0.0000000000000000e+00
+
+[output names]
+z
+
+[output normalization]
+-1.0000000000000000e+00	+9.9998769302960888e-01
+
+</header>
+
+[weights per layer]
+<layer>
+-4.1729342937469482e-01	-2.2465672492980957e+00	+1.1258139610290527e+00	-7.0158332586288452e-01	
++1.1477893590927124e+00	+2.5089375674724579e-02	+2.6767715811729431e-01	+1.0031684637069702e+00	
+</layer>
+<layer>
++2.5062826275825500e-01	
+-6.2471812963485718e-01	
+-2.0578651130199432e-01	
++2.6085931062698364e-01	
+</layer>
+
+[biases per layer]
++0.0000000000000000e+00	+0.0000000000000000e+00	+0.0000000000000000e+00
++7.5714819133281708e-02	+7.7316933870315552e-01	-4.4279521703720093e-01	+4.1041103005409241e-01	
++2.8878501057624817e-01	

From 1a40d51afd58dd01d28189e06c9337010d850af9 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Wed, 23 Nov 2022 15:39:36 +0100
Subject: [PATCH 047/656] Added MLP test case configuration file and unit test

---
 .../multilayer_perceptron/CNeuralNetwork.hpp  | 184 +++++++++++++++---
 .../CReadNeuralNetwork.hpp                    |  10 +-
 SU2_CFD/src/fluid/CCoolProp.cpp               |  28 ---
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        |   5 +-
 TestCases/nicf/coolprop/coolprop_nozzle.cfg   |   2 +-
 .../nicf/datadriven/datadriven_nozzle.cfg     | 128 ++++++++++++
 .../CLookUp_ANN_tests.cpp                     |  36 +++-
 .../multilayer_perceptron/mlp_collection.mlp  |   2 +-
 UnitTests/meson.build                         |   1 +
 9 files changed, 330 insertions(+), 66 deletions(-)
 create mode 100644 TestCases/nicf/datadriven/datadriven_nozzle.cfg

diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
index 54eb19f3238..c5aa90c30fc 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
@@ -41,27 +41,28 @@ namespace MLPToolbox{
 class CNeuralNetwork
 {
 private:
-    std::vector<std::string> input_names,
-                   output_names;
+    std::vector<std::string> input_names,   // MLP input variable names.
+                             output_names;  // MLP output variable names.
 
-    unsigned long n_hidden_layers;
+    unsigned long n_hidden_layers;  // Number of hidden layers (layers between input and output layer).
 
-    CLayer *inputLayer,
-           *outputLayer;
+    CLayer *inputLayer,     // Pointer to network input layer.
+           *outputLayer;    // Pointer to network output layer.
 
-    std::vector<CLayer*> hiddenLayers,
-                    total_layers;
+    std::vector<CLayer*> hiddenLayers,  // Hidden layer collection.
+                         total_layers;  // Hidden layers plus in/output layers
 
-    //std::vector<std::vector<std::vector<su2double>>> weights;
-    std::vector<su2activematrix> weights_mat;
-    std::vector<std::vector<su2double>> values;
+    std::vector<su2activematrix> weights_mat;   // Weights of synapses connecting layers
 
-    std::vector<std::pair<su2double, su2double>> input_norm,
-                                       output_norm;
-    std::vector<su2double> last_inputs;
+    std::vector<std::pair<su2double, su2double>> input_norm,    // Normalization factors for network inputs
+                                                 output_norm;   // Normalization factors for network outputs
 
-    su2double* ANN_outputs;
+    std::vector<su2double> last_inputs; // Inputs from previous lookup operation. Evaluation of the network 
+                                        // is skipped if current inputs are the same as the last inputs.
 
+    su2double* ANN_outputs; // Pointer to network outputs
+
+    /*--- Activation function types that are currently supported ---*/
     enum ENUM_ACTIVATION_FUNCTION {
         NONE=0,
         LINEAR=1,
@@ -79,46 +80,169 @@ class CNeuralNetwork
 public:
     CNeuralNetwork();
     ~CNeuralNetwork(){
-        for(std::size_t i=0; i<total_layers.size(); i++){
-            delete total_layers.at(i);
+        delete inputLayer;
+        delete outputLayer;
+        for(std::size_t i=1; i<total_layers.size()-1; i++){
+            delete total_layers[i];
         }
         delete [] ANN_outputs;
         delete [] activation_function_types;
     };
+    /*!
+    * \brief Set the input layer of the network.
+    * \param[in] n_neurons - Number of inputs
+    */
     void defineInputLayer(unsigned long n_neurons);
+
+    /*!
+    * \brief Set the output layer of the network.
+    * \param[in] n_neurons - Number of outputs
+    */
     void defineOutputLayer(unsigned long n_neurons);
+
+    /*!
+    * \brief Add a hidden layer to the network
+    * \param[in] n_neurons - Hidden layer size.
+    */
     void push_hidden_layer(unsigned long n_neurons);
+
+    /*!
+    * \brief Set the weight value of a specific synapse.
+    * \param[in] i_layer - current layer.
+    * \param[in] i_neuron - neuron index in current layer.
+    * \param[in] j_neuron - neuron index of connecting neuron.
+    * \param[in] value - weight value.
+    */
     void setWeight(unsigned long i_layer, unsigned long i_neuron, unsigned long j_neuron, su2double value);
+
+    /*!
+    * \brief Set bias value at a specific neuron.
+    * \param[in] i_layer - Layer index.
+    * \param[in] i_neuron - Neuron index of current layer.
+    * \param[in] value - Bias value.
+    */
     void setBias(unsigned long i_layer, unsigned long i_neuron, su2double value){total_layers.at(i_layer)->setBias(i_neuron, value);}
+
+    /*!
+    * \brief Set layer activation function.
+    * \param[in] i_layer - Layer index.
+    * \param[in] input - Activation function name.
+    */
     void setActivationFunction(unsigned long i_layer, std::string input);
+
+    /*!
+    * \brief Display the network architecture in the terminal.
+    */
     void displayNetwork();
+
+    /*!
+    * \brief Size the weight layers in the network according to its architecture.
+    */
     void sizeWeights();
-    void sizeInputs(unsigned long n_inputs){last_inputs.resize(n_inputs); for(unsigned long iInput=0; iInput<n_inputs; iInput++) last_inputs.at(iInput) = 0.0;}
+
+    /*!
+    * \brief Size the vector of previous inputs.
+    * \param[in] n_inputs - Number of inputs.
+    */
+    void sizeInputs(unsigned long n_inputs) { last_inputs.resize(n_inputs); for(unsigned long iInput=0; iInput<n_inputs; iInput++) last_inputs.at(iInput) = 0.0; }
+    
+    /*!
+    * \brief Get the number of connecting regions in the network.
+    * \returns number of spaces in between layers.
+    */
     unsigned long getNWeightLayers(){return total_layers.size()-1;}
+
+    /*!
+    * \brief Get the total number of layers in the network
+    * \returns number of netowork layers.
+    */
     unsigned long getNLayers(){return total_layers.size();}
 
-    unsigned long getNNeurons(unsigned long iLayer){;
-    return total_layers.at(iLayer)->getNNeurons();}
+    /*!
+    * \brief Get neuron count in a layer.
+    * \param[in] iLayer - Layer index.
+    * \returns number of neurons in the layer.
+    */
+    unsigned long getNNeurons(unsigned long iLayer) { return total_layers.at(iLayer)->getNNeurons(); }
 
+    /*!
+    * \brief Evaluate the network.
+    */
     void predict(std::vector<su2double> &inputs);
 
+    /*!
+    * \brief Set the normalization factors for the input layer
+    * \param[in] iInput - Input index.
+    * \param[in] input_min - Minimum input value.
+    * \param[in] input_max - Maximum input value.
+    */
+    void SetInputNorm(unsigned long iInput, su2double input_min, su2double input_max) { input_norm.at(iInput) = make_pair(input_min, input_max); }
 
-    void SetInputNorm(unsigned long iInput, su2double input_min, su2double input_max){input_norm.at(iInput) = make_pair(input_min, input_max);}
-    void SetOutputNorm(unsigned long iOutput, su2double output_min, su2double output_max){output_norm.at(iOutput) = make_pair(output_min, output_max);}
+    /*!
+    * \brief Set the normalization factors for the output layer
+    * \param[in] iOutput - Input index.
+    * \param[in] input_min - Minimum output value.
+    * \param[in] input_max - Maximum output value.
+    */
+    void SetOutputNorm(unsigned long iOutput, su2double output_min, su2double output_max){ output_norm.at(iOutput) = make_pair(output_min, output_max); }
     
-    void PushOutputName(std::string input){output_names.push_back(input);}
-    void PushInputName(std::string input){input_names.push_back(input);}
+    /*!
+    * \brief Add an output variable name to the network.
+    * \param[in] input - Input variable name.
+    */
+    void PushOutputName(std::string input) { output_names.push_back(input); }
+
+    /*!
+    * \brief Add an input variable name to the network.
+    * \param[in] output - Output variable name.
+    */
+    void PushInputName(std::string input) { input_names.push_back(input); }
    
-    std::string GetInputName(std::size_t iInput){return input_names[iInput];}
-    std::string GetOutputName(std::size_t iOutput){return output_names[iOutput];}
+    /*!
+    * \brief Get network input variable name.
+    * \param[in] iInput - Input variable index.
+    * \returns input variable name.
+    */
+    std::string GetInputName(std::size_t iInput) { return input_names[iInput]; }
 
-    std::size_t GetnInputs(){return input_names.size();}
-    std::size_t GetnOutputs(){return output_names.size();}
+    /*!
+    * \brief Get network output variable name.
+    * \param[in] iOutput - Output variable index.
+    * \returns output variable name.
+    */
+    std::string GetOutputName(std::size_t iOutput) { return output_names[iOutput]; }
 
-    su2double GetANN_Output(std::size_t iOutput){return ANN_outputs[iOutput];}
-    void SizeActivationFunctions(unsigned long n_layers){activation_function_types = new ENUM_ACTIVATION_FUNCTION[n_layers]; 
-    }
+    /*!
+    * \brief Get network number of inputs.
+    * \returns Number of network inputs
+    */
+    std::size_t GetnInputs() { return input_names.size(); }
+
+    /*!
+    * \brief Get network number of outputs.
+    * \returns Number of network outputs
+    */
+    std::size_t GetnOutputs() { return output_names.size(); }
+
+    /*!
+    * \brief Get network evaluation output.
+    * \param[in] iOutput - output index.
+    * \returns Prediction value.
+    */
+    su2double GetANN_Output(std::size_t iOutput) { return ANN_outputs[iOutput]; }
+
+    /*!
+    * \brief Set the activation function array size.
+    * \param[in] n_layers - network layer count.
+    */
+    void SizeActivationFunctions(unsigned long n_layers) { activation_function_types = new ENUM_ACTIVATION_FUNCTION[n_layers]; }
 
+    /*!
+    * \brief Compute neuron activation function input.
+    * \param[in] iLayer - Network layer index.
+    * \param[in] iNeuron - Layer neuron index.
+    * \returns Neuron activation function input.
+    */
     su2double ComputeX(std::size_t iLayer, std::size_t iNeuron){
         su2double x;
         x = total_layers[iLayer]->getBias(iNeuron);
diff --git a/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
index 7921023762b..a06509dfb85 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
@@ -37,11 +37,13 @@ namespace MLPToolbox{
 
 class CReadNeuralNetwork {
     private:
-    std::vector<std::string> input_names;
-    std::vector<std::string> output_names;
+    std::vector<std::string> input_names,   // Network input variable names.
+                             output_names;  // Network output variable names.
 
-    std::string filename;
-    unsigned long n_layers;
+    std::string filename;       // Network input filename.
+
+    unsigned long n_layers;     // Number of layers in the network.
+    
     std::vector<unsigned long> n_neurons;
     std::vector<std::vector<std::vector<su2double>>> weights;
     std::vector<std::vector<su2double>> biases;
diff --git a/SU2_CFD/src/fluid/CCoolProp.cpp b/SU2_CFD/src/fluid/CCoolProp.cpp
index 9121c8164ed..61dfb5840cb 100644
--- a/SU2_CFD/src/fluid/CCoolProp.cpp
+++ b/SU2_CFD/src/fluid/CCoolProp.cpp
@@ -37,34 +37,6 @@ CCoolProp::CCoolProp(string fluidname) : CFluidModel() {
   Pressure_Critical = fluid_entity->p_critical();
   Temperature_Critical = fluid_entity->T_critical();
   acentric_factor = fluid_entity->acentric_factor();
-
-  su2double p = 5e4;
-  su2double T = 250;
-  su2double p_max = 2e6;
-  su2double T_max = 600;
-  su2double delta_p = (p_max - p)/500;
-  su2double delta_T = (T_max - T)/500;
-  cout << "rho, e, s, dsde_rho, dsdrho_e, d2sde2, d2sdedrho, d2sdrho2, pressure, temperature, soundspeed2" << endl;
-  for(unsigned long i=0;i<500;i++){
-    p = 5e4;
-    for(unsigned long j=0; j<500;j++){
-      fluid_entity->update(CoolProp::PT_INPUTS, p, T);
-      cout << fluid_entity->rhomass() << ", "
-           << fluid_entity->umass() << ", "
-           << fluid_entity->smass() << ", "
-           << fluid_entity->first_partial_deriv(CoolProp::iSmass, CoolProp::iUmass, CoolProp::iDmass) << ", "
-           << fluid_entity->first_partial_deriv(CoolProp::iSmass, CoolProp::iDmass, CoolProp::iUmass) << ", "
-           << fluid_entity->second_partial_deriv(CoolProp::iSmass, CoolProp::iUmass, CoolProp::iDmass, CoolProp::iUmass, CoolProp::iDmass) << ", "
-           << fluid_entity->second_partial_deriv(CoolProp::iSmass, CoolProp::iUmass, CoolProp::iDmass, CoolProp::iDmass, CoolProp::iUmass) << ", "
-           << fluid_entity->second_partial_deriv(CoolProp::iSmass, CoolProp::iDmass, CoolProp::iUmass, CoolProp::iDmass, CoolProp::iUmass) << ", "
-           << p << ", "
-           << T << ", "
-           << pow(fluid_entity->speed_sound(), 2) << endl;
-      p += delta_p;
-    }
-    T += delta_T;
-
-  }
 }
 
 CCoolProp::~CCoolProp() {}
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index b95f7c81986..f3f26e9c8eb 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -1,7 +1,7 @@
 /*!
  * \file CDataDrivenFluid.cpp
  * \brief Source of the data-driven fluid model class
- * \author E.Bunschoten
+ * \author E.Bunschoten M.Mayer A.Capiello
  * \version 7.4.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
@@ -133,16 +133,19 @@ void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
     break;
   }
 
+  /*--- Compute speed of sound ---*/
   su2double blue_term = (dsdrho_e * (2 - rho * pow(dsde_rho, -1) * d2sdedrho) + rho * d2sdrho2);
   su2double green_term = (- pow(dsde_rho, -1) * d2sde2 * dsdrho_e + d2sdedrho);
   
   SoundSpeed2 = - rho * pow(dsde_rho, -1) * (blue_term - rho * green_term * (dsdrho_e / dsde_rho));
 
+  /*--- Compute primary flow variables ---*/
   Temperature = 1.0 / dsde_rho;
   Pressure = -pow(rho, 2) * Temperature * dsdrho_e;
   Density = rho;
   StaticEnergy = e;
   
+  /*--- Compute secondary flow variables ---*/
   dTde_rho = -pow(dsde_rho, -2)*d2sde2;
   dTdrho_e = 0.0;
 
diff --git a/TestCases/nicf/coolprop/coolprop_nozzle.cfg b/TestCases/nicf/coolprop/coolprop_nozzle.cfg
index 7a3f6a1ac24..87e809107c0 100644
--- a/TestCases/nicf/coolprop/coolprop_nozzle.cfg
+++ b/TestCases/nicf/coolprop/coolprop_nozzle.cfg
@@ -85,7 +85,7 @@ CFL_REDUCTION_TURB= 1.0
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
 % Number of total iterations
-ITER= 101
+ITER= 1
 CONV_RESIDUAL_MINVAL= -24
 CONV_STARTITER= 10
 
diff --git a/TestCases/nicf/datadriven/datadriven_nozzle.cfg b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
new file mode 100644
index 00000000000..12dfc48d026
--- /dev/null
+++ b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
@@ -0,0 +1,128 @@
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+%                                                                              %
+% SU2 configuration file                                                       %
+% Case description: Non-ideal compressible fluid flow in a converging-         %
+%                   diverging supersonic nozzle with CoolProp library          %
+% Author: Peng Yan, Alberto Guardone                                           %
+% Institution: Politecnico di Milano                                           %
+% Date: 2022.10.8                                                              %
+% File Version  7.4.0 Blackbird                                                %
+%                                                                              %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+SOLVER= RANS
+KIND_TURB_MODEL= SST
+MATH_PROBLEM= DIRECT
+RESTART_SOL= YES
+SYSTEM_MEASUREMENTS= SI
+%
+% -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
+%
+% Mach number (non-dimensional, based on the free-stream values)
+MACH_NUMBER= 1E-9
+AOA= 0.0
+SIDESLIP_ANGLE= 0.0
+INIT_OPTION= TD_CONDITIONS
+FREESTREAM_OPTION= TEMPERATURE_FS
+FREESTREAM_PRESSURE= 904388
+%
+% Free-stream temperature (288.15 K, 518.67 R by default)
+FREESTREAM_TEMPERATURE= 542.13
+REF_DIMENSIONALIZATION= DIMENSIONAL
+
+% ---- DATADRIVEN FLUID MODEL DEFINITION -------%
+%
+FLUID_MODEL = DATADRIVEN_FLUID
+INTERPOLATION_METHOD = MLP 
+FILENAME_INTERPOLATOR = mlp_collection.mlp 
+DATADRIVEN_NEWTON_RELAXATION = 0.02
+DATADRIVEN_FLUID_INITIAL_DENSITY = 8.20106
+DATADRIVEN_FLUID_INITIAL_ENERGY = 4.19552e+05
+
+% --------------------------- VISCOSITY MODEL ---------------------------------%
+VISCOSITY_MODEL= CONSTANT_VISCOSITY
+MU_CONSTANT= 1.21409E-05
+
+% --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
+CONDUCTIVITY_MODEL= CONSTANT_CONDUCTIVITY
+THERMAL_CONDUCTIVITY_CONSTANT= 0.030542828
+
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+MARKER_HEATFLUX= ( WALL, 0.0 )
+MARKER_SYM= ( SYMMETRY )
+MARKER_RIEMANN= ( INFLOW, TOTAL_CONDITIONS_PT, 904388, 542.13, 1.0, 0.0, 0.0, OUTFLOW, STATIC_PRESSURE, 200000.0, 0.0, 0.0, 0.0, 0.0 )
+
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+NUM_METHOD_GRAD= GREEN_GAUSS
+CFL_NUMBER= 10.0
+CFL_ADAPT= YES
+CFL_ADAPT_PARAM= ( 0.1, 2.0, 10.0, 1000.0 )
+MAX_DELTA_TIME= 1E6
+
+% ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
+MUSCL_FLOW= YES
+SLOPE_LIMITER_FLOW= NONE
+MUSCL_TURB= NO
+
+% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
+LINEAR_SOLVER= FGMRES
+LINEAR_SOLVER_PREC= ILU
+LINEAR_SOLVER_ILU_FILL_IN= 0
+LINEAR_SOLVER_ERROR= 1E-6
+LINEAR_SOLVER_ITER= 10
+
+% -------------------------- MULTIGRID PARAMETERS -----------------------------%
+%
+% Multi-grid levels (0 = no multi-grid)
+MGLEVEL= 0
+
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+CONV_NUM_METHOD_FLOW= ROE
+ENTROPY_FIX_COEFF= 0.1
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+
+% -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
+CONV_NUM_METHOD_TURB= SCALAR_UPWIND
+TIME_DISCRE_TURB= EULER_IMPLICIT
+CFL_REDUCTION_TURB= 1.0
+
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
+% Number of total iterations
+ITER= 101
+CONV_RESIDUAL_MINVAL= -24
+CONV_STARTITER= 10
+
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+%
+% Mesh input file
+MESH_FILENAME= ../coolprop/coolprop_nozzle.su2
+%
+% Mesh input file format (SU2, CGNS)
+MESH_FORMAT= SU2
+%
+% Mesh output file
+MESH_OUT_FILENAME= mesh_out.su2
+%
+% Restart flow input file
+SOLUTION_FILENAME= solution_flow.dat
+TABULAR_FORMAT= CSV
+%
+% Output file convergence history (w/o extension)
+CONV_FILENAME= history
+%
+% Output file restart flow
+RESTART_FILENAME= restart_flow.dat
+%
+% Output file flow (w/o extension) variables
+VOLUME_FILENAME= flow
+%
+% Output file surface flow coefficient (w/o extension)
+SURFACE_FILENAME= surface_flow
+%
+% Writing solution file frequency
+OUTPUT_WRT_FREQ= 50
+%
+% Screen output
+SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG)
diff --git a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
index 13e3709f3f8..2c61c44fa44 100644
--- a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
+++ b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
@@ -26,10 +26,44 @@
  */
 
 #include "catch.hpp"
+#include "../../../../Common/include/CConfig.hpp"
 #include "../../../../Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp"
 #include "../../../../Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp"
 
 TEST_CASE("LookUp ANN test", "[LookUpANN]"){
-  CLookUp_ANN ANN("mlp_collection.mlp");
 
+  MLPToolbox::CLookUp_ANN ANN("src/SU2/UnitTests/Common/toolboxes/multilayer_perceptron/mlp_collection.mlp");
+  std::vector<std::string> MLP_input_names,
+                           MLP_output_names;
+  std::vector<su2double> MLP_inputs;
+  std::vector<su2double*> MLP_outputs;
+  su2double x,y,z;
+
+  /*--- Define MLP inputs and outputs ---*/
+  MLP_input_names.push_back("x");
+  MLP_input_names.push_back("y");
+  MLP_inputs.resize(2);
+
+  MLP_output_names.push_back("z");
+  MLP_outputs.push_back(&z);
+
+  /*--- Generate input-output map ---*/
+  MLPToolbox::CIOMap iomap(&ANN, MLP_input_names, MLP_output_names);
+
+  /*--- MLP evaluation on point in the middle of the training data range ---*/
+  x = 1.0;
+  y = -0.5;
+
+  MLP_inputs[0] = x;
+  MLP_inputs[1] = y;
+  ANN.Predict_ANN(&iomap, MLP_inputs, MLP_outputs);
+  CHECK(z == Approx(0.344829));
+
+  /*--- MLP evaluation on point outside the training data range ---*/
+  x = 3.0;
+  y = -10;
+  MLP_inputs[0] = x;
+  MLP_inputs[1] = y;
+  ANN.Predict_ANN(&iomap, MLP_inputs, MLP_outputs);
+  CHECK(z == Approx(0.012737));
 }
diff --git a/UnitTests/Common/toolboxes/multilayer_perceptron/mlp_collection.mlp b/UnitTests/Common/toolboxes/multilayer_perceptron/mlp_collection.mlp
index 620e796825e..b441964701b 100644
--- a/UnitTests/Common/toolboxes/multilayer_perceptron/mlp_collection.mlp
+++ b/UnitTests/Common/toolboxes/multilayer_perceptron/mlp_collection.mlp
@@ -2,4 +2,4 @@
 1
 
 [MLP file names]
-simple_mlp.mlp 
+src/SU2/UnitTests/Common/toolboxes/multilayer_perceptron/simple_mlp.mlp 
diff --git a/UnitTests/meson.build b/UnitTests/meson.build
index 3875cf1b576..1c806b67ca4 100644
--- a/UnitTests/meson.build
+++ b/UnitTests/meson.build
@@ -12,6 +12,7 @@ su2_cfd_tests = files(['Common/geometry/primal_grid/CPrimalGrid_tests.cpp',
                        'Common/vectorization.cpp',
                        'Common/toolboxes/ndflattener_tests.cpp',
                        'Common/containers/CLookupTable_tests.cpp',
+                       'Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp',
                        'SU2_CFD/numerics/CNumerics_tests.cpp',
                        'SU2_CFD/gradients.cpp',
                        'SU2_CFD/windowing.cpp'])

From 205a40479d124b7e52d9b9b9e1050d3bcbf94794 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Wed, 23 Nov 2022 15:49:37 +0100
Subject: [PATCH 048/656] Fixed build error

---
 Common/src/containers/CFileReaderLUT.cpp | 3 ---
 1 file changed, 3 deletions(-)

diff --git a/Common/src/containers/CFileReaderLUT.cpp b/Common/src/containers/CFileReaderLUT.cpp
index d18ab05f7f8..789e444dab4 100644
--- a/Common/src/containers/CFileReaderLUT.cpp
+++ b/Common/src/containers/CFileReaderLUT.cpp
@@ -193,7 +193,6 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
   if (rank == MASTER_NODE) cout << "loading data block" << endl;
 
   SkipToFlag(file_stream, line, "<Data>");
-  unsigned long i_level = 0;
   bool eoLevel = true;
   unsigned long pointCounter = 0;
   unsigned long levelCounter = 0;
@@ -238,7 +237,6 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
   if (rank == MASTER_NODE) cout << "loading connectivity block" << endl;
 
   SkipToFlag(file_stream, line, "<Connectivity>");
-  i_level = 0;
   unsigned long triCounter = 0;
   eoLevel = true;
   levelCounter = 0;
@@ -292,7 +290,6 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
   if (rank == MASTER_NODE) cout << "loading hull block" << endl;
 
   SkipToFlag(file_stream, line, "<Hull>");
-  i_level = 0;
   unsigned long hullCounter = 0;
   eoLevel = true;
   levelCounter = 0;

From 7280ff1dde51446853292952f1f28154210036a2 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 25 Nov 2022 10:05:31 +0100
Subject: [PATCH 049/656] Fixed further build errors

---
 Common/include/containers/CFileReaderLUT.hpp | 4 ++--
 Common/include/containers/CLookUpTable.hpp   | 2 +-
 Common/src/containers/CLookUpTable.cpp       | 6 +++---
 3 files changed, 6 insertions(+), 6 deletions(-)

diff --git a/Common/include/containers/CFileReaderLUT.hpp b/Common/include/containers/CFileReaderLUT.hpp
index fbd31bc84fb..ecb48139041 100644
--- a/Common/include/containers/CFileReaderLUT.hpp
+++ b/Common/include/containers/CFileReaderLUT.hpp
@@ -99,9 +99,9 @@ class CFileReaderLUT {
 
   inline const std::vector<unsigned long>& GetHull(std::size_t i_level=0) const { return hull[i_level]; }
 
-  inline const su2double GetTableLevel(std::size_t i_level) const { return table_levels[i_level]; }
+  inline su2double GetTableLevel(std::size_t i_level) const { return table_levels[i_level]; }
   
-  inline const unsigned short GetTableDim() const { return table_dim; }
+  inline unsigned short GetTableDim() const { return table_dim; }
 
   void ReadRawLUT(const std::string& file_name);
 };
diff --git a/Common/include/containers/CLookUpTable.hpp b/Common/include/containers/CLookUpTable.hpp
index b92f0903aef..2e10ce28edb 100644
--- a/Common/include/containers/CLookUpTable.hpp
+++ b/Common/include/containers/CLookUpTable.hpp
@@ -55,7 +55,7 @@ class CLookUpTable {
   unsigned long n_variables;
   unsigned long *n_hull_points;
   unsigned long n_table_levels = 1;
-  su2double *z_values_levels;
+  su2double *z_values_levels = nullptr;
 
   /*! 
    * \brief the lower and upper limits of the z, y and x variable.
diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index f3e455a1418..12e2ed08622 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -134,9 +134,9 @@ void CLookUpTable::LoadTableRaw(const string& var_file_name_lut) {
     cout << " done." << endl;
 }
 
-void CLookUpTable::FindTableLimits(const string& name_x, const string& name_y) {
-  int idx_X = GetIndexOfVar(name_x);
-  int idx_Y = GetIndexOfVar(name_y);
+void CLookUpTable::FindTableLimits(const string& name_cv1, const string& name_cv2) {
+  int idx_X = GetIndexOfVar(name_cv1);
+  int idx_Y = GetIndexOfVar(name_cv2);
   limits_table_x = new pair<su2double, su2double>[n_table_levels];
   limits_table_y = new pair<su2double, su2double>[n_table_levels];
 

From 1f17501aed6c4137e0437440aaffce5b0685309c Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 25 Nov 2022 10:29:43 +0100
Subject: [PATCH 050/656] Replaced std::vector with su2vector where possible

---
 Common/include/containers/CFileReaderLUT.hpp  |  9 ++++-----
 Common/include/containers/CLookUpTable.hpp    | 11 +++++------
 Common/include/containers/CTrapezoidalMap.hpp |  8 ++++----
 Common/src/containers/CFileReaderLUT.cpp      |  6 +++---
 Common/src/containers/CLookUpTable.cpp        | 13 +++++++------
 Common/src/containers/CTrapezoidalMap.cpp     |  6 +++---
 6 files changed, 26 insertions(+), 27 deletions(-)

diff --git a/Common/include/containers/CFileReaderLUT.hpp b/Common/include/containers/CFileReaderLUT.hpp
index ecb48139041..8e602eb45a0 100644
--- a/Common/include/containers/CFileReaderLUT.hpp
+++ b/Common/include/containers/CFileReaderLUT.hpp
@@ -55,7 +55,7 @@ class CFileReaderLUT {
   /*! \brief Holds the variable names stored in the table file. 
    * Order is in sync with tableFlamelet.
    */
-  std::vector<std::string> names_var;
+  su2vector<std::string> names_var;
 
   /*! \brief Holds all data stored in the table. 
    * First index addresses the variable while second index addresses the point.
@@ -64,8 +64,7 @@ class CFileReaderLUT {
 
   su2matrix<unsigned long> *triangles;
 
-  std::vector<unsigned long> *hull;
-
+  su2vector<unsigned long> *hull;
   /*! \brief Searches for the position of flag in file_stream and 
    *         sets the stream position of file_stream to that position.
    */
@@ -91,13 +90,13 @@ class CFileReaderLUT {
   inline unsigned long GetNVariables() const { return n_variables; }
   inline unsigned long GetNLevels() const { return n_levels; }
 
-  inline const std::vector<std::string>& GetNamesVar() const { return names_var; }
+  inline const su2vector<std::string>& GetNamesVar() const { return names_var; }
 
   inline const su2activematrix& GetTableData(std::size_t i_level=0) const { return table_data[i_level]; }
 
   inline const su2matrix<unsigned long>& GetTriangles(std::size_t i_level=0) const { return triangles[i_level]; }
 
-  inline const std::vector<unsigned long>& GetHull(std::size_t i_level=0) const { return hull[i_level]; }
+  inline const su2vector<unsigned long>& GetHull(std::size_t i_level=0) const { return hull[i_level]; }
 
   inline su2double GetTableLevel(std::size_t i_level) const { return table_levels[i_level]; }
   
diff --git a/Common/include/containers/CLookUpTable.hpp b/Common/include/containers/CLookUpTable.hpp
index 2e10ce28edb..87db8a1e88c 100644
--- a/Common/include/containers/CLookUpTable.hpp
+++ b/Common/include/containers/CLookUpTable.hpp
@@ -67,7 +67,7 @@ class CLookUpTable {
   /*! \brief Holds the variable names stored in the table file.
    * Order is in sync with data
    */
-  std::vector<std::string> names_var;
+  su2vector<std::string> names_var;
 
   /*! \brief
    * Holds all data stored in the table. First index addresses the variable
@@ -77,21 +77,20 @@ class CLookUpTable {
 
   su2matrix<unsigned long> *triangles;
 
-  /* we do not know this size in advance until we go through the entire lookup table */
-  std::vector<std::vector<unsigned long> > *edges;
-  std::vector<std::vector<unsigned long> > *edge_to_triangle;
+  std::vector<su2vector<unsigned long> > *edges;
+  su2vector<std::vector<unsigned long> > *edge_to_triangle;
 
   /*! \brief 
    * The hull contains the boundary of the lookup table.
    */
-  std::vector<unsigned long> *hull;
+  su2vector<unsigned long> *hull;
 
   CTrapezoidalMap *trap_map_x_y;
 
   /*! \brief 
    * vector of all the weight factors for the interpolation.
    */
-  std::vector<su2activematrix> *interp_mat_inv_x_y;
+  su2vector<su2activematrix> *interp_mat_inv_x_y;
 
   /*! \brief 
    * returns the index to the variable in the lookup table.
diff --git a/Common/include/containers/CTrapezoidalMap.hpp b/Common/include/containers/CTrapezoidalMap.hpp
index 284c2c9d88a..61e5f8f5b0a 100644
--- a/Common/include/containers/CTrapezoidalMap.hpp
+++ b/Common/include/containers/CTrapezoidalMap.hpp
@@ -49,11 +49,11 @@
   su2activematrix edge_limits_x;
   su2activematrix edge_limits_y;
 
-  std::vector<std::vector<unsigned long> > edge_to_triangle;
+  su2vector<std::vector<unsigned long> > edge_to_triangle;
 
   /* The value that each edge which intersects the band takes within that
    * same band. Used to sort the edges */
-  std::vector<std::vector<std::pair<su2double, unsigned long> > > y_edge_at_band_mid;
+  su2vector<std::vector<std::pair<su2double, unsigned long> > > y_edge_at_band_mid;
 
  public:
 
@@ -62,8 +62,8 @@
   CTrapezoidalMap(const su2double* samples_x,
                   const su2double* samples_y,
                   const unsigned long size,
-                  const std::vector<std::vector<unsigned long> >& edges,
-                  const std::vector<std::vector<unsigned long> >& edge_to_triangle);
+                  const std::vector<su2vector<unsigned long> >& edges,
+                  const su2vector<std::vector<unsigned long> >& edge_to_triangle);
 
   /*!
    * \brief return the index to the triangle that contains the coordinates (val_x,val_y) 
diff --git a/Common/src/containers/CFileReaderLUT.cpp b/Common/src/containers/CFileReaderLUT.cpp
index 789e444dab4..191e88a08dd 100644
--- a/Common/src/containers/CFileReaderLUT.cpp
+++ b/Common/src/containers/CFileReaderLUT.cpp
@@ -138,12 +138,12 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
 
     /*--- variable names ---*/
     if (line.compare("[Variable names]") == 0) {
-      
+      names_var.resize(n_variables);
       for (unsigned long i = 0; i < n_variables; i++){
 
         /*--- grab a single line ---*/
         GetNextNonEmptyLine(file_stream, line);
-        names_var.push_back(line.substr(line.find(":")+1)); 
+        names_var[i] = line.substr(line.find(":")+1); 
       }
     }
 
@@ -182,7 +182,7 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
     triangles[i_level].resize(GetNTriangles(i_level), 3);
 
   if (rank == MASTER_NODE) cout << "allocating memory for the hull points, size = " << GetNHullPoints() << endl;
-  hull = new vector<unsigned long>[n_levels];
+  hull = new su2vector<unsigned long>[n_levels];
   for(unsigned long i_level=0; i_level<n_levels; i_level++)
     hull[i_level].resize(GetNHullPoints(i_level));
 
diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index 12e2ed08622..5c096528fac 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -104,11 +104,11 @@ void CLookUpTable::LoadTableRaw(const string& var_file_name_lut) {
   n_triangles         = new unsigned long[n_table_levels];
   n_hull_points       = new unsigned long[n_table_levels];
   table_data          = new su2activematrix[n_table_levels];
-  hull                = new std::vector<unsigned long>[n_table_levels];
+  hull                = new su2vector<unsigned long>[n_table_levels];
   triangles           = new su2matrix<unsigned long>[n_table_levels];
-  interp_mat_inv_x_y  = new std::vector<su2activematrix>[n_table_levels];
-  edges               = new std::vector<std::vector<unsigned long> >[n_table_levels];
-  edge_to_triangle    = new std::vector<std::vector<unsigned long> >[n_table_levels];
+  interp_mat_inv_x_y  = new su2vector<su2activematrix>[n_table_levels];
+  edges               = new std::vector<su2vector<unsigned long> >[n_table_levels];
+  edge_to_triangle    = new su2vector<std::vector<unsigned long> >[n_table_levels];
 
   for(unsigned long i_level=0; i_level<n_table_levels; i_level++){
     n_points[i_level] = file_reader.GetNPoints(i_level);
@@ -261,7 +261,7 @@ void CLookUpTable::IdentifyUniqueEdges() {
 
       /* Store the edge so that the lower index of the pair is always first. */
       if (iPoint < GlobalIndex) {
-        vector<unsigned long> edge(2);
+        su2vector<unsigned long> edge(2);
         edge[0] = iPoint;
         edge[1] = GlobalIndex;
         edges[i_level].push_back(edge);
@@ -305,6 +305,7 @@ void CLookUpTable::ComputeInterpCoeffs() {
 
     /* calculate weights for each triangle (basically a distance function) and
     * build inverse interpolation matrices */
+    interp_mat_inv_x_y[i_level].resize(n_triangles[i_level]);
     for (unsigned long i_triangle = 0; i_triangle < n_triangles[i_level]; i_triangle++) {
 
       for (int p = 0; p < 3; p++) {
@@ -313,7 +314,7 @@ void CLookUpTable::ComputeInterpCoeffs() {
 
       su2activematrix x_interp_mat_inv(3, 3);
       GetInterpMatInv(val_x, val_y, next_triangle, x_interp_mat_inv);
-      interp_mat_inv_x_y[i_level].push_back(x_interp_mat_inv);
+      interp_mat_inv_x_y[i_level][i_triangle] = x_interp_mat_inv;
     }
   }
 }
diff --git a/Common/src/containers/CTrapezoidalMap.cpp b/Common/src/containers/CTrapezoidalMap.cpp
index 21d7cb535ac..f651c6a2cfe 100644
--- a/Common/src/containers/CTrapezoidalMap.cpp
+++ b/Common/src/containers/CTrapezoidalMap.cpp
@@ -38,12 +38,12 @@ using namespace std;
  * NOTE: the current implementation is actually the simpler 'slab' approach.
  */
 CTrapezoidalMap::CTrapezoidalMap(const su2double* samples_x, const su2double* samples_y, const unsigned long size,
-                                 vector<vector<unsigned long> > const& edges,
-                                 vector<vector<unsigned long> > const& val_edge_to_triangle) {
+                                 vector<su2vector<unsigned long> > const& edges,
+                                 su2vector<vector<unsigned long> > const& val_edge_to_triangle) {
   int rank = SU2_MPI::GetRank();
   su2double startTime = SU2_MPI::Wtime();
 
-  edge_to_triangle = vector<vector<unsigned long> >(val_edge_to_triangle);
+  edge_to_triangle = su2vector<vector<unsigned long> >(val_edge_to_triangle);
 
   unique_bands_x.assign(samples_x,samples_x+size);
 

From 054a8ff9443814b08fdae1d342537f549b341adf Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 25 Nov 2022 11:18:00 +0100
Subject: [PATCH 051/656] Replaced std::vector by su2vector where possible

---
 .../multilayer_perceptron/CIOMap.hpp          |  8 +--
 .../multilayer_perceptron/CLayer.hpp          |  2 +-
 .../multilayer_perceptron/CLookUp_ANN.hpp     | 14 +++---
 .../multilayer_perceptron/CNeuralNetwork.hpp  | 22 ++++-----
 .../multilayer_perceptron/CIOMap.cpp          |  8 +--
 .../multilayer_perceptron/CLookUp_ANN.cpp     | 18 +++----
 .../multilayer_perceptron/CNeuralNetwork.cpp  |  8 +--
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp    |  6 +--
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        | 49 +++++++++++++------
 .../CLookUp_ANN_tests.cpp                     | 17 ++++---
 10 files changed, 87 insertions(+), 65 deletions(-)

diff --git a/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp b/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
index 8d0c97aa696..d4494cc0aad 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
@@ -95,7 +95,7 @@ namespace MLPToolbox
         * \param[in] inputs - Input names for the call function. These should match with at least one of the MLP inputs.
         * \param[in] outputs - Output names for the call function. These should match with at least one of the MLP outputs.
         */
-        CIOMap(CLookUp_ANN*MLP_collection, std::vector<std::string> &inputs, std::vector<std::string> &outputs);
+        CIOMap(CLookUp_ANN*MLP_collection, su2vector<std::string> &inputs, su2vector<std::string> &outputs);
 
         /*!
         * \brief Set MLP index in IO map
@@ -110,7 +110,7 @@ namespace MLPToolbox
         * \param[in] inputs - vector with call input variable names
         * \param[in] outputs - vector with call output variable names
         */
-        void PairVariableswithMLPs(CLookUp_ANN * MLP_collection, std::vector<std::string> &inputs, std::vector<std::string> &outputs);
+        void PairVariableswithMLPs(CLookUp_ANN * MLP_collection, su2vector<std::string> &inputs, su2vector<std::string> &outputs);
 
         /*!
         * \brief Get the number of MLPs in the current IO map
@@ -175,8 +175,8 @@ namespace MLPToolbox
         * \param[in] inputs - call inputs
         * \return Vector with call inputs in the correct order of the loaded MLP
         */
-        std::vector<su2double> GetMLP_Inputs(std::size_t i_Map, std::vector<su2double>&inputs) const {
-            std::vector<su2double> MLP_input;
+        su2vector<su2double> GetMLP_Inputs(std::size_t i_Map, su2vector<su2double>&inputs) const {
+            su2vector<su2double> MLP_input;
             MLP_input.resize(Input_Map[i_Map].size());
 
             for(std::size_t i_Input=0; i_Input<Input_Map[i_Map].size(); i_Input++){
diff --git a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
index 92566312809..e3e760451ca 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
@@ -46,7 +46,7 @@ class CLayer
 public:
     CLayer();
     CLayer(unsigned long n_neurons);
-
+    ~CLayer(){delete neurons;}
     /*!
     * \brief Set current layer neuron count
     * \param[in] n_neurons - Number of neurons in this layer
diff --git a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
index f2306470a98..ae8392965a0 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
@@ -55,7 +55,7 @@ class CLookUp_ANN
 
     private:
     int rank{0};
-    std::vector<CNeuralNetwork*> NeuralNetworks;  /*!< std::vector containing all loaded neural networks. */
+    su2vector<CNeuralNetwork*> NeuralNetworks;  /*!< std::vector containing all loaded neural networks. */
 
     std::vector<std::string> ANN_filenames;       /*!< Filenames containing ANN architecture information. */
 
@@ -96,10 +96,10 @@ class CLookUp_ANN
     * \param[in] inputs - input values
     * \param[in] outputs - pointers to output variables
     */
-    void Predict_ANN(CIOMap *input_output_map, std::vector<su2double> &inputs, std::vector<su2double*> &outputs);
+    void Predict_ANN(CIOMap *input_output_map, su2vector<su2double> &inputs, su2vector<su2double*> &outputs);
 
     ~CLookUp_ANN(){for(std::size_t i_ANN=0; i_ANN<number_of_variables; i_ANN++)
-        delete NeuralNetworks.at(i_ANN);
+        delete NeuralNetworks[i_ANN];
     };
 
     /*!
@@ -113,21 +113,21 @@ class CLookUp_ANN
     * \param[in] output_names - output variable names to check
     * \param[in] input_output_map - pointer to input-output map to be checked
     */
-    bool Check_Duplicate_Outputs(std::vector<std::string> &output_names, CIOMap *input_output_map) const;
+    bool Check_Duplicate_Outputs(su2vector<std::string> &output_names, CIOMap *input_output_map) const;
 
     /*!
     * \brief Check if all output variables are present in the loaded ANNs
     * \param[in] output_names - output variable names to check
     * \param[in] input_output_map - pointer to input-output map to be checked
     */
-    bool Check_Use_of_Outputs(std::vector<std::string> &output_names, CIOMap *input_output_map) const;
+    bool Check_Use_of_Outputs(su2vector<std::string> &output_names, CIOMap *input_output_map) const;
 
     /*!
     * \brief Check if all input variables are present in the loaded ANNs
     * \param[in] input_names - input variable names to check
     * \param[in] input_output_map - pointer to input-output map to be checked
     */
-    bool Check_Use_of_Inputs(std::vector<std::string> &input_names, CIOMap *input_output_map) const;
+    bool Check_Use_of_Inputs(su2vector<std::string> &input_names, CIOMap *input_output_map) const;
 
     /*!
     * \brief Map variable names to ANN inputs or outputs
@@ -135,7 +135,7 @@ class CLookUp_ANN
     * \param[in] variable_names - variable names to map to ANN inputs or outputs
     * \param[in] input - map to inputs (true) or outputs (false)
     */
-    std::vector<pair<std::size_t, std::size_t>> FindVariable_Indices(std::size_t i_ANN, std::vector<std::string> variable_names, bool input) const;
+    std::vector<pair<std::size_t, std::size_t>> FindVariable_Indices(std::size_t i_ANN, su2vector<std::string> variable_names, bool input) const;
     
 };  
 
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
index c5aa90c30fc..66466db5308 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
@@ -49,15 +49,15 @@ class CNeuralNetwork
     CLayer *inputLayer,     // Pointer to network input layer.
            *outputLayer;    // Pointer to network output layer.
 
-    std::vector<CLayer*> hiddenLayers,  // Hidden layer collection.
-                         total_layers;  // Hidden layers plus in/output layers
+    std::vector<CLayer*> hiddenLayers;  // Hidden layer collection.
+    su2vector<CLayer*>   total_layers;  // Hidden layers plus in/output layers
 
-    std::vector<su2activematrix> weights_mat;   // Weights of synapses connecting layers
+    su2vector<su2activematrix> weights_mat;   // Weights of synapses connecting layers
 
-    std::vector<std::pair<su2double, su2double>> input_norm,    // Normalization factors for network inputs
+    su2vector<std::pair<su2double, su2double>> input_norm,    // Normalization factors for network inputs
                                                  output_norm;   // Normalization factors for network outputs
 
-    std::vector<su2double> last_inputs; // Inputs from previous lookup operation. Evaluation of the network 
+    su2vector<su2double> last_inputs; // Inputs from previous lookup operation. Evaluation of the network 
                                         // is skipped if current inputs are the same as the last inputs.
 
     su2double* ANN_outputs; // Pointer to network outputs
@@ -121,7 +121,7 @@ class CNeuralNetwork
     * \param[in] i_neuron - Neuron index of current layer.
     * \param[in] value - Bias value.
     */
-    void setBias(unsigned long i_layer, unsigned long i_neuron, su2double value){total_layers.at(i_layer)->setBias(i_neuron, value);}
+    void setBias(unsigned long i_layer, unsigned long i_neuron, su2double value){total_layers[i_layer]->setBias(i_neuron, value);}
 
     /*!
     * \brief Set layer activation function.
@@ -144,7 +144,7 @@ class CNeuralNetwork
     * \brief Size the vector of previous inputs.
     * \param[in] n_inputs - Number of inputs.
     */
-    void sizeInputs(unsigned long n_inputs) { last_inputs.resize(n_inputs); for(unsigned long iInput=0; iInput<n_inputs; iInput++) last_inputs.at(iInput) = 0.0; }
+    void sizeInputs(unsigned long n_inputs) { last_inputs.resize(n_inputs); for(unsigned long iInput=0; iInput<n_inputs; iInput++) last_inputs[iInput] = 0.0; }
     
     /*!
     * \brief Get the number of connecting regions in the network.
@@ -163,12 +163,12 @@ class CNeuralNetwork
     * \param[in] iLayer - Layer index.
     * \returns number of neurons in the layer.
     */
-    unsigned long getNNeurons(unsigned long iLayer) { return total_layers.at(iLayer)->getNNeurons(); }
+    unsigned long getNNeurons(unsigned long iLayer) { return total_layers[iLayer]->getNNeurons(); }
 
     /*!
     * \brief Evaluate the network.
     */
-    void predict(std::vector<su2double> &inputs);
+    void predict(su2vector<su2double> &inputs);
 
     /*!
     * \brief Set the normalization factors for the input layer
@@ -176,7 +176,7 @@ class CNeuralNetwork
     * \param[in] input_min - Minimum input value.
     * \param[in] input_max - Maximum input value.
     */
-    void SetInputNorm(unsigned long iInput, su2double input_min, su2double input_max) { input_norm.at(iInput) = make_pair(input_min, input_max); }
+    void SetInputNorm(unsigned long iInput, su2double input_min, su2double input_max) { input_norm[iInput] = make_pair(input_min, input_max); }
 
     /*!
     * \brief Set the normalization factors for the output layer
@@ -184,7 +184,7 @@ class CNeuralNetwork
     * \param[in] input_min - Minimum output value.
     * \param[in] input_max - Maximum output value.
     */
-    void SetOutputNorm(unsigned long iOutput, su2double output_min, su2double output_max){ output_norm.at(iOutput) = make_pair(output_min, output_max); }
+    void SetOutputNorm(unsigned long iOutput, su2double output_min, su2double output_max){ output_norm[iOutput] = make_pair(output_min, output_max); }
     
     /*!
     * \brief Add an output variable name to the network.
diff --git a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
index 36d08a081db..f1cc8f00bb4 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
@@ -32,7 +32,7 @@
 #include <cmath>
 #include <fstream>
 
-MLPToolbox::CIOMap::CIOMap(CLookUp_ANN*MLP_collection, vector<string> &inputs, vector<string> &outputs){
+MLPToolbox::CIOMap::CIOMap(CLookUp_ANN*MLP_collection, su2vector<std::string> &inputs, su2vector<std::string> &outputs){
     /* Generate an input-output map given a set of call inputs and call outputs. These inputs are 
     mapped to the inputs of the loaded MLPs in the MLP_collection object. The call outputs are 
     then matched to the MLPs with matching inputs.
@@ -51,7 +51,7 @@ MLPToolbox::CIOMap::CIOMap(CLookUp_ANN*MLP_collection, vector<string> &inputs, v
         //MLP_collection->Check_Duplicate_Outputs(outputs, this);
     }
 }
-void MLPToolbox::CIOMap::PairVariableswithMLPs(CLookUp_ANN*MLP_collection, vector<string> &inputs, vector<string> &outputs){
+void MLPToolbox::CIOMap::PairVariableswithMLPs(CLookUp_ANN*MLP_collection, su2vector<std::string> &inputs, su2vector<std::string> &outputs){
     /*
     In this function, the call inputs and outputs are matched to those within the MLP collection. 
     */
@@ -61,13 +61,13 @@ void MLPToolbox::CIOMap::PairVariableswithMLPs(CLookUp_ANN*MLP_collection, vecto
     for(size_t i_MLP=0; i_MLP<MLP_collection->GetNANNs(); i_MLP++){
 
         // Mapped call inputs to MLP inputs
-        vector<pair<size_t, size_t>> Input_Indices = MLP_collection->FindVariable_Indices(i_MLP, inputs, true);
+        std::vector<pair<size_t, size_t>> Input_Indices = MLP_collection->FindVariable_Indices(i_MLP, inputs, true);
         isInput = Input_Indices.size() > 0;
 
         if(isInput){
             // Only when the MLP inputs match with a portion of the call inputs are the output variable checks performed
 
-            vector<pair<size_t, size_t>> Output_Indices = MLP_collection->FindVariable_Indices(i_MLP, outputs, false);
+            std::vector<pair<size_t, size_t>> Output_Indices = MLP_collection->FindVariable_Indices(i_MLP, outputs, false);
             isOutput = Output_Indices.size() > 0;
 
             if(isOutput){
diff --git a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
index 4642a8a9bd4..77c7a062f7e 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
@@ -47,15 +47,15 @@ MLPToolbox::CLookUp_ANN::CLookUp_ANN(string inputFileName)
     ReadANNInputFile(inputFileName);
     for(size_t i_ANN=0; i_ANN<number_of_variables; i_ANN++){
         
-        NeuralNetworks.at(i_ANN) = new CNeuralNetwork;
+        NeuralNetworks[i_ANN] = new CNeuralNetwork;
         if(rank == MASTER_NODE)
             cout << "Generating neural network for " << ANN_filenames.at(i_ANN) << endl;
-        GenerateANN(NeuralNetworks.at(i_ANN), ANN_filenames.at(i_ANN));
+        GenerateANN(NeuralNetworks[i_ANN], ANN_filenames.at(i_ANN));
     }
 }
 
 
-vector<pair<size_t, size_t>> MLPToolbox::CLookUp_ANN::FindVariable_Indices(size_t i_ANN, vector<string> variable_names, bool input) const {
+vector<pair<size_t, size_t>> MLPToolbox::CLookUp_ANN::FindVariable_Indices(size_t i_ANN, su2vector<string> variable_names, bool input) const {
     vector<pair<size_t, size_t>> variable_indices;
     size_t nVar = input ? NeuralNetworks[i_ANN]->GetnInputs() : NeuralNetworks[i_ANN]->GetnOutputs();
 
@@ -63,7 +63,7 @@ vector<pair<size_t, size_t>> MLPToolbox::CLookUp_ANN::FindVariable_Indices(size_
         for(size_t jVar=0; jVar<variable_names.size(); jVar++){
             string ANN_varname = input ? NeuralNetworks[i_ANN]->GetInputName(iVar) : NeuralNetworks[i_ANN]->GetOutputName(iVar);
             
-            if(variable_names.at(jVar).compare(ANN_varname) == 0){
+            if(variable_names[jVar].compare(ANN_varname) == 0){
                 variable_indices.push_back(make_pair(jVar, iVar));
                 //cout << variable_names[jVar] << " : " << jVar << " | " << ANN_varname << " : " << iVar << endl;
             }
@@ -72,10 +72,10 @@ vector<pair<size_t, size_t>> MLPToolbox::CLookUp_ANN::FindVariable_Indices(size_
     return variable_indices;
 }
 
-void MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap *input_output_map, vector<su2double>& inputs, vector<su2double*>& outputs){
+void MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap *input_output_map, su2vector<su2double>& inputs, su2vector<su2double*>& outputs){
     for(size_t i_map=0; i_map<input_output_map->GetNMLPs(); i_map++){
         size_t i_ANN = input_output_map->GetMLPIndex(i_map);
-        vector<su2double> ANN_inputs = input_output_map->GetMLP_Inputs(i_map, inputs);
+        su2vector<su2double> ANN_inputs = input_output_map->GetMLP_Inputs(i_map, inputs);
         NeuralNetworks[i_ANN]->predict(ANN_inputs);
         for(size_t i=0; i < input_output_map->GetNMappedOutputs(i_map); i++){
             *outputs[input_output_map->GetOutputIndex(i_map, i)] = NeuralNetworks[i_ANN]->GetANN_Output(input_output_map->GetMLPOutputIndex(i_map, i));
@@ -181,7 +181,7 @@ string MLPToolbox::CLookUp_ANN::SkipToFlag(ifstream *file_stream, string flag) {
 }
 
 
-bool MLPToolbox::CLookUp_ANN::Check_Duplicate_Outputs(vector<string> &output_names, CIOMap *input_output_map) const {
+bool MLPToolbox::CLookUp_ANN::Check_Duplicate_Outputs(su2vector<string> &output_names, CIOMap *input_output_map) const {
     unsigned short n_occurances;
     bool duplicate{false};
     vector<string> duplicate_variables;
@@ -208,7 +208,7 @@ bool MLPToolbox::CLookUp_ANN::Check_Duplicate_Outputs(vector<string> &output_nam
 }
 
 
-bool MLPToolbox::CLookUp_ANN::Check_Use_of_Inputs(vector<string> &input_names, CIOMap *input_output_map) const {
+bool MLPToolbox::CLookUp_ANN::Check_Use_of_Inputs(su2vector<string> &input_names, CIOMap *input_output_map) const {
 vector<string> missing_inputs;
 bool inputs_are_present{true};
 for(size_t iInput=0; iInput<input_names.size(); iInput ++){
@@ -234,7 +234,7 @@ if(missing_inputs.size() > 0){
 return inputs_are_present;
 }
 
-bool MLPToolbox::CLookUp_ANN::Check_Use_of_Outputs(vector<string> &output_names, CIOMap * input_output_map) const {
+bool MLPToolbox::CLookUp_ANN::Check_Use_of_Outputs(su2vector<string> &output_names, CIOMap * input_output_map) const {
     /* Check wether all output variables are in the loaded MLPs */
     
     vector<string> missing_outputs;     
diff --git a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
index ebc712e15e5..96bd5879d4c 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
@@ -32,7 +32,7 @@
 using namespace std;
 
 
-void MLPToolbox::CNeuralNetwork::predict(vector<su2double> &inputs){
+void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
     su2double x, x_norm, y, y_norm;
     size_t iNeuron, iLayer, nNeurons_current;
     bool same_point{true};
@@ -182,11 +182,11 @@ void MLPToolbox::CNeuralNetwork::push_hidden_layer(unsigned long n_neurons){
 void MLPToolbox::CNeuralNetwork::sizeWeights(){
     
     total_layers.resize(n_hidden_layers + 2);
-    total_layers.at(0) = inputLayer;
+    total_layers[0] = inputLayer;
     for(size_t iLayer=0; iLayer<n_hidden_layers; iLayer++){
-        total_layers.at(iLayer + 1) = hiddenLayers.at(iLayer);
+        total_layers[iLayer + 1] = hiddenLayers.at(iLayer);
     }
-    total_layers.at(total_layers.size()-1) = outputLayer;
+    total_layers[total_layers.size()-1] = outputLayer;
 
     weights_mat.resize(n_hidden_layers+1);
     weights_mat[0].resize(hiddenLayers[0]->getNNeurons(), inputLayer->getNNeurons());
diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index deb893edd6b..c2d520a33d1 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -58,15 +58,15 @@ class CDataDrivenFluid : public CFluidModel {
   su2double Gamma_Minus_One{0.0}; /*!< \brief Ratio of Specific Heats Minus One. */
   su2double Gas_Constant{0.0};    /*!< \brief Gas Constant. */
   
-  vector<string> input_names_rhoe,        // Data-driven method input variable names of the independent variables (density, energy).
+  su2vector<string> input_names_rhoe,        // Data-driven method input variable names of the independent variables (density, energy).
                  output_names_rhoe;       // Output variable names listed in the data-driven method input file name.
 
-  vector<su2double*> outputs_rhoe;        // Pointers to output variables.
+  su2vector<su2double*> outputs_rhoe;        // Pointers to output variables.
 
   /*--- Class variables for the multi-layer perceptron method ---*/
   MLPToolbox::CLookUp_ANN * lookup_mlp;   // multi-layer perceptron collection.
   MLPToolbox::CIOMap * iomap_rhoe;        // input-output map.
-  vector<su2double> MLP_inputs;           // inputs for the multi-layer perceptron look-up operation.
+  su2vector<su2double> MLP_inputs;           // inputs for the multi-layer perceptron look-up operation.
 
   /*--- Class variables for the look-up table method ---*/
   CLookUpTable *lookup_table;
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index f3f26e9c8eb..4c65ecd49ef 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -81,24 +81,34 @@ CDataDrivenFluid::~CDataDrivenFluid(){
 void CDataDrivenFluid::MapInputs_to_Outputs(){
 
   /*--- Inputs of the data-driven method are density and internal energy. ---*/
-  input_names_rhoe.push_back("Density");
+  input_names_rhoe.resize(2);
   idx_rho = 0;
-  input_names_rhoe.push_back("Energy");
   idx_e = 1;
+  input_names_rhoe[idx_rho] = "Density";
+  input_names_rhoe[idx_e] = "Energy";
 
   /*--- Required outputs for the interpolation method are entropy and its partial derivatives with respect to energy and density ---*/
-  output_names_rhoe.push_back("s");
-  outputs_rhoe.push_back(&Entropy);
-  output_names_rhoe.push_back("dsde_rho");
-  outputs_rhoe.push_back(&dsde_rho);
-  output_names_rhoe.push_back("dsdrho_e");
-  outputs_rhoe.push_back(&dsdrho_e);
-  output_names_rhoe.push_back("d2sde2");
-  outputs_rhoe.push_back(&d2sde2);
-  output_names_rhoe.push_back("d2sdedrho");
-  outputs_rhoe.push_back(&d2sdedrho);
-  output_names_rhoe.push_back("d2sdrho2");
-  outputs_rhoe.push_back(&d2sdrho2);
+  size_t n_outputs = 6;
+  size_t idx_s = 0, 
+         idx_dsde_rho = 1, 
+         idx_dsdrho_e = 2,
+         idx_d2sde2 = 3,
+         idx_d2sdedrho = 4,
+         idx_d2sdrho2 = 5;
+
+  output_names_rhoe.resize(n_outputs); 
+  output_names_rhoe[idx_s] = "s";
+  outputs_rhoe[idx_s] = &Entropy;
+  output_names_rhoe[idx_dsde_rho] = "dsde_rho";
+  outputs_rhoe[idx_dsde_rho] = &dsde_rho;
+  output_names_rhoe[idx_dsdrho_e] = "dsdrho_e";
+  outputs_rhoe[idx_dsdrho_e] = &dsdrho_e;
+  output_names_rhoe[idx_d2sde2] = "d2sde2";
+  outputs_rhoe[idx_d2sde2] = &d2sde2;
+  output_names_rhoe[idx_d2sdedrho] = "d2sdedrho";
+  outputs_rhoe[idx_d2sdedrho] = &d2sdedrho;
+  output_names_rhoe[idx_d2sdrho2] = "d2sdrho2";
+  outputs_rhoe[idx_d2sdrho2] = &d2sdrho2;
 
   /*--- Further preprocessing of input and output variables ---*/
   switch (Kind_DataDriven_Method)
@@ -117,6 +127,8 @@ void CDataDrivenFluid::MapInputs_to_Outputs(){
 void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
   Density = rho;
   StaticEnergy = e;
+  std::vector<std::string> output_names_rhoe_LUT;
+  std::vector<su2double*> outputs_LUT;
   switch (Kind_DataDriven_Method)
   {
   case ENUM_DATADRIVEN_METHOD::MLP:
@@ -128,7 +140,14 @@ void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
     lookup_mlp->Predict_ANN(iomap_rhoe, MLP_inputs, outputs_rhoe);
     break;
   case ENUM_DATADRIVEN_METHOD::LUT:
-    lookup_table->LookUp_ProgEnth(output_names_rhoe, outputs_rhoe, rho, e, "Density", "Energy");
+
+    output_names_rhoe_LUT.resize(output_names_rhoe.size());
+    for(size_t iOutput=0; iOutput<output_names_rhoe.size(); iOutput++) { output_names_rhoe_LUT[iOutput] = output_names_rhoe[iOutput]; }
+
+    outputs_LUT.resize(outputs_rhoe.size());
+    for(size_t iOutput=0; iOutput<outputs_rhoe.size(); iOutput++) { outputs_LUT[iOutput] = outputs_rhoe[iOutput]; }
+
+    lookup_table->LookUp_ProgEnth(output_names_rhoe_LUT, outputs_LUT, rho, e, "Density", "Energy");
   default:
     break;
   }
diff --git a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
index 2c61c44fa44..f2ec5387764 100644
--- a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
+++ b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
@@ -33,19 +33,22 @@
 TEST_CASE("LookUp ANN test", "[LookUpANN]"){
 
   MLPToolbox::CLookUp_ANN ANN("src/SU2/UnitTests/Common/toolboxes/multilayer_perceptron/mlp_collection.mlp");
-  std::vector<std::string> MLP_input_names,
+  su2vector<std::string> MLP_input_names,
                            MLP_output_names;
-  std::vector<su2double> MLP_inputs;
-  std::vector<su2double*> MLP_outputs;
+  su2vector<su2double> MLP_inputs;
+  su2vector<su2double*> MLP_outputs;
   su2double x,y,z;
 
   /*--- Define MLP inputs and outputs ---*/
-  MLP_input_names.push_back("x");
-  MLP_input_names.push_back("y");
+  MLP_input_names.resize(2);
+  MLP_input_names[0] = "x";
+  MLP_input_names[1] = "y";
   MLP_inputs.resize(2);
 
-  MLP_output_names.push_back("z");
-  MLP_outputs.push_back(&z);
+  MLP_outputs.resize(1);
+  MLP_output_names.resize(1);
+  MLP_output_names[0] = "z";
+  MLP_outputs[0] = &z;
 
   /*--- Generate input-output map ---*/
   MLPToolbox::CIOMap iomap(&ANN, MLP_input_names, MLP_output_names);

From bbf884d15a293604df358fa3eab274b1ae15bd40 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 25 Nov 2022 14:20:33 +0100
Subject: [PATCH 052/656] implemented delete statements for unreleased
 resources

---
 Common/src/containers/CLookUpTable.cpp | 3 +++
 1 file changed, 3 insertions(+)

diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index 5c096528fac..bf3a2431720 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -88,6 +88,9 @@ CLookUpTable::~CLookUpTable()
   delete [] interp_mat_inv_x_y;
   delete [] edges;
   delete [] edge_to_triangle;
+  delete [] limits_table_x;
+  delete [] limits_table_y;
+  if(z_values_levels != nullptr) delete z_values_levels;
 }
 
 void CLookUpTable::LoadTableRaw(const string& var_file_name_lut) {

From 84bef02c7f18a15310d688e9397b3ee5aeda4abb Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 25 Nov 2022 16:05:27 +0100
Subject: [PATCH 053/656] Fixed some more alerts

---
 Common/src/containers/CLookUpTable.cpp | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index bf3a2431720..5aa626924cb 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -90,7 +90,7 @@ CLookUpTable::~CLookUpTable()
   delete [] edge_to_triangle;
   delete [] limits_table_x;
   delete [] limits_table_y;
-  if(z_values_levels != nullptr) delete z_values_levels;
+  if(z_values_levels != nullptr) delete [] z_values_levels;
 }
 
 void CLookUpTable::LoadTableRaw(const string& var_file_name_lut) {
@@ -455,7 +455,7 @@ void CLookUpTable::Linear_Interpolation(su2double val_z, std::pair<unsigned long
   su2double factor_upper = (val_z - val_z_lower) / (val_z_upper - val_z_lower);
   su2double factor_lower = (val_z_upper - val_z) / (val_z_upper - val_z_lower);
 
-  for(unsigned short iVar=0; iVar<var_vals.size(); iVar++){
+  for(size_t iVar=0; iVar<var_vals.size(); iVar++){
     *var_vals[iVar] = lower_values[iVar] * factor_lower + upper_values[iVar] * factor_upper;
   }
 }

From b09022375406a7af62bea3da1ac1e33c4ac0dbbb Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Thu, 1 Dec 2022 14:53:07 +0100
Subject: [PATCH 054/656] Added MLP-driven fluid model test case and fixed
 build error

---
 .github/workflows/regression.yml              |  2 +-
 .../multilayer_perceptron/CLayer.hpp          |  2 +-
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        |  1 +
 .../nicf/datadriven/datadriven_nozzle.cfg     | 28 ++++++++++---------
 TestCases/parallel_regression.py              |  7 +++++
 5 files changed, 25 insertions(+), 15 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 8e2d4414353..ed2f35d4e93 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:220614-1237
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c feature_multilayer_perceptron -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:220614-1237
         with:
diff --git a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
index e3e760451ca..32d71d26d94 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
@@ -46,7 +46,7 @@ class CLayer
 public:
     CLayer();
     CLayer(unsigned long n_neurons);
-    ~CLayer(){delete neurons;}
+    ~CLayer(){delete [] neurons;}
     /*!
     * \brief Set current layer neuron count
     * \param[in] n_neurons - Number of neurons in this layer
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 4c65ecd49ef..126a3245bb6 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -96,6 +96,7 @@ void CDataDrivenFluid::MapInputs_to_Outputs(){
          idx_d2sdedrho = 4,
          idx_d2sdrho2 = 5;
 
+  outputs_rhoe.resize(n_outputs);
   output_names_rhoe.resize(n_outputs); 
   output_names_rhoe[idx_s] = "s";
   outputs_rhoe[idx_s] = &Entropy;
diff --git a/TestCases/nicf/datadriven/datadriven_nozzle.cfg b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
index 12dfc48d026..b9a70862135 100644
--- a/TestCases/nicf/datadriven/datadriven_nozzle.cfg
+++ b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
@@ -2,9 +2,10 @@
 %                                                                              %
 % SU2 configuration file                                                       %
 % Case description: Non-ideal compressible fluid flow in a converging-         %
-%                   diverging supersonic nozzle with CoolProp library          %
-% Author: Peng Yan, Alberto Guardone                                           %
-% Institution: Politecnico di Milano                                           %
+%                   diverging supersonic nozzle using a multi-layer perceptron %
+%                   for thermodynamic state calculations.                      %
+% Author: Evert Bunschoten                                                     %
+% Institution: Delft University of Technology                                  %
 % Date: 2022.10.8                                                              %
 % File Version  7.4.0 Blackbird                                                %
 %                                                                              %
@@ -14,7 +15,7 @@
 SOLVER= RANS
 KIND_TURB_MODEL= SST
 MATH_PROBLEM= DIRECT
-RESTART_SOL= YES
+RESTART_SOL= NO
 SYSTEM_MEASUREMENTS= SI
 %
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
@@ -24,11 +25,12 @@ MACH_NUMBER= 1E-9
 AOA= 0.0
 SIDESLIP_ANGLE= 0.0
 INIT_OPTION= TD_CONDITIONS
-FREESTREAM_OPTION= TEMPERATURE_FS
+FREESTREAM_OPTION= DENSITY_FS
 FREESTREAM_PRESSURE= 904388
 %
 % Free-stream temperature (288.15 K, 518.67 R by default)
 FREESTREAM_TEMPERATURE= 542.13
+FREESTREAM_DENSITY= 5.54548
 REF_DIMENSIONALIZATION= DIMENSIONAL
 
 % ---- DATADRIVEN FLUID MODEL DEFINITION -------%
@@ -36,9 +38,9 @@ REF_DIMENSIONALIZATION= DIMENSIONAL
 FLUID_MODEL = DATADRIVEN_FLUID
 INTERPOLATION_METHOD = MLP 
 FILENAME_INTERPOLATOR = mlp_collection.mlp 
-DATADRIVEN_NEWTON_RELAXATION = 0.02
-DATADRIVEN_FLUID_INITIAL_DENSITY = 8.20106
-DATADRIVEN_FLUID_INITIAL_ENERGY = 4.19552e+05
+DATADRIVEN_NEWTON_RELAXATION = 0.06
+DATADRIVEN_FLUID_INITIAL_DENSITY = 5.54548
+DATADRIVEN_FLUID_INITIAL_ENERGY = 1.8e+05
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
@@ -51,7 +53,7 @@ THERMAL_CONDUCTIVITY_CONSTANT= 0.030542828
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 MARKER_HEATFLUX= ( WALL, 0.0 )
 MARKER_SYM= ( SYMMETRY )
-MARKER_RIEMANN= ( INFLOW, TOTAL_CONDITIONS_PT, 904388, 542.13, 1.0, 0.0, 0.0, OUTFLOW, STATIC_PRESSURE, 200000.0, 0.0, 0.0, 0.0, 0.0 )
+MARKER_RIEMANN= ( INFLOW, TOTAL_CONDITIONS_PT,  904388, 542.13, 1.0, 0.0, 0.0, OUTFLOW, STATIC_PRESSURE, 200000.0, 0.0, 0.0, 0.0, 0.0 )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 NUM_METHOD_GRAD= GREEN_GAUSS
@@ -61,7 +63,7 @@ CFL_ADAPT_PARAM= ( 0.1, 2.0, 10.0, 1000.0 )
 MAX_DELTA_TIME= 1E6
 
 % ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
-MUSCL_FLOW= YES
+MUSCL_FLOW= NO
 SLOPE_LIMITER_FLOW= NONE
 MUSCL_TURB= NO
 
@@ -90,14 +92,14 @@ CFL_REDUCTION_TURB= 1.0
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
 % Number of total iterations
-ITER= 101
+ITER= 51
 CONV_RESIDUAL_MINVAL= -24
 CONV_STARTITER= 10
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
 % Mesh input file
-MESH_FILENAME= ../coolprop/coolprop_nozzle.su2
+MESH_FILENAME= coolprop_nozzle.su2
 %
 % Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
@@ -122,7 +124,7 @@ VOLUME_FILENAME= flow
 SURFACE_FILENAME= surface_flow
 %
 % Writing solution file frequency
-OUTPUT_WRT_FREQ= 50
+OUTPUT_WRT_FREQ= 10
 %
 % Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG)
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 75833a37f67..a97977af46b 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -930,6 +930,13 @@ def main():
     coolprop_transportModel.test_vals = [-4.527922, -1.308741, 4.630469, 0.000000, 0.000000]
     test_list.append(coolprop_transportModel)
 
+    datadriven_MLP           = TestCase('datadriven_MLP')
+    datadriven_MLP.cfg_dir   = "nicf/datadriven"
+    datadriven_MLP.cfg_file  = "datadriven_nozzle.cfg"
+    datadriven_MLP.test_iter = 100
+    datadriven_MLP.test_vals = [-3.419718, -2.279820, 3.423614, 0.000000, 0.000000]
+    test_list.append(datadriven_MLP)
+
     ######################################
     ### Turbomachinery                 ###
     ######################################

From 2f82b5d1e5b9e19b68ac0bb12bc61e22aca07113 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Thu, 1 Dec 2022 14:55:03 +0100
Subject: [PATCH 055/656] Added MLP-driven fluid model test case

---
 .github/workflows/regression.yml | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index ed2f35d4e93..8e2d4414353 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:220614-1237
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c feature_multilayer_perceptron -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:220614-1237
         with:

From 7eb2180c43d6a2a9778a50ced41c62a064f4c551 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Thu, 1 Dec 2022 15:02:11 +0100
Subject: [PATCH 056/656] Changed test case branch in runTests.sh to allow
 access to MLP fluid model test case

---
 docker/test/Dockerfile | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/docker/test/Dockerfile b/docker/test/Dockerfile
index dd168ef4965..8be2bd24c8e 100644
--- a/docker/test/Dockerfile
+++ b/docker/test/Dockerfile
@@ -4,4 +4,4 @@ FROM su2code/build-su2:20191029
 COPY runTests.sh /runTests.sh
 
 # Code file to execute when the docker container starts up (`entrypoint.sh`)
-ENTRYPOINT ["/runTests.sh"]
+ENTRYPOINT ["/runTests.sh -c feature_multilayer_perceptron"]

From f4323a307a9977bd78ad68841a83aaec0bd34bc7 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Thu, 1 Dec 2022 16:15:09 +0100
Subject: [PATCH 057/656] Added range check to MLP evaluation

---
 .../multilayer_perceptron/CLookUp_ANN.hpp     |  3 ++-
 .../multilayer_perceptron/CNeuralNetwork.hpp  |  3 +++
 .../multilayer_perceptron/CLookUp_ANN.cpp     | 23 +++++++++++++++----
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp    |  2 ++
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        |  6 +++--
 .../nicf/datadriven/datadriven_nozzle.cfg     |  8 +++----
 6 files changed, 34 insertions(+), 11 deletions(-)

diff --git a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
index ae8392965a0..7734c38a01b 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
@@ -95,8 +95,9 @@ class CLookUp_ANN
     * \param[in] input_output_map - input-output map coupling desired inputs and outputs to loaded ANNs
     * \param[in] inputs - input values
     * \param[in] outputs - pointers to output variables
+    * \returns Within output normalization range.
     */
-    void Predict_ANN(CIOMap *input_output_map, su2vector<su2double> &inputs, su2vector<su2double*> &outputs);
+    unsigned long Predict_ANN(CIOMap *input_output_map, su2vector<su2double> &inputs, su2vector<su2double*> &outputs);
 
     ~CLookUp_ANN(){for(std::size_t i_ANN=0; i_ANN<number_of_variables; i_ANN++)
         delete NeuralNetworks[i_ANN];
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
index 66466db5308..1acdc182e46 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
@@ -186,6 +186,9 @@ class CNeuralNetwork
     */
     void SetOutputNorm(unsigned long iOutput, su2double output_min, su2double output_max){ output_norm[iOutput] = make_pair(output_min, output_max); }
     
+    std::pair<su2double, su2double> GetInputNorm(unsigned long iInput) const { return input_norm[iInput]; }
+
+    std::pair<su2double, su2double> GetOutputNorm(unsigned long iOutput) const { return output_norm[iOutput]; }
     /*!
     * \brief Add an output variable name to the network.
     * \param[in] input - Input variable name.
diff --git a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
index 77c7a062f7e..74d82f22a9f 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
@@ -72,16 +72,31 @@ vector<pair<size_t, size_t>> MLPToolbox::CLookUp_ANN::FindVariable_Indices(size_
     return variable_indices;
 }
 
-void MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap *input_output_map, su2vector<su2double>& inputs, su2vector<su2double*>& outputs){
+unsigned long MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap *input_output_map, su2vector<su2double>& inputs, su2vector<su2double*>& outputs){
+    bool within_range,
+         MLP_was_evaluated = false;
     for(size_t i_map=0; i_map<input_output_map->GetNMLPs(); i_map++){
+        within_range = true;
         size_t i_ANN = input_output_map->GetMLPIndex(i_map);
         su2vector<su2double> ANN_inputs = input_output_map->GetMLP_Inputs(i_map, inputs);
-        NeuralNetworks[i_ANN]->predict(ANN_inputs);
-        for(size_t i=0; i < input_output_map->GetNMappedOutputs(i_map); i++){
-            *outputs[input_output_map->GetOutputIndex(i_map, i)] = NeuralNetworks[i_ANN]->GetANN_Output(input_output_map->GetMLPOutputIndex(i_map, i));
+        
+        for(size_t i_input=0; i_input < ANN_inputs.size(); i_input++) {
+            std::pair<su2double, su2double> ANN_input_limits = NeuralNetworks[i_ANN]->GetInputNorm(i_input);
+            if((ANN_inputs[i_input] < ANN_input_limits.first) || (ANN_inputs[i_input] > ANN_input_limits.second)) {
+                within_range = false;
+            }
+        }
+        if(within_range){
+            NeuralNetworks[i_ANN]->predict(ANN_inputs);
+            MLP_was_evaluated = true;
+            for(size_t i=0; i < input_output_map->GetNMappedOutputs(i_map); i++){
+                *outputs[input_output_map->GetOutputIndex(i_map, i)] = NeuralNetworks[i_ANN]->GetANN_Output(input_output_map->GetMLPOutputIndex(i_map, i));
+            }
         }
     }
+    return MLP_was_evaluated ? 0 : 1;
 }
+
 void MLPToolbox::CLookUp_ANN::GenerateANN(CNeuralNetwork * ANN, string fileName)
 {
     CReadNeuralNetwork Reader = CReadNeuralNetwork(fileName);
diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index c2d520a33d1..cb058bca7f8 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -71,6 +71,8 @@ class CDataDrivenFluid : public CFluidModel {
   /*--- Class variables for the look-up table method ---*/
   CLookUpTable *lookup_table;
 
+  unsigned long within_range;
+
   void MapInputs_to_Outputs();
 
  public:
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 126a3245bb6..29f25417c03 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -130,6 +130,7 @@ void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
   StaticEnergy = e;
   std::vector<std::string> output_names_rhoe_LUT;
   std::vector<su2double*> outputs_LUT;
+  unsigned long exit_code;
   switch (Kind_DataDriven_Method)
   {
   case ENUM_DATADRIVEN_METHOD::MLP:
@@ -138,7 +139,7 @@ void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
     MLP_inputs[idx_e]   = StaticEnergy;
 
     /* --- Evaluate MLP --- */
-    lookup_mlp->Predict_ANN(iomap_rhoe, MLP_inputs, outputs_rhoe);
+    exit_code = lookup_mlp->Predict_ANN(iomap_rhoe, MLP_inputs, outputs_rhoe);
     break;
   case ENUM_DATADRIVEN_METHOD::LUT:
 
@@ -177,7 +178,8 @@ void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
   Gamma = Cp / Cv;
   Gamma_Minus_One = Gamma - 1;
   Gas_Constant = Cp - Cv;
-  
+
+  within_range = exit_code;
 }
 
 void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
diff --git a/TestCases/nicf/datadriven/datadriven_nozzle.cfg b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
index b9a70862135..4d7bd921ef2 100644
--- a/TestCases/nicf/datadriven/datadriven_nozzle.cfg
+++ b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
@@ -26,11 +26,11 @@ AOA= 0.0
 SIDESLIP_ANGLE= 0.0
 INIT_OPTION= TD_CONDITIONS
 FREESTREAM_OPTION= DENSITY_FS
-FREESTREAM_PRESSURE= 904388
+FREESTREAM_PRESSURE= 250000.0
 %
 % Free-stream temperature (288.15 K, 518.67 R by default)
-FREESTREAM_TEMPERATURE= 542.13
-FREESTREAM_DENSITY= 5.54548
+FREESTREAM_TEMPERATURE= 400.0
+FREESTREAM_DENSITY= 2.0
 REF_DIMENSIONALIZATION= DIMENSIONAL
 
 % ---- DATADRIVEN FLUID MODEL DEFINITION -------%
@@ -53,7 +53,7 @@ THERMAL_CONDUCTIVITY_CONSTANT= 0.030542828
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 MARKER_HEATFLUX= ( WALL, 0.0 )
 MARKER_SYM= ( SYMMETRY )
-MARKER_RIEMANN= ( INFLOW, TOTAL_CONDITIONS_PT,  904388, 542.13, 1.0, 0.0, 0.0, OUTFLOW, STATIC_PRESSURE, 200000.0, 0.0, 0.0, 0.0, 0.0 )
+MARKER_RIEMANN= ( INFLOW, TOTAL_CONDITIONS_PT,  250000.0, 400, 1.0, 0.0, 0.0, OUTFLOW, STATIC_PRESSURE, 200000.0, 0.0, 0.0, 0.0, 0.0 )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 NUM_METHOD_GRAD= GREEN_GAUSS

From 3a4938d3ee6f548b01ab70021754e1aab64a28fd Mon Sep 17 00:00:00 2001
From: Evert Bunschoten <38651601+EvertBunschoten@users.noreply.github.com>
Date: Thu, 1 Dec 2022 16:30:48 +0100
Subject: [PATCH 058/656] changed regression branch to
 feature_multilayer_perceptron

---
 .github/workflows/regression.yml | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 8e2d4414353..ed2f35d4e93 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:220614-1237
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c feature_multilayer_perceptron -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:220614-1237
         with:

From 76d239ceb977c3a86e4c91885978f92c3bf5c7f4 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 2 Dec 2022 15:41:40 +0100
Subject: [PATCH 059/656] MLP evaluation is based on query data inclusion,
 addition of Newton solver iterations and dataset extrapolation to output

---
 .../multilayer_perceptron/CLookUp_ANN.cpp     | 38 +++++++-
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp    | 41 ++++++++-
 SU2_CFD/include/fluid/CFluidModel.hpp         | 12 +++
 SU2_CFD/include/variables/CVariable.hpp       | 46 ++++++++++
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        | 87 +++++++++++--------
 SU2_CFD/src/output/CFlowCompOutput.cpp        | 13 +++
 SU2_CFD/src/solvers/CEulerSolver.cpp          | 10 +++
 SU2_CFD/src/variables/CEulerVariable.cpp      |  6 ++
 TestCases/parallel_regression.py              |  1 +
 docker/test/Dockerfile                        |  2 +-
 10 files changed, 215 insertions(+), 41 deletions(-)

diff --git a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
index 74d82f22a9f..045f71ce43a 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
@@ -73,19 +73,35 @@ vector<pair<size_t, size_t>> MLPToolbox::CLookUp_ANN::FindVariable_Indices(size_
 }
 
 unsigned long MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap *input_output_map, su2vector<su2double>& inputs, su2vector<su2double*>& outputs){
-    bool within_range,
-         MLP_was_evaluated = false;
+    /*--- Evaluate MLP based on target input and output variables ---*/
+    bool within_range,              // Within MLP training set range.
+         MLP_was_evaluated = false; // MLP was evaluated within training set range.
+
+    // If queries lie outside the training data set, the nearest MLP will be evaluated through extrapolation.
+    su2double distance_to_query = 1e20; // Overall smallest distance between training data set middle and query.
+    size_t i_ANN_nearest = 0,           // Index of nearest MLP.
+           i_map_nearest = 0;           // Index of nearest iomap index.
+
     for(size_t i_map=0; i_map<input_output_map->GetNMLPs(); i_map++){
         within_range = true;
         size_t i_ANN = input_output_map->GetMLPIndex(i_map);
         su2vector<su2double> ANN_inputs = input_output_map->GetMLP_Inputs(i_map, inputs);
         
+        su2double distance_to_query_i = 0;
         for(size_t i_input=0; i_input < ANN_inputs.size(); i_input++) {
             std::pair<su2double, su2double> ANN_input_limits = NeuralNetworks[i_ANN]->GetInputNorm(i_input);
-            if((ANN_inputs[i_input] < ANN_input_limits.first) || (ANN_inputs[i_input] > ANN_input_limits.second)) {
+
+            /* Check if query input lies within MLP training range */
+            if(!((ANN_inputs[i_input] > ANN_input_limits.first) && (ANN_inputs[i_input] < ANN_input_limits.second))) {
                 within_range = false;
             }
+
+            /* Calculate distance between MLP training range center point and query */
+            su2double middle = 0.5*(ANN_input_limits.second - ANN_input_limits.first);
+            distance_to_query_i += pow((ANN_inputs[i_input] - middle)/(ANN_input_limits.second - ANN_input_limits.first), 2);
         }
+        
+        /* Evaluate MLP when query inputs lie within training data range */
         if(within_range){
             NeuralNetworks[i_ANN]->predict(ANN_inputs);
             MLP_was_evaluated = true;
@@ -93,7 +109,23 @@ unsigned long MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap *input_output_map, su2
                 *outputs[input_output_map->GetOutputIndex(i_map, i)] = NeuralNetworks[i_ANN]->GetANN_Output(input_output_map->GetMLPOutputIndex(i_map, i));
             }
         }
+
+        /* Update minimum distance to query */
+        if(sqrt(distance_to_query_i) < distance_to_query){
+            i_ANN_nearest = i_ANN;
+            distance_to_query = distance_to_query_i;
+            i_map_nearest = i_map;
+        }
     }
+    /* Evaluate nearest MLP in case no query data within range is found */
+    if(!MLP_was_evaluated) {
+        su2vector<su2double> ANN_inputs = input_output_map->GetMLP_Inputs(i_map_nearest, inputs);
+        NeuralNetworks[i_ANN_nearest]->predict(ANN_inputs);
+        for(size_t i=0; i < input_output_map->GetNMappedOutputs(i_map_nearest); i++){
+            *outputs[input_output_map->GetOutputIndex(i_map_nearest, i)] = NeuralNetworks[i_ANN_nearest]->GetANN_Output(input_output_map->GetMLPOutputIndex(i_map_nearest, i));
+        }
+    }
+
     return MLP_was_evaluated ? 0 : 1;
 }
 
diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index cb058bca7f8..4150c6f0080 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -71,10 +71,37 @@ class CDataDrivenFluid : public CFluidModel {
   /*--- Class variables for the look-up table method ---*/
   CLookUpTable *lookup_table;
 
-  unsigned long within_range;
+  unsigned long outside_dataset, // Density-energy combination lies outside data set.
+                nIter_Newton;    // Number of Newton solver iterations.
 
+  /*!
+  * \brief Map dataset variables to specific look-up operations
+  */
   void MapInputs_to_Outputs();
 
+  /*!
+  * \brief Evaluate dataset through multi-layer perceptron.
+  * \param[in] rho - Density value.
+  * \param[in] e - Static energy value.
+  * \return Query point lies outside MLP normalization range (0 is inside, 1 is outside).
+  */
+  unsigned long Predict_MLP(su2double rho, su2double e);
+
+  /*!
+  * \brief Evaluate dataset through look-up table.
+  * \param[in] rho - Density value.
+  * \param[in] e - Static energy value.
+  * \return Query point lies outside table data range (0 is inside, 1 is outside).
+  */
+  unsigned long Predict_LUT(su2double rho, su2double e);
+
+  /*!
+  * \brief Evaluate the data set.
+  * \param[in] rho - Density value.
+  * \param[in] e - Static energy value.
+  */
+  void Evaluate_Dataset(su2double rho, su2double e);
+
  public:
   /*!
    * \brief Constructor of the class.
@@ -141,4 +168,16 @@ class CDataDrivenFluid : public CFluidModel {
   * \param[in] e - Initial value for static energy.
   */
   void SetEnergy(su2double e) override {e_start = e;}
+
+  /*!
+  * \brief Get fluid model extrapolation instance
+  * \return Query point lies outside fluid model data range.
+  */
+  unsigned long GetExtrapolation() override { return outside_dataset; }
+
+  /*!
+  * \brief Get number of Newton solver iterations.
+  * \return Newton solver iteration count at termination.
+  */
+  unsigned long GetnIter_Newton() override { return nIter_Newton; }
 };
diff --git a/SU2_CFD/include/fluid/CFluidModel.hpp b/SU2_CFD/include/fluid/CFluidModel.hpp
index 4a1bc47e403..2741d55edf2 100644
--- a/SU2_CFD/include/fluid/CFluidModel.hpp
+++ b/SU2_CFD/include/fluid/CFluidModel.hpp
@@ -337,4 +337,16 @@ class CFluidModel {
   * \param[in] e - Initial value for static energy.
   */
   virtual void SetEnergy(su2double e) {}
+
+  /*!
+  * \brief Get fluid model extrapolation instance
+  * \return Query point lies outside fluid model data range.
+  */
+  virtual unsigned long GetExtrapolation() { return 0; }
+
+  /*!
+  * \brief Get number of Newton solver iterations.
+  * \return Newton solver iteration count at termination.
+  */
+  virtual unsigned long GetnIter_Newton() { return 0; }
 };
diff --git a/SU2_CFD/include/variables/CVariable.hpp b/SU2_CFD/include/variables/CVariable.hpp
index 2081e3d79fd..48578cbf472 100644
--- a/SU2_CFD/include/variables/CVariable.hpp
+++ b/SU2_CFD/include/variables/CVariable.hpp
@@ -101,6 +101,10 @@ class CVariable {
 
   VectorType SolutionExtra_BGS_k; /*!< \brief Intermediate storage, enables cross term extraction as that is also pushed to Solution. */
 
+  VectorType Dataset_Extrapolation; /*!< \brief Stores instances of dataset bounds violation when using datadriven fluid models. */
+  VectorType nIter_Newtonsolver;    /*!< \brief Stores number of Newton solver iterations when using datadriven fluid models. */
+  VectorType FluidEntropy;          /*!< \brief Stores the fluid entropy value as computed by the datadriven fluid model. */
+
  protected:
   unsigned long nPoint = 0;  /*!< \brief Number of points in the domain. */
   unsigned long nDim = 0;      /*!< \brief Number of dimension of the problem. */
@@ -2266,4 +2270,46 @@ class CVariable {
   virtual su2double GetSourceTerm_DispAdjoint(unsigned long iPoint, unsigned long iDim) const { return 0.0; }
   virtual su2double GetSourceTerm_VelAdjoint(unsigned long iPoint, unsigned long iDim) const { return 0.0; }
 
+  /*!
+    * \brief Set fluid entropy
+    * \param[in] iPoint - Node index
+    * \param[in] entropy - fluid entropy value.
+    */
+  virtual void SetEntropy(unsigned long iPoint, su2double entropy) { FluidEntropy[iPoint] = entropy; };
+
+  /*!
+    * \brief Get fluid entropy
+    * \param[in] iPoint - Node index
+    * \return Entropy - Fluid entropy value
+    */
+  virtual su2double GetEntropy(unsigned long iPoint) const { return FluidEntropy[iPoint]; }
+
+  /*!
+    * \brief Set dataset extrapolation instance
+    * \param[in] iPoint - Node index
+    * \param[in] extrapolation - Extrapolation instance (0 = within dataset, 1 = outside dataset)
+    */
+  virtual void SetDataExtrapolation(unsigned long iPoint, unsigned short extrapolation) { Dataset_Extrapolation[iPoint] = extrapolation; };
+
+  /*!
+    * \brief Get dataset extrapolation instance
+    * \param[in] iPoint - Node index
+    * \return extrapolation - Extrapolation instance (0 = within dataset, 1 = outside dataset)
+    */
+  virtual unsigned short GetDataExtrapolation(unsigned long iPoint) const { return Dataset_Extrapolation[iPoint]; }
+
+  /*!
+    * \brief Set the number of iterations required by a Newton solver used by the fluid model.
+    * \param[in] iPoint - Node index
+    * \param[in] nIter - Number of iterations evaluated by the Newton solver
+    */
+  void SetNewtonSolverIterations(unsigned long iPoint, unsigned long nIter) { nIter_Newtonsolver[iPoint] = nIter; }
+
+  /*!
+    * \brief Get the number of iterations required by a Newton solver used by the fluid model.
+    * \param[in] iPoint - Node index
+    * \return Number of iterations evaluated by the Newton solver
+    */
+  unsigned long GetNewtonSolverIterations(unsigned long iPoint) const { return nIter_Newtonsolver[iPoint]; }
+
 };
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 29f25417c03..9183faf18d8 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -31,10 +31,6 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
 
   Kind_DataDriven_Method = config->GetKind_DataDriven_Method();
 
-  /*--- For this branch, only MLP's are supported for data-driven fluid model. ---*/
-  if(Kind_DataDriven_Method != ENUM_DATADRIVEN_METHOD::MLP)
-    SU2_MPI::Error("Only multi-layer perceptrons are currently accepted for data-driven fluid models.", CURRENT_FUNCTION);
-
   /*--- Retrieve interpolation method file name. ---*/
   input_filename = config->GetDataDriven_Filename();
 
@@ -128,31 +124,8 @@ void CDataDrivenFluid::MapInputs_to_Outputs(){
 void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
   Density = rho;
   StaticEnergy = e;
-  std::vector<std::string> output_names_rhoe_LUT;
-  std::vector<su2double*> outputs_LUT;
-  unsigned long exit_code;
-  switch (Kind_DataDriven_Method)
-  {
-  case ENUM_DATADRIVEN_METHOD::MLP:
-    /* --- Set MLP input vector values --- */
-    MLP_inputs[idx_rho] = Density;
-    MLP_inputs[idx_e]   = StaticEnergy;
-
-    /* --- Evaluate MLP --- */
-    exit_code = lookup_mlp->Predict_ANN(iomap_rhoe, MLP_inputs, outputs_rhoe);
-    break;
-  case ENUM_DATADRIVEN_METHOD::LUT:
-
-    output_names_rhoe_LUT.resize(output_names_rhoe.size());
-    for(size_t iOutput=0; iOutput<output_names_rhoe.size(); iOutput++) { output_names_rhoe_LUT[iOutput] = output_names_rhoe[iOutput]; }
 
-    outputs_LUT.resize(outputs_rhoe.size());
-    for(size_t iOutput=0; iOutput<outputs_rhoe.size(); iOutput++) { outputs_LUT[iOutput] = outputs_rhoe[iOutput]; }
-
-    lookup_table->LookUp_ProgEnth(output_names_rhoe_LUT, outputs_LUT, rho, e, "Density", "Energy");
-  default:
-    break;
-  }
+  Evaluate_Dataset(rho, e);
 
   /*--- Compute speed of sound ---*/
   su2double blue_term = (dsdrho_e * (2 - rho * pow(dsde_rho, -1) * d2sdedrho) + rho * d2sdrho2);
@@ -172,14 +145,6 @@ void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
 
   dPde_rho = -pow(rho, 2) * dTde_rho * dsdrho_e;
   dPdrho_e = -2*rho*Temperature*dsdrho_e - pow(rho, 2)*Temperature*d2sdrho2;
-
-  Cp = (1 / dTde_rho) * ( 1 + (1 / Density)*dPde_rho);
-  Cv = 1 / dTde_rho;
-  Gamma = Cp / Cv;
-  Gamma_Minus_One = Gamma - 1;
-  Gas_Constant = Cp - Cv;
-
-  within_range = exit_code;
 }
 
 void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
@@ -230,6 +195,8 @@ void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
 
   /*--- Calculate thermodynamic state based on converged values for density and energy ---*/
   SetTDState_rhoe(rho, e);
+
+  nIter_Newton = Iter;
 }
 
 void CDataDrivenFluid::SetTDState_Prho(su2double P, su2double rho) {
@@ -278,6 +245,8 @@ void CDataDrivenFluid::SetEnergy_Prho(su2double P, su2double rho) {
 
   /*--- Setting static energy as the converged value ---*/
   StaticEnergy = e;
+
+  nIter_Newton = Iter;
 }
 
 void CDataDrivenFluid::SetTDState_rhoT(su2double rho, su2double T) {
@@ -319,6 +288,8 @@ void CDataDrivenFluid::SetTDState_rhoT(su2double rho, su2double T) {
 
   /*--- Calculate thermodynamic state based on converged values for density and energy ---*/
   SetTDState_rhoe(rho, e);
+
+  nIter_Newton = Iter;
 }
 
 void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
@@ -371,6 +342,8 @@ void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
   }
   /*--- Calculate thermodynamic state based on converged values for density and energy ---*/
   SetTDState_rhoe(rho, e);
+
+  nIter_Newton = Iter;
 }
 
 void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
@@ -422,4 +395,46 @@ void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
 
   /*--- Calculate thermodynamic state based on converged values for density and energy ---*/
   SetTDState_rhoe(rho, e);
+
+  nIter_Newton = Iter;
+}
+
+unsigned long CDataDrivenFluid::Predict_MLP(su2double rho, su2double e) {
+  unsigned long exit_code;
+  MLP_inputs[idx_rho] = rho;
+  MLP_inputs[idx_e] = e;
+  exit_code = lookup_mlp->Predict_ANN(iomap_rhoe, MLP_inputs, outputs_rhoe);
+  dsdrho_e = -exp(dsdrho_e);
+  d2sdrho2 = exp(d2sdrho2);
+
+  return exit_code;
+}
+
+unsigned long CDataDrivenFluid::Predict_LUT(su2double rho, su2double e) {
+  unsigned long exit_code;
+  std::vector<std::string> output_names_rhoe_LUT;
+  std::vector<su2double*> outputs_LUT;
+  output_names_rhoe_LUT.resize(output_names_rhoe.size());
+    for(size_t iOutput=0; iOutput<output_names_rhoe.size(); iOutput++) { output_names_rhoe_LUT[iOutput] = output_names_rhoe[iOutput]; }
+
+  outputs_LUT.resize(outputs_rhoe.size());
+  for(size_t iOutput=0; iOutput<outputs_rhoe.size(); iOutput++) { outputs_LUT[iOutput] = outputs_rhoe[iOutput]; }
+
+  exit_code = lookup_table->LookUp_ProgEnth(output_names_rhoe_LUT, outputs_LUT, rho, e, "Density", "Energy");
+  return exit_code;
+}
+
+void CDataDrivenFluid::Evaluate_Dataset(su2double rho, su2double e) {
+  /*--- Evaluate dataset based on regression method ---*/
+  switch (Kind_DataDriven_Method)
+  {
+  case ENUM_DATADRIVEN_METHOD::LUT:
+    outside_dataset = Predict_LUT(rho, e);
+    break;
+  case ENUM_DATADRIVEN_METHOD::MLP:
+    outside_dataset = Predict_MLP(rho, e);
+    break;
+  default:
+    break;
+  }
 }
\ No newline at end of file
diff --git a/SU2_CFD/src/output/CFlowCompOutput.cpp b/SU2_CFD/src/output/CFlowCompOutput.cpp
index f3005aa6e81..53eef133be7 100644
--- a/SU2_CFD/src/output/CFlowCompOutput.cpp
+++ b/SU2_CFD/src/output/CFlowCompOutput.cpp
@@ -238,6 +238,13 @@ void CFlowCompOutput::SetVolumeOutputFields(CConfig *config){
   AddVolumeOutput("MACH",        "Mach",                    "PRIMITIVE", "Mach number");
   AddVolumeOutput("PRESSURE_COEFF", "Pressure_Coefficient", "PRIMITIVE", "Pressure coefficient");
 
+  // Datadriven fluid model
+  if(config->GetKind_FluidModel() == DATADRIVEN_FLUID){
+    AddVolumeOutput("EXTRAPOLATION", "Extrapolation", "PRIMITIVE", "Density, energy outside data range");
+    AddVolumeOutput("FLUIDMODEL_NEWTONITER", "nIter_Newton", "PRIMITIVE", "Number of iterations evaluated by the Newton solver");
+    AddVolumeOutput("ENTROPY", "Entropy", "PRIMITIVE", "Fluid entropy value");
+  }
+
   if (config->GetViscous()) {
     AddVolumeOutput("LAMINAR_VISCOSITY", "Laminar_Viscosity", "PRIMITIVE", "Laminar viscosity");
 
@@ -316,6 +323,12 @@ void CFlowCompOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolv
   const su2double factor = solver[FLOW_SOL]->GetReferenceDynamicPressure();
   SetVolumeOutputValue("PRESSURE_COEFF", iPoint, (Node_Flow->GetPressure(iPoint) - solver[FLOW_SOL]->GetPressure_Inf())/factor);
 
+  if(config->GetKind_FluidModel() == DATADRIVEN_FLUID){
+    SetVolumeOutputValue("EXTRAPOLATION", iPoint, Node_Flow->GetDataExtrapolation(iPoint));
+    SetVolumeOutputValue("FLUIDMODEL_NEWTONITER", iPoint, Node_Flow->GetNewtonSolverIterations(iPoint));
+    SetVolumeOutputValue("ENTROPY", iPoint, Node_Flow->GetEntropy(iPoint));
+  }
+
   if (config->GetKind_Solver() == MAIN_SOLVER::RANS || config->GetKind_Solver() == MAIN_SOLVER::NAVIER_STOKES){
     SetVolumeOutputValue("LAMINAR_VISCOSITY", iPoint, Node_Flow->GetLaminarViscosity(iPoint));
   }
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index 22056801ba1..d62651c726c 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -1674,6 +1674,12 @@ unsigned long CEulerSolver::SetPrimitive_Variables(CSolver **solver_container, c
     bool physical = nodes->SetPrimVar(iPoint, GetFluidModel());
     nodes->SetSecondaryVar(iPoint, GetFluidModel());
 
+    /*--- Update en---*/
+    if(config->GetKind_FluidModel() == DATADRIVEN_FLUID) {
+      nodes->SetDataExtrapolation(iPoint, GetFluidModel()->GetExtrapolation());
+      nodes->SetEntropy(iPoint, GetFluidModel()->GetEntropy());
+    }
+
     /* Check for non-realizable states for reporting. */
 
     if (!physical) nonPhysicalPoints++;
@@ -4865,6 +4871,10 @@ void CEulerSolver::BC_Riemann(CGeometry *geometry, CSolver **solver_container,
       Energy_b = u_b[nVar-1]/Density_b;
       StaticEnergy_b = Energy_b - 0.5*Velocity2_b;
       GetFluidModel()->SetTDState_rhoe(Density_b, StaticEnergy_b);
+
+      if(config->GetKind_FluidModel() == DATADRIVEN_FLUID)
+        GetNodes()->SetNewtonSolverIterations(iPoint, GetFluidModel()->GetnIter_Newton());
+
       Pressure_b = GetFluidModel()->GetPressure();
       Temperature_b = GetFluidModel()->GetTemperature();
       Enthalpy_b = Energy_b + Pressure_b/Density_b;
diff --git a/SU2_CFD/src/variables/CEulerVariable.cpp b/SU2_CFD/src/variables/CEulerVariable.cpp
index 30ffcc08242..34dd5858846 100644
--- a/SU2_CFD/src/variables/CEulerVariable.cpp
+++ b/SU2_CFD/src/variables/CEulerVariable.cpp
@@ -72,6 +72,12 @@ CEulerVariable::CEulerVariable(su2double density, const su2double *velocity, su2
     WindGust.resize(nPoint,nDim);
     WindGustDer.resize(nPoint,nDim+1);
   }
+
+  if (config->GetKind_FluidModel() == DATADRIVEN_FLUID){
+    Dataset_Extrapolation.resize(nPoint) = 0;
+    nIter_Newtonsolver.resize(nPoint) = 0;
+    FluidEntropy.resize(nPoint) = 0.0;
+  }
 }
 
 bool CEulerVariable::SetPrimVar(unsigned long iPoint, CFluidModel *FluidModel) {
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index a97977af46b..054298c945d 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -930,6 +930,7 @@ def main():
     coolprop_transportModel.test_vals = [-4.527922, -1.308741, 4.630469, 0.000000, 0.000000]
     test_list.append(coolprop_transportModel)
 
+    # Subsonic Q1D nozzle using an MLP for thermodynamic state evaluation
     datadriven_MLP           = TestCase('datadriven_MLP')
     datadriven_MLP.cfg_dir   = "nicf/datadriven"
     datadriven_MLP.cfg_file  = "datadriven_nozzle.cfg"
diff --git a/docker/test/Dockerfile b/docker/test/Dockerfile
index 8be2bd24c8e..dd168ef4965 100644
--- a/docker/test/Dockerfile
+++ b/docker/test/Dockerfile
@@ -4,4 +4,4 @@ FROM su2code/build-su2:20191029
 COPY runTests.sh /runTests.sh
 
 # Code file to execute when the docker container starts up (`entrypoint.sh`)
-ENTRYPOINT ["/runTests.sh -c feature_multilayer_perceptron"]
+ENTRYPOINT ["/runTests.sh"]

From 4b0144cf45916d135df93ea34fa00e1d1480a85c Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 5 Dec 2022 13:32:55 +0100
Subject: [PATCH 060/656] Added legacy 2D lookup methods to CLookUpTable class

---
 Common/include/containers/CLookUpTable.hpp | 40 ++++++++++++++++++++++
 Common/src/containers/CLookUpTable.cpp     | 14 ++++++++
 2 files changed, 54 insertions(+)

diff --git a/Common/include/containers/CLookUpTable.hpp b/Common/include/containers/CLookUpTable.hpp
index 87db8a1e88c..0ccee3585c5 100644
--- a/Common/include/containers/CLookUpTable.hpp
+++ b/Common/include/containers/CLookUpTable.hpp
@@ -247,6 +247,46 @@ class CLookUpTable {
   unsigned long LookUp_XY(const std::vector<std::string>& val_names_var, std::vector<su2double>& val_vars, su2double val_x,
                                 su2double val_y, unsigned long i_level=0);
 
+  /*!
+   * \brief legacy version of the 2D lookup method for 1 value of the single variable "val_name_var" 
+            using controlling variable values(val_prog,val_enth).
+   * \param[in] val_name_var - string name of the variable to look up.
+   * \param[out] val_var - the stored value of the variable to look up.
+   * \param[in] val_prog - value of the progress variable.
+   * \param[in] val_enth - value of the enthalpy.
+   * \param[in] name_prog - name of the progress variable.
+   * \param[in] name_enth - name of the enthalpy variable.
+   * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
+   */
+  unsigned long LookUp_ProgEnth(const std::string& val_name_var, su2double* val_var, su2double val_prog, su2double val_enth, std::string name_prog, std::string name_enth);
+
+  /*!
+   * \brief legacy version of the 2D lookup method for 1 value for each of the variables in "val_name_var" 
+            using controlling variable values(val_x,val_y).
+   * \param[in] val_name_var - vector of string names of the variables to look up.
+   * \param[out] val_vars - pointer to the vector of stored values of the variables to look up.
+   * \param[in] val_prog - value of the progress variable.
+   * \param[in] val_enth - value of the enthalpy.
+   * \param[in] name_prog - name of the progress variable.
+   * \param[in] name_enth - name of the enthalpy variable.
+   * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
+   */
+  unsigned long LookUp_ProgEnth(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars, su2double val_prog,
+                                su2double val_enth, std::string name_prog, std::string name_enth);
+
+  /*!
+   * \brief legacy version of the 2D lookup method for 1 value for each of the variables in "val_name_var" 
+            using controlling variable values(val_x,val_y).
+   * \param[in] val_name_var - vector of string names of the variables to look up.
+   * \param[out] val_vars - pointer to the vector of stored values of the variables to look up.
+   * \param[in] val_prog - value of the progress variable.
+   * \param[in] val_enth - value of the enthalpy.
+   * \param[in] name_prog - name of the progress variable.
+   * \param[in] name_enth - name of the enthalpy variable.
+   * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
+   */
+  unsigned long LookUp_ProgEnth(const std::vector<std::string>& val_names_var, std::vector<su2double>& val_vars, su2double val_x,
+                                su2double val_y, std::string name_prog, std::string name_enth);                          
   /*!
    * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_x,val_y,val_z).
    * \param[in] val_name_var - string name of the variable to look up.
diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index 5aa626924cb..75d8410231d 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -504,6 +504,11 @@ unsigned long CLookUpTable::LookUp_XY(const string& val_name_var, su2double *val
   return exit_code;
 }
 
+unsigned long CLookUpTable::LookUp_ProgEnth(const std::string& val_name_var, su2double* val_var, su2double val_prog, 
+                                            su2double val_enth, std::string name_prog, std::string name_enth) {
+  return LookUp_XY(val_name_var, val_var, val_prog, val_enth);
+}
+
 unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vector<su2double>& val_vars,
                                             su2double val_x, su2double val_y, unsigned long i_level) {
   vector<su2double*> look_up_data;
@@ -517,6 +522,11 @@ unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vecto
   return exit_code;
 }
 
+unsigned long CLookUpTable::LookUp_ProgEnth(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars, su2double val_prog,
+                                su2double val_enth, std::string name_prog, std::string name_enth) {
+  return LookUp_XY(val_names_var, val_vars, val_prog, val_enth);
+}
+
 unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vector<su2double*>& val_vars,
                                             su2double val_x, su2double val_y, unsigned long i_level) {
   unsigned long exit_code = 0;
@@ -572,6 +582,10 @@ unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vecto
   return exit_code;
 }
 
+unsigned long CLookUpTable::LookUp_ProgEnth(const std::vector<std::string>& val_names_var, std::vector<su2double>& val_vars, su2double val_prog,
+                                su2double val_enth, std::string name_prog, std::string name_enth) {
+  return LookUp_XY(val_names_var, val_vars, val_prog, val_enth);
+}
 void CLookUpTable::GetInterpCoeffs(su2double val_x, su2double val_y, su2activematrix& interp_mat_inv,
                                    std::array<su2double,3>& interp_coeffs) {
 

From 259cf1c6afaf475f18f1fb7d19c9546535aec242 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Thu, 8 Dec 2022 20:05:47 -0800
Subject: [PATCH 061/656] Update CDeformationDriver

---
 .../include/drivers/CDeformationDriver.hpp    |  155 +--
 SU2_DEF/src/drivers/CDeformationDriver.cpp    | 1077 ++++++++---------
 2 files changed, 600 insertions(+), 632 deletions(-)

diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index 507978d77e7..b0d08f21836 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -31,84 +31,89 @@
 #include "../../../Common/include/CConfig.hpp"
 #undef ENABLE_MAPS
 
-#include "../../../Common/include/parallelization/mpi_structure.hpp"
-
+#include "../../../Common/include/drivers/CDriverBase.hpp"
+#include "../../../Common/include/geometry/CGeometry.hpp"
 #include "../../../Common/include/grid_movement/CSurfaceMovement.hpp"
 #include "../../../Common/include/grid_movement/CVolumetricMovement.hpp"
-#include "../../../SU2_CFD/include/output/COutput.hpp"
+#include "../../../Common/include/parallelization/mpi_structure.hpp"
 #include "../../../SU2_CFD/include/numerics/CNumerics.hpp"
-#include "../../../Common/include/geometry/CGeometry.hpp"
-#include "../../../Common/include/drivers/CDriverBase.hpp"
+#include "../../../SU2_CFD/include/output/COutput.hpp"
 
 class CDeformationDriver : public CDriverBase {
-    
-protected:
-    bool haveSurfaceDeformation = false;  // flag used to determine whether surface deformation is available for output
-    
-public:
-    /*!
-     * \brief Constructor of the class.
-     * \param[in] confFile - Configuration file name.
-     * \param[in] MPICommunicator - MPI communicator for SU2.
-     */
-    CDeformationDriver(char* confFile, SU2_Comm MPICommunicator);
-    
-    /*!
-     * \brief Destructor of the class.
-     */
-    ~CDeformationDriver(void);
-    
-    /*!
-     * \brief [Overload] Launch the computation for single-zone problems.
-     */
-    void Run();
-    
-    /*!
-     * \brief Output the mesh.
-     */
-    void Output();
-    
-    /*!
-     * \brief Deallocation routine
-     */
-    void Postprocessing();
-    
-    void CommunicateMeshDisplacements(void);
-    
-protected:
-    /*!
-     * \brief Read in the config and mesh files.
-     */
-    void Input_Preprocessing();
-    
-    /*!
-     * \brief Construction of the edge-based data structure.
-     */
-    void Geometrical_Preprocessing();
-    
-    /*!
-     * \brief Preprocess the output container.
-     */
-    void Output_Preprocessing();
-    
-    /*!
-     * \brief Preprocess the mesh solver container.
-     */
-    void Solver_Preprocessing();
-    
-    /*!
-     * \brief Preprocess the numerics container.
-     */
-    void Numerics_Preprocessing();
-    
-    /*!
-     * \brief Mesh deformation based on linear elasticity solver (CMeshSolver).
-     */
-    void Update();
-    
-    /*!
-     * \brief Mesh deformation based on legacy implementation.
-     */
-    void Update_Legacy();
-    
+ protected:
+  bool haveSurfaceDeformation = false;  // flag used to determine whether surface deformation is available for output
+
+ public:
+  /*!
+   * \brief Constructor of the class.
+   * \param[in] confFile - Configuration file name.
+   * \param[in] MPICommunicator - MPI communicator for SU2.
+   */
+  CDeformationDriver(char* confFile, SU2_Comm MPICommunicator);
+
+  /*!
+   * \brief Destructor of the class.
+   */
+  ~CDeformationDriver(void);
+
+  /*!
+   * \brief Preprocess the driver data.
+   */
+  void Preprocess();
+
+  /*!
+   * \brief Launch the driver computation.
+   */
+  void Run();
+
+  /*!
+   * \brief Output the mesh.
+   */
+  void Output();
+
+  /*!
+   * \brief Deallocation routine.
+   */
+  void Postprocessing();
+
+  /*!
+   * \brief Communicate boundary mesh displacements.
+   */
+  void CommunicateMeshDisplacements(void);
+
+ protected:
+  /*!
+   * \brief Read in the config and mesh files.
+   */
+  void Input_Preprocessing();
+
+  /*!
+   * \brief Construction of the edge-based data structure.
+   */
+  void Geometrical_Preprocessing();
+
+  /*!
+   * \brief Preprocess the output container.
+   */
+  void Output_Preprocessing();
+
+  /*!
+   * \brief Preprocess the mesh solver container.
+   */
+  void Solver_Preprocessing();
+
+  /*!
+   * \brief Preprocess the numerics container.
+   */
+  void Numerics_Preprocessing();
+
+  /*!
+   * \brief Mesh deformation based on linear elasticity solver (CMeshSolver).
+   */
+  void Update();
+
+  /*!
+   * \brief Mesh deformation based on legacy implementation.
+   */
+  void Update_Legacy();
 };
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 2c577ed2c7f..4a5e0febd32 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -28,624 +28,587 @@
 #include "../../include/drivers/CDeformationDriver.hpp"
 
 #include "../../../Common/include/geometry/CPhysicalGeometry.hpp"
-#include "../../../Common/include/toolboxes/geometry_toolbox.hpp"
-#include "../../../SU2_CFD/include/solvers/CMeshSolver.hpp"
-#include "../../../SU2_CFD/include/output/CMeshOutput.hpp"
 #include "../../../SU2_CFD/include/numerics/elasticity/CFEALinearElasticity.hpp"
+#include "../../../SU2_CFD/include/output/CMeshOutput.hpp"
+#include "../../../SU2_CFD/include/solvers/CMeshSolver.hpp"
 
 using namespace std;
 
-CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator):
-CDriverBase(confFile, 1, MPICommunicator)
-{
-    
-    /*--- Initialize Medipack (must also be here so it is initialized from python) ---*/
+CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
+    : CDriverBase(confFile, 1, MPICommunicator) {
+
+/*--- Initialize MeDiPack (must also be here to initialize it from Python) ---*/
 #ifdef HAVE_MPI
 #if defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)
-    SU2_MPI::Init_AMPI();
+  SU2_MPI::Init_AMPI();
 #endif
 #endif
-    
-    SU2_MPI::SetComm(MPICommunicator);
-    
-    rank = SU2_MPI::GetRank();
-    size = SU2_MPI::GetSize();
-    
-    /*--- Initialize containers --- */
-    
-    SetContainers_Null();
-    
-    /*--- Preprocessing of the config files. ---*/
-    
-    Input_Preprocessing();
-    
-    /*--- Set up a timer for performance benchmarking ---*/
-    
-    StartTime = SU2_MPI::Wtime();
-    
-    /*--- Preprocessing of the geometry for all zones. ---*/
-    
-    Geometrical_Preprocessing();
-    
-    /*--- Preprocessing of the output for all zones. ---*/
-    
-    Output_Preprocessing();
-    
-    if (driver_config->GetDeform_Mesh()){
-        
-        /*--- Preprocessing of the mesh solver for all zones. ---*/
-        
-        Solver_Preprocessing();
-        
-        /*--- Preprocessing of the mesh solver for all zones. ---*/
-        
-        Numerics_Preprocessing();
-        
-    }
-    
-    /*--- Preprocessing time is reported now, but not included in the next compute portion. ---*/
-    
-    StopTime = SU2_MPI::Wtime();
-    
-    /*--- Compute/print the total time for performance benchmarking. ---*/
-    
-    UsedTime = StopTime-StartTime;
-    UsedTimePreproc    = UsedTime;
-    UsedTimeCompute    = 0.0;
-    
-}
 
-CDeformationDriver::~CDeformationDriver(void) {
-    
+  SU2_MPI::SetComm(MPICommunicator);
+
+  rank = SU2_MPI::GetRank();
+  size = SU2_MPI::GetSize();
+
+  /*--- Initialize containers. --- */
+
+  SetContainers_Null();
+
+  /*--- Preprocessing of the config files. ---*/
+
+  Input_Preprocessing();
+
+  /*--- Set up a timer for performance benchmarking. ---*/
+
+  StartTime = SU2_MPI::Wtime();
+
+  /*--- Preprocessing of the geometry for all zones. ---*/
+
+  Geometrical_Preprocessing();
+
+  /*--- Preprocessing of the output for all zones. ---*/
+
+  Output_Preprocessing();
+
+  if (driver_config->GetDeform_Mesh()) {
+    /*--- Preprocessing of the mesh solver for all zones. ---*/
+
+    Solver_Preprocessing();
+
+    /*--- Preprocessing of the mesh solver for all zones. ---*/
+
+    Numerics_Preprocessing();
+
+  }
+
+  /*--- Preprocessing time is reported now, but not included in the next compute portion. ---*/
+
+  StopTime = SU2_MPI::Wtime();
+
+  /*--- Compute the total time for performance benchmarking. ---*/
+
+  UsedTime = StopTime - StartTime;
+  UsedTimePreproc = UsedTime;
+  UsedTimeCompute = 0.0;
 }
 
+CDeformationDriver::~CDeformationDriver(void) {}
+
 void CDeformationDriver::Input_Preprocessing() {
-    
-    /*--- Initialize a char to store the zone filename ---*/
-    char zone_file_name[MAX_STRING_SIZE];
-    
-    /*--- Initialize the configuration of the driver ---*/
-    driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DEF);
-    
-    nZone = driver_config->GetnZone();
-    
-    /*--- Loop over all zones to initialize the various classes. In most
-     cases, nZone is equal to one. This represents the solution of a partial
-     differential equation on a single block, unstructured mesh. ---*/
-    
-    for (iZone = 0; iZone < nZone; iZone++) {
-        
-        /*--- Definition of the configuration option class for all zones. In this
-         constructor, the input configuration file is parsed and all options are
-         read and stored. ---*/
-        
-        if (driver_config->GetnConfigFiles() > 0){
-            strcpy(zone_file_name, driver_config->GetConfigFilename(iZone).c_str());
-            
-            config_container[iZone] = new CConfig(driver_config, zone_file_name, SU2_COMPONENT::SU2_DEF, iZone, nZone, true);
-        } else {
-            config_container[iZone] = new CConfig(driver_config, config_file_name, SU2_COMPONENT::SU2_DEF, iZone, nZone, true);
-        }
-        
-        config_container[iZone]->SetMPICommunicator(SU2_MPI::GetComm());
+  /*--- Initialize a char to store the zone filename. ---*/
+
+  char zone_file_name[MAX_STRING_SIZE];
+
+  /*--- Initialize the configuration of the driver. ---*/
+
+  driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DEF);
+
+  nZone = driver_config->GetnZone();
+
+  /*--- Loop over all zones to initialize the various classes. In most
+   cases, nZone is equal to one. This represents the solution of a partial
+   differential equation on a single block, unstructured mesh. ---*/
+
+  for (iZone = 0; iZone < nZone; iZone++) {
+    /*--- Definition of the configuration option class for all zones. In this
+     constructor, the input configuration file is parsed and all options are
+     read and stored. ---*/
+
+    if (driver_config->GetnConfigFiles() > 0) {
+      strcpy(zone_file_name, driver_config->GetConfigFilename(iZone).c_str());
+      config_container[iZone] = new CConfig(driver_config, zone_file_name, SU2_COMPONENT::SU2_DEF, iZone, nZone, true);
+    } else {
+      config_container[iZone] = new CConfig(driver_config, config_file_name, SU2_COMPONENT::SU2_DEF, iZone, nZone, true);
     }
-    
-    /*--- Set the multizone part of the problem. ---*/
-    
-    if (driver_config->GetMultizone_Problem()){
-        for (iZone = 0; iZone < nZone; iZone++) {
-            
-            /*--- Set the interface markers for multizone ---*/
-            
-            config_container[iZone]->SetMultizone(driver_config, config_container);
-        }
+
+    config_container[iZone]->SetMPICommunicator(SU2_MPI::GetComm());
+  }
+
+  /*--- Set the multi-zone part of the problem. ---*/
+
+  if (driver_config->GetMultizone_Problem()) {
+    for (iZone = 0; iZone < nZone; iZone++) {
+      /*--- Set the interface markers for multi-zone. ---*/
+
+      config_container[iZone]->SetMultizone(driver_config, config_container);
     }
+  }
 
-    /*--- Keep a reference to the main (ZONE 0) config ---*/
-    main_config = config_container[ZONE_0];
+  /*--- Keep a reference to the main (ZONE 0) config. ---*/
+
+  main_config = config_container[ZONE_0];
 }
 
 void CDeformationDriver::Geometrical_Preprocessing() {
-    
-    for (iZone = 0; iZone < nZone; iZone++) {
-        
-        /*--- Definition of the geometry class to store the primal grid in the partitioning process. ---*/
-        
-        CGeometry *geometry_aux = nullptr;
-        
-        /*--- All ranks process the grid and call ParMETIS for partitioning ---*/
-        
-        geometry_aux = new CPhysicalGeometry(config_container[iZone], iZone, nZone);
-        
-        /*--- Color the initial grid and set the send-receive domains (ParMETIS) ---*/
-        
-        geometry_aux->SetColorGrid_Parallel(config_container[iZone]);
-        
-        /*--- Build the grid data structures using the ParMETIS coloring. ---*/
-        
-        unsigned short nInst_Zone = nInst[iZone];
-        unsigned short nMesh = 1;
-        
-        geometry_container[iZone] = new CGeometry**[nInst_Zone] ();
-        geometry_container[iZone][INST_0] = new CGeometry*[nMesh] ();
-        geometry_container[iZone][INST_0][MESH_0] = new CPhysicalGeometry(geometry_aux, config_container[iZone]);
-        
-        /*--- Deallocate the memory of geometry_aux ---*/
-        
-        delete geometry_aux;
-        
-        /*--- Add the Send/Receive boundaries ---*/
-        
-        geometry_container[iZone][INST_0][MESH_0]->SetSendReceive(config_container[iZone]);
-        
-        /*--- Add the Send/Receive boundaries ---*/
-        
-        geometry_container[iZone][INST_0][MESH_0]->SetBoundaries(config_container[iZone]);
-        
-        /*--- Computational grid preprocesing ---*/
-        
-        if (rank == MASTER_NODE) cout << endl << "----------------------- Preprocessing computations ----------------------" << endl;
-        
-        /*--- Compute elements surrounding points, points surrounding points ---*/
-        
-        if (rank == MASTER_NODE) cout << "Setting local point connectivity." <<endl;
-        geometry_container[iZone][INST_0][MESH_0]->SetPoint_Connectivity();
-        
-        /*--- Check the orientation before computing geometrical quantities ---*/
-        
-        geometry_container[iZone][INST_0][MESH_0]->SetBoundVolume();
-        if (config_container[iZone]->GetReorientElements()) {
-            if (rank == MASTER_NODE) cout << "Checking the numerical grid orientation of the interior elements." <<endl;
-            geometry_container[iZone][INST_0][MESH_0]->Check_IntElem_Orientation(config_container[iZone]);
-            geometry_container[iZone][INST_0][MESH_0]->Check_BoundElem_Orientation(config_container[iZone]);
-        }
-        
-        /*--- Create the edge structure ---*/
-        
-        if (rank == MASTER_NODE) cout << "Identify edges and vertices." <<endl;
-        geometry_container[iZone][INST_0][MESH_0]->SetEdges();
-        geometry_container[iZone][INST_0][MESH_0]->SetVertex(config_container[iZone]);
-        
-        if (config_container[iZone]->GetDesign_Variable(0) != NO_DEFORMATION) {
-            
-            /*--- Create the dual control volume structures ---*/
-            
-            if (rank == MASTER_NODE) cout << "Setting the bound control volume structure." << endl;
-            geometry_container[iZone][INST_0][MESH_0]->SetControlVolume(config_container[iZone], ALLOCATE);
-            geometry_container[iZone][INST_0][MESH_0]->SetBoundControlVolume(config_container[iZone], ALLOCATE);
-        }
-        
-        /*--- Create the point-to-point MPI communication structures. ---*/
-        
-        geometry_container[iZone][INST_0][MESH_0]->PreprocessP2PComms(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
-        
+  for (iZone = 0; iZone < nZone; iZone++) {
+    /*--- Definition of the geometry class to store the primal grid in the partitioning process. ---*/
+
+    CGeometry* geometry_aux = nullptr;
+
+    /*--- All ranks process the grid and call ParMETIS for partitioning. ---*/
+
+    geometry_aux = new CPhysicalGeometry(config_container[iZone], iZone, nZone);
+
+    /*--- Color the initial grid and set the send-receive domains (ParMETIS). ---*/
+
+    geometry_aux->SetColorGrid_Parallel(config_container[iZone]);
+
+    /*--- Build the grid data structures using the ParMETIS coloring. ---*/
+
+    unsigned short nInst_Zone = nInst[iZone];
+    unsigned short nMesh = 1;
+
+    geometry_container[iZone] = new CGeometry**[nInst_Zone]();
+    geometry_container[iZone][INST_0] = new CGeometry*[nMesh]();
+    geometry_container[iZone][INST_0][MESH_0] = new CPhysicalGeometry(geometry_aux, config_container[iZone]);
+
+    /*--- Deallocate the memory of geometry_aux. ---*/
+
+    delete geometry_aux;
+
+    /*--- Add the Send/Receive boundaries. ---*/
+
+    geometry_container[iZone][INST_0][MESH_0]->SetSendReceive(config_container[iZone]);
+
+    /*--- Add the Send/Receive boundaries. ---*/
+
+    geometry_container[iZone][INST_0][MESH_0]->SetBoundaries(config_container[iZone]);
+
+    /*--- Computational grid preprocessing. ---*/
+
+    if (rank == MASTER_NODE) cout << endl << "----------------------- Preprocessing computations ----------------------" << endl;
+
+    /*--- Compute elements surrounding points, points surrounding points. ---*/
+
+    if (rank == MASTER_NODE) cout << "Setting local point connectivity." << endl;
+    geometry_container[iZone][INST_0][MESH_0]->SetPoint_Connectivity();
+
+    /*--- Check the orientation before computing geometrical quantities. ---*/
+
+    geometry_container[iZone][INST_0][MESH_0]->SetBoundVolume();
+    if (config_container[iZone]->GetReorientElements()) {
+      if (rank == MASTER_NODE) cout << "Checking the numerical grid orientation of the interior elements." << endl;
+      geometry_container[iZone][INST_0][MESH_0]->Check_IntElem_Orientation(config_container[iZone]);
+      geometry_container[iZone][INST_0][MESH_0]->Check_BoundElem_Orientation(config_container[iZone]);
+    }
+
+    /*--- Create the edge structure. ---*/
+
+    if (rank == MASTER_NODE) cout << "Identify edges and vertices." << endl;
+    geometry_container[iZone][INST_0][MESH_0]->SetEdges();
+    geometry_container[iZone][INST_0][MESH_0]->SetVertex(config_container[iZone]);
+
+    if (config_container[iZone]->GetDesign_Variable(0) != NO_DEFORMATION) {
+      /*--- Create the dual control volume structures. ---*/
+
+      if (rank == MASTER_NODE) cout << "Setting the bound control volume structure." << endl;
+      geometry_container[iZone][INST_0][MESH_0]->SetControlVolume(config_container[iZone], ALLOCATE);
+      geometry_container[iZone][INST_0][MESH_0]->SetBoundControlVolume(config_container[iZone], ALLOCATE);
     }
-    
-    /*--- Get the number of dimensions ---*/
-    nDim = geometry_container[ZONE_0][INST_0][MESH_0]->GetnDim();
 
-    /*--- Keep a reference to the main (ZONE_0, INST_0, MESH_0) geometry ---*/
-    main_geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    /*--- Create the point-to-point MPI communication structures. ---*/
+
+    geometry_container[iZone][INST_0][MESH_0]->PreprocessP2PComms(geometry_container[iZone][INST_0][MESH_0],config_container[iZone]);
+  }
+
+  /*--- Get the number of dimensions. ---*/
 
+  nDim = geometry_container[ZONE_0][INST_0][MESH_0]->GetnDim();
+
+  /*--- Keep a reference to the main (ZONE_0, INST_0, MESH_0) geometry. ---*/
+
+  main_geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 }
 
 void CDeformationDriver::Output_Preprocessing() {
-    
-    for (iZone = 0; iZone < nZone; iZone++) {
-        
-        /*--- Allocate the mesh output ---*/
-        
-        output_container[iZone] = new CMeshOutput(config_container[iZone], geometry_container[iZone][INST_0][MESH_0]->GetnDim());
-        
-        /*--- Preprocess the volume output ---*/
-        
-        output_container[iZone]->PreprocessVolumeOutput(config_container[iZone]);
-        
-        /*--- Preprocess history --- */
-        
-        output_container[iZone]->PreprocessHistoryOutput(config_container[iZone], false);
-        
-    }
+  for (iZone = 0; iZone < nZone; iZone++) {
+    /*--- Allocate the mesh output. ---*/
+
+    output_container[iZone] = new CMeshOutput(config_container[iZone], geometry_container[iZone][INST_0][MESH_0]->GetnDim());
+
+    /*--- Preprocess the volume output. ---*/
+
+    output_container[iZone]->PreprocessVolumeOutput(config_container[iZone]);
+
+    /*--- Preprocess history. --- */
+
+    output_container[iZone]->PreprocessHistoryOutput(config_container[iZone], false);
+  }
 }
 
 void CDeformationDriver::Solver_Preprocessing() {
-    
-    for (iZone = 0; iZone < nZone; iZone++) {
-        unsigned short nInst_Zone = nInst[iZone];
-        unsigned short nMesh = 1;
-        unsigned short nSols = MAX_SOLS;
-        
-        
-        solver_container[iZone] = new CSolver*** [nInst_Zone] ();
-        solver_container[iZone][INST_0] = new CSolver** [nMesh] ();
-        solver_container[iZone][INST_0][MESH_0] = new CSolver* [nSols] ();
-        solver_container[iZone][INST_0][MESH_0][MESH_SOL] = new CMeshSolver(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
-    }
+  for (iZone = 0; iZone < nZone; iZone++) {
+    unsigned short nInst_Zone = nInst[iZone];
+    unsigned short nMesh = 1;
+    unsigned short nSols = MAX_SOLS;
+
+    solver_container[iZone] = new CSolver***[nInst_Zone]();
+    solver_container[iZone][INST_0] = new CSolver**[nMesh]();
+    solver_container[iZone][INST_0][MESH_0] = new CSolver*[nSols]();
+    solver_container[iZone][INST_0][MESH_0][MESH_SOL] =
+        new CMeshSolver(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
+  }
 }
 
 void CDeformationDriver::Numerics_Preprocessing() {
-    
-    for (iZone = 0; iZone < nZone; iZone++) {
-        unsigned short nInst_Zone = nInst[iZone];
-        unsigned short nMesh = 1;
-        unsigned short nSols = MAX_SOLS;
-        unsigned int nTerm = omp_get_num_threads() * MAX_TERMS;
-        
-        numerics_container[iZone] = new CNumerics**** [nInst_Zone] ();
-        numerics_container[iZone][INST_0] = new CNumerics*** [nMesh] ();
-        numerics_container[iZone][INST_0][MESH_0] = new CNumerics** [nSols] ();
-        numerics_container[iZone][INST_0][MESH_0][MESH_SOL] = new CNumerics* [nTerm] ();
-        
-        for (int thread = 0; thread < omp_get_max_threads(); ++thread) {
-            const int iTerm = FEA_TERM + thread * MAX_TERMS;
-            const int nDim = geometry_container[iZone][INST_0][MESH_0]->GetnDim();
-            
-            numerics_container[iZone][INST_0][MESH_0][MESH_SOL][iTerm] = new CFEAMeshElasticity(nDim, nDim, geometry_container[iZone][INST_0][MESH_0]->GetnElem(), config_container[iZone]);
-        }
-        
+  for (iZone = 0; iZone < nZone; iZone++) {
+    unsigned short nInst_Zone = nInst[iZone];
+    unsigned short nMesh = 1;
+    unsigned short nSols = MAX_SOLS;
+    unsigned int nTerm = omp_get_num_threads() * MAX_TERMS;
+
+    numerics_container[iZone] = new CNumerics****[nInst_Zone]();
+    numerics_container[iZone][INST_0] = new CNumerics***[nMesh]();
+    numerics_container[iZone][INST_0][MESH_0] = new CNumerics**[nSols]();
+    numerics_container[iZone][INST_0][MESH_0][MESH_SOL] = new CNumerics*[nTerm]();
+
+    for (int thread = 0; thread < omp_get_max_threads(); ++thread) {
+      const int iTerm = FEA_TERM + thread * MAX_TERMS;
+      const int nDim = geometry_container[iZone][INST_0][MESH_0]->GetnDim();
+
+      numerics_container[iZone][INST_0][MESH_0][MESH_SOL][iTerm] = new CFEAMeshElasticity(
+          nDim, nDim, geometry_container[iZone][INST_0][MESH_0]->GetnElem(), config_container[iZone]);
     }
-    
+  }
 }
 
+void CDeformationDriver::Preprocess() {}
+
 void CDeformationDriver::Run() {
-    
-    /* --- Start measuring computation time ---*/
-    
-    StartTime = SU2_MPI::Wtime();
-    
-    /*--- Surface grid deformation using design variables ---*/
-    
-    if (driver_config->GetDeform_Mesh()) {
-        Update();
-    }
-    else {
-        Update_Legacy();
-    }
-    
-    /*--- Synchronization point after a single solver iteration. Compute the
-     wall clock time required. ---*/
-    
-    StopTime = SU2_MPI::Wtime();
-    
-    UsedTimeCompute = StopTime-StartTime;
-    if (rank == MASTER_NODE) {
-        cout << "\nCompleted in " << fixed << UsedTimeCompute << " seconds on "<< size;
-        
-        if (size == 1) cout << " core." << endl; else cout << " cores." << endl;
-    }
-    
-    /*--- Output the deformed mesh ---*/
-    Output();
-    
+  /* --- Start measuring computation time. ---*/
+
+  StartTime = SU2_MPI::Wtime();
+
+  /*--- Surface grid deformation using design variables. ---*/
+
+  if (driver_config->GetDeform_Mesh()) {
+    Update();
+  } else {
+    Update_Legacy();
+  }
+
+  /*--- Synchronization point after a single solver iteration. Compute the wall clock time required. ---*/
+
+  StopTime = SU2_MPI::Wtime();
+
+  UsedTimeCompute = StopTime - StartTime;
+  if (rank == MASTER_NODE) {
+    cout << "\nCompleted in " << fixed << UsedTimeCompute << " seconds on " << size;
+
+    if (size == 1) cout << " core." << endl; else cout << " cores." << endl;
+  }
+
+  /*--- Output the deformed mesh. ---*/
+
+  Output();
 }
 
 void CDeformationDriver::Update() {
-    
-    for (iZone = 0; iZone < nZone; iZone++){
-        
-        /*--- Set the stiffness of each element mesh into the mesh numerics ---*/
-        
-        solver_container[iZone][INST_0][MESH_0][MESH_SOL]->SetMesh_Stiffness(numerics_container[iZone][INST_0][MESH_0][MESH_SOL], config_container[iZone]);
-        
-        /*--- Deform the volume grid around the new boundary locations ---*/
-        
-        solver_container[iZone][INST_0][MESH_0][MESH_SOL]->DeformMesh(geometry_container[iZone][INST_0][MESH_0], numerics_container[iZone][INST_0][MESH_0][MESH_SOL], config_container[iZone]);
-        
-    }
+  for (iZone = 0; iZone < nZone; iZone++) {
+    /*--- Set the stiffness of each element mesh into the mesh numerics. ---*/
+
+    solver_container[iZone][INST_0][MESH_0][MESH_SOL]->SetMesh_Stiffness(numerics_container[iZone][INST_0][MESH_0][MESH_SOL], config_container[iZone]);
+
+    /*--- Deform the volume grid around the new boundary locations. ---*/
+
+    solver_container[iZone][INST_0][MESH_0][MESH_SOL]->DeformMesh(geometry_container[iZone][INST_0][MESH_0],
+                                                                  numerics_container[iZone][INST_0][MESH_0][MESH_SOL],
+                                                                  config_container[iZone]);
+  }
 }
 
 void CDeformationDriver::Update_Legacy() {
-    
-    for (iZone = 0; iZone < nZone; iZone++){
-        
-        if (config_container[iZone]->GetDesign_Variable(0) != NO_DEFORMATION) {
-            unsigned short nInst_Zone = nInst[iZone];
-            
-            /*--- Definition of the Class for grid movement ---*/
-            grid_movement[iZone] = new CVolumetricMovement* [nInst_Zone] ();
-            grid_movement[iZone][INST_0] = new CVolumetricMovement(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
-            
-            /*--- Save original coordinates to be reused in convexity checking procedure ---*/
-            auto OriginalCoordinates = geometry_container[iZone][INST_0][MESH_0]->nodes->GetCoord();
-            
-            /*--- First check for volumetric grid deformation/transformations ---*/
-            
-            if (config_container[iZone]->GetDesign_Variable(0) == SCALE_GRID) {
-                
-                if (rank == MASTER_NODE)
-                    cout << endl << "--------------------- Volumetric grid scaling (ZONE " << iZone <<") ------------------" << endl;
-                grid_movement[iZone][INST_0]->SetVolume_Scaling(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], false);
-                
-            } else if (config_container[iZone]->GetDesign_Variable(0) == TRANSLATE_GRID) {
-                
-                if (rank == MASTER_NODE)
-                    cout << endl << "------------------- Volumetric grid translation (ZONE " << iZone <<") ----------------" << endl;
-                grid_movement[iZone][INST_0]->SetVolume_Translation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], false);
-                
-            } else if (config_container[iZone]->GetDesign_Variable(0) == ROTATE_GRID) {
-                
-                if (rank == MASTER_NODE)
-                    cout << endl << "--------------------- Volumetric grid rotation (ZONE " << iZone <<") -----------------" << endl;
-                grid_movement[iZone][INST_0]->SetVolume_Rotation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], false);
-                
-            } else {
-                
-                /*--- If no volume-type deformations are requested, then this is a
-                 surface-based deformation or FFD set up. ---*/
-                
-                if (rank == MASTER_NODE)
-                    cout << endl << "--------------------- Surface grid deformation (ZONE " << iZone <<") -----------------" << endl;
-                
-                /*--- Definition and initialization of the surface deformation class ---*/
-                
-                surface_movement[iZone] = new CSurfaceMovement();
-                haveSurfaceDeformation = true;
-                
-                /*--- Copy coordinates to the surface structure ---*/
-                
-                surface_movement[iZone]->CopyBoundary(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
-                
-                /*--- Surface grid deformation ---*/
-                
-                if (rank == MASTER_NODE) cout << "Performing the deformation of the surface grid." << endl;
-                auto TotalDeformation = surface_movement[iZone]->SetSurface_Deformation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
-                
-                if (config_container[iZone]->GetDesign_Variable(0) != FFD_SETTING) {
-                    
-                    if (rank == MASTER_NODE)
-                        cout << endl << "------------------- Volumetric grid deformation (ZONE " << iZone <<") ----------------" << endl;
-                    
-                    if (rank == MASTER_NODE)
-                        cout << "Performing the deformation of the volumetric grid." << endl;
-                    grid_movement[iZone][INST_0]->SetVolume_Deformation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], false);
-                    
-                    /*--- Get parameters for convexity check ---*/
-                    bool ConvexityCheck;
-                    unsigned short ConvexityCheck_MaxIter, ConvexityCheck_MaxDepth;
-                    
-                    tie(ConvexityCheck, ConvexityCheck_MaxIter, ConvexityCheck_MaxDepth) = config_container[iZone]->GetConvexityCheck();
-                    
-                    /*--- Recursively change deformations if there are nonconvex elements. ---*/
-                    
-                    if (ConvexityCheck && geometry_container[iZone][INST_0][MESH_0]->GetnNonconvexElements() > 0) {
-                        if (rank == MASTER_NODE) {
-                            cout << "Nonconvex elements present after deformation. " << endl;
-                            cout << "Recursively lowering deformation magnitude." << endl;
-                        }
-                        
-                        /*--- Load initial deformation values ---*/
-                        auto InitialDeformation = TotalDeformation;
-                        
-                        unsigned short ConvexityCheckIter, RecursionDepth = 0;
-                        su2double DeformationFactor = 1.0, DeformationDifference = 1.0;
-                        for (ConvexityCheckIter = 1; ConvexityCheckIter <= ConvexityCheck_MaxIter; ConvexityCheckIter++) {
-                            
-                            /*--- Recursively change deformation magnitude:
-                             decrease if there are nonconvex elements, increase otherwise ---*/
-                            DeformationDifference /= 2.0;
-                            
-                            if (geometry_container[iZone][INST_0][MESH_0]->GetnNonconvexElements() > 0) {
-                                DeformationFactor -= DeformationDifference;
-                            } else {
-                                RecursionDepth += 1;
-                                
-                                if (RecursionDepth == ConvexityCheck_MaxDepth) {
-                                    if (rank == MASTER_NODE) {
-                                        cout << "Maximum recursion depth reached." << endl;
-                                        cout << "Remaining amount of original deformation: ";
-                                        cout << DeformationFactor*100.0 << " percent. " << endl;
-                                    }
-                                    break;
-                                }
-                                
-                                DeformationFactor += DeformationDifference;
-                            }
-                            
-                            /*--- Load mesh to start every iteration with an undeformed grid ---*/
-                            for (auto iPoint = 0ul; iPoint < OriginalCoordinates.rows(); iPoint++) {
-                                for (auto iDim = 0ul; iDim < OriginalCoordinates.cols(); iDim++) {
-                                    geometry_container[iZone][INST_0][MESH_0]->nodes->SetCoord(iPoint, iDim, OriginalCoordinates(iPoint,iDim));
-                                }
-                            }
-                            
-                            /*--- Set deformation magnitude as percentage of initial deformation ---*/
-                            for (auto iDV = 0u; iDV < driver_config->GetnDV(); iDV++) {
-                                for (auto iDV_Value = 0u; iDV_Value < driver_config->GetnDV_Value(iDV); iDV_Value++) {
-                                    config_container[iZone]->SetDV_Value(iDV, iDV_Value, InitialDeformation[iDV][iDV_Value]*DeformationFactor);
-                                }
-                            }
-                            
-                            /*--- Surface grid deformation ---*/
-                            if (rank == MASTER_NODE) cout << "Performing the deformation of the surface grid." << endl;
-                            
-                            TotalDeformation = surface_movement[iZone]->SetSurface_Deformation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
-                            
-                            if (rank == MASTER_NODE)
-                                cout << endl << "------------------- Volumetric grid deformation (ZONE " << iZone <<") ----------------" << endl;
-                            
-                            if (rank == MASTER_NODE)
-                                cout << "Performing the deformation of the volumetric grid." << endl;
-                            grid_movement[iZone][INST_0]->SetVolume_Deformation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], false);
-                            
-                            if (rank == MASTER_NODE) {
-                                cout << "Number of nonconvex elements for iteration " << ConvexityCheckIter << ": ";
-                                cout << geometry_container[iZone][INST_0][MESH_0]->GetnNonconvexElements() << endl;
-                                cout << "Remaining amount of original deformation: ";
-                                cout << DeformationFactor*100.0 << " percent. " << endl;
-                            }
-                            
-                        }
-                        
-                    }
-                    
+  for (iZone = 0; iZone < nZone; iZone++) {
+    if (config_container[iZone]->GetDesign_Variable(0) != NO_DEFORMATION) {
+      unsigned short nInst_Zone = nInst[iZone];
+
+      /*--- Definition of the Class for grid movement. ---*/
+
+      grid_movement[iZone] = new CVolumetricMovement*[nInst_Zone]();
+      grid_movement[iZone][INST_0] = new CVolumetricMovement(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
+
+      /*--- Save original coordinates to be reused in convexity checking procedure. ---*/
+
+      auto OriginalCoordinates = geometry_container[iZone][INST_0][MESH_0]->nodes->GetCoord();
+
+      /*--- First check for volumetric grid deformation/transformations. ---*/
+
+      if (config_container[iZone]->GetDesign_Variable(0) == SCALE_GRID) {
+        if (rank == MASTER_NODE)
+          cout << endl << "--------------------- Volumetric grid scaling (ZONE " << iZone << ") ------------------" << endl;
+        grid_movement[iZone][INST_0]->SetVolume_Scaling(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], false);
+
+      } else if (config_container[iZone]->GetDesign_Variable(0) == TRANSLATE_GRID) {
+        if (rank == MASTER_NODE)
+          cout << endl << "------------------- Volumetric grid translation (ZONE " << iZone << ") ----------------" << endl;
+        grid_movement[iZone][INST_0]->SetVolume_Translation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], false);
+
+      } else if (config_container[iZone]->GetDesign_Variable(0) == ROTATE_GRID) {
+        if (rank == MASTER_NODE)
+          cout << endl << "--------------------- Volumetric grid rotation (ZONE " << iZone << ") -----------------" << endl;
+        grid_movement[iZone][INST_0]->SetVolume_Rotation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], false);
+
+      } else {
+        /*--- If no volume-type deformations are requested, then this is a
+         * surface-based deformation or FFD set up. ---*/
+
+        if (rank == MASTER_NODE)
+          cout << endl << "--------------------- Surface grid deformation (ZONE " << iZone << ") -----------------" << endl;
+
+        /*--- Definition and initialization of the surface deformation class. ---*/
+
+        surface_movement[iZone] = new CSurfaceMovement();
+        haveSurfaceDeformation = true;
+
+        /*--- Copy coordinates to the surface structure. ---*/
+
+        surface_movement[iZone]->CopyBoundary(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
+
+        /*--- Surface grid deformation. ---*/
+
+        if (rank == MASTER_NODE) cout << "Performing the deformation of the surface grid." << endl;
+        auto TotalDeformation = surface_movement[iZone]->SetSurface_Deformation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
+
+        if (config_container[iZone]->GetDesign_Variable(0) != FFD_SETTING) {
+          if (rank == MASTER_NODE)
+            cout << endl << "------------------- Volumetric grid deformation (ZONE " << iZone << ") ----------------" << endl;
+
+          if (rank == MASTER_NODE) cout << "Performing the deformation of the volumetric grid." << endl;
+          grid_movement[iZone][INST_0]->SetVolume_Deformation(geometry_container[iZone][INST_0][MESH_0],config_container[iZone], false);
+
+          /*--- Get parameters for convexity check. ---*/
+          bool ConvexityCheck;
+          unsigned short ConvexityCheck_MaxIter, ConvexityCheck_MaxDepth;
+
+          tie(ConvexityCheck, ConvexityCheck_MaxIter, ConvexityCheck_MaxDepth) = config_container[iZone]->GetConvexityCheck();
+
+          /*--- Recursively change deformations if there are non-convex elements. ---*/
+
+          if (ConvexityCheck && geometry_container[iZone][INST_0][MESH_0]->GetnNonconvexElements() > 0) {
+            if (rank == MASTER_NODE) {
+              cout << "Non-convex elements present after deformation." << endl;
+              cout << "Recursively lowering deformation magnitude." << endl;
+            }
+
+            /*--- Load initial deformation values. ---*/
+
+            auto InitialDeformation = TotalDeformation;
+
+            unsigned short ConvexityCheckIter, RecursionDepth = 0;
+            su2double DeformationFactor = 1.0, DeformationDifference = 1.0;
+            for (ConvexityCheckIter = 1; ConvexityCheckIter <= ConvexityCheck_MaxIter; ConvexityCheckIter++) {
+              /*--- Recursively change deformation magnitude (decrease for non-convex elements, increase otherwise). ---*/
+
+              DeformationDifference /= 2.0;
+
+              if (geometry_container[iZone][INST_0][MESH_0]->GetnNonconvexElements() > 0) {
+                DeformationFactor -= DeformationDifference;
+              } else {
+                RecursionDepth += 1;
+
+                if (RecursionDepth == ConvexityCheck_MaxDepth) {
+                  if (rank == MASTER_NODE) {
+                    cout << "Maximum recursion depth reached." << endl;
+                    cout << "Remaining amount of original deformation: ";
+                    cout << DeformationFactor * 100.0 << " percent. " << endl;
+                  }
+                  break;
+                }
+
+                DeformationFactor += DeformationDifference;
+              }
+
+              /*--- Load mesh to start every iteration with an undeformed grid. ---*/
+
+              for (auto iPoint = 0ul; iPoint < OriginalCoordinates.rows(); iPoint++) {
+                for (auto iDim = 0ul; iDim < OriginalCoordinates.cols(); iDim++) {
+                  geometry_container[iZone][INST_0][MESH_0]->nodes->SetCoord(iPoint, iDim, OriginalCoordinates(iPoint, iDim));
                 }
-                
+              }
+
+              /*--- Set deformation magnitude as percentage of initial deformation. ---*/
+
+              for (auto iDV = 0u; iDV < driver_config->GetnDV(); iDV++) {
+                for (auto iDV_Value = 0u; iDV_Value < driver_config->GetnDV_Value(iDV); iDV_Value++) {
+                  config_container[iZone]->SetDV_Value(iDV, iDV_Value,InitialDeformation[iDV][iDV_Value] * DeformationFactor);
+                }
+              }
+
+              /*--- Surface grid deformation. ---*/
+
+              if (rank == MASTER_NODE) cout << "Performing the deformation of the surface grid." << endl;
+
+              TotalDeformation = surface_movement[iZone]->SetSurface_Deformation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
+
+              if (rank == MASTER_NODE)
+                cout << endl << "------------------- Volumetric grid deformation (ZONE " << iZone << ") ----------------" << endl;
+
+              if (rank == MASTER_NODE) cout << "Performing the deformation of the volumetric grid." << endl;
+              grid_movement[iZone][INST_0]->SetVolume_Deformation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], false);
+
+              if (rank == MASTER_NODE) {
+                cout << "Number of non-convex elements for iteration " << ConvexityCheckIter << ": ";
+                cout << geometry_container[iZone][INST_0][MESH_0]->GetnNonconvexElements() << endl;
+                cout << "Remaining amount of original deformation: ";
+                cout << DeformationFactor * 100.0 << " percent. " << endl;
+              }
             }
-            
+          }
         }
-        
+      }
     }
-    
+  }
 }
 
 void CDeformationDriver::Output() {
-    
-    /*--- Output deformed grid for visualization, if requested (surface and volumetric), in parallel
-     requires to move all the data to the master node---*/
-    
-    if (rank == MASTER_NODE) cout << endl << "----------------------- Write deformed grid files -----------------------" << endl;
-    
-    for (iZone = 0; iZone < nZone; iZone++){
-        
-        /*--- Compute Mesh Quality if requested. Necessary geometry preprocessing re-done beforehand. ---*/
-        
-        if (config_container[iZone]->GetWrt_MeshQuality() && !driver_config->GetStructuralProblem()) {
-            
-            if (rank == MASTER_NODE) cout << "Recompute geometry properties necessary to evaluate mesh quality statistics.\n";
-            
-            geometry_container[iZone][INST_0][MESH_0]->SetPoint_Connectivity();
-            geometry_container[iZone][INST_0][MESH_0]->SetBoundVolume();
-            geometry_container[iZone][INST_0][MESH_0]->SetEdges();
-            geometry_container[iZone][INST_0][MESH_0]->SetVertex(config_container[iZone]);
-            geometry_container[iZone][INST_0][MESH_0]->SetControlVolume(config_container[iZone], ALLOCATE);
-            geometry_container[iZone][INST_0][MESH_0]->SetBoundControlVolume(config_container[iZone], ALLOCATE);
-            
-            if (rank == MASTER_NODE) cout << "Computing mesh quality statistics for the dual control volumes.\n";
-            geometry_container[iZone][INST_0][MESH_0]->ComputeMeshQualityStatistics(config_container[iZone]);
-        }// Mesh Quality Output
-        
-        /*--- Load the data --- */
-        
-        output_container[iZone]->Load_Data(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], nullptr);
-        
-        output_container[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone][INST_0][MESH_0], OUTPUT_TYPE::MESH, driver_config->GetMesh_Out_FileName());
-        
-        /*--- Set the file names for the visualization files ---*/
-        
-        output_container[iZone]->SetVolume_Filename("volume_deformed");
-        output_container[iZone]->SetSurface_Filename("surface_deformed");
-        
-        for (unsigned short iFile = 0; iFile < config_container[iZone]->GetnVolumeOutputFiles(); iFile++){
-            auto FileFormat = config_container[iZone]->GetVolumeOutputFiles();
-            if (FileFormat[iFile] != OUTPUT_TYPE::RESTART_ASCII &&
-                FileFormat[iFile] != OUTPUT_TYPE::RESTART_BINARY &&
-                FileFormat[iFile] != OUTPUT_TYPE::CSV)
-                output_container[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone][INST_0][MESH_0], FileFormat[iFile]);
-        }
+  /*--- Output deformed grid for visualization, if requested (surface and volumetric), in parallel
+   requires to move all the data to the master node. ---*/
+
+  if (rank == MASTER_NODE)
+    cout << endl << "----------------------- Write deformed grid files -----------------------" << endl;
+
+  for (iZone = 0; iZone < nZone; iZone++) {
+    /*--- Compute Mesh Quality if requested. Necessary geometry preprocessing re-done beforehand. ---*/
+
+    if (config_container[iZone]->GetWrt_MeshQuality() && !driver_config->GetStructuralProblem()) {
+      if (rank == MASTER_NODE) cout << "Recompute geometry properties necessary to evaluate mesh quality statistics.\n";
+
+      geometry_container[iZone][INST_0][MESH_0]->SetPoint_Connectivity();
+      geometry_container[iZone][INST_0][MESH_0]->SetBoundVolume();
+      geometry_container[iZone][INST_0][MESH_0]->SetEdges();
+      geometry_container[iZone][INST_0][MESH_0]->SetVertex(config_container[iZone]);
+      geometry_container[iZone][INST_0][MESH_0]->SetControlVolume(config_container[iZone], ALLOCATE);
+      geometry_container[iZone][INST_0][MESH_0]->SetBoundControlVolume(config_container[iZone], ALLOCATE);
+
+      if (rank == MASTER_NODE) cout << "Computing mesh quality statistics for the dual control volumes.\n";
+      geometry_container[iZone][INST_0][MESH_0]->ComputeMeshQualityStatistics(config_container[iZone]);
     }
-    
-    if (!driver_config->GetDeform_Mesh()) {
-        if ((config_container[ZONE_0]->GetDesign_Variable(0) != NO_DEFORMATION) &&
-            (config_container[ZONE_0]->GetDesign_Variable(0) != SCALE_GRID)     &&
-            (config_container[ZONE_0]->GetDesign_Variable(0) != TRANSLATE_GRID) &&
-            (config_container[ZONE_0]->GetDesign_Variable(0) != ROTATE_GRID)) {
-            
-            /*--- Write the the free-form deformation boxes after deformation (if defined). ---*/
-            if (!haveSurfaceDeformation) {
-                if (rank == MASTER_NODE) cout << "No FFD information available." << endl;
-            }
-            else {
-                if (rank == MASTER_NODE) cout << "Adding any FFD information to the SU2 file." << endl;
-                
-                surface_movement[ZONE_0]->WriteFFDInfo(surface_movement, geometry_container, config_container);
-            }
-        }
+
+    /*--- Load the data. --- */
+
+    output_container[iZone]->Load_Data(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], nullptr);
+
+    output_container[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone][INST_0][MESH_0],OUTPUT_TYPE::MESH, driver_config->GetMesh_Out_FileName());
+
+    /*--- Set the file names for the visualization files. ---*/
+
+    output_container[iZone]->SetVolume_Filename("volume_deformed");
+    output_container[iZone]->SetSurface_Filename("surface_deformed");
+
+    for (unsigned short iFile = 0; iFile < config_container[iZone]->GetnVolumeOutputFiles(); iFile++) {
+      auto FileFormat = config_container[iZone]->GetVolumeOutputFiles();
+      if (FileFormat[iFile] != OUTPUT_TYPE::RESTART_ASCII && FileFormat[iFile] != OUTPUT_TYPE::RESTART_BINARY &&
+          FileFormat[iFile] != OUTPUT_TYPE::CSV)
+        output_container[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone][INST_0][MESH_0],FileFormat[iFile]);
+    }
+  }
+
+  if (!driver_config->GetDeform_Mesh()) {
+    if ((config_container[ZONE_0]->GetDesign_Variable(0) != NO_DEFORMATION) &&
+        (config_container[ZONE_0]->GetDesign_Variable(0) != SCALE_GRID) &&
+        (config_container[ZONE_0]->GetDesign_Variable(0) != TRANSLATE_GRID) &&
+        (config_container[ZONE_0]->GetDesign_Variable(0) != ROTATE_GRID)) {
+
+      /*--- Write the free form deformation boxes after deformation if defined. ---*/
+      if (!haveSurfaceDeformation) {
+        if (rank == MASTER_NODE) cout << "No FFD information available." << endl;
+      } else {
+        if (rank == MASTER_NODE) cout << "Adding any FFD information to the SU2 file." << endl;
+
+        surface_movement[ZONE_0]->WriteFFDInfo(surface_movement, geometry_container, config_container);
+      }
     }
+  }
 }
 
 void CDeformationDriver::Postprocessing() {
-    
-    if (rank == MASTER_NODE)
-        cout << endl <<"------------------------- Solver Postprocessing -------------------------" << endl;
-    
-    delete driver_config;
-    driver_config = nullptr;
-    
-    for (iZone = 0; iZone < nZone; iZone++) {
-        if (numerics_container[iZone] != nullptr) {
-            for (unsigned int iTerm = 0; iTerm < MAX_TERMS*omp_get_max_threads(); iTerm++) {
-                delete numerics_container[iZone][INST_0][MESH_0][MESH_SOL][iTerm];
-                delete [] numerics_container[iZone][INST_0][MESH_0][MESH_SOL];
-                delete [] numerics_container[iZone][INST_0][MESH_0];
-                delete [] numerics_container[iZone][INST_0];
-            }
-            delete [] numerics_container[iZone];
-        }
-    }
-    delete [] numerics_container;
-    if (rank == MASTER_NODE) cout << "Deleted CNumerics container." << endl;
-    
-    for (iZone = 0; iZone < nZone; iZone++) {
-        if (solver_container[iZone] != nullptr) {
-            delete solver_container[iZone][INST_0][MESH_0][MESH_SOL];
-            delete [] solver_container[iZone][INST_0][MESH_0];
-            delete [] solver_container[iZone][INST_0];
-            delete [] solver_container[iZone];
-        }
+  if (rank == MASTER_NODE)
+    cout << endl << "------------------------- Solver Postprocessing -------------------------" << endl;
+
+  if (driver_config != nullptr) delete[] driver_config;
+
+  for (iZone = 0; iZone < nZone; iZone++) {
+    if (numerics_container[iZone] != nullptr) {
+      for (unsigned int iTerm = 0; iTerm < MAX_TERMS * omp_get_max_threads(); iTerm++) {
+        delete numerics_container[iZone][INST_0][MESH_0][MESH_SOL][iTerm];
+        delete[] numerics_container[iZone][INST_0][MESH_0][MESH_SOL];
+        delete[] numerics_container[iZone][INST_0][MESH_0];
+        delete[] numerics_container[iZone][INST_0];
+      }
+      delete[] numerics_container[iZone];
     }
-    delete [] solver_container;
-    if (rank == MASTER_NODE) cout << "Deleted CSolver container." << endl;
-    
-    if (geometry_container != nullptr) {
-        for (iZone = 0; iZone < nZone; iZone++) {
-            delete geometry_container[iZone][INST_0][MESH_0];
-            delete [] geometry_container[iZone][INST_0];
-            delete [] geometry_container[iZone];
-        }
-        delete [] geometry_container;
+  }
+  delete[] numerics_container;
+  if (rank == MASTER_NODE) cout << "Deleted CNumerics container." << endl;
+
+  for (iZone = 0; iZone < nZone; iZone++) {
+    if (solver_container[iZone] != nullptr) {
+      delete solver_container[iZone][INST_0][MESH_0][MESH_SOL];
+      delete[] solver_container[iZone][INST_0][MESH_0];
+      delete[] solver_container[iZone][INST_0];
+      delete[] solver_container[iZone];
     }
-    if (rank == MASTER_NODE) cout << "Deleted CGeometry container." << endl;
-    
+  }
+  delete[] solver_container;
+  if (rank == MASTER_NODE) cout << "Deleted CSolver container." << endl;
+
+  if (geometry_container != nullptr) {
     for (iZone = 0; iZone < nZone; iZone++) {
-        delete [] FFDBox[iZone];
+      delete geometry_container[iZone][INST_0][MESH_0];
+      delete[] geometry_container[iZone][INST_0];
+      delete[] geometry_container[iZone];
     }
-    delete [] FFDBox;
-    if (rank == MASTER_NODE) cout << "Deleted CFreeFormDefBox class." << endl;
-    
-    if (surface_movement != nullptr) {
-        for (iZone = 0; iZone < nZone; iZone++) {
-            delete surface_movement[iZone];
-        }
-        delete [] surface_movement;
+    delete[] geometry_container;
+  }
+  if (rank == MASTER_NODE) cout << "Deleted CGeometry container." << endl;
+
+  for (iZone = 0; iZone < nZone; iZone++) {
+    delete[] FFDBox[iZone];
+  }
+  delete[] FFDBox;
+  if (rank == MASTER_NODE) cout << "Deleted CFreeFormDefBox class." << endl;
+
+  if (surface_movement != nullptr) {
+    for (iZone = 0; iZone < nZone; iZone++) {
+      delete surface_movement[iZone];
     }
-    if (rank == MASTER_NODE) cout << "Deleted CSurfaceMovement class." << endl;
-    
-    if (grid_movement != nullptr) {
-        for (iZone = 0; iZone < nZone; iZone++) {
-            delete grid_movement[iZone][INST_0];
-            delete [] grid_movement[iZone];
-        }
-        delete [] grid_movement;
+    delete[] surface_movement;
+  }
+  if (rank == MASTER_NODE) cout << "Deleted CSurfaceMovement class." << endl;
+
+  if (grid_movement != nullptr) {
+    for (iZone = 0; iZone < nZone; iZone++) {
+      delete grid_movement[iZone][INST_0];
+      delete[] grid_movement[iZone];
     }
-    if (rank == MASTER_NODE) cout << "Deleted CVolumetricMovement class." << endl;
-    
-    if (config_container != nullptr) {
-        for (iZone = 0; iZone < nZone; iZone++) {
-            delete config_container[iZone];
-        }
-        delete [] config_container;
+    delete[] grid_movement;
+  }
+  if (rank == MASTER_NODE) cout << "Deleted CVolumetricMovement class." << endl;
+
+  if (config_container != nullptr) {
+    for (iZone = 0; iZone < nZone; iZone++) {
+      delete config_container[iZone];
     }
-    if (rank == MASTER_NODE) cout << "Deleted CConfig container." << endl;
-    
-    if (output_container != nullptr) {
-        for (iZone = 0; iZone < nZone; iZone++) {
-            delete output_container[iZone];
-        }
-        delete [] output_container;
+    delete[] config_container;
+  }
+  if (rank == MASTER_NODE) cout << "Deleted CConfig container." << endl;
+
+  if (output_container != nullptr) {
+    for (iZone = 0; iZone < nZone; iZone++) {
+      delete output_container[iZone];
     }
-    if (rank == MASTER_NODE) cout << "Deleted COutput class." << endl;
-    
-    if (nInst != nullptr) delete [] nInst;
-    
-    /*--- Exit the solver cleanly ---*/
-    
-    if (rank == MASTER_NODE)
-        cout << endl << "------------------------- Exit Success (SU2_DEF) ------------------------" << endl << endl;
+    delete[] output_container;
+  }
+  if (rank == MASTER_NODE) cout << "Deleted COutput class." << endl;
+
+  if (nInst != nullptr) delete[] nInst;
+
+  /*--- Exit the solver cleanly. ---*/
+
+  if (rank == MASTER_NODE)
+    cout << endl << "------------------------- Exit Success (SU2_DEF) ------------------------" << endl << endl;
 }
 
 void CDeformationDriver::CommunicateMeshDisplacements(void) {
-    
-    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->InitiateComms(geometry_container[ZONE_0][INST_0][MESH_0], config_container[ZONE_0], MESH_DISPLACEMENTS);
-    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->CompleteComms(geometry_container[ZONE_0][INST_0][MESH_0], config_container[ZONE_0], MESH_DISPLACEMENTS);
-    
+  solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->InitiateComms(geometry_container[ZONE_0][INST_0][MESH_0],config_container[ZONE_0], MESH_DISPLACEMENTS);
+  solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->CompleteComms(geometry_container[ZONE_0][INST_0][MESH_0],config_container[ZONE_0], MESH_DISPLACEMENTS);
 }

From 44c24a53f5b1f7ed6d4267199ae7cd12fc9fc7a9 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Thu, 8 Dec 2022 20:19:31 -0800
Subject: [PATCH 062/656] Update CDiscAdjDeformationDriver

---
 .../drivers/CDiscAdjDeformationDriver.hpp     |  218 +-
 .../src/drivers/CDiscAdjDeformationDriver.cpp | 1898 +++++++++--------
 2 files changed, 1057 insertions(+), 1059 deletions(-)

diff --git a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
index 176f89b93f9..d7857dbf5dc 100644
--- a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file CDiscAdjDeformationDriver.cpp
  * \brief Headers of the main subroutines for driving the projection of sensitivities.
- * \author T. Economon, H. Kline, R. Sanchez
+ * \author T. Economon, H. Kline, R. Sanchez, A. Gastaldi, H. Patel
  * \version 7.3.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
@@ -31,128 +31,118 @@
 #include "../../../Common/include/CConfig.hpp"
 #undef ENABLE_MAPS
 
-#include "../../../Common/include/parallelization/mpi_structure.hpp"
-#include "../../../Common/include/geometry/CGeometry.hpp"
+#include "../../../Common/include/drivers/CDriverBase.hpp"
 #include "../../../Common/include/fem/fem_geometry_structure.hpp"
+#include "../../../Common/include/geometry/CGeometry.hpp"
 #include "../../../Common/include/grid_movement/CSurfaceMovement.hpp"
 #include "../../../Common/include/grid_movement/CVolumetricMovement.hpp"
-#include "../../../SU2_CFD/include/output/COutput.hpp"
+#include "../../../Common/include/parallelization/mpi_structure.hpp"
+#include "../../../SU2_CFD/include/numerics/CGradSmoothing.hpp"
 #include "../../../SU2_CFD/include/output/CBaselineOutput.hpp"
+#include "../../../SU2_CFD/include/output/COutput.hpp"
 #include "../../../SU2_CFD/include/solvers/CBaselineSolver.hpp"
-
-#include "../../../Common/include/drivers/CDriverBase.hpp"
 #include "../../../SU2_CFD/include/solvers/CGradientSmoothingSolver.hpp"
-#include "../../../SU2_CFD/include/numerics/CGradSmoothing.hpp"
 
-/*!
- * \class CDiscAdjDeformationDriver
- * \brief Class for driving sensitivity projections.
- * \author A. Gastaldi, H. Patel
- * \version 7.3.0 "Blackbird"
- */
 class CDiscAdjDeformationDriver : public CDriverBase {
-    
 protected:
-    su2double** Gradient;
-    ofstream Gradient_file; 
-    
+ su2double** Gradient;
+ ofstream Gradient_file;
+
 public:
-    /*!
-     * \brief Constructor of the class.
-     * \param[in] confFile - Configuration file name.
-     * \param[in] MPICommunicator - MPI communicator for SU2.
-     */
-    CDiscAdjDeformationDriver(char* confFile, SU2_Comm MPICommunicator);
-    
-    /*!
-     * \brief Destructor of the class.
-     */
-    ~CDiscAdjDeformationDriver(void);
-    
-    /*!
-     * \brief [Overload] Launch the computation for single-zone problems.
-     */
-    void Run();
-    
-    /*!
-     * \brief Deallocation routine
-     */
-    void Postprocessing();
-    
+ /*!
+  * \brief Constructor of the class.
+  * \param[in] confFile - Configuration file name.
+  * \param[in] MPICommunicator - MPI communicator for SU2.
+  */
+ CDiscAdjDeformationDriver(char* confFile, SU2_Comm MPICommunicator);
+
+ /*!
+  * \brief Destructor of the class.
+  */
+ ~CDiscAdjDeformationDriver(void);
+
+ /*!
+  * \brief Preprocess the driver data (includes solution allocation and initialization).
+  */
+ void Preprocess();
+
+ /*!
+  * \brief Launch the driver computation.
+  */
+ void Run();
+
+ /*!
+  * \brief Deallocation routine.
+  */
+ void Postprocessing();
+
 protected:
-    
-    /*!
-     * \brief Read in the config and mesh files.
-     */
-    void Input_Preprocessing();
-    
-    /*!
-     * \brief Construction of the edge-based data structure.
-     */
-    void Geometrical_Preprocessing();
-    
-    /*!
-     * \brief Preprocess the output container.
-     */
-    void Output_Preprocessing();
-    
-    /*!
-     * \brief Projection of the surface sensitivity using finite differences (FD).
-     * \param[in] geometry - Geometrical definition of the problem.
-     * \param[in] config - Definition of the particular problem.
-     * \param[in] surface_movement - Surface movement class of the problem.
-     * \param[in] Gradient_file - Output file to store the gradient data.
-     */
-    
-    void SetProjection_FD(CGeometry *geometry, CConfig *config, CSurfaceMovement *surface_movement, su2double **Gradient);
-    
-    /*!
-     * \brief Projection of the surface sensitivity using algorithmic differentiation (AD).
-     * \param[in] geometry - Geometrical definition of the problem.
-     * \param[in] config - Definition of the particular problem.
-     * \param[in] surface_movement - Surface movement class of the problem.
-     * \param[in] Gradient_file - Output file to store the gradient data.
-     */
-    
-    void SetProjection_AD(CGeometry *geometry, CConfig *config, CSurfaceMovement *surface_movement, su2double **Gradient);
-    
-    /*!
-     * \brief Prints the gradient information to a file.
-     * \param[in] Gradient - The gradient data.
-     * \param[in] config - Definition of the particular problem.
-     * \param[in] Gradient_file - Output file to store the gradient data.
-     */
-    
-    void OutputGradient(su2double** Gradient, CConfig* config, ofstream& Gradient_file);
-    
-    /*!
-     * \brief Write the sensitivity (including mesh sensitivity) computed with the discrete adjoint method
-     *  on the surface and in the volume to a file.
-     * \param[in] geometry - Geometrical definition of the problem.
-     * \param[in] config - Definition of the particular problem.
-     * \param[in] val_nZone - Number of Zones.
-     */
-    
-    void SetSensitivity_Files(CGeometry ****geometry, CConfig **config, unsigned short val_nZone);
-    
-    /*!
-     * \brief Treatment of derivatives with the Sobolev smoothing solver.
-     * \param[in] geometry - Geometrical definition of the problem.
-     * \param[in] config - Definition of the particular problem.
-     * \param[in] grid_movement - Volumetric movement class of the problem.
-     */
-    
-    void DerivativeTreatment_MeshSensitivity(CGeometry *geometry, CConfig *config, CVolumetricMovement *grid_movement);
-    
-    /*!
-     * \brief Treatment of derivatives with the Sobolev smoothing solver.
-     * \param[in] geometry - Geometrical definition of the problem.
-     * \param[in] config - Definition of the particular problem.
-     * \param[in] grid_movement - Volumetric movement class of the problem.
-     * \param[in] surface_movement - Surface movement class of the problem.
-     * \param[in] Gradient - Output array to store the gradient data.
-     */
-    
-    void DerivativeTreatment_Gradient(CGeometry *geometry, CConfig *config, CVolumetricMovement *grid_movement, CSurfaceMovement *surface_movement, su2double **Gradient);
-    
+ /*!
+  * \brief Read in the config and mesh files.
+  */
+ void Input_Preprocessing();
+
+ /*!
+  * \brief Construction of the edge-based data structure.
+  */
+ void Geometrical_Preprocessing();
+
+ /*!
+  * \brief Preprocess the output container.
+  */
+ void Output_Preprocessing();
+
+ /*!
+  * \brief Projection of the surface sensitivity using finite differences (FD).
+  * \param[in] geometry - Geometrical definition of the problem.
+  * \param[in] config - Definition of the particular problem.
+  * \param[in] surface_movement - Surface movement class of the problem.
+  * \param[in] Gradient_file - Output file to store the gradient data.
+  */
+ void SetProjection_FD(CGeometry* geometry, CConfig* config, CSurfaceMovement* surface_movement, su2double** Gradient);
+
+ /*!
+  * \brief Projection of the surface sensitivity using algorithmic differentiation (AD).
+  * \param[in] geometry - Geometrical definition of the problem.
+  * \param[in] config - Definition of the particular problem.
+  * \param[in] surface_movement - Surface movement class of the problem.
+  * \param[in] Gradient_file - Output file to store the gradient data.
+  */
+ void SetProjection_AD(CGeometry* geometry, CConfig* config, CSurfaceMovement* surface_movement, su2double** Gradient);
+
+ /*!
+  * \brief Prints the gradient information to a file.
+  * \param[in] Gradient - The gradient data.
+  * \param[in] config - Definition of the particular problem.
+  * \param[in] Gradient_file - Output file to store the gradient data.
+  */
+ void OutputGradient(su2double** Gradient, CConfig* config, ofstream& Gradient_file);
+
+ /*!
+  * \brief Write the sensitivity (including mesh sensitivity) computed with the discrete adjoint method
+  *  on the surface and in the volume to a file.
+  * \param[in] geometry - Geometrical definition of the problem.
+  * \param[in] config - Definition of the particular problem.
+  * \param[in] val_nZone - Number of Zones.
+  */
+ void SetSensitivity_Files(CGeometry**** geometry, CConfig** config, unsigned short val_nZone);
+
+ /*!
+  * \brief Treatment of derivatives with the Sobolev smoothing solver.
+  * \param[in] geometry - Geometrical definition of the problem.
+  * \param[in] config - Definition of the particular problem.
+  * \param[in] grid_movement - Volumetric movement class of the problem.
+  */
+ void DerivativeTreatment_MeshSensitivity(CGeometry* geometry, CConfig* config, CVolumetricMovement* grid_movement);
+
+ /*!
+  * \brief Treatment of derivatives with the Sobolev smoothing solver.
+  * \param[in] geometry - Geometrical definition of the problem.
+  * \param[in] config - Definition of the particular problem.
+  * \param[in] grid_movement - Volumetric movement class of the problem.
+  * \param[in] surface_movement - Surface movement class of the problem.
+  * \param[in] Gradient - Output array to store the gradient data.
+  */
+ void DerivativeTreatment_Gradient(CGeometry* geometry, CConfig* config, CVolumetricMovement* grid_movement,
+                                   CSurfaceMovement* surface_movement, su2double** Gradient);
 };
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index 94768b3c0e4..5390c366322 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -31,1027 +31,1035 @@
 
 using namespace std;
 
-CDiscAdjDeformationDriver::CDiscAdjDeformationDriver(char* confFile, SU2_Comm MPICommunicator):
-CDriverBase(confFile, 1, MPICommunicator)
-{
-    /*--- Initialize Medipack (must also be here so it is initialized from python) ---*/
+CDiscAdjDeformationDriver::CDiscAdjDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
+    : CDriverBase(confFile, 1, MPICommunicator) {
+
+/*--- Initialize MeDiPack (must also be here to initialize it from Python). ---*/
 #ifdef HAVE_MPI
 #if defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)
-    SU2_MPI::Init_AMPI();
+  SU2_MPI::Init_AMPI();
 #endif
 #endif
-    
-    SU2_MPI::SetComm(MPICommunicator);
-    
-    rank = SU2_MPI::GetRank();
-    size = SU2_MPI::GetSize();
-    
-    /*--- Initialize containers --- */
-    
-    SetContainers_Null();
-    
-    /*--- Preprocessing of the config files. ---*/
-    
-    Input_Preprocessing();
-    
-    /*--- Set up a timer for performance benchmarking ---*/
-    
-    StartTime = SU2_MPI::Wtime();
-    
-    /*--- Preprocessing of the geometry for all zones. ---*/
-    
-    Geometrical_Preprocessing();
-    
-    /*--- Preprocessing of the outputs for all zones. ---*/
-    
-    Output_Preprocessing();
-    
-    /*--- Preprocessing time is reported now, but not included in the next compute portion. ---*/
-    
-    StopTime = SU2_MPI::Wtime();
-    
-    /*--- Compute/print the total time for performance benchmarking. ---*/
-    
-    UsedTime = StopTime-StartTime;
-    UsedTimePreproc    = UsedTime;
-    UsedTimeCompute    = 0.0;
-    
-}
 
-CDiscAdjDeformationDriver::~CDiscAdjDeformationDriver(void) {
-    
+  SU2_MPI::SetComm(MPICommunicator);
+
+  rank = SU2_MPI::GetRank();
+  size = SU2_MPI::GetSize();
+
+  /*--- Initialize containers. --- */
+
+  SetContainers_Null();
+
+  /*--- Preprocessing of the config files. ---*/
+
+  Input_Preprocessing();
+
+  /*--- Initialize structure to store the gradient. ---*/
+
+  unsigned short nDV = config_container[ZONE_0]->GetnDV();
+  Gradient = new su2double*[nDV];
+
+  for (auto iDV = 0u; iDV < nDV; iDV++) {
+    /*--- Initialize to zero ---*/
+    unsigned short nValue = config_container[ZONE_0]->GetnDV_Value(iDV);
+
+    Gradient[iDV] = new su2double[nValue];
+  }
+
+  /*--- Set up a timer for performance benchmarking. ---*/
+
+  StartTime = SU2_MPI::Wtime();
+
+  /*--- Preprocessing of the geometry for all zones. ---*/
+
+  Geometrical_Preprocessing();
+
+  /*--- Preprocessing of the outputs for all zones. ---*/
+
+  Output_Preprocessing();
+
+  /*--- Preprocessing time is reported now, but not included in the next compute portion. ---*/
+
+  StopTime = SU2_MPI::Wtime();
+
+  /*--- Compute the total time for performance benchmarking. ---*/
+
+  UsedTime = StopTime - StartTime;
+  UsedTimePreproc = UsedTime;
+  UsedTimeCompute = 0.0;
 }
 
+CDiscAdjDeformationDriver::~CDiscAdjDeformationDriver(void) {}
+
 void CDiscAdjDeformationDriver::Input_Preprocessing() {
-    
-    /*--- Initialize a char to store the zone filename ---*/
-    char zone_file_name[MAX_STRING_SIZE];
-    
-    /*--- Initialize the configuration of the driver ---*/
-    driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DEF);
-    
-    nZone = driver_config->GetnZone();
-    
-    /*--- Loop over all zones to initialize the various classes. In most
-     cases, nZone is equal to one. This represents the solution of a partial
-     differential equation on a single block, unstructured mesh. ---*/
-    
-    for (iZone = 0; iZone < nZone; iZone++) {
-        
-        /*--- Definition of the configuration option class for all zones. In this
-         constructor, the input configuration file is parsed and all options are
-         read and stored. ---*/
-        
-        if (driver_config->GetnConfigFiles() > 0){
-            strcpy(zone_file_name, driver_config->GetConfigFilename(iZone).c_str());
-            config_container[iZone] = new CConfig(driver_config, zone_file_name, SU2_COMPONENT::SU2_DOT, iZone, nZone, true);
-        } else {
-            config_container[iZone] = new CConfig(driver_config, config_file_name, SU2_COMPONENT::SU2_DOT, iZone, nZone, true);
-        }
-        
-        config_container[iZone]->SetMPICommunicator(SU2_MPI::GetComm());
-        
-        if (!config_container[iZone]->GetDiscrete_Adjoint()) {
-            SU2_MPI::Error("The discrete adjoint solver was not specified in the configuration file.", CURRENT_FUNCTION);
-        }
-        
+  /*--- Initialize a char to store the zone filename. ---*/
+
+  char zone_file_name[MAX_STRING_SIZE];
+
+  /*--- Initialize the configuration of the driver. ---*/
+
+  driver_config = new CConfig(config_file_name, SU2_COMPONENT::SU2_DEF);
+
+  nZone = driver_config->GetnZone();
+
+  /*--- Loop over all zones to initialize the various classes. In most
+   * cases, nZone is equal to one. This represents the solution of a partial
+   * differential equation on a single block, unstructured mesh. ---*/
+
+  for (iZone = 0; iZone < nZone; iZone++) {
+    /*--- Definition of the configuration option class for all zones. In this
+     * constructor, the input configuration file is parsed and all options are
+     * read and stored. ---*/
+
+    if (driver_config->GetnConfigFiles() > 0) {
+      strcpy(zone_file_name, driver_config->GetConfigFilename(iZone).c_str());
+      config_container[iZone] = new CConfig(driver_config, zone_file_name, SU2_COMPONENT::SU2_DOT, iZone, nZone, true);
+    } else {
+      config_container[iZone] = new CConfig(driver_config, config_file_name, SU2_COMPONENT::SU2_DOT, iZone, nZone, true);
     }
-    
-    /*--- Set the multizone part of the problem. ---*/
-    if (driver_config->GetMultizone_Problem()){
-        for (iZone = 0; iZone < nZone; iZone++) {
-            /*--- Set the interface markers for multizone ---*/
-            config_container[iZone]->SetMultizone(driver_config, config_container);
-        }
+
+    config_container[iZone]->SetMPICommunicator(SU2_MPI::GetComm());
+
+    if (!config_container[iZone]->GetDiscrete_Adjoint()) {
+      SU2_MPI::Error("The discrete adjoint solver was not specified in the configuration file.", CURRENT_FUNCTION);
+    }
+  }
+
+  /*--- Set the multi-zone part of the problem. ---*/
+
+  if (driver_config->GetMultizone_Problem()) {
+    for (iZone = 0; iZone < nZone; iZone++) {
+      /*--- Set the interface markers for multi-zone. ---*/
+
+      config_container[iZone]->SetMultizone(driver_config, config_container);
     }
+  }
 
-    /*--- Keep a reference to the main (ZONE 0) config ---*/
-    main_config = config_container[ZONE_0];
+  /*--- Keep a reference to the main (ZONE 0) config. ---*/
+
+  main_config = config_container[ZONE_0];
 }
 
 void CDiscAdjDeformationDriver::Geometrical_Preprocessing() {
-    
-    /*--- Loop over all zones to initialize the various classes. In most
-     cases, nZone is equal to one. This represents the solution of a partial
-     differential equation on a single block, unstructured mesh. ---*/
-    unsigned short nMesh = 1;
-    
-    for (iZone = 0; iZone < nZone; iZone++) {
-        
-        /*--- Determine whether or not the FEM solver is used, which decides the
-         type of geometry classes that are instantiated. ---*/
-        const bool fem_solver = config_container[iZone]->GetFEMSolver();
-        
-        /*--- Read the number of instances for each zone ---*/
-        
-        nInst[iZone] = config_container[iZone]->GetnTimeInstances();
-        
-        geometry_container[iZone] = new CGeometry**[nInst[iZone]];
-        
-        for (iInst = 0; iInst < nInst[iZone]; iInst++){
-            
-            /*--- Definition of the geometry class to store the primal grid in the partitioning process. ---*/
-            
-            CGeometry *geometry_aux = nullptr;
-            
-            /*--- All ranks process the grid and call ParMETIS for partitioning ---*/
-            
-            geometry_aux = new CPhysicalGeometry(config_container[iZone], iZone, nZone);
-            
-            /*--- Color the initial grid and set the send-receive domains (ParMETIS) ---*/
-            
-            if ( fem_solver ) geometry_aux->SetColorFEMGrid_Parallel(config_container[iZone]);
-            else              geometry_aux->SetColorGrid_Parallel(config_container[iZone]);
-            
-            /*--- Build the grid data structures using the ParMETIS coloring. ---*/
-            
-            if( fem_solver ) {
-                switch( config_container[iZone]->GetKind_FEM_Flow() ) {
-                    case DG: {
-                        geometry_container[iZone][iInst] = new CGeometry*[nMesh];
-                        geometry_container[iZone][iInst][MESH_0] = new CMeshFEM_DG(geometry_aux, config_container[iZone]);
-                        break;
-                    }
-                }
-            }
-            else {
-                geometry_container[iZone][iInst] = new CGeometry*[nMesh];
-                geometry_container[iZone][iInst][MESH_0] = new CPhysicalGeometry(geometry_aux, config_container[iZone]);
-            }
-            
-            /*--- Deallocate the memory of geometry_aux ---*/
-            
-            delete geometry_aux;
-            
-            /*--- Add the Send/Receive boundaries ---*/
-            
-            geometry_container[iZone][iInst][MESH_0]->SetSendReceive(config_container[iZone]);
-            
-            /*--- Add the Send/Receive boundaries ---*/
-            
-            geometry_container[iZone][iInst][MESH_0]->SetBoundaries(config_container[iZone]);
-            
-            /*--- Create the vertex structure (required for MPI) ---*/
-            
-            if (rank == MASTER_NODE) cout << "Identify vertices." << endl;
-            geometry_container[iZone][iInst][MESH_0]->SetVertex(config_container[iZone]);
-            
-            /*--- Store the global to local mapping after preprocessing. ---*/
-            
-            if (rank == MASTER_NODE) cout << "Storing a mapping from global to local point index." << endl;
-            geometry_container[iZone][iInst][MESH_0]->SetGlobal_to_Local_Point();
-            
-            /* Test for a fem solver, because some more work must be done. */
-            
-            if (fem_solver) {
-                
-                /*--- Carry out a dynamic cast to CMeshFEM_DG, such that it is not needed to
-                 define all virtual functions in the base class CGeometry. ---*/
-                CMeshFEM_DG *DGMesh = dynamic_cast<CMeshFEM_DG *>(geometry_container[iZone][iInst][MESH_0]);
-                
-                /*--- Determine the standard elements for the volume elements. ---*/
-                if (rank == MASTER_NODE) cout << "Creating standard volume elements." << endl;
-                DGMesh->CreateStandardVolumeElements(config_container[iZone]);
-                
-                /*--- Create the face information needed to compute the contour integral
-                 for the elements in the Discontinuous Galerkin formulation. ---*/
-                if (rank == MASTER_NODE) cout << "Creating face information." << endl;
-                DGMesh->CreateFaces(config_container[iZone]);
-            }
-        }
-        
-        if (rank == MASTER_NODE)
-            cout << "\n----------------------- Preprocessing computations ----------------------" << endl;
-        
-        /*--- Compute elements surrounding points, points surrounding points ---*/
-        
-        if (rank == MASTER_NODE) cout << "Setting local point connectivity." << endl;
-        geometry_container[iZone][INST_0][MESH_0]->SetPoint_Connectivity();
-        
-        /*--- Check the orientation before computing geometrical quantities ---*/
-        
-        geometry_container[iZone][INST_0][MESH_0]->SetBoundVolume();
-        if (config_container[iZone]->GetReorientElements()) {
-            if (rank == MASTER_NODE) cout << "Checking the numerical grid orientation of the elements." << endl;
-            geometry_container[iZone][INST_0][MESH_0]->Check_IntElem_Orientation(config_container[iZone]);
-            geometry_container[iZone][INST_0][MESH_0]->Check_BoundElem_Orientation(config_container[iZone]);
+  /*--- Loop over all zones to initialize the various classes. In most
+   * cases, nZone is equal to one. This represents the solution of a partial
+   * differential equation on a single block, unstructured mesh. ---*/
+
+  unsigned short nMesh = 1;
+
+  for (iZone = 0; iZone < nZone; iZone++) {
+    /*--- Determine if the FEM solver is used, which decides the type of geometry classes that are instantiated. ---*/
+
+    const bool fem_solver = config_container[iZone]->GetFEMSolver();
+
+    /*--- Read the number of instances for each zone. ---*/
+
+    nInst[iZone] = config_container[iZone]->GetnTimeInstances();
+
+    geometry_container[iZone] = new CGeometry**[nInst[iZone]];
+
+    for (iInst = 0; iInst < nInst[iZone]; iInst++) {
+      /*--- Definition of the geometry class to store the primal grid in the partitioning process. ---*/
+
+      CGeometry* geometry_aux = nullptr;
+
+      /*--- All ranks process the grid and call ParMETIS for partitioning. ---*/
+
+      geometry_aux = new CPhysicalGeometry(config_container[iZone], iZone, nZone);
+
+      /*--- Color the initial grid and set the send-receive domains (ParMETIS). ---*/
+
+      if (fem_solver) {
+        geometry_aux->SetColorFEMGrid_Parallel(config_container[iZone]);
+      } else {
+        geometry_aux->SetColorGrid_Parallel(config_container[iZone]);
+      }
+
+      /*--- Build the grid data structures using the ParMETIS coloring. ---*/
+
+      if (fem_solver) {
+        switch (config_container[iZone]->GetKind_FEM_Flow()) {
+          case DG:
+            geometry_container[iZone][iInst] = new CGeometry*[nMesh];
+            geometry_container[iZone][iInst][MESH_0] = new CMeshFEM_DG(geometry_aux, config_container[iZone]);
+            break;
         }
-        
-        /*--- Create the edge structure ---*/
-        
-        if (rank == MASTER_NODE) cout << "Identify edges and vertices." << endl;
-        geometry_container[iZone][INST_0][MESH_0]->SetEdges(); geometry_container[iZone][INST_0][MESH_0]->SetVertex(config_container[iZone]);
-        
-        /*--- Create the dual control volume structures ---*/
-        
-        if (rank == MASTER_NODE) cout << "Setting the bound control volume structure." << endl;
-        geometry_container[iZone][INST_0][MESH_0]->SetBoundControlVolume(config_container[ZONE_0], ALLOCATE);
-        
-        /*--- Store the global to local mapping after preprocessing. ---*/
-        
-        if (rank == MASTER_NODE) cout << "Storing a mapping from global to local point index." << endl;
-        geometry_container[iZone][INST_0][MESH_0]->SetGlobal_to_Local_Point();
-        
-        /*--- Create the point-to-point MPI communication structures. ---*/
-        
-        geometry_container[iZone][INST_0][MESH_0]->PreprocessP2PComms(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
-        
+      } else {
+        geometry_container[iZone][iInst] = new CGeometry*[nMesh];
+        geometry_container[iZone][iInst][MESH_0] = new CPhysicalGeometry(geometry_aux, config_container[iZone]);
+      }
+
+      /*--- Deallocate the memory of geometry_aux. ---*/
+
+      delete geometry_aux;
+
+      /*--- Add the Send/Receive boundaries. ---*/
+
+      geometry_container[iZone][iInst][MESH_0]->SetSendReceive(config_container[iZone]);
+
+      /*--- Add the Send/Receive boundaries. ---*/
+
+      geometry_container[iZone][iInst][MESH_0]->SetBoundaries(config_container[iZone]);
+
+      /*--- Create the vertex structure (required for MPI). ---*/
+
+      if (rank == MASTER_NODE) cout << "Identify vertices." << endl;
+      geometry_container[iZone][iInst][MESH_0]->SetVertex(config_container[iZone]);
+
+      /*--- Store the global to local mapping after preprocessing. ---*/
+
+      if (rank == MASTER_NODE) cout << "Storing a mapping from global to local point index." << endl;
+      geometry_container[iZone][iInst][MESH_0]->SetGlobal_to_Local_Point();
+
+      /*--- Test for a fem solver, because some more work must be done. ---*/
+
+      if (fem_solver) {
+        /*--- Carry out a dynamic cast to CMeshFEM_DG, such that it is not needed to
+         * define all virtual functions in the base class CGeometry. ---*/
+
+        CMeshFEM_DG* DGMesh = dynamic_cast<CMeshFEM_DG*>(geometry_container[iZone][iInst][MESH_0]);
+
+        /*--- Determine the standard elements for the volume elements. ---*/
+
+        if (rank == MASTER_NODE) cout << "Creating standard volume elements." << endl;
+        DGMesh->CreateStandardVolumeElements(config_container[iZone]);
+
+        /*--- Create the face information needed to compute the contour integral
+         * for the elements in the Discontinuous Galerkin formulation. ---*/
+
+        if (rank == MASTER_NODE) cout << "Creating face information." << endl;
+        DGMesh->CreateFaces(config_container[iZone]);
+      }
     }
 
-    /*--- Keep a reference to the main (ZONE_0, INST_0, MESH_0) geometry ---*/
-    main_geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+    if (rank == MASTER_NODE)
+      cout << "\n----------------------- Preprocessing computations ----------------------" << endl;
+
+    /*--- Compute elements surrounding points, points surrounding points. ---*/
+
+    if (rank == MASTER_NODE) cout << "Setting local point connectivity." << endl;
+    geometry_container[iZone][INST_0][MESH_0]->SetPoint_Connectivity();
+
+    /*--- Check the orientation before computing geometrical quantities. ---*/
+
+    geometry_container[iZone][INST_0][MESH_0]->SetBoundVolume();
+    if (config_container[iZone]->GetReorientElements()) {
+      if (rank == MASTER_NODE) cout << "Checking the numerical grid orientation of the elements." << endl;
+      geometry_container[iZone][INST_0][MESH_0]->Check_IntElem_Orientation(config_container[iZone]);
+      geometry_container[iZone][INST_0][MESH_0]->Check_BoundElem_Orientation(config_container[iZone]);
+    }
+
+    /*--- Create the edge structure. ---*/
+
+    if (rank == MASTER_NODE) cout << "Identify edges and vertices." << endl;
+    geometry_container[iZone][INST_0][MESH_0]->SetEdges();
+    geometry_container[iZone][INST_0][MESH_0]->SetVertex(config_container[iZone]);
+
+    /*--- Create the dual control volume structures. ---*/
+
+    if (rank == MASTER_NODE) cout << "Setting the bound control volume structure." << endl;
+    geometry_container[iZone][INST_0][MESH_0]->SetBoundControlVolume(config_container[ZONE_0], ALLOCATE);
+
+    /*--- Store the global to local mapping after preprocessing. ---*/
+
+    if (rank == MASTER_NODE) cout << "Storing a mapping from global to local point index." << endl;
+    geometry_container[iZone][INST_0][MESH_0]->SetGlobal_to_Local_Point();
 
+    /*--- Create the point-to-point MPI communication structures. ---*/
+
+    geometry_container[iZone][INST_0][MESH_0]->PreprocessP2PComms(geometry_container[iZone][INST_0][MESH_0],
+                                                                  config_container[iZone]);
+  }
+
+  /*--- Keep a reference to the main (ZONE_0, INST_0, MESH_0) geometry. ---*/
+
+  main_geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 }
 
-void CDiscAdjDeformationDriver::Output_Preprocessing() {
-    
+void CDiscAdjDeformationDriver::Output_Preprocessing() {}
+
+void CDiscAdjDeformationDriver::Preprocess() {
+  for (iZone = 0; iZone < nZone; iZone++) {
+    if (rank == MASTER_NODE) cout << "Reading volume sensitivities at each node from file." << endl;
+    unsigned short nInst_Zone = nInst[iZone];
+
+    grid_movement[iZone] = new CVolumetricMovement*[nInst_Zone]();
+    grid_movement[iZone][INST_0] = new CVolumetricMovement(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
+
+    /*--- Read in sensitivities from file. ---*/
+
+    if (config_container[ZONE_0]->GetSensitivity_Format() == UNORDERED_ASCII)
+      geometry_container[iZone][INST_0][MESH_0]->ReadUnorderedSensitivity(config_container[iZone]);
+    else
+      geometry_container[iZone][INST_0][MESH_0]->SetSensitivity(config_container[iZone]);
+  }
 }
 
 void CDiscAdjDeformationDriver::Run() {
-    
-    for (iZone = 0; iZone < nZone; iZone++) {
-        if (rank == MASTER_NODE) cout << "Reading volume sensitivities at each node from file." << endl;
-        unsigned short nInst_Zone = nInst[iZone];
-        
-        grid_movement[iZone] = new CVolumetricMovement* [nInst_Zone] ();
-        grid_movement[iZone][INST_0] = new CVolumetricMovement(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
-        
-        /*--- Read in sensitivities from file. ---*/
-        if (config_container[ZONE_0]->GetSensitivity_Format() == UNORDERED_ASCII)
-            geometry_container[iZone][INST_0][MESH_0]->ReadUnorderedSensitivity(config_container[iZone]);
-        else
-            geometry_container[iZone][INST_0][MESH_0]->SetSensitivity(config_container[iZone]);
-        
-        if (rank == MASTER_NODE) cout << "\n---------------------- Mesh sensitivity computation ---------------------" << endl;
-        if (config_container[iZone]->GetDiscrete_Adjoint() && config_container[iZone]->GetSmoothGradient() &&
-            config_container[iZone]->GetSobMode() == ENUM_SOBOLEV_MODUS::MESH_LEVEL) {
-            DerivativeTreatment_MeshSensitivity(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], grid_movement[iZone][INST_0]);
+  for (iZone = 0; iZone < nZone; iZone++) {
+    if (rank == MASTER_NODE)
+      cout << "\n---------------------- Mesh sensitivity computation ---------------------" << endl;
+    if (config_container[iZone]->GetDiscrete_Adjoint() && config_container[iZone]->GetSmoothGradient() &&
+        config_container[iZone]->GetSobMode() == ENUM_SOBOLEV_MODUS::MESH_LEVEL) {
+      DerivativeTreatment_MeshSensitivity(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], grid_movement[iZone][INST_0]);
+    } else {
+      grid_movement[iZone][INST_0]->SetVolume_Deformation(geometry_container[iZone][INST_0][MESH_0],
+                                                          config_container[iZone], false, true);
+    }
+  }
+
+  if (rank == MASTER_NODE)
+    cout << "\n------------------------ Mesh sensitivity Output ------------------------" << endl;
+
+  SetSensitivity_Files(geometry_container, config_container, nZone);
+
+  Gradient_file.precision(driver_config->OptionIsSet("OUTPUT_PRECISION") ? driver_config->GetOutput_Precision() : 6);
+
+  /*--- For multi-zone computations the gradient contributions are summed up and written into one file. ---*/
+
+  for (iZone = 0; iZone < nZone; iZone++) {
+    if ((config_container[iZone]->GetDesign_Variable(0) != NONE) &&
+        (config_container[iZone]->GetDesign_Variable(0) != SURFACE_FILE)) {
+      if (rank == MASTER_NODE)
+        cout << "\n---------- Start gradient evaluation using sensitivity information ----------" << endl;
+
+      /*--- Definition of the Class for surface deformation. ---*/
+
+      surface_movement[iZone] = new CSurfaceMovement();
+
+      /*--- Copy coordinates to the surface structure. ---*/
+
+      surface_movement[iZone]->CopyBoundary(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
+
+      /*--- If AD mode is enabled we can use it to compute the projection, otherwise we use finite differences. ---*/
+
+      if (config_container[iZone]->GetAD_Mode()) {
+        if (config_container[iZone]->GetSmoothGradient()) {
+          DerivativeTreatment_Gradient(geometry_container[iZone][INST_0][MESH_0], config_container[iZone],
+                                       grid_movement[iZone][INST_0], surface_movement[iZone], Gradient);
         } else {
-            grid_movement[iZone][INST_0]->SetVolume_Deformation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], false, true);
+          SetProjection_AD(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], surface_movement[iZone], Gradient);
         }
+      } else {
+        SetProjection_FD(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], surface_movement[iZone], Gradient);
+      }
     }
-    
-    if (rank == MASTER_NODE) cout << "\n------------------------ Mesh sensitivity Output ------------------------" << endl;
-    SetSensitivity_Files(geometry_container, config_container, nZone);
-    
-    /*--- Initialize structure to store the gradient ---*/
-    Gradient = new su2double*[config_container[ZONE_0]->GetnDV()];
-    
-    for (auto iDV = 0u; iDV  < config_container[ZONE_0]->GetnDV(); iDV++) {
-        /*--- Initialize to zero ---*/
-        Gradient[iDV] = new su2double[config_container[ZONE_0]->GetnDV_Value(iDV)]();
-    }
-    
-    Gradient_file.precision(driver_config->OptionIsSet("OUTPUT_PRECISION") ? driver_config->GetOutput_Precision() : 6);
-    
-    /*--- For multizone computations the gradient contributions are summed up and written into one file. ---*/
-    for (iZone = 0; iZone < nZone; iZone++){
-        if ((config_container[iZone]->GetDesign_Variable(0) != NONE) &&
-            (config_container[iZone]->GetDesign_Variable(0) != SURFACE_FILE)) {
-            
-            if (rank == MASTER_NODE)
-                cout << "\n---------- Start gradient evaluation using sensitivity information ----------" << endl;
-            
-            /*--- Definition of the Class for surface deformation ---*/
-            
-            surface_movement[iZone] = new CSurfaceMovement();
-            
-            /*--- Copy coordinates to the surface structure ---*/
-            
-            surface_movement[iZone]->CopyBoundary(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
-
-            /*--- If AD mode is enabled we can use it to compute the projection,
-             *    otherwise we use finite differences. ---*/
-            
-            if (config_container[iZone]->GetAD_Mode()) {
-                if (config_container[iZone]->GetSmoothGradient()) {
-                    DerivativeTreatment_Gradient(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], grid_movement[iZone][INST_0], surface_movement[iZone] , Gradient);
-                } else {
-                    SetProjection_AD(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], surface_movement[iZone] , Gradient);
-                }
-            } else {
-                SetProjection_FD(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], surface_movement[iZone] , Gradient);
-            }
-        }
-    } // for iZone
-    
-    /*--- Write the gradient to a file ---*/
-    
-    if (rank == MASTER_NODE)
-        Gradient_file.open(config_container[ZONE_0]->GetObjFunc_Grad_FileName().c_str(), ios::out);
-    
-    /*--- Print gradients to screen and writes to file ---*/
-    
-    OutputGradient(Gradient, config_container[ZONE_0], Gradient_file);
-    
+  }
+
+  /*--- Write the gradient to a file. ---*/
+
+  if (rank == MASTER_NODE) Gradient_file.open(config_container[ZONE_0]->GetObjFunc_Grad_FileName().c_str(), ios::out);
+
+  /*--- Print gradients to screen and writes to file. ---*/
+
+  OutputGradient(Gradient, config_container[ZONE_0], Gradient_file);
 }
 
 void CDiscAdjDeformationDriver::Postprocessing() {
-    
-    for (auto iDV = 0u; iDV  < config_container[ZONE_0]->GetnDV(); iDV++){
-        delete [] Gradient[iDV];
+  for (auto iDV = 0u; iDV < config_container[ZONE_0]->GetnDV(); iDV++) {
+    delete[] Gradient[iDV];
+  }
+  delete[] Gradient;
+
+  delete driver_config;
+  driver_config = nullptr;
+
+  if (rank == MASTER_NODE)
+    cout << "\n------------------------- Solver Postprocessing -------------------------" << endl;
+
+  for (iZone = 0; iZone < nZone; iZone++) {
+    if (numerics_container[iZone] != nullptr) {
+      delete[] numerics_container[iZone];
     }
-    delete [] Gradient;
-    
-    delete driver_config;
-    driver_config = nullptr;
-    
-    if (rank == MASTER_NODE)
-        cout << "\n------------------------- Solver Postprocessing -------------------------" << endl;
-    
-    for (iZone = 0; iZone < nZone; iZone++) {
-        if (numerics_container[iZone] != nullptr) {
-            delete [] numerics_container[iZone];
-        }
+  }
+  delete[] numerics_container;
+  if (rank == MASTER_NODE) cout << "Deleted CNumerics container." << endl;
+
+  for (iZone = 0; iZone < nZone; iZone++) {
+    if (solver_container[iZone] != nullptr) {
+      delete[] solver_container[iZone];
     }
-    delete [] numerics_container;
-    if (rank == MASTER_NODE) cout << "Deleted CNumerics container." << endl;
-    
+  }
+  delete[] solver_container;
+  if (rank == MASTER_NODE) cout << "Deleted CSolver container." << endl;
+
+  if (geometry_container != nullptr) {
     for (iZone = 0; iZone < nZone; iZone++) {
-        if (solver_container[iZone] != nullptr) {
-            delete [] solver_container[iZone];
+      if (geometry_container[iZone] != nullptr) {
+        for (iInst = 0; iInst < nInst[iZone]; iInst++) {
+          delete geometry_container[iZone][iInst][MESH_0];
+          delete[] geometry_container[iZone][iInst];
         }
+        delete[] geometry_container[iZone];
+      }
     }
-    delete [] solver_container;
-    if (rank == MASTER_NODE) cout << "Deleted CSolver container." << endl;
-    
-    if (geometry_container != nullptr) {
-        for (iZone = 0; iZone < nZone; iZone++) {
-            if (geometry_container[iZone] != nullptr) {
-                for (iInst = 0; iInst < nInst[iZone]; iInst++){
-                    delete geometry_container[iZone][iInst][MESH_0];
-                    delete [] geometry_container[iZone][iInst];
-                }
-                delete [] geometry_container[iZone];
-            }
-        }
-        delete [] geometry_container;
-    }
-    if (rank == MASTER_NODE) cout << "Deleted CGeometry container." << endl;
-    
+    delete[] geometry_container;
+  }
+  if (rank == MASTER_NODE) cout << "Deleted CGeometry container." << endl;
+
+  for (iZone = 0; iZone < nZone; iZone++) {
+    delete[] FFDBox[iZone];
+  }
+  delete[] FFDBox;
+  if (rank == MASTER_NODE) cout << "Deleted CFreeFormDefBox class." << endl;
+
+  if (surface_movement != nullptr) {
     for (iZone = 0; iZone < nZone; iZone++) {
-        delete [] FFDBox[iZone];
+      delete surface_movement[iZone];
     }
-    delete [] FFDBox;
-    if (rank == MASTER_NODE) cout << "Deleted CFreeFormDefBox class." << endl;
-    
-    if (surface_movement != nullptr) {
-        for (iZone = 0; iZone < nZone; iZone++) {
-            delete surface_movement[iZone];
-        }
-        delete [] surface_movement;
-    }
-    if (rank == MASTER_NODE) cout << "Deleted CSurfaceMovement class." << endl;
-    
-    if (grid_movement != nullptr) {
-        for (iZone = 0; iZone < nZone; iZone++) {
-            if (grid_movement[iZone] != nullptr) {
-                for (iInst = 0; iInst < nInst[iZone]; iInst++){
-                    delete grid_movement[iZone][iInst];
-                }
-                delete [] grid_movement[iZone];
-            }
+    delete[] surface_movement;
+  }
+  if (rank == MASTER_NODE) cout << "Deleted CSurfaceMovement class." << endl;
+
+  if (grid_movement != nullptr) {
+    for (iZone = 0; iZone < nZone; iZone++) {
+      if (grid_movement[iZone] != nullptr) {
+        for (iInst = 0; iInst < nInst[iZone]; iInst++) {
+          delete grid_movement[iZone][iInst];
         }
-        delete [] grid_movement;
+        delete[] grid_movement[iZone];
+      }
     }
-    if (rank == MASTER_NODE) cout << "Deleted CVolumetricMovement class." << endl;
-    
-    if (config_container != nullptr) {
-        for (iZone = 0; iZone < nZone; iZone++) {
-            delete config_container[iZone];
-        }
-        delete [] config_container;
+    delete[] grid_movement;
+  }
+  if (rank == MASTER_NODE) cout << "Deleted CVolumetricMovement class." << endl;
+
+  if (config_container != nullptr) {
+    for (iZone = 0; iZone < nZone; iZone++) {
+      delete config_container[iZone];
     }
-    if (rank == MASTER_NODE) cout << "Deleted CConfig container." << endl;
-    
-    if (output_container != nullptr) {
-        for (iZone = 0; iZone < nZone; iZone++) {
-            delete output_container[iZone];
-        }
-        delete [] output_container;
+    delete[] config_container;
+  }
+  if (rank == MASTER_NODE) cout << "Deleted CConfig container." << endl;
+
+  if (output_container != nullptr) {
+    for (iZone = 0; iZone < nZone; iZone++) {
+      delete output_container[iZone];
     }
-    if (rank == MASTER_NODE) cout << "Deleted COutput class." << endl;
-    
-    if (nInst != nullptr) delete [] nInst;
-    
-    /*--- Exit the solver cleanly ---*/
-    
-    if (rank == MASTER_NODE)
-        cout << endl << "------------------------- Exit Success (SU2_DEF_AD) ------------------------" << endl << endl;
-    
+    delete[] output_container;
+  }
+  if (rank == MASTER_NODE) cout << "Deleted COutput class." << endl;
+
+  if (nInst != nullptr) delete[] nInst;
+
+  /*--- Exit the solver cleanly. ---*/
+
+  if (rank == MASTER_NODE)
+    cout << endl << "------------------------- Exit Success (SU2_DEF_AD) ------------------------" << endl << endl;
 }
 
-void CDiscAdjDeformationDriver::SetProjection_FD(CGeometry *geometry, CConfig *config, CSurfaceMovement *surface_movement, su2double** Gradient){
-    
-    unsigned short iDV, nDV, iFFDBox, nDV_Value, iMarker, iDim;
-    unsigned long iVertex, iPoint;
-    su2double delta_eps, my_Gradient, localGradient, *Normal, dS, *VarCoord, Sensitivity,
-    dalpha[3], deps[3], dalpha_deps;
-    bool *UpdatePoint, MoveSurface, Local_MoveSurface;
-    CFreeFormDefBox **FFDBox;
-    
-    int rank = SU2_MPI::GetRank();
-    
-    nDV = config->GetnDV();
-    
-    /*--- Boolean controlling points to be updated ---*/
-    
-    UpdatePoint = new bool[geometry->GetnPoint()];
-    
-    /*--- Definition of the FFD deformation class ---*/
-    
-    unsigned short nFFDBox = MAX_NUMBER_FFD;
-    FFDBox = new CFreeFormDefBox*[nFFDBox];
-    for (iFFDBox = 0; iFFDBox < MAX_NUMBER_FFD; iFFDBox++) FFDBox[iFFDBox] = nullptr;
-    
-    for (iDV = 0; iDV  < nDV; iDV++){
-        nDV_Value = config->GetnDV_Value(iDV);
-        if (nDV_Value != 1){
-            SU2_MPI::Error("The projection using finite differences currently only supports a fixed direction of movement for FFD points.", CURRENT_FUNCTION);
-        }
+void CDiscAdjDeformationDriver::SetProjection_FD(CGeometry* geometry, CConfig* config,
+                                                 CSurfaceMovement* surface_movement, su2double** Gradient) {
+  unsigned short iDV, nDV, iFFDBox, nDV_Value, iMarker, iDim;
+  unsigned long iVertex, iPoint;
+  su2double delta_eps, my_Gradient, localGradient, *Normal, dS, *VarCoord, Sensitivity, dalpha[3], deps[3], dalpha_deps;
+  bool *UpdatePoint, MoveSurface, Local_MoveSurface;
+  CFreeFormDefBox** FFDBox;
+
+  int rank = SU2_MPI::GetRank();
+
+  nDV = config->GetnDV();
+
+  /*--- Boolean controlling points to be updated. ---*/
+
+  UpdatePoint = new bool[geometry->GetnPoint()];
+
+  /*--- Definition of the FFD deformation class. ---*/
+
+  unsigned short nFFDBox = MAX_NUMBER_FFD;
+  FFDBox = new CFreeFormDefBox*[nFFDBox];
+  for (iFFDBox = 0; iFFDBox < MAX_NUMBER_FFD; iFFDBox++) FFDBox[iFFDBox] = nullptr;
+
+  for (iDV = 0; iDV < nDV; iDV++) {
+    nDV_Value = config->GetnDV_Value(iDV);
+    if (nDV_Value != 1) {
+      SU2_MPI::Error("The projection using finite differences currently only supports a fixed direction of movement for FFD points.", CURRENT_FUNCTION);
     }
-    
-    /*--- Continuous adjoint gradient computation ---*/
-    
-    if (rank == MASTER_NODE)
-        cout << "Evaluate functional gradient using Finite Differences." << endl;
-    
-    for (iDV = 0; iDV < nDV; iDV++) {
-        
-        MoveSurface = true;
-        Local_MoveSurface = true;
-        
-        /*--- Free Form deformation based ---*/
-        
-        if ((config->GetDesign_Variable(iDV) == FFD_CONTROL_POINT_2D) ||
-            (config->GetDesign_Variable(iDV) == FFD_CAMBER_2D) ||
-            (config->GetDesign_Variable(iDV) == FFD_THICKNESS_2D) ||
-            (config->GetDesign_Variable(iDV) == FFD_TWIST_2D) ||
-            (config->GetDesign_Variable(iDV) == FFD_CONTROL_POINT) ||
-            (config->GetDesign_Variable(iDV) == FFD_NACELLE) ||
-            (config->GetDesign_Variable(iDV) == FFD_GULL) ||
-            (config->GetDesign_Variable(iDV) == FFD_TWIST) ||
-            (config->GetDesign_Variable(iDV) == FFD_ROTATION) ||
-            (config->GetDesign_Variable(iDV) == FFD_CAMBER) ||
-            (config->GetDesign_Variable(iDV) == FFD_THICKNESS) ||
-            (config->GetDesign_Variable(iDV) == FFD_ANGLE_OF_ATTACK)) {
-            
-            /*--- Read the FFD information in the first iteration ---*/
-            
-            if (iDV == 0) {
-                
-                if (rank == MASTER_NODE)
-                    cout << "Read the FFD information from mesh file." << endl;
-                
-                /*--- Read the FFD information from the grid file ---*/
-                
-                surface_movement->ReadFFDInfo(geometry, config, FFDBox, config->GetMesh_FileName());
-                
-                /*--- If the FFDBox was not defined in the input file ---*/
-                if (!surface_movement->GetFFDBoxDefinition()) {
-                    SU2_MPI::Error("The input grid doesn't have the entire FFD information!", CURRENT_FUNCTION);
-                }
-                
-                for (iFFDBox = 0; iFFDBox < surface_movement->GetnFFDBox(); iFFDBox++) {
-                    
-                    if (rank == MASTER_NODE) cout << "Checking FFD box dimension." << endl;
-                    surface_movement->CheckFFDDimension(geometry, config, FFDBox[iFFDBox], iFFDBox);
-                    
-                    if (rank == MASTER_NODE) cout << "Check the FFD box intersections with the solid surfaces." << endl;
-                    surface_movement->CheckFFDIntersections(geometry, config, FFDBox[iFFDBox], iFFDBox);
-                    
-                }
-                
-                if (rank == MASTER_NODE)
-                    cout <<"-------------------------------------------------------------------------" << endl;
-                
-            }
-            
-            if (rank == MASTER_NODE) {
-                cout << endl << "Design variable number "<< iDV <<"." << endl;
-                cout << "Performing 3D deformation of the surface." << endl;
-            }
-            
-            /*--- Apply the control point change ---*/
-            
-            MoveSurface = false;
-            
-            for (iFFDBox = 0; iFFDBox < surface_movement->GetnFFDBox(); iFFDBox++) {
-                
-                /*--- Reset FFD box ---*/
-                
-                switch (config->GetDesign_Variable(iDV) ) {
-                    case FFD_CONTROL_POINT_2D : Local_MoveSurface = surface_movement->SetFFDCPChange_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-                    case FFD_CAMBER_2D :        Local_MoveSurface = surface_movement->SetFFDCamber_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-                    case FFD_THICKNESS_2D :     Local_MoveSurface = surface_movement->SetFFDThickness_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-                    case FFD_TWIST_2D :         Local_MoveSurface = surface_movement->SetFFDTwist_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-                    case FFD_CONTROL_POINT :    Local_MoveSurface = surface_movement->SetFFDCPChange(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-                    case FFD_NACELLE :          Local_MoveSurface = surface_movement->SetFFDNacelle(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-                    case FFD_GULL :             Local_MoveSurface = surface_movement->SetFFDGull(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-                    case FFD_TWIST :            Local_MoveSurface = surface_movement->SetFFDTwist(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-                    case FFD_ROTATION :         Local_MoveSurface = surface_movement->SetFFDRotation(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-                    case FFD_CAMBER :           Local_MoveSurface = surface_movement->SetFFDCamber(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-                    case FFD_THICKNESS :        Local_MoveSurface = surface_movement->SetFFDThickness(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-                    case FFD_CONTROL_SURFACE :  Local_MoveSurface = surface_movement->SetFFDControl_Surface(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true); break;
-                    case FFD_ANGLE_OF_ATTACK :  Gradient[iDV][0] = config->GetAoA_Sens(); break;
-                }
-                
-                /*--- Recompute cartesian coordinates using the new control points position ---*/
-                
-                if (Local_MoveSurface) {
-                    MoveSurface = true;
-                    surface_movement->SetCartesianCoord(geometry, config, FFDBox[iFFDBox], iFFDBox, true);
-                }
-                
-            }
-            
-        }
-        
-        /*--- Hicks Henne design variable ---*/
-        
-        else if (config->GetDesign_Variable(iDV) == HICKS_HENNE) {
-            surface_movement->SetHicksHenne(geometry, config, iDV, true);
-        }
-        
-        /*--- Surface bump design variable ---*/
-        
-        else if (config->GetDesign_Variable(iDV) == SURFACE_BUMP) {
-            surface_movement->SetSurface_Bump(geometry, config, iDV, true);
-        }
-        
-        /*--- Kulfan (CST) design variable ---*/
-        
-        else if (config->GetDesign_Variable(iDV) == CST) {
-            surface_movement->SetCST(geometry, config, iDV, true);
+  }
+
+  /*--- Continuous adjoint gradient computation. ---*/
+
+  if (rank == MASTER_NODE) cout << "Evaluate functional gradient using Finite Differences." << endl;
+
+  for (iDV = 0; iDV < nDV; iDV++) {
+    MoveSurface = true;
+    Local_MoveSurface = true;
+
+    /*--- Free form deformation based. ---*/
+
+    if ((config->GetDesign_Variable(iDV) == FFD_CONTROL_POINT_2D) ||
+        (config->GetDesign_Variable(iDV) == FFD_CAMBER_2D) || (config->GetDesign_Variable(iDV) == FFD_THICKNESS_2D) ||
+        (config->GetDesign_Variable(iDV) == FFD_TWIST_2D) || (config->GetDesign_Variable(iDV) == FFD_CONTROL_POINT) ||
+        (config->GetDesign_Variable(iDV) == FFD_NACELLE) || (config->GetDesign_Variable(iDV) == FFD_GULL) ||
+        (config->GetDesign_Variable(iDV) == FFD_TWIST) || (config->GetDesign_Variable(iDV) == FFD_ROTATION) ||
+        (config->GetDesign_Variable(iDV) == FFD_CAMBER) || (config->GetDesign_Variable(iDV) == FFD_THICKNESS) ||
+        (config->GetDesign_Variable(iDV) == FFD_ANGLE_OF_ATTACK)) {
+      /*--- Read the FFD information in the first iteration. ---*/
+
+      if (iDV == 0) {
+        if (rank == MASTER_NODE) cout << "Read the FFD information from mesh file." << endl;
+
+        /*--- Read the FFD information from the grid file. ---*/
+
+        surface_movement->ReadFFDInfo(geometry, config, FFDBox, config->GetMesh_FileName());
+
+        /*--- If the FFDBox was not defined in the input file. ---*/
+
+        if (!surface_movement->GetFFDBoxDefinition()) {
+          SU2_MPI::Error("The input grid doesn't have the entire FFD information!", CURRENT_FUNCTION);
         }
-        
-        /*--- Displacement design variable ---*/
-        
-        else if (config->GetDesign_Variable(iDV) == TRANSLATION) {
-            surface_movement->SetTranslation(geometry, config, iDV, true);
+
+        for (iFFDBox = 0; iFFDBox < surface_movement->GetnFFDBox(); iFFDBox++) {
+          if (rank == MASTER_NODE) cout << "Checking FFD box dimension." << endl;
+          surface_movement->CheckFFDDimension(geometry, config, FFDBox[iFFDBox], iFFDBox);
+
+          if (rank == MASTER_NODE) cout << "Check the FFD box intersections with the solid surfaces." << endl;
+          surface_movement->CheckFFDIntersections(geometry, config, FFDBox[iFFDBox], iFFDBox);
         }
-        
-        /*--- Angle of Attack design variable ---*/
-        
-        else if (config->GetDesign_Variable(iDV) == ANGLE_OF_ATTACK) {
+
+        if (rank == MASTER_NODE)
+          cout << "-------------------------------------------------------------------------" << endl;
+      }
+
+      if (rank == MASTER_NODE) {
+        cout << endl << "Design variable number " << iDV << "." << endl;
+        cout << "Performing 3D deformation of the surface." << endl;
+      }
+
+      /*--- Apply the control point change. ---*/
+
+      MoveSurface = false;
+
+      for (iFFDBox = 0; iFFDBox < surface_movement->GetnFFDBox(); iFFDBox++) {
+        /*--- Reset FFD box. ---*/
+
+        switch (config->GetDesign_Variable(iDV)) {
+          case FFD_CONTROL_POINT_2D:
+            Local_MoveSurface =
+                surface_movement->SetFFDCPChange_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true);
+            break;
+          case FFD_CAMBER_2D:
+            Local_MoveSurface = surface_movement->SetFFDCamber_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true);
+            break;
+          case FFD_THICKNESS_2D:
+            Local_MoveSurface =
+                surface_movement->SetFFDThickness_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true);
+            break;
+          case FFD_TWIST_2D:
+            Local_MoveSurface = surface_movement->SetFFDTwist_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true);
+            break;
+          case FFD_CONTROL_POINT:
+            Local_MoveSurface = surface_movement->SetFFDCPChange(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true);
+            break;
+          case FFD_NACELLE:
+            Local_MoveSurface = surface_movement->SetFFDNacelle(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true);
+            break;
+          case FFD_GULL:
+            Local_MoveSurface = surface_movement->SetFFDGull(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true);
+            break;
+          case FFD_TWIST:
+            Local_MoveSurface = surface_movement->SetFFDTwist(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true);
+            break;
+          case FFD_ROTATION:
+            Local_MoveSurface = surface_movement->SetFFDRotation(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true);
+            break;
+          case FFD_CAMBER:
+            Local_MoveSurface = surface_movement->SetFFDCamber(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true);
+            break;
+          case FFD_THICKNESS:
+            Local_MoveSurface = surface_movement->SetFFDThickness(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true);
+            break;
+          case FFD_CONTROL_SURFACE:
+            Local_MoveSurface =
+                surface_movement->SetFFDControl_Surface(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true);
+            break;
+          case FFD_ANGLE_OF_ATTACK:
             Gradient[iDV][0] = config->GetAoA_Sens();
+            break;
         }
-        
-        /*--- Scale design variable ---*/
-        
-        else if (config->GetDesign_Variable(iDV) == SCALE) {
-            surface_movement->SetScale(geometry, config, iDV, true);
-        }
-        
-        /*--- Rotation design variable ---*/
-        
-        else if (config->GetDesign_Variable(iDV) == ROTATION) {
-            surface_movement->SetRotation(geometry, config, iDV, true);
-        }
-        
-        /*--- NACA_4Digits design variable ---*/
-        
-        else if (config->GetDesign_Variable(iDV) == NACA_4DIGITS) {
-            surface_movement->SetNACA_4Digits(geometry, config);
-        }
-        
-        /*--- Parabolic design variable ---*/
-        
-        else if (config->GetDesign_Variable(iDV) == PARABOLIC) {
-            surface_movement->SetParabolic(geometry, config);
-        }
-        
-        /*--- Design variable not implemented ---*/
-        
-        else {
-            if (rank == MASTER_NODE)
-                cout << "Design Variable not implemented yet" << endl;
-        }
-        
-        /*--- Load the delta change in the design variable (finite difference step). ---*/
-        
-        if ((config->GetDesign_Variable(iDV) != ANGLE_OF_ATTACK) &&
-            (config->GetDesign_Variable(iDV) != FFD_ANGLE_OF_ATTACK)) {
-            
-            /*--- If the Angle of attack is not involved, reset the value of the gradient ---*/
-            
-            my_Gradient = 0.0; Gradient[iDV][0] = 0.0;
-            
-            if (MoveSurface) {
-                
-                delta_eps = config->GetDV_Value(iDV);
-                
-                for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++)
-                    UpdatePoint[iPoint] = true;
-                
-                for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-                    if (config->GetMarker_All_DV(iMarker) == YES) {
-                        for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
-                            
-                            iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
-                            if ((iPoint < geometry->GetnPointDomain()) && UpdatePoint[iPoint]) {
-                                
-                                Normal = geometry->vertex[iMarker][iVertex]->GetNormal();
-                                VarCoord = geometry->vertex[iMarker][iVertex]->GetVarCoord();
-                                Sensitivity = geometry->vertex[iMarker][iVertex]->GetAuxVar();
-                                
-                                dS = 0.0;
-                                for (iDim = 0; iDim < geometry->GetnDim(); iDim++) {
-                                    dS += Normal[iDim]*Normal[iDim];
-                                    deps[iDim] = VarCoord[iDim] / delta_eps;
-                                }
-                                dS = sqrt(dS);
-                                
-                                dalpha_deps = 0.0;
-                                for (iDim = 0; iDim < geometry->GetnDim(); iDim++) {
-                                    dalpha[iDim] = Normal[iDim] / dS;
-                                    dalpha_deps -= dalpha[iDim]*deps[iDim];
-                                }
-                                
-                                my_Gradient += Sensitivity*dalpha_deps;
-                                UpdatePoint[iPoint] = false;
-                            }
-                        }
-                    }
-                }
-            }
-            
-            SU2_MPI::Allreduce(&my_Gradient, &localGradient, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-            Gradient[iDV][0] += localGradient;
+
+        /*--- Recompute cartesian coordinates using the new control points position. ---*/
+
+        if (Local_MoveSurface) {
+          MoveSurface = true;
+          surface_movement->SetCartesianCoord(geometry, config, FFDBox[iFFDBox], iFFDBox, true);
         }
+      }
     }
-    
-    /*--- Delete memory for parameterization. ---*/
-    
-    if (FFDBox != nullptr) {
-        for (iFFDBox = 0; iFFDBox < MAX_NUMBER_FFD; iFFDBox++) {
-            if (FFDBox[iFFDBox] != nullptr) {
-                delete FFDBox[iFFDBox];
-            }
-        }
-        delete [] FFDBox;
+
+    /*--- Hicks-Henne design variable. ---*/
+
+    else if (config->GetDesign_Variable(iDV) == HICKS_HENNE) {
+      surface_movement->SetHicksHenne(geometry, config, iDV, true);
     }
-    
-    delete [] UpdatePoint;
-    
-}
 
+    /*--- Surface bump design variable. ---*/
 
-void CDiscAdjDeformationDriver::SetProjection_AD(CGeometry *geometry, CConfig *config, CSurfaceMovement *surface_movement, su2double** Gradient){
-    
-    su2double *VarCoord = nullptr, Sensitivity, my_Gradient, localGradient, *Normal, Area = 0.0;
-    unsigned short iDV_Value = 0, iMarker, nMarker, iDim, nDim, iDV, nDV;
-    unsigned long iVertex, nVertex, iPoint;
-    
-    const int rank = SU2_MPI::GetRank();
-    
-    nMarker = config->GetnMarker_All();
-    nDim    = geometry->GetnDim();
-    nDV     = config->GetnDV();
-    
-    /*--- Discrete adjoint gradient computation ---*/
-    
-    if (rank == MASTER_NODE)
-        cout  << endl << "Evaluate functional gradient using Algorithmic Differentiation (ZONE " << config->GetiZone() << ")." << endl;
-    
-    /*--- Start recording of operations ---*/
-    
-    AD::StartRecording();
-    
-    /*--- Register design variables as input and set them to zero
-     * (since we want to have the derivative at alpha = 0, i.e. for the current design) ---*/
-    
-    for (iDV = 0; iDV < nDV; iDV++){
-        
-        for (iDV_Value = 0; iDV_Value < config->GetnDV_Value(iDV); iDV_Value++){
-            
-            config->SetDV_Value(iDV, iDV_Value, 0.0);
-            
-            AD::RegisterInput(config->GetDV_Value(iDV, iDV_Value));
-        }
+    else if (config->GetDesign_Variable(iDV) == SURFACE_BUMP) {
+      surface_movement->SetSurface_Bump(geometry, config, iDV, true);
     }
-    
-    /*--- Call the surface deformation routine ---*/
-    
-    surface_movement->SetSurface_Deformation(geometry, config);
-    
-    /*--- Stop the recording --- */
-    
-    AD::StopRecording();
-    
-    /*--- Create a structure to identify points that have been already visited.
-     * We need that to make sure to set the sensitivity of surface points only once
-     *  (Markers share points, so we would visit them more than once in the loop over the markers below) ---*/
-    
-    vector<bool> visited(geometry->GetnPoint(), false);
-    
-    /*--- Initialize the derivatives of the output of the surface deformation routine
-     * with the discrete adjoints from the CFD solution ---*/
-    
-    for (iMarker = 0; iMarker < nMarker; iMarker++) {
-        if (config->GetMarker_All_DV(iMarker) == YES) {
-            nVertex = geometry->nVertex[iMarker];
-            for (iVertex = 0; iVertex <nVertex; iVertex++) {
-                iPoint      = geometry->vertex[iMarker][iVertex]->GetNode();
-                if (!visited[iPoint]){
-                    VarCoord    = geometry->vertex[iMarker][iVertex]->GetVarCoord();
-                    Normal      = geometry->vertex[iMarker][iVertex]->GetNormal();
-                    
-                    Area = 0.0;
-                    for (iDim = 0; iDim < nDim; iDim++){
-                        Area += Normal[iDim]*Normal[iDim];
-                    }
-                    Area = sqrt(Area);
-                    
-                    for (iDim = 0; iDim < nDim; iDim++){
-                        if (config->GetDiscrete_Adjoint()){
-                            Sensitivity = geometry->GetSensitivity(iPoint, iDim);
-                        } else {
-                            Sensitivity = -Normal[iDim]*geometry->vertex[iMarker][iVertex]->GetAuxVar()/Area;
-                        }
-                        SU2_TYPE::SetDerivative(VarCoord[iDim], SU2_TYPE::GetValue(Sensitivity));
-                    }
-                    visited[iPoint] = true;
+
+    /*--- Kulfan (CST) design variable. ---*/
+
+    else if (config->GetDesign_Variable(iDV) == CST) {
+      surface_movement->SetCST(geometry, config, iDV, true);
+    }
+
+    /*--- Displacement design variable. ---*/
+
+    else if (config->GetDesign_Variable(iDV) == TRANSLATION) {
+      surface_movement->SetTranslation(geometry, config, iDV, true);
+    }
+
+    /*--- Angle of Attack design variable. ---*/
+
+    else if (config->GetDesign_Variable(iDV) == ANGLE_OF_ATTACK) {
+      Gradient[iDV][0] = config->GetAoA_Sens();
+    }
+
+    /*--- Scale design variable. ---*/
+
+    else if (config->GetDesign_Variable(iDV) == SCALE) {
+      surface_movement->SetScale(geometry, config, iDV, true);
+    }
+
+    /*--- Rotation design variable. ---*/
+
+    else if (config->GetDesign_Variable(iDV) == ROTATION) {
+      surface_movement->SetRotation(geometry, config, iDV, true);
+    }
+
+    /*--- NACA_4Digits design variable. ---*/
+
+    else if (config->GetDesign_Variable(iDV) == NACA_4DIGITS) {
+      surface_movement->SetNACA_4Digits(geometry, config);
+    }
+
+    /*--- Parabolic design variable. ---*/
+
+    else if (config->GetDesign_Variable(iDV) == PARABOLIC) {
+      surface_movement->SetParabolic(geometry, config);
+    }
+
+    /*--- Design variable not implemented. ---*/
+
+    else {
+      if (rank == MASTER_NODE) cout << "Design Variable not implemented yet" << endl;
+    }
+
+    /*--- Load the delta change in the design variable (finite difference step). ---*/
+
+    if ((config->GetDesign_Variable(iDV) != ANGLE_OF_ATTACK) &&
+        (config->GetDesign_Variable(iDV) != FFD_ANGLE_OF_ATTACK)) {
+      /*--- If the Angle of attack is not involved, reset the value of the gradient. ---*/
+
+      my_Gradient = 0.0;
+      Gradient[iDV][0] = 0.0;
+
+      if (MoveSurface) {
+        delta_eps = config->GetDV_Value(iDV);
+
+        for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++) UpdatePoint[iPoint] = true;
+
+        for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
+          if (config->GetMarker_All_DV(iMarker) == YES) {
+            for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
+              iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+              if ((iPoint < geometry->GetnPointDomain()) && UpdatePoint[iPoint]) {
+                Normal = geometry->vertex[iMarker][iVertex]->GetNormal();
+                VarCoord = geometry->vertex[iMarker][iVertex]->GetVarCoord();
+                Sensitivity = geometry->vertex[iMarker][iVertex]->GetAuxVar();
+
+                dS = 0.0;
+                for (iDim = 0; iDim < geometry->GetnDim(); iDim++) {
+                  dS += Normal[iDim] * Normal[iDim];
+                  deps[iDim] = VarCoord[iDim] / delta_eps;
+                }
+                dS = sqrt(dS);
+
+                dalpha_deps = 0.0;
+                for (iDim = 0; iDim < geometry->GetnDim(); iDim++) {
+                  dalpha[iDim] = Normal[iDim] / dS;
+                  dalpha_deps -= dalpha[iDim] * deps[iDim];
                 }
+
+                my_Gradient += Sensitivity * dalpha_deps;
+                UpdatePoint[iPoint] = false;
+              }
             }
+          }
         }
+      }
+
+      SU2_MPI::Allreduce(&my_Gradient, &localGradient, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
+      Gradient[iDV][0] += localGradient;
     }
-    
-    /*--- Compute derivatives and extract gradient ---*/
-    
-    AD::ComputeAdjoint();
-    
-    for (iDV = 0; iDV  < nDV; iDV++){
-        
-        for (iDV_Value = 0; iDV_Value < config->GetnDV_Value(iDV); iDV_Value++) {
-            
-            my_Gradient = SU2_TYPE::GetDerivative(config->GetDV_Value(iDV, iDV_Value));
-            
-            SU2_MPI::Allreduce(&my_Gradient, &localGradient, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-            
-            /*--- Angle of Attack design variable (this is different,
-             the value comes form the input file) ---*/
-            
-            if ((config->GetDesign_Variable(iDV) == ANGLE_OF_ATTACK) ||
-                (config->GetDesign_Variable(iDV) == FFD_ANGLE_OF_ATTACK))  {
-                Gradient[iDV][iDV_Value] = config->GetAoA_Sens();
-            }
-            
-            Gradient[iDV][iDV_Value] += localGradient;
-        }
+  }
+
+  /*--- Delete memory for parameterization. ---*/
+
+  if (FFDBox != nullptr) {
+    for (iFFDBox = 0; iFFDBox < MAX_NUMBER_FFD; iFFDBox++) {
+      if (FFDBox[iFFDBox] != nullptr) {
+        delete FFDBox[iFFDBox];
+      }
     }
-    
-    AD::Reset();
-    
+    delete[] FFDBox;
+  }
+
+  delete[] UpdatePoint;
 }
 
-void CDiscAdjDeformationDriver::OutputGradient(su2double** Gradient, CConfig* config, ofstream& Gradient_file){
-    
-    unsigned short nDV, iDV, iDV_Value, nDV_Value;
-    
-    int rank = SU2_MPI::GetRank();
-    
-    nDV = config->GetnDV();
-    
-    /*--- Loop through all design variables and their gradients ---*/
-    
-    for (iDV = 0; iDV  < nDV; iDV++){
-        nDV_Value = config->GetnDV_Value(iDV);
-        if (rank == MASTER_NODE){
-            
-            /*--- Print the kind of design variable on screen ---*/
-            
-            cout << endl << "Design variable (";
-            for (std::map<string, ENUM_PARAM>::const_iterator it = Param_Map.begin(); it != Param_Map.end(); ++it ){
-                if (it->second == config->GetDesign_Variable(iDV)){
-                    cout << it->first << ") number "<< iDV << "." << endl;
-                }
-            }
-            
-            /*--- Print the kind of objective function to screen ---*/
-            
-            for (std::map<string, ENUM_OBJECTIVE>::const_iterator it = Objective_Map.begin(); it != Objective_Map.end(); ++it ){
-                if (it->second == config->GetKind_ObjFunc()){
-                    cout << it->first << " gradient : ";
-                    if (iDV == 0) Gradient_file << it->first << " gradient " << endl;
-                }
-            }
-            
-            /*--- Print the gradient to file and screen ---*/
-            
-            for (iDV_Value = 0; iDV_Value < nDV_Value; iDV_Value++){
-                cout << Gradient[iDV][iDV_Value];
-                if (iDV_Value != nDV_Value-1 ){
-                    cout << ", ";
-                }
-                Gradient_file << Gradient[iDV][iDV_Value] << endl;
+void CDiscAdjDeformationDriver::SetProjection_AD(CGeometry* geometry, CConfig* config,
+                                                 CSurfaceMovement* surface_movement, su2double** Gradient) {
+  su2double *VarCoord = nullptr, Sensitivity, my_Gradient, localGradient, *Normal, Area = 0.0;
+  unsigned short iDV_Value = 0, iMarker, nMarker, iDim, nDim, iDV, nDV;
+  unsigned long iVertex, nVertex, iPoint;
+
+  const int rank = SU2_MPI::GetRank();
+
+  nMarker = config->GetnMarker_All();
+  nDim = geometry->GetnDim();
+  nDV = config->GetnDV();
+
+  /*--- Discrete adjoint gradient computation. ---*/
+
+  if (rank == MASTER_NODE)
+    cout << endl
+         << "Evaluate functional gradient using Algorithmic Differentiation (ZONE " << config->GetiZone() << ")."
+         << endl;
+
+  /*--- Start recording of operations. ---*/
+
+  AD::StartRecording();
+
+  /*--- Register design variables as input and set them to zero
+   * (since we want to have the derivative at alpha = 0, i.e. for the current design). ---*/
+
+  for (iDV = 0; iDV < nDV; iDV++) {
+    for (iDV_Value = 0; iDV_Value < config->GetnDV_Value(iDV); iDV_Value++) {
+      config->SetDV_Value(iDV, iDV_Value, 0.0);
+
+      AD::RegisterInput(config->GetDV_Value(iDV, iDV_Value));
+    }
+  }
+
+  /*--- Call the surface deformation routine. ---*/
+
+  surface_movement->SetSurface_Deformation(geometry, config);
+
+  /*--- Stop the recording. --- */
+
+  AD::StopRecording();
+
+  /*--- Create a structure to identify points that have been already visited.
+   * We need that to make sure to set the sensitivity of surface points only once.
+   * Markers share points, so we would visit them more than once in the loop over the markers below). ---*/
+
+  vector<bool> visited(geometry->GetnPoint(), false);
+
+  /*--- Initialize the derivatives of the output of the surface deformation routine
+   * with the discrete adjoints from the CFD solution. ---*/
+
+  for (iMarker = 0; iMarker < nMarker; iMarker++) {
+    if (config->GetMarker_All_DV(iMarker) == YES) {
+      nVertex = geometry->nVertex[iMarker];
+      for (iVertex = 0; iVertex < nVertex; iVertex++) {
+        iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+        if (!visited[iPoint]) {
+          VarCoord = geometry->vertex[iMarker][iVertex]->GetVarCoord();
+          Normal = geometry->vertex[iMarker][iVertex]->GetNormal();
+
+          Area = 0.0;
+          for (iDim = 0; iDim < nDim; iDim++) {
+            Area += Normal[iDim] * Normal[iDim];
+          }
+          Area = sqrt(Area);
+
+          for (iDim = 0; iDim < nDim; iDim++) {
+            if (config->GetDiscrete_Adjoint()) {
+              Sensitivity = geometry->GetSensitivity(iPoint, iDim);
+            } else {
+              Sensitivity = -Normal[iDim] * geometry->vertex[iMarker][iVertex]->GetAuxVar() / Area;
             }
-            cout << endl;
-            cout <<"-------------------------------------------------------------------------" << endl;
+            SU2_TYPE::SetDerivative(VarCoord[iDim], SU2_TYPE::GetValue(Sensitivity));
+          }
+          visited[iPoint] = true;
         }
+      }
     }
+  }
+
+  /*--- Compute derivatives and extract gradient. ---*/
+
+  AD::ComputeAdjoint();
+
+  for (iDV = 0; iDV < nDV; iDV++) {
+    for (iDV_Value = 0; iDV_Value < config->GetnDV_Value(iDV); iDV_Value++) {
+      my_Gradient = SU2_TYPE::GetDerivative(config->GetDV_Value(iDV, iDV_Value));
+
+      SU2_MPI::Allreduce(&my_Gradient, &localGradient, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
+
+      /*--- Angle of Attack design variable (this is different, the value comes form the input file). ---*/
+
+      if ((config->GetDesign_Variable(iDV) == ANGLE_OF_ATTACK) ||
+          (config->GetDesign_Variable(iDV) == FFD_ANGLE_OF_ATTACK)) {
+        Gradient[iDV][iDV_Value] = config->GetAoA_Sens();
+      }
+
+      Gradient[iDV][iDV_Value] += localGradient;
+    }
+  }
+
+  AD::Reset();
 }
 
+void CDiscAdjDeformationDriver::OutputGradient(su2double** Gradient, CConfig* config, ofstream& Gradient_file) {
 
-void CDiscAdjDeformationDriver::SetSensitivity_Files(CGeometry ****geometry, CConfig **config, unsigned short val_nZone) {
-    
-    unsigned short iMarker,iDim, nDim, nMarker, nVar;
-    unsigned long iVertex, iPoint, nPoint, nVertex;
-    su2double *Normal, Prod, Sens = 0.0, SensDim, Area;
-    
-    unsigned short iZone;
-    
-    CSolver *solver  = nullptr;
-    COutput *output  = nullptr;
-    
-    for (iZone = 0; iZone < val_nZone; iZone++) {
-        
-        nPoint = geometry[iZone][INST_0][MESH_0]->GetnPoint();
-        nDim   = geometry[iZone][INST_0][MESH_0]->GetnDim();
-        nMarker = config[iZone]->GetnMarker_All();
-        nVar = nDim + 1;
-        
-        /*--- We create a baseline solver to easily merge the sensitivity information ---*/
-        
-        vector<string> fieldnames;
-        fieldnames.push_back("\"Point\"");
-        fieldnames.push_back("\"x\"");
-        fieldnames.push_back("\"y\"");
-        if (nDim == 3) {
-            fieldnames.push_back("\"z\"");
-        }
-        fieldnames.push_back("\"Sensitivity_x\"");
-        fieldnames.push_back("\"Sensitivity_y\"");
-        if (nDim == 3) {
-            fieldnames.push_back("\"Sensitivity_z\"");
-        }
-        fieldnames.push_back("\"Surface_Sensitivity\"");
-        
-        solver = new CBaselineSolver(geometry[iZone][INST_0][MESH_0], config[iZone], nVar+nDim, fieldnames);
-        
-        for (iPoint = 0; iPoint < nPoint; iPoint++) {
-            for (iDim = 0; iDim < nDim; iDim++) {
-                solver->GetNodes()->SetSolution(iPoint, iDim,      geometry[iZone][INST_0][MESH_0]->nodes->GetCoord(iPoint, iDim));
-                solver->GetNodes()->SetSolution(iPoint, iDim+nDim, geometry[iZone][INST_0][MESH_0]->GetSensitivity(iPoint, iDim));
-            }
+  unsigned short nDV, iDV, iDV_Value, nDV_Value;
+
+  int rank = SU2_MPI::GetRank();
+
+  nDV = config->GetnDV();
+
+  /*--- Loop through all design variables and their gradients. ---*/
+
+  for (iDV = 0; iDV < nDV; iDV++) {
+    nDV_Value = config->GetnDV_Value(iDV);
+    if (rank == MASTER_NODE) {
+      /*--- Print the kind of design variable on screen. ---*/
+
+      cout << endl << "Design variable (";
+      for (std::map<string, ENUM_PARAM>::const_iterator it = Param_Map.begin(); it != Param_Map.end(); ++it) {
+        if (it->second == config->GetDesign_Variable(iDV)) {
+          cout << it->first << ") number " << iDV << "." << endl;
         }
-        
-        /*--- Compute the sensitivity in normal direction ---*/
-        
-        for (iMarker = 0; iMarker < nMarker; iMarker++) {
-            
-            if(config[iZone]->GetSolid_Wall(iMarker) || (config[iZone]->GetMarker_All_DV(iMarker) == YES )) {
-                
-                nVertex = geometry[iZone][INST_0][MESH_0]->GetnVertex(iMarker);
-                
-                for (iVertex = 0; iVertex < nVertex; iVertex++) {
-                    iPoint = geometry[iZone][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-                    Normal = geometry[iZone][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNormal();
-                    Prod = 0.0;
-                    Area = 0.0;
-                    for (iDim = 0; iDim < nDim; iDim++) {
-                        
-                        /*--- Retrieve the gradient calculated with discrete adjoint method ---*/
-                        
-                        SensDim = geometry[iZone][INST_0][MESH_0]->GetSensitivity(iPoint, iDim);
-                        
-                        /*--- Calculate scalar product for projection onto the normal vector ---*/
-                        
-                        Prod += Normal[iDim]*SensDim;
-                        
-                        Area += Normal[iDim]*Normal[iDim];
-                    }
-                    
-                    Area = sqrt(Area);
-                    
-                    /*--- Projection of the gradient onto the normal vector of the surface ---*/
-                    
-                    Sens = Prod/Area;
-                    
-                    solver->GetNodes()->SetSolution(iPoint, 2*nDim, Sens);
-                    
-                }
-            }
+      }
+
+      /*--- Print the kind of objective function to screen. ---*/
+
+      for (std::map<string, ENUM_OBJECTIVE>::const_iterator it = Objective_Map.begin(); it != Objective_Map.end(); ++it) {
+        if (it->second == config->GetKind_ObjFunc()) {
+          cout << it->first << " gradient : ";
+          if (iDV == 0) Gradient_file << it->first << " gradient " << endl;
         }
-        
-        output = new CBaselineOutput(config[iZone], nDim, solver);
-        output->PreprocessVolumeOutput(config[iZone]);
-        output->PreprocessHistoryOutput(config[iZone], false);
-        
-        /*--- Load the data --- */
-        
-        output->Load_Data(geometry[iZone][INST_0][MESH_0], config[iZone], &solver);
-        
-        /*--- Set the surface filename ---*/
-        
-        output->SetSurface_Filename(config[iZone]->GetSurfSens_FileName());
-        
-        /*--- Set the volume filename ---*/
-        
-        output->SetVolume_Filename(config[iZone]->GetVolSens_FileName());
-        
-        /*--- Write to file ---*/
-        
-        for (unsigned short iFile = 0; iFile < config[iZone]->GetnVolumeOutputFiles(); iFile++){
-            auto FileFormat = config[iZone]->GetVolumeOutputFiles();
-            if (FileFormat[iFile] != OUTPUT_TYPE::RESTART_ASCII &&
-                FileFormat[iFile] != OUTPUT_TYPE::RESTART_BINARY &&
-                FileFormat[iFile] != OUTPUT_TYPE::CSV)
-                output->WriteToFile(config[iZone], geometry[iZone][INST_0][MESH_0], FileFormat[iFile]);
+      }
+
+      /*--- Print the gradient to file and screen. ---*/
+
+      for (iDV_Value = 0; iDV_Value < nDV_Value; iDV_Value++) {
+        cout << Gradient[iDV][iDV_Value];
+        if (iDV_Value != nDV_Value - 1) {
+          cout << ", ";
         }
-        
-        /*--- Free memory ---*/
-        
-        delete output;
-        delete solver;
-        
+        Gradient_file << Gradient[iDV][iDV_Value] << endl;
+      }
+      cout << endl;
+      cout << "-------------------------------------------------------------------------" << endl;
     }
-    
+  }
 }
 
-void CDiscAdjDeformationDriver::DerivativeTreatment_MeshSensitivity(CGeometry *geometry, CConfig *config, CVolumetricMovement *grid_movement) {
-    
-    int rank = SU2_MPI::GetRank();
-    
-    /*--- Warning if choosen smoothing mode is unsupported.
-     * This is the default option if the user has not specified a mode in the config file. ---*/
-    if (config->GetSobMode() == ENUM_SOBOLEV_MODUS::NONE) {
-        SU2_MPI::Error("Unsupported operation modus for the Sobolev Smoothing Solver.", CURRENT_FUNCTION);
+void CDiscAdjDeformationDriver::SetSensitivity_Files(CGeometry**** geometry, CConfig** config,
+                                                     unsigned short val_nZone) {
+  unsigned short iMarker, iDim, nDim, nMarker, nVar;
+  unsigned long iVertex, iPoint, nPoint, nVertex;
+  su2double *Normal, Prod, Sens = 0.0, SensDim, Area;
+
+  unsigned short iZone;
+
+  CSolver* solver = nullptr;
+  COutput* output = nullptr;
+
+  for (iZone = 0; iZone < val_nZone; iZone++) {
+    nPoint = geometry[iZone][INST_0][MESH_0]->GetnPoint();
+    nDim = geometry[iZone][INST_0][MESH_0]->GetnDim();
+    nMarker = config[iZone]->GetnMarker_All();
+    nVar = nDim + 1;
+
+    /*--- We create a baseline solver to easily merge the sensitivity information. ---*/
+
+    vector<string> fieldnames;
+    fieldnames.push_back("\"Point\"");
+    fieldnames.push_back("\"x\"");
+    fieldnames.push_back("\"y\"");
+    if (nDim == 3) {
+      fieldnames.push_back("\"z\"");
     }
-    
-    /*-- Construct the smoothing solver and numerics ---*/
-    std::unique_ptr<CSolver> solver(new CGradientSmoothingSolver(geometry, config));
-    unsigned dim = (config->GetSmoothOnSurface() ? geometry->GetnDim() - 1 : geometry->GetnDim());
-    std::unique_ptr<CNumerics> numerics(new CGradSmoothing(dim, config));
-    
-    if (rank == MASTER_NODE)  cout << "Sobolev Smoothing of derivatives is active." << endl;
-    
-    /*--- Apply the smoothing procedure on the mesh level. ---*/
-    if (config->GetSobMode() == ENUM_SOBOLEV_MODUS::MESH_LEVEL) {
-        if (rank == MASTER_NODE) cout << "  working on mesh level" << endl;
-        
-        /*--- Work with the surface derivatives. ---*/
-        if (config->GetSmoothOnSurface()) {
-            
-            /*--- Project to surface and then smooth on surface. ---*/
-            grid_movement->SetVolume_Deformation(geometry, config, false, true);
-            
-            /*--- Get the sensitivities from the geometry class to work with. ---*/
-            solver->ReadSensFromGeometry(geometry);
-            
-            /*--- Perform the smoothing procedure on all boundaries marked as DV marker. ---*/
-            solver->ApplyGradientSmoothingSurface(geometry, numerics.get(), config);
-            
-            /*--- After appling the solver write the results back ---*/
-            solver->WriteSensToGeometry(geometry);
-            
-        /*--- Work with the volume derivatives. ---*/
-        } else {
-            
-            /*--- Get the sensitivities from the geometry class to work with. ---*/
-            solver->ReadSensFromGeometry(geometry);
-            
-            solver->ApplyGradientSmoothingVolume(geometry, numerics.get(), config);
-            
-            /*--- After appling the solver write the results back ---*/
-            solver->WriteSensToGeometry(geometry);
-            
-            /*--- Projection is applied after smoothing. ---*/
-            grid_movement->SetVolume_Deformation(geometry, config, false, true);
+    fieldnames.push_back("\"Sensitivity_x\"");
+    fieldnames.push_back("\"Sensitivity_y\"");
+    if (nDim == 3) {
+      fieldnames.push_back("\"Sensitivity_z\"");
+    }
+    fieldnames.push_back("\"Surface_Sensitivity\"");
+
+    solver = new CBaselineSolver(geometry[iZone][INST_0][MESH_0], config[iZone], nVar + nDim, fieldnames);
+
+    for (iPoint = 0; iPoint < nPoint; iPoint++) {
+      for (iDim = 0; iDim < nDim; iDim++) {
+        solver->GetNodes()->SetSolution(iPoint, iDim, geometry[iZone][INST_0][MESH_0]->nodes->GetCoord(iPoint, iDim));
+        solver->GetNodes()->SetSolution(iPoint, iDim + nDim, geometry[iZone][INST_0][MESH_0]->GetSensitivity(iPoint, iDim));
+      }
+    }
+
+    /*--- Compute the sensitivity in normal direction. ---*/
+
+    for (iMarker = 0; iMarker < nMarker; iMarker++) {
+      if (config[iZone]->GetSolid_Wall(iMarker) || (config[iZone]->GetMarker_All_DV(iMarker) == YES)) {
+        nVertex = geometry[iZone][INST_0][MESH_0]->GetnVertex(iMarker);
+
+        for (iVertex = 0; iVertex < nVertex; iVertex++) {
+          iPoint = geometry[iZone][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+          Normal = geometry[iZone][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNormal();
+          Prod = 0.0;
+          Area = 0.0;
+          for (iDim = 0; iDim < nDim; iDim++) {
+            /*--- Retrieve the gradient calculated with discrete adjoint method. ---*/
+
+            SensDim = geometry[iZone][INST_0][MESH_0]->GetSensitivity(iPoint, iDim);
+
+            /*--- Calculate scalar product for projection onto the normal vector. ---*/
+
+            Prod += Normal[iDim] * SensDim;
+
+            Area += Normal[iDim] * Normal[iDim];
+          }
+
+          Area = sqrt(Area);
+
+          /*--- Projection of the gradient onto the normal vector of the surface. ---*/
+
+          Sens = Prod / Area;
+
+          solver->GetNodes()->SetSolution(iPoint, 2 * nDim, Sens);
         }
-        
+      }
     }
-    
-}
 
-void CDiscAdjDeformationDriver::DerivativeTreatment_Gradient(CGeometry *geometry, CConfig *config, CVolumetricMovement* grid_movement, CSurfaceMovement *surface_movement, su2double** Gradient) {
-    
-    int rank = SU2_MPI::GetRank();
-    
-    /*--- Error if choosen smoothing mode is unsupported.
-     * This is the default option if the user has not specified a mode in the config file. ---*/
-    if (config->GetSobMode() == ENUM_SOBOLEV_MODUS::NONE) {
-        SU2_MPI::Error("Unsupported operation modus for the Sobolev Smoothing Solver.", CURRENT_FUNCTION);
+    output = new CBaselineOutput(config[iZone], nDim, solver);
+    output->PreprocessVolumeOutput(config[iZone]);
+    output->PreprocessHistoryOutput(config[iZone], false);
+
+    /*--- Load the data. --- */
+
+    output->Load_Data(geometry[iZone][INST_0][MESH_0], config[iZone], &solver);
+
+    /*--- Set the surface filename. ---*/
+
+    output->SetSurface_Filename(config[iZone]->GetSurfSens_FileName());
+
+    /*--- Set the volume filename. ---*/
+
+    output->SetVolume_Filename(config[iZone]->GetVolSens_FileName());
+
+    /*--- Write to file. ---*/
+
+    for (unsigned short iFile = 0; iFile < config[iZone]->GetnVolumeOutputFiles(); iFile++) {
+      auto FileFormat = config[iZone]->GetVolumeOutputFiles();
+      if (FileFormat[iFile] != OUTPUT_TYPE::RESTART_ASCII && FileFormat[iFile] != OUTPUT_TYPE::RESTART_BINARY &&
+          FileFormat[iFile] != OUTPUT_TYPE::CSV)
+        output->WriteToFile(config[iZone], geometry[iZone][INST_0][MESH_0], FileFormat[iFile]);
     }
-    
-    /*-- Construct the smoothing solver and numerics ---*/
-    std::unique_ptr<CSolver> solver(new CGradientSmoothingSolver(geometry, config));
-    unsigned dim = (config->GetSmoothOnSurface() ? geometry->GetnDim() - 1 : geometry->GetnDim());
-    std::unique_ptr<CNumerics> numerics(new CGradSmoothing(dim, config));
-    
-    if (rank == MASTER_NODE)  cout << "Sobolev Smoothing of derivatives is active." << endl;
-    
-    /*--- Get the sensitivities from the geometry class to work with. ---*/
-    solver->ReadSensFromGeometry(geometry);
-    
-    /*--- Apply the smoothing procedure on the DV level. ---*/
-    if (config->GetSobMode() == ENUM_SOBOLEV_MODUS::PARAM_LEVEL_COMPLETE) {
-        solver->ApplyGradientSmoothingDV(geometry, numerics.get(), surface_movement, grid_movement, config, Gradient);
-        
-    /*--- If smoothing already took place on the mesh level, or none is requested, just do standard projection. ---*/
-    } else if (config->GetSobMode() == ENUM_SOBOLEV_MODUS::ONLY_GRAD ||
-               config->GetSobMode() == ENUM_SOBOLEV_MODUS::MESH_LEVEL) {
-        solver->RecordTapeAndCalculateOriginalGradient(geometry, surface_movement, grid_movement, config, Gradient);
+
+    /*--- Free memory. ---*/
+
+    delete output;
+    delete solver;
+  }
+}
+
+void CDiscAdjDeformationDriver::DerivativeTreatment_MeshSensitivity(CGeometry* geometry, CConfig* config,
+                                                                    CVolumetricMovement* grid_movement) {
+  int rank = SU2_MPI::GetRank();
+
+  /*--- Warning if chosen smoothing mode is unsupported.
+   * This is the default option if the user has not specified a mode in the config file. ---*/
+
+  if (config->GetSobMode() == ENUM_SOBOLEV_MODUS::NONE) {
+    SU2_MPI::Error("Unsupported operation modus for the Sobolev Smoothing Solver.", CURRENT_FUNCTION);
+  }
+
+  /*-- Construct the smoothing solver and numerics. ---*/
+
+  std::unique_ptr<CSolver> solver(new CGradientSmoothingSolver(geometry, config));
+  unsigned dim = (config->GetSmoothOnSurface() ? geometry->GetnDim() - 1 : geometry->GetnDim());
+  std::unique_ptr<CNumerics> numerics(new CGradSmoothing(dim, config));
+
+  if (rank == MASTER_NODE) cout << "Sobolev Smoothing of derivatives is active." << endl;
+
+  /*--- Apply the smoothing procedure on the mesh level. ---*/
+
+  if (config->GetSobMode() == ENUM_SOBOLEV_MODUS::MESH_LEVEL) {
+    if (rank == MASTER_NODE) cout << "  working on mesh level" << endl;
+
+    /*--- Work with the surface derivatives. ---*/
+    if (config->GetSmoothOnSurface()) {
+      /*--- Project to surface and then smooth on surface. ---*/
+
+      grid_movement->SetVolume_Deformation(geometry, config, false, true);
+
+      /*--- Get the sensitivities from the geometry class to work with. ---*/
+
+      solver->ReadSensFromGeometry(geometry);
+
+      /*--- Perform the smoothing procedure on all boundaries marked as DV marker. ---*/
+
+      solver->ApplyGradientSmoothingSurface(geometry, numerics.get(), config);
+
+      /*--- After applying the solver write the results back. ---*/
+
+      solver->WriteSensToGeometry(geometry);
+
+    /*--- Work with the volume derivatives. ---*/
+    } else {
+      /*--- Get the sensitivities from the geometry class to work with. ---*/
+
+      solver->ReadSensFromGeometry(geometry);
+
+      solver->ApplyGradientSmoothingVolume(geometry, numerics.get(), config);
+
+      /*--- After applying the solver write the results back. ---*/
+
+      solver->WriteSensToGeometry(geometry);
+
+      /*--- Projection is applied after smoothing. ---*/
+
+      grid_movement->SetVolume_Deformation(geometry, config, false, true);
     }
-    
+  }
+}
+
+void CDiscAdjDeformationDriver::DerivativeTreatment_Gradient(CGeometry* geometry, CConfig* config,
+                                                             CVolumetricMovement* grid_movement,
+                                                             CSurfaceMovement* surface_movement, su2double** Gradient) {
+  int rank = SU2_MPI::GetRank();
+
+  /*--- Error if chosen smoothing mode is unsupported.
+   * This is the default option if the user has not specified a mode in the config file. ---*/
+
+  if (config->GetSobMode() == ENUM_SOBOLEV_MODUS::NONE) {
+    SU2_MPI::Error("Unsupported operation modus for the Sobolev Smoothing Solver.", CURRENT_FUNCTION);
+  }
+
+  /*-- Construct the smoothing solver and numerics. ---*/
+
+  std::unique_ptr<CSolver> solver(new CGradientSmoothingSolver(geometry, config));
+  unsigned dim = (config->GetSmoothOnSurface() ? geometry->GetnDim() - 1 : geometry->GetnDim());
+  std::unique_ptr<CNumerics> numerics(new CGradSmoothing(dim, config));
+
+  if (rank == MASTER_NODE) cout << "Sobolev Smoothing of derivatives is active." << endl;
+
+  /*--- Get the sensitivities from the geometry class to work with. ---*/
+
+  solver->ReadSensFromGeometry(geometry);
+
+  /*--- Apply the smoothing procedure on the DV level. ---*/
+  if (config->GetSobMode() == ENUM_SOBOLEV_MODUS::PARAM_LEVEL_COMPLETE) {
+    solver->ApplyGradientSmoothingDV(geometry, numerics.get(), surface_movement, grid_movement, config, Gradient);
+
+  /*--- If smoothing already took place on the mesh level, or none is requested, just do standard projection. ---*/
+  } else if (config->GetSobMode() == ENUM_SOBOLEV_MODUS::ONLY_GRAD ||
+             config->GetSobMode() == ENUM_SOBOLEV_MODUS::MESH_LEVEL) {
+    solver->RecordTapeAndCalculateOriginalGradient(geometry, surface_movement, grid_movement, config, Gradient);
+  }
 }

From 30ea6c4de6e9a4faf22f37bd3c9f7ed2e7f2a6d5 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Thu, 8 Dec 2022 20:31:42 -0800
Subject: [PATCH 063/656] Update CDriverBase

---
 Common/include/drivers/CDriverBase.hpp | 1097 +++++++++--------
 Common/src/drivers/CDriverBase.cpp     | 1537 ++++++++++++++++--------
 2 files changed, 1645 insertions(+), 989 deletions(-)

diff --git a/Common/include/drivers/CDriverBase.hpp b/Common/include/drivers/CDriverBase.hpp
index 1fa0d011ca2..b5804091ce3 100644
--- a/Common/include/drivers/CDriverBase.hpp
+++ b/Common/include/drivers/CDriverBase.hpp
@@ -27,499 +27,614 @@
 
 #pragma once
 
-#include "../CConfig.hpp"
 #include "../../../SU2_CFD/include/numerics/CNumerics.hpp"
-#include "../../../SU2_CFD/include/solvers/CSolver.hpp"
 #include "../../../SU2_CFD/include/output/COutput.hpp"
+#include "../../../SU2_CFD/include/solvers/CSolver.hpp"
+#include "../CConfig.hpp"
 
 class CDriverBase {
-    
-protected:
-    
-    int rank,                                       /*!< \brief MPI Rank. */
-    size;                                           /*!< \brief MPI Size. */
-    char* config_file_name;                         /*!< \brief Configuration file name of the problem.*/
-    
-    su2double StartTime,                            /*!< \brief Start point of the timer for performance benchmarking.*/
-    StopTime,                                       /*!< \brief Stop point of the timer for performance benchmarking.*/
-    UsedTimePreproc,                                /*!< \brief Elapsed time between Start and Stop point of the timer for tracking preprocessing phase.*/
-    UsedTimeCompute,                                /*!< \brief Elapsed time between Start and Stop point of the timer for tracking compute phase.*/
-    UsedTime;                                       /*!< \brief Elapsed time between Start and Stop point of the timer.*/
-    
-    unsigned long TimeIter;
-    
-    unsigned short iMesh,                           /*!< \brief Iterator on mesh levels.*/
-    iZone,                                          /*!< \brief Iterator on zones.*/
-    nZone,                                          /*!< \brief Total number of zones in the problem. */
-    nDim,                                           /*!< \brief Number of dimensions.*/
-    iInst,                                          /*!< \brief Iterator on instance levels.*/
-    *nInst,                                         /*!< \brief Total number of instances in the problem (per zone). */
-    **interface_types;                              /*!< \brief Type of coupling between the distinct (physical) zones.*/
-    
-    CConfig *driver_config;                         /*!< \brief Definition of the driver configuration. */
-    COutput *driver_output;                         /*!< \brief Definition of the driver output. */
-
-    CConfig **config_container;                     /*!< \brief Definition of the particular problem. */
-    COutput **output_container;                     /*!< \brief Pointer to the COutput class. */
-    CGeometry ****geometry_container;               /*!< \brief Geometrical definition of the problem. */
-    CSolver *****solver_container;                  /*!< \brief Container vector with all the solutions. */
-    CNumerics ******numerics_container;             /*!< \brief Description of the numerical method (the way in which the equations are solved). */
-    CSurfaceMovement **surface_movement;            /*!< \brief Surface movement classes of the problem. */
-    CVolumetricMovement ***grid_movement;           /*!< \brief Volume grid movement classes of the problem. */
-    CFreeFormDefBox*** FFDBox;                      /*!< \brief FFD FFDBoxes of the problem. */
-    
-    CConfig *main_config;                           /*!< \brief Reference to the base (i.e. ZONE 0) configuration (used in the driver API). */
-    CGeometry *main_geometry;                       /*!< \brief Reference to the base (i.E. ZONE, INST, MESH 0) geometry (used in the driver API). */
-    
-public:
-    
-    /*!
-     * \brief Constructor of the class.
-     * \param[in] confFile - Configuration file name.
-     * \param[in] val_nZone - Total number of zones.
-     * \param[in] MPICommunicator - MPI communicator for SU2.
-     */
-    CDriverBase(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator);
-    
-    /*!
-     * \brief Destructor of the class.
-     */
-    virtual ~CDriverBase(void);
-    
-    /*!
-     * \brief A virtual member.
-     */
-    virtual void Preprocessing() {};
-    
-    /*!
-     * \brief A virtual member.
-     */
-    virtual void Run() {};
-    
-    /*!
-     * \brief A virtual member.
-     */
-    virtual void Update() {};
-    
-    /*!
-     * \brief A virtual member.
-     */
-    virtual void Update_Legacy() {};
-    
-    /*!
-     * \brief A virtual member.
-     */
-    virtual void Output() {};
-    
-    /*!
-     * \brief A virtual member.
-     */
-    virtual void Postprocessing() {};
-    /*!
-     * \brief Get the number of markers in the mesh.
-     * \return Number of markers.
-     */
-    unsigned short GetNumberMarkers() const;
-    
-    /*!
-     * \brief Get all the boundary markers tags with their associated indices.
-     * \return List of boundary markers tags with their indices.
-     */
-    map<string, unsigned short> GetMarkerIndices() const;
-    
-    /*!
-     * \brief Get all the boundary markers tags with their associated types.
-     * \return List of boundary markers tags with their types.
-     */
-    map<string, string> GetMarkerTypes() const;
-    
-    /*!
-     * \brief Get all the boundary marker tags.
-     * \return List of boundary markers tags.
-     */
-    vector<string> GetMarkerTags() const;
-
-    /*!
-     * \brief Get all the deformable boundary marker tags.
-     * \return List of deformable boundary markers tags.
-     */
-    vector<string> GetDeformableMarkerTags() const;
-    
-    /*!
-     * \brief Get the number of dimensions of the mesh.
-     * \return Number of dimensions.
-     */
-    unsigned long GetNumberDimensions() const;
-    
-    /*!
-     * \brief Get the number of elements in the mesh.
-     * \return Number of elements.
-     */
-    unsigned long GetNumberElements() const;
-    
-    /*!
-     * \brief Get the number of elements in the marker.
-     * \param[in] iMarker - Marker index.
-     * \return Number of elements.
-     */
-    unsigned long GetNumberMarkerElements(unsigned short iMarker) const;
-    
-    /*!
-     * \brief Get the global IDs of the mesh elements.
-     * \return Global element IDs.
-     */
-    vector<unsigned long> GetElementIDs() const;
-    
-    /*!
-     * \brief Get the global ID of a mesh element.
-     * \param[in] iElem - Mesh element index.
-     * \return Global element ID.
-     */
-    unsigned long GetElementIDs(unsigned long iElem) const;
-    
-    /*!
-     * \brief Get the global IDs of the marker elements.
-     * \param[in] iMarker - Marker index.
-     * \return Global element IDs.
-     */
-    vector<unsigned long> GetMarkerElementIDs(unsigned short iMarker) const;
-    
-    /*!
-     * \brief Get the global IDs of a marker element.
-     * \param[in] iMarker - Marker index.
-     * \param[in] iBound - Marker element index.
-     * \return Global element ID.
-     */
-    unsigned long GetMarkerElementIDs(unsigned short iMarker, unsigned long iBound) const;
-    
-    /*!
-     * \brief Get the table of vertex IDs belonging to the mesh elements.
-     * \return Element connectivities (nElem, nNode)
-     */
-    vector<vector<unsigned long>> GetElementConnectivities() const;
-    
-    /*!
-     * \brief Get the row of vertex IDs belonging to a mesh element.
-     * \param[in] iElem - Mesh element index.
-     * \return Element connectivity (nNode)
-     */
-    vector<unsigned long> GetElementConnectivities(unsigned long iElem) const;
-    
-    /*!
-     * \brief Get the table of vertex IDs belonging to the marker elements.
-     * \param[in] iMarker - Marker index.
-     * \return Element connectivities (nBound, nNode).
-     */
-    vector<vector<unsigned long>> GetMarkerElementConnectivities(unsigned short iMarker) const;
-    
-    /*!
-     * \brief Get the row of vertex IDs belonging to a marker element.
-     * \param[in] iMarker - Marker index.
-     * \param[in] iBound - Marker element index.
-     * \return Element connectivity (nNode).
-     */
-    vector<unsigned long> GetMarkerElementConnectivities(unsigned short iMarker, unsigned long iBound) const;
-    
-    /*!
-     * \brief Get the number of vertices in the mesh.
-     * \return Number of vertices.
-     */
-    unsigned long GetNumberVertices() const;
-    
-    /*!
-     * \brief Get the number of vertices in the marker.
-     * \param[in] iMarker - Marker index.
-     * \return Number of vertices.
-     */
-    unsigned long GetNumberMarkerVertices(unsigned short iMarker) const;
-    
-    /*!
-     * \brief Get the number of halo vertices in the mesh.
-     * \return Number of vertices.
-     */
-    unsigned long GetNumberHaloVertices() const;
-    
-    /*!
-     * \brief Get the number of halo vertices in the marker.
-     * \param[in] iMarker - Marker index.
-     * \return Number of vertices.
-     */
-    unsigned long GetNumberMarkerHaloVertices(unsigned short iMarker) const;
-    
-    /*!
-     * \brief Get the mesh vertex indices of the marker vertices.
-     * \param[in] iMarker - Marker index.
-     * \return Mesh vertex indices.
-     */
-    vector<unsigned long> GetMarkerVertexIndices(unsigned short iMarker) const;
-    
-    /*!
-     * \brief Get the mesh vertex index of a marker vertex.
-     * \param[in] iMarker - Marker index.
-     * \param[in] iVertex - Marker vertex index.
-     * \return Mesh vertex index.
-     */
-    unsigned long GetMarkerVertexIndices(unsigned short iMarker, unsigned long iVertex) const;
-    
-    /*!
-     * \brief Get the global IDs of the mesh vertices.
-     * \return Global vertex IDs.
-     */
-    vector<unsigned long> GetVertexIDs() const;
-
-    /*!
-     * \brief Get the global ID of a mesh vertex.
-     * \param[in] iPoint - Mesh vertex index.
-     * \return Global vertex ID.
-     */
-    unsigned long GetVertexIDs(unsigned long iPoint) const;
-    
-    /*!
-     * \brief Get the global IDs of the marker vertices.
-     * \param[in] iMarker - Marker index.
-     * \return Global vertex IDs.
-     */
-    vector<unsigned long> GetMarkerVertexIDs(unsigned short iMarker) const;
-    
-    /*!
-     * \brief Get the global ID of a marker vertex.
-     * \param[in] iMarker - Marker index.
-     * \param[in] iVertex - Marker vertex index.
-     * \return Global vertex ID.
-     */
-    unsigned long GetMarkerVertexIDs(unsigned short iMarker, unsigned long iVertex) const;
-    
-    /*!
-     * \brief Get the halo flags of the mesh vertices.
-     * \return Vertex domain flags.
-     */
-    vector<bool> GetDomain() const;
-    
-    /*!
-     * \brief Get the halo flag of a mesh vertex.
-     * \param[in] iPoint - Mesh vertex index.
-     * \return Vertex domain flag.
-     */
-    bool GetDomain(unsigned long iPoint) const;
-    
-    /*!
-     * \brief Get the halo flags of the marker vertices.
-     * \param[in] iMarker - Marker index.
-     * \return Vertex domain flags.
-     */
-    vector<bool> GetMarkerDomain(unsigned short iMarker) const;
-    
-    /*!
-     * \brief Get the halo flag of a marker vertex.
-     * \param[in] iMarker - Marker index.
-     * \param[in] iVertex - Marker vertex index.
-     * \return Vertex domain flag.
-     */
-    bool GetMarkerDomain(unsigned short iMarker, unsigned long iVertex) const;
-    
-    /*!
-     * \brief Get the initial (un-deformed) coordinates of the mesh vertices.
-     * \return Initial vertex coordinates (nPoint, nDim).
-     */
-    vector<vector<passivedouble>> GetInitialCoordinates() const;
-
-    /*!
-     * \brief Get the initial (un-deformed) coordinates of a mesh vertex.
-     * \param[in] iPoint - Mesh vertex index.
-     * \return Initial vertex coordinates (nDim).
-     */
-    vector<passivedouble> GetInitialCoordinates(unsigned long iPoint) const;
-    
-    /*!
-     * \brief Get the initial (un-deformed) coordinates of the marker vertices.
-     * \param[in] iMarker - Marker index.
-     * \return Initial vertex coordinates (nVertex, nDim).
-     */
-    vector<vector<passivedouble>> GetMarkerInitialCoordinates(unsigned short iMarker) const;
-    
-    /*!
-     * \brief Get the initial (un-deformed) coordinates of a marker vertex.
-     * \param[in] iMarker - Marker index.
-     * \param[in] iVertex - Marker vertex index.
-     * \return Initial vertex coordinates (nDim).
-     */
-    vector<passivedouble> GetMarkerInitialCoordinates(unsigned short iMarker, unsigned long iVertex) const;
-    
-    /*!
-     * \brief Get the coordinates of the mesh vertices.
-     * \return Vertex coordinates (nPoint, nDim).
-     */
-    vector<vector<passivedouble>> GetCoordinates() const;
-
-    /*!
-     * \brief Get the coordinates of a mesh vertex.
-     * \param[in] iPoint - Mesh vertex index.
-     * \return Vertex coordinates (nDim).
-     */
-    vector<passivedouble> GetCoordinates(unsigned long iPoint) const;
-    
-    /*!
-     * \brief Get the coordinates of the marker vertices.
-     * \param[in] iMarker - Marker index.
-     * \return Vertex coordinates (nVertex, nDim).
-     */
-    vector<vector<passivedouble>> GetMarkerCoordinates(unsigned short iMarker) const;
-    
-    /*!
-     * \brief Get the coordinates of a marker vertex.
-     * \param[in] iMarker - Marker index.
-     * \param[in] iVertex - Marker vertex index.
-     * \return Vertex coordinates (nDim).
-     */
-    vector<passivedouble> GetMarkerCoordinates(unsigned short iMarker, unsigned long iVertex) const;
-    
-    /*!
-     * \brief Set the coordinates of the mesh vertices.
-     * \param[in] values - Vertex coordinates (nPoint, nDim).
-     */
-    void SetCoordinates(vector<vector<passivedouble>> values);
-    
-    /*!
-     * \brief Set the coordinates of a mesh vertex.
-     * \param[in] iPoint - Mesh vertex index.
-     * \param[in] values - Vertex coordinates (nDim).
-     */
-    void SetCoordinates(unsigned long iPoint, vector<passivedouble> values);
-    
-    /*!
-     * \brief Set the coordinates of the marker vertices.
-     * \param[in] iMarker - Marker index.
-     * \param[in] values - Vertex coordinates (nVertex, nDim).
-     */
-    void SetMarkerCoordinates(unsigned short iMarker, vector<vector<passivedouble>> values);
-    
-    /*!
-     * \brief Set the coordinates of a marker vertex.
-     * \param[in] iMarker - Marker index.
-     * \param[in] iVertex - Marker vertex index.
-     * \param[in] values - Vertex coordinates (nDim).
-     */
-    void SetMarkerCoordinates(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values);
-    
-    /*!
-     * \brief Get the displacements of the marker vertices.
-     * \param[in] iMarker - Marker index.
-     * \return Vertex displacements (nVertex, nDim).
-     */
-    vector<vector<passivedouble>> GetMarkerDisplacements(unsigned short iMarker) const;
-    
-    /*!
-     * \brief Get the displacements of a marker vertex.
-     * \param[in] iMarker - Marker index.
-     * \param[in] iVertex - Marker vertex index.
-     * \return Vertex displacements (nDim).
-     */
-    vector<passivedouble> GetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex) const;
-    
-    /*!
-     * \brief Set the displacements of the marker vertices.
-     * \param[in] iMarker - Marker index.
-     * \param[in] values - Vertex displacements (nVertex, nDim).
-     */
-    void SetMarkerDisplacements(unsigned short iMarker, vector<vector<passivedouble>> values);
-    
-    /*!
-     * \brief Set the displacements of a marker vertex.
-     * \param[in] iMarker - Marker index.
-     * \param[in] iVertex - Marker vertex index.
-     * \param[in] values - Vertex displacements (nDim).
-     */
-    void SetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values);
-    
-    /*!
-     * \brief Get the velocities of the marker vertices.
-     * \param[in] iMarker - Marker index.
-     * \return Vertex velocities (nVertex, nDim).
-     */
-    vector<vector<passivedouble>> GetMarkerVelocities(unsigned short iMarker) const;
-
-    /*!
-     * \brief Get the velocities of a marker vertex.
-     * \param[in] iMarker - Marker index.
-     * \param[in] iVertex - Marker vertex index.
-     * \return Vertex velocities (nDim).
-     */
-    vector<passivedouble> GetMarkerVelocities(unsigned short iMarker, unsigned long iVertex) const;
-    
-    /*!
-     * \brief Set the velocities of the marker vertices.
-     * \param[in] iMarker - Marker index.
-     * \param[in] values - Vertex velocities (nVertex, nDim).
-     */
-    void SetMarkerVelocities(unsigned short iMarker, vector<vector<passivedouble>> values);
-    
-    /*!
-     * \brief Set the velocities of a marker vertex.
-     * \param[in] iMarker - Marker index.
-     * \param[in] iVertex - Marker vertex index.
-     * \param[in] values - Vertex velocities (nDim).
-     */
-    void SetMarkerVelocities(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values);
-    
-    /*!
-     * \brief Get the normal vectors at the marker vertices.
-     * \param[in] iMarker - Marker index.
-     * \param[in] normalize - If true, the unit (i.e. normalized) normal vector is returned.
-     * \return Normal vector at the vertex (nVertex, nDim).
-     */
-    vector<vector<passivedouble>> GetMarkerVertexNormals(unsigned short iMarker, bool normalize = false) const;
-    
-    /*!
-     * \brief Get the normal vectors at a marker vertex.
-     * \param[in] iMarker - Marker index.
-     * \param[in] iVertex - Marker vertex index.
-     * \param[in] normalize - If true, the unit (i.e. normalized) normal vector is returned.
-     * \return Normal vector at the vertex (nDim).
-     */
-    vector<passivedouble> GetMarkerVertexNormals(unsigned short iMarker, unsigned long iVertex, bool normalize = false) const;
-    
-    /*!
-     * \brief Communicate the boundary mesh displacements in a python call
-     */
-    void CommunicateMeshDisplacements(void);
-    
-protected:
-    
-    /*!
-     * \brief Initialize Containers
-     */
-    void SetContainers_Null();
-    
-    /*!
-     * \brief Read in the config and mesh files.
-     */
-    void Input_Preprocessing(CConfig **&config, CConfig *&driver_config);
-    
-    /*!
-     * \brief Construction of the edge-based data structure and the multigrid structure.
-     */
-    void Geometrical_Preprocessing(CConfig *config, CGeometry **&geometry, bool dummy);
-    
-    /*!
-     * \brief Definition and allocation of all solution classes.
-     * \param[in] solver_container - Container vector with all the solutions.
-     * \param[in] geometry - Geometrical definition of the problem.
-     * \param[in] config - Definition of the particular problem.
-     */
-    void Solver_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***&solver);
-    
-    /*!
-     * \brief Definition and allocation of all solver classes.
-     * \param[in] numerics_container - Description of the numerical method (the way in which the equations are solved).
-     * \param[in] geometry - Geometrical definition of the problem.
-     * \param[in] solver_container - Container vector with all the solutions.
-     * \param[in] config - Definition of the particular problem.
-     */
-    void Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***solver, CNumerics ****&numerics) const;
-    
-    /*!
-     * \brief Preprocess the output container.
-     */
-    void Output_Preprocessing(CConfig **config, CConfig *driver_config, COutput **&output_container, COutput *&driver_output);
-    
+ protected:
+  int rank,               /*!< \brief MPI Rank. */
+      size;               /*!< \brief MPI Size. */
+  char* config_file_name; /*!< \brief Configuration file name of the problem. */
+
+  su2double StartTime, /*!< \brief Start point of the timer for performance benchmarking. */
+      StopTime,        /*!< \brief Stop point of the timer for performance benchmarking. */
+      UsedTimePreproc, /*!< \brief Elapsed time between Start and Stop point of the timer for tracking preprocessing
+                                    phase. */
+      UsedTimeCompute, /*!< \brief Elapsed time between Start and Stop point of the timer for tracking compute phase. */
+      UsedTime;        /*!< \brief Elapsed time between Start and Stop point of the timer. */
+
+  unsigned long TimeIter;
+
+  unsigned short iMesh,  /*!< \brief Iterator on mesh levels. */
+      iZone,             /*!< \brief Iterator on zones. */
+      nZone,             /*!< \brief Total number of zones in the problem. */
+      nDim,              /*!< \brief Number of dimensions. */
+      iInst,             /*!< \brief Iterator on instance levels. */
+      *nInst,            /*!< \brief Total number of instances in the problem (per zone). */
+      **interface_types; /*!< \brief Type of coupling between the distinct (physical) zones. */
+
+  CConfig* driver_config; /*!< \brief Definition of the driver configuration. */
+  COutput* driver_output; /*!< \brief Definition of the driver output. */
+
+  CConfig** config_container;           /*!< \brief Definition of the particular problem. */
+  COutput** output_container;           /*!< \brief Pointer to the COutput class. */
+  CGeometry**** geometry_container;     /*!< \brief Geometrical definition of the problem. */
+  CSolver***** solver_container;        /*!< \brief Container vector with all the solutions. */
+  CNumerics****** numerics_container;   /*!< \brief Description of the numerical method (the way in which the equations
+                                           are solved). */
+  CSurfaceMovement** surface_movement;  /*!< \brief Surface movement classes of the problem. */
+  CVolumetricMovement*** grid_movement; /*!< \brief Volume grid movement classes of the problem. */
+  CFreeFormDefBox*** FFDBox;            /*!< \brief FFD FFDBoxes of the problem. */
+
+  CConfig* main_config;     /*!< \brief Reference to base (i.e. ZONE 0) configuration (used in driver API). */
+  CGeometry* main_geometry; /*!< \brief Reference to base (i.e. ZONE, INST, MESH 0) geometry (used in driver API). */
+
+ public:
+  /*!
+   * \brief Constructor of the class.
+   * \param[in] confFile - Configuration file name.
+   * \param[in] val_nZone - Total number of zones.
+   * \param[in] MPICommunicator - MPI communicator for SU2.
+   */
+  CDriverBase(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator);
+
+  /*!
+   * \brief Destructor of the class.
+   */
+  virtual ~CDriverBase(void);
+
+  /*!
+   * \brief A virtual member.
+   */
+  virtual void Preprocessing(){};
+
+  /*!
+   * \brief A virtual member.
+   */
+  virtual void Run(){};
+
+  /*!
+   * \brief A virtual member.
+   */
+  virtual void Update(){};
+
+  /*!
+   * \brief A virtual member.
+   */
+  virtual void Update_Legacy(){};
+
+  /*!
+   * \brief A virtual member.
+   */
+  virtual void Output(){};
+
+  /*!
+   * \brief A virtual member.
+   */
+  virtual void Postprocessing(){};
+
+  /*!
+   * \brief Get the number of design variables.
+   * \return Number of design variables.
+   */
+  unsigned short GetNumberDesignVariables() const;
+
+  /*!
+   * \brief Get the number of FFD boxes.
+   * \return Number of FFD boxes.
+   */
+  unsigned short GetNumberFFDBoxes() const;
+
+  /*!
+   * \brief Get the number of FFD box corner points.
+   * \param[in] iFFDBox - FFD box index.
+   * \return Number of FFD box corner points.
+   */
+  unsigned short GetNumberFFDBoxCornerPoints(unsigned short iFFDBox) const;
+
+  /*!
+   * \brief Get the number of FFD box control points.
+   * \param[in] iFFDBox - FFD box index.
+   * \return Number of FFD box control points.
+   */
+  unsigned short GetNumberFFDBoxControlPoints(unsigned short iFFDBox) const;
+
+  /*!
+   * \brief Get the number of FFD box surface points.
+   * \param[in] iFFDBox - FFD box index.
+   * \return Number of FFD box surface points.
+   */
+  unsigned long GetNumberFFDBoxSurfacePoints(unsigned short iFFDBox) const;
+
+  /*!
+   * \brief Get the FFD box marker IDs.
+   * \param[in] iFFDBox - FFD box index.
+   * \return FFD box marker IDs.
+   */
+  vector<unsigned short> GetFFDBoxMarkerIDs(unsigned short iFFDBox) const;
+
+  /*!
+   * \brief Get the FFD box vertex IDs.
+   * \param[in] iFFDBox - FFD box index.
+   * \return FFD box vertex IDs.
+   */
+  vector<unsigned long> GetFFDBoxVertexIDs(unsigned short iFFDBox) const;
+
+  /*!
+   * \brief Get the FFD box grid point IDs.
+   * \param[in] iFFDBox - FFD box index.
+   * \return FFD box grid point IDs.
+   */
+  vector<unsigned long> GetFFDBoxPointIDs(unsigned short iFFDBox) const;
+
+  /*!
+   * \brief Get the FFD box corner coordinates.
+   * \param[in] iFFDBox - FFD box index.
+   * \return FFD box corner coordinates.
+   */
+  vector<vector<passivedouble>> GetFFDBoxCornerCoordinates(unsigned short iFFDBox) const;
+
+  /*!
+   * \brief Get the FFD box control point coordinates.
+   * \param[in] iFFDBox - FFD box index.
+   * \return FFD box control point coordinates.
+   */
+  vector<vector<passivedouble>> GetFFDBoxControlPointCoordinates(unsigned short iFFDBox) const;
+
+  /*!
+   * \brief Get the FFD box control point coordinates.
+   * \param[in] iFFDBox - FFD box index.
+   * \param[in] iOrder - Local i-index of the control point.
+   * \param[in] jOrder - Local j-index of the control point.
+   * \param[in] kOrder - Local k-index of the control point.
+   * \return FFD box control point coordinates.
+   */
+  vector<passivedouble> GetFFDBoxControlPointCoordinates(unsigned short iFFDBox, unsigned int iOrder,
+                                                         unsigned int jOrder, unsigned int kOrder) const;
+
+  /*!
+   * \brief Get the FFD box surface coordinates.
+   * \param[in] iFFDBox - FFD box index.
+   * \param[in] parametric - Boolean to indicate if parametric coordinates should be returned.
+   * \return FFD box surface coordinates.
+   */
+  vector<vector<passivedouble>> GetFFDBoxSurfaceCoordinates(unsigned short iFFDBox, bool parametric = false) const;
+
+  /*!
+   * \brief Get the FFD box surface coordinates.
+   * \param[in] iFFDBox - FFD box index.
+   * \param[in] iPoint - FFD surface point index.
+   * \param[in] parametric - Boolean to indicate if parametric coordinates should be returned.
+   * \return FFD box surface coordinates.
+   */
+  vector<passivedouble> GetFFDBoxSurfaceCoordinates(unsigned short iFFDBox, unsigned long iPoint,
+                                                    bool parametric = false) const;
+
+  /*!
+   * \brief Get the number of markers in the mesh.
+   * \return Number of markers.
+   */
+  unsigned short GetNumberMarkers() const;
+
+  /*!
+   * \brief Get all the boundary markers tags with their associated indices.
+   * \return List of boundary markers tags with their indices.
+   */
+  map<string, unsigned short> GetMarkerIndices() const;
+
+  /*!
+   * \brief Get all the boundary markers tags with their associated types.
+   * \return List of boundary markers tags with their types.
+   */
+  map<string, string> GetMarkerTypes() const;
+
+  /*!
+   * \brief Get all the boundary marker tags.
+   * \return List of boundary markers tags.
+   */
+  vector<string> GetMarkerTags() const;
+
+  /*!
+   * \brief Get all the deformable boundary marker tags.
+   * \return List of deformable boundary markers tags.
+   */
+  vector<string> GetDeformableMarkerTags() const;
+
+  /*!
+   * \brief Get the number of dimensions of the mesh.
+   * \return Number of dimensions.
+   */
+  unsigned long GetNumberDimensions() const;
+
+  /*!
+   * \brief Get the number of elements in the mesh.
+   * \return Number of elements.
+   */
+  unsigned long GetNumberElements() const;
+
+  /*!
+   * \brief Get the number of elements in the marker.
+   * \param[in] iMarker - Marker index.
+   * \return Number of elements.
+   */
+  unsigned long GetNumberMarkerElements(unsigned short iMarker) const;
+
+  /*!
+   * \brief Get the global IDs of the mesh elements.
+   * \return Global element IDs.
+   */
+  vector<unsigned long> GetElementIDs() const;
+
+  /*!
+   * \brief Get the global ID of a mesh element.
+   * \param[in] iElem - Mesh element index.
+   * \return Global element ID.
+   */
+  unsigned long GetElementIDs(unsigned long iElem) const;
+
+  /*!
+   * \brief Get the global IDs of the marker elements.
+   * \param[in] iMarker - Marker index.
+   * \return Global element IDs.
+   */
+  vector<unsigned long> GetMarkerElementIDs(unsigned short iMarker) const;
+
+  /*!
+   * \brief Get the global IDs of a marker element.
+   * \param[in] iMarker - Marker index.
+   * \param[in] iBound - Marker element index.
+   * \return Global element ID.
+   */
+  unsigned long GetMarkerElementIDs(unsigned short iMarker, unsigned long iBound) const;
+
+  /*!
+   * \brief Get the table of vertex IDs belonging to the mesh elements.
+   * \return Element connectivities (nElem, nNode)
+   */
+  vector<vector<unsigned long>> GetElementConnectivities() const;
+
+  /*!
+   * \brief Get the row of vertex IDs belonging to a mesh element.
+   * \param[in] iElem - Mesh element index.
+   * \return Element connectivity (nNode)
+   */
+  vector<unsigned long> GetElementConnectivities(unsigned long iElem) const;
+
+  /*!
+   * \brief Get the table of vertex IDs belonging to the marker elements.
+   * \param[in] iMarker - Marker index.
+   * \return Element connectivities (nBound, nNode).
+   */
+  vector<vector<unsigned long>> GetMarkerElementConnectivities(unsigned short iMarker) const;
+
+  /*!
+   * \brief Get the row of vertex IDs belonging to a marker element.
+   * \param[in] iMarker - Marker index.
+   * \param[in] iBound - Marker element index.
+   * \return Element connectivity (nNode).
+   */
+  vector<unsigned long> GetMarkerElementConnectivities(unsigned short iMarker, unsigned long iBound) const;
+
+  /*!
+   * \brief Get the number of vertices in the mesh.
+   * \return Number of vertices.
+   */
+  unsigned long GetNumberVertices() const;
+
+  /*!
+   * \brief Get the number of vertices in the marker.
+   * \param[in] iMarker - Marker index.
+   * \return Number of vertices.
+   */
+  unsigned long GetNumberMarkerVertices(unsigned short iMarker) const;
+
+  /*!
+   * \brief Get the number of halo vertices in the mesh.
+   * \return Number of vertices.
+   */
+  unsigned long GetNumberHaloVertices() const;
+
+  /*!
+   * \brief Get the number of halo vertices in the marker.
+   * \param[in] iMarker - Marker index.
+   * \return Number of vertices.
+   */
+  unsigned long GetNumberMarkerHaloVertices(unsigned short iMarker) const;
+
+  /*!
+   * \brief Get the mesh vertex indices of the marker vertices.
+   * \param[in] iMarker - Marker index.
+   * \return Mesh vertex indices.
+   */
+  vector<unsigned long> GetMarkerVertexIndices(unsigned short iMarker) const;
+
+  /*!
+   * \brief Get the mesh vertex index of a marker vertex.
+   * \param[in] iMarker - Marker index.
+   * \param[in] iVertex - Marker vertex index.
+   * \return Mesh vertex index.
+   */
+  unsigned long GetMarkerVertexIndices(unsigned short iMarker, unsigned long iVertex) const;
+
+  /*!
+   * \brief Get the global IDs of the mesh vertices.
+   * \return Global vertex IDs.
+   */
+  vector<unsigned long> GetVertexIDs() const;
+
+  /*!
+   * \brief Get the global ID of a mesh vertex.
+   * \param[in] iPoint - Mesh vertex index.
+   * \return Global vertex ID.
+   */
+  unsigned long GetVertexIDs(unsigned long iPoint) const;
+
+  /*!
+   * \brief Get the global IDs of the marker vertices.
+   * \param[in] iMarker - Marker index.
+   * \return Global vertex IDs.
+   */
+  vector<unsigned long> GetMarkerVertexIDs(unsigned short iMarker) const;
+
+  /*!
+   * \brief Get the global ID of a marker vertex.
+   * \param[in] iMarker - Marker index.
+   * \param[in] iVertex - Marker vertex index.
+   * \return Global vertex ID.
+   */
+  unsigned long GetMarkerVertexIDs(unsigned short iMarker, unsigned long iVertex) const;
+
+  /*!
+   * \brief Get the halo flags of the mesh vertices.
+   * \return Vertex domain flags.
+   */
+  vector<bool> GetDomain() const;
+
+  /*!
+   * \brief Get the halo flag of a mesh vertex.
+   * \param[in] iPoint - Mesh vertex index.
+   * \return Vertex domain flag.
+   */
+  bool GetDomain(unsigned long iPoint) const;
+
+  /*!
+   * \brief Get the halo flags of the marker vertices.
+   * \param[in] iMarker - Marker index.
+   * \return Vertex domain flags.
+   */
+  vector<bool> GetMarkerDomain(unsigned short iMarker) const;
+
+  /*!
+   * \brief Get the halo flag of a marker vertex.
+   * \param[in] iMarker - Marker index.
+   * \param[in] iVertex - Marker vertex index.
+   * \return Vertex domain flag.
+   */
+  bool GetMarkerDomain(unsigned short iMarker, unsigned long iVertex) const;
+
+  /*!
+   * \brief Get the initial (un-deformed) coordinates of the mesh vertices.
+   * \return Initial vertex coordinates (nPoint, nDim).
+   */
+  vector<vector<passivedouble>> GetInitialCoordinates() const;
+
+  /*!
+   * \brief Get the initial (un-deformed) coordinates of a mesh vertex.
+   * \param[in] iPoint - Mesh vertex index.
+   * \return Initial vertex coordinates (nDim).
+   */
+  vector<passivedouble> GetInitialCoordinates(unsigned long iPoint) const;
+
+  /*!
+   * \brief Get the initial (un-deformed) coordinates of the marker vertices.
+   * \param[in] iMarker - Marker index.
+   * \return Initial vertex coordinates (nVertex, nDim).
+   */
+  vector<vector<passivedouble>> GetMarkerInitialCoordinates(unsigned short iMarker) const;
+
+  /*!
+   * \brief Get the initial (un-deformed) coordinates of a marker vertex.
+   * \param[in] iMarker - Marker index.
+   * \param[in] iVertex - Marker vertex index.
+   * \return Initial vertex coordinates (nDim).
+   */
+  vector<passivedouble> GetMarkerInitialCoordinates(unsigned short iMarker, unsigned long iVertex) const;
+
+  /*!
+   * \brief Get the coordinates of the mesh vertices.
+   * \return Vertex coordinates (nPoint, nDim).
+   */
+  vector<vector<passivedouble>> GetCoordinates() const;
+
+  /*!
+   * \brief Get the coordinates of a mesh vertex.
+   * \param[in] iPoint - Mesh vertex index.
+   * \return Vertex coordinates (nDim).
+   */
+  vector<passivedouble> GetCoordinates(unsigned long iPoint) const;
+
+  /*!
+   * \brief Get the coordinates of the marker vertices.
+   * \param[in] iMarker - Marker index.
+   * \return Vertex coordinates (nVertex, nDim).
+   */
+  vector<vector<passivedouble>> GetMarkerCoordinates(unsigned short iMarker) const;
+
+  /*!
+   * \brief Get the coordinates of a marker vertex.
+   * \param[in] iMarker - Marker index.
+   * \param[in] iVertex - Marker vertex index.
+   * \return Vertex coordinates (nDim).
+   */
+  vector<passivedouble> GetMarkerCoordinates(unsigned short iMarker, unsigned long iVertex) const;
+
+  /*!
+   * \brief Set the coordinates of the mesh vertices.
+   * \param[in] values - Vertex coordinates (nPoint, nDim).
+   */
+  void SetCoordinates(vector<vector<passivedouble>> values);
+
+  /*!
+   * \brief Set the coordinates of a mesh vertex.
+   * \param[in] iPoint - Mesh vertex index.
+   * \param[in] values - Vertex coordinates (nDim).
+   */
+  void SetCoordinates(unsigned long iPoint, vector<passivedouble> values);
+
+  /*!
+   * \brief Set the coordinates of the marker vertices.
+   * \param[in] iMarker - Marker index.
+   * \param[in] values - Vertex coordinates (nVertex, nDim).
+   */
+  void SetMarkerCoordinates(unsigned short iMarker, vector<vector<passivedouble>> values);
+
+  /*!
+   * \brief Set the coordinates of a marker vertex.
+   * \param[in] iMarker - Marker index.
+   * \param[in] iVertex - Marker vertex index.
+   * \param[in] values - Vertex coordinates (nDim).
+   */
+  void SetMarkerCoordinates(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values);
+
+  /*!
+   * \brief Get the displacements of the marker vertices.
+   * \param[in] iMarker - Marker index.
+   * \return Vertex displacements (nVertex, nDim).
+   */
+  vector<vector<passivedouble>> GetMarkerDisplacements(unsigned short iMarker) const;
+
+  /*!
+   * \brief Get the displacements of a marker vertex.
+   * \param[in] iMarker - Marker index.
+   * \param[in] iVertex - Marker vertex index.
+   * \return Vertex displacements (nDim).
+   */
+  vector<passivedouble> GetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex) const;
+
+  /*!
+   * \brief Set the displacements of the marker vertices.
+   * \param[in] iMarker - Marker index.
+   * \param[in] values - Vertex displacements (nVertex, nDim).
+   */
+  void SetMarkerDisplacements(unsigned short iMarker, vector<vector<passivedouble>> values);
+
+  /*!
+   * \brief Set the displacements of a marker vertex.
+   * \param[in] iMarker - Marker index.
+   * \param[in] iVertex - Marker vertex index.
+   * \param[in] values - Vertex displacements (nDim).
+   */
+  void SetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values);
+
+  /*!
+   * \brief Get the velocities of the marker vertices.
+   * \param[in] iMarker - Marker index.
+   * \return Vertex velocities (nVertex, nDim).
+   */
+  vector<vector<passivedouble>> GetMarkerVelocities(unsigned short iMarker) const;
+
+  /*!
+   * \brief Get the velocities of a marker vertex.
+   * \param[in] iMarker - Marker index.
+   * \param[in] iVertex - Marker vertex index.
+   * \return Vertex velocities (nDim).
+   */
+  vector<passivedouble> GetMarkerVelocities(unsigned short iMarker, unsigned long iVertex) const;
+
+  /*!
+   * \brief Set the velocities of the marker vertices.
+   * \param[in] iMarker - Marker index.
+   * \param[in] values - Vertex velocities (nVertex, nDim).
+   */
+  void SetMarkerVelocities(unsigned short iMarker, vector<vector<passivedouble>> values);
+
+  /*!
+   * \brief Set the velocities of a marker vertex.
+   * \param[in] iMarker - Marker index.
+   * \param[in] iVertex - Marker vertex index.
+   * \param[in] values - Vertex velocities (nDim).
+   */
+  void SetMarkerVelocities(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values);
+
+  /*!
+   * \brief Get the normal vectors at the marker vertices.
+   * \param[in] iMarker - Marker index.
+   * \param[in] normalize - If true, the unit (i.e. normalized) normal vector is returned.
+   * \return Normal vector at the vertex (nVertex, nDim).
+   */
+  vector<vector<passivedouble>> GetMarkerVertexNormals(unsigned short iMarker, bool normalize = false) const;
+
+  /*!
+   * \brief Get the normal vectors at a marker vertex.
+   * \param[in] iMarker - Marker index.
+   * \param[in] iVertex - Marker vertex index.
+   * \param[in] normalize - If true, the unit (i.e. normalized) normal vector is returned.
+   * \return Normal vector at the vertex (nDim).
+   */
+  vector<passivedouble> GetMarkerVertexNormals(unsigned short iMarker, unsigned long iVertex,
+                                               bool normalize = false) const;
+
+  /*!
+   * \brief Communicate the boundary mesh displacements.
+   */
+  void CommunicateMeshDisplacements(void);
+
+ protected:
+  /*!
+   * \brief Initialize Containers
+   */
+  void SetContainers_Null();
+
+  /*!
+   * \brief Read in the config and mesh files.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] driver_config - Definition of the driver configuration.
+   */
+  void Input_Preprocessing(CConfig**& config, CConfig*& driver_config);
+
+  /*!
+   * \brief Construction of the edge-based data structure and the multi-grid structure.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] dummy - Definition of the dummy driver.
+   */
+  void Geometrical_Preprocessing(CConfig* config, CGeometry**& geometry, bool dummy);
+
+  /*!
+   * \brief Definition and allocation of all solution classes.
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void Solver_Preprocessing(CConfig* config, CGeometry** geometry, CSolver***& solver);
+
+  /*!
+   * \brief Definition and allocation of all solver classes.
+   * \param[in] numerics_container - Description of the numerical method (the way in which the equations are solved).
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void Numerics_Preprocessing(CConfig* config, CGeometry** geometry, CSolver*** solver, CNumerics****& numerics) const;
+
+  /*!
+   * \brief Preprocess the output container.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] driver_config - Definition of the driver configuration.
+   * \param[in] output_container - Container vector with all the outputs.
+   * \param[in] driver_output - Definition of the driver output.
+   */
+  void Output_Preprocessing(CConfig** config, CConfig* driver_config, COutput**& output_container,
+                            COutput*& driver_output);
+
+  /*!
+   * \brief Read the free form deformation box information from the input mesh file.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] FFDBox - Definition of the FFD boxes of the problem.
+   * \param[in] val_mesh_filename - Name of the input mesh file.
+   */
+  void ReadFFDInfo(CGeometry* geometry, CConfig* config, CFreeFormDefBox** FFDBox, string val_mesh_filename);
 };
diff --git a/Common/src/drivers/CDriverBase.cpp b/Common/src/drivers/CDriverBase.cpp
index b778a6ab99b..f0b75542b0b 100644
--- a/Common/src/drivers/CDriverBase.cpp
+++ b/Common/src/drivers/CDriverBase.cpp
@@ -32,717 +32,1258 @@
 
 using namespace std;
 
-CDriverBase::CDriverBase(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator): 
-config_file_name(confFile),
-StartTime(0.0),
-StopTime(0.0),
-UsedTime(0.0),
-TimeIter(0),
-nZone(val_nZone)
-{
-    
+CDriverBase::CDriverBase(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator)
+    : config_file_name(confFile), StartTime(0.0), StopTime(0.0), UsedTime(0.0), TimeIter(0), nZone(val_nZone) {}
+
+CDriverBase::~CDriverBase(void) {}
+
+void CDriverBase::SetContainers_Null() {
+  /*--- Create pointers to all the classes that may be used by drivers. In general, the pointers are instantiated
+   * down a hierarchy over all zones, multi-grid levels, equation sets, and equation terms as described in the comments
+   * below. ---*/
+
+  config_container = nullptr;
+  output_container = nullptr;
+  geometry_container = nullptr;
+  solver_container = nullptr;
+  numerics_container = nullptr;
+
+  surface_movement = nullptr;
+  grid_movement = nullptr;
+  FFDBox = nullptr;
+
+  config_container = new CConfig*[nZone]();
+  output_container = new COutput*[nZone]();
+  geometry_container = new CGeometry***[nZone]();
+  solver_container = new CSolver****[nZone]();
+  numerics_container = new CNumerics*****[nZone]();
+  surface_movement = new CSurfaceMovement*[nZone]();
+  grid_movement = new CVolumetricMovement**[nZone]();
+  FFDBox = new CFreeFormDefBox**[nZone]();
+
+  nInst = new unsigned short[nZone];
+
+  for (iZone = 0; iZone < nZone; iZone++) {
+    nInst[iZone] = 1;
+    FFDBox[iZone] = new CFreeFormDefBox*[MAX_NUMBER_FFD];
+  }
+
+  driver_config = nullptr;
+  driver_output = nullptr;
+
+  main_config = nullptr;
+  main_geometry = nullptr;
+}
+
+unsigned short CDriverBase::GetNumberDesignVariables() const { return main_config->GetnDV(); }
+
+unsigned short CDriverBase::GetNumberFFDBoxes() const { return main_config->GetnFFDBox(); }
+
+unsigned short CDriverBase::GetNumberFFDBoxCornerPoints(unsigned short iFFDBox) const {
+  return FFDBox[ZONE_0][iFFDBox]->GetnCornerPoints();
 }
 
-CDriverBase::~CDriverBase(void) {
-    
+unsigned short CDriverBase::GetNumberFFDBoxControlPoints(unsigned short iFFDBox) const {
+  return FFDBox[ZONE_0][iFFDBox]->GetnControlPoints();
 }
 
-void CDriverBase::SetContainers_Null() {
-    
-    /*--- Create pointers to all of the classes that may be used by drivers. In general, the pointers are instantiated down a
-     hierarchy over all zones, multigrid levels, equation sets, and equation
-     terms as described in the comments below. ---*/
-    
-    config_container      = nullptr;
-    output_container      = nullptr;
-    geometry_container    = nullptr;
-    solver_container      = nullptr;
-    numerics_container    = nullptr;
-    
-    surface_movement      = nullptr;
-    grid_movement         = nullptr;
-    FFDBox                = nullptr;
-    
-    config_container      = new CConfig*[nZone] ();
-    output_container      = new COutput*[nZone] ();
-    geometry_container    = new CGeometry***[nZone] ();
-    solver_container      = new CSolver****[nZone] ();
-    numerics_container    = new CNumerics*****[nZone] ();
-    surface_movement      = new CSurfaceMovement*[nZone] ();
-    grid_movement         = new CVolumetricMovement**[nZone] ();
-    FFDBox                = new CFreeFormDefBox**[nZone] ();
-    
-    nInst                 = new unsigned short[nZone];
-    
-    for (iZone = 0; iZone < nZone; iZone++) {
-        nInst[iZone] = 1;
+unsigned long CDriverBase::GetNumberFFDBoxSurfacePoints(unsigned short iFFDBox) const {
+  return FFDBox[ZONE_0][iFFDBox]->GetnSurfacePoint();
+}
+
+vector<unsigned short> CDriverBase::GetFFDBoxMarkerIDs(unsigned short iFFDBox) const {
+  vector<unsigned short> values;
+
+  for (auto iPoint = 0ul; iPoint < GetNumberFFDBoxSurfacePoints(iFFDBox); iPoint++) {
+    values.push_back(FFDBox[ZONE_0][iFFDBox]->Get_MarkerIndex(iPoint));
+  }
+  return values;
+}
+
+vector<unsigned long> CDriverBase::GetFFDBoxVertexIDs(unsigned short iFFDBox) const {
+  vector<unsigned long> values;
+
+  for (auto iPoint = 0ul; iPoint < GetNumberFFDBoxSurfacePoints(iFFDBox); iPoint++) {
+    values.push_back(FFDBox[ZONE_0][iFFDBox]->Get_VertexIndex(iPoint));
+  }
+  return values;
+}
+
+vector<unsigned long> CDriverBase::GetFFDBoxPointIDs(unsigned short iFFDBox) const {
+  vector<unsigned long> values;
+
+  for (auto iPoint = 0ul; iPoint < GetNumberFFDBoxSurfacePoints(iFFDBox); iPoint++) {
+    values.push_back(FFDBox[ZONE_0][iFFDBox]->Get_PointIndex(iPoint));
+  }
+  return values;
+}
+
+vector<vector<passivedouble>> CDriverBase::GetFFDBoxCornerCoordinates(unsigned short iFFDBox) const {
+  vector<vector<passivedouble>> values;
+
+  for (auto iPoint = 0u; iPoint < GetNumberFFDBoxCornerPoints(iFFDBox); iPoint++) {
+    vector<passivedouble> coords;
+
+    const su2double* coord = FFDBox[ZONE_0][iFFDBox]->GetCoordCornerPoints(iPoint);
+
+    for (auto iDim = 0u; iDim < nDim; iDim++) {
+      coords.push_back(SU2_TYPE::GetValue(coord[iDim]));
+    }
+
+    values.push_back(coords);
+  }
+
+  return values;
+}
+
+vector<vector<passivedouble>> CDriverBase::GetFFDBoxControlPointCoordinates(unsigned short iFFDBox) const {
+  vector<vector<passivedouble>> values;
+
+  for (auto iOrder = 0u; iOrder < FFDBox[ZONE_0][iFFDBox]->GetlOrder(); iOrder++) {
+    for (auto jOrder = 0u; jOrder < FFDBox[ZONE_0][iFFDBox]->GetmOrder(); jOrder++) {
+      for (auto kOrder = 0u; kOrder < FFDBox[ZONE_0][iFFDBox]->GetnOrder(); kOrder++) {
+        values.push_back(GetFFDBoxControlPointCoordinates(iFFDBox, iOrder, jOrder, kOrder));
+      }
     }
-    
-    driver_config = nullptr;
-    driver_output = nullptr;
+  }
 
-    main_config = nullptr;
-    main_geometry = nullptr;
+  return values;
 }
 
-unsigned short CDriverBase::GetNumberMarkers() const {
-    return main_config->GetnMarker_All();
+vector<passivedouble> CDriverBase::GetFFDBoxControlPointCoordinates(unsigned short iFFDBox, unsigned int iOrder,
+                                                                    unsigned int jOrder, unsigned int kOrder) const {
+  vector<passivedouble> values;
+
+  const su2double* coord = FFDBox[ZONE_0][iFFDBox]->GetCoordControlPoints(iOrder, jOrder, kOrder);
+
+  for (auto iDim = 0u; iDim < nDim; iDim++) {
+    values.push_back(SU2_TYPE::GetValue(coord[iDim]));
+  }
+
+  return values;
 }
 
+vector<vector<passivedouble>> CDriverBase::GetFFDBoxSurfaceCoordinates(unsigned short iFFDBox, bool parametric) const {
+  vector<vector<passivedouble>> values;
+
+  for (auto iPoint = 0ul; iPoint < GetNumberFFDBoxSurfacePoints(iFFDBox); iPoint++) {
+    values.push_back(GetFFDBoxSurfaceCoordinates(iFFDBox, iPoint, parametric));
+  }
+
+  return values;
+}
+
+vector<passivedouble> CDriverBase::GetFFDBoxSurfaceCoordinates(unsigned short iFFDBox, unsigned long iPoint,
+                                                               bool parametric) const {
+  vector<passivedouble> values;
+  const su2double* coord;
+
+  if (parametric) {
+    coord = FFDBox[ZONE_0][iFFDBox]->Get_ParametricCoord(iPoint);
+  } else {
+    coord = FFDBox[ZONE_0][iFFDBox]->Get_CartesianCoord(iPoint);
+  }
+
+  for (auto iDim = 0u; iDim < nDim; iDim++) {
+    values.push_back(SU2_TYPE::GetValue(coord[iDim]));
+  }
+
+  return values;
+}
+
+unsigned short CDriverBase::GetNumberMarkers() const { return main_config->GetnMarker_All(); }
+
 map<string, unsigned short> CDriverBase::GetMarkerIndices() const {
-    const auto nMarker = main_config->GetnMarker_All();
-    map<string, unsigned short> indexMap;
-    
-    for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
-        auto tag = main_config->GetMarker_All_TagBound(iMarker);
+  const auto nMarker = main_config->GetnMarker_All();
+  map<string, unsigned short> indexMap;
 
-        indexMap[tag] = iMarker;
-    }
-    
-    return indexMap;
+  for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
+    auto tag = main_config->GetMarker_All_TagBound(iMarker);
+
+    indexMap[tag] = iMarker;
+  }
+
+  return indexMap;
 }
 
 map<string, string> CDriverBase::GetMarkerTypes() const {
-    map<string, string> typeMap;
-    string type;
-    
-    for (auto iMarker = 0u; iMarker < main_config->GetnMarker_All(); iMarker++) {
-        auto tag = main_config->GetMarker_All_TagBound(iMarker);
-        auto kindBC = main_config->GetMarker_All_KindBC(iMarker);
-        
-        switch(kindBC) {
-            case EULER_WALL:
-                type = "EULER_WALL";
-                break;
-            case FAR_FIELD:
-                type = "FARFIELD";
-                break;
-            case ISOTHERMAL:
-                type = "ISOTHERMAL";
-                break;
-            case HEAT_FLUX:
-                type = "HEATFLUX";
-                break;
-            case INLET_FLOW:
-                type = "INLET_FLOW";
-                break;
-            case OUTLET_FLOW:
-                type = "OUTLET_FLOW";
-                break;
-            case SYMMETRY_PLANE:
-                type = "SYMMETRY";
-                break;
-            case SEND_RECEIVE:
-                type = "SEND_RECEIVE";
-                break;
-            default:
-                type = "UNKNOWN_TYPE";
-        }
-        typeMap[tag] = type;
-    }
-    
-    return typeMap;
+  map<string, string> typeMap;
+  string type;
+
+  for (auto iMarker = 0u; iMarker < main_config->GetnMarker_All(); iMarker++) {
+    auto tag = main_config->GetMarker_All_TagBound(iMarker);
+    auto kindBC = main_config->GetMarker_All_KindBC(iMarker);
+
+    switch (kindBC) {
+      case EULER_WALL:
+        type = "EULER_WALL";
+        break;
+      case FAR_FIELD:
+        type = "FARFIELD";
+        break;
+      case ISOTHERMAL:
+        type = "ISOTHERMAL";
+        break;
+      case HEAT_FLUX:
+        type = "HEATFLUX";
+        break;
+      case INLET_FLOW:
+        type = "INLET_FLOW";
+        break;
+      case OUTLET_FLOW:
+        type = "OUTLET_FLOW";
+        break;
+      case SYMMETRY_PLANE:
+        type = "SYMMETRY";
+        break;
+      case SEND_RECEIVE:
+        type = "SEND_RECEIVE";
+        break;
+      default:
+        type = "UNKNOWN_TYPE";
+    }
+    typeMap[tag] = type;
+  }
+
+  return typeMap;
 }
 
 vector<string> CDriverBase::GetMarkerTags() const {
-    vector<string> tags;
-    const auto nMarker = main_config->GetnMarker_All();
-    
-    for(auto iMarker = 0u; iMarker < nMarker; iMarker++){
-        tags.push_back(main_config->GetMarker_All_TagBound(iMarker));
-    }
-    
-    return tags;
+  vector<string> tags;
+  const auto nMarker = main_config->GetnMarker_All();
+
+  for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
+    tags.push_back(main_config->GetMarker_All_TagBound(iMarker));
+  }
+
+  return tags;
 }
 
 vector<string> CDriverBase::GetDeformableMarkerTags() const {
-    vector<string> tags;
-    const auto nMarker = main_config->GetnMarker_Deform_Mesh();
-    
-    for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
-        tags.push_back(main_config->GetMarker_Deform_Mesh_TagBound(iMarker));
-    }
-    
-    return tags;
-}
+  vector<string> tags;
+  const auto nMarker = main_config->GetnMarker_Deform_Mesh();
 
-unsigned long CDriverBase::GetNumberDimensions() const {
-    return main_geometry->GetnDim();
-}
+  for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
+    tags.push_back(main_config->GetMarker_Deform_Mesh_TagBound(iMarker));
+  }
 
-unsigned long CDriverBase::GetNumberElements() const {
-    return main_geometry->GetnElem();
+  return tags;
 }
 
+unsigned long CDriverBase::GetNumberDimensions() const { return main_geometry->GetnDim(); }
+
+unsigned long CDriverBase::GetNumberElements() const { return main_geometry->GetnElem(); }
+
 unsigned long CDriverBase::GetNumberMarkerElements(unsigned short iMarker) const {
-    if (iMarker >= GetNumberMarkers()) {
-        SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
-    }
+  if (iMarker >= GetNumberMarkers()) {
+    SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
+  }
 
-    return main_geometry->GetnElem_Bound(iMarker);
+  return main_geometry->GetnElem_Bound(iMarker);
 }
 
 vector<unsigned long> CDriverBase::GetElementIDs() const {
-    const auto nElem = GetNumberElements();
+  const auto nElem = GetNumberElements();
 
-    vector<unsigned long> values;
+  vector<unsigned long> values;
 
-    for (auto iElem = 0ul; iElem < nElem; iElem++) {
-        values.push_back(GetElementIDs(iElem));
-    }
-    
-    return values;
+  for (auto iElem = 0ul; iElem < nElem; iElem++) {
+    values.push_back(GetElementIDs(iElem));
+  }
+
+  return values;
 }
 
 unsigned long CDriverBase::GetElementIDs(unsigned long iElem) const {
-    if (iElem >= GetNumberElements()) {
-        SU2_MPI::Error("Element index exceeds size.", CURRENT_FUNCTION);
-    }
+  if (iElem >= GetNumberElements()) {
+    SU2_MPI::Error("Element index exceeds size.", CURRENT_FUNCTION);
+  }
 
-    return main_geometry->elem[iElem]->GetGlobalIndex();
+  return main_geometry->elem[iElem]->GetGlobalIndex();
 }
 
-vector<unsigned long> CDriverBase::GetMarkerElementIDs(unsigned short iMarker) const { 
-    const auto nBound = GetNumberMarkerElements(iMarker);
+vector<unsigned long> CDriverBase::GetMarkerElementIDs(unsigned short iMarker) const {
+  const auto nBound = GetNumberMarkerElements(iMarker);
 
-    vector<unsigned long> values;
-     
-    for (auto iBound = 0ul; iBound < nBound; iBound++) {
-        values.push_back(GetMarkerElementIDs(iMarker, iBound));
-    }
-    
-    return values;
+  vector<unsigned long> values;
+
+  for (auto iBound = 0ul; iBound < nBound; iBound++) {
+    values.push_back(GetMarkerElementIDs(iMarker, iBound));
+  }
+
+  return values;
 }
 
 unsigned long CDriverBase::GetMarkerElementIDs(unsigned short iMarker, unsigned long iBound) const {
-    if (iBound >= GetNumberMarkerElements(iMarker)) {
-        SU2_MPI::Error("Marker element index exceeds size.", CURRENT_FUNCTION);
-    }
+  if (iBound >= GetNumberMarkerElements(iMarker)) {
+    SU2_MPI::Error("Marker element index exceeds size.", CURRENT_FUNCTION);
+  }
 
-    return main_geometry->bound[iMarker][iBound]->GetGlobalIndex();
+  return main_geometry->bound[iMarker][iBound]->GetGlobalIndex();
 }
 
 vector<vector<unsigned long>> CDriverBase::GetElementConnectivities() const {
-    const auto nElem = GetNumberElements();
-    
-    vector<vector<unsigned long>> values;
+  const auto nElem = GetNumberElements();
 
-    for (auto iElem = 0ul; iElem < nElem; iElem++) {
-        values.push_back(GetElementConnectivities(iElem));
-    }
-    
-    return values;
+  vector<vector<unsigned long>> values;
+
+  for (auto iElem = 0ul; iElem < nElem; iElem++) {
+    values.push_back(GetElementConnectivities(iElem));
+  }
+
+  return values;
 }
 
 vector<unsigned long> CDriverBase::GetElementConnectivities(unsigned long iElem) const {
-    if (iElem >= GetNumberElements()) {
-        SU2_MPI::Error("Element index exceeds size.", CURRENT_FUNCTION);
-    }
-    
-    unsigned short nNode = main_geometry->elem[iElem]->GetnNodes();
-    
-    vector<unsigned long> values; 
+  if (iElem >= GetNumberElements()) {
+    SU2_MPI::Error("Element index exceeds size.", CURRENT_FUNCTION);
+  }
 
-    for (auto iNode = 0u; iNode < nNode; iNode++) {
-        unsigned long iPoint = main_geometry->elem[iElem]->GetNode(iNode);
+  unsigned short nNode = main_geometry->elem[iElem]->GetnNodes();
 
-        values.push_back(main_geometry->nodes->GetGlobalIndex(iPoint));
-    }
-    
-    return values;
+  vector<unsigned long> values;
+
+  for (auto iNode = 0u; iNode < nNode; iNode++) {
+    unsigned long iPoint = main_geometry->elem[iElem]->GetNode(iNode);
+
+    values.push_back(main_geometry->nodes->GetGlobalIndex(iPoint));
+  }
+
+  return values;
 }
 
 vector<vector<unsigned long>> CDriverBase::GetMarkerElementConnectivities(unsigned short iMarker) const {
-    const auto nBound = GetNumberMarkerElements(iMarker);
-    
-    vector<vector<unsigned long>> values;
+  const auto nBound = GetNumberMarkerElements(iMarker);
 
-    for (auto iBound = 0ul; iBound < nBound; iBound++) {
-        values.push_back(GetMarkerElementConnectivities(iMarker, iBound));
-    }
-    
-    return values;
+  vector<vector<unsigned long>> values;
+
+  for (auto iBound = 0ul; iBound < nBound; iBound++) {
+    values.push_back(GetMarkerElementConnectivities(iMarker, iBound));
+  }
+
+  return values;
 }
 
 vector<unsigned long> CDriverBase::GetMarkerElementConnectivities(unsigned short iMarker, unsigned long iBound) const {
-    if (iBound >= GetNumberMarkerElements(iMarker)) {
-        SU2_MPI::Error("Marker element index exceeds size.", CURRENT_FUNCTION);
-    }
-    
-    unsigned short nNode = main_geometry->bound[iMarker][iBound]->GetnNodes();
-    
-    vector<unsigned long> values; 
+  if (iBound >= GetNumberMarkerElements(iMarker)) {
+    SU2_MPI::Error("Marker element index exceeds size.", CURRENT_FUNCTION);
+  }
 
-    for (auto iNode = 0u; iNode < nNode; iNode++) {
-        unsigned long iPoint = main_geometry->bound[iMarker][iBound]->GetNode(iNode);
+  unsigned short nNode = main_geometry->bound[iMarker][iBound]->GetnNodes();
 
-        values.push_back(main_geometry->nodes->GetGlobalIndex(iPoint));
-    }
-    
-    return values;
-}
+  vector<unsigned long> values;
+
+  for (auto iNode = 0u; iNode < nNode; iNode++) {
+    unsigned long iPoint = main_geometry->bound[iMarker][iBound]->GetNode(iNode);
+
+    values.push_back(main_geometry->nodes->GetGlobalIndex(iPoint));
+  }
 
-unsigned long CDriverBase::GetNumberVertices() const {
-    return main_geometry->GetnPoint();
+  return values;
 }
 
+unsigned long CDriverBase::GetNumberVertices() const { return main_geometry->GetnPoint(); }
+
 unsigned long CDriverBase::GetNumberMarkerVertices(unsigned short iMarker) const {
-    if (iMarker >= GetNumberMarkers()) {
-        SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
-    }
+  if (iMarker >= GetNumberMarkers()) {
+    SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
+  }
 
-    return main_geometry->GetnVertex(iMarker);
+  return main_geometry->GetnVertex(iMarker);
 }
 
 unsigned long CDriverBase::GetNumberHaloVertices() const {
-    const auto nPoint = GetNumberVertices();
-    unsigned long nHalo = 0;
-    
-    for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
-        if (!(main_geometry->nodes->GetDomain(iPoint))) {
-            nHalo += 1;
-        }
+  const auto nPoint = GetNumberVertices();
+  unsigned long nHalo = 0;
+
+  for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
+    if (!(main_geometry->nodes->GetDomain(iPoint))) {
+      nHalo += 1;
     }
-    
-    return nHalo;
+  }
+
+  return nHalo;
 }
 
 unsigned long CDriverBase::GetNumberMarkerHaloVertices(unsigned short iMarker) const {
-    const auto nVertex = GetNumberMarkerVertices(iMarker);
-    unsigned long nHalo = 0;
-    
-    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
-        
-        if (!(main_geometry->nodes->GetDomain(iPoint))) {
-            nHalo += 1;
-        }
+  const auto nVertex = GetNumberMarkerVertices(iMarker);
+  unsigned long nHalo = 0;
+
+  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+    auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
+
+    if (!(main_geometry->nodes->GetDomain(iPoint))) {
+      nHalo += 1;
     }
-    
-    return nHalo;
+  }
+
+  return nHalo;
 }
 
 vector<unsigned long> CDriverBase::GetMarkerVertexIndices(unsigned short iMarker) const {
-    const auto nVertex = GetNumberMarkerVertices(iMarker);
-    
-    vector<unsigned long> values;
+  const auto nVertex = GetNumberMarkerVertices(iMarker);
 
-    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        values.push_back(GetMarkerVertexIndices(iMarker, iVertex));
-    }
-    
-    return values;
+  vector<unsigned long> values;
+
+  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+    values.push_back(GetMarkerVertexIndices(iMarker, iVertex));
+  }
+
+  return values;
 }
 
 unsigned long CDriverBase::GetMarkerVertexIndices(unsigned short iMarker, unsigned long iVertex) const {
-    if (iVertex >= GetNumberMarkerVertices(iMarker)) {
-        SU2_MPI::Error("Marker vertex index exceeds size.", CURRENT_FUNCTION);
-    }
-    
-    return geometry_container[MESH_0][INST_0][ZONE_0]->vertex[iMarker][iVertex]->GetNode();
+  if (iVertex >= GetNumberMarkerVertices(iMarker)) {
+    SU2_MPI::Error("Vertex index exceeds marker size.", CURRENT_FUNCTION);
+  }
+
+  return geometry_container[MESH_0][INST_0][ZONE_0]->vertex[iMarker][iVertex]->GetNode();
 }
 
 vector<unsigned long> CDriverBase::GetVertexIDs() const {
-    const auto nPoint = GetNumberVertices();
-    
-    vector<unsigned long> values;
+  const auto nPoint = GetNumberVertices();
 
-    for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
-        values.push_back(GetVertexIDs(iPoint));
-    }
-    
-    return values;
+  vector<unsigned long> values;
+
+  for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
+    values.push_back(GetVertexIDs(iPoint));
+  }
+
+  return values;
 }
 
 unsigned long CDriverBase::GetVertexIDs(unsigned long iPoint) const {
-    if (iPoint >= GetNumberVertices()) {
-        SU2_MPI::Error("Vertex index exceeds size.", CURRENT_FUNCTION);
-    }
+  if (iPoint >= GetNumberVertices()) {
+    SU2_MPI::Error("Vertex index exceeds mesh size.", CURRENT_FUNCTION);
+  }
 
-    return main_geometry->nodes->GetGlobalIndex(iPoint);
+  return main_geometry->nodes->GetGlobalIndex(iPoint);
 }
 
 vector<unsigned long> CDriverBase::GetMarkerVertexIDs(unsigned short iMarker) const {
-    const auto nVertex = GetNumberMarkerVertices(iMarker); 
-    
-    vector<unsigned long> values;
+  const auto nVertex = GetNumberMarkerVertices(iMarker);
 
-    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        values.push_back(GetMarkerVertexIDs(iMarker, iVertex));
-    }
-    
-    return values;
+  vector<unsigned long> values;
+
+  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+    values.push_back(GetMarkerVertexIDs(iMarker, iVertex));
+  }
+
+  return values;
 }
 
 unsigned long CDriverBase::GetMarkerVertexIDs(unsigned short iMarker, unsigned long iVertex) const {
-    auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
+  auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
 
-    return main_geometry->nodes->GetGlobalIndex(iPoint);
+  return main_geometry->nodes->GetGlobalIndex(iPoint);
 }
 
 vector<bool> CDriverBase::GetDomain() const {
-    const auto nPoint = GetNumberVertices();
+  const auto nPoint = GetNumberVertices();
 
-    vector<bool> values;
-    
-    for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
-        values.push_back(GetDomain(iPoint));
-    }
-    
-    return values;
+  vector<bool> values;
+
+  for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
+    values.push_back(GetDomain(iPoint));
+  }
+
+  return values;
 }
 
 bool CDriverBase::GetDomain(unsigned long iPoint) const {
-    if (iPoint >= GetNumberVertices()) {
-        SU2_MPI::Error("Vertex index exceeds size.", CURRENT_FUNCTION);
-    }
-    
-    return main_geometry->nodes->GetDomain(iPoint);
+  if (iPoint >= GetNumberVertices()) {
+    SU2_MPI::Error("Vertex index exceeds mesh size.", CURRENT_FUNCTION);
+  }
+
+  return main_geometry->nodes->GetDomain(iPoint);
 }
 
 vector<bool> CDriverBase::GetMarkerDomain(unsigned short iMarker) const {
-    const auto nVertex = GetNumberMarkerVertices(iMarker);
+  const auto nVertex = GetNumberMarkerVertices(iMarker);
 
-    vector<bool> values;
-    
-    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        values.push_back(GetMarkerDomain(iMarker, iVertex));
-    }
-    
-    return values;
+  vector<bool> values;
+
+  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+    values.push_back(GetMarkerDomain(iMarker, iVertex));
+  }
+
+  return values;
 }
 
 bool CDriverBase::GetMarkerDomain(unsigned short iMarker, unsigned long iVertex) const {
-    auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
-    
-    return main_geometry->nodes->GetDomain(iPoint);
+  auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
+
+  return main_geometry->nodes->GetDomain(iPoint);
 }
 
 vector<vector<passivedouble>> CDriverBase::GetInitialCoordinates() const {
-    const auto nPoint = GetNumberVertices();
+  const auto nPoint = GetNumberVertices();
 
-    vector<vector<passivedouble>> values;
-    
-    for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
-        values.push_back(GetInitialCoordinates(iPoint));
-    }
-    
-    return values;
+  vector<vector<passivedouble>> values;
+
+  for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
+    values.push_back(GetInitialCoordinates(iPoint));
+  }
+
+  return values;
 }
 
 vector<passivedouble> CDriverBase::GetInitialCoordinates(unsigned long iPoint) const {
-    if (iPoint >= GetNumberVertices()) {
-        SU2_MPI::Error("Vertex index exceeds size.", CURRENT_FUNCTION);
-    }
+  if (iPoint >= GetNumberVertices()) {
+    SU2_MPI::Error("Vertex index exceeds mesh size.", CURRENT_FUNCTION);
+  }
 
-    vector<passivedouble> values (nDim, 0.0);
-    
-    if (!main_config->GetDeform_Mesh()) {
-        return values;
-    }
+  vector<passivedouble> values(nDim, 0.0);
 
-    for (auto iDim = 0u; iDim < nDim; iDim++) {
-        const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord(iPoint, iDim);
-        
-        values[iDim] = SU2_TYPE::GetValue(value);
-    }
-    
+  if (!main_config->GetDeform_Mesh()) {
     return values;
+  }
+
+  for (auto iDim = 0u; iDim < nDim; iDim++) {
+    const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord(iPoint, iDim);
+
+    values[iDim] = SU2_TYPE::GetValue(value);
+  }
+
+  return values;
 }
 
 vector<vector<passivedouble>> CDriverBase::GetMarkerInitialCoordinates(unsigned short iMarker) const {
-    const auto nVertex = GetNumberMarkerVertices(iMarker);
+  const auto nVertex = GetNumberMarkerVertices(iMarker);
 
-    vector<vector<passivedouble>> values;
-    
-    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        values.push_back(GetMarkerInitialCoordinates(iMarker, iVertex));
-    }
-    
-    return values;
+  vector<vector<passivedouble>> values;
+
+  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+    values.push_back(GetMarkerInitialCoordinates(iMarker, iVertex));
+  }
+
+  return values;
 }
 
 vector<passivedouble> CDriverBase::GetMarkerInitialCoordinates(unsigned short iMarker, unsigned long iVertex) const {
-    auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
+  auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
 
-    vector<passivedouble> values(nDim, 0.0);
+  vector<passivedouble> values(nDim, 0.0);
 
-    if (!main_config->GetDeform_Mesh()) {
-        return values;
-    }
+  if (!main_config->GetDeform_Mesh()) {
+    return values;
+  }
 
-    for (auto iDim = 0u; iDim < nDim; iDim++) {
-        const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord(iPoint, iDim);
+  for (auto iDim = 0u; iDim < nDim; iDim++) {
+    const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord(iPoint, iDim);
 
-        values[iDim] = SU2_TYPE::GetValue(value);
-    }
-    
-    return values;
+    values[iDim] = SU2_TYPE::GetValue(value);
+  }
+
+  return values;
 }
 
 vector<vector<passivedouble>> CDriverBase::GetCoordinates() const {
-    const auto nPoint = GetNumberVertices();
+  const auto nPoint = GetNumberVertices();
 
-    vector<vector<passivedouble>> values;
-    
-    for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
-        values.push_back(GetCoordinates(iPoint));
-    }
-    
-    return values;
+  vector<vector<passivedouble>> values;
+
+  for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
+    values.push_back(GetCoordinates(iPoint));
+  }
+
+  return values;
 }
 
 vector<passivedouble> CDriverBase::GetCoordinates(unsigned long iPoint) const {
-    if (iPoint >= GetNumberVertices()) {
-        SU2_MPI::Error("Vertex index exceeds size.", CURRENT_FUNCTION);
-    }
+  if (iPoint >= GetNumberVertices()) {
+    SU2_MPI::Error("Vertex index exceeds mesh size.", CURRENT_FUNCTION);
+  }
 
-    vector<passivedouble> values;
-    
-    for (auto iDim = 0u; iDim < nDim; iDim++) {
-        const su2double value = main_geometry->nodes->GetCoord(iPoint, iDim);
-        
-        values.push_back(SU2_TYPE::GetValue(value));
-    }
-    
-    return values;
+  vector<passivedouble> values;
+
+  for (auto iDim = 0u; iDim < nDim; iDim++) {
+    const su2double value = main_geometry->nodes->GetCoord(iPoint, iDim);
+
+    values.push_back(SU2_TYPE::GetValue(value));
+  }
+
+  return values;
 }
 
 vector<vector<passivedouble>> CDriverBase::GetMarkerCoordinates(unsigned short iMarker) const {
-    const auto nVertex = GetNumberMarkerVertices(iMarker);
+  const auto nVertex = GetNumberMarkerVertices(iMarker);
 
-    vector<vector<passivedouble>> values;
-    
-    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        values.push_back(GetMarkerCoordinates(iMarker, iVertex));
-    }
-    
-    return values;
+  vector<vector<passivedouble>> values;
+
+  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+    values.push_back(GetMarkerCoordinates(iMarker, iVertex));
+  }
+
+  return values;
 }
 
 vector<passivedouble> CDriverBase::GetMarkerCoordinates(unsigned short iMarker, unsigned long iVertex) const {
-    auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
+  auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
 
-    vector<passivedouble> values;
-    
-    for (auto iDim = 0u; iDim < nDim; iDim++) {
-        const su2double value = main_geometry->nodes->GetCoord(iPoint, iDim);
-        
-        values.push_back(SU2_TYPE::GetValue(value));
-    }
-    
-    return values;
+  vector<passivedouble> values;
+
+  for (auto iDim = 0u; iDim < nDim; iDim++) {
+    const su2double value = main_geometry->nodes->GetCoord(iPoint, iDim);
+
+    values.push_back(SU2_TYPE::GetValue(value));
+  }
+
+  return values;
 }
 
 void CDriverBase::SetCoordinates(vector<vector<passivedouble>> values) {
-    const auto nPoint = GetNumberVertices();
-    
-    if (values.size() != nPoint) {
-        SU2_MPI::Error("Invalid number of vertices !", CURRENT_FUNCTION);
-    }
-    
-    for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
-        SetCoordinates(iPoint, values[iPoint]);
-    }
+  const auto nPoint = GetNumberVertices();
+
+  if (values.size() != nPoint) {
+    SU2_MPI::Error("Invalid number of vertices!", CURRENT_FUNCTION);
+  }
+
+  for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
+    SetCoordinates(iPoint, values[iPoint]);
+  }
 }
 
 void CDriverBase::SetCoordinates(unsigned long iPoint, vector<passivedouble> values) {
-    if (iPoint >= GetNumberVertices()) {
-        SU2_MPI::Error("Vertex index exceeds size.", CURRENT_FUNCTION);
-    }
-
-    if (values.size() != nDim) {
-        SU2_MPI::Error("Invalid number of dimensions !", CURRENT_FUNCTION);
-    }
-    
-    for (auto iDim = 0u; iDim < nDim; iDim++) {
-        main_geometry->nodes->SetCoord(iPoint, iDim, values[iDim]);
-    }
+  if (iPoint >= GetNumberVertices()) {
+    SU2_MPI::Error("Vertex index exceeds mesh size.", CURRENT_FUNCTION);
+  }
+  if (values.size() != nDim) {
+    SU2_MPI::Error("Invalid number of dimensions!", CURRENT_FUNCTION);
+  }
+
+  for (auto iDim = 0u; iDim < nDim; iDim++) {
+    main_geometry->nodes->SetCoord(iPoint, iDim, values[iDim]);
+  }
 }
 
 void CDriverBase::SetMarkerCoordinates(unsigned short iMarker, vector<vector<passivedouble>> values) {
-    const auto nVertex = GetNumberMarkerVertices(iMarker);
+  const auto nVertex = GetNumberMarkerVertices(iMarker);
 
-    if (values.size() != nVertex) {
-        SU2_MPI::Error("Invalid number of marker vertices !", CURRENT_FUNCTION);
-    }
-    
-    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        SetMarkerCoordinates(iMarker, iVertex, values[iVertex]);
-    }
+  if (values.size() != nVertex) {
+    SU2_MPI::Error("Invalid number of marker vertices!", CURRENT_FUNCTION);
+  }
+
+  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+    SetMarkerCoordinates(iMarker, iVertex, values[iVertex]);
+  }
 }
 
 void CDriverBase::SetMarkerCoordinates(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
-    auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
+  auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
 
-    if (values.size() != nDim) {
-        SU2_MPI::Error("Invalid number of dimensions !", CURRENT_FUNCTION);
-    }
-    
-    for (auto iDim = 0u; iDim < nDim; iDim++) {
-        main_geometry->nodes->SetCoord(iPoint, iDim, values[iDim]);
-    }
+  if (values.size() != nDim) {
+    SU2_MPI::Error("Invalid number of dimensions!", CURRENT_FUNCTION);
+  }
+
+  for (auto iDim = 0u; iDim < nDim; iDim++) {
+    main_geometry->nodes->SetCoord(iPoint, iDim, values[iDim]);
+  }
 }
 
 vector<vector<passivedouble>> CDriverBase::GetMarkerDisplacements(unsigned short iMarker) const {
-    const auto nVertex = GetNumberMarkerVertices(iMarker);
+  const auto nVertex = GetNumberMarkerVertices(iMarker);
 
-    vector<vector<passivedouble>> values;
-    
-    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        values.push_back(GetMarkerDisplacements(iMarker, iVertex));
-    }
-    
-    return values;
+  vector<vector<passivedouble>> values;
+
+  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+    values.push_back(GetMarkerDisplacements(iMarker, iVertex));
+  }
+
+  return values;
 }
 
 vector<passivedouble> CDriverBase::GetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex) const {
-    auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
+  auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
 
-    vector<passivedouble> values (nDim, 0.0);
-    
-    if (!main_config->GetDeform_Mesh()) {
-        return values;
-    }
-    
-    for (auto iDim = 0u; iDim < nDim; iDim++) {
-        const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetBound_Disp(iPoint, iDim);
-        
-        values[iDim] = SU2_TYPE::GetValue(value);
-    }
-    
+  vector<passivedouble> values(nDim, 0.0);
+
+  if (!main_config->GetDeform_Mesh()) {
     return values;
+  }
+
+  for (auto iDim = 0u; iDim < nDim; iDim++) {
+    const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetBound_Disp(iPoint, iDim);
+
+    values[iDim] = SU2_TYPE::GetValue(value);
+  }
+
+  return values;
 }
 
 void CDriverBase::SetMarkerDisplacements(unsigned short iMarker, vector<vector<passivedouble>> values) {
-    if (!main_config->GetDeform_Mesh()) {
-        SU2_MPI::Error("Mesh solver is not defined !", CURRENT_FUNCTION);
-    }
+  if (!main_config->GetDeform_Mesh()) {
+    SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
+  }
 
-    const auto nVertex = GetNumberMarkerVertices(iMarker);
+  const auto nVertex = GetNumberMarkerVertices(iMarker);
 
-    if (values.size() != nVertex) {
-        SU2_MPI::Error("Invalid number of marker vertices !", CURRENT_FUNCTION);
-    }
-    
-    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        SetMarkerDisplacements(iMarker, iVertex, values[iVertex]);
-    }
+  if (values.size() != nVertex) {
+    SU2_MPI::Error("Invalid number of marker vertices!", CURRENT_FUNCTION);
+  }
+
+  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+    SetMarkerDisplacements(iMarker, iVertex, values[iVertex]);
+  }
 }
 
 void CDriverBase::SetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
-    if (!main_config->GetDeform_Mesh()) {
-        SU2_MPI::Error("Mesh solver is not defined !", CURRENT_FUNCTION);
-    }
+  if (!main_config->GetDeform_Mesh()) {
+    SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
+  }
 
-    auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
+  auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
 
-    if (values.size() != nDim) {
-        SU2_MPI::Error("Invalid number of dimensions !", CURRENT_FUNCTION);
-    }
-    
-    for (auto iDim = 0u; iDim < nDim; iDim++) {
-        solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->SetBound_Disp(iPoint, iDim, values[iDim]);
-    }
+  if (values.size() != nDim) {
+    SU2_MPI::Error("Invalid number of dimensions!", CURRENT_FUNCTION);
+  }
+
+  for (auto iDim = 0u; iDim < nDim; iDim++) {
+    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->SetBound_Disp(iPoint, iDim, values[iDim]);
+  }
 }
 
 vector<vector<passivedouble>> CDriverBase::GetMarkerVelocities(unsigned short iMarker) const {
-    const auto nVertex = GetNumberMarkerVertices(iMarker);
+  const auto nVertex = GetNumberMarkerVertices(iMarker);
 
-    vector<vector<passivedouble>> values;
-    
-    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        values.push_back(GetMarkerVelocities(iMarker, iVertex));
-    }
-    
-    return values;
+  vector<vector<passivedouble>> values;
+
+  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+    values.push_back(GetMarkerVelocities(iMarker, iVertex));
+  }
+
+  return values;
 }
 
 vector<passivedouble> CDriverBase::GetMarkerVelocities(unsigned short iMarker, unsigned long iVertex) const {
-    auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
+  auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
 
-    vector<passivedouble> values (nDim, 0.0);
-    
-    if (!main_config->GetDeform_Mesh()) {
-        return values;
-    }
-    
-    for (auto iDim = 0u; iDim < nDim; iDim++) {
-        const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetBound_Vel(iPoint, iDim);
-        
-        values[iDim] = SU2_TYPE::GetValue(value);
-    }
-    
+  vector<passivedouble> values(nDim, 0.0);
+
+  if (!main_config->GetDeform_Mesh()) {
     return values;
+  }
+
+  for (auto iDim = 0u; iDim < nDim; iDim++) {
+    const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetBound_Vel(iPoint, iDim);
+
+    values[iDim] = SU2_TYPE::GetValue(value);
+  }
+
+  return values;
 }
 
 void CDriverBase::SetMarkerVelocities(unsigned short iMarker, vector<vector<passivedouble>> values) {
-    if (!main_config->GetDeform_Mesh()) {
-        SU2_MPI::Error("Mesh solver is not defined !", CURRENT_FUNCTION);
-    }
+  if (!main_config->GetDeform_Mesh()) {
+    SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
+  }
 
-    const auto nVertex = GetNumberMarkerVertices(iMarker);
+  const auto nVertex = GetNumberMarkerVertices(iMarker);
 
-    if (values.size() != nVertex) {
-        SU2_MPI::Error("Invalid number of marker vertices !", CURRENT_FUNCTION);
-    }
-    
-    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        SetMarkerVelocities(iMarker, iVertex, values[iVertex]);
-    }
+  if (values.size() != nVertex) {
+    SU2_MPI::Error("Invalid number of marker vertices!", CURRENT_FUNCTION);
+  }
+
+  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+    SetMarkerVelocities(iMarker, iVertex, values[iVertex]);
+  }
 }
 
 void CDriverBase::SetMarkerVelocities(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
-    if (!main_config->GetDeform_Mesh()) {
-        SU2_MPI::Error("Mesh solver is not defined !", CURRENT_FUNCTION);
-    }
+  if (!main_config->GetDeform_Mesh()) {
+    SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
+  }
 
-    auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
+  auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
 
-    if (values.size() != nDim) {
-        SU2_MPI::Error("Invalid number of dimensions !", CURRENT_FUNCTION);
-    }
-    
-    for (auto iDim = 0u; iDim < nDim; iDim++) {
-        solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->SetBound_Disp(iPoint, iDim, values[iDim]);
-    }
+  if (values.size() != nDim) {
+    SU2_MPI::Error("Invalid number of dimensions!", CURRENT_FUNCTION);
+  }
+
+  for (auto iDim = 0u; iDim < nDim; iDim++) {
+    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->SetBound_Disp(iPoint, iDim, values[iDim]);
+  }
 }
 
 vector<vector<passivedouble>> CDriverBase::GetMarkerVertexNormals(unsigned short iMarker, bool normalize) const {
-    const auto nVertex = GetNumberMarkerVertices(iMarker);
+  const auto nVertex = GetNumberMarkerVertices(iMarker);
+
+  vector<vector<passivedouble>> values;
+
+  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
+    values.push_back(GetMarkerVertexNormals(iMarker, iVertex, normalize = normalize));
+  }
+
+  return values;
+}
 
-    vector<vector<passivedouble>> values;
-    
-    for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-        values.push_back(GetMarkerVertexNormals(iMarker, iVertex, normalize=normalize));
+vector<passivedouble> CDriverBase::GetMarkerVertexNormals(unsigned short iMarker, unsigned long iVertex,
+                                                          bool normalize) const {
+  if (iVertex >= GetNumberMarkerVertices(iMarker)) {
+    SU2_MPI::Error("Vertex index exceeds marker size.", CURRENT_FUNCTION);
+  }
+
+  vector<passivedouble> values(nDim, 0.0);
+
+  auto normal = main_geometry->vertex[iMarker][iVertex]->GetNormal();
+  auto area = GeometryToolbox::Norm(nDim, normal);
+
+  for (auto iDim = 0u; iDim < nDim; iDim++) {
+    if (normalize) {
+      values[iDim] = SU2_TYPE::GetValue(normal[iDim] / area);
+    } else {
+      values[iDim] = SU2_TYPE::GetValue(normal[iDim]);
     }
-    
-    return values;
+  }
+
+  return values;
 }
 
-vector<passivedouble> CDriverBase::GetMarkerVertexNormals(unsigned short iMarker, unsigned long iVertex, bool normalize) const {
-    if (iVertex >= GetNumberMarkerVertices(iMarker)) {
-        SU2_MPI::Error("Marker vertex index exceeds size.", CURRENT_FUNCTION);
+void CDriverBase::CommunicateMeshDisplacements(void) {
+  solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->InitiateComms(main_geometry, main_config, MESH_DISPLACEMENTS);
+  solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->CompleteComms(main_geometry, main_config, MESH_DISPLACEMENTS);
+}
+
+void CDriverBase::ReadFFDInfo(CGeometry* geometry, CConfig* config, CFreeFormDefBox** FFDBox, string val_mesh_filename) {
+  string text_line, iTag;
+  ifstream mesh_file;
+  su2double CPcoord[3], coord[] = {0, 0, 0};
+  unsigned short degree[3], iFFDBox, iCornerPoints, iControlPoints, iMarker, iDegree, jDegree, kDegree, iChar,
+      LevelFFDBox, nParentFFDBox, iParentFFDBox, nChildFFDBox, iChildFFDBox, nMarker, *nCornerPoints, *nControlPoints;
+  unsigned long iSurfacePoints, iPoint, jPoint, iVertex, nVertex, nPoint, iElem = 0, nElem, my_nSurfPoints, nSurfPoints,
+                                                                          *nSurfacePoints;
+  su2double XCoord, YCoord;
+
+  bool polar = (config->GetFFD_CoordSystem() == POLAR);
+  unsigned short nDim = geometry->GetnDim(), iDim;
+  unsigned short SplineOrder[3];
+  unsigned short Blending = 0;
+
+  unsigned short nFFDBox = 0;
+  unsigned short nLevel = 0;
+  bool FFDBoxDefinition = false;
+
+  mesh_file.open(val_mesh_filename);
+  if (mesh_file.fail()) {
+    SU2_MPI::Error("There is no geometry file (ReadFFDInfo)!!", CURRENT_FUNCTION);
+  }
+
+  while (getline(mesh_file, text_line)) {
+    /*--- Read the inner elements. ---*/
+
+    string::size_type position = text_line.find("NELEM=", 0);
+    if (position != string::npos) {
+      text_line.erase(0, 6);
+      nElem = atoi(text_line.c_str());
+      for (iElem = 0; iElem < nElem; iElem++) {
+        getline(mesh_file, text_line);
+      }
+    }
+
+    /*--- Read the inner points. ---*/
+
+    position = text_line.find("NPOIN=", 0);
+    if (position != string::npos) {
+      text_line.erase(0, 6);
+      nPoint = atoi(text_line.c_str());
+      for (iPoint = 0; iPoint < nPoint; iPoint++) {
+        getline(mesh_file, text_line);
+      }
+    }
+
+    /*--- Read the boundaries. ---*/
+
+    position = text_line.find("NMARK=", 0);
+    if (position != string::npos) {
+      text_line.erase(0, 6);
+      nMarker = atoi(text_line.c_str());
+      for (iMarker = 0; iMarker < nMarker; iMarker++) {
+        getline(mesh_file, text_line);
+        getline(mesh_file, text_line);
+        text_line.erase(0, 13);
+        nVertex = atoi(text_line.c_str());
+        for (iVertex = 0; iVertex < nVertex; iVertex++) {
+          getline(mesh_file, text_line);
+        }
+      }
     }
 
-    vector<passivedouble> values;
+    /*--- Read the FFDBox information. ---*/
 
-    auto normal = main_geometry->vertex[iMarker][iVertex]->GetNormal();
-    auto area   = GeometryToolbox::Norm(nDim, normal);
-    
-    for (auto iDim = 0u; iDim < nDim; iDim++) {
-        if (normalize) {
-            values[iDim] = SU2_TYPE::GetValue(normal[iDim]/area);
+    position = text_line.find("FFD_NBOX=", 0);
+    if (position != string::npos) {
+      text_line.erase(0, 9);
+      nFFDBox = atoi(text_line.c_str());
+
+      if (rank == MASTER_NODE) cout << nFFDBox << " Free Form Deformation boxes." << endl;
+
+      nCornerPoints = new unsigned short[nFFDBox];
+      nControlPoints = new unsigned short[nFFDBox];
+      nSurfacePoints = new unsigned long[nFFDBox];
+
+      getline(mesh_file, text_line);
+      text_line.erase(0, 11);
+      nLevel = atoi(text_line.c_str());
+
+      if (rank == MASTER_NODE) cout << nLevel << " Free Form Deformation nested levels." << endl;
+
+      for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) {
+        /*--- Read the name of the FFD box. ---*/
+
+        getline(mesh_file, text_line);
+        text_line.erase(0, 8);
+
+        /*--- Remove extra data from the FFDBox name. ---*/
+
+        string::size_type position;
+        for (iChar = 0; iChar < 20; iChar++) {
+          position = text_line.find(" ", 0);
+          if (position != string::npos) text_line.erase(position, 1);
+          position = text_line.find("\r", 0);
+          if (position != string::npos) text_line.erase(position, 1);
+          position = text_line.find("\n", 0);
+          if (position != string::npos) text_line.erase(position, 1);
+        }
+
+        string TagFFDBox = text_line.c_str();
+
+        if (rank == MASTER_NODE) cout << "FFD box tag: " << TagFFDBox << ". ";
+
+        /*--- Read the level of the FFD box. ---*/
+
+        getline(mesh_file, text_line);
+        text_line.erase(0, 10);
+        LevelFFDBox = atoi(text_line.c_str());
+
+        if (rank == MASTER_NODE) cout << "FFD box level: " << LevelFFDBox << ". ";
+
+        /*--- Read the degree of the FFD box. ---*/
+
+        if (nDim == 2) {
+          if (polar) {
+            getline(mesh_file, text_line);
+            text_line.erase(0, 13);
+            degree[0] = atoi(text_line.c_str());
+            degree[1] = 1;
+            getline(mesh_file, text_line);
+            text_line.erase(0, 13);
+            degree[2] = atoi(text_line.c_str());
+          } else {
+            getline(mesh_file, text_line);
+            text_line.erase(0, 13);
+            degree[0] = atoi(text_line.c_str());
+            getline(mesh_file, text_line);
+            text_line.erase(0, 13);
+            degree[1] = atoi(text_line.c_str());
+            degree[2] = 1;
+          }
         } else {
-            values[iDim] = SU2_TYPE::GetValue(normal[iDim]);
+          getline(mesh_file, text_line);
+          text_line.erase(0, 13);
+          degree[0] = atoi(text_line.c_str());
+          getline(mesh_file, text_line);
+          text_line.erase(0, 13);
+          degree[1] = atoi(text_line.c_str());
+          getline(mesh_file, text_line);
+          text_line.erase(0, 13);
+          degree[2] = atoi(text_line.c_str());
         }
-    }
 
-    return values;
-}
+        if (rank == MASTER_NODE) {
+          if (nDim == 2) {
+            if (polar)
+              cout << "Degrees: " << degree[0] << ", " << degree[2] << "." << endl;
+            else
+              cout << "Degrees: " << degree[0] << ", " << degree[1] << "." << endl;
+          } else
+            cout << "Degrees: " << degree[0] << ", " << degree[1] << ", " << degree[2] << "." << endl;
+        }
 
+        getline(mesh_file, text_line);
+        if (text_line.substr(0, 12) != "FFD_BLENDING") {
+          SU2_MPI::Error(
+              string("Deprecated FFD information found in mesh file.\n") +
+                  string(
+                      "FFD information generated with SU2 version <= 4.3 is incompatible with the current version.") +
+                  string("Run SU2_DEF again with DV_KIND= FFD_SETTING."),
+              CURRENT_FUNCTION);
+        }
+        text_line.erase(0, 14);
+        if (text_line == "BEZIER") {
+          Blending = BEZIER;
+        }
+        if (text_line == "BSPLINE_UNIFORM") {
+          Blending = BSPLINE_UNIFORM;
+        }
 
-void CDriverBase::CommunicateMeshDisplacements(void) {
-    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->InitiateComms(main_geometry, main_config, MESH_DISPLACEMENTS);
-    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->CompleteComms(main_geometry, main_config, MESH_DISPLACEMENTS);
+        if (Blending == BSPLINE_UNIFORM) {
+          getline(mesh_file, text_line);
+          text_line.erase(0, 17);
+          SplineOrder[0] = atoi(text_line.c_str());
+          getline(mesh_file, text_line);
+          text_line.erase(0, 17);
+          SplineOrder[1] = atoi(text_line.c_str());
+          if (nDim == 3) {
+            getline(mesh_file, text_line);
+            text_line.erase(0, 17);
+            SplineOrder[2] = atoi(text_line.c_str());
+          } else {
+            SplineOrder[2] = 2;
+          }
+        }
+        if (rank == MASTER_NODE) {
+          if (Blending == BSPLINE_UNIFORM) {
+            cout << "FFD Blending using B-Splines. ";
+            cout << "Order: " << SplineOrder[0] << ", " << SplineOrder[1];
+            if (nDim == 3) cout << ", " << SplineOrder[2];
+            cout << ". " << endl;
+          }
+          if (Blending == BEZIER) {
+            cout << "FFD Blending using Bezier Curves." << endl;
+          }
+        }
+
+        FFDBox[iFFDBox] = new CFreeFormDefBox(degree, SplineOrder, Blending);
+        FFDBox[iFFDBox]->SetTag(TagFFDBox);
+        FFDBox[iFFDBox]->SetLevel(LevelFFDBox);
+
+        /*--- Read the number of parents boxes. ---*/
+
+        getline(mesh_file, text_line);
+        text_line.erase(0, 12);
+        nParentFFDBox = atoi(text_line.c_str());
+        if (rank == MASTER_NODE) cout << "Number of parent boxes: " << nParentFFDBox << ". ";
+        for (iParentFFDBox = 0; iParentFFDBox < nParentFFDBox; iParentFFDBox++) {
+          getline(mesh_file, text_line);
+
+          /*--- Remove extra data from the FFDBox name. ---*/
+
+          string::size_type position;
+          for (iChar = 0; iChar < 20; iChar++) {
+            position = text_line.find(" ", 0);
+            if (position != string::npos) text_line.erase(position, 1);
+            position = text_line.find("\r", 0);
+            if (position != string::npos) text_line.erase(position, 1);
+            position = text_line.find("\n", 0);
+            if (position != string::npos) text_line.erase(position, 1);
+          }
+
+          string ParentFFDBox = text_line.c_str();
+          FFDBox[iFFDBox]->SetParentFFDBox(ParentFFDBox);
+        }
+
+        /*--- Read the number of children boxes. ---*/
+
+        getline(mesh_file, text_line);
+        text_line.erase(0, 13);
+        nChildFFDBox = atoi(text_line.c_str());
+        if (rank == MASTER_NODE) cout << "Number of child boxes: " << nChildFFDBox << "." << endl;
+
+        for (iChildFFDBox = 0; iChildFFDBox < nChildFFDBox; iChildFFDBox++) {
+          getline(mesh_file, text_line);
+
+          /*--- Remove extra data from the FFDBox name. ---*/
+
+          string::size_type position;
+          for (iChar = 0; iChar < 20; iChar++) {
+            position = text_line.find(" ", 0);
+            if (position != string::npos) text_line.erase(position, 1);
+            position = text_line.find("\r", 0);
+            if (position != string::npos) text_line.erase(position, 1);
+            position = text_line.find("\n", 0);
+            if (position != string::npos) text_line.erase(position, 1);
+          }
+
+          string ChildFFDBox = text_line.c_str();
+          FFDBox[iFFDBox]->SetChildFFDBox(ChildFFDBox);
+        }
+
+        /*--- Read the number of the corner points. ---*/
+
+        getline(mesh_file, text_line);
+        text_line.erase(0, 18);
+        nCornerPoints[iFFDBox] = atoi(text_line.c_str());
+        if (rank == MASTER_NODE) cout << "Corner points: " << nCornerPoints[iFFDBox] << ". ";
+        if (nDim == 2) nCornerPoints[iFFDBox] = nCornerPoints[iFFDBox] * SU2_TYPE::Int(2);
+
+        /*--- Read the coordinates of the corner points. ---*/
+
+        if (nDim == 2) {
+          if (polar) {
+            getline(mesh_file, text_line);
+            istringstream FFDBox_line_1(text_line);
+            FFDBox_line_1 >> XCoord;
+            FFDBox_line_1 >> YCoord;
+
+            CPcoord[0] = XCoord;
+            CPcoord[1] = cos(0.1) * YCoord;
+            CPcoord[2] = -sin(0.1) * YCoord;
+            FFDBox[iFFDBox]->SetCoordCornerPoints(coord, 4);
+
+            CPcoord[0] = XCoord;
+            CPcoord[1] = cos(0.1) * YCoord;
+            CPcoord[2] = sin(0.1) * YCoord;
+            FFDBox[iFFDBox]->SetCoordCornerPoints(coord, 7);
+
+            getline(mesh_file, text_line);
+            istringstream FFDBox_line_2(text_line);
+            FFDBox_line_2 >> XCoord;
+            FFDBox_line_2 >> YCoord;
+
+            CPcoord[0] = XCoord;
+            CPcoord[1] = cos(0.1) * YCoord;
+            CPcoord[2] = -sin(0.1) * YCoord;
+            FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, 0);
+
+            CPcoord[0] = XCoord;
+            CPcoord[1] = cos(0.1) * YCoord;
+            CPcoord[2] = sin(0.1) * YCoord;
+            FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, 3);
+
+            getline(mesh_file, text_line);
+            istringstream FFDBox_line_3(text_line);
+            FFDBox_line_3 >> XCoord;
+            FFDBox_line_3 >> YCoord;
+
+            CPcoord[0] = XCoord;
+            CPcoord[1] = cos(0.1) * YCoord;
+            CPcoord[2] = -sin(0.1) * YCoord;
+            FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, 1);
+
+            CPcoord[0] = XCoord;
+            CPcoord[1] = cos(0.1) * YCoord;
+            CPcoord[2] = sin(0.1) * YCoord;
+            FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, 2);
+
+            getline(mesh_file, text_line);
+            istringstream FFDBox_line_4(text_line);
+            FFDBox_line_4 >> XCoord;
+            FFDBox_line_4 >> YCoord;
+
+            CPcoord[0] = XCoord;
+            CPcoord[1] = cos(0.1) * YCoord;
+            CPcoord[2] = -sin(0.1) * YCoord;
+            FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, 5);
+
+            CPcoord[0] = XCoord;
+            CPcoord[1] = cos(0.1) * YCoord;
+            CPcoord[2] = sin(0.1) * YCoord;
+            FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, 6);
+
+          } else {
+            for (iCornerPoints = 0; iCornerPoints < nCornerPoints[iFFDBox]; iCornerPoints++) {
+              if (iCornerPoints < nCornerPoints[iFFDBox] / SU2_TYPE::Int(2)) {
+                getline(mesh_file, text_line);
+                istringstream FFDBox_line(text_line);
+                FFDBox_line >> CPcoord[0];
+                FFDBox_line >> CPcoord[1];
+                CPcoord[2] = -0.5;
+              } else {
+                CPcoord[0] =
+                    FFDBox[iFFDBox]->GetCoordCornerPoints(0, iCornerPoints - nCornerPoints[iFFDBox] / SU2_TYPE::Int(2));
+                CPcoord[1] =
+                    FFDBox[iFFDBox]->GetCoordCornerPoints(1, iCornerPoints - nCornerPoints[iFFDBox] / SU2_TYPE::Int(2));
+                CPcoord[2] = 0.5;
+              }
+              FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, iCornerPoints);
+            }
+          }
+
+        } else {
+          for (iCornerPoints = 0; iCornerPoints < nCornerPoints[iFFDBox]; iCornerPoints++) {
+            getline(mesh_file, text_line);
+            istringstream FFDBox_line(text_line);
+            FFDBox_line >> CPcoord[0];
+            FFDBox_line >> CPcoord[1];
+            FFDBox_line >> CPcoord[2];
+            FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, iCornerPoints);
+          }
+        }
+
+        /*--- Read the number of the control points. ---*/
+
+        getline(mesh_file, text_line);
+        text_line.erase(0, 19);
+        nControlPoints[iFFDBox] = atoi(text_line.c_str());
+
+        if (rank == MASTER_NODE) cout << "Control points: " << nControlPoints[iFFDBox] << ". ";
+
+        /*--- Method to identify if there is a FFDBox definition. ---*/
+
+        if (nControlPoints[iFFDBox] != 0) FFDBoxDefinition = true;
+
+        /*--- Read the coordinates of the control points. ---*/
+
+        for (iControlPoints = 0; iControlPoints < nControlPoints[iFFDBox]; iControlPoints++) {
+          getline(mesh_file, text_line);
+          istringstream FFDBox_line(text_line);
+          FFDBox_line >> iDegree;
+          FFDBox_line >> jDegree;
+          FFDBox_line >> kDegree;
+          FFDBox_line >> CPcoord[0];
+          FFDBox_line >> CPcoord[1];
+          FFDBox_line >> CPcoord[2];
+          FFDBox[iFFDBox]->SetCoordControlPoints(CPcoord, iDegree, jDegree, kDegree);
+          FFDBox[iFFDBox]->SetCoordControlPoints_Copy(CPcoord, iDegree, jDegree, kDegree);
+        }
+
+        getline(mesh_file, text_line);
+        text_line.erase(0, 19);
+        nSurfacePoints[iFFDBox] = atoi(text_line.c_str());
+
+        /*--- The surface points parametric coordinates (all the nodes read the FFD
+         * information but they only store their part). ---*/
+
+        my_nSurfPoints = 0;
+        for (iSurfacePoints = 0; iSurfacePoints < nSurfacePoints[iFFDBox]; iSurfacePoints++) {
+          getline(mesh_file, text_line);
+          istringstream FFDBox_line(text_line);
+          FFDBox_line >> iTag;
+          FFDBox_line >> iPoint;
+
+          if (config->GetMarker_All_TagBound(iTag) != -1) {
+            iMarker = config->GetMarker_All_TagBound(iTag);
+            FFDBox_line >> CPcoord[0];
+            FFDBox_line >> CPcoord[1];
+            FFDBox_line >> CPcoord[2];
+
+            for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
+              jPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+              if (iPoint == geometry->nodes->GetGlobalIndex(jPoint)) {
+                for (iDim = 0; iDim < nDim; iDim++) {
+                  coord[iDim] = geometry->nodes->GetCoord(jPoint, iDim);
+                }
+                FFDBox[iFFDBox]->Set_MarkerIndex(iMarker);
+                FFDBox[iFFDBox]->Set_VertexIndex(iVertex);
+                FFDBox[iFFDBox]->Set_PointIndex(jPoint);
+                FFDBox[iFFDBox]->Set_ParametricCoord(CPcoord);
+                FFDBox[iFFDBox]->Set_CartesianCoord(coord);
+                my_nSurfPoints++;
+              }
+            }
+          }
+        }
+
+        nSurfacePoints[iFFDBox] = my_nSurfPoints;
+
+#ifdef HAVE_MPI
+        nSurfPoints = 0;
+        SU2_MPI::Allreduce(&my_nSurfPoints, &nSurfPoints, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
+        if (rank == MASTER_NODE) cout << "Surface points: " << nSurfPoints << "." << endl;
+#else
+        nSurfPoints = my_nSurfPoints;
+        if (rank == MASTER_NODE) cout << "Surface points: " << nSurfPoints << "." << endl;
+#endif
+      }
+
+      delete[] nCornerPoints;
+      delete[] nControlPoints;
+      delete[] nSurfacePoints;
+    }
+  }
+  mesh_file.close();
+
+  if (nFFDBox == 0) {
+    if (rank == MASTER_NODE) cout << "There is no FFD box definition. Just in case, check the .su2 file" << endl;
+  }
 }

From bb19bd0346016fb2b3c6957e375e4233533bcb17 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Thu, 8 Dec 2022 20:43:38 -0800
Subject: [PATCH 064/656] Update SU2_DEF and SU2_DOT

---
 SU2_DEF/include/SU2_DEF.hpp |  9 ++--
 SU2_DEF/src/SU2_DEF.cpp     | 87 +++++++++++++++++++-----------------
 SU2_DOT/include/SU2_DOT.hpp | 10 ++---
 SU2_DOT/src/SU2_DOT.cpp     | 88 ++++++++++++++++++++-----------------
 4 files changed, 102 insertions(+), 92 deletions(-)

diff --git a/SU2_DEF/include/SU2_DEF.hpp b/SU2_DEF/include/SU2_DEF.hpp
index 4825094fae2..645e6e29768 100644
--- a/SU2_DEF/include/SU2_DEF.hpp
+++ b/SU2_DEF/include/SU2_DEF.hpp
@@ -1,7 +1,6 @@
 /*!
  * \file SU2_DEF.hpp
  * \brief Headers of the main subroutines of the code SU2_DEF.
- *        The subroutines and functions are in the <i>SU2_DEF.cpp</i> file.
  * \author F. Palacios, T. Economon
  * \version 7.3.1 "Blackbird"
  *
@@ -35,11 +34,11 @@
 #include "../../Common/include/CConfig.hpp"
 #undef ENABLE_MAPS
 
-#include "drivers/CDeformationDriver.hpp"
-
+#include <cmath>
 #include <cstdlib>
-#include <iostream>
 #include <iomanip>
-#include <cmath>
+#include <iostream>
+
+#include "drivers/CDeformationDriver.hpp"
 
 using namespace std;
diff --git a/SU2_DEF/src/SU2_DEF.cpp b/SU2_DEF/src/SU2_DEF.cpp
index 515bd8d6cfb..d15fce2e60e 100644
--- a/SU2_DEF/src/SU2_DEF.cpp
+++ b/SU2_DEF/src/SU2_DEF.cpp
@@ -29,47 +29,54 @@
 
 using namespace std;
 
-int main(int argc, char *argv[]) {
-    
-    char config_file_name[MAX_STRING_SIZE];
-    
-    /*--- Create a pointer to the main SU2_DEF Driver ---*/
-    
-    CDeformationDriver* driver = nullptr;
-    
-    /*--- MPI initialization ---*/
-    
+int main(int argc, char* argv[]) {
+
+  char config_file_name[MAX_STRING_SIZE];
+
+  /*--- Create a pointer to the main SU2_DEF Driver ---*/
+
+  CDeformationDriver* driver = nullptr;
+
+  /*--- MPI initialization ---*/
+
 #if defined(HAVE_OMP) && defined(HAVE_MPI)
-    int provided;
-    SU2_MPI::Init_thread(&argc, &argv, MPI_THREAD_FUNNELED, &provided);
+  int provided;
+  SU2_MPI::Init_thread(&argc, &argv, MPI_THREAD_FUNNELED, &provided);
 #else
-    SU2_MPI::Init(&argc, &argv);
+  SU2_MPI::Init(&argc, &argv);
 #endif
-    SU2_MPI::Comm comm = SU2_MPI::GetComm();
-    
-    /*--- Load in the number of zones and spatial dimensions in the mesh file
-     (if no config file is specified, default.cfg is used) ---*/
-    
-    if (argc == 2) { strcpy(config_file_name, argv[1]); }
-    else { strcpy(config_file_name, "default.cfg"); }
-    
-    /*--- Initialize the mesh deformation driver ---*/
-    
-    driver = new CDeformationDriver(config_file_name, comm);
-    
-    /*--- Launch the main external loop of the solver. ---*/
-    
-    driver->Run();
-    
-    /*--- Postprocess all the containers, close history file, exit SU2. ---*/
-    
-    driver->Postprocessing();
-    
-    delete driver;
-    
-    /*--- Finalize MPI parallelization ---*/
-    SU2_MPI::Finalize();
-    
-    return EXIT_SUCCESS;
-    
+  SU2_MPI::Comm comm = SU2_MPI::GetComm();
+
+  /*--- Load in the number of zones and spatial dimensions in the mesh file
+   (if no config file is specified, default.cfg is used). ---*/
+
+  if (argc == 2) {
+    strcpy(config_file_name, argv[1]);
+  } else {
+    strcpy(config_file_name, "default.cfg");
+  }
+
+  /*--- Initialize the mesh deformation driver. ---*/
+
+  driver = new CDeformationDriver(config_file_name, comm);
+
+  /*--- Preprocess the solver data. ---*/
+
+  driver->Preprocess();
+
+  /*--- Launch the main external loop of the solver. ---*/
+
+  driver->Run();
+
+  /*--- Postprocess all the containers, close history file, and exit SU2. ---*/
+
+  driver->Postprocessing();
+
+  delete driver;
+
+  /*--- Finalize MPI parallelization. ---*/
+
+  SU2_MPI::Finalize();
+
+  return EXIT_SUCCESS;
 }
diff --git a/SU2_DOT/include/SU2_DOT.hpp b/SU2_DOT/include/SU2_DOT.hpp
index d087a9eb1b2..cc201e1d50b 100644
--- a/SU2_DOT/include/SU2_DOT.hpp
+++ b/SU2_DOT/include/SU2_DOT.hpp
@@ -1,7 +1,6 @@
 /*!
  * \file SU2_DOT.hpp
  * \brief Headers of the main subroutines of the code SU2_DOT.
- *        The subroutines and functions are in the <i>SU2_DOT.cpp</i> file.
  * \author F. Palacios, T. Economon
  * \version 7.3.1 "Blackbird"
  *
@@ -32,14 +31,13 @@
 #include "../../Common/include/CConfig.hpp"
 #undef ENABLE_MAPS
 
-#include "../../Common/include/parallelization/mpi_structure.hpp"
-#include "../../Common/include/parallelization/omp_structure.hpp"
-
+#include <cmath>
 #include <cstdlib>
-#include <iostream>
 #include <iomanip>
-#include <cmath>
+#include <iostream>
 
+#include "../../Common/include/parallelization/mpi_structure.hpp"
+#include "../../Common/include/parallelization/omp_structure.hpp"
 #include "../../SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp"
 
 using namespace std;
diff --git a/SU2_DOT/src/SU2_DOT.cpp b/SU2_DOT/src/SU2_DOT.cpp
index cb362511793..4d01c6e4793 100644
--- a/SU2_DOT/src/SU2_DOT.cpp
+++ b/SU2_DOT/src/SU2_DOT.cpp
@@ -25,52 +25,58 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #include "../include/SU2_DOT.hpp"
 
 using namespace std;
 
-int main(int argc, char *argv[]) {
-    
-    char config_file_name[MAX_STRING_SIZE];
-    
-    /*--- Create a pointer to the main SU2_DEF Driver ---*/
-    
-    CDiscAdjDeformationDriver* driver = nullptr;
-    
-    /*--- MPI initialization ---*/
-    
+int main(int argc, char* argv[]) {
+
+  char config_file_name[MAX_STRING_SIZE];
+
+  /*--- Create a pointer to the main SU2_DEF Driver. ---*/
+
+  CDiscAdjDeformationDriver* driver = nullptr;
+
+  /*--- MPI initialization. ---*/
+
 #if defined(HAVE_OMP) && defined(HAVE_MPI)
-    int provided;
-    SU2_MPI::Init_thread(&argc, &argv, MPI_THREAD_FUNNELED, &provided);
+  int provided;
+  SU2_MPI::Init_thread(&argc, &argv, MPI_THREAD_FUNNELED, &provided);
 #else
-    SU2_MPI::Init(&argc, &argv);
+  SU2_MPI::Init(&argc, &argv);
 #endif
-    SU2_MPI::Comm comm = SU2_MPI::GetComm();
-    
-    /*--- Load in the number of zones and spatial dimensions in the mesh file
-     (if no config file is specified, default.cfg is used) ---*/
-    
-    if (argc == 2) { strcpy(config_file_name, argv[1]); }
-    else { strcpy(config_file_name, "default.cfg"); }
-    
-    /*--- Initialize the mesh deformation driver ---*/
-    
-    driver = new CDiscAdjDeformationDriver(config_file_name, comm);
-    
-    /*--- Launch the main external loop of the solver. ---*/
-    
-    driver->Run();
-    
-    /*--- Postprocess all the containers, close history file, exit SU2. ---*/
-    
-    driver->Postprocessing();
-    
-    delete driver;
-    
-    /*--- Finalize MPI parallelization ---*/
-    SU2_MPI::Finalize();
-    
-    return EXIT_SUCCESS;
-    
+  SU2_MPI::Comm comm = SU2_MPI::GetComm();
+
+  /*--- Load in the number of zones and spatial dimensions in the mesh file
+   (if no config file is specified, default.cfg is used). ---*/
+
+  if (argc == 2) {
+    strcpy(config_file_name, argv[1]);
+  } else {
+    strcpy(config_file_name, "default.cfg");
+  }
+
+  /*--- Initialize the mesh deformation driver. ---*/
+
+  driver = new CDiscAdjDeformationDriver(config_file_name, comm);
+
+  /*--- Preprocess the solver data. ---*/
+
+  driver->Preprocess();
+
+  /*--- Launch the main external loop of the solver. ---*/
+
+  driver->Run();
+
+  /*--- Postprocess all the containers, close history file, and exit SU2. ---*/
+
+  driver->Postprocessing();
+
+  delete driver;
+
+  /*--- Finalize MPI parallelization. ---*/
+
+  SU2_MPI::Finalize();
+
+  return EXIT_SUCCESS;
 }

From 7b545bc581df6c1f4390bb330fc432b0c23c8507 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Thu, 8 Dec 2022 21:01:41 -0800
Subject: [PATCH 065/656] Add vector<unsigned short> template for Python
 wrapper

---
 SU2_PY/pySU2/pySU2.i | 1 +
 1 file changed, 1 insertion(+)

diff --git a/SU2_PY/pySU2/pySU2.i b/SU2_PY/pySU2/pySU2.i
index 0aa3dddc212..56da2437af2 100644
--- a/SU2_PY/pySU2/pySU2.i
+++ b/SU2_PY/pySU2/pySU2.i
@@ -64,6 +64,7 @@ threads="1"
 
 namespace std {
    %template() vector<bool>;
+   %template() vector<unsigned short>;
    %template() vector<unsigned long>;
    %template() vector<vector<unsigned long>>;
    %template() vector<double>;

From 8d4974fd6907b9853ef37a116e90480bb4ae7e7b Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Thu, 8 Dec 2022 23:28:28 -0800
Subject: [PATCH 066/656] Fix compilation error caused by hdf5 static library

---
 externals/cgns/hdf5/meson.build | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/externals/cgns/hdf5/meson.build b/externals/cgns/hdf5/meson.build
index f85d5ba86d9..7b558a49c4e 100644
--- a/externals/cgns/hdf5/meson.build
+++ b/externals/cgns/hdf5/meson.build
@@ -25,7 +25,7 @@ hdf5_conf_data.set('version', '1.12.1')
 ext_deps = []
 
 
-opt_zlib = dependency('zlib', required: false, static: true)
+opt_zlib = dependency('zlib', required: false, static: false)
 opt_szip = dependency('szip', required: false, static: true)
 
 if opt_zlib.found() and cc.has_header('zlib.h')

From 23d03ca9b38a3cbae3f29f4f9259c08cf5bfc040 Mon Sep 17 00:00:00 2001
From: Harsh Patel <patelha57@gmail.com>
Date: Fri, 9 Dec 2022 16:06:52 -0800
Subject: [PATCH 067/656] Update submodule versions

---
 externals/meson | 2 +-
 externals/opdi  | 2 +-
 2 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/externals/meson b/externals/meson
index 29ef4478df6..41c650a040d 160000
--- a/externals/meson
+++ b/externals/meson
@@ -1 +1 @@
-Subproject commit 29ef4478df6d3aaca40c7993f125b29409be1de2
+Subproject commit 41c650a040d50e0912d268af7a903a9ce1456dfa
diff --git a/externals/opdi b/externals/opdi
index e56f79cada2..1aabf5bd1ed 160000
--- a/externals/opdi
+++ b/externals/opdi
@@ -1 +1 @@
-Subproject commit e56f79cada202d21e7425f5d5cfd5b1153f2465e
+Subproject commit 1aabf5bd1ed77611742eb655002f2ac7a3dddef9

From df160c0f3345092830ca3936275c89a07b9d73ca Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Sat, 10 Dec 2022 11:48:23 -0800
Subject: [PATCH 068/656] Update CoDiPack submodule version

---
 externals/codi | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/externals/codi b/externals/codi
index 6a67202a388..96ac78ec5bc 160000
--- a/externals/codi
+++ b/externals/codi
@@ -1 +1 @@
-Subproject commit 6a67202a3887c8da490fdfde82bc46507de68692
+Subproject commit 96ac78ec5bcc5ac25b785e79b16ed76fca22d736

From 3a8ddae427e038e0e71d22dc49e5fc02ad262ee7 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Sat, 10 Dec 2022 15:40:14 -0800
Subject: [PATCH 069/656] Apply clang format to CDriver.hpp

---
 SU2_CFD/include/drivers/CDriver.hpp | 1567 +++++++++++++--------------
 1 file changed, 778 insertions(+), 789 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index aeb1467980b..50366afd833 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -28,14 +28,12 @@
 
 #pragma once
 
+#include "../../../Common/include/drivers/CDriverBase.hpp"
+#include "../../../Common/include/geometry/CGeometry.hpp"
 #include "../../../Common/include/parallelization/mpi_structure.hpp"
-
 #include "../integration/CIntegration.hpp"
-#include "../solvers/CSolver.hpp"
 #include "../interfaces/CInterface.hpp"
-
-#include "../../../Common/include/geometry/CGeometry.hpp"
-#include "../../../Common/include/drivers/CDriverBase.hpp"
+#include "../solvers/CSolver.hpp"
 
 using namespace std;
 
@@ -52,627 +50,633 @@ class COutput;
  */
 
 class CDriver : public CDriverBase {
-    
-protected:
-    
-    char runtime_file_name[MAX_STRING_SIZE];
-    su2double UsedTimeOutput;                     /*!< \brief Elapsed time between Start and Stop point of the timer for tracking output phase.*/
-    
-    su2double BandwidthSum = 0.0;                 /*!< \brief Aggregate value of the bandwidth for writing restarts (to be average later).*/
-    unsigned long IterCount,                       /*!< \brief Iteration count stored for performance benchmarking.*/
-    OutputCount;                                  /*!< \brief Output count stored for performance benchmarking.*/
-    unsigned long DOFsPerPoint;                    /*!< \brief Number of unknowns at each vertex, i.e., number of equations solved. */
-    su2double Mpoints;                            /*!< \brief Total number of grid points in millions in the calculation (including ghost points).*/
-    su2double MpointsDomain;                      /*!< \brief Total number of grid points in millions in the calculation (excluding ghost points).*/
-    su2double MDOFs;                              /*!< \brief Total number of DOFs in millions in the calculation (including ghost points).*/
-    su2double MDOFsDomain;                        /*!< \brief Total number of DOFs in millions in the calculation (excluding ghost points).*/
-    
-    ofstream **ConvHist_file;                     /*!< \brief Convergence history file.*/
-    ofstream FSIHist_file;                        /*!< \brief FSI convergence history file.*/
-    
-    bool StopCalc,                                /*!< \brief Stop computation flag.*/
-    mixingplane,                                  /*!< \brief mixing-plane simulation flag.*/
-    fsi,                                          /*!< \brief FSI simulation flag.*/
-    fem_solver;                                   /*!< \brief FEM fluid solver simulation flag. */
-    
-    CIteration ***iteration_container;            /*!< \brief Container vector with all the iteration methods. */
-    CIntegration ****integration_container;       /*!< \brief Container vector with all the integration methods. */
-    vector<vector<unique_ptr<CInterpolator> > >
-    interpolator_container;                       /*!< \brief Definition of the interpolation method between non-matching discretizations of the interface. */
-    CInterface ***interface_container;            /*!< \brief Definition of the interface of information and physics. */
-    bool dry_run;                                 /*!< \brief Flag if SU2_CFD was started as dry-run via "SU2_CFD -d <config>.cfg" */
-    
-public:
-    
-    /*!
-     * \brief Constructor of the class.
-     * \param[in] confFile - Configuration file name.
-     * \param[in] val_nZone - Total number of zones.
-     * \param[in] val_nDim - Number of dimensions.
-     * \param[in] MPICommunicator - MPI communicator for SU2.
-     */
-    CDriver(char* confFile,
-            unsigned short val_nZone,
-            SU2_Comm MPICommunicator, bool dummy_geo);
-    
-    /*!
-     * \brief Destructor of the class.
-     */
-    virtual ~CDriver(void);
-    
-    /*!
-     * \brief A virtual member.
-     */
-    virtual void Run() { };
-    
-protected:
-    
-    /*!
-     * \brief Init_Containers
-     */
-    void SetContainers_Null();
-    
-    /*!
-     * \brief Read in the config and mesh files.
-     */
-    void Input_Preprocessing(CConfig **&config, CConfig *&driver_config);
-    
-    /*!
-     * \brief Construction of the edge-based data structure and the multigrid structure.
-     */
-    void Geometrical_Preprocessing(CConfig *config, CGeometry **&geometry, bool dummy);
-    
-    /*!
-     * \brief Do the geometrical preprocessing for the DG FEM solver.
-     */
-    void Geometrical_Preprocessing_DGFEM(CConfig *config, CGeometry **&geometry);
-    
-    /*!
-     * \brief Geometrical_Preprocessing_FVM
-     */
-    void Geometrical_Preprocessing_FVM(CConfig *config, CGeometry **&geometry);
-    
-    /*!
-     * \brief Definition of the physics iteration class or within a single zone.
-     * \param[in] iteration_container - Pointer to the iteration container to be instantiated.
-     * \param[in] config - Definition of the particular problem.
-     * \param[in] iZone - Index of the zone.
-     */
-    void Iteration_Preprocessing(CConfig *config, CIteration *&iteration) const;
-    
-    /*!
-     * \brief Definition and allocation of all solution classes.
-     * \param[in] solver_container - Container vector with all the solutions.
-     * \param[in] geometry - Geometrical definition of the problem.
-     * \param[in] config - Definition of the particular problem.
-     */
-    void Solver_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***&solver);
-    
-    /*!
-     * \brief Restart of the solvers from the restart files.
-     * \param[in] solver_container - Container vector with all the solutions.
-     * \param[in] geometry - Geometrical definition of the problem.
-     * \param[in] config - Definition of the particular problem.
-     */
-    void Solver_Restart(CSolver ***solver, CGeometry **geometry, CConfig *config, bool update_geo);
-    
-    /*!
-     * \brief Definition and allocation of all solution classes.
-     * \param[in] solver_container - Container vector with all the solutions.
-     * \param[in] geometry - Geometrical definition of the problem.
-     * \param[in] config - Definition of the particular problem.
-     */
-    void Solver_Postprocessing(CSolver ****solver, CGeometry **geometry, CConfig *config, unsigned short val_iInst);
-    
-    /*!
-     * \brief Definition and allocation of all integration classes.
-     * \param[in] config - Definition of the particular problem.
-     * \param[in] solver - Container vector with all the solutions.
-     * \param[out] integration - Container vector with all the integration methods.
-     */
-    void Integration_Preprocessing(CConfig *config, CSolver **solver, CIntegration **&integration) const;
-    
-    /*!
-     * \brief Definition and allocation of all integration classes.
-     * \param[in] integration_container - Container vector with all the integration methods.
-     * \param[in] geometry - Geometrical definition of the problem.
-     * \param[in] config - Definition of the particular problem.
-     */
-    void Integration_Postprocessing(CIntegration ***integration, CGeometry **geometry, CConfig *config, unsigned short val_iInst);
-    
-    /*!
-     * \brief Definition and allocation of all interface classes.
-     */
-    void Interface_Preprocessing(CConfig **config, CSolver *****solver, CGeometry ****geometry,
-                                 unsigned short **interface_types, CInterface ***interface,
-                                 vector<vector<unique_ptr<CInterpolator> > > &interpolation);
-    
-    /*!
-     * \brief Definition and allocation of all solver classes.
-     * \param[in] numerics_container - Description of the numerical method (the way in which the equations are solved).
-     * \param[in] geometry - Geometrical definition of the problem.
-     * \param[in] solver_container - Container vector with all the solutions.
-     * \param[in] config - Definition of the particular problem.
-     */
-    void Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***solver, CNumerics ****&numerics) const;
-    
-    /*!
-     * \brief Helper to instantiate turbulence numerics specialized for different flow solvers.
-     */
-    template <class FlowIndices>
-    void InstantiateTurbulentNumerics(unsigned short nVar_Turb, int offset, const CConfig *config,
-                                      const CSolver* turb_solver, CNumerics ****&numerics) const;
-
-    /*!
-     * \brief Helper to instantiate transition numerics specialized for different flow solvers.
-     */
-    template <class FlowIndices>
-    void InstantiateTransitionNumerics(unsigned short nVar_Trans, int offset, const CConfig *config,
-                                      const CSolver* trans_solver, CNumerics ****&numerics) const;
-    /*!
-     * \brief Helper to instantiate species transport numerics specialized for different flow solvers.
-     */
-    template <class FlowIndices>
-    void InstantiateSpeciesNumerics(unsigned short nVar_Species, int offset, const CConfig *config,
-                                    const CSolver* species_solver, CNumerics ****&numerics) const;
-    
-    /*!
-     * \brief Definition and allocation of all solver classes.
-     * \param[in] numerics_container - Description of the numerical method (the way in which the equations are solved).
-     * \param[in] solver_container - Container vector with all the solutions.
-     * \param[in] geometry - Geometrical definition of the problem.
-     * \param[in] config - Definition of the particular problem.
-     */
-    void Numerics_Postprocessing(CNumerics *****numerics, CSolver ***solver, CGeometry **geometry, CConfig *config, unsigned short val_iInst);
-    
-    /*!
-     * \brief GridMovement_Preprocessing
-     * \param config
-     * \param geometry
-     * \param solver
-     * \param iteration
-     * \param grid_movement
-     * \param surface_movement
-     */
-    void DynamicMesh_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***solver, CIteration *iteration, CVolumetricMovement *&grid_movement, CSurfaceMovement *&surface_movement) const;
-    
-    /*!
-     * \brief Initialize Python interface functionalities
-     */
-    void PythonInterface_Preprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver);
-    
-    /*!
-     * \brief Preprocess the output container.
-     */
-    void Output_Preprocessing(CConfig **config, CConfig *driver_config, COutput **&output_container, COutput *&driver_output);
-    
-    /*!
-     * \brief Initiate value for static mesh movement such as the gridVel for the ROTATING frame.
-     */
-    void StaticMesh_Preprocessing(const CConfig *config, CGeometry **geometry);
-    
-    /*!
-     * \brief Initiate value for static mesh movement such as the gridVel for the ROTATING frame.
-     */
-    void Turbomachinery_Preprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver,
-                                      CInterface*** interface);
-    
-    /*!
-     * \brief A virtual member.
-     * \param[in] donorZone - zone in which the displacements will be predicted.
-     * \param[in] targetZone - zone which receives the predicted displacements.
-     */
-    virtual void Predict_Displacements(unsigned short donorZone, unsigned short targetZone) {}
-    
-    /*!
-     * \brief A virtual member.
-     * \param[in] donorZone - zone in which the tractions will be predicted.
-     * \param[in] targetZone - zone which receives the predicted traction.
-     */
-    virtual void Predict_Tractions(unsigned short donorZone, unsigned short targetZone) {}
-    
-    /*!
-     * \brief A virtual member.
-     * \param[in] donorZone - zone in which the displacements will be transferred.
-     * \param[in] targetZone - zone which receives the tractions transferred.
-     */
-    virtual void Transfer_Displacements(unsigned short donorZone, unsigned short targetZone) {}
-    
-    /*!
-     * \brief A virtual member.
-     * \param[in] donorZone - zone from which the tractions will be transferred.
-     * \param[in] targetZone - zone which receives the tractions transferred.
-     */
-    virtual void Transfer_Tractions(unsigned short donorZone, unsigned short targetZone) {}
-    
-    /*!
-     * \brief A virtual member.
-     * \param[in] donorZone - origin of the information.
-     * \param[in] targetZone - destination of the information.
-     * \param[in] iOuterIter - Fluid-Structure Interaction subiteration.
-     */
-    virtual void Relaxation_Displacements(unsigned short donorZone, unsigned short targetZone, unsigned long iOuterIter) {}
-    
-    /*!
-     * \brief A virtual member.
-     * \param[in] donorZone - origin of the information.
-     * \param[in] targetZone - destination of the information.
-     * \param[in] iOuterIter - Fluid-Structure Interaction subiteration.
-     */
-    virtual void Relaxation_Tractions(unsigned short donorZone, unsigned short targetZone, unsigned long iOuterIter) {}
-    
-    /*!
-     * \brief A virtual member to run a Block Gauss-Seidel iteration in multizone problems.
-     */
-    virtual void Run_GaussSeidel(){}
-    
-    /*!
-     * \brief A virtual member to run a Block-Jacobi iteration in multizone problems.
-     */
-    virtual void Run_Jacobi(){}
-    
-    /*!
-     * \brief A virtual member.
-     */
-    virtual void Update() {}
-    
-    /*!
-     * \brief Print out the direct residuals.
-     * \param[in] kind_recording - Type of recording (full list in ENUM_RECORDING, option_structure.hpp)
-     */
-    void Print_DirectResidual(RECORDING kind_recording);
-    
-public:
-    
-    /*!
-     * \brief Launch the computation for all zones and all physics.
-     */
-    virtual void StartSolver() {}
-    
-    /*!
-     * \brief Deallocation routine
-     */
-    void Postprocessing();
-    
-    /*!
-     * \brief A virtual member.
-     */
-    virtual void ResetConvergence();
-    
-    /*!
-     * \brief Perform some pre-processing before an iteration of the physics.
-     */
-    virtual void Preprocess(unsigned long TimeIter){ }
-    
-    /*!
-     * \brief Monitor the computation.
-     */
-    virtual bool Monitor(unsigned long TimeIter){ return false; }
-    
-    /*!
-     * \brief Output the solution in solution file.
-     */
-    virtual void Output(unsigned long TimeIter){ }
-    
-    /*!
-     * \brief Perform a dynamic mesh deformation, including grid velocity computation and update of the multigrid structure.
-     */
-    virtual void DynamicMeshUpdate(unsigned long TimeIter) { }
-    
-    /*!
-     * \brief Perform a dynamic mesh deformation, including grid velocity computation and update of the multigrid structure.
-     */
-    virtual void DynamicMeshUpdate(unsigned short val_iZone, unsigned long TimeIter) { }
-    
-    /*!
-     * \brief Perform a mesh deformation as initial condition.
-     */
-    virtual void SetInitialMesh() { }
-    
-    /*!
-     * \brief Process the boundary conditions and update the multigrid structure.
-     */
-    void BoundaryConditionsUpdate();
-    
-    /*!
-     * \brief Get the total drag.
-     * \return Total drag.
-     */
-    passivedouble Get_Drag() const;
-    
-    /*!
-     * \brief Get the total lift.
-     * \return Total lift.
-     */
-    passivedouble Get_Lift() const;
-    
-    /*!
-     * \brief Get the total x moment.
-     * \return Total x moment.
-     */
-    passivedouble Get_Mx() const;
-    
-    /*!
-     * \brief Get the total y moment.
-     * \return Total y moment.
-     */
-    passivedouble Get_My() const;
-    
-    /*!
-     * \brief Get the total z moment.
-     * \return Total z moment.
-     */
-    passivedouble Get_Mz() const;
-    
-    /*!
-     * \brief Get the total drag coefficient.
-     * \return Total drag coefficient.
-     */
-    passivedouble Get_DragCoeff() const;
-    
-    /*!
-     * \brief Get the total lift coefficient.
-     * \return Total lift coefficient.
-     */
-    passivedouble Get_LiftCoeff() const;
-    
-    /*!
-     * \brief Get the number of external iterations.
-     * \return Number of external iterations.
-     */
-    unsigned long GetnTimeIter() const;
-    
-    /*!
-     * \brief Get the current external iteration.
-     * \return Current external iteration.
-     */
-    unsigned long GetTime_Iter() const;
-    
-    /*!
-     * \brief Get the unsteady time step.
-     * \return Unsteady time step.
-     */
-    passivedouble GetUnsteady_TimeStep() const;
-    
-    /*!
-     * \brief Get the name of the output file for the surface.
-     * \return File name for the surface output.
-     */
-    string GetSurfaceFileName() const;
-    
-    /*!
-     * \brief Get the temperature at a vertex on a specified marker.
-     * \param[in] iMarker - Marker identifier.
-     * \param[in] iVertex - Vertex identifier.
-     * \return Temperature of the vertex.
-     */
-    passivedouble GetVertexTemperature(unsigned short iMarker, unsigned long iVertex) const;
-    
-    /*!
-     * \brief Set the temperature of a vertex on a specified marker.
-     * \param[in] iMarker - Marker identifier.
-     * \param[in] iVertex - Vertex identifier.
-     * \param[in] val_WallTemp - Value of the temperature.
-     */
-    void SetVertexTemperature(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallTemp);
-    
-    /*!
-     * \brief Get the heat flux at a vertex on a specified marker (3 components).
-     * \param[in] iMarker - Marker identifier.
-     * \param[in] iVertex - Vertex identifier.
-     * \return True if the vertex is a halo node.
-     */
-    vector<passivedouble> GetVertexHeatFluxes(unsigned short iMarker, unsigned long iVertex) const;
-    
-    /*!
-     * \brief Get the wall normal component of the heat flux at a vertex on a specified marker.
-     * \param[in] iMarker - Marker identifier.
-     * \param[in] iVertex - Vertex identifier.
-     * \return Wall normal component of the heat flux at the vertex.
-     */
-    passivedouble GetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex) const;
-    
-    /*!
-     * \brief Set the wall normal component of the heat flux at a vertex on a specified marker.
-     * \param[in] iMarker - Marker identifier.
-     * \param[in] iVertex - Vertex identifier.
-     * \param[in] val_WallHeatFlux - Value of the normal heat flux.
-     */
-    void SetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallHeatFlux);
-    
-    /*!
-     * \brief Get the thermal conductivity at a vertex on a specified marker.
-     * \param[in] iMarker - Marker identifier.
-     * \param[in] iVertex - Vertex identifier.
-     * \return Thermal conductivity at the vertex.
-     */
-    passivedouble GetThermalConductivity(unsigned short iMarker, unsigned long iVertex) const;
-    
-    /*!
-     * \brief Preprocess the inlets via file input for all solvers.
-     * \param[in] solver_container - Container vector with all the solutions.
-     * \param[in] geometry - Geometrical definition of the problem.
-     * \param[in] config - Definition of the particular problem.
-     */
-    void Inlet_Preprocessing(CSolver ***solver, CGeometry **geometry, CConfig *config) const;
-    
-    /*!
-     * \brief Get all the CHT boundary marker tags.
-     * \return List of CHT boundary markers tags.
-     */
-    vector<string> GetCHTMarkerTags() const;
-    
-    /*!
-     * \brief Get all the inlet boundary marker tags.
-     * \return List of inlet boundary markers tags.
-     */
-    vector<string> GetInletMarkerTags() const;
-    
-    /*!
-     * \brief Return the sensitivities of the mesh boundary vertices.
-     * \param[in] iMarker - Marker identifier.
-     * \param[in] iVertex - Vertex identifier.
-     * \return Vector of sensitivities.
-     */
-    vector<passivedouble> GetMeshDisp_Sensitivity(unsigned short iMarker, unsigned long iVertex) const;
-    
-    /*!
-     * \brief Set the load in X direction for the structural solver.
-     * \param[in] iMarker - Marker identifier.
-     * \param[in] iVertex - Vertex identifier.
-     * \param[in] LoadX - Value of the load in the direction X.
-     * \param[in] LoadX - Value of the load in the direction Y.
-     * \param[in] LoadX - Value of the load in the direction Z.
-     */
-    void SetFEA_Loads(unsigned short iMarker, unsigned long iVertex, passivedouble LoadX, passivedouble LoadY, passivedouble LoadZ);
-    
-    /*!
-     * \brief Return the displacements from the FEA solver.
-     * \param[in] iMarker - Marker identifier.
-     * \param[in] iVertex - Vertex identifier.
-     * \return Vector of displacements.
-     */
-    vector<passivedouble> GetFEA_Displacements(unsigned short iMarker, unsigned long iVertex) const;
-    
-    /*!
-     * \brief Return the velocities from the FEA Solver.
-     * \param[in] iMarker - Marker identifier.
-     * \param[in] iVertex - Vertex identifier.
-     * \return Vector of velocities.
-     */
-    vector<passivedouble> GetFEA_Velocity(unsigned short iMarker, unsigned long iVertex) const;
-    
-    /*!
-     * \brief Return the velocities from the FEA Solver.
-     * \param[in] iMarker - Marker identifier.
-     * \param[in] iVertex - Vertex identifier.
-     * \return Vector of velocities at time n.
-     */
-    vector<passivedouble> GetFEA_Velocity_n(unsigned short iMarker, unsigned long iVertex) const;
-    
-    /*!
-     * \brief Get the sensitivity of the flow loads for the structural solver.
-     * \param[in] iMarker - Marker identifier.
-     * \param[in] iVertex - Vertex identifier.
-     * \param[in] LoadX - Value of the load in the direction X.
-     * \param[in] LoadX - Value of the load in the direction Y.
-     * \param[in] LoadX - Value of the load in the direction Z.
-     */
-    vector<passivedouble> GetFlowLoad_Sensitivity(unsigned short iMarker, unsigned long iVertex) const;
-    
-    /*!
-     * \brief Get the flow load (from the extra step - the repeated methods should be unified once the postprocessing
-     * strategy is in place).
-     * \param[in] iMarker - Marker identifier.
-     * \param[in] iVertex - Vertex identifier.
-     */
-    vector<passivedouble> GetFlowLoad(unsigned short iMarker, unsigned long iVertex) const;
-    
-    /*!
-     * \brief Set the adjoint of the flow tractions (from the extra step -
-     * the repeated methods should be unified once the postprocessing strategy is in place).
-     * \param[in] iMarker - Marker identifier.
-     * \param[in] iVertex - Vertex identifier.
-     * \param[in] val_AdjointX - Value of the adjoint in the direction X.
-     * \param[in] val_AdjointY - Value of the adjoint in the direction Y.
-     * \param[in] val_AdjointZ - Value of the adjoint in the direction Z.
-     */
-    void SetFlowLoad_Adjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
-                             passivedouble val_AdjointY, passivedouble val_AdjointZ);
-    
-    /*!
-     * \brief Set the adjoint of the structural displacements (from an outside source)
-     * \param[in] iMarker - Marker identifier.
-     * \param[in] iVertex - Vertex identifier.
-     * \param[in] val_AdjointX - Value of the adjoint in the direction X.
-     * \param[in] val_AdjointY - Value of the adjoint in the direction Y.
-     * \param[in] val_AdjointZ - Value of the adjoint in the direction Z.
-     */
-    void SetSourceTerm_DispAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
-                                   passivedouble val_AdjointY, passivedouble val_AdjointZ);
-    void SetSourceTerm_VelAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
-                                  passivedouble val_AdjointY, passivedouble val_AdjointZ);
-    
-    /*!
-     * \brief Set the position of the heat source.
-     * \param[in] alpha - Angle of rotation respect to Z axis.
-     * \param[in] pos_x - Position X.
-     * \param[in] pos_y - Position Y.
-     * \param[in] pos_z - Position Z.
-     */
-    void SetHeatSource_Position(passivedouble alpha, passivedouble pos_x, passivedouble pos_y, passivedouble pos_z);
-    
-    /*!
-     * \brief Set the direction of the inlet.
-     * \param[in] iMarker - Marker index.
-     * \param[in] alpha - Angle (Zpos).
-     */
-    void SetInlet_Angle(unsigned short iMarker, passivedouble alpha);
-    
-    /*!
-     * \brief Sum the number of primal or adjoint variables for all solvers in a given zone.
-     * \param[in] iZone - Index of the zone.
-     * \param[in] adjoint - True to consider adjoint solvers instead of primal.
-     * \return Total number of solution variables.
-     */
-    unsigned short GetTotalNumberOfVariables(unsigned short iZone, bool adjoint) const {
-        unsigned short nVar = 0;
-        for (auto iSol = 0u; iSol < MAX_SOLS; iSol++) {
-            auto solver = solver_container[iZone][INST_0][MESH_0][iSol];
-            if (solver && (solver->GetAdjoint() == adjoint)) nVar += solver->GetnVar();
-        }
-        return nVar;
-    }
-    
-    /*!
-     * \brief Set the solution of all solvers (adjoint or primal) in a zone.
-     * \param[in] iZone - Index of the zone.
-     * \param[in] adjoint - True to consider adjoint solvers instead of primal.
-     * \param[in] solution - Solution object with interface (iPoint,iVar).
-     * \tparam Old - If true set "old solutions" instead.
-     */
-    template<class Container, bool Old = false>
-    void SetAllSolutions(unsigned short iZone, bool adjoint, const Container& solution) {
-        const auto nPoint = geometry_container[iZone][INST_0][MESH_0]->GetnPoint();
-        for (auto iSol = 0u, offset = 0u; iSol < MAX_SOLS; ++iSol) {
-            auto solver = solver_container[iZone][INST_0][MESH_0][iSol];
-            if (!(solver && (solver->GetAdjoint() == adjoint))) continue;
-            for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint)
-                for (auto iVar = 0ul; iVar < solver->GetnVar(); ++iVar)
-                    if (!Old) solver->GetNodes()->SetSolution(iPoint, iVar, solution(iPoint,offset+iVar));
-                    else solver->GetNodes()->SetSolution_Old(iPoint, iVar, solution(iPoint,offset+iVar));
-            offset += solver->GetnVar();
-        }
+ protected:
+  char runtime_file_name[MAX_STRING_SIZE];
+  su2double
+      UsedTimeOutput; /*!< \brief Elapsed time between Start and Stop point of the timer for tracking output phase.*/
+
+  su2double BandwidthSum =
+      0.0;                    /*!< \brief Aggregate value of the bandwidth for writing restarts (to be average later).*/
+  unsigned long IterCount,    /*!< \brief Iteration count stored for performance benchmarking.*/
+      OutputCount;            /*!< \brief Output count stored for performance benchmarking.*/
+  unsigned long DOFsPerPoint; /*!< \brief Number of unknowns at each vertex, i.e., number of equations solved. */
+  su2double Mpoints; /*!< \brief Total number of grid points in millions in the calculation (including ghost points).*/
+  su2double
+      MpointsDomain; /*!< \brief Total number of grid points in millions in the calculation (excluding ghost points).*/
+  su2double MDOFs;   /*!< \brief Total number of DOFs in millions in the calculation (including ghost points).*/
+  su2double MDOFsDomain; /*!< \brief Total number of DOFs in millions in the calculation (excluding ghost points).*/
+
+  ofstream** ConvHist_file; /*!< \brief Convergence history file.*/
+  ofstream FSIHist_file;    /*!< \brief FSI convergence history file.*/
+
+  bool StopCalc,   /*!< \brief Stop computation flag.*/
+      mixingplane, /*!< \brief mixing-plane simulation flag.*/
+      fsi,         /*!< \brief FSI simulation flag.*/
+      fem_solver;  /*!< \brief FEM fluid solver simulation flag. */
+
+  CIteration*** iteration_container;      /*!< \brief Container vector with all the iteration methods. */
+  CIntegration**** integration_container; /*!< \brief Container vector with all the integration methods. */
+  vector<vector<unique_ptr<CInterpolator>>>
+      interpolator_container; /*!< \brief Definition of the interpolation method between non-matching discretizations of
+                                 the interface. */
+  CInterface*** interface_container; /*!< \brief Definition of the interface of information and physics. */
+  bool dry_run;                      /*!< \brief Flag if SU2_CFD was started as dry-run via "SU2_CFD -d <config>.cfg" */
+
+ public:
+  /*!
+   * \brief Constructor of the class.
+   * \param[in] confFile - Configuration file name.
+   * \param[in] val_nZone - Total number of zones.
+   * \param[in] val_nDim - Number of dimensions.
+   * \param[in] MPICommunicator - MPI communicator for SU2.
+   */
+  CDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator, bool dummy_geo);
+
+  /*!
+   * \brief Destructor of the class.
+   */
+  virtual ~CDriver(void);
+
+  /*!
+   * \brief A virtual member.
+   */
+  virtual void Run(){};
+
+ protected:
+  /*!
+   * \brief Init_Containers
+   */
+  void SetContainers_Null();
+
+  /*!
+   * \brief Read in the config and mesh files.
+   */
+  void Input_Preprocessing(CConfig**& config, CConfig*& driver_config);
+
+  /*!
+   * \brief Construction of the edge-based data structure and the multi-grid structure.
+   */
+  void Geometrical_Preprocessing(CConfig* config, CGeometry**& geometry, bool dummy);
+
+  /*!
+   * \brief Do the geometrical preprocessing for the DG FEM solver.
+   */
+  void Geometrical_Preprocessing_DGFEM(CConfig* config, CGeometry**& geometry);
+
+  /*!
+   * \brief Geometrical_Preprocessing_FVM
+   */
+  void Geometrical_Preprocessing_FVM(CConfig* config, CGeometry**& geometry);
+
+  /*!
+   * \brief Definition of the physics iteration class or within a single zone.
+   * \param[in] iteration_container - Pointer to the iteration container to be instantiated.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] iZone - Index of the zone.
+   */
+  void Iteration_Preprocessing(CConfig* config, CIteration*& iteration) const;
+
+  /*!
+   * \brief Definition and allocation of all solution classes.
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void Solver_Preprocessing(CConfig* config, CGeometry** geometry, CSolver***& solver);
+
+  /*!
+   * \brief Restart of the solvers from the restart files.
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void Solver_Restart(CSolver*** solver, CGeometry** geometry, CConfig* config, bool update_geo);
+
+  /*!
+   * \brief Definition and allocation of all solution classes.
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void Solver_Postprocessing(CSolver**** solver, CGeometry** geometry, CConfig* config, unsigned short val_iInst);
+
+  /*!
+   * \brief Definition and allocation of all integration classes.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] solver - Container vector with all the solutions.
+   * \param[out] integration - Container vector with all the integration methods.
+   */
+  void Integration_Preprocessing(CConfig* config, CSolver** solver, CIntegration**& integration) const;
+
+  /*!
+   * \brief Definition and allocation of all integration classes.
+   * \param[in] integration_container - Container vector with all the integration methods.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void Integration_Postprocessing(CIntegration*** integration, CGeometry** geometry, CConfig* config,
+                                  unsigned short val_iInst);
+
+  /*!
+   * \brief Definition and allocation of all interface classes.
+   */
+  void Interface_Preprocessing(CConfig** config, CSolver***** solver, CGeometry**** geometry,
+                               unsigned short** interface_types, CInterface*** interface,
+                               vector<vector<unique_ptr<CInterpolator>>>& interpolation);
+
+  /*!
+   * \brief Definition and allocation of all solver classes.
+   * \param[in] numerics_container - Description of the numerical method (the way in which the equations are solved).
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void Numerics_Preprocessing(CConfig* config, CGeometry** geometry, CSolver*** solver, CNumerics****& numerics) const;
+
+  /*!
+   * \brief Helper to instantiate turbulence numerics specialized for different flow solvers.
+   */
+  template <class FlowIndices>
+  void InstantiateTurbulentNumerics(unsigned short nVar_Turb, int offset, const CConfig* config,
+                                    const CSolver* turb_solver, CNumerics****& numerics) const;
+
+  /*!
+   * \brief Helper to instantiate transition numerics specialized for different flow solvers.
+   */
+  template <class FlowIndices>
+  void InstantiateTransitionNumerics(unsigned short nVar_Trans, int offset, const CConfig* config,
+                                     const CSolver* trans_solver, CNumerics****& numerics) const;
+  /*!
+   * \brief Helper to instantiate species transport numerics specialized for different flow solvers.
+   */
+  template <class FlowIndices>
+  void InstantiateSpeciesNumerics(unsigned short nVar_Species, int offset, const CConfig* config,
+                                  const CSolver* species_solver, CNumerics****& numerics) const;
+
+  /*!
+   * \brief Definition and allocation of all solver classes.
+   * \param[in] numerics_container - Description of the numerical method (the way in which the equations are solved).
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void Numerics_Postprocessing(CNumerics***** numerics, CSolver*** solver, CGeometry** geometry, CConfig* config,
+                               unsigned short val_iInst);
+
+  /*!
+   * \brief GridMovement_Preprocessing
+   * \param config
+   * \param geometry
+   * \param solver
+   * \param iteration
+   * \param grid_movement
+   * \param surface_movement
+   */
+  void DynamicMesh_Preprocessing(CConfig* config, CGeometry** geometry, CSolver*** solver, CIteration* iteration,
+                                 CVolumetricMovement*& grid_movement, CSurfaceMovement*& surface_movement) const;
+
+  /*!
+   * \brief Initialize Python interface functionalities
+   */
+  void PythonInterface_Preprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver);
+
+  /*!
+   * \brief Preprocess the output container.
+   */
+  void Output_Preprocessing(CConfig** config, CConfig* driver_config, COutput**& output_container,
+                            COutput*& driver_output);
+
+  /*!
+   * \brief Initiate value for static mesh movement such as the gridVel for the ROTATING frame.
+   */
+  void StaticMesh_Preprocessing(const CConfig* config, CGeometry** geometry);
+
+  /*!
+   * \brief Initiate value for static mesh movement such as the gridVel for the ROTATING frame.
+   */
+  void Turbomachinery_Preprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver,
+                                    CInterface*** interface);
+
+  /*!
+   * \brief A virtual member.
+   * \param[in] donorZone - zone in which the displacements will be predicted.
+   * \param[in] targetZone - zone which receives the predicted displacements.
+   */
+  virtual void Predict_Displacements(unsigned short donorZone, unsigned short targetZone) {}
+
+  /*!
+   * \brief A virtual member.
+   * \param[in] donorZone - zone in which the tractions will be predicted.
+   * \param[in] targetZone - zone which receives the predicted traction.
+   */
+  virtual void Predict_Tractions(unsigned short donorZone, unsigned short targetZone) {}
+
+  /*!
+   * \brief A virtual member.
+   * \param[in] donorZone - zone in which the displacements will be transferred.
+   * \param[in] targetZone - zone which receives the tractions transferred.
+   */
+  virtual void Transfer_Displacements(unsigned short donorZone, unsigned short targetZone) {}
+
+  /*!
+   * \brief A virtual member.
+   * \param[in] donorZone - zone from which the tractions will be transferred.
+   * \param[in] targetZone - zone which receives the tractions transferred.
+   */
+  virtual void Transfer_Tractions(unsigned short donorZone, unsigned short targetZone) {}
+
+  /*!
+   * \brief A virtual member.
+   * \param[in] donorZone - origin of the information.
+   * \param[in] targetZone - destination of the information.
+   * \param[in] iOuterIter - Fluid-Structure Interaction subiteration.
+   */
+  virtual void Relaxation_Displacements(unsigned short donorZone, unsigned short targetZone, unsigned long iOuterIter) {}
+
+  /*!
+   * \brief A virtual member.
+   * \param[in] donorZone - origin of the information.
+   * \param[in] targetZone - destination of the information.
+   * \param[in] iOuterIter - Fluid-Structure Interaction subiteration.
+   */
+  virtual void Relaxation_Tractions(unsigned short donorZone, unsigned short targetZone, unsigned long iOuterIter) {}
+
+  /*!
+   * \brief A virtual member to run a Block Gauss-Seidel iteration in multi-zone problems.
+   */
+  virtual void Run_GaussSeidel() {}
+
+  /*!
+   * \brief A virtual member to run a Block-Jacobi iteration in multi-zone problems.
+   */
+  virtual void Run_Jacobi() {}
+
+  /*!
+   * \brief A virtual member.
+   */
+  virtual void Update() {}
+
+  /*!
+   * \brief Print out the direct residuals.
+   * \param[in] kind_recording - Type of recording (full list in ENUM_RECORDING, option_structure.hpp)
+   */
+  void Print_DirectResidual(RECORDING kind_recording);
+
+ public:
+  /*!
+   * \brief Launch the computation for all zones and all physics.
+   */
+  virtual void StartSolver() {}
+
+  /*!
+   * \brief Deallocation routine
+   */
+  void Postprocessing();
+
+  /*!
+   * \brief A virtual member.
+   */
+  virtual void ResetConvergence();
+
+  /*!
+   * \brief Perform some pre-processing before an iteration of the physics.
+   */
+  virtual void Preprocess(unsigned long TimeIter) {}
+
+  /*!
+   * \brief Monitor the computation.
+   */
+  virtual bool Monitor(unsigned long TimeIter) { return false; }
+
+  /*!
+   * \brief Output the solution in solution file.
+   */
+  virtual void Output(unsigned long TimeIter) {}
+
+  /*!
+   * \brief Perform a dynamic mesh deformation, including grid velocity computation and update of the multi-grid
+   * structure.
+   */
+  virtual void DynamicMeshUpdate(unsigned long TimeIter) {}
+
+  /*!
+   * \brief Perform a dynamic mesh deformation, including grid velocity computation and update of the multi-grid
+   * structure.
+   */
+  virtual void DynamicMeshUpdate(unsigned short val_iZone, unsigned long TimeIter) {}
+
+  /*!
+   * \brief Perform a mesh deformation as initial condition.
+   */
+  virtual void SetInitialMesh() {}
+
+  /*!
+   * \brief Process the boundary conditions and update the multi-grid structure.
+   */
+  void BoundaryConditionsUpdate();
+
+  /*!
+   * \brief Get the total drag.
+   * \return Total drag.
+   */
+  passivedouble Get_Drag() const;
+
+  /*!
+   * \brief Get the total lift.
+   * \return Total lift.
+   */
+  passivedouble Get_Lift() const;
+
+  /*!
+   * \brief Get the total x moment.
+   * \return Total x moment.
+   */
+  passivedouble Get_Mx() const;
+
+  /*!
+   * \brief Get the total y moment.
+   * \return Total y moment.
+   */
+  passivedouble Get_My() const;
+
+  /*!
+   * \brief Get the total z moment.
+   * \return Total z moment.
+   */
+  passivedouble Get_Mz() const;
+
+  /*!
+   * \brief Get the total drag coefficient.
+   * \return Total drag coefficient.
+   */
+  passivedouble Get_DragCoeff() const;
+
+  /*!
+   * \brief Get the total lift coefficient.
+   * \return Total lift coefficient.
+   */
+  passivedouble Get_LiftCoeff() const;
+
+  /*!
+   * \brief Get the number of external iterations.
+   * \return Number of external iterations.
+   */
+  unsigned long GetnTimeIter() const;
+
+  /*!
+   * \brief Get the current external iteration.
+   * \return Current external iteration.
+   */
+  unsigned long GetTime_Iter() const;
+
+  /*!
+   * \brief Get the unsteady time step.
+   * \return Unsteady time step.
+   */
+  passivedouble GetUnsteady_TimeStep() const;
+
+  /*!
+   * \brief Get the name of the output file for the surface.
+   * \return File name for the surface output.
+   */
+  string GetSurfaceFileName() const;
+
+  /*!
+   * \brief Get the temperature at a vertex on a specified marker.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \return Temperature of the vertex.
+   */
+  passivedouble GetVertexTemperature(unsigned short iMarker, unsigned long iVertex) const;
+
+  /*!
+   * \brief Set the temperature of a vertex on a specified marker.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \param[in] val_WallTemp - Value of the temperature.
+   */
+  void SetVertexTemperature(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallTemp);
+
+  /*!
+   * \brief Get the heat flux at a vertex on a specified marker (3 components).
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \return True if the vertex is a halo node.
+   */
+  vector<passivedouble> GetVertexHeatFluxes(unsigned short iMarker, unsigned long iVertex) const;
+
+  /*!
+   * \brief Get the wall normal component of the heat flux at a vertex on a specified marker.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \return Wall normal component of the heat flux at the vertex.
+   */
+  passivedouble GetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex) const;
+
+  /*!
+   * \brief Set the wall normal component of the heat flux at a vertex on a specified marker.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \param[in] val_WallHeatFlux - Value of the normal heat flux.
+   */
+  void SetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallHeatFlux);
+
+  /*!
+   * \brief Get the thermal conductivity at a vertex on a specified marker.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \return Thermal conductivity at the vertex.
+   */
+  passivedouble GetThermalConductivity(unsigned short iMarker, unsigned long iVertex) const;
+
+  /*!
+   * \brief Preprocess the inlets via file input for all solvers.
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void Inlet_Preprocessing(CSolver*** solver, CGeometry** geometry, CConfig* config) const;
+
+  /*!
+   * \brief Get all the CHT boundary marker tags.
+   * \return List of CHT boundary markers tags.
+   */
+  vector<string> GetCHTMarkerTags() const;
+
+  /*!
+   * \brief Get all the inlet boundary marker tags.
+   * \return List of inlet boundary markers tags.
+   */
+  vector<string> GetInletMarkerTags() const;
+
+  /*!
+   * \brief Return the sensitivities of the mesh boundary vertices.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \return Vector of sensitivities.
+   */
+  vector<passivedouble> GetMeshDisp_Sensitivity(unsigned short iMarker, unsigned long iVertex) const;
+
+  /*!
+   * \brief Set the load in X direction for the structural solver.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \param[in] LoadX - Value of the load in the direction X.
+   * \param[in] LoadX - Value of the load in the direction Y.
+   * \param[in] LoadX - Value of the load in the direction Z.
+   */
+  void SetFEA_Loads(unsigned short iMarker, unsigned long iVertex, passivedouble LoadX, passivedouble LoadY,
+                    passivedouble LoadZ);
+
+  /*!
+   * \brief Return the displacements from the FEA solver.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \return Vector of displacements.
+   */
+  vector<passivedouble> GetFEA_Displacements(unsigned short iMarker, unsigned long iVertex) const;
+
+  /*!
+   * \brief Return the velocities from the FEA Solver.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \return Vector of velocities.
+   */
+  vector<passivedouble> GetFEA_Velocity(unsigned short iMarker, unsigned long iVertex) const;
+
+  /*!
+   * \brief Return the velocities from the FEA Solver.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \return Vector of velocities at time n.
+   */
+  vector<passivedouble> GetFEA_Velocity_n(unsigned short iMarker, unsigned long iVertex) const;
+
+  /*!
+   * \brief Get the sensitivity of the flow loads for the structural solver.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \param[in] LoadX - Value of the load in the direction X.
+   * \param[in] LoadX - Value of the load in the direction Y.
+   * \param[in] LoadX - Value of the load in the direction Z.
+   */
+  vector<passivedouble> GetFlowLoad_Sensitivity(unsigned short iMarker, unsigned long iVertex) const;
+
+  /*!
+   * \brief Get the flow load (from the extra step - the repeated methods should be unified once the postprocessing
+   * strategy is in place).
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   */
+  vector<passivedouble> GetFlowLoad(unsigned short iMarker, unsigned long iVertex) const;
+
+  /*!
+   * \brief Set the adjoint of the flow tractions (from the extra step -
+   * the repeated methods should be unified once the postprocessing strategy is in place).
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \param[in] val_AdjointX - Value of the adjoint in the direction X.
+   * \param[in] val_AdjointY - Value of the adjoint in the direction Y.
+   * \param[in] val_AdjointZ - Value of the adjoint in the direction Z.
+   */
+  void SetFlowLoad_Adjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
+                           passivedouble val_AdjointY, passivedouble val_AdjointZ);
+
+  /*!
+   * \brief Set the adjoint of the structural displacements (from an outside source)
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \param[in] val_AdjointX - Value of the adjoint in the direction X.
+   * \param[in] val_AdjointY - Value of the adjoint in the direction Y.
+   * \param[in] val_AdjointZ - Value of the adjoint in the direction Z.
+   */
+  void SetSourceTerm_DispAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
+                                 passivedouble val_AdjointY, passivedouble val_AdjointZ);
+  void SetSourceTerm_VelAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
+                                passivedouble val_AdjointY, passivedouble val_AdjointZ);
+
+  /*!
+   * \brief Set the position of the heat source.
+   * \param[in] alpha - Angle of rotation respect to Z axis.
+   * \param[in] pos_x - Position X.
+   * \param[in] pos_y - Position Y.
+   * \param[in] pos_z - Position Z.
+   */
+  void SetHeatSource_Position(passivedouble alpha, passivedouble pos_x, passivedouble pos_y, passivedouble pos_z);
+
+  /*!
+   * \brief Set the direction of the inlet.
+   * \param[in] iMarker - Marker index.
+   * \param[in] alpha - Angle (Zpos).
+   */
+  void SetInlet_Angle(unsigned short iMarker, passivedouble alpha);
+
+  /*!
+   * \brief Sum the number of primal or adjoint variables for all solvers in a given zone.
+   * \param[in] iZone - Index of the zone.
+   * \param[in] adjoint - True to consider adjoint solvers instead of primal.
+   * \return Total number of solution variables.
+   */
+  unsigned short GetTotalNumberOfVariables(unsigned short iZone, bool adjoint) const {
+    unsigned short nVar = 0;
+    for (auto iSol = 0u; iSol < MAX_SOLS; iSol++) {
+      auto solver = solver_container[iZone][INST_0][MESH_0][iSol];
+      if (solver && (solver->GetAdjoint() == adjoint)) nVar += solver->GetnVar();
     }
-    
-    /*!
-     * \brief Set the "old solution" of all solvers (adjoint or primal) in a zone.
-     */
-    template<class Container>
-    void SetAllSolutionsOld(unsigned short iZone, bool adjoint, const Container& solution) {
-        SetAllSolutions<Container,true>(iZone, adjoint, solution);
+    return nVar;
+  }
+
+  /*!
+   * \brief Set the solution of all solvers (adjoint or primal) in a zone.
+   * \param[in] iZone - Index of the zone.
+   * \param[in] adjoint - True to consider adjoint solvers instead of primal.
+   * \param[in] solution - Solution object with interface (iPoint,iVar).
+   * \tparam Old - If true set "old solutions" instead.
+   */
+  template <class Container, bool Old = false>
+  void SetAllSolutions(unsigned short iZone, bool adjoint, const Container& solution) {
+    const auto nPoint = geometry_container[iZone][INST_0][MESH_0]->GetnPoint();
+    for (auto iSol = 0u, offset = 0u; iSol < MAX_SOLS; ++iSol) {
+      auto solver = solver_container[iZone][INST_0][MESH_0][iSol];
+      if (!(solver && (solver->GetAdjoint() == adjoint))) continue;
+      for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint)
+        for (auto iVar = 0ul; iVar < solver->GetnVar(); ++iVar)
+          if (!Old) {
+            solver->GetNodes()->SetSolution(iPoint, iVar, solution(iPoint, offset + iVar));
+          } else {
+            solver->GetNodes()->SetSolution_Old(iPoint, iVar, solution(iPoint, offset + iVar));
+          }
+      offset += solver->GetnVar();
     }
-    
-    /*!
-     * \brief Get the solution of all solvers (adjoint or primal) in a zone.
-     * \param[in] iZone - Index of the zone.
-     * \param[in] adjoint - True to consider adjoint solvers instead of primal.
-     * \param[out] solution - Solution object with interface (iPoint,iVar).
-     */
-    template<class Container>
-    void GetAllSolutions(unsigned short iZone, bool adjoint, Container& solution) const {
-        const auto nPoint = geometry_container[iZone][INST_0][MESH_0]->GetnPoint();
-        for (auto iSol = 0u, offset = 0u; iSol < MAX_SOLS; ++iSol) {
-            auto solver = solver_container[iZone][INST_0][MESH_0][iSol];
-            if (!(solver && (solver->GetAdjoint() == adjoint))) continue;
-            const auto& sol = solver->GetNodes()->GetSolution();
-            for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint)
-                for (auto iVar = 0ul; iVar < solver->GetnVar(); ++iVar)
-                    solution(iPoint,offset+iVar) = SU2_TYPE::GetValue(sol(iPoint,iVar));
-            offset += solver->GetnVar();
-        }
+  }
+
+  /*!
+   * \brief Set the "old solution" of all solvers (adjoint or primal) in a zone.
+   */
+  template <class Container>
+  void SetAllSolutionsOld(unsigned short iZone, bool adjoint, const Container& solution) {
+    SetAllSolutions<Container, true>(iZone, adjoint, solution);
+  }
+
+  /*!
+   * \brief Get the solution of all solvers (adjoint or primal) in a zone.
+   * \param[in] iZone - Index of the zone.
+   * \param[in] adjoint - True to consider adjoint solvers instead of primal.
+   * \param[out] solution - Solution object with interface (iPoint,iVar).
+   */
+  template <class Container>
+  void GetAllSolutions(unsigned short iZone, bool adjoint, Container& solution) const {
+    const auto nPoint = geometry_container[iZone][INST_0][MESH_0]->GetnPoint();
+    for (auto iSol = 0u, offset = 0u; iSol < MAX_SOLS; ++iSol) {
+      auto solver = solver_container[iZone][INST_0][MESH_0][iSol];
+      if (!(solver && (solver->GetAdjoint() == adjoint))) continue;
+      const auto& sol = solver->GetNodes()->GetSolution();
+      for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint)
+        for (auto iVar = 0ul; iVar < solver->GetnVar(); ++iVar)
+          solution(iPoint, offset + iVar) = SU2_TYPE::GetValue(sol(iPoint, iVar));
+      offset += solver->GetnVar();
     }
-    
+  }
 };
 
 /*!
@@ -682,71 +686,66 @@ class CDriver : public CDriverBase {
  * \author T. Economon, G. Gori
  */
 class CFluidDriver : public CDriver {
-    
-protected:
-    unsigned long Max_Iter;
-    
-protected:
-    
-    /*!
-     * \brief Constructor of the class.
-     * \param[in] confFile - Configuration file name.
-     * \param[in] val_nZone - Total number of zones.
-     * \param[in] val_nDim - Number of dimensions.
-     * \param[in] MPICommunicator - MPI communicator for SU2.
-     */
-    CFluidDriver(char* confFile,
-                 unsigned short val_nZone,
-                 SU2_Comm MPICommunicator);
-    
-public:
-    /*!
-     * \brief Destructor of the class.
-     */
-    ~CFluidDriver(void) override;
-    
-    /*!
-     * \brief Launch the computation for all zones and all physics.
-     */
-    void StartSolver() override;
-    
-    /*!
-     * \brief Run a single iteration of the physics within multiple zones.
-     */
-    void Run() override;
-    
-    /*!
-     * \brief Update the dual-time solution within multiple zones.
-     */
-    void Update() override;
-    
-    /*!
-     * \brief Output the solution in solution file.
-     */
-    void Output(unsigned long InnerIter) override;
-    
-    /*!
-     * \brief Monitor the computation.
-     */
-    bool Monitor(unsigned long ExtIter) override;
-    
-    /*!
-     * \brief Perform some pre-processing before an iteration of the physics.
-     */
-    void Preprocess(unsigned long Iter) override;
-    
-    /*!
-     * \brief Perform a dynamic mesh deformation, included grid velocity computation and the update of the multigrid structure (multiple zone).
-     */
-    void DynamicMeshUpdate(unsigned long TimeIter) override;
-    
-    /*!
-     * \brief Transfer data among different zones (multiple zone).
-     */
-    void Transfer_Data(unsigned short donorZone, unsigned short targetZone);
-    
-};
+ protected:
+  unsigned long Max_Iter;
+
+ protected:
+  /*!
+   * \brief Constructor of the class.
+   * \param[in] confFile - Configuration file name.
+   * \param[in] val_nZone - Total number of zones.
+   * \param[in] val_nDim - Number of dimensions.
+   * \param[in] MPICommunicator - MPI communicator for SU2.
+   */
+  CFluidDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator);
+
+ public:
+  /*!
+   * \brief Destructor of the class.
+   */
+  ~CFluidDriver(void) override;
+
+  /*!
+   * \brief Launch the computation for all zones and all physics.
+   */
+  void StartSolver() override;
+
+  /*!
+   * \brief Run a single iteration of the physics within multiple zones.
+   */
+  void Run() override;
 
+  /*!
+   * \brief Update the dual-time solution within multiple zones.
+   */
+  void Update() override;
+
+  /*!
+   * \brief Output the solution in solution file.
+   */
+  void Output(unsigned long InnerIter) override;
+
+  /*!
+   * \brief Monitor the computation.
+   */
+  bool Monitor(unsigned long ExtIter) override;
+
+  /*!
+   * \brief Perform some pre-processing before an iteration of the physics.
+   */
+  void Preprocess(unsigned long Iter) override;
+
+  /*!
+   * \brief Perform a dynamic mesh deformation, included grid velocity computation and the update of the multi-grid
+   * structure (multiple zone).
+   */
+  void DynamicMeshUpdate(unsigned long TimeIter) override;
+
+  /*!
+   * \brief Transfer data among different zones (multiple zone).
+   */
+  void Transfer_Data(unsigned short donorZone, unsigned short targetZone);
+};
 
 /*!
  * \class CTurbomachineryDriver
@@ -755,51 +754,45 @@ class CFluidDriver : public CDriver {
  * \author S. Vitale
  */
 class CTurbomachineryDriver : public CFluidDriver {
-private:
-    COutputLegacy* output_legacy;
-    
-public:
-    
-    /*!
-     * \brief Constructor of the class.
-     * \param[in] confFile - Configuration file name.
-     * \param[in] val_nZone - Total number of zones.
-     * \param[in] val_nDim - Number of dimensions.
-     * \param[in] val_periodic - Bool for periodic BCs.
-     * \param[in] MPICommunicator - MPI communicator for SU2.
-     */
-    CTurbomachineryDriver(char* confFile,
-                          unsigned short val_nZone,
-                          SU2_Comm MPICommunicator);
-    
-    /*!
-     * \brief Destructor of the class.
-     */
-    ~CTurbomachineryDriver(void) override;
-    
-    /*!
-     * \brief Run a single iteration of the physics within multiple zones.
-     */
-    
-    void Run() override;
-    
-    /*!
-     * \brief Set Mixing Plane interface within multiple zones.
-     */
-    void SetMixingPlane(unsigned short iZone);
-    
-    /*!
-     * \brief Set Mixing Plane interface within multiple zones.
-     */
-    void SetTurboPerformance(unsigned short targetZone);
-    
-    /*!
-     * \brief Monitor the computation.
-     */
-    bool Monitor(unsigned long TimeIter) override;
-    
-    
-    
+ private:
+  COutputLegacy* output_legacy;
+
+ public:
+  /*!
+   * \brief Constructor of the class.
+   * \param[in] confFile - Configuration file name.
+   * \param[in] val_nZone - Total number of zones.
+   * \param[in] val_nDim - Number of dimensions.
+   * \param[in] val_periodic - Bool for periodic BCs.
+   * \param[in] MPICommunicator - MPI communicator for SU2.
+   */
+  CTurbomachineryDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator);
+
+  /*!
+   * \brief Destructor of the class.
+   */
+  ~CTurbomachineryDriver(void) override;
+
+  /*!
+   * \brief Run a single iteration of the physics within multiple zones.
+   */
+
+  void Run() override;
+
+  /*!
+   * \brief Set Mixing Plane interface within multiple zones.
+   */
+  void SetMixingPlane(unsigned short iZone);
+
+  /*!
+   * \brief Set Mixing Plane interface within multiple zones.
+   */
+  void SetTurboPerformance(unsigned short targetZone);
+
+  /*!
+   * \brief Monitor the computation.
+   */
+  bool Monitor(unsigned long TimeIter) override;
 };
 
 /*!
@@ -809,61 +802,57 @@ class CTurbomachineryDriver : public CFluidDriver {
  * \author T. Economon
  */
 class CHBDriver : public CFluidDriver {
-    
-private:
-    COutputLegacy* output_legacy;
-    unsigned short nInstHB;
-    su2double **D; /*!< \brief Harmonic Balance operator. */
-    
-public:
-    
-    /*!
-     * \brief Constructor of the class.
-     * \param[in] confFile - Configuration file name.
-     * \param[in] val_nZone - Total number of zones.
-     * \param[in] val_nDim - Number of dimensions.
-     * \param[in] MPICommunicator - MPI communicator for SU2.
-     */
-    CHBDriver(char* confFile,
-              unsigned short val_nZone,
-              SU2_Comm MPICommunicator);
-    
-    /*!
-     * \brief Destructor of the class.
-     */
-    ~CHBDriver(void) override;
-    
-    /*!
-     * \brief Run a single iteration of a Harmonic Balance problem.
-     */
-    void Run() override;
-    
-    /*!
-     * \brief Computation and storage of the Harmonic Balance method source terms.
-     * \author T. Economon, K. Naik
-     * \param[in] iZone - Current zone number.
-     */
-    void SetHarmonicBalance(unsigned short iZone);
-    
-    /*!
-     * \brief Precondition Harmonic Balance source term for stability
-     * \author J. Howison
-     */
-    void StabilizeHarmonicBalance();
-    
-    /*!
-     * \brief Computation of the Harmonic Balance operator matrix for harmonic balance.
-     * \author A. Rubino, S. Nimmagadda
-     */
-    void ComputeHB_Operator();
-    
-    /*!
-     * \brief Update the solution for the Harmonic Balance.
-     */
-    void Update() override;
-    
-    /*!
-     * \brief Reset the convergence flag (set to false) of the solver for the Harmonic Balance.
-     */
-    void ResetConvergence() override;
+ private:
+  COutputLegacy* output_legacy;
+  unsigned short nInstHB;
+  su2double** D; /*!< \brief Harmonic Balance operator. */
+
+ public:
+  /*!
+   * \brief Constructor of the class.
+   * \param[in] confFile - Configuration file name.
+   * \param[in] val_nZone - Total number of zones.
+   * \param[in] val_nDim - Number of dimensions.
+   * \param[in] MPICommunicator - MPI communicator for SU2.
+   */
+  CHBDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator);
+
+  /*!
+   * \brief Destructor of the class.
+   */
+  ~CHBDriver(void) override;
+
+  /*!
+   * \brief Run a single iteration of a Harmonic Balance problem.
+   */
+  void Run() override;
+
+  /*!
+   * \brief Computation and storage of the Harmonic Balance method source terms.
+   * \author T. Economon, K. Naik
+   * \param[in] iZone - Current zone number.
+   */
+  void SetHarmonicBalance(unsigned short iZone);
+
+  /*!
+   * \brief Precondition Harmonic Balance source term for stability
+   * \author J. Howison
+   */
+  void StabilizeHarmonicBalance();
+
+  /*!
+   * \brief Computation of the Harmonic Balance operator matrix for harmonic balance.
+   * \author A. Rubino, S. Nimmagadda
+   */
+  void ComputeHB_Operator();
+
+  /*!
+   * \brief Update the solution for the Harmonic Balance.
+   */
+  void Update() override;
+
+  /*!
+   * \brief Reset the convergence flag (set to false) of the solver for the Harmonic Balance.
+   */
+  void ResetConvergence() override;
 };

From 3c3b4a5d7b6c5e2c78bba3d56bb3b84a06ac4609 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Sat, 10 Dec 2022 15:45:00 -0800
Subject: [PATCH 070/656] Fix copyright dates

---
 Common/include/drivers/CDriverBase.hpp                | 2 +-
 Common/src/drivers/CDriverBase.cpp                    | 2 +-
 SU2_DEF/include/drivers/CDeformationDriver.hpp        | 2 +-
 SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp | 2 +-
 SU2_DEF/src/drivers/CDeformationDriver.cpp            | 2 +-
 SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp     | 2 +-
 6 files changed, 6 insertions(+), 6 deletions(-)

diff --git a/Common/include/drivers/CDriverBase.hpp b/Common/include/drivers/CDriverBase.hpp
index 09107b4d685..e3acace3892 100644
--- a/Common/include/drivers/CDriverBase.hpp
+++ b/Common/include/drivers/CDriverBase.hpp
@@ -9,7 +9,7 @@
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2021, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public
diff --git a/Common/src/drivers/CDriverBase.cpp b/Common/src/drivers/CDriverBase.cpp
index 9d5ec62f32d..9c7d69bbd5b 100644
--- a/Common/src/drivers/CDriverBase.cpp
+++ b/Common/src/drivers/CDriverBase.cpp
@@ -9,7 +9,7 @@
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2021, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser/ General Public
diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index f27c0155a81..bded29a1f0d 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -9,7 +9,7 @@
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2021, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public
diff --git a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
index da663dcf022..783e21c98dd 100644
--- a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
@@ -9,7 +9,7 @@
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2021, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 51604c3c72e..6140f4526a9 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -9,7 +9,7 @@
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2021, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser/ General Public
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index a513081b338..f483eb0dabf 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -9,7 +9,7 @@
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2021, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public

From 23716f32d1803d8068af6d86f4dd55f9c8753953 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Sat, 10 Dec 2022 15:50:05 -0800
Subject: [PATCH 071/656] Add Python support for incompressible and NEMO
 solvers

---
 SU2_CFD/src/python_wrapper_structure.cpp | 8 +++++++-
 1 file changed, 7 insertions(+), 1 deletion(-)

diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index 6ec8e594669..e3046eda5fd 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -50,7 +50,12 @@ void CDriver::PythonInterface_Preprocessing(CConfig **config, CGeometry ****geom
             
             if ((config[iZone]->GetKind_Solver() == MAIN_SOLVER::EULER) ||
                 (config[iZone]->GetKind_Solver() == MAIN_SOLVER::NAVIER_STOKES) ||
-                (config[iZone]->GetKind_Solver() == MAIN_SOLVER::RANS)) {
+                (config[iZone]->GetKind_Solver() == MAIN_SOLVER::RANS) ||
+                (config[iZone]->GetKind_Solver() == MAIN_SOLVER::INC_EULER) ||
+                (config[iZone]->GetKind_Solver() == MAIN_SOLVER::INC_NAVIER_STOKES) ||
+                (config[iZone]->GetKind_Solver() == MAIN_SOLVER::INC_RANS) ||
+                (config[iZone]->GetKind_Solver() == MAIN_SOLVER::NEMO_EULER) ||
+                (config[iZone]->GetKind_Solver() == MAIN_SOLVER::NEMO_NAVIER_STOKES)) {
                 
                 solver[iZone][INST_0][MESH_0][FLOW_SOL]->UpdateCustomBoundaryConditions(geometry[iZone][INST_0], config[iZone]);
             }
@@ -387,6 +392,7 @@ void CDriver::ResetConvergence() {
                 
             case MAIN_SOLVER::EULER: case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::RANS:
             case MAIN_SOLVER::INC_EULER: case MAIN_SOLVER::INC_NAVIER_STOKES: case MAIN_SOLVER::INC_RANS:
+            case MAIN_SOLVER::NEMO_EULER: case MAIN_SOLVER::NEMO_NAVIER_STOKES:
                 integration_container[iZone][INST_0][FLOW_SOL]->SetConvergence(false);
                 if (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::RANS) integration_container[iZone][INST_0][TURB_SOL]->SetConvergence(false);
                 if(config_container[iZone]->GetKind_Trans_Model() == TURB_TRANS_MODEL::LM) integration_container[iZone][INST_0][TRANS_SOL]->SetConvergence(false);

From cd523cdfb0385bcd65cf0a4d7fced133cbbdf54e Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Sat, 10 Dec 2022 15:54:26 -0800
Subject: [PATCH 072/656] Add more boundary conditions for GetMarkerTypes()

---
 Common/src/drivers/CDriverBase.cpp | 26 +++++++++++++++++++++++++-
 1 file changed, 25 insertions(+), 1 deletion(-)

diff --git a/Common/src/drivers/CDriverBase.cpp b/Common/src/drivers/CDriverBase.cpp
index 9c7d69bbd5b..cc222d50e6c 100644
--- a/Common/src/drivers/CDriverBase.cpp
+++ b/Common/src/drivers/CDriverBase.cpp
@@ -225,7 +225,10 @@ map<string, string> CDriverBase::GetMarkerTypes() const {
         type = "ISOTHERMAL";
         break;
       case HEAT_FLUX:
-        type = "HEATFLUX";
+        type = "HEAT_FLUX";
+        break;
+      case HEAT_TRANSFER:
+        type = "HEAT_TRANSFER";
         break;
       case INLET_FLOW:
         type = "INLET_FLOW";
@@ -233,6 +236,27 @@ map<string, string> CDriverBase::GetMarkerTypes() const {
       case OUTLET_FLOW:
         type = "OUTLET_FLOW";
         break;
+      case SUPERSONIC_INLET:
+        type = "SUPERSONIC_INLET";
+        break;
+      case SUPERSONIC_OUTLET:
+        type = "SUPERSONIC_OUTLET";
+        break;
+      case RIEMANN_BOUNDARY:
+        type = "RIEMANN";
+        break;
+      case GILES_BOUNDARY:
+        type = "GILES";
+        break;
+      case DISPLACEMENT_BOUNDARY:
+        type = "DISPLACEMENT";
+        break;
+      case LOAD_BOUNDARY:
+        type = "LOAD";
+        break;
+      case PERIODIC_BOUNDARY:
+        type = "PERIODIC";
+        break;
       case SYMMETRY_PLANE:
         type = "SYMMETRY";
         break;

From 3ea9b55fb3f7e81a024e62ec4c4b84283adba04b Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Sat, 10 Dec 2022 16:35:31 -0800
Subject: [PATCH 073/656] Fix unused variable error in regression tests

---
 Common/src/drivers/CDriverBase.cpp | 5 -----
 1 file changed, 5 deletions(-)

diff --git a/Common/src/drivers/CDriverBase.cpp b/Common/src/drivers/CDriverBase.cpp
index cc222d50e6c..dd1e3f9c88e 100644
--- a/Common/src/drivers/CDriverBase.cpp
+++ b/Common/src/drivers/CDriverBase.cpp
@@ -885,7 +885,6 @@ void CDriverBase::ReadFFDInfo(CGeometry* geometry, CConfig* config, CFreeFormDef
 
   unsigned short nFFDBox = 0;
   unsigned short nLevel = 0;
-  bool FFDBoxDefinition = false;
 
   mesh_file.open(val_mesh_filename);
   if (mesh_file.fail()) {
@@ -1232,10 +1231,6 @@ void CDriverBase::ReadFFDInfo(CGeometry* geometry, CConfig* config, CFreeFormDef
 
         if (rank == MASTER_NODE) cout << "Control points: " << nControlPoints[iFFDBox] << ". ";
 
-        /*--- Method to identify if there is a FFDBox definition. ---*/
-
-        if (nControlPoints[iFFDBox] != 0) FFDBoxDefinition = true;
-
         /*--- Read the coordinates of the control points. ---*/
 
         for (iControlPoints = 0; iControlPoints < nControlPoints[iFFDBox]; iControlPoints++) {

From d83d0e4d7ffc702ec3b2d2d72c6359a01b5c6b3f Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 12 Dec 2022 14:37:03 +0100
Subject: [PATCH 074/656] Merged with develop and fixed bug in 2D interpolation
 where table level would not be selected properly

---
 Common/src/containers/CLookUpTable.cpp | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index 75d8410231d..b53763ec4ee 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -487,7 +487,7 @@ unsigned long CLookUpTable::LookUp_XY(const string& val_name_var, su2double *val
       for (int p = 0; p < 3; p++) 
         triangle[p] = triangles[i_level][id_triangle][p]; 
 
-      *val_var = Interpolate(GetDataP(val_name_var), triangle, interp_coeffs);
+      *val_var = Interpolate(GetDataP(val_name_var, i_level), triangle, interp_coeffs);
       exit_code = 0;
     } else {
       /* in bounding box but outside of table */
@@ -573,7 +573,7 @@ unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vecto
         /* first, copy the single triangle from the large triangle list*/
         for (int p = 0; p < 3; p++) 
           triangle[p] = triangles[i_level][id_triangle][p]; 
-        *val_vars[i_var] = Interpolate(GetDataP(val_names_var[i_var]), triangle, interp_coeffs);
+        *val_vars[i_var] = Interpolate(GetDataP(val_names_var[i_var], i_level), triangle, interp_coeffs);
       }
       else
         *val_vars[i_var] = GetDataP(val_names_var[i_var], i_level)[nearest_neighbor];

From 8aa6a58784a92fc137d16992771796f1d0c7ab4f Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Mon, 12 Dec 2022 11:13:50 -0800
Subject: [PATCH 075/656] Update code documentation blocks in CDriver.hpp

---
 SU2_CFD/include/drivers/CDriver.hpp | 75 ++++++++++++++++++++---------
 1 file changed, 51 insertions(+), 24 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index 50366afd833..b9f752b3bfb 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -87,8 +87,8 @@ class CDriver : public CDriverBase {
    * \brief Constructor of the class.
    * \param[in] confFile - Configuration file name.
    * \param[in] val_nZone - Total number of zones.
-   * \param[in] val_nDim - Number of dimensions.
    * \param[in] MPICommunicator - MPI communicator for SU2.
+   * \param[in] dummy_geo - Dummy geometric definition of the problem.
    */
   CDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator, bool dummy_geo);
 
@@ -110,53 +110,63 @@ class CDriver : public CDriverBase {
 
   /*!
    * \brief Read in the config and mesh files.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] driver_config - Definition of the driver configuration.
    */
   void Input_Preprocessing(CConfig**& config, CConfig*& driver_config);
 
   /*!
    * \brief Construction of the edge-based data structure and the multi-grid structure.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] dummy - Definition of the dummy driver.
    */
   void Geometrical_Preprocessing(CConfig* config, CGeometry**& geometry, bool dummy);
 
   /*!
    * \brief Do the geometrical preprocessing for the DG FEM solver.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Geometrical definition of the problem.
    */
   void Geometrical_Preprocessing_DGFEM(CConfig* config, CGeometry**& geometry);
 
   /*!
    * \brief Geometrical_Preprocessing_FVM
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Geometrical definition of the problem.
    */
   void Geometrical_Preprocessing_FVM(CConfig* config, CGeometry**& geometry);
 
   /*!
    * \brief Definition of the physics iteration class or within a single zone.
-   * \param[in] iteration_container - Pointer to the iteration container to be instantiated.
    * \param[in] config - Definition of the particular problem.
-   * \param[in] iZone - Index of the zone.
+   * \param[in] iteration - Pointer to the iteration container to be instantiated.
    */
   void Iteration_Preprocessing(CConfig* config, CIteration*& iteration) const;
 
   /*!
    * \brief Definition and allocation of all solution classes.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver - Container vector with all the solutions.
    */
   void Solver_Preprocessing(CConfig* config, CGeometry** geometry, CSolver***& solver);
 
   /*!
    * \brief Restart of the solvers from the restart files.
-   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] solver - Container vector with all the solutions.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
+   * \param[in] update_geo - Boolean to indicate if geometry should be updated.
    */
   void Solver_Restart(CSolver*** solver, CGeometry** geometry, CConfig* config, bool update_geo);
 
   /*!
    * \brief Definition and allocation of all solution classes.
-   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] solver - Container vector with all the solutions.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
+   * \param[in] val_iInst - Current solver instance.
    */
   void Solver_Postprocessing(CSolver**** solver, CGeometry** geometry, CConfig* config, unsigned short val_iInst);
 
@@ -164,21 +174,28 @@ class CDriver : public CDriverBase {
    * \brief Definition and allocation of all integration classes.
    * \param[in] config - Definition of the particular problem.
    * \param[in] solver - Container vector with all the solutions.
-   * \param[out] integration - Container vector with all the integration methods.
+   * \param[in] integration - Container vector with all the integration methods.
    */
   void Integration_Preprocessing(CConfig* config, CSolver** solver, CIntegration**& integration) const;
 
   /*!
    * \brief Definition and allocation of all integration classes.
-   * \param[in] integration_container - Container vector with all the integration methods.
+   * \param[in] integration - Container vector with all the integration methods.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
+   * \param[in] val_iInst - Current solver instance.
    */
   void Integration_Postprocessing(CIntegration*** integration, CGeometry** geometry, CConfig* config,
                                   unsigned short val_iInst);
 
   /*!
    * \brief Definition and allocation of all interface classes.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] solver - Container vector with all the solutions.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] interface_types - Type of coupling between the distinct (physical) zones.
+   * \param[in] interface - Class defining the physical transfer of information.
+   * \param[in] interpolation -  Object defining the interpolation.
    */
   void Interface_Preprocessing(CConfig** config, CSolver***** solver, CGeometry**** geometry,
                                unsigned short** interface_types, CInterface*** interface,
@@ -186,10 +203,10 @@ class CDriver : public CDriverBase {
 
   /*!
    * \brief Definition and allocation of all solver classes.
-   * \param[in] numerics_container - Description of the numerical method (the way in which the equations are solved).
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] solver_container - Container vector with all the solutions.
    * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver - Container vector with all the solutions.
+   * \param[in] numerics - Description of the numerical method (the way in which the equations are solved).
    */
   void Numerics_Preprocessing(CConfig* config, CGeometry** geometry, CSolver*** solver, CNumerics****& numerics) const;
 
@@ -215,44 +232,58 @@ class CDriver : public CDriverBase {
 
   /*!
    * \brief Definition and allocation of all solver classes.
-   * \param[in] numerics_container - Description of the numerical method (the way in which the equations are solved).
-   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] numerics - Description of the numerical method (the way in which the equations are solved).
+   * \param[in] solver - Container vector with all the solutions.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
+   * \param[in] val_iInst - Current solver instance.
    */
   void Numerics_Postprocessing(CNumerics***** numerics, CSolver*** solver, CGeometry** geometry, CConfig* config,
                                unsigned short val_iInst);
 
   /*!
    * \brief GridMovement_Preprocessing
-   * \param config
-   * \param geometry
-   * \param solver
-   * \param iteration
-   * \param grid_movement
-   * \param surface_movement
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver - Container vector with all the solutions.
+   * \param[in] iteration - Container vector with all the iteration methods.
+   * \param[in] grid_movement - Volume grid movement classes of the problem.
+   * \param[in] surface_movement - Surface movement classes of the problem.
    */
   void DynamicMesh_Preprocessing(CConfig* config, CGeometry** geometry, CSolver*** solver, CIteration* iteration,
                                  CVolumetricMovement*& grid_movement, CSurfaceMovement*& surface_movement) const;
 
   /*!
    * \brief Initialize Python interface functionalities
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver - Container vector with all the solutions.
    */
   void PythonInterface_Preprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver);
 
   /*!
    * \brief Preprocess the output container.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] driver_config - Definition of the driver configuration.
+   * \param[in] output_container - Container vector with all the outputs.
+   * \param[in] driver_output - Definition of the driver output.
    */
   void Output_Preprocessing(CConfig** config, CConfig* driver_config, COutput**& output_container,
                             COutput*& driver_output);
 
   /*!
    * \brief Initiate value for static mesh movement such as the gridVel for the ROTATING frame.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Geometrical definition of the problem.
    */
   void StaticMesh_Preprocessing(const CConfig* config, CGeometry** geometry);
 
   /*!
    * \brief Initiate value for static mesh movement such as the gridVel for the ROTATING frame.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver - Container vector with all the solutions.
+   * \param[in] interface - Class defining the physical transfer of information.
    */
   void Turbomachinery_Preprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver,
                                     CInterface*** interface);
@@ -694,7 +725,6 @@ class CFluidDriver : public CDriver {
    * \brief Constructor of the class.
    * \param[in] confFile - Configuration file name.
    * \param[in] val_nZone - Total number of zones.
-   * \param[in] val_nDim - Number of dimensions.
    * \param[in] MPICommunicator - MPI communicator for SU2.
    */
   CFluidDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator);
@@ -762,8 +792,6 @@ class CTurbomachineryDriver : public CFluidDriver {
    * \brief Constructor of the class.
    * \param[in] confFile - Configuration file name.
    * \param[in] val_nZone - Total number of zones.
-   * \param[in] val_nDim - Number of dimensions.
-   * \param[in] val_periodic - Bool for periodic BCs.
    * \param[in] MPICommunicator - MPI communicator for SU2.
    */
   CTurbomachineryDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator);
@@ -812,7 +840,6 @@ class CHBDriver : public CFluidDriver {
    * \brief Constructor of the class.
    * \param[in] confFile - Configuration file name.
    * \param[in] val_nZone - Total number of zones.
-   * \param[in] val_nDim - Number of dimensions.
    * \param[in] MPICommunicator - MPI communicator for SU2.
    */
   CHBDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator);

From 08c6885dbcbd994d293f0eb2f8be4bfea4bda24d Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Mon, 12 Dec 2022 17:03:34 -0500
Subject: [PATCH 076/656] adding collision parameters for air-7

---
 SU2_CFD/src/fluid/CSU2TCLib.cpp | 174 ++++++++++++++++++++++----------
 1 file changed, 119 insertions(+), 55 deletions(-)

diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index e6513195860..2111cccb780 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -254,10 +254,15 @@ CSU2TCLib::CSU2TCLib(const CConfig* config, unsigned short val_nDim, bool viscou
     //   Others:                 a = 1, b = 0
     Tcf_a[0] = 0.5; Tcf_b[0] = 0.5; Tcb_a[0] = 1;  Tcb_b[0] = 0;
     Tcf_a[1] = 0.5; Tcf_b[1] = 0.5; Tcb_a[1] = 1;  Tcb_b[1] = 0;
+
     /*--- Dissociation potential [KJ/kg] ---*/
     Diss[0] = 3.36E4;
     Diss[1] = 0.0;
+
     /*--- Collision integral data ---*/
+    // Index 1: collider
+    // Index 2: partner
+    // Index 3: A1, A2, A3
     Omega00(0,0,0) = -6.0614558E-03;  Omega00(0,0,1) = 1.2689102E-01;   Omega00(0,0,2) = -1.0616948E+00;  Omega00(0,0,3) = 8.0955466E+02;
     Omega00(0,1,0) = -1.0796249E-02;  Omega00(0,1,1) = 2.2656509E-01;   Omega00(0,1,2) = -1.7910602E+00;  Omega00(0,1,3) = 4.0455218E+03;
     Omega00(1,0,0) = -1.0796249E-02;  Omega00(1,0,1) = 2.2656509E-01;   Omega00(1,0,2) = -1.7910602E+00;  Omega00(1,0,3) = 4.0455218E+03;
@@ -564,6 +569,9 @@ CSU2TCLib::CSU2TCLib(const CConfig* config, unsigned short val_nDim, bool viscou
     Tcf_a[15] = 1.0; Tcf_b[15] = 0.0; Tcb_a[15] = 1;  Tcb_b[15] = 0;
     Tcf_a[16] = 1.0; Tcf_b[16] = 0.0; Tcb_a[16] = 1;  Tcb_b[16] = 0;
     /*--- Collision integral data ---*/
+    // Index 1: collider
+    // Index 2: partner
+    // Index 3: A1, A2, A3
     // Omega(0,0) ----------------------
     //N2
     Omega00(0,0,0) = -6.0614558E-03;  Omega00(0,0,1) = 1.2689102E-01;   Omega00(0,0,2) = -1.0616948E+00;  Omega00(0,0,3) = 8.0955466E+02;
@@ -745,6 +753,10 @@ CSU2TCLib::CSU2TCLib(const CConfig* config, unsigned short val_nDim, bool viscou
     CharElTemp.resize(nSpecies,maxEl) = su2double(0.0);
     ElDegeneracy.resize(nSpecies,maxEl) = su2double(0.0);      
    
+    // e: 1 state
+    CharElTemp(0,0) = 0.000000000000000E+00;
+    ElDegeneracy(0,0) = 1;
+
     //N2: 15 states
     CharElTemp(1,0)  = 0.000000000000000E+00;
     CharElTemp(1,1)  = 7.223156514095200E+04;
@@ -859,9 +871,6 @@ CSU2TCLib::CSU2TCLib(const CConfig* config, unsigned short val_nDim, bool viscou
     ElDegeneracy(6,5) = 1;
     ElDegeneracy(6,6) = 2;
     ElDegeneracy(6,7) = 2;
-    // e: 1 state
-    CharElTemp(0,0) = 0.000000000000000E+00;
-    ElDegeneracy(0,0) = 1;
 
     /*--- Set reaction maps ---*/
     // N2 dissociation
@@ -1008,72 +1017,127 @@ CSU2TCLib::CSU2TCLib(const CConfig* config, unsigned short val_nDim, bool viscou
     Tcf_a[20] = 1.0; Tcf_b[20] = 0.0; Tcb_a[20] = 0.5; Tcb_b[20] = 0.5;
     Tcf_a[21] = 0.0; Tcf_b[21] = 1.0; Tcb_a[21] = 0;   Tcb_b[21] = 1;    
 
-    //TODO: Implement Collision Integral Data for AIR-7 (JN)
     /*--- Collision integral data ---*/
-    //TODO: ELECTRONS HAvE NO OMEGAS....NEED TO ALTER LOOPS? or add dummy vector.....
+    // Index 1: collider
+    // Index 2: partner
+    // Index 3: A1, A2, A3
+
     // Omega(0,0) ----------------------
+    //e-  (TODO: NO+ and e-,  NO+ and NO+, e- and e- ??????)
+    Omega00(0,0,0) = 0.0000000E+00;  Omega00(0,0,1) = 0.0000000E+00;  Omega00(0,0,2) = 0.0000000E+00;  Omega00(0,0,3) = 0.0000000E+00;
+    Omega00(0,1,0) = -1.0525124E-02; Omega00(0,1,1) = 1.3498950E-01;  Omega00(0,1,2) = 1.2524805E-01;  Omega00(0,1,3) = 1.5066506E-01;
+    Omega00(0,2,0) = 2.3527001E-02;  Omega00(0,2,1) = -6.9632323E-01; Omega00(0,2,2) = 6.8035475E+00;  Omega00(0,2,3) = 1.8335509E-09;
+    Omega00(0,3,0) = 1.0414818E-01;  Omega00(0,3,1) = -2.8369126E+00; Omega00(0,3,2) = 2.5323135E+01;  Omega00(0,3,3) = 7.7138358E-32;
+    Omega00(0,4,0) = 0.0000000E+00;  Omega00(0,4,1) = 1.6554247E-01;  Omega00(0,4,2) = -3.4986344E+00; Omega00(0,4,3) = 5.9268038E+08;
+    Omega00(0,5,0) = 9.9865506E-03;  Omega00(0,5,1) = -2.7407431E-01; Omega00(0,5,2) = 2.6561032E+00;  Omega00(0,5,3) = 4.3080676E-04;
+    Omega00(0,6,0) = 0.0000000E+00;  Omega00(0,6,1) = 0.0000000E+00;  Omega00(0,6,2) = 0.0000000E+00;  Omega00(0,6,3) = 0.0000000E+00;
     //N2
-    Omega00(0,0,0) = -6.0614558E-03;  Omega00(0,0,1) = 1.2689102E-01;   Omega00(0,0,2) = -1.0616948E+00;  Omega00(0,0,3) = 8.0955466E+02;
-    Omega00(0,1,0) = -3.7959091E-03;  Omega00(0,1,1) = 9.5708295E-02;   Omega00(0,1,2) = -1.0070611E+00;  Omega00(0,1,3) = 8.9392313E+02;
-    Omega00(0,2,0) = -1.9295666E-03;  Omega00(0,2,1) = 2.7995735E-02;   Omega00(0,2,2) = -3.1588514E-01;  Omega00(0,2,3) = 1.2880734E+02;
-    Omega00(0,3,0) = -1.0796249E-02;  Omega00(0,3,1) = 2.2656509E-01;   Omega00(0,3,2) = -1.7910602E+00;  Omega00(0,3,3) = 4.0455218E+03;
-    Omega00(0,4,0) = -2.7244269E-03;  Omega00(0,4,1) = 6.9587171E-02;   Omega00(0,4,2) = -7.9538667E-01;  Omega00(0,4,3) = 4.0673730E+02;
+    Omega00(1,0,0) = -1.0525124E-02; Omega00(1,0,1) = 1.3498950E-01;  Omega00(1,0,2) = 1.2524805E-01;  Omega00(1,0,3) = 1.5066506E-01;
+    Omega00(1,1,0) = -6.0614558E-03; Omega00(1,1,1) = 1.2689102E-01;  Omega00(1,1,2) = -1.0616948E+00; Omega00(1,1,3) = 8.0955466E+02;
+    Omega00(1,2,0) = -3.7959091E-03; Omega00(1,2,1) = 9.5708295E-02;  Omega00(1,2,2) = -1.0070611E+00; Omega00(1,2,3) = 8.9392313E+02;
+    Omega00(1,3,0) = -1.9295666E-03; Omega00(1,3,1) = 2.7995735E-02;  Omega00(1,3,2) = -3.1588514E-01; Omega00(1,3,3) = 1.2880734E+02;
+    Omega00(1,4,0) = -1.0796249E-02; Omega00(1,4,1) = 2.2656509E-01;  Omega00(1,4,2) = -1.7910602E+00; Omega00(1,4,3) = 4.0455218E+03;
+    Omega00(1,5,0) = -2.7244269E-03; Omega00(1,5,1) = 6.9587171E-02;  Omega00(1,5,2) = -7.9538667E-01; Omega00(1,5,3) = 4.0673730E+02;
+    Omega00(1,6,0) = 0.0000000E+00;  Omega00(1,6,1) = 9.1205839E-02;  Omega00(1,6,2) = -1.8728231E+00; Omega00(1,6,3) = 2.4432020E+05;
     //O2
-    Omega00(2,0,0) = -3.7959091E-03;  Omega00(1,0,1) = 9.5708295E-02;   Omega00(1,0,2) = -1.0070611E+00;  Omega00(1,0,3) = 8.9392313E+02;
-    Omega00(2,1,0) = -8.0682650E-04;  Omega00(1,1,1) = 1.6602480E-02;   Omega00(1,1,2) = -3.1472774E-01;  Omega00(1,1,3) = 1.4116458E+02;
-    Omega00(2,2,0) = -6.4433840E-04;  Omega00(1,2,1) = 8.5378580E-03;   Omega00(1,2,2) = -2.3225102E-01;  Omega00(1,2,3) = 1.1371608E+02;
-    Omega00(2,3,0) = -1.1453028E-03;  Omega00(1,3,1) = 1.2654140E-02;   Omega00(1,3,2) = -2.2435218E-01;  Omega00(1,3,3) = 7.7201588E+01;
-    Omega00(2,4,0) = -4.8405803E-03;  Omega00(1,4,1) = 1.0297688E-01;   Omega00(1,4,2) = -9.6876576E-01;  Omega00(1,4,3) = 6.1629812E+02;
+    Omega00(2,0,0) = 2.3527001E-02;  Omega00(2,0,1) = -6.9632323E-01; Omega00(2,0,2) = 6.8035475E+00;  Omega00(2,0,3) = 1.8335509E-09;
+    Omega00(2,1,0) = -3.7959091E-03; Omega00(2,1,1) = 9.5708295E-02;  Omega00(2,1,2) = -1.0070611E+00; Omega00(2,1,3) = 8.9392313E+02;
+    Omega00(2,2,0) = -8.0682650E-04; Omega00(2,2,1) = 1.6602480E-02;  Omega00(2,2,2) = -3.1472774E-01; Omega00(2,2,3) = 1.4116458E+02;
+    Omega00(2,3,0) = -6.4433840E-04; Omega00(2,3,1) = 8.5378580E-03;  Omega00(2,3,2) = -2.3225102E-01; Omega00(2,3,3) = 1.1371608E+02;
+    Omega00(2,4,0) = -1.1453028E-03; Omega00(2,4,1) = 1.2654140E-02;  Omega00(2,4,2) = -2.2435218E-01; Omega00(2,4,3) = 7.7201588E+01;
+    Omega00(2,5,0) = -4.8405803E-03; Omega00(2,5,1) = 1.0297688E-01;  Omega00(2,5,2) = -9.6876576E-01; Omega00(2,5,3) = 6.1629812E+02;
+    Omega00(2,6,0) = -3.7822765E-03; Omega00(2,6,1) = 1.7967016E-01;  Omega00(2,6,2) = -2.5409098E+00; Omega00(2,6,3) = 1.1840435E+06;
     //NO
-    Omega00(2,0,0) = -1.9295666E-03;  Omega00(2,0,1) = 2.7995735E-02;   Omega00(2,0,2) = -3.1588514E-01;  Omega00(2,0,3) = 1.2880734E+02;
-    Omega00(2,1,0) = -6.4433840E-04;  Omega00(2,1,1) = 8.5378580E-03;   Omega00(2,1,2) = -2.3225102E-01;  Omega00(2,1,3) = 1.1371608E+02;
-    Omega00(2,2,0) = -0.0000000E+00;  Omega00(2,2,1) = -1.1056066E-02;  Omega00(2,2,2) = -5.9216250E-02;  Omega00(2,2,3) = 7.2542367E+01;
-    Omega00(2,3,0) = -1.5770918E-03;  Omega00(2,3,1) = 1.9578381E-02;   Omega00(2,3,2) = -2.7873624E-01;  Omega00(2,3,3) = 9.9547944E+01;
-    Omega00(2,4,0) = -1.0885815E-03;  Omega00(2,4,1) = 1.1883688E-02;   Omega00(2,4,2) = -2.1844909E-01;  Omega00(2,4,3) = 7.5512560E+01;
+    Omega00(3,0,0) = 1.0414818E-01;  Omega00(3,0,1) = -2.8369126E+00; Omega00(3,0,2) = 2.5323135E+01;  Omega00(3,0,3) = 7.7138358E-32;
+    Omega00(3,1,0) = -1.9295666E-03; Omega00(3,1,1) = 2.7995735E-02;  Omega00(3,1,2) = -3.1588514E-01; Omega00(3,1,3) = 1.2880734E+02;
+    Omega00(3,2,0) = -6.4433840E-04; Omega00(3,2,1) = 8.5378580E-03;  Omega00(3,2,2) = -2.3225102E-01; Omega00(3,2,3) = 1.1371608E+02;
+    Omega00(3,3,0) = -0.0000000E+00; Omega00(3,3,1) = -1.1056066E-02; Omega00(3,3,2) = -5.9216250E-02; Omega00(3,3,3) = 7.2542367E+01;
+    Omega00(3,4,0) = -1.5770918E-03; Omega00(3,4,1) = 1.9578381E-02;  Omega00(3,4,2) = -2.7873624E-01; Omega00(3,4,3) = 9.9547944E+01;
+    Omega00(3,5,0) = -1.0885815E-03; Omega00(3,5,1) = 1.1883688E-02;  Omega00(3,5,2) = -2.1844909E-01; Omega00(3,5,3) = 7.5512560E+01;
+    Omega00(3,6,0) = -8.1158474E-03; Omega00(3,6,1) = 2.1474280E-01;  Omega00(3,6,2) = -2.0148450E+00; Omega00(3,6,3) = 6.2986385E+04;
     //N
-    Omega00(3,0,0) = -1.0796249E-02;  Omega00(3,0,1) = 2.2656509E-01;   Omega00(3,0,2) = -1.7910602E+00;  Omega00(3,0,3) = 4.0455218E+03;
-    Omega00(3,1,0) = -1.1453028E-03;  Omega00(3,1,1) = 1.2654140E-02;   Omega00(3,1,2) = -2.2435218E-01;  Omega00(3,1,3) = 7.7201588E+01;
-    Omega00(3,2,0) = -1.5770918E-03;  Omega00(3,2,1) = 1.9578381E-02;   Omega00(3,2,2) = -2.7873624E-01;  Omega00(3,2,3) = 9.9547944E+01;
-    Omega00(3,3,0) = -9.6083779E-03;  Omega00(3,3,1) = 2.0938971E-01;   Omega00(3,3,2) = -1.7386904E+00;  Omega00(3,3,3) = 3.3587983E+03;
-    Omega00(3,4,0) = -7.8147689E-03;  Omega00(3,4,1) = 1.6792705E-01;   Omega00(3,4,2) = -1.4308628E+00;  Omega00(3,4,3) = 1.6628859E+03;
+    Omega00(4,0,0) = 0.0000000E+00;  Omega00(4,0,1) = 1.6554247E-01;  Omega00(4,0,2) = -3.4986344E+00; Omega00(4,0,3) = 5.9268038E+08;
+    Omega00(4,1,0) = -1.0796249E-02; Omega00(4,1,1) = 2.2656509E-01;  Omega00(4,1,2) = -1.7910602E+00; Omega00(4,1,3) = 4.0455218E+03;
+    Omega00(4,2,0) = -1.1453028E-03; Omega00(4,2,1) = 1.2654140E-02;  Omega00(4,2,2) = -2.2435218E-01; Omega00(4,2,3) = 7.7201588E+01;
+    Omega00(4,3,0) = -1.5770918E-03; Omega00(4,3,1) = 1.9578381E-02;  Omega00(4,3,2) = -2.7873624E-01; Omega00(4,3,3) = 9.9547944E+01;
+    Omega00(4,4,0) = -9.6083779E-03; Omega00(4,4,1) = 2.0938971E-01;  Omega00(4,4,2) = -1.7386904E+00; Omega00(4,4,3) = 3.3587983E+03;
+    Omega00(4,5,0) = -7.8147689E-03; Omega00(4,5,1) = 1.6792705E-01;  Omega00(4,5,2) = -1.4308628E+00; Omega00(4,5,3) = 1.6628859E+03;
+    Omega00(4,6,0) = -1.9605234E-02; Omega00(4,6,1) = 5.5570872E-01;  Omega00(4,6,2) = -5.4285702E+00; Omega00(4,6,3) = 1.3574446E+09;
     //O
-    Omega00(4,0,0) = -2.7244269E-03;  Omega00(4,0,1) = 6.9587171E-02;   Omega00(4,0,2) = -7.9538667E-01;  Omega00(4,0,3) = 4.0673730E+02;
-    Omega00(4,1,0) = -4.8405803E-03;  Omega00(4,1,1) = 1.0297688E-01;   Omega00(4,1,2) = -9.6876576E-01;  Omega00(4,1,3) = 6.1629812E+02;
-    Omega00(4,2,0) = -1.0885815E-03;  Omega00(4,2,1) = 1.1883688E-02;   Omega00(4,2,2) = -2.1844909E-01;  Omega00(4,2,3) = 7.5512560E+01;
-    Omega00(4,3,0) = -7.8147689E-03;  Omega00(4,3,1) = 1.6792705E-01;   Omega00(4,3,2) = -1.4308628E+00;  Omega00(4,3,3) = 1.6628859E+03;
-    Omega00(4,4,0) = -6.4040535E-03;  Omega00(4,4,1) = 1.4629949E-01;   Omega00(4,4,2) = -1.3892121E+00;  Omega00(4,4,3) = 2.0903441E+03;
+    Omega00(5,0,0) = 9.9865506E-03;  Omega00(5,0,1) = -2.7407431E-01; Omega00(5,0,2) = 2.6561032E+00;  Omega00(5,0,3) = 4.3080676E-04;
+    Omega00(5,1,0) = -2.7244269E-03; Omega00(5,1,1) = 6.9587171E-02;  Omega00(5,1,2) = -7.9538667E-01; Omega00(5,1,3) = 4.0673730E+02;
+    Omega00(5,2,0) = -4.8405803E-03; Omega00(5,2,1) = 1.0297688E-01;  Omega00(5,2,2) = -9.6876576E-01; Omega00(5,2,3) = 6.1629812E+02;
+    Omega00(5,3,0) = -1.0885815E-03; Omega00(5,3,1) = 1.1883688E-02;  Omega00(5,3,2) = -2.1844909E-01; Omega00(5,3,3) = 7.5512560E+01;
+    Omega00(5,4,0) = -7.8147689E-03; Omega00(5,4,1) = 1.6792705E-01;  Omega00(5,4,2) = -1.4308628E+00; Omega00(5,4,3) = 1.6628859E+03;
+    Omega00(5,5,0) = -6.4040535E-03; Omega00(5,5,1) = 1.4629949E-01;  Omega00(5,5,2) = -1.3892121E+00; Omega00(5,5,3) = 2.0903441E+03;
+    Omega00(5,6,0) = -1.6409054E-02; Omega00(5,6,1) = 4.6352852E-01;  Omega00(5,6,2) = -4.5479735E+00; Omega00(5,6,3) = 7.4250671E+07;
+    //NO+
+    Omega00(6,0,0) = 0.0000000E+00;  Omega00(6,0,1) = 0.0000000E+00;  Omega00(6,0,2) = 0.0000000E+00;  Omega00(6,0,3) = 0.0000000E+00;
+    Omega00(6,1,0) = 0.0000000E+00;  Omega00(6,1,1) = 9.1205839E-02;  Omega00(6,1,2) = -1.8728231E+00; Omega00(6,1,3) = 2.4432020E+05;
+    Omega00(6,2,0) = -3.7822765E-03; Omega00(6,2,1) = 1.7967016E-01;  Omega00(6,2,2) = -2.5409098E+00; Omega00(6,2,3) = 1.1840435E+06;
+    Omega00(6,3,0) = -8.1158474E-03; Omega00(6,3,1) = 2.1474280E-01;  Omega00(6,3,2) = -2.0148450E+00; Omega00(6,3,3) = 6.2986385E+04;
+    Omega00(6,4,0) = -1.9605234E-02; Omega00(6,4,1) = 5.5570872E-01;  Omega00(6,4,2) = -5.4285702E+00; Omega00(6,4,3) = 1.3574446E+09;
+    Omega00(6,5,0) = -1.6409054E-02; Omega00(6,5,1) = 4.6352852E-01;  Omega00(6,5,2) = -4.5479735E+00; Omega00(6,5,3) = 7.4250671E+07;
+    Omega00(6,6,0) = 0.0000000E+00;  Omega00(6,6,1) = 0.0000000E+00;  Omega00(6,6,2) = 0.0000000E+00;  Omega00(6,6,3) = 0.0000000E+00;
+
 
     // Omega(1,1) ----------------------
+    //e-    (TODO: NO+ and e-,  NO+ and NO+, e- and e- ??????)
+    Omega11(0,0,0) = 0.0000000E+00;  Omega11(0,0,1) = 0.0000000E+00;  Omega11(0,0,2) = 0.0000000E+00;  Omega11(0,0,3) = 0.0000000E+00;
+    Omega11(0,1,0) = -4.2254948E-03; Omega11(0,1,1) = -5.2965163E-02; Omega11(0,1,2) = 1.9157708E+00;  Omega11(0,1,3) = 6.3263309E-04;
+    Omega11(0,2,0) = 9.6744867E-03;  Omega11(0,2,1) = -3.3759583E-01; Omega11(0,2,2) = 3.7952121E+00;  Omega11(0,2,3) = 6.8468036E-06;
+    Omega11(0,3,0) = 0.0000000E+00;  Omega11(0,3,1) = 5.4444485E-02;  Omega11(0,3,2) = -1.2854128E+00; Omega11(0,3,3) = 1.3857556E+04;
+    Omega11(0,4,0) = -1.0903638E-01; Omega11(0,4,1) = 2.8678381E+00;  Omega11(0,4,2) = -2.5297550E+01; Omega11(0,4,3) = 3.4838798E+33;
+    Omega11(0,5,0) = -1.7924100E-02; Omega11(0,5,1) = 4.0402656E-01;  Omega11(0,5,2) = -2.6712374E+00; Omega11(0,5,3) = 4.1447669E+02;
+    Omega11(0,6,0) = 0.0000000E+00;  Omega11(0,6,1) = 0.0000000E+00;  Omega11(0,6,2) = 0.0000000E+00;  Omega11(0,6,3) = 0.0000000E+00;
     //N2
-    Omega11(0,0,0) = -7.6303990E-03;  Omega11(0,0,1) = 1.6878089E-01;   Omega11(0,0,2) = -1.4004234E+00;  Omega11(0,0,3) = 2.1427708E+03;
-    Omega11(0,1,0) = -8.0457321E-03;  Omega11(0,1,1) = 1.9228905E-01;   Omega11(0,1,2) = -1.7102854E+00;  Omega11(0,1,3) = 5.2213857E+03;
-    Omega11(0,2,0) = -6.8237776E-03;  Omega11(0,2,1) = 1.4360616E-01;   Omega11(0,2,2) = -1.1922240E+00;  Omega11(0,2,3) = 1.2433086E+03;
-    Omega11(0,3,0) = -8.3493693E-03;  Omega11(0,3,1) = 1.7808911E-01;   Omega11(0,3,2) = -1.4466155E+00;  Omega11(0,3,3) = 1.9324210E+03;
-    Omega11(0,4,0) = -8.3110691E-03;  Omega11(0,4,1) = 1.9617877E-01;   Omega11(0,4,2) = -1.7205427E+00;  Omega11(0,4,3) = 4.0812829E+03;
+    Omega11(1,0,0) = -4.2254948E-03; Omega11(1,0,1) = -5.2965163E-02; Omega11(1,0,2) = 1.9157708E+00;  Omega11(1,0,3) = 6.3263309E-04;
+    Omega11(1,1,0) = -7.6303990E-03; Omega11(1,1,1) = 1.6878089E-01;  Omega11(1,1,2) = -1.4004234E+00; Omega11(1,1,3) = 2.1427708E+03;
+    Omega11(1,2,0) = -8.0457321E-03; Omega11(1,2,1) = 1.9228905E-01;  Omega11(1,2,2) = -1.7102854E+00; Omega11(1,2,3) = 5.2213857E+03;
+    Omega11(1,3,0) = -6.8237776E-03; Omega11(1,3,1) = 1.4360616E-01;  Omega11(1,3,2) = -1.1922240E+00; Omega11(1,3,3) = 1.2433086E+03;
+    Omega11(1,4,0) = -8.3493693E-03; Omega11(1,4,1) = 1.7808911E-01;  Omega11(1,4,2) = -1.4466155E+00; Omega11(1,4,3) = 1.9324210E+03;
+    Omega11(1,5,0) = -8.3110691E-03; Omega11(1,5,1) = 1.9617877E-01;  Omega11(1,5,2) = -1.7205427E+00; Omega11(1,5,3) = 4.0812829E+03;
+    Omega11(1,6,0) = 0.0000000E+00;  Omega11(1,6,1) = 8.5112236E-02;  Omega11(1,6,2) = -1.7460044E+00; Omega11(1,6,3) = 1.4498969E+05;
     //O2
-    Omega11(1,0,0) = -8.0457321E-03;  Omega11(1,0,1) = 1.9228905E-01;   Omega11(1,0,2) = -1.7102854E+00;  Omega11(1,0,3) = 5.2213857E+03;
-    Omega11(1,1,0) = -6.2931612E-03;  Omega11(1,1,1) = 1.4624645E-01;   Omega11(1,1,2) = -1.3006927E+00;  Omega11(1,1,3) = 1.8066892E+03;
-    Omega11(1,2,0) = -6.8508672E-03;  Omega11(1,2,1) = 1.5524564E-01;   Omega11(1,2,2) = -1.3479583E+00;  Omega11(1,2,3) = 2.0037890E+03;
-    Omega11(1,3,0) = -1.0608832E-03;  Omega11(1,3,1) = 1.1782595E-02;   Omega11(1,3,2) = -2.1246301E-01;  Omega11(1,3,3) = 8.4561598E+01;
-    Omega11(1,4,0) = -3.7969686E-03;  Omega11(1,4,1) = 7.6789981E-02;   Omega11(1,4,2) = -7.3056809E-01;  Omega11(1,4,3) = 3.3958171E+02;
+    Omega11(2,0,0) = 9.6744867E-03;  Omega11(2,0,1) = -3.3759583E-01; Omega11(2,0,2) = 3.7952121E+00;  Omega11(2,0,3) = 6.8468036E-06;
+    Omega11(2,1,0) = -8.0457321E-03; Omega11(2,1,1) = 1.9228905E-01;  Omega11(2,1,2) = -1.7102854E+00; Omega11(2,1,3) = 5.2213857E+03;
+    Omega11(2,2,0) = -6.2931612E-03; Omega11(2,2,1) = 1.4624645E-01;  Omega11(2,2,2) = -1.3006927E+00; Omega11(2,2,3) = 1.8066892E+03;
+    Omega11(2,3,0) = -6.8508672E-03; Omega11(2,3,1) = 1.5524564E-01;  Omega11(2,3,2) = -1.3479583E+00; Omega11(2,3,3) = 2.0037890E+03;
+    Omega11(2,4,0) = -1.0608832E-03; Omega11(2,4,1) = 1.1782595E-02;  Omega11(2,4,2) = -2.1246301E-01; Omega11(2,4,3) = 8.4561598E+01;
+    Omega11(2,5,0) = -3.7969686E-03; Omega11(2,5,1) = 7.6789981E-02;  Omega11(2,5,2) = -7.3056809E-01; Omega11(2,5,3) = 3.3958171E+02;
+    Omega11(2,6,0) = 0.0000000E+00;  Omega11(2,6,1) = 8.4737359E-02;  Omega11(2,6,2) = -1.7290488E+00; Omega11(2,6,3) = 1.2485194E+05;
     //NO
-    Omega11(2,0,0) = -6.8237776E-03;  Omega11(2,0,1) = 1.4360616E-01;   Omega11(2,0,2) = -1.1922240E+00;  Omega11(2,0,3) = 1.2433086E+03;
-    Omega11(2,1,0) = -6.8508672E-03;  Omega11(2,1,1) = 1.5524564E-01;   Omega11(2,1,2) = -1.3479583E+00;  Omega11(2,1,3) = 2.0037890E+03;
-    Omega11(2,2,0) = -7.4942466E-03;  Omega11(2,2,1) = 1.6626193E-01;   Omega11(2,2,2) = -1.4107027E+00;  Omega11(2,2,3) = 2.3097604E+03;
-    Omega11(2,3,0) = -1.4719259E-03;  Omega11(2,3,1) = 1.8446968E-02;   Omega11(2,3,2) = -2.6460411E-01;  Omega11(2,3,3) = 1.0911124E+02;
-    Omega11(2,4,0) = -1.0066279E-03;  Omega11(2,4,1) = 1.1029264E-02;   Omega11(2,4,2) = -2.0671266E-01;  Omega11(2,4,3) = 8.2644384E+01;
+    Omega11(3,0,0) = 0.0000000E+00;  Omega11(0,3,1) = 5.4444485E-02;  Omega11(0,3,2) = -1.2854128E+00; Omega11(0,3,3) = 1.3857556E+04;
+    Omega11(3,1,0) = -6.8237776E-03; Omega11(3,1,1) = 1.4360616E-01;  Omega11(3,1,2) = -1.1922240E+00; Omega11(3,1,3) = 1.2433086E+03;
+    Omega11(3,2,0) = -6.8508672E-03; Omega11(3,2,1) = 1.5524564E-01;  Omega11(3,2,2) = -1.3479583E+00; Omega11(3,2,3) = 2.0037890E+03;
+    Omega11(3,3,0) = -7.4942466E-03; Omega11(3,3,1) = 1.6626193E-01;  Omega11(3,3,2) = -1.4107027E+00; Omega11(3,3,3) = 2.3097604E+03;
+    Omega11(3,4,0) = -1.4719259E-03; Omega11(3,4,1) = 1.8446968E-02;  Omega11(3,4,2) = -2.6460411E-01; Omega11(3,4,3) = 1.0911124E+02;
+    Omega11(3,5,0) = -1.0066279E-03; Omega11(3,5,1) = 1.1029264E-02;  Omega11(3,5,2) = -2.0671266E-01; Omega11(3,5,3) = 8.2644384E+01;
+    Omega11(3,6,0) = 1.1055777E-02;  Omega11(3,6,1) = -1.6621846E-01; Omega11(3,6,2) = 1.4372166E-01;  Omega11(3,6,3) = 1.3182061E+03;
     //N
-    Omega11(3,0,0) = -8.3493693E-03;  Omega11(3,0,1) = 1.7808911E-01;   Omega11(3,0,2) = -1.4466155E+00;  Omega11(3,0,3) = 1.9324210E+03;
-    Omega11(3,1,0) = -1.0608832E-03;  Omega11(3,1,1) = 1.1782595E-02;   Omega11(3,1,2) = -2.1246301E-01;  Omega11(3,1,3) = 8.4561598E+01;
-    Omega11(3,2,0) = -1.4719259E-03;  Omega11(3,2,1) = 1.8446968E-02;   Omega11(3,2,2) = -2.6460411E-01;  Omega11(3,2,3) = 1.0911124E+02;
-    Omega11(3,3,0) = -7.7439615E-03;  Omega11(3,3,1) = 1.7129007E-01;   Omega11(3,3,2) = -1.4809088E+00;  Omega11(3,3,3) = 2.1284951E+03;
-    Omega11(3,4,0) = -5.0478143E-03;  Omega11(3,4,1) = 1.0236186E-01;   Omega11(3,4,2) = -9.0058935E-01;  Omega11(3,4,3) = 4.4472565E+02;
+    Omega11(4,0,0) = -1.0903638E-01; Omega11(4,0,1) = 2.8678381E+00;  Omega11(4,0,2) = -2.5297550E+01; Omega11(4,0,3) = 3.4838798E+33;
+    Omega11(4,1,0) = -8.3493693E-03; Omega11(4,1,1) = 1.7808911E-01;  Omega11(4,1,2) = -1.4466155E+00; Omega11(4,1,3) = 1.9324210E+03;
+    Omega11(4,2,0) = -1.0608832E-03; Omega11(4,2,1) = 1.1782595E-02;  Omega11(4,2,2) = -2.1246301E-01; Omega11(4,2,3) = 8.4561598E+01;
+    Omega11(4,3,0) = -1.4719259E-03; Omega11(4,3,1) = 1.8446968E-02;  Omega11(4,3,2) = -2.6460411E-01; Omega11(4,3,3) = 1.0911124E+02;
+    Omega11(4,4,0) = -7.7439615E-03; Omega11(4,4,1) = 1.7129007E-01;  Omega11(4,4,2) = -1.4809088E+00; Omega11(4,4,3) = 2.1284951E+03;
+    Omega11(4,5,0) = -5.0478143E-03; Omega11(4,5,1) = 1.0236186E-01;  Omega11(4,5,2) = -9.0058935E-01; Omega11(4,5,3) = 4.4472565E+02;
+    Omega11(4,6,0) = -2.1009546E-02; Omega11(4,6,1) = 5.8910426E-01;  Omega11(4,6,2) = -5.6681361E+00; Omega11(4,6,3) = 2.4486594E+09;
     //O
-    Omega11(4,0,0) = -8.3110691E-03;  Omega11(4,0,1) = 1.9617877E-01;   Omega11(4,0,2) = -1.7205427E+00;  Omega11(4,0,3) = 4.0812829E+03;
-    Omega11(4,1,0) = -3.7969686E-03;  Omega11(4,1,1) = 7.6789981E-02;   Omega11(4,1,2) = -7.3056809E-01;  Omega11(4,1,3) = 3.3958171E+02;
-    Omega11(4,2,0) = -1.0066279E-03;  Omega11(4,2,1) = 1.1029264E-02;   Omega11(4,2,2) = -2.0671266E-01;  Omega11(4,2,3) = 8.2644384E+01;
-    Omega11(4,3,0) = -5.0478143E-03;  Omega11(4,3,1) = 1.0236186E-01;   Omega11(4,3,2) = -9.0058935E-01;  Omega11(4,3,3) = 4.4472565E+02;
-    Omega11(4,4,0) = -4.2451096E-03;  Omega11(4,4,1) = 9.6820337E-02;   Omega11(4,4,2) = -9.9770795E-01;  Omega11(4,4,3) = 8.3320644E+02;
+    Omega11(5,0,0) = -1.7924100E-02; Omega11(5,0,1) = 4.0402656E-01;  Omega11(5,0,2) = -2.6712374E+00; Omega11(5,0,3) = 4.1447669E+02;
+    Omega11(5,1,0) = -8.3110691E-03; Omega11(5,1,1) = 1.9617877E-01;  Omega11(5,1,2) = -1.7205427E+00; Omega11(5,1,3) = 4.0812829E+03;
+    Omega11(5,2,0) = -3.7969686E-03; Omega11(5,2,1) = 7.6789981E-02;  Omega11(5,2,2) = -7.3056809E-01; Omega11(5,2,3) = 3.3958171E+02;
+    Omega11(5,3,0) = -1.0066279E-03; Omega11(5,3,1) = 1.1029264E-02;  Omega11(5,3,2) = -2.0671266E-01; Omega11(5,3,3) = 8.2644384E+01;
+    Omega11(5,4,0) = -5.0478143E-03; Omega11(5,4,1) = 1.0236186E-01;  Omega11(5,4,2) = -9.0058935E-01; Omega11(5,4,3) = 4.4472565E+02;
+    Omega11(5,5,0) = -4.2451096E-03; Omega11(5,5,1) = 9.6820337E-02;  Omega11(5,5,2) = -9.9770795E-01; Omega11(5,5,3) = 8.3320644E+02;
+    Omega11(5,6,0) = -1.5315132E-02; Omega11(5,6,1) = 4.3541627E-01;  Omega11(5,6,2) = -4.2864279E+00; Omega11(5,6,3) = 3.5125207E+07;
+    //NO+
+    Omega11(6,0,0) = 0.0000000E+00;  Omega11(6,0,1) = 0.0000000E+00;  Omega11(6,0,2) = 0.0000000E+00;  Omega11(6,0,3) = 0.0000000E+00;
+    Omega11(6,1,0) = 0.0000000E+00;  Omega11(6,1,1) = 8.5112236E-02;  Omega11(6,1,2) = -1.7460044E+00; Omega11(6,1,3) = 1.4498969E+05;
+    Omega11(6,2,0) = 0.0000000E+00;  Omega11(6,2,1) = 8.4737359E-02;  Omega11(6,2,2) = -1.7290488E+00; Omega11(6,2,3) = 1.2485194E+05;
+    Omega11(6,3,0) = 1.1055777E-02;  Omega11(6,3,1) = -1.6621846E-01; Omega11(6,3,2) = 1.4372166E-01;  Omega11(6,3,3) = 1.3182061E+03;
+    Omega11(6,4,0) = -2.1009546E-02; Omega11(6,4,1) = 5.8910426E-01;  Omega11(6,4,2) = -5.6681361E+00; Omega11(6,4,3) = 2.4486594E+09;
+    Omega11(6,5,0) = -1.5315132E-02; Omega11(6,5,1) = 4.3541627E-01;  Omega11(6,5,2) = -4.2864279E+00; Omega11(6,5,3) = 3.5125207E+07;
+    Omega11(6,6,0) = 0.0000000E+00;  Omega11(6,6,1) = 0.0000000E+00;  Omega11(6,6,2) = 0.0000000E+00;  Omega11(6,6,3) = 0.0000000E+00;
 
     // Creation/Destruction (+1/-1), Index of monoatomic reactants
     // Monoatomic species (N,O) recombine into diaatomic (N2, O2)

From e816d6e25b67fe5a2ff9d5ffc2173197ae96e33f Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 13 Dec 2022 10:56:45 +0100
Subject: [PATCH 077/656] Added comments, made table display function
 compatible with 3D tables

---
 Common/include/containers/CLookUpTable.hpp |  69 ++++--
 Common/src/containers/CFileReaderLUT.cpp   |  14 +-
 Common/src/containers/CLookUpTable.cpp     | 274 ++++++++++++++-------
 Common/src/containers/CTrapezoidalMap.cpp  |   7 -
 4 files changed, 239 insertions(+), 125 deletions(-)

diff --git a/Common/include/containers/CLookUpTable.hpp b/Common/include/containers/CLookUpTable.hpp
index 0ccee3585c5..a281c7a35ef 100644
--- a/Common/include/containers/CLookUpTable.hpp
+++ b/Common/include/containers/CLookUpTable.hpp
@@ -44,21 +44,23 @@ class CLookUpTable {
  protected:
   int rank; /*!< \brief MPI Rank. */
 
-  std::string file_name_lut;
-  std::string version_lut;
-  std::string version_reader;
-  std::string name_CV1,   // Name of controlling variable 1 
-              name_CV2;   // Name of xontrolling variable 2
-
-  unsigned long *n_points;
-  unsigned long *n_triangles;
-  unsigned long n_variables;
-  unsigned long *n_hull_points;
-  unsigned long n_table_levels = 1;
-  su2double *z_values_levels = nullptr;
+  std::string file_name_lut,  // LUT file name.
+              version_lut,    // LUT version as specified in LUT file.
+              version_reader, // Reader version (should be equal or above LUT version).
+              name_CV1,       // Name of controlling variable 1.
+              name_CV2;       // Name of xontrolling variable 2.
 
+  unsigned long *n_points,          // Number of data points per table level.
+                *n_triangles,       // Cell count per table level.
+                *n_hull_points,     // Number of boundary points per table level.
+                n_variables,        // Number of variables stored in the table.
+                n_table_levels = 1; // Number of table levels in the z-direction.
+
+  su2double *z_values_levels = nullptr; // Constant z-values of each table level.
+
+  unsigned short table_dim = 2; // Table dimension.
   /*! 
-   * \brief the lower and upper limits of the z, y and x variable.
+   * \brief the lower and upper limits of the z, y and x variable for each table level.
    */
   std::pair<su2double, su2double> limits_table_z;
   std::pair<su2double, su2double> *limits_table_y;
@@ -75,8 +77,15 @@ class CLookUpTable {
    */
   su2activematrix *table_data;
 
+  /*! \brief
+   * Holds all connectivity data stored in the table for each level. First index 
+   * addresses the variable while second index addresses the point.
+   */
   su2matrix<unsigned long> *triangles;
 
+  /*! \brief
+   * Edge information for each table level.
+   */
   std::vector<su2vector<unsigned long> > *edges;
   su2vector<std::vector<unsigned long> > *edge_to_triangle;
 
@@ -85,6 +94,9 @@ class CLookUpTable {
    */
   su2vector<unsigned long> *hull;
 
+  /*! \brief 
+   * Trapezoidal map objects for the table levels.
+   */
   CTrapezoidalMap *trap_map_x_y;
 
   /*! \brief 
@@ -170,10 +182,29 @@ class CLookUpTable {
   su2double Interpolate(const su2double* val_samples, std::array<unsigned long,3>& val_triangle,
                         std::array<su2double,3>& val_interp_coeffs);
 
-  void Linear_Interpolation(su2double val_z, std::pair<unsigned long, unsigned long> &inclusion_levels, su2double&lower_value,su2double&upper_value, su2double*&var_vals);
+  
+  /*!
+   * \brief Perform linear interpolation between two table levels for a single variable.
+   * \param[in] val_z - z-coordinate of the query point.
+   * \param[in] lower_level - Table level index of the table level directly below the query point.
+   * \param[in] upper_level - Table level index of the table level directly above the query point.
+   * \param[in] lower_value - Result from x-y interpolation on the lower table level.
+   * \param[in] upper_value - Result from x-y interpolation on the upper table level.
+   * \param[in] val_vars - Pointer to interpolation result.
+  */
+  void Linear_Interpolation(const su2double val_z, const unsigned long lower_level, const unsigned long upper_level, su2double&lower_value,su2double&upper_value, su2double*&var_vals);
 
 
-  void Linear_Interpolation(su2double val_z, std::pair<unsigned long, unsigned long> &inclusion_levels, std::vector<su2double>&lower_values,std::vector<su2double>&upper_values, std::vector<su2double*>&var_vals);
+  /*!
+   * \brief Perform linear interpolation between two table levels for a vector of variables.
+   * \param[in] val_z - z-coordinate of the query point.
+   * \param[in] lower_level - Table level index of the table level directly below the query point.
+   * \param[in] upper_level - Table level index of the table level directly above the query point.
+   * \param[in] lower_values - Results from x-y interpolation on the lower table level.
+   * \param[in] upper_values - Results from x-y interpolation on the upper table level.
+   * \param[in] val_vars - Pointer to interpolation results for all interpolation variables.
+  */
+  void Linear_Interpolation(const su2double val_z, const unsigned long lower_level, const unsigned long upper_level, std::vector<su2double>&lower_values,std::vector<su2double>&upper_values, std::vector<su2double*>&var_vals);
 
   /*!
    * \brief find the point on the hull (boundary of the table) that is closest to the point P(val_x,val_y).
@@ -310,7 +341,13 @@ class CLookUpTable {
   unsigned long LookUp_XYZ(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars, su2double val_x,
                                 su2double val_y, su2double val_z=0);
   
-  std::pair<unsigned long, unsigned long> FindInclusionLevels(su2double val_z, bool *within_limits);
+  /*!
+  * \brief Find the table levels with constant z-values directly above and below query val_z.
+  * \param[in] val_z - Z-coordinate of query point.
+  * \param[in] within_limits - Whether query point lies within table bounds.
+  * \returns pair of inclusion level indices (first = lower level index, second = upper level index)
+  */
+  std::pair<unsigned long, unsigned long> FindInclusionLevels(const su2double val_z, bool *within_limits);
 
   /*!
    * \brief determine the minimum and maximum value of the second controlling variable.
diff --git a/Common/src/containers/CFileReaderLUT.cpp b/Common/src/containers/CFileReaderLUT.cpp
index 191e88a08dd..1fd99cf5f77 100644
--- a/Common/src/containers/CFileReaderLUT.cpp
+++ b/Common/src/containers/CFileReaderLUT.cpp
@@ -34,7 +34,7 @@
 using namespace std;
 
 void CFileReaderLUT::ReadRawLUT(const string& file_name) {
-  version_reader = "1.0.1";
+  version_reader = "1.1.0";
 
   /*--- Store MPI rank. ---*/
   rank = SU2_MPI::GetRank();
@@ -280,12 +280,6 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
     
   }
 
-  if (n_triangles[0] != triCounter)
-    SU2_MPI::Error(
-        "Number of read triangles does not match number of points "
-        "specified in lookup table library header.",
-        CURRENT_FUNCTION);
-
   /*--- read hull points ---*/
   if (rank == MASTER_NODE) cout << "loading hull block" << endl;
 
@@ -328,12 +322,6 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
       }
   }
 
-  if (n_hull_points[0] != hullCounter)
-    SU2_MPI::Error(
-        "Number of read hull points does not match number of points "
-        "specified in lookup table library header.",
-        CURRENT_FUNCTION);
-
   file_stream.close();
 
 }
diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index b53763ec4ee..addf38e2eaa 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -56,20 +56,57 @@ CLookUpTable::CLookUpTable(const string& var_file_name_lut, const string& name_x
   PrintTableInfo();
 
   if (rank == MASTER_NODE)
+  switch (table_dim)
+  {
+  case 2:
     cout << "Building a trapezoidal map for the (" + name_x + ", " + name_y + ") "
             "space ..."
          << endl;
+    break;
+  case 3:
+    cout << "Building trapezoidal map stack for the (" + name_x + ", " + name_y + ") "
+              "space ..."
+          << endl;
+    break;
+  default:
+    break;
+  }
+
   trap_map_x_y = new CTrapezoidalMap[n_table_levels];
-  for(auto i_level = 0ul; i_level<n_table_levels; i_level++)
+  su2double startTime = SU2_MPI::Wtime();
+  for(auto i_level = 0ul; i_level<n_table_levels; i_level++){
     trap_map_x_y[i_level] = CTrapezoidalMap(GetDataP(name_x, i_level), GetDataP(name_y, i_level), table_data[i_level].cols(), edges[i_level], edge_to_triangle[i_level]);
-
-  if (rank == MASTER_NODE) 
-    cout << " done." << endl;
-
-  if (rank == MASTER_NODE) 
+    /* Display a progress bar to monitor table generation process */
+    if(rank == MASTER_NODE){
+      su2double progress = su2double(i_level) / n_table_levels;
+      unsigned short barwidth = 65;
+      int pos = barwidth * progress;
+      cout << "[";
+      for(int iBar=0; iBar<barwidth; ++iBar){
+          if(iBar < pos) cout << "=";
+          else cout << " ";
+      }
+      cout << "] "<< int(100*progress) << " %\r";
+      cout.flush();
+    }
+  }
+  su2double stopTime = SU2_MPI::Wtime();
+
+  if (rank == MASTER_NODE){
+    switch (table_dim)
+    {
+    case 2:
+      cout << "Construction of trapezoidal map took " << stopTime-startTime << " seconds\n" << endl;
+      break;
+    case 3:
+      cout << "Construction of trapezoidal map stack took " << stopTime-startTime << " seconds\n" << endl;
+      break;
+    default:
+      break;
+    }
     cout << "Precomputing interpolation coefficients..." << endl;
-  
-
+  }
+    
   ComputeInterpCoeffs();
 
   if (rank == MASTER_NODE) 
@@ -100,7 +137,7 @@ void CLookUpTable::LoadTableRaw(const string& var_file_name_lut) {
     cout << "Loading lookup table, filename = " << var_file_name_lut << " ..." << endl;
 
   file_reader.ReadRawLUT(var_file_name_lut);
-  unsigned short table_dim = file_reader.GetTableDim();
+  table_dim = file_reader.GetTableDim();
   n_table_levels = file_reader.GetNLevels();
 
   n_points            = new unsigned long[n_table_levels];
@@ -154,10 +191,16 @@ void CLookUpTable::FindTableLimits(const string& name_cv1, const string& name_cv
     limits_table_x[i_level] = make_pair(min_x, max_x);
     limits_table_y[i_level] = make_pair(min_y, max_y);
   }
+
+  if(table_dim = 3){
+    su2double min_z, max_z;
+    min_z = *min_element(z_values_levels, z_values_levels + n_table_levels);
+    max_z = *max_element(z_values_levels, z_values_levels + n_table_levels);
+    limits_table_z = make_pair(min_z, max_z);
+  }
 }
 
 void CLookUpTable::PrintTableInfo() {
-  //TODO: make compatible with 3D table
   if (rank == MASTER_NODE) {
     cout << setfill(' ');
     cout << endl;
@@ -167,25 +210,66 @@ void CLookUpTable::PrintTableInfo() {
     cout << "| File name:" << setw(54) << right << file_name_lut << " |" << endl;
     cout << "| Table version:" << setw(50) << right << version_lut << " |" << endl;
     cout << "| Table reader version:" << setw(43) << right << version_reader << " |" << endl;
+    cout << "| Table dimension:" << setw(48) << right << table_dim << " |" << endl;
     cout << "| Number of variables:" << setw(44) << right << n_variables << " |" << endl;
-    cout << "| Number of points:" << setw(47) << right << n_points[0] << " |" << endl;
-    cout << "| Number of triangles:" << setw(44) << right << n_triangles[0] << " |" << endl;
-    cout << "| Number of edges:" << setw(48) << right << edges[0].size() << " |" << endl;
-    cout << "+------------------------------------------------------------------+" << endl;
-    cout << "| Minimum Y:" << setw(47) << right << limits_table_y[0].first << " |" << endl;
-    cout << "| Maximum Y:" << setw(47) << right << limits_table_y[0].second << " |" << endl;
-    cout << "| Minimum X:" << setw(38) << right << limits_table_x[0].first << " |" << endl;
-    cout << "| Maximum X:" << setw(38) << right << limits_table_x[0].second << " |" << endl;
-    cout << "+------------------------------------------------------------------+" << endl;
-    cout << "| Variable names:                                                  |" << endl;
-    cout << "|                                                                  |" << endl;
 
-    for (unsigned long i_var = 0; i_var < names_var.size(); i_var++)
-      cout << "| " << right << setw(3) << i_var << ": " << left << setw(59) << names_var[i_var] << " |" << endl;
-
-    cout << "+------------------------------------------------------------------+" << endl;
-
-    cout << endl;
+    su2double n_points_av = 0, n_tria_av = 0, n_edges_av = 0, min_x=1/EPS, max_x = -1/EPS, min_y=1/EPS, max_y = -1/EPS;
+    for(auto i_level=0ul; i_level<n_table_levels; i_level++){
+      n_points_av += n_points[i_level] / n_table_levels;
+      n_tria_av += n_triangles[i_level] / n_table_levels;
+      n_edges_av += edges[i_level].size() / n_table_levels;
+      min_x = min(min_x, limits_table_x[i_level].first);
+      min_y = min(min_y, limits_table_y[i_level].first);
+      max_x = max(max_x, limits_table_x[i_level].second);
+      max_y = max(max_y, limits_table_y[i_level].second);
+    }
+    switch (table_dim)
+    {
+    case 2:
+      cout << "| Number of points:" << setw(47) << right << n_points_av << " |" << endl;
+      cout << "| Number of triangles:" << setw(44) << right << n_tria_av << " |" << endl;
+      cout << "| Number of edges:" << setw(48) << right << n_edges_av << " |" << endl;
+      cout << "+------------------------------------------------------------------+" << endl;
+      cout << "| Minimum Y:" << setw(54) << right << min_y << " |" << endl;
+      cout << "| Maximum Y:" << setw(54) << right << max_y << " |" << endl;
+      cout << "| Minimum X:" << setw(54) << right << min_x << " |" << endl;
+      cout << "| Maximum X:" << setw(54) << right << max_x << " |" << endl;
+      cout << "+------------------------------------------------------------------+" << endl;
+      cout << "| Variable names:                                                  |" << endl;
+      cout << "|                                                                  |" << endl;
+
+      for (unsigned long i_var = 0; i_var < names_var.size(); i_var++)
+        cout << "| " << right << setw(3) << i_var << ": " << left << setw(59) << names_var[i_var] << " |" << endl;
+
+      cout << "+------------------------------------------------------------------+" << endl;
+
+      cout << endl;
+      break;
+    case 3:
+      
+      cout << "| Number of table levels:" << setw(41) << right << n_table_levels << " |" << endl;
+      cout << "| Average number of points:" << setw(39) << right << floor(n_points_av) << " |" << endl;
+      cout << "| Average number of triangles:" << setw(36) << right << floor(n_tria_av) << " |" << endl;
+      cout << "| Average number of edges:" << setw(40) << right << floor(n_edges_av) << " |" << endl;
+      cout << "+------------------------------------------------------------------+" << endl;
+      cout << "| Minimum Z:" << setw(54) << right << limits_table_z.first << " |" << endl;
+      cout << "| Maximum Z:" << setw(54) << right << limits_table_z.second << " |" << endl;
+      cout << "| Minimum Y:" << setw(54) << right << min_y << " |" << endl;
+      cout << "| Maximum Y:" << setw(54) << right << max_y << " |" << endl;
+      cout << "| Minimum X:" << setw(54) << right << min_x << " |" << endl;
+      cout << "| Maximum X:" << setw(54) << right << max_x << " |" << endl;
+      cout << "+------------------------------------------------------------------+" << endl;
+      cout << "| Variable names:                                                  |" << endl;
+      cout << "|                                                                  |" << endl;
+
+      for (unsigned long i_var = 0; i_var < names_var.size(); i_var++)
+        cout << "| " << right << setw(3) << i_var << ": " << left << setw(59) << names_var[i_var] << " |" << endl;
+
+      cout << "+------------------------------------------------------------------+" << endl;
+      break;
+    default:
+      break;
+    }
   }
 }
 
@@ -348,113 +432,124 @@ void CLookUpTable::GetInterpMatInv(const su2double* vec_x, const su2double* vec_
 
 }
 
-std::pair<unsigned long, unsigned long> CLookUpTable::FindInclusionLevels(su2double val_z, bool*within_table_limits)
+std::pair<unsigned long, unsigned long> CLookUpTable::FindInclusionLevels(const su2double val_z, bool*within_table_limits)
 {
-  std::pair<unsigned long, unsigned long> inclusion_levels;
+  /*--- Find the table levels with constant z-values directly below and above the query value val_z ---*/
+
+  /* Check if val_z lies outside table bounds */
   if(val_z >= limits_table_z.second){
     *within_table_limits = false;
-    inclusion_levels = std::make_pair(n_table_levels-1, n_table_levels-1);
+    return std::make_pair(n_table_levels-1, n_table_levels-1);
   }else if(val_z <= limits_table_z.first){
     *within_table_limits = false;
-    inclusion_levels = std::make_pair(0, 0);
+    return std::make_pair(0, 0);
   }else{
+    std::pair<unsigned long, unsigned long> inclusion_levels;
+    /* Loop over table levels to find the levels directly above and below the query value */
     for(auto i_level = 0ul; i_level < n_table_levels-1; i_level++){
       if((val_z >= z_values_levels[i_level]) && (val_z < z_values_levels[i_level+1])){
         *within_table_limits = true;
         inclusion_levels = std::make_pair(i_level, i_level+1);
       }
     }
+    return inclusion_levels;
   }
-  return inclusion_levels;
 }
 
 unsigned long CLookUpTable::LookUp_XYZ(const std::string& val_name_var, su2double* val_var, su2double val_x,
                                 su2double val_y, su2double val_z)
 {
-  bool within_z_limits, exit_code;
-  unsigned long lower_level, upper_level;
-  std::pair<unsigned long, unsigned long> inclusion_levels;
-  if(val_z == 0){
-    inclusion_levels = std::make_pair(0, 0);
-    within_z_limits = false;
-  }else{
-    inclusion_levels = FindInclusionLevels(val_z, &within_z_limits);
-  }
+  /*--- Perform quasi-3D interpolation for a single variable named val_name_var on a query point 
+        with coordinates val_x, val_y, and val_z ---*/
+
+  /* 1: Find table levels directly above and below the query point (the levels that sandwhich val_z) */
+  bool within_z_limits = true;
+  std::pair<unsigned long, unsigned long> inclusion_levels = FindInclusionLevels(val_z, &within_z_limits);
   
   if(within_z_limits){
-    lower_level = inclusion_levels.first;
-    upper_level = inclusion_levels.second;
+    /* 2: Perform 2D interpolations on upper and lower inclusion levels */
+    unsigned long lower_level = inclusion_levels.first;
+    unsigned long upper_level = inclusion_levels.second;
+
     su2double val_var_lower, val_var_upper;
     unsigned long exit_code_lower = LookUp_XY(val_name_var, &val_var_lower, val_x, val_y, lower_level);
     unsigned long exit_code_upper = LookUp_XY(val_name_var, &val_var_upper, val_x, val_y, upper_level);
 
-    Linear_Interpolation(val_z, inclusion_levels, val_var_lower, val_var_upper, val_var);
+    /* 3: Perform linear interpolation along the z-direction using the x-y interpolation results
+             from upper and lower trapezoidal maps */
+    Linear_Interpolation(val_z, lower_level, upper_level, val_var_lower, val_var_upper, val_var);
 
     return max(exit_code_lower, exit_code_upper);
   }else{
-    lower_level = inclusion_levels.first;
-    exit_code = LookUp_XY(val_name_var, val_var, val_x, val_y, lower_level);
-    if( val_z == 0 ){
-      return exit_code;
-    }else{
-      return 1;
-    }
+    /* Perform single, 2D interpolation when val_z lies outside table bounds */
+    unsigned long bound_level = inclusion_levels.first;
+    LookUp_XY(val_name_var, val_var, val_x, val_y, bound_level);
+    return 1;
   }
 }
 unsigned long CLookUpTable::LookUp_XYZ(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars, su2double val_x,
                                 su2double val_y, su2double val_z)
 {
-  bool within_z_limits, exit_code;
-  unsigned long lower_level, upper_level;
-  std::pair<unsigned long, unsigned long> inclusion_levels;
-  if(val_z == 0){
-    inclusion_levels = std::make_pair(0, 0);
-    within_z_limits = false;
-  }else{
-    inclusion_levels = FindInclusionLevels(val_z, &within_z_limits);
-  }
+  /*--- Perform quasi-3D interpolation for a vector of variables with names val_names_var 
+        on a query point with coordinates val_x, val_y, and val_z ---*/
+
+  /* 1: Find table levels directly above and below the query point (the levels that sandwhich val_z) */
+  bool within_z_limits = true;
+  std::pair<unsigned long, unsigned long> inclusion_levels = FindInclusionLevels(val_z, &within_z_limits);
   
   if(within_z_limits){
-    lower_level = inclusion_levels.first;
-    upper_level = inclusion_levels.second;
+    /* 2: Perform 2D interpolations on upper and lower inclusion levels */
+    unsigned long lower_level = inclusion_levels.first;
+    unsigned long upper_level = inclusion_levels.second;
+
     std::vector<su2double> val_vars_lower, val_vars_upper;
     val_vars_lower.resize(val_vars.size());
     val_vars_upper.resize(val_vars.size());
     unsigned long exit_code_lower = LookUp_XY(val_names_var, val_vars_lower, val_x, val_y, lower_level);
     unsigned long exit_code_upper = LookUp_XY(val_names_var, val_vars_upper, val_x, val_y, upper_level);
 
-    Linear_Interpolation(val_z, inclusion_levels, val_vars_lower, val_vars_upper, val_vars);
+    /* 3: Perform linear interpolation along the z-direction using the x-y interpolation results
+             from upper and lower trapezoidal maps */
+    Linear_Interpolation(val_z, lower_level, upper_level, val_vars_lower, val_vars_upper, val_vars);
 
     return max(exit_code_lower, exit_code_upper);
   }else{
-    lower_level = inclusion_levels.first;
-    exit_code = LookUp_XY(val_names_var, val_vars, val_x, val_y, lower_level);
-    if( val_z == 0 ){
-      return exit_code;
-    }else{
-      return 1;
-    }
+    /* Perform single, 2D interpolation when val_z lies outside table bounds */
+    unsigned long bound_level = inclusion_levels.first;
+    LookUp_XY(val_names_var, val_vars, val_x, val_y, bound_level);
+    return 1;
   }
 }
 
-void CLookUpTable::Linear_Interpolation(su2double val_z, std::pair<unsigned long, unsigned long> &inclusion_levels, su2double&lower_value,su2double&upper_value, su2double*&var_val)
+void CLookUpTable::Linear_Interpolation(const su2double val_z, const unsigned long lower_level, const unsigned long upper_level, su2double&lower_value,su2double&upper_value, su2double*&var_val)
 {
-  su2double val_z_lower = z_values_levels[inclusion_levels.first];
-  su2double val_z_upper = z_values_levels[inclusion_levels.second];
+  /* Perform linear interpolation along the z-direction of the table for a single variable */
+
+  /* Retrieve constant z-values of inclusion levels */
+  su2double val_z_lower = z_values_levels[lower_level];
+  su2double val_z_upper = z_values_levels[upper_level];
+
+  /* Compute linear interpolation coefficients */
   su2double factor_upper = (val_z - val_z_lower) / (val_z_upper - val_z_lower);
   su2double factor_lower = (val_z_upper - val_z) / (val_z_upper - val_z_lower);
 
+  /* Perform linear interpolation */
   *var_val = lower_value * factor_lower + upper_value * factor_upper;
-  
 }
 
-void CLookUpTable::Linear_Interpolation(su2double val_z, std::pair<unsigned long, unsigned long> &inclusion_levels, std::vector<su2double>&lower_values,std::vector<su2double>&upper_values, std::vector<su2double*>&var_vals)
+void CLookUpTable::Linear_Interpolation(const su2double val_z, const unsigned long lower_level, const unsigned long upper_level, std::vector<su2double>&lower_values,std::vector<su2double>&upper_values, std::vector<su2double*>&var_vals)
 {
-  su2double val_z_lower = z_values_levels[inclusion_levels.first];
-  su2double val_z_upper = z_values_levels[inclusion_levels.second];
+  /* Perform linear interpolation along the z-direction of the table for multiple variables */
+
+  /* Retrieve constant z-values of inclusion levels */
+  su2double val_z_lower = z_values_levels[lower_level];
+  su2double val_z_upper = z_values_levels[upper_level];
+
+  /* Compute linear interpolation coefficients */
   su2double factor_upper = (val_z - val_z_lower) / (val_z_upper - val_z_lower);
   su2double factor_lower = (val_z_upper - val_z) / (val_z_upper - val_z_lower);
 
+  /* Perform linear interpolation */
   for(size_t iVar=0; iVar<var_vals.size(); iVar++){
     *var_vals[iVar] = lower_values[iVar] * factor_lower + upper_values[iVar] * factor_upper;
   }
@@ -504,17 +599,12 @@ unsigned long CLookUpTable::LookUp_XY(const string& val_name_var, su2double *val
   return exit_code;
 }
 
-unsigned long CLookUpTable::LookUp_ProgEnth(const std::string& val_name_var, su2double* val_var, su2double val_prog, 
-                                            su2double val_enth, std::string name_prog, std::string name_enth) {
-  return LookUp_XY(val_name_var, val_var, val_prog, val_enth);
-}
-
 unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vector<su2double>& val_vars,
                                             su2double val_x, su2double val_y, unsigned long i_level) {
-  vector<su2double*> look_up_data;
+  vector<su2double*> look_up_data(val_names_var.size());
 
   for (long unsigned int i_var = 0; i_var < val_vars.size(); ++i_var) {
-    look_up_data.push_back(&val_vars[i_var]);
+    look_up_data[i_var] = &val_vars[i_var];
   }
 
   unsigned long exit_code = LookUp_XY(val_names_var, look_up_data, val_x, val_y, i_level);
@@ -522,16 +612,26 @@ unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vecto
   return exit_code;
 }
 
+unsigned long CLookUpTable::LookUp_ProgEnth(const std::string& val_name_var, su2double* val_var, su2double val_prog, 
+                                            su2double val_enth, std::string name_prog, std::string name_enth) {
+  return LookUp_XY(val_name_var, val_var, val_prog, val_enth);
+}
+
 unsigned long CLookUpTable::LookUp_ProgEnth(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars, su2double val_prog,
                                 su2double val_enth, std::string name_prog, std::string name_enth) {
   return LookUp_XY(val_names_var, val_vars, val_prog, val_enth);
 }
 
+unsigned long CLookUpTable::LookUp_ProgEnth(const std::vector<std::string>& val_names_var, std::vector<su2double>& val_vars, su2double val_prog,
+                                su2double val_enth, std::string name_prog, std::string name_enth) {
+  return LookUp_XY(val_names_var, val_vars, val_prog, val_enth);
+}
+
 unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vector<su2double*>& val_vars,
                                             su2double val_x, su2double val_y, unsigned long i_level) {
   unsigned long exit_code = 0;
   unsigned long nearest_neighbor = 0;
-  unsigned long id_triangle;
+  unsigned long id_triangle = 0;
   std::array<su2double,3> interp_coeffs{0};
   std::array<unsigned long,3> triangle{0};
 
@@ -582,10 +682,6 @@ unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vecto
   return exit_code;
 }
 
-unsigned long CLookUpTable::LookUp_ProgEnth(const std::vector<std::string>& val_names_var, std::vector<su2double>& val_vars, su2double val_prog,
-                                su2double val_enth, std::string name_prog, std::string name_enth) {
-  return LookUp_XY(val_names_var, val_vars, val_prog, val_enth);
-}
 void CLookUpTable::GetInterpCoeffs(su2double val_x, su2double val_y, su2activematrix& interp_mat_inv,
                                    std::array<su2double,3>& interp_coeffs) {
 
diff --git a/Common/src/containers/CTrapezoidalMap.cpp b/Common/src/containers/CTrapezoidalMap.cpp
index f651c6a2cfe..80e49026483 100644
--- a/Common/src/containers/CTrapezoidalMap.cpp
+++ b/Common/src/containers/CTrapezoidalMap.cpp
@@ -40,9 +40,6 @@ using namespace std;
 CTrapezoidalMap::CTrapezoidalMap(const su2double* samples_x, const su2double* samples_y, const unsigned long size,
                                  vector<su2vector<unsigned long> > const& edges,
                                  su2vector<vector<unsigned long> > const& val_edge_to_triangle) {
-  int rank = SU2_MPI::GetRank();
-  su2double startTime = SU2_MPI::Wtime();
-
   edge_to_triangle = su2vector<vector<unsigned long> >(val_edge_to_triangle);
 
   unique_bands_x.assign(samples_x,samples_x+size);
@@ -128,10 +125,6 @@ CTrapezoidalMap::CTrapezoidalMap(const su2double* samples_x, const su2double* sa
 
     i_band++;
   }
-
-  su2double stopTime = SU2_MPI::Wtime();
-
-  if (rank == MASTER_NODE) cout << "Construction of trapezoidal map took " << stopTime-startTime << " seconds\n" << endl;
 }
 
 

From f3a71e8f3e624abe7df5db3054b0c84c14cbe802 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 13 Dec 2022 11:15:23 +0100
Subject: [PATCH 078/656] Fixed build error

---
 Common/src/containers/CLookUpTable.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index addf38e2eaa..2e5f4d08581 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -192,7 +192,7 @@ void CLookUpTable::FindTableLimits(const string& name_cv1, const string& name_cv
     limits_table_y[i_level] = make_pair(min_y, max_y);
   }
 
-  if(table_dim = 3){
+  if(table_dim == 3){
     su2double min_z, max_z;
     min_z = *min_element(z_values_levels, z_values_levels + n_table_levels);
     max_z = *max_element(z_values_levels, z_values_levels + n_table_levels);

From 3637d167ac78fed2e51c3c6eff45053fce7a8615 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 13 Dec 2022 11:28:52 +0100
Subject: [PATCH 079/656] Fixed build error

---
 Common/src/containers/CLookUpTable.cpp | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index 2e5f4d08581..f98a1ac4836 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -80,13 +80,13 @@ CLookUpTable::CLookUpTable(const string& var_file_name_lut, const string& name_x
     if(rank == MASTER_NODE){
       su2double progress = su2double(i_level) / n_table_levels;
       unsigned short barwidth = 65;
-      int pos = barwidth * progress;
+      auto pos = barwidth * progress;
       cout << "[";
       for(int iBar=0; iBar<barwidth; ++iBar){
           if(iBar < pos) cout << "=";
           else cout << " ";
       }
-      cout << "] "<< int(100*progress) << " %\r";
+      cout << "] "<< floor(100*progress) << " %\r";
       cout.flush();
     }
   }

From 728e6f1ff5c8c836ef0b4a43eb1c9c64cf72bd74 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 13 Dec 2022 13:10:32 +0100
Subject: [PATCH 080/656] Added more comments, fixed some style
 inconsistencies, and set auto variables where possible

---
 .../multilayer_perceptron/CIOMap.hpp          |  32 ++--
 .../multilayer_perceptron/CLayer.hpp          |  28 ++--
 .../multilayer_perceptron/CLookUp_ANN.hpp     |   7 -
 .../multilayer_perceptron/CNeuralNetwork.hpp  |  20 +--
 .../multilayer_perceptron/CNeuron.hpp         |  22 ++-
 .../multilayer_perceptron/CIOMap.cpp          |  11 +-
 .../multilayer_perceptron/CLookUp_ANN.cpp     | 138 ++++++++----------
 .../multilayer_perceptron/CNeuralNetwork.cpp  |  64 ++++----
 .../CReadNeuralNetwork.cpp                    |  75 +++++-----
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        |  33 +++--
 10 files changed, 204 insertions(+), 226 deletions(-)

diff --git a/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp b/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
index d4494cc0aad..e4b357afa96 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
@@ -84,8 +84,6 @@ namespace MLPToolbox
         std::vector<std::vector<std::pair<std::size_t, std::size_t>>> 
             Input_Map,      /*!< Mapping of call variable inputs to matching MLP inputs */
             Output_Map;     /*!< Mapping of call variable outputs to matching MLP outputs */
-
-        std::vector<std::vector<su2double>> input_indices;  /*!< */
         
         public:
 
@@ -99,9 +97,9 @@ namespace MLPToolbox
 
         /*!
         * \brief Set MLP index in IO map
-        * \param[in] i_MLP - loaded MLP index
+        * \param[in] iMLP - loaded MLP index
         */
-        void Push_MLP_index(std::size_t i_MLP){MLP_indices.push_back(i_MLP);};
+        void Push_MLP_index(std::size_t iMLP){ MLP_indices.push_back(iMLP); }
 
         /*!
         * \brief Pair call inputs and outputs with the inputs and outputs of 
@@ -116,58 +114,58 @@ namespace MLPToolbox
         * \brief Get the number of MLPs in the current IO map
         * \return number of MLPs with matching inputs and output(s)
         */
-        std::size_t GetNMLPs() const {return MLP_indices.size();}
+        std::size_t GetNMLPs() const { return MLP_indices.size(); }
 
         /*!
         * \brief Get the loaded MLP index
         * \return MLP index
         */
-        std::size_t GetMLPIndex(std::size_t i_Map) const {return MLP_indices[i_Map];}
+        std::size_t GetMLPIndex(std::size_t i_Map) const { return MLP_indices[i_Map]; }
 
         /*!
         * \brief Get the call input variable index 
         * \param[in] i_Map - input-output mapping index of the IO map
-        * \param[in] i_Input - input index of the call input variable
+        * \param[in] iInput - input index of the call input variable
         * \return MLP input variable index
         */
-        std::size_t GetInputIndex(std::size_t i_Map, std::size_t i_Input) const {return Input_Map[i_Map][i_Input].first;}
+        std::size_t GetInputIndex(std::size_t i_Map, std::size_t iInput) const { return Input_Map[i_Map][iInput].first; }
 
         /*!
         * \brief Get the call output variable index 
         * \param[in] i_Map - input-output mapping index of the IO map
-        * \param[in] i_Output - output index of the call input variable
+        * \param[in] iOutput - output index of the call input variable
         * \return call variable output index
         */
-        std::size_t GetOutputIndex(std::size_t i_Map, std::size_t i_Output) const {return Output_Map[i_Map][i_Output].first;}
+        std::size_t GetOutputIndex(std::size_t i_Map, std::size_t iOutput) const { return Output_Map[i_Map][iOutput].first; }
 
         /*!
         * \brief Get the MLP output variable index 
         * \param[in] i_Map - input-output mapping index of the IO map
-        * \param[in] i_Output - output index of the call input variable
+        * \param[in] iOutput - output index of the call input variable
         * \return MLP output variable index
         */
-        std::size_t GetMLPOutputIndex(std::size_t i_Map, std::size_t i_Output) const {return Output_Map[i_Map][i_Output].second;}
+        std::size_t GetMLPOutputIndex(std::size_t i_Map, std::size_t iOutput) const { return Output_Map[i_Map][iOutput].second; }
 
         /*!
         * \brief Get the number of matching output variables between the call and MLP outputs
         * \param[in] i_Map - input-output mapping index of the IO map
         * \return Number of matching variables between the loaded MLP and call variables
         */
-        std::size_t GetNMappedOutputs(std::size_t i_Map) const {return Output_Map[i_Map].size();}
+        std::size_t GetNMappedOutputs(std::size_t i_Map) const { return Output_Map[i_Map].size(); }
 
         /*!
         * \brief Get the mapping of MLP outputs matching to call outputs
         * \param[in] i_Map - input-output mapping index of the IO map
         * \return Mapping of MLP output variables to call variables
         */
-        std::vector<std::pair<std::size_t, std::size_t>> GetOutputMapping(std::size_t i_map) const {return Output_Map[i_map];}
+        std::vector<std::pair<std::size_t, std::size_t>> GetOutputMapping(std::size_t i_map) const { return Output_Map[i_map]; }
 
         /*!
         * \brief Get the mapping of MLP inputs to call inputs
         * \param[in] i_Map - input-output mapping index of the IO map
         * \return Mapping of MLP input variables to call inputs
         */
-        std::vector<std::pair<std::size_t, std::size_t>> GetInputMapping(std::size_t i_map) const{return Input_Map[i_map];}
+        std::vector<std::pair<std::size_t, std::size_t>> GetInputMapping(std::size_t i_map) const { return Input_Map[i_map]; }
         
         /*!
         * \brief Get the mapped inputs for the MLP at i_Map
@@ -179,8 +177,8 @@ namespace MLPToolbox
             su2vector<su2double> MLP_input;
             MLP_input.resize(Input_Map[i_Map].size());
 
-            for(std::size_t i_Input=0; i_Input<Input_Map[i_Map].size(); i_Input++){
-                MLP_input[i_Input] = inputs[GetInputIndex(i_Map, i_Input)];
+            for(std::size_t iInput=0; iInput<Input_Map[i_Map].size(); iInput++){
+                MLP_input[iInput] = inputs[GetInputIndex(i_Map, iInput)];
             }
             return MLP_input;
         }
diff --git a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
index 32d71d26d94..07b0bdb8e46 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
@@ -45,86 +45,86 @@ class CLayer
     std::string activation_type;             /*!< Activation function type applied to the current layer*/
 public:
     CLayer();
-    CLayer(unsigned long n_neurons);
-    ~CLayer(){delete [] neurons;}
+    CLayer( unsigned long n_neurons );
+    ~CLayer(){ delete [] neurons; }
     /*!
     * \brief Set current layer neuron count
     * \param[in] n_neurons - Number of neurons in this layer
     */
-    void setNNeurons(unsigned long n_neurons);
+    void setNNeurons( unsigned long n_neurons );
 
     /*!
     * \brief Get the current layer neuron count
     * \return Neuron count
     */
-    unsigned long getNNeurons() const {return number_of_neurons;};
+    unsigned long getNNeurons() const { return number_of_neurons; }
 
     /*!
     * \brief Define current layer as input layer
     * \param[in] input - input layer identifyer
     */
-    void setInput(bool def){is_input = def;};
+    void setInput(bool def){ is_input = def; }
 
     /*!
     * \brief Get input layer identifyer
     * \return input layer identifyer
     */
-    bool isInput() const {return is_input;};
+    bool isInput() const { return is_input; }
 
     /*!
     * \brief Set the output value of a neuron in the layer
     * \param[in] i_neuron - Neuron index
     * \param[in] output_value - Activation function output
     */
-    void setOutput(std::size_t i_neuron, su2double value){neurons[i_neuron].setOutput(value);}
+    void setOutput(std::size_t i_neuron, su2double value){ neurons[i_neuron].setOutput(value); }
 
     /*!
     * \brief Get the output value of a neuron in the layer
     * \param[in] i_neuron - Neuron index
     * \return Neuron output value
     */
-    su2double getOutput(std::size_t i_neuron) const {return neurons[i_neuron].getOutput();}
+    su2double getOutput(std::size_t i_neuron) const { return neurons[i_neuron].getOutput(); }
 
     /*!
     * \brief Set the input value of a neuron in the layer
     * \param[in] i_neuron - Neuron index
     * \param[in] input_value - Activation function input
     */
-    void setInput(std::size_t i_neuron, su2double value){neurons[i_neuron].setInput(value);}
+    void setInput(std::size_t i_neuron, su2double value){ neurons[i_neuron].setInput(value); }
 
     /*!
     * \brief Get the input value of a neuron in the layer
     * \param[in] i_neuron - Neuron index
     * \return Neuron input value
     */
-    su2double getInput(std::size_t i_neuron) const {return neurons[i_neuron].getInput();}
+    su2double getInput(std::size_t i_neuron) const { return neurons[i_neuron].getInput(); }
 
     /*!
     * \brief Set the bias value of a neuron in the layer
     * \param[in] i_neuron - Neuron index
     * \param[in] bias_value - Bias value
     */
-    void setBias(std::size_t i_neuron, su2double value){neurons[i_neuron].setBias(value);}
+    void setBias(std::size_t i_neuron, su2double value){ neurons[i_neuron].setBias(value); }
 
     /*!
     * \brief Get the bias value of a neuron in the layer
     * \param[in] i_neuron - Neuron index
     * \return Neuron bias value
     */
-    su2double getBias(std::size_t i_neuron){return neurons[i_neuron].getBias();}
+    su2double getBias(std::size_t i_neuron){ return neurons[i_neuron].getBias(); }
 
     /*!
     * \brief Get the output-input gradient of a neuron in the layer
     * \param[in] i_neuron - Neuron index
     * \return Gradient of neuron output wrt input
     */
-    su2double getdYdX(std::size_t i_neuron){return neurons[i_neuron].getGradient();}
+    su2double getdYdX(std::size_t i_neuron){ return neurons[i_neuron].getGradient(); }
 
     /*!
     * \brief Get the activation function name applied to this layer
     * \return name of the activation function
     */
-    string getActivationType(){return activation_type;}
+    string getActivationType(){ return activation_type; }
     
 };
 
diff --git a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
index 7734c38a01b..82cec12f2d3 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
@@ -109,13 +109,6 @@ class CLookUp_ANN
     */
     std::size_t GetNANNs() const {return NeuralNetworks.size();}
 
-    /*!
-    * \brief Check if variables occur more than once in ANN outputs
-    * \param[in] output_names - output variable names to check
-    * \param[in] input_output_map - pointer to input-output map to be checked
-    */
-    bool Check_Duplicate_Outputs(su2vector<std::string> &output_names, CIOMap *input_output_map) const;
-
     /*!
     * \brief Check if all output variables are present in the loaded ANNs
     * \param[in] output_names - output variable names to check
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
index 1acdc182e46..cd270ca14e1 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
@@ -121,7 +121,7 @@ class CNeuralNetwork
     * \param[in] i_neuron - Neuron index of current layer.
     * \param[in] value - Bias value.
     */
-    void setBias(unsigned long i_layer, unsigned long i_neuron, su2double value){total_layers[i_layer]->setBias(i_neuron, value);}
+    void setBias(unsigned long i_layer, unsigned long i_neuron, su2double value){ total_layers[i_layer]->setBias(i_neuron, value); }
 
     /*!
     * \brief Set layer activation function.
@@ -150,20 +150,20 @@ class CNeuralNetwork
     * \brief Get the number of connecting regions in the network.
     * \returns number of spaces in between layers.
     */
-    unsigned long getNWeightLayers(){return total_layers.size()-1;}
+    unsigned long getNWeightLayers() const { return total_layers.size()-1; }
 
     /*!
     * \brief Get the total number of layers in the network
     * \returns number of netowork layers.
     */
-    unsigned long getNLayers(){return total_layers.size();}
+    unsigned long getNLayers() const { return total_layers.size(); }
 
     /*!
     * \brief Get neuron count in a layer.
     * \param[in] iLayer - Layer index.
     * \returns number of neurons in the layer.
     */
-    unsigned long getNNeurons(unsigned long iLayer) { return total_layers[iLayer]->getNNeurons(); }
+    unsigned long getNNeurons(unsigned long iLayer) const { return total_layers[iLayer]->getNNeurons(); }
 
     /*!
     * \brief Evaluate the network.
@@ -206,33 +206,33 @@ class CNeuralNetwork
     * \param[in] iInput - Input variable index.
     * \returns input variable name.
     */
-    std::string GetInputName(std::size_t iInput) { return input_names[iInput]; }
+    std::string GetInputName(std::size_t iInput) const { return input_names[iInput]; }
 
     /*!
     * \brief Get network output variable name.
     * \param[in] iOutput - Output variable index.
     * \returns output variable name.
     */
-    std::string GetOutputName(std::size_t iOutput) { return output_names[iOutput]; }
+    std::string GetOutputName(std::size_t iOutput) const { return output_names[iOutput]; }
 
     /*!
     * \brief Get network number of inputs.
     * \returns Number of network inputs
     */
-    std::size_t GetnInputs() { return input_names.size(); }
+    std::size_t GetnInputs() const { return input_names.size(); }
 
     /*!
     * \brief Get network number of outputs.
     * \returns Number of network outputs
     */
-    std::size_t GetnOutputs() { return output_names.size(); }
+    std::size_t GetnOutputs() const { return output_names.size(); }
 
     /*!
     * \brief Get network evaluation output.
     * \param[in] iOutput - output index.
     * \returns Prediction value.
     */
-    su2double GetANN_Output(std::size_t iOutput) { return ANN_outputs[iOutput]; }
+    su2double GetANN_Output(std::size_t iOutput) const { return ANN_outputs[iOutput]; }
 
     /*!
     * \brief Set the activation function array size.
@@ -246,7 +246,7 @@ class CNeuralNetwork
     * \param[in] iNeuron - Layer neuron index.
     * \returns Neuron activation function input.
     */
-    su2double ComputeX(std::size_t iLayer, std::size_t iNeuron){
+    su2double ComputeX(std::size_t iLayer, std::size_t iNeuron) const {
         su2double x;
         x = total_layers[iLayer]->getBias(iNeuron);
         std::size_t nNeurons_previous = total_layers[iLayer - 1]->getNNeurons();
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
index 3e1cefd1d6f..f06802f4688 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
@@ -32,7 +32,6 @@
 #include <cstdlib>
 
 #include "../../CConfig.hpp"
-//#include "../../linear_algebra/blas_structure.hpp"
 
 namespace MLPToolbox{
 class CNeuron
@@ -45,67 +44,66 @@ class CNeuron
               bias{0};              /*!< Bias value at current neuron */
 
 public:
-    CNeuron(){};
 
     /*!
     * \brief Set neuron identification number
     * \param[in] input - Identification number
     */
-    void setNumber(unsigned long input){i_neuron = input;}
+    void setNumber(unsigned long input){ i_neuron = input; }
 
     /*!
     * \brief Get neuron identification number
     * \return Identification number
     */
-    unsigned long getNumber() const {return i_neuron;}
+    unsigned long getNumber() const { return i_neuron; }
 
     /*!
     * \brief Set neuron output value
     * \param[in] input - activation function output value
     */
-    void setOutput(su2double input){output = input;}
+    void setOutput(su2double input){ output = input; }
 
     /*!
     * \brief Get neuron output value
     * \return Output value
     */
-    su2double getOutput() const {return output;}
+    su2double getOutput() const { return output; }
 
     /*!
     * \brief Set neuron input value
     * \param[in] input - activation function input value
     */
-    void setInput(su2double x){input = x;}
+    void setInput(su2double x){ input = x; }
 
     /*!
     * \brief Get neuron input value
     * \return input value
     */
-    su2double getInput() const {return input;}
+    su2double getInput() const { return input; }
 
     /*!
     * \brief Set neuron bias
     * \param[in] input - bias value
     */
-    void setBias(su2double input){bias = input;}
+    void setBias(su2double input){ bias = input; }
 
     /*!
     * \brief Get neuron bias value
     * \return bias value
     */
-    su2double getBias() const {return bias;}
+    su2double getBias() const { return bias; }
 
     /*!
     * \brief Set neuron output gradient with respect to its input value
     * \param[in] input - Derivative of activation function with respect to input
     */
-    void setGradient(su2double input){doutput_dinput = input;}
+    void setGradient(su2double input){ doutput_dinput = input; }
 
     /*!
     * \brief Get neuron output gradient with respect to input value
     * \return output gradient wrt input value
     */
-    su2double getGradient() const {return doutput_dinput;}
+    su2double getGradient() const { return doutput_dinput; }
 };
 
 }
diff --git a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
index f1cc8f00bb4..42627195ab0 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
@@ -46,9 +46,6 @@ MLPToolbox::CIOMap::CIOMap(CLookUp_ANN*MLP_collection, su2vector<std::string> &i
 
         // Check wether all call outputs are present in the MLP collection
         MLP_collection->Check_Use_of_Outputs(outputs, this);
-
-        // Check wether there are any duplicates in the MLP outputs
-        //MLP_collection->Check_Duplicate_Outputs(outputs, this);
     }
 }
 void MLPToolbox::CIOMap::PairVariableswithMLPs(CLookUp_ANN*MLP_collection, su2vector<std::string> &inputs, su2vector<std::string> &outputs){
@@ -58,22 +55,22 @@ void MLPToolbox::CIOMap::PairVariableswithMLPs(CLookUp_ANN*MLP_collection, su2ve
     bool isInput, isOutput;
 
     // Looping over the loaded MLPs to check wether the MLP inputs match with the call inputs
-    for(size_t i_MLP=0; i_MLP<MLP_collection->GetNANNs(); i_MLP++){
+    for(size_t iMLP=0; iMLP<MLP_collection->GetNANNs(); iMLP++){
 
         // Mapped call inputs to MLP inputs
-        std::vector<pair<size_t, size_t>> Input_Indices = MLP_collection->FindVariable_Indices(i_MLP, inputs, true);
+        std::vector<pair<size_t, size_t>> Input_Indices = MLP_collection->FindVariable_Indices(iMLP, inputs, true);
         isInput = Input_Indices.size() > 0;
 
         if(isInput){
             // Only when the MLP inputs match with a portion of the call inputs are the output variable checks performed
 
-            std::vector<pair<size_t, size_t>> Output_Indices = MLP_collection->FindVariable_Indices(i_MLP, outputs, false);
+            std::vector<pair<size_t, size_t>> Output_Indices = MLP_collection->FindVariable_Indices(iMLP, outputs, false);
             isOutput = Output_Indices.size() > 0;
 
             if(isOutput){
 
                 // Update input and output mapping if both inputs and outputs match
-                MLP_indices.push_back(i_MLP);
+                MLP_indices.push_back(iMLP);
                 Input_Map.push_back(Input_Indices);
                 Output_Map.push_back(Output_Indices);
             }
diff --git a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
index 045f71ce43a..0f7566796bd 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
@@ -37,35 +37,35 @@ using namespace std;
 
 MLPToolbox::CLookUp_ANN::CLookUp_ANN(string inputFileName)
 {
-    
     #ifdef HAVE_MPI
     MPI_Comm_rank(MPI_COMM_WORLD, &rank);
     #endif
     if(rank == MASTER_NODE)
         cout << "Generating ANN collection" << endl;
 
+    /* Read MLP collection input file */
     ReadANNInputFile(inputFileName);
-    for(size_t i_ANN=0; i_ANN<number_of_variables; i_ANN++){
-        
+
+    /* Generate a multi-layer perceptron for every file listed in the MLP collection file */
+    for(auto i_ANN=0u; i_ANN<number_of_variables; i_ANN++){
         NeuralNetworks[i_ANN] = new CNeuralNetwork;
         if(rank == MASTER_NODE)
-            cout << "Generating neural network for " << ANN_filenames.at(i_ANN) << endl;
-        GenerateANN(NeuralNetworks[i_ANN], ANN_filenames.at(i_ANN));
+            cout << "Generating neural network for " << ANN_filenames[i_ANN] << endl;
+        GenerateANN(NeuralNetworks[i_ANN], ANN_filenames[i_ANN]);
     }
 }
 
 
 vector<pair<size_t, size_t>> MLPToolbox::CLookUp_ANN::FindVariable_Indices(size_t i_ANN, su2vector<string> variable_names, bool input) const {
+    /* Find loaded MLPs that have the same input variable names as the variables listed in variable_names */
     vector<pair<size_t, size_t>> variable_indices;
-    size_t nVar = input ? NeuralNetworks[i_ANN]->GetnInputs() : NeuralNetworks[i_ANN]->GetnOutputs();
+    auto nVar = input ? NeuralNetworks[i_ANN]->GetnInputs() : NeuralNetworks[i_ANN]->GetnOutputs();
 
-    for(size_t iVar=0; iVar<nVar; iVar++){
-        for(size_t jVar=0; jVar<variable_names.size(); jVar++){
+    for(auto iVar=0u; iVar<nVar; iVar++){
+        for(auto jVar=0u; jVar<variable_names.size(); jVar++){
             string ANN_varname = input ? NeuralNetworks[i_ANN]->GetInputName(iVar) : NeuralNetworks[i_ANN]->GetOutputName(iVar);
-            
             if(variable_names[jVar].compare(ANN_varname) == 0){
                 variable_indices.push_back(make_pair(jVar, iVar));
-                //cout << variable_names[jVar] << " : " << jVar << " | " << ANN_varname << " : " << iVar << endl;
             }
         }
     }
@@ -82,14 +82,14 @@ unsigned long MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap *input_output_map, su2
     size_t i_ANN_nearest = 0,           // Index of nearest MLP.
            i_map_nearest = 0;           // Index of nearest iomap index.
 
-    for(size_t i_map=0; i_map<input_output_map->GetNMLPs(); i_map++){
+    for(auto i_map=0u; i_map<input_output_map->GetNMLPs(); i_map++){
         within_range = true;
-        size_t i_ANN = input_output_map->GetMLPIndex(i_map);
-        su2vector<su2double> ANN_inputs = input_output_map->GetMLP_Inputs(i_map, inputs);
+        auto i_ANN = input_output_map->GetMLPIndex(i_map);
+        auto ANN_inputs = input_output_map->GetMLP_Inputs(i_map, inputs);
         
         su2double distance_to_query_i = 0;
-        for(size_t i_input=0; i_input < ANN_inputs.size(); i_input++) {
-            std::pair<su2double, su2double> ANN_input_limits = NeuralNetworks[i_ANN]->GetInputNorm(i_input);
+        for(auto i_input=0u; i_input < ANN_inputs.size(); i_input++) {
+            auto ANN_input_limits = NeuralNetworks[i_ANN]->GetInputNorm(i_input);
 
             /* Check if query input lies within MLP training range */
             if(!((ANN_inputs[i_input] > ANN_input_limits.first) && (ANN_inputs[i_input] < ANN_input_limits.second))) {
@@ -105,7 +105,7 @@ unsigned long MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap *input_output_map, su2
         if(within_range){
             NeuralNetworks[i_ANN]->predict(ANN_inputs);
             MLP_was_evaluated = true;
-            for(size_t i=0; i < input_output_map->GetNMappedOutputs(i_map); i++){
+            for(auto i=0u; i < input_output_map->GetNMappedOutputs(i_map); i++){
                 *outputs[input_output_map->GetOutputIndex(i_map, i)] = NeuralNetworks[i_ANN]->GetANN_Output(input_output_map->GetMLPOutputIndex(i_map, i));
             }
         }
@@ -119,9 +119,9 @@ unsigned long MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap *input_output_map, su2
     }
     /* Evaluate nearest MLP in case no query data within range is found */
     if(!MLP_was_evaluated) {
-        su2vector<su2double> ANN_inputs = input_output_map->GetMLP_Inputs(i_map_nearest, inputs);
+        auto ANN_inputs = input_output_map->GetMLP_Inputs(i_map_nearest, inputs);
         NeuralNetworks[i_ANN_nearest]->predict(ANN_inputs);
-        for(size_t i=0; i < input_output_map->GetNMappedOutputs(i_map_nearest); i++){
+        for(auto i=0u; i < input_output_map->GetNMappedOutputs(i_map_nearest); i++){
             *outputs[input_output_map->GetOutputIndex(i_map_nearest, i)] = NeuralNetworks[i_ANN_nearest]->GetANN_Output(input_output_map->GetMLPOutputIndex(i_map_nearest, i));
         }
     }
@@ -131,6 +131,9 @@ unsigned long MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap *input_output_map, su2
 
 void MLPToolbox::CLookUp_ANN::GenerateANN(CNeuralNetwork * ANN, string fileName)
 {
+    /*--- Generate MLP architecture based on information in MLP input file ---*/
+
+    /* Read MLP input file */
     CReadNeuralNetwork Reader = CReadNeuralNetwork(fileName);
     
     // Read MLP input file
@@ -139,14 +142,14 @@ void MLPToolbox::CLookUp_ANN::GenerateANN(CNeuralNetwork * ANN, string fileName)
     // Generate basic layer architectures
     ANN->defineInputLayer(Reader.GetNInputs());
     ANN->sizeInputs(Reader.GetNInputs());
-    for(size_t iInput=0; iInput<Reader.GetNInputs(); iInput++){
+    for(auto iInput=0u; iInput<Reader.GetNInputs(); iInput++){
         ANN->PushInputName(Reader.GetInputName(iInput));
     }
-    for(size_t iLayer=1; iLayer<Reader.GetNlayers()-1; iLayer++){
+    for(auto iLayer=1u; iLayer<Reader.GetNlayers()-1; iLayer++){
         ANN->push_hidden_layer(Reader.GetNneurons(iLayer));
     }
     ANN->defineOutputLayer(Reader.GetNOutputs());
-    for(size_t iOutput=0; iOutput<Reader.GetNOutputs(); iOutput++){
+    for(auto iOutput=0u; iOutput<Reader.GetNOutputs(); iOutput++){
         ANN->PushOutputName(Reader.GetOutputName(iOutput));
     }
 
@@ -155,10 +158,10 @@ void MLPToolbox::CLookUp_ANN::GenerateANN(CNeuralNetwork * ANN, string fileName)
 
     // Define weights and activation functions
     ANN->SizeActivationFunctions(ANN->getNWeightLayers()+1);
-    for(size_t i_layer = 0; i_layer < ANN->getNWeightLayers(); i_layer++){
+    for(auto i_layer=0u; i_layer < ANN->getNWeightLayers(); i_layer++){
         ANN->setActivationFunction(i_layer, Reader.GetActivationFunction(i_layer));
-        for(size_t i_neuron=0; i_neuron < ANN->getNNeurons(i_layer); i_neuron++){
-            for(size_t j_neuron=0; j_neuron<ANN->getNNeurons(i_layer+1); j_neuron++){
+        for(auto i_neuron=0u; i_neuron < ANN->getNNeurons(i_layer); i_neuron++){
+            for(auto j_neuron=0u; j_neuron<ANN->getNNeurons(i_layer+1); j_neuron++){
                 ANN->setWeight(i_layer, i_neuron, j_neuron, Reader.GetWeight(i_layer, i_neuron, j_neuron));
             }
         }
@@ -168,17 +171,17 @@ void MLPToolbox::CLookUp_ANN::GenerateANN(CNeuralNetwork * ANN, string fileName)
     ANN->setActivationFunction(ANN->getNWeightLayers(), Reader.GetActivationFunction(ANN->getNWeightLayers()));
     
     // Set neuron biases
-    for(size_t i_layer=0; i_layer<ANN->getNWeightLayers()+1; i_layer++){
-        for(size_t i_neuron=0; i_neuron<ANN->getNNeurons(i_layer); i_neuron++){
+    for(auto i_layer=0u; i_layer<ANN->getNWeightLayers()+1; i_layer++){
+        for(auto i_neuron=0u; i_neuron<ANN->getNNeurons(i_layer); i_neuron++){
             ANN->setBias(i_layer, i_neuron, Reader.GetBias(i_layer, i_neuron));
         }
     }
     
     // Define input and output layer normalization values
-    for(unsigned long iInput=0; iInput<Reader.GetNInputs(); iInput++){
+    for(auto iInput=0u; iInput<Reader.GetNInputs(); iInput++){
         ANN->SetInputNorm(iInput, Reader.GetInputNorm(iInput).first, Reader.GetInputNorm(iInput).second);
     }
-    for(unsigned long iOutput=0; iOutput<Reader.GetNOutputs(); iOutput++){
+    for(auto iOutput=0u; iOutput<Reader.GetNOutputs(); iOutput++){
         ANN->SetOutputNorm(iOutput, Reader.GetOutputNorm(iOutput).first, Reader.GetOutputNorm(iOutput).second);
     }
     
@@ -227,76 +230,49 @@ string MLPToolbox::CLookUp_ANN::SkipToFlag(ifstream *file_stream, string flag) {
   return line;
 }
 
-
-bool MLPToolbox::CLookUp_ANN::Check_Duplicate_Outputs(su2vector<string> &output_names, CIOMap *input_output_map) const {
-    unsigned short n_occurances;
-    bool duplicate{false};
-    vector<string> duplicate_variables;
-    for(size_t i_Output =0; i_Output < output_names.size(); i_Output++){
-        n_occurances = 0;
-        for(size_t i_map=0; i_map<input_output_map->GetNMLPs(); i_map++){
-            vector<pair<size_t, size_t>> output_map = input_output_map->GetOutputMapping(i_map);
-            for(size_t j_Output=0; j_Output<output_map.size(); j_Output++){
-                if(output_map[j_Output].first == i_Output) n_occurances++;
-            }
-        }
-        if(n_occurances > 1){
-            duplicate_variables.push_back(output_names[i_Output]);
-            duplicate = true;
-        }
-    }
-    if(duplicate){
-        string message{"Variables "};
-        for(size_t iVar=0; iVar<duplicate_variables.size(); iVar++) message += duplicate_variables[iVar] + " ";
-        SU2_MPI::Error(message + "occur more than once in the loaded ANN outputs.", CURRENT_FUNCTION);
-    }
-    
-    return duplicate;
-}
-
-
 bool MLPToolbox::CLookUp_ANN::Check_Use_of_Inputs(su2vector<string> &input_names, CIOMap *input_output_map) const {
-vector<string> missing_inputs;
-bool inputs_are_present{true};
-for(size_t iInput=0; iInput<input_names.size(); iInput ++){
-    bool found_input = false;
-    for(size_t i_map=0; i_map < input_output_map->GetNMLPs(); i_map++){
-        vector<pair<size_t, size_t>> input_map = input_output_map->GetInputMapping(i_map);
-        for(size_t jInput=0; jInput<input_map.size(); jInput++){
-            if(input_map[jInput].first == iInput){
-                found_input = true;
+    /*--- Check wether all input variables are in the loaded MLPs ---*/
+    vector<string> missing_inputs;
+    bool inputs_are_present{true};
+    for(auto iInput=0u; iInput<input_names.size(); iInput ++){
+        bool found_input = false;
+        for(auto i_map=0u; i_map < input_output_map->GetNMLPs(); i_map++){
+            auto input_map = input_output_map->GetInputMapping(i_map);
+            for(auto jInput=0u; jInput<input_map.size(); jInput++){
+                if(input_map[jInput].first == iInput){
+                    found_input = true;
+                }
             }
         }
+        if(!found_input){
+            missing_inputs.push_back(input_names[iInput]);
+            inputs_are_present = false;
+        };
     }
-    if(!found_input){
-        missing_inputs.push_back(input_names[iInput]);
-        inputs_are_present = false;
-    };
-}
-if(missing_inputs.size() > 0){
-    string message{"Inputs "};
-    for(size_t iVar=0; iVar<missing_inputs.size(); iVar++) message += missing_inputs[iVar] + " ";
-    SU2_MPI::Error(message + "are not present in any loaded ANN.", CURRENT_FUNCTION);
-}
-return inputs_are_present;
+    if(missing_inputs.size() > 0){
+        string message{"Inputs "};
+        for(size_t iVar=0; iVar<missing_inputs.size(); iVar++) message += missing_inputs[iVar] + " ";
+        SU2_MPI::Error(message + "are not present in any loaded ANN.", CURRENT_FUNCTION);
+    }
+    return inputs_are_present;
 }
 
 bool MLPToolbox::CLookUp_ANN::Check_Use_of_Outputs(su2vector<string> &output_names, CIOMap * input_output_map) const {
-    /* Check wether all output variables are in the loaded MLPs */
+    /*--- Check wether all output variables are in the loaded MLPs ---*/
     
     vector<string> missing_outputs;     
     bool outputs_are_present{true};
     /* Looping over the target outputs */
-    for(size_t iOutput=0; iOutput<output_names.size(); iOutput ++){
+    for(auto iOutput=0u; iOutput<output_names.size(); iOutput ++){
 
         bool found_output{false};
 
         /* Looping over all the selected ANNs */
-        for(size_t i_map=0; i_map < input_output_map->GetNMLPs(); i_map++){
-            vector<pair<size_t, size_t>> output_map = input_output_map->GetOutputMapping(i_map);
+        for(auto i_map=0u; i_map < input_output_map->GetNMLPs(); i_map++){
+            auto output_map = input_output_map->GetOutputMapping(i_map);
 
             /* Looping over the outputs of the output map of the current ANN */
-            for(size_t jOutput=0; jOutput<output_map.size(); jOutput++){
+            for(auto jOutput=0u; jOutput<output_map.size(); jOutput++){
                 if(output_map[jOutput].first == iOutput) found_output = true;
             }
         }
diff --git a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
index 96bd5879d4c..8bec59d2095 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
@@ -33,28 +33,36 @@ using namespace std;
 
 
 void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
-    su2double x, x_norm, y, y_norm;
-    size_t iNeuron, iLayer, nNeurons_current;
+    /*--- Evaluate MLP for given inputs ---*/
+
+    su2double y, y_norm;
     bool same_point{true};
-    for(iNeuron=0; iNeuron<inputLayer->getNNeurons(); iNeuron++){
-        x_norm = (inputs[iNeuron] - input_norm[iNeuron].first)/(input_norm[iNeuron].second - input_norm[iNeuron].first);
+
+    /* Normalize input and check if inputs are the same w.r.t last evaluation */
+    for(auto iNeuron=0u; iNeuron<inputLayer->getNNeurons(); iNeuron++){
+        su2double x_norm = (inputs[iNeuron] - input_norm[iNeuron].first)/(input_norm[iNeuron].second - input_norm[iNeuron].first);
         if(abs(x_norm - inputLayer->getOutput(iNeuron)) > 0) same_point = false;
         inputLayer->setOutput(iNeuron, x_norm);
     }
     if(!same_point){
         su2double alpha=1.67326324;
         su2double lambda=1.05070098;
-        for(iLayer=1; iLayer<n_hidden_layers + 2; iLayer++){
-            nNeurons_current = total_layers[iLayer]->getNNeurons();
-
-            for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
+        /* Traverse MLP and compute inputs and outputs for the neurons in each layer */
+        for(auto iLayer=1u; iLayer<n_hidden_layers + 2; iLayer++){
+            auto nNeurons_current = total_layers[iLayer]->getNNeurons(); // Neuron count of current layer
+            su2double x;    // Neuron input value
+            
+            /* Compute and store input value for each neuron */
+            for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
                 x = ComputeX(iLayer, iNeuron);
                 total_layers[iLayer]->setInput(iNeuron, x);
             }
+
+            /* Compute and store neuron output based on activation function */
             switch (activation_function_types[iLayer])
                 {
                 case ENUM_ACTIVATION_FUNCTION::SMOOTH_SLOPE:
-                    for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
+                    for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
                         x = total_layers[iLayer]->getInput(iNeuron);
                         if(x > 0){
                             y = x;
@@ -65,7 +73,7 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
                     }
                     break;
                 case ENUM_ACTIVATION_FUNCTION::ELU:
-                    for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
+                    for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
                         x = total_layers[iLayer]->getInput(iNeuron);
                         if(x > 0){
                             y = x;
@@ -76,14 +84,14 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
                     }
                     break;
                 case ENUM_ACTIVATION_FUNCTION::LINEAR:
-                    for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
+                    for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
                         x = total_layers[iLayer]->getInput(iNeuron);
                         y = x;
                         total_layers[iLayer]->setOutput(iNeuron, y);
                     }
                     break;
                 case ENUM_ACTIVATION_FUNCTION::RELU:
-                    for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
+                    for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
                         x = total_layers[iLayer]->getInput(iNeuron);
                         if(x > 0){
                             y = x;
@@ -94,28 +102,28 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
                     }
                     break;
                 case ENUM_ACTIVATION_FUNCTION::SWISH:
-                    for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
+                    for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
                         x = total_layers[iLayer]->getInput(iNeuron);
                         y = x / (1 + exp(-x));
                         total_layers[iLayer]->setOutput(iNeuron, y);
                     }
                     break;
                 case ENUM_ACTIVATION_FUNCTION::TANH:
-                    for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
+                    for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
                         x = total_layers[iLayer]->getInput(iNeuron);
                         y = tanh(x);
                         total_layers[iLayer]->setOutput(iNeuron, y);
                     }
                     break;
                 case ENUM_ACTIVATION_FUNCTION::SIGMOID:
-                    for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
+                    for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
                         x = total_layers[iLayer]->getInput(iNeuron);
                         y = 1.0/(1 + exp(-x));
                         total_layers[iLayer]->setOutput(iNeuron, y);
                     }
                     break;
                 case ENUM_ACTIVATION_FUNCTION::SELU:
-                    for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
+                    for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
                         x = total_layers[iLayer]->getInput(iNeuron);
                         if(x > 0.0){
                             y = lambda * x;
@@ -126,8 +134,7 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
                     }
                     break;
                 case ENUM_ACTIVATION_FUNCTION::GELU:
-                    
-                    for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
+                    for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
                         x = total_layers[iLayer]->getInput(iNeuron);
 
                         y = 0.5 * x * (1 + tanh(sqrt(2 / PI_NUMBER) * (x + 0.044715 * pow(x, 3))));
@@ -135,22 +142,22 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
                     }
                     break;
                 case ENUM_ACTIVATION_FUNCTION::NONE:
-                    for(iNeuron=0; iNeuron<nNeurons_current; iNeuron++){
+                    for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
                         y = 0.0;
                         total_layers[iLayer]->setOutput(iNeuron, y);
                     }
                     break;
                 default:
                     break;
-                }
-                
+                } // activation_function_types
         }
     }
-    for(iNeuron=0; iNeuron<outputLayer->getNNeurons(); iNeuron++){
+    /* Compute and de-normalize MLP output */
+    for(auto iNeuron=0u; iNeuron<outputLayer->getNNeurons(); iNeuron++){
         y_norm = outputLayer->getOutput(iNeuron);
         y = y_norm*(output_norm[iNeuron].second - output_norm[iNeuron].first) + output_norm[iNeuron].first;
         
-        // Setting output value
+        /* Storing output value */
         ANN_outputs[iNeuron] = y;
     }
 }
@@ -180,17 +187,19 @@ void MLPToolbox::CNeuralNetwork::push_hidden_layer(unsigned long n_neurons){
 }
 
 void MLPToolbox::CNeuralNetwork::sizeWeights(){
-    
+    /* Size weight matrices based on neuron counts in each layer */
+
+    /* Generate vector containing input, output, and hidden layer references */
     total_layers.resize(n_hidden_layers + 2);
     total_layers[0] = inputLayer;
-    for(size_t iLayer=0; iLayer<n_hidden_layers; iLayer++){
-        total_layers[iLayer + 1] = hiddenLayers.at(iLayer);
+    for(auto iLayer=0u; iLayer<n_hidden_layers; iLayer++){
+        total_layers[iLayer + 1] = hiddenLayers[iLayer];
     }
     total_layers[total_layers.size()-1] = outputLayer;
 
     weights_mat.resize(n_hidden_layers+1);
     weights_mat[0].resize(hiddenLayers[0]->getNNeurons(), inputLayer->getNNeurons());
-    for(size_t iLayer=1; iLayer<n_hidden_layers; iLayer++){
+    for(auto iLayer=1u; iLayer<n_hidden_layers; iLayer++){
         weights_mat[iLayer].resize(hiddenLayers[iLayer]->getNNeurons(), hiddenLayers[iLayer-1]->getNNeurons());
     }
     weights_mat[n_hidden_layers].resize(outputLayer->getNNeurons(), hiddenLayers[n_hidden_layers-1]->getNNeurons());
@@ -210,6 +219,7 @@ void MLPToolbox::CNeuralNetwork::displayNetwork(){
 
 void MLPToolbox::CNeuralNetwork::setActivationFunction(unsigned long i_layer, string input)
 {
+    /*--- Translate activation function name from input file to a number ---*/
     if(input.compare("linear") == 0){
         activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::LINEAR;
         return;
diff --git a/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
index 73e49fda1e1..3440da71d97 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
@@ -41,8 +41,10 @@ void MLPToolbox::CReadNeuralNetwork::ReadMLPFile(){
     }
 
     string line, word;
-    double input_min, input_max, output_min, output_max;
-    bool eoHeader{false}, found_layercount{false}, found_input_names{false}, found_output_names{false};
+    bool eoHeader = false, 
+         found_layercount = false, 
+         found_input_names = false, 
+         found_output_names = false;
 
     /* Read general architecture information from file header */
 
@@ -70,27 +72,26 @@ void MLPToolbox::CReadNeuralNetwork::ReadMLPFile(){
           SU2_MPI::Error("No layer count provided before defining neuron count per layer", CURRENT_FUNCTION);
         }
         // Loop over layer count and size neuron count and bias count per layer accordingly
-        for(size_t iLayer=0; iLayer<n_layers; iLayer++){
+        for(auto iLayer=0u; iLayer<n_layers; iLayer++){
           getline(file_stream, line);
-          n_neurons.at(iLayer) = stoul(line);
-          biases.at(iLayer).resize(n_neurons.at(iLayer));
+          n_neurons[iLayer] = stoul(line);
+          biases[iLayer].resize(n_neurons[iLayer]);
         }
         // Loop over spaces between layers and size the weight matrices accordingly
-        for(size_t iLayer=0; iLayer<n_layers-1; iLayer++){
-          weights.at(iLayer).resize(n_neurons.at(iLayer));
-          for(size_t iNeuron=0; iNeuron<n_neurons.at(iLayer); iNeuron++){
-            weights.at(iLayer).at(iNeuron).resize(n_neurons.at(iLayer+1));
+        for(auto iLayer=0u; iLayer<n_layers-1; iLayer++){
+          weights[iLayer].resize(n_neurons[iLayer]);
+          for(size_t iNeuron=0; iNeuron<n_neurons[iLayer]; iNeuron++){
+            weights[iLayer][iNeuron].resize(n_neurons[iLayer+1]);
           }
         }
-        // Size input normalization according to number of inputs
-        input_norm.resize(n_neurons.at(0));
-        // Set default input normalization
-        for(size_t iNeuron=0; iNeuron<n_neurons.at(0); iNeuron++) input_norm.at(iNeuron) = make_pair(0, 1);
-
-        // Size output normalization according to number of outputs
-        output_norm.resize(n_neurons.at(n_neurons.size()-1));
-        // Set default output normalization
-        for(size_t iNeuron=0; iNeuron<n_neurons.at(n_neurons.size()-1); iNeuron++) output_norm.at(iNeuron) = make_pair(0, 1);
+        /* Size input and output normalization and set default values */
+        input_norm.resize(n_neurons[0]);
+        for(auto iNeuron=0u; iNeuron<n_neurons[0]; iNeuron++) 
+          input_norm[iNeuron] = make_pair(0, 1);
+
+        output_norm.resize(n_neurons[n_neurons.size()-1]);
+        for(auto iNeuron=0u; iNeuron<n_neurons[n_neurons.size()-1]; iNeuron++) 
+          output_norm[iNeuron] = make_pair(0, 1);
       }
 
       /* Read layer activation function types */
@@ -98,11 +99,11 @@ void MLPToolbox::CReadNeuralNetwork::ReadMLPFile(){
         if(!found_layercount){
           SU2_MPI::Error("No layer count provided before providing layer activation functions", CURRENT_FUNCTION);
         }
-        for(size_t iLayer=0; iLayer<n_layers; iLayer++){
+        for(auto iLayer=0u; iLayer<n_layers; iLayer++){
           getline(file_stream, line);
           istringstream activation_stream(line);
           activation_stream >> word;
-          activation_functions.at(iLayer) = word;
+          activation_functions[iLayer] = word;
         }    
       }
 
@@ -115,22 +116,22 @@ void MLPToolbox::CReadNeuralNetwork::ReadMLPFile(){
           getline(file_stream, line);
         }
 
-        if(input_names.size() != n_neurons.at(0)){
+        if(input_names.size() != n_neurons[0]){
           SU2_MPI::Error("Number of input variable names inconsistent with number of MLP inputs", CURRENT_FUNCTION);
         }
       }
 
       /* In case input normalization is applied, read upper and lower input bounds */
       if(line.compare("[input normalization]") == 0){
-        for(size_t iInput=0; iInput<input_norm.size(); iInput++){
+        for(auto iInput=0u; iInput<input_norm.size(); iInput++){
           getline(file_stream, line);
           if(line.compare("") != 0){
             istringstream input_norm_stream(line);
             input_norm_stream >> word;
-            input_min = stold(word);
+            su2double input_min = stold(word);
             input_norm_stream >> word;
-            input_max = stold(word);
-            input_norm.at(iInput) = make_pair(input_min, input_max);
+            su2double input_max = stold(word);
+            input_norm[iInput] = make_pair(input_min, input_max);
           }
         }
       }
@@ -144,22 +145,22 @@ void MLPToolbox::CReadNeuralNetwork::ReadMLPFile(){
           getline(file_stream, line);
         }
 
-        if(output_names.size() != (n_neurons.at(n_neurons.size()-1))){
+        if(output_names.size() != (n_neurons[n_neurons.size()-1])){
           SU2_MPI::Error("Number of output variable names inconsistent with number of MLP outputs", CURRENT_FUNCTION);
         }
       }
 
       /* In case output normalization is applied, read upper and lower output bounds */
       if(line.compare("[output normalization]") == 0){
-        for(size_t iOutput=0; iOutput<output_norm.size(); iOutput++){
+        for(auto iOutput=0u; iOutput<output_norm.size(); iOutput++){
           getline(file_stream, line);
           if(line.compare("") != 0){
             istringstream output_norm_stream(line);
             output_norm_stream >> word;
-            output_min = stold(word);
+            su2double output_min = stold(word);
             output_norm_stream >> word;
-            output_max = stold(word);
-            output_norm.at(iOutput) = make_pair(output_min, output_max);
+            su2double output_max = stold(word);
+            output_norm[iOutput] = make_pair(output_min, output_max);
           }
         }
       }
@@ -177,14 +178,14 @@ void MLPToolbox::CReadNeuralNetwork::ReadMLPFile(){
 
     /* Read weights for each layer */
     line = SkipToFlag(&file_stream, "[weights per layer]");
-    for(size_t iLayer=0; iLayer<n_layers-1; iLayer++){
+    for(auto iLayer=0u; iLayer<n_layers-1; iLayer++){
       getline(file_stream, line);
-      for(size_t iNeuron=0; iNeuron<n_neurons.at(iLayer); iNeuron++){
+      for(auto iNeuron=0u; iNeuron<n_neurons[iLayer]; iNeuron++){
         getline(file_stream, line);
         istringstream weight_stream(line);
-        for(size_t jNeuron=0; jNeuron<n_neurons.at(iLayer+1); jNeuron++){
+        for(auto jNeuron=0u; jNeuron<n_neurons[iLayer+1]; jNeuron++){
           weight_stream >> word;
-          weights.at(iLayer).at(iNeuron).at(jNeuron) = stold(word);
+          weights[iLayer][iNeuron][jNeuron] = stold(word);
         }
       }
       getline(file_stream, line);
@@ -192,12 +193,12 @@ void MLPToolbox::CReadNeuralNetwork::ReadMLPFile(){
     
     /* Read biases for each neuron */
     line = SkipToFlag(&file_stream, "[biases per layer]");
-    for(size_t iLayer=0; iLayer<n_layers; iLayer++){
+    for(auto iLayer=0u; iLayer<n_layers; iLayer++){
       getline(file_stream, line);
       istringstream bias_stream(line);
-      for(size_t iNeuron=0; iNeuron<n_neurons.at(iLayer); iNeuron++){
+      for(auto iNeuron=0u; iNeuron<n_neurons[iLayer]; iNeuron++){
         bias_stream >> word;
-        biases.at(iLayer).at(iNeuron) = stold(word);
+        biases[iLayer][iNeuron] = stold(word);
       }
     }
 
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 9183faf18d8..84bc6aa9065 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -108,28 +108,24 @@ void CDataDrivenFluid::MapInputs_to_Outputs(){
   outputs_rhoe[idx_d2sdrho2] = &d2sdrho2;
 
   /*--- Further preprocessing of input and output variables ---*/
-  switch (Kind_DataDriven_Method)
-  {
-  case ENUM_DATADRIVEN_METHOD::MLP:
+  if(Kind_DataDriven_Method == ENUM_DATADRIVEN_METHOD::MLP){
     /*--- Map MLP inputs to outputs ---*/
     iomap_rhoe = new MLPToolbox::CIOMap(lookup_mlp, input_names_rhoe, output_names_rhoe);
     MLP_inputs.resize(2);
-    break;
-  
-  default:
-    break;
   }
 }
 
 void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
+  /*--- Compute thermodynamic state based on density and energy ---*/
+
   Density = rho;
   StaticEnergy = e;
 
   Evaluate_Dataset(rho, e);
 
   /*--- Compute speed of sound ---*/
-  su2double blue_term = (dsdrho_e * (2 - rho * pow(dsde_rho, -1) * d2sdedrho) + rho * d2sdrho2);
-  su2double green_term = (- pow(dsde_rho, -1) * d2sde2 * dsdrho_e + d2sdedrho);
+  auto blue_term = (dsdrho_e * (2 - rho * pow(dsde_rho, -1) * d2sdedrho) + rho * d2sdrho2);
+  auto green_term = (- pow(dsde_rho, -1) * d2sde2 * dsdrho_e + d2sdedrho);
   
   SoundSpeed2 = - rho * pow(dsde_rho, -1) * (blue_term - rho * green_term * (dsdrho_e / dsde_rho));
 
@@ -202,7 +198,6 @@ void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
 void CDataDrivenFluid::SetTDState_Prho(su2double P, su2double rho) {
   /*--- Computing static energy according to pressure and density ---*/
   SetEnergy_Prho(P, rho);
-  
 
   /*--- Calculate thermodynamic state based on converged value for energy ---*/
   SetTDState_rhoe(rho, StaticEnergy);
@@ -400,10 +395,14 @@ void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
 }
 
 unsigned long CDataDrivenFluid::Predict_MLP(su2double rho, su2double e) {
-  unsigned long exit_code;
   MLP_inputs[idx_rho] = rho;
   MLP_inputs[idx_e] = e;
-  exit_code = lookup_mlp->Predict_ANN(iomap_rhoe, MLP_inputs, outputs_rhoe);
+
+  /* Evaluate MLP collection for the given values for density and energy */
+  unsigned long exit_code = lookup_mlp->Predict_ANN(iomap_rhoe, MLP_inputs, outputs_rhoe);
+
+  /* Apply exponential transformation to the MLP outputs for the first and second 
+     derivative of the entropy w.r.t density */
   dsdrho_e = -exp(dsdrho_e);
   d2sdrho2 = exp(d2sdrho2);
 
@@ -415,10 +414,16 @@ unsigned long CDataDrivenFluid::Predict_LUT(su2double rho, su2double e) {
   std::vector<std::string> output_names_rhoe_LUT;
   std::vector<su2double*> outputs_LUT;
   output_names_rhoe_LUT.resize(output_names_rhoe.size());
-    for(size_t iOutput=0; iOutput<output_names_rhoe.size(); iOutput++) { output_names_rhoe_LUT[iOutput] = output_names_rhoe[iOutput]; }
+  for(auto iOutput=0u; iOutput<output_names_rhoe.size(); iOutput++) 
+  { 
+    output_names_rhoe_LUT[iOutput] = output_names_rhoe[iOutput]; 
+  }
 
   outputs_LUT.resize(outputs_rhoe.size());
-  for(size_t iOutput=0; iOutput<outputs_rhoe.size(); iOutput++) { outputs_LUT[iOutput] = outputs_rhoe[iOutput]; }
+  for(auto iOutput=0u; iOutput<outputs_rhoe.size(); iOutput++) 
+  { 
+    outputs_LUT[iOutput] = outputs_rhoe[iOutput]; 
+  }
 
   exit_code = lookup_table->LookUp_ProgEnth(output_names_rhoe_LUT, outputs_LUT, rho, e, "Density", "Energy");
   return exit_code;

From 513ee66a3149490f03e328491c7671337fd2c92c Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Wed, 14 Dec 2022 16:09:30 +0100
Subject: [PATCH 081/656] Fixed bug in determining the nearest MLP to a query
 point outside the training range

---
 .../multilayer_perceptron/CLookUp_ANN.cpp     |  4 +--
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        | 32 +++++++++----------
 SU2_CFD/src/solvers/CEulerSolver.cpp          |  8 ++---
 3 files changed, 22 insertions(+), 22 deletions(-)

diff --git a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
index 0f7566796bd..79a2b1643fa 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
@@ -92,12 +92,12 @@ unsigned long MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap *input_output_map, su2
             auto ANN_input_limits = NeuralNetworks[i_ANN]->GetInputNorm(i_input);
 
             /* Check if query input lies within MLP training range */
-            if(!((ANN_inputs[i_input] > ANN_input_limits.first) && (ANN_inputs[i_input] < ANN_input_limits.second))) {
+            if((ANN_inputs[i_input] < ANN_input_limits.first) || (ANN_inputs[i_input] > ANN_input_limits.second)) {
                 within_range = false;
             }
 
             /* Calculate distance between MLP training range center point and query */
-            su2double middle = 0.5*(ANN_input_limits.second - ANN_input_limits.first);
+            su2double middle = 0.5*(ANN_input_limits.second + ANN_input_limits.first);
             distance_to_query_i += pow((ANN_inputs[i_input] - middle)/(ANN_input_limits.second - ANN_input_limits.first), 2);
         }
         
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 84bc6aa9065..d733ea63f7c 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -149,11 +149,11 @@ void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
   su2double rho = rho_start, 
             e = e_start;
 
-  su2double tolerance_P = 10, // Tolerance for pressure solution
-            tolerance_T = 1;  // Tolerance for temperature solution
+  su2double tolerance_P = 1, // Tolerance percentage for pressure solution
+            tolerance_T = 1;  // Tolerance percentage for temperature solution
 
   bool converged = false;         // Convergence flag
-  unsigned long iter_max = 1000,  // Maximum number of iterations
+  unsigned long iter_max = 500,  // Maximum number of iterations
                 Iter = 0;       
 
   su2double delta_P,      // Pressure residual
@@ -171,7 +171,7 @@ void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
     delta_P = Pressure - P;
     delta_T = Temperature - T;
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if((abs(delta_P) < tolerance_P) && (abs(delta_T) < tolerance_T)){
+    if((100*abs(delta_P)/P < tolerance_P) && (100*abs(delta_T)/T < tolerance_T)){
       converged = true;
     }else{
       
@@ -207,10 +207,10 @@ void CDataDrivenFluid::SetEnergy_Prho(su2double P, su2double rho) {
   /*--- Setting initial values for energy ---*/
   su2double e = e_start;
 
-  su2double tolerance_P = 10; // Tolerance for pressure solution
+  su2double tolerance_P = 1.0; // Tolerance percentage for pressure solution
 
   bool converged = false;         // Convergence flag
-  unsigned long iter_max = 1000,  // Maximum number of iterations
+  unsigned long iter_max = 200,  // Maximum number of iterations
                 Iter = 0;       
 
   su2double delta_P,      // Pressure residual
@@ -224,11 +224,11 @@ void CDataDrivenFluid::SetEnergy_Prho(su2double P, su2double rho) {
     /*--- Determine pressure and temperature residuals ---*/
     delta_P = Pressure - P;
 
+    su2double partial_diff = abs(delta_P)/P;
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if((abs(delta_P) < tolerance_P)){
+    if((100*partial_diff < tolerance_P)){
       converged = true;
     }else{
-      
       /*--- Compute step size for energy ---*/
       delta_e = delta_P / dPde_rho;
 
@@ -252,7 +252,7 @@ void CDataDrivenFluid::SetTDState_rhoT(su2double rho, su2double T) {
   su2double tolerance_T = 1;  // Tolerance for temperature solution
 
   bool converged = false;         // Convergence flag
-  unsigned long iter_max = 1000,  // Maximum number of iterations
+  unsigned long iter_max = 500,  // Maximum number of iterations
                 Iter = 0;       
 
   su2double delta_T,      // Temperature residual
@@ -268,7 +268,7 @@ void CDataDrivenFluid::SetTDState_rhoT(su2double rho, su2double T) {
     delta_T = Temperature - T;
 
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if((abs(delta_T) < tolerance_T)){
+    if(100*(abs(delta_T)/T < tolerance_T)){
       converged = true;
     }else{
       
@@ -293,11 +293,11 @@ void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
   su2double rho = rho_start, 
             e = e_start;
 
-  su2double tolerance_h = 10, // Tolerance for enthalpy solution
+  su2double tolerance_h = 1, // Tolerance for enthalpy solution
             tolerance_s = 1;  // Tolerance for entropy solution
 
   bool converged = false;         // Convergence flag
-  unsigned long iter_max = 1000,  // Maximum number of iterations
+  unsigned long iter_max = 500,  // Maximum number of iterations
                 Iter = 0;       
 
   su2double delta_h,      // Enthalpy
@@ -318,7 +318,7 @@ void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
     delta_s = Entropy - s;
 
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if((abs(delta_h) < tolerance_h) && (abs(delta_s) < tolerance_s)){
+    if((100*abs(delta_h)/h < tolerance_h) && (100*abs(delta_s)/s < tolerance_s)){
       converged = true;
     }else{
       
@@ -347,11 +347,11 @@ void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
   su2double rho = rho_start, 
             e = e_start;
 
-  su2double tolerance_P = 10, // Tolerance for pressure solution
+  su2double tolerance_P = 1, // Tolerance for pressure solution
             tolerance_s = 1;  // Tolerance for entropy solution
 
   bool converged = false;         // Convergence flag
-  unsigned long iter_max = 1000,  // Maximum number of iterations
+  unsigned long iter_max = 500,  // Maximum number of iterations
                 Iter = 0;       
 
   su2double delta_P,      // Enthalpy
@@ -371,7 +371,7 @@ void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
     delta_s = Entropy - s;
 
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if((abs(delta_P) < tolerance_P) && (abs(delta_s) < tolerance_s)){
+    if((100*abs(delta_P)/P < tolerance_P) && (100*abs(delta_s)/s < tolerance_s)){
       converged = true;
     }else{
 
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index d62651c726c..447d0ce7d8d 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -4653,6 +4653,10 @@ void CEulerSolver::BC_Riemann(CGeometry *geometry, CSolver **solver_container,
 
       GetFluidModel()->SetTDState_rhoe(Density_i, StaticEnergy_i);
 
+      /*--- Set initial values for density and energy for Newton solvers in fluid model ---*/
+      GetFluidModel()->SetDensity(Density_i);
+      GetFluidModel()->SetEnergy(StaticEnergy_i);
+
       Pressure_i = GetFluidModel()->GetPressure();
       Enthalpy_i = Energy_i + Pressure_i/Density_i;
 
@@ -4681,10 +4685,6 @@ void CEulerSolver::BC_Riemann(CGeometry *geometry, CSolver **solver_container,
         P_Total /= config->GetPressure_Ref();
         T_Total /= config->GetTemperature_Ref();
 
-        /*--- Set initial values for density and energy for Newton solvers in fluid model ---*/
-        GetFluidModel()->SetDensity(Density_i);
-        GetFluidModel()->SetEnergy(StaticEnergy_i);
-
         /* --- Computes the total state --- */
         GetFluidModel()->SetTDState_PT(P_Total, T_Total);
         Enthalpy_e = GetFluidModel()->GetStaticEnergy()+ GetFluidModel()->GetPressure()/GetFluidModel()->GetDensity();

From d0cc4d336d0200a32348f40d8392478affed8201 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Wed, 14 Dec 2022 21:49:48 +0100
Subject: [PATCH 082/656] Made commenting more consistent, changed datadriven
 input file option to be an array of filenames within the config file

---
 Common/include/CConfig.hpp                    | 15 ++++--
 .../multilayer_perceptron/CLookUp_ANN.hpp     | 14 +++---
 .../multilayer_perceptron/CNeuralNetwork.hpp  | 13 +++--
 Common/src/CConfig.cpp                        |  2 +-
 .../multilayer_perceptron/CLookUp_ANN.cpp     | 49 ++++++++++---------
 .../multilayer_perceptron/CNeuralNetwork.cpp  | 27 +++++-----
 .../multilayer_perceptron/CNeuron.cpp         |  2 +-
 .../CReadNeuralNetwork.cpp                    | 11 +++--
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp    |  2 -
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        |  9 ++--
 .../CLookUp_ANN_tests.cpp                     |  5 +-
 11 files changed, 80 insertions(+), 69 deletions(-)

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index eec4067226f..a9107b1d1e7 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -523,7 +523,8 @@ class CConfig {
   Kind_TimeIntScheme_Species,   /*!< \brief Time integration for the species model. */
   Kind_TimeIntScheme_Heat,      /*!< \brief Time integration for the wave equations. */
   Kind_TimeStep_Heat,           /*!< \brief Time stepping method for the (fvm) heat equation. */
-  Kind_DataDriven_Method;       /*!< \brief Method used for datset regression in datadriven fluid models. */
+  Kind_DataDriven_Method,       /*!< \brief Method used for datset regression in datadriven fluid models. */
+  n_Datadriven_files;
 
   su2double DataDriven_Relaxation_Factor, /*!< \brief Relaxation factor for Newton solvers in datadriven fluid models. */
             DataDriven_initial_density,   /*!< \brief Initial density value for Newton solvers in datadriven fluid models. */
@@ -805,7 +806,7 @@ class CConfig {
   SurfSens_FileName,             /*!< \brief Output file for the sensitivity on the surface (discrete adjoint). */
   VolSens_FileName,              /*!< \brief Output file for the sensitivity in the volume (discrete adjoint). */
   ObjFunc_Hess_FileName,         /*!< \brief Hessian approximation obtained by the Sobolev smoothing solver. */
-  DataDriven_Method_FileName;    /*!< \brief Dataset information for datadriven fluid models. */
+  *DataDriven_Method_FileNames;    /*!< \brief Dataset information for datadriven fluid models. */
 
   bool
   Wrt_Performance,           /*!< \brief Write the performance summary at the end of a calculation.  */
@@ -3782,7 +3783,15 @@ class CConfig {
    * \brief Get name of the input file for the data-driven fluid model interpolation method.
    * \return Name of the input file for the interpolation method.
    */
-  string GetDataDriven_Filename(void) const { return DataDriven_Method_FileName; }
+  string GetDataDriven_Filename(unsigned short i_file=0) const { return DataDriven_Method_FileNames[i_file]; }
+
+  string* GetDataDriven_FileNames(void) const { return DataDriven_Method_FileNames; }
+
+  /*!
+   * \brief Get number of listed look-up table or multi-layer perceptron input files.
+   * \return Number of listed datadriven method input files.
+   */
+  unsigned short GetNDataDriven_Files(void) const { return n_Datadriven_files; }
 
   /*!
    * \brief Get Newton solver relaxation factor for data-driven fluid models.
diff --git a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
index 82cec12f2d3..a737413b6a0 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
@@ -59,7 +59,7 @@ class CLookUp_ANN
 
     std::vector<std::string> ANN_filenames;       /*!< Filenames containing ANN architecture information. */
 
-    unsigned long number_of_variables;  /*!< Number of loaded ANNs. */
+    unsigned short number_of_variables;  /*!< Number of loaded ANNs. */
 
     /*!
    * \brief Skip to certain flag in file.
@@ -86,10 +86,11 @@ class CLookUp_ANN
     
     /*!
     * \brief ANN collection class constructor
-    * \param[in] filename - filename containing list of ANN input files
+    * \param[in] n_inputs - Number of MLP files to be loaded.
+    * \param[in] input_filenames - String array containing MLP input file names. 
     */
-    CLookUp_ANN(std::string fileName);
-    
+    CLookUp_ANN(const unsigned short n_inputs, const std::string*input_filenames);
+
     /*!
     * \brief Evaluate loaded ANNs for given inputs and outputs
     * \param[in] input_output_map - input-output map coupling desired inputs and outputs to loaded ANNs
@@ -99,8 +100,9 @@ class CLookUp_ANN
     */
     unsigned long Predict_ANN(CIOMap *input_output_map, su2vector<su2double> &inputs, su2vector<su2double*> &outputs);
 
-    ~CLookUp_ANN(){for(std::size_t i_ANN=0; i_ANN<number_of_variables; i_ANN++)
-        delete NeuralNetworks[i_ANN];
+    ~CLookUp_ANN() { 
+        for(std::size_t i_ANN=0; i_ANN<number_of_variables; i_ANN++)
+            delete NeuralNetworks[i_ANN];
     };
 
     /*!
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
index cd270ca14e1..c49a8e323fb 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file CNeuralNetwork.hpp
  * \brief Declaration of the neural network class
- * \author E. Bunschoten
+ * \author E.C.Bunschoten
  * \version 7.4.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
@@ -44,10 +44,10 @@ class CNeuralNetwork
     std::vector<std::string> input_names,   // MLP input variable names.
                              output_names;  // MLP output variable names.
 
-    unsigned long n_hidden_layers;  // Number of hidden layers (layers between input and output layer).
+    unsigned long n_hidden_layers = 0;  // Number of hidden layers (layers between input and output layer).
 
-    CLayer *inputLayer,     // Pointer to network input layer.
-           *outputLayer;    // Pointer to network output layer.
+    CLayer *inputLayer = nullptr,     // Pointer to network input layer.
+           *outputLayer = nullptr;    // Pointer to network output layer.
 
     std::vector<CLayer*> hiddenLayers;  // Hidden layer collection.
     su2vector<CLayer*>   total_layers;  // Hidden layers plus in/output layers
@@ -78,7 +78,6 @@ class CNeuralNetwork
     ENUM_ACTIVATION_FUNCTION * activation_function_types;
 
 public:
-    CNeuralNetwork();
     ~CNeuralNetwork(){
         delete inputLayer;
         delete outputLayer;
@@ -113,7 +112,7 @@ class CNeuralNetwork
     * \param[in] j_neuron - neuron index of connecting neuron.
     * \param[in] value - weight value.
     */
-    void setWeight(unsigned long i_layer, unsigned long i_neuron, unsigned long j_neuron, su2double value);
+    void setWeight(unsigned long i_layer, unsigned long i_neuron, unsigned long j_neuron, su2double value) { weights_mat[i_layer][j_neuron][i_neuron] = value; };
 
     /*!
     * \brief Set bias value at a specific neuron.
@@ -133,7 +132,7 @@ class CNeuralNetwork
     /*!
     * \brief Display the network architecture in the terminal.
     */
-    void displayNetwork();
+    void displayNetwork() const;
 
     /*!
     * \brief Size the weight layers in the network according to its architecture.
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 5e3e09d8343..2200f4d2862 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -1166,7 +1166,7 @@ void CConfig::SetConfig_Options() {
   /*!\brief INTERPOLATION_METHOD \n DESCRIPTION: Interpolation method used to determine the thermodynamic state of the fluid. \n OPTIONS: See \link DataDrivenMethod_Map \endlink DEFAULT: MLP \ingroup Config*/
   addEnumOption("INTERPOLATION_METHOD",Kind_DataDriven_Method, DataDrivenMethod_Map, MLP);
   /*!\brief FILENAME_INTERPOLATOR \n DESCRIPTION: Input file for the interpolation method. \n \ingroup Config*/
-  addStringOption("FILENAME_INTERPOLATOR", DataDriven_Method_FileName, "MLP_collection.mlp");
+  addStringListOption("FILENAMES_INTERPOLATOR", n_Datadriven_files, DataDriven_Method_FileNames);
   /*!\brief DATADRIVEN_NEWTON_RELAXATION \n DESCRIPTION: Relaxation factor for Newton solvers in data-driven fluid model. \n \ingroup Config*/
   addDoubleOption("DATADRIVEN_NEWTON_RELAXATION", DataDriven_Relaxation_Factor, 0.05);
   /*!\brief DATADRIVEN_FLUID_INITIAL_DENSITY \n DESCRIPTION: Initial value for the density in the Newton solvers in the data-driven fluid model. \n \ingroup Config*/
diff --git a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
index 79a2b1643fa..3bf605c297b 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
@@ -2,7 +2,7 @@
  * \file CLookUp_ANN.cpp
  * \brief Implementation of the multi-layer perceptron class to be 
  *      used for look-up operations.
- * \author E. Bunschoten
+ * \author E.C.Bunschoten
  * \version 7.4.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
@@ -35,7 +35,7 @@
 
 using namespace std;
 
-MLPToolbox::CLookUp_ANN::CLookUp_ANN(string inputFileName)
+MLPToolbox::CLookUp_ANN::CLookUp_ANN(const unsigned short n_inputs, const string*input_filenames)
 {
     #ifdef HAVE_MPI
     MPI_Comm_rank(MPI_COMM_WORLD, &rank);
@@ -43,21 +43,21 @@ MLPToolbox::CLookUp_ANN::CLookUp_ANN(string inputFileName)
     if(rank == MASTER_NODE)
         cout << "Generating ANN collection" << endl;
 
-    /* Read MLP collection input file */
-    ReadANNInputFile(inputFileName);
+    number_of_variables = n_inputs;
 
-    /* Generate a multi-layer perceptron for every file listed in the MLP collection file */
-    for(auto i_ANN=0u; i_ANN<number_of_variables; i_ANN++){
-        NeuralNetworks[i_ANN] = new CNeuralNetwork;
-        if(rank == MASTER_NODE)
-            cout << "Generating neural network for " << ANN_filenames[i_ANN] << endl;
-        GenerateANN(NeuralNetworks[i_ANN], ANN_filenames[i_ANN]);
+    NeuralNetworks.resize(n_inputs);
+    for(auto i_MLP=0u; i_MLP < n_inputs; i_MLP++){
+        NeuralNetworks[i_MLP] = new CNeuralNetwork;
+        if(rank == MASTER_NODE) 
+            cout << "Generating neural network for " << input_filenames[i_MLP] << endl;
+        GenerateANN(NeuralNetworks[i_MLP], input_filenames[i_MLP]);
     }
+        
 }
 
-
 vector<pair<size_t, size_t>> MLPToolbox::CLookUp_ANN::FindVariable_Indices(size_t i_ANN, su2vector<string> variable_names, bool input) const {
-    /* Find loaded MLPs that have the same input variable names as the variables listed in variable_names */
+    /*--- Find loaded MLPs that have the same input variable names as the variables listed in variable_names ---*/
+
     vector<pair<size_t, size_t>> variable_indices;
     auto nVar = input ? NeuralNetworks[i_ANN]->GetnInputs() : NeuralNetworks[i_ANN]->GetnOutputs();
 
@@ -77,7 +77,7 @@ unsigned long MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap *input_output_map, su2
     bool within_range,              // Within MLP training set range.
          MLP_was_evaluated = false; // MLP was evaluated within training set range.
 
-    // If queries lie outside the training data set, the nearest MLP will be evaluated through extrapolation.
+    /* If queries lie outside the training data set, the nearest MLP will be evaluated through extrapolation. */
     su2double distance_to_query = 1e20; // Overall smallest distance between training data set middle and query.
     size_t i_ANN_nearest = 0,           // Index of nearest MLP.
            i_map_nearest = 0;           // Index of nearest iomap index.
@@ -91,7 +91,7 @@ unsigned long MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap *input_output_map, su2
         for(auto i_input=0u; i_input < ANN_inputs.size(); i_input++) {
             auto ANN_input_limits = NeuralNetworks[i_ANN]->GetInputNorm(i_input);
 
-            /* Check if query input lies within MLP training range */
+            /* Check if query input lies outside MLP training range */
             if((ANN_inputs[i_input] < ANN_input_limits.first) || (ANN_inputs[i_input] > ANN_input_limits.second)) {
                 within_range = false;
             }
@@ -126,6 +126,7 @@ unsigned long MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap *input_output_map, su2
         }
     }
 
+    /* Return 1 if query data lies outside the range of any of the loaded MLPs */
     return MLP_was_evaluated ? 0 : 1;
 }
 
@@ -136,10 +137,10 @@ void MLPToolbox::CLookUp_ANN::GenerateANN(CNeuralNetwork * ANN, string fileName)
     /* Read MLP input file */
     CReadNeuralNetwork Reader = CReadNeuralNetwork(fileName);
     
-    // Read MLP input file
+    /* Read MLP input file */
     Reader.ReadMLPFile();
 
-    // Generate basic layer architectures
+    /* Generate basic layer architectures */
     ANN->defineInputLayer(Reader.GetNInputs());
     ANN->sizeInputs(Reader.GetNInputs());
     for(auto iInput=0u; iInput<Reader.GetNInputs(); iInput++){
@@ -153,10 +154,10 @@ void MLPToolbox::CLookUp_ANN::GenerateANN(CNeuralNetwork * ANN, string fileName)
         ANN->PushOutputName(Reader.GetOutputName(iOutput));
     }
 
-    // Size weights of each layer
+    /* Size weights of each layer */
     ANN->sizeWeights();
 
-    // Define weights and activation functions
+    /* Define weights and activation functions */
     ANN->SizeActivationFunctions(ANN->getNWeightLayers()+1);
     for(auto i_layer=0u; i_layer < ANN->getNWeightLayers(); i_layer++){
         ANN->setActivationFunction(i_layer, Reader.GetActivationFunction(i_layer));
@@ -170,14 +171,14 @@ void MLPToolbox::CLookUp_ANN::GenerateANN(CNeuralNetwork * ANN, string fileName)
     }
     ANN->setActivationFunction(ANN->getNWeightLayers(), Reader.GetActivationFunction(ANN->getNWeightLayers()));
     
-    // Set neuron biases
+    /* Set neuron biases */
     for(auto i_layer=0u; i_layer<ANN->getNWeightLayers()+1; i_layer++){
         for(auto i_neuron=0u; i_neuron<ANN->getNNeurons(i_layer); i_neuron++){
             ANN->setBias(i_layer, i_neuron, Reader.GetBias(i_layer, i_neuron));
         }
     }
     
-    // Define input and output layer normalization values
+    /* Define input and output layer normalization values */
     for(auto iInput=0u; iInput<Reader.GetNInputs(); iInput++){
         ANN->SetInputNorm(iInput, Reader.GetInputNorm(iInput).first, Reader.GetInputNorm(iInput).second);
     }
@@ -189,6 +190,8 @@ void MLPToolbox::CLookUp_ANN::GenerateANN(CNeuralNetwork * ANN, string fileName)
 
 void MLPToolbox::CLookUp_ANN::ReadANNInputFile(string inputFileName)
 {
+    /*--- Read MLP collection input file and store relevant data ---*/
+
     ifstream file_stream;
     istringstream stream_names_var;
     istringstream stream_filenames;
@@ -199,8 +202,7 @@ void MLPToolbox::CLookUp_ANN::ReadANNInputFile(string inputFileName)
                     CURRENT_FUNCTION);
     }
 
-    string line;
-    string word;
+    string line, word;
 
     line = SkipToFlag(&file_stream, "[number of MLP files]");
     getline(file_stream, line);
@@ -215,6 +217,9 @@ void MLPToolbox::CLookUp_ANN::ReadANNInputFile(string inputFileName)
         ANN_filenames.push_back(word);
     }
     ANN_filenames.pop_back();
+    if(ANN_filenames.size() != number_of_variables)
+        SU2_MPI::Error(string("Inconsistency betwee"),
+                    CURRENT_FUNCTION);
 }
 string MLPToolbox::CLookUp_ANN::SkipToFlag(ifstream *file_stream, string flag) {
   string line;
diff --git a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
index 8bec59d2095..76855992caf 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
@@ -2,7 +2,7 @@
  * \file CNeuralNetwork.cpp
  * \brief Implementation of the NeuralNetwork class to be used
  *      for evaluation of multi-layer perceptrons.
- * \author E. Bunschoten
+ * \author E.C.Bunschoten
  * \version 7.4.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
@@ -35,8 +35,8 @@ using namespace std;
 void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
     /*--- Evaluate MLP for given inputs ---*/
 
-    su2double y, y_norm;
-    bool same_point{true};
+    su2double y;           // Activation function output.
+    bool same_point = true;
 
     /* Normalize input and check if inputs are the same w.r.t last evaluation */
     for(auto iNeuron=0u; iNeuron<inputLayer->getNNeurons(); iNeuron++){
@@ -44,6 +44,7 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
         if(abs(x_norm - inputLayer->getOutput(iNeuron)) > 0) same_point = false;
         inputLayer->setOutput(iNeuron, x_norm);
     }
+    /* Skip evaluation process if current point is the same as during the previous evaluation */
     if(!same_point){
         su2double alpha=1.67326324;
         su2double lambda=1.05070098;
@@ -154,7 +155,7 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
     }
     /* Compute and de-normalize MLP output */
     for(auto iNeuron=0u; iNeuron<outputLayer->getNNeurons(); iNeuron++){
-        y_norm = outputLayer->getOutput(iNeuron);
+        su2double y_norm = outputLayer->getOutput(iNeuron);
         y = y_norm*(output_norm[iNeuron].second - output_norm[iNeuron].first) + output_norm[iNeuron].first;
         
         /* Storing output value */
@@ -162,32 +163,31 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
     }
 }
 
-MLPToolbox::CNeuralNetwork::CNeuralNetwork(){
-    inputLayer = nullptr;
-    outputLayer = nullptr;
-    n_hidden_layers = 0;
-}
-
 
 void MLPToolbox::CNeuralNetwork::defineInputLayer(unsigned long n_neurons){
+    /*--- Define the input layer of the network ---*/
     inputLayer = new CLayer(n_neurons);
+
+    /* Mark layer as input layer */
     inputLayer->setInput(true);
     input_norm.resize(n_neurons);
 }
 
 void MLPToolbox::CNeuralNetwork::defineOutputLayer(unsigned long n_neurons){
+    /*--- Define the output layer of the network ---*/
     outputLayer = new CLayer(n_neurons);
     output_norm.resize(n_neurons);
 }
 
 void MLPToolbox::CNeuralNetwork::push_hidden_layer(unsigned long n_neurons){
+    /*--- Add a hidden layer to the network ---*/
     CLayer *newLayer = new CLayer(n_neurons);
     hiddenLayers.push_back(newLayer);
     n_hidden_layers ++;
 }
 
 void MLPToolbox::CNeuralNetwork::sizeWeights(){
-    /* Size weight matrices based on neuron counts in each layer */
+    /*--- Size weight matrices based on neuron counts in each layer ---*/
 
     /* Generate vector containing input, output, and hidden layer references */
     total_layers.resize(n_hidden_layers + 2);
@@ -207,10 +207,7 @@ void MLPToolbox::CNeuralNetwork::sizeWeights(){
     ANN_outputs = new su2double[outputLayer->getNNeurons()];
 }   
 
-void MLPToolbox::CNeuralNetwork::setWeight(unsigned long i_layer, unsigned long i_neuron, unsigned long j_neuron, su2double value){
-    weights_mat[i_layer][j_neuron][i_neuron] = value;
-}
-void MLPToolbox::CNeuralNetwork::displayNetwork(){
+void MLPToolbox::CNeuralNetwork::displayNetwork() const {
     /*!
     TODO:
     find way of displaying network architectures
diff --git a/Common/src/toolboxes/multilayer_perceptron/CNeuron.cpp b/Common/src/toolboxes/multilayer_perceptron/CNeuron.cpp
index f52bdb007f2..3d00506c41e 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CNeuron.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CNeuron.cpp
@@ -2,7 +2,7 @@
  * \file CNeuron.cpp
  * \brief Implementation of the neuron class to be used within the 
  *      Layer class as a part of the NeuralNetwork class.
- * \author E. Bunschoten
+ * \author E.C.Bunschoten
  * \version 7.4.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
diff --git a/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
index 3440da71d97..271cb11a6af 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
@@ -2,7 +2,7 @@
  * \file ReadNeuralNetwork.cpp
  * \brief Implementation of the reader class to read .mlp input files
  *      used to set up multi-layer perceptrons.
- * \author E. Bunschoten
+ * \author E.C.Bunschoten
  * \version 7.4.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
@@ -71,13 +71,13 @@ void MLPToolbox::CReadNeuralNetwork::ReadMLPFile(){
         if(!found_layercount){
           SU2_MPI::Error("No layer count provided before defining neuron count per layer", CURRENT_FUNCTION);
         }
-        // Loop over layer count and size neuron count and bias count per layer accordingly
+        /* Loop over layer count and size neuron count and bias count per layer accordingly */
         for(auto iLayer=0u; iLayer<n_layers; iLayer++){
           getline(file_stream, line);
           n_neurons[iLayer] = stoul(line);
           biases[iLayer].resize(n_neurons[iLayer]);
         }
-        // Loop over spaces between layers and size the weight matrices accordingly
+        /* Loop over spaces between layers and size the weight matrices accordingly */
         for(auto iLayer=0u; iLayer<n_layers-1; iLayer++){
           weights[iLayer].resize(n_neurons[iLayer]);
           for(size_t iNeuron=0; iNeuron<n_neurons[iLayer]; iNeuron++){
@@ -168,7 +168,9 @@ void MLPToolbox::CReadNeuralNetwork::ReadMLPFile(){
       if(line.compare("</header>") == 0){
         eoHeader = true;
       }
-    }
+    } // eoHeader
+
+    /* Error checking */
     if(!found_input_names){
       SU2_MPI::Error("No MLP input variable names provided", CURRENT_FUNCTION);
     }
@@ -207,6 +209,7 @@ void MLPToolbox::CReadNeuralNetwork::ReadMLPFile(){
 }
 
 string MLPToolbox::CReadNeuralNetwork::SkipToFlag(ifstream *file_stream, string flag) {
+  /*--- Search file for a line and set it as the current line in the file stream ---*/
   string line;
   getline(*file_stream, line);
 
diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index 4150c6f0080..fcdc440252d 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -49,8 +49,6 @@ class CDataDrivenFluid : public CFluidModel {
   su2double Newton_Relaxation,     // Relaxation factor for Newton solvers.
             rho_start,             // Initial value for the density in Newton solver processes.
             e_start;               // Initial value for the energy in Newton solver processes.
-
-  string input_filename;    // Data-driven method input file name.
   
   su2double dsde_rho, dsdrho_e, d2sde2, d2sdedrho, d2sdrho2;
   
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index d733ea63f7c..1be3b117a01 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -31,17 +31,14 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
 
   Kind_DataDriven_Method = config->GetKind_DataDriven_Method();
 
-  /*--- Retrieve interpolation method file name. ---*/
-  input_filename = config->GetDataDriven_Filename();
-
   /*--- Set up interpolation algorithm according to data-driven method. Currently only MLP's are supported. ---*/
   switch (Kind_DataDriven_Method)
   {
   case ENUM_DATADRIVEN_METHOD::MLP:
-    lookup_mlp = new MLPToolbox::CLookUp_ANN(input_filename);
+    lookup_mlp = new MLPToolbox::CLookUp_ANN(config->GetNDataDriven_Files(), config->GetDataDriven_FileNames());
     break;
   case ENUM_DATADRIVEN_METHOD::LUT:
-    lookup_table = new CLookUpTable(input_filename, "Density", "Energy");
+    lookup_table = new CLookUpTable(config->GetDataDriven_Filename(), "Density", "Energy");
     break;
   default:
     break;
@@ -268,7 +265,7 @@ void CDataDrivenFluid::SetTDState_rhoT(su2double rho, su2double T) {
     delta_T = Temperature - T;
 
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if(100*(abs(delta_T)/T < tolerance_T)){
+    if(100*abs(delta_T)/T < tolerance_T){
       converged = true;
     }else{
       
diff --git a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
index f2ec5387764..73b2479c91f 100644
--- a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
+++ b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
@@ -31,8 +31,9 @@
 #include "../../../../Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp"
 
 TEST_CASE("LookUp ANN test", "[LookUpANN]"){
-
-  MLPToolbox::CLookUp_ANN ANN("src/SU2/UnitTests/Common/toolboxes/multilayer_perceptron/mlp_collection.mlp");
+  std::string MLP_input_files[] = {"src/SU2/UnitTests/Common/toolboxes/multilayer_perceptron/mlp_collection.mlp"};
+  unsigned short n_MLPs = 1;
+  MLPToolbox::CLookUp_ANN ANN(n_MLPs, MLP_input_files);
   su2vector<std::string> MLP_input_names,
                            MLP_output_names;
   su2vector<su2double> MLP_inputs;

From 0342d2fcae84bfb0caf473f7a64c1c24ce65668a Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Thu, 15 Dec 2022 10:54:40 +0100
Subject: [PATCH 083/656] Replaced arrays with su2vectors where possible

---
 Common/include/containers/CFileReaderLUT.hpp | 18 ++++----
 Common/include/containers/CLookUpTable.hpp   | 44 +++++++++---------
 Common/src/containers/CFileReaderLUT.cpp     | 30 +++++--------
 Common/src/containers/CLookUpTable.cpp       | 47 +++++++-------------
 4 files changed, 56 insertions(+), 83 deletions(-)

diff --git a/Common/include/containers/CFileReaderLUT.hpp b/Common/include/containers/CFileReaderLUT.hpp
index 8e602eb45a0..d44182fb254 100644
--- a/Common/include/containers/CFileReaderLUT.hpp
+++ b/Common/include/containers/CFileReaderLUT.hpp
@@ -46,11 +46,12 @@ class CFileReaderLUT {
   std::string version_lut;
   std::string version_reader;
   unsigned long n_levels = 1;
-  unsigned long *n_points;
-  unsigned long *n_triangles;
-  unsigned long *n_hull_points;
+  su2vector<unsigned long> n_points, 
+                           n_triangles, 
+                           n_hull_points;
+
   unsigned long n_variables;
-  su2double *table_levels = nullptr;
+  su2vector<su2double> table_levels;
 
   /*! \brief Holds the variable names stored in the table file. 
    * Order is in sync with tableFlamelet.
@@ -60,11 +61,11 @@ class CFileReaderLUT {
   /*! \brief Holds all data stored in the table. 
    * First index addresses the variable while second index addresses the point.
    */
-  su2activematrix *table_data;
+  su2vector<su2activematrix>table_data;
 
-  su2matrix<unsigned long> *triangles;
+  su2vector<su2matrix<unsigned long>>triangles;
 
-  su2vector<unsigned long> *hull;
+  su2vector<su2vector<unsigned long>>hull;
   /*! \brief Searches for the position of flag in file_stream and 
    *         sets the stream position of file_stream to that position.
    */
@@ -80,8 +81,7 @@ class CFileReaderLUT {
   bool GetStrippedLine(std::ifstream& file_stream, std::string& line) const;
 
  public:
-  CFileReaderLUT(){};
-  ~CFileReaderLUT();
+ 
   inline const std::string& GetVersionLUT() const { return version_lut; }
   inline const std::string& GetVersionReader() const { return version_reader; }
   inline unsigned long GetNPoints(std::size_t i_level=0) const { return n_points[i_level]; }
diff --git a/Common/include/containers/CLookUpTable.hpp b/Common/include/containers/CLookUpTable.hpp
index a281c7a35ef..340b86f1300 100644
--- a/Common/include/containers/CLookUpTable.hpp
+++ b/Common/include/containers/CLookUpTable.hpp
@@ -44,27 +44,28 @@ class CLookUpTable {
  protected:
   int rank; /*!< \brief MPI Rank. */
 
-  std::string file_name_lut,  // LUT file name.
-              version_lut,    // LUT version as specified in LUT file.
-              version_reader, // Reader version (should be equal or above LUT version).
-              name_CV1,       // Name of controlling variable 1.
-              name_CV2;       // Name of xontrolling variable 2.
+  std::string file_name_lut,  /*!< \brief LUT file name.*/ 
+              version_lut,    /*!< \brief LUT version as specified in LUT file.*/ 
+              version_reader, /*!< \brief Reader version (should be equal or above LUT version).*/ 
+              name_CV1,       /*!< \brief Name of controlling variable 1.*/ 
+              name_CV2;       /*!< \brief Name of xontrolling variable 2.*/ 
 
-  unsigned long *n_points,          // Number of data points per table level.
-                *n_triangles,       // Cell count per table level.
-                *n_hull_points,     // Number of boundary points per table level.
-                n_variables,        // Number of variables stored in the table.
-                n_table_levels = 1; // Number of table levels in the z-direction.
+  su2vector<unsigned long>  n_points,       /*!< \brief Number of data poins per table level.*/ 
+                            n_triangles,    /*!< \brief Number of triangles per table level.*/ 
+                            n_hull_points;  /*!< \brief Number of outer boundary points per table level.*/ 
 
-  su2double *z_values_levels = nullptr; // Constant z-values of each table level.
+  unsigned long n_variables,      
+                n_table_levels=1;
 
-  unsigned short table_dim = 2; // Table dimension.
+  su2vector<su2double> z_values_levels; /*!< \brief Constant z-values of each table level.*/ 
+
+  unsigned short table_dim = 2;/*!< \brief Table dimension.*/ 
   /*! 
    * \brief the lower and upper limits of the z, y and x variable for each table level.
    */
   std::pair<su2double, su2double> limits_table_z;
-  std::pair<su2double, su2double> *limits_table_y;
-  std::pair<su2double, su2double> *limits_table_x;
+  su2vector<std::pair<su2double, su2double>> limits_table_y, 
+                                             limits_table_x;
 
   /*! \brief Holds the variable names stored in the table file.
    * Order is in sync with data
@@ -75,34 +76,34 @@ class CLookUpTable {
    * Holds all data stored in the table. First index addresses the variable
    * while second index addresses the point.
    */
-  su2activematrix *table_data;
+  su2vector<su2activematrix> table_data;
 
   /*! \brief
    * Holds all connectivity data stored in the table for each level. First index 
    * addresses the variable while second index addresses the point.
    */
-  su2matrix<unsigned long> *triangles;
+  su2vector<su2matrix<unsigned long>>triangles;
 
   /*! \brief
    * Edge information for each table level.
    */
-  std::vector<su2vector<unsigned long> > *edges;
-  su2vector<std::vector<unsigned long> > *edge_to_triangle;
+  su2vector<std::vector<su2vector<unsigned long>>>edges;
+  su2vector<su2vector<std::vector<unsigned long>>>edge_to_triangle;
 
   /*! \brief 
    * The hull contains the boundary of the lookup table.
    */
-  su2vector<unsigned long> *hull;
+  su2vector<su2vector<unsigned long>>hull;
 
   /*! \brief 
    * Trapezoidal map objects for the table levels.
    */
-  CTrapezoidalMap *trap_map_x_y;
+  su2vector<CTrapezoidalMap>trap_map_x_y;
 
   /*! \brief 
    * vector of all the weight factors for the interpolation.
    */
-  su2vector<su2activematrix> *interp_mat_inv_x_y;
+  su2vector<su2vector<su2activematrix>>interp_mat_inv_x_y;
 
   /*! \brief 
    * returns the index to the variable in the lookup table.
@@ -239,7 +240,6 @@ class CLookUpTable {
 
  public:
   CLookUpTable(const std::string& file_name_lut, const std::string& name_x, const std::string& name_y);
-  ~CLookUpTable();
 
   /*!
    * \brief print information to screen.
diff --git a/Common/src/containers/CFileReaderLUT.cpp b/Common/src/containers/CFileReaderLUT.cpp
index 1fd99cf5f77..6714bfcf697 100644
--- a/Common/src/containers/CFileReaderLUT.cpp
+++ b/Common/src/containers/CFileReaderLUT.cpp
@@ -72,9 +72,9 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
         table_dim = 2;
         n_levels = 1;
         found_level_count = true;
-        n_points      = new unsigned long[n_levels];
-        n_triangles   = new unsigned long[n_levels];
-        n_hull_points = new unsigned long[n_levels];
+        n_points.resize(n_levels);
+        n_triangles.resize(n_levels);
+        n_hull_points.resize(n_levels);
       }else if(version_lut.compare("1.1.0") == 0){
         table_dim = 3;
       }else{
@@ -88,10 +88,10 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
       GetNextNonEmptyLine(file_stream, line);
       n_levels = stoul(line);
       
-      n_points      = new unsigned long[n_levels];
-      n_triangles   = new unsigned long[n_levels];
-      n_hull_points = new unsigned long[n_levels];
-      table_levels  = new su2double[n_levels];
+      n_points.resize(n_levels);
+      n_triangles.resize(n_levels);
+      n_hull_points.resize(n_levels);
+      table_levels.resize(n_levels);
     }
 
     /*--- number of points in LUT ---*/
@@ -172,17 +172,17 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
 
   /*--- now that n_variables, n_points, n_hull_points and n_variables are available, allocate memory ---*/
   if (rank == MASTER_NODE) cout << "allocating memory for the data, size = ( " << GetNVariables() << " , " << GetNPoints() << " )" << endl;
-  table_data = new su2activematrix[n_levels];
+  table_data.resize(n_levels);
   for(unsigned long i_level=0; i_level<n_levels; i_level++)
     table_data[i_level].resize(GetNVariables(), GetNPoints(i_level));
 
   if (rank == MASTER_NODE) cout << "allocating memory for the triangles, size = "<< GetNTriangles() << endl;
-  triangles = new su2matrix<unsigned long>[n_levels];
+  triangles.resize(n_levels);
   for(unsigned long i_level=0; i_level<n_levels; i_level++)
     triangles[i_level].resize(GetNTriangles(i_level), 3);
 
   if (rank == MASTER_NODE) cout << "allocating memory for the hull points, size = " << GetNHullPoints() << endl;
-  hull = new su2vector<unsigned long>[n_levels];
+  hull.resize(n_levels);
   for(unsigned long i_level=0; i_level<n_levels; i_level++)
     hull[i_level].resize(GetNHullPoints(i_level));
 
@@ -326,16 +326,6 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
 
 }
 
-CFileReaderLUT::~CFileReaderLUT(){
-  delete [] n_triangles;
-  delete [] n_hull_points;
-  delete [] n_points;
-  delete [] table_data;
-  delete [] hull;
-  delete [] triangles;
-  if(table_levels != nullptr) delete [] table_levels;
-}
-
 void CFileReaderLUT::SkipToFlag(ifstream& file_stream, const string& current_line, const string& flag) const {
   string next_line = "";
 
diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index f98a1ac4836..7537c95fea6 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -72,7 +72,7 @@ CLookUpTable::CLookUpTable(const string& var_file_name_lut, const string& name_x
     break;
   }
 
-  trap_map_x_y = new CTrapezoidalMap[n_table_levels];
+  trap_map_x_y.resize(n_table_levels);//= new CTrapezoidalMap[n_table_levels];
   su2double startTime = SU2_MPI::Wtime();
   for(auto i_level = 0ul; i_level<n_table_levels; i_level++){
     trap_map_x_y[i_level] = CTrapezoidalMap(GetDataP(name_x, i_level), GetDataP(name_y, i_level), table_data[i_level].cols(), edges[i_level], edge_to_triangle[i_level]);
@@ -113,23 +113,6 @@ CLookUpTable::CLookUpTable(const string& var_file_name_lut, const string& name_x
     cout << "LUT fluid model ready for use" << endl;
 }
 
-CLookUpTable::~CLookUpTable()
-{
-  delete [] trap_map_x_y;
-  delete [] n_points;
-  delete [] n_triangles;
-  delete [] n_hull_points;
-  delete [] table_data;
-  delete [] hull;
-  delete [] triangles;
-  delete [] interp_mat_inv_x_y;
-  delete [] edges;
-  delete [] edge_to_triangle;
-  delete [] limits_table_x;
-  delete [] limits_table_y;
-  if(z_values_levels != nullptr) delete [] z_values_levels;
-}
-
 void CLookUpTable::LoadTableRaw(const string& var_file_name_lut) {
   CFileReaderLUT file_reader;
 
@@ -140,15 +123,15 @@ void CLookUpTable::LoadTableRaw(const string& var_file_name_lut) {
   table_dim = file_reader.GetTableDim();
   n_table_levels = file_reader.GetNLevels();
 
-  n_points            = new unsigned long[n_table_levels];
-  n_triangles         = new unsigned long[n_table_levels];
-  n_hull_points       = new unsigned long[n_table_levels];
-  table_data          = new su2activematrix[n_table_levels];
-  hull                = new su2vector<unsigned long>[n_table_levels];
-  triangles           = new su2matrix<unsigned long>[n_table_levels];
-  interp_mat_inv_x_y  = new su2vector<su2activematrix>[n_table_levels];
-  edges               = new std::vector<su2vector<unsigned long> >[n_table_levels];
-  edge_to_triangle    = new su2vector<std::vector<unsigned long> >[n_table_levels];
+  n_points.resize(n_table_levels); 
+  n_triangles.resize(n_table_levels);
+  n_hull_points.resize(n_table_levels);
+  table_data.resize(n_table_levels);
+  hull.resize(n_table_levels);
+  triangles.resize(n_table_levels);
+  interp_mat_inv_x_y.resize(n_table_levels);
+  edges.resize(n_table_levels);
+  edge_to_triangle.resize(n_table_levels);
 
   for(unsigned long i_level=0; i_level<n_table_levels; i_level++){
     n_points[i_level] = file_reader.GetNPoints(i_level);
@@ -165,7 +148,7 @@ void CLookUpTable::LoadTableRaw(const string& var_file_name_lut) {
   names_var = file_reader.GetNamesVar();
 
   if(table_dim == 3){
-    z_values_levels = new su2double[n_table_levels];
+    z_values_levels.resize(n_table_levels);
     for(unsigned long i_level=0; i_level<n_table_levels; i_level++){
       z_values_levels[i_level] = file_reader.GetTableLevel(i_level);
     }
@@ -177,8 +160,8 @@ void CLookUpTable::LoadTableRaw(const string& var_file_name_lut) {
 void CLookUpTable::FindTableLimits(const string& name_cv1, const string& name_cv2) {
   int idx_X = GetIndexOfVar(name_cv1);
   int idx_Y = GetIndexOfVar(name_cv2);
-  limits_table_x = new pair<su2double, su2double>[n_table_levels];
-  limits_table_y = new pair<su2double, su2double>[n_table_levels];
+  limits_table_x.resize(n_table_levels);
+  limits_table_y.resize(n_table_levels);
 
   /* we find the lowest and highest value of y and x in the table */
   for(auto i_level=0u; i_level<n_table_levels; i_level++)
@@ -194,8 +177,8 @@ void CLookUpTable::FindTableLimits(const string& name_cv1, const string& name_cv
 
   if(table_dim == 3){
     su2double min_z, max_z;
-    min_z = *min_element(z_values_levels, z_values_levels + n_table_levels);
-    max_z = *max_element(z_values_levels, z_values_levels + n_table_levels);
+    min_z = z_values_levels[0];
+    max_z = z_values_levels[n_table_levels - 1];
     limits_table_z = make_pair(min_z, max_z);
   }
 }

From f278813736d06aa3cd27e8ee2dc31c3156e57d78 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Thu, 15 Dec 2022 15:10:44 +0100
Subject: [PATCH 084/656] Removed redundant commented line

---
 Common/src/containers/CLookUpTable.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index 7537c95fea6..df4758db1b5 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -72,7 +72,7 @@ CLookUpTable::CLookUpTable(const string& var_file_name_lut, const string& name_x
     break;
   }
 
-  trap_map_x_y.resize(n_table_levels);//= new CTrapezoidalMap[n_table_levels];
+  trap_map_x_y.resize(n_table_levels);
   su2double startTime = SU2_MPI::Wtime();
   for(auto i_level = 0ul; i_level<n_table_levels; i_level++){
     trap_map_x_y[i_level] = CTrapezoidalMap(GetDataP(name_x, i_level), GetDataP(name_y, i_level), table_data[i_level].cols(), edges[i_level], edge_to_triangle[i_level]);

From 0e23ce6e474660097cb0711b87f1089444cb855e Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 19 Dec 2022 16:05:26 +0100
Subject: [PATCH 085/656] Removed necessity to provide a separate MLP
 collection input file and added preliminary MLP derivative computation

---
 .../multilayer_perceptron/CLayer.hpp          | 11 ++-
 .../multilayer_perceptron/CLookUp_ANN.hpp     |  8 --
 .../multilayer_perceptron/CNeuralNetwork.hpp  |  9 +++
 .../multilayer_perceptron/CNeuron.hpp         |  6 +-
 .../multilayer_perceptron/CLookUp_ANN.cpp     | 47 -----------
 .../multilayer_perceptron/CNeuralNetwork.cpp  | 80 ++++++++++++++++++-
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        | 18 ++---
 SU2_CFD/src/solvers/CEulerSolver.cpp          |  6 +-
 .../nicf/datadriven/datadriven_nozzle.cfg     |  2 +-
 .../CLookUp_ANN_tests.cpp                     |  2 +-
 .../multilayer_perceptron/mlp_collection.mlp  |  5 --
 11 files changed, 114 insertions(+), 80 deletions(-)
 delete mode 100644 UnitTests/Common/toolboxes/multilayer_perceptron/mlp_collection.mlp

diff --git a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
index 07b0bdb8e46..ac51e22ffeb 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
@@ -118,7 +118,16 @@ class CLayer
     * \param[in] i_neuron - Neuron index
     * \return Gradient of neuron output wrt input
     */
-    su2double getdYdX(std::size_t i_neuron){ return neurons[i_neuron].getGradient(); }
+    su2double getdYdX(std::size_t i_neuron, std::size_t iInput){ return neurons[i_neuron].getGradient(iInput); }
+
+    /*!
+    * \brief Get the output-input gradient of a neuron in the layer
+    * \param[in] i_neuron - Neuron index
+    * \return Gradient of neuron output wrt input
+    */
+    void setdYdX(std::size_t i_neuron, std::size_t iInput, su2double dy_dx){ neurons[i_neuron].setGradient(iInput, dy_dx); }
+
+    void sizeGradients(std::size_t nInputs) { for(auto iNeuron=0u; iNeuron < number_of_neurons; iNeuron++) neurons[iNeuron].sizeGradient(nInputs); }
 
     /*!
     * \brief Get the activation function name applied to this layer
diff --git a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
index a737413b6a0..e98e9fc2213 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
@@ -57,8 +57,6 @@ class CLookUp_ANN
     int rank{0};
     su2vector<CNeuralNetwork*> NeuralNetworks;  /*!< std::vector containing all loaded neural networks. */
 
-    std::vector<std::string> ANN_filenames;       /*!< Filenames containing ANN architecture information. */
-
     unsigned short number_of_variables;  /*!< Number of loaded ANNs. */
 
     /*!
@@ -75,12 +73,6 @@ class CLookUp_ANN
     * \param[in] filename - filename containing ANN architecture information
     */
     void GenerateANN(CNeuralNetwork*ANN, std::string filename);
-
-    /*!
-    * \brief Read ANN architecture input file
-    * \param[in] filename - filename containing ANN architecture information
-    */
-    void ReadANNInputFile(std::string fileName); 
     
     public: 
     
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
index c49a8e323fb..037bf8e7708 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
@@ -61,6 +61,7 @@ class CNeuralNetwork
                                         // is skipped if current inputs are the same as the last inputs.
 
     su2double* ANN_outputs; // Pointer to network outputs
+    su2matrix<su2double> dOutputs_dInputs;
 
     /*--- Activation function types that are currently supported ---*/
     enum ENUM_ACTIVATION_FUNCTION {
@@ -233,6 +234,7 @@ class CNeuralNetwork
     */
     su2double GetANN_Output(std::size_t iOutput) const { return ANN_outputs[iOutput]; }
 
+    su2double GetOutput_Input_Derivative(std::size_t iOutput, std::size_t iInput) const { return dOutputs_dInputs[iOutput][iInput]; }
     /*!
     * \brief Set the activation function array size.
     * \param[in] n_layers - network layer count.
@@ -254,6 +256,13 @@ class CNeuralNetwork
         }
         return x;
     }
+    su2double ComputedOutputdInput(std::size_t iLayer, std::size_t iNeuron, std::size_t iInput) const {
+        su2double doutput_dinput = 0;
+        for(auto jNeuron=0u; jNeuron<total_layers[iLayer - 1]->getNNeurons(); jNeuron++){
+            doutput_dinput += weights_mat[iLayer - 1][iNeuron][jNeuron] * total_layers[iLayer-1]->getdYdX(jNeuron, iInput);
+        }
+        return doutput_dinput;
+    }
 };
 
 
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
index f06802f4688..1122e343309 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
@@ -42,6 +42,7 @@ class CNeuron
               input{0},             /*!< Input value of the current neuron */
               doutput_dinput{0},    /*!< Gradient of output with respect to input */
               bias{0};              /*!< Bias value at current neuron */
+    su2vector<su2double> doutput_dinputs;
 
 public:
 
@@ -93,17 +94,18 @@ class CNeuron
     */
     su2double getBias() const { return bias; }
 
+    void sizeGradient(std::size_t nInputs) { doutput_dinputs.resize(nInputs); }
     /*!
     * \brief Set neuron output gradient with respect to its input value
     * \param[in] input - Derivative of activation function with respect to input
     */
-    void setGradient(su2double input){ doutput_dinput = input; }
+    void setGradient(std::size_t iInput, su2double input){ doutput_dinputs[iInput] = input; }
 
     /*!
     * \brief Get neuron output gradient with respect to input value
     * \return output gradient wrt input value
     */
-    su2double getGradient() const { return doutput_dinput; }
+    su2double getGradient(std::size_t iInput) const { return doutput_dinputs[iInput]; }
 };
 
 }
diff --git a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
index 3bf605c297b..3806aed5e03 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
@@ -188,53 +188,6 @@ void MLPToolbox::CLookUp_ANN::GenerateANN(CNeuralNetwork * ANN, string fileName)
     
 }
 
-void MLPToolbox::CLookUp_ANN::ReadANNInputFile(string inputFileName)
-{
-    /*--- Read MLP collection input file and store relevant data ---*/
-
-    ifstream file_stream;
-    istringstream stream_names_var;
-    istringstream stream_filenames;
-    file_stream.open(inputFileName.c_str(), ifstream::in);
-
-    if (!file_stream.is_open()) {
-      SU2_MPI::Error(string("There is no MLP collection file file called ") + inputFileName,
-                    CURRENT_FUNCTION);
-    }
-
-    string line, word;
-
-    line = SkipToFlag(&file_stream, "[number of MLP files]");
-    getline(file_stream, line);
-    number_of_variables = stoul(line);
-    NeuralNetworks.resize(number_of_variables);
-
-    line = SkipToFlag(&file_stream, "[MLP file names]");
-    getline(file_stream, line);
-    stream_filenames.str(line);
-    while(stream_filenames){
-        stream_filenames >> word;
-        ANN_filenames.push_back(word);
-    }
-    ANN_filenames.pop_back();
-    if(ANN_filenames.size() != number_of_variables)
-        SU2_MPI::Error(string("Inconsistency betwee"),
-                    CURRENT_FUNCTION);
-}
-string MLPToolbox::CLookUp_ANN::SkipToFlag(ifstream *file_stream, string flag) {
-  string line;
-  getline(*file_stream, line);
-
-  while (line.compare(flag) != 0 && !(*file_stream).eof()) {
-    getline(*file_stream, line);
-  }
-
-  if ((*file_stream).eof())
-    SU2_MPI::Error("Flag " + flag + " not found in file", CURRENT_FUNCTION);
-
-  return line;
-}
-
 bool MLPToolbox::CLookUp_ANN::Check_Use_of_Inputs(su2vector<string> &input_names, CIOMap *input_output_map) const {
     /*--- Check wether all input variables are in the loaded MLPs ---*/
     vector<string> missing_inputs;
diff --git a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
index 76855992caf..28b2c745552 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
@@ -35,14 +35,15 @@ using namespace std;
 void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
     /*--- Evaluate MLP for given inputs ---*/
 
-    su2double y;           // Activation function output.
+    su2double y, dy_dx;           // Activation function output.
     bool same_point = true;
-
+    bool compute_gradient = false; // TODO: get this from function inputs
     /* Normalize input and check if inputs are the same w.r.t last evaluation */
     for(auto iNeuron=0u; iNeuron<inputLayer->getNNeurons(); iNeuron++){
         su2double x_norm = (inputs[iNeuron] - input_norm[iNeuron].first)/(input_norm[iNeuron].second - input_norm[iNeuron].first);
         if(abs(x_norm - inputLayer->getOutput(iNeuron)) > 0) same_point = false;
         inputLayer->setOutput(iNeuron, x_norm);
+        if(compute_gradient) inputLayer->setdYdX(iNeuron, iNeuron, 1 / (input_norm[iNeuron].second - input_norm[iNeuron].first));
     }
     /* Skip evaluation process if current point is the same as during the previous evaluation */
     if(!same_point){
@@ -57,6 +58,12 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
             for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
                 x = ComputeX(iLayer, iNeuron);
                 total_layers[iLayer]->setInput(iNeuron, x);
+                if(compute_gradient){
+                    for(auto iInput=0u; iInput<inputLayer->getNNeurons(); iInput++){
+                        dy_dx = ComputedOutputdInput(iLayer, iNeuron, iInput);
+                        total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx);
+                    }
+                }
             }
 
             /* Compute and store neuron output based on activation function */
@@ -78,10 +85,17 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
                         x = total_layers[iLayer]->getInput(iNeuron);
                         if(x > 0){
                             y = x;
+                            if(compute_gradient) dy_dx = 1.0;
                         }else{
                             y = exp(x) - 1;
+                            if(compute_gradient) dy_dx = exp(x);
                         }
                         total_layers[iLayer]->setOutput(iNeuron, y);
+                        if(compute_gradient){
+                            for(auto iInput=0u; iInput<inputLayer->getNNeurons(); iInput++){
+                                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+                            }
+                        }
                     }
                     break;
                 case ENUM_ACTIVATION_FUNCTION::LINEAR:
@@ -89,6 +103,12 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
                         x = total_layers[iLayer]->getInput(iNeuron);
                         y = x;
                         total_layers[iLayer]->setOutput(iNeuron, y);
+                        if(compute_gradient){
+                            dy_dx = 1.0;
+                            for(auto iInput=0u; iInput<inputLayer->getNNeurons(); iInput++){
+                                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+                            }
+                        }
                     }
                     break;
                 case ENUM_ACTIVATION_FUNCTION::RELU:
@@ -96,10 +116,17 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
                         x = total_layers[iLayer]->getInput(iNeuron);
                         if(x > 0){
                             y = x;
+                            if(compute_gradient) dy_dx = 1.0;
                         }else{
                             y = 0.0;
+                            if(compute_gradient) dy_dx = 0.0;
                         }
                         total_layers[iLayer]->setOutput(iNeuron, y);
+                        if(compute_gradient){
+                            for(auto iInput=0u; iInput<inputLayer->getNNeurons(); iInput++){
+                                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+                            }
+                        }
                     }
                     break;
                 case ENUM_ACTIVATION_FUNCTION::SWISH:
@@ -107,6 +134,12 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
                         x = total_layers[iLayer]->getInput(iNeuron);
                         y = x / (1 + exp(-x));
                         total_layers[iLayer]->setOutput(iNeuron, y);
+                        if(compute_gradient){
+                            dy_dx = exp(x)*(x + exp(x) + 1)/pow(exp(x) + 1, 2);
+                            for(auto iInput=0u; iInput<inputLayer->getNNeurons(); iInput++){
+                                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+                            }
+                        }
                     }
                     break;
                 case ENUM_ACTIVATION_FUNCTION::TANH:
@@ -114,6 +147,12 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
                         x = total_layers[iLayer]->getInput(iNeuron);
                         y = tanh(x);
                         total_layers[iLayer]->setOutput(iNeuron, y);
+                        if(compute_gradient){
+                            dy_dx = 1 / pow(cosh(x), 2);
+                            for(auto iInput=0u; iInput<inputLayer->getNNeurons(); iInput++){
+                                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+                            }
+                        }
                     }
                     break;
                 case ENUM_ACTIVATION_FUNCTION::SIGMOID:
@@ -121,6 +160,12 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
                         x = total_layers[iLayer]->getInput(iNeuron);
                         y = 1.0/(1 + exp(-x));
                         total_layers[iLayer]->setOutput(iNeuron, y);
+                        if(compute_gradient){
+                            dy_dx = exp(-x) / pow(exp(-x) + 1, 2);
+                            for(auto iInput=0u; iInput<inputLayer->getNNeurons(); iInput++){
+                                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+                            }
+                        }
                     }
                     break;
                 case ENUM_ACTIVATION_FUNCTION::SELU:
@@ -128,10 +173,17 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
                         x = total_layers[iLayer]->getInput(iNeuron);
                         if(x > 0.0){
                             y = lambda * x;
+                            if(compute_gradient) dy_dx = lambda;
                         }else{
                             y = lambda * alpha * (exp(x) - 1);
+                            if(compute_gradient) dy_dx = lambda * alpha * exp(x);
                         }
                         total_layers[iLayer]->setOutput(iNeuron, y);
+                        if(compute_gradient){
+                            for(auto iInput=0u; iInput<inputLayer->getNNeurons(); iInput++){
+                                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+                            }
+                        }
                     }
                     break;
                 case ENUM_ACTIVATION_FUNCTION::GELU:
@@ -140,12 +192,24 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
 
                         y = 0.5 * x * (1 + tanh(sqrt(2 / PI_NUMBER) * (x + 0.044715 * pow(x, 3))));
                         total_layers[iLayer]->setOutput(iNeuron, y);
+                        if(compute_gradient){
+                            dy_dx = 0.5*(tanh(0.0356774*pow(x, 3) + 0.797885 * x) + (0.107032*pow(x, 3) + 0.797885*x)*pow(cosh(x), -2)*(0.0356774*pow(x, 3) + 0.797885 * x));
+                            for(auto iInput=0u; iInput<inputLayer->getNNeurons(); iInput++){
+                                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+                            }
+                        }
                     }
                     break;
                 case ENUM_ACTIVATION_FUNCTION::NONE:
                     for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
                         y = 0.0;
                         total_layers[iLayer]->setOutput(iNeuron, y);
+                        if(compute_gradient){
+                            dy_dx = 0.0;
+                            for(auto iInput=0u; iInput<inputLayer->getNNeurons(); iInput++){
+                                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+                            }
+                        }
                     }
                     break;
                 default:
@@ -157,7 +221,13 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
     for(auto iNeuron=0u; iNeuron<outputLayer->getNNeurons(); iNeuron++){
         su2double y_norm = outputLayer->getOutput(iNeuron);
         y = y_norm*(output_norm[iNeuron].second - output_norm[iNeuron].first) + output_norm[iNeuron].first;
-        
+        if(compute_gradient){
+            dy_dx = (output_norm[iNeuron].second - output_norm[iNeuron].first);
+            for(auto iInput=0u; iInput<inputLayer->getNNeurons(); iInput++){
+                outputLayer->setdYdX(iNeuron, iInput, dy_dx * outputLayer->getdYdX(iNeuron, iInput));
+                dOutputs_dInputs[iNeuron][iInput] = outputLayer->getdYdX(iNeuron, iInput);
+            }
+        }
         /* Storing output value */
         ANN_outputs[iNeuron] = y;
     }
@@ -205,6 +275,10 @@ void MLPToolbox::CNeuralNetwork::sizeWeights(){
     weights_mat[n_hidden_layers].resize(outputLayer->getNNeurons(), hiddenLayers[n_hidden_layers-1]->getNNeurons());
 
     ANN_outputs = new su2double[outputLayer->getNNeurons()];
+    dOutputs_dInputs.resize(outputLayer->getNNeurons(), inputLayer->getNNeurons());
+    for(auto iLayer=0u; iLayer<n_hidden_layers+2; iLayer++){
+        total_layers[iLayer]->sizeGradients(inputLayer->getNNeurons());
+    }
 }   
 
 void MLPToolbox::CNeuralNetwork::displayNetwork() const {
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 1be3b117a01..1ed94127899 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -146,8 +146,8 @@ void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
   su2double rho = rho_start, 
             e = e_start;
 
-  su2double tolerance_P = 1, // Tolerance percentage for pressure solution
-            tolerance_T = 1;  // Tolerance percentage for temperature solution
+  su2double tolerance_P = 0.1, // Tolerance percentage for pressure solution
+            tolerance_T = 0.1;  // Tolerance percentage for temperature solution
 
   bool converged = false;         // Convergence flag
   unsigned long iter_max = 500,  // Maximum number of iterations
@@ -204,10 +204,10 @@ void CDataDrivenFluid::SetEnergy_Prho(su2double P, su2double rho) {
   /*--- Setting initial values for energy ---*/
   su2double e = e_start;
 
-  su2double tolerance_P = 1.0; // Tolerance percentage for pressure solution
+  su2double tolerance_P = 0.1; // Tolerance percentage for pressure solution
 
   bool converged = false;         // Convergence flag
-  unsigned long iter_max = 200,  // Maximum number of iterations
+  unsigned long iter_max = 500,  // Maximum number of iterations
                 Iter = 0;       
 
   su2double delta_P,      // Pressure residual
@@ -246,7 +246,7 @@ void CDataDrivenFluid::SetTDState_rhoT(su2double rho, su2double T) {
   /*--- Setting initial values for density and energy ---*/
   su2double e = e_start;
 
-  su2double tolerance_T = 1;  // Tolerance for temperature solution
+  su2double tolerance_T = 0.1;  // Tolerance for temperature solution
 
   bool converged = false;         // Convergence flag
   unsigned long iter_max = 500,  // Maximum number of iterations
@@ -290,8 +290,8 @@ void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
   su2double rho = rho_start, 
             e = e_start;
 
-  su2double tolerance_h = 1, // Tolerance for enthalpy solution
-            tolerance_s = 1;  // Tolerance for entropy solution
+  su2double tolerance_h = 0.1, // Tolerance for enthalpy solution
+            tolerance_s = 0.1;  // Tolerance for entropy solution
 
   bool converged = false;         // Convergence flag
   unsigned long iter_max = 500,  // Maximum number of iterations
@@ -344,8 +344,8 @@ void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
   su2double rho = rho_start, 
             e = e_start;
 
-  su2double tolerance_P = 1, // Tolerance for pressure solution
-            tolerance_s = 1;  // Tolerance for entropy solution
+  su2double tolerance_P = 0.1, // Tolerance for pressure solution
+            tolerance_s = 0.1;  // Tolerance for entropy solution
 
   bool converged = false;         // Convergence flag
   unsigned long iter_max = 500,  // Maximum number of iterations
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index 447d0ce7d8d..bab9229cb15 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -1677,7 +1677,7 @@ unsigned long CEulerSolver::SetPrimitive_Variables(CSolver **solver_container, c
     /*--- Update en---*/
     if(config->GetKind_FluidModel() == DATADRIVEN_FLUID) {
       nodes->SetDataExtrapolation(iPoint, GetFluidModel()->GetExtrapolation());
-      nodes->SetEntropy(iPoint, GetFluidModel()->GetEntropy());
+      nodes->SetEntropy(iPoint, GetFluidModel()->GetStaticEnergy());
     }
 
     /* Check for non-realizable states for reporting. */
@@ -4654,8 +4654,8 @@ void CEulerSolver::BC_Riemann(CGeometry *geometry, CSolver **solver_container,
       GetFluidModel()->SetTDState_rhoe(Density_i, StaticEnergy_i);
 
       /*--- Set initial values for density and energy for Newton solvers in fluid model ---*/
-      GetFluidModel()->SetDensity(Density_i);
-      GetFluidModel()->SetEnergy(StaticEnergy_i);
+      GetFluidModel()->SetDensity(0.5*(Density_i + config->GetDensity_Init_DataDriven()));
+      GetFluidModel()->SetEnergy(0.5*(StaticEnergy_i + config->GetEnergy_Init_DataDriven()));
 
       Pressure_i = GetFluidModel()->GetPressure();
       Enthalpy_i = Energy_i + Pressure_i/Density_i;
diff --git a/TestCases/nicf/datadriven/datadriven_nozzle.cfg b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
index 4d7bd921ef2..2fac6c2b7c2 100644
--- a/TestCases/nicf/datadriven/datadriven_nozzle.cfg
+++ b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
@@ -37,7 +37,7 @@ REF_DIMENSIONALIZATION= DIMENSIONAL
 %
 FLUID_MODEL = DATADRIVEN_FLUID
 INTERPOLATION_METHOD = MLP 
-FILENAME_INTERPOLATOR = mlp_collection.mlp 
+FILENAMES_INTERPOLATOR = (mlp_air.mlp)
 DATADRIVEN_NEWTON_RELAXATION = 0.06
 DATADRIVEN_FLUID_INITIAL_DENSITY = 5.54548
 DATADRIVEN_FLUID_INITIAL_ENERGY = 1.8e+05
diff --git a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
index 73b2479c91f..e231623b84f 100644
--- a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
+++ b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
@@ -31,7 +31,7 @@
 #include "../../../../Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp"
 
 TEST_CASE("LookUp ANN test", "[LookUpANN]"){
-  std::string MLP_input_files[] = {"src/SU2/UnitTests/Common/toolboxes/multilayer_perceptron/mlp_collection.mlp"};
+  std::string MLP_input_files[] = {"src/SU2/UnitTests/Common/toolboxes/multilayer_perceptron/simple_mlp.mlp"};
   unsigned short n_MLPs = 1;
   MLPToolbox::CLookUp_ANN ANN(n_MLPs, MLP_input_files);
   su2vector<std::string> MLP_input_names,
diff --git a/UnitTests/Common/toolboxes/multilayer_perceptron/mlp_collection.mlp b/UnitTests/Common/toolboxes/multilayer_perceptron/mlp_collection.mlp
deleted file mode 100644
index b441964701b..00000000000
--- a/UnitTests/Common/toolboxes/multilayer_perceptron/mlp_collection.mlp
+++ /dev/null
@@ -1,5 +0,0 @@
-[number of MLP files]
-1
-
-[MLP file names]
-src/SU2/UnitTests/Common/toolboxes/multilayer_perceptron/simple_mlp.mlp 

From 94349ef78bff84576d153902a2a9527d52757328 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 20 Dec 2022 17:42:43 +0100
Subject: [PATCH 086/656] Implemented some of Pedro's comments

---
 Common/include/containers/CLookUpTable.hpp    | 18 +++--
 Common/include/containers/CTrapezoidalMap.hpp |  2 +-
 Common/src/containers/CFileReaderLUT.cpp      |  4 +-
 Common/src/containers/CLookUpTable.cpp        | 81 +++++++++----------
 Common/src/containers/CTrapezoidalMap.cpp     |  2 +-
 5 files changed, 51 insertions(+), 56 deletions(-)

diff --git a/Common/include/containers/CLookUpTable.hpp b/Common/include/containers/CLookUpTable.hpp
index 340b86f1300..47136f19fcb 100644
--- a/Common/include/containers/CLookUpTable.hpp
+++ b/Common/include/containers/CLookUpTable.hpp
@@ -63,8 +63,8 @@ class CLookUpTable {
   /*! 
    * \brief the lower and upper limits of the z, y and x variable for each table level.
    */
-  std::pair<su2double, su2double> limits_table_z;
-  su2vector<std::pair<su2double, su2double>> limits_table_y, 
+  std::pair<su2double*, su2double*> limits_table_z;
+  su2vector<std::pair<su2double*, su2double*>> limits_table_y, 
                                              limits_table_x;
 
   /*! \brief Holds the variable names stored in the table file.
@@ -87,7 +87,7 @@ class CLookUpTable {
   /*! \brief
    * Edge information for each table level.
    */
-  su2vector<std::vector<su2vector<unsigned long>>>edges;
+  su2vector<std::vector<std::array<unsigned long,2>>>edges;
   su2vector<su2vector<std::vector<unsigned long>>>edge_to_triangle;
 
   /*! \brief 
@@ -193,7 +193,8 @@ class CLookUpTable {
    * \param[in] upper_value - Result from x-y interpolation on the upper table level.
    * \param[in] val_vars - Pointer to interpolation result.
   */
-  void Linear_Interpolation(const su2double val_z, const unsigned long lower_level, const unsigned long upper_level, su2double&lower_value,su2double&upper_value, su2double*&var_vals);
+  void Linear_Interpolation(const su2double val_z, const unsigned long lower_level, const unsigned long upper_level,
+                            su2double &lower_value, su2double &upper_value, su2double* &var_vals) const;
 
 
   /*!
@@ -205,7 +206,8 @@ class CLookUpTable {
    * \param[in] upper_values - Results from x-y interpolation on the upper table level.
    * \param[in] val_vars - Pointer to interpolation results for all interpolation variables.
   */
-  void Linear_Interpolation(const su2double val_z, const unsigned long lower_level, const unsigned long upper_level, std::vector<su2double>&lower_values,std::vector<su2double>&upper_values, std::vector<su2double*>&var_vals);
+  void Linear_Interpolation (const su2double val_z, const unsigned long lower_level, const unsigned long upper_level, 
+                            std::vector<su2double>&lower_values, std::vector<su2double>&upper_values, std::vector<su2double*>&var_vals) const;
 
   /*!
    * \brief find the point on the hull (boundary of the table) that is closest to the point P(val_x,val_y).
@@ -347,13 +349,13 @@ class CLookUpTable {
   * \param[in] within_limits - Whether query point lies within table bounds.
   * \returns pair of inclusion level indices (first = lower level index, second = upper level index)
   */
-  std::pair<unsigned long, unsigned long> FindInclusionLevels(const su2double val_z, bool *within_limits);
+  std::pair<unsigned long, unsigned long> FindInclusionLevels(const su2double val_z);
 
   /*!
    * \brief determine the minimum and maximum value of the second controlling variable.
    * \returns pair of minimum and maximum value of controlling variable 2.
    */
-  inline std::pair<su2double, su2double> GetTableLimitsY(unsigned long i_level = 0) const {
+  inline std::pair<su2double*, su2double*> GetTableLimitsY(unsigned long i_level = 0) const {
     return limits_table_y[i_level];
   }
 
@@ -361,7 +363,7 @@ class CLookUpTable {
    * \brief determine the minimum and maximum value of the first controlling variable.
    * \returns pair of minimum and maximum value of controlling variable 1.
    */
-  inline std::pair<su2double, su2double> GetTableLimitsX(unsigned long i_level = 0) const {
+  inline std::pair<su2double*, su2double*> GetTableLimitsX(unsigned long i_level = 0) const {
     return limits_table_x[i_level];
   }
 
diff --git a/Common/include/containers/CTrapezoidalMap.hpp b/Common/include/containers/CTrapezoidalMap.hpp
index 61e5f8f5b0a..1e6958f1f6a 100644
--- a/Common/include/containers/CTrapezoidalMap.hpp
+++ b/Common/include/containers/CTrapezoidalMap.hpp
@@ -62,7 +62,7 @@
   CTrapezoidalMap(const su2double* samples_x,
                   const su2double* samples_y,
                   const unsigned long size,
-                  const std::vector<su2vector<unsigned long> >& edges,
+                  const std::vector<std::array<unsigned long,2> >& edges,
                   const su2vector<std::vector<unsigned long> >& edge_to_triangle);
 
   /*!
diff --git a/Common/src/containers/CFileReaderLUT.cpp b/Common/src/containers/CFileReaderLUT.cpp
index 6714bfcf697..9625075b17a 100644
--- a/Common/src/containers/CFileReaderLUT.cpp
+++ b/Common/src/containers/CFileReaderLUT.cpp
@@ -257,7 +257,7 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
         eoLevel = true;
         if (n_triangles[levelCounter] != triCounter)
         SU2_MPI::Error(
-            "Number of read points on level " + std::to_string(levelCounter) + " does not match number of points "
+            "Number of read triangles on level " + std::to_string(levelCounter) + " does not match number of triangles "
             "specified in lookup table library header.",
             CURRENT_FUNCTION);
         levelCounter++;
@@ -304,7 +304,7 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
         eoLevel = true;
         if (n_hull_points[levelCounter] != hullCounter)
         SU2_MPI::Error(
-            "Number of read points on level " + std::to_string(levelCounter) + " does not match number of points "
+            "Number of read hull nodes on level " + std::to_string(levelCounter) + " does not match number of hull nodes "
             "specified in lookup table library header.",
             CURRENT_FUNCTION);
         levelCounter++;
diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index df4758db1b5..7109de8f484 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -74,19 +74,17 @@ CLookUpTable::CLookUpTable(const string& var_file_name_lut, const string& name_x
 
   trap_map_x_y.resize(n_table_levels);
   su2double startTime = SU2_MPI::Wtime();
+  unsigned short barwidth=65;
   for(auto i_level = 0ul; i_level<n_table_levels; i_level++){
     trap_map_x_y[i_level] = CTrapezoidalMap(GetDataP(name_x, i_level), GetDataP(name_y, i_level), table_data[i_level].cols(), edges[i_level], edge_to_triangle[i_level]);
     /* Display a progress bar to monitor table generation process */
     if(rank == MASTER_NODE){
       su2double progress = su2double(i_level) / n_table_levels;
-      unsigned short barwidth = 65;
-      auto pos = barwidth * progress;
-      cout << "[";
-      for(int iBar=0; iBar<barwidth; ++iBar){
-          if(iBar < pos) cout << "=";
-          else cout << " ";
-      }
-      cout << "] "<< floor(100*progress) << " %\r";
+      int done = int(progress*barwidth);
+      int to_do = barwidth - done;
+      cout << "[" << setfill('=') << setw(done);
+      cout << '>';
+      cout << setfill(' ') << setw(to_do) << std::right << "] " << 100*progress << "%\r";
       cout.flush();
     }
   }
@@ -166,20 +164,12 @@ void CLookUpTable::FindTableLimits(const string& name_cv1, const string& name_cv
   /* we find the lowest and highest value of y and x in the table */
   for(auto i_level=0u; i_level<n_table_levels; i_level++)
   {
-    su2double min_x, max_x, min_y, max_y;
-    min_y = *min_element(&table_data[i_level][idx_Y][0], &table_data[i_level][idx_Y][0]+table_data[i_level].cols());
-    min_x = *min_element(&table_data[i_level][idx_X][0], &table_data[i_level][idx_X][0]+table_data[i_level].cols());
-    max_y = *max_element(&table_data[i_level][idx_Y][0], &table_data[i_level][idx_Y][0]+table_data[i_level].cols());
-    max_x = *max_element(&table_data[i_level][idx_X][0], &table_data[i_level][idx_X][0]+table_data[i_level].cols());
-    limits_table_x[i_level] = make_pair(min_x, max_x);
-    limits_table_y[i_level] = make_pair(min_y, max_y);
+    limits_table_y[i_level] = minmax_element(table_data[i_level][idx_Y], table_data[i_level][idx_Y]+table_data[i_level].cols());
+    limits_table_x[i_level] = minmax_element(table_data[i_level][idx_X], table_data[i_level][idx_X]+table_data[i_level].cols());
   }
 
   if(table_dim == 3){
-    su2double min_z, max_z;
-    min_z = z_values_levels[0];
-    max_z = z_values_levels[n_table_levels - 1];
-    limits_table_z = make_pair(min_z, max_z);
+    limits_table_z = minmax_element(&z_values_levels[0], &z_values_levels[0]+z_values_levels.cols());
   }
 }
 
@@ -201,10 +191,10 @@ void CLookUpTable::PrintTableInfo() {
       n_points_av += n_points[i_level] / n_table_levels;
       n_tria_av += n_triangles[i_level] / n_table_levels;
       n_edges_av += edges[i_level].size() / n_table_levels;
-      min_x = min(min_x, limits_table_x[i_level].first);
-      min_y = min(min_y, limits_table_y[i_level].first);
-      max_x = max(max_x, limits_table_x[i_level].second);
-      max_y = max(max_y, limits_table_y[i_level].second);
+      min_x = min(min_x, *limits_table_x[i_level].first);
+      min_y = min(min_y, *limits_table_y[i_level].first);
+      max_x = max(max_x, *limits_table_x[i_level].second);
+      max_y = max(max_y, *limits_table_y[i_level].second);
     }
     switch (table_dim)
     {
@@ -331,7 +321,7 @@ void CLookUpTable::IdentifyUniqueEdges() {
 
       /* Store the edge so that the lower index of the pair is always first. */
       if (iPoint < GlobalIndex) {
-        su2vector<unsigned long> edge(2);
+        std::array<unsigned long,2> edge;
         edge[0] = iPoint;
         edge[1] = GlobalIndex;
         edges[i_level].push_back(edge);
@@ -415,23 +405,20 @@ void CLookUpTable::GetInterpMatInv(const su2double* vec_x, const su2double* vec_
 
 }
 
-std::pair<unsigned long, unsigned long> CLookUpTable::FindInclusionLevels(const su2double val_z, bool*within_table_limits)
+std::pair<unsigned long, unsigned long> CLookUpTable::FindInclusionLevels(const su2double val_z)
 {
   /*--- Find the table levels with constant z-values directly below and above the query value val_z ---*/
 
   /* Check if val_z lies outside table bounds */
-  if(val_z >= limits_table_z.second){
-    *within_table_limits = false;
+  if(val_z >= *limits_table_z.second){
     return std::make_pair(n_table_levels-1, n_table_levels-1);
-  }else if(val_z <= limits_table_z.first){
-    *within_table_limits = false;
+  }else if(val_z <= *limits_table_z.first){
     return std::make_pair(0, 0);
   }else{
     std::pair<unsigned long, unsigned long> inclusion_levels;
     /* Loop over table levels to find the levels directly above and below the query value */
     for(auto i_level = 0ul; i_level < n_table_levels-1; i_level++){
       if((val_z >= z_values_levels[i_level]) && (val_z < z_values_levels[i_level+1])){
-        *within_table_limits = true;
         inclusion_levels = std::make_pair(i_level, i_level+1);
       }
     }
@@ -446,9 +433,9 @@ unsigned long CLookUpTable::LookUp_XYZ(const std::string& val_name_var, su2doubl
         with coordinates val_x, val_y, and val_z ---*/
 
   /* 1: Find table levels directly above and below the query point (the levels that sandwhich val_z) */
-  bool within_z_limits = true;
-  std::pair<unsigned long, unsigned long> inclusion_levels = FindInclusionLevels(val_z, &within_z_limits);
-  
+  std::pair<unsigned long, unsigned long> inclusion_levels = FindInclusionLevels(val_z);
+  bool within_z_limits = (inclusion_levels.first != inclusion_levels.second);
+
   if(within_z_limits){
     /* 2: Perform 2D interpolations on upper and lower inclusion levels */
     unsigned long lower_level = inclusion_levels.first;
@@ -477,8 +464,8 @@ unsigned long CLookUpTable::LookUp_XYZ(const std::vector<std::string>& val_names
         on a query point with coordinates val_x, val_y, and val_z ---*/
 
   /* 1: Find table levels directly above and below the query point (the levels that sandwhich val_z) */
-  bool within_z_limits = true;
-  std::pair<unsigned long, unsigned long> inclusion_levels = FindInclusionLevels(val_z, &within_z_limits);
+  std::pair<unsigned long, unsigned long> inclusion_levels = FindInclusionLevels(val_z);
+  bool within_z_limits = (inclusion_levels.first != inclusion_levels.second);
   
   if(within_z_limits){
     /* 2: Perform 2D interpolations on upper and lower inclusion levels */
@@ -504,7 +491,8 @@ unsigned long CLookUpTable::LookUp_XYZ(const std::vector<std::string>& val_names
   }
 }
 
-void CLookUpTable::Linear_Interpolation(const su2double val_z, const unsigned long lower_level, const unsigned long upper_level, su2double&lower_value,su2double&upper_value, su2double*&var_val)
+void CLookUpTable::Linear_Interpolation(const su2double val_z, const unsigned long lower_level, const unsigned long upper_level, 
+                                        su2double& lower_value, su2double& upper_value, su2double*& var_val) const
 {
   /* Perform linear interpolation along the z-direction of the table for a single variable */
 
@@ -520,7 +508,9 @@ void CLookUpTable::Linear_Interpolation(const su2double val_z, const unsigned lo
   *var_val = lower_value * factor_lower + upper_value * factor_upper;
 }
 
-void CLookUpTable::Linear_Interpolation(const su2double val_z, const unsigned long lower_level, const unsigned long upper_level, std::vector<su2double>&lower_values,std::vector<su2double>&upper_values, std::vector<su2double*>&var_vals)
+void CLookUpTable::Linear_Interpolation(const su2double val_z, const unsigned long lower_level, const unsigned long upper_level, 
+                                        std::vector<su2double>& lower_values, std::vector<su2double>& upper_values, 
+                                        std::vector<su2double*>& var_vals) const
 {
   /* Perform linear interpolation along the z-direction of the table for multiple variables */
 
@@ -539,7 +529,8 @@ void CLookUpTable::Linear_Interpolation(const su2double val_z, const unsigned lo
 }
 
 unsigned long CLookUpTable::LookUp_XY(const string& val_name_var, su2double *val_var, su2double val_x,
-                                            su2double val_y, unsigned long i_level) {
+                                            su2double val_y, unsigned long i_level)
+{
   unsigned long exit_code = 0;
 
   if (val_name_var.compare("NULL") == 0) {
@@ -549,8 +540,8 @@ unsigned long CLookUpTable::LookUp_XY(const string& val_name_var, su2double *val
   }
 
   /* check if x and y value is in table range */
-  if ((val_x >= limits_table_x[i_level].first && val_x <= limits_table_x[i_level].second) &&
-      (val_y >= limits_table_y[i_level].first && val_y <= limits_table_y[i_level].second)){
+  if ((val_x >= *limits_table_x[i_level].first && val_x <= *limits_table_x[i_level].second) &&
+      (val_y >= *limits_table_y[i_level].first && val_y <= *limits_table_y[i_level].second)){
 
     /* find the triangle that holds the (x, y) point */
     unsigned long id_triangle = trap_map_x_y[i_level].GetTriangle(val_x, val_y);
@@ -583,7 +574,8 @@ unsigned long CLookUpTable::LookUp_XY(const string& val_name_var, su2double *val
 }
 
 unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vector<su2double>& val_vars,
-                                            su2double val_x, su2double val_y, unsigned long i_level) {
+                                            su2double val_x, su2double val_y, unsigned long i_level) 
+{
   vector<su2double*> look_up_data(val_names_var.size());
 
   for (long unsigned int i_var = 0; i_var < val_vars.size(); ++i_var) {
@@ -596,7 +588,8 @@ unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vecto
 }
 
 unsigned long CLookUpTable::LookUp_ProgEnth(const std::string& val_name_var, su2double* val_var, su2double val_prog, 
-                                            su2double val_enth, std::string name_prog, std::string name_enth) {
+                                            su2double val_enth, std::string name_prog, std::string name_enth)
+{
   return LookUp_XY(val_name_var, val_var, val_prog, val_enth);
 }
 
@@ -620,8 +613,8 @@ unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vecto
 
   /* check if x value is in table x-dimension range
    * and if y is in table y-dimension table range */
-  if ((val_x >= limits_table_x[i_level].first && val_x <= limits_table_x[i_level].second) &&
-      (val_y >= limits_table_y[i_level].first && val_y <= limits_table_y[i_level].second)){
+  if ((val_x >= *limits_table_x[i_level].first && val_x <= *limits_table_x[i_level].second) &&
+      (val_y >= *limits_table_y[i_level].first && val_y <= *limits_table_y[i_level].second)){
     /* if so, try to find the triangle that holds the (prog, enth) point */
     id_triangle = trap_map_x_y[i_level].GetTriangle(val_x, val_y);
 
diff --git a/Common/src/containers/CTrapezoidalMap.cpp b/Common/src/containers/CTrapezoidalMap.cpp
index 80e49026483..767a1dde131 100644
--- a/Common/src/containers/CTrapezoidalMap.cpp
+++ b/Common/src/containers/CTrapezoidalMap.cpp
@@ -38,7 +38,7 @@ using namespace std;
  * NOTE: the current implementation is actually the simpler 'slab' approach.
  */
 CTrapezoidalMap::CTrapezoidalMap(const su2double* samples_x, const su2double* samples_y, const unsigned long size,
-                                 vector<su2vector<unsigned long> > const& edges,
+                                 vector<std::array<unsigned long,2> > const& edges,
                                  su2vector<vector<unsigned long> > const& val_edge_to_triangle) {
   edge_to_triangle = su2vector<vector<unsigned long> >(val_edge_to_triangle);
 

From 4e5952d98772d52c13dbbeca735283edd560c106 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Tue, 20 Dec 2022 14:18:42 -0800
Subject: [PATCH 087/656] Add error checks for FFD functions, fix FFD read
 segfault

---
 Common/src/drivers/CDriverBase.cpp | 80 ++++++++++++++++++++++++++++++
 SU2_CFD/src/drivers/CDriver.cpp    |  6 +--
 2 files changed, 82 insertions(+), 4 deletions(-)

diff --git a/Common/src/drivers/CDriverBase.cpp b/Common/src/drivers/CDriverBase.cpp
index dd1e3f9c88e..ab2e60049b6 100644
--- a/Common/src/drivers/CDriverBase.cpp
+++ b/Common/src/drivers/CDriverBase.cpp
@@ -80,18 +80,46 @@ unsigned short CDriverBase::GetNumberDesignVariables() const { return main_confi
 unsigned short CDriverBase::GetNumberFFDBoxes() const { return main_config->GetnFFDBox(); }
 
 unsigned short CDriverBase::GetNumberFFDBoxCornerPoints(unsigned short iFFDBox) const {
+  if (GetNumberFFDBoxes() == 0) {
+    SU2_MPI::Error("FFD Box definition not found in the mesh file.", CURRENT_FUNCTION);
+  }
+  if (iFFDBox >= GetNumberFFDBoxes()) {
+    SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
+  }
+
   return FFDBox[ZONE_0][iFFDBox]->GetnCornerPoints();
 }
 
 unsigned short CDriverBase::GetNumberFFDBoxControlPoints(unsigned short iFFDBox) const {
+  if (GetNumberFFDBoxes() == 0) {
+    SU2_MPI::Error("FFD Box definition not found in the mesh file.", CURRENT_FUNCTION);
+  }
+  if (iFFDBox >= GetNumberFFDBoxes()) {
+    SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
+  }
+
   return FFDBox[ZONE_0][iFFDBox]->GetnControlPoints();
 }
 
 unsigned long CDriverBase::GetNumberFFDBoxSurfacePoints(unsigned short iFFDBox) const {
+  if (GetNumberFFDBoxes() == 0) {
+    SU2_MPI::Error("FFD Box definition not found in the mesh file.", CURRENT_FUNCTION);
+  }
+  if (iFFDBox >= GetNumberFFDBoxes()) {
+    SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
+  }
+
   return FFDBox[ZONE_0][iFFDBox]->GetnSurfacePoint();
 }
 
 vector<unsigned short> CDriverBase::GetFFDBoxMarkerIDs(unsigned short iFFDBox) const {
+  if (GetNumberFFDBoxes() == 0) {
+    SU2_MPI::Error("FFD Box definition not found in the mesh file.", CURRENT_FUNCTION);
+  }
+  if (iFFDBox >= GetNumberFFDBoxes()) {
+    SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
+  }
+
   vector<unsigned short> values;
 
   for (auto iPoint = 0ul; iPoint < GetNumberFFDBoxSurfacePoints(iFFDBox); iPoint++) {
@@ -101,6 +129,13 @@ vector<unsigned short> CDriverBase::GetFFDBoxMarkerIDs(unsigned short iFFDBox) c
 }
 
 vector<unsigned long> CDriverBase::GetFFDBoxVertexIDs(unsigned short iFFDBox) const {
+  if (GetNumberFFDBoxes() == 0) {
+    SU2_MPI::Error("FFD Box definition not found in the mesh file.", CURRENT_FUNCTION);
+  }
+  if (iFFDBox >= GetNumberFFDBoxes()) {
+    SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
+  }
+
   vector<unsigned long> values;
 
   for (auto iPoint = 0ul; iPoint < GetNumberFFDBoxSurfacePoints(iFFDBox); iPoint++) {
@@ -110,6 +145,13 @@ vector<unsigned long> CDriverBase::GetFFDBoxVertexIDs(unsigned short iFFDBox) co
 }
 
 vector<unsigned long> CDriverBase::GetFFDBoxPointIDs(unsigned short iFFDBox) const {
+  if (GetNumberFFDBoxes() == 0) {
+    SU2_MPI::Error("FFD Box definition not found in the mesh file.", CURRENT_FUNCTION);
+  }
+  if (iFFDBox >= GetNumberFFDBoxes()) {
+    SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
+  }
+
   vector<unsigned long> values;
 
   for (auto iPoint = 0ul; iPoint < GetNumberFFDBoxSurfacePoints(iFFDBox); iPoint++) {
@@ -119,6 +161,13 @@ vector<unsigned long> CDriverBase::GetFFDBoxPointIDs(unsigned short iFFDBox) con
 }
 
 vector<vector<passivedouble>> CDriverBase::GetFFDBoxCornerCoordinates(unsigned short iFFDBox) const {
+  if (GetNumberFFDBoxes() == 0) {
+    SU2_MPI::Error("FFD Box definition not found in the mesh file.", CURRENT_FUNCTION);
+  }
+  if (iFFDBox >= GetNumberFFDBoxes()) {
+    SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
+  }
+
   vector<vector<passivedouble>> values;
 
   for (auto iPoint = 0u; iPoint < GetNumberFFDBoxCornerPoints(iFFDBox); iPoint++) {
@@ -137,6 +186,13 @@ vector<vector<passivedouble>> CDriverBase::GetFFDBoxCornerCoordinates(unsigned s
 }
 
 vector<vector<passivedouble>> CDriverBase::GetFFDBoxControlPointCoordinates(unsigned short iFFDBox) const {
+  if (GetNumberFFDBoxes() == 0) {
+    SU2_MPI::Error("FFD Box definition not found in the mesh file.", CURRENT_FUNCTION);
+  }
+  if (iFFDBox >= GetNumberFFDBoxes()) {
+    SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
+  }
+
   vector<vector<passivedouble>> values;
 
   for (auto iOrder = 0u; iOrder < FFDBox[ZONE_0][iFFDBox]->GetlOrder(); iOrder++) {
@@ -152,6 +208,13 @@ vector<vector<passivedouble>> CDriverBase::GetFFDBoxControlPointCoordinates(unsi
 
 vector<passivedouble> CDriverBase::GetFFDBoxControlPointCoordinates(unsigned short iFFDBox, unsigned int iOrder,
                                                                     unsigned int jOrder, unsigned int kOrder) const {
+  if (GetNumberFFDBoxes() == 0) {
+    SU2_MPI::Error("FFD Box definition not found in the mesh file.", CURRENT_FUNCTION);
+  }
+  if (iFFDBox >= GetNumberFFDBoxes()) {
+    SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
+  }
+
   vector<passivedouble> values;
 
   const su2double* coord = FFDBox[ZONE_0][iFFDBox]->GetCoordControlPoints(iOrder, jOrder, kOrder);
@@ -164,6 +227,13 @@ vector<passivedouble> CDriverBase::GetFFDBoxControlPointCoordinates(unsigned sho
 }
 
 vector<vector<passivedouble>> CDriverBase::GetFFDBoxSurfaceCoordinates(unsigned short iFFDBox, bool parametric) const {
+  if (GetNumberFFDBoxes() == 0) {
+    SU2_MPI::Error("FFD Box definition not found in the mesh file.", CURRENT_FUNCTION);
+  }
+  if (iFFDBox >= GetNumberFFDBoxes()) {
+    SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
+  }
+
   vector<vector<passivedouble>> values;
 
   for (auto iPoint = 0ul; iPoint < GetNumberFFDBoxSurfacePoints(iFFDBox); iPoint++) {
@@ -175,6 +245,16 @@ vector<vector<passivedouble>> CDriverBase::GetFFDBoxSurfaceCoordinates(unsigned
 
 vector<passivedouble> CDriverBase::GetFFDBoxSurfaceCoordinates(unsigned short iFFDBox, unsigned long iPoint,
                                                                bool parametric) const {
+  if (GetNumberFFDBoxes() == 0) {
+    SU2_MPI::Error("FFD Box definition not found in the mesh file.", CURRENT_FUNCTION);
+  }
+  if (iFFDBox >= GetNumberFFDBoxes()) {
+    SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
+  }
+  if (iPoint >= GetNumberFFDBoxSurfacePoints()) {
+    SU2_MPI::Error("FFD Box vertex index exceeds mesh size.", CURRENT_FUNCTION);
+  }
+
   vector<passivedouble> values;
   const su2double* coord;
 
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index 331c50b1ee4..23fb0b70a00 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -177,10 +177,8 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
     }
   }
 
-  /*--- Read free-form deformation design variables data. --- */
-  if (main_config->GetnFFDBox() != 0) {
-    ReadFFDInfo(main_geometry, main_config, FFDBox[ZONE_0], main_config->GetMesh_FileName());
-  }
+  /*--- Read free form deformation design variables data. --- */
+  ReadFFDInfo(geometry_container[ZONE_0][INST_0][MESH_0], config_container[ZONE_0], FFDBox[ZONE_0], config_container[ZONE_0]->GetMesh_FileName());
 
   /*--- Before we proceed with the zone loop we have to compute the wall distances.
      * This computation depends on all zones at once. ---*/

From 35eb6ada05949842bfe2c7dcc2b52a315727126c Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Tue, 20 Dec 2022 14:29:43 -0800
Subject: [PATCH 088/656] Fix missing input argument in CDriverBase.cpp

---
 Common/src/drivers/CDriverBase.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/Common/src/drivers/CDriverBase.cpp b/Common/src/drivers/CDriverBase.cpp
index ab2e60049b6..20b65f9a974 100644
--- a/Common/src/drivers/CDriverBase.cpp
+++ b/Common/src/drivers/CDriverBase.cpp
@@ -251,7 +251,7 @@ vector<passivedouble> CDriverBase::GetFFDBoxSurfaceCoordinates(unsigned short iF
   if (iFFDBox >= GetNumberFFDBoxes()) {
     SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
   }
-  if (iPoint >= GetNumberFFDBoxSurfacePoints()) {
+  if (iPoint >= GetNumberFFDBoxSurfacePoints(iFFDBox)) {
     SU2_MPI::Error("FFD Box vertex index exceeds mesh size.", CURRENT_FUNCTION);
   }
 

From 68edc822c01e02851960d7c997e918deb9235b15 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Wed, 21 Dec 2022 20:59:21 -0800
Subject: [PATCH 089/656] Fix FFD read error when there is no geometry file

---
 Common/src/drivers/CDriverBase.cpp | 5 +++++
 1 file changed, 5 insertions(+)

diff --git a/Common/src/drivers/CDriverBase.cpp b/Common/src/drivers/CDriverBase.cpp
index 20b65f9a974..74dda47ce3b 100644
--- a/Common/src/drivers/CDriverBase.cpp
+++ b/Common/src/drivers/CDriverBase.cpp
@@ -966,6 +966,11 @@ void CDriverBase::ReadFFDInfo(CGeometry* geometry, CConfig* config, CFreeFormDef
   unsigned short nFFDBox = 0;
   unsigned short nLevel = 0;
 
+  if (config->GetMesh_FileFormat() != SU2) {
+    if (rank == MASTER_NODE) cout << "Mesh file format is not .su2 so FFD box information cannot be extracted." << endl;
+    return;
+  }
+
   mesh_file.open(val_mesh_filename);
   if (mesh_file.fail()) {
     SU2_MPI::Error("There is no geometry file (ReadFFDInfo)!!", CURRENT_FUNCTION);

From 62be0487a02373c4c77a6dda5a30ccecc2746dc7 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Thu, 22 Dec 2022 11:38:52 +0100
Subject: [PATCH 090/656] Improved clang formatting

---
 .../multilayer_perceptron/CIOMap.hpp          |   4 +-
 .../multilayer_perceptron/CLayer.hpp          |  22 +--
 .../multilayer_perceptron/CLookUp_ANN.hpp     |  12 +-
 .../multilayer_perceptron/CNeuralNetwork.hpp  |  38 +++--
 .../multilayer_perceptron/CNeuron.hpp         |  17 ++-
 .../CReadNeuralNetwork.hpp                    | 132 ++++++++++++++----
 .../multilayer_perceptron/CIOMap.cpp          |   2 +-
 .../multilayer_perceptron/CLayer.cpp          |   2 +-
 .../multilayer_perceptron/CLookUp_ANN.cpp     |   6 +-
 .../multilayer_perceptron/CNeuralNetwork.cpp  |  23 +--
 .../multilayer_perceptron/CNeuron.cpp         |   2 +-
 .../CReadNeuralNetwork.cpp                    |  38 +++--
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp    |   2 +-
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        |   2 +-
 .../CLookUp_ANN_tests.cpp                     |   2 +-
 15 files changed, 187 insertions(+), 117 deletions(-)

diff --git a/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp b/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
index e4b357afa96..0b74c6bb939 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
@@ -2,7 +2,7 @@
  * \file CIOMap.hpp
  * \brief Declaration of input-to-output mapping class for artifical neural networks
  * \author E. Bunschoten
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -99,7 +99,7 @@ namespace MLPToolbox
         * \brief Set MLP index in IO map
         * \param[in] iMLP - loaded MLP index
         */
-        void Push_MLP_index(std::size_t iMLP){ MLP_indices.push_back(iMLP); }
+        void Push_MLP_index(std::size_t iMLP) { MLP_indices.push_back(iMLP); }
 
         /*!
         * \brief Pair call inputs and outputs with the inputs and outputs of 
diff --git a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
index ac51e22ffeb..b29800c52d0 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
@@ -2,7 +2,7 @@
  * \file CLayer.hpp
  * \brief Declaration of artificial neural network interpolation class
  * \author E. Bunschoten
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -63,7 +63,7 @@ class CLayer
     * \brief Define current layer as input layer
     * \param[in] input - input layer identifyer
     */
-    void setInput(bool def){ is_input = def; }
+    void setInput(bool def) { is_input = def; }
 
     /*!
     * \brief Get input layer identifyer
@@ -76,7 +76,7 @@ class CLayer
     * \param[in] i_neuron - Neuron index
     * \param[in] output_value - Activation function output
     */
-    void setOutput(std::size_t i_neuron, su2double value){ neurons[i_neuron].setOutput(value); }
+    void setOutput(std::size_t i_neuron, su2double value) { neurons[i_neuron].setOutput(value); }
 
     /*!
     * \brief Get the output value of a neuron in the layer
@@ -90,7 +90,7 @@ class CLayer
     * \param[in] i_neuron - Neuron index
     * \param[in] input_value - Activation function input
     */
-    void setInput(std::size_t i_neuron, su2double value){ neurons[i_neuron].setInput(value); }
+    void setInput(std::size_t i_neuron, su2double value) { neurons[i_neuron].setInput(value); }
 
     /*!
     * \brief Get the input value of a neuron in the layer
@@ -104,36 +104,40 @@ class CLayer
     * \param[in] i_neuron - Neuron index
     * \param[in] bias_value - Bias value
     */
-    void setBias(std::size_t i_neuron, su2double value){ neurons[i_neuron].setBias(value); }
+    void setBias(std::size_t i_neuron, su2double value) { neurons[i_neuron].setBias(value); }
 
     /*!
     * \brief Get the bias value of a neuron in the layer
     * \param[in] i_neuron - Neuron index
     * \return Neuron bias value
     */
-    su2double getBias(std::size_t i_neuron){ return neurons[i_neuron].getBias(); }
+    su2double getBias(std::size_t i_neuron) const { return neurons[i_neuron].getBias(); }
 
     /*!
     * \brief Get the output-input gradient of a neuron in the layer
     * \param[in] i_neuron - Neuron index
     * \return Gradient of neuron output wrt input
     */
-    su2double getdYdX(std::size_t i_neuron, std::size_t iInput){ return neurons[i_neuron].getGradient(iInput); }
+    su2double getdYdX(std::size_t i_neuron, std::size_t iInput) const { return neurons[i_neuron].getGradient(iInput); }
 
     /*!
     * \brief Get the output-input gradient of a neuron in the layer
     * \param[in] i_neuron - Neuron index
     * \return Gradient of neuron output wrt input
     */
-    void setdYdX(std::size_t i_neuron, std::size_t iInput, su2double dy_dx){ neurons[i_neuron].setGradient(iInput, dy_dx); }
+    void setdYdX(std::size_t i_neuron, std::size_t iInput, su2double dy_dx) { neurons[i_neuron].setGradient(iInput, dy_dx); }
 
+    /*!
+    * \brief Size neuron output derivative wrt network inputs.
+    * \param[in] nInputs - Number of network inputs.
+    */
     void sizeGradients(std::size_t nInputs) { for(auto iNeuron=0u; iNeuron < number_of_neurons; iNeuron++) neurons[iNeuron].sizeGradient(nInputs); }
 
     /*!
     * \brief Get the activation function name applied to this layer
     * \return name of the activation function
     */
-    string getActivationType(){ return activation_type; }
+    string getActivationType() const { return activation_type; }
     
 };
 
diff --git a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
index e98e9fc2213..f800b3709c4 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
@@ -2,7 +2,7 @@
  * \file CLookUp_ANN.hpp
  * \brief Declaration of artificial neural network interpolation class
  * \author E. Bunschoten
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -59,14 +59,6 @@ class CLookUp_ANN
 
     unsigned short number_of_variables;  /*!< Number of loaded ANNs. */
 
-    /*!
-   * \brief Skip to certain flag in file.
-   * \param[in] file_stream - input stream of file
-   * \param[in] flag - line to search for
-   * \return line in file.
-   */
-    std::string SkipToFlag(ifstream *file_stream, std::string flag); 
-
     /*!
     * \brief Load ANN architecture
     * \param[in] ANN - pointer to target NeuralNetwork class
@@ -101,7 +93,7 @@ class CLookUp_ANN
     * \brief Get number of loaded ANNs
     * \return number of loaded ANNs
     */
-    std::size_t GetNANNs() const {return NeuralNetworks.size();}
+    std::size_t GetNANNs() const { return NeuralNetworks.size(); }
 
     /*!
     * \brief Check if all output variables are present in the loaded ANNs
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
index 037bf8e7708..589afe0d7e9 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
@@ -2,7 +2,7 @@
  * \file CNeuralNetwork.hpp
  * \brief Declaration of the neural network class
  * \author E.C.Bunschoten
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -41,8 +41,8 @@ namespace MLPToolbox{
 class CNeuralNetwork
 {
 private:
-    std::vector<std::string> input_names,   // MLP input variable names.
-                             output_names;  // MLP output variable names.
+    su2vector<std::string> input_names,   // MLP input variable names.
+                           output_names;  // MLP output variable names.
 
     unsigned long n_hidden_layers = 0;  // Number of hidden layers (layers between input and output layer).
 
@@ -61,20 +61,19 @@ class CNeuralNetwork
                                         // is skipped if current inputs are the same as the last inputs.
 
     su2double* ANN_outputs; // Pointer to network outputs
-    su2matrix<su2double> dOutputs_dInputs;
+    su2matrix<su2double> dOutputs_dInputs; // Network output derivatives w.r.t inputs
 
     /*--- Activation function types that are currently supported ---*/
     enum ENUM_ACTIVATION_FUNCTION {
         NONE=0,
         LINEAR=1,
         RELU=2,
-        SMOOTH_SLOPE=3,
-        ELU = 4,
-        GELU = 5,
-        SELU = 6,
-        SIGMOID = 7,
-        SWISH = 8,
-        TANH = 9
+        ELU = 3,
+        GELU = 4,
+        SELU = 5,
+        SIGMOID = 6,
+        SWISH = 7,
+        TANH = 8
     };
     ENUM_ACTIVATION_FUNCTION * activation_function_types;
 
@@ -167,8 +166,10 @@ class CNeuralNetwork
 
     /*!
     * \brief Evaluate the network.
+    * \param[in] inputs - Network input variable values.
+    * \param[in] compute_gradient - Compute the derivatives of the outputs wrt inputs.
     */
-    void predict(su2vector<su2double> &inputs);
+    void predict(su2vector<su2double> &inputs, bool compute_gradient=false);
 
     /*!
     * \brief Set the normalization factors for the input layer
@@ -193,13 +194,13 @@ class CNeuralNetwork
     * \brief Add an output variable name to the network.
     * \param[in] input - Input variable name.
     */
-    void PushOutputName(std::string input) { output_names.push_back(input); }
+    void SetOutputName(size_t iOutput, std::string input) { output_names[iOutput] = input; }
 
     /*!
     * \brief Add an input variable name to the network.
     * \param[in] output - Output variable name.
     */
-    void PushInputName(std::string input) { input_names.push_back(input); }
+    void SetInputName(size_t iInput, std::string input) { input_names[iInput] = input; }
    
     /*!
     * \brief Get network input variable name.
@@ -234,7 +235,14 @@ class CNeuralNetwork
     */
     su2double GetANN_Output(std::size_t iOutput) const { return ANN_outputs[iOutput]; }
 
-    su2double GetOutput_Input_Derivative(std::size_t iOutput, std::size_t iInput) const { return dOutputs_dInputs[iOutput][iInput]; }
+    /*!
+    * \brief Get network output derivative w.r.t specific input.
+    * \param[in] iOutput - output variable index.
+    * \param[in] iInput - input variable index.
+    * \returns Output derivative w.r.t input.
+    */
+    su2double GetANN_Output_Input_Derivative(std::size_t iOutput, std::size_t iInput) const { return dOutputs_dInputs[iOutput][iInput]; }
+
     /*!
     * \brief Set the activation function array size.
     * \param[in] n_layers - network layer count.
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
index 1122e343309..1f131c96dab 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
@@ -2,7 +2,7 @@
  * \file CNeuron.hpp
  * \brief Declaration of artificial neural network perceptron class
  * \author E. Bunschoten
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -50,7 +50,7 @@ class CNeuron
     * \brief Set neuron identification number
     * \param[in] input - Identification number
     */
-    void setNumber(unsigned long input){ i_neuron = input; }
+    void setNumber(unsigned long input) { i_neuron = input; }
 
     /*!
     * \brief Get neuron identification number
@@ -62,7 +62,7 @@ class CNeuron
     * \brief Set neuron output value
     * \param[in] input - activation function output value
     */
-    void setOutput(su2double input){ output = input; }
+    void setOutput(su2double input) { output = input; }
 
     /*!
     * \brief Get neuron output value
@@ -74,7 +74,7 @@ class CNeuron
     * \brief Set neuron input value
     * \param[in] input - activation function input value
     */
-    void setInput(su2double x){ input = x; }
+    void setInput(su2double x) { input = x; }
 
     /*!
     * \brief Get neuron input value
@@ -86,7 +86,7 @@ class CNeuron
     * \brief Set neuron bias
     * \param[in] input - bias value
     */
-    void setBias(su2double input){ bias = input; }
+    void setBias(su2double input) { bias = input; }
 
     /*!
     * \brief Get neuron bias value
@@ -94,12 +94,17 @@ class CNeuron
     */
     su2double getBias() const { return bias; }
 
+    /*!
+    * \brief Size the derivative of the neuron output wrt MLP inputs.
+    * \param[in] nInputs - Number of MLP inputs.
+    */
     void sizeGradient(std::size_t nInputs) { doutput_dinputs.resize(nInputs); }
+    
     /*!
     * \brief Set neuron output gradient with respect to its input value
     * \param[in] input - Derivative of activation function with respect to input
     */
-    void setGradient(std::size_t iInput, su2double input){ doutput_dinputs[iInput] = input; }
+    void setGradient(std::size_t iInput, su2double input) { doutput_dinputs[iInput] = input; }
 
     /*!
     * \brief Get neuron output gradient with respect to input value
diff --git a/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
index a06509dfb85..5a0291dbf82 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
@@ -2,7 +2,7 @@
  * \file CReadNeuralNetwork.hpp
  * \brief Declaration of MLP input file reader class
  * \author E. Bunschoten
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -32,46 +32,124 @@
 #include <cstdlib>
 #include <vector>
 #include "../../CConfig.hpp"
-
+#include "../../containers/CFileReaderLUT.hpp"
 namespace MLPToolbox{
 
 class CReadNeuralNetwork {
     private:
-    std::vector<std::string> input_names,   // Network input variable names.
-                             output_names;  // Network output variable names.
+    su2vector<std::string> input_names,   /*!< Input variable names. */
+                           output_names;  /*!< Output variable names. */
 
-    std::string filename;       // Network input filename.
+    std::string filename;       /*!< MLP input filename. */
 
-    unsigned long n_layers;     // Number of layers in the network.
+    unsigned long n_layers;     /*!< Network total layer count. */
     
-    std::vector<unsigned long> n_neurons;
-    std::vector<std::vector<std::vector<su2double>>> weights;
-    std::vector<std::vector<su2double>> biases;
-    std::vector<std::string> activation_functions;
+    su2vector<unsigned long> n_neurons;  /*!<  Neuron count per layer. */
+
+    su2vector<su2activematrix> weights_mat; /*!< Network synapse weights. */
+
+    su2vector<su2vector<su2double>> biases_mat; /*!< Bias values per neuron. */
+
+    su2vector<std::string> activation_functions;    /*!< Activation function per layer. */
 
-    std::vector<std::pair<su2double, su2double>> input_norm;
-    std::vector<std::pair<su2double, su2double>> output_norm;
+    su2vector<std::pair<su2double, su2double>> input_norm,  /*!< Input variable normalization values (min, max). */
+                                               output_norm; /*!< Output variable normalization values (min, max). */
     public:
 
+    /*!
+    * \brief CReadNeuralNetwork class constructor
+    * \param[in] filename_in - .mlp input file name containing network information.
+    */
     CReadNeuralNetwork(std::string filename_in);
+
+    /*!
+    * \brief Read input file and store necessary information
+    */
     void ReadMLPFile();
 
+    /*!
+    * \brief Go to a specific line in file.
+    * \param[in] file_stream - input file stream.
+    * \param[in] flag - line to be skipped to.
+    * \returns flag line
+    */
     std::string SkipToFlag(std::ifstream *file_stream, std::string flag);
     
-    unsigned long GetNInputs(){return n_neurons.at(0);}
-    unsigned long GetNOutputs(){return n_neurons.at(n_layers - 1);}
-
-    unsigned long GetNlayers(){return n_layers;}
-    unsigned long GetNneurons(std::size_t iLayer){return n_neurons.at(iLayer);}
-    su2double GetWeight(std::size_t iLayer, std::size_t iNeuron, std::size_t jNeuron){return weights.at(iLayer).at(iNeuron).at(jNeuron);}
-    su2double GetBias(std::size_t iLayer, std::size_t iNeuron){return biases.at(iLayer).at(iNeuron);}
-    std::pair<su2double, su2double> GetInputNorm(std::size_t iInput){return input_norm.at(iInput);}
-    std::pair<su2double, su2double> GetOutputNorm(std::size_t iOutput){return output_norm.at(iOutput);}
-    std::string GetActivationFunction(std::size_t iLayer){return activation_functions.at(iLayer);}
-
-    std::string GetInputName(std::size_t iInput){return input_names.at(iInput);}
-    std::string GetOutputName(std::size_t iOutput){return output_names.at(iOutput);}
-    
-    ~CReadNeuralNetwork(){};
+    /*!
+    * \brief Get number of read input variables.
+    * \returns Number of neurons in the input layer.
+    */
+    unsigned long GetNInputs() const { return n_neurons[0]; }
+
+    /*!
+    * \brief Get number of read output variables.
+    * \returns Number of neurons in the output layer.
+    */
+    unsigned long GetNOutputs() const { return n_neurons[n_layers - 1]; }
+
+    /*!
+    * \brief Get total number of layers in the network.
+    * \returns Total layer count.
+    */
+    unsigned long GetNlayers() const { return n_layers; }
+
+    /*!
+    * \brief Get neuron count of a specific layer.
+    * \param[in] iLayer - Total layer index.
+    * \returns Number of neurons in the layer.
+    */
+    unsigned long GetNneurons(std::size_t iLayer) const { return n_neurons[iLayer]; }
+
+    /*!
+    * \brief Get synapse weight between two neurons in subsequent layers.
+    * \param[in] iLayer - Total layer index.
+    * \param[in] iNeuron - Neuron index in layer with index iLayer.
+    * \param[in] jNeuron - Neuron index in subsequent layer.
+    * \returns Weight value
+    */
+    su2double GetWeight(std::size_t iLayer, std::size_t iNeuron, std::size_t jNeuron) const { return weights_mat[iLayer][iNeuron][jNeuron]; }
+
+    /*!
+    * \brief Get bias value of specific neuron.
+    * \param[in] iLayer - Total layer index.
+    * \param[in] iNeuron - Neuron index.
+    * \returns Bias value
+    */
+    su2double GetBias(std::size_t iLayer, std::size_t iNeuron) const { return biases_mat[iLayer][iNeuron]; }
+
+    /*!
+    * \brief Get input variable normalization values.
+    * \param[in] iInput - Input variable index.
+    * \returns Input normalization values (min first, max second)
+    */
+    std::pair<su2double, su2double> GetInputNorm(std::size_t iInput) const { return input_norm[iInput]; }
+
+    /*!
+    * \brief Get output variable normalization values.
+    * \param[in] iOutput - Input variable index.
+    * \returns Output normalization values (min first, max second)
+    */
+    std::pair<su2double, su2double> GetOutputNorm(std::size_t iOutput) const { return output_norm[iOutput]; }
+
+    /*!
+    * \brief Get layer activation function type.
+    * \param[in] iLayer - Total layer index.
+    * \returns Layer activation function type.
+    */
+    std::string GetActivationFunction(std::size_t iLayer) const { return activation_functions[iLayer]; }
+
+    /*!
+    * \brief Get input variable name.
+    * \param[in] iInput - Input variable index.
+    * \returns Input variable name.
+    */
+    std::string GetInputName(std::size_t iInput) const { return input_names[iInput]; }
+
+    /*!
+    * \brief Get output variable name.
+    * \param[in] iOutput - Output variable index.
+    * \returns Output variable name.
+    */
+    std::string GetOutputName(std::size_t iOutput) const { return output_names[iOutput]; }
 };
 }
diff --git a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
index 42627195ab0..3eb37f7cb07 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
@@ -3,7 +3,7 @@
  * \brief Implementation of the input-output mapping class for the 
  *      use of multi-layer perceptrons in SU2
  * \author E. Bunschoten
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp b/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp
index b53a397fbd5..db5ab9f5e47 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp
@@ -3,7 +3,7 @@
  * \brief Implementation of the Layer class to be used in the NeuralNetwork
  *      class
  * \author E. Bunschoten
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
index 3806aed5e03..c596224d808 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
@@ -3,7 +3,7 @@
  * \brief Implementation of the multi-layer perceptron class to be 
  *      used for look-up operations.
  * \author E.C.Bunschoten
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -144,14 +144,14 @@ void MLPToolbox::CLookUp_ANN::GenerateANN(CNeuralNetwork * ANN, string fileName)
     ANN->defineInputLayer(Reader.GetNInputs());
     ANN->sizeInputs(Reader.GetNInputs());
     for(auto iInput=0u; iInput<Reader.GetNInputs(); iInput++){
-        ANN->PushInputName(Reader.GetInputName(iInput));
+        ANN->SetInputName(iInput, Reader.GetInputName(iInput));
     }
     for(auto iLayer=1u; iLayer<Reader.GetNlayers()-1; iLayer++){
         ANN->push_hidden_layer(Reader.GetNneurons(iLayer));
     }
     ANN->defineOutputLayer(Reader.GetNOutputs());
     for(auto iOutput=0u; iOutput<Reader.GetNOutputs(); iOutput++){
-        ANN->PushOutputName(Reader.GetOutputName(iOutput));
+        ANN->SetOutputName(iOutput, Reader.GetOutputName(iOutput));
     }
 
     /* Size weights of each layer */
diff --git a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
index 28b2c745552..a8da9b9e840 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
@@ -3,7 +3,7 @@
  * \brief Implementation of the NeuralNetwork class to be used
  *      for evaluation of multi-layer perceptrons.
  * \author E.C.Bunschoten
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -32,17 +32,17 @@
 using namespace std;
 
 
-void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
+void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs, bool compute_gradient){
     /*--- Evaluate MLP for given inputs ---*/
 
     su2double y, dy_dx;           // Activation function output.
     bool same_point = true;
-    bool compute_gradient = false; // TODO: get this from function inputs
     /* Normalize input and check if inputs are the same w.r.t last evaluation */
     for(auto iNeuron=0u; iNeuron<inputLayer->getNNeurons(); iNeuron++){
         su2double x_norm = (inputs[iNeuron] - input_norm[iNeuron].first)/(input_norm[iNeuron].second - input_norm[iNeuron].first);
         if(abs(x_norm - inputLayer->getOutput(iNeuron)) > 0) same_point = false;
         inputLayer->setOutput(iNeuron, x_norm);
+
         if(compute_gradient) inputLayer->setdYdX(iNeuron, iNeuron, 1 / (input_norm[iNeuron].second - input_norm[iNeuron].first));
     }
     /* Skip evaluation process if current point is the same as during the previous evaluation */
@@ -69,17 +69,6 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs){
             /* Compute and store neuron output based on activation function */
             switch (activation_function_types[iLayer])
                 {
-                case ENUM_ACTIVATION_FUNCTION::SMOOTH_SLOPE:
-                    for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
-                        x = total_layers[iLayer]->getInput(iNeuron);
-                        if(x > 0){
-                            y = x;
-                        }else{
-                            y = tanh(x);
-                        }
-                        total_layers[iLayer]->setOutput(iNeuron, y);
-                    }
-                    break;
                 case ENUM_ACTIVATION_FUNCTION::ELU:
                     for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
                         x = total_layers[iLayer]->getInput(iNeuron);
@@ -241,12 +230,14 @@ void MLPToolbox::CNeuralNetwork::defineInputLayer(unsigned long n_neurons){
     /* Mark layer as input layer */
     inputLayer->setInput(true);
     input_norm.resize(n_neurons);
+    input_names.resize(n_neurons);
 }
 
 void MLPToolbox::CNeuralNetwork::defineOutputLayer(unsigned long n_neurons){
     /*--- Define the output layer of the network ---*/
     outputLayer = new CLayer(n_neurons);
     output_norm.resize(n_neurons);
+    output_names.resize(n_neurons);
 }
 
 void MLPToolbox::CNeuralNetwork::push_hidden_layer(unsigned long n_neurons){
@@ -299,10 +290,6 @@ void MLPToolbox::CNeuralNetwork::setActivationFunction(unsigned long i_layer, st
         activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::RELU;
         return;
     }
-    if((input.compare("smooth_slope") == 0)){
-        activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::SMOOTH_SLOPE;
-        return;
-    }
     if((input.compare("elu") == 0)){
         activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::ELU;
         return;
diff --git a/Common/src/toolboxes/multilayer_perceptron/CNeuron.cpp b/Common/src/toolboxes/multilayer_perceptron/CNeuron.cpp
index 3d00506c41e..6c1446ea6e3 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CNeuron.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CNeuron.cpp
@@ -3,7 +3,7 @@
  * \brief Implementation of the neuron class to be used within the 
  *      Layer class as a part of the NeuralNetwork class.
  * \author E.C.Bunschoten
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
index 271cb11a6af..c97b9173c38 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
@@ -3,7 +3,7 @@
  * \brief Implementation of the reader class to read .mlp input files
  *      used to set up multi-layer perceptrons.
  * \author E.C.Bunschoten
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -26,9 +26,10 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 #include "../../../include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp"
+#include "../../../include/containers/CFileReaderLUT.hpp"
 using namespace std;
 
-MLPToolbox::CReadNeuralNetwork::CReadNeuralNetwork(string filename_in){
+MLPToolbox::CReadNeuralNetwork::CReadNeuralNetwork(string filename_in) {
     filename = filename_in;
 }
 
@@ -57,8 +58,8 @@ void MLPToolbox::CReadNeuralNetwork::ReadMLPFile(){
         getline(file_stream, line);
         n_layers = stoul(line);
         n_neurons.resize(n_layers);
-        biases.resize(n_layers);
-        weights.resize(n_layers-1);
+        biases_mat.resize(n_layers);
+        weights_mat.resize(n_layers - 1);
         activation_functions.resize(n_layers);
 
         found_layercount = true;
@@ -75,14 +76,11 @@ void MLPToolbox::CReadNeuralNetwork::ReadMLPFile(){
         for(auto iLayer=0u; iLayer<n_layers; iLayer++){
           getline(file_stream, line);
           n_neurons[iLayer] = stoul(line);
-          biases[iLayer].resize(n_neurons[iLayer]);
+          biases_mat[iLayer].resize(n_neurons[iLayer]);
         }
         /* Loop over spaces between layers and size the weight matrices accordingly */
         for(auto iLayer=0u; iLayer<n_layers-1; iLayer++){
-          weights[iLayer].resize(n_neurons[iLayer]);
-          for(size_t iNeuron=0; iNeuron<n_neurons[iLayer]; iNeuron++){
-            weights[iLayer][iNeuron].resize(n_neurons[iLayer+1]);
-          }
+          weights_mat[iLayer].resize(n_neurons[iLayer], n_neurons[iLayer + 1]);
         }
         /* Size input and output normalization and set default values */
         input_norm.resize(n_neurons[0]);
@@ -110,14 +108,11 @@ void MLPToolbox::CReadNeuralNetwork::ReadMLPFile(){
       /* Read MLP input variable names */
       if(line.compare("[input names]") == 0){
         found_input_names = true;
-        getline(file_stream, line);
-        while(line.compare("") != 0){
-          input_names.push_back(line);
+        input_names.resize(n_neurons[0]);
+        for(auto iInput=0u; iInput < n_neurons[0]; iInput++) {
           getline(file_stream, line);
-        }
-
-        if(input_names.size() != n_neurons[0]){
-          SU2_MPI::Error("Number of input variable names inconsistent with number of MLP inputs", CURRENT_FUNCTION);
+          input_names[iInput] = line;
+          
         }
       }
 
@@ -139,10 +134,11 @@ void MLPToolbox::CReadNeuralNetwork::ReadMLPFile(){
       /* Read MLP output variable names */
       if(line.compare("[output names]") == 0){
         found_output_names = true;
-        getline(file_stream, line);
-        while(line.compare("") != 0){
-          output_names.push_back(line);
+        auto n_outputs = n_neurons[n_neurons.size() - 1];
+        output_names.resize(n_outputs);
+        for(auto iOutput=0u; iOutput<n_outputs; iOutput++){
           getline(file_stream, line);
+          output_names[iOutput] = line;
         }
 
         if(output_names.size() != (n_neurons[n_neurons.size()-1])){
@@ -187,7 +183,7 @@ void MLPToolbox::CReadNeuralNetwork::ReadMLPFile(){
         istringstream weight_stream(line);
         for(auto jNeuron=0u; jNeuron<n_neurons[iLayer+1]; jNeuron++){
           weight_stream >> word;
-          weights[iLayer][iNeuron][jNeuron] = stold(word);
+          weights_mat[iLayer][iNeuron][jNeuron] = stold(word);
         }
       }
       getline(file_stream, line);
@@ -200,7 +196,7 @@ void MLPToolbox::CReadNeuralNetwork::ReadMLPFile(){
       istringstream bias_stream(line);
       for(auto iNeuron=0u; iNeuron<n_neurons[iLayer]; iNeuron++){
         bias_stream >> word;
-        biases[iLayer][iNeuron] = stold(word);
+        biases_mat[iLayer][iNeuron] = stold(word);
       }
     }
 
diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index fcdc440252d..81b03586d8f 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -3,7 +3,7 @@
  * \brief Defines a template fluid model class using multilayer perceptrons
  *  for theromodynamic state definition
  * \author E.Bunschoten
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 1ed94127899..475550de39c 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -2,7 +2,7 @@
  * \file CDataDrivenFluid.cpp
  * \brief Source of the data-driven fluid model class
  * \author E.Bunschoten M.Mayer A.Capiello
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
index e231623b84f..f4669364e78 100644
--- a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
+++ b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
@@ -2,7 +2,7 @@
  * \file CLookUp_ANN_tests.cpp
  * \brief Unit tests for NdFlattener template classes.
  * \author M. Aehle
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *

From 9ad958c81af77eb05cdf87c09aac4155f70ec6da Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Thu, 22 Dec 2022 10:54:46 -0800
Subject: [PATCH 091/656] Update pysu2 function names in FSIInterface.py

---
 SU2_PY/FSI_tools/FSIInterface.py | 34 ++++++++++++++++++++------------
 1 file changed, 21 insertions(+), 13 deletions(-)

diff --git a/SU2_PY/FSI_tools/FSIInterface.py b/SU2_PY/FSI_tools/FSIInterface.py
index e4e89dce7ce..616628162a8 100644
--- a/SU2_PY/FSI_tools/FSIInterface.py
+++ b/SU2_PY/FSI_tools/FSIInterface.py
@@ -227,15 +227,15 @@ def connect(self, FSI_config, FluidSolver, SolidSolver):
         if FluidSolver is not None:
             print('Fluid solver is initialized on process {}'.format(myid))
             self.haveFluidSolver = True
-            allMovingMarkersTags = FluidSolver.GetAllDeformMeshMarkersTag()
-            allMarkersID = FluidSolver.GetAllBoundaryMarkers()
+            allMovingMarkersTags = FluidSolver.GetDeformableMarkerTags()
+            allMarkersID = FluidSolver.GetMarkerTags()
             if not allMovingMarkersTags:
                 raise Exception('No interface for FSI was defined.')
             else:
                 if allMovingMarkersTags[0] in allMarkersID.keys():
                     self.fluidInterfaceIdentifier = allMarkersID[allMovingMarkersTags[0]]
             if self.fluidInterfaceIdentifier is not None:
-                self.nLocalFluidInterfaceNodes = FluidSolver.GetNumberVertices(self.fluidInterfaceIdentifier)
+                self.nLocalFluidInterfaceNodes = FluidSolver.GetNumberMarkerVertices(self.fluidInterfaceIdentifier)
             if self.nLocalFluidInterfaceNodes != 0:
               self.haveFluidInterface = True
               print('Number of interface fluid nodes (halo nodes included) on proccess {} : {}'.format(myid,self.nLocalFluidInterfaceNodes))
@@ -300,8 +300,8 @@ def connect(self, FSI_config, FluidSolver, SolidSolver):
         # Calculate the number of halo nodes on each partition
         self.nLocalFluidInterfaceHaloNode = 0
         for iVertex in range(self.nLocalFluidInterfaceNodes):
-            if FluidSolver.IsAHaloNode(self.fluidInterfaceIdentifier, iVertex):
-              GlobalIndex = FluidSolver.GetVertexGlobalIndex(self.fluidInterfaceIdentifier, iVertex)
+            if not FluidSolver.GetMarkerDomain(self.fluidInterfaceIdentifier, iVertex):
+              GlobalIndex = FluidSolver.GetMarkerVertexIDs(self.fluidInterfaceIdentifier, iVertex)
               self.FluidHaloNodeList[GlobalIndex] = iVertex
               self.nLocalFluidInterfaceHaloNode += 1
         # Calculate the number of physical (= not halo) nodes on each partition
@@ -565,8 +565,12 @@ def interfaceMapping(self,FluidSolver, SolidSolver, FSI_config):
             # Note that the fluid solver is separated in more processors outside the python script
             # thus when, from a core, we request for the vertices on the interface, we only obtain
             # those in that core
-            GlobalIndex = FluidSolver.GetVertexGlobalIndex(self.fluidInterfaceIdentifier, iVertex)
-            posx, posy, posz = FluidSolver.GetInitialMeshCoord(self.fluidInterfaceIdentifier, iVertex)
+            GlobalIndex = FluidSolver.GetMarkerVertexIDs(self.fluidInterfaceIdentifier, iVertex)
+            if self.nDim == 2:
+                posx, posy = FluidSolver.GetMarkerInitialCoordinates(self.fluidInterfaceIdentifier, iVertex)
+                posz = 0
+            else:
+                posx, posy, posz = FluidSolver.GetMarkerInitialCoordinates(self.fluidInterfaceIdentifier, iVertex)
             if GlobalIndex not in self.FluidHaloNodeList[myid].keys():
               fluidIndexing_temp[GlobalIndex] = self.__getGlobalIndex('fluid', myid, localIndex)
               self.localFluidInterface_array_X_init[localIndex] = posx
@@ -1456,7 +1460,7 @@ def getFluidInterfaceNodalForce(self, FSI_config, FluidSolver):
 
         # --- Get the fluid interface loads from the fluid solver and directly fill the corresponding PETSc vector ---
         for iVertex in range(self.nLocalFluidInterfaceNodes):
-            GlobalIndex = FluidSolver.GetVertexGlobalIndex(self.fluidInterfaceIdentifier, iVertex)
+            GlobalIndex = FluidSolver.GetMarkerVertexIDs(self.fluidInterfaceIdentifier, iVertex)
             if GlobalIndex not in self.FluidHaloNodeList[myid].keys():
               loadX, loadY, loadZ = FluidSolver.GetFlowLoad(self.fluidInterfaceIdentifier, iVertex)
               iGlobalVertex = self.__getGlobalIndex('fluid', myid, localIndex)
@@ -1486,15 +1490,15 @@ def setFluidInterfaceVarCoord(self, FluidSolver):
         # --- Send the new fluid interface position to the fluid solver (on each partition, halo nodes included) ---
         localIndex = 0
         for iVertex in range(self.nLocalFluidInterfaceNodes):
-            GlobalIndex = FluidSolver.GetVertexGlobalIndex(self.fluidInterfaceIdentifier, iVertex)
+            GlobalIndex = FluidSolver.GetMarkerVertexIDs(self.fluidInterfaceIdentifier, iVertex)
             if GlobalIndex in self.FluidHaloNodeList[myid].keys():
               DispX, DispY, DispZ = self.haloNodesDisplacements[GlobalIndex]
-              FluidSolver.SetMeshDisplacement(self.fluidInterfaceIdentifier, int(iVertex), DispX, DispY, DispZ)
+              FluidSolver.SetMarkerDisplacements(self.fluidInterfaceIdentifier, int(iVertex), np.array([DispX, DispY, DispZ]))
             else:
               DispX = self.localFluidInterface_array_DispX[localIndex]
               DispY = self.localFluidInterface_array_DispY[localIndex]
               DispZ = self.localFluidInterface_array_DispZ[localIndex]
-              FluidSolver.SetMeshDisplacement(self.fluidInterfaceIdentifier, int(iVertex), DispX, DispY, DispZ)
+              FluidSolver.SetMarkerDisplacements(self.fluidInterfaceIdentifier, int(iVertex), np.array([DispX, DispY, DispZ]))
               localIndex += 1
 
 
@@ -2142,8 +2146,12 @@ def MapModes(self, FSI_config, FluidSolver, SolidSolver):
 
       nodeNormals = {}
       for iVertex in range(self.nLocalFluidInterfaceNodes):
-        nx, ny, nz = FluidSolver.GetVertexNormal(self.fluidInterfaceIdentifier, iVertex, False)
-        GlobalIndex = FluidSolver.GetVertexGlobalIndex(self.fluidInterfaceIdentifier, iVertex)
+        if self.nDim == 2:
+            nx, ny = FluidSolver.GetMarkerVertexNormals(self.fluidInterfaceIdentifier, iVertex, False)
+            nz = 0
+        else:
+            nx, ny, nz = FluidSolver.GetMarkerVertexNormals(self.fluidInterfaceIdentifier, iVertex, False)
+        GlobalIndex = FluidSolver.GetMarkerVertexIDs(self.fluidInterfaceIdentifier, iVertex)
         nodeNormals[GlobalIndex] = [nx, ny, nz]
 
       nodeNormals = self.comm.gather(nodeNormals, root=self.rootProcess)

From 3b46ee098bf7dea6eee8eba51a475435d0cdb2d2 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Thu, 22 Dec 2022 16:22:06 -0800
Subject: [PATCH 092/656] Modify regression workflow

---
 .github/workflows/regression.yml | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 8e2d4414353..37c3dc637f9 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:220614-1237
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c feature_FFD -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:220614-1237
         with:

From a4450bbbd1f0170267476e4af7cc762a2f99d09d Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Thu, 22 Dec 2022 18:23:41 -0800
Subject: [PATCH 093/656]  Update pysu2 function names in translating NACA0012
 test case

---
 TestCases/py_wrapper/translating_NACA0012/run_su2.py | 8 ++++----
 1 file changed, 4 insertions(+), 4 deletions(-)

diff --git a/TestCases/py_wrapper/translating_NACA0012/run_su2.py b/TestCases/py_wrapper/translating_NACA0012/run_su2.py
index 731c109184d..a4abfee0b6e 100644
--- a/TestCases/py_wrapper/translating_NACA0012/run_su2.py
+++ b/TestCases/py_wrapper/translating_NACA0012/run_su2.py
@@ -35,8 +35,8 @@ def run_solver(self):
         self.comm.barrier()
 
     def save_forces(self):
-        solver_all_moving_markers = np.array(self.FluidSolver.GetAllDeformMeshMarkersTag())
-        solver_marker_ids = self.FluidSolver.GetAllBoundaryMarkers()
+        solver_all_moving_markers = np.array(self.FluidSolver.GetDeformableMarkerTags())
+        solver_marker_ids = self.FluidSolver.GetMarkerTags()
         # The surface marker and the partitioning of the solver usually don't agree.
         # Thus, it is necessary to figure out if the partition of the current mpi process has
         # a node that belongs to a moving surface marker.
@@ -46,10 +46,10 @@ def save_forces(self):
 
         for marker in solver_all_moving_markers[has_moving_marker]:
             solver_marker_id = solver_marker_ids[marker]
-            n_vertices = self.FluidSolver.GetNumberVertices(solver_marker_id)
+            n_vertices = self.FluidSolver.GetNumberMarkerVertices(solver_marker_id)
             for i_vertex in range(n_vertices):
                 fxyz = self.FluidSolver.GetFlowLoad(solver_marker_id, i_vertex)
-                GlobalIndex = self.FluidSolver.GetVertexGlobalIndex(solver_marker_id, i_vertex)
+                GlobalIndex = self.FluidSolver.GetMarkerVertexIDs(solver_marker_id, i_vertex)
                 f.write('{}, {:.2f}, {:.2f}, {:.2f}\n'.format(GlobalIndex, fxyz[0], fxyz[1], fxyz[2]))
         f.close()
 

From 57a7faf38cb7306f262aeb66f9a10fbfc6d54ad8 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Thu, 22 Dec 2022 18:28:21 -0800
Subject: [PATCH 094/656] Fix continuous adjoint solver error handling in
 CDiscAdjDeformationDriver

---
 SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index f483eb0dabf..9e55a74c11a 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -120,8 +120,8 @@ void CDiscAdjDeformationDriver::Input_Preprocessing() {
 
     config_container[iZone]->SetMPICommunicator(SU2_MPI::GetComm());
 
-    if (!config_container[iZone]->GetDiscrete_Adjoint()) {
-      SU2_MPI::Error("The discrete adjoint solver was not specified in the configuration file.", CURRENT_FUNCTION);
+    if (!config_container[iZone]->GetDiscrete_Adjoint() && !config_container[iZone]->GetContinuous_Adjoint()) {
+      SU2_MPI::Error("An adjoint solver (discrete or continuous) was not specified in the configuration file.", CURRENT_FUNCTION);
     }
   }
 

From 5c1ec48ef8f712b67afe88faa8011ace8282cfc6 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Wed, 28 Dec 2022 14:56:34 -0800
Subject: [PATCH 095/656] Move CDriverBase from Common to SU2_CFD

---
 Common/src/drivers/meson.build                        | 1 -
 SU2_CFD/include/drivers/CDriver.hpp                   | 2 +-
 {Common => SU2_CFD}/include/drivers/CDriverBase.hpp   | 8 ++++----
 {Common => SU2_CFD}/src/drivers/CDriverBase.cpp       | 4 ++--
 SU2_CFD/src/meson.build                               | 3 ++-
 SU2_DEF/include/drivers/CDeformationDriver.hpp        | 2 +-
 SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp | 2 +-
 SU2_PY/pySU2/pySU2.i                                  | 9 ++++-----
 SU2_PY/pySU2/pySU2ad.i                                | 9 ++++-----
 9 files changed, 19 insertions(+), 21 deletions(-)
 delete mode 100644 Common/src/drivers/meson.build
 rename {Common => SU2_CFD}/include/drivers/CDriverBase.hpp (99%)
 rename {Common => SU2_CFD}/src/drivers/CDriverBase.cpp (99%)

diff --git a/Common/src/drivers/meson.build b/Common/src/drivers/meson.build
deleted file mode 100644
index bcee2ba35cb..00000000000
--- a/Common/src/drivers/meson.build
+++ /dev/null
@@ -1 +0,0 @@
-common_src += files(['CDriverBase.cpp'])
diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index 1d4e6f913b8..c6fbde07c5a 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -28,12 +28,12 @@
 
 #pragma once
 
-#include "../../../Common/include/drivers/CDriverBase.hpp"
 #include "../../../Common/include/geometry/CGeometry.hpp"
 #include "../../../Common/include/parallelization/mpi_structure.hpp"
 #include "../integration/CIntegration.hpp"
 #include "../interfaces/CInterface.hpp"
 #include "../solvers/CSolver.hpp"
+#include "CDriverBase.hpp"
 
 using namespace std;
 
diff --git a/Common/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
similarity index 99%
rename from Common/include/drivers/CDriverBase.hpp
rename to SU2_CFD/include/drivers/CDriverBase.hpp
index e3acace3892..4eb8490bb73 100644
--- a/Common/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -27,10 +27,10 @@
 
 #pragma once
 
-#include "../../../SU2_CFD/include/numerics/CNumerics.hpp"
-#include "../../../SU2_CFD/include/output/COutput.hpp"
-#include "../../../SU2_CFD/include/solvers/CSolver.hpp"
-#include "../CConfig.hpp"
+#include "../../../Common/include/CConfig.hpp"
+#include "../numerics/CNumerics.hpp"
+#include "../output/COutput.hpp"
+#include "../solvers/CSolver.hpp"
 
 class CDriverBase {
  protected:
diff --git a/Common/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
similarity index 99%
rename from Common/src/drivers/CDriverBase.cpp
rename to SU2_CFD/src/drivers/CDriverBase.cpp
index 74dda47ce3b..dba80d8b8db 100644
--- a/Common/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -27,8 +27,8 @@
 
 #include "../../include/drivers/CDriverBase.hpp"
 
-#include "../../include/geometry/CPhysicalGeometry.hpp"
-#include "../../include/toolboxes/geometry_toolbox.hpp"
+#include "../../../Common/include/geometry/CPhysicalGeometry.hpp"
+#include "../../../Common/include/toolboxes/geometry_toolbox.hpp"
 
 using namespace std;
 
diff --git a/SU2_CFD/src/meson.build b/SU2_CFD/src/meson.build
index d7c7d156c41..53b2081c660 100644
--- a/SU2_CFD/src/meson.build
+++ b/SU2_CFD/src/meson.build
@@ -165,7 +165,8 @@ su2_cfd_src += files(['drivers/CDriver.cpp',
                       'drivers/CSinglezoneDriver.cpp',
                       'drivers/CDiscAdjMultizoneDriver.cpp',
                       'drivers/CDiscAdjSinglezoneDriver.cpp',
-                      'drivers/CDummyDriver.cpp'])
+                      'drivers/CDummyDriver.cpp',
+                      'drivers/CDriverBase.cpp'])
 
 su2_cfd_src += files(['integration/CIntegration.cpp',
                       'integration/CIntegrationFactory.cpp',
diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index bded29a1f0d..62954de5b73 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -31,11 +31,11 @@
 #include "../../../Common/include/CConfig.hpp"
 #undef ENABLE_MAPS
 
-#include "../../../Common/include/drivers/CDriverBase.hpp"
 #include "../../../Common/include/geometry/CGeometry.hpp"
 #include "../../../Common/include/grid_movement/CSurfaceMovement.hpp"
 #include "../../../Common/include/grid_movement/CVolumetricMovement.hpp"
 #include "../../../Common/include/parallelization/mpi_structure.hpp"
+#include "../../../SU2_CFD/include/drivers/CDriverBase.hpp"
 #include "../../../SU2_CFD/include/numerics/CNumerics.hpp"
 #include "../../../SU2_CFD/include/output/COutput.hpp"
 
diff --git a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
index 783e21c98dd..d5b42b958e5 100644
--- a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
@@ -31,12 +31,12 @@
 #include "../../../Common/include/CConfig.hpp"
 #undef ENABLE_MAPS
 
-#include "../../../Common/include/drivers/CDriverBase.hpp"
 #include "../../../Common/include/fem/fem_geometry_structure.hpp"
 #include "../../../Common/include/geometry/CGeometry.hpp"
 #include "../../../Common/include/grid_movement/CSurfaceMovement.hpp"
 #include "../../../Common/include/grid_movement/CVolumetricMovement.hpp"
 #include "../../../Common/include/parallelization/mpi_structure.hpp"
+#include "../../../SU2_CFD/include/drivers/CDriverBase.hpp"
 #include "../../../SU2_CFD/include/numerics/CGradSmoothing.hpp"
 #include "../../../SU2_CFD/include/output/CBaselineOutput.hpp"
 #include "../../../SU2_CFD/include/output/COutput.hpp"
diff --git a/SU2_PY/pySU2/pySU2.i b/SU2_PY/pySU2/pySU2.i
index 44a6c0c4f33..1d8c424cd28 100644
--- a/SU2_PY/pySU2/pySU2.i
+++ b/SU2_PY/pySU2/pySU2.i
@@ -37,12 +37,11 @@ directors="1",
 threads="1"
 ) pysu2
 %{
-
-#include "../../Common/include/drivers/CDriverBase.hpp"
+#include "../../SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CDriver.hpp"
-#include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
+#include "../../SU2_CFD/include/drivers/CDriverBase.hpp"
 #include "../../SU2_CFD/include/drivers/CMultizoneDriver.hpp"
-#include "../../SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp"
+#include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
 #include "../../SU2_DEF/include/drivers/CDeformationDriver.hpp"
 
 %}
@@ -93,8 +92,8 @@ const unsigned int MESH_1 = 1; /*!< \brief Definition of the finest grid level.
 const unsigned int ZONE_0 = 0; /*!< \brief Definition of the first grid domain. */
 const unsigned int ZONE_1 = 1; /*!< \brief Definition of the first grid domain. */
 
-%include "../../Common/include/drivers/CDriverBase.hpp"
 %include "../../SU2_CFD/include/drivers/CDriver.hpp"
+%include "../../SU2_CFD/include/drivers/CDriverBase.hpp"
 %include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CMultizoneDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp"
diff --git a/SU2_PY/pySU2/pySU2ad.i b/SU2_PY/pySU2/pySU2ad.i
index b581fb86038..7b347f5cbe1 100644
--- a/SU2_PY/pySU2/pySU2ad.i
+++ b/SU2_PY/pySU2/pySU2ad.i
@@ -37,12 +37,11 @@ directors="1",
 threads="1"
 ) pysu2ad
 %{
-
-#include "../../Common/include/drivers/CDriverBase.hpp"
+#include "../../SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CDriver.hpp"
-#include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
+#include "../../SU2_CFD/include/drivers/CDriverBase.hpp"
 #include "../../SU2_CFD/include/drivers/CMultizoneDriver.hpp"
-#include "../../SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp"
+#include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
 #include "../../SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp"
 
 %}
@@ -92,8 +91,8 @@ const unsigned int MESH_1 = 1; /*!< \brief Definition of the finest grid level.
 const unsigned int ZONE_0 = 0; /*!< \brief Definition of the first grid domain. */
 const unsigned int ZONE_1 = 1; /*!< \brief Definition of the first grid domain. */
 
-%include "../../Common/include/drivers/CDriverBase.hpp"
 %include "../../SU2_CFD/include/drivers/CDriver.hpp"
+%include "../../SU2_CFD/include/drivers/CDriverBase.hpp"
 %include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CMultizoneDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp"

From 50a2011969c742853b493b2fbe63846af6ecda07 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Wed, 28 Dec 2022 15:06:00 -0800
Subject: [PATCH 096/656] Remove 'drivers' subdirectory from meson build file
 in Common

---
 Common/src/meson.build | 1 -
 1 file changed, 1 deletion(-)

diff --git a/Common/src/meson.build b/Common/src/meson.build
index 332b61108bf..3d84e6ea17a 100644
--- a/Common/src/meson.build
+++ b/Common/src/meson.build
@@ -13,7 +13,6 @@ subdir('geometry/elements')
 subdir('geometry/dual_grid')
 subdir('geometry/primal_grid')
 subdir('geometry/meshreader')
-subdir('drivers')
 subdir('containers')
 subdir('interface_interpolation')
 subdir('fem')

From 3c8f5cd84eea3a870c6f3b0bf2b74fdbdfead498 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Wed, 28 Dec 2022 16:02:53 -0800
Subject: [PATCH 097/656] Remove pysu2 FFD functions from CDriverBase

---
 SU2_CFD/include/drivers/CDriverBase.hpp | 106 +---
 SU2_CFD/src/drivers/CDriver.cpp         |   4 -
 SU2_CFD/src/drivers/CDriverBase.cpp     | 636 ------------------------
 3 files changed, 6 insertions(+), 740 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index 4eb8490bb73..cec1a78c58a 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -127,91 +127,6 @@ class CDriverBase {
    */
   unsigned short GetNumberFFDBoxes() const;
 
-  /*!
-   * \brief Get the number of FFD box corner points.
-   * \param[in] iFFDBox - FFD box index.
-   * \return Number of FFD box corner points.
-   */
-  unsigned short GetNumberFFDBoxCornerPoints(unsigned short iFFDBox) const;
-
-  /*!
-   * \brief Get the number of FFD box control points.
-   * \param[in] iFFDBox - FFD box index.
-   * \return Number of FFD box control points.
-   */
-  unsigned short GetNumberFFDBoxControlPoints(unsigned short iFFDBox) const;
-
-  /*!
-   * \brief Get the number of FFD box surface points.
-   * \param[in] iFFDBox - FFD box index.
-   * \return Number of FFD box surface points.
-   */
-  unsigned long GetNumberFFDBoxSurfacePoints(unsigned short iFFDBox) const;
-
-  /*!
-   * \brief Get the FFD box marker IDs.
-   * \param[in] iFFDBox - FFD box index.
-   * \return FFD box marker IDs.
-   */
-  vector<unsigned short> GetFFDBoxMarkerIDs(unsigned short iFFDBox) const;
-
-  /*!
-   * \brief Get the FFD box vertex IDs.
-   * \param[in] iFFDBox - FFD box index.
-   * \return FFD box vertex IDs.
-   */
-  vector<unsigned long> GetFFDBoxVertexIDs(unsigned short iFFDBox) const;
-
-  /*!
-   * \brief Get the FFD box grid point IDs.
-   * \param[in] iFFDBox - FFD box index.
-   * \return FFD box grid point IDs.
-   */
-  vector<unsigned long> GetFFDBoxPointIDs(unsigned short iFFDBox) const;
-
-  /*!
-   * \brief Get the FFD box corner coordinates.
-   * \param[in] iFFDBox - FFD box index.
-   * \return FFD box corner coordinates.
-   */
-  vector<vector<passivedouble>> GetFFDBoxCornerCoordinates(unsigned short iFFDBox) const;
-
-  /*!
-   * \brief Get the FFD box control point coordinates.
-   * \param[in] iFFDBox - FFD box index.
-   * \return FFD box control point coordinates.
-   */
-  vector<vector<passivedouble>> GetFFDBoxControlPointCoordinates(unsigned short iFFDBox) const;
-
-  /*!
-   * \brief Get the FFD box control point coordinates.
-   * \param[in] iFFDBox - FFD box index.
-   * \param[in] iOrder - Local i-index of the control point.
-   * \param[in] jOrder - Local j-index of the control point.
-   * \param[in] kOrder - Local k-index of the control point.
-   * \return FFD box control point coordinates.
-   */
-  vector<passivedouble> GetFFDBoxControlPointCoordinates(unsigned short iFFDBox, unsigned int iOrder,
-                                                         unsigned int jOrder, unsigned int kOrder) const;
-
-  /*!
-   * \brief Get the FFD box surface coordinates.
-   * \param[in] iFFDBox - FFD box index.
-   * \param[in] parametric - Boolean to indicate if parametric coordinates should be returned.
-   * \return FFD box surface coordinates.
-   */
-  vector<vector<passivedouble>> GetFFDBoxSurfaceCoordinates(unsigned short iFFDBox, bool parametric = false) const;
-
-  /*!
-   * \brief Get the FFD box surface coordinates.
-   * \param[in] iFFDBox - FFD box index.
-   * \param[in] iPoint - FFD surface point index.
-   * \param[in] parametric - Boolean to indicate if parametric coordinates should be returned.
-   * \return FFD box surface coordinates.
-   */
-  vector<passivedouble> GetFFDBoxSurfaceCoordinates(unsigned short iFFDBox, unsigned long iPoint,
-                                                    bool parametric = false) const;
-
   /*!
    * \brief Get the number of markers in the mesh.
    * \return Number of markers.
@@ -583,7 +498,7 @@ class CDriverBase {
 
  protected:
   /*!
-   * \brief Initialize Containers
+   * \brief Initialize containers.
    */
   void SetContainers_Null();
 
@@ -604,18 +519,18 @@ class CDriverBase {
 
   /*!
    * \brief Definition and allocation of all solution classes.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver - Container vector with all the solutions.
    */
   void Solver_Preprocessing(CConfig* config, CGeometry** geometry, CSolver***& solver);
 
   /*!
    * \brief Definition and allocation of all solver classes.
-   * \param[in] numerics_container - Description of the numerical method (the way in which the equations are solved).
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] solver_container - Container vector with all the solutions.
    * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver - Container vector with all the solutions.
+   * \param[in] numerics - Description of the numerical method (the way in which the equations are solved).
    */
   void Numerics_Preprocessing(CConfig* config, CGeometry** geometry, CSolver*** solver, CNumerics****& numerics) const;
 
@@ -628,13 +543,4 @@ class CDriverBase {
    */
   void Output_Preprocessing(CConfig** config, CConfig* driver_config, COutput**& output_container,
                             COutput*& driver_output);
-
-  /*!
-   * \brief Read the free form deformation box information from the input mesh file.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] FFDBox - Definition of the FFD boxes of the problem.
-   * \param[in] val_mesh_filename - Name of the input mesh file.
-   */
-  void ReadFFDInfo(CGeometry* geometry, CConfig* config, CFreeFormDefBox** FFDBox, string val_mesh_filename);
 };
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index d7302267d35..c0a6c49f217 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -177,9 +177,6 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
     }
   }
 
-  /*--- Read free form deformation design variables data. --- */
-  ReadFFDInfo(geometry_container[ZONE_0][INST_0][MESH_0], config_container[ZONE_0], FFDBox[ZONE_0], config_container[ZONE_0]->GetMesh_FileName());
-
   /*--- Before we proceed with the zone loop we have to compute the wall distances.
      * This computation depends on all zones at once. ---*/
   if (rank == MASTER_NODE)
@@ -356,7 +353,6 @@ void CDriver::SetContainers_Null(){
   for (iZone = 0; iZone < nZone; iZone++) {
     interface_types[iZone] = new unsigned short[nZone];
     nInst[iZone] = 1;
-    FFDBox[iZone] = new CFreeFormDefBox*[MAX_NUMBER_FFD];
   }
 
   strcpy(runtime_file_name, "runtime.dat");
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index dba80d8b8db..4009c76fa26 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -79,198 +79,6 @@ unsigned short CDriverBase::GetNumberDesignVariables() const { return main_confi
 
 unsigned short CDriverBase::GetNumberFFDBoxes() const { return main_config->GetnFFDBox(); }
 
-unsigned short CDriverBase::GetNumberFFDBoxCornerPoints(unsigned short iFFDBox) const {
-  if (GetNumberFFDBoxes() == 0) {
-    SU2_MPI::Error("FFD Box definition not found in the mesh file.", CURRENT_FUNCTION);
-  }
-  if (iFFDBox >= GetNumberFFDBoxes()) {
-    SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
-  }
-
-  return FFDBox[ZONE_0][iFFDBox]->GetnCornerPoints();
-}
-
-unsigned short CDriverBase::GetNumberFFDBoxControlPoints(unsigned short iFFDBox) const {
-  if (GetNumberFFDBoxes() == 0) {
-    SU2_MPI::Error("FFD Box definition not found in the mesh file.", CURRENT_FUNCTION);
-  }
-  if (iFFDBox >= GetNumberFFDBoxes()) {
-    SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
-  }
-
-  return FFDBox[ZONE_0][iFFDBox]->GetnControlPoints();
-}
-
-unsigned long CDriverBase::GetNumberFFDBoxSurfacePoints(unsigned short iFFDBox) const {
-  if (GetNumberFFDBoxes() == 0) {
-    SU2_MPI::Error("FFD Box definition not found in the mesh file.", CURRENT_FUNCTION);
-  }
-  if (iFFDBox >= GetNumberFFDBoxes()) {
-    SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
-  }
-
-  return FFDBox[ZONE_0][iFFDBox]->GetnSurfacePoint();
-}
-
-vector<unsigned short> CDriverBase::GetFFDBoxMarkerIDs(unsigned short iFFDBox) const {
-  if (GetNumberFFDBoxes() == 0) {
-    SU2_MPI::Error("FFD Box definition not found in the mesh file.", CURRENT_FUNCTION);
-  }
-  if (iFFDBox >= GetNumberFFDBoxes()) {
-    SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
-  }
-
-  vector<unsigned short> values;
-
-  for (auto iPoint = 0ul; iPoint < GetNumberFFDBoxSurfacePoints(iFFDBox); iPoint++) {
-    values.push_back(FFDBox[ZONE_0][iFFDBox]->Get_MarkerIndex(iPoint));
-  }
-  return values;
-}
-
-vector<unsigned long> CDriverBase::GetFFDBoxVertexIDs(unsigned short iFFDBox) const {
-  if (GetNumberFFDBoxes() == 0) {
-    SU2_MPI::Error("FFD Box definition not found in the mesh file.", CURRENT_FUNCTION);
-  }
-  if (iFFDBox >= GetNumberFFDBoxes()) {
-    SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
-  }
-
-  vector<unsigned long> values;
-
-  for (auto iPoint = 0ul; iPoint < GetNumberFFDBoxSurfacePoints(iFFDBox); iPoint++) {
-    values.push_back(FFDBox[ZONE_0][iFFDBox]->Get_VertexIndex(iPoint));
-  }
-  return values;
-}
-
-vector<unsigned long> CDriverBase::GetFFDBoxPointIDs(unsigned short iFFDBox) const {
-  if (GetNumberFFDBoxes() == 0) {
-    SU2_MPI::Error("FFD Box definition not found in the mesh file.", CURRENT_FUNCTION);
-  }
-  if (iFFDBox >= GetNumberFFDBoxes()) {
-    SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
-  }
-
-  vector<unsigned long> values;
-
-  for (auto iPoint = 0ul; iPoint < GetNumberFFDBoxSurfacePoints(iFFDBox); iPoint++) {
-    values.push_back(FFDBox[ZONE_0][iFFDBox]->Get_PointIndex(iPoint));
-  }
-  return values;
-}
-
-vector<vector<passivedouble>> CDriverBase::GetFFDBoxCornerCoordinates(unsigned short iFFDBox) const {
-  if (GetNumberFFDBoxes() == 0) {
-    SU2_MPI::Error("FFD Box definition not found in the mesh file.", CURRENT_FUNCTION);
-  }
-  if (iFFDBox >= GetNumberFFDBoxes()) {
-    SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
-  }
-
-  vector<vector<passivedouble>> values;
-
-  for (auto iPoint = 0u; iPoint < GetNumberFFDBoxCornerPoints(iFFDBox); iPoint++) {
-    vector<passivedouble> coords;
-
-    const su2double* coord = FFDBox[ZONE_0][iFFDBox]->GetCoordCornerPoints(iPoint);
-
-    for (auto iDim = 0u; iDim < nDim; iDim++) {
-      coords.push_back(SU2_TYPE::GetValue(coord[iDim]));
-    }
-
-    values.push_back(coords);
-  }
-
-  return values;
-}
-
-vector<vector<passivedouble>> CDriverBase::GetFFDBoxControlPointCoordinates(unsigned short iFFDBox) const {
-  if (GetNumberFFDBoxes() == 0) {
-    SU2_MPI::Error("FFD Box definition not found in the mesh file.", CURRENT_FUNCTION);
-  }
-  if (iFFDBox >= GetNumberFFDBoxes()) {
-    SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
-  }
-
-  vector<vector<passivedouble>> values;
-
-  for (auto iOrder = 0u; iOrder < FFDBox[ZONE_0][iFFDBox]->GetlOrder(); iOrder++) {
-    for (auto jOrder = 0u; jOrder < FFDBox[ZONE_0][iFFDBox]->GetmOrder(); jOrder++) {
-      for (auto kOrder = 0u; kOrder < FFDBox[ZONE_0][iFFDBox]->GetnOrder(); kOrder++) {
-        values.push_back(GetFFDBoxControlPointCoordinates(iFFDBox, iOrder, jOrder, kOrder));
-      }
-    }
-  }
-
-  return values;
-}
-
-vector<passivedouble> CDriverBase::GetFFDBoxControlPointCoordinates(unsigned short iFFDBox, unsigned int iOrder,
-                                                                    unsigned int jOrder, unsigned int kOrder) const {
-  if (GetNumberFFDBoxes() == 0) {
-    SU2_MPI::Error("FFD Box definition not found in the mesh file.", CURRENT_FUNCTION);
-  }
-  if (iFFDBox >= GetNumberFFDBoxes()) {
-    SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
-  }
-
-  vector<passivedouble> values;
-
-  const su2double* coord = FFDBox[ZONE_0][iFFDBox]->GetCoordControlPoints(iOrder, jOrder, kOrder);
-
-  for (auto iDim = 0u; iDim < nDim; iDim++) {
-    values.push_back(SU2_TYPE::GetValue(coord[iDim]));
-  }
-
-  return values;
-}
-
-vector<vector<passivedouble>> CDriverBase::GetFFDBoxSurfaceCoordinates(unsigned short iFFDBox, bool parametric) const {
-  if (GetNumberFFDBoxes() == 0) {
-    SU2_MPI::Error("FFD Box definition not found in the mesh file.", CURRENT_FUNCTION);
-  }
-  if (iFFDBox >= GetNumberFFDBoxes()) {
-    SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
-  }
-
-  vector<vector<passivedouble>> values;
-
-  for (auto iPoint = 0ul; iPoint < GetNumberFFDBoxSurfacePoints(iFFDBox); iPoint++) {
-    values.push_back(GetFFDBoxSurfaceCoordinates(iFFDBox, iPoint, parametric));
-  }
-
-  return values;
-}
-
-vector<passivedouble> CDriverBase::GetFFDBoxSurfaceCoordinates(unsigned short iFFDBox, unsigned long iPoint,
-                                                               bool parametric) const {
-  if (GetNumberFFDBoxes() == 0) {
-    SU2_MPI::Error("FFD Box definition not found in the mesh file.", CURRENT_FUNCTION);
-  }
-  if (iFFDBox >= GetNumberFFDBoxes()) {
-    SU2_MPI::Error("FFD Box index exceeds size.", CURRENT_FUNCTION);
-  }
-  if (iPoint >= GetNumberFFDBoxSurfacePoints(iFFDBox)) {
-    SU2_MPI::Error("FFD Box vertex index exceeds mesh size.", CURRENT_FUNCTION);
-  }
-
-  vector<passivedouble> values;
-  const su2double* coord;
-
-  if (parametric) {
-    coord = FFDBox[ZONE_0][iFFDBox]->Get_ParametricCoord(iPoint);
-  } else {
-    coord = FFDBox[ZONE_0][iFFDBox]->Get_CartesianCoord(iPoint);
-  }
-
-  for (auto iDim = 0u; iDim < nDim; iDim++) {
-    values.push_back(SU2_TYPE::GetValue(coord[iDim]));
-  }
-
-  return values;
-}
-
 unsigned short CDriverBase::GetNumberMarkers() const { return main_config->GetnMarker_All(); }
 
 map<string, unsigned short> CDriverBase::GetMarkerIndices() const {
@@ -947,447 +755,3 @@ void CDriverBase::CommunicateMeshDisplacements(void) {
   solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->InitiateComms(main_geometry, main_config, MESH_DISPLACEMENTS);
   solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->CompleteComms(main_geometry, main_config, MESH_DISPLACEMENTS);
 }
-
-void CDriverBase::ReadFFDInfo(CGeometry* geometry, CConfig* config, CFreeFormDefBox** FFDBox, string val_mesh_filename) {
-  string text_line, iTag;
-  ifstream mesh_file;
-  su2double CPcoord[3], coord[] = {0, 0, 0};
-  unsigned short degree[3], iFFDBox, iCornerPoints, iControlPoints, iMarker, iDegree, jDegree, kDegree, iChar,
-      LevelFFDBox, nParentFFDBox, iParentFFDBox, nChildFFDBox, iChildFFDBox, nMarker, *nCornerPoints, *nControlPoints;
-  unsigned long iSurfacePoints, iPoint, jPoint, iVertex, nVertex, nPoint, iElem = 0, nElem, my_nSurfPoints, nSurfPoints,
-                                                                          *nSurfacePoints;
-  su2double XCoord, YCoord;
-
-  bool polar = (config->GetFFD_CoordSystem() == POLAR);
-  unsigned short nDim = geometry->GetnDim(), iDim;
-  unsigned short SplineOrder[3];
-  unsigned short Blending = 0;
-
-  unsigned short nFFDBox = 0;
-  unsigned short nLevel = 0;
-
-  if (config->GetMesh_FileFormat() != SU2) {
-    if (rank == MASTER_NODE) cout << "Mesh file format is not .su2 so FFD box information cannot be extracted." << endl;
-    return;
-  }
-
-  mesh_file.open(val_mesh_filename);
-  if (mesh_file.fail()) {
-    SU2_MPI::Error("There is no geometry file (ReadFFDInfo)!!", CURRENT_FUNCTION);
-  }
-
-  while (getline(mesh_file, text_line)) {
-    /*--- Read the inner elements. ---*/
-
-    string::size_type position = text_line.find("NELEM=", 0);
-    if (position != string::npos) {
-      text_line.erase(0, 6);
-      nElem = atoi(text_line.c_str());
-      for (iElem = 0; iElem < nElem; iElem++) {
-        getline(mesh_file, text_line);
-      }
-    }
-
-    /*--- Read the inner points. ---*/
-
-    position = text_line.find("NPOIN=", 0);
-    if (position != string::npos) {
-      text_line.erase(0, 6);
-      nPoint = atoi(text_line.c_str());
-      for (iPoint = 0; iPoint < nPoint; iPoint++) {
-        getline(mesh_file, text_line);
-      }
-    }
-
-    /*--- Read the boundaries. ---*/
-
-    position = text_line.find("NMARK=", 0);
-    if (position != string::npos) {
-      text_line.erase(0, 6);
-      nMarker = atoi(text_line.c_str());
-      for (iMarker = 0; iMarker < nMarker; iMarker++) {
-        getline(mesh_file, text_line);
-        getline(mesh_file, text_line);
-        text_line.erase(0, 13);
-        nVertex = atoi(text_line.c_str());
-        for (iVertex = 0; iVertex < nVertex; iVertex++) {
-          getline(mesh_file, text_line);
-        }
-      }
-    }
-
-    /*--- Read the FFDBox information. ---*/
-
-    position = text_line.find("FFD_NBOX=", 0);
-    if (position != string::npos) {
-      text_line.erase(0, 9);
-      nFFDBox = atoi(text_line.c_str());
-
-      if (rank == MASTER_NODE) cout << nFFDBox << " Free Form Deformation boxes." << endl;
-
-      nCornerPoints = new unsigned short[nFFDBox];
-      nControlPoints = new unsigned short[nFFDBox];
-      nSurfacePoints = new unsigned long[nFFDBox];
-
-      getline(mesh_file, text_line);
-      text_line.erase(0, 11);
-      nLevel = atoi(text_line.c_str());
-
-      if (rank == MASTER_NODE) cout << nLevel << " Free Form Deformation nested levels." << endl;
-
-      for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) {
-        /*--- Read the name of the FFD box. ---*/
-
-        getline(mesh_file, text_line);
-        text_line.erase(0, 8);
-
-        /*--- Remove extra data from the FFDBox name. ---*/
-
-        string::size_type position;
-        for (iChar = 0; iChar < 20; iChar++) {
-          position = text_line.find(" ", 0);
-          if (position != string::npos) text_line.erase(position, 1);
-          position = text_line.find("\r", 0);
-          if (position != string::npos) text_line.erase(position, 1);
-          position = text_line.find("\n", 0);
-          if (position != string::npos) text_line.erase(position, 1);
-        }
-
-        string TagFFDBox = text_line.c_str();
-
-        if (rank == MASTER_NODE) cout << "FFD box tag: " << TagFFDBox << ". ";
-
-        /*--- Read the level of the FFD box. ---*/
-
-        getline(mesh_file, text_line);
-        text_line.erase(0, 10);
-        LevelFFDBox = atoi(text_line.c_str());
-
-        if (rank == MASTER_NODE) cout << "FFD box level: " << LevelFFDBox << ". ";
-
-        /*--- Read the degree of the FFD box. ---*/
-
-        if (nDim == 2) {
-          if (polar) {
-            getline(mesh_file, text_line);
-            text_line.erase(0, 13);
-            degree[0] = atoi(text_line.c_str());
-            degree[1] = 1;
-            getline(mesh_file, text_line);
-            text_line.erase(0, 13);
-            degree[2] = atoi(text_line.c_str());
-          } else {
-            getline(mesh_file, text_line);
-            text_line.erase(0, 13);
-            degree[0] = atoi(text_line.c_str());
-            getline(mesh_file, text_line);
-            text_line.erase(0, 13);
-            degree[1] = atoi(text_line.c_str());
-            degree[2] = 1;
-          }
-        } else {
-          getline(mesh_file, text_line);
-          text_line.erase(0, 13);
-          degree[0] = atoi(text_line.c_str());
-          getline(mesh_file, text_line);
-          text_line.erase(0, 13);
-          degree[1] = atoi(text_line.c_str());
-          getline(mesh_file, text_line);
-          text_line.erase(0, 13);
-          degree[2] = atoi(text_line.c_str());
-        }
-
-        if (rank == MASTER_NODE) {
-          if (nDim == 2) {
-            if (polar)
-              cout << "Degrees: " << degree[0] << ", " << degree[2] << "." << endl;
-            else
-              cout << "Degrees: " << degree[0] << ", " << degree[1] << "." << endl;
-          } else
-            cout << "Degrees: " << degree[0] << ", " << degree[1] << ", " << degree[2] << "." << endl;
-        }
-
-        getline(mesh_file, text_line);
-        if (text_line.substr(0, 12) != "FFD_BLENDING") {
-          SU2_MPI::Error(
-              string("Deprecated FFD information found in mesh file.\n") +
-                  string(
-                      "FFD information generated with SU2 version <= 4.3 is incompatible with the current version.") +
-                  string("Run SU2_DEF again with DV_KIND= FFD_SETTING."),
-              CURRENT_FUNCTION);
-        }
-        text_line.erase(0, 14);
-        if (text_line == "BEZIER") {
-          Blending = BEZIER;
-        }
-        if (text_line == "BSPLINE_UNIFORM") {
-          Blending = BSPLINE_UNIFORM;
-        }
-
-        if (Blending == BSPLINE_UNIFORM) {
-          getline(mesh_file, text_line);
-          text_line.erase(0, 17);
-          SplineOrder[0] = atoi(text_line.c_str());
-          getline(mesh_file, text_line);
-          text_line.erase(0, 17);
-          SplineOrder[1] = atoi(text_line.c_str());
-          if (nDim == 3) {
-            getline(mesh_file, text_line);
-            text_line.erase(0, 17);
-            SplineOrder[2] = atoi(text_line.c_str());
-          } else {
-            SplineOrder[2] = 2;
-          }
-        }
-        if (rank == MASTER_NODE) {
-          if (Blending == BSPLINE_UNIFORM) {
-            cout << "FFD Blending using B-Splines. ";
-            cout << "Order: " << SplineOrder[0] << ", " << SplineOrder[1];
-            if (nDim == 3) cout << ", " << SplineOrder[2];
-            cout << ". " << endl;
-          }
-          if (Blending == BEZIER) {
-            cout << "FFD Blending using Bezier Curves." << endl;
-          }
-        }
-
-        FFDBox[iFFDBox] = new CFreeFormDefBox(degree, SplineOrder, Blending);
-        FFDBox[iFFDBox]->SetTag(TagFFDBox);
-        FFDBox[iFFDBox]->SetLevel(LevelFFDBox);
-
-        /*--- Read the number of parents boxes. ---*/
-
-        getline(mesh_file, text_line);
-        text_line.erase(0, 12);
-        nParentFFDBox = atoi(text_line.c_str());
-        if (rank == MASTER_NODE) cout << "Number of parent boxes: " << nParentFFDBox << ". ";
-        for (iParentFFDBox = 0; iParentFFDBox < nParentFFDBox; iParentFFDBox++) {
-          getline(mesh_file, text_line);
-
-          /*--- Remove extra data from the FFDBox name. ---*/
-
-          string::size_type position;
-          for (iChar = 0; iChar < 20; iChar++) {
-            position = text_line.find(" ", 0);
-            if (position != string::npos) text_line.erase(position, 1);
-            position = text_line.find("\r", 0);
-            if (position != string::npos) text_line.erase(position, 1);
-            position = text_line.find("\n", 0);
-            if (position != string::npos) text_line.erase(position, 1);
-          }
-
-          string ParentFFDBox = text_line.c_str();
-          FFDBox[iFFDBox]->SetParentFFDBox(ParentFFDBox);
-        }
-
-        /*--- Read the number of children boxes. ---*/
-
-        getline(mesh_file, text_line);
-        text_line.erase(0, 13);
-        nChildFFDBox = atoi(text_line.c_str());
-        if (rank == MASTER_NODE) cout << "Number of child boxes: " << nChildFFDBox << "." << endl;
-
-        for (iChildFFDBox = 0; iChildFFDBox < nChildFFDBox; iChildFFDBox++) {
-          getline(mesh_file, text_line);
-
-          /*--- Remove extra data from the FFDBox name. ---*/
-
-          string::size_type position;
-          for (iChar = 0; iChar < 20; iChar++) {
-            position = text_line.find(" ", 0);
-            if (position != string::npos) text_line.erase(position, 1);
-            position = text_line.find("\r", 0);
-            if (position != string::npos) text_line.erase(position, 1);
-            position = text_line.find("\n", 0);
-            if (position != string::npos) text_line.erase(position, 1);
-          }
-
-          string ChildFFDBox = text_line.c_str();
-          FFDBox[iFFDBox]->SetChildFFDBox(ChildFFDBox);
-        }
-
-        /*--- Read the number of the corner points. ---*/
-
-        getline(mesh_file, text_line);
-        text_line.erase(0, 18);
-        nCornerPoints[iFFDBox] = atoi(text_line.c_str());
-        if (rank == MASTER_NODE) cout << "Corner points: " << nCornerPoints[iFFDBox] << ". ";
-        if (nDim == 2) nCornerPoints[iFFDBox] = nCornerPoints[iFFDBox] * SU2_TYPE::Int(2);
-
-        /*--- Read the coordinates of the corner points. ---*/
-
-        if (nDim == 2) {
-          if (polar) {
-            getline(mesh_file, text_line);
-            istringstream FFDBox_line_1(text_line);
-            FFDBox_line_1 >> XCoord;
-            FFDBox_line_1 >> YCoord;
-
-            CPcoord[0] = XCoord;
-            CPcoord[1] = cos(0.1) * YCoord;
-            CPcoord[2] = -sin(0.1) * YCoord;
-            FFDBox[iFFDBox]->SetCoordCornerPoints(coord, 4);
-
-            CPcoord[0] = XCoord;
-            CPcoord[1] = cos(0.1) * YCoord;
-            CPcoord[2] = sin(0.1) * YCoord;
-            FFDBox[iFFDBox]->SetCoordCornerPoints(coord, 7);
-
-            getline(mesh_file, text_line);
-            istringstream FFDBox_line_2(text_line);
-            FFDBox_line_2 >> XCoord;
-            FFDBox_line_2 >> YCoord;
-
-            CPcoord[0] = XCoord;
-            CPcoord[1] = cos(0.1) * YCoord;
-            CPcoord[2] = -sin(0.1) * YCoord;
-            FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, 0);
-
-            CPcoord[0] = XCoord;
-            CPcoord[1] = cos(0.1) * YCoord;
-            CPcoord[2] = sin(0.1) * YCoord;
-            FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, 3);
-
-            getline(mesh_file, text_line);
-            istringstream FFDBox_line_3(text_line);
-            FFDBox_line_3 >> XCoord;
-            FFDBox_line_3 >> YCoord;
-
-            CPcoord[0] = XCoord;
-            CPcoord[1] = cos(0.1) * YCoord;
-            CPcoord[2] = -sin(0.1) * YCoord;
-            FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, 1);
-
-            CPcoord[0] = XCoord;
-            CPcoord[1] = cos(0.1) * YCoord;
-            CPcoord[2] = sin(0.1) * YCoord;
-            FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, 2);
-
-            getline(mesh_file, text_line);
-            istringstream FFDBox_line_4(text_line);
-            FFDBox_line_4 >> XCoord;
-            FFDBox_line_4 >> YCoord;
-
-            CPcoord[0] = XCoord;
-            CPcoord[1] = cos(0.1) * YCoord;
-            CPcoord[2] = -sin(0.1) * YCoord;
-            FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, 5);
-
-            CPcoord[0] = XCoord;
-            CPcoord[1] = cos(0.1) * YCoord;
-            CPcoord[2] = sin(0.1) * YCoord;
-            FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, 6);
-
-          } else {
-            for (iCornerPoints = 0; iCornerPoints < nCornerPoints[iFFDBox]; iCornerPoints++) {
-              if (iCornerPoints < nCornerPoints[iFFDBox] / SU2_TYPE::Int(2)) {
-                getline(mesh_file, text_line);
-                istringstream FFDBox_line(text_line);
-                FFDBox_line >> CPcoord[0];
-                FFDBox_line >> CPcoord[1];
-                CPcoord[2] = -0.5;
-              } else {
-                CPcoord[0] =
-                    FFDBox[iFFDBox]->GetCoordCornerPoints(0, iCornerPoints - nCornerPoints[iFFDBox] / SU2_TYPE::Int(2));
-                CPcoord[1] =
-                    FFDBox[iFFDBox]->GetCoordCornerPoints(1, iCornerPoints - nCornerPoints[iFFDBox] / SU2_TYPE::Int(2));
-                CPcoord[2] = 0.5;
-              }
-              FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, iCornerPoints);
-            }
-          }
-
-        } else {
-          for (iCornerPoints = 0; iCornerPoints < nCornerPoints[iFFDBox]; iCornerPoints++) {
-            getline(mesh_file, text_line);
-            istringstream FFDBox_line(text_line);
-            FFDBox_line >> CPcoord[0];
-            FFDBox_line >> CPcoord[1];
-            FFDBox_line >> CPcoord[2];
-            FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, iCornerPoints);
-          }
-        }
-
-        /*--- Read the number of the control points. ---*/
-
-        getline(mesh_file, text_line);
-        text_line.erase(0, 19);
-        nControlPoints[iFFDBox] = atoi(text_line.c_str());
-
-        if (rank == MASTER_NODE) cout << "Control points: " << nControlPoints[iFFDBox] << ". ";
-
-        /*--- Read the coordinates of the control points. ---*/
-
-        for (iControlPoints = 0; iControlPoints < nControlPoints[iFFDBox]; iControlPoints++) {
-          getline(mesh_file, text_line);
-          istringstream FFDBox_line(text_line);
-          FFDBox_line >> iDegree;
-          FFDBox_line >> jDegree;
-          FFDBox_line >> kDegree;
-          FFDBox_line >> CPcoord[0];
-          FFDBox_line >> CPcoord[1];
-          FFDBox_line >> CPcoord[2];
-          FFDBox[iFFDBox]->SetCoordControlPoints(CPcoord, iDegree, jDegree, kDegree);
-          FFDBox[iFFDBox]->SetCoordControlPoints_Copy(CPcoord, iDegree, jDegree, kDegree);
-        }
-
-        getline(mesh_file, text_line);
-        text_line.erase(0, 19);
-        nSurfacePoints[iFFDBox] = atoi(text_line.c_str());
-
-        /*--- The surface points parametric coordinates (all the nodes read the FFD
-         * information but they only store their part). ---*/
-
-        my_nSurfPoints = 0;
-        for (iSurfacePoints = 0; iSurfacePoints < nSurfacePoints[iFFDBox]; iSurfacePoints++) {
-          getline(mesh_file, text_line);
-          istringstream FFDBox_line(text_line);
-          FFDBox_line >> iTag;
-          FFDBox_line >> iPoint;
-
-          if (config->GetMarker_All_TagBound(iTag) != -1) {
-            iMarker = config->GetMarker_All_TagBound(iTag);
-            FFDBox_line >> CPcoord[0];
-            FFDBox_line >> CPcoord[1];
-            FFDBox_line >> CPcoord[2];
-
-            for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
-              jPoint = geometry->vertex[iMarker][iVertex]->GetNode();
-              if (iPoint == geometry->nodes->GetGlobalIndex(jPoint)) {
-                for (iDim = 0; iDim < nDim; iDim++) {
-                  coord[iDim] = geometry->nodes->GetCoord(jPoint, iDim);
-                }
-                FFDBox[iFFDBox]->Set_MarkerIndex(iMarker);
-                FFDBox[iFFDBox]->Set_VertexIndex(iVertex);
-                FFDBox[iFFDBox]->Set_PointIndex(jPoint);
-                FFDBox[iFFDBox]->Set_ParametricCoord(CPcoord);
-                FFDBox[iFFDBox]->Set_CartesianCoord(coord);
-                my_nSurfPoints++;
-              }
-            }
-          }
-        }
-
-        nSurfacePoints[iFFDBox] = my_nSurfPoints;
-
-#ifdef HAVE_MPI
-        nSurfPoints = 0;
-        SU2_MPI::Allreduce(&my_nSurfPoints, &nSurfPoints, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
-        if (rank == MASTER_NODE) cout << "Surface points: " << nSurfPoints << "." << endl;
-#else
-        nSurfPoints = my_nSurfPoints;
-        if (rank == MASTER_NODE) cout << "Surface points: " << nSurfPoints << "." << endl;
-#endif
-      }
-
-      delete[] nCornerPoints;
-      delete[] nControlPoints;
-      delete[] nSurfacePoints;
-    }
-  }
-  mesh_file.close();
-
-  if (nFFDBox == 0) {
-    if (rank == MASTER_NODE) cout << "There is no FFD box definition. Just in case, check the .su2 file" << endl;
-  }
-}

From 030030ad31dab0dd4eec27952ccfe43126751d58 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Wed, 28 Dec 2022 16:51:48 -0800
Subject: [PATCH 098/656] Apply clang format to python_wrapper_structure.cpp

---
 SU2_CFD/src/python_wrapper_structure.cpp | 1058 +++++++++++-----------
 1 file changed, 504 insertions(+), 554 deletions(-)

diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index 9ee05047ee9..b3d8feed938 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -1,324 +1,292 @@
 /*!
- * \file python_wrapper_structure.cpp
- * \brief Driver subroutines that are used by the Python wrapper. Those routines are usually called from an external Python environment.
- * \author D. Thomas
- * \version 7.5.0 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-
+* \file python_wrapper_structure.cpp
+* \brief Driver subroutines that are used by the Python wrapper (usually called from an external Python environment).
+* \author D. Thomas
+* \version 7.5.0 "Blackbird"
+*
+* SU2 Project Website: https://su2code.github.io
+*
+* The SU2 Project is maintained by the SU2 Foundation
+* (http://su2foundation.org)
+*
+* Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+*
+* SU2 is free software; you can redistribute it and/or
+* modify it under the terms of the GNU Lesser General Public
+* License as published by the Free Software Foundation; either
+* version 2.1 of the License, or (at your option) any later version.
+*
+* SU2 is distributed in the hope that it will be useful,
+* but WITHOUT ANY WARRANTY; without even the implied warranty of
+* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+* Lesser General Public License for more details.
+*
+* You should have received a copy of the GNU Lesser General Public
+* License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+*/
 
+#include "../../Common/include/toolboxes/geometry_toolbox.hpp"
 #include "../include/drivers/CDriver.hpp"
 #include "../include/drivers/CSinglezoneDriver.hpp"
-#include "../../Common/include/toolboxes/geometry_toolbox.hpp"
 
-void CDriver::PythonInterface_Preprocessing(CConfig **config, CGeometry ****geometry, CSolver *****solver){
-    
-    int rank = MASTER_NODE;
-    SU2_MPI::Comm_rank(SU2_MPI::GetComm(), &rank);
-    
-    /* --- Initialize boundary conditions customization, this is achieve through the Python wrapper --- */
-    for(iZone=0; iZone < nZone; iZone++){
-        
-        if (config[iZone]->GetnMarker_PyCustom() > 0){
-            
-            if (rank == MASTER_NODE) cout << endl << "----------------- Python Interface Preprocessing ( Zone "<< iZone <<" ) -----------------" << endl;
-            
-            if (rank == MASTER_NODE) cout << "Setting customized boundary conditions for zone " << iZone << endl;
-            for (iMesh = 0; iMesh <= config[iZone]->GetnMGLevels(); iMesh++) {
-                geometry[iZone][INST_0][iMesh]->SetCustomBoundary(config[iZone]);
-            }
-            geometry[iZone][INST_0][MESH_0]->UpdateCustomBoundaryConditions(geometry[iZone][INST_0], config[iZone]);
-            
-            if ((config[iZone]->GetKind_Solver() == MAIN_SOLVER::EULER) ||
-                (config[iZone]->GetKind_Solver() == MAIN_SOLVER::NAVIER_STOKES) ||
-                (config[iZone]->GetKind_Solver() == MAIN_SOLVER::RANS) ||
-                (config[iZone]->GetKind_Solver() == MAIN_SOLVER::INC_EULER) ||
-                (config[iZone]->GetKind_Solver() == MAIN_SOLVER::INC_NAVIER_STOKES) ||
-                (config[iZone]->GetKind_Solver() == MAIN_SOLVER::INC_RANS) ||
-                (config[iZone]->GetKind_Solver() == MAIN_SOLVER::NEMO_EULER) ||
-                (config[iZone]->GetKind_Solver() == MAIN_SOLVER::NEMO_NAVIER_STOKES)) {
-                
-                solver[iZone][INST_0][MESH_0][FLOW_SOL]->UpdateCustomBoundaryConditions(geometry[iZone][INST_0], config[iZone]);
-            }
-        }
+void CDriver::PythonInterface_Preprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver) {
+  int rank = MASTER_NODE;
+  SU2_MPI::Comm_rank(SU2_MPI::GetComm(), &rank);
+
+  /* --- Initialize boundary conditions customization, this is achieved through the Python wrapper. --- */
+  for (iZone = 0; iZone < nZone; iZone++) {
+    if (config[iZone]->GetnMarker_PyCustom() > 0) {
+      if (rank == MASTER_NODE) cout << "----------------- Python Interface Preprocessing ( Zone " << iZone << " ) -----------------" << endl;
+
+      if (rank == MASTER_NODE) cout << "Setting customized boundary conditions for zone " << iZone << endl;
+      for (iMesh = 0; iMesh <= config[iZone]->GetnMGLevels(); iMesh++) {
+        geometry[iZone][INST_0][iMesh]->SetCustomBoundary(config[iZone]);
+      }
+      geometry[iZone][INST_0][MESH_0]->UpdateCustomBoundaryConditions(geometry[iZone][INST_0], config[iZone]);
+
+      if ((config[iZone]->GetKind_Solver() == MAIN_SOLVER::EULER) ||
+          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::NAVIER_STOKES) ||
+          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::RANS) ||
+          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::INC_EULER) ||
+          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::INC_NAVIER_STOKES) ||
+          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::INC_RANS) ||
+          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::NEMO_EULER) ||
+          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::NEMO_NAVIER_STOKES)) {
+        solver[iZone][INST_0][MESH_0][FLOW_SOL]->UpdateCustomBoundaryConditions(geometry[iZone][INST_0], config[iZone]);
+      }
     }
-    
+  }
 }
 
 /////////////////////////////////////////////////////////////////////////////
-/* Functions related to the global performance indices (Lift, Drag, ecc..) */
+/* Functions related to the global performance indices (Lift, Drag, etc.)  */
 /////////////////////////////////////////////////////////////////////////////
 
 passivedouble CDriver::Get_Drag() const {
-    
-    unsigned short val_iZone = ZONE_0;
-    unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
-    su2double CDrag, factor, val_Drag;
-    
-    /*--- Calculate drag force based on drag coefficient ---*/
-    factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
-    CDrag = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CD();
-    
-    val_Drag = CDrag*factor;
-    
-    return SU2_TYPE::GetValue(val_Drag);
+  unsigned short val_iZone = ZONE_0;
+  unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
+  su2double CDrag, factor, val_Drag;
+
+  /*--- Calculate drag force based on drag coefficient ---*/
+  factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
+  CDrag = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CD();
+
+  val_Drag = CDrag * factor;
+
+  return SU2_TYPE::GetValue(val_Drag);
 }
 
 passivedouble CDriver::Get_Lift() const {
-    
-    unsigned short val_iZone = ZONE_0;
-    unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
-    su2double CLift, factor, val_Lift;
-    
-    /*--- Calculate drag force based on drag coefficient ---*/
-    factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
-    CLift = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CL();
-    
-    val_Lift = CLift*factor;
-    
-    return SU2_TYPE::GetValue(val_Lift);
+  unsigned short val_iZone = ZONE_0;
+  unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
+  su2double CLift, factor, val_Lift;
+
+  /*--- Calculate drag force based on drag coefficient ---*/
+  factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
+  CLift = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CL();
+
+  val_Lift = CLift * factor;
+
+  return SU2_TYPE::GetValue(val_Lift);
 }
 
 passivedouble CDriver::Get_Mx() const {
-    
-    unsigned short val_iZone = ZONE_0;
-    unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
-    su2double CMx, RefLengthCoeff, factor, val_Mx;
-    
-    RefLengthCoeff = config_container[val_iZone]->GetRefLength();
-    
-    /*--- Calculate moment around x-axis based on coefficients ---*/
-    factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
-    CMx = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMx();
-    
-    val_Mx = CMx*factor*RefLengthCoeff;
-    
-    return SU2_TYPE::GetValue(val_Mx);
+  unsigned short val_iZone = ZONE_0;
+  unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
+  su2double CMx, RefLengthCoeff, factor, val_Mx;
+
+  RefLengthCoeff = config_container[val_iZone]->GetRefLength();
+
+  /*--- Calculate moment around x-axis based on coefficients ---*/
+  factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
+  CMx = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMx();
+
+  val_Mx = CMx * factor * RefLengthCoeff;
+
+  return SU2_TYPE::GetValue(val_Mx);
 }
 
 passivedouble CDriver::Get_My() const {
-    
-    unsigned short val_iZone = ZONE_0;
-    unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
-    su2double CMy, RefLengthCoeff, factor, val_My;
-    
-    RefLengthCoeff = config_container[val_iZone]->GetRefLength();
-    
-    /*--- Calculate moment around x-axis based on coefficients ---*/
-    factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
-    CMy = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMy();
-    
-    val_My = CMy*factor*RefLengthCoeff;
-    
-    return SU2_TYPE::GetValue(val_My);
+  unsigned short val_iZone = ZONE_0;
+  unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
+  su2double CMy, RefLengthCoeff, factor, val_My;
+
+  RefLengthCoeff = config_container[val_iZone]->GetRefLength();
+
+  /*--- Calculate moment around x-axis based on coefficients ---*/
+  factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
+  CMy = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMy();
+
+  val_My = CMy * factor * RefLengthCoeff;
+
+  return SU2_TYPE::GetValue(val_My);
 }
 
 passivedouble CDriver::Get_Mz() const {
-    
-    unsigned short val_iZone = ZONE_0;
-    unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
-    su2double CMz, RefLengthCoeff, factor, val_Mz;
-    
-    RefLengthCoeff = config_container[val_iZone]->GetRefLength();
-    
-    /*--- Calculate moment around z-axis based on coefficients ---*/
-    factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
-    CMz = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMz();
-    
-    val_Mz = CMz*factor*RefLengthCoeff;
-    
-    return SU2_TYPE::GetValue(val_Mz);
+  unsigned short val_iZone = ZONE_0;
+  unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
+  su2double CMz, RefLengthCoeff, factor, val_Mz;
+
+  RefLengthCoeff = config_container[val_iZone]->GetRefLength();
+
+  /*--- Calculate moment around z-axis based on coefficients ---*/
+  factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
+  CMz = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMz();
+
+  val_Mz = CMz * factor * RefLengthCoeff;
+
+  return SU2_TYPE::GetValue(val_Mz);
 }
 
 passivedouble CDriver::Get_DragCoeff() const {
-    
-    unsigned short val_iZone = ZONE_0;
-    unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
-    su2double CDrag;
-    
-    CDrag = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CD();
-    
-    return SU2_TYPE::GetValue(CDrag);
+  unsigned short val_iZone = ZONE_0;
+  unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
+  su2double CDrag;
+
+  CDrag = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CD();
+
+  return SU2_TYPE::GetValue(CDrag);
 }
 
 passivedouble CDriver::Get_LiftCoeff() const {
-    
-    unsigned short val_iZone = ZONE_0;
-    unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
-    su2double CLift;
-    
-    CLift = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CL();
-    
-    return SU2_TYPE::GetValue(CLift);
+  unsigned short val_iZone = ZONE_0;
+  unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
+  su2double CLift;
+
+  CLift = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CL();
+
+  return SU2_TYPE::GetValue(CLift);
 }
 
 //////////////////////////////////////////////////////////////////////////////////
-/* Functions to obtain global parameters from SU2 (time steps, delta t, ecc...) */
+/* Functions to obtain global parameters from SU2 (time steps, delta t, etc.)   */
 //////////////////////////////////////////////////////////////////////////////////
 
-unsigned long CDriver::GetnTimeIter() const {
-    
-    return config_container[ZONE_0]->GetnTime_Iter();
-}
+unsigned long CDriver::GetnTimeIter() const { return config_container[ZONE_0]->GetnTime_Iter(); }
 
-unsigned long CDriver::GetTime_Iter() const{
-    
-    return TimeIter;
-}
+unsigned long CDriver::GetTime_Iter() const { return TimeIter; }
 
 passivedouble CDriver::GetUnsteady_TimeStep() const {
-    
-    return SU2_TYPE::GetValue(config_container[ZONE_0]->GetTime_Step());
+  return SU2_TYPE::GetValue(config_container[ZONE_0]->GetTime_Step());
 }
 
-string CDriver::GetSurfaceFileName() const {
-    
-    return config_container[ZONE_0]->GetSurfCoeff_FileName();
-}
+string CDriver::GetSurfaceFileName() const { return config_container[ZONE_0]->GetSurfCoeff_FileName(); }
 
 ///////////////////////////////////////////////////////////////////////////////
 /* Functions related to CHT solver                                           */
 ///////////////////////////////////////////////////////////////////////////////
 
 passivedouble CDriver::GetVertexTemperature(unsigned short iMarker, unsigned long iVertex) const {
-    
-    unsigned long iPoint;
-    su2double vertexWallTemp(0.0);
-    
-    bool compressible = (config_container[ZONE_0]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
-    
-    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-    
-    if(geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint) && compressible){
-        vertexWallTemp = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetTemperature(iPoint);
-    }
-    
-    return SU2_TYPE::GetValue(vertexWallTemp);
-    
+  unsigned long iPoint;
+  su2double vertexWallTemp(0.0);
+
+  bool compressible = (config_container[ZONE_0]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
+
+  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+
+  if (geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint) && compressible) {
+    vertexWallTemp = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetTemperature(iPoint);
+  }
+
+  return SU2_TYPE::GetValue(vertexWallTemp);
 }
 
-void CDriver::SetVertexTemperature(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallTemp){
-    
-    geometry_container[ZONE_0][INST_0][MESH_0]->SetCustomBoundaryTemperature(iMarker, iVertex, val_WallTemp);
+void CDriver::SetVertexTemperature(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallTemp) {
+  geometry_container[ZONE_0][INST_0][MESH_0]->SetCustomBoundaryTemperature(iMarker, iVertex, val_WallTemp);
 }
 
 vector<passivedouble> CDriver::GetVertexHeatFluxes(unsigned short iMarker, unsigned long iVertex) const {
-    
-    unsigned long iPoint;
-    unsigned short iDim;
-    su2double Prandtl_Lam  = config_container[ZONE_0]->GetPrandtl_Lam();
-    su2double Gas_Constant = config_container[ZONE_0]->GetGas_ConstantND();
-    su2double Gamma = config_container[ZONE_0]->GetGamma();
-    su2double Gamma_Minus_One = Gamma - 1.0;
-    su2double Cp = (Gamma / Gamma_Minus_One) * Gas_Constant;
-    su2double laminar_viscosity, thermal_conductivity;
-    vector<su2double> GradT (3,0.0);
-    vector<su2double> HeatFlux (3,0.0);
-    vector<passivedouble> HeatFluxPassive (3,0.0);
-    
-    bool compressible = (config_container[ZONE_0]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
-    
-    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-    
-    if(compressible){
-        laminar_viscosity    = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
-        thermal_conductivity = Cp * (laminar_viscosity/Prandtl_Lam);
-        for(iDim=0; iDim < nDim; iDim++){
-            GradT[iDim] = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetGradient_Primitive(iPoint, 0, iDim);
-            HeatFlux[iDim] = -thermal_conductivity*GradT[iDim];
-        }
+  unsigned long iPoint;
+  unsigned short iDim;
+  su2double Prandtl_Lam = config_container[ZONE_0]->GetPrandtl_Lam();
+  su2double Gas_Constant = config_container[ZONE_0]->GetGas_ConstantND();
+  su2double Gamma = config_container[ZONE_0]->GetGamma();
+  su2double Gamma_Minus_One = Gamma - 1.0;
+  su2double Cp = (Gamma / Gamma_Minus_One) * Gas_Constant;
+  su2double laminar_viscosity, thermal_conductivity;
+  vector<su2double> GradT(3, 0.0);
+  vector<su2double> HeatFlux(3, 0.0);
+  vector<passivedouble> HeatFluxPassive(3, 0.0);
+
+  bool compressible = (config_container[ZONE_0]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
+
+  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+
+  if (compressible) {
+    laminar_viscosity = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
+    thermal_conductivity = Cp * (laminar_viscosity / Prandtl_Lam);
+    for (iDim = 0; iDim < nDim; iDim++) {
+      GradT[iDim] = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetGradient_Primitive(iPoint, 0, iDim);
+      HeatFlux[iDim] = -thermal_conductivity * GradT[iDim];
     }
-    
-    HeatFluxPassive[0] = SU2_TYPE::GetValue(HeatFlux[0]);
-    HeatFluxPassive[1] = SU2_TYPE::GetValue(HeatFlux[1]);
-    HeatFluxPassive[2] = SU2_TYPE::GetValue(HeatFlux[2]);
-    
-    return HeatFluxPassive;
-}
-
-passivedouble CDriver::GetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex) const{
-    
-    unsigned long iPoint;
-    unsigned short iDim;
-    su2double vertexWallHeatFlux;
-    su2double Prandtl_Lam  = config_container[ZONE_0]->GetPrandtl_Lam();
-    su2double Gas_Constant = config_container[ZONE_0]->GetGas_ConstantND();
-    su2double Gamma = config_container[ZONE_0]->GetGamma();
-    su2double Gamma_Minus_One = Gamma - 1.0;
-    su2double Cp = (Gamma / Gamma_Minus_One) * Gas_Constant;
-    su2double Area;
-    su2double laminar_viscosity, thermal_conductivity, dTdn;
-    su2double *Normal, GradT[3] = {0.0,0.0,0.0}, UnitNormal[3] = {0.0,0.0,0.0};
-    
-    bool compressible = (config_container[ZONE_0]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
-    
-    vertexWallHeatFlux = 0.0;
-    dTdn = 0.0;
-    
-    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-    
-    if(geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint) && compressible){
-        Normal = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNormal();
-        
-        Area = GeometryToolbox::Norm(nDim, Normal);
-        
-        for (iDim = 0; iDim < nDim; iDim++)
-            UnitNormal[iDim] = Normal[iDim]/Area;
-        
-        laminar_viscosity    = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
-        thermal_conductivity = Cp * (laminar_viscosity/Prandtl_Lam);
-        /*Compute wall heat flux (normal to the wall) based on computed temperature gradient*/
-        for(iDim=0; iDim < nDim; iDim++){
-            GradT[iDim] = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetGradient_Primitive(iPoint, 0, iDim);
-            dTdn += GradT[iDim]*UnitNormal[iDim];
-        }
-        
-        vertexWallHeatFlux = -thermal_conductivity*dTdn;
+  }
+
+  HeatFluxPassive[0] = SU2_TYPE::GetValue(HeatFlux[0]);
+  HeatFluxPassive[1] = SU2_TYPE::GetValue(HeatFlux[1]);
+  HeatFluxPassive[2] = SU2_TYPE::GetValue(HeatFlux[2]);
+
+  return HeatFluxPassive;
+}
+
+passivedouble CDriver::GetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex) const {
+  unsigned long iPoint;
+  unsigned short iDim;
+  su2double vertexWallHeatFlux;
+  su2double Prandtl_Lam = config_container[ZONE_0]->GetPrandtl_Lam();
+  su2double Gas_Constant = config_container[ZONE_0]->GetGas_ConstantND();
+  su2double Gamma = config_container[ZONE_0]->GetGamma();
+  su2double Gamma_Minus_One = Gamma - 1.0;
+  su2double Cp = (Gamma / Gamma_Minus_One) * Gas_Constant;
+  su2double Area;
+  su2double laminar_viscosity, thermal_conductivity, dTdn;
+  su2double *Normal, GradT[3] = {0.0, 0.0, 0.0}, UnitNormal[3] = {0.0, 0.0, 0.0};
+
+  bool compressible = (config_container[ZONE_0]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
+
+  vertexWallHeatFlux = 0.0;
+  dTdn = 0.0;
+
+  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+
+  if (geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint) && compressible) {
+    Normal = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNormal();
+
+    Area = GeometryToolbox::Norm(nDim, Normal);
+
+    for (iDim = 0; iDim < nDim; iDim++) UnitNormal[iDim] = Normal[iDim] / Area;
+
+    laminar_viscosity = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
+    thermal_conductivity = Cp * (laminar_viscosity / Prandtl_Lam);
+    /*Compute wall heat flux (normal to the wall) based on computed temperature gradient*/
+    for (iDim = 0; iDim < nDim; iDim++) {
+      GradT[iDim] = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetGradient_Primitive(iPoint, 0, iDim);
+      dTdn += GradT[iDim] * UnitNormal[iDim];
     }
-    
-    return SU2_TYPE::GetValue(vertexWallHeatFlux);
+
+    vertexWallHeatFlux = -thermal_conductivity * dTdn;
+  }
+
+  return SU2_TYPE::GetValue(vertexWallHeatFlux);
 }
 
-void CDriver::SetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallHeatFlux){
-    
-    geometry_container[ZONE_0][INST_0][MESH_0]->SetCustomBoundaryHeatFlux(iMarker, iVertex, val_WallHeatFlux);
+void CDriver::SetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallHeatFlux) {
+  geometry_container[ZONE_0][INST_0][MESH_0]->SetCustomBoundaryHeatFlux(iMarker, iVertex, val_WallHeatFlux);
 }
 
 passivedouble CDriver::GetThermalConductivity(unsigned short iMarker, unsigned long iVertex) const {
-    
-    unsigned long iPoint;
-    su2double Prandtl_Lam  = config_container[ZONE_0]->GetPrandtl_Lam();
-    su2double Gas_Constant = config_container[ZONE_0]->GetGas_ConstantND();
-    su2double Gamma = config_container[ZONE_0]->GetGamma();
-    su2double Gamma_Minus_One = Gamma - 1.0;
-    su2double Cp = (Gamma / Gamma_Minus_One) * Gas_Constant;
-    su2double laminar_viscosity, thermal_conductivity;
-    
-    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-    laminar_viscosity    = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
-    thermal_conductivity = Cp * (laminar_viscosity/Prandtl_Lam);
-    
-    return SU2_TYPE::GetValue(thermal_conductivity);
-    
+  unsigned long iPoint;
+  su2double Prandtl_Lam = config_container[ZONE_0]->GetPrandtl_Lam();
+  su2double Gas_Constant = config_container[ZONE_0]->GetGas_ConstantND();
+  su2double Gamma = config_container[ZONE_0]->GetGamma();
+  su2double Gamma_Minus_One = Gamma - 1.0;
+  su2double Cp = (Gamma / Gamma_Minus_One) * Gas_Constant;
+  su2double laminar_viscosity, thermal_conductivity;
+
+  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+  laminar_viscosity = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
+  thermal_conductivity = Cp * (laminar_viscosity / Prandtl_Lam);
+
+  return SU2_TYPE::GetValue(thermal_conductivity);
 }
 
 ////////////////////////////////////////////////////////////////////////////////
@@ -326,231 +294,228 @@ passivedouble CDriver::GetThermalConductivity(unsigned short iMarker, unsigned l
 ////////////////////////////////////////////////////////////////////////////////
 
 vector<string> CDriver::GetCHTMarkerTags() const {
-    vector<string> tags;
-    const auto nMarker = config_container[ZONE_0]->GetnMarker_All();
-    
-    //The CHT markers can be identified as the markers that are customizable with a BC type HEAT_FLUX or ISOTHERMAL.
-    for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
-        if ((config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == HEAT_FLUX || 
-             config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == ISOTHERMAL) && config_container[ZONE_0]->GetMarker_All_PyCustom(iMarker)){
-            
-            tags.push_back(config_container[ZONE_0]->GetMarker_All_TagBound(iMarker));
-        }
+  vector<string> tags;
+  const auto nMarker = config_container[ZONE_0]->GetnMarker_All();
+
+  // The CHT markers can be identified as the markers that are customizable with a BC type HEAT_FLUX or ISOTHERMAL.
+  for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
+    if ((config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == HEAT_FLUX ||
+         config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == ISOTHERMAL) &&
+        config_container[ZONE_0]->GetMarker_All_PyCustom(iMarker)) {
+      tags.push_back(config_container[ZONE_0]->GetMarker_All_TagBound(iMarker));
     }
-    
-    return tags;
+  }
+
+  return tags;
 }
 
 vector<string> CDriver::GetInletMarkerTags() const {
-    vector<string> tags;
-    const auto nMarker = config_container[ZONE_0]->GetnMarker_All();
-    
-    for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
-        bool isCustomizable = config_container[ZONE_0]->GetMarker_All_PyCustom(iMarker);
-        bool isInlet = (config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == INLET_FLOW);
-        
-        if (isCustomizable && isInlet) {
-            tags.push_back(config_container[ZONE_0]->GetMarker_All_TagBound(iMarker));
-        }
-    }
-    
-    return tags;
-}
-
-void CDriver::SetHeatSource_Position(passivedouble alpha, passivedouble pos_x, passivedouble pos_y, passivedouble pos_z){
-    
-    CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][RAD_SOL];
-    
-    config_container[ZONE_0]->SetHeatSource_Rot_Z(alpha);
-    config_container[ZONE_0]->SetHeatSource_Center(pos_x, pos_y, pos_z);
-    
-    solver->SetVolumetricHeatSource(geometry_container[ZONE_0][INST_0][MESH_0], config_container[ZONE_0]);
-    
-}
-
-void CDriver::SetInlet_Angle(unsigned short iMarker, passivedouble alpha){
-    
-    su2double alpha_rad = alpha * PI_NUMBER/180.0;
-    
-    unsigned long iVertex;
-    
-    for (iVertex = 0; iVertex < geometry_container[ZONE_0][INST_0][MESH_0]->nVertex[iMarker]; iVertex++){
-        solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->SetInlet_FlowDir(iMarker, iVertex, 0, cos(alpha_rad));
-        solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->SetInlet_FlowDir(iMarker, iVertex, 1, sin(alpha_rad));
+  vector<string> tags;
+  const auto nMarker = config_container[ZONE_0]->GetnMarker_All();
+
+  for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
+    bool isCustomizable = config_container[ZONE_0]->GetMarker_All_PyCustom(iMarker);
+    bool isInlet = (config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == INLET_FLOW);
+
+    if (isCustomizable && isInlet) {
+      tags.push_back(config_container[ZONE_0]->GetMarker_All_TagBound(iMarker));
     }
-    
+  }
+
+  return tags;
+}
+
+void CDriver::SetHeatSource_Position(passivedouble alpha, passivedouble pos_x, passivedouble pos_y,
+                                     passivedouble pos_z) {
+  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][RAD_SOL];
+
+  config_container[ZONE_0]->SetHeatSource_Rot_Z(alpha);
+  config_container[ZONE_0]->SetHeatSource_Center(pos_x, pos_y, pos_z);
+
+  solver->SetVolumetricHeatSource(geometry_container[ZONE_0][INST_0][MESH_0], config_container[ZONE_0]);
+}
+
+void CDriver::SetInlet_Angle(unsigned short iMarker, passivedouble alpha) {
+  su2double alpha_rad = alpha * PI_NUMBER / 180.0;
+
+  unsigned long iVertex;
+
+  for (iVertex = 0; iVertex < geometry_container[ZONE_0][INST_0][MESH_0]->nVertex[iMarker]; iVertex++) {
+    solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->SetInlet_FlowDir(iMarker, iVertex, 0, cos(alpha_rad));
+    solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->SetInlet_FlowDir(iMarker, iVertex, 1, sin(alpha_rad));
+  }
 }
 
 /////////////////////////////////////////////////////////////////////////////////////////////////////////////////
-/* Functions related to simulation control, high level functions (reset convergence, set initial mesh, ecc...) */
+/* Functions related to simulation control, high level functions (reset convergence, set initial mesh, etc.)   */
 /////////////////////////////////////////////////////////////////////////////////////////////////////////////////
 
 void CDriver::ResetConvergence() {
-    
-    for(iZone = 0; iZone < nZone; iZone++) {
-        switch (config_container[iZone]->GetKind_Solver()) {
-                
-            case MAIN_SOLVER::EULER: case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::RANS:
-            case MAIN_SOLVER::INC_EULER: case MAIN_SOLVER::INC_NAVIER_STOKES: case MAIN_SOLVER::INC_RANS:
-            case MAIN_SOLVER::NEMO_EULER: case MAIN_SOLVER::NEMO_NAVIER_STOKES:
-                integration_container[iZone][INST_0][FLOW_SOL]->SetConvergence(false);
-                if (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::RANS) integration_container[iZone][INST_0][TURB_SOL]->SetConvergence(false);
-                if(config_container[iZone]->GetKind_Trans_Model() == TURB_TRANS_MODEL::LM) integration_container[iZone][INST_0][TRANS_SOL]->SetConvergence(false);
-                break;
-                
-            case MAIN_SOLVER::FEM_ELASTICITY:
-                integration_container[iZone][INST_0][FEA_SOL]->SetConvergence(false);
-                break;
-                
-            case MAIN_SOLVER::ADJ_EULER: case MAIN_SOLVER::ADJ_NAVIER_STOKES: case MAIN_SOLVER::ADJ_RANS: case MAIN_SOLVER::DISC_ADJ_EULER: case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_RANS:
-            case MAIN_SOLVER::DISC_ADJ_INC_EULER: case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_INC_RANS:
-                integration_container[iZone][INST_0][ADJFLOW_SOL]->SetConvergence(false);
-                if( (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::ADJ_RANS) || (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_RANS) )
-                    integration_container[iZone][INST_0][ADJTURB_SOL]->SetConvergence(false);
-                break;
-                
-            default:
-                break;
-        }
+  for (auto iZone = 0u; iZone < nZone; iZone++) {
+    switch (main_config->GetKind_Solver()) {
+      case MAIN_SOLVER::EULER:
+      case MAIN_SOLVER::NAVIER_STOKES:
+      case MAIN_SOLVER::RANS:
+      case MAIN_SOLVER::INC_EULER:
+      case MAIN_SOLVER::INC_NAVIER_STOKES:
+      case MAIN_SOLVER::INC_RANS:
+      case MAIN_SOLVER::NEMO_EULER:
+      case MAIN_SOLVER::NEMO_NAVIER_STOKES:
+        integration_container[iZone][INST_0][FLOW_SOL]->SetConvergence(false);
+        if (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::RANS)
+          integration_container[iZone][INST_0][TURB_SOL]->SetConvergence(false);
+        if (config_container[iZone]->GetKind_Trans_Model() == TURB_TRANS_MODEL::LM)
+          integration_container[iZone][INST_0][TRANS_SOL]->SetConvergence(false);
+        break;
+
+      case MAIN_SOLVER::FEM_ELASTICITY:
+        integration_container[iZone][INST_0][FEA_SOL]->SetConvergence(false);
+        break;
+
+      case MAIN_SOLVER::ADJ_EULER:
+      case MAIN_SOLVER::ADJ_NAVIER_STOKES:
+      case MAIN_SOLVER::ADJ_RANS:
+      case MAIN_SOLVER::DISC_ADJ_EULER:
+      case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES:
+      case MAIN_SOLVER::DISC_ADJ_RANS:
+      case MAIN_SOLVER::DISC_ADJ_INC_EULER:
+      case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES:
+      case MAIN_SOLVER::DISC_ADJ_INC_RANS:
+        integration_container[iZone][INST_0][ADJFLOW_SOL]->SetConvergence(false);
+        if ((config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::ADJ_RANS) ||
+            (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_RANS))
+          integration_container[iZone][INST_0][ADJTURB_SOL]->SetConvergence(false);
+        break;
+
+      default:
+        break;
     }
-    
+  }
 }
 
 void CSinglezoneDriver::SetInitialMesh() {
-    
-    DynamicMeshUpdate(0);
-    
-    SU2_OMP_PARALLEL {
-        // Overwrite fictious velocities
-        for (iMesh = 0u; iMesh <= config_container[ZONE_0]->GetnMGLevels(); iMesh++) {
-            SU2_OMP_FOR_STAT(roundUpDiv(geometry_container[ZONE_0][INST_0][iMesh]->GetnPoint(),omp_get_max_threads()))
-            for (unsigned long iPoint = 0; iPoint < geometry_container[ZONE_0][INST_0][iMesh]->GetnPoint(); iPoint++) {
-                
-                /*--- Overwrite fictitious velocities ---*/
-                su2double Grid_Vel[3] = {0.0, 0.0, 0.0};
-                
-                /*--- Set the grid velocity for this coarse node. ---*/
-                geometry_container[ZONE_0][INST_0][iMesh]->nodes->SetGridVel(iPoint, Grid_Vel);
-            }
-            END_SU2_OMP_FOR
-            /*--- Push back the volume. ---*/
-            geometry_container[ZONE_0][INST_0][iMesh]->nodes->SetVolume_n();
-            geometry_container[ZONE_0][INST_0][iMesh]->nodes->SetVolume_nM1();
-        }
-        /*--- Push back the solution so that there is no fictious velocity at the next step. ---*/
-        solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->Set_Solution_time_n();
-        solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->Set_Solution_time_n1();
-    }
-    END_SU2_OMP_PARALLEL
-}
-
-void CDriver::BoundaryConditionsUpdate(){
-    
-    int rank = MASTER_NODE;
-    unsigned short iZone;
-    
-    SU2_MPI::Comm_rank(SU2_MPI::GetComm(), &rank);
-    
-    if(rank == MASTER_NODE) cout << "Updating boundary conditions." << endl;
-    for(iZone = 0; iZone < nZone; iZone++){
-        geometry_container[iZone][INST_0][MESH_0]->UpdateCustomBoundaryConditions(geometry_container[iZone][INST_0], config_container[iZone]);
+  DynamicMeshUpdate(0);
+
+  SU2_OMP_PARALLEL {
+    for (iMesh = 0u; iMesh <= main_config->GetnMGLevels(); iMesh++) {
+      SU2_OMP_FOR_STAT(roundUpDiv(geometry_container[ZONE_0][INST_0][iMesh]->GetnPoint(), omp_get_max_threads()))
+      for (auto iPoint = 0ul; iPoint < geometry_container[ZONE_0][INST_0][iMesh]->GetnPoint(); iPoint++) {
+        /*--- Overwrite fictitious velocities. ---*/
+        su2double Grid_Vel[3] = {0.0, 0.0, 0.0};
+
+        /*--- Set the grid velocity for this coarse node. ---*/
+        geometry_container[ZONE_0][INST_0][iMesh]->nodes->SetGridVel(iPoint, Grid_Vel);
+      }
+      END_SU2_OMP_FOR
+      /*--- Push back the volume. ---*/
+      geometry_container[ZONE_0][INST_0][iMesh]->nodes->SetVolume_n();
+      geometry_container[ZONE_0][INST_0][iMesh]->nodes->SetVolume_nM1();
     }
+    /*--- Push back the solution so that there is no fictitious velocity at the next step. ---*/
+    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->Set_Solution_time_n();
+    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->Set_Solution_time_n1();
+  }
+  END_SU2_OMP_PARALLEL
+}
+
+void CDriver::BoundaryConditionsUpdate() {
+  int rank = MASTER_NODE;
+
+  SU2_MPI::Comm_rank(SU2_MPI::GetComm(), &rank);
+
+  if (rank == MASTER_NODE) cout << "Updating boundary conditions." << endl;
+  for (auto iZone = 0u; iZone < nZone; iZone++) {
+    geometry_container[iZone][INST_0][MESH_0]->UpdateCustomBoundaryConditions(geometry_container[iZone][INST_0],config_container[iZone]);
+  }
 }
 
 ////////////////////////////////////////////////////////////////////////////////
 /* Functions related to finite elements                                       */
 ////////////////////////////////////////////////////////////////////////////////
 
-void CDriver::SetFEA_Loads(unsigned short iMarker, unsigned long iVertex, passivedouble LoadX,
-                           passivedouble LoadY, passivedouble LoadZ) {
-    
-    unsigned long iPoint;
-    su2double NodalForce[3] = {0.0,0.0,0.0};
-    NodalForce[0] = LoadX;
-    NodalForce[1] = LoadY;
-    NodalForce[2] = LoadZ;
-    
-    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-    solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL]->GetNodes()->Set_FlowTraction(iPoint,NodalForce);
-    
+void CDriver::SetFEA_Loads(unsigned short iMarker, unsigned long iVertex, passivedouble LoadX, passivedouble LoadY,
+                           passivedouble LoadZ) {
+  unsigned long iPoint;
+  su2double NodalForce[3] = {0.0, 0.0, 0.0};
+  NodalForce[0] = LoadX;
+  NodalForce[1] = LoadY;
+  NodalForce[2] = LoadZ;
+
+  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+  solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL]->GetNodes()->Set_FlowTraction(iPoint, NodalForce);
 }
 
 vector<passivedouble> CDriver::GetFEA_Displacements(unsigned short iMarker, unsigned long iVertex) const {
-    
-    unsigned long iPoint;
-    vector<su2double> Displacements(3, 0.0);
-    vector<passivedouble> Displacements_passive(3, 0.0);
-    
-    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-    CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
-    CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-    
-    Displacements[0] = solver->GetNodes()->GetSolution(iPoint, 0);
-    Displacements[1] = solver->GetNodes()->GetSolution(iPoint, 1);
+  unsigned long iPoint;
+  vector<su2double> Displacements(3, 0.0);
+  vector<passivedouble> Displacements_passive(3, 0.0);
+
+  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
+  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+
+  Displacements[0] = solver->GetNodes()->GetSolution(iPoint, 0);
+  Displacements[1] = solver->GetNodes()->GetSolution(iPoint, 1);
+  if (geometry->GetnDim() == 3)
+    Displacements[2] = solver->GetNodes()->GetSolution(iPoint, 2);
+  else
+    Displacements[2] = 0.0;
+
+  Displacements_passive[0] = SU2_TYPE::GetValue(Displacements[0]);
+  Displacements_passive[1] = SU2_TYPE::GetValue(Displacements[1]);
+  Displacements_passive[2] = SU2_TYPE::GetValue(Displacements[2]);
+
+  return Displacements_passive;
+}
+
+vector<passivedouble> CDriver::GetFEA_Velocity(unsigned short iMarker, unsigned long iVertex) const {
+  unsigned long iPoint;
+  vector<su2double> Velocity(3, 0.0);
+  vector<passivedouble> Velocity_passive(3, 0.0);
+
+  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
+  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+
+  if (config_container[ZONE_0]->GetDynamic_Analysis() == DYNAMIC) {
+    Velocity[0] = solver->GetNodes()->GetSolution_Vel(iPoint, 0);
+    Velocity[1] = solver->GetNodes()->GetSolution_Vel(iPoint, 1);
     if (geometry->GetnDim() == 3)
-        Displacements[2] = solver->GetNodes()->GetSolution(iPoint, 2);
+      Velocity[2] = solver->GetNodes()->GetSolution_Vel(iPoint, 2);
     else
-        Displacements[2] = 0.0;
-    
-    Displacements_passive[0] = SU2_TYPE::GetValue(Displacements[0]);
-    Displacements_passive[1] = SU2_TYPE::GetValue(Displacements[1]);
-    Displacements_passive[2] = SU2_TYPE::GetValue(Displacements[2]);
-    
-    return Displacements_passive;
-}
+      Velocity[2] = 0.0;
+  }
 
+  Velocity_passive[0] = SU2_TYPE::GetValue(Velocity[0]);
+  Velocity_passive[1] = SU2_TYPE::GetValue(Velocity[1]);
+  Velocity_passive[2] = SU2_TYPE::GetValue(Velocity[2]);
 
-vector<passivedouble> CDriver::GetFEA_Velocity(unsigned short iMarker, unsigned long iVertex) const {
-    
-    unsigned long iPoint;
-    vector<su2double> Velocity(3, 0.0);
-    vector<passivedouble> Velocity_passive(3,0.0);
-    
-    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-    CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
-    CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-    
-    if (config_container[ZONE_0]->GetDynamic_Analysis() == DYNAMIC){
-        Velocity[0] = solver->GetNodes()->GetSolution_Vel(iPoint, 0);
-        Velocity[1] = solver->GetNodes()->GetSolution_Vel(iPoint, 1);
-        if (geometry->GetnDim() == 3)
-            Velocity[2] = solver->GetNodes()->GetSolution_Vel(iPoint, 2);
-        else
-            Velocity[2] = 0.0;
-    }
-    
-    Velocity_passive[0] = SU2_TYPE::GetValue(Velocity[0]);
-    Velocity_passive[1] = SU2_TYPE::GetValue(Velocity[1]);
-    Velocity_passive[2] = SU2_TYPE::GetValue(Velocity[2]);
-    
-    return Velocity_passive;
+  return Velocity_passive;
 }
 
 vector<passivedouble> CDriver::GetFEA_Velocity_n(unsigned short iMarker, unsigned long iVertex) const {
-    
-    unsigned long iPoint;
-    vector<su2double> Velocity_n(3, 0.0);
-    vector<passivedouble> Velocity_n_passive(3, 0.0);
-    
-    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-    CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
-    CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-    
-    if (config_container[ZONE_0]->GetDynamic_Analysis() == DYNAMIC){
-        Velocity_n[0] = solver->GetNodes()->GetSolution_Vel_time_n(iPoint, 0);
-        Velocity_n[1] = solver->GetNodes()->GetSolution_Vel_time_n(iPoint, 1);
-        if (geometry->GetnDim() == 3)
-            Velocity_n[2] = solver->GetNodes()->GetSolution_Vel_time_n(iPoint, 2);
-        else
-            Velocity_n[2] = 0.0;
-    }
-    
-    Velocity_n_passive[0] = SU2_TYPE::GetValue(Velocity_n[0]);
-    Velocity_n_passive[1] = SU2_TYPE::GetValue(Velocity_n[1]);
-    Velocity_n_passive[2] = SU2_TYPE::GetValue(Velocity_n[2]);
-    
-    return Velocity_n_passive;
-    
+  unsigned long iPoint;
+  vector<su2double> Velocity_n(3, 0.0);
+  vector<passivedouble> Velocity_n_passive(3, 0.0);
+
+  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
+  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+
+  if (config_container[ZONE_0]->GetDynamic_Analysis() == DYNAMIC) {
+    Velocity_n[0] = solver->GetNodes()->GetSolution_Vel_time_n(iPoint, 0);
+    Velocity_n[1] = solver->GetNodes()->GetSolution_Vel_time_n(iPoint, 1);
+    if (geometry->GetnDim() == 3)
+      Velocity_n[2] = solver->GetNodes()->GetSolution_Vel_time_n(iPoint, 2);
+    else
+      Velocity_n[2] = 0.0;
+  }
+
+  Velocity_n_passive[0] = SU2_TYPE::GetValue(Velocity_n[0]);
+  Velocity_n_passive[1] = SU2_TYPE::GetValue(Velocity_n[1]);
+  Velocity_n_passive[2] = SU2_TYPE::GetValue(Velocity_n[2]);
+
+  return Velocity_n_passive;
 }
 
 ////////////////////////////////////////////////////////////////////////////////
@@ -558,123 +523,108 @@ vector<passivedouble> CDriver::GetFEA_Velocity_n(unsigned short iMarker, unsigne
 ////////////////////////////////////////////////////////////////////////////////
 
 vector<passivedouble> CDriver::GetMeshDisp_Sensitivity(unsigned short iMarker, unsigned long iVertex) const {
-    
-    unsigned long iPoint;
-    vector<su2double> Disp_Sens(3, 0.0);
-    vector<passivedouble> Disp_Sens_passive(3, 0.0);
-    
-    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-    CSolver *solver =  solver_container[ZONE_0][INST_0][MESH_0][ADJMESH_SOL];
-    CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-    
-    Disp_Sens[0] = solver->GetNodes()->GetBoundDisp_Sens(iPoint, 0);
-    Disp_Sens[1] = solver->GetNodes()->GetBoundDisp_Sens(iPoint, 1);
-    if (geometry->GetnDim() == 3)
-        Disp_Sens[2] = solver->GetNodes()->GetBoundDisp_Sens(iPoint, 2);
-    else
-        Disp_Sens[2] = 0.0;
-    
-    Disp_Sens_passive[0] = SU2_TYPE::GetValue(Disp_Sens[0]);
-    Disp_Sens_passive[1] = SU2_TYPE::GetValue(Disp_Sens[1]);
-    Disp_Sens_passive[2] = SU2_TYPE::GetValue(Disp_Sens[2]);
-    
-    return Disp_Sens_passive;
-    
+  unsigned long iPoint;
+  vector<su2double> Disp_Sens(3, 0.0);
+  vector<passivedouble> Disp_Sens_passive(3, 0.0);
+
+  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][ADJMESH_SOL];
+  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+
+  Disp_Sens[0] = solver->GetNodes()->GetBoundDisp_Sens(iPoint, 0);
+  Disp_Sens[1] = solver->GetNodes()->GetBoundDisp_Sens(iPoint, 1);
+  if (geometry->GetnDim() == 3)
+    Disp_Sens[2] = solver->GetNodes()->GetBoundDisp_Sens(iPoint, 2);
+  else
+    Disp_Sens[2] = 0.0;
+
+  Disp_Sens_passive[0] = SU2_TYPE::GetValue(Disp_Sens[0]);
+  Disp_Sens_passive[1] = SU2_TYPE::GetValue(Disp_Sens[1]);
+  Disp_Sens_passive[2] = SU2_TYPE::GetValue(Disp_Sens[2]);
+
+  return Disp_Sens_passive;
 }
 
 vector<passivedouble> CDriver::GetFlowLoad_Sensitivity(unsigned short iMarker, unsigned long iVertex) const {
-    
-    unsigned long iPoint;
-    vector<su2double> FlowLoad_Sens(3, 0.0);
-    vector<passivedouble> FlowLoad_Sens_passive(3, 0.0);
-    
-    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-    CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
-    CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-    
-    FlowLoad_Sens[0] = solver->GetNodes()->GetFlowTractionSensitivity(iPoint, 0);
-    FlowLoad_Sens[1] = solver->GetNodes()->GetFlowTractionSensitivity(iPoint, 1);
-    if (geometry->GetnDim() == 3)
-        FlowLoad_Sens[2] = solver->GetNodes()->GetFlowTractionSensitivity(iPoint, 2);
-    else
-        FlowLoad_Sens[2] = 0.0;
-    
-    FlowLoad_Sens_passive[0] = SU2_TYPE::GetValue(FlowLoad_Sens[0]);
-    FlowLoad_Sens_passive[1] = SU2_TYPE::GetValue(FlowLoad_Sens[1]);
-    FlowLoad_Sens_passive[2] = SU2_TYPE::GetValue(FlowLoad_Sens[2]);
-    
-    return FlowLoad_Sens_passive;
-    
+  unsigned long iPoint;
+  vector<su2double> FlowLoad_Sens(3, 0.0);
+  vector<passivedouble> FlowLoad_Sens_passive(3, 0.0);
+
+  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
+  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+
+  FlowLoad_Sens[0] = solver->GetNodes()->GetFlowTractionSensitivity(iPoint, 0);
+  FlowLoad_Sens[1] = solver->GetNodes()->GetFlowTractionSensitivity(iPoint, 1);
+  if (geometry->GetnDim() == 3)
+    FlowLoad_Sens[2] = solver->GetNodes()->GetFlowTractionSensitivity(iPoint, 2);
+  else
+    FlowLoad_Sens[2] = 0.0;
+
+  FlowLoad_Sens_passive[0] = SU2_TYPE::GetValue(FlowLoad_Sens[0]);
+  FlowLoad_Sens_passive[1] = SU2_TYPE::GetValue(FlowLoad_Sens[1]);
+  FlowLoad_Sens_passive[2] = SU2_TYPE::GetValue(FlowLoad_Sens[2]);
+
+  return FlowLoad_Sens_passive;
 }
 
 void CDriver::SetFlowLoad_Adjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
                                   passivedouble val_AdjointY, passivedouble val_AdjointZ) {
-    
-    CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL];
-    CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-    
-    solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 0, val_AdjointX);
-    solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 1, val_AdjointY);
-    if (geometry->GetnDim() == 3)
-        solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 2, val_AdjointZ);
-    
+  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL];
+  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+
+  solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 0, val_AdjointX);
+  solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 1, val_AdjointY);
+  if (geometry->GetnDim() == 3) solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 2, val_AdjointZ);
 }
 
 void CDriver::SetSourceTerm_DispAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
                                         passivedouble val_AdjointY, passivedouble val_AdjointZ) {
-    
-    unsigned long iPoint;
-    
-    CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
-    CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-    
-    solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 0, val_AdjointX);
-    solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 1, val_AdjointY);
-    if (geometry->GetnDim() == 3)
-        solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 2, val_AdjointZ);
-    
+  unsigned long iPoint;
+
+  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
+  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+
+  solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 0, val_AdjointX);
+  solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 1, val_AdjointY);
+  if (geometry->GetnDim() == 3) solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 2, val_AdjointZ);
 }
 
 void CDriver::SetSourceTerm_VelAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
                                        passivedouble val_AdjointY, passivedouble val_AdjointZ) {
-    
-    CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
-    CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-    const auto iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-    
-    solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 0, val_AdjointX);
-    solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 1, val_AdjointY);
-    if (geometry->GetnDim() == 3)
-        solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 2, val_AdjointZ);
-    
+  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
+  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+  const auto iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+
+  solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 0, val_AdjointX);
+  solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 1, val_AdjointY);
+  if (geometry->GetnDim() == 3) solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 2, val_AdjointZ);
 }
 
 ////////////////////////////////////////////////////////////////////////////////
-/* Functions related to flow loads */
+/* Functions related to flow loads                                             */
 ////////////////////////////////////////////////////////////////////////////////
 
 vector<passivedouble> CDriver::GetFlowLoad(unsigned short iMarker, unsigned long iVertex) const {
-    
-    vector<su2double> FlowLoad(3, 0.0);
-    vector<passivedouble> FlowLoad_passive(3, 0.0);
-    
-    CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL];
-    CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-    
-    if (config_container[ZONE_0]->GetSolid_Wall(iMarker)) {
-        FlowLoad[0] = solver->GetVertexTractions(iMarker, iVertex, 0);
-        FlowLoad[1] = solver->GetVertexTractions(iMarker, iVertex, 1);
-        if (geometry->GetnDim() == 3)
-            FlowLoad[2] = solver->GetVertexTractions(iMarker, iVertex, 2);
-        else
-            FlowLoad[2] = 0.0;
-    }
-    
-    FlowLoad_passive[0] = SU2_TYPE::GetValue(FlowLoad[0]);
-    FlowLoad_passive[1] = SU2_TYPE::GetValue(FlowLoad[1]);
-    FlowLoad_passive[2] = SU2_TYPE::GetValue(FlowLoad[2]);
-    
-    return FlowLoad_passive;
-    
+  vector<su2double> FlowLoad(3, 0.0);
+  vector<passivedouble> FlowLoad_passive(3, 0.0);
+
+  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL];
+  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+
+  if (config_container[ZONE_0]->GetSolid_Wall(iMarker)) {
+    FlowLoad[0] = solver->GetVertexTractions(iMarker, iVertex, 0);
+    FlowLoad[1] = solver->GetVertexTractions(iMarker, iVertex, 1);
+    if (geometry->GetnDim() == 3)
+      FlowLoad[2] = solver->GetVertexTractions(iMarker, iVertex, 2);
+    else
+      FlowLoad[2] = 0.0;
+  }
+
+  FlowLoad_passive[0] = SU2_TYPE::GetValue(FlowLoad[0]);
+  FlowLoad_passive[1] = SU2_TYPE::GetValue(FlowLoad[1]);
+  FlowLoad_passive[2] = SU2_TYPE::GetValue(FlowLoad[2]);
+
+  return FlowLoad_passive;
 }

From bf07e5b18fbfb0e2934f252eb205647d2f12b8e8 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Wed, 28 Dec 2022 16:53:55 -0800
Subject: [PATCH 099/656] Update SU2 version number

---
 SU2_CFD/include/drivers/CDriverBase.hpp               | 2 +-
 SU2_CFD/src/drivers/CDriverBase.cpp                   | 2 +-
 SU2_DEF/include/drivers/CDeformationDriver.hpp        | 2 +-
 SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp | 2 +-
 SU2_DEF/src/drivers/CDeformationDriver.cpp            | 2 +-
 SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp     | 2 +-
 TestCases/nicf/coolprop/fluidModel.cfg                | 2 +-
 TestCases/nicf/coolprop/transportModel.cfg            | 2 +-
 8 files changed, 8 insertions(+), 8 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index cec1a78c58a..a2d138760ff 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -2,7 +2,7 @@
  * \file CDriverBase.hpp
  * \brief Base class template for all drivers.
  * \author H. Patel, A. Gastaldi
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index 4009c76fa26..fcac9907521 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -2,7 +2,7 @@
  * \file CDriverBase.hpp
  * \brief Base class template for all drivers.
  * \author H. Patel, A. Gastaldi
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index 62954de5b73..9e6fee12097 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -2,7 +2,7 @@
  * \file CDeformationDriver.hpp
  * \brief Headers of the main subroutines for driving the mesh deformation.
  * \author A. Gastaldi, H. Patel
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
index d5b42b958e5..0760513ed05 100644
--- a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjDeformationDriver.cpp
  * \brief Headers of the main subroutines for driving the projection of sensitivities.
  * \author T. Economon, H. Kline, R. Sanchez, A. Gastaldi, H. Patel
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 6140f4526a9..99ed2dab30a 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -2,7 +2,7 @@
  * \file CDeformationDriver.cpp
  * \brief Main subroutines for driving the mesh deformation.
  * \author A. Gastaldi, H. Patel
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index 9e55a74c11a..0b01614eec5 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjDeformationDriver.cpp
  * \brief Main subroutines for driving the projection of sensitivities.
  * \author T. Economon, H. Kline, R. Sanchez, A. Gastaldi, H. Patel
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/TestCases/nicf/coolprop/fluidModel.cfg b/TestCases/nicf/coolprop/fluidModel.cfg
index 6b2fb858bc6..44df7a39118 100644
--- a/TestCases/nicf/coolprop/fluidModel.cfg
+++ b/TestCases/nicf/coolprop/fluidModel.cfg
@@ -6,7 +6,7 @@
 % Author: Peng Yan, Alberto Guardone                                           %
 % Institution: Politecnico di Milano                                           %
 % Date: 2022.10.8                                                              %
-% File Version  7.4.0 Blackbird                                                %
+% File Version  7.5.0 Blackbird                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nicf/coolprop/transportModel.cfg b/TestCases/nicf/coolprop/transportModel.cfg
index b4b1d9c4906..491073a2734 100644
--- a/TestCases/nicf/coolprop/transportModel.cfg
+++ b/TestCases/nicf/coolprop/transportModel.cfg
@@ -6,7 +6,7 @@
 % Author: Peng Yan, Alberto Guardone                                           %
 % Institution: Politecnico di Milano                                           %
 % Date: 2022.11.26                                                             %
-% File Version  7.4.0 Blackbird                                                %
+% File Version  7.5.0 Blackbird                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 

From adecd156f32a2948832c6d962e56d494a0d0a052 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Wed, 28 Dec 2022 18:27:25 -0800
Subject: [PATCH 100/656] Remove ENABLE_MAPS from header files

---
 SU2_DEF/include/SU2_DEF.hpp                           | 10 +++-------
 SU2_DEF/include/drivers/CDeformationDriver.hpp        |  3 ---
 SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp |  3 ---
 SU2_DOT/include/SU2_DOT.hpp                           |  5 +----
 4 files changed, 4 insertions(+), 17 deletions(-)

diff --git a/SU2_DEF/include/SU2_DEF.hpp b/SU2_DEF/include/SU2_DEF.hpp
index a3aaada5218..c851b1d35d1 100644
--- a/SU2_DEF/include/SU2_DEF.hpp
+++ b/SU2_DEF/include/SU2_DEF.hpp
@@ -27,18 +27,14 @@
 
 #pragma once
 
-#include "../../Common/include/parallelization/mpi_structure.hpp"
-#include "../../Common/include/parallelization/omp_structure.hpp"
-
-#define ENABLE_MAPS
-#include "../../Common/include/CConfig.hpp"
-#undef ENABLE_MAPS
-
 #include <cmath>
 #include <cstdlib>
 #include <iomanip>
 #include <iostream>
 
+#include "../../Common/include/CConfig.hpp"
+#include "../../Common/include/parallelization/mpi_structure.hpp"
+#include "../../Common/include/parallelization/omp_structure.hpp"
 #include "drivers/CDeformationDriver.hpp"
 
 using namespace std;
diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index 9e6fee12097..01eecee0df5 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -27,10 +27,7 @@
 
 #pragma once
 
-#define ENABLE_MAPS
 #include "../../../Common/include/CConfig.hpp"
-#undef ENABLE_MAPS
-
 #include "../../../Common/include/geometry/CGeometry.hpp"
 #include "../../../Common/include/grid_movement/CSurfaceMovement.hpp"
 #include "../../../Common/include/grid_movement/CVolumetricMovement.hpp"
diff --git a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
index 0760513ed05..998b89fbe1b 100644
--- a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
@@ -27,10 +27,7 @@
 
 #pragma once
 
-#define ENABLE_MAPS
 #include "../../../Common/include/CConfig.hpp"
-#undef ENABLE_MAPS
-
 #include "../../../Common/include/fem/fem_geometry_structure.hpp"
 #include "../../../Common/include/geometry/CGeometry.hpp"
 #include "../../../Common/include/grid_movement/CSurfaceMovement.hpp"
diff --git a/SU2_DOT/include/SU2_DOT.hpp b/SU2_DOT/include/SU2_DOT.hpp
index 8b918e52abd..77f39c7085e 100644
--- a/SU2_DOT/include/SU2_DOT.hpp
+++ b/SU2_DOT/include/SU2_DOT.hpp
@@ -27,15 +27,12 @@
 
 #pragma once
 
-#define ENABLE_MAPS
-#include "../../Common/include/CConfig.hpp"
-#undef ENABLE_MAPS
-
 #include <cmath>
 #include <cstdlib>
 #include <iomanip>
 #include <iostream>
 
+#include "../../Common/include/CConfig.hpp"
 #include "../../Common/include/parallelization/mpi_structure.hpp"
 #include "../../Common/include/parallelization/omp_structure.hpp"
 #include "../../SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp"

From 4353a260a68413ef1f3f2068120e5eb1768b1cbf Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Thu, 29 Dec 2022 18:44:14 -0800
Subject: [PATCH 101/656] Update function names in CDriverBase, fix variable
 designations

---
 SU2_CFD/include/drivers/CDriverBase.hpp | 203 ++++++++++++------------
 SU2_CFD/src/drivers/CDriverBase.cpp     | 150 ++++++++---------
 2 files changed, 180 insertions(+), 173 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index a2d138760ff..6ff1781eb09 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -1,6 +1,6 @@
 /*!
  * \file CDriverBase.hpp
- * \brief Base class template for all drivers.
+ * \brief Base class for all drivers.
  * \author H. Patel, A. Gastaldi
  * \version 7.5.0 "Blackbird"
  *
@@ -32,6 +32,13 @@
 #include "../output/COutput.hpp"
 #include "../solvers/CSolver.hpp"
 
+/*!
+ * \class CDriverBase
+ * \ingroup Drivers
+ * \brief Base class for all drivers.
+ * \author H. Patel, A. Gastaldi
+ */
+
 class CDriverBase {
  protected:
   int rank,               /*!< \brief MPI Rank. */
@@ -177,147 +184,147 @@ class CDriverBase {
   unsigned long GetNumberMarkerElements(unsigned short iMarker) const;
 
   /*!
-   * \brief Get the global IDs of the mesh elements.
-   * \return Global element IDs.
+   * \brief Get the global indices of the mesh elements.
+   * \return Global element indices (nElem).
    */
-  vector<unsigned long> GetElementIDs() const;
+  vector<unsigned long> GetElements() const;
 
   /*!
-   * \brief Get the global ID of a mesh element.
+   * \brief Get the global index of a mesh element.
    * \param[in] iElem - Mesh element index.
-   * \return Global element ID.
+   * \return Global element index.
    */
-  unsigned long GetElementIDs(unsigned long iElem) const;
+  unsigned long GetElements(unsigned long iElem) const;
 
   /*!
-   * \brief Get the global IDs of the marker elements.
+   * \brief Get the global indices of the marker elements.
    * \param[in] iMarker - Marker index.
-   * \return Global element IDs.
+   * \return Global element indices (nElem).
    */
-  vector<unsigned long> GetMarkerElementIDs(unsigned short iMarker) const;
+  vector<unsigned long> GetMarkerElements(unsigned short iMarker) const;
 
   /*!
-   * \brief Get the global IDs of a marker element.
+   * \brief Get the global index of a marker element.
    * \param[in] iMarker - Marker index.
-   * \param[in] iBound - Marker element index.
-   * \return Global element ID.
+   * \param[in] iElem - Marker element index.
+   * \return Global element index.
    */
-  unsigned long GetMarkerElementIDs(unsigned short iMarker, unsigned long iBound) const;
+  unsigned long GetMarkerElements(unsigned short iMarker, unsigned long iElem) const;
 
   /*!
-   * \brief Get the table of vertex IDs belonging to the mesh elements.
-   * \return Element connectivities (nElem, nNode)
+   * \brief Get the global node indices of the mesh elements.
+   * \return Element global node indices (nElem, nNode).
    */
-  vector<vector<unsigned long>> GetElementConnectivities() const;
+  vector<vector<unsigned long>> GetElementNodes() const;
 
   /*!
-   * \brief Get the row of vertex IDs belonging to a mesh element.
+   * \brief Get the global node indices of a mesh element.
    * \param[in] iElem - Mesh element index.
-   * \return Element connectivity (nNode)
+   * \return Element global node indices (nNode).
    */
-  vector<unsigned long> GetElementConnectivities(unsigned long iElem) const;
+  vector<unsigned long> GetElementNodes(unsigned long iElem) const;
 
   /*!
-   * \brief Get the table of vertex IDs belonging to the marker elements.
+   * \brief Get the global node indices of the marker elements.
    * \param[in] iMarker - Marker index.
-   * \return Element connectivities (nBound, nNode).
+   * \return Element global node indices (nElem, nVertex).
    */
-  vector<vector<unsigned long>> GetMarkerElementConnectivities(unsigned short iMarker) const;
+  vector<vector<unsigned long>> GetMarkerElementNodes(unsigned short iMarker) const;
 
   /*!
-   * \brief Get the row of vertex IDs belonging to a marker element.
+   * \brief Get the global node indices of a marker element.
    * \param[in] iMarker - Marker index.
-   * \param[in] iBound - Marker element index.
-   * \return Element connectivity (nNode).
+   * \param[in] iElem - Marker element index.
+   * \return Element global node indices (nVertex).
    */
-  vector<unsigned long> GetMarkerElementConnectivities(unsigned short iMarker, unsigned long iBound) const;
+  vector<unsigned long> GetMarkerElementNodes(unsigned short iMarker, unsigned long iElem) const;
 
   /*!
-   * \brief Get the number of vertices in the mesh.
-   * \return Number of vertices.
+   * \brief Get the number of nodes in the mesh.
+   * \return Number of nodes.
    */
-  unsigned long GetNumberVertices() const;
+  unsigned long GetNumberNodes() const;
 
   /*!
-   * \brief Get the number of vertices in the marker.
+   * \brief Get the number of nodes in the marker.
    * \param[in] iMarker - Marker index.
-   * \return Number of vertices.
+   * \return Number of nodes.
    */
-  unsigned long GetNumberMarkerVertices(unsigned short iMarker) const;
+  unsigned long GetNumberMarkerNodes(unsigned short iMarker) const;
 
   /*!
-   * \brief Get the number of halo vertices in the mesh.
-   * \return Number of vertices.
+   * \brief Get the number of halo nodes in the mesh.
+   * \return Number of halo nodes.
    */
-  unsigned long GetNumberHaloVertices() const;
+  unsigned long GetNumberHaloNodes() const;
 
   /*!
-   * \brief Get the number of halo vertices in the marker.
+   * \brief Get the number of halo nodes in the marker.
    * \param[in] iMarker - Marker index.
-   * \return Number of vertices.
+   * \return Number of halo nodes.
    */
-  unsigned long GetNumberMarkerHaloVertices(unsigned short iMarker) const;
+  unsigned long GetNumberMarkerHaloNodes(unsigned short iMarker) const;
 
   /*!
-   * \brief Get the mesh vertex indices of the marker vertices.
+   * \brief Get the vertices of the marker.
    * \param[in] iMarker - Marker index.
-   * \return Mesh vertex indices.
+   * \return Marker vertices (nVertex).
    */
-  vector<unsigned long> GetMarkerVertexIndices(unsigned short iMarker) const;
+  vector<unsigned long> GetMarkerVertices(unsigned short iMarker) const;
 
   /*!
-   * \brief Get the mesh vertex index of a marker vertex.
+   * \brief Get the vertex of a marker.
    * \param[in] iMarker - Marker index.
    * \param[in] iVertex - Marker vertex index.
-   * \return Mesh vertex index.
+   * \return Marker vertex.
    */
-  unsigned long GetMarkerVertexIndices(unsigned short iMarker, unsigned long iVertex) const;
+  unsigned long GetMarkerVertices(unsigned short iMarker, unsigned long iVertex) const;
 
   /*!
-   * \brief Get the global IDs of the mesh vertices.
-   * \return Global vertex IDs.
+   * \brief Get the global node indices.
+   * \return Global node indices (nNode).
    */
-  vector<unsigned long> GetVertexIDs() const;
+  vector<unsigned long> GetNodes() const;
 
   /*!
-   * \brief Get the global ID of a mesh vertex.
-   * \param[in] iPoint - Mesh vertex index.
-   * \return Global vertex ID.
+   * \brief Get the global node index.
+   * \param[in] iPoint - Mesh node index.
+   * \return Global node index.
    */
-  unsigned long GetVertexIDs(unsigned long iPoint) const;
+  unsigned long GetNodes(unsigned long iPoint) const;
 
   /*!
-   * \brief Get the global IDs of the marker vertices.
+   * \brief Get the global node indices of the marker vertices.
    * \param[in] iMarker - Marker index.
-   * \return Global vertex IDs.
+   * \return Global node indices (nVertex).
    */
-  vector<unsigned long> GetMarkerVertexIDs(unsigned short iMarker) const;
+  vector<unsigned long> GetMarkerNodes(unsigned short iMarker) const;
 
   /*!
-   * \brief Get the global ID of a marker vertex.
+   * \brief Get the global node index of a marker vertex.
    * \param[in] iMarker - Marker index.
    * \param[in] iVertex - Marker vertex index.
-   * \return Global vertex ID.
+   * \return Global node index.
    */
-  unsigned long GetMarkerVertexIDs(unsigned short iMarker, unsigned long iVertex) const;
+  unsigned long GetMarkerNodes(unsigned short iMarker, unsigned long iVertex) const;
 
   /*!
-   * \brief Get the halo flags of the mesh vertices.
-   * \return Vertex domain flags.
+   * \brief Get the halo flags of the mesh nodes.
+   * \return Node domain flags (nNode).
    */
   vector<bool> GetDomain() const;
 
   /*!
-   * \brief Get the halo flag of a mesh vertex.
-   * \param[in] iPoint - Mesh vertex index.
-   * \return Vertex domain flag.
+   * \brief Get the halo flag of a mesh node.
+   * \param[in] iPoint - Mesh node index.
+   * \return Node domain flag.
    */
   bool GetDomain(unsigned long iPoint) const;
 
   /*!
    * \brief Get the halo flags of the marker vertices.
    * \param[in] iMarker - Marker index.
-   * \return Vertex domain flags.
+   * \return Domain flags (nVertex).
    */
   vector<bool> GetMarkerDomain(unsigned short iMarker) const;
 
@@ -325,27 +332,27 @@ class CDriverBase {
    * \brief Get the halo flag of a marker vertex.
    * \param[in] iMarker - Marker index.
    * \param[in] iVertex - Marker vertex index.
-   * \return Vertex domain flag.
+   * \return Domain flag.
    */
   bool GetMarkerDomain(unsigned short iMarker, unsigned long iVertex) const;
 
   /*!
-   * \brief Get the initial (un-deformed) coordinates of the mesh vertices.
-   * \return Initial vertex coordinates (nPoint, nDim).
+   * \brief Get the initial (un-deformed) coordinates of the mesh nodes.
+   * \return Initial node coordinates (nNode, nDim).
    */
   vector<vector<passivedouble>> GetInitialCoordinates() const;
 
   /*!
-   * \brief Get the initial (un-deformed) coordinates of a mesh vertex.
-   * \param[in] iPoint - Mesh vertex index.
-   * \return Initial vertex coordinates (nDim).
+   * \brief Get the initial (un-deformed) coordinates of a mesh node.
+   * \param[in] iPoint - Mesh node index.
+   * \return Initial node coordinates (nDim).
    */
   vector<passivedouble> GetInitialCoordinates(unsigned long iPoint) const;
 
   /*!
    * \brief Get the initial (un-deformed) coordinates of the marker vertices.
    * \param[in] iMarker - Marker index.
-   * \return Initial vertex coordinates (nVertex, nDim).
+   * \return Initial node coordinates (nVertex, nDim).
    */
   vector<vector<passivedouble>> GetMarkerInitialCoordinates(unsigned short iMarker) const;
 
@@ -353,27 +360,27 @@ class CDriverBase {
    * \brief Get the initial (un-deformed) coordinates of a marker vertex.
    * \param[in] iMarker - Marker index.
    * \param[in] iVertex - Marker vertex index.
-   * \return Initial vertex coordinates (nDim).
+   * \return Initial node coordinates (nDim).
    */
   vector<passivedouble> GetMarkerInitialCoordinates(unsigned short iMarker, unsigned long iVertex) const;
 
   /*!
-   * \brief Get the coordinates of the mesh vertices.
-   * \return Vertex coordinates (nPoint, nDim).
+   * \brief Get the coordinates of the mesh nodes.
+   * \return Node coordinates (nNode, nDim).
    */
   vector<vector<passivedouble>> GetCoordinates() const;
 
   /*!
-   * \brief Get the coordinates of a mesh vertex.
-   * \param[in] iPoint - Mesh vertex index.
-   * \return Vertex coordinates (nDim).
+   * \brief Get the coordinates of a mesh node.
+   * \param[in] iPoint - Mesh node index.
+   * \return Node coordinates (nDim).
    */
   vector<passivedouble> GetCoordinates(unsigned long iPoint) const;
 
   /*!
    * \brief Get the coordinates of the marker vertices.
    * \param[in] iMarker - Marker index.
-   * \return Vertex coordinates (nVertex, nDim).
+   * \return Node coordinates (nVertex, nDim).
    */
   vector<vector<passivedouble>> GetMarkerCoordinates(unsigned short iMarker) const;
 
@@ -381,27 +388,27 @@ class CDriverBase {
    * \brief Get the coordinates of a marker vertex.
    * \param[in] iMarker - Marker index.
    * \param[in] iVertex - Marker vertex index.
-   * \return Vertex coordinates (nDim).
+   * \return Node coordinates (nDim).
    */
   vector<passivedouble> GetMarkerCoordinates(unsigned short iMarker, unsigned long iVertex) const;
 
   /*!
-   * \brief Set the coordinates of the mesh vertices.
-   * \param[in] values - Vertex coordinates (nPoint, nDim).
+   * \brief Set the coordinates of the mesh nodes.
+   * \param[in] values - Node coordinates (nNode, nDim).
    */
   void SetCoordinates(vector<vector<passivedouble>> values);
 
   /*!
-   * \brief Set the coordinates of a mesh vertex.
-   * \param[in] iPoint - Mesh vertex index.
-   * \param[in] values - Vertex coordinates (nDim).
+   * \brief Set the coordinates of a mesh node.
+   * \param[in] iPoint - Mesh node index.
+   * \param[in] values - Node coordinates (nDim).
    */
   void SetCoordinates(unsigned long iPoint, vector<passivedouble> values);
 
   /*!
    * \brief Set the coordinates of the marker vertices.
    * \param[in] iMarker - Marker index.
-   * \param[in] values - Vertex coordinates (nVertex, nDim).
+   * \param[in] values - Node coordinates (nVertex, nDim).
    */
   void SetMarkerCoordinates(unsigned short iMarker, vector<vector<passivedouble>> values);
 
@@ -409,14 +416,14 @@ class CDriverBase {
    * \brief Set the coordinates of a marker vertex.
    * \param[in] iMarker - Marker index.
    * \param[in] iVertex - Marker vertex index.
-   * \param[in] values - Vertex coordinates (nDim).
+   * \param[in] values - Node coordinates (nDim).
    */
   void SetMarkerCoordinates(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values);
 
   /*!
    * \brief Get the displacements of the marker vertices.
    * \param[in] iMarker - Marker index.
-   * \return Vertex displacements (nVertex, nDim).
+   * \return Node displacements (nVertex, nDim).
    */
   vector<vector<passivedouble>> GetMarkerDisplacements(unsigned short iMarker) const;
 
@@ -424,14 +431,14 @@ class CDriverBase {
    * \brief Get the displacements of a marker vertex.
    * \param[in] iMarker - Marker index.
    * \param[in] iVertex - Marker vertex index.
-   * \return Vertex displacements (nDim).
+   * \return Node displacements (nDim).
    */
   vector<passivedouble> GetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex) const;
 
   /*!
    * \brief Set the displacements of the marker vertices.
    * \param[in] iMarker - Marker index.
-   * \param[in] values - Vertex displacements (nVertex, nDim).
+   * \param[in] values - Node displacements (nVertex, nDim).
    */
   void SetMarkerDisplacements(unsigned short iMarker, vector<vector<passivedouble>> values);
 
@@ -439,14 +446,14 @@ class CDriverBase {
    * \brief Set the displacements of a marker vertex.
    * \param[in] iMarker - Marker index.
    * \param[in] iVertex - Marker vertex index.
-   * \param[in] values - Vertex displacements (nDim).
+   * \param[in] values - Node displacements (nDim).
    */
   void SetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values);
 
   /*!
    * \brief Get the velocities of the marker vertices.
    * \param[in] iMarker - Marker index.
-   * \return Vertex velocities (nVertex, nDim).
+   * \return Node velocities (nVertex, nDim).
    */
   vector<vector<passivedouble>> GetMarkerVelocities(unsigned short iMarker) const;
 
@@ -454,14 +461,14 @@ class CDriverBase {
    * \brief Get the velocities of a marker vertex.
    * \param[in] iMarker - Marker index.
    * \param[in] iVertex - Marker vertex index.
-   * \return Vertex velocities (nDim).
+   * \return Node velocities (nDim).
    */
   vector<passivedouble> GetMarkerVelocities(unsigned short iMarker, unsigned long iVertex) const;
 
   /*!
    * \brief Set the velocities of the marker vertices.
    * \param[in] iMarker - Marker index.
-   * \param[in] values - Vertex velocities (nVertex, nDim).
+   * \param[in] values - Node velocities (nVertex, nDim).
    */
   void SetMarkerVelocities(unsigned short iMarker, vector<vector<passivedouble>> values);
 
@@ -469,24 +476,24 @@ class CDriverBase {
    * \brief Set the velocities of a marker vertex.
    * \param[in] iMarker - Marker index.
    * \param[in] iVertex - Marker vertex index.
-   * \param[in] values - Vertex velocities (nDim).
+   * \param[in] values - Node velocities (nDim).
    */
   void SetMarkerVelocities(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values);
 
   /*!
-   * \brief Get the normal vectors at the marker vertices.
+   * \brief Get the normal vectors of the marker vertices.
    * \param[in] iMarker - Marker index.
    * \param[in] normalize - If true, the unit (i.e. normalized) normal vector is returned.
-   * \return Normal vector at the vertex (nVertex, nDim).
+   * \return Node normal vectors (nVertex, nDim).
    */
   vector<vector<passivedouble>> GetMarkerVertexNormals(unsigned short iMarker, bool normalize = false) const;
 
   /*!
-   * \brief Get the normal vectors at a marker vertex.
+   * \brief Get the normal vector of a marker vertex.
    * \param[in] iMarker - Marker index.
    * \param[in] iVertex - Marker vertex index.
    * \param[in] normalize - If true, the unit (i.e. normalized) normal vector is returned.
-   * \return Normal vector at the vertex (nDim).
+   * \return Node normal vector (nDim).
    */
   vector<passivedouble> GetMarkerVertexNormals(unsigned short iMarker, unsigned long iVertex,
                                                bool normalize = false) const;
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index fcac9907521..726dabe44f9 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -194,19 +194,19 @@ unsigned long CDriverBase::GetNumberMarkerElements(unsigned short iMarker) const
   return main_geometry->GetnElem_Bound(iMarker);
 }
 
-vector<unsigned long> CDriverBase::GetElementIDs() const {
+vector<unsigned long> CDriverBase::GetElements() const {
   const auto nElem = GetNumberElements();
 
   vector<unsigned long> values;
 
   for (auto iElem = 0ul; iElem < nElem; iElem++) {
-    values.push_back(GetElementIDs(iElem));
+    values.push_back(GetElements(iElem));
   }
 
   return values;
 }
 
-unsigned long CDriverBase::GetElementIDs(unsigned long iElem) const {
+unsigned long CDriverBase::GetElements(unsigned long iElem) const {
   if (iElem >= GetNumberElements()) {
     SU2_MPI::Error("Element index exceeds size.", CURRENT_FUNCTION);
   }
@@ -214,39 +214,39 @@ unsigned long CDriverBase::GetElementIDs(unsigned long iElem) const {
   return main_geometry->elem[iElem]->GetGlobalIndex();
 }
 
-vector<unsigned long> CDriverBase::GetMarkerElementIDs(unsigned short iMarker) const {
-  const auto nBound = GetNumberMarkerElements(iMarker);
+vector<unsigned long> CDriverBase::GetMarkerElements(unsigned short iMarker) const {
+  const auto nElem = GetNumberMarkerElements(iMarker);
 
   vector<unsigned long> values;
 
-  for (auto iBound = 0ul; iBound < nBound; iBound++) {
-    values.push_back(GetMarkerElementIDs(iMarker, iBound));
+  for (auto iElem = 0ul; iElem < nElem; iElem++) {
+    values.push_back(GetMarkerElements(iMarker, iElem));
   }
 
   return values;
 }
 
-unsigned long CDriverBase::GetMarkerElementIDs(unsigned short iMarker, unsigned long iBound) const {
-  if (iBound >= GetNumberMarkerElements(iMarker)) {
+unsigned long CDriverBase::GetMarkerElements(unsigned short iMarker, unsigned long iElem) const {
+  if (iElem >= GetNumberMarkerElements(iMarker)) {
     SU2_MPI::Error("Marker element index exceeds size.", CURRENT_FUNCTION);
   }
 
-  return main_geometry->bound[iMarker][iBound]->GetGlobalIndex();
+  return main_geometry->bound[iMarker][iElem]->GetGlobalIndex();
 }
 
-vector<vector<unsigned long>> CDriverBase::GetElementConnectivities() const {
+vector<vector<unsigned long>> CDriverBase::GetElementNodes() const {
   const auto nElem = GetNumberElements();
 
   vector<vector<unsigned long>> values;
 
   for (auto iElem = 0ul; iElem < nElem; iElem++) {
-    values.push_back(GetElementConnectivities(iElem));
+    values.push_back(GetElementNodes(iElem));
   }
 
   return values;
 }
 
-vector<unsigned long> CDriverBase::GetElementConnectivities(unsigned long iElem) const {
+vector<unsigned long> CDriverBase::GetElementNodes(unsigned long iElem) const {
   if (iElem >= GetNumberElements()) {
     SU2_MPI::Error("Element index exceeds size.", CURRENT_FUNCTION);
   }
@@ -264,29 +264,29 @@ vector<unsigned long> CDriverBase::GetElementConnectivities(unsigned long iElem)
   return values;
 }
 
-vector<vector<unsigned long>> CDriverBase::GetMarkerElementConnectivities(unsigned short iMarker) const {
-  const auto nBound = GetNumberMarkerElements(iMarker);
+vector<vector<unsigned long>> CDriverBase::GetMarkerElementNodes(unsigned short iMarker) const {
+  const auto nElem = GetNumberMarkerElements(iMarker);
 
   vector<vector<unsigned long>> values;
 
-  for (auto iBound = 0ul; iBound < nBound; iBound++) {
-    values.push_back(GetMarkerElementConnectivities(iMarker, iBound));
+  for (auto iElem = 0ul; iElem < nElem; iElem++) {
+    values.push_back(GetMarkerElementNodes(iMarker, iElem));
   }
 
   return values;
 }
 
-vector<unsigned long> CDriverBase::GetMarkerElementConnectivities(unsigned short iMarker, unsigned long iBound) const {
-  if (iBound >= GetNumberMarkerElements(iMarker)) {
+vector<unsigned long> CDriverBase::GetMarkerElementNodes(unsigned short iMarker, unsigned long iElem) const {
+  if (iElem >= GetNumberMarkerElements(iMarker)) {
     SU2_MPI::Error("Marker element index exceeds size.", CURRENT_FUNCTION);
   }
 
-  unsigned short nNode = main_geometry->bound[iMarker][iBound]->GetnNodes();
+  unsigned short nNode = main_geometry->bound[iMarker][iElem]->GetnNodes();
 
   vector<unsigned long> values;
 
   for (auto iNode = 0u; iNode < nNode; iNode++) {
-    unsigned long iPoint = main_geometry->bound[iMarker][iBound]->GetNode(iNode);
+    unsigned long iPoint = main_geometry->bound[iMarker][iElem]->GetNode(iNode);
 
     values.push_back(main_geometry->nodes->GetGlobalIndex(iPoint));
   }
@@ -294,9 +294,9 @@ vector<unsigned long> CDriverBase::GetMarkerElementConnectivities(unsigned short
   return values;
 }
 
-unsigned long CDriverBase::GetNumberVertices() const { return main_geometry->GetnPoint(); }
+unsigned long CDriverBase::GetNumberNodes() const { return main_geometry->GetnPoint(); }
 
-unsigned long CDriverBase::GetNumberMarkerVertices(unsigned short iMarker) const {
+unsigned long CDriverBase::GetNumberMarkerNodes(unsigned short iMarker) const {
   if (iMarker >= GetNumberMarkers()) {
     SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
   }
@@ -304,8 +304,8 @@ unsigned long CDriverBase::GetNumberMarkerVertices(unsigned short iMarker) const
   return main_geometry->GetnVertex(iMarker);
 }
 
-unsigned long CDriverBase::GetNumberHaloVertices() const {
-  const auto nPoint = GetNumberVertices();
+unsigned long CDriverBase::GetNumberHaloNodes() const {
+  const auto nPoint = GetNumberNodes();
   unsigned long nHalo = 0;
 
   for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
@@ -317,12 +317,12 @@ unsigned long CDriverBase::GetNumberHaloVertices() const {
   return nHalo;
 }
 
-unsigned long CDriverBase::GetNumberMarkerHaloVertices(unsigned short iMarker) const {
-  const auto nVertex = GetNumberMarkerVertices(iMarker);
+unsigned long CDriverBase::GetNumberMarkerHaloNodes(unsigned short iMarker) const {
+  const auto nVertex = GetNumberMarkerNodes(iMarker);
   unsigned long nHalo = 0;
 
   for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-    auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
+    auto iPoint = GetMarkerVertices(iMarker, iVertex);
 
     if (!(main_geometry->nodes->GetDomain(iPoint))) {
       nHalo += 1;
@@ -332,66 +332,66 @@ unsigned long CDriverBase::GetNumberMarkerHaloVertices(unsigned short iMarker) c
   return nHalo;
 }
 
-vector<unsigned long> CDriverBase::GetMarkerVertexIndices(unsigned short iMarker) const {
-  const auto nVertex = GetNumberMarkerVertices(iMarker);
+vector<unsigned long> CDriverBase::GetMarkerVertices(unsigned short iMarker) const {
+  const auto nVertex = GetNumberMarkerNodes(iMarker);
 
   vector<unsigned long> values;
 
   for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-    values.push_back(GetMarkerVertexIndices(iMarker, iVertex));
+    values.push_back(GetMarkerVertices(iMarker, iVertex));
   }
 
   return values;
 }
 
-unsigned long CDriverBase::GetMarkerVertexIndices(unsigned short iMarker, unsigned long iVertex) const {
-  if (iVertex >= GetNumberMarkerVertices(iMarker)) {
+unsigned long CDriverBase::GetMarkerVertices(unsigned short iMarker, unsigned long iVertex) const {
+  if (iVertex >= GetNumberMarkerNodes(iMarker)) {
     SU2_MPI::Error("Vertex index exceeds marker size.", CURRENT_FUNCTION);
   }
 
   return geometry_container[MESH_0][INST_0][ZONE_0]->vertex[iMarker][iVertex]->GetNode();
 }
 
-vector<unsigned long> CDriverBase::GetVertexIDs() const {
-  const auto nPoint = GetNumberVertices();
+vector<unsigned long> CDriverBase::GetNodes() const {
+  const auto nPoint = GetNumberNodes();
 
   vector<unsigned long> values;
 
   for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
-    values.push_back(GetVertexIDs(iPoint));
+    values.push_back(GetNodes(iPoint));
   }
 
   return values;
 }
 
-unsigned long CDriverBase::GetVertexIDs(unsigned long iPoint) const {
-  if (iPoint >= GetNumberVertices()) {
-    SU2_MPI::Error("Vertex index exceeds mesh size.", CURRENT_FUNCTION);
+unsigned long CDriverBase::GetNodes(unsigned long iPoint) const {
+  if (iPoint >= GetNumberNodes()) {
+    SU2_MPI::Error("Node index exceeds mesh size.", CURRENT_FUNCTION);
   }
 
   return main_geometry->nodes->GetGlobalIndex(iPoint);
 }
 
-vector<unsigned long> CDriverBase::GetMarkerVertexIDs(unsigned short iMarker) const {
-  const auto nVertex = GetNumberMarkerVertices(iMarker);
+vector<unsigned long> CDriverBase::GetMarkerNodes(unsigned short iMarker) const {
+  const auto nVertex = GetNumberMarkerNodes(iMarker);
 
   vector<unsigned long> values;
 
   for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-    values.push_back(GetMarkerVertexIDs(iMarker, iVertex));
+    values.push_back(GetMarkerNodes(iMarker, iVertex));
   }
 
   return values;
 }
 
-unsigned long CDriverBase::GetMarkerVertexIDs(unsigned short iMarker, unsigned long iVertex) const {
-  auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
+unsigned long CDriverBase::GetMarkerNodes(unsigned short iMarker, unsigned long iVertex) const {
+  auto iPoint = GetMarkerVertices(iMarker, iVertex);
 
   return main_geometry->nodes->GetGlobalIndex(iPoint);
 }
 
 vector<bool> CDriverBase::GetDomain() const {
-  const auto nPoint = GetNumberVertices();
+  const auto nPoint = GetNumberNodes();
 
   vector<bool> values;
 
@@ -403,15 +403,15 @@ vector<bool> CDriverBase::GetDomain() const {
 }
 
 bool CDriverBase::GetDomain(unsigned long iPoint) const {
-  if (iPoint >= GetNumberVertices()) {
-    SU2_MPI::Error("Vertex index exceeds mesh size.", CURRENT_FUNCTION);
+  if (iPoint >= GetNumberNodes()) {
+    SU2_MPI::Error("Node index exceeds mesh size.", CURRENT_FUNCTION);
   }
 
   return main_geometry->nodes->GetDomain(iPoint);
 }
 
 vector<bool> CDriverBase::GetMarkerDomain(unsigned short iMarker) const {
-  const auto nVertex = GetNumberMarkerVertices(iMarker);
+  const auto nVertex = GetNumberMarkerNodes(iMarker);
 
   vector<bool> values;
 
@@ -423,13 +423,13 @@ vector<bool> CDriverBase::GetMarkerDomain(unsigned short iMarker) const {
 }
 
 bool CDriverBase::GetMarkerDomain(unsigned short iMarker, unsigned long iVertex) const {
-  auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
+  auto iPoint = GetMarkerVertices(iMarker, iVertex);
 
   return main_geometry->nodes->GetDomain(iPoint);
 }
 
 vector<vector<passivedouble>> CDriverBase::GetInitialCoordinates() const {
-  const auto nPoint = GetNumberVertices();
+  const auto nPoint = GetNumberNodes();
 
   vector<vector<passivedouble>> values;
 
@@ -441,8 +441,8 @@ vector<vector<passivedouble>> CDriverBase::GetInitialCoordinates() const {
 }
 
 vector<passivedouble> CDriverBase::GetInitialCoordinates(unsigned long iPoint) const {
-  if (iPoint >= GetNumberVertices()) {
-    SU2_MPI::Error("Vertex index exceeds mesh size.", CURRENT_FUNCTION);
+  if (iPoint >= GetNumberNodes()) {
+    SU2_MPI::Error("Node index exceeds mesh size.", CURRENT_FUNCTION);
   }
 
   vector<passivedouble> values(nDim, 0.0);
@@ -461,7 +461,7 @@ vector<passivedouble> CDriverBase::GetInitialCoordinates(unsigned long iPoint) c
 }
 
 vector<vector<passivedouble>> CDriverBase::GetMarkerInitialCoordinates(unsigned short iMarker) const {
-  const auto nVertex = GetNumberMarkerVertices(iMarker);
+  const auto nVertex = GetNumberMarkerNodes(iMarker);
 
   vector<vector<passivedouble>> values;
 
@@ -473,7 +473,7 @@ vector<vector<passivedouble>> CDriverBase::GetMarkerInitialCoordinates(unsigned
 }
 
 vector<passivedouble> CDriverBase::GetMarkerInitialCoordinates(unsigned short iMarker, unsigned long iVertex) const {
-  auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
+  auto iPoint = GetMarkerVertices(iMarker, iVertex);
 
   vector<passivedouble> values(nDim, 0.0);
 
@@ -491,7 +491,7 @@ vector<passivedouble> CDriverBase::GetMarkerInitialCoordinates(unsigned short iM
 }
 
 vector<vector<passivedouble>> CDriverBase::GetCoordinates() const {
-  const auto nPoint = GetNumberVertices();
+  const auto nPoint = GetNumberNodes();
 
   vector<vector<passivedouble>> values;
 
@@ -503,8 +503,8 @@ vector<vector<passivedouble>> CDriverBase::GetCoordinates() const {
 }
 
 vector<passivedouble> CDriverBase::GetCoordinates(unsigned long iPoint) const {
-  if (iPoint >= GetNumberVertices()) {
-    SU2_MPI::Error("Vertex index exceeds mesh size.", CURRENT_FUNCTION);
+  if (iPoint >= GetNumberNodes()) {
+    SU2_MPI::Error("Node index exceeds mesh size.", CURRENT_FUNCTION);
   }
 
   vector<passivedouble> values;
@@ -519,7 +519,7 @@ vector<passivedouble> CDriverBase::GetCoordinates(unsigned long iPoint) const {
 }
 
 vector<vector<passivedouble>> CDriverBase::GetMarkerCoordinates(unsigned short iMarker) const {
-  const auto nVertex = GetNumberMarkerVertices(iMarker);
+  const auto nVertex = GetNumberMarkerNodes(iMarker);
 
   vector<vector<passivedouble>> values;
 
@@ -531,7 +531,7 @@ vector<vector<passivedouble>> CDriverBase::GetMarkerCoordinates(unsigned short i
 }
 
 vector<passivedouble> CDriverBase::GetMarkerCoordinates(unsigned short iMarker, unsigned long iVertex) const {
-  auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
+  auto iPoint = GetMarkerVertices(iMarker, iVertex);
 
   vector<passivedouble> values;
 
@@ -545,10 +545,10 @@ vector<passivedouble> CDriverBase::GetMarkerCoordinates(unsigned short iMarker,
 }
 
 void CDriverBase::SetCoordinates(vector<vector<passivedouble>> values) {
-  const auto nPoint = GetNumberVertices();
+  const auto nPoint = GetNumberNodes();
 
   if (values.size() != nPoint) {
-    SU2_MPI::Error("Invalid number of vertices!", CURRENT_FUNCTION);
+    SU2_MPI::Error("Invalid number of nodes!", CURRENT_FUNCTION);
   }
 
   for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
@@ -557,8 +557,8 @@ void CDriverBase::SetCoordinates(vector<vector<passivedouble>> values) {
 }
 
 void CDriverBase::SetCoordinates(unsigned long iPoint, vector<passivedouble> values) {
-  if (iPoint >= GetNumberVertices()) {
-    SU2_MPI::Error("Vertex index exceeds mesh size.", CURRENT_FUNCTION);
+  if (iPoint >= GetNumberNodes()) {
+    SU2_MPI::Error("Node index exceeds mesh size.", CURRENT_FUNCTION);
   }
   if (values.size() != nDim) {
     SU2_MPI::Error("Invalid number of dimensions!", CURRENT_FUNCTION);
@@ -570,7 +570,7 @@ void CDriverBase::SetCoordinates(unsigned long iPoint, vector<passivedouble> val
 }
 
 void CDriverBase::SetMarkerCoordinates(unsigned short iMarker, vector<vector<passivedouble>> values) {
-  const auto nVertex = GetNumberMarkerVertices(iMarker);
+  const auto nVertex = GetNumberMarkerNodes(iMarker);
 
   if (values.size() != nVertex) {
     SU2_MPI::Error("Invalid number of marker vertices!", CURRENT_FUNCTION);
@@ -582,7 +582,7 @@ void CDriverBase::SetMarkerCoordinates(unsigned short iMarker, vector<vector<pas
 }
 
 void CDriverBase::SetMarkerCoordinates(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
-  auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
+  auto iPoint = GetMarkerVertices(iMarker, iVertex);
 
   if (values.size() != nDim) {
     SU2_MPI::Error("Invalid number of dimensions!", CURRENT_FUNCTION);
@@ -594,7 +594,7 @@ void CDriverBase::SetMarkerCoordinates(unsigned short iMarker, unsigned long iVe
 }
 
 vector<vector<passivedouble>> CDriverBase::GetMarkerDisplacements(unsigned short iMarker) const {
-  const auto nVertex = GetNumberMarkerVertices(iMarker);
+  const auto nVertex = GetNumberMarkerNodes(iMarker);
 
   vector<vector<passivedouble>> values;
 
@@ -606,7 +606,7 @@ vector<vector<passivedouble>> CDriverBase::GetMarkerDisplacements(unsigned short
 }
 
 vector<passivedouble> CDriverBase::GetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex) const {
-  auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
+  auto iPoint = GetMarkerVertices(iMarker, iVertex);
 
   vector<passivedouble> values(nDim, 0.0);
 
@@ -628,7 +628,7 @@ void CDriverBase::SetMarkerDisplacements(unsigned short iMarker, vector<vector<p
     SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
   }
 
-  const auto nVertex = GetNumberMarkerVertices(iMarker);
+  const auto nVertex = GetNumberMarkerNodes(iMarker);
 
   if (values.size() != nVertex) {
     SU2_MPI::Error("Invalid number of marker vertices!", CURRENT_FUNCTION);
@@ -644,7 +644,7 @@ void CDriverBase::SetMarkerDisplacements(unsigned short iMarker, unsigned long i
     SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
   }
 
-  auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
+  auto iPoint = GetMarkerVertices(iMarker, iVertex);
 
   if (values.size() != nDim) {
     SU2_MPI::Error("Invalid number of dimensions!", CURRENT_FUNCTION);
@@ -656,7 +656,7 @@ void CDriverBase::SetMarkerDisplacements(unsigned short iMarker, unsigned long i
 }
 
 vector<vector<passivedouble>> CDriverBase::GetMarkerVelocities(unsigned short iMarker) const {
-  const auto nVertex = GetNumberMarkerVertices(iMarker);
+  const auto nVertex = GetNumberMarkerNodes(iMarker);
 
   vector<vector<passivedouble>> values;
 
@@ -668,7 +668,7 @@ vector<vector<passivedouble>> CDriverBase::GetMarkerVelocities(unsigned short iM
 }
 
 vector<passivedouble> CDriverBase::GetMarkerVelocities(unsigned short iMarker, unsigned long iVertex) const {
-  auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
+  auto iPoint = GetMarkerVertices(iMarker, iVertex);
 
   vector<passivedouble> values(nDim, 0.0);
 
@@ -690,7 +690,7 @@ void CDriverBase::SetMarkerVelocities(unsigned short iMarker, vector<vector<pass
     SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
   }
 
-  const auto nVertex = GetNumberMarkerVertices(iMarker);
+  const auto nVertex = GetNumberMarkerNodes(iMarker);
 
   if (values.size() != nVertex) {
     SU2_MPI::Error("Invalid number of marker vertices!", CURRENT_FUNCTION);
@@ -706,7 +706,7 @@ void CDriverBase::SetMarkerVelocities(unsigned short iMarker, unsigned long iVer
     SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
   }
 
-  auto iPoint = GetMarkerVertexIndices(iMarker, iVertex);
+  auto iPoint = GetMarkerVertices(iMarker, iVertex);
 
   if (values.size() != nDim) {
     SU2_MPI::Error("Invalid number of dimensions!", CURRENT_FUNCTION);
@@ -718,7 +718,7 @@ void CDriverBase::SetMarkerVelocities(unsigned short iMarker, unsigned long iVer
 }
 
 vector<vector<passivedouble>> CDriverBase::GetMarkerVertexNormals(unsigned short iMarker, bool normalize) const {
-  const auto nVertex = GetNumberMarkerVertices(iMarker);
+  const auto nVertex = GetNumberMarkerNodes(iMarker);
 
   vector<vector<passivedouble>> values;
 
@@ -731,7 +731,7 @@ vector<vector<passivedouble>> CDriverBase::GetMarkerVertexNormals(unsigned short
 
 vector<passivedouble> CDriverBase::GetMarkerVertexNormals(unsigned short iMarker, unsigned long iVertex,
                                                           bool normalize) const {
-  if (iVertex >= GetNumberMarkerVertices(iMarker)) {
+  if (iVertex >= GetNumberMarkerNodes(iMarker)) {
     SU2_MPI::Error("Vertex index exceeds marker size.", CURRENT_FUNCTION);
   }
 

From 0c61d0a2fe77119c3387fe663fb144f4902fa9dc Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Thu, 29 Dec 2022 21:55:34 -0800
Subject: [PATCH 102/656] Fix maps build error, fix pysu2 dependency

---
 SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp | 10 +---------
 SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp     | 11 ++++++++++-
 SU2_PY/pySU2/pySU2.i                                  |  2 +-
 SU2_PY/pySU2/pySU2ad.i                                |  2 +-
 4 files changed, 13 insertions(+), 12 deletions(-)

diff --git a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
index 998b89fbe1b..534b0cddb16 100644
--- a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
@@ -27,18 +27,10 @@
 
 #pragma once
 
-#include "../../../Common/include/CConfig.hpp"
 #include "../../../Common/include/fem/fem_geometry_structure.hpp"
-#include "../../../Common/include/geometry/CGeometry.hpp"
-#include "../../../Common/include/grid_movement/CSurfaceMovement.hpp"
-#include "../../../Common/include/grid_movement/CVolumetricMovement.hpp"
 #include "../../../Common/include/parallelization/mpi_structure.hpp"
+#include "../../../Common/include/parallelization/omp_structure.hpp"
 #include "../../../SU2_CFD/include/drivers/CDriverBase.hpp"
-#include "../../../SU2_CFD/include/numerics/CGradSmoothing.hpp"
-#include "../../../SU2_CFD/include/output/CBaselineOutput.hpp"
-#include "../../../SU2_CFD/include/output/COutput.hpp"
-#include "../../../SU2_CFD/include/solvers/CBaselineSolver.hpp"
-#include "../../../SU2_CFD/include/solvers/CGradientSmoothingSolver.hpp"
 
 class CDiscAdjDeformationDriver : public CDriverBase {
 protected:
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index 0b01614eec5..362c237e56a 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -25,9 +25,18 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-#include "../../include/drivers/CDiscAdjDeformationDriver.hpp"
+#define ENABLE_MAPS
+#include "../../../Common/include/CConfig.hpp"
+#undef ENABLE_MAPS
 
 #include "../../../Common/include/geometry/CPhysicalGeometry.hpp"
+#include "../../../Common/include/grid_movement/CSurfaceMovement.hpp"
+#include "../../../Common/include/grid_movement/CVolumetricMovement.hpp"
+#include "../../../SU2_CFD/include/numerics/CGradSmoothing.hpp"
+#include "../../../SU2_CFD/include/output/CBaselineOutput.hpp"
+#include "../../../SU2_CFD/include/solvers/CBaselineSolver.hpp"
+#include "../../../SU2_CFD/include/solvers/CGradientSmoothingSolver.hpp"
+#include "../../include/drivers/CDiscAdjDeformationDriver.hpp"
 
 using namespace std;
 
diff --git a/SU2_PY/pySU2/pySU2.i b/SU2_PY/pySU2/pySU2.i
index 1d8c424cd28..7cf25ca6f09 100644
--- a/SU2_PY/pySU2/pySU2.i
+++ b/SU2_PY/pySU2/pySU2.i
@@ -92,8 +92,8 @@ const unsigned int MESH_1 = 1; /*!< \brief Definition of the finest grid level.
 const unsigned int ZONE_0 = 0; /*!< \brief Definition of the first grid domain. */
 const unsigned int ZONE_1 = 1; /*!< \brief Definition of the first grid domain. */
 
-%include "../../SU2_CFD/include/drivers/CDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CDriverBase.hpp"
+%include "../../SU2_CFD/include/drivers/CDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CMultizoneDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp"
diff --git a/SU2_PY/pySU2/pySU2ad.i b/SU2_PY/pySU2/pySU2ad.i
index 7b347f5cbe1..f8aec4044f3 100644
--- a/SU2_PY/pySU2/pySU2ad.i
+++ b/SU2_PY/pySU2/pySU2ad.i
@@ -91,8 +91,8 @@ const unsigned int MESH_1 = 1; /*!< \brief Definition of the finest grid level.
 const unsigned int ZONE_0 = 0; /*!< \brief Definition of the first grid domain. */
 const unsigned int ZONE_1 = 1; /*!< \brief Definition of the first grid domain. */
 
-%include "../../SU2_CFD/include/drivers/CDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CDriverBase.hpp"
+%include "../../SU2_CFD/include/drivers/CDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CMultizoneDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp"

From a447ae3ae3447d69488d84b748b857a9dea9bf72 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Fri, 30 Dec 2022 12:24:29 -0800
Subject: [PATCH 103/656] Update function names in FSIInterface.py and Python
 test cases

---
 SU2_PY/FSI_tools/FSIInterface.py                     | 12 ++++++------
 .../disc_adj_flow/mesh_disp_sens/run_adjoint.py      |  2 +-
 .../launch_flatPlate_rigidMotion.py                  |  4 ++--
 .../launch_unsteady_CHT_FlatPlate.py                 |  4 ++--
 TestCases/py_wrapper/translating_NACA0012/run_su2.py |  4 ++--
 5 files changed, 13 insertions(+), 13 deletions(-)

diff --git a/SU2_PY/FSI_tools/FSIInterface.py b/SU2_PY/FSI_tools/FSIInterface.py
index 616628162a8..0ab227fde57 100644
--- a/SU2_PY/FSI_tools/FSIInterface.py
+++ b/SU2_PY/FSI_tools/FSIInterface.py
@@ -235,7 +235,7 @@ def connect(self, FSI_config, FluidSolver, SolidSolver):
                 if allMovingMarkersTags[0] in allMarkersID.keys():
                     self.fluidInterfaceIdentifier = allMarkersID[allMovingMarkersTags[0]]
             if self.fluidInterfaceIdentifier is not None:
-                self.nLocalFluidInterfaceNodes = FluidSolver.GetNumberMarkerVertices(self.fluidInterfaceIdentifier)
+                self.nLocalFluidInterfaceNodes = FluidSolver.GetNumberMarkerNodes(self.fluidInterfaceIdentifier)
             if self.nLocalFluidInterfaceNodes != 0:
               self.haveFluidInterface = True
               print('Number of interface fluid nodes (halo nodes included) on proccess {} : {}'.format(myid,self.nLocalFluidInterfaceNodes))
@@ -301,7 +301,7 @@ def connect(self, FSI_config, FluidSolver, SolidSolver):
         self.nLocalFluidInterfaceHaloNode = 0
         for iVertex in range(self.nLocalFluidInterfaceNodes):
             if not FluidSolver.GetMarkerDomain(self.fluidInterfaceIdentifier, iVertex):
-              GlobalIndex = FluidSolver.GetMarkerVertexIDs(self.fluidInterfaceIdentifier, iVertex)
+              GlobalIndex = FluidSolver.GetMarkerNodes(self.fluidInterfaceIdentifier, iVertex)
               self.FluidHaloNodeList[GlobalIndex] = iVertex
               self.nLocalFluidInterfaceHaloNode += 1
         # Calculate the number of physical (= not halo) nodes on each partition
@@ -565,7 +565,7 @@ def interfaceMapping(self,FluidSolver, SolidSolver, FSI_config):
             # Note that the fluid solver is separated in more processors outside the python script
             # thus when, from a core, we request for the vertices on the interface, we only obtain
             # those in that core
-            GlobalIndex = FluidSolver.GetMarkerVertexIDs(self.fluidInterfaceIdentifier, iVertex)
+            GlobalIndex = FluidSolver.GetMarkerNodes(self.fluidInterfaceIdentifier, iVertex)
             if self.nDim == 2:
                 posx, posy = FluidSolver.GetMarkerInitialCoordinates(self.fluidInterfaceIdentifier, iVertex)
                 posz = 0
@@ -1460,7 +1460,7 @@ def getFluidInterfaceNodalForce(self, FSI_config, FluidSolver):
 
         # --- Get the fluid interface loads from the fluid solver and directly fill the corresponding PETSc vector ---
         for iVertex in range(self.nLocalFluidInterfaceNodes):
-            GlobalIndex = FluidSolver.GetMarkerVertexIDs(self.fluidInterfaceIdentifier, iVertex)
+            GlobalIndex = FluidSolver.GetMarkerNodes(self.fluidInterfaceIdentifier, iVertex)
             if GlobalIndex not in self.FluidHaloNodeList[myid].keys():
               loadX, loadY, loadZ = FluidSolver.GetFlowLoad(self.fluidInterfaceIdentifier, iVertex)
               iGlobalVertex = self.__getGlobalIndex('fluid', myid, localIndex)
@@ -1490,7 +1490,7 @@ def setFluidInterfaceVarCoord(self, FluidSolver):
         # --- Send the new fluid interface position to the fluid solver (on each partition, halo nodes included) ---
         localIndex = 0
         for iVertex in range(self.nLocalFluidInterfaceNodes):
-            GlobalIndex = FluidSolver.GetMarkerVertexIDs(self.fluidInterfaceIdentifier, iVertex)
+            GlobalIndex = FluidSolver.GetMarkerNodes(self.fluidInterfaceIdentifier, iVertex)
             if GlobalIndex in self.FluidHaloNodeList[myid].keys():
               DispX, DispY, DispZ = self.haloNodesDisplacements[GlobalIndex]
               FluidSolver.SetMarkerDisplacements(self.fluidInterfaceIdentifier, int(iVertex), np.array([DispX, DispY, DispZ]))
@@ -2151,7 +2151,7 @@ def MapModes(self, FSI_config, FluidSolver, SolidSolver):
             nz = 0
         else:
             nx, ny, nz = FluidSolver.GetMarkerVertexNormals(self.fluidInterfaceIdentifier, iVertex, False)
-        GlobalIndex = FluidSolver.GetMarkerVertexIDs(self.fluidInterfaceIdentifier, iVertex)
+        GlobalIndex = FluidSolver.GetMarkerNodes(self.fluidInterfaceIdentifier, iVertex)
         nodeNormals[GlobalIndex] = [nx, ny, nz]
 
       nodeNormals = self.comm.gather(nodeNormals, root=self.rootProcess)
diff --git a/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
index e098d06640b..905a43ddb56 100755
--- a/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
@@ -80,7 +80,7 @@ def main():
   nVertex_Marker = 0         #total number of vertices (physical + halo)
 
   if MarkerID != None:
-    nVertex_Marker = SU2Driver.GetNumberMarkerVertices(MarkerID)
+    nVertex_Marker = SU2Driver.GetNumberMarkerNodes(MarkerID)
 
   # Time loop is defined in Python so that we have acces to SU2 functionalities at each time step
   if rank == 0:
diff --git a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
index 88a8d2e3ece..85c9483fddd 100755
--- a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
+++ b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
@@ -91,8 +91,8 @@ def main():
   nVertex_MovingMarker_PHYS = 0    #number of physical vertices
 
   if MovingMarkerID != None:
-    nVertex_MovingMarker = SU2Driver.GetNumberMarkerVertices(MovingMarkerID)
-    nVertex_MovingMarker_HALO = SU2Driver.GetNumberMarkerHaloVertices(MovingMarkerID)
+    nVertex_MovingMarker = SU2Driver.GetNumberMarkerNodes(MovingMarkerID)
+    nVertex_MovingMarker_HALO = SU2Driver.GetNumberMarkerHaloNodes(MovingMarkerID)
     nVertex_MovingMarker_PHYS = nVertex_MovingMarker - nVertex_MovingMarker_HALO
 
   # Retrieve some control parameters from the driver
diff --git a/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py b/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
index 8e9b6ca9679..57aec6661fa 100755
--- a/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
+++ b/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
@@ -90,8 +90,8 @@ def main():
   nVertex_CHTMarker_PHYS = 0    # number of physical vertices
 
   if CHTMarkerID != None:
-    nVertex_CHTMarker = SU2Driver.GetNumberMarkerVertices(CHTMarkerID)
-    nVertex_CHTMarker_HALO = SU2Driver.GetNumberMarkerHaloVertices(CHTMarkerID)
+    nVertex_CHTMarker = SU2Driver.GetNumberMarkerNodes(CHTMarkerID)
+    nVertex_CHTMarker_HALO = SU2Driver.GetNumberMarkerHaloNodes(CHTMarkerID)
     nVertex_CHTMarker_PHYS = nVertex_CHTMarker - nVertex_CHTMarker_HALO
 
   # Retrieve some control parameters from the driver
diff --git a/TestCases/py_wrapper/translating_NACA0012/run_su2.py b/TestCases/py_wrapper/translating_NACA0012/run_su2.py
index a4abfee0b6e..5cc7a679ab4 100644
--- a/TestCases/py_wrapper/translating_NACA0012/run_su2.py
+++ b/TestCases/py_wrapper/translating_NACA0012/run_su2.py
@@ -46,10 +46,10 @@ def save_forces(self):
 
         for marker in solver_all_moving_markers[has_moving_marker]:
             solver_marker_id = solver_marker_ids[marker]
-            n_vertices = self.FluidSolver.GetNumberMarkerVertices(solver_marker_id)
+            n_vertices = self.FluidSolver.GetNumberMarkerNodes(solver_marker_id)
             for i_vertex in range(n_vertices):
                 fxyz = self.FluidSolver.GetFlowLoad(solver_marker_id, i_vertex)
-                GlobalIndex = self.FluidSolver.GetMarkerVertexIDs(solver_marker_id, i_vertex)
+                GlobalIndex = self.FluidSolver.GetMarkerNodes(solver_marker_id, i_vertex)
                 f.write('{}, {:.2f}, {:.2f}, {:.2f}\n'.format(GlobalIndex, fxyz[0], fxyz[1], fxyz[2]))
         f.close()
 

From 93b4ac00985172a4d8828fc3f1a662acea561b3b Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Fri, 30 Dec 2022 14:43:44 -0800
Subject: [PATCH 104/656] Fix segfault from accessing main_config and
 main_geometry

---
 SU2_CFD/src/drivers/CDriver.cpp | 7 +++++++
 1 file changed, 7 insertions(+)

diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index c0a6c49f217..6d9321c8fdd 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -603,6 +603,10 @@ void CDriver::Input_Preprocessing(CConfig **&config, CConfig *&driver_config) {
     }
   }
 
+  /*--- Keep a reference to the main (ZONE 0) config. ---*/
+
+  main_config = config_container[ZONE_0];
+
   /*--- Determine whether or not the FEM solver is used, which decides the type of
    *    geometry classes that are instantiated. Only adapted for single-zone problems ---*/
 
@@ -707,6 +711,9 @@ void CDriver::Geometrical_Preprocessing(CConfig* config, CGeometry **&geometry,
 
   }
 
+  /*--- Keep a reference to the main (ZONE_0, INST_0, MESH_0) geometry. ---*/
+
+  main_geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 }
 
 void CDriver::Geometrical_Preprocessing_FVM(CConfig *config, CGeometry **&geometry) {

From bc9893cc44125bf61e25004d9e93075bd5294d8b Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Fri, 30 Dec 2022 15:40:03 -0800
Subject: [PATCH 105/656] Fix attribute error in translating NACA0012 pysu2
 test case

---
 TestCases/py_wrapper/translating_NACA0012/run_su2.py | 5 +++--
 1 file changed, 3 insertions(+), 2 deletions(-)

diff --git a/TestCases/py_wrapper/translating_NACA0012/run_su2.py b/TestCases/py_wrapper/translating_NACA0012/run_su2.py
index 5cc7a679ab4..c8b114410ec 100644
--- a/TestCases/py_wrapper/translating_NACA0012/run_su2.py
+++ b/TestCases/py_wrapper/translating_NACA0012/run_su2.py
@@ -36,11 +36,12 @@ def run_solver(self):
 
     def save_forces(self):
         solver_all_moving_markers = np.array(self.FluidSolver.GetDeformableMarkerTags())
-        solver_marker_ids = self.FluidSolver.GetMarkerTags()
+        solver_markers = self.FluidSolver.GetMarkerTags()
+        solver_marker_ids = self.FluidSolver.GetMarkerIndices()
         # The surface marker and the partitioning of the solver usually don't agree.
         # Thus, it is necessary to figure out if the partition of the current mpi process has
         # a node that belongs to a moving surface marker.
-        has_moving_marker = [marker in solver_marker_ids.keys() for marker in solver_all_moving_markers]
+        has_moving_marker = [marker in solver_markers for marker in solver_all_moving_markers]
 
         f = open('forces_'+str(self.myid)+'.csv','w')
 

From e7e1bc1d7291bf8bdd38cf3b527062a87a3c071e Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 2 Jan 2023 13:25:29 +0100
Subject: [PATCH 106/656] Fixed bug in table unit tests

---
 .../Common/containers/CLookupTable_tests.cpp     | 16 ++++++++--------
 1 file changed, 8 insertions(+), 8 deletions(-)

diff --git a/UnitTests/Common/containers/CLookupTable_tests.cpp b/UnitTests/Common/containers/CLookupTable_tests.cpp
index c410a01bf0f..b91474e33fe 100644
--- a/UnitTests/Common/containers/CLookupTable_tests.cpp
+++ b/UnitTests/Common/containers/CLookupTable_tests.cpp
@@ -67,12 +67,12 @@ TEST_CASE("LUTreader", "[tabulated chemistry]") {
   /* find the table limits */
   
   auto limitsEnth = look_up_table.GetTableLimitsY();
-  CHECK(limitsEnth.first == Approx(-1.0));
-  CHECK(limitsEnth.second == Approx(1.0));
+  CHECK(SU2_TYPE::GetValue(*limitsEnth.first) == Approx(-1.0));
+  CHECK(SU2_TYPE::GetValue(*limitsEnth.second) == Approx(1.0));
 
   auto limitsProgvar = look_up_table.GetTableLimitsX();
-  CHECK(limitsProgvar.first == Approx(0.0));
-  CHECK(limitsProgvar.second == Approx(1.0));
+  CHECK(SU2_TYPE::GetValue(*limitsProgvar.first) == Approx(0.0));
+  CHECK(SU2_TYPE::GetValue(*limitsProgvar.second) == Approx(1.0));
 
   /* lookup value outside of lookup table */
 
@@ -117,12 +117,12 @@ TEST_CASE("LUTreader_3D", "[tabulated chemistry]") {
   /* find the table limits */
   
   auto limitsEnth = look_up_table.GetTableLimitsY();
-  CHECK(limitsEnth.first == Approx(-1.0));
-  CHECK(limitsEnth.second == Approx(1.0));
+  CHECK(SU2_TYPE::GetValue(*limitsEnth.first) == Approx(-1.0));
+  CHECK(SU2_TYPE::GetValue(*limitsEnth.second) == Approx(1.0));
 
   auto limitsProgvar = look_up_table.GetTableLimitsX();
-  CHECK(limitsProgvar.first == Approx(0.0));
-  CHECK(limitsProgvar.second == Approx(1.0));
+  CHECK(SU2_TYPE::GetValue(*limitsProgvar.first) == Approx(0.0));
+  CHECK(SU2_TYPE::GetValue(*limitsProgvar.second) == Approx(1.0));
 
   /* lookup value outside of lookup table */
 

From 5170ad5900c2d1a93cea8fe26277bda9616cd61d Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 2 Jan 2023 13:47:11 +0100
Subject: [PATCH 107/656] Replaced 'name_x' and 'name_y' in lookup table
 constructor with 'name_cv1' and 'name_cv2'

---
 Common/include/containers/CLookUpTable.hpp |  8 ++++----
 Common/src/containers/CLookUpTable.cpp     | 18 +++++++++---------
 2 files changed, 13 insertions(+), 13 deletions(-)

diff --git a/Common/include/containers/CLookUpTable.hpp b/Common/include/containers/CLookUpTable.hpp
index 6efb3920b06..0189faff883 100644
--- a/Common/include/containers/CLookUpTable.hpp
+++ b/Common/include/containers/CLookUpTable.hpp
@@ -132,10 +132,10 @@ class CLookUpTable {
    * \brief find the table limits, i.e. the minimum and maximum values of the 2 independent.
    * controlling variables. We put the values in the variables.
    * limits_table_x[2] and limit_table_y[2].
-   * \param[in] name_x - the string name for the first controlling variable.
-   * \param[in] name_y - the string name of the second controlling variable.
+   * \param[in] name_CV1 - the string name for the first controlling variable.
+   * \param[in] name_CV2 - the string name of the second controlling variable.
    */
-  void FindTableLimits(const std::string& name_x, const std::string& name_y);
+  void FindTableLimits(const std::string& name_CV1, const std::string& name_CV2);
 
   /*!
    * \brief construct a list of all the edges and a list of the pair of elements left and right of the edge.
@@ -241,7 +241,7 @@ class CLookUpTable {
   }
 
  public:
-  CLookUpTable(const std::string& file_name_lut, const std::string& name_x, const std::string& name_y);
+  CLookUpTable(const std::string& file_name_lut, const std::string& name_CV1_in, const std::string& name_CV2_in);
 
   /*!
    * \brief print information to screen.
diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index 485cedf947f..5be9cb26348 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -31,17 +31,17 @@
 
 using namespace std;
 
-CLookUpTable::CLookUpTable(const string& var_file_name_lut, const string& name_x, const string& name_y) {
-  file_name_lut = var_file_name_lut;
+CLookUpTable::CLookUpTable(const string& var_file_name_lut, const string& name_CV1_in, const string& name_CV2_in) :
+file_name_lut{var_file_name_lut}, 
+name_CV1{name_CV1_in}, 
+name_CV2{name_CV2_in} 
+{
 
   rank = SU2_MPI::GetRank();
 
-  name_CV1 = name_x;
-  name_CV2 = name_y;
-
   LoadTableRaw(var_file_name_lut);
 
-  FindTableLimits(name_x, name_y);
+  FindTableLimits(name_CV1, name_CV2);
 
   if (rank == MASTER_NODE)
     cout << "Detecting all unique edges and setting edge to triangle connectivity "
@@ -59,12 +59,12 @@ CLookUpTable::CLookUpTable(const string& var_file_name_lut, const string& name_x
   switch (table_dim)
   {
   case 2:
-    cout << "Building a trapezoidal map for the (" + name_x + ", " + name_y + ") "
+    cout << "Building a trapezoidal map for the (" + name_CV1 + ", " + name_CV2 + ") "
             "space ..."
          << endl;
     break;
   case 3:
-    cout << "Building trapezoidal map stack for the (" + name_x + ", " + name_y + ") "
+    cout << "Building trapezoidal map stack for the (" + name_CV1 + ", " + name_CV2 + ") "
               "space ..."
           << endl;
     break;
@@ -76,7 +76,7 @@ CLookUpTable::CLookUpTable(const string& var_file_name_lut, const string& name_x
   su2double startTime = SU2_MPI::Wtime();
   unsigned short barwidth=65;
   for(auto i_level = 0ul; i_level<n_table_levels; i_level++){
-    trap_map_x_y[i_level] = CTrapezoidalMap(GetDataP(name_x, i_level), GetDataP(name_y, i_level), table_data[i_level].cols(), edges[i_level], edge_to_triangle[i_level]);
+    trap_map_x_y[i_level] = CTrapezoidalMap(GetDataP(name_CV1, i_level), GetDataP(name_CV2, i_level), table_data[i_level].cols(), edges[i_level], edge_to_triangle[i_level]);
     /* Display a progress bar to monitor table generation process */
     if(rank == MASTER_NODE){
       su2double progress = su2double(i_level) / n_table_levels;

From 23404d7ea0ca1bbdadfbe2e832696916fb417e09 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 3 Jan 2023 15:22:14 +0100
Subject: [PATCH 108/656] Applied clang formatting to LUT related files

---
 Common/include/containers/CFileReaderLUT.hpp  |  82 ++-
 Common/include/containers/CLookUpTable.hpp    | 138 ++--
 Common/include/containers/CTrapezoidalMap.hpp |  59 +-
 Common/src/containers/CFileReaderLUT.cpp      | 138 ++--
 Common/src/containers/CLookUpTable.cpp        | 589 +++++++++---------
 Common/src/containers/CTrapezoidalMap.cpp     |  31 +-
 6 files changed, 518 insertions(+), 519 deletions(-)

diff --git a/Common/include/containers/CFileReaderLUT.hpp b/Common/include/containers/CFileReaderLUT.hpp
index 27dc72271af..929d75d3703 100644
--- a/Common/include/containers/CFileReaderLUT.hpp
+++ b/Common/include/containers/CFileReaderLUT.hpp
@@ -46,27 +46,25 @@ class CFileReaderLUT {
   std::string version_lut;
   std::string version_reader;
   unsigned long n_levels = 1;
-  su2vector<unsigned long> n_points, 
-                           n_triangles, 
-                           n_hull_points;
+  su2vector<unsigned long> n_points, n_triangles, n_hull_points;
 
   unsigned long n_variables;
   su2vector<su2double> table_levels;
 
-  /*! \brief Holds the variable names stored in the table file. 
+  /*! \brief Holds the variable names stored in the table file.
    * Order is in sync with tableFlamelet.
    */
   su2vector<std::string> names_var;
 
-  /*! \brief Holds all data stored in the table. 
+  /*! \brief Holds all data stored in the table.
    * First index addresses the variable while second index addresses the point.
    */
-  su2vector<su2activematrix>table_data;
+  su2vector<su2activematrix> table_data;
 
-  su2vector<su2matrix<unsigned long>>triangles;
+  su2vector<su2matrix<unsigned long>> triangles;
 
-  su2vector<su2vector<unsigned long>>hull;
-  /*! \brief Searches for the position of flag in file_stream and 
+  su2vector<su2vector<unsigned long>> hull;
+  /*! \brief Searches for the position of flag in file_stream and
    *         sets the stream position of file_stream to that position.
    */
   void SkipToFlag(std::ifstream& file_stream, const std::string& current_line, const std::string& flag) const;
@@ -74,33 +72,81 @@ class CFileReaderLUT {
   /*! \brief Extracts the next non-empty characters from file_stream and stores them into line.
    */
   bool GetNextNonEmptyLine(std::ifstream& file_stream, std::string& line) const;
-  
+
   /*! \brief Extracts characters from file_stream, removes trailing control characters,
    *         and stores them into line.
    */
   bool GetStrippedLine(std::ifstream& file_stream, std::string& line) const;
 
  public:
- 
+  /*! \brief Get table version as listed in input file.
+   */
   inline const std::string& GetVersionLUT() const { return version_lut; }
+
+  /*! \brief Get table reader version.
+   */
   inline const std::string& GetVersionReader() const { return version_reader; }
-  inline unsigned long GetNPoints(std::size_t i_level=0) const { return n_points[i_level]; }
-  inline unsigned long GetNTriangles(std::size_t i_level=0) const { return n_triangles[i_level]; }
-  inline unsigned long GetNHullPoints(std::size_t i_level=0) const { return n_hull_points[i_level]; }
+
+  /*! \brief Get number of data points at specific table level.
+   * \param[in] i_level - table level index.
+   * \returns data point count at table level.
+   */
+  inline unsigned long GetNPoints(std::size_t i_level = 0) const { return n_points[i_level]; }
+
+  /*! \brief Get number of triangles at specific table level.
+   * \param[in] i_level - table level index.
+   * \returns triangle count at table level.
+   */
+  inline unsigned long GetNTriangles(std::size_t i_level = 0) const { return n_triangles[i_level]; }
+
+  /*! \brief Get number of hull points at specific table level.
+   * \param[in] i_level - table level index.
+   * \returns hull point count at table level.
+   */
+  inline unsigned long GetNHullPoints(std::size_t i_level = 0) const { return n_hull_points[i_level]; }
+
+  /*! \brief Get number of variables for which data is stored in the table
+   */
   inline unsigned long GetNVariables() const { return n_variables; }
+
+  /*! \brief Get number of table levels.
+   */
   inline unsigned long GetNLevels() const { return n_levels; }
 
+  /*! \brief Get variable names for which data is stored in the table
+   */
   inline const su2vector<std::string>& GetNamesVar() const { return names_var; }
 
-  inline const su2activematrix& GetTableData(std::size_t i_level=0) const { return table_data[i_level]; }
+  /*! \brief Get table data at a specific level.
+   * \param[in] i_level - table level index.
+   * \returns table data
+   */
+  inline const su2activematrix& GetTableData(std::size_t i_level = 0) const { return table_data[i_level]; }
 
-  inline const su2matrix<unsigned long>& GetTriangles(std::size_t i_level=0) const { return triangles[i_level]; }
+  /*! \brief Get table connectivity at a specific level.
+   * \param[in] i_level - table level index.
+   * \returns data connectivity
+   */
+  inline const su2matrix<unsigned long>& GetTriangles(std::size_t i_level = 0) const { return triangles[i_level]; }
 
-  inline const su2vector<unsigned long>& GetHull(std::size_t i_level=0) const { return hull[i_level]; }
+  /*! \brief Get hull node information at a specific table level.
+   * \param[in] i_level - table level index.
+   * \returns hull node indices.
+   */
+  inline const su2vector<unsigned long>& GetHull(std::size_t i_level = 0) const { return hull[i_level]; }
 
+  /*! \brief Get table level value.
+   * \param[in] i_level - table level index.
+   * \returns value of the third controlling variable at table level.
+   */
   inline su2double GetTableLevel(std::size_t i_level) const { return table_levels[i_level]; }
-  
+
+  /*! \brief Get table dimension
+   */
   inline unsigned short GetTableDim() const { return table_dim; }
 
+  /*! \brief Read LUT file and store information
+   * \param[in] file_name - LUT input file name.
+   */
   void ReadRawLUT(const std::string& file_name);
 };
diff --git a/Common/include/containers/CLookUpTable.hpp b/Common/include/containers/CLookUpTable.hpp
index 0189faff883..378cee18bab 100644
--- a/Common/include/containers/CLookUpTable.hpp
+++ b/Common/include/containers/CLookUpTable.hpp
@@ -27,10 +27,10 @@
 
 #pragma once
 
+#include <array>
 #include <iomanip>
 #include <string>
 #include <vector>
-#include <array>
 
 #include "../../Common/include/option_structure.hpp"
 #include "CFileReaderLUT.hpp"
@@ -44,28 +44,26 @@ class CLookUpTable {
  protected:
   int rank; /*!< \brief MPI Rank. */
 
-  std::string file_name_lut,  /*!< \brief LUT file name.*/ 
-              version_lut,    /*!< \brief LUT version as specified in LUT file.*/ 
-              version_reader, /*!< \brief Reader version (should be equal or above LUT version).*/ 
-              name_CV1,       /*!< \brief Name of controlling variable 1.*/ 
-              name_CV2;       /*!< \brief Name of xontrolling variable 2.*/ 
+  std::string file_name_lut, /*!< \brief LUT file name.*/
+      version_lut,           /*!< \brief LUT version as specified in LUT file.*/
+      version_reader,        /*!< \brief Reader version (should be equal or above LUT version).*/
+      name_CV1,              /*!< \brief Name of controlling variable 1.*/
+      name_CV2;              /*!< \brief Name of xontrolling variable 2.*/
 
-  su2vector<unsigned long>  n_points,       /*!< \brief Number of data poins per table level.*/ 
-                            n_triangles,    /*!< \brief Number of triangles per table level.*/ 
-                            n_hull_points;  /*!< \brief Number of outer boundary points per table level.*/ 
+  su2vector<unsigned long> n_points, /*!< \brief Number of data poins per table level.*/
+      n_triangles,                   /*!< \brief Number of triangles per table level.*/
+      n_hull_points;                 /*!< \brief Number of outer boundary points per table level.*/
 
-  unsigned long n_variables,      
-                n_table_levels=1;
+  unsigned long n_variables, n_table_levels = 1;
 
-  su2vector<su2double> z_values_levels; /*!< \brief Constant z-values of each table level.*/ 
+  su2vector<su2double> z_values_levels; /*!< \brief Constant z-values of each table level.*/
 
-  unsigned short table_dim = 2;/*!< \brief Table dimension.*/ 
-  /*! 
+  unsigned short table_dim = 2; /*!< \brief Table dimension.*/
+  /*!
    * \brief the lower and upper limits of the z, y and x variable for each table level.
    */
   std::pair<su2double*, su2double*> limits_table_z;
-  su2vector<std::pair<su2double*, su2double*>> limits_table_y, 
-                                             limits_table_x;
+  su2vector<std::pair<su2double*, su2double*>> limits_table_y, limits_table_x;
 
   /*! \brief Holds the variable names stored in the table file.
    * Order is in sync with data
@@ -79,33 +77,33 @@ class CLookUpTable {
   su2vector<su2activematrix> table_data;
 
   /*! \brief
-   * Holds all connectivity data stored in the table for each level. First index 
+   * Holds all connectivity data stored in the table for each level. First index
    * addresses the variable while second index addresses the point.
    */
-  su2vector<su2matrix<unsigned long>>triangles;
+  su2vector<su2matrix<unsigned long>> triangles;
 
   /*! \brief
    * Edge information for each table level.
    */
-  su2vector<std::vector<std::array<unsigned long,2>>>edges;
-  su2vector<su2vector<std::vector<unsigned long>>>edge_to_triangle;
+  su2vector<std::vector<std::array<unsigned long, 2>>> edges;
+  su2vector<su2vector<std::vector<unsigned long>>> edge_to_triangle;
 
-  /*! \brief 
+  /*! \brief
    * The hull contains the boundary of the lookup table.
    */
-  su2vector<su2vector<unsigned long>>hull;
+  su2vector<su2vector<unsigned long>> hull;
 
-  /*! \brief 
+  /*! \brief
    * Trapezoidal map objects for the table levels.
    */
-  su2vector<CTrapezoidalMap>trap_map_x_y;
+  su2vector<CTrapezoidalMap> trap_map_x_y;
 
-  /*! \brief 
+  /*! \brief
    * vector of all the weight factors for the interpolation.
    */
-  su2vector<su2vector<su2activematrix>>interp_mat_inv_x_y;
+  su2vector<su2vector<su2activematrix>> interp_mat_inv_x_y;
 
-  /*! \brief 
+  /*! \brief
    * returns the index to the variable in the lookup table.
    */
   inline unsigned int GetIndexOfVar(const std::string& nameVar) const {
@@ -124,7 +122,7 @@ class CLookUpTable {
    * \brief Get the pointer to the column data of the table (density, temperature, source terms, ...).
    * \returns pointer to the column data.
    */
-  inline const su2double* GetDataP(const std::string& name_var, unsigned long i_level=0) const {
+  inline const su2double* GetDataP(const std::string& name_var, unsigned long i_level = 0) const {
     return table_data[i_level][GetIndexOfVar(name_var)];
   }
 
@@ -145,12 +143,12 @@ class CLookUpTable {
   /*!
    * \brief read the lookup table from file and store the data.
    * \param[in] file_name_lut - the filename of the lookup table.
-  */
+   */
   void LoadTableRaw(const std::string& file_name_lut);
 
   /*!
    * \brief compute vector of all (inverse) interpolation coefficients "interp_mat_inv_x_y" of all triangles.
-  */
+   */
   void ComputeInterpCoeffs();
 
   /*!
@@ -159,8 +157,8 @@ class CLookUpTable {
    * \param[in] vec_y - pointer to second coordinate (enthalpy).
    * \param[in] point_ids - single triangle data.
    * \param[out] interp_mat_inv - inverse matrix for interpolation.
-  */
-  void GetInterpMatInv(const su2double* vec_x, const su2double* vec_y, std::array<unsigned long,3>& point_ids,
+   */
+  void GetInterpMatInv(const su2double* vec_x, const su2double* vec_y, std::array<unsigned long, 3>& point_ids,
                        su2activematrix& interp_mat_inv);
 
   /*!
@@ -169,9 +167,9 @@ class CLookUpTable {
    * \param[in] val_y - value of second coordinate (enthalpy).
    * \param[in] interp_mat_inv - inverse matrix for interpolation.
    * \param[out] interp_coeffs - interpolation coefficients.
-  */
+   */
   void GetInterpCoeffs(su2double val_x, su2double val_y, su2activematrix& interp_mat_inv,
-                       std::array<su2double,3>& interp_coeffs);
+                       std::array<su2double, 3>& interp_coeffs);
 
   /*!
    * \brief compute interpolated value of a point P in the triangle.
@@ -179,11 +177,10 @@ class CLookUpTable {
    * \param[in] val_triangle - ID to the triangle.
    * \param[in] val_interp_coeffs - interpolation coefficients using the point data in P.
    * \returns resulting value of the interpolation.
-  */
-  su2double Interpolate(const su2double* val_samples, std::array<unsigned long,3>& val_triangle,
-                        std::array<su2double,3>& val_interp_coeffs);
+   */
+  su2double Interpolate(const su2double* val_samples, std::array<unsigned long, 3>& val_triangle,
+                        std::array<su2double, 3>& val_interp_coeffs);
 
-  
   /*!
    * \brief Perform linear interpolation between two table levels for a single variable.
    * \param[in] val_z - z-coordinate of the query point.
@@ -192,10 +189,9 @@ class CLookUpTable {
    * \param[in] lower_value - Result from x-y interpolation on the lower table level.
    * \param[in] upper_value - Result from x-y interpolation on the upper table level.
    * \param[in] val_vars - Pointer to interpolation result.
-  */
+   */
   void Linear_Interpolation(const su2double val_z, const unsigned long lower_level, const unsigned long upper_level,
-                            su2double &lower_value, su2double &upper_value, su2double* &var_vals) const;
-
+                            su2double& lower_value, su2double& upper_value, su2double*& var_vals) const;
 
   /*!
    * \brief Perform linear interpolation between two table levels for a vector of variables.
@@ -205,9 +201,10 @@ class CLookUpTable {
    * \param[in] lower_values - Results from x-y interpolation on the lower table level.
    * \param[in] upper_values - Results from x-y interpolation on the upper table level.
    * \param[in] val_vars - Pointer to interpolation results for all interpolation variables.
-  */
-  void Linear_Interpolation (const su2double val_z, const unsigned long lower_level, const unsigned long upper_level, 
-                            std::vector<su2double>&lower_values, std::vector<su2double>&upper_values, std::vector<su2double*>&var_vals) const;
+   */
+  void Linear_Interpolation(const su2double val_z, const unsigned long lower_level, const unsigned long upper_level,
+                            std::vector<su2double>& lower_values, std::vector<su2double>& upper_values,
+                            std::vector<su2double*>& var_vals) const;
 
   /*!
    * \brief find the point on the hull (boundary of the table) that is closest to the point P(val_x,val_y).
@@ -215,7 +212,7 @@ class CLookUpTable {
    * \param[in] val_y - second coordinate of point P(val_x,val_y) to check.
    * \returns point id of the nearest neighbor on the hull.
    */
-  unsigned long FindNearestNeighborOnHull(su2double val_x, su2double val_y, unsigned long i_level=0);
+  unsigned long FindNearestNeighborOnHull(su2double val_x, su2double val_y, unsigned long i_level = 0);
 
   /*!
    * \brief determine if a point P(val_x,val_y) is inside the triangle val_id_triangle.
@@ -224,7 +221,7 @@ class CLookUpTable {
    * \param[in] val_id_triangle - ID of the triangle to check.
    * \returns true if the point is in the triangle, false if it is outside.
    */
-  bool IsInTriangle(su2double val_x, su2double val_y, unsigned long val_id_triangle, unsigned long i_level=0);
+  bool IsInTriangle(su2double val_x, su2double val_y, unsigned long val_id_triangle, unsigned long i_level = 0);
 
   /*!
    * \brief compute the area of a triangle given the 3 points of the triangle.
@@ -256,7 +253,8 @@ class CLookUpTable {
    * \param[in] val_y - value of controlling variable 2.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
-  unsigned long LookUp_XY(const std::string& val_name_var, su2double* val_var, su2double val_x, su2double val_y, unsigned long i_level=0);
+  unsigned long LookUp_XY(const std::string& val_name_var, su2double* val_var, su2double val_x, su2double val_y,
+                          unsigned long i_level = 0);
 
   /*!
    * \brief lookup 1 value for each of the variables in "val_name_var" using controlling variable values(val_x,val_y).
@@ -266,8 +264,8 @@ class CLookUpTable {
    * \param[in] val_y - value of controlling variable 2.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
-  unsigned long LookUp_XY(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars, su2double val_x,
-                                su2double val_y, unsigned long i_level=0);
+  unsigned long LookUp_XY(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars,
+                          su2double val_x, su2double val_y, unsigned long i_level = 0);
 
   /*!
    * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_x,val_y).
@@ -277,11 +275,11 @@ class CLookUpTable {
    * \param[in] val_y - value of controlling variable 2.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
-  unsigned long LookUp_XY(const std::vector<std::string>& val_names_var, std::vector<su2double>& val_vars, su2double val_x,
-                                su2double val_y, unsigned long i_level=0);
+  unsigned long LookUp_XY(const std::vector<std::string>& val_names_var, std::vector<su2double>& val_vars,
+                          su2double val_x, su2double val_y, unsigned long i_level = 0);
 
   /*!
-   * \brief legacy version of the 2D lookup method for 1 value of the single variable "val_name_var" 
+   * \brief legacy version of the 2D lookup method for 1 value of the single variable "val_name_var"
             using controlling variable values(val_prog,val_enth).
    * \param[in] val_name_var - string name of the variable to look up.
    * \param[out] val_var - the stored value of the variable to look up.
@@ -291,10 +289,11 @@ class CLookUpTable {
    * \param[in] name_enth - name of the enthalpy variable.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
-  unsigned long LookUp_ProgEnth(const std::string& val_name_var, su2double* val_var, su2double val_prog, su2double val_enth, std::string name_prog, std::string name_enth);
+  unsigned long LookUp_ProgEnth(const std::string& val_name_var, su2double* val_var, su2double val_prog,
+                                su2double val_enth, std::string name_prog, std::string name_enth);
 
   /*!
-   * \brief legacy version of the 2D lookup method for 1 value for each of the variables in "val_name_var" 
+   * \brief legacy version of the 2D lookup method for 1 value for each of the variables in "val_name_var"
             using controlling variable values(val_x,val_y).
    * \param[in] val_name_var - vector of string names of the variables to look up.
    * \param[out] val_vars - pointer to the vector of stored values of the variables to look up.
@@ -304,11 +303,11 @@ class CLookUpTable {
    * \param[in] name_enth - name of the enthalpy variable.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
-  unsigned long LookUp_ProgEnth(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars, su2double val_prog,
-                                su2double val_enth, std::string name_prog, std::string name_enth);
+  unsigned long LookUp_ProgEnth(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars,
+                                su2double val_prog, su2double val_enth, std::string name_prog, std::string name_enth);
 
   /*!
-   * \brief legacy version of the 2D lookup method for 1 value for each of the variables in "val_name_var" 
+   * \brief legacy version of the 2D lookup method for 1 value for each of the variables in "val_name_var"
             using controlling variable values(val_x,val_y).
    * \param[in] val_name_var - vector of string names of the variables to look up.
    * \param[out] val_vars - pointer to the vector of stored values of the variables to look up.
@@ -318,8 +317,8 @@ class CLookUpTable {
    * \param[in] name_enth - name of the enthalpy variable.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
-  unsigned long LookUp_ProgEnth(const std::vector<std::string>& val_names_var, std::vector<su2double>& val_vars, su2double val_x,
-                                su2double val_y, std::string name_prog, std::string name_enth);                          
+  unsigned long LookUp_ProgEnth(const std::vector<std::string>& val_names_var, std::vector<su2double>& val_vars,
+                                su2double val_x, su2double val_y, std::string name_prog, std::string name_enth);
   /*!
    * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_x,val_y,val_z).
    * \param[in] val_name_var - string name of the variable to look up.
@@ -329,7 +328,8 @@ class CLookUpTable {
    * \param[in] val_z - value of controlling variable 3.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
-  unsigned long LookUp_XYZ(const std::string& val_name_var, su2double* val_var, su2double val_x, su2double val_y, su2double val_z);
+  unsigned long LookUp_XYZ(const std::string& val_name_var, su2double* val_var, su2double val_x, su2double val_y,
+                           su2double val_z);
 
   /*!
    * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_x,val_y,val_z).
@@ -340,15 +340,15 @@ class CLookUpTable {
    * \param[in] val_z - value of controlling variable 3.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
-  unsigned long LookUp_XYZ(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars, su2double val_x,
-                                su2double val_y, su2double val_z=0);
-  
+  unsigned long LookUp_XYZ(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars,
+                           su2double val_x, su2double val_y, su2double val_z = 0);
+
   /*!
-  * \brief Find the table levels with constant z-values directly above and below query val_z.
-  * \param[in] val_z - Z-coordinate of query point.
-  * \param[in] within_limits - Whether query point lies within table bounds.
-  * \returns pair of inclusion level indices (first = lower level index, second = upper level index)
-  */
+   * \brief Find the table levels with constant z-values directly above and below query val_z.
+   * \param[in] val_z - Z-coordinate of query point.
+   * \param[in] within_limits - Whether query point lies within table bounds.
+   * \returns pair of inclusion level indices (first = lower level index, second = upper level index)
+   */
   std::pair<unsigned long, unsigned long> FindInclusionLevels(const su2double val_z);
 
   /*!
@@ -366,6 +366,4 @@ class CLookUpTable {
   inline std::pair<su2double*, su2double*> GetTableLimitsX(unsigned long i_level = 0) const {
     return limits_table_x[i_level];
   }
-
-  
 };
diff --git a/Common/include/containers/CTrapezoidalMap.hpp b/Common/include/containers/CTrapezoidalMap.hpp
index aea6b11e124..b1fc7968b3d 100644
--- a/Common/include/containers/CTrapezoidalMap.hpp
+++ b/Common/include/containers/CTrapezoidalMap.hpp
@@ -36,13 +36,12 @@
 /*!
  * \class CTrapezoidalMap
  * \ingroup LookUpInterp
- * \brief Construction of trapezoidal map for tabulated lookup 
+ * \brief Construction of trapezoidal map for tabulated lookup
  * \author: D. Mayer, T. Economon
  * \version 7.5.0 "Blackbird"
  */
-  class CTrapezoidalMap {
+class CTrapezoidalMap {
  protected:
-
   /* The unique values of x which exist in the data */
   std::vector<su2double> unique_bands_x;
 
@@ -56,51 +55,45 @@
   su2vector<std::vector<std::pair<su2double, unsigned long> > > y_edge_at_band_mid;
 
  public:
-
   CTrapezoidalMap() = default;
 
-  CTrapezoidalMap(const su2double* samples_x,
-                  const su2double* samples_y,
-                  const unsigned long size,
-                  const std::vector<std::array<unsigned long,2> >& edges,
+  CTrapezoidalMap(const su2double* samples_x, const su2double* samples_y, const unsigned long size,
+                  const std::vector<std::array<unsigned long, 2> >& edges,
                   const su2vector<std::vector<unsigned long> >& edge_to_triangle);
 
   /*!
-   * \brief return the index to the triangle that contains the coordinates (val_x,val_y) 
-   * \param[in]  val_x  - x-coordinate or first independent variable 
+   * \brief return the index to the triangle that contains the coordinates (val_x,val_y)
+   * \param[in]  val_x  - x-coordinate or first independent variable
    * \param[in]  val_y  - y-coordinate or second independent variable
-   * \param[out] val_index - index to the triangle 
+   * \param[out] val_index - index to the triangle
    */
   unsigned long GetTriangle(su2double val_x, su2double val_y);
 
-
   /*!
-   * \brief get the indices of the vertical coordinate band (xmin,xmax) in the 2D search space 
-   * that contains the coordinate val_x  
-   * \param[in]  val_x  - x-coordinate or first independent variable 
-   * \param[out] val_band - a pair(i_low,i_up) , the lower index and upper index between which the value val_x 
-   * can be found 
+   * \brief get the indices of the vertical coordinate band (xmin,xmax) in the 2D search space
+   * that contains the coordinate val_x
+   * \param[in]  val_x  - x-coordinate or first independent variable
+   * \param[out] val_band - a pair(i_low,i_up) , the lower index and upper index between which the value val_x
+   * can be found
    */
   std::pair<unsigned long, unsigned long> GetBand(su2double val_x);
 
-
- /*!
-  * \brief for a given coordinate (val_x,value), known to be in the band (xmin,xmax) with band index (i_low,i_up),
-  * find the edges in the band (these edges come from the triangulation) that enclose the coordinate 
-  * \param[in]  val_band - pair i_low,i_up 
-  * \param[in]  val_x  - x-coordinate or first independent variable 
-  * \param[in]  val_y  - y-coordinate or first independent variable 
-  * \param[out] pair (edge_low,edge_up) - lower edge and upper edge of a triangle that encloses the coordinate 
-  */
-  std::pair<unsigned long, unsigned long> GetEdges(std::pair<unsigned long, unsigned long> val_band,
-                                                   su2double val_x,
+  /*!
+   * \brief for a given coordinate (val_x,value), known to be in the band (xmin,xmax) with band index (i_low,i_up),
+   * find the edges in the band (these edges come from the triangulation) that enclose the coordinate
+   * \param[in]  val_band - pair i_low,i_up
+   * \param[in]  val_x  - x-coordinate or first independent variable
+   * \param[in]  val_y  - y-coordinate or first independent variable
+   * \param[out] pair (edge_low,edge_up) - lower edge and upper edge of a triangle that encloses the coordinate
+   */
+  std::pair<unsigned long, unsigned long> GetEdges(std::pair<unsigned long, unsigned long> val_band, su2double val_x,
                                                    su2double val_y) const;
 
- /*!
-  * \brief determine if the x-coordinate falls within the bounds xmin,xmax of the table  
-  * \param[in]  val_x  - x-coordinate or first independent variable 
-  * \param[out] bool - true if val_x is within (xmin,xmax) 
-  */
+  /*!
+   * \brief determine if the x-coordinate falls within the bounds xmin,xmax of the table
+   * \param[in]  val_x  - x-coordinate or first independent variable
+   * \param[out] bool - true if val_x is within (xmin,xmax)
+   */
   inline bool IsInsideHullX(su2double val_x) {
     return (val_x >= unique_bands_x.front()) && (val_x <= unique_bands_x.back());
   }
diff --git a/Common/src/containers/CFileReaderLUT.cpp b/Common/src/containers/CFileReaderLUT.cpp
index d6382232181..4f288e8930a 100644
--- a/Common/src/containers/CFileReaderLUT.cpp
+++ b/Common/src/containers/CFileReaderLUT.cpp
@@ -62,32 +62,30 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
   table_dim = 2;
   bool found_level_count = false;
   while (GetNextNonEmptyLine(file_stream, line) && !eoHeader) {
-
     /*--- check version_lut ---*/
     if (line.compare("[Version]") == 0) {
       GetNextNonEmptyLine(file_stream, line);
       version_lut = line;
 
-      if(version_lut.compare("1.0.1") == 0){
+      if (version_lut.compare("1.0.1") == 0) {
         table_dim = 2;
         n_levels = 1;
         found_level_count = true;
         n_points.resize(n_levels);
         n_triangles.resize(n_levels);
         n_hull_points.resize(n_levels);
-      }else if(version_lut.compare("1.1.0") == 0){
+      } else if (version_lut.compare("1.1.0") == 0) {
         table_dim = 3;
-      }else{
+      } else {
         SU2_MPI::Error("Version conflict between LUT reader and LUT library file.", CURRENT_FUNCTION);
       }
     }
 
-    if (line.compare("[Number of table levels]") == 0)
-    {
+    if (line.compare("[Number of table levels]") == 0) {
       found_level_count = true;
       GetNextNonEmptyLine(file_stream, line);
       n_levels = stoul(line);
-      
+
       n_points.resize(n_levels);
       n_triangles.resize(n_levels);
       n_hull_points.resize(n_levels);
@@ -96,9 +94,9 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
 
     /*--- number of points in LUT ---*/
     if (line.compare("[Number of points]") == 0) {
-      if(!found_level_count)
+      if (!found_level_count)
         SU2_MPI::Error("Number of points provided before specifying level count.", CURRENT_FUNCTION);
-      for(unsigned long i_level=0; i_level<n_levels; i_level++){
+      for (unsigned long i_level = 0; i_level < n_levels; i_level++) {
         GetNextNonEmptyLine(file_stream, line);
         n_points[i_level] = stoi(line);
       }
@@ -106,9 +104,9 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
 
     /*--- number of triangles in LUT ---*/
     if (line.compare("[Number of triangles]") == 0) {
-      if(!found_level_count)
+      if (!found_level_count)
         SU2_MPI::Error("Number of triangles provided before specifying level count.", CURRENT_FUNCTION);
-      for(unsigned long i_level=0; i_level<n_levels; i_level++){
+      for (unsigned long i_level = 0; i_level < n_levels; i_level++) {
         GetNextNonEmptyLine(file_stream, line);
         n_triangles[i_level] = stoi(line);
       }
@@ -116,16 +114,16 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
 
     /*--- number of points on the hull ---*/
     if (line.compare("[Number of hull points]") == 0) {
-      if(!found_level_count)
+      if (!found_level_count)
         SU2_MPI::Error("Number of hull points provided before specifying level count.", CURRENT_FUNCTION);
-      for(unsigned long i_level=0; i_level<n_levels; i_level++){
+      for (unsigned long i_level = 0; i_level < n_levels; i_level++) {
         GetNextNonEmptyLine(file_stream, line);
         n_hull_points[i_level] = stoi(line);
       }
     }
 
     if (line.compare("[Table levels]") == 0) {
-      for(unsigned long i_level=0; i_level<n_levels; i_level++){
+      for (unsigned long i_level = 0; i_level < n_levels; i_level++) {
         GetNextNonEmptyLine(file_stream, line);
         table_levels[i_level] = stod(line);
       }
@@ -139,28 +137,25 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
     /*--- variable names ---*/
     if (line.compare("[Variable names]") == 0) {
       names_var.resize(n_variables);
-      for (unsigned long i = 0; i < n_variables; i++){
-
+      for (unsigned long i = 0; i < n_variables; i++) {
         /*--- grab a single line ---*/
         GetNextNonEmptyLine(file_stream, line);
-        names_var[i] = line.substr(line.find(":")+1); 
+        names_var[i] = line.substr(line.find(":") + 1);
       }
     }
 
     /*--- check if end of header is reached ---*/
     if (line.compare("</Header>") == 0) eoHeader = true;
   }
-    
 
   /*--- check header quantities ---*/
-  for(unsigned long i_level=0; i_level < n_levels; i_level++){
+  for (unsigned long i_level = 0; i_level < n_levels; i_level++) {
     if (n_points[i_level] == 0 || n_triangles[i_level] == 0 || n_variables == 0 || n_hull_points[i_level] == 0)
-    SU2_MPI::Error(
-        "Number of points, triangles, hull points, or variables in lookup table "
-        "library header is zero.",
-        CURRENT_FUNCTION);
+      SU2_MPI::Error(
+          "Number of points, triangles, hull points, or variables in lookup table "
+          "library header is zero.",
+          CURRENT_FUNCTION);
   }
-  
 
   /*--- check if number of variables is consistent ---*/
   if (n_variables != names_var.size())
@@ -171,20 +166,19 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
         CURRENT_FUNCTION);
 
   /*--- now that n_variables, n_points, n_hull_points and n_variables are available, allocate memory ---*/
-  if (rank == MASTER_NODE) cout << "allocating memory for the data, size = ( " << GetNVariables() << " , " << GetNPoints() << " )" << endl;
+  if (rank == MASTER_NODE)
+    cout << "allocating memory for the data, size = ( " << GetNVariables() << " , " << GetNPoints() << " )" << endl;
   table_data.resize(n_levels);
-  for(unsigned long i_level=0; i_level<n_levels; i_level++)
+  for (unsigned long i_level = 0; i_level < n_levels; i_level++)
     table_data[i_level].resize(GetNVariables(), GetNPoints(i_level));
 
-  if (rank == MASTER_NODE) cout << "allocating memory for the triangles, size = "<< GetNTriangles() << endl;
+  if (rank == MASTER_NODE) cout << "allocating memory for the triangles, size = " << GetNTriangles() << endl;
   triangles.resize(n_levels);
-  for(unsigned long i_level=0; i_level<n_levels; i_level++)
-    triangles[i_level].resize(GetNTriangles(i_level), 3);
+  for (unsigned long i_level = 0; i_level < n_levels; i_level++) triangles[i_level].resize(GetNTriangles(i_level), 3);
 
   if (rank == MASTER_NODE) cout << "allocating memory for the hull points, size = " << GetNHullPoints() << endl;
   hull.resize(n_levels);
-  for(unsigned long i_level=0; i_level<n_levels; i_level++)
-    hull[i_level].resize(GetNHullPoints(i_level));
+  for (unsigned long i_level = 0; i_level < n_levels; i_level++) hull[i_level].resize(GetNHullPoints(i_level));
 
   /*--- flush any cout ---*/
   if (rank == MASTER_NODE) cout << endl;
@@ -197,26 +191,25 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
   unsigned long pointCounter = 0;
   unsigned long levelCounter = 0;
   while (GetNextNonEmptyLine(file_stream, line) && !eoData) {
-
     /*--- check if end of data is reached ---*/
     if (line.compare("</Data>") == 0) eoData = true;
 
     if (!eoData) {
-      if(line.compare("<Level>") == 0){
+      if (line.compare("<Level>") == 0) {
         eoLevel = false;
         pointCounter = 0;
         GetNextNonEmptyLine(file_stream, line);
       }
-      if(line.compare("</Level>") == 0){
+      if (line.compare("</Level>") == 0) {
         eoLevel = true;
         if (n_points[levelCounter] != pointCounter)
-        SU2_MPI::Error(
-            "Number of read points on level " + std::to_string(levelCounter) + " does not match number of points "
-            "specified in lookup table library header.",
-            CURRENT_FUNCTION);
+          SU2_MPI::Error("Number of read points on level " + std::to_string(levelCounter) +
+                             " does not match number of points "
+                             "specified in lookup table library header.",
+                         CURRENT_FUNCTION);
         levelCounter++;
       }
-      if(!eoLevel || (table_dim == 2)){
+      if (!eoLevel || (table_dim == 2)) {
         /*--- one line contains values for one point for all variables ---*/
         istringstream streamDataLine(line);
 
@@ -231,8 +224,6 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
     }
   }
 
-  
-
   /*--- read connectivity ---*/
   if (rank == MASTER_NODE) cout << "loading connectivity block" << endl;
 
@@ -241,34 +232,33 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
   eoLevel = true;
   levelCounter = 0;
   while (GetNextNonEmptyLine(file_stream, line) && !eoConnectivity) {
-    if (!line.empty() && (line[line.length()-1] == '\n' || line[line.length()-1] == '\r' )) {
-      line.erase(line.length()-1);
+    if (!line.empty() && (line[line.length() - 1] == '\n' || line[line.length() - 1] == '\r')) {
+      line.erase(line.length() - 1);
     }
     /*--- check if end of data is reached ---*/
     if (line.compare("</Connectivity>") == 0) eoConnectivity = true;
 
     if (!eoConnectivity) {
-      if(line.compare("<Level>") == 0){
+      if (line.compare("<Level>") == 0) {
         eoLevel = false;
         triCounter = 0;
         GetNextNonEmptyLine(file_stream, line);
       }
-      if(line.compare("</Level>") == 0){
+      if (line.compare("</Level>") == 0) {
         eoLevel = true;
         if (n_triangles[levelCounter] != triCounter)
-        SU2_MPI::Error(
-            "Number of read triangles on level " + std::to_string(levelCounter) + " does not match number of triangles "
-            "specified in lookup table library header.",
-            CURRENT_FUNCTION);
+          SU2_MPI::Error("Number of read triangles on level " + std::to_string(levelCounter) +
+                             " does not match number of triangles "
+                             "specified in lookup table library header.",
+                         CURRENT_FUNCTION);
         levelCounter++;
       }
-      if(!eoLevel || (table_dim == 2)){
+      if (!eoLevel || (table_dim == 2)) {
         /*--- one line contains values for one triangle (3 points) ---*/
         istringstream streamTriLine(line);
 
         /*--- add next line to triangles ---*/
         for (int iPoint = 0; iPoint < 3; iPoint++) {
-
           streamTriLine >> word;
 
           /*--- lookup table index starts with 1, convert to c++ indexing starting with 0: ---*/
@@ -277,7 +267,6 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
         triCounter++;
       }
     }
-    
   }
 
   /*--- read hull points ---*/
@@ -288,28 +277,28 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
   eoLevel = true;
   levelCounter = 0;
   while (GetNextNonEmptyLine(file_stream, line) && !eoHull) {
-    if (!line.empty() && (line[line.length()-1] == '\n' || line[line.length()-1] == '\r' )) {
-      line.erase(line.length()-1);
+    if (!line.empty() && (line[line.length() - 1] == '\n' || line[line.length() - 1] == '\r')) {
+      line.erase(line.length() - 1);
     }
     /*--- check if end of data is reached ---*/
     if (line.compare("</Hull>") == 0) eoHull = true;
 
     if (!eoHull) {
-      if(line.compare("<Level>") == 0){
+      if (line.compare("<Level>") == 0) {
         eoLevel = false;
         hullCounter = 0;
         GetNextNonEmptyLine(file_stream, line);
       }
-      if(line.compare("</Level>") == 0){
+      if (line.compare("</Level>") == 0) {
         eoLevel = true;
         if (n_hull_points[levelCounter] != hullCounter)
-        SU2_MPI::Error(
-            "Number of read hull nodes on level " + std::to_string(levelCounter) + " does not match number of hull nodes "
-            "specified in lookup table library header.",
-            CURRENT_FUNCTION);
+          SU2_MPI::Error("Number of read hull nodes on level " + std::to_string(levelCounter) +
+                             " does not match number of hull nodes "
+                             "specified in lookup table library header.",
+                         CURRENT_FUNCTION);
         levelCounter++;
       }
-      if(!eoLevel || (table_dim == 2)){
+      if (!eoLevel || (table_dim == 2)) {
         /*--- one line contains one point ID for one point on the hull  ---*/
         istringstream streamHullLine(line);
 
@@ -319,11 +308,10 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
         hull[levelCounter][hullCounter] = stol(word) - 1;
         hullCounter++;
       }
-      }
+    }
   }
 
   file_stream.close();
-
 }
 
 void CFileReaderLUT::SkipToFlag(ifstream& file_stream, const string& current_line, const string& flag) const {
@@ -342,12 +330,11 @@ void CFileReaderLUT::SkipToFlag(ifstream& file_stream, const string& current_lin
 }
 
 bool CFileReaderLUT::GetNextNonEmptyLine(ifstream& file_stream, string& line) const {
-
   /*--- get next line and save return value ---*/
   bool return_value = GetStrippedLine(file_stream, line);
-  
+
   /*--- skip empty lines ---*/
-  while (line.empty() && !(file_stream).eof()){
+  while (line.empty() && !(file_stream).eof()) {
     return_value = GetStrippedLine(file_stream, line);
   }
 
@@ -356,16 +343,15 @@ bool CFileReaderLUT::GetNextNonEmptyLine(ifstream& file_stream, string& line) co
 }
 
 bool CFileReaderLUT::GetStrippedLine(ifstream& file_stream, string& line) const {
+  /*--- get next line and save return value ---*/
+  getline(file_stream, line);
 
-    /*--- get next line and save return value ---*/
-    getline(file_stream, line);
-
-    /*--- find last non-control-character character ---*/
-    size_t end = line.find_last_not_of(" \n\r\t\f\v");
+  /*--- find last non-control-character character ---*/
+  size_t end = line.find_last_not_of(" \n\r\t\f\v");
 
-    /*--- clean up line ---*/
-    line = (end == string::npos) ? "" : line.substr(0, end + 1);
+  /*--- clean up line ---*/
+  line = (end == string::npos) ? "" : line.substr(0, end + 1);
 
-    /*--- return true if line is not empty, else return false ---*/
-    return !line.empty();
-  }
\ No newline at end of file
+  /*--- return true if line is not empty, else return false ---*/
+  return !line.empty();
+}
\ No newline at end of file
diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index 5be9cb26348..e9222b0b6b4 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -26,17 +26,14 @@
  */
 
 #include "../../../Common/include/containers/CLookUpTable.hpp"
+
 #include "../../../Common/include/linear_algebra/blas_structure.hpp"
 #include "../../../Common/include/toolboxes/CSquareMatrixCM.hpp"
 
 using namespace std;
 
-CLookUpTable::CLookUpTable(const string& var_file_name_lut, const string& name_CV1_in, const string& name_CV2_in) :
-file_name_lut{var_file_name_lut}, 
-name_CV1{name_CV1_in}, 
-name_CV2{name_CV2_in} 
-{
-
+CLookUpTable::CLookUpTable(const string& var_file_name_lut, const string& name_CV1_in, const string& name_CV2_in)
+    : file_name_lut{var_file_name_lut}, name_CV1{name_CV1_in}, name_CV2{name_CV2_in} {
   rank = SU2_MPI::GetRank();
 
   LoadTableRaw(var_file_name_lut);
@@ -50,78 +47,75 @@ name_CV2{name_CV2_in}
 
   IdentifyUniqueEdges();
 
-  if (rank == MASTER_NODE) 
-    cout << " done." << endl;
+  if (rank == MASTER_NODE) cout << " done." << endl;
 
   PrintTableInfo();
 
-  if (rank == MASTER_NODE)
-  switch (table_dim)
-  {
-  case 2:
-    cout << "Building a trapezoidal map for the (" + name_CV1 + ", " + name_CV2 + ") "
-            "space ..."
-         << endl;
-    break;
-  case 3:
-    cout << "Building trapezoidal map stack for the (" + name_CV1 + ", " + name_CV2 + ") "
-              "space ..."
-          << endl;
-    break;
-  default:
-    break;
-  }
+  if (rank == MASTER_NODE) switch (table_dim) {
+      case 2:
+        cout << "Building a trapezoidal map for the (" + name_CV1 + ", " + name_CV2 +
+                    ") "
+                    "space ..."
+             << endl;
+        break;
+      case 3:
+        cout << "Building trapezoidal map stack for the (" + name_CV1 + ", " + name_CV2 +
+                    ") "
+                    "space ..."
+             << endl;
+        break;
+      default:
+        break;
+    }
 
   trap_map_x_y.resize(n_table_levels);
   su2double startTime = SU2_MPI::Wtime();
-  unsigned short barwidth=65;
-  for(auto i_level = 0ul; i_level<n_table_levels; i_level++){
-    trap_map_x_y[i_level] = CTrapezoidalMap(GetDataP(name_CV1, i_level), GetDataP(name_CV2, i_level), table_data[i_level].cols(), edges[i_level], edge_to_triangle[i_level]);
+  unsigned short barwidth = 65;
+  for (auto i_level = 0ul; i_level < n_table_levels; i_level++) {
+    trap_map_x_y[i_level] = CTrapezoidalMap(GetDataP(name_CV1, i_level), GetDataP(name_CV2, i_level),
+                                            table_data[i_level].cols(), edges[i_level], edge_to_triangle[i_level]);
     /* Display a progress bar to monitor table generation process */
-    if(rank == MASTER_NODE){
+    if (rank == MASTER_NODE) {
       su2double progress = su2double(i_level) / n_table_levels;
-      auto completed = floor(progress*barwidth);
+      auto completed = floor(progress * barwidth);
       auto to_do = barwidth - completed;
       cout << "[" << setfill('=') << setw(completed);
       cout << '>';
-      cout << setfill(' ') << setw(to_do) << std::right << "] " << 100*progress << "%\r";
+      cout << setfill(' ') << setw(to_do) << std::right << "] " << 100 * progress << "%\r";
       cout.flush();
     }
   }
   su2double stopTime = SU2_MPI::Wtime();
 
-  if (rank == MASTER_NODE){
-    switch (table_dim)
-    {
-    case 2:
-      cout << "Construction of trapezoidal map took " << stopTime-startTime << " seconds\n" << endl;
-      break;
-    case 3:
-      cout << "Construction of trapezoidal map stack took " << stopTime-startTime << " seconds\n" << endl;
-      break;
-    default:
-      break;
+  if (rank == MASTER_NODE) {
+    switch (table_dim) {
+      case 2:
+        cout << "Construction of trapezoidal map took " << stopTime - startTime << " seconds\n" << endl;
+        break;
+      case 3:
+        cout << "Construction of trapezoidal map stack took " << stopTime - startTime << " seconds\n" << endl;
+        break;
+      default:
+        break;
     }
     cout << "Precomputing interpolation coefficients..." << endl;
   }
-    
+
   ComputeInterpCoeffs();
 
-  if (rank == MASTER_NODE) 
-    cout << "LUT fluid model ready for use" << endl;
+  if (rank == MASTER_NODE) cout << "LUT fluid model ready for use" << endl;
 }
 
 void CLookUpTable::LoadTableRaw(const string& var_file_name_lut) {
   CFileReaderLUT file_reader;
 
-  if (rank == MASTER_NODE) 
-    cout << "Loading lookup table, filename = " << var_file_name_lut << " ..." << endl;
+  if (rank == MASTER_NODE) cout << "Loading lookup table, filename = " << var_file_name_lut << " ..." << endl;
 
   file_reader.ReadRawLUT(var_file_name_lut);
   table_dim = file_reader.GetTableDim();
   n_table_levels = file_reader.GetNLevels();
 
-  n_points.resize(n_table_levels); 
+  n_points.resize(n_table_levels);
   n_triangles.resize(n_table_levels);
   n_hull_points.resize(n_table_levels);
   table_data.resize(n_table_levels);
@@ -131,7 +125,7 @@ void CLookUpTable::LoadTableRaw(const string& var_file_name_lut) {
   edges.resize(n_table_levels);
   edge_to_triangle.resize(n_table_levels);
 
-  for(unsigned long i_level=0; i_level<n_table_levels; i_level++){
+  for (unsigned long i_level = 0; i_level < n_table_levels; i_level++) {
     n_points[i_level] = file_reader.GetNPoints(i_level);
     n_triangles[i_level] = file_reader.GetNTriangles(i_level);
     n_hull_points[i_level] = file_reader.GetNHullPoints(i_level);
@@ -139,37 +133,37 @@ void CLookUpTable::LoadTableRaw(const string& var_file_name_lut) {
     triangles[i_level] = file_reader.GetTriangles(i_level);
     hull[i_level] = file_reader.GetHull(i_level);
   }
-  
+
   n_variables = file_reader.GetNVariables();
   version_lut = file_reader.GetVersionLUT();
   version_reader = file_reader.GetVersionReader();
   names_var = file_reader.GetNamesVar();
 
-  if(table_dim == 3){
+  if (table_dim == 3) {
     z_values_levels.resize(n_table_levels);
-    for(unsigned long i_level=0; i_level<n_table_levels; i_level++){
+    for (unsigned long i_level = 0; i_level < n_table_levels; i_level++) {
       z_values_levels[i_level] = file_reader.GetTableLevel(i_level);
     }
   }
-  if (rank == MASTER_NODE) 
-    cout << " done." << endl;
+  if (rank == MASTER_NODE) cout << " done." << endl;
 }
 
 void CLookUpTable::FindTableLimits(const string& name_cv1, const string& name_cv2) {
-  int idx_X = GetIndexOfVar(name_cv1);
-  int idx_Y = GetIndexOfVar(name_cv2);
+  int idx_CV1 = GetIndexOfVar(name_cv1);
+  int idx_CV2 = GetIndexOfVar(name_cv2);
   limits_table_x.resize(n_table_levels);
   limits_table_y.resize(n_table_levels);
 
   /* we find the lowest and highest value of y and x in the table */
-  for(auto i_level=0u; i_level<n_table_levels; i_level++)
-  {
-    limits_table_y[i_level] = minmax_element(table_data[i_level][idx_Y], table_data[i_level][idx_Y]+table_data[i_level].cols());
-    limits_table_x[i_level] = minmax_element(table_data[i_level][idx_X], table_data[i_level][idx_X]+table_data[i_level].cols());
+  for (auto i_level = 0u; i_level < n_table_levels; i_level++) {
+    limits_table_y[i_level] =
+        minmax_element(table_data[i_level][idx_CV2], table_data[i_level][idx_CV2] + table_data[i_level].cols());
+    limits_table_x[i_level] =
+        minmax_element(table_data[i_level][idx_CV1], table_data[i_level][idx_CV1] + table_data[i_level].cols());
   }
 
-  if(table_dim == 3){
-    limits_table_z = minmax_element(&z_values_levels[0], &z_values_levels[0]+z_values_levels.cols());
+  if (table_dim == 3) {
+    limits_table_z = minmax_element(&z_values_levels[0], &z_values_levels[0] + z_values_levels.cols());
   }
 }
 
@@ -186,8 +180,9 @@ void CLookUpTable::PrintTableInfo() {
     cout << "| Table dimension:" << setw(48) << right << table_dim << " |" << endl;
     cout << "| Number of variables:" << setw(44) << right << n_variables << " |" << endl;
 
-    su2double n_points_av = 0, n_tria_av = 0, n_edges_av = 0, min_x=1/EPS, max_x = -1/EPS, min_y=1/EPS, max_y = -1/EPS;
-    for(auto i_level=0ul; i_level<n_table_levels; i_level++){
+    su2double n_points_av = 0, n_tria_av = 0, n_edges_av = 0, min_x = 1 / EPS, max_x = -1 / EPS, min_y = 1 / EPS,
+              max_y = -1 / EPS;
+    for (auto i_level = 0ul; i_level < n_table_levels; i_level++) {
       n_points_av += n_points[i_level] / n_table_levels;
       n_tria_av += n_triangles[i_level] / n_table_levels;
       n_edges_av += edges[i_level].size() / n_table_levels;
@@ -196,191 +191,186 @@ void CLookUpTable::PrintTableInfo() {
       max_x = max(max_x, *limits_table_x[i_level].second);
       max_y = max(max_y, *limits_table_y[i_level].second);
     }
-    switch (table_dim)
-    {
-    case 2:
-      cout << "| Number of points:" << setw(47) << right << n_points_av << " |" << endl;
-      cout << "| Number of triangles:" << setw(44) << right << n_tria_av << " |" << endl;
-      cout << "| Number of edges:" << setw(48) << right << n_edges_av << " |" << endl;
-      cout << "+------------------------------------------------------------------+" << endl;
-      cout << "| Minimum Y:" << setw(54) << right << min_y << " |" << endl;
-      cout << "| Maximum Y:" << setw(54) << right << max_y << " |" << endl;
-      cout << "| Minimum X:" << setw(54) << right << min_x << " |" << endl;
-      cout << "| Maximum X:" << setw(54) << right << max_x << " |" << endl;
-      cout << "+------------------------------------------------------------------+" << endl;
-      cout << "| Variable names:                                                  |" << endl;
-      cout << "|                                                                  |" << endl;
-
-      for (unsigned long i_var = 0; i_var < names_var.size(); i_var++)
-        cout << "| " << right << setw(3) << i_var << ": " << left << setw(59) << names_var[i_var] << " |" << endl;
-
-      cout << "+------------------------------------------------------------------+" << endl;
-
-      cout << endl;
-      break;
-    case 3:
-      
-      cout << "| Number of table levels:" << setw(41) << right << n_table_levels << " |" << endl;
-      cout << "| Average number of points:" << setw(39) << right << floor(n_points_av) << " |" << endl;
-      cout << "| Average number of triangles:" << setw(36) << right << floor(n_tria_av) << " |" << endl;
-      cout << "| Average number of edges:" << setw(40) << right << floor(n_edges_av) << " |" << endl;
-      cout << "+------------------------------------------------------------------+" << endl;
-      cout << "| Minimum Z:" << setw(54) << right << limits_table_z.first << " |" << endl;
-      cout << "| Maximum Z:" << setw(54) << right << limits_table_z.second << " |" << endl;
-      cout << "| Minimum Y:" << setw(54) << right << min_y << " |" << endl;
-      cout << "| Maximum Y:" << setw(54) << right << max_y << " |" << endl;
-      cout << "| Minimum X:" << setw(54) << right << min_x << " |" << endl;
-      cout << "| Maximum X:" << setw(54) << right << max_x << " |" << endl;
-      cout << "+------------------------------------------------------------------+" << endl;
-      cout << "| Variable names:                                                  |" << endl;
-      cout << "|                                                                  |" << endl;
-
-      for (unsigned long i_var = 0; i_var < names_var.size(); i_var++)
-        cout << "| " << right << setw(3) << i_var << ": " << left << setw(59) << names_var[i_var] << " |" << endl;
-
-      cout << "+------------------------------------------------------------------+" << endl;
-      break;
-    default:
-      break;
+    switch (table_dim) {
+      case 2:
+        cout << "| Number of points:" << setw(47) << right << n_points_av << " |" << endl;
+        cout << "| Number of triangles:" << setw(44) << right << n_tria_av << " |" << endl;
+        cout << "| Number of edges:" << setw(48) << right << n_edges_av << " |" << endl;
+        cout << "+------------------------------------------------------------------+" << endl;
+        cout << "| Minimum Y:" << setw(54) << right << min_y << " |" << endl;
+        cout << "| Maximum Y:" << setw(54) << right << max_y << " |" << endl;
+        cout << "| Minimum X:" << setw(54) << right << min_x << " |" << endl;
+        cout << "| Maximum X:" << setw(54) << right << max_x << " |" << endl;
+        cout << "+------------------------------------------------------------------+" << endl;
+        cout << "| Variable names:                                                  |" << endl;
+        cout << "|                                                                  |" << endl;
+
+        for (unsigned long i_var = 0; i_var < names_var.size(); i_var++)
+          cout << "| " << right << setw(3) << i_var << ": " << left << setw(59) << names_var[i_var] << " |" << endl;
+
+        cout << "+------------------------------------------------------------------+" << endl;
+
+        cout << endl;
+        break;
+      case 3:
+
+        cout << "| Number of table levels:" << setw(41) << right << n_table_levels << " |" << endl;
+        cout << "| Average number of points:" << setw(39) << right << floor(n_points_av) << " |" << endl;
+        cout << "| Average number of triangles:" << setw(36) << right << floor(n_tria_av) << " |" << endl;
+        cout << "| Average number of edges:" << setw(40) << right << floor(n_edges_av) << " |" << endl;
+        cout << "+------------------------------------------------------------------+" << endl;
+        cout << "| Minimum Z:" << setw(54) << right << limits_table_z.first << " |" << endl;
+        cout << "| Maximum Z:" << setw(54) << right << limits_table_z.second << " |" << endl;
+        cout << "| Minimum Y:" << setw(54) << right << min_y << " |" << endl;
+        cout << "| Maximum Y:" << setw(54) << right << max_y << " |" << endl;
+        cout << "| Minimum X:" << setw(54) << right << min_x << " |" << endl;
+        cout << "| Maximum X:" << setw(54) << right << max_x << " |" << endl;
+        cout << "+------------------------------------------------------------------+" << endl;
+        cout << "| Variable names:                                                  |" << endl;
+        cout << "|                                                                  |" << endl;
+
+        for (unsigned long i_var = 0; i_var < names_var.size(); i_var++)
+          cout << "| " << right << setw(3) << i_var << ": " << left << setw(59) << names_var[i_var] << " |" << endl;
+
+        cout << "+------------------------------------------------------------------+" << endl;
+        break;
+      default:
+        break;
     }
   }
 }
 
 void CLookUpTable::IdentifyUniqueEdges() {
+  for (auto i_level = 0u; i_level < n_table_levels; i_level++) {
+    /* loop through elements and store the vector of element IDs (neighbors)
+       for each of the points in the table */
 
-  for(auto i_level=0u; i_level<n_table_levels; i_level++){
-
-  /* loop through elements and store the vector of element IDs (neighbors)
-     for each of the points in the table */
-
-  vector<vector<unsigned long> > neighborElemsOfPoint;
-  
-  neighborElemsOfPoint.resize(n_points[i_level]);
-  for (unsigned long iElem = 0; iElem < n_triangles[i_level]; iElem++) {
-    /* loop over 3 points per triangle */
-    for (unsigned long iPoint = 0; iPoint < N_POINTS_TRIANGLE; iPoint++) {
-      /* get the global ID of the current point */
-      const unsigned long GlobalIndex = triangles[i_level][iElem][iPoint];
+    vector<vector<unsigned long> > neighborElemsOfPoint;
 
-      /* add the current element ID to the neighbor list for this point */
-      neighborElemsOfPoint[GlobalIndex].push_back(iElem);
-    }
-  }
-
-  /* remove duplicates from the neighboring element lists*/
-  vector<unsigned long>::iterator vecIt;
-  for (unsigned long iPoint = 0; iPoint < n_points[i_level]; iPoint++) {
-    /* sort neighboring elements for each point */
-    sort(neighborElemsOfPoint[iPoint].begin(), neighborElemsOfPoint[iPoint].end());
-
-    /* uniquify list of neighboring elements */
-    vecIt = unique(neighborElemsOfPoint[iPoint].begin(), neighborElemsOfPoint[iPoint].end());
-
-    /* adjust size of vector */
-    neighborElemsOfPoint[iPoint].resize(vecIt - neighborElemsOfPoint[iPoint].begin());
-  }
-
-  /* loop through all neighboring elements of each point and store
-     the point IDs that are neighboring points */
-  vector<vector<unsigned long> > neighborPointsOfPoint;
-  neighborPointsOfPoint.resize(n_points[i_level]);
-  for (unsigned long iPoint = 0; iPoint < n_points[i_level]; iPoint++) {
-    for (unsigned long iElem = 0; iElem < neighborElemsOfPoint[iPoint].size(); iElem++) {
-      /* loop over element points */
-      for (unsigned long jPoint = 0; jPoint < N_POINTS_TRIANGLE; jPoint++) {
+    neighborElemsOfPoint.resize(n_points[i_level]);
+    for (unsigned long iElem = 0; iElem < n_triangles[i_level]; iElem++) {
+      /* loop over 3 points per triangle */
+      for (unsigned long iPoint = 0; iPoint < N_POINTS_TRIANGLE; iPoint++) {
         /* get the global ID of the current point */
-        const unsigned long GlobalIndex = triangles[i_level][neighborElemsOfPoint[iPoint][iElem]][jPoint];
+        const unsigned long GlobalIndex = triangles[i_level][iElem][iPoint];
 
         /* add the current element ID to the neighbor list for this point */
-        if (GlobalIndex != iPoint) neighborPointsOfPoint[iPoint].push_back(GlobalIndex);
+        neighborElemsOfPoint[GlobalIndex].push_back(iElem);
       }
     }
-  }
 
-  /* remove duplicates from the neighboring points lists */
-  for (unsigned long iPoint = 0; iPoint < n_points[i_level]; iPoint++) {
-    /* sort neighboring points for each point */
-    sort(neighborPointsOfPoint[iPoint].begin(), neighborPointsOfPoint[iPoint].end());
+    /* remove duplicates from the neighboring element lists*/
+    vector<unsigned long>::iterator vecIt;
+    for (unsigned long iPoint = 0; iPoint < n_points[i_level]; iPoint++) {
+      /* sort neighboring elements for each point */
+      sort(neighborElemsOfPoint[iPoint].begin(), neighborElemsOfPoint[iPoint].end());
 
-    /* uniquify list of neighboring elements */
-    vecIt = unique(neighborPointsOfPoint[iPoint].begin(), neighborPointsOfPoint[iPoint].end());
+      /* uniquify list of neighboring elements */
+      vecIt = unique(neighborElemsOfPoint[iPoint].begin(), neighborElemsOfPoint[iPoint].end());
 
-    /* adjust size of vector */
-    neighborPointsOfPoint[iPoint].resize(vecIt - neighborPointsOfPoint[iPoint].begin());
-  }
+      /* adjust size of vector */
+      neighborElemsOfPoint[iPoint].resize(vecIt - neighborElemsOfPoint[iPoint].begin());
+    }
 
-  /* loop through our point neighbors and fill the vector of the unique
-     point pairs making up each edge in the grid. We impose a requirement
-     that the smaller global index is in the first position and the larger
-     is in the second to make for a unique set, so there's no need to
-     remove duplicates. */
-  for (unsigned long iPoint = 0; iPoint < n_points[i_level]; iPoint++) {
-    for (unsigned long jPoint = 0; jPoint < neighborPointsOfPoint[iPoint].size(); jPoint++) {
-      /* Store the neighbor index more clearly. */
-      const unsigned long GlobalIndex = neighborPointsOfPoint[iPoint][jPoint];
-
-      /* Store the edge so that the lower index of the pair is always first. */
-      if (iPoint < GlobalIndex) {
-        std::array<unsigned long,2> edge;
-        edge[0] = iPoint;
-        edge[1] = GlobalIndex;
-        edges[i_level].push_back(edge);
+    /* loop through all neighboring elements of each point and store
+       the point IDs that are neighboring points */
+    vector<vector<unsigned long> > neighborPointsOfPoint;
+    neighborPointsOfPoint.resize(n_points[i_level]);
+    for (unsigned long iPoint = 0; iPoint < n_points[i_level]; iPoint++) {
+      for (unsigned long iElem = 0; iElem < neighborElemsOfPoint[iPoint].size(); iElem++) {
+        /* loop over element points */
+        for (unsigned long jPoint = 0; jPoint < N_POINTS_TRIANGLE; jPoint++) {
+          /* get the global ID of the current point */
+          const unsigned long GlobalIndex = triangles[i_level][neighborElemsOfPoint[iPoint][iElem]][jPoint];
+
+          /* add the current element ID to the neighbor list for this point */
+          if (GlobalIndex != iPoint) neighborPointsOfPoint[iPoint].push_back(GlobalIndex);
+        }
       }
     }
-  }
 
+    /* remove duplicates from the neighboring points lists */
+    for (unsigned long iPoint = 0; iPoint < n_points[i_level]; iPoint++) {
+      /* sort neighboring points for each point */
+      sort(neighborPointsOfPoint[iPoint].begin(), neighborPointsOfPoint[iPoint].end());
 
-  /* Loop over our edges data structure. For the first point in each
-   pair, loop through the neighboring elements and store the two
-   elements that contain the second point in the edge ('left' and 'right' of the edge). */
-  edge_to_triangle[i_level].resize(edges[i_level].size());
-  for (unsigned long iEdge = 0; iEdge < edges[i_level].size(); iEdge++) {
-    /* Store the two points of the edge more clearly. */
-    const unsigned long iPoint = edges[i_level][iEdge][0];
-    const unsigned long jPoint = edges[i_level][iEdge][1];
+      /* uniquify list of neighboring elements */
+      vecIt = unique(neighborPointsOfPoint[iPoint].begin(), neighborPointsOfPoint[iPoint].end());
 
-    /* Loop over all neighboring elements to iPoint. */
-    for (unsigned long iElem = 0; iElem < neighborElemsOfPoint[iPoint].size(); iElem++) {
-      /* loop over 3 points per triangle */
-      for (unsigned long kPoint = 0; kPoint < N_POINTS_TRIANGLE; kPoint++) {
-        /* Get the global ID of the current point. */
-        const unsigned long GlobalIndex = triangles[i_level][neighborElemsOfPoint[iPoint][iElem]][kPoint];
+      /* adjust size of vector */
+      neighborPointsOfPoint[iPoint].resize(vecIt - neighborPointsOfPoint[iPoint].begin());
+    }
 
-        /* Add the current element ID to the neighbor list for this point. */
-        if (GlobalIndex == jPoint) edge_to_triangle[i_level][iEdge].push_back(neighborElemsOfPoint[iPoint][iElem]);
+    /* loop through our point neighbors and fill the vector of the unique
+       point pairs making up each edge in the grid. We impose a requirement
+       that the smaller global index is in the first position and the larger
+       is in the second to make for a unique set, so there's no need to
+       remove duplicates. */
+    for (unsigned long iPoint = 0; iPoint < n_points[i_level]; iPoint++) {
+      for (unsigned long jPoint = 0; jPoint < neighborPointsOfPoint[iPoint].size(); jPoint++) {
+        /* Store the neighbor index more clearly. */
+        const unsigned long GlobalIndex = neighborPointsOfPoint[iPoint][jPoint];
+
+        /* Store the edge so that the lower index of the pair is always first. */
+        if (iPoint < GlobalIndex) {
+          std::array<unsigned long, 2> edge;
+          edge[0] = iPoint;
+          edge[1] = GlobalIndex;
+          edges[i_level].push_back(edge);
+        }
+      }
+    }
+
+    /* Loop over our edges data structure. For the first point in each
+     pair, loop through the neighboring elements and store the two
+     elements that contain the second point in the edge ('left' and 'right' of the edge). */
+    edge_to_triangle[i_level].resize(edges[i_level].size());
+    for (unsigned long iEdge = 0; iEdge < edges[i_level].size(); iEdge++) {
+      /* Store the two points of the edge more clearly. */
+      const unsigned long iPoint = edges[i_level][iEdge][0];
+      const unsigned long jPoint = edges[i_level][iEdge][1];
+
+      /* Loop over all neighboring elements to iPoint. */
+      for (unsigned long iElem = 0; iElem < neighborElemsOfPoint[iPoint].size(); iElem++) {
+        /* loop over 3 points per triangle */
+        for (unsigned long kPoint = 0; kPoint < N_POINTS_TRIANGLE; kPoint++) {
+          /* Get the global ID of the current point. */
+          const unsigned long GlobalIndex = triangles[i_level][neighborElemsOfPoint[iPoint][iElem]][kPoint];
+
+          /* Add the current element ID to the neighbor list for this point. */
+          if (GlobalIndex == jPoint) edge_to_triangle[i_level][iEdge].push_back(neighborElemsOfPoint[iPoint][iElem]);
+        }
       }
     }
-  }
   }
 }
 
 void CLookUpTable::ComputeInterpCoeffs() {
-  for(auto i_level=0ul; i_level<n_table_levels; i_level++){
+  for (auto i_level = 0ul; i_level < n_table_levels; i_level++) {
     /* build KD tree for y, x space */
 
     std::array<unsigned long, 3> next_triangle;
 
-    const su2double* val_x = GetDataP(name_CV1, i_level);
-    const su2double* val_y = GetDataP(name_CV2, i_level);
+    const su2double* val_CV1 = GetDataP(name_CV1, i_level);
+    const su2double* val_CV2 = GetDataP(name_CV2, i_level);
 
     /* calculate weights for each triangle (basically a distance function) and
-    * build inverse interpolation matrices */
+     * build inverse interpolation matrices */
     interp_mat_inv_x_y[i_level].resize(n_triangles[i_level]);
     for (unsigned long i_triangle = 0; i_triangle < n_triangles[i_level]; i_triangle++) {
-
       for (int p = 0; p < 3; p++) {
         next_triangle[p] = triangles[i_level][i_triangle][p];
       }
 
       su2activematrix x_interp_mat_inv(3, 3);
-      GetInterpMatInv(val_x, val_y, next_triangle, x_interp_mat_inv);
+      GetInterpMatInv(val_CV1, val_CV2, next_triangle, x_interp_mat_inv);
       interp_mat_inv_x_y[i_level][i_triangle] = x_interp_mat_inv;
     }
   }
 }
 
 void CLookUpTable::GetInterpMatInv(const su2double* vec_x, const su2double* vec_y,
-                                   std::array<unsigned long,3>& point_ids, su2activematrix& interp_mat_inv) {
+                                   std::array<unsigned long, 3>& point_ids, su2activematrix& interp_mat_inv) {
   const unsigned int M = 3;
   CSquareMatrixCM global_M(3);
 
@@ -389,85 +379,81 @@ void CLookUpTable::GetInterpMatInv(const su2double* vec_x, const su2double* vec_
     su2double x = vec_x[point_ids[i_point]];
     su2double y = vec_y[point_ids[i_point]];
 
-    global_M(i_point,0) = SU2_TYPE::GetValue(1.0);
-    global_M(i_point,1) = SU2_TYPE::GetValue(x);
-    global_M(i_point,2) = SU2_TYPE::GetValue(y);
+    global_M(i_point, 0) = SU2_TYPE::GetValue(1.0);
+    global_M(i_point, 1) = SU2_TYPE::GetValue(x);
+    global_M(i_point, 2) = SU2_TYPE::GetValue(y);
   }
 
   global_M.Invert();
   global_M.Transpose();
- 
-  for (unsigned int i=0; i<M; i++){
-    for (unsigned int j=0; j<M; j++){
-      interp_mat_inv[i][j] = global_M(i,j);
+
+  for (unsigned int i = 0; i < M; i++) {
+    for (unsigned int j = 0; j < M; j++) {
+      interp_mat_inv[i][j] = global_M(i, j);
     }
   }
-
 }
 
-std::pair<unsigned long, unsigned long> CLookUpTable::FindInclusionLevels(const su2double val_z)
-{
+std::pair<unsigned long, unsigned long> CLookUpTable::FindInclusionLevels(const su2double val_z) {
   /*--- Find the table levels with constant z-values directly below and above the query value val_z ---*/
 
   /* Check if val_z lies outside table bounds */
-  if(val_z >= *limits_table_z.second){
-    return std::make_pair(n_table_levels-1, n_table_levels-1);
-  }else if(val_z <= *limits_table_z.first){
+  if (val_z >= *limits_table_z.second) {
+    return std::make_pair(n_table_levels - 1, n_table_levels - 1);
+  } else if (val_z <= *limits_table_z.first) {
     return std::make_pair(0, 0);
-  }else{
+  } else {
     std::pair<unsigned long, unsigned long> inclusion_levels;
     /* Loop over table levels to find the levels directly above and below the query value */
-    for(auto i_level = 0ul; i_level < n_table_levels-1; i_level++){
-      if((val_z >= z_values_levels[i_level]) && (val_z < z_values_levels[i_level+1])){
-        inclusion_levels = std::make_pair(i_level, i_level+1);
+    for (auto i_level = 0ul; i_level < n_table_levels - 1; i_level++) {
+      if ((val_z >= z_values_levels[i_level]) && (val_z < z_values_levels[i_level + 1])) {
+        inclusion_levels = std::make_pair(i_level, i_level + 1);
       }
     }
     return inclusion_levels;
   }
 }
 
-unsigned long CLookUpTable::LookUp_XYZ(const std::string& val_name_var, su2double* val_var, su2double val_x,
-                                su2double val_y, su2double val_z)
-{
-  /*--- Perform quasi-3D interpolation for a single variable named val_name_var on a query point 
-        with coordinates val_x, val_y, and val_z ---*/
+unsigned long CLookUpTable::LookUp_XYZ(const std::string& val_name_var, su2double* val_var, su2double val_CV1,
+                                       su2double val_CV2, su2double val_z) {
+  /*--- Perform quasi-3D interpolation for a single variable named val_name_var on a query point
+        with coordinates val_CV1, val_CV2, and val_z ---*/
 
   /* 1: Find table levels directly above and below the query point (the levels that sandwhich val_z) */
   std::pair<unsigned long, unsigned long> inclusion_levels = FindInclusionLevels(val_z);
   bool within_z_limits = (inclusion_levels.first != inclusion_levels.second);
 
-  if(within_z_limits){
+  if (within_z_limits) {
     /* 2: Perform 2D interpolations on upper and lower inclusion levels */
     unsigned long lower_level = inclusion_levels.first;
     unsigned long upper_level = inclusion_levels.second;
 
     su2double val_var_lower, val_var_upper;
-    unsigned long exit_code_lower = LookUp_XY(val_name_var, &val_var_lower, val_x, val_y, lower_level);
-    unsigned long exit_code_upper = LookUp_XY(val_name_var, &val_var_upper, val_x, val_y, upper_level);
+    unsigned long exit_code_lower = LookUp_XY(val_name_var, &val_var_lower, val_CV1, val_CV2, lower_level);
+    unsigned long exit_code_upper = LookUp_XY(val_name_var, &val_var_upper, val_CV1, val_CV2, upper_level);
 
     /* 3: Perform linear interpolation along the z-direction using the x-y interpolation results
              from upper and lower trapezoidal maps */
     Linear_Interpolation(val_z, lower_level, upper_level, val_var_lower, val_var_upper, val_var);
 
     return max(exit_code_lower, exit_code_upper);
-  }else{
+  } else {
     /* Perform single, 2D interpolation when val_z lies outside table bounds */
     unsigned long bound_level = inclusion_levels.first;
-    LookUp_XY(val_name_var, val_var, val_x, val_y, bound_level);
+    LookUp_XY(val_name_var, val_var, val_CV1, val_CV2, bound_level);
     return 1;
   }
 }
-unsigned long CLookUpTable::LookUp_XYZ(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars, su2double val_x,
-                                su2double val_y, su2double val_z)
-{
-  /*--- Perform quasi-3D interpolation for a vector of variables with names val_names_var 
-        on a query point with coordinates val_x, val_y, and val_z ---*/
+unsigned long CLookUpTable::LookUp_XYZ(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars,
+                                       su2double val_CV1, su2double val_CV2, su2double val_z) {
+  /*--- Perform quasi-3D interpolation for a vector of variables with names val_names_var
+        on a query point with coordinates val_CV1, val_CV2, and val_z ---*/
 
   /* 1: Find table levels directly above and below the query point (the levels that sandwhich val_z) */
   std::pair<unsigned long, unsigned long> inclusion_levels = FindInclusionLevels(val_z);
   bool within_z_limits = (inclusion_levels.first != inclusion_levels.second);
-  
-  if(within_z_limits){
+
+  if (within_z_limits) {
     /* 2: Perform 2D interpolations on upper and lower inclusion levels */
     unsigned long lower_level = inclusion_levels.first;
     unsigned long upper_level = inclusion_levels.second;
@@ -475,25 +461,25 @@ unsigned long CLookUpTable::LookUp_XYZ(const std::vector<std::string>& val_names
     std::vector<su2double> val_vars_lower, val_vars_upper;
     val_vars_lower.resize(val_vars.size());
     val_vars_upper.resize(val_vars.size());
-    unsigned long exit_code_lower = LookUp_XY(val_names_var, val_vars_lower, val_x, val_y, lower_level);
-    unsigned long exit_code_upper = LookUp_XY(val_names_var, val_vars_upper, val_x, val_y, upper_level);
+    unsigned long exit_code_lower = LookUp_XY(val_names_var, val_vars_lower, val_CV1, val_CV2, lower_level);
+    unsigned long exit_code_upper = LookUp_XY(val_names_var, val_vars_upper, val_CV1, val_CV2, upper_level);
 
     /* 3: Perform linear interpolation along the z-direction using the x-y interpolation results
              from upper and lower trapezoidal maps */
     Linear_Interpolation(val_z, lower_level, upper_level, val_vars_lower, val_vars_upper, val_vars);
 
     return max(exit_code_lower, exit_code_upper);
-  }else{
+  } else {
     /* Perform single, 2D interpolation when val_z lies outside table bounds */
     unsigned long bound_level = inclusion_levels.first;
-    LookUp_XY(val_names_var, val_vars, val_x, val_y, bound_level);
+    LookUp_XY(val_names_var, val_vars, val_CV1, val_CV2, bound_level);
     return 1;
   }
 }
 
-void CLookUpTable::Linear_Interpolation(const su2double val_z, const unsigned long lower_level, const unsigned long upper_level, 
-                                        su2double& lower_value, su2double& upper_value, su2double*& var_val) const
-{
+void CLookUpTable::Linear_Interpolation(const su2double val_z, const unsigned long lower_level,
+                                        const unsigned long upper_level, su2double& lower_value, su2double& upper_value,
+                                        su2double*& var_val) const {
   /* Perform linear interpolation along the z-direction of the table for a single variable */
 
   /* Retrieve constant z-values of inclusion levels */
@@ -508,10 +494,9 @@ void CLookUpTable::Linear_Interpolation(const su2double val_z, const unsigned lo
   *var_val = lower_value * factor_lower + upper_value * factor_upper;
 }
 
-void CLookUpTable::Linear_Interpolation(const su2double val_z, const unsigned long lower_level, const unsigned long upper_level, 
-                                        std::vector<su2double>& lower_values, std::vector<su2double>& upper_values, 
-                                        std::vector<su2double*>& var_vals) const
-{
+void CLookUpTable::Linear_Interpolation(const su2double val_z, const unsigned long lower_level,
+                                        const unsigned long upper_level, std::vector<su2double>& lower_values,
+                                        std::vector<su2double>& upper_values, std::vector<su2double*>& var_vals) const {
   /* Perform linear interpolation along the z-direction of the table for multiple variables */
 
   /* Retrieve constant z-values of inclusion levels */
@@ -523,14 +508,13 @@ void CLookUpTable::Linear_Interpolation(const su2double val_z, const unsigned lo
   su2double factor_lower = (val_z_upper - val_z) / (val_z_upper - val_z_lower);
 
   /* Perform linear interpolation */
-  for(size_t iVar=0; iVar<var_vals.size(); iVar++){
+  for (size_t iVar = 0; iVar < var_vals.size(); iVar++) {
     *var_vals[iVar] = lower_values[iVar] * factor_lower + upper_values[iVar] * factor_upper;
   }
 }
 
-unsigned long CLookUpTable::LookUp_XY(const string& val_name_var, su2double *val_var, su2double val_x,
-                                            su2double val_y, unsigned long i_level)
-{
+unsigned long CLookUpTable::LookUp_XY(const string& val_name_var, su2double* val_var, su2double val_CV1, su2double val_CV2,
+                                      unsigned long i_level) {
   unsigned long exit_code = 0;
 
   if (val_name_var.compare("NULL") == 0) {
@@ -540,102 +524,100 @@ unsigned long CLookUpTable::LookUp_XY(const string& val_name_var, su2double *val
   }
 
   /* check if x and y value is in table range */
-  if ((val_x >= *limits_table_x[i_level].first && val_x <= *limits_table_x[i_level].second) &&
-      (val_y >= *limits_table_y[i_level].first && val_y <= *limits_table_y[i_level].second)){
-
+  if ((val_CV1 >= *limits_table_x[i_level].first && val_CV1 <= *limits_table_x[i_level].second) &&
+      (val_CV2 >= *limits_table_y[i_level].first && val_CV2 <= *limits_table_y[i_level].second)) {
     /* find the triangle that holds the (x, y) point */
-    unsigned long id_triangle = trap_map_x_y[i_level].GetTriangle(val_x, val_y);
+    unsigned long id_triangle = trap_map_x_y[i_level].GetTriangle(val_CV1, val_CV2);
 
-    if (IsInTriangle(val_x, val_y, id_triangle, i_level)) {
+    if (IsInTriangle(val_CV1, val_CV2, id_triangle, i_level)) {
       /* get interpolation coefficients for point on triangle */
-      std::array<su2double,3> interp_coeffs{0};
-      GetInterpCoeffs(val_x, val_y, interp_mat_inv_x_y[i_level][id_triangle], interp_coeffs);
+      std::array<su2double, 3> interp_coeffs{0};
+      GetInterpCoeffs(val_CV1, val_CV2, interp_mat_inv_x_y[i_level][id_triangle], interp_coeffs);
 
       /* first, copy the single triangle from the large triangle list*/
-      std::array<unsigned long,3> triangle{0};
-      for (int p = 0; p < 3; p++) 
-        triangle[p] = triangles[i_level][id_triangle][p]; 
+      std::array<unsigned long, 3> triangle{0};
+      for (int p = 0; p < 3; p++) triangle[p] = triangles[i_level][id_triangle][p];
 
       *val_var = Interpolate(GetDataP(val_name_var, i_level), triangle, interp_coeffs);
       exit_code = 0;
     } else {
       /* in bounding box but outside of table */
-      unsigned long nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, i_level);
+      unsigned long nearest_neighbor = FindNearestNeighborOnHull(val_CV1, val_CV2, i_level);
       *val_var = GetDataP(val_name_var, i_level)[nearest_neighbor];
       exit_code = 1;
     }
   } else {
     /* lookup is outside of table bounding box */
-    unsigned long nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, i_level);
+    unsigned long nearest_neighbor = FindNearestNeighborOnHull(val_CV1, val_CV2, i_level);
     *val_var = GetDataP(val_name_var, i_level)[nearest_neighbor];
     exit_code = 1;
   }
   return exit_code;
 }
 
-unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vector<su2double>& val_vars,
-                                            su2double val_x, su2double val_y, unsigned long i_level) 
-{
+unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vector<su2double>& val_vars, su2double val_CV1,
+                                      su2double val_CV2, unsigned long i_level) {
   vector<su2double*> look_up_data(val_names_var.size());
 
   for (long unsigned int i_var = 0; i_var < val_vars.size(); ++i_var) {
     look_up_data[i_var] = &val_vars[i_var];
   }
 
-  unsigned long exit_code = LookUp_XY(val_names_var, look_up_data, val_x, val_y, i_level);
+  unsigned long exit_code = LookUp_XY(val_names_var, look_up_data, val_CV1, val_CV2, i_level);
 
   return exit_code;
 }
 
-unsigned long CLookUpTable::LookUp_ProgEnth(const std::string& val_name_var, su2double* val_var, su2double val_prog, 
-                                            su2double val_enth, std::string name_prog, std::string name_enth)
-{
+unsigned long CLookUpTable::LookUp_ProgEnth(const std::string& val_name_var, su2double* val_var, su2double val_prog,
+                                            su2double val_enth, std::string name_prog, std::string name_enth) {
   return LookUp_XY(val_name_var, val_var, val_prog, val_enth);
 }
 
-unsigned long CLookUpTable::LookUp_ProgEnth(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars, su2double val_prog,
-                                su2double val_enth, std::string name_prog, std::string name_enth) {
+unsigned long CLookUpTable::LookUp_ProgEnth(const std::vector<std::string>& val_names_var,
+                                            std::vector<su2double*>& val_vars, su2double val_prog, su2double val_enth,
+                                            std::string name_prog, std::string name_enth) {
   return LookUp_XY(val_names_var, val_vars, val_prog, val_enth);
 }
 
-unsigned long CLookUpTable::LookUp_ProgEnth(const std::vector<std::string>& val_names_var, std::vector<su2double>& val_vars, su2double val_prog,
-                                su2double val_enth, std::string name_prog, std::string name_enth) {
+unsigned long CLookUpTable::LookUp_ProgEnth(const std::vector<std::string>& val_names_var,
+                                            std::vector<su2double>& val_vars, su2double val_prog, su2double val_enth,
+                                            std::string name_prog, std::string name_enth) {
   return LookUp_XY(val_names_var, val_vars, val_prog, val_enth);
 }
 
 unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vector<su2double*>& val_vars,
-                                            su2double val_x, su2double val_y, unsigned long i_level) {
+                                      su2double val_CV1, su2double val_CV2, unsigned long i_level) {
   unsigned long exit_code = 0;
   unsigned long nearest_neighbor = 0;
   unsigned long id_triangle = 0;
-  std::array<su2double,3> interp_coeffs{0};
-  std::array<unsigned long,3> triangle{0};
+  std::array<su2double, 3> interp_coeffs{0};
+  std::array<unsigned long, 3> triangle{0};
 
   /* check if x value is in table x-dimension range
    * and if y is in table y-dimension table range */
-  if ((val_x >= *limits_table_x[i_level].first && val_x <= *limits_table_x[i_level].second) &&
-      (val_y >= *limits_table_y[i_level].first && val_y <= *limits_table_y[i_level].second)){
+  if ((val_CV1 >= *limits_table_x[i_level].first && val_CV1 <= *limits_table_x[i_level].second) &&
+      (val_CV2 >= *limits_table_y[i_level].first && val_CV2 <= *limits_table_y[i_level].second)) {
     /* if so, try to find the triangle that holds the (prog, enth) point */
-    id_triangle = trap_map_x_y[i_level].GetTriangle(val_x, val_y);
+    id_triangle = trap_map_x_y[i_level].GetTriangle(val_CV1, val_CV2);
 
     /* check if point is inside a triangle (if table domain is non-rectangular,
      * the previous range check might be true but the point could still be outside of the domain) */
-    if (IsInTriangle(val_x, val_y, id_triangle, i_level)) {
+    if (IsInTriangle(val_CV1, val_CV2, id_triangle, i_level)) {
       /* if so, get interpolation coefficients for point in  the triangle */
-      GetInterpCoeffs(val_x, val_y, interp_mat_inv_x_y[i_level][id_triangle], interp_coeffs);
+      GetInterpCoeffs(val_CV1, val_CV2, interp_mat_inv_x_y[i_level][id_triangle], interp_coeffs);
 
       /* exit_code 0 means point was in triangle */
       exit_code = 0;
 
     } else {
       /* if point is not inside a triangle (outside table domain) search nearest neighbor */
-      nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, i_level);
+      nearest_neighbor = FindNearestNeighborOnHull(val_CV1, val_CV2, i_level);
       exit_code = 1;
     }
 
   } else {
     /* if point is outside of table ranges, find nearest neighbor */
-    nearest_neighbor = FindNearestNeighborOnHull(val_x, val_y, i_level);
+    nearest_neighbor = FindNearestNeighborOnHull(val_CV1, val_CV2, i_level);
     exit_code = 1;
   }
 
@@ -644,24 +626,20 @@ unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vecto
     if (val_names_var[i_var].compare("NULL") == 0) {
       *val_vars[i_var] = 0.0;
     } else {
-      if (exit_code == 0){
-
+      if (exit_code == 0) {
         /* first, copy the single triangle from the large triangle list*/
-        for (int p = 0; p < 3; p++) 
-          triangle[p] = triangles[i_level][id_triangle][p]; 
+        for (int p = 0; p < 3; p++) triangle[p] = triangles[i_level][id_triangle][p];
         *val_vars[i_var] = Interpolate(GetDataP(val_names_var[i_var], i_level), triangle, interp_coeffs);
-      }
-      else
+      } else
         *val_vars[i_var] = GetDataP(val_names_var[i_var], i_level)[nearest_neighbor];
     }
   }
   return exit_code;
 }
 
-void CLookUpTable::GetInterpCoeffs(su2double val_x, su2double val_y, su2activematrix& interp_mat_inv,
-                                   std::array<su2double,3>& interp_coeffs) {
-
-  std::array<su2double,3> query_vector = {1,val_x,val_y};
+void CLookUpTable::GetInterpCoeffs(su2double val_CV1, su2double val_CV2, su2activematrix& interp_mat_inv,
+                                   std::array<su2double, 3>& interp_coeffs) {
+  std::array<su2double, 3> query_vector = {1, val_CV1, val_CV2};
 
   su2double d;
   for (int i = 0; i < 3; i++) {
@@ -673,8 +651,8 @@ void CLookUpTable::GetInterpCoeffs(su2double val_x, su2double val_y, su2activema
   }
 }
 
-su2double CLookUpTable::Interpolate(const su2double* val_samples, std::array<unsigned long,3>& val_triangle,
-                                    std::array<su2double,3>& val_interp_coeffs) {
+su2double CLookUpTable::Interpolate(const su2double* val_samples, std::array<unsigned long, 3>& val_triangle,
+                                    std::array<su2double, 3>& val_interp_coeffs) {
   su2double result = 0;
   su2double z = 0;
 
@@ -686,7 +664,7 @@ su2double CLookUpTable::Interpolate(const su2double* val_samples, std::array<uns
   return result;
 }
 
-unsigned long CLookUpTable::FindNearestNeighborOnHull(su2double val_x, su2double val_y, unsigned long i_level) {
+unsigned long CLookUpTable::FindNearestNeighborOnHull(su2double val_CV1, su2double val_CV2, unsigned long i_level) {
   su2double min_distance = 1.e99;
   su2double next_distance = 1.e99;
   su2double next_x_norm;
@@ -698,14 +676,14 @@ unsigned long CLookUpTable::FindNearestNeighborOnHull(su2double val_x, su2double
 
   su2double norm_coeff_x = 1. / (limits_table_x[i_level].second - limits_table_x[i_level].first);
   su2double norm_coeff_y = 1. / (limits_table_y[i_level].second - limits_table_y[i_level].first);
-  su2double val_x_norm = val_x / (limits_table_x[i_level].second - limits_table_x[i_level].first);
-  su2double val_y_norm = val_y / (limits_table_y[i_level].second - limits_table_y[i_level].first);
+  su2double val_CV1_norm = val_CV1 / (limits_table_x[i_level].second - limits_table_x[i_level].first);
+  su2double val_CV2_norm = val_CV2 / (limits_table_y[i_level].second - limits_table_y[i_level].first);
 
   for (unsigned long i_point = 0; i_point < n_hull_points[i_level]; ++i_point) {
     next_x_norm = x_table[hull[i_level][i_point]] * norm_coeff_x;
     next_y_norm = y_table[hull[i_level][i_point]] * norm_coeff_y;
 
-    next_distance = sqrt(pow(val_x_norm - next_x_norm, 2) + pow(val_y_norm - next_y_norm, 2));
+    next_distance = sqrt(pow(val_CV1_norm - next_x_norm, 2) + pow(val_CV2_norm - next_y_norm, 2));
 
     if (next_distance < min_distance) {
       min_distance = next_distance;
@@ -715,21 +693,22 @@ unsigned long CLookUpTable::FindNearestNeighborOnHull(su2double val_x, su2double
   return neighbor_id;
 }
 
-bool CLookUpTable::IsInTriangle(su2double val_x, su2double val_y, unsigned long val_id_triangle, unsigned long i_level) {
+bool CLookUpTable::IsInTriangle(su2double val_CV1, su2double val_CV2, unsigned long val_id_triangle,
+                                unsigned long i_level) {
   su2double tri_x_0 = GetDataP(name_CV1, i_level)[triangles[i_level][val_id_triangle][0]];
   su2double tri_y_0 = GetDataP(name_CV2, i_level)[triangles[i_level][val_id_triangle][0]];
 
   su2double tri_x_1 = GetDataP(name_CV1, i_level)[triangles[i_level][val_id_triangle][1]];
   su2double tri_y_1 = GetDataP(name_CV2, i_level)[triangles[i_level][val_id_triangle][1]];
-  
+
   su2double tri_x_2 = GetDataP(name_CV1, i_level)[triangles[i_level][val_id_triangle][2]];
   su2double tri_y_2 = GetDataP(name_CV2, i_level)[triangles[i_level][val_id_triangle][2]];
 
   su2double area_tri = TriArea(tri_x_0, tri_y_0, tri_x_1, tri_y_1, tri_x_2, tri_y_2);
 
-  su2double area_0 = TriArea(val_x, val_y, tri_x_1, tri_y_1, tri_x_2, tri_y_2);
-  su2double area_1 = TriArea(tri_x_0, tri_y_0, val_x, val_y, tri_x_2, tri_y_2);
-  su2double area_2 = TriArea(tri_x_0, tri_y_0, tri_x_1, tri_y_1, val_x, val_y);
+  su2double area_0 = TriArea(val_CV1, val_CV2, tri_x_1, tri_y_1, tri_x_2, tri_y_2);
+  su2double area_1 = TriArea(tri_x_0, tri_y_0, val_CV1, val_CV2, tri_x_2, tri_y_2);
+  su2double area_2 = TriArea(tri_x_0, tri_y_0, tri_x_1, tri_y_1, val_CV1, val_CV2);
 
   return (abs(area_tri - (area_0 + area_1 + area_2)) < area_tri * 1e-10);
-}
+}
\ No newline at end of file
diff --git a/Common/src/containers/CTrapezoidalMap.cpp b/Common/src/containers/CTrapezoidalMap.cpp
index ab33623458c..fe2e2acb490 100644
--- a/Common/src/containers/CTrapezoidalMap.cpp
+++ b/Common/src/containers/CTrapezoidalMap.cpp
@@ -32,17 +32,17 @@
 
 using namespace std;
 
-/* Trapezoidal map implementation. Reference: 
- * M. de Berg, O. Cheong M. van Kreveld, M. Overmars, 
+/* Trapezoidal map implementation. Reference:
+ * M. de Berg, O. Cheong M. van Kreveld, M. Overmars,
  * Computational Geometry, Algorithms and Applications pp. 121-146 (2008)
  * NOTE: the current implementation is actually the simpler 'slab' approach.
  */
 CTrapezoidalMap::CTrapezoidalMap(const su2double* samples_x, const su2double* samples_y, const unsigned long size,
-                                 vector<std::array<unsigned long,2> > const& edges,
+                                 vector<std::array<unsigned long, 2> > const& edges,
                                  su2vector<vector<unsigned long> > const& val_edge_to_triangle) {
   edge_to_triangle = su2vector<vector<unsigned long> >(val_edge_to_triangle);
 
-  unique_bands_x.assign(samples_x,samples_x+size);
+  unique_bands_x.assign(samples_x, samples_x + size);
 
   /* sort x_bands and make them unique */
   sort(unique_bands_x.begin(), unique_bands_x.end());
@@ -127,9 +127,8 @@ CTrapezoidalMap::CTrapezoidalMap(const su2double* samples_x, const su2double* sa
   }
 }
 
-
 unsigned long CTrapezoidalMap::GetTriangle(su2double val_x, su2double val_y) {
-//unsigned long CTrapezoidalMap::GetTriangle(su2double val_x, su2double val_y) const {
+  // unsigned long CTrapezoidalMap::GetTriangle(su2double val_x, su2double val_y) const {
   /* find x band in which val_x sits */
   pair<unsigned long, unsigned long> band = GetBand(val_x);
 
@@ -138,13 +137,11 @@ unsigned long CTrapezoidalMap::GetTriangle(su2double val_x, su2double val_y) {
 
   /* identify the triangle using the two edges */
   std::array<unsigned long, 2> triangles_edge_low;
-  
-  for (int i=0;i<2;i++)
-   triangles_edge_low[i] = edge_to_triangle[edges.first][i];
-   
+
+  for (int i = 0; i < 2; i++) triangles_edge_low[i] = edge_to_triangle[edges.first][i];
+
   std::array<unsigned long, 2> triangles_edge_up;
-  for (int i=0;i<2;i++)
-   triangles_edge_up[i] = edge_to_triangle[edges.second][i];
+  for (int i = 0; i < 2; i++) triangles_edge_up[i] = edge_to_triangle[edges.second][i];
 
   sort(triangles_edge_low.begin(), triangles_edge_low.end());
   sort(triangles_edge_up.begin(), triangles_edge_up.end());
@@ -166,18 +163,18 @@ pair<unsigned long, unsigned long> CTrapezoidalMap::GetBand(su2double val_x) {
   if (val_x < unique_bands_x.front()) val_x = unique_bands_x.front();
   if (val_x > unique_bands_x.back()) val_x = unique_bands_x.back();
 
-  std::pair<std::vector<su2double>::iterator,std::vector<su2double>::iterator> bounds;
-  bounds = std::equal_range (unique_bands_x.begin(), unique_bands_x.end(), val_x);
+  std::pair<std::vector<su2double>::iterator, std::vector<su2double>::iterator> bounds;
+  bounds = std::equal_range(unique_bands_x.begin(), unique_bands_x.end(), val_x);
 
   /*--- if upper bound = 0, then use the range [0,1] ---*/
-  i_up =  max<unsigned long>(1, bounds.first - unique_bands_x.begin());
-  i_low = i_up-1;
+  i_up = max<unsigned long>(1, bounds.first - unique_bands_x.begin());
+  i_low = i_up - 1;
 
   return make_pair(i_low, i_up);
 }
 
 pair<unsigned long, unsigned long> CTrapezoidalMap::GetEdges(pair<unsigned long, unsigned long> val_band,
-                                                             su2double val_x, su2double val_y) const{
+                                                             su2double val_x, su2double val_y) const {
   su2double next_y;
   su2double y_edge_low;
   su2double y_edge_up;

From c67a476d216bae3c7a4df00070a0c346f88dea6f Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 3 Jan 2023 16:12:00 +0100
Subject: [PATCH 109/656] Replaced x and y with CV1 and CV2 where relevant

---
 Common/include/containers/CLookUpTable.hpp | 68 +++++++++++-----------
 1 file changed, 34 insertions(+), 34 deletions(-)

diff --git a/Common/include/containers/CLookUpTable.hpp b/Common/include/containers/CLookUpTable.hpp
index 378cee18bab..518f1eb36c4 100644
--- a/Common/include/containers/CLookUpTable.hpp
+++ b/Common/include/containers/CLookUpTable.hpp
@@ -163,12 +163,12 @@ class CLookUpTable {
 
   /*!
    * \brief compute the interpolation coefficients for the triangular interpolation.
-   * \param[in] val_x - value of first coordinate (progress variable).
-   * \param[in] val_y - value of second coordinate (enthalpy).
+   * \param[in] val_CV1 - value of first coordinate (progress variable).
+   * \param[in] val_CV2 - value of second coordinate (enthalpy).
    * \param[in] interp_mat_inv - inverse matrix for interpolation.
    * \param[out] interp_coeffs - interpolation coefficients.
    */
-  void GetInterpCoeffs(su2double val_x, su2double val_y, su2activematrix& interp_mat_inv,
+  void GetInterpCoeffs(su2double val_CV1, su2double val_CV2, su2activematrix& interp_mat_inv,
                        std::array<su2double, 3>& interp_coeffs);
 
   /*!
@@ -207,21 +207,21 @@ class CLookUpTable {
                             std::vector<su2double*>& var_vals) const;
 
   /*!
-   * \brief find the point on the hull (boundary of the table) that is closest to the point P(val_x,val_y).
-   * \param[in] val_x - first coordinate of point P(val_x,val_y) to check.
-   * \param[in] val_y - second coordinate of point P(val_x,val_y) to check.
+   * \brief find the point on the hull (boundary of the table) that is closest to the point P(val_CV1,val_CV2).
+   * \param[in] val_CV1 - first coordinate of point P(val_CV1,val_CV2) to check.
+   * \param[in] val_CV2 - second coordinate of point P(val_CV1,val_CV2) to check.
    * \returns point id of the nearest neighbor on the hull.
    */
-  unsigned long FindNearestNeighborOnHull(su2double val_x, su2double val_y, unsigned long i_level = 0);
+  unsigned long FindNearestNeighborOnHull(su2double val_CV1, su2double val_CV2, unsigned long i_level = 0);
 
   /*!
-   * \brief determine if a point P(val_x,val_y) is inside the triangle val_id_triangle.
-   * \param[in] val_x - first coordinate of point P(val_x,val_y) to check.
-   * \param[in] val_y - second coordinate of point P(val_x,val_y) to check.
+   * \brief determine if a point P(val_CV1,val_CV2) is inside the triangle val_id_triangle.
+   * \param[in] val_CV1 - first coordinate of point P(val_CV1,val_CV2) to check.
+   * \param[in] val_CV2 - second coordinate of point P(val_CV1,val_CV2) to check.
    * \param[in] val_id_triangle - ID of the triangle to check.
    * \returns true if the point is in the triangle, false if it is outside.
    */
-  bool IsInTriangle(su2double val_x, su2double val_y, unsigned long val_id_triangle, unsigned long i_level = 0);
+  bool IsInTriangle(su2double val_CV1, su2double val_CV2, unsigned long val_id_triangle, unsigned long i_level = 0);
 
   /*!
    * \brief compute the area of a triangle given the 3 points of the triangle.
@@ -246,37 +246,37 @@ class CLookUpTable {
   void PrintTableInfo();
 
   /*!
-   * \brief lookup 1 value of the single variable "val_name_var" using controlling variable values(val_x,val_y).
+   * \brief lookup 1 value of the single variable "val_name_var" using controlling variable values(val_CV1,val_CV2).
    * \param[in] val_name_var - string name of the variable to look up.
    * \param[out] val_var - the stored value of the variable to look up.
-   * \param[in] val_x - value of controlling variable 1.
-   * \param[in] val_y - value of controlling variable 2.
+   * \param[in] val_CV1 - value of controlling variable 1.
+   * \param[in] val_CV2 - value of controlling variable 2.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
-  unsigned long LookUp_XY(const std::string& val_name_var, su2double* val_var, su2double val_x, su2double val_y,
+  unsigned long LookUp_XY(const std::string& val_name_var, su2double* val_var, su2double val_CV1, su2double val_CV2,
                           unsigned long i_level = 0);
 
   /*!
-   * \brief lookup 1 value for each of the variables in "val_name_var" using controlling variable values(val_x,val_y).
+   * \brief lookup 1 value for each of the variables in "val_name_var" using controlling variable values(val_CV1,val_CV2).
    * \param[in] val_names_var - vector of string names of the variables to look up.
    * \param[out] val_vars - pointer to the vector of stored values of the variables to look up.
-   * \param[in] val_x - value of controlling variable 1.
-   * \param[in] val_y - value of controlling variable 2.
+   * \param[in] val_CV1 - value of controlling variable 1.
+   * \param[in] val_CV2 - value of controlling variable 2.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
   unsigned long LookUp_XY(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars,
-                          su2double val_x, su2double val_y, unsigned long i_level = 0);
+                          su2double val_CV1, su2double val_CV2, unsigned long i_level = 0);
 
   /*!
-   * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_x,val_y).
+   * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_CV1,val_CV2).
    * \param[in] val_name_var - string name of the variable to look up.
    * \param[out] val_var - the stored value of the variable to look up.
-   * \param[in] val_x - value of controlling variable 1.
-   * \param[in] val_y - value of controlling variable 2.
+   * \param[in] val_CV1 - value of controlling variable 1.
+   * \param[in] val_CV2 - value of controlling variable 2.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
   unsigned long LookUp_XY(const std::vector<std::string>& val_names_var, std::vector<su2double>& val_vars,
-                          su2double val_x, su2double val_y, unsigned long i_level = 0);
+                          su2double val_CV1, su2double val_CV2, unsigned long i_level = 0);
 
   /*!
    * \brief legacy version of the 2D lookup method for 1 value of the single variable "val_name_var"
@@ -294,7 +294,7 @@ class CLookUpTable {
 
   /*!
    * \brief legacy version of the 2D lookup method for 1 value for each of the variables in "val_name_var"
-            using controlling variable values(val_x,val_y).
+            using controlling variable values(val_CV1,val_CV2).
    * \param[in] val_name_var - vector of string names of the variables to look up.
    * \param[out] val_vars - pointer to the vector of stored values of the variables to look up.
    * \param[in] val_prog - value of the progress variable.
@@ -308,7 +308,7 @@ class CLookUpTable {
 
   /*!
    * \brief legacy version of the 2D lookup method for 1 value for each of the variables in "val_name_var"
-            using controlling variable values(val_x,val_y).
+            using controlling variable values(val_CV1,val_CV2).
    * \param[in] val_name_var - vector of string names of the variables to look up.
    * \param[out] val_vars - pointer to the vector of stored values of the variables to look up.
    * \param[in] val_prog - value of the progress variable.
@@ -318,30 +318,30 @@ class CLookUpTable {
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
   unsigned long LookUp_ProgEnth(const std::vector<std::string>& val_names_var, std::vector<su2double>& val_vars,
-                                su2double val_x, su2double val_y, std::string name_prog, std::string name_enth);
+                                su2double val_CV1, su2double val_CV2, std::string name_prog, std::string name_enth);
   /*!
-   * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_x,val_y,val_z).
+   * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_CV1,val_CV2,val_z).
    * \param[in] val_name_var - string name of the variable to look up.
    * \param[out] val_var - the stored value of the variable to look up.
-   * \param[in] val_x - value of controlling variable 1.
-   * \param[in] val_y - value of controlling variable 2.
+   * \param[in] val_CV1 - value of controlling variable 1.
+   * \param[in] val_CV2 - value of controlling variable 2.
    * \param[in] val_z - value of controlling variable 3.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
-  unsigned long LookUp_XYZ(const std::string& val_name_var, su2double* val_var, su2double val_x, su2double val_y,
+  unsigned long LookUp_XYZ(const std::string& val_name_var, su2double* val_var, su2double val_CV1, su2double val_CV2,
                            su2double val_z);
 
   /*!
-   * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_x,val_y,val_z).
+   * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_CV1,val_CV2,val_z).
    * \param[in] val_name_var - string name of the variable to look up.
    * \param[out] val_var - the stored value of the variable to look up.
-   * \param[in] val_x - value of controlling variable 1.
-   * \param[in] val_y - value of controlling variable 2.
+   * \param[in] val_CV1 - value of controlling variable 1.
+   * \param[in] val_CV2 - value of controlling variable 2.
    * \param[in] val_z - value of controlling variable 3.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
   unsigned long LookUp_XYZ(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars,
-                           su2double val_x, su2double val_y, su2double val_z = 0);
+                           su2double val_CV1, su2double val_CV2, su2double val_z = 0);
 
   /*!
    * \brief Find the table levels with constant z-values directly above and below query val_z.

From cc29f494a2dc68de1220c9a61a21fa29431a55a2 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 3 Jan 2023 16:45:37 +0100
Subject: [PATCH 110/656] added clang formatting to multilayer-perceptron files

---
 .../multilayer_perceptron/CIOMap.hpp          | 304 +++++-----
 .../multilayer_perceptron/CLayer.hpp          | 216 +++----
 .../multilayer_perceptron/CLookUp_ANN.hpp     | 169 +++---
 .../multilayer_perceptron/CNeuralNetwork.hpp  | 485 ++++++++--------
 .../multilayer_perceptron/CNeuron.hpp         | 159 +++---
 .../CReadNeuralNetwork.hpp                    | 238 ++++----
 .../multilayer_perceptron/CIOMap.cpp          |  75 +--
 .../multilayer_perceptron/CLayer.cpp          |  28 +-
 .../multilayer_perceptron/CLookUp_ANN.cpp     | 380 ++++++-------
 .../multilayer_perceptron/CNeuralNetwork.cpp  | 534 +++++++++---------
 .../multilayer_perceptron/CNeuron.cpp         |   7 +-
 .../CReadNeuralNetwork.cpp                    | 277 +++++----
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp    | 104 ++--
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        | 263 ++++-----
 14 files changed, 1607 insertions(+), 1632 deletions(-)

diff --git a/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp b/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
index 0b74c6bb939..be4613fcc3b 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
@@ -27,160 +27,164 @@
 #pragma once
 
 #include <cmath>
-#include <string>
+#include <cstdlib>
 #include <iostream>
 #include <limits>
-#include <cstdlib>
+#include <string>
 #include <vector>
+
 #include "../../linear_algebra/blas_structure.hpp"
 #include "CLookUp_ANN.hpp"
 
-namespace MLPToolbox
+namespace MLPToolbox {
+
+class CLookUp_ANN;
+
+class CIOMap
+/*!
+ *\class CIOMap
+ *\brief This class is used by the CLookUp_ANN class to assign user-defined inputs
+ * and outputs to loaded multi-layer perceptrons. When a look-up operation is called
+ * with a specific CIOMap, the multi-layer perceptrons are evaluated with input and
+ * output variables coinciding with the desired input and output variable names.
+ *
+ *
+ * For example, in a custom, data-driven fluid model, MLP's are used for thermodynamic state
+ * definition. There are three MLP's loaded. MLP_1 predicts temperature and specific heat
+ * based on density and energy. MLP_2 predicts pressure and speed of sound based on density and
+ * energy as well. MLP_3 predicts density and energy based on pressure and temperature.
+ * During a certain look-up operation in the CFluidModel, temperature, speed of sound and pressure
+ * are needed for a given density and energy. What the CIOMap does is to point to MLP_1 for
+ * temperature evalutation, and to MLP_2 for pressure and speed of sound evaluation. MLP_3 is
+ * not considered, as the respective inputs and outputs don't match with the function call
+ * inputs and outputs.
+ *
+ *  call variables:      MLP inputs:                     MLP outputs:           call outputs:
+ *
+ *                        2--> energy --|            |--> temperature --> 1
+ *                                      |--> MLP_1 --|
+ *  1:density            1--> density --|            |--> c_p                   1:temperature
+ *  2:energy                                                                    2:speed of sound
+ *                       1--> density --|            |--> pressure --> 3        3:pressure
+ *                                      |--> MLP_2 --|
+ *                        2--> energy --|            |--> speed of sound --> 2
+ *
+ *                           pressure --|            |--> density
+ *                                      |--> MLP_3 --|
+ *                        temperature --|            |--> energy
+ *
+ *
+ * \author E.Bunschoten
+ */
+
 {
-        
-    class CLookUp_ANN;
-
-    class CIOMap
-    /*! 
-    *\class CIOMap
-    *\brief This class is used by the CLookUp_ANN class to assign user-defined inputs 
-    * and outputs to loaded multi-layer perceptrons. When a look-up operation is called
-    * with a specific CIOMap, the multi-layer perceptrons are evaluated with input and
-    * output variables coinciding with the desired input and output variable names.
-    * 
-    *
-    * For example, in a custom, data-driven fluid model, MLP's are used for thermodynamic state
-    * definition. There are three MLP's loaded. MLP_1 predicts temperature and specific heat 
-    * based on density and energy. MLP_2 predicts pressure and speed of sound based on density and
-    * energy as well. MLP_3 predicts density and energy based on pressure and temperature.
-    * During a certain look-up operation in the CFluidModel, temperature, speed of sound and pressure 
-    * are needed for a given density and energy. What the CIOMap does is to point to MLP_1 for 
-    * temperature evalutation, and to MLP_2 for pressure and speed of sound evaluation. MLP_3 is 
-    * not considered, as the respective inputs and outputs don't match with the function call
-    * inputs and outputs.
-    * 
-    *  call variables:      MLP inputs:                     MLP outputs:           call outputs:
-    *   
-    *                        2--> energy --|            |--> temperature --> 1       
-    *                                      |--> MLP_1 --|       
-    *  1:density            1--> density --|            |--> c_p                   1:temperature
-    *  2:energy                                                                    2:speed of sound
-    *                       1--> density --|            |--> pressure --> 3        3:pressure
-    *                                      |--> MLP_2 --|
-    *                        2--> energy --|            |--> speed of sound --> 2
-    * 
-    *                           pressure --|            |--> density
-    *                                      |--> MLP_3 --|
-    *                        temperature --|            |--> energy
-    * 
-    * 
-    * \author E.Bunschoten
-    */
-
-    {
-        private:
-        std::vector<std::size_t> MLP_indices;       /*!< Loaded MLP index */
-
-        std::vector<std::vector<std::pair<std::size_t, std::size_t>>> 
-            Input_Map,      /*!< Mapping of call variable inputs to matching MLP inputs */
-            Output_Map;     /*!< Mapping of call variable outputs to matching MLP outputs */
-        
-        public:
-
-        /*!
-        * \brief CIOMap class constructor;
-        * \param[in] MLP_collection - Pointer to CLookUp_ANN class for which the input-output amap is to be created
-        * \param[in] inputs - Input names for the call function. These should match with at least one of the MLP inputs.
-        * \param[in] outputs - Output names for the call function. These should match with at least one of the MLP outputs.
-        */
-        CIOMap(CLookUp_ANN*MLP_collection, su2vector<std::string> &inputs, su2vector<std::string> &outputs);
-
-        /*!
-        * \brief Set MLP index in IO map
-        * \param[in] iMLP - loaded MLP index
-        */
-        void Push_MLP_index(std::size_t iMLP) { MLP_indices.push_back(iMLP); }
-
-        /*!
-        * \brief Pair call inputs and outputs with the inputs and outputs of 
-                the loaded MLPs
-        * \param[in] MLP_collection - pointer to MLP collection class
-        * \param[in] inputs - vector with call input variable names
-        * \param[in] outputs - vector with call output variable names
-        */
-        void PairVariableswithMLPs(CLookUp_ANN * MLP_collection, su2vector<std::string> &inputs, su2vector<std::string> &outputs);
-
-        /*!
-        * \brief Get the number of MLPs in the current IO map
-        * \return number of MLPs with matching inputs and output(s)
-        */
-        std::size_t GetNMLPs() const { return MLP_indices.size(); }
-
-        /*!
-        * \brief Get the loaded MLP index
-        * \return MLP index
-        */
-        std::size_t GetMLPIndex(std::size_t i_Map) const { return MLP_indices[i_Map]; }
-
-        /*!
-        * \brief Get the call input variable index 
-        * \param[in] i_Map - input-output mapping index of the IO map
-        * \param[in] iInput - input index of the call input variable
-        * \return MLP input variable index
-        */
-        std::size_t GetInputIndex(std::size_t i_Map, std::size_t iInput) const { return Input_Map[i_Map][iInput].first; }
-
-        /*!
-        * \brief Get the call output variable index 
-        * \param[in] i_Map - input-output mapping index of the IO map
-        * \param[in] iOutput - output index of the call input variable
-        * \return call variable output index
-        */
-        std::size_t GetOutputIndex(std::size_t i_Map, std::size_t iOutput) const { return Output_Map[i_Map][iOutput].first; }
-
-        /*!
-        * \brief Get the MLP output variable index 
-        * \param[in] i_Map - input-output mapping index of the IO map
-        * \param[in] iOutput - output index of the call input variable
-        * \return MLP output variable index
-        */
-        std::size_t GetMLPOutputIndex(std::size_t i_Map, std::size_t iOutput) const { return Output_Map[i_Map][iOutput].second; }
-
-        /*!
-        * \brief Get the number of matching output variables between the call and MLP outputs
-        * \param[in] i_Map - input-output mapping index of the IO map
-        * \return Number of matching variables between the loaded MLP and call variables
-        */
-        std::size_t GetNMappedOutputs(std::size_t i_Map) const { return Output_Map[i_Map].size(); }
-
-        /*!
-        * \brief Get the mapping of MLP outputs matching to call outputs
-        * \param[in] i_Map - input-output mapping index of the IO map
-        * \return Mapping of MLP output variables to call variables
-        */
-        std::vector<std::pair<std::size_t, std::size_t>> GetOutputMapping(std::size_t i_map) const { return Output_Map[i_map]; }
-
-        /*!
-        * \brief Get the mapping of MLP inputs to call inputs
-        * \param[in] i_Map - input-output mapping index of the IO map
-        * \return Mapping of MLP input variables to call inputs
-        */
-        std::vector<std::pair<std::size_t, std::size_t>> GetInputMapping(std::size_t i_map) const { return Input_Map[i_map]; }
-        
-        /*!
-        * \brief Get the mapped inputs for the MLP at i_Map
-        * \param[in] i_Map - input-output mapping index of the IO map
-        * \param[in] inputs - call inputs
-        * \return Vector with call inputs in the correct order of the loaded MLP
-        */
-        su2vector<su2double> GetMLP_Inputs(std::size_t i_Map, su2vector<su2double>&inputs) const {
-            su2vector<su2double> MLP_input;
-            MLP_input.resize(Input_Map[i_Map].size());
-
-            for(std::size_t iInput=0; iInput<Input_Map[i_Map].size(); iInput++){
-                MLP_input[iInput] = inputs[GetInputIndex(i_Map, iInput)];
-            }
-            return MLP_input;
-        }
-    };
-}
+ private:
+  std::vector<std::size_t> MLP_indices; /*!< Loaded MLP index */
+
+  std::vector<std::vector<std::pair<std::size_t, std::size_t>>>
+      Input_Map,  /*!< Mapping of call variable inputs to matching MLP inputs */
+      Output_Map; /*!< Mapping of call variable outputs to matching MLP outputs */
+
+ public:
+  /*!
+   * \brief CIOMap class constructor;
+   * \param[in] MLP_collection - Pointer to CLookUp_ANN class for which the input-output amap is to be created
+   * \param[in] inputs - Input names for the call function. These should match with at least one of the MLP inputs.
+   * \param[in] outputs - Output names for the call function. These should match with at least one of the MLP outputs.
+   */
+  CIOMap(CLookUp_ANN* MLP_collection, su2vector<std::string>& inputs, su2vector<std::string>& outputs);
+
+  /*!
+   * \brief Set MLP index in IO map
+   * \param[in] iMLP - loaded MLP index
+   */
+  void Push_MLP_index(std::size_t iMLP) { MLP_indices.push_back(iMLP); }
+
+  /*!
+  * \brief Pair call inputs and outputs with the inputs and outputs of
+          the loaded MLPs
+  * \param[in] MLP_collection - pointer to MLP collection class
+  * \param[in] inputs - vector with call input variable names
+  * \param[in] outputs - vector with call output variable names
+  */
+  void PairVariableswithMLPs(CLookUp_ANN* MLP_collection, su2vector<std::string>& inputs,
+                             su2vector<std::string>& outputs);
+
+  /*!
+   * \brief Get the number of MLPs in the current IO map
+   * \return number of MLPs with matching inputs and output(s)
+   */
+  std::size_t GetNMLPs() const { return MLP_indices.size(); }
+
+  /*!
+   * \brief Get the loaded MLP index
+   * \return MLP index
+   */
+  std::size_t GetMLPIndex(std::size_t i_Map) const { return MLP_indices[i_Map]; }
+
+  /*!
+   * \brief Get the call input variable index
+   * \param[in] i_Map - input-output mapping index of the IO map
+   * \param[in] iInput - input index of the call input variable
+   * \return MLP input variable index
+   */
+  std::size_t GetInputIndex(std::size_t i_Map, std::size_t iInput) const { return Input_Map[i_Map][iInput].first; }
+
+  /*!
+   * \brief Get the call output variable index
+   * \param[in] i_Map - input-output mapping index of the IO map
+   * \param[in] iOutput - output index of the call input variable
+   * \return call variable output index
+   */
+  std::size_t GetOutputIndex(std::size_t i_Map, std::size_t iOutput) const { return Output_Map[i_Map][iOutput].first; }
+
+  /*!
+   * \brief Get the MLP output variable index
+   * \param[in] i_Map - input-output mapping index of the IO map
+   * \param[in] iOutput - output index of the call input variable
+   * \return MLP output variable index
+   */
+  std::size_t GetMLPOutputIndex(std::size_t i_Map, std::size_t iOutput) const {
+    return Output_Map[i_Map][iOutput].second;
+  }
+
+  /*!
+   * \brief Get the number of matching output variables between the call and MLP outputs
+   * \param[in] i_Map - input-output mapping index of the IO map
+   * \return Number of matching variables between the loaded MLP and call variables
+   */
+  std::size_t GetNMappedOutputs(std::size_t i_Map) const { return Output_Map[i_Map].size(); }
+
+  /*!
+   * \brief Get the mapping of MLP outputs matching to call outputs
+   * \param[in] i_Map - input-output mapping index of the IO map
+   * \return Mapping of MLP output variables to call variables
+   */
+  std::vector<std::pair<std::size_t, std::size_t>> GetOutputMapping(std::size_t i_map) const {
+    return Output_Map[i_map];
+  }
+
+  /*!
+   * \brief Get the mapping of MLP inputs to call inputs
+   * \param[in] i_Map - input-output mapping index of the IO map
+   * \return Mapping of MLP input variables to call inputs
+   */
+  std::vector<std::pair<std::size_t, std::size_t>> GetInputMapping(std::size_t i_map) const { return Input_Map[i_map]; }
+
+  /*!
+   * \brief Get the mapped inputs for the MLP at i_Map
+   * \param[in] i_Map - input-output mapping index of the IO map
+   * \param[in] inputs - call inputs
+   * \return Vector with call inputs in the correct order of the loaded MLP
+   */
+  su2vector<su2double> GetMLP_Inputs(std::size_t i_Map, su2vector<su2double>& inputs) const {
+    su2vector<su2double> MLP_input;
+    MLP_input.resize(Input_Map[i_Map].size());
+
+    for (std::size_t iInput = 0; iInput < Input_Map[i_Map].size(); iInput++) {
+      MLP_input[iInput] = inputs[GetInputIndex(i_Map, iInput)];
+    }
+    return MLP_input;
+  }
+};
+}  // namespace MLPToolbox
\ No newline at end of file
diff --git a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
index b29800c52d0..920b256f156 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
@@ -27,118 +27,120 @@
 #pragma once
 
 #include <cmath>
+#include <cstdlib>
 #include <iostream>
 #include <limits>
-#include <cstdlib>
 
 #include "../../CConfig.hpp"
-#include "CNeuron.hpp"
 #include "../../linear_algebra/blas_structure.hpp"
+#include "CNeuron.hpp"
 
-namespace MLPToolbox{
-class CLayer
-{
-private:
-    unsigned long number_of_neurons;    /*!< Neuron count in current layer */
-    CNeuron * neurons;                   /*!< Array of neurons in current layer */
-    bool is_input;                      /*!< Input layer identifyer */
-    std::string activation_type;             /*!< Activation function type applied to the current layer*/
-public:
-    CLayer();
-    CLayer( unsigned long n_neurons );
-    ~CLayer(){ delete [] neurons; }
-    /*!
-    * \brief Set current layer neuron count
-    * \param[in] n_neurons - Number of neurons in this layer
-    */
-    void setNNeurons( unsigned long n_neurons );
-
-    /*!
-    * \brief Get the current layer neuron count
-    * \return Neuron count
-    */
-    unsigned long getNNeurons() const { return number_of_neurons; }
-
-    /*!
-    * \brief Define current layer as input layer
-    * \param[in] input - input layer identifyer
-    */
-    void setInput(bool def) { is_input = def; }
-
-    /*!
-    * \brief Get input layer identifyer
-    * \return input layer identifyer
-    */
-    bool isInput() const { return is_input; }
-
-    /*!
-    * \brief Set the output value of a neuron in the layer
-    * \param[in] i_neuron - Neuron index
-    * \param[in] output_value - Activation function output
-    */
-    void setOutput(std::size_t i_neuron, su2double value) { neurons[i_neuron].setOutput(value); }
-
-    /*!
-    * \brief Get the output value of a neuron in the layer
-    * \param[in] i_neuron - Neuron index
-    * \return Neuron output value
-    */
-    su2double getOutput(std::size_t i_neuron) const { return neurons[i_neuron].getOutput(); }
-
-    /*!
-    * \brief Set the input value of a neuron in the layer
-    * \param[in] i_neuron - Neuron index
-    * \param[in] input_value - Activation function input
-    */
-    void setInput(std::size_t i_neuron, su2double value) { neurons[i_neuron].setInput(value); }
-
-    /*!
-    * \brief Get the input value of a neuron in the layer
-    * \param[in] i_neuron - Neuron index
-    * \return Neuron input value
-    */
-    su2double getInput(std::size_t i_neuron) const { return neurons[i_neuron].getInput(); }
-
-    /*!
-    * \brief Set the bias value of a neuron in the layer
-    * \param[in] i_neuron - Neuron index
-    * \param[in] bias_value - Bias value
-    */
-    void setBias(std::size_t i_neuron, su2double value) { neurons[i_neuron].setBias(value); }
-
-    /*!
-    * \brief Get the bias value of a neuron in the layer
-    * \param[in] i_neuron - Neuron index
-    * \return Neuron bias value
-    */
-    su2double getBias(std::size_t i_neuron) const { return neurons[i_neuron].getBias(); }
-
-    /*!
-    * \brief Get the output-input gradient of a neuron in the layer
-    * \param[in] i_neuron - Neuron index
-    * \return Gradient of neuron output wrt input
-    */
-    su2double getdYdX(std::size_t i_neuron, std::size_t iInput) const { return neurons[i_neuron].getGradient(iInput); }
-
-    /*!
-    * \brief Get the output-input gradient of a neuron in the layer
-    * \param[in] i_neuron - Neuron index
-    * \return Gradient of neuron output wrt input
-    */
-    void setdYdX(std::size_t i_neuron, std::size_t iInput, su2double dy_dx) { neurons[i_neuron].setGradient(iInput, dy_dx); }
-
-    /*!
-    * \brief Size neuron output derivative wrt network inputs.
-    * \param[in] nInputs - Number of network inputs.
-    */
-    void sizeGradients(std::size_t nInputs) { for(auto iNeuron=0u; iNeuron < number_of_neurons; iNeuron++) neurons[iNeuron].sizeGradient(nInputs); }
-
-    /*!
-    * \brief Get the activation function name applied to this layer
-    * \return name of the activation function
-    */
-    string getActivationType() const { return activation_type; }
-    
+namespace MLPToolbox {
+class CLayer {
+ private:
+  unsigned long number_of_neurons; /*!< Neuron count in current layer */
+  CNeuron* neurons;                /*!< Array of neurons in current layer */
+  bool is_input;                   /*!< Input layer identifyer */
+  std::string activation_type;     /*!< Activation function type applied to the current layer*/
+ public:
+  CLayer();
+  CLayer(unsigned long n_neurons);
+  ~CLayer() { delete[] neurons; }
+  /*!
+   * \brief Set current layer neuron count
+   * \param[in] n_neurons - Number of neurons in this layer
+   */
+  void setNNeurons(unsigned long n_neurons);
+
+  /*!
+   * \brief Get the current layer neuron count
+   * \return Neuron count
+   */
+  unsigned long getNNeurons() const { return number_of_neurons; }
+
+  /*!
+   * \brief Define current layer as input layer
+   * \param[in] input - input layer identifyer
+   */
+  void setInput(bool def) { is_input = def; }
+
+  /*!
+   * \brief Get input layer identifyer
+   * \return input layer identifyer
+   */
+  bool isInput() const { return is_input; }
+
+  /*!
+   * \brief Set the output value of a neuron in the layer
+   * \param[in] i_neuron - Neuron index
+   * \param[in] output_value - Activation function output
+   */
+  void setOutput(std::size_t i_neuron, su2double value) { neurons[i_neuron].setOutput(value); }
+
+  /*!
+   * \brief Get the output value of a neuron in the layer
+   * \param[in] i_neuron - Neuron index
+   * \return Neuron output value
+   */
+  su2double getOutput(std::size_t i_neuron) const { return neurons[i_neuron].getOutput(); }
+
+  /*!
+   * \brief Set the input value of a neuron in the layer
+   * \param[in] i_neuron - Neuron index
+   * \param[in] input_value - Activation function input
+   */
+  void setInput(std::size_t i_neuron, su2double value) { neurons[i_neuron].setInput(value); }
+
+  /*!
+   * \brief Get the input value of a neuron in the layer
+   * \param[in] i_neuron - Neuron index
+   * \return Neuron input value
+   */
+  su2double getInput(std::size_t i_neuron) const { return neurons[i_neuron].getInput(); }
+
+  /*!
+   * \brief Set the bias value of a neuron in the layer
+   * \param[in] i_neuron - Neuron index
+   * \param[in] bias_value - Bias value
+   */
+  void setBias(std::size_t i_neuron, su2double value) { neurons[i_neuron].setBias(value); }
+
+  /*!
+   * \brief Get the bias value of a neuron in the layer
+   * \param[in] i_neuron - Neuron index
+   * \return Neuron bias value
+   */
+  su2double getBias(std::size_t i_neuron) const { return neurons[i_neuron].getBias(); }
+
+  /*!
+   * \brief Get the output-input gradient of a neuron in the layer
+   * \param[in] i_neuron - Neuron index
+   * \return Gradient of neuron output wrt input
+   */
+  su2double getdYdX(std::size_t i_neuron, std::size_t iInput) const { return neurons[i_neuron].getGradient(iInput); }
+
+  /*!
+   * \brief Get the output-input gradient of a neuron in the layer
+   * \param[in] i_neuron - Neuron index
+   * \return Gradient of neuron output wrt input
+   */
+  void setdYdX(std::size_t i_neuron, std::size_t iInput, su2double dy_dx) {
+    neurons[i_neuron].setGradient(iInput, dy_dx);
+  }
+
+  /*!
+   * \brief Size neuron output derivative wrt network inputs.
+   * \param[in] nInputs - Number of network inputs.
+   */
+  void sizeGradients(std::size_t nInputs) {
+    for (auto iNeuron = 0u; iNeuron < number_of_neurons; iNeuron++) neurons[iNeuron].sizeGradient(nInputs);
+  }
+
+  /*!
+   * \brief Get the activation function name applied to this layer
+   * \return name of the activation function
+   */
+  string getActivationType() const { return activation_type; }
 };
 
-}
+}  // namespace MLPToolbox
diff --git a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
index f800b3709c4..f17c52a92d3 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
@@ -28,96 +28,93 @@
 #pragma once
 
 #include <cmath>
-#include <string>
+#include <cstdlib>
 #include <iostream>
 #include <limits>
-#include <cstdlib>
+#include <string>
 #include <vector>
+
 #include "../../CConfig.hpp"
 #include "../../linear_algebra/blas_structure.hpp"
-#include "CNeuralNetwork.hpp"
 #include "CIOMap.hpp"
+#include "CNeuralNetwork.hpp"
 
-
-namespace MLPToolbox{
-
-class CLookUp_ANN
-{
-    /*! 
-    *\class CLookUp_ANN
-    *\brief This class allows for the evaluation of one or more multi-layer perceptrons in for example
-    * thermodynamic state look-up operations. The multi-layer perceptrons are loaded in the order listed
-    * in the MLP collection file. Each multi-layer perceptron is generated based on the 
-    * architecture described in its respective input file. When evaluating the MLP collection, an
-    * input-output map is used to find the correct MLP corresponding to the call function inputs and 
-    * outputs.  
-    */
-
-    private:
-    int rank{0};
-    su2vector<CNeuralNetwork*> NeuralNetworks;  /*!< std::vector containing all loaded neural networks. */
-
-    unsigned short number_of_variables;  /*!< Number of loaded ANNs. */
-
-    /*!
-    * \brief Load ANN architecture
-    * \param[in] ANN - pointer to target NeuralNetwork class
-    * \param[in] filename - filename containing ANN architecture information
-    */
-    void GenerateANN(CNeuralNetwork*ANN, std::string filename);
-    
-    public: 
-    
-    /*!
-    * \brief ANN collection class constructor
-    * \param[in] n_inputs - Number of MLP files to be loaded.
-    * \param[in] input_filenames - String array containing MLP input file names. 
-    */
-    CLookUp_ANN(const unsigned short n_inputs, const std::string*input_filenames);
-
-    /*!
-    * \brief Evaluate loaded ANNs for given inputs and outputs
-    * \param[in] input_output_map - input-output map coupling desired inputs and outputs to loaded ANNs
-    * \param[in] inputs - input values
-    * \param[in] outputs - pointers to output variables
-    * \returns Within output normalization range.
-    */
-    unsigned long Predict_ANN(CIOMap *input_output_map, su2vector<su2double> &inputs, su2vector<su2double*> &outputs);
-
-    ~CLookUp_ANN() { 
-        for(std::size_t i_ANN=0; i_ANN<number_of_variables; i_ANN++)
-            delete NeuralNetworks[i_ANN];
-    };
-
-    /*!
-    * \brief Get number of loaded ANNs
-    * \return number of loaded ANNs
-    */
-    std::size_t GetNANNs() const { return NeuralNetworks.size(); }
-
-    /*!
-    * \brief Check if all output variables are present in the loaded ANNs
-    * \param[in] output_names - output variable names to check
-    * \param[in] input_output_map - pointer to input-output map to be checked
-    */
-    bool Check_Use_of_Outputs(su2vector<std::string> &output_names, CIOMap *input_output_map) const;
-
-    /*!
-    * \brief Check if all input variables are present in the loaded ANNs
-    * \param[in] input_names - input variable names to check
-    * \param[in] input_output_map - pointer to input-output map to be checked
-    */
-    bool Check_Use_of_Inputs(su2vector<std::string> &input_names, CIOMap *input_output_map) const;
-
-    /*!
-    * \brief Map variable names to ANN inputs or outputs
-    * \param[in] i_ANN - loaded ANN index
-    * \param[in] variable_names - variable names to map to ANN inputs or outputs
-    * \param[in] input - map to inputs (true) or outputs (false)
-    */
-    std::vector<pair<std::size_t, std::size_t>> FindVariable_Indices(std::size_t i_ANN, su2vector<std::string> variable_names, bool input) const;
-    
-};  
-
-}
-
+namespace MLPToolbox {
+
+class CLookUp_ANN {
+  /*!
+   *\class CLookUp_ANN
+   *\brief This class allows for the evaluation of one or more multi-layer perceptrons in for example
+   * thermodynamic state look-up operations. The multi-layer perceptrons are loaded in the order listed
+   * in the MLP collection file. Each multi-layer perceptron is generated based on the
+   * architecture described in its respective input file. When evaluating the MLP collection, an
+   * input-output map is used to find the correct MLP corresponding to the call function inputs and
+   * outputs.
+   */
+
+ private:
+  int rank{0};
+  su2vector<CNeuralNetwork*> NeuralNetworks; /*!< std::vector containing all loaded neural networks. */
+
+  unsigned short number_of_variables; /*!< Number of loaded ANNs. */
+
+  /*!
+   * \brief Load ANN architecture
+   * \param[in] ANN - pointer to target NeuralNetwork class
+   * \param[in] filename - filename containing ANN architecture information
+   */
+  void GenerateANN(CNeuralNetwork* ANN, std::string filename);
+
+ public:
+  /*!
+   * \brief ANN collection class constructor
+   * \param[in] n_inputs - Number of MLP files to be loaded.
+   * \param[in] input_filenames - String array containing MLP input file names.
+   */
+  CLookUp_ANN(const unsigned short n_inputs, const std::string* input_filenames);
+
+  /*!
+   * \brief Evaluate loaded ANNs for given inputs and outputs
+   * \param[in] input_output_map - input-output map coupling desired inputs and outputs to loaded ANNs
+   * \param[in] inputs - input values
+   * \param[in] outputs - pointers to output variables
+   * \returns Within output normalization range.
+   */
+  unsigned long Predict_ANN(CIOMap* input_output_map, su2vector<su2double>& inputs, su2vector<su2double*>& outputs);
+
+  ~CLookUp_ANN() {
+    for (std::size_t i_ANN = 0; i_ANN < number_of_variables; i_ANN++) delete NeuralNetworks[i_ANN];
+  };
+
+  /*!
+   * \brief Get number of loaded ANNs
+   * \return number of loaded ANNs
+   */
+  std::size_t GetNANNs() const { return NeuralNetworks.size(); }
+
+  /*!
+   * \brief Check if all output variables are present in the loaded ANNs
+   * \param[in] output_names - output variable names to check
+   * \param[in] input_output_map - pointer to input-output map to be checked
+   */
+  bool Check_Use_of_Outputs(su2vector<std::string>& output_names, CIOMap* input_output_map) const;
+
+  /*!
+   * \brief Check if all input variables are present in the loaded ANNs
+   * \param[in] input_names - input variable names to check
+   * \param[in] input_output_map - pointer to input-output map to be checked
+   */
+  bool Check_Use_of_Inputs(su2vector<std::string>& input_names, CIOMap* input_output_map) const;
+
+  /*!
+   * \brief Map variable names to ANN inputs or outputs
+   * \param[in] i_ANN - loaded ANN index
+   * \param[in] variable_names - variable names to map to ANN inputs or outputs
+   * \param[in] input - map to inputs (true) or outputs (false)
+   */
+  std::vector<pair<std::size_t, std::size_t>> FindVariable_Indices(std::size_t i_ANN,
+                                                                   su2vector<std::string> variable_names,
+                                                                   bool input) const;
+};
+
+}  // namespace MLPToolbox
\ No newline at end of file
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
index 589afe0d7e9..b55cf07f7b7 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
@@ -28,252 +28,263 @@
 #pragma once
 
 #include <cmath>
+#include <cstdlib>
 #include <cstring>
 #include <iostream>
 #include <limits>
-#include <cstdlib>
 
 #include "../../CConfig.hpp"
 #include "../../linear_algebra/blas_structure.hpp"
 #include "CLayer.hpp"
 
-namespace MLPToolbox{
-class CNeuralNetwork
-{
-private:
-    su2vector<std::string> input_names,   // MLP input variable names.
-                           output_names;  // MLP output variable names.
-
-    unsigned long n_hidden_layers = 0;  // Number of hidden layers (layers between input and output layer).
-
-    CLayer *inputLayer = nullptr,     // Pointer to network input layer.
-           *outputLayer = nullptr;    // Pointer to network output layer.
-
-    std::vector<CLayer*> hiddenLayers;  // Hidden layer collection.
-    su2vector<CLayer*>   total_layers;  // Hidden layers plus in/output layers
-
-    su2vector<su2activematrix> weights_mat;   // Weights of synapses connecting layers
-
-    su2vector<std::pair<su2double, su2double>> input_norm,    // Normalization factors for network inputs
-                                                 output_norm;   // Normalization factors for network outputs
-
-    su2vector<su2double> last_inputs; // Inputs from previous lookup operation. Evaluation of the network 
-                                        // is skipped if current inputs are the same as the last inputs.
-
-    su2double* ANN_outputs; // Pointer to network outputs
-    su2matrix<su2double> dOutputs_dInputs; // Network output derivatives w.r.t inputs
-
-    /*--- Activation function types that are currently supported ---*/
-    enum ENUM_ACTIVATION_FUNCTION {
-        NONE=0,
-        LINEAR=1,
-        RELU=2,
-        ELU = 3,
-        GELU = 4,
-        SELU = 5,
-        SIGMOID = 6,
-        SWISH = 7,
-        TANH = 8
-    };
-    ENUM_ACTIVATION_FUNCTION * activation_function_types;
-
-public:
-    ~CNeuralNetwork(){
-        delete inputLayer;
-        delete outputLayer;
-        for(std::size_t i=1; i<total_layers.size()-1; i++){
-            delete total_layers[i];
-        }
-        delete [] ANN_outputs;
-        delete [] activation_function_types;
-    };
-    /*!
-    * \brief Set the input layer of the network.
-    * \param[in] n_neurons - Number of inputs
-    */
-    void defineInputLayer(unsigned long n_neurons);
-
-    /*!
-    * \brief Set the output layer of the network.
-    * \param[in] n_neurons - Number of outputs
-    */
-    void defineOutputLayer(unsigned long n_neurons);
-
-    /*!
-    * \brief Add a hidden layer to the network
-    * \param[in] n_neurons - Hidden layer size.
-    */
-    void push_hidden_layer(unsigned long n_neurons);
-
-    /*!
-    * \brief Set the weight value of a specific synapse.
-    * \param[in] i_layer - current layer.
-    * \param[in] i_neuron - neuron index in current layer.
-    * \param[in] j_neuron - neuron index of connecting neuron.
-    * \param[in] value - weight value.
-    */
-    void setWeight(unsigned long i_layer, unsigned long i_neuron, unsigned long j_neuron, su2double value) { weights_mat[i_layer][j_neuron][i_neuron] = value; };
-
-    /*!
-    * \brief Set bias value at a specific neuron.
-    * \param[in] i_layer - Layer index.
-    * \param[in] i_neuron - Neuron index of current layer.
-    * \param[in] value - Bias value.
-    */
-    void setBias(unsigned long i_layer, unsigned long i_neuron, su2double value){ total_layers[i_layer]->setBias(i_neuron, value); }
-
-    /*!
-    * \brief Set layer activation function.
-    * \param[in] i_layer - Layer index.
-    * \param[in] input - Activation function name.
-    */
-    void setActivationFunction(unsigned long i_layer, std::string input);
-
-    /*!
-    * \brief Display the network architecture in the terminal.
-    */
-    void displayNetwork() const;
-
-    /*!
-    * \brief Size the weight layers in the network according to its architecture.
-    */
-    void sizeWeights();
-
-    /*!
-    * \brief Size the vector of previous inputs.
-    * \param[in] n_inputs - Number of inputs.
-    */
-    void sizeInputs(unsigned long n_inputs) { last_inputs.resize(n_inputs); for(unsigned long iInput=0; iInput<n_inputs; iInput++) last_inputs[iInput] = 0.0; }
-    
-    /*!
-    * \brief Get the number of connecting regions in the network.
-    * \returns number of spaces in between layers.
-    */
-    unsigned long getNWeightLayers() const { return total_layers.size()-1; }
-
-    /*!
-    * \brief Get the total number of layers in the network
-    * \returns number of netowork layers.
-    */
-    unsigned long getNLayers() const { return total_layers.size(); }
-
-    /*!
-    * \brief Get neuron count in a layer.
-    * \param[in] iLayer - Layer index.
-    * \returns number of neurons in the layer.
-    */
-    unsigned long getNNeurons(unsigned long iLayer) const { return total_layers[iLayer]->getNNeurons(); }
-
-    /*!
-    * \brief Evaluate the network.
-    * \param[in] inputs - Network input variable values.
-    * \param[in] compute_gradient - Compute the derivatives of the outputs wrt inputs.
-    */
-    void predict(su2vector<su2double> &inputs, bool compute_gradient=false);
-
-    /*!
-    * \brief Set the normalization factors for the input layer
-    * \param[in] iInput - Input index.
-    * \param[in] input_min - Minimum input value.
-    * \param[in] input_max - Maximum input value.
-    */
-    void SetInputNorm(unsigned long iInput, su2double input_min, su2double input_max) { input_norm[iInput] = make_pair(input_min, input_max); }
-
-    /*!
-    * \brief Set the normalization factors for the output layer
-    * \param[in] iOutput - Input index.
-    * \param[in] input_min - Minimum output value.
-    * \param[in] input_max - Maximum output value.
-    */
-    void SetOutputNorm(unsigned long iOutput, su2double output_min, su2double output_max){ output_norm[iOutput] = make_pair(output_min, output_max); }
-    
-    std::pair<su2double, su2double> GetInputNorm(unsigned long iInput) const { return input_norm[iInput]; }
-
-    std::pair<su2double, su2double> GetOutputNorm(unsigned long iOutput) const { return output_norm[iOutput]; }
-    /*!
-    * \brief Add an output variable name to the network.
-    * \param[in] input - Input variable name.
-    */
-    void SetOutputName(size_t iOutput, std::string input) { output_names[iOutput] = input; }
-
-    /*!
-    * \brief Add an input variable name to the network.
-    * \param[in] output - Output variable name.
-    */
-    void SetInputName(size_t iInput, std::string input) { input_names[iInput] = input; }
-   
-    /*!
-    * \brief Get network input variable name.
-    * \param[in] iInput - Input variable index.
-    * \returns input variable name.
-    */
-    std::string GetInputName(std::size_t iInput) const { return input_names[iInput]; }
-
-    /*!
-    * \brief Get network output variable name.
-    * \param[in] iOutput - Output variable index.
-    * \returns output variable name.
-    */
-    std::string GetOutputName(std::size_t iOutput) const { return output_names[iOutput]; }
-
-    /*!
-    * \brief Get network number of inputs.
-    * \returns Number of network inputs
-    */
-    std::size_t GetnInputs() const { return input_names.size(); }
-
-    /*!
-    * \brief Get network number of outputs.
-    * \returns Number of network outputs
-    */
-    std::size_t GetnOutputs() const { return output_names.size(); }
-
-    /*!
-    * \brief Get network evaluation output.
-    * \param[in] iOutput - output index.
-    * \returns Prediction value.
-    */
-    su2double GetANN_Output(std::size_t iOutput) const { return ANN_outputs[iOutput]; }
-
-    /*!
-    * \brief Get network output derivative w.r.t specific input.
-    * \param[in] iOutput - output variable index.
-    * \param[in] iInput - input variable index.
-    * \returns Output derivative w.r.t input.
-    */
-    su2double GetANN_Output_Input_Derivative(std::size_t iOutput, std::size_t iInput) const { return dOutputs_dInputs[iOutput][iInput]; }
-
-    /*!
-    * \brief Set the activation function array size.
-    * \param[in] n_layers - network layer count.
-    */
-    void SizeActivationFunctions(unsigned long n_layers) { activation_function_types = new ENUM_ACTIVATION_FUNCTION[n_layers]; }
-
-    /*!
-    * \brief Compute neuron activation function input.
-    * \param[in] iLayer - Network layer index.
-    * \param[in] iNeuron - Layer neuron index.
-    * \returns Neuron activation function input.
-    */
-    su2double ComputeX(std::size_t iLayer, std::size_t iNeuron) const {
-        su2double x;
-        x = total_layers[iLayer]->getBias(iNeuron);
-        std::size_t nNeurons_previous = total_layers[iLayer - 1]->getNNeurons();
-        for(std::size_t jNeuron=0; jNeuron<nNeurons_previous; jNeuron++){
-            x += weights_mat[iLayer - 1][iNeuron][jNeuron] * total_layers[iLayer-1]->getOutput(jNeuron);
-        }
-        return x;
+namespace MLPToolbox {
+class CNeuralNetwork {
+ private:
+  su2vector<std::string> input_names,  // MLP input variable names.
+      output_names;                    // MLP output variable names.
+
+  unsigned long n_hidden_layers = 0;  // Number of hidden layers (layers between input and output layer).
+
+  CLayer *inputLayer = nullptr,  // Pointer to network input layer.
+      *outputLayer = nullptr;    // Pointer to network output layer.
+
+  std::vector<CLayer*> hiddenLayers;  // Hidden layer collection.
+  su2vector<CLayer*> total_layers;    // Hidden layers plus in/output layers
+
+  su2vector<su2activematrix> weights_mat;  // Weights of synapses connecting layers
+
+  su2vector<std::pair<su2double, su2double>> input_norm,  // Normalization factors for network inputs
+      output_norm;                                        // Normalization factors for network outputs
+
+  su2vector<su2double> last_inputs;  // Inputs from previous lookup operation. Evaluation of the network
+                                     // is skipped if current inputs are the same as the last inputs.
+
+  su2double* ANN_outputs;                 // Pointer to network outputs
+  su2matrix<su2double> dOutputs_dInputs;  // Network output derivatives w.r.t inputs
+
+  /*--- Activation function types that are currently supported ---*/
+  enum ENUM_ACTIVATION_FUNCTION {
+    NONE = 0,
+    LINEAR = 1,
+    RELU = 2,
+    ELU = 3,
+    GELU = 4,
+    SELU = 5,
+    SIGMOID = 6,
+    SWISH = 7,
+    TANH = 8
+  };
+  ENUM_ACTIVATION_FUNCTION* activation_function_types;
+
+ public:
+  ~CNeuralNetwork() {
+    delete inputLayer;
+    delete outputLayer;
+    for (std::size_t i = 1; i < total_layers.size() - 1; i++) {
+      delete total_layers[i];
+    }
+    delete[] ANN_outputs;
+    delete[] activation_function_types;
+  };
+  /*!
+   * \brief Set the input layer of the network.
+   * \param[in] n_neurons - Number of inputs
+   */
+  void defineInputLayer(unsigned long n_neurons);
+
+  /*!
+   * \brief Set the output layer of the network.
+   * \param[in] n_neurons - Number of outputs
+   */
+  void defineOutputLayer(unsigned long n_neurons);
+
+  /*!
+   * \brief Add a hidden layer to the network
+   * \param[in] n_neurons - Hidden layer size.
+   */
+  void push_hidden_layer(unsigned long n_neurons);
+
+  /*!
+   * \brief Set the weight value of a specific synapse.
+   * \param[in] i_layer - current layer.
+   * \param[in] i_neuron - neuron index in current layer.
+   * \param[in] j_neuron - neuron index of connecting neuron.
+   * \param[in] value - weight value.
+   */
+  void setWeight(unsigned long i_layer, unsigned long i_neuron, unsigned long j_neuron, su2double value) {
+    weights_mat[i_layer][j_neuron][i_neuron] = value;
+  };
+
+  /*!
+   * \brief Set bias value at a specific neuron.
+   * \param[in] i_layer - Layer index.
+   * \param[in] i_neuron - Neuron index of current layer.
+   * \param[in] value - Bias value.
+   */
+  void setBias(unsigned long i_layer, unsigned long i_neuron, su2double value) {
+    total_layers[i_layer]->setBias(i_neuron, value);
+  }
+
+  /*!
+   * \brief Set layer activation function.
+   * \param[in] i_layer - Layer index.
+   * \param[in] input - Activation function name.
+   */
+  void setActivationFunction(unsigned long i_layer, std::string input);
+
+  /*!
+   * \brief Display the network architecture in the terminal.
+   */
+  void displayNetwork() const;
+
+  /*!
+   * \brief Size the weight layers in the network according to its architecture.
+   */
+  void sizeWeights();
+
+  /*!
+   * \brief Size the vector of previous inputs.
+   * \param[in] n_inputs - Number of inputs.
+   */
+  void sizeInputs(unsigned long n_inputs) {
+    last_inputs.resize(n_inputs);
+    for (unsigned long iInput = 0; iInput < n_inputs; iInput++) last_inputs[iInput] = 0.0;
+  }
+
+  /*!
+   * \brief Get the number of connecting regions in the network.
+   * \returns number of spaces in between layers.
+   */
+  unsigned long getNWeightLayers() const { return total_layers.size() - 1; }
+
+  /*!
+   * \brief Get the total number of layers in the network
+   * \returns number of netowork layers.
+   */
+  unsigned long getNLayers() const { return total_layers.size(); }
+
+  /*!
+   * \brief Get neuron count in a layer.
+   * \param[in] iLayer - Layer index.
+   * \returns number of neurons in the layer.
+   */
+  unsigned long getNNeurons(unsigned long iLayer) const { return total_layers[iLayer]->getNNeurons(); }
+
+  /*!
+   * \brief Evaluate the network.
+   * \param[in] inputs - Network input variable values.
+   * \param[in] compute_gradient - Compute the derivatives of the outputs wrt inputs.
+   */
+  void predict(su2vector<su2double>& inputs, bool compute_gradient = false);
+
+  /*!
+   * \brief Set the normalization factors for the input layer
+   * \param[in] iInput - Input index.
+   * \param[in] input_min - Minimum input value.
+   * \param[in] input_max - Maximum input value.
+   */
+  void SetInputNorm(unsigned long iInput, su2double input_min, su2double input_max) {
+    input_norm[iInput] = make_pair(input_min, input_max);
+  }
+
+  /*!
+   * \brief Set the normalization factors for the output layer
+   * \param[in] iOutput - Input index.
+   * \param[in] input_min - Minimum output value.
+   * \param[in] input_max - Maximum output value.
+   */
+  void SetOutputNorm(unsigned long iOutput, su2double output_min, su2double output_max) {
+    output_norm[iOutput] = make_pair(output_min, output_max);
+  }
+
+  std::pair<su2double, su2double> GetInputNorm(unsigned long iInput) const { return input_norm[iInput]; }
+
+  std::pair<su2double, su2double> GetOutputNorm(unsigned long iOutput) const { return output_norm[iOutput]; }
+  /*!
+   * \brief Add an output variable name to the network.
+   * \param[in] input - Input variable name.
+   */
+  void SetOutputName(size_t iOutput, std::string input) { output_names[iOutput] = input; }
+
+  /*!
+   * \brief Add an input variable name to the network.
+   * \param[in] output - Output variable name.
+   */
+  void SetInputName(size_t iInput, std::string input) { input_names[iInput] = input; }
+
+  /*!
+   * \brief Get network input variable name.
+   * \param[in] iInput - Input variable index.
+   * \returns input variable name.
+   */
+  std::string GetInputName(std::size_t iInput) const { return input_names[iInput]; }
+
+  /*!
+   * \brief Get network output variable name.
+   * \param[in] iOutput - Output variable index.
+   * \returns output variable name.
+   */
+  std::string GetOutputName(std::size_t iOutput) const { return output_names[iOutput]; }
+
+  /*!
+   * \brief Get network number of inputs.
+   * \returns Number of network inputs
+   */
+  std::size_t GetnInputs() const { return input_names.size(); }
+
+  /*!
+   * \brief Get network number of outputs.
+   * \returns Number of network outputs
+   */
+  std::size_t GetnOutputs() const { return output_names.size(); }
+
+  /*!
+   * \brief Get network evaluation output.
+   * \param[in] iOutput - output index.
+   * \returns Prediction value.
+   */
+  su2double GetANN_Output(std::size_t iOutput) const { return ANN_outputs[iOutput]; }
+
+  /*!
+   * \brief Get network output derivative w.r.t specific input.
+   * \param[in] iOutput - output variable index.
+   * \param[in] iInput - input variable index.
+   * \returns Output derivative w.r.t input.
+   */
+  su2double GetANN_Output_Input_Derivative(std::size_t iOutput, std::size_t iInput) const {
+    return dOutputs_dInputs[iOutput][iInput];
+  }
+
+  /*!
+   * \brief Set the activation function array size.
+   * \param[in] n_layers - network layer count.
+   */
+  void SizeActivationFunctions(unsigned long n_layers) {
+    activation_function_types = new ENUM_ACTIVATION_FUNCTION[n_layers];
+  }
+
+  /*!
+   * \brief Compute neuron activation function input.
+   * \param[in] iLayer - Network layer index.
+   * \param[in] iNeuron - Layer neuron index.
+   * \returns Neuron activation function input.
+   */
+  su2double ComputeX(std::size_t iLayer, std::size_t iNeuron) const {
+    su2double x;
+    x = total_layers[iLayer]->getBias(iNeuron);
+    std::size_t nNeurons_previous = total_layers[iLayer - 1]->getNNeurons();
+    for (std::size_t jNeuron = 0; jNeuron < nNeurons_previous; jNeuron++) {
+      x += weights_mat[iLayer - 1][iNeuron][jNeuron] * total_layers[iLayer - 1]->getOutput(jNeuron);
     }
-    su2double ComputedOutputdInput(std::size_t iLayer, std::size_t iNeuron, std::size_t iInput) const {
-        su2double doutput_dinput = 0;
-        for(auto jNeuron=0u; jNeuron<total_layers[iLayer - 1]->getNNeurons(); jNeuron++){
-            doutput_dinput += weights_mat[iLayer - 1][iNeuron][jNeuron] * total_layers[iLayer-1]->getdYdX(jNeuron, iInput);
-        }
-        return doutput_dinput;
+    return x;
+  }
+  su2double ComputedOutputdInput(std::size_t iLayer, std::size_t iNeuron, std::size_t iInput) const {
+    su2double doutput_dinput = 0;
+    for (auto jNeuron = 0u; jNeuron < total_layers[iLayer - 1]->getNNeurons(); jNeuron++) {
+      doutput_dinput += weights_mat[iLayer - 1][iNeuron][jNeuron] * total_layers[iLayer - 1]->getdYdX(jNeuron, iInput);
     }
+    return doutput_dinput;
+  }
 };
 
-
-}
-
-
+}  // namespace MLPToolbox
\ No newline at end of file
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
index 1f131c96dab..0a709a97b84 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
@@ -27,91 +27,88 @@
 #pragma once
 
 #include <cmath>
+#include <cstdlib>
 #include <iostream>
 #include <limits>
-#include <cstdlib>
 
 #include "../../CConfig.hpp"
 
-namespace MLPToolbox{
-class CNeuron
-{
-private:
-    unsigned long i_neuron;         /*!< Neuron identification number */
-    su2double output{0},            /*!< Output value of the current neuron */
-              input{0},             /*!< Input value of the current neuron */
-              doutput_dinput{0},    /*!< Gradient of output with respect to input */
-              bias{0};              /*!< Bias value at current neuron */
-    su2vector<su2double> doutput_dinputs;
-
-public:
-
-    /*!
-    * \brief Set neuron identification number
-    * \param[in] input - Identification number
-    */
-    void setNumber(unsigned long input) { i_neuron = input; }
-
-    /*!
-    * \brief Get neuron identification number
-    * \return Identification number
-    */
-    unsigned long getNumber() const { return i_neuron; }
-
-    /*!
-    * \brief Set neuron output value
-    * \param[in] input - activation function output value
-    */
-    void setOutput(su2double input) { output = input; }
-
-    /*!
-    * \brief Get neuron output value
-    * \return Output value
-    */
-    su2double getOutput() const { return output; }
-
-    /*!
-    * \brief Set neuron input value
-    * \param[in] input - activation function input value
-    */
-    void setInput(su2double x) { input = x; }
-
-    /*!
-    * \brief Get neuron input value
-    * \return input value
-    */
-    su2double getInput() const { return input; }
-
-    /*!
-    * \brief Set neuron bias
-    * \param[in] input - bias value
-    */
-    void setBias(su2double input) { bias = input; }
-
-    /*!
-    * \brief Get neuron bias value
-    * \return bias value
-    */
-    su2double getBias() const { return bias; }
-
-    /*!
-    * \brief Size the derivative of the neuron output wrt MLP inputs.
-    * \param[in] nInputs - Number of MLP inputs.
-    */
-    void sizeGradient(std::size_t nInputs) { doutput_dinputs.resize(nInputs); }
-    
-    /*!
-    * \brief Set neuron output gradient with respect to its input value
-    * \param[in] input - Derivative of activation function with respect to input
-    */
-    void setGradient(std::size_t iInput, su2double input) { doutput_dinputs[iInput] = input; }
-
-    /*!
-    * \brief Get neuron output gradient with respect to input value
-    * \return output gradient wrt input value
-    */
-    su2double getGradient(std::size_t iInput) const { return doutput_dinputs[iInput]; }
+namespace MLPToolbox {
+class CNeuron {
+ private:
+  unsigned long i_neuron; /*!< Neuron identification number */
+  su2double output{0},    /*!< Output value of the current neuron */
+      input{0},           /*!< Input value of the current neuron */
+      doutput_dinput{0},  /*!< Gradient of output with respect to input */
+      bias{0};            /*!< Bias value at current neuron */
+  su2vector<su2double> doutput_dinputs;
+
+ public:
+  /*!
+   * \brief Set neuron identification number
+   * \param[in] input - Identification number
+   */
+  void setNumber(unsigned long input) { i_neuron = input; }
+
+  /*!
+   * \brief Get neuron identification number
+   * \return Identification number
+   */
+  unsigned long getNumber() const { return i_neuron; }
+
+  /*!
+   * \brief Set neuron output value
+   * \param[in] input - activation function output value
+   */
+  void setOutput(su2double input) { output = input; }
+
+  /*!
+   * \brief Get neuron output value
+   * \return Output value
+   */
+  su2double getOutput() const { return output; }
+
+  /*!
+   * \brief Set neuron input value
+   * \param[in] input - activation function input value
+   */
+  void setInput(su2double x) { input = x; }
+
+  /*!
+   * \brief Get neuron input value
+   * \return input value
+   */
+  su2double getInput() const { return input; }
+
+  /*!
+   * \brief Set neuron bias
+   * \param[in] input - bias value
+   */
+  void setBias(su2double input) { bias = input; }
+
+  /*!
+   * \brief Get neuron bias value
+   * \return bias value
+   */
+  su2double getBias() const { return bias; }
+
+  /*!
+   * \brief Size the derivative of the neuron output wrt MLP inputs.
+   * \param[in] nInputs - Number of MLP inputs.
+   */
+  void sizeGradient(std::size_t nInputs) { doutput_dinputs.resize(nInputs); }
+
+  /*!
+   * \brief Set neuron output gradient with respect to its input value
+   * \param[in] input - Derivative of activation function with respect to input
+   */
+  void setGradient(std::size_t iInput, su2double input) { doutput_dinputs[iInput] = input; }
+
+  /*!
+   * \brief Get neuron output gradient with respect to input value
+   * \return output gradient wrt input value
+   */
+  su2double getGradient(std::size_t iInput) const { return doutput_dinputs[iInput]; }
 };
 
-}
-
+}  // namespace MLPToolbox
\ No newline at end of file
diff --git a/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
index 5a0291dbf82..e9f930032bb 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
@@ -27,129 +27,131 @@
 #pragma once
 
 #include <cmath>
+#include <cstdlib>
 #include <iostream>
 #include <limits>
-#include <cstdlib>
 #include <vector>
+
 #include "../../CConfig.hpp"
 #include "../../containers/CFileReaderLUT.hpp"
-namespace MLPToolbox{
+namespace MLPToolbox {
 
 class CReadNeuralNetwork {
-    private:
-    su2vector<std::string> input_names,   /*!< Input variable names. */
-                           output_names;  /*!< Output variable names. */
-
-    std::string filename;       /*!< MLP input filename. */
-
-    unsigned long n_layers;     /*!< Network total layer count. */
-    
-    su2vector<unsigned long> n_neurons;  /*!<  Neuron count per layer. */
-
-    su2vector<su2activematrix> weights_mat; /*!< Network synapse weights. */
-
-    su2vector<su2vector<su2double>> biases_mat; /*!< Bias values per neuron. */
-
-    su2vector<std::string> activation_functions;    /*!< Activation function per layer. */
-
-    su2vector<std::pair<su2double, su2double>> input_norm,  /*!< Input variable normalization values (min, max). */
-                                               output_norm; /*!< Output variable normalization values (min, max). */
-    public:
-
-    /*!
-    * \brief CReadNeuralNetwork class constructor
-    * \param[in] filename_in - .mlp input file name containing network information.
-    */
-    CReadNeuralNetwork(std::string filename_in);
-
-    /*!
-    * \brief Read input file and store necessary information
-    */
-    void ReadMLPFile();
-
-    /*!
-    * \brief Go to a specific line in file.
-    * \param[in] file_stream - input file stream.
-    * \param[in] flag - line to be skipped to.
-    * \returns flag line
-    */
-    std::string SkipToFlag(std::ifstream *file_stream, std::string flag);
-    
-    /*!
-    * \brief Get number of read input variables.
-    * \returns Number of neurons in the input layer.
-    */
-    unsigned long GetNInputs() const { return n_neurons[0]; }
-
-    /*!
-    * \brief Get number of read output variables.
-    * \returns Number of neurons in the output layer.
-    */
-    unsigned long GetNOutputs() const { return n_neurons[n_layers - 1]; }
-
-    /*!
-    * \brief Get total number of layers in the network.
-    * \returns Total layer count.
-    */
-    unsigned long GetNlayers() const { return n_layers; }
-
-    /*!
-    * \brief Get neuron count of a specific layer.
-    * \param[in] iLayer - Total layer index.
-    * \returns Number of neurons in the layer.
-    */
-    unsigned long GetNneurons(std::size_t iLayer) const { return n_neurons[iLayer]; }
-
-    /*!
-    * \brief Get synapse weight between two neurons in subsequent layers.
-    * \param[in] iLayer - Total layer index.
-    * \param[in] iNeuron - Neuron index in layer with index iLayer.
-    * \param[in] jNeuron - Neuron index in subsequent layer.
-    * \returns Weight value
-    */
-    su2double GetWeight(std::size_t iLayer, std::size_t iNeuron, std::size_t jNeuron) const { return weights_mat[iLayer][iNeuron][jNeuron]; }
-
-    /*!
-    * \brief Get bias value of specific neuron.
-    * \param[in] iLayer - Total layer index.
-    * \param[in] iNeuron - Neuron index.
-    * \returns Bias value
-    */
-    su2double GetBias(std::size_t iLayer, std::size_t iNeuron) const { return biases_mat[iLayer][iNeuron]; }
-
-    /*!
-    * \brief Get input variable normalization values.
-    * \param[in] iInput - Input variable index.
-    * \returns Input normalization values (min first, max second)
-    */
-    std::pair<su2double, su2double> GetInputNorm(std::size_t iInput) const { return input_norm[iInput]; }
-
-    /*!
-    * \brief Get output variable normalization values.
-    * \param[in] iOutput - Input variable index.
-    * \returns Output normalization values (min first, max second)
-    */
-    std::pair<su2double, su2double> GetOutputNorm(std::size_t iOutput) const { return output_norm[iOutput]; }
-
-    /*!
-    * \brief Get layer activation function type.
-    * \param[in] iLayer - Total layer index.
-    * \returns Layer activation function type.
-    */
-    std::string GetActivationFunction(std::size_t iLayer) const { return activation_functions[iLayer]; }
-
-    /*!
-    * \brief Get input variable name.
-    * \param[in] iInput - Input variable index.
-    * \returns Input variable name.
-    */
-    std::string GetInputName(std::size_t iInput) const { return input_names[iInput]; }
-
-    /*!
-    * \brief Get output variable name.
-    * \param[in] iOutput - Output variable index.
-    * \returns Output variable name.
-    */
-    std::string GetOutputName(std::size_t iOutput) const { return output_names[iOutput]; }
+ private:
+  su2vector<std::string> input_names, /*!< Input variable names. */
+      output_names;                   /*!< Output variable names. */
+
+  std::string filename; /*!< MLP input filename. */
+
+  unsigned long n_layers; /*!< Network total layer count. */
+
+  su2vector<unsigned long> n_neurons; /*!<  Neuron count per layer. */
+
+  su2vector<su2activematrix> weights_mat; /*!< Network synapse weights. */
+
+  su2vector<su2vector<su2double>> biases_mat; /*!< Bias values per neuron. */
+
+  su2vector<std::string> activation_functions; /*!< Activation function per layer. */
+
+  su2vector<std::pair<su2double, su2double>> input_norm, /*!< Input variable normalization values (min, max). */
+      output_norm;                                       /*!< Output variable normalization values (min, max). */
+ public:
+  /*!
+   * \brief CReadNeuralNetwork class constructor
+   * \param[in] filename_in - .mlp input file name containing network information.
+   */
+  CReadNeuralNetwork(std::string filename_in);
+
+  /*!
+   * \brief Read input file and store necessary information
+   */
+  void ReadMLPFile();
+
+  /*!
+   * \brief Go to a specific line in file.
+   * \param[in] file_stream - input file stream.
+   * \param[in] flag - line to be skipped to.
+   * \returns flag line
+   */
+  std::string SkipToFlag(std::ifstream* file_stream, std::string flag);
+
+  /*!
+   * \brief Get number of read input variables.
+   * \returns Number of neurons in the input layer.
+   */
+  unsigned long GetNInputs() const { return n_neurons[0]; }
+
+  /*!
+   * \brief Get number of read output variables.
+   * \returns Number of neurons in the output layer.
+   */
+  unsigned long GetNOutputs() const { return n_neurons[n_layers - 1]; }
+
+  /*!
+   * \brief Get total number of layers in the network.
+   * \returns Total layer count.
+   */
+  unsigned long GetNlayers() const { return n_layers; }
+
+  /*!
+   * \brief Get neuron count of a specific layer.
+   * \param[in] iLayer - Total layer index.
+   * \returns Number of neurons in the layer.
+   */
+  unsigned long GetNneurons(std::size_t iLayer) const { return n_neurons[iLayer]; }
+
+  /*!
+   * \brief Get synapse weight between two neurons in subsequent layers.
+   * \param[in] iLayer - Total layer index.
+   * \param[in] iNeuron - Neuron index in layer with index iLayer.
+   * \param[in] jNeuron - Neuron index in subsequent layer.
+   * \returns Weight value
+   */
+  su2double GetWeight(std::size_t iLayer, std::size_t iNeuron, std::size_t jNeuron) const {
+    return weights_mat[iLayer][iNeuron][jNeuron];
+  }
+
+  /*!
+   * \brief Get bias value of specific neuron.
+   * \param[in] iLayer - Total layer index.
+   * \param[in] iNeuron - Neuron index.
+   * \returns Bias value
+   */
+  su2double GetBias(std::size_t iLayer, std::size_t iNeuron) const { return biases_mat[iLayer][iNeuron]; }
+
+  /*!
+   * \brief Get input variable normalization values.
+   * \param[in] iInput - Input variable index.
+   * \returns Input normalization values (min first, max second)
+   */
+  std::pair<su2double, su2double> GetInputNorm(std::size_t iInput) const { return input_norm[iInput]; }
+
+  /*!
+   * \brief Get output variable normalization values.
+   * \param[in] iOutput - Input variable index.
+   * \returns Output normalization values (min first, max second)
+   */
+  std::pair<su2double, su2double> GetOutputNorm(std::size_t iOutput) const { return output_norm[iOutput]; }
+
+  /*!
+   * \brief Get layer activation function type.
+   * \param[in] iLayer - Total layer index.
+   * \returns Layer activation function type.
+   */
+  std::string GetActivationFunction(std::size_t iLayer) const { return activation_functions[iLayer]; }
+
+  /*!
+   * \brief Get input variable name.
+   * \param[in] iInput - Input variable index.
+   * \returns Input variable name.
+   */
+  std::string GetInputName(std::size_t iInput) const { return input_names[iInput]; }
+
+  /*!
+   * \brief Get output variable name.
+   * \param[in] iOutput - Output variable index.
+   * \returns Output variable name.
+   */
+  std::string GetOutputName(std::size_t iOutput) const { return output_names[iOutput]; }
 };
-}
+}  // namespace MLPToolbox
\ No newline at end of file
diff --git a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
index 3eb37f7cb07..1f48f6f5292 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
@@ -1,6 +1,6 @@
 /*!
  * \file CIOMap.cpp
- * \brief Implementation of the input-output mapping class for the 
+ * \brief Implementation of the input-output mapping class for the
  *      use of multi-layer perceptrons in SU2
  * \author E. Bunschoten
  * \version 7.5.0 "Blackbird"
@@ -32,48 +32,51 @@
 #include <cmath>
 #include <fstream>
 
-MLPToolbox::CIOMap::CIOMap(CLookUp_ANN*MLP_collection, su2vector<std::string> &inputs, su2vector<std::string> &outputs){
-    /* Generate an input-output map given a set of call inputs and call outputs. These inputs are 
-    mapped to the inputs of the loaded MLPs in the MLP_collection object. The call outputs are 
-    then matched to the MLPs with matching inputs.
-    */
-    PairVariableswithMLPs(MLP_collection, inputs, outputs);
+#include "../../../include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp"
 
-    // Perform checks on input-output validity
-    if(outputs.size() > 0){
-        // Check wether all call inputs are used
-        MLP_collection->Check_Use_of_Inputs(inputs, this);
+MLPToolbox::CIOMap::CIOMap(CLookUp_ANN* MLP_collection, su2vector<std::string>& inputs,
+                           su2vector<std::string>& outputs) {
 
-        // Check wether all call outputs are present in the MLP collection
-        MLP_collection->Check_Use_of_Outputs(outputs, this);
-    }
-}
-void MLPToolbox::CIOMap::PairVariableswithMLPs(CLookUp_ANN*MLP_collection, su2vector<std::string> &inputs, su2vector<std::string> &outputs){
-    /*
-    In this function, the call inputs and outputs are matched to those within the MLP collection. 
-    */
-    bool isInput, isOutput;
+    /* Generate an input-output map given a set of call inputs and call outputs. These inputs 
+  mapped to the inputs of the loaded MLPs in the MLP_collection object. The call outputs are
+  then matched to the MLPs with matching inputs.
+  */
+  PairVariableswithMLPs(MLP_collection, inputs, outputs);
 
-    // Looping over the loaded MLPs to check wether the MLP inputs match with the call inputs
-    for(size_t iMLP=0; iMLP<MLP_collection->GetNANNs(); iMLP++){
+  // Perform checks on input-output validity
+  if (outputs.size() > 0) {
+    // Check wether all call inputs are used
+    MLP_collection->Check_Use_of_Inputs(inputs, this);
 
-        // Mapped call inputs to MLP inputs
-        std::vector<pair<size_t, size_t>> Input_Indices = MLP_collection->FindVariable_Indices(iMLP, inputs, true);
-        isInput = Input_Indices.size() > 0;
+    // Check wether all call outputs are present in the MLP collection
+    MLP_collection->Check_Use_of_Outputs(outputs, this);
+  }
+}
+void MLPToolbox::CIOMap::PairVariableswithMLPs(CLookUp_ANN* MLP_collection, su2vector<std::string>& inputs,
+                                               su2vector<std::string>& outputs) {
+  /*
+  In this function, the call inputs and outputs are matched to those within the MLP collection.
+  */
+  bool isInput, isOutput;
 
-        if(isInput){
-            // Only when the MLP inputs match with a portion of the call inputs are the output variable checks performed
+  // Looping over the loaded MLPs to check wether the MLP inputs match with the call inputs
+  for (size_t iMLP = 0; iMLP < MLP_collection->GetNANNs(); iMLP++) {
+    // Mapped call inputs to MLP inputs
+    std::vector<pair<size_t, size_t>> Input_Indices = MLP_collection->FindVariable_Indices(iMLP, inputs, true);
+    isInput = Input_Indices.size() > 0;
 
-            std::vector<pair<size_t, size_t>> Output_Indices = MLP_collection->FindVariable_Indices(iMLP, outputs, false);
-            isOutput = Output_Indices.size() > 0;
+    if (isInput) {
+      // Only when the MLP inputs match with a portion of the call inputs are the output variable checks performed
 
-            if(isOutput){
+      std::vector<pair<size_t, size_t>> Output_Indices = MLP_collection->FindVariable_Indices(iMLP, outputs, false);
+      isOutput = Output_Indices.size() > 0;
 
-                // Update input and output mapping if both inputs and outputs match
-                MLP_indices.push_back(iMLP);
-                Input_Map.push_back(Input_Indices);
-                Output_Map.push_back(Output_Indices);
-            }
-        }
+      if (isOutput) {
+        // Update input and output mapping if both inputs and outputs match
+        MLP_indices.push_back(iMLP);
+        Input_Map.push_back(Input_Indices);
+        Output_Map.push_back(Output_Indices);
+      }
     }
+  }
 }
\ No newline at end of file
diff --git a/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp b/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp
index db5ab9f5e47..82da5aa6a50 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp
@@ -26,25 +26,25 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 #include "../../../include/toolboxes/multilayer_perceptron/CLayer.hpp"
+
 #include <cstring>
 using namespace std;
 
 MLPToolbox::CLayer::CLayer() : CLayer(1) {}
 
-MLPToolbox::CLayer::CLayer(unsigned long n_neurons) : number_of_neurons{n_neurons}, is_input{false}
-{
-    neurons = new CNeuron[n_neurons];
-    for(size_t i=0; i<number_of_neurons; i++){
-        neurons[i].setNumber(i+1);
-    }
+MLPToolbox::CLayer::CLayer(unsigned long n_neurons) : number_of_neurons{n_neurons}, is_input{false} {
+  neurons = new CNeuron[n_neurons];
+  for (size_t i = 0; i < number_of_neurons; i++) {
+    neurons[i].setNumber(i + 1);
+  }
 }
 
-void MLPToolbox::CLayer::setNNeurons(unsigned long n_neurons){
-    if(number_of_neurons != n_neurons){
-        delete [] neurons;
-        neurons = new CNeuron[n_neurons];
-        for(size_t i=0; i<number_of_neurons; i++){
-            neurons[i].setNumber(i+1);
-        }
+void MLPToolbox::CLayer::setNNeurons(unsigned long n_neurons) {
+  if (number_of_neurons != n_neurons) {
+    delete[] neurons;
+    neurons = new CNeuron[n_neurons];
+    for (size_t i = 0; i < number_of_neurons; i++) {
+      neurons[i].setNumber(i + 1);
     }
-}
+  }
+}
\ No newline at end of file
diff --git a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
index c596224d808..71f99b4834a 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
@@ -1,6 +1,6 @@
 /*!
  * \file CLookUp_ANN.cpp
- * \brief Implementation of the multi-layer perceptron class to be 
+ * \brief Implementation of the multi-layer perceptron class to be
  *      used for look-up operations.
  * \author E.C.Bunschoten
  * \version 7.5.0 "Blackbird"
@@ -26,223 +26,223 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 #include "../../../include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp"
-#include "../../../include/toolboxes/multilayer_perceptron/CIOMap.hpp"
-#include "../../../include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp"
-#include <iostream>
-#include <string>
+
 #include <cmath>
 #include <fstream>
+#include <iostream>
+#include <string>
+
+#include "../../../include/toolboxes/multilayer_perceptron/CIOMap.hpp"
+#include "../../../include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp"
 
 using namespace std;
 
-MLPToolbox::CLookUp_ANN::CLookUp_ANN(const unsigned short n_inputs, const string*input_filenames)
-{
-    #ifdef HAVE_MPI
-    MPI_Comm_rank(MPI_COMM_WORLD, &rank);
-    #endif
-    if(rank == MASTER_NODE)
-        cout << "Generating ANN collection" << endl;
-
-    number_of_variables = n_inputs;
-
-    NeuralNetworks.resize(n_inputs);
-    for(auto i_MLP=0u; i_MLP < n_inputs; i_MLP++){
-        NeuralNetworks[i_MLP] = new CNeuralNetwork;
-        if(rank == MASTER_NODE) 
-            cout << "Generating neural network for " << input_filenames[i_MLP] << endl;
-        GenerateANN(NeuralNetworks[i_MLP], input_filenames[i_MLP]);
-    }
-        
-}
+MLPToolbox::CLookUp_ANN::CLookUp_ANN(const unsigned short n_inputs, const string* input_filenames) {
+#ifdef HAVE_MPI
+  MPI_Comm_rank(MPI_COMM_WORLD, &rank);
+#endif
+  if (rank == MASTER_NODE) cout << "Generating ANN collection" << endl;
 
-vector<pair<size_t, size_t>> MLPToolbox::CLookUp_ANN::FindVariable_Indices(size_t i_ANN, su2vector<string> variable_names, bool input) const {
-    /*--- Find loaded MLPs that have the same input variable names as the variables listed in variable_names ---*/
+  number_of_variables = n_inputs;
 
-    vector<pair<size_t, size_t>> variable_indices;
-    auto nVar = input ? NeuralNetworks[i_ANN]->GetnInputs() : NeuralNetworks[i_ANN]->GetnOutputs();
+  NeuralNetworks.resize(n_inputs);
+  for (auto i_MLP = 0u; i_MLP < n_inputs; i_MLP++) {
+    NeuralNetworks[i_MLP] = new CNeuralNetwork;
+    if (rank == MASTER_NODE) cout << "Generating neural network for " << input_filenames[i_MLP] << endl;
+    GenerateANN(NeuralNetworks[i_MLP], input_filenames[i_MLP]);
+  }
+}
 
-    for(auto iVar=0u; iVar<nVar; iVar++){
-        for(auto jVar=0u; jVar<variable_names.size(); jVar++){
-            string ANN_varname = input ? NeuralNetworks[i_ANN]->GetInputName(iVar) : NeuralNetworks[i_ANN]->GetOutputName(iVar);
-            if(variable_names[jVar].compare(ANN_varname) == 0){
-                variable_indices.push_back(make_pair(jVar, iVar));
-            }
-        }
+vector<pair<size_t, size_t>> MLPToolbox::CLookUp_ANN::FindVariable_Indices(size_t i_ANN,
+                                                                           su2vector<string> variable_names,
+                                                                           bool input) const {
+  /*--- Find loaded MLPs that have the same input variable names as the variables listed in variable_names ---*/
+
+  vector<pair<size_t, size_t>> variable_indices;
+  auto nVar = input ? NeuralNetworks[i_ANN]->GetnInputs() : NeuralNetworks[i_ANN]->GetnOutputs();
+
+  for (auto iVar = 0u; iVar < nVar; iVar++) {
+    for (auto jVar = 0u; jVar < variable_names.size(); jVar++) {
+      string ANN_varname =
+          input ? NeuralNetworks[i_ANN]->GetInputName(iVar) : NeuralNetworks[i_ANN]->GetOutputName(iVar);
+      if (variable_names[jVar].compare(ANN_varname) == 0) {
+        variable_indices.push_back(make_pair(jVar, iVar));
+      }
     }
-    return variable_indices;
+  }
+  return variable_indices;
 }
 
-unsigned long MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap *input_output_map, su2vector<su2double>& inputs, su2vector<su2double*>& outputs){
-    /*--- Evaluate MLP based on target input and output variables ---*/
-    bool within_range,              // Within MLP training set range.
-         MLP_was_evaluated = false; // MLP was evaluated within training set range.
-
-    /* If queries lie outside the training data set, the nearest MLP will be evaluated through extrapolation. */
-    su2double distance_to_query = 1e20; // Overall smallest distance between training data set middle and query.
-    size_t i_ANN_nearest = 0,           // Index of nearest MLP.
-           i_map_nearest = 0;           // Index of nearest iomap index.
-
-    for(auto i_map=0u; i_map<input_output_map->GetNMLPs(); i_map++){
-        within_range = true;
-        auto i_ANN = input_output_map->GetMLPIndex(i_map);
-        auto ANN_inputs = input_output_map->GetMLP_Inputs(i_map, inputs);
-        
-        su2double distance_to_query_i = 0;
-        for(auto i_input=0u; i_input < ANN_inputs.size(); i_input++) {
-            auto ANN_input_limits = NeuralNetworks[i_ANN]->GetInputNorm(i_input);
-
-            /* Check if query input lies outside MLP training range */
-            if((ANN_inputs[i_input] < ANN_input_limits.first) || (ANN_inputs[i_input] > ANN_input_limits.second)) {
-                within_range = false;
-            }
-
-            /* Calculate distance between MLP training range center point and query */
-            su2double middle = 0.5*(ANN_input_limits.second + ANN_input_limits.first);
-            distance_to_query_i += pow((ANN_inputs[i_input] - middle)/(ANN_input_limits.second - ANN_input_limits.first), 2);
-        }
-        
-        /* Evaluate MLP when query inputs lie within training data range */
-        if(within_range){
-            NeuralNetworks[i_ANN]->predict(ANN_inputs);
-            MLP_was_evaluated = true;
-            for(auto i=0u; i < input_output_map->GetNMappedOutputs(i_map); i++){
-                *outputs[input_output_map->GetOutputIndex(i_map, i)] = NeuralNetworks[i_ANN]->GetANN_Output(input_output_map->GetMLPOutputIndex(i_map, i));
-            }
-        }
-
-        /* Update minimum distance to query */
-        if(sqrt(distance_to_query_i) < distance_to_query){
-            i_ANN_nearest = i_ANN;
-            distance_to_query = distance_to_query_i;
-            i_map_nearest = i_map;
-        }
-    }
-    /* Evaluate nearest MLP in case no query data within range is found */
-    if(!MLP_was_evaluated) {
-        auto ANN_inputs = input_output_map->GetMLP_Inputs(i_map_nearest, inputs);
-        NeuralNetworks[i_ANN_nearest]->predict(ANN_inputs);
-        for(auto i=0u; i < input_output_map->GetNMappedOutputs(i_map_nearest); i++){
-            *outputs[input_output_map->GetOutputIndex(i_map_nearest, i)] = NeuralNetworks[i_ANN_nearest]->GetANN_Output(input_output_map->GetMLPOutputIndex(i_map_nearest, i));
-        }
+unsigned long MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap* input_output_map, su2vector<su2double>& inputs,
+                                                   su2vector<su2double*>& outputs) {
+  /*--- Evaluate MLP based on target input and output variables ---*/
+  bool within_range,              // Within MLP training set range.
+      MLP_was_evaluated = false;  // MLP was evaluated within training set range.
+
+  /* If queries lie outside the training data set, the nearest MLP will be evaluated through extrapolation. */
+  su2double distance_to_query = 1e20;  // Overall smallest distance between training data set middle and query.
+  size_t i_ANN_nearest = 0,            // Index of nearest MLP.
+      i_map_nearest = 0;               // Index of nearest iomap index.
+
+  for (auto i_map = 0u; i_map < input_output_map->GetNMLPs(); i_map++) {
+    within_range = true;
+    auto i_ANN = input_output_map->GetMLPIndex(i_map);
+    auto ANN_inputs = input_output_map->GetMLP_Inputs(i_map, inputs);
+
+    su2double distance_to_query_i = 0;
+    for (auto i_input = 0u; i_input < ANN_inputs.size(); i_input++) {
+      auto ANN_input_limits = NeuralNetworks[i_ANN]->GetInputNorm(i_input);
+
+      /* Check if query input lies outside MLP training range */
+      if ((ANN_inputs[i_input] < ANN_input_limits.first) || (ANN_inputs[i_input] > ANN_input_limits.second)) {
+        within_range = false;
+      }
+
+      /* Calculate distance between MLP training range center point and query */
+      su2double middle = 0.5 * (ANN_input_limits.second + ANN_input_limits.first);
+      distance_to_query_i +=
+          pow((ANN_inputs[i_input] - middle) / (ANN_input_limits.second - ANN_input_limits.first), 2);
     }
 
-    /* Return 1 if query data lies outside the range of any of the loaded MLPs */
-    return MLP_was_evaluated ? 0 : 1;
-}
-
-void MLPToolbox::CLookUp_ANN::GenerateANN(CNeuralNetwork * ANN, string fileName)
-{
-    /*--- Generate MLP architecture based on information in MLP input file ---*/
-
-    /* Read MLP input file */
-    CReadNeuralNetwork Reader = CReadNeuralNetwork(fileName);
-    
-    /* Read MLP input file */
-    Reader.ReadMLPFile();
-
-    /* Generate basic layer architectures */
-    ANN->defineInputLayer(Reader.GetNInputs());
-    ANN->sizeInputs(Reader.GetNInputs());
-    for(auto iInput=0u; iInput<Reader.GetNInputs(); iInput++){
-        ANN->SetInputName(iInput, Reader.GetInputName(iInput));
+    /* Evaluate MLP when query inputs lie within training data range */
+    if (within_range) {
+      NeuralNetworks[i_ANN]->predict(ANN_inputs);
+      MLP_was_evaluated = true;
+      for (auto i = 0u; i < input_output_map->GetNMappedOutputs(i_map); i++) {
+        *outputs[input_output_map->GetOutputIndex(i_map, i)] =
+            NeuralNetworks[i_ANN]->GetANN_Output(input_output_map->GetMLPOutputIndex(i_map, i));
+      }
     }
-    for(auto iLayer=1u; iLayer<Reader.GetNlayers()-1; iLayer++){
-        ANN->push_hidden_layer(Reader.GetNneurons(iLayer));
+
+    /* Update minimum distance to query */
+    if (sqrt(distance_to_query_i) < distance_to_query) {
+      i_ANN_nearest = i_ANN;
+      distance_to_query = distance_to_query_i;
+      i_map_nearest = i_map;
     }
-    ANN->defineOutputLayer(Reader.GetNOutputs());
-    for(auto iOutput=0u; iOutput<Reader.GetNOutputs(); iOutput++){
-        ANN->SetOutputName(iOutput, Reader.GetOutputName(iOutput));
+  }
+  /* Evaluate nearest MLP in case no query data within range is found */
+  if (!MLP_was_evaluated) {
+    auto ANN_inputs = input_output_map->GetMLP_Inputs(i_map_nearest, inputs);
+    NeuralNetworks[i_ANN_nearest]->predict(ANN_inputs);
+    for (auto i = 0u; i < input_output_map->GetNMappedOutputs(i_map_nearest); i++) {
+      *outputs[input_output_map->GetOutputIndex(i_map_nearest, i)] =
+          NeuralNetworks[i_ANN_nearest]->GetANN_Output(input_output_map->GetMLPOutputIndex(i_map_nearest, i));
     }
+  }
 
-    /* Size weights of each layer */
-    ANN->sizeWeights();
-
-    /* Define weights and activation functions */
-    ANN->SizeActivationFunctions(ANN->getNWeightLayers()+1);
-    for(auto i_layer=0u; i_layer < ANN->getNWeightLayers(); i_layer++){
-        ANN->setActivationFunction(i_layer, Reader.GetActivationFunction(i_layer));
-        for(auto i_neuron=0u; i_neuron < ANN->getNNeurons(i_layer); i_neuron++){
-            for(auto j_neuron=0u; j_neuron<ANN->getNNeurons(i_layer+1); j_neuron++){
-                ANN->setWeight(i_layer, i_neuron, j_neuron, Reader.GetWeight(i_layer, i_neuron, j_neuron));
-            }
-        }
+  /* Return 1 if query data lies outside the range of any of the loaded MLPs */
+  return MLP_was_evaluated ? 0 : 1;
+}
 
-        
-    }
-    ANN->setActivationFunction(ANN->getNWeightLayers(), Reader.GetActivationFunction(ANN->getNWeightLayers()));
-    
-    /* Set neuron biases */
-    for(auto i_layer=0u; i_layer<ANN->getNWeightLayers()+1; i_layer++){
-        for(auto i_neuron=0u; i_neuron<ANN->getNNeurons(i_layer); i_neuron++){
-            ANN->setBias(i_layer, i_neuron, Reader.GetBias(i_layer, i_neuron));
-        }
-    }
-    
-    /* Define input and output layer normalization values */
-    for(auto iInput=0u; iInput<Reader.GetNInputs(); iInput++){
-        ANN->SetInputNorm(iInput, Reader.GetInputNorm(iInput).first, Reader.GetInputNorm(iInput).second);
+void MLPToolbox::CLookUp_ANN::GenerateANN(CNeuralNetwork* ANN, string fileName) {
+  /*--- Generate MLP architecture based on information in MLP input file ---*/
+
+  /* Read MLP input file */
+  CReadNeuralNetwork Reader = CReadNeuralNetwork(fileName);
+
+  /* Read MLP input file */
+  Reader.ReadMLPFile();
+
+  /* Generate basic layer architectures */
+  ANN->defineInputLayer(Reader.GetNInputs());
+  ANN->sizeInputs(Reader.GetNInputs());
+  for (auto iInput = 0u; iInput < Reader.GetNInputs(); iInput++) {
+    ANN->SetInputName(iInput, Reader.GetInputName(iInput));
+  }
+  for (auto iLayer = 1u; iLayer < Reader.GetNlayers() - 1; iLayer++) {
+    ANN->push_hidden_layer(Reader.GetNneurons(iLayer));
+  }
+  ANN->defineOutputLayer(Reader.GetNOutputs());
+  for (auto iOutput = 0u; iOutput < Reader.GetNOutputs(); iOutput++) {
+    ANN->SetOutputName(iOutput, Reader.GetOutputName(iOutput));
+  }
+
+  /* Size weights of each layer */
+  ANN->sizeWeights();
+
+  /* Define weights and activation functions */
+  ANN->SizeActivationFunctions(ANN->getNWeightLayers() + 1);
+  for (auto i_layer = 0u; i_layer < ANN->getNWeightLayers(); i_layer++) {
+    ANN->setActivationFunction(i_layer, Reader.GetActivationFunction(i_layer));
+    for (auto i_neuron = 0u; i_neuron < ANN->getNNeurons(i_layer); i_neuron++) {
+      for (auto j_neuron = 0u; j_neuron < ANN->getNNeurons(i_layer + 1); j_neuron++) {
+        ANN->setWeight(i_layer, i_neuron, j_neuron, Reader.GetWeight(i_layer, i_neuron, j_neuron));
+      }
     }
-    for(auto iOutput=0u; iOutput<Reader.GetNOutputs(); iOutput++){
-        ANN->SetOutputNorm(iOutput, Reader.GetOutputNorm(iOutput).first, Reader.GetOutputNorm(iOutput).second);
+  }
+  ANN->setActivationFunction(ANN->getNWeightLayers(), Reader.GetActivationFunction(ANN->getNWeightLayers()));
+
+  /* Set neuron biases */
+  for (auto i_layer = 0u; i_layer < ANN->getNWeightLayers() + 1; i_layer++) {
+    for (auto i_neuron = 0u; i_neuron < ANN->getNNeurons(i_layer); i_neuron++) {
+      ANN->setBias(i_layer, i_neuron, Reader.GetBias(i_layer, i_neuron));
     }
-    
+  }
+
+  /* Define input and output layer normalization values */
+  for (auto iInput = 0u; iInput < Reader.GetNInputs(); iInput++) {
+    ANN->SetInputNorm(iInput, Reader.GetInputNorm(iInput).first, Reader.GetInputNorm(iInput).second);
+  }
+  for (auto iOutput = 0u; iOutput < Reader.GetNOutputs(); iOutput++) {
+    ANN->SetOutputNorm(iOutput, Reader.GetOutputNorm(iOutput).first, Reader.GetOutputNorm(iOutput).second);
+  }
 }
 
-bool MLPToolbox::CLookUp_ANN::Check_Use_of_Inputs(su2vector<string> &input_names, CIOMap *input_output_map) const {
-    /*--- Check wether all input variables are in the loaded MLPs ---*/
-    vector<string> missing_inputs;
-    bool inputs_are_present{true};
-    for(auto iInput=0u; iInput<input_names.size(); iInput ++){
-        bool found_input = false;
-        for(auto i_map=0u; i_map < input_output_map->GetNMLPs(); i_map++){
-            auto input_map = input_output_map->GetInputMapping(i_map);
-            for(auto jInput=0u; jInput<input_map.size(); jInput++){
-                if(input_map[jInput].first == iInput){
-                    found_input = true;
-                }
-            }
+bool MLPToolbox::CLookUp_ANN::Check_Use_of_Inputs(su2vector<string>& input_names, CIOMap* input_output_map) const {
+  /*--- Check wether all input variables are in the loaded MLPs ---*/
+  vector<string> missing_inputs;
+  bool inputs_are_present{true};
+  for (auto iInput = 0u; iInput < input_names.size(); iInput++) {
+    bool found_input = false;
+    for (auto i_map = 0u; i_map < input_output_map->GetNMLPs(); i_map++) {
+      auto input_map = input_output_map->GetInputMapping(i_map);
+      for (auto jInput = 0u; jInput < input_map.size(); jInput++) {
+        if (input_map[jInput].first == iInput) {
+          found_input = true;
         }
-        if(!found_input){
-            missing_inputs.push_back(input_names[iInput]);
-            inputs_are_present = false;
-        };
-    }
-    if(missing_inputs.size() > 0){
-        string message{"Inputs "};
-        for(size_t iVar=0; iVar<missing_inputs.size(); iVar++) message += missing_inputs[iVar] + " ";
-        SU2_MPI::Error(message + "are not present in any loaded ANN.", CURRENT_FUNCTION);
+      }
     }
-    return inputs_are_present;
+    if (!found_input) {
+      missing_inputs.push_back(input_names[iInput]);
+      inputs_are_present = false;
+    };
+  }
+  if (missing_inputs.size() > 0) {
+    string message{"Inputs "};
+    for (size_t iVar = 0; iVar < missing_inputs.size(); iVar++) message += missing_inputs[iVar] + " ";
+    SU2_MPI::Error(message + "are not present in any loaded ANN.", CURRENT_FUNCTION);
+  }
+  return inputs_are_present;
 }
 
-bool MLPToolbox::CLookUp_ANN::Check_Use_of_Outputs(su2vector<string> &output_names, CIOMap * input_output_map) const {
-    /*--- Check wether all output variables are in the loaded MLPs ---*/
-    
-    vector<string> missing_outputs;     
-    bool outputs_are_present{true};
-    /* Looping over the target outputs */
-    for(auto iOutput=0u; iOutput<output_names.size(); iOutput ++){
+bool MLPToolbox::CLookUp_ANN::Check_Use_of_Outputs(su2vector<string>& output_names, CIOMap* input_output_map) const {
+  /*--- Check wether all output variables are in the loaded MLPs ---*/
 
-        bool found_output{false};
+  vector<string> missing_outputs;
+  bool outputs_are_present{true};
+  /* Looping over the target outputs */
+  for (auto iOutput = 0u; iOutput < output_names.size(); iOutput++) {
+    bool found_output{false};
 
-        /* Looping over all the selected ANNs */
-        for(auto i_map=0u; i_map < input_output_map->GetNMLPs(); i_map++){
-            auto output_map = input_output_map->GetOutputMapping(i_map);
+    /* Looping over all the selected ANNs */
+    for (auto i_map = 0u; i_map < input_output_map->GetNMLPs(); i_map++) {
+      auto output_map = input_output_map->GetOutputMapping(i_map);
 
-            /* Looping over the outputs of the output map of the current ANN */
-            for(auto jOutput=0u; jOutput<output_map.size(); jOutput++){
-                if(output_map[jOutput].first == iOutput) found_output = true;
-            }
-        }
-        if(!found_output){
-            missing_outputs.push_back(output_names[iOutput]);
-            outputs_are_present = false;
-        };
-    }
-    if(missing_outputs.size() > 0){
-        string message{"Outputs "};
-        for(size_t iVar=0; iVar<missing_outputs.size(); iVar++) message += missing_outputs[iVar] + " ";
-        SU2_MPI::Error(message + "are not present in any loaded ANN.", CURRENT_FUNCTION);
+      /* Looping over the outputs of the output map of the current ANN */
+      for (auto jOutput = 0u; jOutput < output_map.size(); jOutput++) {
+        if (output_map[jOutput].first == iOutput) found_output = true;
+      }
     }
-    return outputs_are_present;
+    if (!found_output) {
+      missing_outputs.push_back(output_names[iOutput]);
+      outputs_are_present = false;
+    };
+  }
+  if (missing_outputs.size() > 0) {
+    string message{"Outputs "};
+    for (size_t iVar = 0; iVar < missing_outputs.size(); iVar++) message += missing_outputs[iVar] + " ";
+    SU2_MPI::Error(message + "are not present in any loaded ANN.", CURRENT_FUNCTION);
+  }
+  return outputs_are_present;
 }
\ No newline at end of file
diff --git a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
index a8da9b9e840..954562a7f0b 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
@@ -26,298 +26,300 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 #include "../../../include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp"
-#include "../../../include/toolboxes/multilayer_perceptron/CLayer.hpp"
+
 #include <iostream>
+
+#include "../../../include/toolboxes/multilayer_perceptron/CLayer.hpp"
 #include "../../../include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp"
 using namespace std;
 
+void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double>& inputs, bool compute_gradient) {
+  /*--- Evaluate MLP for given inputs ---*/
 
-void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double> &inputs, bool compute_gradient){
-    /*--- Evaluate MLP for given inputs ---*/
+  su2double y = 0, dy_dx = 0;  // Activation function output.
+  bool same_point = true;
+  /* Normalize input and check if inputs are the same w.r.t last evaluation */
+  for (auto iNeuron = 0u; iNeuron < inputLayer->getNNeurons(); iNeuron++) {
+    su2double x_norm =
+        (inputs[iNeuron] - input_norm[iNeuron].first) / (input_norm[iNeuron].second - input_norm[iNeuron].first);
+    if (abs(x_norm - inputLayer->getOutput(iNeuron)) > 0) same_point = false;
+    inputLayer->setOutput(iNeuron, x_norm);
 
-    su2double y, dy_dx;           // Activation function output.
-    bool same_point = true;
-    /* Normalize input and check if inputs are the same w.r.t last evaluation */
-    for(auto iNeuron=0u; iNeuron<inputLayer->getNNeurons(); iNeuron++){
-        su2double x_norm = (inputs[iNeuron] - input_norm[iNeuron].first)/(input_norm[iNeuron].second - input_norm[iNeuron].first);
-        if(abs(x_norm - inputLayer->getOutput(iNeuron)) > 0) same_point = false;
-        inputLayer->setOutput(iNeuron, x_norm);
+    if (compute_gradient)
+      inputLayer->setdYdX(iNeuron, iNeuron, 1 / (input_norm[iNeuron].second - input_norm[iNeuron].first));
+  }
+  /* Skip evaluation process if current point is the same as during the previous evaluation */
+  if (!same_point) {
+    su2double alpha = 1.67326324;
+    su2double lambda = 1.05070098;
+    /* Traverse MLP and compute inputs and outputs for the neurons in each layer */
+    for (auto iLayer = 1u; iLayer < n_hidden_layers + 2; iLayer++) {
+      auto nNeurons_current = total_layers[iLayer]->getNNeurons();  // Neuron count of current layer
+      su2double x;                                                  // Neuron input value
 
-        if(compute_gradient) inputLayer->setdYdX(iNeuron, iNeuron, 1 / (input_norm[iNeuron].second - input_norm[iNeuron].first));
-    }
-    /* Skip evaluation process if current point is the same as during the previous evaluation */
-    if(!same_point){
-        su2double alpha=1.67326324;
-        su2double lambda=1.05070098;
-        /* Traverse MLP and compute inputs and outputs for the neurons in each layer */
-        for(auto iLayer=1u; iLayer<n_hidden_layers + 2; iLayer++){
-            auto nNeurons_current = total_layers[iLayer]->getNNeurons(); // Neuron count of current layer
-            su2double x;    // Neuron input value
-            
-            /* Compute and store input value for each neuron */
-            for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
-                x = ComputeX(iLayer, iNeuron);
-                total_layers[iLayer]->setInput(iNeuron, x);
-                if(compute_gradient){
-                    for(auto iInput=0u; iInput<inputLayer->getNNeurons(); iInput++){
-                        dy_dx = ComputedOutputdInput(iLayer, iNeuron, iInput);
-                        total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx);
-                    }
-                }
-            }
+      /* Compute and store input value for each neuron */
+      for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
+        x = ComputeX(iLayer, iNeuron);
+        total_layers[iLayer]->setInput(iNeuron, x);
+        if (compute_gradient) {
+          for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
+            dy_dx = ComputedOutputdInput(iLayer, iNeuron, iInput);
+            total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx);
+          }
+        }
+      }
 
-            /* Compute and store neuron output based on activation function */
-            switch (activation_function_types[iLayer])
-                {
-                case ENUM_ACTIVATION_FUNCTION::ELU:
-                    for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
-                        x = total_layers[iLayer]->getInput(iNeuron);
-                        if(x > 0){
-                            y = x;
-                            if(compute_gradient) dy_dx = 1.0;
-                        }else{
-                            y = exp(x) - 1;
-                            if(compute_gradient) dy_dx = exp(x);
-                        }
-                        total_layers[iLayer]->setOutput(iNeuron, y);
-                        if(compute_gradient){
-                            for(auto iInput=0u; iInput<inputLayer->getNNeurons(); iInput++){
-                                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
-                            }
-                        }
-                    }
-                    break;
-                case ENUM_ACTIVATION_FUNCTION::LINEAR:
-                    for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
-                        x = total_layers[iLayer]->getInput(iNeuron);
-                        y = x;
-                        total_layers[iLayer]->setOutput(iNeuron, y);
-                        if(compute_gradient){
-                            dy_dx = 1.0;
-                            for(auto iInput=0u; iInput<inputLayer->getNNeurons(); iInput++){
-                                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
-                            }
-                        }
-                    }
-                    break;
-                case ENUM_ACTIVATION_FUNCTION::RELU:
-                    for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
-                        x = total_layers[iLayer]->getInput(iNeuron);
-                        if(x > 0){
-                            y = x;
-                            if(compute_gradient) dy_dx = 1.0;
-                        }else{
-                            y = 0.0;
-                            if(compute_gradient) dy_dx = 0.0;
-                        }
-                        total_layers[iLayer]->setOutput(iNeuron, y);
-                        if(compute_gradient){
-                            for(auto iInput=0u; iInput<inputLayer->getNNeurons(); iInput++){
-                                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
-                            }
-                        }
-                    }
-                    break;
-                case ENUM_ACTIVATION_FUNCTION::SWISH:
-                    for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
-                        x = total_layers[iLayer]->getInput(iNeuron);
-                        y = x / (1 + exp(-x));
-                        total_layers[iLayer]->setOutput(iNeuron, y);
-                        if(compute_gradient){
-                            dy_dx = exp(x)*(x + exp(x) + 1)/pow(exp(x) + 1, 2);
-                            for(auto iInput=0u; iInput<inputLayer->getNNeurons(); iInput++){
-                                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
-                            }
-                        }
-                    }
-                    break;
-                case ENUM_ACTIVATION_FUNCTION::TANH:
-                    for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
-                        x = total_layers[iLayer]->getInput(iNeuron);
-                        y = tanh(x);
-                        total_layers[iLayer]->setOutput(iNeuron, y);
-                        if(compute_gradient){
-                            dy_dx = 1 / pow(cosh(x), 2);
-                            for(auto iInput=0u; iInput<inputLayer->getNNeurons(); iInput++){
-                                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
-                            }
-                        }
-                    }
-                    break;
-                case ENUM_ACTIVATION_FUNCTION::SIGMOID:
-                    for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
-                        x = total_layers[iLayer]->getInput(iNeuron);
-                        y = 1.0/(1 + exp(-x));
-                        total_layers[iLayer]->setOutput(iNeuron, y);
-                        if(compute_gradient){
-                            dy_dx = exp(-x) / pow(exp(-x) + 1, 2);
-                            for(auto iInput=0u; iInput<inputLayer->getNNeurons(); iInput++){
-                                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
-                            }
-                        }
-                    }
-                    break;
-                case ENUM_ACTIVATION_FUNCTION::SELU:
-                    for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
-                        x = total_layers[iLayer]->getInput(iNeuron);
-                        if(x > 0.0){
-                            y = lambda * x;
-                            if(compute_gradient) dy_dx = lambda;
-                        }else{
-                            y = lambda * alpha * (exp(x) - 1);
-                            if(compute_gradient) dy_dx = lambda * alpha * exp(x);
-                        }
-                        total_layers[iLayer]->setOutput(iNeuron, y);
-                        if(compute_gradient){
-                            for(auto iInput=0u; iInput<inputLayer->getNNeurons(); iInput++){
-                                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
-                            }
-                        }
-                    }
-                    break;
-                case ENUM_ACTIVATION_FUNCTION::GELU:
-                    for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
-                        x = total_layers[iLayer]->getInput(iNeuron);
+      /* Compute and store neuron output based on activation function */
+      switch (activation_function_types[iLayer]) {
+        case ENUM_ACTIVATION_FUNCTION::ELU:
+          for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
+            x = total_layers[iLayer]->getInput(iNeuron);
+            if (x > 0) {
+              y = x;
+              if (compute_gradient) dy_dx = 1.0;
+            } else {
+              y = exp(x) - 1;
+              if (compute_gradient) dy_dx = exp(x);
+            }
+            total_layers[iLayer]->setOutput(iNeuron, y);
+            if (compute_gradient) {
+              for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
+                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+              }
+            }
+          }
+          break;
+        case ENUM_ACTIVATION_FUNCTION::LINEAR:
+          for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
+            x = total_layers[iLayer]->getInput(iNeuron);
+            y = x;
+            total_layers[iLayer]->setOutput(iNeuron, y);
+            if (compute_gradient) {
+              dy_dx = 1.0;
+              for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
+                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+              }
+            }
+          }
+          break;
+        case ENUM_ACTIVATION_FUNCTION::RELU:
+          for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
+            x = total_layers[iLayer]->getInput(iNeuron);
+            if (x > 0) {
+              y = x;
+              if (compute_gradient) dy_dx = 1.0;
+            } else {
+              y = 0.0;
+              if (compute_gradient) dy_dx = 0.0;
+            }
+            total_layers[iLayer]->setOutput(iNeuron, y);
+            if (compute_gradient) {
+              for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
+                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+              }
+            }
+          }
+          break;
+        case ENUM_ACTIVATION_FUNCTION::SWISH:
+          for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
+            x = total_layers[iLayer]->getInput(iNeuron);
+            y = x / (1 + exp(-x));
+            total_layers[iLayer]->setOutput(iNeuron, y);
+            if (compute_gradient) {
+              dy_dx = exp(x) * (x + exp(x) + 1) / pow(exp(x) + 1, 2);
+              for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
+                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+              }
+            }
+          }
+          break;
+        case ENUM_ACTIVATION_FUNCTION::TANH:
+          for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
+            x = total_layers[iLayer]->getInput(iNeuron);
+            y = tanh(x);
+            total_layers[iLayer]->setOutput(iNeuron, y);
+            if (compute_gradient) {
+              dy_dx = 1 / pow(cosh(x), 2);
+              for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
+                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+              }
+            }
+          }
+          break;
+        case ENUM_ACTIVATION_FUNCTION::SIGMOID:
+          for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
+            x = total_layers[iLayer]->getInput(iNeuron);
+            y = 1.0 / (1 + exp(-x));
+            total_layers[iLayer]->setOutput(iNeuron, y);
+            if (compute_gradient) {
+              dy_dx = exp(-x) / pow(exp(-x) + 1, 2);
+              for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
+                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+              }
+            }
+          }
+          break;
+        case ENUM_ACTIVATION_FUNCTION::SELU:
+          for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
+            x = total_layers[iLayer]->getInput(iNeuron);
+            if (x > 0.0) {
+              y = lambda * x;
+              if (compute_gradient) dy_dx = lambda;
+            } else {
+              y = lambda * alpha * (exp(x) - 1);
+              if (compute_gradient) dy_dx = lambda * alpha * exp(x);
+            }
+            total_layers[iLayer]->setOutput(iNeuron, y);
+            if (compute_gradient) {
+              for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
+                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+              }
+            }
+          }
+          break;
+        case ENUM_ACTIVATION_FUNCTION::GELU:
+          for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
+            x = total_layers[iLayer]->getInput(iNeuron);
 
-                        y = 0.5 * x * (1 + tanh(sqrt(2 / PI_NUMBER) * (x + 0.044715 * pow(x, 3))));
-                        total_layers[iLayer]->setOutput(iNeuron, y);
-                        if(compute_gradient){
-                            dy_dx = 0.5*(tanh(0.0356774*pow(x, 3) + 0.797885 * x) + (0.107032*pow(x, 3) + 0.797885*x)*pow(cosh(x), -2)*(0.0356774*pow(x, 3) + 0.797885 * x));
-                            for(auto iInput=0u; iInput<inputLayer->getNNeurons(); iInput++){
-                                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
-                            }
-                        }
-                    }
-                    break;
-                case ENUM_ACTIVATION_FUNCTION::NONE:
-                    for(auto iNeuron=0u; iNeuron<nNeurons_current; iNeuron++){
-                        y = 0.0;
-                        total_layers[iLayer]->setOutput(iNeuron, y);
-                        if(compute_gradient){
-                            dy_dx = 0.0;
-                            for(auto iInput=0u; iInput<inputLayer->getNNeurons(); iInput++){
-                                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
-                            }
-                        }
-                    }
-                    break;
-                default:
-                    break;
-                } // activation_function_types
-        }
-    }
-    /* Compute and de-normalize MLP output */
-    for(auto iNeuron=0u; iNeuron<outputLayer->getNNeurons(); iNeuron++){
-        su2double y_norm = outputLayer->getOutput(iNeuron);
-        y = y_norm*(output_norm[iNeuron].second - output_norm[iNeuron].first) + output_norm[iNeuron].first;
-        if(compute_gradient){
-            dy_dx = (output_norm[iNeuron].second - output_norm[iNeuron].first);
-            for(auto iInput=0u; iInput<inputLayer->getNNeurons(); iInput++){
-                outputLayer->setdYdX(iNeuron, iInput, dy_dx * outputLayer->getdYdX(iNeuron, iInput));
-                dOutputs_dInputs[iNeuron][iInput] = outputLayer->getdYdX(iNeuron, iInput);
+            y = 0.5 * x * (1 + tanh(sqrt(2 / PI_NUMBER) * (x + 0.044715 * pow(x, 3))));
+            total_layers[iLayer]->setOutput(iNeuron, y);
+            if (compute_gradient) {
+              dy_dx = 0.5 * (tanh(0.0356774 * pow(x, 3) + 0.797885 * x) + (0.107032 * pow(x, 3) + 0.797885 * x) *
+                                                                              pow(cosh(x), -2) *
+                                                                              (0.0356774 * pow(x, 3) + 0.797885 * x));
+              for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
+                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+              }
             }
-        }
-        /* Storing output value */
-        ANN_outputs[iNeuron] = y;
+          }
+          break;
+        case ENUM_ACTIVATION_FUNCTION::NONE:
+          for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
+            y = 0.0;
+            total_layers[iLayer]->setOutput(iNeuron, y);
+            if (compute_gradient) {
+              dy_dx = 0.0;
+              for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
+                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+              }
+            }
+          }
+          break;
+        default:
+          break;
+      }  // activation_function_types
+    }
+  }
+  /* Compute and de-normalize MLP output */
+  for (auto iNeuron = 0u; iNeuron < outputLayer->getNNeurons(); iNeuron++) {
+    su2double y_norm = outputLayer->getOutput(iNeuron);
+    y = y_norm * (output_norm[iNeuron].second - output_norm[iNeuron].first) + output_norm[iNeuron].first;
+    if (compute_gradient) {
+      dy_dx = (output_norm[iNeuron].second - output_norm[iNeuron].first);
+      for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
+        outputLayer->setdYdX(iNeuron, iInput, dy_dx * outputLayer->getdYdX(iNeuron, iInput));
+        dOutputs_dInputs[iNeuron][iInput] = outputLayer->getdYdX(iNeuron, iInput);
+      }
     }
+    /* Storing output value */
+    ANN_outputs[iNeuron] = y;
+  }
 }
 
+void MLPToolbox::CNeuralNetwork::defineInputLayer(unsigned long n_neurons) {
+  /*--- Define the input layer of the network ---*/
+  inputLayer = new CLayer(n_neurons);
 
-void MLPToolbox::CNeuralNetwork::defineInputLayer(unsigned long n_neurons){
-    /*--- Define the input layer of the network ---*/
-    inputLayer = new CLayer(n_neurons);
-
-    /* Mark layer as input layer */
-    inputLayer->setInput(true);
-    input_norm.resize(n_neurons);
-    input_names.resize(n_neurons);
+  /* Mark layer as input layer */
+  inputLayer->setInput(true);
+  input_norm.resize(n_neurons);
+  input_names.resize(n_neurons);
 }
 
-void MLPToolbox::CNeuralNetwork::defineOutputLayer(unsigned long n_neurons){
-    /*--- Define the output layer of the network ---*/
-    outputLayer = new CLayer(n_neurons);
-    output_norm.resize(n_neurons);
-    output_names.resize(n_neurons);
+void MLPToolbox::CNeuralNetwork::defineOutputLayer(unsigned long n_neurons) {
+  /*--- Define the output layer of the network ---*/
+  outputLayer = new CLayer(n_neurons);
+  output_norm.resize(n_neurons);
+  output_names.resize(n_neurons);
 }
 
-void MLPToolbox::CNeuralNetwork::push_hidden_layer(unsigned long n_neurons){
-    /*--- Add a hidden layer to the network ---*/
-    CLayer *newLayer = new CLayer(n_neurons);
-    hiddenLayers.push_back(newLayer);
-    n_hidden_layers ++;
+void MLPToolbox::CNeuralNetwork::push_hidden_layer(unsigned long n_neurons) {
+  /*--- Add a hidden layer to the network ---*/
+  CLayer* newLayer = new CLayer(n_neurons);
+  hiddenLayers.push_back(newLayer);
+  n_hidden_layers++;
 }
 
-void MLPToolbox::CNeuralNetwork::sizeWeights(){
-    /*--- Size weight matrices based on neuron counts in each layer ---*/
+void MLPToolbox::CNeuralNetwork::sizeWeights() {
+  /*--- Size weight matrices based on neuron counts in each layer ---*/
 
-    /* Generate vector containing input, output, and hidden layer references */
-    total_layers.resize(n_hidden_layers + 2);
-    total_layers[0] = inputLayer;
-    for(auto iLayer=0u; iLayer<n_hidden_layers; iLayer++){
-        total_layers[iLayer + 1] = hiddenLayers[iLayer];
-    }
-    total_layers[total_layers.size()-1] = outputLayer;
+  /* Generate vector containing input, output, and hidden layer references */
+  total_layers.resize(n_hidden_layers + 2);
+  total_layers[0] = inputLayer;
+  for (auto iLayer = 0u; iLayer < n_hidden_layers; iLayer++) {
+    total_layers[iLayer + 1] = hiddenLayers[iLayer];
+  }
+  total_layers[total_layers.size() - 1] = outputLayer;
 
-    weights_mat.resize(n_hidden_layers+1);
-    weights_mat[0].resize(hiddenLayers[0]->getNNeurons(), inputLayer->getNNeurons());
-    for(auto iLayer=1u; iLayer<n_hidden_layers; iLayer++){
-        weights_mat[iLayer].resize(hiddenLayers[iLayer]->getNNeurons(), hiddenLayers[iLayer-1]->getNNeurons());
-    }
-    weights_mat[n_hidden_layers].resize(outputLayer->getNNeurons(), hiddenLayers[n_hidden_layers-1]->getNNeurons());
+  weights_mat.resize(n_hidden_layers + 1);
+  weights_mat[0].resize(hiddenLayers[0]->getNNeurons(), inputLayer->getNNeurons());
+  for (auto iLayer = 1u; iLayer < n_hidden_layers; iLayer++) {
+    weights_mat[iLayer].resize(hiddenLayers[iLayer]->getNNeurons(), hiddenLayers[iLayer - 1]->getNNeurons());
+  }
+  weights_mat[n_hidden_layers].resize(outputLayer->getNNeurons(), hiddenLayers[n_hidden_layers - 1]->getNNeurons());
 
-    ANN_outputs = new su2double[outputLayer->getNNeurons()];
-    dOutputs_dInputs.resize(outputLayer->getNNeurons(), inputLayer->getNNeurons());
-    for(auto iLayer=0u; iLayer<n_hidden_layers+2; iLayer++){
-        total_layers[iLayer]->sizeGradients(inputLayer->getNNeurons());
-    }
-}   
+  ANN_outputs = new su2double[outputLayer->getNNeurons()];
+  dOutputs_dInputs.resize(outputLayer->getNNeurons(), inputLayer->getNNeurons());
+  for (auto iLayer = 0u; iLayer < n_hidden_layers + 2; iLayer++) {
+    total_layers[iLayer]->sizeGradients(inputLayer->getNNeurons());
+  }
+}
 
 void MLPToolbox::CNeuralNetwork::displayNetwork() const {
-    /*!
-    TODO:
-    find way of displaying network architectures
-    */
+  /*!
+  TODO:
+  find way of displaying network architectures
+  */
 }
 
-void MLPToolbox::CNeuralNetwork::setActivationFunction(unsigned long i_layer, string input)
-{
-    /*--- Translate activation function name from input file to a number ---*/
-    if(input.compare("linear") == 0){
-        activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::LINEAR;
-        return;
-    }
-    if(input.compare("relu") == 0){
-        activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::RELU;
-        return;
-    }
-    if((input.compare("elu") == 0)){
-        activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::ELU;
-        return;
-    }
-    if(input.compare("swish") == 0){
-        activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::SWISH;
-        return;
-    }
-    if(input.compare("sigmoid") == 0){
-        activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::SIGMOID;
-        return;
-    }
-    if(input.compare("tanh") == 0){
-        activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::TANH;
-        return;
-    }
-    if(input.compare("selu") == 0){
-        activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::SELU;
-        return;
-    }
-    if(input.compare("gelu") == 0){
-        activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::GELU;
-        return;
-    }
-    if(input.compare("none") == 0){
-        activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::NONE;
-        return;
-    }
-    SU2_MPI::Error("Unknown activation function type: " + input, CURRENT_FUNCTION);
+void MLPToolbox::CNeuralNetwork::setActivationFunction(unsigned long i_layer, string input) {
+  /*--- Translate activation function name from input file to a number ---*/
+  if (input.compare("linear") == 0) {
+    activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::LINEAR;
+    return;
+  }
+  if (input.compare("relu") == 0) {
+    activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::RELU;
+    return;
+  }
+  if ((input.compare("elu") == 0)) {
+    activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::ELU;
+    return;
+  }
+  if (input.compare("swish") == 0) {
+    activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::SWISH;
+    return;
+  }
+  if (input.compare("sigmoid") == 0) {
+    activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::SIGMOID;
+    return;
+  }
+  if (input.compare("tanh") == 0) {
+    activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::TANH;
+    return;
+  }
+  if (input.compare("selu") == 0) {
+    activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::SELU;
+    return;
+  }
+  if (input.compare("gelu") == 0) {
+    activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::GELU;
+    return;
+  }
+  if (input.compare("none") == 0) {
+    activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::NONE;
     return;
+  }
+  SU2_MPI::Error("Unknown activation function type: " + input, CURRENT_FUNCTION);
+  return;
 }
diff --git a/Common/src/toolboxes/multilayer_perceptron/CNeuron.cpp b/Common/src/toolboxes/multilayer_perceptron/CNeuron.cpp
index 6c1446ea6e3..2ff20a60f09 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CNeuron.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CNeuron.cpp
@@ -1,6 +1,6 @@
 /*!
  * \file CNeuron.cpp
- * \brief Implementation of the neuron class to be used within the 
+ * \brief Implementation of the neuron class to be used within the
  *      Layer class as a part of the NeuralNetwork class.
  * \author E.C.Bunschoten
  * \version 7.5.0 "Blackbird"
@@ -26,8 +26,9 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 #include "../../../include/toolboxes/multilayer_perceptron/CNeuron.hpp"
-#include <iostream>
-#include <cstring>
+
 #include <cmath>
+#include <cstring>
+#include <iostream>
 
 using namespace std;
\ No newline at end of file
diff --git a/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
index c97b9173c38..ac31994e436 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
@@ -26,185 +26,173 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 #include "../../../include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp"
+
 #include "../../../include/containers/CFileReaderLUT.hpp"
 using namespace std;
 
-MLPToolbox::CReadNeuralNetwork::CReadNeuralNetwork(string filename_in) {
-    filename = filename_in;
-}
+MLPToolbox::CReadNeuralNetwork::CReadNeuralNetwork(string filename_in) { filename = filename_in; }
 
-void MLPToolbox::CReadNeuralNetwork::ReadMLPFile(){
-    ifstream file_stream;
-    file_stream.open(filename.c_str(), ifstream::in);
-    if (!file_stream.is_open()) {
-      SU2_MPI::Error(string("There is no MLP file called ") + filename,
-                    CURRENT_FUNCTION);
-    }
+void MLPToolbox::CReadNeuralNetwork::ReadMLPFile() {
+  ifstream file_stream;
+  file_stream.open(filename.c_str(), ifstream::in);
+  if (!file_stream.is_open()) {
+    SU2_MPI::Error(string("There is no MLP file called ") + filename, CURRENT_FUNCTION);
+  }
 
-    string line, word;
-    bool eoHeader = false, 
-         found_layercount = false, 
-         found_input_names = false, 
-         found_output_names = false;
+  string line, word;
+  bool eoHeader = false, found_layercount = false, found_input_names = false, found_output_names = false;
 
-    /* Read general architecture information from file header */
+  /* Read general architecture information from file header */
 
-    line = SkipToFlag(&file_stream, "<header>");
+  line = SkipToFlag(&file_stream, "<header>");
 
-    while(getline(file_stream, line) && !eoHeader){
+  while (getline(file_stream, line) && !eoHeader) {
+    /* Read layer count */
+    if (line.compare("[number of layers]") == 0) {
+      getline(file_stream, line);
+      n_layers = stoul(line);
+      n_neurons.resize(n_layers);
+      biases_mat.resize(n_layers);
+      weights_mat.resize(n_layers - 1);
+      activation_functions.resize(n_layers);
 
-      /* Read layer count */
-      if(line.compare("[number of layers]") == 0){
-        getline(file_stream, line);
-        n_layers = stoul(line);
-        n_neurons.resize(n_layers);
-        biases_mat.resize(n_layers);
-        weights_mat.resize(n_layers - 1);
-        activation_functions.resize(n_layers);
+      found_layercount = true;
+    }
 
-        found_layercount = true;
+    /* Set number of neurons for each layer */
+    if (line.compare("[neurons per layer]") == 0) {
+      /* In case layer count was not yet provided, return an error */
+      if (!found_layercount) {
+        SU2_MPI::Error("No layer count provided before defining neuron count per layer", CURRENT_FUNCTION);
       }
-
-      /* Set number of neurons for each layer */
-      if(line.compare("[neurons per layer]") == 0){
-
-        /* In case layer count was not yet provided, return an error */
-        if(!found_layercount){
-          SU2_MPI::Error("No layer count provided before defining neuron count per layer", CURRENT_FUNCTION);
-        }
-        /* Loop over layer count and size neuron count and bias count per layer accordingly */
-        for(auto iLayer=0u; iLayer<n_layers; iLayer++){
-          getline(file_stream, line);
-          n_neurons[iLayer] = stoul(line);
-          biases_mat[iLayer].resize(n_neurons[iLayer]);
-        }
-        /* Loop over spaces between layers and size the weight matrices accordingly */
-        for(auto iLayer=0u; iLayer<n_layers-1; iLayer++){
-          weights_mat[iLayer].resize(n_neurons[iLayer], n_neurons[iLayer + 1]);
-        }
-        /* Size input and output normalization and set default values */
-        input_norm.resize(n_neurons[0]);
-        for(auto iNeuron=0u; iNeuron<n_neurons[0]; iNeuron++) 
-          input_norm[iNeuron] = make_pair(0, 1);
-
-        output_norm.resize(n_neurons[n_neurons.size()-1]);
-        for(auto iNeuron=0u; iNeuron<n_neurons[n_neurons.size()-1]; iNeuron++) 
-          output_norm[iNeuron] = make_pair(0, 1);
+      /* Loop over layer count and size neuron count and bias count per layer accordingly */
+      for (auto iLayer = 0u; iLayer < n_layers; iLayer++) {
+        getline(file_stream, line);
+        n_neurons[iLayer] = stoul(line);
+        biases_mat[iLayer].resize(n_neurons[iLayer]);
       }
-
-      /* Read layer activation function types */
-      if(line.compare("[activation function]") == 0){
-        if(!found_layercount){
-          SU2_MPI::Error("No layer count provided before providing layer activation functions", CURRENT_FUNCTION);
-        }
-        for(auto iLayer=0u; iLayer<n_layers; iLayer++){
-          getline(file_stream, line);
-          istringstream activation_stream(line);
-          activation_stream >> word;
-          activation_functions[iLayer] = word;
-        }    
+      /* Loop over spaces between layers and size the weight matrices accordingly */
+      for (auto iLayer = 0u; iLayer < n_layers - 1; iLayer++) {
+        weights_mat[iLayer].resize(n_neurons[iLayer], n_neurons[iLayer + 1]);
       }
+      /* Size input and output normalization and set default values */
+      input_norm.resize(n_neurons[0]);
+      for (auto iNeuron = 0u; iNeuron < n_neurons[0]; iNeuron++) input_norm[iNeuron] = make_pair(0, 1);
 
-      /* Read MLP input variable names */
-      if(line.compare("[input names]") == 0){
-        found_input_names = true;
-        input_names.resize(n_neurons[0]);
-        for(auto iInput=0u; iInput < n_neurons[0]; iInput++) {
-          getline(file_stream, line);
-          input_names[iInput] = line;
-          
-        }
-      }
+      output_norm.resize(n_neurons[n_neurons.size() - 1]);
+      for (auto iNeuron = 0u; iNeuron < n_neurons[n_neurons.size() - 1]; iNeuron++)
+        output_norm[iNeuron] = make_pair(0, 1);
+    }
 
-      /* In case input normalization is applied, read upper and lower input bounds */
-      if(line.compare("[input normalization]") == 0){
-        for(auto iInput=0u; iInput<input_norm.size(); iInput++){
-          getline(file_stream, line);
-          if(line.compare("") != 0){
-            istringstream input_norm_stream(line);
-            input_norm_stream >> word;
-            su2double input_min = stold(word);
-            input_norm_stream >> word;
-            su2double input_max = stold(word);
-            input_norm[iInput] = make_pair(input_min, input_max);
-          }
-        }
+    /* Read layer activation function types */
+    if (line.compare("[activation function]") == 0) {
+      if (!found_layercount) {
+        SU2_MPI::Error("No layer count provided before providing layer activation functions", CURRENT_FUNCTION);
       }
+      for (auto iLayer = 0u; iLayer < n_layers; iLayer++) {
+        getline(file_stream, line);
+        istringstream activation_stream(line);
+        activation_stream >> word;
+        activation_functions[iLayer] = word;
+      }
+    }
 
-      /* Read MLP output variable names */
-      if(line.compare("[output names]") == 0){
-        found_output_names = true;
-        auto n_outputs = n_neurons[n_neurons.size() - 1];
-        output_names.resize(n_outputs);
-        for(auto iOutput=0u; iOutput<n_outputs; iOutput++){
-          getline(file_stream, line);
-          output_names[iOutput] = line;
-        }
-
-        if(output_names.size() != (n_neurons[n_neurons.size()-1])){
-          SU2_MPI::Error("Number of output variable names inconsistent with number of MLP outputs", CURRENT_FUNCTION);
-        }
+    /* Read MLP input variable names */
+    if (line.compare("[input names]") == 0) {
+      found_input_names = true;
+      input_names.resize(n_neurons[0]);
+      for (auto iInput = 0u; iInput < n_neurons[0]; iInput++) {
+        getline(file_stream, line);
+        input_names[iInput] = line;
       }
+    }
 
-      /* In case output normalization is applied, read upper and lower output bounds */
-      if(line.compare("[output normalization]") == 0){
-        for(auto iOutput=0u; iOutput<output_norm.size(); iOutput++){
-          getline(file_stream, line);
-          if(line.compare("") != 0){
-            istringstream output_norm_stream(line);
-            output_norm_stream >> word;
-            su2double output_min = stold(word);
-            output_norm_stream >> word;
-            su2double output_max = stold(word);
-            output_norm[iOutput] = make_pair(output_min, output_max);
-          }
+    /* In case input normalization is applied, read upper and lower input bounds */
+    if (line.compare("[input normalization]") == 0) {
+      for (auto iInput = 0u; iInput < input_norm.size(); iInput++) {
+        getline(file_stream, line);
+        if (line.compare("") != 0) {
+          istringstream input_norm_stream(line);
+          input_norm_stream >> word;
+          su2double input_min = stold(word);
+          input_norm_stream >> word;
+          su2double input_max = stold(word);
+          input_norm[iInput] = make_pair(input_min, input_max);
         }
       }
+    }
 
-      if(line.compare("</header>") == 0){
-        eoHeader = true;
+    /* Read MLP output variable names */
+    if (line.compare("[output names]") == 0) {
+      found_output_names = true;
+      auto n_outputs = n_neurons[n_neurons.size() - 1];
+      output_names.resize(n_outputs);
+      for (auto iOutput = 0u; iOutput < n_outputs; iOutput++) {
+        getline(file_stream, line);
+        output_names[iOutput] = line;
       }
-    } // eoHeader
 
-    /* Error checking */
-    if(!found_input_names){
-      SU2_MPI::Error("No MLP input variable names provided", CURRENT_FUNCTION);
-    }
-    if(!found_output_names){
-      SU2_MPI::Error("No MLP output variable names provided", CURRENT_FUNCTION);
+      if (output_names.size() != (n_neurons[n_neurons.size() - 1])) {
+        SU2_MPI::Error("Number of output variable names inconsistent with number of MLP outputs", CURRENT_FUNCTION);
+      }
     }
 
-    /* Read weights for each layer */
-    line = SkipToFlag(&file_stream, "[weights per layer]");
-    for(auto iLayer=0u; iLayer<n_layers-1; iLayer++){
-      getline(file_stream, line);
-      for(auto iNeuron=0u; iNeuron<n_neurons[iLayer]; iNeuron++){
+    /* In case output normalization is applied, read upper and lower output bounds */
+    if (line.compare("[output normalization]") == 0) {
+      for (auto iOutput = 0u; iOutput < output_norm.size(); iOutput++) {
         getline(file_stream, line);
-        istringstream weight_stream(line);
-        for(auto jNeuron=0u; jNeuron<n_neurons[iLayer+1]; jNeuron++){
-          weight_stream >> word;
-          weights_mat[iLayer][iNeuron][jNeuron] = stold(word);
+        if (line.compare("") != 0) {
+          istringstream output_norm_stream(line);
+          output_norm_stream >> word;
+          su2double output_min = stold(word);
+          output_norm_stream >> word;
+          su2double output_max = stold(word);
+          output_norm[iOutput] = make_pair(output_min, output_max);
         }
       }
-      getline(file_stream, line);
     }
-    
-    /* Read biases for each neuron */
-    line = SkipToFlag(&file_stream, "[biases per layer]");
-    for(auto iLayer=0u; iLayer<n_layers; iLayer++){
-      getline(file_stream, line);
-      istringstream bias_stream(line);
-      for(auto iNeuron=0u; iNeuron<n_neurons[iLayer]; iNeuron++){
-        bias_stream >> word;
-        biases_mat[iLayer][iNeuron] = stold(word);
-      }
+
+    if (line.compare("</header>") == 0) {
+      eoHeader = true;
     }
+  }  // eoHeader
 
+  /* Error checking */
+  if (!found_input_names) {
+    SU2_MPI::Error("No MLP input variable names provided", CURRENT_FUNCTION);
+  }
+  if (!found_output_names) {
+    SU2_MPI::Error("No MLP output variable names provided", CURRENT_FUNCTION);
+  }
 
+  /* Read weights for each layer */
+  line = SkipToFlag(&file_stream, "[weights per layer]");
+  for (auto iLayer = 0u; iLayer < n_layers - 1; iLayer++) {
+    getline(file_stream, line);
+    for (auto iNeuron = 0u; iNeuron < n_neurons[iLayer]; iNeuron++) {
+      getline(file_stream, line);
+      istringstream weight_stream(line);
+      for (auto jNeuron = 0u; jNeuron < n_neurons[iLayer + 1]; jNeuron++) {
+        weight_stream >> word;
+        weights_mat[iLayer][iNeuron][jNeuron] = stold(word);
+      }
+    }
+    getline(file_stream, line);
+  }
 
+  /* Read biases for each neuron */
+  line = SkipToFlag(&file_stream, "[biases per layer]");
+  for (auto iLayer = 0u; iLayer < n_layers; iLayer++) {
+    getline(file_stream, line);
+    istringstream bias_stream(line);
+    for (auto iNeuron = 0u; iNeuron < n_neurons[iLayer]; iNeuron++) {
+      bias_stream >> word;
+      biases_mat[iLayer][iNeuron] = stold(word);
+    }
+  }
 }
 
-string MLPToolbox::CReadNeuralNetwork::SkipToFlag(ifstream *file_stream, string flag) {
+string MLPToolbox::CReadNeuralNetwork::SkipToFlag(ifstream* file_stream, string flag) {
   /*--- Search file for a line and set it as the current line in the file stream ---*/
   string line;
   getline(*file_stream, line);
@@ -213,8 +201,7 @@ string MLPToolbox::CReadNeuralNetwork::SkipToFlag(ifstream *file_stream, string
     getline(*file_stream, line);
   }
 
-  if ((*file_stream).eof())
-    cout << "line not in file!" << endl;
+  if ((*file_stream).eof()) cout << "line not in file!" << endl;
 
   return line;
 }
\ No newline at end of file
diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index 81b03586d8f..4589e3a378a 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -28,76 +28,76 @@
 
 #pragma once
 
-#include "CFluidModel.hpp"
-#include "../../../Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp"
 #include "../../../Common/include/containers/CLookUpTable.hpp"
+#include "../../../Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp"
+#include "CFluidModel.hpp"
 
 /*!
  * \class CDataDrivenFluid
- * \brief Template class for fluid model definition using multi-layer perceptrons for 
+ * \brief Template class for fluid model definition using multi-layer perceptrons for
  * fluid dynamic state definition.
  * \author: E.Bunschoten.
  */
 class CDataDrivenFluid : public CFluidModel {
  protected:
+  unsigned short Kind_DataDriven_Method = ENUM_DATADRIVEN_METHOD::LUT;  // Interpolation method for data set evaluation
 
-  unsigned short Kind_DataDriven_Method = ENUM_DATADRIVEN_METHOD::LUT;       // Interpolation method for data set evaluation
+  size_t idx_rho,  // Interpolator index for density input
+      idx_e;       // Interpolator index for energy input
 
-  size_t idx_rho,    // Interpolator index for density input
-         idx_e;      // Interpolator index for energy input
+  su2double Newton_Relaxation,  // Relaxation factor for Newton solvers.
+      rho_start,                // Initial value for the density in Newton solver processes.
+      e_start;                  // Initial value for the energy in Newton solver processes.
 
-  su2double Newton_Relaxation,     // Relaxation factor for Newton solvers.
-            rho_start,             // Initial value for the density in Newton solver processes.
-            e_start;               // Initial value for the energy in Newton solver processes.
-  
   su2double dsde_rho, dsdrho_e, d2sde2, d2sdedrho, d2sdrho2;
-  
+
   su2double Gamma{0.0};           /*!< \brief Ratio of Specific Heats. */
   su2double Gamma_Minus_One{0.0}; /*!< \brief Ratio of Specific Heats Minus One. */
   su2double Gas_Constant{0.0};    /*!< \brief Gas Constant. */
-  
-  su2vector<string> input_names_rhoe,        // Data-driven method input variable names of the independent variables (density, energy).
-                 output_names_rhoe;       // Output variable names listed in the data-driven method input file name.
 
-  su2vector<su2double*> outputs_rhoe;        // Pointers to output variables.
+  su2vector<string>
+      input_names_rhoe,   // Data-driven method input variable names of the independent variables (density, energy).
+      output_names_rhoe;  // Output variable names listed in the data-driven method input file name.
+
+  su2vector<su2double*> outputs_rhoe;  // Pointers to output variables.
 
   /*--- Class variables for the multi-layer perceptron method ---*/
-  MLPToolbox::CLookUp_ANN * lookup_mlp;   // multi-layer perceptron collection.
-  MLPToolbox::CIOMap * iomap_rhoe;        // input-output map.
-  su2vector<su2double> MLP_inputs;           // inputs for the multi-layer perceptron look-up operation.
+  MLPToolbox::CLookUp_ANN* lookup_mlp;  // multi-layer perceptron collection.
+  MLPToolbox::CIOMap* iomap_rhoe;       // input-output map.
+  su2vector<su2double> MLP_inputs;      // inputs for the multi-layer perceptron look-up operation.
 
   /*--- Class variables for the look-up table method ---*/
-  CLookUpTable *lookup_table;
+  CLookUpTable* lookup_table;
 
-  unsigned long outside_dataset, // Density-energy combination lies outside data set.
-                nIter_Newton;    // Number of Newton solver iterations.
+  unsigned long outside_dataset,  // Density-energy combination lies outside data set.
+      nIter_Newton;               // Number of Newton solver iterations.
 
   /*!
-  * \brief Map dataset variables to specific look-up operations
-  */
+   * \brief Map dataset variables to specific look-up operations
+   */
   void MapInputs_to_Outputs();
 
   /*!
-  * \brief Evaluate dataset through multi-layer perceptron.
-  * \param[in] rho - Density value.
-  * \param[in] e - Static energy value.
-  * \return Query point lies outside MLP normalization range (0 is inside, 1 is outside).
-  */
+   * \brief Evaluate dataset through multi-layer perceptron.
+   * \param[in] rho - Density value.
+   * \param[in] e - Static energy value.
+   * \return Query point lies outside MLP normalization range (0 is inside, 1 is outside).
+   */
   unsigned long Predict_MLP(su2double rho, su2double e);
 
   /*!
-  * \brief Evaluate dataset through look-up table.
-  * \param[in] rho - Density value.
-  * \param[in] e - Static energy value.
-  * \return Query point lies outside table data range (0 is inside, 1 is outside).
-  */
+   * \brief Evaluate dataset through look-up table.
+   * \param[in] rho - Density value.
+   * \param[in] e - Static energy value.
+   * \return Query point lies outside table data range (0 is inside, 1 is outside).
+   */
   unsigned long Predict_LUT(su2double rho, su2double e);
 
   /*!
-  * \brief Evaluate the data set.
-  * \param[in] rho - Density value.
-  * \param[in] e - Static energy value.
-  */
+   * \brief Evaluate the data set.
+   * \param[in] rho - Density value.
+   * \param[in] e - Static energy value.
+   */
   void Evaluate_Dataset(su2double rho, su2double e);
 
  public:
@@ -156,26 +156,26 @@ class CDataDrivenFluid : public CFluidModel {
   void SetTDState_Ps(su2double P, su2double s) override;
 
   /*!
-  * \brief Set the initial guess for the density in Newton solvers
-  * \param[in] rho - Initial value for density.
-  */
-  void SetDensity(su2double rho) override {rho_start = rho;}
+   * \brief Set the initial guess for the density in Newton solvers
+   * \param[in] rho - Initial value for density.
+   */
+  void SetDensity(su2double rho) override { rho_start = rho; }
 
   /*!
-  * \brief Set the initial guess for the static energy in Newton solvers
-  * \param[in] e - Initial value for static energy.
-  */
-  void SetEnergy(su2double e) override {e_start = e;}
+   * \brief Set the initial guess for the static energy in Newton solvers
+   * \param[in] e - Initial value for static energy.
+   */
+  void SetEnergy(su2double e) override { e_start = e; }
 
   /*!
-  * \brief Get fluid model extrapolation instance
-  * \return Query point lies outside fluid model data range.
-  */
+   * \brief Get fluid model extrapolation instance
+   * \return Query point lies outside fluid model data range.
+   */
   unsigned long GetExtrapolation() override { return outside_dataset; }
 
   /*!
-  * \brief Get number of Newton solver iterations.
-  * \return Newton solver iteration count at termination.
-  */
+   * \brief Get number of Newton solver iterations.
+   * \return Newton solver iteration count at termination.
+   */
   unsigned long GetnIter_Newton() override { return nIter_Newton; }
-};
+};
\ No newline at end of file
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 475550de39c..b7f63ceab59 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -28,22 +28,20 @@
 #include "../../include/fluid/CDataDrivenFluid.hpp"
 
 CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
-
   Kind_DataDriven_Method = config->GetKind_DataDriven_Method();
 
   /*--- Set up interpolation algorithm according to data-driven method. Currently only MLP's are supported. ---*/
-  switch (Kind_DataDriven_Method)
-  {
-  case ENUM_DATADRIVEN_METHOD::MLP:
-    lookup_mlp = new MLPToolbox::CLookUp_ANN(config->GetNDataDriven_Files(), config->GetDataDriven_FileNames());
-    break;
-  case ENUM_DATADRIVEN_METHOD::LUT:
-    lookup_table = new CLookUpTable(config->GetDataDriven_Filename(), "Density", "Energy");
-    break;
-  default:
-    break;
+  switch (Kind_DataDriven_Method) {
+    case ENUM_DATADRIVEN_METHOD::MLP:
+      lookup_mlp = new MLPToolbox::CLookUp_ANN(config->GetNDataDriven_Files(), config->GetDataDriven_FileNames());
+      break;
+    case ENUM_DATADRIVEN_METHOD::LUT:
+      lookup_table = new CLookUpTable(config->GetDataDriven_Filename(), "Density", "Energy");
+      break;
+    default:
+      break;
   }
-  
+
   /*--- Relaxation factor for Newton solvers. ---*/
   Newton_Relaxation = config->GetRelaxation_DataDriven();
 
@@ -52,27 +50,23 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
 
   /*--- Set initial values for density and energy based on config options ---*/
   rho_start = config->GetDensity_Init_DataDriven();
-  e_start   = config->GetEnergy_Init_DataDriven();
-  
+  e_start = config->GetEnergy_Init_DataDriven();
 }
 
-CDataDrivenFluid::~CDataDrivenFluid(){
-  switch (Kind_DataDriven_Method)
-  {
-  case ENUM_DATADRIVEN_METHOD::MLP:
-    delete iomap_rhoe;
-    delete lookup_mlp;
-    break;
-  case ENUM_DATADRIVEN_METHOD::LUT:
-    delete lookup_table;
-    break;
-  default:
-    break;
+CDataDrivenFluid::~CDataDrivenFluid() {
+  switch (Kind_DataDriven_Method) {
+    case ENUM_DATADRIVEN_METHOD::MLP:
+      delete iomap_rhoe;
+      delete lookup_mlp;
+      break;
+    case ENUM_DATADRIVEN_METHOD::LUT:
+      delete lookup_table;
+      break;
+    default:
+      break;
   }
-  
 }
-void CDataDrivenFluid::MapInputs_to_Outputs(){
-
+void CDataDrivenFluid::MapInputs_to_Outputs() {
   /*--- Inputs of the data-driven method are density and internal energy. ---*/
   input_names_rhoe.resize(2);
   idx_rho = 0;
@@ -80,17 +74,13 @@ void CDataDrivenFluid::MapInputs_to_Outputs(){
   input_names_rhoe[idx_rho] = "Density";
   input_names_rhoe[idx_e] = "Energy";
 
-  /*--- Required outputs for the interpolation method are entropy and its partial derivatives with respect to energy and density ---*/
+  /*--- Required outputs for the interpolation method are entropy and its partial derivatives with respect to energy and
+   * density ---*/
   size_t n_outputs = 6;
-  size_t idx_s = 0, 
-         idx_dsde_rho = 1, 
-         idx_dsdrho_e = 2,
-         idx_d2sde2 = 3,
-         idx_d2sdedrho = 4,
-         idx_d2sdrho2 = 5;
+  size_t idx_s = 0, idx_dsde_rho = 1, idx_dsdrho_e = 2, idx_d2sde2 = 3, idx_d2sdedrho = 4, idx_d2sdrho2 = 5;
 
   outputs_rhoe.resize(n_outputs);
-  output_names_rhoe.resize(n_outputs); 
+  output_names_rhoe.resize(n_outputs);
   output_names_rhoe[idx_s] = "s";
   outputs_rhoe[idx_s] = &Entropy;
   output_names_rhoe[idx_dsde_rho] = "dsde_rho";
@@ -105,7 +95,7 @@ void CDataDrivenFluid::MapInputs_to_Outputs(){
   outputs_rhoe[idx_d2sdrho2] = &d2sdrho2;
 
   /*--- Further preprocessing of input and output variables ---*/
-  if(Kind_DataDriven_Method == ENUM_DATADRIVEN_METHOD::MLP){
+  if (Kind_DataDriven_Method == ENUM_DATADRIVEN_METHOD::MLP) {
     /*--- Map MLP inputs to outputs ---*/
     iomap_rhoe = new MLPToolbox::CIOMap(lookup_mlp, input_names_rhoe, output_names_rhoe);
     MLP_inputs.resize(2);
@@ -122,56 +112,52 @@ void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
 
   /*--- Compute speed of sound ---*/
   auto blue_term = (dsdrho_e * (2 - rho * pow(dsde_rho, -1) * d2sdedrho) + rho * d2sdrho2);
-  auto green_term = (- pow(dsde_rho, -1) * d2sde2 * dsdrho_e + d2sdedrho);
-  
-  SoundSpeed2 = - rho * pow(dsde_rho, -1) * (blue_term - rho * green_term * (dsdrho_e / dsde_rho));
+  auto green_term = (-pow(dsde_rho, -1) * d2sde2 * dsdrho_e + d2sdedrho);
+
+  SoundSpeed2 = -rho * pow(dsde_rho, -1) * (blue_term - rho * green_term * (dsdrho_e / dsde_rho));
 
   /*--- Compute primary flow variables ---*/
   Temperature = 1.0 / dsde_rho;
   Pressure = -pow(rho, 2) * Temperature * dsdrho_e;
   Density = rho;
   StaticEnergy = e;
-  
+
   /*--- Compute secondary flow variables ---*/
-  dTde_rho = -pow(dsde_rho, -2)*d2sde2;
+  dTde_rho = -pow(dsde_rho, -2) * d2sde2;
   dTdrho_e = 0.0;
 
   dPde_rho = -pow(rho, 2) * dTde_rho * dsdrho_e;
-  dPdrho_e = -2*rho*Temperature*dsdrho_e - pow(rho, 2)*Temperature*d2sdrho2;
+  dPdrho_e = -2 * rho * Temperature * dsdrho_e - pow(rho, 2) * Temperature * d2sdrho2;
 }
 
 void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
-
   /*--- Setting initial values for density and energy ---*/
-  su2double rho = rho_start, 
-            e = e_start;
+  su2double rho = rho_start, e = e_start;
 
-  su2double tolerance_P = 0.1, // Tolerance percentage for pressure solution
-            tolerance_T = 0.1;  // Tolerance percentage for temperature solution
+  su2double tolerance_P = 0.1,  // Tolerance percentage for pressure solution
+      tolerance_T = 0.1;        // Tolerance percentage for temperature solution
 
-  bool converged = false;         // Convergence flag
+  bool converged = false;        // Convergence flag
   unsigned long iter_max = 500,  // Maximum number of iterations
-                Iter = 0;       
+      Iter = 0;
 
-  su2double delta_P,      // Pressure residual
-            delta_T,      // Temperature residual
-            delta_rho,    // Density step size
-            delta_e,      // Energy step size
-            determinant;  // Jacobian determinant
+  su2double delta_P,  // Pressure residual
+      delta_T,        // Temperature residual
+      delta_rho,      // Density step size
+      delta_e,        // Energy step size
+      determinant;    // Jacobian determinant
   /*--- Initiating Newton solver ---*/
-  while(!converged && (Iter < iter_max)){
-
+  while (!converged && (Iter < iter_max)) {
     /*--- Determine thermodynamic state based on current density and energy*/
-    SetTDState_rhoe(rho ,e);
+    SetTDState_rhoe(rho, e);
 
     /*--- Determine pressure and temperature residuals ---*/
     delta_P = Pressure - P;
     delta_T = Temperature - T;
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if((100*abs(delta_P)/P < tolerance_P) && (100*abs(delta_T)/T < tolerance_T)){
+    if ((100 * abs(delta_P) / P < tolerance_P) && (100 * abs(delta_T) / T < tolerance_T)) {
       converged = true;
-    }else{
-      
+    } else {
       /*--- Compute step size for density and energy ---*/
       determinant = dPdrho_e * dTde_rho - dPde_rho * dTdrho_e;
 
@@ -181,9 +167,8 @@ void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
       /*--- Update density and energy values ---*/
       rho -= Newton_Relaxation * delta_rho;
       e -= Newton_Relaxation * delta_e;
-      
     }
-    Iter ++;
+    Iter++;
   }
 
   /*--- Calculate thermodynamic state based on converged values for density and energy ---*/
@@ -200,39 +185,38 @@ void CDataDrivenFluid::SetTDState_Prho(su2double P, su2double rho) {
   SetTDState_rhoe(rho, StaticEnergy);
 }
 
-void CDataDrivenFluid::SetEnergy_Prho(su2double P, su2double rho) { 
+void CDataDrivenFluid::SetEnergy_Prho(su2double P, su2double rho) {
   /*--- Setting initial values for energy ---*/
   su2double e = e_start;
 
-  su2double tolerance_P = 0.1; // Tolerance percentage for pressure solution
+  su2double tolerance_P = 0.1;  // Tolerance percentage for pressure solution
 
-  bool converged = false;         // Convergence flag
+  bool converged = false;        // Convergence flag
   unsigned long iter_max = 500,  // Maximum number of iterations
-                Iter = 0;       
-
-  su2double delta_P,      // Pressure residual
-            delta_e;      // Energy step size
+      Iter = 0;
 
-  while(!converged && (Iter < iter_max)){
+  su2double delta_P,  // Pressure residual
+      delta_e;        // Energy step size
 
+  while (!converged && (Iter < iter_max)) {
     /*--- Determine thermodynamic state based on current density and energy*/
-    SetTDState_rhoe(rho ,e);
+    SetTDState_rhoe(rho, e);
 
     /*--- Determine pressure and temperature residuals ---*/
     delta_P = Pressure - P;
 
-    su2double partial_diff = abs(delta_P)/P;
+    su2double partial_diff = abs(delta_P) / P;
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if((100*partial_diff < tolerance_P)){
+    if ((100 * partial_diff < tolerance_P)) {
       converged = true;
-    }else{
+    } else {
       /*--- Compute step size for energy ---*/
       delta_e = delta_P / dPde_rho;
 
       /*--- energy value ---*/
       e -= Newton_Relaxation * delta_e;
     }
-    Iter ++;
+    Iter++;
   }
 
   /*--- Setting static energy as the converged value ---*/
@@ -242,40 +226,36 @@ void CDataDrivenFluid::SetEnergy_Prho(su2double P, su2double rho) {
 }
 
 void CDataDrivenFluid::SetTDState_rhoT(su2double rho, su2double T) {
-
   /*--- Setting initial values for density and energy ---*/
   su2double e = e_start;
 
   su2double tolerance_T = 0.1;  // Tolerance for temperature solution
 
-  bool converged = false;         // Convergence flag
+  bool converged = false;        // Convergence flag
   unsigned long iter_max = 500,  // Maximum number of iterations
-                Iter = 0;       
+      Iter = 0;
 
-  su2double delta_T,      // Temperature residual
-            delta_e;  // Energy increment
+  su2double delta_T,  // Temperature residual
+      delta_e;        // Energy increment
 
   /*--- Initiating Newton solver ---*/
-  while(!converged && (Iter < iter_max)){
-
+  while (!converged && (Iter < iter_max)) {
     /*--- Determine thermodynamic state based on current density and energy*/
-    SetTDState_rhoe(rho ,e);
+    SetTDState_rhoe(rho, e);
 
     /*--- Determine temperature residual ---*/
     delta_T = Temperature - T;
 
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if(100*abs(delta_T)/T < tolerance_T){
+    if (100 * abs(delta_T) / T < tolerance_T) {
       converged = true;
-    }else{
-      
-
+    } else {
       delta_e = delta_T / dTde_rho;
 
       /*--- Update energy value ---*/
       e -= Newton_Relaxation * delta_e;
     }
-    Iter ++;
+    Iter++;
   }
 
   /*--- Calculate thermodynamic state based on converged values for density and energy ---*/
@@ -285,29 +265,26 @@ void CDataDrivenFluid::SetTDState_rhoT(su2double rho, su2double T) {
 }
 
 void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
-
   /*--- Setting initial values for density and energy ---*/
-  su2double rho = rho_start, 
-            e = e_start;
+  su2double rho = rho_start, e = e_start;
 
-  su2double tolerance_h = 0.1, // Tolerance for enthalpy solution
-            tolerance_s = 0.1;  // Tolerance for entropy solution
+  su2double tolerance_h = 0.1,  // Tolerance for enthalpy solution
+      tolerance_s = 0.1;        // Tolerance for entropy solution
 
-  bool converged = false;         // Convergence flag
+  bool converged = false;        // Convergence flag
   unsigned long iter_max = 500,  // Maximum number of iterations
-                Iter = 0;       
+      Iter = 0;
 
-  su2double delta_h,      // Enthalpy
-            delta_s,      // Entropy residual
-            delta_rho,    // Density step size
-            delta_e,      // Energy step size
-            determinant;  // Jacobian determinant
+  su2double delta_h,  // Enthalpy
+      delta_s,        // Entropy residual
+      delta_rho,      // Density step size
+      delta_e,        // Energy step size
+      determinant;    // Jacobian determinant
 
   /*--- Initiating Newton solver ---*/
-  while(!converged && (Iter < iter_max)){
-
+  while (!converged && (Iter < iter_max)) {
     /*--- Determine thermodynamic state based on current density and energy*/
-    SetTDState_rhoe(rho ,e);
+    SetTDState_rhoe(rho, e);
 
     su2double Enthalpy = e + Pressure / rho;
     /*--- Determine pressure and temperature residuals ---*/
@@ -315,12 +292,11 @@ void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
     delta_s = Entropy - s;
 
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if((100*abs(delta_h)/h < tolerance_h) && (100*abs(delta_s)/s < tolerance_s)){
+    if ((100 * abs(delta_h) / h < tolerance_h) && (100 * abs(delta_s) / s < tolerance_s)) {
       converged = true;
-    }else{
-      
+    } else {
       su2double dh_de = 1 + dPde_rho / rho;
-      su2double dh_drho = -Pressure*pow(rho, -2) + dPdrho_e / rho;
+      su2double dh_drho = -Pressure * pow(rho, -2) + dPdrho_e / rho;
 
       determinant = dh_drho * dsde_rho - dh_de * dsdrho_e;
       delta_rho = (dsde_rho * delta_h - dh_de * delta_s) / determinant;
@@ -330,7 +306,7 @@ void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
       rho -= Newton_Relaxation * delta_rho;
       e -= Newton_Relaxation * delta_e;
     }
-    Iter ++;
+    Iter++;
   }
   /*--- Calculate thermodynamic state based on converged values for density and energy ---*/
   SetTDState_rhoe(rho, e);
@@ -339,40 +315,36 @@ void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
 }
 
 void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
-  
   /*--- Setting initial values for density and energy ---*/
-  su2double rho = rho_start, 
-            e = e_start;
+  su2double rho = rho_start, e = e_start;
 
-  su2double tolerance_P = 0.1, // Tolerance for pressure solution
-            tolerance_s = 0.1;  // Tolerance for entropy solution
+  su2double tolerance_P = 0.1,  // Tolerance for pressure solution
+      tolerance_s = 0.1;        // Tolerance for entropy solution
 
-  bool converged = false;         // Convergence flag
+  bool converged = false;        // Convergence flag
   unsigned long iter_max = 500,  // Maximum number of iterations
-                Iter = 0;       
+      Iter = 0;
 
-  su2double delta_P,      // Enthalpy
-            delta_s,      // Entropy residual
-            delta_rho,    // Density step size
-            delta_e,      // Energy step size
-            determinant;  // Jacobian determinant
+  su2double delta_P,  // Enthalpy
+      delta_s,        // Entropy residual
+      delta_rho,      // Density step size
+      delta_e,        // Energy step size
+      determinant;    // Jacobian determinant
 
   /*--- Initiating Newton solver ---*/
-  while(!converged && (Iter < iter_max)){
-
+  while (!converged && (Iter < iter_max)) {
     /*--- Determine thermodynamic state based on current density and energy*/
-    SetTDState_rhoe(rho ,e);
+    SetTDState_rhoe(rho, e);
 
     /*--- Determine pressure and temperature residuals ---*/
     delta_P = Pressure - P;
     delta_s = Entropy - s;
 
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if((100*abs(delta_P)/P < tolerance_P) && (100*abs(delta_s)/s < tolerance_s)){
+    if ((100 * abs(delta_P) / P < tolerance_P) && (100 * abs(delta_s) / s < tolerance_s)) {
       converged = true;
-    }else{
-
-       /*--- Compute step size for density and energy ---*/
+    } else {
+      /*--- Compute step size for density and energy ---*/
       determinant = dPdrho_e * dsde_rho - dPde_rho * dsdrho_e;
 
       delta_rho = (dsde_rho * delta_P - dPde_rho * delta_s) / determinant;
@@ -382,7 +354,7 @@ void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
       rho -= Newton_Relaxation * delta_rho;
       e -= Newton_Relaxation * delta_e;
     }
-    Iter ++;
+    Iter++;
   }
 
   /*--- Calculate thermodynamic state based on converged values for density and energy ---*/
@@ -398,7 +370,7 @@ unsigned long CDataDrivenFluid::Predict_MLP(su2double rho, su2double e) {
   /* Evaluate MLP collection for the given values for density and energy */
   unsigned long exit_code = lookup_mlp->Predict_ANN(iomap_rhoe, MLP_inputs, outputs_rhoe);
 
-  /* Apply exponential transformation to the MLP outputs for the first and second 
+  /* Apply exponential transformation to the MLP outputs for the first and second
      derivative of the entropy w.r.t density */
   dsdrho_e = -exp(dsdrho_e);
   d2sdrho2 = exp(d2sdrho2);
@@ -411,15 +383,13 @@ unsigned long CDataDrivenFluid::Predict_LUT(su2double rho, su2double e) {
   std::vector<std::string> output_names_rhoe_LUT;
   std::vector<su2double*> outputs_LUT;
   output_names_rhoe_LUT.resize(output_names_rhoe.size());
-  for(auto iOutput=0u; iOutput<output_names_rhoe.size(); iOutput++) 
-  { 
-    output_names_rhoe_LUT[iOutput] = output_names_rhoe[iOutput]; 
+  for (auto iOutput = 0u; iOutput < output_names_rhoe.size(); iOutput++) {
+    output_names_rhoe_LUT[iOutput] = output_names_rhoe[iOutput];
   }
 
   outputs_LUT.resize(outputs_rhoe.size());
-  for(auto iOutput=0u; iOutput<outputs_rhoe.size(); iOutput++) 
-  { 
-    outputs_LUT[iOutput] = outputs_rhoe[iOutput]; 
+  for (auto iOutput = 0u; iOutput < outputs_rhoe.size(); iOutput++) {
+    outputs_LUT[iOutput] = outputs_rhoe[iOutput];
   }
 
   exit_code = lookup_table->LookUp_ProgEnth(output_names_rhoe_LUT, outputs_LUT, rho, e, "Density", "Energy");
@@ -428,15 +398,14 @@ unsigned long CDataDrivenFluid::Predict_LUT(su2double rho, su2double e) {
 
 void CDataDrivenFluid::Evaluate_Dataset(su2double rho, su2double e) {
   /*--- Evaluate dataset based on regression method ---*/
-  switch (Kind_DataDriven_Method)
-  {
-  case ENUM_DATADRIVEN_METHOD::LUT:
-    outside_dataset = Predict_LUT(rho, e);
-    break;
-  case ENUM_DATADRIVEN_METHOD::MLP:
-    outside_dataset = Predict_MLP(rho, e);
-    break;
-  default:
-    break;
+  switch (Kind_DataDriven_Method) {
+    case ENUM_DATADRIVEN_METHOD::LUT:
+      outside_dataset = Predict_LUT(rho, e);
+      break;
+    case ENUM_DATADRIVEN_METHOD::MLP:
+      outside_dataset = Predict_MLP(rho, e);
+      break;
+    default:
+      break;
   }
 }
\ No newline at end of file

From ae130fab7f4122722dfcf57d857f578363d44e78 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 3 Jan 2023 16:48:33 +0100
Subject: [PATCH 111/656] added clang formatting to multilayer-perceptron files

---
 .github/workflows/regression.yml | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 003525f926c..af744ec202b 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c feature_multilayer_perceptron -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
         with:

From 027e23be1ad51697db4d6c49fcc6b6a32cb0ccb9 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 3 Jan 2023 16:50:02 +0100
Subject: [PATCH 112/656] added clang formatting to multilayer-perceptron files

---
 .github/workflows/regression.yml | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index af744ec202b..e749e661e70 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
         with:

From c69ed9249a416606023ecbe7a84191678196292c Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Wed, 4 Jan 2023 13:24:58 -0800
Subject: [PATCH 113/656] Modify regression workflow

---
 .github/workflows/regression.yml | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index b622d6c88af..e749e661e70 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c feature_FFD -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
         with:

From abe96dec521d9bbef68be8cfc7c2cc82a870bfd1 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Tue, 10 Jan 2023 15:00:57 -0800
Subject: [PATCH 114/656] Fix memory deallocation error in CDeformationDriver

---
 SU2_CFD/src/drivers/CDriverBase.cpp        |  1 -
 SU2_DEF/src/drivers/CDeformationDriver.cpp | 46 +++++++++++-----------
 2 files changed, 22 insertions(+), 25 deletions(-)

diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index 726dabe44f9..fd7b2948301 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -65,7 +65,6 @@ void CDriverBase::SetContainers_Null() {
 
   for (iZone = 0; iZone < nZone; iZone++) {
     nInst[iZone] = 1;
-    FFDBox[iZone] = new CFreeFormDefBox*[MAX_NUMBER_FFD];
   }
 
   driver_config = nullptr;
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 99ed2dab30a..712cd8e194d 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -524,32 +524,32 @@ void CDeformationDriver::Postprocessing() {
   if (rank == MASTER_NODE)
     cout << endl << "------------------------- Solver Postprocessing -------------------------" << endl;
 
-  if (driver_config != nullptr) delete[] driver_config;
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    if (numerics_container[iZone] != nullptr) {
-      for (unsigned int iTerm = 0; iTerm < MAX_TERMS * omp_get_max_threads(); iTerm++) {
-        delete numerics_container[iZone][INST_0][MESH_0][MESH_SOL][iTerm];
-        delete[] numerics_container[iZone][INST_0][MESH_0][MESH_SOL];
-        delete[] numerics_container[iZone][INST_0][MESH_0];
-        delete[] numerics_container[iZone][INST_0];
+  if (driver_config->GetDeform_Mesh()) {
+    for (iZone = 0; iZone < nZone; iZone++) {
+      if (numerics_container[iZone] != nullptr) {
+        for (unsigned int iTerm = 0; iTerm < MAX_TERMS * omp_get_max_threads(); iTerm++) {
+          delete numerics_container[iZone][INST_0][MESH_0][MESH_SOL][iTerm];
+          delete[] numerics_container[iZone][INST_0][MESH_0][MESH_SOL];
+          delete[] numerics_container[iZone][INST_0][MESH_0];
+          delete[] numerics_container[iZone][INST_0];
+        }
+        delete[] numerics_container[iZone];
       }
-      delete[] numerics_container[iZone];
     }
-  }
-  delete[] numerics_container;
-  if (rank == MASTER_NODE) cout << "Deleted CNumerics container." << endl;
+    delete[] numerics_container;
+    if (rank == MASTER_NODE) cout << "Deleted CNumerics container." << endl;
 
-  for (iZone = 0; iZone < nZone; iZone++) {
-    if (solver_container[iZone] != nullptr) {
-      delete solver_container[iZone][INST_0][MESH_0][MESH_SOL];
-      delete[] solver_container[iZone][INST_0][MESH_0];
-      delete[] solver_container[iZone][INST_0];
-      delete[] solver_container[iZone];
+    for (iZone = 0; iZone < nZone; iZone++) {
+      if (solver_container[iZone] != nullptr) {
+        delete solver_container[iZone][INST_0][MESH_0][MESH_SOL];
+        delete[] solver_container[iZone][INST_0][MESH_0];
+        delete[] solver_container[iZone][INST_0];
+        delete[] solver_container[iZone];
+      }
     }
+    delete[] solver_container;
+    if (rank == MASTER_NODE) cout << "Deleted CSolver container." << endl;
   }
-  delete[] solver_container;
-  if (rank == MASTER_NODE) cout << "Deleted CSolver container." << endl;
 
   if (geometry_container != nullptr) {
     for (iZone = 0; iZone < nZone; iZone++) {
@@ -561,9 +561,6 @@ void CDeformationDriver::Postprocessing() {
   }
   if (rank == MASTER_NODE) cout << "Deleted CGeometry container." << endl;
 
-  for (iZone = 0; iZone < nZone; iZone++) {
-    delete[] FFDBox[iZone];
-  }
   delete[] FFDBox;
   if (rank == MASTER_NODE) cout << "Deleted CFreeFormDefBox class." << endl;
 
@@ -590,6 +587,7 @@ void CDeformationDriver::Postprocessing() {
     }
     delete[] config_container;
   }
+  delete driver_config;
   if (rank == MASTER_NODE) cout << "Deleted CConfig container." << endl;
 
   if (output_container != nullptr) {

From 47b1966ca1e62a88294665dc1223538f42468e79 Mon Sep 17 00:00:00 2001
From: patelha57 <patelha57@gmail.com>
Date: Tue, 10 Jan 2023 17:17:38 -0800
Subject: [PATCH 115/656] Fix continuous adjoint solver errors in
 CDiscAdjDeformationDriver

---
 .../src/drivers/CDiscAdjDeformationDriver.cpp | 52 ++++++++++++-------
 1 file changed, 32 insertions(+), 20 deletions(-)

diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index 362c237e56a..d65f150d2a9 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -289,38 +289,50 @@ void CDiscAdjDeformationDriver::Output_Preprocessing() {}
 
 void CDiscAdjDeformationDriver::Preprocess() {
   for (iZone = 0; iZone < nZone; iZone++) {
-    if (rank == MASTER_NODE) cout << "Reading volume sensitivities at each node from file." << endl;
-    unsigned short nInst_Zone = nInst[iZone];
+    if (!config_container[iZone]->GetDiscrete_Adjoint()) {
+      if (rank == MASTER_NODE) cout << "Reading surface sensitivities at each node from file." << endl;
+      geometry_container[iZone][INST_0][MESH_0]->SetBoundSensitivity(config_container[iZone]);
 
-    grid_movement[iZone] = new CVolumetricMovement*[nInst_Zone]();
-    grid_movement[iZone][INST_0] = new CVolumetricMovement(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
+    } else {
+      if (rank == MASTER_NODE) cout << "Reading volume sensitivities at each node from file." << endl;
+      unsigned short nInst_Zone = nInst[iZone];
+
+      grid_movement[iZone] = new CVolumetricMovement*[nInst_Zone]();
+      grid_movement[iZone][INST_0] = new CVolumetricMovement(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
 
-    /*--- Read in sensitivities from file. ---*/
+      /*--- Read in sensitivities from file. ---*/
 
-    if (config_container[ZONE_0]->GetSensitivity_Format() == UNORDERED_ASCII)
-      geometry_container[iZone][INST_0][MESH_0]->ReadUnorderedSensitivity(config_container[iZone]);
-    else
-      geometry_container[iZone][INST_0][MESH_0]->SetSensitivity(config_container[iZone]);
+      if (config_container[ZONE_0]->GetSensitivity_Format() == UNORDERED_ASCII)
+        geometry_container[iZone][INST_0][MESH_0]->ReadUnorderedSensitivity(config_container[iZone]);
+      else
+        geometry_container[iZone][INST_0][MESH_0]->SetSensitivity(config_container[iZone]);
+    }
   }
 }
 
 void CDiscAdjDeformationDriver::Run() {
   for (iZone = 0; iZone < nZone; iZone++) {
-    if (rank == MASTER_NODE)
-      cout << "\n---------------------- Mesh sensitivity computation ---------------------" << endl;
-    if (config_container[iZone]->GetDiscrete_Adjoint() && config_container[iZone]->GetSmoothGradient() &&
-        config_container[iZone]->GetSobMode() == ENUM_SOBOLEV_MODUS::MESH_LEVEL) {
-      DerivativeTreatment_MeshSensitivity(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], grid_movement[iZone][INST_0]);
+    if (!config_container[iZone]->GetDiscrete_Adjoint()) {
+      continue;
     } else {
-      grid_movement[iZone][INST_0]->SetVolume_Deformation(geometry_container[iZone][INST_0][MESH_0],
-                                                          config_container[iZone], false, true);
+      if (rank == MASTER_NODE)
+        cout << "\n---------------------- Mesh sensitivity computation ---------------------" << endl;
+      if (config_container[iZone]->GetDiscrete_Adjoint() && config_container[iZone]->GetSmoothGradient() &&
+          config_container[iZone]->GetSobMode() == ENUM_SOBOLEV_MODUS::MESH_LEVEL) {
+        DerivativeTreatment_MeshSensitivity(geometry_container[iZone][INST_0][MESH_0], config_container[iZone],
+                                            grid_movement[iZone][INST_0]);
+      } else {
+        grid_movement[iZone][INST_0]->SetVolume_Deformation(geometry_container[iZone][INST_0][MESH_0],
+                                                            config_container[iZone], false, true);
+      }
     }
   }
 
-  if (rank == MASTER_NODE)
-    cout << "\n------------------------ Mesh sensitivity Output ------------------------" << endl;
-
-  SetSensitivity_Files(geometry_container, config_container, nZone);
+  if (config_container[ZONE_0]->GetDiscrete_Adjoint()) {
+    if (rank == MASTER_NODE)
+      cout << "\n------------------------ Mesh sensitivity Output ------------------------" << endl;
+    SetSensitivity_Files(geometry_container, config_container, nZone);
+  }
 
   Gradient_file.precision(driver_config->OptionIsSet("OUTPUT_PRECISION") ? driver_config->GetOutput_Precision() : 6);
 

From 3ebd12b9d5e5e479d05232278a33ce6e0b2ea9f5 Mon Sep 17 00:00:00 2001
From: Harsh Patel <51417692+patelha57@users.noreply.github.com>
Date: Wed, 11 Jan 2023 11:35:17 -0800
Subject: [PATCH 116/656] Update CDriver.hpp

Co-authored-by: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
---
 SU2_CFD/include/drivers/CDriver.hpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index c6fbde07c5a..a2755337263 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -1,5 +1,5 @@
 /*!
- * \file driver_structure.hpp
+ * \file CDriver.hpp
  * \brief Headers of the main subroutines for driving single or multi-zone problems.
  *        The subroutines and functions are in the <i>driver_structure.cpp</i> file.
  * \author T. Economon, H. Kline, R. Sanchez

From 2f8bd4df30492059578c1767d7dc094fe291062b Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Thu, 12 Jan 2023 20:25:58 -0500
Subject: [PATCH 117/656] update to develop

---
 .github/release.yml                           |  20 +
 .github/workflows/regression.yml              |  40 +-
 .github/workflows/release-management.yml      |   2 +-
 AUTHORS.md                                    |   3 +
 Common/include/CConfig.hpp                    |  57 +-
 Common/include/adt/CADTBaseClass.hpp          |   2 +-
 Common/include/adt/CADTComparePointClass.hpp  |   2 +-
 Common/include/adt/CADTElemClass.hpp          |   4 +-
 Common/include/adt/CADTNodeClass.hpp          |   2 +-
 Common/include/adt/CADTPointsOnlyClass.hpp    |   2 +-
 Common/include/adt/CBBoxTargetClass.hpp       |   4 +-
 Common/include/basic_types/ad_structure.hpp   |   2 +-
 .../basic_types/datatype_structure.hpp        |   2 +-
 Common/include/code_config.hpp                |   2 +-
 Common/include/containers/C2DContainer.hpp    |   2 +-
 .../containers/CFastFindAndEraseQueue.hpp     |   2 +-
 Common/include/containers/CFileReaderLUT.hpp  |   2 +-
 Common/include/containers/CLookUpTable.hpp    |   2 +-
 Common/include/containers/CTrapezoidalMap.hpp |   4 +-
 Common/include/containers/CVertexMap.hpp      |   2 +-
 .../containers/container_decorators.hpp       |   2 +-
 Common/include/fem/fem_cgns_elements.hpp      |   2 +-
 .../fem/fem_gauss_jacobi_quadrature.hpp       |   4 +-
 Common/include/fem/fem_geometry_structure.hpp |  24 +-
 Common/include/fem/fem_standard_element.hpp   |  10 +-
 .../fem/geometry_structure_fem_part.hpp       |   2 +-
 Common/include/geometry/CDummyGeometry.hpp    |   2 +-
 Common/include/geometry/CGeometry.hpp         |  35 +-
 .../include/geometry/CMultiGridGeometry.hpp   |   2 +-
 Common/include/geometry/CMultiGridQueue.hpp   |   2 +-
 Common/include/geometry/CPhysicalGeometry.hpp |   2 +-
 .../include/geometry/dual_grid/CDualGrid.hpp  |   2 +-
 Common/include/geometry/dual_grid/CEdge.hpp   |   2 +-
 Common/include/geometry/dual_grid/CPoint.hpp  |   2 +-
 .../geometry/dual_grid/CTurboVertex.hpp       |   2 +-
 Common/include/geometry/dual_grid/CVertex.hpp |   2 +-
 Common/include/geometry/elements/CElement.hpp |   4 +-
 .../geometry/elements/CElementProperty.hpp    |   6 +-
 .../geometry/elements/CGaussVariable.hpp      |   4 +-
 .../geometry/meshreader/CBoxMeshReaderFVM.hpp |   2 +-
 .../meshreader/CCGNSMeshReaderFVM.hpp         |   2 +-
 .../geometry/meshreader/CMeshReaderFVM.hpp    |   2 +-
 .../meshreader/CRectangularMeshReaderFVM.hpp  |   2 +-
 .../meshreader/CSU2ASCIIMeshReaderFVM.hpp     |   2 +-
 .../geometry/primal_grid/CHexahedron.hpp      |   2 +-
 Common/include/geometry/primal_grid/CLine.hpp |   2 +-
 .../geometry/primal_grid/CPrimalGrid.hpp      |   2 +-
 .../primal_grid/CPrimalGridBoundFEM.hpp       |   4 +-
 .../geometry/primal_grid/CPrimalGridFEM.hpp   |   4 +-
 .../include/geometry/primal_grid/CPrism.hpp   |   2 +-
 .../include/geometry/primal_grid/CPyramid.hpp |   2 +-
 .../geometry/primal_grid/CQuadrilateral.hpp   |   2 +-
 .../geometry/primal_grid/CTetrahedron.hpp     |   2 +-
 .../geometry/primal_grid/CTriangle.hpp        |   2 +-
 .../geometry/primal_grid/CVertexMPI.hpp       |   2 +-
 Common/include/graph_coloring_structure.hpp   |   4 +-
 .../grid_movement/CBSplineBlending.hpp        |   2 +-
 .../include/grid_movement/CBezierBlending.hpp |   2 +-
 .../grid_movement/CFreeFormBlending.hpp       |   2 +-
 .../include/grid_movement/CFreeFormDefBox.hpp |   2 +-
 .../include/grid_movement/CGridMovement.hpp   |   2 +-
 .../grid_movement/CSurfaceMovement.hpp        |   2 +-
 .../grid_movement/CVolumetricMovement.hpp     |   2 +-
 .../interface_interpolation/CInterpolator.hpp |   2 +-
 .../CInterpolatorFactory.hpp                  |   2 +-
 .../CIsoparametric.hpp                        |   2 +-
 .../interface_interpolation/CMirror.hpp       |   2 +-
 .../CNearestNeighbor.hpp                      |   2 +-
 .../CRadialBasisFunction.hpp                  |   2 +-
 .../interface_interpolation/CSlidingMesh.hpp  |   2 +-
 .../linear_algebra/CMatrixVectorProduct.hpp   |   2 +-
 .../include/linear_algebra/CPastixWrapper.hpp |   2 +-
 .../linear_algebra/CPreconditioner.hpp        |   4 +-
 Common/include/linear_algebra/CSysMatrix.hpp  |   9 +-
 Common/include/linear_algebra/CSysMatrix.inl  |   5 +-
 Common/include/linear_algebra/CSysSolve.hpp   |   2 +-
 Common/include/linear_algebra/CSysSolve_b.hpp |   2 +-
 Common/include/linear_algebra/CSysVector.hpp  |   2 +-
 .../include/linear_algebra/blas_structure.hpp |   4 +-
 .../linear_algebra/vector_expressions.hpp     |   2 +-
 Common/include/option_structure.hpp           | 131 ++-
 Common/include/option_structure.inl           |   2 +-
 .../include/parallelization/mpi_structure.cpp |   2 +-
 .../include/parallelization/mpi_structure.hpp |   2 +-
 .../include/parallelization/omp_structure.cpp |   2 +-
 .../include/parallelization/omp_structure.hpp |   2 +-
 .../parallelization/special_vectorization.hpp |   2 +-
 .../include/parallelization/vectorization.hpp |   2 +-
 Common/include/toolboxes/C1DInterpolation.hpp |   2 +-
 .../include/toolboxes/CLinearPartitioner.hpp  |   2 +-
 .../toolboxes/CQuasiNewtonInvLeastSquares.hpp |   2 +-
 Common/include/toolboxes/CSquareMatrixCM.hpp  |   2 +-
 Common/include/toolboxes/CSymmetricMatrix.hpp |   2 +-
 .../include/toolboxes/MMS/CIncTGVSolution.hpp |   2 +-
 .../toolboxes/MMS/CInviscidVortexSolution.hpp |   2 +-
 .../toolboxes/MMS/CMMSIncEulerSolution.hpp    |   2 +-
 .../toolboxes/MMS/CMMSIncNSSolution.hpp       |   2 +-
 .../MMS/CMMSNSTwoHalfCirclesSolution.hpp      |   2 +-
 .../MMS/CMMSNSTwoHalfSpheresSolution.hpp      |   2 +-
 .../toolboxes/MMS/CMMSNSUnitQuadSolution.hpp  |   2 +-
 .../MMS/CMMSNSUnitQuadSolutionWallBC.hpp      |   2 +-
 .../toolboxes/MMS/CNSUnitQuadSolution.hpp     |   2 +-
 .../toolboxes/MMS/CRinglebSolution.hpp        |   2 +-
 Common/include/toolboxes/MMS/CTGVSolution.hpp |   2 +-
 .../toolboxes/MMS/CUserDefinedSolution.hpp    |   2 +-
 .../toolboxes/MMS/CVerificationSolution.hpp   |   2 +-
 .../include/toolboxes/allocation_toolbox.hpp  |   2 +-
 Common/include/toolboxes/geometry_toolbox.hpp |   2 +-
 Common/include/toolboxes/graph_toolbox.hpp    |   4 +-
 Common/include/toolboxes/ndflattener.hpp      |   2 +-
 Common/include/toolboxes/printing_toolbox.hpp |   2 +-
 Common/include/wall_model.hpp                 |   4 +-
 Common/lib/Makefile.am                        |   2 +-
 Common/src/CConfig.cpp                        |  81 +-
 Common/src/adt/CADTBaseClass.cpp              |   2 +-
 Common/src/adt/CADTElemClass.cpp              |   2 +-
 Common/src/adt/CADTPointsOnlyClass.cpp        |   2 +-
 Common/src/basic_types/ad_structure.cpp       |   2 +-
 Common/src/containers/CFileReaderLUT.cpp      |   2 +-
 Common/src/containers/CLookUpTable.cpp        |   2 +-
 Common/src/containers/CTrapezoidalMap.cpp     |   2 +-
 Common/src/fem/fem_cgns_elements.cpp          |   2 +-
 .../src/fem/fem_gauss_jacobi_quadrature.cpp   |   2 +-
 Common/src/fem/fem_geometry_structure.cpp     |   2 +-
 Common/src/fem/fem_integration_rules.cpp      |   2 +-
 Common/src/fem/fem_standard_element.cpp       |   2 +-
 Common/src/fem/fem_wall_distance.cpp          |   2 +-
 Common/src/fem/fem_work_estimate_metis.cpp    |   2 +-
 .../src/fem/geometry_structure_fem_part.cpp   |   2 +-
 Common/src/geometry/CDummyGeometry.cpp        |   2 +-
 Common/src/geometry/CGeometry.cpp             | 178 +++-
 Common/src/geometry/CMultiGridGeometry.cpp    |   4 +-
 Common/src/geometry/CMultiGridQueue.cpp       |   2 +-
 Common/src/geometry/CPhysicalGeometry.cpp     |   2 +-
 Common/src/geometry/dual_grid/CDualGrid.cpp   |   2 +-
 Common/src/geometry/dual_grid/CEdge.cpp       |   2 +-
 Common/src/geometry/dual_grid/CPoint.cpp      |   2 +-
 .../src/geometry/dual_grid/CTurboVertex.cpp   |   2 +-
 Common/src/geometry/dual_grid/CVertex.cpp     |   2 +-
 Common/src/geometry/elements/CElement.cpp     |   2 +-
 Common/src/geometry/elements/CHEXA8.cpp       |   2 +-
 Common/src/geometry/elements/CLINE.cpp        |   2 +-
 Common/src/geometry/elements/CPRISM6.cpp      |   2 +-
 Common/src/geometry/elements/CPYRAM5.cpp      |   2 +-
 Common/src/geometry/elements/CPYRAM6.cpp      |   2 +-
 Common/src/geometry/elements/CQUAD4.cpp       |   2 +-
 Common/src/geometry/elements/CTETRA1.cpp      |   2 +-
 Common/src/geometry/elements/CTETRA4.cpp      |   2 +-
 Common/src/geometry/elements/CTRIA1.cpp       |   2 +-
 Common/src/geometry/elements/CTRIA3.cpp       |   2 +-
 .../geometry/meshreader/CBoxMeshReaderFVM.cpp |   2 +-
 .../meshreader/CCGNSMeshReaderFVM.cpp         |   2 +-
 .../geometry/meshreader/CMeshReaderFVM.cpp    |   2 +-
 .../meshreader/CRectangularMeshReaderFVM.cpp  |   2 +-
 .../meshreader/CSU2ASCIIMeshReaderFVM.cpp     |   2 +-
 .../src/geometry/primal_grid/CHexahedron.cpp  |   2 +-
 Common/src/geometry/primal_grid/CLine.cpp     |   2 +-
 .../src/geometry/primal_grid/CPrimalGrid.cpp  |   2 +-
 .../primal_grid/CPrimalGridBoundFEM.cpp       |   2 +-
 .../geometry/primal_grid/CPrimalGridFEM.cpp   |   2 +-
 Common/src/geometry/primal_grid/CPrism.cpp    |   2 +-
 Common/src/geometry/primal_grid/CPyramid.cpp  |   2 +-
 .../geometry/primal_grid/CQuadrilateral.cpp   |   2 +-
 .../src/geometry/primal_grid/CTetrahedron.cpp |   2 +-
 Common/src/geometry/primal_grid/CTriangle.cpp |   2 +-
 .../src/geometry/primal_grid/CVertexMPI.cpp   |   2 +-
 Common/src/graph_coloring_structure.cpp       |   2 +-
 Common/src/grid_movement/CBSplineBlending.cpp |   2 +-
 Common/src/grid_movement/CBezierBlending.cpp  |   2 +-
 .../src/grid_movement/CFreeFormBlending.cpp   |   2 +-
 Common/src/grid_movement/CFreeFormDefBox.cpp  |   2 +-
 Common/src/grid_movement/CGridMovement.cpp    |   2 +-
 Common/src/grid_movement/CSurfaceMovement.cpp |   2 +-
 .../src/grid_movement/CVolumetricMovement.cpp |   2 +-
 .../interface_interpolation/CInterpolator.cpp |   2 +-
 .../CInterpolatorFactory.cpp                  |   2 +-
 .../CIsoparametric.cpp                        |   2 +-
 .../src/interface_interpolation/CMirror.cpp   |   2 +-
 .../CNearestNeighbor.cpp                      |   2 +-
 .../CRadialBasisFunction.cpp                  |   2 +-
 .../interface_interpolation/CSlidingMesh.cpp  |   2 +-
 Common/src/linear_algebra/CPastixWrapper.cpp  |   2 +-
 Common/src/linear_algebra/CSysMatrix.cpp      | 226 +----
 Common/src/linear_algebra/CSysSolve.cpp       |   2 +-
 Common/src/linear_algebra/CSysSolve_b.cpp     |   2 +-
 Common/src/linear_algebra/CSysVector.cpp      |   2 +-
 Common/src/linear_algebra/blas_structure.cpp  |   2 +-
 Common/src/toolboxes/C1DInterpolation.cpp     |   2 +-
 Common/src/toolboxes/CLinearPartitioner.cpp   |   2 +-
 Common/src/toolboxes/CSquareMatrixCM.cpp      |   2 +-
 Common/src/toolboxes/CSymmetricMatrix.cpp     |   2 +-
 Common/src/toolboxes/MMS/CIncTGVSolution.cpp  |   2 +-
 .../toolboxes/MMS/CInviscidVortexSolution.cpp |   2 +-
 .../toolboxes/MMS/CMMSIncEulerSolution.cpp    |   2 +-
 .../src/toolboxes/MMS/CMMSIncNSSolution.cpp   |   2 +-
 .../MMS/CMMSNSTwoHalfCirclesSolution.cpp      |   2 +-
 .../MMS/CMMSNSTwoHalfSpheresSolution.cpp      |   2 +-
 .../toolboxes/MMS/CMMSNSUnitQuadSolution.cpp  |   2 +-
 .../MMS/CMMSNSUnitQuadSolutionWallBC.cpp      |   2 +-
 .../src/toolboxes/MMS/CNSUnitQuadSolution.cpp |   2 +-
 Common/src/toolboxes/MMS/CRinglebSolution.cpp |   2 +-
 Common/src/toolboxes/MMS/CTGVSolution.cpp     |   2 +-
 .../toolboxes/MMS/CUserDefinedSolution.cpp    |   2 +-
 .../toolboxes/MMS/CVerificationSolution.cpp   |   2 +-
 .../CMMSIncEulerSolution.py                   |   2 +-
 .../CreateMMSSourceTerms/CMMSIncNSSolution.py |   2 +-
 Common/src/toolboxes/printing_toolbox.cpp     |   2 +-
 Common/src/wall_model.cpp                     |   2 +-
 Docs/docmain.hpp                              |   4 +-
 QuickStart/inv_NACA0012.cfg                   |   2 +-
 README.md                                     |   2 +-
 SU2_CFD/include/CMarkerProfileReaderFVM.hpp   |   2 +-
 SU2_CFD/include/SU2_CFD.hpp                   |   2 +-
 SU2_CFD/include/definition_structure.hpp      |   2 +-
 .../drivers/CDiscAdjMultizoneDriver.hpp       |   2 +-
 .../drivers/CDiscAdjSinglezoneDriver.hpp      |   4 +-
 SU2_CFD/include/drivers/CDriver.hpp           |   2 +-
 SU2_CFD/include/drivers/CDummyDriver.hpp      |   2 +-
 SU2_CFD/include/drivers/CMultizoneDriver.hpp  |   4 +-
 SU2_CFD/include/drivers/CSinglezoneDriver.hpp |   4 +-
 SU2_CFD/include/fluid/CConductivityModel.hpp  |   2 +-
 .../include/fluid/CConstantConductivity.hpp   |   2 +-
 .../fluid/CConstantConductivityRANS.hpp       |   2 +-
 SU2_CFD/include/fluid/CConstantDensity.hpp    |   2 +-
 .../include/fluid/CConstantDiffusivity.hpp    |   2 +-
 .../fluid/CConstantLewisDiffusivity.hpp       |   2 +-
 SU2_CFD/include/fluid/CConstantPrandtl.hpp    |   2 +-
 .../include/fluid/CConstantPrandtlRANS.hpp    |   2 +-
 SU2_CFD/include/fluid/CConstantSchmidt.hpp    |   2 +-
 SU2_CFD/include/fluid/CConstantViscosity.hpp  |   2 +-
 SU2_CFD/include/fluid/CCoolProp.hpp           |   2 +-
 .../include/fluid/CCoolPropConductivity.hpp   |   2 +-
 SU2_CFD/include/fluid/CCoolPropViscosity.hpp  |   2 +-
 SU2_CFD/include/fluid/CDiffusivityModel.hpp   |   2 +-
 SU2_CFD/include/fluid/CFluidModel.hpp         |   2 +-
 SU2_CFD/include/fluid/CFluidScalar.hpp        |   2 +-
 SU2_CFD/include/fluid/CIdealGas.hpp           |   2 +-
 SU2_CFD/include/fluid/CIncIdealGas.hpp        |   2 +-
 .../include/fluid/CIncIdealGasPolynomial.hpp  |   2 +-
 SU2_CFD/include/fluid/CMutationTCLib.hpp      |   2 +-
 SU2_CFD/include/fluid/CNEMOGas.hpp            |   2 +-
 SU2_CFD/include/fluid/CPengRobinson.hpp       |   2 +-
 .../include/fluid/CPolynomialConductivity.hpp |   2 +-
 .../fluid/CPolynomialConductivityRANS.hpp     |   2 +-
 .../include/fluid/CPolynomialViscosity.hpp    |   2 +-
 SU2_CFD/include/fluid/CSU2TCLib.hpp           |   2 +-
 SU2_CFD/include/fluid/CSutherland.hpp         |   2 +-
 SU2_CFD/include/fluid/CVanDerWaalsGas.hpp     |   2 +-
 SU2_CFD/include/fluid/CViscosityModel.hpp     |   2 +-
 .../gradients/computeGradientsGreenGauss.hpp  |   2 +-
 .../computeGradientsLeastSquares.hpp          |   2 +-
 .../integration/CFEM_DG_Integration.hpp       |   4 +-
 SU2_CFD/include/integration/CIntegration.hpp  |   2 +-
 .../integration/CIntegrationFactory.hpp       |   2 +-
 .../integration/CMultiGridIntegration.hpp     |   2 +-
 .../integration/CNewtonIntegration.hpp        |   2 +-
 .../integration/CSingleGridIntegration.hpp    |   2 +-
 .../integration/CStructuralIntegration.hpp    |   2 +-
 SU2_CFD/include/interfaces/CInterface.hpp     |   4 +-
 .../cfd/CConservativeVarsInterface.hpp        |   2 +-
 .../interfaces/cfd/CMixingPlaneInterface.hpp  |   2 +-
 .../interfaces/cfd/CSlidingInterface.hpp      |   2 +-
 .../cht/CConjugateHeatInterface.hpp           |   2 +-
 .../fsi/CDiscAdjFlowTractionInterface.hpp     |   2 +-
 .../fsi/CDisplacementsInterface.hpp           |   2 +-
 .../interfaces/fsi/CFlowTractionInterface.hpp |   2 +-
 .../include/iteration/CAdjFluidIteration.hpp  |   2 +-
 .../iteration/CDiscAdjFEAIteration.hpp        |   2 +-
 .../iteration/CDiscAdjFluidIteration.hpp      |   2 +-
 .../iteration/CDiscAdjHeatIteration.hpp       |   2 +-
 SU2_CFD/include/iteration/CFEAIteration.hpp   |   4 +-
 .../include/iteration/CFEMFluidIteration.hpp  |   4 +-
 SU2_CFD/include/iteration/CFluidIteration.hpp |   2 +-
 SU2_CFD/include/iteration/CHeatIteration.hpp  |   2 +-
 SU2_CFD/include/iteration/CIteration.hpp      |   2 +-
 .../include/iteration/CIterationFactory.hpp   |   2 +-
 SU2_CFD/include/iteration/CTurboIteration.hpp |   2 +-
 SU2_CFD/include/limiters/CLimiterDetails.hpp  |   2 +-
 SU2_CFD/include/limiters/computeLimiters.hpp  |   2 +-
 .../include/limiters/computeLimiters_impl.hpp |   2 +-
 SU2_CFD/include/numerics/CGradSmoothing.hpp   |   2 +-
 SU2_CFD/include/numerics/CNumerics.hpp        |  53 +-
 .../include/numerics/NEMO/CNEMONumerics.hpp   |   2 +-
 .../include/numerics/NEMO/NEMO_diffusion.hpp  |   6 +-
 .../include/numerics/NEMO/NEMO_sources.hpp    |   4 +-
 .../include/numerics/NEMO/convection/ausm.hpp |   2 +-
 .../numerics/NEMO/convection/ausmplusup2.hpp  |   2 +-
 .../numerics/NEMO/convection/ausmpwplus.hpp   |   2 +-
 .../include/numerics/NEMO/convection/lax.hpp  |   2 +-
 .../include/numerics/NEMO/convection/msw.hpp  |   4 +-
 .../include/numerics/NEMO/convection/roe.hpp  |   4 +-
 .../continuous_adjoint/adj_convection.hpp     |   2 +-
 .../continuous_adjoint/adj_diffusion.hpp      |   2 +-
 .../continuous_adjoint/adj_sources.hpp        |   2 +-
 .../numerics/elasticity/CFEAElasticity.hpp    |   4 +-
 .../elasticity/CFEALinearElasticity.hpp       |   6 +-
 .../elasticity/CFEANonlinearElasticity.hpp    |   4 +-
 .../numerics/elasticity/nonlinear_models.hpp  |  10 +-
 .../numerics/flow/convection/ausm_slau.hpp    |   2 +-
 .../numerics/flow/convection/centered.hpp     |   2 +-
 .../include/numerics/flow/convection/cusp.hpp |   2 +-
 .../include/numerics/flow/convection/fds.hpp  |   2 +-
 .../include/numerics/flow/convection/fvs.hpp  |   2 +-
 .../include/numerics/flow/convection/hllc.hpp |   6 +-
 .../include/numerics/flow/convection/roe.hpp  |   6 +-
 .../include/numerics/flow/flow_diffusion.hpp  |   2 +-
 .../include/numerics/flow/flow_sources.hpp    |  54 +-
 SU2_CFD/include/numerics/heat.hpp             |  46 +-
 SU2_CFD/include/numerics/radiation.hpp        |   2 +-
 .../numerics/scalar/scalar_convection.hpp     |   2 +-
 .../numerics/scalar/scalar_diffusion.hpp      |  37 +-
 .../numerics/scalar/scalar_sources.hpp        |   2 +-
 .../numerics/species/species_convection.hpp   |   2 +-
 .../numerics/species/species_diffusion.hpp    |   2 +-
 .../numerics/species/species_sources.hpp      |   2 +-
 SU2_CFD/include/numerics/template.hpp         |   2 +-
 .../turbulent/transition/trans_convection.hpp |   2 +-
 .../transition/trans_correlations.hpp         | 192 +++++
 .../turbulent/transition/trans_diffusion.hpp  |  10 +-
 .../turbulent/transition/trans_sources.hpp    | 412 ++++++----
 .../numerics/turbulent/turb_convection.hpp    |   2 +-
 .../numerics/turbulent/turb_diffusion.hpp     |  11 +-
 .../numerics/turbulent/turb_sources.hpp       |  46 +-
 .../include/numerics_simd/CNumericsSIMD.cpp   |   2 +-
 .../include/numerics_simd/CNumericsSIMD.hpp   |   2 +-
 .../flow/convection/centered.hpp              |   2 +-
 .../numerics_simd/flow/convection/common.hpp  |   2 +-
 .../numerics_simd/flow/convection/roe.hpp     |   4 +-
 .../numerics_simd/flow/diffusion/common.hpp   |   2 +-
 .../flow/diffusion/viscous_fluxes.hpp         |   2 +-
 .../include/numerics_simd/flow/variables.hpp  |   2 +-
 SU2_CFD/include/numerics_simd/util.hpp        |   2 +-
 .../include/output/CAdjElasticityOutput.hpp   |   2 +-
 SU2_CFD/include/output/CAdjFlowCompOutput.hpp |   2 +-
 SU2_CFD/include/output/CAdjFlowIncOutput.hpp  |   2 +-
 SU2_CFD/include/output/CAdjFlowOutput.hpp     |   2 +-
 SU2_CFD/include/output/CAdjHeatOutput.hpp     |   2 +-
 SU2_CFD/include/output/CBaselineOutput.hpp    |   2 +-
 SU2_CFD/include/output/CElasticityOutput.hpp  |   2 +-
 SU2_CFD/include/output/CFVMOutput.hpp         |   4 +-
 SU2_CFD/include/output/CFlowCompFEMOutput.hpp |   2 +-
 SU2_CFD/include/output/CFlowCompOutput.hpp    |   2 +-
 SU2_CFD/include/output/CFlowIncOutput.hpp     |   2 +-
 SU2_CFD/include/output/CFlowOutput.hpp        |   2 +-
 SU2_CFD/include/output/CHeatOutput.hpp        |   2 +-
 SU2_CFD/include/output/CMeshOutput.hpp        |   2 +-
 SU2_CFD/include/output/CMultizoneOutput.hpp   |   2 +-
 SU2_CFD/include/output/CNEMOCompOutput.hpp    |   2 +-
 SU2_CFD/include/output/COutput.hpp            |   2 +-
 SU2_CFD/include/output/COutputFactory.hpp     |   2 +-
 SU2_CFD/include/output/COutputLegacy.hpp      |   2 +-
 .../output/filewriter/CCGNSFileWriter.hpp     |   2 +-
 .../output/filewriter/CCSVFileWriter.hpp      |   2 +-
 .../output/filewriter/CFEMDataSorter.hpp      |   2 +-
 .../output/filewriter/CFVMDataSorter.hpp      |   2 +-
 .../include/output/filewriter/CFileWriter.hpp |   2 +-
 .../output/filewriter/CParallelDataSorter.hpp |   2 +-
 .../filewriter/CParaviewBinaryFileWriter.hpp  |   2 +-
 .../output/filewriter/CParaviewFileWriter.hpp |   2 +-
 .../filewriter/CParaviewVTMFileWriter.hpp     |   2 +-
 .../filewriter/CParaviewXMLFileWriter.hpp     |   2 +-
 .../output/filewriter/CSTLFileWriter.hpp      |   4 +-
 .../filewriter/CSU2BinaryFileWriter.hpp       |   2 +-
 .../output/filewriter/CSU2FileWriter.hpp      |   2 +-
 .../output/filewriter/CSU2MeshFileWriter.hpp  |   2 +-
 .../filewriter/CSurfaceFEMDataSorter.hpp      |   2 +-
 .../filewriter/CSurfaceFVMDataSorter.hpp      |   2 +-
 .../filewriter/CTecplotBinaryFileWriter.hpp   |   2 +-
 .../output/filewriter/CTecplotFileWriter.hpp  |   2 +-
 .../include/output/tools/CWindowingTools.hpp  |   2 +-
 SU2_CFD/include/sgs_model.hpp                 |  10 +-
 SU2_CFD/include/sgs_model.inl                 |   2 +-
 SU2_CFD/include/solvers/CAdjEulerSolver.hpp   |   2 +-
 SU2_CFD/include/solvers/CAdjNSSolver.hpp      |   2 +-
 SU2_CFD/include/solvers/CAdjTurbSolver.hpp    |   2 +-
 SU2_CFD/include/solvers/CBaselineSolver.hpp   |   2 +-
 .../include/solvers/CBaselineSolver_FEM.hpp   |   4 +-
 SU2_CFD/include/solvers/CDiscAdjFEASolver.hpp |   2 +-
 .../include/solvers/CDiscAdjMeshSolver.hpp    |   2 +-
 SU2_CFD/include/solvers/CDiscAdjSolver.hpp    |   2 +-
 SU2_CFD/include/solvers/CEulerSolver.hpp      |   2 +-
 SU2_CFD/include/solvers/CFEASolver.hpp        |   2 +-
 SU2_CFD/include/solvers/CFEASolverBase.hpp    |   2 +-
 .../include/solvers/CFEM_DG_EulerSolver.hpp   |   4 +-
 SU2_CFD/include/solvers/CFEM_DG_NSSolver.hpp  |   4 +-
 .../include/solvers/CFVMFlowSolverBase.hpp    |   2 +-
 .../include/solvers/CFVMFlowSolverBase.inl    |   2 +-
 .../solvers/CGradientSmoothingSolver.hpp      |   2 +-
 SU2_CFD/include/solvers/CHeatSolver.hpp       |  89 +-
 SU2_CFD/include/solvers/CIncEulerSolver.hpp   |   2 +-
 SU2_CFD/include/solvers/CIncNSSolver.hpp      |   2 +-
 SU2_CFD/include/solvers/CMeshSolver.hpp       |   2 +-
 SU2_CFD/include/solvers/CNEMOEulerSolver.hpp  |   4 +-
 SU2_CFD/include/solvers/CNEMONSSolver.hpp     |   2 +-
 SU2_CFD/include/solvers/CNSSolver.hpp         |   2 +-
 SU2_CFD/include/solvers/CRadP1Solver.hpp      |   4 +-
 SU2_CFD/include/solvers/CRadSolver.hpp        |   2 +-
 SU2_CFD/include/solvers/CScalarSolver.hpp     |  26 +-
 SU2_CFD/include/solvers/CScalarSolver.inl     |  31 +-
 SU2_CFD/include/solvers/CSolver.hpp           |   2 +-
 SU2_CFD/include/solvers/CSolverFactory.hpp    |   2 +-
 SU2_CFD/include/solvers/CSpeciesSolver.hpp    |   2 +-
 SU2_CFD/include/solvers/CTemplateSolver.hpp   |   2 +-
 SU2_CFD/include/solvers/CTransLMSolver.hpp    |   8 +-
 SU2_CFD/include/solvers/CTurbSASolver.hpp     |   2 +-
 SU2_CFD/include/solvers/CTurbSSTSolver.hpp    |   2 +-
 SU2_CFD/include/solvers/CTurbSolver.hpp       |   2 +-
 SU2_CFD/include/task_definition.hpp           |   4 +-
 SU2_CFD/include/task_definition.inl           |   2 +-
 .../include/variables/CAdjEulerVariable.hpp   |   2 +-
 SU2_CFD/include/variables/CAdjNSVariable.hpp  |   2 +-
 .../include/variables/CAdjTurbVariable.hpp    |   2 +-
 .../include/variables/CBaselineVariable.hpp   |   2 +-
 .../variables/CDiscAdjFEABoundVariable.hpp    |   4 +-
 .../variables/CDiscAdjMeshBoundVariable.hpp   |   2 +-
 .../include/variables/CDiscAdjVariable.hpp    |   2 +-
 SU2_CFD/include/variables/CEulerVariable.hpp  |   2 +-
 .../include/variables/CFEABoundVariable.hpp   |   4 +-
 SU2_CFD/include/variables/CFEAVariable.hpp    |   4 +-
 SU2_CFD/include/variables/CFlowVariable.hpp   |   2 +-
 SU2_CFD/include/variables/CHeatVariable.hpp   |  35 +-
 .../include/variables/CIncEulerVariable.hpp   |   2 +-
 SU2_CFD/include/variables/CIncNSVariable.hpp  |   2 +-
 .../include/variables/CMeshBoundVariable.hpp  |   2 +-
 SU2_CFD/include/variables/CMeshElement.hpp    |   2 +-
 SU2_CFD/include/variables/CMeshVariable.hpp   |   2 +-
 .../include/variables/CNEMOEulerVariable.hpp  |   2 +-
 SU2_CFD/include/variables/CNEMONSVariable.hpp |   2 +-
 SU2_CFD/include/variables/CNSVariable.hpp     |   2 +-
 .../include/variables/CPrimitiveIndices.hpp   |   2 +-
 SU2_CFD/include/variables/CRadP1Variable.hpp  |   2 +-
 SU2_CFD/include/variables/CRadVariable.hpp    |   2 +-
 SU2_CFD/include/variables/CScalarVariable.hpp |   2 +-
 .../variables/CSobolevSmoothingVariable.hpp   |   2 +-
 .../include/variables/CSpeciesVariable.hpp    |   2 +-
 .../include/variables/CTransLMVariable.hpp    |   2 +-
 SU2_CFD/include/variables/CTurbSAVariable.hpp |  17 +-
 .../include/variables/CTurbSSTVariable.hpp    |   2 +-
 SU2_CFD/include/variables/CTurbVariable.hpp   |  32 +-
 SU2_CFD/include/variables/CVariable.hpp       |  45 +-
 SU2_CFD/obj/Makefile.am                       |   2 +-
 SU2_CFD/src/CMarkerProfileReaderFVM.cpp       |   2 +-
 SU2_CFD/src/SU2_CFD.cpp                       |   4 +-
 SU2_CFD/src/definition_structure.cpp          |   2 +-
 .../src/drivers/CDiscAdjMultizoneDriver.cpp   |   2 +-
 .../src/drivers/CDiscAdjSinglezoneDriver.cpp  |   2 +-
 SU2_CFD/src/drivers/CDriver.cpp               |  11 +-
 SU2_CFD/src/drivers/CDummyDriver.cpp          |   2 +-
 SU2_CFD/src/drivers/CMultizoneDriver.cpp      |   2 +-
 SU2_CFD/src/drivers/CSinglezoneDriver.cpp     |   2 +-
 SU2_CFD/src/fluid/CCoolProp.cpp               |   2 +-
 SU2_CFD/src/fluid/CFluidModel.cpp             |   2 +-
 SU2_CFD/src/fluid/CFluidScalar.cpp            |   2 +-
 SU2_CFD/src/fluid/CIdealGas.cpp               |   2 +-
 SU2_CFD/src/fluid/CMutationTCLib.cpp          |   2 +-
 SU2_CFD/src/fluid/CNEMOGas.cpp                |   2 +-
 SU2_CFD/src/fluid/CPengRobinson.cpp           |   2 +-
 SU2_CFD/src/fluid/CSU2TCLib.cpp               |   2 +-
 SU2_CFD/src/fluid/CVanDerWaalsGas.cpp         |   2 +-
 .../src/integration/CFEM_DG_Integration.cpp   |   2 +-
 SU2_CFD/src/integration/CIntegration.cpp      |   2 +-
 .../src/integration/CIntegrationFactory.cpp   |   2 +-
 .../src/integration/CMultiGridIntegration.cpp |   2 +-
 .../src/integration/CNewtonIntegration.cpp    |   2 +-
 .../integration/CSingleGridIntegration.cpp    |   2 +-
 .../integration/CStructuralIntegration.cpp    |   2 +-
 SU2_CFD/src/interfaces/CInterface.cpp         |   2 +-
 .../cfd/CConservativeVarsInterface.cpp        |   2 +-
 .../interfaces/cfd/CMixingPlaneInterface.cpp  |   2 +-
 .../src/interfaces/cfd/CSlidingInterface.cpp  |   2 +-
 .../cht/CConjugateHeatInterface.cpp           |   2 +-
 .../fsi/CDiscAdjFlowTractionInterface.cpp     |   2 +-
 .../fsi/CDisplacementsInterface.cpp           |   2 +-
 .../interfaces/fsi/CFlowTractionInterface.cpp |   2 +-
 SU2_CFD/src/iteration/CAdjFluidIteration.cpp  |  31 +-
 .../src/iteration/CDiscAdjFEAIteration.cpp    |   2 +-
 .../src/iteration/CDiscAdjFluidIteration.cpp  |   2 +-
 .../src/iteration/CDiscAdjHeatIteration.cpp   |   2 +-
 SU2_CFD/src/iteration/CFEAIteration.cpp       |   2 +-
 SU2_CFD/src/iteration/CFEMFluidIteration.cpp  |  27 +-
 SU2_CFD/src/iteration/CFluidIteration.cpp     |  40 +-
 SU2_CFD/src/iteration/CHeatIteration.cpp      |   2 +-
 SU2_CFD/src/iteration/CIteration.cpp          |   2 +-
 SU2_CFD/src/iteration/CIterationFactory.cpp   |   2 +-
 SU2_CFD/src/iteration/CTurboIteration.cpp     |   2 +-
 SU2_CFD/src/limiters/CLimiterDetails.cpp      |   2 +-
 SU2_CFD/src/numerics/CGradSmoothing.cpp       |   2 +-
 SU2_CFD/src/numerics/CNumerics.cpp            |   2 +-
 SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp   |   2 +-
 SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp  |   2 +-
 SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp    |   2 +-
 SU2_CFD/src/numerics/NEMO/convection/ausm.cpp |   2 +-
 .../numerics/NEMO/convection/ausmplusup2.cpp  |   2 +-
 .../numerics/NEMO/convection/ausmpwplus.cpp   |   2 +-
 SU2_CFD/src/numerics/NEMO/convection/lax.cpp  |   2 +-
 SU2_CFD/src/numerics/NEMO/convection/msw.cpp  |   2 +-
 SU2_CFD/src/numerics/NEMO/convection/roe.cpp  |   2 +-
 .../continuous_adjoint/adj_convection.cpp     |   2 +-
 .../continuous_adjoint/adj_diffusion.cpp      |   2 +-
 .../continuous_adjoint/adj_sources.cpp        |   2 +-
 .../numerics/elasticity/CFEAElasticity.cpp    |   2 +-
 .../elasticity/CFEALinearElasticity.cpp       |   2 +-
 .../elasticity/CFEANonlinearElasticity.cpp    |   2 +-
 .../numerics/elasticity/nonlinear_models.cpp  |   2 +-
 .../numerics/flow/convection/ausm_slau.cpp    |   2 +-
 .../src/numerics/flow/convection/centered.cpp |   2 +-
 SU2_CFD/src/numerics/flow/convection/cusp.cpp |   2 +-
 SU2_CFD/src/numerics/flow/convection/fds.cpp  |   2 +-
 SU2_CFD/src/numerics/flow/convection/fvs.cpp  |   2 +-
 SU2_CFD/src/numerics/flow/convection/hllc.cpp |   2 +-
 SU2_CFD/src/numerics/flow/convection/roe.cpp  |   2 +-
 SU2_CFD/src/numerics/flow/flow_diffusion.cpp  |   2 +-
 SU2_CFD/src/numerics/flow/flow_sources.cpp    | 101 ++-
 SU2_CFD/src/numerics/heat.cpp                 |  42 +-
 SU2_CFD/src/numerics/radiation.cpp            |   2 +-
 .../src/numerics/scalar/scalar_sources.cpp    |   2 +-
 .../src/numerics/species/species_sources.cpp  |   2 +-
 SU2_CFD/src/numerics/template.cpp             |   2 +-
 SU2_CFD/src/output/CAdjElasticityOutput.cpp   |   2 +-
 SU2_CFD/src/output/CAdjFlowCompOutput.cpp     |   2 +-
 SU2_CFD/src/output/CAdjFlowIncOutput.cpp      |   2 +-
 SU2_CFD/src/output/CAdjFlowOutput.cpp         |   2 +-
 SU2_CFD/src/output/CAdjHeatOutput.cpp         |   2 +-
 SU2_CFD/src/output/CBaselineOutput.cpp        |   2 +-
 SU2_CFD/src/output/CElasticityOutput.cpp      |   2 +-
 SU2_CFD/src/output/CFVMOutput.cpp             |  10 +-
 SU2_CFD/src/output/CFlowCompFEMOutput.cpp     |   2 +-
 SU2_CFD/src/output/CFlowCompOutput.cpp        |   2 +-
 SU2_CFD/src/output/CFlowIncOutput.cpp         |   2 +-
 SU2_CFD/src/output/CFlowOutput.cpp            |  21 +-
 SU2_CFD/src/output/CHeatOutput.cpp            |   2 +-
 SU2_CFD/src/output/CMeshOutput.cpp            |   2 +-
 SU2_CFD/src/output/CMultizoneOutput.cpp       |   2 +-
 SU2_CFD/src/output/CNEMOCompOutput.cpp        |   2 +-
 SU2_CFD/src/output/COutput.cpp                |   2 +-
 SU2_CFD/src/output/COutputFactory.cpp         |   2 +-
 .../src/output/filewriter/CCGNSFileWriter.cpp |   2 +-
 .../src/output/filewriter/CCSVFileWriter.cpp  |   2 +-
 .../src/output/filewriter/CFEMDataSorter.cpp  |   2 +-
 .../src/output/filewriter/CFVMDataSorter.cpp  |   2 +-
 .../output/filewriter/CParallelDataSorter.cpp |   2 +-
 .../output/filewriter/CParallelFileWriter.cpp |   2 +-
 .../filewriter/CParaviewBinaryFileWriter.cpp  |   2 +-
 .../output/filewriter/CParaviewFileWriter.cpp |   2 +-
 .../filewriter/CParaviewVTMFileWriter.cpp     |   2 +-
 .../filewriter/CParaviewXMLFileWriter.cpp     |   2 +-
 .../src/output/filewriter/CSTLFileWriter.cpp  |   2 +-
 .../filewriter/CSU2BinaryFileWriter.cpp       |   2 +-
 .../src/output/filewriter/CSU2FileWriter.cpp  |   2 +-
 .../output/filewriter/CSU2MeshFileWriter.cpp  |   2 +-
 .../filewriter/CSurfaceFEMDataSorter.cpp      |   2 +-
 .../filewriter/CSurfaceFVMDataSorter.cpp      |   2 +-
 .../filewriter/CTecplotBinaryFileWriter.cpp   |   2 +-
 .../output/filewriter/CTecplotFileWriter.cpp  |   2 +-
 SU2_CFD/src/output/output_physics.cpp         |   2 +-
 .../src/output/output_structure_legacy.cpp    |   2 +-
 SU2_CFD/src/output/tools/CWindowingTools.cpp  |   2 +-
 SU2_CFD/src/python_wrapper_structure.cpp      |   2 +-
 SU2_CFD/src/solvers/CAdjEulerSolver.cpp       |   9 +-
 SU2_CFD/src/solvers/CAdjNSSolver.cpp          |   9 +-
 SU2_CFD/src/solvers/CAdjTurbSolver.cpp        |  10 +-
 SU2_CFD/src/solvers/CBaselineSolver.cpp       |   2 +-
 SU2_CFD/src/solvers/CBaselineSolver_FEM.cpp   |   2 +-
 SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp     |   2 +-
 SU2_CFD/src/solvers/CDiscAdjMeshSolver.cpp    |   2 +-
 SU2_CFD/src/solvers/CDiscAdjSolver.cpp        |   2 +-
 SU2_CFD/src/solvers/CEulerSolver.cpp          |  47 +-
 SU2_CFD/src/solvers/CFEASolver.cpp            |   2 +-
 SU2_CFD/src/solvers/CFEASolverBase.cpp        |   2 +-
 SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp   |   2 +-
 SU2_CFD/src/solvers/CFEM_DG_NSSolver.cpp      |   2 +-
 .../src/solvers/CGradientSmoothingSolver.cpp  |   2 +-
 SU2_CFD/src/solvers/CHeatSolver.cpp           | 774 ++++++------------
 SU2_CFD/src/solvers/CIncEulerSolver.cpp       |   9 +-
 SU2_CFD/src/solvers/CIncNSSolver.cpp          |   2 +-
 SU2_CFD/src/solvers/CMeshSolver.cpp           |   2 +-
 SU2_CFD/src/solvers/CNEMOEulerSolver.cpp      | 547 ++++++-------
 SU2_CFD/src/solvers/CNEMONSSolver.cpp         |   2 +-
 SU2_CFD/src/solvers/CNSSolver.cpp             |   2 +-
 SU2_CFD/src/solvers/CRadP1Solver.cpp          |   2 +-
 SU2_CFD/src/solvers/CRadSolver.cpp            |   2 +-
 SU2_CFD/src/solvers/CSolver.cpp               |   2 +-
 SU2_CFD/src/solvers/CSolverFactory.cpp        |   3 +-
 SU2_CFD/src/solvers/CSpeciesSolver.cpp        |  11 +-
 SU2_CFD/src/solvers/CTemplateSolver.cpp       |   2 +-
 SU2_CFD/src/solvers/CTransLMSolver.cpp        |  76 +-
 SU2_CFD/src/solvers/CTurbSASolver.cpp         |  67 +-
 SU2_CFD/src/solvers/CTurbSSTSolver.cpp        |  52 +-
 SU2_CFD/src/solvers/CTurbSolver.cpp           |   2 +-
 SU2_CFD/src/variables/CAdjEulerVariable.cpp   |   2 +-
 SU2_CFD/src/variables/CAdjNSVariable.cpp      |   2 +-
 SU2_CFD/src/variables/CAdjTurbVariable.cpp    |   2 +-
 SU2_CFD/src/variables/CBaselineVariable.cpp   |   2 +-
 .../variables/CDiscAdjFEABoundVariable.cpp    |   2 +-
 .../variables/CDiscAdjMeshBoundVariable.cpp   |   2 +-
 SU2_CFD/src/variables/CDiscAdjVariable.cpp    |   2 +-
 SU2_CFD/src/variables/CEulerVariable.cpp      |   8 +-
 SU2_CFD/src/variables/CFEABoundVariable.cpp   |   2 +-
 SU2_CFD/src/variables/CFEAVariable.cpp        |   2 +-
 SU2_CFD/src/variables/CFlowVariable.cpp       |   2 +-
 SU2_CFD/src/variables/CHeatVariable.cpp       |  37 +-
 SU2_CFD/src/variables/CIncEulerVariable.cpp   |   2 +-
 SU2_CFD/src/variables/CIncNSVariable.cpp      |   2 +-
 SU2_CFD/src/variables/CMeshBoundVariable.cpp  |   2 +-
 SU2_CFD/src/variables/CMeshElement.cpp        |   2 +-
 SU2_CFD/src/variables/CMeshVariable.cpp       |   2 +-
 SU2_CFD/src/variables/CNEMOEulerVariable.cpp  |   2 +-
 SU2_CFD/src/variables/CNEMONSVariable.cpp     |   2 +-
 SU2_CFD/src/variables/CNSVariable.cpp         |   2 +-
 SU2_CFD/src/variables/CRadP1Variable.cpp      |   2 +-
 SU2_CFD/src/variables/CRadVariable.cpp        |   2 +-
 SU2_CFD/src/variables/CScalarVariable.cpp     |   2 +-
 .../variables/CSobolevSmoothingVariable.cpp   |   2 +-
 SU2_CFD/src/variables/CSpeciesVariable.cpp    |   2 +-
 SU2_CFD/src/variables/CTransLMVariable.cpp    |   2 +-
 SU2_CFD/src/variables/CTurbSAVariable.cpp     |   3 +-
 SU2_CFD/src/variables/CTurbSSTVariable.cpp    |   2 +-
 SU2_CFD/src/variables/CTurbVariable.cpp       |   9 +-
 SU2_CFD/src/variables/CVariable.cpp           |   2 +-
 SU2_DEF/include/SU2_DEF.hpp                   |   2 +-
 SU2_DEF/obj/Makefile.am                       |   2 +-
 SU2_DEF/src/SU2_DEF.cpp                       |   2 +-
 SU2_DOT/include/SU2_DOT.hpp                   |   2 +-
 SU2_DOT/obj/Makefile.am                       |   2 +-
 SU2_DOT/src/SU2_DOT.cpp                       |   2 +-
 SU2_GEO/include/SU2_GEO.hpp                   |   2 +-
 SU2_GEO/obj/Makefile.am                       |   2 +-
 SU2_GEO/src/SU2_GEO.cpp                       |   2 +-
 SU2_PY/FSI_tools/FSIInterface.py              |   2 +-
 SU2_PY/FSI_tools/FSI_config.py                |   2 +-
 SU2_PY/Makefile.am                            |   2 +-
 SU2_PY/OptimalPropeller.py                    |   2 +-
 SU2_PY/SU2/eval/design.py                     |   2 +-
 SU2_PY/SU2/eval/functions.py                  |   2 +-
 SU2_PY/SU2/eval/gradients.py                  |   2 +-
 SU2_PY/SU2/io/config.py                       |   2 +-
 SU2_PY/SU2/io/config_options.py               |   2 +-
 SU2_PY/SU2/io/data.py                         |   2 +-
 SU2_PY/SU2/io/filelock.py                     |   2 +-
 SU2_PY/SU2/io/redirect.py                     |   2 +-
 SU2_PY/SU2/io/state.py                        |   2 +-
 SU2_PY/SU2/io/tools.py                        |   2 +-
 SU2_PY/SU2/opt/project.py                     |   2 +-
 SU2_PY/SU2/opt/scipy_tools.py                 |   2 +-
 SU2_PY/SU2/run/adjoint.py                     |   2 +-
 SU2_PY/SU2/run/deform.py                      |   2 +-
 SU2_PY/SU2/run/direct.py                      |   2 +-
 SU2_PY/SU2/run/geometry.py                    |   2 +-
 SU2_PY/SU2/run/interface.py                   |   2 +-
 SU2_PY/SU2/run/merge.py                       |   2 +-
 SU2_PY/SU2/run/projection.py                  |   2 +-
 SU2_PY/SU2/util/filter_adjoint.py             |   2 +-
 SU2_PY/SU2/util/plot.py                       |   2 +-
 SU2_PY/SU2/util/polarSweepLib.py              |   2 +-
 SU2_PY/SU2/util/which.py                      |   2 +-
 SU2_PY/SU2_CFD.py                             |   2 +-
 SU2_PY/SU2_Nastran/pysu2_nastran.py           |   2 +-
 SU2_PY/change_version_number.py               |   6 +-
 SU2_PY/compute_multipoint.py                  |   2 +-
 SU2_PY/compute_polar.py                       |   2 +-
 SU2_PY/compute_stability.py                   |   2 +-
 SU2_PY/compute_uncertainty.py                 |   2 +-
 SU2_PY/config_gui.py                          |   2 +-
 SU2_PY/continuous_adjoint.py                  |   2 +-
 SU2_PY/convert_to_csv.py                      |   2 +-
 SU2_PY/direct_differentiation.py              |   2 +-
 SU2_PY/discrete_adjoint.py                    |   2 +-
 SU2_PY/finite_differences.py                  |   2 +-
 SU2_PY/fsi_computation.py                     |   2 +-
 SU2_PY/merge_solution.py                      |   2 +-
 SU2_PY/mesh_deformation.py                    |   2 +-
 SU2_PY/package_tests.py                       |   2 +-
 SU2_PY/parallel_computation.py                |   2 +-
 SU2_PY/parallel_computation_fsi.py            |   2 +-
 SU2_PY/parse_config.py                        |   2 +-
 SU2_PY/profiling.py                           |   2 +-
 SU2_PY/pySU2/Makefile.am                      |   2 +-
 SU2_PY/pySU2/pySU2.i                          |   2 +-
 SU2_PY/pySU2/pySU2ad.i                        |   2 +-
 SU2_PY/set_ffd_design_var.py                  |   2 +-
 SU2_PY/shape_optimization.py                  |   4 +-
 SU2_PY/topology_optimization.py               |   2 +-
 SU2_PY/updateHistoryMap.py                    |   2 +-
 SU2_SOL/include/SU2_SOL.hpp                   |   2 +-
 SU2_SOL/obj/Makefile.am                       |   2 +-
 SU2_SOL/src/SU2_SOL.cpp                       |   2 +-
 TestCases/TestCase.py                         |   2 +-
 .../aeroelastic/aeroelastic_NACA64A010.cfg    | 147 +---
 .../air_nozzle/air_nozzle_restart.cfg         |  31 +-
 .../cont_adj_euler/naca0012/inv_NACA0012.cfg  | 223 +----
 .../naca0012/inv_NACA0012_FD.cfg              | 221 +----
 .../naca0012/inv_NACA0012_discadj.cfg         | 211 +----
 .../cont_adj_euler/oneram6/inv_ONERAM6.cfg    | 258 +-----
 .../cont_adj_euler/wedge/inv_wedge_ROE.cfg    | 247 +-----
 .../wedge/inv_wedge_ROE_multiobj.cfg          | 265 +-----
 .../cylinder/lam_cylinder.cfg                 | 197 +----
 .../naca0012_sub/lam_NACA0012.cfg             | 206 +----
 .../naca0012_trans/lam_NACA0012.cfg           | 214 +----
 .../cont_adj_rans/naca0012/turb_nasa.cfg      | 193 +----
 .../naca0012/turb_nasa_binary.cfg             | 192 +----
 .../cont_adj_rans/oneram6/turb_ONERAM6.cfg    | 231 +-----
 .../cont_adj_rans/rae2822/turb_SA_RAE2822.cfg | 209 +----
 .../control_surface/inv_ONERAM6_moving.cfg    | 221 +----
 .../control_surface/inv_ONERAM6_setting.cfg   | 221 +----
 .../coupled_cht/comp_2d/cht_2d_3cylinders.cfg |  55 +-
 .../coupled_cht/comp_2d/flow_cylinder.cfg     | 115 +--
 .../coupled_cht/comp_2d/solid_cylinder1.cfg   |  97 +--
 .../coupled_cht/comp_2d/solid_cylinder2.cfg   | 107 +--
 .../coupled_cht/comp_2d/solid_cylinder3.cfg   | 108 +--
 .../disc_adj_incomp_2d/cht_2d_3cylinders.cfg  |  55 +-
 .../disc_adj_incomp_2d/flow_cylinder.cfg      | 148 +---
 .../disc_adj_incomp_2d/solid_cylinder1.cfg    |  97 +--
 .../disc_adj_incomp_2d/solid_cylinder2.cfg    | 107 +--
 .../disc_adj_incomp_2d/solid_cylinder3.cfg    | 105 ---
 .../chtMaster.cfg                             |  46 +-
 .../disc_adj_unsteadyCHT_cylinder/fluid.cfg   |  28 +-
 .../disc_adj_unsteadyCHT_cylinder/solid.cfg   |  22 +-
 .../incomp_2d/cht_2d_3cylinders.cfg           |  57 +-
 .../coupled_cht/incomp_2d/flow_cylinder.cfg   | 143 ----
 .../coupled_cht/incomp_2d/solid_cylinder1.cfg |  94 ---
 .../coupled_cht/incomp_2d/solid_cylinder2.cfg | 104 ---
 .../coupled_cht/incomp_2d/solid_cylinder3.cfg | 104 ---
 .../incomp_2d_unsteady/cht_2d_3cylinders.cfg  |  39 +-
 .../incomp_2d_unsteady/flow_cylinder.cfg      | 134 ---
 .../incomp_2d_unsteady/solid_cylinder1.cfg    |  86 --
 .../incomp_2d_unsteady/solid_cylinder2.cfg    |  89 +-
 .../incomp_2d_unsteady/solid_cylinder3.cfg    |  89 +-
 TestCases/ddes/flatplate/ddes_flatplate.cfg   | 127 +--
 .../deformation/brick_hex/def_brick_hex.cfg   | 146 +---
 .../brick_hex_rans/def_brick_hex_rans.cfg     | 150 +---
 .../brick_prism/def_brick_prism.cfg           | 147 +---
 .../brick_prism_rans/def_brick_prism_rans.cfg | 147 +---
 .../deformation/brick_pyra/def_brick_pyra.cfg | 149 +---
 .../deformation/brick_tets/def_brick_tets.cfg | 149 +---
 .../cylindrical_ffd/def_cylindrical.cfg       | 176 +---
 .../intersection_prevention/def_intersect.cfg | 264 +-----
 .../deformation/naca0012/def_NACA0012.cfg     | 215 +----
 .../naca0012/surface_file_NACA0012.cfg        | 223 +----
 .../deformation/naca4412/def_NACA4412.cfg     | 202 +----
 TestCases/deformation/rae2822/def_RAE2822.cfg | 245 +-----
 .../spherical_ffd/def_spherical.cfg           | 178 +---
 .../spherical_ffd/def_spherical_bspline.cfg   | 183 +----
 .../disc_adj_euler/arina2k/Arina2KRS.cfg      | 401 +--------
 .../cylinder3D/inv_cylinder3D.cfg             | 197 +----
 .../inv_NACA0012_pitching.cfg                 | 194 +----
 .../disc_adj_euler/oneram6/inv_ONERAM6.cfg    | 139 +---
 TestCases/disc_adj_fea/configAD_fem.cfg       |   2 +-
 .../disc_adj_fsi/Airfoil_2d/configFEA.cfg     |  19 +-
 .../disc_adj_fsi/Airfoil_2d/configFlow.cfg    |  27 +-
 TestCases/disc_adj_fsi/configFEA.cfg          |   2 +-
 TestCases/disc_adj_fsi/configFlow.cfg         |   2 +-
 TestCases/disc_adj_fsi/dyn_fsi/configFEA.cfg  |  20 +-
 TestCases/disc_adj_fsi/dyn_fsi/configFlow.cfg |  25 +-
 TestCases/disc_adj_heat/disc_adj_heat.cfg     |   9 +-
 .../naca0012/incomp_NACA0012_disc.cfg         | 145 +---
 .../cylinder/heated_cylinder.cfg              | 336 +-------
 .../naca0012/turb_naca0012_sa.cfg             | 211 +----
 .../naca0012/turb_naca0012_sst.cfg            | 210 +----
 TestCases/disc_adj_rans/cylinder/cylinder.cfg | 248 +-----
 .../cylinder/cylinder_Windowing.cfg           | 218 +----
 .../cylinder/cylinder_Windowing_AD.cfg        | 155 +---
 .../cylinder_DT_1ST/cylinder.cfg              | 245 +-----
 TestCases/disc_adj_rans/naca0012/naca0012.cfg |  76 +-
 .../naca0012/turb_NACA0012_sa.cfg             | 138 +---
 .../naca0012/turb_NACA0012_sst.cfg            | 140 +---
 .../transonic_stator_2D/transonic_stator.cfg  | 282 +------
 TestCases/euler/CRM/inv_CRM_JST.cfg           | 140 +---
 TestCases/euler/biparabolic/BIPARABOLIC.cfg   | 159 +---
 TestCases/euler/bluntbody/blunt.cfg           | 119 +--
 TestCases/euler/channel/inv_channel.cfg       | 117 +--
 TestCases/euler/channel/inv_channel_RK.cfg    | 121 +--
 TestCases/euler/naca0012/inv_NACA0012.cfg     | 214 +----
 TestCases/euler/naca0012/inv_NACA0012_Roe.cfg | 113 +--
 TestCases/euler/oneram6/inv_ONERAM6.cfg       | 262 +-----
 TestCases/euler/wedge/inv_wedge_HLLC.cfg      | 150 +---
 TestCases/fea_fsi/Airfoil_RBF/config.cfg      |   3 +-
 TestCases/fea_fsi/Airfoil_RBF/configFEA.cfg   |   3 +-
 TestCases/fea_fsi/Airfoil_RBF/configFlow.cfg  |   3 +-
 .../fea_fsi/DynBeam_2d/configBeam_2d.cfg      |   2 +-
 TestCases/fea_fsi/MixElemsKnowles/config.cfg  |   2 +-
 TestCases/fea_fsi/SquareCyl_Beam/config.cfg   | 157 +---
 .../fea_fsi/StatBeam_3d/configBeam_3d.cfg     |   2 +-
 .../fea_fsi/WallChannel_2d/configFEA.cfg      |   1 -
 .../fea_fsi/WallChannel_2d/configFSI.cfg      |   1 -
 .../fea_fsi/WallChannel_2d/configFlow.cfg     |   1 -
 TestCases/fea_fsi/dyn_fsi/configFlow.cfg      |   1 -
 TestCases/fea_fsi/stat_fsi/config.cfg         |   1 -
 TestCases/fea_fsi/stat_fsi/configFEA.cfg      |   7 +-
 TestCases/fea_fsi/stat_fsi/configFlow.cfg     |   9 -
 TestCases/fea_topology/config.cfg             |   5 +-
 .../quick_start/settings_compliance.cfg       |   1 -
 .../quick_start/settings_volfrac.cfg          |   3 +-
 TestCases/fixed_cl/naca0012/inv_NACA0012.cfg  | 219 +----
 .../naca0012/inv_NACA0012_ContAdj.cfg         | 223 +----
 .../naca0012/inv_NACA0012_gradsmooth.cfg      |   5 +-
 .../oneram6/ONERAM6_gradsmooth.cfg            |   3 +-
 TestCases/gust/inv_gust_NACA0012.cfg          | 134 +--
 TestCases/harmonic_balance/HB.cfg             | 257 +-----
 .../hb_rans_preconditioning/davis.cfg         | 144 +---
 .../2D/Quad32X32_nPoly4/InviscidVortex.cfg    |  99 +--
 .../3D/nPoly2_Tets/InviscidVortex.cfg         |  98 +--
 .../3D/nPoly4_Tets/InviscidVortex.cfg         |  99 +--
 .../fem_NACA0012.cfg                          |  92 +--
 .../NACA0012_5thOrder/fem_NACA0012.cfg        |  97 +--
 .../NACA0012_5thOrder/fem_NACA0012_reg.cfg    | 100 +--
 .../Ringleb/Quad100X50_nPoly3/Ringleb.cfg     |  95 +--
 .../Quad100X50_nPoly3/Ringleb_WallBC.cfg      |  95 +--
 .../Ringleb/Quad100X50_nPoly4/Ringleb.cfg     |  96 +--
 .../Quad100X50_nPoly4/Ringleb_WallBC.cfg      |  95 +--
 .../Ringleb/Quad200X100_nPoly4/Ringleb.cfg    |  96 +--
 .../Quad200X100_nPoly4/Ringleb_WallBC.cfg     |  95 +--
 .../Quad50X50_HalfGeom_nPoly4/Ringleb.cfg     |  96 +--
 .../Ringleb_WallBC.cfg                        |  95 +--
 .../Ringleb.cfg                               |  96 +--
 .../Ringleb_WallBC.cfg                        |  95 +--
 .../Triangle50X50_HalfGeom_nPoly4/Ringleb.cfg |  96 +--
 .../Ringleb_WallBC.cfg                        |  95 +--
 .../Sphere_4thOrder_Hexa/fem_Sphere.cfg       |  92 +--
 .../Sphere_4thOrder_Tet/fem_Sphere.cfg        |  96 +--
 .../nPoly1/fem_SubsonicChannel.cfg            | 102 +--
 .../nPoly1/fem_SubsonicChannel_Farfield.cfg   |  96 +--
 .../nPoly2/fem_SubsonicChannel.cfg            | 101 +--
 .../nPoly2/fem_SubsonicChannel_Farfield.cfg   |  97 +--
 .../nPoly4/fem_SubsonicChannel.cfg            | 102 +--
 .../nPoly4/fem_SubsonicChannel_Farfield.cfg   |  98 +--
 .../nPoly3/fem_Cylinder_reg.cfg               |  98 +--
 .../FlatPlate/nPoly4/lam_flatplate_reg.cfg    | 105 +--
 .../nPoly3_QuadDominant/fem_Sphere_reg.cfg    | 100 +--
 .../fem_Sphere_reg_ADER.cfg                   | 108 +--
 .../nPoly4/fem_unst_cylinder.cfg              | 104 +--
 .../nPoly4/fem_unst_cylinder_ADER.cfg         | 115 +--
 TestCases/hybrid_regression.py                |   2 +-
 TestCases/hybrid_regression_AD.py             |   2 +-
 .../incomp_euler/naca0012/incomp_NACA0012.cfg | 106 +--
 TestCases/incomp_euler/nozzle/inv_nozzle.cfg  | 121 +--
 .../incomp_navierstokes/bend/lam_bend.cfg     | 155 ----
 .../buoyancy_cavity/lam_buoyancy_cavity.cfg   | 152 +---
 .../cylinder/incomp_cylinder.cfg              | 100 +--
 .../cylinder/poly_cylinder.cfg                | 173 +---
 .../chtPinArray_2d/BC_HeatTransfer.cfg        |   2 +-
 .../chtPinArray_2d/DA_configMaster.cfg        |  32 +-
 .../chtPinArray_2d/FD_configMaster.cfg        |  40 +-
 .../chtPinArray_2d/configFluid.cfg            |   2 +-
 .../chtPinArray_2d/configMaster.cfg           |  36 +-
 .../chtPinArray_2d/configSolid.cfg            |   2 +-
 .../chtPinArray_2d/of_grad_findiff.csv.ref    |   2 +-
 .../chtPinArray_3d/configFluid.cfg            |   2 +-
 .../chtPinArray_3d/configMaster.cfg           |   4 +-
 .../chtPinArray_3d/configSolid.cfg            |   2 +-
 .../dp-adjoint_chtPinArray_2d/configFluid.cfg |   2 +-
 .../configMaster.cfg                          |  31 +-
 .../dp-adjoint_chtPinArray_2d/configSolid.cfg |   2 +-
 .../pipeSlice_3d/sp_pipeSlice_3d_dp_hf_tp.cfg |   6 +-
 .../incomp_rans/AhmedBody/turb_ahmed.cfg      | 193 -----
 TestCases/incomp_rans/naca0012/naca0012.cfg   | 138 +---
 .../naca0012/naca0012_SST_SUST.cfg            | 137 +---
 .../rough_flatplate_incomp.cfg                | 174 +---
 TestCases/mms/dg_navierstokes/lam_mms_dg.cfg  | 103 +--
 .../mms/dg_navierstokes_3d/lam_mms_dg_3d.cfg  | 117 +--
 TestCases/mms/dg_ringleb/ringleb_dg.cfg       | 106 +--
 .../mms/fvm_incomp_euler/inv_mms_jst.cfg      | 130 +--
 .../fvm_incomp_navierstokes/lam_mms_fds.cfg   | 141 +---
 .../mms/fvm_navierstokes/lam_mms_roe.cfg      | 152 +---
 TestCases/moving_wall/cavity/lam_cavity.cfg   | 132 +--
 .../spinning_cylinder/spinning_cylinder.cfg   | 140 +---
 .../naca0012/inv_NACA0012_ffd.cfg             | 242 +-----
 .../cylinder/cylinder_lowmach.cfg             | 121 +--
 .../navierstokes/cylinder/lam_cylinder.cfg    | 118 +--
 .../navierstokes/flatplate/lam_flatplate.cfg  |   3 +-
 .../flatplate/lam_flatplate_unst.cfg          |   4 +-
 .../navierstokes/naca0012/lam_NACA0012.cfg    | 115 +--
 TestCases/navierstokes/periodic2D/config.cfg  |   1 -
 .../poiseuille/lam_poiseuille.cfg             | 142 +---
 .../poiseuille/profile_poiseuille.cfg         | 163 +---
 TestCases/nicf/LS89/turb_SA_PR.cfg            | 186 +----
 TestCases/nicf/LS89/turb_SST_PR.cfg           | 185 +----
 TestCases/nicf/coolprop/fluidModel.cfg        |  32 +-
 TestCases/nicf/coolprop/transportModel.cfg    |  36 +-
 TestCases/nicf/edge/edge_PPR.cfg              | 132 +--
 TestCases/nicf/edge/edge_VW.cfg               | 130 +--
 .../nonequilibrium/invwedge/invwedge.cfg      |  74 +-
 .../invwedge/invwedge_ss_inlet.cfg            |  79 ++
 .../finitechemistry/thermalbath.cfg           |  96 +--
 .../finitechemistry/weakly_ionized.cfg        |   4 +-
 .../thermalbath/frozen/thermalbath_frozen.cfg |  97 +--
 .../nonequilibrium/viscous/axi_visccone.cfg   |   2 +-
 .../nonequilibrium/viscous/partial_cat.cfg    |   3 +-
 .../nonequilibrium/viscous/super_cat.cfg      |   3 +-
 .../viscwedge_mpp/viscwedge_mpp.cfg           |  78 +-
 .../equivalentarea_naca64206/NACA64206.cfg    |  21 +-
 .../inv_wedge_ROE_2surf_1obj.cfg              | 263 +-----
 .../inv_wedge_ROE_multiobj.cfg                | 262 +-----
 .../inv_wedge_ROE_multiobj_1surf.cfg          | 263 +-----
 .../inv_wedge_ROE_multiobj_combo.cfg          | 262 +-----
 .../inv_NACA0012_multipoint.cfg               | 224 +----
 .../pitching_NACA64A010.cfg                   | 223 +----
 .../pitching_oneram6/pitching_ONERAM6.cfg     | 238 +-----
 .../rotating_naca0012/rotating_NACA0012.cfg   | 210 +----
 .../steady_inverse_design/inv_NACA0012.cfg    | 214 +----
 .../steady_naca0012/inv_NACA0012_adv.cfg      | 231 +-----
 .../steady_naca0012/inv_NACA0012_basic.cfg    | 216 +----
 .../steady_oneram6/inv_ONERAM6_adv.cfg        | 247 +-----
 .../steady_oneram6/inv_ONERAM6_basic.cfg      | 249 +-----
 .../optimization_rans/naca0012/naca0012.cfg   |  77 +-
 .../pitching_naca64a010/turb_NACA64A010.cfg   | 241 +-----
 .../pitching_oneram6/turb_ONERAM6.cfg         | 259 +-----
 .../steady_oneram6/turb_ONERAM6.cfg           | 226 +----
 .../steady_rae2822/turb_SA_RAE2822.cfg        | 216 +----
 TestCases/parallel_regression.py              |  31 +-
 TestCases/parallel_regression_AD.py           |  62 +-
 TestCases/pastix_support/config.cfg           |   3 +-
 TestCases/pastix_support/readme.txt           |   2 +-
 TestCases/polar/naca0012/inv_NACA0012.cfg     | 225 +----
 .../flow_load_sens/run_adjoint.py             |   2 +-
 .../mesh_disp_sens/configAD_flow.cfg          |  37 -
 .../mesh_disp_sens/run_adjoint.py             |   2 +-
 .../flatPlate_rigidMotion_Conf.cfg            | 145 +---
 .../launch_flatPlate_rigidMotion.py           |   2 +-
 .../launch_unsteady_CHT_FlatPlate.py          |   2 +-
 .../unsteady_CHT_FlatPlate_Conf.cfg           | 301 +------
 .../translating_NACA0012/config.cfg           |   1 -
 .../radiation/p1adjoint/configp1adjoint.cfg   |   2 +-
 TestCases/radiation/p1model/configp1.cfg      |   3 +-
 .../propeller_variable_load.cfg               | 169 +---
 .../rans/flatplate/turb_SA_flatplate.cfg      | 134 +--
 .../flatplate/turb_SA_flatplate_species.cfg   | 114 +--
 .../rans/flatplate/turb_SST_flatplate.cfg     | 132 +--
 TestCases/rans/naca0012/turb_NACA0012_sa.cfg  | 139 +---
 TestCases/rans/naca0012/turb_NACA0012_sst.cfg | 141 +---
 .../naca0012/turb_NACA0012_sst_1994-KLm.cfg   |   3 +-
 .../naca0012/turb_NACA0012_sst_2003-Vm.cfg    |   3 +-
 .../rans/naca0012/turb_NACA0012_sst_2003m.cfg |   3 +-
 .../turb_NACA0012_sst_expliciteuler.cfg       |   5 +-
 .../turb_NACA0012_sst_fixedvalues.cfg         |   6 +-
 .../turb_NACA0012_sst_multigrid_restart.cfg   | 244 +-----
 .../rans/naca0012/turb_NACA0012_sst_sust.cfg  | 104 +--
 TestCases/rans/oneram6/turb_ONERAM6.cfg       | 165 +---
 TestCases/rans/oneram6/turb_ONERAM6_nk.cfg    |   5 +-
 TestCases/rans/oneram6/turb_ONERAM6_vc.cfg    | 130 +++
 TestCases/rans/propeller/propeller.cfg        | 158 +---
 TestCases/rans/rae2822/turb_SA_RAE2822.cfg    | 222 +----
 TestCases/rans/rae2822/turb_SST_RAE2822.cfg   | 130 +--
 .../rans/rae2822/turb_SST_SUST_RAE2822.cfg    | 130 +--
 .../rans/restart_directdiff_naca/naca0012.cfg |  76 +-
 TestCases/rans/s809/trans_s809.cfg            | 127 +--
 TestCases/rans/s809/turb_S809.cfg             | 142 +---
 TestCases/rans/vki_turbine/turb_vki.cfg       | 150 +---
 .../rans_uq/naca0012/turb_NACA0012_uq.cfg     | 138 +---
 .../rans_uq/naca0012/turb_NACA0012_uq_1c.cfg  | 144 +---
 .../rans_uq/naca0012/turb_NACA0012_uq_2c.cfg  | 141 +---
 .../rans_uq/naca0012/turb_NACA0012_uq_3c.cfg  | 140 +---
 .../naca0012/turb_NACA0012_uq_p1c1.cfg        | 142 +---
 .../naca0012/turb_NACA0012_uq_p1c2.cfg        | 140 +---
 .../caradonna_tung/rot_caradonna_tung.cfg     | 121 +--
 TestCases/rotating/naca0012/rot_NACA0012.cfg  | 232 +-----
 TestCases/serial_regression.py                |   4 +-
 TestCases/serial_regression_AD.py             |  40 +-
 .../sliding_interface/bars_SST_2D/bars.cfg    | 199 +----
 .../sliding_interface/bars_SST_2D/zone_1.cfg  |  11 +-
 .../sliding_interface/bars_SST_2D/zone_2.cfg  |  10 +-
 .../sliding_interface/bars_SST_2D/zone_3.cfg  |  11 +-
 .../channel_2D/channel_2D_NN.cfg              | 136 +--
 .../channel_2D/channel_2D_WA.cfg              | 131 +--
 .../sliding_interface/channel_2D/zone_1.cfg   |   9 -
 .../sliding_interface/channel_2D/zone_2.cfg   |  13 +-
 .../sliding_interface/channel_2D/zone_3.cfg   |  11 +-
 .../channel_3D/channel_3D_NN.cfg              | 136 +--
 .../channel_3D/channel_3D_WA.cfg              | 133 +--
 .../sliding_interface/channel_3D/zone_1.cfg   |   5 +-
 .../sliding_interface/channel_3D/zone_2.cfg   |  12 +-
 .../sliding_interface/channel_3D/zone_3.cfg   |  11 +-
 .../incompressible_steady/config.cfg          |   2 +-
 .../incompressible_steady/configCircle.cfg    |  21 +-
 .../incompressible_steady/configOut.cfg       |  18 +-
 .../incompressible_unsteady/config.cfg        |   2 +-
 .../incompressible_unsteady/configCircle.cfg  |  19 +-
 .../incompressible_unsteady/configOut.cfg     |  21 +-
 TestCases/sliding_interface/pipe/pipe_NN.cfg  | 141 +---
 TestCases/sliding_interface/pipe/pipe_WA.cfg  | 140 +---
 TestCases/sliding_interface/pipe/zone_1.cfg   |  12 +-
 TestCases/sliding_interface/pipe/zone_2.cfg   |  13 +-
 TestCases/sliding_interface/pipe/zone_3.cfg   |  12 +-
 TestCases/sliding_interface/pipe/zone_4.cfg   |  14 +-
 TestCases/sliding_interface/pipe/zone_5.cfg   |  14 +-
 .../rotating_cylinders/rot_cylinders_NN.cfg   | 137 +---
 .../rotating_cylinders/rot_cylinders_WA.cfg   | 138 +---
 .../rotating_cylinders/zone_1.cfg             |   9 -
 .../rotating_cylinders/zone_2.cfg             |  10 -
 .../rotating_cylinders/zone_3.cfg             |   9 -
 .../single_stage/single_stage_NN.cfg          | 168 +---
 .../single_stage/single_stage_WA.cfg          | 165 +---
 .../sliding_interface/single_stage/zone_1.cfg |  11 +-
 .../sliding_interface/single_stage/zone_2.cfg |  12 +-
 .../sup_vor_shed_NN.cfg                       | 141 +---
 .../sup_vor_shed_WA.cfg                       | 139 +---
 .../supersonic_vortex_shedding/zone_1.cfg     |  12 +-
 .../supersonic_vortex_shedding/zone_2.cfg     |  12 +-
 .../uniform_flow/uniform_NN.cfg               | 135 +--
 .../uniform_flow/uniform_WA.cfg               | 135 +--
 .../sliding_interface/uniform_flow/zone_1.cfg |  11 +-
 .../sliding_interface/uniform_flow/zone_2.cfg |  11 +-
 .../periodic_pins/configSolid.cfg             |   8 +-
 .../multizone/configMaster.cfg                |   5 +-
 .../species_transport/multizone/zone1.cfg     |   1 -
 .../species_transport/multizone/zone2.cfg     |   1 -
 .../passive_transport.cfg                     |   5 +-
 .../DAspecies3_primitiveVenturi.cfg           |   5 +-
 .../species2_primitiveVenturi.cfg             |   5 +-
 ...pecies2_primitiveVenturi_boundedscalar.cfg |   5 +-
 .../species2_primitiveVenturi_mixingmodel.cfg |   5 +-
 ...eVenturi_mixingmodel_TURBULENT_MARKERS.cfg |   2 +-
 ...itiveVenturi_mixingmodel_boundedscalar.cfg |   5 +-
 ...iveVenturi_mixingmodel_heatcapacity_H2.cfg |   5 +-
 ...Venturi_mixingmodel_heatcapacity_H2_ND.cfg |   5 +-
 ...primitiveVenturi_mixingmodel_viscosity.cfg |   5 +-
 .../species3_primitiveVenturi.cfg             |   5 +-
 .../species3_primitiveVenturi_inletFile.cfg   |   5 +-
 .../transitional_BC_model_ConfigFile.cfg      | 139 +---
 .../transitional_BC_model_ConfigFile.cfg      | 158 +---
 .../transitional_BC_model_ConfigFile.cfg      | 155 +---
 .../APU_turbocharger/Jones_restart.cfg        |  12 +-
 .../turbomachinery/APU_turbocharger/rotor.cfg |  11 -
 .../APU_turbocharger/rotor_restart.cfg        |  11 -
 .../APU_turbocharger/stator.cfg               |   4 -
 .../axial_stage_2D/Axial_stage2D.cfg          | 179 +---
 .../turbomachinery/axial_stage_2D/zone_1.cfg  |   7 +-
 .../turbomachinery/axial_stage_2D/zone_2.cfg  |  10 +-
 .../centrifugal_blade/centrifugal_blade.cfg   | 214 +----
 .../centrifugal_stage/centrifugal_stage.cfg   | 217 +----
 .../transonic_stator_restart.cfg              |   8 +-
 .../sa/rae2822/turb_SA_BSL_RAE2822.cfg        |  89 +-
 .../sa/rae2822/turb_SA_COMP_EDW_RAE2822.cfg   |  88 --
 .../sa/rae2822/turb_SA_COMP_RAE2822.cfg       |  89 +-
 .../sa/rae2822/turb_SA_EDW_RAE2822.cfg        |  89 +-
 .../sa/rae2822/turb_SA_NEG_RAE2822.cfg        | 106 +--
 .../sa/rae2822/turb_SA_QCR_RAE2822.cfg        |  88 --
 TestCases/tutorials.py                        |  20 +-
 .../config_incomp_turb_sa.cfg                 |  15 +-
 .../pitching_NACA64A010.cfg                   | 221 +----
 .../turb_NACA64A010.cfg                       | 239 +-----
 .../plunging_naca0012/plunging_NACA0012.cfg   | 129 +--
 .../unsteady/square_cylinder/turb_square.cfg  | 149 +---
 .../user_defined_functions/lam_flatplate.cfg  |   2 +-
 TestCases/vandv.py                            |   2 +-
 .../compressible_SA/turb_SA_flatplate.cfg     |   9 +-
 .../compressible_SST/turb_SST_flatplate.cfg   |   9 +-
 .../incompressible_SA/turb_SA_flatplate.cfg   |   9 +-
 .../incompressible_SST/turb_SST_flatplate.cfg |  13 +-
 .../Common/containers/CLookupTable_tests.cpp  |   2 +-
 UnitTests/Common/geometry/CGeometry_test.cpp  |   2 +-
 .../geometry/dual_grid/CDualGrid_tests.cpp    |   2 +-
 .../primal_grid/CPrimalGrid_tests.cpp         |   2 +-
 UnitTests/Common/simple_ad_test.cpp           |   2 +-
 UnitTests/Common/simple_directdiff_test.cpp   |   2 +-
 .../toolboxes/C1DInterpolation_tests.cpp      |   2 +-
 .../CQuasiNewtonInvLeastSquares_tests.cpp     |   2 +-
 .../Common/toolboxes/ndflattener_tests.cpp    |   2 +-
 UnitTests/Common/vectorization.cpp            |   2 +-
 UnitTests/SU2_CFD/gradients.cpp               |   2 +-
 .../SU2_CFD/numerics/CNumerics_tests.cpp      |   2 +-
 UnitTests/SU2_CFD/windowing.cpp               |   2 +-
 UnitTests/UnitQuadTestCase.hpp                |   2 +-
 UnitTests/test_driver.cpp                     |   2 +-
 config_template.cfg                           |  15 +-
 externals/Makefile.am                         |   2 +-
 externals/tecio/Makefile.am                   |   2 +-
 legacy/Makefile.am                            |   2 +-
 legacy/configure.ac                           |   2 +-
 legacy/preconfigure.py                        |   2 +-
 meson.build                                   |  32 +-
 meson.py                                      |   2 +-
 meson_scripts/init.py                         |   2 +-
 su2omp.syntax.json                            |   2 +-
 1073 files changed, 4087 insertions(+), 37291 deletions(-)
 create mode 100644 .github/release.yml
 create mode 100644 SU2_CFD/include/numerics/turbulent/transition/trans_correlations.hpp
 create mode 100644 TestCases/nonequilibrium/invwedge/invwedge_ss_inlet.cfg
 create mode 100644 TestCases/rans/oneram6/turb_ONERAM6_vc.cfg

diff --git a/.github/release.yml b/.github/release.yml
new file mode 100644
index 00000000000..4ec929fc17c
--- /dev/null
+++ b/.github/release.yml
@@ -0,0 +1,20 @@
+# .github/release.yml
+
+changelog:
+  exclude:
+    labels:
+      - 'changelog:none'
+  categories:
+      - title: ':rocket: Experimental Features'
+        labels:
+          - 'changelog:feature'
+      - title: ':pill: Bug Fixes'
+        labels:
+          - 'changelog:fix'
+      - title: ':wrench: Maintenance'
+        labels:
+          - 'changelog:chore'
+      - title: 'Other Changes'
+        labels:
+          - "*"
+
diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 8e2d4414353..e749e661e70 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -6,7 +6,7 @@ on:
       - 'develop'
       - 'master'
   pull_request:
-    branches: 
+    branches:
       - 'develop'
       - 'master'
   workflow_call:
@@ -22,7 +22,7 @@ jobs:
     name: Build SU2
     strategy:
       fail-fast: false
-      matrix: 
+      matrix:
         config_set: [BaseMPI, ReverseMPI, ForwardMPI, BaseNoMPI, ReverseNoMPI, ForwardNoMPI, BaseOMP, ReverseOMP, ForwardOMP]
         include:
           - config_set: BaseMPI
@@ -32,7 +32,7 @@ jobs:
           - config_set: ForwardMPI
             flags: '-Denable-directdiff=true -Denable-normal=false -Denable-tests=true --warnlevel=3 --werror'
           - config_set: BaseNoMPI
-            flags: '-Denable-pywrapper=true -Dwith-mpi=disabled -Denable-tests=true --warnlevel=3 --werror'
+            flags: '-Denable-pywrapper=true -Denable-openblas=true -Dwith-mpi=disabled -Denable-tests=true --warnlevel=3 --werror'
           - config_set: ReverseNoMPI
             flags: '-Denable-autodiff=true -Denable-normal=false -Dwith-mpi=disabled -Denable-pywrapper=true -Denable-tests=true --warnlevel=3 --werror'
           - config_set: ForwardNoMPI
@@ -51,24 +51,24 @@ jobs:
           path: ccache
           key: ${{ matrix.config_set }}-${{ github.sha }}
           restore-keys: ${{ matrix.config_set }}
-      - name: Pre Cleanup 
-        uses: docker://ghcr.io/su2code/su2/build-su2:221027-0442
+      - name: Pre Cleanup
+        uses: docker://ghcr.io/su2code/su2/build-su2:221224-1158
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
-      - name: Build 
-        uses: docker://ghcr.io/su2code/su2/build-su2:221027-0442
+      - name: Build
+        uses: docker://ghcr.io/su2code/su2/build-su2:221224-1158
         with:
           args: -b ${{github.ref}} -f "${{matrix.flags}}"
       - name: Compress binaries
         run: tar -zcvf install_bin.tgz install/bin
-      - name: Upload Binaries 
+      - name: Upload Binaries
         uses: actions/upload-artifact@v3
         with:
           name: ${{ matrix.config_set }}
           path: install_bin.tgz
       - name: Post Cleanup
-        uses: docker://ghcr.io/su2code/su2/build-su2:221027-0442
+        uses: docker://ghcr.io/su2code/su2/build-su2:221224-1158
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -78,7 +78,7 @@ jobs:
     needs: build
     strategy:
       fail-fast: false
-      matrix: 
+      matrix:
         testscript: ['vandv.py', 'tutorials.py', 'parallel_regression.py', 'parallel_regression_AD.py', 'serial_regression.py', 'serial_regression_AD.py', 'hybrid_regression.py', 'hybrid_regression_AD.py']
         include:
           - testscript: 'vandv.py'
@@ -99,7 +99,7 @@ jobs:
             tag: OMP
     steps:
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:220614-1237
+        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -119,18 +119,18 @@ jobs:
               tar -zxvf install_bin.tgz
               ls -lah install/bin/
               cp -r install/bin/* $BIN_FOLDER;
-              popd; 
+              popd;
             fi
           done
           chmod a+x $BIN_FOLDER/*
           ls -lahR $BIN_FOLDER
       - name: Run Tests in Container
-        uses: docker://ghcr.io/su2code/su2/test-su2:220614-1237
+        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
           args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
       - name: Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:220614-1237
+        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -150,8 +150,8 @@ jobs:
           - testdriver: 'test_driver_DD'
             tag: MPI
     steps:
-      - name: Pre Cleanup 
-        uses: docker://ghcr.io/su2code/su2/test-su2:220614-1237
+      - name: Pre Cleanup
+        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -196,8 +196,8 @@ jobs:
           branch="${{github.ref}}"
           name="SU2"
           SRC_FOLDER="$PWD/src"
-          mkdir -p $SRC_FOLDER 
-          cd $SRC_FOLDER 
+          mkdir -p $SRC_FOLDER
+          cd $SRC_FOLDER
           git clone --recursive --depth=1 --shallow-submodules https://github.com/su2code/SU2 $name
           cd $name
           git config --add remote.origin.fetch '+refs/pull/*/merge:refs/remotes/origin/refs/pull/*/merge'
@@ -212,11 +212,11 @@ jobs:
           echo $PWD
           ls -lahR
       - name: Run Unit Tests
-        uses: docker://ghcr.io/su2code/su2/test-su2:220614-1237
+        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
         with:
           entrypoint: install/bin/${{matrix.testdriver}}
       - name: Post Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:220614-1237
+        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
diff --git a/.github/workflows/release-management.yml b/.github/workflows/release-management.yml
index adba5b895b5..921724fcc9e 100644
--- a/.github/workflows/release-management.yml
+++ b/.github/workflows/release-management.yml
@@ -35,7 +35,7 @@ jobs:
           key: ${{ matrix.os_bin }}-${{ github.sha }}
           restore-keys: ${{ matrix.os_bin }}
       - name: Build
-        uses: docker://ghcr.io/su2code/su2/build-su2-cross:220716-1459
+        uses: docker://ghcr.io/su2code/su2/build-su2-cross:221224-1158
         with:
           args: -b ${{ github.sha }} -f "${{matrix.flags}}"
       - name: Create Archive
diff --git a/AUTHORS.md b/AUTHORS.md
index 53a02f26eb3..0413260bd35 100644
--- a/AUTHORS.md
+++ b/AUTHORS.md
@@ -90,6 +90,7 @@ Jessie Lauzon
 João Loureiro
 Johannes Blühdorn
 JonathanSmith1936
+Josy P. Pullockara
 Kedar Naik
 LaSerpe
 Lennaert Tol
@@ -121,6 +122,7 @@ Scott Imlay
 Steffen Schotthöfer
 Steven Endres
 Sunoh Kang
+T. N. Venkatesh
 Teus van der Stelt
 Thomas D. Economon
 Tim Albring
@@ -128,6 +130,7 @@ TobiKattmann
 Trent Lukaczyk
 VivaanKhatri
 Wally Maier
+Y. Chandukrishna
 Zan Xu
 aaronyicongfu
 aeroamit
diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index 90f92ec6c42..a56c907ed9d 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -3,7 +3,7 @@
  * \brief All the information about the definition of the physical problem.
  *        The subroutines and functions are in the <i>CConfig.cpp</i> file.
  * \author F. Palacios, T. Economon, B. Tracey
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -125,6 +125,7 @@ class CConfig {
   Low_Mach_Precon,          /*!< \brief Flag to know if we are using a low Mach number preconditioner. */
   Low_Mach_Corr,            /*!< \brief Flag to know if we are using a low Mach number correction. */
   GravityForce,             /*!< \brief Flag to know if the gravity force is incuded in the formulation. */
+  VorticityConfinement,     /*!< \brief Flag to know if the Vorticity Confinement is included in the formulation. */
   SubsonicEngine,           /*!< \brief Engine intake subsonic region. */
   Frozen_Visc_Cont,         /*!< \brief Flag for cont. adjoint problem with/without frozen viscosity. */
   Frozen_Visc_Disc,         /*!< \brief Flag for disc. adjoint problem with/without frozen viscosity. */
@@ -147,6 +148,7 @@ class CConfig {
   su2double dCMy_dCL;          /*!< \brief Fixed Cl mode derivate. */
   su2double dCMz_dCL;          /*!< \brief Fixed Cl mode derivate. */
   su2double CL_Target;         /*!< \brief Fixed Cl mode Target Cl. */
+  su2double Confinement_Param; /*!< \brief Confinement paramenter for Vorticity Confinement method. */
   TIME_MARCHING TimeMarching;        /*!< \brief Steady or unsteady (time stepping or dual time stepping) computation. */
   unsigned short Dynamic_Analysis;   /*!< \brief Static or dynamic structural analysis. */
   su2double FixAzimuthalLine;        /*!< \brief Fix an azimuthal line due to misalignments of the nearfield. */
@@ -284,7 +286,6 @@ class CConfig {
   su2double *Inlet_Temperature;              /*!< \brief Specified temperatures for a supersonic inlet boundaries. */
   su2double *Inlet_Pressure;                 /*!< \brief Specified static pressures for supersonic inlet boundaries. */
   su2double **Inlet_Velocity;                /*!< \brief Specified flow velocity vectors for supersonic inlet boundaries. */
-  su2double **Inlet_MassFrac;                /*!< \brief Specified Mass fraction vectors for supersonic inlet boundaries (NEMO solver). */
   su2double **Inlet_SpeciesVal;              /*!< \brief Specified species vector for inlet boundaries. */
   su2double **Inlet_TurbVal;                 /*!< \brief Specified turbulent intensity and viscosity ratio for inlet boundaries. */
   su2double *EngineInflow_Target;            /*!< \brief Specified fan face targets for nacelle boundaries. */
@@ -589,6 +590,8 @@ class CConfig {
   SPECIES_MODEL Kind_Species_Model; /*!< \brief Species model definition. */
   TURB_SGS_MODEL Kind_SGS_Model;    /*!< \brief LES SGS model definition. */
   TURB_TRANS_MODEL Kind_Trans_Model;  /*!< \brief Transition model definition. */
+  TURB_TRANS_CORRELATION Kind_Trans_Correlation;  /*!< \brief Transition correlation model definition. */
+  su2double hRoughness;             /*!< \brief RMS roughness for Transition model. */
   unsigned short Kind_ActDisk, Kind_Engine_Inflow,
   *Kind_Data_Riemann,
   *Kind_Data_Giles;                /*!< \brief Kind of inlet boundary treatment. */
@@ -715,8 +718,10 @@ class CConfig {
   string *Config_Filenames;           /*!< \brief List of names for configuration files. */
   SST_OPTIONS *SST_Options;           /*!< \brief List of modifications/corrections/versions of SST turbulence model.*/
   SA_OPTIONS *SA_Options;             /*!< \brief List of modifications/corrections/versions of SA turbulence model.*/
+  LM_OPTIONS *LM_Options;             /*!< \brief List of modifications/corrections/versions of SA turbulence model.*/
   unsigned short nSST_Options;        /*!< \brief Number of SST options specified. */
   unsigned short nSA_Options;         /*!< \brief Number of SA options specified. */
+  unsigned short nLM_Options;         /*!< \brief Number of SA options specified. */
   WALL_FUNCTIONS  *Kind_WallFunctions;        /*!< \brief The kind of wall function to use for the corresponding markers. */
   unsigned short  **IntInfo_WallFunctions;    /*!< \brief Additional integer information for the wall function markers. */
   su2double       **DoubleInfo_WallFunctions; /*!< \brief Additional double information for the wall function markers. */
@@ -1155,6 +1160,7 @@ class CConfig {
   bool Multizone_Residual;        /*!< \brief Determines if memory should be allocated for the multizone residual. */
   SST_ParsedOptions sstParsedOptions; /*!< \brief Additional parameters for the SST turbulence model. */
   SA_ParsedOptions saParsedOptions;   /*!< \brief Additional parameters for the SA turbulence model. */
+  LM_ParsedOptions lmParsedOptions;   /*!< \brief Additional parameters for the LM transition model. */
   su2double uq_delta_b;         /*!< \brief Parameter used to perturb eigenvalues of Reynolds Stress Matrix */
   unsigned short eig_val_comp;  /*!< \brief Parameter used to determine type of eigenvalue perturbation */
   su2double uq_urlx;            /*!< \brief Under-relaxation factor */
@@ -1183,6 +1189,7 @@ class CConfig {
 
   /* other NEMO configure options*/
   unsigned short nSpecies_Cat_Wall,         /*!< \brief No. of species for a catalytic wall. */
+  nSpecies_inlet,                           /*!< \brief No. of species for NEMO inlet. */
   iWall_Catalytic,                          /*!< \brief Iterator over catalytic walls. */
   nWall_Catalytic;                          /*!< \brief No. of catalytic walls. */
   su2double *Gas_Composition,               /*!< \brief Initial mass fractions of flow [dimensionless]. */
@@ -1197,6 +1204,8 @@ class CConfig {
   *Wall_Catalytic;                          /*!< \brief Pointer to catalytic walls. */
   TRANSCOEFFMODEL   Kind_TransCoeffModel;   /*!< \brief Transport coefficient Model for NEMO solver. */
   su2double CatalyticEfficiency;            /*!< \brief Wall catalytic efficiency. */
+  su2double *Inlet_MassFrac;                /*!< \brief Specified Mass fraction vectors for NEMO inlet boundaries. */
+  su2double Inlet_Temperature_ve;           /*!< \brief Specified Tve for supersonic inlet boundaries (NEMO solver). */
 
   /*--- Additional species solver options ---*/
   bool Species_Clipping;           /*!< \brief Boolean that activates solution clipping for scalar transport. */
@@ -1578,6 +1587,12 @@ class CConfig {
    */
   su2double GetGamma(void) const { return Gamma; }
 
+  /*!
+   * \brief Get the value of the Confinement Parameter.
+   * \return Value of the constant: Confinement Parameter
+   */
+  su2double GetConfinement_Param(void) const { return Confinement_Param; }
+
   /*!
    * \brief Get the values of the CFL adaption parameters.
    * \return Value of CFL adaption parameter
@@ -4316,6 +4331,18 @@ class CConfig {
    */
   TURB_TRANS_MODEL GetKind_Trans_Model(void) const { return Kind_Trans_Model; }
 
+  /*!
+   * \brief Get the kind of the transition correlations.
+   * \return Kind of the transition correlation.
+   */
+  TURB_TRANS_CORRELATION GetKind_Trans_Correlation(void) const { return Kind_Trans_Correlation; }
+
+  /*!
+   * \brief Get RMS roughness for Transtion model from config
+   * \return Value of roughness.
+   */
+  su2double GethRoughness(void) const { return hRoughness; }
+  
   /*!
    * \brief Get the kind of the species model.
    * \return Kind of the species model.
@@ -5986,6 +6013,12 @@ class CConfig {
    */
   bool GetGravityForce(void) const { return GravityForce; }
 
+  /*!
+   * \brief Get information about the Vorticity Confinement.
+   * \return <code>TRUE</code> if it uses Vorticity Confinement; otherwise <code>FALSE</code>.
+   */
+  bool GetVorticityConfinement(void) const { return VorticityConfinement; }
+
   /*!
    * \brief Get information about the body force.
    * \return <code>TRUE</code> if it uses a body force; otherwise <code>FALSE</code>.
@@ -6655,6 +6688,20 @@ class CConfig {
    */
   const su2double* GetInlet_Velocity(string val_index) const;
 
+  /*!
+   * \brief Get the mass fraction vector for a NEMO inlet boundary.
+   * \param[in] val_index - Index corresponding to the inlet boundary.
+   * \return The inlet velocity vector.
+   */
+  const su2double* GetInlet_MassFrac() const { return Inlet_MassFrac; }
+
+  /*!
+   * \brief Get the Tve value for a NEMO inlet boundary.
+   * \param[in] val_index - Index corresponding to the inlet boundary.
+   * \return The inlet velocity vector.
+   */
+  su2double GetInlet_Temperature_ve() const { return Inlet_Temperature_ve; }
+
   /*!
    * \brief Get the total pressure at an inlet boundary.
    * \param[in] val_index - Index corresponding to the inlet boundary.
@@ -9685,4 +9732,10 @@ class CConfig {
    */
   SA_ParsedOptions GetSAParsedOptions() const { return saParsedOptions; }
 
+  /*!
+   * \brief Get parsed LM option data structure.
+   * \return LM option data structure.
+   */
+  LM_ParsedOptions GetLMParsedOptions() const { return lmParsedOptions; }
+
 };
diff --git a/Common/include/adt/CADTBaseClass.hpp b/Common/include/adt/CADTBaseClass.hpp
index 92f7977a748..b9ad331cdbc 100644
--- a/Common/include/adt/CADTBaseClass.hpp
+++ b/Common/include/adt/CADTBaseClass.hpp
@@ -2,7 +2,7 @@
  * \file CADTBaseClass.hpp
  * \brief Base class for storing an ADT in an arbitrary number of dimensions.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/adt/CADTComparePointClass.hpp b/Common/include/adt/CADTComparePointClass.hpp
index f1b5ffc1662..e405a7a3aa6 100644
--- a/Common/include/adt/CADTComparePointClass.hpp
+++ b/Common/include/adt/CADTComparePointClass.hpp
@@ -2,7 +2,7 @@
  * \file CADTComparePointClass.hpp
  * \brief subroutines for comparing two points in an alternating digital tree (ADT).
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/adt/CADTElemClass.hpp b/Common/include/adt/CADTElemClass.hpp
index 8fbb97b8696..5acd203af22 100644
--- a/Common/include/adt/CADTElemClass.hpp
+++ b/Common/include/adt/CADTElemClass.hpp
@@ -2,7 +2,7 @@
  * \file CADTElemClass.hpp
  * \brief Class for storing an ADT of (linear) elements in an arbitrary number of dimensions.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -36,7 +36,7 @@
  * \ingroup ADT
  * \brief  Class for storing an ADT of (linear) elements in an arbitrary number of dimensions.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CADTElemClass : public CADTBaseClass {
 private:
diff --git a/Common/include/adt/CADTNodeClass.hpp b/Common/include/adt/CADTNodeClass.hpp
index c6f5a565628..ac311b9e2c0 100644
--- a/Common/include/adt/CADTNodeClass.hpp
+++ b/Common/include/adt/CADTNodeClass.hpp
@@ -2,7 +2,7 @@
  * \file CADTNodeClass.hpp
  * \brief Class for storing the information needed in a node of an ADT.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/adt/CADTPointsOnlyClass.hpp b/Common/include/adt/CADTPointsOnlyClass.hpp
index 7d73582b6a5..8157a9c92d9 100644
--- a/Common/include/adt/CADTPointsOnlyClass.hpp
+++ b/Common/include/adt/CADTPointsOnlyClass.hpp
@@ -2,7 +2,7 @@
  * \file CADTPointsOnlyClass.hpp
  * \brief Class for storing an ADT of only points in an arbitrary number of dimensions.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/adt/CBBoxTargetClass.hpp b/Common/include/adt/CBBoxTargetClass.hpp
index 27d539b0660..3e294ad765d 100644
--- a/Common/include/adt/CBBoxTargetClass.hpp
+++ b/Common/include/adt/CBBoxTargetClass.hpp
@@ -3,7 +3,7 @@
  * \brief Class for storing the information of a possible bounding box candidate
            during a minimum distance search.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -35,7 +35,7 @@
  * \brief  Class for storing the information of a possible bounding box candidate
            during a minimum distance search.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 struct CBBoxTargetClass {
 
diff --git a/Common/include/basic_types/ad_structure.hpp b/Common/include/basic_types/ad_structure.hpp
index 27e7946a622..b03660f9d5f 100644
--- a/Common/include/basic_types/ad_structure.hpp
+++ b/Common/include/basic_types/ad_structure.hpp
@@ -2,7 +2,7 @@
  * \file ad_structure.hpp
  * \brief Main routines for the algorithmic differentiation (AD) structure.
  * \author T. Albring, J. Blühdorn
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/basic_types/datatype_structure.hpp b/Common/include/basic_types/datatype_structure.hpp
index 8b708830820..5abca7ead4a 100644
--- a/Common/include/basic_types/datatype_structure.hpp
+++ b/Common/include/basic_types/datatype_structure.hpp
@@ -2,7 +2,7 @@
  * \file datatype_structure.hpp
  * \brief Headers for generalized datatypes, defines an interface for AD types.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/code_config.hpp b/Common/include/code_config.hpp
index 7bb34cffbdb..1a58061896c 100644
--- a/Common/include/code_config.hpp
+++ b/Common/include/code_config.hpp
@@ -2,7 +2,7 @@
  * \file code_config.hpp
  * \brief Header file for collecting common macros, definitions and type configurations.
  * \author T. Albring, P. Gomes, J. Blühdorn
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/containers/C2DContainer.hpp b/Common/include/containers/C2DContainer.hpp
index 5ad79a52d70..5230a5a7b65 100644
--- a/Common/include/containers/C2DContainer.hpp
+++ b/Common/include/containers/C2DContainer.hpp
@@ -2,7 +2,7 @@
  * \file C2DContainer.hpp
  * \brief A templated vector/matrix object.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/containers/CFastFindAndEraseQueue.hpp b/Common/include/containers/CFastFindAndEraseQueue.hpp
index d021fe62bc7..b612bf745be 100644
--- a/Common/include/containers/CFastFindAndEraseQueue.hpp
+++ b/Common/include/containers/CFastFindAndEraseQueue.hpp
@@ -3,7 +3,7 @@
  * \brief A queue-type container (push back, pop front), but with
  *        fast deletion of arbitrary items (possibly in the middle).
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/containers/CFileReaderLUT.hpp b/Common/include/containers/CFileReaderLUT.hpp
index a000b2ddc60..fd3c93c7dfd 100644
--- a/Common/include/containers/CFileReaderLUT.hpp
+++ b/Common/include/containers/CFileReaderLUT.hpp
@@ -2,7 +2,7 @@
  * \file CFileReaderLUT.hpp
  * \brief reading lookup table for tabulated fluid properties
  * \author D. Mayer, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/containers/CLookUpTable.hpp b/Common/include/containers/CLookUpTable.hpp
index ecb59c97aa1..8e3a720d75d 100644
--- a/Common/include/containers/CLookUpTable.hpp
+++ b/Common/include/containers/CLookUpTable.hpp
@@ -2,7 +2,7 @@
  * \file CLookupTable.hpp
  * \brief tabulation of fluid properties
  * \author D. Mayer, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/containers/CTrapezoidalMap.hpp b/Common/include/containers/CTrapezoidalMap.hpp
index 284c2c9d88a..e67b43fbebf 100644
--- a/Common/include/containers/CTrapezoidalMap.hpp
+++ b/Common/include/containers/CTrapezoidalMap.hpp
@@ -2,7 +2,7 @@
  * \file CTrapezoidalMap.hpp
  * \brief Implementation of the trapezoidal map for tabulation and lookup of fluid properties
  * \author D. Mayer, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -38,7 +38,7 @@
  * \ingroup LookUpInterp
  * \brief Construction of trapezoidal map for tabulated lookup 
  * \author: D. Mayer, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
   class CTrapezoidalMap {
  protected:
diff --git a/Common/include/containers/CVertexMap.hpp b/Common/include/containers/CVertexMap.hpp
index 46975b3bc62..d3d0134525a 100644
--- a/Common/include/containers/CVertexMap.hpp
+++ b/Common/include/containers/CVertexMap.hpp
@@ -2,7 +2,7 @@
  * \file CVertexMap.hpp
  * \brief An index to index lookup vector.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/containers/container_decorators.hpp b/Common/include/containers/container_decorators.hpp
index da40ee702b3..b3c1c2a08d4 100644
--- a/Common/include/containers/container_decorators.hpp
+++ b/Common/include/containers/container_decorators.hpp
@@ -3,7 +3,7 @@
  * \brief Collection of small classes that decorate C2DContainer to
  * augment its functionality, e.g. give it extra dimensions.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/fem/fem_cgns_elements.hpp b/Common/include/fem/fem_cgns_elements.hpp
index a42a78ddcfb..de8ed3d8757 100644
--- a/Common/include/fem/fem_cgns_elements.hpp
+++ b/Common/include/fem/fem_cgns_elements.hpp
@@ -4,7 +4,7 @@
  *        with high order elements.
  *        The functions are in the <i>cgns_elements.cpp</i> file.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/fem/fem_gauss_jacobi_quadrature.hpp b/Common/include/fem/fem_gauss_jacobi_quadrature.hpp
index c05261a4b32..8f5cfa06810 100644
--- a/Common/include/fem/fem_gauss_jacobi_quadrature.hpp
+++ b/Common/include/fem/fem_gauss_jacobi_quadrature.hpp
@@ -6,7 +6,7 @@
           All the functions in this class are based on the program JACOBI_RULE
           of John Burkardt.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -95,7 +95,7 @@ using namespace std;
  * \brief Class used to determine the quadrature points of the Gauss Jacobi
           integration rules.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CGaussJacobiQuadrature {
 public:
diff --git a/Common/include/fem/fem_geometry_structure.hpp b/Common/include/fem/fem_geometry_structure.hpp
index 8674fe6f451..d90a4a05c12 100644
--- a/Common/include/fem/fem_geometry_structure.hpp
+++ b/Common/include/fem/fem_geometry_structure.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for creating the geometrical structure for the FEM solver.
  *        The subroutines and functions are in the <i>fem_geometry_structure.cpp</i> file.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -41,7 +41,7 @@ using namespace std;
 /*!
  * \class CLong3T
  * \brief Help class used to store three longs as one entity.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 struct CLong3T {
   long long0 = 0;  /*!< \brief First long to store in this class. */
@@ -59,7 +59,7 @@ struct CLong3T {
  * \class CReorderElements
  * \brief Class, used to reorder the owned elements after the partitioning.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CReorderElements {
 private:
@@ -131,7 +131,7 @@ class CReorderElements {
  * \brief Functor, used for a different sorting of the faces than the < operator
  *        of CFaceOfElement.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CVolumeElementFEM;   // Forward declaration to avoid problems.
 class CSortFaces {
@@ -172,7 +172,7 @@ class CSortFaces {
  * \brief Functor, used for a different sorting of the faces than the < operator
  *        of CSurfaceElementFEM.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 struct CSurfaceElementFEM;   // Forward declaration to avoid problems.
 struct CSortBoundaryFaces {
@@ -189,7 +189,7 @@ struct CSortBoundaryFaces {
  * \class CVolumeElementFEM
  * \brief Class to store a volume element for the FEM solver.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CVolumeElementFEM {
 public:
@@ -283,7 +283,7 @@ class CVolumeElementFEM {
  * \class CPointFEM
  * \brief Class to a point for the FEM solver.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 struct CPointFEM {
   unsigned long globalID;    /*!< \brief The global ID of this point in the grid. */
@@ -308,7 +308,7 @@ struct CPointFEM {
  * \class CInternalFaceElementFEM
  * \brief Class to store an internal face for the FEM solver.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 struct CInternalFaceElementFEM {
   unsigned short VTK_Type;     /*!< \brief Element type using the VTK convention. */
@@ -353,7 +353,7 @@ struct CInternalFaceElementFEM {
  * \class CSurfaceElementFEM
  * \brief Class to store a surface element for the FEM solver.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 struct CSurfaceElementFEM {
   unsigned short VTK_Type;     /*!< \brief Element type using the VTK convention. */
@@ -415,7 +415,7 @@ struct CSurfaceElementFEM {
  * \class CBoundaryFEM
  * \brief Class to store a boundary for the FEM solver.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 struct CBoundaryFEM {
   string markerTag;  /*!< \brief Marker tag of this boundary. */
@@ -438,7 +438,7 @@ struct CBoundaryFEM {
  * \class CMeshFEM
  * \brief Base class for the FEM solver.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CMeshFEM: public CGeometry {
 protected:
@@ -712,7 +712,7 @@ class CMeshFEM: public CGeometry {
  * \class CMeshFEM_DG
  * \brief Class which contains all the variables for the DG FEM solver.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CMeshFEM_DG: public CMeshFEM {
 protected:
diff --git a/Common/include/fem/fem_standard_element.hpp b/Common/include/fem/fem_standard_element.hpp
index b275b3ec027..727edc20e1e 100644
--- a/Common/include/fem/fem_standard_element.hpp
+++ b/Common/include/fem/fem_standard_element.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main functions for the FEM standard elements.
  *        The functions are in the <i>fem_standard_element.cpp</i> file.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -40,7 +40,7 @@ using namespace std;
  * \class CFEMStandardElementBase
  * \brief Base class for a FEM standard element.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CFEMStandardElementBase {
 protected:
@@ -781,7 +781,7 @@ class CFEMStandardElementBase {
  * \class CFEMStandardElement
  * \brief Class to define a FEM standard element.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CFEMStandardElement : public CFEMStandardElementBase {
 private:
@@ -1220,7 +1220,7 @@ class CFEMStandardElement : public CFEMStandardElementBase {
  * \class CFEMStandardInternalFace
  * \brief Class to define a FEM standard internal face.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CFEMStandardInternalFace : public CFEMStandardElementBase {
 private:
@@ -1546,7 +1546,7 @@ class CFEMStandardInternalFace : public CFEMStandardElementBase {
  * \class CFEMStandardBoundaryFace
  * \brief Class to define a FEM standard boundary face.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CFEMStandardBoundaryFace : public CFEMStandardElementBase {
 private:
diff --git a/Common/include/fem/geometry_structure_fem_part.hpp b/Common/include/fem/geometry_structure_fem_part.hpp
index 52d46439035..d39ca499a41 100644
--- a/Common/include/fem/geometry_structure_fem_part.hpp
+++ b/Common/include/fem/geometry_structure_fem_part.hpp
@@ -2,7 +2,7 @@
  * \file geometry_structure_fem_part.hpp
  * \brief Helper classes for the Fluid FEM solver.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/CDummyGeometry.hpp b/Common/include/geometry/CDummyGeometry.hpp
index 39200d39d5f..7ceb1788df0 100644
--- a/Common/include/geometry/CDummyGeometry.hpp
+++ b/Common/include/geometry/CDummyGeometry.hpp
@@ -2,7 +2,7 @@
  * \file CDummyGeometry.hpp
  * \brief Headers of the dummy geometry class used in "dry run" mode.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/CGeometry.hpp b/Common/include/geometry/CGeometry.hpp
index cfcc6d237f3..c5ffdb5cf7b 100644
--- a/Common/include/geometry/CGeometry.hpp
+++ b/Common/include/geometry/CGeometry.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for creating the geometrical structure.
  *        The subroutines and functions are in the <i>CGeometry.cpp</i> file.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -28,6 +28,7 @@
 
 #pragma once
 
+#include <limits>
 #include "../parallelization/mpi_structure.hpp"
 
 #ifdef HAVE_METIS
@@ -72,7 +73,7 @@ using namespace std;
  * \author F. Palacios
  */
 class CGeometry {
-protected:
+ protected:
   enum : size_t {OMP_MIN_SIZE = 32}; /*!< \brief Chunk size for small loops. */
   enum : size_t {MAXNDIM = 3};
 
@@ -186,7 +187,30 @@ class CGeometry {
 
   ColMajorMatrix<uint8_t> CoarseGridColor_;  /*!< \brief Coarse grid levels, colorized. */
 
-public:
+ public:
+  /*!< \brief Linelets (mesh lines perpendicular to stretching direction). */
+  struct CLineletInfo {
+    /*!< \brief Detect isotropic mesh region. */
+    static passivedouble ALPHA_ISOTROPIC() { return 0.8; }
+    enum : unsigned long {MAX_LINELET_POINTS = 32}; /*!< \brief Maximum points per linelet. */
+
+    std::vector<std::vector<unsigned long>> linelets; /*!< \brief Point indices for each linelet. */
+
+    /*!< \brief Index of the linelet of each point ("linelets" transfered to points). */
+    std::vector<unsigned> lineletIdx;
+
+    /*!< \brief Signals that a point is not on a linelet. */
+    enum : unsigned {NO_LINELET = std::numeric_limits<unsigned>::max()};
+
+    /*!< \brief Coloring for OpenMP parallelization, "linelets" is sorted by color. */
+    std::vector<unsigned long> colorOffsets;
+
+    std::vector<uint8_t> lineletColor;  /*!< \brief Coloring transfered to points, for visualization. */
+  };
+ protected:
+  mutable CLineletInfo lineletInfo;
+
+ public:
   /*--- Main geometric elements of the grid. ---*/
 
   CPrimalGrid** elem{nullptr};           /*!< \brief Element vector (primal grid information). */
@@ -1658,6 +1682,11 @@ class CGeometry {
    */
   inline unsigned long GetElementColorGroupSize() const { return elemColorGroupSize; }
 
+  /*!
+   * \brief Get the linelet definition, this function computes the linelets if that has not been done yet.
+   */
+  const CLineletInfo& GetLineletInfo(const CConfig* config) const;
+
   /*!
    * \brief Compute an ADT including the coordinates of all viscous markers
    * \param[in] config - Definition of the particular problem.
diff --git a/Common/include/geometry/CMultiGridGeometry.hpp b/Common/include/geometry/CMultiGridGeometry.hpp
index 3473356d68f..375974fe1d5 100644
--- a/Common/include/geometry/CMultiGridGeometry.hpp
+++ b/Common/include/geometry/CMultiGridGeometry.hpp
@@ -2,7 +2,7 @@
  * \file CMultiGridGeometry.hpp
  * \brief Headers of the multigrid geometry class.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/CMultiGridQueue.hpp b/Common/include/geometry/CMultiGridQueue.hpp
index b6006ce6d28..e74667d865f 100644
--- a/Common/include/geometry/CMultiGridQueue.hpp
+++ b/Common/include/geometry/CMultiGridQueue.hpp
@@ -3,7 +3,7 @@
  * \brief Header of the multigrid queue class for the FVM solver.
  *        The subroutines and functions are in the <i>CMultiGridQueue.cpp</i> file.
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/CPhysicalGeometry.hpp b/Common/include/geometry/CPhysicalGeometry.hpp
index 3a23507f2c3..a82abaeab91 100644
--- a/Common/include/geometry/CPhysicalGeometry.hpp
+++ b/Common/include/geometry/CPhysicalGeometry.hpp
@@ -2,7 +2,7 @@
  * \file CPhysicalGeometry.hpp
  * \brief Headers of the physical geometry class used to read meshes from file.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/dual_grid/CDualGrid.hpp b/Common/include/geometry/dual_grid/CDualGrid.hpp
index 7d686be406c..07b08a2aa5f 100644
--- a/Common/include/geometry/dual_grid/CDualGrid.hpp
+++ b/Common/include/geometry/dual_grid/CDualGrid.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for doing the complete dual grid structure.
  *        The subroutines and functions are in the <i>CDualGrid.cpp</i> file.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/dual_grid/CEdge.hpp b/Common/include/geometry/dual_grid/CEdge.hpp
index 98310c94c97..657021fb848 100644
--- a/Common/include/geometry/dual_grid/CEdge.hpp
+++ b/Common/include/geometry/dual_grid/CEdge.hpp
@@ -2,7 +2,7 @@
  * \file CEdge.hpp
  * \brief Declaration of the edge class <i>CEdge.cpp</i> file.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/dual_grid/CPoint.hpp b/Common/include/geometry/dual_grid/CPoint.hpp
index ec27487896c..b5750ddb4d2 100644
--- a/Common/include/geometry/dual_grid/CPoint.hpp
+++ b/Common/include/geometry/dual_grid/CPoint.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration of the point class that stores geometric and adjacency
  *        information for dual control volumes.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/dual_grid/CTurboVertex.hpp b/Common/include/geometry/dual_grid/CTurboVertex.hpp
index 0fb66e5f4c5..7f10e08f4b8 100644
--- a/Common/include/geometry/dual_grid/CTurboVertex.hpp
+++ b/Common/include/geometry/dual_grid/CTurboVertex.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for doing the complete dual grid structure.
  *        The subroutines and functions are in the <i>CTurboVertex.cpp</i> file.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/dual_grid/CVertex.hpp b/Common/include/geometry/dual_grid/CVertex.hpp
index a53be9453c6..e280a4303bc 100644
--- a/Common/include/geometry/dual_grid/CVertex.hpp
+++ b/Common/include/geometry/dual_grid/CVertex.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for doing the complete dual grid structure.
  *        The subroutines and functions are in the <i>CVertex.cpp</i> file.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/elements/CElement.hpp b/Common/include/geometry/elements/CElement.hpp
index 9b34b73935a..87825a9f6ff 100644
--- a/Common/include/geometry/elements/CElement.hpp
+++ b/Common/include/geometry/elements/CElement.hpp
@@ -3,7 +3,7 @@
  * \brief Main header of the Finite Element structure declaring the abstract
  *        interface and the available finite element types.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -952,7 +952,7 @@ class CPYRAM5 final : public CElementWithKnownSizes<5,5,3> {
  * \ingroup FemAlgos
  * \brief Prism element with 6 Gauss Points
  * \author R. Sanchez, F. Palacios, A. Bueno, T. Economon, S. Padron.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CPRISM6 final : public CElementWithKnownSizes<6,6,3> {
 private:
diff --git a/Common/include/geometry/elements/CElementProperty.hpp b/Common/include/geometry/elements/CElementProperty.hpp
index 380eb55e677..2fb9408de4d 100644
--- a/Common/include/geometry/elements/CElementProperty.hpp
+++ b/Common/include/geometry/elements/CElementProperty.hpp
@@ -2,7 +2,7 @@
  * \file CElementProperty.hpp
  * \brief Light classes to define finite element properties.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -32,7 +32,7 @@
  * \ingroup Elasticity_Equations
  * \brief Base class for defining element properties.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CProperty {
 protected:
@@ -108,7 +108,7 @@ class CProperty {
  * \ingroup Elasticity_Equations
  * \brief Class for defining element properties for the structural solver.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CElementProperty final : public CProperty {
 private:
diff --git a/Common/include/geometry/elements/CGaussVariable.hpp b/Common/include/geometry/elements/CGaussVariable.hpp
index 235ae4eb6d4..8036543e266 100644
--- a/Common/include/geometry/elements/CGaussVariable.hpp
+++ b/Common/include/geometry/elements/CGaussVariable.hpp
@@ -2,7 +2,7 @@
  * \file CGaussVariable.hpp
  * \brief Light-weight class to store Gaussian point information.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -33,7 +33,7 @@
  * \class CGaussVariable
  * \ingroup FemAlgos
  * \brief Main class for defining the gaussian points.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CGaussVariable {
 protected:
diff --git a/Common/include/geometry/meshreader/CBoxMeshReaderFVM.hpp b/Common/include/geometry/meshreader/CBoxMeshReaderFVM.hpp
index 00fb18a02fb..5b345bd348c 100644
--- a/Common/include/geometry/meshreader/CBoxMeshReaderFVM.hpp
+++ b/Common/include/geometry/meshreader/CBoxMeshReaderFVM.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CBoxMeshReaderFVM.
  *        The implementations are in the <i>CBoxMeshReaderFVM.cpp</i> file.
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/meshreader/CCGNSMeshReaderFVM.hpp b/Common/include/geometry/meshreader/CCGNSMeshReaderFVM.hpp
index 3b27f63f74d..358f9e36d43 100644
--- a/Common/include/geometry/meshreader/CCGNSMeshReaderFVM.hpp
+++ b/Common/include/geometry/meshreader/CCGNSMeshReaderFVM.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CCGNSMeshReaderFVM.
  *        The implementations are in the <i>CCGNSMeshReaderFVM.cpp</i> file.
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/meshreader/CMeshReaderFVM.hpp b/Common/include/geometry/meshreader/CMeshReaderFVM.hpp
index 477c1de077c..c812c73bae9 100644
--- a/Common/include/geometry/meshreader/CMeshReaderFVM.hpp
+++ b/Common/include/geometry/meshreader/CMeshReaderFVM.hpp
@@ -4,7 +4,7 @@
  * \brief Header file for the class CMeshReaderFVM.
  *        The implementations are in the <i>CMeshReaderFVM.cpp</i> file.
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/meshreader/CRectangularMeshReaderFVM.hpp b/Common/include/geometry/meshreader/CRectangularMeshReaderFVM.hpp
index 0a7f42db09a..ea225bc46fc 100644
--- a/Common/include/geometry/meshreader/CRectangularMeshReaderFVM.hpp
+++ b/Common/include/geometry/meshreader/CRectangularMeshReaderFVM.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CRectangularMeshReaderFVM.
  *        The implementations are in the <i>CRectangularMeshReaderFVM.cpp</i> file.
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/meshreader/CSU2ASCIIMeshReaderFVM.hpp b/Common/include/geometry/meshreader/CSU2ASCIIMeshReaderFVM.hpp
index 2bc0aacd8e1..5302a1ec06c 100644
--- a/Common/include/geometry/meshreader/CSU2ASCIIMeshReaderFVM.hpp
+++ b/Common/include/geometry/meshreader/CSU2ASCIIMeshReaderFVM.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CSU2ASCIIMeshReaderFVM.
  *        The implementations are in the <i>CSU2ASCIIMeshReaderFVM.cpp</i> file.
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/primal_grid/CHexahedron.hpp b/Common/include/geometry/primal_grid/CHexahedron.hpp
index c44500810b2..7683791ab76 100644
--- a/Common/include/geometry/primal_grid/CHexahedron.hpp
+++ b/Common/include/geometry/primal_grid/CHexahedron.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for storing the primal grid structure.
  *        The subroutines and functions are in the <i>CHexahedron.cpp</i> file.
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/primal_grid/CLine.hpp b/Common/include/geometry/primal_grid/CLine.hpp
index 01dc25324ea..4c0b7a0fd97 100644
--- a/Common/include/geometry/primal_grid/CLine.hpp
+++ b/Common/include/geometry/primal_grid/CLine.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for storing the primal grid structure.
  *        The subroutines and functions are in the <i>CLine.cpp</i> file.
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/primal_grid/CPrimalGrid.hpp b/Common/include/geometry/primal_grid/CPrimalGrid.hpp
index 8ad0c4056b4..9f169b3e120 100644
--- a/Common/include/geometry/primal_grid/CPrimalGrid.hpp
+++ b/Common/include/geometry/primal_grid/CPrimalGrid.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for storing the primal grid structure.
  *        The subroutines and functions are in the <i>primal_grid_structure.cpp</i> file.
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/primal_grid/CPrimalGridBoundFEM.hpp b/Common/include/geometry/primal_grid/CPrimalGridBoundFEM.hpp
index f078974c59e..e0a4f7809f1 100644
--- a/Common/include/geometry/primal_grid/CPrimalGridBoundFEM.hpp
+++ b/Common/include/geometry/primal_grid/CPrimalGridBoundFEM.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for storing the primal grid structure.
  *        The subroutines and functions are in the <i>CPrimalGridBoundFEM.cpp</i> file.
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -33,7 +33,7 @@
 /*!
  * \class CPrimalGridBoundFEM
  * \brief Class to define primal grid boundary element for the FEM solver.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CPrimalGridBoundFEM final: public CPrimalGrid {
 private:
diff --git a/Common/include/geometry/primal_grid/CPrimalGridFEM.hpp b/Common/include/geometry/primal_grid/CPrimalGridFEM.hpp
index 773783be452..539c5ac29b1 100644
--- a/Common/include/geometry/primal_grid/CPrimalGridFEM.hpp
+++ b/Common/include/geometry/primal_grid/CPrimalGridFEM.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for storing the primal grid structure.
  *        The subroutines and functions are in the <i>CPrimalGridFEM.cpp</i> file.
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -34,7 +34,7 @@
 /*!
  * \class CPrimalGridFEM
  * \brief Class to define primal grid element for the FEM solver.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CPrimalGridFEM final: public CPrimalGrid {
 private:
diff --git a/Common/include/geometry/primal_grid/CPrism.hpp b/Common/include/geometry/primal_grid/CPrism.hpp
index 64782bf867b..45f36344e5f 100644
--- a/Common/include/geometry/primal_grid/CPrism.hpp
+++ b/Common/include/geometry/primal_grid/CPrism.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for storing the primal grid structure.
  *        The subroutines and functions are in the <i>CPrism.cpp</i> file.
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/primal_grid/CPyramid.hpp b/Common/include/geometry/primal_grid/CPyramid.hpp
index ed909b48b37..1b3c326a177 100644
--- a/Common/include/geometry/primal_grid/CPyramid.hpp
+++ b/Common/include/geometry/primal_grid/CPyramid.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for storing the primal grid structure.
  *        The subroutines and functions are in the <i>CPyramid.cpp</i> file.
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/primal_grid/CQuadrilateral.hpp b/Common/include/geometry/primal_grid/CQuadrilateral.hpp
index 1de14f32e27..512dd0e8702 100644
--- a/Common/include/geometry/primal_grid/CQuadrilateral.hpp
+++ b/Common/include/geometry/primal_grid/CQuadrilateral.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for storing the primal grid structure.
  *        The subroutines and functions are in the <i>CQuadrilateral.cpp</i> file.
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/primal_grid/CTetrahedron.hpp b/Common/include/geometry/primal_grid/CTetrahedron.hpp
index 0999dc1287d..eb09b738514 100644
--- a/Common/include/geometry/primal_grid/CTetrahedron.hpp
+++ b/Common/include/geometry/primal_grid/CTetrahedron.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for storing the primal grid structure.
  *        The subroutines and functions are in the <i>CTetrahedron.cpp</i> file.
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/primal_grid/CTriangle.hpp b/Common/include/geometry/primal_grid/CTriangle.hpp
index 67d3b397a47..b1a67a7c6e7 100644
--- a/Common/include/geometry/primal_grid/CTriangle.hpp
+++ b/Common/include/geometry/primal_grid/CTriangle.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for storing the primal grid structure.
  *        The subroutines and functions are in the <i>CTriangle.cpp</i> file.
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/primal_grid/CVertexMPI.hpp b/Common/include/geometry/primal_grid/CVertexMPI.hpp
index adb2fa44d9b..4b9691a324e 100644
--- a/Common/include/geometry/primal_grid/CVertexMPI.hpp
+++ b/Common/include/geometry/primal_grid/CVertexMPI.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for storing the primal grid structure.
  *        The subroutines and functions are in the <i>primal_grid_structure.cpp</i> file.
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/graph_coloring_structure.hpp b/Common/include/graph_coloring_structure.hpp
index 197c01baa28..69fb47cc5e8 100644
--- a/Common/include/graph_coloring_structure.hpp
+++ b/Common/include/graph_coloring_structure.hpp
@@ -4,7 +4,7 @@
  *        coloring of a given graph. The functions are in the
  *        <i>graph_coloring_structure.cpp</i> file.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -41,7 +41,7 @@ using namespace std;
  * \ingroup Graph
  * \brief Class, which provides distributed graph coloring algorithms.
  * \author: E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CGraphColoringStructure {
 public:
diff --git a/Common/include/grid_movement/CBSplineBlending.hpp b/Common/include/grid_movement/CBSplineBlending.hpp
index 8937929e390..3d09ce98468 100644
--- a/Common/include/grid_movement/CBSplineBlending.hpp
+++ b/Common/include/grid_movement/CBSplineBlending.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the CBSplineBlending class.
  *        Defines blending using uniform BSplines
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/grid_movement/CBezierBlending.hpp b/Common/include/grid_movement/CBezierBlending.hpp
index 08d3fb07f60..042292eb908 100644
--- a/Common/include/grid_movement/CBezierBlending.hpp
+++ b/Common/include/grid_movement/CBezierBlending.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the CBezierBlending class.
  *        Defines blending using Bernsteinpolynomials (Bezier Curves)
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/grid_movement/CFreeFormBlending.hpp b/Common/include/grid_movement/CFreeFormBlending.hpp
index e52e41114a2..0c6edf54686 100644
--- a/Common/include/grid_movement/CFreeFormBlending.hpp
+++ b/Common/include/grid_movement/CFreeFormBlending.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the CFreeFormBlending class.
  *        It is the parent class for the FFD blending function
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/grid_movement/CFreeFormDefBox.hpp b/Common/include/grid_movement/CFreeFormDefBox.hpp
index 65bbfb17ba3..745f8a4bb6c 100644
--- a/Common/include/grid_movement/CFreeFormDefBox.hpp
+++ b/Common/include/grid_movement/CFreeFormDefBox.hpp
@@ -2,7 +2,7 @@
  * \file CFreeFormDefBox.hpp
  * \brief Headers of the CFreeFormDefBox class.
  * \author F. Palacios & A. Galdran.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/grid_movement/CGridMovement.hpp b/Common/include/grid_movement/CGridMovement.hpp
index 2b312232f59..6ab5792c413 100644
--- a/Common/include/grid_movement/CGridMovement.hpp
+++ b/Common/include/grid_movement/CGridMovement.hpp
@@ -2,7 +2,7 @@
  * \file CGridMovement.hpp
  * \brief Headers of the CGridMovement class
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/grid_movement/CSurfaceMovement.hpp b/Common/include/grid_movement/CSurfaceMovement.hpp
index 48a356626c4..c6b6198b4a9 100644
--- a/Common/include/grid_movement/CSurfaceMovement.hpp
+++ b/Common/include/grid_movement/CSurfaceMovement.hpp
@@ -2,7 +2,7 @@
  * \file CSurfaceMovement.hpp
  * \brief Headers of the CSurfaceMovement class.
  * \author F. Palacios, T. Economon.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/grid_movement/CVolumetricMovement.hpp b/Common/include/grid_movement/CVolumetricMovement.hpp
index 0e31f34970c..0be1b93d65e 100644
--- a/Common/include/grid_movement/CVolumetricMovement.hpp
+++ b/Common/include/grid_movement/CVolumetricMovement.hpp
@@ -2,7 +2,7 @@
  * \file CVolumetricMovement.hpp
  * \brief Headers of the CVolumetricMovement class.
  * \author F. Palacios, A. Bueno, T. Economon, S. Padron.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/interface_interpolation/CInterpolator.hpp b/Common/include/interface_interpolation/CInterpolator.hpp
index f4aa4fd71a3..a398cd7679c 100644
--- a/Common/include/interface_interpolation/CInterpolator.hpp
+++ b/Common/include/interface_interpolation/CInterpolator.hpp
@@ -2,7 +2,7 @@
  * \file CInterpolator.hpp
  * \brief Base class for multiphysics interpolation.
  * \author H. Kline
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/interface_interpolation/CInterpolatorFactory.hpp b/Common/include/interface_interpolation/CInterpolatorFactory.hpp
index 922bb647b13..c1531e95dea 100644
--- a/Common/include/interface_interpolation/CInterpolatorFactory.hpp
+++ b/Common/include/interface_interpolation/CInterpolatorFactory.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file CInterpolatorFactory.hpp
  * \brief Factory to generate interpolator objects.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/interface_interpolation/CIsoparametric.hpp b/Common/include/interface_interpolation/CIsoparametric.hpp
index bf43b5990ec..8f357061985 100644
--- a/Common/include/interface_interpolation/CIsoparametric.hpp
+++ b/Common/include/interface_interpolation/CIsoparametric.hpp
@@ -2,7 +2,7 @@
  * \file CIsoparametric.hpp
  * \brief Isoparametric interpolation using FE shape functions.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/interface_interpolation/CMirror.hpp b/Common/include/interface_interpolation/CMirror.hpp
index d537f3c12b9..8a6d9ad3541 100644
--- a/Common/include/interface_interpolation/CMirror.hpp
+++ b/Common/include/interface_interpolation/CMirror.hpp
@@ -2,7 +2,7 @@
  * \file CMirror.hpp
  * \brief Mirror interpolation for the conservative (work-wise) approach in FSI problems.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/interface_interpolation/CNearestNeighbor.hpp b/Common/include/interface_interpolation/CNearestNeighbor.hpp
index 437218f60af..732a511fe84 100644
--- a/Common/include/interface_interpolation/CNearestNeighbor.hpp
+++ b/Common/include/interface_interpolation/CNearestNeighbor.hpp
@@ -2,7 +2,7 @@
  * \file CNearestNeighbor.hpp
  * \brief Nearest Neighbor interpolation class.
  * \author H. Kline
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/interface_interpolation/CRadialBasisFunction.hpp b/Common/include/interface_interpolation/CRadialBasisFunction.hpp
index 9f9d3d957fc..4a53ace572e 100644
--- a/Common/include/interface_interpolation/CRadialBasisFunction.hpp
+++ b/Common/include/interface_interpolation/CRadialBasisFunction.hpp
@@ -2,7 +2,7 @@
  * \file CRadialBasisFunction.hpp
  * \brief Radial basis function interpolation.
  * \author Joel Ho, P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/interface_interpolation/CSlidingMesh.hpp b/Common/include/interface_interpolation/CSlidingMesh.hpp
index df7eef3ae04..770733c3665 100644
--- a/Common/include/interface_interpolation/CSlidingMesh.hpp
+++ b/Common/include/interface_interpolation/CSlidingMesh.hpp
@@ -2,7 +2,7 @@
  * \file CSlidingMesh.hpp
  * \brief Sliding mesh interpolation.
  * \author H. Kline
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/linear_algebra/CMatrixVectorProduct.hpp b/Common/include/linear_algebra/CMatrixVectorProduct.hpp
index 5b851f3ab3d..577f74aa3db 100644
--- a/Common/include/linear_algebra/CMatrixVectorProduct.hpp
+++ b/Common/include/linear_algebra/CMatrixVectorProduct.hpp
@@ -3,7 +3,7 @@
  * \brief Headers for the classes related to sparse matrix-vector product wrappers.
  *        The actual operations are currently implemented mostly by CSysMatrix.
  * \author F. Palacios, J. Hicken, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/linear_algebra/CPastixWrapper.hpp b/Common/include/linear_algebra/CPastixWrapper.hpp
index 82dd0c0c4f4..fb40c40d7df 100644
--- a/Common/include/linear_algebra/CPastixWrapper.hpp
+++ b/Common/include/linear_algebra/CPastixWrapper.hpp
@@ -3,7 +3,7 @@
  * \brief An interface to the INRIA solver PaStiX
  *        (http://pastix.gforge.inria.fr/files/README-txt.html)
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/linear_algebra/CPreconditioner.hpp b/Common/include/linear_algebra/CPreconditioner.hpp
index 722e8e312aa..2ca619c11dd 100644
--- a/Common/include/linear_algebra/CPreconditioner.hpp
+++ b/Common/include/linear_algebra/CPreconditioner.hpp
@@ -3,7 +3,7 @@
  * \brief Classes related to linear preconditioner wrappers.
  *        The actual operations are currently implemented mostly by CSysMatrix.
  * \author F. Palacios, J. Hicken, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -270,7 +270,7 @@ class CLineletPreconditioner final : public CPreconditioner<ScalarType> {
    * \note Request the associated matrix to build the preconditioner.
    */
   inline void Build() override {
-    sparse_matrix.BuildJacobiPreconditioner();
+    sparse_matrix.BuildLineletPreconditioner(geometry, config);
   }
 };
 
diff --git a/Common/include/linear_algebra/CSysMatrix.hpp b/Common/include/linear_algebra/CSysMatrix.hpp
index 230328451c9..c05ff216f19 100644
--- a/Common/include/linear_algebra/CSysMatrix.hpp
+++ b/Common/include/linear_algebra/CSysMatrix.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration of the block-sparse matrix class.
  *        The implemtation is in <i>CSysMatrix.cpp</i>.
  * \author F. Palacios, A. Bueno, T. Economon, P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -148,10 +148,6 @@ class CSysMatrix {
 
   ScalarType *invM;                 /*!< \brief Inverse of (Jacobi) preconditioner, or diagonal of ILU. */
 
-  unsigned long nLinelet;                      /*!< \brief Number of Linelets in the system. */
-  vector<bool> LineletBool;                    /*!< \brief Identify if a point belong to a Linelet. */
-  vector<vector<unsigned long> > LineletPoint; /*!< \brief Linelet structure. */
-
   /*--- Temporary (hence mutable) working memory used in the Linelet preconditioner, outer vector is for threads ---*/
   mutable vector<vector<const ScalarType*> > LineletUpper; /*!< \brief Pointers to the upper blocks of the tri-diag system (working memory). */
   mutable vector<vector<ScalarType> > LineletInvDiag;      /*!< \brief Inverse of the diagonal blocks of the tri-diag system (working memory). */
@@ -886,9 +882,8 @@ class CSysMatrix {
    * \brief Build the Linelet preconditioner.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
-   * \return Average number of points per linelet.
    */
-  unsigned long BuildLineletPreconditioner(CGeometry *geometry, const CConfig *config);
+  void BuildLineletPreconditioner(const CGeometry *geometry, const CConfig *config);
 
   /*!
    * \brief Multiply CSysVector by the preconditioner
diff --git a/Common/include/linear_algebra/CSysMatrix.inl b/Common/include/linear_algebra/CSysMatrix.inl
index e280b0f07b1..435a6ba2675 100644
--- a/Common/include/linear_algebra/CSysMatrix.inl
+++ b/Common/include/linear_algebra/CSysMatrix.inl
@@ -5,7 +5,7 @@
  *       of the .cpp file and so they are hidden to avoid triggering
  *       recompilation of other units when changes are made here.
  * \author F. Palacios, A. Bueno, T. Economon, P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -192,7 +192,8 @@ FORCEINLINE void CSysMatrix<ScalarType>::UpperProduct(const CSysVector<ScalarTyp
 
   for (auto index = dia_ptr[row_i]+1; index < row_ptr[row_i+1]; index++) {
     auto col_j = col_ind[index];
-    if (col_j < col_ub)
+    /*--- Always include halos. ---*/
+    if (col_j < col_ub || col_j >= nPointDomain)
       MatrixVectorProductAdd(&matrix[index*nVar*nEqn], &vec[col_j*nEqn], prod);
   }
 }
diff --git a/Common/include/linear_algebra/CSysSolve.hpp b/Common/include/linear_algebra/CSysSolve.hpp
index 0007865bb03..104796599d0 100644
--- a/Common/include/linear_algebra/CSysSolve.hpp
+++ b/Common/include/linear_algebra/CSysSolve.hpp
@@ -3,7 +3,7 @@
  * \brief Headers for the classes related to linear solvers (CG, FGMRES, etc)
  *        The subroutines and functions are in the <i>CSysSolve.cpp</i> file.
  * \author J. Hicken, F. Palacios, T. Economon, P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/linear_algebra/CSysSolve_b.hpp b/Common/include/linear_algebra/CSysSolve_b.hpp
index eae9de62ad4..f7c16e34ddc 100644
--- a/Common/include/linear_algebra/CSysSolve_b.hpp
+++ b/Common/include/linear_algebra/CSysSolve_b.hpp
@@ -2,7 +2,7 @@
  * \file CSysSolve_b.hpp
  * \brief Routines for the linear solver used in the reverse sweep of AD.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/linear_algebra/CSysVector.hpp b/Common/include/linear_algebra/CSysVector.hpp
index c41cd4ce930..07af5d1d973 100644
--- a/Common/include/linear_algebra/CSysVector.hpp
+++ b/Common/include/linear_algebra/CSysVector.hpp
@@ -3,7 +3,7 @@
  * \brief Declararion and inlines of the vector class used in the
  * solution of large, distributed, sparse linear systems.
  * \author P. Gomes, F. Palacios, J. Hicken, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/linear_algebra/blas_structure.hpp b/Common/include/linear_algebra/blas_structure.hpp
index da1f57d2cbe..5e41da73450 100644
--- a/Common/include/linear_algebra/blas_structure.hpp
+++ b/Common/include/linear_algebra/blas_structure.hpp
@@ -4,7 +4,7 @@
           operations, which are typically found in the BLAS libraries.
           The functions are in the <i>blass_structure.cpp</i> file.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -41,7 +41,7 @@ class CConfig;
  * \ingroup BLAS
  * \brief Class, which serves as an interface to the BLAS functionalities needed.
  * \author: E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CBlasStructure {
 public:
diff --git a/Common/include/linear_algebra/vector_expressions.hpp b/Common/include/linear_algebra/vector_expressions.hpp
index a394e37426d..3a56ee45b2b 100644
--- a/Common/include/linear_algebra/vector_expressions.hpp
+++ b/Common/include/linear_algebra/vector_expressions.hpp
@@ -2,7 +2,7 @@
  * \file vector_expressions.hpp
  * \brief Expression templates for vector types with coefficient-wise operations.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index 152a3829d27..d39d6abde86 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -2,7 +2,7 @@
  * \file option_structure.hpp
  * \brief Defines classes for referencing options for easy input in CConfig
  * \author J. Hicken, B. Tracey
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -272,22 +272,8 @@ static const MapType<std::string, MAIN_SOLVER> Solver_Map = {
   MakePair("FEM_LES", MAIN_SOLVER::FEM_LES)
   MakePair("NEMO_EULER",MAIN_SOLVER::NEMO_EULER)
   MakePair("NEMO_NAVIER_STOKES",MAIN_SOLVER::NEMO_NAVIER_STOKES)
-  MakePair("ADJ_EULER", MAIN_SOLVER::ADJ_EULER)
-  MakePair("ADJ_NAVIER_STOKES", MAIN_SOLVER::ADJ_NAVIER_STOKES)
-  MakePair("ADJ_RANS", MAIN_SOLVER::ADJ_RANS )
   MakePair("HEAT_EQUATION", MAIN_SOLVER::HEAT_EQUATION)
   MakePair("ELASTICITY", MAIN_SOLVER::FEM_ELASTICITY)
-  MakePair("DISC_ADJ_EULER", MAIN_SOLVER::DISC_ADJ_EULER)
-  MakePair("DISC_ADJ_RANS", MAIN_SOLVER::DISC_ADJ_RANS)
-  MakePair("DISC_ADJ_NAVIERSTOKES", MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES)
-  MakePair("DISC_ADJ_INC_EULER", MAIN_SOLVER::DISC_ADJ_INC_EULER)
-  MakePair("DISC_ADJ_INC_RANS", MAIN_SOLVER::DISC_ADJ_INC_RANS)
-  MakePair("DISC_ADJ_INC_NAVIERSTOKES", MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES)
-  MakePair("DISC_ADJ_HEAT_EQUATION", MAIN_SOLVER::DISC_ADJ_HEAT)
-  MakePair("DISC_ADJ_FEM_EULER", MAIN_SOLVER::DISC_ADJ_FEM_EULER)
-  MakePair("DISC_ADJ_FEM_RANS", MAIN_SOLVER::DISC_ADJ_FEM_RANS)
-  MakePair("DISC_ADJ_FEM_NS", MAIN_SOLVER::DISC_ADJ_FEM_NS)
-  MakePair("DISC_ADJ_FEM", MAIN_SOLVER::DISC_ADJ_FEM)
   MakePair("TEMPLATE_SOLVER", MAIN_SOLVER::TEMPLATE_SOLVER)
   MakePair("MULTIPHYSICS", MAIN_SOLVER::MULTIPHYSICS)
 };
@@ -689,7 +675,7 @@ enum class MIXINGVISCOSITYMODEL {
   DAVIDSON, /*!< \brief Davidson mixing viscosity model. */
 };
 static const MapType<std::string, MIXINGVISCOSITYMODEL> MixingViscosityModel_Map = {
-  MakePair("WILKE", MIXINGVISCOSITYMODEL::WILKE) 
+  MakePair("WILKE", MIXINGVISCOSITYMODEL::WILKE)
   MakePair("DAVIDSON", MIXINGVISCOSITYMODEL::DAVIDSON)
 };
 
@@ -1182,6 +1168,119 @@ static const MapType<std::string, TURB_TRANS_MODEL> Trans_Model_Map = {
   MakePair("LM", TURB_TRANS_MODEL::LM)
 };
 
+/*!
+ * \brief LM Options
+ */
+enum class LM_OPTIONS {
+  NONE,         /*!< \brief No option / default. */
+  LM2015,       /*!< \brief Cross-flow corrections. */
+  MALAN,        /*!< \brief Kind of transition correlation model (Malan). */
+  SULUKSNA,     /*!< \brief Kind of transition correlation model (Suluksna). */
+  KRAUSE,       /*!< \brief Kind of transition correlation model (Krause). */
+  KRAUSE_HYPER, /*!< \brief Kind of transition correlation model (Krause hypersonic). */
+  MEDIDA_BAEDER,/*!< \brief Kind of transition correlation model (Medida-Baeder). */
+  MEDIDA,       /*!< \brief Kind of transition correlation model (Medida). */
+  MENTER_LANGTRY,   /*!< \brief Kind of transition correlation model (Menter-Langtry). */
+  DEFAULT       /*!< \brief Kind of transition correlation model (Menter-Langtry if SST, MALAN if SA). */
+};
+
+static const MapType<std::string, LM_OPTIONS> LM_Options_Map = {
+  MakePair("NONE", LM_OPTIONS::NONE)
+  MakePair("LM2015", LM_OPTIONS::LM2015)
+  MakePair("MALAN", LM_OPTIONS::MALAN)
+  MakePair("SULUKSNA", LM_OPTIONS::SULUKSNA)
+  MakePair("KRAUSE", LM_OPTIONS::KRAUSE)
+  MakePair("KRAUSE_HYPER", LM_OPTIONS::KRAUSE_HYPER)
+  MakePair("MEDIDA_BAEDER", LM_OPTIONS::MEDIDA_BAEDER)
+  MakePair("MENTER_LANGTRY", LM_OPTIONS::MENTER_LANGTRY)
+  MakePair("DEFAULT", LM_OPTIONS::DEFAULT)
+};
+
+/*!
+ * \brief Types of transition correlations
+ */
+enum class TURB_TRANS_CORRELATION {
+  MALAN,        /*!< \brief Kind of transition correlation model (Malan). */
+  SULUKSNA,     /*!< \brief Kind of transition correlation model (Suluksna). */
+  KRAUSE,       /*!< \brief Kind of transition correlation model (Krause). */
+  KRAUSE_HYPER, /*!< \brief Kind of transition correlation model (Krause hypersonic). */
+  MEDIDA_BAEDER,/*!< \brief Kind of transition correlation model (Medida-Baeder). */
+  MEDIDA,       /*!< \brief Kind of transition correlation model (Medida). */
+  MENTER_LANGTRY,   /*!< \brief Kind of transition correlation model (Menter-Langtry). */
+  DEFAULT       /*!< \brief Kind of transition correlation model (Menter-Langtry if SST, MALAN if SA). */
+};
+
+/*!
+ * \brief Structure containing parsed LM options.
+ */
+struct LM_ParsedOptions {
+  LM_OPTIONS version = LM_OPTIONS::NONE;  /*!< \brief LM base model. */
+  bool LM2015 = false;                    /*!< \brief Use cross-flow corrections. */
+  TURB_TRANS_CORRELATION Correlation = TURB_TRANS_CORRELATION::DEFAULT;
+};
+
+/*!
+ * \brief Function to parse LM options.
+ * \param[in] LM_Options - Selected LM option from config.
+ * \param[in] nLM_Options - Number of options selected.
+ * \param[in] rank - MPI rank.
+ * \return Struct with SA options.
+ */
+inline LM_ParsedOptions ParseLMOptions(const LM_OPTIONS *LM_Options, unsigned short nLM_Options, int rank, TURB_MODEL Kind_Turb_Model) {
+  LM_ParsedOptions LMParsedOptions;
+
+  auto IsPresent = [&](LM_OPTIONS option) {
+    const auto lm_options_end = LM_Options + nLM_Options;
+    return std::find(LM_Options, lm_options_end, option) != lm_options_end;
+  };
+
+  LMParsedOptions.LM2015 = IsPresent(LM_OPTIONS::LM2015);
+
+  int NFoundCorrelations = 0;
+  if (IsPresent(LM_OPTIONS::MALAN)) {
+    LMParsedOptions.Correlation = TURB_TRANS_CORRELATION::MALAN;
+    NFoundCorrelations++;
+  }
+  if (IsPresent(LM_OPTIONS::SULUKSNA)) {
+    LMParsedOptions.Correlation = TURB_TRANS_CORRELATION::SULUKSNA;
+    NFoundCorrelations++;
+  }
+  if (IsPresent(LM_OPTIONS::KRAUSE)) {
+    LMParsedOptions.Correlation = TURB_TRANS_CORRELATION::KRAUSE;
+    NFoundCorrelations++;
+  }
+  if (IsPresent(LM_OPTIONS::KRAUSE_HYPER)) {
+    LMParsedOptions.Correlation = TURB_TRANS_CORRELATION::KRAUSE_HYPER;
+    NFoundCorrelations++;
+  }
+  if (IsPresent(LM_OPTIONS::MEDIDA_BAEDER)) {
+    LMParsedOptions.Correlation = TURB_TRANS_CORRELATION::MEDIDA_BAEDER;
+    NFoundCorrelations++;
+  }
+  if (IsPresent(LM_OPTIONS::MEDIDA)) {
+    LMParsedOptions.Correlation = TURB_TRANS_CORRELATION::MEDIDA;
+    NFoundCorrelations++;
+  }
+  if (IsPresent(LM_OPTIONS::MENTER_LANGTRY)) {
+    LMParsedOptions.Correlation = TURB_TRANS_CORRELATION::MENTER_LANGTRY;
+    NFoundCorrelations++;
+  }
+
+  if (NFoundCorrelations > 1) {
+    SU2_MPI::Error("Two correlations selected for LM_OPTIONS. Please choose only one.", CURRENT_FUNCTION);
+  }
+
+  if (LMParsedOptions.Correlation == TURB_TRANS_CORRELATION::DEFAULT){
+    if (Kind_Turb_Model == TURB_MODEL::SST) {
+      LMParsedOptions.Correlation = TURB_TRANS_CORRELATION::MENTER_LANGTRY;
+    } else if (Kind_Turb_Model == TURB_MODEL::SA) {
+      LMParsedOptions.Correlation = TURB_TRANS_CORRELATION::MALAN;
+    }
+  }
+
+  return LMParsedOptions;
+}
+
 /*!
  * \brief types of species transport models
  */
diff --git a/Common/include/option_structure.inl b/Common/include/option_structure.inl
index 5e09efe9aa2..706b9f8c05f 100644
--- a/Common/include/option_structure.inl
+++ b/Common/include/option_structure.inl
@@ -3,7 +3,7 @@
  * \brief Template derived classes from COption, defined here as we
  *        only include them where needed to reduce compilation time.
  * \author J. Hicken, B. Tracey
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/parallelization/mpi_structure.cpp b/Common/include/parallelization/mpi_structure.cpp
index e4abe6ab79f..d280cad159a 100644
--- a/Common/include/parallelization/mpi_structure.cpp
+++ b/Common/include/parallelization/mpi_structure.cpp
@@ -2,7 +2,7 @@
  * \file mpi_structure.cpp
  * \brief Main subroutines for the mpi structures.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/parallelization/mpi_structure.hpp b/Common/include/parallelization/mpi_structure.hpp
index 06a65a6fef7..52d629a5968 100644
--- a/Common/include/parallelization/mpi_structure.hpp
+++ b/Common/include/parallelization/mpi_structure.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the mpi interface for generalized datatypes.
  *        The subroutines and functions are in the <i>mpi_structure.cpp</i> file.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/parallelization/omp_structure.cpp b/Common/include/parallelization/omp_structure.cpp
index 09a50c3ba72..af8dd0337bb 100644
--- a/Common/include/parallelization/omp_structure.cpp
+++ b/Common/include/parallelization/omp_structure.cpp
@@ -3,7 +3,7 @@
  * \brief Source file counterpart for omp_structure.hpp.
  * \note Contains OpDiLib initialization, finalization and includes the OpDiLib source file.
  * \author J. Blühdorn
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/parallelization/omp_structure.hpp b/Common/include/parallelization/omp_structure.hpp
index 7ead8947d12..d6a161ab684 100644
--- a/Common/include/parallelization/omp_structure.hpp
+++ b/Common/include/parallelization/omp_structure.hpp
@@ -13,7 +13,7 @@
  *       defined here with suitable fallback versions to limit the spread of
  *       compiler tricks in other areas of the code.
  * \author P. Gomes, J. Blühdorn
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/parallelization/special_vectorization.hpp b/Common/include/parallelization/special_vectorization.hpp
index 9e4d74da021..cbdc7388eb5 100644
--- a/Common/include/parallelization/special_vectorization.hpp
+++ b/Common/include/parallelization/special_vectorization.hpp
@@ -2,7 +2,7 @@
  * \file special_vectorization.hpp
  * \brief Code generator header to create specializations of simd::Array.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/parallelization/vectorization.hpp b/Common/include/parallelization/vectorization.hpp
index d90b0afb8f0..2d38834a9de 100644
--- a/Common/include/parallelization/vectorization.hpp
+++ b/Common/include/parallelization/vectorization.hpp
@@ -2,7 +2,7 @@
  * \file vectorization.hpp
  * \brief Implementation of a portable SIMD type.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/C1DInterpolation.hpp b/Common/include/toolboxes/C1DInterpolation.hpp
index 263f9f1f962..5168b76073b 100644
--- a/Common/include/toolboxes/C1DInterpolation.hpp
+++ b/Common/include/toolboxes/C1DInterpolation.hpp
@@ -2,7 +2,7 @@
  * \file C1DInterpolation.hpp
  * \brief Classes for 1D interpolation.
  * \author Aman Baig, P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/CLinearPartitioner.hpp b/Common/include/toolboxes/CLinearPartitioner.hpp
index 6e9fe5847e8..165c639ee02 100644
--- a/Common/include/toolboxes/CLinearPartitioner.hpp
+++ b/Common/include/toolboxes/CLinearPartitioner.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CLinearPartitioner.
  *        The implementations are in the <i>CLinearPartitioner.cpp</i> file.
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/CQuasiNewtonInvLeastSquares.hpp b/Common/include/toolboxes/CQuasiNewtonInvLeastSquares.hpp
index d5222b4437c..f03a1713799 100644
--- a/Common/include/toolboxes/CQuasiNewtonInvLeastSquares.hpp
+++ b/Common/include/toolboxes/CQuasiNewtonInvLeastSquares.hpp
@@ -7,7 +7,7 @@
  * \note Based on the IQN-ILS method, see DOI 10.1007/s11831-013-9085-5 and
  * references therein.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/CSquareMatrixCM.hpp b/Common/include/toolboxes/CSquareMatrixCM.hpp
index 39836fafaca..85abfff5520 100644
--- a/Common/include/toolboxes/CSquareMatrixCM.hpp
+++ b/Common/include/toolboxes/CSquareMatrixCM.hpp
@@ -3,7 +3,7 @@
  * \brief Dense general square matrix, used for example in DG standard elements
  *        in Column Major order storage.
  * \author Edwin van der Weide, Pedro Gomes.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/CSymmetricMatrix.hpp b/Common/include/toolboxes/CSymmetricMatrix.hpp
index ba5f83ee368..b15fdd95f0c 100644
--- a/Common/include/toolboxes/CSymmetricMatrix.hpp
+++ b/Common/include/toolboxes/CSymmetricMatrix.hpp
@@ -2,7 +2,7 @@
  * \file CSymmetricMatrix.hpp
  * \brief Dense symmetric matrix, used for example in RBF interpolation.
  * \author Joel Ho, P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CIncTGVSolution.hpp b/Common/include/toolboxes/MMS/CIncTGVSolution.hpp
index cb67803a6e5..9271464afac 100644
--- a/Common/include/toolboxes/MMS/CIncTGVSolution.hpp
+++ b/Common/include/toolboxes/MMS/CIncTGVSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CIncTGVSolution.
  *        The implementations are in the <i>CIncTGVSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CInviscidVortexSolution.hpp b/Common/include/toolboxes/MMS/CInviscidVortexSolution.hpp
index 486bbd69d9f..504fad4f6a6 100644
--- a/Common/include/toolboxes/MMS/CInviscidVortexSolution.hpp
+++ b/Common/include/toolboxes/MMS/CInviscidVortexSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CInviscidVortexSolution.
  *        The implementations are in the <i>CInviscidVortexSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CMMSIncEulerSolution.hpp b/Common/include/toolboxes/MMS/CMMSIncEulerSolution.hpp
index 1eabb63ab11..87434bac5f4 100644
--- a/Common/include/toolboxes/MMS/CMMSIncEulerSolution.hpp
+++ b/Common/include/toolboxes/MMS/CMMSIncEulerSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CMMSIncEulerSolution.
  *        The implementations are in the <i>CMMSIncEulerSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CMMSIncNSSolution.hpp b/Common/include/toolboxes/MMS/CMMSIncNSSolution.hpp
index 957444e9677..06d4ffccf10 100644
--- a/Common/include/toolboxes/MMS/CMMSIncNSSolution.hpp
+++ b/Common/include/toolboxes/MMS/CMMSIncNSSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CMMSIncNSSolution.
  *        The implementations are in the <i>CMMSIncNSSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.hpp b/Common/include/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.hpp
index f12022038f4..eed8ebcc1ab 100644
--- a/Common/include/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.hpp
+++ b/Common/include/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CMMSNSTwoHalfCirclesSolution.
  *        The implementations are in the <i>CMMSNSTwoHalfCirclesSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.hpp b/Common/include/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.hpp
index 5a922b57d01..52e1434fc43 100644
--- a/Common/include/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.hpp
+++ b/Common/include/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CMMSNSTwoHalfSpheresSolution.
  *        The implementations are in the <i>CMMSNSTwoHalfSpheresSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolution.hpp b/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolution.hpp
index b7d58c89f69..57cfb7e5c64 100644
--- a/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolution.hpp
+++ b/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CMMSNSUnitQuadSolution.
  *        The implementations are in the <i>CMMSNSUnitQuadSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.hpp b/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.hpp
index fd953208064..64d9db28c4e 100644
--- a/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.hpp
+++ b/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CMMSNSUnitQuadSolutionWallBC.
  *        The implementations are in the <i>CMMSNSUnitQuadSolutionWallBC.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CNSUnitQuadSolution.hpp b/Common/include/toolboxes/MMS/CNSUnitQuadSolution.hpp
index 3d2f0bb5084..10a3d312995 100644
--- a/Common/include/toolboxes/MMS/CNSUnitQuadSolution.hpp
+++ b/Common/include/toolboxes/MMS/CNSUnitQuadSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CNSUnitQuadSolution.hpp.
  *        The implementations are in the <i>CNSUnitQuadSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CRinglebSolution.hpp b/Common/include/toolboxes/MMS/CRinglebSolution.hpp
index 246d7267dfd..9847b350586 100644
--- a/Common/include/toolboxes/MMS/CRinglebSolution.hpp
+++ b/Common/include/toolboxes/MMS/CRinglebSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CRinglebSolution.hpp.
  *        The implementations are in the <i>CRinglebSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CTGVSolution.hpp b/Common/include/toolboxes/MMS/CTGVSolution.hpp
index 516af49eef9..67da2e88f5a 100644
--- a/Common/include/toolboxes/MMS/CTGVSolution.hpp
+++ b/Common/include/toolboxes/MMS/CTGVSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CTGVSolution.
  *        The implementations are in the <i>CTGVSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CUserDefinedSolution.hpp b/Common/include/toolboxes/MMS/CUserDefinedSolution.hpp
index 129cca904ca..ed4e4bfcda4 100644
--- a/Common/include/toolboxes/MMS/CUserDefinedSolution.hpp
+++ b/Common/include/toolboxes/MMS/CUserDefinedSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CUserDefinedSolution.
  *        The implementations are in the <i>CUserDefinedSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CVerificationSolution.hpp b/Common/include/toolboxes/MMS/CVerificationSolution.hpp
index 2715bf225c7..10143fbc8cd 100644
--- a/Common/include/toolboxes/MMS/CVerificationSolution.hpp
+++ b/Common/include/toolboxes/MMS/CVerificationSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the base class CVerificationSolution.
  *        The implementations are in the <i>CVerificationSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/allocation_toolbox.hpp b/Common/include/toolboxes/allocation_toolbox.hpp
index 61520bb90c3..2c630f7d550 100644
--- a/Common/include/toolboxes/allocation_toolbox.hpp
+++ b/Common/include/toolboxes/allocation_toolbox.hpp
@@ -5,7 +5,7 @@
  * \note  These are "kernel" functions, only to be used with good reason,
  *        always try to use higher level container classes.
  * \author P. Gomes, D. Kavolis
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/geometry_toolbox.hpp b/Common/include/toolboxes/geometry_toolbox.hpp
index d1ed11250e5..52a0018483d 100644
--- a/Common/include/toolboxes/geometry_toolbox.hpp
+++ b/Common/include/toolboxes/geometry_toolbox.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file geometry_toolbox.hpp
  * \brief Collection of common lightweight geometry-oriented methods.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/graph_toolbox.hpp b/Common/include/toolboxes/graph_toolbox.hpp
index 87a45720b3a..16cc515a1c0 100644
--- a/Common/include/toolboxes/graph_toolbox.hpp
+++ b/Common/include/toolboxes/graph_toolbox.hpp
@@ -2,7 +2,7 @@
  * \file graph_toolbox.hpp
  * \brief Functions and classes to build/represent sparse graphs or sparse patterns.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -530,7 +530,7 @@ T createNaturalColoring(Index_t numInnerIndexes)
  * \param[out] indexColor - Optional, vector with colors given to the outer indices.
  * \return Coloring in the same type of the input pattern.
  */
-template<class T, typename Color_t = char, size_t MaxColors = 64, size_t MaxMB = 128>
+template<typename Color_t = char, size_t MaxColors = 64, size_t MaxMB = 128, class T>
 T colorSparsePattern(const T& pattern, size_t groupSize = 1, bool balanceColors = false,
                      std::vector<Color_t>* indexColor = nullptr)
 {
diff --git a/Common/include/toolboxes/ndflattener.hpp b/Common/include/toolboxes/ndflattener.hpp
index 88382a85a70..035deb64dbc 100644
--- a/Common/include/toolboxes/ndflattener.hpp
+++ b/Common/include/toolboxes/ndflattener.hpp
@@ -2,7 +2,7 @@
  * \file ndflattener.hpp
  * \brief Flatten pointer-to-pointer-... arrays for MPI communication
  * \author M. Aehle
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/printing_toolbox.hpp b/Common/include/toolboxes/printing_toolbox.hpp
index aeff299b7bd..5edad78315d 100644
--- a/Common/include/toolboxes/printing_toolbox.hpp
+++ b/Common/include/toolboxes/printing_toolbox.hpp
@@ -2,7 +2,7 @@
  * \file printing_toolbox.hpp
  * \brief Header file for the printing toolbox.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/wall_model.hpp b/Common/include/wall_model.hpp
index 3374cd4d0bd..57cd67df5c2 100644
--- a/Common/include/wall_model.hpp
+++ b/Common/include/wall_model.hpp
@@ -2,7 +2,7 @@
  * \file wall_model.hpp
  * \brief Headers for the wall model functions for large eddy simulations.
  * \author E. van der Weide, T. Economon, P. Urbanczyk
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -42,7 +42,7 @@ class CFluidModel;
  * \class CWallModel
  * \brief Base class for defining the LES wall model.
  * \author: E. van der Weide, T. Economon, P. Urbanczyk
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CWallModel {
 
diff --git a/Common/lib/Makefile.am b/Common/lib/Makefile.am
index af2046cf826..aef8fdd4c00 100644
--- a/Common/lib/Makefile.am
+++ b/Common/lib/Makefile.am
@@ -3,7 +3,7 @@
 # \file Makefile.am
 # \brief Makefile for the SU2 common library
 # \author M. Colonno, T. Economon, F. Palacios
-# \version 7.4.0 "Blackbird"
+# \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 96f08f6220a..0357290120f 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -2,7 +2,7 @@
  * \file CConfig.cpp
  * \brief Main file for managing the config file
  * \author F. Palacios, T. Economon, B. Tracey, H. Kline
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -1103,6 +1103,10 @@ void CConfig::SetConfig_Options() {
 
   /*!\brief KIND_TRANS_MODEL \n DESCRIPTION: Specify transition model OPTIONS: see \link Trans_Model_Map \endlink \n DEFAULT: NONE \ingroup Config*/
   addEnumOption("KIND_TRANS_MODEL", Kind_Trans_Model, Trans_Model_Map, TURB_TRANS_MODEL::NONE);
+  /*!\brief SST_OPTIONS \n DESCRIPTION: Specify LM transition model options/correlations. \n Options: see \link LM_Options_Map \endlink \n DEFAULT: NONE \ingroup Config*/
+  addEnumListOption("LM_OPTIONS", nLM_Options, LM_Options, LM_Options_Map);
+  /*!\brief HROUGHNESS \n DESCRIPTION: Value of RMS roughness for transition model \n DEFAULT: 1E-6 \ingroup Config*/
+  addDoubleOption("HROUGHNESS", hRoughness, 1e-6);
 
   /*!\brief KIND_SCALAR_MODEL \n DESCRIPTION: Specify scalar transport model \n Options: see \link Scalar_Model_Map \endlink \n DEFAULT: NONE \ingroup Config*/
   addEnumOption("KIND_SCALAR_MODEL", Kind_Species_Model, Species_Model_Map, SPECIES_MODEL::NONE);
@@ -1126,6 +1130,8 @@ void CConfig::SetConfig_Options() {
   addBoolOption("AXISYMMETRIC", Axisymmetric, false);
   /* DESCRIPTION: Add the gravity force */
   addBoolOption("GRAVITY_FORCE", GravityForce, false);
+  /* DESCRIPTION: Add the Vorticity Confinement term*/
+  addBoolOption("VORTICITY_CONFINEMENT", VorticityConfinement, false);
   /* DESCRIPTION: Apply a body force as a source term (NO, YES) */
   addBoolOption("BODY_FORCE", Body_Force, false);
   body_force[0] = 0.0; body_force[1] = 0.0; body_force[2] = 0.0;
@@ -1162,6 +1168,8 @@ void CConfig::SetConfig_Options() {
   /*!\brief FLUID_NAME \n DESCRIPTION: Fluid name \n OPTIONS: see coolprop homepage \n DEFAULT: nitrogen \ingroup Config*/
   addStringOption("FLUID_NAME", FluidName, string("nitrogen"));
 
+  /*!\brief CONFINEMENT_PARAM \n DESCRIPTION: Input Confinement Parameter for Vorticity Confinement*/
+  addDoubleOption("CONFINEMENT_PARAM", Confinement_Param, 0.0);
 
   /*!\par CONFIG_CATEGORY: Freestream Conditions \ingroup Config*/
   /*--- Options related to freestream specification ---*/
@@ -1187,6 +1195,10 @@ void CConfig::SetConfig_Options() {
   addEnumOption("TRANSPORT_COEFF_MODEL", Kind_TransCoeffModel, TransCoeffModel_Map, TRANSCOEFFMODEL::WILKE);
   /* DESCRIPTION: Specify mass fraction of each species */
   addDoubleListOption("GAS_COMPOSITION", nSpecies, Gas_Composition);
+  /* DESCRIPTION: Specify mass fraction of each species for NEMO inlet*/
+  addDoubleListOption("INLET_GAS_COMPOSITION", nSpecies_inlet, Inlet_MassFrac);
+  /*!\brief INLET_TEMPERATURE_VE \n DESCRIPTION: NEMO inlet temperature_ve (K), if left 0 K, set to Ttr value \ingroup Config*/
+  addDoubleOption("INLET_TEMPERATURE_VE", Inlet_Temperature_ve, 0.0);
   /* DESCRIPTION: Specify if mixture is frozen */
   addBoolOption("FROZEN_MIXTURE", frozen, false);
   /* DESCRIPTION: Specify if there is ionization */
@@ -3230,7 +3242,7 @@ void CConfig::SetHeader(SU2_COMPONENT val_software) const{
   if ((iZone == 0) && (rank == MASTER_NODE)){
     cout << endl << "-------------------------------------------------------------------------" << endl;
     cout << "|    ___ _   _ ___                                                      |" << endl;
-    cout << "|   / __| | | |_  )   Release 7.4.0 \"Blackbird\"                         |" << endl;
+    cout << "|   / __| | | |_  )   Release 7.5.0 \"Blackbird\"                         |" << endl;
     cout << "|   \\__ \\ |_| |/ /                                                      |" << endl;
     switch (val_software) {
     case SU2_COMPONENT::SU2_CFD: cout << "|   |___/\\___//___|   Suite (Computational Fluid Dynamics Code)         |" << endl; break;
@@ -3455,6 +3467,16 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
     SU2_MPI::Error("Axisymmetry is currently only supported for KIND_TURB_MODEL chosen as SST", CURRENT_FUNCTION);
   }
 
+  /*--- Postprocess LM_OPTIONS into structure. ---*/
+  if (Kind_Trans_Model == TURB_TRANS_MODEL::LM) {
+    lmParsedOptions = ParseLMOptions(LM_Options, nLM_Options, rank, Kind_Turb_Model);
+
+    /*--- Check if problem is 2D and LM2015 has been selected ---*/
+    if (lmParsedOptions.LM2015 && val_nDim == 2) {
+      SU2_MPI::Error("LM2015 is available only for 3D problems", CURRENT_FUNCTION);
+    }
+  }
+
   /*--- Set the boolean Wall_Functions equal to true if there is a
    definition for the wall founctions ---*/
 
@@ -4748,10 +4770,6 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
     for (int i=0; i<7; ++i) eng_cyl[i] /= 12.0;
   }
 
-  if ((Kind_Turb_Model != TURB_MODEL::SST) && Kind_Trans_Model == TURB_TRANS_MODEL::LM) {
-    SU2_MPI::Error("LM transition model currently only available in combination with SST turbulence model!", CURRENT_FUNCTION);
-  }
-
   if(Turb_Fixed_Values && !OptionIsSet("TURB_FIXED_VALUES_DOMAIN")){
     SU2_MPI::Error("TURB_FIXED_VALUES activated, but no domain set with TURB_FIXED_VALUES_DOMAIN.", CURRENT_FUNCTION);
   }
@@ -4889,6 +4907,18 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
     }
   }
 
+  /*--- Vorticity confinement feature currently not supported for incompressible or non-equilibrium model or axisymmetric flows. ---*/
+
+  if ((Kind_Solver == MAIN_SOLVER::INC_EULER
+    || Kind_Solver == MAIN_SOLVER::INC_NAVIER_STOKES
+    || Kind_Solver == MAIN_SOLVER::INC_RANS
+    || Kind_Solver == MAIN_SOLVER::NEMO_EULER
+    || Kind_Solver == MAIN_SOLVER::NEMO_NAVIER_STOKES
+    || Axisymmetric)
+    && VorticityConfinement) {
+    SU2_MPI::Error("Vorticity confinement feature currently not supported for incompressible or non-equilibrium model or axisymmetric flows.", CURRENT_FUNCTION);
+  }
+
   /*--- Check the coefficients for the polynomial models. ---*/
 
   if (Kind_Solver != MAIN_SOLVER::INC_EULER && Kind_Solver != MAIN_SOLVER::INC_NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::INC_RANS) {
@@ -6082,7 +6112,35 @@ void CConfig::SetOutput(SU2_COMPONENT val_software, unsigned short val_izone) {
         }
         switch (Kind_Trans_Model) {
           case TURB_TRANS_MODEL::NONE:  break;
-          case TURB_TRANS_MODEL::LM:    cout << "Transition model: Langtry and Menter's 4 equation model (2009)" << endl; break;
+          case TURB_TRANS_MODEL::LM: {
+            cout << "Transition model: Langtry and Menter's 4 equation model";
+            if (lmParsedOptions.LM2015) {
+              cout << " w/ cross-flow corrections (2015)" << endl;
+            } else {
+              cout << " (2009)" << endl;
+            }
+            break;
+          }
+        }
+        if (Kind_Trans_Model == TURB_TRANS_MODEL::LM) {
+
+          cout << "Correlation Functions: ";
+          switch (lmParsedOptions.Correlation) {
+            case TURB_TRANS_CORRELATION::MALAN: cout << "Malan et al. (2009)" << endl;  break;
+            case TURB_TRANS_CORRELATION::SULUKSNA: cout << "Suluksna et al. (2009)" << endl;  break;
+            case TURB_TRANS_CORRELATION::KRAUSE: cout << "Krause et al. (2008)" << endl;  break;
+            case TURB_TRANS_CORRELATION::KRAUSE_HYPER: cout << "Krause et al. (2008, paper)" << endl;  break;
+            case TURB_TRANS_CORRELATION::MEDIDA_BAEDER: cout << "Medida and Baeder (2011)" << endl;  break;
+            case TURB_TRANS_CORRELATION::MEDIDA: cout << "Medida PhD (2014)" << endl;  break;
+            case TURB_TRANS_CORRELATION::MENTER_LANGTRY: cout << "Menter and Langtry (2009)" << endl;  break;
+            case TURB_TRANS_CORRELATION::DEFAULT:
+              switch (Kind_Turb_Model) {
+                case TURB_MODEL::SA: cout << "Malan et al. (2009)" << endl;  break;
+                case TURB_MODEL::SST: cout << "Menter and Langtry (2009)" << endl;  break;
+                case TURB_MODEL::NONE: SU2_MPI::Error("No turbulence model has been selected but LM transition model is active.", CURRENT_FUNCTION); break;
+              }
+              break;
+          }
         }
         cout << "Hybrid RANS/LES: ";
         switch (Kind_HybridRANSLES) {
@@ -8372,9 +8430,11 @@ void CConfig::SetGlobalParam(MAIN_SOLVER val_solver,
 
   switch (val_solver) {
     case MAIN_SOLVER::EULER: case MAIN_SOLVER::INC_EULER: case MAIN_SOLVER::NEMO_EULER:
+    case MAIN_SOLVER::DISC_ADJ_EULER: case MAIN_SOLVER::DISC_ADJ_INC_EULER:
       SetFlowParam();
       break;
     case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::INC_NAVIER_STOKES: case MAIN_SOLVER::NEMO_NAVIER_STOKES:
+    case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES:
       SetFlowParam();
       SetSpeciesParam();
 
@@ -8384,6 +8444,7 @@ void CConfig::SetGlobalParam(MAIN_SOLVER val_solver,
       }
       break;
     case MAIN_SOLVER::RANS: case MAIN_SOLVER::INC_RANS:
+    case MAIN_SOLVER::DISC_ADJ_RANS: case MAIN_SOLVER::DISC_ADJ_INC_RANS:
       SetFlowParam();
       SetTurbParam();
       SetSpeciesParam();
@@ -8401,7 +8462,11 @@ void CConfig::SetGlobalParam(MAIN_SOLVER val_solver,
       break;
     case MAIN_SOLVER::FEM_EULER:
     case MAIN_SOLVER::FEM_NAVIER_STOKES:
+    case MAIN_SOLVER::FEM_RANS:
     case MAIN_SOLVER::FEM_LES:
+    case MAIN_SOLVER::DISC_ADJ_FEM_EULER:
+    case MAIN_SOLVER::DISC_ADJ_FEM_NS:
+    case MAIN_SOLVER::DISC_ADJ_FEM_RANS:
       if (val_system == RUNTIME_FLOW_SYS) {
         SetKind_ConvNumScheme(Kind_ConvNumScheme_FEM_Flow, Kind_Centered_Flow,
                               Kind_Upwind_Flow, Kind_SlopeLimit_Flow,
@@ -8427,6 +8492,7 @@ void CConfig::SetGlobalParam(MAIN_SOLVER val_solver,
       }
       break;
     case MAIN_SOLVER::HEAT_EQUATION:
+    case MAIN_SOLVER::DISC_ADJ_HEAT:
       if (val_system == RUNTIME_HEAT_SYS) {
         SetKind_ConvNumScheme(NONE, CENTERED::NONE, UPWIND::NONE, LIMITER::NONE, NONE, NONE);
         SetKind_TimeIntScheme(Kind_TimeIntScheme_Heat);
@@ -8434,6 +8500,7 @@ void CConfig::SetGlobalParam(MAIN_SOLVER val_solver,
       break;
 
     case MAIN_SOLVER::FEM_ELASTICITY:
+    case MAIN_SOLVER::DISC_ADJ_FEM:
 
       Current_DynTime = static_cast<su2double>(TimeIter)*Delta_DynTime;
 
diff --git a/Common/src/adt/CADTBaseClass.cpp b/Common/src/adt/CADTBaseClass.cpp
index b38ecac1c6c..d4bdbcad0d1 100644
--- a/Common/src/adt/CADTBaseClass.cpp
+++ b/Common/src/adt/CADTBaseClass.cpp
@@ -2,7 +2,7 @@
  * \file CADTBaseClass.cpp
  * \brief Base class for storing an ADT in an arbitrary number of dimensions.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/adt/CADTElemClass.cpp b/Common/src/adt/CADTElemClass.cpp
index 38375a88056..b100b192c0a 100644
--- a/Common/src/adt/CADTElemClass.cpp
+++ b/Common/src/adt/CADTElemClass.cpp
@@ -2,7 +2,7 @@
  * \file CADTElemClass.cpp
  * \brief Class for storing an ADT of (linear) elements in an arbitrary number of dimensions.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/adt/CADTPointsOnlyClass.cpp b/Common/src/adt/CADTPointsOnlyClass.cpp
index dc99a542f82..31ae4d20a23 100644
--- a/Common/src/adt/CADTPointsOnlyClass.cpp
+++ b/Common/src/adt/CADTPointsOnlyClass.cpp
@@ -2,7 +2,7 @@
  * \file CADTPointsOnlyClass.cpp
  * \brief Class for storing an ADT of only points in an arbitrary number of dimensions.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/basic_types/ad_structure.cpp b/Common/src/basic_types/ad_structure.cpp
index d67bd486a8b..e5512da6598 100644
--- a/Common/src/basic_types/ad_structure.cpp
+++ b/Common/src/basic_types/ad_structure.cpp
@@ -2,7 +2,7 @@
  * \file ad_structure.cpp
  * \brief Main subroutines for the algorithmic differentiation (AD) structure.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/containers/CFileReaderLUT.cpp b/Common/src/containers/CFileReaderLUT.cpp
index 081293eded1..c88e6b7a36c 100644
--- a/Common/src/containers/CFileReaderLUT.cpp
+++ b/Common/src/containers/CFileReaderLUT.cpp
@@ -2,7 +2,7 @@
  * \file CFileReaderLUT.hpp
  * \brief reading lookup table for tabulated fluid properties
  * \author D. Mayer, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index a0e84c2926e..2c782f208d2 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -2,7 +2,7 @@
  * \file CLookupTable.cpp
  * \brief tabulation of fluid properties
  * \author D. Mayer, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/containers/CTrapezoidalMap.cpp b/Common/src/containers/CTrapezoidalMap.cpp
index 21d7cb535ac..4e7155d3592 100644
--- a/Common/src/containers/CTrapezoidalMap.cpp
+++ b/Common/src/containers/CTrapezoidalMap.cpp
@@ -2,7 +2,7 @@
  * \file CTrapezoidalMap.cpp
  * \brief Implementation of the trapezoidal map for tabulation and lookup of fluid properties
  * \author D. Mayer, T. Economon, N. Beishuizen
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/fem/fem_cgns_elements.cpp b/Common/src/fem/fem_cgns_elements.cpp
index 715c70bccb4..e614c350a48 100644
--- a/Common/src/fem/fem_cgns_elements.cpp
+++ b/Common/src/fem/fem_cgns_elements.cpp
@@ -2,7 +2,7 @@
  * \file fem_cgns_elements.cpp
  * \brief CGNS element definitions and conversions to the SU2 standard.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/fem/fem_gauss_jacobi_quadrature.cpp b/Common/src/fem/fem_gauss_jacobi_quadrature.cpp
index bd18f3cef00..ca674b8055b 100644
--- a/Common/src/fem/fem_gauss_jacobi_quadrature.cpp
+++ b/Common/src/fem/fem_gauss_jacobi_quadrature.cpp
@@ -4,7 +4,7 @@
           quadrature rules. All the functions in this file are based on the
           program JACOBI_RULE of John Burkardt.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/fem/fem_geometry_structure.cpp b/Common/src/fem/fem_geometry_structure.cpp
index 80243cb4535..a0e88ffd171 100644
--- a/Common/src/fem/fem_geometry_structure.cpp
+++ b/Common/src/fem/fem_geometry_structure.cpp
@@ -2,7 +2,7 @@
  * \file fem_geometry_structure.cpp
  * \brief Functions for creating the primal grid for the FEM solver.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/fem/fem_integration_rules.cpp b/Common/src/fem/fem_integration_rules.cpp
index d81f8ea0110..0bf79fc9dd8 100644
--- a/Common/src/fem/fem_integration_rules.cpp
+++ b/Common/src/fem/fem_integration_rules.cpp
@@ -2,7 +2,7 @@
  * \file fem_integration_rules.cpp
  * \brief FEM integration rules for the standard elements.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/fem/fem_standard_element.cpp b/Common/src/fem/fem_standard_element.cpp
index fff76c88abc..aa281ee2683 100644
--- a/Common/src/fem/fem_standard_element.cpp
+++ b/Common/src/fem/fem_standard_element.cpp
@@ -2,7 +2,7 @@
  * \file fem_standard_element.cpp
  * \brief Functions for the FEM standard elements.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/fem/fem_wall_distance.cpp b/Common/src/fem/fem_wall_distance.cpp
index fc97fd28f22..2341359dfd7 100644
--- a/Common/src/fem/fem_wall_distance.cpp
+++ b/Common/src/fem/fem_wall_distance.cpp
@@ -2,7 +2,7 @@
  * \file fem_wall_distance.cpp
  * \brief Main subroutines for computing the wall distance for the FEM solver.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/fem/fem_work_estimate_metis.cpp b/Common/src/fem/fem_work_estimate_metis.cpp
index f416fc696ff..eaab51d39fe 100644
--- a/Common/src/fem/fem_work_estimate_metis.cpp
+++ b/Common/src/fem/fem_work_estimate_metis.cpp
@@ -3,7 +3,7 @@
  * \brief This file contains the implementation of the member functions WorkEstimateMetis
           for the FEM standard elements.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/fem/geometry_structure_fem_part.cpp b/Common/src/fem/geometry_structure_fem_part.cpp
index 39a7a12cf5e..1bb8f0a0b6a 100644
--- a/Common/src/fem/geometry_structure_fem_part.cpp
+++ b/Common/src/fem/geometry_structure_fem_part.cpp
@@ -2,7 +2,7 @@
  * \file geometry_structure_fem_part.cpp
  * \brief Main subroutines for distributin the grid for the Fluid FEM solver.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/CDummyGeometry.cpp b/Common/src/geometry/CDummyGeometry.cpp
index 47704817d66..3626ef51196 100644
--- a/Common/src/geometry/CDummyGeometry.cpp
+++ b/Common/src/geometry/CDummyGeometry.cpp
@@ -2,7 +2,7 @@
  * \file CDummyGeometry.hpp
  * \brief Implementation of the dummy geometry class used in "dry run" mode.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/CGeometry.cpp b/Common/src/geometry/CGeometry.cpp
index a548c3fe1bc..87ed7214f60 100644
--- a/Common/src/geometry/CGeometry.cpp
+++ b/Common/src/geometry/CGeometry.cpp
@@ -2,7 +2,7 @@
  * \file CGeometry.cpp
  * \brief Implementation of the base geometry class.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -25,6 +25,8 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
+#include <unordered_set>
+
 #include "../../include/geometry/CGeometry.hpp"
 #include "../../include/geometry/elements/CElement.hpp"
 #include "../../include/parallelization/omp_structure.hpp"
@@ -3843,7 +3845,7 @@ void CGeometry::ColorMGLevels(unsigned short nMGLevels, const CGeometry* const*
     /*--- Color the coarse points. ---*/
     vector<tColor> color;
     const auto& adjacency = geometry[iMesh]->nodes->GetPoints();
-    if (colorSparsePattern<CCompressedSparsePatternUL, tColor, nColor>(adjacency, 1, false, &color).empty())
+    if (colorSparsePattern<tColor, nColor>(adjacency, 1, false, &color).empty())
       continue;
 
     /*--- Propagate colors to fine mesh. ---*/
@@ -3859,6 +3861,178 @@ void CGeometry::ColorMGLevels(unsigned short nMGLevels, const CGeometry* const*
   }
 }
 
+const CGeometry::CLineletInfo& CGeometry::GetLineletInfo(const CConfig* config) const {
+  auto& li = lineletInfo;
+  if (!li.linelets.empty() || nPoint == 0) return li;
+
+  li.lineletIdx.resize(nPoint, CLineletInfo::NO_LINELET);
+
+  /*--- Estimate number of linelets. ---*/
+
+  unsigned long nLinelet = 0;
+  for (auto iMarker = 0u; iMarker < config->GetnMarker_All(); iMarker++) {
+    if (config->GetSolid_Wall(iMarker) || config->GetMarker_All_KindBC(iMarker) == DISPLACEMENT_BOUNDARY) {
+      nLinelet += nVertex[iMarker];
+    }
+  }
+
+  /*--- If the domain contains well defined Linelets ---*/
+
+  unsigned long maxNPoints = 0, sumNPoints = 0;
+
+  if (nLinelet != 0) {
+    /*--- Define the basic linelets, starting from each vertex, preventing duplication of points. ---*/
+
+    li.linelets.resize(nLinelet);
+    nLinelet = 0;
+    for (auto iMarker = 0u; iMarker < config->GetnMarker_All(); iMarker++) {
+      if (config->GetSolid_Wall(iMarker) || config->GetMarker_All_KindBC(iMarker) == DISPLACEMENT_BOUNDARY) {
+        for (auto iVertex = 0ul; iVertex < nVertex[iMarker]; iVertex++) {
+          const auto iPoint = vertex[iMarker][iVertex]->GetNode();
+          if (li.lineletIdx[iPoint] == CLineletInfo::NO_LINELET && nodes->GetDomain(iPoint)) {
+            li.linelets[nLinelet].push_back(iPoint);
+            li.lineletIdx[iPoint] = nLinelet;
+            ++nLinelet;
+          }
+        }
+      }
+    }
+    li.linelets.resize(nLinelet);
+
+    /*--- Create the linelet structure. ---*/
+
+    nLinelet = 0;
+    for (auto& linelet : li.linelets) {
+      while (linelet.size() < CLineletInfo::MAX_LINELET_POINTS) {
+        const auto iPoint = linelet.back();
+
+        /*--- Compute the value of the max and min weights to detect if this region is isotropic. ---*/
+
+        su2double max_weight = 0.0, min_weight = std::numeric_limits<su2double>::max();
+        for (auto iNode = 0u; iNode < nodes->GetnPoint(iPoint); iNode++) {
+          const auto jPoint = nodes->GetPoint(iPoint, iNode);
+          const auto iEdge = nodes->GetEdge(iPoint, iNode);
+          const auto* normal = edges->GetNormal(iEdge);
+          const su2double area = GeometryToolbox::Norm(nDim, normal);
+          const su2double volume_iPoint = nodes->GetVolume(iPoint);
+          const su2double volume_jPoint = nodes->GetVolume(jPoint);
+          const su2double weight = 0.5 * area * (1.0 / volume_iPoint + 1.0 / volume_jPoint);
+          max_weight = max(max_weight, weight);
+          min_weight = min(min_weight, weight);
+        }
+
+        /*--- Isotropic, stop this linelet. ---*/
+        if (min_weight / max_weight > CLineletInfo::ALPHA_ISOTROPIC()) break;
+
+        /*--- Otherwise, add the closest valid neighbor. ---*/
+
+        su2double min_dist2 = std::numeric_limits<su2double>::max();
+        auto next_Point = iPoint;
+        const auto* iCoord = nodes->GetCoord(iPoint);
+
+        for (const auto jPoint : nodes->GetPoints(iPoint)) {
+          if (li.lineletIdx[jPoint] == CLineletInfo::NO_LINELET && nodes->GetDomain(jPoint)) {
+            const auto* jCoord = nodes->GetCoord(jPoint);
+            const su2double d2 = GeometryToolbox::SquaredDistance(nDim, iCoord, jCoord);
+            su2double cosTheta = 1;
+            if (linelet.size() > 1) {
+              const auto* kCoord = nodes->GetCoord(linelet[linelet.size() - 2]);
+              su2double dij[3] = {0.0}, dki[3] = {0.0};
+              GeometryToolbox::Distance(nDim, iCoord, kCoord, dki);
+              GeometryToolbox::Distance(nDim, jCoord, iCoord, dij);
+              cosTheta = GeometryToolbox::DotProduct(3, dki, dij) / sqrt(d2 * GeometryToolbox::SquaredNorm(nDim, dki));
+            }
+            if (d2 < min_dist2 && cosTheta > 0.7071) {
+              next_Point = jPoint;
+              min_dist2 = d2;
+            }
+          }
+        }
+
+        /*--- Did not find a suitable point. ---*/
+        if (next_Point == iPoint) break;
+
+        linelet.push_back(next_Point);
+        li.lineletIdx[next_Point] = nLinelet;
+      }
+      ++nLinelet;
+
+      maxNPoints = max<unsigned long>(maxNPoints, linelet.size());
+      sumNPoints += linelet.size();
+    }
+  }
+
+  /*--- Average linelet size over all ranks. ---*/
+
+  unsigned long globalNPoints, globalNLineLets;
+  SU2_MPI::Allreduce(&sumNPoints, &globalNPoints, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&nLinelet, &globalNLineLets, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
+
+  if (rank == MASTER_NODE) {
+    std::cout << "Computed linelet structure, "
+              << static_cast<unsigned long>(passivedouble(globalNPoints) / globalNLineLets)
+              << " points in each line (average)." << std::endl;
+  }
+
+  /*--- Color the linelets for OpenMP parallelization and visualization. ---*/
+
+  /*--- Adjacency between lines, computed from point neighbors. ---*/
+  std::vector<std::vector<unsigned long>> adjacency(nLinelet);
+  for (auto iLine = 0ul; iLine < nLinelet; ++iLine) {
+    std::unordered_set<unsigned long> neighbors;
+    for (const auto iPoint : li.linelets[iLine]) {
+      neighbors.insert(iPoint);
+      for (const auto jPoint : nodes->GetPoints(iPoint)) {
+        neighbors.insert(jPoint);
+      }
+    }
+    adjacency[iLine].reserve(neighbors.size());
+    for (const auto iPoint : neighbors) {
+      adjacency[iLine].push_back(iPoint);
+    }
+  }
+
+  const auto coloring = colorSparsePattern<uint8_t, std::numeric_limits<uint8_t>::max()>(
+      CCompressedSparsePatternUL(adjacency), 1, true);
+  const auto nColors = coloring.getOuterSize();
+
+  /*--- Sort linelets by color. ---*/
+  std::vector<std::vector<unsigned long>> sortedLinelets;
+  sortedLinelets.reserve(nLinelet);
+  li.colorOffsets.reserve(nColors + 1);
+  li.colorOffsets.push_back(0);
+
+  for (auto iColor = 0ul; iColor < nColors; ++iColor) {
+    for (const auto iLine : coloring.getInnerIter(iColor)) {
+      /*--- Store the new linelet index for its points. ---*/
+      for (const auto iPoint : li.linelets[iLine]) {
+        li.lineletIdx[iPoint] = sortedLinelets.size();
+      }
+      sortedLinelets.push_back(std::move(li.linelets[iLine]));
+    }
+    li.colorOffsets.push_back(sortedLinelets.size());
+  }
+  li.linelets = std::move(sortedLinelets);
+
+  /*--- For visualization, offset colors to avoid coloring across ranks. ---*/
+  std::vector<unsigned long> allNColors(size);
+  SU2_MPI::Allgather(&nColors, 1, MPI_UNSIGNED_LONG, allNColors.data(), 1, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
+  unsigned long offset = 0;
+  for (int i = 0; i < rank; ++i) offset += allNColors[i];
+
+  /*--- Finally, transfer colors to points, using "0" as "no linelet". ---*/
+  li.lineletColor.resize(nPoint, 0);
+  for (auto iColor = 0ul; iColor < nColors; ++iColor) {
+    for (auto iLine = li.colorOffsets[iColor]; iLine < li.colorOffsets[iColor + 1]; ++iLine) {
+      for (const auto iPoint : li.linelets[iLine]) {
+        li.lineletColor[iPoint] = 1 + offset + iColor;
+      }
+    }
+  }
+
+  return li;
+}
+
 void CGeometry::ComputeWallDistance(const CConfig* const* config_container, CGeometry ****geometry_container){
 
   int nZone = config_container[ZONE_0]->GetnZone();
diff --git a/Common/src/geometry/CMultiGridGeometry.cpp b/Common/src/geometry/CMultiGridGeometry.cpp
index e5b69edb35b..06cb35d0c9f 100644
--- a/Common/src/geometry/CMultiGridGeometry.cpp
+++ b/Common/src/geometry/CMultiGridGeometry.cpp
@@ -2,7 +2,7 @@
  * \file CMultiGridGeometry.cpp
  * \brief Implementation of the multigrid geometry class.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -511,6 +511,8 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
   SU2_MPI::Allreduce(&nPoint, &Global_nPointCoarse, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
   SU2_MPI::Allreduce(&nPointFine, &Global_nPointFine, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
 
+  SetGlobal_nPointDomain(Global_nPointCoarse);
+
   if (iMesh != MESH_0) {
     const su2double factor = 1.5;
     const su2double Coeff = pow(su2double(Global_nPointFine) / Global_nPointCoarse, 1.0 / nDim);
diff --git a/Common/src/geometry/CMultiGridQueue.cpp b/Common/src/geometry/CMultiGridQueue.cpp
index d2f51cb20a7..50d731939ad 100644
--- a/Common/src/geometry/CMultiGridQueue.cpp
+++ b/Common/src/geometry/CMultiGridQueue.cpp
@@ -2,7 +2,7 @@
  * \file CMultiGridQueue.cpp
  * \brief Implementation of the multigrid queue class for the FVM solver.
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/CPhysicalGeometry.cpp b/Common/src/geometry/CPhysicalGeometry.cpp
index d097edc0ede..25f4bed5c46 100644
--- a/Common/src/geometry/CPhysicalGeometry.cpp
+++ b/Common/src/geometry/CPhysicalGeometry.cpp
@@ -2,7 +2,7 @@
  * \file CPhysicalGeometry.cpp
  * \brief Implementation of the physical geometry class.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/dual_grid/CDualGrid.cpp b/Common/src/geometry/dual_grid/CDualGrid.cpp
index e6d46914b27..0a71a8e716e 100644
--- a/Common/src/geometry/dual_grid/CDualGrid.cpp
+++ b/Common/src/geometry/dual_grid/CDualGrid.cpp
@@ -2,7 +2,7 @@
  * \file CDualGrid.cpp
  * \brief Main classes for defining the dual grid
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/dual_grid/CEdge.cpp b/Common/src/geometry/dual_grid/CEdge.cpp
index 0f079084235..f4fbf8189f6 100644
--- a/Common/src/geometry/dual_grid/CEdge.cpp
+++ b/Common/src/geometry/dual_grid/CEdge.cpp
@@ -2,7 +2,7 @@
  * \file CEdge.cpp
  * \brief Implementation of the edge class.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/dual_grid/CPoint.cpp b/Common/src/geometry/dual_grid/CPoint.cpp
index 60492a71500..3d392128b31 100644
--- a/Common/src/geometry/dual_grid/CPoint.cpp
+++ b/Common/src/geometry/dual_grid/CPoint.cpp
@@ -2,7 +2,7 @@
  * \file CPoint.cpp
  * \brief Main classes for defining the points of the dual grid
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/dual_grid/CTurboVertex.cpp b/Common/src/geometry/dual_grid/CTurboVertex.cpp
index 3e1b7b690da..c0f8e6a0309 100644
--- a/Common/src/geometry/dual_grid/CTurboVertex.cpp
+++ b/Common/src/geometry/dual_grid/CTurboVertex.cpp
@@ -2,7 +2,7 @@
  * \file CTurboVertex.cpp
  * \brief Main classes for defining the turbo vertices of the dual grid
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/dual_grid/CVertex.cpp b/Common/src/geometry/dual_grid/CVertex.cpp
index 3e5018931bb..cc6b43f1081 100644
--- a/Common/src/geometry/dual_grid/CVertex.cpp
+++ b/Common/src/geometry/dual_grid/CVertex.cpp
@@ -2,7 +2,7 @@
  * \file CVertex.cpp
  * \brief Main classes for defining the vertices of the dual grid
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/elements/CElement.cpp b/Common/src/geometry/elements/CElement.cpp
index ccac8e64077..850ac3e6429 100644
--- a/Common/src/geometry/elements/CElement.cpp
+++ b/Common/src/geometry/elements/CElement.cpp
@@ -2,7 +2,7 @@
  * \file CElement.cpp
  * \brief Definition of the Finite Element structure (elements)
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/elements/CHEXA8.cpp b/Common/src/geometry/elements/CHEXA8.cpp
index f221b97e29c..3071ce61033 100644
--- a/Common/src/geometry/elements/CHEXA8.cpp
+++ b/Common/src/geometry/elements/CHEXA8.cpp
@@ -2,7 +2,7 @@
  * \file CHEXA8.cpp
  * \brief Definition of 8-node hexa element with 8 Gauss points.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/elements/CLINE.cpp b/Common/src/geometry/elements/CLINE.cpp
index 3fad2f970e3..9fc9dd77ddd 100644
--- a/Common/src/geometry/elements/CLINE.cpp
+++ b/Common/src/geometry/elements/CLINE.cpp
@@ -2,7 +2,7 @@
  * \file CLINE.cpp
  * \brief Definition of the 2-node line element with two Gauss points.
  * \author T. Dick
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/elements/CPRISM6.cpp b/Common/src/geometry/elements/CPRISM6.cpp
index e4f9c765b09..4586177a4d3 100644
--- a/Common/src/geometry/elements/CPRISM6.cpp
+++ b/Common/src/geometry/elements/CPRISM6.cpp
@@ -2,7 +2,7 @@
  * \file CPRISM6.cpp
  * \brief Definition of the 6-node triangular prism element with 6 Gauss points.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/elements/CPYRAM5.cpp b/Common/src/geometry/elements/CPYRAM5.cpp
index e143e90e973..c0f89e95bd4 100644
--- a/Common/src/geometry/elements/CPYRAM5.cpp
+++ b/Common/src/geometry/elements/CPYRAM5.cpp
@@ -2,7 +2,7 @@
  * \file CPYRAM5.cpp
  * \brief Definition of 5-node pyramid element with 5 Gauss points.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/elements/CPYRAM6.cpp b/Common/src/geometry/elements/CPYRAM6.cpp
index fd838369dc8..84257fd97d4 100644
--- a/Common/src/geometry/elements/CPYRAM6.cpp
+++ b/Common/src/geometry/elements/CPYRAM6.cpp
@@ -2,7 +2,7 @@
  * \file CPYRAM6.cpp
  * \brief Definition of 5-node pyramid element with 6 Gauss points.
  * \author T.Dick
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/elements/CQUAD4.cpp b/Common/src/geometry/elements/CQUAD4.cpp
index b62a0bac4d9..f2014f6894e 100644
--- a/Common/src/geometry/elements/CQUAD4.cpp
+++ b/Common/src/geometry/elements/CQUAD4.cpp
@@ -2,7 +2,7 @@
  * \file CQUAD4.cpp
  * \brief Definition of the 4-node quadrilateral element with 4 Gauss points.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/elements/CTETRA1.cpp b/Common/src/geometry/elements/CTETRA1.cpp
index 8a8a98fef6d..7fc967ba383 100644
--- a/Common/src/geometry/elements/CTETRA1.cpp
+++ b/Common/src/geometry/elements/CTETRA1.cpp
@@ -2,7 +2,7 @@
  * \file CTETRA1.cpp
  * \brief Definition of 4-node tetra element with 1 Gauss point.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/elements/CTETRA4.cpp b/Common/src/geometry/elements/CTETRA4.cpp
index fd4131ef852..30675b590d7 100644
--- a/Common/src/geometry/elements/CTETRA4.cpp
+++ b/Common/src/geometry/elements/CTETRA4.cpp
@@ -2,7 +2,7 @@
  * \file CTETRA4.cpp
  * \brief Definition of 4-node tetrahedral element with 4 Gauss point.
  * \author T. Dick
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/elements/CTRIA1.cpp b/Common/src/geometry/elements/CTRIA1.cpp
index bc71226c9ff..dc2a8835a47 100644
--- a/Common/src/geometry/elements/CTRIA1.cpp
+++ b/Common/src/geometry/elements/CTRIA1.cpp
@@ -2,7 +2,7 @@
  * \file CTRIA1.cpp
  * \brief Definition of the 3-node triangular element with one Gauss point.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/elements/CTRIA3.cpp b/Common/src/geometry/elements/CTRIA3.cpp
index 5e486d3aa79..cdc2750b1d0 100644
--- a/Common/src/geometry/elements/CTRIA3.cpp
+++ b/Common/src/geometry/elements/CTRIA3.cpp
@@ -2,7 +2,7 @@
  * \file CTRIA3.cpp
  * \brief Definition of the 3-node triangular element with three Gauss points.
  * \author T. Dick
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/meshreader/CBoxMeshReaderFVM.cpp b/Common/src/geometry/meshreader/CBoxMeshReaderFVM.cpp
index fea9929f705..9e0e6b571cc 100644
--- a/Common/src/geometry/meshreader/CBoxMeshReaderFVM.cpp
+++ b/Common/src/geometry/meshreader/CBoxMeshReaderFVM.cpp
@@ -3,7 +3,7 @@
  * \brief Reads a 3D box grid into linear partitions for the
  *        finite volume solver (FVM).
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/meshreader/CCGNSMeshReaderFVM.cpp b/Common/src/geometry/meshreader/CCGNSMeshReaderFVM.cpp
index 2799e3ae838..3d07be19cc9 100644
--- a/Common/src/geometry/meshreader/CCGNSMeshReaderFVM.cpp
+++ b/Common/src/geometry/meshreader/CCGNSMeshReaderFVM.cpp
@@ -3,7 +3,7 @@
  * \brief Class that reads a single zone of a CGNS mesh file from disk into
  *        linear partitions across all ranks.
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/meshreader/CMeshReaderFVM.cpp b/Common/src/geometry/meshreader/CMeshReaderFVM.cpp
index 4a4e0caaf29..b3f51710768 100644
--- a/Common/src/geometry/meshreader/CMeshReaderFVM.cpp
+++ b/Common/src/geometry/meshreader/CMeshReaderFVM.cpp
@@ -3,7 +3,7 @@
  * \brief Helper class that provides the counts for each rank in a linear
  *        partitioning given the global count as input.
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/meshreader/CRectangularMeshReaderFVM.cpp b/Common/src/geometry/meshreader/CRectangularMeshReaderFVM.cpp
index 3b6c98bdf59..7c337782d5a 100644
--- a/Common/src/geometry/meshreader/CRectangularMeshReaderFVM.cpp
+++ b/Common/src/geometry/meshreader/CRectangularMeshReaderFVM.cpp
@@ -3,7 +3,7 @@
  * \brief Reads a 2D rectangular grid into linear partitions for the
  *        finite volume solver (FVM).
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/meshreader/CSU2ASCIIMeshReaderFVM.cpp b/Common/src/geometry/meshreader/CSU2ASCIIMeshReaderFVM.cpp
index c4c84e4c458..4dc3f4d343e 100644
--- a/Common/src/geometry/meshreader/CSU2ASCIIMeshReaderFVM.cpp
+++ b/Common/src/geometry/meshreader/CSU2ASCIIMeshReaderFVM.cpp
@@ -3,7 +3,7 @@
  * \brief Reads a native SU2 ASCII grid into linear partitions for the
  *        finite volume solver (FVM).
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/primal_grid/CHexahedron.cpp b/Common/src/geometry/primal_grid/CHexahedron.cpp
index acd40a714ed..1dcaa3647dd 100644
--- a/Common/src/geometry/primal_grid/CHexahedron.cpp
+++ b/Common/src/geometry/primal_grid/CHexahedron.cpp
@@ -2,7 +2,7 @@
  * \file CHexahedron.cpp
  * \brief Main classes for defining the primal grid elements
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/primal_grid/CLine.cpp b/Common/src/geometry/primal_grid/CLine.cpp
index 9761fb8b2e5..318866865da 100644
--- a/Common/src/geometry/primal_grid/CLine.cpp
+++ b/Common/src/geometry/primal_grid/CLine.cpp
@@ -2,7 +2,7 @@
  * \file CLine.cpp
  * \brief Main classes for defining the primal grid elements
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/primal_grid/CPrimalGrid.cpp b/Common/src/geometry/primal_grid/CPrimalGrid.cpp
index e7ce4e2ef21..2d301454d57 100644
--- a/Common/src/geometry/primal_grid/CPrimalGrid.cpp
+++ b/Common/src/geometry/primal_grid/CPrimalGrid.cpp
@@ -2,7 +2,7 @@
  * \file CPrimalGrid.cpp
  * \brief Main classes for defining the primal grid elements
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/primal_grid/CPrimalGridBoundFEM.cpp b/Common/src/geometry/primal_grid/CPrimalGridBoundFEM.cpp
index e813a8c6679..5b22e7d4b3d 100644
--- a/Common/src/geometry/primal_grid/CPrimalGridBoundFEM.cpp
+++ b/Common/src/geometry/primal_grid/CPrimalGridBoundFEM.cpp
@@ -2,7 +2,7 @@
  * \file CPrimalGridBoundFEM.cpp
  * \brief Main classes for defining the primal grid elements
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/primal_grid/CPrimalGridFEM.cpp b/Common/src/geometry/primal_grid/CPrimalGridFEM.cpp
index 47eb459c4bc..09ab5003815 100644
--- a/Common/src/geometry/primal_grid/CPrimalGridFEM.cpp
+++ b/Common/src/geometry/primal_grid/CPrimalGridFEM.cpp
@@ -2,7 +2,7 @@
  * \file CPrimalGridFEM.cpp
  * \brief Main classes for defining the primal grid elements
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/primal_grid/CPrism.cpp b/Common/src/geometry/primal_grid/CPrism.cpp
index e3f381e2920..9baa19871be 100644
--- a/Common/src/geometry/primal_grid/CPrism.cpp
+++ b/Common/src/geometry/primal_grid/CPrism.cpp
@@ -2,7 +2,7 @@
  * \file CPrism.cpp
  * \brief Main classes for defining the primal grid elements
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/primal_grid/CPyramid.cpp b/Common/src/geometry/primal_grid/CPyramid.cpp
index f7a94f14784..b91d82d90c3 100644
--- a/Common/src/geometry/primal_grid/CPyramid.cpp
+++ b/Common/src/geometry/primal_grid/CPyramid.cpp
@@ -2,7 +2,7 @@
  * \file CPyramid.cpp
  * \brief Main classes for defining the primal grid elements
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/primal_grid/CQuadrilateral.cpp b/Common/src/geometry/primal_grid/CQuadrilateral.cpp
index aff35ab9056..cc6bda8c146 100644
--- a/Common/src/geometry/primal_grid/CQuadrilateral.cpp
+++ b/Common/src/geometry/primal_grid/CQuadrilateral.cpp
@@ -2,7 +2,7 @@
  * \file CQuadrilateral.cpp
  * \brief Main classes for defining the primal grid elements
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/primal_grid/CTetrahedron.cpp b/Common/src/geometry/primal_grid/CTetrahedron.cpp
index b8bfc1f73c9..42ac28b95a4 100644
--- a/Common/src/geometry/primal_grid/CTetrahedron.cpp
+++ b/Common/src/geometry/primal_grid/CTetrahedron.cpp
@@ -2,7 +2,7 @@
  * \file CTetrahedron.cpp
  * \brief Main classes for defining the primal grid elements
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/primal_grid/CTriangle.cpp b/Common/src/geometry/primal_grid/CTriangle.cpp
index d8c4c3cf5b6..76a6b66e888 100644
--- a/Common/src/geometry/primal_grid/CTriangle.cpp
+++ b/Common/src/geometry/primal_grid/CTriangle.cpp
@@ -2,7 +2,7 @@
  * \file CTriangle.cpp
  * \brief Main classes for defining the primal grid elements
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/primal_grid/CVertexMPI.cpp b/Common/src/geometry/primal_grid/CVertexMPI.cpp
index 260ba776d5d..845ded95ce5 100644
--- a/Common/src/geometry/primal_grid/CVertexMPI.cpp
+++ b/Common/src/geometry/primal_grid/CVertexMPI.cpp
@@ -2,7 +2,7 @@
  * \file CVertexMPI.cpp
  * \brief Main classes for defining the primal grid elements
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/graph_coloring_structure.cpp b/Common/src/graph_coloring_structure.cpp
index d9599f8e59e..80c9d74e143 100644
--- a/Common/src/graph_coloring_structure.cpp
+++ b/Common/src/graph_coloring_structure.cpp
@@ -2,7 +2,7 @@
  * \file graph_coloring_structure.cpp
  * \brief Functions used to carry out the coloring of a given graph.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/grid_movement/CBSplineBlending.cpp b/Common/src/grid_movement/CBSplineBlending.cpp
index 8b407628248..32d5b01aa1b 100644
--- a/Common/src/grid_movement/CBSplineBlending.cpp
+++ b/Common/src/grid_movement/CBSplineBlending.cpp
@@ -2,7 +2,7 @@
  * \file CBSplineBlending.cpp
  * \brief Subroutines for B-Spline blening for FFDs
  * \author F. Palacios, T. Economon, S. Padron
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/grid_movement/CBezierBlending.cpp b/Common/src/grid_movement/CBezierBlending.cpp
index dce8649eb0e..5b30eca8641 100644
--- a/Common/src/grid_movement/CBezierBlending.cpp
+++ b/Common/src/grid_movement/CBezierBlending.cpp
@@ -2,7 +2,7 @@
  * \file CBezierBlending.cpp
  * \brief Subroutines for Bezier blending for FFDs
  * \author F. Palacios, T. Economon, S. Padron
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/grid_movement/CFreeFormBlending.cpp b/Common/src/grid_movement/CFreeFormBlending.cpp
index 0bd6b1b0fca..c0b2a7f2ebe 100644
--- a/Common/src/grid_movement/CFreeFormBlending.cpp
+++ b/Common/src/grid_movement/CFreeFormBlending.cpp
@@ -2,7 +2,7 @@
  * \file CFreeFormBlending.cpp
  * \brief Parent class for FFD Blending functions
  * \author F. Palacios, T. Economon, S. Padron
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/grid_movement/CFreeFormDefBox.cpp b/Common/src/grid_movement/CFreeFormDefBox.cpp
index 9a817df8ea3..d9e959ef105 100644
--- a/Common/src/grid_movement/CFreeFormDefBox.cpp
+++ b/Common/src/grid_movement/CFreeFormDefBox.cpp
@@ -2,7 +2,7 @@
  * \file CFreeFormDefBox.cpp
  * \brief Subroutines for handling Free-Form Deformation Boxes
  * \author F. Palacios, T. Economon, S. Padron
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/grid_movement/CGridMovement.cpp b/Common/src/grid_movement/CGridMovement.cpp
index ed3b00c3eb0..82b7f193e5c 100644
--- a/Common/src/grid_movement/CGridMovement.cpp
+++ b/Common/src/grid_movement/CGridMovement.cpp
@@ -2,7 +2,7 @@
  * \file CGridMovement.cpp
  * \brief Parent class for grid movement classes
  * \author F. Palacios, T. Economon, S. Padron
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/grid_movement/CSurfaceMovement.cpp b/Common/src/grid_movement/CSurfaceMovement.cpp
index 5bfa600280f..4087a3d2ce0 100644
--- a/Common/src/grid_movement/CSurfaceMovement.cpp
+++ b/Common/src/grid_movement/CSurfaceMovement.cpp
@@ -2,7 +2,7 @@
  * \file CSurfaceMovement.cpp
  * \brief Subroutines for moving mesh surface elements
  * \author F. Palacios, T. Economon, S. Padron
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/grid_movement/CVolumetricMovement.cpp b/Common/src/grid_movement/CVolumetricMovement.cpp
index 6cd8b1fc0f0..189e474ca4f 100644
--- a/Common/src/grid_movement/CVolumetricMovement.cpp
+++ b/Common/src/grid_movement/CVolumetricMovement.cpp
@@ -2,7 +2,7 @@
  * \file CVolumetricMovement.cpp
  * \brief Subroutines for moving mesh volume elements
  * \author F. Palacios, T. Economon, S. Padron
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/interface_interpolation/CInterpolator.cpp b/Common/src/interface_interpolation/CInterpolator.cpp
index 620c5122de0..7be9c8eaf49 100644
--- a/Common/src/interface_interpolation/CInterpolator.cpp
+++ b/Common/src/interface_interpolation/CInterpolator.cpp
@@ -2,7 +2,7 @@
  * \file CInterpolator.cpp
  * \brief Definition of the base class for interface interpolation.
  * \author H. Kline
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/interface_interpolation/CInterpolatorFactory.cpp b/Common/src/interface_interpolation/CInterpolatorFactory.cpp
index b2693e1791c..1998d663aa4 100644
--- a/Common/src/interface_interpolation/CInterpolatorFactory.cpp
+++ b/Common/src/interface_interpolation/CInterpolatorFactory.cpp
@@ -1,7 +1,7 @@
 /*!
  * \file CInterpolatorFactory.cpp
  * \brief Factory to generate interpolator objects.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/interface_interpolation/CIsoparametric.cpp b/Common/src/interface_interpolation/CIsoparametric.cpp
index c4101e143f0..f81499e0f55 100644
--- a/Common/src/interface_interpolation/CIsoparametric.cpp
+++ b/Common/src/interface_interpolation/CIsoparametric.cpp
@@ -2,7 +2,7 @@
  * \file CIsoparametric.cpp
  * \brief Implementation isoparametric interpolation (using FE shape functions).
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/interface_interpolation/CMirror.cpp b/Common/src/interface_interpolation/CMirror.cpp
index d3b32caac1f..1a80bc0938b 100644
--- a/Common/src/interface_interpolation/CMirror.cpp
+++ b/Common/src/interface_interpolation/CMirror.cpp
@@ -2,7 +2,7 @@
  * \file CMirror.cpp
  * \brief Implementation of mirror interpolation (conservative approach in FSI problems).
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/interface_interpolation/CNearestNeighbor.cpp b/Common/src/interface_interpolation/CNearestNeighbor.cpp
index ed4f1dbb6f3..3eb67377a82 100644
--- a/Common/src/interface_interpolation/CNearestNeighbor.cpp
+++ b/Common/src/interface_interpolation/CNearestNeighbor.cpp
@@ -2,7 +2,7 @@
  * \file CNearestNeighbor.cpp
  * \brief Implementation of nearest neighbor interpolation.
  * \author H. Kline
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/interface_interpolation/CRadialBasisFunction.cpp b/Common/src/interface_interpolation/CRadialBasisFunction.cpp
index cbb28fb968e..94b9cb5ebd2 100644
--- a/Common/src/interface_interpolation/CRadialBasisFunction.cpp
+++ b/Common/src/interface_interpolation/CRadialBasisFunction.cpp
@@ -2,7 +2,7 @@
  * \file CRadialBasisFunction.cpp
  * \brief Implementation of RBF interpolation.
  * \author Joel Ho, P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/interface_interpolation/CSlidingMesh.cpp b/Common/src/interface_interpolation/CSlidingMesh.cpp
index 11a73075cf5..6e1f3515624 100644
--- a/Common/src/interface_interpolation/CSlidingMesh.cpp
+++ b/Common/src/interface_interpolation/CSlidingMesh.cpp
@@ -2,7 +2,7 @@
  * \file CSlidingMesh.cpp
  * \brief Implementation of sliding mesh interpolation.
  * \author H. Kline
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/linear_algebra/CPastixWrapper.cpp b/Common/src/linear_algebra/CPastixWrapper.cpp
index 71910e9ad11..e6adda91df6 100644
--- a/Common/src/linear_algebra/CPastixWrapper.cpp
+++ b/Common/src/linear_algebra/CPastixWrapper.cpp
@@ -3,7 +3,7 @@
  * \brief An interface to the INRIA solver PaStiX
  *        (http://pastix.gforge.inria.fr/files/README-txt.html)
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/linear_algebra/CSysMatrix.cpp b/Common/src/linear_algebra/CSysMatrix.cpp
index dea7835572a..c6616cdd368 100644
--- a/Common/src/linear_algebra/CSysMatrix.cpp
+++ b/Common/src/linear_algebra/CSysMatrix.cpp
@@ -2,7 +2,7 @@
  * \file CSysMatrix.cpp
  * \brief Implementation of the sparse matrix class.
  * \author F. Palacios, A. Bueno, T. Economon, P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -40,7 +40,6 @@ CSysMatrix<ScalarType>::CSysMatrix() :
   nPoint = nPointDomain = nVar = nEqn = 0;
   nnz = nnz_ilu = 0;
   ilu_fill_in = 0;
-  nLinelet = 0;
 
   omp_partitions    = nullptr;
 
@@ -883,17 +882,13 @@ void CSysMatrix<ScalarType>::ComputeLU_SGSPreconditioner(const CSysVector<Scalar
     const auto row_end = omp_partitions[thread+1];
     if (begin == row_end) continue;
 
-    /*--- On the last thread partition the upper
-     *    product should consider halo columns. ---*/
-    const auto col_end = (row_end==nPointDomain)? nPoint : row_end;
-
     ScalarType up_prod[MAXNVAR], dia_prod[MAXNVAR];
 
     for (auto iPoint = row_end; iPoint > begin;) {
       iPoint--; // because of unsigned type
       auto idx = iPoint*nVar;
       DiagonalProduct(prod, iPoint, dia_prod);          // Compute D.x*
-      UpperProduct(prod, iPoint, col_end, up_prod);     // Compute U.x_(n+1)
+      UpperProduct(prod, iPoint, row_end, up_prod);     // Compute U.x_(n+1)
       VectorSubtraction(dia_prod, up_prod, &prod[idx]); // Compute y = D.x*-U.x_(n+1)
       Gauss_Elimination(iPoint, &prod[idx]);            // Solve D.x* = y
     }
@@ -908,168 +903,33 @@ void CSysMatrix<ScalarType>::ComputeLU_SGSPreconditioner(const CSysVector<Scalar
 }
 
 template<class ScalarType>
-unsigned long CSysMatrix<ScalarType>::BuildLineletPreconditioner(CGeometry *geometry, const CConfig *config) {
-
-  assert(omp_get_thread_num()==0 && "Linelet preconditioner cannot be built by multiple threads.");
+void CSysMatrix<ScalarType>::BuildLineletPreconditioner(const CGeometry *geometry, const CConfig *config) {
 
-  bool add_point;
-  unsigned long iEdge, iPoint, jPoint, index_Point, iLinelet, iVertex, next_Point, counter, iElem;
-  unsigned short iMarker, iNode;
-  su2double alpha = 0.9, weight, max_weight, area, volume_iPoint, volume_jPoint;
-  const su2double* normal;
-  unsigned long Local_nPoints, Local_nLineLets, Global_nPoints, Global_nLineLets, max_nElem;
+  BuildJacobiPreconditioner();
 
-  /*--- Memory allocation --*/
+  /*--- Allocate working vectors if not done yet. ---*/
+  if (!LineletUpper.empty()) return;
 
-  vector<bool> check_Point(nPoint,true);
+  const auto nThreads = omp_get_max_threads();
 
-  LineletBool.clear();
-  LineletBool.resize(nPoint,false);
-
-  nLinelet = 0;
-  for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-    if (config->GetSolid_Wall(iMarker) ||
-        (config->GetMarker_All_KindBC(iMarker) == DISPLACEMENT_BOUNDARY)) {
-      nLinelet += geometry->nVertex[iMarker];
+  BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
+    const auto& li = geometry->GetLineletInfo(config);
+    if (!li.linelets.empty()) {
+      LineletUpper.resize(nThreads);
+      LineletVector.resize(nThreads);
+      LineletInvDiag.resize(nThreads);
     }
   }
+  END_SU2_OMP_SAFE_GLOBAL_ACCESS
 
-  /*--- If the domain contains well defined Linelets ---*/
-
-  if (nLinelet != 0) {
-
-    /*--- Basic initial allocation ---*/
-
-    LineletPoint.resize(nLinelet);
-
-    /*--- Define the basic linelets, starting from each vertex ---*/
-
-    iLinelet = 0;
-
-    for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-      if (config->GetSolid_Wall(iMarker) ||
-          (config->GetMarker_All_KindBC(iMarker) == DISPLACEMENT_BOUNDARY))
-      {
-        for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
-          iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
-          LineletPoint[iLinelet].push_back(iPoint);
-          check_Point[iPoint] = false;
-          iLinelet++;
-        }
-      }
-    }
-
-    /*--- Create the linelet structure ---*/
-
-    iLinelet = 0;
-
-    do {
-
-      index_Point = 0;
-
-      do {
-
-        /*--- Compute the value of the max weight ---*/
-
-        iPoint = LineletPoint[iLinelet][index_Point];
-        max_weight = 0.0;
-        for (iNode = 0; iNode < geometry->nodes->GetnPoint(iPoint); iNode++) {
-          jPoint = geometry->nodes->GetPoint(iPoint, iNode);
-          if ((check_Point[jPoint]) && geometry->nodes->GetDomain(jPoint)) {
-            iEdge = geometry->FindEdge(iPoint, jPoint);
-            normal = geometry->edges->GetNormal(iEdge);
-            if (geometry->GetnDim() == 3) area = sqrt(normal[0]*normal[0]+normal[1]*normal[1]+normal[2]*normal[2]);
-            else area = sqrt(normal[0]*normal[0]+normal[1]*normal[1]);
-            volume_iPoint = geometry->nodes->GetVolume(iPoint);
-            volume_jPoint = geometry->nodes->GetVolume(jPoint);
-            weight = 0.5*area*((1.0/volume_iPoint)+(1.0/volume_jPoint));
-            max_weight = max(max_weight, weight);
-          }
-        }
-
-        /*--- Verify if any face of the control volume must be added ---*/
-
-        add_point = false;
-        counter = 0;
-        next_Point = geometry->nodes->GetPoint(iPoint, 0);
-        for (iNode = 0; iNode < geometry->nodes->GetnPoint(iPoint); iNode++) {
-          jPoint = geometry->nodes->GetPoint(iPoint, iNode);
-          iEdge = geometry->FindEdge(iPoint, jPoint);
-          normal = geometry->edges->GetNormal(iEdge);
-          if (geometry->GetnDim() == 3) area = sqrt(normal[0]*normal[0]+normal[1]*normal[1]+normal[2]*normal[2]);
-          else area = sqrt(normal[0]*normal[0]+normal[1]*normal[1]);
-          volume_iPoint = geometry->nodes->GetVolume(iPoint);
-          volume_jPoint = geometry->nodes->GetVolume(jPoint);
-          weight = 0.5*area*((1.0/volume_iPoint)+(1.0/volume_jPoint));
-          if (((check_Point[jPoint]) && (weight/max_weight > alpha) && (geometry->nodes->GetDomain(jPoint))) &&
-              ((index_Point == 0) || ((index_Point > 0) && (jPoint != LineletPoint[iLinelet][index_Point-1])))) {
-            add_point = true;
-            next_Point = jPoint;
-            counter++;
-          }
-        }
-
-        /*--- We have arrived to an isotropic zone ---*/
-
-        if (counter > 1) add_point = false;
-
-        /*--- Add a typical point to the linelet, no leading edge ---*/
-
-        if (add_point) {
-          LineletPoint[iLinelet].push_back(next_Point);
-          check_Point[next_Point] = false;
-          index_Point++;
-        }
-
-      } while (add_point);
-      iLinelet++;
-    } while (iLinelet < nLinelet);
-
-    /*--- Identify the points that belong to a Linelet ---*/
-
-    for (iLinelet = 0; iLinelet < nLinelet; iLinelet++) {
-      for (iElem = 0; iElem < LineletPoint[iLinelet].size(); iElem++) {
-        iPoint = LineletPoint[iLinelet][iElem];
-        LineletBool[iPoint] = true;
-      }
-    }
-
-    /*--- Identify the maximum number of elements in a Linelet ---*/
-
-    max_nElem = LineletPoint[0].size();
-    for (iLinelet = 1; iLinelet < nLinelet; iLinelet++)
-      if (LineletPoint[iLinelet].size() > max_nElem)
-        max_nElem = LineletPoint[iLinelet].size();
-
-  }
-
-  /*--- The domain doesn't have well defined linelets ---*/
-
-  else {
-
-    max_nElem = 0;
-
-  }
-
-  /*--- Screen output ---*/
-
-  Local_nPoints = 0;
-  for (iLinelet = 0; iLinelet < nLinelet; iLinelet++) {
-    Local_nPoints += LineletPoint[iLinelet].size();
+  SU2_OMP_FOR_STAT(1)
+  for (int iThread = 0; iThread < nThreads; ++iThread) {
+    const auto size = CGeometry::CLineletInfo::MAX_LINELET_POINTS;
+    LineletUpper[iThread].resize(size, nullptr);
+    LineletVector[iThread].resize(size * nVar, 0.0);
+    LineletInvDiag[iThread].resize(size * nVar * nVar, 0.0);
   }
-  Local_nLineLets = nLinelet;
-
-  SU2_MPI::Allreduce(&Local_nPoints, &Global_nPoints, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
-  SU2_MPI::Allreduce(&Local_nLineLets, &Global_nLineLets, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
-
-  /*--- Memory allocation --*/
-
-  LineletUpper.resize(omp_get_max_threads(), vector<const ScalarType*>(max_nElem,nullptr));
-  LineletVector.resize(omp_get_max_threads(), vector<ScalarType>(max_nElem*nVar,0.0));
-  LineletInvDiag.resize(omp_get_max_threads(), vector<ScalarType>(max_nElem*nVar*nVar,0.0));
-
-  return (unsigned long)(passivedouble(Global_nPoints) / Global_nLineLets);
-
+  END_SU2_OMP_FOR
 }
 
 template<class ScalarType>
@@ -1078,32 +938,34 @@ void CSysMatrix<ScalarType>::ComputeLineletPreconditioner(const CSysVector<Scala
   /*--- Coherent view of vectors. ---*/
   SU2_OMP_BARRIER
 
-  /*--- Jacobi preconditioning where there is no linelet ---*/
+  const auto& li = geometry->GetLineletInfo(config);
+
+  /*--- Jacobi preconditioning where there are no linelets. ---*/
 
   SU2_OMP_FOR_(schedule(dynamic,omp_heavy_size) SU2_NOWAIT)
   for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++)
-    if (!LineletBool[iPoint])
+    if (li.lineletIdx[iPoint] == CGeometry::CLineletInfo::NO_LINELET)
       MatrixVectorProduct(&(invM[iPoint*nVar*nVar]), &vec[iPoint*nVar], &prod[iPoint*nVar]);
   END_SU2_OMP_FOR
 
-  /*--- Solve each linelet using the Thomas algorithm ---*/
+  /*--- Solve the tridiagonal systems for the linelets. ---*/
 
   SU2_OMP_FOR_DYN(1)
-  for (auto iLinelet = 0ul; iLinelet < nLinelet; iLinelet++) {
+  for (auto iLinelet = 0ul; iLinelet < li.linelets.size(); iLinelet++) {
 
     /*--- Get references to the working vectors allocated for this thread. ---*/
 
-    int thread = omp_get_thread_num();
-    vector<const ScalarType*>& lineletUpper = LineletUpper[thread];
-    vector<ScalarType>& lineletInvDiag = LineletInvDiag[thread];
-    vector<ScalarType>& lineletVector = LineletVector[thread];
+    const int thread = omp_get_thread_num();
+    auto& lineletUpper = LineletUpper[thread];
+    auto& lineletInvDiag = LineletInvDiag[thread];
+    auto& lineletVector = LineletVector[thread];
 
     /*--- Initialize the solution vector with the rhs ---*/
 
-    auto nElem = LineletPoint[iLinelet].size();
+    const auto nElem = li.linelets[iLinelet].size();
 
     for (auto iElem = 0ul; iElem < nElem; iElem++) {
-      auto iPoint = LineletPoint[iLinelet][iElem];
+      const auto iPoint = li.linelets[iLinelet][iElem];
       for (auto iVar = 0ul; iVar < nVar; iVar++)
         lineletVector[iElem*nVar+iVar] = vec[iPoint*nVar+iVar];
     }
@@ -1114,22 +976,22 @@ void CSysMatrix<ScalarType>::ComputeLineletPreconditioner(const CSysVector<Scala
     ScalarType aux_block[MAXNVAR*MAXNVAR], aux_vector[MAXNVAR];
 
     /*--- Copy diagonal block for first point in this linelet. ---*/
-    MatrixCopy(&matrix[dia_ptr[LineletPoint[iLinelet][0]]*nVar*nVar],
+    MatrixCopy(&matrix[dia_ptr[li.linelets[iLinelet][0]]*nVar*nVar],
                lineletInvDiag.data());
 
     for (auto iElem = 1ul; iElem < nElem; iElem++) {
 
       /*--- Setup pointers to required matrices and vectors ---*/
-      auto im1Point = LineletPoint[iLinelet][iElem-1];
-      auto iPoint = LineletPoint[iLinelet][iElem];
+      const auto im1Point = li.linelets[iLinelet][iElem-1];
+      const auto iPoint = li.linelets[iLinelet][iElem];
 
-      auto d = &matrix[dia_ptr[iPoint]*nVar*nVar];
-      auto l = GetBlock(iPoint, im1Point);
-      auto u = GetBlock(im1Point, iPoint);
+      const auto* d = &matrix[dia_ptr[iPoint]*nVar*nVar];
+      const auto* l = GetBlock(iPoint, im1Point);
+      const auto* u = GetBlock(im1Point, iPoint);
 
-      auto inv_dm1 = &lineletInvDiag[(iElem-1)*nVar*nVar];
-      auto d_prime = &lineletInvDiag[iElem*nVar*nVar];
-      auto b_prime = &lineletVector[iElem*nVar];
+      auto* inv_dm1 = &lineletInvDiag[(iElem-1)*nVar*nVar];
+      auto* d_prime = &lineletInvDiag[iElem*nVar*nVar];
+      auto* b_prime = &lineletVector[iElem*nVar];
 
       /*--- Invert previous modified diagonal ---*/
       MatrixCopy(inv_dm1, aux_block);
@@ -1157,7 +1019,7 @@ void CSysMatrix<ScalarType>::ComputeLineletPreconditioner(const CSysVector<Scala
 
     /*--- x_i = d_i^{-1}*(b_i - u_i*x_{i+1}) ---*/
     for (auto iElem = nElem-1; iElem > 0; --iElem) {
-      auto inv_dm1 = &lineletInvDiag[(iElem-1)*nVar*nVar];
+      const auto* inv_dm1 = &lineletInvDiag[(iElem-1)*nVar*nVar];
       MatrixVectorProduct(lineletUpper[iElem-1], &lineletVector[iElem*nVar], aux_vector);
       VectorSubtraction(&lineletVector[(iElem-1)*nVar], aux_vector, aux_vector);
       MatrixVectorProduct(inv_dm1, aux_vector, &lineletVector[(iElem-1)*nVar]);
@@ -1166,7 +1028,7 @@ void CSysMatrix<ScalarType>::ComputeLineletPreconditioner(const CSysVector<Scala
     /*--- Copy results to product vector ---*/
 
     for (auto iElem = 0ul; iElem < nElem; iElem++) {
-      auto iPoint = LineletPoint[iLinelet][iElem];
+      const auto iPoint = li.linelets[iLinelet][iElem];
       for (auto iVar = 0ul; iVar < nVar; iVar++)
         prod[iPoint*nVar+iVar] = lineletVector[iElem*nVar+iVar];
     }
diff --git a/Common/src/linear_algebra/CSysSolve.cpp b/Common/src/linear_algebra/CSysSolve.cpp
index 54406fdfc8c..f40b3dfa6d1 100644
--- a/Common/src/linear_algebra/CSysSolve.cpp
+++ b/Common/src/linear_algebra/CSysSolve.cpp
@@ -2,7 +2,7 @@
  * \file CSysSolve.cpp
  * \brief Main classes required for solving linear systems of equations
  * \author J. Hicken, F. Palacios, T. Economon, P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/linear_algebra/CSysSolve_b.cpp b/Common/src/linear_algebra/CSysSolve_b.cpp
index c381eb26d39..060b884dd47 100644
--- a/Common/src/linear_algebra/CSysSolve_b.cpp
+++ b/Common/src/linear_algebra/CSysSolve_b.cpp
@@ -2,7 +2,7 @@
  * \file CSysSolve_b.cpp
  * \brief Routines for the linear solver used in the reverse sweep of AD.
  * \author T. Albring, J. Blühdorn
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/linear_algebra/CSysVector.cpp b/Common/src/linear_algebra/CSysVector.cpp
index 4afadf9413b..c7f831d970d 100644
--- a/Common/src/linear_algebra/CSysVector.cpp
+++ b/Common/src/linear_algebra/CSysVector.cpp
@@ -2,7 +2,7 @@
  * \file CSysVector.cpp
  * \brief Implementation and explicit instantiations of CSysVector.
  * \author P. Gomes, F. Palacios, J. Hicken, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/linear_algebra/blas_structure.cpp b/Common/src/linear_algebra/blas_structure.cpp
index 896523fe47f..e18182388d4 100644
--- a/Common/src/linear_algebra/blas_structure.cpp
+++ b/Common/src/linear_algebra/blas_structure.cpp
@@ -3,7 +3,7 @@
  * \brief Implementation of the functions that either simulate BLAS functionality
           or interface to an actual BLAS implementation.
  * \author E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/C1DInterpolation.cpp b/Common/src/toolboxes/C1DInterpolation.cpp
index f7ea3d7d31c..e363a13fe7e 100644
--- a/Common/src/toolboxes/C1DInterpolation.cpp
+++ b/Common/src/toolboxes/C1DInterpolation.cpp
@@ -2,7 +2,7 @@
  * \file C1DInterpolation.cpp
  * \brief Classes for 1D interpolation.
  * \author Aman Baig, P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/CLinearPartitioner.cpp b/Common/src/toolboxes/CLinearPartitioner.cpp
index 3c6bc37b08c..b09a45548d1 100644
--- a/Common/src/toolboxes/CLinearPartitioner.cpp
+++ b/Common/src/toolboxes/CLinearPartitioner.cpp
@@ -3,7 +3,7 @@
  * \brief Helper class that provides the counts for each rank in a linear
  *        partitioning given the global count as input.
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/CSquareMatrixCM.cpp b/Common/src/toolboxes/CSquareMatrixCM.cpp
index 9103f1c9a82..bf33c75b5f1 100644
--- a/Common/src/toolboxes/CSquareMatrixCM.cpp
+++ b/Common/src/toolboxes/CSquareMatrixCM.cpp
@@ -2,7 +2,7 @@
  * \file CSquareMatrixCM.cpp
  * \brief Implementation of dense matrix helper class in Column Major order (see hpp).
  * \author Edwin van der Weide, Pedro Gomes.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/CSymmetricMatrix.cpp b/Common/src/toolboxes/CSymmetricMatrix.cpp
index 002f6c5055a..70453dd6b57 100644
--- a/Common/src/toolboxes/CSymmetricMatrix.cpp
+++ b/Common/src/toolboxes/CSymmetricMatrix.cpp
@@ -2,7 +2,7 @@
  * \file CSymmetricMatrix.cpp
  * \brief Implementation of dense symmetric matrix helper class (see hpp).
  * \author Joel Ho, P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CIncTGVSolution.cpp b/Common/src/toolboxes/MMS/CIncTGVSolution.cpp
index 77fb2869144..10b219fb1eb 100644
--- a/Common/src/toolboxes/MMS/CIncTGVSolution.cpp
+++ b/Common/src/toolboxes/MMS/CIncTGVSolution.cpp
@@ -2,7 +2,7 @@
  * \file CIncTGVSolution.cpp
  * \brief Implementations of the member functions of CIncTGVSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CInviscidVortexSolution.cpp b/Common/src/toolboxes/MMS/CInviscidVortexSolution.cpp
index 599361712b4..53655c0c0b0 100644
--- a/Common/src/toolboxes/MMS/CInviscidVortexSolution.cpp
+++ b/Common/src/toolboxes/MMS/CInviscidVortexSolution.cpp
@@ -2,7 +2,7 @@
  * \file CInviscidVortexSolution.cpp
  * \brief Implementations of the member functions of CInviscidVortexSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CMMSIncEulerSolution.cpp b/Common/src/toolboxes/MMS/CMMSIncEulerSolution.cpp
index ea8f3d5274b..9635364caf6 100644
--- a/Common/src/toolboxes/MMS/CMMSIncEulerSolution.cpp
+++ b/Common/src/toolboxes/MMS/CMMSIncEulerSolution.cpp
@@ -2,7 +2,7 @@
  * \file CMMSIncEulerSolution.cpp
  * \brief Implementations of the member functions of CMMSIncEulerSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CMMSIncNSSolution.cpp b/Common/src/toolboxes/MMS/CMMSIncNSSolution.cpp
index bf3c8cd908c..29723df00d4 100644
--- a/Common/src/toolboxes/MMS/CMMSIncNSSolution.cpp
+++ b/Common/src/toolboxes/MMS/CMMSIncNSSolution.cpp
@@ -2,7 +2,7 @@
  * \file CMMSIncNSSolution.cpp
  * \brief Implementations of the member functions of CMMSIncNSSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.cpp b/Common/src/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.cpp
index ae5a7d690de..3a1e2b87353 100644
--- a/Common/src/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.cpp
+++ b/Common/src/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.cpp
@@ -2,7 +2,7 @@
  * \file CMMSNSTwoHalfCirclesSolution.cpp
  * \brief Implementations of the member functions of CMMSNSTwoHalfCirclesSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.cpp b/Common/src/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.cpp
index bcfa32544db..6f4394fba6d 100644
--- a/Common/src/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.cpp
+++ b/Common/src/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.cpp
@@ -2,7 +2,7 @@
  * \file CMMSNSTwoHalfSpheresSolution.cpp
  * \brief Implementations of the member functions of CMMSNSTwoHalfSpheresSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolution.cpp b/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolution.cpp
index aade4c9e804..29402ee5c26 100644
--- a/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolution.cpp
+++ b/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolution.cpp
@@ -2,7 +2,7 @@
  * \file CMMSNSUnitQuadSolution.cpp
  * \brief Implementations of the member functions of CMMSNSUnitQuadSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.cpp b/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.cpp
index 0d90b3d7e10..175cbf34ac7 100644
--- a/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.cpp
+++ b/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.cpp
@@ -2,7 +2,7 @@
  * \file CMMSNSUnitQuadSolutionWallBC.cpp
  * \brief Implementations of the member functions of CMMSNSUnitQuadSolutionWallBC.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CNSUnitQuadSolution.cpp b/Common/src/toolboxes/MMS/CNSUnitQuadSolution.cpp
index 9495c5d89aa..420df21258d 100644
--- a/Common/src/toolboxes/MMS/CNSUnitQuadSolution.cpp
+++ b/Common/src/toolboxes/MMS/CNSUnitQuadSolution.cpp
@@ -2,7 +2,7 @@
  * \file CNSUnitQuadSolution.cpp
  * \brief Implementations of the member functions of CNSUnitQuadSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CRinglebSolution.cpp b/Common/src/toolboxes/MMS/CRinglebSolution.cpp
index f5725491515..b559326ed41 100644
--- a/Common/src/toolboxes/MMS/CRinglebSolution.cpp
+++ b/Common/src/toolboxes/MMS/CRinglebSolution.cpp
@@ -2,7 +2,7 @@
  * \file CRinglebSolution.cpp
  * \brief Implementations of the member functions of CRinglebSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CTGVSolution.cpp b/Common/src/toolboxes/MMS/CTGVSolution.cpp
index 737e4b2b96a..758b75899ee 100644
--- a/Common/src/toolboxes/MMS/CTGVSolution.cpp
+++ b/Common/src/toolboxes/MMS/CTGVSolution.cpp
@@ -2,7 +2,7 @@
  * \file CTGVSolution.cpp
  * \brief Implementations of the member functions of CTGVSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CUserDefinedSolution.cpp b/Common/src/toolboxes/MMS/CUserDefinedSolution.cpp
index 12370cc5562..8984a7edc75 100644
--- a/Common/src/toolboxes/MMS/CUserDefinedSolution.cpp
+++ b/Common/src/toolboxes/MMS/CUserDefinedSolution.cpp
@@ -2,7 +2,7 @@
  * \file CUserDefinedSolution.cpp
  * \brief Implementations of the member functions of CUserDefinedSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CVerificationSolution.cpp b/Common/src/toolboxes/MMS/CVerificationSolution.cpp
index 3d686b89ae3..b13c30d6fb8 100644
--- a/Common/src/toolboxes/MMS/CVerificationSolution.cpp
+++ b/Common/src/toolboxes/MMS/CVerificationSolution.cpp
@@ -2,7 +2,7 @@
  * \file CVerificationSolution.cpp
  * \brief Implementations of the member functions of CVerificationSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncEulerSolution.py b/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncEulerSolution.py
index 92f18531374..e7e202bead6 100755
--- a/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncEulerSolution.py
+++ b/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncEulerSolution.py
@@ -4,7 +4,7 @@
 #  \brief Python script that generates the source terms for a 
 #         manufactured solution for the incompressible Euler eqns.
 #  \author T. Economon
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncNSSolution.py b/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncNSSolution.py
index 4371bb9124d..4f6be23498e 100755
--- a/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncNSSolution.py
+++ b/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncNSSolution.py
@@ -4,7 +4,7 @@
 #  \brief Python script that generates the source terms for a 
 #         manufactured solution for the incompressible Navier-Stokes eqns.
 #  \author T. Economon
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/Common/src/toolboxes/printing_toolbox.cpp b/Common/src/toolboxes/printing_toolbox.cpp
index 5038c52e8f8..a942684f459 100644
--- a/Common/src/toolboxes/printing_toolbox.cpp
+++ b/Common/src/toolboxes/printing_toolbox.cpp
@@ -2,7 +2,7 @@
  * \file printing_toolbox.cpp
  * \brief Printing tools
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/wall_model.cpp b/Common/src/wall_model.cpp
index e6f816f7b33..afeba736bfa 100644
--- a/Common/src/wall_model.cpp
+++ b/Common/src/wall_model.cpp
@@ -3,7 +3,7 @@
  * \brief File, which contains the implementation for the wall model functions
  *        for large eddy simulations.
  * \author E. van der Weide, T. Economon, P. Urbanczyk
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Docs/docmain.hpp b/Docs/docmain.hpp
index aa13b120141..777967dbd32 100644
--- a/Docs/docmain.hpp
+++ b/Docs/docmain.hpp
@@ -2,7 +2,7 @@
  * \file docmain.hpp
  * \brief This file contains documentation for Doxygen and does not have any significance with respect to C++.
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -26,7 +26,7 @@
  */
 
 /*! 
- * \mainpage SU2 version 7.4.0 "Blackbird"
+ * \mainpage SU2 version 7.5.0 "Blackbird"
  * SU2 suite is an open-source collection of C++ based software tools
  * to perform PDE analysis and PDE constrained optimization.  The toolset is designed with 
  * computational fluid dynamics and aerodynamic shape optimization in mind, but is extensible to
diff --git a/QuickStart/inv_NACA0012.cfg b/QuickStart/inv_NACA0012.cfg
index 8b583c98fd1..d434c88d73e 100644
--- a/QuickStart/inv_NACA0012.cfg
+++ b/QuickStart/inv_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.4.0 "Blackbird"                                                  %
+% File Version 7.5.0 "Blackbird"                                                  %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/README.md b/README.md
index b092a036f17..26b394001df 100644
--- a/README.md
+++ b/README.md
@@ -3,7 +3,7 @@
 </p>
 
 
-# SU2 (ver. 7.4.0 "Blackbird"): The Open-Source CFD Code
+# SU2 (ver. 7.5.0 "Blackbird"): The Open-Source CFD Code
 
 Computational analysis tools have revolutionized the way we design engineering systems, but most established codes are proprietary, unavailable, or prohibitively expensive for many users. The SU2 team is changing this, making multiphysics analysis and design optimization freely available as open-source software and involving everyone in its creation and development. 
 
diff --git a/SU2_CFD/include/CMarkerProfileReaderFVM.hpp b/SU2_CFD/include/CMarkerProfileReaderFVM.hpp
index 14c08252778..742e75ce37e 100644
--- a/SU2_CFD/include/CMarkerProfileReaderFVM.hpp
+++ b/SU2_CFD/include/CMarkerProfileReaderFVM.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CMarkerProfileReaderFVM.
  *        The implementations are in the <i>CMarkerProfileReaderFVM.cpp</i> file.
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/SU2_CFD.hpp b/SU2_CFD/include/SU2_CFD.hpp
index d8f169fd48f..1b56e2aa124 100644
--- a/SU2_CFD/include/SU2_CFD.hpp
+++ b/SU2_CFD/include/SU2_CFD.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines of the code SU2_CFD.
  *        The subroutines and functions are in the <i>SU2_CFD.cpp</i> file.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/definition_structure.hpp b/SU2_CFD/include/definition_structure.hpp
index cf9f959de2c..61317ee7a81 100644
--- a/SU2_CFD/include/definition_structure.hpp
+++ b/SU2_CFD/include/definition_structure.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines used by SU2_CFD.
  *        The subroutines and functions are in the <i>definition_structure.cpp</i> file.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/drivers/CDiscAdjMultizoneDriver.hpp b/SU2_CFD/include/drivers/CDiscAdjMultizoneDriver.hpp
index f3ee345adc4..e501c48eb1d 100644
--- a/SU2_CFD/include/drivers/CDiscAdjMultizoneDriver.hpp
+++ b/SU2_CFD/include/drivers/CDiscAdjMultizoneDriver.hpp
@@ -2,7 +2,7 @@
  * \class CDiscAdjMultizoneDriver.hpp
  * \brief Class for driving adjoint multi-zone problems.
  * \author O. Burghardt, P. Gomes, T. Albring, R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp b/SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp
index 8aec81d2e0e..557162809d1 100644
--- a/SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp
+++ b/SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for driving single or multi-zone problems.
  *        The subroutines and functions are in the <i>driver_structure.cpp</i> file.
  * \author T. Economon, H. Kline, R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -34,7 +34,7 @@
  * \ingroup DiscAdj
  * \brief Class for driving single-zone adjoint solvers.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CDiscAdjSinglezoneDriver : public CSinglezoneDriver {
 protected:
diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index 1e2b5e407ee..efeef08e708 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for driving single or multi-zone problems.
  *        The subroutines and functions are in the <i>driver_structure.cpp</i> file.
  * \author T. Economon, H. Kline, R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/drivers/CDummyDriver.hpp b/SU2_CFD/include/drivers/CDummyDriver.hpp
index 7d71a39c586..9c6616c6e79 100644
--- a/SU2_CFD/include/drivers/CDummyDriver.hpp
+++ b/SU2_CFD/include/drivers/CDummyDriver.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for driving single or multi-zone problems.
  *        The subroutines and functions are in the <i>driver_structure.cpp</i> file.
  * \author T. Economon, H. Kline, R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/drivers/CMultizoneDriver.hpp b/SU2_CFD/include/drivers/CMultizoneDriver.hpp
index c743be2c8f0..866666f4cb7 100644
--- a/SU2_CFD/include/drivers/CMultizoneDriver.hpp
+++ b/SU2_CFD/include/drivers/CMultizoneDriver.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for driving single or multi-zone problems.
  *        The subroutines and functions are in the <i>driver_structure.cpp</i> file.
  * \author T. Economon, H. Kline, R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -35,7 +35,7 @@
  * \ingroup Drivers
  * \brief Class for driving zone-specific iterations.
  * \author R. Sanchez, O. Burghardt
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CMultizoneDriver : public CDriver {
 protected:
diff --git a/SU2_CFD/include/drivers/CSinglezoneDriver.hpp b/SU2_CFD/include/drivers/CSinglezoneDriver.hpp
index 50e65f35abf..3fd469b5ee3 100644
--- a/SU2_CFD/include/drivers/CSinglezoneDriver.hpp
+++ b/SU2_CFD/include/drivers/CSinglezoneDriver.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for driving single or multi-zone problems.
  *        The subroutines and functions are in the <i>driver_structure.cpp</i> file.
  * \author T. Economon, H. Kline, R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -34,7 +34,7 @@
  * \ingroup Drivers
  * \brief Class for driving single-zone solvers.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CSinglezoneDriver : public CDriver {
 protected:
diff --git a/SU2_CFD/include/fluid/CConductivityModel.hpp b/SU2_CFD/include/fluid/CConductivityModel.hpp
index 3eab8712b86..eb8b36f9546 100644
--- a/SU2_CFD/include/fluid/CConductivityModel.hpp
+++ b/SU2_CFD/include/fluid/CConductivityModel.hpp
@@ -2,7 +2,7 @@
  * \file CConductivityModel.hpp
  * \brief Defines an interface class for thermal conductivity models.
  * \author S. Vitale, M. Pini, G. Gori, A. Guardone, P. Colonna, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CConstantConductivity.hpp b/SU2_CFD/include/fluid/CConstantConductivity.hpp
index 8ac9a2e8028..caf4b3115a5 100644
--- a/SU2_CFD/include/fluid/CConstantConductivity.hpp
+++ b/SU2_CFD/include/fluid/CConstantConductivity.hpp
@@ -2,7 +2,7 @@
  * \file CConstantConductivity.hpp
  * \brief Defines a constant laminar thermal conductivity model.
  * \author S. Vitale, M. Pini, G. Gori, A. Guardone, P. Colonna, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CConstantConductivityRANS.hpp b/SU2_CFD/include/fluid/CConstantConductivityRANS.hpp
index c3f83a45eda..70b0bea1ae4 100644
--- a/SU2_CFD/include/fluid/CConstantConductivityRANS.hpp
+++ b/SU2_CFD/include/fluid/CConstantConductivityRANS.hpp
@@ -2,7 +2,7 @@
  * \file CConstantConductivityRANS.hpp
  * \brief Defines a constant conductivity model for RANS problems.
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CConstantDensity.hpp b/SU2_CFD/include/fluid/CConstantDensity.hpp
index d459a22b5a8..16655ee587e 100644
--- a/SU2_CFD/include/fluid/CConstantDensity.hpp
+++ b/SU2_CFD/include/fluid/CConstantDensity.hpp
@@ -2,7 +2,7 @@
  * \file CConstantDensity.hpp
  * \brief Defines the incompressible constant density model.
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CConstantDiffusivity.hpp b/SU2_CFD/include/fluid/CConstantDiffusivity.hpp
index 94fb3620181..3f68eb59647 100644
--- a/SU2_CFD/include/fluid/CConstantDiffusivity.hpp
+++ b/SU2_CFD/include/fluid/CConstantDiffusivity.hpp
@@ -2,7 +2,7 @@
  * \file CConstantDiffusivity.hpp
  * \brief Defines constant mass diffusivity.
  * \author T. Economon, Cristopher Morales Ubal
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CConstantLewisDiffusivity.hpp b/SU2_CFD/include/fluid/CConstantLewisDiffusivity.hpp
index 13886d5278d..646918643eb 100644
--- a/SU2_CFD/include/fluid/CConstantLewisDiffusivity.hpp
+++ b/SU2_CFD/include/fluid/CConstantLewisDiffusivity.hpp
@@ -2,7 +2,7 @@
  * \file CConstantLewisDiffusivity.hpp
  * \brief Defines Constant Lewis mass diffusivity.
  * \author M.Heimgartner, C.Morales
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CConstantPrandtl.hpp b/SU2_CFD/include/fluid/CConstantPrandtl.hpp
index de2aa835175..b268bf61e59 100644
--- a/SU2_CFD/include/fluid/CConstantPrandtl.hpp
+++ b/SU2_CFD/include/fluid/CConstantPrandtl.hpp
@@ -2,7 +2,7 @@
  * \file CConstantPrandtl.hpp
  * \brief Defines a non-constant laminar Prandtl number thermal conductivity model.
  * \author S. Vitale, M. Pini, G. Gori, A. Guardone, P. Colonna, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CConstantPrandtlRANS.hpp b/SU2_CFD/include/fluid/CConstantPrandtlRANS.hpp
index 4dfe5011bdb..9ea7aac705d 100644
--- a/SU2_CFD/include/fluid/CConstantPrandtlRANS.hpp
+++ b/SU2_CFD/include/fluid/CConstantPrandtlRANS.hpp
@@ -2,7 +2,7 @@
  * \file CConstantPrandtlRANS.hpp
  * \brief Defines a non-constant effective thermal conductivity for RANS problems using Prandtl numbers.
  * \author S. Vitale, M. Pini, G. Gori, A. Guardone, P. Colonna, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CConstantSchmidt.hpp b/SU2_CFD/include/fluid/CConstantSchmidt.hpp
index a2c4f524a45..01991492f9f 100644
--- a/SU2_CFD/include/fluid/CConstantSchmidt.hpp
+++ b/SU2_CFD/include/fluid/CConstantSchmidt.hpp
@@ -2,7 +2,7 @@
  * \file CConstantSchmidt.hpp
  * \brief Defines a mass diffusivity model with constant Schmidt numbers.
  * \author S. Vitale, M. Pini, G. Gori, A. Guardone, P. Colonna, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CConstantViscosity.hpp b/SU2_CFD/include/fluid/CConstantViscosity.hpp
index 028e34eb552..5a95be95cca 100644
--- a/SU2_CFD/include/fluid/CConstantViscosity.hpp
+++ b/SU2_CFD/include/fluid/CConstantViscosity.hpp
@@ -2,7 +2,7 @@
  * \file CConstantViscosity.hpp
  * \brief Defines a constant laminar viscosity model.
  * \author S. Vitale, M. Pini, G. Gori, A. Guardone, P. Colonna, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CCoolProp.hpp b/SU2_CFD/include/fluid/CCoolProp.hpp
index 823be270bbb..9d42b8dd8b6 100644
--- a/SU2_CFD/include/fluid/CCoolProp.hpp
+++ b/SU2_CFD/include/fluid/CCoolProp.hpp
@@ -2,7 +2,7 @@
  * \file CCoolProp.hpp
  * \brief Defines the state-of-the-art fluid model from CoolProp library.
  * \author P. Yan, G. Gori, A. Guardone
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CCoolPropConductivity.hpp b/SU2_CFD/include/fluid/CCoolPropConductivity.hpp
index 55e8d2744bf..594ede4a99e 100644
--- a/SU2_CFD/include/fluid/CCoolPropConductivity.hpp
+++ b/SU2_CFD/include/fluid/CCoolPropConductivity.hpp
@@ -2,7 +2,7 @@
  * \file CCoolPropConductivity.hpp
  * \brief Defines laminar thermal conductivity model from CoolProp.
  * \author P.YAn, G. Gori, A. Guardone
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CCoolPropViscosity.hpp b/SU2_CFD/include/fluid/CCoolPropViscosity.hpp
index b4708f2aae6..bf3287d83d8 100644
--- a/SU2_CFD/include/fluid/CCoolPropViscosity.hpp
+++ b/SU2_CFD/include/fluid/CCoolPropViscosity.hpp
@@ -2,7 +2,7 @@
  * \file CCoolPropViscosity.hpp
  * \brief Defines CoolPropviscosity model.
  * \author P.Yan, G. Gori, A. Guardone,
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CDiffusivityModel.hpp b/SU2_CFD/include/fluid/CDiffusivityModel.hpp
index 2db44471082..d9433d3bd6c 100644
--- a/SU2_CFD/include/fluid/CDiffusivityModel.hpp
+++ b/SU2_CFD/include/fluid/CDiffusivityModel.hpp
@@ -2,7 +2,7 @@
  * \file CDiffusivityModel.hpp
  * \brief Interface class for defining mass diffusivity models.
  * \author T. Economon, C. Morales
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CFluidModel.hpp b/SU2_CFD/include/fluid/CFluidModel.hpp
index b57badc99c9..e9444605b45 100644
--- a/SU2_CFD/include/fluid/CFluidModel.hpp
+++ b/SU2_CFD/include/fluid/CFluidModel.hpp
@@ -2,7 +2,7 @@
  * \file CFluidModel.hpp
  * \brief Defines the main fluid model class for thermophysical properties.
  * \author S. Vitale, G. Gori, M. Pini, A. Guardone, P. Colonna, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CFluidScalar.hpp b/SU2_CFD/include/fluid/CFluidScalar.hpp
index 619b869c757..32e0cf5781b 100644
--- a/SU2_CFD/include/fluid/CFluidScalar.hpp
+++ b/SU2_CFD/include/fluid/CFluidScalar.hpp
@@ -2,7 +2,7 @@
  * \file CFluidScalar.hpp
  * \brief  Defines the multicomponent incompressible Ideal Gas model for mixtures.
  * \author T. Economon, Mark Heimgartner, Cristopher Morales Ubal
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CIdealGas.hpp b/SU2_CFD/include/fluid/CIdealGas.hpp
index 95f73894cd0..9c0d2c5409e 100644
--- a/SU2_CFD/include/fluid/CIdealGas.hpp
+++ b/SU2_CFD/include/fluid/CIdealGas.hpp
@@ -2,7 +2,7 @@
  * \file CIdealGas.hpp
  * \brief Defines the ideal gas model.
  * \author S. Vitale, G. Gori, M. Pini, A. Guardone, P. Colonna
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CIncIdealGas.hpp b/SU2_CFD/include/fluid/CIncIdealGas.hpp
index 4a476dab235..7dcde9300c4 100644
--- a/SU2_CFD/include/fluid/CIncIdealGas.hpp
+++ b/SU2_CFD/include/fluid/CIncIdealGas.hpp
@@ -2,7 +2,7 @@
  * \file CIncIdealGas.hpp
  * \brief Defines the incompressible Ideal Gas model.
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CIncIdealGasPolynomial.hpp b/SU2_CFD/include/fluid/CIncIdealGasPolynomial.hpp
index d4edce5fe99..f473fcd2796 100644
--- a/SU2_CFD/include/fluid/CIncIdealGasPolynomial.hpp
+++ b/SU2_CFD/include/fluid/CIncIdealGasPolynomial.hpp
@@ -2,7 +2,7 @@
  * \file CIncIdealGasPolynomial.hpp
  * \brief Defines the incompressible Ideal Gas model with polynomial Cp.
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CMutationTCLib.hpp b/SU2_CFD/include/fluid/CMutationTCLib.hpp
index 355523e58bc..96ca9bd6908 100644
--- a/SU2_CFD/include/fluid/CMutationTCLib.hpp
+++ b/SU2_CFD/include/fluid/CMutationTCLib.hpp
@@ -2,7 +2,7 @@
  * \file CMutationTCLib.hpp
  * \brief Defines the class for the link to Mutation++ ThermoChemistry library.
  * \author C. Garbacz
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CNEMOGas.hpp b/SU2_CFD/include/fluid/CNEMOGas.hpp
index 3eb6828a6cb..eba5fbcc5fa 100644
--- a/SU2_CFD/include/fluid/CNEMOGas.hpp
+++ b/SU2_CFD/include/fluid/CNEMOGas.hpp
@@ -2,7 +2,7 @@
  * \file CNEMOGas.hpp
  * \brief Defines the nonequilibrium gas model.
  * \author C. Garbacz, W. Maier, S. R. Copeland
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CPengRobinson.hpp b/SU2_CFD/include/fluid/CPengRobinson.hpp
index 333b90f6be6..a7f64aef14d 100644
--- a/SU2_CFD/include/fluid/CPengRobinson.hpp
+++ b/SU2_CFD/include/fluid/CPengRobinson.hpp
@@ -2,7 +2,7 @@
  * \file CPengRobinson.hpp
  * \brief Defines the Peng-Robinson model.
  * \author S. Vitale, G. Gori, M. Pini, A. Guardone, P. Colonna
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CPolynomialConductivity.hpp b/SU2_CFD/include/fluid/CPolynomialConductivity.hpp
index d34d923f41b..132732b6f1c 100644
--- a/SU2_CFD/include/fluid/CPolynomialConductivity.hpp
+++ b/SU2_CFD/include/fluid/CPolynomialConductivity.hpp
@@ -2,7 +2,7 @@
  * \file CPolynomialConductivity.hpp
  * \brief Defines a non-constant laminar thermal conductivity using a polynomial function of temperature.
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CPolynomialConductivityRANS.hpp b/SU2_CFD/include/fluid/CPolynomialConductivityRANS.hpp
index 8488fa1fbb3..3b09be6384b 100644
--- a/SU2_CFD/include/fluid/CPolynomialConductivityRANS.hpp
+++ b/SU2_CFD/include/fluid/CPolynomialConductivityRANS.hpp
@@ -3,7 +3,7 @@
  * \brief Defines a non-constant thermal conductivity using a polynomial function of temperature
  *        for RANS problems with the addition of a turbulent component based on a turbulent Prandtl number.
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CPolynomialViscosity.hpp b/SU2_CFD/include/fluid/CPolynomialViscosity.hpp
index b6d54344da8..86a46d645dd 100644
--- a/SU2_CFD/include/fluid/CPolynomialViscosity.hpp
+++ b/SU2_CFD/include/fluid/CPolynomialViscosity.hpp
@@ -2,7 +2,7 @@
  * \file CPolynomialViscosity.hpp
  * \brief Defines a laminar viscosity model as a polynomial function of temperature.
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CSU2TCLib.hpp b/SU2_CFD/include/fluid/CSU2TCLib.hpp
index c0c97d953df..e3d5b5d3b23 100644
--- a/SU2_CFD/include/fluid/CSU2TCLib.hpp
+++ b/SU2_CFD/include/fluid/CSU2TCLib.hpp
@@ -2,7 +2,7 @@
  * \file CSU2TCLib.hpp
  * \brief Defines the classes for different user defined ThermoChemistry libraries.
  * \author C. Garbacz, W. Maier, S. R. Copeland
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CSutherland.hpp b/SU2_CFD/include/fluid/CSutherland.hpp
index 048750adff9..c5896a54fcd 100644
--- a/SU2_CFD/include/fluid/CSutherland.hpp
+++ b/SU2_CFD/include/fluid/CSutherland.hpp
@@ -2,7 +2,7 @@
  * \file CSutherland.hpp
  * \brief Defines Sutherland's Law for laminar viscosity.
  * \author S. Vitale, M. Pini, G. Gori, A. Guardone, P. Colonna, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CVanDerWaalsGas.hpp b/SU2_CFD/include/fluid/CVanDerWaalsGas.hpp
index 4118006117e..c171e36be64 100644
--- a/SU2_CFD/include/fluid/CVanDerWaalsGas.hpp
+++ b/SU2_CFD/include/fluid/CVanDerWaalsGas.hpp
@@ -2,7 +2,7 @@
  * \file CVanDerWaalsGas.hpp
  * \brief Declaration of the Polytropic Van der Waals model.
  * \author S. Vitale, G. Gori, M. Pini, A. Guardone, P. Colonna
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CViscosityModel.hpp b/SU2_CFD/include/fluid/CViscosityModel.hpp
index a7cf00c2154..1e21fe4e0be 100644
--- a/SU2_CFD/include/fluid/CViscosityModel.hpp
+++ b/SU2_CFD/include/fluid/CViscosityModel.hpp
@@ -2,7 +2,7 @@
  * \file CViscosityModel.hpp
  * \brief Interface class for defining laminar viscosity models.
  * \author S. Vitale, M. Pini, G. Gori, A. Guardone, P. Colonna, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/gradients/computeGradientsGreenGauss.hpp b/SU2_CFD/include/gradients/computeGradientsGreenGauss.hpp
index f475e986935..07f79b395b6 100644
--- a/SU2_CFD/include/gradients/computeGradientsGreenGauss.hpp
+++ b/SU2_CFD/include/gradients/computeGradientsGreenGauss.hpp
@@ -4,7 +4,7 @@
  * \note This allows the same implementation to be used for conservative
  *       and primitive variables of any solver.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/gradients/computeGradientsLeastSquares.hpp b/SU2_CFD/include/gradients/computeGradientsLeastSquares.hpp
index c4540ea0a8a..c04e8b6009e 100644
--- a/SU2_CFD/include/gradients/computeGradientsLeastSquares.hpp
+++ b/SU2_CFD/include/gradients/computeGradientsLeastSquares.hpp
@@ -3,7 +3,7 @@
  * \brief Generic implementation of Least-Squares gradient computation.
  * \note This allows the same implementation to be used for conservative
  *       and primitive variables of any solver.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/integration/CFEM_DG_Integration.hpp b/SU2_CFD/include/integration/CFEM_DG_Integration.hpp
index 6ff988d5192..f76edda2079 100644
--- a/SU2_CFD/include/integration/CFEM_DG_Integration.hpp
+++ b/SU2_CFD/include/integration/CFEM_DG_Integration.hpp
@@ -2,7 +2,7 @@
  * \file CFEM_DG_Integration.hpp
  * \brief Declaration of class for integration with the FEM DG solver.
  * \author E. van der Weide, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -32,7 +32,7 @@
  * \ingroup Drivers
  * \brief Class for integration with the FEM DG solver.
  * \author E. van der Weide, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CFEM_DG_Integration final : public CIntegration {
 public:
diff --git a/SU2_CFD/include/integration/CIntegration.hpp b/SU2_CFD/include/integration/CIntegration.hpp
index ab34ad16164..84b43bb04f1 100644
--- a/SU2_CFD/include/integration/CIntegration.hpp
+++ b/SU2_CFD/include/integration/CIntegration.hpp
@@ -2,7 +2,7 @@
  * \file CIntegration.hpp
  * \brief Declaration of the main routines to orchestrate space and time integration.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/integration/CIntegrationFactory.hpp b/SU2_CFD/include/integration/CIntegrationFactory.hpp
index 9d709823e3a..89d11e3aba8 100644
--- a/SU2_CFD/include/integration/CIntegrationFactory.hpp
+++ b/SU2_CFD/include/integration/CIntegrationFactory.hpp
@@ -2,7 +2,7 @@
  * \file CIntegrationFactory.hpp
  * \brief Headers of the CIntegrationFactory class
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/integration/CMultiGridIntegration.hpp b/SU2_CFD/include/integration/CMultiGridIntegration.hpp
index 63b060cb0ea..f4bcb84c5ef 100644
--- a/SU2_CFD/include/integration/CMultiGridIntegration.hpp
+++ b/SU2_CFD/include/integration/CMultiGridIntegration.hpp
@@ -2,7 +2,7 @@
  * \file CMultiGridIntegration.hpp
  * \brief Declaration of class for time integration using a multigrid method.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/integration/CNewtonIntegration.hpp b/SU2_CFD/include/integration/CNewtonIntegration.hpp
index 1b4ff748b9a..a04693f439e 100644
--- a/SU2_CFD/include/integration/CNewtonIntegration.hpp
+++ b/SU2_CFD/include/integration/CNewtonIntegration.hpp
@@ -2,7 +2,7 @@
  * \file CNewtonIntegration.hpp
  * \brief Newton-Krylov integration.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/integration/CSingleGridIntegration.hpp b/SU2_CFD/include/integration/CSingleGridIntegration.hpp
index 764017cbcd4..ca97fcdaede 100644
--- a/SU2_CFD/include/integration/CSingleGridIntegration.hpp
+++ b/SU2_CFD/include/integration/CSingleGridIntegration.hpp
@@ -2,7 +2,7 @@
  * \file CSingleGridIntegration.hpp
  * \brief Declaration of class for numerical integration of fine grid-only problems.
  * \author A. Bueno.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/integration/CStructuralIntegration.hpp b/SU2_CFD/include/integration/CStructuralIntegration.hpp
index 707840c92c9..26f397628f6 100644
--- a/SU2_CFD/include/integration/CStructuralIntegration.hpp
+++ b/SU2_CFD/include/integration/CStructuralIntegration.hpp
@@ -2,7 +2,7 @@
  * \file CStructuralIntegration.hpp
  * \brief Declaration of class for numerical integration of structural problems.
  * \author R. Sanchez.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/interfaces/CInterface.hpp b/SU2_CFD/include/interfaces/CInterface.hpp
index ddf2ccc36e2..622d325248d 100644
--- a/SU2_CFD/include/interfaces/CInterface.hpp
+++ b/SU2_CFD/include/interfaces/CInterface.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations and inlines of the transfer structure.
  *        The subroutines and functions are in the physics folders.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -51,7 +51,7 @@ using namespace std;
  * \ingroup Interfaces
  * \brief Main class for defining the physical transfer of information.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 
 class CInterface {
diff --git a/SU2_CFD/include/interfaces/cfd/CConservativeVarsInterface.hpp b/SU2_CFD/include/interfaces/cfd/CConservativeVarsInterface.hpp
index 6e97ddd3d36..1b3d724775e 100644
--- a/SU2_CFD/include/interfaces/cfd/CConservativeVarsInterface.hpp
+++ b/SU2_CFD/include/interfaces/cfd/CConservativeVarsInterface.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer conservative variables
  *        from a generic zone into another one.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/interfaces/cfd/CMixingPlaneInterface.hpp b/SU2_CFD/include/interfaces/cfd/CMixingPlaneInterface.hpp
index 1cf12088232..78e1f602e0a 100644
--- a/SU2_CFD/include/interfaces/cfd/CMixingPlaneInterface.hpp
+++ b/SU2_CFD/include/interfaces/cfd/CMixingPlaneInterface.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer average variables
  *        needed for MixingPlane computation from a generic zone into another one.
  * \author S. Vitale
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/interfaces/cfd/CSlidingInterface.hpp b/SU2_CFD/include/interfaces/cfd/CSlidingInterface.hpp
index 8bcaf560731..633ff04f806 100644
--- a/SU2_CFD/include/interfaces/cfd/CSlidingInterface.hpp
+++ b/SU2_CFD/include/interfaces/cfd/CSlidingInterface.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer conservative variables
  *        from a generic zone into another
  * \author G. Gori Politecnico di Milano
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/interfaces/cht/CConjugateHeatInterface.hpp b/SU2_CFD/include/interfaces/cht/CConjugateHeatInterface.hpp
index 002dcd01308..d29e37d2455 100644
--- a/SU2_CFD/include/interfaces/cht/CConjugateHeatInterface.hpp
+++ b/SU2_CFD/include/interfaces/cht/CConjugateHeatInterface.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer temperature and heatflux
  *        density for conjugate heat interfaces between structure and fluid zones.
  * \author O. Burghardt
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/interfaces/fsi/CDiscAdjFlowTractionInterface.hpp b/SU2_CFD/include/interfaces/fsi/CDiscAdjFlowTractionInterface.hpp
index 8f7a822ebc4..9866c4e30ac 100644
--- a/SU2_CFD/include/interfaces/fsi/CDiscAdjFlowTractionInterface.hpp
+++ b/SU2_CFD/include/interfaces/fsi/CDiscAdjFlowTractionInterface.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer flow tractions
  *        from a fluid zone into a structural zone in a discrete adjoint simulation.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/interfaces/fsi/CDisplacementsInterface.hpp b/SU2_CFD/include/interfaces/fsi/CDisplacementsInterface.hpp
index c61cebfb302..bffe292b263 100644
--- a/SU2_CFD/include/interfaces/fsi/CDisplacementsInterface.hpp
+++ b/SU2_CFD/include/interfaces/fsi/CDisplacementsInterface.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer boundary displacements
  *        from a structural zone into a fluid zone.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/interfaces/fsi/CFlowTractionInterface.hpp b/SU2_CFD/include/interfaces/fsi/CFlowTractionInterface.hpp
index 6f3f4370988..c3fa8a00e78 100644
--- a/SU2_CFD/include/interfaces/fsi/CFlowTractionInterface.hpp
+++ b/SU2_CFD/include/interfaces/fsi/CFlowTractionInterface.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer flow tractions
  *        from a fluid zone into a structural zone.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/iteration/CAdjFluidIteration.hpp b/SU2_CFD/include/iteration/CAdjFluidIteration.hpp
index 7b0cdbff1ee..25a4ef1c28f 100644
--- a/SU2_CFD/include/iteration/CAdjFluidIteration.hpp
+++ b/SU2_CFD/include/iteration/CAdjFluidIteration.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the iteration classes used by SU2_CFD.
  *        Each CIteration class represents an available physics package.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/iteration/CDiscAdjFEAIteration.hpp b/SU2_CFD/include/iteration/CDiscAdjFEAIteration.hpp
index 7064932a7ff..d0b82d9e4b3 100644
--- a/SU2_CFD/include/iteration/CDiscAdjFEAIteration.hpp
+++ b/SU2_CFD/include/iteration/CDiscAdjFEAIteration.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the iteration classes used by SU2_CFD.
  *        Each CIteration class represents an available physics package.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/iteration/CDiscAdjFluidIteration.hpp b/SU2_CFD/include/iteration/CDiscAdjFluidIteration.hpp
index 8a4cebaf00b..2de46eb263f 100644
--- a/SU2_CFD/include/iteration/CDiscAdjFluidIteration.hpp
+++ b/SU2_CFD/include/iteration/CDiscAdjFluidIteration.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the iteration classes used by SU2_CFD.
  *        Each CIteration class represents an available physics package.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/iteration/CDiscAdjHeatIteration.hpp b/SU2_CFD/include/iteration/CDiscAdjHeatIteration.hpp
index 054e83f225d..90f7d481ad4 100644
--- a/SU2_CFD/include/iteration/CDiscAdjHeatIteration.hpp
+++ b/SU2_CFD/include/iteration/CDiscAdjHeatIteration.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the iteration classes used by SU2_CFD.
  *        Each CIteration class represents an available physics package.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/iteration/CFEAIteration.hpp b/SU2_CFD/include/iteration/CFEAIteration.hpp
index 17c81e56235..b0e5cced78c 100644
--- a/SU2_CFD/include/iteration/CFEAIteration.hpp
+++ b/SU2_CFD/include/iteration/CFEAIteration.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the iteration classes used by SU2_CFD.
  *        Each CIteration class represents an available physics package.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -35,7 +35,7 @@
  * \ingroup Drivers
  * \brief Class for driving an iteration of structural analysis.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CFEAIteration : public CIteration {
  public:
diff --git a/SU2_CFD/include/iteration/CFEMFluidIteration.hpp b/SU2_CFD/include/iteration/CFEMFluidIteration.hpp
index 4d550c7e102..87c0ede107e 100644
--- a/SU2_CFD/include/iteration/CFEMFluidIteration.hpp
+++ b/SU2_CFD/include/iteration/CFEMFluidIteration.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the iteration classes used by SU2_CFD.
  *        Each CIteration class represents an available physics package.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -35,7 +35,7 @@
  * \ingroup Drivers
  * \brief Class for driving an iteration of the finite element flow system.
  * \author T. Economon, E. van der Weide
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CFEMFluidIteration : public CFluidIteration {
  public:
diff --git a/SU2_CFD/include/iteration/CFluidIteration.hpp b/SU2_CFD/include/iteration/CFluidIteration.hpp
index 93c0f11043f..62c1467a7d8 100644
--- a/SU2_CFD/include/iteration/CFluidIteration.hpp
+++ b/SU2_CFD/include/iteration/CFluidIteration.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the iteration classes used by SU2_CFD.
  *        Each CIteration class represents an available physics package.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/iteration/CHeatIteration.hpp b/SU2_CFD/include/iteration/CHeatIteration.hpp
index 6cd1cf80a34..11a7be72314 100644
--- a/SU2_CFD/include/iteration/CHeatIteration.hpp
+++ b/SU2_CFD/include/iteration/CHeatIteration.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the iteration classes used by SU2_CFD.
  *        Each CIteration class represents an available physics package.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/iteration/CIteration.hpp b/SU2_CFD/include/iteration/CIteration.hpp
index dc3fa290813..c432551dc2a 100644
--- a/SU2_CFD/include/iteration/CIteration.hpp
+++ b/SU2_CFD/include/iteration/CIteration.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the iteration classes used by SU2_CFD.
  *        Each CIteration class represents an available physics package.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/iteration/CIterationFactory.hpp b/SU2_CFD/include/iteration/CIterationFactory.hpp
index bc587680b76..cd6fd01f3f8 100644
--- a/SU2_CFD/include/iteration/CIterationFactory.hpp
+++ b/SU2_CFD/include/iteration/CIterationFactory.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the iteration classes used by SU2_CFD.
  *        Each CIteration class represents an available physics package.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/iteration/CTurboIteration.hpp b/SU2_CFD/include/iteration/CTurboIteration.hpp
index f9f75363995..8d6af4f2e6d 100644
--- a/SU2_CFD/include/iteration/CTurboIteration.hpp
+++ b/SU2_CFD/include/iteration/CTurboIteration.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the iteration classes used by SU2_CFD.
  *        Each CIteration class represents an available physics package.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/limiters/CLimiterDetails.hpp b/SU2_CFD/include/limiters/CLimiterDetails.hpp
index 2a5c06c28dc..189c091e731 100644
--- a/SU2_CFD/include/limiters/CLimiterDetails.hpp
+++ b/SU2_CFD/include/limiters/CLimiterDetails.hpp
@@ -3,7 +3,7 @@
  * \brief A class template that allows defining limiters via
  *        specialization of particular details.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/limiters/computeLimiters.hpp b/SU2_CFD/include/limiters/computeLimiters.hpp
index 685f2fd786e..8c7a105882d 100644
--- a/SU2_CFD/include/limiters/computeLimiters.hpp
+++ b/SU2_CFD/include/limiters/computeLimiters.hpp
@@ -2,7 +2,7 @@
  * \file computeLimiters.hpp
  * \brief Compute limiters wrapper function.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/limiters/computeLimiters_impl.hpp b/SU2_CFD/include/limiters/computeLimiters_impl.hpp
index 48a1dacbe2b..bb6fa93f315 100644
--- a/SU2_CFD/include/limiters/computeLimiters_impl.hpp
+++ b/SU2_CFD/include/limiters/computeLimiters_impl.hpp
@@ -4,7 +4,7 @@
  * \note Common methods are derived by defining small details
  *       via specialization of CLimiterDetails.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/CGradSmoothing.hpp b/SU2_CFD/include/numerics/CGradSmoothing.hpp
index 2590601bbb8..e6d1e7dfabb 100644
--- a/SU2_CFD/include/numerics/CGradSmoothing.hpp
+++ b/SU2_CFD/include/numerics/CGradSmoothing.hpp
@@ -2,7 +2,7 @@
  * \file CGradSmoothing.hpp
  * \brief Declarations and inlines of the numerics class for gradient smoothing.
  * \author T.Dick
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/CNumerics.hpp b/SU2_CFD/include/numerics/CNumerics.hpp
index d493ac5c365..4eea7d9debd 100644
--- a/SU2_CFD/include/numerics/CNumerics.hpp
+++ b/SU2_CFD/include/numerics/CNumerics.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration of the base numerics class, the
  *        implementation is in the CNumerics.cpp file.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -71,9 +71,6 @@ class CNumerics {
   Thermal_Conductivity_j,    /*!< \brief Thermal conductivity at point j. */
   Thermal_Conductivity_ve_i, /*!< \brief vibrational-electronic Thermal conductivity at point i. */
   Thermal_Conductivity_ve_j, /*!< \brief vibrational-electronic Thermal conductivity at point j. */
-  Thermal_Diffusivity_i,     /*!< \brief Thermal diffusivity at point i. */
-  Thermal_Diffusivity_j;     /*!< \brief Thermal diffusivity at point j. */
-  su2double
   Cp_i,               /*!< \brief Cp at point i. */
   Cp_j;               /*!< \brief Cp at point j. */
   su2double
@@ -83,7 +80,8 @@ class CNumerics {
   turb_ke_i,  /*!< \brief Turbulent kinetic energy at point i. */
   turb_ke_j;  /*!< \brief Turbulent kinetic energy at point j. */
   su2double
-  intermittency_eff_i;  /*!< \brief effective intermittency at point i. */
+  intermittency_eff_i, /*!< \brief effective intermittency at point i. */
+  intermittency_i; /*!< \brief intermittency at point i. */
   su2double
   Pressure_i,  /*!< \brief Pressure at point i. */
   Pressure_j;  /*!< \brief Pressure at point j. */
@@ -157,6 +155,8 @@ class CNumerics {
   TurbPsi_Grad_j,  /*!< \brief Gradient of adjoint turbulent variables at point j. */
   AuxVar_Grad_i,   /*!< \brief Gradient of an auxiliary variable at point i. */
   AuxVar_Grad_j;   /*!< \brief Gradient of an auxiliary variable at point i. */
+  su2double
+  LocalGridLength_i; /*!< \brief Local grid length at point i. */
   const su2double *RadVar_Source;  /*!< \brief Source term from the radiative heat transfer equation. */
   const su2double
   *Coord_i,      /*!< \brief Cartesians coordinates of point i. */
@@ -169,7 +169,8 @@ class CNumerics {
   su2double
   TimeStep,    /*!< \brief Time step useful in dual time method. */
   Area,        /*!< \brief Area of the face i-j. */
-  Volume;      /*!< \brief Volume of the control volume around point i. */
+  Volume,      /*!< \brief Volume of the control volume around point i. */
+  AvgVolume;    /*!< \brief Average of the control Volume around point i for vorticity confinement parameter correction */
   su2double vel2_inf;     /*!< \brief value of the square of freestream speed. */
   const su2double
   *WindGust_i,  /*!< \brief Wind gust at point i. */
@@ -392,6 +393,14 @@ class CNumerics {
     TransVar_Grad_j = val_transvar_grad_j;
   }
 
+  /*!
+   * \brief Set the value of the turbulent variable.
+   * \param[in] val_transvar_i - Value of the turbulent variable at point i.
+   */
+  inline void SetLocalGridLength(const su2double val_localGridLength_i) {
+    LocalGridLength_i = val_localGridLength_i;
+  }
+
   /*!
    * \brief Set the value of the adjoint turbulent variable.
    * \param[in] val_turbpsivar_i - Value of the adjoint turbulent variable at point i.
@@ -711,6 +720,20 @@ class CNumerics {
     intermittency_eff_i = val_intermittency_eff_i;
   }
 
+  /*!
+   * \brief Set the value of the intermittency for the LM model.
+   * \param[in] intermittency_i - Value of the intermittency at point i.
+   */
+  void SetIntermittency(su2double val_intermittency_i) {
+    intermittency_i = val_intermittency_i;
+  }
+
+  /*!
+   * \brief Get the value of the effective intermittency for the transition model.
+   * \param[in] intermittency_eff_i - Value of the effective intermittency at point i.
+   */
+  su2double GetIntermittencyEff() const { return intermittency_eff_i; }
+
   /*!
    * \brief Set the gradient of the auxiliary variables.
    * \param[in] val_auxvar_grad_i - Gradient of the auxiliary variable at point i.
@@ -768,18 +791,6 @@ class CNumerics {
     Thermal_Conductivity_ve_j = val_thermal_conductivity_ve_j;
   }
 
-  /*!
-   * \brief Set the thermal diffusivity (translational/rotational)
-   * \param[in] val_thermal_diffusivity_i - Value of the thermal diffusivity at point i.
-   * \param[in] val_thermal_diffusivity_j - Value of the thermal diffusivity at point j.
-   * \param[in] iSpecies - Value of the species.
-   */
-  inline void SetThermalDiffusivity(su2double val_thermal_diffusivity_i,
-                                    su2double val_thermal_diffusivity_j) {
-    Thermal_Diffusivity_i = val_thermal_diffusivity_i;
-    Thermal_Diffusivity_j = val_thermal_diffusivity_j;
-  }
-
   /*!
    * \brief Set the specifc heat c_p.
    * \param[in] val_specific_heat_i - Value of the specific heat at point i.
@@ -984,6 +995,12 @@ class CNumerics {
    */
   inline void SetVolume(su2double val_volume) { Volume = val_volume; }
 
+  /*!
+   * \brief Set the value of AvgVolume Variable.
+   * \param[in] val_avgvolume AvgVolume Variable.
+   */
+  inline void SetAvgVolume(su2double val_avgvolume) { AvgVolume = val_avgvolume; }
+
   /*!
   * \brief Sets the values of the roe dissipation.
   * \param[in] diss_i - Dissipation value at node i
diff --git a/SU2_CFD/include/numerics/NEMO/CNEMONumerics.hpp b/SU2_CFD/include/numerics/NEMO/CNEMONumerics.hpp
index 3ca4f7a2aba..08c11113168 100644
--- a/SU2_CFD/include/numerics/NEMO/CNEMONumerics.hpp
+++ b/SU2_CFD/include/numerics/NEMO/CNEMONumerics.hpp
@@ -2,7 +2,7 @@
  * \file CNEMONumerics.hpp
  * \brief Base class template NEMO numerics.
  * \author C. Garbacz, W. Maier, S. R. Copeland
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/NEMO/NEMO_diffusion.hpp b/SU2_CFD/include/numerics/NEMO/NEMO_diffusion.hpp
index 0f0d176222b..e3d9f79f5f3 100644
--- a/SU2_CFD/include/numerics/NEMO/NEMO_diffusion.hpp
+++ b/SU2_CFD/include/numerics/NEMO/NEMO_diffusion.hpp
@@ -2,7 +2,7 @@
  * \file NEMO_diffusion.hpp
  * \brief Declarations of numerics classes for viscous flux computation.
  * \author S.R. Copeland, W. Maier, C. Garbacz.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -34,7 +34,7 @@
  * \brief Class for computing viscous term using the average of gradients.
  * \ingroup ViscDiscr
  * \author S.R. Copeland, W. Maier, C. Garbacz
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CAvgGrad_NEMO : public CNEMONumerics {
 private:
@@ -90,7 +90,7 @@ class CAvgGrad_NEMO : public CNEMONumerics {
  * \brief Class for computing viscous term using the average of gradients.
  * \ingroup ViscDiscr
  * \author C. Garbacz, W. Maier, S.R. Copeland.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CAvgGradCorrected_NEMO : public CNEMONumerics {
 private:
diff --git a/SU2_CFD/include/numerics/NEMO/NEMO_sources.hpp b/SU2_CFD/include/numerics/NEMO/NEMO_sources.hpp
index 05dc3495eb8..e07017acba2 100644
--- a/SU2_CFD/include/numerics/NEMO/NEMO_sources.hpp
+++ b/SU2_CFD/include/numerics/NEMO/NEMO_sources.hpp
@@ -2,7 +2,7 @@
  * \file NEMO_sources.hpp
  * \brief Declarations of numerics classes for source-term integration.
  * \author C. Garbacz, W. Maier, S. Copeland.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -34,7 +34,7 @@
  * \brief Class for two-temperature model source terms.
  * \ingroup SourceDiscr
  * \author C. Garbacz, W. Maier, S. Copeland.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CSource_NEMO : public CNEMONumerics {
 private:
diff --git a/SU2_CFD/include/numerics/NEMO/convection/ausm.hpp b/SU2_CFD/include/numerics/NEMO/convection/ausm.hpp
index 37a5adafd11..a7d5f3187be 100644
--- a/SU2_CFD/include/numerics/NEMO/convection/ausm.hpp
+++ b/SU2_CFD/include/numerics/NEMO/convection/ausm.hpp
@@ -2,7 +2,7 @@
  * \file ausm.hpp
  * \brief Declaration of numerics classes for the AUSM family of schemes in NEMO.
  * \author F. Palacios, S.R. Copeland, W. Maier, C. Garbacz
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/NEMO/convection/ausmplusup2.hpp b/SU2_CFD/include/numerics/NEMO/convection/ausmplusup2.hpp
index 08bbb4e6744..9c6ec1c95b3 100644
--- a/SU2_CFD/include/numerics/NEMO/convection/ausmplusup2.hpp
+++ b/SU2_CFD/include/numerics/NEMO/convection/ausmplusup2.hpp
@@ -2,7 +2,7 @@
  * \file ausmplusup2.hpp
  * \brief Declaration of numerics classes for the AUSM family of schemes in NEMO - AUSM+UP2.
  * \author W. Maier, A. Sachedeva, C. Garbacz.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/NEMO/convection/ausmpwplus.hpp b/SU2_CFD/include/numerics/NEMO/convection/ausmpwplus.hpp
index 45bf4545ce6..d1172cf9c6b 100644
--- a/SU2_CFD/include/numerics/NEMO/convection/ausmpwplus.hpp
+++ b/SU2_CFD/include/numerics/NEMO/convection/ausmpwplus.hpp
@@ -2,7 +2,7 @@
  * \file ausmpwplus.hpp
  * \brief Declaration of numerics classes for the AUSM family of schemes in NEMO - AUSMPWPLUS.
  * \author F. Palacios, W.Maier, C. Garbacz
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/NEMO/convection/lax.hpp b/SU2_CFD/include/numerics/NEMO/convection/lax.hpp
index 9102c7defb5..c5e8f46e0a4 100644
--- a/SU2_CFD/include/numerics/NEMO/convection/lax.hpp
+++ b/SU2_CFD/include/numerics/NEMO/convection/lax.hpp
@@ -2,7 +2,7 @@
  * \file lax.hpp
  * \brief Declaration of numerics classes for Lax centered scheme.
  * \author F. Palacios, S.R. Copeland, W. Maier, C. Garbacz
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/NEMO/convection/msw.hpp b/SU2_CFD/include/numerics/NEMO/convection/msw.hpp
index 1ebcce0f546..80b1bac4544 100644
--- a/SU2_CFD/include/numerics/NEMO/convection/msw.hpp
+++ b/SU2_CFD/include/numerics/NEMO/convection/msw.hpp
@@ -2,7 +2,7 @@
  * \file msw.hpp
  * \brief Declaration of numerics classes for modified Steger-Warming scheme.
  * \author ADL Stanford, S.R. Copeland, W. Maier, C. Garbacz
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -34,7 +34,7 @@
  * \brief Class for solving a flux-vector splitting method by Steger & Warming, modified version.
  * \ingroup ConvDiscr
  * \author ADL Stanford, S.R. Copeland, W. Maier, C. Garbacz
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CUpwMSW_NEMO : public CNEMONumerics {
 private:
diff --git a/SU2_CFD/include/numerics/NEMO/convection/roe.hpp b/SU2_CFD/include/numerics/NEMO/convection/roe.hpp
index 751abe4149e..4db3e26b859 100644
--- a/SU2_CFD/include/numerics/NEMO/convection/roe.hpp
+++ b/SU2_CFD/include/numerics/NEMO/convection/roe.hpp
@@ -2,7 +2,7 @@
  * \file roe.hpp
  * \brief Declarations of numerics classes for Roe-type schemes in NEMO.
  * \author S.R. Copeland, W. Maier, C. Garbacz
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -34,7 +34,7 @@
  * \brief Class for evaluating the Riemann problem using Roe's scheme for a two-temperature model.
  * \ingroup ConvDiscr
  * \author S. R. Copeland, W. Maier, C. Garbacz
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CUpwRoe_NEMO : public CNEMONumerics {
 private:
diff --git a/SU2_CFD/include/numerics/continuous_adjoint/adj_convection.hpp b/SU2_CFD/include/numerics/continuous_adjoint/adj_convection.hpp
index d18f12b4245..a335f190f4d 100644
--- a/SU2_CFD/include/numerics/continuous_adjoint/adj_convection.hpp
+++ b/SU2_CFD/include/numerics/continuous_adjoint/adj_convection.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for continuous adjoint
  *        convective discretization. Implemented in adj_convection.cpp.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/continuous_adjoint/adj_diffusion.hpp b/SU2_CFD/include/numerics/continuous_adjoint/adj_diffusion.hpp
index 4f44d128c97..341081eaff7 100644
--- a/SU2_CFD/include/numerics/continuous_adjoint/adj_diffusion.hpp
+++ b/SU2_CFD/include/numerics/continuous_adjoint/adj_diffusion.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for continuous adjoint
  *        diffusion discretization. Implemented in adj_diffusion.cpp.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/continuous_adjoint/adj_sources.hpp b/SU2_CFD/include/numerics/continuous_adjoint/adj_sources.hpp
index 1b2e33f63ab..4ca6744bccc 100644
--- a/SU2_CFD/include/numerics/continuous_adjoint/adj_sources.hpp
+++ b/SU2_CFD/include/numerics/continuous_adjoint/adj_sources.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for continuous adjoint
  *        source term integration. Implemented in adj_sources.cpp.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/elasticity/CFEAElasticity.hpp b/SU2_CFD/include/numerics/elasticity/CFEAElasticity.hpp
index 45156ccf858..463ef33aceb 100644
--- a/SU2_CFD/include/numerics/elasticity/CFEAElasticity.hpp
+++ b/SU2_CFD/include/numerics/elasticity/CFEAElasticity.hpp
@@ -2,7 +2,7 @@
  * \file CFEAElasticity.hpp
  * \brief Declaration and inlines of the base class for elasticity problems.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -38,7 +38,7 @@
  *        The methods we override in this class with an empty implementation are here just to better
  *        document the public interface of this class hierarchy.
  * \author R.Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CFEAElasticity : public CNumerics {
 
diff --git a/SU2_CFD/include/numerics/elasticity/CFEALinearElasticity.hpp b/SU2_CFD/include/numerics/elasticity/CFEALinearElasticity.hpp
index 3b125593ae0..c8097e1eee9 100644
--- a/SU2_CFD/include/numerics/elasticity/CFEALinearElasticity.hpp
+++ b/SU2_CFD/include/numerics/elasticity/CFEALinearElasticity.hpp
@@ -2,7 +2,7 @@
  * \file CFEALinearElasticity.hpp
  * \brief Declaration and inlines of the linear elasticity FE numerics class.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -35,7 +35,7 @@
  * \brief Class for computing the stiffness matrix of a linear, elastic problem.
  * \ingroup Elasticity_Equations
  * \author R.Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CFEALinearElasticity : public CFEAElasticity {
 protected:
@@ -90,7 +90,7 @@ class CFEALinearElasticity : public CFEAElasticity {
  * \brief Particular case of linear elasticity used for mesh deformation.
  * \ingroup Elasticity_Equations
  * \author R.Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CFEAMeshElasticity final : public CFEALinearElasticity {
 
diff --git a/SU2_CFD/include/numerics/elasticity/CFEANonlinearElasticity.hpp b/SU2_CFD/include/numerics/elasticity/CFEANonlinearElasticity.hpp
index 5a697f914d6..44a7420c78b 100644
--- a/SU2_CFD/include/numerics/elasticity/CFEANonlinearElasticity.hpp
+++ b/SU2_CFD/include/numerics/elasticity/CFEANonlinearElasticity.hpp
@@ -2,7 +2,7 @@
  * \file CFEANonlinearElasticity.hpp
  * \brief Declaration and inlines of the nonlinear elasticity FE numerics class.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -37,7 +37,7 @@
  *        Compute_Plane_Stress_Term and Compute_Stress_Tensor.
  * \ingroup Elasticity_Equations
  * \author R.Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CFEANonlinearElasticity : public CFEAElasticity {
 
diff --git a/SU2_CFD/include/numerics/elasticity/nonlinear_models.hpp b/SU2_CFD/include/numerics/elasticity/nonlinear_models.hpp
index e0aa7384614..fed3e392496 100644
--- a/SU2_CFD/include/numerics/elasticity/nonlinear_models.hpp
+++ b/SU2_CFD/include/numerics/elasticity/nonlinear_models.hpp
@@ -2,7 +2,7 @@
  * \file nonlinear_models.hpp
  * \brief Declarations of nonlinear constitutive models.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -35,7 +35,7 @@
  * \brief Class for computing the constitutive and stress tensors for a neo-Hookean material model, compressible.
  * \ingroup Elasticity_Equations
  * \author R.Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CFEM_NeoHookean_Comp final : public CFEANonlinearElasticity {
 
@@ -83,7 +83,7 @@ class CFEM_NeoHookean_Comp final : public CFEANonlinearElasticity {
  * \brief Constitutive and stress tensors for a Knowles stored-energy function, nearly incompressible.
  * \ingroup Elasticity_Equations
  * \author R.Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CFEM_Knowles_NearInc final : public CFEANonlinearElasticity {
 
@@ -134,7 +134,7 @@ class CFEM_Knowles_NearInc final : public CFEANonlinearElasticity {
  * \brief Class for computing the constitutive and stress tensors for a dielectric elastomer.
  * \ingroup Elasticity_Equations
  * \author R.Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CFEM_DielectricElastomer final : public CFEANonlinearElasticity {
 
@@ -182,7 +182,7 @@ class CFEM_DielectricElastomer final : public CFEANonlinearElasticity {
  * \brief Class for computing the constitutive and stress tensors for a nearly-incompressible ideal DE.
  * \ingroup Elasticity_Equations
  * \author R.Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CFEM_IdealDE final : public CFEANonlinearElasticity {
 
diff --git a/SU2_CFD/include/numerics/flow/convection/ausm_slau.hpp b/SU2_CFD/include/numerics/flow/convection/ausm_slau.hpp
index e611c71aada..3de66b6ed70 100644
--- a/SU2_CFD/include/numerics/flow/convection/ausm_slau.hpp
+++ b/SU2_CFD/include/numerics/flow/convection/ausm_slau.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration of numerics classes for the AUSM family of schemes,
  *        including SLAU. The implementation is in ausm.cpp.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/flow/convection/centered.hpp b/SU2_CFD/include/numerics/flow/convection/centered.hpp
index 1cf42d0edf4..7c6e3acddeb 100644
--- a/SU2_CFD/include/numerics/flow/convection/centered.hpp
+++ b/SU2_CFD/include/numerics/flow/convection/centered.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration of numerics classes for centered schemes,
  *        the implementation is in centered.cpp.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/flow/convection/cusp.hpp b/SU2_CFD/include/numerics/flow/convection/cusp.hpp
index 595553e8520..fa2233c2d55 100644
--- a/SU2_CFD/include/numerics/flow/convection/cusp.hpp
+++ b/SU2_CFD/include/numerics/flow/convection/cusp.hpp
@@ -2,7 +2,7 @@
  * \file cusp.hpp
  * \brief Declaration of the CUSP numerics class.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/flow/convection/fds.hpp b/SU2_CFD/include/numerics/flow/convection/fds.hpp
index c33d4be5d57..937beee45b9 100644
--- a/SU2_CFD/include/numerics/flow/convection/fds.hpp
+++ b/SU2_CFD/include/numerics/flow/convection/fds.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of classes for Flux-Difference-Spliting schemes,
  *        the implementations are in fds.cpp
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/flow/convection/fvs.hpp b/SU2_CFD/include/numerics/flow/convection/fvs.hpp
index 8b9c4b1e4b2..0dab5b38a83 100644
--- a/SU2_CFD/include/numerics/flow/convection/fvs.hpp
+++ b/SU2_CFD/include/numerics/flow/convection/fvs.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of classes for Flux-Vector-Spliting schemes,
  *        the implementations are in fvs.cpp.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/flow/convection/hllc.hpp b/SU2_CFD/include/numerics/flow/convection/hllc.hpp
index 892ecfa796c..ea7797f9ffe 100644
--- a/SU2_CFD/include/numerics/flow/convection/hllc.hpp
+++ b/SU2_CFD/include/numerics/flow/convection/hllc.hpp
@@ -2,7 +2,7 @@
  * \file hllc.hpp
  * \brief Declaration of HLLC numerics classes, implemented in hllc.cpp.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -34,7 +34,7 @@
  * \brief Class for solving an approximate Riemann HLLC.
  * \ingroup ConvDiscr
  * \author G. Gori, Politecnico di Milano
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CUpwHLLC_Flow final : public CNumerics {
 private:
@@ -86,7 +86,7 @@ class CUpwHLLC_Flow final : public CNumerics {
  * \brief Class for solving an approximate Riemann HLLC.
  * \ingroup ConvDiscr
  * \author G. Gori, Politecnico di Milano
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CUpwGeneralHLLC_Flow final : public CNumerics {
 private:
diff --git a/SU2_CFD/include/numerics/flow/convection/roe.hpp b/SU2_CFD/include/numerics/flow/convection/roe.hpp
index fb41808f162..ca17ee8ab00 100644
--- a/SU2_CFD/include/numerics/flow/convection/roe.hpp
+++ b/SU2_CFD/include/numerics/flow/convection/roe.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for Roe-type schemes,
  *        implemented in roe.cpp.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -119,7 +119,7 @@ class CUpwRoe_Flow final : public CUpwRoeBase_Flow {
  * \brief Class for solving an approximate Riemann solver of L2Roe for the flow equations.
  * \ingroup ConvDiscr
  * \author E. Molina, A. Bueno, F. Palacios, P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CUpwL2Roe_Flow final : public CUpwRoeBase_Flow {
 private:
@@ -149,7 +149,7 @@ class CUpwL2Roe_Flow final : public CUpwRoeBase_Flow {
  * \brief Class for solving an approximate Riemann solver of LMRoe for the flow equations.
  * \ingroup ConvDiscr
  * \author E. Molina, A. Bueno, F. Palacios, P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CUpwLMRoe_Flow final : public CUpwRoeBase_Flow {
 private:
diff --git a/SU2_CFD/include/numerics/flow/flow_diffusion.hpp b/SU2_CFD/include/numerics/flow/flow_diffusion.hpp
index 0664250b2df..21fcbf05033 100644
--- a/SU2_CFD/include/numerics/flow/flow_diffusion.hpp
+++ b/SU2_CFD/include/numerics/flow/flow_diffusion.hpp
@@ -2,7 +2,7 @@
  * \file flow_diffusion.hpp
  * \brief Declarations of numerics classes for viscous flux computation.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/flow/flow_sources.hpp b/SU2_CFD/include/numerics/flow/flow_sources.hpp
index 69cea9237b6..e0f7234556e 100644
--- a/SU2_CFD/include/numerics/flow/flow_sources.hpp
+++ b/SU2_CFD/include/numerics/flow/flow_sources.hpp
@@ -2,7 +2,7 @@
  * \file flow_sources.hpp
  * \brief Declarations of numerics classes for source-term integration.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -177,7 +177,7 @@ class CSourceBodyForce final : public CSourceBase_Flow {
  * \brief Class for the source term integration of a body force in the incompressible solver.
  * \ingroup SourceDiscr
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CSourceIncBodyForce final : public CSourceBase_Flow {
   su2double Body_Force_Vector[3];
@@ -204,7 +204,7 @@ class CSourceIncBodyForce final : public CSourceBase_Flow {
  * \brief Class for the source term integration of the Boussinesq approximation for incompressible flow.
  * \ingroup SourceDiscr
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CSourceBoussinesq final : public CSourceBase_Flow {
   su2double Gravity_Vector[3];
@@ -306,6 +306,54 @@ class CSourceIncRotatingFrame_Flow final : public CSourceBase_Flow {
 
 };
 
+/*!
+ * \class CSourceVorticityConfinement
+ * \brief Class for a source term due to vorticity confinement.
+ * \ingroup SourceDiscr
+ * \brief Vorticity Confinement (VC) technique to counter the numerical
+ * diffusion offered by the numerical scheme
+ * \author: Y Chandukrishna, Josy P Pullockara, T N Venkatesh.
+ * Computational and Theoretical Fluid Dynamics division,
+ * CSIR-National Aerospace Laboratories (NAL), Bangalore.
+ * Academy of Scientific and Innovative Research (AcSIR), Ghaziabad.
+ * First release date : 23 December 2022
+ * modified on:
+ *
+ * VC technique introduces an additional term to the N-S equations that
+ * counters the numerical difusion offerd by the numerical schemes. The
+ * additional term is introduced as a source term. VC technique requires an
+ * input confinement parameter that controls the magnitude of the source
+ * term. A suitable Confinement parameter is problem, scheme and grid
+ * dependant.
+ *
+ * Required changes in config file -
+ * VORTICITY_CONFINEMENT = YES
+ * CONFINEMENT_PARAMETER = <0.0(default)>
+ * Currently have support for Viscous, Inviscid cases for both 2D and 3D
+ * problems. Can be used along with other source terms also.
+ *
+ * The current implementation follows,
+ * R. Loehner and C. Yang, Vorticity confinement on unstructured grids, 2002.
+ * N. Butsuntorn and A. Jameson, Time Spectral Method for Rotorcraft Flow, 2008.
+ */
+class CSourceVorticityConfinement final : public CSourceBase_Flow {
+public:
+  /*!
+   * \brief Constructor of the class.
+   * \param[in] val_nDim - Number of dimensions of the problem.
+   * \param[in] val_nVar - Number of variables of the problem.
+   * \param[in] config - Definition of the particular problem.
+   */
+  CSourceVorticityConfinement(unsigned short val_nDim, unsigned short val_nVar, const CConfig* config);
+
+  /*!
+   * \brief Residual of the rotational frame source term.
+   * \param[in] config - Definition of the particular problem.
+   * \return Lightweight const-view of residual and Jacobian.
+   */
+  ResidualType<> ComputeResidual(const CConfig* config) override;
+};
+
 /*!
  * \class CSourceWindGust
  * \brief Class for a source term due to a wind gust.
diff --git a/SU2_CFD/include/numerics/heat.hpp b/SU2_CFD/include/numerics/heat.hpp
index 7104fb69ea3..f5076a434be 100644
--- a/SU2_CFD/include/numerics/heat.hpp
+++ b/SU2_CFD/include/numerics/heat.hpp
@@ -2,7 +2,7 @@
  * \file heat.hpp
  * \brief Declarations of numerics classes for heat transfer problems.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -27,14 +27,14 @@
 
 #pragma once
 
-#include "CNumerics.hpp"
+#include "scalar/scalar_diffusion.hpp"
 
 /*!
  * \class CCentSca_Heat
  * \brief Class for scalar centered scheme.
  * \ingroup ConvDiscr
  * \author O. Burghardt
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CCentSca_Heat : public CNumerics {
 private:
@@ -68,7 +68,7 @@ class CCentSca_Heat : public CNumerics {
  * \brief Class for doing a scalar upwind solver for the heat convection equation.
  * \ingroup ConvDiscr
  * \author O. Burghardt.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CUpwSca_Heat : public CNumerics {
 private:
@@ -98,28 +98,38 @@ class CUpwSca_Heat : public CNumerics {
  * \brief Class for computing viscous term using average of gradients without correction (heat equation).
  * \ingroup ViscDiscr
  * \author O. Burghardt.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
-class CAvgGrad_Heat : public CNumerics {
-private:
-  bool implicit, correct;
-
-public:
+class CAvgGrad_Heat final : public CAvgGrad_Scalar<CNoFlowIndices> {
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] val_nDim - Number of dimensions of the problem.
-   * \param[in] val_nVar - Number of variables of the problem.
    * \param[in] config - Definition of the particular problem.
-   * \param[in] correct - Correct the gradient.
+   * \param[in] correct - Whether to correct the gradient.
    */
-  CAvgGrad_Heat(unsigned short val_nDim, unsigned short val_nVar, const CConfig *config, bool correct);
+  CAvgGrad_Heat(unsigned short val_nDim, const CConfig *config, bool correct)
+    : CAvgGrad_Scalar<CNoFlowIndices>(val_nDim, 1, correct, config) {}
 
+ private:
   /*!
-   * \brief Compute the viscous heat residual using an average of gradients with correction.
-   * \param[out] val_residual - Pointer to the total residual.
-   * \param[out] Jacobian_i - Jacobian of the numerical method at node i (implicit computation).
-   * \param[out] Jacobian_j - Jacobian of the numerical method at node j (implicit computation).
+   * \brief Adds extra variables to AD
+   */
+  void ExtraADPreaccIn(void) override {
+    AD::SetPreaccIn(*Diffusion_Coeff_i, *Diffusion_Coeff_j);
+  }
+
+  /*!
+   * \brief Heat-specific specific steps in the ComputeResidual method
    * \param[in] config - Definition of the particular problem.
    */
-  void ComputeResidual(su2double *val_residual, su2double **Jacobian_i, su2double **Jacobian_j, CConfig *config) override;
+  void FinishResidualCalc(const CConfig* config) override {
+    const su2double Thermal_Diffusivity_Mean = 0.5 * (*Diffusion_Coeff_i + *Diffusion_Coeff_j);
+
+    Flux[0] = Thermal_Diffusivity_Mean * Proj_Mean_GradScalarVar[0];
+
+    /*--- Use TSL for Jacobians. ---*/
+    Jacobian_i[0][0] = -Thermal_Diffusivity_Mean * proj_vector_ij;
+    Jacobian_j[0][0] = Thermal_Diffusivity_Mean * proj_vector_ij;
+  }
 };
diff --git a/SU2_CFD/include/numerics/radiation.hpp b/SU2_CFD/include/numerics/radiation.hpp
index 4f81d23e42e..98a50e9fa42 100644
--- a/SU2_CFD/include/numerics/radiation.hpp
+++ b/SU2_CFD/include/numerics/radiation.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the classes used to compute
  *        residual terms in radiation problems.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/scalar/scalar_convection.hpp b/SU2_CFD/include/numerics/scalar/scalar_convection.hpp
index 0bee8810425..c403af3ee43 100644
--- a/SU2_CFD/include/numerics/scalar/scalar_convection.hpp
+++ b/SU2_CFD/include/numerics/scalar/scalar_convection.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for discretization of
  *        convective fluxes in scalar problems.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/scalar/scalar_diffusion.hpp b/SU2_CFD/include/numerics/scalar/scalar_diffusion.hpp
index 028b43b165d..82793741241 100644
--- a/SU2_CFD/include/numerics/scalar/scalar_diffusion.hpp
+++ b/SU2_CFD/include/numerics/scalar/scalar_diffusion.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for discretization of
  *        viscous fluxes in scalar problems.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -30,6 +30,18 @@
 
 #include "../CNumerics.hpp"
 
+/*!
+ * \class CNoFlowIndices
+ * \brief Dummy flow indices class to use CAvgGrad_Scalar when flow variables are not available.
+ * For example, solid heat transfer problems.
+ */
+struct CNoFlowIndices {
+  CNoFlowIndices(int, int) {}
+  inline int Density() const { return 0; }
+  inline int LaminarViscosity() const { return 0; }
+  inline int EddyViscosity() const { return 0; }
+};
+
 /*!
  * \class CAvgGrad_Scalar
  * \brief Template class for computing viscous residual of scalar values
@@ -57,7 +69,7 @@ class CAvgGrad_Scalar : public CNumerics {
   su2double* Jacobian_j[MAXNVAR];             /*!< \brief Flux Jacobian w.r.t. node j. */
   su2double JacobianBuffer[2*MAXNVAR*MAXNVAR];/*!< \brief Static storage for the two Jacobians. */
 
-  const bool correct_gradient = false, implicit = false, incompressible = false;
+  const bool correct_gradient = false, incompressible = false;
 
   /*!
    * \brief A pure virtual function; Adds any extra variables to AD
@@ -84,7 +96,6 @@ class CAvgGrad_Scalar : public CNumerics {
     : CNumerics(val_nDim, val_nVar, config),
       idx(val_nDim, config->GetnSpecies()),
       correct_gradient(correct_grad),
-      implicit(config->GetKind_TimeIntScheme_Turb() == EULER_IMPLICIT),
       incompressible(config->GetKind_Regime() == ENUM_REGIME::INCOMPRESSIBLE) {
     if (nVar > MAXNVAR) {
       SU2_MPI::Error("Static arrays are too small.", CURRENT_FUNCTION);
@@ -116,15 +127,17 @@ class CAvgGrad_Scalar : public CNumerics {
       AD::SetPreaccIn(ScalarVar_i, nVar);
       AD::SetPreaccIn(ScalarVar_j, nVar);
     }
-    AD::SetPreaccIn(V_i[idx.Density()], V_i[idx.LaminarViscosity()], V_i[idx.EddyViscosity()]);
-    AD::SetPreaccIn(V_j[idx.Density()], V_j[idx.LaminarViscosity()], V_j[idx.EddyViscosity()]);
-
-    Density_i = V_i[idx.Density()];
-    Density_j = V_j[idx.Density()];
-    Laminar_Viscosity_i = V_i[idx.LaminarViscosity()];
-    Laminar_Viscosity_j = V_j[idx.LaminarViscosity()];
-    Eddy_Viscosity_i = V_i[idx.EddyViscosity()];
-    Eddy_Viscosity_j = V_j[idx.EddyViscosity()];
+    if (!std::is_same<FlowIndices, CNoFlowIndices>::value) {
+      AD::SetPreaccIn(V_i[idx.Density()], V_i[idx.LaminarViscosity()], V_i[idx.EddyViscosity()]);
+      AD::SetPreaccIn(V_j[idx.Density()], V_j[idx.LaminarViscosity()], V_j[idx.EddyViscosity()]);
+
+      Density_i = V_i[idx.Density()];
+      Density_j = V_j[idx.Density()];
+      Laminar_Viscosity_i = V_i[idx.LaminarViscosity()];
+      Laminar_Viscosity_j = V_j[idx.LaminarViscosity()];
+      Eddy_Viscosity_i = V_i[idx.EddyViscosity()];
+      Eddy_Viscosity_j = V_j[idx.EddyViscosity()];
+    }
 
     ExtraADPreaccIn();
 
diff --git a/SU2_CFD/include/numerics/scalar/scalar_sources.hpp b/SU2_CFD/include/numerics/scalar/scalar_sources.hpp
index e893f9be64b..a8b78dbc65a 100644
--- a/SU2_CFD/include/numerics/scalar/scalar_sources.hpp
+++ b/SU2_CFD/include/numerics/scalar/scalar_sources.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file scalar_sources.hpp
  * \brief Declarations of numerics classes for integration of source terms in scalar problems.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/species/species_convection.hpp b/SU2_CFD/include/numerics/species/species_convection.hpp
index 64f296faff8..46890678b2e 100644
--- a/SU2_CFD/include/numerics/species/species_convection.hpp
+++ b/SU2_CFD/include/numerics/species/species_convection.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for discretization of
  *        convective fluxes in species problems.
  * \author T. Kattmann
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/species/species_diffusion.hpp b/SU2_CFD/include/numerics/species/species_diffusion.hpp
index 00661a2a1c7..d8ba7b5023f 100644
--- a/SU2_CFD/include/numerics/species/species_diffusion.hpp
+++ b/SU2_CFD/include/numerics/species/species_diffusion.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for discretization of
  *        viscous fluxes in species problems.
  * \author T. Kattmann
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/species/species_sources.hpp b/SU2_CFD/include/numerics/species/species_sources.hpp
index aab3733669c..81dba0f8c7c 100644
--- a/SU2_CFD/include/numerics/species/species_sources.hpp
+++ b/SU2_CFD/include/numerics/species/species_sources.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for integration of source
  *        terms in species problems.
  * \author T. Kattmann
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/template.hpp b/SU2_CFD/include/numerics/template.hpp
index 2eb67f61d75..e81a536acd8 100644
--- a/SU2_CFD/include/numerics/template.hpp
+++ b/SU2_CFD/include/numerics/template.hpp
@@ -5,7 +5,7 @@
  *        new schemes in SU2, in practice you should look for a similar
  *        scheme and try to re-use functionality (not by copy-paste).
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/turbulent/transition/trans_convection.hpp b/SU2_CFD/include/numerics/turbulent/transition/trans_convection.hpp
index 92a9b99bae7..88de5a666e2 100644
--- a/SU2_CFD/include/numerics/turbulent/transition/trans_convection.hpp
+++ b/SU2_CFD/include/numerics/turbulent/transition/trans_convection.hpp
@@ -3,7 +3,7 @@
  * \brief Delarations of numerics classes for discretization of
  *        convective fluxes in transition problems.
  * \author S. Kang
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/turbulent/transition/trans_correlations.hpp b/SU2_CFD/include/numerics/turbulent/transition/trans_correlations.hpp
new file mode 100644
index 00000000000..bb80218ac6d
--- /dev/null
+++ b/SU2_CFD/include/numerics/turbulent/transition/trans_correlations.hpp
@@ -0,0 +1,192 @@
+/*!
+ * \file trans_correlations.hpp
+ * \brief Numerics class for the LM model's correlation functions.
+ * \version 7.5.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+
+#pragma once
+
+/*!
+ * \class TransLMCorrelations
+ * \brief Class for LM model's correlation functions.
+ * \ingroup SourceDiscr
+ * \author A. Rausa.
+ */
+class TransLMCorrelations {
+ private:
+
+  LM_ParsedOptions options;
+
+ public:
+
+  /*!
+   * \brief Set LM options.
+   * \param[in] val_options - LM options structure.
+   */
+  void SetOptions(const LM_ParsedOptions val_options){
+    options = val_options;
+  }
+
+  /*!
+   * \brief Compute Re_theta_c from correlations.
+   * \param[in] Tu - Turbulence intensity.
+   * \param[in] Re_theta_t - Re_theta_t (TransVar[1]).
+   * \param[out] rethetac - Corrected value for Re_theta.
+   */
+  su2double ReThetaC_Correlations(const su2double Tu, const su2double Re_theta_t) const {
+
+    su2double rethetac = 0.0;
+
+    switch (options.Correlation) {
+      case TURB_TRANS_CORRELATION::MALAN: {
+        rethetac = min(0.615 * Re_theta_t + 61.5, Re_theta_t);
+        break;
+      }
+
+      case TURB_TRANS_CORRELATION::SULUKSNA: {
+        rethetac = min(0.1 * exp(-0.0022 * Re_theta_t + 12), 300.0);
+        break;
+      }
+
+      case TURB_TRANS_CORRELATION::KRAUSE: {
+        rethetac = 0.91 * Re_theta_t + 5.32;
+        break;
+      }
+
+      case TURB_TRANS_CORRELATION::KRAUSE_HYPER: {
+        const su2double FirstTerm = -0.042 * pow(Tu, 3);
+        const su2double SecondTerm = 0.4233 * pow(Tu, 2);
+        const su2double ThirdTerm = 0.0118 * pow(Tu, 1);
+        rethetac = Re_theta_t / (FirstTerm + SecondTerm + ThirdTerm + 1.0744);
+        break;
+      }
+
+      case TURB_TRANS_CORRELATION::MEDIDA_BAEDER: {
+        const su2double FirstTerm = 4.45 * pow(Tu, 3);
+        const su2double SecondTerm = 5.7 * pow(Tu, 2);
+        const su2double ThirdTerm = 1.37 * pow(Tu, 1);
+        rethetac = (FirstTerm - SecondTerm + ThirdTerm + 0.585) * Re_theta_t;
+        break;
+      }
+
+      case TURB_TRANS_CORRELATION::MEDIDA: {
+        rethetac = 0.62 * Re_theta_t;
+        break;
+      }
+
+      case TURB_TRANS_CORRELATION::MENTER_LANGTRY: {
+        if (Re_theta_t <= 1870) {
+          const su2double FirstTerm = (-396.035 * pow(10, -2));
+          const su2double SecondTerm = (10120.656 * pow(10, -4)) * Re_theta_t;
+          const su2double ThirdTerm = (-868.230 * pow(10, -6)) * pow(Re_theta_t, 2);
+          const su2double ForthTerm = (696.506 * pow(10, -9)) * pow(Re_theta_t, 3);
+          const su2double FifthTerm = (-174.105 * pow(10, -12)) * pow(Re_theta_t, 4);
+          rethetac = FirstTerm + SecondTerm + ThirdTerm + ForthTerm + FifthTerm;
+        } else {
+          rethetac = Re_theta_t - (593.11 + 0.482 * (Re_theta_t - 1870.0));
+        }
+
+        break;
+      }
+      case TURB_TRANS_CORRELATION::DEFAULT:
+        SU2_MPI::Error("Transition correlation is set to DEFAULT but no default value has ben set in the code.",
+                       CURRENT_FUNCTION);
+        break;
+    }
+
+    return rethetac;
+  }
+
+  /*!
+   * \brief Compute FLength from correlations.
+   * \param[in] Tu - Turbulence intensity.
+   * \param[in] Re_theta_t - Re_theta_t (TransVar[1]).
+   * \param[out] F_length1 - Value for the F_length1 variable.
+   */
+  su2double FLength_Correlations(const su2double Tu, const su2double Re_theta_t) const {
+    su2double F_length1 = 0.0;
+
+    switch (options.Correlation) {
+      case TURB_TRANS_CORRELATION::MALAN: {
+        F_length1 = min(exp(7.168 - 0.01173 * Re_theta_t) + 0.5, 300.0);
+        break;
+      }
+
+      case TURB_TRANS_CORRELATION::SULUKSNA: {
+        const su2double FirstTerm = -pow(0.025 * Re_theta_t, 2) + 1.47 * Re_theta_t - 120.0;
+        F_length1 = min(max(FirstTerm, 125.0), Re_theta_t);
+        break;
+      }
+
+      case TURB_TRANS_CORRELATION::KRAUSE: {
+        F_length1 = 3.39 * Re_theta_t + 55.03;
+        break;
+      }
+
+      case TURB_TRANS_CORRELATION::KRAUSE_HYPER: {
+        if (Tu <= 1.) {
+          F_length1 = log(Re_theta_t + 1) / Tu;
+        } else {
+          const su2double FirstTerm = 0.2337 * pow(Tu, 2);
+          const su2double SecondTerm = -1.3493 * pow(Tu, 1);
+          F_length1 = log(Re_theta_t + 1) * (FirstTerm + SecondTerm + 2.1449);
+        }
+        break;
+      }
+
+      case TURB_TRANS_CORRELATION::MEDIDA_BAEDER: {
+        const su2double FirstTerm = 0.171 * pow(Tu, 2);
+        const su2double SecondTerm = 0.0083 * pow(Tu, 1);
+        F_length1 = (FirstTerm - SecondTerm + 0.0306);
+        break;
+      }
+
+      case TURB_TRANS_CORRELATION::MEDIDA: {
+        F_length1 = 40;
+        break;
+      }
+
+      case TURB_TRANS_CORRELATION::MENTER_LANGTRY: {
+        if (Re_theta_t < 400) {
+          F_length1 = 39.8189 + (-119.270 * pow(10, -4)) * Re_theta_t +
+                      (-132.567 * pow(10, -6)) * Re_theta_t * Re_theta_t;
+        } else if (Re_theta_t < 596) {
+          F_length1 = 263.404 + (-123.939 * pow(10, -2)) * Re_theta_t +
+                      (194.548 * pow(10, -5)) * pow(Re_theta_t, 2) +
+                      (-101.695 * pow(10, -8)) * pow(Re_theta_t, 3);
+        } else if (Re_theta_t < 1200) {
+          F_length1 = 0.5 - (3.0 * pow(10, -4)) * (Re_theta_t - 596.0);
+        } else {
+          F_length1 = 0.3188;
+        }
+        break;
+      }
+      case TURB_TRANS_CORRELATION::DEFAULT:
+        SU2_MPI::Error("Transition correlation is set to DEFAULT but no default value has ben set in the code.",
+                       CURRENT_FUNCTION);
+        break;
+    }
+
+    return F_length1;
+  }
+};
diff --git a/SU2_CFD/include/numerics/turbulent/transition/trans_diffusion.hpp b/SU2_CFD/include/numerics/turbulent/transition/trans_diffusion.hpp
index ff59c94084a..0ad86cf349d 100644
--- a/SU2_CFD/include/numerics/turbulent/transition/trans_diffusion.hpp
+++ b/SU2_CFD/include/numerics/turbulent/transition/trans_diffusion.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for discretization of
  *        viscous fluxes in transition problems.
  * \author S. Kang
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -50,10 +50,9 @@ class CAvgGrad_TransLM final : public CAvgGrad_Scalar<FlowIndices> {
   using Base::ScalarVar_j;
   using Base::Proj_Mean_GradScalarVar;
   using Base::proj_vector_ij;
-  using Base::implicit;
   using Base::Flux;
   using Base::Jacobian_i;
-  using Base::Jacobian_j;  
+  using Base::Jacobian_j;
 
   /*!
    * \brief Adds any extra variables to AD
@@ -65,7 +64,8 @@ class CAvgGrad_TransLM final : public CAvgGrad_Scalar<FlowIndices> {
    * \param[in] config - Definition of the particular problem.
    */
   void FinishResidualCalc(const CConfig* config) override {
-   
+    const bool implicit = config->GetKind_TimeIntScheme() == EULER_IMPLICIT;
+
     /*--- Compute mean effective dynamic viscosity ---*/
     const su2double diff_i_gamma = Laminar_Viscosity_i + Eddy_Viscosity_i;
     const su2double diff_j_gamma = Laminar_Viscosity_j + Eddy_Viscosity_j;
@@ -101,5 +101,5 @@ class CAvgGrad_TransLM final : public CAvgGrad_Scalar<FlowIndices> {
   CAvgGrad_TransLM(unsigned short val_nDim, unsigned short val_nVar, bool correct_grad, const CConfig* config)
     : CAvgGrad_Scalar<FlowIndices>(val_nDim, val_nVar, correct_grad, config){
   }
-  
+
 };
diff --git a/SU2_CFD/include/numerics/turbulent/transition/trans_sources.hpp b/SU2_CFD/include/numerics/turbulent/transition/trans_sources.hpp
index 8f01a803705..de013fb1a67 100644
--- a/SU2_CFD/include/numerics/turbulent/transition/trans_sources.hpp
+++ b/SU2_CFD/include/numerics/turbulent/transition/trans_sources.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file trans_sources.hpp
  * \brief Numerics classes for integration of source terms in transition problems.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -27,7 +27,7 @@
 #pragma once
 #include "../../../../../Common/include/toolboxes/geometry_toolbox.hpp"
 #include "../../scalar/scalar_sources.hpp"
-
+#include "./trans_correlations.hpp"
 
 /*!
  * \class CSourcePieceWise_TranLM
@@ -40,6 +40,8 @@ class CSourcePieceWise_TransLM final : public CNumerics {
  private:
   const FlowIndices idx; /*!< \brief Object to manage the access to the flow primitives. */
 
+  const LM_ParsedOptions options;
+
   /*--- LM Closure constants ---*/
   const su2double c_e1 = 1.0;
   const su2double c_a1 = 2.0;
@@ -48,11 +50,20 @@ class CSourcePieceWise_TransLM final : public CNumerics {
   const su2double sigmaf = 1.0;
   const su2double s1 = 2.0;
   const su2double c_theta = 0.03;
+  const su2double c_CF = 0.6;
   const su2double sigmat = 2.0;
 
+  TURB_FAMILY TurbFamily;
+  su2double hRoughness;
+
+  su2double IntermittencySep = 1.0;
+  su2double IntermittencyEff = 1.0;
+
   su2double Residual[2];
   su2double* Jacobian_i[2];
-  su2double Jacobian_Buffer[4];// Static storage for the Jacobian (which needs to be pointer for return type).
+  su2double Jacobian_Buffer[4];  // Static storage for the Jacobian (which needs to be pointer for return type).
+
+  TransLMCorrelations TransCorrelations;
 
  public:
   /*!
@@ -61,13 +72,18 @@ class CSourcePieceWise_TransLM final : public CNumerics {
    * \param[in] val_nVar - Number of variables of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  CSourcePieceWise_TransLM(unsigned short val_nDim, unsigned short val_nVar, const CConfig* config) 
-      : CNumerics(val_nDim, 2, config),
-        idx(val_nDim, config->GetnSpecies()) {
-    
+  CSourcePieceWise_TransLM(unsigned short val_nDim, unsigned short val_nVar, const CConfig* config)
+      : CNumerics(val_nDim, 2, config), idx(val_nDim, config->GetnSpecies()), options(config->GetLMParsedOptions()){
     /*--- "Allocate" the Jacobian using the static buffer. ---*/
     Jacobian_i[0] = Jacobian_Buffer;
     Jacobian_i[1] = Jacobian_Buffer + 2;
+
+    TurbFamily = TurbModelFamily(config->GetKind_Turb_Model());
+
+    hRoughness = config->GethRoughness();
+
+    TransCorrelations.SetOptions(options);
+    
   }
 
   /*!
@@ -76,178 +92,234 @@ class CSourcePieceWise_TransLM final : public CNumerics {
    * \return A lightweight const-view (read-only) of the residual/flux and Jacobians.
    */
   ResidualType<> ComputeResidual(const CConfig* config) override {
-  /*--- ScalarVar[0] = k, ScalarVar[0] = w, TransVar[0] = gamma, and TransVar[0] = ReThetaT ---*/
-  /*--- dU/dx = PrimVar_Grad[1][0] ---*/
-  AD::StartPreacc();
-  AD::SetPreaccIn(StrainMag_i);
-  AD::SetPreaccIn(ScalarVar_i, nVar);
-  AD::SetPreaccIn(ScalarVar_Grad_i, nVar, nDim);
-  AD::SetPreaccIn(TransVar_i, nVar);
-  AD::SetPreaccIn(TransVar_Grad_i, nVar, nDim);
-  AD::SetPreaccIn(Volume); AD::SetPreaccIn(dist_i);
-  AD::SetPreaccIn(&V_i[idx.Velocity()], nDim);
-  AD::SetPreaccIn(PrimVar_Grad_i, nDim+idx.Velocity(), nDim);
-  AD::SetPreaccIn(Vorticity_i, 3);
-
-  su2double VorticityMag = sqrt(Vorticity_i[0]*Vorticity_i[0] +
-                                Vorticity_i[1]*Vorticity_i[1] +
-                                Vorticity_i[2]*Vorticity_i[2]);
-  
-  const su2double vel_u = V_i[idx.Velocity()];
-  const su2double vel_v = V_i[1+idx.Velocity()];
-  const su2double vel_w = (nDim ==3) ? V_i[2+idx.Velocity()] : 0.0;
-
-  const su2double Velocity_Mag = sqrt(vel_u*vel_u + vel_v*vel_v + vel_w*vel_w);
-
-  AD::SetPreaccIn(V_i[idx.Density()], V_i[idx.LaminarViscosity()], V_i[idx.EddyViscosity()]);
-
-  Density_i = V_i[idx.Density()];
-  Laminar_Viscosity_i = V_i[idx.LaminarViscosity()];
-  Eddy_Viscosity_i = V_i[idx.EddyViscosity()];
-
-  Residual[0] = 0.0;       Residual[1] = 0.0;
-  Jacobian_i[0][0] = 0.0;  Jacobian_i[0][1] = 0.0;
-  Jacobian_i[1][0] = 0.0;  Jacobian_i[1][1] = 0.0;
-  
-  if (dist_i > 1e-10) {
-
-    /*--- Corr_RetC correlation*/
-    su2double Corr_Rec = 0.0;
-    if(TransVar_i[1] <= 1870){
-     Corr_Rec = TransVar_i[1] - (396.035e-02 + (-120.656e-04)*TransVar_i[1] + (868.230e-06)*pow(TransVar_i[1], 2.) 
-                                +(-696.506e-09)*pow(TransVar_i[1], 3.) + (174.105e-12)*pow(TransVar_i[1], 4.));
-    } else {
-     Corr_Rec = TransVar_i[1] - (  593.11 + (TransVar_i[1] - 1870.0) * 0.482);
-    }
+    /*--- ScalarVar[0] = k, ScalarVar[0] = w, TransVar[0] = gamma, and TransVar[0] = ReThetaT ---*/
+    /*--- dU/dx = PrimVar_Grad[1][0] ---*/
+    AD::StartPreacc();
+    AD::SetPreaccIn(StrainMag_i);
+    AD::SetPreaccIn(ScalarVar_i, nVar);
+    AD::SetPreaccIn(ScalarVar_Grad_i, nVar, nDim);
+    AD::SetPreaccIn(TransVar_i, nVar);
+    AD::SetPreaccIn(TransVar_Grad_i, nVar, nDim);
+    AD::SetPreaccIn(Volume);
+    AD::SetPreaccIn(dist_i);
+    AD::SetPreaccIn(&V_i[idx.Velocity()], nDim);
+    AD::SetPreaccIn(PrimVar_Grad_i, nDim + idx.Velocity(), nDim);
+    AD::SetPreaccIn(Vorticity_i, 3);
+
+    su2double VorticityMag =
+        sqrt(Vorticity_i[0] * Vorticity_i[0] + Vorticity_i[1] * Vorticity_i[1] + Vorticity_i[2] * Vorticity_i[2]);
+
+    const su2double vel_u = V_i[idx.Velocity()];
+    const su2double vel_v = V_i[1 + idx.Velocity()];
+    const su2double vel_w = (nDim == 3) ? V_i[2 + idx.Velocity()] : 0.0;
+
+    const su2double Velocity_Mag = sqrt(vel_u * vel_u + vel_v * vel_v + vel_w * vel_w);
+
+    AD::SetPreaccIn(V_i[idx.Density()], V_i[idx.LaminarViscosity()], V_i[idx.EddyViscosity()]);
+
+    Density_i = V_i[idx.Density()];
+    Laminar_Viscosity_i = V_i[idx.LaminarViscosity()];
+    Eddy_Viscosity_i = V_i[idx.EddyViscosity()];
+
+    Residual[0] = 0.0;
+    Residual[1] = 0.0;
+    Jacobian_i[0][0] = 0.0;
+    Jacobian_i[0][1] = 0.0;
+    Jacobian_i[1][0] = 0.0;
+    Jacobian_i[1][1] = 0.0;
 
-    /*--- F_length correlation*/
-    su2double Corr_F_length = 0.0;
-    if(TransVar_i[1] < 400){
-      Corr_F_length = 398.189e-01 + (-119.270e-04)*TransVar_i[1] + (-132.567e-06) * pow(TransVar_i[1], 2.);
-    } 
-    else if(TransVar_i[1] >= 400 && TransVar_i[1] < 596) {
-      Corr_F_length = 263.404 + (-123.939e-02) * TransVar_i[1] + (194.548e-5) * pow(TransVar_i[1], 2.) + (-101.695e-08) * pow(TransVar_i[1], 3.);
-    } 
-    else if(TransVar_i[1] >= 596 && TransVar_i[1] < 1200) {
-      Corr_F_length = 0.5 - (TransVar_i[1] - 596.0) * 3.0e-04;
-    } 
-    else {
-      Corr_F_length = 0.3188;
-    }    
-
-    /*--- F_length ---*/
-    const su2double r_omega = Density_i*dist_i*dist_i*ScalarVar_i[1]/Laminar_Viscosity_i;
-    const su2double f_sub = exp(-pow(r_omega/200.0, 2));
-    const su2double F_length = Corr_F_length *(1.-f_sub) + 40.0*f_sub;
-
-    /*--- F_onset ---*/
-    const su2double R_t = Density_i*ScalarVar_i[0]/ Laminar_Viscosity_i/ ScalarVar_i[1];
-    const su2double Re_v = Density_i*dist_i*dist_i*StrainMag_i/Laminar_Viscosity_i;
-    const su2double F_onset1 = Re_v / (2.193 * Corr_Rec);
-    const su2double F_onset2 = min(max(F_onset1, pow(F_onset1, 4.0)), 2.0);
-    const su2double F_onset3 = max(1.0 - pow(R_t/2.5, 3.0), 0.0);
-    const su2double F_onset = max(F_onset2 - F_onset3, 0.0);
-
-    /*-- Gradient of velocity magnitude ---*/
-
-    su2double dU_dx = 0.5/Velocity_Mag*( 2.*vel_u*PrimVar_Grad_i[1][0]
-                              +2.*vel_v*PrimVar_Grad_i[2][0]);
-    if (nDim==3)
-      dU_dx += 0.5/Velocity_Mag*( 2.*vel_w*PrimVar_Grad_i[3][0]);
-
-    su2double dU_dy = 0.5/Velocity_Mag*( 2.*vel_u*PrimVar_Grad_i[1][1]
-                              +2.*vel_v*PrimVar_Grad_i[2][1]);
-    if (nDim==3)
-      dU_dy += 0.5/Velocity_Mag*( 2.*vel_w*PrimVar_Grad_i[3][1]);
-
-    su2double dU_dz = 0.0;
-    if (nDim==3)
-      dU_dz = 0.5/Velocity_Mag*( 2.*vel_u*PrimVar_Grad_i[1][2]
-                                +2.*vel_v*PrimVar_Grad_i[2][2]
-                                +2.*vel_w*PrimVar_Grad_i[3][2]);
-
-    su2double du_ds = vel_u/Velocity_Mag*dU_dx + vel_v/Velocity_Mag*dU_dy;
-    if (nDim==3)
-      du_ds += vel_w/Velocity_Mag * dU_dz;
-    
-    /*-- Calculate blending function f_theta --*/
+    if (dist_i > 1e-10) {
+      su2double Tu = 1.0;
+      if (TurbFamily == TURB_FAMILY::KW) Tu = max(100.0 * sqrt(2.0 * ScalarVar_i[0] / 3.0) / Velocity_Mag, 0.027);
+      if (TurbFamily == TURB_FAMILY::SA) Tu = config->GetTurbulenceIntensity_FreeStream() * 100;
 
-    const su2double time_scale = 500.0*Laminar_Viscosity_i/Density_i/ Velocity_Mag /Velocity_Mag;
-    const su2double theta_bl = TransVar_i[1]*Laminar_Viscosity_i / Density_i /Velocity_Mag;
-    const su2double delta_bl = 7.5*theta_bl;
-    const su2double delta = 50.0*VorticityMag*dist_i/Velocity_Mag*delta_bl + 1e-20;
-    
-    const su2double re_omega = Density_i*ScalarVar_i[1]*dist_i*dist_i/Laminar_Viscosity_i;
-    const su2double f_wake = exp(-pow(re_omega/(1.0e+05),2));
-    
-    const su2double var1 = (TransVar_i[0]-1.0/c_e2)/(1.0-1.0/c_e2);
-    const su2double var2 = 1.0 - pow(var1,2.0);
-    const su2double f_theta = min(max(f_wake*exp(-pow(dist_i/delta, 4)), var2), 1.0);
-    const su2double f_turb = exp(-pow(R_t/4, 4));
-
-    /*--- Corr_RetT correlation*/
-    su2double Corr_Ret_lim = 20.0;
-    su2double f_lambda = 1.0;
-    
-    su2double Retheta_Error = 200.0 , Retheta_old = 0.0;
-    su2double lambda = 0.0;
-    su2double Corr_Ret = 20.0;
-    const su2double Tu = max(100.0*sqrt( 2.0 * ScalarVar_i[0] / 3.0 ) / Velocity_Mag,0.027);
-    
-    for (int iter=0; iter<100 ; iter++) {
-      
-      su2double theta = Corr_Ret * Laminar_Viscosity_i / Density_i/ Velocity_Mag;
-      lambda = Density_i*theta*theta/ Laminar_Viscosity_i*du_ds;
-      lambda = min(max(-0.1, lambda), 0.1);
-
-      if (lambda<=0.0) {
-        f_lambda = 1. - (-12.986*lambda - 123.66*lambda*lambda -
-                         405.689*lambda*lambda*lambda)*exp(-pow(Tu/1.5, 1.5));
-      } else {
-        f_lambda = 1. + 0.275*(1.-exp(-35.*lambda))*exp(-Tu/0.5);
-      }
+      /*--- Corr_RetC correlation*/
+      const su2double Corr_Rec = TransCorrelations.ReThetaC_Correlations(Tu, TransVar_i[1]);
 
-      if (Tu <= 1.3) {
-        Corr_Ret = f_lambda * (1173.51 - 589.428*Tu + 0.2196/Tu/Tu);
-      } else {
-        Corr_Ret = 331.5 * f_lambda*pow(Tu - 0.5658,-0.671);
-      }
-      Corr_Ret = max(Corr_Ret, Corr_Ret_lim);
+      /*--- F_length correlation*/
+      const su2double Corr_F_length = TransCorrelations.FLength_Correlations(Tu, TransVar_i[1]);
 
-      Retheta_Error = fabs(Retheta_old -Corr_Ret)/Retheta_old;
+      /*--- F_length ---*/
+      su2double F_length = 0.0;
+      if (TurbFamily == TURB_FAMILY::KW) {
+        const su2double r_omega = Density_i * dist_i * dist_i * ScalarVar_i[1] / Laminar_Viscosity_i;
+        const su2double f_sub = exp(-pow(r_omega / 200.0, 2));
+        F_length = Corr_F_length * (1. - f_sub) + 40.0 * f_sub;
+      }
+      if (TurbFamily == TURB_FAMILY::SA) F_length = Corr_F_length;
+
+      /*--- F_onset ---*/
+      su2double R_t = 1.0;
+      if (TurbFamily == TURB_FAMILY::KW) R_t = Density_i * ScalarVar_i[0] / Laminar_Viscosity_i / ScalarVar_i[1];
+      if (TurbFamily == TURB_FAMILY::SA) R_t = Eddy_Viscosity_i / Laminar_Viscosity_i;
+
+      const su2double Re_v = Density_i * dist_i * dist_i * StrainMag_i / Laminar_Viscosity_i;
+      const su2double F_onset1 = Re_v / (2.193 * Corr_Rec);
+      su2double F_onset2 = 1.0;
+      su2double F_onset3 = 1.0;
+      if (TurbFamily == TURB_FAMILY::KW) {
+        F_onset2 = min(max(F_onset1, pow(F_onset1, 4.0)), 2.0);
+        F_onset3 = max(1.0 - pow(R_t / 2.5, 3.0), 0.0);
+      }
+      if (TurbFamily == TURB_FAMILY::SA) {
+        F_onset2 = min(max(F_onset1, pow(F_onset1, 4.0)), 4.0);
+        F_onset3 = max(2.0 - pow(R_t / 2.5, 3.0), 0.0);
+      }
+      const su2double F_onset = max(F_onset2 - F_onset3, 0.0);
+
+      /*-- Gradient of velocity magnitude ---*/
+
+      su2double dU_dx = 0.5 / Velocity_Mag * (2. * vel_u * PrimVar_Grad_i[1][0] + 2. * vel_v * PrimVar_Grad_i[2][0]);
+      if (nDim == 3) dU_dx += 0.5 / Velocity_Mag * (2. * vel_w * PrimVar_Grad_i[3][0]);
+
+      su2double dU_dy = 0.5 / Velocity_Mag * (2. * vel_u * PrimVar_Grad_i[1][1] + 2. * vel_v * PrimVar_Grad_i[2][1]);
+      if (nDim == 3) dU_dy += 0.5 / Velocity_Mag * (2. * vel_w * PrimVar_Grad_i[3][1]);
+
+      su2double dU_dz = 0.0;
+      if (nDim == 3)
+        dU_dz =
+            0.5 / Velocity_Mag *
+            (2. * vel_u * PrimVar_Grad_i[1][2] + 2. * vel_v * PrimVar_Grad_i[2][2] + 2. * vel_w * PrimVar_Grad_i[3][2]);
+
+      su2double du_ds = vel_u / Velocity_Mag * dU_dx + vel_v / Velocity_Mag * dU_dy;
+      if (nDim == 3) du_ds += vel_w / Velocity_Mag * dU_dz;
+
+      /*-- Calculate blending function f_theta --*/
+      su2double time_scale = 500.0 * Laminar_Viscosity_i / Density_i / Velocity_Mag / Velocity_Mag;
+      if (options.LM2015)
+        time_scale = min(time_scale,
+                         Density_i * LocalGridLength_i * LocalGridLength_i / (Laminar_Viscosity_i + Eddy_Viscosity_i));
+      const su2double theta_bl = TransVar_i[1] * Laminar_Viscosity_i / Density_i / Velocity_Mag;
+      const su2double delta_bl = 7.5 * theta_bl;
+      const su2double delta = 50.0 * VorticityMag * dist_i / Velocity_Mag * delta_bl + 1e-20;
+
+      su2double f_wake = 0.0;
+      if (TurbFamily == TURB_FAMILY::KW) {
+        const su2double re_omega = Density_i * ScalarVar_i[1] * dist_i * dist_i / Laminar_Viscosity_i;
+        f_wake = exp(-pow(re_omega / (1.0e+05), 2));
+      }
+      if (TurbFamily == TURB_FAMILY::SA) f_wake = 1.0;
+
+      const su2double var1 = (TransVar_i[0] - 1.0 / c_e2) / (1.0 - 1.0 / c_e2);
+      const su2double var2 = 1.0 - pow(var1, 2.0);
+      const su2double f_theta = min(max(f_wake * exp(-pow(dist_i / delta, 4)), var2), 1.0);
+      const su2double f_turb = exp(-pow(R_t / 4, 4));
+
+      su2double f_theta_2 = 0.0;
+      if (options.LM2015)
+        f_theta_2 = min(f_wake * exp(-pow(dist_i / delta, 4.0)), 1.0);
+
+      /*--- Corr_Ret correlation*/
+      const su2double Corr_Ret_lim = 20.0;
+      su2double f_lambda = 1.0;
+
+      su2double Retheta_Error = 200.0, Retheta_old = 0.0;
+      su2double lambda = 0.0;
+      su2double Corr_Ret = 20.0;
+
+      for (int iter = 0; iter < 100; iter++) {
+        su2double theta = Corr_Ret * Laminar_Viscosity_i / Density_i / Velocity_Mag;
+        lambda = Density_i * theta * theta / Laminar_Viscosity_i * du_ds;
+        lambda = min(max(-0.1, lambda), 0.1);
+
+        if (lambda <= 0.0) {
+          f_lambda = 1. - (-12.986 * lambda - 123.66 * lambda * lambda - 405.689 * lambda * lambda * lambda) *
+                              exp(-pow(Tu / 1.5, 1.5));
+        } else {
+          f_lambda = 1. + 0.275 * (1. - exp(-35. * lambda)) * exp(-Tu / 0.5);
+        }
+
+        if (Tu <= 1.3) {
+          Corr_Ret = f_lambda * (1173.51 - 589.428 * Tu + 0.2196 / Tu / Tu);
+        } else {
+          Corr_Ret = 331.5 * f_lambda * pow(Tu - 0.5658, -0.671);
+        }
+        Corr_Ret = max(Corr_Ret, Corr_Ret_lim);
+
+        Retheta_Error = fabs(Retheta_old - Corr_Ret) / Retheta_old;
+
+        if (Retheta_Error < 0.0000001) {
+          break;
+        }
+
+        Retheta_old = Corr_Ret;
+      }
 
-      if(Retheta_Error < 0.0000001){
-        iter = 101;
+      /*-- Corr_RetT_SCF Correlations--*/
+      su2double ReThetat_SCF = 0.0;
+      if (options.LM2015) {
+        su2double VelocityNormalized[3];
+        VelocityNormalized[0] = vel_u / Velocity_Mag;
+        VelocityNormalized[1] = vel_v / Velocity_Mag;
+        if (nDim == 3) VelocityNormalized[2] = vel_w / Velocity_Mag;
+
+        su2double StreamwiseVort = 0.0;
+        for (auto iDim = 0u; iDim < nDim; iDim++) {
+          StreamwiseVort += VelocityNormalized[iDim] * Vorticity_i[iDim];
+        }
+        StreamwiseVort = abs(StreamwiseVort);
+
+        const su2double H_CF = StreamwiseVort * dist_i / Velocity_Mag;
+        const su2double DeltaH_CF = H_CF * (1.0 + min(Eddy_Viscosity_i / Laminar_Viscosity_i, 0.4));
+        const su2double DeltaH_CF_Minus = max(-1.0 * (0.1066 - DeltaH_CF), 0.0);
+        const su2double DeltaH_CF_Plus = max(0.1066 - DeltaH_CF, 0.0);
+        const su2double fDeltaH_CF_Minus = 75.0 * tanh(DeltaH_CF_Minus / 0.0125);
+        const su2double fDeltaH_CF_Plus = 6200 * DeltaH_CF_Plus + 50000 * DeltaH_CF_Plus * DeltaH_CF_Plus;
+
+        const su2double toll = 1e-5;
+        su2double error = toll + 1.0;
+        su2double thetat_SCF = 0.0;
+        su2double rethetat_SCF_old = 20.0;
+        const int nMax = 100;
+
+        int iter;
+        for (iter = 0; iter < nMax && error > toll; iter++) {
+          thetat_SCF = rethetat_SCF_old * Laminar_Viscosity_i / (Density_i * (Velocity_Mag / 0.82));
+          thetat_SCF = max(1e-20, thetat_SCF);
+
+          ReThetat_SCF = -35.088 * log(hRoughness / thetat_SCF) + 319.51 + fDeltaH_CF_Plus - fDeltaH_CF_Minus;
+
+          error = abs(ReThetat_SCF - rethetat_SCF_old) / rethetat_SCF_old;
+
+          rethetat_SCF_old = ReThetat_SCF;
+        }
       }
 
-      Retheta_old = Corr_Ret;
+      /*-- production term of Intermeittency(Gamma) --*/
+      const su2double Pg =
+          F_length * c_a1 * Density_i * StrainMag_i * sqrt(F_onset * TransVar_i[0]) * (1.0 - c_e1 * TransVar_i[0]);
+
+      /*-- destruction term of Intermeittency(Gamma) --*/
+      const su2double Dg = c_a2 * Density_i * VorticityMag * TransVar_i[0] * f_turb * (c_e2 * TransVar_i[0] - 1.0);
+
+      /*-- production term of ReThetaT --*/
+      const su2double PRethetat = c_theta * Density_i / time_scale * (Corr_Ret - TransVar_i[1]) * (1.0 - f_theta);
+
+      /*-- destruction term of ReThetaT --*/
+      // It should not be with the minus sign but I put for consistency
+      su2double DRethetat = 0.0;
+      if (options.LM2015)
+        DRethetat = -c_theta * (Density_i / time_scale) * c_CF * min(ReThetat_SCF - TransVar_i[1], 0.0) * f_theta_2;
+
+      /*--- Source ---*/
+      Residual[0] += (Pg - Dg) * Volume;
+      Residual[1] += (PRethetat - DRethetat) * Volume;
+
+      /*--- Implicit part ---*/
+      Jacobian_i[0][0] = (F_length * c_a1 * StrainMag_i * sqrt(F_onset) *
+                              (0.5 * pow(TransVar_i[0], -0.5) - 1.5 * c_e1 * pow(TransVar_i[0], 0.5)) -
+                          c_a2 * VorticityMag * f_turb * (2.0 * c_e2 * TransVar_i[0] - 1.0)) *
+                         Volume;
+      Jacobian_i[0][1] = 0.0;
+      Jacobian_i[1][0] = 0.0;
+      Jacobian_i[1][1] = -c_theta / time_scale * (1.0 - f_theta) * Volume;
+      if (options.LM2015 && ReThetat_SCF - TransVar_i[1] < 0)
+        Jacobian_i[1][1] += (c_theta / time_scale) * c_CF * f_theta_2 * Volume;
     }
-    
-    /*-- production term of Intermeittency(Gamma) --*/
-    const su2double Pg = F_length*c_a1*Density_i*StrainMag_i*sqrt(F_onset*TransVar_i[0])*(1.0 - c_e1 * TransVar_i[0]);
-
-    /*-- destruction term of Intermeittency(Gamma) --*/
-    const su2double Dg = c_a2*Density_i*VorticityMag*TransVar_i[0]*f_turb*(c_e2*TransVar_i[0] - 1.0);
-
-    /*-- production term of ReThetaT --*/
-    const su2double Pthetat = c_theta*Density_i/time_scale * (Corr_Ret-TransVar_i[1])  * (1.0-f_theta);
 
-    /*--- Source ---*/
-    Residual[0] += (Pg - Dg)*Volume;
-    Residual[1] += Pthetat*Volume;
+    AD::SetPreaccOut(Residual, nVar);
+    AD::EndPreacc();
 
-    /*--- Implicit part ---*/   
-    Jacobian_i[0][0] = (F_length*c_a1*StrainMag_i*sqrt(F_onset)*(0.5*pow(TransVar_i[0], -0.5) -1.5*c_e1*pow(TransVar_i[0], 0.5))
-                       - c_a2 * VorticityMag*f_turb*(2.0*c_e2*TransVar_i[0]-1.0) )*Volume;
-    Jacobian_i[0][1] = 0.0;
-    Jacobian_i[1][0] = 0.0;
-    Jacobian_i[1][1] = -c_theta/time_scale*(1.0-f_theta)*Volume;
-  }  
-  
-  AD::SetPreaccOut(Residual, nVar);
-  AD::EndPreacc();
-
-  return ResidualType<>(Residual, Jacobian_i, nullptr);
+    return ResidualType<>(Residual, Jacobian_i, nullptr);
   }
 };
-
diff --git a/SU2_CFD/include/numerics/turbulent/turb_convection.hpp b/SU2_CFD/include/numerics/turbulent/turb_convection.hpp
index 652a0c907b4..9723d186bbf 100644
--- a/SU2_CFD/include/numerics/turbulent/turb_convection.hpp
+++ b/SU2_CFD/include/numerics/turbulent/turb_convection.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for discretization of
  *        convective fluxes in turbulence problems.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/turbulent/turb_diffusion.hpp b/SU2_CFD/include/numerics/turbulent/turb_diffusion.hpp
index bf5f6097387..f871588c47c 100644
--- a/SU2_CFD/include/numerics/turbulent/turb_diffusion.hpp
+++ b/SU2_CFD/include/numerics/turbulent/turb_diffusion.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for discretization of
  *        viscous fluxes in turbulence problems.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -47,7 +47,6 @@ class CAvgGrad_TurbSA final : public CAvgGrad_Scalar<FlowIndices> {
   using Base::ScalarVar_j;
   using Base::Proj_Mean_GradScalarVar;
   using Base::proj_vector_ij;
-  using Base::implicit;
   using Base::Flux;
   using Base::Jacobian_i;
   using Base::Jacobian_j;
@@ -64,6 +63,8 @@ class CAvgGrad_TurbSA final : public CAvgGrad_Scalar<FlowIndices> {
    * \param[in] config - Definition of the particular problem.
    */
   void FinishResidualCalc(const CConfig* config) override {
+    const bool implicit = config->GetKind_TimeIntScheme() == EULER_IMPLICIT;
+
     /*--- Compute mean effective viscosity ---*/
 
     const su2double nu_i = Laminar_Viscosity_i/Density_i;
@@ -111,7 +112,6 @@ class CAvgGrad_TurbSA_Neg final : public CAvgGrad_Scalar<FlowIndices> {
   using Base::ScalarVar_j;
   using Base::Proj_Mean_GradScalarVar;
   using Base::proj_vector_ij;
-  using Base::implicit;
   using Base::Flux;
   using Base::Jacobian_i;
   using Base::Jacobian_j;
@@ -129,6 +129,8 @@ class CAvgGrad_TurbSA_Neg final : public CAvgGrad_Scalar<FlowIndices> {
    * \param[in] config - Definition of the particular problem.
    */
   void FinishResidualCalc(const CConfig* config) override {
+    const bool implicit = config->GetKind_TimeIntScheme() == EULER_IMPLICIT;
+
     /*--- Compute mean effective viscosity ---*/
 
     const su2double nu_i = Laminar_Viscosity_i/Density_i;
@@ -191,7 +193,6 @@ class CAvgGrad_TurbSST final : public CAvgGrad_Scalar<FlowIndices> {
   using Base::ScalarVar_j;
   using Base::Proj_Mean_GradScalarVar;
   using Base::proj_vector_ij;
-  using Base::implicit;
   using Base::Flux;
   using Base::Jacobian_i;
   using Base::Jacobian_j;
@@ -215,6 +216,8 @@ class CAvgGrad_TurbSST final : public CAvgGrad_Scalar<FlowIndices> {
    * \param[in] config - Definition of the particular problem.
    */
   void FinishResidualCalc(const CConfig* config) override {
+    const bool implicit = config->GetKind_TimeIntScheme() == EULER_IMPLICIT;
+
     /*--- Compute the blended constant for the viscous terms ---*/
     const su2double sigma_kine_i = F1_i*sigma_k1 + (1.0 - F1_i)*sigma_k2;
     const su2double sigma_kine_j = F1_j*sigma_k1 + (1.0 - F1_j)*sigma_k2;
diff --git a/SU2_CFD/include/numerics/turbulent/turb_sources.hpp b/SU2_CFD/include/numerics/turbulent/turb_sources.hpp
index 62906b233ac..e11880bb41e 100644
--- a/SU2_CFD/include/numerics/turbulent/turb_sources.hpp
+++ b/SU2_CFD/include/numerics/turbulent/turb_sources.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file turb_sources.hpp
  * \brief Numerics classes for integration of source terms in turbulence problems.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -53,7 +53,9 @@ struct CSAVariables {
   su2double ft2, d_ft2, r, d_r, g, d_g, glim, fw, d_fw, Ji, d_Ji, S, Shat, d_Shat, fv1, d_fv1, fv2, d_fv2;
 
   /*--- List of helpers ---*/
-  su2double Omega, dist_i_2, inv_k2_d2, inv_Shat, g_6, norm2_Grad, gamma_bc;
+  su2double Omega, dist_i_2, inv_k2_d2, inv_Shat, g_6, norm2_Grad;
+  
+  su2double intermittency, interDestrFactor;
 };
 
 /*!
@@ -66,7 +68,6 @@ struct CSAVariables {
 template <class FlowIndices, class Omega, class ft2, class ModVort, class rFunc, class SourceTerms>
 class CSourceBase_TurbSA : public CNumerics {
  protected:
-  su2double Gamma_BC = 0.0;
 
   /*--- Residual and Jacobian ---*/
   su2double Residual, *Jacobian_i;
@@ -75,6 +76,8 @@ class CSourceBase_TurbSA : public CNumerics {
   const FlowIndices idx; /*!< \brief Object to manage the access to the flow primitives. */
   const SA_ParsedOptions options; /*!< \brief Struct with SA options. */
 
+  bool transition_LM;
+
  public:
   /*!
    * \brief Constructor of the class.
@@ -84,17 +87,13 @@ class CSourceBase_TurbSA : public CNumerics {
   CSourceBase_TurbSA(unsigned short nDim, const CConfig* config)
       : CNumerics(nDim, 1, config),
         idx(nDim, config->GetnSpecies()),
-        options(config->GetSAParsedOptions()) {
+        options(config->GetSAParsedOptions()),
+        transition_LM(config->GetKind_Trans_Model() == TURB_TRANS_MODEL::LM) {
     /*--- Setup the Jacobian pointer, we need to return su2double** but we know
      * the Jacobian is 1x1 so we use this trick to avoid heap allocation. ---*/
     Jacobian_i = &Jacobian_Buffer;
   }
 
-  /*!
-   * \brief Get the intermittency for the BC transition model.
-   * \return Value of the intermittency.
-   */
-  su2double GetGammaBC() const final { return Gamma_BC; }
 
   /*!
    * \brief Residual for source term integration.
@@ -191,11 +190,22 @@ class CSourceBase_TurbSA : public CNumerics {
         const su2double term2 = sqrt(max((nu_t * chi_2) / nu, 0.0));
         const su2double term_exponential = (term1 + term2);
 
-        Gamma_BC = 1.0 - exp(-term_exponential);
-        var.gamma_bc = Gamma_BC;
+        intermittency_eff_i = 1.0 - exp(-term_exponential);
+        var.intermittency = intermittency_eff_i;
+        var.interDestrFactor = 1;
+
+      } else if (transition_LM){
+
+        var.intermittency = intermittency_eff_i;
+        //var.intermittency = 1.0;
+        // Is wrong the reference from NASA?
+        // Original max(min(gamma, 0.5), 1.0) always gives 1 as result.
+        var.interDestrFactor = min(max(intermittency_i, 0.5), 1.0);
+
       } else {
         /*--- Do not modify the production. ---*/
-        var.gamma_bc = 1.0;
+        var.intermittency = 1.0;
+        var.interDestrFactor = 1.0;
       }
 
       /*--- Compute production, destruction and cross production and jacobian ---*/
@@ -386,7 +396,7 @@ struct Bsl {
 
   static void ComputeProduction(const su2double& nue, const CSAVariables& var, su2double& production,
                                 su2double& jacobian) {
-    const su2double factor = var.gamma_bc * var.cb1;
+    const su2double factor = var.intermittency * var.cb1;
     production = factor * (1.0 - var.ft2) * var.Shat * nue;
     jacobian += factor * (-var.Shat * nue * var.d_ft2 + (1.0 - var.ft2) * (nue * var.d_Shat + var.Shat));
   }
@@ -395,8 +405,8 @@ struct Bsl {
                                  su2double& jacobian) {
     const su2double cb1_k2 = var.cb1 / var.k2;
     const su2double factor = var.cw1 * var.fw - cb1_k2 * var.ft2;
-    destruction = factor * pow(nue, 2) / var.dist_i_2;
-    jacobian -= ((var.cw1 * var.d_fw - cb1_k2 * var.d_ft2) * pow(nue, 2) + factor * 2 * nue) / var.dist_i_2;
+    destruction = var.interDestrFactor * factor * pow(nue, 2) / var.dist_i_2;
+    jacobian -= var.interDestrFactor * ((var.cw1 * var.d_fw - cb1_k2 * var.d_ft2) * pow(nue, 2) + factor * 2 * nue) / var.dist_i_2;
   }
 
   static void ComputeCrossProduction(const su2double& nue, const CSAVariables& var, su2double& cross_production,
@@ -421,7 +431,7 @@ struct Neg {
 
   static void ComputeProduction(const su2double& nue, const CSAVariables& var, su2double& production,
                                 su2double& jacobian) {
-    const su2double dP_dnu = var.gamma_bc * var.cb1 * (1.0 - var.ct3) * var.S;
+    const su2double dP_dnu = var.intermittency * var.cb1 * (1.0 - var.ct3) * var.S;
     production = dP_dnu * nue;
     jacobian += dP_dnu;
   }
@@ -430,8 +440,8 @@ struct Neg {
                                  su2double& jacobian) {
     /*--- The destruction when nue < 0 is added instead of the usual subtraction, hence the negative sign. ---*/
     const su2double dD_dnu = -var.cw1 * nue / var.dist_i_2;
-    destruction = dD_dnu * nue;
-    jacobian -= 2 * dD_dnu;
+    destruction = dD_dnu * nue * var.interDestrFactor;
+    jacobian -= 2 * dD_dnu * var.interDestrFactor;
   }
 
   static void ComputeCrossProduction(const su2double& nue, const CSAVariables& var, su2double& cross_production,
diff --git a/SU2_CFD/include/numerics_simd/CNumericsSIMD.cpp b/SU2_CFD/include/numerics_simd/CNumericsSIMD.cpp
index c967217c854..3b40b5f4d92 100644
--- a/SU2_CFD/include/numerics_simd/CNumericsSIMD.cpp
+++ b/SU2_CFD/include/numerics_simd/CNumericsSIMD.cpp
@@ -4,7 +4,7 @@
  * \note This should be the only cpp for this family of classes
  * (which are all templates). All compilation takes place here.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics_simd/CNumericsSIMD.hpp b/SU2_CFD/include/numerics_simd/CNumericsSIMD.hpp
index 3339dada920..82cdadbd8b8 100644
--- a/SU2_CFD/include/numerics_simd/CNumericsSIMD.hpp
+++ b/SU2_CFD/include/numerics_simd/CNumericsSIMD.hpp
@@ -2,7 +2,7 @@
  * \file CNumericsSIMD.hpp
  * \brief Vectorized (SIMD) numerics classes.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics_simd/flow/convection/centered.hpp b/SU2_CFD/include/numerics_simd/flow/convection/centered.hpp
index ab8487275c8..d5358d771ba 100644
--- a/SU2_CFD/include/numerics_simd/flow/convection/centered.hpp
+++ b/SU2_CFD/include/numerics_simd/flow/convection/centered.hpp
@@ -2,7 +2,7 @@
  * \file centered.hpp
  * \brief Centered convective schemes.
  * \author P. Gomes, F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics_simd/flow/convection/common.hpp b/SU2_CFD/include/numerics_simd/flow/convection/common.hpp
index 10f245c5243..e88f58c98b4 100644
--- a/SU2_CFD/include/numerics_simd/flow/convection/common.hpp
+++ b/SU2_CFD/include/numerics_simd/flow/convection/common.hpp
@@ -2,7 +2,7 @@
  * \file common.hpp
  * \brief Common convection-related methods.
  * \author P. Gomes, F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics_simd/flow/convection/roe.hpp b/SU2_CFD/include/numerics_simd/flow/convection/roe.hpp
index f3e3defc844..99cff97f445 100644
--- a/SU2_CFD/include/numerics_simd/flow/convection/roe.hpp
+++ b/SU2_CFD/include/numerics_simd/flow/convection/roe.hpp
@@ -2,7 +2,7 @@
  * \file roe.hpp
  * \brief Roe-family of convective schemes.
  * \author P. Gomes, A. Bueno, F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -168,7 +168,7 @@ class CRoeBase : public Base {
 
     VectorDbl<nVar> flux;
     for (size_t iVar = 0; iVar < nVar; ++iVar) {
-      flux(iVar) = kappa * (flux_i(iVar) + flux_j(iVar));
+      flux(iVar) = 0.5 * (flux_i(iVar) + flux_j(iVar));
     }
 
     MatrixDbl<nVar> jac_i, jac_j;
diff --git a/SU2_CFD/include/numerics_simd/flow/diffusion/common.hpp b/SU2_CFD/include/numerics_simd/flow/diffusion/common.hpp
index 9484315d6ab..ecef279e5ed 100644
--- a/SU2_CFD/include/numerics_simd/flow/diffusion/common.hpp
+++ b/SU2_CFD/include/numerics_simd/flow/diffusion/common.hpp
@@ -2,7 +2,7 @@
  * \file common.hpp
  * \brief Helper functions for viscous methods.
  * \author P. Gomes, C. Pederson, A. Bueno, F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics_simd/flow/diffusion/viscous_fluxes.hpp b/SU2_CFD/include/numerics_simd/flow/diffusion/viscous_fluxes.hpp
index 39e6b508974..16f4fc08459 100644
--- a/SU2_CFD/include/numerics_simd/flow/diffusion/viscous_fluxes.hpp
+++ b/SU2_CFD/include/numerics_simd/flow/diffusion/viscous_fluxes.hpp
@@ -2,7 +2,7 @@
  * \file viscous_fluxes.hpp
  * \brief Decorator classes for computation of viscous fluxes.
  * \author P. Gomes, C. Pederson, A. Bueno, F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics_simd/flow/variables.hpp b/SU2_CFD/include/numerics_simd/flow/variables.hpp
index 920ddd0825c..51cddb2a8a7 100644
--- a/SU2_CFD/include/numerics_simd/flow/variables.hpp
+++ b/SU2_CFD/include/numerics_simd/flow/variables.hpp
@@ -2,7 +2,7 @@
  * \file variables.hpp
  * \brief Collection of types to store physical variables.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics_simd/util.hpp b/SU2_CFD/include/numerics_simd/util.hpp
index 1a0a16dd6b1..8e67cce67f1 100644
--- a/SU2_CFD/include/numerics_simd/util.hpp
+++ b/SU2_CFD/include/numerics_simd/util.hpp
@@ -2,7 +2,7 @@
  * \file util.hpp
  * \brief Generic auxiliary functions.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CAdjElasticityOutput.hpp b/SU2_CFD/include/output/CAdjElasticityOutput.hpp
index 20bab529488..fa49e4a8a81 100644
--- a/SU2_CFD/include/output/CAdjElasticityOutput.hpp
+++ b/SU2_CFD/include/output/CAdjElasticityOutput.hpp
@@ -2,7 +2,7 @@
  * \file CAdjElasticityOutput.hpp
  * \brief Headers of the adjoint elasticity output class.
  * \author T. Albring, R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CAdjFlowCompOutput.hpp b/SU2_CFD/include/output/CAdjFlowCompOutput.hpp
index b45fdf4dde4..e1662e286f3 100644
--- a/SU2_CFD/include/output/CAdjFlowCompOutput.hpp
+++ b/SU2_CFD/include/output/CAdjFlowCompOutput.hpp
@@ -2,7 +2,7 @@
  * \file CAdjFlowCompOutput.hpp
  * \brief Headers of the adjoint compressible flow output.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CAdjFlowIncOutput.hpp b/SU2_CFD/include/output/CAdjFlowIncOutput.hpp
index b265b571bde..f187bd4516f 100644
--- a/SU2_CFD/include/output/CAdjFlowIncOutput.hpp
+++ b/SU2_CFD/include/output/CAdjFlowIncOutput.hpp
@@ -2,7 +2,7 @@
  * \file CAdjFlowIncOutput.hpp
  * \brief Headers of the adjoint incompressible flow output.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CAdjFlowOutput.hpp b/SU2_CFD/include/output/CAdjFlowOutput.hpp
index d8ddc06d699..afe064e9da5 100644
--- a/SU2_CFD/include/output/CAdjFlowOutput.hpp
+++ b/SU2_CFD/include/output/CAdjFlowOutput.hpp
@@ -2,7 +2,7 @@
  * \file CAdjFlowOutput.hpp
  * \brief Headers of the adjoint flow output.
  * \author T. Kattmann
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CAdjHeatOutput.hpp b/SU2_CFD/include/output/CAdjHeatOutput.hpp
index 0752d7223e6..7c8071468e8 100644
--- a/SU2_CFD/include/output/CAdjHeatOutput.hpp
+++ b/SU2_CFD/include/output/CAdjHeatOutput.hpp
@@ -2,7 +2,7 @@
  * \file CAdjHeatOutput.hpp
  * \brief Headers of the adjoint heat output.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CBaselineOutput.hpp b/SU2_CFD/include/output/CBaselineOutput.hpp
index 2bb6b515796..fd066ec5e67 100644
--- a/SU2_CFD/include/output/CBaselineOutput.hpp
+++ b/SU2_CFD/include/output/CBaselineOutput.hpp
@@ -2,7 +2,7 @@
  * \file CBaselineOutput.hpp
  * \brief  Headers of the baseline output.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CElasticityOutput.hpp b/SU2_CFD/include/output/CElasticityOutput.hpp
index c65bc967e5f..e4238757719 100644
--- a/SU2_CFD/include/output/CElasticityOutput.hpp
+++ b/SU2_CFD/include/output/CElasticityOutput.hpp
@@ -2,7 +2,7 @@
  * \file CElasticityOutput.hpp
  * \brief  Headers of the elasticity output.
  * \author F. Palacios, T. Economon, M. Colonno
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CFVMOutput.hpp b/SU2_CFD/include/output/CFVMOutput.hpp
index 70ed557b406..07034524ba6 100644
--- a/SU2_CFD/include/output/CFVMOutput.hpp
+++ b/SU2_CFD/include/output/CFVMOutput.hpp
@@ -2,7 +2,7 @@
  * \file CFVMOutput.hpp
  * \brief  Headers of the Finite Volume Method output.
  * \author T. Kattmann
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -30,7 +30,7 @@
 #include "COutput.hpp"
 
 class CFVMOutput : public COutput{
-protected:
+ protected:
   /*!
    * \brief Constructor of the class
    */
diff --git a/SU2_CFD/include/output/CFlowCompFEMOutput.hpp b/SU2_CFD/include/output/CFlowCompFEMOutput.hpp
index 40293e0c042..9514ea4c491 100644
--- a/SU2_CFD/include/output/CFlowCompFEMOutput.hpp
+++ b/SU2_CFD/include/output/CFlowCompFEMOutput.hpp
@@ -2,7 +2,7 @@
  * \file CFlowCompFEMOutput.hpp
  * \brief  Headers of the compressible FEM flow output.
  * \author R. Sanchez, T. Albring.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CFlowCompOutput.hpp b/SU2_CFD/include/output/CFlowCompOutput.hpp
index d7e79017a05..c6c0b01b35a 100644
--- a/SU2_CFD/include/output/CFlowCompOutput.hpp
+++ b/SU2_CFD/include/output/CFlowCompOutput.hpp
@@ -2,7 +2,7 @@
  * \file CFlowCompOutput.hpp
  * \brief  Headers of the compressible flow output.
  * \author R. Sanchez, T. Albring.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CFlowIncOutput.hpp b/SU2_CFD/include/output/CFlowIncOutput.hpp
index 63ffddd9eea..a72f3c2b7a9 100644
--- a/SU2_CFD/include/output/CFlowIncOutput.hpp
+++ b/SU2_CFD/include/output/CFlowIncOutput.hpp
@@ -2,7 +2,7 @@
  * \file CFlowIncOutput.hpp
  * \brief  Headers of the incompressible flow output.
  * \author T. Albring, R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CFlowOutput.hpp b/SU2_CFD/include/output/CFlowOutput.hpp
index 3271c8926cd..44a7f55fbb2 100644
--- a/SU2_CFD/include/output/CFlowOutput.hpp
+++ b/SU2_CFD/include/output/CFlowOutput.hpp
@@ -2,7 +2,7 @@
  * \file CFlowOutput.hpp
  * \brief  Headers of the flow output.
  * \author F. Palacios, T. Economon, M. Colonno
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CHeatOutput.hpp b/SU2_CFD/include/output/CHeatOutput.hpp
index f5864b98a3b..be5cdf74822 100644
--- a/SU2_CFD/include/output/CHeatOutput.hpp
+++ b/SU2_CFD/include/output/CHeatOutput.hpp
@@ -2,7 +2,7 @@
  * \file CHeatOutput.hpp
  * \brief Headers of the heat output.
  * \author R. Sanchez, T. Albring.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CMeshOutput.hpp b/SU2_CFD/include/output/CMeshOutput.hpp
index 8109db90bd2..f31c853099b 100644
--- a/SU2_CFD/include/output/CMeshOutput.hpp
+++ b/SU2_CFD/include/output/CMeshOutput.hpp
@@ -2,7 +2,7 @@
  * \file CMeshOutput.hpp
  * \brief Headers of the mesh output.
  * \author R. Sanchez, T. Albring.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CMultizoneOutput.hpp b/SU2_CFD/include/output/CMultizoneOutput.hpp
index 0ea4e4b6fa9..d6ea055408e 100644
--- a/SU2_CFD/include/output/CMultizoneOutput.hpp
+++ b/SU2_CFD/include/output/CMultizoneOutput.hpp
@@ -2,7 +2,7 @@
  * \file CMultizoneOutput.hpp
  * \brief Headers of the main subroutines for screen and history output in multizone problems.
  * \author R. Sanchez, T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CNEMOCompOutput.hpp b/SU2_CFD/include/output/CNEMOCompOutput.hpp
index 15aa3402c8f..4e8eab774e0 100644
--- a/SU2_CFD/include/output/CNEMOCompOutput.hpp
+++ b/SU2_CFD/include/output/CNEMOCompOutput.hpp
@@ -2,7 +2,7 @@
  * \file CNEMOCompOutput.hpp
  * \brief  Headers of the compressible flow output.
  * \author R. Sanchez, W. Maier.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/COutput.hpp b/SU2_CFD/include/output/COutput.hpp
index 6caefdca1a4..0396ac6c80f 100644
--- a/SU2_CFD/include/output/COutput.hpp
+++ b/SU2_CFD/include/output/COutput.hpp
@@ -2,7 +2,7 @@
  * \file COutput.hpp
  * \brief Headers of the output class.
  * \author T.Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/COutputFactory.hpp b/SU2_CFD/include/output/COutputFactory.hpp
index 4f33703ab22..0caf981c7fa 100644
--- a/SU2_CFD/include/output/COutputFactory.hpp
+++ b/SU2_CFD/include/output/COutputFactory.hpp
@@ -2,7 +2,7 @@
  * \file COutputFactory.hpp
  * \brief Headers of the output class.
  * \author T.Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/COutputLegacy.hpp b/SU2_CFD/include/output/COutputLegacy.hpp
index 9c2305904fe..3a0d95d9675 100644
--- a/SU2_CFD/include/output/COutputLegacy.hpp
+++ b/SU2_CFD/include/output/COutputLegacy.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for generating the file outputs.
  *        The subroutines and functions are in the <i>output_structure_legacy.cpp</i> file.
  * \author F. Palacios, T. Economon, M. Colonno
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CCGNSFileWriter.hpp b/SU2_CFD/include/output/filewriter/CCGNSFileWriter.hpp
index 301c4000ba0..ef6d2024bdc 100644
--- a/SU2_CFD/include/output/filewriter/CCGNSFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CCGNSFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CCGNSFileWriter.hpp
  * \brief Headers for CGNS file writer class.
  * \author G. Baldan
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CCSVFileWriter.hpp b/SU2_CFD/include/output/filewriter/CCSVFileWriter.hpp
index cd3be009a5a..60082486fe0 100644
--- a/SU2_CFD/include/output/filewriter/CCSVFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CCSVFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CCSVFileWriter.hpp
  * \brief Headers fo the CSV file writer class.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CFEMDataSorter.hpp b/SU2_CFD/include/output/filewriter/CFEMDataSorter.hpp
index 6c1b798726c..269ce833613 100644
--- a/SU2_CFD/include/output/filewriter/CFEMDataSorter.hpp
+++ b/SU2_CFD/include/output/filewriter/CFEMDataSorter.hpp
@@ -2,7 +2,7 @@
  * \file CFEMDataSorter.hpp
  * \brief Headers fo the FEM data sorter class.
  * \author T. Albring, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CFVMDataSorter.hpp b/SU2_CFD/include/output/filewriter/CFVMDataSorter.hpp
index 38a378c9623..47ff42246f5 100644
--- a/SU2_CFD/include/output/filewriter/CFVMDataSorter.hpp
+++ b/SU2_CFD/include/output/filewriter/CFVMDataSorter.hpp
@@ -2,7 +2,7 @@
  * \file CFVMDataSorter.hpp
  * \brief Headers fo the FVM data sorter class.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CFileWriter.hpp b/SU2_CFD/include/output/filewriter/CFileWriter.hpp
index 6ba68d8a35d..846f1211551 100644
--- a/SU2_CFD/include/output/filewriter/CFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CFileWriter.hpp
  * \brief Headers fo the file writer class.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CParallelDataSorter.hpp b/SU2_CFD/include/output/filewriter/CParallelDataSorter.hpp
index fbf66db999e..3726332caab 100644
--- a/SU2_CFD/include/output/filewriter/CParallelDataSorter.hpp
+++ b/SU2_CFD/include/output/filewriter/CParallelDataSorter.hpp
@@ -2,7 +2,7 @@
  * \file CParallelDataSorter.hpp
  * \brief Headers fo the data sorter class.
  * \author T. Albring, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CParaviewBinaryFileWriter.hpp b/SU2_CFD/include/output/filewriter/CParaviewBinaryFileWriter.hpp
index 2998c070b70..cd9e1e9c22e 100644
--- a/SU2_CFD/include/output/filewriter/CParaviewBinaryFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CParaviewBinaryFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CParaviewBinaryFileWriter.hpp
  * \brief Headers fo paraview binary file writer class.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CParaviewFileWriter.hpp b/SU2_CFD/include/output/filewriter/CParaviewFileWriter.hpp
index 0390bd5b193..4b1a25fd952 100644
--- a/SU2_CFD/include/output/filewriter/CParaviewFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CParaviewFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CParaviewFileWriter.hpp
  * \brief Headers fo the paraview file writer class.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CParaviewVTMFileWriter.hpp b/SU2_CFD/include/output/filewriter/CParaviewVTMFileWriter.hpp
index 6adf7b9f0da..5890f172d8f 100644
--- a/SU2_CFD/include/output/filewriter/CParaviewVTMFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CParaviewVTMFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CParaviewVTMFileWriter.hpp
  * \brief Headers fo paraview binary file writer class.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CParaviewXMLFileWriter.hpp b/SU2_CFD/include/output/filewriter/CParaviewXMLFileWriter.hpp
index 940df034b7a..7920bc25eac 100644
--- a/SU2_CFD/include/output/filewriter/CParaviewXMLFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CParaviewXMLFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CParaviewXMLFileWriter.hpp
  * \brief Headers fo paraview binary file writer class.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CSTLFileWriter.hpp b/SU2_CFD/include/output/filewriter/CSTLFileWriter.hpp
index 9245d672df1..e44f5e6fa00 100644
--- a/SU2_CFD/include/output/filewriter/CSTLFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CSTLFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CSTLFileWriter.hpp
  * \brief Headers fo the STL file writer class.
  * \author T. Kattmann, T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -33,7 +33,7 @@
  * \class CSTLFileWriter
  * \brief Class for writing STL output files.
  * \author T. Kattmann, T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CSTLFileWriter final : public CFileWriter{
 private:
diff --git a/SU2_CFD/include/output/filewriter/CSU2BinaryFileWriter.hpp b/SU2_CFD/include/output/filewriter/CSU2BinaryFileWriter.hpp
index ca89d8ff2b7..a38e0b8b519 100644
--- a/SU2_CFD/include/output/filewriter/CSU2BinaryFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CSU2BinaryFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CSU2BinaryFileWriter.hpp
  * \brief Headers fo the SU2 binary file writer class.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CSU2FileWriter.hpp b/SU2_CFD/include/output/filewriter/CSU2FileWriter.hpp
index fd2317d5f15..d80766ed2df 100644
--- a/SU2_CFD/include/output/filewriter/CSU2FileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CSU2FileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CSU2FileWriter.hpp
  * \brief Headers fo the CSV file writer class.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CSU2MeshFileWriter.hpp b/SU2_CFD/include/output/filewriter/CSU2MeshFileWriter.hpp
index c95d6bc6f71..e6b75be19d0 100644
--- a/SU2_CFD/include/output/filewriter/CSU2MeshFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CSU2MeshFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CSU2MeshFileWriter.hpp
  * \brief Headers fo the CSV file writer class.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CSurfaceFEMDataSorter.hpp b/SU2_CFD/include/output/filewriter/CSurfaceFEMDataSorter.hpp
index 913474fa0f8..3678117b4bd 100644
--- a/SU2_CFD/include/output/filewriter/CSurfaceFEMDataSorter.hpp
+++ b/SU2_CFD/include/output/filewriter/CSurfaceFEMDataSorter.hpp
@@ -2,7 +2,7 @@
  * \file CSurfaceFEMDataSorter.hpp
  * \brief Headers fo the surface FEM data sorter class.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CSurfaceFVMDataSorter.hpp b/SU2_CFD/include/output/filewriter/CSurfaceFVMDataSorter.hpp
index 588b080a76c..793bb615b31 100644
--- a/SU2_CFD/include/output/filewriter/CSurfaceFVMDataSorter.hpp
+++ b/SU2_CFD/include/output/filewriter/CSurfaceFVMDataSorter.hpp
@@ -2,7 +2,7 @@
  * \file CSurfaceFVMDataSorter.hpp
  * \brief Headers for the surface FVM data sorter class.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CTecplotBinaryFileWriter.hpp b/SU2_CFD/include/output/filewriter/CTecplotBinaryFileWriter.hpp
index 930a367ebfe..424233b03d5 100644
--- a/SU2_CFD/include/output/filewriter/CTecplotBinaryFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CTecplotBinaryFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CTecplotBinaryFileWriter.hpp
  * \brief Headers fo the tecplot binary writer class.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CTecplotFileWriter.hpp b/SU2_CFD/include/output/filewriter/CTecplotFileWriter.hpp
index 1e20343e2df..b1041dcffa0 100644
--- a/SU2_CFD/include/output/filewriter/CTecplotFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CTecplotFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CTecplotFileWriter.hpp
  * \brief Headers fo the tecplot ASCII writer class.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/tools/CWindowingTools.hpp b/SU2_CFD/include/output/tools/CWindowingTools.hpp
index 1ccb4fa717c..7c3163fdc79 100644
--- a/SU2_CFD/include/output/tools/CWindowingTools.hpp
+++ b/SU2_CFD/include/output/tools/CWindowingTools.hpp
@@ -2,7 +2,7 @@
  * \file signal_processing_toolbox.hpp
  * \brief Header file for the signal processing toolbox.
  * \author S. Schotthöfer
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/sgs_model.hpp b/SU2_CFD/include/sgs_model.hpp
index eedb85de095..5249e794215 100644
--- a/SU2_CFD/include/sgs_model.hpp
+++ b/SU2_CFD/include/sgs_model.hpp
@@ -2,7 +2,7 @@
  * \file sgs_model.hpp
  * \brief Headers of the LES subgrid scale models of the SU2 solvers.
  * \author E. van der Weide, T. Economon, P. Urbanczyk
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -38,7 +38,7 @@ using namespace std;
  * \class CSGSModel
  * \brief Base class for defining the LES subgrid scale model.
  * \author: E. van der Weide, T. Economon, P. Urbanczyk
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CSGSModel {
 
@@ -224,7 +224,7 @@ class CSGSModel {
  * \class CSmagorinskyModel
  * \brief Derived class for defining the Smagorinsky SGS model.
  * \author: E. van der Weide, T. Economon, P. Urbanczyk
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CSmagorinskyModel : public CSGSModel {
 
@@ -413,7 +413,7 @@ class CSmagorinskyModel : public CSGSModel {
  * \class CWALEModel
  * \brief Derived class for defining the WALE SGS model.
  * \author: E. van der Weide, T. Economon, P. Urbanczyk
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CWALEModel : public CSGSModel {
 
@@ -601,7 +601,7 @@ class CWALEModel : public CSGSModel {
  * \class CVremanModel
  * \brief Derived class for defining the WALE SGS model.
  * \author: E. van der Weide, T. Economon, P. Urbanczyk, E. Molina
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CVremanModel : public CSGSModel {
 
diff --git a/SU2_CFD/include/sgs_model.inl b/SU2_CFD/include/sgs_model.inl
index 10602f1d501..3d5eec16a2a 100644
--- a/SU2_CFD/include/sgs_model.inl
+++ b/SU2_CFD/include/sgs_model.inl
@@ -2,7 +2,7 @@
  * \file sgs_model.inl
  * \brief In-Line subroutines of the <i>sgs_model.hpp</i> file.
  * \author E. van der Weide, T. Economon, P. Urbanczyk
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CAdjEulerSolver.hpp b/SU2_CFD/include/solvers/CAdjEulerSolver.hpp
index 999b2a68195..06c534d868b 100644
--- a/SU2_CFD/include/solvers/CAdjEulerSolver.hpp
+++ b/SU2_CFD/include/solvers/CAdjEulerSolver.hpp
@@ -2,7 +2,7 @@
  * \file CAdjEulerSolver.hpp
  * \brief Headers of the CAdjEulerSolver class
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CAdjNSSolver.hpp b/SU2_CFD/include/solvers/CAdjNSSolver.hpp
index 80403dbf4fa..469cc8e6061 100644
--- a/SU2_CFD/include/solvers/CAdjNSSolver.hpp
+++ b/SU2_CFD/include/solvers/CAdjNSSolver.hpp
@@ -2,7 +2,7 @@
  * \file CAdjNSSolver.hpp
  * \brief Headers of the CAdjNSSolver class
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CAdjTurbSolver.hpp b/SU2_CFD/include/solvers/CAdjTurbSolver.hpp
index 008126945a4..1d0868510d3 100644
--- a/SU2_CFD/include/solvers/CAdjTurbSolver.hpp
+++ b/SU2_CFD/include/solvers/CAdjTurbSolver.hpp
@@ -2,7 +2,7 @@
  * \file CAdjTurbSolver.hpp
  * \brief Headers of the CAdjTurbSolver class
  * \author F. Palacios, A. Bueno.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CBaselineSolver.hpp b/SU2_CFD/include/solvers/CBaselineSolver.hpp
index 9cd37c826fd..3cd7c9f1f88 100644
--- a/SU2_CFD/include/solvers/CBaselineSolver.hpp
+++ b/SU2_CFD/include/solvers/CBaselineSolver.hpp
@@ -2,7 +2,7 @@
  * \file CBaslineSolver.hpp
  * \brief Headers of the CBaselineSolver class
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CBaselineSolver_FEM.hpp b/SU2_CFD/include/solvers/CBaselineSolver_FEM.hpp
index 62b284e28e0..88bcc2911cc 100644
--- a/SU2_CFD/include/solvers/CBaselineSolver_FEM.hpp
+++ b/SU2_CFD/include/solvers/CBaselineSolver_FEM.hpp
@@ -2,7 +2,7 @@
  * \file CBaslineSolver_FEM.hpp
  * \brief Headers of the CBaselineSolver class
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -31,7 +31,7 @@
  * \class CBaselineSolver_FEM
  * \brief Main class for defining a baseline solution from a restart file for the DG-FEM solver output.
  * \author T. Economon.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CBaselineSolver_FEM final : public CSolver {
 protected:
diff --git a/SU2_CFD/include/solvers/CDiscAdjFEASolver.hpp b/SU2_CFD/include/solvers/CDiscAdjFEASolver.hpp
index 7906a54bb2d..71d3286cdf9 100644
--- a/SU2_CFD/include/solvers/CDiscAdjFEASolver.hpp
+++ b/SU2_CFD/include/solvers/CDiscAdjFEASolver.hpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjFEASolver.hpp
  * \brief Headers of the CDiscAdjFEASolver class
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CDiscAdjMeshSolver.hpp b/SU2_CFD/include/solvers/CDiscAdjMeshSolver.hpp
index ba77ac9d80b..41471dfb40e 100644
--- a/SU2_CFD/include/solvers/CDiscAdjMeshSolver.hpp
+++ b/SU2_CFD/include/solvers/CDiscAdjMeshSolver.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to compute the
  *        the discrete adjoint of the linear-elastic mesh solver.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CDiscAdjSolver.hpp b/SU2_CFD/include/solvers/CDiscAdjSolver.hpp
index dea2ee227ef..8e87c9dcd56 100644
--- a/SU2_CFD/include/solvers/CDiscAdjSolver.hpp
+++ b/SU2_CFD/include/solvers/CDiscAdjSolver.hpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjSolver.hpp
  * \brief Headers of the CDiscAdjSolver class
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CEulerSolver.hpp b/SU2_CFD/include/solvers/CEulerSolver.hpp
index ef8c6b6af05..739d0be041b 100644
--- a/SU2_CFD/include/solvers/CEulerSolver.hpp
+++ b/SU2_CFD/include/solvers/CEulerSolver.hpp
@@ -2,7 +2,7 @@
  * \file CEulerSolver.hpp
  * \brief Headers of the CEulerSolver class
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CFEASolver.hpp b/SU2_CFD/include/solvers/CFEASolver.hpp
index ae06c383e3d..88849b8c926 100644
--- a/SU2_CFD/include/solvers/CFEASolver.hpp
+++ b/SU2_CFD/include/solvers/CFEASolver.hpp
@@ -2,7 +2,7 @@
  * \file CFEASolver.hpp
  * \brief Finite element solver for elasticity problems.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CFEASolverBase.hpp b/SU2_CFD/include/solvers/CFEASolverBase.hpp
index ba40652e750..e686b51fa2d 100644
--- a/SU2_CFD/include/solvers/CFEASolverBase.hpp
+++ b/SU2_CFD/include/solvers/CFEASolverBase.hpp
@@ -2,7 +2,7 @@
  * \file CFEASolver.hpp
  * \brief Base class template for all FEA solvers using the SU2 internal finite elements.
  * \author T. Dick
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CFEM_DG_EulerSolver.hpp b/SU2_CFD/include/solvers/CFEM_DG_EulerSolver.hpp
index 8941fd044b4..03b12c32c4c 100644
--- a/SU2_CFD/include/solvers/CFEM_DG_EulerSolver.hpp
+++ b/SU2_CFD/include/solvers/CFEM_DG_EulerSolver.hpp
@@ -2,7 +2,7 @@
  * \file CFEM_DG_EulerSolver.hpp
  * \brief Headers of the CFEM_DG_EulerSolver class
  * \author E. van der Weide, T. Economon, J. Alonso
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -35,7 +35,7 @@
  * \brief Main class for defining the Euler Discontinuous Galerkin finite element flow solver.
  * \ingroup Euler_Equations
  * \author E. van der Weide, T. Economon, J. Alonso
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CFEM_DG_EulerSolver : public CSolver {
 protected:
diff --git a/SU2_CFD/include/solvers/CFEM_DG_NSSolver.hpp b/SU2_CFD/include/solvers/CFEM_DG_NSSolver.hpp
index f22532fcac2..70519714a35 100644
--- a/SU2_CFD/include/solvers/CFEM_DG_NSSolver.hpp
+++ b/SU2_CFD/include/solvers/CFEM_DG_NSSolver.hpp
@@ -2,7 +2,7 @@
  * \file CFEM_DG_NSSolver.hpp
  * \brief Headers of the CFEM_DG_NSSolver class
  * \author E. van der Weide, T. Economon, J. Alonso
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -35,7 +35,7 @@
  * \brief Main class for defining the Navier-Stokes Discontinuous Galerkin finite element flow solver.
  * \ingroup Navier_Stokes_Equations
  * \author E. van der Weide, T. Economon, J. Alonso
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CFEM_DG_NSSolver final : public CFEM_DG_EulerSolver {
 private:
diff --git a/SU2_CFD/include/solvers/CFVMFlowSolverBase.hpp b/SU2_CFD/include/solvers/CFVMFlowSolverBase.hpp
index 0b52f52d90b..4b9df8712a6 100644
--- a/SU2_CFD/include/solvers/CFVMFlowSolverBase.hpp
+++ b/SU2_CFD/include/solvers/CFVMFlowSolverBase.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file CFVMFlowSolverBase.hpp
  * \brief Base class template for all FVM flow solvers.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CFVMFlowSolverBase.inl b/SU2_CFD/include/solvers/CFVMFlowSolverBase.inl
index a62962e8104..e594598bfd9 100644
--- a/SU2_CFD/include/solvers/CFVMFlowSolverBase.inl
+++ b/SU2_CFD/include/solvers/CFVMFlowSolverBase.inl
@@ -1,7 +1,7 @@
 /*!
  * \file CFVMFlowSolverBase.inl
  * \brief Base class template for all FVM flow solvers.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CGradientSmoothingSolver.hpp b/SU2_CFD/include/solvers/CGradientSmoothingSolver.hpp
index a3733c3d1f8..29361eb6563 100644
--- a/SU2_CFD/include/solvers/CGradientSmoothingSolver.hpp
+++ b/SU2_CFD/include/solvers/CGradientSmoothingSolver.hpp
@@ -2,7 +2,7 @@
  * \file CGradientSmoothingSolver.hpp
  * \brief SOlver class for Sobolev smoothing of sensitivities.
  * \author T. Dick
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CHeatSolver.hpp b/SU2_CFD/include/solvers/CHeatSolver.hpp
index 92d2421850f..5668af4243f 100644
--- a/SU2_CFD/include/solvers/CHeatSolver.hpp
+++ b/SU2_CFD/include/solvers/CHeatSolver.hpp
@@ -2,7 +2,7 @@
  * \file CHeatSolver.hpp
  * \brief Headers of the CHeatSolver class
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -27,16 +27,16 @@
 
 #pragma once
 
-#include "CSolver.hpp"
+#include "CScalarSolver.hpp"
 #include "../variables/CHeatVariable.hpp"
 
 /*!
  * \class CHeatSolver
  * \brief Main class for defining the finite-volume heat solver.
  * \author O. Burghardt
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
-class CHeatSolver final : public CSolver {
+class CHeatSolver final : public CScalarSolver<CHeatVariable> {
 protected:
   static constexpr size_t MAXNDIM = 3; /*!< \brief Max number of space dimensions, used in some static arrays. */
   static constexpr size_t MAXNVAR = 1; /*!< \brief Max number of variables, for static arrays. */
@@ -44,7 +44,9 @@ class CHeatSolver final : public CSolver {
   const bool flow; /*!< \brief Use solver as a scalar transport equation of Temperature for the inc solver. */
   const bool heat_equation; /*!< \brief use solver for heat conduction in solids. */
 
-  unsigned short nVarFlow, nMarker;
+  su2double Global_Delta_Time = 0.0, Global_Delta_UnstTimeND = 0.0;
+
+  unsigned short nVarFlow;
   vector<vector<su2double> > HeatFlux;
   vector<su2double> HeatFlux_per_Marker;
   su2double Total_HeatFlux;
@@ -52,19 +54,48 @@ class CHeatSolver final : public CSolver {
   vector<su2double> AverageT_per_Marker;
   su2double Total_AverageT;
   su2double AllBound_AverageT;
-  vector<su2double>  Primitive_Flow_i;
+  vector<su2double> Primitive_Flow_i;
   vector<su2double> Primitive_Flow_j;
   vector<su2double> Surface_Areas;
   su2double Total_HeatFlux_Areas;
   su2double Total_HeatFlux_Areas_Monitor;
   vector<su2activematrix> ConjugateVar;
 
-  CHeatVariable* nodes = nullptr;  /*!< \brief The highest level in the variable hierarchy this solver can safely use. */
-
   /*!
-   * \brief Return nodes to allow CSolver::base_nodes to be set.
+   * \brief Applies an isothermal condition to a vertex of a marker.
    */
-  inline CVariable* GetBaseClassPointerToNodes() override { return nodes; }
+  void IsothermalBoundaryCondition(CGeometry *geometry, CSolver *flow_solver, const CConfig *config,
+                                   unsigned short iMarker, unsigned long iVertex, const su2double& temperature) {
+
+    const auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+    if (!geometry->nodes->GetDomain(iPoint)) return;
+
+    const bool implicit = config->GetKind_TimeIntScheme() == EULER_IMPLICIT;
+    const su2double prandtl_lam = config->GetPrandtl_Lam();
+    const su2double const_diffusivity = config->GetThermalDiffusivity();
+
+    const auto Point_Normal = geometry->vertex[iMarker][iVertex]->GetNormal_Neighbor();
+
+    const auto* Normal = geometry->vertex[iMarker][iVertex]->GetNormal();
+    const su2double Area = GeometryToolbox::Norm(nDim, Normal);
+
+    const auto* Coord_i = geometry->nodes->GetCoord(iPoint);
+    const auto* Coord_j = geometry->nodes->GetCoord(Point_Normal);
+    const su2double dist_ij = GeometryToolbox::Distance(nDim, Coord_i, Coord_j);
+
+    const su2double dTdn = -(nodes->GetTemperature(Point_Normal) - temperature) / dist_ij;
+
+    su2double thermal_diffusivity = const_diffusivity;
+    if (flow) {
+      thermal_diffusivity = flow_solver->GetNodes()->GetLaminarViscosity(iPoint) / prandtl_lam;
+    }
+    LinSysRes(iPoint, 0) -= thermal_diffusivity * dTdn * Area;
+
+    if (implicit) {
+      su2double Jacobian_i[] = {-thermal_diffusivity / dist_ij * Area};
+      Jacobian.SubtractBlock2Diag(iPoint, &Jacobian_i);
+    }
+  }
 
 public:
 
@@ -73,11 +104,6 @@ class CHeatSolver final : public CSolver {
    */
   CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iMesh);
 
-  /*!
-   * \brief Destructor of the class.
-   */
-  ~CHeatSolver(void) override;
-
   /*!
    * \brief Restart residual and compute gradients.
    * \param[in] geometry - Geometrical definition of the problem.
@@ -247,15 +273,6 @@ class CHeatSolver final : public CSolver {
                                   CConfig *config,
                                   unsigned short val_marker) override;
 
-  /*!
-   * \brief Impose a periodic boundary condition by summing contributions from the complete control volume.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] numerics - Description of the numerical method.
-   * \param[in] config - Definition of the particular problem.
-   */
-  void BC_Periodic(CGeometry* geometry, CSolver** solver_container, CNumerics* numerics, CConfig* config) final;
-
   /*!
    * \brief Set the conjugate heat variables.
    * \param[in] val_marker        - marker index
@@ -330,26 +347,6 @@ class CHeatSolver final : public CSolver {
     }
   }
 
-  /*!
-   * \brief Update the solution using an implicit solver.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] config - Definition of the particular problem.
-   */
-  void ImplicitEuler_Iteration(CGeometry *geometry,
-                               CSolver **solver_container,
-                               CConfig *config) override;
-
-  /*!
-   * \brief Update the solution using an explicit solver.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] config - Definition of the particular problem.
-   */
-  void ExplicitEuler_Iteration(CGeometry *geometry,
-                               CSolver **solver_container,
-                               CConfig *config) override;
-
   /*!
    * \brief A virtual member.
    * \param[in] geometry - Geometrical definition of the problem.
@@ -400,4 +397,8 @@ class CHeatSolver final : public CSolver {
    */
   inline su2double GetHeatFlux(unsigned short val_marker, unsigned long val_vertex) const override { return HeatFlux[val_marker][val_vertex]; }
 
+  /*!
+   * \brief Does not support OpenMP+MPI yet.
+   */
+  inline bool GetHasHybridParallel() const override { return false; }
 };
diff --git a/SU2_CFD/include/solvers/CIncEulerSolver.hpp b/SU2_CFD/include/solvers/CIncEulerSolver.hpp
index e6916932e62..b9c1c6d5f00 100644
--- a/SU2_CFD/include/solvers/CIncEulerSolver.hpp
+++ b/SU2_CFD/include/solvers/CIncEulerSolver.hpp
@@ -2,7 +2,7 @@
  * \file CIncEulerSolver.hpp
  * \brief Headers of the CIncEulerSolver class
  * \author F. Palacios, T. Economon, T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CIncNSSolver.hpp b/SU2_CFD/include/solvers/CIncNSSolver.hpp
index 69d68672750..8d8dcf19d31 100644
--- a/SU2_CFD/include/solvers/CIncNSSolver.hpp
+++ b/SU2_CFD/include/solvers/CIncNSSolver.hpp
@@ -2,7 +2,7 @@
  * \file CIncNSSolver.hpp
  * \brief Headers of the CIncNSSolver class
  * \author F. Palacios, T. Economon, T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CMeshSolver.hpp b/SU2_CFD/include/solvers/CMeshSolver.hpp
index e50611b4c4b..145bf54769b 100644
--- a/SU2_CFD/include/solvers/CMeshSolver.hpp
+++ b/SU2_CFD/include/solvers/CMeshSolver.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to compute the deformation of
  *        the volumetric numerical grid using the linear elasticity solver.
  * \author Ruben Sanchez, based on CVolumetricMovement developments (F. Palacios, A. Bueno, T. Economon, S. Padron)
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CNEMOEulerSolver.hpp b/SU2_CFD/include/solvers/CNEMOEulerSolver.hpp
index ffdee77143d..84d17dfeb88 100644
--- a/SU2_CFD/include/solvers/CNEMOEulerSolver.hpp
+++ b/SU2_CFD/include/solvers/CNEMOEulerSolver.hpp
@@ -2,7 +2,7 @@
  * \file CNEMOEulerSolver.hpp
  * \brief Headers of the CNEMOEulerSolver class
  * \author S. R. Copeland, F. Palacios, W. Maier.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -36,7 +36,7 @@
  * \brief Main class for defining the NEMO Euler's flow solver.
  * \ingroup Euler_Equations
  * \author S. R. Copeland, F. Palacios, W. Maier.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CNEMOEulerSolver : public CFVMFlowSolverBase<CNEMOEulerVariable, ENUM_REGIME::COMPRESSIBLE> {
 protected:
diff --git a/SU2_CFD/include/solvers/CNEMONSSolver.hpp b/SU2_CFD/include/solvers/CNEMONSSolver.hpp
index 4c948d3656a..b3ba042f9dc 100644
--- a/SU2_CFD/include/solvers/CNEMONSSolver.hpp
+++ b/SU2_CFD/include/solvers/CNEMONSSolver.hpp
@@ -2,7 +2,7 @@
  * \file CNEMONSSolver.hpp
  * \brief Headers of the CNEMONSSolver class
  * \author S. R. Copeland, F. Palacios, W. Maier.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CNSSolver.hpp b/SU2_CFD/include/solvers/CNSSolver.hpp
index ca88c6cb59e..2a495de4f76 100644
--- a/SU2_CFD/include/solvers/CNSSolver.hpp
+++ b/SU2_CFD/include/solvers/CNSSolver.hpp
@@ -2,7 +2,7 @@
  * \file CNSSolver.hpp
  * \brief Headers of the CNSSolver class
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CRadP1Solver.hpp b/SU2_CFD/include/solvers/CRadP1Solver.hpp
index 3ff893dbcb1..338bd2e0893 100644
--- a/SU2_CFD/include/solvers/CRadP1Solver.hpp
+++ b/SU2_CFD/include/solvers/CRadP1Solver.hpp
@@ -2,7 +2,7 @@
  * \file CRadP1Solver.hpp
  * \brief Declaration and inlines of the class to compute a P1 radiation problem.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -241,7 +241,7 @@ class CRadP1Solver final: public CRadSolver {
    * \param[in] Iteration - Index of the current iteration.
    */
   void SetTime_Step(CGeometry *geometry, CSolver **solver_container, CConfig *config,
-                    unsigned short iMesh, unsigned long Iteration) override ;
+                    unsigned short iMesh, unsigned long Iteration) override;
 
   /*!
    * \brief Set the freestream temperature.
diff --git a/SU2_CFD/include/solvers/CRadSolver.hpp b/SU2_CFD/include/solvers/CRadSolver.hpp
index 05e0855b850..b4cb928326d 100644
--- a/SU2_CFD/include/solvers/CRadSolver.hpp
+++ b/SU2_CFD/include/solvers/CRadSolver.hpp
@@ -2,7 +2,7 @@
  * \file CRadSolver.hpp
  * \brief Declaration and inlines of the class to compute a generic radiation solver.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CScalarSolver.hpp b/SU2_CFD/include/solvers/CScalarSolver.hpp
index 5301fef5ad3..e7ec30d5900 100644
--- a/SU2_CFD/include/solvers/CScalarSolver.hpp
+++ b/SU2_CFD/include/solvers/CScalarSolver.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file CScalarSolver.hpp
  * \brief Headers of the CScalarSolver class
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -103,7 +103,8 @@ class CScalarSolver : public CSolver {
                                          CGeometry* geometry, CSolver** solver_container, CNumerics* numerics,
                                          CConfig* config) {
     const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
-    auto* flowNodes = su2staticcast_p<CFlowVariable*>(solver_container[FLOW_SOL]->GetNodes());
+    CFlowVariable* flowNodes = solver_container[FLOW_SOL] ?
+        su2staticcast_p<CFlowVariable*>(solver_container[FLOW_SOL]->GetNodes()) : nullptr;
 
     /*--- Points in edge ---*/
 
@@ -117,7 +118,9 @@ class CScalarSolver : public CSolver {
 
     /*--- Conservative variables w/o reconstruction ---*/
 
-    numerics->SetPrimitive(flowNodes->GetPrimitive(iPoint), flowNodes->GetPrimitive(jPoint));
+    if (flowNodes) {
+      numerics->SetPrimitive(flowNodes->GetPrimitive(iPoint), flowNodes->GetPrimitive(jPoint));
+    }
 
     /*--- Turbulent variables w/o reconstruction, and its gradients ---*/
 
@@ -156,6 +159,8 @@ class CScalarSolver : public CSolver {
   void BC_Fluid_Interface_impl(const SolverSpecificNumericsFunc& SolverSpecificNumerics, CGeometry *geometry,
                                CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics,
                                CConfig *config) {
+    if (solver_container[FLOW_SOL] == nullptr) return;
+
     const auto nPrimVar = solver_container[FLOW_SOL]->GetnPrimVar();
     su2activevector PrimVar_j(nPrimVar);
     su2double solution_j[MAXNVAR] = {0.0};
@@ -436,6 +441,17 @@ class CScalarSolver : public CSolver {
     END_SU2_OMP_FOR
   }
 
+  /*!
+   * \brief This base implementation simply copies the time step of the flow solver.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] iMesh - Index of the mesh in multigrid computations.
+   * \param[in] Iteration - Index of the current iteration.
+   */
+  void SetTime_Step(CGeometry *geometry, CSolver **solver_container, CConfig *config,
+                    unsigned short iMesh, unsigned long Iteration) override;
+
   /*!
    * \brief Prepare an implicit iteration.
    * \param[in] geometry - Geometrical definition of the problem.
@@ -466,7 +482,7 @@ class CScalarSolver : public CSolver {
    * \param[in] solver_container - Container vector with all the solutions.
    * \param[in] config - Definition of the particular problem.
    */
-  void ImplicitEuler_Iteration(CGeometry* geometry, CSolver** solver_container, CConfig* config) override;
+  void ImplicitEuler_Iteration(CGeometry* geometry, CSolver** solver_container, CConfig* config) final;
 
   /*!
    * \brief Set the total residual adding the term that comes from the Dual Time-Stepping Strategy.
@@ -478,7 +494,7 @@ class CScalarSolver : public CSolver {
    * \param[in] RunTime_EqSystem - System of equations which is going to be solved.
    */
   void SetResidual_DualTime(CGeometry* geometry, CSolver** solver_container, CConfig* config, unsigned short iRKStep,
-                            unsigned short iMesh, unsigned short RunTime_EqSystem) final;
+                            unsigned short iMesh, unsigned short RunTime_EqSystem) override;
 
   /*!
    * \brief Load a solution from a restart file.
diff --git a/SU2_CFD/include/solvers/CScalarSolver.inl b/SU2_CFD/include/solvers/CScalarSolver.inl
index 099e2268069..a6f795a2bbe 100644
--- a/SU2_CFD/include/solvers/CScalarSolver.inl
+++ b/SU2_CFD/include/solvers/CScalarSolver.inl
@@ -1,7 +1,7 @@
 /*!
  * \file CScalarSolver.inl
  * \brief Main subroutines of CScalarSolver class
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -424,10 +424,21 @@ void CScalarSolver<VariableType>::BC_Far_Field(CGeometry* geometry, CSolver** so
 }
 
 template <class VariableType>
-void CScalarSolver<VariableType>::PrepareImplicitIteration(CGeometry* geometry, CSolver** solver_container,
-                                                           CConfig* config) {
+void CScalarSolver<VariableType>::SetTime_Step(CGeometry *geometry, CSolver **solver_container, CConfig *config,
+                                               unsigned short iMesh, unsigned long Iteration) {
   const auto flowNodes = solver_container[FLOW_SOL]->GetNodes();
 
+  SU2_OMP_FOR_STAT(omp_chunk_size)
+  for (unsigned long iPoint = 0; iPoint < nPointDomain; iPoint++) {
+    su2double dt = nodes->GetLocalCFL(iPoint) / flowNodes->GetLocalCFL(iPoint) * flowNodes->GetDelta_Time(iPoint);
+    nodes->SetDelta_Time(iPoint, dt);
+  }
+  END_SU2_OMP_FOR
+}
+
+template <class VariableType>
+void CScalarSolver<VariableType>::PrepareImplicitIteration(CGeometry* geometry, CSolver** solver_container,
+                                                           CConfig* config) {
   /*--- Set shared residual variables to 0 and declare
    *    local ones for current thread to work on. ---*/
 
@@ -440,11 +451,8 @@ void CScalarSolver<VariableType>::PrepareImplicitIteration(CGeometry* geometry,
 
   SU2_OMP_FOR_(schedule(static, omp_chunk_size) SU2_NOWAIT)
   for (unsigned long iPoint = 0; iPoint < nPointDomain; iPoint++) {
-    /// TODO: This could be the SetTime_Step of this solver.
-    su2double dt = nodes->GetLocalCFL(iPoint) / flowNodes->GetLocalCFL(iPoint) * flowNodes->GetDelta_Time(iPoint);
-    nodes->SetDelta_Time(iPoint, dt);
-
     /*--- Modify matrix diagonal to improve diagonal dominance. ---*/
+    const su2double dt = nodes->GetDelta_Time(iPoint);
 
     if (dt != 0.0) {
       su2double Vol = geometry->nodes->GetVolume(iPoint) + geometry->nodes->GetPeriodicVolume(iPoint);
@@ -476,8 +484,6 @@ void CScalarSolver<VariableType>::CompleteImplicitIteration(CGeometry* geometry,
                                                             CConfig* config) {
   const bool compressible = (config->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
 
-  const auto flowNodes = solver_container[FLOW_SOL]->GetNodes();
-
   ComputeUnderRelaxationFactor(config);
 
   /*--- Update solution (system written in terms of increments) ---*/
@@ -486,6 +492,8 @@ void CScalarSolver<VariableType>::CompleteImplicitIteration(CGeometry* geometry,
     /*--- Update the scalar solution. For transport equations, where Solution is not equivalent with the transported
      * quantity, multiply the respective factor.  ---*/
     if (Conservative) {
+      const auto flowNodes = solver_container[FLOW_SOL]->GetNodes();
+
       SU2_OMP_FOR_STAT(omp_chunk_size)
       for (unsigned long iPoint = 0; iPoint < nPointDomain; iPoint++) {
         /*--- Multiply the Solution var with density to get the conservative transported quantity, if necessary. ---*/
@@ -547,16 +555,13 @@ void CScalarSolver<VariableType>::ImplicitEuler_Iteration(CGeometry* geometry, C
 template <class VariableType>
 void CScalarSolver<VariableType>::ExplicitEuler_Iteration(CGeometry* geometry, CSolver** solver_container,
                                                           CConfig* config) {
-  const auto flowNodes = solver_container[FLOW_SOL]->GetNodes();
-
   /*--- Local residual variables for current thread ---*/
   su2double resMax[MAXNVAR] = {0.0}, resRMS[MAXNVAR] = {0.0};
   unsigned long idxMax[MAXNVAR] = {0};
 
   SU2_OMP_FOR_STAT(omp_chunk_size)
   for (unsigned long iPoint = 0; iPoint < nPointDomain; iPoint++) {
-    const su2double dt = nodes->GetLocalCFL(iPoint) / flowNodes->GetLocalCFL(iPoint) * flowNodes->GetDelta_Time(iPoint);
-    nodes->SetDelta_Time(iPoint, dt);
+    const su2double dt = nodes->GetDelta_Time(iPoint);
     const su2double Vol = geometry->nodes->GetVolume(iPoint) + geometry->nodes->GetPeriodicVolume(iPoint);
 
     for (auto iVar = 0u; iVar < nVar; iVar++) {
diff --git a/SU2_CFD/include/solvers/CSolver.hpp b/SU2_CFD/include/solvers/CSolver.hpp
index 851406bcc7f..26ce5eeabf2 100644
--- a/SU2_CFD/include/solvers/CSolver.hpp
+++ b/SU2_CFD/include/solvers/CSolver.hpp
@@ -2,7 +2,7 @@
  * \file CSolver.hpp
  * \brief Headers of the CSolver class which is inherited by all of the other solvers
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CSolverFactory.hpp b/SU2_CFD/include/solvers/CSolverFactory.hpp
index 8ed6371ed4a..3a9dfb1e91d 100644
--- a/SU2_CFD/include/solvers/CSolverFactory.hpp
+++ b/SU2_CFD/include/solvers/CSolverFactory.hpp
@@ -2,7 +2,7 @@
  * \file CSolverFactory.hpp
  * \brief Headers of the CSolverFactory class
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CSpeciesSolver.hpp b/SU2_CFD/include/solvers/CSpeciesSolver.hpp
index 38a846943fd..6f209b0fda6 100644
--- a/SU2_CFD/include/solvers/CSpeciesSolver.hpp
+++ b/SU2_CFD/include/solvers/CSpeciesSolver.hpp
@@ -2,7 +2,7 @@
  * \file CSpeciesSolver.hpp
  * \brief Headers of the CSpeciesSolver class
  * \author T. Kattmann.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CTemplateSolver.hpp b/SU2_CFD/include/solvers/CTemplateSolver.hpp
index 63b4aa1a0bb..03b7bcd5d81 100644
--- a/SU2_CFD/include/solvers/CTemplateSolver.hpp
+++ b/SU2_CFD/include/solvers/CTemplateSolver.hpp
@@ -2,7 +2,7 @@
  * \file CTemplateSolver.hpp
  * \brief Headers of the CTemplateSolver class
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CTransLMSolver.hpp b/SU2_CFD/include/solvers/CTransLMSolver.hpp
index 1ced793c9ac..acdf90fb9a4 100644
--- a/SU2_CFD/include/solvers/CTransLMSolver.hpp
+++ b/SU2_CFD/include/solvers/CTransLMSolver.hpp
@@ -2,7 +2,7 @@
  * \file CTransLMSolver.hpp
  * \brief Headers of the CTransLMSolver class
  * \author A. Aranake
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -28,6 +28,7 @@
 #pragma once
 
 #include "CTurbSolver.hpp"
+#include "../numerics/turbulent/transition/trans_correlations.hpp"
 
 /*!
  * \class CTransLMSolver
@@ -39,6 +40,11 @@
 class CTransLMSolver final : public CTurbSolver {
 private:
 
+  LM_ParsedOptions options;
+  TURB_FAMILY TurbFamily;
+
+  TransLMCorrelations TransCorrelations;
+
 public:
   /*!
    * \overload
diff --git a/SU2_CFD/include/solvers/CTurbSASolver.hpp b/SU2_CFD/include/solvers/CTurbSASolver.hpp
index 8a09ad00cff..90db2a70041 100644
--- a/SU2_CFD/include/solvers/CTurbSASolver.hpp
+++ b/SU2_CFD/include/solvers/CTurbSASolver.hpp
@@ -2,7 +2,7 @@
  * \file CTurbSASolver.hpp
  * \brief Headers of the CTurbSASolver class
  * \author A. Bueno.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CTurbSSTSolver.hpp b/SU2_CFD/include/solvers/CTurbSSTSolver.hpp
index c4b4625744d..93962d328f1 100644
--- a/SU2_CFD/include/solvers/CTurbSSTSolver.hpp
+++ b/SU2_CFD/include/solvers/CTurbSSTSolver.hpp
@@ -2,7 +2,7 @@
  * \file CTurbSSTSolver.hpp
  * \brief Headers of the CTurbSSTSolver class
  * \author A. Campos, F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CTurbSolver.hpp b/SU2_CFD/include/solvers/CTurbSolver.hpp
index f1eb1df8b8d..78d48b2d8cf 100644
--- a/SU2_CFD/include/solvers/CTurbSolver.hpp
+++ b/SU2_CFD/include/solvers/CTurbSolver.hpp
@@ -2,7 +2,7 @@
  * \file CTurbSolver.hpp
  * \brief Headers of the CTurbSolver class
  * \author A. Bueno.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/task_definition.hpp b/SU2_CFD/include/task_definition.hpp
index 89573d81cb1..1b11d020297 100644
--- a/SU2_CFD/include/task_definition.hpp
+++ b/SU2_CFD/include/task_definition.hpp
@@ -2,7 +2,7 @@
  * \file task_definition.hpp
  * \brief Header of the task definition class for the SU2 solvers.
  * \author E. van der Weide, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -37,7 +37,7 @@ using namespace std;
  * \class CTaskDefinition
  * \brief Class for defining a task to be carried out
  * \author: E. van der Weide, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CTaskDefinition {
 
diff --git a/SU2_CFD/include/task_definition.inl b/SU2_CFD/include/task_definition.inl
index f47d5632e26..e75462050df 100644
--- a/SU2_CFD/include/task_definition.inl
+++ b/SU2_CFD/include/task_definition.inl
@@ -2,7 +2,7 @@
  * \file task_definition.inl
  * \brief In-Line subroutines of the <i>task_definition.hpp</i> file.
  * \author E. van der Weide, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CAdjEulerVariable.hpp b/SU2_CFD/include/variables/CAdjEulerVariable.hpp
index ee09668d67d..a7451999638 100644
--- a/SU2_CFD/include/variables/CAdjEulerVariable.hpp
+++ b/SU2_CFD/include/variables/CAdjEulerVariable.hpp
@@ -2,7 +2,7 @@
  * \file CAdjEulerVariable.hpp
  * \brief Main class for defining the variables of the adjoint Euler solver.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CAdjNSVariable.hpp b/SU2_CFD/include/variables/CAdjNSVariable.hpp
index 9fab9f4c024..1b05e19f46d 100644
--- a/SU2_CFD/include/variables/CAdjNSVariable.hpp
+++ b/SU2_CFD/include/variables/CAdjNSVariable.hpp
@@ -2,7 +2,7 @@
  * \file CAdjNSVariable.hpp
  * \brief Main class for defining the variables of the adjoint Navier-Stokes solver.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CAdjTurbVariable.hpp b/SU2_CFD/include/variables/CAdjTurbVariable.hpp
index d9ada41be9f..ba8bee98d87 100644
--- a/SU2_CFD/include/variables/CAdjTurbVariable.hpp
+++ b/SU2_CFD/include/variables/CAdjTurbVariable.hpp
@@ -2,7 +2,7 @@
  * \file CAdjTurbVariable.hpp
  * \brief Main class for defining the variables of the adjoint turbulence model.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CBaselineVariable.hpp b/SU2_CFD/include/variables/CBaselineVariable.hpp
index 5bd585f02af..d916a17dc3a 100644
--- a/SU2_CFD/include/variables/CBaselineVariable.hpp
+++ b/SU2_CFD/include/variables/CBaselineVariable.hpp
@@ -2,7 +2,7 @@
  * \file CBaselineVariable.hpp
  * \brief Main class for defining the variables of a baseline solution from a restart file (for output).
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CDiscAdjFEABoundVariable.hpp b/SU2_CFD/include/variables/CDiscAdjFEABoundVariable.hpp
index fd9516b51e7..08052962ed2 100644
--- a/SU2_CFD/include/variables/CDiscAdjFEABoundVariable.hpp
+++ b/SU2_CFD/include/variables/CDiscAdjFEABoundVariable.hpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjFEABoundVariable.hpp
  * \brief Main class for defining the variables of the adjoint FEA solver at the boundary.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -35,7 +35,7 @@
  * \ingroup DiscAdj
  * \brief Main class for defining the variables on the FEA boundaries for adjoint applications.
  * \author R. Sanchez.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CDiscAdjFEABoundVariable final : public CDiscAdjVariable {
 private:
diff --git a/SU2_CFD/include/variables/CDiscAdjMeshBoundVariable.hpp b/SU2_CFD/include/variables/CDiscAdjMeshBoundVariable.hpp
index 40ea701e37e..48b3e6d022a 100644
--- a/SU2_CFD/include/variables/CDiscAdjMeshBoundVariable.hpp
+++ b/SU2_CFD/include/variables/CDiscAdjMeshBoundVariable.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class
  *        to define the adjoint variables of the mesh movement.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CDiscAdjVariable.hpp b/SU2_CFD/include/variables/CDiscAdjVariable.hpp
index 8111fcc83b3..308fe86dc99 100644
--- a/SU2_CFD/include/variables/CDiscAdjVariable.hpp
+++ b/SU2_CFD/include/variables/CDiscAdjVariable.hpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjVariable.hpp
  * \brief Main class for defining the variables of the adjoint solver.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CEulerVariable.hpp b/SU2_CFD/include/variables/CEulerVariable.hpp
index a072c1a0544..2cf9a8b6076 100644
--- a/SU2_CFD/include/variables/CEulerVariable.hpp
+++ b/SU2_CFD/include/variables/CEulerVariable.hpp
@@ -2,7 +2,7 @@
  * \file CEulerVariable.hpp
  * \brief Class for defining the variables of the compressible Euler solver.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CFEABoundVariable.hpp b/SU2_CFD/include/variables/CFEABoundVariable.hpp
index 508b881324b..f7034f6db8d 100644
--- a/SU2_CFD/include/variables/CFEABoundVariable.hpp
+++ b/SU2_CFD/include/variables/CFEABoundVariable.hpp
@@ -2,7 +2,7 @@
  * \file CFEABoundVariable.hpp
  * \brief Class for defining the variables on the FEA boundaries for FSI applications.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -37,7 +37,7 @@
  * A map is constructed so that variables can be referenced by iPoint instead of iVertex.
  * \ingroup Structural Finite Element Analysis Variables
  * \author R. Sanchez.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CFEABoundVariable final : public CFEAVariable {
 protected:
diff --git a/SU2_CFD/include/variables/CFEAVariable.hpp b/SU2_CFD/include/variables/CFEAVariable.hpp
index dbfe0d009a2..277d3c98edb 100644
--- a/SU2_CFD/include/variables/CFEAVariable.hpp
+++ b/SU2_CFD/include/variables/CFEAVariable.hpp
@@ -2,7 +2,7 @@
  * \file CFEAVariable.hpp
  * \brief Class for defining the variables of the FEM structural problem.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -34,7 +34,7 @@
  * \brief Class for defining the variables of the FEM structural problem.
  * \ingroup Structural Finite Element Analysis Variables
  * \author F. Palacios, R. Sanchez.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
 class CFEAVariable : public CVariable {
 protected:
diff --git a/SU2_CFD/include/variables/CFlowVariable.hpp b/SU2_CFD/include/variables/CFlowVariable.hpp
index 501b0fd4a1f..27c7b54d1c4 100644
--- a/SU2_CFD/include/variables/CFlowVariable.hpp
+++ b/SU2_CFD/include/variables/CFlowVariable.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file CFlowVariable.hpp
  * \brief Class for defining the common variables of flow solvers.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CHeatVariable.hpp b/SU2_CFD/include/variables/CHeatVariable.hpp
index b486f8238e0..b093cc8f284 100644
--- a/SU2_CFD/include/variables/CHeatVariable.hpp
+++ b/SU2_CFD/include/variables/CHeatVariable.hpp
@@ -2,7 +2,7 @@
  * \file CHeatVariable.hpp
  * \brief Class for defining the variables of the finite-volume heat equation solver.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -27,20 +27,18 @@
 
 #pragma once
 
-#include "CVariable.hpp"
+#include "CScalarVariable.hpp"
 
 /*!
  * \class CHeatVariable
  * \brief Class for defining the variables of the finite-volume heat equation solver.
  * \author O. Burghardt
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  */
-class CHeatVariable final : public CVariable {
-protected:
-  CVectorOfMatrix& Gradient_Reconstruction;  /*!< \brief Reference to the gradient of the primitive variables for MUSCL reconstruction for the convective term */
-  CVectorOfMatrix Gradient_Aux;              /*!< \brief Auxiliary structure to store a second gradient for reconstruction, if required. */
-
+class CHeatVariable final : public CScalarVariable {
 public:
+  static constexpr size_t MAXNVAR = 1; /*!< \brief Max number of variables, for static arrays. */
+
   /*!
    * \brief Constructor of the class.
    * \param[in] heat - Values of the Heat solution (initialization value).
@@ -51,29 +49,10 @@ class CHeatVariable final : public CVariable {
    */
   CHeatVariable(su2double heat, unsigned long npoint, unsigned long ndim, unsigned long nvar, CConfig *config);
 
-  /*!
-   * \brief Destructor of the class.
-   */
-  ~CHeatVariable() override = default;
-
-  /*!
-   * \brief Get the array of the reconstruction variables gradient at a node.
-   * \param[in] iPoint - Index of the current node.
-   * \return Array of the reconstruction variables gradient at a node.
-   */
-  inline CMatrixView<su2double> GetGradient_Reconstruction(unsigned long iPoint) final { return Gradient_Reconstruction[iPoint]; }
-
-  /*!
-   * \brief Get the reconstruction gradient for primitive variable at all points.
-   * \return Reference to variable reconstruction gradient.
-   */
-  inline CVectorOfMatrix& GetGradient_Reconstruction() final { return Gradient_Reconstruction; }
-  inline const CVectorOfMatrix& GetGradient_Reconstruction() const final { return Gradient_Reconstruction; }
-
   /*!
    * \brief Get the temperature of the point.
    * \return Value of the temperature of the point.
    */
-  inline su2double GetTemperature(unsigned long iPoint) const final { return Solution(iPoint,0); }
+  inline su2double GetTemperature(unsigned long iPoint) const final { return Solution(iPoint, 0); }
 
 };
diff --git a/SU2_CFD/include/variables/CIncEulerVariable.hpp b/SU2_CFD/include/variables/CIncEulerVariable.hpp
index 9670f3db9ef..a5626e5181c 100644
--- a/SU2_CFD/include/variables/CIncEulerVariable.hpp
+++ b/SU2_CFD/include/variables/CIncEulerVariable.hpp
@@ -2,7 +2,7 @@
  * \file CIncEulerVariable.hpp
  * \brief Class for defining the variables of the incompressible Euler solver.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CIncNSVariable.hpp b/SU2_CFD/include/variables/CIncNSVariable.hpp
index e1b23751f87..2a459dee443 100644
--- a/SU2_CFD/include/variables/CIncNSVariable.hpp
+++ b/SU2_CFD/include/variables/CIncNSVariable.hpp
@@ -3,7 +3,7 @@
  * \brief Class for defining the variables of the incompressible
           Navier-Stokes solver.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CMeshBoundVariable.hpp b/SU2_CFD/include/variables/CMeshBoundVariable.hpp
index 64d6caf2658..68b6752bcaf 100644
--- a/SU2_CFD/include/variables/CMeshBoundVariable.hpp
+++ b/SU2_CFD/include/variables/CMeshBoundVariable.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class
  *        to define the variables of the mesh movement at the moving boundaries.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CMeshElement.hpp b/SU2_CFD/include/variables/CMeshElement.hpp
index 8a8936d3632..b910b02694e 100644
--- a/SU2_CFD/include/variables/CMeshElement.hpp
+++ b/SU2_CFD/include/variables/CMeshElement.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class
  *        to define the variables of the mesh movement.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CMeshVariable.hpp b/SU2_CFD/include/variables/CMeshVariable.hpp
index 3751a37511b..8cf4b7f1b91 100644
--- a/SU2_CFD/include/variables/CMeshVariable.hpp
+++ b/SU2_CFD/include/variables/CMeshVariable.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class
  *        to define the variables of the mesh movement.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CNEMOEulerVariable.hpp b/SU2_CFD/include/variables/CNEMOEulerVariable.hpp
index b135bddd4b7..74def5d40ef 100644
--- a/SU2_CFD/include/variables/CNEMOEulerVariable.hpp
+++ b/SU2_CFD/include/variables/CNEMOEulerVariable.hpp
@@ -2,7 +2,7 @@
  * \file CNEMOEulerVariable.hpp
  * \brief Class for defining the variables of the compressible NEMO Euler solver.
  * \author C. Garbacz, W. Maier, S.R. Copeland
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CNEMONSVariable.hpp b/SU2_CFD/include/variables/CNEMONSVariable.hpp
index c57be1def02..926a9a80458 100644
--- a/SU2_CFD/include/variables/CNEMONSVariable.hpp
+++ b/SU2_CFD/include/variables/CNEMONSVariable.hpp
@@ -2,7 +2,7 @@
  * \file CNEMONSVariable.hpp
  * \brief Class for defining the variables of the compressible NEMO Navier-Stokes solver.
  * \author C. Garbacz, W. Maier, S.R. Copeland.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CNSVariable.hpp b/SU2_CFD/include/variables/CNSVariable.hpp
index caa98149eda..12ea5d3e730 100644
--- a/SU2_CFD/include/variables/CNSVariable.hpp
+++ b/SU2_CFD/include/variables/CNSVariable.hpp
@@ -2,7 +2,7 @@
  * \file CNSVariable.hpp
  * \brief Class for defining the variables of the compressible Navier-Stokes solver.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CPrimitiveIndices.hpp b/SU2_CFD/include/variables/CPrimitiveIndices.hpp
index 1e53d63b87c..64296db44b8 100644
--- a/SU2_CFD/include/variables/CPrimitiveIndices.hpp
+++ b/SU2_CFD/include/variables/CPrimitiveIndices.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file CPrimitiveIndices.hpp
  * \brief Abstract representation of flow primitive variable indices that tries to be efficient.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CRadP1Variable.hpp b/SU2_CFD/include/variables/CRadP1Variable.hpp
index 493d3448624..ed808ae78f8 100644
--- a/SU2_CFD/include/variables/CRadP1Variable.hpp
+++ b/SU2_CFD/include/variables/CRadP1Variable.hpp
@@ -2,7 +2,7 @@
  * \file CRadP1Variable.hpp
  * \brief Class for defining the variables of the P1 radiation model.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CRadVariable.hpp b/SU2_CFD/include/variables/CRadVariable.hpp
index 30806f9cf2f..a4bb9979255 100644
--- a/SU2_CFD/include/variables/CRadVariable.hpp
+++ b/SU2_CFD/include/variables/CRadVariable.hpp
@@ -2,7 +2,7 @@
  * \file CRadVariable.hpp
  * \brief Class for defining the variables of the radiation solver.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CScalarVariable.hpp b/SU2_CFD/include/variables/CScalarVariable.hpp
index 8b80a35bca5..1f63168419b 100644
--- a/SU2_CFD/include/variables/CScalarVariable.hpp
+++ b/SU2_CFD/include/variables/CScalarVariable.hpp
@@ -2,7 +2,7 @@
  * \file CScalarVariable.hpp
  * \brief Base class for defining the shared variables of scalar solvers.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CSobolevSmoothingVariable.hpp b/SU2_CFD/include/variables/CSobolevSmoothingVariable.hpp
index b56c66caf01..0ac3c9fa93f 100644
--- a/SU2_CFD/include/variables/CSobolevSmoothingVariable.hpp
+++ b/SU2_CFD/include/variables/CSobolevSmoothingVariable.hpp
@@ -2,7 +2,7 @@
  * \file CSobolevSmoothingVariable.hpp
  * \brief Class for defining the variables of the gradient smoothing.
  * \author T.Dick
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CSpeciesVariable.hpp b/SU2_CFD/include/variables/CSpeciesVariable.hpp
index fc5fec7b37f..654b38fd23e 100644
--- a/SU2_CFD/include/variables/CSpeciesVariable.hpp
+++ b/SU2_CFD/include/variables/CSpeciesVariable.hpp
@@ -2,7 +2,7 @@
  * \file CSpeciesVariable.hpp
  * \brief Base class for defining the variables of the species transport model.
  * \author T. Kattmann
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CTransLMVariable.hpp b/SU2_CFD/include/variables/CTransLMVariable.hpp
index 89e68406fc7..c3893023d55 100644
--- a/SU2_CFD/include/variables/CTransLMVariable.hpp
+++ b/SU2_CFD/include/variables/CTransLMVariable.hpp
@@ -2,7 +2,7 @@
  * \file CTransLMVariable.hpp
  * \brief Declaration of the variables of the transition model.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CTurbSAVariable.hpp b/SU2_CFD/include/variables/CTurbSAVariable.hpp
index 9abffc2a68c..4d0429efcb4 100644
--- a/SU2_CFD/include/variables/CTurbSAVariable.hpp
+++ b/SU2_CFD/include/variables/CTurbSAVariable.hpp
@@ -2,7 +2,7 @@
  * \file CTurbSAVariable.hpp
  * \brief Declaration of the variables of the SA turbulence model.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -39,7 +39,6 @@
 class CTurbSAVariable final : public CTurbVariable {
 
 private:
-  VectorType gamma_BC;         /*!< \brief Value of the intermittency for the BC trans. model. */
   VectorType DES_LengthScale;
   VectorType Vortex_Tilting;
 
@@ -61,20 +60,6 @@ class CTurbSAVariable final : public CTurbVariable {
    */
   ~CTurbSAVariable() override = default;
 
-  /*!
-   * \brief Get the intermittency of the BC transition model.
-   * \param[in] iPoint - Point index.
-   * \return Value of the intermittency of the BC transition model.
-   */
-  inline su2double GetGammaBC(unsigned long iPoint) const override { return gamma_BC(iPoint); }
-
-  /*!
-   * \brief Set the intermittency of the BC transition model.
-   * \param[in] iPoint - Point index.
-   * \param[in] val_gamma - New value of the intermittency.
-   */
-  inline void SetGammaBC(unsigned long iPoint, su2double val_gamma) override { gamma_BC(iPoint) = val_gamma; }
-
   /*!
    * \brief Get the DES length scale
    * \param[in] iPoint - Point index.
diff --git a/SU2_CFD/include/variables/CTurbSSTVariable.hpp b/SU2_CFD/include/variables/CTurbSSTVariable.hpp
index e01809979ec..e8a5d4559aa 100644
--- a/SU2_CFD/include/variables/CTurbSSTVariable.hpp
+++ b/SU2_CFD/include/variables/CTurbSSTVariable.hpp
@@ -2,7 +2,7 @@
  * \file CTurbSSTVariable.hpp
  * \brief Declaration of the variables of the SST turbulence model.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CTurbVariable.hpp b/SU2_CFD/include/variables/CTurbVariable.hpp
index 70615d5138e..62f7e582896 100644
--- a/SU2_CFD/include/variables/CTurbVariable.hpp
+++ b/SU2_CFD/include/variables/CTurbVariable.hpp
@@ -2,7 +2,7 @@
  * \file CTurbVariable.hpp
  * \brief Base class for defining the variables of the turbulence model.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -41,6 +41,8 @@ class CTurbVariable : public CScalarVariable {
 
 public:
   static constexpr size_t MAXNVAR = 2;
+  VectorType turb_index;
+  VectorType intermittency;         /*!< \brief Value of the intermittency for the trans. model. */
 
   /*!
    * \brief Constructor of the class.
@@ -70,5 +72,33 @@ class CTurbVariable : public CScalarVariable {
    */
   inline void SetmuT(unsigned long iPoint, su2double val_muT) final { muT(iPoint) = val_muT; }
 
+  /*!
+    * \brief Set the value of the turbulence index.
+   * \param[in] iPoint - Point index.
+   * \param[in] val_turb_index - Value of the turbulence index.
+   */
+  inline void SetTurbIndex(unsigned long iPoint, su2double val_turb_index) final { turb_index(iPoint) = val_turb_index; }
+
+  /*!
+   * \brief Get the value of the turbulence index.
+   * \param[in] iPoint - Point index.
+   * \return Value of the intermittency of the turbulence index.
+   */
+  inline su2double GetTurbIndex(unsigned long iPoint) const final { return turb_index(iPoint); }
+
+  /*!
+   * \brief Get the intermittency of the transition model.
+   * \param[in] iPoint - Point index.
+   * \return Value of the intermittency of the transition model.
+   */
+  inline su2double GetIntermittency(unsigned long iPoint) const final { return intermittency(iPoint); }
+
+  /*!
+   * \brief Set the intermittency of the transition model.
+   * \param[in] iPoint - Point index.
+   * \param[in] val_intermittency - New value of the intermittency.
+   */
+  inline void SetIntermittency(unsigned long iPoint, su2double val_intermittency) final { intermittency(iPoint) = val_intermittency; }
+
 };
 
diff --git a/SU2_CFD/include/variables/CVariable.hpp b/SU2_CFD/include/variables/CVariable.hpp
index 208e7de585b..73ac61075d6 100644
--- a/SU2_CFD/include/variables/CVariable.hpp
+++ b/SU2_CFD/include/variables/CVariable.hpp
@@ -4,7 +4,7 @@
           variables, function definitions in file <i>CVariable.cpp</i>.
           All variables are children of at least this class.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -1137,9 +1137,16 @@ class CVariable {
   /*!
    * \brief A virtual member.
    * \param[in] iPoint - Point index.
-   * \return Returns intermittency
+   * \return Sets separation intermittency
    */
-  inline virtual su2double GetIntermittency(unsigned long iPoint) const { return 0.0; }
+  inline virtual void SetGammaSep(unsigned long iPoint, su2double gamma_sep) {}
+
+  /*!
+   * \brief A virtual member.
+   * \param[in] iPoint - Point index.
+   * \return Sets Effective intermittency
+   */
+  inline virtual void SetGammaEff(unsigned long iPoint) {}
 
   /*!
    * \brief A virtual member.
@@ -1670,6 +1677,18 @@ class CVariable {
    */
   inline virtual su2double GetmuT(unsigned long iPoint) const { return 0.0; }
 
+  /*!
+   * \brief Get the value of the intermittency.
+   * \return the value of the intermittency.
+   */
+  inline virtual su2double GetIntermittency(unsigned long iPoint) const { return 0.0; }
+  
+  /*!
+   * \brief Set the intermittency.   
+   * \param[in] val_dist - Value of the  intermittency.
+   */
+  inline virtual void SetIntermittency(unsigned long iPoint, su2double val_Intermittency) {}
+
   /*!
    * \brief Get the value of the separation intermittency.
    * \return the value of the separation intermittency.
@@ -1677,8 +1696,8 @@ class CVariable {
   inline virtual su2double GetIntermittencySep(unsigned long iPoint) const { return 0.0; }
 
   /*!
-   * \brief Set the separation intermittency(gamma).
-   * \param[in] val_dist - Value of the separation intermittency(gamma).
+   * \brief Set the separation intermittency (gamma_sep).
+   * \param[in] val_dist - Value of the separation intermittency (gamma_sep).
    */
   inline virtual void SetIntermittencySep(unsigned long iPoint, su2double val_Intermittency_sep) {}
 
@@ -1689,8 +1708,8 @@ class CVariable {
   inline virtual su2double GetIntermittencyEff(unsigned long iPoint) const { return 0.0; }
 
   /*!
-   * \brief Set the effective intermittency(gamma).
-   * \param[in] Value of the effective intermittency(gamma).
+   * \brief Set the effective intermittency (gamma_eff).
+   * \param[in] Value of the effective intermittency (gamma_eff).
    */
   inline virtual void SetIntermittencyEff(unsigned long iPoint, su2double val_Intermittency_eff) {}
 
@@ -1700,6 +1719,18 @@ class CVariable {
    */
   inline virtual void SetmuT(unsigned long iPoint, su2double val_muT) {}
 
+  /*!
+   * \brief Set the value of the turbulence index.
+   * \param[in] val_turb_index - turbulence index
+   */
+  inline virtual void SetTurbIndex(unsigned long iPoint, su2double val_turb_index) {}
+
+  /*!
+   * \brief Get the value of the turbulence index.
+   * \return val_turb_index - turbulence index
+   */
+  inline virtual su2double GetTurbIndex(unsigned long iPoint) const {return 0.0;}
+
   /*!
    * \brief A virtual member.
    * \param[in] iVar - Index of the variable.
diff --git a/SU2_CFD/obj/Makefile.am b/SU2_CFD/obj/Makefile.am
index ac68053fce6..632dfceae27 100644
--- a/SU2_CFD/obj/Makefile.am
+++ b/SU2_CFD/obj/Makefile.am
@@ -3,7 +3,7 @@
 # \file Makefile.am
 # \brief Makefile for SU2_CFD
 # \author M. Colonno, T. Economon, F. Palacios
-# \version 7.4.0 "Blackbird"
+# \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_CFD/src/CMarkerProfileReaderFVM.cpp b/SU2_CFD/src/CMarkerProfileReaderFVM.cpp
index 7b91cacb925..96a3d7a8e5b 100644
--- a/SU2_CFD/src/CMarkerProfileReaderFVM.cpp
+++ b/SU2_CFD/src/CMarkerProfileReaderFVM.cpp
@@ -2,7 +2,7 @@
  * \file CMarkerProfileReaderFVM.cpp
  * \brief Class that handles the reading of marker profile files.
  * \author T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/SU2_CFD.cpp b/SU2_CFD/src/SU2_CFD.cpp
index d5197f8c4dc..a6a6a92f69c 100644
--- a/SU2_CFD/src/SU2_CFD.cpp
+++ b/SU2_CFD/src/SU2_CFD.cpp
@@ -2,7 +2,7 @@
  * \file SU2_CFD.cpp
  * \brief Main file of the SU2 Computational Fluid Dynamics code
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -47,7 +47,7 @@ int main(int argc, char *argv[]) {
 
   /*--- Command line parsing ---*/
 
-  CLI::App app{"SU2 v7.4.0 \"Blackbird\", The Open-Source CFD Code"};
+  CLI::App app{"SU2 v7.5.0 \"Blackbird\", The Open-Source CFD Code"};
   app.add_flag("-d,--dryrun", dry_run, "Enable dry run mode.\n"
                                        "Only execute preprocessing steps using a dummy geometry.");
   app.add_option("-t,--threads", num_threads, "Number of OpenMP threads per MPI rank.");
diff --git a/SU2_CFD/src/definition_structure.cpp b/SU2_CFD/src/definition_structure.cpp
index 1e60e6338ee..fd12fcc9a1d 100644
--- a/SU2_CFD/src/definition_structure.cpp
+++ b/SU2_CFD/src/definition_structure.cpp
@@ -2,7 +2,7 @@
  * \file definition_structure.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
index 960a2a8ef4a..c30d44b9fdc 100644
--- a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjMultizoneDriver.cpp
  * \brief The main subroutines for driving adjoint multi-zone problems
  * \author O. Burghardt, P. Gomes, T. Albring, R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
index 2d943c5351e..7d346ef74c6 100644
--- a/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
@@ -2,7 +2,7 @@
  * \file driver_adjoint_singlezone.cpp
  * \brief The main subroutines for driving adjoint single-zone problems.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index 4eed3037c64..0b2c5d94aab 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -2,7 +2,7 @@
  * \file CDriver.cpp
  * \brief The main subroutines for driving single or multi-zone problems.
  * \author T. Economon, H. Kline, R. Sanchez, F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -1910,8 +1910,13 @@ void CDriver::Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSol
       else if ((incompressible && (config->GetKind_Streamwise_Periodic() != ENUM_STREAMWISE_PERIODIC::NONE)) &&
                (config->GetEnergy_Equation() && !config->GetStreamwise_Periodic_Temperature()))
         numerics[iMGlevel][FLOW_SOL][source_second_term] = new CSourceIncStreamwisePeriodic_Outlet(nDim, nVar_Flow, config);
+      else if (config->GetVorticityConfinement() == YES) {
+        /*--- Vorticity Confinement term as a second source term to allow the use of VC along with other source terms ---*/
+        numerics[iMGlevel][FLOW_SOL][source_second_term] = new CSourceVorticityConfinement(nDim, nVar_Flow, config);
+      }
       else
         numerics[iMGlevel][FLOW_SOL][source_second_term] = new CSourceNothing(nDim, nVar_Flow, config);
+
     }
 
   }
@@ -2114,8 +2119,8 @@ void CDriver::Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSol
     /*--- Definition of the viscous scheme for each equation and mesh level ---*/
     for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
 
-      numerics[iMGlevel][HEAT_SOL][visc_term] = new CAvgGrad_Heat(nDim, nVar_Heat, config, true);
-      numerics[iMGlevel][HEAT_SOL][visc_bound_term] = new CAvgGrad_Heat(nDim, nVar_Heat, config, false);
+      numerics[iMGlevel][HEAT_SOL][visc_term] = new CAvgGrad_Heat(nDim, config, true);
+      numerics[iMGlevel][HEAT_SOL][visc_bound_term] = new CAvgGrad_Heat(nDim, config, false);
 
       switch (config->GetKind_ConvNumScheme_Heat()) {
 
diff --git a/SU2_CFD/src/drivers/CDummyDriver.cpp b/SU2_CFD/src/drivers/CDummyDriver.cpp
index e2094d14eb6..22815f7ab4e 100644
--- a/SU2_CFD/src/drivers/CDummyDriver.cpp
+++ b/SU2_CFD/src/drivers/CDummyDriver.cpp
@@ -2,7 +2,7 @@
  * \file CDummyDriver.cpp
  * \brief Dummy driver class for running the preprocessing without geometry preprocessing.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/drivers/CMultizoneDriver.cpp b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
index 878de90221c..7f982ac7fc8 100644
--- a/SU2_CFD/src/drivers/CMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
@@ -2,7 +2,7 @@
  * \file driver_structure.cpp
  * \brief The main subroutines for driving multi-zone problems.
  * \author R. Sanchez, O. Burghardt
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/drivers/CSinglezoneDriver.cpp b/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
index 07d96744946..dc196dca0c6 100644
--- a/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
@@ -2,7 +2,7 @@
  * \file driver_direct_singlezone.cpp
  * \brief The main subroutines for driving single-zone problems.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/fluid/CCoolProp.cpp b/SU2_CFD/src/fluid/CCoolProp.cpp
index 7a6815ad9fc..e632580edf4 100644
--- a/SU2_CFD/src/fluid/CCoolProp.cpp
+++ b/SU2_CFD/src/fluid/CCoolProp.cpp
@@ -2,7 +2,7 @@
  * \file CCoolProp.cpp
  * \brief Source of the fluid model from CoolProp.
  * \author P. Yan, G. Gori, A. Guardone
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/fluid/CFluidModel.cpp b/SU2_CFD/src/fluid/CFluidModel.cpp
index 250c2bcbbbf..03cead75136 100644
--- a/SU2_CFD/src/fluid/CFluidModel.cpp
+++ b/SU2_CFD/src/fluid/CFluidModel.cpp
@@ -2,7 +2,7 @@
  * \file CFluidModel.cpp
  * \brief Source of the fluid model base class containing thermo-physical subroutines.
  * \author S.Vitale, M.Pini, G.Gori, A.Guardone, P.Colonna, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/fluid/CFluidScalar.cpp b/SU2_CFD/src/fluid/CFluidScalar.cpp
index eb8f4624aec..5415c6adad0 100644
--- a/SU2_CFD/src/fluid/CFluidScalar.cpp
+++ b/SU2_CFD/src/fluid/CFluidScalar.cpp
@@ -2,7 +2,7 @@
  * \file CFluidScalar.cpp
  * \brief Defines the multicomponent incompressible Ideal Gas model for mixtures.
  * \author T. Economon, Mark Heimgartner, Cristopher Morales Ubal
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/fluid/CIdealGas.cpp b/SU2_CFD/src/fluid/CIdealGas.cpp
index 993d5b36648..fd17c96e053 100644
--- a/SU2_CFD/src/fluid/CIdealGas.cpp
+++ b/SU2_CFD/src/fluid/CIdealGas.cpp
@@ -2,7 +2,7 @@
  * \file CIdealGas.cpp
  * \brief Source of the ideal gas model.
  * \author S. Vitale, G. Gori, M. Pini, A. Guardone, P. Colonna
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/fluid/CMutationTCLib.cpp b/SU2_CFD/src/fluid/CMutationTCLib.cpp
index 32d252a55ef..1621ff0583d 100644
--- a/SU2_CFD/src/fluid/CMutationTCLib.cpp
+++ b/SU2_CFD/src/fluid/CMutationTCLib.cpp
@@ -2,7 +2,7 @@
  * \file CMutationTCLib.cpp
  * \brief Source of the Mutation++ 2T nonequilibrium gas model.
  * \author C. Garbacz
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/fluid/CNEMOGas.cpp b/SU2_CFD/src/fluid/CNEMOGas.cpp
index bf6db15c61c..348d9b162ca 100644
--- a/SU2_CFD/src/fluid/CNEMOGas.cpp
+++ b/SU2_CFD/src/fluid/CNEMOGas.cpp
@@ -2,7 +2,7 @@
  * \file CNEMOGas.cpp
  * \brief Source of the nonequilibrium gas model.
  * \author C. Garbacz, W. Maier, S. R. Copeland
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/fluid/CPengRobinson.cpp b/SU2_CFD/src/fluid/CPengRobinson.cpp
index 66abe62f4f4..ddfe4f99e1c 100644
--- a/SU2_CFD/src/fluid/CPengRobinson.cpp
+++ b/SU2_CFD/src/fluid/CPengRobinson.cpp
@@ -2,7 +2,7 @@
  * \file CPengRobinson.cpp
  * \brief Source of the Peng-Robinson model.
  * \author S. Vitale, G. Gori, M. Pini, A. Guardone, P. Colonna
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 2111cccb780..d5b40df5cdf 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -2,7 +2,7 @@
  * \file CSU2TCLib.cpp
  * \brief Source of user defined 2T nonequilibrium gas model.
  * \author C. Garbacz, W. Maier, S. R. Copeland
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/fluid/CVanDerWaalsGas.cpp b/SU2_CFD/src/fluid/CVanDerWaalsGas.cpp
index afbabc85444..92a400209f0 100644
--- a/SU2_CFD/src/fluid/CVanDerWaalsGas.cpp
+++ b/SU2_CFD/src/fluid/CVanDerWaalsGas.cpp
@@ -2,7 +2,7 @@
  * \file CVanDerWaalsGas.cpp
  * \brief Source of the Polytropic Van der Waals model.
  * \author S. Vitale, G. Gori, M. Pini, A. Guardone, P. Colonna
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/integration/CFEM_DG_Integration.cpp b/SU2_CFD/src/integration/CFEM_DG_Integration.cpp
index 366a1e55ee2..3deb590a7bf 100644
--- a/SU2_CFD/src/integration/CFEM_DG_Integration.cpp
+++ b/SU2_CFD/src/integration/CFEM_DG_Integration.cpp
@@ -2,7 +2,7 @@
  * \file CFEM_DG_Integration.cpp
  * \brief Definition of time and space integration for the DG solver.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/integration/CIntegration.cpp b/SU2_CFD/src/integration/CIntegration.cpp
index 3287dfb9aab..5e23dcc64bb 100644
--- a/SU2_CFD/src/integration/CIntegration.cpp
+++ b/SU2_CFD/src/integration/CIntegration.cpp
@@ -2,7 +2,7 @@
  * \file CIntegration.cpp
  * \brief Implementation of the base class for space and time integration.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/integration/CIntegrationFactory.cpp b/SU2_CFD/src/integration/CIntegrationFactory.cpp
index 9406394f02c..4a130fdba4a 100644
--- a/SU2_CFD/src/integration/CIntegrationFactory.cpp
+++ b/SU2_CFD/src/integration/CIntegrationFactory.cpp
@@ -2,7 +2,7 @@
  * \file CIntegrationFactory.cpp
  * \brief Main subroutines for CIntegrationFactory .
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/integration/CMultiGridIntegration.cpp b/SU2_CFD/src/integration/CMultiGridIntegration.cpp
index 3a96d873069..24b2a22058e 100644
--- a/SU2_CFD/src/integration/CMultiGridIntegration.cpp
+++ b/SU2_CFD/src/integration/CMultiGridIntegration.cpp
@@ -2,7 +2,7 @@
  * \file CMultiGridIntegration.cpp
  * \brief Implementation of the multigrid integration class.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/integration/CNewtonIntegration.cpp b/SU2_CFD/src/integration/CNewtonIntegration.cpp
index ea7bc7ea439..6792659b24c 100644
--- a/SU2_CFD/src/integration/CNewtonIntegration.cpp
+++ b/SU2_CFD/src/integration/CNewtonIntegration.cpp
@@ -2,7 +2,7 @@
  * \file CNewtonIntegration.cpp
  * \brief Newton-Krylov integration.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/integration/CSingleGridIntegration.cpp b/SU2_CFD/src/integration/CSingleGridIntegration.cpp
index 45c2c464930..7c167b74927 100644
--- a/SU2_CFD/src/integration/CSingleGridIntegration.cpp
+++ b/SU2_CFD/src/integration/CSingleGridIntegration.cpp
@@ -2,7 +2,7 @@
  * \file CSingleGridIntegration.cpp
  * \brief Single (fine) grid integration class implementation.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/integration/CStructuralIntegration.cpp b/SU2_CFD/src/integration/CStructuralIntegration.cpp
index dfd93d1483f..84125fda415 100644
--- a/SU2_CFD/src/integration/CStructuralIntegration.cpp
+++ b/SU2_CFD/src/integration/CStructuralIntegration.cpp
@@ -2,7 +2,7 @@
  * \file CStructuralIntegration.cpp
  * \brief Space and time integration for structural problems.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/interfaces/CInterface.cpp b/SU2_CFD/src/interfaces/CInterface.cpp
index d3a1f813c1d..6695ba3678f 100644
--- a/SU2_CFD/src/interfaces/CInterface.cpp
+++ b/SU2_CFD/src/interfaces/CInterface.cpp
@@ -2,7 +2,7 @@
  * \file CInterface.cpp
  * \brief Main subroutines for MPI transfer of information between zones
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/interfaces/cfd/CConservativeVarsInterface.cpp b/SU2_CFD/src/interfaces/cfd/CConservativeVarsInterface.cpp
index 196e3c34dbf..8301b631fad 100644
--- a/SU2_CFD/src/interfaces/cfd/CConservativeVarsInterface.cpp
+++ b/SU2_CFD/src/interfaces/cfd/CConservativeVarsInterface.cpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer conservative variables
  *        from a generic zone into another one.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/interfaces/cfd/CMixingPlaneInterface.cpp b/SU2_CFD/src/interfaces/cfd/CMixingPlaneInterface.cpp
index efce7831d37..4e4e9f1d77d 100644
--- a/SU2_CFD/src/interfaces/cfd/CMixingPlaneInterface.cpp
+++ b/SU2_CFD/src/interfaces/cfd/CMixingPlaneInterface.cpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer average variables
  *        needed for MixingPlane computation from a generic zone into another one.
  * \author S. Vitale
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/interfaces/cfd/CSlidingInterface.cpp b/SU2_CFD/src/interfaces/cfd/CSlidingInterface.cpp
index 3a8fdff399f..0529e7ab682 100644
--- a/SU2_CFD/src/interfaces/cfd/CSlidingInterface.cpp
+++ b/SU2_CFD/src/interfaces/cfd/CSlidingInterface.cpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer conservative variables
  *        from a generic zone into another
  * \author G. Gori Politecnico di Milano
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/interfaces/cht/CConjugateHeatInterface.cpp b/SU2_CFD/src/interfaces/cht/CConjugateHeatInterface.cpp
index ee8510da9ad..e6606ce33f0 100644
--- a/SU2_CFD/src/interfaces/cht/CConjugateHeatInterface.cpp
+++ b/SU2_CFD/src/interfaces/cht/CConjugateHeatInterface.cpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer temperature and heatflux
  *        density for conjugate heat interfaces between structure and fluid zones.
  * \author O. Burghardt
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/interfaces/fsi/CDiscAdjFlowTractionInterface.cpp b/SU2_CFD/src/interfaces/fsi/CDiscAdjFlowTractionInterface.cpp
index b70f8584a56..72a34390171 100644
--- a/SU2_CFD/src/interfaces/fsi/CDiscAdjFlowTractionInterface.cpp
+++ b/SU2_CFD/src/interfaces/fsi/CDiscAdjFlowTractionInterface.cpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer flow tractions
  *        from a fluid zone into a structural zone in a discrete adjoint simulation.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/interfaces/fsi/CDisplacementsInterface.cpp b/SU2_CFD/src/interfaces/fsi/CDisplacementsInterface.cpp
index 1fff081e6c1..e2ecb2f735f 100644
--- a/SU2_CFD/src/interfaces/fsi/CDisplacementsInterface.cpp
+++ b/SU2_CFD/src/interfaces/fsi/CDisplacementsInterface.cpp
@@ -2,7 +2,7 @@
  * \file CDisplacementsInterface.cpp
  * \brief Main subroutines for transferring boundary displacements.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/interfaces/fsi/CFlowTractionInterface.cpp b/SU2_CFD/src/interfaces/fsi/CFlowTractionInterface.cpp
index 756010da59d..e0cc061d47a 100644
--- a/SU2_CFD/src/interfaces/fsi/CFlowTractionInterface.cpp
+++ b/SU2_CFD/src/interfaces/fsi/CFlowTractionInterface.cpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer flow tractions
  *        from a fluid zone into a structural zone.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/iteration/CAdjFluidIteration.cpp b/SU2_CFD/src/iteration/CAdjFluidIteration.cpp
index 1320de1ff42..022e8fba2a2 100644
--- a/SU2_CFD/src/iteration/CAdjFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CAdjFluidIteration.cpp
@@ -2,7 +2,7 @@
  * \file CAdjFluidIteration.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -51,11 +51,16 @@ void CAdjFluidIteration::Preprocess(COutput* output, CIntegration**** integratio
   /*--- Continuous adjoint Euler, Navier-Stokes or Reynolds-averaged Navier-Stokes (RANS) equations ---*/
 
   if ((InnerIter == 0) || (config[val_iZone]->GetTime_Marching() != TIME_MARCHING::STEADY)) {
-    if (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::ADJ_EULER)
-      config[val_iZone]->SetGlobalParam(MAIN_SOLVER::ADJ_EULER, RUNTIME_FLOW_SYS);
-    if (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::ADJ_NAVIER_STOKES)
-      config[val_iZone]->SetGlobalParam(MAIN_SOLVER::ADJ_NAVIER_STOKES, RUNTIME_FLOW_SYS);
-    if (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::ADJ_RANS) config[val_iZone]->SetGlobalParam(MAIN_SOLVER::ADJ_RANS, RUNTIME_FLOW_SYS);
+    const auto kind_solver = config[val_iZone]->GetKind_Solver();
+    switch (kind_solver) {
+      case MAIN_SOLVER::ADJ_EULER:
+      case MAIN_SOLVER::ADJ_NAVIER_STOKES:
+      case MAIN_SOLVER::ADJ_RANS:
+        config[val_iZone]->SetGlobalParam(kind_solver, RUNTIME_FLOW_SYS);
+        break;
+      default:
+        break;
+    }
 
     /*--- Solve the Euler, Navier-Stokes or Reynolds-averaged Navier-Stokes (RANS) equations (one iteration) ---*/
 
@@ -78,7 +83,7 @@ void CAdjFluidIteration::Preprocess(COutput* output, CIntegration**** integratio
       /*--- Solve transition model ---*/
 
       if (config[val_iZone]->GetKind_Trans_Model() == TURB_TRANS_MODEL::LM) {
-        config[val_iZone]->SetGlobalParam(MAIN_SOLVER::RANS, RUNTIME_TRANS_SYS);
+        config[val_iZone]->SetGlobalParam(MAIN_SOLVER::ADJ_RANS, RUNTIME_TRANS_SYS);
         integration[val_iZone][val_iInst][TRANS_SOL]->SingleGrid_Iteration(geometry, solver, numerics, config,
                                                                            RUNTIME_TRANS_SYS, val_iZone, val_iInst);
       }
@@ -127,19 +132,13 @@ void CAdjFluidIteration::Iterate(COutput* output, CIntegration**** integration,
                                  CSolver***** solver, CNumerics****** numerics, CConfig** config,
                                  CSurfaceMovement** surface_movement, CVolumetricMovement*** grid_movement,
                                  CFreeFormDefBox*** FFDBox, unsigned short val_iZone, unsigned short val_iInst) {
-  switch (config[val_iZone]->GetKind_Solver()) {
+  const auto kind_solver = config[val_iZone]->GetKind_Solver();
+  switch (kind_solver) {
     case MAIN_SOLVER::ADJ_EULER:
-      config[val_iZone]->SetGlobalParam(MAIN_SOLVER::ADJ_EULER, RUNTIME_ADJFLOW_SYS);
-      break;
-
     case MAIN_SOLVER::ADJ_NAVIER_STOKES:
-      config[val_iZone]->SetGlobalParam(MAIN_SOLVER::ADJ_NAVIER_STOKES, RUNTIME_ADJFLOW_SYS);
-      break;
-
     case MAIN_SOLVER::ADJ_RANS:
-      config[val_iZone]->SetGlobalParam(MAIN_SOLVER::ADJ_RANS, RUNTIME_ADJFLOW_SYS);
+      config[val_iZone]->SetGlobalParam(kind_solver, RUNTIME_ADJFLOW_SYS);
       break;
-
     default:
       break;
   }
diff --git a/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
index 00e34052500..d7e8e037935 100644
--- a/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjFEAIteration.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
index 3e6cbba9266..6d4bc92c3ed 100644
--- a/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjFluidIteration.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
index 7a3698376de..d06dc22c08b 100644
--- a/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjHeatIteration.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/iteration/CFEAIteration.cpp b/SU2_CFD/src/iteration/CFEAIteration.cpp
index fae9ae4f181..9f1c954cd5f 100644
--- a/SU2_CFD/src/iteration/CFEAIteration.cpp
+++ b/SU2_CFD/src/iteration/CFEAIteration.cpp
@@ -2,7 +2,7 @@
  * \file CFEAIteration.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/iteration/CFEMFluidIteration.cpp b/SU2_CFD/src/iteration/CFEMFluidIteration.cpp
index 57aec2815ff..499f1740bd2 100644
--- a/SU2_CFD/src/iteration/CFEMFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CFEMFluidIteration.cpp
@@ -2,7 +2,7 @@
  * \file CFEMFluidIteration.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -47,17 +47,20 @@ void CFEMFluidIteration::Iterate(COutput* output, CIntegration**** integration,
                                  CFreeFormDefBox*** FFDBox, unsigned short val_iZone, unsigned short val_iInst) {
   /*--- Update global parameters ---*/
 
-  if (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::FEM_EULER || config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_FEM_EULER)
-    config[val_iZone]->SetGlobalParam(MAIN_SOLVER::FEM_EULER, RUNTIME_FLOW_SYS);
-
-  if (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::FEM_NAVIER_STOKES ||
-      config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_FEM_NS)
-    config[val_iZone]->SetGlobalParam(MAIN_SOLVER::FEM_NAVIER_STOKES, RUNTIME_FLOW_SYS);
-
-  if (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::FEM_RANS || config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_FEM_RANS)
-    config[val_iZone]->SetGlobalParam(MAIN_SOLVER::FEM_RANS, RUNTIME_FLOW_SYS);
-
-  if (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::FEM_LES) config[val_iZone]->SetGlobalParam(MAIN_SOLVER::FEM_LES, RUNTIME_FLOW_SYS);
+  const auto kind_solver = config[val_iZone]->GetKind_Solver();
+  switch (kind_solver) {
+    case MAIN_SOLVER::FEM_EULER:
+    case MAIN_SOLVER::DISC_ADJ_FEM_EULER:
+    case MAIN_SOLVER::FEM_NAVIER_STOKES:
+    case MAIN_SOLVER::DISC_ADJ_FEM_NS:
+    case MAIN_SOLVER::FEM_RANS:
+    case MAIN_SOLVER::DISC_ADJ_FEM_RANS:
+    case MAIN_SOLVER::FEM_LES:
+      config[val_iZone]->SetGlobalParam(kind_solver, RUNTIME_FLOW_SYS);
+      break;
+    default:
+      break;
+  }
 
   /*--- Solve the Euler, Navier-Stokes, RANS or LES equations (one iteration) ---*/
 
diff --git a/SU2_CFD/src/iteration/CFluidIteration.cpp b/SU2_CFD/src/iteration/CFluidIteration.cpp
index 864478cd822..a39031ae6ee 100644
--- a/SU2_CFD/src/iteration/CFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CFluidIteration.cpp
@@ -2,7 +2,7 @@
  * \file CFluidIteration.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -71,35 +71,7 @@ void CFluidIteration::Iterate(COutput* output, CIntegration**** integration, CGe
 
   /*--- Update global parameters ---*/
 
-  MAIN_SOLVER main_solver = MAIN_SOLVER::NONE;
-
-  switch (config[val_iZone]->GetKind_Solver()) {
-    case MAIN_SOLVER::EULER:
-    case MAIN_SOLVER::DISC_ADJ_EULER:
-    case MAIN_SOLVER::INC_EULER:
-    case MAIN_SOLVER::DISC_ADJ_INC_EULER:
-    case MAIN_SOLVER::NEMO_EULER:
-      main_solver = MAIN_SOLVER::EULER;
-      break;
-
-    case MAIN_SOLVER::NAVIER_STOKES:
-    case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES:
-    case MAIN_SOLVER::INC_NAVIER_STOKES:
-    case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES:
-    case MAIN_SOLVER::NEMO_NAVIER_STOKES:
-      main_solver = MAIN_SOLVER::NAVIER_STOKES;
-      break;
-
-    case MAIN_SOLVER::RANS:
-    case MAIN_SOLVER::DISC_ADJ_RANS:
-    case MAIN_SOLVER::INC_RANS:
-    case MAIN_SOLVER::DISC_ADJ_INC_RANS:
-      main_solver = MAIN_SOLVER::RANS;
-      break;
-
-    default:
-      break;
-  }
+  const auto main_solver = config[val_iZone]->GetKind_Solver();
   config[val_iZone]->SetGlobalParam(main_solver, RUNTIME_FLOW_SYS);
 
   /*--- Solve the Euler, Navier-Stokes or Reynolds-averaged Navier-Stokes (RANS) equations (one iteration) ---*/
@@ -109,8 +81,8 @@ void CFluidIteration::Iterate(COutput* output, CIntegration**** integration, CGe
 
   /*--- If the flow integration is not fully coupled, run the various single grid integrations. ---*/
 
-  if ((main_solver == MAIN_SOLVER::RANS) && !frozen_visc) {
-    
+  if (config[val_iZone]->GetKind_Turb_Model() != TURB_MODEL::NONE && !frozen_visc) {
+
     /*--- Solve transition model ---*/
 
     if (config[val_iZone]->GetKind_Trans_Model() == TURB_TRANS_MODEL::LM) {
@@ -118,12 +90,12 @@ void CFluidIteration::Iterate(COutput* output, CIntegration**** integration, CGe
       integration[val_iZone][val_iInst][TRANS_SOL]->SingleGrid_Iteration(geometry, solver, numerics, config,
                                                                          RUNTIME_TRANS_SYS, val_iZone, val_iInst);
     }
-    
+
     /*--- Solve the turbulence model ---*/
 
     config[val_iZone]->SetGlobalParam(main_solver, RUNTIME_TURB_SYS);
     integration[val_iZone][val_iInst][TURB_SOL]->SingleGrid_Iteration(geometry, solver, numerics, config,
-                                                                      RUNTIME_TURB_SYS, val_iZone, val_iInst);    
+                                                                      RUNTIME_TURB_SYS, val_iZone, val_iInst);
   }
 
   if (config[val_iZone]->GetKind_Species_Model() != SPECIES_MODEL::NONE){
diff --git a/SU2_CFD/src/iteration/CHeatIteration.cpp b/SU2_CFD/src/iteration/CHeatIteration.cpp
index b17cd2bc2c3..8b78885a152 100644
--- a/SU2_CFD/src/iteration/CHeatIteration.cpp
+++ b/SU2_CFD/src/iteration/CHeatIteration.cpp
@@ -2,7 +2,7 @@
  * \file CHeatIteration.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/iteration/CIteration.cpp b/SU2_CFD/src/iteration/CIteration.cpp
index 90750078678..ae3442e95bb 100644
--- a/SU2_CFD/src/iteration/CIteration.cpp
+++ b/SU2_CFD/src/iteration/CIteration.cpp
@@ -2,7 +2,7 @@
  * \file iteration_structure.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/iteration/CIterationFactory.cpp b/SU2_CFD/src/iteration/CIterationFactory.cpp
index 948ea885f40..fac25d838a6 100644
--- a/SU2_CFD/src/iteration/CIterationFactory.cpp
+++ b/SU2_CFD/src/iteration/CIterationFactory.cpp
@@ -2,7 +2,7 @@
  * \file CAdjFluidIteration.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/iteration/CTurboIteration.cpp b/SU2_CFD/src/iteration/CTurboIteration.cpp
index f74fa8034e6..fad8866e048 100644
--- a/SU2_CFD/src/iteration/CTurboIteration.cpp
+++ b/SU2_CFD/src/iteration/CTurboIteration.cpp
@@ -2,7 +2,7 @@
  * \file CTurboIteration.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/limiters/CLimiterDetails.cpp b/SU2_CFD/src/limiters/CLimiterDetails.cpp
index 98e5d4724aa..23353805b7f 100644
--- a/SU2_CFD/src/limiters/CLimiterDetails.cpp
+++ b/SU2_CFD/src/limiters/CLimiterDetails.cpp
@@ -3,7 +3,7 @@
  * \brief A class template that allows defining limiters via
  *        specialization of particular details.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/CGradSmoothing.cpp b/SU2_CFD/src/numerics/CGradSmoothing.cpp
index 0a6fb533a3a..af0e62b4068 100644
--- a/SU2_CFD/src/numerics/CGradSmoothing.cpp
+++ b/SU2_CFD/src/numerics/CGradSmoothing.cpp
@@ -2,7 +2,7 @@
  * \file CGradSmoothing.cpp
  * \brief Numerics for gradient smoothing problems.
  * \author T.Dick
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/CNumerics.cpp b/SU2_CFD/src/numerics/CNumerics.cpp
index 43ccc81f7c0..ff0423058fa 100644
--- a/SU2_CFD/src/numerics/CNumerics.cpp
+++ b/SU2_CFD/src/numerics/CNumerics.cpp
@@ -4,7 +4,7 @@
  *        Contains methods for common tasks, e.g. compute flux
  *        Jacobians.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp b/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp
index ee1df5aaff0..753ba843c08 100644
--- a/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp
+++ b/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp
@@ -4,7 +4,7 @@
  *        Contains methods for common tasks, e.g. compute flux
  *        Jacobians.
  * \author S.R. Copeland, W. Maier, C. Garbacz
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp b/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
index 02a957e1f78..f764949536c 100644
--- a/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
+++ b/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
@@ -3,7 +3,7 @@
  * \brief Implementation of numerics classes for discretization
  *        of viscous fluxes in fluid flow NEMO problems.
  * \author S.R. Copeland, W. Maier, C. Garbacz
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp b/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp
index fce5bfb3667..736ed507ed8 100644
--- a/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp
+++ b/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp
@@ -3,7 +3,7 @@
  * \brief Implementation of numerics classes for integration
  *        of source terms in fluid flow NEMO problems.
  * \author C. Garbacz, W. Maier, S. Copeland.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/NEMO/convection/ausm.cpp b/SU2_CFD/src/numerics/NEMO/convection/ausm.cpp
index 4ac98341e58..8a336c67db3 100644
--- a/SU2_CFD/src/numerics/NEMO/convection/ausm.cpp
+++ b/SU2_CFD/src/numerics/NEMO/convection/ausm.cpp
@@ -2,7 +2,7 @@
  * \file ausm.cpp
  * \brief Implementations of the AUSM-family of schemes in NEMO.
  * \author F. Palacios, S.R. Copeland, W. Maier, C. Garbacz
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/NEMO/convection/ausmplusup2.cpp b/SU2_CFD/src/numerics/NEMO/convection/ausmplusup2.cpp
index b9be7c61831..e55c05be34d 100644
--- a/SU2_CFD/src/numerics/NEMO/convection/ausmplusup2.cpp
+++ b/SU2_CFD/src/numerics/NEMO/convection/ausmplusup2.cpp
@@ -2,7 +2,7 @@
  * \file ausmplusup2.cpp
  * \brief Implementations of the AUSM-family of schemes - AUSM+UP2.
  * \author W. Maier, A. Sachedeva, C. Garbacz
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/NEMO/convection/ausmpwplus.cpp b/SU2_CFD/src/numerics/NEMO/convection/ausmpwplus.cpp
index 3b88853bab5..38597ec2395 100644
--- a/SU2_CFD/src/numerics/NEMO/convection/ausmpwplus.cpp
+++ b/SU2_CFD/src/numerics/NEMO/convection/ausmpwplus.cpp
@@ -2,7 +2,7 @@
  * \file ausmpwplus.cpp
  * \brief Implementations of the AUSM-family of schemes - AUSMPWPLUS.
  * \author F. Palacios, W. Maier, C. Garbacz
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/NEMO/convection/lax.cpp b/SU2_CFD/src/numerics/NEMO/convection/lax.cpp
index 0dd467183d5..237e99e5696 100644
--- a/SU2_CFD/src/numerics/NEMO/convection/lax.cpp
+++ b/SU2_CFD/src/numerics/NEMO/convection/lax.cpp
@@ -2,7 +2,7 @@
  * \file lax.cpp
  * \brief Implementations of Lax centered scheme.
  * \author F. Palacios, S.R. Copeland, W. Maier, C. Garbacz
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/NEMO/convection/msw.cpp b/SU2_CFD/src/numerics/NEMO/convection/msw.cpp
index 9da640a1585..f77998fcdb8 100644
--- a/SU2_CFD/src/numerics/NEMO/convection/msw.cpp
+++ b/SU2_CFD/src/numerics/NEMO/convection/msw.cpp
@@ -2,7 +2,7 @@
  * \file msw.cpp
  * \brief Implementations of the modified Steger-Warming scheme.
  * \author ADL Stanford, S.R. Copeland, W. Maier, C. Garbacz
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/NEMO/convection/roe.cpp b/SU2_CFD/src/numerics/NEMO/convection/roe.cpp
index d86732fdf00..b03947faf42 100644
--- a/SU2_CFD/src/numerics/NEMO/convection/roe.cpp
+++ b/SU2_CFD/src/numerics/NEMO/convection/roe.cpp
@@ -2,7 +2,7 @@
  * \file roe.cpp
  * \brief Implementations of Roe-type schemes in NEMO.
  * \author S. R. Copeland, W. Maier, C. Garbacz
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/continuous_adjoint/adj_convection.cpp b/SU2_CFD/src/numerics/continuous_adjoint/adj_convection.cpp
index 2eb7b9fba87..27a5b22379b 100644
--- a/SU2_CFD/src/numerics/continuous_adjoint/adj_convection.cpp
+++ b/SU2_CFD/src/numerics/continuous_adjoint/adj_convection.cpp
@@ -2,7 +2,7 @@
  * \file adj_convection.cpp
  * \brief Implementation of adjoint convection numerics classes.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/continuous_adjoint/adj_diffusion.cpp b/SU2_CFD/src/numerics/continuous_adjoint/adj_diffusion.cpp
index aa2c97ef061..8b187ccc3f9 100644
--- a/SU2_CFD/src/numerics/continuous_adjoint/adj_diffusion.cpp
+++ b/SU2_CFD/src/numerics/continuous_adjoint/adj_diffusion.cpp
@@ -2,7 +2,7 @@
  * \file adj_diffusion.cpp
  * \brief Implementation of adjoint diffusion numerics classes.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/continuous_adjoint/adj_sources.cpp b/SU2_CFD/src/numerics/continuous_adjoint/adj_sources.cpp
index 66ed7bf74ed..3bf58bb9fa6 100644
--- a/SU2_CFD/src/numerics/continuous_adjoint/adj_sources.cpp
+++ b/SU2_CFD/src/numerics/continuous_adjoint/adj_sources.cpp
@@ -2,7 +2,7 @@
  * \file adj_sources.cpp
  * \brief Implementation of adjoint source numerics classes.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/elasticity/CFEAElasticity.cpp b/SU2_CFD/src/numerics/elasticity/CFEAElasticity.cpp
index 2970855fed5..f8e85a87438 100644
--- a/SU2_CFD/src/numerics/elasticity/CFEAElasticity.cpp
+++ b/SU2_CFD/src/numerics/elasticity/CFEAElasticity.cpp
@@ -2,7 +2,7 @@
  * \file CFEAElasticity.cpp
  * \brief Base class for all elasticity problems.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/elasticity/CFEALinearElasticity.cpp b/SU2_CFD/src/numerics/elasticity/CFEALinearElasticity.cpp
index 13a76139392..b42b1c42ed4 100644
--- a/SU2_CFD/src/numerics/elasticity/CFEALinearElasticity.cpp
+++ b/SU2_CFD/src/numerics/elasticity/CFEALinearElasticity.cpp
@@ -2,7 +2,7 @@
  * \file CFEALinearElasticity.cpp
  * \brief Classes for linear elasticity problems.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/elasticity/CFEANonlinearElasticity.cpp b/SU2_CFD/src/numerics/elasticity/CFEANonlinearElasticity.cpp
index 0cdcef0cb0e..ff950f321a1 100644
--- a/SU2_CFD/src/numerics/elasticity/CFEANonlinearElasticity.cpp
+++ b/SU2_CFD/src/numerics/elasticity/CFEANonlinearElasticity.cpp
@@ -3,7 +3,7 @@
  * \brief This file contains the routines for setting the tangent matrix and
  *        residual of a FEM nonlinear elastic structural problem.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/elasticity/nonlinear_models.cpp b/SU2_CFD/src/numerics/elasticity/nonlinear_models.cpp
index 3699984242e..0947c1ebe4d 100644
--- a/SU2_CFD/src/numerics/elasticity/nonlinear_models.cpp
+++ b/SU2_CFD/src/numerics/elasticity/nonlinear_models.cpp
@@ -2,7 +2,7 @@
  * \file nonlinear_models.cpp
  * \brief Definition of nonlinear constitutive models.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/flow/convection/ausm_slau.cpp b/SU2_CFD/src/numerics/flow/convection/ausm_slau.cpp
index b3fd3c7b6d5..cebb6209ab1 100644
--- a/SU2_CFD/src/numerics/flow/convection/ausm_slau.cpp
+++ b/SU2_CFD/src/numerics/flow/convection/ausm_slau.cpp
@@ -2,7 +2,7 @@
  * \file ausm_slau.cpp
  * \brief Implementations of the AUSM-family of schemes.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/flow/convection/centered.cpp b/SU2_CFD/src/numerics/flow/convection/centered.cpp
index 6eeca4ca231..1ff083d950b 100644
--- a/SU2_CFD/src/numerics/flow/convection/centered.cpp
+++ b/SU2_CFD/src/numerics/flow/convection/centered.cpp
@@ -2,7 +2,7 @@
  * \file centered.cpp
  * \brief Implementations of centered schemes.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/flow/convection/cusp.cpp b/SU2_CFD/src/numerics/flow/convection/cusp.cpp
index a683bd4ad9b..b10206425c2 100644
--- a/SU2_CFD/src/numerics/flow/convection/cusp.cpp
+++ b/SU2_CFD/src/numerics/flow/convection/cusp.cpp
@@ -2,7 +2,7 @@
  * \file cusp.cpp
  * \brief Implementation of the CUSP scheme.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/flow/convection/fds.cpp b/SU2_CFD/src/numerics/flow/convection/fds.cpp
index 44d30bf877e..33a53a37e45 100644
--- a/SU2_CFD/src/numerics/flow/convection/fds.cpp
+++ b/SU2_CFD/src/numerics/flow/convection/fds.cpp
@@ -2,7 +2,7 @@
  * \file fds.cpp
  * \brief Implementation of Flux-Difference-Splitting schemes.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/flow/convection/fvs.cpp b/SU2_CFD/src/numerics/flow/convection/fvs.cpp
index c8271a0d7e8..18f29534a74 100644
--- a/SU2_CFD/src/numerics/flow/convection/fvs.cpp
+++ b/SU2_CFD/src/numerics/flow/convection/fvs.cpp
@@ -2,7 +2,7 @@
  * \file fvs.cpp
  * \brief Implementations of Flux-Vector-Splitting schemes.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/flow/convection/hllc.cpp b/SU2_CFD/src/numerics/flow/convection/hllc.cpp
index 0c9cc187d35..149a6491c3d 100644
--- a/SU2_CFD/src/numerics/flow/convection/hllc.cpp
+++ b/SU2_CFD/src/numerics/flow/convection/hllc.cpp
@@ -2,7 +2,7 @@
  * \file hllc.cpp
  * \brief Implementations of HLLC schemes.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/flow/convection/roe.cpp b/SU2_CFD/src/numerics/flow/convection/roe.cpp
index 6713f5b8f58..26422506229 100644
--- a/SU2_CFD/src/numerics/flow/convection/roe.cpp
+++ b/SU2_CFD/src/numerics/flow/convection/roe.cpp
@@ -2,7 +2,7 @@
  * \file roe.cpp
  * \brief Implementations of Roe-type schemes.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/flow/flow_diffusion.cpp b/SU2_CFD/src/numerics/flow/flow_diffusion.cpp
index 7cdd6417697..ce11fea684e 100644
--- a/SU2_CFD/src/numerics/flow/flow_diffusion.cpp
+++ b/SU2_CFD/src/numerics/flow/flow_diffusion.cpp
@@ -3,7 +3,7 @@
  * \brief Implementation of numerics classes for discretization
  *        of viscous fluxes in fluid flow problems.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/flow/flow_sources.cpp b/SU2_CFD/src/numerics/flow/flow_sources.cpp
index b1779970b39..7b6d0a43021 100644
--- a/SU2_CFD/src/numerics/flow/flow_sources.cpp
+++ b/SU2_CFD/src/numerics/flow/flow_sources.cpp
@@ -3,7 +3,7 @@
  * \brief Implementation of numerics classes for integration
  *        of source terms in fluid flow problems.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -616,6 +616,105 @@ CNumerics::ResidualType<> CSourceIncRotatingFrame_Flow::ComputeResidual(const CC
   return ResidualType<>(residual, jacobian, nullptr);
 }
 
+CSourceVorticityConfinement::CSourceVorticityConfinement(unsigned short val_nDim, unsigned short val_nVar,
+                                                         const CConfig* config)
+    : CSourceBase_Flow(val_nDim, val_nVar, config) {
+  Gamma = config->GetGamma();
+  Gamma_Minus_One = Gamma - 1.0;
+}
+
+CNumerics::ResidualType<> CSourceVorticityConfinement::ComputeResidual(const CConfig* config) {
+  /*--- density, \rho ---*/
+  const su2double rho = V_i[nDim + 2];
+
+  /*--- velocity, U = (u, v, w) ---*/
+  su2double U[3] = {V_i[1], V_i[2], 0.0};
+  if (nDim == 3) U[2] = V_i[3];
+  const su2double U_abs = max(GeometryToolbox::Norm(3, U), 1e-12);
+
+  /*--- vorticity, \omega ---*/
+  const su2double omega[3] = {Vorticity_i[0], Vorticity_i[1], Vorticity_i[2]};
+
+  /*--- grad of the mag of vorticity, \nabla|\omega| = AuxVar_Grad_i[0] ---*/
+  const su2double omega_abs_grad_abs = max(GeometryToolbox::Norm(3, AuxVar_Grad_i[0]), 1e-12);
+
+  /*--- unit vector, n along \nabla|\omega| ---*/
+  const su2double n[3] = {
+      AuxVar_Grad_i[0][0] / omega_abs_grad_abs,
+      AuxVar_Grad_i[0][1] / omega_abs_grad_abs,
+      AuxVar_Grad_i[0][2] / omega_abs_grad_abs,
+  };
+
+  /*--- n \cross \omega ---*/
+  su2double nXomega[3] = {0.0, 0.0, 0.0};
+  GeometryToolbox::CrossProduct(n, omega, nXomega);
+  const su2double nXomega_U = GeometryToolbox::DotProduct(3, nXomega, U);
+
+  /*--- vorticity confinement parameter ---*/
+  const su2double vc_config = config->GetConfinement_Param();
+  su2double vc = vc_config * (1 + log10(pow((1 + (Volume / AvgVolume)), 1.0 / 3.0)));
+
+  /*--- correction to vc near viscous wall ---*/
+  const bool viscous = config->GetViscous();
+  if (viscous) {
+    su2double U_infty[3] = {config->GetVelocity_FreeStreamND()[0], config->GetVelocity_FreeStreamND()[1], 0.0};
+    if (nDim == 3) U_infty[2] = config->GetVelocity_FreeStreamND()[2];
+    const su2double U_infty_abs = max(GeometryToolbox::Norm(3, U_infty), 1e-12);
+    const su2double L = config->GetLength_Reynolds();
+    const su2double mu = V_i[nDim + 5];                   // viscosity
+    const su2double mu_t = V_i[nDim + 6];                 // turbulent or eddy viscosity
+    const su2double mu_eff = mu + mu_t;                   // effective or total viscosity
+    const su2double Re = rho * U_infty_abs * L / mu_eff;  // Reynolds number
+    const su2double delta = 5 * L / sqrt(Re);             // boundary layer thickness
+
+    if (dist_i <= 4 * delta) {
+      vc *= 0.0;
+    }
+  }
+
+  /*--- source terms: S / rho ---*/
+  const su2double vc_Uabs_Volume = vc * U_abs * Volume;
+  const su2double S_u_rho = -nXomega[0] * vc_Uabs_Volume;
+  const su2double S_v_rho = -nXomega[1] * vc_Uabs_Volume;
+  const su2double S_w_rho = -nXomega[2] * vc_Uabs_Volume;
+  const su2double S_E_rho = -nXomega_U * vc_Uabs_Volume;
+
+  residual[0] = 0.0;
+  residual[1] = rho * S_u_rho;
+  residual[2] = rho * S_v_rho;
+  if (nDim == 2) {
+    residual[3] = rho * S_E_rho;
+  }
+  if (nDim == 3) {
+    residual[3] = rho * S_w_rho;
+    residual[4] = rho * S_E_rho;
+  }
+
+  const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+  if (implicit) {
+    for (unsigned iVar = 0; iVar < nVar; iVar++) {
+      for (unsigned jVar = 0; jVar < nVar; jVar++) {
+        jacobian[iVar][jVar] = 0.0;
+      }
+    }
+
+    jacobian[1][0] = S_u_rho;
+    jacobian[2][0] = S_v_rho;
+    if (nDim == 2) {
+      jacobian[3][1] = S_u_rho;
+      jacobian[3][2] = S_v_rho;
+    }
+    if (nDim == 3) {
+      jacobian[3][0] = S_w_rho;
+      jacobian[4][1] = S_u_rho;
+      jacobian[4][2] = S_v_rho;
+      jacobian[4][3] = S_w_rho;
+    }
+  }
+
+  return ResidualType<>(residual, jacobian, nullptr);
+}
+
 CSourceWindGust::CSourceWindGust(unsigned short val_nDim, unsigned short val_nVar, const CConfig* config) :
                  CSourceBase_Flow(val_nDim, val_nVar, config) { }
 
diff --git a/SU2_CFD/src/numerics/heat.cpp b/SU2_CFD/src/numerics/heat.cpp
index 3830c857180..f18c2a69b62 100644
--- a/SU2_CFD/src/numerics/heat.cpp
+++ b/SU2_CFD/src/numerics/heat.cpp
@@ -2,7 +2,7 @@
  * \file heat.cpp
  * \brief Implementation of numerics classes for heat transfer.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -160,43 +160,3 @@ void CUpwSca_Heat::ComputeResidual(su2double *val_residual, su2double **val_Jaco
   AD::EndPreacc();
 
 }
-
-CAvgGrad_Heat::CAvgGrad_Heat(unsigned short val_nDim, unsigned short val_nVar,
-                             const CConfig *config, bool correct_) :
-               CNumerics(val_nDim, val_nVar, config) {
-
-  implicit = (config->GetKind_TimeIntScheme_Heat() == EULER_IMPLICIT);
-  correct = correct_;
-}
-
-void CAvgGrad_Heat::ComputeResidual(su2double *val_residual, su2double **Jacobian_i,
-                                    su2double **Jacobian_j, CConfig *config) {
-  constexpr int nVar = 1;
-
-  AD::StartPreacc();
-  AD::SetPreaccIn(Coord_i, nDim); AD::SetPreaccIn(Coord_j, nDim);
-  AD::SetPreaccIn(Normal, nDim);
-  AD::SetPreaccIn(Temp_i); AD::SetPreaccIn(Temp_j);
-  AD::SetPreaccIn(ConsVar_Grad_i[0],nDim); AD::SetPreaccIn(ConsVar_Grad_j[0],nDim);
-  AD::SetPreaccIn(Thermal_Diffusivity_i); AD::SetPreaccIn(Thermal_Conductivity_j);
-
-  su2double NormalGrad[nVar], CorrectedGrad[nVar];
-
-  auto proj_vector_ij = ComputeProjectedGradient(nDim, nVar, Normal, Coord_i, Coord_j, ConsVar_Grad_i,
-                                                 ConsVar_Grad_j, correct, &Temp_i, &Temp_j,
-                                                 NormalGrad, CorrectedGrad);
-
-  const su2double Thermal_Diffusivity_Mean = 0.5*(Thermal_Diffusivity_i + Thermal_Diffusivity_j);
-
-  val_residual[0] = Thermal_Diffusivity_Mean*CorrectedGrad[0];
-
-  /*--- For Jacobians -> Use of TSL approx. to compute derivatives of the gradients ---*/
-  if (implicit) {
-    Jacobian_i[0][0] = -Thermal_Diffusivity_Mean*proj_vector_ij;
-    Jacobian_j[0][0] = Thermal_Diffusivity_Mean*proj_vector_ij;
-  }
-
-  AD::SetPreaccOut(val_residual, nVar);
-  AD::EndPreacc();
-
-}
diff --git a/SU2_CFD/src/numerics/radiation.cpp b/SU2_CFD/src/numerics/radiation.cpp
index bb3d5a9fcae..b3295fac20f 100644
--- a/SU2_CFD/src/numerics/radiation.cpp
+++ b/SU2_CFD/src/numerics/radiation.cpp
@@ -3,7 +3,7 @@
  * \brief This file contains the implementation of the numerical
  *        methods for radiation.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/scalar/scalar_sources.cpp b/SU2_CFD/src/numerics/scalar/scalar_sources.cpp
index a2f4a71495e..d51c2ca7711 100644
--- a/SU2_CFD/src/numerics/scalar/scalar_sources.cpp
+++ b/SU2_CFD/src/numerics/scalar/scalar_sources.cpp
@@ -1,7 +1,7 @@
 /*!
  * \file scalar_sources.cpp
  * \brief Implementation of numerics classes for integration of scalar source-terms.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/species/species_sources.cpp b/SU2_CFD/src/numerics/species/species_sources.cpp
index 50183ac85ea..3d89a2619db 100644
--- a/SU2_CFD/src/numerics/species/species_sources.cpp
+++ b/SU2_CFD/src/numerics/species/species_sources.cpp
@@ -3,7 +3,7 @@
  * \brief Implementation of numerics classes for integration of
  *        species transport source-terms.
  * \author T. Kattmann
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/template.cpp b/SU2_CFD/src/numerics/template.cpp
index ba6743ddfbe..b1c6c4462f9 100644
--- a/SU2_CFD/src/numerics/template.cpp
+++ b/SU2_CFD/src/numerics/template.cpp
@@ -2,7 +2,7 @@
  * \file template.cpp
  * \brief Empty implementation of numerics templates, see .hpp file.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CAdjElasticityOutput.cpp b/SU2_CFD/src/output/CAdjElasticityOutput.cpp
index 636c578944e..baf0b59e24b 100644
--- a/SU2_CFD/src/output/CAdjElasticityOutput.cpp
+++ b/SU2_CFD/src/output/CAdjElasticityOutput.cpp
@@ -2,7 +2,7 @@
  * \file CAdjElasticityOutput.cpp
  * \brief Main subroutines for elasticity discrete adjoint output
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CAdjFlowCompOutput.cpp b/SU2_CFD/src/output/CAdjFlowCompOutput.cpp
index d94f1b00348..4c5cfa58173 100644
--- a/SU2_CFD/src/output/CAdjFlowCompOutput.cpp
+++ b/SU2_CFD/src/output/CAdjFlowCompOutput.cpp
@@ -2,7 +2,7 @@
  * \file CAdjFlowCompOutput.cpp
  * \brief Main subroutines for flow discrete adjoint output
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CAdjFlowIncOutput.cpp b/SU2_CFD/src/output/CAdjFlowIncOutput.cpp
index 647b734c3cd..f653d4332fa 100644
--- a/SU2_CFD/src/output/CAdjFlowIncOutput.cpp
+++ b/SU2_CFD/src/output/CAdjFlowIncOutput.cpp
@@ -2,7 +2,7 @@
  * \file CAdjFlowIncOutput.cpp
  * \brief Main subroutines for flow discrete adjoint output
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CAdjFlowOutput.cpp b/SU2_CFD/src/output/CAdjFlowOutput.cpp
index 947063152e7..f47197e6fc1 100644
--- a/SU2_CFD/src/output/CAdjFlowOutput.cpp
+++ b/SU2_CFD/src/output/CAdjFlowOutput.cpp
@@ -2,7 +2,7 @@
  * \file CAdjFlowOutput.cpp
  * \brief Main subroutines for flow discrete adjoint output
  * \author T. Kattmann
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CAdjHeatOutput.cpp b/SU2_CFD/src/output/CAdjHeatOutput.cpp
index 654e5ddece7..2610c5a9f13 100644
--- a/SU2_CFD/src/output/CAdjHeatOutput.cpp
+++ b/SU2_CFD/src/output/CAdjHeatOutput.cpp
@@ -2,7 +2,7 @@
  * \file CAdjHeatOutput.cpp
  * \brief Main subroutines for flow discrete adjoint output
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CBaselineOutput.cpp b/SU2_CFD/src/output/CBaselineOutput.cpp
index 4a335ace77a..37cbb2cd1b1 100644
--- a/SU2_CFD/src/output/CBaselineOutput.cpp
+++ b/SU2_CFD/src/output/CBaselineOutput.cpp
@@ -2,7 +2,7 @@
  * \file CBaselineOutput.cpp
  * \brief Main subroutines for flow discrete adjoint output
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CElasticityOutput.cpp b/SU2_CFD/src/output/CElasticityOutput.cpp
index 156d6c9a3f0..fd077ff6544 100644
--- a/SU2_CFD/src/output/CElasticityOutput.cpp
+++ b/SU2_CFD/src/output/CElasticityOutput.cpp
@@ -2,7 +2,7 @@
  * \file CElasticityOutput.cpp
  * \brief Main subroutines for FEA output
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CFVMOutput.cpp b/SU2_CFD/src/output/CFVMOutput.cpp
index 29e628ce99c..92bdf73e399 100644
--- a/SU2_CFD/src/output/CFVMOutput.cpp
+++ b/SU2_CFD/src/output/CFVMOutput.cpp
@@ -2,7 +2,7 @@
  * \file CFVMOutput.cpp
  * \brief Main subroutines for Finite Volume Method output
  * \author T. Kattmann
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -56,6 +56,10 @@ void CFVMOutput::AddCommonFVMOutputs(const CConfig *config) {
     name << "Coarse_Grid_" << iMesh;
     AddVolumeOutput(key.str(), name.str(), "MULTIGRID", "Coarse mesh");
   }
+
+  if (config->GetKind_Linear_Solver_Prec() == LINELET) {
+    AddVolumeOutput("LINELET", "Linelet", "LINELET", "Mesh lines built for the line implicit preconditioner");
+  }
 }
 
 void CFVMOutput::LoadCommonFVMOutputs(const CConfig* config, const CGeometry* geometry, unsigned long iPoint) {
@@ -76,4 +80,8 @@ void CFVMOutput::LoadCommonFVMOutputs(const CConfig* config, const CGeometry* ge
       SetVolumeOutputValue(key.str(), iPoint, geometry->CoarseGridColor(iPoint,iMesh-1));
     }
   }
+
+  if (config->GetKind_Linear_Solver_Prec() == LINELET) {
+    SetVolumeOutputValue("LINELET", iPoint, geometry->GetLineletInfo(config).lineletColor[iPoint]);
+  }
 }
diff --git a/SU2_CFD/src/output/CFlowCompFEMOutput.cpp b/SU2_CFD/src/output/CFlowCompFEMOutput.cpp
index 4a3626172fe..9a405b3acd5 100644
--- a/SU2_CFD/src/output/CFlowCompFEMOutput.cpp
+++ b/SU2_CFD/src/output/CFlowCompFEMOutput.cpp
@@ -2,7 +2,7 @@
  * \file CFlowCompFEMOutput.cpp
  * \brief Main subroutines for compressible flow output
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CFlowCompOutput.cpp b/SU2_CFD/src/output/CFlowCompOutput.cpp
index f3005aa6e81..896f0d4f03e 100644
--- a/SU2_CFD/src/output/CFlowCompOutput.cpp
+++ b/SU2_CFD/src/output/CFlowCompOutput.cpp
@@ -2,7 +2,7 @@
  * \file CFlowCompOutput.cpp
  * \brief Main subroutines for compressible flow output
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CFlowIncOutput.cpp b/SU2_CFD/src/output/CFlowIncOutput.cpp
index 6223fb14dea..c98685c5058 100644
--- a/SU2_CFD/src/output/CFlowIncOutput.cpp
+++ b/SU2_CFD/src/output/CFlowIncOutput.cpp
@@ -2,7 +2,7 @@
  * \file CFlowIncOutput.cpp
  * \brief Main subroutines for incompressible flow output
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index e5fe3a0d001..cb88b9f9f26 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -2,7 +2,7 @@
  * \file CFlowOutput.cpp
  * \brief Common functions for flow output.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -945,7 +945,7 @@ void CFlowOutput::AddHistoryOutputFields_ScalarBGS_RES(const CConfig* config) {
   }
 
   switch (config->GetKind_Trans_Model()) {    
-    case TURB_TRANS_MODEL::LM: 
+    case TURB_TRANS_MODEL::LM:
       /// DESCRIPTION: Maximum residual of the intermittency (LM model).
       AddHistoryOutput("BGS_INTERMITTENCY", "bgs[LM_1]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the intermittency (LM model).", HistoryFieldType::RESIDUAL);
       /// DESCRIPTION: Maximum residual of the momentum thickness Reynolds number (LM model).
@@ -1019,6 +1019,8 @@ void CFlowOutput::LoadHistoryData_Scalar(const CConfig* config, const CSolver* c
         SetHistoryOutputValue("BGS_INTERMITTENCY", log10(solver[TRANS_SOL]->GetRes_BGS(0)));
         SetHistoryOutputValue("BGS_RE_THETA_T", log10(solver[TRANS_SOL]->GetRes_BGS(1)));
       }
+      SetHistoryOutputValue("LINSOL_ITER_TRANS", solver[TRANS_SOL]->GetIterLinSolver());
+      SetHistoryOutputValue("LINSOL_RESIDUAL_TRANS", log10(solver[TRANS_SOL]->GetResLinSolver()));
       break;
 
     case TURB_TRANS_MODEL::NONE: break;
@@ -1059,6 +1061,7 @@ void CFlowOutput::SetVolumeOutputFields_ScalarSolution(const CConfig* config){
       AddVolumeOutput("RE_THETA_T", "LM_Re_t", "SOLUTION", "LM RE_THETA_T");
       AddVolumeOutput("INTERMITTENCY_SEP", "LM_gamma_sep", "PRIMITIVE", "LM intermittency");
       AddVolumeOutput("INTERMITTENCY_EFF", "LM_gamma_eff", "PRIMITIVE", "LM RE_THETA_T");
+      AddVolumeOutput("TURB_INDEX", "Turb_index", "PRIMITIVE", "Turbulence index");
       break;
 
     case TURB_TRANS_MODEL::NONE:
@@ -1203,7 +1206,7 @@ void CFlowOutput::LoadVolumeData_Scalar(const CConfig* config, const CSolver* co
   }
 
   if (config->GetSAParsedOptions().bc) {
-    SetVolumeOutputValue("INTERMITTENCY", iPoint, Node_Turb->GetGammaBC(iPoint));
+    SetVolumeOutputValue("INTERMITTENCY", iPoint, Node_Turb->GetIntermittencyEff(iPoint));
   }
 
   switch (config->GetKind_Trans_Model()) {    
@@ -1212,6 +1215,7 @@ void CFlowOutput::LoadVolumeData_Scalar(const CConfig* config, const CSolver* co
       SetVolumeOutputValue("RE_THETA_T", iPoint, Node_Trans->GetSolution(iPoint, 1));
       SetVolumeOutputValue("INTERMITTENCY_SEP", iPoint, Node_Trans->GetIntermittencySep(iPoint));
       SetVolumeOutputValue("INTERMITTENCY_EFF", iPoint, Node_Trans->GetIntermittencyEff(iPoint));
+      SetVolumeOutputValue("TURB_INDEX", iPoint, Node_Turb->GetTurbIndex(iPoint));
       SetVolumeOutputValue("RES_INTERMITTENCY", iPoint, trans_solver->LinSysRes(iPoint, 0));
       SetVolumeOutputValue("RES_RE_THETA_T", iPoint, trans_solver->LinSysRes(iPoint, 1));
       break;
@@ -2202,7 +2206,7 @@ void CFlowOutput::WriteForcesBreakdown(const CConfig* config, const CSolver* flo
 
   file << "\n-------------------------------------------------------------------------\n";
   file << "|    ___ _   _ ___                                                      |\n";
-  file << "|   / __| | | |_  )   Release 7.4.0 \"Blackbird\"                         |\n";
+  file << "|   / __| | | |_  )   Release 7.5.0 \"Blackbird\"                         |\n";
   file << "|   \\__ \\ |_| |/ /                                                      |\n";
   file << "|   |___/\\___//___|   Suite (Computational Fluid Dynamics Code)         |\n";
   file << "|                                                                       |\n";
@@ -2267,8 +2271,13 @@ void CFlowOutput::WriteForcesBreakdown(const CConfig* config, const CSolver* flo
         file << "Transition model: ";
         switch (Kind_Trans_Model) {
         case TURB_TRANS_MODEL::NONE: break;        
-        case TURB_TRANS_MODEL::LM:
-          file << "Langtry and Menter's transition\n";
+        case TURB_TRANS_MODEL::LM:     
+          file << "Langtry and Menter's transition";
+          if (config->GetLMParsedOptions().LM2015) {
+            file << " w/ cross-flow corrections (2015)\n";
+          } else {
+            file << " (2009)\n";
+          }
           break;
         }
       }
diff --git a/SU2_CFD/src/output/CHeatOutput.cpp b/SU2_CFD/src/output/CHeatOutput.cpp
index 10216bbc55f..dcbd2758f91 100644
--- a/SU2_CFD/src/output/CHeatOutput.cpp
+++ b/SU2_CFD/src/output/CHeatOutput.cpp
@@ -2,7 +2,7 @@
  * \file CHeatOutput.cpp
  * \brief Main subroutines for the heat solver output
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CMeshOutput.cpp b/SU2_CFD/src/output/CMeshOutput.cpp
index 25d4cf5daf9..5fb59214ec6 100644
--- a/SU2_CFD/src/output/CMeshOutput.cpp
+++ b/SU2_CFD/src/output/CMeshOutput.cpp
@@ -2,7 +2,7 @@
  * \file CMeshOutput.cpp
  * \brief Main subroutines for the heat solver output
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CMultizoneOutput.cpp b/SU2_CFD/src/output/CMultizoneOutput.cpp
index 646cce08178..3c62a950545 100644
--- a/SU2_CFD/src/output/CMultizoneOutput.cpp
+++ b/SU2_CFD/src/output/CMultizoneOutput.cpp
@@ -2,7 +2,7 @@
  * \file CMultizoneOutput.cpp
  * \brief Main subroutines for multizone output
  * \author R. Sanchez, T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CNEMOCompOutput.cpp b/SU2_CFD/src/output/CNEMOCompOutput.cpp
index 9516a08b67e..54b68bddfe8 100644
--- a/SU2_CFD/src/output/CNEMOCompOutput.cpp
+++ b/SU2_CFD/src/output/CNEMOCompOutput.cpp
@@ -2,7 +2,7 @@
  * \file CNEMOCompOutput.cpp
  * \brief Main subroutines for compressible flow output
  * \author W. Maier, R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/COutput.cpp b/SU2_CFD/src/output/COutput.cpp
index ab78e0ea735..b4abcf18724 100644
--- a/SU2_CFD/src/output/COutput.cpp
+++ b/SU2_CFD/src/output/COutput.cpp
@@ -2,7 +2,7 @@
  * \file COutput.cpp
  * \brief Main subroutines for output solver information
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/COutputFactory.cpp b/SU2_CFD/src/output/COutputFactory.cpp
index 1b65d03ba0f..9f81699fdb9 100644
--- a/SU2_CFD/src/output/COutputFactory.cpp
+++ b/SU2_CFD/src/output/COutputFactory.cpp
@@ -2,7 +2,7 @@
  * \file COutputFactory.cpp
  * \brief Main subroutines for output solver information
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CCGNSFileWriter.cpp b/SU2_CFD/src/output/filewriter/CCGNSFileWriter.cpp
index a2137298036..75a8ec4a4a9 100644
--- a/SU2_CFD/src/output/filewriter/CCGNSFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CCGNSFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CCGNSFileWriter.cpp
  * \brief Filewriter class for CGNS format.
  * \author G. Baldan
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CCSVFileWriter.cpp b/SU2_CFD/src/output/filewriter/CCSVFileWriter.cpp
index a88caa369d7..0f4a9a9a849 100644
--- a/SU2_CFD/src/output/filewriter/CCSVFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CCSVFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CCSVFileWriter.cpp
  * \brief CSV Writer output class
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CFEMDataSorter.cpp b/SU2_CFD/src/output/filewriter/CFEMDataSorter.cpp
index 80b0e2d226e..dfda9e755c6 100644
--- a/SU2_CFD/src/output/filewriter/CFEMDataSorter.cpp
+++ b/SU2_CFD/src/output/filewriter/CFEMDataSorter.cpp
@@ -2,7 +2,7 @@
  * \file CFEMDataSorter.cpp
  * \brief Datasorter class for FEM solvers.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CFVMDataSorter.cpp b/SU2_CFD/src/output/filewriter/CFVMDataSorter.cpp
index b89d7e5b5a8..01a74caa29e 100644
--- a/SU2_CFD/src/output/filewriter/CFVMDataSorter.cpp
+++ b/SU2_CFD/src/output/filewriter/CFVMDataSorter.cpp
@@ -2,7 +2,7 @@
  * \file CFVMDataSorter.cpp
  * \brief Datasorter class for FVM solvers.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CParallelDataSorter.cpp b/SU2_CFD/src/output/filewriter/CParallelDataSorter.cpp
index 21843088e7d..f86e76fa8fc 100644
--- a/SU2_CFD/src/output/filewriter/CParallelDataSorter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParallelDataSorter.cpp
@@ -2,7 +2,7 @@
  * \file CParallelDataSorter.cpp
  * \brief Datasorter base class.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CParallelFileWriter.cpp b/SU2_CFD/src/output/filewriter/CParallelFileWriter.cpp
index c89ff4313d3..d9b2931835a 100644
--- a/SU2_CFD/src/output/filewriter/CParallelFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParallelFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CParallelFileWriter.cpp
  * \brief Filewriter base class.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CParaviewBinaryFileWriter.cpp b/SU2_CFD/src/output/filewriter/CParaviewBinaryFileWriter.cpp
index 9fa2b9e6920..8fb0ccf0d6a 100644
--- a/SU2_CFD/src/output/filewriter/CParaviewBinaryFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParaviewBinaryFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CParaviewBinaryFileWriter.cpp
  * \brief Filewriter class for Paraview binary format.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CParaviewFileWriter.cpp b/SU2_CFD/src/output/filewriter/CParaviewFileWriter.cpp
index 8c21f647e35..8df6dc31543 100644
--- a/SU2_CFD/src/output/filewriter/CParaviewFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParaviewFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CParaviewFileWriter.cpp
  * \brief Filewriter class for Paraview ASCII format.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CParaviewVTMFileWriter.cpp b/SU2_CFD/src/output/filewriter/CParaviewVTMFileWriter.cpp
index 527bfb01e2d..fd4b629f2af 100644
--- a/SU2_CFD/src/output/filewriter/CParaviewVTMFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParaviewVTMFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CParaviewVTMFileWriter.cpp
  * \brief Filewriter class for Paraview binary format.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CParaviewXMLFileWriter.cpp b/SU2_CFD/src/output/filewriter/CParaviewXMLFileWriter.cpp
index 29555b9e4b7..8add80e74f3 100644
--- a/SU2_CFD/src/output/filewriter/CParaviewXMLFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParaviewXMLFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CParaviewXMLFileWriter.cpp
  * \brief Filewriter class for Paraview binary format.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CSTLFileWriter.cpp b/SU2_CFD/src/output/filewriter/CSTLFileWriter.cpp
index 23e193da3d6..036a9165fdc 100644
--- a/SU2_CFD/src/output/filewriter/CSTLFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CSTLFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CSTLFileWriter.cpp
  * \brief STL Writer output class
  * \author T. Kattmann, T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CSU2BinaryFileWriter.cpp b/SU2_CFD/src/output/filewriter/CSU2BinaryFileWriter.cpp
index 3b2993d2464..8c4ee4a375f 100644
--- a/SU2_CFD/src/output/filewriter/CSU2BinaryFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CSU2BinaryFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CSU2BinaryFileWriter.cpp
  * \brief Filewriter class SU2 native binary format.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CSU2FileWriter.cpp b/SU2_CFD/src/output/filewriter/CSU2FileWriter.cpp
index adb7053faed..2d833816f13 100644
--- a/SU2_CFD/src/output/filewriter/CSU2FileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CSU2FileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CSU2FileWriter.cpp
  * \brief Filewriter class SU2 native ASCII (CSV) format.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CSU2MeshFileWriter.cpp b/SU2_CFD/src/output/filewriter/CSU2MeshFileWriter.cpp
index 10b84b47301..43ca7cc0660 100644
--- a/SU2_CFD/src/output/filewriter/CSU2MeshFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CSU2MeshFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CSU2MeshFileWriter.cpp
  * \brief Filewriter class SU2 native mesh format.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CSurfaceFEMDataSorter.cpp b/SU2_CFD/src/output/filewriter/CSurfaceFEMDataSorter.cpp
index 17cccd4ac89..280c854c24e 100644
--- a/SU2_CFD/src/output/filewriter/CSurfaceFEMDataSorter.cpp
+++ b/SU2_CFD/src/output/filewriter/CSurfaceFEMDataSorter.cpp
@@ -2,7 +2,7 @@
  * \file CSurfaceFEMDataSorter.cpp
  * \brief Datasorter for FEM surfaces.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CSurfaceFVMDataSorter.cpp b/SU2_CFD/src/output/filewriter/CSurfaceFVMDataSorter.cpp
index 8283b8acd52..9850c795e9a 100644
--- a/SU2_CFD/src/output/filewriter/CSurfaceFVMDataSorter.cpp
+++ b/SU2_CFD/src/output/filewriter/CSurfaceFVMDataSorter.cpp
@@ -2,7 +2,7 @@
  * \file CSurfaceFVMDataSorter.cpp
  * \brief Datasorter for FVM surfaces.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CTecplotBinaryFileWriter.cpp b/SU2_CFD/src/output/filewriter/CTecplotBinaryFileWriter.cpp
index 6fa0fd7dca8..daabbac1db6 100644
--- a/SU2_CFD/src/output/filewriter/CTecplotBinaryFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CTecplotBinaryFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CTecplotBinaryFileWriter.cpp
  * \brief Filewriter class for Tecplot binary format.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CTecplotFileWriter.cpp b/SU2_CFD/src/output/filewriter/CTecplotFileWriter.cpp
index 24ec8f254ae..b3b096edc5b 100644
--- a/SU2_CFD/src/output/filewriter/CTecplotFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CTecplotFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CTecplotFileWriter.cpp
  * \brief Filewriter class for Tecplot ASCII format.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/output_physics.cpp b/SU2_CFD/src/output/output_physics.cpp
index ac181d4ab26..8c49ca91e18 100644
--- a/SU2_CFD/src/output/output_physics.cpp
+++ b/SU2_CFD/src/output/output_physics.cpp
@@ -2,7 +2,7 @@
  * \file output_physics.cpp
  * \brief Main subroutines to compute physical output quantities such as CL, CD, entropy generation, mass flow, ecc... .
  * \author S. Vitale
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/output_structure_legacy.cpp b/SU2_CFD/src/output/output_structure_legacy.cpp
index dee71a0fc70..4e4c6f94606 100644
--- a/SU2_CFD/src/output/output_structure_legacy.cpp
+++ b/SU2_CFD/src/output/output_structure_legacy.cpp
@@ -2,7 +2,7 @@
  * \file output_structure_legacy.cpp
  * \brief Main subroutines for output solver information
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/tools/CWindowingTools.cpp b/SU2_CFD/src/output/tools/CWindowingTools.cpp
index c649046ff94..92ca7d8429e 100644
--- a/SU2_CFD/src/output/tools/CWindowingTools.cpp
+++ b/SU2_CFD/src/output/tools/CWindowingTools.cpp
@@ -2,7 +2,7 @@
  * \file signal_processing_toolbox.cpp
  * \brief Signal processing tools
  * \author S. Schotthöfer
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index c604f9b8e5c..f02bfb6f092 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -2,7 +2,7 @@
  * \file python_wrapper_structure.cpp
  * \brief Driver subroutines that are used by the Python wrapper. Those routines are usually called from an external Python environment.
  * \author D. Thomas
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CAdjEulerSolver.cpp b/SU2_CFD/src/solvers/CAdjEulerSolver.cpp
index 4ad223934f8..3207ccc351c 100644
--- a/SU2_CFD/src/solvers/CAdjEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CAdjEulerSolver.cpp
@@ -2,7 +2,7 @@
  * \file CAdjEulerSolver.cpp
  * \brief Main subroutines for solving Euler adjoint problems.
  * \author F. Palacios, T. Economon, H. Kline
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -51,7 +51,7 @@ CAdjEulerSolver::CAdjEulerSolver(void) : CSolver() {
 CAdjEulerSolver::CAdjEulerSolver(CGeometry *geometry, CConfig *config, unsigned short iMesh) : CSolver() {
   unsigned long iPoint, iVertex, iMarker, jMarker;
   string text_line, mesh_filename;
-  unsigned short iDim, iVar, nLineLets;
+  unsigned short iDim, iVar;
   ifstream restart_file;
   string filename, AdjExt;
   su2double myArea_Monitored, *Normal;
@@ -170,11 +170,6 @@ CAdjEulerSolver::CAdjEulerSolver(CGeometry *geometry, CConfig *config, unsigned
       cout << "Initialize Jacobian structure (Adjoint Euler). MG level: " << iMesh <<"." << endl;
     Jacobian.Initialize(nPoint, nPointDomain, nVar, nVar, true, geometry, config);
 
-    if (config->GetKind_Linear_Solver_Prec() == LINELET) {
-      nLineLets = Jacobian.BuildLineletPreconditioner(geometry, config);
-      if (rank == MASTER_NODE) cout << "Compute linelet structure. " << nLineLets << " elements in each line (average)." << endl;
-    }
-
     if (axisymmetric) {
       Jacobian_Axisymmetric = new su2double* [nVar];
       for (iVar = 0; iVar < nVar; iVar++)
diff --git a/SU2_CFD/src/solvers/CAdjNSSolver.cpp b/SU2_CFD/src/solvers/CAdjNSSolver.cpp
index a0a0c8f5b0c..651df0675c9 100644
--- a/SU2_CFD/src/solvers/CAdjNSSolver.cpp
+++ b/SU2_CFD/src/solvers/CAdjNSSolver.cpp
@@ -2,7 +2,7 @@
  * \file CAdjNSSolver.cpp
  * \brief Main subroutines for solving Navier-Stokes adjoint problems.
  * \author F. Palacios, T. Economon, H. Kline
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -35,7 +35,7 @@ CAdjNSSolver::CAdjNSSolver(void) : CAdjEulerSolver() { }
 CAdjNSSolver::CAdjNSSolver(CGeometry *geometry, CConfig *config, unsigned short iMesh) : CAdjEulerSolver() {
   unsigned long iPoint, iVertex;
   string text_line, mesh_filename;
-  unsigned short iDim, iVar, iMarker, nLineLets;
+  unsigned short iDim, iVar, iMarker;
   ifstream restart_file;
   string filename, AdjExt;
 
@@ -141,11 +141,6 @@ CAdjNSSolver::CAdjNSSolver(CGeometry *geometry, CConfig *config, unsigned short
       cout << "Initialize Jacobian structure (Adjoint N-S). MG level: " << iMesh <<"." << endl;
     Jacobian.Initialize(nPoint, nPointDomain, nVar, nVar, true, geometry, config);
 
-    if (config->GetKind_Linear_Solver_Prec() == LINELET) {
-      nLineLets = Jacobian.BuildLineletPreconditioner(geometry, config);
-      if (rank == MASTER_NODE) cout << "Compute linelet structure. " << nLineLets << " elements in each line (average)." << endl;
-    }
-
   } else {
     if (rank == MASTER_NODE)
       cout << "Explicit scheme. No Jacobian structure (Adjoint N-S). MG level: " << iMesh <<"." << endl;
diff --git a/SU2_CFD/src/solvers/CAdjTurbSolver.cpp b/SU2_CFD/src/solvers/CAdjTurbSolver.cpp
index 99ebbc7640d..bc01707e4c2 100644
--- a/SU2_CFD/src/solvers/CAdjTurbSolver.cpp
+++ b/SU2_CFD/src/solvers/CAdjTurbSolver.cpp
@@ -2,7 +2,7 @@
  * \file CAdjTurbVariable.cpp
  * \brief Main subroutines for solving turbulent adjoint problems.
  * \author F. Palacios, A. Bueno, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -32,8 +32,6 @@ CAdjTurbSolver::CAdjTurbSolver(void) : CSolver() {}
 
 CAdjTurbSolver::CAdjTurbSolver(CGeometry *geometry, CConfig *config, unsigned short iMesh) : CSolver() {
 
-  unsigned short nLineLets;
-
   adjoint = true;
 
   nDim = geometry->GetnDim();
@@ -83,12 +81,6 @@ CAdjTurbSolver::CAdjTurbSolver(CGeometry *geometry, CConfig *config, unsigned sh
 
   /*--- Initialization of the structure of the whole Jacobian ---*/
   Jacobian.Initialize(nPoint, nPointDomain, nVar, nVar, true, geometry, config);
-
-  if (config->GetKind_Linear_Solver_Prec() == LINELET) {
-    nLineLets = Jacobian.BuildLineletPreconditioner(geometry, config);
-    if (rank == MASTER_NODE) cout << "Compute linelet structure. " << nLineLets << " elements in each line (average)." << endl;
-  }
-
   Jacobian.SetValZero();
   LinSysSol.Initialize(nPoint, nPointDomain, nVar, 0.0);
   LinSysRes.Initialize(nPoint, nPointDomain, nVar, 0.0);
diff --git a/SU2_CFD/src/solvers/CBaselineSolver.cpp b/SU2_CFD/src/solvers/CBaselineSolver.cpp
index 922247dbe79..9fb4e2dd25f 100644
--- a/SU2_CFD/src/solvers/CBaselineSolver.cpp
+++ b/SU2_CFD/src/solvers/CBaselineSolver.cpp
@@ -2,7 +2,7 @@
  * \file CBaselineSolver.cpp
  * \brief Main subroutines for CBaselineSolver class.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CBaselineSolver_FEM.cpp b/SU2_CFD/src/solvers/CBaselineSolver_FEM.cpp
index 7eabb72e90c..e4b8074bd62 100644
--- a/SU2_CFD/src/solvers/CBaselineSolver_FEM.cpp
+++ b/SU2_CFD/src/solvers/CBaselineSolver_FEM.cpp
@@ -2,7 +2,7 @@
  * \file CBaselineSolver_FEM.cpp
  * \brief Main subroutines for CBaselineSolver_FEM class.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp b/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
index c7c2c0a8da7..585532eb12a 100644
--- a/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
+++ b/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjFEASolver.cpp
  * \brief Main subroutines for solving adjoint FEM elasticity problems.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CDiscAdjMeshSolver.cpp b/SU2_CFD/src/solvers/CDiscAdjMeshSolver.cpp
index c33c6791871..3ecf8198c21 100644
--- a/SU2_CFD/src/solvers/CDiscAdjMeshSolver.cpp
+++ b/SU2_CFD/src/solvers/CDiscAdjMeshSolver.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjMeshSolver.cpp
  * \brief Main subroutines for solving the discrete adjoint mesh problem.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CDiscAdjSolver.cpp b/SU2_CFD/src/solvers/CDiscAdjSolver.cpp
index 33b97f8d42b..2698e4aefec 100644
--- a/SU2_CFD/src/solvers/CDiscAdjSolver.cpp
+++ b/SU2_CFD/src/solvers/CDiscAdjSolver.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjSolver.cpp
  * \brief Main subroutines for solving the discrete adjoint problem.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index ecf9cd26b88..38668efbd57 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -2,7 +2,7 @@
  * \file CEulerSolver.cpp
  * \brief Main subroutines for solving Finite-Volume Euler flow problems.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -65,7 +65,7 @@ CEulerSolver::CEulerSolver(CGeometry *geometry, CConfig *config,
 
   int Unst_RestartIter = 0;
   unsigned long iPoint, iMarker, counter_local = 0, counter_global = 0;
-  unsigned short iDim, nLineLets;
+  unsigned short iDim;
   su2double StaticEnergy, Density, Velocity2, Pressure, Temperature;
 
   /*--- A grid is defined as dynamic if there's rigid grid movement or grid deformation AND the problem is time domain ---*/
@@ -161,12 +161,6 @@ CEulerSolver::CEulerSolver(CGeometry *geometry, CConfig *config,
       cout << "Initialize Jacobian structure (" << description << "). MG level: " << iMesh <<"." << endl;
 
     Jacobian.Initialize(nPoint, nPointDomain, nVar, nVar, true, geometry, config, ReducerStrategy);
-
-    if (config->GetKind_Linear_Solver_Prec() == LINELET) {
-      nLineLets = Jacobian.BuildLineletPreconditioner(geometry, config);
-      if (rank == MASTER_NODE)
-        cout << "Compute linelet structure. " << nLineLets << " elements in each line (average)." << endl;
-    }
   }
   else {
     if (rank == MASTER_NODE)
@@ -2017,6 +2011,7 @@ void CEulerSolver::Source_Residual(CGeometry *geometry, CSolver **solver_contain
   const bool harmonic_balance = (config->GetTime_Marching() == TIME_MARCHING::HARMONIC_BALANCE);
   const bool windgust         = config->GetWind_Gust();
   const bool body_force       = config->GetBody_Force();
+  const bool vorticity_confinement = config->GetVorticityConfinement();
   const bool ideal_gas        = (config->GetKind_FluidModel() == STANDARD_AIR) ||
                                 (config->GetKind_FluidModel() == IDEAL_GAS);
   const bool rans             = (config->GetKind_Turb_Model() != TURB_MODEL::NONE);
@@ -2215,6 +2210,42 @@ void CEulerSolver::Source_Residual(CGeometry *geometry, CSolver **solver_contain
     END_SU2_OMP_FOR
   }
 
+  if (vorticity_confinement) {
+
+    CNumerics* second_numerics = numerics_container[SOURCE_SECOND_TERM + omp_get_thread_num()*MAX_TERMS];
+
+    /*--- calculate and set the average volume ---*/
+    const su2double AvgVolume = config->GetDomainVolume() / geometry->GetGlobal_nPointDomain();
+    second_numerics->SetAvgVolume(AvgVolume);
+
+    /*--- set vorticity magnitude as auxilliary variable ---*/
+    SU2_OMP_FOR_STAT(omp_chunk_size)
+    for (iPoint = 0; iPoint < nPoint; iPoint++) {
+      const su2double VorticityMag = max(GeometryToolbox::Norm(3, nodes->GetVorticity(iPoint)), 1e-12);
+      nodes->SetAuxVar(iPoint, 0, VorticityMag);
+    }
+    END_SU2_OMP_FOR
+
+    /*--- calculate the gradient of the vorticity magnitude (AuxVarGradient) ---*/
+    SetAuxVar_Gradient_GG(geometry, config);
+
+    SU2_OMP_FOR_DYN(omp_chunk_size)
+    for (iPoint = 0; iPoint < nPointDomain; iPoint++) {
+      second_numerics->SetPrimitive(nodes->GetPrimitive(iPoint), nullptr);
+      second_numerics->SetVorticity(nodes->GetVorticity(iPoint), nullptr);
+      second_numerics->SetAuxVarGrad(nodes->GetAuxVarGradient(iPoint), nullptr);
+      second_numerics->SetDistance(geometry->nodes->GetWall_Distance(iPoint), 0);
+      second_numerics->SetVolume(geometry->nodes->GetVolume(iPoint));
+      auto residual = second_numerics->ComputeResidual(config);
+
+      LinSysRes.AddBlock(iPoint, residual);
+
+      if (implicit) Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
+    }
+    END_SU2_OMP_FOR
+
+  }
+
   /*--- Check if a verification solution is to be computed. ---*/
 
   if ( VerificationSolution ) {
diff --git a/SU2_CFD/src/solvers/CFEASolver.cpp b/SU2_CFD/src/solvers/CFEASolver.cpp
index 016231bcc5f..83006a3037f 100644
--- a/SU2_CFD/src/solvers/CFEASolver.cpp
+++ b/SU2_CFD/src/solvers/CFEASolver.cpp
@@ -2,7 +2,7 @@
  * \file CFEASolver.cpp
  * \brief Main subroutines for solving direct FEM elasticity problems.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CFEASolverBase.cpp b/SU2_CFD/src/solvers/CFEASolverBase.cpp
index d80dfc8e8bf..8bbbf87037c 100644
--- a/SU2_CFD/src/solvers/CFEASolverBase.cpp
+++ b/SU2_CFD/src/solvers/CFEASolverBase.cpp
@@ -2,7 +2,7 @@
  * \file CFEASolverBase.cpp
  * \brief Common class template for FEA solvers
  * \author T. Dick
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp b/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
index 8779c86c322..04f103addea 100644
--- a/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
@@ -2,7 +2,7 @@
  * \file CFEM_DG_EulerSolver.cpp
  * \brief Main subroutines for solving finite element Euler flow problems
  * \author J. Alonso, E. van der Weide, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CFEM_DG_NSSolver.cpp b/SU2_CFD/src/solvers/CFEM_DG_NSSolver.cpp
index 98675bc1fa2..2e8352dd647 100644
--- a/SU2_CFD/src/solvers/CFEM_DG_NSSolver.cpp
+++ b/SU2_CFD/src/solvers/CFEM_DG_NSSolver.cpp
@@ -2,7 +2,7 @@
  * \file CFEM_DG_NSSolver.cpp
  * \brief Main subroutines for solving finite element Navier-Stokes flow problems
  * \author J. Alonso, E. van der Weide, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CGradientSmoothingSolver.cpp b/SU2_CFD/src/solvers/CGradientSmoothingSolver.cpp
index fe1e6924bf2..8dbdaeda383 100644
--- a/SU2_CFD/src/solvers/CGradientSmoothingSolver.cpp
+++ b/SU2_CFD/src/solvers/CGradientSmoothingSolver.cpp
@@ -2,7 +2,7 @@
  * \file CGradientSmoothing.cpp
  * \brief Main solver routines for the gradient smoothing problem.
  * \author T. Dick
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CHeatSolver.cpp b/SU2_CFD/src/solvers/CHeatSolver.cpp
index 76c44a21da2..d4f385f4a6c 100644
--- a/SU2_CFD/src/solvers/CHeatSolver.cpp
+++ b/SU2_CFD/src/solvers/CHeatSolver.cpp
@@ -2,7 +2,7 @@
  * \file CHeatSolver.cpp
  * \brief Main subroutines for solving the heat equation
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -26,13 +26,21 @@
  */
 
 #include "../../include/solvers/CHeatSolver.hpp"
+#include <cstddef>
 #include "../../../Common/include/toolboxes/geometry_toolbox.hpp"
+#include "../../include/solvers/CScalarSolver.inl"
 
-CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iMesh) : CSolver(),
-             flow(config->GetFluidProblem()), heat_equation(config->GetHeatProblem()) {
+/*--- Explicit instantiation of the parent class of CHeatSolver. ---*/
+template class CScalarSolver<CHeatVariable>;
 
-  /* A grid is defined as dynamic if there's rigid grid movement or grid deformation AND the problem is time domain */
-  dynamic_grid = config->GetDynamic_Grid();
+CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iMesh)
+  : CScalarSolver<CHeatVariable>(geometry, config, false),
+    flow(config->GetFluidProblem()), heat_equation(config->GetHeatProblem()) {
+
+  /*--- This solver will not run with OpenMP yet so force this to false. ---*/
+#ifdef HAVE_OMP
+  ReducerStrategy = false;
+#endif
 
   /*--- Dimension of the problem --> temperature is the only conservative variable ---*/
 
@@ -47,13 +55,6 @@ CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iM
   /*--- Define geometry constants in the solver structure ---*/
 
   nDim = geometry->GetnDim();
-  nMarker = config->GetnMarker_All();
-
-  /*--- Store the number of vertices on each marker for deallocation later ---*/
-
-  nVertex.resize(nMarker);
-  for (auto iMarker = 0u; iMarker < nMarker; iMarker++)
-    nVertex[iMarker] = geometry->nVertex[iMarker];
 
   /*--- Define some auxiliary vector related with the residual ---*/
 
@@ -80,12 +81,6 @@ CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iM
 
   if (rank == MASTER_NODE) cout << "Initialize Jacobian structure (heat equation) MG level: " << iMesh << "." << endl;
   Jacobian.Initialize(nPoint, nPointDomain, nVar, nVar, true, geometry, config);
-
-  if (config->GetKind_Linear_Solver_Prec() == LINELET) {
-    auto nLineLets = Jacobian.BuildLineletPreconditioner(geometry, config);
-    if (rank == MASTER_NODE) cout << "Compute linelet structure. " << nLineLets << " elements in each line (average)." << endl;
-  }
-
   LinSysSol.Initialize(nPoint, nPointDomain, nVar, 0.0);
   LinSysRes.Initialize(nPoint, nPointDomain, nVar, 0.0);
 
@@ -176,14 +171,21 @@ CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iM
   InitiateComms(geometry, config, SOLUTION);
   CompleteComms(geometry, config, SOLUTION);
 
-  /*--- Add the solver name (max 8 characters) ---*/
+  /*--- Store the initial CFL number for all grid points. ---*/
 
-  SolverName = "HEAT";
-}
+  const su2double CFL = config->GetCFL(MGLevel) * config->GetCFLRedCoeff_Turb();
+  SU2_OMP_FOR_STAT(omp_chunk_size)
+  for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
+    nodes->SetLocalCFL(iPoint, CFL);
+  }
+  END_SU2_OMP_FOR
+  Min_CFL_Local = CFL;
+  Max_CFL_Local = CFL;
+  Avg_CFL_Local = CFL;
 
-CHeatSolver::~CHeatSolver(void) {
+  /*--- Add the solver name (max 8 characters) ---*/
 
-  delete nodes;
+  SolverName = "HEAT";
 }
 
 void CHeatSolver::Preprocessing(CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, unsigned short iRKStep, unsigned short RunTime_EqSystem, bool Output) {
@@ -195,27 +197,7 @@ void CHeatSolver::Preprocessing(CGeometry *geometry, CSolver **solver_container,
     SetUndivided_Laplacian(geometry, config);
   }
 
-  for (auto iPoint = 0ul; iPoint < nPoint; iPoint ++) {
-
-    /*--- Initialize the residual vector ---*/
-
-    LinSysRes.SetBlock_Zero(iPoint);
-  }
-
-  /*--- Initialize the Jacobian matrices ---*/
-
-  Jacobian.SetValZero();
-
-  if (config->GetReconstructionGradientRequired()) {
-    if (config->GetKind_Gradient_Method_Recon() == GREEN_GAUSS)
-      SetSolution_Gradient_GG(geometry, config, true);
-    if (config->GetKind_Gradient_Method_Recon() == LEAST_SQUARES)
-      SetSolution_Gradient_LS(geometry, config, true);
-    if (config->GetKind_Gradient_Method_Recon() == WEIGHTED_LEAST_SQUARES)
-      SetSolution_Gradient_LS(geometry, config, true);
-  }
-  if (config->GetKind_Gradient_Method() == GREEN_GAUSS) SetSolution_Gradient_GG(geometry, config);
-  if (config->GetKind_Gradient_Method() == WEIGHTED_LEAST_SQUARES) SetSolution_Gradient_LS(geometry, config);
+  CommonPreprocessing(geometry, config, Output);
 }
 
 void CHeatSolver::Postprocessing(CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh) { }
@@ -444,63 +426,30 @@ void CHeatSolver::Viscous_Residual(CGeometry *geometry, CSolver **solver_contain
 
   CNumerics* numerics = numerics_container[VISC_TERM];
 
-  su2double laminar_viscosity, Prandtl_Lam, Prandtl_Turb, eddy_viscosity_i, eddy_viscosity_j,
-            thermal_diffusivity_i, thermal_diffusivity_j, Temp_i, Temp_j;
+  const CVariable* flow_nodes = flow ? solver_container[FLOW_SOL]->GetNodes() : nullptr;
 
-  const bool turb = ((config->GetKind_Solver() == MAIN_SOLVER::INC_RANS) || (config->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_INC_RANS));
-
-  eddy_viscosity_i = 0.0;
-  eddy_viscosity_j = 0.0;
-  laminar_viscosity = config->GetMu_ConstantND();
-  Prandtl_Lam = config->GetPrandtl_Lam();
-  Prandtl_Turb = config->GetPrandtl_Turb();
+  const su2double const_diffusivity = config->GetThermalDiffusivity();
+  const su2double pr_lam = config->GetPrandtl_Lam();
+  const su2double pr_turb = config->GetPrandtl_Turb();
 
   for (auto iEdge = 0ul; iEdge < geometry->GetnEdge(); iEdge++) {
+    su2double thermal_diffusivity_i{}, thermal_diffusivity_j{};
 
-    const auto iPoint = geometry->edges->GetNode(iEdge,0);
-    const auto jPoint = geometry->edges->GetNode(iEdge,1);
-
-    /*--- Points coordinates, and normal vector ---*/
-
-    numerics->SetCoord(geometry->nodes->GetCoord(iPoint),
-                       geometry->nodes->GetCoord(jPoint));
-    numerics->SetNormal(geometry->edges->GetNormal(iEdge));
-
-    const auto Temp_i_Grad = nodes->GetGradient(iPoint);
-    const auto Temp_j_Grad = nodes->GetGradient(jPoint);
-    numerics->SetConsVarGradient(Temp_i_Grad, Temp_j_Grad);
-
-    /*--- Primitive variables w/o reconstruction ---*/
-    Temp_i = nodes->GetTemperature(iPoint);
-    Temp_j = nodes->GetTemperature(jPoint);
-    numerics->SetTemperature(Temp_i, Temp_j);
-
-    /*--- Eddy viscosity to compute thermal conductivity ---*/
-    if (flow) {
-      if (turb) {
-        eddy_viscosity_i = solver_container[TURB_SOL]->GetNodes()->GetmuT(iPoint);
-        eddy_viscosity_j = solver_container[TURB_SOL]->GetNodes()->GetmuT(jPoint);
+    /*--- Computes the thermal diffusivity to use in the viscous numerics. ---*/
+    auto compute_thermal_diffusivity = [&](unsigned long iPoint, unsigned long jPoint) {
+      if (flow) {
+        thermal_diffusivity_i = flow_nodes->GetLaminarViscosity(iPoint) / pr_lam +
+                                flow_nodes->GetEddyViscosity(iPoint) / pr_turb;
+        thermal_diffusivity_j = flow_nodes->GetLaminarViscosity(jPoint) / pr_lam +
+                                flow_nodes->GetEddyViscosity(jPoint) / pr_turb;
+        numerics->SetDiffusionCoeff(&thermal_diffusivity_i, &thermal_diffusivity_j);
       }
-      thermal_diffusivity_i = (laminar_viscosity/Prandtl_Lam) + (eddy_viscosity_i/Prandtl_Turb);
-      thermal_diffusivity_j = (laminar_viscosity/Prandtl_Lam) + (eddy_viscosity_j/Prandtl_Turb);
-    }
-    else {
-      thermal_diffusivity_i = config->GetThermalDiffusivity();
-      thermal_diffusivity_j = config->GetThermalDiffusivity();
-    }
-
-    numerics->SetThermalDiffusivity(thermal_diffusivity_i,thermal_diffusivity_j);
-
-    /*--- Compute residual, and Jacobians ---*/
-
-    numerics->ComputeResidual(Residual, Jacobian_i, Jacobian_j, config);
-
-    /*--- Add and subtract residual, and update Jacobians ---*/
-
-    LinSysRes.SubtractBlock(iPoint, Residual);
-    LinSysRes.AddBlock(jPoint, Residual);
-
-    Jacobian.UpdateBlocksSub(iEdge, iPoint, jPoint, Jacobian_i, Jacobian_j);
+      else {
+        numerics->SetDiffusionCoeff(&const_diffusivity, &const_diffusivity);
+      }
+    };
+    /*--- Compute residual and Jacobians. ---*/
+    Viscous_Residual_impl(compute_thermal_diffusivity, iEdge, geometry, solver_container, numerics, config);
   }
 }
 
@@ -559,52 +508,14 @@ void CHeatSolver::Set_Heatflux_Areas(CGeometry *geometry, CConfig *config) {
   delete[] Local_Surface_Areas;
 }
 
-void CHeatSolver::BC_Isothermal_Wall(CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config,
-                                       unsigned short val_marker) {
-
-  unsigned long iPoint, Point_Normal;
-  su2double *Normal, *Coord_i, *Coord_j, Area, dist_ij, Twall, dTdn;
-  const bool implicit = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
-
-  const su2double laminar_viscosity = config->GetMu_ConstantND();
-  const su2double Prandtl_Lam = config->GetPrandtl_Lam();
-  const su2double thermal_diffusivity = flow ? laminar_viscosity/Prandtl_Lam : config->GetThermalDiffusivity();
-
-  //su2double Prandtl_Turb = config->GetPrandtl_Turb();
-  //laminar_viscosity = config->GetViscosity_FreeStreamND(); // TDE check for consistency for CHT
+void CHeatSolver::BC_Isothermal_Wall(CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics,
+                                     CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
 
-  string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
-
-  Twall = config->GetIsothermal_Temperature(Marker_Tag)/config->GetTemperature_Ref();
+  const auto Marker_Tag = config->GetMarker_All_TagBound(val_marker);
+  const su2double Twall = config->GetIsothermal_Temperature(Marker_Tag) / config->GetTemperature_Ref();
 
   for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
-
-    iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
-
-    if (geometry->nodes->GetDomain(iPoint)) {
-
-        Point_Normal = geometry->vertex[val_marker][iVertex]->GetNormal_Neighbor();
-
-        Normal = geometry->vertex[val_marker][iVertex]->GetNormal();
-        Area = GeometryToolbox::Norm(nDim, Normal);
-
-        Coord_i = geometry->nodes->GetCoord(iPoint);
-        Coord_j = geometry->nodes->GetCoord(Point_Normal);
-        dist_ij = 0;
-        for (auto iDim = 0u; iDim < nDim; iDim++)
-          dist_ij += (Coord_j[iDim]-Coord_i[iDim])*(Coord_j[iDim]-Coord_i[iDim]);
-        dist_ij = sqrt(dist_ij);
-
-        dTdn = -(nodes->GetTemperature(Point_Normal) - Twall)/dist_ij;
-
-        Res_Visc[0] = thermal_diffusivity*dTdn*Area;
-
-        if(implicit)
-          Jacobian_i[0][0] = -thermal_diffusivity/dist_ij * Area;
-
-        LinSysRes.SubtractBlock(iPoint, Res_Visc);
-        Jacobian.SubtractBlock2Diag(iPoint, Jacobian_i);
-    }
+    IsothermalBoundaryCondition(geometry, solver_container[FLOW_SOL], config, val_marker, iVertex, Twall);
   }
 }
 
@@ -619,19 +530,13 @@ void CHeatSolver::BC_HeatFlux_Wall(CGeometry* geometry, CSolver** solver_contain
 
   for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
     const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
+    if (!geometry->nodes->GetDomain(iPoint)) continue;
 
-    if (geometry->nodes->GetDomain(iPoint)) {
-      const auto Normal = geometry->vertex[val_marker][iVertex]->GetNormal();
-      const auto Area = GeometryToolbox::Norm(nDim, Normal);
-
-      Res_Visc[0] = 0.0;
-
-      Res_Visc[0] = Wall_HeatFlux * Area;
-
-      /*--- Viscous contribution to the residual at the wall ---*/
-
-      LinSysRes.SubtractBlock(iPoint, Res_Visc);
-    }
+    /*--- Viscous contribution to the residual at the wall. ---*/
+    const auto* Normal = geometry->vertex[val_marker][iVertex]->GetNormal();
+    const su2double Area = GeometryToolbox::Norm(nDim, Normal);
+    const su2double flux = Wall_HeatFlux * Area;
+    LinSysRes(iPoint, 0) -= flux;
   }
 }
 
@@ -639,23 +544,16 @@ void CHeatSolver::BC_Inlet(CGeometry *geometry, CSolver **solver_container,
                             CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
 
   unsigned short iDim;
-  unsigned long iVertex, iPoint, Point_Normal;
+  unsigned long iVertex, iPoint;
   su2double Vel_Mag, *V_inlet, *V_domain;
 
-  bool viscous              = config->GetViscous();
-  bool implicit             = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
-  string Marker_Tag         = config->GetMarker_All_TagBound(val_marker);
+  const bool viscous = config->GetViscous();
+  const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+  const auto Marker_Tag = config->GetMarker_All_TagBound(val_marker);
 
   su2double Normal[MAXNDIM];
 
-  su2double *Coord_i, *Coord_j, Area, dist_ij, laminar_viscosity, thermal_diffusivity, Twall, dTdn, Prandtl_Lam;
-  //su2double Prandtl_Turb;
-  Prandtl_Lam = config->GetPrandtl_Lam();
-//  Prandtl_Turb = config->GetPrandtl_Turb();
-  laminar_viscosity = config->GetMu_ConstantND();
-  //laminar_viscosity = config->GetViscosity_FreeStreamND(); //TDE check for consistency with CHT
-
-  Twall = config->GetTemperature_FreeStreamND();
+  const su2double Twall = config->GetTemperature_FreeStreamND();
 
   for (iVertex = 0; iVertex < geometry->nVertex[val_marker]; iVertex++) {
 
@@ -666,7 +564,7 @@ void CHeatSolver::BC_Inlet(CGeometry *geometry, CSolver **solver_container,
       geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
       for (iDim = 0; iDim < nDim; iDim++) Normal[iDim] = -Normal[iDim];
 
-      if(flow) {
+      if (flow) {
 
         /*--- Normal vector for this vertex (negate for outward convention) ---*/
 
@@ -710,33 +608,7 @@ void CHeatSolver::BC_Inlet(CGeometry *geometry, CSolver **solver_container,
       /*--- Viscous contribution ---*/
 
       if (viscous) {
-
-        Point_Normal = geometry->vertex[val_marker][iVertex]->GetNormal_Neighbor();
-
-        geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
-        Area = GeometryToolbox::Norm(nDim, Normal);
-
-        Coord_i = geometry->nodes->GetCoord(iPoint);
-        Coord_j = geometry->nodes->GetCoord(Point_Normal);
-        dist_ij = 0;
-        for (iDim = 0; iDim < nDim; iDim++)
-          dist_ij += (Coord_j[iDim]-Coord_i[iDim])*(Coord_j[iDim]-Coord_i[iDim]);
-        dist_ij = sqrt(dist_ij);
-
-        dTdn = -(nodes->GetTemperature(Point_Normal) - Twall)/dist_ij;
-
-        thermal_diffusivity = laminar_viscosity/Prandtl_Lam;
-
-        Res_Visc[0] = thermal_diffusivity*dTdn*Area;
-
-        if(implicit) {
-
-          Jacobian_i[0][0] = -thermal_diffusivity/dist_ij * Area;
-        }
-        /*--- Viscous contribution to the residual at the wall ---*/
-
-        LinSysRes.SubtractBlock(iPoint, Res_Visc);
-        Jacobian.SubtractBlock2Diag(iPoint, Jacobian_i);
+        IsothermalBoundaryCondition(geometry, solver_container[FLOW_SOL], config, val_marker, iVertex, Twall);
       }
     }
   }
@@ -874,20 +746,6 @@ void CHeatSolver::BC_ConjugateHeat_Interface(CGeometry *geometry, CSolver **solv
   }
 }
 
-void CHeatSolver::BC_Periodic(CGeometry* geometry, CSolver** solver_container, CNumerics* numerics,
-                                           CConfig* config) {
-  /*--- Complete residuals for periodic boundary conditions. We loop over
-   the periodic BCs in matching pairs so that, in the event that there are
-   adjacent periodic markers, the repeated points will have their residuals
-   accumulated corectly during the communications. For implicit calculations
-   the Jacobians and linear system are also correctly adjusted here. ---*/
-
-  for (unsigned short iPeriodic = 1; iPeriodic <= config->GetnMarker_Periodic() / 2; iPeriodic++) {
-    InitiatePeriodicComms(geometry, config, iPeriodic, PERIODIC_RESIDUAL);
-    CompletePeriodicComms(geometry, config, iPeriodic, PERIODIC_RESIDUAL);
-  }
-}
-
 void CHeatSolver::Heat_Fluxes(CGeometry *geometry, CSolver **solver_container, CConfig *config) {
 
   unsigned long iPointNormal;
@@ -1004,339 +862,215 @@ void CHeatSolver::Heat_Fluxes(CGeometry *geometry, CSolver **solver_container, C
 void CHeatSolver::SetTime_Step(CGeometry *geometry, CSolver **solver_container, CConfig *config,
                                unsigned short iMesh, unsigned long Iteration) {
 
-  unsigned long iPoint, jPoint;
-  su2double Area, Vol, laminar_viscosity, eddy_viscosity, thermal_diffusivity, Prandtl_Lam, Prandtl_Turb, Mean_ProjVel, Mean_BetaInc2, Mean_DensityInc, Mean_SoundSpeed, Lambda;
-  su2double Global_Delta_Time = 0.0, Global_Delta_UnstTimeND = 0.0, Local_Delta_Time = 0.0, Local_Delta_Time_Inv, Local_Delta_Time_Visc, CFL_Reduction, K_v = 0.25;
-  const su2double* Normal;
-
-  const bool turb = ((config->GetKind_Solver() == MAIN_SOLVER::INC_RANS) || (config->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_INC_RANS));
-  const bool dual_time = ((config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
-                    (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND));
-  const bool implicit = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
-
-  eddy_viscosity    = 0.0;
-  laminar_viscosity = config->GetMu_ConstantND();
-  Prandtl_Lam = config->GetPrandtl_Lam();
-  Prandtl_Turb = config->GetPrandtl_Turb();
+  const bool implicit      = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+  const bool time_stepping = (config->GetTime_Marching() == TIME_MARCHING::TIME_STEPPING);
+  const bool dual_time     = (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
+                             (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND);
+  const su2double K_v = 0.25;
 
-  thermal_diffusivity = config->GetThermalDiffusivity();
+  const su2double prandtl_lam = config->GetPrandtl_Lam();
+  const su2double prandtl_turb = config->GetPrandtl_Turb();
+  const su2double constant_thermal_diffusivity = config->GetThermalDiffusivity();
 
-  /*--- Compute spectral radius based on thermal conductivity ---*/
+  const CVariable* flow_nodes = solver_container[FLOW_SOL] ? solver_container[FLOW_SOL]->GetNodes() : nullptr;
 
-  Min_Delta_Time = 1.E30; Max_Delta_Time = 0.0;
-  CFL_Reduction = config->GetCFLRedCoeff_Turb();
+  /*--- Init thread-shared variables to compute min/max values.
+   *    Critical sections are used for this instead of reduction
+   *    clauses for compatibility with OpenMP 2.0 (Windows...). ---*/
+  BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
+    Min_Delta_Time = 1e30;
+    Max_Delta_Time = 0.0;
+    Global_Delta_UnstTimeND = 1e30;
+  } END_SU2_OMP_SAFE_GLOBAL_ACCESS
 
-  for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
-    nodes->SetMax_Lambda_Inv(iPoint,0.0);
-    nodes->SetMax_Lambda_Visc(iPoint,0.0);
-  }
+  /*--- Loop domain points. ---*/
 
-  /*--- Loop interior edges ---*/
-
-  for (auto iEdge = 0ul; iEdge < geometry->GetnEdge(); iEdge++) {
+  SU2_OMP_FOR_DYN(omp_chunk_size)
+  for (auto iPoint = 0ul; iPoint < nPointDomain; ++iPoint) {
 
-    iPoint = geometry->edges->GetNode(iEdge,0);
-    jPoint = geometry->edges->GetNode(iEdge,1);
+    /*--- Set maximum eigenvalues to zero. ---*/
 
-    /*--- get the edge's normal vector to compute the edge's area ---*/
-    Normal = geometry->edges->GetNormal(iEdge);
-    Area = GeometryToolbox::Norm(nDim, Normal);
+    nodes->SetMax_Lambda_Visc(iPoint, 0.0);
 
-    /*--- Inviscid contribution ---*/
-
-    if (flow) {
-      Mean_ProjVel = 0.5 * (solver_container[FLOW_SOL]->GetNodes()->GetProjVel(iPoint,Normal) + solver_container[FLOW_SOL]->GetNodes()->GetProjVel(jPoint,Normal));
-      Mean_BetaInc2 = 0.5 * (solver_container[FLOW_SOL]->GetNodes()->GetBetaInc2(iPoint) + solver_container[FLOW_SOL]->GetNodes()->GetBetaInc2(jPoint));
-      Mean_DensityInc = 0.5 * (solver_container[FLOW_SOL]->GetNodes()->GetDensity(iPoint) + solver_container[FLOW_SOL]->GetNodes()->GetDensity(jPoint));
-      Mean_SoundSpeed = sqrt(Mean_ProjVel*Mean_ProjVel + (Mean_BetaInc2/Mean_DensityInc)*Area*Area);
-
-      Lambda = fabs(Mean_ProjVel) + Mean_SoundSpeed;
-      if (geometry->nodes->GetDomain(iPoint)) nodes->AddMax_Lambda_Inv(iPoint, Lambda);
-      if (geometry->nodes->GetDomain(jPoint)) nodes->AddMax_Lambda_Inv(jPoint, Lambda);
-    }
+    /*--- Loop over the neighbors of point i. ---*/
 
-    /*--- Viscous contribution ---*/
+    for (unsigned short iNeigh = 0; iNeigh < geometry->nodes->GetnPoint(iPoint); ++iNeigh) {
+      const auto jPoint = geometry->nodes->GetPoint(iPoint,iNeigh);
+      const auto iEdge = geometry->nodes->GetEdge(iPoint,iNeigh);
+      const auto* Normal = geometry->edges->GetNormal(iEdge);
+      const su2double Area2 = GeometryToolbox::SquaredNorm(nDim, Normal);
 
-    thermal_diffusivity = config->GetThermalDiffusivity();
-    if(flow) {
-      if(turb) {
-        eddy_viscosity = solver_container[TURB_SOL]->GetNodes()->GetmuT(iPoint);
+      if (flow) {
+        const su2double laminar_viscosity = 0.5 * (flow_nodes->GetLaminarViscosity(iPoint) +
+                                                   flow_nodes->GetLaminarViscosity(jPoint));
+        const su2double eddy_viscosity = 0.5 * (flow_nodes->GetEddyViscosity(iPoint) +
+                                                flow_nodes->GetEddyViscosity(jPoint));
+
+        const su2double thermal_diffusivity = laminar_viscosity / prandtl_lam + eddy_viscosity / prandtl_turb;
+        nodes->AddMax_Lambda_Visc(iPoint, thermal_diffusivity * Area2);
+      } else {
+        nodes->AddMax_Lambda_Visc(iPoint, constant_thermal_diffusivity * Area2);
       }
-
-      thermal_diffusivity = laminar_viscosity/Prandtl_Lam + eddy_viscosity/Prandtl_Turb;
     }
-
-    Lambda = thermal_diffusivity*Area*Area;
-    if (geometry->nodes->GetDomain(iPoint)) nodes->AddMax_Lambda_Visc(iPoint, Lambda);
-    if (geometry->nodes->GetDomain(jPoint)) nodes->AddMax_Lambda_Visc(jPoint, Lambda);
-
   }
+  END_SU2_OMP_FOR
 
   /*--- Loop boundary edges ---*/
 
-  for (auto iMarker = 0u; iMarker < geometry->GetnMarker(); iMarker++) {
-    for (auto iVertex = 0ul; iVertex < geometry->GetnVertex(iMarker); iVertex++) {
-
-      /*--- Point identification, Normal vector and area ---*/
+  for (unsigned short iMarker = 0; iMarker < geometry->GetnMarker(); iMarker++) {
+    if ((config->GetMarker_All_KindBC(iMarker) != INTERNAL_BOUNDARY) &&
+        (config->GetMarker_All_KindBC(iMarker) != NEARFIELD_BOUNDARY) &&
+        (config->GetMarker_All_KindBC(iMarker) != PERIODIC_BOUNDARY)) {
 
-      iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
-      Normal = geometry->vertex[iMarker][iVertex]->GetNormal();
-      Area = GeometryToolbox::Norm(nDim, Normal);
+      SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
+      for (auto iVertex = 0ul; iVertex < geometry->GetnVertex(iMarker); iVertex++) {
 
-      /*--- Inviscid contribution ---*/
+        /*--- Point identification, Normal vector and area ---*/
 
-      if (flow) {
-        Mean_ProjVel = solver_container[FLOW_SOL]->GetNodes()->GetProjVel(iPoint, Normal);
-        Mean_BetaInc2 = solver_container[FLOW_SOL]->GetNodes()->GetBetaInc2(iPoint);
-        Mean_DensityInc = solver_container[FLOW_SOL]->GetNodes()->GetDensity(iPoint);
-        Mean_SoundSpeed = sqrt(Mean_ProjVel*Mean_ProjVel + (Mean_BetaInc2/Mean_DensityInc)*Area*Area);
+        const auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
 
-        Lambda = fabs(Mean_ProjVel) + Mean_SoundSpeed;
-        if (geometry->nodes->GetDomain(iPoint)) nodes->AddMax_Lambda_Inv(iPoint, Lambda);
-      }
+        if (!geometry->nodes->GetDomain(iPoint)) continue;
 
-      /*--- Viscous contribution ---*/
+        const auto* Normal = geometry->vertex[iMarker][iVertex]->GetNormal();
+        const su2double Area2 = GeometryToolbox::SquaredNorm(nDim, Normal);
 
-      thermal_diffusivity = config->GetThermalDiffusivity();
-      if(flow) {
-        if(turb) {
-          eddy_viscosity = solver_container[TURB_SOL]->GetNodes()->GetmuT(iPoint);
+        if (flow) {
+          const su2double thermal_diffusivity = flow_nodes->GetLaminarViscosity(iPoint) / prandtl_lam +
+                                                flow_nodes->GetEddyViscosity(iPoint) / prandtl_turb;
+          nodes->AddMax_Lambda_Visc(iPoint, thermal_diffusivity * Area2);
+        } else {
+          nodes->AddMax_Lambda_Visc(iPoint, constant_thermal_diffusivity * Area2);
         }
-
-        thermal_diffusivity = laminar_viscosity/Prandtl_Lam + eddy_viscosity/Prandtl_Turb;
       }
-
-      Lambda = thermal_diffusivity*Area*Area;
-      if (geometry->nodes->GetDomain(iPoint)) nodes->AddMax_Lambda_Visc(iPoint, Lambda);
-
+      END_SU2_OMP_FOR
     }
   }
 
-  /*--- Each element uses their own speed, steady state simulation ---*/
-
-  for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
-
-    Vol = geometry->nodes->GetVolume(iPoint);
-
-    if (Vol != 0.0) {
-
-      if(flow) {
-        Local_Delta_Time_Inv = config->GetCFL(iMesh)*Vol / nodes->GetMax_Lambda_Inv(iPoint);
-        Local_Delta_Time_Visc = config->GetCFL(iMesh)*K_v*Vol*Vol/ nodes->GetMax_Lambda_Visc(iPoint);
-      }
-      else {
-        Local_Delta_Time_Inv = config->GetMax_DeltaTime();
-        Local_Delta_Time_Visc = config->GetCFL(iMesh)*K_v*Vol*Vol/ nodes->GetMax_Lambda_Visc(iPoint);
-        //Local_Delta_Time_Visc = 100.0*K_v*Vol*Vol/ nodes->GetMax_Lambda_Visc(iPoint);
-      }
+  /*--- Each element uses their own speed, steady state simulation. ---*/
+  {
+    /*--- Thread-local variables for min/max reduction. ---*/
+    su2double minDt = 1e30, maxDt = 0.0;
 
-      /*--- Time step setting method ---*/
+    SU2_OMP_FOR_(schedule(static,omp_chunk_size) SU2_NOWAIT)
+    for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
 
-      if (config->GetKind_TimeStep_Heat() == BYFLOW && flow) {
-        Local_Delta_Time = solver_container[FLOW_SOL]->GetNodes()->GetDelta_Time(iPoint);
-      }
-      else if (config->GetKind_TimeStep_Heat() == MINIMUM) {
-        Local_Delta_Time = min(Local_Delta_Time_Inv, Local_Delta_Time_Visc);
-      }
-      else if (config->GetKind_TimeStep_Heat() == CONVECTIVE) {
-        Local_Delta_Time = Local_Delta_Time_Inv;
-      }
-      else if (config->GetKind_TimeStep_Heat() == VISCOUS) {
-        Local_Delta_Time = Local_Delta_Time_Visc;
+      su2double local_delta_time = 0.0;
+
+      const su2double Vol = geometry->nodes->GetVolume(iPoint);
+      if (Vol != 0.0) {
+        local_delta_time = nodes->GetLocalCFL(iPoint) * K_v * pow(Vol, 2) / nodes->GetMax_Lambda_Visc(iPoint);
+        if (flow) {
+          switch (config->GetKind_TimeStep_Heat()) {
+            case BYFLOW:
+            case CONVECTIVE:
+              local_delta_time = flow_nodes->GetDelta_Time(iPoint);
+              break;
+            case MINIMUM:
+              local_delta_time = min(local_delta_time, flow_nodes->GetDelta_Time(iPoint));
+              break;
+            case VISCOUS:
+              break;
+            default:
+              break;
+          }
+        }
+        minDt = min(minDt, local_delta_time);
+        maxDt = max(maxDt, local_delta_time);
       }
-
-      /*--- Min-Max-Logic ---*/
-
-      Global_Delta_Time = min(Global_Delta_Time, Local_Delta_Time);
-      Min_Delta_Time = min(Min_Delta_Time, Local_Delta_Time);
-      Max_Delta_Time = max(Max_Delta_Time, Local_Delta_Time);
-      if (Local_Delta_Time > config->GetMax_DeltaTime())
-        Local_Delta_Time = config->GetMax_DeltaTime();
-
-      nodes->SetDelta_Time(iPoint,CFL_Reduction*Local_Delta_Time);
+      nodes->SetDelta_Time(iPoint, local_delta_time);
     }
-    else {
-      nodes->SetDelta_Time(iPoint,0.0);
+    END_SU2_OMP_FOR
+    /*--- Min/max over threads. ---*/
+    SU2_OMP_CRITICAL
+    {
+      Min_Delta_Time = min(Min_Delta_Time, minDt);
+      Max_Delta_Time = max(Max_Delta_Time, maxDt);
+      Global_Delta_Time = Min_Delta_Time;
     }
+    END_SU2_OMP_CRITICAL
   }
 
-  /*--- Compute the max and the min dt (in parallel) ---*/
-  if (config->GetComm_Level() == COMM_FULL) {
-#ifdef HAVE_MPI
-    su2double rbuf_time, sbuf_time;
-    sbuf_time = Min_Delta_Time;
-    SU2_MPI::Reduce(&sbuf_time, &rbuf_time, 1, MPI_DOUBLE, MPI_MIN, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Bcast(&rbuf_time, 1, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    Min_Delta_Time = rbuf_time;
-
-    sbuf_time = Max_Delta_Time;
-    SU2_MPI::Reduce(&sbuf_time, &rbuf_time, 1, MPI_DOUBLE, MPI_MAX, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Bcast(&rbuf_time, 1, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    Max_Delta_Time = rbuf_time;
-#endif
-  }
+  /*--- Compute the min/max dt (in parallel, now over mpi ranks). ---*/
 
-  /*--- For exact time solution use the minimum delta time of the whole mesh ---*/
-  if (config->GetTime_Marching() == TIME_MARCHING::TIME_STEPPING) {
-#ifdef HAVE_MPI
-    su2double rbuf_time, sbuf_time;
-    sbuf_time = Global_Delta_Time;
-    SU2_MPI::Reduce(&sbuf_time, &rbuf_time, 1, MPI_DOUBLE, MPI_MIN, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Bcast(&rbuf_time, 1, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    Global_Delta_Time = rbuf_time;
-#endif
-    for (iPoint = 0; iPoint < nPointDomain; iPoint++)
-      nodes->SetDelta_Time(iPoint,Global_Delta_Time);
-  }
+  BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
+    if (config->GetComm_Level() == COMM_FULL) {
+      su2double rbuf_time;
+      SU2_MPI::Allreduce(&Min_Delta_Time, &rbuf_time, 1, MPI_DOUBLE, MPI_MIN, SU2_MPI::GetComm());
+      Min_Delta_Time = rbuf_time;
 
-  /*--- Recompute the unsteady time step for the dual time strategy
-   if the unsteady CFL is diferent from 0 ---*/
-  if ((dual_time) && (Iteration == 0) && (config->GetUnst_CFL() != 0.0) && (iMesh == MESH_0)) {
-    Global_Delta_UnstTimeND = config->GetUnst_CFL()*Global_Delta_Time/config->GetCFL(iMesh);
-
-#ifdef HAVE_MPI
-    su2double rbuf_time, sbuf_time;
-    sbuf_time = Global_Delta_UnstTimeND;
-    SU2_MPI::Reduce(&sbuf_time, &rbuf_time, 1, MPI_DOUBLE, MPI_MIN, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Bcast(&rbuf_time, 1, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    Global_Delta_UnstTimeND = rbuf_time;
-#endif
-    config->SetDelta_UnstTimeND(Global_Delta_UnstTimeND);
-  }
+      SU2_MPI::Allreduce(&Max_Delta_Time, &rbuf_time, 1, MPI_DOUBLE, MPI_MAX, SU2_MPI::GetComm());
+      Max_Delta_Time = rbuf_time;
+    }
+  } END_SU2_OMP_SAFE_GLOBAL_ACCESS
 
-  /*--- The pseudo local time (explicit integration) cannot be greater than the physical time ---*/
-  if (dual_time)
-    for (iPoint = 0; iPoint < nPointDomain; iPoint++) {
-      if (!implicit) {
-        cout << "Using unsteady time: " << config->GetDelta_UnstTimeND() << endl;
-        Local_Delta_Time = min((2.0/3.0)*config->GetDelta_UnstTimeND(), nodes->GetDelta_Time(iPoint));
-        nodes->SetDelta_Time(iPoint,Local_Delta_Time);
-      }
-  }
-}
+  /*--- For exact time solution use the minimum delta time of the whole mesh. ---*/
+  if (time_stepping) {
 
-void CHeatSolver::ExplicitEuler_Iteration(CGeometry *geometry, CSolver **solver_container, CConfig *config) {
+    /*--- If the unsteady CFL is set to zero, it uses the defined unsteady time step,
+     *    otherwise it computes the time step based on the unsteady CFL. ---*/
 
-  su2double *local_Residual, *local_Res_TruncError, Vol, Delta, Res;
+    BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS
+    {
+      if (config->GetUnst_CFL() == 0.0) {
+        Global_Delta_Time = config->GetDelta_UnstTime();
+      }
+      else {
+        Global_Delta_Time = Min_Delta_Time;
+      }
+      Max_Delta_Time = Global_Delta_Time;
 
-  SetResToZero();
+      config->SetDelta_UnstTimeND(Global_Delta_Time);
+    }
+    END_SU2_OMP_SAFE_GLOBAL_ACCESS
 
-  /*--- Update the solution ---*/
+    /*--- Sets the regular CFL equal to the unsteady CFL. ---*/
 
-  for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
-    Vol = geometry->nodes->GetVolume(iPoint);
-    Delta = nodes->GetDelta_Time(iPoint) / Vol;
-
-    local_Res_TruncError = nodes->GetResTruncError(iPoint);
-    local_Residual = LinSysRes.GetBlock(iPoint);
-
-    if (!config->GetContinuous_Adjoint()) {
-      for (auto iVar = 0u; iVar < nVar; iVar++) {
-        Res = local_Residual[iVar] + local_Res_TruncError[iVar];
-        nodes->AddSolution(iPoint,iVar, -Res*Delta);
-        Residual_RMS[iVar] += Res*Res;
-        AddRes_Max(iVar, fabs(Res), geometry->nodes->GetGlobalIndex(iPoint), geometry->nodes->GetCoord(iPoint));
-      }
+    SU2_OMP_FOR_STAT(omp_chunk_size)
+    for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
+      nodes->SetLocalCFL(iPoint, config->GetUnst_CFL());
+      nodes->SetDelta_Time(iPoint, Global_Delta_Time);
     }
+    END_SU2_OMP_FOR
 
   }
 
-  /*--- MPI solution ---*/
-
-  InitiateComms(geometry, config, SOLUTION);
-  CompleteComms(geometry, config, SOLUTION);
-
-  /*--- Compute the root mean square residual ---*/
-
-  SetResidual_RMS(geometry, config);
-
-}
-
+  /*--- Recompute the unsteady time step for the dual time strategy if the unsteady CFL is diferent from 0.
+    * This is only done once because in dual time the time step cannot be variable. ---*/
 
-void CHeatSolver::ImplicitEuler_Iteration(CGeometry *geometry, CSolver **solver_container, CConfig *config) {
+  if (dual_time && (Iteration == config->GetRestart_Iter()) && (config->GetUnst_CFL() != 0.0) && (iMesh == MESH_0)) {
 
-  /*--- Set maximum residual to zero ---*/
+    /*--- Thread-local variable for reduction. ---*/
+    su2double glbDtND = 1e30;
 
-  SetResToZero();
-
-  /*--- Build implicit system ---*/
-
-  for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
-
-    /*--- Read the residual ---*/
-
-    su2double* local_Res_TruncError = nodes->GetResTruncError(iPoint);
-
-    /*--- Modify matrix diagonal to assure diagonal dominance ---*/
-
-    const su2double dt = nodes->GetDelta_Time(iPoint);
-    if (dt != 0.0) {
-      /*--- For nodes on periodic boundaries, add the respective partner volume. ---*/
-      // Identical for flow and heat
-      const su2double Vol = geometry->nodes->GetVolume(iPoint) + geometry->nodes->GetPeriodicVolume(iPoint);
-      Jacobian.AddVal2Diag(iPoint, Vol / dt);
-
-    } else {
-      Jacobian.SetVal2Diag(iPoint, 1.0);
-      for (auto iVar = 0u; iVar < nVar; iVar++) {
-        const auto total_index = iPoint*nVar + iVar;
-        LinSysRes[total_index] = 0.0;
-        local_Res_TruncError[iVar] = 0.0;
-      }
-    }
-
-    /*--- Right hand side of the system (-Residual) and initial guess (x = 0) ---*/
-
-    for (auto iVar = 0; iVar < nVar; iVar++) {
-      const auto total_index = iPoint*nVar+iVar;
-      LinSysRes[total_index] = - (LinSysRes[total_index] + local_Res_TruncError[iVar]);
-      LinSysSol[total_index] = 0.0;
-      Residual_RMS[iVar] += LinSysRes[total_index]*LinSysRes[total_index];
-      AddRes_Max(iVar, fabs(LinSysRes[total_index]), geometry->nodes->GetGlobalIndex(iPoint), geometry->nodes->GetCoord(iPoint));
+    SU2_OMP_FOR_(schedule(static,omp_chunk_size) SU2_NOWAIT)
+    for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
+      glbDtND = min(glbDtND, config->GetUnst_CFL()*Global_Delta_Time / nodes->GetLocalCFL(iPoint));
     }
-  }
+    END_SU2_OMP_FOR
+    SU2_OMP_CRITICAL
+    Global_Delta_UnstTimeND = min(Global_Delta_UnstTimeND, glbDtND);
+    END_SU2_OMP_CRITICAL
 
-  /*--- Initialize residual and solution at the ghost points ---*/
+    BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS
+    {
+      SU2_MPI::Allreduce(&Global_Delta_UnstTimeND, &glbDtND, 1, MPI_DOUBLE, MPI_MIN, SU2_MPI::GetComm());
+      Global_Delta_UnstTimeND = glbDtND;
 
-  for (auto iPoint = nPointDomain; iPoint < nPoint; iPoint++) {
-    for (auto iVar = 0u; iVar < nVar; iVar++) {
-      const auto total_index = iPoint*nVar + iVar;
-      LinSysRes[total_index] = 0.0;
-      LinSysSol[total_index] = 0.0;
+      config->SetDelta_UnstTimeND(Global_Delta_UnstTimeND);
     }
+    END_SU2_OMP_SAFE_GLOBAL_ACCESS
   }
 
-  /*--- Solve or smooth the linear system ---*/
-
-  auto iter = System.Solve(Jacobian, LinSysRes, LinSysSol, geometry, config);
-
-  /*--- Store the the number of iterations of the linear solver ---*/
-  SetIterLinSolver(iter);
-
-  /*--- Store the value of the residual. ---*/
-  SetResLinSolver(System.GetResidual());
+  /*--- The pseudo local time (explicit integration) cannot be greater than the physical time ---*/
 
-  for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
-    for (auto iVar = 0u; iVar < nVar; iVar++) {
-      nodes->AddSolution(iPoint,iVar, LinSysSol[iPoint*nVar+iVar]);
+  if (dual_time && !implicit) {
+    SU2_OMP_FOR_STAT(omp_chunk_size)
+    for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
+      su2double dt = min((2.0/3.0)*config->GetDelta_UnstTimeND(), nodes->GetDelta_Time(iPoint));
+      nodes->SetDelta_Time(iPoint, dt);
     }
+    END_SU2_OMP_FOR
   }
-
-  /*--- Synchronize the solution between master and passive periodic nodes after the linear solve. ---*/
-  for (unsigned short iPeriodic = 1; iPeriodic <= config->GetnMarker_Periodic() / 2; iPeriodic++) {
-    InitiatePeriodicComms(geometry, config, iPeriodic, PERIODIC_IMPLICIT);
-    CompletePeriodicComms(geometry, config, iPeriodic, PERIODIC_IMPLICIT);
-  }
-
-  /*--- MPI solution ---*/
-
-  InitiateComms(geometry, config, SOLUTION);
-  CompleteComms(geometry, config, SOLUTION);
-
-  /*--- Compute the root mean square residual ---*/
-
-  SetResidual_RMS(geometry, config);
-
 }
 
 void CHeatSolver::SetInitialCondition(CGeometry **geometry, CSolver ***solver_container, CConfig *config, unsigned long TimeIter) {
@@ -1388,67 +1122,57 @@ void CHeatSolver::SetInitialCondition(CGeometry **geometry, CSolver ***solver_co
 
 void CHeatSolver::SetResidual_DualTime(CGeometry *geometry, CSolver **solver_container, CConfig *config,
                                        unsigned short iRKStep, unsigned short iMesh, unsigned short RunTime_EqSystem) {
-
-  /*--- Local variables ---*/
-
-  const su2double *U_time_n, *U_time_nP1, *U_time_nM1;
-  su2double Volume_nP1;
-
+  if (flow) {
+    CScalarSolver<CHeatVariable>::SetResidual_DualTime(geometry, solver_container, config, iRKStep, iMesh, RunTime_EqSystem);
+    return;
+  }
   const bool first_order  = (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST);
   const bool second_order = (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND);
-  const bool implicit = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
+  const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
 
   /*--- Store the physical time step ---*/
 
   const su2double TimeStep = config->GetDelta_UnstTimeND();
 
-  /*--- Compute the dual time-stepping source term for static meshes ---*/
+  /*--- Compute the dual time-stepping source term ---*/
+  /*--- Loop over all nodes (excluding halos) ---*/
 
-  if (!dynamic_grid) {
+  AD::StartNoSharedReading();
 
-    /*--- Loop over all nodes (excluding halos) ---*/
-
-    for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
-
-      /*--- Retrieve the solution at time levels n-1, n, and n+1. Note that
-       we are currently iterating on U^n+1 and that U^n & U^n-1 are fixed,
-       previous solutions that are stored in memory. ---*/
-
-      U_time_nM1 = nodes->GetSolution_time_n1(iPoint);
-      U_time_n   = nodes->GetSolution_time_n(iPoint);
-      U_time_nP1 = nodes->GetSolution(iPoint);
+  SU2_OMP_FOR_STAT(omp_chunk_size)
+  for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
 
-      /*--- CV volume at time n+1. As we are on a static mesh, the volume
-       of the CV will remained fixed for all time steps. ---*/
+    /*--- Retrieve the solution at time levels n-1, n, and n+1. Note that
+      we are currently iterating on U^n+1 and that U^n & U^n-1 are fixed,
+      previous solutions that are stored in memory. ---*/
 
-      Volume_nP1 = geometry->nodes->GetVolume(iPoint);
+    const auto* U_time_nM1 = nodes->GetSolution_time_n1(iPoint);
+    const auto* U_time_n = nodes->GetSolution_time_n(iPoint);
+    const auto* U_time_nP1 = nodes->GetSolution(iPoint);
 
-      /*--- Compute the dual time-stepping source term based on the chosen
-       time discretization scheme (1st- or 2nd-order).---*/
+    /*--- CV volume at time n+1. As we are on a static mesh, the volume
+      of the CV will remained fixed for all time steps. ---*/
 
-      for (auto iVar = 0u; iVar < nVar; iVar++) {
-        if (first_order)
-          Residual[iVar] = (U_time_nP1[iVar] - U_time_n[iVar])*Volume_nP1 / TimeStep;
-        if (second_order)
-          Residual[iVar] = ( 3.0*U_time_nP1[iVar] - 4.0*U_time_n[iVar]
-                            +1.0*U_time_nM1[iVar])*Volume_nP1 / (2.0*TimeStep);
-      }
+    const su2double Volume_nP1 = geometry->nodes->GetVolume(iPoint);
 
-      /*--- Store the residual and compute the Jacobian contribution due
-       to the dual time source term. ---*/
+    /*--- Compute the dual time-stepping source term based on the chosen
+      time discretization scheme (1st- or 2nd-order).---*/
 
-      LinSysRes.AddBlock(iPoint, Residual);
-      if (implicit) {
-        for (auto iVar = 0u; iVar < nVar; iVar++) {
-          for (auto jVar = 0u; jVar < nVar; jVar++) Jacobian_i[iVar][jVar] = 0.0;
-          if (first_order)
-            Jacobian_i[iVar][iVar] = Volume_nP1 / TimeStep;
-          if (second_order)
-            Jacobian_i[iVar][iVar] = (Volume_nP1*3.0)/(2.0*TimeStep);
-        }
+    for (auto iVar = 0u; iVar < nVar; iVar++) {
+      if (first_order)
+        LinSysRes(iPoint, iVar) += (U_time_nP1[iVar] - U_time_n[iVar]) * Volume_nP1 / TimeStep;
+      if (second_order)
+        LinSysRes(iPoint, iVar) += (3.0 * U_time_nP1[iVar] - 4.0 * U_time_n[iVar] +
+                                    1.0 * U_time_nM1[iVar]) * Volume_nP1 / (2.0 * TimeStep);
+    }
 
-        Jacobian.AddBlock2Diag(iPoint, Jacobian_i);
-      }
+    /*--- Compute the Jacobian contribution due to the dual time source term. ---*/
+    if (implicit) {
+      if (first_order) Jacobian.AddVal2Diag(iPoint, Volume_nP1 / TimeStep);
+      if (second_order) Jacobian.AddVal2Diag(iPoint, (Volume_nP1 * 3.0) / (2.0 * TimeStep));
     }
   }
+  END_SU2_OMP_FOR
+
+  AD::EndNoSharedReading();
 }
diff --git a/SU2_CFD/src/solvers/CIncEulerSolver.cpp b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
index a85c66fa11b..8ba501758d6 100644
--- a/SU2_CFD/src/solvers/CIncEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
@@ -2,7 +2,7 @@
  * \file CIncEulerSolver.cpp
  * \brief Main subroutines for solving incompressible flow (Euler, Navier-Stokes, etc.).
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -45,7 +45,7 @@ CIncEulerSolver::CIncEulerSolver(CGeometry *geometry, CConfig *config, unsigned
    *    being called by itself, or by its derived class CIncNSSolver. ---*/
   const string description = navier_stokes? "Navier-Stokes" : "Euler";
 
-  unsigned short iMarker, nLineLets;
+  unsigned short iMarker;
   ifstream restart_file;
   unsigned short nZone = geometry->GetnZone();
   bool restart = (config->GetRestart() || config->GetRestart_Flow());
@@ -161,11 +161,6 @@ CIncEulerSolver::CIncEulerSolver(CGeometry *geometry, CConfig *config, unsigned
       cout << "Initialize Jacobian structure (" << description << "). MG level: " << iMesh <<"." << endl;
 
     Jacobian.Initialize(nPoint, nPointDomain, nVar, nVar, true, geometry, config, ReducerStrategy);
-
-    if (config->GetKind_Linear_Solver_Prec() == LINELET) {
-      nLineLets = Jacobian.BuildLineletPreconditioner(geometry, config);
-      if (rank == MASTER_NODE) cout << "Compute linelet structure. " << nLineLets << " elements in each line (average)." << endl;
-    }
   }
   else {
     if (rank == MASTER_NODE)
diff --git a/SU2_CFD/src/solvers/CIncNSSolver.cpp b/SU2_CFD/src/solvers/CIncNSSolver.cpp
index 79063af583b..f14322a3343 100644
--- a/SU2_CFD/src/solvers/CIncNSSolver.cpp
+++ b/SU2_CFD/src/solvers/CIncNSSolver.cpp
@@ -2,7 +2,7 @@
  * \file CIncNSSolver.cpp
  * \brief Main subroutines for solving Navier-Stokes incompressible flow.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CMeshSolver.cpp b/SU2_CFD/src/solvers/CMeshSolver.cpp
index 7deb66aac17..e921dc534ec 100644
--- a/SU2_CFD/src/solvers/CMeshSolver.cpp
+++ b/SU2_CFD/src/solvers/CMeshSolver.cpp
@@ -2,7 +2,7 @@
  * \file CMeshSolver.cpp
  * \brief Main subroutines to solve moving meshes using a pseudo-linear elastic approach.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp b/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
index 7283e425964..ea4e4b60aec 100644
--- a/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
@@ -1,8 +1,8 @@
 /*!
  * \file CNEMOEulerSolver.cpp
  * \brief Headers of the CNEMOEulerSolver class
- * \author S. R. Copeland, F. Palacios, W. Maier, C. Garbacz
- * \version 7.4.0 "Blackbird"
+ * \author S. R. Copeland, F. Palacios, W. Maier, C. Garbacz, J. Needels
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -57,7 +57,6 @@ CNEMOEulerSolver::CNEMOEulerSolver(CGeometry *geometry, CConfig *config,
 
   int Unst_RestartIter = 0;
   unsigned long iMarker;
-  unsigned short nLineLets;
   su2double *Mvec_Inf, Alpha, Beta;
 
   /*--- A grid is defined as dynamic if there's rigid grid movement or grid deformation AND the problem is time domain ---*/
@@ -137,11 +136,6 @@ CNEMOEulerSolver::CNEMOEulerSolver(CGeometry *geometry, CConfig *config,
     /*--- Jacobians and vector  structures for implicit computations ---*/
     if (rank == MASTER_NODE) cout << "Initialize Jacobian structure (" << description << "). MG level: " << iMesh <<"." << endl;
     Jacobian.Initialize(nPoint, nPointDomain, nVar, nVar, true, geometry, config);
-
-    if (config->GetKind_Linear_Solver_Prec() == LINELET) {
-      nLineLets = Jacobian.BuildLineletPreconditioner(geometry, config);
-      if (rank == MASTER_NODE) cout << "Compute linelet structure. " << nLineLets << " elements in each line (average)." << endl;
-    }
   }
   else {
     if (rank == MASTER_NODE)  cout<< "Explicit Scheme. No Jacobian structure (" << description << "). MG level: " << iMesh <<"."<<endl;
@@ -1509,90 +1503,86 @@ void CNEMOEulerSolver::BC_Sym_Plane(CGeometry *geometry, CSolver **solver_contai
   }
 }
 
-void CNEMOEulerSolver::BC_Far_Field(CGeometry *geometry, CSolver **solver_container,
-                                    CNumerics *conv_numerics, CNumerics *visc_numerics,
-                                    CConfig *config, unsigned short val_marker) {
-
-  unsigned short iDim;
-  unsigned long iVertex, iPoint, Point_Normal;
-
-  su2double *V_infty, *V_domain, *U_infty, *U_domain;
-
-  /*--- Set booleans from configuration parameters ---*/
-  bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
-  bool viscous  = config->GetViscous();
+void CNEMOEulerSolver::BC_Far_Field(CGeometry *geometry,
+                                    CSolver **solver_container,
+                                    CNumerics *conv_numerics,
+                                    CNumerics *visc_numerics, CConfig *config,
+                                    unsigned short val_marker) {
 
   /*--- Allocate arrays ---*/
-  su2double *Normal = new su2double[nDim];
+  su2double Normal[MAXNDIM] = {0.0};
 
   /*--- Loop over all the vertices on this boundary (val_marker) ---*/
-  for (iVertex = 0; iVertex < geometry->nVertex[val_marker]; iVertex++) {
-    iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
-
-    /*--- Allocate the value at the infinity ---*/
-    V_infty = GetCharacPrimVar(val_marker, iVertex);
+  for (unsigned long iVertex = 0; iVertex < geometry->nVertex[val_marker];
+       iVertex++) {
+    const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
     /*--- Check if the node belongs to the domain (i.e, not a halo node) ---*/
     if (geometry->nodes->GetDomain(iPoint)) {
 
       /*--- Retrieve index of the closest interior node ---*/
-      Point_Normal = geometry->vertex[val_marker][iVertex]->GetNormal_Neighbor(); //only used for implicit
+      const auto Point_Normal = geometry->vertex[val_marker][iVertex]
+              ->GetNormal_Neighbor(); // only used for implicit
 
       /*--- Pass boundary node normal to CNumerics ---*/
       geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
-      for (iDim = 0; iDim < nDim; iDim++) Normal[iDim] = -Normal[iDim];
+      for (unsigned short iDim = 0; iDim < nDim; iDim++)
+        Normal[iDim] = -Normal[iDim];
       conv_numerics->SetNormal(Normal);
 
-      /*--- Retrieve solution at the boundary node & free-stream ---*/
-      U_domain = nodes->GetSolution(iPoint);
-      V_domain = nodes->GetPrimitive(iPoint);
-      U_infty  = node_infty->GetSolution(0);
-      V_infty  = node_infty->GetPrimitive(0);
-
       /*--- Pass conserved & primitive variables to CNumerics ---*/
-      conv_numerics->SetConservative(U_domain, U_infty);
-      conv_numerics->SetPrimitive(V_domain, V_infty);
+      conv_numerics->SetConservative(nodes->GetSolution(iPoint),
+                                     node_infty->GetSolution(0));
+      conv_numerics->SetPrimitive(nodes->GetPrimitive(iPoint),
+                                  node_infty->GetPrimitive(0));
 
       /*--- Pass supplementary information to CNumerics ---*/
-      conv_numerics->SetdPdU  (nodes->GetdPdU(iPoint),   node_infty->GetdPdU(0));
-      conv_numerics->SetdTdU  (nodes->GetdTdU(iPoint),   node_infty->GetdTdU(0));
-      conv_numerics->SetdTvedU(nodes->GetdTvedU(iPoint), node_infty->GetdTvedU(0));
-      conv_numerics->SetEve   (nodes->GetEve(iPoint),    node_infty->GetEve(0));
-      conv_numerics->SetCvve  (nodes->GetCvve(iPoint),   node_infty->GetCvve(0));
-      conv_numerics->SetGamma (nodes->GetGamma(iPoint),  node_infty->GetGamma(0));
+      conv_numerics->SetdPdU(nodes->GetdPdU(iPoint), node_infty->GetdPdU(0));
+      conv_numerics->SetdTdU(nodes->GetdTdU(iPoint), node_infty->GetdTdU(0));
+      conv_numerics->SetdTvedU(nodes->GetdTvedU(iPoint),
+                               node_infty->GetdTvedU(0));
+      conv_numerics->SetEve(nodes->GetEve(iPoint), node_infty->GetEve(0));
+      conv_numerics->SetCvve(nodes->GetCvve(iPoint), node_infty->GetCvve(0));
+      conv_numerics->SetGamma(nodes->GetGamma(iPoint), node_infty->GetGamma(0));
 
       /*--- Compute the convective residual (and Jacobian) ---*/
-      // Note: This uses the specified boundary num. method specified in driver_structure.cpp
+      // Note: This uses the specified boundary num. method specified in
+      // driver_structure.cpp
       auto residual = conv_numerics->ComputeResidual(config);
 
       /*--- Apply contribution to the linear system ---*/
       LinSysRes.AddBlock(iPoint, residual);
 
+      const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
       if (implicit)
         Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
 
       /*--- Viscous contribution ---*/
+      bool viscous = config->GetViscous();
       if (viscous) {
         su2double Coord_Reflected[MAXNDIM];
-        GeometryToolbox::PointPointReflect(nDim, geometry->nodes->GetCoord(Point_Normal),
-                                                 geometry->nodes->GetCoord(iPoint), Coord_Reflected);
-        visc_numerics->SetCoord(geometry->nodes->GetCoord(iPoint), Coord_Reflected );
+        GeometryToolbox::PointPointReflect(
+            nDim, geometry->nodes->GetCoord(Point_Normal),
+            geometry->nodes->GetCoord(iPoint), Coord_Reflected);
+        visc_numerics->SetCoord(geometry->nodes->GetCoord(iPoint),
+                                Coord_Reflected);
         visc_numerics->SetNormal(Normal);
 
         /*--- Primitive variables, and gradient ---*/
         visc_numerics->SetConservative(nodes->GetSolution(iPoint),
-                                       node_infty->GetSolution(0) );
+                                       node_infty->GetSolution(0));
         visc_numerics->SetPrimitive(nodes->GetPrimitive(iPoint),
-                                    node_infty->GetPrimitive(0) );
+                                    node_infty->GetPrimitive(0));
         visc_numerics->SetPrimVarGradient(nodes->GetGradient_Primitive(iPoint),
-                                          node_infty->GetGradient_Primitive(0) );
+                                          node_infty->GetGradient_Primitive(0));
 
         /*--- Pass supplementary information to CNumerics ---*/
-        visc_numerics->SetdPdU  (nodes->GetdPdU(iPoint),   node_infty->GetdPdU(0));
-        visc_numerics->SetdTdU  (nodes->GetdTdU(iPoint),   node_infty->GetdTdU(0));
-        visc_numerics->SetdTvedU(nodes->GetdTvedU(iPoint), node_infty->GetdTvedU(0));
-        visc_numerics->SetEve   (nodes->GetEve(iPoint),    node_infty->GetEve(0));
-        visc_numerics->SetCvve  (nodes->GetCvve(iPoint),   node_infty->GetCvve(0));
+        visc_numerics->SetdPdU(nodes->GetdPdU(iPoint), node_infty->GetdPdU(0));
+        visc_numerics->SetdTdU(nodes->GetdTdU(iPoint), node_infty->GetdTdU(0));
+        visc_numerics->SetdTvedU(nodes->GetdTvedU(iPoint),
+                                 node_infty->GetdTvedU(0));
+        visc_numerics->SetEve(nodes->GetEve(iPoint), node_infty->GetEve(0));
+        visc_numerics->SetCvve(nodes->GetCvve(iPoint), node_infty->GetCvve(0));
 
         /*--- Species diffusion coefficients ---*/
         visc_numerics->SetDiffusionCoeff(nodes->GetDiffusionCoeff(iPoint),
@@ -1607,12 +1597,14 @@ void CNEMOEulerSolver::BC_Far_Field(CGeometry *geometry, CSolver **solver_contai
                                         nodes->GetEddyViscosity(iPoint));
 
         /*--- Thermal conductivity ---*/
-        visc_numerics->SetThermalConductivity(nodes->GetThermalConductivity(iPoint),
-                                              nodes->GetThermalConductivity(iPoint));
+        visc_numerics->SetThermalConductivity(
+            nodes->GetThermalConductivity(iPoint),
+            nodes->GetThermalConductivity(iPoint));
 
         /*--- Vib-el. thermal conductivity ---*/
-        visc_numerics->SetThermalConductivity_ve(nodes->GetThermalConductivity_ve(iPoint),
-                                                 nodes->GetThermalConductivity_ve(iPoint));
+        visc_numerics->SetThermalConductivity_ve(
+            nodes->GetThermalConductivity_ve(iPoint),
+            nodes->GetThermalConductivity_ve(iPoint));
 
         /*--- Compute and update residual ---*/
         auto residual = visc_numerics->ComputeResidual(config);
@@ -1624,9 +1616,6 @@ void CNEMOEulerSolver::BC_Far_Field(CGeometry *geometry, CSolver **solver_contai
       }
     }
   }
-
-  /*--- Free locally allocated memory ---*/
-  delete [] Normal;
 }
 
 void CNEMOEulerSolver::BC_Inlet(CGeometry *geometry, CSolver **solver_container,
@@ -2154,281 +2143,205 @@ void CNEMOEulerSolver::BC_Outlet(CGeometry *geometry, CSolver **solver_container
 
 }
 
-void CNEMOEulerSolver::BC_Supersonic_Inlet(CGeometry *geometry, CSolver **solver_container,
-                                           CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
-
-SU2_MPI::Error("BC_SUPERSONIC_INLET: Not operational in NEMO.", CURRENT_FUNCTION);
-
-//  unsigned short iDim, iVar;
-//  unsigned long iVertex, iPoint, Point_Normal;
-//  su2double Density, Pressure, Temperature, Temperature_ve, Energy, *Velocity, Velocity2, soundspeed;
-//  su2double Gas_Constant = config->GetGas_ConstantND();
-//
-//  bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
-//  bool dynamic_grid  = config->GetGrid_Movement();
-//  bool viscous              = config->GetViscous();
-//  string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
-//
-//  su2double RuSI  = UNIVERSAL_GAS_CONSTANT;
-//  su2double Ru = 1000.0*RuSI;
-//
-//  su2double *U_inlet = new su2double[nVar];     su2double *U_domain = new su2double[nVar];
-//  su2double *V_inlet = new su2double[nPrimVar]; su2double *V_domain = new su2double[nPrimVar];
-//  su2double *Normal = new su2double[nDim];
-
-/* ----------------------------------------------------------------------------- */
-/* ----------------------------------------------------------------------------- */
-/* The block of code commented below needs to be updated to use Fluidmodel class */
-/* ----------------------------------------------------------------------------- */
-/* ----------------------------------------------------------------------------- */
-
-//  /*--- Supersonic inlet flow: there are no outgoing characteristics,
-//   so all flow variables can be imposed at the inlet.
-//   First, retrieve the specified values for the primitive variables. ---*/
-//  //ASSUME TVE = T for the time being
-//  auto Mass_Frac      = config->GetInlet_MassFrac(Marker_Tag);
-//  Temperature    = config->GetInlet_Temperature(Marker_Tag);
-//  Pressure       = config->GetInlet_Pressure(Marker_Tag);
-//  Velocity       = config->GetInlet_Velocity(Marker_Tag);
-//  Temperature_ve = Temperature;
-//
-//  /*--- Compute Density and Species Densities ---*/
-//  for (iSpecies = 0; iSpecies < nHeavy; iSpecies++)
-//    denom += Mass_Frac[iSpecies] * (Ru/Ms[iSpecies]) * Temperature;
-//  for (iSpecies = 0; iSpecies < nEl; iSpecies++)
-//    denom += Mass_Frac[nSpecies-1] * (Ru/Ms[nSpecies-1]) * Temperature_ve;
-//  Density = Pressure / denom;
-//
-//  /*--- Compute Soundspeed and Velocity squared ---*/
-//  for (iSpecies = 0; iSpecies < nHeavy; iSpecies++) {
-//    conc += Mass_Frac[iSpecies]*Density/Ms[iSpecies];
-//    rhoCvtr += Density*Mass_Frac[iSpecies] * (3.0/2.0 + xi[iSpecies]/2.0) * Ru/Ms[iSpecies];
-//  }
-//  soundspeed = sqrt((1.0 + Ru/rhoCvtr*conc) * Pressure/Density);
-//
-//  Velocity2 = 0.0;
-//  for (iDim = 0; iDim < nDim; iDim++)
-//    Velocity2 += Velocity[iDim]*Velocity[iDim];
-//
-//  /*--- Non-dim. the inputs if necessary. ---*/
-//  // Need to update this portion
-//  //Temperature = Temperature/config->GetTemperature_Ref();
-//  //Pressure    = Pressure/config->GetPressure_Ref();
-//  //Density     = Density/config->GetDensity_Ref();
-//  //for (iDim = 0; iDim < nDim; iDim++)
-//  //  Velocity[iDim] = Velocity[iDim]/config->GetVelocity_Ref();
-//
-//  /*--- Compute energy (RRHO) from supplied primitive quanitites ---*/
-//  for (iSpecies = 0; iSpecies < nHeavy; iSpecies++) {
-//
-//    // Species density
-//    rhos = Mass_Frac[iSpecies]*Density;
-//
-//    // Species formation energy
-//    Ef = hf[iSpecies] - Ru/Ms[iSpecies]*Tref[iSpecies];
-//
-//    // Species vibrational energy
-//    if (thetav[iSpecies] != 0.0)
-//      Ev = Ru/Ms[iSpecies] * thetav[iSpecies] / (exp(thetav[iSpecies]/Temperature_ve)-1.0);
-//    else
-//      Ev = 0.0;
-//
-//    // Species electronic energy
-//    num = 0.0;
-//    denom = g[iSpecies][0] * exp(thetae[iSpecies][0]/Temperature_ve);
-//    for (iEl = 1; iEl < nElStates[iSpecies]; iEl++) {
-//      num   += g[iSpecies][iEl] * thetae[iSpecies][iEl] * exp(-thetae[iSpecies][iEl]/Temperature_ve);
-//      denom += g[iSpecies][iEl] * exp(-thetae[iSpecies][iEl]/Temperature_ve);
-//    }
-//    Ee = Ru/Ms[iSpecies] * (num/denom);
-//
-//    // Mixture total energy
-//    rhoE += rhos * ((3.0/2.0+xi[iSpecies]/2.0) * Ru/Ms[iSpecies] * (Temperature-Tref[iSpecies])
-//                    + Ev + Ee + Ef + 0.5*Velocity2);
-//
-//    // Mixture vibrational-electronic energy
-//    rhoEve += rhos * (Ev + Ee);
-//  }
-//
-//  /*--- Setting Conservative Variables ---*/
-//  for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
-//    U_inlet[iSpecies] = Mass_Frac[iSpecies]*Density;
-//  for (iDim = 0; iDim < nDim; iDim++)
-//    U_inlet[nSpecies+iDim] = Density*Velocity[iDim];
-//  U_inlet[nVar-2] = rhoE;
-//  U_inlet[nVar-1] = rhoEve;
-//
-//  /*--- Setting Primitive Vaariables ---*/
-//  for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
-//    V_inlet[iSpecies] = Mass_Frac[iSpecies]*Density;
-//  V_inlet[nSpecies] = Temperature;
-//  V_inlet[nSpecies+1] = Temperature_ve;
-//  for (iDim = 0; iDim < nDim; iDim++)
-//    V_inlet[nSpecies+2+iDim] = Velocity[iDim];
-//  V_inlet[nSpecies+2+nDim] = Pressure;
-//  V_inlet[nSpecies+3+nDim] = Density;
-//  V_inlet[nSpecies+4+nDim] = rhoE+Pressure/Density;
-//  V_inlet[nSpecies+5+nDim] = soundspeed;
-//  V_inlet[nSpecies+6+nDim] = rhoCvtr;
-
-/* ----------------------------------------------------------------------------- */
-/* ----------------------------------------------------------------------------- */
-/* The block of code that needs to be updated to use Fluidmodel class end here   */
-/* ----------------------------------------------------------------------------- */
-/* ----------------------------------------------------------------------------- */
-
-//  //This requires Newtown Raphson.....So this is not currently operational (See Deathstar)
-//  //V_inlet[nSpecies+7+nDim] = rhoCvve;
-//
-//  /*--- Loop over all the vertices on this boundary marker ---*/
-//  for(iVertex = 0; iVertex < geometry->nVertex[val_marker]; iVertex++) {
-//    iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
-//
-//    /*--- Check if the node belongs to the domain (i.e, not a halo node) ---*/
-//    if (geometry->nodes->GetDomain(iPoint)) {
-//
-//      /*--- Index of the closest interior node ---*/
-//      Point_Normal = geometry->vertex[val_marker][iVertex]->GetNormal_Neighbor();
-//
-//      /*--- Current solution at this boundary node ---*/
-//      for (iVar = 0; iVar < nVar; iVar++) U_domain[iVar] = nodes->GetSolution(iPoint,iVar);
-//      for (iVar = 0; iVar < nPrimVar; iVar++) V_domain[iVar] = nodes->GetPrimitive(iPoint,iVar);
-//
-//      /*--- Normal vector for this vertex (negate for outward convention) ---*/
-//      geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
-//      for (iDim = 0; iDim < nDim; iDim++) Normal[iDim] = -Normal[iDim];
-//
-//      su2double Area = 0.0;
-//      for (iDim = 0; iDim < nDim; iDim++)
-//        Area += Normal[iDim]*Normal[iDim];
-//      Area = sqrt (Area);
-//
-//      /*--- Set various quantities in the solver class ---*/
-//      conv_numerics->SetNormal(Normal);
-//      conv_numerics->SetConservative(U_domain, U_inlet);
-//      conv_numerics->SetPrimitive(V_domain, V_inlet);
-//
-//      /*--- Pass supplementary info to CNumerics ---*/
-//      conv_numerics->SetdPdU(nodes->GetdPdU(iPoint), node_infty->GetdPdU(0));
-//      conv_numerics->SetdTdU(nodes->GetdTdU(iPoint), node_infty->GetdTdU(0));
-//      conv_numerics->SetdTvedU(nodes->GetdTvedU(iPoint), node_infty->GetdTvedU(0));
-//      conv_numerics->SetEve(nodes->GetEve(iPoint), node_infty->GetEve(0));
-//      conv_numerics->SetCvve(nodes->GetCvve(iPoint), node_infty->GetCvve(0));
-//
-//      if (dynamic_grid)
-//        conv_numerics->SetGridVel(geometry->nodes->GetGridVel(iPoint),
-//                                  geometry->nodes->GetGridVel(iPoint));
-//
-//      /*--- Compute the residual using an upwind scheme ---*/
-//      auto residual = conv_numerics->ComputeResidual(config);
-//      LinSysRes.AddBlock(iPoint, residual);
-//
-//      /*--- Jacobian contribution for implicit integration ---*/
-//      //if (implicit)
-//      //  Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
-//
-//      /*--- Viscous contribution ---*/
-//      if (viscous) {
-//
-//        /*--- Set the normal vector and the coordinates ---*/
-//        visc_numerics->SetNormal(Normal);
-//        su2double Coord_Reflected[MAXNDIM];
-//        GeometryToolbox::PointPointReflect(nDim, geometry->nodes->GetCoord(Point_Normal),
-//                                           geometry->nodes->GetCoord(iPoint), Coord_Reflected);
-//        visc_numerics->SetCoord(geometry->nodes->GetCoord(iPoint), Coord_Reflected);
-//
-//        /*--- Primitive variables, and gradient ---*/
-//        visc_numerics->SetPrimitive(V_domain, V_inlet);
-//        visc_numerics->SetPrimVarGradient(nodes->GetGradient_Primitive(iPoint), nodes->GetGradient_Primitive(iPoint));
-//
-//        /*--- Laminar viscosity ---*/
-//        visc_numerics->SetLaminarViscosity(nodes->GetLaminarViscosity(iPoint), nodes->GetLaminarViscosity(iPoint));
-//
-//        /*--- Compute and update residual ---*/
-//        auto residual = visc_numerics->ComputeResidual(config);
-//        LinSysRes.SubtractBlock(iPoint, residual);
-//
-//        /*--- Jacobian contribution for implicit integration ---*/
-//        //if (implicit)
-//        //  Jacobian.SubtractBlock2Diag(iPoint, residual.Jacobian_i);
-//      }
-//
-//    }
-//  }
-//
-//  /*--- Free locally allocated memory ---*/
-//  delete [] U_domain;
-//  delete [] U_inlet;
-//  delete [] V_domain;
-//  delete [] V_inlet;
-//  delete [] Normal;
-
-}
+void CNEMOEulerSolver::BC_Supersonic_Inlet(
+    CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics,
+    CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
 
-void CNEMOEulerSolver::BC_Supersonic_Outlet(CGeometry *geometry, CSolver **solver_container,
-                                            CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
-  unsigned short iDim;
-  unsigned long iVertex, iPoint;
-  su2double *V_outlet, *V_domain;
-  su2double *U_outlet, *U_domain;
+  /*--- Supersonic inlet flow: there are no outgoing characteristics,
+   so all flow variables can be imposed at the inlet.
+   First, retrieve the specified values for the primitive variables. ---*/
 
-  bool implicit     = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
-  string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
+  const string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
 
-  su2double *Normal = new su2double[nDim];
+  const su2double Temperature = config->GetInlet_Temperature(Marker_Tag);
+  const su2double Pressure = config->GetInlet_Pressure(Marker_Tag);
+  const su2double *Velocity = config->GetInlet_Velocity(Marker_Tag);
+  const su2double *Mass_Frac = config->GetInlet_MassFrac();
+  su2double Temperature_ve = config->GetInlet_Temperature_ve();
 
-  /*--- Supersonic outlet flow: there are no ingoing characteristics,
-   so all flow variables can should be interpolated from the domain. ---*/
+  /*--- If no Tve value specified (left as 0 K default), set to Ttr value ---*/
+  if (Temperature_ve == 0.0) {
+    Temperature_ve = Temperature;
+  }
 
-  /*--- Loop over all the vertices on this boundary marker ---*/
-  for (iVertex = 0; iVertex < geometry->nVertex[val_marker]; iVertex++) {
+  /*--- Set mixture state ---*/
+  FluidModel->SetTDStatePTTv(Pressure, Mass_Frac, Temperature, Temperature_ve);
 
-    iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
+  /*--- Compute Ma vector for flow direction ---*/
+  const su2double soundspeed = FluidModel->ComputeSoundSpeed();
 
-    /*--- Check if the node belongs to the domain (i.e, not a halo node) ---*/
-    if (geometry->nodes->GetDomain(iPoint)) {
+  su2double Mvec[MAXNDIM] = {0.0};
 
-      /*--- Current solution at this boundary node ---*/
-      V_domain = nodes->GetPrimitive(iPoint);
-      U_domain = nodes->GetSolution(iPoint);
+  for (unsigned short iDim = 0; iDim < nDim; iDim++)
+    Mvec[iDim] = Velocity[iDim] / soundspeed;
 
-      /*--- Allocate the value at the outlet ---*/
-      V_outlet = GetCharacPrimVar(val_marker, iVertex);
-      V_outlet = V_domain;
-      U_outlet = U_domain;
+  /*--- Allocate inlet node to compute gradients for numerics ---*/
+  CNEMOEulerVariable node_inlet(Pressure, Mass_Frac, Mvec, Temperature,
+                                Temperature_ve, 1, nDim, nVar, nPrimVar,
+                                nPrimVarGrad, config, FluidModel);
+  node_inlet.SetPrimVar(0, FluidModel);
 
-      /*--- Normal vector for this vertex (negate for outward convention) ---*/
-      geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
-      for (iDim = 0; iDim < nDim; iDim++) Normal[iDim] = -Normal[iDim];
+  su2double Normal[MAXNDIM] = {0.0};
 
-      /*--- Set various quantities in the solver class ---*/
-      conv_numerics->SetNormal(Normal);
-      conv_numerics->SetPrimitive(V_domain, V_outlet);
-      conv_numerics->SetConservative(U_domain, U_outlet);
+  /*--- Loop over all the vertices on this boundary marker ---*/
+  for (unsigned long iVertex = 0; iVertex < geometry->nVertex[val_marker];
+       iVertex++) {
+    const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
-      /*--- Pass supplementary information to CNumerics ---*/
-      conv_numerics->SetdPdU  (nodes->GetdPdU(iPoint),   nodes->GetdPdU(iPoint));
-      conv_numerics->SetdTdU  (nodes->GetdTdU(iPoint),   nodes->GetdTdU(iPoint));
-      conv_numerics->SetdTvedU(nodes->GetdTvedU(iPoint), nodes->GetdTvedU(iPoint));
-      conv_numerics->SetEve   (nodes->GetEve(iPoint),    nodes->GetEve(iPoint));
-      conv_numerics->SetCvve  (nodes->GetCvve(iPoint),   nodes->GetCvve(iPoint));
-      conv_numerics->SetGamma (nodes->GetGamma(iPoint),  nodes->GetGamma(iPoint));
+    /*--- Check if the node belongs to the domain (i.e, not a halo node) ---*/
+    if (!geometry->nodes->GetDomain(iPoint))
+      continue;
+
+    /*--- Index of the closest interior node ---*/
+    const auto Point_Normal =
+        geometry->vertex[val_marker][iVertex]->GetNormal_Neighbor();
+
+    /*--- Normal vector for this vertex (negate for outward convention) ---*/
+    geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
+    for (unsigned short iDim = 0; iDim < nDim; iDim++)
+      Normal[iDim] = -Normal[iDim];
+
+    /*--- Set various quantities in the solver class ---*/
+    conv_numerics->SetNormal(Normal);
+    conv_numerics->SetConservative(nodes->GetSolution(iPoint),
+                                   node_inlet.GetSolution(0));
+    conv_numerics->SetPrimitive(nodes->GetPrimitive(iPoint),
+                                node_inlet.GetPrimitive(0));
+
+    /*--- Pass supplementary info to CNumerics ---*/
+    conv_numerics->SetdPdU(nodes->GetdPdU(iPoint), node_inlet.GetdPdU(0));
+    conv_numerics->SetdTdU(nodes->GetdTdU(iPoint), node_inlet.GetdTdU(0));
+    conv_numerics->SetdTvedU(nodes->GetdTvedU(iPoint), node_inlet.GetdTvedU(0));
+    conv_numerics->SetEve(nodes->GetEve(iPoint), node_inlet.GetEve(0));
+    conv_numerics->SetCvve(nodes->GetCvve(iPoint), node_inlet.GetCvve(0));
+
+    const bool dynamic_grid = config->GetGrid_Movement();
+    if (dynamic_grid)
+      conv_numerics->SetGridVel(geometry->nodes->GetGridVel(iPoint),
+                                geometry->nodes->GetGridVel(iPoint));
+
+    /*--- Compute the residual using an upwind scheme ---*/
+    auto residual = conv_numerics->ComputeResidual(config);
+    LinSysRes.AddBlock(iPoint, residual);
+
+    /*--- Jacobian contribution for implicit integration ---*/
+    const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+    if (implicit)
+      Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
+
+    /*--- Viscous contribution ---*/
+    bool viscous = config->GetViscous();
+    if (viscous) {
 
-      if (dynamic_grid)
-        conv_numerics->SetGridVel(geometry->nodes->GetGridVel(iPoint),
-                                  geometry->nodes->GetGridVel(iPoint));
+      /*--- Set the normal vector and the coordinates ---*/
+      su2double Coord_Reflected[MAXNDIM];
+      GeometryToolbox::PointPointReflect(
+          nDim, geometry->nodes->GetCoord(Point_Normal),
+          geometry->nodes->GetCoord(iPoint), Coord_Reflected);
+      visc_numerics->SetCoord(geometry->nodes->GetCoord(iPoint),
+                              Coord_Reflected);
+      visc_numerics->SetNormal(Normal);
+
+      /*--- Primitive variables, and gradient ---*/
+      visc_numerics->SetConservative(nodes->GetSolution(iPoint),
+                                     node_inlet.GetSolution(0));
+      visc_numerics->SetPrimitive(nodes->GetPrimitive(iPoint),
+                                  node_inlet.GetPrimitive(0));
+      visc_numerics->SetPrimVarGradient(nodes->GetGradient_Primitive(iPoint),
+                                        node_inlet.GetGradient_Primitive(0));
 
-      /*--- Compute the residual using an upwind scheme ---*/
-      auto residual = conv_numerics->ComputeResidual(config);
-      LinSysRes.AddBlock(iPoint, residual);
+      /*--- Pass supplementary information to CNumerics ---*/
+      visc_numerics->SetdPdU(nodes->GetdPdU(iPoint), node_inlet.GetdPdU(0));
+      visc_numerics->SetdTdU(nodes->GetdTdU(iPoint), node_inlet.GetdTdU(0));
+      visc_numerics->SetdTvedU(nodes->GetdTvedU(iPoint),
+                               node_inlet.GetdTvedU(0));
+      visc_numerics->SetEve(nodes->GetEve(iPoint), node_inlet.GetEve(0));
+      visc_numerics->SetCvve(nodes->GetCvve(iPoint), node_inlet.GetCvve(0));
+
+      /*--- Species diffusion coefficients ---*/
+      visc_numerics->SetDiffusionCoeff(nodes->GetDiffusionCoeff(iPoint),
+                                       nodes->GetDiffusionCoeff(iPoint));
+      /*--- Laminar viscosity ---*/
+      visc_numerics->SetLaminarViscosity(nodes->GetLaminarViscosity(iPoint),
+                                         nodes->GetLaminarViscosity(iPoint));
+      /*--- Eddy viscosity ---*/
+      visc_numerics->SetEddyViscosity(nodes->GetEddyViscosity(iPoint),
+                                      nodes->GetEddyViscosity(iPoint));
+      /*--- Thermal conductivity ---*/
+      visc_numerics->SetThermalConductivity(
+          nodes->GetThermalConductivity(iPoint),
+          nodes->GetThermalConductivity(iPoint));
+      /*--- Vib-el. thermal conductivity ---*/
+      visc_numerics->SetThermalConductivity_ve(
+          nodes->GetThermalConductivity_ve(iPoint),
+          nodes->GetThermalConductivity_ve(iPoint));
+
+      /*--- Compute and update residual ---*/
+      auto residual = visc_numerics->ComputeResidual(config);
+      LinSysRes.SubtractBlock(iPoint, residual);
 
       /*--- Jacobian contribution for implicit integration ---*/
       if (implicit)
-        Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
+        Jacobian.SubtractBlock2Diag(iPoint, residual.jacobian_i);
     }
   }
+}
 
-  /*--- Free locally allocated memory ---*/
-  delete [] Normal;
+void CNEMOEulerSolver::BC_Supersonic_Outlet(
+    CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics,
+    CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
+
+  /*--- Supersonic outlet flow: there are no ingoing characteristics,
+   so all flow variables can should be interpolated from the domain. ---*/
+
+  su2double Normal[MAXNDIM] = {0.0};
+
+  const string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
+
+  /*--- Loop over all the vertices on this boundary marker ---*/
+  for (unsigned long iVertex = 0; iVertex < geometry->nVertex[val_marker];
+       iVertex++) {
 
+    const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
+
+    /*--- Check if the node belongs to the domain (i.e, not a halo node) ---*/
+    if (!geometry->nodes->GetDomain(iPoint))
+      continue;
+
+    /*--- Normal vector for this vertex (negate for outward convention) ---*/
+    geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
+    for (unsigned short iDim = 0; iDim < nDim; iDim++)
+      Normal[iDim] = -Normal[iDim];
+
+    /*--- Set various quantities in the solver class, outlet properties are
+     * equal to domain properties ---*/
+    conv_numerics->SetNormal(Normal);
+    conv_numerics->SetPrimitive(nodes->GetPrimitive(iPoint),
+                                nodes->GetPrimitive(iPoint));
+    conv_numerics->SetConservative(nodes->GetSolution(iPoint),
+                                   nodes->GetSolution(iPoint));
+
+    /*--- Pass supplementary information to CNumerics ---*/
+    conv_numerics->SetdPdU(nodes->GetdPdU(iPoint), nodes->GetdPdU(iPoint));
+    conv_numerics->SetdTdU(nodes->GetdTdU(iPoint), nodes->GetdTdU(iPoint));
+    conv_numerics->SetdTvedU(nodes->GetdTvedU(iPoint),
+                             nodes->GetdTvedU(iPoint));
+    conv_numerics->SetEve(nodes->GetEve(iPoint), nodes->GetEve(iPoint));
+    conv_numerics->SetCvve(nodes->GetCvve(iPoint), nodes->GetCvve(iPoint));
+    conv_numerics->SetGamma(nodes->GetGamma(iPoint), nodes->GetGamma(iPoint));
+
+    const bool dynamic_grid = config->GetGrid_Movement();
+    if (dynamic_grid)
+      conv_numerics->SetGridVel(geometry->nodes->GetGridVel(iPoint),
+                                geometry->nodes->GetGridVel(iPoint));
+
+    /*--- Compute the residual using an upwind scheme ---*/
+    auto residual = conv_numerics->ComputeResidual(config);
+    LinSysRes.AddBlock(iPoint, residual);
+
+    /*--- Jacobian contribution for implicit integration ---*/
+    const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+    if (implicit)
+      Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
+  }
 }
diff --git a/SU2_CFD/src/solvers/CNEMONSSolver.cpp b/SU2_CFD/src/solvers/CNEMONSSolver.cpp
index 0b37f996fe9..617a0d31e90 100644
--- a/SU2_CFD/src/solvers/CNEMONSSolver.cpp
+++ b/SU2_CFD/src/solvers/CNEMONSSolver.cpp
@@ -2,7 +2,7 @@
  * \file CNEMONSSolver.cpp
  * \brief Headers of the CNEMONSSolver class
  * \author S. R. Copeland, F. Palacios, W. Maier.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CNSSolver.cpp b/SU2_CFD/src/solvers/CNSSolver.cpp
index 9ba1d572158..f1144f95e91 100644
--- a/SU2_CFD/src/solvers/CNSSolver.cpp
+++ b/SU2_CFD/src/solvers/CNSSolver.cpp
@@ -2,7 +2,7 @@
  * \file CNSSolver.cpp
  * \brief Main subroutines for solving Finite-Volume Navier-Stokes flow problems.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CRadP1Solver.cpp b/SU2_CFD/src/solvers/CRadP1Solver.cpp
index 0be7f191148..cfb5a20b07c 100644
--- a/SU2_CFD/src/solvers/CRadP1Solver.cpp
+++ b/SU2_CFD/src/solvers/CRadP1Solver.cpp
@@ -2,7 +2,7 @@
  * \file CRadP1Solver.cpp
  * \brief Main subroutines for solving P1 radiation problems.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CRadSolver.cpp b/SU2_CFD/src/solvers/CRadSolver.cpp
index 1c08adff597..5fc59d1963a 100644
--- a/SU2_CFD/src/solvers/CRadSolver.cpp
+++ b/SU2_CFD/src/solvers/CRadSolver.cpp
@@ -2,7 +2,7 @@
  * \file CRadP1Solver.cpp
  * \brief Main subroutines for solving generic radiation problems (P1, M1, discrete ordinates...)
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CSolver.cpp b/SU2_CFD/src/solvers/CSolver.cpp
index 951b0b33ef7..2d7c1f326fa 100644
--- a/SU2_CFD/src/solvers/CSolver.cpp
+++ b/SU2_CFD/src/solvers/CSolver.cpp
@@ -2,7 +2,7 @@
  * \file CSolver.cpp
  * \brief Main subroutines for CSolver class.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CSolverFactory.cpp b/SU2_CFD/src/solvers/CSolverFactory.cpp
index 08f756835cb..bf2a09ddfe5 100644
--- a/SU2_CFD/src/solvers/CSolverFactory.cpp
+++ b/SU2_CFD/src/solvers/CSolverFactory.cpp
@@ -2,7 +2,7 @@
  * \file CSolverFactory.cpp
  * \brief Main subroutines for CSolverFactoryclass.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -100,6 +100,7 @@ CSolver** CSolverFactory::CreateSolverContainer(MAIN_SOLVER kindMainSolver, CCon
       solver[HEAT_SOL] = CreateSubSolver(SUB_SOLVER_TYPE::HEAT, solver, geometry, config, iMGLevel);
       solver[SPECIES_SOL] = CreateSubSolver(SUB_SOLVER_TYPE::SPECIES, solver, geometry, config, iMGLevel);
       solver[TURB_SOL] = CreateSubSolver(SUB_SOLVER_TYPE::TURB, solver, geometry, config, iMGLevel);
+      solver[TRANS_SOL] = CreateSubSolver(SUB_SOLVER_TYPE::TRANSITION, solver, geometry, config, iMGLevel);
       solver[RAD_SOL]  = CreateSubSolver(SUB_SOLVER_TYPE::RADIATION, solver, geometry, config, iMGLevel);
       break;
     case MAIN_SOLVER::HEAT_EQUATION:
diff --git a/SU2_CFD/src/solvers/CSpeciesSolver.cpp b/SU2_CFD/src/solvers/CSpeciesSolver.cpp
index 456b6d5f12c..2b2dddba029 100644
--- a/SU2_CFD/src/solvers/CSpeciesSolver.cpp
+++ b/SU2_CFD/src/solvers/CSpeciesSolver.cpp
@@ -2,7 +2,7 @@
  * \file CSpeciesSolver.cpp
  * \brief Main subroutines of CSpeciesSolver class
  * \author T. Kattmann
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -81,13 +81,6 @@ CSpeciesSolver::CSpeciesSolver(CGeometry* geometry, CConfig* config, unsigned sh
 
     if (rank == MASTER_NODE) cout << "Initialize Jacobian structure (species transport model)." << endl;
     Jacobian.Initialize(nPoint, nPointDomain, nVar, nVar, true, geometry, config, ReducerStrategy);
-
-    if (config->GetKind_Linear_Solver_Prec() == LINELET) {
-      const auto nLineLets = Jacobian.BuildLineletPreconditioner(geometry, config);
-      if (rank == MASTER_NODE)
-        cout << "Compute linelet structure. " << nLineLets << " elements in each line (average)." << endl;
-    }
-
     LinSysSol.Initialize(nPoint, nPointDomain, nVar, 0.0);
     LinSysRes.Initialize(nPoint, nPointDomain, nVar, 0.0);
     System.SetxIsZero(true);
@@ -292,7 +285,7 @@ void CSpeciesSolver::LoadRestart(CGeometry** geometry, CSolver*** solver, CConfi
 void CSpeciesSolver::Preprocessing(CGeometry* geometry, CSolver** solver_container, CConfig* config,
                                    unsigned short iMesh, unsigned short iRKStep, unsigned short RunTime_EqSystem,
                                    bool Output) {
-  config->SetGlobalParam(config->GetKind_Solver(), RunTime_EqSystem);
+  SU2_OMP_SAFE_GLOBAL_ACCESS(config->SetGlobalParam(config->GetKind_Solver(), RunTime_EqSystem);)
 
   /*--- Set the laminar mass Diffusivity for the species solver. ---*/
   SU2_OMP_FOR_STAT(omp_chunk_size)
diff --git a/SU2_CFD/src/solvers/CTemplateSolver.cpp b/SU2_CFD/src/solvers/CTemplateSolver.cpp
index 9d67e4e0760..7fb240f9f26 100644
--- a/SU2_CFD/src/solvers/CTemplateSolver.cpp
+++ b/SU2_CFD/src/solvers/CTemplateSolver.cpp
@@ -2,7 +2,7 @@
  * \file CTemplateSolver.cpp
  * \brief Subroutines to be implemented for any new solvers
  * \author F. Palacios
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CTransLMSolver.cpp b/SU2_CFD/src/solvers/CTransLMSolver.cpp
index df487b96515..01a254e98b7 100644
--- a/SU2_CFD/src/solvers/CTransLMSolver.cpp
+++ b/SU2_CFD/src/solvers/CTransLMSolver.cpp
@@ -2,7 +2,7 @@
  * \file CTransLMSolver.cpp
  * \brief Main subroutines for Langtry-Menter Transition model solver.
  * \author A. Aranake, S. Kang.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -40,7 +40,6 @@
 
 CTransLMSolver::CTransLMSolver(CGeometry *geometry, CConfig *config, unsigned short iMesh)
     : CTurbSolver(geometry, config, true) {
-  unsigned short nLineLets;
   unsigned long iPoint;
   ifstream restart_file;
   string text_line;
@@ -61,6 +60,11 @@ CTransLMSolver::CTransLMSolver(CGeometry *geometry, CConfig *config, unsigned sh
 
   nDim = geometry->GetnDim();
 
+  /*--- Define variables needed for transition from config file */
+  options = config->GetLMParsedOptions();
+  TransCorrelations.SetOptions(options);
+  TurbFamily = TurbModelFamily(config->GetKind_Turb_Model());
+
   /*--- Single grid simulation ---*/
 
   if (iMesh == MESH_0) {
@@ -76,12 +80,6 @@ CTransLMSolver::CTransLMSolver(CGeometry *geometry, CConfig *config, unsigned sh
 
     if (rank == MASTER_NODE) cout << "Initialize Jacobian structure (LM transition model)." << endl;
     Jacobian.Initialize(nPoint, nPointDomain, nVar, nVar, true, geometry, config, ReducerStrategy);
-
-    if (config->GetKind_Linear_Solver_Prec() == LINELET) {
-      nLineLets = Jacobian.BuildLineletPreconditioner(geometry, config);
-      if (rank == MASTER_NODE) cout << "Compute linelet structure. " << nLineLets << " elements in each line (average)." << endl;
-    }
-
     LinSysSol.Initialize(nPoint, nPointDomain, nVar, 0.0);
     LinSysRes.Initialize(nPoint, nPointDomain, nVar, 0.0);
     System.SetxIsZero(true);
@@ -176,7 +174,7 @@ CTransLMSolver::CTransLMSolver(CGeometry *geometry, CConfig *config, unsigned sh
 
 void CTransLMSolver::Preprocessing(CGeometry *geometry, CSolver **solver_container, CConfig *config,
          unsigned short iMesh, unsigned short iRKStep, unsigned short RunTime_EqSystem, bool Output) {
-  config->SetGlobalParam(config->GetKind_Solver(), RunTime_EqSystem);
+  SU2_OMP_SAFE_GLOBAL_ACCESS(config->SetGlobalParam(config->GetKind_Solver(), RunTime_EqSystem);)
 
   /*--- Upwind second order reconstruction and gradients ---*/
   CommonPreprocessing(geometry, config, Output);
@@ -195,43 +193,61 @@ void CTransLMSolver::Postprocessing(CGeometry *geometry, CSolver **solver_contai
 
   AD::StartNoSharedReading();
   auto* flowNodes = su2staticcast_p<CFlowVariable*>(solver_container[FLOW_SOL]->GetNodes());
+  auto* turbNodes = su2staticcast_p<CTurbVariable*>(solver_container[TURB_SOL]->GetNodes());
 
   SU2_OMP_FOR_STAT(omp_chunk_size)
   for (unsigned long iPoint = 0; iPoint < nPoint; iPoint ++) {
 
+    // Here the nodes already have the new solution, thus I have to compute everything from scratch
+
     const su2double rho = flowNodes->GetDensity(iPoint);
     const su2double mu  = flowNodes->GetLaminarViscosity(iPoint);
+    const su2double muT = turbNodes->GetmuT(iPoint);
     const su2double dist = geometry->nodes->GetWall_Distance(iPoint);
     su2double VorticityMag = GeometryToolbox::Norm(3, flowNodes->GetVorticity(iPoint));
     su2double StrainMag =flowNodes->GetStrainMag(iPoint);
     VorticityMag = max(VorticityMag, 1e-12);
     StrainMag = max(StrainMag, 1e-12); // safety against division by zero
-    const su2double Intermittecy = nodes->GetSolution(iPoint,0);
+    const su2double Intermittency = nodes->GetSolution(iPoint,0);
     const su2double Re_t = nodes->GetSolution(iPoint,1);
     const su2double Re_v = rho*dist*dist*StrainMag/mu;
-    const su2double omega = solver_container[TURB_SOL]->GetNodes()->GetSolution(iPoint,1);
-    const su2double k = solver_container[TURB_SOL]->GetNodes()->GetSolution(iPoint,0);
-
-    su2double Corr_Rec = 0.0;
-    if(Re_t <= 1870){
-     Corr_Rec = Re_t - (396.035e-02 + (-120.656e-04)*Re_t + (868.230e-06)*pow(Re_t, 2.)
-                                +( -696.506e-09)*pow(Re_t, 3.) + (174.105e-12)*pow(Re_t, 4.));
-    } else {
-     Corr_Rec = Re_t - ( 593.11 + (Re_t - 1870.0) * 0.482);
-    }
-
-    const su2double R_t = rho*k/ mu/ omega;
-    const su2double f_reattach = exp(-pow(R_t/20,4));
-    const su2double re_omega = rho*omega*dist*dist/mu;
-    const su2double f_wake = exp(-pow(re_omega/(1.0e+05),2));
     const su2double vel_u = flowNodes->GetVelocity(iPoint, 0);
     const su2double vel_v = flowNodes->GetVelocity(iPoint, 1);
     const su2double vel_w = (nDim ==3) ? flowNodes->GetVelocity(iPoint, 2) : 0.0;
     const su2double VelocityMag = sqrt(vel_u*vel_u + vel_v*vel_v + vel_w*vel_w);
+    su2double omega = 0.0;
+    su2double k = 0.0;
+    if(TurbFamily == TURB_FAMILY::KW){
+      omega = turbNodes->GetSolution(iPoint,1);
+      k = turbNodes->GetSolution(iPoint,0);
+    }
+    su2double Tu = 1.0;
+    if(TurbFamily == TURB_FAMILY::KW)
+      Tu = max(100.0*sqrt( 2.0 * k / 3.0 ) / VelocityMag,0.027);
+    if(TurbFamily == TURB_FAMILY::SA)
+      Tu = config->GetTurbulenceIntensity_FreeStream()*100;
+
+    const su2double Corr_Rec = TransCorrelations.ReThetaC_Correlations(Tu, Re_t);
+
+    su2double R_t = 1.0;
+    if(TurbFamily == TURB_FAMILY::KW)
+      R_t = rho*k/ mu/ omega;
+    if(TurbFamily == TURB_FAMILY::SA)
+      R_t = muT/ mu;
+
+    const su2double f_reattach = exp(-pow(R_t/20,4));
+    su2double f_wake = 0.0;
+    if(TurbFamily == TURB_FAMILY::KW){
+      const su2double re_omega = rho*omega*dist*dist/mu;
+      f_wake = exp(-pow(re_omega/(1.0e+05),2));
+    }
+    if(TurbFamily == TURB_FAMILY::SA)
+      f_wake = 1.0;
+
     const su2double theta_bl   = Re_t*mu / rho /VelocityMag;
     const su2double delta_bl   = 7.5*theta_bl;
     const su2double delta      = 50.0*VorticityMag*dist/VelocityMag*delta_bl + 1e-20;
-    const su2double var1 = (Intermittecy-1.0/50.0)/(1.0-1.0/50.0);
+    const su2double var1 = (Intermittency-1.0/50.0)/(1.0-1.0/50.0);
     const su2double var2 = 1.0 - pow(var1,2.0);
     const su2double f_theta = min(max(f_wake*exp(-pow(dist/delta, 4)), var2), 1.0);
     su2double Intermittency_Sep = 2.0*max(0.0, Re_v/(3.235*Corr_Rec)-1.0)*f_reattach;
@@ -314,9 +330,14 @@ void CTransLMSolver::Source_Residual(CGeometry *geometry, CSolver **solver_conta
 
     numerics->SetStrainMag(flowNodes->GetStrainMag(iPoint), 0.0);
 
-    /*--- Set coordnate (for debugging) ---*/
+    /*--- Set coordinate (for debugging) ---*/
     numerics->SetCoord(geometry->nodes->GetCoord(iPoint), nullptr);
 
+    if (options.LM2015) {
+      /*--- Set local grid length (for LM2015)*/
+      numerics->SetLocalGridLength(geometry->nodes->GetMaxLength(iPoint));
+    }
+
     /*--- Compute the source term ---*/
 
     auto residual = numerics->ComputeResidual(config);
@@ -554,6 +575,7 @@ void CTransLMSolver::LoadRestart(CGeometry** geometry, CSolver*** solver, CConfi
   /*--- Interpolate the solution down to the coarse multigrid levels ---*/
 
   for (auto iMesh = 1u; iMesh <= config->GetnMGLevels(); iMesh++) {
+
     MultigridRestriction(*geometry[iMesh - 1], solver[iMesh - 1][TRANS_SOL]->GetNodes()->GetSolution(),
                          *geometry[iMesh], solver[iMesh][TRANS_SOL]->GetNodes()->GetSolution());
     solver[iMesh][TRANS_SOL]->InitiateComms(geometry[iMesh], config, SOLUTION);
diff --git a/SU2_CFD/src/solvers/CTurbSASolver.cpp b/SU2_CFD/src/solvers/CTurbSASolver.cpp
index 2913591606a..30d7308cd2e 100644
--- a/SU2_CFD/src/solvers/CTurbSASolver.cpp
+++ b/SU2_CFD/src/solvers/CTurbSASolver.cpp
@@ -2,7 +2,7 @@
  * \file CTurbSASolver.cpp
  * \brief Main subroutines of CTurbSASolver class
  * \author F. Palacios, A. Bueno
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -34,8 +34,6 @@
 
 CTurbSASolver::CTurbSASolver(CGeometry *geometry, CConfig *config, unsigned short iMesh, CFluidModel* FluidModel)
              : CTurbSolver(geometry, config, false) {
-
-  unsigned short nLineLets;
   unsigned long iPoint;
   su2double Density_Inf, Viscosity_Inf, Factor_nu_Inf, Factor_nu_Engine, Factor_nu_ActDisk;
 
@@ -71,12 +69,6 @@ CTurbSASolver::CTurbSASolver(CGeometry *geometry, CConfig *config, unsigned shor
 
     if (rank == MASTER_NODE) cout << "Initialize Jacobian structure (SA model)." << endl;
     Jacobian.Initialize(nPoint, nPointDomain, nVar, nVar, true, geometry, config, ReducerStrategy);
-
-    if (config->GetKind_Linear_Solver_Prec() == LINELET) {
-      nLineLets = Jacobian.BuildLineletPreconditioner(geometry, config);
-      if (rank == MASTER_NODE) cout << "Compute linelet structure. " << nLineLets << " elements in each line (average)." << endl;
-    }
-
     LinSysSol.Initialize(nPoint, nPointDomain, nVar, 0.0);
     LinSysRes.Initialize(nPoint, nPointDomain, nVar, 0.0);
     System.SetxIsZero(true);
@@ -250,6 +242,52 @@ void CTurbSASolver::Postprocessing(CGeometry *geometry, CSolver **solver_contain
   }
   END_SU2_OMP_FOR
 
+
+  /*--- Compute turbulence index ---*/
+  if (config->GetKind_Trans_Model() != TURB_TRANS_MODEL::NONE || config->GetSAParsedOptions().bc) {
+    auto* flowNodes = su2staticcast_p<CFlowVariable*>(solver_container[FLOW_SOL]->GetNodes());
+
+    for (auto iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++){
+      if (config->GetViscous_Wall(iMarker)) {
+        SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
+        for (auto iVertex = 0u; iVertex < geometry->nVertex[iMarker]; iVertex++) {
+          const auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+
+          /*--- Check if the node belongs to the domain (i.e, not a halo node) ---*/
+
+          if (geometry->nodes->GetDomain(iPoint)) {
+            const auto jPoint = geometry->vertex[iMarker][iVertex]->GetNormal_Neighbor();
+
+            su2double FrictionVelocity = 0.0;
+            /*--- Formulation varies for 2D and 3D problems: in 3D the friction velocity is assumed to be sqrt(mu * |Omega|)
+            (provided by the reference paper https://doi.org/10.2514/6.1992-439), whereas in 2D we have to use the
+            standard definition sqrt(c_f / rho) since Omega = 0.  ---*/
+            if(nDim == 2){
+              su2double shearStress = 0.0;
+              for(auto iDim = 0u; iDim < nDim; iDim++) {
+                shearStress += pow(solver_container[FLOW_SOL]->GetCSkinFriction(iMarker, iVertex, iDim), 2.0);
+              }
+              shearStress = sqrt(shearStress);
+
+              FrictionVelocity = sqrt(shearStress/flowNodes->GetDensity(iPoint));
+            } else {
+              su2double VorticityMag = max(GeometryToolbox::Norm(3, flowNodes->GetVorticity(iPoint)), 1e-12);
+              FrictionVelocity = sqrt(flowNodes->GetLaminarViscosity(iPoint)*VorticityMag);
+            }
+
+            const su2double wall_dist = geometry->nodes->GetWall_Distance(jPoint);
+            const su2double Derivative = nodes->GetSolution(jPoint, 0) / wall_dist;
+            const su2double turbulence_index = Derivative / (FrictionVelocity * 0.41);
+
+            nodes->SetTurbIndex(iPoint, turbulence_index);
+
+          }
+        }
+        END_SU2_OMP_FOR
+      }
+    }
+  }
+
   AD::EndNoSharedReading();
 }
 
@@ -338,14 +376,21 @@ void CTurbSASolver::Source_Residual(CGeometry *geometry, CSolver **solver_contai
 
     }
 
+    /*--- Effective Intermittency ---*/
+
+    if (config->GetKind_Trans_Model() != TURB_TRANS_MODEL::NONE) {
+      numerics->SetIntermittencyEff(solver_container[TRANS_SOL]->GetNodes()->GetIntermittencyEff(iPoint));
+      numerics->SetIntermittency(solver_container[TRANS_SOL]->GetNodes()->GetSolution(iPoint, 0));
+    }
+
     /*--- Compute the source term ---*/
 
     auto residual = numerics->ComputeResidual(config);
 
     /*--- Store the intermittency ---*/
 
-    if (transition_BC) {
-      nodes->SetGammaBC(iPoint,numerics->GetGammaBC());
+    if (transition_BC || config->GetKind_Trans_Model() != TURB_TRANS_MODEL::NONE) {
+      nodes->SetIntermittency(iPoint,numerics->GetIntermittencyEff());
     }
 
     /*--- Subtract residual and the Jacobian ---*/
diff --git a/SU2_CFD/src/solvers/CTurbSSTSolver.cpp b/SU2_CFD/src/solvers/CTurbSSTSolver.cpp
index a3c7e8d4f49..c2f1983cd73 100644
--- a/SU2_CFD/src/solvers/CTurbSSTSolver.cpp
+++ b/SU2_CFD/src/solvers/CTurbSSTSolver.cpp
@@ -2,7 +2,7 @@
  * \file CTurbSSTSolver.cpp
  * \brief Main subroutines of CTurbSSTSolver class
  * \author F. Palacios, A. Bueno
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -34,7 +34,6 @@
 
 CTurbSSTSolver::CTurbSSTSolver(CGeometry *geometry, CConfig *config, unsigned short iMesh)
     : CTurbSolver(geometry, config, true) {
-  unsigned short nLineLets;
   unsigned long iPoint;
   ifstream restart_file;
   string text_line;
@@ -72,12 +71,6 @@ CTurbSSTSolver::CTurbSSTSolver(CGeometry *geometry, CConfig *config, unsigned sh
 
     if (rank == MASTER_NODE) cout << "Initialize Jacobian structure (SST model)." << endl;
     Jacobian.Initialize(nPoint, nPointDomain, nVar, nVar, true, geometry, config, ReducerStrategy);
-
-    if (config->GetKind_Linear_Solver_Prec() == LINELET) {
-      nLineLets = Jacobian.BuildLineletPreconditioner(geometry, config);
-      if (rank == MASTER_NODE) cout << "Compute linelet structure. " << nLineLets << " elements in each line (average)." << endl;
-    }
-
     LinSysSol.Initialize(nPoint, nPointDomain, nVar, 0.0);
     LinSysRes.Initialize(nPoint, nPointDomain, nVar, 0.0);
     System.SetxIsZero(true);
@@ -246,6 +239,40 @@ void CTurbSSTSolver::Postprocessing(CGeometry *geometry, CSolver **solver_contai
   }
   END_SU2_OMP_FOR
 
+
+  /*--- Compute turbulence index ---*/
+  if (config->GetKind_Trans_Model() != TURB_TRANS_MODEL::NONE) {
+    for (auto iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++)
+      if (config->GetViscous_Wall(iMarker)) {
+        SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
+        for (auto iVertex = 0u; iVertex < geometry->nVertex[iMarker]; iVertex++) {
+          const auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+
+          /*--- Check if the node belongs to the domain (i.e, not a halo node) ---*/
+
+          if (geometry->nodes->GetDomain(iPoint)) {
+            const auto jPoint = geometry->vertex[iMarker][iVertex]->GetNormal_Neighbor();
+
+            su2double shearStress = 0.0;
+            for(auto iDim = 0u; iDim < nDim; iDim++) {
+              shearStress += pow(solver_container[FLOW_SOL]->GetCSkinFriction(iMarker, iVertex, iDim), 2.0);
+            }
+            shearStress = sqrt(shearStress);
+
+            const su2double FrictionVelocity = sqrt(shearStress/flowNodes->GetDensity(iPoint));
+            const su2double wall_dist = geometry->nodes->GetWall_Distance(jPoint);
+            const su2double Derivative = flowNodes->GetLaminarViscosity(jPoint) * pow(nodes->GetSolution(jPoint, 0), 0.673) / wall_dist;
+            const su2double turbulence_index = 6.1 * Derivative / pow(FrictionVelocity, 2.346);
+
+            nodes->SetTurbIndex(iPoint, turbulence_index);
+
+          }
+        }
+        END_SU2_OMP_FOR
+      }
+  }
+
+
   AD::EndNoSharedReading();
 }
 
@@ -322,8 +349,7 @@ void CTurbSSTSolver::Source_Residual(CGeometry *geometry, CSolver **solver_conta
     numerics->SetCrossDiff(nodes->GetCrossDiff(iPoint));
 
     /*--- Effective Intermittency ---*/
-
-    if (TURB_TRANS_MODEL::LM == config->GetKind_Trans_Model()) {
+    if (config->GetKind_Trans_Model() == TURB_TRANS_MODEL::LM) {
       numerics->SetIntermittencyEff(solver_container[TRANS_SOL]->GetNodes()->GetIntermittencyEff(iPoint));
     }
 
@@ -336,6 +362,12 @@ void CTurbSSTSolver::Source_Residual(CGeometry *geometry, CSolver **solver_conta
 
     auto residual = numerics->ComputeResidual(config);
 
+    /*--- Store the intermittency ---*/
+
+    if (config->GetKind_Trans_Model() != TURB_TRANS_MODEL::NONE) {
+      nodes->SetIntermittency(iPoint, numerics->GetIntermittencyEff());
+    }
+
     /*--- Subtract residual and the Jacobian ---*/
 
     LinSysRes.SubtractBlock(iPoint, residual);
diff --git a/SU2_CFD/src/solvers/CTurbSolver.cpp b/SU2_CFD/src/solvers/CTurbSolver.cpp
index 035acd9f2e3..06b000bc46d 100644
--- a/SU2_CFD/src/solvers/CTurbSolver.cpp
+++ b/SU2_CFD/src/solvers/CTurbSolver.cpp
@@ -2,7 +2,7 @@
  * \file CTurbSolver.cpp
  * \brief Main subroutines of CTurbSolver class
  * \author F. Palacios, A. Bueno
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CAdjEulerVariable.cpp b/SU2_CFD/src/variables/CAdjEulerVariable.cpp
index 7bde7b6c0eb..628bfac6985 100644
--- a/SU2_CFD/src/variables/CAdjEulerVariable.cpp
+++ b/SU2_CFD/src/variables/CAdjEulerVariable.cpp
@@ -2,7 +2,7 @@
  * \file CAdjEulerVariable.cpp
  * \brief Definition of the solution fields.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CAdjNSVariable.cpp b/SU2_CFD/src/variables/CAdjNSVariable.cpp
index e4873aff720..8654a2a3aac 100644
--- a/SU2_CFD/src/variables/CAdjNSVariable.cpp
+++ b/SU2_CFD/src/variables/CAdjNSVariable.cpp
@@ -2,7 +2,7 @@
  * \file CAdjNSVariable.cpp
  * \brief Definition of the solution fields.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CAdjTurbVariable.cpp b/SU2_CFD/src/variables/CAdjTurbVariable.cpp
index d52bfcbd5e7..ecb99adcf88 100644
--- a/SU2_CFD/src/variables/CAdjTurbVariable.cpp
+++ b/SU2_CFD/src/variables/CAdjTurbVariable.cpp
@@ -2,7 +2,7 @@
  * \file CAdjTurbVariable.cpp
  * \brief Definition of the solution fields.
  * \author F. Palacios, A. Bueno
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CBaselineVariable.cpp b/SU2_CFD/src/variables/CBaselineVariable.cpp
index 66b957eec35..bb962db9b8e 100644
--- a/SU2_CFD/src/variables/CBaselineVariable.cpp
+++ b/SU2_CFD/src/variables/CBaselineVariable.cpp
@@ -2,7 +2,7 @@
  * \file CBaselineVariable.cpp
  * \brief Definition of the solution fields.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CDiscAdjFEABoundVariable.cpp b/SU2_CFD/src/variables/CDiscAdjFEABoundVariable.cpp
index 7e248790f14..b3f17c7fb11 100644
--- a/SU2_CFD/src/variables/CDiscAdjFEABoundVariable.cpp
+++ b/SU2_CFD/src/variables/CDiscAdjFEABoundVariable.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjFEAVariable.cpp
  * \brief Definition of the variables for FEM adjoint elastic structural problems.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CDiscAdjMeshBoundVariable.cpp b/SU2_CFD/src/variables/CDiscAdjMeshBoundVariable.cpp
index 4fc72f3614a..6eb634a9c4f 100644
--- a/SU2_CFD/src/variables/CDiscAdjMeshBoundVariable.cpp
+++ b/SU2_CFD/src/variables/CDiscAdjMeshBoundVariable.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjMeshVariable.cpp
  * \brief Main subroutines for the discrete adjoint mesh variable structure.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CDiscAdjVariable.cpp b/SU2_CFD/src/variables/CDiscAdjVariable.cpp
index 25954093036..497ade11dd3 100644
--- a/SU2_CFD/src/variables/CDiscAdjVariable.cpp
+++ b/SU2_CFD/src/variables/CDiscAdjVariable.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjVariable.cpp
  * \brief Main subroutines for the discrete adjoint variable structure.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CEulerVariable.cpp b/SU2_CFD/src/variables/CEulerVariable.cpp
index 30ffcc08242..f7b4e17e1b4 100644
--- a/SU2_CFD/src/variables/CEulerVariable.cpp
+++ b/SU2_CFD/src/variables/CEulerVariable.cpp
@@ -2,7 +2,7 @@
  * \file CEulerVariable.cpp
  * \brief Definition of the solution fields.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -72,6 +72,12 @@ CEulerVariable::CEulerVariable(su2double density, const su2double *velocity, su2
     WindGust.resize(nPoint,nDim);
     WindGustDer.resize(nPoint,nDim+1);
   }
+
+  if (config->GetVorticityConfinement()) {
+    nAuxVar = 1;
+    Grad_AuxVar.resize(nPoint, nAuxVar, nDim, 0.0);
+    AuxVar.resize(nPoint, nAuxVar) = su2double(0.0);
+  }
 }
 
 bool CEulerVariable::SetPrimVar(unsigned long iPoint, CFluidModel *FluidModel) {
diff --git a/SU2_CFD/src/variables/CFEABoundVariable.cpp b/SU2_CFD/src/variables/CFEABoundVariable.cpp
index 6b72de425e2..94940b8c952 100644
--- a/SU2_CFD/src/variables/CFEABoundVariable.cpp
+++ b/SU2_CFD/src/variables/CFEABoundVariable.cpp
@@ -2,7 +2,7 @@
  * \file CFEABoundVariable.cpp
  * \brief Definition of the variables for FEM elastic structural problems.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CFEAVariable.cpp b/SU2_CFD/src/variables/CFEAVariable.cpp
index 8633398051f..633d94efb1d 100644
--- a/SU2_CFD/src/variables/CFEAVariable.cpp
+++ b/SU2_CFD/src/variables/CFEAVariable.cpp
@@ -2,7 +2,7 @@
  * \file CFEAVariable.cpp
  * \brief Definition of the variables for FEM elastic structural problems.
  * \author R. Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CFlowVariable.cpp b/SU2_CFD/src/variables/CFlowVariable.cpp
index 6feeaccdd52..261e94cabba 100644
--- a/SU2_CFD/src/variables/CFlowVariable.cpp
+++ b/SU2_CFD/src/variables/CFlowVariable.cpp
@@ -1,7 +1,7 @@
 /*!
  * \file CFlowVariable.cpp
  * \brief Definition of common solution fields for flow solvers.
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CHeatVariable.cpp b/SU2_CFD/src/variables/CHeatVariable.cpp
index 9802e8d26a1..1f696a2f66f 100644
--- a/SU2_CFD/src/variables/CHeatVariable.cpp
+++ b/SU2_CFD/src/variables/CHeatVariable.cpp
@@ -2,7 +2,7 @@
  * \file CHeatVariable.cpp
  * \brief Definition of the variables for heat equation problems.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -25,16 +25,13 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #include "../../include/variables/CHeatVariable.hpp"
 
-
 CHeatVariable::CHeatVariable(su2double heat, unsigned long npoint, unsigned long ndim, unsigned long nvar, CConfig *config)
-  : CVariable(npoint, ndim, nvar, config), Gradient_Reconstruction(config->GetReconstructionGradientRequired() ? Gradient_Aux : Gradient) {
+  : CScalarVariable(npoint, ndim, nvar, config) {
 
-  bool low_fidelity = false;
-  bool dual_time = ((config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
-                    (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND));
+  const bool dual_time = ((config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
+                          (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND));
 
   /*--- Initialization of heat variable ---*/
 
@@ -43,14 +40,14 @@ CHeatVariable::CHeatVariable(su2double heat, unsigned long npoint, unsigned long
 
   /*--- Allocate residual structures ---*/
 
-  Res_TruncError.resize(nPoint,nVar) = su2double(0.0);
+  Res_TruncError.resize(nPoint, nVar) = su2double(0.0);
 
   /*--- Only for residual smoothing (multigrid) ---*/
 
   for (unsigned long iMesh = 0; iMesh <= config->GetnMGLevels(); iMesh++) {
-    if ((config->GetMG_CorrecSmooth(iMesh) > 0) || low_fidelity) {
-      Residual_Sum.resize(nPoint,nVar);
-      Residual_Old.resize(nPoint,nVar);
+    if (config->GetMG_CorrecSmooth(iMesh) > 0) {
+      Residual_Sum.resize(nPoint, nVar);
+      Residual_Old.resize(nPoint, nVar);
       break;
     }
   }
@@ -61,27 +58,11 @@ CHeatVariable::CHeatVariable(su2double heat, unsigned long npoint, unsigned long
     Solution_time_n1 = heat;
   }
 
-  /*--- Gradient related fields ---*/
-  Gradient.resize(nPoint,nVar,nDim,0.0);
-
-  if (config->GetReconstructionGradientRequired()) {
-    Gradient_Aux.resize(nPoint,nVar,nDim,0.0);
-  }
-
-  if (config->GetLeastSquaresRequired()) {
-    Rmatrix.resize(nPoint,nDim,nDim,0.0);
-  }
-
   if (config->GetKind_ConvNumScheme_Heat() == SPACE_CENTERED)
-    Undivided_Laplacian.resize(nPoint,nVar);
+    Undivided_Laplacian.resize(nPoint, nVar);
 
   Max_Lambda_Inv.resize(nPoint);
   Max_Lambda_Visc.resize(nPoint);
-  Delta_Time.resize(nPoint);
-
-  /* Under-relaxation parameter. */
-  UnderRelaxation.resize(nPoint) = su2double(1.0);
-  LocalCFL.resize(nPoint) = su2double(0.0);
 
   if (config->GetMultizone_Problem())
     Set_BGSSolution_k();
diff --git a/SU2_CFD/src/variables/CIncEulerVariable.cpp b/SU2_CFD/src/variables/CIncEulerVariable.cpp
index aa7eec96db1..df48f82da5c 100644
--- a/SU2_CFD/src/variables/CIncEulerVariable.cpp
+++ b/SU2_CFD/src/variables/CIncEulerVariable.cpp
@@ -2,7 +2,7 @@
  * \file CIncEulerVariable.cpp
  * \brief Definition of the variable classes for incompressible flow.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CIncNSVariable.cpp b/SU2_CFD/src/variables/CIncNSVariable.cpp
index 3c644ac13c0..a3458a9eb46 100644
--- a/SU2_CFD/src/variables/CIncNSVariable.cpp
+++ b/SU2_CFD/src/variables/CIncNSVariable.cpp
@@ -2,7 +2,7 @@
  * \file CIncNSVariable.cpp
  * \brief Definition of the variable classes for incompressible flow.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CMeshBoundVariable.cpp b/SU2_CFD/src/variables/CMeshBoundVariable.cpp
index 6bb5f97e1cd..568d7d12713 100644
--- a/SU2_CFD/src/variables/CMeshBoundVariable.cpp
+++ b/SU2_CFD/src/variables/CMeshBoundVariable.cpp
@@ -2,7 +2,7 @@
  * \file CMeshBoundVariable.cpp
  * \brief Definition of the boundary variables for mesh motion using a pseudo-elastic approach.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CMeshElement.cpp b/SU2_CFD/src/variables/CMeshElement.cpp
index 8fb48e2a6d4..aeabfcea921 100644
--- a/SU2_CFD/src/variables/CMeshElement.cpp
+++ b/SU2_CFD/src/variables/CMeshElement.cpp
@@ -2,7 +2,7 @@
  * \file CMeshElement.cpp
  * \brief Definition of the mesh elements for mesh deformation using a pseudo-elastic approach.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CMeshVariable.cpp b/SU2_CFD/src/variables/CMeshVariable.cpp
index dd1a85ae8ab..17e69a9376b 100644
--- a/SU2_CFD/src/variables/CMeshVariable.cpp
+++ b/SU2_CFD/src/variables/CMeshVariable.cpp
@@ -2,7 +2,7 @@
  * \file CMeshVariable.cpp
  * \brief Definition of the variables for mesh motion using a pseudo-elastic approach.
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CNEMOEulerVariable.cpp b/SU2_CFD/src/variables/CNEMOEulerVariable.cpp
index 22deb6b9f9a..e9026821d92 100644
--- a/SU2_CFD/src/variables/CNEMOEulerVariable.cpp
+++ b/SU2_CFD/src/variables/CNEMOEulerVariable.cpp
@@ -2,7 +2,7 @@
  * \file CNEMOEulerVariable.cpp
  * \brief Definition of the solution fields.
  * \author C. Garbacz, W. Maier, S.R. Copeland
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CNEMONSVariable.cpp b/SU2_CFD/src/variables/CNEMONSVariable.cpp
index 52c193a2765..00ebcb62029 100644
--- a/SU2_CFD/src/variables/CNEMONSVariable.cpp
+++ b/SU2_CFD/src/variables/CNEMONSVariable.cpp
@@ -2,7 +2,7 @@
  * \file CNEMONSVariable.cpp
  * \brief Definition of the solution fields.
  * \author C. Garbacz, W. Maier, S.R. Copeland
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CNSVariable.cpp b/SU2_CFD/src/variables/CNSVariable.cpp
index 11221a34eae..cbc52de9673 100644
--- a/SU2_CFD/src/variables/CNSVariable.cpp
+++ b/SU2_CFD/src/variables/CNSVariable.cpp
@@ -2,7 +2,7 @@
  * \file CNSVariable.cpp
  * \brief Definition of the solution fields.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CRadP1Variable.cpp b/SU2_CFD/src/variables/CRadP1Variable.cpp
index ac7f579fe6c..c380cc67507 100644
--- a/SU2_CFD/src/variables/CRadP1Variable.cpp
+++ b/SU2_CFD/src/variables/CRadP1Variable.cpp
@@ -2,7 +2,7 @@
  * \file CRadP1Variable.cpp
  * \brief Definition of the P1 model variables
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CRadVariable.cpp b/SU2_CFD/src/variables/CRadVariable.cpp
index c67bf8c41ff..a681ee0c8fe 100644
--- a/SU2_CFD/src/variables/CRadVariable.cpp
+++ b/SU2_CFD/src/variables/CRadVariable.cpp
@@ -2,7 +2,7 @@
  * \file CRadVariable.cpp
  * \brief Definition of the radiation variables
  * \author Ruben Sanchez
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CScalarVariable.cpp b/SU2_CFD/src/variables/CScalarVariable.cpp
index 3a333c5fe30..8ce392aab6b 100644
--- a/SU2_CFD/src/variables/CScalarVariable.cpp
+++ b/SU2_CFD/src/variables/CScalarVariable.cpp
@@ -2,7 +2,7 @@
  * \file CScalarVariable.cpp
  * \brief Definition of the solution fields.
  * \author F. Palacios, A. Bueno
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CSobolevSmoothingVariable.cpp b/SU2_CFD/src/variables/CSobolevSmoothingVariable.cpp
index 275f3207095..d9c18c7d20d 100644
--- a/SU2_CFD/src/variables/CSobolevSmoothingVariable.cpp
+++ b/SU2_CFD/src/variables/CSobolevSmoothingVariable.cpp
@@ -2,7 +2,7 @@
  * \file CSobolevSmoothingVariable.cpp
  * \brief Definition of the variables for gradient smoothing problems.
  * \author T. Dick
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CSpeciesVariable.cpp b/SU2_CFD/src/variables/CSpeciesVariable.cpp
index 210ac62bdde..7a8a0787410 100644
--- a/SU2_CFD/src/variables/CSpeciesVariable.cpp
+++ b/SU2_CFD/src/variables/CSpeciesVariable.cpp
@@ -2,7 +2,7 @@
  * \file CSpeciesVariable.cpp
  * \brief Definition of the solution fields.
  * \author T. Kattmann
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CTransLMVariable.cpp b/SU2_CFD/src/variables/CTransLMVariable.cpp
index 0ef5e53a545..df345c23aef 100644
--- a/SU2_CFD/src/variables/CTransLMVariable.cpp
+++ b/SU2_CFD/src/variables/CTransLMVariable.cpp
@@ -2,7 +2,7 @@
  * \file CTransLMVariable.cpp
  * \brief Definition of the solution fields.
  * \author A. Aranake, S. Kang
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CTurbSAVariable.cpp b/SU2_CFD/src/variables/CTurbSAVariable.cpp
index 3d2ac8dfcfa..2779dc4fb8a 100644
--- a/SU2_CFD/src/variables/CTurbSAVariable.cpp
+++ b/SU2_CFD/src/variables/CTurbSAVariable.cpp
@@ -2,7 +2,7 @@
  * \file CTurbSAVariable.cpp
  * \brief Definition of the solution fields.
  * \author F. Palacios, A. Bueno
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -46,7 +46,6 @@ CTurbSAVariable::CTurbSAVariable(su2double val_nu_tilde, su2double val_muT, unsi
     Solution_time_n1 = Solution;
   }
 
-  gamma_BC.resize(nPoint);
   DES_LengthScale.resize(nPoint) = su2double(0.0);
   Vortex_Tilting.resize(nPoint);
 }
diff --git a/SU2_CFD/src/variables/CTurbSSTVariable.cpp b/SU2_CFD/src/variables/CTurbSSTVariable.cpp
index a4c37d52e17..c4506529d10 100644
--- a/SU2_CFD/src/variables/CTurbSSTVariable.cpp
+++ b/SU2_CFD/src/variables/CTurbSSTVariable.cpp
@@ -2,7 +2,7 @@
  * \file CTurbSSTVariable.cpp
  * \brief Definition of the solution fields.
  * \author F. Palacios, A. Bueno
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CTurbVariable.cpp b/SU2_CFD/src/variables/CTurbVariable.cpp
index 6fa45ff1d07..a1035f922db 100644
--- a/SU2_CFD/src/variables/CTurbVariable.cpp
+++ b/SU2_CFD/src/variables/CTurbVariable.cpp
@@ -2,7 +2,7 @@
  * \file CTurbVariable.cpp
  * \brief Definition of the solution fields.
  * \author F. Palacios, A. Bueno
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -30,4 +30,9 @@
 
 
 CTurbVariable::CTurbVariable(unsigned long npoint, unsigned long ndim, unsigned long nvar, CConfig *config)
-  : CScalarVariable(npoint, ndim, nvar, config) { }
+  : CScalarVariable(npoint, ndim, nvar, config) {
+
+    turb_index.resize(nPoint) = su2double(1.0);
+    intermittency.resize(nPoint) = su2double(1.0);
+
+   }
diff --git a/SU2_CFD/src/variables/CVariable.cpp b/SU2_CFD/src/variables/CVariable.cpp
index a6eda70718f..c56ad1838e9 100644
--- a/SU2_CFD/src/variables/CVariable.cpp
+++ b/SU2_CFD/src/variables/CVariable.cpp
@@ -2,7 +2,7 @@
  * \file CVariable.cpp
  * \brief Definition of the solution fields.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_DEF/include/SU2_DEF.hpp b/SU2_DEF/include/SU2_DEF.hpp
index 46ebf3c0c2e..ee29a732ad9 100644
--- a/SU2_DEF/include/SU2_DEF.hpp
+++ b/SU2_DEF/include/SU2_DEF.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines of the code SU2_DEF.
  *        The subroutines and functions are in the <i>SU2_DEF.cpp</i> file.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_DEF/obj/Makefile.am b/SU2_DEF/obj/Makefile.am
index 84650dbad04..5081ba4fc04 100644
--- a/SU2_DEF/obj/Makefile.am
+++ b/SU2_DEF/obj/Makefile.am
@@ -3,7 +3,7 @@
 # \file Makefile.am
 # \brief Makefile for SU2_DEF
 # \author M. Colonno, T. Economon, F. Palacios
-# \version 7.4.0 "Blackbird"
+# \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_DEF/src/SU2_DEF.cpp b/SU2_DEF/src/SU2_DEF.cpp
index d6f853571c8..d50ef1fc374 100644
--- a/SU2_DEF/src/SU2_DEF.cpp
+++ b/SU2_DEF/src/SU2_DEF.cpp
@@ -2,7 +2,7 @@
  * \file SU2_DEF.cpp
  * \brief Main file of Mesh Deformation Code (SU2_DEF).
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_DOT/include/SU2_DOT.hpp b/SU2_DOT/include/SU2_DOT.hpp
index a3942f6b0a3..a386e880c63 100644
--- a/SU2_DOT/include/SU2_DOT.hpp
+++ b/SU2_DOT/include/SU2_DOT.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines of the code SU2_DOT.
  *        The subroutines and functions are in the <i>SU2_DOT.cpp</i> file.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_DOT/obj/Makefile.am b/SU2_DOT/obj/Makefile.am
index 635f6a54938..e53553b1d41 100644
--- a/SU2_DOT/obj/Makefile.am
+++ b/SU2_DOT/obj/Makefile.am
@@ -3,7 +3,7 @@
 # \file Makefile.am
 # \brief Makefile for SU2_DOT
 # \author M. Colonno, T. Economon, F. Palacios
-# \version 7.4.0 "Blackbird"
+# \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_DOT/src/SU2_DOT.cpp b/SU2_DOT/src/SU2_DOT.cpp
index e15bd2af8ee..e1dd7355194 100644
--- a/SU2_DOT/src/SU2_DOT.cpp
+++ b/SU2_DOT/src/SU2_DOT.cpp
@@ -2,7 +2,7 @@
  * \file SU2_DOT.cpp
  * \brief Main file of the Gradient Projection Code (SU2_DOT).
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_GEO/include/SU2_GEO.hpp b/SU2_GEO/include/SU2_GEO.hpp
index 05e7422a688..2fcc154d90f 100644
--- a/SU2_GEO/include/SU2_GEO.hpp
+++ b/SU2_GEO/include/SU2_GEO.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines of the code SU2_GEO.
  *        The subroutines and functions are in the <i>SU2_GEO.cpp</i> file.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_GEO/obj/Makefile.am b/SU2_GEO/obj/Makefile.am
index 5fc074d5601..aea8c2931eb 100644
--- a/SU2_GEO/obj/Makefile.am
+++ b/SU2_GEO/obj/Makefile.am
@@ -3,7 +3,7 @@
 # \file Makefile.am
 # \brief Makefile for SU2_GEO
 # \author M. Colonno, T. Economon, F. Palacios
-# \version 7.4.0 "Blackbird"
+# \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_GEO/src/SU2_GEO.cpp b/SU2_GEO/src/SU2_GEO.cpp
index 509778f251d..99097964873 100644
--- a/SU2_GEO/src/SU2_GEO.cpp
+++ b/SU2_GEO/src/SU2_GEO.cpp
@@ -2,7 +2,7 @@
  * \file SU2_GEO.cpp
  * \brief Main file of the Geometry Definition Code (SU2_GEO).
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_PY/FSI_tools/FSIInterface.py b/SU2_PY/FSI_tools/FSIInterface.py
index d09fec9e5c2..e4e89dce7ce 100644
--- a/SU2_PY/FSI_tools/FSIInterface.py
+++ b/SU2_PY/FSI_tools/FSIInterface.py
@@ -3,7 +3,7 @@
 ## \file FSIInterface.py
 #  \brief FSI interface class that handles fluid/solid solvers synchronisation and communication.
 #  \authors Nicola Fonzi, Vittorio Cavalieri based on the work of David Thomas
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/FSI_tools/FSI_config.py b/SU2_PY/FSI_tools/FSI_config.py
index 1cf397f54ba..8bd7920dee1 100644
--- a/SU2_PY/FSI_tools/FSI_config.py
+++ b/SU2_PY/FSI_tools/FSI_config.py
@@ -3,7 +3,7 @@
 ## \file FSI_config.py
 #  \brief Python class for handling configuration file for FSI computation.
 #  \authors Nicola Fonzi, Vittorio Cavalieri based on the work of David Thomas
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/Makefile.am b/SU2_PY/Makefile.am
index cb7f1eca66e..8e0ab1f5dbf 100644
--- a/SU2_PY/Makefile.am
+++ b/SU2_PY/Makefile.am
@@ -3,7 +3,7 @@
 # \file Makefile.am
 # \brief Makefile for the SU2 Python framework
 # \author M. Colonno, T. Economon, F. Palacios, T. Lukaczyk
-# \version 7.4.0 "Blackbird"
+# \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/OptimalPropeller.py b/SU2_PY/OptimalPropeller.py
index 709096b1253..e3057d1d48a 100644
--- a/SU2_PY/OptimalPropeller.py
+++ b/SU2_PY/OptimalPropeller.py
@@ -1,7 +1,7 @@
 ## \file OptimalPropeller.py
 #  \brief Python script for generating the ActuatorDisk.dat file.
 #  \author E. Saetta, L. Russo, R. Tognaccini
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/eval/design.py b/SU2_PY/SU2/eval/design.py
index 4ffc1382e1e..69f5930ae59 100644
--- a/SU2_PY/SU2/eval/design.py
+++ b/SU2_PY/SU2/eval/design.py
@@ -3,7 +3,7 @@
 ## \file design.py
 #  \brief python package for designs
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/eval/functions.py b/SU2_PY/SU2/eval/functions.py
index 58d793b1ba1..fb767a87f66 100644
--- a/SU2_PY/SU2/eval/functions.py
+++ b/SU2_PY/SU2/eval/functions.py
@@ -3,7 +3,7 @@
 ## \file functions.py
 #  \brief python package for functions
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/eval/gradients.py b/SU2_PY/SU2/eval/gradients.py
index c784fef1106..2298a475999 100644
--- a/SU2_PY/SU2/eval/gradients.py
+++ b/SU2_PY/SU2/eval/gradients.py
@@ -3,7 +3,7 @@
 ## \file gradients.py
 #  \brief python package for gradients
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/io/config.py b/SU2_PY/SU2/io/config.py
index f887723947d..21fe28d79da 100755
--- a/SU2_PY/SU2/io/config.py
+++ b/SU2_PY/SU2/io/config.py
@@ -3,7 +3,7 @@
 ## \file config.py
 #  \brief python package for config 
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/io/config_options.py b/SU2_PY/SU2/io/config_options.py
index 991ca0b56a0..16d5ee9ee1a 100644
--- a/SU2_PY/SU2/io/config_options.py
+++ b/SU2_PY/SU2/io/config_options.py
@@ -1,7 +1,7 @@
 # \file config_options.py
 #  \brief python package for config
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/io/data.py b/SU2_PY/SU2/io/data.py
index 60c641d9c33..1454b983414 100644
--- a/SU2_PY/SU2/io/data.py
+++ b/SU2_PY/SU2/io/data.py
@@ -3,7 +3,7 @@
 ## \file data.py
 #  \brief python package for data utility functions 
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/io/filelock.py b/SU2_PY/SU2/io/filelock.py
index cf19b74683d..9b281b08304 100644
--- a/SU2_PY/SU2/io/filelock.py
+++ b/SU2_PY/SU2/io/filelock.py
@@ -3,7 +3,7 @@
 ## \file filelock.py
 #  \brief python package for filelocking 
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/io/redirect.py b/SU2_PY/SU2/io/redirect.py
index bbf5412df2b..548f93aa991 100644
--- a/SU2_PY/SU2/io/redirect.py
+++ b/SU2_PY/SU2/io/redirect.py
@@ -3,7 +3,7 @@
 ## \file redirect.py
 #  \brief python package for file redirection 
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/io/state.py b/SU2_PY/SU2/io/state.py
index 16977ded814..66bf2e9c51a 100644
--- a/SU2_PY/SU2/io/state.py
+++ b/SU2_PY/SU2/io/state.py
@@ -3,7 +3,7 @@
 ## \file state.py
 #  \brief python package for state 
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/io/tools.py b/SU2_PY/SU2/io/tools.py
index a3a6afea0b8..2522ff0c2f8 100755
--- a/SU2_PY/SU2/io/tools.py
+++ b/SU2_PY/SU2/io/tools.py
@@ -3,7 +3,7 @@
 ## \file tools.py
 #  \brief file i/o functions
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/opt/project.py b/SU2_PY/SU2/opt/project.py
index 5d144421cbf..486cc195667 100644
--- a/SU2_PY/SU2/opt/project.py
+++ b/SU2_PY/SU2/opt/project.py
@@ -3,7 +3,7 @@
 ## \file project.py
 #  \brief package for optimization projects
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/opt/scipy_tools.py b/SU2_PY/SU2/opt/scipy_tools.py
index b46df92ed79..cd931688a01 100644
--- a/SU2_PY/SU2/opt/scipy_tools.py
+++ b/SU2_PY/SU2/opt/scipy_tools.py
@@ -3,7 +3,7 @@
 ## \file scipy_tools.py
 #  \brief tools for interfacing with scipy
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/run/adjoint.py b/SU2_PY/SU2/run/adjoint.py
index 035c9fda9da..bdc1f416061 100644
--- a/SU2_PY/SU2/run/adjoint.py
+++ b/SU2_PY/SU2/run/adjoint.py
@@ -3,7 +3,7 @@
 ## \file adjoint.py
 #  \brief python package for running adjoint problems 
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/run/deform.py b/SU2_PY/SU2/run/deform.py
index 445397c924f..e742f6b0e2a 100644
--- a/SU2_PY/SU2/run/deform.py
+++ b/SU2_PY/SU2/run/deform.py
@@ -3,7 +3,7 @@
 ## \file deform.py
 #  \brief python package for deforming meshes
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/run/direct.py b/SU2_PY/SU2/run/direct.py
index 6632dd0dcab..520caf468ba 100644
--- a/SU2_PY/SU2/run/direct.py
+++ b/SU2_PY/SU2/run/direct.py
@@ -3,7 +3,7 @@
 ## \file direct.py
 #  \brief python package for running direct solutions
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/run/geometry.py b/SU2_PY/SU2/run/geometry.py
index 1fd77e1fd22..45296cf9509 100644
--- a/SU2_PY/SU2/run/geometry.py
+++ b/SU2_PY/SU2/run/geometry.py
@@ -3,7 +3,7 @@
 ## \file geometry.py
 #  \brief python package for running geometry analyses
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/run/interface.py b/SU2_PY/SU2/run/interface.py
index 548bf8eafaa..a0512d5aef3 100644
--- a/SU2_PY/SU2/run/interface.py
+++ b/SU2_PY/SU2/run/interface.py
@@ -3,7 +3,7 @@
 ## \file interface.py
 #  \brief python package interfacing with the SU2 suite
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/run/merge.py b/SU2_PY/SU2/run/merge.py
index 07e29a6ac52..65fa96db065 100644
--- a/SU2_PY/SU2/run/merge.py
+++ b/SU2_PY/SU2/run/merge.py
@@ -1,7 +1,7 @@
 ## \file merge.py
 #  \brief python package for merging meshes
 #  \author T. Economon, T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/run/projection.py b/SU2_PY/SU2/run/projection.py
index dc7c1a0340b..254db62ca29 100644
--- a/SU2_PY/SU2/run/projection.py
+++ b/SU2_PY/SU2/run/projection.py
@@ -3,7 +3,7 @@
 ## \file projection.py
 #  \brief python package for running gradient projection
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/util/filter_adjoint.py b/SU2_PY/SU2/util/filter_adjoint.py
index f693ec618bf..da73328a37e 100644
--- a/SU2_PY/SU2/util/filter_adjoint.py
+++ b/SU2_PY/SU2/util/filter_adjoint.py
@@ -3,7 +3,7 @@
 ## \file filter_adjoint.py
 #  \brief Applies various filters to the adjoint surface sensitivities of an airfoil
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/util/plot.py b/SU2_PY/SU2/util/plot.py
index 366d8a8314e..aef78d6e7bf 100644
--- a/SU2_PY/SU2/util/plot.py
+++ b/SU2_PY/SU2/util/plot.py
@@ -3,7 +3,7 @@
 ## \file plot.py
 #  \brief python package for plotting
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/util/polarSweepLib.py b/SU2_PY/SU2/util/polarSweepLib.py
index bed78770927..729232a4412 100755
--- a/SU2_PY/SU2/util/polarSweepLib.py
+++ b/SU2_PY/SU2/util/polarSweepLib.py
@@ -2,7 +2,7 @@
 # \file polarSweepLib.py
 #  \brief Functions library for compute_polar.py script.
 #  \author E Arad
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2/util/which.py b/SU2_PY/SU2/util/which.py
index efe0a9297fb..ec79e78b9b8 100644
--- a/SU2_PY/SU2/util/which.py
+++ b/SU2_PY/SU2/util/which.py
@@ -3,7 +3,7 @@
 ## \file which.py
 #  \brief looks for where a program is
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2_CFD.py b/SU2_PY/SU2_CFD.py
index 98e9d70a6f4..1d71584278c 100755
--- a/SU2_PY/SU2_CFD.py
+++ b/SU2_PY/SU2_CFD.py
@@ -3,7 +3,7 @@
 ## \file SU2_CFD.py
 #  \brief Python script to launch SU2_CFD through the Python Wrapper.
 #  \author David Thomas
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/SU2_Nastran/pysu2_nastran.py b/SU2_PY/SU2_Nastran/pysu2_nastran.py
index f2ba4183527..6647c23b372 100644
--- a/SU2_PY/SU2_Nastran/pysu2_nastran.py
+++ b/SU2_PY/SU2_Nastran/pysu2_nastran.py
@@ -3,7 +3,7 @@
 ## \file pysu2_nastran.py
 #  \brief Structural solver using Nastran models
 #  \authors Nicola Fonzi, Vittorio Cavalieri, based on the work of David Thomas
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/change_version_number.py b/SU2_PY/change_version_number.py
index 4201a2f41ab..715bcbf996a 100755
--- a/SU2_PY/change_version_number.py
+++ b/SU2_PY/change_version_number.py
@@ -3,7 +3,7 @@
 ## \file change_version_number.py
 #  \brief Python script for updating the version number of the SU2 suite.
 #  \author A. Aranake
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
@@ -42,8 +42,8 @@
 if not options.version:
     parser.error("new version number must be provided with -v option")
 
-oldvers  = '7.4.0 "Blackbird"'
-oldvers_q= r'7.4.0 \"Blackbird\"'
+oldvers  = '7.5.0 "Blackbird"'
+oldvers_q= r'7.5.0 \"Blackbird\"'
 newvers  = str(options.version) + ' "' + str(options.releasename) + '"'
 newvers_q= str(options.version) + ' \\"' + str(options.releasename) + '\\"'
 #oldvers = 'Copyright 2012-2022, SU2'
diff --git a/SU2_PY/compute_multipoint.py b/SU2_PY/compute_multipoint.py
index ddae9ce2b93..32966f00b89 100755
--- a/SU2_PY/compute_multipoint.py
+++ b/SU2_PY/compute_multipoint.py
@@ -3,7 +3,7 @@
 ## \file Compute_multipoint.py
 #  \brief Python script for performing a multipoint design.
 #  \author Indiana Stokes
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/compute_polar.py b/SU2_PY/compute_polar.py
index fd0ad527b21..4f0d5712cf7 100755
--- a/SU2_PY/compute_polar.py
+++ b/SU2_PY/compute_polar.py
@@ -3,7 +3,7 @@
 ## \file Compute_polar.py
 #  \brief Python script for performing polar sweep.
 #  \author E Arad (based on T. Lukaczyk and  F. Palacios script)
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/compute_stability.py b/SU2_PY/compute_stability.py
index 67c504e7319..cf7b19d72b2 100755
--- a/SU2_PY/compute_stability.py
+++ b/SU2_PY/compute_stability.py
@@ -3,7 +3,7 @@
 ## \file compute_stability.py
 #  \brief Python script for performing the shape optimization.
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/compute_uncertainty.py b/SU2_PY/compute_uncertainty.py
index eca3a775c6e..a55f0ccee2a 100755
--- a/SU2_PY/compute_uncertainty.py
+++ b/SU2_PY/compute_uncertainty.py
@@ -3,7 +3,7 @@
 ## \file compute_uncertainty.py
 #  \brief Python script for performing model-form UQ for SST turbulence model
 #  \author J. Mukhopadhaya
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/config_gui.py b/SU2_PY/config_gui.py
index 90755201249..0f7caf1c82b 100755
--- a/SU2_PY/config_gui.py
+++ b/SU2_PY/config_gui.py
@@ -3,7 +3,7 @@
 ## \file config_gui.py
 #  \brief _____________.
 #  \author A. Aranake
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/continuous_adjoint.py b/SU2_PY/continuous_adjoint.py
index 931bd8b54fc..7e24facc3bc 100755
--- a/SU2_PY/continuous_adjoint.py
+++ b/SU2_PY/continuous_adjoint.py
@@ -3,7 +3,7 @@
 ## \file continuous_adjoint.py
 #  \brief Python script for continuous adjoint computation using the SU2 suite.
 #  \author F. Palacios, T. Economon, T. Lukaczyk
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/convert_to_csv.py b/SU2_PY/convert_to_csv.py
index fa3428c2f82..5a064673eb8 100755
--- a/SU2_PY/convert_to_csv.py
+++ b/SU2_PY/convert_to_csv.py
@@ -3,7 +3,7 @@
 ## \file convert_to_csv.py
 #  \brief This script converts SU2 ASCII restart files generated with a version prior v7 to the CSV format
 #  \author T. Albring
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/direct_differentiation.py b/SU2_PY/direct_differentiation.py
index 5873ea5d5f6..3e17188ec63 100755
--- a/SU2_PY/direct_differentiation.py
+++ b/SU2_PY/direct_differentiation.py
@@ -3,7 +3,7 @@
 ## \file direct_differentiation.py
 #  \brief Python script for doing the direct differentiation computation using the SU2 suite.
 #  \author F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/discrete_adjoint.py b/SU2_PY/discrete_adjoint.py
index c599ec8ccfa..55a857b4b3d 100755
--- a/SU2_PY/discrete_adjoint.py
+++ b/SU2_PY/discrete_adjoint.py
@@ -3,7 +3,7 @@
 ## \file discrete_adjoint.py
 #  \brief Python script for doing the discrete adjoint computation using the SU2 suite.
 #  \author F. Palacios, T. Economon, T. Lukaczyk
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/finite_differences.py b/SU2_PY/finite_differences.py
index 6a762769509..cf4ffcecda5 100755
--- a/SU2_PY/finite_differences.py
+++ b/SU2_PY/finite_differences.py
@@ -3,7 +3,7 @@
 ## \file finite_differences.py
 #  \brief Python script for doing the finite differences computation using the SU2 suite.
 #  \author F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/fsi_computation.py b/SU2_PY/fsi_computation.py
index 7caf6aedac3..84bc07d200a 100644
--- a/SU2_PY/fsi_computation.py
+++ b/SU2_PY/fsi_computation.py
@@ -3,7 +3,7 @@
 ## \file fsi_computation.py
 #  \brief Python wrapper code for FSI computation by coupling a third-party structural solver to SU2.
 #  \authors Nicola Fonzi, Vittorio Cavalieri based on the work of David Thomas
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/merge_solution.py b/SU2_PY/merge_solution.py
index 8b5c7d65fff..52539f71db8 100755
--- a/SU2_PY/merge_solution.py
+++ b/SU2_PY/merge_solution.py
@@ -3,7 +3,7 @@
 ## \file merge_solution.py
 #  \brief Python script for merging of the solution files.
 #  \author F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/mesh_deformation.py b/SU2_PY/mesh_deformation.py
index 7ea233593d7..9f6ffe0da18 100755
--- a/SU2_PY/mesh_deformation.py
+++ b/SU2_PY/mesh_deformation.py
@@ -3,7 +3,7 @@
 ## \file mesh_deformation.py
 #  \brief Python script for doing the parallel deformation using SU2_DEF.
 #  \author F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/package_tests.py b/SU2_PY/package_tests.py
index cc14a2afd29..3f92929ff23 100755
--- a/SU2_PY/package_tests.py
+++ b/SU2_PY/package_tests.py
@@ -3,7 +3,7 @@
 ## \file package_tests.py
 #  \brief _____________.
 #  \author T. Lukaczyk
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/parallel_computation.py b/SU2_PY/parallel_computation.py
index d5aa0043e44..4ef5f056073 100755
--- a/SU2_PY/parallel_computation.py
+++ b/SU2_PY/parallel_computation.py
@@ -3,7 +3,7 @@
 ## \file parallel_computation.py
 #  \brief Python script for doing the continuous adjoint computation using the SU2 suite.
 #  \author T. Economon, T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/parallel_computation_fsi.py b/SU2_PY/parallel_computation_fsi.py
index f60595dbaee..fbb5c3a903d 100755
--- a/SU2_PY/parallel_computation_fsi.py
+++ b/SU2_PY/parallel_computation_fsi.py
@@ -3,7 +3,7 @@
 ## \file parallel_computation_fsi.py
 #  \brief Python script for running FSI simulations using the SU2 suite.
 #  \author T. Economon, T. Lukaczyk, F. Palacios, H. Kline, R. Sanchez
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/parse_config.py b/SU2_PY/parse_config.py
index 8ff678a482e..dba492e8faa 100755
--- a/SU2_PY/parse_config.py
+++ b/SU2_PY/parse_config.py
@@ -3,7 +3,7 @@
 ## \file parse_config.py
 #  \brief Builds a worksheet of all SU2.cpp options
 #  \author A. Aranake, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/profiling.py b/SU2_PY/profiling.py
index 98da128c6ae..f9f45f68523 100755
--- a/SU2_PY/profiling.py
+++ b/SU2_PY/profiling.py
@@ -3,7 +3,7 @@
 ## \file profiling.py
 #  \brief Python script for postprocessing the SU2 custom profiling (profiling.csv)
 #  \author T. Economon
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/pySU2/Makefile.am b/SU2_PY/pySU2/Makefile.am
index 6b749935da1..210c5df9341 100644
--- a/SU2_PY/pySU2/Makefile.am
+++ b/SU2_PY/pySU2/Makefile.am
@@ -3,7 +3,7 @@
 # \file Makefile.am
 # \brief Makefile for the SU2 Python wrapper.
 # \author D. Thomas
-# \version 7.4.0 "Blackbird"
+# \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/pySU2/pySU2.i b/SU2_PY/pySU2/pySU2.i
index 3c21c1e9a87..d54f03501ca 100644
--- a/SU2_PY/pySU2/pySU2.i
+++ b/SU2_PY/pySU2/pySU2.i
@@ -4,7 +4,7 @@
 # \file pySU2.i
 # \brief Configuration file for the Swig compilation of the Python wrapper.
 # \author D. Thomas
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/pySU2/pySU2ad.i b/SU2_PY/pySU2/pySU2ad.i
index e595a3f2cdd..f93d3f099de 100644
--- a/SU2_PY/pySU2/pySU2ad.i
+++ b/SU2_PY/pySU2/pySU2ad.i
@@ -4,7 +4,7 @@
 # \file pySU2ad.i
 # \brief Configuration file for the Swig compilation of the Python wrapper.
 # \author D. Thomas, R. Sanchez
-# \version 7.4.0 "Blackbird"
+# \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/set_ffd_design_var.py b/SU2_PY/set_ffd_design_var.py
index be8e5667f6f..c114f16ac03 100755
--- a/SU2_PY/set_ffd_design_var.py
+++ b/SU2_PY/set_ffd_design_var.py
@@ -3,7 +3,7 @@
 ## \file set_ffd_design_var.py
 #  \brief Python script for automatically generating a list of FFD variables.
 #  \author T. Economon, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/shape_optimization.py b/SU2_PY/shape_optimization.py
index 48a5d7752e9..e56b7c41e9f 100755
--- a/SU2_PY/shape_optimization.py
+++ b/SU2_PY/shape_optimization.py
@@ -3,7 +3,7 @@
 ## \file shape_optimization.py
 #  \brief Python script for performing the shape optimization.
 #  \author T. Economon, T. Lukaczyk, F. Palacios
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
@@ -63,7 +63,7 @@ def main():
     
     sys.stdout.write('\n-------------------------------------------------------------------------\n')
     sys.stdout.write('|    ___ _   _ ___                                                      |\n')
-    sys.stdout.write('|   / __| | | |_  )   Release 7.4.0 \"Blackbird\"                         |\n')
+    sys.stdout.write('|   / __| | | |_  )   Release 7.5.0 \"Blackbird\"                         |\n')
     sys.stdout.write('|   \\__ \\ |_| |/ /                                                      |\n')
     sys.stdout.write('|   |___/\\___//___|   Aerodynamic Shape Optimization Script             |\n')
     sys.stdout.write('|                                                                       |\n')
diff --git a/SU2_PY/topology_optimization.py b/SU2_PY/topology_optimization.py
index 4b9957c4696..a8fd8f96802 100755
--- a/SU2_PY/topology_optimization.py
+++ b/SU2_PY/topology_optimization.py
@@ -2,7 +2,7 @@
 
 ## \file topology_optimization.py
 #  \brief Python script to drive SU2 in topology optimization.
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_PY/updateHistoryMap.py b/SU2_PY/updateHistoryMap.py
index 7e86ac4d8c4..49dfc382e7b 100644
--- a/SU2_PY/updateHistoryMap.py
+++ b/SU2_PY/updateHistoryMap.py
@@ -3,7 +3,7 @@
 ## \file updateHistoryMap.py
 #  \brief Python script for updating the historyMap.py file.
 #  \author T. Albring
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/SU2_SOL/include/SU2_SOL.hpp b/SU2_SOL/include/SU2_SOL.hpp
index 14a97c812ff..e11a7e8e7e2 100644
--- a/SU2_SOL/include/SU2_SOL.hpp
+++ b/SU2_SOL/include/SU2_SOL.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines of the code SU2_SOL.
  *        The subroutines and functions are in the <i>SU2_SOL.cpp</i> file.
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_SOL/obj/Makefile.am b/SU2_SOL/obj/Makefile.am
index d57da15bfb2..94b99d59ffb 100644
--- a/SU2_SOL/obj/Makefile.am
+++ b/SU2_SOL/obj/Makefile.am
@@ -3,7 +3,7 @@
 # \file Makefile.am
 # \brief Makefile for SU2_SOL
 # \author M. Colonno, T. Economon, F. Palacios
-# \version 7.4.0 "Blackbird"
+# \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_SOL/src/SU2_SOL.cpp b/SU2_SOL/src/SU2_SOL.cpp
index 64b0cf5fedd..7bb2afb7cb5 100644
--- a/SU2_SOL/src/SU2_SOL.cpp
+++ b/SU2_SOL/src/SU2_SOL.cpp
@@ -2,7 +2,7 @@
  * \file SU2_SOL.cpp
  * \brief Main file for the solution export/conversion code (SU2_SOL).
  * \author F. Palacios, T. Economon
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/TestCases/TestCase.py b/TestCases/TestCase.py
index c4fdf7635e8..96058193aaf 100644
--- a/TestCases/TestCase.py
+++ b/TestCases/TestCase.py
@@ -3,7 +3,7 @@
 ## \file TestCase.py
 #  \brief Python class for automated regression testing of SU2 examples
 #  \author A. Aranake, A. Campos, T. Economon, T. Lukaczyk, S. Padron
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/TestCases/aeroelastic/aeroelastic_NACA64A010.cfg b/TestCases/aeroelastic/aeroelastic_NACA64A010.cfg
index 42d975893dc..bf98f82f088 100644
--- a/TestCases/aeroelastic/aeroelastic_NACA64A010.cfg
+++ b/TestCases/aeroelastic/aeroelastic_NACA64A010.cfg
@@ -5,88 +5,49 @@
 % Author: Santiago Padron                                                      %
 % Institution: Stanford University                                             %
 % Date: 07-09-15                                                               %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
-%
-%
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.85
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 1.0
-%
-% Free-stream pressure (101325.0 N/m^2, 2116.216 psf by default)
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K, 518.67 R by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation (m or in)
 REF_ORIGIN_MOMENT_X = -0.5
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional
-% moment (m or in)
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic
-% calculation) (m^2 or in^2)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= DIMENSIONAL
 
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Time domain
 TIME_DOMAIN=YES
-%
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER, SPECTRAL_METHOD)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-%
-% Time Step for dual time stepping simulations (s)
 TIME_STEP= 0.00174532925199
 % 36 steps per period, based on the pitch natural frequency
 %
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 50.0
-%
-% Number of internal iterations (dual time method)
 INNER_ITER= 100
 
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
-SURFACE_MOVEMENT= AEROELASTIC
 %
-% Motion mach number (non-dimensional). Used for initializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
+SURFACE_MOVEMENT= AEROELASTIC
 MACH_MOTION= 0.85
-%
-% Moving wall boundary marker(s) (NONE = no marker, ignored for RIGID_MOTION)
 MARKER_MOVING= ( airfoil )
 
 % -------------- AEROELASTIC SIMULATION (Typical Section Model) ---------------%
-% Activated by GRID_MOVEMENT_KIND option
 %
 % The flutter speed index (modifies the freestream condition in the solver)
 FLUTTER_SPEED_INDEX = 1.3
@@ -113,188 +74,88 @@ AEROELASTIC_ITER = 3
 
 % --------------------------- GUST SIMULATION ---------------------------------%
 %
-% Apply a wind gust (NO, YES)
 WIND_GUST = NO
-%
-% Type of gust (NONE, TOP_HAT, SINE, ONE_M_COSINE, VORTEX, EOG)
 GUST_TYPE = TOP_HAT
-%
-% Direction of the gust (X_DIR or Y_DIR)
 GUST_DIR = Y_DIR
-%
-% Gust wavelenght (meters)
 GUST_WAVELENGTH= 7.90876841815
 % 1/4 of period based on the pitch natural frequency
 %
-% Number of gust periods
 GUST_PERIODS= 1.0
-%
-% Gust amplitude (m/s)
 GUST_AMPL= 8.78841285061
 % Corresponds to 1 deg AoA.
 %
-% Time at which to begin the gust (sec)
 GUST_BEGIN_TIME= 0.0
-%
-% Location at which the gust begins (meters) */
 GUST_BEGIN_LOC= -7.90876841815
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Far-field boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( airfoil )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% CFL number (stating value for the adaptive CFL number)
 CFL_NUMBER= 4.0
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-grid levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.75
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH_JESPERSEN)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Entropy fix coefficient (0.0 implies no entropy fixing, 1.0 implies scalar
-%                          artificial dissipation)
 ENTROPY_FIX_COEFF= 0.001
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, JACOBI)
 DEFORM_LINEAR_SOLVER_PREC= LU_SGS
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= NO
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Number of total iterations
 TIME_ITER= 360
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 0
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA64A010_hybrid_inv.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency for physical time steps (dual time)
 OUTPUT_WRT_FREQ= 1000
-%
-%
-% Screen output
 SCREEN_OUTPUT= (TIME_ITER, INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG_ON_SURFACE, PLUNGE, PITCH) 
-%
-OUTPUT_FILES= (RESTART_ASCII)
-
+OUTPUT_FILES= (RESTART_ASCII)
\ No newline at end of file
diff --git a/TestCases/axisymmetric_rans/air_nozzle/air_nozzle_restart.cfg b/TestCases/axisymmetric_rans/air_nozzle/air_nozzle_restart.cfg
index e02de724994..b5ef5f46717 100644
--- a/TestCases/axisymmetric_rans/air_nozzle/air_nozzle_restart.cfg
+++ b/TestCases/axisymmetric_rans/air_nozzle/air_nozzle_restart.cfg
@@ -4,7 +4,7 @@
 % Case description: Axisymmetric supersonic converging-diverging air nozzle    %
 % Author: Florian Dittmann                                                     %
 % Date: 2021.12.02                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
@@ -13,36 +13,32 @@
 SOLVER= RANS
 KIND_TURB_MODEL= SST
 RESTART_SOL= YES
-%
 AXISYMMETRIC= YES
-%
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
 MACH_NUMBER= 1E-9
-%
 INIT_OPTION= TD_CONDITIONS
-%
 FREESTREAM_OPTION= TEMPERATURE_FS
 FREESTREAM_PRESSURE= 1400000
 FREESTREAM_TEMPERATURE= 373.15
-%
 REF_DIMENSIONALIZATION= DIMENSIONAL
-%
+
 % ---- IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
 FLUID_MODEL= STANDARD_AIR
-%
+
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
 MU_CONSTANT= 1.716E-5
-%
+
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
 CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
 PRANDTL_LAM= 0.72
 PRANDTL_TURB= 0.90
-%
+
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
 MARKER_HEATFLUX= ( WALL, 0.0 )
@@ -58,12 +54,12 @@ CFL_NUMBER= 1000.0
 CFL_ADAPT= NO
 MAX_DELTA_TIME= 1E6
 OBJECTIVE_FUNCTION= DRAG
-%
+
 % ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
 %
 MUSCL_FLOW= YES
 SLOPE_LIMITER_FLOW= NONE
-%
+
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
 LINEAR_SOLVER= FGMRES
@@ -71,33 +67,30 @@ LINEAR_SOLVER_PREC= ILU
 LINEAR_SOLVER_ILU_FILL_IN= 0
 LINEAR_SOLVER_ERROR= 0.01
 LINEAR_SOLVER_ITER= 10
-%
+
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= ROE
 ENTROPY_FIX_COEFF= 0.1
 TIME_DISCRE_FLOW= EULER_IMPLICIT
-%
+
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
 TIME_DISCRE_TURB= EULER_IMPLICIT
 CFL_REDUCTION_TURB= 1.0
-%
+
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
 ITER= 3000
 CONV_RESIDUAL_MINVAL= -12
 CONV_STARTITER= 10
-%
+
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
 MESH_FILENAME= nozzle.su2
-%
 SOLUTION_FILENAME= solution_flow.dat
 RESTART_FILENAME= restart_flow.dat
 OUTPUT_WRT_FREQ= 1000
-%
-% Note: This cfg is used for a primal and adjoint Testcase, therefore both residuals are present here.
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, RMS_TKE, RMS_DISSIPATION, TOTAL_HEATFLUX, \
                 RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, RMS_ADJ_TKE, RMS_ADJ_DISSIPATION, SENS_AOA, SENS_MACH)
diff --git a/TestCases/cont_adj_euler/naca0012/inv_NACA0012.cfg b/TestCases/cont_adj_euler/naca0012/inv_NACA0012.cfg
index c1c2da535ec..fc0e4fe97bf 100644
--- a/TestCases/cont_adj_euler/naca0012/inv_NACA0012.cfg
+++ b/TestCases/cont_adj_euler/naca0012/inv_NACA0012.cfg
@@ -5,351 +5,136 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= CONTINUOUS_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
-%
-% Number of zones
 NZONES= 1
+
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AOA= 1.25
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
-NUM_METHOD_GRAD= GREEN_GAUSS
 %
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE, TOTAL_HEAT,
-%                                     MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                     INVERSE_DESIGN_HEATFLUX)
+NUM_METHOD_GRAD= GREEN_GAUSS
 OBJECTIVE_FUNCTION= DRAG
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 150
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
-%
-% Linear solver ILU preconditioner fill-in level (1 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 2, 2 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 1.0
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 1.0
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.5
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION, 
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION)
 DV_KIND= HICKS_HENNE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation 
-%   - HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-%   - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-%   - PARABOLIC ( 1st digit, 2nd and 3rd digit )
-%   - DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-%   - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= ( 1, 0.5 )
-%
-% Value of the shape deformation deformation
 DV_VALUE= 0.01
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, JACOBI)
 DEFORM_LINEAR_SOLVER_PREC= ILU
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 1000
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Deformation coefficient (in theory from -1.0 to 0.5, a large value is also valid)
 DEFORM_COEFF = 1E6
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                           WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= WALL_DISTANCE
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA0012_inv.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-%
-% Screen output
 SCREEN_OUTPUT = (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_GEO, SENS_AOA, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG) 
 HISTORY_OUTPUT= (ITER, RMS_RES, AERO_COEFF, SENSITIVITY)
 VOLUME_OUTPUT= (COORDINATES, SOLUTION, PRESSURE, TEMPERATURE, SENSITIVITY)
 OUTPUT_FILES=(RESTART_ASCII, PARAVIEW, SURFACE_CSV)
+
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.001
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= ( LIFT > 0.327 ) * 0.001; ( MOMENT_Z > 0.0 ) * 0.001; ( AIRFOIL_THICKNESS > 0.12 ) * 0.001
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 ); ( 30, 1.0 | airfoil | 0, 0.20 ); ( 30, 1.0 | airfoil | 0, 0.25 ); ( 30, 1.0 | airfoil | 0, 0.30 ); ( 30, 1.0 | airfoil | 0, 0.35 ); ( 30, 1.0 | airfoil | 0, 0.40 ); ( 30, 1.0 | airfoil | 0, 0.45 ); ( 30, 1.0 | airfoil | 0, 0.50 ); ( 30, 1.0 | airfoil | 0, 0.55 ); ( 30, 1.0 | airfoil | 0, 0.60 ); ( 30, 1.0 | airfoil | 0, 0.65 ); ( 30, 1.0 | airfoil | 0, 0.70 ); ( 30, 1.0 | airfoil | 0, 0.75 ); ( 30, 1.0 | airfoil | 0, 0.80 ); ( 30, 1.0 | airfoil | 0, 0.85 ); ( 30, 1.0 | airfoil | 0, 0.90 ); ( 30, 1.0 | airfoil | 0, 0.95 ); ( 30, 1.0 | airfoil | 1, 0.05 ); ( 30, 1.0 | airfoil | 1, 0.10 ); ( 30, 1.0 | airfoil | 1, 0.15 ); ( 30, 1.0 | airfoil | 1, 0.20 ); ( 30, 1.0 | airfoil | 1, 0.25 ); ( 30, 1.0 | airfoil | 1, 0.30 ); ( 30, 1.0 | airfoil | 1, 0.35 ); ( 30, 1.0 | airfoil | 1, 0.40 ); ( 30, 1.0 | airfoil | 1, 0.45 ); ( 30, 1.0 | airfoil | 1, 0.50 ); ( 30, 1.0 | airfoil | 1, 0.55 ); ( 30, 1.0 | airfoil | 1, 0.60 ); ( 30, 1.0 | airfoil | 1, 0.65 ); ( 30, 1.0 | airfoil | 1, 0.70 ); ( 30, 1.0 | airfoil | 1, 0.75 ); ( 30, 1.0 | airfoil | 1, 0.80 ); ( 30, 1.0 | airfoil | 1, 0.85 ); ( 30, 1.0 | airfoil | 1, 0.90 ); ( 30, 1.0 | airfoil | 1, 0.95 )
diff --git a/TestCases/cont_adj_euler/naca0012/inv_NACA0012_FD.cfg b/TestCases/cont_adj_euler/naca0012/inv_NACA0012_FD.cfg
index 2555b363c9c..782221988e0 100644
--- a/TestCases/cont_adj_euler/naca0012/inv_NACA0012_FD.cfg
+++ b/TestCases/cont_adj_euler/naca0012/inv_NACA0012_FD.cfg
@@ -5,347 +5,134 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= CONTINUOUS_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
-%
-% Number of Zones
 NZONES= 1
+
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AOA= 1.25
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Finite difference step size for python scripts (0.001 default, recommended
-%                                                 0.001 x REF_LENGTH)
 FIN_DIFF_STEP = 0.001
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
-NUM_METHOD_GRAD= GREEN_GAUSS
 %
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE, TOTAL_HEAT,
-%                                     MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                     INVERSE_DESIGN_HEATFLUX)
+NUM_METHOD_GRAD= GREEN_GAUSS
 OBJECTIVE_FUNCTION= DRAG
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 10
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (1 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 2, 2 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 1.0
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 1.0
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.5
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION, 
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION)
 DV_KIND= HICKS_HENNE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation 
-%   - HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-%   - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-%   - PARABOLIC ( 1st digit, 2nd and 3rd digit )
-%   - DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-%   - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= ( 1, 0.5 )
-%
-% Value of the shape deformation deformation
 DV_VALUE= 0.01
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
 %
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, JACOBI)
 DEFORM_LINEAR_SOLVER_PREC= LU_SGS
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 1000
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Deformation coefficient (in theory from -1.0 to 0.5, a large value is also valid)
 DEFORM_COEFF = 1E6
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                           WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= WALL_DISTANCE
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA0012_inv.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-%
-% History output
 HISTORY_OUTPUT=(ITER, RMS_RES, AERO_COEFF, D_AERO_COEFF)
 OUTPUT_FILES=(RESTART_ASCII, PARAVIEW)
+
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.001
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= ( LIFT > 0.327 ) * 0.001; ( MOMENT_Z > 0.0 ) * 0.001; ( AIRFOIL_THICKNESS > 0.12 ) * 0.001
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 ); 
diff --git a/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg b/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg
index 84130bf40e4..55835cfbedb 100644
--- a/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg
+++ b/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg
@@ -5,311 +5,108 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               TNE2_EULER, TNE2_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DISCRETE_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
+
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AOA= 1.25
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
-NUM_METHOD_GRAD= GREEN_GAUSS
 %
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE, TOTAL_HEAT,
-%                                     MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                     INVERSE_DESIGN_HEATFLUX)
+NUM_METHOD_GRAD= GREEN_GAUSS
 OBJECTIVE_FUNCTION= DRAG
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 150
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
-MG_PRE_SMOOTH= ( 1, 2, 2, 2 )
-%
-% Multi-Grid PostSmoothing Level
-MG_POST_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 1.0
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 1.0
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.5
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION, 
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION)
 DV_KIND= HICKS_HENNE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation 
-%   - HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-%   - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-%   - PARABOLIC ( 1st digit, 2nd and 3rd digit )
-%   - DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-%   - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= ( 1, 0.5 )
-%
-% Value of the shape deformation deformation
 DV_VALUE= 0.01
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                           WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= WALL_DISTANCE
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA0012_inv.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-%
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_PRESS, SENS_AOA)
-%
 OUTPUT_FILES=(RESTART_ASCII)
-%
+
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.001
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= ( LIFT > 0.327 ) * 0.001; ( MOMENT_Z > 0.0 ) * 0.001; ( AIRFOIL_THICKNESS > 0.12 ) * 0.001
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 ); ( 30, 1.0 | airfoil | 0, 0.20 ); ( 30, 1.0 | airfoil | 0, 0.25 ); ( 30, 1.0 | airfoil | 0, 0.30 ); ( 30, 1.0 | airfoil | 0, 0.35 ); ( 30, 1.0 | airfoil | 0, 0.40 ); ( 30, 1.0 | airfoil | 0, 0.45 ); ( 30, 1.0 | airfoil | 0, 0.50 ); ( 30, 1.0 | airfoil | 0, 0.55 ); ( 30, 1.0 | airfoil | 0, 0.60 ); ( 30, 1.0 | airfoil | 0, 0.65 ); ( 30, 1.0 | airfoil | 0, 0.70 ); ( 30, 1.0 | airfoil | 0, 0.75 ); ( 30, 1.0 | airfoil | 0, 0.80 ); ( 30, 1.0 | airfoil | 0, 0.85 ); ( 30, 1.0 | airfoil | 0, 0.90 ); ( 30, 1.0 | airfoil | 0, 0.95 ); ( 30, 1.0 | airfoil | 1, 0.05 ); ( 30, 1.0 | airfoil | 1, 0.10 ); ( 30, 1.0 | airfoil | 1, 0.15 ); ( 30, 1.0 | airfoil | 1, 0.20 ); ( 30, 1.0 | airfoil | 1, 0.25 ); ( 30, 1.0 | airfoil | 1, 0.30 ); ( 30, 1.0 | airfoil | 1, 0.35 ); ( 30, 1.0 | airfoil | 1, 0.40 ); ( 30, 1.0 | airfoil | 1, 0.45 ); ( 30, 1.0 | airfoil | 1, 0.50 ); ( 30, 1.0 | airfoil | 1, 0.55 ); ( 30, 1.0 | airfoil | 1, 0.60 ); ( 30, 1.0 | airfoil | 1, 0.65 ); ( 30, 1.0 | airfoil | 1, 0.70 ); ( 30, 1.0 | airfoil | 1, 0.75 ); ( 30, 1.0 | airfoil | 1, 0.80 ); ( 30, 1.0 | airfoil | 1, 0.85 ); ( 30, 1.0 | airfoil | 1, 0.90 ); ( 30, 1.0 | airfoil | 1, 0.95 )
diff --git a/TestCases/cont_adj_euler/oneram6/inv_ONERAM6.cfg b/TestCases/cont_adj_euler/oneram6/inv_ONERAM6.cfg
index 21ce4bcc237..0014082c1ff 100644
--- a/TestCases/cont_adj_euler/oneram6/inv_ONERAM6.cfg
+++ b/TestCases/cont_adj_euler/oneram6/inv_ONERAM6.cfg
@@ -5,403 +5,151 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2015.08.25                                                             %
-% File Version 7.4.0 "Blackbird" 	                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= CONTINUOUS_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8395
-%
-% Angle of attack (degrees)
 AOA= 3.06
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only for Euler equations)
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yaMAIN_BOX non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_VEL_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 implies no marker)
 MARKER_EULER= ( WING )
-%
-% Marker of the far field (0 implies no marker)
 MARKER_FAR= ( FARFIELD )
-%
-% Marker of symmetry boundary (0 implies no marker)
 MARKER_SYM= ( SYMMETRY )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( WING )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( WING )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( WING )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 99999
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= YES
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.9
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.9
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= NONE
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.5
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------&
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 25
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_ONERAM6_inv_ffd.su2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
-% Mesh input file format (SU2)
 MESH_FORMAT= SU2
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution frequency
 OUTPUT_WRT_FREQ= 100
-%
-% Screen output
 SCREEN_OUTPUT = (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_GEO, SENS_AOA)
-%
 OUTPUT_FILES=(RESTART_ASCII)
+
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING,
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC, NACA_4DIGITS, AIRFOIL)
 DV_KIND= FFD_CONTROL_POINT
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( WING )
-%
-% Parameters of the shape deformation
-% - TRANSLATION ( x_Disp, y_Disp, z_Disp ), as a unit vector
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - SCALE ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - PARABOLIC ( Center, Thickness )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - AIRFOIL ( 1.0 )
 DV_PARAM= ( MAIN_BOX, 2, 3, 1, 0.0, 0.0, 1.0 )
-%
-% Value of the shape deformation
 DV_VALUE= 0.05
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES,
-%                                                      BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 2
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= NO
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-10
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 500
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (MAIN_BOX, -0.0403, 0.0, -0.04836, 0.8463, 0.0, -0.04836, 1.209, 1.2896, -0.04836, 0.6851, 1.2896, -0.04836, -0.0403, 0.0, 0.04836, 0.8463, 0.0, 0.04836, 1.209, 1.2896, 0.04836, 0.6851, 1.2896, 0.04836)
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= (10, 8, 1)
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= 2ND_DERIVATIVE
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 1.0
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= ( LIFT > 0.282557 ) * 1.0
-%
-% Maximum number of iterations
 OPT_ITERATIONS= 100
-%
-% Requested accuracy
 OPT_ACCURACY= 1E-6
-%
-% Upper bound for each design variable
 OPT_BOUND_UPPER= 0.1
-%
-% Lower bound for each design variable
 OPT_BOUND_LOWER= -0.1
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 11, 1.0 | WING | MAIN_BOX, 0, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 0, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 0, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 0, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 0, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 0, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 0, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 0, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 0, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 0, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 0, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 0, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 8, 1, 0.0, 0.0, 1.0 )
diff --git a/TestCases/cont_adj_euler/wedge/inv_wedge_ROE.cfg b/TestCases/cont_adj_euler/wedge/inv_wedge_ROE.cfg
index 16d33602149..bfe12dc6acd 100644
--- a/TestCases/cont_adj_euler/wedge/inv_wedge_ROE.cfg
+++ b/TestCases/cont_adj_euler/wedge/inv_wedge_ROE.cfg
@@ -5,374 +5,137 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2012.10.07                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               TNE2_EULER, TNE2_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= CONTINUOUS_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
+
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 2.0
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 100000.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( upper, lower )
-%
-% Supersonic inlet boundary marker(s) (NONE = no marker) 
-% Total Conditions: (inlet marker, temperature, static pressure, velocity_x, 
-%           velocity_y, velocity_z, ... ), i.e. all variables specified.
 MARKER_SUPERSONIC_INLET= ( inlet, 300.0, 100000.0, 695.4290761824674, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
 MARKER_OUTLET= ( outlet, 10000.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( lower )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( outlet )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER=100
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= BCGSTAB
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.8
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.006
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Relaxation coefficient
 RELAXATION_FACTOR_ADJOINT= 1.0
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.8
-%
-% Limit value for the adjoint variable
 LIMIT_ADJFLOW= 1E15
-%
-% Multigrid adjoint problem (NO, YES)
 MG_ADJFLOW= NO
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE, 
-%                                             SURFACE_MASSFLOW)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= SURFACE_TOTAL_PRESSURE
-%
-% Marker on which to track one-dimensionalized outputs
 MARKER_ANALYZE  = (outlet)
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -11
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
+
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_wedge_inv_FFD.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-% Screen output
 SCREEN_OUTPUT = (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_GEO, SENS_AOA) 
-%
 OUTPUT_FILES=(RESTART_ASCII)
+
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-10
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 500
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (MAIN_BOX, 0.5, -0.25, 0, 1.5, -0.25, 0, 1.5, 0.25,  0, 0.5, 0.25,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= (10, 1,0)
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= 2ND_DERIVATIVE
+
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION, 
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION)
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( lower )
-%
 DV_KIND= FFD_CONTROL_POINT_2D
-%
-%
-% Parameters of the shape deformation 
-%   - HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-%   - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-%   - PARABOLIC ( 1st digit, 2nd and 3rd digit )
-%   - DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-%   - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= (MAIN_BOX, 3,0, 0,1.0,0,0 )
-%
-% Value of the shape deformation deformation
 DV_VALUE= 0.5
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Sca
 OPT_OBJECTIVE=SURFACE_TOTAL_PRESSURE
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= NONE
-%
-% Maximum number of iterations
 OPT_ITERATIONS= 100
-%
-% Requested accuracy
 OPT_ACCURACY= 1E-6
-%
-% Upper bound for each design variable
 OPT_BOUND_UPPER= 0.1
-%
-% Lower bound for each design variable
 OPT_BOUND_LOWER= -0.1
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= (19, 1.0| lower | MAIN_BOX, 3,0,0,1.0);(19, 1.0| lower | MAIN_BOX, 4,0,0,1.0);(19, 1.0| lower | MAIN_BOX, 5,0,0,1.0);(19, 1.0| lower | MAIN_BOX, 6,0,0,1.0)
diff --git a/TestCases/cont_adj_euler/wedge/inv_wedge_ROE_multiobj.cfg b/TestCases/cont_adj_euler/wedge/inv_wedge_ROE_multiobj.cfg
index 67455358a0b..d64c99e4559 100644
--- a/TestCases/cont_adj_euler/wedge/inv_wedge_ROE_multiobj.cfg
+++ b/TestCases/cont_adj_euler/wedge/inv_wedge_ROE_multiobj.cfg
@@ -6,398 +6,143 @@
 % Author: H.L. Kline, modified from inviscid wedge by Thomas D. Economon       %
 % Institution: Stanford University                                             %
 % Date: 2018.01.07                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               TNE2_EULER, TNE2_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= CONTINUOUS_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
-% Number of Zones
 NZONES= 1
-%
 OUTPUT_FILES=(RESTART_ASCII)
+
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 2.0
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 100000.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( upper, lower )
-%
-% Supersonic inlet boundary marker(s) (NONE = no marker) 
-% Total Conditions: (inlet marker, temperature, static pressure, velocity_x, 
-%           velocity_y, velocity_z, ... ), i.e. all variables specified.
 MARKER_SUPERSONIC_INLET= ( inlet, 300.0, 100000.0, 695.4290761824674, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
 MARKER_OUTLET= ( outlet, 10000.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( lower )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= (outlet, lower)
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER=1000
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= BCGSTAB
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (1 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
 
-
-
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.8
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.006
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Relaxation coefficient
 RELAXATION_FACTOR_ADJOINT= 1.0
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.8
-%
-% Limit value for the adjoint variable
 LIMIT_ADJFLOW= 1E15
-%
-% Multigrid adjoint problem (NO, YES)
 MG_ADJFLOW= NO
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE, 
-%                                             SURFACE_MASSFLOW)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION = SURFACE_TOTAL_PRESSURE, DRAG
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT= -1.0E-7,1.0
-%
-% Marker on which to track one-dimensionalized quantities
 MARKER_ANALYZE  = (outlet)
-%
-% Method to compute the average value in MARKER_ANALYZE (AREA, MASSFLUX).
 MARKER_ANALYZE_AVERAGE = AREA
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -11
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
+
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_wedge_inv_FFD.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-%
-% Read binary restart files
 READ_BINARY_RESTART = NO
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-10
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 500
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (MAIN_BOX, 0.5, -0.25, 0, 1.5, -0.25, 0, 1.5, 0.25,  0, 0.5, 0.25,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= (10, 1,0)
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= 2ND_DERIVATIVE
+
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION, 
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION)
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( lower )
-%
 DV_KIND= FFD_CONTROL_POINT_2D
-%
-%
-% Parameters of the shape deformation 
-%   - HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-%   - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-%   - PARABOLIC ( 1st digit, 2nd and 3rd digit )
-%   - DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-%   - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= (MAIN_BOX, 3,0, 0,1.0,0,0 )
-%
-% Value of the shape deformation deformation
 DV_VALUE= 0.5
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-% 
-% History output
 HISTORY_OUTPUT= (ITER, RMS_RES, AERO_COEFF)
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor, separated by semicolons.
-% To include quadratic penalty function: use OPT_CONSTRAINT option syntax within the OPT_OBJECTIVE list.
-% ex= Objective * Scale
 OPT_OBJECTIVE=SURFACE_TOTAL_PRESSURE*-1E-4; (DRAG = 0.05)*1E6
-%
-% Use combined objective within gradient evaluation: may reduce cost to compute gradients when using the adjoint formulation.
 OPT_COMBINE_OBJECTIVE = YES
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= NONE
-%
-% Maximum number of iterations
 OPT_ITERATIONS= 1
-%
-% Requested accuracy
 OPT_ACCURACY= 1E-6
-%
-% Upper bound for each design variable
 OPT_BOUND_UPPER= 0.1
-%
-% Lower bound for each design variable
 OPT_BOUND_LOWER= -0.1
-%
-% Optimization design variables, separated by semicolons
-DEFINITION_DV= (19, 1.0| lower | MAIN_BOX, 3,0,0,1.0);(19, 1.0| lower | MAIN_BOX, 4,0,0,1.0);(19, 1.0| lower | MAIN_BOX, 5,0,0,1.0);(19, 1.0| lower | MAIN_BOX, 6,0,0,1.0)
-
+DEFINITION_DV= (19, 1.0| lower | MAIN_BOX, 3,0,0,1.0);(19, 1.0| lower | MAIN_BOX, 4,0,0,1.0);(19, 1.0| lower | MAIN_BOX, 5,0,0,1.0);(19, 1.0| lower | MAIN_BOX, 6,0,0,1.0)
\ No newline at end of file
diff --git a/TestCases/cont_adj_navierstokes/cylinder/lam_cylinder.cfg b/TestCases/cont_adj_navierstokes/cylinder/lam_cylinder.cfg
index 1a6c985f1fa..9ca74a9381b 100644
--- a/TestCases/cont_adj_navierstokes/cylinder/lam_cylinder.cfg
+++ b/TestCases/cont_adj_navierstokes/cylinder/lam_cylinder.cfg
@@ -5,307 +5,116 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.03.01                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                        
 SOLVER= NAVIER_STOKES
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= CONTINUOUS_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.1
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 40.0
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( cylinder, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( cylinder )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( cylinder )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE, TOTAL_HEAT,
-%                                     MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                     INVERSE_DESIGN_HEATFLUX)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 150
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= BCGSTAB
-%
-% Preconditioner of the Krylov linear solver (NONE, JACOBI, LINELET)
-%LINEAR_SOLVER_PREC= NONE
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-8
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 1
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.8
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.0, 0.001 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.001 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.75
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, PARABOLIC, NACA_4DIGITS, 
-%                      DISPLACEMENT, ROTATION, FFD_CONTROL_POINT, 
-%                      FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION, FFD_CAMBER, FFD_THICKNESS, FFD_VOLUME)
 DV_KIND= HICKS_HENNE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( cylinder )
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( Center, Thickness )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- OBSTACLE ( Center, Bump size )
-% 	- FFD_CONTROL_POINT ( FFD_BoxTag ID, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% 	- FFD_DIHEDRAL_ANGLE ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_TWIST_ANGLE ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_ROTATION ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_CAMBER ( FFD_BoxTag ID, i_Ind, j_Ind )
-% 	- FFD_THICKNESS ( FFD_BoxTag ID, i_Ind, j_Ind )
-% 	- FFD_VOLUME ( FFD_BoxTag ID, i_Ind, j_Ind )
 DV_PARAM= ( 1, 0.5 )
-%
-% New value of the shape deformation
 DV_VALUE= 0.05
-%
-% Hold the grid fixed in a region (NO, YES)
 HOLD_GRID_FIXED= NO
-%
-% Coordinates of the box where the grid will be deformed (Xmin, Ymin, Zmin, Xmax, Ymax, Zmax)
 HOLD_GRID_FIXED_COORD= ( -0.5, -0.49, 0.0, 2.5, 0.49, 0.0 )
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -14
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_cylinder_lam.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1000
-%
-% 
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_GEO, SENS_AOA)
-%
 OUTPUT_FILES=(RESTART_ASCII)
+
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-
 DEFINITION_DV= ( 30, 1.0 | cylinder | 0, 0.961538461538 ); ( 30, 1.0 | cylinder | 0, 0.923076923077 ); ( 30, 1.0 | cylinder | 0, 0.884615384615 ); ( 30, 1.0 | cylinder | 0, 0.846153846154 ); ( 30, 1.0 | cylinder | 0, 0.807692307692 ); ( 30, 1.0 | cylinder | 0, 0.769230769231 ); ( 30, 1.0 | cylinder | 0, 0.730769230769 ); ( 30, 1.0 | cylinder | 0, 0.692307692308 ); ( 30, 1.0 | cylinder | 0, 0.653846153846 ); ( 30, 1.0 | cylinder | 0, 0.615384615385 ); ( 30, 1.0 | cylinder | 0, 0.576923076923 ); ( 30, 1.0 | cylinder | 0, 0.538461538462 ); ( 30, 1.0 | cylinder | 0, 0.5 ); ( 30, 1.0 | cylinder | 0, 0.461538461538 ); ( 30, 1.0 | cylinder | 0, 0.423076923077 ); ( 30, 1.0 | cylinder | 0, 0.384615384615 ); ( 30, 1.0 | cylinder | 0, 0.346153846154 ); ( 30, 1.0 | cylinder | 0, 0.307692307692 ); ( 30, 1.0 | cylinder | 0, 0.269230769231 ); ( 30, 1.0 | cylinder | 0, 0.230769230769 ); ( 30, 1.0 | cylinder | 0, 0.192307692308 ); ( 30, 1.0 | cylinder | 0, 0.153846153846 ); ( 30, 1.0 | cylinder | 0, 0.115384615385 ); ( 30, 1.0 | cylinder | 0, 0.0769230769231 ); ( 30, 1.0 | cylinder | 0, 0.0384615384615 ); ( 30, 1.0 | cylinder | 1, 0.0384615384615 ); ( 30, 1.0 | cylinder | 1, 0.0769230769231 ); ( 30, 1.0 | cylinder | 1, 0.115384615385 ); ( 30, 1.0 | cylinder | 1, 0.153846153846 ); ( 30, 1.0 | cylinder | 1, 0.192307692308 ); ( 30, 1.0 | cylinder | 1, 0.230769230769 ); ( 30, 1.0 | cylinder | 1, 0.269230769231 ); ( 30, 1.0 | cylinder | 1, 0.307692307692 ); ( 30, 1.0 | cylinder | 1, 0.346153846154 ); ( 30, 1.0 | cylinder | 1, 0.384615384615 ); ( 30, 1.0 | cylinder | 1, 0.423076923077 ); ( 30, 1.0 | cylinder | 1, 0.461538461538 ); ( 30, 1.0 | cylinder | 1, 0.5 ); ( 30, 1.0 | cylinder | 1, 0.538461538462 ); ( 30, 1.0 | cylinder | 1, 0.576923076923 ); ( 30, 1.0 | cylinder | 1, 0.615384615385 ); ( 30, 1.0 | cylinder | 1, 0.653846153846 ); ( 30, 1.0 | cylinder | 1, 0.692307692308 ); ( 30, 1.0 | cylinder | 1, 0.730769230769 ); ( 30, 1.0 | cylinder | 1, 0.769230769231 ); ( 30, 1.0 | cylinder | 1, 0.807692307692 ); ( 30, 1.0 | cylinder | 1, 0.846153846154 ); ( 30, 1.0 | cylinder | 1, 0.884615384615 ); ( 30, 1.0 | cylinder | 1, 0.923076923077 ); ( 30, 1.0 | cylinder | 1, 0.961538461538 )
diff --git a/TestCases/cont_adj_navierstokes/naca0012_sub/lam_NACA0012.cfg b/TestCases/cont_adj_navierstokes/naca0012_sub/lam_NACA0012.cfg
index bc81449a9c6..b6717b1454d 100644
--- a/TestCases/cont_adj_navierstokes/naca0012_sub/lam_NACA0012.cfg
+++ b/TestCases/cont_adj_navierstokes/naca0012_sub/lam_NACA0012.cfg
@@ -5,306 +5,106 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: Jul 18th, 2014                                                         %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES, NS_PLASMA)
-%                               
 SOLVER= NAVIER_STOKES
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= CONTINUOUS_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.3
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 2.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 3000.0
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 150
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-10
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 2, 2 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.85
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.85
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.001 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.001 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.25
-%
-% Limit value for the adjoint variable
 LIMIT_ADJFLOW= 1E6
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION, 
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION)
 DV_KIND= HICKS_HENNE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( 1st digit, 2nd and 3rd digit )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= ( 1, 0.5 )
-%
-% Value of the shape deformation deformation
 DV_VALUE= 0.01
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA0012_lam_hybrid_v2.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 5000
-%
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_GEO, SENS_AOA)
-%
 OUTPUT_FILES= (RESTART_ASCII)
+
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.01
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= (LIFT > 0.1) * 0.01
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 ); ( 30, 1.0 | airfoil | 0, 0.20 ); ( 30, 1.0 | airfoil | 0, 0.25 ); ( 30, 1.0 | airfoil | 0, 0.30 ); ( 30, 1.0 | airfoil | 0, 0.35 ); ( 30, 1.0 | airfoil | 0, 0.40 ); ( 30, 1.0 | airfoil | 0, 0.45 ); ( 30, 1.0 | airfoil | 0, 0.50 ); ( 30, 1.0 | airfoil | 0, 0.55 ); ( 30, 1.0 | airfoil | 0, 0.60 ); ( 30, 1.0 | airfoil | 0, 0.65 ); ( 30, 1.0 | airfoil | 0, 0.70 ); ( 30, 1.0 | airfoil | 0, 0.75 ); ( 30, 1.0 | airfoil | 0, 0.80 ); ( 30, 1.0 | airfoil | 0, 0.85 ); ( 30, 1.0 | airfoil | 0, 0.90 ); ( 30, 1.0 | airfoil | 0, 0.95 ); ( 30, 1.0 | airfoil | 1, 0.05 ); ( 30, 1.0 | airfoil | 1, 0.10 ); ( 30, 1.0 | airfoil | 1, 0.15 ); ( 30, 1.0 | airfoil | 1, 0.20 ); ( 30, 1.0 | airfoil | 1, 0.25 ); ( 30, 1.0 | airfoil | 1, 0.30 ); ( 30, 1.0 | airfoil | 1, 0.35 ); ( 30, 1.0 | airfoil | 1, 0.40 ); ( 30, 1.0 | airfoil | 1, 0.45 ); ( 30, 1.0 | airfoil | 1, 0.50 ); ( 30, 1.0 | airfoil | 1, 0.55 ); ( 30, 1.0 | airfoil | 1, 0.60 ); ( 30, 1.0 | airfoil | 1, 0.65 ); ( 30, 1.0 | airfoil | 1, 0.70 ); ( 30, 1.0 | airfoil | 1, 0.75 ); ( 30, 1.0 | airfoil | 1, 0.80 ); ( 30, 1.0 | airfoil | 1, 0.85 ); ( 30, 1.0 | airfoil | 1, 0.90 ); ( 30, 1.0 | airfoil | 1, 0.95 )
diff --git a/TestCases/cont_adj_navierstokes/naca0012_trans/lam_NACA0012.cfg b/TestCases/cont_adj_navierstokes/naca0012_trans/lam_NACA0012.cfg
index fa6323eb3a0..69b13f82505 100644
--- a/TestCases/cont_adj_navierstokes/naca0012_trans/lam_NACA0012.cfg
+++ b/TestCases/cont_adj_navierstokes/naca0012_trans/lam_NACA0012.cfg
@@ -5,318 +5,110 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: Jul 18th, 2014                                                         %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES, NS_PLASMA)
-%                               
 SOLVER= NAVIER_STOKES
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= CONTINUOUS_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 10.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 500.0
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 25.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 150
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-8
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 2, 2 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.5
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.5
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 1.0
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.0, 0.001 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.001 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.1
-%
-% Limit value for the adjoint variable
 LIMIT_ADJFLOW= 1E6
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION, 
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION)
 DV_KIND= HICKS_HENNE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( 1st digit, 2nd and 3rd digit )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= ( 1, 0.5 )
-%
-% Value of the shape deformation deformation
 DV_VALUE= 0.01
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -13
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA0012_lam_hybrid_v2.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 10000
-%
 SCREEN_WRT_FREQ_INNER= 5
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_GEO, SENS_AOA)
-%
 OUTPUT_FILES=(RESTART_ASCII)
+
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.01
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= (LIFT > 0.1) * 0.01
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.95 ); ( 30, 1.0 | airfoil | 0, 0.90 ); ( 30, 1.0 | airfoil | 0, 0.85 ); ( 30, 1.0 | airfoil | 0, 0.80 ); ( 30, 1.0 | airfoil | 0, 0.75 ); ( 30, 1.0 | airfoil | 0, 0.70 ); ( 30, 1.0 | airfoil | 0, 0.65 ); ( 30, 1.0 | airfoil | 0, 0.60 ); ( 30, 1.0 | airfoil | 0, 0.55 ); ( 30, 1.0 | airfoil | 0, 0.50 ); ( 30, 1.0 | airfoil | 0, 0.45 ); ( 30, 1.0 | airfoil | 0, 0.40 ); ( 30, 1.0 | airfoil | 0, 0.35 ); ( 30, 1.0 | airfoil | 0, 0.30 ); ( 30, 1.0 | airfoil | 0, 0.25 ); ( 30, 1.0 | airfoil | 0, 0.20 ); ( 30, 1.0 | airfoil | 0, 0.15 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 1, 0.05 ); ( 30, 1.0 | airfoil | 1, 0.10 ); ( 30, 1.0 | airfoil | 1, 0.15 ); ( 30, 1.0 | airfoil | 1, 0.20 ); ( 30, 1.0 | airfoil | 1, 0.25 ); ( 30, 1.0 | airfoil | 1, 0.30 ); ( 30, 1.0 | airfoil | 1, 0.35 ); ( 30, 1.0 | airfoil | 1, 0.40 ); ( 30, 1.0 | airfoil | 1, 0.45 ); ( 30, 1.0 | airfoil | 1, 0.50 ); ( 30, 1.0 | airfoil | 1, 0.55 ); ( 30, 1.0 | airfoil | 1, 0.60 ); ( 30, 1.0 | airfoil | 1, 0.65 ); ( 30, 1.0 | airfoil | 1, 0.70 ); ( 30, 1.0 | airfoil | 1, 0.75 ); ( 30, 1.0 | airfoil | 1, 0.80 ); ( 30, 1.0 | airfoil | 1, 0.85 ); ( 30, 1.0 | airfoil | 1, 0.90 ); ( 30, 1.0 | airfoil | 1, 0.95 )
diff --git a/TestCases/cont_adj_rans/naca0012/turb_nasa.cfg b/TestCases/cont_adj_rans/naca0012/turb_nasa.cfg
index 5b305afa197..0a289d40e06 100644
--- a/TestCases/cont_adj_rans/naca0012/turb_nasa.cfg
+++ b/TestCases/cont_adj_rans/naca0012/turb_nasa.cfg
@@ -5,303 +5,116 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.03.01                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
-%
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= CONTINUOUS_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.15
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.0E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 100
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= BCGSTAB
-%
-% Preconditioner of the Krylov linear solver (NONE, JACOBI, LINELET)
-%LINEAR_SOLVER_PREC= NONE
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-8
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 4 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.9
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.9
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.01
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.005 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE, TOTAL_HEAT,
-%                                     MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                     INVERSE_DESIGN_HEATFLUX)
-OBJECTIVE_FUNCTION= DRAG
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
+OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.002 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.25
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Adjoint frozen viscosity (NO, YES)
 FROZEN_VISC_CONT= YES
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, PARABOLIC, NACA_4DIGITS, 
-%                      DISPLACEMENT, ROTATION, FFD_CONTROL_POINT, 
-%                      FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION, FFD_CAMBER, FFD_THICKNESS, FFD_VOLUME)
 DV_KIND= HICKS_HENNE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( Center, Thickness )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- OBSTACLE ( Center, Bump size )
-% 	- FFD_CONTROL_POINT ( FFD_BoxTag ID, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% 	- FFD_DIHEDRAL_ANGLE ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_TWIST_ANGLE ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_ROTATION ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_CAMBER ( FFD_BoxTag ID, i_Ind, j_Ind )
-% 	- FFD_THICKNESS ( FFD_BoxTag ID, i_Ind, j_Ind )
-% 	- FFD_VOLUME ( FFD_BoxTag ID, i_Ind, j_Ind )
 DV_PARAM= ( 1, 0.5 )
-%
-% New value of the shape deformation
 DV_VALUE= 0.05
-%
-% Hold the grid fixed in a region (NO, YES)
 HOLD_GRID_FIXED= NO
-%
-% Coordinates of the box where the grid will be deformed (Xmin, Ymin, Zmin, Xmax, Ymax, Zmax)
 HOLD_GRID_FIXED_COORD= ( -0.5, -0.49, 0.0, 2.5, 0.49, 0.0 )
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= naca0012rans_ff10.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1000
-%
-%
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_GEO, SENS_AOA)
-%
 OUTPUT_FILES=(RESTART_ASCII)
-
diff --git a/TestCases/cont_adj_rans/naca0012/turb_nasa_binary.cfg b/TestCases/cont_adj_rans/naca0012/turb_nasa_binary.cfg
index 9ecb7996561..2da4c41af3e 100644
--- a/TestCases/cont_adj_rans/naca0012/turb_nasa_binary.cfg
+++ b/TestCases/cont_adj_rans/naca0012/turb_nasa_binary.cfg
@@ -5,302 +5,116 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.03.01                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
-%
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= CONTINUOUS_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= YES
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.15
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.0E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 22
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= BCGSTAB
-%
-% Preconditioner of the Krylov linear solver (NONE, JACOBI, LINELET)
 %LINEAR_SOLVER_PREC= NONE
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-8
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 4 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.9
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.9
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.01
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.005 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE, TOTAL_HEAT,
-%                                     MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                     INVERSE_DESIGN_HEATFLUX)
-OBJECTIVE_FUNCTION= DRAG
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
+OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.002 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.25
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Adjoint frozen viscosity (NO, YES)
 FROZEN_VISC_CONT= YES
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, PARABOLIC, NACA_4DIGITS, 
-%                      DISPLACEMENT, ROTATION, FFD_CONTROL_POINT, 
-%                      FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION, FFD_CAMBER, FFD_THICKNESS, FFD_VOLUME)
 DV_KIND= HICKS_HENNE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( Center, Thickness )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- OBSTACLE ( Center, Bump size )
-% 	- FFD_CONTROL_POINT ( FFD_BoxTag ID, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% 	- FFD_DIHEDRAL_ANGLE ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_TWIST_ANGLE ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_ROTATION ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_CAMBER ( FFD_BoxTag ID, i_Ind, j_Ind )
-% 	- FFD_THICKNESS ( FFD_BoxTag ID, i_Ind, j_Ind )
-% 	- FFD_VOLUME ( FFD_BoxTag ID, i_Ind, j_Ind )
 DV_PARAM= ( 1, 0.5 )
-%
-% New value of the shape deformation
 DV_VALUE= 0.05
-%
-% Hold the grid fixed in a region (NO, YES)
 HOLD_GRID_FIXED= NO
-%
-% Coordinates of the box where the grid will be deformed (Xmin, Ymin, Zmin, Xmax, Ymax, Zmax)
 HOLD_GRID_FIXED_COORD= ( -0.5, -0.49, 0.0, 2.5, 0.49, 0.0 )
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= naca0012rans_ff10.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= bin_solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= bin_solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1000
-%
-%
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_GEO, SENS_AOA)
-
diff --git a/TestCases/cont_adj_rans/oneram6/turb_ONERAM6.cfg b/TestCases/cont_adj_rans/oneram6/turb_ONERAM6.cfg
index 3b4cded45b6..5a4fe311f45 100644
--- a/TestCases/cont_adj_rans/oneram6/turb_ONERAM6.cfg
+++ b/TestCases/cont_adj_rans/oneram6/turb_ONERAM6.cfg
@@ -5,367 +5,140 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.03.01                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES, etc.)     
 SOLVER= NAVIER_STOKES
-%
-% Specify turbulence model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= CONTINUOUS_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8395
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 3.06
-%
-% Side-slip angle (degrees, only for compressible flows)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 11.72E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 0.64607
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 0.64607
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( wing, 0.0 )
-%
-% Far-field boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Symmetry boundary marker(s) (NONE = no marker)
 MARKER_SYM= ( symmetry )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( wing )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( wing )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 4.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 EXT_ITER= 10
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (NONE, JACOBI, LINELET)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-5
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.7
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.7
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE)
-OBJECTIVE_FUNCTION= DRAG
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
+OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Slope limiter (VENKATAKRISHNAN, SHARP_EDGES)
 SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.8
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
-%
-% Sensitivity smoothing (NONE, SOBOLEV, BIGRID)
 SENS_SMOOTHING= NONE
-%
-% Adjoint frozen viscosity (NO, YES)
 FROZEN_VISC= YES
 
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
 %
-% Marker(s) of the surface where geometrical based function will be evaluated
 GEO_MARKER= ( wing )
-%
-% Description of the geometry to be analyzed (AIRFOIL, WING, FUSELAGE)
 GEO_DESCRIPTION= WING
-%
-% Coordinate of the stations to be analyzed
 GEO_LOCATION_STATIONS= (0.0, 0.2, 0.4, 0.6, 0.8)
-%
-% Geometrical bounds (Y coordinate) for the wing geometry analysis or
-% fuselage evaluation (X coordinate).
 GEO_BOUNDS= (0.0806, 1.1284)
-%
-% Plot loads and Cp distributions on each airfoil section
 GEO_PLOT_STATIONS= NO
-%
-% Geometrical evaluation mode (FUNCTION, GRADIENT)
 GEO_MODE= FUNCTION
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Kind of deformation (FFD_SETTING, FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC,
-%                      NACA_4DIGITS, DISPLACEMENT, ROTATION, FFD_CONTROL_POINT, 
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CAMBER, FFD_THICKNESS, SURFACE_FILE)
 DV_KIND= FFD_CONTROL_POINT
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( wing )
-%
-% Parameters of the shape deformation
-%       - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-%       - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-%       - PARABOLIC ( Center, Thickness )
-%       - DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-%       - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%       - OBSTACLE ( Center, Bump size )
-%       - FFD_CONTROL_POINT ( FFD_BoxTag ID, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-%       - FFD_DIHEDRAL_ANGLE ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%       - FFD_TWIST_ANGLE ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%       - FFD_ROTATION ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%       - FFD_CAMBER ( FFD_BoxTag ID, i_Ind, j_Ind )
-%       - FFD_THICKNESS ( FFD_BoxTag ID, i_Ind, j_Ind )
-%       - FFD_VOLUME ( FFD_BoxTag ID, i_Ind, j_Ind )
 DV_PARAM= ( WING_BOX, 2, 2, 1, 0.0, 0.0, 1.0 )
-%
-% New value of the shape deformation
 DV_VALUE= 0.1
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 1
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-5
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_ONERAM6_turb.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1000
-%
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-
-% Optimization objective function with optional scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.02
-
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='  (LIFT > 0.267) * 0.02
 OPT_CONSTRAINT= (LIFT > 0.268) * 0.02; (STATION1_THICKNESS > 0.0570) * 0.02; (STATION2_THICKNESS > 0.0513) * 0.02; (STATION3_THICKNESS > 0.0457) * 0.02; (STATION4_THICKNESS > 0.0399) * 0.02; (STATION5_THICKNESS > 0.0343) * 0.02
-
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 11, 1.0 | wing | WING_BOX, 0, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 1, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 2, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 3, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 4, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 0, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 1, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 2, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 3, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 4, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 0, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 1, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 2, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 3, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 4, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 0, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 1, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 2, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 3, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 4, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 0, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 1, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 2, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 3, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 4, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 0, 0, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 1, 0, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 2, 0, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 3, 0, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 4, 0, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 0, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 1, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 2, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 3, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 4, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 0, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 1, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 2, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 3, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 4, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 0, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 1, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 2, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 3, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 4, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 0, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 1, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 2, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 3, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 4, 4, 0, 0.0, 0.0, 1.0 )
diff --git a/TestCases/cont_adj_rans/rae2822/turb_SA_RAE2822.cfg b/TestCases/cont_adj_rans/rae2822/turb_SA_RAE2822.cfg
index 490d476a1e6..bb5b60a1b78 100644
--- a/TestCases/cont_adj_rans/rae2822/turb_SA_RAE2822.cfg
+++ b/TestCases/cont_adj_rans/rae2822/turb_SA_RAE2822.cfg
@@ -5,321 +5,120 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES, NS_PLASMA)
-%                               
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= CONTINUOUS_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.729
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 2.31
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.5E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( AIRFOIL, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( FARFIELD )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( AIRFOIL )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( AIRFOIL )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 ITER= 150
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= BCGSTAB
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.95
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.95
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.01 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE, TOTAL_HEAT,
-%                                     MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                     INVERSE_DESIGN_HEATFLUX)
-OBJECTIVE_FUNCTION= DRAG
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
+OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.001 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.25
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Adjoint frozen viscosity (NO, YES)
 FROZEN_VISC_CONT= YES
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -13
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_RAE2822_turb.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1000
-%
-%
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_GEO, SENS_AOA)
-%
 OUTPUT_FILES= (RESTART_ASCII)
+
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, PARABOLIC, NACA_4DIGITS, 
-%                      DISPLACEMENT, ROTATION, FFD_CONTROL_POINT, 
-%                      FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION, FFD_CAMBER, FFD_THICKNESS, FFD_VOLUME
-%                      SURFACE_FILE)
 DV_KIND= FFD_SETTING
-%
-% Marker of the surface to which we are going apply the shape deformation
 DV_MARKER= ( AIRFOIL )
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( Center, Thickness )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- OBSTACLE ( Center, Bump size )
-% 	- FFD_CONTROL_POINT ( FFD_BoxTag ID, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% 	- FFD_DIHEDRAL_ANGLE ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_TWIST_ANGLE ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_ROTATION ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_CAMBER ( FFD_BoxTag ID, i_Ind, j_Ind )
-% 	- FFD_THICKNESS ( FFD_BoxTag ID, i_Ind, j_Ind )
-% 	- FFD_VOLUME ( FFD_BoxTag ID, i_Ind, j_Ind )
 DV_PARAM= ( 1, 0.5 )
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-
-% Optimization objective function with optional scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.001
-
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= NONE
-
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 30, 1.0 | AIRFOIL | 0, 0.05 ); ( 30, 1.0 | AIRFOIL | 0, 0.10 ); ( 30, 1.0 | AIRFOIL | 0, 0.15 ); ( 30, 1.0 | AIRFOIL | 0, 0.20 ); ( 30, 1.0 | AIRFOIL | 0, 0.25 ); ( 30, 1.0 | AIRFOIL | 0, 0.30 ); ( 30, 1.0 | AIRFOIL | 0, 0.35 ); ( 30, 1.0 | AIRFOIL | 0, 0.40 ); ( 30, 1.0 | AIRFOIL | 0, 0.45 ); ( 30, 1.0 | AIRFOIL | 0, 0.50 ); ( 30, 1.0 | AIRFOIL | 0, 0.55 ); ( 30, 1.0 | AIRFOIL | 0, 0.60 ); ( 30, 1.0 | AIRFOIL | 0, 0.65 ); ( 30, 1.0 | AIRFOIL | 0, 0.70 ); ( 30, 1.0 | AIRFOIL | 0, 0.75 ); ( 30, 1.0 | AIRFOIL | 0, 0.80 ); ( 30, 1.0 | AIRFOIL | 0, 0.85 ); ( 30, 1.0 | AIRFOIL | 0, 0.90 ); ( 30, 1.0 | AIRFOIL | 0, 0.95 ); ( 30, 1.0 | AIRFOIL | 1, 0.05 ); ( 30, 1.0 | AIRFOIL | 1, 0.10 ); ( 30, 1.0 | AIRFOIL | 1, 0.15 ); ( 30, 1.0 | AIRFOIL | 1, 0.20 ); ( 30, 1.0 | AIRFOIL | 1, 0.25 ); ( 30, 1.0 | AIRFOIL | 1, 0.30 ); ( 30, 1.0 | AIRFOIL | 1, 0.35 ); ( 30, 1.0 | AIRFOIL | 1, 0.40 ); ( 30, 1.0 | AIRFOIL | 1, 0.45 ); ( 30, 1.0 | AIRFOIL | 1, 0.50 ); ( 30, 1.0 | AIRFOIL | 1, 0.55 ); ( 30, 1.0 | AIRFOIL | 1, 0.60 ); ( 30, 1.0 | AIRFOIL | 1, 0.65 ); ( 30, 1.0 | AIRFOIL | 1, 0.70 ); ( 30, 1.0 | AIRFOIL | 1, 0.75 ); ( 30, 1.0 | AIRFOIL | 1, 0.80 ); ( 30, 1.0 | AIRFOIL | 1, 0.85 ); ( 30, 1.0 | AIRFOIL | 1, 0.90 ); ( 30, 1.0 | AIRFOIL | 1, 0.95 )
diff --git a/TestCases/control_surface/inv_ONERAM6_moving.cfg b/TestCases/control_surface/inv_ONERAM6_moving.cfg
index 6a0e11929e8..5b2387101c8 100644
--- a/TestCases/control_surface/inv_ONERAM6_moving.cfg
+++ b/TestCases/control_surface/inv_ONERAM6_moving.cfg
@@ -5,350 +5,135 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 09.07.2011                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8395
-%
-% Angle of attack (degrees)
 AOA= 3.06
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only for Euler equations)
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % --------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.058 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.058
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 implies no marker)
 MARKER_EULER= ( UPPER_SIDE, LOWER_SIDE, TIP )
-%
-% Marker of the far field (0 implies no marker)
 MARKER_FAR= ( XNORMAL_FACES, ZNORMAL_FACES, YNORMAL_FACE )
-%
-% Marker of symmetry boundary (0 implies no marker)
 MARKER_SYM= ( SYMMETRY_FACE )
-%
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( UPPER_SIDE, LOWER_SIDE, TIP )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( UPPER_SIDE, LOWER_SIDE, TIP )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
-% Numerical method for computation of spatial gradients: (GREEN_GAUSS, 
-%                                                WIEGHTED_LEAST_SQUARES)
-NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 EXT_ITER= 99999
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.9
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.9
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.04 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE, TOTAL_HEAT,
-%                                     MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                     INVERSE_DESIGN_HEATFLUX)
-OBJECTIVE_FUNCTION= DRAG
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
+OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.04 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.5
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------&
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -6
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 100
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_ONERAM6_inv_FFD.su2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
-% Mesh input file format (SU2)
 MESH_FORMAT= SU2
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution frequency
 OUTPUT_WRT_FREQ= 50
-%
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Kind of deformation (FFD_SETTING, FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC,
-%                      NACA_4DIGITS, DISPLACEMENT, ROTATION, FFD_CONTROL_POINT, 
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CAMBER, FFD_THICKNESS, FFD_CONTROL_SURFACE, SURFACE_FILE, AIRFOIL)
 DV_KIND= FFD_CONTROL_SURFACE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( UPPER_SIDE, LOWER_SIDE, TIP )
-%
-% Parameters of the shape deformation 
-% 	- FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% 	- FFD_DIHEDRAL_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% 	- FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% 	- FFD_VOLUME ( FFD_BoxTag, i_Ind, j_Ind )
 DV_PARAM= ( FLAP, 0.630005, 0.0620207, 0.0, 0.847989, 0.79647, 0.0 )
-%
-% New value of the shape deformation
 DV_VALUE= -5.0
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 50
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-8
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 1000
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-
-% Optimization objective function with optional scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 100.0
-
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= (LIFT > 0.2855362768) * 100.0
-
-% List of design variables (Design variables are separated by semicolons)
 DEFINITION_DV= ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 0, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 1, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 2, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 3, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 4, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 0, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 1, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 2, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 3, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 4, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 0, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 1, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 2, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 3, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 4, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 0, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 1, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 2, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 3, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 4, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 0, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 1, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 2, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 3, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 4, 4, 1, 0.0, 0.0, 1.0 )
diff --git a/TestCases/control_surface/inv_ONERAM6_setting.cfg b/TestCases/control_surface/inv_ONERAM6_setting.cfg
index b634ce49464..ab9f9b8e35c 100644
--- a/TestCases/control_surface/inv_ONERAM6_setting.cfg
+++ b/TestCases/control_surface/inv_ONERAM6_setting.cfg
@@ -5,350 +5,135 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 09.07.2011                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8395
-%
-% Angle of attack (degrees)
 AOA= 3.06
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only for Euler equations)
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % --------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.058 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.058
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 implies no marker)
 MARKER_EULER= ( UPPER_SIDE, LOWER_SIDE, TIP )
-%
-% Marker of the far field (0 implies no marker)
 MARKER_FAR= ( XNORMAL_FACES, ZNORMAL_FACES, YNORMAL_FACE )
-%
-% Marker of symmetry boundary (0 implies no marker)
 MARKER_SYM= ( SYMMETRY_FACE )
-%
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( UPPER_SIDE, LOWER_SIDE, TIP )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( UPPER_SIDE, LOWER_SIDE, TIP )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
-% Numerical method for computation of spatial gradients: (GREEN_GAUSS, 
-%                                                WIEGHTED_LEAST_SQUARES)
-NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 EXT_ITER= 99999
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.9
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.9
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.04 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE, TOTAL_HEAT,
-%                                     MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                     INVERSE_DESIGN_HEATFLUX)
-OBJECTIVE_FUNCTION= DRAG
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
+OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.04 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.5
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------&
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -6
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 100
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_ONERAM6_inv.su2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_ONERAM6_inv_FFD.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
-% Mesh input file format (SU2)
 MESH_FORMAT= SU2
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution frequency
 OUTPUT_WRT_FREQ= 50
-%
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Kind of deformation (FFD_SETTING, FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC,
-%                      NACA_4DIGITS, DISPLACEMENT, ROTATION, FFD_CONTROL_POINT, 
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CAMBER, FFD_THICKNESS, FFD_CONTROL_SURFACE, SURFACE_FILE, AIRFOIL)
 DV_KIND= FFD_SETTING
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( UPPER_SIDE, LOWER_SIDE, TIP )
-%
-% Parameters of the shape deformation 
-% 	- FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% 	- FFD_DIHEDRAL_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% 	- FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% 	- FFD_VOLUME ( FFD_BoxTag, i_Ind, j_Ind )
 DV_PARAM= ( FLAP, 0.630005, 0.0620207, 0.0, 0.847989, 0.79647, 0.0 )
-%
-% New value of the shape deformation
 DV_VALUE= -5.0
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 50
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-8
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 1000
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-
-% Optimization objective function with optional scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 100.0
-
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= (LIFT > 0.2855362768) * 100.0
-
-% List of design variables (Design variables are separated by semicolons)
 DEFINITION_DV= ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 0, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 1, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 2, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 3, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 4, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 0, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 1, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 2, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 3, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 4, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 0, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 1, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 2, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 3, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 4, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 0, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 1, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 2, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 3, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 4, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 0, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 1, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 2, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 3, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 4, 4, 1, 0.0, 0.0, 1.0 )
diff --git a/TestCases/coupled_cht/comp_2d/cht_2d_3cylinders.cfg b/TestCases/coupled_cht/comp_2d/cht_2d_3cylinders.cfg
index bbdadbb0a4e..195ba2dcd9f 100644
--- a/TestCases/coupled_cht/comp_2d/cht_2d_3cylinders.cfg
+++ b/TestCases/coupled_cht/comp_2d/cht_2d_3cylinders.cfg
@@ -5,75 +5,26 @@
 % Author: O. Burghardt                                                          %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 6, 2020                                                         %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= MULTIPHYSICS
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-%
 CONFIG_LIST = (flow_cylinder.cfg, solid_cylinder1.cfg, solid_cylinder2.cfg, solid_cylinder3.cfg)
-%
-%
 MARKER_ZONE_INTERFACE= (cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2, cylinder_outer3, cylinder_inner3)
-%
-%
 MARKER_CHT_INTERFACE= (cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2, cylinder_outer3, cylinder_inner3)
-%
-%
 TIME_DOMAIN = NO
-%
-% Number of total iterations
 OUTER_ITER = 11
-%
-% Mesh input file
 MESH_FILENAME= mesh_cht_3cyl.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
 
-% These are just default parameters so that we can run SU2_DOT_AD, they have no physical meaning for this test case.
-
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (NO_DEFORMATION, TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING, FFD_NACELLE
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS, FFD_TWIST
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D, FFD_TWIST_2D,
-%                      HICKS_HENNE, SURFACE_BUMP)
+% These are just default parameters so that we can run SU2_DOT_AD, they have no physical meaning for this test case.
 DV_KIND= HICKS_HENNE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2, cylinder_outer3, cylinder_inner3  )
-%
-% Parameters of the shape deformation
-% - NO_DEFORMATION ( 1.0 )
-% - TRANSLATION ( x_Disp, y_Disp, z_Disp ), as a unit vector
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - SCALE ( 1.0 )
-% - ANGLE_OF_ATTACK ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_NACELLE ( FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Disp, phi_Disp )
-% - FFD_GULL ( FFD_BoxTag, j_Ind )
-% - FFD_ANGLE_OF_ATTACK ( FFD_BoxTag, 1.0 )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_TWIST ( FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - FFD_TWIST_2D ( FFD_BoxTag, x_Orig, y_Orig )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - SURFACE_BUMP ( x_Start, x_End, x_Loc )
 DV_PARAM= (0.0, 0.5)
-%
-% Value of the shape deformation
 DV_VALUE= 0.1
diff --git a/TestCases/coupled_cht/comp_2d/flow_cylinder.cfg b/TestCases/coupled_cht/comp_2d/flow_cylinder.cfg
index a6290d58da0..3b7870d310b 100644
--- a/TestCases/coupled_cht/comp_2d/flow_cylinder.cfg
+++ b/TestCases/coupled_cht/comp_2d/flow_cylinder.cfg
@@ -7,192 +7,79 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= NAVIER_STOKES
-%
-% If Navier-Stokes, kind of turbulent model (NONE, SA)
 KIND_TURB_MODEL= NONE
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= TOTAL_HEATFLUX
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT = 1.0
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART = YES
-%
-% Data written to history file
 HISTORY_OUTPUT=( ITER, RMS_RES, HEAT )
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.2
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Side-slip angle (degrees, only for compressible flows)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 297.62
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 100
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( cylinder_outer1, cylinder_outer2, cylinder_outer3 )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( cylinder_outer1, cylinder_outer2, cylinder_outer3 )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 10.0, 10000.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER_JACOBI,
-%                                                      SMOOTHER_ILU, SMOOTHER_LUSGS,
-%                                                      SMOOTHER_LINELET)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -19
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 200
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
-DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-
+DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
\ No newline at end of file
diff --git a/TestCases/coupled_cht/comp_2d/solid_cylinder1.cfg b/TestCases/coupled_cht/comp_2d/solid_cylinder1.cfg
index 0e963250a54..a68eec8fb9c 100644
--- a/TestCases/coupled_cht/comp_2d/solid_cylinder1.cfg
+++ b/TestCases/coupled_cht/comp_2d/solid_cylinder1.cfg
@@ -7,95 +7,43 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= HEAT_EQUATION
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= TOTAL_HEATFLUX
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT = 1.0
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART = YES
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
 MARKER_ISOTHERMAL= ( core1, 350.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= (cylinder_inner1 )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( NONE )
 
 % ---------------- (SOLIDS) CONDUCTION CONDITION DEFINITION -------------------%
 %
-% We should keep the dimensionalization of the coupled flow solver
 INC_NONDIM= DIMENSIONAL
-%
-% Temperature initialization value
 FREESTREAM_TEMPERATURE= 350.0
 %
 % Nettis case: hollow cylinder (air w/ 4x the conductivity)
 %
-% Solid density (kg/m^3)
 MATERIAL_DENSITY= 0.000210322
-%
-% Solid specific heat (J/kg*K)
 SPECIFIC_HEAT_CP= 1004.703
-%
-% Solid thermal conductivity (W/m*K)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.1028
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 10.0, 10000.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER_JACOBI,
-%                                                      SMOOTHER_ILU, SMOOTHER_LUSGS,
-%                                                      SMOOTHER_LINELET)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
@@ -104,74 +52,31 @@ TIME_DISCRE_HEAT= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -19
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 200
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
-DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-
+DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
\ No newline at end of file
diff --git a/TestCases/coupled_cht/comp_2d/solid_cylinder2.cfg b/TestCases/coupled_cht/comp_2d/solid_cylinder2.cfg
index 8384cdc4e88..18c18588158 100644
--- a/TestCases/coupled_cht/comp_2d/solid_cylinder2.cfg
+++ b/TestCases/coupled_cht/comp_2d/solid_cylinder2.cfg
@@ -7,181 +7,76 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= HEAT_EQUATION
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= TOTAL_HEATFLUX
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT = 1.0
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART = YES
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
 MARKER_ISOTHERMAL= ( core2, 350.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= (cylinder_inner2)
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( NONE )
 
 % ---------------- (SOLIDS) CONDUCTION CONDITION DEFINITION -------------------%
 %
-% We should keep the dimensionalization of the coupled flow solver
 INC_NONDIM= DIMENSIONAL
-%
-% Temperature initialization value
 FREESTREAM_TEMPERATURE= 350.0
 %
 % Nettis case: hollow cylinder (air w/ 4x the conductivity)
 %
-% Solid density (kg/m^3)
 MATERIAL_DENSITY= 0.000210322
-%
-% Solid specific heat (J/kg*K)
 SPECIFIC_HEAT_CP= 1004.703
-%
-% Solid thermal conductivity (W/m*K)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.1028
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 10.0, 10000.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER_JACOBI,
-%                                                      SMOOTHER_ILU, SMOOTHER_LUSGS,
-%                                                      SMOOTHER_LINELET)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Time discretization (EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_HEAT= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -19
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 200
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
-DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-
+DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
\ No newline at end of file
diff --git a/TestCases/coupled_cht/comp_2d/solid_cylinder3.cfg b/TestCases/coupled_cht/comp_2d/solid_cylinder3.cfg
index 9c4e5713efb..d3784d904ca 100644
--- a/TestCases/coupled_cht/comp_2d/solid_cylinder3.cfg
+++ b/TestCases/coupled_cht/comp_2d/solid_cylinder3.cfg
@@ -7,181 +7,75 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= HEAT_EQUATION
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= TOTAL_HEATFLUX
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT = 1.0
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART = YES
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
 MARKER_ISOTHERMAL= ( core3, 350.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( cylinder_inner3 )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( NONE )
 
 % ---------------- (SOLIDS) CONDUCTION CONDITION DEFINITION -------------------%
 %
-% We should keep the dimensionalization of the coupled flow solver
 INC_NONDIM= DIMENSIONAL
-%
-% Temperature initialization value
 FREESTREAM_TEMPERATURE= 350.0
 %
 % Nettis case: hollow cylinder (air w/ 4x the conductivity)
 %
-% Solid density (kg/m^3)
 MATERIAL_DENSITY= 0.000210322
-%
-% Solid specific heat (J/kg*K)
 SPECIFIC_HEAT_CP= 1004.703
-%
-% Solid thermal conductivity (W/m*K)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.1028
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 10.0, 10000.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER_JACOBI,
-%                                                      SMOOTHER_ILU, SMOOTHER_LUSGS,
-%                                                      SMOOTHER_LINELET)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
-%
-% Time discretization (EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_HEAT= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -19
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 200
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
-DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-
+DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
\ No newline at end of file
diff --git a/TestCases/coupled_cht/disc_adj_incomp_2d/cht_2d_3cylinders.cfg b/TestCases/coupled_cht/disc_adj_incomp_2d/cht_2d_3cylinders.cfg
index 19ded27f542..002f8283853 100644
--- a/TestCases/coupled_cht/disc_adj_incomp_2d/cht_2d_3cylinders.cfg
+++ b/TestCases/coupled_cht/disc_adj_incomp_2d/cht_2d_3cylinders.cfg
@@ -5,75 +5,26 @@
 % Author: O. Burghardt, T. Economon                                             %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: August 8, 2019                                                          %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)             
 SOLVER= MULTIPHYSICS
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT)
 MATH_PROBLEM= DISCRETE_ADJOINT
-%
-% 
 CONFIG_LIST = (flow_cylinder.cfg, solid_cylinder1.cfg, solid_cylinder2.cfg, solid_cylinder3.cfg)
-%
-%
 MARKER_ZONE_INTERFACE= (cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2, cylinder_outer3, cylinder_inner3)
-%
-%
 MARKER_CHT_INTERFACE= (cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2, cylinder_outer3, cylinder_inner3)
-%
-%
 TIME_DOMAIN = NO
-%
-% Number of total iterations
 OUTER_ITER = 11
-%
-% Mesh input file
 MESH_FILENAME= mesh_cht_3cyl.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
 
-% These are just default parameters so that we can run SU2_DOT_AD, they have no physical meaning for this test case.
-
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (NO_DEFORMATION, TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING, FFD_NACELLE
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS, FFD_TWIST
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D, FFD_TWIST_2D,
-%                      HICKS_HENNE, SURFACE_BUMP)
+% These are just default parameters so that we can run SU2_DOT_AD, they have no physical meaning for this test case.
 DV_KIND= HICKS_HENNE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2, cylinder_outer3, cylinder_inner3  )
-%
-% Parameters of the shape deformation
-% - NO_DEFORMATION ( 1.0 )
-% - TRANSLATION ( x_Disp, y_Disp, z_Disp ), as a unit vector
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - SCALE ( 1.0 )
-% - ANGLE_OF_ATTACK ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_NACELLE ( FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Disp, phi_Disp )
-% - FFD_GULL ( FFD_BoxTag, j_Ind )
-% - FFD_ANGLE_OF_ATTACK ( FFD_BoxTag, 1.0 )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_TWIST ( FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - FFD_TWIST_2D ( FFD_BoxTag, x_Orig, y_Orig )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - SURFACE_BUMP ( x_Start, x_End, x_Loc )
 DV_PARAM= (0.0, 0.5)
-%
-% Value of the shape deformation
 DV_VALUE= 0.1
diff --git a/TestCases/coupled_cht/disc_adj_incomp_2d/flow_cylinder.cfg b/TestCases/coupled_cht/disc_adj_incomp_2d/flow_cylinder.cfg
index 2a738735d09..500d5db42f1 100644
--- a/TestCases/coupled_cht/disc_adj_incomp_2d/flow_cylinder.cfg
+++ b/TestCases/coupled_cht/disc_adj_incomp_2d/flow_cylinder.cfg
@@ -7,246 +7,102 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                           
 SOLVER= INC_NAVIER_STOKES
-%
-% If Navier-Stokes, kind of turbulent model (NONE, SA)
 KIND_TURB_MODEL= NONE
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
-%
+
 % Gradient for this test case from direct differentiation (to confirm adjoints results, if desired): -0.716778
-%
 OBJECTIVE_FUNCTION= TOTAL_HEATFLUX
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT = 1.0
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART = YES
-%
-% Data written to history file
 HISTORY_OUTPUT=(ITER, RMS_RES, HEAT )
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= (cylinder_outer1, cylinder_outer2, cylinder_outer3)
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= (cylinder_outer1, cylinder_outer2, cylinder_outer3)
 
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
-% Density model within the incompressible flow solver.
-% Options are CONSTANT (default), BOUSSINESQ, or VARIABLE. If VARIABLE,
-% an appropriate fluid model must be selected.
 INC_DENSITY_MODEL= VARIABLE
-%
-% Solve the energy equation in the incompressible flow solver
 INC_ENERGY_EQUATION = YES
-%
-% Initial density for incompressible flows (1.2886 kg/m^3 by default)
 INC_DENSITY_INIT= 0.000210322
-%
-% Initial velocity for incompressible flows (1.0,0,0 m/s by default)
 INC_VELOCITY_INIT= ( 3.40297, 0.0, 0.0 )
-%
-% Initial temperature for incompressible flows that include the
-% energy equation (288.15 K by default). Value is ignored if
-% INC_ENERGY_EQUATION is false.
 INC_TEMPERATURE_INIT= 288.15
-%
-% Non-dimensionalization scheme for incompressible flows. Options are
-% INITIAL_VALUES (default), REFERENCE_VALUES, or DIMENSIONAL.
-% INC_*_REF values are ignored unless REFERENCE_VALUES is chosen.
 INC_NONDIM= DIMENSIONAL
 
 % ---- IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
-% Fluid model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS,
-%              CONSTANT_DENSITY, INC_IDEAL_GAS)
 FLUID_MODEL= INC_IDEAL_GAS
-%
-% Specific heat at constant pressure, Cp (1004.703 J/kg*K (air)).
-% Incompressible fluids with energy eqn. only (CONSTANT_DENSITY, INC_IDEAL_GAS).
 SPECIFIC_HEAT_CP= 1004.703
-%
-% Molecular weight for an incompressible ideal gas (28.96 g/mol (air) default)
-% Incompressible fluids with energy eqn. only (CONSTANT_DENSITY, INC_IDEAL_GAS).
 MOLECULAR_WEIGHT= 28.96
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.7893e-05
-%
-% Sutherland Viscosity Ref (1.716E-5 default value for AIR SI)
 MU_REF= 1.716E-5
-%
-% Sutherland Temperature Ref (273.15 K default value for AIR SI)
 MU_T_REF= 273.15
-%
-% Sutherland constant (110.4 default value for AIR SI)
 SUTHERLAND_CONSTANT= 110.4
 
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
-% Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL).
 CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
-%
-% Molecular Thermal Conductivity that would be constant (0.0257 by default)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.0257
-%
-% Laminar Prandtl number (0.72 (air), only for CONSTANT_PRANDTL)
 PRANDTL_LAM= 0.72
-%
-% Turbulent Prandtl number (0.9 (air), only for CONSTANT_PRANDTL)
 PRANDTL_TURB= 0.90
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 10.0, 10000.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER_JACOBI,
-%                                                      SMOOTHER_ILU, SMOOTHER_LUSGS,
-%                                                      SMOOTHER_LINELET)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= FDS
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -19
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 200
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
-DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-
+DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
\ No newline at end of file
diff --git a/TestCases/coupled_cht/disc_adj_incomp_2d/solid_cylinder1.cfg b/TestCases/coupled_cht/disc_adj_incomp_2d/solid_cylinder1.cfg
index a63963c9542..99b61f65992 100644
--- a/TestCases/coupled_cht/disc_adj_incomp_2d/solid_cylinder1.cfg
+++ b/TestCases/coupled_cht/disc_adj_incomp_2d/solid_cylinder1.cfg
@@ -7,95 +7,43 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                           
 SOLVER= HEAT_EQUATION
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= TOTAL_HEATFLUX
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT = 1.0
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART = YES
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
 MARKER_ISOTHERMAL= ( core1, 350.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= (cylinder_inner1 )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( NONE )
 
 % ---------------- (SOLIDS) CONDUCTION CONDITION DEFINITION -------------------%
 %
 % We should keep the dimensionalization of the coupled flow solver
 INC_NONDIM= DIMENSIONAL
-%
-% Temperature initialization value
 FREESTREAM_TEMPERATURE= 350.0
 %
 % Nettis case: hollow cylinder (air w/ 4x the conductivity)
-%
-% Solid density (kg/m^3)
 MATERIAL_DENSITY= 0.000210322
-%
-% Solid specific heat (J/kg*K)
 SPECIFIC_HEAT_CP = 1004.703
-%
-% Solid thermal conductivity (W/m*K)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.1028
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 10.0, 10000.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER_JACOBI,
-%                                                      SMOOTHER_ILU, SMOOTHER_LUSGS,
-%                                                      SMOOTHER_LINELET)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
@@ -104,74 +52,31 @@ TIME_DISCRE_HEAT= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -19
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 200
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
-DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-
+DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
\ No newline at end of file
diff --git a/TestCases/coupled_cht/disc_adj_incomp_2d/solid_cylinder2.cfg b/TestCases/coupled_cht/disc_adj_incomp_2d/solid_cylinder2.cfg
index 37fffcd287b..bb8267047bb 100644
--- a/TestCases/coupled_cht/disc_adj_incomp_2d/solid_cylinder2.cfg
+++ b/TestCases/coupled_cht/disc_adj_incomp_2d/solid_cylinder2.cfg
@@ -7,181 +7,76 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                           
 SOLVER= HEAT_EQUATION
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= TOTAL_HEATFLUX
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT = 1.0
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART = YES
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
 MARKER_ISOTHERMAL= ( core2, 350.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= (cylinder_inner2)
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( NONE )
 
 % ---------------- (SOLIDS) CONDUCTION CONDITION DEFINITION -------------------%
 %
 % We should keep the dimensionalization of the coupled flow solver
 INC_NONDIM= DIMENSIONAL
-%
-% Temperature initialization value
 FREESTREAM_TEMPERATURE= 350.0
 %
 % Nettis case: hollow cylinder (air w/ 4x the conductivity)
-%
-% Solid density (kg/m^3)
 MATERIAL_DENSITY= 0.000210322
-%
-% Solid specific heat (J/kg*K)
 SPECIFIC_HEAT_CP = 1004.703
-%
-% Solid thermal conductivity (W/m*K)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.1028
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 10.0, 10000.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER_JACOBI,
-%                                                      SMOOTHER_ILU, SMOOTHER_LUSGS,
-%                                                      SMOOTHER_LINELET)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Time discretization (EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_HEAT= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -19
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 200
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
-DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-
+DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
\ No newline at end of file
diff --git a/TestCases/coupled_cht/disc_adj_incomp_2d/solid_cylinder3.cfg b/TestCases/coupled_cht/disc_adj_incomp_2d/solid_cylinder3.cfg
index 6e95af6bce7..5670dc79ea0 100644
--- a/TestCases/coupled_cht/disc_adj_incomp_2d/solid_cylinder3.cfg
+++ b/TestCases/coupled_cht/disc_adj_incomp_2d/solid_cylinder3.cfg
@@ -7,181 +7,76 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                           
 SOLVER= HEAT_EQUATION
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= TOTAL_HEATFLUX
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT = 1.0
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART = YES
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
 MARKER_ISOTHERMAL= ( core3, 350.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( cylinder_inner3 )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( NONE )
 
 % ---------------- (SOLIDS) CONDUCTION CONDITION DEFINITION -------------------%
 %
 % We should keep the dimensionalization of the coupled flow solver
 INC_NONDIM= DIMENSIONAL
-%
-% Temperature initialization value
 FREESTREAM_TEMPERATURE= 350.0
 %
 % Nettis case: hollow cylinder (air w/ 4x the conductivity)
-%
-% Solid density (kg/m^3)
 MATERIAL_DENSITY= 0.000210322
-%
-% Solid specific heat (J/kg*K)
 SPECIFIC_HEAT_CP = 1004.703
-%
-% Solid thermal conductivity (W/m*K)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.1028
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 10.0, 10000.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER_JACOBI,
-%                                                      SMOOTHER_ILU, SMOOTHER_LUSGS,
-%                                                      SMOOTHER_LINELET)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Time discretization (EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_HEAT= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -19
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 200
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-
diff --git a/TestCases/coupled_cht/disc_adj_unsteadyCHT_cylinder/chtMaster.cfg b/TestCases/coupled_cht/disc_adj_unsteadyCHT_cylinder/chtMaster.cfg
index a32ece5723b..6f3f5c486da 100644
--- a/TestCases/coupled_cht/disc_adj_unsteadyCHT_cylinder/chtMaster.cfg
+++ b/TestCases/coupled_cht/disc_adj_unsteadyCHT_cylinder/chtMaster.cfg
@@ -10,91 +10,62 @@ SOLUTION_FILENAME= solution
 RESTART_FILENAME= solution
 %
 CONFIG_LIST = ( fluid.cfg, solid.cfg )
-%
 MARKER_ZONE_INTERFACE= ( cylinder_fluid, cylinder_solid )
 MARKER_CHT_INTERFACE=  ( cylinder_fluid, cylinder_solid )
-%
+
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
 TIME_DOMAIN= YES
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-%
 TIME_STEP= 500
-%
 MAX_TIME= 1e9
 % For a primal restart change TIME_ITER=56 for the correct number of steps. 54 is for the adjoint run.
 TIME_ITER= 54
 % For the primal (and therefore FD sweep) OUTER_ITER=200 is suitable.
 % For an accurate adjont run set OUTER_ITER=500. 100 is for the regression test.
 OUTER_ITER= 100
-%INNER_ITER= 1
-%
 UNST_ADJOINT_ITER= 56
-%
 ITER_AVERAGE_OBJ= 54
-%
+
 % ------------------------- INPUT/OUTPUT FILE INFORMATION --------------------------%
 %
 MESH_FILENAME= MeshCHT.su2
-%
 SCREEN_OUTPUT= (TIME_ITER, OUTER_ITER, BGS_ADJ_PRESSURE[0], BGS_ADJ_VELOCITY-X[0], BGS_ADJ_VELOCITY-Y[0], BGS_ADJ_TEMPERATURE[0], BGS_ADJ_TEMPERATURE[1], SENS_TEMP[0], SENS_GEO[0], SENS_GEO[1] )
 % Suitable output for primal simulations
 %SCREEN_OUTPUT= (TIME_ITER, OUTER_ITER, WALL_TIME, BGS_PRESSURE[0], BGS_TEMPERATURE[0], BGS_TEMPERATURE[1], DRAG[0], AVG_TEMPERATURE[1] )
 SCREEN_WRT_FREQ_OUTER= 50
-%
 HISTORY_OUTPUT= ( ITER, BGS_RES[0], RMS_RES[0], BGS_RES[1], RMS_RES[1],\
  FLOW_COEFF[0], HEAT[0], AERO_COEFF[0], HEAT[1],\
  LINSOL[0], LINSOL[1], TAVG_HEAT[1])
-%
 OUTPUT_FILES= (RESTART, PARAVIEW)
 OUTPUT_WRT_FREQ= 1
 VOLUME_FILENAME= flow
 WRT_PERFORMANCE= YES
-%
 SOLUTION_ADJ_FILENAME= solution_adj
 RESTART_ADJ_FILENAME= solution_adj
 VOLUME_ADJ_FILENAME= flow_adj
-%
 TABULAR_FORMAT= CSV
 GRAD_OBJFUNC_FILENAME= of_grad.csv
 OUTPUT_PRECISION=16
-%
+
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
 FFD_TOLERANCE= 1E-10
 FFD_ITERATIONS= 500
-%
-% FFD box definition: 2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
-% Counterclockwise definition of FFD cornerpoints
 FFD_DEFINITION= (BOX,\
  -0.6,-0.6,0.0,\
   0.6,-0.6,0.0,\
   0.6, 0.6,0.0,\
  -0.6, 0.6,0.0,\
  0.0,0.0,0.0,  0.0,0.0,0.0  0.0,0.0,0.0,  0.0,0.0,0.0 )
-%
-% FFD box degree: 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= (8, 1, 0)
-%
-% Surface grid continuity at the intersection with the faces of the FFD boxes.
-% To keep a particular level of surface continuity, SU2 automatically freezes the right
-% number of control point planes (NO_DERIVATIVE, 1ST_DERIVATIVE, 2ND_DERIVATIVE, USER_INPUT)
 FFD_CONTINUITY= NO_DERIVATIVE
-%
+
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-%DV_KIND= FFD_SETTING
 % First 9 are upper, second 9 are lower DV's
 DV_KIND= FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D, FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( cylinder_fluid, cylinder_solid )
-%
-% Parameters of the shape deformation
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-%DV_PARAM= ( 1.0 )
 DV_PARAM= \
 ( BOX, 0, 1, 0.0, 1.0);\
 ( BOX, 1, 1, 0.0, 1.0);\
@@ -114,10 +85,8 @@ DV_PARAM= \
 ( BOX, 6, 0, 0.0, 1.0);\
 ( BOX, 7, 0, 0.0, 1.0);\
 ( BOX, 8, 0, 0.0, 1.0)
-%
-% Value of the shape deformation
 DV_VALUE= 1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0, 1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0
-%
+
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
 DEFORM_LINEAR_SOLVER= FGMRES
@@ -125,10 +94,8 @@ DEFORM_LINEAR_SOLVER_PREC= ILU
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
 DEFORM_NONLINEAR_ITER= 1
 DEFORM_LINEAR_SOLVER_ITER= 1000
-%
 DEFORM_CONSOLE_OUTPUT= YES
 DEFORM_STIFFNESS_TYPE= WALL_DISTANCE
-%
 DEFINITION_DV= \
 ( 19, 1.0 | cylinder_fluid, cylinder_solid | BOX, 0, 1, 0.0, 1.0 ); \
 ( 19, 1.0 | cylinder_fluid, cylinder_solid | BOX, 1, 1, 0.0, 1.0 ); \
@@ -147,5 +114,4 @@ DEFINITION_DV= \
 ( 19, 1.0 | cylinder_fluid, cylinder_solid | BOX, 5, 0, 0.0, 1.0 ); \
 ( 19, 1.0 | cylinder_fluid, cylinder_solid | BOX, 6, 0, 0.0, 1.0 ); \
 ( 19, 1.0 | cylinder_fluid, cylinder_solid | BOX, 7, 0, 0.0, 1.0 ); \
-( 19, 1.0 | cylinder_fluid, cylinder_solid | BOX, 8, 0, 0.0, 1.0 )
-
+( 19, 1.0 | cylinder_fluid, cylinder_solid | BOX, 8, 0, 0.0, 1.0 )
\ No newline at end of file
diff --git a/TestCases/coupled_cht/disc_adj_unsteadyCHT_cylinder/fluid.cfg b/TestCases/coupled_cht/disc_adj_unsteadyCHT_cylinder/fluid.cfg
index b4fe5b28efb..d4e4a3ce2ef 100644
--- a/TestCases/coupled_cht/disc_adj_unsteadyCHT_cylinder/fluid.cfg
+++ b/TestCases/coupled_cht/disc_adj_unsteadyCHT_cylinder/fluid.cfg
@@ -1,11 +1,10 @@
 % TobiKattmann 2021-03-11
 %
 SOLVER= INC_NAVIER_STOKES
-%
 OBJECTIVE_FUNCTION= AVG_TEMPERATURE
 %OBJECTIVE_FUNCTION= DRAG
 OBJECTIVE_WEIGHT= 0.0
-%
+
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
 INC_NONDIM= DIMENSIONAL
@@ -19,7 +18,6 @@ INC_VELOCITY_INIT= ( 2.0e-4, 0.0, 0.0 )
 INC_ENERGY_EQUATION= YES
 INC_TEMPERATURE_INIT= 288.15
 SPECIFIC_HEAT_CP= 4180
-%
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
 MU_CONSTANT= 1.0e-3
 %
@@ -27,54 +25,40 @@ MU_CONSTANT= 1.0e-3
 % lambda_water = 0.6 => Pr = 4180 * 1e-3 / 0.6 = 6.96
 CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
 PRANDTL_LAM = 6.96
-%
+
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
 MARKER_FAR= ( farfield )
 %MARKER_HEATFLUX= ( cylinder_fluid, 1e2 )
-%
+
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
 CFL_NUMBER= 1e3
 CFL_ADAPT= NO
 CFL_ADAPT_PARAM= ( 0.8, 1.4, 10.0, 1e10, 0.001 )
-%
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
+
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
 LINEAR_SOLVER= FGMRES
 LINEAR_SOLVER_PREC= ILU
-%LINEAR_SOLVER_ERROR= 1E-4
 LINEAR_SOLVER_ERROR= 1E-8
 LINEAR_SOLVER_ITER= 20
-%
 CONV_NUM_METHOD_FLOW= FDS
 MUSCL_FLOW= YES
 SLOPE_LIMITER_FLOW= NONE
 TIME_DISCRE_FLOW= EULER_IMPLICIT
-%
+
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
 CONV_RESIDUAL_MINVAL= -20
 CONV_STARTITER= 2000
 CONV_CAUCHY_ELEMS= 100
 CONV_CAUCHY_EPS= 1E-6
-%
+
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-%MESH_FILENAME= fluid.su2
-%
-%SCREEN_OUTPUT= (TIME_ITER, WALL_TIME, INNER_ITER, RMS_PRESSURE, RMS_VELOCITY-X, DRAG, LIFT, AVG_TEMPERATURE, TOTAL_HEATFLUX )
-%SCREEN_WRT_FREQ_INNER= 100
-%
-%HISTORY_OUTPUT= (ITER, RMS_RES, AERO_COEFF, HEAT, FLOW_COEFF, LINSOL)
-%HISTORY_WRT_FREQ_INNER= 100
 MARKER_MONITORING= ( cylinder_fluid )
 MARKER_ANALYZE= ( cylinder_fluid )
 MARKER_ANALYZE_AVERAGE= AREA
-%
-%OUTPUT_FILES= ( RESTART, PARAVIEW )
-
diff --git a/TestCases/coupled_cht/disc_adj_unsteadyCHT_cylinder/solid.cfg b/TestCases/coupled_cht/disc_adj_unsteadyCHT_cylinder/solid.cfg
index 56aad35a2c0..3fb2d6bafd2 100644
--- a/TestCases/coupled_cht/disc_adj_unsteadyCHT_cylinder/solid.cfg
+++ b/TestCases/coupled_cht/disc_adj_unsteadyCHT_cylinder/solid.cfg
@@ -1,11 +1,10 @@
 % 2021-03-11 TobiKattmann
 %
 SOLVER= HEAT_EQUATION
-%
 OBJECTIVE_FUNCTION= AVG_TEMPERATURE
 %OBJECTIVE_FUNCTION= DRAG
 OBJECTIVE_WEIGHT= 1.0
-%
+
 % ---------------- (SOLIDS) CONDUCTION CONDITION DEFINITION -------------------%
 %
 % ~Aluminium at room temperature
@@ -15,45 +14,38 @@ FREESTREAM_TEMPERATURE= 340.0
 MATERIAL_DENSITY= 2719
 SPECIFIC_HEAT_CP = 0.8710
 THERMAL_CONDUCTIVITY_CONSTANT= 200
-%
+
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
 MARKER_HEATFLUX= ( inner_pin, 1e3 )
-%
+
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
 CFL_NUMBER= 1e4
 CFL_ADAPT= NO
 CFL_ADAPT_PARAM= ( 0.1, 2.0, 10.0, 1e10, 0.001 )
-%
 BETA_FACTOR= 50
 MAX_DELTA_TIME= 1.0
-%
+
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
 LINEAR_SOLVER= FGMRES
 LINEAR_SOLVER_PREC= ILU
 LINEAR_SOLVER_ERROR= 1E-15
 LINEAR_SOLVER_ITER= 20
-%
+
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
 CONV_RESIDUAL_MINVAL= -20
 CONV_STARTITER= 10000
-%
+
 % -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_HEAT = SPACE_CENTERED
 TIME_DISCRE_HEAT= EULER_IMPLICIT
-%
+
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-%MESH_FILENAME= solid.su2
-%
-%HISTORY_OUTPUT= (ITER, RMS_RES, HEAT, LINSOL)
 HISTORY_OUTPUT= (HEAT)
 MARKER_MONITORING= ( inner_pin )
-%MARKER_ANALYZE= ( inner_pin )
-
diff --git a/TestCases/coupled_cht/incomp_2d/cht_2d_3cylinders.cfg b/TestCases/coupled_cht/incomp_2d/cht_2d_3cylinders.cfg
index 40687a73746..cb4f1982f9f 100644
--- a/TestCases/coupled_cht/incomp_2d/cht_2d_3cylinders.cfg
+++ b/TestCases/coupled_cht/incomp_2d/cht_2d_3cylinders.cfg
@@ -5,78 +5,27 @@
 % Author: O. Burghardt, T. Economon                                             %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: August 8, 2019                                                          %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)             
 SOLVER= MULTIPHYSICS
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% 
 CONFIG_LIST = (flow_cylinder.cfg, solid_cylinder1.cfg, solid_cylinder2.cfg, solid_cylinder3.cfg)
-%
-%
 MARKER_ZONE_INTERFACE= (cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2, cylinder_outer3, cylinder_inner3)
-%
-%
 MARKER_CHT_INTERFACE= (cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2, cylinder_outer3, cylinder_inner3)
-%
-%
 CHT_COUPLING_METHOD= DIRECT_TEMPERATURE_ROBIN_HEATFLUX
-%
-%
 TIME_DOMAIN = NO
-%
-% Number of total iterations
 OUTER_ITER = 11
-%
-% Mesh input file
 MESH_FILENAME= mesh_cht_3cyl.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
 
-% These are just default parameters so that we can run SU2_DOT_AD, they have no physical meaning for this test case.
-
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (NO_DEFORMATION, TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING, FFD_NACELLE
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS, FFD_TWIST
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D, FFD_TWIST_2D,
-%                      HICKS_HENNE, SURFACE_BUMP)
+% These are just default parameters so that we can run SU2_DOT_AD, they have no physical meaning for this test case.
 DV_KIND= HICKS_HENNE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2, cylinder_outer3, cylinder_inner3  )
-%
-% Parameters of the shape deformation
-% - NO_DEFORMATION ( 1.0 )
-% - TRANSLATION ( x_Disp, y_Disp, z_Disp ), as a unit vector
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - SCALE ( 1.0 )
-% - ANGLE_OF_ATTACK ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_NACELLE ( FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Disp, phi_Disp )
-% - FFD_GULL ( FFD_BoxTag, j_Ind )
-% - FFD_ANGLE_OF_ATTACK ( FFD_BoxTag, 1.0 )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_TWIST ( FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - FFD_TWIST_2D ( FFD_BoxTag, x_Orig, y_Orig )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - SURFACE_BUMP ( x_Start, x_End, x_Loc )
 DV_PARAM= (0.0, 0.5)
-%
-% Value of the shape deformation
 DV_VALUE= 0.1
diff --git a/TestCases/coupled_cht/incomp_2d/flow_cylinder.cfg b/TestCases/coupled_cht/incomp_2d/flow_cylinder.cfg
index ea34a488071..360d8a94e50 100644
--- a/TestCases/coupled_cht/incomp_2d/flow_cylinder.cfg
+++ b/TestCases/coupled_cht/incomp_2d/flow_cylinder.cfg
@@ -7,243 +7,100 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                           
 SOLVER= INC_NAVIER_STOKES
-%
-% If Navier-Stokes, kind of turbulent model (NONE, SA)
 KIND_TURB_MODEL= NONE
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= TOTAL_HEATFLUX
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT = 1.0
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART = YES
-%
-% Data written to history file
 HISTORY_OUTPUT=(ITER, RMS_RES, HEAT )
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= (cylinder_outer1, cylinder_outer2, cylinder_outer3)
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= (cylinder_outer1, cylinder_outer2, cylinder_outer3)
 
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
-% Density model within the incompressible flow solver.
-% Options are CONSTANT (default), BOUSSINESQ, or VARIABLE. If VARIABLE,
-% an appropriate fluid model must be selected.
 INC_DENSITY_MODEL= VARIABLE
-%
-% Solve the energy equation in the incompressible flow solver
 INC_ENERGY_EQUATION = YES
-%
-% Initial density for incompressible flows (1.2886 kg/m^3 by default)
 INC_DENSITY_INIT= 0.000210322
-%
-% Initial velocity for incompressible flows (1.0,0,0 m/s by default)
 INC_VELOCITY_INIT= ( 3.40297, 0.0, 0.0 )
-%
-% Initial temperature for incompressible flows that include the
-% energy equation (288.15 K by default). Value is ignored if
-% INC_ENERGY_EQUATION is false.
 INC_TEMPERATURE_INIT= 288.15
-%
-% Non-dimensionalization scheme for incompressible flows. Options are
-% INITIAL_VALUES (default), REFERENCE_VALUES, or DIMENSIONAL.
-% INC_*_REF values are ignored unless REFERENCE_VALUES is chosen.
 INC_NONDIM= DIMENSIONAL
 
 % ---- IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
-% Fluid model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS,
-%              CONSTANT_DENSITY, INC_IDEAL_GAS)
 FLUID_MODEL= INC_IDEAL_GAS
-%
-% Specific heat at constant pressure, Cp (1004.703 J/kg*K (air)).
-% Incompressible fluids with energy eqn. only (CONSTANT_DENSITY, INC_IDEAL_GAS).
 SPECIFIC_HEAT_CP= 1004.703
-%
-% Molecular weight for an incompressible ideal gas (28.96 g/mol (air) default)
-% Incompressible fluids with energy eqn. only (CONSTANT_DENSITY, INC_IDEAL_GAS).
 MOLECULAR_WEIGHT= 28.96
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.7893e-05
-%
-% Sutherland Viscosity Ref (1.716E-5 default value for AIR SI)
 MU_REF= 1.716E-5
-%
-% Sutherland Temperature Ref (273.15 K default value for AIR SI)
 MU_T_REF= 273.15
-%
-% Sutherland constant (110.4 default value for AIR SI)
 SUTHERLAND_CONSTANT= 110.4
 
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
-% Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL).
 CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
-%
-% Molecular Thermal Conductivity that would be constant (0.0257 by default)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.0257
-%
-% Laminar Prandtl number (0.72 (air), only for CONSTANT_PRANDTL)
 PRANDTL_LAM= 0.72
-%
-% Turbulent Prandtl number (0.9 (air), only for CONSTANT_PRANDTL)
 PRANDTL_TURB= 0.90
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 10.0, 10000.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER_JACOBI,
-%                                                      SMOOTHER_ILU, SMOOTHER_LUSGS,
-%                                                      SMOOTHER_LINELET)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= FDS
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -19
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 200
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-
diff --git a/TestCases/coupled_cht/incomp_2d/solid_cylinder1.cfg b/TestCases/coupled_cht/incomp_2d/solid_cylinder1.cfg
index ba2a43f5b39..63a00c08dea 100644
--- a/TestCases/coupled_cht/incomp_2d/solid_cylinder1.cfg
+++ b/TestCases/coupled_cht/incomp_2d/solid_cylinder1.cfg
@@ -7,95 +7,44 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                           
 SOLVER= HEAT_EQUATION
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= TOTAL_HEATFLUX
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT = 1.0
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART = YES
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
 MARKER_ISOTHERMAL= ( core1, 350.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= (cylinder_inner1 )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( NONE )
 
 % ---------------- (SOLIDS) CONDUCTION CONDITION DEFINITION -------------------%
 %
 % We should keep the dimensionalization of the coupled flow solver
 INC_NONDIM= DIMENSIONAL
-%
-% Temperature initialization value
 FREESTREAM_TEMPERATURE= 350.0
 %
 % Nettis case: hollow cylinder (air w/ 4x the conductivity)
 %
-% Solid density (kg/m^3)
 MATERIAL_DENSITY= 0.000210322
-%
-% Solid specific heat (J/kg*K)
 SPECIFIC_HEAT_CP= 1004.703
-%
-% Solid thermal conductivity (W/m*K)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.1028
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 10.0, 10000.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER_JACOBI,
-%                                                      SMOOTHER_ILU, SMOOTHER_LUSGS,
-%                                                      SMOOTHER_LINELET)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
@@ -104,74 +53,31 @@ TIME_DISCRE_HEAT= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -19
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 200
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-
diff --git a/TestCases/coupled_cht/incomp_2d/solid_cylinder2.cfg b/TestCases/coupled_cht/incomp_2d/solid_cylinder2.cfg
index 6f336369e9d..ab8221cce5c 100644
--- a/TestCases/coupled_cht/incomp_2d/solid_cylinder2.cfg
+++ b/TestCases/coupled_cht/incomp_2d/solid_cylinder2.cfg
@@ -7,181 +7,77 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                           
 SOLVER= HEAT_EQUATION
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= TOTAL_HEATFLUX
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT = 1.0
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART = YES
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
 MARKER_ISOTHERMAL= ( core2, 350.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= (cylinder_inner2)
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( NONE )
 
 % ---------------- (SOLIDS) CONDUCTION CONDITION DEFINITION -------------------%
 %
 % We should keep the dimensionalization of the coupled flow solver
 INC_NONDIM= DIMENSIONAL
-%
-% Temperature initialization value
 FREESTREAM_TEMPERATURE= 350.0
 %
 % Nettis case: hollow cylinder (air w/ 4x the conductivity)
 %
-% Solid density (kg/m^3)
 MATERIAL_DENSITY= 0.000210322
-%
-% Solid specific heat (J/kg*K)
 SPECIFIC_HEAT_CP= 1004.703
-%
-% Solid thermal conductivity (W/m*K)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.1028
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 10.0, 10000.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER_JACOBI,
-%                                                      SMOOTHER_ILU, SMOOTHER_LUSGS,
-%                                                      SMOOTHER_LINELET)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Time discretization (EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_HEAT= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -19
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 200
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-
diff --git a/TestCases/coupled_cht/incomp_2d/solid_cylinder3.cfg b/TestCases/coupled_cht/incomp_2d/solid_cylinder3.cfg
index 5c45bfb3105..7db6b4b6c75 100644
--- a/TestCases/coupled_cht/incomp_2d/solid_cylinder3.cfg
+++ b/TestCases/coupled_cht/incomp_2d/solid_cylinder3.cfg
@@ -7,181 +7,77 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                           
 SOLVER= HEAT_EQUATION
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= TOTAL_HEATFLUX
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT = 1.0
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART = YES
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
 MARKER_ISOTHERMAL= ( core3, 350.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( cylinder_inner3 )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( NONE )
 
 % ---------------- (SOLIDS) CONDUCTION CONDITION DEFINITION -------------------%
 %
 % We should keep the dimensionalization of the coupled flow solver
 INC_NONDIM= DIMENSIONAL
-%
-% Temperature initialization value
 FREESTREAM_TEMPERATURE= 350.0
 %
 % Nettis case: hollow cylinder (air w/ 4x the conductivity)
 %
-% Solid density (kg/m^3)
 MATERIAL_DENSITY= 0.000210322
-%
-% Solid specific heat (J/kg*K)
 SPECIFIC_HEAT_CP= 1004.703
-%
-% Solid thermal conductivity (W/m*K)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.1028
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 10.0, 10000.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER_JACOBI,
-%                                                      SMOOTHER_ILU, SMOOTHER_LUSGS,
-%                                                      SMOOTHER_LINELET)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Time discretization (EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_HEAT= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -19
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 200
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-
diff --git a/TestCases/coupled_cht/incomp_2d_unsteady/cht_2d_3cylinders.cfg b/TestCases/coupled_cht/incomp_2d_unsteady/cht_2d_3cylinders.cfg
index 2c13eae13e4..edb3c23823f 100644
--- a/TestCases/coupled_cht/incomp_2d_unsteady/cht_2d_3cylinders.cfg
+++ b/TestCases/coupled_cht/incomp_2d_unsteady/cht_2d_3cylinders.cfg
@@ -5,59 +5,24 @@
 % Author: O. Burghardt, T. Economon                                             %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: August 8, 2019                                                          %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
-%
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 SOLVER= MULTIPHYSICS
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-%
 CONFIG_LIST = (flow_cylinder.cfg, solid_cylinder1.cfg, solid_cylinder2.cfg, solid_cylinder3.cfg)
-%
-%
 MARKER_ZONE_INTERFACE= (cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2, cylinder_outer3, cylinder_inner3)
-%
-%
 MARKER_CHT_INTERFACE= (cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2, cylinder_outer3, cylinder_inner3)
-%
-% Time domain simulation
 TIME_DOMAIN = YES
-%
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER,
-%                      DUAL_TIME_STEPPING-2ND_ORDER, HARMONIC_BALANCE)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-%
-% Time Step for dual time stepping simulations (s) -- Only used when UNST_CFL_NUMBER = 0.0
-% For the DG-FEM solver it is used as a synchronization time when UNST_CFL_NUMBER != 0.0
 TIME_STEP= 0.05
-%
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 100.0
-%
-% Maximum number of time iterations
 TIME_ITER= 3
-%
-% Number of total iterations
 OUTER_ITER = 10
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 100.0
-%
-% Mesh input file
 MESH_FILENAME= mesh_cht_3cyl.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-%
 HISTORY_OUTPUT= (ITER, BGS_RES[0], BGS_RES[1], BGS_RES[2], BGS_RES[3], HEAT[0], AERO_COEFF[0])
-%
-%
 OUTPUT_FILES=(RESTART, PARAVIEW_MULTIBLOCK)
diff --git a/TestCases/coupled_cht/incomp_2d_unsteady/flow_cylinder.cfg b/TestCases/coupled_cht/incomp_2d_unsteady/flow_cylinder.cfg
index ffc9c528454..c99794377c8 100644
--- a/TestCases/coupled_cht/incomp_2d_unsteady/flow_cylinder.cfg
+++ b/TestCases/coupled_cht/incomp_2d_unsteady/flow_cylinder.cfg
@@ -7,230 +7,96 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= INC_NAVIER_STOKES
-%
-% If Navier-Stokes, kind of turbulent model (NONE, SA)
 KIND_TURB_MODEL= NONE
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= TOTAL_HEATFLUX
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT = 1.0
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART = YES
-%
-% Data written to history file
 HISTORY_OUTPUT=(ITER, RMS_RES, HEAT)
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= (cylinder_outer1, cylinder_outer2, cylinder_outer3)
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= (cylinder_outer1, cylinder_outer2, cylinder_outer3)
 
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
-% Density model within the incompressible flow solver.
-% Options are CONSTANT (default), BOUSSINESQ, or VARIABLE. If VARIABLE,
-% an appropriate fluid model must be selected.
 INC_DENSITY_MODEL= VARIABLE
-%
-% Solve the energy equation in the incompressible flow solver
 INC_ENERGY_EQUATION = YES
-%
-% Initial density for incompressible flows (1.2886 kg/m^3 by default)
 INC_DENSITY_INIT= 0.0210322
-%
-% Initial velocity for incompressible flows (1.0,0,0 m/s by default)
 INC_VELOCITY_INIT= ( 3.40297, 0.0, 0.0 )
-%
-% Initial temperature for incompressible flows that include the
-% energy equation (288.15 K by default). Value is ignored if
-% INC_ENERGY_EQUATION is false.
 INC_TEMPERATURE_INIT= 288.15
-%
-% Non-dimensionalization scheme for incompressible flows. Options are
-% INITIAL_VALUES (default), REFERENCE_VALUES, or DIMENSIONAL.
-% INC_*_REF values are ignored unless REFERENCE_VALUES is chosen.
 INC_NONDIM= DIMENSIONAL
 
 % ---- IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
-% Fluid model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS,
-%              CONSTANT_DENSITY, INC_IDEAL_GAS)
 FLUID_MODEL= INC_IDEAL_GAS
-%
-% Specific heat at constant pressure, Cp (1004.703 J/kg*K (air)).
-% Incompressible fluids with energy eqn. only (CONSTANT_DENSITY, INC_IDEAL_GAS).
 SPECIFIC_HEAT_CP= 1004.703
-%
-% Molecular weight for an incompressible ideal gas (28.96 g/mol (air) default)
-% Incompressible fluids with energy eqn. only (CONSTANT_DENSITY, INC_IDEAL_GAS).
 MOLECULAR_WEIGHT= 28.96
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.7893e-05
-%
-% Sutherland Viscosity Ref (1.716E-5 default value for AIR SI)
 MU_REF= 1.716E-5
-%
-% Sutherland Temperature Ref (273.15 K default value for AIR SI)
 MU_T_REF= 273.15
-%
-% Sutherland constant (110.4 default value for AIR SI)
 SUTHERLAND_CONSTANT= 110.4
 
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
-% Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL).
 CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
-%
-% Molecular Thermal Conductivity that would be constant (0.0257 by default)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.0257
-%
-% Laminar Prandtl number (0.72 (air), only for CONSTANT_PRANDTL)
 PRANDTL_LAM= 0.72
-%
-% Turbulent Prandtl number (0.9 (air), only for CONSTANT_PRANDTL)
 PRANDTL_TURB= 0.90
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER_JACOBI,
-%                                                      SMOOTHER_ILU, SMOOTHER_LUSGS,
-%                                                      SMOOTHER_LINELET)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= FDS
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -19
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 200
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-
diff --git a/TestCases/coupled_cht/incomp_2d_unsteady/solid_cylinder1.cfg b/TestCases/coupled_cht/incomp_2d_unsteady/solid_cylinder1.cfg
index 524001f3a88..a0d29c2fce9 100644
--- a/TestCases/coupled_cht/incomp_2d_unsteady/solid_cylinder1.cfg
+++ b/TestCases/coupled_cht/incomp_2d_unsteady/solid_cylinder1.cfg
@@ -7,82 +7,39 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= HEAT_EQUATION
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= TOTAL_HEATFLUX
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT = 1.0
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART = YES
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
 MARKER_ISOTHERMAL= ( core1, 350.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= (cylinder_inner1 )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( NONE )
 
 % ---------------- (SOLIDS) CONDUCTION CONDITION DEFINITION -------------------%
 %
 % We should keep the dimensionalization of the coupled flow solver
 INC_NONDIM= DIMENSIONAL
-%
-% Temperature initialization value
 FREESTREAM_TEMPERATURE= 288.15
 %
 % Nettis case: hollow cylinder (air w/ 4x the conductivity)
-%
-% Solid density (kg/m^3)
 MATERIAL_DENSITY= 0.0210322
-%
-% Solid specific heat (J/kg*K)
 SPECIFIC_HEAT_CP= 1004.703
-%
-% Solid thermal conductivity (W/m*K)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.1028
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER_JACOBI,
-%                                                      SMOOTHER_ILU, SMOOTHER_LUSGS,
-%                                                      SMOOTHER_LINELET)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
@@ -91,74 +48,31 @@ TIME_DISCRE_HEAT= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -19
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 200
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-
diff --git a/TestCases/coupled_cht/incomp_2d_unsteady/solid_cylinder2.cfg b/TestCases/coupled_cht/incomp_2d_unsteady/solid_cylinder2.cfg
index 09bb6a3d2d2..5aee001767d 100644
--- a/TestCases/coupled_cht/incomp_2d_unsteady/solid_cylinder2.cfg
+++ b/TestCases/coupled_cht/incomp_2d_unsteady/solid_cylinder2.cfg
@@ -7,159 +7,72 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= HEAT_EQUATION
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= TOTAL_HEATFLUX
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT = 1.0
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART = YES
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
 MARKER_ISOTHERMAL= ( core2, 350.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= (cylinder_inner2)
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( NONE )
 
 % ---------------- (SOLIDS) CONDUCTION CONDITION DEFINITION -------------------%
 %
 % We should keep the dimensionalization of the coupled flow solver
 INC_NONDIM= DIMENSIONAL
-%
-% Temperature initialization value
 FREESTREAM_TEMPERATURE= 288.15
 %
 % Nettis case: hollow cylinder (air w/ 4x the conductivity)
-%
-% Solid density (kg/m^3)
 MATERIAL_DENSITY= 0.0210322
-%
-% Solid specific heat (J/kg*K)
 SPECIFIC_HEAT_CP= 1004.703
-%
-% Solid thermal conductivity (W/m*K)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.1028
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER_JACOBI,
-%                                                      SMOOTHER_ILU, SMOOTHER_LUSGS,
-%                                                      SMOOTHER_LINELET)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Time discretization (EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_HEAT= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -19
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 200
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
-DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-
+DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
\ No newline at end of file
diff --git a/TestCases/coupled_cht/incomp_2d_unsteady/solid_cylinder3.cfg b/TestCases/coupled_cht/incomp_2d_unsteady/solid_cylinder3.cfg
index d0867a6c833..31dd8103509 100644
--- a/TestCases/coupled_cht/incomp_2d_unsteady/solid_cylinder3.cfg
+++ b/TestCases/coupled_cht/incomp_2d_unsteady/solid_cylinder3.cfg
@@ -7,159 +7,72 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= HEAT_EQUATION
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= TOTAL_HEATFLUX
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT = 1.0
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART = YES
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
 MARKER_ISOTHERMAL= ( core3, 350.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( cylinder_inner3 )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( NONE )
 
 % ---------------- (SOLIDS) CONDUCTION CONDITION DEFINITION -------------------%
 %
 % We should keep the dimensionalization of the coupled flow solver
 INC_NONDIM= DIMENSIONAL
-%
-% Temperature initialization value
 FREESTREAM_TEMPERATURE= 288.15
 %
 % Nettis case: hollow cylinder (air w/ 4x the conductivity)
-%
-% Solid density (kg/m^3)
 MATERIAL_DENSITY= 0.0210322
-%
-% Solid specific heat (J/kg*K)
 SPECIFIC_HEAT_CP= 1004.703
-%
-% Solid thermal conductivity (W/m*K)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.1028
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER_JACOBI,
-%                                                      SMOOTHER_ILU, SMOOTHER_LUSGS,
-%                                                      SMOOTHER_LINELET)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Time discretization (EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_HEAT= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -19
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 200
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
-DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-
+DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
\ No newline at end of file
diff --git a/TestCases/ddes/flatplate/ddes_flatplate.cfg b/TestCases/ddes/flatplate/ddes_flatplate.cfg
index 13878517e61..cfbf729eacf 100644
--- a/TestCases/ddes/flatplate/ddes_flatplate.cfg
+++ b/TestCases/ddes/flatplate/ddes_flatplate.cfg
@@ -5,226 +5,103 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.10                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= RANS
-%
-% If Navier-Stokes, kind of turbulent model (NONE, SA)
 KIND_TURB_MODEL= SA
 HYBRID_RANSLES= SA_EDDES
-%
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.2
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 5000000.0
-%
-% Reynolds length (in meters)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 2.0
 
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 
-% Enable time domain
 TIME_DOMAIN= YES
-%
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER, TIME_SPECTRAL)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
 %
-% Time Step for dual time stepping simulations (s)
 % U_inf = 69.4448 - dt*=0.02 - dt=0.000288
 TIME_STEP= 0.000288
-%
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 20.0
-%
-% Unsteady Courant-Friedrichs-Lewy number of the finest grid
 UNST_CFL_NUMBER= 0.0
-%
-% Number of internal iterations (dual time method)
 INNER_ITER= 20
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( wall, 0.0 )
-%
-% Inlet boundary marker(s) (NONE = no marker) 
-% Format: ( inlet marker, total temperature, total pressure, flow_direction_x, 
-%           flow_direction_y, flow_direction_z, ... )
 MARKER_INLET= ( inlet, 302.4, 118309.784, 1.0, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure, ... )
 MARKER_OUTLET= ( outlet, 115056.0, farfield, 115056.0 )
-%
-% Symmetry boundary marker(s) (NONE = no marker)
 MARKER_SYM= ( symmetry )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( wall )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( wall )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 TIME_ITER= 10
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Coefficient for the Venkat's limiter (upwind scheme). A larger values decrease
-%             the extent of limiting, values approaching zero cause
-%             lower-order approximation to the solution (0.05 by default)
 VENKAT_LIMITER_COEFF= 0.05
-%
+
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= SLAU2
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -15
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 0
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_flatplate_turb_137x97.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-%
-% Writing solution file frequency for physical time steps (dual time)
 OUTPUT_WRT_FREQ= 1000
-%
-% Screen output
 SCREEN_OUTPUT= (TIME_ITER, INNER_ITER, RMS_DENSITY, RMS_NU_TILDE, LIFT, DRAG, TOTAL_HEATFLUX)
diff --git a/TestCases/deformation/brick_hex/def_brick_hex.cfg b/TestCases/deformation/brick_hex/def_brick_hex.cfg
index 556da04b539..4864a6bcf25 100755
--- a/TestCases/deformation/brick_hex/def_brick_hex.cfg
+++ b/TestCases/deformation/brick_hex/def_brick_hex.cfg
@@ -5,245 +5,105 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2016.05.31                                                             %
-% File Version SU2 v4.1.3                                                      %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (POTENTIAL_FLOW, EULER, NAVIER_STOKES, 
-%                               MULTI_SPECIES_NAVIER_STOKES, TWO_PHASE_FLOW, 
-%                               COMBUSTION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED, ONE_SHOT_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation (m or in)
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 = no marker)
 MARKER_EULER= ( z_m )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( x_p, x_m, y_p, z_p, y_m )
-%
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( z_m )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( z_m )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
-NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 CFL_NUMBER= 4.0
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 5
-%
-% Linear solver for the implicit formulation (LU_SGS, SYM_GAUSS_SEIDEL, BCGSTAB)
 LINEAR_SOLVER= FGMRES
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % --------------------- FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                              ROE-2ND_ORDER, AUSM-1ST_ORDER, AUSM-2ND_ORDER,
-%                              HLLC-1ST_ORDER, HLLC-2ND_ORDER)
 CONV_NUM_METHOD_FLOW= JST
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING,
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC, NACA_4DIGITS, AIRFOIL)
 DV_KIND= FFD_CONTROL_POINT
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( z_m )
-%
-% Parameters of the shape deformation
-% - TRANSLATION ( x_Disp, y_Disp, z_Disp ), as a unit vector
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - SCALE ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - PARABOLIC ( Center, Thickness )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - AIRFOIL ( 1.0 )
 DV_PARAM= ( MAIN_BOX, 2, 2, 1, 0.0, 0.0, 1.0 )
-%
-% Value of the shape deformation
 DV_VALUE= 3.0
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, JACOBI)
 DEFORM_LINEAR_SOLVER_PREC= LU_SGS
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 1000
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Deformation coefficient (in theory from -1.0 to 0.5, a large value is also valid)
 DEFORM_COEFF = 1E6
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-15
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 1000
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (MAIN_BOX, 0.01, 0.01, -0.25, 1.99, 0.01, -0.25, 1.99, 0.99, -0.25, 0.01, 0.99, -0.25, 0.01, 0.01, 0.25, 1.99, 0.01, 0.25, 1.99, 0.99, 0.25, 0.01, 0.99, 0.25)
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= (4, 4, 1)
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= 1ST_DERIVATIVE
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= mesh_brick_hex_ffd.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= mesh_brick_hex_ffd.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
diff --git a/TestCases/deformation/brick_hex_rans/def_brick_hex_rans.cfg b/TestCases/deformation/brick_hex_rans/def_brick_hex_rans.cfg
index c792b4f6690..49720c93729 100755
--- a/TestCases/deformation/brick_hex_rans/def_brick_hex_rans.cfg
+++ b/TestCases/deformation/brick_hex_rans/def_brick_hex_rans.cfg
@@ -5,250 +5,106 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2016.05.31                                                             %
-% File Version SU2 v4.1.3                                                      %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (POTENTIAL_FLOW, EULER, NAVIER_STOKES, 
-%                               MULTI_SPECIES_NAVIER_STOKES, TWO_PHASE_FLOW, 
-%                               COMBUSTION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED, ONE_SHOT_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation (m or in)
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 = no marker)
 MARKER_EULER= ( z_m )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( x_p, x_m, y_p, z_p, y_m )
-%
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( z_m )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( z_m )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
-NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 CFL_NUMBER= 4.0
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 5
-%
-% Linear solver for the implicit formulation (LU_SGS, SYM_GAUSS_SEIDEL, BCGSTAB)
 LINEAR_SOLVER= FGMRES
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % --------------------- FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                              ROE-2ND_ORDER, AUSM-1ST_ORDER, AUSM-2ND_ORDER,
-%                              HLLC-1ST_ORDER, HLLC-2ND_ORDER)
 CONV_NUM_METHOD_FLOW= JST
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING,
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC, NACA_4DIGITS, AIRFOIL)
 DV_KIND= FFD_CONTROL_POINT
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( z_m )
-%
-% Parameters of the shape deformation
-% - TRANSLATION ( x_Disp, y_Disp, z_Disp ), as a unit vector
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - SCALE ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - PARABOLIC ( Center, Thickness )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - AIRFOIL ( 1.0 )
 DV_PARAM= ( MAIN_BOX, 2, 2, 1, 0.0, 0.0, 1.0 )
-%
-% Value of the shape deformation
 DV_VALUE= 3.0
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, JACOBI)
 DEFORM_LINEAR_SOLVER_PREC= LU_SGS
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 1000
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Deformation coefficient (in theory from -1.0 to 0.5, a large value is also valid)
 DEFORM_COEFF = 1E6
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-15
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 1000
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (MAIN_BOX, 0.01, 0.01, -0.25, 1.99, 0.01, -0.25, 1.99, 0.99, -0.25, 0.01, 0.99, -0.25, 0.01, 0.01, 0.25, 1.99, 0.01, 0.25, 1.99, 0.99, 0.25, 0.01, 0.99, 0.25)
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= (4, 4, 1)
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= 1ST_DERIVATIVE
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= mesh_brick_hex_rans_ffd.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= mesh_brick_hex_rans_ffd.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-
diff --git a/TestCases/deformation/brick_prism/def_brick_prism.cfg b/TestCases/deformation/brick_prism/def_brick_prism.cfg
index 08f17f6795a..2d50bb38399 100755
--- a/TestCases/deformation/brick_prism/def_brick_prism.cfg
+++ b/TestCases/deformation/brick_prism/def_brick_prism.cfg
@@ -5,246 +5,105 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2016.05.31                                                             %
-% File Version SU2 v4.1.3                                                      %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (POTENTIAL_FLOW, EULER, NAVIER_STOKES, 
-%                               MULTI_SPECIES_NAVIER_STOKES, TWO_PHASE_FLOW, 
-%                               COMBUSTION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED, ONE_SHOT_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation (m or in)
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 = no marker)
 MARKER_EULER= ( z_m )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( x_p, x_m, y_p, z_p, y_m )
-%
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( z_m )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( z_m )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
-NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 CFL_NUMBER= 4.0
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 5
-%
-% Linear solver for the implicit formulation (LU_SGS, SYM_GAUSS_SEIDEL, BCGSTAB)
 LINEAR_SOLVER= FGMRES
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % --------------------- FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                              ROE-2ND_ORDER, AUSM-1ST_ORDER, AUSM-2ND_ORDER,
-%                              HLLC-1ST_ORDER, HLLC-2ND_ORDER)
 CONV_NUM_METHOD_FLOW= JST
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING,
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC, NACA_4DIGITS, AIRFOIL)
 DV_KIND= FFD_CONTROL_POINT
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( z_m )
-%
-% Parameters of the shape deformation
-% - TRANSLATION ( x_Disp, y_Disp, z_Disp ), as a unit vector
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - SCALE ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - PARABOLIC ( Center, Thickness )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - AIRFOIL ( 1.0 )
 DV_PARAM= ( MAIN_BOX, 2, 2, 1, 0.0, 0.0, 1.0 )
-%
-% Value of the shape deformation
 DV_VALUE= 3.0
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, JACOBI)
 DEFORM_LINEAR_SOLVER_PREC= LU_SGS
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 1000
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Deformation coefficient (in theory from -1.0 to 0.5, a large value is also valid)
 DEFORM_COEFF = 1E6
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-15
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 1000
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (MAIN_BOX, 0.01, 0.01, -0.25, 1.99, 0.01, -0.25, 1.99, 0.99, -0.25, 0.01, 0.99, -0.25, 0.01, 0.01, 0.25, 1.99, 0.01, 0.25, 1.99, 0.99, 0.25, 0.01, 0.99, 0.25)
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= (4, 4, 1)
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= 1ST_DERIVATIVE
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= mesh_brick_prism_ffd.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= mesh_brick_prism_ffd.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-
diff --git a/TestCases/deformation/brick_prism_rans/def_brick_prism_rans.cfg b/TestCases/deformation/brick_prism_rans/def_brick_prism_rans.cfg
index ccdeb4b4812..f2707e4f519 100755
--- a/TestCases/deformation/brick_prism_rans/def_brick_prism_rans.cfg
+++ b/TestCases/deformation/brick_prism_rans/def_brick_prism_rans.cfg
@@ -5,246 +5,105 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2016.05.31                                                             %
-% File Version SU2 v4.1.3                                                      %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (POTENTIAL_FLOW, EULER, NAVIER_STOKES, 
-%                               MULTI_SPECIES_NAVIER_STOKES, TWO_PHASE_FLOW, 
-%                               COMBUSTION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED, ONE_SHOT_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation (m or in)
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 = no marker)
 MARKER_EULER= ( z_m )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( x_p, x_m, y_p, z_p, y_m )
-%
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( z_m )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( z_m )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
-NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 CFL_NUMBER= 4.0
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 5
-%
-% Linear solver for the implicit formulation (LU_SGS, SYM_GAUSS_SEIDEL, BCGSTAB)
 LINEAR_SOLVER= FGMRES
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % --------------------- FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                              ROE-2ND_ORDER, AUSM-1ST_ORDER, AUSM-2ND_ORDER,
-%                              HLLC-1ST_ORDER, HLLC-2ND_ORDER)
 CONV_NUM_METHOD_FLOW= JST
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING,
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC, NACA_4DIGITS, AIRFOIL)
 DV_KIND= FFD_CONTROL_POINT
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( z_m )
-%
-% Parameters of the shape deformation
-% - TRANSLATION ( x_Disp, y_Disp, z_Disp ), as a unit vector
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - SCALE ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - PARABOLIC ( Center, Thickness )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - AIRFOIL ( 1.0 )
 DV_PARAM= ( MAIN_BOX, 2, 2, 1, 0.0, 0.0, 1.0 )
-%
-% Value of the shape deformation
 DV_VALUE= 5.0
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, JACOBI)
 DEFORM_LINEAR_SOLVER_PREC= LU_SGS
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 1000
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Deformation coefficient (in theory from -1.0 to 0.5, a large value is also valid)
 DEFORM_COEFF = 1E6
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= WALL_DISTANCE
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-15
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 1000
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (MAIN_BOX, 0.01, 0.01, -0.25, 1.99, 0.01, -0.25, 1.99, 0.99, -0.25, 0.01, 0.99, -0.25, 0.01, 0.01, 0.25, 1.99, 0.01, 0.25, 1.99, 0.99, 0.25, 0.01, 0.99, 0.25)
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= (4, 4, 1)
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= 1ST_DERIVATIVE
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= mesh_brick_prism_rans_ffd.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= mesh_brick_prism_rans_ffd.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-
diff --git a/TestCases/deformation/brick_pyra/def_brick_pyra.cfg b/TestCases/deformation/brick_pyra/def_brick_pyra.cfg
index de18b89bf9d..82a1e35e3c9 100755
--- a/TestCases/deformation/brick_pyra/def_brick_pyra.cfg
+++ b/TestCases/deformation/brick_pyra/def_brick_pyra.cfg
@@ -5,249 +5,106 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2016.05.31                                                             %
-% File Version SU2 v4.1.3                                                      %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (POTENTIAL_FLOW, EULER, NAVIER_STOKES, 
-%                               MULTI_SPECIES_NAVIER_STOKES, TWO_PHASE_FLOW, 
-%                               COMBUSTION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED, ONE_SHOT_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation (m or in)
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 = no marker)
 MARKER_EULER= ( z_m )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( x_p, x_m, y_p, z_p, y_m )
-%
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( z_m )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( z_m )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
-NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 CFL_NUMBER= 4.0
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 5
-%
-% Linear solver for the implicit formulation (LU_SGS, SYM_GAUSS_SEIDEL, BCGSTAB)
 LINEAR_SOLVER= FGMRES
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % --------------------- FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                              ROE-2ND_ORDER, AUSM-1ST_ORDER, AUSM-2ND_ORDER,
-%                              HLLC-1ST_ORDER, HLLC-2ND_ORDER)
 CONV_NUM_METHOD_FLOW= JST
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING,
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC, NACA_4DIGITS, AIRFOIL)
 DV_KIND= FFD_CONTROL_POINT
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( z_m )
-%
-% Parameters of the shape deformation
-% - TRANSLATION ( x_Disp, y_Disp, z_Disp ), as a unit vector
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - SCALE ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - PARABOLIC ( Center, Thickness )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - AIRFOIL ( 1.0 )
 DV_PARAM= ( MAIN_BOX, 2, 2, 1, 0.0, 0.0, 1.0 )
-%
-% Value of the shape deformation
 DV_VALUE= 3.0
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, JACOBI)
 DEFORM_LINEAR_SOLVER_PREC= LU_SGS
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 1000
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Deformation coefficient (in theory from -1.0 to 0.5, a large value is also valid)
 DEFORM_COEFF = 1E6
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-15
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 1000
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (MAIN_BOX, 0.01, 0.01, -0.25, 1.99, 0.01, -0.25, 1.99, 0.99, -0.25, 0.01, 0.99, -0.25, 0.01, 0.01, 0.25, 1.99, 0.01, 0.25, 1.99, 0.99, 0.25, 0.01, 0.99, 0.25)
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= (4, 4, 1)
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= 1ST_DERIVATIVE
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= mesh_brick_pyra_ffd.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= mesh_brick_pyra_ffd.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-
diff --git a/TestCases/deformation/brick_tets/def_brick_tets.cfg b/TestCases/deformation/brick_tets/def_brick_tets.cfg
index 6bf27364f2f..e0b62d50675 100755
--- a/TestCases/deformation/brick_tets/def_brick_tets.cfg
+++ b/TestCases/deformation/brick_tets/def_brick_tets.cfg
@@ -5,249 +5,106 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2016.05.31                                                             %
-% File Version SU2 v4.1.3                                                      %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (POTENTIAL_FLOW, EULER, NAVIER_STOKES, 
-%                               MULTI_SPECIES_NAVIER_STOKES, TWO_PHASE_FLOW, 
-%                               COMBUSTION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED, ONE_SHOT_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation (m or in)
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 = no marker)
 MARKER_EULER= ( z_m )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( x_p, x_m, y_p, z_p, y_m )
-%
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( z_m )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( z_m )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
-NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 CFL_NUMBER= 4.0
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 5
-%
-% Linear solver for the implicit formulation (LU_SGS, SYM_GAUSS_SEIDEL, BCGSTAB)
 LINEAR_SOLVER= FGMRES
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % --------------------- FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                              ROE-2ND_ORDER, AUSM-1ST_ORDER, AUSM-2ND_ORDER,
-%                              HLLC-1ST_ORDER, HLLC-2ND_ORDER)
 CONV_NUM_METHOD_FLOW= JST
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING,
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC, NACA_4DIGITS, AIRFOIL)
 DV_KIND= FFD_CONTROL_POINT
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( z_m )
-%
-% Parameters of the shape deformation
-% - TRANSLATION ( x_Disp, y_Disp, z_Disp ), as a unit vector
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - SCALE ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - PARABOLIC ( Center, Thickness )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - AIRFOIL ( 1.0 )
 DV_PARAM= ( MAIN_BOX, 2, 2, 1, 0.0, 0.0, 1.0 )
-%
-% Value of the shape deformation
 DV_VALUE= 5.0
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, JACOBI)
 DEFORM_LINEAR_SOLVER_PREC= LU_SGS
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 1000
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Deformation coefficient (in theory from -1.0 to 0.5, a large value is also valid)
 DEFORM_COEFF = 1E6
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-15
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 1000
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (MAIN_BOX, 0.01, 0.01, -0.25, 1.99, 0.01, -0.25, 1.99, 0.99, -0.25, 0.01, 0.99, -0.25, 0.01, 0.01, 0.25, 1.99, 0.01, 0.25, 1.99, 0.99, 0.25, 0.01, 0.99, 0.25)
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= (4, 4, 1)
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= 1ST_DERIVATIVE
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= mesh_brick_tets_ffd.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= mesh_brick_tets_ffd.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-
diff --git a/TestCases/deformation/cylindrical_ffd/def_cylindrical.cfg b/TestCases/deformation/cylindrical_ffd/def_cylindrical.cfg
index 4723fcfb33b..6a9f1e04da3 100644
--- a/TestCases/deformation/cylindrical_ffd/def_cylindrical.cfg
+++ b/TestCases/deformation/cylindrical_ffd/def_cylindrical.cfg
@@ -5,295 +5,121 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)
 SOLVER= EULER 
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% System of measurements (SI, US)
-% International system of units (SI): ( meters, kilograms, Kelvins,
-%                                       Newtons = kg m/s^2, Pascals = N/m^2, 
-%                                       Density = kg/m^3, Speed = m/s,
-%                                       Equiv. Area = m^2 )
-% United States customary units (US): ( inches, slug, Rankines, lbf = slug ft/s^2, 
-%                                       psf = lbf/ft^2, Density = slug/ft^3, 
-%                                       Speed = ft/s, Equiv. Area = ft^2 )
 SYSTEM_MEASUREMENTS= US
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Side-slip angle (degrees, only for compressible flows)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream temperature (518.67 R by default)
 FREESTREAM_TEMPERATURE= 518.67
-%
-% Free-stream pressure (101325.0 N/m^2, 2116.216 psf by default)
 FREESTREAM_PRESSURE= 2116.216 
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation (in)
 REF_ORIGIN_MOMENT_X = 0.0
 REF_ORIGIN_MOMENT_Y = 0.0
 REF_ORIGIN_MOMENT_Z = 0.0
-%
-% Reference length for pitching, rolling, and yawing non-dimensional
-% moment (in)
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic
-% calculation) (in^2)
 REF_AREA= 0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= DIMENSIONAL
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( CYLINDER )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( FARFIELD )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( CYLINDER )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( CYLINDER )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( CYLINDER )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS 
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.0, 1.0, 1.0, 10.0 )
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, AVG_TOTAL_PRESSURE, 
-%                                             MASS_FLOW_RATE)
 OBJECTIVE_FUNCTION= DRAG
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Sensitivity for detecting sharp edges (< 3 high sensitivity).
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Venkatakrishnan's limiter coefficient (from 0.3 to 0.003)
 VENKAT_LIMITER_COEFF= 0.003
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-12
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH_JESPERSEN)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING,
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS
-%                      FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, FFD_ROTATION,
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC, NACA_4DIGITS, AIRFOIL)
 DV_KIND= FFD_CONTROL_POINT 
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( CYLINDER )
-%
-% Parameters of the shape deformation
-% - TRANSLATION ( x_Disp, y_Disp, z_Disp )
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - SCALE ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_DIHEDRAL_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - PARABOLIC ( Center, Thickness )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - AIRFOIL ( 1.0 )
 DV_PARAM= ( CYLINDER_BOX, 0, 3, 2, 1.0, 0.0, 0.0 )
-%
-% Value of the shape deformation
 DV_VALUE= 1.0 
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 100
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-10
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 1000
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (CYLINDER_BOX, -0.6, -0.1, 1.5, -0.6, -0.1, 0.5, -0.6, 0.1, 0.5, -0.6, 0.1, 1.5, 0.6, -0.1, 1.5, 0.6, -0.1, 0.5, 0.6, 0.1, 0.5, 0.6, 0.1, 1.5)
-%
-% FFD box degree: 3D case (r_degree, theta_degree, phi_degree)
 FFD_DEGREE= (1, 9, 4)
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= 1ST_DERIVATIVE
-%
-% FFD coordinate system (CARTESIAN, CYLINDRICAL, SPHERICAL)
 FFD_COORD_SYSTEM= CYLINDRICAL
-%
-% Axis for the FFD box (cylindrical and spherical coordinates)
 FFD_AXIS= (0.0, 0.0, 0.0)
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Number of total iterations
 ITER= 5
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= cylindrical.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency for physical time steps (dual time)
 OUTPUT_WRT_FREQ= 1
-%
-%
diff --git a/TestCases/deformation/intersection_prevention/def_intersect.cfg b/TestCases/deformation/intersection_prevention/def_intersect.cfg
index 0501383900a..39375b4b679 100644
--- a/TestCases/deformation/intersection_prevention/def_intersect.cfg
+++ b/TestCases/deformation/intersection_prevention/def_intersect.cfg
@@ -15,353 +15,150 @@
 % Institution:                                                                 %
 %   Technische Universiteit Eindhoven                                          %
 % Date: 2021.01.08                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER = INC_NAVIER_STOKES
-
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= NONE
-
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT)
 MATH_PROBLEM= DIRECT
-
-% Restart solution (NO, YES)
 RESTART_SOL = NO
-
 AXISYMMETRIC = NO
 
-%
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
-% Density model within the incompressible flow solver.
-% Options are CONSTANT (default), BOUSSINESQ, or VARIABLE. If VARIABLE,
-% an appropriate fluid model must be selected.
-
 INC_DENSITY_MODEL= CONSTANT
-
-% Solve the energy equation in the incompressible flow solver
 INC_ENERGY_EQUATION = NO
-
-% Initial density for incompressible flows
-% (1.2886 kg/m^3 by default (air), 998.2 Kg/m^3 (water))
 INC_DENSITY_INIT= 1.1728
-
-% Initial velocity for incompressible flows (1.0,0,0 m/s by default)
 INC_VELOCITY_INIT= (1.0, 0.0, 0.0 )
-
-% Initial temperature for incompressible flows that include the 
-% energy equation (288.15 K by default). Value is ignored if 
-% INC_ENERGY_EQUATION is false.
 INC_TEMPERATURE_INIT= 300.0
-
-% List of inlet types for incompressible flows. List length must
-% match number of inlet markers. Options: VELOCITY_INLET, PRESSURE_INLET.
 INC_INLET_TYPE= VELOCITY_INLET
-%
-% Damping coefficient for iterative updates at pressure inlets. (0.1 by default)
 INC_INLET_DAMPING= 0.1
-
-% List of outlet types for incompressible flows. List length must
-% match number of outlet markers. Options: PRESSURE_OUTLET, MASS_FLOW_OUTLET
 INC_OUTLET_TYPE= PRESSURE_OUTLET
-%
-% Damping coefficient for iterative updates at mass flow outlets. (0.1 by default)
 INC_OUTLET_DAMPING= 0.1
-
-% Non-dimensionalization scheme for incompressible flows. Options are
-% INITIAL_VALUES (default), REFERENCE_VALUES, or DIMENSIONAL.
-% INC_*_REF values are ignored unless REFERENCE_VALUES is chosen.
 INC_NONDIM= DIMENSIONAL
 
-
 % ---- IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
-% Fluid model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS, 
-%              CONSTANT_DENSITY, INC_IDEAL_GAS)
 FLUID_MODEL= CONSTANT_DENSITY
-%
-% Specific heat at constant pressure, Cp (1004.703 J/kg*K (air)).
-% Incompressible fluids with energy eqn. only (CONSTANT_DENSITY, INC_IDEAL_GAS).
 SPECIFIC_HEAT_CP= 1004.703
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.83463e-05
 
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
-% Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL).
 CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
-%
-% Laminar Prandtl number (0.72 (air), only for CONSTANT_PRANDTL)
 PRANDTL_LAM= 0.72
-%
-% Turbulent Prandtl number (0.9 (air), only for CONSTANT_PRANDTL)
 PRANDTL_TURB= 0.90
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
-
-% Reference origin for moment computation
+%
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 0.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
-
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
-
+%
 MARKER_PLOTTING = (outlet)
 MARKER_ANALYZE = (outlet)
-
 MARKER_HEATFLUX= (wall_inner_bottom, 0.0, wall_inner_right, 0.0, wall_inner_top, 0.0)
-
 SPECIFIED_INLET_PROFILE= NO
-
 INLET_FILENAME = inletVelocity.dat
-
 INLET_MATCHING_TOLERANCE= 1e-5
-
-% Inlet boundary marker(s)
 MARKER_INLET = (inlet, 300.0, 1.0, 1.0, 0.0, 0.0)
-
-% Outler boundary marker (s)
 MARKER_OUTLET = (outlet, 0.0)
-
-% Symmetry boundary marker
 MARKER_SYM = (wall_outer)
-
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= (outlet)
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
-
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
+%
 NUM_METHOD_GRAD= GREEN_GAUSS
-
-% Courant-Friedrichs-Lewy condition of the finest grid
-
 CFL_NUMBER=100
-
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-
-
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-
-% Number of total iterations
-%EXT_ITER = 25
 ITER = 10000
-
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 50
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
-
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
+%
 LINEAR_SOLVER= FGMRES
-
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= ILU
-
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-10
-
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 100
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.8
-
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.8
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
-
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
+%
 CONV_NUM_METHOD_FLOW= FDS
-
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= NO
-
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= NONE
-
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 10.0
-
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.05, 0.02 )
-
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
-
 CONV_NUM_METHOD_ADJFLOW= FDS
 ADJ_JST_SENSOR_COEFF= ( 0.05, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-
-% Min value of the residual (log10 of the residual)
+%
 CONV_RESIDUAL_MINVAL= -10
-
-% Start convergence criteria at iteration number
 CONV_STARTITER= 100
-
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 20
-
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-
-% Function to apply the criteria (LIFT, DRAG, NEARFIELD_PRESS, SENS_GEOMETRY, 
-% 	      	    		 SENS_MACH, DELTA_LIFT, DELTA_DRAG)
-
 SCREEN_OUTPUT = INNER_ITER WALL_TIME RMS_PRESSURE RMS_VELOCITY-X RMS_ADJ_PRESSURE RMS_ADJ_VELOCITY-X U
 CONV_FIELD = (RMS_PRESSURE, RMS_ADJ_PRESSURE)
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+%
 MESH_FORMAT= SU2
-
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 OUTPUT_FILES = (RESTART, PARAVIEW_ASCII, SURFACE_CSV) 
-%
 TABULAR_FORMAT = CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-
 VOLUME_OUTPUT= RESIDUAL PRIMITIVE SOURCE SENSITIVITY COEFFICIENT
-
-% Writing convergence history frequency
 SCREEN_WRT_FREQ_INNER = 1
 SCREEN_WRT_FREQ_OUTER = 1
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (NO_DEFORMATION, TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING, FFD_NACELLE
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS, FFD_TWIST
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D, FFD_TWIST_2D,
-%                      HICKS_HENNE, SURFACE_BUMP)
-
 DV_KIND= FFD_CONTROL_POINT_2D, FFD_CONTROL_POINT_2D, FFD_CONTROL_POINT_2D, FFD_CONTROL_POINT_2D, FFD_CONTROL_POINT_2D, FFD_CONTROL_POINT_2D, FFD_CONTROL_POINT_2D, FFD_CONTROL_POINT_2D, FFD_CONTROL_POINT_2D, FFD_CONTROL_POINT_2D, FFD_CONTROL_POINT_2D, FFD_CONTROL_POINT_2D, FFD_CONTROL_POINT_2D, FFD_CONTROL_POINT_2D, FFD_CONTROL_POINT_2D, FFD_CONTROL_POINT_2D, FFD_CONTROL_POINT_2D, FFD_CONTROL_POINT_2D, FFD_CONTROL_POINT_2D, FFD_CONTROL_POINT_2D, FFD_CONTROL_POINT_2D, FFD_CONTROL_POINT_2D 
-
 MESH_FILENAME = mesh_ffd.su2
-
-% Mesh output file
 MESH_OUT_FILENAME= mesh_ffd_deformed.su2
-
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= (wall_inner_bottom, wall_inner_right, wall_inner_top)
-
-% Parameters of the shape deformation
 DV_PARAM= (MAIN_BOX, 0, 0, 0.0, 1.0); (MAIN_BOX, 1, 0, 0.0, 1.0); (MAIN_BOX, 2, 0, 0.0, 1.0); (MAIN_BOX, 3, 0, 0.0, 1.0); (MAIN_BOX, 4, 0, 0.0, 1.0); (MAIN_BOX, 5, 0, 0.0, 1.0); (MAIN_BOX, 6, 0, 0.0, 1.0); (MAIN_BOX, 7, 0, 0.0, 1.0); (MAIN_BOX, 8, 0, 0.0, 1.0); (MAIN_BOX, 9, 0, 0.0, 1.0); (MAIN_BOX, 10, 0, 0.0, 1.0); (MAIN_BOX, 0, 1, 0.0, 1.0); (MAIN_BOX, 1, 1, 0.0, 1.0); (MAIN_BOX, 2, 1, 0.0, 1.0); (MAIN_BOX, 3, 1, 0.0, 1.0); (MAIN_BOX, 4, 1, 0.0, 1.0); (MAIN_BOX, 5, 1, 0.0, 1.0); (MAIN_BOX, 6, 1, 0.0, 1.0); (MAIN_BOX, 7, 1, 0.0, 1.0); (MAIN_BOX, 8, 1, 0.0, 1.0); (MAIN_BOX, 9, 1, 0.0, 1.0); (MAIN_BOX, 10, 1, 0.0, 1.0) 
-
-% Value of the shape deformation
 DV_VALUE = 0, 0.0002, 0.0004, 0.0006, 0.0008, 0.001, 0.0012, 0.0014, 0.0016, 0.0018, 0.002, 0,-0.0002, -0.0004, -0.0006, -0.0008, -0.0010, -0.0012, -0.0014, -0.0016, -0.0018, -0.002
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 1000
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Factor to multiply smallest cell volume for deform tolerance (0.001 default)
-% DEFORM_TOL_FACTOR = 1e-10
 DEFORM_LINEAR_SOLVER_ERROR = 1e-5
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= WALL_DISTANCE
-%
-
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-10
-
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 500
 
 % ----- CHECK AND REPAIR MESH INTERSECTION ------------------------- %
+%
 % Parameters to check and repair self-intersections within FFD box 
 % (after deformation)
 %
@@ -373,6 +170,7 @@ FFD_INTPREV_ITER = 2
 FFD_INTPREV_DEPTH= 3
 
 % ----- CHECK AND REPAIR NONCONVEX CELLS  ------------------------- %
+%
 % Parameters to check and repair nonconvex elements in mesh 
 % (after deformation)
 %
@@ -384,59 +182,17 @@ CONVEXITY_CHECK_ITER = 10
 CONVEXITY_CHECK_DEPTH = 3
 % -------------------------------------------------------------------------- %
 
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (MAIN_BOX, 0.02, 0.005, 0,   0.05, 0.005, 0.0,   0.05, 0.007, 0.0,   0.02, 0.007, 0.0,   0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
-
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= ( 10, 1, 0)
-
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= USER_INPUT
-
-%
-% Optimization objective function with scaling factor, separated by semicolons.
-% To include quadratic penalty function: use OPT_CONSTRAINT option syntax within the OPT_OBJECTIVE list.
-% ex= Objective * Scale
-%OPT_OBJECTIVE= TOTAL_HEATFLUX * 1e-5
 OPT_OBJECTIVE= DRAG*5.0e-3
-
-%
-% Optimization constraint functions with pushing factors (affects its value, not the gradient  in the python scripts), separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= NONE
-
-%
-% Factor to reduce the norm of the gradient (affects the objective function and gradient in the python scripts)
-% In general, a norm of the gradient ~1E-6 is desired.
 OPT_GRADIENT_FACTOR= 1.0
-%
-% Factor to relax or accelerate the optimizer convergence (affects the line search in SU2_DEF)
-% In general, surface deformations of 0.01'' or 0.0001m are desirable
 OPT_RELAX_FACTOR= 1.0
-%
-% Maximum number of iterations
 OPT_ITERATIONS= 20
-%
-% Requested accuracy
 OPT_ACCURACY= 1E-200
-
-% Optimization bound (bounds the line search in SU2_DEF)
 OPT_LINE_SEARCH_BOUND= 1E6
-%
-% Upper bound for each design variable (bound in the python optimizer)
 OPT_BOUND_UPPER =  1e10
 OPT_BOUND_LOWER = -1e10
-
-%
-% Finite difference step size for python scripts (0.001 default, recommended
-%                                                                                                 0.001 x REF_LENGTH)
 FIN_DIFF_STEP = 1e-3
-%
 DEFINITION_DV= (19, 1.0 | wall_inner_bottom, wall_inner_right, wall_inner_top | MAIN_BOX, 0, 0, 0.0, 1.0); (19, 1.0 | wall_inner_bottom, wall_inner_right, wall_inner_top | MAIN_BOX, 1, 0, 0.0, 1.0); (19, 1.0 | wall_inner_bottom, wall_inner_right, wall_inner_top | MAIN_BOX, 2, 0, 0.0, 1.0); (19, 1.0 | wall_inner_bottom, wall_inner_right, wall_inner_top | MAIN_BOX, 3, 0, 0.0, 1.0); (19, 1.0 | wall_inner_bottom, wall_inner_right, wall_inner_top | MAIN_BOX, 4, 0, 0.0, 1.0); (19, 1.0 | wall_inner_bottom, wall_inner_right, wall_inner_top | MAIN_BOX, 5, 0, 0.0, 1.0); (19, 1.0 | wall_inner_bottom, wall_inner_right, wall_inner_top | MAIN_BOX, 6, 0, 0.0, 1.0); (19, 1.0 | wall_inner_bottom, wall_inner_right, wall_inner_top | MAIN_BOX, 7, 0, 0.0, 1.0); (19, 1.0 | wall_inner_bottom, wall_inner_right, wall_inner_top | MAIN_BOX, 8, 0, 0.0, 1.0); (19, 1.0 | wall_inner_bottom, wall_inner_right, wall_inner_top | MAIN_BOX, 9, 0, 0.0, 1.0); (19, 1.0 | wall_inner_bottom, wall_inner_right, wall_inner_top | MAIN_BOX, 10, 0, 0.0, 1.0); (19, 1.0 | wall_inner_bottom, wall_inner_right, wall_inner_top | MAIN_BOX, 0, 1, 0.0, 1.0); (19, 1.0 | wall_inner_bottom, wall_inner_right, wall_inner_top | MAIN_BOX, 1, 1, 0.0, 1.0); (19, 1.0 | wall_inner_bottom, wall_inner_right, wall_inner_top | MAIN_BOX, 2, 1, 0.0, 1.0); (19, 1.0 | wall_inner_bottom, wall_inner_right, wall_inner_top | MAIN_BOX, 3, 1, 0.0, 1.0); (19, 1.0 | wall_inner_bottom, wall_inner_right, wall_inner_top | MAIN_BOX, 4, 1, 0.0, 1.0); (19, 1.0 | wall_inner_bottom, wall_inner_right, wall_inner_top | MAIN_BOX, 5, 1, 0.0, 1.0); (19, 1.0 | wall_inner_bottom, wall_inner_right, wall_inner_top | MAIN_BOX, 6, 1, 0.0, 1.0); (19, 1.0 | wall_inner_bottom, wall_inner_right, wall_inner_top | MAIN_BOX, 7, 1, 0.0, 1.0); (19, 1.0 | wall_inner_bottom, wall_inner_right, wall_inner_top | MAIN_BOX, 8, 1, 0.0, 1.0); (19, 1.0 | wall_inner_bottom, wall_inner_right, wall_inner_top | MAIN_BOX, 9, 1, 0.0, 1.0); (19, 1.0 | wall_inner_bottom, wall_inner_right, wall_inner_top | MAIN_BOX, 10, 1, 0.0, 1.0) 
diff --git a/TestCases/deformation/naca0012/def_NACA0012.cfg b/TestCases/deformation/naca0012/def_NACA0012.cfg
index 2b0032c28d0..d6e316a1d29 100644
--- a/TestCases/deformation/naca0012/def_NACA0012.cfg
+++ b/TestCases/deformation/naca0012/def_NACA0012.cfg
@@ -5,345 +5,134 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AOA= 1.25
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= DIMENSIONAL
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (NONE = no marker)
 MARKER_FAR= ( farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( airfoil )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( airfoil )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 4.0
-%
-% Number of total iterations
 ITER= 250
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 1.0
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 1.0
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.5
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (FFD_SETTING, FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC,
-%                      NACA_4DIGITS, DISPLACEMENT, ROTATION, FFD_CONTROL_POINT, 
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CAMBER, FFD_THICKNESS, SURFACE_FILE, AIRFOIL)
 DV_KIND= HICKS_HENNE 
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation
-% - FFD_CONTROL_POINT_2D ( FFD_Box_ID, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_Box_ID, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_Box_ID, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - FOURIER ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), index, cos(0)/sin(1) )
-% - SPHERICAL ( ControlPoint_Index, Theta_Disp, R_Disp )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - PARABOLIC ( Center, Thickness )
-% - DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - OBSTACLE ( Center, Bump size )
 DV_PARAM= ( 1, 0.5 )
-%
-% Value of the shape deformation
 DV_VALUE= 0.1
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, JACOBI)
 DEFORM_LINEAR_SOLVER_PREC= LU_SGS
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 1000
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Deformation coefficient (in theory from -1.0 to 0.5, a large value is also valid)
 DEFORM_COEFF = 1E6
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= mesh_NACA0012_inv.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= mesh_NACA0012_inv.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.001
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= ( LIFT > 0.328188 ) * 0.001; ( MOMENT_Z > 0.034068 ) * 0.001; ( AIRFOIL_THICKNESS > 0.11 ) * 0.001
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 ); ( 30, 1.0 | airfoil | 0, 0.20 ); ( 30, 1.0 | airfoil | 0, 0.25 ); ( 30, 1.0 | airfoil | 0, 0.30 ); ( 30, 1.0 | airfoil | 0, 0.35 ); ( 30, 1.0 | airfoil | 0, 0.40 ); ( 30, 1.0 | airfoil | 0, 0.45 ); ( 30, 1.0 | airfoil | 0, 0.50 ); ( 30, 1.0 | airfoil | 0, 0.55 ); ( 30, 1.0 | airfoil | 0, 0.60 ); ( 30, 1.0 | airfoil | 0, 0.65 ); ( 30, 1.0 | airfoil | 0, 0.70 ); ( 30, 1.0 | airfoil | 0, 0.75 ); ( 30, 1.0 | airfoil | 0, 0.80 ); ( 30, 1.0 | airfoil | 0, 0.85 ); ( 30, 1.0 | airfoil | 0, 0.90 ); ( 30, 1.0 | airfoil | 0, 0.95 ); ( 30, 1.0 | airfoil | 1, 0.05 ); ( 30, 1.0 | airfoil | 1, 0.10 ); ( 30, 1.0 | airfoil | 1, 0.15 ); ( 30, 1.0 | airfoil | 1, 0.20 ); ( 30, 1.0 | airfoil | 1, 0.25 ); ( 30, 1.0 | airfoil | 1, 0.30 ); ( 30, 1.0 | airfoil | 1, 0.35 ); ( 30, 1.0 | airfoil | 1, 0.40 ); ( 30, 1.0 | airfoil | 1, 0.45 ); ( 30, 1.0 | airfoil | 1, 0.50 ); ( 30, 1.0 | airfoil | 1, 0.55 ); ( 30, 1.0 | airfoil | 1, 0.60 ); ( 30, 1.0 | airfoil | 1, 0.65 ); ( 30, 1.0 | airfoil | 1, 0.70 ); ( 30, 1.0 | airfoil | 1, 0.75 ); ( 30, 1.0 | airfoil | 1, 0.80 ); ( 30, 1.0 | airfoil | 1, 0.85 ); ( 30, 1.0 | airfoil | 1, 0.90 ); ( 30, 1.0 | airfoil | 1, 0.95 )
diff --git a/TestCases/deformation/naca0012/surface_file_NACA0012.cfg b/TestCases/deformation/naca0012/surface_file_NACA0012.cfg
index 599a2bd90a6..7ebeb30173c 100644
--- a/TestCases/deformation/naca0012/surface_file_NACA0012.cfg
+++ b/TestCases/deformation/naca0012/surface_file_NACA0012.cfg
@@ -5,353 +5,134 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AOA= 1.25
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= DIMENSIONAL
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (NONE = no marker)
 MARKER_FAR= ( farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( airfoil )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( airfoil )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 4.0
-%
-% Number of total iterations
 ITER= 250
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 1.0
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 1.0
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.5
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (FFD_SETTING, FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC,
-%                      NACA_4DIGITS, DISPLACEMENT, ROTATION, FFD_CONTROL_POINT, 
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CAMBER, FFD_THICKNESS, SURFACE_FILE, AIRFOIL)
 DV_KIND= SURFACE_FILE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation
-% - FFD_CONTROL_POINT_2D ( FFD_Box_ID, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_Box_ID, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_Box_ID, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - FOURIER ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), index, cos(0)/sin(1) )
-% - SPHERICAL ( ControlPoint_Index, Theta_Disp, R_Disp )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - PARABOLIC ( Center, Thickness )
-% - DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - OBSTACLE ( Center, Bump size )
 DV_PARAM= ( 1, 0.5 )
-%
-% Value of the shape deformation
 DV_VALUE= 0.1
-%
-% Filename for surface deformation from external parameterization. List moving
-% markers in DV_MARKER and provide ASCII file with format:
-% GlobalID_0, x_0, y_0, z_0
-% GlobalID_1, x_1, y_1, z_1
-%   ...
-% GlobalID_N, x_N, y_N, z_N
-% where N is the total number of vertices on all moving markers, and x/y/z are
-% the new position of each vertex. Points can be in any order.
 DV_FILENAME= surface_bump.dat
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, JACOBI)
 DEFORM_LINEAR_SOLVER_PREC= LU_SGS
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 1000
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Deformation coefficient (in theory from -1.0 to 0.5, a large value is also valid)
 DEFORM_COEFF = 1E6
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= mesh_NACA0012_inv.su2
-%MESH_FILENAME= mesh_def.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= mesh_NACA0012_inv.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.001
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= ( LIFT > 0.328188 ) * 0.001; ( MOMENT_Z > 0.034068 ) * 0.001; ( AIRFOIL_THICKNESS > 0.11 ) * 0.001
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 ); ( 30, 1.0 | airfoil | 0, 0.20 ); ( 30, 1.0 | airfoil | 0, 0.25 ); ( 30, 1.0 | airfoil | 0, 0.30 ); ( 30, 1.0 | airfoil | 0, 0.35 ); ( 30, 1.0 | airfoil | 0, 0.40 ); ( 30, 1.0 | airfoil | 0, 0.45 ); ( 30, 1.0 | airfoil | 0, 0.50 ); ( 30, 1.0 | airfoil | 0, 0.55 ); ( 30, 1.0 | airfoil | 0, 0.60 ); ( 30, 1.0 | airfoil | 0, 0.65 ); ( 30, 1.0 | airfoil | 0, 0.70 ); ( 30, 1.0 | airfoil | 0, 0.75 ); ( 30, 1.0 | airfoil | 0, 0.80 ); ( 30, 1.0 | airfoil | 0, 0.85 ); ( 30, 1.0 | airfoil | 0, 0.90 ); ( 30, 1.0 | airfoil | 0, 0.95 ); ( 30, 1.0 | airfoil | 1, 0.05 ); ( 30, 1.0 | airfoil | 1, 0.10 ); ( 30, 1.0 | airfoil | 1, 0.15 ); ( 30, 1.0 | airfoil | 1, 0.20 ); ( 30, 1.0 | airfoil | 1, 0.25 ); ( 30, 1.0 | airfoil | 1, 0.30 ); ( 30, 1.0 | airfoil | 1, 0.35 ); ( 30, 1.0 | airfoil | 1, 0.40 ); ( 30, 1.0 | airfoil | 1, 0.45 ); ( 30, 1.0 | airfoil | 1, 0.50 ); ( 30, 1.0 | airfoil | 1, 0.55 ); ( 30, 1.0 | airfoil | 1, 0.60 ); ( 30, 1.0 | airfoil | 1, 0.65 ); ( 30, 1.0 | airfoil | 1, 0.70 ); ( 30, 1.0 | airfoil | 1, 0.75 ); ( 30, 1.0 | airfoil | 1, 0.80 ); ( 30, 1.0 | airfoil | 1, 0.85 ); ( 30, 1.0 | airfoil | 1, 0.90 ); ( 30, 1.0 | airfoil | 1, 0.95 )
diff --git a/TestCases/deformation/naca4412/def_NACA4412.cfg b/TestCases/deformation/naca4412/def_NACA4412.cfg
index dfd8d82cbe3..e1905e3f3ff 100644
--- a/TestCases/deformation/naca4412/def_NACA4412.cfg
+++ b/TestCases/deformation/naca4412/def_NACA4412.cfg
@@ -6,328 +6,128 @@
 % Author: Thomas D. Economon	                                               %
 % Institution: Stanford University                                             %
 % Date: 2016.05.06                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)                             
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.09
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 13.87
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 297.778
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 1520000.0
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_VEL_EQ_ONE
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( pressure, 0.0,  suction, 0.0,  TE, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( pressure, suction, TE )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( pressure, suction, TE )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 15.0
-%
-% Max Delta time
 MAX_DELTA_TIME= 1E10
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 10.0, 1000.0 )
-%
-% Number of total iterations
 ITER= 99999
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE, 
-%                                             SURFACE_MASSFLOW)
 OBJECTIVE_FUNCTION= DRAG
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-10
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3)
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.9
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.9
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Relaxation coefficient
 RELAXATION_FACTOR_ADJOINT= 1.0
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.15
-%
-% Limit value for the adjoint variable
 LIMIT_ADJFLOW= 1E6
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E0
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA4412_turb.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1000
-%
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (FFD_SETTING, FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC,
-%                      NACA_4DIGITS, DISPLACEMENT, ROTATION, FFD_CONTROL_POINT,
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CAMBER, FFD_THICKNESS, SURFACE_FILE, AIRFOIL)
 DV_KIND= HICKS_HENNE 
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( pressure, suction, TE )
-%
-% Parameters of the shape deformation
-% - FFD_CONTROL_POINT_2D ( FFD_Box_ID, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_Box_ID, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_Box_ID, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - FOURIER ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), index, cos(0)/sin(1) )
-% - SPHERICAL ( ControlPoint_Index, Theta_Disp, R_Disp )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - PARABOLIC ( Center, Thickness )
-% - DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - OBSTACLE ( Center, Bump size )
 DV_PARAM= ( 1, 0.5 )
-%
-% Value of the shape deformation
 DV_VALUE= 0.1
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 1000
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Deformation coefficient (in theory from -1.0 to 0.5, a large value is also valid)
 DEFORM_COEFF = 1E6
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= WALL_DISTANCE
-
diff --git a/TestCases/deformation/rae2822/def_RAE2822.cfg b/TestCases/deformation/rae2822/def_RAE2822.cfg
index ea6d14c847b..e71b485970c 100644
--- a/TestCases/deformation/rae2822/def_RAE2822.cfg
+++ b/TestCases/deformation/rae2822/def_RAE2822.cfg
@@ -5,282 +5,117 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                        
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.729
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 2.31
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.5E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_VEL_EQ_ONE
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( AIRFOIL, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( FARFIELD )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( AIRFOIL )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( AIRFOIL )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 ITER= 99999
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-5
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.95
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.95
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE, TOTAL_HEAT,
-%                                     MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                     INVERSE_DESIGN_HEATFLUX)
-OBJECTIVE_FUNCTION= DRAG
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
+OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.01 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.5
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Adjoint frozen viscosity (NO, YES)
 FROZEN_VISC_CONT= YES
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -13
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_RAE2822_turb_ffd.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
 OUTPUT_FILES=(PARAVIEW_ASCII)
+
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING,
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC, NACA_4DIGITS, AIRFOIL)
-%
-% Parameters of the shape deformation
-% - TRANSLATION ( x_Disp, y_Disp, z_Disp ), as a unit vector
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - SCALE ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - PARABOLIC ( Center, Thickness )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - AIRFOIL ( 1.0 )
-%
 DV_KIND= FFD_CONTROL_POINT_2D
 DV_MARKER= ( AIRFOIL )
 DV_PARAM= ( MAIN_BOX, 7, 1, 0.0, 1.0)
@@ -288,99 +123,25 @@ DV_VALUE= 0.1
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 1000
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Deformation coefficient (in theory from -1.0 to 0.5, a large value is also valid)
 DEFORM_COEFF = 1E6
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-15
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 500
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (MAIN_BOX, -0.00000001, -0.07, 0.0, 1.00000001, -0.07, 0.0, 1.00000001, 0.07, 0.0, -0.00000001, 0.07, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= ( 14, 1, 0)
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= 2ND_DERIVATIVE
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-
-% Optimization objective function with optional scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.001
-
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= NONE
-
-% List of design variables (Design variables are separated by semicolons)
 DEFINITION_DV= ( 19, 1.0 | AIRFOIL | MAIN_BOX, 0, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 1, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 2, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 3, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 4, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 5, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 6, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 7, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 8, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 9, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 10, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 11, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 12, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 13, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 14, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 0, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 1, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 2, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 3, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 4, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 5, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 6, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 7, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 8, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 9, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 10, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 11, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 12, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 13, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | MAIN_BOX, 14, 1, 0.0, 1.0 )
 
diff --git a/TestCases/deformation/spherical_ffd/def_spherical.cfg b/TestCases/deformation/spherical_ffd/def_spherical.cfg
index d1f910c3234..8960ae42f06 100644
--- a/TestCases/deformation/spherical_ffd/def_spherical.cfg
+++ b/TestCases/deformation/spherical_ffd/def_spherical.cfg
@@ -5,298 +5,122 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)
 SOLVER= EULER 
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% System of measurements (SI, US)
-% International system of units (SI): ( meters, kilograms, Kelvins,
-%                                       Newtons = kg m/s^2, Pascals = N/m^2, 
-%                                       Density = kg/m^3, Speed = m/s,
-%                                       Equiv. Area = m^2 )
-% United States customary units (US): ( inches, slug, Rankines, lbf = slug ft/s^2, 
-%                                       psf = lbf/ft^2, Density = slug/ft^3, 
-%                                       Speed = ft/s, Equiv. Area = ft^2 )
 SYSTEM_MEASUREMENTS= US
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Side-slip angle (degrees, only for compressible flows)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream temperature (518.67 R by default)
 FREESTREAM_TEMPERATURE= 518.67
-%
-% Free-stream pressure (101325.0 N/m^2, 2116.216 psf by default)
 FREESTREAM_PRESSURE= 2116.216 
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation (in)
 REF_ORIGIN_MOMENT_X = 0.0
 REF_ORIGIN_MOMENT_Y = 0.0
 REF_ORIGIN_MOMENT_Z = 0.0
-%
-% Reference length for pitching, rolling, and yawing non-dimensional
-% moment (in)
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic
-% calculation) (in^2)
 REF_AREA= 0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= DIMENSIONAL
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( SPHERE, 0.0)
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( FARFIELD )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( SPHERE )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( SPHERE )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( SPHERE )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS 
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.0, 1.0, 1.0, 10.0 )
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, AVG_TOTAL_PRESSURE, 
-%                                             MASS_FLOW_RATE)
 OBJECTIVE_FUNCTION= DRAG
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Sensitivity for detecting sharp edges (< 3 high sensitivity).
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Venkatakrishnan's limiter coefficient (from 0.3 to 0.003)
 VENKAT_LIMITER_COEFF= 0.003
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-12
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH_JESPERSEN)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING,
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS
-%                      FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, FFD_ROTATION,
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC, NACA_4DIGITS, AIRFOIL)
 DV_KIND= FFD_CONTROL_POINT 
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( SPHERE )
-%
-% Parameters of the shape deformation
-% - TRANSLATION ( x_Disp, y_Disp, z_Disp )
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - SCALE ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_DIHEDRAL_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - PARABOLIC ( Center, Thickness )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - AIRFOIL ( 1.0 )
 DV_PARAM= ( SPHERE_BOX, 0, 3, 2, 1.0, 0.0, 0.0 )
-%
-% Value of the shape deformation
 DV_VALUE= 0.1 
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, JACOBI)
 DEFORM_LINEAR_SOLVER_PREC= LU_SGS
-%
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 100
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-10
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 1000
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (SPHERE_BOX, -0.6, -0.1, 1.0, -0.6, -0.1, 0.5, -0.6, 0.1, 0.5, -0.6, 0.1, 1.0, 0.6, -0.1, 1.0, 0.6, -0.1, 0.5, 0.6, 0.1, 0.5, 0.6, 0.1, 1.0)
-%
-% FFD box degree: 3D case (r_degree, theta_degree, phi_degree)
 FFD_DEGREE= (1, 9, 4)
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= 1ST_DERIVATIVE
-%
-% FFD coordinate system (CARTESIAN, CYLINDRICAL, SPHERICAL)
 FFD_COORD_SYSTEM= SPHERICAL
-%
-% Axis for the FFD box (cylindrical and spherical coordinates)
 FFD_AXIS= (0.0, 0.0, 0.0)
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Number of total iterations
 ITER= 5
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= spherical.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2 
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1500
-%
-%
diff --git a/TestCases/deformation/spherical_ffd/def_spherical_bspline.cfg b/TestCases/deformation/spherical_ffd/def_spherical_bspline.cfg
index 20a995bca7f..db9825dd3ef 100644
--- a/TestCases/deformation/spherical_ffd/def_spherical_bspline.cfg
+++ b/TestCases/deformation/spherical_ffd/def_spherical_bspline.cfg
@@ -5,305 +5,124 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)
 SOLVER= EULER 
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% System of measurements (SI, US)
-% International system of units (SI): ( meters, kilograms, Kelvins,
-%                                       Newtons = kg m/s^2, Pascals = N/m^2, 
-%                                       Density = kg/m^3, Speed = m/s,
-%                                       Equiv. Area = m^2 )
-% United States customary units (US): ( inches, slug, Rankines, lbf = slug ft/s^2, 
-%                                       psf = lbf/ft^2, Density = slug/ft^3, 
-%                                       Speed = ft/s, Equiv. Area = ft^2 )
 SYSTEM_MEASUREMENTS= US
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Side-slip angle (degrees, only for compressible flows)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream temperature (518.67 R by default)
 FREESTREAM_TEMPERATURE= 518.67
-%
-% Free-stream pressure (101325.0 N/m^2, 2116.216 psf by default)
 FREESTREAM_PRESSURE= 2116.216 
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation (in)
 REF_ORIGIN_MOMENT_X = 0.0
 REF_ORIGIN_MOMENT_Y = 0.0
 REF_ORIGIN_MOMENT_Z = 0.0
-%
-% Reference length for pitching, rolling, and yawing non-dimensional
-% moment (in)
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic
-% calculation) (in^2)
 REF_AREA= 0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= DIMENSIONAL
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( SPHERE, 0.0)
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( FARFIELD )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( SPHERE )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( SPHERE )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( SPHERE )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS 
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.0, 1.0, 1.0, 10.0 )
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, AVG_TOTAL_PRESSURE, 
-%                                             MASS_FLOW_RATE)
 OBJECTIVE_FUNCTION= DRAG
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Sensitivity for detecting sharp edges (< 3 high sensitivity).
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Venkatakrishnan's limiter coefficient (from 0.3 to 0.003)
 VENKAT_LIMITER_COEFF= 0.003
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-12
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH_JESPERSEN)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING,
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS
-%                      FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, FFD_ROTATION,
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC, NACA_4DIGITS, AIRFOIL)
 DV_KIND= FFD_CONTROL_POINT
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( SPHERE )
-%
-% Parameters of the shape deformation
-% - TRANSLATION ( x_Disp, y_Disp, z_Disp )
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - SCALE ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_DIHEDRAL_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - PARABOLIC ( Center, Thickness )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - AIRFOIL ( 1.0 )
 DV_PARAM= ( SPHERE_BOX, 0, 3, 2, 1.0, 0.0, 0.0 )
-%
-% Value of the shape deformation
 DV_VALUE= 0.1 
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, JACOBI)
 DEFORM_LINEAR_SOLVER_PREC= LU_SGS
-%
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 100
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-10
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 1000
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (SPHERE_BOX, -0.6, -0.1, 1.0, -0.6, -0.1, 0.5, -0.6, 0.1, 0.5, -0.6, 0.1, 1.0, 0.6, -0.1, 1.0, 0.6, -0.1, 0.5, 0.6, 0.1, 0.5, 0.6, 0.1, 1.0)
-%
-% FFD box degree: 3D case (r_degree, theta_degree, phi_degree)
 FFD_DEGREE= (1, 9, 4)
-%
-%
-% FFD Blending function: Bezier curves with global support (BEZIER), uniform BSplines with local support (BSPLINE_UNIFORM)
 FFD_BLENDING= BSPLINE_UNIFORM
-%
-% Order of the BSplines 
 FFD_BSPLINE_ORDER= 2, 2, 2
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= 1ST_DERIVATIVE
-%
-% FFD coordinate system (CARTESIAN, CYLINDRICAL, SPHERICAL)
 FFD_COORD_SYSTEM= SPHERICAL
-%
-% Axis for the FFD box (cylindrical and spherical coordinates)
 FFD_AXIS= (0.0, 0.0, 0.0)
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Number of total iterations
 ITER= 5
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= spherical_bspline.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2 
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1500
-%
-%
diff --git a/TestCases/disc_adj_euler/arina2k/Arina2KRS.cfg b/TestCases/disc_adj_euler/arina2k/Arina2KRS.cfg
index 6c097f96917..c6646926676 100644
--- a/TestCases/disc_adj_euler/arina2k/Arina2KRS.cfg
+++ b/TestCases/disc_adj_euler/arina2k/Arina2KRS.cfg
@@ -6,156 +6,65 @@
 % Author: Jairo Paes Cavalcante Filho [Based on T. Economon & M. Pini work]    %
 % Institution: University of São Paulo                                         %
 % Date: 8-JUL-2018                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Specify turbulence model (NONE, SA, SA_NEG, SST, SA_E, SA_COMP, SA_E_COMP)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT)
 MATH_PROBLEM= DISCRETE_ADJOINT
-%
-%
-% Axisymmetric simulation, only compressible flows (NO, YES)
 AXISYMMETRIC= NO
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Discard the data storaged in the solution and geometry files
-% e.g. AOA, dCL/dAoA, dCD/dCL, iter, etc.
-% Note that AoA in the solution and geometry files is critical
-% to aero design using AoA as a variable. (NO, YES)
 DISCARD_INFILES= NO
-%
-% System of measurements (SI, US)
-% International system of units (SI): ( meters, kilograms, Kelvins,
-%                                       Newtons = kg m/s^2, Pascals = N/m^2, 
-%                                       Density = kg/m^3, Speed = m/s,
-%                                       Equiv. Area = m^2 )
-% United States customary units (US): ( inches, slug, Rankines, lbf = slug ft/s^2, 
-%                                       psf = lbf/ft^2, Density = slug/ft^3, 
-%                                       Speed = ft/s, Equiv. Area = ft^2 )
 SYSTEM_MEASUREMENTS= SI
 
 % -------------------- COMPRESSIBLE FREE-STREAM 
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.2395
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Side-slip angle (degrees, only for compressible flows)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream option to choose between density and temperature (default) for
-% initializing the solution (TEMPERATURE_FS, DENSITY_FS)
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-% Free-stream pressure (101325.0 N/m^2, 2116.216 psf by default)
 FREESTREAM_PRESSURE= 100000.0
-%
-% Free-stream temperature (288.15 K, 518.67 R by default)
 FREESTREAM_TEMPERATURE= 288.0
 %
-% Free-stream density (1.2886 Kg/m^3, 0.0025 slug/ft^3 by default)
 FREESTREAM_DENSITY= 1.2092
-%
-% Free-stream velocity (1.0 m/s, 1.0 ft/s by default)
 FREESTREAM_VELOCITY= ( 1.0, 0.00, 0.00 )
-%
-% Compressible flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
-% Reference origin for moment computation (m or in)
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for moment non-dimensional coefficients (m or in)
 REF_LENGTH= 1.0
-%
-% Reference area for non-dimensional force coefficients (0 implies automatic
-% calculation) (m^2 or in^2)
 REF_AREA= 1.0
-%
+
 % ---- IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
-% Fluid model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS,
-%              CONSTANT_DENSITY, INC_IDEAL_GAS)
 FLUID_MODEL= IDEAL_GAS
-%
-% Ratio of specific heats (1.4 default and the value is hardcoded
-%                          for the model STANDARD_AIR, compressible only)
 GAMMA_VALUE= 1.338
-%
-% Specific gas constant (287.058 J/kg*K default and this value is hardcoded
-%                        for the model STANDARD_AIR, compressible only)
 GAS_CONSTANT= 518.28
-%
-% Critical Temperature (131.00 K by default)
 CRITICAL_TEMPERATURE= 190.564
-%
-% Critical Pressure (3588550.0 N/m^2 by default)
 CRITICAL_PRESSURE= 4599200.0
-%
-% Acentric factor (0.035 (air))
 ACENTRIC_FACTOR= 0.01142
-%
+
 % ------------------------ SUPERSONIC SIMULATION ------------------------------%
-% Evaluate equivalent area on the Near-Field (NO, YES)
+%
 EQUIV_AREA= NO
 
 % --------------------- INVERSE DESIGN SIMULATION -----------------------------%
 %
-% Evaluate an inverse design problem using Cp (NO, YES)
 INV_DESIGN_CP= YES
-%
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( WALL1 )
-%
-% Symmetry boundary marker(s) (NONE = no marker)
 MARKER_SYM= ( SYMMETRY )
-%
-% Internal boundary marker(s) e.g. no boundary condition (NONE = no marker)
 MARKER_INTERNAL= ( NONE )
-%
-% Near-Field boundary marker(s) (NONE = no marker)
 MARKER_NEARFIELD= ( NONE )
-%
-% Inlet boundary type (TOTAL_CONDITIONS, MASS_FLOW)
 INLET_TYPE= TOTAL_CONDITIONS
-%
-% Read inlet profile from a file (YES, NO) default: NO
 SPECIFIED_INLET_PROFILE= NO
-%
-% Inlet boundary marker(s) with the following formats (NONE = no marker)
-% Total Conditions: (inlet marker, total temp, total pressure, flow_direction_x,
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-% Mass Flow: (inlet marker, density, velocity magnitude, flow_direction_x,
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-% Incompressible: (inlet marker, temperature, velocity magnitude, flow_direction_x,
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
 MARKER_INLET= ( INFLOW, 288.0 100000.0, 1.0, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
 MARKER_OUTLET= ( OUTFLOW, 83049.0 )
 %
 MARKER_SHROUD= (NONE)
@@ -166,447 +75,145 @@ MARKER_GILES= ( NONE )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( WALL1 )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( WALL1 )
-%
-% Marker(s) of the surface where custom thermal BC's are defined.
 MARKER_PYTHON_CUSTOM = ( NONE )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( WALL1 )
-%
-% Marker(s) of the surface that is going to be analyzed in detail (massflow, average pressure, distortion, etc)
 MARKER_ANALYZE = ( WALL1 )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% CFL number (initial value for the adaptive CFL number)
 CFL_NUMBER= 0.94
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.25, 50.0 )
-%
-% Maximum Delta Time in local time stepping simulations
 MAX_DELTA_TIME= 1E6
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE, 
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= INVERSE_DESIGN_PRESSURE
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT = 1.0
 
 % ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
 %
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence adjoint equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJTURB= NO
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_ADJTURB= VENKATAKRISHNAN
-%
-% Coefficient for the Venkat's limiter (upwind scheme). A larger values decrease
-%             the extent of limiting, values approaching zero cause
-%             lower-order approximation to the solution (0.05 by default)
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Coefficient for the adjoint sharp edges limiter (3.0 by default).
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
-%
-% 1st order artificial dissipation coefficients for
-%     the Lax–Friedrichs method ( 0.15 by default )
 LAX_SENSOR_COEFF= 0.15
-%
-% 2nd and 4th order artificial dissipation coefficients for
-%     the JST method ( 0.5, 0.02 by default )
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% 1st order artificial dissipation coefficients for
-%     the adjoint Lax–Friedrichs method ( 0.15 by default )
 ADJ_LAX_SENSOR_COEFF= 0.15
-%
-% 2nd, and 4th order artificial dissipation coefficients for
-%     the adjoint JST method ( 0.5, 0.02 by default )
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-grid levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.75
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW, FDS)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Post-reconstruction correction for low Mach number flows (NO, YES)
 LOW_MACH_CORR= NO
-%
-% Roe-Turkel preconditioning for low Mach number flows (NO, YES)
 LOW_MACH_PREC= NO
-%
-% Entropy fix coefficient (0.0 implies no entropy fixing, 1.0 implies scalar
-%                          artificial dissipation)
 ENTROPY_FIX_COEFF= 0.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
-%
-% Relaxation coefficient
-
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Relaxation coefficient
 RELAXATION_FACTOR_ADJOINT= 1.0
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.96
-%
-% Limit value for the adjoint variable
 LIMIT_ADJFLOW= 1E6
-%
-% Use multigrid in the adjoint problem (NO, YES)
 MG_ADJFLOW= YES
 
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
 %
-% Marker(s) of the surface where geometrical based function will be evaluated
 GEO_MARKER= ( WALL1 )
-%
-% Description of the geometry to be analyzed (AIRFOIL, WING)
 GEO_DESCRIPTION= AIRFOIL
-%
-% Plot loads and Cp distributions on each airfoil section
 GEO_PLOT_STATIONS= NO
-%
-% Geometrical evaluation mode (FUNCTION, GRADIENT)
 GEO_MODE= FUNCTION
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (NO_DEFORMATION, SCALE_GRID, TRANSLATE_GRID, ROTATE_GRID,
-%                      FFD_SETTING, FFD_NACELLE,
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS, FFD_TWIST
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D, 
-%                      FFD_TWIST_2D, HICKS_HENNE, SURFACE_BUMP, SURFACE_FILE)
 DV_KIND= HICKS_HENNE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( WALL1 )
-%
-% Parameters of the shape deformation
-% - NO_DEFORMATION ( 1.0 )
-% - TRANSLATE_GRID ( x_Disp, y_Disp, z_Disp ), as a unit vector
-% - ROTATE_GRID ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End ) axis, DV_VALUE in deg.
-% - SCALE_GRID ( 1.0 )
-% - ANGLE_OF_ATTACK ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_NACELLE ( FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Disp, phi_Disp )
-% - FFD_GULL ( FFD_BoxTag, j_Ind )
-% - FFD_ANGLE_OF_ATTACK ( FFD_BoxTag, 1.0 )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_TWIST ( FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - FFD_TWIST_2D ( FFD_BoxTag, x_Orig, y_Orig )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - SURFACE_BUMP ( x_Start, x_End, x_Loc )
-%
 DV_PARAM= ( 0, 0.5 )
-%
-% Value of the shape deformation
 DV_VALUE= 0.01
-%
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= BCGSTAB
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, JACOBI)
 DEFORM_LINEAR_SOLVER_PREC= LU_SGS
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 1000
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Deformation coefficient (linear elasticity limits from -1.0 to 0.5, a larger
-% value is also possible)
 DEFORM_COEFF = 0.1
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                           WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-%
-% Deform the grid only close to the surface. It is possible to specify how much
-% of the volumetric grid is going to be deformed in meters or inches (1E6 by default)
 DEFORM_LIMIT = 0.3
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Number of total iterations
 ITER= 12000
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -9.00
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 20
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= Arina2Kmesh.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= MESHOUT_Arina2Kmesh.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1000
-%
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= YES
-%
-% Reorient elements based on potential negative volumes (YES/NO)
 REORIENT_ELEMENTS= YES
-%
-% Screen output
 SCREEN_OUTPUT = (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_PRESS, SENS_AOA)
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-%
-% Optimization objective function with scaling factor, separated by semicolons.
-% To include quadratic penalty function: use OPT_CONSTRAINT option syntax within the OPT_OBJECTIVE list.
-% ex= Objective * Scale
 OPT_OBJECTIVE= INVERSE_DESIGN_PRESSURE * 0.9
-%
-% Optimization constraint functions with pushing factors (affects its value, not the gradient  in the python scripts), separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= ( AIRFOIL_THICKNESS > 0.049999999999 ) * 0.9
-%OPT_CONSTRAINT= NONE 
-%
-% Factor to reduce the norm of the gradient (affects the objective function and gradient in the python scripts)
-% In general, a norm of the gradient ~1E-6 is desired.
 OPT_GRADIENT_FACTOR= 1E-6
-%
-% Factor to relax or accelerate the optimizer convergence (affects the line search in SU2_DEF)
-% In general, surface deformations of 0.01'' or 0.0001m are desirable
 OPT_RELAX_FACTOR= 1E3
-%
-% Maximum number of iterations
 OPT_ITERATIONS= 1
-%
-% Requested accuracy
 OPT_ACCURACY= 1E-1
-%
-% Optimization bound (bounds the line search in SU2_DEF)
 OPT_LINE_SEARCH_BOUND= 1E6
-%
-% Upper bound for each design variable (bound in the python optimizer)
 OPT_BOUND_UPPER= 5E-3
-%
-% Lower bound for each design variable (bound in the python optimizer)
 OPT_BOUND_LOWER= -5E-3
-%
-% Finite difference step size for python scripts (0.001 default, recommended
-%												  0.001 x REF_LENGTH)
 FIN_DIFF_STEP = 0.001
-%
-% Optimization design variables, separated by semicolons
-%
 DEFINITION_DV= ( 30 , 1.0 | WALL1 | 0 , 0.05  ); ( 30 , 1.0 | WALL1 | 0 , 0.1  ); ( 30 , 1.0 | WALL1 | 0 , 0.15  ); ( 30 , 1.0 | WALL1 | 0 , 0.2  ); ( 30 , 1.0 | WALL1 | 0 , 0.25  ); ( 30 , 1.0 | WALL1 | 0 , 0.3  ); ( 30 , 1.0 | WALL1 | 0 , 0.35  ); ( 30 , 1.0 | WALL1 | 0 , 0.4  ); ( 30 , 1.0 | WALL1 | 0 , 0.45  ); ( 30 , 1.0 | WALL1 | 0 , 0.5  ); ( 30 , 1.0 | WALL1 | 0 , 0.505  ); ( 30 , 1.0 | WALL1 | 0 , 0.510  ); ( 30 , 1.0 | WALL1 | 0 , 0.515  ); ( 30 , 1.0 | WALL1 | 0 , 0.520  ); ( 30 , 1.0 | WALL1 | 0 , 0.525  ); ( 30 , 1.0 | WALL1 | 0 , 0.530  ); ( 30 , 1.0 | WALL1 | 0 , 0.535  ); ( 30 , 1.0 | WALL1 | 0 , 0.540  ); ( 30 , 1.0 | WALL1 | 0 , 0.545  ); ( 30 , 1.0 | WALL1 | 0 , 0.550  ); ( 30 , 1.0 | WALL1 | 0 , 0.555  ); ( 30 , 1.0 | WALL1 | 0 , 0.560  ); ( 30 , 1.0 | WALL1 | 0 , 0.565  ); ( 30 , 1.0 | WALL1 | 0 , 0.570  ); ( 30 , 1.0 | WALL1 | 0 , 0.575  ); ( 30 , 1.0 | WALL1 | 0 , 0.580  ); ( 30 , 1.0 | WALL1 | 0 , 0.585  ); ( 30 , 1.0 | WALL1 | 0 , 0.590  ); ( 30 , 1.0 | WALL1 | 0 , 0.595  ); ( 30 , 1.0 | WALL1 | 0 , 0.600  ); ( 30 , 1.0 | WALL1 | 0 , 0.605  ); ( 30 , 1.0 | WALL1 | 0 , 0.610  ); ( 30 , 1.0 | WALL1 | 0 , 0.615  ); ( 30 , 1.0 | WALL1 | 0 , 0.620  ); ( 30 , 1.0 | WALL1 | 0 , 0.625  ); ( 30 , 1.0 | WALL1 | 0 , 0.630  ); ( 30 , 1.0 | WALL1 | 0 , 0.635  ); ( 30 , 1.0 | WALL1 | 0 , 0.640  ); ( 30 , 1.0 | WALL1 | 0 , 0.645  ); ( 30 , 1.0 | WALL1 | 0 , 0.650  ); ( 30 , 1.0 | WALL1 | 0 , 0.655  ); ( 30 , 1.0 | WALL1 | 0 , 0.660  ); ( 30 , 1.0 | WALL1 | 0 , 0.665  ); ( 30 , 1.0 | WALL1 | 0 , 0.670  ); ( 30 , 1.0 | WALL1 | 0 , 0.675  ); ( 30 , 1.0 | WALL1 | 0 , 0.680  ); ( 30 , 1.0 | WALL1 | 0 , 0.685  ); ( 30 , 1.0 | WALL1 | 0 , 0.690  ); ( 30 , 1.0 | WALL1 | 0 , 0.695  ); ( 30 , 1.0 | WALL1 | 0 , 0.700  ); ( 30 , 1.0 | WALL1 | 0 , 0.705  ); ( 30 , 1.0 | WALL1 | 0 , 0.710  ); ( 30 , 1.0 | WALL1 | 0 , 0.715  ); ( 30 , 1.0 | WALL1 | 0 , 0.720  ); ( 30 , 1.0 | WALL1 | 0 , 0.725  ); ( 30 , 1.0 | WALL1 | 0 , 0.730  ); ( 30 , 1.0 | WALL1 | 0 , 0.735  ); ( 30 , 1.0 | WALL1 | 0 , 0.740  ); ( 30 , 1.0 | WALL1 | 0 , 0.745  ); ( 30 , 1.0 | WALL1 | 0 , 0.750  ); ( 30 , 1.0 | WALL1 | 0 , 0.755  ); ( 30 , 1.0 | WALL1 | 0 , 0.760  ); ( 30 , 1.0 | WALL1 | 0 , 0.765  ); ( 30 , 1.0 | WALL1 | 0 , 0.770  ); ( 30 , 1.0 | WALL1 | 0 , 0.775  ); ( 30 , 1.0 | WALL1 | 0 , 0.780  ); ( 30 , 1.0 | WALL1 | 0 , 0.785  ); ( 30 , 1.0 | WALL1 | 0 , 0.790  ); ( 30 , 1.0 | WALL1 | 0 , 0.795  ); ( 30 , 1.0 | WALL1 | 0 , 0.8  ); ( 30 , 1.0 | WALL1 | 0 , 0.85 ); ( 30 , 1.0 | WALL1 | 0 , 0.9  ); ( 30 , 1.0 | WALL1 | 0 , 0.95  )
 %
-% Use combined objective within gradient evaluation: may reduce cost to compute gradients when using the adjoint formulation.
 OPT_COMBINE_OBJECTIVE = YES
diff --git a/TestCases/disc_adj_euler/cylinder3D/inv_cylinder3D.cfg b/TestCases/disc_adj_euler/cylinder3D/inv_cylinder3D.cfg
index 4da72568647..c91b61acab8 100644
--- a/TestCases/disc_adj_euler/cylinder3D/inv_cylinder3D.cfg
+++ b/TestCases/disc_adj_euler/cylinder3D/inv_cylinder3D.cfg
@@ -5,226 +5,89 @@
 % Author: ___________________________________________________________________  %
 % Institution: ______________________________________________________________  %
 % Date: __________                                                             %
-% File Version 7.4.0 "Blackbird"                                                   %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT)
 MATH_PROBLEM= DISCRETE_ADJOINT
 %
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Discard the data storaged in the solution and geometry files
-% e.g. AOA, dCL/dAoA, dCD/dCL, iter, etc.
-% Note that AoA in the solution and geometry files is critical
-% to aero design using AoA as a variable. (NO, YES)
 DISCARD_INFILES= NO
-%
-% System of measurements (SI, US)
-% International system of units (SI): ( meters, kilograms, Kelvins,
-%                                       Newtons = kg m/s^2, Pascals = N/m^2, 
-%                                       Density = kg/m^3, Speed = m/s,
-%                                       Equiv. Area = m^2 )
-% United States customary units (US): ( inches, slug, Rankines, lbf = slug ft/s^2, 
-%                                       psf = lbf/ft^2, Density = slug/ft^3, 
-%                                       Speed = ft/s, Equiv. Area = ft^2 )
 SYSTEM_MEASUREMENTS= SI
-%
-% Reorient elements based on potential negative volumes (YES/NO)
 REORIENT_ELEMENTS= NO 
 HISTORY_OUTPUT= (ITER, RMS_RES, SENSITIVITY)
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.3
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2, 2116.216 psf by default)
 FREESTREAM_PRESSURE= 101325.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation (m or in)
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for moment non-dimensional coefficients (m or in)
 REF_LENGTH= 1.0
-%
-% Reference area for non-dimensional force coefficients (0 implies automatic
-% calculation) (m^2 or in^2)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes (no-slip), constant heat flux wall  marker(s) (NONE = no marker)
-% Format: ( marker name, constant heat flux (J/m^2), ... )
 MARKER_EULER= (CYLINDER_DOWN, CYLINDER_UP, SIDE, WALL)
-%
-% Inlet boundary type (TOTAL_CONDITIONS, MASS_FLOW)
 INLET_TYPE= MASS_FLOW 
-%
-% Inlet boundary marker(s) with the following formats (NONE = no marker)
-% Total Conditions: (inlet marker, total temp, total pressure, flow_direction_x,
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-% Mass Flow: (inlet marker, density, velocity magnitude, flow_direction_x,
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-% Incompressible: (inlet marker, NULL, velocity magnitude, flow_direction_x,
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
 MARKER_INLET= ( IN, 1.22498, 102.089, 1.0, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
 MARKER_OUTLET= ( OUT, 101325 )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( CYLINDER_DOWN, CYLINDER_UP )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( CYLINDER_DOWN, CYLINDER_UP )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( CYLINDER_DOWN, CYLINDER_UP )
-%
-% Marker(s) of the surface that is going to be analyzed in detail (massflow, average pressure, distortion, etc)
 MARKER_ANALYZE = ( IN, OUT )
-%
-% Method to compute the average value in MARKER_ANALYZE (AREA, MASSFLUX).
 MARKER_ANALYZE_AVERAGE = AREA 
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% CFL number (initial value for the adaptive CFL number)
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.25, 50.0 )
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= LIFT 
 
 % ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
 %
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence adjoint equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJTURB= NO
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_ADJTURB= VENKATAKRISHNAN
-%
-% Coefficient for the Venkat's limiter (upwind scheme). A larger values decrease
-%             the extent of limiting, values approaching zero cause
-%             lower-order approximation to the solution (0.05 by default)
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Coefficient for the adjoint sharp edges limiter (3.0 by default).
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
-%
-% 1st order artificial dissipation coefficients for
-%     the Lax–Friedrichs method ( 0.15 by default )
 LAX_SENSOR_COEFF= 0.15
-%
-% 2nd and 4th order artificial dissipation coefficients for
-%     the JST method ( 0.5, 0.02 by default )
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% 1st order artificial dissipation coefficients for
-%     the adjoint Lax–Friedrichs method ( 0.15 by default )
 ADJ_LAX_SENSOR_COEFF= 0.15
-%
-% 2nd, and 4th order artificial dissipation coefficients for
-%     the adjoint JST method ( 0.5, 0.02 by default )
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 3
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
-%
-% Relaxation coefficient
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
@@ -232,93 +95,37 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % adjoint formulation. The AD will use the numerical methods in
 % the ADJOINT-FLOW NUMERICAL METHOD DEFINITION section (NO, YES)
 INCONSISTENT_DISC= NO
-%
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Relaxation coefficient
 RELAXATION_FACTOR_ADJOINT= 0.95
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.8
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Number of total iterations
 ITER= 100
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= cylinder3D.cgns
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= CGNS
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 2525
-%
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= YES
-%  
-%Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_PRESS, SENS_AOA)
diff --git a/TestCases/disc_adj_euler/naca0012_pitching/inv_NACA0012_pitching.cfg b/TestCases/disc_adj_euler/naca0012_pitching/inv_NACA0012_pitching.cfg
index 03f0cfcba25..ae54063eeeb 100644
--- a/TestCases/disc_adj_euler/naca0012_pitching/inv_NACA0012_pitching.cfg
+++ b/TestCases/disc_adj_euler/naca0012_pitching/inv_NACA0012_pitching.cfg
@@ -1,30 +1,16 @@
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION) 
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DISCRETE_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 TIME_ITER= 5
 INNER_ITER= 50
 
-%EXT_ITER= 151
-%UNST_INT_ITER= 110
-SCREEN_OUTPUT=(TIME_ITER, INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_PRESS, SENS_AOA)
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER,
-%                      DUAL_TIME_STEPPING-2ND_ORDER)
 TIME_DOMAIN= YES
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-%
-% Time Step for dual time stepping simulations (s)
 TIME_STEP= 0.0023555025613149587
 % 24 steps per period: 0.0024536485013697488
 % 25 steps per period: 0.0023555025613149587
@@ -32,306 +18,132 @@ TIME_STEP= 0.0023555025613149587
 % Total Physical Time for dual time stepping simulations (s)
 % 150 steps
 MAX_TIME= 0.354
-%
-% Iteration number to begin unsteady restarts
 RESTART_ITER= 10
-%
-% Starting direct iteration for unsteady adjoint
 UNST_ADJOINT_ITER= 151
 
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Dynamic mesh simulation (NO, YES)
 GRID_MOVEMENT= RIGID_MOTION
-%
-% Motion mach number (non-dimensional). Used for initializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.796
-%
-% Coordinates of the rigid motion origin
 MOTION_ORIGIN= (0.248 0.0 0.0)
-%
-% Pitching angular freq. (rad/s) about x, y, & z axes (RIGID_MOTION only)
 PITCHING_OMEGA= (0.0 0.0 106.69842)
-%
-% Pitching amplitude (degrees) about x, y, & z axes (RIGID_MOTION only)
 PITCHING_AMPL= (0.0 0.0 1.01)
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AOA= 1.25
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (LU_SGS,
-%                                              SYM_GAUSS_SEIDEL, BCGSTAB, GMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (NONE, JACOBI, LINELET, LUSGS)
 LINEAR_SOLVER_PREC= ILU
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 1.0
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 1.0
 
 % --------------------- FLOW NUMERICAL METHOD DEFINITION ----------------------%
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                              ROE-2ND_ORDER)
-CONV_NUM_METHOD_FLOW= JST
 %
-% Slope limiter (VENKATAKRISHNAN)
+CONV_NUM_METHOD_FLOW= JST
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE)
+%
 OBJECTIVE_FUNCTION= EFFICIENCY
 OPT_OBJECTIVE= EFFICIENCY
-%
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                              ROE-2ND_ORDER)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Slope limiter (VENKATAKRISHNAN, SHARP_EDGES)
 SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.8
-%
-% Limit value for the adjoint variable
 LIMIT_ADJFLOW= 1E6
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-10
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 500
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (airfoil_box, -0.1, -0.25, 0, 1.1, -0.25, 0, 1.1, 0.25, 0, -0.1, 0.25, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0)
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= (10, 1, 0)
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= 2ND_DERIVATIVE
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (FFD_SETTING, FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, COSINE_BUMP, PARABOLIC,
-%                      NACA_4DIGITS, DISPLACEMENT, ROTATION, FFD_CONTROL_POINT,
-%                      FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, FFD_ROTATION,
-%                      FFD_CAMBER, FFD_THICKNESS, FFD_CONTROL_SURFACE, SURFACE_FILE, AIRFOIL)
-%DV_KIND= FFD_CONTROL_POINT, FFD_CONTROL_POINT, FFD_CONTROL_POINT, FFD_CONTROL_POINT, FFD_CONTROL_POINT, FFD_CONTROL_POINT, FFD_CONTROL_POINT, FFD_CONTROL_POINT, FFD_CONTROL_POINT, FFD_CONTROL_POINT, FFD_CONTROL_POINT, FFD_CONTROL_POINT, FFD_CONTROL_POINT, FFD_CONTROL_POINT, FFD_CONTROL_POINT, FFD_CONTROL_POINT, FFD_CONTROL_POINT, FFD_CONTROL_POINT, FFD_CONTROL_POINT, FFD_CONTROL_POINT, FFD_CONTROL_POINT, FFD_CONTROL_POINT
 DV_KIND= FFD_SETTING
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation
-%       - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-%       - FFD_DIHEDRAL_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%       - FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%       - FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%       - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-%       - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-%       - FFD_VOLUME ( FFD_BoxTag, i_Ind, j_Ind )
-%DV_PARAM= ( airfoil_box, 0, 0, 0, 0.0, 1.0, 0.0 ); ( airfoil_box, 1, 0, 0, 0.0, 1.0, 0.0 ); ( airfoil_box, 2, 0, 0, 0.0, 1.0, 0.0 ); ( airfoil_box, 3, 0, 0, 0.0, 1.0, 0.0 ); ( airfoil_box, 4, 0, 0, 0.0, 1.0, 0.0 ); ( airfoil_box, 5, 0, 0, 0.0, 1.0, 0.0 ); ( airfoil_box, 6, 0, 0, 0.0, 1.0, 0.0 ); ( airfoil_box, 7, 0, 0, 0.0, 1.0, 0.0 ); ( airfoil_box, 8, 0, 0, 0.0, 1.0, 0.0 ); ( airfoil_box, 9, 0, 0, 0.0, 1.0, 0.0 ); ( airfoil_box, 10, 0, 0, 0.0, 1.0, 0.0 ); ( airfoil_box, 0, 1, 0, 0.0, 1.0, 0.0 ); ( airfoil_box, 1, 1, 0, 0.0, 1.0, 0.0 ); ( airfoil_box, 2, 1, 0, 0.0, 1.0, 0.0 ); ( airfoil_box, 3, 1, 0, 0.0, 1.0, 0.0 ); ( airfoil_box, 4, 1, 0, 0.0, 1.0, 0.0 ); ( airfoil_box, 5, 1, 0, 0.0, 1.0, 0.0 ); ( airfoil_box, 6, 1, 0, 0.0, 1.0, 0.0 ); ( airfoil_box, 7, 1, 0, 0.0, 1.0, 0.0 ); ( airfoil_box, 8, 1, 0, 0.0, 1.0, 0.0 ); ( airfoil_box, 9, 1, 0, 0.0, 1.0, 0.0 ); ( airfoil_box, 10, 1, 0, 0.0, 1.0, 0.0 )
 DV_PARAM= ( airfoil_box, 5, 0, 0, 0.0, 1.0, 0.0 )
-%
-% New value of the shape deformation
-%DV_VALUE= 0.05, 0.05, 0.05, 0.05, 0.05, 0.05, 0.05, 0.05, 0.05, 0.05, 0.05, 0.05, 0.05, 0.05, 0.05, 0.05, 0.05, 0.05, 0.05, 0.05, 0.05, 0.05
 DV_VALUE= 0.05
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Factor to multiply smallest cell volume for deform tolerance (0.001 default)
 DEFORM_LINEAR_SOLVER_ERROR = 0.000000001
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -20
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA0012_inv_FFD.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency for physical time steps (dual time)
 OUTPUT_WRT_FREQ= 1
-%
-
-% Optimization design variables, separated by semicolons
-% FFD_CONTROL_POINT (Y)
+SCREEN_OUTPUT=(TIME_ITER, INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_PRESS, SENS_AOA)
 DEFINITION_DV= ( 11, 1.0 | airfoil | airfoil_box, 0, 0, 0, 0.0, 1.0, 0.0 ); ( 11, 1.0 | airfoil | airfoil_box, 1, 0, 0, 0.0, 1.0, 0.0 ); ( 11, 1.0 | airfoil | airfoil_box, 2, 0, 0, 0.0, 1.0, 0.0 ); ( 11, 1.0 | airfoil | airfoil_box, 3, 0, 0, 0.0, 1.0, 0.0 ); ( 11, 1.0 | airfoil | airfoil_box, 4, 0, 0, 0.0, 1.0, 0.0 ); ( 11, 1.0 | airfoil | airfoil_box, 5, 0, 0, 0.0, 1.0, 0.0 ); ( 11, 1.0 | airfoil | airfoil_box, 6, 0, 0, 0.0, 1.0, 0.0 ); ( 11, 1.0 | airfoil | airfoil_box, 7, 0, 0, 0.0, 1.0, 0.0 ); ( 11, 1.0 | airfoil | airfoil_box, 8, 0, 0, 0.0, 1.0, 0.0 ); ( 11, 1.0 | airfoil | airfoil_box, 9, 0, 0, 0.0, 1.0, 0.0 ); ( 11, 1.0 | airfoil | airfoil_box, 10, 0, 0, 0.0, 1.0, 0.0 ); ( 11, 1.0 | airfoil | airfoil_box, 0, 1, 0, 0.0, 1.0, 0.0 ); ( 11, 1.0 | airfoil | airfoil_box, 1, 1, 0, 0.0, 1.0, 0.0 ); ( 11, 1.0 | airfoil | airfoil_box, 2, 1, 0, 0.0, 1.0, 0.0 ); ( 11, 1.0 | airfoil | airfoil_box, 3, 1, 0, 0.0, 1.0, 0.0 ); ( 11, 1.0 | airfoil | airfoil_box, 4, 1, 0, 0.0, 1.0, 0.0 ); ( 11, 1.0 | airfoil | airfoil_box, 5, 1, 0, 0.0, 1.0, 0.0 ); ( 11, 1.0 | airfoil | airfoil_box, 6, 1, 0, 0.0, 1.0, 0.0 ); ( 11, 1.0 | airfoil | airfoil_box, 7, 1, 0, 0.0, 1.0, 0.0 ); ( 11, 1.0 | airfoil | airfoil_box, 8, 1, 0, 0.0, 1.0, 0.0 ); ( 11, 1.0 | airfoil | airfoil_box, 9, 1, 0, 0.0, 1.0, 0.0 ); ( 11, 1.0 | airfoil | airfoil_box, 10, 1, 0, 0.0, 1.0, 0.0 )
-
diff --git a/TestCases/disc_adj_euler/oneram6/inv_ONERAM6.cfg b/TestCases/disc_adj_euler/oneram6/inv_ONERAM6.cfg
index ea005f88ee6..0443e598253 100644
--- a/TestCases/disc_adj_euler/oneram6/inv_ONERAM6.cfg
+++ b/TestCases/disc_adj_euler/oneram6/inv_ONERAM6.cfg
@@ -2,241 +2,110 @@
 %                                                                              %
 % SU2 configuration file                                                       %
 % Case description: Optimization case for the ONERA M6 wing in inviscid flow   %
-% Author: Francisco Palacios, Heather Kline	         	       	                 %
-% Institution: Stanford University	                                            %
+% Author: Francisco Palacios, Heather Kline                                    %
+% Institution: Stanford University                                             %
 % Date: 01.17.2017                                                             %
-% File Version 7.4.0 "Blackbird"                                                   %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT)
 MATH_PROBLEM= DISCRETE_ADJOINT 
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Discard the data storaged in the solution and geometry files
-% e.g. AOA, dCL/dAoA, dCD/dCL, iter, etc.
-% Note that AoA in the solution and geometry files is critical
-% to aero design using AoA as a variable. (NO, YES)
 DISCARD_INFILES= YES
-
-
 ITER = 11
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8395
-%
-% Angle of attack (degrees)
 AOA= 3.06
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only for Euler equations)
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % -------------------------- CL DRIVER DEFINITION -----------------------------%
 %
-% Activate fixed lift mode (specify a CL instead of AoA, NO/YES)
 FIXED_CL_MODE= NO 
-%
-% Target coefficient of lift for fixed lift mode (0.80 by default)
 TARGET_CL= 0.286 
-%
-% Estimation of dCL/dAlpha (0.2 per degree by default)
 DCL_DALPHA= 0.1
-%
-% Maximum number of iterations between AoA updates
 UPDATE_AOA_ITER_LIMIT= 100
-%
-% Number of iterations to evaluate dCL_dAlpha by using finite differences (500 by default)
 ITER_DCL_DALPHA= 500
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.2015
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 0.64607
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 implies no marker)
 MARKER_EULER= ( UPPER_SIDE, LOWER_SIDE, TIP )
-%
-% Marker of the far field (0 implies no marker)
 MARKER_FAR= ( XNORMAL_FACES, ZNORMAL_FACES, YNORMAL_FACE )
-%
-% Marker of symmetry boundary (0 implies no marker)
 MARKER_SYM= ( SYMMETRY_FACE )
-%
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( UPPER_SIDE, LOWER_SIDE, TIP )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( UPPER_SIDE, LOWER_SIDE, TIP )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 7.5
-%
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, ILU, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= ILU 
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2 
 
 % --------------------- FLOW NUMERICAL METHOD DEFINITION ----------------------%
-% Convective numerical method: (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                               ROE-2ND_ORDER)
-CONV_NUM_METHOD_FLOW= JST
 %
-% 2nd and 4th order artificial dissipation coefficients
+CONV_NUM_METHOD_FLOW= JST
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ----------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method: (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                               ROE-2ND_ORDER)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.75
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
 %
-% Marker(s) of the surface where geometrical based function will be evaluated
 GEO_MARKER= ( UPPER_SIDE, LOWER_SIDE, TIP )
-%
-% Description of the geometry to be analyzed (AIRFOIL, WING)
 GEO_DESCRIPTION= WING
-%
-% Coordinate of the stations to be analyzed
 GEO_LOCATION_STATIONS= (0.0, 0.2, 0.4, 0.6, 0.8)
-%
-% Geometrical bounds (Y coordinate) for the wing geometry analysis or
-% fuselage evaluation (X coordinate)
 GEO_BOUNDS= (0, 0.8)
-%
-% Plot loads and Cp distributions on each airfoil section
 GEO_PLOT_STATIONS= YES 
-%
-% Number of section cuts to make when calculating wing geometry
 GEO_NUMBER_STATIONS= 25
-%
-% Geometrical evaluation mode (FUNCTION, GRADIENT)
 GEO_MODE= FUNCTION
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------&
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 25
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_ONERAM6_inv.su2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
-% Mesh input file format (SU2)
 MESH_FORMAT= SU2
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 100
-%
diff --git a/TestCases/disc_adj_fea/configAD_fem.cfg b/TestCases/disc_adj_fea/configAD_fem.cfg
index 010a200d5bf..f5150911716 100644
--- a/TestCases/disc_adj_fea/configAD_fem.cfg
+++ b/TestCases/disc_adj_fea/configAD_fem.cfg
@@ -4,7 +4,7 @@
 % Author: R.Sanchez                                                            %
 % Institution: Imperial College London                                         %
 % Date: 2017.11.29                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 SOLVER= ELASTICITY
diff --git a/TestCases/disc_adj_fsi/Airfoil_2d/configFEA.cfg b/TestCases/disc_adj_fsi/Airfoil_2d/configFEA.cfg
index fab6a9064f7..625809928eb 100755
--- a/TestCases/disc_adj_fsi/Airfoil_2d/configFEA.cfg
+++ b/TestCases/disc_adj_fsi/Airfoil_2d/configFEA.cfg
@@ -1,6 +1,6 @@
 % Physics -------------------------------------------------------------- %
 SOLVER= ELASTICITY
-%
+
 % Optimization --------------------------------------------------------- %
 GRAD_OBJFUNC_FILENAME= of_grad.dat
 REFERENCE_NODE= 234
@@ -8,21 +8,21 @@ REFERENCE_NODE_DISPLACEMENT= (0.0, 0.0)
 REFERENCE_NODE_PENALTY= 1.0
 DESIGN_VARIABLE_FEA= YOUNG_MODULUS
 CUSTOM_OBJFUNC= '1e2 * (1e3 * REFERENCE_NODE + TOPOL_COMPLIANCE)'
-%
+
 % Solid properties ----------------------------------------------------- %
 MATERIAL_MODEL= NEO_HOOKEAN
 ELASTICITY_MODULUS= 7E9
 POISSON_RATIO= 0.35
 MATERIAL_DENSITY= 2700.0
-%
+
 % Boundary conditions -------------------------------------------------- %
 MARKER_CLAMPED= ( clamped )
 MARKER_FLUID_LOAD= ( pressure_side_s, suction_side_s )
-%
+
 % Solid numerics ------------------------------------------------------- %
 GEOMETRIC_CONDITIONS= LARGE_DEFORMATIONS
 FORMULATION_ELASTICITY_2D= PLANE_STRESS
-%
+
 % Linear solvers ------------------------------------------------------- %
 LINEAR_SOLVER= CONJUGATE_GRADIENT
 LINEAR_SOLVER_PREC= ILU
@@ -30,28 +30,25 @@ LINEAR_SOLVER_ERROR= 1E-8
 LINEAR_SOLVER_ITER= 1000
 DISCADJ_LIN_SOLVER= CONJUGATE_GRADIENT
 DISCADJ_LIN_PREC= ILU
-%
+
 % Convergence criteria ------------------------------------------------- %
 BGS_RELAXATION= FIXED_PARAMETER
 STAT_RELAX_PARAMETER= 1.0
 INNER_ITER= 11
 % Incremental load on to test that it does not break the discadj, it should only affect the direct solution.
 INCREMENTAL_LOAD= YES
-%
+
 % In\Out --------------------------------------------------------------- %
 MESH_FILENAME= mesh.su2
 MESH_FORMAT= SU2
-%
+
 RESTART_SOL= NO
 SOLUTION_FILENAME= solution_solid.dat
 SOLUTION_ADJ_FILENAME= adjoint_solid.dat
 RESTART_FILENAME= solution_solid.dat
 RESTART_ADJ_FILENAME= adjoint_solid.dat
-%
 TABULAR_FORMAT= CSV
 VOLUME_FILENAME= solid
 VOLUME_ADJ_FILENAME= adjoint_solid
-%
 SCREEN_WRT_FREQ_INNER= 10
 CONV_FILENAME= history
-
diff --git a/TestCases/disc_adj_fsi/Airfoil_2d/configFlow.cfg b/TestCases/disc_adj_fsi/Airfoil_2d/configFlow.cfg
index 16b9836e62d..845c4799654 100755
--- a/TestCases/disc_adj_fsi/Airfoil_2d/configFlow.cfg
+++ b/TestCases/disc_adj_fsi/Airfoil_2d/configFlow.cfg
@@ -1,11 +1,11 @@
 % Physics -------------------------------------------------------------- %
 SOLVER= EULER
 KIND_TURB_MODEL= NONE
-%
+
 % Optimization --------------------------------------------------------- %
 GRAD_OBJFUNC_FILENAME= of_grad.dat
 CUSTOM_OBJFUNC= '1e5 * DRAG'
-%
+
 % Compressible free-stream conditions ---------------------------------- %
 MACH_NUMBER= 0.8
 AOA= 2.5
@@ -14,20 +14,20 @@ FREESTREAM_OPTION= TEMPERATURE_FS
 FREESTREAM_PRESSURE= 101325.0
 FREESTREAM_TEMPERATURE= 273.15
 REYNOLDS_LENGTH= 0.5
-%
+
 % Fluid properties ----------------------------------------------------- %
 FLUID_MODEL= IDEAL_GAS
 GAMMA_VALUE= 1.4
 GAS_CONSTANT= 287.87
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
 MU_CONSTANT= 1.716E-5
-%
+
 % Boundary conditions -------------------------------------------------- %
 MARKER_FAR= ( farfield )
 MARKER_EULER= ( leading_edge, pressure_side, suction_side)
 MARKER_DEFORM_MESH= ( leading_edge, pressure_side, suction_side )
 DEFORM_MESH= YES
-%
+
 % Post processing and monitoring --------------------------------------- %
 REF_ORIGIN_MOMENT_X= -0.125
 REF_ORIGIN_MOMENT_Y= 0.00
@@ -37,17 +37,17 @@ REF_AREA= 0.5
 MARKER_PLOTTING= ( leading_edge, pressure_side, suction_side )
 MARKER_MONITORING= ( leading_edge, pressure_side, suction_side )
 MARKER_DESIGNING= ( leading_edge, pressure_side, suction_side )
-%
+
 % Common numerics settings --------------------------------------------- %
 REF_DIMENSIONALIZATION= DIMENSIONAL
 NUM_METHOD_GRAD= GREEN_GAUSS
 CFL_NUMBER= 500.0
-%
+
 % Flow numerics -------------------------------------------------------- %
 CONV_NUM_METHOD_FLOW= JST
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
-%
+
 % Linear solvers ------------------------------------------------------- %
 LINEAR_SOLVER= FGMRES
 LINEAR_SOLVER_PREC= ILU
@@ -65,7 +65,7 @@ DEFORM_LINEAR_SOLVER_ERROR= 1e-8
 DEFORM_LINEAR_SOLVER_ITER= 1000
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 DEFORM_POISSONS_RATIO= 1e6
-%
+
 % Convergence criteria ------------------------------------------------- %
 % interaction
 TIME_ITER= 1
@@ -75,23 +75,20 @@ STAT_RELAX_PARAMETER= 1.0
 INNER_ITER= 51
 CONV_STARTITER= 0
 CONV_RESIDUAL_MINVAL= -9
-%
+
 % In\Out --------------------------------------------------------------- %
 MESH_FILENAME= mesh.su2
 MESH_FORMAT= SU2
-%
+
 RESTART_SOL= NO
 SOLUTION_FILENAME= solution_fluid.dat
 SOLUTION_ADJ_FILENAME= adjoint_fluid.dat
 RESTART_FILENAME= solution_fluid.dat
 RESTART_ADJ_FILENAME= adjoint_fluid.dat
-%
 TABULAR_FORMAT= CSV
 VOLUME_FILENAME= fluid
 VOLUME_ADJ_FILENAME= adjoint_fluid
 SURFACE_FILENAME= surface_fluid
 SURFACE_ADJ_FILENAME= adjoint_surface_fluid
-%
 SCREEN_WRT_FREQ_INNER= 10
-CONV_FILENAME= history
-
+CONV_FILENAME= history
\ No newline at end of file
diff --git a/TestCases/disc_adj_fsi/configFEA.cfg b/TestCases/disc_adj_fsi/configFEA.cfg
index e463f9d1047..4d321bef7c7 100644
--- a/TestCases/disc_adj_fsi/configFEA.cfg
+++ b/TestCases/disc_adj_fsi/configFEA.cfg
@@ -4,7 +4,7 @@
 % Author: R.Sanchez                                                            %
 % Institution: Imperial College London                                         %
 % Date: 2017.11.29                                                             %
-% File Version 7.4.0 "Blackbird"                                                  %
+% File Version 7.5.0 "Blackbird"                                                  %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 SOLVER= ELASTICITY
diff --git a/TestCases/disc_adj_fsi/configFlow.cfg b/TestCases/disc_adj_fsi/configFlow.cfg
index b7554cec015..81c78d40b39 100644
--- a/TestCases/disc_adj_fsi/configFlow.cfg
+++ b/TestCases/disc_adj_fsi/configFlow.cfg
@@ -4,7 +4,7 @@
 % Author: R.Sanchez                                                            %
 % Institution: Imperial College London                                         %
 % Date: 2017.11.29                                                             %
-% File Version 7.4.0 "Blackbird"                                                   %
+% File Version 7.5.0 "Blackbird"                                                   %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 SOLVER= NAVIER_STOKES
diff --git a/TestCases/disc_adj_fsi/dyn_fsi/configFEA.cfg b/TestCases/disc_adj_fsi/dyn_fsi/configFEA.cfg
index c657a817932..7070a14d4a5 100644
--- a/TestCases/disc_adj_fsi/dyn_fsi/configFEA.cfg
+++ b/TestCases/disc_adj_fsi/dyn_fsi/configFEA.cfg
@@ -1,11 +1,11 @@
 % Physics -------------------------------------------------------------- %
 SOLVER= ELASTICITY
-%
+
 % Time settings --------------------------------------------------------- %
 TIME_DISCRE_FEA= NEWMARK_IMPLICIT
 NEWMARK_BETA=0.2601
 NEWMARK_GAMMA=0.52
-%
+
 % Optimization --------------------------------------------------------- %
 FEA_ADVANCED_MODE= YES
 FEA_FILENAME= element_properties.dat
@@ -14,21 +14,21 @@ REFERENCE_NODE= 234
 REFERENCE_NODE_DISPLACEMENT= (0.0, 0.0)
 REFERENCE_NODE_PENALTY= 1.0
 DESIGN_VARIABLE_FEA= YOUNG_MODULUS
-%
+
 % Solid properties ----------------------------------------------------- %
 MATERIAL_MODEL= NEO_HOOKEAN
 ELASTICITY_MODULUS= 7E8
 POISSON_RATIO= 0.35
 MATERIAL_DENSITY= 2700.0
-%
+
 % Boundary conditions -------------------------------------------------- %
 MARKER_CLAMPED= ( clamped )
 MARKER_FLUID_LOAD= ( pressure_side_s, suction_side_s )
-%
+
 % Solid numerics ------------------------------------------------------- %
 GEOMETRIC_CONDITIONS= LARGE_DEFORMATIONS
 FORMULATION_ELASTICITY_2D= PLANE_STRESS
-%
+
 % Linear solvers ------------------------------------------------------- %
 LINEAR_SOLVER= CONJUGATE_GRADIENT
 LINEAR_SOLVER_PREC= ILU
@@ -36,29 +36,27 @@ LINEAR_SOLVER_ERROR= 1E-8
 LINEAR_SOLVER_ITER= 1000
 DISCADJ_LIN_SOLVER= CONJUGATE_GRADIENT
 DISCADJ_LIN_PREC= ILU
-%
+
 % Convergence criteria ------------------------------------------------- %
 BGS_RELAXATION= FIXED_PARAMETER
 STAT_RELAX_PARAMETER= 1.0
 INNER_ITER= 11
 % Incremental load on to test that it does not break the discadj, it should only affect the direct solution.
 INCREMENTAL_LOAD= NO
-%
+
 % In\Out --------------------------------------------------------------- %
 MESH_FILENAME= mesh.su2
 MESH_FORMAT= SU2
-%
+
 RESTART_SOL= NO
 SOLUTION_FILENAME= solution_solid.dat
 SOLUTION_ADJ_FILENAME= adjoint_solid.dat
 OUTPUT_WRT_FREQ= 1
 RESTART_FILENAME= solution_solid.dat
 RESTART_ADJ_FILENAME= adjoint_solid.dat
-%
 TABULAR_FORMAT= CSV
 VOLUME_FILENAME= solid
 VOLUME_ADJ_FILENAME= adjoint_solid
-%
 SCREEN_WRT_FREQ_INNER= 10
 CONV_FILENAME= history
 HISTORY_OUTPUT= ITER, RMS_RES, STRUCT_COEFF, TAVG_STRUCT_COEFF
diff --git a/TestCases/disc_adj_fsi/dyn_fsi/configFlow.cfg b/TestCases/disc_adj_fsi/dyn_fsi/configFlow.cfg
index 04cf4c83c6e..fbb5552efc8 100644
--- a/TestCases/disc_adj_fsi/dyn_fsi/configFlow.cfg
+++ b/TestCases/disc_adj_fsi/dyn_fsi/configFlow.cfg
@@ -1,13 +1,13 @@
 % Physics -------------------------------------------------------------- %
 SOLVER= EULER
 KIND_TURB_MODEL= NONE
-%
+
 % Time settings --------------------------------------------------------- %
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-%
+
 % Optimization --------------------------------------------------------- %
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
+
 % Compressible free-stream conditions ---------------------------------- %
 MACH_NUMBER= 0.8
 AOA= 5.0
@@ -16,20 +16,20 @@ FREESTREAM_OPTION= TEMPERATURE_FS
 FREESTREAM_PRESSURE= 101325.0
 FREESTREAM_TEMPERATURE= 273.15
 REYNOLDS_LENGTH= 0.5
-%
+
 % Fluid properties ----------------------------------------------------- %
 FLUID_MODEL= IDEAL_GAS
 GAMMA_VALUE= 1.4
 GAS_CONSTANT= 287.87
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
 MU_CONSTANT= 1.716E-5
-%
+
 % Boundary conditions -------------------------------------------------- %
 MARKER_FAR= ( farfield )
 MARKER_EULER= ( leading_edge, pressure_side, suction_side)
 MARKER_DEFORM_MESH= ( leading_edge, pressure_side, suction_side )
 DEFORM_MESH= YES
-%
+
 % Post processing and monitoring --------------------------------------- %
 REF_ORIGIN_MOMENT_X= -0.125
 REF_ORIGIN_MOMENT_Y= 0.00
@@ -39,17 +39,17 @@ REF_AREA= 0.5
 MARKER_PLOTTING= ( leading_edge, pressure_side, suction_side )
 MARKER_MONITORING= ( leading_edge, pressure_side, suction_side )
 MARKER_DESIGNING= ( leading_edge, pressure_side, suction_side )
-%
+
 % Common numerics settings --------------------------------------------- %
 REF_DIMENSIONALIZATION= DIMENSIONAL
 NUM_METHOD_GRAD= GREEN_GAUSS
 CFL_NUMBER= 1000.0
-%
+
 % Flow numerics -------------------------------------------------------- %
 CONV_NUM_METHOD_FLOW= JST
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
-%
+
 % Linear solvers ------------------------------------------------------- %
 LINEAR_SOLVER= BCGSTAB
 LINEAR_SOLVER_PREC= ILU
@@ -58,7 +58,6 @@ LINEAR_SOLVER_ITER= 25
 DISCADJ_LIN_SOLVER= SMOOTHER
 DISCADJ_LIN_PREC= ILU
 LINEAR_SOLVER_SMOOTHER_RELAXATION= 0.7
-% Multigrid
 MGLEVEL= 0
 NEWTON_KRYLOV= YES
 QUASI_NEWTON_NUM_SAMPLES= 999
@@ -69,7 +68,7 @@ DEFORM_LINEAR_SOLVER_ERROR= 1e-8
 DEFORM_LINEAR_SOLVER_ITER= 1000
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 DEFORM_POISSONS_RATIO= 1e6
-%
+
 % Convergence criteria ------------------------------------------------- %
 % interaction
 BGS_RELAXATION= FIXED_PARAMETER
@@ -78,7 +77,7 @@ STAT_RELAX_PARAMETER= 1.0
 INNER_ITER= 31
 CONV_STARTITER= 0
 CONV_RESIDUAL_MINVAL= -7
-%
+
 % In\Out --------------------------------------------------------------- %
 MESH_FILENAME= mesh.su2
 MESH_FORMAT= SU2
@@ -89,13 +88,11 @@ SOLUTION_ADJ_FILENAME= adjoint_fluid.dat
 OUTPUT_WRT_FREQ= 1
 RESTART_FILENAME= solution_fluid.dat
 RESTART_ADJ_FILENAME= adjoint_fluid.dat
-%
 TABULAR_FORMAT= CSV
 VOLUME_FILENAME= fluid
 VOLUME_ADJ_FILENAME= adjoint_fluid
 SURFACE_FILENAME= surface_fluid
 SURFACE_ADJ_FILENAME= adjoint_surface_fluid
-%
 SCREEN_WRT_FREQ_INNER= 10
 CONV_FILENAME= history
 HISTORY_OUTPUT= ITER, RMS_RES, AERO_COEFF, TAVG_AERO_COEFF
diff --git a/TestCases/disc_adj_heat/disc_adj_heat.cfg b/TestCases/disc_adj_heat/disc_adj_heat.cfg
index 928fdcfa76b..78df9c1bd58 100644
--- a/TestCases/disc_adj_heat/disc_adj_heat.cfg
+++ b/TestCases/disc_adj_heat/disc_adj_heat.cfg
@@ -6,7 +6,7 @@
 % Author: Ole Burghardt                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: November 26th, 2018                                                     %
-% File Version 7.4.0 "Blackbird"                                                   %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -27,9 +27,6 @@ SYSTEM_MEASUREMENTS= SI
 
 OBJECTIVE_FUNCTION= TOTAL_HEATFLUX
 
-%DIRECT_DIFF=DESIGN_VARIABLES
-
-
 ITER = 11
 
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
@@ -116,7 +113,6 @@ JST_SENSOR_COEFF= ( 0.5, 0.05 )
 
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
-
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
@@ -148,7 +144,6 @@ CONV_CAUCHY_ELEMS= 100
 
 CONV_CAUCHY_EPS= 1E-10
 
-
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 
 DV_KIND= FFD_CONTROL_POINT_2D
@@ -219,6 +214,4 @@ SURFACE_ADJ_FILENAME= surface_adjoint
 
 OUTPUT_WRT_FREQ= 1
 
-
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_ADJ_PRESSURE, RMS_ADJ_NU_TILDE, RMS_ADJ_HEAT, SENS_VEL_IN, SENS_PRESS_OUT)
diff --git a/TestCases/disc_adj_incomp_euler/naca0012/incomp_NACA0012_disc.cfg b/TestCases/disc_adj_incomp_euler/naca0012/incomp_NACA0012_disc.cfg
index c39e08442fa..112157c7428 100644
--- a/TestCases/disc_adj_incomp_euler/naca0012/incomp_NACA0012_disc.cfg
+++ b/TestCases/disc_adj_incomp_euler/naca0012/incomp_NACA0012_disc.cfg
@@ -4,237 +4,102 @@
 % Case description: Subsonic incompressible inviscid flow around a NACA0012    %
 % Author: Thomas D. Economon                                                   %
 % Date: 2018.10.30                                                             %
-% File Version 7.4.0 "Blackbird"                                                  %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= INC_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DISCRETE_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
 
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
-% Initial density for incompressible flows
-% (1.2886 kg/m^3 by default (air), 998.2 Kg/m^3 (water))
 INC_DENSITY_INIT= 1.2886
-%
-% Initial velocity for incompressible flows (1.0,0,0 m/s by default)
 INC_VELOCITY_INIT= ( 33.1588, 1.15793, 0.0 )
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
-NUM_METHOD_GRAD= GREEN_GAUSS
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
+NUM_METHOD_GRAD= GREEN_GAUSS
 CFL_NUMBER= 8.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 501
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
+
 OBJECTIVE_FUNCTION= LIFT
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT = 1.0
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 1.0
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 1.0
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.001
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.0, 0.01 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION, 
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION)
-DV_KIND= HICKS_HENNE
 %
-% Marker of the surface in which we are going apply the shape deformation
+DV_KIND= HICKS_HENNE
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( 1st digit, 2nd and 3rd digit )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= ( 1, 0.5 )
-%
-% Value of the shape deformation deformation
 DV_VALUE= 0.01
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -15
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA0012_inv.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-%
-% Screen output
 SCREEN_OUTPUT = (INNER_ITER, RMS_ADJ_PRESSURE, RMS_ADJ_VELOCITY-X, SENS_PRESS, SENS_AOA)
-%
 OUTPUT_FILES=(RESTART_ASCII)
+
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% List of design variables (Design variables are separated by semicolons)
-% From 1 to 99, Geometrycal design variables.
-%  - HICKS_HENNE ( 1, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%  - NACA_4DIGITS ( 4, Scale | Mark. List |  1st digit, 2nd digit, 3rd and 4th digit )
-%  - ROTATION ( 6, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-% From 100 to 199, Flow solver design variables.
-%  - MACH_NUMBER ( 101, Scale | Markers List )
-%  - AOA ( 102, Scale | Markers List )
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 ); ( 30, 1.0 | airfoil | 0, 0.20 ); ( 30, 1.0 | airfoil | 0, 0.25 ); ( 30, 1.0 | airfoil | 0, 0.30 ); ( 30, 1.0 | airfoil | 0, 0.35 ); ( 30, 1.0 | airfoil | 0, 0.40 ); ( 30, 1.0 | airfoil | 0, 0.45 ); ( 30, 1.0 | airfoil | 0, 0.50 ); ( 30, 1.0 | airfoil | 0, 0.55 ); ( 30, 1.0 | airfoil | 0, 0.60 ); ( 30, 1.0 | airfoil | 0, 0.65 ); ( 30, 1.0 | airfoil | 0, 0.70 ); ( 30, 1.0 | airfoil | 0, 0.75 ); ( 30, 1.0 | airfoil | 0, 0.80 ); ( 30, 1.0 | airfoil | 0, 0.85 ); ( 30, 1.0 | airfoil | 0, 0.90 ); ( 30, 1.0 | airfoil | 0, 0.95 ); ( 30, 1.0 | airfoil | 1, 0.05 ); ( 30, 1.0 | airfoil | 1, 0.10 ); ( 30, 1.0 | airfoil | 1, 0.15 ); ( 30, 1.0 | airfoil | 1, 0.20 ); ( 30, 1.0 | airfoil | 1, 0.25 ); ( 30, 1.0 | airfoil | 1, 0.30 ); ( 30, 1.0 | airfoil | 1, 0.35 ); ( 30, 1.0 | airfoil | 1, 0.40 ); ( 30, 1.0 | airfoil | 1, 0.45 ); ( 30, 1.0 | airfoil | 1, 0.50 ); ( 30, 1.0 | airfoil | 1, 0.55 ); ( 30, 1.0 | airfoil | 1, 0.60 ); ( 30, 1.0 | airfoil | 1, 0.65 ); ( 30, 1.0 | airfoil | 1, 0.70 ); ( 30, 1.0 | airfoil | 1, 0.75 ); ( 30, 1.0 | airfoil | 1, 0.80 ); ( 30, 1.0 | airfoil | 1, 0.85 ); ( 30, 1.0 | airfoil | 1, 0.90 ); ( 30, 1.0 | airfoil | 1, 0.95 )
diff --git a/TestCases/disc_adj_incomp_navierstokes/cylinder/heated_cylinder.cfg b/TestCases/disc_adj_incomp_navierstokes/cylinder/heated_cylinder.cfg
index cbaf640dbef..7fd8587c5c9 100644
--- a/TestCases/disc_adj_incomp_navierstokes/cylinder/heated_cylinder.cfg
+++ b/TestCases/disc_adj_incomp_navierstokes/cylinder/heated_cylinder.cfg
@@ -4,457 +4,160 @@
 % Case description: Steady incompressible laminar flow past a heated cylinder  %
 % Author: Thomas D. Economon                                                   %
 % Date: 2018.06.10                                                             %
-% File Version 7.4.0 "Blackbird"                                                  %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                           
 SOLVER= INC_NAVIER_STOKES
-%
-% If Navier-Stokes, kind of turbulent model (NONE, SA)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DISCRETE_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
-% Density model within the incompressible flow solver.
-% Options are CONSTANT (default), BOUSSINESQ, or VARIABLE. If VARIABLE,
-% an appropriate fluid model must be selected.
 INC_DENSITY_MODEL= VARIABLE
-%
-% Solve the energy equation in the incompressible flow solver
 INC_ENERGY_EQUATION = YES
-%
-% Initial density for incompressible flows (1.2886 kg/m^3 by default)
 INC_DENSITY_INIT= 0.000210322
-%
-% Initial velocity for incompressible flows (1.0,0,0 m/s by default)
 INC_VELOCITY_INIT= ( 3.40297, 0.0, 0.0 )
-%
-% Initial temperature for incompressible flows that include the
-% energy equation (288.15 K by default). Value is ignored if
-% INC_ENERGY_EQUATION is false.
 INC_TEMPERATURE_INIT= 288.15
 
 % ---- IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
-% Fluid model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS,
-%              CONSTANT_DENSITY, INC_IDEAL_GAS)
 FLUID_MODEL= INC_IDEAL_GAS
-%
-% Specific heat at constant pressure, Cp (1004.703 J/kg*K (air)).
-% Incompressible fluids with energy eqn. only (CONSTANT_DENSITY, INC_IDEAL_GAS).
 SPECIFIC_HEAT_CP= 1004.703
-%
-% Molecular weight for an incompressible ideal gas (28.96 g/mol (air) default)
-% Incompressible fluids with energy eqn. only (CONSTANT_DENSITY, INC_IDEAL_GAS).
 MOLECULAR_WEIGHT= 28.96
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= SUTHERLAND
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.7893e-05
-%
-% Sutherland Viscosity Ref (1.716E-5 default value for AIR SI)
 MU_REF= 1.716E-5
-%
-% Sutherland Temperature Ref (273.15 K default value for AIR SI)
 MU_T_REF= 273.15
-%
-% Sutherland constant (110.4 default value for AIR SI)
 SUTHERLAND_CONSTANT= 110.4
 
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
-% Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL).
 CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
-%
-% Molecular Thermal Conductivity that would be constant (0.0257 by default)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.0257
-%
-% Laminar Prandtl number (0.72 (air), only for CONSTANT_PRANDTL)
 PRANDTL_LAM= 0.72
-%
-% Turbulent Prandtl number (0.9 (air), only for CONSTANT_PRANDTL)
 PRANDTL_TURB= 0.90
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_ISOTHERMAL= ( cylinder, 1000.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( cylinder )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( cylinder )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1000.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 10.0, 10000.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 1000
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= TOTAL_HEATFLUX
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT = 1.0
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.8
-
 % ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
 %
-% Coefficient for the Venkat's limiter (upwind scheme). A larger values decrease
-%             the extent of limiting, values approaching zero cause
-%             lower-order approximation to the solution (0.05 by default)
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Coefficient for the adjoint sharp edges limiter (3.0 by default).
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
-%
-% 1st order artificial dissipation coefficients for
-%     the Lax–Friedrichs method ( 0.15 by default )
 LAX_SENSOR_COEFF= 0.15
-%
-% 2nd and 4th order artificial dissipation coefficients for
-%     the JST method ( 0.5, 0.02 by default )
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% 1st order artificial dissipation coefficients for
-%     the adjoint Lax–Friedrichs method ( 0.15 by default )
 ADJ_LAX_SENSOR_COEFF= 0.15
-%
-% 2nd, and 4th order artificial dissipation coefficients for
-%     the adjoint JST method ( 0.5, 0.02 by default )
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= FDS
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_cylinder_lam_ffd.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-%
-% Screen output 
 SCREEN_OUTPUT= (INNER_ITER, RMS_ADJ_PRESSURE, RMS_ADJ_TEMPERATURE, SENS_PRESS, SENS_AOA)
+
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (NO_DEFORMATION, TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING, FFD_NACELLE
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS, FFD_TWIST
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D, FFD_TWIST_2D,
-%                      HICKS_HENNE, SURFACE_BUMP)
 DV_KIND= FFD_CONTROL_POINT_2D
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( cylinder )
-%
-% Parameters of the shape deformation
-% - NO_DEFORMATION ( 1.0 )
-% - TRANSLATION ( x_Disp, y_Disp, z_Disp ), as a unit vector
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - SCALE ( 1.0 )
-% - ANGLE_OF_ATTACK ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_NACELLE ( FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Disp, phi_Disp )
-% - FFD_GULL ( FFD_BoxTag, j_Ind )
-% - FFD_ANGLE_OF_ATTACK ( FFD_BoxTag, 1.0 )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_TWIST ( FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - FFD_TWIST_2D ( FFD_BoxTag, x_Orig, y_Orig )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - SURFACE_BUMP ( x_Start, x_End, x_Loc )
 DV_PARAM= ( MAIN_BOX, 12, 1, 0.0, 1.0 )
-%
-% Value of the shape deformation
 DV_VALUE= 0.1
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 1000
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-15
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 500
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (MAIN_BOX, -0.1, -0.6, 0.0, 1.1, -0.6, 0.0, 1.1, 0.6, 0.0, -0.1, 0.6, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= ( 24, 1, 0)
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= 2ND_DERIVATIVE
 
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
 %
-% Marker(s) of the surface where geometrical based function will be evaluated
 GEO_MARKER= ( cylinder )
-%
-% Description of the geometry to be analyzed (AIRFOIL, WING, FUSELAGE, NACELLE)
 GEO_DESCRIPTION= AIRFOIL
-%
-% Coordinate of the stations to be analyzed
 GEO_LOCATION_STATIONS= (0.0, 0.5, 1.0)
-%
-% Geometrical bounds (Y coordinate) for the wing geometry analysis or
-% fuselage evaluation (X coordinate), or nacelle evaluation (theta coordinate)
 GEO_BOUNDS= (1.5, 3.5)
-%
-% Location of the nacelle axis (point coordinates and axis)
-%GEO_NACELLE_LOCATION= (0.0, 0.0, 0.0, 1.0, 0.0, 0.0)
-%
-% Plot loads and Cp distributions on each airfoil section
 GEO_PLOT_STATIONS= NO
-%
-% Number of section cuts to make when calculating wing geometry
 GEO_NUMBER_STATIONS= 25
-%
-% Geometrical evaluation mode (FUNCTION, GRADIENT)
 GEO_MODE= FUNCTION
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Definition of multipoint design problems, this option should be combined with the
-% the prefix MULTIPOINT in the objective function or constraint (e.g. MULTIPOINT_DRAG, MULTIPOINT_LIFT, etc.)
 MULTIPOINT_MACH_NUMBER= (0.79, 0.8, 0.81)
 MULTIPOINT_AOA= (1.25, 1.25, 1.25)
 MULTIPOINT_SIDESLIP_ANGLE= (0.0, 0.0, 0.0)
@@ -464,21 +167,7 @@ MULTIPOINT_FREESTREAM_PRESSURE= (101325.0, 101325.0, 101325.0)
 MULTIPOINT_FREESTREAM_TEMPERATURE= (288.15, 288.15, 288.15)
 MULTIPOINT_WEIGHT= (0.33333, 0.33333, 0.33333)
 %
-% Optimization objective function with scaling factor, separated by semicolons.
-% To include quadratic penalty function: use OPT_CONSTRAINT option syntax within the OPT_OBJECTIVE list.
-% ex= Objective * Scale
-%OPT_OBJECTIVE= TOTAL_HEATFLUX * 1e-5
 OPT_OBJECTIVE= DRAG * 1.0
-%
-% Optimization constraint functions with pushing factors (affects its value, not the gradient  in the python scripts), separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
-%OPT_CONSTRAINT= ( DRAG < 1.68 ) * 1.0; ( AIRFOIL_CHORD < 1.01 ) * 1.0
-%OPT_CONSTRAINT= ( AIRFOIL_CHORD < 1.01 ) * 1.0; ( AIRFOIL_AREA > 0.785422 ) * 1.0
-%OPT_CONSTRAINT= ( AIRFOIL_CHORD < 1.01 ) * 1.0; ( AIRFOIL_THICKNESS > 0.12 ) * 1.0
-%OPT_CONSTRAINT= ( AIRFOIL_THICKNESS > 0.12 ) * 1e-1
-%OPT_CONSTRAINT= ( AIRFOIL_THICKNESS > 1.0 ) * 1e-1
-%OPT_CONSTRAINT= ( AIRFOIL_AREA > 0.785422 ) * 1e-1
-%OPT_CONSTRAINT= NONE
 OPT_CONSTRAINT= ( DRAG < 2.06 ) * 1.0
 %
 % NACA 0012 Area: 0.0816925 m^2, Thickness: 0.120011 m
@@ -487,33 +176,12 @@ OPT_CONSTRAINT= ( DRAG < 2.06 ) * 1.0
 % Station 1. ZCoord: 0 m, Area: 0.785422 m^2, Thickness: 1 m, 
 % Chord: 1 m, LE radius: 2 1/m, ToC: 1, Alpha: 0.9 deg.
 %
-%
-% Factor to reduce the norm of the gradient (affects the objective function and gradient in the python scripts)
-% In general, a norm of the gradient ~1E-6 is desired.
-OPT_GRADIENT_FACTOR= 1.0
-%
-% Factor to relax or accelerate the optimizer convergence (affects the line search in SU2_DEF)
-% In general, surface deformations of 0.01'' or 0.0001m are desirable
 OPT_RELAX_FACTOR= 1.0
-%
-% Maximum number of iterations
 OPT_ITERATIONS= 100
-%
-% Requested accuracy
 OPT_ACCURACY= 1E-10
 %
-% Optimization bound (bounds the line search in SU2_DEF)
 OPT_LINE_SEARCH_BOUND= 1E6
-%
-% Upper bound for each design variable (bound in the python optimizer)
 OPT_BOUND_UPPER= 0.5
-%
-% Lower bound for each design variable (bound in the python optimizer)
 OPT_BOUND_LOWER= -0.5
-%
-% Finite difference step size for python scripts (0.001 default, recommended
-%                                                                                                 0.001 x REF_LENGTH)
 FIN_DIFF_STEP = 1e-3
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 19, 1.0 | cylinder | MAIN_BOX, 0, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 1, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 2, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 3, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 4, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 5, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 6, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 7, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 8, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 9, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 10, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 11, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 12, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 13, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 14, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 15, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 16, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 17, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 18, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 19, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 20, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 21, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 22, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 23, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 24, 0, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 0, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 1, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 2, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 3, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 4, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 5, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 6, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 7, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 8, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 9, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 10, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 11, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 12, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 13, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 14, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 15, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 16, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 17, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 18, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 19, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 20, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 21, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 22, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 23, 1, 0.0, 1.0 ); ( 19, 1.0 | cylinder | MAIN_BOX, 24, 1, 0.0, 1.0 )
diff --git a/TestCases/disc_adj_incomp_rans/naca0012/turb_naca0012_sa.cfg b/TestCases/disc_adj_incomp_rans/naca0012/turb_naca0012_sa.cfg
index adc4a731aac..c9a9e489edc 100755
--- a/TestCases/disc_adj_incomp_rans/naca0012/turb_naca0012_sa.cfg
+++ b/TestCases/disc_adj_incomp_rans/naca0012/turb_naca0012_sa.cfg
@@ -5,323 +5,118 @@
 %                   http://turbmodels.larc.nasa.gov/naca0012_val_sa.html       %
 % Author: Thomas D. Economon & Francisco Palacios                              %
 % Date: 2018.06.10                                                             %
-% File Version 7.4.0 "Blackbird"                                                  %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= INC_RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DISCRETE_ADJOINT
-%
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
+
 % -------------------- INCOMPRESSIBLE FREE-STREAM DEFINITION ------------------%
 %
-% Free-stream density (1.2886 Kg/m^3 (air), 998.2 Kg/m^3 (water))
 INC_DENSITY_INIT= 2.13163
-%
-% Free-stream velocity (m/s)
-% AoA 0.0 deg
-%INC_VELOCITY_INIT= ( 52.1572, 0.0, 0.0 )
 % AoA 10 deg
 INC_VELOCITY_INIT= ( 51.36481493540834, 9.0570027322096198, 0.0 )
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.853e-05
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 25.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 25.0, 10000.0 )
-%
-% Maximum Delta Time in local time stepping simulations
 MAX_DELTA_TIME= 1E6
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 99999
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= DRAG
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT = 1.0
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-10
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.8
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= FDS
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= NONE
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.0, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION,
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE,
-%                      FFD_ROTATION)
-DV_KIND= HICKS_HENNE
 %
-% Marker of the surface in which we are going apply the shape deformation
+DV_KIND= HICKS_HENNE
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation
-%       - HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-%       - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-%       - PARABOLIC ( 1st digit, 2nd and 3rd digit )
-%       - DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-%       - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= ( 1, 0.5 )
-%
-% Value of the shape deformation deformation
 DV_VALUE= 0.01
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -14
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= n0012_225-65.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow_sa.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-%
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_ADJ_PRESSURE, RMS_ADJ_NU_TILDE, SENS_PRESS, SENS_AOA)
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 ); ( 30, 1.0 | airfoil | 0, 0.20 ); ( 30, 1.0 | airfoil | 0, 0.25 ); ( 30, 1.0 | airfoil | 0, 0.30 ); ( 30, 1.0 | airfoil | 0, 0.35 ); ( 30, 1.0 | airfoil | 0, 0.40 ); ( 30, 1.0 | airfoil | 0, 0.45 ); ( 30, 1.0 | airfoil | 0, 0.50 ); ( 30, 1.0 | airfoil | 0, 0.55 ); ( 30, 1.0 | airfoil | 0, 0.60 ); ( 30, 1.0 | airfoil | 0, 0.65 ); ( 30, 1.0 | airfoil | 0, 0.70 ); ( 30, 1.0 | airfoil | 0, 0.75 ); ( 30, 1.0 | airfoil | 0, 0.80 ); ( 30, 1.0 | airfoil | 0, 0.85 ); ( 30, 1.0 | airfoil | 0, 0.90 ); ( 30, 1.0 | airfoil | 0, 0.95 ); ( 30, 1.0 | airfoil | 1, 0.05 ); ( 30, 1.0 | airfoil | 1, 0.10 ); ( 30, 1.0 | airfoil | 1, 0.15 ); ( 30, 1.0 | airfoil | 1, 0.20 ); ( 30, 1.0 | airfoil | 1, 0.25 ); ( 30, 1.0 | airfoil | 1, 0.30 ); ( 30, 1.0 | airfoil | 1, 0.35 ); ( 30, 1.0 | airfoil | 1, 0.40 ); ( 30, 1.0 | airfoil | 1, 0.45 ); ( 30, 1.0 | airfoil | 1, 0.50 ); ( 30, 1.0 | airfoil | 1, 0.55 ); ( 30, 1.0 | airfoil | 1, 0.60 ); ( 30, 1.0 | airfoil | 1, 0.65 ); ( 30, 1.0 | airfoil | 1, 0.70 ); ( 30, 1.0 | airfoil | 1, 0.75 ); ( 30, 1.0 | airfoil | 1, 0.80 ); ( 30, 1.0 | airfoil | 1, 0.85 ); ( 30, 1.0 | airfoil | 1, 0.90 ); ( 30, 1.0 | airfoil | 1, 0.95 )
diff --git a/TestCases/disc_adj_incomp_rans/naca0012/turb_naca0012_sst.cfg b/TestCases/disc_adj_incomp_rans/naca0012/turb_naca0012_sst.cfg
index 92bab13866e..b3172cd2ed1 100755
--- a/TestCases/disc_adj_incomp_rans/naca0012/turb_naca0012_sst.cfg
+++ b/TestCases/disc_adj_incomp_rans/naca0012/turb_naca0012_sst.cfg
@@ -5,322 +5,118 @@
 %                   http://turbmodels.larc.nasa.gov/naca0012_val_sst.html      %
 % Author: Thomas D. Economon & Francisco Palacios                              %
 % Date: 2018.06.10                                                             %
-% File Version 7.4.0 "Blackbird"                                                  %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= INC_RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SST
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DISCRETE_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % -------------------- INCOMPRESSIBLE FREE-STREAM DEFINITION ------------------%
 %
-% Free-stream density (1.2886 Kg/m^3 (air), 998.2 Kg/m^3 (water))
 INC_DENSITY_INIT= 2.13163
-%
-% Free-stream velocity (m/s)
-% AoA 0.0 deg
-%INC_VELOCITY_INIT= ( 52.1572, 0.0, 0.0 )
 % AoA 10 deg
 INC_VELOCITY_INIT= ( 51.36481493540834, 9.0570027322096198, 0.0 )
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.853e-05
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 25.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 25.0, 10000.0 )
-%
-% Maximum Delta Time in local time stepping simulations
 MAX_DELTA_TIME= 1E6
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 99999
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= DRAG
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT = 1.0
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-10
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.8
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= FDS
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= NONE
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.0, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION,
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE,
-%                      FFD_ROTATION)
-DV_KIND= HICKS_HENNE
 %
-% Marker of the surface in which we are going apply the shape deformation
+DV_KIND= HICKS_HENNE
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation
-%       - HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-%       - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-%       - PARABOLIC ( 1st digit, 2nd and 3rd digit )
-%       - DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-%       - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= ( 1, 0.5 )
-%
-% Value of the shape deformation deformation
 DV_VALUE= 0.01
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -14
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= n0012_225-65.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow_sst.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-%
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_ADJ_PRESSURE, RMS_ADJ_TKE, RMS_ADJ_DISSIPATION, SENS_PRESS, SENS_AOA)
+
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 ); ( 30, 1.0 | airfoil | 0, 0.20 ); ( 30, 1.0 | airfoil | 0, 0.25 ); ( 30, 1.0 | airfoil | 0, 0.30 ); ( 30, 1.0 | airfoil | 0, 0.35 ); ( 30, 1.0 | airfoil | 0, 0.40 ); ( 30, 1.0 | airfoil | 0, 0.45 ); ( 30, 1.0 | airfoil | 0, 0.50 ); ( 30, 1.0 | airfoil | 0, 0.55 ); ( 30, 1.0 | airfoil | 0, 0.60 ); ( 30, 1.0 | airfoil | 0, 0.65 ); ( 30, 1.0 | airfoil | 0, 0.70 ); ( 30, 1.0 | airfoil | 0, 0.75 ); ( 30, 1.0 | airfoil | 0, 0.80 ); ( 30, 1.0 | airfoil | 0, 0.85 ); ( 30, 1.0 | airfoil | 0, 0.90 ); ( 30, 1.0 | airfoil | 0, 0.95 ); ( 30, 1.0 | airfoil | 1, 0.05 ); ( 30, 1.0 | airfoil | 1, 0.10 ); ( 30, 1.0 | airfoil | 1, 0.15 ); ( 30, 1.0 | airfoil | 1, 0.20 ); ( 30, 1.0 | airfoil | 1, 0.25 ); ( 30, 1.0 | airfoil | 1, 0.30 ); ( 30, 1.0 | airfoil | 1, 0.35 ); ( 30, 1.0 | airfoil | 1, 0.40 ); ( 30, 1.0 | airfoil | 1, 0.45 ); ( 30, 1.0 | airfoil | 1, 0.50 ); ( 30, 1.0 | airfoil | 1, 0.55 ); ( 30, 1.0 | airfoil | 1, 0.60 ); ( 30, 1.0 | airfoil | 1, 0.65 ); ( 30, 1.0 | airfoil | 1, 0.70 ); ( 30, 1.0 | airfoil | 1, 0.75 ); ( 30, 1.0 | airfoil | 1, 0.80 ); ( 30, 1.0 | airfoil | 1, 0.85 ); ( 30, 1.0 | airfoil | 1, 0.90 ); ( 30, 1.0 | airfoil | 1, 0.95 )
diff --git a/TestCases/disc_adj_rans/cylinder/cylinder.cfg b/TestCases/disc_adj_rans/cylinder/cylinder.cfg
index 547dacdc116..b1e82ab0372 100644
--- a/TestCases/disc_adj_rans/cylinder/cylinder.cfg
+++ b/TestCases/disc_adj_rans/cylinder/cylinder.cfg
@@ -5,373 +5,137 @@
 % Author: Tim Albring                                                          %
 % Institution: TU Kaiserslautern                                               %
 % Date: 2016.06.14                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= NAVIER_STOKES
-%
-% If Navier-Stokes, kind of turbulent model (NONE, SA)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DISCRETE_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
 
 TIME_DOMAIN = YES
 TIME_ITER = 10
-%
+
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER, TIME_SPECTRAL)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-%
-% Time Step for dual time stepping simulations (s)
 TIME_STEP= 0.0015
-%
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 3.75
 % 2500 iterations - 3.75
 % 3500 iterations - 5.25
 % 5000 iterations - 7.50
-%
-% Number of internal iterations (dual time method)
 INNER_ITER= 30
-%
-% Direct iteration to start the adjoint solver
 UNST_ADJOINT_ITER= 10
-%
-% Number of time-steps to average (counted from the back)
 ITER_AVERAGE_OBJ= 10
-%
+
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.1
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 100.0
-%
-% Reynolds length (in meters)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( Cylinder, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( Farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( Cylinder )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( Cylinder )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Objective function
 OBJECTIVE_FUNCTION=DRAG
+
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.7
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.7
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 1.0
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-5
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_cylinder.su2
-%
-% Mesh input file format (SU2, CGNS NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency for physical time steps (dual time)
 OUTPUT_WRT_FREQ= 1
-%
-%
-% Screen output
 SCREEN_OUTPUT= (TIME_ITER, INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_PRESS, SENS_AOA)
-%
 OUTPUT_FILES= (RESTART_ASCII)
+
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING,
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC, NACA_4DIGITS, AIRFOIL)
 DV_KIND= HICKS_HENNE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( Cylinder )
-%
-% Parameters of the shape deformation
-% - TRANSLATION ( x_Disp, y_Disp, z_Disp ), as a unit vector
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - SCALE ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - PARABOLIC ( Center, Thickness )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - AIRFOIL ( 1.0 )
 DV_PARAM= ( 0, 0.5 )
-%
-% Value of the shape deformation
 DV_VALUE= 1.0
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 1000
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
+
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.01
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= NONE 
-%
-% Maximum number of iterations
 OPT_ITERATIONS= 100
-%
-% Requested accuracy
 OPT_ACCURACY= 1E-6
-%
-% Upper bound for each design variable
 OPT_BOUND_UPPER= 0.1
-%
-% Lower bound for each design variable
 OPT_BOUND_LOWER= -0.1
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 30, 1.0 | Cylinder | 0, 0.05 ); ( 30, 1.0 | Cylinder | 0, 0.10 ); ( 30, 1.0 | Cylinder | 0, 0.15 ); ( 30, 1.0 | Cylinder | 0, 0.20 ); ( 30, 1.0 | Cylinder | 0, 0.25 ); ( 30, 1.0 | Cylinder | 0, 0.30 ); ( 30, 1.0 | Cylinder | 0, 0.35 ); ( 30, 1.0 | Cylinder | 0, 0.40 ); ( 30, 1.0 | Cylinder | 0, 0.45 ); ( 30, 1.0 | Cylinder | 0, 0.50 ); ( 30, 1.0 | Cylinder | 0, 0.55 ); ( 30, 1.0 | Cylinder | 0, 0.60 ); ( 30, 1.0 | Cylinder | 0, 0.65 ); ( 30, 1.0 | Cylinder | 0, 0.70 ); ( 30, 1.0 | Cylinder | 0, 0.75 ); ( 30, 1.0 | Cylinder | 0, 0.80 ); ( 30, 1.0 | Cylinder | 0, 0.85 ); ( 30, 1.0 | Cylinder | 0, 0.90 ); ( 30, 1.0 | Cylinder | 0, 0.95 ); ( 30, 1.0 | Cylinder | 1, 0.05 ); ( 30, 1.0 | Cylinder | 1, 0.10 ); ( 30, 1.0 | Cylinder | 1, 0.15 ); ( 30, 1.0 | Cylinder | 1, 0.20 ); ( 30, 1.0 | Cylinder | 1, 0.25 ); ( 30, 1.0 | Cylinder | 1, 0.30 ); ( 30, 1.0 | Cylinder | 1, 0.35 ); ( 30, 1.0 | Cylinder | 1, 0.40 ); ( 30, 1.0 | Cylinder | 1, 0.45 ); ( 30, 1.0 | Cylinder | 1, 0.50 ); ( 30, 1.0 | Cylinder | 1, 0.55 ); ( 30, 1.0 | Cylinder | 1, 0.60 ); ( 30, 1.0 | Cylinder | 1, 0.65 ); ( 30, 1.0 | Cylinder | 1, 0.70 ); ( 30, 1.0 | Cylinder | 1, 0.75 ); ( 30, 1.0 | Cylinder | 1, 0.80 ); ( 30, 1.0 | Cylinder | 1, 0.85 ); ( 30, 1.0 | Cylinder | 1, 0.90 ); ( 30, 1.0 | Cylinder | 1, 0.95 )
-%
diff --git a/TestCases/disc_adj_rans/cylinder/cylinder_Windowing.cfg b/TestCases/disc_adj_rans/cylinder/cylinder_Windowing.cfg
index 62090efc4e2..b2278676f04 100644
--- a/TestCases/disc_adj_rans/cylinder/cylinder_Windowing.cfg
+++ b/TestCases/disc_adj_rans/cylinder/cylinder_Windowing.cfg
@@ -5,336 +5,132 @@
 % Author: Tim Albring                                                          %
 % Institution: TU Kaiserslautern                                               %
 % Date: 2016.06.14                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= NAVIER_STOKES
-%
-% If Navier-Stokes, kind of turbulent model (NONE, SA)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
 DIRECT_DIFF = DESIGN_VARIABLES
 
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= YES
 
 TIME_DOMAIN = YES
 TIME_ITER = 10
-%
+
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER, TIME_SPECTRAL)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-%
-% Time Step for dual time stepping simulations (s)
 TIME_STEP= 0.0015
-%
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 3.75
-%
-% Number of internal iterations (dual time method)
 INNER_ITER= 30
-%
-% Direct iteration to start the adjoint solver
 UNST_ADJOINT_ITER= 10
-%
-% Number of time-steps to average (counted from the back)
 ITER_AVERAGE_OBJ= 10
-%
-%%  Windowed output time averaging
-% Time iteration to start the windowed time average in a direct run
 WINDOW_START_ITER = 1
-%
-% Window used for reverse sweep and direct run. Options (SQUARE, HANN, HANN_SQUARE, BUMP) Square is default. 
 WINDOW_FUNCTION = HANN
-%
+
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.1
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 100.0
-%
-% Reynolds length (in meters)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( Cylinder, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( Farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( Cylinder )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( Cylinder )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
+
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
-%
+
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 1.0
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-5
-%
-%% Time convergence monitoring
 WINDOW_CAUCHY_CRIT = YES
-%
-% List of time convergence fields 
 CONV_WINDOW_FIELD = (TAVG_DRAG, TAVG_LIFT)
-%
-% Time Convergence Monitoring starts at Iteration WINDOW_START_ITER + CONV_WINDOW_STARTITER
 CONV_WINDOW_STARTITER = 0
-%
-% Epsilon to control the series convergence
 CONV_WINDOW_CAUCHY_EPS = 1
-%
-% Number of elements to apply the criteria
 CONV_WINDOW_CAUCHY_ELEMS = 2
-%
+
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_cylinder.su2
-%
-% Mesh input file format (SU2, CGNS NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Screen output
 SCREEN_OUTPUT= (TIME_ITER, INNER_ITER, DRAG, LIFT, TAVG_DRAG, TAVG_LIFT,  CAUCHY_TAVG_DRAG)
 HISTORY_OUTPUT = (ITER, TAVG_AERO_COEFF, AERO_COEFF)
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING,
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC, NACA_4DIGITS, AIRFOIL)
 DV_KIND= HICKS_HENNE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( Cylinder )
-%
-% Parameters of the shape deformation
-% - TRANSLATION ( x_Disp, y_Disp, z_Disp ), as a unit vector
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - SCALE ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - PARABOLIC ( Center, Thickness )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - AIRFOIL ( 1.0 )
 DV_PARAM= ( 0, 0.5 )
-%
-% Value of the shape deformation
 DV_VALUE= 1.0
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 1000
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
+
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 30, 1.0 | Cylinder | 0, 0.05 ); ( 30, 1.0 | Cylinder | 0, 0.10 ); ( 30, 1.0 | Cylinder | 0, 0.15 ); ( 30, 1.0 | Cylinder | 0, 0.20 ); ( 30, 1.0 | Cylinder | 0, 0.25 ); ( 30, 1.0 | Cylinder | 0, 0.30 ); ( 30, 1.0 | Cylinder | 0, 0.35 ); ( 30, 1.0 | Cylinder | 0, 0.40 ); ( 30, 1.0 | Cylinder | 0, 0.45 ); ( 30, 1.0 | Cylinder | 0, 0.50 ); ( 30, 1.0 | Cylinder | 0, 0.55 ); ( 30, 1.0 | Cylinder | 0, 0.60 ); ( 30, 1.0 | Cylinder | 0, 0.65 ); ( 30, 1.0 | Cylinder | 0, 0.70 ); ( 30, 1.0 | Cylinder | 0, 0.75 ); ( 30, 1.0 | Cylinder | 0, 0.80 ); ( 30, 1.0 | Cylinder | 0, 0.85 ); ( 30, 1.0 | Cylinder | 0, 0.90 ); ( 30, 1.0 | Cylinder | 0, 0.95 ); ( 30, 1.0 | Cylinder | 1, 0.05 ); ( 30, 1.0 | Cylinder | 1, 0.10 ); ( 30, 1.0 | Cylinder | 1, 0.15 ); ( 30, 1.0 | Cylinder | 1, 0.20 ); ( 30, 1.0 | Cylinder | 1, 0.25 ); ( 30, 1.0 | Cylinder | 1, 0.30 ); ( 30, 1.0 | Cylinder | 1, 0.35 ); ( 30, 1.0 | Cylinder | 1, 0.40 ); ( 30, 1.0 | Cylinder | 1, 0.45 ); ( 30, 1.0 | Cylinder | 1, 0.50 ); ( 30, 1.0 | Cylinder | 1, 0.55 ); ( 30, 1.0 | Cylinder | 1, 0.60 ); ( 30, 1.0 | Cylinder | 1, 0.65 ); ( 30, 1.0 | Cylinder | 1, 0.70 ); ( 30, 1.0 | Cylinder | 1, 0.75 ); ( 30, 1.0 | Cylinder | 1, 0.80 ); ( 30, 1.0 | Cylinder | 1, 0.85 ); ( 30, 1.0 | Cylinder | 1, 0.90 ); ( 30, 1.0 | Cylinder | 1, 0.95 )
-%
diff --git a/TestCases/disc_adj_rans/cylinder/cylinder_Windowing_AD.cfg b/TestCases/disc_adj_rans/cylinder/cylinder_Windowing_AD.cfg
index 52a55632fff..94291557ed8 100644
--- a/TestCases/disc_adj_rans/cylinder/cylinder_Windowing_AD.cfg
+++ b/TestCases/disc_adj_rans/cylinder/cylinder_Windowing_AD.cfg
@@ -5,259 +5,120 @@
 % Author: Tim Albring                                                          %
 % Institution: TU Kaiserslautern                                               %
 % Date: 2016.06.14                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= NAVIER_STOKES
-%
-% If Navier-Stokes, kind of turbulent model (NONE, SA)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DISCRETE_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
 
 TIME_DOMAIN = YES
 TIME_ITER = 10
-%
+
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER, TIME_SPECTRAL)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-%
-% Time Step for dual time stepping simulations (s)
 TIME_STEP= 0.0015
-%
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 3.75
-%
-% Number of internal iterations (dual time method)
 INNER_ITER= 30
-%
-% Direct iteration to start the adjoint solver
 UNST_ADJOINT_ITER= 10
-%
-% Number of time-steps to average (counted from the back)
 ITER_AVERAGE_OBJ= 5
 %
 %%  Windowed output time averaging
-% Time iteration to start the windowed time average in a direct run
 WINDOW_START_ITER = 5
 %
 % Window used for reverse sweep and direct run. Options (SQUARE, HANN, HANN_SQUARE, BUMP) Square is default. 
 WINDOW_FUNCTION = HANN
-%
+
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.1
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 100.0
-%
-% Reynolds length (in meters)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( Cylinder, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( Farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( Cylinder )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( Cylinder )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Objective function
 OBJECTIVE_FUNCTION=DRAG
+
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
-%
+
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 1.0
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-5
-%
-%% Time convergence monitoring
 WINDOW_CAUCHY_CRIT = YES
-%
-% List of time convergence fields 
 CONV_WINDOW_FIELD = TAVG_DRAG
-%
-% Time Convergence Monitoring starts at Iteration WINDOW_START_ITER + CONV_WINDOW_STARTITER
 CONV_WINDOW_STARTITER = 0
-%
-% Epsilon to control the series convergence
 CONV_WINDOW_CAUCHY_EPS = 1
-%
-% Number of elements to apply the criteria
 CONV_WINDOW_CAUCHY_ELEMS = 2
-%
+
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_cylinder.su2
-%
-% Mesh input file format (SU2, CGNS NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
-% Screen output
 SCREEN_OUTPUT= (TIME_ITER, INNER_ITER, RMS_ADJ_DENSITY)
 HISTORY_OUTPUT = (ITER, TAVG_AERO_COEFF, D_TAVG_AERO_COEFF, AERO_COEFF)
 OUTPUT_FILES = (RESTART_ASCII)
-%
-%
+
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 1000
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
+
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 30, 1.0 | Cylinder | 0, 0.05 ); ( 30, 1.0 | Cylinder | 0, 0.10 ); ( 30, 1.0 | Cylinder | 0, 0.15 ); ( 30, 1.0 | Cylinder | 0, 0.20 ); ( 30, 1.0 | Cylinder | 0, 0.25 ); ( 30, 1.0 | Cylinder | 0, 0.30 ); ( 30, 1.0 | Cylinder | 0, 0.35 ); ( 30, 1.0 | Cylinder | 0, 0.40 ); ( 30, 1.0 | Cylinder | 0, 0.45 ); ( 30, 1.0 | Cylinder | 0, 0.50 ); ( 30, 1.0 | Cylinder | 0, 0.55 ); ( 30, 1.0 | Cylinder | 0, 0.60 ); ( 30, 1.0 | Cylinder | 0, 0.65 ); ( 30, 1.0 | Cylinder | 0, 0.70 ); ( 30, 1.0 | Cylinder | 0, 0.75 ); ( 30, 1.0 | Cylinder | 0, 0.80 ); ( 30, 1.0 | Cylinder | 0, 0.85 ); ( 30, 1.0 | Cylinder | 0, 0.90 ); ( 30, 1.0 | Cylinder | 0, 0.95 ); ( 30, 1.0 | Cylinder | 1, 0.05 ); ( 30, 1.0 | Cylinder | 1, 0.10 ); ( 30, 1.0 | Cylinder | 1, 0.15 ); ( 30, 1.0 | Cylinder | 1, 0.20 ); ( 30, 1.0 | Cylinder | 1, 0.25 ); ( 30, 1.0 | Cylinder | 1, 0.30 ); ( 30, 1.0 | Cylinder | 1, 0.35 ); ( 30, 1.0 | Cylinder | 1, 0.40 ); ( 30, 1.0 | Cylinder | 1, 0.45 ); ( 30, 1.0 | Cylinder | 1, 0.50 ); ( 30, 1.0 | Cylinder | 1, 0.55 ); ( 30, 1.0 | Cylinder | 1, 0.60 ); ( 30, 1.0 | Cylinder | 1, 0.65 ); ( 30, 1.0 | Cylinder | 1, 0.70 ); ( 30, 1.0 | Cylinder | 1, 0.75 ); ( 30, 1.0 | Cylinder | 1, 0.80 ); ( 30, 1.0 | Cylinder | 1, 0.85 ); ( 30, 1.0 | Cylinder | 1, 0.90 ); ( 30, 1.0 | Cylinder | 1, 0.95 )
-%
diff --git a/TestCases/disc_adj_rans/cylinder_DT_1ST/cylinder.cfg b/TestCases/disc_adj_rans/cylinder_DT_1ST/cylinder.cfg
index 79e61349f97..07d40ece13b 100644
--- a/TestCases/disc_adj_rans/cylinder_DT_1ST/cylinder.cfg
+++ b/TestCases/disc_adj_rans/cylinder_DT_1ST/cylinder.cfg
@@ -5,374 +5,141 @@
 % Author: Tim Albring                                                          %
 % Institution: TU Kaiserslautern                                               %
 % Date: 2016.06.14                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= NAVIER_STOKES
-%
-% If Navier-Stokes, kind of turbulent model (NONE, SA)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DISCRETE_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
 
 TIME_DOMAIN = YES
 TIME_ITER = 10
-%
+
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER, TIME_SPECTRAL)
 TIME_MARCHING= DUAL_TIME_STEPPING-1ST_ORDER
-%
-% Time Step for dual time stepping simulations (s)
 TIME_STEP= 0.0015
-%
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 3.75
 % 2500 iterations - 3.75
 % 3500 iterations - 5.25
 % 5000 iterations - 7.50
-%
-% Number of internal iterations (dual time method)
 INNER_ITER= 30
-%
-% Direct iteration to start the adjoint solver
 UNST_ADJOINT_ITER= 10
 %
 % Number of time-steps to average (counted from the back)
 ITER_AVERAGE_OBJ= 10
-%
+
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.1
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 100.0
-%
-% Reynolds length (in meters)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( Cylinder, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( Farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( Cylinder )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( Cylinder )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-%
-% Objective function
 OBJECTIVE_FUNCTION=DRAG
+
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= ILU
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.7
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.7
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 1.0
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
 %
 % Slope limiter (NONE, VENKATAKRISHNAN, BARTH)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-5
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_cylinder.su2
-%
-% Mesh input file format (SU2, CGNS NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= solution_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= solution_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency for physical time steps (dual time)
 OUTPUT_WRT_FREQ= 1
-%
-%
-% Screen output
 SCREEN_OUTPUT= (TIME_ITER, INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_PRESS, SENS_AOA)
-%
 OUTPUT_FILES= (RESTART_ASCII)
+
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING,
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC, NACA_4DIGITS, AIRFOIL)
 DV_KIND= HICKS_HENNE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( Cylinder )
-%
-% Parameters of the shape deformation
-% - TRANSLATION ( x_Disp, y_Disp, z_Disp ), as a unit vector
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - SCALE ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - PARABOLIC ( Center, Thickness )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - AIRFOIL ( 1.0 )
 DV_PARAM= ( 0, 0.5 )
-%
-% Value of the shape deformation
 DV_VALUE= 1.0
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 1000
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
+
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.01
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= NONE 
-%
-% Maximum number of iterations
 OPT_ITERATIONS= 100
-%
-% Requested accuracy
 OPT_ACCURACY= 1E-6
-%
-% Upper bound for each design variable
 OPT_BOUND_UPPER= 0.1
-%
-% Lower bound for each design variable
 OPT_BOUND_LOWER= -0.1
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 30, 1.0 | Cylinder | 0, 0.05 ); ( 30, 1.0 | Cylinder | 0, 0.10 ); ( 30, 1.0 | Cylinder | 0, 0.15 ); ( 30, 1.0 | Cylinder | 0, 0.20 ); ( 30, 1.0 | Cylinder | 0, 0.25 ); ( 30, 1.0 | Cylinder | 0, 0.30 ); ( 30, 1.0 | Cylinder | 0, 0.35 ); ( 30, 1.0 | Cylinder | 0, 0.40 ); ( 30, 1.0 | Cylinder | 0, 0.45 ); ( 30, 1.0 | Cylinder | 0, 0.50 ); ( 30, 1.0 | Cylinder | 0, 0.55 ); ( 30, 1.0 | Cylinder | 0, 0.60 ); ( 30, 1.0 | Cylinder | 0, 0.65 ); ( 30, 1.0 | Cylinder | 0, 0.70 ); ( 30, 1.0 | Cylinder | 0, 0.75 ); ( 30, 1.0 | Cylinder | 0, 0.80 ); ( 30, 1.0 | Cylinder | 0, 0.85 ); ( 30, 1.0 | Cylinder | 0, 0.90 ); ( 30, 1.0 | Cylinder | 0, 0.95 ); ( 30, 1.0 | Cylinder | 1, 0.05 ); ( 30, 1.0 | Cylinder | 1, 0.10 ); ( 30, 1.0 | Cylinder | 1, 0.15 ); ( 30, 1.0 | Cylinder | 1, 0.20 ); ( 30, 1.0 | Cylinder | 1, 0.25 ); ( 30, 1.0 | Cylinder | 1, 0.30 ); ( 30, 1.0 | Cylinder | 1, 0.35 ); ( 30, 1.0 | Cylinder | 1, 0.40 ); ( 30, 1.0 | Cylinder | 1, 0.45 ); ( 30, 1.0 | Cylinder | 1, 0.50 ); ( 30, 1.0 | Cylinder | 1, 0.55 ); ( 30, 1.0 | Cylinder | 1, 0.60 ); ( 30, 1.0 | Cylinder | 1, 0.65 ); ( 30, 1.0 | Cylinder | 1, 0.70 ); ( 30, 1.0 | Cylinder | 1, 0.75 ); ( 30, 1.0 | Cylinder | 1, 0.80 ); ( 30, 1.0 | Cylinder | 1, 0.85 ); ( 30, 1.0 | Cylinder | 1, 0.90 ); ( 30, 1.0 | Cylinder | 1, 0.95 )
-%
diff --git a/TestCases/disc_adj_rans/naca0012/naca0012.cfg b/TestCases/disc_adj_rans/naca0012/naca0012.cfg
index 744204d570d..1a4132396b0 100644
--- a/TestCases/disc_adj_rans/naca0012/naca0012.cfg
+++ b/TestCases/disc_adj_rans/naca0012/naca0012.cfg
@@ -5,7 +5,7 @@
 % Author: Steffen Schotthöfer                                                  %
 % Institution: TU Kaiserslautern                                               %
 % Date: Mar 16, 2017                                                           %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -15,192 +15,118 @@
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES, NS_PLASMA)                    
 SOLVER= RANS
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DISCRETE_ADJOINT
-% Objective function
 OBJECTIVE_FUNCTION=DRAG
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-% Restart iteration
 RESTART_ITER = 10
 %
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Time Domain
 TIME_DOMAIN = YES
-% Unsteady simulation
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-% Time Step for dual time stepping simulations (s)
 TIME_STEP= 5e-4
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 105000
-%Maximum Number of physical time steps used for primal and ajoint run.
 TIME_ITER= 15
-% Number of internal iterations (dual time method)
 INNER_ITER= 2
-%Number of iterations to average the objective 
 ITER_AVERAGE_OBJ =  3      
-%Iteration number to begin the reverse time integration in the direct solver for the unsteady adjoint.
 UNST_ADJOINT_ITER = 15
-% Start iteration for windowing
 WINDOW_START_ITER = 12 
-% Window used for reverse sweep. Options (SQUARE, HANN, HANN_SQUARE, BUMP)
 WINDOW_FUNCTION = HANN_SQUARE
 %
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.3
-% Angle of attack (degrees, only for compressible flows)
 AOA= 17.0
-% De-Dimensionalization
 REF_DIMENSIONALIZATION = DIMENSIONAL
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 293.0
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 1e+6
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 %
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 %
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker
 MARKER_HEATFLUX= ( AIRFOIL, 0.0)
-% Farfield boundary marker
 MARKER_FAR= ( FARFIELD)
-% Internal boundary marker(s) e.g. no boundary condition 
 MARKER_INTERNAL= ( FWH1 )
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= (  AIRFOIL )
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= (AIRFOIL)
 %
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 20.0
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 %
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method 
 CONV_NUM_METHOD_FLOW= JST
-% 1st, 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= (  0.5, 0.01 )
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-% Muscl flow for turbulent simulation
 MUSCL_TURB= NO
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 %
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Field to apply Cauchy Criterion to
 CONV_FIELD= REL_RMS_DENSITY
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -9
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 10
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-5
 %
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Output settings
 HISTORY_WRT_FREQ_INNER=0
 SCREEN_WRT_FREQ_INNER =1
 SCREEN_OUTPUT=(INNER_ITER, TIME_ITER, RMS_ADJ_DENSITY, RMS_DENSITY, , REL_RMS_DENSITY,REL_RMS_ADJ_DENSITY, DRAG, TAVG_DRAG)
 HISTORY_OUTPUT=(ITER, RMS_RES, AERO_COEFF, TAVG_AERO_COEFF, ADJ_AERO_COEFF)
-%
-% Mesh input file
 MESH_FILENAME= naca0012_FFD.su2
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= restart_adj.dat
 TABULAR_FORMAT= CSV
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= 0_history
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1
 %
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation 
 DV_KIND= FFD_CONTROL_POINT_2D
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( AIRFOIL )
-% Parameters of the shape deformation
 DV_PARAM= ( AIRFOIL_BOX, 0.0, 0.0, 1.0, 0.0)
-% Value of the shape deformation
 DV_VALUE= 0.01
-% Surface deformation input filename (SURFACE_FILE DV only)
 DV_FILENAME= mesh_motion.dat
 %
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 1000
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-% Factor to multiply smallest cell volume for deform tolerance (0.001 default)
 DEFORM_LINEAR_SOLVER_ERROR =  1E-6
-% Type of element stiffness imposed for FEA mesh deformation
 DEFORM_STIFFNESS_TYPE= WALL_DISTANCE
-% Optimization objective function with scaling factor
 OPT_OBJECTIVE= DRAG * 1.0
 OPT_GRADIENT_FACTOR= 0.1
 OPT_RELAX_FACTOR= 1
 OPT_BOUND_UPPER= 0.05
 OPT_BOUND_LOWER= -0.05
-% Optimization constraint functions with scaling factors, separated by semicolons
 OPT_CONSTRAINT= ( LIFT > 0.96 ) * 1.0
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 0, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 0, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 0, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 0, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 0, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 0, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 0, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 0, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 0, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 0, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 0, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 1, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 1, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 1, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 1, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 1, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 1, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 1, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 1, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 1, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 1, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 1, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 2, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 2, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 2, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 2, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 2, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 2, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 2, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 2, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 2, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 2, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 2, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 3, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 3, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 3, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 3, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 3, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 3, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 3, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 3, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 3, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 3, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 3, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 4, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 4, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 4, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 4, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 4, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 4, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 4, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 4, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 4, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 4, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 4, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 5, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 5, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 5, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 5, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 5, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 5, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 5, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 5, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 5, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 5, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 5, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 6, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 6, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 6, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 6, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 6, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 6, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 6, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 6, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 6, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 6, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 6, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 7, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 7, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 7, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 7, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 7, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 7, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 7, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 7, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 7, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 7, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 7, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 8, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 8, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 8, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 8, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 8, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 8, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 8, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 8, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 8, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 8, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 8, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 9, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 9, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 9, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 9, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 9, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 9, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 9, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 9, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 9, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 9, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 9, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 10, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 10, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 10, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 10, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 10, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 10, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 10, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 10, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 10, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 10, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 10, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 2, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 2, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 2, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 2, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 2, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 2, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 2, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 2, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 2, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 2, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 2, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 3, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 3, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 3, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 3, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 3, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 3, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 3, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 3, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 3, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 3, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 3, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 4, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 4, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 4, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 4, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 4, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 4, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 4, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 4, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 4, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 4, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 4, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 5, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 5, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 5, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 5, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 5, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 5, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 5, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 5, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 5, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 5, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 5, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 6, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 6, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 6, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 6, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 6, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 6, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 6, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 6, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 6, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 6, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 6, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 7, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 7, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 7, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 7, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 7, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 7, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 7, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 7, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 7, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 7, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 7, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 8, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 8, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 8, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 8, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 8, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 8, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 8, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 8, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 8, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 8, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 8, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 9, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 9, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 9, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 9, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 9, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 9, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 9, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 9, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 9, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 9, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 9, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 10, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 10, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 10, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 10, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 10, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 10, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 10, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 10, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 10, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 10, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 10, 0.0, 1.0 )
-%
diff --git a/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sa.cfg b/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sa.cfg
index ffa1ff84f2d..5429a5e2bc0 100644
--- a/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sa.cfg
+++ b/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sa.cfg
@@ -6,235 +6,101 @@
 % Author: Francisco Palacios	                                               %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations                             
 SOLVER= RANS
-%
-% Specify turbulence model
 KIND_TURB_MODEL= SA
 SA_OPTIONS= NEGATIVE, EXPERIMENTAL
-%
-% Mathematical problem
 MATH_PROBLEM= DISCRETE_ADJOINT
-%
-% Restart solution
 RESTART_SOL= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.15
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 10.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.0E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Max Delta time
 MAX_DELTA_TIME= 1E10
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 ITER= 99999
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-10
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 1, 1, 1, 1, 1 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_TURB= NONE
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= n0012_113-33.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow_sa.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1000
-%
-%
-% Screen output
-SCREEN_OUTPUT = (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_NU_TILDE, SENS_PRESS, SENS_AOA RMS_DENSITY RMS_NU_TILDE LIFT DRAG LINSOL_ITER LINSOL_RESIDUAL LINSOL_ITER_TURB LINSOL_RESIDUAL_TURB)
-
+SCREEN_OUTPUT = (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_NU_TILDE, SENS_PRESS, SENS_AOA RMS_DENSITY RMS_NU_TILDE LIFT DRAG LINSOL_ITER LINSOL_RESIDUAL LINSOL_ITER_TURB LINSOL_RESIDUAL_TURB)
\ No newline at end of file
diff --git a/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sst.cfg b/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sst.cfg
index ae362b476ec..af09bdb7fff 100644
--- a/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sst.cfg
+++ b/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sst.cfg
@@ -6,236 +6,100 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               TNE2_EULER, TNE2_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                             
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SST
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DISCRETE_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.15
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 10.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.0E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Max Delta time
 MAX_DELTA_TIME= 1E10
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= YES
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 0.1, 1.2, 1.0, 100.0 )
-%
-% Number of total iterations
 ITER= 10000
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-10
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 1, 1, 1, 1, 1 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= n0012_113-33.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow_sst.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1000
-%
-%
-% Screen output
-SCREEN_OUTPUT = (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_TKE, SENS_PRESS, SENS_AOA RMS_DENSITY RMS_TKE LIFT DRAG)
-
+SCREEN_OUTPUT = (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_TKE, SENS_PRESS, SENS_AOA RMS_DENSITY RMS_TKE LIFT DRAG)
\ No newline at end of file
diff --git a/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg b/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg
index 931279f1128..2337d51dafd 100644
--- a/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg
+++ b/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg
@@ -5,412 +5,184 @@
 % Author: S. Vitale                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: 2017.03.01                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-%
-%
+
+
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)                         
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SST)
 KIND_TURB_MODEL= SST
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED)
 MATH_PROBLEM= DISCRETE_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% number of zones (needed for python scripts)
 NZONES= 1
-%
 SINGLEZONE_DRIVER=NO
-%
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.1
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 70.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 13.0E+5
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE=  592.295
-%
-% Free-stream temperature (1.2886 Kg/m3 by default)
 FREESTREAM_DENSITY= 1.7418
-%
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-% Free-stream Turbulence Intensity
 FREESTREAM_TURBULENCEINTENSITY = 0.03
-%
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
-%
-%Init option to choose between Reynolds (default) or thermodynamics quantities for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
-%
+
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
-%
-%
+
 % ------------------------------ EQUATION OF STATE ----------------------------%
 %
-% Different gas model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS)
 FLUID_MODEL= PR_GAS
-%
-% Ratio of specific heats (1.4 default and the value is hardcoded
-%                          for the model STANDARD_AIR)
 GAMMA_VALUE= 1.0165
-%
-% Specific gas constant (287.058 J/kg*K default and this value is hardcoded 
-%                        for the model STANDARD_AIR)
 GAS_CONSTANT= 35.23
-%
-% Critical Temperature (273.15 K by default)
 CRITICAL_TEMPERATURE= 564.1
-%
-% Critical Pressure (101325.0 N/m^2 by default)
 CRITICAL_PRESSURE= 1415000.0
-%
-% Acentri factor (0.035 (air))
 ACENTRIC_FACTOR= 0.529
-%
-%
+
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.3764E-5
-%
-% Sutherland Viscosity Ref (1.716E-5 default value for AIR SI)
 MU_REF= 1.716E-5
-%
-% Sutherland Temperature Ref (273.15 K default value for AIR SI)
 MU_T_REF= 273.15
-%
-% Sutherland constant (110.4 default value for AIR SI)
 SUTHERLAND_CONSTANT= 110.4
-%
-%
+
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
-% Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL).
 CONDUCTIVITY_MODEL= CONSTANT_CONDUCTIVITY
-%
-% Molecular Thermal Conductivity that would be constant (0.0257 by default)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.047280
-%
-%
+
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= (airfoil, 0.0)
-%
-% Periodic boundary marker(s) (NONE = no marker)
-% Format: ( periodic marker, donor marker, rot_cen_x, rot_cen_y, rot_cen_z, rot_angle_x-axis, rot_angle_y-axis, rot_angle_z-axis, translation_x, translation_y, translation_z)
 MARKER_PERIODIC= ( periodic_1, periodic_2, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.05749995, 0.0 )
-%
-%
+
 %-------- INFLOW/OUTFLOW BOUNDARY CONDITION SPECIFIC FOR TURBOMACHINERY --------%
 %
-% Inflow and Outflow markers must be specified, for each blade (zone), following the natural groth of the machine (i.e, from the first blade to the last)
 MARKER_TURBOMACHINERY= (inflow, outflow)
-%
-% Giles boundary condition for inflow, outfolw and mixing-plane
-% Format inlet:  ( marker, TOTAL_CONDITIONS_PT, Total Pressure , Total Temperature, Flow dir-norm, Flow dir-tang, Flow dir-span, under-relax-avg, under-relax-fourier)
-% Format outlet: ( marker, STATIC_PRESSURE, Static Pressure value, -, -, -, -, under-relax-avg, under-relax-fourier)
-% Format mixing-plane in and out: ( marker, MIXING_IN or MIXING_OUT, -, -, -, -, -, -, under-relax-avg, under-relax-fourier)
 MARKER_GILES= (inflow, TOTAL_CONDITIONS_PT, 13.8686E+05, 592.295, 1.0, 0.0, 0.0, 1.0, 1.0, outflow, STATIC_PRESSURE, 9.00E+05, 0.0, 0.0, 0.0, 0.0, 1.0, 1.0)
-%
-%YES Non reflectivity activated, NO the Giles BC behaves as a normal 1D characteristic-based BC
 SPATIAL_FOURIER= YES
+
 %---------------------------- TURBOMACHINERY SIMULATION -----------------------------%
 %
-% Specify kind of architecture (AXIAL, CENTRIPETAL, CENTRIFUGAL, CENTRIPETAL_AXIAL)
 TURBOMACHINERY_KIND = AXIAL
-%
-% Specify ramp option for Outlet pressure (YES, NO) default NO
 RAMP_OUTLET_PRESSURE= NO
-%
-% Parameters of the outlet pressure ramp (starting outlet pressure, updating-iteration-frequency, total number of iteration for the ramp)
 RAMP_OUTLET_PRESSURE_COEFF= (700000.0, 10.0, 500)
-%
-% Specify Kind of average process for linearizing the Navier-Stokes equation at inflow and outflow BC included mixing-plane
-% (ALGEBRAIC, AREA, MASSSFLUX, MIXEDOUT) default AREA 
 AVERAGE_PROCESS_KIND= MIXEDOUT
-%
-% Specify Kind of average process for computing turbomachienry performance parameters
-% (ALGEBRAIC, AREA, MASSSFLUX, MIXEDOUT) default AREA
 PERFORMANCE_AVERAGE_PROCESS_KIND= MIXEDOUT
-%
-%Parameters of the Newton method for the MIXEDOUT average algorithm (under relaxation factor, tollerance, max number of iterations) 
 MIXEDOUT_COEFF= (1.0, 1.0E-05, 15)
-%
-% Limit of Mach number below which the mixedout algorithm is substituted with a AREA average algorithm
 AVERAGE_MACH_LIMIT= 0.03
-%
-%
+
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING= (airfoil)
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING= (airfoil)
-%
-%
+
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 40.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value, CFL max value )
 CFL_ADAPT_PARAM= ( 1.3, 1.2, 1.0, 10.0)
-%
-%
+
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
-%
-%
+
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% ----------- NOT WORKING WITH PERIODIC BOUNDARY CONDITIONS !!!!! --------------%
-%
+% ----------- NOT WORKING WITH PERIODIC BOUNDARY CONDITIONS !!!!! -------------%
 %
+
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
-%
-%
+
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Entropy fix coefficient (0.0 implies no entropy fixing, 1.0 implies scalar artificial dissipation, 0.001 default)
 ENTROPY_FIX_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
-%
-% Relaxation coefficient
-%
-%
+
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
-%
-%
+
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (NO_DEFORMATION, TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING, FFD_NACELLE
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS, FFD_TWIST
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D, FFD_TWIST_2D,
-%                      HICKS_HENNE, SURFACE_BUMP)
 DV_KIND= FFD_SETTING
-% 
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation
 DV_PARAM= ( MAIN_BOX, 3.0, 4.0, 0.0, 0.0)
-%
-% Value of the shape deformation
 DV_VALUE= 0.01
-%
-%
+
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
-DEFORM_LINEAR_SOLVER_ITER= 250
-%
 %
+DEFORM_LINEAR_SOLVER_ITER= 250
+
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-10
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 500
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (MAIN_BOX, -0.007280, 0.012690, 0.0, 0.024666, 0.02200, 0.0, 0.04785, -0.04985, 0.0, 0.01709, -0.05911, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= ( 4 , 4 , 0 )
-%
-% Surface grid continuity at the intersection with the faces of the FFD boxes.
-% To keep a particular level of surface continuity, SU2 automatically freezes the right
-% number of control point planes (NO_DERIVATIVE, 1ST_DERIVATIVE, 2ND_DERIVATIVE, USER_INPUT)
 FFD_CONTINUITY= 2ND_DERIVATIVE
-%
-%
+
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 19, 1.0 | airfoil | MAIN_BOX, 0, 0, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 1, 0, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 2, 0, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 3, 0, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 4, 0, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 0, 1, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 1, 1, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 2, 1, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 3, 1, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 4, 1, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 0, 2, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 1, 2, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 2, 2, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 3, 2, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 4, 2, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 0, 3, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 1, 3, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 2, 3, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 3, 3, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 4, 3, 0.0, 0.0 )
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= ( FLOW_ANGLE_OUT < -74.0 ) * 0.001
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= ENTROPY_GENERATION* 0.0001
-%
-% Maximum number of iterations
 OPT_ITERATIONS= 19
-%
-% Requested accuracy
 OPT_ACCURACY= 1E-10
-%
-%
+
 % --------------------- OBJECTIVE FUNCTION DEFINITION -----------------------%
 %
-% Objective function in optimization problem 
 OBJECTIVE_FUNCTION= ENTROPY_GENERATION
-%
-%
+
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Number of total iterations
 ITER= 2001
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
-%
-%
+
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_stator_turb.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= su2mesh_per_optimal.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 500
-%
-%
 SCREEN_OUTPUT=(INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_TKE)
diff --git a/TestCases/euler/CRM/inv_CRM_JST.cfg b/TestCases/euler/CRM/inv_CRM_JST.cfg
index 5aaecad073d..8a321cf5a94 100644
--- a/TestCases/euler/CRM/inv_CRM_JST.cfg
+++ b/TestCases/euler/CRM/inv_CRM_JST.cfg
@@ -5,238 +5,104 @@
 % Author: Thomas D. Economon	      	      	              	       	       %
 % Institution: Stanford University				                               %
 % Date: 2012.10.07                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8395
-%
-% Angle of attack (degrees)
 AOA= 3.06
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only for Euler equations)
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 implies no marker)
 MARKER_EULER= ( fuselage , Wing , HTP)
-%
-% Marker of the far field (0 implies no marker)
 MARKER_FAR= ( FarField )
-%
-% Marker of symmetry boundary (0 implies no marker)
 MARKER_SYM= ( SymmetryPlane )
-%
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( fuselage , Wing , HTP )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( fuselage , Wing , HTP )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
-% Numerical method for computation of spatial gradients: (GREEN_GAUSS, 
-%                                                WIEGHTED_LEAST_SQUARES)
-NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 EXT_ITER= 99999
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.9
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.9
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.04 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE, TOTAL_HEAT,
-%                                     MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                     INVERSE_DESIGN_HEATFLUX)
-OBJECTIVE_FUNCTION= DRAG
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
+OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.04 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.5
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------&
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -6
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 100
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= grid_crm_dpw4_MB-structured.su2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
-% Mesh input file format (SU2)
 MESH_FORMAT= SU2
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution frequency
 OUTPUT_WRT_FREQ= 50
-%
diff --git a/TestCases/euler/biparabolic/BIPARABOLIC.cfg b/TestCases/euler/biparabolic/BIPARABOLIC.cfg
index 63fb2fed33d..0db5bc08be8 100644
--- a/TestCases/euler/biparabolic/BIPARABOLIC.cfg
+++ b/TestCases/euler/biparabolic/BIPARABOLIC.cfg
@@ -5,266 +5,113 @@
 % Author: Trent W. Lukaczyk                                                    %
 % Institution: Stanford University                                             %
 % Date: 2012.08.16                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 1.7
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ------------------------ SUPERSONIC SIMULATION ------------------------------%
 %
-% Evaluate equivalent area on the Near-Field (NO, YES)
 EQUIV_AREA= YES
-%
-% Integration limits of the equivalent area ( xmin, xmax, Dist_NearField )
 EA_INT_LIMIT= ( -100.0, 100.0, 2.0 )
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
-% Euler wall boundary marker(s) (NONE = no marker)
-MARKER_EULER= ( airfoil )
 %
-% Farfield boundary marker(s) (NONE = no marker)
+MARKER_EULER= ( airfoil )
 MARKER_FAR= ( farfield )
-%
-% Near-Field boundary marker(s) (NONE = no marker)
 MARKER_NEARFIELD= ( upper_nearfield, lower_nearfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil, upper_nearfield )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 25.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 EXT_ITER= 99999999
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3 
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.95
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.95
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE, TOTAL_HEAT,
-%                                     MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                     INVERSE_DESIGN_HEATFLUX)
-OBJECTIVE_FUNCTION= EQUIVALENT_AREA
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
+OBJECTIVE_FUNCTION= EQUIVALENT_AREA
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.8
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, PARABOLIC, NACA_4DIGITS, 
-%                      DISPLACEMENT, ROTATION, FFD_CONTROL_POINT, 
-%                      FFD_TWIST,
-%                      FFD_ROTATION, FFD_CAMBER, FFD_THICKNESS, FFD_VOLUME)
 DV_KIND= PARABOLIC
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE ( Lower(0)/Upper(1) side, x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( Center, Thickness )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% 	- FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% 	- FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% 	- FFD_VOLUME ( FFD_BoxTag, i_Ind, j_Ind )
 DV_PARAM= ( 0.5, 5 )
-%
-% New value of the shape deformation
 DV_VALUE= 0.01
-%
-% Hold the grid fixed in a region (NO, YES)
 HOLD_GRID_FIXED= YES
-%
-% Coordinates of the box where the grid will be deformed (Xmin, Ymin, Zmin, Xmax, Ymax, Zmax)
 HOLD_GRID_FIXED_COORD= ( -0.2, -0.4, 0.0, 2.2, 0.4, 0.0 )
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -6
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_BIPARABOLIC_sup.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= volume_flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= volume_adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 100
-%
diff --git a/TestCases/euler/bluntbody/blunt.cfg b/TestCases/euler/bluntbody/blunt.cfg
index 2c9081c015b..855a95d700b 100644
--- a/TestCases/euler/bluntbody/blunt.cfg
+++ b/TestCases/euler/bluntbody/blunt.cfg
@@ -5,198 +5,85 @@
 % Author: Amit Sachdeva                                                        %
 % Institution: ADSG-VSSC                                                       %
 % Date: 2019.01.23                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
-RESTART_SOL= NO 
-%
+RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 6.0  
-%
-% Angle of attack (degrees)
 AOA= 0.0 
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 0.785398
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( wall )
-%
-% Marker of the far field (NONE = no marker)
 MARKER_FAR= ( far )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( wall )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( wall )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 3.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO 
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.1, 0.9, 5.0, 50.0 )
-%
-% Number of total iterations
 ITER= 2500 
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES  
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS    
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5 
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 1.0
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 1.0
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, SLAU, SLAU2, 
-%                               AUSMPLUSUP, AUSMPLUSUP2 HLLC, TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= AUSMPLUSUP     
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= NO 
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= blunt_91.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= blunt_91.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-%
-% Screen output 
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
diff --git a/TestCases/euler/channel/inv_channel.cfg b/TestCases/euler/channel/inv_channel.cfg
index 90d3ab84953..7140461e2f0 100644
--- a/TestCases/euler/channel/inv_channel.cfg
+++ b/TestCases/euler/channel/inv_channel.cfg
@@ -5,216 +5,101 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2012.09.29                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
-%
-% Physical governing equations (EULER, NAVIER_STOKES, NS_PLASMA)
 %                               
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Side-slip angle (degrees, only for compressible flows)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default)  
 FREESTREAM_PRESSURE= 101300.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( upper_wall, lower_wall )
-%
-% Inlet boundary marker(s) (NONE = no marker) 
-% Format: ( inlet marker, total temperature, total pressure, flow_direction_x, 
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-% Default: Mach ~ 0.1
 MARKER_INLET= ( inlet, 288.6, 102010.0, 1.0, 0.0, 0.0 )
 % Comment above line and uncomment next for  Mach ~ 0.7 (transonic)
 %MARKER_INLET= ( inlet, 316.224, 140513.23, 1.0, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
 MARKER_OUTLET= ( outlet, 101300.0 )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( lower_wall )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( upper_wall, lower_wall )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 6.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 EXT_ITER= 999999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.9
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.9
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_channel_256x128.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
diff --git a/TestCases/euler/channel/inv_channel_RK.cfg b/TestCases/euler/channel/inv_channel_RK.cfg
index e5c88a43d30..9041a7d4c42 100644
--- a/TestCases/euler/channel/inv_channel_RK.cfg
+++ b/TestCases/euler/channel/inv_channel_RK.cfg
@@ -5,212 +5,95 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2012.10.07                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Side-slip angle (degrees, only for compressible flows)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default)  
 FREESTREAM_PRESSURE= 101300.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( upper_wall, lower_wall )
-%
-% Inlet boundary marker(s) (NONE = no marker) 
-% Format: ( inlet marker, total temperature, total pressure, flow_direction_x, 
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-% Default: Mach ~ 0.7 (Transonic)
 MARKER_INLET= ( inlet, 316.224, 140513.23, 1.0, 0.0, 0.0 )
 % Comment above line and uncomment next for  Mach ~ 0.1
 %MARKER_INLET= ( inlet, 288.6, 102010.0, 1.0, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
 MARKER_OUTLET= ( outlet, 101300.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( lower_wall )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( upper_wall, lower_wall )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 110
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= BCGSTAB
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.9
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.9
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= RUNGE-KUTTA_EXPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_channel_256x128.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-% 
-% Screen output
 SCREEN_OUTPUT = (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
diff --git a/TestCases/euler/naca0012/inv_NACA0012.cfg b/TestCases/euler/naca0012/inv_NACA0012.cfg
index 8c735b8ee8e..ddf59229ab3 100644
--- a/TestCases/euler/naca0012/inv_NACA0012.cfg
+++ b/TestCases/euler/naca0012/inv_NACA0012.cfg
@@ -5,334 +5,128 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
+
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AOA= 1.25
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (NONE = no marker)
 MARKER_FAR= ( farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( airfoil )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( airfoil )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 ITER= 250
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 1.0
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 1.0
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.5
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (FFD_SETTING, FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC,
-%                      NACA_4DIGITS, DISPLACEMENT, ROTATION, FFD_CONTROL_POINT, 
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CAMBER, FFD_THICKNESS, SURFACE_FILE, AIRFOIL)
 DV_KIND= HICKS_HENNE 
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation
-% - FFD_CONTROL_POINT_2D ( FFD_Box_ID, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_Box_ID, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_Box_ID, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - FOURIER ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), index, cos(0)/sin(1) )
-% - SPHERICAL ( ControlPoint_Index, Theta_Disp, R_Disp )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - PARABOLIC ( Center, Thickness )
-% - DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - OBSTACLE ( Center, Bump size )
 DV_PARAM= ( 1, 0.5 )
-%
-% Value of the shape deformation
 DV_VALUE= 0.01
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= mesh_NACA0012_inv.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= mesh_NACA0012_inv.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-%
-% Screen output fields
 SCREEN_OUTPUT = (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
+
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.001
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= ( LIFT > 0.328188 ) * 0.001; ( MOMENT_Z > 0.034068 ) * 0.001; ( AIRFOIL_THICKNESS > 0.11 ) * 0.001
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 ); ( 30, 1.0 | airfoil | 0, 0.20 ); ( 30, 1.0 | airfoil | 0, 0.25 ); ( 30, 1.0 | airfoil | 0, 0.30 ); ( 30, 1.0 | airfoil | 0, 0.35 ); ( 30, 1.0 | airfoil | 0, 0.40 ); ( 30, 1.0 | airfoil | 0, 0.45 ); ( 30, 1.0 | airfoil | 0, 0.50 ); ( 30, 1.0 | airfoil | 0, 0.55 ); ( 30, 1.0 | airfoil | 0, 0.60 ); ( 30, 1.0 | airfoil | 0, 0.65 ); ( 30, 1.0 | airfoil | 0, 0.70 ); ( 30, 1.0 | airfoil | 0, 0.75 ); ( 30, 1.0 | airfoil | 0, 0.80 ); ( 30, 1.0 | airfoil | 0, 0.85 ); ( 30, 1.0 | airfoil | 0, 0.90 ); ( 30, 1.0 | airfoil | 0, 0.95 ); ( 30, 1.0 | airfoil | 1, 0.05 ); ( 30, 1.0 | airfoil | 1, 0.10 ); ( 30, 1.0 | airfoil | 1, 0.15 ); ( 30, 1.0 | airfoil | 1, 0.20 ); ( 30, 1.0 | airfoil | 1, 0.25 ); ( 30, 1.0 | airfoil | 1, 0.30 ); ( 30, 1.0 | airfoil | 1, 0.35 ); ( 30, 1.0 | airfoil | 1, 0.40 ); ( 30, 1.0 | airfoil | 1, 0.45 ); ( 30, 1.0 | airfoil | 1, 0.50 ); ( 30, 1.0 | airfoil | 1, 0.55 ); ( 30, 1.0 | airfoil | 1, 0.60 ); ( 30, 1.0 | airfoil | 1, 0.65 ); ( 30, 1.0 | airfoil | 1, 0.70 ); ( 30, 1.0 | airfoil | 1, 0.75 ); ( 30, 1.0 | airfoil | 1, 0.80 ); ( 30, 1.0 | airfoil | 1, 0.85 ); ( 30, 1.0 | airfoil | 1, 0.90 ); ( 30, 1.0 | airfoil | 1, 0.95 )
diff --git a/TestCases/euler/naca0012/inv_NACA0012_Roe.cfg b/TestCases/euler/naca0012/inv_NACA0012_Roe.cfg
index 0c3e28654f8..c4ac9f21203 100644
--- a/TestCases/euler/naca0012/inv_NACA0012_Roe.cfg
+++ b/TestCases/euler/naca0012/inv_NACA0012_Roe.cfg
@@ -5,200 +5,91 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2012.10.07                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (POTENTIAL_FLOW, EULER, NAVIER_STOKES, 
-%                               MULTI_SPECIES_NAVIER_STOKES, TWO_PHASE_FLOW, 
-%                               COMBUSTION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AOA= 1.25
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
-
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
-NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 CFL_NUMBER= 4.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 110
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= BCGSTAB
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 2, 2 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 1.0
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 1.0
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.01
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA0012_inv.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-%
-% Screen output fields
 SCREEN_OUTPUT = (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
diff --git a/TestCases/euler/oneram6/inv_ONERAM6.cfg b/TestCases/euler/oneram6/inv_ONERAM6.cfg
index 37452c3a79d..e777e3d2bc4 100644
--- a/TestCases/euler/oneram6/inv_ONERAM6.cfg
+++ b/TestCases/euler/oneram6/inv_ONERAM6.cfg
@@ -3,409 +3,153 @@
 % SU2 configuration file                                                       %
 % Case description: ONERA M6 wing in inviscid, transonic flow                  %
 % Author: Thomas D. Economon	      	      	              	       	       %
-% Institution: Stanford University				               %
+% Institution: Stanford University                                             %
 % Date: 2015.08.25                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
-%
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8395
-%
-% Angle of attack (degrees)
 AOA= 3.06
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only for Euler equations)
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yaMAIN_BOX non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_VEL_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 implies no marker)
 MARKER_EULER= ( WING )
-%
-% Marker of the far field (0 implies no marker)
 MARKER_FAR= ( FARFIELD )
-%
-% Marker of symmetry boundary (0 implies no marker)
 MARKER_SYM= ( SYMMETRY )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( WING )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( WING )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( WING )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 99999
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= YES
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.9
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.9
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.5
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------&
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 25
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_ONERAM6_inv_ffd.su2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
-% Mesh input file format (SU2)
 MESH_FORMAT= SU2
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution frequency
 OUTPUT_WRT_FREQ= 100
-%
-%
-% Screen output fields
 SCREEN_OUTPUT = (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
-%
 OUTPUT_FILES= (RESTART_ASCII, CGNS, SURFACE_CGNS)
+
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING,
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC, NACA_4DIGITS, AIRFOIL)
 DV_KIND= FFD_CONTROL_POINT
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( WING )
-%
-% Parameters of the shape deformation
-% - TRANSLATION ( x_Disp, y_Disp, z_Disp ), as a unit vector
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - SCALE ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - PARABOLIC ( Center, Thickness )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - AIRFOIL ( 1.0 )
 DV_PARAM= ( MAIN_BOX, 2, 3, 1, 0.0, 0.0, 1.0 )
-%
-% Value of the shape deformation
 DV_VALUE= 0.05
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES,
-%                                                      BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 2
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= NO
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-10
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 500
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (MAIN_BOX, -0.0403, 0.0, -0.04836, 0.8463, 0.0, -0.04836, 1.209, 1.2896, -0.04836, 0.6851, 1.2896, -0.04836, -0.0403, 0.0, 0.04836, 0.8463, 0.0, 0.04836, 1.209, 1.2896, 0.04836, 0.6851, 1.2896, 0.04836)
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= (10, 8, 1)
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= 2ND_DERIVATIVE
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 1.0
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= ( LIFT > 0.282557 ) * 1.0
-%
-% Maximum number of iterations
 OPT_ITERATIONS= 100
-%
-% Requested accuracy
 OPT_ACCURACY= 1E-6
-%
-% Upper bound for each design variable
 OPT_BOUND_UPPER= 0.1
-%
-% Lower bound for each design variable
 OPT_BOUND_LOWER= -0.1
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 11, 1.0 | WING | MAIN_BOX, 0, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 0, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 0, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 0, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 0, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 0, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 0, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 0, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 0, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 0, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 0, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 0, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 1, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 2, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 3, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 4, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 5, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 6, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 7, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 8, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 9, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | WING | MAIN_BOX, 10, 8, 1, 0.0, 0.0, 1.0 )
diff --git a/TestCases/euler/wedge/inv_wedge_HLLC.cfg b/TestCases/euler/wedge/inv_wedge_HLLC.cfg
index adf29537564..d9662291509 100644
--- a/TestCases/euler/wedge/inv_wedge_HLLC.cfg
+++ b/TestCases/euler/wedge/inv_wedge_HLLC.cfg
@@ -5,248 +5,100 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2012.10.07                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 2.0
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 100000.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( upper, lower )
-%
-% Supersonic inlet boundary marker(s) (NONE = no marker) 
-% Total Conditions: (inlet marker, temperature, static pressure, velocity_x, 
-%           velocity_y, velocity_z, ... ), i.e. all variables specified.
 MARKER_SUPERSONIC_INLET= ( inlet, 300.0, 100000.0, 695.4290761824674, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
 MARKER_OUTLET= ( outlet, 10000.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( lower )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( upper, lower )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 11000
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= BCGSTAB
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.8
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= HLLC
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.006
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -13
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_wedge_inv.cgns
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= CGNS
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-%
-% Screen output fields
 SCREEN_OUTPUT = (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING,
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS
-%                      FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, FFD_ROTATION,
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC, NACA_4DIGITS, AIRFOIL)
 DV_KIND= SCALE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( upper, lower, inlet, outlet )
-%
-% Parameters of the shape deformation
-% - TRANSLATION ( x_Disp, y_Disp, z_Disp )
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - SCALE ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_DIHEDRAL_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - PARABOLIC ( Center, Thickness )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - AIRFOIL ( 1.0 )
 DV_PARAM= ( 1.0 )
-%
-% Value of the shape deformation
 DV_VALUE= 1.0
diff --git a/TestCases/fea_fsi/Airfoil_RBF/config.cfg b/TestCases/fea_fsi/Airfoil_RBF/config.cfg
index d7c785d4ce3..73cfd069047 100755
--- a/TestCases/fea_fsi/Airfoil_RBF/config.cfg
+++ b/TestCases/fea_fsi/Airfoil_RBF/config.cfg
@@ -3,7 +3,7 @@
 % Case description: 2D airfoil FSI with radial basis function interp.          %
 % Institution: Imperial College London                                         %
 % Date: 2015.08.12                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 SOLVER = MULTIPHYSICS
@@ -22,4 +22,3 @@ OUTER_ITER = 50
 
 % enable this option to see convergence output for individual zones
 WRT_ZONE_CONV = NO
-
diff --git a/TestCases/fea_fsi/Airfoil_RBF/configFEA.cfg b/TestCases/fea_fsi/Airfoil_RBF/configFEA.cfg
index 2e94b469839..7c1d9e0d70e 100644
--- a/TestCases/fea_fsi/Airfoil_RBF/configFEA.cfg
+++ b/TestCases/fea_fsi/Airfoil_RBF/configFEA.cfg
@@ -2,7 +2,7 @@
 % SU2 configuration file                                                 %
 % Case description: 2D airfoil FSI with radial basis function interp.    %
 % Institution: Imperial College London                                   %
-% File Version 7.4.0 "Blackbird"                                         %
+% File Version 7.5.0 "Blackbird"                                         %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
 % Interface options ---------------------------------------------------- %
@@ -66,4 +66,3 @@ VOLUME_FILENAME= solid
 % history and screen
 SCREEN_WRT_FREQ_INNER= 10
 CONV_FILENAME= history
-
diff --git a/TestCases/fea_fsi/Airfoil_RBF/configFlow.cfg b/TestCases/fea_fsi/Airfoil_RBF/configFlow.cfg
index 671fd8bb64a..d307f30dd64 100644
--- a/TestCases/fea_fsi/Airfoil_RBF/configFlow.cfg
+++ b/TestCases/fea_fsi/Airfoil_RBF/configFlow.cfg
@@ -2,7 +2,7 @@
 % SU2 configuration file                                                 %
 % Case description: 2D airfoil FSI with radial basis function interp.    %
 % Institution: Imperial College London                                   %
-% File Version 7.4.0 "Blackbird"                                         %
+% File Version 7.5.0 "Blackbird"                                         %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
 % Interface options ---------------------------------------------------- %
@@ -124,4 +124,3 @@ SURFACE_FILENAME= surface_fluid
 % history and screen
 SCREEN_WRT_FREQ_INNER= 10
 CONV_FILENAME= history
-
diff --git a/TestCases/fea_fsi/DynBeam_2d/configBeam_2d.cfg b/TestCases/fea_fsi/DynBeam_2d/configBeam_2d.cfg
index f1ed1c759a2..2f422131d9e 100644
--- a/TestCases/fea_fsi/DynBeam_2d/configBeam_2d.cfg
+++ b/TestCases/fea_fsi/DynBeam_2d/configBeam_2d.cfg
@@ -4,7 +4,7 @@
 % Author: Ruben Sanchez Fernandez                                              %
 % Institution: Imperial College London                                         %
 % Date: 2016.02.01                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
                     
 SOLVER= ELASTICITY
diff --git a/TestCases/fea_fsi/MixElemsKnowles/config.cfg b/TestCases/fea_fsi/MixElemsKnowles/config.cfg
index 9b44d7fce1c..a4150bbc044 100644
--- a/TestCases/fea_fsi/MixElemsKnowles/config.cfg
+++ b/TestCases/fea_fsi/MixElemsKnowles/config.cfg
@@ -4,7 +4,7 @@
 % Case description: Tip-loaded 3D cantilever beam, mix of element types,       %
 %                   nonlinear elasticity with Knowles material model.          %
 % Institution: Imperial College London                                         %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/fea_fsi/SquareCyl_Beam/config.cfg b/TestCases/fea_fsi/SquareCyl_Beam/config.cfg
index 6dcf4f1e959..c8986a27105 100644
--- a/TestCases/fea_fsi/SquareCyl_Beam/config.cfg
+++ b/TestCases/fea_fsi/SquareCyl_Beam/config.cfg
@@ -5,35 +5,19 @@
 % Author: Ruben Sanchez Fernandez                                              %
 % Institution: Imperial College London                                         %
 % Date: 2016.06.01                                                             %
-% File Version 4.3.0 "cardinal"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               TNE2_EULER, TNE2_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FLUID_STRUCTURE_INTERACTION
-%
 FSI_FLUID_PROBLEM = NAVIER_STOKES
-%
 FSI_STRUCTURAL_PROBLEM = ELASTICITY
-%
-% If Navier-Stokes, kind of turbulent model (NONE, SA)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED, ONE_SHOT_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
-% Unsteady restart iteration (need previous restart files)
 RESTART_ITER= 2
-%
-% Restart the solution from a steady state solution (sets Grid Vel to 0)
 RESTART_STEADY_STATE = NO
 
 % -----------------------------------------------------------------------------%
@@ -42,38 +26,23 @@ RESTART_STEADY_STATE = NO
 
 % --------------------------- MESH INPUT FILE ---------------------------------%
 %
-% Mesh input file format (SU2, CGNS NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh input file
 MESH_FILENAME= mesh.su2
 
 % ------------------------------- TIME STEP -----------------------------------%
 %
-% Time Step for dual time stepping fluid simulations (s)
 TIME_STEP= 0.01
-%
-% Number of total iterations
 TIME_ITER= 35
 
 % --------------------------- FSI CONVERGENCE ---------------------------------%
 %
-% Number of Fluid Structure Interaction subiterations
 FSI_ITER= 10
-%
-% Relaxation for the block Gauss Seidel Method
 BGS_RELAXATION = FIXED_PARAMETER
-%
-% Relaxation parameter
 STAT_RELAX_PARAMETER= 0.7
-%
-%
-% Min value of the residual in the boundary displacement (log10 of the residual)
 CONV_RESIDUAL_MINVAL_FSI= -5.92
 
 % -------------------------- BOUNDARY CONDITIONS ------------------------------%
 %
-% Marker interface
 MARKER_ZONE_INTERFACE = (UpperBeam, UpperBeamS, RightBeam, RightBeamS, LowerBeam, LowerBeamS)
 
 % -----------------------------------------------------------------------------%
@@ -82,51 +51,30 @@ MARKER_ZONE_INTERFACE = (UpperBeam, UpperBeamS, RightBeam, RightBeamS, LowerBeam
 
 % -------------------------- PROBLEM DEFINITION -------------------------------%
 %
-% Geometric conditions
 GEOMETRIC_CONDITIONS= LARGE_DEFORMATIONS
-%
-% Material model
 MATERIAL_MODEL= NEO_HOOKEAN
 
 % --------------------------- MATERIAL CONSTANTS ------------------------------%
 %
-% Value of the Elasticity modulus
 ELASTICITY_MODULUS=1.25E5
-%
-% Value of the Poisson ratio
 POISSON_RATIO=0.35
-%
-% Value of the material density
 MATERIAL_DENSITY=50
-%
-% Elasticity formulation for 2D problems
 FORMULATION_ELASTICITY_2D = PLANE_STRESS
 
 % -------------------------- CONVERGENCE CRITERIA -----------------------------%
 %
-% Maximum number of subiterations for the structural solver
 NONLINEAR_FEM_INT_ITER = 20
-%
-% Convergence tolerances
 
 % -------------------------- DYNAMIC SIMULATION -------------------------------%
 %
-% Dynamic structural analysis
 DYNAMIC_ANALYSIS= YES
-%
-% Time discretization
 TIME_DISCRE_FEA= NEWMARK_IMPLICIT
-%
-% Newmark parameters
 NEWMARK_BETA=0.2601
 NEWMARK_GAMMA=0.52
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Clamped boundary marker(s)
 MARKER_CLAMPED = ( Clamped )
-%
-% Load boundary marker(s)
 MARKER_PRESSURE= ( RightBeamS , 0, LowerBeamS, 0, UpperBeamS, 0)
 
 % -----------------------------------------------------------------------------%
@@ -135,87 +83,48 @@ MARKER_PRESSURE= ( RightBeamS , 0, LowerBeamS, 0, UpperBeamS, 0)
 
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER, TIME_SPECTRAL)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-%
-% Total Physical Time for dual time stepping simulations (s)
 UNST_TIME= 1.0
 
 % --------------------------- FLOW CONVERGENCE --------------------------------%
 %
-% Number of internal iterations (dual time method)
 UNST_INT_ITER= 1000
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 180
-%
-% Mach number
 MACH_NUMBER = 0.15
 MACH_MOTION = 0.15
-%
-% Fix the value of the density and viscosity of the flow
 FREESTREAM_OPTION = DENSITY_FS
 FREESTREAM_DENSITY = 1.18
 VISCOSITY_MODEL = CONSTANT_VISCOSITY
 MU_CONSTANT = 1.82E-5
-%
-% Initialization option
 INIT_OPTION = TD_CONDITIONS
-%
-% Freestream pressure and temperature
 FREESTREAM_PRESSURE = 2.8873220339
 FREESTREAM_TEMPERATURE = 0.0085240024
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 0.01
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 0.01
-%
-% Length to compute the Reynolds number
 REYNOLDS_LENGTH=0.01
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s)
 MARKER_HEATFLUX= ( Square, 0.0, UpperBeam, 0.0, RightBeam, 0.0, LowerBeam, 0.0 )
-%
-% Inlet boundary marker(s)
-% Format: ( inlet marker, total temperature, total pressure, flow_direction_x,
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
 MARKER_INLET= ( Inlet, 0.0085240024, 2.9330537305, 1.0, 0.0, 0.0 )
-%
-% Outlet boundary marker(s)
-% Format: ( outlet marker, back pressure (static), ... )
 MARKER_OUTLET= ( Outlet, 2.8873220339)
-%
-% Euler boundary marker(s)
 MARKER_EULER= ( Upper, Lower )
 
 
 % ------------------------ MARKER MONITORING ----------------------------------%
 %
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( UpperBeam, RightBeam, LowerBeam)
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( UpperBeam, RightBeam, LowerBeam)
 
 % -----------------------------------------------------------------------------%
@@ -223,43 +132,21 @@ MARKER_MONITORING= ( UpperBeam, RightBeam, LowerBeam)
 % -----------------------------------------------------------------------------%
 %
 TABULAR_FORMAT= CSV
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= results_flow
-%
-% Output file name (PARAVIEW, TECPLOT)
 VOLUME_STRUCTURE_FILENAME= results_beam
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Forces breakdown file
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Output file name (PARAVIEW, TECPLOT)
 SOLUTION_STRUCTURE_FILENAME= solution_beam.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart flow
 RESTART_STRUCTURE_FILENAME= restart_beam.dat
-%
-%
-% Writing solution file frequency for physical time steps (dual time)
 OUTPUT_WRT_FREQ= 1
 
 % -----------------------------------------------------------------------------%
 % --------------------------- MESH PARAMETERS ---------------------------------%
 % -----------------------------------------------------------------------------%
 %
-% Maximum number of iterations when solving the mesh update
 DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Steps in the mesh updating
 DEFORM_NONLINEAR_ITER= 1
 
 % -----------------------------------------------------------------------------%
@@ -268,74 +155,32 @@ DEFORM_NONLINEAR_ITER= 1
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.0
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 FSI_LINEAR_SOLVER_STRUC= FGMRES
-%
-% Preconditioner for the structural problem
 FSI_LINEAR_SOLVER_PREC_STRUC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 FSI_LINEAR_SOLVER_ERROR_STRUC= 1E-7
-%
-% Number of iterations for the linear solver for the structural problem
 FSI_LINEAR_SOLVER_ITER_STRUC = 1000
 
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 1.0
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-5
-%
-
diff --git a/TestCases/fea_fsi/StatBeam_3d/configBeam_3d.cfg b/TestCases/fea_fsi/StatBeam_3d/configBeam_3d.cfg
index 88be065e4a6..926495e2602 100644
--- a/TestCases/fea_fsi/StatBeam_3d/configBeam_3d.cfg
+++ b/TestCases/fea_fsi/StatBeam_3d/configBeam_3d.cfg
@@ -4,7 +4,7 @@
 % Author: Ruben Sanchez Fernandez                                              %
 % Institution: Imperial College London                                         %
 % Date: 2016.02.01                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
                      
 SOLVER= ELASTICITY
diff --git a/TestCases/fea_fsi/WallChannel_2d/configFEA.cfg b/TestCases/fea_fsi/WallChannel_2d/configFEA.cfg
index d2234449cdc..7486d208bf3 100644
--- a/TestCases/fea_fsi/WallChannel_2d/configFEA.cfg
+++ b/TestCases/fea_fsi/WallChannel_2d/configFEA.cfg
@@ -50,4 +50,3 @@ OUTPUT_WRT_FREQ= 1
 VOLUME_FILENAME= results_wall
 RESTART_FILENAME= solution_wall.dat
 SOLUTION_FILENAME= solution_wall.dat
-
diff --git a/TestCases/fea_fsi/WallChannel_2d/configFSI.cfg b/TestCases/fea_fsi/WallChannel_2d/configFSI.cfg
index 1063a65d96d..5cac2231c19 100644
--- a/TestCases/fea_fsi/WallChannel_2d/configFSI.cfg
+++ b/TestCases/fea_fsi/WallChannel_2d/configFSI.cfg
@@ -22,4 +22,3 @@ OUTPUT_FILES=(RESTART_ASCII, PARAVIEW)
 OUTER_ITER = 5
 % Only required by the python scripts
 MATH_PROBLEM = DIRECT
-
diff --git a/TestCases/fea_fsi/WallChannel_2d/configFlow.cfg b/TestCases/fea_fsi/WallChannel_2d/configFlow.cfg
index b2fae4869db..e14c17898bd 100644
--- a/TestCases/fea_fsi/WallChannel_2d/configFlow.cfg
+++ b/TestCases/fea_fsi/WallChannel_2d/configFlow.cfg
@@ -77,4 +77,3 @@ OUTPUT_WRT_FREQ= 1
 VOLUME_FILENAME= results_flow
 RESTART_FILENAME= solution_flow.dat
 SOLUTION_FILENAME= solution_flow.dat
-
diff --git a/TestCases/fea_fsi/dyn_fsi/configFlow.cfg b/TestCases/fea_fsi/dyn_fsi/configFlow.cfg
index 8f81173a29a..b2f12dfcf10 100644
--- a/TestCases/fea_fsi/dyn_fsi/configFlow.cfg
+++ b/TestCases/fea_fsi/dyn_fsi/configFlow.cfg
@@ -12,7 +12,6 @@ MARKER_DEFORM_MESH= ( wallUpwF, wallDownF, wallUpperF )
 
 INNER_ITER=50
 
-
 MATH_PROBLEM= DIRECT
 READ_BINARY_RESTART= NO
 
diff --git a/TestCases/fea_fsi/stat_fsi/config.cfg b/TestCases/fea_fsi/stat_fsi/config.cfg
index 8e74726c7a9..029d94ef928 100755
--- a/TestCases/fea_fsi/stat_fsi/config.cfg
+++ b/TestCases/fea_fsi/stat_fsi/config.cfg
@@ -22,4 +22,3 @@ RESTART_ITER = 0
 
 TIME_DOMAIN = NO
 OUTER_ITER = 8
-
diff --git a/TestCases/fea_fsi/stat_fsi/configFEA.cfg b/TestCases/fea_fsi/stat_fsi/configFEA.cfg
index 8f291ad93f5..3ce2b13322c 100755
--- a/TestCases/fea_fsi/stat_fsi/configFEA.cfg
+++ b/TestCases/fea_fsi/stat_fsi/configFEA.cfg
@@ -9,10 +9,6 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               TNE2_EULER, TNE2_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= ELASTICITY
 MATH_PROBLEM= DIRECT
 
@@ -24,7 +20,6 @@ MATERIAL_COMPRESSIBILITY= COMPRESSIBLE
 NONLINEAR_FEM_SOLUTION_METHOD = NEWTON_RAPHSON
 INNER_ITER = 10
 
-
 INCREMENTAL_LOAD = NO
 
 % --------------------------- TIME STEP ISSUES --------------------------------%
@@ -66,7 +61,7 @@ POISSON_RATIO=0.4
 % -------------------------- DYNAMIC SIMULATION -------------------------------%
 DYNAMIC_ANALYSIS= NO
 TIME_DISCRE_FEA= NEWMARK_IMPLICIT
-%
+
 % -------------------------- STRUCTURAL SOLVER --------------------------------%
 
 LINEAR_SOLVER = CONJUGATE_GRADIENT
diff --git a/TestCases/fea_fsi/stat_fsi/configFlow.cfg b/TestCases/fea_fsi/stat_fsi/configFlow.cfg
index 0fc8c53c8b5..a20f5947d7f 100755
--- a/TestCases/fea_fsi/stat_fsi/configFlow.cfg
+++ b/TestCases/fea_fsi/stat_fsi/configFlow.cfg
@@ -9,10 +9,6 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               TNE2_EULER, TNE2_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= NAVIER_STOKES
 
 KIND_TURB_MODEL= NONE
@@ -63,7 +59,6 @@ MARKER_MONITORING= ( wallF )
 % -------------------------- FLUID SIMULATION ---------------------------------%
 
 TIME_DOMAIN=NO
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 4.01
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
@@ -104,10 +99,6 @@ LINEAR_SOLVER_PREC= ILU
 LINEAR_SOLVER_ERROR= 1E-6
 LINEAR_SOLVER_ITER= 2
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-
-MGLEVEL= 0
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 
 CONV_NUM_METHOD_FLOW= ROE
diff --git a/TestCases/fea_topology/config.cfg b/TestCases/fea_topology/config.cfg
index e652c0d4f48..ad1e25dae7a 100644
--- a/TestCases/fea_topology/config.cfg
+++ b/TestCases/fea_topology/config.cfg
@@ -2,7 +2,7 @@
 % SU2 configuration file                                                 %
 % Case description: 4 by 1 cantilever optim. for stiff. @ 50% material   %
 % Institution: Imperial College London                                   %
-% File Version 7.4.0 "Blackbird"                                            %
+% File Version 7.5.0 "Blackbird"                                         %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
 % Optimization
@@ -105,5 +105,4 @@ RESTART_ADJ_FILENAME= restart_adj.dat
 % or delete them to use best practice values.
 PARMETIS_TOLERANCE= 0.05
 PARMETIS_EDGE_WEIGHT= 0
-PARMETIS_POINT_WEIGHT= 1
-
+PARMETIS_POINT_WEIGHT= 1
\ No newline at end of file
diff --git a/TestCases/fea_topology/quick_start/settings_compliance.cfg b/TestCases/fea_topology/quick_start/settings_compliance.cfg
index a535068f4bf..d9cf275df75 100644
--- a/TestCases/fea_topology/quick_start/settings_compliance.cfg
+++ b/TestCases/fea_topology/quick_start/settings_compliance.cfg
@@ -48,4 +48,3 @@ TABULAR_FORMAT= CSV
 SOLUTION_FILENAME= direct.dat
 RESTART_FILENAME= direct.dat
 OUTPUT_FILES= PARAVIEW
-
diff --git a/TestCases/fea_topology/quick_start/settings_volfrac.cfg b/TestCases/fea_topology/quick_start/settings_volfrac.cfg
index 2319a83c041..a3ec2ebc3cb 100644
--- a/TestCases/fea_topology/quick_start/settings_volfrac.cfg
+++ b/TestCases/fea_topology/quick_start/settings_volfrac.cfg
@@ -47,5 +47,4 @@ MESH_FORMAT= SU2
 TABULAR_FORMAT= CSV
 SOLUTION_FILENAME= direct.dat
 RESTART_FILENAME= direct.dat
-OUTPUT_FILES= PARAVIEW
-
+OUTPUT_FILES= PARAVIEW
\ No newline at end of file
diff --git a/TestCases/fixed_cl/naca0012/inv_NACA0012.cfg b/TestCases/fixed_cl/naca0012/inv_NACA0012.cfg
index 6d7d0310e1a..6bd807aa5e2 100644
--- a/TestCases/fixed_cl/naca0012/inv_NACA0012.cfg
+++ b/TestCases/fixed_cl/naca0012/inv_NACA0012.cfg
@@ -5,350 +5,137 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
 READ_BINARY_RESTART=NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AOA= 1.25
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % -------------------------- CL DRIVER DEFINITION -----------------------------%
 %
-% Activate fixed lift mode (specify a CL instead of AoA, NO/YES)
 FIXED_CL_MODE= YES
-%
-% Target coefficient of lift for fixed lift mode (0.0 by default)
 TARGET_CL= 0.30
-%
-% Estimation of dCL/dAlpha (0.2 per degree by default)
 DCL_DALPHA= 0.2
-%
-% Maximum number of iterations between AoA updates
 UPDATE_AOA_ITER_LIMIT= 20
-%
-% Number of iterations to evaluate dCL/dAlpha at the end of the simulation
 ITER_DCL_DALPHA= 50
-%
-% Evaluate DeltaC_D/DeltaC_X during runtime (YES) or use the provided numbers (NO).
 EVAL_DOF_DCX= YES
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (NONE = no marker)
 MARKER_FAR= ( farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( airfoil )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( airfoil )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Number of total iterations
 ITER= 1000
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 1.0
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 1.0
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.5
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (FFD_SETTING, FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC,
-%                      NACA_4DIGITS, DISPLACEMENT, ROTATION, FFD_CONTROL_POINT, 
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CAMBER, FFD_THICKNESS, SURFACE_FILE, AIRFOIL)
 DV_KIND= HICKS_HENNE 
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation
-% - FFD_CONTROL_POINT_2D ( FFD_Box_ID, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_Box_ID, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_Box_ID, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - FOURIER ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), index, cos(0)/sin(1) )
-% - SPHERICAL ( ControlPoint_Index, Theta_Disp, R_Disp )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - PARABOLIC ( Center, Thickness )
-% - DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - OBSTACLE ( Center, Bump size )
 DV_PARAM= ( 1, 0.5 )
-%
-% Value of the shape deformation
 DV_VALUE= 0.01
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= mesh_NACA0012_inv.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= mesh_NACA0012_inv.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-%
-% Screen output fields
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
-%
 OUTPUT_FILES= (RESTART_ASCII)
+
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.001
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= ( LIFT > 0.328188 ) * 0.001; ( MOMENT_Z > 0.034068 ) * 0.001; ( AIRFOIL_THICKNESS > 0.11 ) * 0.001
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 ); ( 30, 1.0 | airfoil | 0, 0.20 ); ( 30, 1.0 | airfoil | 0, 0.25 ); ( 30, 1.0 | airfoil | 0, 0.30 ); ( 30, 1.0 | airfoil | 0, 0.35 ); ( 30, 1.0 | airfoil | 0, 0.40 ); ( 30, 1.0 | airfoil | 0, 0.45 ); ( 30, 1.0 | airfoil | 0, 0.50 ); ( 30, 1.0 | airfoil | 0, 0.55 ); ( 30, 1.0 | airfoil | 0, 0.60 ); ( 30, 1.0 | airfoil | 0, 0.65 ); ( 30, 1.0 | airfoil | 0, 0.70 ); ( 30, 1.0 | airfoil | 0, 0.75 ); ( 30, 1.0 | airfoil | 0, 0.80 ); ( 30, 1.0 | airfoil | 0, 0.85 ); ( 30, 1.0 | airfoil | 0, 0.90 ); ( 30, 1.0 | airfoil | 0, 0.95 ); ( 30, 1.0 | airfoil | 1, 0.05 ); ( 30, 1.0 | airfoil | 1, 0.10 ); ( 30, 1.0 | airfoil | 1, 0.15 ); ( 30, 1.0 | airfoil | 1, 0.20 ); ( 30, 1.0 | airfoil | 1, 0.25 ); ( 30, 1.0 | airfoil | 1, 0.30 ); ( 30, 1.0 | airfoil | 1, 0.35 ); ( 30, 1.0 | airfoil | 1, 0.40 ); ( 30, 1.0 | airfoil | 1, 0.45 ); ( 30, 1.0 | airfoil | 1, 0.50 ); ( 30, 1.0 | airfoil | 1, 0.55 ); ( 30, 1.0 | airfoil | 1, 0.60 ); ( 30, 1.0 | airfoil | 1, 0.65 ); ( 30, 1.0 | airfoil | 1, 0.70 ); ( 30, 1.0 | airfoil | 1, 0.75 ); ( 30, 1.0 | airfoil | 1, 0.80 ); ( 30, 1.0 | airfoil | 1, 0.85 ); ( 30, 1.0 | airfoil | 1, 0.90 ); ( 30, 1.0 | airfoil | 1, 0.95 )
diff --git a/TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg b/TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg
index e2abc971bb9..a48b39230c5 100644
--- a/TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg
+++ b/TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg
@@ -5,353 +5,138 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= CONTINUOUS_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
-%
-OUTPUT_FILES= (RESTART_ASCII)
+
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AOA= 1.25
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % -------------------------- CL DRIVER DEFINITION ----------------------------%
 %
-% Activate fixed lift mode (specify a CL instead of AoA, NO/YES)
 FIXED_CL_MODE= YES
-%
-% Target coefficient of lift for fixed lift mode (0.0 by default)
 TARGET_CL= 0.30
-%
-% Maximum number of iterations between AoA updates
 UPDATE_AOA_ITER_LIMIT= 20
-%
-% Number of iterations to evaluate dCL/dAlpha at the end of the simulation
 ITER_DCL_DALPHA= 250
-%
-% Estimation of dCL/dAlpha (0.2 per degree by default)
 DCL_DALPHA= 0.2
-%
-% Estimation dCD/dCL (0.07 by default)
 DCD_DCL_VALUE= 0.07
-%
-% Evaluate DeltaC_D/DeltaC_X during runtime (YES) or use the provided numbers (NO).
 EVAL_DOF_DCX= YES
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (NONE = no marker)
 MARKER_FAR= ( farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( airfoil )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( airfoil )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Number of total iterations
 ITER= 500
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 1.0
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 1.0
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.5
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (FFD_SETTING, FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC,
-%                      NACA_4DIGITS, DISPLACEMENT, ROTATION, FFD_CONTROL_POINT, 
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CAMBER, FFD_THICKNESS, SURFACE_FILE, AIRFOIL)
 DV_KIND= HICKS_HENNE 
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation
-% - FFD_CONTROL_POINT_2D ( FFD_Box_ID, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_Box_ID, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_Box_ID, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - FOURIER ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), index, cos(0)/sin(1) )
-% - SPHERICAL ( ControlPoint_Index, Theta_Disp, R_Disp )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - PARABOLIC ( Center, Thickness )
-% - DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - OBSTACLE ( Center, Bump size )
 DV_PARAM= ( 1, 0.5 )
-%
-% Value of the shape deformation
 DV_VALUE= 0.01
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -14
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= mesh_NACA0012_inv.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= mesh_NACA0012_inv.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-% Screen output
 SCREEN_OUTPUT = (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_GEO, SENS_AOA) 
+OUTPUT_FILES= (RESTART_ASCII)
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.001
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= ( LIFT > 0.328188 ) * 0.001; ( MOMENT_Z > 0.034068 ) * 0.001; ( AIRFOIL_THICKNESS > 0.11 ) * 0.001
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 ); ( 30, 1.0 | airfoil | 0, 0.20 ); ( 30, 1.0 | airfoil | 0, 0.25 ); ( 30, 1.0 | airfoil | 0, 0.30 ); ( 30, 1.0 | airfoil | 0, 0.35 ); ( 30, 1.0 | airfoil | 0, 0.40 ); ( 30, 1.0 | airfoil | 0, 0.45 ); ( 30, 1.0 | airfoil | 0, 0.50 ); ( 30, 1.0 | airfoil | 0, 0.55 ); ( 30, 1.0 | airfoil | 0, 0.60 ); ( 30, 1.0 | airfoil | 0, 0.65 ); ( 30, 1.0 | airfoil | 0, 0.70 ); ( 30, 1.0 | airfoil | 0, 0.75 ); ( 30, 1.0 | airfoil | 0, 0.80 ); ( 30, 1.0 | airfoil | 0, 0.85 ); ( 30, 1.0 | airfoil | 0, 0.90 ); ( 30, 1.0 | airfoil | 0, 0.95 ); ( 30, 1.0 | airfoil | 1, 0.05 ); ( 30, 1.0 | airfoil | 1, 0.10 ); ( 30, 1.0 | airfoil | 1, 0.15 ); ( 30, 1.0 | airfoil | 1, 0.20 ); ( 30, 1.0 | airfoil | 1, 0.25 ); ( 30, 1.0 | airfoil | 1, 0.30 ); ( 30, 1.0 | airfoil | 1, 0.35 ); ( 30, 1.0 | airfoil | 1, 0.40 ); ( 30, 1.0 | airfoil | 1, 0.45 ); ( 30, 1.0 | airfoil | 1, 0.50 ); ( 30, 1.0 | airfoil | 1, 0.55 ); ( 30, 1.0 | airfoil | 1, 0.60 ); ( 30, 1.0 | airfoil | 1, 0.65 ); ( 30, 1.0 | airfoil | 1, 0.70 ); ( 30, 1.0 | airfoil | 1, 0.75 ); ( 30, 1.0 | airfoil | 1, 0.80 ); ( 30, 1.0 | airfoil | 1, 0.85 ); ( 30, 1.0 | airfoil | 1, 0.90 ); ( 30, 1.0 | airfoil | 1, 0.95 )
diff --git a/TestCases/grad_smooth/naca0012/inv_NACA0012_gradsmooth.cfg b/TestCases/grad_smooth/naca0012/inv_NACA0012_gradsmooth.cfg
index c251fbfcd6b..7bcc4043e92 100644
--- a/TestCases/grad_smooth/naca0012/inv_NACA0012_gradsmooth.cfg
+++ b/TestCases/grad_smooth/naca0012/inv_NACA0012_gradsmooth.cfg
@@ -4,7 +4,7 @@
 % Case description: Sobolev smoothing for gradient on the NACA 0012 airfoil    %
 % Author: Thomas Dick (TU Kaiserslautern)                                      %
 % Date: 11.11.2021                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -161,5 +161,4 @@ VOLUME_ADJ_FILENAME= adjoint
 GRAD_OBJFUNC_FILENAME= of_grad.dat
 SURFACE_FILENAME= surface_flow
 SURFACE_ADJ_FILENAME= surface_adjoint
-READ_BINARY_RESTART= YES
-
+READ_BINARY_RESTART= YES
\ No newline at end of file
diff --git a/TestCases/grad_smooth/oneram6/ONERAM6_gradsmooth.cfg b/TestCases/grad_smooth/oneram6/ONERAM6_gradsmooth.cfg
index 41174ed4d1f..a6360efc1ba 100644
--- a/TestCases/grad_smooth/oneram6/ONERAM6_gradsmooth.cfg
+++ b/TestCases/grad_smooth/oneram6/ONERAM6_gradsmooth.cfg
@@ -4,7 +4,7 @@
 % Case description: Sobolev smoothing for gradient on the ONERA M6 wing        %
 % Author: Thomas Dick (TU Kaiserslautern)                                      %
 % Date: 11.11.2021                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -240,4 +240,3 @@ GRAD_OBJFUNC_FILENAME= of_grad.dat
 SURFACE_FILENAME= surface_flow
 SURFACE_ADJ_FILENAME= surface_adjoint
 READ_BINARY_RESTART= YES
-
diff --git a/TestCases/gust/inv_gust_NACA0012.cfg b/TestCases/gust/inv_gust_NACA0012.cfg
index 3dbc52d8e03..cd689f7afad 100644
--- a/TestCases/gust/inv_gust_NACA0012.cfg
+++ b/TestCases/gust/inv_gust_NACA0012.cfg
@@ -5,79 +5,42 @@
 % Author: Santiago Padron                                                      %
 % Institution: Stanford University                                             %
 % Date: 06-26-2015                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.2
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2, 2116.216 psf by default)
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K, 518.67 R by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation (m or in)
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional
-% moment (m or in)
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic
-% calculation) (m^2 or in^2)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= DIMENSIONAL
 
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Enable time domain
 TIME_DOMAIN=YES
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER, SPECTRAL_METHOD)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-%
-% Time Step for dual time stepping simulations (s)
 TIME_STEP= 0.001469304
 % Corresponds to a ds of 0.2
-%
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 50.0
-%
-% Number of internal iterations (dual time method)
 INNER_ITER= 100
 
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Type of dynamic mesh (NONE, RIGID_MOTION, DEFORMING, ROTATING_FRAME,
-%                       MOVING_WALL, AEROELASTIC, ELASTICITY,
-%                       EXTERNAL, AEROELASTIC_RIGID_MOTION)
 GRID_MOVEMENT= GUST
-%
-% Motion mach number (non-dimensional). Used for initializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.2
 
 % --------------------------- GUST SIMULATION ---------------------------------%
@@ -86,178 +49,83 @@ MACH_MOTION= 0.2
 % and the GRID_MOVEMENT_KIND to be set to GUST or any of the other options. 
 % Apply a wind gust (NO, YES)
 WIND_GUST = YES
-%
-% Type of gust (NONE, TOP_HAT, SINE, ONE_M_COSINE, VORTEX, EOG)
 GUST_TYPE = SINE
-%
-% Direction of the gust (X_DIR or Y_DIR)
 GUST_DIR = Y_DIR
-%
-% Gust wavelenght (meters)
 GUST_WAVELENGTH= 25.0
-%
-% Number of gust periods
 GUST_PERIODS= 1.0
-%
-% Gust amplitude (m/s)
 GUST_AMPL= 2.37668682
 % Corresponds to 2 deg AoA.
 %
-% Time at which to begin the gust (sec)
 GUST_BEGIN_TIME= 0.0
-%
-% Location at which the gust begins (meters) */
 GUST_BEGIN_LOC= -25.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Far-field boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( airfoil )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% CFL number (stating value for the adaptive CFL number)
 CFL_NUMBER= 10.0
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-grid levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.75
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH_JESPERSEN)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Entropy fix coefficient (0.0 implies no entropy fixing, 1.0 implies scalar
-%                          artificial dissipation)
 ENTROPY_FIX_COEFF= 0.001
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Number of total iterations
 TIME_ITER= 401
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 0
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA0012_inv.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency for physical time steps (dual time)
 OUTPUT_WRT_FREQ= 1000
-%
-%
-% Screen output
 SCREEN_OUTPUT= (TIME_ITER, INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
diff --git a/TestCases/harmonic_balance/HB.cfg b/TestCases/harmonic_balance/HB.cfg
index 62dfb1a84b0..b124ef012b4 100644
--- a/TestCases/harmonic_balance/HB.cfg
+++ b/TestCases/harmonic_balance/HB.cfg
@@ -5,369 +5,128 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2016.20.09                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION,FEM_ELASTICITY, 
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, LINEARIZED, ONE_SHOT_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
+
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER, HARMONIC_BALANCE)
 TIME_MARCHING= HARMONIC_BALANCE
-%
-% Number of time instances (Zones)
 TIME_INSTANCES= 3
-% 
-% Period of Harmonic Balance simulation
 HB_PERIOD= 0.05891103435003335
-%
-% List of frequencies to be resolved for harmonic balance method
 OMEGA_HB = (0,106.69842,-106.69842)
-%
-% Time Step for dual time stepping simulations (s)
-%UNST_TIMESTEP= 0.0023555025613149587
-% 24 steps per period: 0.0024536485013697488
-% 25 steps per period: 0.0023555025613149587
-%
-% Total Physical Time for dual time stepping simulations (s)
-%UNST_TIME= 2.0
-% 10 periods: 0.5888756403287397
-%
-% Number of internal iterations (dual time method)
-%UNST_INT_ITER= 100
-%
-% Type of mesh motion (NONE, FLUTTER, RIGID_ROTATION, RIGID_PITCHING)
+
 GRID_MOVEMENT= RIGID_MOTION
-%
 MOTION_ORIGIN= ( 0.248 0.0 0.0 )
-
 PITCHING_OMEGA= ( 0.0 0.0 106.69842)
-
 PITCHING_AMPL= ( 0.0 0.0 1.01 )
  
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.796
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( farfield )
 %
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
-NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 CFL_NUMBER= 1.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 70000
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (NONE, JACOBI, LINELET)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
-MG_PRE_SMOOTH= ( 2, 2, 2, 2 )
-%
-% Multi-Grid PostSmoothing Level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 1.0
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 1.0
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
-%TIME_DISCRE_FLOW= RUNGE-KUTTA_EXPLICIT
 TIME_DISCRE_FLOW= EULER_IMPLICIT
-%
+
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE, TOTAL_HEAT,
-%                                     MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                     INVERSE_DESIGN_HEATFLUX)
-OBJECTIVE_FUNCTION= DRAG
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
+OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.6
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Adjoint frozen viscosity (NO, YES)
 FROZEN_VISC_CONT= NO
+
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION,
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE,
-%                      FFD_ROTATION)
 DV_KIND= HICKS_HENNE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation
-%	- HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-%	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-%	- PARABOLIC ( 1st digit, 2nd and 3rd digit )
-%	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-%	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= ( 1, 0.5 )
-%
-% Value of the shape deformation deformation
 DV_VALUE= 1.0
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA64A010_inv.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 500
-%
-%
+
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 ); ( 30, 1.0 | airfoil | 0, 0.20 ); ( 30, 1.0 | airfoil | 0, 0.25 ); ( 30, 1.0 | airfoil | 0, 0.30 ); ( 30, 1.0 | airfoil | 0, 0.35 ); ( 30, 1.0 | airfoil | 0, 0.40 ); ( 30, 1.0 | airfoil | 0, 0.45 ); ( 30, 1.0 | airfoil | 0, 0.50 ); ( 30, 1.0 | airfoil | 0, 0.55 ); ( 30, 1.0 | airfoil | 0, 0.60 ); ( 30, 1.0 | airfoil | 0, 0.65 ); ( 30, 1.0 | airfoil | 0, 0.70 ); ( 30, 1.0 | airfoil | 0, 0.75 ); ( 30, 1.0 | airfoil | 0, 0.80 ); ( 30, 1.0 | airfoil | 0, 0.85 ); ( 30, 1.0 | airfoil | 0, 0.90 ); ( 30, 1.0 | airfoil | 0, 0.95 ); ( 30, 1.0 | airfoil | 1, 0.05 ); ( 30, 1.0 | airfoil | 1, 0.10 ); ( 30, 1.0 | airfoil | 1, 0.15 ); ( 30, 1.0 | airfoil | 1, 0.20 ); ( 30, 1.0 | airfoil | 1, 0.25 ); ( 30, 1.0 | airfoil | 1, 0.30 ); ( 30, 1.0 | airfoil | 1, 0.35 ); ( 30, 1.0 | airfoil | 1, 0.40 ); ( 30, 1.0 | airfoil | 1, 0.45 ); ( 30, 1.0 | airfoil | 1, 0.50 ); ( 30, 1.0 | airfoil | 1, 0.55 ); ( 30, 1.0 | airfoil | 1, 0.60 ); ( 30, 1.0 | airfoil | 1, 0.65 ); ( 30, 1.0 | airfoil | 1, 0.70 ); ( 30, 1.0 | airfoil | 1, 0.75 ); ( 30, 1.0 | airfoil | 1, 0.80 ); ( 30, 1.0 | airfoil | 1, 0.85 ); ( 30, 1.0 | airfoil | 1, 0.90 ); ( 30, 1.0 | airfoil | 1, 0.95 )
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.001
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= NONE
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 30, 1.0 | airfoil | 1, 0.75 ) 
-%( 30, 1.0 | airfoil | 1, 0.5 ); ( 30, 1.0 | airfoil | 1, 0.75 ); ( 30, 1.0 | airfoil | 0, 0.5 ); ( 30, 1.0 | airfoil | 0, 0.75 )
-%( 30, 1.0 | airfoil | 1, 0.5 )
-
-
diff --git a/TestCases/harmonic_balance/hb_rans_preconditioning/davis.cfg b/TestCases/harmonic_balance/hb_rans_preconditioning/davis.cfg
index 0010ca1e28a..279b7d9d046 100644
--- a/TestCases/harmonic_balance/hb_rans_preconditioning/davis.cfg
+++ b/TestCases/harmonic_balance/hb_rans_preconditioning/davis.cfg
@@ -5,239 +5,103 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2016.20.09                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION,FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, LINEARIZED, ONE_SHOT_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
+
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER,
-%                      DUAL_TIME_STEPPING-2ND_ORDER, HARMONIC_BALANCE)
 TIME_MARCHING= HARMONIC_BALANCE
-%
-% Number of time instances (Zones)
 TIME_INSTANCES= 7
-%
-% Precondition harmonic balance source term (NO, YES)
 HB_PRECONDITION= YES
-%
-% Period of Harmonic Balance simulation
 HB_PERIOD= 0.057465
-%
-% List of frequencies to be resolved for harmonic balance method
 OMEGA_HB = (0,109.339, 218.678, 328.017,-109.339, -218.678, -328.017)
-%
-%
-% Type of mesh motion (NONE, FLUTTER, RIGID_ROTATION, RIGID_PITCHING)
+
 GRID_MOVEMENT= RIGID_MOTION
-%
 MOTION_ORIGIN= ( 0.25 0.0 0.0)
-
 PITCHING_OMEGA= ( 0.0 0.0 109.933 )
-
 PITCHING_AMPL= ( 0.0 0.0 1.01 )
 
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.796
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 12.56E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 0.992
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES,
-%                                         WEIGHTED_LEAST_SQUARES)
-NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 CFL_NUMBER= 3.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 70000
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (NONE, JACOBI, LINELET)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
-MG_PRE_SMOOTH= ( 2, 2, 2, 2 )
-%
-% Multi-Grid PostSmoothing Level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 1.0
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 1.0
-
 % ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
 %
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the Venkat's limiter (upwind scheme). A larger values decrease
-%             the extent of limiting, values approaching zero cause
-%             lower-order approximation to the solution (0.05 by default)
 VENKAT_LIMITER_COEFF= 0.05
-%
-% 2nd and 4th order artificial dissipation coefficients for
-%     the JST method ( 0.5, 0.02 by default )
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= n64a010_turb.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 500
-%
diff --git a/TestCases/hom_euler/InviscidVortex/2D/Quad32X32_nPoly4/InviscidVortex.cfg b/TestCases/hom_euler/InviscidVortex/2D/Quad32X32_nPoly4/InviscidVortex.cfg
index eb134ab808e..36f985e82b6 100644
--- a/TestCases/hom_euler/InviscidVortex/2D/Quad32X32_nPoly4/InviscidVortex.cfg
+++ b/TestCases/hom_euler/InviscidVortex/2D/Quad32X32_nPoly4/InviscidVortex.cfg
@@ -7,176 +7,79 @@
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 1.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 1.0
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= DIMENSIONAL
 
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
 TIME_DOMAIN=YES
-%
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER,
-%                      DUAL_TIME_STEPPING-2ND_ORDER, TIME_SPECTRAL)
-%TIME_MARCHING= NO
 TIME_MARCHING= TIME_STEPPING
-%
-% Time Step for time accurate simulations (s) -- Only used when UNST_CFL_NUMBER = 0.0
 TIME_STEP= 2.0e-3
-%
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 50.0
-%
-% Unsteady Courant-Friedrichs-Lewy number of the finest grid
 UNST_CFL_NUMBER= 0.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Periodic boundary marker(s) (NONE = no marker)
-% Format: ( periodic marker, donor marker, rotation_center_x, rotation_center_y,
-% rotation_center_z, rotation_angle_x-axis, rotation_angle_y-axis,
-% rotation_angle_z-axis, translation_x, translation_y, translation_z, ... )
 MARKER_PERIODIC= ( PeriodicBottom, PeriodicTop, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 2.0, 0.0, PeriodicLeft, PeriodicRight, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 2.0, 0.0, 0.0)
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 0.2
-%
-% Number of total iterations
 EXT_ITER= 5000
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5 , 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
-%QUADRATURE_FACTOR_CURVED_FEM = 3.0
 QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= CLASSICAL_RK4_EXPLICIT
-%
-% Time discretization. Must be set equal to TIME_DISCRE_FEM_FLOW.
 TIME_DISCRE_FLOW= CLASSICAL_RK4_EXPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -15
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= Quad32X32_nPoly4.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= Quad32X32_nPoly4.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
-%SOLUTION_FILENAME= solution_flow.dat
 SOLUTION_FILENAME= SolInterpolFrom3rdOrder.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency for physical time steps (dual time)
 OUTPUT_WRT_FREQ= 40
-%
diff --git a/TestCases/hom_euler/InviscidVortex/3D/nPoly2_Tets/InviscidVortex.cfg b/TestCases/hom_euler/InviscidVortex/3D/nPoly2_Tets/InviscidVortex.cfg
index d28863f54f2..97ccb4efb2d 100644
--- a/TestCases/hom_euler/InviscidVortex/3D/nPoly2_Tets/InviscidVortex.cfg
+++ b/TestCases/hom_euler/InviscidVortex/3D/nPoly2_Tets/InviscidVortex.cfg
@@ -6,176 +6,80 @@
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 %RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 1.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 1.0
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= DIMENSIONAL
 
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
 TIME_DOMAIN=YES
-%
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER,
-%                      DUAL_TIME_STEPPING-2ND_ORDER, TIME_SPECTRAL)
-%TIME_MARCHING= NO
 TIME_MARCHING= TIME_STEPPING
-%
-% Time Step for time accurate simulations (s) -- Only used when UNST_CFL_NUMBER = 0.0
 TIME_STEP= 2.0e-3
-%
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 50.0
-%
-% Unsteady Courant-Friedrichs-Lewy number of the finest grid
 UNST_CFL_NUMBER= 0.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Periodic boundary marker(s) (NONE = no marker)
-% Format: ( periodic marker, donor marker, rotation_center_x, rotation_center_y,
-% rotation_center_z, rotation_angle_x-axis, rotation_angle_y-axis,
-% rotation_angle_z-axis, translation_x, translation_y, translation_z, ... )
 MARKER_PERIODIC= ( Bottom, Top, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 2.0, Left, Right, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 2.0, 0.0, Back, Front, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 2.0, 0.0, 0.0)
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 0.2
-%
-% Number of total iterations
 EXT_ITER= 5000
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5 , 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
-%QUADRATURE_FACTOR_CURVED_FEM = 3.0
 QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= CLASSICAL_RK4_EXPLICIT
-%
-% Time discretization. Must be set equal to TIME_DISCRE_FEM_FLOW.
 TIME_DISCRE_FLOW= CLASSICAL_RK4_EXPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -15
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= Tets_nPoly2.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= Tets_nPoly2.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
-%SOLUTION_FILENAME= solution_flow.dat
 SOLUTION_FILENAME= SolInterpolFrom3rdOrder.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency for physical time steps (dual time)
 OUTPUT_WRT_FREQ= 100
-%
diff --git a/TestCases/hom_euler/InviscidVortex/3D/nPoly4_Tets/InviscidVortex.cfg b/TestCases/hom_euler/InviscidVortex/3D/nPoly4_Tets/InviscidVortex.cfg
index 96339555967..72525894606 100644
--- a/TestCases/hom_euler/InviscidVortex/3D/nPoly4_Tets/InviscidVortex.cfg
+++ b/TestCases/hom_euler/InviscidVortex/3D/nPoly4_Tets/InviscidVortex.cfg
@@ -6,176 +6,79 @@
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 1.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 1.0
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= DIMENSIONAL
 
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
 TIME_DOMAIN=YES
-%
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER,
-%                      DUAL_TIME_STEPPING-2ND_ORDER, TIME_SPECTRAL)
-%TIME_MARCHING= NO
 TIME_MARCHING= TIME_STEPPING
-%
-% Time Step for time accurate simulations (s) -- Only used when UNST_CFL_NUMBER = 0.0
 TIME_STEP= 1.0e-3
-%
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 50.0
-%
-% Unsteady Courant-Friedrichs-Lewy number of the finest grid
 UNST_CFL_NUMBER= 0.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Periodic boundary marker(s) (NONE = no marker)
-% Format: ( periodic marker, donor marker, rotation_center_x, rotation_center_y,
-% rotation_center_z, rotation_angle_x-axis, rotation_angle_y-axis,
-% rotation_angle_z-axis, translation_x, translation_y, translation_z, ... )
 MARKER_PERIODIC= ( Bottom, Top, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 2.0, Left, Right, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 2.0, 0.0, Back, Front, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 2.0, 0.0, 0.0)
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 0.2
-%
-% Number of total iterations
 EXT_ITER= 5000
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5 , 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
-%QUADRATURE_FACTOR_CURVED_FEM = 3.0
 QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= CLASSICAL_RK4_EXPLICIT
-%
-% Time discretization. Must be set equal to TIME_DISCRE_FEM_FLOW.
 TIME_DISCRE_FLOW= CLASSICAL_RK4_EXPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -15
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= Tets_nPoly4.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= Tets_nPoly4.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
-%SOLUTION_FILENAME= solution_flow.dat
 SOLUTION_FILENAME= SolInterpolFrom3rdOrder.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency for physical time steps (dual time)
 OUTPUT_WRT_FREQ= 100
-%
diff --git a/TestCases/hom_euler/NACA0012_3D_Hybrid_4thOrder/fem_NACA0012.cfg b/TestCases/hom_euler/NACA0012_3D_Hybrid_4thOrder/fem_NACA0012.cfg
index 7cc900eab4e..13f2b44354d 100644
--- a/TestCases/hom_euler/NACA0012_3D_Hybrid_4thOrder/fem_NACA0012.cfg
+++ b/TestCases/hom_euler/NACA0012_3D_Hybrid_4thOrder/fem_NACA0012.cfg
@@ -5,172 +5,84 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.3
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.50
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( Airfoil, Symmetry0, Symmetry1 )
-%
-% Marker of the far field (NONE = no marker)
 MARKER_FAR= ( Farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( Airfoil )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( Airfoil )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( Airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 0.2
-%
-% Number of total iterations
 EXT_ITER= 1000
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5 , 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667 , 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
-% Time discretization. Must be set equal to TIME_DISCRE_FEM_FLOW.
 TIME_DISCRE_FLOW= RUNGE-KUTTA_EXPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= NACA0012_3D_nPoly3.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= NACA0012_3D_nPoly3.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 2500
-%
diff --git a/TestCases/hom_euler/NACA0012_5thOrder/fem_NACA0012.cfg b/TestCases/hom_euler/NACA0012_5thOrder/fem_NACA0012.cfg
index 5ab6174533d..87d1acf4338 100644
--- a/TestCases/hom_euler/NACA0012_5thOrder/fem_NACA0012.cfg
+++ b/TestCases/hom_euler/NACA0012_5thOrder/fem_NACA0012.cfg
@@ -5,180 +5,87 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 %RESTART_SOL= YES
-%
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
 % Mach number (non-dimensional, based on the free-stream values)
-%MACH_NUMBER= 0.63
 MACH_NUMBER= 0.3
-%
-% Angle of attack (degrees)
 AoA= 2.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (NONE = no marker)
 MARKER_FAR= ( farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( airfoil )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( airfoil )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 0.1
-%
-% Number of total iterations
 ITER= 40000
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5 , 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
-%QUADRATURE_FACTOR_CURVED_FEM = 3.0
 QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
-% Time discretization. Must be set equal to TIME_DISCRE_FEM_FLOW.
 TIME_DISCRE_FLOW= RUNGE-KUTTA_EXPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= Naca0012_nPoly4.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= Naca0012_nPoly4.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
-%SOLUTION_FILENAME= solution_flow.dat
 SOLUTION_FILENAME= solution_flow.dat_FullyConverged
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 50000
-%
-%
-% Screen output fields
 SCREEN_OUTPUT = (RMS_DENSITY, RMS_MOMENTUM-X, RMS_ENERGY, LIFT, DRAG)
diff --git a/TestCases/hom_euler/NACA0012_5thOrder/fem_NACA0012_reg.cfg b/TestCases/hom_euler/NACA0012_5thOrder/fem_NACA0012_reg.cfg
index 2a1a25f69ec..f340cedd490 100644
--- a/TestCases/hom_euler/NACA0012_5thOrder/fem_NACA0012_reg.cfg
+++ b/TestCases/hom_euler/NACA0012_5thOrder/fem_NACA0012_reg.cfg
@@ -5,183 +5,87 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
-%RESTART_SOL= NO
 RESTART_SOL= YES
 READ_BINARY_RESTART= NO
-%
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
-%MACH_NUMBER= 0.63
 MACH_NUMBER= 0.3
-%
-% Angle of attack (degrees)
 AoA= 2.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (NONE = no marker)
 MARKER_FAR= ( farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( airfoil )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( airfoil )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 0.1
-%
-% Number of total iterations
 ITER= 11
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5 , 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
-%QUADRATURE_FACTOR_CURVED_FEM = 3.0
 QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Use the lumped mass matrix for steady DGFEM computations (NO, YES)
 USE_LUMPED_MASSMATRIX_DGFEM= YES
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
-% Time discretization. Must be set equal to TIME_DISCRE_FEM_FLOW.
 TIME_DISCRE_FLOW= RUNGE-KUTTA_EXPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= Naca0012_nPoly4.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= Naca0012_nPoly4.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow_naca0012.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 50000
-%
-%
-% Screen output fields
 SCREEN_OUTPUT=(INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
diff --git a/TestCases/hom_euler/Ringleb/Quad100X50_nPoly3/Ringleb.cfg b/TestCases/hom_euler/Ringleb/Quad100X50_nPoly3/Ringleb.cfg
index ef852f53a50..5510644aec0 100644
--- a/TestCases/hom_euler/Ringleb/Quad100X50_nPoly3/Ringleb.cfg
+++ b/TestCases/hom_euler/Ringleb/Quad100X50_nPoly3/Ringleb.cfg
@@ -4,171 +4,78 @@
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 %RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
-%MARKER_EULER= ( LeftBoundary, RightBoundary )
-%
-% Custom boundaries
-%MARKER_CUSTOM= ( BottomBoundary, TopBoundary )
 MARKER_CUSTOM= ( BottomBoundary, LeftBoundary, RightBoundary, TopBoundary )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( LeftBoundary, RightBoundary )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%CFL_NUMBER= 0.2       % For AUSM
-%
-% Number of total iterations
 EXT_ITER= 10000
-%EXT_ITER= 1
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5, 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%RIEMANN_SOLVER_FEM= AUSM
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= Quad100X50_nPoly3.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= Quad100X50_nPoly3.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 5000
-%
 SCREEN_WRT_FREQ_INNER= 100
diff --git a/TestCases/hom_euler/Ringleb/Quad100X50_nPoly3/Ringleb_WallBC.cfg b/TestCases/hom_euler/Ringleb/Quad100X50_nPoly3/Ringleb_WallBC.cfg
index 2e49e978a93..2777cd8b4e5 100644
--- a/TestCases/hom_euler/Ringleb/Quad100X50_nPoly3/Ringleb_WallBC.cfg
+++ b/TestCases/hom_euler/Ringleb/Quad100X50_nPoly3/Ringleb_WallBC.cfg
@@ -4,171 +4,78 @@
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( LeftBoundary, RightBoundary )
-%
-% Custom boundaries
 MARKER_CUSTOM= ( BottomBoundary, TopBoundary )
-%MARKER_CUSTOM= ( BottomBoundary, LeftBoundary, RightBoundary, TopBoundary )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( LeftBoundary, RightBoundary )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%CFL_NUMBER= 0.2       % For AUSM
-%
-% Number of total iterations
 EXT_ITER= 10000
-%EXT_ITER= 1
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5, 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%RIEMANN_SOLVER_FEM= AUSM
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= Quad100X50_nPoly3.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= Quad100X50_nPoly3.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 5000
-%
 SCREEN_WRT_FREQ_INNER= 100
diff --git a/TestCases/hom_euler/Ringleb/Quad100X50_nPoly4/Ringleb.cfg b/TestCases/hom_euler/Ringleb/Quad100X50_nPoly4/Ringleb.cfg
index 63c86040241..7b117f6dbfa 100644
--- a/TestCases/hom_euler/Ringleb/Quad100X50_nPoly4/Ringleb.cfg
+++ b/TestCases/hom_euler/Ringleb/Quad100X50_nPoly4/Ringleb.cfg
@@ -4,171 +4,77 @@
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
-%MARKER_EULER= ( LeftBoundary, RightBoundary )
-%
-% Custom boundaries
-%MARKER_CUSTOM= ( BottomBoundary, TopBoundary )
 MARKER_CUSTOM= ( BottomBoundary, LeftBoundary, RightBoundary, TopBoundary )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( LeftBoundary, RightBoundary )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%CFL_NUMBER= 0.2       % For AUSM
-%
-% Number of total iterations
 EXT_ITER= 10000
-%EXT_ITER= 1
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5, 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%RIEMANN_SOLVER_FEM= AUSM
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= Quad100X50_nPoly4.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= Quad100X50_nPoly4.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 5000
-%
 SCREEN_WRT_FREQ_INNER= 100
diff --git a/TestCases/hom_euler/Ringleb/Quad100X50_nPoly4/Ringleb_WallBC.cfg b/TestCases/hom_euler/Ringleb/Quad100X50_nPoly4/Ringleb_WallBC.cfg
index 4ebb364b64f..071154a66e1 100644
--- a/TestCases/hom_euler/Ringleb/Quad100X50_nPoly4/Ringleb_WallBC.cfg
+++ b/TestCases/hom_euler/Ringleb/Quad100X50_nPoly4/Ringleb_WallBC.cfg
@@ -4,171 +4,78 @@
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( LeftBoundary, RightBoundary )
-%
-% Custom boundaries
 MARKER_CUSTOM= ( BottomBoundary, TopBoundary )
-%MARKER_CUSTOM= ( BottomBoundary, LeftBoundary, RightBoundary, TopBoundary )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( LeftBoundary, RightBoundary )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%CFL_NUMBER= 0.2       % For AUSM
-%
-% Number of total iterations
 EXT_ITER= 10000
-%EXT_ITER= 1
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5, 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%RIEMANN_SOLVER_FEM= AUSM
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= Quad100X50_nPoly4.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= Quad100X50_nPoly4.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 5000
-%
 SCREEN_WRT_FREQ_INNER= 100
diff --git a/TestCases/hom_euler/Ringleb/Quad200X100_nPoly4/Ringleb.cfg b/TestCases/hom_euler/Ringleb/Quad200X100_nPoly4/Ringleb.cfg
index f243de834f1..fb801004899 100644
--- a/TestCases/hom_euler/Ringleb/Quad200X100_nPoly4/Ringleb.cfg
+++ b/TestCases/hom_euler/Ringleb/Quad200X100_nPoly4/Ringleb.cfg
@@ -4,171 +4,77 @@
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
-%MARKER_EULER= ( LeftBoundary, RightBoundary )
-%
-% Custom boundaries
-%MARKER_CUSTOM= ( BottomBoundary, TopBoundary )
 MARKER_CUSTOM= ( BottomBoundary, LeftBoundary, RightBoundary, TopBoundary )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( LeftBoundary, RightBoundary )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%CFL_NUMBER= 0.2       % For AUSM
-%
-% Number of total iterations
 EXT_ITER= 10000
-%EXT_ITER= 1
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5, 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%RIEMANN_SOLVER_FEM= AUSM
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= Quad200X100_nPoly4.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= Quad200X100_nPoly4.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 5000
-%
 SCREEN_WRT_FREQ_INNER= 100
diff --git a/TestCases/hom_euler/Ringleb/Quad200X100_nPoly4/Ringleb_WallBC.cfg b/TestCases/hom_euler/Ringleb/Quad200X100_nPoly4/Ringleb_WallBC.cfg
index a7cae8c8a0e..cb5db14c9f2 100644
--- a/TestCases/hom_euler/Ringleb/Quad200X100_nPoly4/Ringleb_WallBC.cfg
+++ b/TestCases/hom_euler/Ringleb/Quad200X100_nPoly4/Ringleb_WallBC.cfg
@@ -4,171 +4,78 @@
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( LeftBoundary, RightBoundary )
-%
-% Custom boundaries
 MARKER_CUSTOM= ( BottomBoundary, TopBoundary )
-%MARKER_CUSTOM= ( BottomBoundary, LeftBoundary, RightBoundary, TopBoundary )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( LeftBoundary, RightBoundary )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%CFL_NUMBER= 0.2       % For AUSM
-%
-% Number of total iterations
 EXT_ITER= 10000
-%EXT_ITER= 1
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5, 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%RIEMANN_SOLVER_FEM= AUSM
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= Quad200X100_nPoly4.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= Quad200X100_nPoly4.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 5000
-%
 SCREEN_WRT_FREQ_INNER= 100
diff --git a/TestCases/hom_euler/Ringleb/Quad50X50_HalfGeom_nPoly4/Ringleb.cfg b/TestCases/hom_euler/Ringleb/Quad50X50_HalfGeom_nPoly4/Ringleb.cfg
index 47ef84a4909..885873e4d23 100644
--- a/TestCases/hom_euler/Ringleb/Quad50X50_HalfGeom_nPoly4/Ringleb.cfg
+++ b/TestCases/hom_euler/Ringleb/Quad50X50_HalfGeom_nPoly4/Ringleb.cfg
@@ -4,171 +4,77 @@
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
-%MARKER_EULER= ( LeftBoundary, RightBoundary )
-%
-% Custom boundaries
-%MARKER_CUSTOM= ( BottomBoundary, TopBoundary )
 MARKER_CUSTOM= ( BottomBoundary, LeftBoundary, RightBoundary, TopBoundary )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( LeftBoundary, RightBoundary )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%CFL_NUMBER= 0.2       % For AUSM
-%
-% Number of total iterations
 EXT_ITER= 10000
-%EXT_ITER= 1
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5, 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%RIEMANN_SOLVER_FEM= AUSM
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= Quad50X50_HalfGeom_nPoly4.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= Quad50X50_HalfGeom_nPoly4.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 5000
-%
 SCREEN_WRT_FREQ_INNER= 100
diff --git a/TestCases/hom_euler/Ringleb/Quad50X50_HalfGeom_nPoly4/Ringleb_WallBC.cfg b/TestCases/hom_euler/Ringleb/Quad50X50_HalfGeom_nPoly4/Ringleb_WallBC.cfg
index b615c7acf33..090d5249bd8 100644
--- a/TestCases/hom_euler/Ringleb/Quad50X50_HalfGeom_nPoly4/Ringleb_WallBC.cfg
+++ b/TestCases/hom_euler/Ringleb/Quad50X50_HalfGeom_nPoly4/Ringleb_WallBC.cfg
@@ -4,171 +4,78 @@
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( LeftBoundary, RightBoundary )
-%
-% Custom boundaries
 MARKER_CUSTOM= ( BottomBoundary, TopBoundary )
-%MARKER_CUSTOM= ( BottomBoundary, LeftBoundary, RightBoundary, TopBoundary )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( LeftBoundary, RightBoundary )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%CFL_NUMBER= 0.2       % For AUSM
-%
-% Number of total iterations
 EXT_ITER= 10000
-%EXT_ITER= 1
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5, 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%RIEMANN_SOLVER_FEM= AUSM
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= Quad50X50_HalfGeom_nPoly4.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= Quad50X50_HalfGeom_nPoly4.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 5000
-%
 SCREEN_WRT_FREQ_INNER= 100
diff --git a/TestCases/hom_euler/Ringleb/QuadDominantUnstr100X100_HalfGeom_nPoly4/Ringleb.cfg b/TestCases/hom_euler/Ringleb/QuadDominantUnstr100X100_HalfGeom_nPoly4/Ringleb.cfg
index ae18e91cb01..c9220619fca 100644
--- a/TestCases/hom_euler/Ringleb/QuadDominantUnstr100X100_HalfGeom_nPoly4/Ringleb.cfg
+++ b/TestCases/hom_euler/Ringleb/QuadDominantUnstr100X100_HalfGeom_nPoly4/Ringleb.cfg
@@ -4,171 +4,77 @@
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
-%MARKER_EULER= ( LeftBoundary, RightBoundary )
-%
-% Custom boundaries
-%MARKER_CUSTOM= ( BottomBoundary, TopBoundary )
 MARKER_CUSTOM= ( BottomBoundary, LeftBoundary, RightBoundary, TopBoundary )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( LeftBoundary, RightBoundary )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%CFL_NUMBER= 0.2       % For AUSM
-%
-% Number of total iterations
 EXT_ITER= 10000
-%EXT_ITER= 1
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5, 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%RIEMANN_SOLVER_FEM= AUSM
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= QuadDominantUnstr100X100_HalfGeom_nPoly4.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= QuadDominantUnstr100X100_HalfGeom_nPoly4.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 5000
-%
 SCREEN_WRT_FREQ_INNER= 100
diff --git a/TestCases/hom_euler/Ringleb/QuadDominantUnstr100X100_HalfGeom_nPoly4/Ringleb_WallBC.cfg b/TestCases/hom_euler/Ringleb/QuadDominantUnstr100X100_HalfGeom_nPoly4/Ringleb_WallBC.cfg
index 989c9017e5b..392f6199857 100644
--- a/TestCases/hom_euler/Ringleb/QuadDominantUnstr100X100_HalfGeom_nPoly4/Ringleb_WallBC.cfg
+++ b/TestCases/hom_euler/Ringleb/QuadDominantUnstr100X100_HalfGeom_nPoly4/Ringleb_WallBC.cfg
@@ -4,171 +4,78 @@
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( LeftBoundary, RightBoundary )
-%
-% Custom boundaries
 MARKER_CUSTOM= ( BottomBoundary, TopBoundary )
-%MARKER_CUSTOM= ( BottomBoundary, LeftBoundary, RightBoundary, TopBoundary )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( LeftBoundary, RightBoundary )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%CFL_NUMBER= 0.2       % For AUSM
-%
-% Number of total iterations
 EXT_ITER= 10000
-%EXT_ITER= 1
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5, 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%RIEMANN_SOLVER_FEM= AUSM
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= QuadDominantUnstr100X100_HalfGeom_nPoly4.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= QuadDominantUnstr100X100_HalfGeom_nPoly4.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 5000
-%
 SCREEN_WRT_FREQ_INNER= 100
diff --git a/TestCases/hom_euler/Ringleb/Triangle50X50_HalfGeom_nPoly4/Ringleb.cfg b/TestCases/hom_euler/Ringleb/Triangle50X50_HalfGeom_nPoly4/Ringleb.cfg
index 17b35beb82f..db2e805fab2 100644
--- a/TestCases/hom_euler/Ringleb/Triangle50X50_HalfGeom_nPoly4/Ringleb.cfg
+++ b/TestCases/hom_euler/Ringleb/Triangle50X50_HalfGeom_nPoly4/Ringleb.cfg
@@ -4,171 +4,77 @@
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
-%MARKER_EULER= ( LeftBoundary, RightBoundary )
-%
-% Custom boundaries
-%MARKER_CUSTOM= ( BottomBoundary, TopBoundary )
 MARKER_CUSTOM= ( BottomBoundary, LeftBoundary, RightBoundary, TopBoundary )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( LeftBoundary, RightBoundary )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%CFL_NUMBER= 0.2       % For AUSM
-%
-% Number of total iterations
 EXT_ITER= 10000
-%EXT_ITER= 1
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5, 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%RIEMANN_SOLVER_FEM= AUSM
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= TriangleUnstr50X50_HalfGeom_nPoly4.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= TriangleUnstr50X50_HalfGeom_nPoly4.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 5000
-%
 SCREEN_WRT_FREQ_INNER= 100
diff --git a/TestCases/hom_euler/Ringleb/Triangle50X50_HalfGeom_nPoly4/Ringleb_WallBC.cfg b/TestCases/hom_euler/Ringleb/Triangle50X50_HalfGeom_nPoly4/Ringleb_WallBC.cfg
index 50f09adc21a..2178ed57e75 100644
--- a/TestCases/hom_euler/Ringleb/Triangle50X50_HalfGeom_nPoly4/Ringleb_WallBC.cfg
+++ b/TestCases/hom_euler/Ringleb/Triangle50X50_HalfGeom_nPoly4/Ringleb_WallBC.cfg
@@ -4,171 +4,78 @@
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( LeftBoundary, RightBoundary )
-%
-% Custom boundaries
 MARKER_CUSTOM= ( BottomBoundary, TopBoundary )
-%MARKER_CUSTOM= ( BottomBoundary, LeftBoundary, RightBoundary, TopBoundary )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( LeftBoundary, RightBoundary )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%CFL_NUMBER= 0.2       % For AUSM
-%
-% Number of total iterations
 EXT_ITER= 10000
-%EXT_ITER= 1
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5, 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%RIEMANN_SOLVER_FEM= AUSM
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= TriangleUnstr50X50_HalfGeom_nPoly4.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= TriangleUnstr50X50_HalfGeom_nPoly4.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 5000
-%
 SCREEN_WRT_FREQ_INNER= 100
diff --git a/TestCases/hom_euler/Sphere_4thOrder_Hexa/fem_Sphere.cfg b/TestCases/hom_euler/Sphere_4thOrder_Hexa/fem_Sphere.cfg
index ddff9cd0bf0..0984ff6b139 100644
--- a/TestCases/hom_euler/Sphere_4thOrder_Hexa/fem_Sphere.cfg
+++ b/TestCases/hom_euler/Sphere_4thOrder_Hexa/fem_Sphere.cfg
@@ -5,172 +5,84 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.3
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( Sphere )
-%
-% Marker of the far field (NONE = no marker)
 MARKER_FAR= ( Farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( Sphere )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( Sphere )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( Sphere )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 0.2
-%
-% Number of total iterations
 EXT_ITER= 100
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
-% QUADRATURE_FACTOR_CURVED_FEM = 3.0
 QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
-% Time discretization. Must be set equal to TIME_DISCRE_FEM_FLOW.
 TIME_DISCRE_FLOW= RUNGE-KUTTA_EXPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= SphereCoarse_4thOrder.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= SphereCoarse_4thOrder.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
diff --git a/TestCases/hom_euler/Sphere_4thOrder_Tet/fem_Sphere.cfg b/TestCases/hom_euler/Sphere_4thOrder_Tet/fem_Sphere.cfg
index fd8c8f50147..495aab30a6a 100644
--- a/TestCases/hom_euler/Sphere_4thOrder_Tet/fem_Sphere.cfg
+++ b/TestCases/hom_euler/Sphere_4thOrder_Tet/fem_Sphere.cfg
@@ -5,176 +5,84 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.3
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( Sphere )
-%
-% Marker of the far field (NONE = no marker)
 MARKER_FAR= ( Farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( Sphere )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( Sphere )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( Sphere )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 0.2
-%
-% Number of total iterations
 EXT_ITER= 400
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5 , 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
-%QUADRATURE_FACTOR_CURVED_FEM = 3.0
 QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
-% Time discretization. Must be set equal to TIME_DISCRE_FEM_FLOW.
 TIME_DISCRE_FLOW= RUNGE-KUTTA_EXPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-%MESH_FILENAME= SphereNPoly3.su2
-MESH_FILENAME= Sphere_4thOrder.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= Sphere_4thOrder.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
-%SOLUTION_FILENAME= solution_flow.dat
 SOLUTION_FILENAME= SolInterpolFrom3rdOrder.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 500
-%
diff --git a/TestCases/hom_euler/SubsonicChannel/nPoly1/fem_SubsonicChannel.cfg b/TestCases/hom_euler/SubsonicChannel/nPoly1/fem_SubsonicChannel.cfg
index 04b8b30643f..384960cd63c 100644
--- a/TestCases/hom_euler/SubsonicChannel/nPoly1/fem_SubsonicChannel.cfg
+++ b/TestCases/hom_euler/SubsonicChannel/nPoly1/fem_SubsonicChannel.cfg
@@ -5,183 +5,85 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( LowerWall, UpperWall )
-%
-% Inlet boundary marker(s) (NONE = no marker) 
-% Format: ( inlet marker, total temperature, total pressure, flow_direction_x,
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
 MARKER_INLET= ( Inlet, 300.0, 120193.0, 1.0, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
 MARKER_OUTLET= ( Outlet, 101325.0 )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( LowerWall )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( LowerWall )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( LowerWall )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.5
-%CFL_NUMBER= 0.2       % For AUSM
-%
-% Number of total iterations
 EXT_ITER= 180000
-%EXT_ITER= 1
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5, 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%RIEMANN_SOLVER_FEM= AUSM
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= SubsonicChannel_nPoly1.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= SubsonicChannel_nPoly1.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 5000
-%
 SCREEN_WRT_FREQ_INNER= 100
diff --git a/TestCases/hom_euler/SubsonicChannel/nPoly1/fem_SubsonicChannel_Farfield.cfg b/TestCases/hom_euler/SubsonicChannel/nPoly1/fem_SubsonicChannel_Farfield.cfg
index 0d16c30adc5..64811ea7125 100644
--- a/TestCases/hom_euler/SubsonicChannel/nPoly1/fem_SubsonicChannel_Farfield.cfg
+++ b/TestCases/hom_euler/SubsonicChannel/nPoly1/fem_SubsonicChannel_Farfield.cfg
@@ -5,176 +5,84 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( LowerWall, UpperWall )
-%
-% Marker of the far field (NONE = no marker)
 MARKER_FAR= ( Inlet, Outlet )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( LowerWall )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( LowerWall )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( LowerWall )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.5
-%CFL_NUMBER= 0.2       % For AUSM
-%
-% Number of total iterations
 EXT_ITER= 180000
-%EXT_ITER= 1
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5, 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%RIEMANN_SOLVER_FEM= AUSM
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= SubsonicChannel_nPoly1.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= SubsonicChannel_nPoly1.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 5000
-%
 SCREEN_WRT_FREQ_INNER= 100
diff --git a/TestCases/hom_euler/SubsonicChannel/nPoly2/fem_SubsonicChannel.cfg b/TestCases/hom_euler/SubsonicChannel/nPoly2/fem_SubsonicChannel.cfg
index 6a883ae3f88..72873ff0d2b 100644
--- a/TestCases/hom_euler/SubsonicChannel/nPoly2/fem_SubsonicChannel.cfg
+++ b/TestCases/hom_euler/SubsonicChannel/nPoly2/fem_SubsonicChannel.cfg
@@ -5,183 +5,86 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 %RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( LowerWall, UpperWall )
-%
-% Inlet boundary marker(s) (NONE = no marker) 
-% Format: ( inlet marker, total temperature, total pressure, flow_direction_x,
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
 MARKER_INLET= ( Inlet, 300.0, 120193.0, 1.0, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
 MARKER_OUTLET= ( Outlet, 101325.0 )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( LowerWall )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( LowerWall )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( LowerWall )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.5
-%CFL_NUMBER= 0.2       % For AUSM
-%
-% Number of total iterations
 EXT_ITER= 180000
-%EXT_ITER= 1
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5, 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%RIEMANN_SOLVER_FEM= AUSM
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= SubsonicChannel_nPoly2.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= SubsonicChannel_nPoly2.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 5000
-%
 SCREEN_WRT_FREQ_INNER= 100
diff --git a/TestCases/hom_euler/SubsonicChannel/nPoly2/fem_SubsonicChannel_Farfield.cfg b/TestCases/hom_euler/SubsonicChannel/nPoly2/fem_SubsonicChannel_Farfield.cfg
index 226031ccf28..73bc5b5b02b 100644
--- a/TestCases/hom_euler/SubsonicChannel/nPoly2/fem_SubsonicChannel_Farfield.cfg
+++ b/TestCases/hom_euler/SubsonicChannel/nPoly2/fem_SubsonicChannel_Farfield.cfg
@@ -5,176 +5,83 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( LowerWall, UpperWall )
-%
-% Marker of the far field (NONE = no marker)
 MARKER_FAR= ( Inlet, Outlet )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( LowerWall )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( LowerWall )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( LowerWall )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.5
-%CFL_NUMBER= 0.2       % For AUSM
-%
-% Number of total iterations
 EXT_ITER= 180000
-%EXT_ITER= 1
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5, 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%RIEMANN_SOLVER_FEM= AUSM
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= SubsonicChannel_nPoly2.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= SubsonicChannel_nPoly2.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 5000
-%
 SCREEN_WRT_FREQ_INNER= 100
diff --git a/TestCases/hom_euler/SubsonicChannel/nPoly4/fem_SubsonicChannel.cfg b/TestCases/hom_euler/SubsonicChannel/nPoly4/fem_SubsonicChannel.cfg
index 63139113bba..3c9f10b0afc 100644
--- a/TestCases/hom_euler/SubsonicChannel/nPoly4/fem_SubsonicChannel.cfg
+++ b/TestCases/hom_euler/SubsonicChannel/nPoly4/fem_SubsonicChannel.cfg
@@ -5,183 +5,85 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( LowerWall, UpperWall )
-%
-% Inlet boundary marker(s) (NONE = no marker) 
-% Format: ( inlet marker, total temperature, total pressure, flow_direction_x,
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
 MARKER_INLET= ( Inlet, 300.0, 120193.0, 1.0, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
 MARKER_OUTLET= ( Outlet, 101325.0 )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( LowerWall )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( LowerWall )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( LowerWall )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.5
-%CFL_NUMBER= 0.2       % For AUSM
-%
-% Number of total iterations
 EXT_ITER= 180000
-%EXT_ITER= 1
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5, 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%RIEMANN_SOLVER_FEM= AUSM
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= SubsonicChannel_nPoly4.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= SubsonicChannel_nPoly4.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 5000
-%
 SCREEN_WRT_FREQ_INNER= 100
diff --git a/TestCases/hom_euler/SubsonicChannel/nPoly4/fem_SubsonicChannel_Farfield.cfg b/TestCases/hom_euler/SubsonicChannel/nPoly4/fem_SubsonicChannel_Farfield.cfg
index e1e0b18d4c5..88c753a0bf2 100644
--- a/TestCases/hom_euler/SubsonicChannel/nPoly4/fem_SubsonicChannel_Farfield.cfg
+++ b/TestCases/hom_euler/SubsonicChannel/nPoly4/fem_SubsonicChannel_Farfield.cfg
@@ -5,176 +5,82 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH_MOMENT= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( LowerWall, UpperWall )
-%
-% Marker of the far field (NONE = no marker)
 MARKER_FAR= ( Inlet, Outlet )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( LowerWall )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( LowerWall )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( LowerWall )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.5
-%CFL_NUMBER= 0.2       % For AUSM
-%
-% Number of total iterations
 EXT_ITER= 180000
-%EXT_ITER= 1
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5, 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%RIEMANN_SOLVER_FEM= AUSM
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= SubsonicChannel_nPoly4.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= SubsonicChannel_nPoly4.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 5000
-%
 SCREEN_WRT_FREQ_INNER= 100
diff --git a/TestCases/hom_navierstokes/CylinderViscous/nPoly3/fem_Cylinder_reg.cfg b/TestCases/hom_navierstokes/CylinderViscous/nPoly3/fem_Cylinder_reg.cfg
index cff1ce4c7ed..6af8bc91e95 100644
--- a/TestCases/hom_navierstokes/CylinderViscous/nPoly3/fem_Cylinder_reg.cfg
+++ b/TestCases/hom_navierstokes/CylinderViscous/nPoly3/fem_Cylinder_reg.cfg
@@ -5,176 +5,86 @@
 % Author: Edwin van der Weide                                                  %
 % Institution: University of Twente                                            %
 % Date: 2016.07.15                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_NAVIER_STOKES
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.2
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 40
-%
-% Reynolds length (1 m, 1 inch by default)
 REYNOLDS_LENGTH= 1.0
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
-%
+
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( Cylinder, 0.0 )
-%
-% Marker of the far field (NONE = no marker)
 MARKER_FAR= ( Farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( Cylinder )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( Cylinder )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( Cylinder )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 0.05
-%
-% Number of total iterations
 ITER= 11
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%
-% Use the lumped mass matrix for steady DGFEM computations (NO, YES)
 USE_LUMPED_MASSMATRIX_DGFEM= YES
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
+
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= CylinderViscous_nPoly3.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= CylinderViscous_nPoly3.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-%
-% Screen output fields
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
diff --git a/TestCases/hom_navierstokes/FlatPlate/nPoly4/lam_flatplate_reg.cfg b/TestCases/hom_navierstokes/FlatPlate/nPoly4/lam_flatplate_reg.cfg
index e59db6fc51d..f06e96808a9 100644
--- a/TestCases/hom_navierstokes/FlatPlate/nPoly4/lam_flatplate_reg.cfg
+++ b/TestCases/hom_navierstokes/FlatPlate/nPoly4/lam_flatplate_reg.cfg
@@ -5,185 +5,82 @@
 % Author: Thomas D. Economon	                                               %
 % Institution: Stanford University                                             %
 % Date: 2013.09.30                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_NAVIER_STOKES
-%
-% Specify turbulence model (NONE, SA)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.2
-%
-% Angle of attack (degrees, only for compressible flows)
 AoA= 0.0
-%
-% Side-slip angle (degrees, only for compressible flows)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 297.62
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 1301233.166
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 0.3048
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 0.3048
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_VEL_EQ_ONE
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes (no-slip), constant heat flux wall  marker(s) (NONE = no marker)
-% Format: ( marker name, constant heat flux (J/m^2), ... )
 MARKER_HEATFLUX= ( wall, 0.0 )
-%
-% Symmetry boundary marker(s) (NONE = no marker)
 MARKER_SYM= ( symmetry )
-%
-% Inlet boundary marker(s) (NONE = no marker) 
-% Format: ( inlet marker, total temperature, total pressure, flow_direction_x,
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
 MARKER_INLET= ( inlet, 300.0, 100000.0, 1.0, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
 MARKER_OUTLET= ( outlet, 97250.0, farfield, 97250.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( wall )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( wall )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.0
-%
-% Number of total iterations
 ITER= 26
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%
-% Factor for the symmetrizing terms in the DG FEM discretization (1.0 by default)
 THETA_INTERIOR_PENALTY_DG_FEM = 1.0
-%
-% Use the lumped mass matrix for steady DGFEM computations (NO, YES)
 USE_LUMPED_MASSMATRIX_DGFEM= YES
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
-%TIME_DISCRE_FEM_FLOW= CLASSICAL_RK4_EXPLICIT
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -15
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_flatplate_64x64_p4.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1000
-%
-% 
-% Screen output fields
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
-
diff --git a/TestCases/hom_navierstokes/SphereViscous/nPoly3_QuadDominant/fem_Sphere_reg.cfg b/TestCases/hom_navierstokes/SphereViscous/nPoly3_QuadDominant/fem_Sphere_reg.cfg
index 73cbbdafd59..77f351ca468 100644
--- a/TestCases/hom_navierstokes/SphereViscous/nPoly3_QuadDominant/fem_Sphere_reg.cfg
+++ b/TestCases/hom_navierstokes/SphereViscous/nPoly3_QuadDominant/fem_Sphere_reg.cfg
@@ -5,178 +5,86 @@
 % Author: Edwin van der Weide                                                  %
 % Institution: University of Twente                                            %
 % Date: 2016.07.15                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_NAVIER_STOKES
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.2
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 40
-%
-% Reynolds length (1 m, 1 inch by default)
 REYNOLDS_LENGTH= 1.0
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 3.141592654
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
-%
+
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( Sphere, 0.0 )
-%
-% Marker of the far field (NONE = no marker)
 MARKER_FAR= ( Farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( Sphere )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( Sphere )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( Sphere )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 0.15
-%
-% Number of total iterations
 ITER= 11
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%
-% Use the lumped mass matrix for steady DGFEM computations (NO, YES)
 USE_LUMPED_MASSMATRIX_DGFEM= YES
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
+
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= SphereViscous_QuadDominant_Coarse_nPoly3.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= SphereViscous_QuadDominant_Coarse_nPoly3.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%SOLUTION_FILENAME= InterpolFromNPoly1.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 2500
-%
-%
-% Screen output
 SCREEN_OUTPUT = (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
diff --git a/TestCases/hom_navierstokes/SphereViscous/nPoly3_QuadDominant/fem_Sphere_reg_ADER.cfg b/TestCases/hom_navierstokes/SphereViscous/nPoly3_QuadDominant/fem_Sphere_reg_ADER.cfg
index 1b6ae5d3117..6ad166bb421 100644
--- a/TestCases/hom_navierstokes/SphereViscous/nPoly3_QuadDominant/fem_Sphere_reg_ADER.cfg
+++ b/TestCases/hom_navierstokes/SphereViscous/nPoly3_QuadDominant/fem_Sphere_reg_ADER.cfg
@@ -5,201 +5,97 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_NAVIER_STOKES
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 %RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.2
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 40
-%
-% Reynolds length (1 m, 1 inch by default)
 REYNOLDS_LENGTH= 1.0
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 3.141592654
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( Sphere, 0.0 )
-%
-% Marker of the far field (NONE = no marker)
 MARKER_FAR= ( Farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( Sphere )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( Sphere )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( Sphere )
 
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
 TIME_DOMAIN=YES
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER,
-%                      DUAL_TIME_STEPPING-2ND_ORDER, TIME_SPECTRAL)
 TIME_MARCHING= TIME_STEPPING
-%
-% Time Step for time accurate simulations (s) -- Only used when UNST_CFL_NUMBER = 0.0
 TIME_STEP= 2.0e-6
-%
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 50.0
-%
-% Unsteady Courant-Friedrichs-Lewy number of the finest grid
 UNST_CFL_NUMBER= 0.15
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 0.125
-%
-% Number of total iterations
 TIME_ITER= 11
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= ADER_DG
-%
-% Time discretization. Must be set equal to TIME_DISCRE_FEM_FLOW.
 TIME_DISCRE_FLOW= ADER_DG
-%
-% Number of time DOFs for the predictor step of ADER-DG (2 by default)
 TIME_DOFS_ADER_DG= 3
-% Factor applied during quadrature in time for ADER-DG. (2.0 by default)
 QUADRATURE_FACTOR_TIME_ADER_DG = 2.0
-%
-% Type of discretization used in the predictor step of ADER-DG (ADER_ALIASED_PREDICTOR by default)
 ADER_PREDICTOR= ADER_ALIASED_PREDICTOR
-%ADER_PREDICTOR= ADER_NON_ALIASED_PREDICTOR
-% Number of time levels for time accurate local time stepping. (1 by default, max. allowed 15)
 LEVELS_TIME_ACCURATE_LTS= 4
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -15
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= SphereViscous_QuadDominant_Coarse_nPoly3.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= SphereViscous_QuadDominant_Coarse_nPoly3.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1000
-%
-% 
-% Screen output
 SCREEN_OUTPUT = (TIME_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
-
diff --git a/TestCases/hom_navierstokes/UnsteadyCylinder/nPoly4/fem_unst_cylinder.cfg b/TestCases/hom_navierstokes/UnsteadyCylinder/nPoly4/fem_unst_cylinder.cfg
index 9dd811269b9..156556b8f5f 100644
--- a/TestCases/hom_navierstokes/UnsteadyCylinder/nPoly4/fem_unst_cylinder.cfg
+++ b/TestCases/hom_navierstokes/UnsteadyCylinder/nPoly4/fem_unst_cylinder.cfg
@@ -5,195 +5,95 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_NAVIER_STOKES
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
 RESTART_ITER=1
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.1
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 100.0
-%
-% Reynolds length (in meters)
 REYNOLDS_LENGTH= 1.0
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( Cylinder, 0.0 )
-%
-% Marker of the far field (NONE = no marker)
 MARKER_FAR= ( Farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( Cylinder )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( Cylinder )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( Cylinder )
 
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Enable time dependent simulation
 TIME_DOMAIN=YES
-%
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER,
-%                      DUAL_TIME_STEPPING-2ND_ORDER, TIME_SPECTRAL)
 TIME_MARCHING= TIME_STEPPING
-%
-% Time Step for time accurate simulations (s) -- Only used when UNST_CFL_NUMBER = 0.0
 TIME_STEP= 1e-6
-%
 MAX_TIME= 50.0
-%
-% Unsteady Courant-Friedrichs-Lewy number of the finest grid
 UNST_CFL_NUMBER= 0.05
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 0.125
-%
-% Number of total iterations
 TIME_ITER= 12
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= CLASSICAL_RK4_EXPLICIT
-%
-% Time discretization. Must be set equal to TIME_DISCRE_FEM_FLOW.
 TIME_DISCRE_FLOW= CLASSICAL_RK4_EXPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -15
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= CylinderViscous_nPoly4.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= CylinderViscous_nPoly4.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency for physical time steps (dual time)
 OUTPUT_WRT_FREQ= 10000
-%
-%
-% Screen output
 SCREEN_OUTPUT= (TIME_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
diff --git a/TestCases/hom_navierstokes/UnsteadyCylinder/nPoly4/fem_unst_cylinder_ADER.cfg b/TestCases/hom_navierstokes/UnsteadyCylinder/nPoly4/fem_unst_cylinder_ADER.cfg
index b3a86d84c14..f46bd2a6935 100644
--- a/TestCases/hom_navierstokes/UnsteadyCylinder/nPoly4/fem_unst_cylinder_ADER.cfg
+++ b/TestCases/hom_navierstokes/UnsteadyCylinder/nPoly4/fem_unst_cylinder_ADER.cfg
@@ -5,208 +5,99 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_NAVIER_STOKES
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
 RESTART_ITER= 1
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.1
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 100.0
-%
-% Reynolds length (in meters)
 REYNOLDS_LENGTH= 1.0
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( Cylinder, 0.0 )
-%
-% Marker of the far field (NONE = no marker)
 MARKER_FAR= ( Farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( Cylinder )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( Cylinder )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( Cylinder )
 
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Time dependent problem
 TIME_DOMAIN= YES
-%
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER,
-%                      DUAL_TIME_STEPPING-2ND_ORDER, TIME_SPECTRAL)
 TIME_MARCHING= TIME_STEPPING
-%
-% Time Step for time accurate simulations (s) -- Only used when UNST_CFL_NUMBER = 0.0
 TIME_STEP= 1.6e-5
-%
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 50.0
-%
-% Unsteady Courant-Friedrichs-Lewy number of the finest grid
 UNST_CFL_NUMBER= 0.05
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 0.125
-%
-% Number of total iterations
 TIME_ITER= 11
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= ADER_DG
-%
-% Time discretization. Must be set equal to TIME_DISCRE_FEM_FLOW.
 TIME_DISCRE_FLOW= ADER_DG
-%
-% Number of time DOFs for the predictor step of ADER-DG (2 by default)
 TIME_DOFS_ADER_DG= 3
-% Factor applied during quadrature in time for ADER-DG. (2.0 by default)
 QUADRATURE_FACTOR_TIME_ADER_DG = 2.0
-%
-% Type of discretization used in the predictor step of ADER-DG (ADER_ALIASED_PREDICTOR by default)
 ADER_PREDICTOR= ADER_ALIASED_PREDICTOR
-%ADER_PREDICTOR= ADER_NON_ALIASED_PREDICTOR
-% Number of time levels for time accurate local time stepping. (1 by default, max. allowed 15)
 LEVELS_TIME_ACCURATE_LTS= 8
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -15
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= CylinderViscous_nPoly4.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= CylinderViscous_nPoly4.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency for physical time steps (dual time)
 OUTPUT_WRT_FREQ= 10000
-%
-%
-% Screen output
-SCREEN_OUTPUT= (TIME_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
-
+SCREEN_OUTPUT= (TIME_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
\ No newline at end of file
diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index f8d2cdd68f0..2127f2371dd 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -3,7 +3,7 @@
 ## \file hybrid_regression.py
 #  \brief Python script for automated regression testing of SU2 examples
 #  \author A. Aranake, A. Campos, T. Economon, T. Lukaczyk, S. Padron
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/hybrid_regression_AD.py b/TestCases/hybrid_regression_AD.py
index b7fcea8fab4..8c23b8fb20d 100644
--- a/TestCases/hybrid_regression_AD.py
+++ b/TestCases/hybrid_regression_AD.py
@@ -3,7 +3,7 @@
 ## \file hybrid_regression_AD.py
 #  \brief Python script for automated regression testing of SU2 examples
 #  \author A. Aranake, A. Campos, T. Economon, T. Lukaczyk, S. Padron
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/TestCases/incomp_euler/naca0012/incomp_NACA0012.cfg b/TestCases/incomp_euler/naca0012/incomp_NACA0012.cfg
index 41688fc1c0f..8c7ffe8925c 100644
--- a/TestCases/incomp_euler/naca0012/incomp_NACA0012.cfg
+++ b/TestCases/incomp_euler/naca0012/incomp_NACA0012.cfg
@@ -5,187 +5,85 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 09/18/2011                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                           
 SOLVER= INC_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
+
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
-% Initial density for incompressible flows (1.2886 kg/m^3 by default)
 INC_DENSITY_INIT= 998.2
-%
-% Initial velocity for incompressible flows (1.0,0,0 m/s by default)
 INC_VELOCITY_INIT= ( 1.775, 0.0, 0.0 )
-%
-% List of inlet types for incompressible flows. List length must
-% match number of inlet markers. Options: VELOCITY_INLET, PRESSURE_INLET.
 INC_INLET_TYPE= VELOCITY_INLET
-%
-% Damping coefficient for iterative updates at pressure inlets. (0.1 by default)
 INC_INLET_DAMPING= 0.1
-%
-% List of outlet types for incompressible flows. List length must
-% match number of outlet markers. Options: PRESSURE_OUTLET, MASS_FLOW_OUTLET
 INC_OUTLET_TYPE= PRESSURE_OUTLET
-%
-% Damping coefficient for iterative updates at mass flow outlets. (0.1 by default)
 INC_OUTLET_DAMPING= 0.1
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( airfoil, lower_wall, upper_wall )
-%
-% Incompressible: (inlet marker, NULL, velocity magnitude, flow_direction_x,
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
 MARKER_INLET= ( inlet, 0.0, 1.775, 1.0, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
 MARKER_OUTLET= ( outlet, 0.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 3.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 9999
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.85
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.85
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= FDS
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.0002
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.04 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 50
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA0012_5deg_6814.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 200
-%
-%
-% Screen output fields
 SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_VELOCITY-X, LIFT, DRAG)
-
diff --git a/TestCases/incomp_euler/nozzle/inv_nozzle.cfg b/TestCases/incomp_euler/nozzle/inv_nozzle.cfg
index 8f6d0c7398f..ec0ea824baf 100644
--- a/TestCases/incomp_euler/nozzle/inv_nozzle.cfg
+++ b/TestCases/incomp_euler/nozzle/inv_nozzle.cfg
@@ -4,212 +4,93 @@
 % Case description: Inv. inc. nozzle with pressure inlet and mass flow outlet  %
 % Author: Thomas D. Economon                                                   %
 % Date: 2018.11.30                                                             %
-% File Version 7.4.0 "Blackbird"                                                  %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= INC_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
 
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
-% Density model within the incompressible flow solver.
-% Options are CONSTANT (default), BOUSSINESQ, or VARIABLE. If VARIABLE,
-% an appropriate fluid model must be selected.
 INC_DENSITY_MODEL= CONSTANT
-%
-% Solve the energy equation in the incompressible flow solver
 INC_ENERGY_EQUATION = NO
-%
-% Initial density for incompressible flows (1.2886 kg/m^3 by default)
 INC_DENSITY_INIT= 1.0
-%
-% Initial velocity for incompressible flows (1.0,0,0 m/s by default)
 INC_VELOCITY_INIT= ( 1.0, 0.0, 0.0 )
-%
-% Initial temperature for incompressible flows that include the
-% energy equation (288.15 K by default). Value is ignored if
-% INC_ENERGY_EQUATION is false.
 INC_TEMPERATURE_INIT= 288.15
-%
-% List of inlet types for incompressible flows. List length must
-% match number of inlet markers. Options: VELOCITY_INLET, PRESSURE_INLET.
 INC_INLET_TYPE= PRESSURE_INLET
-%
-% Damping coefficient for iterative updates at pressure inlets. (0.1 by default)
 INC_INLET_DAMPING= 0.1
-%
-% List of outlet types for incompressible flows. List length must
-% match number of outlet markers. Options: PRESSURE_OUTLET, MASS_FLOW_OUTLET
 INC_OUTLET_TYPE= MASS_FLOW_OUTLET
-%
-% Damping coefficient for iterative updates at mass flow outlets. (0.1 by default)
 INC_OUTLET_DAMPING= 0.1
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference area for non-dimensional force coefficients (0 implies automatic
-% calculation) (m^2 or in^2)
 REF_AREA= 0.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( sides )
-%
-% Inlet boundary marker(s) with the following formats (NONE = no marker)
-% Total Conditions: (inlet marker, total temp, total pressure, flow_direction_x,
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-% Mass Flow: (inlet marker, density, velocity magnitude, flow_direction_x,
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-% Inc. Velocity: (inlet marker, temperature, velocity magnitude, flow_direction_x,
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-% Inc. Pressure: (inlet marker, temperature, total pressure, flow_direction_x,
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
 MARKER_INLET= ( inlet, 288.15, 1.0, 1.0, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Compressible: ( outlet marker, back pressure (static thermodynamic), ... )
-% Inc. Pressure: ( outlet marker, back pressure (static gauge in Pa), ... )
-% Inc. Mass Flow: ( outlet marker, mass flow target (kg/s), ... )
 MARKER_OUTLET= ( outlet, 1.5 )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( sides )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( sides )
-%
-% Marker(s) of the surface that is going to be analyzed in detail (massflow, average pressure, distortion, etc)
 MARKER_ANALYZE = ( outlet, inlet )
-%
-% Method to compute the average value in MARKER_ANALYZE (AREA, MASSFLUX).
 MARKER_ANALYZE_AVERAGE = AREA
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% CFL number (initial value for the adaptive CFL number)
 CFL_NUMBER= 15.0
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-grid levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.95
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.95
 
 % ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
 %
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW, FDS)
 CONV_NUM_METHOD_FLOW= FDS
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Number of total iterations
 ITER= 9999
-%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_nozzle_inv.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 50
-% 
-% Screen output fields
 SCREEN_OUTPUT = (INNER_ITER, RMS_PRESSURE, RMS_VELOCITY-X, LIFT, DRAG)
-
diff --git a/TestCases/incomp_navierstokes/bend/lam_bend.cfg b/TestCases/incomp_navierstokes/bend/lam_bend.cfg
index ff86b3b2bbb..02226a59427 100755
--- a/TestCases/incomp_navierstokes/bend/lam_bend.cfg
+++ b/TestCases/incomp_navierstokes/bend/lam_bend.cfg
@@ -9,250 +9,95 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               TNE2_EULER, TNE2_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= INC_NAVIER_STOKES
-%
-% Specify turbulence model (NONE, SA, SST)
 KIND_TURB_MODEL= NONE
 %
 % Mathematical problem (DIRECT, ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
-% Density model within the incompressible flow solver.
-% Options are CONSTANT (default), BOUSSINESQ, or VARIABLE. If VARIABLE,
-% an appropriate fluid model must be selected.
 INC_DENSITY_MODEL= CONSTANT
-%
-% Solve the energy equation in the incompressible flow solver
 INC_ENERGY_EQUATION = NO
-%
-% Initial density for incompressible flows
-% (1.2886 kg/m^3 by default (air), 998.2 Kg/m^3 (water))
 INC_DENSITY_INIT= 1.2886
-%
-% Initial velocity for incompressible flows (1.0,0,0 m/s by default)
 INC_VELOCITY_INIT= ( 0.1, 0.0, 0.0 )
-%
-% Initial temperature for incompressible flows that include the
-% energy equation (288.15 K by default). Value is ignored if
-% INC_ENERGY_EQUATION is false.
 INC_TEMPERATURE_INIT= 288.15
-%
-% Non-dimensionalization scheme for incompressible flows. Options are
-% INITIAL_VALUES (default), REFERENCE_VALUES, or DIMENSIONAL.
-% INC_*_REF values are ignored unless REFERENCE_VALUES is chosen.
 INC_NONDIM= INITIAL_VALUES
-%
-% Reference density for incompressible flows (1.0 kg/m^3 by default)
 INC_DENSITY_REF= 1.0
-%
-% Reference velocity for incompressible flows (1.0 m/s by default)
 INC_VELOCITY_REF= 1.0
-%
-% Reference temperature for incompressible flows that include the
-% energy equation (1.0 K by default)
 INC_TEMPERATURE_REF = 1.0
-%
-% List of inlet types for incompressible flows. List length must
-% match number of inlet markers. Options: VELOCITY_INLET, PRESSURE_INLET.
 INC_INLET_TYPE= VELOCITY_INLET
-%
-% Damping coefficient for iterative updates at pressure inlets. (0.1 by default)
 INC_INLET_DAMPING= 0.1
-%
-% List of outlet types for incompressible flows. List length must
-% match number of outlet markers. Options: PRESSURE_OUTLET, MASS_FLOW_OUTLET
 INC_OUTLET_TYPE= PRESSURE_OUTLET
-%
-% Damping coefficient for iterative updates at mass flow outlets. (0.1 by default)
 INC_OUTLET_DAMPING= 0.1
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY, POLYNOMIAL_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.716E-5
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation (m or in)
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment (m or in)
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation) (m^2 or in^2)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes (no-slip), constant heat flux wall  marker(s) (NONE = no marker)
-% Format: ( marker name, constant heat flux (J/m^2), ... )
 MARKER_HEATFLUX= ( WALL1, 0.0, WALL2, 0.0 )
-%
-% Inlet boundary marker(s) with the following formats (NONE = no marker)
-% Inc. Pressure: (inlet marker, temperature, total pressure, flow_direction_x,
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
 MARKER_INLET= ( INLET, 288.15, 0.1, 1.0, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Compressible: ( outlet marker, back pressure (static thermodynamic), ... )
-% Inc. Pressure: ( outlet marker, back pressure (static gauge in Pa), ... )
-% Inc. Mass Flow: ( outlet marker, mass flow target (kg/s), ... )
 MARKER_OUTLET= ( OUTLET, 0.0 )
-%
-% Symmetry boundary marker(s) (NONE = no marker)
 MARKER_SYM= ( SYMMETRY )
-%
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( INLET, OUTLET, WALL1, WALL2, SYMMETRY )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( INLET, OUTLET, WALL1, WALL2, SYMMETRY )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1e2
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER_JACOBI, 
-%                                                      SMOOTHER_ILU0, SMOOTHER_LUSGS, 
-%                                                      SMOOTHER_LINELET)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU0, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid Cycle (0 = V cycle, 1 = W Cycle)
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= FDS
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Number of total iterations
 ITER= 11
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_bend_coarse.cgns
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= CGNS
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1000
-%
 SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_VELOCITY-X, LIFT, DRAG)
diff --git a/TestCases/incomp_navierstokes/buoyancy_cavity/lam_buoyancy_cavity.cfg b/TestCases/incomp_navierstokes/buoyancy_cavity/lam_buoyancy_cavity.cfg
index 57f75787315..04fdbd4a5f2 100644
--- a/TestCases/incomp_navierstokes/buoyancy_cavity/lam_buoyancy_cavity.cfg
+++ b/TestCases/incomp_navierstokes/buoyancy_cavity/lam_buoyancy_cavity.cfg
@@ -2,265 +2,119 @@
 %                                                                              %
 % SU2 configuration file                                                       %
 % Case description: Buoyancy-driven flow inside a cavity                       %
-% Author: Thomas D. Economon						       %
+% Author: Thomas D. Economon                                                   %
 % Date: 2018.06.10                                                             %
-% File Version 7.4.0 "Blackbird"                                                  %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= INC_NAVIER_STOKES
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
+
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
-% Density model within the incompressible flow solver.
-% Options are CONSTANT (default), BOUSSINESQ, or VARIABLE. If VARIABLE,
-% an appropriate fluid model must be selected.
 INC_DENSITY_MODEL= VARIABLE
-%
-% Solve the energy equation in the incompressible flow solver
 INC_ENERGY_EQUATION = YES
 %
-% Initial density for incompressible flows (1.2886 kg/m^3 by default)
 % Uncomment a density below for a desired Rayleigh number
 %INC_DENSITY_INIT= 0.00018903539834  % Ra ~ 1e3
 %INC_DENSITY_INIT= 0.00059778241716  % Ra ~ 1e4
 %INC_DENSITY_INIT= 0.00189035398341  % Ra ~ 1e5
 INC_DENSITY_INIT= 0.00597782417156  % Ra ~ 1e6
 %
-% Initial velocity for incompressible flows (1.0,0,0 m/s by default)
 INC_VELOCITY_INIT= ( 1.0, 0.0, 0.0 )
-%
-% Initial temperature for incompressible flows that include the
-% energy equation (288.15 K by default). Value is ignored if
-% INC_ENERGY_EQUATION is false.
 INC_TEMPERATURE_INIT= 288.15
 
 % ---- IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
-% Fluid model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS,
-%              CONSTANT_DENSITY, INC_IDEAL_GAS)
 FLUID_MODEL= INC_IDEAL_GAS
-%
-% Specific heat at constant pressure, Cp (1004.703 J/kg*K (air)).
-% Incompressible fluids with energy eqn. only (CONSTANT_DENSITY, INC_IDEAL_GAS).
 SPECIFIC_HEAT_CP= 1004.703
-%
-% Molecular weight for an incompressible ideal gas (28.96 g/mol (air) default)
-% Incompressible fluids with energy eqn. only (CONSTANT_DENSITY, INC_IDEAL_GAS).
 MOLECULAR_WEIGHT= 28.96
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.716e-5
 
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
-% Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL).
 CONDUCTIVITY_MODEL= CONSTANT_CONDUCTIVITY
-%
-% Molecular Thermal Conductivity that would be constant (0.0257 by default)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.0246295028571
 
 % ----------------------- BODY FORCE DEFINITION -------------------------------%
 %
-% Apply a body force as a source term (NO, YES)
 BODY_FORCE= YES
-%
-% Vector of body force values (BodyForce_X, BodyForce_Y, BodyForce_Z)
 BODY_FORCE_VECTOR= ( 0.0, -9.81, 0.0 )
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes (no-slip), constant heat flux wall  marker(s) (NONE = no marker)
-% Format: ( marker name, constant heat flux (J/m^2), ... )
 MARKER_HEATFLUX= ( upper, 0.0, lower, 0.0 )
-%
-% Navier-Stokes (no-slip), isothermal wall marker(s) (NONE = no marker)
-% Format: ( marker name, constant wall temperature (K), ... )
 MARKER_ISOTHERMAL= ( left, 461.04, right, 115.26 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( upper, left, right, lower )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( NONE )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1e2
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 15.0, 1e10)
-%
-% Maximum Delta Time in local time stepping simulations
 MAX_DELTA_TIME= 1E6
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.8
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= FDS
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_cavity_65x65.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 100
-%
-%
-% Screen output fields
 SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_TEMPERATURE, LIFT, DRAG)
 
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
-%
-% Geometrical bounds (Y coordinate) for the wing geometry analysis or
-% fuselage evaluation (X coordinate).
 GEO_BOUNDS= ( 0.499, 0.501)
diff --git a/TestCases/incomp_navierstokes/cylinder/incomp_cylinder.cfg b/TestCases/incomp_navierstokes/cylinder/incomp_cylinder.cfg
index 2e226bff625..43008838809 100644
--- a/TestCases/incomp_navierstokes/cylinder/incomp_cylinder.cfg
+++ b/TestCases/incomp_navierstokes/cylinder/incomp_cylinder.cfg
@@ -5,182 +5,86 @@
 % Author: Francisco Palacios						                           %
 % Institution: Stanford University                                             %
 % Date: 2012.03.14                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                           
 SOLVER= INC_NAVIER_STOKES
-%
-% If Navier-Stokes, kind of turbulent model (NONE, SA)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
 
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
-% Initial density for incompressible flows (1.2886 kg/m^3 by default)
 INC_DENSITY_INIT= 998.2
-%
-% Initial velocity for incompressible flows (1.0,0,0 m/s by default)
 INC_VELOCITY_INIT= ( 0.000008, 0.0, 0.0 )
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 0.798E-3
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
+
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( cylinder, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( cylinder )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( cylinder )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 5000
-%
-% Coefficient for the Venkat's limiter. A larger values decrease the extent of limiting,
-%             values approaching zero cause lower-order approximation to the solution.
-%             Recomend value for VENKATAKRISHNAN limiter ~0.5
-%             Recomend value for VENKATAKRISHNAN_WANG limiter ~0.05
 VENKAT_LIMITER_COEFF= 0.01
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.75
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= FDS
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.04 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_cylinder_lam.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 100
-%
-% Screen output fields
 SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_VELOCITY-X, LIFT, DRAG)
-
diff --git a/TestCases/incomp_navierstokes/cylinder/poly_cylinder.cfg b/TestCases/incomp_navierstokes/cylinder/poly_cylinder.cfg
index 13328b81314..67168dd50f6 100644
--- a/TestCases/incomp_navierstokes/cylinder/poly_cylinder.cfg
+++ b/TestCases/incomp_navierstokes/cylinder/poly_cylinder.cfg
@@ -5,286 +5,117 @@
 %                   custom fluid using polynomial fluid models.                %
 % Author: Thomas D. Economon                                                   %
 % Date: 2018.12.02                                                             %
-% File Version 7.4.0 "Blackbird"                                                  %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                           
 SOLVER= INC_NAVIER_STOKES
-%
-% If Navier-Stokes, kind of turbulent model (NONE, SA)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
+
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
-% Density model within the incompressible flow solver.
-% Options are CONSTANT (default), BOUSSINESQ, or VARIABLE. If VARIABLE,
-% an appropriate fluid model must be selected.
 INC_DENSITY_MODEL= VARIABLE
-%
-% Solve the energy equation in the incompressible flow solver
 INC_ENERGY_EQUATION = YES
-%
-% Initial density for incompressible flows (1.2886 kg/m^3 by default)
 INC_DENSITY_INIT= 0.000210322
-%
-% Initial velocity for incompressible flows (1.0,0,0 m/s by default)
 INC_VELOCITY_INIT= ( 3.40297, 0.0, 0.0 )
-%
-% Initial temperature for incompressible flows that include the
-% energy equation (288.15 K by default). Value is ignored if
-% INC_ENERGY_EQUATION is false.
 INC_TEMPERATURE_INIT= 288.15
-%
-% Non-dimensionalization scheme for incompressible flows. Options are
-% INITIAL_VALUES (default), REFERENCE_VALUES, or DIMENSIONAL.
-% INC_*_REF values are ignored unless REFERENCE_VALUES is chosen.
 INC_NONDIM= DIMENSIONAL
 
 % ---- IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
-% Different gas model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS)
 FLUID_MODEL= INC_IDEAL_GAS_POLY
-%
-% Specific heat at constant pressure, Cp (1004.703 J/kg*K (air)).
-% Incompressible fluids with energy eqn. only (CONSTANT_DENSITY, INC_IDEAL_GAS).
 SPECIFIC_HEAT_CP= 1004.703
-%
-% Molecular weight for an incompressible ideal gas (28.96 g/mol (air) default)
 MOLECULAR_WEIGHT= 28.96
-%
-% Temperature polynomial coefficients (up to quartic) for specific heat Cp.
-% Format -> Cp(T) : b0 + b1*T + b2*T^2 + b3*T^3 + b4*T^4
 CP_POLYCOEFFS= ( 1004.703, 0.1, 0.0, 0.0, 0.0)
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= POLYNOMIAL_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.7893e-05
-%
-% Temperature polynomial coefficients (up to quartic) for viscosity.
-% Format -> Mu(T) : b0 + b1*T + b2*T^2 + b3*T^3 + b4*T^4
 MU_POLYCOEFFS= (1.7893e-05, 1e-8, 0.0, 0.0, 0.0)
 
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
-% Laminar Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL,
-% POLYNOMIAL_CONDUCTIVITY).
 CONDUCTIVITY_MODEL= POLYNOMIAL_CONDUCTIVITY
-%
-% Molecular Thermal Conductivity that would be constant (0.0257 by default)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.0257
-%
-% Laminar Prandtl number (0.72 (air), only for CONSTANT_PRANDTL)
 PRANDTL_LAM= 0.72
-%
-% Temperature polynomial coefficients (up to quartic) for conductivity.
-% Format -> Kt(T) : b0 + b1*T + b2*T^2 + b3*T^3 + b4*T^4
 KT_POLYCOEFFS= (0.0257, 1e-5, 0.0, 0.0, 0.0)
-%
-% Definition of the turbulent thermal conductivity model for RANS
-% (CONSTANT_PRANDTL_TURB by default, NONE).
 TURBULENT_CONDUCTIVITY_MODEL= CONSTANT_PRANDTL_TURB
-%
-% Turbulent Prandtl number (0.9 (air) by default)
 PRANDTL_TURB= 0.90
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_ISOTHERMAL= ( cylinder, 1000.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( cylinder )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( cylinder )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1000.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 10.0, 10000.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 1000
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.8
-
 % ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
 %
-% Coefficient for the Venkat's limiter (upwind scheme). A larger values decrease
-%             the extent of limiting, values approaching zero cause
-%             lower-order approximation to the solution (0.05 by default)
 VENKAT_LIMITER_COEFF= 0.05
-%
-% 1st order artificial dissipation coefficients for
-%     the Lax–Friedrichs method ( 0.15 by default )
 LAX_SENSOR_COEFF= 0.15
-%
-% 2nd and 4th order artificial dissipation coefficients for
-%     the JST method ( 0.5, 0.02 by default )
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= FDS
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -14
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 %
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_cylinder_lam.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-%
-% Screen output fields
 SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_TEMPERATURE, LIFT, DRAG, TOTAL_HEATFLUX)
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/BC_HeatTransfer.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/BC_HeatTransfer.cfg
index ccda9f380a7..f022d02a736 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/BC_HeatTransfer.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/BC_HeatTransfer.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Robert Bosch GmbH                                               %
 % Date: 2020.12.15                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/DA_configMaster.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/DA_configMaster.cfg
index aa405f0aeed..914d10383f8 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/DA_configMaster.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/DA_configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                           %
 % Institution: Robert Bosch GmbH                                                %
 % Date: 2020.12.15                                                              %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
@@ -19,16 +19,11 @@ MARKER_CHT_INTERFACE= ( fluid_pin1_interface, solid_pin1_interface, fluid_pin2_i
 %
 CONV_RESIDUAL_MINVAL= -26
 %
-% Number of total iterations
 OUTER_ITER= 3000
-%
-%CHT_ROBIN= NO
-%
 SCREEN_OUTPUT= (OUTER_ITER, BGS_ADJ_PRESSURE[0], BGS_ADJ_TEMPERATURE[0], BGS_ADJ_TEMPERATURE[1])
 SCREEN_WRT_FREQ_OUTER= 100
 %
 HISTORY_OUTPUT= ( ITER, BGS_RES[0], BGS_RES[1], RMS_RES[0], RMS_RES[1] )
-%
 OUTPUT_FILES= ( RESTART, PARAVIEW_MULTIBLOCK )
 OUTPUT_WRT_FREQ= 1000
 %
@@ -36,37 +31,25 @@ MESH_FILENAME= 2D-PinArray_FFD.su2
 MESH_FORMAT= SU2
 %
 SOLUTION_ADJ_FILENAME= restart_adj
-%
+
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
 FFD_TOLERANCE= 1E-10
 FFD_ITERATIONS= 500
 %
-% FFD box definition: 2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (BOX,  0.0029772,0.0,0.0,  0.0081772,0.0,0.0  0.0081772,0.0026,0.0,  0.0029772,0.0026,0.0, 0.0,0.0,0.0,  0.0,0.0,0.0  0.0,0.0,0.0,  0.0,0.0,0.0 )
 %
-% FFD box degree: 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= (8, 1, 0)
 %
-% Surface grid continuity at the intersection with the faces of the FFD boxes.
-% To keep a particular level of surface continuity, SU2 automatically freezes the right
-% number of control point planes (NO_DERIVATIVE, 1ST_DERIVATIVE, 2ND_DERIVATIVE, USER_INPUT)
 FFD_CONTINUITY= NO_DERIVATIVE
-%
+
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-%DV_KIND= FFD_SETTING
 DV_KIND= FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D
 %
-% Marker of the surface in which we are going apply the shape deformation
 MARKER_SYM= ( fluid_symmetry  )
 DV_MARKER= ( fluid_pin2_interface, solid_pin2_interface, fluid_symmetry )
 %
-% Parameters of the shape deformation
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-%DV_PARAM= ( 1.0 )
 DV_PARAM= \
 ( BOX, 0, 1, 0.0, 1.0);\
 ( BOX, 1, 1, 0.0, 1.0);\
@@ -78,10 +61,8 @@ DV_PARAM= \
 ( BOX, 7, 1, 0.0, 1.0);\
 ( BOX, 8, 1, 0.0, 1.0)
 %
-% Value of the shape deformation
-%DV_VALUE= 1.0
 DV_VALUE= 1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0
-%
+
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
 DEFORM_LINEAR_SOLVER= FGMRES
@@ -94,9 +75,6 @@ DEFORM_LINEAR_SOLVER_ITER= 1000
 DEFORM_CONSOLE_OUTPUT= YES
 DEFORM_STIFFNESS_TYPE= WALL_DISTANCE
 %
-% Deformation coefficient (linear elasticity limits from -1.0 to 0.5, a larger
-% value is also possible)
-% !!! What is this doing !!!
 DEFORM_COEFF = 1E6
 %
 DEFINITION_DV= \
@@ -109,5 +87,3 @@ DEFINITION_DV= \
 ( 19, 1.0 | fluid_pin2_interface, solid_pin2_interface, fluid_symmetry | BOX, 6, 1, 0.0, 1.0 );\
 ( 19, 1.0 | fluid_pin2_interface, solid_pin2_interface, fluid_symmetry | BOX, 7, 1, 0.0, 1.0 );\
 ( 19, 1.0 | fluid_pin2_interface, solid_pin2_interface, fluid_symmetry | BOX, 8, 1, 0.0, 1.0 )
-
-%DEFORM_MESH= YES
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/FD_configMaster.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/FD_configMaster.cfg
index d448a4f34d6..d9bb6ed2dd0 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/FD_configMaster.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/FD_configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                           %
 % Institution: Robert Bosch GmbH                                                %
 % Date: 2020.12.15                                                              %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
@@ -22,9 +22,6 @@ CONV_RESIDUAL_MINVAL= -26
 % FOR FAST RUNING REGRESSION TEST ONLY!
 % FOR GADIENT VALIDATION USE OUTER_ITER= 3000!
 OUTER_ITER= 101
-
-%
-%CHT_ROBIN= NO
 %
 SCREEN_OUTPUT= ( WALL_TIME, OUTER_ITER, BGS_PRESSURE[0], BGS_TEMPERATURE[0], BGS_TEMPERATURE[1], STREAMWISE_MASSFLOW[0], STREAMWISE_DP[0], AVG_TEMPERATURE[1] )
 SCREEN_WRT_FREQ_OUTER= 100
@@ -45,52 +42,26 @@ SOLUTION_ADJ_FILENAME= restart_adj
 RESTART_FILENAME= restart
 CONV_FILENAME= history
 TABULAR_FORMAT= CSV
-%
+
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
 FFD_TOLERANCE= 1E-10
 FFD_ITERATIONS= 500
 %
-% FFD box definition: 2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (BOX,  0.0029772,0.0,0.0,  0.0081772,0.0,0.0  0.0081772,0.0026,0.0,  0.0029772,0.0026,0.0, 0.0,0.0,0.0,  0.0,0.0,0.0  0.0,0.0,0.0,  0.0,0.0,0.0 )
 %
-% FFD box degree: 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= (8, 1, 0)
 %
-% Surface grid continuity at the intersection with the faces of the FFD boxes.
-% To keep a particular level of surface continuity, SU2 automatically freezes the right
-% number of control point planes (NO_DERIVATIVE, 1ST_DERIVATIVE, 2ND_DERIVATIVE, USER_INPUT)
 FFD_CONTINUITY= NO_DERIVATIVE
 %
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
 DV_KIND= FFD_SETTING
-%DV_KIND= FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D
-%
-% Marker of the surface in which we are going apply the shape deformation
 MARKER_SYM= ( fluid_symmetry  )
 DV_MARKER= ( fluid_pin2_interface, solid_pin2_interface, fluid_symmetry )
-%
-% Parameters of the shape deformation
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
 DV_PARAM= ( 1.0 )
-%DV_PARAM= \
-%( BOX, 0, 1, 0.0, 1.0);\
-%( BOX, 1, 1, 0.0, 1.0);\
-%( BOX, 2, 1, 0.0, 1.0);\
-%( BOX, 3, 1, 0.0, 1.0);\
-%( BOX, 4, 1, 0.0, 1.0);\
-%( BOX, 5, 1, 0.0, 1.0);\
-%( BOX, 6, 1, 0.0, 1.0);\
-%( BOX, 7, 1, 0.0, 1.0);\
-%( BOX, 8, 1, 0.0, 1.0)
-%
-% Value of the shape deformation
 DV_VALUE= 1.0
-%DV_VALUE= 1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0
-%
+
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
 DEFORM_LINEAR_SOLVER= FGMRES
@@ -103,9 +74,6 @@ DEFORM_LINEAR_SOLVER_ITER= 1000
 DEFORM_CONSOLE_OUTPUT= YES
 DEFORM_STIFFNESS_TYPE= WALL_DISTANCE
 %
-% Deformation coefficient (linear elasticity limits from -1.0 to 0.5, a larger
-% value is also possible)
-% !!! What is this doing !!!
 DEFORM_COEFF = 1E6
 %
 % For gradient validation uncomment the other DV's!
@@ -120,8 +88,6 @@ DEFINITION_DV= \
 %( 19, 1.0 | fluid_pin2_interface, solid_pin2_interface, fluid_symmetry | BOX, 7, 1, 0.0, 1.0 );\
 %( 19, 1.0 | fluid_pin2_interface, solid_pin2_interface, fluid_symmetry | BOX, 8, 1, 0.0, 1.0 )
 
-%DEFORM_MESH= YES
-
 OPT_OBJECTIVE= AVG_TOTALTEMP
 FIN_DIFF_STEP= 1e-8
 NZONES=2
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configFluid.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configFluid.cfg
index 1c2e83b46e0..6f866eadaf6 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configFluid.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configFluid.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Robert Bosch GmbH                                               %
 % Date: 2020.12.15                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configMaster.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configMaster.cfg
index e20f5b4503d..db829877167 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configMaster.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                           %
 % Institution: Robert Bosch GmbH                                                %
 % Date: 2020.12.15                                                              %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
@@ -19,11 +19,8 @@ MARKER_CHT_INTERFACE= ( fluid_pin1_interface, solid_pin1_interface, fluid_pin2_i
 %
 CONV_RESIDUAL_MINVAL= -26
 %
-% Number of total iterations
 OUTER_ITER= 4000
 %
-%CHT_ROBIN= NO
-%
 SCREEN_OUTPUT= ( OUTER_ITER, BGS_PRESSURE[0], BGS_TEMPERATURE[0], BGS_TEMPERATURE[1], STREAMWISE_MASSFLOW[0], STREAMWISE_DP[0], AVG_TEMPERATURE[1], SURFACE_MASSFLOW[0] )
 SCREEN_WRT_FREQ_OUTER= 100
 %
@@ -34,43 +31,25 @@ OUTPUT_WRT_FREQ= 1000
 %
 MESH_FILENAME= 2D-PinArray_FFD.su2
 MESH_FORMAT= SU2
-%
+
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
 FFD_TOLERANCE= 1E-10
 FFD_ITERATIONS= 500
 %
-% FFD box definition: 2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (BOX,  0.0029772,0.0,0.0,  0.0081772,0.0,0.0  0.0081772,0.0026,0.0,  0.0029772,0.0026,0.0, 0.0,0.0,0.0,  0.0,0.0,0.0  0.0,0.0,0.0,  0.0,0.0,0.0 )
 %
-% FFD box degree: 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= (8, 1, 0)
 %
-% Surface grid continuity at the intersection with the faces of the FFD boxes.
-% To keep a particular level of surface continuity, SU2 automatically freezes the right
-% number of control point planes (NO_DERIVATIVE, 1ST_DERIVATIVE, 2ND_DERIVATIVE, USER_INPUT)
 FFD_CONTINUITY= NO_DERIVATIVE
-%
+
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Config options for writing the FFD-box into the mesh.
-% Comment these options if they appear elsewhere in the .cfg file.
-%DV_KIND= FFD_SETTING
-%DV_PARAM= ( 1.0 )
-%DV_VALUE= 1.0
-%MESH_FILENAME= 2D-PinArray.su2
-%MESH_OUT_FILENAME= 2D-PinArray_FFD.su2
 MARKER_SYM= ( fluid_symmetry  )
 
 DV_KIND= FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( fluid_pin2_interface, solid_pin2_interface, fluid_symmetry )
 %
-% Parameters of the shape deformation
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
 DV_PARAM= \
 ( BOX, 0, 1, 0.0, 1.0);\
 ( BOX, 1, 1, 0.0, 1.0);\
@@ -81,10 +60,8 @@ DV_PARAM= \
 ( BOX, 6, 1, 0.0, 1.0);\
 ( BOX, 7, 1, 0.0, 1.0);\
 ( BOX, 8, 1, 0.0, 1.0)
-%
-% Value of the shape deformation
 DV_VALUE= 1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0
-%
+
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
 DEFORM_LINEAR_SOLVER= FGMRES
@@ -97,9 +74,6 @@ DEFORM_LINEAR_SOLVER_ITER= 1000
 DEFORM_CONSOLE_OUTPUT= YES
 DEFORM_STIFFNESS_TYPE= WALL_DISTANCE
 %
-% Deformation coefficient (linear elasticity limits from -1.0 to 0.5, a larger
-% value is also possible)
-% !!! What is this doing !!!
 DEFORM_COEFF = 1E6
 %
 DEFINITION_DV= \
@@ -112,5 +86,3 @@ DEFINITION_DV= \
 ( 19, 1.0 | fluid_pin2_interface, solid_pin2_interface, fluid_symmetry | BOX, 6, 1, 0.0, 1.0 );\
 ( 19, 1.0 | fluid_pin2_interface, solid_pin2_interface, fluid_symmetry | BOX, 7, 1, 0.0, 1.0 );\
 ( 19, 1.0 | fluid_pin2_interface, solid_pin2_interface, fluid_symmetry | BOX, 8, 1, 0.0, 1.0 )
-
-%DEFORM_MESH= YES
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configSolid.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configSolid.cfg
index 0a5cce0773f..377699c079f 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configSolid.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configSolid.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Robert Bosch GmbH                                               %
 % Date: 2020.12.15                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/of_grad_findiff.csv.ref b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/of_grad_findiff.csv.ref
index 51f3fad3680..82730a5fe1e 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/of_grad_findiff.csv.ref
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/of_grad_findiff.csv.ref
@@ -1,2 +1,2 @@
 "VARIABLE"      , "AVG_DENSITY[0]", "AVG_ENTHALPY[0]", "AVG_NORMALVEL[0]", "DRAG[0]"       , "EFFICIENCY[0]" , "FORCE_X[0]"    , "FORCE_Y[0]"    , "FORCE_Z[0]"    , "LIFT[0]"       , "MOMENT_X[0]"   , "MOMENT_Y[0]"   , "MOMENT_Z[0]"   , "SIDEFORCE[0]"  , "SURFACE_MACH[0]", "SURFACE_MASSFLOW[0]", "SURFACE_MOM_DISTORTION[0]", "SURFACE_PRESSURE_DROP[0]", "SURFACE_SECONDARY[0]", "SURFACE_SECOND_OVER_UNIFORM[0]", "SURFACE_STATIC_PRESSURE[0]", "SURFACE_STATIC_TEMPERATURE[0]", "SURFACE_TOTAL_PRESSURE[0]", "SURFACE_TOTAL_TEMPERATURE[0]", "SURFACE_UNIFORMITY[0]", "AVG_TEMPERATURE[1]", "MAXIMUM_HEATFLUX[1]", "TOTAL_HEATFLUX[1]", "FINDIFF_STEP"  
-0               , 0.0             , -100000.01639127731, -1.1101999999881826e-08, 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , -0.0399999991462785, 0.0                , -2.1099999997220564      , 0.0                     , 2.1799999999627673  , 3.8000000007754053            , 319.9999980552093         , -39.999997625272954          , 318.0000007318995        , -39.999997625272954         , -1.400000004814217   , -139.99999737279722, 0.0                , -540.0000077315781, 1e-08           
+0               , 0.0             , -100000.01639127731, -1.1103000000496327e-08, 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , -0.0399999991462785, 3.3309999998872306e-08, -2.1099999997220564      , 0.0                     , 2.1799999999627673  , 3.8000000007754053            , 319.9999980552093         , -39.999997625272954          , 318.0000007318995        , -39.999997625272954         , -1.400000004814217   , -139.99999737279722, 0.0                , -540.0000077315781, 1e-08           
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configFluid.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configFluid.cfg
index 7927df53201..cfa54a86b52 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configFluid.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configFluid.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Robert Bosch GmbH                                               %
 % Date: 07.06.2019                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configMaster.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configMaster.cfg
index b49a68ea08e..5325519c672 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configMaster.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                           %
 % Institution: Robert Bosch GmbH                                                %
 % Date: 2020.12.15                                                              %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
@@ -21,7 +21,6 @@ MARKER_CHT_INTERFACE= (fluid_bottom_interface, solid_bottom_interface, fluid_pin
 OUTER_ITER = 31
 %
 CONV_RESIDUAL_MINVAL= -26
-%
 SCREEN_OUTPUT= (OUTER_ITER, BGS_PRESSURE[0], BGS_TEMPERATURE[0], BGS_TEMPERATURE[1], STREAMWISE_MASSFLOW[0], STREAMWISE_DP[0], AVG_TEMPERATURE[1], TOTAL_HEATFLUX[0] )
 SCREEN_WRT_FREQ_OUTER= 100
 %
@@ -30,7 +29,6 @@ HISTORY_OUTPUT= ( ITER, RMS_RES[0], RMS_RES[1], STREAMWISE_PERIODIC[0], FLOW_COE
 OUTPUT_FILES= (RESTART, PARAVIEW_MULTIBLOCK)
 OUTPUT_WRT_FREQ= 2500
 %
-% Mesh input file
 MESH_FILENAME= 3D_chtPinArray_coarse.su2
 %
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configSolid.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configSolid.cfg
index 859ae62aa5e..6961daef9fc 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configSolid.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configSolid.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Robert Bosch GmbH                                               %
 % Date: 07.06.2019                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configFluid.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configFluid.cfg
index 882dd2a2650..051efb7f9fd 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configFluid.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configFluid.cfg
@@ -4,7 +4,7 @@
 % Case description: Unit Cell flow around pin array (fluid)                    %
 % Author: T. Kattmann                                                          %
 % Date: 2022.02.10                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configMaster.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configMaster.cfg
index aa59323e839..d5329424e79 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configMaster.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                           %
 % Institution: None                                                             %
 % Date: 2022.02.10                                                              %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
@@ -51,41 +51,20 @@ MESH_FILENAME= 2D-PinArray.su2
 FFD_TOLERANCE= 1E-10
 FFD_ITERATIONS= 500
 %
-% FFD box definition: 2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (BOX,   0.0029772, 0.0,     0.0,   0.0081772, 0.0,     0.0,   0.0081772, 0.00322, 0.0,    0.0029772, 0.00322, 0.0,   0.0,0.0,0.0,   0.0,0.0,0.0   0.0,0.0,0.0,   0.0,0.0,0.0 ); \
            (FRONTBOX,  -0.0026,    0.00322, 0.0,   0.0026,    0.00322, 0.0,   0.0026,    0.0,     0.0,   -0.0026,    0.0,     0.0,   0.0,0.0,0.0,   0.0,0.0,0.0   0.0,0.0,0.0,   0.0,0.0,0.0 ); \
             (BACKBOX,   0.0085544, 0.00322, 0.0,   0.0137544, 0.00322, 0.0,   0.0137544, 0.0,     0.0,    0.0085544, 0.0,     0.0,   0.0,0.0,0.0,   0.0,0.0,0.0   0.0,0.0,0.0,   0.0,0.0,0.0 )
 %
-% FFD box degree: 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= (8, 8, 0); (8, 8, 0); (8, 8, 0)
-%
-% Surface grid continuity at the intersection with the faces of the FFD boxes.
-% To keep a particular level of surface continuity, SU2 automatically freezes the right
-% number of control point planes (NO_DERIVATIVE, 1ST_DERIVATIVE, 2ND_DERIVATIVE, USER_INPUT)
 FFD_CONTINUITY= USER_INPUT
-%
-% BEZIER, BSPLINE_UNIFORM
-%FFD_BLENDING= BEZIER
 FFD_BLENDING= BSPLINE_UNIFORM
 FFD_BSPLINE_ORDER= 4,3,2
-%
+
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Config options for writing the FFD-box into the mesh.
-% Comment these options if they appear elsewhere in the .cfg file.
-%DV_KIND= FFD_SETTING
-%DV_PARAM= ( 1.0 )
-%DV_VALUE= 1.0
-
 DV_KIND= FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= fluid_pin2_interface, solid_pin2_interface, fluid_pin1_interface, solid_pin1_interface, fluid_pin3_interface, solid_pin3_interface, fluid_inlet, solid_pin1_inlet, fluid_outlet, solid_pin3_outlet
-%
-% Parameters of the shape deformation
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
+
 DV_PARAM= \
 ( BOX, 1, 5, 0.0, 1.0);\
 ( BOX, 2, 5, 0.0, 1.0);\
@@ -94,10 +73,8 @@ DV_PARAM= \
 ( BOX, 5, 5, 0.0, 1.0);\
 ( BOX, 6, 5, 0.0, 1.0);\
 ( BOX, 7, 5, 0.0, 1.0)
-%
-% Value of the shape deformation
 DV_VALUE=0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0
-%
+
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
 DEFORM_LINEAR_SOLVER= FGMRES
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configSolid.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configSolid.cfg
index 9e590f5e7c7..b0c3c4eb25f 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configSolid.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configSolid.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: None                                                            %
 % Date: 2022.02.10                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/pipeSlice_3d/sp_pipeSlice_3d_dp_hf_tp.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/pipeSlice_3d/sp_pipeSlice_3d_dp_hf_tp.cfg
index e71ed2646b7..bb4f244001c 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/pipeSlice_3d/sp_pipeSlice_3d_dp_hf_tp.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/pipeSlice_3d/sp_pipeSlice_3d_dp_hf_tp.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Robert Bosch GmbH                                               %
 % Date: 2020.12.14                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -48,7 +48,6 @@ MARKER_ANALYZE_AVERAGE = AREA
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 %CFL_NUMBER= 1e10
 CFL_NUMBER= 50000
-%CFL_ADAPT= YES
 CFL_ADAPT= NO
 CFL_ADAPT_PARAM= ( 0.5, 10, 15.0, 1e30 )
 ITER= 15000
@@ -72,7 +71,7 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 CONV_RESIDUAL_MINVAL= -24
 CONV_STARTITER= 10
 %
-% ------------------------- INPUT/OUTPUT INFORMATION ----------------------.su2
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
 MESH_FILENAME= pipe1cell3D.su2
 %
@@ -80,6 +79,5 @@ OUTPUT_FILES= ( RESTART, PARAVIEW_MULTIBLOCK, SURFACE_TECPLOT_ASCII )
 OUTPUT_WRT_FREQ= 1000
 %
 HISTORY_OUTPUT= ( RMS_RES, FLOW_COEFF, STREAMWISE_PERIODIC, LINSOL )
-%
 SCREEN_OUTPUT= ( INNER_ITER, RMS_PRESSURE, RMS_VELOCITY-X, RMS_VELOCITY-Z, STREAMWISE_MASSFLOW )
 SCREEN_WRT_FREQ_INNER= 100
diff --git a/TestCases/incomp_rans/AhmedBody/turb_ahmed.cfg b/TestCases/incomp_rans/AhmedBody/turb_ahmed.cfg
index ca9b65f484b..b8046ad1c99 100644
--- a/TestCases/incomp_rans/AhmedBody/turb_ahmed.cfg
+++ b/TestCases/incomp_rans/AhmedBody/turb_ahmed.cfg
@@ -8,327 +8,134 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= INC_NAVIER_STOKES
-%
-% Specify turbulence model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Reynolds length (1 m, 1 inch by default)
 %REYNOLDS_LENGTH= 1.044
 
 % -------------------- INCOMPRESSIBLE FREE-STREAM DEFINITION ------------------%
 %
-%
-% Initial density for incompressible flows
-% (1.2886 kg/m^3 by default (air), 998.2 Kg/m^3 (water))
 INC_DENSITY_INIT= 1.2642
-%
-% Initial velocity for incompressible flows (1.0,0,0 m/s by default)
 % Re ~ 4.29E6 based on L ~ 1.044
 INC_VELOCITY_INIT= ( 60.0, 0.0, 0.0 )
-%
-% Free-stream viscosity (1.853E-5 N s/m^2, 3.87E-7 lbf s/ft^2 by default)
 FREESTREAM_VISCOSITY= 1.845E-5
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.845E-5
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 10.69
 REF_ORIGIN_MOMENT_Y =  0.00
 REF_ORIGIN_MOMENT_Z =  0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.044
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 0.677
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes (no-slip), constant heat flux wall  marker(s) (NONE = no marker)
-% Format: ( marker name, constant heat flux (J/m^2), ... )
 MARKER_HEATFLUX= ( body, 0.0 )
-%
-% Far-field boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( x1, x0, y1, y0, z1 )
-%
-% Symmetry boundary marker(s) (NONE = no marker)
 MARKER_SYM= ( z0 )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( body )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( body )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( body )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE, 
-%                                             SURFACE_MASSFLOW)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 25.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 EXT_ITER= 99999
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.5
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.5
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= FDS
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH_JESPERSEN)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.0, 0.01 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
 %
-% Marker(s) of the surface where geometrical based function will be evaluated
 GEO_MARKER= ( body )
-%
-% Description of the geometry to be analyzed (AIRFOIL, WING, FUSELAGE)
 GEO_DESCRIPTION= FUSELAGE
-%
-% Coordinate of the stations to be analyzed
 GEO_LOCATION_STATIONS= (0.0, 0.5, 1.0)
-%
-% Geometrical bounds (Y coordinate) for the wing geometry analysis or
-% fuselage evaluation (X coordinate).
 GEO_BOUNDS= (-0.19, 0.19)
-%
-% Plot loads and Cp distributions on each airfoil section
 GEO_PLOT_STATIONS= NO
-%
-% Number of section cuts to make when calculating wing geometry
 GEO_NUMBER_STATIONS= 25
-%
-% Geometrical evaluation mode (FUNCTION, GRADIENT)
 GEO_MODE= FUNCTION
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (FFD_SETTING, FFD_EDGE, FFD_CONTROL_POINT, 
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CAMBER, FFD_THICKNESS)
 DV_KIND= FFD_SETTING
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( body )
-%
-% Parameters of the shape deformation
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_SURFACE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
 DV_PARAM= ( REAR_BOX, 0, 0, -1, 0.0, -1.0, 0.0 )
-%
-% Value of the shape deformation
 DV_VALUE= 0.05
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= WALL_DISTANCE
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-8
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 500
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -14
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= AhmedBodyMesh_FFD.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
diff --git a/TestCases/incomp_rans/naca0012/naca0012.cfg b/TestCases/incomp_rans/naca0012/naca0012.cfg
index bf63a853d22..625c4407cbf 100644
--- a/TestCases/incomp_rans/naca0012/naca0012.cfg
+++ b/TestCases/incomp_rans/naca0012/naca0012.cfg
@@ -6,241 +6,105 @@
 % Author: Francisco Palacios	                                               %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= INC_RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
 
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER)
 TIME_MARCHING= NO
 
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
-% Initial density for incompressible flows (1.2886 kg/m^3 by default)
 INC_DENSITY_INIT= 2.13163
-%
-% Initial velocity for incompressible flows (1.0,0,0 m/s by default)
 INC_VELOCITY_INIT= ( 52.1572, 0.0, 0.0 )
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.853e-05
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 ITER= 2500
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.01
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= FDS
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA0012_turb_897x257.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 100
-%
-%
-% Screen output fields
 SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_NU_TILDE, LIFT, DRAG, TOTAL_HEATFLUX)
-
diff --git a/TestCases/incomp_rans/naca0012/naca0012_SST_SUST.cfg b/TestCases/incomp_rans/naca0012/naca0012_SST_SUST.cfg
index 0a320eeb4a6..8e9e7920c08 100644
--- a/TestCases/incomp_rans/naca0012/naca0012_SST_SUST.cfg
+++ b/TestCases/incomp_rans/naca0012/naca0012_SST_SUST.cfg
@@ -6,241 +6,106 @@
 % Author: Francisco Palacios	                                               %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= INC_RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SST
 SST_OPTIONS=(SUSTAINING)
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER)
 TIME_MARCHING= NO
 
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
-% Initial density for incompressible flows (1.2886 kg/m^3 by default)
 INC_DENSITY_INIT= 2.13163
-%
-% Initial velocity for incompressible flows (1.0,0,0 m/s by default)
 INC_VELOCITY_INIT= ( 52.1572, 0.0, 0.0 )
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.853e-05
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 ITER= 2500
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.01
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= FDS
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA0012_turb_897x257.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 100
-%
-%
-% Screen output fields
 SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG)
-
diff --git a/TestCases/incomp_rans/rough_flatplate/rough_flatplate_incomp.cfg b/TestCases/incomp_rans/rough_flatplate/rough_flatplate_incomp.cfg
index 4c1f69b9cd8..4e174b80541 100644
--- a/TestCases/incomp_rans/rough_flatplate/rough_flatplate_incomp.cfg
+++ b/TestCases/incomp_rans/rough_flatplate/rough_flatplate_incomp.cfg
@@ -5,282 +5,114 @@
 %                   pressure gradient                                          %
 % Author: Akshay Koodly                                                        %
 % Date: 2020.07.07                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= INC_RANS
-%
-% If Navier-Stokes, kind of turbulent model (NONE, SA)
 KIND_TURB_MODEL= SA
-
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
+
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
-% Density model within the incompressible flow solver.
-% Options are CONSTANT (default), BOUSSINESQ, or VARIABLE. If VARIABLE,
-% an appropriate fluid model must be selected.
 INC_DENSITY_MODEL= CONSTANT
-%
-% Solve the energy equation in the incompressible flow solver
 INC_ENERGY_EQUATION = NO
-%
-% Initial density for incompressible flows (1.2886 kg/m^3 by default)
 INC_DENSITY_INIT= 1.32905
-%
-% Initial velocity for incompressible flows (1.0,0,0 m/s by default)
 INC_VELOCITY_INIT= ( 69.4448, 0.0, 0.0 )
-%
-% Initial temperature for incompressible flows that include the
-% energy equation (288.15 K by default). Value is ignored if
-% INC_ENERGY_EQUATION is false.
 INC_TEMPERATURE_INIT= 300.0
-%
-% Non-dimensionalization scheme for incompressible flows. Options are
-% INITIAL_VALUES (default), REFERENCE_VALUES, or DIMENSIONAL.
-% INC_*_REF values are ignored unless REFERENCE_VALUES is chosen.
 INC_NONDIM= INITIAL_VALUES
-%
-% Reference density for incompressible flows (1.0 kg/m^3 by default)
 INC_DENSITY_REF= 1.0
-%
-% Reference velocity for incompressible flows (1.0 m/s by default)
 INC_VELOCITY_REF= 1.0
-%
-% Reference temperature for incompressible flows that include the
-% energy equation (1.0 K by default)
 INC_TEMPERATURE_REF = 1.0
-%
-% List of inlet types for incompressible flows. List length must
-% match number of inlet markers. Options: VELOCITY_INLET, PRESSURE_INLET.
 INC_INLET_TYPE= VELOCITY_INLET
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.84592e-05
-%
-% Sutherland Viscosity Ref (1.716E-5 default value for AIR SI)
 MU_REF= 1.716E-5
-%
-% Sutherland Temperature Ref (273.15 K default value for AIR SI)
 MU_T_REF= 273.15
-%
-% Sutherland constant (110.4 default value for AIR SI)
 SUTHERLAND_CONSTANT= 110.4
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 2.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( wall, 0.0 )
-%WALL_ROUGHNESS = (wall, 0.000061)
-%WALL_ROUGHNESS = (wall, 0.000123)
 WALL_ROUGHNESS = (wall, 0.000246)
-%WALL_ROUGHNESS = (wall, 0.000984)
-%
-%
-% Inlet boundary marker(s) (NONE = no marker) 
-% Format: ( inlet marker, total temperature, total pressure, flow_direction_x, 
-%           flow_direction_y, flow_direction_z, ... )
 MARKER_INLET= ( inlet, 300.0, 69.4448, 1.0, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure, ... )
 MARKER_OUTLET= ( outlet, 0.0, farfield, 0.0 )
-%
 INC_OUTLET_TYPE= PRESSURE_OUTLET,PRESSURE_OUTLET
-%
-% Symmetry boundary marker(s) (NONE = no marker)
 MARKER_SYM= ( symmetry )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( wall )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( wall )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 100.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.1, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 1000
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-12
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.1
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.8
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= FDS
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
+
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
 CONV_FIELD= RMS_VELOCITY-X
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -14
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
-%MESH_FILENAME= mesh_flatplate_turb_69x49.su2
 MESH_FILENAME= mesh_flatplate_turb_137x97.su2
-%MESH_FILENAME= mesh_flatplate_turb_273x193.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow
-%
 TABULAR_FORMAT= CSV
-
 OUTPUT_FILES= RESTART, PARAVIEW, SURFACE_PARAVIEW
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 100, 50, 50
-%
-%
 SCREEN_OUTPUT= (WALL_TIME,INNER_ITER, RMS_VELOCITY-X, RMS_NU_TILDE, LIFT,DRAG)
-%
 WRT_FORCES_BREAKDOWN= YES
diff --git a/TestCases/mms/dg_navierstokes/lam_mms_dg.cfg b/TestCases/mms/dg_navierstokes/lam_mms_dg.cfg
index 5b3b260f163..64bb9fdddaf 100644
--- a/TestCases/mms/dg_navierstokes/lam_mms_dg.cfg
+++ b/TestCases/mms/dg_navierstokes/lam_mms_dg.cfg
@@ -2,176 +2,83 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_NAVIER_STOKES
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Specify the verification solution(NO_VERIFICATION_SOLUTION, INVISCID_VORTEX,
-%                                   RINGLEB, NS_UNIT_QUAD, TAYLOR_GREEN_VORTEX,
-%                                   MMS_NS_UNIT_QUAD, USER_DEFINED_SOLUTION)
 KIND_VERIFICATION_SOLUTION= MMS_NS_UNIT_QUAD
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.1
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 40
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
+
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Different gas model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS)
 FLUID_MODEL= IDEAL_GAS
-%
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.0
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 10.0
-%
+
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
-% Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL).
 CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
-%
-% Laminar Prandtl number
 PRANDTL_LAM= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= DIMENSIONAL
-%
+
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
 MARKER_CUSTOM= ( BottomBoundary, LeftBoundary, RightBoundary, TopBoundary )
 
-
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 0.03
-%
-% Number of total iterations
 ITER= 101
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Factor for the symmetrizing terms in the DG FEM discretization (1.0 by default)
 THETA_INTERIOR_PENALTY_DG_FEM = 1.0
-%THETA_INTERIOR_PENALTY_DG_FEM = 0.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
+
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= UnitQuadStructured_8X8_nPoly3.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= UnitQuadStructured_8X8_nPoly3.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 25000
-%
-%
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
diff --git a/TestCases/mms/dg_navierstokes_3d/lam_mms_dg_3d.cfg b/TestCases/mms/dg_navierstokes_3d/lam_mms_dg_3d.cfg
index 868b5ceb9ba..39521a77686 100644
--- a/TestCases/mms/dg_navierstokes_3d/lam_mms_dg_3d.cfg
+++ b/TestCases/mms/dg_navierstokes_3d/lam_mms_dg_3d.cfg
@@ -2,194 +2,87 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_NAVIER_STOKES
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Specify the verification solution(NO_VERIFICATION_SOLUTION, INVISCID_VORTEX,
-%                                   RINGLEB, NS_UNIT_QUAD, TAYLOR_GREEN_VORTEX,
-%                                   MMS_NS_UNIT_QUAD, MMS_NS_TWO_HALF_SPHERES,
-%                                   MMS_INC_EULER, MMS_INC_NS,
-%                                   USER_DEFINED_SOLUTION)
 KIND_VERIFICATION_SOLUTION= MMS_NS_TWO_HALF_SPHERES
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.1
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 40
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
+
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Different gas model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS)
 FLUID_MODEL= IDEAL_GAS
-%
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-%
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 10.0
-%
+
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
-% Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL).
 CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
-%
-% Laminar Prandtl number
 PRANDTL_LAM= 0.72
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= DIMENSIONAL
-%REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
-%
+
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-%MARKER_CUSTOM= ( PlaneZ0, OuterSphere, InnerSphere )
-%
 MARKER_CUSTOM= ( PlaneZ0 )
-%
-% Marker adiabatic wall (NONE = no marker)
 MARKER_HEATFLUX= ( InnerSphere, 0.0 )
-%
-% Marker isothermal wall (NONE = no marker)
 MARKER_ISOTHERMAL= ( OuterSphere, 400.0 )
-%
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 0.2
-%CFL_NUMBER=1.e-30
-%
-% Number of total iterations
 ITER= 101
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%
-% Factor for the symmetrizing terms in the DG FEM discretization (1.0 by default)
 THETA_INTERIOR_PENALTY_DG_FEM = 1.0
-%
-% Compute the entropy in the fluid model (YES, NO)
 COMPUTE_ENTROPY_FLUID_MODEL= NO
-%
-% Use the lumped mass matrix for steady DGFEM computations (NO, YES)
 USE_LUMPED_MASSMATRIX_DGFEM= YES
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
+
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= SphereInSphereStructured_nPoly3.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= SphereInSphereStructured_nPoly3.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 25000
-%
-%
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
diff --git a/TestCases/mms/dg_ringleb/ringleb_dg.cfg b/TestCases/mms/dg_ringleb/ringleb_dg.cfg
index 31e71eb0d8c..6f3e431e1b3 100644
--- a/TestCases/mms/dg_ringleb/ringleb_dg.cfg
+++ b/TestCases/mms/dg_ringleb/ringleb_dg.cfg
@@ -5,190 +5,88 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               FEM_EULER, FEM_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= FEM_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Specify the verification solution(NO_VERIFICATION_SOLUTION, INVISCID_VORTEX,
-%                                   RINGLEB, NS_UNIT_QUAD, TAYLOR_GREEN_VORTEX,
-%                                   MMS_NS_UNIT_QUAD, USER_DEFINED_SOLUTION)
 KIND_VERIFICATION_SOLUTION= RINGLEB
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 %RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AoA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
-%MARKER_EULER= ( LeftBoundary, RightBoundary )
-%
-% Custom boundaries
-%MARKER_CUSTOM= ( Symmetry, TopBoundary )
 MARKER_CUSTOM= ( Symmetry, LeftBoundary, RightBoundary, TopBoundary )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( LeftBoundary, RightBoundary )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( LeftBoundary, RightBoundary )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.0
-%CFL_NUMBER= 0.2       % For AUSM
-%
-% Number of total iterations
 ITER= 101
-%ITER= 1
-%
-% Runge-Kutta alpha coefficients
-%RK_ALPHA_COEFF= ( 0.25, 0.166667, 0.375, 0.5, 1.0 )
 RK_ALPHA_COEFF= ( 0.666667, 0.666667, 1.0 )
 
 % ------------------ FEM FLOW NUMERICAL METHOD DEFINITION ----------------------%
 %
-% Convective numerical method (DG)
 NUM_METHOD_FEM_FLOW= DG
-%
-% Riemann solver used for DG (ROE, LAX-FRIEDRICH, AUSM, AUSMPW+, HLLC, VAN_LEER)
 RIEMANN_SOLVER_FEM= ROE
 %RIEMANN_SOLVER_FEM= AUSM
-%
-% Constant factor applied for quadrature with straight elements (2.0 by default)
 QUADRATURE_FACTOR_STRAIGHT_FEM = 2.0
-%QUADRATURE_FACTOR_STRAIGHT_FEM = 3.0
-%
-% Constant factor applied for quadrature with curved elements (3.0 by default)
 QUADRATURE_FACTOR_CURVED_FEM = 3.0
-%QUADRATURE_FACTOR_CURVED_FEM = 2.0
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT)
 TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
-%
-%
-% Compute the entropy in the fluid model (YES, NO)
 COMPUTE_ENTROPY_FLUID_MODEL= YES
-%
-% Use the lumped mass matrix for steady DGFEM computations (NO, YES)
 USE_LUMPED_MASSMATRIX_DGFEM= YES
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= QuadDominant25X25_nPoly3.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= QuadDominant25X25_nPoly3.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 5000
-%
-%
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
diff --git a/TestCases/mms/fvm_incomp_euler/inv_mms_jst.cfg b/TestCases/mms/fvm_incomp_euler/inv_mms_jst.cfg
index e8130c81aca..64a58e3e80e 100755
--- a/TestCases/mms/fvm_incomp_euler/inv_mms_jst.cfg
+++ b/TestCases/mms/fvm_incomp_euler/inv_mms_jst.cfg
@@ -4,218 +4,90 @@
 % Case description: Incompressible inviscid MMS test case                      %
 % Author: Thomas D. Economon                                                   %
 % Date: 2019.04.09                                                             %
-% File Version 7.4.0 "Blackbird"                                                  %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= INC_EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Specify the verification solution(NO_VERIFICATION_SOLUTION, INVISCID_VORTEX,
-%                                   RINGLEB, NS_UNIT_QUAD, TAYLOR_GREEN_VORTEX,
-%                                   MMS_NS_UNIT_QUAD, MMS_INC_EULER, MMS_INC_NS,
-%                                   USER_DEFINED_SOLUTION)
 KIND_VERIFICATION_SOLUTION= MMS_INC_EULER
 
 % -------------------- INCOMPRESSIBLE FREE-STREAM DEFINITION ------------------%
 %
-% Initial density for incompressible flows
-% (1.2886 kg/m^3 by default (air), 998.2 Kg/m^3 (water))
 INC_DENSITY_INIT= 1.0
-%
-% Initial velocity for incompressible flows (1.0,0,0 m/s by default)
 INC_VELOCITY_INIT= ( 1.0, 0.0, 0.0 )
-%
-% Non-dimensionalization scheme for incompressible flows. Options are
-% INITIAL_VALUES (default), REFERENCE_VALUES, or DIMENSIONAL.
-% INC_*_REF values are ignored unless REFERENCE_VALUES is chosen.
 INC_NONDIM= DIMENSIONAL
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Marker(s) of the surface(s) where custom boundary conditions are imposed.
 MARKER_CUSTOM= ( left, right, upper, lower )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( left, right, upper, lower )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( left, right, upper, lower )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 25.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 25.0, 10000.0 )
-%
-% Maximum Delta Time in local time stepping simulations
 MAX_DELTA_TIME= 1E30
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 9999
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 1, 1, 1, 1 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.8
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -15
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= square.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 50
-%
-%
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_VELOCITY-X, LIFT, DRAG)
diff --git a/TestCases/mms/fvm_incomp_navierstokes/lam_mms_fds.cfg b/TestCases/mms/fvm_incomp_navierstokes/lam_mms_fds.cfg
index c4dc584cf07..48da7ebb28d 100755
--- a/TestCases/mms/fvm_incomp_navierstokes/lam_mms_fds.cfg
+++ b/TestCases/mms/fvm_incomp_navierstokes/lam_mms_fds.cfg
@@ -4,240 +4,101 @@
 % Case description: Incompressible laminar MMS test case                       %
 % Author: Thomas D. Economon                                                   %
 % Date: 2019.04.09                                                             %
-% File Version 7.4.0 "Blackbird"                                                  %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= INC_NAVIER_STOKES
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Specify the verification solution(NO_VERIFICATION_SOLUTION, INVISCID_VORTEX,
-%                                   RINGLEB, NS_UNIT_QUAD, TAYLOR_GREEN_VORTEX,
-%                                   MMS_NS_UNIT_QUAD, MMS_INC_NS,
-%                                   USER_DEFINED_SOLUTION)
 KIND_VERIFICATION_SOLUTION= MMS_INC_NS
 
 % -------------------- INCOMPRESSIBLE FREE-STREAM DEFINITION ------------------%
 %
-% Initial density for incompressible flows
-% (1.2886 kg/m^3 by default (air), 998.2 Kg/m^3 (water))
 INC_DENSITY_INIT= 1.0
-%
-% Initial velocity for incompressible flows (1.0,0,0 m/s by default)
 INC_VELOCITY_INIT= ( 1.0, 0.0, 0.0 )
-%
-% Non-dimensionalization scheme for incompressible flows. Options are
-% INITIAL_VALUES (default), REFERENCE_VALUES, or DIMENSIONAL.
-% INC_*_REF values are ignored unless REFERENCE_VALUES is chosen.
 INC_NONDIM= DIMENSIONAL
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 0.5
 
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
-% Laminar Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL,
-% POLYNOMIAL_CONDUCTIVITY).
 CONDUCTIVITY_MODEL= CONSTANT_CONDUCTIVITY
-%
-% Molecular Thermal Conductivity that would be constant (0.0257 by default)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.0257
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Marker(s) of the surface(s) where custom boundary conditions are imposed.
 MARKER_CUSTOM= ( left, right, upper, lower )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( left, right, upper, lower )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( left, right, upper, lower )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1e4
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 25.0, 10000.0 )
-%
-% Maximum Delta Time in local time stepping simulations
 MAX_DELTA_TIME= 1E30
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 9999
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 1, 1, 1, 1 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.8
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= FDS
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -15
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= square.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 50
-%
-% 
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_VELOCITY-X, LIFT, DRAG)
diff --git a/TestCases/mms/fvm_navierstokes/lam_mms_roe.cfg b/TestCases/mms/fvm_navierstokes/lam_mms_roe.cfg
index 8229a753ae9..c1185747e5a 100755
--- a/TestCases/mms/fvm_navierstokes/lam_mms_roe.cfg
+++ b/TestCases/mms/fvm_navierstokes/lam_mms_roe.cfg
@@ -4,257 +4,107 @@
 % Case description: Compressible laminar MMS test case                         %
 % Author: Thomas D. Economon                                                   %
 % Date: 2019.04.09                                                             %
-% File Version 7.4.0 "Blackbird"                                                  %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= NAVIER_STOKES
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Specify the verification solution(NO_VERIFICATION_SOLUTION, INVISCID_VORTEX,
-%                                   RINGLEB, NS_UNIT_QUAD, TAYLOR_GREEN_VORTEX,
-%                                   MMS_NS_UNIT_QUAD, MMS_INC_NS,
-%                                   USER_DEFINED_SOLUTION)
 KIND_VERIFICATION_SOLUTION= MMS_NS_UNIT_QUAD
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Side-slip angle (degrees, only for compressible flows)
 SIDESLIP_ANGLE= 0.0
-%
-% Init option to choose between Reynolds (default) or thermodynamics quantities
-% for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
-%
-% Free-stream option to choose between density and temperature (default) for
-% initializing the solution (TEMPERATURE_FS, DENSITY_FS)
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-% Free-stream pressure (101325.0 N/m^2, 2116.216 psf by default)
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K, 518.67 R by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Free-stream density (1.2886 Kg/m^3, 0.0025 slug/ft^3 by default)
 FREESTREAM_DENSITY= 1.2886
-%
-% Compressible flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= DIMENSIONAL
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.716E-5
 
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
-% Laminar Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL,
-% POLYNOMIAL_CONDUCTIVITY).
 CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
-%
-% Laminar Prandtl number (0.72 (air), only for CONSTANT_PRANDTL)
 PRANDTL_LAM= 0.72
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Marker(s) of the surface(s) where custom boundary conditions are imposed.
 MARKER_CUSTOM= ( left, right, upper, lower )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( left, right, upper, lower )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( left, right, upper, lower )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 25.0, 10000.0 )
-%
-% Maximum Delta Time in local time stepping simulations
 MAX_DELTA_TIME= 1E30
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 9999
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 1, 1, 1, 1 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.8
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -14
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= square.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 50
-%
-%
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
diff --git a/TestCases/moving_wall/cavity/lam_cavity.cfg b/TestCases/moving_wall/cavity/lam_cavity.cfg
index 8140296d6b2..40b5b348d09 100644
--- a/TestCases/moving_wall/cavity/lam_cavity.cfg
+++ b/TestCases/moving_wall/cavity/lam_cavity.cfg
@@ -2,227 +2,105 @@
 %                                                                              %
 % SU2 configuration file                                                       %
 % Case description: Laminar flow inside of a lid-driven cavity                 %
-% Author: Thomas D. Economon						                                       %
-% Institution: Stanford University					                                   %
+% Author: Thomas D. Economon                                                   %
+% Institution: Stanford University                                             %
 % Date: 2013.10.01                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= NAVIER_STOKES
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.05
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Side-slip angle (degrees, only for compressible flows)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 1000.0
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Type of dynamic mesh (NONE, RIGID_MOTION, DEFORMING, ROTATING_FRAME,
-%                       MOVING_WALL, AEROELASTIC, ELASTICITY, EXTERNAL)
 SURFACE_MOVEMENT= MOVING_WALL
-%
-% Motion mach number (non-dimensional). Used for initializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.1
-%
-% Moving wall boundary marker(s) (NONE = no marker, ignored for RIGID_MOTION)
 MARKER_MOVING= ( upper )
-%
-% Translational velocity (m/s) in the x, y, & z directions
 SURFACE_TRANSLATION_RATE= 33.179 0.0 0.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes (no-slip), constant heat flux wall  marker(s) (NONE = no marker)
-% Format: ( marker name, constant heat flux (J/m^2), ... )
 MARKER_HEATFLUX= ( upper, 0.0, left, 0.0, right, 0.0, lower, 0.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( upper, left, right, lower )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( upper, left, right, lower )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.9
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.9
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_cavity_stretch.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-%
-% Screen output 
-SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
-
+SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
\ No newline at end of file
diff --git a/TestCases/moving_wall/spinning_cylinder/spinning_cylinder.cfg b/TestCases/moving_wall/spinning_cylinder/spinning_cylinder.cfg
index a2f90b1df4b..6b16de3a5a0 100644
--- a/TestCases/moving_wall/spinning_cylinder/spinning_cylinder.cfg
+++ b/TestCases/moving_wall/spinning_cylinder/spinning_cylinder.cfg
@@ -2,244 +2,114 @@
 %                                                                              %
 % SU2 configuration file                                                       %
 % Case description: Laminar flow around a spinning cylinder                    %
-% Author: Thomas D. Economon						       %
-% Institution: Stanford University					       %
+% Author: Thomas D. Economon                                                   %
+% Institution: Stanford University                                             %
 % Date: 2013.08.21                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= NAVIER_STOKES
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-% 
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.1
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 200.0
-%
-% Reynolds length (in meters)
 REYNOLDS_LENGTH= 1.0
+
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Type of dynamic mesh (NONE, RIGID_MOTION, DEFORMING, ROTATING_FRAME,
-%                       MOVING_WALL, AEROELASTIC, EXTERNAL)
 SURFACE_MOVEMENT= MOVING_WALL
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.1
-%
-% Moving wall boundary marker(s) (NONE = no marker, ignored for RIGID_MOTION)
 MARKER_MOVING= ( cylinder )
-%
-% Coordinates of the motion origin
 SURFACE_MOTION_ORIGIN= 0.5 0.0 0.0 
-%
-% Angular velocity vector (rad/s) about the motion origin
 SURFACE_ROTATION_RATE = 0.0 0.0 -199.0738
+
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes (no-slip), constant heat flux wall  marker(s) (NONE = no marker)
-% Format: ( marker name, constant heat flux (J/m^2), ... )
 MARKER_HEATFLUX= ( cylinder, 0.0 )
-%
-% Far-field boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( cylinder )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( cylinder )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 100.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 ITER= 99999
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.5
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.5
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= NONE
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -15
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-7
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_cylinder_lam.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 100
-%
-%
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
diff --git a/TestCases/multiple_ffd/naca0012/inv_NACA0012_ffd.cfg b/TestCases/multiple_ffd/naca0012/inv_NACA0012_ffd.cfg
index 749b7992b02..63ac0e6024d 100644
--- a/TestCases/multiple_ffd/naca0012/inv_NACA0012_ffd.cfg
+++ b/TestCases/multiple_ffd/naca0012/inv_NACA0012_ffd.cfg
@@ -5,248 +5,112 @@
 % Author: Francisco Palacios, Charanya Venkatesan-Crome                        %
 % Institution: Stanford University                                             %
 % Date: 2018.07.23                                                             %
-% File Version 7.4.0 "Blackbird"                                                  %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION) 
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
-%
-OUTPUT_FILES=(RESTART_ASCII)
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AOA= 1.25
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 = no marker)
 MARKER_EULER= ( airfoil_upper, airfoil_lower )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( airfoil_upper, airfoil_lower )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil_upper, airfoil_lower )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 10
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (LU_SGS,
-%                                              SYM_GAUSS_SEIDEL, BCGSTAB, GMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (NONE, JACOBI, LINELET, LUSGS)
 LINEAR_SOLVER_PREC= ILU
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 1.0
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 1.0
 
 % --------------------- FLOW NUMERICAL METHOD DEFINITION ----------------------%
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                              ROE-2ND_ORDER)
-CONV_NUM_METHOD_FLOW= JST
 %
-% Slope limiter (VENKATAKRISHNAN)
+CONV_NUM_METHOD_FLOW= JST
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE)
-OBJECTIVE_FUNCTION= DRAG
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                              ROE-2ND_ORDER)
+OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Slope limiter (VENKATAKRISHNAN, SHARP_EDGES)
 SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.8
-%
-% Limit value for the adjoint variable
 LIMIT_ADJFLOW= 1E6
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
-%
-% Sensitivity smoothing (NONE, SOBOLEV, BIGRID)
 SENS_SMOOTHING= NONE
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION, 
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION)
 DV_KIND= FFD_SETTING
-%DV_KIND= FFD_CONTROL_POINT
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil_upper, airfoil_lower )
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( 1st digit, 2nd and 3rd digit )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= ( UPPER, 1, 0, 0, 0.0, 1.0, 0.0 )
-%
-% Value of the shape deformation deformation
 DV_VALUE= 0.001
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-10
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 500
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= ( LOWER, 0.075, -0.075, 0.0, 0.625, -0.075, 0.0, 0.625, -0.02, 0.0, 0.075, -0.02, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0 ); ( UPPER, 0.075, 0.02, 0.0, 0.625, 0.02, 0.0, 0.625, 0.075, 0.0, 0.075, 0.075, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0 )
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= ( 4, 1, 0 ); (4, 1, 0)
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
-%FFD_CONTINUITY= 2ND_DERIVATIVE
 FFD_CONTINUITY= USER_INPUT
 
-% Definition of the FFD planes to be frozen in the FFD (x,y,z).
-% Value from 0 FFD degree in that direction. Pick a value larger than degree if you don't want to fix any plane.
 FFD_FIX_I= (0,4)
 FFD_FIX_J= (15)
 FFD_FIX_K= (15)
@@ -254,131 +118,37 @@ FFD_FIX_K= (15)
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -9
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA0012_multiFFD.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT 
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 50
-%
-%
 HISTORY_OUTPUT=(ITER, RMS_RES, AERO_COEFF, D_AERO_COEFF)
+OUTPUT_FILES= (RESTART_ASCII)
+
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.001
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= ( LIFT > 0.327 ) * 0.001; ( MOMENT_Z > 0.0 ) * 0.001; ( AIRFOIL_THICKNESS > 0.12 ) * 0.001
-%
-% Maximum number of optimizer iterations
 OPT_ITERATIONS= 1
-%
-% Requested accuracy
 OPT_ACCURACY= 1E-6
-%
-% Upper bound for each design variable
 OPT_BOUND_UPPER= 0.1
-%
-% Lower bound for each design variable
 OPT_BOUND_LOWER= -0.1
-%
-% Optimization design variables, separated by semicolons
-
-% FFD_CONTROL_POINT (Y)
 DEFINITION_DV= ( 11, 1.0 | airfoil_upper | UPPER, 1, 0, 0, 0.0, 1.0, 0.0 ); ( 11, 1.0 | airfoil_lower | LOWER, 1, 0, 0, 0.0, 1.0, 0.0 )
diff --git a/TestCases/navierstokes/cylinder/cylinder_lowmach.cfg b/TestCases/navierstokes/cylinder/cylinder_lowmach.cfg
index 98097644088..a975b7403e2 100644
--- a/TestCases/navierstokes/cylinder/cylinder_lowmach.cfg
+++ b/TestCases/navierstokes/cylinder/cylinder_lowmach.cfg
@@ -5,217 +5,98 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.09.30                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               TNE2_EULER, TNE2_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= NAVIER_STOKES
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.01
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 40.0
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( cylinder, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( cylinder )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( cylinder )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 4.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.8
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= HLLC
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 10.0
-%
-% Low Mach correction
 LOW_MACH_CORR= YES
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_cylinder_lam.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-%
-% Screen output fields
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG, TOTAL_HEATFLUX)
diff --git a/TestCases/navierstokes/cylinder/lam_cylinder.cfg b/TestCases/navierstokes/cylinder/lam_cylinder.cfg
index 50e5c0e802a..e6629d4fc99 100644
--- a/TestCases/navierstokes/cylinder/lam_cylinder.cfg
+++ b/TestCases/navierstokes/cylinder/lam_cylinder.cfg
@@ -5,211 +5,97 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.09.30                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= NAVIER_STOKES
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.1
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 40.0
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( cylinder, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( cylinder )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( cylinder )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 4.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.8
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 10.0
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_cylinder_lam.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-% 
-% Screen output fields
 SCREEN_OUTPUT = (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG, TOTAL_HEATFLUX)
diff --git a/TestCases/navierstokes/flatplate/lam_flatplate.cfg b/TestCases/navierstokes/flatplate/lam_flatplate.cfg
index 226aadbd7e3..18435bf9caa 100644
--- a/TestCases/navierstokes/flatplate/lam_flatplate.cfg
+++ b/TestCases/navierstokes/flatplate/lam_flatplate.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon						                           %
 % Institution: Stanford University					                           %
 % Date: 2013.09.30                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -92,4 +92,3 @@ RESTART_ADJ_FILENAME= restart_adj.dat
 GRAD_OBJFUNC_FILENAME= of_grad.dat
 OUTPUT_WRT_FREQ= 250
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, DRAG, SURFACE_MASSFLOW, TOTAL_HEATFLUX, TOTAL_HEATFLUX_ON_SURFACE)
-
diff --git a/TestCases/navierstokes/flatplate/lam_flatplate_unst.cfg b/TestCases/navierstokes/flatplate/lam_flatplate_unst.cfg
index 6c8028fb76c..46285433567 100644
--- a/TestCases/navierstokes/flatplate/lam_flatplate_unst.cfg
+++ b/TestCases/navierstokes/flatplate/lam_flatplate_unst.cfg
@@ -2,7 +2,7 @@
 %                                                                              %
 % SU2 configuration file                                                       %
 % Case description: Test interp. restart, and auto time-step for dual-time     %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
@@ -57,7 +57,6 @@ TIME_DOMAIN= YES
 UNST_CFL_NUMBER= 20
 TIME_MARCHING= DUAL_TIME_STEPPING-1ST_ORDER
 
-
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
 LINEAR_SOLVER= SMOOTHER
@@ -84,5 +83,4 @@ INNER_ITER= 20
 MESH_FORMAT= BOX
 MESH_BOX_LENGTH= (0.01, 0.01, 0.1)
 MESH_BOX_SIZE= (17, 33, 129)
-%
 SCREEN_OUTPUT= (TIME_ITER, INNER_ITER, CUR_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_MOMENTUM-Z, RMS_ENERGY, FORCE_Z, LINSOL_RESIDUAL)
diff --git a/TestCases/navierstokes/naca0012/lam_NACA0012.cfg b/TestCases/navierstokes/naca0012/lam_NACA0012.cfg
index ef5e2e573b5..e30de09d1c0 100644
--- a/TestCases/navierstokes/naca0012/lam_NACA0012.cfg
+++ b/TestCases/navierstokes/naca0012/lam_NACA0012.cfg
@@ -5,203 +5,92 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: Sep 28, 2012                                                           %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
-%
-% Physical governing equations (EULER, NAVIER_STOKES, NS_PLASMA)
-%                               
+%                            
 SOLVER= NAVIER_STOKES
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 1.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 5000.0
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 EXT_ITER= 99999
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 2, 2 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.85
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.85
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.0001
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA0012_lam_hybrid_v1.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-
diff --git a/TestCases/navierstokes/periodic2D/config.cfg b/TestCases/navierstokes/periodic2D/config.cfg
index 7e8184b9835..de898e849de 100644
--- a/TestCases/navierstokes/periodic2D/config.cfg
+++ b/TestCases/navierstokes/periodic2D/config.cfg
@@ -70,5 +70,4 @@ INNER_ITER= 5000
 MESH_FORMAT= SU2
 MESH_FILENAME= sector.su2
 OUTPUT_WRT_FREQ= 9999
-%
 SCREEN_OUTPUT= ( INNER_ITER, RMS_RES, LINSOL_RESIDUAL, SURFACE_PRESSURE_DROP )
diff --git a/TestCases/navierstokes/poiseuille/lam_poiseuille.cfg b/TestCases/navierstokes/poiseuille/lam_poiseuille.cfg
index f921d8778c0..51d0e0baccf 100644
--- a/TestCases/navierstokes/poiseuille/lam_poiseuille.cfg
+++ b/TestCases/navierstokes/poiseuille/lam_poiseuille.cfg
@@ -2,253 +2,117 @@
 %                                                                              %
 % SU2 configuration file                                                       %
 % Case description: Poiseuille flow case for testing a body force/periodicity  %
-% Author: Thomas D. Economon				                       %
+% Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2017.02.27                                                             %
-% File Version 7.4.0 "Blackbird"                                                   %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= NAVIER_STOKES
-%
-% Specify turbulence model (NONE, SA)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
-%
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.0028284271247461901
 % V : 1 m/s
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 90.0
-%
-% Init option to choose between Reynolds (default) or thermodynamics quantities
-% for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
-%
-% Free-stream option to choose between density and temperature (default) for
-% initializing the solution (TEMPERATURE_FS, DENSITY_FS)
 FREESTREAM_OPTION= DENSITY_FS
-%
-% Free-stream pressure (101325.0 N/m^2, 2116.216 psf by default)
 FREESTREAM_PRESSURE= 100000.0
-%
-% Free-stream density (1.2886 Kg/m^3, 0.0025 slug/ft^3 by default)
 FREESTREAM_DENSITY= 1.0
-%
-% Reynolds length (1 m, 1 inch by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation (m or in)
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional
-% moment (m or in)
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic
-% calculation) (m^2 or in^2)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= DIMENSIONAL
 
 % ---- IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
-% Different gas model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS)
 FLUID_MODEL= IDEAL_GAS
-%
-% Ratio of specific heats (1.4 default and the value is hardcoded
-%                          for the model STANDARD_AIR)
 GAMMA_VALUE= 1.25
-%
-% Specific gas constant (287.058 J/kg*K default and this value is hardcoded 
-%                        for the model STANDARD_AIR)
 GAS_CONSTANT= 200.0
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 0.1
 
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
-% Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL).
 CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
-%
-% Molecular Thermal Conductivity that would be constant (0.0257 by default)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.0257
-%
-% Constant Prandtl number
 PRANDTL_LAM = 1.0
 
 % ----------------------- BODY FORCE DEFINITION -------------------------------%
 %
-% Apply a body force as a source term (NO, YES)
 BODY_FORCE= YES
-%
-% Vector of body force values (BodyForce_X, BodyForce_Y, BodyForce_Z)
 BODY_FORCE_VECTOR= ( 0.0, 1.2, 0.0 )
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes (no-slip), constant heat flux wall  marker(s) (NONE = no marker)
-% Format: ( marker name, constant heat flux (J/m^2), ... )
 MARKER_HEATFLUX= ( left, 0.0, right, 0.0 )
-%
-% Periodic boundary marker(s) (NONE = no marker)
-% Format: ( periodic marker, donor marker, rotation_center_x, rotation_center_y, 
-% rotation_center_z, rotation_angle_x-axis, rotation_angle_y-axis, 
-% rotation_angle_z-axis, translation_x, translation_y, translation_z, ... )
 MARKER_PERIODIC= ( lower, upper, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 1.0, 0.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( lower )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( left, right )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 15.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 15.0, 10000.0 )
-%
-% Number of total iterations
 ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION ----------------------.su2
 %
-% Mesh input file
 MESH_FILENAME= mesh_poiseuille_51x51.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 500
-%
-%
-% Screen output 
 SCREEN_OUTPUT=(INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG, TOTAL_HEATFLUX)
-%
 OUTPUT_FILES=(RESTART_ASCII)
diff --git a/TestCases/navierstokes/poiseuille/profile_poiseuille.cfg b/TestCases/navierstokes/poiseuille/profile_poiseuille.cfg
index e59ed842dc2..ee36e6794ff 100644
--- a/TestCases/navierstokes/poiseuille/profile_poiseuille.cfg
+++ b/TestCases/navierstokes/poiseuille/profile_poiseuille.cfg
@@ -5,282 +5,123 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Robert Bosch LLC                                                %
 % Date: 2018.03.19                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= NAVIER_STOKES
-%
-% Specify turbulence model (NONE, SA)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
-% Discard the restart metadata (iteration numbers)
 DISCARD_INFILES= YES
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.0028284271247461901
 % V : 1 m/s
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 90.0
-%
-% Init option to choose between Reynolds (default) or thermodynamics quantities
-% for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
-%
-% Free-stream option to choose between density and temperature (default) for
-% initializing the solution (TEMPERATURE_FS, DENSITY_FS)
 FREESTREAM_OPTION= DENSITY_FS
-%
-% Free-stream pressure (101325.0 N/m^2, 2116.216 psf by default)
 FREESTREAM_PRESSURE= 100000.0
-%
-% Free-stream density (1.2886 Kg/m^3, 0.0025 slug/ft^3 by default)
 FREESTREAM_DENSITY= 1.0
-%
-% Reynolds length (1 m, 1 inch by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation (m or in)
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional
-% moment (m or in)
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic
-% calculation) (m^2 or in^2)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= DIMENSIONAL
 
 % ---- IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
-% Different gas model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS)
 FLUID_MODEL= IDEAL_GAS
-%
-% Ratio of specific heats (1.4 default and the value is hardcoded
-%                          for the model STANDARD_AIR)
 GAMMA_VALUE= 1.25
-%
-% Specific gas constant (287.058 J/kg*K default and this value is hardcoded 
-%                        for the model STANDARD_AIR)
 GAS_CONSTANT= 200.0
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 0.1
 
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
-% Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL).
 CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
 %
-% Molecular Thermal Conductivity that would be constant (0.0257 by default)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.0257
-%
-% Constant Prandtl number
 PRANDTL_LAM = 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes (no-slip), constant heat flux wall  marker(s) (NONE = no marker)
-% Format: ( marker name, constant heat flux (J/m^2), ... )
 MARKER_HEATFLUX= ( left, 0.0, right, 0.0 )
-%
-% Inlet boundary type (TOTAL_CONDITIONS, MASS_FLOW)
 INLET_TYPE= MASS_FLOW
-%
-% Read inlet profile from a file (YES, NO) default: NO
+
 SPECIFIED_INLET_PROFILE= YES
-%
-% File specifying inlet profile
 INLET_FILENAME= inlet_poiseuille.dat
-%
-% Inlet boundary marker(s) with the following formats (NONE = no marker)
-% Total Conditions: (inlet marker, total temp, total pressure, flow_direction_x,
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-% Mass Flow: (inlet marker, density, velocity magnitude, flow_direction_x,
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-% Incompressible: (inlet marker, NULL, velocity magnitude, flow_direction_x,
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
 MARKER_INLET= ( lower, 1.0, 1.0, 0.0, 1.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
 MARKER_OUTLET= ( upper, 100000.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( upper )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( left, right )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 15.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 15.0, 10000.0 )
-%
-% Number of total iterations
 ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-grid levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.8
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION ----------------------.su2
 %
-% Mesh input file
 MESH_FILENAME= mesh_poiseuille_51x51.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow_profile.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 25
-%
-%
-% Screen output fields
 SCREEN_OUTPUT=(INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
diff --git a/TestCases/nicf/LS89/turb_SA_PR.cfg b/TestCases/nicf/LS89/turb_SA_PR.cfg
index 1d2c122e672..682d1ba26a8 100644
--- a/TestCases/nicf/LS89/turb_SA_PR.cfg
+++ b/TestCases/nicf/LS89/turb_SA_PR.cfg
@@ -5,312 +5,130 @@
 % Author: M. Pini, S. Vitale                                                   %
 % Institution: Delft University of Technology                                  %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                         
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 1100000.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 592.295
-
-% Free-stream temperature (1.2886 Kg/m3 by default)
 FREESTREAM_DENSITY= 1.2886
-
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-% Free-stream Turbulence Intensity
 FREESTREAM_TURBULENCEINTENSITY = 0.05
-%
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.0E5
-%
 INIT_OPTION= TD_CONDITIONS
-%
-%SYSTEM_MEASUREMENTS= US
+
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ---- IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
-% Different gas model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS)
 FLUID_MODEL= PR_GAS
-%
-% Ratio of specific heats (1.4 default and the value is hardcoded
-%                          for the model STANDARD_AIR)
 GAMMA_VALUE= 1.0165
-%
-% Specific gas constant (287.058 J/kg*K default and this value is hardcoded 
-%                        for the model STANDARD_AIR)
 GAS_CONSTANT= 35.23
-%
-% Critical Temperature (288.15 K by default)
 CRITICAL_TEMPERATURE= 564.1
-%
-% Critical Pressure (101325.0 N/m^2 by default)
 CRITICAL_PRESSURE= 1415000
-%
-% Critical Density (1.2886 Kg/m3 by default)
 CRITICAL_DENSITY= 256.74
-%
-% Acentri factor (0.035 (air))
 ACENTRIC_FACTOR= 0.529
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.3764E-5
-%
-% Sutherland Viscosity Ref (1.716E-5 default value for AIR SI)
 MU_REF= 1.716E-5
-%
-% Sutherland Temperature Ref (288.15 K default value for AIR SI)
 MU_T_REF= 288.15
-%
-% Sutherland constant (110.4 default value for AIR SI)
 SUTHERLAND_CONSTANT= 110.4
 
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
-% Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL).
 CONDUCTIVITY_MODEL= CONSTANT_CONDUCTIVITY
-%
-% Molecular Thermal Conductivity that would be constant (0.0257 by default)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.047280
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Inlet boundary type (TOTAL_CONDITIONS, MASS_FLOW)
 INLET_TYPE= TOTAL_CONDITIONS
-%
-% Inlet boundary marker(s) with the following formats (NONE = no marker) 
-% Total Conditions: (inlet marker, total temp, total pressure, flow_direction_x, 
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-% Mass Flow: (inlet marker, density, velocity magnitude, flow_direction_x, 
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-%MARKER_INLET= ( inflow, 404.1, 0.904E+05, 1.0, 0.0, 0.0 )
 MARKER_RIEMANN= (inflow, TOTAL_CONDITIONS_PT, 13.8686E+05, 592.295, 1.0, 0.0, 0.0, outflow, STATIC_PRESSURE, 11.00E+05, 0.0, 0.0, 0.0, 0.0)
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
-%MARKER_OUTLET= ( outflow, 0.523E+05 )
-%
-% Periodic boundary marker(s) (NONE = no marker)
-% Format: ( periodic marker, donor marker, rotation_center_x, rotation_center_y, 
-% rotation_center_z, rotation_angle_x-axis, rotation_angle_y-axis, 
-% rotation_angle_z-axis, translation_x, translation_y, translation_z, ... )
 MARKER_PERIODIC= ( periodic_1, periodic_2, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, -0.05749995, 0.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 ITER= 5000
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.75
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_vki_turbine_prepbc.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 500
-%
-% 
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_NU_TILDE, LIFT, DRAG)
diff --git a/TestCases/nicf/LS89/turb_SST_PR.cfg b/TestCases/nicf/LS89/turb_SST_PR.cfg
index b72839445b7..a611ef7e427 100644
--- a/TestCases/nicf/LS89/turb_SST_PR.cfg
+++ b/TestCases/nicf/LS89/turb_SST_PR.cfg
@@ -5,312 +5,131 @@
 % Author: M. Pini, S. Vitale                                                   %
 % Institution: Delft University of Technology                                  %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                         
 SOLVER= NAVIER_STOKES
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SST
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 1100000.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 592.295
-
-% Free-stream temperature (1.2886 Kg/m3 by default)
 FREESTREAM_DENSITY= 1.2886
-
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-% Free-stream Turbulence Intensity
 FREESTREAM_TURBULENCEINTENSITY = 0.05
-%
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.0E5
-%
 INIT_OPTION= TD_CONDITIONS
-%
-%SYSTEM_MEASUREMENTS= US
+
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ---- IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
-% Different gas model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS)
 FLUID_MODEL= PR_GAS
-%
-% Ratio of specific heats (1.4 default and the value is hardcoded
-%                          for the model STANDARD_AIR)
 GAMMA_VALUE= 1.0165
-%
-% Specific gas constant (287.058 J/kg*K default and this value is hardcoded 
-%                        for the model STANDARD_AIR)
 GAS_CONSTANT= 35.23
-%
-% Critical Temperature (288.15 K by default)
 CRITICAL_TEMPERATURE= 564.1
-%
-% Critical Pressure (101325.0 N/m^2 by default)
 CRITICAL_PRESSURE= 1415000
-%
-% Critical Density (1.2886 Kg/m3 by default)
 CRITICAL_DENSITY= 256.74
-%
-% Acentri factor (0.035 (air))
 ACENTRIC_FACTOR= 0.529
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.3764E-5
-%
-% Sutherland Viscosity Ref (1.716E-5 default value for AIR SI)
 MU_REF= 1.716E-5
-%
-% Sutherland Temperature Ref (288.15 K default value for AIR SI)
 MU_T_REF= 288.15
-%
-% Sutherland constant (110.4 default value for AIR SI)
 SUTHERLAND_CONSTANT= 110.4
 
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
-% Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL).
 CONDUCTIVITY_MODEL= CONSTANT_CONDUCTIVITY
-%
-% Molecular Thermal Conductivity that would be constant (0.0257 by default)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.047280
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Inlet boundary type (TOTAL_CONDITIONS, MASS_FLOW)
 INLET_TYPE= TOTAL_CONDITIONS
-%
-% Inlet boundary marker(s) with the following formats (NONE = no marker) 
-% Total Conditions: (inlet marker, total temp, total pressure, flow_direction_x, 
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-% Mass Flow: (inlet marker, density, velocity magnitude, flow_direction_x, 
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-%MARKER_INLET= ( inflow, 404.1, 0.904E+05, 1.0, 0.0, 0.0 )
 MARKER_RIEMANN= (inflow, TOTAL_CONDITIONS_PT, 13.8686E+05, 592.295, 1.0, 0.0, 0.0, outflow, STATIC_PRESSURE, 11.00E+05, 0.0, 0.0, 0.0, 0.0)
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
-%MARKER_OUTLET= ( outflow, 0.523E+05 )
-%
-% Periodic boundary marker(s) (NONE = no marker)
-% Format: ( periodic marker, donor marker, rotation_center_x, rotation_center_y, 
-% rotation_center_z, rotation_angle_x-axis, rotation_angle_y-axis, 
-% rotation_angle_z-axis, translation_x, translation_y, translation_z, ... )
 MARKER_PERIODIC= ( periodic_1, periodic_2, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, -0.05749995, 0.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 ITER= 5000
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.75
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_vki_turbine_prepbc.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 500
-%
-
-% 
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG)
diff --git a/TestCases/nicf/coolprop/fluidModel.cfg b/TestCases/nicf/coolprop/fluidModel.cfg
index 7a3f6a1ac24..6b2fb858bc6 100644
--- a/TestCases/nicf/coolprop/fluidModel.cfg
+++ b/TestCases/nicf/coolprop/fluidModel.cfg
@@ -16,18 +16,15 @@ KIND_TURB_MODEL= SST
 MATH_PROBLEM= DIRECT
 RESTART_SOL= YES
 SYSTEM_MEASUREMENTS= SI
-%
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 1E-9
 AOA= 0.0
 SIDESLIP_ANGLE= 0.0
 INIT_OPTION= TD_CONDITIONS
 FREESTREAM_OPTION= TEMPERATURE_FS
 FREESTREAM_PRESSURE= 904388
-%
-% Free-stream temperature (288.15 K, 518.67 R by default)
 FREESTREAM_TEMPERATURE= 542.13
 REF_DIMENSIONALIZATION= DIMENSIONAL
 
@@ -35,6 +32,7 @@ REF_DIMENSIONALIZATION= DIMENSIONAL
 %
 FLUID_MODEL = COOLPROP
 FLUID_NAME  = nitrogen
+
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
 MU_CONSTANT= 1.21409E-05
@@ -67,11 +65,6 @@ LINEAR_SOLVER_ILU_FILL_IN= 0
 LINEAR_SOLVER_ERROR= 1E-6
 LINEAR_SOLVER_ITER= 10
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-grid levels (0 = no multi-grid)
-MGLEVEL= 0
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 CONV_NUM_METHOD_FLOW= ROE
 ENTROPY_FIX_COEFF= 0.1
@@ -83,41 +76,20 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
 CFL_REDUCTION_TURB= 1.0
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Number of total iterations
 ITER= 101
 CONV_RESIDUAL_MINVAL= -24
 CONV_STARTITER= 10
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= coolprop_nozzle.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 50
-%
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG)
diff --git a/TestCases/nicf/coolprop/transportModel.cfg b/TestCases/nicf/coolprop/transportModel.cfg
index 6b6d4ddb81f..b4b1d9c4906 100644
--- a/TestCases/nicf/coolprop/transportModel.cfg
+++ b/TestCases/nicf/coolprop/transportModel.cfg
@@ -5,7 +5,7 @@
 %                   diverging supersonic nozzle with CoolProp library          %
 % Author: Peng Yan, Alberto Guardone                                           %
 % Institution: Politecnico di Milano                                           %
-% Date: 2022.11.26                                                              %
+% Date: 2022.11.26                                                             %
 % File Version  7.4.0 Blackbird                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
@@ -16,23 +16,18 @@ KIND_TURB_MODEL= SST
 MATH_PROBLEM= DIRECT
 RESTART_SOL= YES
 SYSTEM_MEASUREMENTS= SI
-%
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
-%
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 1E-9
 AOA= 0.0
 SIDESLIP_ANGLE= 0.0
 INIT_OPTION= TD_CONDITIONS
 FREESTREAM_OPTION= TEMPERATURE_FS
 FREESTREAM_PRESSURE= 904388
-%
-% Free-stream temperature (288.15 K, 518.67 R by default)
 FREESTREAM_TEMPERATURE= 542.13
 REF_DIMENSIONALIZATION= DIMENSIONAL
 
 % ---- IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
-%
 FLUID_MODEL = COOLPROP
 FLUID_NAME  = Nitrogen
 VISCOSITY_MODEL = COOLPROP
@@ -62,11 +57,6 @@ LINEAR_SOLVER_ILU_FILL_IN= 0
 LINEAR_SOLVER_ERROR= 1E-6
 LINEAR_SOLVER_ITER= 10
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-grid levels (0 = no multi-grid)
-MGLEVEL= 0
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 CONV_NUM_METHOD_FLOW= ROE
 ENTROPY_FIX_COEFF= 0.1
@@ -78,41 +68,19 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
 CFL_REDUCTION_TURB= 1.0
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Number of total iterations
 ITER= 101
 CONV_RESIDUAL_MINVAL= -24
 CONV_STARTITER= 10
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-%
-% Mesh input file
 MESH_FILENAME= coolprop_nozzle.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 50
-%
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG)
diff --git a/TestCases/nicf/edge/edge_PPR.cfg b/TestCases/nicf/edge/edge_PPR.cfg
index 80d3ace0d95..8ce5f2a50b4 100644
--- a/TestCases/nicf/edge/edge_PPR.cfg
+++ b/TestCases/nicf/edge/edge_PPR.cfg
@@ -5,232 +5,104 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2012.09.29                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
-%
-% Physical governing equations (EULER, NAVIER_STOKES, NS_PLASMA)
 %                               
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
 
-%---------------------- REFERENCE VALUE DEFINITION ---------------------------%
-
-% ----------- COMPRESSIBLE FREE-STREAM DEFINITION ----------%
+% ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 1.7
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 1500112.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 564.1 
-
-% Free-stream temperature (1.2886 Kg/m3 by default)
 FREESTREAM_DENSITY= 230.0
-
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= DENSITY_FS
 
 % ---- IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
 % Values are characteristic for an MDM siloxane fluid near its critical point
-%
-% Different gas model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS)
-% Change this flag to select a different equation of state
 FLUID_MODEL= PR_GAS
-%
-% Ratio of specific heats (1.4 default and the value is hardcoded
-%                          for the model STANDARD_AIR)
 GAMMA_VALUE= 1.0125
-%
-% Specific gas constant (287.058 J/kg*K default and this value is hardcoded 
-%                        for the model STANDARD_AIR)
 GAS_CONSTANT= 35.152
 %
-%
-% Critical Temperature (131.00 K by default)
 CRITICAL_TEMPERATURE= 564.1
-%
-% Critical Pressure (3588550.0 N/m^2 by default)
 CRITICAL_PRESSURE= 1415200
-%
-% Critical Density (263.0 Kg/m3 by default)
 CRITICAL_DENSITY= 256.82
 %
-% Acentri factor (0.035 (air))
 ACENTRIC_FACTOR= 0.529
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( WALL1, WALL2 )
-%
 MARKER_RIEMANN= (INFLOW, STATIC_SUPERSONIC_INFLOW_PD, 1500112, 202.8878, 1.7, 0.0, 0.0, OUTFLOW, STATIC_PRESSURE, 1000.0, 0.0, 0.0, 0.0, 0.0)
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( NONE )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( WALL1 )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 500
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.9
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.9
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= NO
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-% 
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
diff --git a/TestCases/nicf/edge/edge_VW.cfg b/TestCases/nicf/edge/edge_VW.cfg
index cc023e17647..44e1f5c7c69 100644
--- a/TestCases/nicf/edge/edge_VW.cfg
+++ b/TestCases/nicf/edge/edge_VW.cfg
@@ -5,232 +5,106 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2012.09.29                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES, NS_PLASMA)
-%                               
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-
-%---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 
-% ----------- COMPRESSIBLE FREE-STREAM DEFINITION ----------%
+% ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 1.7
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 1500112.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 564.1 
-
-% Free-stream temperature (1.2886 Kg/m3 by default)
 FREESTREAM_DENSITY= 230.0
-
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= DENSITY_FS
 
 % ---- IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
 % Values are characteristic for an MDM siloxane fluid near its critical point
 %
-% Different gas model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS)
-% Change this flag to select a different equation of state
 FLUID_MODEL= VW_GAS
-%
-% Ratio of specific heats (1.4 default and the value is hardcoded
-%                          for the model STANDARD_AIR)
 GAMMA_VALUE= 1.0125
-%
-% Specific gas constant (287.058 J/kg*K default and this value is hardcoded 
-%                        for the model STANDARD_AIR)
 GAS_CONSTANT= 35.152
 %
-%
-% Critical Temperature (131.00 K by default)
 CRITICAL_TEMPERATURE= 564.1
-%
-% Critical Pressure (3588550.0 N/m^2 by default)
 CRITICAL_PRESSURE= 1415200
-%
-% Critical Density (263.0 Kg/m3 by default)
 CRITICAL_DENSITY= 256.82
 %
-% Acentri factor (0.035 (air))
 ACENTRIC_FACTOR= 0.529
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( WALL1, WALL2 )
-%
 MARKER_RIEMANN= (INFLOW, STATIC_SUPERSONIC_INFLOW_PD, 1500112, 202.8878, 1.7, 0.0, 0.0, OUTFLOW, STATIC_PRESSURE, 1000.0, 0.0, 0.0, 0.0, 0.0)
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( NONE )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( WALL1 )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 500
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.9
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.9
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= NO
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-% 
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
diff --git a/TestCases/nonequilibrium/invwedge/invwedge.cfg b/TestCases/nonequilibrium/invwedge/invwedge.cfg
index c198585d78b..604a12145ae 100644
--- a/TestCases/nonequilibrium/invwedge/invwedge.cfg
+++ b/TestCases/nonequilibrium/invwedge/invwedge.cfg
@@ -5,144 +5,72 @@
 % Author: C. Garbacz                                                           %
 % Institution: Strathclyde University                                          %
 % Date: 2020.11.01                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= NEMO_EULER
-%
 GAS_MODEL= AIR-5
-%
 GAS_COMPOSITION= (0.77, 0.23, 0.0, 0.0, 0.0)
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 5
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 FREESTREAM_TEMPERATURE_VE= 288.15
 
 % ---- NONEQUILIBRIUM GAS, IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
-% Fluid model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS,
-%              CONSTANT_DENSITY, INC_IDEAL_GAS, INC_IDEAL_GAS_POLY, MUTATIONPP, SU2_NONEQ)
 FLUID_MODEL= SU2_NONEQ
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( Euler, Wall )
 MARKER_OUTLET= ( Exit, 10 )
 MARKER_FAR = ( Farfield, Inlet )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= (NONE )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( Wall )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 3
-%
-% Number of total iterations
 ITER= 11
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= BCGSTAB
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -----------------------------------------------------------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= AUSM
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
-%
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -50
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= invwedge.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat  
-%
 TABULAR_FORMAT= TECPLOT 
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= convergence
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= soln_volume
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= soln_surface     
-%
-
 OUTPUT_WRT_FREQ= 100
-
 OUTPUT_FILES= (RESTART_ASCII, PARAVIEW_ASCII)
diff --git a/TestCases/nonequilibrium/invwedge/invwedge_ss_inlet.cfg b/TestCases/nonequilibrium/invwedge/invwedge_ss_inlet.cfg
new file mode 100644
index 00000000000..707af980723
--- /dev/null
+++ b/TestCases/nonequilibrium/invwedge/invwedge_ss_inlet.cfg
@@ -0,0 +1,79 @@
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+%                                                                              %
+% SU2 configuration file                                                       %
+% Case description: Mach 5 inviscid flow over a 10deg wedge - NEMO SS Inlet    %
+% Author: J. Needels                                                           %
+% Institution: Stanford University                                             %
+% Date: 2022.1.11                                                              %
+% File Version 7.5.0 "Blackbird"                                               %
+%                                                                              %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
+SOLVER= NEMO_EULER
+GAS_MODEL= AIR-5
+GAS_COMPOSITION= (0.77, 0.23, 0.0, 0.0, 0.0)
+MATH_PROBLEM= DIRECT
+RESTART_SOL= NO
+
+% ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
+%
+MACH_NUMBER= 5
+AOA= 0.0
+SIDESLIP_ANGLE= 0.0
+FREESTREAM_PRESSURE= 101325.0
+FREESTREAM_TEMPERATURE= 288.15
+FREESTREAM_TEMPERATURE_VE= 288.15
+
+% ---- NONEQUILIBRIUM GAS, IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
+%
+FLUID_MODEL= SU2_NONEQ
+
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
+MARKER_EULER= ( Euler, Wall )
+MARKER_OUTLET= ( Exit, 10 )
+MARKER_FAR = ( Farfield )
+MARKER_SUPERSONIC_INLET = ( Inlet, 288.15, 101325.0, 1705.16, 0.0, 0.0 )
+INLET_GAS_COMPOSITION = (0.77, 0.23, 0.0, 0.0, 0.0)
+INLET_TEMPERATURE_VE = 288.15
+MARKER_PLOTTING= ( NONE )
+MARKER_MONITORING= ( Wall )
+
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
+CFL_NUMBER= 3
+ITER= 11
+LINEAR_SOLVER= BCGSTAB
+LINEAR_SOLVER_ERROR= 1E-6
+LINEAR_SOLVER_ITER= 5
+
+% -----------------------------------------------------------------------%
+%
+CONV_NUM_METHOD_FLOW= AUSM
+MUSCL_FLOW= YES
+SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
+VENKAT_LIMITER_COEFF= 0.05
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
+CONV_RESIDUAL_MINVAL= -50
+CONV_STARTITER= 10
+CONV_CAUCHY_ELEMS= 100
+CONV_CAUCHY_EPS= 1E-10
+
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+%
+MESH_FILENAME= invwedge.su2
+MESH_FORMAT= SU2
+SOLUTION_FILENAME= restart_flow.dat  
+TABULAR_FORMAT= TECPLOT 
+CONV_FILENAME= convergence
+RESTART_FILENAME= restart_flow.dat
+VOLUME_FILENAME= soln_volume
+SURFACE_FILENAME= soln_surface     
+OUTPUT_WRT_FREQ= 100
+OUTPUT_FILES= (RESTART_ASCII, PARAVIEW_ASCII)
diff --git a/TestCases/nonequilibrium/thermalbath/finitechemistry/thermalbath.cfg b/TestCases/nonequilibrium/thermalbath/finitechemistry/thermalbath.cfg
index 6d28571e1b2..9169529de25 100644
--- a/TestCases/nonequilibrium/thermalbath/finitechemistry/thermalbath.cfg
+++ b/TestCases/nonequilibrium/thermalbath/finitechemistry/thermalbath.cfg
@@ -7,163 +7,81 @@
 % Author: C. Garbacz                                                           %
 % Institution: Strathclyde University                                          %
 % Date: 2019.04.10                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= NEMO_EULER         
-%
 GAS_MODEL= N2
-%
 GAS_COMPOSITION=(0.666667, 0.333333)
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
 READ_BINARY_RESTART= NO
-%
 TIME_MARCHING=TIME_STEPPING
 TIME_DOMAIN= YES
 TIME_STEP= 0.000000001 % 1.e-09
 MAX_TIME= 0.001
-%
+
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE_STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.0
-% Angle of attack (degrees)
 AOA = 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)
 FREESTREAM_PRESSURE = 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE = 30000
-%
-%Free-stream vibrational temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE_VE= 1000 
-%
+
 % ---- NONEQUILIBRIUM GAS, IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
-% Fluid model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS,
-%              CONSTANT_DENSITY, INC_IDEAL_GAS, INC_IDEAL_GAS_POLY, MUTATIONPP, SU2_NONEQ)
 FLUID_MODEL= SU2_NONEQ
-%
+
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_SYM= (left,bottom,top,right )
-%
-% Marker(s) of the surface to be plotted or designed
-%MARKER_MONITORING= ( bottom )
-%
+
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.0
-%
-% Number of total iterations
 TIME_ITER= 11
-%
+
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= ILU
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-10
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= AUSM
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_EXPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -50
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
-% Function to apply the criteria (LIFT, DRAG, NEARFIELD_PRESS, SENS_GEOMETRY, 
-% 	      	    		 SENS_MACH, DELTA_LIFT, DELTA_DRAG)
-OBJECTIVE_FUNCTION= DRAG
+
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= 5x5Mesh.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
 OUTPUT_FILES= (RESTART_ASCII)
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= test_flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
 SCREEN_WRT_FREQ_INNER= 10
-
 OUTPUT_WRT_FREQ= 10
diff --git a/TestCases/nonequilibrium/thermalbath/finitechemistry/weakly_ionized.cfg b/TestCases/nonequilibrium/thermalbath/finitechemistry/weakly_ionized.cfg
index c9b8be33cb2..22d7907f7a5 100644
--- a/TestCases/nonequilibrium/thermalbath/finitechemistry/weakly_ionized.cfg
+++ b/TestCases/nonequilibrium/thermalbath/finitechemistry/weakly_ionized.cfg
@@ -10,9 +10,6 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= NEMO_EULER         
 GAS_MODEL= AIR-7
 GAS_COMPOSITION=(0.0, 0.767, 0.233, 0.0, 0.0, 0.0, 0.0)
@@ -33,6 +30,7 @@ FREESTREAM_TEMPERATURE = 30000
 FREESTREAM_TEMPERATURE_VE= 1000 
 
 % ---- NONEQUILIBRIUM GAS, IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
+%
 FLUID_MODEL= SU2_NONEQ
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
diff --git a/TestCases/nonequilibrium/thermalbath/frozen/thermalbath_frozen.cfg b/TestCases/nonequilibrium/thermalbath/frozen/thermalbath_frozen.cfg
index 1340054f7e4..0d6aff1f891 100644
--- a/TestCases/nonequilibrium/thermalbath/frozen/thermalbath_frozen.cfg
+++ b/TestCases/nonequilibrium/thermalbath/frozen/thermalbath_frozen.cfg
@@ -6,165 +6,82 @@
 % Author: C. Garbacz                                                           %
 % Institution: Strathclyde University                                          %
 % Date: 2019.04.10                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= NEMO_EULER         
-%
 GAS_MODEL= N2
-%
 GAS_COMPOSITION=(0.666667, 0.333333)
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
 READ_BINARY_RESTART= NO
-%
 TIME_MARCHING=TIME_STEPPING
 TIME_DOMAIN= YES
 TIME_STEP= 0.000000001 % 1.e-09
 MAX_TIME= 0.001
-%
+
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE_STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.0
-% Angle of attack (degrees)
 AOA = 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)
 FREESTREAM_PRESSURE = 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE = 30000
-%
-%Free-stream vibrational temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE_VE= 1000 
-%
+
 % ---- NONEQUILIBRIUM GAS, IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
-% Fluid model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS,
-%              CONSTANT_DENSITY, INC_IDEAL_GAS, INC_IDEAL_GAS_POLY, MUTATIONPP, SU2_NONEQ)
 FLUID_MODEL= SU2_NONEQ
-%
 FROZEN_MIXTURE= YES
-%
+
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_SYM= (left,bottom,top,right )
-%
-% Marker(s) of the surface to be plotted or designed
 %MARKER_MONITORING= ( bottom )
-%
+
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.0
-%
-% Number of total iterations
 TIME_ITER= 11
-%
+
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= ILU
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-10
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= AUSM
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_EXPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -50
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
-% Function to apply the criteria (LIFT, DRAG, NEARFIELD_PRESS, SENS_GEOMETRY, 
-% 	      	    		 SENS_MACH, DELTA_LIFT, DELTA_DRAG)
-OBJECTIVE_FUNCTION= DRAG
+
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= 5x5Mesh.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
 OUTPUT_FILES= (RESTART_ASCII, TECPLOT_ASCII)
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= test_flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
 SCREEN_WRT_FREQ_INNER= 10
-
 OUTPUT_WRT_FREQ= 10
diff --git a/TestCases/nonequilibrium/viscous/axi_visccone.cfg b/TestCases/nonequilibrium/viscous/axi_visccone.cfg
index bc976a28601..b2f76f8a785 100644
--- a/TestCases/nonequilibrium/viscous/axi_visccone.cfg
+++ b/TestCases/nonequilibrium/viscous/axi_visccone.cfg
@@ -4,7 +4,7 @@
 % Case description: Mach 5 viscous flow over a 10deg axisymmetric cone         %
 % Author: C. Garbacz                                                           %
 % Institution: Strathclyde University                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nonequilibrium/viscous/partial_cat.cfg b/TestCases/nonequilibrium/viscous/partial_cat.cfg
index d848fe962d2..b0b37728fdc 100644
--- a/TestCases/nonequilibrium/viscous/partial_cat.cfg
+++ b/TestCases/nonequilibrium/viscous/partial_cat.cfg
@@ -5,7 +5,7 @@
 %                   catalytic walls - gamma model, effeciency = 0.2            %
 % Author: J. Needels                                                           %
 % Institution: Stanford University                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -36,7 +36,6 @@ FLUID_MODEL= SU2_NONEQ
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( Euler)
 MARKER_ISOTHERMAL= (Wall, 300)
 MARKER_OUTLET= ( Exit, 5 )
diff --git a/TestCases/nonequilibrium/viscous/super_cat.cfg b/TestCases/nonequilibrium/viscous/super_cat.cfg
index a4bde59a0ea..b11a8b8d8cc 100644
--- a/TestCases/nonequilibrium/viscous/super_cat.cfg
+++ b/TestCases/nonequilibrium/viscous/super_cat.cfg
@@ -5,7 +5,7 @@
 %                   catalytic walls - gamma model, effeciency = 0.2            %
 % Author: J. Needels                                                           %
 % Institution: Stanford University                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -36,7 +36,6 @@ FLUID_MODEL= SU2_NONEQ
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( Euler)
 MARKER_ISOTHERMAL= (Wall, 300)
 MARKER_OUTLET= ( Exit, 5 )
diff --git a/TestCases/nonequilibrium/viscwedge_mpp/viscwedge_mpp.cfg b/TestCases/nonequilibrium/viscwedge_mpp/viscwedge_mpp.cfg
index 465ed03bccd..a62a1a4d87d 100644
--- a/TestCases/nonequilibrium/viscwedge_mpp/viscwedge_mpp.cfg
+++ b/TestCases/nonequilibrium/viscwedge_mpp/viscwedge_mpp.cfg
@@ -5,148 +5,74 @@
 % Author: C. Garbacz                                                           %
 % Institution: Strathclyde University                                          %
 % Date: 2020.11.01                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= NEMO_NAVIER_STOKES
-%
 GAS_MODEL= air_5
-%
 GAS_COMPOSITION= (0.0, 0.0, 0.0, 0.77, 0.23)
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 5
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Init option to choose between Reynolds (default) or thermodynamics quantities
-% for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 10.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 FREESTREAM_TEMPERATURE_VE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 10000
 KIND_TURB_MODEL= NONE
 
 % ---- NONEQUILIBRIUM GAS, IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
-% Fluid model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS,
-%              CONSTANT_DENSITY, INC_IDEAL_GAS, INC_IDEAL_GAS_POLY, MUTATIONPP, SU2_NONEQ)
 FLUID_MODEL= MUTATIONPP
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( Euler)
 MARKER_ISOTHERMAL= (Wall, 300)
 MARKER_OUTLET= ( Exit, 5 )
 MARKER_FAR= ( Farfield, Inlet )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= (NONE )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( Wall )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 0.5
-%
-% Number of total iterations
 ITER= 11
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= BCGSTAB
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -----------------------------------------------------------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= AUSM
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
-%
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the Venkat's limiter (upwind scheme). A larger values decrease
-%             the extent of limiting, values approaching zero cause
-%             lower-order approximation to the solution (0.05 by default)
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_EXPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -15
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
+
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= viscwedge.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat  
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= convergence
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= soln_volume
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= soln_surface     
-%
 OUTPUT_WRT_FREQ= 100
-%
 OUTPUT_FILES= (RESTART_ASCII, PARAVIEW_ASCII)
diff --git a/TestCases/optimization_euler/equivalentarea_naca64206/NACA64206.cfg b/TestCases/optimization_euler/equivalentarea_naca64206/NACA64206.cfg
index 09c21f05503..a7d2293ae9c 100644
--- a/TestCases/optimization_euler/equivalentarea_naca64206/NACA64206.cfg
+++ b/TestCases/optimization_euler/equivalentarea_naca64206/NACA64206.cfg
@@ -5,7 +5,7 @@
 % Author: Yuki Utsumi                                                          %
 % Institution: Individual                                                      %
 % Date: 2021.08.07                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -17,19 +17,10 @@ READ_BINARY_RESTART= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 1.6
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only for Euler equations)
 FREESTREAM_PRESSURE= 11662.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 216.6499
 
 REF_ORIGIN_MOMENT_X = 0.25
@@ -40,6 +31,7 @@ REF_AREA= 0
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ------------------------ SUPERSONIC SIMULATION ------------------------------%
+%
 % MARKER_NEARFIELD needs to be defined on a circumferential boundary within
 % calculation domain so that it captures pressure disturbance from the model.
 % The boundary should have a structured grid with the same number of nodes
@@ -71,17 +63,12 @@ MARKER_SUPERSONIC_OUTLET=(Outlet)
 MARKER_SYM= ( Symmetry )
 MARKER_PLOTTING= ( Wing )
 MARKER_MONITORING= ( Wing )
-%
-% Near-Field boundary marker(s) (NONE = no marker)
 MARKER_NEARFIELD= ( Nearfield )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
 NUM_METHOD_GRAD= GREEN_GAUSS
-
-% Objective function in gradient evaluation
 OBJECTIVE_FUNCTION= EQUIVALENT_AREA
-%
 CFL_NUMBER=3
 CFL_ADAPT= NO
 ITER=4000
@@ -97,10 +84,6 @@ ADJ_SHARP_LIMITER_COEFF= 3.0
 REF_SHARP_EDGES= 3.0
 SENS_REMOVE_SHARP= YES
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-MGLEVEL= 0
-%
 % ----------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION ------------------%
 %
 RELAXATION_FACTOR_ADJOINT= 1.0
diff --git a/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_2surf_1obj.cfg b/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_2surf_1obj.cfg
index 983bc39ff9b..0d7fd536f46 100644
--- a/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_2surf_1obj.cfg
+++ b/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_2surf_1obj.cfg
@@ -7,396 +7,143 @@
 % Author: H.L. Kline, modified from inviscid wedge by Thomas D. Economon       %
 % Institution: Stanford University                                             %
 % Date: 2018.01.07                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               TNE2_EULER, TNE2_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= CONTINUOUS_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
-% Number of Zones
 NZONES= 1
+
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 2.0
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 100000.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( upper, lower )
-%
-% Supersonic inlet boundary marker(s) (NONE = no marker) 
-% Total Conditions: (inlet marker, temperature, static pressure, velocity_x, 
-%           velocity_y, velocity_z, ... ), i.e. all variables specified.
 MARKER_SUPERSONIC_INLET= ( inlet, 300.0, 100000.0, 695.4290761824674, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
 MARKER_OUTLET= ( outlet, 10000.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( lower )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= (outlet,lower)
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER=1
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= BCGSTAB
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (1 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
 
-
-
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.8
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.006
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Relaxation coefficient
 RELAXATION_FACTOR_ADJOINT= 1.0
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.8
-%
-% Limit value for the adjoint variable
 LIMIT_ADJFLOW= 1E15
-%
-% Multigrid adjoint problem (NO, YES)
 MG_ADJFLOW= NO
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE, 
-%                                             SURFACE_MASSFLOW)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION = DRAG
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT= 1.0
-%
-% Marker on which to track one-dimensionalized quantities
 MARKER_ANALYZE  = (outlet)
-%
-% Method to compute the average value in MARKER_ANALYZE (AREA, MASSFLUX).
 MARKER_ANALYZE_AVERAGE = AREA
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -11
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
+
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_wedge_inv_FFD.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-%
-% Read binary restart files
 READ_BINARY_RESTART = NO
-%
 OUTPUT_FILES= (RESTART_ASCII, PARAVIEW, SURFACE_CSV)
+HISTORY_OUTPUT= (ITER, RMS_RES, AERO_COEFF)
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-10
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 500
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (MAIN_BOX, 0.5, -0.25, 0, 1.5, -0.25, 0, 1.5, 0.25,  0, 0.5, 0.25,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= (10, 1,0)
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= 2ND_DERIVATIVE
+
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION, 
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION)
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( lower )
-%
 DV_KIND= FFD_CONTROL_POINT_2D
-%
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( 1st digit, 2nd and 3rd digit )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= (MAIN_BOX, 3,0, 0,1.0,0,0 )
-%
-% Value of the shape deformation deformation
 DV_VALUE= 0.5
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor, separated by semicolons.
-% To include quadratic penalty function: use OPT_CONSTRAINT option syntax within the OPT_OBJECTIVE list.
-% ex= Objective * Scale
 OPT_OBJECTIVE=DRAG
-%
-% Use combined objective within gradient evaluation: may reduce cost to compute gradients when using the adjoint formulation.
 OPT_COMBINE_OBJECTIVE = NO
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= NONE
-%
-% Maximum number of iterations
 OPT_ITERATIONS= 1
-%
-% Requested accuracy
 OPT_ACCURACY= 1E-6
-%
-% Upper bound for each design variable
 OPT_BOUND_UPPER= 0.1
-%
-% Lower bound for each design variable
 OPT_BOUND_LOWER= -0.1
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= (19, 1.0| lower | MAIN_BOX, 3,0,0,1.0);(19, 1.0| lower | MAIN_BOX, 4,0,0,1.0);(19, 1.0| lower | MAIN_BOX, 5,0,0,1.0);(19, 1.0| lower | MAIN_BOX, 6,0,0,1.0)
-
-HISTORY_OUTPUT= (ITER, RMS_RES, AERO_COEFF)
diff --git a/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj.cfg b/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj.cfg
index ebdaad85f10..5622aba2fa2 100644
--- a/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj.cfg
+++ b/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj.cfg
@@ -8,396 +8,144 @@
 % Author: H.L. Kline, modified from inviscid wedge by Thomas D. Economon       %
 % Institution: Stanford University                                             %
 % Date: 2018.01.07                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               TNE2_EULER, TNE2_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= CONTINUOUS_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
-% Number of Zones
 NZONES= 1
+
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 2.0
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 100000.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( upper, lower )
-%
-% Supersonic inlet boundary marker(s) (NONE = no marker) 
-% Total Conditions: (inlet marker, temperature, static pressure, velocity_x, 
-%           velocity_y, velocity_z, ... ), i.e. all variables specified.
 MARKER_SUPERSONIC_INLET= ( inlet, 300.0, 100000.0, 695.4290761824674, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
 MARKER_OUTLET= ( outlet, 10000.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( lower )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= (outlet, lower)
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= YES
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 0.1, 2.0, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER=1
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= BCGSTAB
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (1 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
 
 
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.8
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.006
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-%
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Relaxation coefficient
 RELAXATION_FACTOR_ADJOINT= 1.0
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.8
-%
-% Limit value for the adjoint variable
 LIMIT_ADJFLOW= 1E15
-%
-% Multigrid adjoint problem (NO, YES)
 MG_ADJFLOW= NO
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE, 
-%                                             SURFACE_MASSFLOW)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION = SURFACE_TOTAL_PRESSURE, DRAG
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT= -1.0E-7,1.0
-%
-% Marker on which to track one-dimensionalized quantities
 MARKER_ANALYZE  = (outlet)
-%
-% Method to compute the average value in MARKER_ANALYZE (AREA, MASSFLUX).
 MARKER_ANALYZE_AVERAGE = AREA
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -11
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
+
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_wedge_inv_FFD.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-%
-% Read binary restart files
 READ_BINARY_RESTART = NO
-%
 OUTPUT_FILES = (RESTART_ASCII, PARAVIEW, SURFACE_CSV)
+HISTORY_OUTPUT=(ITER, RMS_RES, AERO_COEFF, FLOW_COEFF, COMBO)
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-10
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 500
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (MAIN_BOX, 0.5, -0.25, 0, 1.5, -0.25, 0, 1.5, 0.25,  0, 0.5, 0.25,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= (10, 1,0)
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= 2ND_DERIVATIVE
+
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION, 
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION)
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( lower )
-%
 DV_KIND= FFD_CONTROL_POINT_2D
-%
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( 1st digit, 2nd and 3rd digit )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= (MAIN_BOX, 3,0, 0,1.0,0,0 )
-%
-% Value of the shape deformation deformation
 DV_VALUE= 0.5
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor, separated by semicolons.
-% To include quadratic penalty function: use OPT_CONSTRAINT option syntax within the OPT_OBJECTIVE list.
-% ex= Objective * Scale
 OPT_OBJECTIVE=SURFACE_TOTAL_PRESSURE*-1E-4; (DRAG = 0.05)*1E6
-%
-% Use combined objective within gradient evaluation: may reduce cost to compute gradients when using the adjoint formulation.
 OPT_COMBINE_OBJECTIVE = NO
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= NONE
-%
-% Maximum number of iterations
 OPT_ITERATIONS= 1
-%
-% Requested accuracy
 OPT_ACCURACY= 1E-6
-%
-% Upper bound for each design variable
 OPT_BOUND_UPPER= 0.1
-%
-% Lower bound for each design variable
 OPT_BOUND_LOWER= -0.1
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= (19, 1.0| lower | MAIN_BOX, 3,0,0,1.0);(19, 1.0| lower | MAIN_BOX, 4,0,0,1.0);(19, 1.0| lower | MAIN_BOX, 5,0,0,1.0);(19, 1.0| lower | MAIN_BOX, 6,0,0,1.0)
-
-HISTORY_OUTPUT=(ITER, RMS_RES, AERO_COEFF, FLOW_COEFF, COMBO)
diff --git a/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj_1surf.cfg b/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj_1surf.cfg
index d2677c1840c..32dae495b59 100644
--- a/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj_1surf.cfg
+++ b/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj_1surf.cfg
@@ -8,396 +8,143 @@
 % Author: H.L. Kline, modified from inviscid wedge by Thomas D. Economon       %
 % Institution: Stanford University                                             %
 % Date: 2018.01.07                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               TNE2_EULER, TNE2_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= CONTINUOUS_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
-% Number of Zones
 NZONES= 1
+
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 2.0
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 100000.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( upper, lower )
-%
-% Supersonic inlet boundary marker(s) (NONE = no marker) 
-% Total Conditions: (inlet marker, temperature, static pressure, velocity_x, 
-%           velocity_y, velocity_z, ... ), i.e. all variables specified.
 MARKER_SUPERSONIC_INLET= ( inlet, 300.0, 100000.0, 695.4290761824674, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
 MARKER_OUTLET= ( outlet, 10000.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( lower )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= (lower)
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER=1
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= BCGSTAB
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (1 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
 
-
-
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.8
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.006
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Relaxation coefficient
 RELAXATION_FACTOR_ADJOINT= 1.0
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.8
-%
-% Limit value for the adjoint variable
 LIMIT_ADJFLOW= 1E15
-%
-% Multigrid adjoint problem (NO, YES)
 MG_ADJFLOW= NO
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE, 
-%                                             SURFACE_MASSFLOW)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION = SURFACE_TOTAL_PRESSURE, DRAG
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT= -1.0E-7,1.0
-%
-% Marker on which to track one-dimensionalized quantities
 MARKER_ANALYZE  = (outlet)
-%
-% Method to compute the average value in MARKER_ANALYZE (AREA, MASSFLUX).
 MARKER_ANALYZE_AVERAGE = AREA
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -11
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
+
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_wedge_inv_FFD.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-%
-% Read binary restart files
 READ_BINARY_RESTART = NO
-%
 OUTPUT_FILES= (RESTART_ASCII, PARAVIEW, SURFACE_CSV)
+HISTORY_OUTPUT=(ITER, RMS_RES, AERO_COEFF, FLOW_COEFF, COMBO)
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-10
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 500
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (MAIN_BOX, 0.5, -0.25, 0, 1.5, -0.25, 0, 1.5, 0.25,  0, 0.5, 0.25,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= (10, 1,0)
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= 2ND_DERIVATIVE
+
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION, 
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION)
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( lower )
-%
 DV_KIND= FFD_CONTROL_POINT_2D
-%
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( 1st digit, 2nd and 3rd digit )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= (MAIN_BOX, 3,0, 0,1.0,0,0 )
-%
-% Value of the shape deformation deformation
 DV_VALUE= 0.5
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor, separated by semicolons.
-% To include quadratic penalty function: use OPT_CONSTRAINT option syntax within the OPT_OBJECTIVE list.
-% ex= Objective * Scale
 OPT_OBJECTIVE=LIFT*-1E-4; (DRAG = 0.05)*1E6
-%
-% Use combined objective within gradient evaluation: may reduce cost to compute gradients when using the adjoint formulation.
 OPT_COMBINE_OBJECTIVE = YES
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= NONE
-%
-% Maximum number of iterations
 OPT_ITERATIONS= 1
-%
-% Requested accuracy
 OPT_ACCURACY= 1E-6
-%
-% Upper bound for each design variable
 OPT_BOUND_UPPER= 0.1
-%
-% Lower bound for each design variable
 OPT_BOUND_LOWER= -0.1
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= (19, 1.0| lower | MAIN_BOX, 3,0,0,1.0);(19, 1.0| lower | MAIN_BOX, 4,0,0,1.0);(19, 1.0| lower | MAIN_BOX, 5,0,0,1.0);(19, 1.0| lower | MAIN_BOX, 6,0,0,1.0)
-
-HISTORY_OUTPUT=(ITER, RMS_RES, AERO_COEFF, FLOW_COEFF, COMBO)
diff --git a/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj_combo.cfg b/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj_combo.cfg
index 0dd7b187c58..d08e451eae9 100644
--- a/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj_combo.cfg
+++ b/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj_combo.cfg
@@ -10,394 +10,142 @@
 % Author: H.L. Kline, modified from inviscid wedge by Thomas D. Economon       %
 % Institution: Stanford University                                             %
 % Date: 2018.01.07                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               TNE2_EULER, TNE2_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= CONTINUOUS_ADJOINT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
-% Number of Zones
 NZONES= 1
+
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 2.0
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 100000.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( upper, lower )
-%
-% Supersonic inlet boundary marker(s) (NONE = no marker) 
-% Total Conditions: (inlet marker, temperature, static pressure, velocity_x, 
-%           velocity_y, velocity_z, ... ), i.e. all variables specified.
 MARKER_SUPERSONIC_INLET= ( inlet, 300.0, 100000.0, 695.4290761824674, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
 MARKER_OUTLET= ( outlet, 10000.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( lower )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= (outlet, lower)
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= YES
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 0.1, 2.0, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER=1
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= BCGSTAB
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (1 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
 
-
-
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.8
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.006
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Relaxation coefficient
 RELAXATION_FACTOR_ADJOINT= 1.0
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.8
-%
-% Limit value for the adjoint variable
 LIMIT_ADJFLOW= 1E15
-%
-% Multigrid adjoint problem (NO, YES)
 MG_ADJFLOW= NO
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE, 
-%                                             SURFACE_MASSFLOW)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION = SURFACE_TOTAL_PRESSURE, DRAG
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT= -1.0E-7,1.0
-%
-% Marker on which to track one-dimensionalized quantities
 MARKER_ANALYZE  = (outlet)
-%
-% Method to compute the average value in MARKER_ANALYZE (AREA, MASSFLUX).
 MARKER_ANALYZE_AVERAGE = AREA
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -11
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
+
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_wedge_inv_FFD.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-%
-% Read binary restart files
 READ_BINARY_RESTART = NO
+HISTORY_OUTPUT=(ITER, RMS_RES, AERO_COEFF, FLOW_COEFF, COMBO)
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-10
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 500
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (MAIN_BOX, 0.5, -0.25, 0, 1.5, -0.25, 0, 1.5, 0.25,  0, 0.5, 0.25,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= (10, 1,0)
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= 2ND_DERIVATIVE
+
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION, 
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION)
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( lower )
-%
 DV_KIND= FFD_CONTROL_POINT_2D
-%
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( 1st digit, 2nd and 3rd digit )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= (MAIN_BOX, 3,0, 0,1.0,0,0 )
-%
-% Value of the shape deformation deformation
 DV_VALUE= 0.5
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor, separated by semicolons.
-% To include quadratic penalty function: use OPT_CONSTRAINT option syntax within the OPT_OBJECTIVE list.
-% ex= Objective * Scale
 OPT_OBJECTIVE=SURFACE_TOTAL_PRESSURE*-1E-4; (DRAG = 0.05)*1E6
-%
-% Use combined objective within gradient evaluation: may reduce cost to compute gradients when using the adjoint formulation.
 OPT_COMBINE_OBJECTIVE = YES
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= NONE
-%
-% Maximum number of iterations
 OPT_ITERATIONS= 1
-%
-% Requested accuracy
 OPT_ACCURACY= 1E-6
-%
-% Upper bound for each design variable
 OPT_BOUND_UPPER= 0.1
-%
-% Lower bound for each design variable
 OPT_BOUND_LOWER= -0.1
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= (19, 1.0| lower | MAIN_BOX, 3,0,0,1.0);(19, 1.0| lower | MAIN_BOX, 4,0,0,1.0);(19, 1.0| lower | MAIN_BOX, 5,0,0,1.0);(19, 1.0| lower | MAIN_BOX, 6,0,0,1.0)
-
-HISTORY_OUTPUT=(ITER, RMS_RES, AERO_COEFF, FLOW_COEFF, COMBO)
diff --git a/TestCases/optimization_euler/multipoint_naca0012/inv_NACA0012_multipoint.cfg b/TestCases/optimization_euler/multipoint_naca0012/inv_NACA0012_multipoint.cfg
index 86558315c5c..55767d72add 100644
--- a/TestCases/optimization_euler/multipoint_naca0012/inv_NACA0012_multipoint.cfg
+++ b/TestCases/optimization_euler/multipoint_naca0012/inv_NACA0012_multipoint.cfg
@@ -5,347 +5,129 @@
 % Author: Indiana Stokes                                                       %
 % Institution:                                                                 %
 % Date: 2017.07.03                                                             %
-% File Version 7.4.0 "Blackbird"                                                   %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION) 
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AOA= 1.25
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 100
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (LU_SGS,
-%                                              SYM_GAUSS_SEIDEL, BCGSTAB, GMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (NONE, JACOBI, LINELET, LUSGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
+% --------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-Grid PreSmoothing Level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 1.0
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 1.0
-
-% --------------------- FLOW NUMERICAL METHOD DEFINITION ----------------------%
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                              ROE-2ND_ORDER)
 CONV_NUM_METHOD_FLOW= JST
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE)
-OBJECTIVE_FUNCTION= DRAG
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                              ROE-2ND_ORDER)
+OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.8
 
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
 %
 % Marker(s) of the surface where geometrical based function will be evaluated
 GEO_MARKER= ( airfoil )
-%
-% Description of the geometry to be analyzed (AIRFOIL, WING, FUSELAGE)
 GEO_DESCRIPTION= AIRFOIL
-%
-% Geometrical evaluation mode (FUNCTION, GRADIENT)
 GEO_MODE= FUNCTION
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION, 
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION)
 DV_KIND= HICKS_HENNE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( 1st digit, 2nd and 3rd digit )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= ( 1, 0.5 )
-%
-% Value of the shape deformation deformation
 DV_VALUE= 1.0
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -13
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA0012_inv.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
 % Definition of multipoint design problems, this option should be combined with the
 % the prefix MULTIPOINT in the objective function or constraint (e.g. MULTIPOINT_DRAG, MULTIPOINT_LIFT, etc.)
 MULTIPOINT_WEIGHT= (0.25, 0.5, 0.25)
 MULTIPOINT_MACH_NUMBER= (0.79, 0.8, 0.81)
-%MULTIPOINT_AOA= (1.25, 1.25, 1.25)
-%MULTIPOINT_SIDESLIP_ANGLE= (0.0, 0.0, 0.0)
-%MULTIPOINT_REYNOLDS_NUMBER= (1E6, 1E6, 1E6)
-%MULTIPOINT_TARGET_CL= (0.8, 0.8, 0.8)
-%MULTIPOINT_FREESTREAM_PRESSURE= (101325.0, 101325.0, 101325.0)
-%MULTIPOINT_FREESTREAM_TEMPERATURE= (288.15, 288.15, 288.15)
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= MULTIPOINT_DRAG * 0.001
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= NONE
-%
-% Maximum number of optimizer iterations
 OPT_ITERATIONS= 100
-%
-% Requested accuracy
 OPT_ACCURACY= 1E-6
-%
-% Upper bound for each design variable
 OPT_BOUND_UPPER= 1E6
-%
-% Lower bound for each design variable
 OPT_BOUND_LOWER= -1E6
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 ); ( 30, 1.0 | airfoil | 0, 0.20 ); ( 30, 1.0 | airfoil | 0, 0.25 ); ( 30, 1.0 | airfoil | 0, 0.30 ); ( 30, 1.0 | airfoil | 0, 0.35 ); ( 30, 1.0 | airfoil | 0, 0.40 ); ( 30, 1.0 | airfoil | 0, 0.45 ); ( 30, 1.0 | airfoil | 0, 0.50 ); ( 30, 1.0 | airfoil | 0, 0.55 ); ( 30, 1.0 | airfoil | 0, 0.60 ); ( 30, 1.0 | airfoil | 0, 0.65 ); ( 30, 1.0 | airfoil | 0, 0.70 ); ( 30, 1.0 | airfoil | 0, 0.75 ); ( 30, 1.0 | airfoil | 0, 0.80 ); ( 30, 1.0 | airfoil | 0, 0.85 ); ( 30, 1.0 | airfoil | 0, 0.90 ); ( 30, 1.0 | airfoil | 0, 0.95 ); ( 30, 1.0 | airfoil | 1, 0.05 ); ( 30, 1.0 | airfoil | 1, 0.10 ); ( 30, 1.0 | airfoil | 1, 0.15 ); ( 30, 1.0 | airfoil | 1, 0.20 ); ( 30, 1.0 | airfoil | 1, 0.25 ); ( 30, 1.0 | airfoil | 1, 0.30 ); ( 30, 1.0 | airfoil | 1, 0.35 ); ( 30, 1.0 | airfoil | 1, 0.40 ); ( 30, 1.0 | airfoil | 1, 0.45 ); ( 30, 1.0 | airfoil | 1, 0.50 ); ( 30, 1.0 | airfoil | 1, 0.55 ); ( 30, 1.0 | airfoil | 1, 0.60 ); ( 30, 1.0 | airfoil | 1, 0.65 ); ( 30, 1.0 | airfoil | 1, 0.70 ); ( 30, 1.0 | airfoil | 1, 0.75 ); ( 30, 1.0 | airfoil | 1, 0.80 ); ( 30, 1.0 | airfoil | 1, 0.85 ); ( 30, 1.0 | airfoil | 1, 0.90 ); ( 30, 1.0 | airfoil | 1, 0.95 )
diff --git a/TestCases/optimization_euler/pitching_naca64a010/pitching_NACA64A010.cfg b/TestCases/optimization_euler/pitching_naca64a010/pitching_NACA64A010.cfg
index 45d484eeb36..a30740c45d2 100644
--- a/TestCases/optimization_euler/pitching_naca64a010/pitching_NACA64A010.cfg
+++ b/TestCases/optimization_euler/pitching_naca64a010/pitching_NACA64A010.cfg
@@ -5,375 +5,156 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-%
-% Time Step for dual time stepping simulations (s)
 TIME_STEP= 0.0023555025613149587
 % 24 steps per period: 0.0024536485013697488
 % 25 steps per period: 0.0023555025613149587
-%
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 0.59
 % 10 periods: 0.5888756403287397
-%
-% Number of internal iterations (dual time method)
 INNER_ITER= 110
-%
-% Starting direct iteration for unsteady adjoint
 UNST_ADJOINT_ITER= 251
 
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Dynamic mesh simulation (NO, YES)
 GRID_MOVEMENT= YES
-%
-% Type of mesh motion (NONE, FLUTTER, RIGID_MOTION)
 GRID_MOVEMENT_KIND= RIGID_MOTION
-%
-% Motion mach number (non-dimensional). Used for initializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.796
-%
-% Coordinates of the rigid motion origin
 MOTION_ORIGIN_X= 0.248
 MOTION_ORIGIN_Y= 0.0
 MOTION_ORIGIN_Z= 0.0
-%
-% Pitching angular freq. (rad/s) about x, y, & z axes (RIGID_MOTION only)
 PITCHING_OMEGA_X= 0.0
 PITCHING_OMEGA_Y= 0.0
 PITCHING_OMEGA_Z= 106.69842
-%
-% Pitching amplitude (degrees) about x, y, & z axes (RIGID_MOTION only)
 PITCHING_AMPL_X= 0.0
 PITCHING_AMPL_Y= 0.0
 PITCHING_AMPL_Z= 1.01
  
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.796
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.248
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( airfoil )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( airfoil )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.9
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.9
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.1
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, TORQUE)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.5
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Adjoint frozen viscosity (NO, YES)
 FROZEN_VISC_CONT= YES
 
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
 %
-% Marker(s) of the surface where geometrical based function will be evaluated
 GEO_MARKER= ( airfoil )
-%
-% Description of the geometry to be analyzed (AIRFOIL, WING, FUSELAGE)
 GEO_DESCRIPTION= AIRFOIL
-%
-% Geometrical evaluation mode (FUNCTION, GRADIENT)
 GEO_MODE= FUNCTION
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION, 
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION)
-DV_KIND= HICKS_HENNE
 %
-% Marker of the surface in which we are going apply the shape deformation
+DV_KIND= HICKS_HENNE
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( 1st digit, 2nd and 3rd digit )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= ( 1, 0.5 )
-%
-% Old value of the deformation for incremental deformations
 DV_VALUE= 0.0
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 %
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA64A010_inv.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1
-%
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-
-% Optimization objective function with optional scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.001
-
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= ( LIFT = 0.0 ) * 0.001; ( AREA > 0.0660957 ) * 0.001
-%
-% List of design variables (Design variables are separated by semicolons)
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.961538461538 ); ( 30, 1.0 | airfoil | 0, 0.923076923077 ); ( 30, 1.0 | airfoil | 0, 0.884615384615 ); ( 30, 1.0 | airfoil | 0, 0.846153846154 ); ( 30, 1.0 | airfoil | 0, 0.807692307692 ); ( 30, 1.0 | airfoil | 0, 0.769230769231 ); ( 30, 1.0 | airfoil | 0, 0.730769230769 ); ( 30, 1.0 | airfoil | 0, 0.692307692308 ); ( 30, 1.0 | airfoil | 0, 0.653846153846 ); ( 30, 1.0 | airfoil | 0, 0.615384615385 ); ( 30, 1.0 | airfoil | 0, 0.576923076923 ); ( 30, 1.0 | airfoil | 0, 0.538461538462 ); ( 30, 1.0 | airfoil | 0, 0.5 ); ( 30, 1.0 | airfoil | 0, 0.461538461538 ); ( 30, 1.0 | airfoil | 0, 0.423076923077 ); ( 30, 1.0 | airfoil | 0, 0.384615384615 ); ( 30, 1.0 | airfoil | 0, 0.346153846154 ); ( 30, 1.0 | airfoil | 0, 0.307692307692 ); ( 30, 1.0 | airfoil | 0, 0.269230769231 ); ( 30, 1.0 | airfoil | 0, 0.230769230769 ); ( 30, 1.0 | airfoil | 0, 0.192307692308 ); ( 30, 1.0 | airfoil | 0, 0.153846153846 ); ( 30, 1.0 | airfoil | 0, 0.115384615385 ); ( 30, 1.0 | airfoil | 0, 0.0769230769231 ); ( 30, 1.0 | airfoil | 0, 0.0384615384615 ); ( 30, 1.0 | airfoil | 1, 0.0384615384615 ); ( 30, 1.0 | airfoil | 1, 0.0769230769231 ); ( 30, 1.0 | airfoil | 1, 0.115384615385 ); ( 30, 1.0 | airfoil | 1, 0.153846153846 ); ( 30, 1.0 | airfoil | 1, 0.192307692308 ); ( 30, 1.0 | airfoil | 1, 0.230769230769 ); ( 30, 1.0 | airfoil | 1, 0.269230769231 ); ( 30, 1.0 | airfoil | 1, 0.307692307692 ); ( 30, 1.0 | airfoil | 1, 0.346153846154 ); ( 30, 1.0 | airfoil | 1, 0.384615384615 ); ( 30, 1.0 | airfoil | 1, 0.423076923077 ); ( 30, 1.0 | airfoil | 1, 0.461538461538 ); ( 30, 1.0 | airfoil | 1, 0.5 ); ( 30, 1.0 | airfoil | 1, 0.538461538462 ); ( 30, 1.0 | airfoil | 1, 0.576923076923 ); ( 30, 1.0 | airfoil | 1, 0.615384615385 ); ( 30, 1.0 | airfoil | 1, 0.653846153846 ); ( 30, 1.0 | airfoil | 1, 0.692307692308 ); ( 30, 1.0 | airfoil | 1, 0.730769230769 ); ( 30, 1.0 | airfoil | 1, 0.769230769231 ); ( 30, 1.0 | airfoil | 1, 0.807692307692 ); ( 30, 1.0 | airfoil | 1, 0.846153846154 ); ( 30, 1.0 | airfoil | 1, 0.884615384615 ); ( 30, 1.0 | airfoil | 1, 0.923076923077 ); ( 30, 1.0 | airfoil | 1, 0.961538461538 )
diff --git a/TestCases/optimization_euler/pitching_oneram6/pitching_ONERAM6.cfg b/TestCases/optimization_euler/pitching_oneram6/pitching_ONERAM6.cfg
index 0fb6e934aea..ea1a5ae6944 100644
--- a/TestCases/optimization_euler/pitching_oneram6/pitching_ONERAM6.cfg
+++ b/TestCases/optimization_euler/pitching_oneram6/pitching_ONERAM6.cfg
@@ -5,384 +5,152 @@
 % Author: Thomas D. Economon	      	      	              	       	       %
 % Institution: Stanford University				                               %
 % Date: 09.07.2011                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8395
-%
-% Angle of attack (degrees)
 AOA= 3.06
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only for Euler equations)
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER,
-%                      DUAL_TIME_STEPPING-2ND_ORDER, HARMONIC_BALANCE)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-%
-% Time Step for dual time stepping simulations (s)
 TIME_STEP= 0.002161633860454094
 % 25 steps per period: 0.002161633860454094
-%
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 0.541
 % 10 periods: 0.5404084651135235
-%
-% Number of internal iterations (dual time method)
 INNER_ITER= 250
-%
-% Direct iteration number at which to begin unsteady adjoint
 UNST_ADJOINT_ITER= 251
 
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Dynamic mesh simulation (NO, YES)
 GRID_MOVEMENT= YES
-%
-% Type of dynamic mesh (NONE, RIGID_MOTION, DEFORMING, ROTATING_FRAME,
-%                       MOVING_WALL, AEROELASTIC, EXTERNAL)
 GRID_MOVEMENT_KIND= RIGID_MOTION
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.8395
-%
-% Coordinates of the motion origin
 MOTION_ORIGIN_X= 0.201475
 MOTION_ORIGIN_Y= 0.0
 MOTION_ORIGIN_Z= 0.0
-%
-% Pitching angular freq. (rad/s) about x, y, & z axes
 PITCHING_OMEGA_X= 0.0
 PITCHING_OMEGA_Y= 116.26733689
 PITCHING_OMEGA_Z= 0.0
-%
-% Pitching amplitude (degrees) about x, y, & z axes
 PITCHING_AMPL_X= 0.0
 PITCHING_AMPL_Y= 2.5
 PITCHING_AMPL_Z= 0.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.2015
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 0.64607
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 implies no marker)
 MARKER_EULER= ( UPPER_SIDE, LOWER_SIDE, TIP )
-%
-% Marker of the far field (0 implies no marker)
 MARKER_FAR= ( XNORMAL_FACES, ZNORMAL_FACES, YNORMAL_FACE )
-%
-% Marker of symmetry boundary (0 implies no marker)
 MARKER_SYM= ( SYMMETRY_FACE )
-%
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( UPPER_SIDE, LOWER_SIDE, TIP )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( UPPER_SIDE, LOWER_SIDE, TIP )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
-% Numerical method for computation of spatial gradients: (GREEN_GAUSS, 
-%                                                WIEGHTED_LEAST_SQUARES)
-NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 CFL_NUMBER= 8.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 99999
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.9
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.9
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.25
-%
-% Limit value for the adjoint variable
 LIMIT_ADJFLOW= 1E6
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= YES
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
 %
-% Marker(s) of the surface where geometrical based function will be evaluated
 GEO_MARKER= ( UPPER_SIDE, LOWER_SIDE, TIP )
-%
-% Description of the geometry to be analyzed (AIRFOIL, WING, FUSELAGE)
 GEO_DESCRIPTION= WING
-%
-% Coordinate of the stations to be analyzed
 GEO_LOCATION_STATIONS= (0.0, 0.2, 0.4, 0.6, 0.8)
-%
-% Geometrical bounds (Y coordinate) for the wing geometry analysis or
-% fuselage evaluation (X coordinate).
 GEO_BOUNDS= (1.5, 3.5)
-%
-% Plot loads and Cp distributions on each airfoil section
 GEO_PLOT_STATIONS= NO
-%
-% Geometrical evaluation mode (FUNCTION, GRADIENT)
 GEO_MODE= FUNCTION
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------&
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_ONERAM6_inv.su2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
-% Mesh input file format (SU2)
 MESH_FORMAT= SU2
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution frequency
 OUTPUT_WRT_FREQ= 1
-%
-%
+
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (FFD_SETTING, FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC,
-%                      NACA_4DIGITS, DISPLACEMENT, ROTATION, FFD_CONTROL_POINT, 
-%                      FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, FFD_ROTATION,
-%                      FFD_CAMBER, FFD_THICKNESS, SURFACE_FILE)
 DV_KIND= FFD_SETTING 
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( UPPER_SIDE, LOWER_SIDE, TIP )
-%
-% Parameters of the shape deformation 
-% 	- FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% 	- FFD_DIHEDRAL_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% 	- FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% 	- FFD_VOLUME ( FFD_BoxTag, i_Ind, j_Ind )
 DV_PARAM= ( 0, 1, 0, 0, 0.0, 0.0, 1.0 )
-%
-% New value of the shape deformation
 DV_VALUE= 0.0
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-
-% Optimization objective function with optional scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.1
-
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= (LIFT > 0.2864) * 0.1; (STATION1_THICKNESS > 0.0570) * 0.1; (STATION2_THICKNESS > 0.0513) * 0.1; (STATION3_THICKNESS > 0.0457) * 0.1; (STATION4_THICKNESS > 0.0399) * 0.1; (STATION5_THICKNESS > 0.0343) * 0.1
-
-% List of design variables (Design variables are separated by semicolons)
 DEFINITION_DV= ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 0, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 1, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 2, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 3, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 4, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 0, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 1, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 2, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 3, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 4, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 0, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 1, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 2, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 3, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 4, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 0, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 1, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 2, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 3, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 4, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 0, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 1, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 2, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 3, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 4, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 0, 0, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 1, 0, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 2, 0, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 3, 0, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 4, 0, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 0, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 1, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 2, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 3, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 4, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 0, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 1, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 2, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 3, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 4, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 0, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 1, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 2, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 3, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 4, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 0, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 1, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 2, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 3, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | 0, 4, 4, 0, 0.0, 0.0, 1.0 )
diff --git a/TestCases/optimization_euler/rotating_naca0012/rotating_NACA0012.cfg b/TestCases/optimization_euler/rotating_naca0012/rotating_NACA0012.cfg
index 38f6db41c40..61766480053 100644
--- a/TestCases/optimization_euler/rotating_naca0012/rotating_NACA0012.cfg
+++ b/TestCases/optimization_euler/rotating_naca0012/rotating_NACA0012.cfg
@@ -5,343 +5,137 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.03.06                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.0
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Dynamic mesh simulation (NO, YES)
 GRID_MOVEMENT= YES
-%
-% Type of dynamic mesh (NONE, RIGID_MOTION, DEFORMING, ROTATING_FRAME,
-%                       MOVING_WALL, AEROELASTIC, EXTERNAL)
 GRID_MOVEMENT_KIND= ROTATING_FRAME
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.79578199852934983
-%
-% Coordinates of the motion origin
 MOTION_ORIGIN_X= 0.5
 MOTION_ORIGIN_Y= -32.0
 MOTION_ORIGIN_Z= 0.0
-%
-% Angular velocity vector (rad/s) about the motion origin
 ROTATION_RATE_X = 0.0
 ROTATION_RATE_Y = 0.0
 ROTATION_RATE_Z = 8.25
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 6.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.95
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.95
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE, AUSM, HLLC)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Slope limiter (VENKATAKRISHNAN)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Slope limiter (VENKATAKRISHNAN, SHARP_EDGES)
 SLOPE_LIMITER_ADJFLOW= SHARP_EDGES
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.8
-%
-% Limit value for the adjoint variable
 LIMIT_ADJFLOW= 1E6
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
-%
-% Sensitivity smoothing (NONE, SOBOLEV, BIGRID)
 SENS_SMOOTHING= NONE
-%
-% Adjoint frozen viscosity (NO, YES)
 FROZEN_VISC_CONT= YES
 
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
 %
-% Geometrical evaluation mode (FUNCTION, GRADIENT)
 GEO_MODE= FUNCTION
-%
-% Marker(s) of the surface where geometrical based func. will be evaluated
 GEO_MARKER= ( airfoil )
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION, 
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION)
-DV_KIND= HICKS_HENNE
 %
-% Marker of the surface in which we are going apply the shape deformation
+DV_KIND= HICKS_HENNE
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( 1st digit, 2nd and 3rd digit )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= ( 1, 0.5 )
-%
-% Old value of the deformation for incremental deformations
 DV_VALUE= 0.05
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -13
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA0012_rot.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-% Optimization objective function with optional scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.001
-
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
-OPT_CONSTRAINT= ( AIRFOIL_THICKNESS > 0.12 ) * 0.001
-%
-% List of design variables (Design variables are separated by semicolons)
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.961538461538 ); ( 30, 1.0 | airfoil | 0, 0.923076923077 ); ( 30, 1.0 | airfoil | 0, 0.884615384615 ); ( 30, 1.0 | airfoil | 0, 0.846153846154 ); ( 30, 1.0 | airfoil | 0, 0.807692307692 ); ( 30, 1.0 | airfoil | 0, 0.769230769231 ); ( 30, 1.0 | airfoil | 0, 0.730769230769 ); ( 30, 1.0 | airfoil | 0, 0.692307692308 ); ( 30, 1.0 | airfoil | 0, 0.653846153846 ); ( 30, 1.0 | airfoil | 0, 0.615384615385 ); ( 30, 1.0 | airfoil | 0, 0.576923076923 ); ( 30, 1.0 | airfoil | 0, 0.538461538462 ); ( 30, 1.0 | airfoil | 0, 0.5 ); ( 30, 1.0 | airfoil | 0, 0.461538461538 ); ( 30, 1.0 | airfoil | 0, 0.423076923077 ); ( 30, 1.0 | airfoil | 0, 0.384615384615 ); ( 30, 1.0 | airfoil | 0, 0.346153846154 ); ( 30, 1.0 | airfoil | 0, 0.307692307692 ); ( 30, 1.0 | airfoil | 0, 0.269230769231 ); ( 30, 1.0 | airfoil | 0, 0.230769230769 ); ( 30, 1.0 | airfoil | 0, 0.192307692308 ); ( 30, 1.0 | airfoil | 0, 0.153846153846 ); ( 30, 1.0 | airfoil | 0, 0.115384615385 ); ( 30, 1.0 | airfoil | 0, 0.0769230769231 ); ( 30, 1.0 | airfoil | 0, 0.0384615384615 ); ( 30, 1.0 | airfoil | 1, 0.0384615384615 ); ( 30, 1.0 | airfoil | 1, 0.0769230769231 ); ( 30, 1.0 | airfoil | 1, 0.115384615385 ); ( 30, 1.0 | airfoil | 1, 0.153846153846 ); ( 30, 1.0 | airfoil | 1, 0.192307692308 ); ( 30, 1.0 | airfoil | 1, 0.230769230769 ); ( 30, 1.0 | airfoil | 1, 0.269230769231 ); ( 30, 1.0 | airfoil | 1, 0.307692307692 ); ( 30, 1.0 | airfoil | 1, 0.346153846154 ); ( 30, 1.0 | airfoil | 1, 0.384615384615 ); ( 30, 1.0 | airfoil | 1, 0.423076923077 ); ( 30, 1.0 | airfoil | 1, 0.461538461538 ); ( 30, 1.0 | airfoil | 1, 0.5 ); ( 30, 1.0 | airfoil | 1, 0.538461538462 ); ( 30, 1.0 | airfoil | 1, 0.576923076923 ); ( 30, 1.0 | airfoil | 1, 0.615384615385 ); ( 30, 1.0 | airfoil | 1, 0.653846153846 ); ( 30, 1.0 | airfoil | 1, 0.692307692308 ); ( 30, 1.0 | airfoil | 1, 0.730769230769 ); ( 30, 1.0 | airfoil | 1, 0.769230769231 ); ( 30, 1.0 | airfoil | 1, 0.807692307692 ); ( 30, 1.0 | airfoil | 1, 0.846153846154 ); ( 30, 1.0 | airfoil | 1, 0.884615384615 ); ( 30, 1.0 | airfoil | 1, 0.923076923077 ); ( 30, 1.0 | airfoil | 1, 0.961538461538 )
diff --git a/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg b/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg
index 9dd9a5cc73c..40ecbf09e0d 100644
--- a/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg
+++ b/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg
@@ -5,345 +5,135 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 3.2.7 "eagle"                                                   %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees)
 AOA= 2.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (NONE = no marker)
 MARKER_FAR= ( farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( airfoil )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( airfoil )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( airfoil )
 
 
 % --------------------- INVERSE DESIGN SIMULATION -----------------------------%
 %
-% Evaluate an inverse design problem using Cp (NO, YES)
 INV_DESIGN_CP= YES
-%
-% Evaluate an inverse design problem using heat flux (NO, YES)
 INV_DESIGN_HEATFLUX= NO
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX)
 OBJECTIVE_FUNCTION= INVERSE_DESIGN_PRESSURE
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.0
-%
-% Number of total iterations
 ITER= 250
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 1.0
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 1.0
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.5
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (FFD_SETTING, FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC,
-%                      NACA_4DIGITS, DISPLACEMENT, ROTATION, FFD_CONTROL_POINT, 
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CAMBER, FFD_THICKNESS, SURFACE_FILE, AIRFOIL)
 DV_KIND= HICKS_HENNE 
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation
-% - FFD_CONTROL_POINT_2D ( FFD_Box_ID, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_Box_ID, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_Box_ID, i_Ind )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - FOURIER ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), index, cos(0)/sin(1) )
-% - SPHERICAL ( ControlPoint_Index, Theta_Disp, R_Disp )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - PARABOLIC ( Center, Thickness )
-% - DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - OBSTACLE ( Center, Bump size )
 DV_PARAM= ( 1, 0.5 )
-%
-% Value of the shape deformation
 DV_VALUE= 0.01
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= mesh_NACA0012_inv_FFD.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= mesh_NACA0012_inv_FFD.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= INVERSE_DESIGN_PRESSURE * 0.001
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= NONE
-%
-% Maximum number of iterations
 OPT_ITERATIONS= 100
-%
-% Requested accuracy
 OPT_ACCURACY= 1E-6
-%
-% Upper bound for each design variable
 OPT_BOUND_UPPER= 0.1
-%
-% Lower bound for each design variable
 OPT_BOUND_LOWER= -0.1
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 19, 1.0 | airfoil | BOX, 0, 0, 0.0, 1.0 ); ( 19, 1.0 | airfoil | BOX, 1, 0, 0.0, 1.0 ); ( 19, 1.0 | airfoil | BOX, 2, 0, 0.0, 1.0 ); ( 19, 1.0 | airfoil | BOX, 3, 0, 0.0, 1.0 ); ( 19, 1.0 | airfoil | BOX, 4, 0, 0.0, 1.0 ); ( 19, 1.0 | airfoil | BOX, 5, 0, 0.0, 1.0 ); ( 19, 1.0 | airfoil | BOX, 6, 0, 0.0, 1.0 ); ( 19, 1.0 | airfoil | BOX, 7, 0, 0.0, 1.0 ); ( 19, 1.0 | airfoil | BOX, 8, 0, 0.0, 1.0 ); ( 19, 1.0 | airfoil | BOX, 9, 0, 0.0, 1.0 ); ( 19, 1.0 | airfoil | BOX, 10, 0, 0.0, 1.0 ); ( 19, 1.0 | airfoil | BOX, 0, 1, 0.0, 1.0 ); ( 19, 1.0 | airfoil | BOX, 1, 1, 0.0, 1.0 ); ( 19, 1.0 | airfoil | BOX, 2, 1, 0.0, 1.0 ); ( 19, 1.0 | airfoil | BOX, 3, 1, 0.0, 1.0 ); ( 19, 1.0 | airfoil | BOX, 4, 1, 0.0, 1.0 ); ( 19, 1.0 | airfoil | BOX, 5, 1, 0.0, 1.0 ); ( 19, 1.0 | airfoil | BOX, 6, 1, 0.0, 1.0 ); ( 19, 1.0 | airfoil | BOX, 7, 1, 0.0, 1.0 ); ( 19, 1.0 | airfoil | BOX, 8, 1, 0.0, 1.0 ); ( 19, 1.0 | airfoil | BOX, 9, 1, 0.0, 1.0 ); ( 19, 1.0 | airfoil | BOX, 10, 1, 0.0, 1.0 )
diff --git a/TestCases/optimization_euler/steady_naca0012/inv_NACA0012_adv.cfg b/TestCases/optimization_euler/steady_naca0012/inv_NACA0012_adv.cfg
index dc87899a9db..5772c607061 100644
--- a/TestCases/optimization_euler/steady_naca0012/inv_NACA0012_adv.cfg
+++ b/TestCases/optimization_euler/steady_naca0012/inv_NACA0012_adv.cfg
@@ -5,362 +5,143 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.09.29                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION) 
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AOA= 1.25
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 250
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (LU_SGS,
-%                                              SYM_GAUSS_SEIDEL, BCGSTAB, GMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (NONE, JACOBI, LINELET, LUSGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 1.0
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 1.0
 
-% --------------------- FLOW NUMERICAL METHOD DEFINITION ----------------------%
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                              ROE-2ND_ORDER)
-CONV_NUM_METHOD_FLOW= JST
+% --------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Slope limiter (VENKATAKRISHNAN)
+CONV_NUM_METHOD_FLOW= JST
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
-% ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE)
-OBJECTIVE_FUNCTION= DRAG
+% ------------------ ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                              ROE-2ND_ORDER)
+OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Slope limiter (VENKATAKRISHNAN, SHARP_EDGES)
 SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.8
-%
-% Limit value for the adjoint variable
 LIMIT_ADJFLOW= 1E6
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
-%
-% Sensitivity smoothing (NONE, SOBOLEV, BIGRID)
 SENS_SMOOTHING= NONE
 
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
 %
-% Marker(s) of the surface where geometrical based function will be evaluated
 GEO_MARKER= ( airfoil )
-%
-% Description of the geometry to be analyzed (AIRFOIL, WING, FUSELAGE)
 GEO_DESCRIPTION= AIRFOIL
-%
-% Geometrical evaluation mode (FUNCTION, GRADIENT)
 GEO_MODE= FUNCTION
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION, 
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION)
 DV_KIND= HICKS_HENNE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( 1st digit, 2nd and 3rd digit )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= ( 1, 0.5 )
-%
-% Value of the shape deformation deformation
 DV_VALUE= 1.0
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -9
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA0012_inv.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 50
-%
-%
-% History output
 HISTORY_OUTPUT= (ITER, RMS_RES, AERO_COEFF)
-%
 OUTPUT_FILES= (RESTART_ASCII, PARAVIEW, SURFACE_CSV)
-%
+
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.001
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= ( LIFT > 0.327 ) * 0.001; ( MOMENT_Z > 0.0 ) * 0.001; ( AIRFOIL_THICKNESS > 0.12 ) * 0.001
-%
-% Maximum number of optimizer iterations
 OPT_ITERATIONS= 100
-%
-% Requested accuracy
 OPT_ACCURACY= 1E-6
-%
-% Upper bound for each design variable
 OPT_BOUND_UPPER= 0.1
-%
-% Lower bound for each design variable
 OPT_BOUND_LOWER= -0.1
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 ); ( 30, 1.0 | airfoil | 0, 0.20 ); ( 30, 1.0 | airfoil | 0, 0.25 ); ( 30, 1.0 | airfoil | 0, 0.30 ); ( 30, 1.0 | airfoil | 0, 0.35 ); ( 30, 1.0 | airfoil | 0, 0.40 ); ( 30, 1.0 | airfoil | 0, 0.45 ); ( 30, 1.0 | airfoil | 0, 0.50 ); ( 30, 1.0 | airfoil | 0, 0.55 ); ( 30, 1.0 | airfoil | 0, 0.60 ); ( 30, 1.0 | airfoil | 0, 0.65 ); ( 30, 1.0 | airfoil | 0, 0.70 ); ( 30, 1.0 | airfoil | 0, 0.75 ); ( 30, 1.0 | airfoil | 0, 0.80 ); ( 30, 1.0 | airfoil | 0, 0.85 ); ( 30, 1.0 | airfoil | 0, 0.90 ); ( 30, 1.0 | airfoil | 0, 0.95 ); ( 30, 1.0 | airfoil | 1, 0.05 ); ( 30, 1.0 | airfoil | 1, 0.10 ); ( 30, 1.0 | airfoil | 1, 0.15 ); ( 30, 1.0 | airfoil | 1, 0.20 ); ( 30, 1.0 | airfoil | 1, 0.25 ); ( 30, 1.0 | airfoil | 1, 0.30 ); ( 30, 1.0 | airfoil | 1, 0.35 ); ( 30, 1.0 | airfoil | 1, 0.40 ); ( 30, 1.0 | airfoil | 1, 0.45 ); ( 30, 1.0 | airfoil | 1, 0.50 ); ( 30, 1.0 | airfoil | 1, 0.55 ); ( 30, 1.0 | airfoil | 1, 0.60 ); ( 30, 1.0 | airfoil | 1, 0.65 ); ( 30, 1.0 | airfoil | 1, 0.70 ); ( 30, 1.0 | airfoil | 1, 0.75 ); ( 30, 1.0 | airfoil | 1, 0.80 ); ( 30, 1.0 | airfoil | 1, 0.85 ); ( 30, 1.0 | airfoil | 1, 0.90 ); ( 30, 1.0 | airfoil | 1, 0.95 )
diff --git a/TestCases/optimization_euler/steady_naca0012/inv_NACA0012_basic.cfg b/TestCases/optimization_euler/steady_naca0012/inv_NACA0012_basic.cfg
index 1d419d02425..94742fdab2e 100644
--- a/TestCases/optimization_euler/steady_naca0012/inv_NACA0012_basic.cfg
+++ b/TestCases/optimization_euler/steady_naca0012/inv_NACA0012_basic.cfg
@@ -5,345 +5,135 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.09.29                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION) 
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
-%RESTART_SOL= YES
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AOA= 1.25
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 1000
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (LU_SGS,
-%                                              SYM_GAUSS_SEIDEL, BCGSTAB, GMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (NONE, JACOBI, LINELET, LUSGS)
 LINEAR_SOLVER_PREC= ILU
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 1.0
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 1.0
 
 % --------------------- FLOW NUMERICAL METHOD DEFINITION ----------------------%
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                              ROE-2ND_ORDER)
-CONV_NUM_METHOD_FLOW= JST
 %
-% Slope limiter (VENKATAKRISHNAN)
+CONV_NUM_METHOD_FLOW= JST
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE)
-OBJECTIVE_FUNCTION= DRAG
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                              ROE-2ND_ORDER)
+OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Slope limiter (VENKATAKRISHNAN, SHARP_EDGES)
 SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.8
-%
-% Limit value for the adjoint variable
 LIMIT_ADJFLOW= 1E6
 
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
 %
-% Marker(s) of the surface where geometrical based function will be evaluated
 GEO_MARKER= ( airfoil )
-%
-% Description of the geometry to be analyzed (AIRFOIL, WING, FUSELAGE)
 GEO_DESCRIPTION= AIRFOIL
-%
-% Geometrical evaluation mode (FUNCTION, GRADIENT)
 GEO_MODE= FUNCTION
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION, 
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION)
 DV_KIND= HICKS_HENNE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( 1st digit, 2nd and 3rd digit )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= ( 1, 0.5 )
-%
-% Value of the shape deformation deformation
 DV_VALUE= 1.0
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -13
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA0012_inv.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.001
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= NONE
-%
-% Maximum number of optimizer iterations
 OPT_ITERATIONS= 100
-%
-% Requested accuracy
 OPT_ACCURACY= 1E-6
-%
-% Upper bound for each design variable
 OPT_BOUND_UPPER= 0.1
-%
-% Lower bound for each design variable
 OPT_BOUND_LOWER= -0.1
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 ); ( 30, 1.0 | airfoil | 0, 0.20 ); ( 30, 1.0 | airfoil | 0, 0.25 ); ( 30, 1.0 | airfoil | 0, 0.30 ); ( 30, 1.0 | airfoil | 0, 0.35 ); ( 30, 1.0 | airfoil | 0, 0.40 ); ( 30, 1.0 | airfoil | 0, 0.45 ); ( 30, 1.0 | airfoil | 0, 0.50 ); ( 30, 1.0 | airfoil | 0, 0.55 ); ( 30, 1.0 | airfoil | 0, 0.60 ); ( 30, 1.0 | airfoil | 0, 0.65 ); ( 30, 1.0 | airfoil | 0, 0.70 ); ( 30, 1.0 | airfoil | 0, 0.75 ); ( 30, 1.0 | airfoil | 0, 0.80 ); ( 30, 1.0 | airfoil | 0, 0.85 ); ( 30, 1.0 | airfoil | 0, 0.90 ); ( 30, 1.0 | airfoil | 0, 0.95 ); ( 30, 1.0 | airfoil | 1, 0.05 ); ( 30, 1.0 | airfoil | 1, 0.10 ); ( 30, 1.0 | airfoil | 1, 0.15 ); ( 30, 1.0 | airfoil | 1, 0.20 ); ( 30, 1.0 | airfoil | 1, 0.25 ); ( 30, 1.0 | airfoil | 1, 0.30 ); ( 30, 1.0 | airfoil | 1, 0.35 ); ( 30, 1.0 | airfoil | 1, 0.40 ); ( 30, 1.0 | airfoil | 1, 0.45 ); ( 30, 1.0 | airfoil | 1, 0.50 ); ( 30, 1.0 | airfoil | 1, 0.55 ); ( 30, 1.0 | airfoil | 1, 0.60 ); ( 30, 1.0 | airfoil | 1, 0.65 ); ( 30, 1.0 | airfoil | 1, 0.70 ); ( 30, 1.0 | airfoil | 1, 0.75 ); ( 30, 1.0 | airfoil | 1, 0.80 ); ( 30, 1.0 | airfoil | 1, 0.85 ); ( 30, 1.0 | airfoil | 1, 0.90 ); ( 30, 1.0 | airfoil | 1, 0.95 )
diff --git a/TestCases/optimization_euler/steady_oneram6/inv_ONERAM6_adv.cfg b/TestCases/optimization_euler/steady_oneram6/inv_ONERAM6_adv.cfg
index 261956c842e..e5c307044e0 100644
--- a/TestCases/optimization_euler/steady_oneram6/inv_ONERAM6_adv.cfg
+++ b/TestCases/optimization_euler/steady_oneram6/inv_ONERAM6_adv.cfg
@@ -5,397 +5,154 @@
 % Author: Francisco Palacios, Heather Kline	               	       	           %
 % Institution: Stanford University	                                           %
 % Date: 01.17.2017                                                             %
-% File Version 7.4.0 "Blackbird"                                                   %
+% File Version 7.5.0 "Blackbird"                                                   %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8395
-%
-% Angle of attack (degrees)
 AOA= 3.06
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only for Euler equations)
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.2015
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 0.64607
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 implies no marker)
 MARKER_EULER= ( UPPER_SIDE, LOWER_SIDE, TIP )
-%
-% Marker of the far field (0 implies no marker)
 MARKER_FAR= ( XNORMAL_FACES, ZNORMAL_FACES, YNORMAL_FACE )
-%
-% Marker of symmetry boundary (0 implies no marker)
 MARKER_SYM= ( SYMMETRY_FACE )
-%
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( UPPER_SIDE, LOWER_SIDE, TIP )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( UPPER_SIDE, LOWER_SIDE, TIP )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= YES
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 0.1, 1.2, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 1000
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= YES
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.95
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.95
 
 % --------------------- FLOW NUMERICAL METHOD DEFINITION ----------------------%
-% Convective numerical method: (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                               ROE-2ND_ORDER)
-CONV_NUM_METHOD_FLOW= JST
 %
-% Slope limiter: (VENKATAKRISHNAN)
+CONV_NUM_METHOD_FLOW= JST
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ----------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method: (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                               ROE-2ND_ORDER)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Slope limiter: (VENKATAKRISHNAN, SHARP_EDGES)
 SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.5
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
 %
-% Marker(s) of the surface where geometrical based function will be evaluated
 GEO_MARKER= ( UPPER_SIDE, LOWER_SIDE, TIP )
-%
-% Description of the geometry to be analyzed (AIRFOIL, WING, FUSELAGE)
 GEO_DESCRIPTION= WING
-%
-% Coordinate of the stations to be analyzed
 GEO_LOCATION_STATIONS= (0.0, 0.2, 0.4, 0.6, 0.8)
-%
-% Geometrical bounds (Y coordinate) for the wing geometry analysis or
-% fuselage evaluation (X coordinate).
 GEO_BOUNDS= (1.5, 3.5)
-%
-% Plot loads and Cp distributions on each airfoil section
 GEO_PLOT_STATIONS= NO
-%
-% Geometrical evaluation mode (FUNCTION, GRADIENT)
 GEO_MODE= FUNCTION
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------&
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -9
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 25
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_ONERAM6_inv_FFD.su2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
-% Mesh input file format (SU2)
 MESH_FORMAT= SU2
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency for physical time steps (dual time)
 OUTPUT_WRT_FREQ= 1
-%
 OUTPUT_FILES=(RESTART, PARAVIEW, SURFACE_CSV)
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-10
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 500
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (WING,-0.0403, 0, -0.04836,0.8463,0, -0.04836,1.209,1.2896, -0.04836,0.6851,1.2896, -0.04836,-0.0403,0, 0.04836,0.8463,0, 0.04836,1.209,1.2896, 0.04836,0.6851,1.2896, 0.04836)
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= (10, 8, 1)
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= 2ND_DERIVATIVE
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (FFD_SETTING, FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, COSINE_BUMP, PARABOLIC,
-%                      NACA_4DIGITS, DISPLACEMENT, ROTATION, FFD_CONTROL_POINT, 
-%                      FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, FFD_ROTATION,
-%                      FFD_CAMBER, FFD_THICKNESS, FFD_CONTROL_SURFACE, SURFACE_FILE, AIRFOIL)
 DV_KIND= FFD_CONTROL_POINT
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( UPPER_SIDE, LOWER_SIDE, TIP )
-%
-% Parameters of the shape deformation 
-% 	- FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% 	- FFD_DIHEDRAL_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% 	- FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% 	- FFD_VOLUME ( FFD_BoxTag, i_Ind, j_Ind )
 DV_PARAM= ( WING, 1, 0, 0, 0.0, 0.0, 1.0 )
-%
-% New value of the shape deformation
 DV_VALUE= 0.0
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 800
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= NO
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= WALL_DISTANCE
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.1
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= (LIFT > 0.2864) * 10.0; (STATION1_THICKNESS > 0.0570) * 0.1; (STATION2_THICKNESS > 0.0513) * 0.1; (STATION3_THICKNESS > 0.0457) * 0.1; (STATION4_THICKNESS > 0.0399) * 0.1; (STATION5_THICKNESS > 0.0343) * 0.1
-%
-% Maximum number of iterations
 OPT_ITERATIONS= 100
-%
-% Requested accuracy
 OPT_ACCURACY= 1E-4
-%
-% Upper bound for each design variable
 OPT_BOUND_UPPER= 0.1
-%
-% Lower bound for each design variable
 OPT_BOUND_LOWER= -0.1
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 8, 1, 0.0, 0.0, 1.0 )
diff --git a/TestCases/optimization_euler/steady_oneram6/inv_ONERAM6_basic.cfg b/TestCases/optimization_euler/steady_oneram6/inv_ONERAM6_basic.cfg
index 0e29f2a0a89..6b9afd7130d 100644
--- a/TestCases/optimization_euler/steady_oneram6/inv_ONERAM6_basic.cfg
+++ b/TestCases/optimization_euler/steady_oneram6/inv_ONERAM6_basic.cfg
@@ -5,396 +5,151 @@
 % Author: Francisco Palacios, Heather Kline    	              	       	       %
 % Institution: Stanford University	                                           %
 % Date: 01.17.2017                                                             %
-% File Version 7.4.0 "Blackbird"                                                   %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8395
-%
-% Angle of attack (degrees)
 AOA= 3.06
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only for Euler equations)
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.2015
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 0.64607
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 implies no marker)
 MARKER_EULER= ( UPPER_SIDE, LOWER_SIDE, TIP )
-%
-% Marker of the far field (0 implies no marker)
 MARKER_FAR= ( XNORMAL_FACES, ZNORMAL_FACES, YNORMAL_FACE )
-%
-% Marker of symmetry boundary (0 implies no marker)
 MARKER_SYM= ( SYMMETRY_FACE )
-%
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( UPPER_SIDE, LOWER_SIDE, TIP )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( UPPER_SIDE, LOWER_SIDE, TIP )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 1000
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 1.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= YES
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.95
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.95
 
 % --------------------- FLOW NUMERICAL METHOD DEFINITION ----------------------%
-% Convective numerical method: (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                               ROE-2ND_ORDER)
-CONV_NUM_METHOD_FLOW= JST
 %
-% Slope limiter: (VENKATAKRISHNAN)
+CONV_NUM_METHOD_FLOW= JST
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ----------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method: (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                               ROE-2ND_ORDER)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Slope limiter: (VENKATAKRISHNAN, SHARP_EDGES)
 SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.5
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
 %
-% Marker(s) of the surface where geometrical based function will be evaluated
 GEO_MARKER= ( UPPER_SIDE, LOWER_SIDE, TIP )
-%
-% Description of the geometry to be analyzed (AIRFOIL, WING, FUSELAGE)
 GEO_DESCRIPTION= WING
-%
-% Coordinate of the stations to be analyzed
 GEO_LOCATION_STATIONS= (0.0, 0.2, 0.4, 0.6, 0.8)
-%
-% Geometrical bounds (Y coordinate) for the wing geometry analysis or
-% fuselage evaluation (X coordinate).
 GEO_BOUNDS= (1.5, 3.5)
-%
-% Plot loads and Cp distributions on each airfoil section
 GEO_PLOT_STATIONS= NO
-%
-% Geometrical evaluation mode (FUNCTION, GRADIENT)
 GEO_MODE= FUNCTION
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------&
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -9
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 25
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_ONERAM6_inv_FFD.su2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
-% Mesh input file format (SU2)
 MESH_FORMAT= SU2
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency for physical time steps (dual time)
 OUTPUT_WRT_FREQ= 1
-%
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
 %
-% Tolerance of the Free-Form Deformation point inversion
 FFD_TOLERANCE= 1E-10
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
 FFD_ITERATIONS= 500
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
-%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
 FFD_DEFINITION= (WING,-0.0403, 0, -0.04836,0.8463,0, -0.04836,1.209,1.2896, -0.04836,0.6851,1.2896, -0.04836,-0.0403,0, 0.04836,0.8463,0, 0.04836,1.209,1.2896, 0.04836,0.6851,1.2896, 0.04836)
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
 FFD_DEGREE= (10, 8, 1)
-%
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
 FFD_CONTINUITY= 2ND_DERIVATIVE
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (FFD_SETTING, FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC,
-%                      NACA_4DIGITS, DISPLACEMENT, ROTATION, FFD_CONTROL_POINT, 
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CAMBER, FFD_THICKNESS, FFD_CONTROL_SURFACE, SURFACE_FILE, AIRFOIL)
 DV_KIND= FFD_CONTROL_POINT
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( UPPER_SIDE, LOWER_SIDE, TIP )
-%
-% Parameters of the shape deformation 
-% 	- FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% 	- FFD_DIHEDRAL_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_TWIST_ANGLE ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_ROTATION ( FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% 	- FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% 	- FFD_VOLUME ( FFD_BoxTag, i_Ind, j_Ind )
 DV_PARAM= ( WING, 1, 0, 0, 0.0, 0.0, 1.0 )
-%
-% New value of the shape deformation
 DV_VALUE= 0.0
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 800
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= NO
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.1
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= NONE
-%
-% Maximum number of iterations
 OPT_ITERATIONS= 100
-%
-% Requested accuracy
 OPT_ACCURACY= 1E-10
-%
-% Upper bound for each design variable
 OPT_BOUND_UPPER= 0.3
-%
-% Lower bound for each design variable
 OPT_BOUND_LOWER= -0.3
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 5, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 6, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 7, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 8, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 5, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 6, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 7, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 0, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 1, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 2, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 3, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 4, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 5, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 6, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 7, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 8, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 9, 8, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | UPPER_SIDE, LOWER_SIDE, TIP | WING, 10, 8, 1, 0.0, 0.0, 1.0 )
diff --git a/TestCases/optimization_rans/naca0012/naca0012.cfg b/TestCases/optimization_rans/naca0012/naca0012.cfg
index 97b5c686ecf..6499f73ec75 100644
--- a/TestCases/optimization_rans/naca0012/naca0012.cfg
+++ b/TestCases/optimization_rans/naca0012/naca0012.cfg
@@ -5,7 +5,7 @@
 % Author: Steffen Schotthöfer                                                  %
 % Institution: TU Kaiserslautern                                               %
 % Date: Mar 16, 2017                                                           %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -15,194 +15,119 @@
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES, NS_PLASMA)                    
 SOLVER= RANS
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DISCRETE_ADJOINT
-% Objective function
 OBJECTIVE_FUNCTION=DRAG
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-% Restart iteration
 RESTART_ITER = 10
 %
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Time Domain
 TIME_DOMAIN = YES
-% Unsteady simulation
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-% Time Step for dual time stepping simulations (s)
 TIME_STEP= 5e-4
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 105000
-%Maximum Number of physical time steps used for primal and ajoint run.
 TIME_ITER= 13
-% Number of internal iterations (dual time method)
 INNER_ITER= 2
-%Number of iterations to average the objective 
 ITER_AVERAGE_OBJ =  3      
-%Iteration number to begin the reverse time integration in the direct solver for the unsteady adjoint.
 UNST_ADJOINT_ITER = 13
-% Start iteration for windowing
 WINDOW_START_ITER = 10 
-% Window used for reverse sweep. Options (SQUARE, HANN, HANN_SQUARE, BUMP)
 WINDOW_FUNCTION = SQUARE
 %
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.3
-% Angle of attack (degrees, only for compressible flows)
 AOA= 17.0
-% De-Dimensionalization
 REF_DIMENSIONALIZATION = DIMENSIONAL
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 293.0
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 1e+6
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 %
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 %
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker
 MARKER_HEATFLUX= ( AIRFOIL, 0.0)
-% Farfield boundary marker
 MARKER_FAR= ( FARFIELD)
-% Internal boundary marker(s) e.g. no boundary condition 
 MARKER_INTERNAL= ( FWH1 )
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= (  AIRFOIL )
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= (AIRFOIL)
 %
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 20.0
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 %
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method 
 CONV_NUM_METHOD_FLOW= JST
-% 1st, 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= (  0.5, 0.01 )
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-% Muscl flow for turbulent simulation
 MUSCL_TURB= NO
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 %
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Field to apply Cauchy Criterion to
 CONV_FIELD= REL_RMS_DENSITY
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -9
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 10
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-5
 %
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Output settings
 HISTORY_WRT_FREQ_INNER=0
 SCREEN_WRT_FREQ_INNER =1
 SCREEN_OUTPUT=(INNER_ITER, TIME_ITER, RMS_ADJ_DENSITY, RMS_DENSITY, , REL_RMS_DENSITY,REL_RMS_ADJ_DENSITY, DRAG, TAVG_DRAG)
 HISTORY_OUTPUT=(ITER, RMS_RES, AERO_COEFF, TAVG_AERO_COEFF, ADJ_AERO_COEFF)
-%
-% Mesh input file
 MESH_FILENAME= naca0012_FFD.su2
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= restart_adj.dat
 TABULAR_FORMAT= CSV
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= 0_history
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1
 %
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation 
 DV_KIND= FFD_CONTROL_POINT_2D
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( AIRFOIL )
-% Parameters of the shape deformation
 DV_PARAM= ( AIRFOIL_BOX, 0.0, 0.0, 1.0, 0.0)
-% Value of the shape deformation
 DV_VALUE= 0.01
-% Surface deformation input filename (SURFACE_FILE DV only)
 DV_FILENAME= mesh_motion.dat
 %
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 1000
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-% Factor to multiply smallest cell volume for deform tolerance (0.001 default)
 DEFORM_LINEAR_SOLVER_ERROR =  1E-6
-% Type of element stiffness imposed for FEA mesh deformation
 DEFORM_STIFFNESS_TYPE= WALL_DISTANCE
-% Maximum number of iterations
 OPT_ITERATIONS= 1
-% Optimization objective function with scaling factor
 OPT_OBJECTIVE= DRAG * 1.0
 OPT_GRADIENT_FACTOR= 0.1
 OPT_RELAX_FACTOR= 1
 OPT_BOUND_UPPER= 0.05
 OPT_BOUND_LOWER= -0.05
-% Optimization constraint functions with scaling factors, separated by semicolons
 OPT_CONSTRAINT= ( LIFT > 0.96 ) * 1.0
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 0, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 0, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 0, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 0, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 0, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 0, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 0, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 0, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 0, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 0, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 0, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 1, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 1, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 1, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 1, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 1, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 1, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 1, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 1, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 1, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 1, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 1, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 2, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 2, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 2, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 2, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 2, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 2, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 2, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 2, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 2, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 2, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 2, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 3, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 3, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 3, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 3, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 3, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 3, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 3, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 3, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 3, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 3, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 3, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 4, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 4, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 4, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 4, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 4, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 4, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 4, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 4, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 4, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 4, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 4, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 5, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 5, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 5, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 5, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 5, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 5, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 5, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 5, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 5, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 5, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 5, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 6, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 6, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 6, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 6, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 6, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 6, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 6, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 6, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 6, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 6, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 6, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 7, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 7, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 7, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 7, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 7, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 7, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 7, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 7, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 7, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 7, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 7, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 8, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 8, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 8, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 8, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 8, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 8, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 8, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 8, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 8, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 8, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 8, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 9, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 9, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 9, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 9, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 9, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 9, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 9, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 9, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 9, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 9, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 9, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 10, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 10, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 10, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 10, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 10, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 10, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 10, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 10, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 10, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 10, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 10, 1.0, 0.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 0, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 1, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 2, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 2, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 2, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 2, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 2, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 2, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 2, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 2, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 2, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 2, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 2, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 3, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 3, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 3, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 3, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 3, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 3, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 3, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 3, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 3, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 3, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 3, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 4, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 4, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 4, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 4, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 4, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 4, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 4, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 4, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 4, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 4, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 4, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 5, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 5, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 5, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 5, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 5, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 5, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 5, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 5, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 5, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 5, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 5, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 6, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 6, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 6, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 6, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 6, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 6, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 6, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 6, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 6, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 6, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 6, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 7, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 7, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 7, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 7, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 7, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 7, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 7, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 7, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 7, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 7, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 7, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 8, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 8, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 8, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 8, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 8, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 8, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 8, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 8, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 8, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 8, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 8, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 9, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 9, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 9, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 9, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 9, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 9, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 9, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 9, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 9, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 9, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 9, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 10, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 1, 10, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 2, 10, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 3, 10, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 4, 10, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 5, 10, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 6, 10, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 7, 10, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 8, 10, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 9, 10, 0.0, 1.0 ); ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 10, 10, 0.0, 1.0 )
-%
diff --git a/TestCases/optimization_rans/pitching_naca64a010/turb_NACA64A010.cfg b/TestCases/optimization_rans/pitching_naca64a010/turb_NACA64A010.cfg
index 10b7d1237fa..031f9cd0ce4 100644
--- a/TestCases/optimization_rans/pitching_naca64a010/turb_NACA64A010.cfg
+++ b/TestCases/optimization_rans/pitching_naca64a010/turb_NACA64A010.cfg
@@ -5,392 +5,157 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= NAVIER_STOKES
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-%
-% Time Step for dual time stepping simulations (s)
 TIME_STEP= 0.0023555025613149587
 % 24 steps per period: 0.0024536485013697488
 % 25 steps per period: 0.0023555025613149587
 % 36 steps per period: 0.0016357592286692995
-%
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 0.59
 % 10 periods: 0.5888756403287397
-%
-% Number of internal iterations (dual time method)
 INNER_ITER= 2000
-%
-% Direct iteration number at which to begin unsteady adjoint
 UNST_ADJOINT_ITER= 251
-%
-% Type of mesh motion (NONE, FLUTTER, RIGID_MOTION)
 GRID_MOVEMENT= RIGID_MOTION
-%
-% Mach number (non-dimensional, based on the mesh velocity and freestream vals.)
 MACH_MOTION= 0.796
-%
-% Coordinates of the rigid motion origin
 MOTION_ORIGIN= 0.248 0.0 0.0
-%
-% Pitching angular freq. (rad/s) about x, y, & z axes (RIGID_MOTION only)
 PITCHING_OMEGA= 0.0 0.0 106.69842
-%
-% Pitching amplitude (degrees) about x, y, & z axes (RIGID_MOTION only)
 PITCHING_AMPL= 0.0 0.0 1.01
-%
  
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.796
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 12560000.0
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.248
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Navier-Stokes  boundary marker(s) (0 = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( airfoil )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( airfoil )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
-NUM_METHOD_GRAD= GREEN_GAUSS
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
+NUM_METHOD_GRAD= GREEN_GAUSS
 CFL_NUMBER= 4.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 EXT_ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.7
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.7
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, TORQUE)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.01 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.9
-%
-% Limit value for the adjoint variable
 LIMIT_ADJFLOW= 1E6
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= YES
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Adjoint frozen viscosity (NO, YES)
 FROZEN_VISC_CONT= YES
 
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
 %
-% Marker(s) of the surface where geometrical based function will be evaluated
 GEO_MARKER= ( airfoil )
-%
-% Description of the geometry to be analyzed (AIRFOIL, WING, FUSELAGE)
 GEO_DESCRIPTION= AIRFOIL
-%
-% Geometrical evaluation mode (FUNCTION, GRADIENT)
 GEO_MODE= FUNCTION
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION, 
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION)
-DV_KIND= HICKS_HENNE
 %
-% Marker of the surface in which we are going apply the shape deformation
+DV_KIND= HICKS_HENNE
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( 1st digit, 2nd and 3rd digit )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= ( 1, 0.5 )
-%
-% Old value of the deformation for incremental deformations
 DV_VALUE= 0.05
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 1
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-5
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA64A010_turb.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= restart_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency for physical time steps (dual time)
 OUTPUT_WRT_FREQ= 1
-%
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with optional scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.001
-
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= ( AREA > 0.0661121 ) * 0.001
-% ( AIRFOIL_THICKNESS > 0.1 ) * 0.001
-% ( AREA > 0.0661121 ) * 0.001
-%
-% List of design variables (Design variables are separated by semicolons)
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.961538461538 ); ( 30, 1.0 | airfoil | 0, 0.923076923077 ); ( 30, 1.0 | airfoil | 0, 0.884615384615 ); ( 30, 1.0 | airfoil | 0, 0.846153846154 ); ( 30, 1.0 | airfoil | 0, 0.807692307692 ); ( 30, 1.0 | airfoil | 0, 0.769230769231 ); ( 30, 1.0 | airfoil | 0, 0.730769230769 ); ( 30, 1.0 | airfoil | 0, 0.692307692308 ); ( 30, 1.0 | airfoil | 0, 0.653846153846 ); ( 30, 1.0 | airfoil | 0, 0.615384615385 ); ( 30, 1.0 | airfoil | 0, 0.576923076923 ); ( 30, 1.0 | airfoil | 0, 0.538461538462 ); ( 30, 1.0 | airfoil | 0, 0.5 ); ( 30, 1.0 | airfoil | 0, 0.461538461538 ); ( 30, 1.0 | airfoil | 0, 0.423076923077 ); ( 30, 1.0 | airfoil | 0, 0.384615384615 ); ( 30, 1.0 | airfoil | 0, 0.346153846154 ); ( 30, 1.0 | airfoil | 0, 0.307692307692 ); ( 30, 1.0 | airfoil | 0, 0.269230769231 ); ( 30, 1.0 | airfoil | 0, 0.230769230769 ); ( 30, 1.0 | airfoil | 0, 0.192307692308 ); ( 30, 1.0 | airfoil | 0, 0.153846153846 ); ( 30, 1.0 | airfoil | 0, 0.115384615385 ); ( 30, 1.0 | airfoil | 0, 0.0769230769231 ); ( 30, 1.0 | airfoil | 0, 0.0384615384615 ); ( 30, 1.0 | airfoil | 1, 0.0384615384615 ); ( 30, 1.0 | airfoil | 1, 0.0769230769231 ); ( 30, 1.0 | airfoil | 1, 0.115384615385 ); ( 30, 1.0 | airfoil | 1, 0.153846153846 ); ( 30, 1.0 | airfoil | 1, 0.192307692308 ); ( 30, 1.0 | airfoil | 1, 0.230769230769 ); ( 30, 1.0 | airfoil | 1, 0.269230769231 ); ( 30, 1.0 | airfoil | 1, 0.307692307692 ); ( 30, 1.0 | airfoil | 1, 0.346153846154 ); ( 30, 1.0 | airfoil | 1, 0.384615384615 ); ( 30, 1.0 | airfoil | 1, 0.423076923077 ); ( 30, 1.0 | airfoil | 1, 0.461538461538 ); ( 30, 1.0 | airfoil | 1, 0.5 ); ( 30, 1.0 | airfoil | 1, 0.538461538462 ); ( 30, 1.0 | airfoil | 1, 0.576923076923 ); ( 30, 1.0 | airfoil | 1, 0.615384615385 ); ( 30, 1.0 | airfoil | 1, 0.653846153846 ); ( 30, 1.0 | airfoil | 1, 0.692307692308 ); ( 30, 1.0 | airfoil | 1, 0.730769230769 ); ( 30, 1.0 | airfoil | 1, 0.769230769231 ); ( 30, 1.0 | airfoil | 1, 0.807692307692 ); ( 30, 1.0 | airfoil | 1, 0.846153846154 ); ( 30, 1.0 | airfoil | 1, 0.884615384615 ); ( 30, 1.0 | airfoil | 1, 0.923076923077 ); ( 30, 1.0 | airfoil | 1, 0.961538461538 )
diff --git a/TestCases/optimization_rans/pitching_oneram6/turb_ONERAM6.cfg b/TestCases/optimization_rans/pitching_oneram6/turb_ONERAM6.cfg
index f217b100ba6..748adfcd216 100644
--- a/TestCases/optimization_rans/pitching_oneram6/turb_ONERAM6.cfg
+++ b/TestCases/optimization_rans/pitching_oneram6/turb_ONERAM6.cfg
@@ -5,412 +5,159 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)             
 SOLVER= NAVIER_STOKES
-%
-% Specify turbulence model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8395
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 3.06
-%
-% Side-slip angle (degrees, only for compressible flows)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 11.72E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 0.64607
 
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER,
-%                      DUAL_TIME_STEPPING-2ND_ORDER, HARMONIC_BALANCE)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-%
-% Time Step for dual time stepping simulations (s)
 TIME_STEP= 0.002161633860454094
 % 25 steps per period: 0.002161633860454094
-%
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 0.379
 % 10 periods: 0.5404084651135235
 % 7 periods: 0.37828592557946644
-%
-% Number of internal iterations (dual time method)
 INNER_ITER= 350
-%
-% Direct iteration number at which to begin unsteady adjoint
 UNST_ADJOINT_ITER= 176
 
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
-% Type of dynamic mesh (NONE, RIGID_MOTION, DEFORMING, ROTATING_FRAME,
-%                       MOVING_WALL, AEROELASTIC, EXTERNAL)
-GRID_MOVEMENT= RIGID_MOTION
 %
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
+GRID_MOVEMENT= RIGID_MOTION
 MACH_MOTION= 0.8395
-%
-% Coordinates of the motion origin
 MOTION_ORIGIN= 0.201475 0.0 0.0
-%
-% Pitching angular freq. (rad/s) about x, y, & z axes
 PITCHING_OMEGA= 0.0 116.26733689 0.0
-%
-% Pitching amplitude (degrees) about x, y, & z axes
 PITCHING_AMPL= 0.0 2.5 0.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 0.64607
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( wing, 0.0 )
-%
-% Far-field boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Symmetry boundary marker(s) (NONE = no marker)
 MARKER_SYM= ( symmetry )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( wing )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( wing )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 EXT_ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (NONE, JACOBI, LINELET)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.7
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.7
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE)
-OBJECTIVE_FUNCTION= DRAG
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
+OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.8
-%
-% Limit value for the adjoint variable
 LIMIT_ADJFLOW= 1E6
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= YES
-%
-% Sensitivity smoothing (NONE, SOBOLEV, BIGRID)
 SENS_SMOOTHING= NONE
-%
-% Adjoint frozen viscosity (NO, YES)
 FROZEN_VISC_CONT= YES
 
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
 %
-% Marker(s) of the surface where geometrical based function will be evaluated
 GEO_MARKER= ( wing )
-%
-% Description of the geometry to be analyzed (AIRFOIL, WING, FUSELAGE)
 GEO_DESCRIPTION= WING
-%
-% Coordinate of the stations to be analyzed
 GEO_LOCATION_STATIONS= (0.0, 0.2, 0.4, 0.6, 0.8)
-%
-% Geometrical bounds (Y coordinate) for the wing geometry analysis or
-% fuselage evaluation (X coordinate).
 GEO_BOUNDS= (0.0806, 1.1284)
-%
-% Plot loads and Cp distributions on each airfoil section
 GEO_PLOT_STATIONS= NO
-%
-% Geometrical evaluation mode (FUNCTION, GRADIENT)
 GEO_MODE= FUNCTION
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, PARABOLIC, NACA_4DIGITS,
-%                      DISPLACEMENT, ROTATION, FFD_CONTROL_POINT,
-%                      FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE,
-%                      FFD_ROTATION, FFD_CAMBER, FFD_THICKNESS, FFD_VOLUME)
 DV_KIND= FFD_CONTROL_POINT
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( wing )
-%
-% Parameters of the shape deformation
-%       - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-%       - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-%       - PARABOLIC ( Center, Thickness )
-%       - DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-%       - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%       - OBSTACLE ( Center, Bump size )
-%       - FFD_CONTROL_POINT ( FFD_BoxTag ID, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-%       - FFD_DIHEDRAL_ANGLE ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%       - FFD_TWIST_ANGLE ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%       - FFD_ROTATION ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%       - FFD_CAMBER ( FFD_BoxTag ID, i_Ind, j_Ind )
-%       - FFD_THICKNESS ( FFD_BoxTag ID, i_Ind, j_Ind )
-%       - FFD_VOLUME ( FFD_BoxTag ID, i_Ind, j_Ind )
 DV_PARAM= ( 0, 2, 2, 1, 0.0, 0.0, 1.0 )
-%
-% New value of the shape deformation
 DV_VALUE= 0.1
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 1
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 50
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-5
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_ONERAM6_turb_tets.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1
-%
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-
-% Optimization objective function with optional scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.02
-
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='  (LIFT > 0.267) * 0.02
 OPT_CONSTRAINT= (LIFT > 0.268) * 0.02; (STATION1_THICKNESS > 0.0570) * 0.02; (STATION2_THICKNESS > 0.0513) * 0.02; (STATION3_THICKNESS > 0.0457) * 0.02; (STATION4_THICKNESS > 0.0399) * 0.02; (STATION5_THICKNESS > 0.0343) * 0.02
-
-% List of design variables (Design variables are separated by semicolons)
 DEFINITION_DV= ( 11, 1.0 | wing | 0, 0, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 1, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 2, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 3, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 4, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 0, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 1, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 2, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 3, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 4, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 0, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 1, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 2, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 3, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 4, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 0, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 1, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 2, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 3, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 4, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 0, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 1, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 2, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 3, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 4, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 0, 0, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 1, 0, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 2, 0, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 3, 0, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 4, 0, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 0, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 1, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 2, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 3, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 4, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 0, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 1, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 2, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 3, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 4, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 0, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 1, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 2, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 3, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 4, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 0, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 1, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 2, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 3, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | 0, 4, 4, 0, 0.0, 0.0, 1.0 )
diff --git a/TestCases/optimization_rans/steady_oneram6/turb_ONERAM6.cfg b/TestCases/optimization_rans/steady_oneram6/turb_ONERAM6.cfg
index 66b7b8c8d84..d8e8f30e129 100644
--- a/TestCases/optimization_rans/steady_oneram6/turb_ONERAM6.cfg
+++ b/TestCases/optimization_rans/steady_oneram6/turb_ONERAM6.cfg
@@ -5,359 +5,135 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.4.0 "Blackbird" 	                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)            
 SOLVER= NAVIER_STOKES
-%
-% Specify turbulence model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8395
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 3.06
-%
-% Side-slip angle (degrees, only for compressible flows)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 11.72E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 0.64607
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 0.64607
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( wing, 0.0 )
-%
-% Far-field boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Symmetry boundary marker(s) (NONE = no marker)
 MARKER_SYM= ( symmetry )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( wing )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( wing )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 4.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 EXT_ITER= 10000
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (NONE, JACOBI, LINELET)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-5
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.7
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.7
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Slope limiter (VENKATAKRISHNAN, SHARP_EDGES)
 SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.8
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
 
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
 %
-% Geometrical evaluation mode (FUNCTION, GRADIENT)
 GEO_MODE= FUNCTION
-%
-% Marker(s) of the surface where geometrical based func. will be evaluated
 GEO_MARKER= ( wing )
-%
-% Orientation of airfoil sections (X_AXIS, Y_AXIS, Z_AXIS)
 GEO_AXIS_STATIONS= Y_AXIS
-%
-% Location (coordinate) of the airfoil sections (MinValue, MaxValue)
 GEO_WING_BOUNDS= (0.0806, 1.1284)
-%
-% Plot loads and Cp distributions on each airfoil section
 GEO_PLOT_STATIONS= NO
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Kind of deformation (FFD_SETTING, FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC,
-%                      NACA_4DIGITS, DISPLACEMENT, ROTATION, FFD_CONTROL_POINT, 
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CAMBER, FFD_THICKNESS, SURFACE_FILE)
 DV_KIND= FFD_CONTROL_POINT
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( wing )
-%
-% Parameters of the shape deformation
-%       - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-%       - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-%       - PARABOLIC ( Center, Thickness )
-%       - DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-%       - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%       - OBSTACLE ( Center, Bump size )
-%       - FFD_CONTROL_POINT ( FFD_BoxTag ID, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-%       - FFD_DIHEDRAL_ANGLE ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%       - FFD_TWIST_ANGLE ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%       - FFD_ROTATION ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%       - FFD_CAMBER ( FFD_BoxTag ID, i_Ind, j_Ind )
-%       - FFD_THICKNESS ( FFD_BoxTag ID, i_Ind, j_Ind )
-%       - FFD_VOLUME ( FFD_BoxTag ID, i_Ind, j_Ind )
 DV_PARAM= ( WING_BOX, 2, 2, 1, 0.0, 0.0, 1.0 )
-%
-% New value of the shape deformation
 DV_VALUE= 0.1
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 1
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-5
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_ONERAM6_turb.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1000
-%
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-
-% Optimization objective function with optional scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.001
-
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= (LIFT > 0.268) * 0.001
-
-% List of design variables (Design variables are separated by semicolons)
 DEFINITION_DV= ( 11, 1.0 | wing | WING_BOX, 0, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 1, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 2, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 3, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 4, 0, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 0, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 1, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 2, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 3, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 4, 1, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 0, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 1, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 2, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 3, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 4, 2, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 0, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 1, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 2, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 3, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 4, 3, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 0, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 1, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 2, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 3, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 4, 4, 1, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 0, 0, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 1, 0, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 2, 0, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 3, 0, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 4, 0, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 0, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 1, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 2, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 3, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 4, 1, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 0, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 1, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 2, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 3, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 4, 2, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 0, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 1, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 2, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 3, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 4, 3, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 0, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 1, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 2, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 3, 4, 0, 0.0, 0.0, 1.0 ); ( 11, 1.0 | wing | WING_BOX, 4, 4, 0, 0.0, 0.0, 1.0 )
diff --git a/TestCases/optimization_rans/steady_rae2822/turb_SA_RAE2822.cfg b/TestCases/optimization_rans/steady_rae2822/turb_SA_RAE2822.cfg
index 67f9d0e22ae..a6344ee4b2d 100644
--- a/TestCases/optimization_rans/steady_rae2822/turb_SA_RAE2822.cfg
+++ b/TestCases/optimization_rans/steady_rae2822/turb_SA_RAE2822.cfg
@@ -5,342 +5,128 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                              
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.729
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 2.31
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.5E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( AIRFOIL, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( FARFIELD )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( AIRFOIL )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( AIRFOIL )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 4.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 ITER= 10000
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.95
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.95
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                              ROE-2ND_ORDER, AUSM-1ST_ORDER, AUSM-2ND_ORDER,
-%                              HLLC-1ST_ORDER, HLLC-2ND_ORDER)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND-1ST_ORDER, 
-%                              SCALAR_UPWIND-2ND_ORDER)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREESURFACE)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE-1ST_ORDER, 
-%                              ROE-2ND_ORDER)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH)
 SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.008 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.75
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Limit value for the adjoint variable
 LIMIT_ADJFLOW= 1E6
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
-%
-% Adjoint frozen viscosity (NO, YES)
 FROZEN_VISC_CONT= YES
 
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
 %
-% Marker(s) of the surface where geometrical based function will be evaluated
 GEO_MARKER= ( airfoil )
-%
-% Description of the geometry to be analyzed (AIRFOIL, WING, FUSELAGE)
 GEO_DESCRIPTION= AIRFOIL
-%
-% Geometrical evaluation mode (FUNCTION, GRADIENT)
 GEO_MODE= FUNCTION
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -9
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_RAE2822_turb.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 10000
-%
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Kind of deformation (FFD_SETTING, FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      HICKS_HENNE, PARABOLIC,
-%                      NACA_4DIGITS, DISPLACEMENT, ROTATION, FFD_CONTROL_POINT, 
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CAMBER, FFD_THICKNESS, SURFACE_FILE)
 DV_KIND= FFD_SETTING
-%
-% Marker of the surface to which we are going apply the shape deformation
 DV_MARKER= ( AIRFOIL )
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( Center, Thickness )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- OBSTACLE ( Center, Bump size )
-% 	- FFD_CONTROL_POINT ( FFD_BoxTag ID, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% 	- FFD_DIHEDRAL_ANGLE ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_TWIST_ANGLE ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_ROTATION ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_CAMBER ( FFD_BoxTag ID, i_Ind, j_Ind )
-% 	- FFD_THICKNESS ( FFD_BoxTag ID, i_Ind, j_Ind )
-% 	- FFD_VOLUME ( FFD_BoxTag ID, i_Ind, j_Ind )
 DV_PARAM= ( 1, 0.5 )
-%
-% New value of the shape deformation
 DV_VALUE= 0.01
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-
-% Optimization objective function with optional scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.001
-
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= ( LIFT > 0.723 ) * 0.001
-
-% List of design variables (Design variables are separated by semicolons)
 DEFINITION_DV= ( 30, 1.0 | AIRFOIL | 0, 0.05 ); ( 30, 1.0 | AIRFOIL | 0, 0.10 ); ( 30, 1.0 | AIRFOIL | 0, 0.15 ); ( 30, 1.0 | AIRFOIL | 0, 0.20 ); ( 30, 1.0 | AIRFOIL | 0, 0.25 ); ( 30, 1.0 | AIRFOIL | 0, 0.30 ); ( 30, 1.0 | AIRFOIL | 0, 0.35 ); ( 30, 1.0 | AIRFOIL | 0, 0.40 ); ( 30, 1.0 | AIRFOIL | 0, 0.45 ); ( 30, 1.0 | AIRFOIL | 0, 0.50 ); ( 30, 1.0 | AIRFOIL | 0, 0.55 ); ( 30, 1.0 | AIRFOIL | 0, 0.60 ); ( 30, 1.0 | AIRFOIL | 0, 0.65 ); ( 30, 1.0 | AIRFOIL | 0, 0.70 ); ( 30, 1.0 | AIRFOIL | 0, 0.75 ); ( 30, 1.0 | AIRFOIL | 0, 0.80 ); ( 30, 1.0 | AIRFOIL | 0, 0.85 ); ( 30, 1.0 | AIRFOIL | 0, 0.90 ); ( 30, 1.0 | AIRFOIL | 0, 0.95 ); ( 30, 1.0 | AIRFOIL | 1, 0.05 ); ( 30, 1.0 | AIRFOIL | 1, 0.10 ); ( 30, 1.0 | AIRFOIL | 1, 0.15 ); ( 30, 1.0 | AIRFOIL | 1, 0.20 ); ( 30, 1.0 | AIRFOIL | 1, 0.25 ); ( 30, 1.0 | AIRFOIL | 1, 0.30 ); ( 30, 1.0 | AIRFOIL | 1, 0.35 ); ( 30, 1.0 | AIRFOIL | 1, 0.40 ); ( 30, 1.0 | AIRFOIL | 1, 0.45 ); ( 30, 1.0 | AIRFOIL | 1, 0.50 ); ( 30, 1.0 | AIRFOIL | 1, 0.55 ); ( 30, 1.0 | AIRFOIL | 1, 0.60 ); ( 30, 1.0 | AIRFOIL | 1, 0.65 ); ( 30, 1.0 | AIRFOIL | 1, 0.70 ); ( 30, 1.0 | AIRFOIL | 1, 0.75 ); ( 30, 1.0 | AIRFOIL | 1, 0.80 ); ( 30, 1.0 | AIRFOIL | 1, 0.85 ); ( 30, 1.0 | AIRFOIL | 1, 0.90 ); ( 30, 1.0 | AIRFOIL | 1, 0.95 )
-
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index c70fc62afad..66d17832076 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -3,7 +3,7 @@
 ## \file parallel_regression.py
 #  \brief Python script for automated regression testing of SU2 examples
 #  \author A. Aranake, A. Campos, T. Economon, T. Lukaczyk, S. Padron
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 #
@@ -80,6 +80,16 @@ def main():
     invwedge.new_output = True
     test_list.append(invwedge)
 
+    # Inviscid single wedge, implicit, NEMO supersonic inlet
+    invwedge_ss_inlet = TestCase('invwedge_ss_inlet')
+    invwedge_ss_inlet.cfg_dir = "nonequilibrium/invwedge"
+    invwedge_ss_inlet.cfg_file = "invwedge_ss_inlet.cfg"
+    invwedge_ss_inlet.test_iter = 10
+    invwedge_ss_inlet.test_vals = [-1.042718, -1.567481, -18.250175, -18.579516, -18.523248, 2.275305, 1.880068, 5.319548, 0.873821]
+    invwedge_ss_inlet.test_vals_aarch64 = [-1.042718, -1.567481, -18.250175, -18.579516, -18.523248, 2.275305, 1.880068, 5.319548, 0.873821]
+    invwedge_ss_inlet.new_output = True
+    test_list.append(invwedge_ss_inlet)
+
     # Viscous single cone - axisymmetric
     visc_cone           = TestCase('visc_cone')
     visc_cone.cfg_dir   = "nonequilibrium/viscous"
@@ -302,6 +312,15 @@ def main():
     turb_oneram6.timeout   = 3200
     test_list.append(turb_oneram6)
 
+    # ONERA M6 Wing - vorticity confinement
+    turb_oneram6_vc = TestCase('turb_oneram6_vc')
+    turb_oneram6_vc.cfg_dir = "rans/oneram6"
+    turb_oneram6_vc.cfg_file = "turb_ONERAM6_vc.cfg"
+    turb_oneram6_vc.test_iter = 15
+    turb_oneram6_vc.test_vals = [-2.262387, -6.626467, 0.228393, 0.140799, -2.7107e+04]
+    turb_oneram6_vc.timeout = 3200
+    test_list.append(turb_oneram6_vc)
+
     # ONERA M6 Wing - Newton-Krylov
     turb_oneram6_nk           = TestCase('turb_oneram6_nk')
     turb_oneram6_nk.cfg_dir   = "rans/oneram6"
@@ -1146,7 +1165,7 @@ def main():
     solid_periodic_pins.cfg_dir   = "solid_heat_conduction/periodic_pins"
     solid_periodic_pins.cfg_file  = "configSolid.cfg"
     solid_periodic_pins.test_iter = 750
-    solid_periodic_pins.test_vals         = [-15.878958, -14.569206, 300.900000, 425.320000, 0.000000, 5.000000, -1.672714] #last 7 lines
+    solid_periodic_pins.test_vals = [-15.878977, -14.569206, 300.900000, 425.320000, 0.000000, 5.000000, -1.672737] #last 7 lines
     solid_periodic_pins.test_vals_aarch64 = [-15.879010, -14.569206, 300.900000, 425.320000, 0.000000, 5.000000, -1.672630] #last 7 lines
     test_list.append(solid_periodic_pins)
 
@@ -1359,7 +1378,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_viscosity.test_vals = [-4.738778, -4.325766, -4.610914, -5.834431, 0.521730, -4.934375, 5.000000, -1.887191, 5.000000, -5.499917, 5.000000, -1.770845, 2.292904, 0.971941, 0.608500, 0.712464]
     species2_primitiveVenturi_mixingmodel_viscosity.new_output = True
     test_list.append(species2_primitiveVenturi_mixingmodel_viscosity)
-    
+
     # 2 species (1 eq) primitive venturi mixing using mixing model including heat capacity and mass diffusivity
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2           = TestCase('species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg')
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg_dir   = "species_transport/venturi_primitive_3species"
@@ -1371,7 +1390,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.new_output = True
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.tol       = 0.00001
     test_list.append(species2_primitiveVenturi_mixingmodel_heatcapacity_H2)
-    
+
     # 2 species (1 eq) primitive venturi mixing using mixing model including heat capacity and mass diffusivity NonDimensional case
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND           = TestCase('species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg')
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg_dir   = "species_transport/venturi_primitive_3species"
@@ -1383,7 +1402,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.new_output = True
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.tol       = 0.00001
     test_list.append(species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND)
-    
+
     # 2 species (1 eq) primitive venturi mixing
     species2_primitiveVenturi           = TestCase('species2_primitiveVenturi')
     species2_primitiveVenturi.cfg_dir   = "species_transport/venturi_primitive_3species"
@@ -1401,7 +1420,7 @@ def main():
     species_primitiveVenturi_boundedscalar.test_vals   = [-5.297585, -4.397797, -4.377086, -5.593131, -1.011782, -5.623540, 5.000000, -1.775123, 5.000000, -4.086339, 5.000000, -2.080187, 0.000424, 0.000424, 0.000000, 0.000000]
     species_primitiveVenturi_boundedscalar.new_output  = True
     test_list.append(species_primitiveVenturi_boundedscalar)
-    
+
     # 2 species (1 eq) primitive venturi mixing using mixing model including inlet markers for turbulent intensity and viscosity ratios
     species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS           = TestCase('species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg')
     species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg_dir   = "species_transport/venturi_primitive_3species"
diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index 0c687ebeed6..1e7e82189df 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -3,11 +3,11 @@
 ## \file parallel_regression.py
 #  \brief Python script for automated regression testing of SU2 examples
 #  \author A. Aranake, A. Campos, T. Economon, T. Lukaczyk, S. Padron
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
-# 
-# The SU2 Project is maintained by the SU2 Foundation 
+#
+# The SU2 Project is maintained by the SU2 Foundation
 # (http://su2foundation.org)
 #
 # Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
@@ -16,7 +16,7 @@
 # modify it under the terms of the GNU Lesser General Public
 # License as published by the Free Software Foundation; either
 # version 2.1 of the License, or (at your option) any later version.
-# 
+#
 # SU2 is distributed in the hope that it will be useful,
 # but WITHOUT ANY WARRANTY; without even the implied warranty of
 # MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
@@ -29,11 +29,11 @@
 from __future__ import print_function
 
 import sys
-from TestCase import TestCase    
+from TestCase import TestCase
 
 def main():
-    '''This program runs SU2 and ensures that the output matches specified values. 
-       This will be used to do checks when code is pushed to github 
+    '''This program runs SU2 and ensures that the output matches specified values.
+       This will be used to do checks when code is pushed to github
        to make sure nothing is broken. '''
 
     test_list = []
@@ -49,7 +49,7 @@ def main():
     discadj_naca0012.test_iter = 100
     discadj_naca0012.test_vals = [-3.561506, -8.926634, -0.000000, 0.005587]
     test_list.append(discadj_naca0012)
-   
+
     # Inviscid Cylinder 3D (multiple markers)
     discadj_cylinder3D           = TestCase('discadj_cylinder3D')
     discadj_cylinder3D.cfg_dir   = "disc_adj_euler/cylinder3D"
@@ -65,7 +65,7 @@ def main():
     discadj_arina2k.test_iter    = 20
     discadj_arina2k.test_vals    = [-3.111181, -3.501516, 6.8705e-02, 0]
     test_list.append(discadj_arina2k)
-    
+
     # Equivalent area NACA64-206
     ea_naca64206              = TestCase('ea_naca64206')
     ea_naca64206.cfg_dir      = "optimization_euler/equivalentarea_naca64206"
@@ -157,16 +157,16 @@ def main():
     #######################################################
     ### Unsteady Disc. adj. compressible RANS           ###
     #######################################################
-   
+
     # Turbulent Cylinder
     discadj_cylinder           = TestCase('unsteady_cylinder')
     discadj_cylinder.cfg_dir   = "disc_adj_rans/cylinder"
-    discadj_cylinder.cfg_file  = "cylinder.cfg" 
+    discadj_cylinder.cfg_file  = "cylinder.cfg"
     discadj_cylinder.test_iter = 9
     discadj_cylinder.test_vals = [3.746909, -1.544883, -0.008321, 0.000014] #last 4 columns
     discadj_cylinder.unsteady  = True
     test_list.append(discadj_cylinder)
-    
+
     ##############################################################
     ### Unsteady Disc. adj. compressible RANS Windowed Average ###
     ##############################################################
@@ -174,12 +174,12 @@ def main():
     # Turbulent Cylinder
     discadj_cylinder           = TestCase('unsteady_cylinder_windowed_average_AD')
     discadj_cylinder.cfg_dir   = "disc_adj_rans/cylinder"
-    discadj_cylinder.cfg_file  = "cylinder_Windowing_AD.cfg" 
+    discadj_cylinder.cfg_file  = "cylinder_Windowing_AD.cfg"
     discadj_cylinder.test_iter = 9
     discadj_cylinder.test_vals = [3.004406] #last column
     discadj_cylinder.unsteady  = True
     test_list.append(discadj_cylinder)
-    
+
     ##############################################################
     ### Unsteady Disc. adj. compressible RANS Windowed Average ###
     ##############################################################
@@ -187,14 +187,14 @@ def main():
     # Turbulent Cylinder
     discadj_cylinder           = TestCase('unsteady_cylinder_windowed_average')
     discadj_cylinder.cfg_dir   = "disc_adj_rans/cylinder"
-    discadj_cylinder.cfg_file  = "cylinder_Windowing.cfg" 
+    discadj_cylinder.cfg_file  = "cylinder_Windowing.cfg"
     discadj_cylinder.test_iter = 6
     discadj_cylinder.test_vals = [0.202349, -0.000119, 1.899933, -0.000050, 1.067900]
     discadj_cylinder.tol       = 0.0001
     discadj_cylinder.command   = TestCase.Command("mpirun -n 2", "SU2_CFD_DIRECTDIFF")
     discadj_cylinder.unsteady  = True
-    test_list.append(discadj_cylinder)  
-    
+    test_list.append(discadj_cylinder)
+
     ##########################################################################
     ### Unsteady Disc. adj. compressible RANS DualTimeStepping 1st order   ###
     ##########################################################################
@@ -224,27 +224,27 @@ def main():
     #######################################################
     ### Disc. adj. turbomachinery                       ###
     #######################################################
-    
+
     # Transonic Stator 2D
     discadj_trans_stator           = TestCase('transonic_stator')
     discadj_trans_stator.cfg_dir   = "disc_adj_turbomachinery/transonic_stator_2D"
-    discadj_trans_stator.cfg_file  = "transonic_stator.cfg" 
+    discadj_trans_stator.cfg_file  = "transonic_stator.cfg"
     discadj_trans_stator.test_iter = 79
     discadj_trans_stator.test_vals = [79.000000, -1.941681, -1.984570]
     test_list.append(discadj_trans_stator)
-    
+
     ###################################
     ### Structural Adjoint          ###
     ###################################
-   
+
     # Structural model
     discadj_fea           = TestCase('discadj_fea')
     discadj_fea.cfg_dir   = "disc_adj_fea"
-    discadj_fea.cfg_file  = "configAD_fem.cfg" 
+    discadj_fea.cfg_file  = "configAD_fem.cfg"
     discadj_fea.test_iter = 4
     discadj_fea.test_vals         = [-2.849774, -3.238669, -0.000364, -8.708700] #last 4 columns
     discadj_fea.test_vals_aarch64 = [-2.849726, -3.238594, -0.000364, -8.708700] #last 4 columns
-    test_list.append(discadj_fea) 
+    test_list.append(discadj_fea)
 
     ###################################
     ### Disc. adj. heat             ###
@@ -255,14 +255,14 @@ def main():
     discadj_heat.cfg_dir   = "disc_adj_heat"
     discadj_heat.cfg_file  = "disc_adj_heat.cfg"
     discadj_heat.test_iter = 10
-    discadj_heat.test_vals         = [-2.280433, 0.714828, -0.743730, -6.767300]
-    discadj_heat.test_vals_aarch64 = [-2.280428, 0.714835, -0.743730, -6.767300]
+    discadj_heat.test_vals         = [-2.344307, 0.721551, -0.507470, -5.612700]
+    discadj_heat.test_vals_aarch64 = [-2.344307, 0.721551, -0.507470, -5.612700]
     test_list.append(discadj_heat)
 
     ###################################
     ### Coupled FSI Adjoint         ###
     ###################################
-   
+
     # Legacy driver
     discadj_fsi           = TestCase('discadj_fsi')
     discadj_fsi.cfg_dir   = "disc_adj_fsi"
@@ -316,8 +316,8 @@ def main():
     da_unsteadyCHT_cylinder.cfg_dir   = "coupled_cht/disc_adj_unsteadyCHT_cylinder"
     da_unsteadyCHT_cylinder.cfg_file  = "chtMaster.cfg"
     da_unsteadyCHT_cylinder.test_iter = 2
-    da_unsteadyCHT_cylinder.test_vals         = [-3.521358, -4.312658, -4.271025, -9.846075, -7.967741, 0.000000, 3.684000, 2.9483e-01]
-    da_unsteadyCHT_cylinder.test_vals_aarch64 = [-3.521358, -4.312658, -4.271025, -9.846075, -7.967741, 0.000000, 3.684000, 2.9483e-01]
+    da_unsteadyCHT_cylinder.test_vals         = [-3.508906, -4.317739, -4.241558, -11.836892, -12.862650, 0.000000, 3.688000, 0.295190]
+    da_unsteadyCHT_cylinder.test_vals_aarch64 = [-3.508906, -4.317739, -4.241558, -11.836892, -12.862650, 0.000000, 3.688000, 0.295190]
     da_unsteadyCHT_cylinder.unsteady  = True
     da_unsteadyCHT_cylinder.multizone = True
     test_list.append(da_unsteadyCHT_cylinder)
@@ -364,7 +364,7 @@ def main():
     # NACA0012 Airfoil
     unsteady_naca0012           = TestCase('unsteady_NACA0012_restart_adjoint')
     unsteady_naca0012.cfg_dir   = "disc_adj_rans/naca0012"
-    unsteady_naca0012.cfg_file  = "naca0012.cfg" 
+    unsteady_naca0012.cfg_file  = "naca0012.cfg"
     unsteady_naca0012.test_iter = 14
     unsteady_naca0012.command   = TestCase.Command(exec = "discrete_adjoint.py", param = "-f")
     unsteady_naca0012.timeout   = 1600
@@ -373,7 +373,7 @@ def main():
     unsteady_naca0012.unsteady  = True
     pass_list.append(unsteady_naca0012.run_filediff())
     test_list.append(unsteady_naca0012)
-    
+
     ####################################################################################
     ### Unsteady Disc. adj. compressible RANS Windowed Average  only adjoint 		 ###
     ####################################################################################
@@ -381,7 +381,7 @@ def main():
     # NACA0012 Airfoil (Test depends on results of "unsteady_NACA0012_restart_adjoint")
     unsteady_naca0012           = TestCase('unsteady_NACA0012_adjoint_only')
     unsteady_naca0012.cfg_dir   = "disc_adj_rans/naca0012"
-    unsteady_naca0012.cfg_file  = "naca0012.cfg" 
+    unsteady_naca0012.cfg_file  = "naca0012.cfg"
     unsteady_naca0012.test_iter = 14
     unsteady_naca0012.command   = TestCase.Command(exec = "discrete_adjoint.py", param = "-m adj -f")
     unsteady_naca0012.timeout   = 1600
diff --git a/TestCases/pastix_support/config.cfg b/TestCases/pastix_support/config.cfg
index 1c9edf1f39c..adc8c4a3fd2 100644
--- a/TestCases/pastix_support/config.cfg
+++ b/TestCases/pastix_support/config.cfg
@@ -2,7 +2,7 @@
 % SU2 configuration file                                                 %
 % PaStiX options (http://pastix.gforge.inria.fr/files/README-txt.html)   %
 % Institution: Imperial College London                                   %
-% File Version 7.4.0 "Blackbird"                                            %
+% File Version 7.5.0 "Blackbird"                                         %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
 % Intro:
@@ -39,4 +39,3 @@ PASTIX_FACTORIZATION_FREQUENCY= 1 % 0 means "only on first iteration"
 % By default the solver runs silently, more verbosity can be set via
 PASTIX_VERBOSITY_LEVEL= 0 % - Silent
 % 1 - On factorization, solves, and cleanup; 2 - Same with more detail.
-
diff --git a/TestCases/pastix_support/readme.txt b/TestCases/pastix_support/readme.txt
index 5fd5c6ffd1a..034388e5314 100644
--- a/TestCases/pastix_support/readme.txt
+++ b/TestCases/pastix_support/readme.txt
@@ -2,7 +2,7 @@
 % SU2 configuration file                                                 %
 % PaStiX support build instructions.                                     %
 % Institution: Imperial College London                                   %
-% File Version 7.4.0 "Blackbird"                                         %
+% File Version 7.5.0 "Blackbird"                                         %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
 % 1 - Download
diff --git a/TestCases/polar/naca0012/inv_NACA0012.cfg b/TestCases/polar/naca0012/inv_NACA0012.cfg
index e91b9b0eee0..c0529986d6a 100644
--- a/TestCases/polar/naca0012/inv_NACA0012.cfg
+++ b/TestCases/polar/naca0012/inv_NACA0012.cfg
@@ -5,354 +5,133 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Number of Zones needed for python scripts
 NZONES= 1
-%
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
 AOA= 1.25
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 273.15
 
 % -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
 %
-% Ratio of specific heats (1.4 (air), only for compressible flows)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
 GAS_CONSTANT= 287.87
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= DIMENSIONAL
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (NONE = no marker)
 MARKER_FAR= ( farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( airfoil )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( airfoil )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 4.0
-%
-% Number of total iterations
 ITER= 11
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 1.0
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 1.0
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-%
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.5
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (NO_DEFORMATION, TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING, FFD_NACELLE
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS, FFD_TWIST
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D, FFD_TWIST_2D,
-%                      HICKS_HENNE, SURFACE_BUMP)
 DV_KIND= FFD_SETTING
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation
-% - NO_DEFORMATION ( 1.0 )
-% - TRANSLATION ( x_Disp, y_Disp, z_Disp ), as a unit vector
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - SCALE ( 1.0 )
-% - ANGLE_OF_ATTACK ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_NACELLE ( FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Disp, phi_Disp )
-% - FFD_GULL ( FFD_BoxTag, j_Ind )
-% - FFD_ANGLE_OF_ATTACK ( FFD_BoxTag, 1.0 )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_TWIST ( FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - FFD_TWIST_2D ( FFD_BoxTag, x_Orig, y_Orig )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - SURFACE_BUMP ( x_Start, x_End, x_Loc )
 DV_PARAM= ( 1, 0.5 )
-%
-% Value of the shape deformation
 DV_VALUE= 0.01
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= mesh_NACA0012_inv.su2
 %
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FILENAME= mesh_NACA0012_inv.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-% 
-% Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
-% 
-% History output
 HISTORY_OUTPUT= (RMS_RES, AERO_COEFF)
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.001
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= ( LIFT > 0.328188 ) * 0.001; ( MOMENT_Z > 0.034068 ) * 0.001; ( AIRFOIL_THICKNESS > 0.11 ) * 0.001
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 ); ( 30, 1.0 | airfoil | 0, 0.20 ); ( 30, 1.0 | airfoil | 0, 0.25 ); ( 30, 1.0 | airfoil | 0, 0.30 ); ( 30, 1.0 | airfoil | 0, 0.35 ); ( 30, 1.0 | airfoil | 0, 0.40 ); ( 30, 1.0 | airfoil | 0, 0.45 ); ( 30, 1.0 | airfoil | 0, 0.50 ); ( 30, 1.0 | airfoil | 0, 0.55 ); ( 30, 1.0 | airfoil | 0, 0.60 ); ( 30, 1.0 | airfoil | 0, 0.65 ); ( 30, 1.0 | airfoil | 0, 0.70 ); ( 30, 1.0 | airfoil | 0, 0.75 ); ( 30, 1.0 | airfoil | 0, 0.80 ); ( 30, 1.0 | airfoil | 0, 0.85 ); ( 30, 1.0 | airfoil | 0, 0.90 ); ( 30, 1.0 | airfoil | 0, 0.95 ); ( 30, 1.0 | airfoil | 1, 0.05 ); ( 30, 1.0 | airfoil | 1, 0.10 ); ( 30, 1.0 | airfoil | 1, 0.15 ); ( 30, 1.0 | airfoil | 1, 0.20 ); ( 30, 1.0 | airfoil | 1, 0.25 ); ( 30, 1.0 | airfoil | 1, 0.30 ); ( 30, 1.0 | airfoil | 1, 0.35 ); ( 30, 1.0 | airfoil | 1, 0.40 ); ( 30, 1.0 | airfoil | 1, 0.45 ); ( 30, 1.0 | airfoil | 1, 0.50 ); ( 30, 1.0 | airfoil | 1, 0.55 ); ( 30, 1.0 | airfoil | 1, 0.60 ); ( 30, 1.0 | airfoil | 1, 0.65 ); ( 30, 1.0 | airfoil | 1, 0.70 ); ( 30, 1.0 | airfoil | 1, 0.75 ); ( 30, 1.0 | airfoil | 1, 0.80 ); ( 30, 1.0 | airfoil | 1, 0.85 ); ( 30, 1.0 | airfoil | 1, 0.90 ); ( 30, 1.0 | airfoil | 1, 0.95 )
diff --git a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
index 9a4333bdecf..6cc8c276be0 100755
--- a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
@@ -3,7 +3,7 @@
 ## \file run_adjoint.py
 #  \brief Python script to launch SU2_CFD_AD and compute the sensitivity of the FEA problem respect to flow loads.
 #  \author Ruben Sanchez
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/configAD_flow.cfg b/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/configAD_flow.cfg
index cde462e8186..a387578e514 100644
--- a/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/configAD_flow.cfg
+++ b/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/configAD_flow.cfg
@@ -10,19 +10,11 @@
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               TNE2_EULER, TNE2_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= INC_NAVIER_STOKES
-
 KIND_TURB_MODEL= NONE
 MATH_PROBLEM= DISCRETE_ADJOINT
-
 RESTART_SOL= NO
-
 MULTIZONE_MESH = NO
-
 ITER = 181
 INNER_ITER = 181
 
@@ -33,15 +25,11 @@ OBJECTIVE_FUNCTION = DRAG
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 
 INC_DENSITY_MODEL= CONSTANT
-
 INC_ENERGY_EQUATION = NO
 INC_DENSITY_INIT= 1.0
 INC_VELOCITY_INIT= ( 1.0, 0.0, 0.0 )
-
 INC_TEMPERATURE_INIT= 300
-
 INC_NONDIM= INITIAL_VALUES
-
 INC_DENSITY_REF= 1.0
 INC_VELOCITY_REF= 1.0
 INC_TEMPERATURE_REF = 1.0
@@ -56,34 +44,27 @@ MU_CONSTANT= 0.001
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-
 REF_LENGTH= 0.01
 REF_AREA= 0.01
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 
 MARKER_HEATFLUX= ( wallF, 0.0 )
-
 INC_INLET_TYPE= VELOCITY_INLET
 INC_OUTLET_TYPE= PRESSURE_OUTLET
-
 MARKER_INLET= ( inlet, 0.0, 1.0, 1.0, 0.0, 0.0 )
 MARKER_OUTLET= ( outlet, 0.0 )
 MARKER_EULER= ( upper, lower )
-
 MARKER_PLOTTING= ( wallF )
 MARKER_MONITORING= ( wallF )
-
 MARKER_DEFORM_MESH= ( wallF )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 CFL_NUMBER= 1000
-
 CFL_ADAPT= NO
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
@@ -93,17 +74,6 @@ LINEAR_SOLVER_PREC= ILU
 LINEAR_SOLVER_ERROR= 1E-15
 LINEAR_SOLVER_ITER= 20
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-
-MGLEVEL= 0
-MGCYCLE= V_CYCLE
-
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-MG_DAMP_RESTRICTION= 0.7
-MG_DAMP_PROLONGATION= 0.7
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 
 CONV_NUM_METHOD_FLOW= FDS
@@ -129,22 +99,16 @@ CONV_CAUCHY_EPS= 1E-5
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 
 MESH_FILENAME= meshFlow.su2
-
 MESH_FORMAT= SU2
 MESH_OUT_FILENAME= mesh_out.su2
-
 SOLUTION_FILENAME= solution_flow.dat
 RESTART_FILENAME= restart_flow.dat
-
 TABULAR_FORMAT= CSV
 CONV_FILENAME= history
-
 VOLUME_FILENAME= flow
 SURFACE_FILENAME= surface_flow
-
 OUTPUT_WRT_FREQ= 1000
 
-
 % --------------------------- MESH PARAMETERS ---------------------------------%
 
 DEFORM_MESH = YES
@@ -158,4 +122,3 @@ DEFORM_LINEAR_SOLVER_ITER = 5000
 DEFORM_CONSOLE_OUTPUT = NO
 
 READ_BINARY_RESTART=NO
-
diff --git a/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
index 2cfdad41f7d..bb42dfcccf2 100755
--- a/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
@@ -3,7 +3,7 @@
 ## \file run_adjoint.py
 #  \brief Python script to launch SU2_CFD_AD
 #  \author Ruben Sanchez
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/py_wrapper/flatPlate_rigidMotion/flatPlate_rigidMotion_Conf.cfg b/TestCases/py_wrapper/flatPlate_rigidMotion/flatPlate_rigidMotion_Conf.cfg
index 83371b2c847..b95f06f8bee 100644
--- a/TestCases/py_wrapper/flatPlate_rigidMotion/flatPlate_rigidMotion_Conf.cfg
+++ b/TestCases/py_wrapper/flatPlate_rigidMotion/flatPlate_rigidMotion_Conf.cfg
@@ -5,232 +5,119 @@
 % Author: ___________________________________________________________________  %
 % Institution: ______________________________________________________________  %
 % Date: __________                                                             %
-% File Version 7.4.0 "Blackbird"                                                   %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= RANS
-%
-% Specify turbulence model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SST
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.03059
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Init option to choose between Reynolds (default) or thermodynamics quantities
-% for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= REYNOLDS
-%
-% Free-stream option to choose between density and temperature (default) for
-% initializing the solution (TEMPERATURE_FS, DENSITY_FS)
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-% Free-stream temperature (288.15 K, 518.67 R by default)
 FREESTREAM_TEMPERATURE= 293.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 24407.25244
-%
-% Reynolds length (1 m, 1 inch by default)
 REYNOLDS_LENGTH= 0.035
-%
+
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation (m or in)
 REF_ORIGIN_MOMENT_X = -0.0028
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for moment non-dimensional coefficients (m or in)
 REF_LENGTH= 0.035
-%
-% Reference area for non-dimensional force coefficients (0 implies automatic
-% calculation) (m^2 or in^2)
 REF_AREA= 0.035
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= DIMENSIONAL
-%
+
 % ---- IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
-% Different gas model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS)
 FLUID_MODEL= STANDARD_AIR
-%
+
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= SUTHERLAND
-%
+
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
-% Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL).
 CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
-%
+
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
 TIME_DOMAIN=YES
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER,
-%                      DUAL_TIME_STEPPING-2ND_ORDER, HARMONIC_BALANCE)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-%
-% Time Step for dual time stepping simulations (s) -- Only used when UNST_CFL_NUMBER = 0.0
 TIME_STEP= 0.003
-%
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 1.0
 TIME_ITER = 9999
-%
-% Number of internal iterations (dual time method)
 INNER_ITER= 10
-%
-% Iteration number to begin unsteady restarts
 RESTART_ITER= 0
+
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
 DEFORM_MESH = YES
 MARKER_DEFORM_MESH = (plate)
-%
+
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes (no-slip), isothermal wall marker(s) (NONE = no marker)
-% Format: ( marker name, constant wall temperature (K), ... )
 MARKER_ISOTHERMAL= ( plate, 293 )
-%
-% Far-field boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
+
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( plate )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( plate )
-%
+
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% CFL number (initial value for the adaptive CFL number)
 CFL_NUMBER= 7.0
-%
+
 % ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
 %
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= NO
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
+
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-grid levels (0 = no multi-grid)
-MGLEVEL= 0
-%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
-%
-%
+
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
+
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, JACOBI)
 DEFORM_LINEAR_SOLVER_PREC= ILU
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 100
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                           WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= WALL_DISTANCE
-%
+
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= 2D_FlatPlate_Rounded.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency for physical time steps (dual time)
 OUTPUT_WRT_FREQ= 3
-%
-% Screen output
 SCREEN_OUTPUT= (TIME_ITER, INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG)
 HISTORY_OUTPUT=(ITER,RMS_RES,AERO_COEFF)
diff --git a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
index e71e06dae2e..efec4c79eb1 100755
--- a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
+++ b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
@@ -3,7 +3,7 @@
 ## \file flatPlate_rigidMotion.py
 #  \brief Python script to launch SU2_CFD with customized unsteady boundary conditions using the Python wrapper.
 #  \author David Thomas
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py b/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
index cfce7894757..d277a617fe7 100755
--- a/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
+++ b/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
@@ -3,7 +3,7 @@
 ## \file launch_unsteady_CHT_FlatPlate.py
 #  \brief Python script to launch SU2_CFD with customized unsteady boundary conditions using the Python wrapper.
 #  \author David Thomas
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/py_wrapper/flatPlate_unsteady_CHT/unsteady_CHT_FlatPlate_Conf.cfg b/TestCases/py_wrapper/flatPlate_unsteady_CHT/unsteady_CHT_FlatPlate_Conf.cfg
index d5b7a297eb8..a893d1f65bc 100644
--- a/TestCases/py_wrapper/flatPlate_unsteady_CHT/unsteady_CHT_FlatPlate_Conf.cfg
+++ b/TestCases/py_wrapper/flatPlate_unsteady_CHT/unsteady_CHT_FlatPlate_Conf.cfg
@@ -5,492 +5,197 @@
 % Author: David THOMAS                                                         %
 % Institution: University of Liège                                             %
 % Date: 12/12/2017                                                             %
-% File Version 7.4.0 "Blackbird"                                                   %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= RANS
-%
-% Specify turbulence model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SST
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-%
-% Axisymmetric simulation, only compressible flows (NO, YES)
 AXISYMMETRIC= NO
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% Discard the data storaged in the solution and geometry files
-% e.g. AOA, dCL/dAoA, dCD/dCL, iter, etc.
-% Note that AoA in the solution and geometry files is critical
-% to aero design using AoA as a variable. (NO, YES)
 DISCARD_INFILES= NO
-%
-% System of measurements (SI, US)
-% International system of units (SI): ( meters, kilograms, Kelvins,
-%                                       Newtons = kg m/s^2, Pascals = N/m^2, 
-%                                       Density = kg/m^3, Speed = m/s,
-%                                       Equiv. Area = m^2 )
-% United States customary units (US): ( inches, slug, Rankines, lbf = slug ft/s^2, 
-%                                       psf = lbf/ft^2, Density = slug/ft^3, 
-%                                       Speed = ft/s, Equiv. Area = ft^2 )
 SYSTEM_MEASUREMENTS= SI
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.03059
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Side-slip angle (degrees, only for compressible flows)
 SIDESLIP_ANGLE= 0.0
-%
-% Init option to choose between Reynolds (default) or thermodynamics quantities
-% for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= REYNOLDS
-%
-% Free-stream option to choose between density and temperature (default) for
-% initializing the solution (TEMPERATURE_FS, DENSITY_FS)
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-% Free-stream pressure (101325.0 N/m^2, 2116.216 psf by default)
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K, 518.67 R by default)
 FREESTREAM_TEMPERATURE= 293.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 24407.25244
-%
-% Reynolds length (1 m, 1 inch by default)
 REYNOLDS_LENGTH= 0.035
 
 % -------------------- INCOMPRESSIBLE FREE-STREAM DEFINITION ------------------%
 %
-% Free-stream density (1.2886 Kg/m^3, 0.0025 slug/ft^3 by default)
 FREESTREAM_DENSITY= 1.204
-%
-% Free-stream velocity (1.0 m/s, 1.0 ft/s by default)
 FREESTREAM_VELOCITY= ( 1.0, 0.00, 0.00 )
-%
-% Free-stream viscosity (1.853E-5 N s/m^2, 3.87E-7 lbf s/ft^2 by default)
 FREESTREAM_VISCOSITY= 1.82E-5
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation (m or in)
 REF_ORIGIN_MOMENT_X = -0.0028
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for moment non-dimensional coefficients (m or in)
 REF_LENGTH= 0.035
-%
-% Reference area for non-dimensional force coefficients (0 implies automatic
-% calculation) (m^2 or in^2)
 REF_AREA= 0.035
-%
-% Aircraft semi-span (0 implies automatic calculation) (m or in)
 SEMI_SPAN= 0.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= DIMENSIONAL
 
 % ---- IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
-% Different gas model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS)
 FLUID_MODEL= STANDARD_AIR
-%
-% Ratio of specific heats (1.4 default and the value is hardcoded
-%                          for the model STANDARD_AIR)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.058 J/kg*K default and this value is hardcoded
-%                        for the model STANDARD_AIR)
 GAS_CONSTANT= 287.058
-%
-% Critical Temperature (131.00 K by default)
 CRITICAL_TEMPERATURE= 131.00
-%
-% Critical Pressure (3588550.0 N/m^2 by default)
 CRITICAL_PRESSURE= 3588550.0
-%
-% Acentri factor (0.035 (air))
 ACENTRIC_FACTOR= 0.035
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= SUTHERLAND
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.716E-5
-%
-% Sutherland Viscosity Ref (1.716E-5 default value for AIR SI)
 MU_REF= 1.716E-5
-%
-% Sutherland Temperature Ref (273.15 K default value for AIR SI)
 MU_T_REF= 273.15
-%
-% Sutherland constant (110.4 default value for AIR SI)
 SUTHERLAND_CONSTANT= 110.4
 
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
-% Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL).
 CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
-%
-% Molecular Thermal Conductivity that would be constant (0.0257 by default)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.0257
 
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
 TIME_DOMAIN=YES
-%
 TIME_ITER= 10
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER,
-%                      DUAL_TIME_STEPPING-2ND_ORDER, HARMONIC_BALANCE)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-%
-% Time Step for dual time stepping simulations (s) -- Only used when UNST_CFL_NUMBER = 0.0
 TIME_STEP= 0.003
-%
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 1.0
-%
-% Unsteady Courant-Friedrichs-Lewy number of the finest grid
 UNST_CFL_NUMBER= 0.0
-%
-% Number of internal iterations (dual time method)
 INNER_ITER= 10
-%
-% Iteration number to begin unsteady restarts
 RESTART_ITER= 0
 
 % ----------------------- BODY FORCE DEFINITION -------------------------------%
 %
-% Apply a body force as a source term (NO, YES)
 BODY_FORCE= NO
-%
-% Vector of body force values (BodyForce_X, BodyForce_Y, BodyForce_Z)
 BODY_FORCE_VECTOR= ( 0.0, 0.0, 0.0 )
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( NONE )
-%
-% Navier-Stokes (no-slip), constant heat flux wall  marker(s) (NONE = no marker)
-% Format: ( marker name, constant heat flux (J/m^2), ... )
-%MARKER_HEATFLUX= ( plate, 1000.0 )
-%
-% Navier-Stokes (no-slip), isothermal wall marker(s) (NONE = no marker)
-% Format: ( marker name, constant wall temperature (K), ... )
 MARKER_ISOTHERMAL= ( plate, 293 )
-%
-% Far-field boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
+
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( plate )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( plate )
-%
-% Marker(s) of the surface where custom thermal BC's are defined.
 MARKER_PYTHON_CUSTOM = (plate)
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( NONE )
-%
-% Marker(s) of the surface that is going to be analyzed in detail (massflow, average pressure, distortion, etc)
 MARKER_ANALYZE = ( NONE )
-%
-% Method to compute the average value in MARKER_ANALYZE (AREA, MASSFLUX).
 MARKER_ANALYZE_AVERAGE = MASSFLUX
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% CFL number (initial value for the adaptive CFL number)
 CFL_NUMBER= 7.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.25, 50.0 )
-%
-% Maximum Delta Time in local time stepping simulations
 MAX_DELTA_TIME= 1E6
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE, 
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= DRAG
-%
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
 OBJECTIVE_WEIGHT = 1.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
 
 % ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
 %
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence adjoint equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJTURB= NO
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_ADJTURB= VENKATAKRISHNAN
-%
-% Coefficient for the Venkat's limiter (upwind scheme). A larger values decrease
-%             the extent of limiting, values approaching zero cause
-%             lower-order approximation to the solution (0.05 by default)
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Coefficient for the adjoint sharp edges limiter (3.0 by default).
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
-%
-% 1st order artificial dissipation coefficients for
-%     the Lax–Friedrichs method ( 0.15 by default )
 LAX_SENSOR_COEFF= 0.15
-%
-% 2nd and 4th order artificial dissipation coefficients for
-%     the JST method ( 0.5, 0.02 by default )
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% 1st order artificial dissipation coefficients for
-%     the adjoint Lax–Friedrichs method ( 0.15 by default )
 ADJ_LAX_SENSOR_COEFF= 0.15
-%
-% 2nd, and 4th order artificial dissipation coefficients for
-%     the adjoint JST method ( 0.5, 0.02 by default )
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-grid levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.75
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
-%
-% Relaxation coefficient
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
-%
-% Relaxation coefficient
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
 DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, JACOBI)
 DEFORM_LINEAR_SOLVER_PREC= ILU
-%
-% Number of smoothing iterations for mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 100
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Deformation coefficient (linear elasticity limits from -1.0 to 0.5, a larger
-% value is also possible)
 DEFORM_COEFF = 1E6
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                           WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= WALL_DISTANCE
-%
-% Deform the grid only close to the surface. It is possible to specify how much
-% of the volumetric grid is going to be deformed in meters or inches (1E6 by default)
 DEFORM_LIMIT = 1E6
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 4
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 10
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= 2D_FlatPlate_Rounded.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency for physical time steps (dual time)
 OUTPUT_WRT_FREQ= 3
-%
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= YES
-%
-% Screen output
 SCREEN_OUTPUT= (TIME_ITER, INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG)
diff --git a/TestCases/py_wrapper/translating_NACA0012/config.cfg b/TestCases/py_wrapper/translating_NACA0012/config.cfg
index 22b9f55cf83..8446a5405a1 100644
--- a/TestCases/py_wrapper/translating_NACA0012/config.cfg
+++ b/TestCases/py_wrapper/translating_NACA0012/config.cfg
@@ -73,4 +73,3 @@ MESH_FILENAME= ../../euler/naca0012/mesh_NACA0012_inv.su2
 MESH_FORMAT= SU2
 SCREEN_OUTPUT= (INNER_ITER, RMS_RES, LIFT, DRAG, MOMENT_X, MOMENT_Y, MOMENT_Z)
 HISTORY_OUTPUT= (INNER_ITER, RMS_RES, AERO_COEFF)
-
diff --git a/TestCases/radiation/p1adjoint/configp1adjoint.cfg b/TestCases/radiation/p1adjoint/configp1adjoint.cfg
index f737c5ad271..50f7a8d57df 100644
--- a/TestCases/radiation/p1adjoint/configp1adjoint.cfg
+++ b/TestCases/radiation/p1adjoint/configp1adjoint.cfg
@@ -4,7 +4,7 @@
 % Case description: Coupled CFD-RHT adjoint problem                            %
 % Author: Ruben Sanchez (TU Kaiserslautern)                                    %
 % Date: 2020-02-13                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/radiation/p1model/configp1.cfg b/TestCases/radiation/p1model/configp1.cfg
index 12871badc25..420953e2e05 100644
--- a/TestCases/radiation/p1model/configp1.cfg
+++ b/TestCases/radiation/p1model/configp1.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez                                                        %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern               %
 % Date: 2019-01-29                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -108,4 +108,3 @@ VOLUME_FILENAME= flow_p1
 
 TABULAR_FORMAT= CSV
 CONV_FILENAME= history_p1
-
diff --git a/TestCases/rans/actuatordisk_variable_load/propeller_variable_load.cfg b/TestCases/rans/actuatordisk_variable_load/propeller_variable_load.cfg
index 09d659ae553..aedbc71c2c7 100644
--- a/TestCases/rans/actuatordisk_variable_load/propeller_variable_load.cfg
+++ b/TestCases/rans/actuatordisk_variable_load/propeller_variable_load.cfg
@@ -8,226 +8,103 @@
 % Comments: Grid file and propeller data courtesy of Mauro Minervino,          %
 %           Centro Italiano Ricerche Aerospaziali (CIRA)                       %
 % Date: 07/08/2020                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 %----------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION -------------------------%
-% Solver type (EULER, NAVIER_STOKES, RANS,
-%              INC_EULER, INC_NAVIER_STOKES, INC_RANS
-%              FEM_EULER, FEM_NAVIER_STOKES, FEM_RANS, FEM_LES,
-%              HEAT_EQUATION_FVM, ELASTICITY)
-SOLVER= RANS
 %
-% Specify turbulence model (NONE, SA, SA_NEG, SST, SA_E, SA_COMP, SA_E_COMP)
+SOLVER= RANS
 KIND_TURB_MODEL= SA
-%
-% Turbulence intensity at freestream
 FREESTREAM_TURBULENCEINTENSITY=0.01
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% System of measurements (SI, US)
-% International system of units (SI): ( meters, kilograms, Kelvins,
-%                                       Newtons = kg m/s^2, Pascals = N/m^2, 
-%                                       Density = kg/m^3, Speed = m/s,
-%                                       Equiv. Area = m^2 )
 SYSTEM_MEASUREMENTS= SI
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.55996
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Side-slip angle (degrees, only for compressible flows)
 SIDESLIP_ANGLE= 0.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 3.65E7
-%
-% Reynolds length (1 m, 1 inch by default)
 REYNOLDS_LENGTH= 5.0292
-%
+
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
-% Reference origin for moment computation (m or in)
+%
 REF_ORIGIN_MOMENT_X = 0.0
 REF_ORIGIN_MOMENT_Y = 0.0
 REF_ORIGIN_MOMENT_Z = 0.0
-%
-% Reference length for moment non-dimensional coefficients (m or in)
 REF_LENGTH= 1.0
-%
-% Reference area for non-dimensional force coefficients (0 implies automatic
-% calculation) (m^2 or in^2)
 REF_AREA= 19.8649
-%
-% Compressible flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                                           FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= DIMENSIONAL
-%
+
 % --------------- ENGINE AND ACTUATOR DISK SIMULATION -------------------------%
-% Highlite area to compute MFR (1 in by default)
-HIGHLITE_AREA= 19.8649
 %
-% Engine nu factor (SA model).
+HIGHLITE_AREA= 19.8649
 ENGINE_NU_FACTOR= 0.0
-%
+
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
-ACTDISK_DOUBLE_SURFACE = YES
 %
-% Actuator disk boundary type (VARIABLE_LOAD, VARIABLES_JUMP, BC_THRUST,
-%                              DRAG_MINUS_THRUST)
+ACTDISK_DOUBLE_SURFACE = YES
 ACTDISK_TYPE= VARIABLE_LOAD
-%
-% Actuator disk data input file name
 ACTDISK_FILENAME= ActuatorDisk.dat
-%
-% Actuator disk boundary marker(s) with the following formats (NONE = no marker)
-% Variable Load: (inlet face marker, outlet face marker,
-%                 0.0, 0.0, 0.0, 0.0, 0.0, 0.0) Markers only effectively used.
 MARKER_ACTDISK = ( DISK, DISK_BACK, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0 )
-%
-% Far-field boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( FF )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Compressible: ( outlet marker, back pressure (static thermodynamic), ... )
 MARKER_OUTLET = ( OUT , 56370.2)
-%
-% Navier-Stokes (no-slip), constant heat flux wall  marker(s) (NONE = no marker)
-% Format: ( marker name, constant heat flux (J/m^2), ... )
 MARKER_HEATFLUX = (SPINNER, 0.0)
-%
+
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
-% Marker(s) of the surface in the surface flow solution file
-MARKER_PLOTTING = ( DISK, DISK_BACK, SPINNER )
 %
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
+MARKER_PLOTTING = ( DISK, DISK_BACK, SPINNER )
 MARKER_MONITORING = ( DISK, DISK_BACK, SPINNER )
-%
-% Marker(s) of the surface that is going to be analyzed in detail (massflow, average pressure, distortion, etc)
 MARKER_ANALYZE = ( DISK, DISK_BACK )
-%
-% Method to compute the average value in MARKER_ANALYZE (AREA, MASSFLUX).
 MARKER_ANALYZE_AVERAGE = MASSFLUX
-%
+
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
-NUM_METHOD_GRAD= GREEN_GAUSS
 %
-% CFL number (initial value for the adaptive CFL number)
+NUM_METHOD_GRAD= GREEN_GAUSS
 CFL_NUMBER= 20.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY, BUFFET,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE, 
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
 OBJECTIVE_FUNCTION= DRAG
-%
+
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
-% Linear solver or smoother for implicit formulations:
-% BCGSTAB, FGMRES, RESTARTED_FGMRES, CONJUGATE_GRADIENT (self-adjoint problems only), SMOOTHER.
-LINEAR_SOLVER= FGMRES
 %
-% Preconditioner of the Krylov linear solver or type of smoother (ILU, LU_SGS, LINELET, JACOBI)
+LINEAR_SOLVER= FGMRES
 LINEAR_SOLVER_PREC= ILU
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-12
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 3
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 1000
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
+
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, AUSMPLUSUP,
-%                              AUSMPLUSUP2, HLLC, TURKEL_PREC, MSW, FDS, SLAU, SLAU2)
-CONV_NUM_METHOD_FLOW= JST
 %
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
+CONV_NUM_METHOD_FLOW= JST
 TIME_DISCRE_FLOW= EULER_IMPLICIT
-%
+
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
-% Convective numerical method (SCALAR_UPWIND)
-CONV_NUM_METHOD_TURB= SCALAR_UPWIND
 %
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
+CONV_NUM_METHOD_TURB= SCALAR_UPWIND
 MUSCL_TURB= NO
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
+
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-% Maximum number of iterations
-ITER= 1500
 %
-% Min value of the residual (log10 of the residual)
+ITER= 1500
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
+
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= propeller_variable_load.su2
 %
-% Mesh input file format (SU2, CGNS)
+MESH_FILENAME= propeller_variable_load.su2
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
 TABULAR_FORMAT= TECPLOT
-%
-% Output file convergence history (w/o extension)
 CONV_FILENAME= history
-%
-% Write the forces breakdown file option (NO, YES)
 WRT_FORCES_BREAKDOWN= YES
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-%
-%
-%
-% Screen output fields
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_NU_TILDE, LIFT, DRAG)
diff --git a/TestCases/rans/flatplate/turb_SA_flatplate.cfg b/TestCases/rans/flatplate/turb_SA_flatplate.cfg
index 8eb6e387249..09608b4bed8 100644
--- a/TestCases/rans/flatplate/turb_SA_flatplate.cfg
+++ b/TestCases/rans/flatplate/turb_SA_flatplate.cfg
@@ -5,238 +5,106 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.10                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= RANS
-%
-% If Navier-Stokes, kind of turbulent model (NONE, SA)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.2
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 5000000.0
-%
-% Reynolds length (in meters)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 2.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( wall, 0.0 )
-%
-% Inlet boundary marker(s) (NONE = no marker) 
-% Format: ( inlet marker, total temperature, total pressure, flow_direction_x, 
-%           flow_direction_y, flow_direction_z, ... )
 MARKER_INLET= ( inlet, 302.4, 118309.784, 1.0, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure, ... )
 MARKER_OUTLET= ( outlet, 115056.0, farfield, 115056.0 )
-%
-% Symmetry boundary marker(s) (NONE = no marker)
 MARKER_SYM= ( symmetry )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( wall )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( wall )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 99999
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.1
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 2, 2, 2, 2)
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.8
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -15
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_flatplate_turb_137x97.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1000
-%
-%
-% Screen output fields
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_NU_TILDE, LIFT, DRAG)
diff --git a/TestCases/rans/flatplate/turb_SA_flatplate_species.cfg b/TestCases/rans/flatplate/turb_SA_flatplate_species.cfg
index e56b67c52ee..b92b30b0e6b 100644
--- a/TestCases/rans/flatplate/turb_SA_flatplate_species.cfg
+++ b/TestCases/rans/flatplate/turb_SA_flatplate_species.cfg
@@ -6,84 +6,45 @@
 % Author: T. Kattmann                                                          %
 % Institution: Bosch Thermotechmniek B.V.                                      %
 % Date: 2021.11.30                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= RANS
-%
-% If Navier-Stokes, kind of turbulent model (NONE, SA)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.2
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 5000000.0
-%
-% Reynolds length (in meters)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 2.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( wall, 0.0 )
-%
 SPECIFIED_INLET_PROFILE= YES
 INLET_FILENAME= inlet.dat
 INC_INLET_TYPE=  VELOCITY_INLET
-% Inlet boundary marker(s) (NONE = no marker) 
-% Format: ( inlet marker, total temperature, total pressure, flow_direction_x, 
-%           flow_direction_y, flow_direction_z, ... )
 MARKER_INLET= ( inlet, 302.4, 118309.784, 1.0, 0.0, 0.0 )
 MARKER_INLET_SPECIES= ( inlet, 1.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure, ... )
 MARKER_OUTLET= ( outlet, 115056.0, farfield, 115056.0 )
-%
-% Symmetry boundary marker(s) (NONE = no marker)
 MARKER_SYM= ( symmetry )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( wall )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( wall )
 
 % -------------------- SCALAR TRANSPORT ---------------------------------------%
@@ -91,132 +52,64 @@ MARKER_MONITORING= ( wall )
 KIND_SCALAR_MODEL= SPECIES_TRANSPORT
 DIFFUSIVITY_MODEL= CONSTANT_DIFFUSIVITY
 DIFFUSIVITY_CONSTANT= 0.001
-%
 CONV_NUM_METHOD_SPECIES= SCALAR_UPWIND
 MUSCL_SPECIES= NO
 SLOPE_LIMITER_SPECIES = NONE
-%
 TIME_DISCRE_SPECIES= EULER_IMPLICIT
-%
 SPECIES_INIT= 1.0
 SPECIES_CLIPPING= YES
 SPECIES_CLIPPING_MIN= 0.0
 SPECIES_CLIPPING_MAX= 1.0
-%
+
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 99999
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.1
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 2, 2, 2, 2)
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.8
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -15
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_flatplate_turb_137x97.su2
-%
 SCREEN_OUTPUT= INNER_ITER WALL_TIME \
                RMS_DENSITY RMS_MOMENTUM-X RMS_MOMENTUM-Y RMS_ENERGY RMS_TKE RMS_DISSIPATION RMS_SPECIES_0 \
                LINSOL_ITER LINSOL_RESIDUAL \
@@ -224,16 +117,13 @@ SCREEN_OUTPUT= INNER_ITER WALL_TIME \
                LINSOL_ITER_SPECIES LINSOL_RESIDUAL_SPECIES \
                SURFACE_SPECIES_0
 SCREEN_WRT_FREQ_INNER= 10
-%
 HISTORY_OUTPUT= ITER RMS_RES LINSOL SPECIES_COEFF SPECIES_COEFF_SURF
 CONV_FILENAME= history
 MARKER_ANALYZE= outlet
 MARKER_ANALYZE_AVERAGE= AREA
-%
 OUTPUT_FILES= RESTART_ASCII, PARAVIEW_MULTIBLOCK
 VOLUME_OUTPUT= RESIDUAL, PRIMITIVE
 OUTPUT_WRT_FREQ= 200
-%
 READ_BINARY_RESTART= NO
 RESTART_FILENAME= restart
 SOLUTION_FILENAME= solution
diff --git a/TestCases/rans/flatplate/turb_SST_flatplate.cfg b/TestCases/rans/flatplate/turb_SST_flatplate.cfg
index 81ffc3a7837..b2a905a9628 100644
--- a/TestCases/rans/flatplate/turb_SST_flatplate.cfg
+++ b/TestCases/rans/flatplate/turb_SST_flatplate.cfg
@@ -5,234 +5,104 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.10                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= RANS
-%
-% If Navier-Stokes, kind of turbulent model (NONE, SA)
 KIND_TURB_MODEL= SST
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.2
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 5000000.0
-%
-% Reynolds length (in meters)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 2.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( wall, 0.0 )
-%
-% Inlet boundary marker(s) (NONE = no marker) 
-% Format: ( inlet marker, total temperature, total pressure, flow_direction_x, 
-%           flow_direction_y, flow_direction_z, ... )
 MARKER_INLET= ( inlet, 302.4, 118309.784, 1.0, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure, ... )
 MARKER_OUTLET= ( outlet, 115056.0, farfield, 115056.0 )
-%
-% Symmetry boundary marker(s) (NONE = no marker)
 MARKER_SYM= ( symmetry )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( wall )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( wall )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 EXT_ITER= 99999
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.1
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 2, 2, 2, 2)
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.8
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -15
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_flatplate_turb_137x97.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1000
-%
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sa.cfg b/TestCases/rans/naca0012/turb_NACA0012_sa.cfg
index 050baad4de2..165d3252ef0 100644
--- a/TestCases/rans/naca0012/turb_NACA0012_sa.cfg
+++ b/TestCases/rans/naca0012/turb_NACA0012_sa.cfg
@@ -6,237 +6,100 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                             
 SOLVER= RANS
-%
-% Specify turbulence model
 KIND_TURB_MODEL= SA
 SA_OPTIONS= NEGATIVE, EXPERIMENTAL
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.15
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 10.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.0E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 NUM_METHOD_GRAD_RECON= LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1000.0
-%
-% Max Delta time
 MAX_DELTA_TIME= 1E10
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 ITER= 99999
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-10
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 1, 1, 1, 1, 1 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= NONE
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_TURB= NONE
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= n0012_225-65.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow_sa.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 10000
-%
-%
-% Screen output fields
 SCREEN_OUTPUT=(INNER_ITER, RMS_DENSITY, RMS_NU_TILDE, LIFT, DRAG, LINSOL_ITER, LINSOL_RESIDUAL, LINSOL_ITER_TURB, LINSOL_RESIDUAL_TURB, TOTAL_HEATFLUX)
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst.cfg
index b50c913304c..b7621b6de30 100644
--- a/TestCases/rans/naca0012/turb_NACA0012_sst.cfg
+++ b/TestCases/rans/naca0012/turb_NACA0012_sst.cfg
@@ -6,243 +6,104 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                             
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SST
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
-%
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.15
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 10.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.0E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 NUM_METHOD_GRAD_RECON= LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1000.0
-%
-% Max Delta time
 MAX_DELTA_TIME= 1E10
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 ITER= 99999
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-10
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 1, 1, 1, 1, 1 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= NONE
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= NONE
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
 % Convergence field
 CONV_FIELD= RMS_DENSITY
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= n0012_225-65.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow_sst.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 10000
-%
-%
-% Screen output fields
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG, LINSOL_RESIDUAL, TOTAL_HEATFLUX)
 OUTPUT_FILES= (RESTART_ASCII, PARAVIEW, SURFACE_PARAVIEW)
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_1994-KLm.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_1994-KLm.cfg
index 2359d135979..932af7b0d51 100644
--- a/TestCases/rans/naca0012/turb_NACA0012_sst_1994-KLm.cfg
+++ b/TestCases/rans/naca0012/turb_NACA0012_sst_1994-KLm.cfg
@@ -3,7 +3,7 @@
 % SU2 configuration file                                                       %
 % Case description: 2D NACA 0012 Airfoil Validation Case (compressible)        %
 %                   SST-1994-KLm implementation                                %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -105,4 +105,3 @@ SURFACE_ADJ_FILENAME= surface_adjoint
 OUTPUT_WRT_FREQ= 10000
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG, LINSOL_RESIDUAL)
 OUTPUT_FILES= (RESTART_ASCII, PARAVIEW, SURFACE_PARAVIEW)
-
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_2003-Vm.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_2003-Vm.cfg
index 499db596789..2f41d396a3f 100644
--- a/TestCases/rans/naca0012/turb_NACA0012_sst_2003-Vm.cfg
+++ b/TestCases/rans/naca0012/turb_NACA0012_sst_2003-Vm.cfg
@@ -3,7 +3,7 @@
 % SU2 configuration file                                                       %
 % Case description: 2D NACA 0012 Airfoil Validation Case (compressible)        %
 %                   SST-2003-Vm implementation                                 %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -105,4 +105,3 @@ SURFACE_ADJ_FILENAME= surface_adjoint
 OUTPUT_WRT_FREQ= 10000
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG, LINSOL_RESIDUAL)
 OUTPUT_FILES= (RESTART_ASCII, PARAVIEW, SURFACE_PARAVIEW)
-
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_2003m.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_2003m.cfg
index 75a59b5a55d..ac0e45ba793 100644
--- a/TestCases/rans/naca0012/turb_NACA0012_sst_2003m.cfg
+++ b/TestCases/rans/naca0012/turb_NACA0012_sst_2003m.cfg
@@ -1,7 +1,7 @@
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %                                                                              %
 % SU2 configuration file, NACA0012 RANS SST-2003m                              %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -90,5 +90,4 @@ RESTART_FILENAME= restart_flow.dat
 VOLUME_FILENAME= flow
 SURFACE_FILENAME= surface_flow
 OUTPUT_WRT_FREQ= 10000
-%
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG, LINSOL_RESIDUAL, TOTAL_HEATFLUX)
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_expliciteuler.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_expliciteuler.cfg
index dac10deebea..80442e62c3e 100644
--- a/TestCases/rans/naca0012/turb_NACA0012_sst_expliciteuler.cfg
+++ b/TestCases/rans/naca0012/turb_NACA0012_sst_expliciteuler.cfg
@@ -5,7 +5,7 @@
 % Author: Max Aehle                                                            %
 % Institution: TU Kaiserslautern                                               %
 % Date: Nov 17th, 2021                                                         %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -64,12 +64,9 @@ CONV_CAUCHY_EPS= 1E-6
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 MESH_FILENAME= n0012_113-33.su2
 MESH_FORMAT= SU2
-%
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG, LINSOL_RESIDUAL)
-%
 TABULAR_FORMAT= CSV
 CONV_FILENAME= history
-%
 OUTPUT_FILES= (RESTART_ASCII, PARAVIEW, SURFACE_PARAVIEW)
 OUTPUT_WRT_FREQ= 10000
 RESTART_FILENAME= restart_flow.dat
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_fixedvalues.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_fixedvalues.cfg
index ceef756604b..0754a8c889e 100644
--- a/TestCases/rans/naca0012/turb_NACA0012_sst_fixedvalues.cfg
+++ b/TestCases/rans/naca0012/turb_NACA0012_sst_fixedvalues.cfg
@@ -2,10 +2,10 @@
 %                                                                              %
 % SU2 configuration file                                                       %
 % Case description: upstream turbulence quantities fixed to far-field value    %
-% Author: Max Aehle
-% Institution: TU Kaiserslautern
+% Author: Max Aehle                                                            %
+% Institution: TU Kaiserslautern                                               %
 % Date: Mar 17th, 2021                                                         %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_multigrid_restart.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_multigrid_restart.cfg
index a70b68edaca..12908d73bb7 100644
--- a/TestCases/rans/naca0012/turb_NACA0012_sst_multigrid_restart.cfg
+++ b/TestCases/rans/naca0012/turb_NACA0012_sst_multigrid_restart.cfg
@@ -6,385 +6,151 @@
 % Author: David E. Manosalvas                                                  %
 % Institution: Stanford University                                             %
 % Date: 02.14.2017                                                             %
-% File Version 7.4.0 "Blackbird"                                                   %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               TNE2_EULER, TNE2_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= RANS
-%
-% Specify turbulence model (NONE, SA, SST)
 KIND_TURB_MODEL= SST
-%
-% Mathematical problem (DIRECT, ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
-%
-% Discard the data storaged in the solution and geometry files
-% e.g. AOA, dCL/dAoA, dCD/dCL, iter, etc.
-% Note that AoA in the solution and geometry files is critical
-% to aero design using AoA as a variable. (NO, YES)
 DISCARD_INFILES= YES
-%
-%
-% System of measurements (SI, US)
-% International system of units (SI): ( meters, kilograms, Kelvins,
-%                                       Newtons = kg m/s^2, Pascals = N/m^2, 
-%                                       Density = kg/m^3, Speed = m/s )
-% United States customary units (US): ( inches, slug, Rankines, lbf = slug ft/s^2, 
-%                                       psf = lbf/ft^2, Density = slug/ft^3, 
-%                                       Speed = ft/s )
 SYSTEM_MEASUREMENTS= SI
-%
-% Gravity force, only incompressible (NO, YES)
 GRAVITY_FORCE= NO
-%
-% Axisymmetric simulation, only compressible (NO, YES)
 AXISYMMETRIC= NO
-%
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.27
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Side-slip angle (degrees, only for compressible flows)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2, 2116.216 psf by default)
 FREESTREAM_PRESSURE= 97582.18
-%
-% Free-stream temperature (288.15 K, 518.67 R by default)
 FREESTREAM_TEMPERATURE= 283.8075
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 2000000
-%
-% Reynolds length (1 m, 1 inch by default)
 REYNOLDS_LENGTH= 0.3238
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 2.4761
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 0.1460
 % A = W*H = 0.3238*0.4509
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_VEL_EQ_ONE
-%
+
 % ---- IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
-% Different gas model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS)
 FLUID_MODEL= STANDARD_AIR
-%
-% Ratio of specific heats (1.4 default and the value is hardcoded
-%                          for the model STANDARD_AIR)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.058 J/kg*K default and this value is hardcoded 
-%                        for the model STANDARD_AIR)
 GAS_CONSTANT= 287.058
-%
-% Critical Temperature (131.00 K by default)
 CRITICAL_TEMPERATURE= 131.00
-%
-% Critical Pressure (3588550.0 N/m^2 by default)
 CRITICAL_PRESSURE= 3588550.0
-%
-% Critical Density (263.0 Kg/m3 by default)
 CRITICAL_DENSITY= 263.0
-%
-% Acentri factor (0.035 (air))
 ACENTRIC_FACTOR= 0.035
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= SUTHERLAND
-%
-% Laminar Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.716E-5
-%
-% Sutherland Viscosity Ref (1.716E-5 default value for AIR SI)
 MU_REF= 1.716E-5
-%
-% Sutherland Temperature Ref (273.15 K default value for AIR SI)
 MU_T_REF= 273.15
-%
-% Sutherland constant (110.4 default value for AIR SI)
 SUTHERLAND_CONSTANT= 110.4
+
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes (no-slip), constant heat flux wall  marker(s) (NONE = no marker)
-% Format: ( marker name, constant heat flux (J/m^2), ... )
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Far-field boundary marker(s) (NONE = no marker)
-%MARKER_FAR= ( inlet, outlet )
 MARKER_FAR= ( farfield )
-%
-% Symmetry boundary marker(s) (NONE = no marker)
-%MARKER_SYM= ( ground, windtunnel )
-%
-% Inlet boundary type (TOTAL_CONDITIONS, MASS_FLOW)
-INLET_TYPE= TOTAL_CONDITIONS
-%
-% Inlet boundary marker(s) with the following formats (NONE = no marker) 
-% Total Conditions: (inlet marker, total temp, total pressure, flow_direction_x, 
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-% Mass Flow: (inlet marker, density, velocity magnitude, flow_direction_x, 
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-%MARKER_INLET= ( inlet, 287.9454, 102653.2,1,0,0)
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
-%MARKER_OUTLET= ( outlet, 97786.1153 )
-%
+
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( airfoil )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( airfoil )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, AVG_TOTAL_PRESSURE, 
-%                                             MASS_FLOW_RATE)
 OBJECTIVE_FUNCTION= DRAG
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-grid levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.8
-%
+
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH_JESPERSEN)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Entropy fix coefficient (0.0 implies no entropy fixing)
 ENTROPY_FIX_COEFF= 0.0
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-%
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.8
-%
-% Limit value for the adjoint variable
 LIMIT_ADJFLOW= 1E6
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Number of total iterations
 ITER= 100
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 30
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 500
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= n0012_113-33.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow_sst_restart.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 500
-%
-% Uses two restart files and switches between them when writting restarts
-%WRT_FLIPFLOP_RESTART = YES
-%
-%
-% Screen output fields
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG)
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_sust.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_sust.cfg
index 54fccbf622a..93e0d01e582 100644
--- a/TestCases/rans/naca0012/turb_NACA0012_sst_sust.cfg
+++ b/TestCases/rans/naca0012/turb_NACA0012_sst_sust.cfg
@@ -6,197 +6,95 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                             
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SST
 SST_OPTIONS=(SUSTAINING)
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
-%
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.15
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 10.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.0E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
-%
-% Free-stream Turbulence Intensity, sqrt(2 k_inf/3)/U_inf (0.0005)
 FREESTREAM_TURBULENCEINTENSITY = 0.001
-%
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 0.1
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 NUM_METHOD_GRAD_RECON= LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1000.0
-%
-% Max Delta time
 MAX_DELTA_TIME= 1E10
-%
-% Number of total iterations
 ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-10
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= NONE
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
 % Convergence field
 CONV_FIELD= RMS_DENSITY
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= n0012_225-65.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow_sst_sust.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 10000
-%
-%
-% Screen output fields
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG, LINSOL_RESIDUAL)
 OUTPUT_FILES= (RESTART_ASCII, PARAVIEW, SURFACE_PARAVIEW)
diff --git a/TestCases/rans/oneram6/turb_ONERAM6.cfg b/TestCases/rans/oneram6/turb_ONERAM6.cfg
index 8ea64f25f0e..acdf3f83ee4 100644
--- a/TestCases/rans/oneram6/turb_ONERAM6.cfg
+++ b/TestCases/rans/oneram6/turb_ONERAM6.cfg
@@ -5,227 +5,97 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.14                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)          
 SOLVER= RANS
-%
-% Specify turbulence model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.8395
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 3.06
-%
-% Side-slip angle (degrees, only for compressible flows)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 11.72E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 0.64607
 
 % ---- IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
-% Different gas model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS)
 FLUID_MODEL= STANDARD_AIR
-%
-% Ratio of specific heats (1.4 default and the value is hardcoded
-%                          for the model STANDARD_AIR)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.058 J/kg*K default and this value is hardcoded 
-%                        for the model STANDARD_AIR)
 GAS_CONSTANT= 287.058
-%
-% Critical Temperature (131.00 K by default)
 CRITICAL_TEMPERATURE= 131.00
-%
-% Critical Pressure (3588550.0 N/m^2 by default)
 CRITICAL_PRESSURE= 3588550.0
-%
-% Critical Density (263.0 Kg/m3 by default)
 CRITICAL_DENSITY= 263.0
-%
-% Acentric factor (0.035 (air))
 ACENTRIC_FACTOR= 0.035
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= SUTHERLAND
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.716E-5
-%
-% Sutherland Viscosity Ref (1.716E-5 default value for AIR SI)
 MU_REF= 1.716E-5
-%
-% Sutherland Temperature Ref (273.15 K default value for AIR SI)
 MU_T_REF= 273.15
-%
-% Sutherland constant (110.4 default value for AIR SI)
 SUTHERLAND_CONSTANT= 110.4
 
-
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 0.64607
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( WING, 0.0 )
-%
-% Far-field boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( FARFIELD )
-%
-% Symmetry boundary marker(s) (NONE = no marker)
 MARKER_SYM= ( SYMMETRY )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( WING )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( WING )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 4.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 999999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (NONE, JACOBI, LINELET)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 2, 2 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 2, 2, 2, 2 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.7
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.7
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 1.0
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
@@ -234,53 +104,20 @@ CONV_CAUCHY_EPS= 1E-6
 PARMETIS_TOLERANCE= 0.05
 PARMETIS_EDGE_WEIGHT= 0
 PARMETIS_POINT_WEIGHT= 1
-%
-% Mesh input file
 MESH_FILENAME= mesh_ONERAM6_turb_hexa_43008.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 OUTPUT_FILES=(RESTART, STL_ASCII, PARAVIEW, SURFACE_PARAVIEW)
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-%
-% Screen output fields
 SCREEN_OUTPUT = (INNER_ITER, RMS_DENSITY, RMS_NU_TILDE, LIFT, DRAG, TOTAL_HEATFLUX)
diff --git a/TestCases/rans/oneram6/turb_ONERAM6_nk.cfg b/TestCases/rans/oneram6/turb_ONERAM6_nk.cfg
index e42f83fd2ed..f1267512326 100644
--- a/TestCases/rans/oneram6/turb_ONERAM6_nk.cfg
+++ b/TestCases/rans/oneram6/turb_ONERAM6_nk.cfg
@@ -2,7 +2,7 @@
 %                                                                              %
 % SU2 configuration file                                                       %
 % Case description: Turbulent flow, ONERA M6, Newton-Krylov solver             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -41,7 +41,7 @@ REF_DIMENSIONALIZATION= FREESTREAM_VEL_EQ_MACH
 TIME_DISCRE_FLOW= EULER_IMPLICIT % what else
 LINEAR_SOLVER_PREC= ILU % or LU_SGS
 
-% --- Things that don't ---
+% --- Things that don't matter ---
 MGLEVEL= 0 % NK replaces MG
 LINEAR_SOLVER= FGMRES % It will be FGMRES regardless
 
@@ -122,4 +122,3 @@ OUTPUT_FILES=(RESTART, PARAVIEW, SURFACE_PARAVIEW)
 OUTPUT_WRT_FREQ= 10000
 SCREEN_OUTPUT = (INNER_ITER, WALL_TIME, RMS_DENSITY, RMS_ENERGY, RMS_NU_TILDE, LIFT, DRAG, LINSOL_ITER, LINSOL_RESIDUAL, AVG_CFL)
 CONV_FILENAME= history
-
diff --git a/TestCases/rans/oneram6/turb_ONERAM6_vc.cfg b/TestCases/rans/oneram6/turb_ONERAM6_vc.cfg
new file mode 100644
index 00000000000..4bfe6dfbdf5
--- /dev/null
+++ b/TestCases/rans/oneram6/turb_ONERAM6_vc.cfg
@@ -0,0 +1,130 @@
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+%                                                                              %
+% SU2 configuration file                                                       %
+% Case description: Turbulent flow past the ONERA M6 wing                      %
+% Author: Thomas D. Economon                                                   %
+% Institution: Stanford University                                             %
+% Date: 2014.06.14                                                             %
+% File Version 7.5.0 "Blackbird"                                                %
+%                                                                              %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
+SOLVER= RANS
+KIND_TURB_MODEL= SA
+MATH_PROBLEM= DIRECT
+RESTART_SOL= NO
+
+% -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
+%
+MACH_NUMBER= 0.8395
+AOA= 3.06
+SIDESLIP_ANGLE= 0.0
+FREESTREAM_TEMPERATURE= 288.15
+REYNOLDS_NUMBER= 11.72E6
+REYNOLDS_LENGTH= 0.64607
+
+% --------------------------- VORTICITY_CONFINEMENT ---------------------------%
+%
+% Enable vorticity confinement (YES/NO)
+VORTICITY_CONFINEMENT = YES
+% Set confinement parameter (0.00 by default)
+CONFINEMENT_PARAM = 0.05
+
+% ---- IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
+%
+FLUID_MODEL= STANDARD_AIR
+GAMMA_VALUE= 1.4
+GAS_CONSTANT= 287.058
+CRITICAL_TEMPERATURE= 131.00
+CRITICAL_PRESSURE= 3588550.0
+CRITICAL_DENSITY= 263.0
+ACENTRIC_FACTOR= 0.035
+
+% --------------------------- VISCOSITY MODEL ---------------------------------%
+%
+VISCOSITY_MODEL= SUTHERLAND
+MU_CONSTANT= 1.716E-5
+MU_REF= 1.716E-5
+MU_T_REF= 273.15
+SUTHERLAND_CONSTANT= 110.4
+
+% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
+%
+REF_ORIGIN_MOMENT_X = 0.25
+REF_ORIGIN_MOMENT_Y = 0.00
+REF_ORIGIN_MOMENT_Z = 0.00
+REF_LENGTH= 0.64607
+REF_AREA= 0
+
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
+MARKER_HEATFLUX= ( WING, 0.0 )
+MARKER_FAR= ( FARFIELD )
+MARKER_SYM= ( SYMMETRY )
+MARKER_PLOTTING= ( WING )
+MARKER_MONITORING= ( WING )
+
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
+NUM_METHOD_GRAD= GREEN_GAUSS
+CFL_NUMBER= 4.0
+CFL_ADAPT= NO
+CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
+RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
+ITER= 20
+
+% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
+%
+LINEAR_SOLVER= FGMRES
+LINEAR_SOLVER_PREC= LU_SGS
+LINEAR_SOLVER_ERROR= 1E-4
+LINEAR_SOLVER_ITER= 5
+
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
+CONV_NUM_METHOD_FLOW= ROE
+MUSCL_FLOW= YES
+SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
+VENKAT_LIMITER_COEFF= 1.0
+JST_SENSOR_COEFF= ( 0.5, 0.02 )
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+
+% -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
+%
+CONV_NUM_METHOD_TURB= SCALAR_UPWIND
+MUSCL_TURB= NO
+SLOPE_LIMITER_TURB= VENKATAKRISHNAN
+TIME_DISCRE_TURB= EULER_IMPLICIT
+
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
+CONV_RESIDUAL_MINVAL= -10
+CONV_STARTITER= 10
+CONV_CAUCHY_ELEMS= 100
+CONV_CAUCHY_EPS= 1E-6
+
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+%
+% These settings are just to reproduce test results, comment them out
+% or delete them to use best practice values.
+PARMETIS_TOLERANCE= 0.05
+PARMETIS_EDGE_WEIGHT= 0
+PARMETIS_POINT_WEIGHT= 1
+MESH_FILENAME= mesh_ONERAM6_turb_hexa_43008.su2
+MESH_FORMAT= SU2
+MESH_OUT_FILENAME= mesh_out.su2
+SOLUTION_FILENAME= restart_flow.dat
+SOLUTION_ADJ_FILENAME= solution_adj.dat
+OUTPUT_FILES=(RESTART, STL_ASCII, PARAVIEW, SURFACE_PARAVIEW)
+TABULAR_FORMAT= CSV
+CONV_FILENAME= history
+RESTART_FILENAME= restart_flow.dat
+RESTART_ADJ_FILENAME= restart_adj.dat
+VOLUME_FILENAME= flow
+VOLUME_ADJ_FILENAME= adjoint
+GRAD_OBJFUNC_FILENAME= of_grad.dat
+SURFACE_FILENAME= surface_flow
+SURFACE_ADJ_FILENAME= surface_adjoint
+OUTPUT_WRT_FREQ= 250
+SCREEN_OUTPUT = (INNER_ITER, RMS_DENSITY, RMS_NU_TILDE, LIFT, DRAG, TOTAL_HEATFLUX)
diff --git a/TestCases/rans/propeller/propeller.cfg b/TestCases/rans/propeller/propeller.cfg
index b6ae7779a58..85c5de1b563 100644
--- a/TestCases/rans/propeller/propeller.cfg
+++ b/TestCases/rans/propeller/propeller.cfg
@@ -5,262 +5,106 @@
 % Author:                                                                      %
 % Institution:                                                                 %
 % Date:                                                                        %
-% File Version 7.4.0 "Blackbird"                                                   %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)
 SOLVER= RANS
-%
-% Specify turbulence model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
-% System of measurements (SI, US)
-% International system of units (SI): ( meters, kilograms, Kelvins,
-%                                       Newtons = kg m/s^2, Pascals = N/m^2, 
-%                                       Density = kg/m^3, Speed = m/s,
-%                                       Equiv. Area = m^2 )
-% United States customary units (US): ( inches, slug, Rankines, lbf = slug ft/s^2, 
-%                                       psf = lbf/ft^2, Density = slug/ft^3, 
-%                                       Speed = ft/s, Equiv. Area = ft^2 )
 SYSTEM_MEASUREMENTS= US
-%
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.3
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Side-slip angle (degrees, only for compressible flows)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream temperature (518.67 R by default)
 FREESTREAM_TEMPERATURE= 393.872
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 59847
-%
-% Reynolds length (1 in by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation (in)
 REF_ORIGIN_MOMENT_X = 0.0
 REF_ORIGIN_MOMENT_Y = 0.0
 REF_ORIGIN_MOMENT_Z = 0.0
-%
-% Reference length for pitching, rolling, and yawing non-dimensional
-% moment (in)
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic
-% calculation) (in^2)
 REF_AREA= 105120.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % --------------- ENGINE AND ACTUATOR DISK SIMULATION -------------------------%
 %
-% Highlite area to compute MFR (1 in by default)
 HIGHLITE_AREA= 1.0
-%
-% Engine nu factor (SA model).
 ENGINE_NU_FACTOR= 30.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier Stokes boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( INNER_NACELLE, 0.0, OUTER_NACELLE, 0.0)
-%
-% Actuator disk boundary type (VARIABLES_JUMP, NET_THRUST, BC_THRUST, 
-%                              DRAG_MINUS_THRUST, POWER)
 ACTDISK_TYPE= VARIABLES_JUMP
-%
-% Actuator disk jump definition using ratio or difference (DIFFERENCE, RATIO)
 ACTDISK_JUMP= DIFFERENCE
-%
-% Actuator disk boundary marker(s) with the following formats (NONE = no marker)
-% Variables Jump: ( inlet face marker, outlet face marker,
-%                   Takeoff pressure jump (psf), Takeoff temperature jump (R), Takeoff rev/min,
-%                   Cruise  pressure jump (psf), Cruise temperature jump (R), Cruise rev/min )
-% Net Thrust: ( inlet face marker, outlet face marker,
-%               Takeoff net thrust (lbs), 0.0, Takeoff rev/min,
-%               Cruise net thrust (lbs), 0.0, Cruise rev/min )
-% BC Thrust: ( inlet face marker, outlet face marker,
-%              Takeoff BC thrust (lbs), 0.0, Takeoff rev/min,
-%              Cruise BC thrust (lbs), 0.0, Cruise rev/min )
-% Drag-Thrust: ( inlet face marker, outlet face marker,
-%                Takeoff Drag-Thrust (lbs), 0.0, Takeoff rev/min,
-%                Cruise Drag-Thrust (lbs), 0.0, Cruise rev/min )
-% Power: ( inlet face marker, outlet face marker,
-%           Takeoff power (HP), 0.0, Takeoff rev/min
-%           Cruise power (HP), 0.0, Cruise rev/min )
 MARKER_ACTDISK = ( ACTDISK, ACTDISK_BACK, 70.5, 10, 0, 70.5, 10, 0 )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( FARFIELD )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( INNER_NACELLE, OUTER_NACELLE, ACTDISK, ACTDISK_BACK )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( INNER_NACELLE, OUTER_NACELLE, ACTDISK, ACTDISK_BACK )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( INNER_NACELLE, OUTER_NACELLE, ACTDISK, ACTDISK_BACK )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS 
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.0, 1.0, 1.0, 10.0 )
-%
-% Objective function in gradient evaluation  (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, AVG_TOTAL_PRESSURE, 
-%                                             MASS_FLOW_RATE)
 OBJECTIVE_FUNCTION= DRAG
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-12
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 3
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH_JESPERSEN)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
-%
-% Relaxation coefficient
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Relaxation coefficient
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Number of total iterations
 ITER= 9999
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= ActuatorDisk.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file with the forces breakdown
 BREAKDOWN_FILENAME= forces_breakdown.dat
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function
 VALUE_OBJFUNC_FILENAME= of_eval.dat
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1500
-%
-%
-% Screen output fields
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_NU_TILDE, LIFT, DRAG)
diff --git a/TestCases/rans/rae2822/turb_SA_RAE2822.cfg b/TestCases/rans/rae2822/turb_SA_RAE2822.cfg
index ead492a7ad8..4096f45b8fd 100644
--- a/TestCases/rans/rae2822/turb_SA_RAE2822.cfg
+++ b/TestCases/rans/rae2822/turb_SA_RAE2822.cfg
@@ -5,342 +5,122 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                        
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.729
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 2.31
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.5E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( AIRFOIL, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( FARFIELD )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( AIRFOIL )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( AIRFOIL )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 ITER= 99999
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= BCGSTAB
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.95
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.95
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE, TOTAL_HEAT,
-%                                     MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                     INVERSE_DESIGN_HEATFLUX)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.01 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.75
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Adjoint frozen viscosity (NO, YES)
 FROZEN_VISC_CONT= YES
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_RAE2822_turb.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-%
-% Screen output fields 
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_NU_TILDE, LIFT, DRAG, TOTAL_HEATFLUX)
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, PARABOLIC, NACA_4DIGITS, 
-%                      DISPLACEMENT, ROTATION, FFD_CONTROL_POINT, 
-%                      FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION, FFD_CAMBER, FFD_THICKNESS, FFD_VOLUME
-%                      SURFACE_FILE)
 DV_KIND= FFD_SETTING
-%
-% Marker of the surface to which we are going apply the shape deformation
 DV_MARKER= ( AIRFOIL )
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( Center, Thickness )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- OBSTACLE ( Center, Bump size )
-% 	- FFD_CONTROL_POINT ( FFD_BoxTag ID, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% 	- FFD_DIHEDRAL_ANGLE ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_TWIST_ANGLE ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_ROTATION ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% 	- FFD_CAMBER ( FFD_BoxTag ID, i_Ind, j_Ind )
-% 	- FFD_THICKNESS ( FFD_BoxTag ID, i_Ind, j_Ind )
-% 	- FFD_VOLUME ( FFD_BoxTag ID, i_Ind, j_Ind )
 DV_PARAM= ( 1, 0.5 )
-%
-% New value of the shape deformation
 DV_VALUE= 0.01
-%
-% Hold the grid fixed in a region (NO, YES)
 HOLD_GRID_FIXED= NO
-%
-% Coordinates of the box where the grid will be deformed (Xmin, Ymin, Zmin, 
-%                                                         Xmax, Ymax, Zmax)
 HOLD_GRID_FIXED_COORD= ( -0.5, -0.49, 0.0, 2.5, 0.49, 0.0 )
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-
-% Optimization objective function with optional scaling factor
-% ex= Objective * Scale
-OPT_OBJECTIVE= DRAG * 0.001
 
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= NONE
-
-% List of design variables (Design variables are separated by semicolons)
 DEFINITION_DV= ( 30, 1.0 | AIRFOIL | 0, 0.05 ); ( 30, 1.0 | AIRFOIL | 0, 0.10 ); ( 30, 1.0 | AIRFOIL | 0, 0.15 ); ( 30, 1.0 | AIRFOIL | 0, 0.20 ); ( 30, 1.0 | AIRFOIL | 0, 0.25 ); ( 30, 1.0 | AIRFOIL | 0, 0.30 ); ( 30, 1.0 | AIRFOIL | 0, 0.35 ); ( 30, 1.0 | AIRFOIL | 0, 0.40 ); ( 30, 1.0 | AIRFOIL | 0, 0.45 ); ( 30, 1.0 | AIRFOIL | 0, 0.50 ); ( 30, 1.0 | AIRFOIL | 0, 0.55 ); ( 30, 1.0 | AIRFOIL | 0, 0.60 ); ( 30, 1.0 | AIRFOIL | 0, 0.65 ); ( 30, 1.0 | AIRFOIL | 0, 0.70 ); ( 30, 1.0 | AIRFOIL | 0, 0.75 ); ( 30, 1.0 | AIRFOIL | 0, 0.80 ); ( 30, 1.0 | AIRFOIL | 0, 0.85 ); ( 30, 1.0 | AIRFOIL | 0, 0.90 ); ( 30, 1.0 | AIRFOIL | 0, 0.95 ); ( 30, 1.0 | AIRFOIL | 1, 0.05 ); ( 30, 1.0 | AIRFOIL | 1, 0.10 ); ( 30, 1.0 | AIRFOIL | 1, 0.15 ); ( 30, 1.0 | AIRFOIL | 1, 0.20 ); ( 30, 1.0 | AIRFOIL | 1, 0.25 ); ( 30, 1.0 | AIRFOIL | 1, 0.30 ); ( 30, 1.0 | AIRFOIL | 1, 0.35 ); ( 30, 1.0 | AIRFOIL | 1, 0.40 ); ( 30, 1.0 | AIRFOIL | 1, 0.45 ); ( 30, 1.0 | AIRFOIL | 1, 0.50 ); ( 30, 1.0 | AIRFOIL | 1, 0.55 ); ( 30, 1.0 | AIRFOIL | 1, 0.60 ); ( 30, 1.0 | AIRFOIL | 1, 0.65 ); ( 30, 1.0 | AIRFOIL | 1, 0.70 ); ( 30, 1.0 | AIRFOIL | 1, 0.75 ); ( 30, 1.0 | AIRFOIL | 1, 0.80 ); ( 30, 1.0 | AIRFOIL | 1, 0.85 ); ( 30, 1.0 | AIRFOIL | 1, 0.90 ); ( 30, 1.0 | AIRFOIL | 1, 0.95 )
-
diff --git a/TestCases/rans/rae2822/turb_SST_RAE2822.cfg b/TestCases/rans/rae2822/turb_SST_RAE2822.cfg
index c6381924789..29fe503e3d7 100644
--- a/TestCases/rans/rae2822/turb_SST_RAE2822.cfg
+++ b/TestCases/rans/rae2822/turb_SST_RAE2822.cfg
@@ -5,227 +5,101 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                          
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SST
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.729
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 2.31
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.5E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
-
-% Free-stream Turbulence Intensity
 FREESTREAM_TURBULENCEINTENSITY = 0.001
-
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( AIRFOIL, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( FARFIELD )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( AIRFOIL )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( AIRFOIL )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 ITER= 99999
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.95
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.95
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_RAE2822_turb.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-% Screen output fields
 SCREEN_OUTPUT = (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG, TOTAL_HEATFLUX)
-
diff --git a/TestCases/rans/rae2822/turb_SST_SUST_RAE2822.cfg b/TestCases/rans/rae2822/turb_SST_SUST_RAE2822.cfg
index 1e5487a0dc8..90cd5e7eea6 100644
--- a/TestCases/rans/rae2822/turb_SST_SUST_RAE2822.cfg
+++ b/TestCases/rans/rae2822/turb_SST_SUST_RAE2822.cfg
@@ -5,228 +5,102 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                          
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SST
 SST_OPTIONS=(SUSTAINING)
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.729
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 2.31
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.5E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
-
-% Free-stream Turbulence Intensity, sqrt(2 k_inf/3)/U_inf (0.0005)
 FREESTREAM_TURBULENCEINTENSITY = 0.001
-
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( AIRFOIL, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( FARFIELD )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( AIRFOIL )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( AIRFOIL )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 ITER= 99999
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.95
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.95
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
+
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_RAE2822_turb.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-% Screen output fields
 SCREEN_OUTPUT = (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG)
-
diff --git a/TestCases/rans/restart_directdiff_naca/naca0012.cfg b/TestCases/rans/restart_directdiff_naca/naca0012.cfg
index c96710af9a5..eb05427dce4 100644
--- a/TestCases/rans/restart_directdiff_naca/naca0012.cfg
+++ b/TestCases/rans/restart_directdiff_naca/naca0012.cfg
@@ -5,7 +5,7 @@
 % Author: Steffen Schotthöfer                                                  %
 % Institution: TU Kaiserslautern                                               %
 % Date: Mar 16, 2017                                                           %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -15,192 +15,118 @@
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES, NS_PLASMA)                    
 SOLVER= RANS
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DISCRETE_ADJOINT
-% Objective function
 OBJECTIVE_FUNCTION=DRAG
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-% Restart iteration
 RESTART_ITER = 10
 %
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Time Domain
 TIME_DOMAIN = YES
-% Unsteady simulation
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-% Time Step for dual time stepping simulations (s)
 TIME_STEP= 5e-4
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 105000
-%Maximum Number of physical time steps used for primal and ajoint run.
 TIME_ITER= 15
-% Number of internal iterations (dual time method)
 INNER_ITER= 2
-%Number of iterations to average the objective 
 ITER_AVERAGE_OBJ =  3      
-%Iteration number to begin the reverse time integration in the direct solver for the unsteady adjoint.
 UNST_ADJOINT_ITER = 15
-% Start iteration for windowing
 WINDOW_START_ITER = 12 
-% Window used for reverse sweep. Options (SQUARE, HANN, HANN_SQUARE, BUMP)
 WINDOW_FUNCTION = HANN_SQUARE
 %
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.3
-% Angle of attack (degrees, only for compressible flows)
 AOA= 17.0
-% De-Dimensionalization
 REF_DIMENSIONALIZATION = DIMENSIONAL
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 293.0
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 1e+6
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 %
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 %
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker
 MARKER_HEATFLUX= ( AIRFOIL, 0.0)
-% Farfield boundary marker
 MARKER_FAR= ( FARFIELD)
-% Internal boundary marker(s) e.g. no boundary condition 
 MARKER_INTERNAL= ( FWH1 )
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= (  AIRFOIL )
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= (AIRFOIL)
 %
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 20.0
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 %
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method 
 CONV_NUM_METHOD_FLOW= JST
-% 1st, 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= (  0.5, 0.01 )
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-% Muscl flow for turbulent simulation
 MUSCL_TURB= NO
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 %
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Field to apply Cauchy Criterion to
 CONV_FIELD= REL_RMS_DENSITY
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -9
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 10
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-5
 %
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Output settings
 HISTORY_WRT_FREQ_INNER=0
 SCREEN_WRT_FREQ_INNER =1
 SCREEN_OUTPUT=(INNER_ITER, TIME_ITER, RMS_ADJ_DENSITY, RMS_DENSITY, , REL_RMS_DENSITY,REL_RMS_ADJ_DENSITY, DRAG, TAVG_DRAG)
 HISTORY_OUTPUT=(D_AERO_COEFF,D_TAVG_AERO_COEFF)
-%
-% Mesh input file
 MESH_FILENAME= naca0012_FFD.su2
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= restart_adj.dat
 TABULAR_FORMAT= CSV
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= 0_history
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1
 %
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation 
 DV_KIND= FFD_CONTROL_POINT_2D
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( AIRFOIL )
-% Parameters of the shape deformation
 DV_PARAM= ( AIRFOIL_BOX, 0.0, 0.0, 1.0, 0.0)
-% Value of the shape deformation
 DV_VALUE= 0.01
-% Surface deformation input filename (SURFACE_FILE DV only)
 DV_FILENAME= mesh_motion.dat
 %
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Number of smoothing iterations for FEA mesh deformation
 DEFORM_LINEAR_SOLVER_ITER= 1000
-% Number of nonlinear deformation iterations (surface deformation increments)
 DEFORM_NONLINEAR_ITER= 1
-% Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
-% Factor to multiply smallest cell volume for deform tolerance (0.001 default)
 DEFORM_LINEAR_SOLVER_ERROR =  1E-6
-% Type of element stiffness imposed for FEA mesh deformation
 DEFORM_STIFFNESS_TYPE= WALL_DISTANCE
-% Optimization objective function with scaling factor
 OPT_OBJECTIVE= DRAG * 1.0
 OPT_GRADIENT_FACTOR= 0.1
 OPT_RELAX_FACTOR= 1
 OPT_BOUND_UPPER= 0.05
 OPT_BOUND_LOWER= -0.05
-% Optimization constraint functions with scaling factors, separated by semicolons
 OPT_CONSTRAINT= ( LIFT > 0.96 ) * 1.0
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 19, 1.0 | AIRFOIL | AIRFOIL_BOX, 0, 0, 1.0, 0.0 ); 
-%
diff --git a/TestCases/rans/s809/trans_s809.cfg b/TestCases/rans/s809/trans_s809.cfg
index 532368f971f..ae025dbee38 100644
--- a/TestCases/rans/s809/trans_s809.cfg
+++ b/TestCases/rans/s809/trans_s809.cfg
@@ -5,228 +5,103 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
 KIND_TRANS_MODEL = LM
 FREESTREAM_INTERMITTENCY = 0.9
 FREESTREAM_TURBULENCEINTENSITY = 0.04
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.1
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 2.0E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( wall, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( inlet,outlet )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( wall )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( wall )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 EXT_ITER= 999999
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.95
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.95
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= s809_2e6.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= trans_mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= trans_solution_flow.dat
-%
-% Restart linear flow input file
 SOLUTION_LIN_FILENAME= trans_solution_lin.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= trans_solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= trans_history
-%
-% Output file restart flow
 RESTART_FILENAME= trans_restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= trans_restart_adj.dat
-%
-% Output file linear flow
 RESTART_LIN_FILENAME= trans_restart_lin.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= trans_flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= trans_adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= trans_of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= trans_surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= trans_surface_adjoint
-%
-% Output file surface linear coefficient (w/o extension)
 SURFACE_LIN_FILENAME= trans_surface_linear
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1000
-%
diff --git a/TestCases/rans/s809/turb_S809.cfg b/TestCases/rans/s809/turb_S809.cfg
index c540294e3b5..85ee14df6b4 100644
--- a/TestCases/rans/s809/turb_S809.cfg
+++ b/TestCases/rans/s809/turb_S809.cfg
@@ -5,234 +5,94 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                   
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.1
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 2.0E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_VEL_EQ_ONE
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( wall, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( inlet, outlet )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( wall )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( wall )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 EXT_ITER= 99999
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.95
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.95
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= s809_2e6.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1000
-%
diff --git a/TestCases/rans/vki_turbine/turb_vki.cfg b/TestCases/rans/vki_turbine/turb_vki.cfg
index e13513523f0..29623e5d410 100644
--- a/TestCases/rans/vki_turbine/turb_vki.cfg
+++ b/TestCases/rans/vki_turbine/turb_vki.cfg
@@ -5,240 +5,92 @@
 % Author: Francisco Palacios, Thomas D. Economon	                           %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                         
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.5
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 350.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.0E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_VEL_EQ_ONE
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Inlet boundary type (TOTAL_CONDITIONS, MASS_FLOW)
 INLET_TYPE= TOTAL_CONDITIONS
-%
-% Inlet boundary marker(s) with the following formats (NONE = no marker) 
-% Total Conditions: (inlet marker, total temp, total pressure, flow_direction_x, 
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-% Mass Flow: (inlet marker, density, velocity magnitude, flow_direction_x, 
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
 MARKER_INLET= ( inflow, 404.1, 0.904E+05, 1.0, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
 MARKER_OUTLET= ( outflow, 0.523E+05 )
-%
-% Periodic boundary marker(s) (NONE = no marker)
-% Format: ( periodic marker, donor marker, rotation_center_x, rotation_center_y, 
-% rotation_center_z, rotation_angle_x-axis, rotation_angle_y-axis, 
-% rotation_angle_z-axis, translation_x, translation_y, translation_z, ... )
 MARKER_PERIODIC= ( periodic_1, periodic_2, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, -0.05749995, 0.0 )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 EXT_ITER= 10
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_vki_turbine_prepbc.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1000
-%
diff --git a/TestCases/rans_uq/naca0012/turb_NACA0012_uq.cfg b/TestCases/rans_uq/naca0012/turb_NACA0012_uq.cfg
index 29b51e13033..4f673d95938 100644
--- a/TestCases/rans_uq/naca0012/turb_NACA0012_uq.cfg
+++ b/TestCases/rans_uq/naca0012/turb_NACA0012_uq.cfg
@@ -6,231 +6,97 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                             
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SST
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
-%
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.15
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 15.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.0E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Max Delta time
 MAX_DELTA_TIME= 1E10
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= YES
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 0.1, 1.2, 10.0, 100.0 )
-%
-% Number of total iterations
 EXT_ITER= 10
+
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 0.05
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 1, 1, 1, 1, 1 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -9
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-5
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_n0012_225-65.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow_sst.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 10000
-%
diff --git a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_1c.cfg b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_1c.cfg
index da8ba37a00d..cec5aba98aa 100644
--- a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_1c.cfg
+++ b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_1c.cfg
@@ -6,48 +6,28 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                             
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SST
-%
-% Using uncertainty quantification module.
 SST_OPTIONS= (UQ)
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.15
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 15.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.0E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ------------------- UNCERTAINTY QUANTIFICATION DEFINITION -------------------%
 %
-
 % Eigenvalue perturbation definition (1, 2, or 3)
 UQ_COMPONENT= 1
 %
@@ -62,195 +42,77 @@ UQ_DELTA_B= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Max Delta time
 MAX_DELTA_TIME= 1E10
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= YES
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 0.1, 1.2, 10.0, 100.0 )
-%
-% Number of total iterations
 ITER= 99999
+
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 0.05
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 1, 1, 1, 1, 1 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -9
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-5
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_n0012_225-65.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 10000
-%
-%
-% Screen output 
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG
-
diff --git a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_2c.cfg b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_2c.cfg
index cf7381b4147..64e099c2e79 100644
--- a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_2c.cfg
+++ b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_2c.cfg
@@ -6,43 +6,24 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                             
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SST
-%
-% Using uncertainty quantification module.
 SST_OPTIONS= (UQ)
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.15
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 15.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.0E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ------------------- UNCERTAINTY QUANTIFICATION DEFINITION -------------------%
@@ -61,194 +42,76 @@ UQ_DELTA_B= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Max Delta time
 MAX_DELTA_TIME= 1E10
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= YES
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 0.1, 1.2, 10.0, 100.0 )
-%
-% Number of total iterations
 ITER= 99999
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 0.05
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 1, 1, 1, 1, 1 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -9
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-5
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_n0012_225-65.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 10000
-%
-%
-% Screen output 
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG
diff --git a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_3c.cfg b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_3c.cfg
index 689d9ab4e27..549a4d13c11 100644
--- a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_3c.cfg
+++ b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_3c.cfg
@@ -6,43 +6,24 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                             
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SST
-%
-% Using uncertainty quantification module.
 SST_OPTIONS= (UQ)
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.15
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 15.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.0E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ------------------- UNCERTAINTY QUANTIFICATION DEFINITION -------------------%
@@ -61,194 +42,79 @@ UQ_DELTA_B= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Max Delta time
 MAX_DELTA_TIME= 1E10
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= YES
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 0.1, 1.2, 10.0, 100.0 )
-%
-% Number of total iterations
 ITER= 99999
+
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 0.05
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 1, 1, 1, 1, 1 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -9
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-5
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_n0012_225-65.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 10000
-%
-%
-% Screen output 
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG
diff --git a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c1.cfg b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c1.cfg
index 0c0b071b737..67f7e5b1386 100644
--- a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c1.cfg
+++ b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c1.cfg
@@ -6,43 +6,24 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
-%
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                             
+%                            
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SST
-%
-% Using uncertainty quantification module.
 SST_OPTIONS= (UQ)
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.15
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 15.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.0E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ------------------- UNCERTAINTY QUANTIFICATION DEFINITION -------------------%
@@ -61,194 +42,79 @@ UQ_DELTA_B= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Max Delta time
 MAX_DELTA_TIME= 1E10
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= YES
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 0.1, 1.2, 10.0, 100.0 )
-%
-% Number of total iterations
 ITER= 99999
+
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 0.05
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 1, 1, 1, 1, 1 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -9
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-5
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_n0012_225-65.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 10000
-%
-%
-% Screen output 
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG)
diff --git a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c2.cfg b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c2.cfg
index e4ebef58581..bc626d93cd5 100644
--- a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c2.cfg
+++ b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c2.cfg
@@ -6,43 +6,24 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                             
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SST
-%
-% Using uncertainty quantification module. 
 SST_OPTIONS= (UQ)
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.15
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 15.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 300.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.0E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ------------------- UNCERTAINTY QUANTIFICATION DEFINITION -------------------%
@@ -61,194 +42,79 @@ UQ_DELTA_B= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Max Delta time
 MAX_DELTA_TIME= 1E10
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= YES
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 0.1, 1.2, 10.0, 100.0 )
-%
-% Number of total iterations
 ITER= 99999
+
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 0.05
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 1, 1, 1, 1, 1 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -9
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-5
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_n0012_225-65.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 10000
-%
-%
-% Screen output 
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG
diff --git a/TestCases/rotating/caradonna_tung/rot_caradonna_tung.cfg b/TestCases/rotating/caradonna_tung/rot_caradonna_tung.cfg
index 72df1fab415..57c1c1c7039 100644
--- a/TestCases/rotating/caradonna_tung/rot_caradonna_tung.cfg
+++ b/TestCases/rotating/caradonna_tung/rot_caradonna_tung.cfg
@@ -5,223 +5,104 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2020.05.24                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.0
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Type of dynamic mesh (NONE, RIGID_MOTION, DEFORMING, ROTATING_FRAME,
-%                       MOVING_WALL, AEROELASTIC, EXTERNAL)
 GRID_MOVEMENT= ROTATING_FRAME
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.877
-%
-% Coordinates of the motion origin
 MOTION_ORIGIN= 0.0 0.0 0.0
-%
-% Angular velocity vector (rad/s) about the motion origin
 ROTATION_RATE = 261.79938779914943 0.0 0.0
 % 1250 RPM -> 130.89969389957471
 % 2500 RPM -> 261.79938779914943
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Marker of the Euler boundary (NONE = no marker)
 MARKER_EULER= ( blade_1, blade_2 )
-%
-% Marker of the far field (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker of the surface which is going to be plotted or designed
 MARKER_PLOTTING= ( blade_1, blade_2 )
-%
-% Marker of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( blade_1, blade_2 )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1e3
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 0.1, 2.0, 15, 1e6 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= ILU
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-10
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.9
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.9
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-10
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_caradonna_tung.su2
-%
-% Mesh input file format (CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_caradonna_tung_periodic.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 100
-%
-
 SCREEN_OUTPUT=(INNER_ITER, WALL_TIME, RMS_DENSITY, LIFT, DRAG, AVG_CFL)
diff --git a/TestCases/rotating/naca0012/rot_NACA0012.cfg b/TestCases/rotating/naca0012/rot_NACA0012.cfg
index 69b6b2ad682..7774c3ef13e 100644
--- a/TestCases/rotating/naca0012/rot_NACA0012.cfg
+++ b/TestCases/rotating/naca0012/rot_NACA0012.cfg
@@ -5,368 +5,140 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2020.06.06                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.0
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Type of dynamic mesh (NONE, RIGID_MOTION, DEFORMING, ROTATING_FRAME,
-%                       MOVING_WALL, AEROELASTIC, EXTERNAL)
 GRID_MOVEMENT= ROTATING_FRAME
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.7958
-%
-% Coordinates of the motion origin
 MOTION_ORIGIN= 0.5 -32.0 0.0
-%
-% Angular velocity vector (rad/s) about the motion origin
 ROTATION_RATE = 0.0 0.0 8.25
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( airfoil )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( airfoil )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1e4
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 ITER= 9999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.95
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.95
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, 
-%                                     TORQUE, FREE_SURFACE, TOTAL_HEAT,
-%                                     MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                     INVERSE_DESIGN_HEATFLUX)
-OBJECTIVE_FUNCTION= DRAG
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
+OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.8
-%
-% Limit value for the adjoint variable
 LIMIT_ADJFLOW= 1E6
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
-%
-% Sensitivity smoothing (NONE, SOBOLEV, BIGRID)
 SENS_SMOOTHING= NONE
-%
-% Adjoint frozen viscosity (NO, YES)
 FROZEN_VISC_CONT= YES
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, PARABOLIC,  
-%                      NACA_4DIGITS, DISPLACEMENT, ROTATION, FFD_CONTROL_POINT, 
-%                      FFD_NACELLE, FFD_TWIST, FFD_ROTATION,
-%                      FFD_CAMBER, FFD_THICKNESS, FFD_VOLUME, SURFACE_FILE)
 DV_KIND= HICKS_HENNE
-%
-% Marker of the surface in which we are going apply the shape deformation
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation 
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - FOURIER ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), index, cos(0)/sin(1) )
-% - SPHERICAL ( ControlPoint_Index, Theta_Disp, R_Disp )
-% - NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% - PARABOLIC ( Center, Thickness )
-% - DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - OBSTACLE ( Center, Bump size )
-% - FFD_CONTROL_POINT ( FFD_BoxTag ID, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_DIHEDRAL_ANGLE ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_TWIST_ANGLE ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_ROTATION ( FFD_BoxTag ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CAMBER ( FFD_BoxTag ID, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag ID, i_Ind, j_Ind )
-% - FFD_VOLUME ( FFD_BoxTag ID, i_Ind, j_Ind )
 DV_PARAM= ( 1, 0.5 )
-%
-% Value of the shape deformation
 DV_VALUE= 0.01
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
-% Hold the grid fixed in a region (NO, YES)
 HOLD_GRID_FIXED= NO
-%
-% Coordinates of the box where the grid will be deformed (Xmin, Ymin, Zmin, 
-%                                                         Xmax, Ymax, Zmax)
-% HOLD_GRID_FIXED_COORD= ( -0.5, -0.49, 0.0, 2.5, 0.49, 0.0 )
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
 CONV_FIELD= RMS_DENSITY
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 SCREEN_OUTPUT=(INNER_ITER, WALL_TIME, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA0012_rot.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1
-%
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.01
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= ( AIRFOIL_THICKNESS > 0.12 ) * 0.01 ;
-%
-% Optimization design variables, separated by semicolons
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.961538461538 ); ( 30, 1.0 | airfoil | 0, 0.923076923077 ); ( 30, 1.0 | airfoil | 0, 0.884615384615 ); ( 30, 1.0 | airfoil | 0, 0.846153846154 ); ( 30, 1.0 | airfoil | 0, 0.807692307692 ); ( 30, 1.0 | airfoil | 0, 0.769230769231 ); ( 30, 1.0 | airfoil | 0, 0.730769230769 ); ( 30, 1.0 | airfoil | 0, 0.692307692308 ); ( 30, 1.0 | airfoil | 0, 0.653846153846 ); ( 30, 1.0 | airfoil | 0, 0.615384615385 ); ( 30, 1.0 | airfoil | 0, 0.576923076923 ); ( 30, 1.0 | airfoil | 0, 0.538461538462 ); ( 30, 1.0 | airfoil | 0, 0.5 ); ( 30, 1.0 | airfoil | 0, 0.461538461538 ); ( 30, 1.0 | airfoil | 0, 0.423076923077 ); ( 30, 1.0 | airfoil | 0, 0.384615384615 ); ( 30, 1.0 | airfoil | 0, 0.346153846154 ); ( 30, 1.0 | airfoil | 0, 0.307692307692 ); ( 30, 1.0 | airfoil | 0, 0.269230769231 ); ( 30, 1.0 | airfoil | 0, 0.230769230769 ); ( 30, 1.0 | airfoil | 0, 0.192307692308 ); ( 30, 1.0 | airfoil | 0, 0.153846153846 ); ( 30, 1.0 | airfoil | 0, 0.115384615385 ); ( 30, 1.0 | airfoil | 0, 0.0769230769231 ); ( 30, 1.0 | airfoil | 0, 0.0384615384615 ); ( 30, 1.0 | airfoil | 1, 0.0384615384615 ); ( 30, 1.0 | airfoil | 1, 0.0769230769231 ); ( 30, 1.0 | airfoil | 1, 0.115384615385 ); ( 30, 1.0 | airfoil | 1, 0.153846153846 ); ( 30, 1.0 | airfoil | 1, 0.192307692308 ); ( 30, 1.0 | airfoil | 1, 0.230769230769 ); ( 30, 1.0 | airfoil | 1, 0.269230769231 ); ( 30, 1.0 | airfoil | 1, 0.307692307692 ); ( 30, 1.0 | airfoil | 1, 0.346153846154 ); ( 30, 1.0 | airfoil | 1, 0.384615384615 ); ( 30, 1.0 | airfoil | 1, 0.423076923077 ); ( 30, 1.0 | airfoil | 1, 0.461538461538 ); ( 30, 1.0 | airfoil | 1, 0.5 ); ( 30, 1.0 | airfoil | 1, 0.538461538462 ); ( 30, 1.0 | airfoil | 1, 0.576923076923 ); ( 30, 1.0 | airfoil | 1, 0.615384615385 ); ( 30, 1.0 | airfoil | 1, 0.653846153846 ); ( 30, 1.0 | airfoil | 1, 0.692307692308 ); ( 30, 1.0 | airfoil | 1, 0.730769230769 ); ( 30, 1.0 | airfoil | 1, 0.769230769231 ); ( 30, 1.0 | airfoil | 1, 0.807692307692 ); ( 30, 1.0 | airfoil | 1, 0.846153846154 ); ( 30, 1.0 | airfoil | 1, 0.884615384615 ); ( 30, 1.0 | airfoil | 1, 0.923076923077 ); ( 30, 1.0 | airfoil | 1, 0.961538461538 )
diff --git a/TestCases/serial_regression.py b/TestCases/serial_regression.py
index 14181589898..9ff934437db 100644
--- a/TestCases/serial_regression.py
+++ b/TestCases/serial_regression.py
@@ -3,7 +3,7 @@
 ## \file serial_regression.py
 #  \brief Python script for automated regression testing of SU2 examples
 #  \author A. Aranake, A. Campos, T. Economon, T. Lukaczyk, S. Padron
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 #
@@ -1132,7 +1132,7 @@ def main():
     airfoilRBF.cfg_dir   = "fea_fsi/Airfoil_RBF"
     airfoilRBF.cfg_file  = "config.cfg"
     airfoilRBF.test_iter = 1
-    airfoilRBF.test_vals = [1.000000, -2.786185, -4.977948]
+    airfoilRBF.test_vals = [1.000000, -2.786183, -4.977959]
     airfoilRBF.multizone = True
     test_list.append(airfoilRBF)
 
diff --git a/TestCases/serial_regression_AD.py b/TestCases/serial_regression_AD.py
index 70ac8135c4d..092c102d191 100644
--- a/TestCases/serial_regression_AD.py
+++ b/TestCases/serial_regression_AD.py
@@ -3,11 +3,11 @@
 ## \file serial_regression.py
 #  \brief Python script for automated regression testing of SU2 examples
 #  \author A. Aranake, A. Campos, T. Economon, T. Lukaczyk, S. Padron
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
-# 
-# The SU2 Project is maintained by the SU2 Foundation 
+#
+# The SU2 Project is maintained by the SU2 Foundation
 # (http://su2foundation.org)
 #
 # Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
@@ -16,7 +16,7 @@
 # modify it under the terms of the GNU Lesser General Public
 # License as published by the Free Software Foundation; either
 # version 2.1 of the License, or (at your option) any later version.
-# 
+#
 # SU2 is distributed in the hope that it will be useful,
 # but WITHOUT ANY WARRANTY; without even the implied warranty of
 # MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
@@ -32,8 +32,8 @@
 from TestCase import TestCase
 
 def main():
-    '''This program runs SU2 and ensures that the output matches specified values. 
-       This will be used to do checks when code is pushed to github 
+    '''This program runs SU2 and ensures that the output matches specified values.
+       This will be used to do checks when code is pushed to github
        to make sure nothing is broken. '''
 
     test_list = []
@@ -58,7 +58,7 @@ def main():
     discadj_cylinder3D.test_vals = [-3.737675, -3.842311, -0.000000, 0.000000]
     test_list.append(discadj_cylinder3D)
 
-    # Arina nozzle 2D  
+    # Arina nozzle 2D
     discadj_arina2k              = TestCase('discadj_arina2k')
     discadj_arina2k.cfg_dir      = "disc_adj_euler/arina2k"
     discadj_arina2k.cfg_file     = "Arina2KRS.cfg"
@@ -69,7 +69,7 @@ def main():
     #######################################################
     ### Disc. adj. compressible RANS                    ###
     #######################################################
-    
+
     # Adjoint turbulent NACA0012 SA
     discadj_rans_naca0012_sa           = TestCase('discadj_rans_naca0012_sa')
     discadj_rans_naca0012_sa.cfg_dir   = "disc_adj_rans/naca0012"
@@ -133,16 +133,16 @@ def main():
     #######################################################
     ### Unsteady Disc. adj. compressible RANS           ###
     #######################################################
-   
+
     # Turbulent Cylinder
     discadj_cylinder           = TestCase('unsteady_cylinder')
     discadj_cylinder.cfg_dir   = "disc_adj_rans/cylinder"
-    discadj_cylinder.cfg_file  = "cylinder.cfg" 
+    discadj_cylinder.cfg_file  = "cylinder.cfg"
     discadj_cylinder.test_iter = 9
     discadj_cylinder.test_vals = [3.746909, -1.544883, -0.008321, 0.000014] #last 4 columns
     discadj_cylinder.unsteady  = True
     test_list.append(discadj_cylinder)
-    
+
     ##########################################################################
     ### Unsteady Disc. adj. compressible RANS DualTimeStepping 1st order   ###
     ##########################################################################
@@ -181,15 +181,15 @@ def main():
     ###################################
     ### Structural Adjoint          ###
     ###################################
-   
+
     # Structural model
     discadj_fea           = TestCase('discadj_fea')
     discadj_fea.cfg_dir   = "disc_adj_fea"
-    discadj_fea.cfg_file  = "configAD_fem.cfg" 
+    discadj_fea.cfg_file  = "configAD_fem.cfg"
     discadj_fea.test_iter = 4
     discadj_fea.test_vals         = [-2.849531, -3.238474, -3.6413e-04, -8.7087] #last 4 columns
     discadj_fea.test_vals_aarch64 = [-2.849570, -3.238519, -3.6413e-04, -8.7087] #last 4 columns
-    test_list.append(discadj_fea)    
+    test_list.append(discadj_fea)
 
     ###################################
     ### Disc. adj. heat             ###
@@ -200,13 +200,13 @@ def main():
     discadj_heat.cfg_dir   = "disc_adj_heat"
     discadj_heat.cfg_file  = "disc_adj_heat.cfg"
     discadj_heat.test_iter = 10
-    discadj_heat.test_vals = [-2.271569, 0.671288, -3.172000, -8.231500] #last 4 columns
+    discadj_heat.test_vals = [-2.350284, 0.665882, -2.649900, -7.006800] #last 4 columns
     test_list.append(discadj_heat)
 
     ###################################
     ### Coupled FSI Adjoint         ###
     ###################################
-   
+
     # Structural model
     discadj_fsi           = TestCase('discadj_fsi')
     discadj_fsi.cfg_dir   = "disc_adj_fsi"
@@ -244,7 +244,7 @@ def main():
             test.tol = 0.00001
 
     pass_list = [ test.run_test() for test in test_list ]
-    
+
     ###################################
     ### Coupled RHT-CFD Adjoint     ###
     ###################################
@@ -265,7 +265,7 @@ def main():
     ######################################
     ### RUN PYTHON TESTS               ###
     ######################################
-    
+
     # test discrete_adjoint.py
     discadj_euler_py = TestCase('discadj_euler_py')
     discadj_euler_py.cfg_dir = "cont_adj_euler/naca0012"
@@ -278,7 +278,7 @@ def main():
     discadj_euler_py.test_file = "of_grad_cd.dat"
     pass_list.append(discadj_euler_py.run_filediff())
     test_list.append(discadj_euler_py)
-    
+
     # test discrete_adjoint with multiple ffd boxes
     discadj_multiple_ffd_py = TestCase('discadj_multiple_ffd_py')
     discadj_multiple_ffd_py.cfg_dir = "multiple_ffd/naca0012"
@@ -382,7 +382,7 @@ def main():
             print('  passed - %s'%test.tag)
         else:
             print('* FAILED - %s'%test.tag)
-    
+
     if all(pass_list):
         sys.exit(0)
     else:
diff --git a/TestCases/sliding_interface/bars_SST_2D/bars.cfg b/TestCases/sliding_interface/bars_SST_2D/bars.cfg
index 87b8c3cd592..cdb2d470575 100644
--- a/TestCases/sliding_interface/bars_SST_2D/bars.cfg
+++ b/TestCases/sliding_interface/bars_SST_2D/bars.cfg
@@ -5,322 +5,137 @@
 % Author: A. Rubino                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: Feb 27th, 2017                                                         %
-% File Version 7.4.0 "Blackbird"                                                   %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
-
+%
 MULTIZONE=YES
-
+%
 TIME_DOMAIN = NO
 TIME_ITER = 3
 TIME_STEP = 0.005
 INNER_ITER= 1
 OUTER_ITER = 100
+%
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               TNE2_EULER, TNE2_NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)                         
 SOLVER= RANS
-% Specify turbulent model (NONE, SA, SST)
 KIND_TURB_MODEL= SST
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
+%
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.3
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 0.1686e5
-%FREESTREAM_PRESSURE= 0.1886e5
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 313.15
-
-% Free-stream temperature (1.2886 Kg/m3 by default)
 FREESTREAM_DENSITY= 1.2886
-
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-% Free-stream Turbulence Intensity
 FREESTREAM_TURBULENCEINTENSITY = 0.025
-%
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
-%REYNOLDS_NUMBER= 2.e5 
-%
-%Init option to choose between Reynolds (default) or thermodynamics quantities for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
 REF_DIMENSIONALIZATION= DIMENSIONAL
-%REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 
 % ---- IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
 %
-% Different gas model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS)
 FLUID_MODEL= STANDARD_AIR
-%
-% Ratio of specific heats (1.4 default and the value is hardcoded
-%                          for the model STANDARD_AIR)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.058 J/kg*K default and this value is hardcoded 
-%                        for the model STANDARD_AIR)
 GAS_CONSTANT= 35.23
-%
-% Critical Temperature (273.15 K by default)
 CRITICAL_TEMPERATURE= 564.1
-%
-% Critical Pressure (101325.0 N/m^2 by default)
 CRITICAL_PRESSURE= 1415000
-%
-% Critical Density (1.2886 Kg/m3 by default)
 CRITICAL_DENSITY= 256.74
-%
-% Acentric factor (0.035 (air))
 ACENTRIC_FACTOR= 0.529
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.0461E-5
-%
-% Sutherland Viscosity Ref (1.716E-5 default value for AIR SI)
 MU_REF= 1.716E-5
-%
-% Sutherland Temperature Ref (273.15 K default value for AIR SI)
 MU_T_REF= 273.15
-%
-% Sutherland constant (110.4 default value for AIR SI)
 SUTHERLAND_CONSTANT= 110.4
 
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
-% Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL).
 CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
-%
-% Molecular Thermal Conductivity that would be constant (0.0257 by default)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.028085
-%
+
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
 MARKER_ZONE_INTERFACE= (outflow_bars, inflow_channel)
 MARKER_FLUID_INTERFACE= (outflow_bars, inflow_channel)
-
-%Dynamic Mesh simulation(Yes, No)
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
-%
-%MARKER_EULER= wall1_bars
 MARKER_HEATFLUX= ( wall1_bars, 0.0 )
-% Inlet boundary type (TOTAL_CONDITIONS, MASS_FLOW)
 INLET_TYPE= TOTAL_CONDITIONS
-%
-% Inlet boundary marker(s) with the following formats (NONE = no marker) 
-% Total Conditions: (inlet marker, total temp, total pressure, flow_direction_x, 
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-% Mass Flow: (inlet marker, density, velocity magnitude, flow_direction_x, 
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.rs
 MARKER_RIEMANN= ( inflow_bars, TOTAL_CONDITIONS_PT, 0.1886e5, 313.15, 1.0, 0.0, 0.0, outflow_channel, STATIC_PRESSURE, 0.1487e5, 0.0, 0.0, 0.0, 0.0)
-%
-% Periodic boundary marker(s) (NONE = no marker)
-% Format: ( periodic marker, donor marker, rotation_center_x, rotation_center_y, 
-% rotation_center_z, rotation_angle_x-axis, rotation_angle_y-axis, 
-% rotation_angle_z-axis, translation_x, translation_y, translation_z, ... )
 MARKER_PERIODIC= ( periodic1_bars, periodic2_bars, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, .105, 0.0, periodic1_channel, periodic2_channel, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, .105, 0.0  )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( wall1_bars )
 MARKER_MONITORING= ( wall1_bars )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.0
-%
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 0.3,20.0 )
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-%
-% Multigrid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multigrid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.75
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.02
-%
-% 2nd and 4th order artificial dissipation coefficients
-%JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_TURB= NONE
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
-%
-% Epsilon for full multigrid method evaluation
-%FULLMG_CONV_CAUCHY_EPS= 1E-4
-%
+
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_bars_turb.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Divide rectangles into triangles (NO, YES)
-%DIVIDE_ELEMENTS= NO
-%
-% Convert a CGNS mesh to SU2 format (YES, NO)
-%CGNS_TO_SU2= NO
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 50
-%
diff --git a/TestCases/sliding_interface/bars_SST_2D/zone_1.cfg b/TestCases/sliding_interface/bars_SST_2D/zone_1.cfg
index 99a0d2f8bf6..3de2ca36a38 100644
--- a/TestCases/sliding_interface/bars_SST_2D/zone_1.cfg
+++ b/TestCases/sliding_interface/bars_SST_2D/zone_1.cfg
@@ -5,20 +5,13 @@
 % Author: A. Rubino                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: Feb 27th, 2017                                                         %
-% File Version 7.4.0 "Blackbird"                                                   %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
-GRID_MOVEMENT= RIGID_MOTION
 %
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
+GRID_MOVEMENT= RIGID_MOTION
 MACH_MOTION= 0.35
-%
-% Origin of the motion
 MOTION_ORIGIN= 0.0 0.0 0.0
-%
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE= 0.0 0.0 0.0
diff --git a/TestCases/sliding_interface/bars_SST_2D/zone_2.cfg b/TestCases/sliding_interface/bars_SST_2D/zone_2.cfg
index 1f61e23c0aa..58725b92dae 100644
--- a/TestCases/sliding_interface/bars_SST_2D/zone_2.cfg
+++ b/TestCases/sliding_interface/bars_SST_2D/zone_2.cfg
@@ -5,21 +5,13 @@
 % Author: A. Rubino                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: Feb 27th, 2017                                                         %
-% File Version 7.4.0 "Blackbird"                                                   %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT= RIGID_MOTION 
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.35
-%
-% Origin of the motion
 MOTION_ORIGIN= 0.0 0.0 0.0
-%
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE = 0.0 0.0 0.1 
diff --git a/TestCases/sliding_interface/bars_SST_2D/zone_3.cfg b/TestCases/sliding_interface/bars_SST_2D/zone_3.cfg
index 93a8b72e77a..e9d4b6f7b3a 100644
--- a/TestCases/sliding_interface/bars_SST_2D/zone_3.cfg
+++ b/TestCases/sliding_interface/bars_SST_2D/zone_3.cfg
@@ -5,20 +5,13 @@
 % Author: A. Rubino                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: Feb 27th, 2017                                                         %
-% File Version 7.4.0 "Blackbird"                                                   %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
-GRID_MOVEMENT= RIGID_MOTION
 %
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
+GRID_MOVEMENT= RIGID_MOTION
 MACH_MOTION= 0.35
-%
-% Origin of the motion
 MOTION_ORIGIN= 0.0 0.0 0.0
-%
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE= 0.0 0.0 -0.1
diff --git a/TestCases/sliding_interface/channel_2D/channel_2D_NN.cfg b/TestCases/sliding_interface/channel_2D/channel_2D_NN.cfg
index 10a96fd8191..60987ed20f6 100644
--- a/TestCases/sliding_interface/channel_2D/channel_2D_NN.cfg
+++ b/TestCases/sliding_interface/channel_2D/channel_2D_NN.cfg
@@ -6,221 +6,91 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
-% Enable multizone mode
 MULTIZONE = YES
-%
-% List of sub config files to specify zone specific options 
 CONFIG_LIST= (zone_1.cfg, zone_2.cfg, zone_3.cfg)
-%
-% Enable time dependent problem
 TIME_DOMAIN = YES
-%
-% Number of time steps
 TIME_ITER = 32000
-%
-% Time step
 TIME_STEP = 0.1
-%
-% Number of outer iterations (Block-Gauss-Seidel)
 OUTER_ITER = 50
-%
-% Inner iterations
 INNER_ITER= 1
-%
 WRT_ZONE_CONV=YES
+%
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)                         
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 %
-%
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
 %
-%
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 3.0
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 95750
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Free-stream Turbulence Intensity
 FREESTREAM_TURBULENCEINTENSITY = 0.1
-%
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
-%
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-%Init option to choose between Reynolds (default) or thermodynamics quantities for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
 %
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( wall )
-%
-% Riemann boundary marker(s)
-% Format inlet:  ( marker, TOTAL_CONDITIONS_PT, Total Pressure, Total Temperature, Flow dir-x, Flow dir-y, Flow dir-z)
-% Format outlet: ( marker, type, STATIC_PRESSURE, Static Pressure, 0.0, 0.0, 0.0, 0.0)
 MARKER_RIEMANN= (up_inlet, STATIC_SUPERSONIC_INFLOW_PT, 95750, 288.15, 3.0, 0.0, 0.0, down_inlet, STATIC_SUPERSONIC_INFLOW_PT, 95750, 288.15, 1.5, 0.0, 0.0,outlet, STATIC_PRESSURE, 95750.0, 0.0, 0.0, 0.0, 0.0)
-%
-% Zone interaction boundary definition
 MARKER_ZONE_INTERFACE= ( internal_interface, inner_interface, domain_interface, external_interface )
 MARKER_FLUID_INTERFACE= ( internal_interface, inner_interface, domain_interface, external_interface )
-
-%
-%
 %
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value, CFL max value )
 CFL_ADAPT_PARAM= ( 0.3, 0.5, 1.0, 1000.0)
 %
-%
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
-%
-%
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-%
-%
+
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
 %
-%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, ROE, AUSM, HLLC)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Entropy fix coefficient (0.0 implies no entropy fixing, 1.0 implies scalar artificial dissipation, 0.001 default)
 ENTROPY_FIX_COEFF= 0.001
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
-% Relaxation coefficient
-%
-%
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 %
-%
-%
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= channel_2D.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= su2mesh_per.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
 TABULAR_FORMAT= CSV	
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1
-%
diff --git a/TestCases/sliding_interface/channel_2D/channel_2D_WA.cfg b/TestCases/sliding_interface/channel_2D/channel_2D_WA.cfg
index abe28ac3db8..be0e1b72874 100644
--- a/TestCases/sliding_interface/channel_2D/channel_2D_WA.cfg
+++ b/TestCases/sliding_interface/channel_2D/channel_2D_WA.cfg
@@ -6,220 +6,91 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
-% Enable multizone mode
 MULTIZONE = YES
-%
-% List of sub config files to specify zone specific options 
 CONFIG_LIST= (zone_1.cfg, zone_2.cfg, zone_3.cfg)
-%
-%
-% Enable time dependent problem
 TIME_DOMAIN = YES
-%
-% Number of time steps
 TIME_ITER = 32000
-%
-% Time step
 TIME_STEP = 0.1
-%
-% Number of outer iterations (Block-Gauss-Seidel)
 OUTER_ITER = 50
-%
-% Inner iterations
 INNER_ITER= 1
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)                         
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 %
-%
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
 %
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 3.0
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 95750
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Free-stream Turbulence Intensity
 FREESTREAM_TURBULENCEINTENSITY = 0.1
-%
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
-%
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-%Init option to choose between Reynolds (default) or thermodynamics quantities for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
 %
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( wall )
-%
-% Riemann boundary marker(s)
-% Format inlet:  ( marker, TOTAL_CONDITIONS_PT, Total Pressure, Total Temperature, Flow dir-x, Flow dir-y, Flow dir-z)
-% Format outlet: ( marker, type, STATIC_PRESSURE, Static Pressure, 0.0, 0.0, 0.0, 0.0)
 MARKER_RIEMANN= (up_inlet, STATIC_SUPERSONIC_INFLOW_PT, 95750, 288.15, 3.0, 0.0, 0.0, down_inlet, STATIC_SUPERSONIC_INFLOW_PT, 95750, 288.15, 1.5, 0.0, 0.0,outlet, STATIC_PRESSURE, 95750.0, 0.0, 0.0, 0.0, 0.0)
-%
-% Zone interaction boundary definition
 MARKER_ZONE_INTERFACE= ( internal_interface, inner_interface, domain_interface, external_interface )
 MARKER_FLUID_INTERFACE= ( internal_interface, inner_interface, domain_interface, external_interface )
-
 KIND_INTERPOLATION= WEIGHTED_AVERAGE
 %
-%
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value, CFL max value )
 CFL_ADAPT_PARAM= ( 0.3, 0.5, 1.0, 1000.0)
 %
-%
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 %
-%
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-%
-%
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
 %
-%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, ROE, AUSM, HLLC)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Entropy fix coefficient (0.0 implies no entropy fixing, 1.0 implies scalar artificial dissipation, 0.001 default)
 ENTROPY_FIX_COEFF= 0.001
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
-% Relaxation coefficient
-%
-%
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 %
-%
-%
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= channel_2D.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= su2mesh_per.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
 TABULAR_FORMAT= CSV	
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1
-%
diff --git a/TestCases/sliding_interface/channel_2D/zone_1.cfg b/TestCases/sliding_interface/channel_2D/zone_1.cfg
index c6f8a353a15..6094dec1657 100644
--- a/TestCases/sliding_interface/channel_2D/zone_1.cfg
+++ b/TestCases/sliding_interface/channel_2D/zone_1.cfg
@@ -1,15 +1,6 @@
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT= RIGID_MOTION
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.35
-%
-
 MOTION_ORIGIN= 0.0 0.0 0.0
-
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE = 0.0 0.0 0.0
-
diff --git a/TestCases/sliding_interface/channel_2D/zone_2.cfg b/TestCases/sliding_interface/channel_2D/zone_2.cfg
index 7bcddf7c656..5ab308f0356 100644
--- a/TestCases/sliding_interface/channel_2D/zone_2.cfg
+++ b/TestCases/sliding_interface/channel_2D/zone_2.cfg
@@ -5,22 +5,13 @@
 % Author: A. Rubino                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: Feb 27th, 2017                                                         %
-% File Version 7.4.0 "Blackbird"                                                   %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
-%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT= RIGID_MOTION
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.35
-%
-
 MOTION_ORIGIN= 0.0 0.0 0.0
-
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE = 0.0 0.0 0.1
-
diff --git a/TestCases/sliding_interface/channel_2D/zone_3.cfg b/TestCases/sliding_interface/channel_2D/zone_3.cfg
index 93a8b72e77a..e9d4b6f7b3a 100644
--- a/TestCases/sliding_interface/channel_2D/zone_3.cfg
+++ b/TestCases/sliding_interface/channel_2D/zone_3.cfg
@@ -5,20 +5,13 @@
 % Author: A. Rubino                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: Feb 27th, 2017                                                         %
-% File Version 7.4.0 "Blackbird"                                                   %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
-GRID_MOVEMENT= RIGID_MOTION
 %
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
+GRID_MOVEMENT= RIGID_MOTION
 MACH_MOTION= 0.35
-%
-% Origin of the motion
 MOTION_ORIGIN= 0.0 0.0 0.0
-%
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE= 0.0 0.0 -0.1
diff --git a/TestCases/sliding_interface/channel_3D/channel_3D_NN.cfg b/TestCases/sliding_interface/channel_3D/channel_3D_NN.cfg
index fc554e29ed7..cf9ff738a0d 100644
--- a/TestCases/sliding_interface/channel_3D/channel_3D_NN.cfg
+++ b/TestCases/sliding_interface/channel_3D/channel_3D_NN.cfg
@@ -6,222 +6,90 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
-% Enable Multizone mode
 MULTIZONE= YES
-%
-% List of config files to specify zone options
 CONFIG_LIST= (zone_1.cfg, zone_2.cfg, zone_3.cfg)
-%
-% Enable time dependent problem
 TIME_DOMAIN = YES
-%
-% Number of time steps
 TIME_ITER = 32000
-%
-% Time step
 TIME_STEP = 0.1
-%
-% Number of outer iterations (Block-Gauss-Seidel)
 OUTER_ITER = 20
-%
-% Inner iterations
 INNER_ITER= 1
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)                         
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 %
-%
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
 %
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 3.0
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 95750
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Free-stream Turbulence Intensity
 FREESTREAM_TURBULENCEINTENSITY = 0.1
-%
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
-%
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-%Init option to choose between Reynolds (default) or thermodynamics quantities for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
 %
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( up_wall, down_wall )
-%
-% Riemann boundary marker(s)
-% Format inlet:  ( marker, TOTAL_CONDITIONS_PT, Total Pressure, Total Temperature, Flow dir-x, Flow dir-y, Flow dir-z)
-% Format outlet: ( marker, type, STATIC_PRESSURE, Static Pressure, 0.0, 0.0, 0.0, 0.0)
 MARKER_RIEMANN= (up_inlet, STATIC_SUPERSONIC_INFLOW_PT, 95750, 288.15, 3.0, 0.0, 0.0, down_inlet, STATIC_SUPERSONIC_INFLOW_PT, 95750, 288.15, 1.5, 0.0, 0.0, up_outlet, STATIC_PRESSURE, 95750.0, 0.0, 0.0, 0.0, 0.0, down_outlet, STATIC_PRESSURE, 95750.0, 0.0, 0.0, 0.0, 0.0)
-%
-% Zone interaction boundary definition
 MARKER_ZONE_INTERFACE= ( internal_interface, inner_interface, domain_interface, external_interface )
 MARKER_FLUID_INTERFACE= ( internal_interface, inner_interface, domain_interface, external_interface )
-
-%KIND_INTERPOLATION= ISOPARAMETRIC
-%
-%
-
-%
 %
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value, CFL max value )
 CFL_ADAPT_PARAM= ( 0.3, 0.5, 1.0, 1000.0)
 %
-%
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
-%
-%
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-%
-%
+
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
 %
-%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, ROE, AUSM, HLLC)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Entropy fix coefficient (0.0 implies no entropy fixing, 1.0 implies scalar artificial dissipation, 0.001 default)
 ENTROPY_FIX_COEFF= 0.001
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
-% Relaxation coefficient
-%
-%
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 %
-%
-%
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= channel_3D.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= su2mesh_per.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
 TABULAR_FORMAT= CSV	
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1
-%
diff --git a/TestCases/sliding_interface/channel_3D/channel_3D_WA.cfg b/TestCases/sliding_interface/channel_3D/channel_3D_WA.cfg
index a0d764aa83e..946a457c9c0 100644
--- a/TestCases/sliding_interface/channel_3D/channel_3D_WA.cfg
+++ b/TestCases/sliding_interface/channel_3D/channel_3D_WA.cfg
@@ -6,220 +6,91 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
-% Enable Multizone mode
 MULTIZONE= YES
-%
-% List of config files to specify zone options
 CONFIG_LIST= (zone_1.cfg, zone_2.cfg, zone_3.cfg)
-%
-% Enable time dependent problem
 TIME_DOMAIN = YES
-%
-% Number of time steps
 TIME_ITER = 32000
-%
-% Time step
 TIME_STEP = 0.1
-%
-% Number of outer iterations (Block-Gauss-Seidel)
 OUTER_ITER = 20
-%
-% Inner iterations
 INNER_ITER= 1
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)                         
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 %
-%
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
+%
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 3.0
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 95750
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Free-stream Turbulence Intensity
 FREESTREAM_TURBULENCEINTENSITY = 0.1
-%
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
-%
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-%Init option to choose between Reynolds (default) or thermodynamics quantities for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
 %
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( up_wall, down_wall )
-%
-% Riemann boundary marker(s)
-% Format inlet:  ( marker, TOTAL_CONDITIONS_PT, Total Pressure, Total Temperature, Flow dir-x, Flow dir-y, Flow dir-z)
-% Format outlet: ( marker, type, STATIC_PRESSURE, Static Pressure, 0.0, 0.0, 0.0, 0.0)
 MARKER_RIEMANN= (up_inlet, STATIC_SUPERSONIC_INFLOW_PT, 95750, 288.15, 3.0, 0.0, 0.0, down_inlet, STATIC_SUPERSONIC_INFLOW_PT, 95750, 288.15, 1.5, 0.0, 0.0, up_outlet, STATIC_PRESSURE, 95750.0, 0.0, 0.0, 0.0, 0.0, down_outlet, STATIC_PRESSURE, 95750.0, 0.0, 0.0, 0.0, 0.0)
-%
-% Zone interaction boundary definition
 MARKER_ZONE_INTERFACE= ( internal_interface, inner_interface, domain_interface, external_interface )
 MARKER_FLUID_INTERFACE= ( internal_interface, inner_interface, domain_interface, external_interface )
-
-
 KIND_INTERPOLATION= WEIGHTED_AVERAGE
 %
-%
-%
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value, CFL max value )
 CFL_ADAPT_PARAM= ( 0.3, 0.5, 1.0, 1000.0)
 %
-%
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 %
-%
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-%
-%
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
 %
-%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, ROE, AUSM, HLLC)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Entropy fix coefficient (0.0 implies no entropy fixing, 1.0 implies scalar artificial dissipation, 0.001 default)
 ENTROPY_FIX_COEFF= 0.001
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
-% Relaxation coefficient
-%
-%
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 %
-%
-%
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= channel_3D.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= su2mesh_per.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
 TABULAR_FORMAT= CSV	
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1
-%
diff --git a/TestCases/sliding_interface/channel_3D/zone_1.cfg b/TestCases/sliding_interface/channel_3D/zone_1.cfg
index e12e7e3e1e0..18fd4b6f495 100644
--- a/TestCases/sliding_interface/channel_3D/zone_1.cfg
+++ b/TestCases/sliding_interface/channel_3D/zone_1.cfg
@@ -6,13 +6,10 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Dynamic mesh simulation (NO, YES)
 GRID_MOVEMENT= NONE
-%
-
diff --git a/TestCases/sliding_interface/channel_3D/zone_2.cfg b/TestCases/sliding_interface/channel_3D/zone_2.cfg
index 07fa5e931f6..236b5b474bf 100644
--- a/TestCases/sliding_interface/channel_3D/zone_2.cfg
+++ b/TestCases/sliding_interface/channel_3D/zone_2.cfg
@@ -6,20 +6,12 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-% ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
+% ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 GRID_MOVEMENT= RIGID_MOTION 
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.35
-%
-
 MOTION_ORIGIN= 0.0 0.0 0.0
-
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE= 0.0 0.0 0.1
diff --git a/TestCases/sliding_interface/channel_3D/zone_3.cfg b/TestCases/sliding_interface/channel_3D/zone_3.cfg
index bbb2b380d7e..36437956c6e 100644
--- a/TestCases/sliding_interface/channel_3D/zone_3.cfg
+++ b/TestCases/sliding_interface/channel_3D/zone_3.cfg
@@ -6,19 +6,12 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT= RIGID_MOTION 
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.35
-%
-
 MOTION_ORIGIN= 0.0 0.0 0.0
-
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE= 0.1 0.0 0.0
diff --git a/TestCases/sliding_interface/incompressible_steady/config.cfg b/TestCases/sliding_interface/incompressible_steady/config.cfg
index b06c6547e8a..54886c165ad 100644
--- a/TestCases/sliding_interface/incompressible_steady/config.cfg
+++ b/TestCases/sliding_interface/incompressible_steady/config.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/incompressible_steady/configCircle.cfg b/TestCases/sliding_interface/incompressible_steady/configCircle.cfg
index 5e19edc13d5..32fbfdae307 100644
--- a/TestCases/sliding_interface/incompressible_steady/configCircle.cfg
+++ b/TestCases/sliding_interface/incompressible_steady/configCircle.cfg
@@ -5,15 +5,12 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
-%
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
+
 SOLVER= INC_NAVIER_STOKES
 KIND_TURB_MODEL= NONE
 MATH_PROBLEM= DIRECT
@@ -74,18 +71,8 @@ LINEAR_SOLVER_ILU_FILL_IN= 0
 LINEAR_SOLVER_ERROR= 1E-8
 LINEAR_SOLVER_ITER= 10
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-
-MGLEVEL= 0
-MGCYCLE= V_CYCLE
-MG_PRE_SMOOTH= ( 1, 1, 1, 1 )
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-MG_DAMP_RESTRICTION= 0.8
-MG_DAMP_PROLONGATION= 0.8
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
-%
+
 CONV_NUM_METHOD_FLOW= FDS
 MUSCL_FLOW= YES
 SLOPE_LIMITER_FLOW= NONE
@@ -104,6 +91,7 @@ CONV_CAUCHY_ELEMS= 100
 CONV_CAUCHY_EPS= 1E-6
 
 % --------------------------- TURBULENCE PARAMETERS --------------------------%
+
 FREESTREAM_TURBULENCEINTENSITY = 0.001
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
 
@@ -132,4 +120,3 @@ SURFACE_FILENAME= surface_flow
 SURFACE_ADJ_FILENAME= surface_adjoint
 
 OUTPUT_WRT_FREQ= 1000
-
diff --git a/TestCases/sliding_interface/incompressible_steady/configOut.cfg b/TestCases/sliding_interface/incompressible_steady/configOut.cfg
index 830aa533aa7..ad23d8924ca 100644
--- a/TestCases/sliding_interface/incompressible_steady/configOut.cfg
+++ b/TestCases/sliding_interface/incompressible_steady/configOut.cfg
@@ -5,15 +5,12 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
-%
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
+
 SOLVER= INC_NAVIER_STOKES
 KIND_TURB_MODEL= NONE
 MATH_PROBLEM= DIRECT
@@ -84,16 +81,6 @@ LINEAR_SOLVER_ILU_FILL_IN= 0
 LINEAR_SOLVER_ERROR= 1E-8
 LINEAR_SOLVER_ITER= 10
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-
-MGLEVEL= 0
-MGCYCLE= V_CYCLE
-MG_PRE_SMOOTH= ( 1, 1, 1, 1 )
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-MG_DAMP_RESTRICTION= 0.8
-MG_DAMP_PROLONGATION= 0.8
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= FDS
@@ -138,4 +125,3 @@ SURFACE_FILENAME= surface_flow
 SURFACE_ADJ_FILENAME= surface_adjoint
 
 OUTPUT_WRT_FREQ= 1000
-
diff --git a/TestCases/sliding_interface/incompressible_unsteady/config.cfg b/TestCases/sliding_interface/incompressible_unsteady/config.cfg
index 81a7c8bbf02..59c3d2330af 100644
--- a/TestCases/sliding_interface/incompressible_unsteady/config.cfg
+++ b/TestCases/sliding_interface/incompressible_unsteady/config.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 6.1.0 "Falcon"                                                   %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg b/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg
index 4082db97ddf..8d35dbd81b1 100644
--- a/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg
+++ b/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg
@@ -5,15 +5,12 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 6.1.0 "Falcon"                                                   %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
-%
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
+
 SOLVER= INC_NAVIER_STOKES
 KIND_TURB_MODEL= NONE
 MATH_PROBLEM= DIRECT
@@ -82,16 +79,6 @@ LINEAR_SOLVER_ILU_FILL_IN= 0
 LINEAR_SOLVER_ERROR= 1E-8
 LINEAR_SOLVER_ITER= 10
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-
-MGLEVEL= 0
-MGCYCLE= V_CYCLE
-MG_PRE_SMOOTH= ( 1, 1, 1, 1 )
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-MG_DAMP_RESTRICTION= 0.8
-MG_DAMP_PROLONGATION= 0.8
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= FDS
@@ -136,5 +123,3 @@ SURFACE_FILENAME= surface_flow
 SURFACE_ADJ_FILENAME= surface_adjoint
 
 OUTPUT_WRT_FREQ= 1
-
-
diff --git a/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg b/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg
index c104e40ec79..d7a7eb33d4a 100644
--- a/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg
+++ b/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg
@@ -5,22 +5,17 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 6.1.0 "Falcon"                                                   %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
-%
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
+
 SOLVER= INC_NAVIER_STOKES
 KIND_TURB_MODEL= NONE
 MATH_PROBLEM= DIRECT
 RESTART_SOL= NO
-
 INC_NONDIM = DIMENSIONAL
-
 MULTIZONE_MESH = NO
 
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
@@ -92,16 +87,6 @@ LINEAR_SOLVER_ILU_FILL_IN= 0
 LINEAR_SOLVER_ERROR= 1E-8
 LINEAR_SOLVER_ITER= 10
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-
-MGLEVEL= 0
-MGCYCLE= V_CYCLE
-MG_PRE_SMOOTH= ( 1, 1, 1, 1 )
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-MG_DAMP_RESTRICTION= 0.8
-MG_DAMP_PROLONGATION= 0.8
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= FDS
@@ -146,5 +131,3 @@ SURFACE_FILENAME= surface_flow
 SURFACE_ADJ_FILENAME= surface_adjoint
 
 OUTPUT_WRT_FREQ= 1
-
-
diff --git a/TestCases/sliding_interface/pipe/pipe_NN.cfg b/TestCases/sliding_interface/pipe/pipe_NN.cfg
index 528a0b56e75..2662bd093d2 100644
--- a/TestCases/sliding_interface/pipe/pipe_NN.cfg
+++ b/TestCases/sliding_interface/pipe/pipe_NN.cfg
@@ -6,228 +6,91 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
-% Enable multizone mode
 MULTIZONE= YES
-%
 MULTIZONE_SOLVER= BLOCK_JACOBI
-%
-% List of config files for zone specific options
 CONFIG_LIST= (zone_1.cfg, zone_2.cfg, zone_3.cfg, zone_4.cfg, zone_5.cfg)
-%
 TIME_DOMAIN=YES
-%
-% Time step
 TIME_STEP= 0.1
-%
 TIME_ITER= 10
-%
 OUTER_ITER=10
-%
 INNER_ITER=1
+%
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)                         
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 %
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
 %
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 3.0
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 95750
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Free-stream Turbulence Intensity
 FREESTREAM_TURBULENCEINTENSITY = 0.1
-%
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
-%
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-%Init option to choose between Reynolds (default) or thermodynamics quantities for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
 %
-%
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( intake_sidewall, component_sidewall_1, component_sidewall_2, component_sidewall_3, component_sidewall_4 )
-%
-% Riemann boundary marker(s)
-% Format inlet:  ( marker, TOTAL_CONDITIONS_PT, Total Pressure, Total Temperature, Flow dir-x, Flow dir-y, Flow dir-z)
-% Format outlet: ( marker, type, STATIC_PRESSURE, Static Pressure, 0.0, 0.0, 0.0, 0.0)
-%
 MARKER_RIEMANN= (intake_upper_inlet, STATIC_SUPERSONIC_INFLOW_PT, 95750, 288.15, 3.0, 0.0, 0.0, intake_lower_inlet, STATIC_SUPERSONIC_INFLOW_PT, 95750, 288.15, 1.5, 0.0, 0.0, outlet_interface_4  STATIC_PRESSURE, 95750.0, 0.0, 0.0, 0.0, 0.0 )
-%
-% Zone interaction boundary definition
 MARKER_ZONE_INTERFACE= ( intake_interface, inlet_interface_1, outlet_interface_1, inlet_interface_2, outlet_interface_2, inlet_interface_3, outlet_interface_3, inlet_interface_4 )
 MARKER_FLUID_INTERFACE= ( intake_interface, inlet_interface_1, outlet_interface_1, inlet_interface_2, outlet_interface_2, inlet_interface_3, outlet_interface_3, inlet_interface_4 )
 %
-
-
-%KIND_INTERPOLATION= ISOPARAMETRIC
-%
-%
-
-%
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value, CFL max value )
 CFL_ADAPT_PARAM= ( 0.3, 0.5, 1.0, 1000.0)
 %
-%
-%
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 %
-%
-%
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-%
-%
-%
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
 %
-%
-%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, ROE, AUSM, HLLC)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Entropy fix coefficient (0.0 implies no entropy fixing, 1.0 implies scalar artificial dissipation, 0.001 default)
 ENTROPY_FIX_COEFF= 0.001
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
-% Relaxation coefficient
-%
-%
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 %
-%
-%
-%
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= pipe.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= su2mesh_per.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
 TABULAR_FORMAT= CSV	
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 50
-%
diff --git a/TestCases/sliding_interface/pipe/pipe_WA.cfg b/TestCases/sliding_interface/pipe/pipe_WA.cfg
index ba5af7ef564..00427123748 100644
--- a/TestCases/sliding_interface/pipe/pipe_WA.cfg
+++ b/TestCases/sliding_interface/pipe/pipe_WA.cfg
@@ -6,227 +6,91 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
-% Enable multizone mode
 MULTIZONE= YES
-%
-% List of config files for zone specific options
 CONFIG_LIST= (zone_1.cfg, zone_2.cfg, zone_3.cfg, zone_4.cfg, zone_5.cfg)
-%
 TIME_DOMAIN=YES
-%
 TIME_STEP= 0.1
-%
 TIME_ITER= 10
-%
 OUTER_ITER=200
-%
 INNER_ITER=1
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)                         
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 %
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-
+%
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 3.0
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 95750
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Free-stream Turbulence Intensity
 FREESTREAM_TURBULENCEINTENSITY = 0.1
-%
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
-%
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-%Init option to choose between Reynolds (default) or thermodynamics quantities for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
 %
-%
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( intake_sidewall, component_sidewall_1, component_sidewall_2, component_sidewall_3, component_sidewall_4 )
-%
-% Riemann boundary marker(s)
-% Format inlet:  ( marker, TOTAL_CONDITIONS_PT, Total Pressure, Total Temperature, Flow dir-x, Flow dir-y, Flow dir-z)
-% Format outlet: ( marker, type, STATIC_PRESSURE, Static Pressure, 0.0, 0.0, 0.0, 0.0)
-%
 MARKER_RIEMANN= (intake_upper_inlet, STATIC_SUPERSONIC_INFLOW_PT, 95750, 288.15, 3.0, 0.0, 0.0, intake_lower_inlet, STATIC_SUPERSONIC_INFLOW_PT, 95750, 288.15, 1.5, 0.0, 0.0, outlet_interface_4  STATIC_PRESSURE, 95750.0, 0.0, 0.0, 0.0, 0.0 )
-%
-% Zone interaction boundary definition
 MARKER_ZONE_INTERFACE= ( intake_interface, inlet_interface_1, outlet_interface_1, inlet_interface_2, outlet_interface_2, inlet_interface_3, outlet_interface_3, inlet_interface_4 )
-%
 MARKER_FLUID_INTERFACE= ( intake_interface, inlet_interface_1, outlet_interface_1, inlet_interface_2, outlet_interface_2, inlet_interface_3, outlet_interface_3, inlet_interface_4 )
-%
-
-%
 KIND_INTERPOLATION= WEIGHTED_AVERAGE
 %
-%
-%
-%
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value, CFL max value )
 CFL_ADAPT_PARAM= ( 0.3, 0.5, 1.0, 1000.0)
 %
-%
-%
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 %
-%
-%
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-%
-%
-%
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
 %
-%
-%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, ROE, AUSM, HLLC)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Entropy fix coefficient (0.0 implies no entropy fixing, 1.0 implies scalar artificial dissipation, 0.001 default)
 ENTROPY_FIX_COEFF= 0.001
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
-% Relaxation coefficient
-%
-%
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 %
-%
-%
-%
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= pipe.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= su2mesh_per.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
 TABULAR_FORMAT= CSV	
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 50
-%
diff --git a/TestCases/sliding_interface/pipe/zone_1.cfg b/TestCases/sliding_interface/pipe/zone_1.cfg
index 9305a491e22..b9ec892d924 100644
--- a/TestCases/sliding_interface/pipe/zone_1.cfg
+++ b/TestCases/sliding_interface/pipe/zone_1.cfg
@@ -6,22 +6,14 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT= RIGID_MOTION 
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.35
-%
-
-MOTION_ORIGIN= 0.0 0.0 0.0
-
 % Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
+MOTION_ORIGIN= 0.0 0.0 0.0
 ROTATION_RATE = 0.0 0.0 0.0
-%
diff --git a/TestCases/sliding_interface/pipe/zone_2.cfg b/TestCases/sliding_interface/pipe/zone_2.cfg
index 95e147231ad..984f550bf93 100644
--- a/TestCases/sliding_interface/pipe/zone_2.cfg
+++ b/TestCases/sliding_interface/pipe/zone_2.cfg
@@ -6,24 +6,13 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
-
 %
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT= RIGID_MOTION 
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.35
-%
-
 MOTION_ORIGIN= 0.0 0.0 0.0
-
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE = 0.1 0.0 0.0
-%
-%
diff --git a/TestCases/sliding_interface/pipe/zone_3.cfg b/TestCases/sliding_interface/pipe/zone_3.cfg
index 6302f1a6ce3..b93def50e39 100644
--- a/TestCases/sliding_interface/pipe/zone_3.cfg
+++ b/TestCases/sliding_interface/pipe/zone_3.cfg
@@ -6,23 +6,13 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
-
 %
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT= RIGID_MOTION 
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.35
-%
-
 MOTION_ORIGIN= 0.0 0.0 0.0
-
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE = 0.2 0.0 0.0
-%
diff --git a/TestCases/sliding_interface/pipe/zone_4.cfg b/TestCases/sliding_interface/pipe/zone_4.cfg
index 6addf18e2ec..1c678c8131f 100644
--- a/TestCases/sliding_interface/pipe/zone_4.cfg
+++ b/TestCases/sliding_interface/pipe/zone_4.cfg
@@ -6,25 +6,13 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
-
 %
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT= RIGID_MOTION 
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.35
-%
-
 MOTION_ORIGIN= 0.0 0.0 0.0
-
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE = -0.1 0.0 0.0
-%
-%
-
diff --git a/TestCases/sliding_interface/pipe/zone_5.cfg b/TestCases/sliding_interface/pipe/zone_5.cfg
index b347a3df03f..984f550bf93 100644
--- a/TestCases/sliding_interface/pipe/zone_5.cfg
+++ b/TestCases/sliding_interface/pipe/zone_5.cfg
@@ -6,25 +6,13 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
-
 %
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT= RIGID_MOTION 
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.35
-%
-
 MOTION_ORIGIN= 0.0 0.0 0.0
-
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE = 0.1 0.0 0.0
-%
-%
-
diff --git a/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_NN.cfg b/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_NN.cfg
index d8e16aa2137..36c0b729f9b 100644
--- a/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_NN.cfg
+++ b/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_NN.cfg
@@ -5,226 +5,91 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
-% Enable multizone mode
 MULTIZONE= YES
-%
-% Config list for zone specific options
 CONFIG_LIST = (zone_1.cfg, zone_2.cfg, zone_3.cfg)
-%
-% Enable time dependent problem
 TIME_DOMAIN = YES
-%
-% Number of time steps
 TIME_ITER = 32000
-%
-% Time step
 TIME_STEP = 0.1
-%
-% Number of outer iterations (Block-Gauss-Seidel)
 OUTER_ITER = 10
-%
-% Inner iterations
 INNER_ITER= 1
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)                         
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 %
-%
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
 %
-%
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 2.5
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 95750
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Free-stream Turbulence Intensity
 FREESTREAM_TURBULENCEINTENSITY = 0.1
-%
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
-%
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-%Init option to choose between Reynolds (default) or thermodynamics quantities for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
 %
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( wall )
-%
-% Riemann boundary marker(s)
-% Format inlet:  ( marker, TOTAL_CONDITIONS_PT, Total Pressure, Total Temperature, Flow dir-x, Flow dir-y, Flow dir-z)
-% Format outlet: ( marker, type, STATIC_PRESSURE, Static Pressure, 0.0, 0.0, 0.0, 0.0)
 MARKER_RIEMANN= (inlet, STATIC_SUPERSONIC_INFLOW_PT, 95750, 288.15, 2.5, 0.0, 0.0, outlet, STATIC_PRESSURE, 9575.0, 0.0, 0.0, 0.0, 0.0)
-%
-% Zone interaction boundary definition
 MARKER_ZONE_INTERFACE= ( domain_interface, external_interface, internal_interface, inner_interface)
 MARKER_FLUID_INTERFACE= ( domain_interface, external_interface, internal_interface, inner_interface)
-
-%KIND_INTERPOLATION= SLIDING_MESH
-%
-% Periodic boundary marker(s) (NONE = no marker)
-% Format: ( periodic marker, donor marker, rot_cen_x, rot_cen_y, rot_cen_z, rot_angle_x-axis, rot_angle_y-axis, rot_angle_z-axis, translation_x, translation_y, translation_z)
 MARKER_SYM= ( up, down )
 %
-%
-%
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value, CFL max value )
 CFL_ADAPT_PARAM= ( 0.3, 0.5, 1.0, 1000.0)
 %
-%
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 %
-%
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-%
-%
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
 %
-%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, ROE, AUSM, HLLC)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= NO
-%
-% Entropy fix coefficient (0.0 implies no entropy fixing, 1.0 implies scalar artificial dissipation, 0.001 default)
 ENTROPY_FIX_COEFF= 0.001
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
-% Relaxation coefficient
-%
-%
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 %
-%
-%
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= rotating_cylinders.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= su2mesh_per.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
 TABULAR_FORMAT= CSV	
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 50
-%
diff --git a/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_WA.cfg b/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_WA.cfg
index 794b9b76d9e..c6e279dd3c1 100644
--- a/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_WA.cfg
+++ b/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_WA.cfg
@@ -5,229 +5,93 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
-%
-% Enable multizone mode
 MULTIZONE= YES
-%
-% Config list for zone specific options
 CONFIG_LIST = (zone_1.cfg, zone_2.cfg, zone_3.cfg)
-%
 MULTIZONE_SOLVER= BLOCK_JACOBI
-%
-% Enable time dependent problem
 TIME_DOMAIN = YES
-%
-% Number of time steps
 TIME_ITER = 32000
-%
-% Time step
 TIME_STEP = 0.1
-%
-% Number of outer iterations (Block-Gauss-Seidel)
 OUTER_ITER = 10
-%
-% Inner iterations
 INNER_ITER= 1
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)                         
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 %
-%
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
 %
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 2.5
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 95750
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Free-stream Turbulence Intensity
 FREESTREAM_TURBULENCEINTENSITY = 0.1
-%
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
-%
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-%Init option to choose between Reynolds (default) or thermodynamics quantities for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
 %
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( wall )
-%
-% Riemann boundary marker(s)
-% Format inlet:  ( marker, TOTAL_CONDITIONS_PT, Total Pressure, Total Temperature, Flow dir-x, Flow dir-y, Flow dir-z)
-% Format outlet: ( marker, type, STATIC_PRESSURE, Static Pressure, 0.0, 0.0, 0.0, 0.0)
 MARKER_RIEMANN= (inlet, STATIC_SUPERSONIC_INFLOW_PT, 95750, 288.15, 2.5, 0.0, 0.0, outlet, STATIC_PRESSURE, 9575.0, 0.0, 0.0, 0.0, 0.0)
-%
-% Zone interaction boundary definition
 MARKER_ZONE_INTERFACE= ( domain_interface, external_interface, internal_interface, inner_interface)
 MARKER_FLUID_INTERFACE= ( domain_interface, external_interface, internal_interface, inner_interface)
-
-%
 KIND_INTERPOLATION= WEIGHTED_AVERAGE
-%
-% Periodic boundary marker(s) (NONE = no marker)
-% Format: ( periodic marker, donor marker, rot_cen_x, rot_cen_y, rot_cen_z, rot_angle_x-axis, rot_angle_y-axis, rot_angle_z-axis, translation_x, translation_y, translation_z)
 MARKER_SYM= ( up, down )
 %
-%
-%
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value, CFL max value )
 CFL_ADAPT_PARAM= ( 0.3, 0.5, 1.0, 1000.0)
 %
-%
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 %
-%
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-%
-%
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
 %
-%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, ROE, AUSM, HLLC)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= NO
-%
-% Entropy fix coefficient (0.0 implies no entropy fixing, 1.0 implies scalar artificial dissipation, 0.001 default)
 ENTROPY_FIX_COEFF= 0.001
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
-% Relaxation coefficient
-%
-%
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 %
-%
-%
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= rotating_cylinders.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= su2mesh_per.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
 TABULAR_FORMAT= CSV	
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 50
-%
diff --git a/TestCases/sliding_interface/rotating_cylinders/zone_1.cfg b/TestCases/sliding_interface/rotating_cylinders/zone_1.cfg
index c6f8a353a15..6094dec1657 100644
--- a/TestCases/sliding_interface/rotating_cylinders/zone_1.cfg
+++ b/TestCases/sliding_interface/rotating_cylinders/zone_1.cfg
@@ -1,15 +1,6 @@
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT= RIGID_MOTION
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.35
-%
-
 MOTION_ORIGIN= 0.0 0.0 0.0
-
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE = 0.0 0.0 0.0
-
diff --git a/TestCases/sliding_interface/rotating_cylinders/zone_2.cfg b/TestCases/sliding_interface/rotating_cylinders/zone_2.cfg
index 08ca4f7db54..2db899e66be 100644
--- a/TestCases/sliding_interface/rotating_cylinders/zone_2.cfg
+++ b/TestCases/sliding_interface/rotating_cylinders/zone_2.cfg
@@ -1,16 +1,6 @@
-
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT= RIGID_MOTION
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.35
-%
-
 MOTION_ORIGIN= 0.0 0.0 0.0
-
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE = 0.0 0.0 0.1
-
diff --git a/TestCases/sliding_interface/rotating_cylinders/zone_3.cfg b/TestCases/sliding_interface/rotating_cylinders/zone_3.cfg
index f3b8e38812a..5899ceb28de 100644
--- a/TestCases/sliding_interface/rotating_cylinders/zone_3.cfg
+++ b/TestCases/sliding_interface/rotating_cylinders/zone_3.cfg
@@ -1,15 +1,6 @@
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT= RIGID_MOTION
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.35
-%
-
 MOTION_ORIGIN= 0.0 0.0 0.0
-
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE = 0.0 0.0 -0.1
-
diff --git a/TestCases/sliding_interface/single_stage/single_stage_NN.cfg b/TestCases/sliding_interface/single_stage/single_stage_NN.cfg
index cfb2030f2e1..38bfc466e59 100644
--- a/TestCases/sliding_interface/single_stage/single_stage_NN.cfg
+++ b/TestCases/sliding_interface/single_stage/single_stage_NN.cfg
@@ -6,266 +6,100 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 4.3.0 "cardinal"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
-% Enable multizone mode
 MULTIZONE= YES
-%
-% List of config files to set zone specific options
 CONFIG_LIST= (zone_1.cfg, zone_2.cfg)
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)                         
 SOLVER= EULER
-%
-% Specify turbulent model (NONE, SA, SST)
 KIND_TURB_MODEL= SST
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 %
-%
-%
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
 TIME_DOMAIN=YES
-%
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-%
-% Time Step for dual time stepping simulations (s)
 TIME_STEP= 0.1
-%
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 10.0
-%
-% Number of internal iterations (dual time method)
 INNER_ITER= 200
-
 RESTART_ITER = 2
 %
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 3.0
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 95750
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Free-stream Turbulence Intensity
 FREESTREAM_TURBULENCEINTENSITY = 0.1
-%
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
-%
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-%Init option to choose between Reynolds (default) or thermodynamics quantities for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
 %
-%
-%
-% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
-%
-%Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
-%REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
-%
-%
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-
 MARKER_EULER= ( stator_sidewall, rotor_sidewall )
-
-% Riemann boundary marker(s)
-% Format inlet:  ( marker, TOTAL_CONDITIONS_PT, Total Pressure, Total Temperature, Flow dir-x, Flow dir-y, Flow dir-z)
-% Format outlet: ( marker, type, STATIC_PRESSURE, Static Pressure, 0.0, 0.0, 0.0, 0.0)
 MARKER_RIEMANN= (upper_inlet, STATIC_SUPERSONIC_INFLOW_PT, 95750, 288.15, 3.0, 0.0, 0.0, lower_inlet, STATIC_SUPERSONIC_INFLOW_PT, 95750, 288.15, 1.5, 0.0, 0.0, outlet, STATIC_PRESSURE, 95750.0, 0.0, 0.0, 0.0, 0.0 )
-
 MARKER_ZONE_INTERFACE= ( stator_interface, rotor_interface )
 MARKER_FLUID_INTERFACE= ( stator_interface, rotor_interface )
-
 KIND_INTERPOLATION= ISOPARAMETRIC
-%KIND_INTERPOLATION= SLIDING_MESH
-%
-%
-
-%
-%
 %
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value, CFL max value )
 CFL_ADAPT_PARAM= ( 0.3, 0.5, 1.0, 1000.0)
 %
-%
-%
-%
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 %
-%
-%
-%
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-%
-%
-%
-%
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
 %
-%
-%
-%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, ROE, AUSM, HLLC)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Entropy fix coefficient (0.0 implies no entropy fixing, 1.0 implies scalar artificial dissipation, 0.001 default)
 ENTROPY_FIX_COEFF= 0.001
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
-% Relaxation coefficient
-%
-%
-%
-%
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 %
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 %
-%
-%
-%
-%
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh.su2
-%MESH_FILENAME= external.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= su2mesh_per.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
 TABULAR_FORMAT= CSV	
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 50
-%
diff --git a/TestCases/sliding_interface/single_stage/single_stage_WA.cfg b/TestCases/sliding_interface/single_stage/single_stage_WA.cfg
index 5a3e0f1ff94..e49e091be7c 100644
--- a/TestCases/sliding_interface/single_stage/single_stage_WA.cfg
+++ b/TestCases/sliding_interface/single_stage/single_stage_WA.cfg
@@ -6,263 +6,100 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 4.3.0 "cardinal"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
-%
-% Enable multizone mode
 MULTIZONE= YES
-%
-% List of config files to set zone specific options
 CONFIG_LIST= (zone_1.cfg, zone_2.cfg)
 %
-%
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)                         
 SOLVER= EULER
-%
-% Specify turbulent model (NONE, SA, SST)
 KIND_TURB_MODEL= SST
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 %
-%
-%
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
 TIME_DOMAIN=YES
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-%
-% Time Step for dual time stepping simulations (s)
 TIME_STEP= 0.1
-%
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 10.0
-%
-% Number of internal iterations (dual time method)
 INNER_ITER= 200
-
 RESTART_ITER = 2
 %
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 3.0
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 95750
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Free-stream Turbulence Intensity
 FREESTREAM_TURBULENCEINTENSITY = 0.1
-%
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
-%
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-%Init option to choose between Reynolds (default) or thermodynamics quantities for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
 %
-%
-%
-% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
-%
-%Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
-%REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
-%
-%
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-
 MARKER_EULER= ( stator_sidewall, rotor_sidewall )
-
-% Riemann boundary marker(s)
-% Format inlet:  ( marker, TOTAL_CONDITIONS_PT, Total Pressure, Total Temperature, Flow dir-x, Flow dir-y, Flow dir-z)
-% Format outlet: ( marker, type, STATIC_PRESSURE, Static Pressure, 0.0, 0.0, 0.0, 0.0)
 MARKER_RIEMANN= (upper_inlet, STATIC_SUPERSONIC_INFLOW_PT, 95750, 288.15, 3.0, 0.0, 0.0, lower_inlet, STATIC_SUPERSONIC_INFLOW_PT, 95750, 288.15, 1.5, 0.0, 0.0, outlet, STATIC_PRESSURE, 95750.0, 0.0, 0.0, 0.0, 0.0 )
-
 MARKER_ZONE_INTERFACE= ( stator_interface, rotor_interface )
 MARKER_FLUID_INTERFACE= ( stator_interface, rotor_interface )
-
-%
 KIND_INTERPOLATION= WEIGHTED_AVERAGE
 %
-%
-%
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value, CFL max value )
 CFL_ADAPT_PARAM= ( 0.3, 0.5, 1.0, 1000.0)
 %
-%
-%
-%
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 %
-%
-%
-%
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-%
-%
-%
-%
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
 %
-%
-%
-%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, ROE, AUSM, HLLC)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Entropy fix coefficient (0.0 implies no entropy fixing, 1.0 implies scalar artificial dissipation, 0.001 default)
 ENTROPY_FIX_COEFF= 0.001
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
-%
-%
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 %
-%
-%
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 %
-%
-%
-%
-%
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh.su2
-%MESH_FILENAME= external.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= su2mesh_per.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
 TABULAR_FORMAT= CSV	
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 50
-%
diff --git a/TestCases/sliding_interface/single_stage/zone_1.cfg b/TestCases/sliding_interface/single_stage/zone_1.cfg
index 46c87be7073..e1f1b675868 100644
--- a/TestCases/sliding_interface/single_stage/zone_1.cfg
+++ b/TestCases/sliding_interface/single_stage/zone_1.cfg
@@ -6,23 +6,14 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 4.3.0 "cardinal"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
 %
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT= RIGID_MOTION
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.35
-%
-
 MOTION_ORIGIN= 0.0 0.0 0.0
-
 % Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE = 0.0 0.0 0.0
-
diff --git a/TestCases/sliding_interface/single_stage/zone_2.cfg b/TestCases/sliding_interface/single_stage/zone_2.cfg
index 27de8c25b1f..374c65aaf88 100644
--- a/TestCases/sliding_interface/single_stage/zone_2.cfg
+++ b/TestCases/sliding_interface/single_stage/zone_2.cfg
@@ -6,23 +6,13 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 4.3.0 "cardinal"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
 %
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT= RIGID_MOTION
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.35
-%
-
 MOTION_ORIGIN= 0.0 0.0 0.0
-
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE = 0.1 0.0 0.0
-
diff --git a/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_NN.cfg b/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_NN.cfg
index 1fccb54cefe..67e13407e3d 100644
--- a/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_NN.cfg
+++ b/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_NN.cfg
@@ -6,228 +6,91 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
-%
-% Enable Multizone mode
 MULTIZONE= YES
-%
-% List of config files to specify zone options
 CONFIG_LIST= (zone_1.cfg, zone_2.cfg)
-%
-% Enable time dependent problem
 TIME_DOMAIN = YES
-%
-% Number of time steps
 TIME_ITER = 32000
-%
-% Time step
 TIME_STEP = 0.1
-%
-% Number of outer iterations (Block-Gauss-Seidel)
 OUTER_ITER = 5
-%
-% Inner iterations
 INNER_ITER= 1
+%
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)                         
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 %
-%
-%
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
 %
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 2.5
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 95750
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Free-stream Turbulence Intensity
 FREESTREAM_TURBULENCEINTENSITY = 0.1
-%
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
-%
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-%Init option to choose between Reynolds (default) or thermodynamics quantities for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
 %
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( wall )
-%
-% Riemann boundary marker(s)
-% Format inlet:  ( marker, TOTAL_CONDITIONS_PT, Total Pressure, Total Temperature, Flow dir-x, Flow dir-y, Flow dir-z)
-% Format outlet: ( marker, type, STATIC_PRESSURE, Static Pressure, 0.0, 0.0, 0.0, 0.0)
 MARKER_RIEMANN= (inlet, STATIC_SUPERSONIC_INFLOW_PT, 95750, 288.15, 2.5, 0.0, 0.0, outlet, STATIC_PRESSURE, 9575.0, 0.0, 0.0, 0.0, 0.0)
-%
-% Zone interaction boundary definition
 MARKER_ZONE_INTERFACE= ( external_interface, internal_interface)
 MARKER_FLUID_INTERFACE= ( external_interface, internal_interface)
-
-%KIND_INTERPOLATION= SLIDING_MESH
-%
-%
-% Periodic boundary marker(s) (NONE = no marker)
-% Format: ( periodic marker, donor marker, rot_cen_x, rot_cen_y, rot_cen_z, rot_angle_x-axis, rot_angle_y-axis, rot_angle_z-axis, translation_x, translation_y, translation_z)
 MARKER_SYM= ( up, down )
 %
-%
-
-%
-%
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value, CFL max value )
 CFL_ADAPT_PARAM= ( 0.3, 0.5, 1.0, 1000.0)
 %
-%
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 %
-%
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-%
-%
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
 %
-%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, ROE, AUSM, HLLC)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Entropy fix coefficient (0.0 implies no entropy fixing, 1.0 implies scalar artificial dissipation, 0.001 default)
 ENTROPY_FIX_COEFF= 0.001
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
-% Relaxation coefficient
-%
-%
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 %
-%
-%
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= cylinder.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= su2mesh_per.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
 TABULAR_FORMAT= CSV	
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 50
-%
diff --git a/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_WA.cfg b/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_WA.cfg
index d4b88aaef24..eeb8ad5166a 100644
--- a/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_WA.cfg
+++ b/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_WA.cfg
@@ -6,228 +6,93 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
-%
-% Enable Multizone mode
 MULTIZONE= YES
-%
 MULTIZONE_SOLVER=BLOCK_JACOBI
-%
-% List of config files to specify zone options
 CONFIG_LIST= (zone_1.cfg, zone_2.cfg)
-%
-% Enable time dependent problem
 TIME_DOMAIN = YES
-%
-% Number of time steps
 TIME_ITER = 32000
-%
-% Time step
 TIME_STEP = 0.1
-%
-% Number of outer iterations (Block-Gauss-Seidel)
 OUTER_ITER = 5
-%
-% Inner iterations
 INNER_ITER= 1
+%
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)                         
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 %
-%
-%
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
 %
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 2.5
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 95750
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Free-stream Turbulence Intensity
 FREESTREAM_TURBULENCEINTENSITY = 0.1
-%
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
-%
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-%Init option to choose between Reynolds (default) or thermodynamics quantities for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
 %
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= ( wall )
-%
-% Riemann boundary marker(s)
-% Format inlet:  ( marker, TOTAL_CONDITIONS_PT, Total Pressure, Total Temperature, Flow dir-x, Flow dir-y, Flow dir-z)
-% Format outlet: ( marker, type, STATIC_PRESSURE, Static Pressure, 0.0, 0.0, 0.0, 0.0)
 MARKER_RIEMANN= (inlet, STATIC_SUPERSONIC_INFLOW_PT, 95750, 288.15, 2.5, 0.0, 0.0, outlet, STATIC_PRESSURE, 9575.0, 0.0, 0.0, 0.0, 0.0)
-%
-% Zone interaction boundary definition
 MARKER_ZONE_INTERFACE= ( external_interface, internal_interface)
 MARKER_FLUID_INTERFACE= ( external_interface, internal_interface)
-
-%
 KIND_INTERPOLATION= WEIGHTED_AVERAGE
-%
-%
-% Periodic boundary marker(s) (NONE = no marker)
-% Format: ( periodic marker, donor marker, rot_cen_x, rot_cen_y, rot_cen_z, rot_angle_x-axis, rot_angle_y-axis, rot_angle_z-axis, translation_x, translation_y, translation_z)
 MARKER_SYM= ( up, down )
 %
-%
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 5.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value, CFL max value )
 CFL_ADAPT_PARAM= ( 0.3, 0.5, 1.0, 1000.0)
 %
-%
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 %
-%
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-%
-%
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
 %
-%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, ROE, AUSM, HLLC)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Entropy fix coefficient (0.0 implies no entropy fixing, 1.0 implies scalar artificial dissipation, 0.001 default)
 ENTROPY_FIX_COEFF= 0.001
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
-% Relaxation coefficient
-%
-%
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 %
-%
-%
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= cylinder.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= su2mesh_per.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
 TABULAR_FORMAT= CSV	
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 50
-%
diff --git a/TestCases/sliding_interface/supersonic_vortex_shedding/zone_1.cfg b/TestCases/sliding_interface/supersonic_vortex_shedding/zone_1.cfg
index c0c8d8075f4..143b120749b 100644
--- a/TestCases/sliding_interface/supersonic_vortex_shedding/zone_1.cfg
+++ b/TestCases/sliding_interface/supersonic_vortex_shedding/zone_1.cfg
@@ -6,19 +6,13 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
-GRID_MOVEMENT= RIGID_MOTION
 %
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
+GRID_MOVEMENT= RIGID_MOTION
 MACH_MOTION= 0.35
-%
-
 MOTION_ORIGIN= 0.0 0.0 0.0
-
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE = 0.0 0.0 0.0
diff --git a/TestCases/sliding_interface/supersonic_vortex_shedding/zone_2.cfg b/TestCases/sliding_interface/supersonic_vortex_shedding/zone_2.cfg
index 7b362521b97..f36feacbaf3 100644
--- a/TestCases/sliding_interface/supersonic_vortex_shedding/zone_2.cfg
+++ b/TestCases/sliding_interface/supersonic_vortex_shedding/zone_2.cfg
@@ -6,19 +6,13 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
-GRID_MOVEMENT= RIGID_MOTION
 %
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
+GRID_MOVEMENT= RIGID_MOTION
 MACH_MOTION= 0.35
-%
-
 MOTION_ORIGIN= 0.4 0.0 0.0
-
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE = 0.0 0.0 0.1
diff --git a/TestCases/sliding_interface/uniform_flow/uniform_NN.cfg b/TestCases/sliding_interface/uniform_flow/uniform_NN.cfg
index 8d26d03a773..437c6e59710 100644
--- a/TestCases/sliding_interface/uniform_flow/uniform_NN.cfg
+++ b/TestCases/sliding_interface/uniform_flow/uniform_NN.cfg
@@ -6,21 +6,14 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
-% Enable Multizone mode
 MULTIZONE= YES
-%
 MULTIZONE_SOLVER=BLOCK_JACOBI
-
-% List of config files to specify zone options
 CONFIG_LIST= (zone_1.cfg, zone_2.cfg)
-%
-%
 TIME_DOMAIN=YES
-%
 TIME_STEP= 1e-04
 TIME_ITER= 10
 OUTER_ITER= 120
@@ -28,203 +21,77 @@ INNER_ITER= 1
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)                         
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 %
-%
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-1ST_ORDER)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
 %
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 1E-9
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 303.15
-%
-% Free-stream Turbulence Intensity
 FREESTREAM_TURBULENCEINTENSITY = 0.1
-%
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
-%
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-%Init option to choose between Reynolds (default) or thermodynamics quantities for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
 %
-%
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Riemann boundary marker(s)
-% Format inlet:  ( marker, TOTAL_CONDITIONS_PT, Total Pressure, Total Temperature, Flow dir-x, Flow dir-y, Flow dir-z)
-% Format outlet: ( marker, type, STATIC_PRESSURE, Static Pressure, 0.0, 0.0, 0.0, 0.0)
 MARKER_RIEMANN= (inlet, TOTAL_CONDITIONS_PT, 133749, 328.23, 1.0, 0.0, 0.0 )
-%
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= (outlet)
-%
-% Zone interaction boundary definition
 MARKER_ZONE_INTERFACE= ( external_interface, internal_interface)
 MARKER_FLUID_INTERFACE= ( external_interface, internal_interface)
-
-%KIND_INTERPOLATION= SLIDING_MESH
-%
-% Periodic boundary marker(s) (NONE = no marker)
-% Format: ( periodic marker, donor marker, rot_cen_x, rot_cen_y, rot_cen_z, rot_angle_x-axis, rot_angle_y-axis, rot_angle_z-axis, translation_x, translation_y, translation_z)
 MARKER_SYM= ( up, down )
 %
-%
-
-%
-%
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 0.5
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value, CFL max value )
 CFL_ADAPT_PARAM= ( 0.3, 0.5, 1.0, 1000.0)
 %
-%
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 %
-%
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-%
-%
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
 %
-%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, ROE, AUSM, HLLC)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Entropy fix coefficient (0.0 implies no entropy fixing, 1.0 implies scalar artificial dissipation, 0.001 default)
 ENTROPY_FIX_COEFF= 0.001
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
-% Relaxation coefficient
-%
-%
-%
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 %
-%
-%
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= su2mesh_per.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 50
-%
diff --git a/TestCases/sliding_interface/uniform_flow/uniform_WA.cfg b/TestCases/sliding_interface/uniform_flow/uniform_WA.cfg
index 484c0f218af..151d70c9d31 100644
--- a/TestCases/sliding_interface/uniform_flow/uniform_WA.cfg
+++ b/TestCases/sliding_interface/uniform_flow/uniform_WA.cfg
@@ -6,21 +6,14 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
-% Enable Multizone mode
 MULTIZONE= YES
-%
 MULTIZONE_SOLVER=BLOCK_JACOBI
-
-% List of config files to specify zone options
 CONFIG_LIST= (zone_1.cfg, zone_2.cfg)
-%
-%
 TIME_DOMAIN=YES
-%
 TIME_STEP= 1e-04
 TIME_ITER= 10
 OUTER_ITER= 120
@@ -28,203 +21,77 @@ INNER_ITER= 1
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)                         
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 %
-%
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-1ST_ORDER)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
 %
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 1E-9
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 101325
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 303.15
-%
-% Free-stream Turbulence Intensity
 FREESTREAM_TURBULENCEINTENSITY = 0.1
-%
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
-%
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-%Init option to choose between Reynolds (default) or thermodynamics quantities for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
 %
-%
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Riemann boundary marker(s)
-% Format inlet:  ( marker, TOTAL_CONDITIONS_PT, Total Pressure, Total Temperature, Flow dir-x, Flow dir-y, Flow dir-z)
-% Format outlet: ( marker, type, STATIC_PRESSURE, Static Pressure, 0.0, 0.0, 0.0, 0.0)
 MARKER_RIEMANN= (inlet, TOTAL_CONDITIONS_PT, 133749, 328.23, 1.0, 0.0, 0.0 )
-%
-% Euler wall boundary marker(s) (NONE = no marker)
 MARKER_EULER= (outlet)
-%
-% Zone interaction boundary definition
 MARKER_ZONE_INTERFACE= ( external_interface, internal_interface)
 MARKER_FLUID_INTERFACE= ( external_interface, internal_interface)
-
 KIND_INTERPOLATION= WEIGHTED_AVERAGE
-%
-% Periodic boundary marker(s) (NONE = no marker)
-% Format: ( periodic marker, donor marker, rot_cen_x, rot_cen_y, rot_cen_z, rot_angle_x-axis, rot_angle_y-axis, rot_angle_z-axis, translation_x, translation_y, translation_z)
 MARKER_SYM= ( up, down )
 %
-%
-
-%
-%
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 0.5
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value, CFL max value )
 CFL_ADAPT_PARAM= ( 0.3, 0.5, 1.0, 1000.0)
 %
-%
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 %
-%
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-%
-%
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
 %
-%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, ROE, AUSM, HLLC)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Entropy fix coefficient (0.0 implies no entropy fixing, 1.0 implies scalar artificial dissipation, 0.001 default)
 ENTROPY_FIX_COEFF= 0.001
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
-% Relaxation coefficient
-%
-%
-%
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 %
-%
-%
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= su2mesh_per.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 50
-%
diff --git a/TestCases/sliding_interface/uniform_flow/zone_1.cfg b/TestCases/sliding_interface/uniform_flow/zone_1.cfg
index 9c6d3ea1f5c..f6ee9f723a3 100644
--- a/TestCases/sliding_interface/uniform_flow/zone_1.cfg
+++ b/TestCases/sliding_interface/uniform_flow/zone_1.cfg
@@ -6,20 +6,13 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT= RIGID_MOTION
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.35
-%
-
 MOTION_ORIGIN= 0.3 0.0 0.0
-
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE = 0.0 0.0 0.0
diff --git a/TestCases/sliding_interface/uniform_flow/zone_2.cfg b/TestCases/sliding_interface/uniform_flow/zone_2.cfg
index c0e492dd475..41be07d38ed 100644
--- a/TestCases/sliding_interface/uniform_flow/zone_2.cfg
+++ b/TestCases/sliding_interface/uniform_flow/zone_2.cfg
@@ -6,20 +6,13 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT= RIGID_MOTION
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.35
-%
-
 MOTION_ORIGIN= 0.3 0.0 0.0
-
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE = 0.0 0.0 160.0
diff --git a/TestCases/solid_heat_conduction/periodic_pins/configSolid.cfg b/TestCases/solid_heat_conduction/periodic_pins/configSolid.cfg
index 062aae7753c..7c712870421 100644
--- a/TestCases/solid_heat_conduction/periodic_pins/configSolid.cfg
+++ b/TestCases/solid_heat_conduction/periodic_pins/configSolid.cfg
@@ -5,17 +5,15 @@
 % Author: T. Kattmann                                                          %
 % Institution: Bosch Thermotechniek B.V.                                       %
 % Date: 2021.09.27                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
 SOLVER= HEAT_EQUATION
-%
 OBJECTIVE_FUNCTION= AVG_TEMPERATURE
 OBJECTIVE_WEIGHT= 1.0
-%
 OPT_OBJECTIVE= AVG_TOTALTEMP
 %
 % ---------------- (SOLIDS) CONDUCTION CONDITION DEFINITION -------------------%
@@ -45,7 +43,6 @@ MARKER_MONITORING = ( solid_pin1_inner, solid_pin3_inner )
 %
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-%NUM_METHOD_GRAD= GREEN_GAUSS
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 CFL_NUMBER= 1e8
 %
@@ -71,12 +68,9 @@ TIME_DISCRE_HEAT= EULER_IMPLICIT
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
 MESH_FILENAME= solid.su2
-%
 SCREEN_OUTPUT= INNER_ITER, RMS_TEMPERATURE, MAX_TEMPERATURE, AVG_TEMPERATURE, TOTAL_HEATFLUX, MAXIMUM_HEATFLUX, LINSOL_ITER, LINSOL_RESIDUAL
 SCREEN_WRT_FREQ_INNER= 50
-%
 HISTORY_OUTPUT= (ITER, RMS_RES, HEAT, LINSOL)
-%
 OUTPUT_FILES= RESTART, PARAVIEW_MULTIBLOCK
 VOLUME_OUTPUT= RESIDUAL
 OUTPUT_WRT_FREQ= 1000
diff --git a/TestCases/species_transport/multizone/configMaster.cfg b/TestCases/species_transport/multizone/configMaster.cfg
index abb71982e9d..141133ddb96 100644
--- a/TestCases/species_transport/multizone/configMaster.cfg
+++ b/TestCases/species_transport/multizone/configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: N. Beishuizen                                                         %
 % Institution: Technische Universiteit Eindhoven                                %
 % Date: November 1, 2022                                                        %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
@@ -15,6 +15,7 @@ CONFIG_LIST = (zone1.cfg, zone2.cfg)
 MARKER_ZONE_INTERFACE=  (ILEFT, IRIGHT)
 MARKER_FLUID_INTERFACE= (ILEFT, IRIGHT)
 OUTER_ITER = 100
+%
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
 NUM_METHOD_GRAD= GREEN_GAUSS
@@ -69,5 +70,3 @@ OUTPUT_WRT_FREQ= (100,200)
 VOLUME_OUTPUT= COORDINATES, SOLUTION
 MARKER_ANALYZE= air_axial_inlet1, gas_inlet1
 MARKER_ANALYZE_AVERAGE=MASSFLUX
-
-%
diff --git a/TestCases/species_transport/multizone/zone1.cfg b/TestCases/species_transport/multizone/zone1.cfg
index 30336f582c8..50c6e455e4c 100644
--- a/TestCases/species_transport/multizone/zone1.cfg
+++ b/TestCases/species_transport/multizone/zone1.cfg
@@ -46,4 +46,3 @@ PRANDTL_TURB= 0.90, 0.90, 0.90
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
 MU_CONSTANT=  (1.716E-5, 1.82e-5, 1.85e-5)
 MIXING_VISCOSITY_MODEL= WILKE
-%
diff --git a/TestCases/species_transport/multizone/zone2.cfg b/TestCases/species_transport/multizone/zone2.cfg
index b60ac3893e4..622685ab51f 100644
--- a/TestCases/species_transport/multizone/zone2.cfg
+++ b/TestCases/species_transport/multizone/zone2.cfg
@@ -46,4 +46,3 @@ PRANDTL_TURB= 0.90, 0.90, 0.90
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
 MU_CONSTANT=  (1.716E-5, 1.82e-5, 1.85e-5)
 MIXING_VISCOSITY_MODEL= WILKE
-%
diff --git a/TestCases/species_transport/passive_transport_validation/passive_transport.cfg b/TestCases/species_transport/passive_transport_validation/passive_transport.cfg
index cd293c4ca18..2ee2aded9d2 100644
--- a/TestCases/species_transport/passive_transport_validation/passive_transport.cfg
+++ b/TestCases/species_transport/passive_transport_validation/passive_transport.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Bosch Thermotechniek B.V                                        %
 % Date: 2021.10.02                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -74,7 +74,7 @@ LINEAR_SOLVER= FGMRES
 LINEAR_SOLVER_PREC= ILU
 LINEAR_SOLVER_ERROR= 1E-5
 LINEAR_SOLVER_ITER= 10
-
+%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= FDS
@@ -94,7 +94,6 @@ MESH_FILENAME = rectangle_mixing.su2
 %
 CUSTOM_OUTPUTS = 'avg_species : MassFlowAvg{SPECIES[0]}[outlet];\
                   avg_check : Function{avg_species - SURFACE_SPECIES_0}'
-%
 SCREEN_OUTPUT = INNER_ITER WALL_TIME RMS_RES LINSOL CUSTOM
 SCREEN_WRT_FREQ_INNER= 10
 %
diff --git a/TestCases/species_transport/venturi_primitive_3species/DAspecies3_primitiveVenturi.cfg b/TestCases/species_transport/venturi_primitive_3species/DAspecies3_primitiveVenturi.cfg
index 16e3ef50617..7d2b486798e 100644
--- a/TestCases/species_transport/venturi_primitive_3species/DAspecies3_primitiveVenturi.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/DAspecies3_primitiveVenturi.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Bosch Thermotechniek B.V.                                       %
 % Date: 2021/10/14                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -80,7 +80,7 @@ LINEAR_SOLVER= FGMRES
 LINEAR_SOLVER_PREC= ILU
 LINEAR_SOLVER_ERROR= 1E-8
 LINEAR_SOLVER_ITER= 20
-
+%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= FDS
@@ -119,7 +119,6 @@ CONV_STARTITER= 10
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
 MESH_FILENAME= primitiveVenturi.su2
-%
 SCREEN_OUTPUT= INNER_ITER WALL_TIME RMS_ADJ_PRESSURE RMS_ADJ_VELOCITY-X RMS_ADJ_VELOCITY-Y RMS_ADJ_TKE RMS_ADJ_DISSIPATION RMS_ADJ_SPECIES_0 RMS_ADJ_SPECIES_1
 SCREEN_WRT_FREQ_INNER= 10
 %
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi.cfg
index 5389af6355d..e35c8080a35 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Bosch Thermotechniek B.V.                                       %
 % Date: 2021/10/14                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -71,7 +71,7 @@ LINEAR_SOLVER= FGMRES
 LINEAR_SOLVER_PREC= ILU
 LINEAR_SOLVER_ERROR= 1E-8
 LINEAR_SOLVER_ITER= 5
-
+%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= FDS
@@ -110,7 +110,6 @@ CONV_STARTITER= 10
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
 MESH_FILENAME= primitiveVenturi.su2
-%
 SCREEN_OUTPUT= INNER_ITER WALL_TIME \
                RMS_PRESSURE RMS_VELOCITY-X RMS_VELOCITY-Y RMS_TKE RMS_DISSIPATION RMS_SPECIES_0 \
                LINSOL_ITER LINSOL_RESIDUAL \
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_boundedscalar.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_boundedscalar.cfg
index 3055bfd0719..17019cef8b9 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_boundedscalar.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_boundedscalar.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Bosch Thermotechniek B.V.                                       %
 % Date: 2021/10/14                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -71,7 +71,7 @@ LINEAR_SOLVER= FGMRES
 LINEAR_SOLVER_PREC= ILU
 LINEAR_SOLVER_ERROR= 1E-8
 LINEAR_SOLVER_ITER= 5
-
+%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= FDS
@@ -110,7 +110,6 @@ CONV_STARTITER= 10
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
 MESH_FILENAME= primitiveVenturi.su2
-%
 SCREEN_OUTPUT= INNER_ITER WALL_TIME \
                RMS_PRESSURE RMS_VELOCITY-X RMS_VELOCITY-Y RMS_TKE RMS_DISSIPATION RMS_SPECIES_0 \
                LINSOL_ITER LINSOL_RESIDUAL \
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel.cfg
index 53f2764f995..b28ffaafaff 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel.cfg
@@ -7,7 +7,7 @@
 % Author: Cristopher Morales Ubal                                              %
 % Institution: Eindhoven University of Technology                              %
 % Date: 2022/06/15                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -83,7 +83,7 @@ LINEAR_SOLVER= FGMRES
 LINEAR_SOLVER_PREC= ILU
 LINEAR_SOLVER_ERROR= 1E-8
 LINEAR_SOLVER_ITER= 5
-
+%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= FDS
@@ -122,7 +122,6 @@ CONV_STARTITER= 10
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
 MESH_FILENAME= primitiveVenturi.su2
-%
 SCREEN_OUTPUT= INNER_ITER WALL_TIME \
                RMS_PRESSURE RMS_VELOCITY-X RMS_VELOCITY-Y RMS_TKE RMS_DISSIPATION RMS_SPECIES_0 \
                LINSOL_ITER LINSOL_RESIDUAL \
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg
index f4fb7f77897..e4908b58a25 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg
@@ -8,7 +8,7 @@
 % Author: Cristopher Morales Ubal                                              %
 % Institution: Eindhoven University of Technology                              %
 % Date: 2022/12/05                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_boundedscalar.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_boundedscalar.cfg
index f51545a1174..9e215bf1871 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_boundedscalar.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_boundedscalar.cfg
@@ -7,7 +7,7 @@
 % Author: Cristopher Morales Ubal                                              %
 % Institution: Eindhoven University of Technology                              %
 % Date: 2022/06/15                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -83,7 +83,7 @@ LINEAR_SOLVER= FGMRES
 LINEAR_SOLVER_PREC= ILU
 LINEAR_SOLVER_ERROR= 1E-8
 LINEAR_SOLVER_ITER= 5
-
+%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= FDS
@@ -122,7 +122,6 @@ CONV_STARTITER= 10
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
 MESH_FILENAME= primitiveVenturi.su2
-%
 SCREEN_OUTPUT= INNER_ITER WALL_TIME \
                RMS_PRESSURE RMS_VELOCITY-X RMS_VELOCITY-Y RMS_TKE RMS_DISSIPATION RMS_SPECIES_0 \
                LINSOL_ITER LINSOL_RESIDUAL \
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg
index 24b943f677b..087cc340b77 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg
@@ -8,7 +8,7 @@
 % Author: Cristopher Morales Ubal                                              %
 % Institution: Eindhoven University of Technology                              %
 % Date: 2022/09/12                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -94,7 +94,7 @@ LINEAR_SOLVER= FGMRES
 LINEAR_SOLVER_PREC= ILU
 LINEAR_SOLVER_ERROR= 1E-8 
 LINEAR_SOLVER_ITER= 30
-
+%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= FDS
@@ -133,7 +133,6 @@ CONV_STARTITER= 10
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
 MESH_FILENAME= primitiveVenturi.su2
-%
 SCREEN_OUTPUT= INNER_ITER WALL_TIME \
                RMS_PRESSURE RMS_VELOCITY-X RMS_VELOCITY-Y RMS_TKE RMS_DISSIPATION RMS_SPECIES_0 RMS_SPECIES_1 \
                LINSOL_ITER LINSOL_RESIDUAL \
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg
index 0f53f027374..9371a65af33 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg
@@ -9,7 +9,7 @@
 % Author: Cristopher Morales Ubal                                              %
 % Institution: Eindhoven University of Technology                              %
 % Date: 2022/10/12                                                            %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -95,7 +95,7 @@ LINEAR_SOLVER= FGMRES
 LINEAR_SOLVER_PREC= ILU
 LINEAR_SOLVER_ERROR= 1E-8 
 LINEAR_SOLVER_ITER= 30
-
+%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= FDS
@@ -134,7 +134,6 @@ CONV_STARTITER= 10
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
 MESH_FILENAME= primitiveVenturi.su2
-%
 SCREEN_OUTPUT= INNER_ITER WALL_TIME \
                RMS_PRESSURE RMS_VELOCITY-X RMS_VELOCITY-Y RMS_TKE RMS_DISSIPATION RMS_SPECIES_0 RMS_SPECIES_1 \
                LINSOL_ITER LINSOL_RESIDUAL \
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_viscosity.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_viscosity.cfg
index e92a8c9088c..6101b0fb652 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_viscosity.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_viscosity.cfg
@@ -7,7 +7,7 @@
 % Author: Cristopher Morales Ubal                                              %
 % Institution: Eindhoven University of Technology                              %
 % Date: 2022/06/27                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -88,7 +88,7 @@ LINEAR_SOLVER= FGMRES
 LINEAR_SOLVER_PREC= ILU
 LINEAR_SOLVER_ERROR= 1E-8 
 LINEAR_SOLVER_ITER= 5
-
+%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= FDS
@@ -127,7 +127,6 @@ CONV_STARTITER= 10
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
 MESH_FILENAME= primitiveVenturi.su2
-%
 SCREEN_OUTPUT= INNER_ITER WALL_TIME \
                RMS_PRESSURE RMS_VELOCITY-X RMS_VELOCITY-Y RMS_TKE RMS_DISSIPATION RMS_SPECIES_0 RMS_SPECIES_1 \
                LINSOL_ITER LINSOL_RESIDUAL \
diff --git a/TestCases/species_transport/venturi_primitive_3species/species3_primitiveVenturi.cfg b/TestCases/species_transport/venturi_primitive_3species/species3_primitiveVenturi.cfg
index 0d00c644b16..6f6cdea604b 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species3_primitiveVenturi.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species3_primitiveVenturi.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Bosch Thermotechniek B.V.                                       %
 % Date: 2021/10/14                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -74,7 +74,7 @@ LINEAR_SOLVER= FGMRES
 LINEAR_SOLVER_PREC= ILU
 LINEAR_SOLVER_ERROR= 1E-8
 LINEAR_SOLVER_ITER= 5
-
+%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= FDS
@@ -113,7 +113,6 @@ CONV_STARTITER= 10
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
 MESH_FILENAME= primitiveVenturi.su2
-%
 SCREEN_OUTPUT= INNER_ITER WALL_TIME \
                RMS_PRESSURE RMS_VELOCITY-X RMS_VELOCITY-Y RMS_TKE RMS_DISSIPATION RMS_SPECIES_0 RMS_SPECIES_1 \
                LINSOL_ITER LINSOL_RESIDUAL \
diff --git a/TestCases/species_transport/venturi_primitive_3species/species3_primitiveVenturi_inletFile.cfg b/TestCases/species_transport/venturi_primitive_3species/species3_primitiveVenturi_inletFile.cfg
index c1cf37ab1a6..a36f4447503 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species3_primitiveVenturi_inletFile.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species3_primitiveVenturi_inletFile.cfg
@@ -6,7 +6,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Bosch Thermotechniek B.V.                                       %
 % Date: 2021/10/14                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -76,7 +76,7 @@ LINEAR_SOLVER= FGMRES
 LINEAR_SOLVER_PREC= ILU
 LINEAR_SOLVER_ERROR= 1E-8
 LINEAR_SOLVER_ITER= 5
-
+%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= FDS
@@ -115,7 +115,6 @@ CONV_STARTITER= 10
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
 MESH_FILENAME= primitiveVenturi.su2
-%
 SCREEN_OUTPUT= INNER_ITER WALL_TIME \
                RMS_PRESSURE RMS_VELOCITY-X RMS_VELOCITY-Y RMS_TKE RMS_DISSIPATION RMS_SPECIES_0 RMS_SPECIES_1 \
                LINSOL_ITER LINSOL_RESIDUAL \
diff --git a/TestCases/transition/E387_Airfoil/transitional_BC_model_ConfigFile.cfg b/TestCases/transition/E387_Airfoil/transitional_BC_model_ConfigFile.cfg
index 6494b94528b..80c94d0f3a1 100644
--- a/TestCases/transition/E387_Airfoil/transitional_BC_model_ConfigFile.cfg
+++ b/TestCases/transition/E387_Airfoil/transitional_BC_model_ConfigFile.cfg
@@ -2,234 +2,103 @@
 %                                                                              %
 % SU2 configuration file                                                       %
 % Case description: Eppler E387 Airfoil at Re = 200K                           %
-% Author: Samet Cakmakcioglu	                                                 %
-% Institution: TOBB University of Economics and Technology             		     %	
-%			   TAI-TUSAS Turkish Aerospace Industries 						                   %
+% Author: Samet Cakmakcioglu                                                   %
+% Institution: TOBB University of Economics and Technology                     %	
+%			   TAI-TUSAS Turkish Aerospace Industries                          %
 % Date: Oct 10th, 2016                                                         %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= INC_RANS
-%
-% Specify turbulence model
 KIND_TURB_MODEL= SA
 SA_OPTIONS= BCM
 FREESTREAM_TURBULENCEINTENSITY = 0.1
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % -------------------- INCOMPRESSIBLE FREE-STREAM DEFINITION ------------------%
 %
-% Free-stream density (1.2886 Kg/m^3 (air), 998.2 Kg/m^3 (water))
 FREESTREAM_DENSITY= 1.2
-%
-% Free-stream velocity (m/s)
 FREESTREAM_VELOCITY= ( 3.0, 0.00, 0.00 )
-%
-% Free-stream viscosity (1.853E-5 Ns/m^2 (air), 0.798E-3 Ns/m^2 (water))
 FREESTREAM_VISCOSITY= 1.8e-05
-
 REF_DIMENSIONALIZATION= DIMENSIONAL
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
-
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 100.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 EXT_ITER= 1000000
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.01
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= FDS
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -20
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= e387_Ogrid.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
diff --git a/TestCases/transition/Schubauer_Klebanoff/transitional_BC_model_ConfigFile.cfg b/TestCases/transition/Schubauer_Klebanoff/transitional_BC_model_ConfigFile.cfg
index 4bbea2c9c8a..32cb81910fa 100644
--- a/TestCases/transition/Schubauer_Klebanoff/transitional_BC_model_ConfigFile.cfg
+++ b/TestCases/transition/Schubauer_Klebanoff/transitional_BC_model_ConfigFile.cfg
@@ -6,265 +6,109 @@
 % Institution: TOBB University of Economics and Technology                     %	
 %              TAI-TUSAS Turkish Aerospace Industries                          %
 % Date: Oct 10th, 2016                                                         %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= INC_RANS
-%
-% Specify turbulence model
 KIND_TURB_MODEL= SA
 SA_OPTIONS= BCM
 FREESTREAM_TURBULENCEINTENSITY = 0.18
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
-% Initial density for incompressible flows (1.2886 kg/m^3 by default)
 INC_DENSITY_INIT= 1.2
-%
-% Initial velocity for incompressible flows (1.0,0,0 m/s by default)
 INC_VELOCITY_INIT= ( 50.1, 0.0, 0.0 )
-%
-% List of inlet types for incompressible flows. List length must
-% match number of inlet markers. Options: VELOCITY_INLET, PRESSURE_INLET.
 INC_INLET_TYPE= VELOCITY_INLET
-%
-% Damping coefficient for iterative updates at pressure inlets. (0.1 by default)
 INC_INLET_DAMPING= 0.1
-%
-% List of outlet types for incompressible flows. List length must
-% match number of outlet markers. Options: PRESSURE_OUTLET, MASS_FLOW_OUTLET
 INC_OUTLET_TYPE= PRESSURE_OUTLET PRESSURE_OUTLET
-%
-% Damping coefficient for iterative updates at mass flow outlets. (0.1 by default)
 INC_OUTLET_DAMPING= 0.1
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.8e-05
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.5
 
-
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( wall, 0.0 )
-%
-% Symmetry Boundary condition
 MARKER_SYM = (symmetry)
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
 MARKER_OUTLET= ( outlet, 0, farfield, 0 )
-%
-% Inlet boundary marker(s) with the following formats (NONE = no marker) 
-% Total Conditions: (inlet marker, total temp, total pressure, flow_direction_x, 
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-% Mass Flow: (inlet marker, density, velocity magnitude, flow_direction_x, 
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-% Incompressible: (inlet marker, NULL, velocity magnitude, flow_direction_x,
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
 MARKER_INLET= ( inlet, 0.0, 50.1, 1.0, 0.0, 0.0)
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( wall )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( wall )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 100.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 ITER= 250000
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.01
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= FDS
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -20
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= grid.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 500
-%
-% Screen output 
 SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_NU_TILDE, LIFT, DRAG)
diff --git a/TestCases/transition/T3A_FlatPlate/transitional_BC_model_ConfigFile.cfg b/TestCases/transition/T3A_FlatPlate/transitional_BC_model_ConfigFile.cfg
index e93d96491bb..42b8775f6b6 100644
--- a/TestCases/transition/T3A_FlatPlate/transitional_BC_model_ConfigFile.cfg
+++ b/TestCases/transition/T3A_FlatPlate/transitional_BC_model_ConfigFile.cfg
@@ -2,253 +2,106 @@
 %                                                                              %
 % SU2 configuration file                                                       %
 % Case description: T3A Flat Plate Bypass Transition                           %
-% Author: Samet Cakmakcioglu	                                                 %
-% Institution: TOBB University of Economics and Technology             		     %	
-%			   TAI-TUSAS Turkish Aerospace Industries 						                   %
+% Author: Samet Cakmakcioglu                                                   %
+% Institution: TOBB University of Economics and Technology                     %	
+%			   TAI-TUSAS Turkish Aerospace Industries                          %
 % Date: Oct 10th, 2016                                                         %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= INC_RANS
-%
-% Specify turbulence model
 KIND_TURB_MODEL= SA
 SA_OPTIONS= BCM
 FREESTREAM_TURBULENCEINTENSITY = 3.0
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % -------------------- INCOMPRESSIBLE FREE-STREAM DEFINITION ------------------%
 %
-% Free-stream density (1.2886 Kg/m^3 (air), 998.2 Kg/m^3 (water))
 FREESTREAM_DENSITY= 1.2
-%
-% Free-stream velocity (m/s)
 FREESTREAM_VELOCITY= ( 5.4, 0.00, 0.00 )
-%
-% Free-stream viscosity (1.853E-5 Ns/m^2 (air), 0.798E-3 Ns/m^2 (water))
 FREESTREAM_VISCOSITY= 1.8e-05
-
 REF_DIMENSIONALIZATION= DIMENSIONAL
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.5
 
-
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( wall, 0.0 )
-%
-% Symmetry Boundary condition
 MARKER_SYM = (symmetry)
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
 MARKER_OUTLET= ( outlet, 0, farfield, 0 )
-%
-% Inlet boundary type (TOTAL_CONDITIONS, MASS_FLOW)
 INLET_TYPE= MASS_FLOW
-%
-% Inlet boundary marker(s) with the following formats (NONE = no marker) 
-% Total Conditions: (inlet marker, total temp, total pressure, flow_direction_x, 
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-% Mass Flow: (inlet marker, density, velocity magnitude, flow_direction_x, 
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-% Incompressible: (inlet marker, NULL, velocity magnitude, flow_direction_x,
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
 MARKER_INLET= ( inlet, 1.2, 5.4, 1.0, 0.0, 0.0)
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( wall )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( wall )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 100.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Number of total iterations
 EXT_ITER= 250000
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.01
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= FDS
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -20
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= grid.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 500
-%
diff --git a/TestCases/turbomachinery/APU_turbocharger/Jones_restart.cfg b/TestCases/turbomachinery/APU_turbocharger/Jones_restart.cfg
index 73fd8e2e482..5f0ae291a78 100755
--- a/TestCases/turbomachinery/APU_turbocharger/Jones_restart.cfg
+++ b/TestCases/turbomachinery/APU_turbocharger/Jones_restart.cfg
@@ -5,7 +5,7 @@
 % Author: S. Vitale                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: Jun 28th, 2017                                                         %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
@@ -19,6 +19,7 @@ KIND_TURB_MODEL= SST
 MATH_PROBLEM= DIRECT
 RESTART_SOL= YES
 DISCARD_INFILES= YES
+%
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
 MACH_NUMBER= 0.05
@@ -69,6 +70,7 @@ MARKER_MIXINGPLANE_INTERFACE= (OUTMIX, INMIX)
 MARKER_GILES= (INFLOW, TOTAL_CONDITIONS_PT, 413.6E+03, 477.6, 1.0, 0.0, 0.0, 1.0, 0.0, OUTMIX, MIXING_OUT, 0.0, 0.0, 0.0, 0.0, 0.0, 0.3, 0.0, INMIX, MIXING_IN, 0.0, 0.0, 0.0, 0.0, 0.0, 0.3, 0.0, OUTFLOW, STATIC_PRESSURE_1D, 67.46E+03, 0.0, 0.0, 0.0, 0.0 , 1.0, 0.0)
 GILES_EXTRA_RELAXFACTOR= (0.05, 0.05)
 SPATIAL_FOURIER= NO
+%
 %---------------------------- TURBOMACHINERY SIMULATION -----------------------------%
 %
 TURBOMACHINERY_KIND= CENTRIPETAL CENTRIPETAL_AXIAL
@@ -81,7 +83,6 @@ PERFORMANCE_AVERAGE_PROCESS_KIND= MIXEDOUT
 MIXEDOUT_COEFF= (1.0, 1.0E-05, 15)
 AVERAGE_MACH_LIMIT= 0.05
 %
-%
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
 MARKER_PLOTTING= (BLADE1, BLADE2)
@@ -100,9 +101,7 @@ LINEAR_SOLVER_PREC= LU_SGS
 LINEAR_SOLVER_ERROR= 1E-4
 LINEAR_SOLVER_ITER= 10
 %
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% ----------- NOT WORKING WITH PERIODIC BOUNDARY CONDITIONS !!!!! --------------%
+% ----------- NOT WORKING WITH PERIODIC BOUNDARY CONDITIONS !!!!! -------------%
 %
 %
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
@@ -151,5 +150,4 @@ VOLUME_ADJ_FILENAME= adjoint
 GRAD_OBJFUNC_FILENAME= of_grad.dat
 SURFACE_FILENAME= surface_flow
 SURFACE_ADJ_FILENAME= surface_adjoint
-OUTPUT_WRT_FREQ= 100
-%
+OUTPUT_WRT_FREQ= 100
\ No newline at end of file
diff --git a/TestCases/turbomachinery/APU_turbocharger/rotor.cfg b/TestCases/turbomachinery/APU_turbocharger/rotor.cfg
index fa77fa7de24..e1b64c618bf 100644
--- a/TestCases/turbomachinery/APU_turbocharger/rotor.cfg
+++ b/TestCases/turbomachinery/APU_turbocharger/rotor.cfg
@@ -1,18 +1,7 @@
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-%
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT= ROTATING_FRAME
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.35
-%
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE= 0.0 0.0 7508.3 
-
-% Specify ramp option fr rotating frame (YES, NO) default NO
 RAMP_ROTATING_FRAME= YES
-%
-% Parameters of the rotating frame ramp (starting rotational speed, updating-iteration-frequency, total number of iteration for the ramp)
 RAMP_ROTATING_FRAME_COEFF= (0.0, 39.0, 500)
diff --git a/TestCases/turbomachinery/APU_turbocharger/rotor_restart.cfg b/TestCases/turbomachinery/APU_turbocharger/rotor_restart.cfg
index 18ca1a4e4cb..df0cc236545 100644
--- a/TestCases/turbomachinery/APU_turbocharger/rotor_restart.cfg
+++ b/TestCases/turbomachinery/APU_turbocharger/rotor_restart.cfg
@@ -1,18 +1,7 @@
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-%
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT= ROTATING_FRAME
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.35
-%
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE= 0.0 0.0 7508.3 
-
-% Specify ramp option fr rotating frame (YES, NO) default NO
 RAMP_ROTATING_FRAME= NO
-%
-% Parameters of the rotating frame ramp (starting rotational speed, updating-iteration-frequency, total number of iteration for the ramp)
 RAMP_ROTATING_FRAME_COEFF= (0.0, 39.0, 500)
diff --git a/TestCases/turbomachinery/APU_turbocharger/stator.cfg b/TestCases/turbomachinery/APU_turbocharger/stator.cfg
index 3fcbeda15ea..caae5fd8bc4 100644
--- a/TestCases/turbomachinery/APU_turbocharger/stator.cfg
+++ b/TestCases/turbomachinery/APU_turbocharger/stator.cfg
@@ -1,7 +1,3 @@
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-%
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT= ROTATING_FRAME
-%
-
diff --git a/TestCases/turbomachinery/axial_stage_2D/Axial_stage2D.cfg b/TestCases/turbomachinery/axial_stage_2D/Axial_stage2D.cfg
index 965d1f44f64..eadd07d2631 100755
--- a/TestCases/turbomachinery/axial_stage_2D/Axial_stage2D.cfg
+++ b/TestCases/turbomachinery/axial_stage_2D/Axial_stage2D.cfg
@@ -5,125 +5,64 @@
 % Author: S. Vitale                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: Feb 28th, 2017                                                         %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
-% Enable multizone mode
 MULTIZONE= YES
-%
-% List of config files
 CONFIG_LIST= (zone_1.cfg, zone_2.cfg)
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
-%                               POISSON_EQUATION)                         
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SST)
 KIND_TURB_MODEL= SST
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 %
-%
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.05
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 140000.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE=  300.0
-%
-% Free-stream temperature (1.2886 Kg/m3 by default)
 FREESTREAM_DENSITY= 1.7418
-%
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-% Free-stream Turbulence Intensity
 FREESTREAM_TURBULENCEINTENSITY = 0.03
-%
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
-%
-%Init option to choose between Reynolds (default) or thermodynamics quantities for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
 %
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
-%
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= DIMENSIONAL
 %
-%
 % ------------------------------ EQUATION OF STATE ----------------------------%
 %
-% Different gas model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS)
 FLUID_MODEL= IDEAL_GAS
-%
-% Ratio of specific heats (1.4 default and the value is hardcoded
-%                          for the model STANDARD_AIR)
 GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.058 J/kg*K default and this value is hardcoded 
-%                        for the model STANDARD_AIR)
 GAS_CONSTANT= 287.058
 %
-%
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= SUTHERLAND
-%
-% Sutherland Viscosity Ref (1.716E-5 default value for AIR SI)
 MU_REF= 1.716E-5
-%
-% Sutherland Temperature Ref (273.15 K default value for AIR SI)
 MU_T_REF= 273.15
-%
-% Sutherland constant (110.4 default value for AIR SI)
 SUTHERLAND_CONSTANT= 110.4
 %
-%
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
-% Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL).
 CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
 %
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( wall1, 0.0, wall2, 0.0)
 %
-% Periodic boundary marker(s) (NONE = no marker)
-% Format: ( periodic marker, donor marker, rot_cen_x, rot_cen_y, rot_cen_z, rot_angle_x-axis, rot_angle_y-axis, rot_angle_z-axis, translation_x, translation_y, translation_z)
 MARKER_PERIODIC= ( periodic1, periodic2, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.04463756775, 0.0, periodic3, periodic4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.04463756775, 0.0)
 %
-%
 %-------- INFLOW/OUTFLOW BOUNDARY CONDITION SPECIFIC FOR TURBOMACHINERY --------%
 %
 % Inflow and Outflow markers must be specified, for each blade (zone), following the natural groth of the machine (i.e, from the first blade to the last)
@@ -132,199 +71,85 @@ MARKER_TURBOMACHINERY= (inflow, outmix, inmix, outflow)
 % Mixing-plane interface markers must be specified to activate the transfer of information between zones
 MARKER_MIXINGPLANE_INTERFACE= (outmix, inmix)
 %
-% Giles boundary condition for inflow, outfolw and mixing-plane
-% Format inlet:  ( marker, TOTAL_CONDITIONS_PT, Total Pressure , Total Temperature, Flow dir-norm, Flow dir-tang, Flow dir-span, under-relax-avg, under-relax-fourier)
-% Format outlet: ( marker, STATIC_PRESSURE, Static Pressure value, -, -, -, -, under-relax-avg, under-relax-fourier)
-% Format mixing-plane in and out: ( marker, MIXING_IN or MIXING_OUT, -, -, -, -, -, -, under-relax-avg, under-relax-fourier)
 MARKER_GILES= (inflow, TOTAL_CONDITIONS_PT, 169623.33, 305.76, 1.0, 0.0, 0.0,1.0,1.0, outmix, MIXING_OUT, 0.0, 0.0, 0.0, 0.0, 0.0,1.0,1.0, inmix, MIXING_IN, 0.0, 0.0, 0.0, 0.0, 0.0,1.0, 1.0 outflow, STATIC_PRESSURE, 99741.00, 0.0, 0.0, 0.0, 0.0,1.0,1.0)
-%
-%YES Non reflectivity activated, NO the Giles BC behaves as a normal 1D characteristic-based BC
 SPATIAL_FOURIER= NO
 %
-%
 %---------------------------- TURBOMACHINERY SIMULATION -----------------------------%
 %
-% Specify kind of architecture (AXIAL, CENTRIPETAL, CENTRIFUGAL, CENTRIPETAL_AXIAL)
 TURBOMACHINERY_KIND= AXIAL AXIAL
-%
-% Specify option for turbulent mixing-plane (YES, NO) default NO
 TURBULENT_MIXINGPLANE= YES
-%
-% Specify ramp option for Outlet pressure (YES, NO) default NO
 RAMP_OUTLET_PRESSURE= NO
-%
-% Parameters of the outlet pressure ramp (starting outlet pressure, updating-iteration-frequency, total number of iteration for the ramp)
 RAMP_OUTLET_PRESSURE_COEFF= (140000.0, 10.0, 2000)
-%
-% Specify Kind of average process for linearizing the Navier-Stokes equation at inflow and outflow BC included mixing-plane
-% (ALGEBRAIC, AREA, MASSSFLUX, MIXEDOUT) default AREA 
 AVERAGE_PROCESS_KIND= MIXEDOUT
-%
-% Specify Kind of average process for computing turbomachienry performance parameters
-% (ALGEBRAIC, AREA, MASSSFLUX, MIXEDOUT) default AREA
 PERFORMANCE_AVERAGE_PROCESS_KIND= MIXEDOUT
-%
-%Parameters of the Newton method for the MIXEDOUT average algorithm (under relaxation factor, tollerance, max number of iterations) 
 MIXEDOUT_COEFF= (1.0, 1.0E-05, 15)
-%
-% Limit of Mach number below which the mixedout algorithm is substituted with a AREA average algorithm
 AVERAGE_MACH_LIMIT= 0.05
 %
-%
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING= (wall1, wall2)
 %
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value, CFL max value )
 CFL_ADAPT_PARAM= ( 1.3, 1.2, 1.0, 10.0)
 %
-
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 10
 %
-%
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% ----------- NOT WORKING WITH PERIODIC BOUNDARY CONDITIONS !!!!! --------------%
+% ---------- NOT WORKING WITH PERIODIC BOUNDARY CONDITIONS !!!!! --------------%
 %
 %
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
 %
-%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= VAN_ALBADA_EDGE
-%
-% Entropy fix coefficient (0.0 implies no entropy fixing, 1.0 implies scalar artificial dissipation, 0.001 default)
 ENTROPY_FIX_COEFF= 0.01
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
-% Relaxation coefficient
-%
-%
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 %
-%
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Number of total iterations
 OUTER_ITER= 21
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 %
-%
-%
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_axial_stage_2d_turb.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= meshout.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1000
-%
diff --git a/TestCases/turbomachinery/axial_stage_2D/zone_1.cfg b/TestCases/turbomachinery/axial_stage_2D/zone_1.cfg
index 01e1dcc6f7a..a73d2ae7007 100644
--- a/TestCases/turbomachinery/axial_stage_2D/zone_1.cfg
+++ b/TestCases/turbomachinery/axial_stage_2D/zone_1.cfg
@@ -5,13 +5,10 @@
 % Author: S. Vitale                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: Feb 28th, 2017                                                         %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-%
+
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT= NONE
-%
-
diff --git a/TestCases/turbomachinery/axial_stage_2D/zone_2.cfg b/TestCases/turbomachinery/axial_stage_2D/zone_2.cfg
index 1bceeab5737..d699eb5acf9 100644
--- a/TestCases/turbomachinery/axial_stage_2D/zone_2.cfg
+++ b/TestCases/turbomachinery/axial_stage_2D/zone_2.cfg
@@ -5,18 +5,12 @@
 % Author: S. Vitale                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: Feb 28th, 2017                                                         %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-%
+
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT= STEADY_TRANSLATION
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.35
-%
-%Steady transaltion rate
 TRANSLATION_RATE= 0.0 -150.0 0.0
diff --git a/TestCases/turbomachinery/centrifugal_blade/centrifugal_blade.cfg b/TestCases/turbomachinery/centrifugal_blade/centrifugal_blade.cfg
index b4b3689bc45..73e924ce3d8 100755
--- a/TestCases/turbomachinery/centrifugal_blade/centrifugal_blade.cfg
+++ b/TestCases/turbomachinery/centrifugal_blade/centrifugal_blade.cfg
@@ -5,340 +5,132 @@
 % Author:S. Vitale                                                             %
 % Institution: Delft University of Technology                                  %
 % Date: Oct 26th, 2015                                                         %
-% File Version 4.0.1 "cardinal"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-%
-%
-%
-%
+
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)                         
 SOLVER= NAVIER_STOKES
-%
-% Specify turbulent model (NONE, SA, SST)
 KIND_TURB_MODEL= SST
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 %
-%
-%
-%
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.05
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 200000.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 510.33
-%
-% Free-stream temperature (1.2886 Kg/m3 by default)
 FREESTREAM_DENSITY= 1.2886
-%
-% Free-stream Turbulence Intensity
 FREESTREAM_TURBULENCEINTENSITY = 0.1
-%
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
-%
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-%Init option to choose between Reynolds (default) or thermodynamics quantities for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
 %
-%
-%
-%
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-%Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 %
-%
-%
-%
 % --------------------------------- FLUID MODEL -----------------------------------%
 %
-% Different gas model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS)
 FLUID_MODEL= PR_GAS
-%
-% Ratio of specific heats (1.4 default and the value is hardcoded for the model STANDARD_AIR)
 GAMMA_VALUE= 1.034
-%
-% Specific gas constant (287.058 J/kg*K default and this value is hardcoded for the model STANDARD_AIR)
 GAS_CONSTANT= 28.03
-%
-% Critical Temperature (273.15 K by default)
 CRITICAL_TEMPERATURE= 586.5
-%
-% Critical Pressure (101325.0 N/m^2 by default)
 CRITICAL_PRESSURE= 1332000.0
-%
-% Acentri factor (0.035 (air))
 ACENTRIC_FACTOR= 0.592
 %
-%
-%
-%
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.0563E-5
-%
-% Sutherland Viscosity Ref (1.716E-5 default value for AIR SI)
 MU_REF= 1.716E-5
-%
-% Sutherland Temperature Ref (273.15 K default value for AIR SI)
 MU_T_REF= 273.15
-%
-% Sutherland constant (110.4 default value for AIR SI)
 SUTHERLAND_CONSTANT= 110.4
 %
-%
-%
-%
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
-% Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL).
 CONDUCTIVITY_MODEL= CONSTANT_CONDUCTIVITY
-%
-% Molecular Thermal Conductivity that would be constant (0.0257 by default)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.025275
 %
-%
-%
-%
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( wall1, 0.0, wall2, 0.0 )
-%
-% Riemann boundary marker(s)
-% Format inlet:  ( marker, TOTAL_CONDITIONS_PT, Total Pressure, Total Temperature, Flow dir-x, Flow dir-y, Flow dir-z)
-% Format outlet: ( marker, type, STATIC_PRESSURE, Static Pressure, 0.0, 0.0, 0.0, 0.0)
 MARKER_RIEMANN= (inflow, TOTAL_CONDITIONS_PT, 366000.0, 515.00, 0.309016, 0.951056, 0.0)
-%
-% Non reflecting boundary marker
-% Format inlet:  ( marker, TOTAL_CONDITIONS_PT, Total Pressure, Total Temperature, Flow dir-x, Flow dir-y, Flow dir-z)
-% Format outlet: ( marker, type, STATIC_PRESSURE, Static Pressure, 0.0, 0.0, 0.0, 0.0)
 MARKER_NRBC= (outflow, STATIC_PRESSURE, 165500.0, 0.0, 0.0, 0.0, 0.0)
-%
-% Kind of Average (ALGEBRAIC_AVERAGE, AREA_AVERAGE, MIXEDOUT_AVERAGE)
 MIXING_PROCESS_TYPE= MIXEDOUT_AVERAGE
-%
-% Periodic boundary marker(s) (NONE = no marker)
-% Format: ( periodic marker, donor marker, rot_cen_x, rot_cen_y, rot_cen_z, rot_angle_x-axis, rot_angle_y-axis, rot_angle_z-axis, translation_x, translation_y, translation_z)
 MARKER_PERIODIC= ( periodic1, periodic2, 0.0, 0.0, 0.0, 0.0, 0.0, 9.47, 0.0, 0.0, 0.0)
 %
-%
-%
-%
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING= ( wall1, wall2 )
 %
 % Marker(s) between turbomachinery performance are evaluated. Use BLADE for single blade, STAGE for stage and TURBINE for a multi-stage.   
 MARKER_TURBO_PERFORMANCE= (inflow, outflow, BLADE)
 %
-%
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Dynamic mesh simulation (NO, YES)
 GRID_MOVEMENT= YES
-%
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT_KIND= ROTATING_FRAME
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.35
-%
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE_X = 0.0
 ROTATION_RATE_Y = 0.0
 ROTATION_RATE_Z = 1990.00
 %
-%
-%
-%
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= YES
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value, CFL max value )
 CFL_ADAPT_PARAM= ( 0.1, 1.2, 10.0, 1000.0)
 %
-%
-%
-%
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 %
-%
-%
-%
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-%
-%
-%
-%
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
 %
-%
-%
-%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, ROE, AUSM, HLLC)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Entropy fix coefficient (0.0 implies no entropy fixing, 1.0 implies scalar artificial dissipation, 0.001 default)
 ENTROPY_FIX_COEFF= 0.001
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
-% Relaxation coefficient
-%
-%
-%
-%
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 %
-%
-%
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Number of total iterations
 ITER= 12000
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 %
-%
-%
-%
-%
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= su2mesh_periodic.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= su2mesh_per.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
-OUTPUT_WRT_FREQ= 500
-%
+OUTPUT_WRT_FREQ= 500
\ No newline at end of file
diff --git a/TestCases/turbomachinery/centrifugal_stage/centrifugal_stage.cfg b/TestCases/turbomachinery/centrifugal_stage/centrifugal_stage.cfg
index 8699a770d24..3455bdb6af1 100755
--- a/TestCases/turbomachinery/centrifugal_stage/centrifugal_stage.cfg
+++ b/TestCases/turbomachinery/centrifugal_stage/centrifugal_stage.cfg
@@ -5,347 +5,132 @@
 % Author: S. Vitale                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: Oct 28th, 2015                                                         %
-% File Version 4.0.1 "cardinal"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
-%
-%
-%
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES)                         
 SOLVER= NAVIER_STOKES
-%
-% Specify turbulent model (NONE, SA, SST)
 KIND_TURB_MODEL= SST
-%
-% Mathematical problem (DIRECT, ADJOINT, LINEARIZED)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 %
-%
-%
-%
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.05
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
 FREESTREAM_PRESSURE= 200000.0
-%
-% Free-stream temperature (273.15 K by default)
 FREESTREAM_TEMPERATURE= 510.33
-%
-% Free-stream temperature (1.2886 Kg/m3 by default)
 FREESTREAM_DENSITY= 1.2886
-%
-% Free-stream Turbulence Intensity
 FREESTREAM_TURBULENCEINTENSITY = 0.1
-%
-% Free-stream Turbulent to Laminar viscosity ratio
 FREESTREAM_TURB2LAMVISCRATIO = 100.0
-%
-% Free-stream option to choose if you want to use Density (DENSITY_FS) or Temperature (TEMPERATURE_FS) to initialize the solution
 FREESTREAM_OPTION= TEMPERATURE_FS
-%
-%Init option to choose between Reynolds (default) or thermodynamics quantities for initializing the solution (REYNOLDS, TD_CONDITIONS)
 INIT_OPTION= TD_CONDITIONS
 %
-%
-%
-%
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-%Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 %
-%
-%
-%
 % --------------------------------- FLUID MODEL -----------------------------------%
 %
-% Different gas model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS)
 FLUID_MODEL= PR_GAS
-%
-% Ratio of specific heats (1.4 default and the value is hardcoded for the model STANDARD_AIR)
 GAMMA_VALUE= 1.034
-%
-% Specific gas constant (287.058 J/kg*K default and this value is hardcoded for the model STANDARD_AIR)
 GAS_CONSTANT= 28.03
-%
-% Critical Temperature (273.15 K by default)
 CRITICAL_TEMPERATURE= 586.5
-%
-% Critical Pressure (101325.0 N/m^2 by default)
 CRITICAL_PRESSURE= 1332000.0
-%
-% Acentri factor (0.035 (air))
 ACENTRIC_FACTOR= 0.592
 %
-%
-%
-%
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY).
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
-%
-% Molecular Viscosity that would be constant (1.716E-5 by default)
 MU_CONSTANT= 1.0563E-5
-%
-% Sutherland Viscosity Ref (1.716E-5 default value for AIR SI)
 MU_REF= 1.716E-5
-%
-% Sutherland Temperature Ref (273.15 K default value for AIR SI)
 MU_T_REF= 273.15
-%
-% Sutherland constant (110.4 default value for AIR SI)
 SUTHERLAND_CONSTANT= 110.4
 %
-%
-%
-%
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
-% Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL).
 CONDUCTIVITY_MODEL= CONSTANT_CONDUCTIVITY
-%
-% Molecular Thermal Conductivity that would be constant (0.0257 by default)
 THERMAL_CONDUCTIVITY_CONSTANT= 0.025275
 %
-%
-%
-%
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( wall1, 0.0, wall2, 0.0,  wall3, 0.0, wall4, 0.0)
-%
-% Riemann boundary marker(s)
-% Format inlet:  ( marker, TOTAL_CONDITIONS_PT, Total Pressure, Total Temperature, Flow dir-x, Flow dir-y, Flow dir-z)
-% Format outlet: ( marker, type, STATIC_PRESSURE, Static Pressure, 0.0, 0.0, 0.0, 0.0)
 MARKER_RIEMANN= (inflow, TOTAL_CONDITIONS_PT, 366000.0, 515.00, 0.52101, -0.85355, 0.0)
-%
-% Non reflecting boundary marker
-% Format inlet:  ( marker, TOTAL_CONDITIONS_PT, Total Pressure, Total Temperature, Flow dir-x, Flow dir-y, Flow dir-z)
-% Format outlet: ( marker, type, STATIC_PRESSURE, Static Pressure, 0.0, 0.0, 0.0, 0.0)
 MARKER_NRBC= (outmix, MIXING_OUT, 0.0, 0.0, 0.0, 0.0, 0.0, inmix, MIXING_IN, 0.0, 0.0, 0.0, 0.0, 0.0, outflow, STATIC_PRESSURE, 95750.0, 0.0, 0.0, 0.0, 0.0)
-%
-% Kind of Average (ALGEBRAIC_AVERAGE, AREA_AVERAGE, MIXEDOUT_AVERAGE)
 MIXING_PROCESS_TYPE= AREA_AVERAGE
-%
-% Mixing plane interface
 MARKER_MIXINGPLANE= (outmix, inmix)
-%
-% Periodic boundary marker(s) (NONE = no marker)
-% Format: ( periodic marker, donor marker, rot_cen_x, rot_cen_y, rot_cen_z, rot_angle_x-axis, rot_angle_y-axis, rot_angle_z-axis, translation_x, translation_y, translation_z)
 MARKER_PERIODIC= (periodic1, periodic2, 0.0, 0.0, 0.0, 0.0, 0.0, 10.29, 0.0, 0.0, 0.0, periodic3, periodic4, 0.0, 0.0, 0.0, 0.0, 0.0, 8.78, 0.0, 0.0, 0.0)
 %
-%
-%
-%
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING= ( wall1, wall2 )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated
 MARKER_MONITORING= ( wall1, wall2 )
-%
-% Marker(s) between turbomachinery performance are evaluated. Use BLADE for single blade, STAGE for stage and TURBINE for a multi-stage.
 MARKER_TURBO_PERFORMANCE= (inflow, outflow, STAGE, inflow, outmix, BLADE, inmix, outflow, BLADE)
 %
-%
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Dynamic mesh simulation (NO, YES)
 GRID_MOVEMENT= YES
-%
-% Type of dynamic mesh (NONE, ROTATING_FRAME)
 GRID_MOVEMENT_KIND= ROTATING_FRAME ROTATING_FRAME
-%
-% Motion mach number (non-dimensional). Used for intitializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.35
-%
-% Angular velocity vector (rad/s) about the motion origi. Example 1250 RPM -> 130.89969389957471 rad/s
 ROTATION_RATE_X = 0.0 0.0 
 ROTATION_RATE_Y = 0.0 0.0 
 ROTATION_RATE_Z = 0.0 1990.0
 %
-%
-%
-%
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= YES
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value, CFL max value )
 CFL_ADAPT_PARAM= ( 0.1, 1.2, 1.0, 1000.0)
 %
-%
-%
-%
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 %
-%
-%
-%
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multigrid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multigrid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
-%
-%
-%
-%
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.05
-%
-% Freeze the value of the limiter after a number of iterations
 LIMITER_ITER= 999999
 %
-%
-%
-%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, ROE, AUSM, HLLC)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= NO
-%
-% Entropy fix coefficient (0.0 implies no entropy fixing, 1.0 implies scalar artificial dissipation, 0.001 default)
 ENTROPY_FIX_COEFF= 0.001
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Slope limiter (VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
-% Relaxation coefficient
-%
-%
-%
-%
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
-%
-% Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
 %
-%
-%
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Number of total iterations
 ITER= 32000
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -16
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 %
-%
-%
-%
-%
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= su2mesh_periodic.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= su2mesh_per.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 500
-%
diff --git a/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg b/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg
index 38a47f4ce4c..73dcf2bddf7 100644
--- a/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg
+++ b/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg
@@ -5,11 +5,10 @@
 % Author: S. Vitale                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: 2017.03.01                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
-%
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
 SOLVER= RANS
@@ -103,7 +102,7 @@ LINEAR_SOLVER_ITER= 5
 %
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% ----------- NOT WORKING WITH PERIODIC BOUNDARY CONDITIONS !!!!! --------------%
+% ----------- NOT WORKING WITH PERIODIC BOUNDARY CONDITIONS !!!!! -------------%
 %
 %
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
@@ -152,5 +151,4 @@ VOLUME_ADJ_FILENAME= adjoint
 GRAD_OBJFUNC_FILENAME= of_grad.dat
 SURFACE_FILENAME= surface_flow
 SURFACE_ADJ_FILENAME= surface_adjoint
-OUTPUT_WRT_FREQ= 500
-%
+OUTPUT_WRT_FREQ= 500
\ No newline at end of file
diff --git a/TestCases/turbulence_models/sa/rae2822/turb_SA_BSL_RAE2822.cfg b/TestCases/turbulence_models/sa/rae2822/turb_SA_BSL_RAE2822.cfg
index e65ee871fa0..4c8538ba5ec 100644
--- a/TestCases/turbulence_models/sa/rae2822/turb_SA_BSL_RAE2822.cfg
+++ b/TestCases/turbulence_models/sa/rae2822/turb_SA_BSL_RAE2822.cfg
@@ -1,167 +1,80 @@
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations                    
 SOLVER= RANS
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.729
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 2.31
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.5E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( AIRFOIL, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( FARFIELD )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( AIRFOIL )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( AIRFOIL )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Number of total iterations
 ITER= 99999
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= BCGSTAB
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.95
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.95
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_RAE2822_turb.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-% Screen output fields 
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG)
diff --git a/TestCases/turbulence_models/sa/rae2822/turb_SA_COMP_EDW_RAE2822.cfg b/TestCases/turbulence_models/sa/rae2822/turb_SA_COMP_EDW_RAE2822.cfg
index fb7b111b3d3..39cd89c64b4 100644
--- a/TestCases/turbulence_models/sa/rae2822/turb_SA_COMP_EDW_RAE2822.cfg
+++ b/TestCases/turbulence_models/sa/rae2822/turb_SA_COMP_EDW_RAE2822.cfg
@@ -1,168 +1,80 @@
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations                    
 SOLVER= RANS
-%
-% Specify turbulence model
 KIND_TURB_MODEL= SA
 SA_OPTIONS= EDWARDS, COMPRESSIBILITY, EXPERIMENTAL
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.729
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 2.31
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.5E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( AIRFOIL, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( FARFIELD )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( AIRFOIL )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( AIRFOIL )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Number of total iterations
 ITER= 99999
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= BCGSTAB
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.95
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.95
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_RAE2822_turb.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-% Screen output fields 
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG)
diff --git a/TestCases/turbulence_models/sa/rae2822/turb_SA_COMP_RAE2822.cfg b/TestCases/turbulence_models/sa/rae2822/turb_SA_COMP_RAE2822.cfg
index aeb8e3dbbf1..8f847257a3a 100644
--- a/TestCases/turbulence_models/sa/rae2822/turb_SA_COMP_RAE2822.cfg
+++ b/TestCases/turbulence_models/sa/rae2822/turb_SA_COMP_RAE2822.cfg
@@ -1,168 +1,81 @@
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations                    
 SOLVER= RANS
-%
-% Specify turbulence model
 KIND_TURB_MODEL= SA
 SA_OPTIONS= COMPRESSIBILITY
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.729
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 2.31
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.5E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( AIRFOIL, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( FARFIELD )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( AIRFOIL )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( AIRFOIL )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Number of total iterations
 ITER= 99999
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= BCGSTAB
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.95
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.95
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_RAE2822_turb.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-% Screen output fields 
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG)
diff --git a/TestCases/turbulence_models/sa/rae2822/turb_SA_EDW_RAE2822.cfg b/TestCases/turbulence_models/sa/rae2822/turb_SA_EDW_RAE2822.cfg
index 70c20176b7f..894dfdf7e7a 100644
--- a/TestCases/turbulence_models/sa/rae2822/turb_SA_EDW_RAE2822.cfg
+++ b/TestCases/turbulence_models/sa/rae2822/turb_SA_EDW_RAE2822.cfg
@@ -1,168 +1,81 @@
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations                    
 SOLVER= RANS
-%
-% Specify turbulence model
 KIND_TURB_MODEL= SA
 SA_OPTIONS= EDWARDS
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.729
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 2.31
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.5E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( AIRFOIL, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( FARFIELD )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( AIRFOIL )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( AIRFOIL )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Number of total iterations
 ITER= 99999
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= BCGSTAB
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.95
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.95
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_RAE2822_turb.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-% Screen output fields 
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG)
diff --git a/TestCases/turbulence_models/sa/rae2822/turb_SA_NEG_RAE2822.cfg b/TestCases/turbulence_models/sa/rae2822/turb_SA_NEG_RAE2822.cfg
index e72242cd8f6..7f54aad5945 100644
--- a/TestCases/turbulence_models/sa/rae2822/turb_SA_NEG_RAE2822.cfg
+++ b/TestCases/turbulence_models/sa/rae2822/turb_SA_NEG_RAE2822.cfg
@@ -2,10 +2,10 @@
 %                                                                              %
 %                                  WARNING                                     %
 %                      This regression test will diverge!                      %
-%									       %
+%                                                                              %
 % This test case is only meant to trigger the negative part of the SA model,   %
 % to check the integrity of the commits. It is inadvisable to use it as an     %
-% starting point for tutorials.						       %
+% starting point for tutorials.                                                %
 % The rae2822 airfoil is a simple (fast) case. A high angle of attack is being %
 % used in order to force the negative part of the SA in a reasonable amount of %
 % iterations. With the current configuration, e.g., convective scheme, CFL     %
@@ -16,173 +16,73 @@
 %
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations                    
 SOLVER= RANS
-%
-% Specify turbulence model
 KIND_TURB_MODEL= SA
 SA_OPTIONS= NEGATIVE, EXPERIMENTAL
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.729
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 20.31
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.5E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( AIRFOIL, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( FARFIELD )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( AIRFOIL )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( AIRFOIL )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= YES
-%
-% Parameters of the adaptive CFL number ( factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 0.5, 1.5, 400.0, 1000.0 )
-%
-% Number of total iterations
 ITER= 99999
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= BCGSTAB
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.95
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.95
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_RAE2822_turb.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-% Screen output fields 
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG, TOTAL_HEATFLUX)
diff --git a/TestCases/turbulence_models/sa/rae2822/turb_SA_QCR_RAE2822.cfg b/TestCases/turbulence_models/sa/rae2822/turb_SA_QCR_RAE2822.cfg
index 05b09d9a911..fba16360d75 100644
--- a/TestCases/turbulence_models/sa/rae2822/turb_SA_QCR_RAE2822.cfg
+++ b/TestCases/turbulence_models/sa/rae2822/turb_SA_QCR_RAE2822.cfg
@@ -1,169 +1,81 @@
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations                    
 SOLVER= RANS
-%
-% Specify turbulence model
 KIND_TURB_MODEL= SA
 SA_OPTIONS= QCR2000
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.729
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 2.31
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 6.5E6
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( AIRFOIL, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( FARFIELD )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( AIRFOIL )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( AIRFOIL )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.5
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Number of total iterations
 ITER= 99999
-%
-% Linear solver for the implicit formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= BCGSTAB
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-grid pre-smoothing level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.95
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.95
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_RAE2822_turb.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
-% Screen output fields 
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG)
diff --git a/TestCases/tutorials.py b/TestCases/tutorials.py
index 5d53be99520..5471eab7258 100644
--- a/TestCases/tutorials.py
+++ b/TestCases/tutorials.py
@@ -3,7 +3,7 @@
 ## \file parallel_regression.py
 #  \brief Python script for automated regression testing of SU2 examples
 #  \author A. Aranake, A. Campos, T. Economon, T. Lukaczyk, S. Padron
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 #
@@ -187,6 +187,24 @@ def main():
     tutorial_trans_flatplate_T3Am.test_vals  = [-6.063550, -1.945057, -3.946359, -0.549026, -3.863798, 2.664577, -2.517606, 1.112977]
     tutorial_trans_flatplate_T3Am.no_restart = True
     test_list.append(tutorial_trans_flatplate_T3Am)
+    
+    # Transitional E387 SA
+    tutorial_trans_e387_sa            = TestCase('tutorial_trans_e387_sa')
+    tutorial_trans_e387_sa.cfg_dir    = "../Tutorials/compressible_flow/Transitional_Airfoil/Langtry_and_Menter/E387"
+    tutorial_trans_e387_sa.cfg_file   = "transitional_SA_LM_model_ConfigFile.cfg"
+    tutorial_trans_e387_sa.test_iter  = 20
+    tutorial_trans_e387_sa.test_vals  = [-6.527027, -5.081543, -0.795267, 1.022557, 0.150240, 2, -9.580670]
+    tutorial_trans_e387_sa.no_restart = True
+    test_list.append(tutorial_trans_e387_sa)
+    
+    # Transitional E387 SST
+    tutorial_trans_e387_sst            = TestCase('tutorial_trans_e387_sst')
+    tutorial_trans_e387_sst.cfg_dir    = "../Tutorials/compressible_flow/Transitional_Airfoil/Langtry_and_Menter/E387"
+    tutorial_trans_e387_sst.cfg_file   = "transitional_SST_LM_model_ConfigFile.cfg"
+    tutorial_trans_e387_sst.test_iter  = 20
+    tutorial_trans_e387_sst.test_vals  = [-6.532421, -5.085785, -0.789723, 1.078391, 0.188263, 2, -9.567014]
+    tutorial_trans_e387_sst.no_restart = True
+    test_list.append(tutorial_trans_e387_sst)
 
     # Turbulent ONERA M6
     tutorial_turb_oneram6            = TestCase('turbulent_oneram6_tutorial')
diff --git a/TestCases/unsteady/pitching_naca0015_rans_inc/config_incomp_turb_sa.cfg b/TestCases/unsteady/pitching_naca0015_rans_inc/config_incomp_turb_sa.cfg
index 7045568c646..ee33ca1ee9c 100644
--- a/TestCases/unsteady/pitching_naca0015_rans_inc/config_incomp_turb_sa.cfg
+++ b/TestCases/unsteady/pitching_naca0015_rans_inc/config_incomp_turb_sa.cfg
@@ -11,10 +11,10 @@ TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
 TIME_STEP= 0.016849% 25 time steps per period
 MAX_TIME= 2.528% 6 periods
 %
-% New driver
 TIME_DOMAIN= YES
 TIME_ITER= 2
 INNER_ITER= 50
+
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
 GRID_MOVEMENT= RIGID_MOTION
@@ -38,7 +38,7 @@ REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
 REF_LENGTH= 1.0
 REF_AREA= 1.0
-%
+
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
 MARKER_HEATFLUX= ( airfoil, 0.0 )
@@ -58,20 +58,11 @@ LINEAR_SOLVER= FGMRES
 LINEAR_SOLVER_PREC= ILU
 LINEAR_SOLVER_ERROR= 1E-14
 LINEAR_SOLVER_ITER= 2
-%LINEAR_SOLVER_ERROR= 1E-8
-%LINEAR_SOLVER_ITER= 2000
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
 VENKAT_LIMITER_COEFF= 0.03
 LIMITER_ITER= 99999
-%ADJ_SHARP_LIMITER_COEFF= 3.0
-%REF_SHARP_EDGES= 3.0
-%SENS_REMOVE_SHARP= NO
-
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-MGLEVEL= 0
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
@@ -79,8 +70,6 @@ CONV_NUM_METHOD_FLOW= JST
 MUSCL_FLOW= YES
 SLOPE_LIMITER_FLOW= NONE
 TIME_DISCRE_FLOW= EULER_IMPLICIT
-
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
diff --git a/TestCases/unsteady/pitching_naca64a010_euler/pitching_NACA64A010.cfg b/TestCases/unsteady/pitching_naca64a010_euler/pitching_NACA64A010.cfg
index e5dfc0ac4ad..edfa9294482 100644
--- a/TestCases/unsteady/pitching_naca64a010_euler/pitching_NACA64A010.cfg
+++ b/TestCases/unsteady/pitching_naca64a010_euler/pitching_NACA64A010.cfg
@@ -5,366 +5,151 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= EULER
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-%
-% Time Step for dual time stepping simulations (s)
 TIME_STEP= 0.0023555025613149587
 % 24 steps per period: 0.0024536485013697488
 % 25 steps per period: 0.0023555025613149587
 %
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 0.59
 % 10 periods: 0.5888756403287397
 %
-% Number of internal iterations (dual time method)
 INNER_ITER= 110
-%
-% Starting direct iteration for unsteady adjoint
 UNST_ADJOINT_ITER= 251
 
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
-% Type of mesh motion (NONE, FLUTTER, RIGID_MOTION)
-%GRID_MOVEMENT= RIGID_MOTION
 %
 SURFACE_MOVEMENT= DEFORMING
-
 MARKER_MOVING= airfoil
-% Motion mach number (non-dimensional). Used for initializing a viscous flow
-% with the Reynolds number and for computing force coeffs. with dynamic meshes.
 MACH_MOTION= 0.796
-%
-% Coordinates of the rigid motion origin
 SURFACE_MOTION_ORIGIN= 0.248 0.0 0.0
-%
-% Pitching angular freq. (rad/s) about x, y, & z axes (RIGID_MOTION only)
 SURFACE_PITCHING_OMEGA= 0.0 0.0 106.69842
-%
-% Pitching amplitude (degrees) about x, y, & z axes (RIGID_MOTION only)
 SURFACE_PITCHING_AMPL= 0.0 0.0 1.01
+
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.796
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.248
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Euler boundary (0 = no marker)
 MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( airfoil )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( airfoil )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 10.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 EXT_ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.9
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.9
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.1
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, TORQUE)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.5
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Adjoint frozen viscosity (NO, YES)
 FROZEN_VISC_CONT= YES
 
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
 %
-% Marker(s) of the surface where geometrical based function will be evaluated
 GEO_MARKER= ( airfoil )
-%
-% Description of the geometry to be analyzed (AIRFOIL, WING, FUSELAGE)
 GEO_DESCRIPTION= AIRFOIL
-%
-% Geometrical evaluation mode (FUNCTION, GRADIENT)
 GEO_MODE= FUNCTION
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION, 
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION)
-DV_KIND= HICKS_HENNE
 %
-% Marker of the surface in which we are going apply the shape deformation
+DV_KIND= HICKS_HENNE
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( 1st digit, 2nd and 3rd digit )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= ( 1, 0.5 )
-%
-% Old value of the deformation for incremental deformations
 DV_VALUE= 0.0
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-6
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA64A010_inv.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 250
-%
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-
-% Optimization objective function with optional scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.001
-
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= ( LIFT = 0.0 ) * 0.001; ( AREA > 0.0660957 ) * 0.001
-%
-% List of design variables (Design variables are separated by semicolons)
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.961538461538 ); ( 30, 1.0 | airfoil | 0, 0.923076923077 ); ( 30, 1.0 | airfoil | 0, 0.884615384615 ); ( 30, 1.0 | airfoil | 0, 0.846153846154 ); ( 30, 1.0 | airfoil | 0, 0.807692307692 ); ( 30, 1.0 | airfoil | 0, 0.769230769231 ); ( 30, 1.0 | airfoil | 0, 0.730769230769 ); ( 30, 1.0 | airfoil | 0, 0.692307692308 ); ( 30, 1.0 | airfoil | 0, 0.653846153846 ); ( 30, 1.0 | airfoil | 0, 0.615384615385 ); ( 30, 1.0 | airfoil | 0, 0.576923076923 ); ( 30, 1.0 | airfoil | 0, 0.538461538462 ); ( 30, 1.0 | airfoil | 0, 0.5 ); ( 30, 1.0 | airfoil | 0, 0.461538461538 ); ( 30, 1.0 | airfoil | 0, 0.423076923077 ); ( 30, 1.0 | airfoil | 0, 0.384615384615 ); ( 30, 1.0 | airfoil | 0, 0.346153846154 ); ( 30, 1.0 | airfoil | 0, 0.307692307692 ); ( 30, 1.0 | airfoil | 0, 0.269230769231 ); ( 30, 1.0 | airfoil | 0, 0.230769230769 ); ( 30, 1.0 | airfoil | 0, 0.192307692308 ); ( 30, 1.0 | airfoil | 0, 0.153846153846 ); ( 30, 1.0 | airfoil | 0, 0.115384615385 ); ( 30, 1.0 | airfoil | 0, 0.0769230769231 ); ( 30, 1.0 | airfoil | 0, 0.0384615384615 ); ( 30, 1.0 | airfoil | 1, 0.0384615384615 ); ( 30, 1.0 | airfoil | 1, 0.0769230769231 ); ( 30, 1.0 | airfoil | 1, 0.115384615385 ); ( 30, 1.0 | airfoil | 1, 0.153846153846 ); ( 30, 1.0 | airfoil | 1, 0.192307692308 ); ( 30, 1.0 | airfoil | 1, 0.230769230769 ); ( 30, 1.0 | airfoil | 1, 0.269230769231 ); ( 30, 1.0 | airfoil | 1, 0.307692307692 ); ( 30, 1.0 | airfoil | 1, 0.346153846154 ); ( 30, 1.0 | airfoil | 1, 0.384615384615 ); ( 30, 1.0 | airfoil | 1, 0.423076923077 ); ( 30, 1.0 | airfoil | 1, 0.461538461538 ); ( 30, 1.0 | airfoil | 1, 0.5 ); ( 30, 1.0 | airfoil | 1, 0.538461538462 ); ( 30, 1.0 | airfoil | 1, 0.576923076923 ); ( 30, 1.0 | airfoil | 1, 0.615384615385 ); ( 30, 1.0 | airfoil | 1, 0.653846153846 ); ( 30, 1.0 | airfoil | 1, 0.692307692308 ); ( 30, 1.0 | airfoil | 1, 0.730769230769 ); ( 30, 1.0 | airfoil | 1, 0.769230769231 ); ( 30, 1.0 | airfoil | 1, 0.807692307692 ); ( 30, 1.0 | airfoil | 1, 0.846153846154 ); ( 30, 1.0 | airfoil | 1, 0.884615384615 ); ( 30, 1.0 | airfoil | 1, 0.923076923077 ); ( 30, 1.0 | airfoil | 1, 0.961538461538 )
diff --git a/TestCases/unsteady/pitching_naca64a010_rans/turb_NACA64A010.cfg b/TestCases/unsteady/pitching_naca64a010_rans/turb_NACA64A010.cfg
index e5e3fedf112..40beee82d23 100644
--- a/TestCases/unsteady/pitching_naca64a010_rans/turb_NACA64A010.cfg
+++ b/TestCases/unsteady/pitching_naca64a010_rans/turb_NACA64A010.cfg
@@ -5,392 +5,159 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= NAVIER_STOKES
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-%
-% Time Step for dual time stepping simulations (s)
 TIME_STEP= 0.0023555025613149587
 % 24 steps per period: 0.0024536485013697488
 % 25 steps per period: 0.0023555025613149587
 % 36 steps per period: 0.0016357592286692995
 %
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 0.59
 % 10 periods: 0.5888756403287397
 %
-% Number of internal iterations (dual time method)
 INNER_ITER= 2000
-%
-% Direct iteration number at which to begin unsteady adjoint
 UNST_ADJOINT_ITER= 251
-%
-% Type of mesh motion (NONE, FLUTTER, RIGID_MOTION)
 GRID_MOVEMENT= RIGID_MOTION
-%
-% Mach number (non-dimensional, based on the mesh velocity and freestream vals.)
 MACH_MOTION= 0.796
-%
-% Coordinates of the rigid motion origin
 MOTION_ORIGIN= 0.248 0.0 0.0
-%
-% Pitching angular freq. (rad/s) about x, y, & z axes (RIGID_MOTION only)
 PITCHING_OMEGA= 0.0 0.0 106.69842
-%
-% Pitching amplitude (degrees) about x, y, & z axes (RIGID_MOTION only)
 PITCHING_AMPL= 0.0 0.0 1.01
-%
  
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.796
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 12560000.0
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.248
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
-% Marker of the Navier-Stokes  boundary marker(s) (0 = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Marker of the far field (0 = no marker)
 MARKER_FAR= ( farfield )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( airfoil )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( airfoil )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
 MARKER_DESIGNING = ( airfoil )
 
 % ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
-NUM_METHOD_GRAD= GREEN_GAUSS
 %
-% Courant-Friedrichs-Lewy condition of the finest grid
+NUM_METHOD_GRAD= GREEN_GAUSS
 CFL_NUMBER= 4.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 EXT_ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 2
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.7
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.7
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the limiter (smooth regions)
 VENKAT_LIMITER_COEFF= 0.03
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
-% Adjoint problem boundary condition (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                     MOMENT_Y, MOMENT_Z, EFFICIENCY, 
-%                                     EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                     FORCE_X, FORCE_Y, FORCE_Z, THRUST, TORQUE)
 OBJECTIVE_FUNCTION= DRAG
-%
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= NONE
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% 2nd, and 4th order artificial dissipation coefficients
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.01 )
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.9
-%
-% Limit value for the adjoint variable
 LIMIT_ADJFLOW= 1E6
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= YES
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-%
-% Adjoint frozen viscosity (NO, YES)
 FROZEN_VISC_CONT= YES
 
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
 %
-% Marker(s) of the surface where geometrical based function will be evaluated
 GEO_MARKER= ( airfoil )
-%
-% Description of the geometry to be analyzed (AIRFOIL, WING, FUSELAGE)
 GEO_DESCRIPTION= AIRFOIL
-%
-% Geometrical evaluation mode (FUNCTION, GRADIENT)
 GEO_MODE= FUNCTION
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
-% Kind of deformation (FFD_SETTING, HICKS_HENNE, HICKS_HENNE_NORMAL, PARABOLIC,
-%                      HICKS_HENNE_SHOCK, NACA_4DIGITS, DISPLACEMENT, ROTATION, 
-%                      FFD_CONTROL_POINT, FFD_DIHEDRAL_ANGLE, FFD_TWIST_ANGLE, 
-%                      FFD_ROTATION)
-DV_KIND= HICKS_HENNE
 %
-% Marker of the surface in which we are going apply the shape deformation
+DV_KIND= HICKS_HENNE
 DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation 
-% 	- HICKS_HENNE_FAMILY ( Lower(0)/Upper(1) side, x_Loc )
-% 	- NACA_4DIGITS ( 1st digit, 2nd digit, 3rd and 4th digit )
-% 	- PARABOLIC ( 1st digit, 2nd and 3rd digit )
-% 	- DISPLACEMENT ( x_Disp, y_Disp, z_Disp )
-% 	- ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
 DV_PARAM= ( 1, 0.5 )
-%
-% Old value of the deformation for incremental deformations
 DV_VALUE= 0.05
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
 CONV_STARTITER= 1
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-5
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA64A010_turb.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= restart_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency for physical time steps (dual time)
 OUTPUT_WRT_FREQ= 1
-%
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
-%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-% 2D Design variables
-%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
-%
-% 3D Design variables
-%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
-%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-%
-% Global design variables
-%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-
-% Optimization objective function with optional scaling factor
-% ex= Objective * Scale
 OPT_OBJECTIVE= DRAG * 0.001
-
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
 OPT_CONSTRAINT= ( AREA > 0.0661121 ) * 0.001
-% ( AIRFOIL_THICKNESS > 0.1 ) * 0.001
-% ( AREA > 0.0661121 ) * 0.001
-%
-% List of design variables (Design variables are separated by semicolons)
 DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.961538461538 ); ( 30, 1.0 | airfoil | 0, 0.923076923077 ); ( 30, 1.0 | airfoil | 0, 0.884615384615 ); ( 30, 1.0 | airfoil | 0, 0.846153846154 ); ( 30, 1.0 | airfoil | 0, 0.807692307692 ); ( 30, 1.0 | airfoil | 0, 0.769230769231 ); ( 30, 1.0 | airfoil | 0, 0.730769230769 ); ( 30, 1.0 | airfoil | 0, 0.692307692308 ); ( 30, 1.0 | airfoil | 0, 0.653846153846 ); ( 30, 1.0 | airfoil | 0, 0.615384615385 ); ( 30, 1.0 | airfoil | 0, 0.576923076923 ); ( 30, 1.0 | airfoil | 0, 0.538461538462 ); ( 30, 1.0 | airfoil | 0, 0.5 ); ( 30, 1.0 | airfoil | 0, 0.461538461538 ); ( 30, 1.0 | airfoil | 0, 0.423076923077 ); ( 30, 1.0 | airfoil | 0, 0.384615384615 ); ( 30, 1.0 | airfoil | 0, 0.346153846154 ); ( 30, 1.0 | airfoil | 0, 0.307692307692 ); ( 30, 1.0 | airfoil | 0, 0.269230769231 ); ( 30, 1.0 | airfoil | 0, 0.230769230769 ); ( 30, 1.0 | airfoil | 0, 0.192307692308 ); ( 30, 1.0 | airfoil | 0, 0.153846153846 ); ( 30, 1.0 | airfoil | 0, 0.115384615385 ); ( 30, 1.0 | airfoil | 0, 0.0769230769231 ); ( 30, 1.0 | airfoil | 0, 0.0384615384615 ); ( 30, 1.0 | airfoil | 1, 0.0384615384615 ); ( 30, 1.0 | airfoil | 1, 0.0769230769231 ); ( 30, 1.0 | airfoil | 1, 0.115384615385 ); ( 30, 1.0 | airfoil | 1, 0.153846153846 ); ( 30, 1.0 | airfoil | 1, 0.192307692308 ); ( 30, 1.0 | airfoil | 1, 0.230769230769 ); ( 30, 1.0 | airfoil | 1, 0.269230769231 ); ( 30, 1.0 | airfoil | 1, 0.307692307692 ); ( 30, 1.0 | airfoil | 1, 0.346153846154 ); ( 30, 1.0 | airfoil | 1, 0.384615384615 ); ( 30, 1.0 | airfoil | 1, 0.423076923077 ); ( 30, 1.0 | airfoil | 1, 0.461538461538 ); ( 30, 1.0 | airfoil | 1, 0.5 ); ( 30, 1.0 | airfoil | 1, 0.538461538462 ); ( 30, 1.0 | airfoil | 1, 0.576923076923 ); ( 30, 1.0 | airfoil | 1, 0.615384615385 ); ( 30, 1.0 | airfoil | 1, 0.653846153846 ); ( 30, 1.0 | airfoil | 1, 0.692307692308 ); ( 30, 1.0 | airfoil | 1, 0.730769230769 ); ( 30, 1.0 | airfoil | 1, 0.769230769231 ); ( 30, 1.0 | airfoil | 1, 0.807692307692 ); ( 30, 1.0 | airfoil | 1, 0.846153846154 ); ( 30, 1.0 | airfoil | 1, 0.884615384615 ); ( 30, 1.0 | airfoil | 1, 0.923076923077 ); ( 30, 1.0 | airfoil | 1, 0.961538461538 )
diff --git a/TestCases/unsteady/plunging_naca0012/plunging_NACA0012.cfg b/TestCases/unsteady/plunging_naca0012/plunging_NACA0012.cfg
index a3f123fc043..d98298bac01 100644
--- a/TestCases/unsteady/plunging_naca0012/plunging_NACA0012.cfg
+++ b/TestCases/unsteady/plunging_naca0012/plunging_NACA0012.cfg
@@ -5,242 +5,117 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: Jun 12, 2014                                                           %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)                             
 SOLVER= NAVIER_STOKES
-%
-% Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= NONE
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= NO
 
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-%
-% Time Step for dual time stepping simulations (s)
 TIME_STEP= 0.0023555025613149587
 % 24 steps per period: 0.0024536485013697488
 % 25 steps per period: 0.0023555025613149587
 %
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 0.5888756403287397
 % 10 periods: 0.5888756403287397
 %
-% Number of internal iterations (dual time method)
 INNER_ITER= 1000
 
 % ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
 %
-% Type of mesh motion (NONE, FLUTTER, RIGID_ROTATION, RIGID_PITCHING)
 GRID_MOVEMENT= RIGID_MOTION
-%
-% Coordinates of the motion origin
 MOTION_ORIGIN= 0.25 0.0 0.0
-%
-% Plunging angular freq. (rad/s) in x, y, & z directions
 PLUNGING_OMEGA= 0.0 106.69842 0.0
-%
-% Plunging amplitude (m) in x, y, & z directions
 PLUNGING_AMPL= 0.0 1.01 0.0
+
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.3
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 1000.0
-%
-% Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( airfoil, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( airfoil )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 1.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 EXT_ITER= 99999
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 0.1
-%
-% Coefficient for the sharp edges limiter
 ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Reference coefficient (sensitivity) for detecting sharp edges.
 REF_SHARP_EDGES= 3.0
-%
-% Remove sharp edges from the sensitivity evaluation (NO, YES)
 SENS_REMOVE_SHARP= NO
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-Grid Levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= V_CYCLE
-%
-% Multi-Grid PreSmoothing Level
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
 MG_POST_SMOOTH= ( 2, 2, 2, 2 )
-%
-% Jacobi implicit smoothing of the correction
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
 MG_DAMP_RESTRICTION= 0.7
-%
-% Damping factor for the correction prolongation
 MG_DAMP_PROLONGATION= 0.7
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
-%
-% Slope limiter (VENKATAKRISHNAN, MINMOD)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -12
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 1
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA0012_lam.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
 OUTPUT_WRT_FREQ= 1
-%
diff --git a/TestCases/unsteady/square_cylinder/turb_square.cfg b/TestCases/unsteady/square_cylinder/turb_square.cfg
index 260d765bc0c..453e477376c 100644
--- a/TestCases/unsteady/square_cylinder/turb_square.cfg
+++ b/TestCases/unsteady/square_cylinder/turb_square.cfg
@@ -5,254 +5,109 @@
 % Author: Thomas D. Economon						                           %
 % Institution: Stanford University                                             %
 % Date: 2013.02.25                                                             %
-% File Version 7.4.0 "Blackbird"                                                %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
 SOLVER= RANS
-%
-% If Navier-Stokes, kind of turbulent model (NONE, SA)
 KIND_TURB_MODEL= SST
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
-% Read binary restart files (YES, NO)
 READ_BINARY_RESTART= NO
-%
-% Unsteady restart iteration (need previous restart files)
 RESTART_ITER= 2
+
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
 %
-% Enable time domain
 TIME_DOMAIN = YES
-%
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER, 
-%                      DUAL_TIME_STEPPING-2ND_ORDER, HARMONIC_BALANCE)
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
-%
-% Time Step for dual time stepping simulations (s)
 TIME_STEP= 0.0015
-%
-% Total Physical Time for dual time stepping simulations (s)
 MAX_TIME= 3.75
 % 2500 iterations - 3.75
 % 3500 iterations - 5.25
 % 5000 iterations - 7.50
 %
-% Number of internal iterations (dual time method)
 INNER_ITER= 10
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.1
-%
-% Angle of attack (degrees)
 AOA= 0.0
-%
-% Side-slip angle (degrees)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
-%
-% Reynolds number (non-dimensional, based on the free-stream values)
 REYNOLDS_NUMBER= 22000.0
-%
-% Reynolds length (in meters)
 REYNOLDS_LENGTH= 1.0
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation
 REF_ORIGIN_MOMENT_X = 0.00
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
 REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
 REF_AREA= 1.0
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= ( square, 0.0 )
-%
-% Farfield boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( inlet, outlet, upper, lower )
-%
-% Marker(s) of the surface to be plotted or designed
 MARKER_PLOTTING= ( square )
-%
-% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
 MARKER_MONITORING= ( square )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% Numerical method for spatial gradients (GREEN_GAUSS, LEAST_SQUARES, 
-%                                         WEIGHTED_LEAST_SQUARES)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
 CFL_NUMBER= 2.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
 TIME_ITER= 3
-%
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
-% Linear solver for the implicit (or discrete adjoint) formulation (BCGSTAB, FGMRES)
 LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
 LINEAR_SOLVER_PREC= LU_SGS
-%
-% Min error of the linear solver for the implicit formulation
 LINEAR_SOLVER_ERROR= 1E-6
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 2
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.7
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.7
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
 CONV_NUM_METHOD_FLOW= ROE
-%
-% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
 MUSCL_FLOW= YES
-%
-% Coefficient for the limiter
 VENKAT_LIMITER_COEFF= 1.0
-%
-% 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
-% Convective numerical method (SCALAR_UPWIND)
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH)
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-%
-% Time discretization (EULER_IMPLICIT)
 TIME_DISCRE_TURB= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -10
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
 CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
 CONV_CAUCHY_EPS= 1E-5
-%
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_square_turb_hybrid.su2
-%
-% Mesh input file format (SU2, CGNS NETCDF_ASCII)
 MESH_FORMAT= SU2
-%
-% Mesh output file
 MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
 TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension) 
 CONV_FILENAME= history
-%
-% Output file restart flow
 RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
 VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
 GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
 SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency for physical time steps (dual time)
 OUTPUT_WRT_FREQ= 1
-%
-% Screen output 
 SCREEN_OUTPUT= (TIME_ITER, INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG, TAVG_LIFT, TAVG_DRAG, TOTAL_HEATFLUX)
-%
 OUTPUT_FILES= (RESTART_ASCII)
diff --git a/TestCases/user_defined_functions/lam_flatplate.cfg b/TestCases/user_defined_functions/lam_flatplate.cfg
index fadc6404de5..e7142ef068e 100644
--- a/TestCases/user_defined_functions/lam_flatplate.cfg
+++ b/TestCases/user_defined_functions/lam_flatplate.cfg
@@ -4,7 +4,7 @@
 % Case description: Test custom outputs and objective function.                %
 % Author: P. Gomes                                                             %
 % Date: 5th Jan 2022                                                           %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/vandv.py b/TestCases/vandv.py
index c5d4c45044b..a28605057a2 100644
--- a/TestCases/vandv.py
+++ b/TestCases/vandv.py
@@ -6,7 +6,7 @@
 #   - Use the SU2 --dry_run mode for configs of large tests.
 #   - Restart from converged results for medium problems.
 #   - Run small cases (<20s) to convergence.
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/wallfunctions/flatplate/compressible_SA/turb_SA_flatplate.cfg b/TestCases/wallfunctions/flatplate/compressible_SA/turb_SA_flatplate.cfg
index 7f3aefd2ca2..c57cfc0343d 100644
--- a/TestCases/wallfunctions/flatplate/compressible_SA/turb_SA_flatplate.cfg
+++ b/TestCases/wallfunctions/flatplate/compressible_SA/turb_SA_flatplate.cfg
@@ -6,7 +6,7 @@
 % Author: Nijso Beishuizen, T. Kattmann                                        %
 % Institution: Bosch Thermotechnology                                          %
 % Date: 2021.09.01                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
@@ -65,11 +65,7 @@ LINEAR_SOLVER= FGMRES
 LINEAR_SOLVER_PREC= ILU
 LINEAR_SOLVER_ERROR= 1e-15
 LINEAR_SOLVER_ITER= 10
-%
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-MGLEVEL= 0
-%
+
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= ROE
@@ -95,7 +91,6 @@ CONV_CAUCHY_EPS= 1E-6
 %
 MESH_FILENAME= ../mesh_flatplate_140x100.su2
 MESH_FORMAT= SU2
-%
 SCREEN_OUTPUT= (INNER_ITER, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, RMS_NU_TILDE, \
                 LINSOL_ITER, LINSOL_RESIDUAL, LIFT, DRAG)
 SCREEN_WRT_FREQ_INNER= 10
diff --git a/TestCases/wallfunctions/flatplate/compressible_SST/turb_SST_flatplate.cfg b/TestCases/wallfunctions/flatplate/compressible_SST/turb_SST_flatplate.cfg
index a572ab8a898..bfc2b2d0748 100644
--- a/TestCases/wallfunctions/flatplate/compressible_SST/turb_SST_flatplate.cfg
+++ b/TestCases/wallfunctions/flatplate/compressible_SST/turb_SST_flatplate.cfg
@@ -6,7 +6,7 @@
 % Author: Nijso Beishuizen, T. Kattmann                                        %
 % Institution: Bosch Thermotechnology                                          %
 % Date: 2021.09.01                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
@@ -65,11 +65,7 @@ LINEAR_SOLVER= FGMRES
 LINEAR_SOLVER_PREC= ILU
 LINEAR_SOLVER_ERROR= 1e-15
 LINEAR_SOLVER_ITER= 10
-%
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-MGLEVEL= 0
-%
+
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= ROE
@@ -95,7 +91,6 @@ CONV_CAUCHY_EPS= 1E-6
 %
 MESH_FILENAME= ../mesh_flatplate_140x100.su2
 MESH_FORMAT= SU2
-%
 SCREEN_OUTPUT= (INNER_ITER, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, RMS_TKE, RMS_DISSIPATION, \
                 LINSOL_ITER, LINSOL_RESIDUAL, LIFT, DRAG)
 SCREEN_WRT_FREQ_INNER= 10
diff --git a/TestCases/wallfunctions/flatplate/incompressible_SA/turb_SA_flatplate.cfg b/TestCases/wallfunctions/flatplate/incompressible_SA/turb_SA_flatplate.cfg
index bd85066cbb7..85c4be8e24d 100644
--- a/TestCases/wallfunctions/flatplate/incompressible_SA/turb_SA_flatplate.cfg
+++ b/TestCases/wallfunctions/flatplate/incompressible_SA/turb_SA_flatplate.cfg
@@ -6,7 +6,7 @@
 % Author: Nijso Beishuizen, T. Kattmann                                        %
 % Institution: Bosch Thermotechnology                                          %
 % Date: 2021.09.01                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
@@ -68,11 +68,7 @@ LINEAR_SOLVER= FGMRES
 LINEAR_SOLVER_PREC= ILU
 LINEAR_SOLVER_ERROR= 1e-15
 LINEAR_SOLVER_ITER= 10
-%
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-MGLEVEL= 0
-%
+
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= FDS
@@ -97,7 +93,6 @@ CONV_CAUCHY_EPS= 1E-6
 %
 MESH_FILENAME= ../mesh_flatplate_140x100.su2
 MESH_FORMAT= SU2
-%
 SCREEN_OUTPUT= (INNER_ITER, WALL_TIME, RMS_PRESSURE, RMS_VELOCITY-X, RMS_VELOCITY-Y, RMS_TEMPERATURE, RMS_NU_TILDE, \
                 LINSOL_ITER, LINSOL_RESIDUAL, LIFT, DRAG)
 SCREEN_WRT_FREQ_INNER= 10
diff --git a/TestCases/wallfunctions/flatplate/incompressible_SST/turb_SST_flatplate.cfg b/TestCases/wallfunctions/flatplate/incompressible_SST/turb_SST_flatplate.cfg
index 93377c3c8c1..ae875576c6c 100644
--- a/TestCases/wallfunctions/flatplate/incompressible_SST/turb_SST_flatplate.cfg
+++ b/TestCases/wallfunctions/flatplate/incompressible_SST/turb_SST_flatplate.cfg
@@ -6,7 +6,7 @@
 % Author: Nijso Beishuizen, T. Kattmann                                        %
 % Institution: Bosch Thermotechnology                                          %
 % Date: 2021.09.01                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
@@ -39,10 +39,8 @@ REF_AREA= 2.0
 %
 MARKER_HEATFLUX= ( wall, 0.0 )
 MARKER_SYM= ( symmetry )
-%
 INC_INLET_TYPE= VELOCITY_INLET
 MARKER_INLET= ( inlet, 302.4, 70.0, 1.0, 0.0, 0.0 )
-%
 INC_OUTLET_TYPE= PRESSURE_OUTLET PRESSURE_OUTLET
 MARKER_OUTLET= ( outlet, 0.0, farfield, 0.0 )
 %
@@ -68,11 +66,7 @@ LINEAR_SOLVER= FGMRES
 LINEAR_SOLVER_PREC= ILU
 LINEAR_SOLVER_ERROR= 1e-15
 LINEAR_SOLVER_ITER= 10
-%
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-MGLEVEL= 0
-%
+
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= FDS
@@ -97,15 +91,12 @@ CONV_CAUCHY_EPS= 1E-6
 %
 MESH_FILENAME= ../mesh_flatplate_140x100.su2
 MESH_FORMAT= SU2
-%
 SCREEN_OUTPUT= (INNER_ITER, WALL_TIME, RMS_PRESSURE, RMS_VELOCITY-X, RMS_VELOCITY-Y, RMS_TEMPERATURE, RMS_TKE, RMS_DISSIPATION, \
                 LINSOL_ITER, LINSOL_RESIDUAL, LIFT, DRAG, TOTAL_HEATFLUX)
 SCREEN_WRT_FREQ_INNER= 10
-%
 HISTORY_OUTPUT= (ITER, RMS_RES, AERO_COEFF, FLOW_COEFF)
 MARKER_PLOTTING= ( wall )
 MARKER_MONITORING= ( wall )
-%
 OUTPUT_FILES= RESTART, PARAVIEW_MULTIBLOCK
 VOLUME_OUTPUT= RESIDUAL, PRIMITIVE
 OUTPUT_WRT_FREQ= 1000, 500 
diff --git a/UnitTests/Common/containers/CLookupTable_tests.cpp b/UnitTests/Common/containers/CLookupTable_tests.cpp
index d19d1800fc0..29b223afc85 100644
--- a/UnitTests/Common/containers/CLookupTable_tests.cpp
+++ b/UnitTests/Common/containers/CLookupTable_tests.cpp
@@ -2,7 +2,7 @@
  * \file CLookupTable_tests.cpp
  * \brief Unit tests for the lookup table.
  * \author N. Beishuizen
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/Common/geometry/CGeometry_test.cpp b/UnitTests/Common/geometry/CGeometry_test.cpp
index 9a42f709ded..1250e1fa72c 100644
--- a/UnitTests/Common/geometry/CGeometry_test.cpp
+++ b/UnitTests/Common/geometry/CGeometry_test.cpp
@@ -2,7 +2,7 @@
  * \file CGeometry_tests.cpp
  * \brief Unit tests for CGeometry.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/Common/geometry/dual_grid/CDualGrid_tests.cpp b/UnitTests/Common/geometry/dual_grid/CDualGrid_tests.cpp
index 638fff15cf8..6e62c87b44f 100644
--- a/UnitTests/Common/geometry/dual_grid/CDualGrid_tests.cpp
+++ b/UnitTests/Common/geometry/dual_grid/CDualGrid_tests.cpp
@@ -2,7 +2,7 @@
  * \file CDualGrid_tests.cpp
  * \brief Unit tests for the dual grid classes
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/Common/geometry/primal_grid/CPrimalGrid_tests.cpp b/UnitTests/Common/geometry/primal_grid/CPrimalGrid_tests.cpp
index 9f238af182c..ba72f34e9ff 100644
--- a/UnitTests/Common/geometry/primal_grid/CPrimalGrid_tests.cpp
+++ b/UnitTests/Common/geometry/primal_grid/CPrimalGrid_tests.cpp
@@ -2,7 +2,7 @@
  * \file CPrimalGrid_tests.cpp
  * \brief Unit tests for the primal grid classes
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/Common/simple_ad_test.cpp b/UnitTests/Common/simple_ad_test.cpp
index 8c44470a47c..42bd4530f8d 100644
--- a/UnitTests/Common/simple_ad_test.cpp
+++ b/UnitTests/Common/simple_ad_test.cpp
@@ -4,7 +4,7 @@
  *        basic functionality, this also serves as a regression test
  *        to make sure that AD works within unit testing.
  * \author C. Pederson
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/Common/simple_directdiff_test.cpp b/UnitTests/Common/simple_directdiff_test.cpp
index cf29beb362f..82dbbba13c6 100644
--- a/UnitTests/Common/simple_directdiff_test.cpp
+++ b/UnitTests/Common/simple_directdiff_test.cpp
@@ -4,7 +4,7 @@
  *        basic functionality, this also serves as a regression test
  *        to make sure that DD works within unit testing.
  * \author C. Pederson
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/Common/toolboxes/C1DInterpolation_tests.cpp b/UnitTests/Common/toolboxes/C1DInterpolation_tests.cpp
index ccc038e5244..d6e0e483011 100644
--- a/UnitTests/Common/toolboxes/C1DInterpolation_tests.cpp
+++ b/UnitTests/Common/toolboxes/C1DInterpolation_tests.cpp
@@ -2,7 +2,7 @@
  * \file C1DInterpolation_tests.cpp
  * \brief Unit tests for splines and what not.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/Common/toolboxes/CQuasiNewtonInvLeastSquares_tests.cpp b/UnitTests/Common/toolboxes/CQuasiNewtonInvLeastSquares_tests.cpp
index c07d6034809..91c8e13019f 100644
--- a/UnitTests/Common/toolboxes/CQuasiNewtonInvLeastSquares_tests.cpp
+++ b/UnitTests/Common/toolboxes/CQuasiNewtonInvLeastSquares_tests.cpp
@@ -3,7 +3,7 @@
  * \brief Unit tests for the CQuasiNewtonInvLeastSquares class.
  * Which should find the root of a n-d linear problem in n+1 iterations.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/Common/toolboxes/ndflattener_tests.cpp b/UnitTests/Common/toolboxes/ndflattener_tests.cpp
index 0a84bb8f585..99a24ea4a3f 100644
--- a/UnitTests/Common/toolboxes/ndflattener_tests.cpp
+++ b/UnitTests/Common/toolboxes/ndflattener_tests.cpp
@@ -2,7 +2,7 @@
  * \file ndflattener_tests.cpp
  * \brief Unit tests for NdFlattener template classes.
  * \author M. Aehle
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/Common/vectorization.cpp b/UnitTests/Common/vectorization.cpp
index ac35ccd0bc0..33ca4f0c66f 100644
--- a/UnitTests/Common/vectorization.cpp
+++ b/UnitTests/Common/vectorization.cpp
@@ -2,7 +2,7 @@
  * \file vectorization.cpp
  * \brief Unit tests for the SIMD type and associated expression templates.
  * \author P. Gomes
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/SU2_CFD/gradients.cpp b/UnitTests/SU2_CFD/gradients.cpp
index 6414812a79e..942fc9bc369 100644
--- a/UnitTests/SU2_CFD/gradients.cpp
+++ b/UnitTests/SU2_CFD/gradients.cpp
@@ -2,7 +2,7 @@
  * \file gradients.cpp
  * \brief Unit tests for gradient calculation.
  * \author P. Gomes, T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/SU2_CFD/numerics/CNumerics_tests.cpp b/UnitTests/SU2_CFD/numerics/CNumerics_tests.cpp
index ab91cab1837..173ec46dff6 100644
--- a/UnitTests/SU2_CFD/numerics/CNumerics_tests.cpp
+++ b/UnitTests/SU2_CFD/numerics/CNumerics_tests.cpp
@@ -2,7 +2,7 @@
  * \file CNumerics_tests.cpp
  * \brief Unit tests for the numerics classes.
  * \author C. Pederson
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/SU2_CFD/windowing.cpp b/UnitTests/SU2_CFD/windowing.cpp
index 4045e09ccaf..ef4b6b795ac 100644
--- a/UnitTests/SU2_CFD/windowing.cpp
+++ b/UnitTests/SU2_CFD/windowing.cpp
@@ -2,7 +2,7 @@
  * \file windowing.cpp
  * \brief Unit tests for windowed time-averaging.
  * \author C. Bauer
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/UnitQuadTestCase.hpp b/UnitTests/UnitQuadTestCase.hpp
index e64024a19b9..eb501ae4671 100644
--- a/UnitTests/UnitQuadTestCase.hpp
+++ b/UnitTests/UnitQuadTestCase.hpp
@@ -2,7 +2,7 @@
  * \file UnitQuadTestCase.hpp
  * \brief Simple unit quad test to be used in unit tests.
  * \author T. Albring
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/test_driver.cpp b/UnitTests/test_driver.cpp
index e2c27024d4c..175888e3dcd 100644
--- a/UnitTests/test_driver.cpp
+++ b/UnitTests/test_driver.cpp
@@ -2,7 +2,7 @@
  * \file test_driver.cpp
  * \brief The main entry point for unit tests (the main()).
  * \author C. Pederson
- * \version 7.4.0 "Blackbird"
+ * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/config_template.cfg b/config_template.cfg
index 26c4dd4b982..a7d0c468d8e 100644
--- a/config_template.cfg
+++ b/config_template.cfg
@@ -5,7 +5,7 @@
 % Author: ___________________________________________________________________  %
 % Institution: ______________________________________________________________  %
 % Date: __________                                                             %
-% File Version 7.4.0 "Blackbird"                                               %
+% File Version 7.5.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -29,6 +29,8 @@ SA_OPTIONS= NONE
 %
 % Transition model (NONE, LM)
 KIND_TRANS_MODEL= NONE
+% Specify versions/correlations of the LM model (LM2015, MALAN, SULUKSNA, KRAUSE, KRAUSE_HYPER, MEDIDA, MEDIDA_BAEDER, MENTER_LANGTRY)
+LM_OPTIONS= NONE
 %
 % Specify subgrid scale model(NONE, IMPLICIT_LES, SMAGORINSKY, WALE, VREMAN)
 KIND_SGS_MODEL= NONE
@@ -367,6 +369,10 @@ GAS_COMPOSITION= (0.77, 0.23, 0.0, 0.0, 0.0)
 % Freeze chemical reactions
 FROZEN_MIXTURE= NO
 %
+% NEMO Inlet Options
+INLET_TEMPERATURE_VE = 288.15
+INLET_GAS_COMPOSITION = (0.77, 0.23, 0.0, 0.0, 0.0)
+%
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
 % Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY, POLYNOMIAL_VISCOSITY).
@@ -764,6 +770,13 @@ BODY_FORCE= NO
 % Vector of body force values (BodyForce_X, BodyForce_Y, BodyForce_Z)
 BODY_FORCE_VECTOR= ( 0.0, 0.0, 0.0 )
 
+% --------------------------- VORTICITY_CONFINEMENT ---------------------------%
+%
+% Enable vorticity confinement (YES/NO)
+VORTICITY_CONFINEMENT = NO
+% Set confinement parameter (0.00 by default)
+CONFINEMENT_PARAM = 0.00
+
 % --------------------- STREAMWISE PERIODICITY DEFINITION ---------------------%
 %
 % Generally for streamwise periodictiy one has to set MARKER_PERIODIC= (<inlet>, <outlet>, ...)
diff --git a/externals/Makefile.am b/externals/Makefile.am
index 8848eefaaea..e01d77a5dbf 100644
--- a/externals/Makefile.am
+++ b/externals/Makefile.am
@@ -3,7 +3,7 @@
 # \file Makefile.am
 # \brief Makefile for external libraries
 # \author B. Kirk, T. Economon, F. Palacios
-# \version 7.4.0 "Blackbird"
+# \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/externals/tecio/Makefile.am b/externals/tecio/Makefile.am
index ecc99d26afb..0eec582e6b1 100644
--- a/externals/tecio/Makefile.am
+++ b/externals/tecio/Makefile.am
@@ -3,7 +3,7 @@
 # \file Makefile.am
 # \brief Makefile for external libraries
 # \author B. Kirk, T. Economon, F. Palacios
-# \version 7.4.0 "Blackbird"
+# \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/legacy/Makefile.am b/legacy/Makefile.am
index 022cace7f87..b98002bac4f 100644
--- a/legacy/Makefile.am
+++ b/legacy/Makefile.am
@@ -3,7 +3,7 @@
 # \file Makefile.am
 # \brief Global makefile for the SU2 project
 # \author M. Colonno, T. Economon, F. Palacios
-# \version 7.4.0 "Blackbird"
+# \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/legacy/configure.ac b/legacy/configure.ac
index 54e35ca089f..3a46b079a78 100644
--- a/legacy/configure.ac
+++ b/legacy/configure.ac
@@ -3,7 +3,7 @@
 # \file configure.ac
 # \brief Main file for configuring the autoconf/automake build process
 # \author M. Colonno, T. Economon, F. Palacios, B. Kirk
-# \version 7.4.0 "Blackbird"
+# \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/legacy/preconfigure.py b/legacy/preconfigure.py
index 688b1cc97b4..b5893cb3c21 100755
--- a/legacy/preconfigure.py
+++ b/legacy/preconfigure.py
@@ -3,7 +3,7 @@
 ## \file configure.py
 #  \brief An extended configuration script.
 #  \author T. Albring
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/meson.build b/meson.build
index 01655e23bb7..883383a7741 100644
--- a/meson.build
+++ b/meson.build
@@ -1,5 +1,5 @@
 project('SU2', 'c', 'cpp',
-        version: '7.4.0 "Blackbird"',
+        version: '7.5.0 "Blackbird"',
         license: 'LGPL2',
         default_options: ['buildtype=release',
                           'warning_level=0',
@@ -237,18 +237,22 @@ if get_option('enable-mpp')
 endif
 
 if get_option('enable-coolprop')
-  cmake = import('cmake')
-  cmake_opts = cmake.subproject_options()
-  cmake_opts.set_override_option('warning_level', '0')
-  cmake_opts.add_cmake_defines({
-    'COOLPROP_STATIC_LIBRARY': true,
-    'CMAKE_MAKE_PROGRAM': meson.source_root() + '/ninja',
-    'CMAKE_POSITION_INDEPENDENT_CODE': 'ON'
-  })
-  coolprop_subproj = cmake.subproject('CoolProp', options: cmake_opts)
-  coolprop_dep = coolprop_subproj.dependency('CoolProp')
-  su2_deps     += coolprop_dep
-  su2_cpp_args += '-DHAVE_COOLPROP'
+  if build_machine.cpu_family() == 'x86' or build_machine.cpu_family() == 'x86_64'
+    cmake = import('cmake')
+    cmake_opts = cmake.subproject_options()
+    cmake_opts.set_override_option('warning_level', '0')
+    cmake_opts.add_cmake_defines({
+      'COOLPROP_STATIC_LIBRARY': true,
+      'CMAKE_MAKE_PROGRAM': meson.source_root() + '/ninja',
+      'CMAKE_POSITION_INDEPENDENT_CODE': 'ON'
+    })
+    coolprop_subproj = cmake.subproject('CoolProp', options: cmake_opts)
+    coolprop_dep = coolprop_subproj.dependency('CoolProp')
+    su2_deps     += coolprop_dep
+    su2_cpp_args += '-DHAVE_COOLPROP'
+  else
+    message('WARNING: CPU is not x86, skipping CoolProp dependency.')
+  endif
 endif
 
 
@@ -283,7 +287,7 @@ endif
 
 message('''-------------------------------------------------------------------------
          |    ___ _   _ ___                                                      |
-         |   / __| | | |_  )   Release 7.4.0 "Blackbird"                         |
+         |   / __| | | |_  )   Release 7.5.0 "Blackbird"                         |
          |   \__ \ |_| |/ /                                                      |
          |   |___/\___//___|   Meson Configuration Summary                       |
          |                                                                       |
diff --git a/meson.py b/meson.py
index 755c0aa589d..6962ef43f77 100755
--- a/meson.py
+++ b/meson.py
@@ -3,7 +3,7 @@
 ## \file meson.py
 #  \brief An extended meson script for setting up the environment and running meson
 #  \author T. Albring
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index f9d6731b72a..1c072e0a039 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -4,7 +4,7 @@
 #  \brief Initializes necessary dependencies for SU2 either using git or it
 #         fetches zip files.
 #  \author T. Albring
-#  \version 7.4.0 "Blackbird"
+#  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
 # 
diff --git a/su2omp.syntax.json b/su2omp.syntax.json
index 3ea6266d6a5..a615c330238 100644
--- a/su2omp.syntax.json
+++ b/su2omp.syntax.json
@@ -4,7 +4,7 @@
     "\\file su2omp.syntax.json",
     "\\brief Definitions for the OpDiLib syntax checker",
     "\\author J. Blühdorn",
-    "\\version 7.4.0 \"Blackbird\"",
+    "\\version 7.5.0 \"Blackbird\"",
 
     "SU2 Project Website: https://su2code.github.io",
 

From 720d4edfba44dd00539cb04ebf76c2b9704a917e Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 13 Jan 2023 10:22:41 +0100
Subject: [PATCH 118/656] changed testcases branch for regression tests

---
 .github/workflows/regression.yml | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index e749e661e70..003525f926c 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c feature_multilayer_perceptron -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
         with:

From 1e0a2ef9b2edf5be060f6a0db58ebc910cc4dc5d Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 13 Jan 2023 13:33:55 +0100
Subject: [PATCH 119/656] Added datadriven fluid test case to regression tests

---
 TestCases/parallel_regression.py | 12 ++++++------
 1 file changed, 6 insertions(+), 6 deletions(-)

diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index d52d31e5491..857e50bc639 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -950,12 +950,12 @@ def main():
     test_list.append(coolprop_transportModel)
 
     # Subsonic Q1D nozzle using an MLP for thermodynamic state evaluation
-    #datadriven_MLP           = TestCase('datadriven_MLP')
-    #datadriven_MLP.cfg_dir   = "nicf/datadriven"
-    #datadriven_MLP.cfg_file  = "datadriven_nozzle.cfg"
-    #datadriven_MLP.test_iter = 100
-    #datadriven_MLP.test_vals = [-3.419718, -2.279820, 3.423614, 0.000000, 0.000000]
-    #test_list.append(datadriven_MLP)
+    datadriven_MLP           = TestCase('datadriven_MLP')
+    datadriven_MLP.cfg_dir   = "nicf/datadriven"
+    datadriven_MLP.cfg_file  = "datadriven_nozzle.cfg"
+    datadriven_MLP.test_iter = 100
+    datadriven_MLP.test_vals = [-3.419718, -2.279820, 3.423614, 0.000000, 0.000000]
+    test_list.append(datadriven_MLP)
 
     ######################################
     ### Turbomachinery                 ###

From 2e0cb94c1969d070507bf9b0c77191bdc005b540 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 13 Jan 2023 14:19:05 +0100
Subject: [PATCH 120/656] Changed MLP file name in datadriven config file to be
 compatible with test case

---
 TestCases/nicf/datadriven/datadriven_nozzle.cfg | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/nicf/datadriven/datadriven_nozzle.cfg b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
index 2fac6c2b7c2..e49a886c11e 100644
--- a/TestCases/nicf/datadriven/datadriven_nozzle.cfg
+++ b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
@@ -37,7 +37,7 @@ REF_DIMENSIONALIZATION= DIMENSIONAL
 %
 FLUID_MODEL = DATADRIVEN_FLUID
 INTERPOLATION_METHOD = MLP 
-FILENAMES_INTERPOLATOR = (mlp_air.mlp)
+FILENAMES_INTERPOLATOR = (MLP_air.mlp)
 DATADRIVEN_NEWTON_RELAXATION = 0.06
 DATADRIVEN_FLUID_INITIAL_DENSITY = 5.54548
 DATADRIVEN_FLUID_INITIAL_ENERGY = 1.8e+05

From 882e4c347b6312e22930e7ca9015f2b1af880314 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 13 Jan 2023 16:13:26 +0100
Subject: [PATCH 121/656] Changed regression values

---
 TestCases/parallel_regression.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 857e50bc639..fa955947494 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -954,7 +954,7 @@ def main():
     datadriven_MLP.cfg_dir   = "nicf/datadriven"
     datadriven_MLP.cfg_file  = "datadriven_nozzle.cfg"
     datadriven_MLP.test_iter = 100
-    datadriven_MLP.test_vals = [-3.419718, -2.279820, 3.423614, 0.000000, 0.000000]
+    datadriven_MLP.test_vals = [-4.716703, -2.781021, 2.476446, 0.000000, 0.000000]
     test_list.append(datadriven_MLP)
 
     ######################################

From 9354e279a690a6159fa1783d3f0e5448dbf75e0b Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Fri, 13 Jan 2023 15:04:41 -0800
Subject: [PATCH 122/656] edits to GY diff model, incorporate ion-ion
 collisions

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 SU2_CFD/src/fluid/CSU2TCLib.cpp | 35 +++++++++++++++++++++++++--------
 1 file changed, 27 insertions(+), 8 deletions(-)

diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index d5b40df5cdf..39543142418 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1883,9 +1883,6 @@ void CSU2TCLib::ThermalConductivitiesWBE(){
 
 void CSU2TCLib::DiffusionCoeffGY(){
 
-  su2double pi = PI_NUMBER;
-  su2double kb = BOLTZMANN_CONSTANT;
-
   /*--- Calculate mixture gas constant ---*/
   su2double gam_t = 0.0;
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
@@ -1893,7 +1890,7 @@ void CSU2TCLib::DiffusionCoeffGY(){
   }
 
   /*--- Mixture thermal conductivity via Gupta-Yos approximation ---*/
-  for (iSpecies = 0; iSpecies < nHeavy; iSpecies++) {
+  for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
 
     /*--- Initialize the species diffusion coefficient ---*/
     DiffusionCoeff[iSpecies] = 0.0;
@@ -1902,17 +1899,39 @@ void CSU2TCLib::DiffusionCoeffGY(){
     su2double Mi    = MolarMass[iSpecies];
     su2double gam_i = rhos[iSpecies] / (Density*Mi);
     su2double denom = 0.0;
-    for (jSpecies = 0; jSpecies < nHeavy; jSpecies++) {
-      if (jSpecies != iSpecies) {
+    for (jSpecies = 0; jSpecies < nSpecies; jSpecies++) {
+      if (jSpecies != iSpecies) { 
 
         su2double Mj    = MolarMass[jSpecies];
         su2double gam_j = rhos[iSpecies] / (Density*Mj);
 
-        /*--- Calculate the Omega^(0,0)_ij collision cross section ---*/
-        su2double Omega_ij = 1E-20 * Omega00(iSpecies,jSpecies,3)
+        su2double pi = PI_NUMBER;
+        su2double kb = BOLTZMANN_CONSTANT;
+
+        /*--- Check whether to use collision cross section data or Coulomb potential ---*/
+        if (Omega00(iSpecies, jSpecies, 0) == 1.0) {
+
+          /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
+          // TODO: Need to rework the bottom section below - add/convert values from option structure
+          su2double e_cgs = 4.8032047E−10; // CGS unit of fundamental electric charge TODO: confirm value
+          su2double kb_cgs = 1.3807E-16; // CGS unit of Boltzmann Constant TODO: confirm value
+          su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6// CGS unit of electron number density TODO: confirm value
+          
+          su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
+          su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
+
+          
+
+          su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log()
+        } else {
+
+          /*--- Calculate the Omega^(0,0)_ij collision cross section ---*/
+          su2double Omega_ij = 1E-20 * Omega00(iSpecies,jSpecies,3)
                             * pow(T, Omega00(iSpecies,jSpecies,0)*log(T)*log(T)
                                    + Omega00(iSpecies,jSpecies,1)*log(T)
                                    + Omega00(iSpecies,jSpecies,2));
+        }
+
         /*--- Calculate "delta1_ij" ---*/
         su2double d1_ij = 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij;
 

From fbf738a50aaa6c1ef77d2e4ddb5c62ca5035c200 Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Fri, 13 Jan 2023 15:38:17 -0800
Subject: [PATCH 123/656] adding formulae for coulomb potential

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 SU2_CFD/src/fluid/CSU2TCLib.cpp | 104 ++++++++++++--------------------
 1 file changed, 39 insertions(+), 65 deletions(-)

diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 39543142418..5318efbf680 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1908,23 +1908,38 @@ void CSU2TCLib::DiffusionCoeffGY(){
         su2double pi = PI_NUMBER;
         su2double kb = BOLTZMANN_CONSTANT;
 
+        // TODO: Need to rework the bottom section below - add/convert values from option structure
+        su2double e_cgs = 4.8032047E−10; // CGS unit of fundamental electric charge TODO: confirm value
+        su2double kb_cgs = 1.3807E-16; // CGS unit of Boltzmann Constant TODO: confirm value
+        su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6// CGS unit of electron number density TODO: confirm value
+          
+        su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
+        su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
+
         /*--- Check whether to use collision cross section data or Coulomb potential ---*/
-        if (Omega00(iSpecies, jSpecies, 0) == 1.0) {
+        if (Omega00(iSpecies, jSpecies, 0) == 1.0) { // attractive potential
 
           /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
-          // TODO: Need to rework the bottom section below - add/convert values from option structure
-          su2double e_cgs = 4.8032047E−10; // CGS unit of fundamental electric charge TODO: confirm value
-          su2double kb_cgs = 1.3807E-16; // CGS unit of Boltzmann Constant TODO: confirm value
-          su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6// CGS unit of electron number density TODO: confirm value
-          
-          su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
-          su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
+          su2double D1 = 0.784;
+          su2double C1 = -0.476;
+          su2double c1 = 0.0313;
 
-          
+          su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1*T_star*(1 - C1 * exp(-c1 * T_star))+1);
 
-          su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log()
+
+        } else if (Omega00(iSpecies, jSpecies, 0) == -1.0) { // repulsive potential
+
+          /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
+          su2double D1 = 0.765;
+          su2double C1 = 0.138;
+          su2double c1 = 0.0106;
+
+          su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1*T_star*(1 - C1 * exp(-c1 * T_star))+1);
+
+            
         } else {
 
+          // TODO: check which omega values to use: (0,0), (1,1), etc.
           /*--- Calculate the Omega^(0,0)_ij collision cross section ---*/
           su2double Omega_ij = 1E-20 * Omega00(iSpecies,jSpecies,3)
                             * pow(T, Omega00(iSpecies,jSpecies,0)*log(T)*log(T)
@@ -1932,65 +1947,24 @@ void CSU2TCLib::DiffusionCoeffGY(){
                                    + Omega00(iSpecies,jSpecies,2));
         }
 
-        /*--- Calculate "delta1_ij" ---*/
-        su2double d1_ij = 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij;
-
-        /*--- Calculate heavy-particle binary diffusion coefficient ---*/
-        su2double D_ij = kb*T/(Pressure*d1_ij);
-        denom += gam_j/D_ij;
+        if (iSpecies == 0) {
+          /*--- Calculate "delta1_ij" ---*/
+          su2double d1_ij = 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*Tve*(Mi+Mj))) * Omega_ij;
+          /*--- Calculate heavy-particle binary diffusion coefficient ---*/
+          su2double D_ij = kb*Tve/(Pressure*d1_ij);
+          denom += gam_j/D_ij;
+        } else {
+          /*--- Calculate "delta1_ij" ---*/
+          su2double d1_ij = 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij;
+          /*--- Calculate heavy-particle binary diffusion coefficient ---*/
+          su2double D_ij = kb*T/(Pressure*d1_ij);
+          denom += gam_j/D_ij;
+        }
       }
     }
-    //if (ionization) {
-    //TODO UPDATE WITH PROPER iElectron value.....
-    //  jSpecies = nSpecies-1;
-    //  su2double Mj       = MolarMass[jSpecies];
-    //  su2double gam_j    = rhos[iSpecies] / (Density*Mj);
-
-      /*--- Calculate the Omega^(0,0)_ij collision cross section ---*/
-    // su2double Omega_ij = 1E-20 * Omega00(iSpecies,jSpecies,3)
-    //      * pow(Tve, Omega00(iSpecies,jSpecies,0)*log(Tve)*log(Tve)
-    //      + Omega00(iSpecies,jSpecies,1)*log(Tve)
-    //      + Omega00(iSpecies,jSpecies,2));
-
-    //  /*--- Calculate "delta1_ij" ---*/
-    //  su2double d1_ij = 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*Tve*(Mi+Mj))) * Omega_ij;
-    //}
-
-    /*--- Assign species diffusion coefficient ---*/
+    
     DiffusionCoeff[iSpecies] = (denom > EPS) ? (gam_t*gam_t*Mi*(1-Mi*gam_i) / denom) : su2double(0.0);
   }
-  // if (ionization) {
-  //TODO: Update correct iElectron....
-  //   iSpecies = nSpecies-1;
-
-  //   /*--- Initialize the species diffusion coefficient ---*/
-  //   DiffusionCoeff[iSpecies] = 0.0;
-
-  //   /*--- Calculate molar concentration ---*/
-  //   Mi      = MolarMass[iSpecies];
-  //   gam_i   = rhos[iSpecies] / (Density*Mi);
-  //   denom = 0.0;
-  //   for (jSpecies = 0; jSpecies < nHeavy; jSpecies++) {
-  //     if (iSpecies != jSpecies) {
-  //       Mj    = MolarMass[jSpecies];
-  //       gam_j = rhos[iSpecies] / (Density*Mj);
-
-  //       /*--- Calculate the Omega^(0,0)_ij collision cross section ---*/
-  //       Omega_ij = 1E-20 * Omega00(iSpecies,jSpecies,3)
-  //           * pow(Tve, Omega00(iSpecies,jSpecies,0)*log(Tve)*log(Tve)
-  //           + Omega00(iSpecies,jSpecies,1)*log(Tve)
-  //           + Omega00(iSpecies,jSpecies,2));
-
-  //       /*--- Calculate "delta1_ij" ---*/
-  //       d1_ij = 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*Tve*(Mi+Mj))) * Omega_ij;
-
-  //       /*--- Calculate heavy-particle binary diffusion coefficient ---*/
-  //       D_ij = kb*Tve/(Pressure*d1_ij);
-  //       denom += gam_j/D_ij;
-  //     }
-  //   }
-  //   DiffusionCoeff[iSpecies] = gam_t*gam_t*MolarMass[iSpecies]*(1-MolarMass[iSpecies]*gam_i) / denom;
-  // }
 }
 
 void CSU2TCLib::ViscosityGY(){

From 42cd42ff9e235717450c8b8b7cdaa925fecfa1d0 Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Sat, 14 Jan 2023 14:54:06 -0800
Subject: [PATCH 124/656] more updates to GY model

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 SU2_CFD/src/fluid/CSU2TCLib.cpp | 216 +++++++++++++++++---------------
 1 file changed, 117 insertions(+), 99 deletions(-)

diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 5318efbf680..df7cc8ec567 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1889,6 +1889,17 @@ void CSU2TCLib::DiffusionCoeffGY(){
     gam_t += rhos[iSpecies] / (Density*MolarMass[iSpecies]);
   }
 
+  // TODO: find a better place to store these
+  /*--- Attractive Coulombic potential constants ---*/
+  const su2double D1_a = 0.784;
+  const su2double C1_a = -0.476;
+  const su2double c1_a = 0.0313;
+
+  /*--- Repulsive Coulombic potential constants ---*/
+  const su2double D1 = 0.765;
+  const su2double C1 = 0.138;
+  const su2double c1 = 0.0106;
+
   /*--- Mixture thermal conductivity via Gupta-Yos approximation ---*/
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
 
@@ -1902,46 +1913,37 @@ void CSU2TCLib::DiffusionCoeffGY(){
     for (jSpecies = 0; jSpecies < nSpecies; jSpecies++) {
       if (jSpecies != iSpecies) { 
 
-        su2double Mj    = MolarMass[jSpecies];
-        su2double gam_j = rhos[iSpecies] / (Density*Mj);
+        const su2double Mj    = MolarMass[jSpecies];
+        const su2double gam_j = rhos[iSpecies] / (Density*Mj);
 
-        su2double pi = PI_NUMBER;
-        su2double kb = BOLTZMANN_CONSTANT;
+        const su2double pi = PI_NUMBER;
+        const su2double kb = BOLTZMANN_CONSTANT;
 
         // TODO: Need to rework the bottom section below - add/convert values from option structure
-        su2double e_cgs = 4.8032047E−10; // CGS unit of fundamental electric charge TODO: confirm value
-        su2double kb_cgs = 1.3807E-16; // CGS unit of Boltzmann Constant TODO: confirm value
-        su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6// CGS unit of electron number density TODO: confirm value
+        const su2double e_cgs = 4.8032047E−10; // CGS unit of fundamental electric charge TODO: confirm value
+        const su2double kb_cgs = 1.3807E-16; // CGS unit of Boltzmann Constant TODO: confirm value
+        const su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6// CGS unit of electron number density TODO: confirm value
           
-        su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
-        su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
+        const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
+        const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
 
         /*--- Check whether to use collision cross section data or Coulomb potential ---*/
         if (Omega00(iSpecies, jSpecies, 0) == 1.0) { // attractive potential
 
           /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
-          su2double D1 = 0.784;
-          su2double C1 = -0.476;
-          su2double c1 = 0.0313;
-
-          su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1*T_star*(1 - C1 * exp(-c1 * T_star))+1);
+          const su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);
 
 
         } else if (Omega00(iSpecies, jSpecies, 0) == -1.0) { // repulsive potential
 
           /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
-          su2double D1 = 0.765;
-          su2double C1 = 0.138;
-          su2double c1 = 0.0106;
+          const su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_r*T_star*(1 - C1_r * exp(-c1_r * T_star))+1);
 
-          su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1*T_star*(1 - C1 * exp(-c1 * T_star))+1);
-
-            
         } else {
 
           // TODO: check which omega values to use: (0,0), (1,1), etc.
           /*--- Calculate the Omega^(0,0)_ij collision cross section ---*/
-          su2double Omega_ij = 1E-20 * Omega00(iSpecies,jSpecies,3)
+          const su2double Omega_ij = 1E-20 * Omega00(iSpecies,jSpecies,3)
                             * pow(T, Omega00(iSpecies,jSpecies,0)*log(T)*log(T)
                                    + Omega00(iSpecies,jSpecies,1)*log(T)
                                    + Omega00(iSpecies,jSpecies,2));
@@ -1949,29 +1951,40 @@ void CSU2TCLib::DiffusionCoeffGY(){
 
         if (iSpecies == 0) {
           /*--- Calculate "delta1_ij" ---*/
-          su2double d1_ij = 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*Tve*(Mi+Mj))) * Omega_ij;
+          const su2double d1_ij = 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*Tve*(Mi+Mj))) * Omega_ij;
           /*--- Calculate heavy-particle binary diffusion coefficient ---*/
-          su2double D_ij = kb*Tve/(Pressure*d1_ij);
+          const su2double D_ij = kb*Tve/(Pressure*d1_ij);
           denom += gam_j/D_ij;
         } else {
           /*--- Calculate "delta1_ij" ---*/
-          su2double d1_ij = 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij;
+          const su2double d1_ij = 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij;
           /*--- Calculate heavy-particle binary diffusion coefficient ---*/
-          su2double D_ij = kb*T/(Pressure*d1_ij);
+          const su2double D_ij = kb*T/(Pressure*d1_ij);
           denom += gam_j/D_ij;
         }
       }
     }
-    
+
     DiffusionCoeff[iSpecies] = (denom > EPS) ? (gam_t*gam_t*Mi*(1-Mi*gam_i) / denom) : su2double(0.0);
   }
 }
 
 void CSU2TCLib::ViscosityGY(){
 
-  su2double pi = PI_NUMBER;
-  su2double Na = AVOGAD_CONSTANT;
-  su2double Mu = 0.0;
+  const su2double pi = PI_NUMBER;
+  const su2double Na = AVOGAD_CONSTANT;
+  const su2double Mu = 0.0;
+
+  // TODO: find a better place to store these
+  /*--- Attractive Coulombic potential constants ---*/
+  const su2double D1_a = 0.784;
+  const su2double C1_a = -0.476;
+  const su2double c1_a = 0.0313;
+
+  /*--- Repulsive Coulombic potential constants ---*/
+  const su2double D1 = 0.765;
+  const su2double C1 = 0.138;
+  const su2double c1 = 0.0106;
 
   /*--- Mixture viscosity via Gupta-Yos approximation ---*/
   for (iSpecies = 0; iSpecies < nHeavy; iSpecies++) {
@@ -1979,81 +1992,61 @@ void CSU2TCLib::ViscosityGY(){
     su2double denom = 0.0;
 
     /*--- Calculate molar concentration ---*/
-    su2double Mi    = MolarMass[iSpecies];
-    su2double gam_i = rhos[iSpecies] / (Density*Mi);
+    const ssu2double Mi    = MolarMass[iSpecies];
+    const su2double gam_i = rhos[iSpecies] / (Density*Mi);
 
     for (jSpecies = 0; jSpecies < nHeavy; jSpecies++) {
-      su2double Mj    = MolarMass[jSpecies];
-      su2double gam_j = rhos[jSpecies] / (Density*Mj);
+      const su2double Mj    = MolarMass[jSpecies];
+      const su2double gam_j = rhos[jSpecies] / (Density*Mj);
 
-      /*--- Calculate "delta" quantities ---*/
-      su2double Omega_ij = 1E-20 * Omega11(iSpecies,jSpecies,3)
+      // TODO: check omegaXX values
+      if (Omega11(iSpecies, jSpecies, 0) == 1.0) { // attractive potential
+
+          /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
+          const su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);
+      
+      } else if (Omega11(iSpecies, jSpecies, 0) == -1.0) { // repulsive potential
+
+          /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
+          const su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_r*T_star*(1 - C1_r * exp(-c1_r * T_star))+1);
+
+      } else {
+
+        const su2double Omega_ij = 1E-20 * Omega11(iSpecies,jSpecies,3)
           * pow(T, Omega11(iSpecies,jSpecies,0)*log(T)*log(T)
           + Omega11(iSpecies,jSpecies,1)*log(T)
           + Omega11(iSpecies,jSpecies,2));
-      su2double d2_ij = 16.0/5.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij;
+      }
 
-      /*--- Add to denominator of viscosity ---*/
-      denom += gam_j*d2_ij;
-    }
-    if (ionization) {
-      jSpecies = nSpecies-1;
-      su2double Mj    = MolarMass[jSpecies];
-      su2double gam_j = rhos[jSpecies] / (Density*Mj);
-
-      /*--- Calculate "delta" quantities ---*/
-      su2double Omega_ij = 1E-20 * Omega11(iSpecies,jSpecies,3)
-          * pow(Tve, Omega11(iSpecies,jSpecies,0)*log(Tve)*log(Tve)
-          + Omega11(iSpecies,jSpecies,1)*log(Tve)
-          + Omega11(iSpecies,jSpecies,2));
-      su2double d2_ij = 16.0/5.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*Tve*(Mi+Mj))) * Omega_ij;
-      denom += gam_j*d2_ij;
+        if (iSpeceis == 0) {
+          /*--- Calculate "delta" quantities ---*/
+          su2double d2_ij = 16.0/5.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*Tve*(Mi+Mj))) * Omega_ij;
+          /*--- Add to denominator of viscosity ---*/
+          denom += gam_j*d2_ij;
+      } else {
+          /*--- Calculate "delta" quantities ---*/
+          su2double d2_ij = 16.0/5.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij;
+          /*--- Add to denominator of viscosity ---*/
+          denom += gam_j*d2_ij;
+      }
     }
-
     /*--- Calculate species laminar viscosity ---*/
     Mu += (Mi/Na * gam_i) / denom;
   }
-  // if (ionization) {
-  //TODO iElectron value!!!!
-  //   iSpecies = nSpecies-1;
-  //   denom = 0.0;
-  //   /*--- Calculate molar concentration ---*/
-  //   Mi    = MolarMass[iSpecies];
-  //   gam_i = rhos[iSpecies] / (Density*Mi);
-  //   for (jSpecies = 0; jSpecies < nSpecies; jSpecies++) {
-  //     Mj    = MolarMass[jSpecies];
-  //     gam_j = rhos[jSpecies] / (Density*Mj);
-  //     /*--- Calculate "delta" quantities ---*/
-  //     Omega_ij = 1E-20 * Omega11(iSpecies,jSpecies,3)
-  //         * pow(Tve, Omega11(iSpecies,jSpecies,0)*log(Tve)*log(Tve)
-  //         + Omega11(iSpecies,jSpecies,1)*log(Tve)
-  //         + Omega11(iSpecies,jSpecies,2));
-  //     d2_ij = 16.0/5.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*Tve*(Mi+Mj))) * Omega_ij;
-  //     /*--- Add to denominator of viscosity ---*/
-  //     denom += gam_j*d2_ij;
-  //   }
-  //   Mu += (Mi/Na * gam_i) / denom;
-  // }
 }
 
 void CSU2TCLib::ThermalConductivitiesGY(){
 
-  su2double Mi, Mj, mi, mj, gam_i, gam_j, denom_t, denom_r, d1_ij, d2_ij, a_ij, Omega_ij;
-
-  su2double pi   = PI_NUMBER;
-  su2double Na   = AVOGAD_CONSTANT;
-  su2double kb   = BOLTZMANN_CONSTANT;
-
-  if (ionization) {
-    SU2_MPI::Error("NEEDS REVISION w/ IONIZATION",CURRENT_FUNCTION);
-  }
+  const su2double pi   = PI_NUMBER;
+  const su2double Na   = AVOGAD_CONSTANT;
+  const su2double kb   = BOLTZMANN_CONSTANT;
 
   /*--- Mixture vibrational-electronic specific heat ---*/
-  Cvves = ComputeSpeciesCvVibEle(Tve);
+  const auto Cvves = ComputeSpeciesCvVibEle(Tve);
   su2double rhoCvve = 0.0;
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
     rhoCvve += rhos[iSpecies]*Cvves[iSpecies];
-  su2double Cvve = rhoCvve/Density;
+  const su2double Cvve = rhoCvve/Density;
 
   /*--- Calculate mixture gas constant ---*/
   su2double R = 0.0;
@@ -2061,40 +2054,65 @@ void CSU2TCLib::ThermalConductivitiesGY(){
     R += Ru * rhos[iSpecies]/Density;
   }
 
+  // TODO: find a better place to store these
+  /*--- Attractive Coulombic potential constants ---*/
+  const su2double D1_a = 0.784;
+  const su2double C1_a = -0.476;
+  const su2double c1_a = 0.0313;
+
+  /*--- Repulsive Coulombic potential constants ---*/
+  const su2double D1 = 0.765;
+  const su2double C1 = 0.138;
+  const su2double c1 = 0.0106;
+
   /*--- Mixture thermal conductivity via Gupta-Yos approximation ---*/
-  ThermalCond_tr = 0.0;
-  ThermalCond_ve = 0.0;
+  su2double ThermalCond_tr = 0.0;
+  su2double ThermalCond_ve = 0.0;
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
 
     /*--- Calculate molar concentration ---*/
-    Mi      = MolarMass[iSpecies];
-    mi      = Mi/Na;
-    gam_i   = rhos[iSpecies] / (Density*Mi);
-    denom_t = 0.0;
-    denom_r = 0.0;
+    const su2double Mi      = MolarMass[iSpecies];
+    const su2double mi      = Mi/Na;
+    const su2double gam_i   = rhos[iSpecies] / (Density*Mi);
+    su2double denom_t = 0.0;
+    su2double denom_r = 0.0;
+
     for (jSpecies = 0; jSpecies < nSpecies; jSpecies++) {
-      Mj    = MolarMass[jSpecies];
-      mj    = Mj/Na;
-      gam_j = rhos[iSpecies] / (Density*Mj);
-      a_ij = 1.0 + (1.0 - mi/mj)*(0.45 - 2.54*mi/mj) / ((1.0 + mi/mj)*(1.0 + mi/mj));
+      const su2double Mj    = MolarMass[jSpecies];
+      const su2double mj    = Mj/Na;
+      const su2double gam_j = rhos[iSpecies] / (Density*Mj);
+      const su2double a_ij = 1.0 + (1.0 - mi/mj)*(0.45 - 2.54*mi/mj) / ((1.0 + mi/mj)*(1.0 + mi/mj));
+
+      if (Omega11(iSpecies, jSpecies, 0) == 1.0) { // attractive potential
+
+        /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
+        const su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);
+      
+      } else if (Omega11(iSpecies, jSpecies, 0) == 1.0) { // repulsive potential
+
+      } else {
+
+      }
+
 
       /*--- Calculate the Omega^(0,0)_ij collision cross section ---*/
-      Omega_ij = 1E-20 * Omega00(iSpecies,jSpecies,3)
+      const su2double Omega_ij = 1E-20 * Omega00(iSpecies,jSpecies,3)
           * pow(T, Omega00(iSpecies,jSpecies,0)*log(T)*log(T)
           + Omega00(iSpecies,jSpecies,1)*log(T)
           + Omega00(iSpecies,jSpecies,2));
 
       /*--- Calculate "delta1_ij" ---*/
-      d1_ij = 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij;
+      const su2double d1_ij = 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij;
 
       /*--- Calculate the Omega^(1,1)_ij collision cross section ---*/
-      Omega_ij = 1E-20 * Omega11(iSpecies,jSpecies,3)
+      const su2double Omega_ij = 1E-20 * Omega11(iSpecies,jSpecies,3)
           * pow(T, Omega11(iSpecies,jSpecies,0)*log(T)*log(T)
           + Omega11(iSpecies,jSpecies,1)*log(T)
           + Omega11(iSpecies,jSpecies,2));
 
       /*--- Calculate "delta2_ij" ---*/
-      d2_ij = 16.0/5.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij;
+      const su2double d2_ij = 16.0/5.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij;
+
       denom_t += a_ij*gam_j*d2_ij;
       denom_r += gam_j*d1_ij;
     }

From bbc901ad34432f764b63e897ea297f661972626e Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Sat, 14 Jan 2023 16:40:08 -0800
Subject: [PATCH 125/656] restructure dij computatiaon, clean up GY functions

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 SU2_CFD/include/fluid/CSU2TCLib.hpp |  10 ++
 SU2_CFD/src/fluid/CSU2TCLib.cpp     | 217 ++++++++++++----------------
 2 files changed, 102 insertions(+), 125 deletions(-)

diff --git a/SU2_CFD/include/fluid/CSU2TCLib.hpp b/SU2_CFD/include/fluid/CSU2TCLib.hpp
index e3d5b5d3b23..e483c7741e2 100644
--- a/SU2_CFD/include/fluid/CSU2TCLib.hpp
+++ b/SU2_CFD/include/fluid/CSU2TCLib.hpp
@@ -71,6 +71,16 @@ class CSU2TCLib : public CNEMOGas {
 
   const su2double T_ref_suth = 273.15; /*!<\brief Reference temperature for Sutherland's model [K] */
 
+  /*--- Attractive Coulombic potential constants ---*/
+  const su2double D1_a = 0.784;
+  const su2double C1_a = -0.476;
+  const su2double c1_a = 0.0313;
+
+  /*--- Repulsive Coulombic potential constants ---*/
+  const su2double D1_r = 0.765;
+  const su2double C1_r = 0.138;
+  const su2double c1_r = 0.0106;
+
   su2activematrix CharElTemp,    /*!< \brief Characteristic temperature of electron states. */
   ElDegeneracy,                  /*!< \brief Degeneracy of electron states. */
   RxnConstantTable,              /*!< \brief Table of chemical equiibrium reaction constants */
diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index df7cc8ec567..c426174fd88 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1881,6 +1881,84 @@ void CSU2TCLib::ThermalConductivitiesWBE(){
   ThermalConductivities[1] = ThermalCond_ve;
 }
 
+su2double CSU2TCLib::ComputeDelta1(su2double Omega, su2double T, ) {
+
+  if (ionization) {
+    // TODO: Need to rework the bottom section below - add/convert values from option structure
+    const su2double e_cgs = 4.8032047E−10; // CGS unit of fundamental electric charge TODO: confirm value
+    const su2double kb_cgs = 1.3807E-16; // CGS unit of Boltzmann Constant TODO: confirm value
+    const su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6// CGS unit of electron number density TODO: confirm value
+      
+    const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
+    const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
+  }
+
+  /*--- Check whether to use collision cross section data or Coulomb potential ---*/
+  if (Omega00(iSpecies, jSpecies, 0) == 1.0) { // attractive potential
+
+    /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
+    const su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);
+
+
+  } else if (Omega00(iSpecies, jSpecies, 0) == -1.0) { // repulsive potential
+
+    /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
+    const su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_r*T_star*(1 - C1_r * exp(-c1_r * T_star))+1);
+
+  } else {
+
+    // TODO: check which omega values to use: (0,0), (1,1), etc.
+    /*--- Calculate the Omega^(0,0)_ij collision cross section ---*/
+    const su2double Omega_ij = 1E-20 * Omega00(iSpecies,jSpecies,3)
+                      * pow(T, Omega00(iSpecies,jSpecies,0)*log(T)*log(T)
+                             + Omega00(iSpecies,jSpecies,1)*log(T)
+                             + Omega00(iSpecies,jSpecies,2));
+  }  
+  
+  const su2double d1_ij = 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij;
+
+  return d1_ij;
+}
+
+su2double CSU2TCLib::ComputeDelta2(su2double Omega, su2double T, ) {
+
+  if (ionization) {
+    // TODO: Need to rework the bottom section below - add/convert values from option structure
+    const su2double e_cgs = 4.8032047E−10; // CGS unit of fundamental electric charge TODO: confirm value
+    const su2double kb_cgs = 1.3807E-16; // CGS unit of Boltzmann Constant TODO: confirm value
+    const su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6// CGS unit of electron number density TODO: confirm value
+      
+    const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
+    const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
+  }
+
+  /*--- Check whether to use collision cross section data or Coulomb potential ---*/
+  if (Omega00(iSpecies, jSpecies, 0) == 1.0) { // attractive potential
+
+    /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
+    const su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);
+
+
+  } else if (Omega00(iSpecies, jSpecies, 0) == -1.0) { // repulsive potential
+
+    /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
+    const su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_r*T_star*(1 - C1_r * exp(-c1_r * T_star))+1);
+
+  } else {
+
+    // TODO: check which omega values to use: (0,0), (1,1), etc.
+    /*--- Calculate the Omega^(0,0)_ij collision cross section ---*/
+    const su2double Omega_ij = 1E-20 * Omega00(iSpecies,jSpecies,3)
+                      * pow(T, Omega00(iSpecies,jSpecies,0)*log(T)*log(T)
+                             + Omega00(iSpecies,jSpecies,1)*log(T)
+                             + Omega00(iSpecies,jSpecies,2));
+  }  
+  
+  const su2double d2_ij = 16.0/5.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij;
+
+  return d2_ij;
+}
+
 void CSU2TCLib::DiffusionCoeffGY(){
 
   /*--- Calculate mixture gas constant ---*/
@@ -1889,17 +1967,6 @@ void CSU2TCLib::DiffusionCoeffGY(){
     gam_t += rhos[iSpecies] / (Density*MolarMass[iSpecies]);
   }
 
-  // TODO: find a better place to store these
-  /*--- Attractive Coulombic potential constants ---*/
-  const su2double D1_a = 0.784;
-  const su2double C1_a = -0.476;
-  const su2double c1_a = 0.0313;
-
-  /*--- Repulsive Coulombic potential constants ---*/
-  const su2double D1 = 0.765;
-  const su2double C1 = 0.138;
-  const su2double c1 = 0.0106;
-
   /*--- Mixture thermal conductivity via Gupta-Yos approximation ---*/
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
 
@@ -1910,6 +1977,7 @@ void CSU2TCLib::DiffusionCoeffGY(){
     su2double Mi    = MolarMass[iSpecies];
     su2double gam_i = rhos[iSpecies] / (Density*Mi);
     su2double denom = 0.0;
+    
     for (jSpecies = 0; jSpecies < nSpecies; jSpecies++) {
       if (jSpecies != iSpecies) { 
 
@@ -1919,52 +1987,18 @@ void CSU2TCLib::DiffusionCoeffGY(){
         const su2double pi = PI_NUMBER;
         const su2double kb = BOLTZMANN_CONSTANT;
 
-        // TODO: Need to rework the bottom section below - add/convert values from option structure
-        const su2double e_cgs = 4.8032047E−10; // CGS unit of fundamental electric charge TODO: confirm value
-        const su2double kb_cgs = 1.3807E-16; // CGS unit of Boltzmann Constant TODO: confirm value
-        const su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6// CGS unit of electron number density TODO: confirm value
-          
-        const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
-        const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
-
-        /*--- Check whether to use collision cross section data or Coulomb potential ---*/
-        if (Omega00(iSpecies, jSpecies, 0) == 1.0) { // attractive potential
-
-          /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
-          const su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);
-
-
-        } else if (Omega00(iSpecies, jSpecies, 0) == -1.0) { // repulsive potential
-
-          /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
-          const su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_r*T_star*(1 - C1_r * exp(-c1_r * T_star))+1);
-
-        } else {
-
-          // TODO: check which omega values to use: (0,0), (1,1), etc.
-          /*--- Calculate the Omega^(0,0)_ij collision cross section ---*/
-          const su2double Omega_ij = 1E-20 * Omega00(iSpecies,jSpecies,3)
-                            * pow(T, Omega00(iSpecies,jSpecies,0)*log(T)*log(T)
-                                   + Omega00(iSpecies,jSpecies,1)*log(T)
-                                   + Omega00(iSpecies,jSpecies,2));
-        }
-
         if (iSpecies == 0) {
-          /*--- Calculate "delta1_ij" ---*/
-          const su2double d1_ij = 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*Tve*(Mi+Mj))) * Omega_ij;
-          /*--- Calculate heavy-particle binary diffusion coefficient ---*/
+          const su2double d1_ij = ComputeDelta1();
           const su2double D_ij = kb*Tve/(Pressure*d1_ij);
           denom += gam_j/D_ij;
         } else {
-          /*--- Calculate "delta1_ij" ---*/
-          const su2double d1_ij = 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij;
-          /*--- Calculate heavy-particle binary diffusion coefficient ---*/
+          const su2double d1_ij = ComputeDelta1();
           const su2double D_ij = kb*T/(Pressure*d1_ij);
           denom += gam_j/D_ij;
         }
       }
     }
-
+    /*--- Calculate species diffusion coefficient ---*/
     DiffusionCoeff[iSpecies] = (denom > EPS) ? (gam_t*gam_t*Mi*(1-Mi*gam_i) / denom) : su2double(0.0);
   }
 }
@@ -1975,19 +2009,8 @@ void CSU2TCLib::ViscosityGY(){
   const su2double Na = AVOGAD_CONSTANT;
   const su2double Mu = 0.0;
 
-  // TODO: find a better place to store these
-  /*--- Attractive Coulombic potential constants ---*/
-  const su2double D1_a = 0.784;
-  const su2double C1_a = -0.476;
-  const su2double c1_a = 0.0313;
-
-  /*--- Repulsive Coulombic potential constants ---*/
-  const su2double D1 = 0.765;
-  const su2double C1 = 0.138;
-  const su2double c1 = 0.0106;
-
   /*--- Mixture viscosity via Gupta-Yos approximation ---*/
-  for (iSpecies = 0; iSpecies < nHeavy; iSpecies++) {
+  for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
 
     su2double denom = 0.0;
 
@@ -1995,38 +2018,15 @@ void CSU2TCLib::ViscosityGY(){
     const ssu2double Mi    = MolarMass[iSpecies];
     const su2double gam_i = rhos[iSpecies] / (Density*Mi);
 
-    for (jSpecies = 0; jSpecies < nHeavy; jSpecies++) {
+    for (jSpecies = 0; jSpecies < nSpecies; jSpecies++) {
       const su2double Mj    = MolarMass[jSpecies];
       const su2double gam_j = rhos[jSpecies] / (Density*Mj);
 
-      // TODO: check omegaXX values
-      if (Omega11(iSpecies, jSpecies, 0) == 1.0) { // attractive potential
-
-          /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
-          const su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);
-      
-      } else if (Omega11(iSpecies, jSpecies, 0) == -1.0) { // repulsive potential
-
-          /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
-          const su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_r*T_star*(1 - C1_r * exp(-c1_r * T_star))+1);
-
-      } else {
-
-        const su2double Omega_ij = 1E-20 * Omega11(iSpecies,jSpecies,3)
-          * pow(T, Omega11(iSpecies,jSpecies,0)*log(T)*log(T)
-          + Omega11(iSpecies,jSpecies,1)*log(T)
-          + Omega11(iSpecies,jSpecies,2));
-      }
-
-        if (iSpeceis == 0) {
-          /*--- Calculate "delta" quantities ---*/
-          su2double d2_ij = 16.0/5.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*Tve*(Mi+Mj))) * Omega_ij;
-          /*--- Add to denominator of viscosity ---*/
+      if (iSpeceis == 0) {
+          const su2double d2_ij = ComputeDelta2();
           denom += gam_j*d2_ij;
       } else {
-          /*--- Calculate "delta" quantities ---*/
-          su2double d2_ij = 16.0/5.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij;
-          /*--- Add to denominator of viscosity ---*/
+          const su2double d2_ij = ComputeDelta2();
           denom += gam_j*d2_ij;
       }
     }
@@ -2054,17 +2054,6 @@ void CSU2TCLib::ThermalConductivitiesGY(){
     R += Ru * rhos[iSpecies]/Density;
   }
 
-  // TODO: find a better place to store these
-  /*--- Attractive Coulombic potential constants ---*/
-  const su2double D1_a = 0.784;
-  const su2double C1_a = -0.476;
-  const su2double c1_a = 0.0313;
-
-  /*--- Repulsive Coulombic potential constants ---*/
-  const su2double D1 = 0.765;
-  const su2double C1 = 0.138;
-  const su2double c1 = 0.0106;
-
   /*--- Mixture thermal conductivity via Gupta-Yos approximation ---*/
   su2double ThermalCond_tr = 0.0;
   su2double ThermalCond_ve = 0.0;
@@ -2083,36 +2072,14 @@ void CSU2TCLib::ThermalConductivitiesGY(){
       const su2double gam_j = rhos[iSpecies] / (Density*Mj);
       const su2double a_ij = 1.0 + (1.0 - mi/mj)*(0.45 - 2.54*mi/mj) / ((1.0 + mi/mj)*(1.0 + mi/mj));
 
-      if (Omega11(iSpecies, jSpecies, 0) == 1.0) { // attractive potential
-
-        /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
-        const su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);
-      
-      } else if (Omega11(iSpecies, jSpecies, 0) == 1.0) { // repulsive potential
-
+      if (iSpecies == 0) {
+        const su2double d1_ij = ComputeDelta1();
+        const su2double d2_ij = ComputeDelta2();
       } else {
-
+        const su2double d1_ij = ComputeDelta1();
+        const su2double d2_ij = ComputeDelta2();
       }
 
-
-      /*--- Calculate the Omega^(0,0)_ij collision cross section ---*/
-      const su2double Omega_ij = 1E-20 * Omega00(iSpecies,jSpecies,3)
-          * pow(T, Omega00(iSpecies,jSpecies,0)*log(T)*log(T)
-          + Omega00(iSpecies,jSpecies,1)*log(T)
-          + Omega00(iSpecies,jSpecies,2));
-
-      /*--- Calculate "delta1_ij" ---*/
-      const su2double d1_ij = 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij;
-
-      /*--- Calculate the Omega^(1,1)_ij collision cross section ---*/
-      const su2double Omega_ij = 1E-20 * Omega11(iSpecies,jSpecies,3)
-          * pow(T, Omega11(iSpecies,jSpecies,0)*log(T)*log(T)
-          + Omega11(iSpecies,jSpecies,1)*log(T)
-          + Omega11(iSpecies,jSpecies,2));
-
-      /*--- Calculate "delta2_ij" ---*/
-      const su2double d2_ij = 16.0/5.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij;
-
       denom_t += a_ij*gam_j*d2_ij;
       denom_r += gam_j*d1_ij;
     }

From 760d51b9a15a5c50cfa0365eef854333880124bb Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Sun, 15 Jan 2023 14:56:45 -0800
Subject: [PATCH 126/656] using function to compute delta, restructuring

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 SU2_CFD/src/fluid/CSU2TCLib.cpp | 73 ++++++++-------------------------
 1 file changed, 18 insertions(+), 55 deletions(-)

diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index c426174fd88..b69263fadaf 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1881,7 +1881,7 @@ void CSU2TCLib::ThermalConductivitiesWBE(){
   ThermalConductivities[1] = ThermalCond_ve;
 }
 
-su2double CSU2TCLib::ComputeDelta1(su2double Omega, su2double T, ) {
+su2double CSU2TCLib::ComputeDelta(unsigned iSpecies, unsigned jSpecies, su2double Mi, su2double Mj, su2double T, bool d1) {
 
   if (ionization) {
     // TODO: Need to rework the bottom section below - add/convert values from option structure
@@ -1915,48 +1915,13 @@ su2double CSU2TCLib::ComputeDelta1(su2double Omega, su2double T, ) {
                              + Omega00(iSpecies,jSpecies,2));
   }  
   
-  const su2double d1_ij = 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij;
-
-  return d1_ij;
-}
-
-su2double CSU2TCLib::ComputeDelta2(su2double Omega, su2double T, ) {
-
-  if (ionization) {
-    // TODO: Need to rework the bottom section below - add/convert values from option structure
-    const su2double e_cgs = 4.8032047E−10; // CGS unit of fundamental electric charge TODO: confirm value
-    const su2double kb_cgs = 1.3807E-16; // CGS unit of Boltzmann Constant TODO: confirm value
-    const su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6// CGS unit of electron number density TODO: confirm value
-      
-    const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
-    const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
-  }
-
-  /*--- Check whether to use collision cross section data or Coulomb potential ---*/
-  if (Omega00(iSpecies, jSpecies, 0) == 1.0) { // attractive potential
-
-    /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
-    const su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);
-
-
-  } else if (Omega00(iSpecies, jSpecies, 0) == -1.0) { // repulsive potential
-
-    /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
-    const su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_r*T_star*(1 - C1_r * exp(-c1_r * T_star))+1);
-
+  if (d1) {
+    const su2double d_ij = 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij; // d1_ij
   } else {
+    const su2double d_ij = 16.0/5.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij; // d2_ij
+  }
 
-    // TODO: check which omega values to use: (0,0), (1,1), etc.
-    /*--- Calculate the Omega^(0,0)_ij collision cross section ---*/
-    const su2double Omega_ij = 1E-20 * Omega00(iSpecies,jSpecies,3)
-                      * pow(T, Omega00(iSpecies,jSpecies,0)*log(T)*log(T)
-                             + Omega00(iSpecies,jSpecies,1)*log(T)
-                             + Omega00(iSpecies,jSpecies,2));
-  }  
-  
-  const su2double d2_ij = 16.0/5.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij;
-
-  return d2_ij;
+  return d_ij;
 }
 
 void CSU2TCLib::DiffusionCoeffGY(){
@@ -1974,10 +1939,10 @@ void CSU2TCLib::DiffusionCoeffGY(){
     DiffusionCoeff[iSpecies] = 0.0;
 
     /*--- Calculate molar concentration ---*/
-    su2double Mi    = MolarMass[iSpecies];
-    su2double gam_i = rhos[iSpecies] / (Density*Mi);
+    const su2double Mi    = MolarMass[iSpecies];
+    const su2double gam_i = rhos[iSpecies] / (Density*Mi);
     su2double denom = 0.0;
-    
+
     for (jSpecies = 0; jSpecies < nSpecies; jSpecies++) {
       if (jSpecies != iSpecies) { 
 
@@ -1988,11 +1953,11 @@ void CSU2TCLib::DiffusionCoeffGY(){
         const su2double kb = BOLTZMANN_CONSTANT;
 
         if (iSpecies == 0) {
-          const su2double d1_ij = ComputeDelta1();
+          const su2double d1_ij = ComputeDelta(iSpecies, jSpecies, Mi, Mj, Tve, true);
           const su2double D_ij = kb*Tve/(Pressure*d1_ij);
           denom += gam_j/D_ij;
         } else {
-          const su2double d1_ij = ComputeDelta1();
+          const su2double d1_ij = ComputeDelta(iSpecies, jSpecies, Mi, Mj, T, true);
           const su2double D_ij = kb*T/(Pressure*d1_ij);
           denom += gam_j/D_ij;
         }
@@ -2005,9 +1970,8 @@ void CSU2TCLib::DiffusionCoeffGY(){
 
 void CSU2TCLib::ViscosityGY(){
 
-  const su2double pi = PI_NUMBER;
   const su2double Na = AVOGAD_CONSTANT;
-  const su2double Mu = 0.0;
+  su2double Mu = 0.0;
 
   /*--- Mixture viscosity via Gupta-Yos approximation ---*/
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
@@ -2023,10 +1987,10 @@ void CSU2TCLib::ViscosityGY(){
       const su2double gam_j = rhos[jSpecies] / (Density*Mj);
 
       if (iSpeceis == 0) {
-          const su2double d2_ij = ComputeDelta2();
+          const su2double d2_ij = ComputeDelta(iSpecies, jSpecies, Mi, Mj, Tve, false);
           denom += gam_j*d2_ij;
       } else {
-          const su2double d2_ij = ComputeDelta2();
+          const su2double d2_ij = ComputeDelta(iSpecies, jSpecies, Mi, Mj, T, false);
           denom += gam_j*d2_ij;
       }
     }
@@ -2037,7 +2001,6 @@ void CSU2TCLib::ViscosityGY(){
 
 void CSU2TCLib::ThermalConductivitiesGY(){
 
-  const su2double pi   = PI_NUMBER;
   const su2double Na   = AVOGAD_CONSTANT;
   const su2double kb   = BOLTZMANN_CONSTANT;
 
@@ -2073,11 +2036,11 @@ void CSU2TCLib::ThermalConductivitiesGY(){
       const su2double a_ij = 1.0 + (1.0 - mi/mj)*(0.45 - 2.54*mi/mj) / ((1.0 + mi/mj)*(1.0 + mi/mj));
 
       if (iSpecies == 0) {
-        const su2double d1_ij = ComputeDelta1();
-        const su2double d2_ij = ComputeDelta2();
+        const su2double d1_ij = ComputeDelta(iSpecies, jSpecies, Mi, Mj, Tve, true);
+        const su2double d2_ij = ComputeDelta(iSpecies, jSpecies, Mi, Mj, Tve, false);
       } else {
-        const su2double d1_ij = ComputeDelta1();
-        const su2double d2_ij = ComputeDelta2();
+        const su2double d1_ij = ComputeDelta(iSpecies, jSpecies, Mi, Mj, T, true);
+        const su2double d2_ij = ComputeDelta(iSpecies, jSpecies, Mi, Mj, T, false);
       }
 
       denom_t += a_ij*gam_j*d2_ij;

From 2b7e3b60a2831536230bc398da60816ec1e4d141 Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Sun, 15 Jan 2023 15:28:17 -0800
Subject: [PATCH 127/656] rework values of necessary constants

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 Common/include/option_structure.hpp | 1 +
 SU2_CFD/src/fluid/CSU2TCLib.cpp     | 7 +++----
 2 files changed, 4 insertions(+), 4 deletions(-)

diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index d39d6abde86..13dfadf7b62 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -94,6 +94,7 @@ const su2double STANDARD_GRAVITY = 9.80665;           /*!< \brief Acceleration d
 const su2double UNIVERSAL_GAS_CONSTANT = 8.3144598;   /*!< \brief Universal gas constant in J/(mol*K) */
 const su2double BOLTZMANN_CONSTANT = 1.3806503E-23;   /*!< \brief Boltzmann's constant [J K^-1] */
 const su2double AVOGAD_CONSTANT = 6.0221415E26; /*!< \brief Avogadro's constant, number of particles in one kmole. */
+const su2double FUND_ELEC_CHARGE_CGS = 4.8032047E−10; /*!< \brief Fundamental electric charge in CGS units, cm^(3/2) g^(1/2) s^(-1). */
 
 const su2double EPS = 1.0E-16;        /*!< \brief Error scale. */
 const su2double TURB_EPS = 1.0E-16;   /*!< \brief Turbulent Error scale. */
diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index b69263fadaf..4b78cf7a083 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1884,10 +1884,9 @@ void CSU2TCLib::ThermalConductivitiesWBE(){
 su2double CSU2TCLib::ComputeDelta(unsigned iSpecies, unsigned jSpecies, su2double Mi, su2double Mj, su2double T, bool d1) {
 
   if (ionization) {
-    // TODO: Need to rework the bottom section below - add/convert values from option structure
-    const su2double e_cgs = 4.8032047E−10; // CGS unit of fundamental electric charge TODO: confirm value
-    const su2double kb_cgs = 1.3807E-16; // CGS unit of Boltzmann Constant TODO: confirm value
-    const su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6// CGS unit of electron number density TODO: confirm value
+    const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
+    const su2double kb_cgs = BOLTZMANN_CONSTANT*1E7; // CGS unit of Boltzmann Constant 
+    const su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6 // CGS unit of electron number density
       
     const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
     const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));

From 9a07e4d9cf9ca36b6897361527f6a01a6d24973e Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Sun, 15 Jan 2023 17:23:20 -0800
Subject: [PATCH 128/656] cleanup

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 SU2_CFD/src/fluid/CSU2TCLib.cpp | 31 +++++++++++++------------------
 1 file changed, 13 insertions(+), 18 deletions(-)

diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 4b78cf7a083..be4ad4610af 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1763,11 +1763,6 @@ vector<su2double>& CSU2TCLib::GetThermalConductivities(){
 
 void CSU2TCLib::DiffusionCoeffWBE(){
 
-  su2double Mi, Mj, Omega_ij, denom;
-  su2activematrix Dij;
-
-  Dij.resize(nSpecies, nSpecies) = su2double(0.0);
-
   /*--- Calculate species mole fraction ---*/
   su2double conc = 0.0;
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
@@ -1790,13 +1785,16 @@ void CSU2TCLib::DiffusionCoeffWBE(){
   /*--- Solve for binary diffusion coefficients ---*/
   // Note: Dij = Dji, so only loop through req'd indices
   // Note: Correlation requires kg/mol, hence 1E-3 conversion from kg/kmol
+  su2activematrix Dij;
+  Dij.resize(nSpecies, nSpecies) = su2double(0.0);
+
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
-    Mi = MolarMass[iSpecies]*1E-3;
+    const su2double Mi = MolarMass[iSpecies]*1E-3;
     for (jSpecies = iSpecies; jSpecies < nSpecies; jSpecies++) {
-      Mj = MolarMass[jSpecies]*1E-3;
+      const su2double Mj = MolarMass[jSpecies]*1E-3;
 
       /*--- Calculate the Omega^(0,0)_ij collision cross section ---*/
-      Omega_ij = 1E-20/PI_NUMBER * Omega00(iSpecies,jSpecies,3)
+      const su2double Omega_ij = 1E-20/PI_NUMBER * Omega00(iSpecies,jSpecies,3)
           * pow(T, Omega00(iSpecies,jSpecies,0)*log(T)*log(T)
           +  Omega00(iSpecies,jSpecies,1)*log(T)
           +  Omega00(iSpecies,jSpecies,2));
@@ -1808,7 +1806,7 @@ void CSU2TCLib::DiffusionCoeffWBE(){
   /*--- Calculate species-mixture diffusion coefficient --*/
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
     DiffusionCoeff[iSpecies] = 0.0;
-    denom = 0.0;
+    su2double denom = 0.0;
     for (jSpecies = 0; jSpecies < nSpecies; jSpecies++) {
       if (jSpecies != iSpecies) {
         denom += MolarFracWBE[jSpecies]/Dij(iSpecies,jSpecies);
@@ -1822,8 +1820,6 @@ void CSU2TCLib::DiffusionCoeffWBE(){
 
 void CSU2TCLib::ViscosityWBE(){
 
-  su2double tmp1, tmp2;
-
   /*--- Calculate species mole fraction ---*/
   su2double conc = 0.0;
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
@@ -1842,8 +1838,8 @@ void CSU2TCLib::ViscosityWBE(){
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
     phis[iSpecies] = 0.0;
     for (jSpecies = 0; jSpecies < nSpecies; jSpecies++) {
-      tmp1 = 1.0 + sqrt(mus[iSpecies]/mus[jSpecies])*pow(MolarMass[jSpecies]/MolarMass[iSpecies], 0.25);
-      tmp2 = sqrt(8.0*(1.0+MolarMass[iSpecies]/MolarMass[jSpecies]));
+      const su2double tmp1 = 1.0 + sqrt(mus[iSpecies]/mus[jSpecies])*pow(MolarMass[jSpecies]/MolarMass[iSpecies], 0.25);
+      const su2double tmp2 = sqrt(8.0*(1.0+MolarMass[iSpecies]/MolarMass[jSpecies]));
       phis[iSpecies] += MolarFracWBE[jSpecies]*tmp1*tmp1/tmp2;
     }
   }
@@ -1885,7 +1881,7 @@ su2double CSU2TCLib::ComputeDelta(unsigned iSpecies, unsigned jSpecies, su2doubl
 
   if (ionization) {
     const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
-    const su2double kb_cgs = BOLTZMANN_CONSTANT*1E7; // CGS unit of Boltzmann Constant 
+    const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
     const su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6 // CGS unit of electron number density
       
     const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
@@ -1893,13 +1889,12 @@ su2double CSU2TCLib::ComputeDelta(unsigned iSpecies, unsigned jSpecies, su2doubl
   }
 
   /*--- Check whether to use collision cross section data or Coulomb potential ---*/
-  if (Omega00(iSpecies, jSpecies, 0) == 1.0) { // attractive potential
+  if (Omega00(iSpecies, jSpecies, 0) == 1.0 && ionization) { // attractive potential
 
     /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
     const su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);
 
-
-  } else if (Omega00(iSpecies, jSpecies, 0) == -1.0) { // repulsive potential
+  } else if (Omega00(iSpecies, jSpecies, 0) == -1.0 && ionization) { // repulsive potential
 
     /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
     const su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_r*T_star*(1 - C1_r * exp(-c1_r * T_star))+1);
@@ -1970,7 +1965,7 @@ void CSU2TCLib::DiffusionCoeffGY(){
 void CSU2TCLib::ViscosityGY(){
 
   const su2double Na = AVOGAD_CONSTANT;
-  su2double Mu = 0.0;
+  Mu = 0.0;
 
   /*--- Mixture viscosity via Gupta-Yos approximation ---*/
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {

From eaaa47f96a6860f665bc39f81c35f07316ddef48 Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Mon, 16 Jan 2023 14:27:47 -0800
Subject: [PATCH 129/656] generalizing for non-ionized

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 SU2_CFD/src/fluid/CSU2TCLib.cpp | 57 ++++++++++++++++-----------------
 1 file changed, 27 insertions(+), 30 deletions(-)

diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index be4ad4610af..8e4be8e71d7 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1347,7 +1347,6 @@ vector<su2double>& CSU2TCLib::ComputeNetProductionRates(bool implicit, const su2
 
   /*--- Initialize variables ---*/
   unsigned short ii, iReaction;
-  su2double Keq;
   ws.resize(nSpecies,0.0);
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies ++)
     ws[iSpecies] = 0.0;
@@ -1356,8 +1355,8 @@ vector<su2double>& CSU2TCLib::ComputeNetProductionRates(bool implicit, const su2
   // Note: These parameters artificially increase the rate-controlling reaction
   //       temperature.  This relaxes some of the stiffness in the chemistry
   //       source term.
-  su2double T_min   = 800.0;
-  su2double epsilon = 80;
+  const su2double T_min   = 800.0;
+  const su2double epsilon = 80;
 
   /*--- Define preferential dissociation coefficient ---*/
   //alpha = 0.3; //TODO: make this a config option?
@@ -1381,7 +1380,7 @@ vector<su2double>& CSU2TCLib::ComputeNetProductionRates(bool implicit, const su2
     ComputeKeqConstants(iReaction);
 
     /*--- Calculate Keq ---*/
-    Keq = exp(  A[0]*(Thb/1E4) + A[1] + A[2]*log(1E4/Thb)
+    const su2double Keq = exp(  A[0]*(Thb/1E4) + A[1] + A[2]*log(1E4/Thb)
         + A[3]*(1E4/Thb) + A[4]*(1E4/Thb)*(1E4/Thb) );
 
     /*--- Calculate rate coefficients ---*/
@@ -1618,10 +1617,6 @@ su2double CSU2TCLib::ComputeEveSourceTerm(){
   // Note: Millikan & White relaxation time (requires P in Atm.)
   // Note: Park limiting cross section
 
-  su2double A_sr, B_sr, num, denom, Cs, sig_s, tau_sr, tauP, tauMW;
-  vector<su2double> MolarFrac;
-  su2activematrix mu;
-
   MolarFrac.resize(nSpecies,0.0);
   mu.resize(nSpecies,nSpecies)=su2double(0.0);
 
@@ -1635,6 +1630,8 @@ su2double CSU2TCLib::ComputeEveSourceTerm(){
     conc += rhos[iSpecies] / MolarMass[iSpecies];
     N    += rhos[iSpecies] / MolarMass[iSpecies] * AVOGAD_CONSTANT;
   }
+
+  vector<su2double> MolarFrac;
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
     MolarFrac[iSpecies] = (rhos[iSpecies] / MolarMass[iSpecies]) / conc;
 
@@ -1642,29 +1639,30 @@ su2double CSU2TCLib::ComputeEveSourceTerm(){
   eve_eq = ComputeSpeciesEve(T, true);
   eve    = ComputeSpeciesEve(Tve, true);
 
+  su2activematrix mu;
   /*--- Loop over species to calculate source term --*/
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
 
     /*--- Millikan & White relaxation time ---*/
-    num   = 0.0;
-    denom = 0.0;
+    su2double num   = 0.0;
+    su2double denom = 0.0;
     for (jSpecies = 0; jSpecies < nSpecies; jSpecies++) {
       mu(iSpecies,jSpecies) = MolarMass[iSpecies]*MolarMass[jSpecies] / (MolarMass[iSpecies] + MolarMass[jSpecies]);
-      A_sr   = 1.16 * 1E-3 * sqrt(mu(iSpecies,jSpecies)) * pow(CharVibTemp[iSpecies], 4.0/3.0);
-      B_sr   = 0.015 * pow(mu(iSpecies,jSpecies), 0.25);
-      tau_sr = 101325.0/Pressure * exp(A_sr*(pow(T,-1.0/3.0) - B_sr) - 18.42);
+      const su2double A_sr   = 1.16 * 1E-3 * sqrt(mu(iSpecies,jSpecies)) * pow(CharVibTemp[iSpecies], 4.0/3.0);
+      const su2double B_sr   = 0.015 * pow(mu(iSpecies,jSpecies), 0.25);
+      const su2double tau_sr = 101325.0/Pressure * exp(A_sr*(pow(T,-1.0/3.0) - B_sr) - 18.42);
 
       num   += MolarFrac[jSpecies];
       denom += MolarFrac[jSpecies] / tau_sr;
     }
 
-    tauMW = num / denom;
+    const su2double tauMW = num / denom;
 
     /*--- Park limiting cross section ---*/
-    Cs    = sqrt((8.0*Ru*T)/(PI_NUMBER*MolarMass[iSpecies]));
-    sig_s = 3E-21*(2.5E9)/(T*T);
+    const su2double Cs    = sqrt((8.0*Ru*T)/(PI_NUMBER*MolarMass[iSpecies]));
+    const su2double sig_s = 3E-21*(2.5E9)/(T*T);
 
-    tauP = 1/(sig_s*Cs*N);
+    const su2double tauP = 1/(sig_s*Cs*N);
 
     /*--- Species relaxation time ---*/
     taus[iSpecies] = tauMW + tauP;
@@ -1683,7 +1681,6 @@ su2double CSU2TCLib::ComputeEveSourceTerm(){
   omega = omegaVT + omegaCV;
 
   return omega;
-
 }
 
 void CSU2TCLib::GetEveSourceTermJacobian(const su2double *V, const su2double *eve, const su2double *cvve, const su2double *dTdU, const su2double* dTvedU, su2double **val_jacobian){
@@ -1877,7 +1874,7 @@ void CSU2TCLib::ThermalConductivitiesWBE(){
   ThermalConductivities[1] = ThermalCond_ve;
 }
 
-su2double CSU2TCLib::ComputeDelta(unsigned iSpecies, unsigned jSpecies, su2double Mi, su2double Mj, su2double T, bool d1) {
+su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies, su2double Mi, su2double Mj, su2double T, bool d1) {
 
   if (ionization) {
     const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
@@ -1946,12 +1943,12 @@ void CSU2TCLib::DiffusionCoeffGY(){
         const su2double pi = PI_NUMBER;
         const su2double kb = BOLTZMANN_CONSTANT;
 
-        if (iSpecies == 0) {
-          const su2double d1_ij = ComputeDelta(iSpecies, jSpecies, Mi, Mj, Tve, true);
+        if (iSpecies == 0 && ionization) {
+          const su2double d1_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, Tve, true);
           const su2double D_ij = kb*Tve/(Pressure*d1_ij);
           denom += gam_j/D_ij;
         } else {
-          const su2double d1_ij = ComputeDelta(iSpecies, jSpecies, Mi, Mj, T, true);
+          const su2double d1_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T, true);
           const su2double D_ij = kb*T/(Pressure*d1_ij);
           denom += gam_j/D_ij;
         }
@@ -1980,11 +1977,11 @@ void CSU2TCLib::ViscosityGY(){
       const su2double Mj    = MolarMass[jSpecies];
       const su2double gam_j = rhos[jSpecies] / (Density*Mj);
 
-      if (iSpeceis == 0) {
-          const su2double d2_ij = ComputeDelta(iSpecies, jSpecies, Mi, Mj, Tve, false);
+      if (iSpeceis == 0 && ionization) {
+          const su2double d2_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, Tve, false);
           denom += gam_j*d2_ij;
       } else {
-          const su2double d2_ij = ComputeDelta(iSpecies, jSpecies, Mi, Mj, T, false);
+          const su2double d2_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T, false);
           denom += gam_j*d2_ij;
       }
     }
@@ -2029,12 +2026,12 @@ void CSU2TCLib::ThermalConductivitiesGY(){
       const su2double gam_j = rhos[iSpecies] / (Density*Mj);
       const su2double a_ij = 1.0 + (1.0 - mi/mj)*(0.45 - 2.54*mi/mj) / ((1.0 + mi/mj)*(1.0 + mi/mj));
 
-      if (iSpecies == 0) {
-        const su2double d1_ij = ComputeDelta(iSpecies, jSpecies, Mi, Mj, Tve, true);
-        const su2double d2_ij = ComputeDelta(iSpecies, jSpecies, Mi, Mj, Tve, false);
+      if (iSpecies == 0 && ionization) {
+        const su2double d1_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, Tve, true);
+        const su2double d2_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, Tve, false);
       } else {
-        const su2double d1_ij = ComputeDelta(iSpecies, jSpecies, Mi, Mj, T, true);
-        const su2double d2_ij = ComputeDelta(iSpecies, jSpecies, Mi, Mj, T, false);
+        const su2double d1_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T, true);
+        const su2double d2_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T, false);
       }
 
       denom_t += a_ij*gam_j*d2_ij;

From 46680b52f32ac0ddbb10c4a41320250768775834 Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Mon, 16 Jan 2023 15:16:05 -0800
Subject: [PATCH 130/656] clearing compile errors

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 Common/include/option_structure.hpp |  2 +-
 SU2_CFD/include/fluid/CSU2TCLib.hpp |  3 ++
 SU2_CFD/src/fluid/CSU2TCLib.cpp     | 50 ++++++++++++++++++-----------
 3 files changed, 36 insertions(+), 19 deletions(-)

diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index 13dfadf7b62..80e45793ecd 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -94,7 +94,7 @@ const su2double STANDARD_GRAVITY = 9.80665;           /*!< \brief Acceleration d
 const su2double UNIVERSAL_GAS_CONSTANT = 8.3144598;   /*!< \brief Universal gas constant in J/(mol*K) */
 const su2double BOLTZMANN_CONSTANT = 1.3806503E-23;   /*!< \brief Boltzmann's constant [J K^-1] */
 const su2double AVOGAD_CONSTANT = 6.0221415E26; /*!< \brief Avogadro's constant, number of particles in one kmole. */
-const su2double FUND_ELEC_CHARGE_CGS = 4.8032047E−10; /*!< \brief Fundamental electric charge in CGS units, cm^(3/2) g^(1/2) s^(-1). */
+const su2double FUND_ELEC_CHARGE_CGS = 4.8032047E-10; /*!< \brief Fundamental electric charge in CGS units, cm^(3/2) g^(1/2) s^(-1). */
 
 const su2double EPS = 1.0E-16;        /*!< \brief Error scale. */
 const su2double TURB_EPS = 1.0E-16;   /*!< \brief Turbulent Error scale. */
diff --git a/SU2_CFD/include/fluid/CSU2TCLib.hpp b/SU2_CFD/include/fluid/CSU2TCLib.hpp
index e483c7741e2..595d1f9e187 100644
--- a/SU2_CFD/include/fluid/CSU2TCLib.hpp
+++ b/SU2_CFD/include/fluid/CSU2TCLib.hpp
@@ -61,6 +61,7 @@ class CSU2TCLib : public CNEMOGas {
   Wall_Catalycity,                /*!< \brief Specified wall species mass-fractions for catalytic boundaries. */
   Particle_Mass,                  /*!< \brief Mass of all particles present in the plasma */
   MolarFracWBE,                   /*!< \brief Molar fractions to be used in Wilke/Blottner/Eucken model */
+  MolarFrac,                      /*!< \brief Molar fractions */
   phis, mus,                      /*!< \brief Auxiliary vectors to be used in Wilke/Blottner/Eucken model */
   A;                              /*!< \brief Auxiliary vector to be used in net production rate computation */
 
@@ -259,6 +260,8 @@ class CSU2TCLib : public CNEMOGas {
    */
   void ThermalConductivitiesSuth();
 
+  su2double ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies, su2double Mi, su2double Mj, su2double T, bool d1);
+
   /*!
    * \brief Get reference temperature.
    */
diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 8e4be8e71d7..162b076bd6b 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1617,6 +1617,8 @@ su2double CSU2TCLib::ComputeEveSourceTerm(){
   // Note: Millikan & White relaxation time (requires P in Atm.)
   // Note: Park limiting cross section
 
+  su2activematrix mu;
+
   MolarFrac.resize(nSpecies,0.0);
   mu.resize(nSpecies,nSpecies)=su2double(0.0);
 
@@ -1639,7 +1641,6 @@ su2double CSU2TCLib::ComputeEveSourceTerm(){
   eve_eq = ComputeSpeciesEve(T, true);
   eve    = ComputeSpeciesEve(Tve, true);
 
-  su2activematrix mu;
   /*--- Loop over species to calculate source term --*/
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
 
@@ -1876,31 +1877,40 @@ void CSU2TCLib::ThermalConductivitiesWBE(){
 
 su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies, su2double Mi, su2double Mj, su2double T, bool d1) {
 
-  if (ionization) {
+  su2double pi = PI_NUMBER;
+
+  su2double Omega_ij;
+
+  /*--- Check whether to use collision cross section data or Coulomb potential ---*/
+  if (Omega00(iSpecies, jSpecies, 0) == 1.0 && ionization) { // attractive potential
+    
     const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
     const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
-    const su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6 // CGS unit of electron number density
+    const su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
       
     const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
     const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
-  }
-
-  /*--- Check whether to use collision cross section data or Coulomb potential ---*/
-  if (Omega00(iSpecies, jSpecies, 0) == 1.0 && ionization) { // attractive potential
-
+    
     /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
-    const su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);
+    Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);
 
   } else if (Omega00(iSpecies, jSpecies, 0) == -1.0 && ionization) { // repulsive potential
 
+    const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
+    const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
+    const su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
+      
+    const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
+    const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
+
     /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
-    const su2double Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_r*T_star*(1 - C1_r * exp(-c1_r * T_star))+1);
+    Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_r*T_star*(1 - C1_r * exp(-c1_r * T_star))+1);
 
   } else {
 
     // TODO: check which omega values to use: (0,0), (1,1), etc.
     /*--- Calculate the Omega^(0,0)_ij collision cross section ---*/
-    const su2double Omega_ij = 1E-20 * Omega00(iSpecies,jSpecies,3)
+    Omega_ij = 1E-20 * Omega00(iSpecies,jSpecies,3)
                       * pow(T, Omega00(iSpecies,jSpecies,0)*log(T)*log(T)
                              + Omega00(iSpecies,jSpecies,1)*log(T)
                              + Omega00(iSpecies,jSpecies,2));
@@ -1908,11 +1918,11 @@ su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies,
   
   if (d1) {
     const su2double d_ij = 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij; // d1_ij
+    return d_ij;
   } else {
     const su2double d_ij = 16.0/5.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij; // d2_ij
+    return d_ij;
   }
-
-  return d_ij;
 }
 
 void CSU2TCLib::DiffusionCoeffGY(){
@@ -1970,14 +1980,14 @@ void CSU2TCLib::ViscosityGY(){
     su2double denom = 0.0;
 
     /*--- Calculate molar concentration ---*/
-    const ssu2double Mi    = MolarMass[iSpecies];
+    const su2double Mi    = MolarMass[iSpecies];
     const su2double gam_i = rhos[iSpecies] / (Density*Mi);
 
     for (jSpecies = 0; jSpecies < nSpecies; jSpecies++) {
       const su2double Mj    = MolarMass[jSpecies];
       const su2double gam_j = rhos[jSpecies] / (Density*Mj);
 
-      if (iSpeceis == 0 && ionization) {
+      if (iSpecies == 0 && ionization) {
           const su2double d2_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, Tve, false);
           denom += gam_j*d2_ij;
       } else {
@@ -2029,13 +2039,17 @@ void CSU2TCLib::ThermalConductivitiesGY(){
       if (iSpecies == 0 && ionization) {
         const su2double d1_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, Tve, true);
         const su2double d2_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, Tve, false);
+
+        denom_t += a_ij*gam_j*d2_ij;
+        denom_r += gam_j*d1_ij;
+      
       } else {
         const su2double d1_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T, true);
         const su2double d2_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T, false);
+      
+        denom_t += a_ij*gam_j*d2_ij;
+        denom_r += gam_j*d1_ij;
       }
-
-      denom_t += a_ij*gam_j*d2_ij;
-      denom_r += gam_j*d1_ij;
     }
 
     /*--- Translational contribution to thermal conductivity ---*/

From 35cce08985a3119999662486ff58e68393c3437d Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Mon, 16 Jan 2023 15:31:08 -0800
Subject: [PATCH 131/656] remove unused vars

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 SU2_CFD/src/fluid/CSU2TCLib.cpp | 1 -
 1 file changed, 1 deletion(-)

diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 162b076bd6b..cd8c3ee9118 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1950,7 +1950,6 @@ void CSU2TCLib::DiffusionCoeffGY(){
         const su2double Mj    = MolarMass[jSpecies];
         const su2double gam_j = rhos[iSpecies] / (Density*Mj);
 
-        const su2double pi = PI_NUMBER;
         const su2double kb = BOLTZMANN_CONSTANT;
 
         if (iSpecies == 0 && ionization) {

From c423828b18ac378ad659eeccad75d4f4a3930db0 Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Mon, 16 Jan 2023 16:52:07 -0800
Subject: [PATCH 132/656] fix segfault

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 SU2_CFD/include/fluid/CSU2TCLib.hpp | 1 -
 SU2_CFD/src/fluid/CSU2TCLib.cpp     | 2 +-
 2 files changed, 1 insertion(+), 2 deletions(-)

diff --git a/SU2_CFD/include/fluid/CSU2TCLib.hpp b/SU2_CFD/include/fluid/CSU2TCLib.hpp
index 595d1f9e187..58fd28a8220 100644
--- a/SU2_CFD/include/fluid/CSU2TCLib.hpp
+++ b/SU2_CFD/include/fluid/CSU2TCLib.hpp
@@ -61,7 +61,6 @@ class CSU2TCLib : public CNEMOGas {
   Wall_Catalycity,                /*!< \brief Specified wall species mass-fractions for catalytic boundaries. */
   Particle_Mass,                  /*!< \brief Mass of all particles present in the plasma */
   MolarFracWBE,                   /*!< \brief Molar fractions to be used in Wilke/Blottner/Eucken model */
-  MolarFrac,                      /*!< \brief Molar fractions */
   phis, mus,                      /*!< \brief Auxiliary vectors to be used in Wilke/Blottner/Eucken model */
   A;                              /*!< \brief Auxiliary vector to be used in net production rate computation */
 
diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index cd8c3ee9118..16d2cb2d380 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1618,6 +1618,7 @@ su2double CSU2TCLib::ComputeEveSourceTerm(){
   // Note: Park limiting cross section
 
   su2activematrix mu;
+  vector<su2double> MolarFrac;
 
   MolarFrac.resize(nSpecies,0.0);
   mu.resize(nSpecies,nSpecies)=su2double(0.0);
@@ -1633,7 +1634,6 @@ su2double CSU2TCLib::ComputeEveSourceTerm(){
     N    += rhos[iSpecies] / MolarMass[iSpecies] * AVOGAD_CONSTANT;
   }
 
-  vector<su2double> MolarFrac;
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
     MolarFrac[iSpecies] = (rhos[iSpecies] / MolarMass[iSpecies]) / conc;
 

From 06ba2d8378f36b10b58b14dd3014720ecc11cb8b Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Mon, 16 Jan 2023 20:25:41 -0800
Subject: [PATCH 133/656] add Coulomb constants, corect collision integrals

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 SU2_CFD/include/fluid/CSU2TCLib.hpp |   6 ++
 SU2_CFD/src/fluid/CSU2TCLib.cpp     | 110 ++++++++++++++++++----------
 2 files changed, 78 insertions(+), 38 deletions(-)

diff --git a/SU2_CFD/include/fluid/CSU2TCLib.hpp b/SU2_CFD/include/fluid/CSU2TCLib.hpp
index 58fd28a8220..97caa81fcf7 100644
--- a/SU2_CFD/include/fluid/CSU2TCLib.hpp
+++ b/SU2_CFD/include/fluid/CSU2TCLib.hpp
@@ -75,11 +75,17 @@ class CSU2TCLib : public CNEMOGas {
   const su2double D1_a = 0.784;
   const su2double C1_a = -0.476;
   const su2double c1_a = 0.0313;
+  const su2double D2_a = 1.262;
+  const su2double C2_a = -0.146;
+  const su2double c2_a = 0.0377;
 
   /*--- Repulsive Coulombic potential constants ---*/
   const su2double D1_r = 0.765;
   const su2double C1_r = 0.138;
   const su2double c1_r = 0.0106;
+  const su2double D2_r = 1.235;
+  const su2double C2_r = 0.157;
+  const su2double c2_r = 0.0274;
 
   su2activematrix CharElTemp,    /*!< \brief Characteristic temperature of electron states. */
   ElDegeneracy,                  /*!< \brief Degeneracy of electron states. */
diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 16d2cb2d380..3f0319d68db 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1024,13 +1024,13 @@ CSU2TCLib::CSU2TCLib(const CConfig* config, unsigned short val_nDim, bool viscou
 
     // Omega(0,0) ----------------------
     //e-  (TODO: NO+ and e-,  NO+ and NO+, e- and e- ??????)
-    Omega00(0,0,0) = 0.0000000E+00;  Omega00(0,0,1) = 0.0000000E+00;  Omega00(0,0,2) = 0.0000000E+00;  Omega00(0,0,3) = 0.0000000E+00;
+    Omega00(0,0,0) = -1.000000E+00;  Omega00(0,0,1) = -1.000000E+00;  Omega00(0,0,2) = -1.000000E+00;  Omega00(0,0,3) = -1.000000E+00;
     Omega00(0,1,0) = -1.0525124E-02; Omega00(0,1,1) = 1.3498950E-01;  Omega00(0,1,2) = 1.2524805E-01;  Omega00(0,1,3) = 1.5066506E-01;
     Omega00(0,2,0) = 2.3527001E-02;  Omega00(0,2,1) = -6.9632323E-01; Omega00(0,2,2) = 6.8035475E+00;  Omega00(0,2,3) = 1.8335509E-09;
     Omega00(0,3,0) = 1.0414818E-01;  Omega00(0,3,1) = -2.8369126E+00; Omega00(0,3,2) = 2.5323135E+01;  Omega00(0,3,3) = 7.7138358E-32;
     Omega00(0,4,0) = 0.0000000E+00;  Omega00(0,4,1) = 1.6554247E-01;  Omega00(0,4,2) = -3.4986344E+00; Omega00(0,4,3) = 5.9268038E+08;
     Omega00(0,5,0) = 9.9865506E-03;  Omega00(0,5,1) = -2.7407431E-01; Omega00(0,5,2) = 2.6561032E+00;  Omega00(0,5,3) = 4.3080676E-04;
-    Omega00(0,6,0) = 0.0000000E+00;  Omega00(0,6,1) = 0.0000000E+00;  Omega00(0,6,2) = 0.0000000E+00;  Omega00(0,6,3) = 0.0000000E+00;
+    Omega00(0,6,0) = 1.0000000E+00;  Omega00(0,6,1) = 1.0000000E+00;  Omega00(0,6,2) = 1.0000000E+00;  Omega00(0,6,3) = 1.0000000E+00;
     //N2
     Omega00(1,0,0) = -1.0525124E-02; Omega00(1,0,1) = 1.3498950E-01;  Omega00(1,0,2) = 1.2524805E-01;  Omega00(1,0,3) = 1.5066506E-01;
     Omega00(1,1,0) = -6.0614558E-03; Omega00(1,1,1) = 1.2689102E-01;  Omega00(1,1,2) = -1.0616948E+00; Omega00(1,1,3) = 8.0955466E+02;
@@ -1072,24 +1072,24 @@ CSU2TCLib::CSU2TCLib(const CConfig* config, unsigned short val_nDim, bool viscou
     Omega00(5,5,0) = -6.4040535E-03; Omega00(5,5,1) = 1.4629949E-01;  Omega00(5,5,2) = -1.3892121E+00; Omega00(5,5,3) = 2.0903441E+03;
     Omega00(5,6,0) = -1.6409054E-02; Omega00(5,6,1) = 4.6352852E-01;  Omega00(5,6,2) = -4.5479735E+00; Omega00(5,6,3) = 7.4250671E+07;
     //NO+
-    Omega00(6,0,0) = 0.0000000E+00;  Omega00(6,0,1) = 0.0000000E+00;  Omega00(6,0,2) = 0.0000000E+00;  Omega00(6,0,3) = 0.0000000E+00;
+    Omega00(6,0,0) = 1.0000000E+00;  Omega00(6,0,1) = 1.0000000E+00;  Omega00(6,0,2) = 1.0000000E+00;  Omega00(6,0,3) = 1.0000000E+00;
     Omega00(6,1,0) = 0.0000000E+00;  Omega00(6,1,1) = 9.1205839E-02;  Omega00(6,1,2) = -1.8728231E+00; Omega00(6,1,3) = 2.4432020E+05;
     Omega00(6,2,0) = -3.7822765E-03; Omega00(6,2,1) = 1.7967016E-01;  Omega00(6,2,2) = -2.5409098E+00; Omega00(6,2,3) = 1.1840435E+06;
     Omega00(6,3,0) = -8.1158474E-03; Omega00(6,3,1) = 2.1474280E-01;  Omega00(6,3,2) = -2.0148450E+00; Omega00(6,3,3) = 6.2986385E+04;
     Omega00(6,4,0) = -1.9605234E-02; Omega00(6,4,1) = 5.5570872E-01;  Omega00(6,4,2) = -5.4285702E+00; Omega00(6,4,3) = 1.3574446E+09;
     Omega00(6,5,0) = -1.6409054E-02; Omega00(6,5,1) = 4.6352852E-01;  Omega00(6,5,2) = -4.5479735E+00; Omega00(6,5,3) = 7.4250671E+07;
-    Omega00(6,6,0) = 0.0000000E+00;  Omega00(6,6,1) = 0.0000000E+00;  Omega00(6,6,2) = 0.0000000E+00;  Omega00(6,6,3) = 0.0000000E+00;
+    Omega00(6,6,0) = -1.000000E+00;  Omega00(6,6,1) = -1.000000E+00;  Omega00(6,6,2) = -1.000000E+00;  Omega00(6,6,3) = -1.000000E+00;
 
 
     // Omega(1,1) ----------------------
     //e-    (TODO: NO+ and e-,  NO+ and NO+, e- and e- ??????)
-    Omega11(0,0,0) = 0.0000000E+00;  Omega11(0,0,1) = 0.0000000E+00;  Omega11(0,0,2) = 0.0000000E+00;  Omega11(0,0,3) = 0.0000000E+00;
+    Omega11(0,0,0) = -1.000000E+00;  Omega11(0,0,1) = -1.000000E+00;  Omega11(0,0,2) = -1.000000E+00;  Omega11(0,0,3) = -1.000000E+00;
     Omega11(0,1,0) = -4.2254948E-03; Omega11(0,1,1) = -5.2965163E-02; Omega11(0,1,2) = 1.9157708E+00;  Omega11(0,1,3) = 6.3263309E-04;
     Omega11(0,2,0) = 9.6744867E-03;  Omega11(0,2,1) = -3.3759583E-01; Omega11(0,2,2) = 3.7952121E+00;  Omega11(0,2,3) = 6.8468036E-06;
     Omega11(0,3,0) = 0.0000000E+00;  Omega11(0,3,1) = 5.4444485E-02;  Omega11(0,3,2) = -1.2854128E+00; Omega11(0,3,3) = 1.3857556E+04;
     Omega11(0,4,0) = -1.0903638E-01; Omega11(0,4,1) = 2.8678381E+00;  Omega11(0,4,2) = -2.5297550E+01; Omega11(0,4,3) = 3.4838798E+33;
     Omega11(0,5,0) = -1.7924100E-02; Omega11(0,5,1) = 4.0402656E-01;  Omega11(0,5,2) = -2.6712374E+00; Omega11(0,5,3) = 4.1447669E+02;
-    Omega11(0,6,0) = 0.0000000E+00;  Omega11(0,6,1) = 0.0000000E+00;  Omega11(0,6,2) = 0.0000000E+00;  Omega11(0,6,3) = 0.0000000E+00;
+    Omega11(0,6,0) = 1.0000000E+00;  Omega11(0,6,1) = 1.0000000E+00;  Omega11(0,6,2) = 1.0000000E+00;  Omega11(0,6,3) = 1.0000000E+00;
     //N2
     Omega11(1,0,0) = -4.2254948E-03; Omega11(1,0,1) = -5.2965163E-02; Omega11(1,0,2) = 1.9157708E+00;  Omega11(1,0,3) = 6.3263309E-04;
     Omega11(1,1,0) = -7.6303990E-03; Omega11(1,1,1) = 1.6878089E-01;  Omega11(1,1,2) = -1.4004234E+00; Omega11(1,1,3) = 2.1427708E+03;
@@ -1131,13 +1131,13 @@ CSU2TCLib::CSU2TCLib(const CConfig* config, unsigned short val_nDim, bool viscou
     Omega11(5,5,0) = -4.2451096E-03; Omega11(5,5,1) = 9.6820337E-02;  Omega11(5,5,2) = -9.9770795E-01; Omega11(5,5,3) = 8.3320644E+02;
     Omega11(5,6,0) = -1.5315132E-02; Omega11(5,6,1) = 4.3541627E-01;  Omega11(5,6,2) = -4.2864279E+00; Omega11(5,6,3) = 3.5125207E+07;
     //NO+
-    Omega11(6,0,0) = 0.0000000E+00;  Omega11(6,0,1) = 0.0000000E+00;  Omega11(6,0,2) = 0.0000000E+00;  Omega11(6,0,3) = 0.0000000E+00;
+    Omega11(6,0,0) = 1.0000000E+00;  Omega11(6,0,1) = 1.0000000E+00;  Omega11(6,0,2) = 1.0000000E+00;  Omega11(6,0,3) = 1.0000000E+00;
     Omega11(6,1,0) = 0.0000000E+00;  Omega11(6,1,1) = 8.5112236E-02;  Omega11(6,1,2) = -1.7460044E+00; Omega11(6,1,3) = 1.4498969E+05;
     Omega11(6,2,0) = 0.0000000E+00;  Omega11(6,2,1) = 8.4737359E-02;  Omega11(6,2,2) = -1.7290488E+00; Omega11(6,2,3) = 1.2485194E+05;
     Omega11(6,3,0) = 1.1055777E-02;  Omega11(6,3,1) = -1.6621846E-01; Omega11(6,3,2) = 1.4372166E-01;  Omega11(6,3,3) = 1.3182061E+03;
     Omega11(6,4,0) = -2.1009546E-02; Omega11(6,4,1) = 5.8910426E-01;  Omega11(6,4,2) = -5.6681361E+00; Omega11(6,4,3) = 2.4486594E+09;
     Omega11(6,5,0) = -1.5315132E-02; Omega11(6,5,1) = 4.3541627E-01;  Omega11(6,5,2) = -4.2864279E+00; Omega11(6,5,3) = 3.5125207E+07;
-    Omega11(6,6,0) = 0.0000000E+00;  Omega11(6,6,1) = 0.0000000E+00;  Omega11(6,6,2) = 0.0000000E+00;  Omega11(6,6,3) = 0.0000000E+00;
+    Omega11(6,6,0) = -1.000000E+00;  Omega11(6,6,1) = -1.000000E+00;  Omega11(6,6,2) = -1.000000E+00;  Omega11(6,6,3) = -1.000000E+00;
 
     // Creation/Destruction (+1/-1), Index of monoatomic reactants
     // Monoatomic species (N,O) recombine into diaatomic (N2, O2)
@@ -1239,7 +1239,6 @@ vector<su2double>& CSU2TCLib::ComputeSpeciesCvVibEle(su2double val_T){
   }
 
   return Cvves;
-
 }
 
 vector<su2double>& CSU2TCLib::ComputeMixtureEnergies(){
@@ -1881,40 +1880,77 @@ su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies,
 
   su2double Omega_ij;
 
-  /*--- Check whether to use collision cross section data or Coulomb potential ---*/
-  if (Omega00(iSpecies, jSpecies, 0) == 1.0 && ionization) { // attractive potential
-    
-    const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
-    const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
-    const su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
+  if (d1) {
+    /*--- Check whether to use collision cross section data or Coulomb potential ---*/
+    if (Omega00(iSpecies, jSpecies, 0) == 1.0 && ionization) { // attractive potential
       
-    const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
-    const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
-    
-    /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
-    Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);
+      const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
+      const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
+      const su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
+        
+      const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
+      const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
+      
+      /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
+      Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);
 
-  } else if (Omega00(iSpecies, jSpecies, 0) == -1.0 && ionization) { // repulsive potential
+    } else if (Omega00(iSpecies, jSpecies, 0) == -1.0 && ionization) { // repulsive potential
 
-    const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
-    const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
-    const su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
-      
-    const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
-    const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
+      const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
+      const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
+      const su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
+        
+      const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
+      const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
+
+      /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
+      Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_r*T_star*(1 - C1_r * exp(-c1_r * T_star))+1);
 
-    /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
-    Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_r*T_star*(1 - C1_r * exp(-c1_r * T_star))+1);
+    } else {
 
+      // TODO: check which omega values to use: (0,0), (1,1), etc.
+      /*--- Calculate the Omega^(0,0)_ij collision cross section ---*/
+      Omega_ij = 1E-20 * Omega00(iSpecies,jSpecies,3)
+                        * pow(T, Omega00(iSpecies,jSpecies,0)*log(T)*log(T)
+                               + Omega00(iSpecies,jSpecies,1)*log(T)
+                               + Omega00(iSpecies,jSpecies,2));
+    }  
   } else {
+        /*--- Check whether to use collision cross section data or Coulomb potential ---*/
+    if (Omega11(iSpecies, jSpecies, 0) == 1.0 && ionization) { // attractive potential
+      
+      const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
+      const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
+      const su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
+        
+      const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
+      const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
+      
+      /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
+      Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D2_a*T_star*(1 - C2_a * exp(-c2_a * T_star))+1);
+
+    } else if (Omega11(iSpecies, jSpecies, 0) == -1.0 && ionization) { // repulsive potential
+
+      const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
+      const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
+      const su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
+        
+      const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
+      const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
+
+      /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
+      Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D2_r*T_star*(1 - C2_r * exp(-c2_r * T_star))+1);
+
+    } else {
 
-    // TODO: check which omega values to use: (0,0), (1,1), etc.
-    /*--- Calculate the Omega^(0,0)_ij collision cross section ---*/
-    Omega_ij = 1E-20 * Omega00(iSpecies,jSpecies,3)
-                      * pow(T, Omega00(iSpecies,jSpecies,0)*log(T)*log(T)
-                             + Omega00(iSpecies,jSpecies,1)*log(T)
-                             + Omega00(iSpecies,jSpecies,2));
-  }  
+      // TODO: check which omega values to use: (0,0), (1,1), etc.
+      /*--- Calculate the Omega^(0,0)_ij collision cross section ---*/
+      Omega_ij = 1E-20 * Omega11(iSpecies,jSpecies,3)
+                        * pow(T, Omega00(iSpecies,jSpecies,0)*log(T)*log(T)
+                               + Omega00(iSpecies,jSpecies,1)*log(T)
+                               + Omega00(iSpecies,jSpecies,2));
+    }  
+  }
   
   if (d1) {
     const su2double d_ij = 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij; // d1_ij
@@ -2094,7 +2130,6 @@ void CSU2TCLib::ThermalConductivitiesSuth(){
 
   ThermalConductivities[0] = k;
   ThermalConductivities[1] = kve;
-
 }
 
 vector<su2double>& CSU2TCLib::ComputeTemperatures(vector<su2double>& val_rhos, su2double rhoE, su2double rhoEve, su2double rhoEvel, su2double Tve_old) {
@@ -2193,7 +2228,6 @@ vector<su2double>& CSU2TCLib::ComputeTemperatures(vector<su2double>& val_rhos, s
   temperatures[1] = Tve;
 
   return temperatures;
-
 }
 
 void CSU2TCLib::GetChemistryEquilConstants(unsigned short iReaction){

From 0ebe329b2be8833792715239a2c03a4ae613f653 Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Mon, 16 Jan 2023 21:11:21 -0800
Subject: [PATCH 134/656] correct config, checks and runs viscwedge for 10
 iters

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 Common/src/CConfig.cpp          |  2 +-
 SU2_CFD/src/fluid/CSU2TCLib.cpp | 10 +---------
 2 files changed, 2 insertions(+), 10 deletions(-)

diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 0357290120f..8746d3da112 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -3923,7 +3923,7 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
       SU2_MPI::Error("Only STANDARD_AIR fluid model can be used with US Measurement System", CURRENT_FUNCTION);
     }
 
-    if (Kind_FluidModel == SU2_NONEQ && (Kind_TransCoeffModel != TRANSCOEFFMODEL::WILKE && Kind_TransCoeffModel != TRANSCOEFFMODEL::SUTHERLAND) ) {
+    if (Kind_FluidModel == SU2_NONEQ && (Kind_TransCoeffModel != TRANSCOEFFMODEL::WILKE && Kind_TransCoeffModel != TRANSCOEFFMODEL::SUTHERLAND && Kind_TransCoeffModel != TRANSCOEFFMODEL::GUPTAYOS) ) {
       SU2_MPI::Error("Only WILKE and SUTHERLAND transport models are stable for the NEMO solver using SU2TClib. Use Mutation++ instead.", CURRENT_FUNCTION);
     }
 
diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 3f0319d68db..14029c8c681 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1,7 +1,7 @@
 /*!
  * \file CSU2TCLib.cpp
  * \brief Source of user defined 2T nonequilibrium gas model.
- * \author C. Garbacz, W. Maier, S. R. Copeland
+ * \author C. Garbacz, W. Maier, S. R. Copeland, J. Needels
  * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
@@ -1023,7 +1023,6 @@ CSU2TCLib::CSU2TCLib(const CConfig* config, unsigned short val_nDim, bool viscou
     // Index 3: A1, A2, A3
 
     // Omega(0,0) ----------------------
-    //e-  (TODO: NO+ and e-,  NO+ and NO+, e- and e- ??????)
     Omega00(0,0,0) = -1.000000E+00;  Omega00(0,0,1) = -1.000000E+00;  Omega00(0,0,2) = -1.000000E+00;  Omega00(0,0,3) = -1.000000E+00;
     Omega00(0,1,0) = -1.0525124E-02; Omega00(0,1,1) = 1.3498950E-01;  Omega00(0,1,2) = 1.2524805E-01;  Omega00(0,1,3) = 1.5066506E-01;
     Omega00(0,2,0) = 2.3527001E-02;  Omega00(0,2,1) = -6.9632323E-01; Omega00(0,2,2) = 6.8035475E+00;  Omega00(0,2,3) = 1.8335509E-09;
@@ -1082,7 +1081,6 @@ CSU2TCLib::CSU2TCLib(const CConfig* config, unsigned short val_nDim, bool viscou
 
 
     // Omega(1,1) ----------------------
-    //e-    (TODO: NO+ and e-,  NO+ and NO+, e- and e- ??????)
     Omega11(0,0,0) = -1.000000E+00;  Omega11(0,0,1) = -1.000000E+00;  Omega11(0,0,2) = -1.000000E+00;  Omega11(0,0,3) = -1.000000E+00;
     Omega11(0,1,0) = -4.2254948E-03; Omega11(0,1,1) = -5.2965163E-02; Omega11(0,1,2) = 1.9157708E+00;  Omega11(0,1,3) = 6.3263309E-04;
     Omega11(0,2,0) = 9.6744867E-03;  Omega11(0,2,1) = -3.3759583E-01; Omega11(0,2,2) = 3.7952121E+00;  Omega11(0,2,3) = 6.8468036E-06;
@@ -1716,7 +1714,6 @@ vector<su2double>& CSU2TCLib::ComputeSpeciesEnthalpy(su2double val_T, su2double
   }
 
   return hs;
-
 }
 
 vector<su2double>& CSU2TCLib::GetDiffusionCoeff(){
@@ -1729,7 +1726,6 @@ vector<su2double>& CSU2TCLib::GetDiffusionCoeff(){
    DiffusionCoeffWBE();
 
   return DiffusionCoeff;
-
 }
 
 su2double CSU2TCLib::GetViscosity(){
@@ -1755,7 +1751,6 @@ vector<su2double>& CSU2TCLib::GetThermalConductivities(){
     ThermalConductivitiesSuth();
 
   return ThermalConductivities;
-
 }
 
 void CSU2TCLib::DiffusionCoeffWBE(){
@@ -1908,7 +1903,6 @@ su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies,
 
     } else {
 
-      // TODO: check which omega values to use: (0,0), (1,1), etc.
       /*--- Calculate the Omega^(0,0)_ij collision cross section ---*/
       Omega_ij = 1E-20 * Omega00(iSpecies,jSpecies,3)
                         * pow(T, Omega00(iSpecies,jSpecies,0)*log(T)*log(T)
@@ -1943,7 +1937,6 @@ su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies,
 
     } else {
 
-      // TODO: check which omega values to use: (0,0), (1,1), etc.
       /*--- Calculate the Omega^(0,0)_ij collision cross section ---*/
       Omega_ij = 1E-20 * Omega11(iSpecies,jSpecies,3)
                         * pow(T, Omega00(iSpecies,jSpecies,0)*log(T)*log(T)
@@ -2107,7 +2100,6 @@ void CSU2TCLib::ViscositySuth(){
 
   /*--- Calculate mixture laminar viscosity ---*/
   Mu = mu_ref[0] * T_nd * sqrt(T_nd) * ((T_ref_suth + Sm_ref[0]) / (T + Sm_ref[0]));
-
 }
 
 void CSU2TCLib::ThermalConductivitiesSuth(){

From da90d040255c8c958cad965f8369900a4d78fe3f Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Mon, 16 Jan 2023 23:19:33 -0800
Subject: [PATCH 135/656] fix ns air-7 config option, tested with air-7 and get
 assertion fail c2dcontainer, need to fix

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 Common/src/CConfig.cpp | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 8746d3da112..2e21198facc 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -6161,8 +6161,8 @@ void CConfig::SetOutput(SU2_COMPONENT val_software, unsigned short val_izone) {
       case MAIN_SOLVER::NEMO_NAVIER_STOKES:
         if (Kind_Regime == ENUM_REGIME::COMPRESSIBLE) cout << "Compressible two-temperature thermochemical non-equilibrium Navier-Stokes equations." << endl;
         if (Kind_FluidModel == SU2_NONEQ){
-          if ((GasModel != "N2") && (GasModel != "AIR-5") && (GasModel != "ARGON"))
-          SU2_MPI::Error("The GAS_MODEL given as input is not valid. Choose one of the options: N2, AIR-5, ARGON.", CURRENT_FUNCTION);
+          if ((GasModel != "N2") && (GasModel != "AIR-5") && (GasModel != "AIR-7") && (GasModel != "ARGON"))
+          SU2_MPI::Error("The GAS_MODEL given as input is not valid. Choose one of the options: N2, AIR-5, AIR-7, ARGON.", CURRENT_FUNCTION);
         }
         break;
       case MAIN_SOLVER::FEM_LES:

From dd364cda8b1f4cc58ceef9afabdd3ac332dc3f9b Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Tue, 17 Jan 2023 13:10:40 -0500
Subject: [PATCH 136/656] adding doxygen comments, updating some warning
 messages

---
 Common/src/CConfig.cpp              |  8 ++++----
 SU2_CFD/include/fluid/CSU2TCLib.hpp | 10 ++++++++++
 2 files changed, 14 insertions(+), 4 deletions(-)

diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 2e21198facc..d25acbc61ad 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -3924,12 +3924,12 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
     }
 
     if (Kind_FluidModel == SU2_NONEQ && (Kind_TransCoeffModel != TRANSCOEFFMODEL::WILKE && Kind_TransCoeffModel != TRANSCOEFFMODEL::SUTHERLAND && Kind_TransCoeffModel != TRANSCOEFFMODEL::GUPTAYOS) ) {
-      SU2_MPI::Error("Only WILKE and SUTHERLAND transport models are stable for the NEMO solver using SU2TClib. Use Mutation++ instead.", CURRENT_FUNCTION);
+      SU2_MPI::Error("Transport model not available for NEMO solver using SU2TCLIB. Please use the WILKE, SUTHERLAND or GUPTAYOS transport model instead.", CURRENT_FUNCTION);
     }
 
     if (Kind_FluidModel == MUTATIONPP &&
         (Kind_TransCoeffModel != TRANSCOEFFMODEL::WILKE && Kind_TransCoeffModel != TRANSCOEFFMODEL::CHAPMANN_ENSKOG)) {
-      SU2_MPI::Error("Only WILKE and Chapmann-Enskog transport model can be used with Mutation++ at the moment.",
+      SU2_MPI::Error("Transport model not available for NEMO solver using MUTATIONPP. Please use the WILKE or CHAPMANN_ENSKOG transport model instead..",
                      CURRENT_FUNCTION);
     }
 
@@ -6155,14 +6155,14 @@ void CConfig::SetOutput(SU2_COMPONENT val_software, unsigned short val_izone) {
         if (Kind_Regime == ENUM_REGIME::COMPRESSIBLE) cout << "Compressible two-temperature thermochemical non-equilibrium Euler equations." << endl;
         if (Kind_FluidModel == SU2_NONEQ){
           if ((GasModel != "N2") && (GasModel != "AIR-5") && (GasModel != "AIR-7") && (GasModel != "ARGON"))
-          SU2_MPI::Error("The GAS_MODEL given as input is not valid. Choose one of the options: N2, AIR-5, AIR-7, ARGON.", CURRENT_FUNCTION);
+            SU2_MPI::Error("The GAS_MODEL given is unavailble using CSU2TCLIB. Choose one of the options: N2, AIR-5, AIR-7, or ARGON.", CURRENT_FUNCTION);
         }
         break;
       case MAIN_SOLVER::NEMO_NAVIER_STOKES:
         if (Kind_Regime == ENUM_REGIME::COMPRESSIBLE) cout << "Compressible two-temperature thermochemical non-equilibrium Navier-Stokes equations." << endl;
         if (Kind_FluidModel == SU2_NONEQ){
           if ((GasModel != "N2") && (GasModel != "AIR-5") && (GasModel != "AIR-7") && (GasModel != "ARGON"))
-          SU2_MPI::Error("The GAS_MODEL given as input is not valid. Choose one of the options: N2, AIR-5, AIR-7, ARGON.", CURRENT_FUNCTION);
+          SU2_MPI::Error("The GAS_MODEL given is unavailble using CSU2TCLIB. Choose one of the options: N2, AIR-5, AIR-7, or ARGON.", CURRENT_FUNCTION);
         }
         break;
       case MAIN_SOLVER::FEM_LES:
diff --git a/SU2_CFD/include/fluid/CSU2TCLib.hpp b/SU2_CFD/include/fluid/CSU2TCLib.hpp
index 97caa81fcf7..6186b2d6ae9 100644
--- a/SU2_CFD/include/fluid/CSU2TCLib.hpp
+++ b/SU2_CFD/include/fluid/CSU2TCLib.hpp
@@ -265,6 +265,16 @@ class CSU2TCLib : public CNEMOGas {
    */
   void ThermalConductivitiesSuth();
 
+  /*!
+   *\brief Compute the collision terms (deltas)
+   *\param[in] iSpecies - Species of gas
+   *\param[in] jSpecies - Collision partner of species i
+   *\param[in] Mi - Molar mass of species i
+   *\param[in] Mj - Molar mass of species j
+   *\param[in] T - Temperature of gas
+   *\param[in] d1 - Whether delta_1 or delta_2 is computed
+   *\param[out] Delta_1 or Delta_2
+   */
   su2double ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies, su2double Mi, su2double Mj, su2double T, bool d1);
 
   /*!

From 91d6065b390f0b53df7a1d6297c7a069563f86ec Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Tue, 17 Jan 2023 13:32:55 -0500
Subject: [PATCH 137/656] update Omega(*,*) to better reflect literature

---
 SU2_CFD/include/fluid/CSU2TCLib.hpp |   4 +-
 SU2_CFD/src/fluid/CSU2TCLib.cpp     | 368 ++++++++++++++--------------
 2 files changed, 186 insertions(+), 186 deletions(-)

diff --git a/SU2_CFD/include/fluid/CSU2TCLib.hpp b/SU2_CFD/include/fluid/CSU2TCLib.hpp
index 6186b2d6ae9..65d91d08090 100644
--- a/SU2_CFD/include/fluid/CSU2TCLib.hpp
+++ b/SU2_CFD/include/fluid/CSU2TCLib.hpp
@@ -93,8 +93,8 @@ class CSU2TCLib : public CNEMOGas {
   Blottner,                      /*!< \brief Blottner viscosity coefficients */
   Dij;                           /*!< \brief Binary diffusion coefficients. */
 
-  C3DDoubleMatrix Omega00,       /*!< \brief Collision integrals (Omega(0,0)) */
-  Omega11;                       /*!< \brief Collision integrals (Omega(1,1)) */
+  C3DDoubleMatrix Omega11,       /*!< \brief Collision integrals (Omega^(1,1)) */
+  Omega22;                       /*!< \brief Collision integrals (Omega^(2,2)) */
 
   /*--- Implicit variables ---*/
   su2double                     /*!< \brief Derivatives w.r.t. conservative variables */
diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 14029c8c681..b9e72272621 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -44,8 +44,8 @@ CSU2TCLib::CSU2TCLib(const CConfig* config, unsigned short val_nDim, bool viscou
   RotationModes.resize(nSpecies,0.0);
   Diss.resize(nSpecies,0.0);
   A.resize(5,0.0);
-  Omega00.resize(nSpecies,nSpecies,4,0.0);
   Omega11.resize(nSpecies,nSpecies,4,0.0);
+  Omega22.resize(nSpecies,nSpecies,4,0.0);
   RxnConstantTable.resize(6,5) = su2double(0.0);
   CatRecombTable.resize(nSpecies,2) = 0;
   Blottner.resize(nSpecies,3)  = su2double(0.0);
@@ -263,14 +263,14 @@ CSU2TCLib::CSU2TCLib(const CConfig* config, unsigned short val_nDim, bool viscou
     // Index 1: collider
     // Index 2: partner
     // Index 3: A1, A2, A3
-    Omega00(0,0,0) = -6.0614558E-03;  Omega00(0,0,1) = 1.2689102E-01;   Omega00(0,0,2) = -1.0616948E+00;  Omega00(0,0,3) = 8.0955466E+02;
-    Omega00(0,1,0) = -1.0796249E-02;  Omega00(0,1,1) = 2.2656509E-01;   Omega00(0,1,2) = -1.7910602E+00;  Omega00(0,1,3) = 4.0455218E+03;
-    Omega00(1,0,0) = -1.0796249E-02;  Omega00(1,0,1) = 2.2656509E-01;   Omega00(1,0,2) = -1.7910602E+00;  Omega00(1,0,3) = 4.0455218E+03;
-    Omega00(1,1,0) = -9.6083779E-03;  Omega00(1,1,1) = 2.0938971E-01;   Omega00(1,1,2) = -1.7386904E+00;  Omega00(1,1,3) = 3.3587983E+03;
-    Omega11(0,0,0) = -7.6303990E-03;  Omega11(0,0,1) = 1.6878089E-01;   Omega11(0,0,2) = -1.4004234E+00;  Omega11(0,0,3) = 2.1427708E+03;
-    Omega11(0,1,0) = -8.3493693E-03;  Omega11(0,1,1) = 1.7808911E-01;   Omega11(0,1,2) = -1.4466155E+00;  Omega11(0,1,3) = 1.9324210E+03;
-    Omega11(1,0,0) = -8.3493693E-03;  Omega11(1,0,1) = 1.7808911E-01;   Omega11(1,0,2) = -1.4466155E+00;  Omega11(1,0,3) = 1.9324210E+03;
-    Omega11(1,1,0) = -7.7439615E-03;  Omega11(1,1,1) = 1.7129007E-01;   Omega11(1,1,2) = -1.4809088E+00;  Omega11(1,1,3) = 2.1284951E+03;
+    Omega11(0,0,0) = -6.0614558E-03;  Omega11(0,0,1) = 1.2689102E-01;   Omega11(0,0,2) = -1.0616948E+00;  Omega11(0,0,3) = 8.0955466E+02;
+    Omega11(0,1,0) = -1.0796249E-02;  Omega11(0,1,1) = 2.2656509E-01;   Omega11(0,1,2) = -1.7910602E+00;  Omega11(0,1,3) = 4.0455218E+03;
+    Omega11(1,0,0) = -1.0796249E-02;  Omega11(1,0,1) = 2.2656509E-01;   Omega11(1,0,2) = -1.7910602E+00;  Omega11(1,0,3) = 4.0455218E+03;
+    Omega11(1,1,0) = -9.6083779E-03;  Omega11(1,1,1) = 2.0938971E-01;   Omega11(1,1,2) = -1.7386904E+00;  Omega11(1,1,3) = 3.3587983E+03;
+    Omega22(0,0,0) = -7.6303990E-03;  Omega22(0,0,1) = 1.6878089E-01;   Omega22(0,0,2) = -1.4004234E+00;  Omega22(0,0,3) = 2.1427708E+03;
+    Omega22(0,1,0) = -8.3493693E-03;  Omega22(0,1,1) = 1.7808911E-01;   Omega22(0,1,2) = -1.4466155E+00;  Omega22(0,1,3) = 1.9324210E+03;
+    Omega22(1,0,0) = -8.3493693E-03;  Omega22(1,0,1) = 1.7808911E-01;   Omega22(1,0,2) = -1.4466155E+00;  Omega22(1,0,3) = 1.9324210E+03;
+    Omega22(1,1,0) = -7.7439615E-03;  Omega22(1,1,1) = 1.7129007E-01;   Omega22(1,1,2) = -1.4809088E+00;  Omega22(1,1,3) = 2.1284951E+03;
 
     /*--- Catayltic wall table---*/
     // Creation/Destruction (+1/-1), Index of monoatomic reactants.
@@ -572,69 +572,69 @@ CSU2TCLib::CSU2TCLib(const CConfig* config, unsigned short val_nDim, bool viscou
     // Index 1: collider
     // Index 2: partner
     // Index 3: A1, A2, A3
-    // Omega(0,0) ----------------------
+    // Omega^(1,1) ----------------------
     //N2
-    Omega00(0,0,0) = -6.0614558E-03;  Omega00(0,0,1) = 1.2689102E-01;   Omega00(0,0,2) = -1.0616948E+00;  Omega00(0,0,3) = 8.0955466E+02;
-    Omega00(0,1,0) = -3.7959091E-03;  Omega00(0,1,1) = 9.5708295E-02;   Omega00(0,1,2) = -1.0070611E+00;  Omega00(0,1,3) = 8.9392313E+02;
-    Omega00(0,2,0) = -1.9295666E-03;  Omega00(0,2,1) = 2.7995735E-02;   Omega00(0,2,2) = -3.1588514E-01;  Omega00(0,2,3) = 1.2880734E+02;
-    Omega00(0,3,0) = -1.0796249E-02;  Omega00(0,3,1) = 2.2656509E-01;   Omega00(0,3,2) = -1.7910602E+00;  Omega00(0,3,3) = 4.0455218E+03;
-    Omega00(0,4,0) = -2.7244269E-03;  Omega00(0,4,1) = 6.9587171E-02;   Omega00(0,4,2) = -7.9538667E-01;  Omega00(0,4,3) = 4.0673730E+02;
+    Omega11(0,0,0) = -6.0614558E-03;  Omega11(0,0,1) = 1.2689102E-01;   Omega11(0,0,2) = -1.0616948E+00;  Omega11(0,0,3) = 8.0955466E+02;
+    Omega11(0,1,0) = -3.7959091E-03;  Omega11(0,1,1) = 9.5708295E-02;   Omega11(0,1,2) = -1.0070611E+00;  Omega11(0,1,3) = 8.9392313E+02;
+    Omega11(0,2,0) = -1.9295666E-03;  Omega11(0,2,1) = 2.7995735E-02;   Omega11(0,2,2) = -3.1588514E-01;  Omega11(0,2,3) = 1.2880734E+02;
+    Omega11(0,3,0) = -1.0796249E-02;  Omega11(0,3,1) = 2.2656509E-01;   Omega11(0,3,2) = -1.7910602E+00;  Omega11(0,3,3) = 4.0455218E+03;
+    Omega11(0,4,0) = -2.7244269E-03;  Omega11(0,4,1) = 6.9587171E-02;   Omega11(0,4,2) = -7.9538667E-01;  Omega11(0,4,3) = 4.0673730E+02;
     //O2
-    Omega00(1,0,0) = -3.7959091E-03;  Omega00(1,0,1) = 9.5708295E-02;   Omega00(1,0,2) = -1.0070611E+00;  Omega00(1,0,3) = 8.9392313E+02;
-    Omega00(1,1,0) = -8.0682650E-04;  Omega00(1,1,1) = 1.6602480E-02;   Omega00(1,1,2) = -3.1472774E-01;  Omega00(1,1,3) = 1.4116458E+02;
-    Omega00(1,2,0) = -6.4433840E-04;  Omega00(1,2,1) = 8.5378580E-03;   Omega00(1,2,2) = -2.3225102E-01;  Omega00(1,2,3) = 1.1371608E+02;
-    Omega00(1,3,0) = -1.1453028E-03;  Omega00(1,3,1) = 1.2654140E-02;   Omega00(1,3,2) = -2.2435218E-01;  Omega00(1,3,3) = 7.7201588E+01;
-    Omega00(1,4,0) = -4.8405803E-03;  Omega00(1,4,1) = 1.0297688E-01;   Omega00(1,4,2) = -9.6876576E-01;  Omega00(1,4,3) = 6.1629812E+02;
+    Omega11(1,0,0) = -3.7959091E-03;  Omega11(1,0,1) = 9.5708295E-02;   Omega11(1,0,2) = -1.0070611E+00;  Omega11(1,0,3) = 8.9392313E+02;
+    Omega11(1,1,0) = -8.0682650E-04;  Omega11(1,1,1) = 1.6602480E-02;   Omega11(1,1,2) = -3.1472774E-01;  Omega11(1,1,3) = 1.4116458E+02;
+    Omega11(1,2,0) = -6.4433840E-04;  Omega11(1,2,1) = 8.5378580E-03;   Omega11(1,2,2) = -2.3225102E-01;  Omega11(1,2,3) = 1.1371608E+02;
+    Omega11(1,3,0) = -1.1453028E-03;  Omega11(1,3,1) = 1.2654140E-02;   Omega11(1,3,2) = -2.2435218E-01;  Omega11(1,3,3) = 7.7201588E+01;
+    Omega11(1,4,0) = -4.8405803E-03;  Omega11(1,4,1) = 1.0297688E-01;   Omega11(1,4,2) = -9.6876576E-01;  Omega11(1,4,3) = 6.1629812E+02;
     //NO
-    Omega00(2,0,0) = -1.9295666E-03;  Omega00(2,0,1) = 2.7995735E-02;   Omega00(2,0,2) = -3.1588514E-01;  Omega00(2,0,3) = 1.2880734E+02;
-    Omega00(2,1,0) = -6.4433840E-04;  Omega00(2,1,1) = 8.5378580E-03;   Omega00(2,1,2) = -2.3225102E-01;  Omega00(2,1,3) = 1.1371608E+02;
-    Omega00(2,2,0) = -0.0000000E+00;  Omega00(2,2,1) = -1.1056066E-02;  Omega00(2,2,2) = -5.9216250E-02;  Omega00(2,2,3) = 7.2542367E+01;
-    Omega00(2,3,0) = -1.5770918E-03;  Omega00(2,3,1) = 1.9578381E-02;   Omega00(2,3,2) = -2.7873624E-01;  Omega00(2,3,3) = 9.9547944E+01;
-    Omega00(2,4,0) = -1.0885815E-03;  Omega00(2,4,1) = 1.1883688E-02;   Omega00(2,4,2) = -2.1844909E-01;  Omega00(2,4,3) = 7.5512560E+01;
+    Omega11(2,0,0) = -1.9295666E-03;  Omega11(2,0,1) = 2.7995735E-02;   Omega11(2,0,2) = -3.1588514E-01;  Omega11(2,0,3) = 1.2880734E+02;
+    Omega11(2,1,0) = -6.4433840E-04;  Omega11(2,1,1) = 8.5378580E-03;   Omega11(2,1,2) = -2.3225102E-01;  Omega11(2,1,3) = 1.1371608E+02;
+    Omega11(2,2,0) = -0.0000000E+00;  Omega11(2,2,1) = -1.1056066E-02;  Omega11(2,2,2) = -5.9216250E-02;  Omega11(2,2,3) = 7.2542367E+01;
+    Omega11(2,3,0) = -1.5770918E-03;  Omega11(2,3,1) = 1.9578381E-02;   Omega11(2,3,2) = -2.7873624E-01;  Omega11(2,3,3) = 9.9547944E+01;
+    Omega11(2,4,0) = -1.0885815E-03;  Omega11(2,4,1) = 1.1883688E-02;   Omega11(2,4,2) = -2.1844909E-01;  Omega11(2,4,3) = 7.5512560E+01;
     //N
-    Omega00(3,0,0) = -1.0796249E-02;  Omega00(3,0,1) = 2.2656509E-01;   Omega00(3,0,2) = -1.7910602E+00;  Omega00(3,0,3) = 4.0455218E+03;
-    Omega00(3,1,0) = -1.1453028E-03;  Omega00(3,1,1) = 1.2654140E-02;   Omega00(3,1,2) = -2.2435218E-01;  Omega00(3,1,3) = 7.7201588E+01;
-    Omega00(3,2,0) = -1.5770918E-03;  Omega00(3,2,1) = 1.9578381E-02;   Omega00(3,2,2) = -2.7873624E-01;  Omega00(3,2,3) = 9.9547944E+01;
-    Omega00(3,3,0) = -9.6083779E-03;  Omega00(3,3,1) = 2.0938971E-01;   Omega00(3,3,2) = -1.7386904E+00;  Omega00(3,3,3) = 3.3587983E+03;
-    Omega00(3,4,0) = -7.8147689E-03;  Omega00(3,4,1) = 1.6792705E-01;   Omega00(3,4,2) = -1.4308628E+00;  Omega00(3,4,3) = 1.6628859E+03;
+    Omega11(3,0,0) = -1.0796249E-02;  Omega11(3,0,1) = 2.2656509E-01;   Omega11(3,0,2) = -1.7910602E+00;  Omega11(3,0,3) = 4.0455218E+03;
+    Omega11(3,1,0) = -1.1453028E-03;  Omega11(3,1,1) = 1.2654140E-02;   Omega11(3,1,2) = -2.2435218E-01;  Omega11(3,1,3) = 7.7201588E+01;
+    Omega11(3,2,0) = -1.5770918E-03;  Omega11(3,2,1) = 1.9578381E-02;   Omega11(3,2,2) = -2.7873624E-01;  Omega11(3,2,3) = 9.9547944E+01;
+    Omega11(3,3,0) = -9.6083779E-03;  Omega11(3,3,1) = 2.0938971E-01;   Omega11(3,3,2) = -1.7386904E+00;  Omega11(3,3,3) = 3.3587983E+03;
+    Omega11(3,4,0) = -7.8147689E-03;  Omega11(3,4,1) = 1.6792705E-01;   Omega11(3,4,2) = -1.4308628E+00;  Omega11(3,4,3) = 1.6628859E+03;
     //O
-    Omega00(4,0,0) = -2.7244269E-03;  Omega00(4,0,1) = 6.9587171E-02;   Omega00(4,0,2) = -7.9538667E-01;  Omega00(4,0,3) = 4.0673730E+02;
-    Omega00(4,1,0) = -4.8405803E-03;  Omega00(4,1,1) = 1.0297688E-01;   Omega00(4,1,2) = -9.6876576E-01;  Omega00(4,1,3) = 6.1629812E+02;
-    Omega00(4,2,0) = -1.0885815E-03;  Omega00(4,2,1) = 1.1883688E-02;   Omega00(4,2,2) = -2.1844909E-01;  Omega00(4,2,3) = 7.5512560E+01;
-    Omega00(4,3,0) = -7.8147689E-03;  Omega00(4,3,1) = 1.6792705E-01;   Omega00(4,3,2) = -1.4308628E+00;  Omega00(4,3,3) = 1.6628859E+03;
-    Omega00(4,4,0) = -6.4040535E-03;  Omega00(4,4,1) = 1.4629949E-01;   Omega00(4,4,2) = -1.3892121E+00;  Omega00(4,4,3) = 2.0903441E+03;
+    Omega11(4,0,0) = -2.7244269E-03;  Omega11(4,0,1) = 6.9587171E-02;   Omega11(4,0,2) = -7.9538667E-01;  Omega11(4,0,3) = 4.0673730E+02;
+    Omega11(4,1,0) = -4.8405803E-03;  Omega11(4,1,1) = 1.0297688E-01;   Omega11(4,1,2) = -9.6876576E-01;  Omega11(4,1,3) = 6.1629812E+02;
+    Omega11(4,2,0) = -1.0885815E-03;  Omega11(4,2,1) = 1.1883688E-02;   Omega11(4,2,2) = -2.1844909E-01;  Omega11(4,2,3) = 7.5512560E+01;
+    Omega11(4,3,0) = -7.8147689E-03;  Omega11(4,3,1) = 1.6792705E-01;   Omega11(4,3,2) = -1.4308628E+00;  Omega11(4,3,3) = 1.6628859E+03;
+    Omega11(4,4,0) = -6.4040535E-03;  Omega11(4,4,1) = 1.4629949E-01;   Omega11(4,4,2) = -1.3892121E+00;  Omega11(4,4,3) = 2.0903441E+03;
  
-    // Omega(1,1) ----------------------
+    // Omega^(2,2) ----------------------
     //N2
-    Omega11(0,0,0) = -7.6303990E-03;  Omega11(0,0,1) = 1.6878089E-01;   Omega11(0,0,2) = -1.4004234E+00;  Omega11(0,0,3) = 2.1427708E+03;
-    Omega11(0,1,0) = -8.0457321E-03;  Omega11(0,1,1) = 1.9228905E-01;   Omega11(0,1,2) = -1.7102854E+00;  Omega11(0,1,3) = 5.2213857E+03;
-    Omega11(0,2,0) = -6.8237776E-03;  Omega11(0,2,1) = 1.4360616E-01;   Omega11(0,2,2) = -1.1922240E+00;  Omega11(0,2,3) = 1.2433086E+03;
-    Omega11(0,3,0) = -8.3493693E-03;  Omega11(0,3,1) = 1.7808911E-01;   Omega11(0,3,2) = -1.4466155E+00;  Omega11(0,3,3) = 1.9324210E+03;
-    Omega11(0,4,0) = -8.3110691E-03;  Omega11(0,4,1) = 1.9617877E-01;   Omega11(0,4,2) = -1.7205427E+00;  Omega11(0,4,3) = 4.0812829E+03;
+    Omega22(0,0,0) = -7.6303990E-03;  Omega22(0,0,1) = 1.6878089E-01;   Omega22(0,0,2) = -1.4004234E+00;  Omega22(0,0,3) = 2.1427708E+03;
+    Omega22(0,1,0) = -8.0457321E-03;  Omega22(0,1,1) = 1.9228905E-01;   Omega22(0,1,2) = -1.7102854E+00;  Omega22(0,1,3) = 5.2213857E+03;
+    Omega22(0,2,0) = -6.8237776E-03;  Omega22(0,2,1) = 1.4360616E-01;   Omega22(0,2,2) = -1.1922240E+00;  Omega22(0,2,3) = 1.2433086E+03;
+    Omega22(0,3,0) = -8.3493693E-03;  Omega22(0,3,1) = 1.7808911E-01;   Omega22(0,3,2) = -1.4466155E+00;  Omega22(0,3,3) = 1.9324210E+03;
+    Omega22(0,4,0) = -8.3110691E-03;  Omega22(0,4,1) = 1.9617877E-01;   Omega22(0,4,2) = -1.7205427E+00;  Omega22(0,4,3) = 4.0812829E+03;
     //O2
-    Omega11(1,0,0) = -8.0457321E-03;  Omega11(1,0,1) = 1.9228905E-01;   Omega11(1,0,2) = -1.7102854E+00;  Omega11(1,0,3) = 5.2213857E+03;
-    Omega11(1,1,0) = -6.2931612E-03;  Omega11(1,1,1) = 1.4624645E-01;   Omega11(1,1,2) = -1.3006927E+00;  Omega11(1,1,3) = 1.8066892E+03;
-    Omega11(1,2,0) = -6.8508672E-03;  Omega11(1,2,1) = 1.5524564E-01;   Omega11(1,2,2) = -1.3479583E+00;  Omega11(1,2,3) = 2.0037890E+03;
-    Omega11(1,3,0) = -1.0608832E-03;  Omega11(1,3,1) = 1.1782595E-02;   Omega11(1,3,2) = -2.1246301E-01;  Omega11(1,3,3) = 8.4561598E+01;
-    Omega11(1,4,0) = -3.7969686E-03;  Omega11(1,4,1) = 7.6789981E-02;   Omega11(1,4,2) = -7.3056809E-01;  Omega11(1,4,3) = 3.3958171E+02;
+    Omega22(1,0,0) = -8.0457321E-03;  Omega22(1,0,1) = 1.9228905E-01;   Omega22(1,0,2) = -1.7102854E+00;  Omega22(1,0,3) = 5.2213857E+03;
+    Omega22(1,1,0) = -6.2931612E-03;  Omega22(1,1,1) = 1.4624645E-01;   Omega22(1,1,2) = -1.3006927E+00;  Omega22(1,1,3) = 1.8066892E+03;
+    Omega22(1,2,0) = -6.8508672E-03;  Omega22(1,2,1) = 1.5524564E-01;   Omega22(1,2,2) = -1.3479583E+00;  Omega22(1,2,3) = 2.0037890E+03;
+    Omega22(1,3,0) = -1.0608832E-03;  Omega22(1,3,1) = 1.1782595E-02;   Omega22(1,3,2) = -2.1246301E-01;  Omega22(1,3,3) = 8.4561598E+01;
+    Omega22(1,4,0) = -3.7969686E-03;  Omega22(1,4,1) = 7.6789981E-02;   Omega22(1,4,2) = -7.3056809E-01;  Omega22(1,4,3) = 3.3958171E+02;
     //NO
-    Omega11(2,0,0) = -6.8237776E-03;  Omega11(2,0,1) = 1.4360616E-01;   Omega11(2,0,2) = -1.1922240E+00;  Omega11(2,0,3) = 1.2433086E+03;
-    Omega11(2,1,0) = -6.8508672E-03;  Omega11(2,1,1) = 1.5524564E-01;   Omega11(2,1,2) = -1.3479583E+00;  Omega11(2,1,3) = 2.0037890E+03;
-    Omega11(2,2,0) = -7.4942466E-03;  Omega11(2,2,1) = 1.6626193E-01;   Omega11(2,2,2) = -1.4107027E+00;  Omega11(2,2,3) = 2.3097604E+03;
-    Omega11(2,3,0) = -1.4719259E-03;  Omega11(2,3,1) = 1.8446968E-02;   Omega11(2,3,2) = -2.6460411E-01;  Omega11(2,3,3) = 1.0911124E+02;
-    Omega11(2,4,0) = -1.0066279E-03;  Omega11(2,4,1) = 1.1029264E-02;   Omega11(2,4,2) = -2.0671266E-01;  Omega11(2,4,3) = 8.2644384E+01;
+    Omega22(2,0,0) = -6.8237776E-03;  Omega22(2,0,1) = 1.4360616E-01;   Omega22(2,0,2) = -1.1922240E+00;  Omega22(2,0,3) = 1.2433086E+03;
+    Omega22(2,1,0) = -6.8508672E-03;  Omega22(2,1,1) = 1.5524564E-01;   Omega22(2,1,2) = -1.3479583E+00;  Omega22(2,1,3) = 2.0037890E+03;
+    Omega22(2,2,0) = -7.4942466E-03;  Omega22(2,2,1) = 1.6626193E-01;   Omega22(2,2,2) = -1.4107027E+00;  Omega22(2,2,3) = 2.3097604E+03;
+    Omega22(2,3,0) = -1.4719259E-03;  Omega22(2,3,1) = 1.8446968E-02;   Omega22(2,3,2) = -2.6460411E-01;  Omega22(2,3,3) = 1.0911124E+02;
+    Omega22(2,4,0) = -1.0066279E-03;  Omega22(2,4,1) = 1.1029264E-02;   Omega22(2,4,2) = -2.0671266E-01;  Omega22(2,4,3) = 8.2644384E+01;
     //N
-    Omega11(3,0,0) = -8.3493693E-03;  Omega11(3,0,1) = 1.7808911E-01;   Omega11(3,0,2) = -1.4466155E+00;  Omega11(3,0,3) = 1.9324210E+03;
-    Omega11(3,1,0) = -1.0608832E-03;  Omega11(3,1,1) = 1.1782595E-02;   Omega11(3,1,2) = -2.1246301E-01;  Omega11(3,1,3) = 8.4561598E+01;
-    Omega11(3,2,0) = -1.4719259E-03;  Omega11(3,2,1) = 1.8446968E-02;   Omega11(3,2,2) = -2.6460411E-01;  Omega11(3,2,3) = 1.0911124E+02;
-    Omega11(3,3,0) = -7.7439615E-03;  Omega11(3,3,1) = 1.7129007E-01;   Omega11(3,3,2) = -1.4809088E+00;  Omega11(3,3,3) = 2.1284951E+03;
-    Omega11(3,4,0) = -5.0478143E-03;  Omega11(3,4,1) = 1.0236186E-01;   Omega11(3,4,2) = -9.0058935E-01;  Omega11(3,4,3) = 4.4472565E+02;
+    Omega22(3,0,0) = -8.3493693E-03;  Omega22(3,0,1) = 1.7808911E-01;   Omega22(3,0,2) = -1.4466155E+00;  Omega22(3,0,3) = 1.9324210E+03;
+    Omega22(3,1,0) = -1.0608832E-03;  Omega22(3,1,1) = 1.1782595E-02;   Omega22(3,1,2) = -2.1246301E-01;  Omega22(3,1,3) = 8.4561598E+01;
+    Omega22(3,2,0) = -1.4719259E-03;  Omega22(3,2,1) = 1.8446968E-02;   Omega22(3,2,2) = -2.6460411E-01;  Omega22(3,2,3) = 1.0911124E+02;
+    Omega22(3,3,0) = -7.7439615E-03;  Omega22(3,3,1) = 1.7129007E-01;   Omega22(3,3,2) = -1.4809088E+00;  Omega22(3,3,3) = 2.1284951E+03;
+    Omega22(3,4,0) = -5.0478143E-03;  Omega22(3,4,1) = 1.0236186E-01;   Omega22(3,4,2) = -9.0058935E-01;  Omega22(3,4,3) = 4.4472565E+02;
     //O
-    Omega11(4,0,0) = -8.3110691E-03;  Omega11(4,0,1) = 1.9617877E-01;   Omega11(4,0,2) = -1.7205427E+00;  Omega11(4,0,3) = 4.0812829E+03;
-    Omega11(4,1,0) = -3.7969686E-03;  Omega11(4,1,1) = 7.6789981E-02;   Omega11(4,1,2) = -7.3056809E-01;  Omega11(4,1,3) = 3.3958171E+02;
-    Omega11(4,2,0) = -1.0066279E-03;  Omega11(4,2,1) = 1.1029264E-02;   Omega11(4,2,2) = -2.0671266E-01;  Omega11(4,2,3) = 8.2644384E+01;
-    Omega11(4,3,0) = -5.0478143E-03;  Omega11(4,3,1) = 1.0236186E-01;   Omega11(4,3,2) = -9.0058935E-01;  Omega11(4,3,3) = 4.4472565E+02;
-    Omega11(4,4,0) = -4.2451096E-03;  Omega11(4,4,1) = 9.6820337E-02;   Omega11(4,4,2) = -9.9770795E-01;  Omega11(4,4,3) = 8.3320644E+02;
+    Omega22(4,0,0) = -8.3110691E-03;  Omega22(4,0,1) = 1.9617877E-01;   Omega22(4,0,2) = -1.7205427E+00;  Omega22(4,0,3) = 4.0812829E+03;
+    Omega22(4,1,0) = -3.7969686E-03;  Omega22(4,1,1) = 7.6789981E-02;   Omega22(4,1,2) = -7.3056809E-01;  Omega22(4,1,3) = 3.3958171E+02;
+    Omega22(4,2,0) = -1.0066279E-03;  Omega22(4,2,1) = 1.1029264E-02;   Omega22(4,2,2) = -2.0671266E-01;  Omega22(4,2,3) = 8.2644384E+01;
+    Omega22(4,3,0) = -5.0478143E-03;  Omega22(4,3,1) = 1.0236186E-01;   Omega22(4,3,2) = -9.0058935E-01;  Omega22(4,3,3) = 4.4472565E+02;
+    Omega22(4,4,0) = -4.2451096E-03;  Omega22(4,4,1) = 9.6820337E-02;   Omega22(4,4,2) = -9.9770795E-01;  Omega22(4,4,3) = 8.3320644E+02;
 
     // Creation/Destruction (+1/-1), Index of monoatomic reactants
     // Monoatomic species (N,O) recombine into diaatomic (N2, O2)
@@ -1022,120 +1022,120 @@ CSU2TCLib::CSU2TCLib(const CConfig* config, unsigned short val_nDim, bool viscou
     // Index 2: partner
     // Index 3: A1, A2, A3
 
-    // Omega(0,0) ----------------------
-    Omega00(0,0,0) = -1.000000E+00;  Omega00(0,0,1) = -1.000000E+00;  Omega00(0,0,2) = -1.000000E+00;  Omega00(0,0,3) = -1.000000E+00;
-    Omega00(0,1,0) = -1.0525124E-02; Omega00(0,1,1) = 1.3498950E-01;  Omega00(0,1,2) = 1.2524805E-01;  Omega00(0,1,3) = 1.5066506E-01;
-    Omega00(0,2,0) = 2.3527001E-02;  Omega00(0,2,1) = -6.9632323E-01; Omega00(0,2,2) = 6.8035475E+00;  Omega00(0,2,3) = 1.8335509E-09;
-    Omega00(0,3,0) = 1.0414818E-01;  Omega00(0,3,1) = -2.8369126E+00; Omega00(0,3,2) = 2.5323135E+01;  Omega00(0,3,3) = 7.7138358E-32;
-    Omega00(0,4,0) = 0.0000000E+00;  Omega00(0,4,1) = 1.6554247E-01;  Omega00(0,4,2) = -3.4986344E+00; Omega00(0,4,3) = 5.9268038E+08;
-    Omega00(0,5,0) = 9.9865506E-03;  Omega00(0,5,1) = -2.7407431E-01; Omega00(0,5,2) = 2.6561032E+00;  Omega00(0,5,3) = 4.3080676E-04;
-    Omega00(0,6,0) = 1.0000000E+00;  Omega00(0,6,1) = 1.0000000E+00;  Omega00(0,6,2) = 1.0000000E+00;  Omega00(0,6,3) = 1.0000000E+00;
+    // Omega^(1,1) ----------------------
+    Omega11(0,0,0) = -1.000000E+00;  Omega11(0,0,1) = -1.000000E+00;  Omega11(0,0,2) = -1.000000E+00;  Omega11(0,0,3) = -1.000000E+00;
+    Omega11(0,1,0) = -1.0525124E-02; Omega11(0,1,1) = 1.3498950E-01;  Omega11(0,1,2) = 1.2524805E-01;  Omega11(0,1,3) = 1.5066506E-01;
+    Omega11(0,2,0) = 2.3527001E-02;  Omega11(0,2,1) = -6.9632323E-01; Omega11(0,2,2) = 6.8035475E+00;  Omega11(0,2,3) = 1.8335509E-09;
+    Omega11(0,3,0) = 1.0414818E-01;  Omega11(0,3,1) = -2.8369126E+00; Omega11(0,3,2) = 2.5323135E+01;  Omega11(0,3,3) = 7.7138358E-32;
+    Omega11(0,4,0) = 0.0000000E+00;  Omega11(0,4,1) = 1.6554247E-01;  Omega11(0,4,2) = -3.4986344E+00; Omega11(0,4,3) = 5.9268038E+08;
+    Omega11(0,5,0) = 9.9865506E-03;  Omega11(0,5,1) = -2.7407431E-01; Omega11(0,5,2) = 2.6561032E+00;  Omega11(0,5,3) = 4.3080676E-04;
+    Omega11(0,6,0) = 1.0000000E+00;  Omega11(0,6,1) = 1.0000000E+00;  Omega11(0,6,2) = 1.0000000E+00;  Omega11(0,6,3) = 1.0000000E+00;
     //N2
-    Omega00(1,0,0) = -1.0525124E-02; Omega00(1,0,1) = 1.3498950E-01;  Omega00(1,0,2) = 1.2524805E-01;  Omega00(1,0,3) = 1.5066506E-01;
-    Omega00(1,1,0) = -6.0614558E-03; Omega00(1,1,1) = 1.2689102E-01;  Omega00(1,1,2) = -1.0616948E+00; Omega00(1,1,3) = 8.0955466E+02;
-    Omega00(1,2,0) = -3.7959091E-03; Omega00(1,2,1) = 9.5708295E-02;  Omega00(1,2,2) = -1.0070611E+00; Omega00(1,2,3) = 8.9392313E+02;
-    Omega00(1,3,0) = -1.9295666E-03; Omega00(1,3,1) = 2.7995735E-02;  Omega00(1,3,2) = -3.1588514E-01; Omega00(1,3,3) = 1.2880734E+02;
-    Omega00(1,4,0) = -1.0796249E-02; Omega00(1,4,1) = 2.2656509E-01;  Omega00(1,4,2) = -1.7910602E+00; Omega00(1,4,3) = 4.0455218E+03;
-    Omega00(1,5,0) = -2.7244269E-03; Omega00(1,5,1) = 6.9587171E-02;  Omega00(1,5,2) = -7.9538667E-01; Omega00(1,5,3) = 4.0673730E+02;
-    Omega00(1,6,0) = 0.0000000E+00;  Omega00(1,6,1) = 9.1205839E-02;  Omega00(1,6,2) = -1.8728231E+00; Omega00(1,6,3) = 2.4432020E+05;
+    Omega11(1,0,0) = -1.0525124E-02; Omega11(1,0,1) = 1.3498950E-01;  Omega11(1,0,2) = 1.2524805E-01;  Omega11(1,0,3) = 1.5066506E-01;
+    Omega11(1,1,0) = -6.0614558E-03; Omega11(1,1,1) = 1.2689102E-01;  Omega11(1,1,2) = -1.0616948E+00; Omega11(1,1,3) = 8.0955466E+02;
+    Omega11(1,2,0) = -3.7959091E-03; Omega11(1,2,1) = 9.5708295E-02;  Omega11(1,2,2) = -1.0070611E+00; Omega11(1,2,3) = 8.9392313E+02;
+    Omega11(1,3,0) = -1.9295666E-03; Omega11(1,3,1) = 2.7995735E-02;  Omega11(1,3,2) = -3.1588514E-01; Omega11(1,3,3) = 1.2880734E+02;
+    Omega11(1,4,0) = -1.0796249E-02; Omega11(1,4,1) = 2.2656509E-01;  Omega11(1,4,2) = -1.7910602E+00; Omega11(1,4,3) = 4.0455218E+03;
+    Omega11(1,5,0) = -2.7244269E-03; Omega11(1,5,1) = 6.9587171E-02;  Omega11(1,5,2) = -7.9538667E-01; Omega11(1,5,3) = 4.0673730E+02;
+    Omega11(1,6,0) = 0.0000000E+00;  Omega11(1,6,1) = 9.1205839E-02;  Omega11(1,6,2) = -1.8728231E+00; Omega11(1,6,3) = 2.4432020E+05;
     //O2
-    Omega00(2,0,0) = 2.3527001E-02;  Omega00(2,0,1) = -6.9632323E-01; Omega00(2,0,2) = 6.8035475E+00;  Omega00(2,0,3) = 1.8335509E-09;
-    Omega00(2,1,0) = -3.7959091E-03; Omega00(2,1,1) = 9.5708295E-02;  Omega00(2,1,2) = -1.0070611E+00; Omega00(2,1,3) = 8.9392313E+02;
-    Omega00(2,2,0) = -8.0682650E-04; Omega00(2,2,1) = 1.6602480E-02;  Omega00(2,2,2) = -3.1472774E-01; Omega00(2,2,3) = 1.4116458E+02;
-    Omega00(2,3,0) = -6.4433840E-04; Omega00(2,3,1) = 8.5378580E-03;  Omega00(2,3,2) = -2.3225102E-01; Omega00(2,3,3) = 1.1371608E+02;
-    Omega00(2,4,0) = -1.1453028E-03; Omega00(2,4,1) = 1.2654140E-02;  Omega00(2,4,2) = -2.2435218E-01; Omega00(2,4,3) = 7.7201588E+01;
-    Omega00(2,5,0) = -4.8405803E-03; Omega00(2,5,1) = 1.0297688E-01;  Omega00(2,5,2) = -9.6876576E-01; Omega00(2,5,3) = 6.1629812E+02;
-    Omega00(2,6,0) = -3.7822765E-03; Omega00(2,6,1) = 1.7967016E-01;  Omega00(2,6,2) = -2.5409098E+00; Omega00(2,6,3) = 1.1840435E+06;
+    Omega11(2,0,0) = 2.3527001E-02;  Omega11(2,0,1) = -6.9632323E-01; Omega11(2,0,2) = 6.8035475E+00;  Omega11(2,0,3) = 1.8335509E-09;
+    Omega11(2,1,0) = -3.7959091E-03; Omega11(2,1,1) = 9.5708295E-02;  Omega11(2,1,2) = -1.0070611E+00; Omega11(2,1,3) = 8.9392313E+02;
+    Omega11(2,2,0) = -8.0682650E-04; Omega11(2,2,1) = 1.6602480E-02;  Omega11(2,2,2) = -3.1472774E-01; Omega11(2,2,3) = 1.4116458E+02;
+    Omega11(2,3,0) = -6.4433840E-04; Omega11(2,3,1) = 8.5378580E-03;  Omega11(2,3,2) = -2.3225102E-01; Omega11(2,3,3) = 1.1371608E+02;
+    Omega11(2,4,0) = -1.1453028E-03; Omega11(2,4,1) = 1.2654140E-02;  Omega11(2,4,2) = -2.2435218E-01; Omega11(2,4,3) = 7.7201588E+01;
+    Omega11(2,5,0) = -4.8405803E-03; Omega11(2,5,1) = 1.0297688E-01;  Omega11(2,5,2) = -9.6876576E-01; Omega11(2,5,3) = 6.1629812E+02;
+    Omega11(2,6,0) = -3.7822765E-03; Omega11(2,6,1) = 1.7967016E-01;  Omega11(2,6,2) = -2.5409098E+00; Omega11(2,6,3) = 1.1840435E+06;
     //NO
-    Omega00(3,0,0) = 1.0414818E-01;  Omega00(3,0,1) = -2.8369126E+00; Omega00(3,0,2) = 2.5323135E+01;  Omega00(3,0,3) = 7.7138358E-32;
-    Omega00(3,1,0) = -1.9295666E-03; Omega00(3,1,1) = 2.7995735E-02;  Omega00(3,1,2) = -3.1588514E-01; Omega00(3,1,3) = 1.2880734E+02;
-    Omega00(3,2,0) = -6.4433840E-04; Omega00(3,2,1) = 8.5378580E-03;  Omega00(3,2,2) = -2.3225102E-01; Omega00(3,2,3) = 1.1371608E+02;
-    Omega00(3,3,0) = -0.0000000E+00; Omega00(3,3,1) = -1.1056066E-02; Omega00(3,3,2) = -5.9216250E-02; Omega00(3,3,3) = 7.2542367E+01;
-    Omega00(3,4,0) = -1.5770918E-03; Omega00(3,4,1) = 1.9578381E-02;  Omega00(3,4,2) = -2.7873624E-01; Omega00(3,4,3) = 9.9547944E+01;
-    Omega00(3,5,0) = -1.0885815E-03; Omega00(3,5,1) = 1.1883688E-02;  Omega00(3,5,2) = -2.1844909E-01; Omega00(3,5,3) = 7.5512560E+01;
-    Omega00(3,6,0) = -8.1158474E-03; Omega00(3,6,1) = 2.1474280E-01;  Omega00(3,6,2) = -2.0148450E+00; Omega00(3,6,3) = 6.2986385E+04;
+    Omega11(3,0,0) = 1.0414818E-01;  Omega11(3,0,1) = -2.8369126E+00; Omega11(3,0,2) = 2.5323135E+01;  Omega11(3,0,3) = 7.7138358E-32;
+    Omega11(3,1,0) = -1.9295666E-03; Omega11(3,1,1) = 2.7995735E-02;  Omega11(3,1,2) = -3.1588514E-01; Omega11(3,1,3) = 1.2880734E+02;
+    Omega11(3,2,0) = -6.4433840E-04; Omega11(3,2,1) = 8.5378580E-03;  Omega11(3,2,2) = -2.3225102E-01; Omega11(3,2,3) = 1.1371608E+02;
+    Omega11(3,3,0) = -0.0000000E+00; Omega11(3,3,1) = -1.1056066E-02; Omega11(3,3,2) = -5.9216250E-02; Omega11(3,3,3) = 7.2542367E+01;
+    Omega11(3,4,0) = -1.5770918E-03; Omega11(3,4,1) = 1.9578381E-02;  Omega11(3,4,2) = -2.7873624E-01; Omega11(3,4,3) = 9.9547944E+01;
+    Omega11(3,5,0) = -1.0885815E-03; Omega11(3,5,1) = 1.1883688E-02;  Omega11(3,5,2) = -2.1844909E-01; Omega11(3,5,3) = 7.5512560E+01;
+    Omega11(3,6,0) = -8.1158474E-03; Omega11(3,6,1) = 2.1474280E-01;  Omega11(3,6,2) = -2.0148450E+00; Omega11(3,6,3) = 6.2986385E+04;
     //N
-    Omega00(4,0,0) = 0.0000000E+00;  Omega00(4,0,1) = 1.6554247E-01;  Omega00(4,0,2) = -3.4986344E+00; Omega00(4,0,3) = 5.9268038E+08;
-    Omega00(4,1,0) = -1.0796249E-02; Omega00(4,1,1) = 2.2656509E-01;  Omega00(4,1,2) = -1.7910602E+00; Omega00(4,1,3) = 4.0455218E+03;
-    Omega00(4,2,0) = -1.1453028E-03; Omega00(4,2,1) = 1.2654140E-02;  Omega00(4,2,2) = -2.2435218E-01; Omega00(4,2,3) = 7.7201588E+01;
-    Omega00(4,3,0) = -1.5770918E-03; Omega00(4,3,1) = 1.9578381E-02;  Omega00(4,3,2) = -2.7873624E-01; Omega00(4,3,3) = 9.9547944E+01;
-    Omega00(4,4,0) = -9.6083779E-03; Omega00(4,4,1) = 2.0938971E-01;  Omega00(4,4,2) = -1.7386904E+00; Omega00(4,4,3) = 3.3587983E+03;
-    Omega00(4,5,0) = -7.8147689E-03; Omega00(4,5,1) = 1.6792705E-01;  Omega00(4,5,2) = -1.4308628E+00; Omega00(4,5,3) = 1.6628859E+03;
-    Omega00(4,6,0) = -1.9605234E-02; Omega00(4,6,1) = 5.5570872E-01;  Omega00(4,6,2) = -5.4285702E+00; Omega00(4,6,3) = 1.3574446E+09;
+    Omega11(4,0,0) = 0.0000000E+00;  Omega11(4,0,1) = 1.6554247E-01;  Omega11(4,0,2) = -3.4986344E+00; Omega11(4,0,3) = 5.9268038E+08;
+    Omega11(4,1,0) = -1.0796249E-02; Omega11(4,1,1) = 2.2656509E-01;  Omega11(4,1,2) = -1.7910602E+00; Omega11(4,1,3) = 4.0455218E+03;
+    Omega11(4,2,0) = -1.1453028E-03; Omega11(4,2,1) = 1.2654140E-02;  Omega11(4,2,2) = -2.2435218E-01; Omega11(4,2,3) = 7.7201588E+01;
+    Omega11(4,3,0) = -1.5770918E-03; Omega11(4,3,1) = 1.9578381E-02;  Omega11(4,3,2) = -2.7873624E-01; Omega11(4,3,3) = 9.9547944E+01;
+    Omega11(4,4,0) = -9.6083779E-03; Omega11(4,4,1) = 2.0938971E-01;  Omega11(4,4,2) = -1.7386904E+00; Omega11(4,4,3) = 3.3587983E+03;
+    Omega11(4,5,0) = -7.8147689E-03; Omega11(4,5,1) = 1.6792705E-01;  Omega11(4,5,2) = -1.4308628E+00; Omega11(4,5,3) = 1.6628859E+03;
+    Omega11(4,6,0) = -1.9605234E-02; Omega11(4,6,1) = 5.5570872E-01;  Omega11(4,6,2) = -5.4285702E+00; Omega11(4,6,3) = 1.3574446E+09;
     //O
-    Omega00(5,0,0) = 9.9865506E-03;  Omega00(5,0,1) = -2.7407431E-01; Omega00(5,0,2) = 2.6561032E+00;  Omega00(5,0,3) = 4.3080676E-04;
-    Omega00(5,1,0) = -2.7244269E-03; Omega00(5,1,1) = 6.9587171E-02;  Omega00(5,1,2) = -7.9538667E-01; Omega00(5,1,3) = 4.0673730E+02;
-    Omega00(5,2,0) = -4.8405803E-03; Omega00(5,2,1) = 1.0297688E-01;  Omega00(5,2,2) = -9.6876576E-01; Omega00(5,2,3) = 6.1629812E+02;
-    Omega00(5,3,0) = -1.0885815E-03; Omega00(5,3,1) = 1.1883688E-02;  Omega00(5,3,2) = -2.1844909E-01; Omega00(5,3,3) = 7.5512560E+01;
-    Omega00(5,4,0) = -7.8147689E-03; Omega00(5,4,1) = 1.6792705E-01;  Omega00(5,4,2) = -1.4308628E+00; Omega00(5,4,3) = 1.6628859E+03;
-    Omega00(5,5,0) = -6.4040535E-03; Omega00(5,5,1) = 1.4629949E-01;  Omega00(5,5,2) = -1.3892121E+00; Omega00(5,5,3) = 2.0903441E+03;
-    Omega00(5,6,0) = -1.6409054E-02; Omega00(5,6,1) = 4.6352852E-01;  Omega00(5,6,2) = -4.5479735E+00; Omega00(5,6,3) = 7.4250671E+07;
+    Omega11(5,0,0) = 9.9865506E-03;  Omega11(5,0,1) = -2.7407431E-01; Omega11(5,0,2) = 2.6561032E+00;  Omega11(5,0,3) = 4.3080676E-04;
+    Omega11(5,1,0) = -2.7244269E-03; Omega11(5,1,1) = 6.9587171E-02;  Omega11(5,1,2) = -7.9538667E-01; Omega11(5,1,3) = 4.0673730E+02;
+    Omega11(5,2,0) = -4.8405803E-03; Omega11(5,2,1) = 1.0297688E-01;  Omega11(5,2,2) = -9.6876576E-01; Omega11(5,2,3) = 6.1629812E+02;
+    Omega11(5,3,0) = -1.0885815E-03; Omega11(5,3,1) = 1.1883688E-02;  Omega11(5,3,2) = -2.1844909E-01; Omega11(5,3,3) = 7.5512560E+01;
+    Omega11(5,4,0) = -7.8147689E-03; Omega11(5,4,1) = 1.6792705E-01;  Omega11(5,4,2) = -1.4308628E+00; Omega11(5,4,3) = 1.6628859E+03;
+    Omega11(5,5,0) = -6.4040535E-03; Omega11(5,5,1) = 1.4629949E-01;  Omega11(5,5,2) = -1.3892121E+00; Omega11(5,5,3) = 2.0903441E+03;
+    Omega11(5,6,0) = -1.6409054E-02; Omega11(5,6,1) = 4.6352852E-01;  Omega11(5,6,2) = -4.5479735E+00; Omega11(5,6,3) = 7.4250671E+07;
     //NO+
-    Omega00(6,0,0) = 1.0000000E+00;  Omega00(6,0,1) = 1.0000000E+00;  Omega00(6,0,2) = 1.0000000E+00;  Omega00(6,0,3) = 1.0000000E+00;
-    Omega00(6,1,0) = 0.0000000E+00;  Omega00(6,1,1) = 9.1205839E-02;  Omega00(6,1,2) = -1.8728231E+00; Omega00(6,1,3) = 2.4432020E+05;
-    Omega00(6,2,0) = -3.7822765E-03; Omega00(6,2,1) = 1.7967016E-01;  Omega00(6,2,2) = -2.5409098E+00; Omega00(6,2,3) = 1.1840435E+06;
-    Omega00(6,3,0) = -8.1158474E-03; Omega00(6,3,1) = 2.1474280E-01;  Omega00(6,3,2) = -2.0148450E+00; Omega00(6,3,3) = 6.2986385E+04;
-    Omega00(6,4,0) = -1.9605234E-02; Omega00(6,4,1) = 5.5570872E-01;  Omega00(6,4,2) = -5.4285702E+00; Omega00(6,4,3) = 1.3574446E+09;
-    Omega00(6,5,0) = -1.6409054E-02; Omega00(6,5,1) = 4.6352852E-01;  Omega00(6,5,2) = -4.5479735E+00; Omega00(6,5,3) = 7.4250671E+07;
-    Omega00(6,6,0) = -1.000000E+00;  Omega00(6,6,1) = -1.000000E+00;  Omega00(6,6,2) = -1.000000E+00;  Omega00(6,6,3) = -1.000000E+00;
+    Omega11(6,0,0) = 1.0000000E+00;  Omega11(6,0,1) = 1.0000000E+00;  Omega11(6,0,2) = 1.0000000E+00;  Omega11(6,0,3) = 1.0000000E+00;
+    Omega11(6,1,0) = 0.0000000E+00;  Omega11(6,1,1) = 9.1205839E-02;  Omega11(6,1,2) = -1.8728231E+00; Omega11(6,1,3) = 2.4432020E+05;
+    Omega11(6,2,0) = -3.7822765E-03; Omega11(6,2,1) = 1.7967016E-01;  Omega11(6,2,2) = -2.5409098E+00; Omega11(6,2,3) = 1.1840435E+06;
+    Omega11(6,3,0) = -8.1158474E-03; Omega11(6,3,1) = 2.1474280E-01;  Omega11(6,3,2) = -2.0148450E+00; Omega11(6,3,3) = 6.2986385E+04;
+    Omega11(6,4,0) = -1.9605234E-02; Omega11(6,4,1) = 5.5570872E-01;  Omega11(6,4,2) = -5.4285702E+00; Omega11(6,4,3) = 1.3574446E+09;
+    Omega11(6,5,0) = -1.6409054E-02; Omega11(6,5,1) = 4.6352852E-01;  Omega11(6,5,2) = -4.5479735E+00; Omega11(6,5,3) = 7.4250671E+07;
+    Omega11(6,6,0) = -1.000000E+00;  Omega11(6,6,1) = -1.000000E+00;  Omega11(6,6,2) = -1.000000E+00;  Omega11(6,6,3) = -1.000000E+00;
 
 
-    // Omega(1,1) ----------------------
-    Omega11(0,0,0) = -1.000000E+00;  Omega11(0,0,1) = -1.000000E+00;  Omega11(0,0,2) = -1.000000E+00;  Omega11(0,0,3) = -1.000000E+00;
-    Omega11(0,1,0) = -4.2254948E-03; Omega11(0,1,1) = -5.2965163E-02; Omega11(0,1,2) = 1.9157708E+00;  Omega11(0,1,3) = 6.3263309E-04;
-    Omega11(0,2,0) = 9.6744867E-03;  Omega11(0,2,1) = -3.3759583E-01; Omega11(0,2,2) = 3.7952121E+00;  Omega11(0,2,3) = 6.8468036E-06;
-    Omega11(0,3,0) = 0.0000000E+00;  Omega11(0,3,1) = 5.4444485E-02;  Omega11(0,3,2) = -1.2854128E+00; Omega11(0,3,3) = 1.3857556E+04;
-    Omega11(0,4,0) = -1.0903638E-01; Omega11(0,4,1) = 2.8678381E+00;  Omega11(0,4,2) = -2.5297550E+01; Omega11(0,4,3) = 3.4838798E+33;
-    Omega11(0,5,0) = -1.7924100E-02; Omega11(0,5,1) = 4.0402656E-01;  Omega11(0,5,2) = -2.6712374E+00; Omega11(0,5,3) = 4.1447669E+02;
-    Omega11(0,6,0) = 1.0000000E+00;  Omega11(0,6,1) = 1.0000000E+00;  Omega11(0,6,2) = 1.0000000E+00;  Omega11(0,6,3) = 1.0000000E+00;
+    // Omega^(2,2) ----------------------
+    Omega22(0,0,0) = -1.000000E+00;  Omega22(0,0,1) = -1.000000E+00;  Omega22(0,0,2) = -1.000000E+00;  Omega22(0,0,3) = -1.000000E+00;
+    Omega22(0,1,0) = -4.2254948E-03; Omega22(0,1,1) = -5.2965163E-02; Omega22(0,1,2) = 1.9157708E+00;  Omega22(0,1,3) = 6.3263309E-04;
+    Omega22(0,2,0) = 9.6744867E-03;  Omega22(0,2,1) = -3.3759583E-01; Omega22(0,2,2) = 3.7952121E+00;  Omega22(0,2,3) = 6.8468036E-06;
+    Omega22(0,3,0) = 0.0000000E+00;  Omega22(0,3,1) = 5.4444485E-02;  Omega22(0,3,2) = -1.2854128E+00; Omega22(0,3,3) = 1.3857556E+04;
+    Omega22(0,4,0) = -1.0903638E-01; Omega22(0,4,1) = 2.8678381E+00;  Omega22(0,4,2) = -2.5297550E+01; Omega22(0,4,3) = 3.4838798E+33;
+    Omega22(0,5,0) = -1.7924100E-02; Omega22(0,5,1) = 4.0402656E-01;  Omega22(0,5,2) = -2.6712374E+00; Omega22(0,5,3) = 4.1447669E+02;
+    Omega22(0,6,0) = 1.0000000E+00;  Omega22(0,6,1) = 1.0000000E+00;  Omega22(0,6,2) = 1.0000000E+00;  Omega22(0,6,3) = 1.0000000E+00;
     //N2
-    Omega11(1,0,0) = -4.2254948E-03; Omega11(1,0,1) = -5.2965163E-02; Omega11(1,0,2) = 1.9157708E+00;  Omega11(1,0,3) = 6.3263309E-04;
-    Omega11(1,1,0) = -7.6303990E-03; Omega11(1,1,1) = 1.6878089E-01;  Omega11(1,1,2) = -1.4004234E+00; Omega11(1,1,3) = 2.1427708E+03;
-    Omega11(1,2,0) = -8.0457321E-03; Omega11(1,2,1) = 1.9228905E-01;  Omega11(1,2,2) = -1.7102854E+00; Omega11(1,2,3) = 5.2213857E+03;
-    Omega11(1,3,0) = -6.8237776E-03; Omega11(1,3,1) = 1.4360616E-01;  Omega11(1,3,2) = -1.1922240E+00; Omega11(1,3,3) = 1.2433086E+03;
-    Omega11(1,4,0) = -8.3493693E-03; Omega11(1,4,1) = 1.7808911E-01;  Omega11(1,4,2) = -1.4466155E+00; Omega11(1,4,3) = 1.9324210E+03;
-    Omega11(1,5,0) = -8.3110691E-03; Omega11(1,5,1) = 1.9617877E-01;  Omega11(1,5,2) = -1.7205427E+00; Omega11(1,5,3) = 4.0812829E+03;
-    Omega11(1,6,0) = 0.0000000E+00;  Omega11(1,6,1) = 8.5112236E-02;  Omega11(1,6,2) = -1.7460044E+00; Omega11(1,6,3) = 1.4498969E+05;
+    Omega22(1,0,0) = -4.2254948E-03; Omega22(1,0,1) = -5.2965163E-02; Omega22(1,0,2) = 1.9157708E+00;  Omega22(1,0,3) = 6.3263309E-04;
+    Omega22(1,1,0) = -7.6303990E-03; Omega22(1,1,1) = 1.6878089E-01;  Omega22(1,1,2) = -1.4004234E+00; Omega22(1,1,3) = 2.1427708E+03;
+    Omega22(1,2,0) = -8.0457321E-03; Omega22(1,2,1) = 1.9228905E-01;  Omega22(1,2,2) = -1.7102854E+00; Omega22(1,2,3) = 5.2213857E+03;
+    Omega22(1,3,0) = -6.8237776E-03; Omega22(1,3,1) = 1.4360616E-01;  Omega22(1,3,2) = -1.1922240E+00; Omega22(1,3,3) = 1.2433086E+03;
+    Omega22(1,4,0) = -8.3493693E-03; Omega22(1,4,1) = 1.7808911E-01;  Omega22(1,4,2) = -1.4466155E+00; Omega22(1,4,3) = 1.9324210E+03;
+    Omega22(1,5,0) = -8.3110691E-03; Omega22(1,5,1) = 1.9617877E-01;  Omega22(1,5,2) = -1.7205427E+00; Omega22(1,5,3) = 4.0812829E+03;
+    Omega22(1,6,0) = 0.0000000E+00;  Omega22(1,6,1) = 8.5112236E-02;  Omega22(1,6,2) = -1.7460044E+00; Omega22(1,6,3) = 1.4498969E+05;
     //O2
-    Omega11(2,0,0) = 9.6744867E-03;  Omega11(2,0,1) = -3.3759583E-01; Omega11(2,0,2) = 3.7952121E+00;  Omega11(2,0,3) = 6.8468036E-06;
-    Omega11(2,1,0) = -8.0457321E-03; Omega11(2,1,1) = 1.9228905E-01;  Omega11(2,1,2) = -1.7102854E+00; Omega11(2,1,3) = 5.2213857E+03;
-    Omega11(2,2,0) = -6.2931612E-03; Omega11(2,2,1) = 1.4624645E-01;  Omega11(2,2,2) = -1.3006927E+00; Omega11(2,2,3) = 1.8066892E+03;
-    Omega11(2,3,0) = -6.8508672E-03; Omega11(2,3,1) = 1.5524564E-01;  Omega11(2,3,2) = -1.3479583E+00; Omega11(2,3,3) = 2.0037890E+03;
-    Omega11(2,4,0) = -1.0608832E-03; Omega11(2,4,1) = 1.1782595E-02;  Omega11(2,4,2) = -2.1246301E-01; Omega11(2,4,3) = 8.4561598E+01;
-    Omega11(2,5,0) = -3.7969686E-03; Omega11(2,5,1) = 7.6789981E-02;  Omega11(2,5,2) = -7.3056809E-01; Omega11(2,5,3) = 3.3958171E+02;
-    Omega11(2,6,0) = 0.0000000E+00;  Omega11(2,6,1) = 8.4737359E-02;  Omega11(2,6,2) = -1.7290488E+00; Omega11(2,6,3) = 1.2485194E+05;
+    Omega22(2,0,0) = 9.6744867E-03;  Omega22(2,0,1) = -3.3759583E-01; Omega22(2,0,2) = 3.7952121E+00;  Omega22(2,0,3) = 6.8468036E-06;
+    Omega22(2,1,0) = -8.0457321E-03; Omega22(2,1,1) = 1.9228905E-01;  Omega22(2,1,2) = -1.7102854E+00; Omega22(2,1,3) = 5.2213857E+03;
+    Omega22(2,2,0) = -6.2931612E-03; Omega22(2,2,1) = 1.4624645E-01;  Omega22(2,2,2) = -1.3006927E+00; Omega22(2,2,3) = 1.8066892E+03;
+    Omega22(2,3,0) = -6.8508672E-03; Omega22(2,3,1) = 1.5524564E-01;  Omega22(2,3,2) = -1.3479583E+00; Omega22(2,3,3) = 2.0037890E+03;
+    Omega22(2,4,0) = -1.0608832E-03; Omega22(2,4,1) = 1.1782595E-02;  Omega22(2,4,2) = -2.1246301E-01; Omega22(2,4,3) = 8.4561598E+01;
+    Omega22(2,5,0) = -3.7969686E-03; Omega22(2,5,1) = 7.6789981E-02;  Omega22(2,5,2) = -7.3056809E-01; Omega22(2,5,3) = 3.3958171E+02;
+    Omega22(2,6,0) = 0.0000000E+00;  Omega22(2,6,1) = 8.4737359E-02;  Omega22(2,6,2) = -1.7290488E+00; Omega22(2,6,3) = 1.2485194E+05;
     //NO
-    Omega11(3,0,0) = 0.0000000E+00;  Omega11(0,3,1) = 5.4444485E-02;  Omega11(0,3,2) = -1.2854128E+00; Omega11(0,3,3) = 1.3857556E+04;
-    Omega11(3,1,0) = -6.8237776E-03; Omega11(3,1,1) = 1.4360616E-01;  Omega11(3,1,2) = -1.1922240E+00; Omega11(3,1,3) = 1.2433086E+03;
-    Omega11(3,2,0) = -6.8508672E-03; Omega11(3,2,1) = 1.5524564E-01;  Omega11(3,2,2) = -1.3479583E+00; Omega11(3,2,3) = 2.0037890E+03;
-    Omega11(3,3,0) = -7.4942466E-03; Omega11(3,3,1) = 1.6626193E-01;  Omega11(3,3,2) = -1.4107027E+00; Omega11(3,3,3) = 2.3097604E+03;
-    Omega11(3,4,0) = -1.4719259E-03; Omega11(3,4,1) = 1.8446968E-02;  Omega11(3,4,2) = -2.6460411E-01; Omega11(3,4,3) = 1.0911124E+02;
-    Omega11(3,5,0) = -1.0066279E-03; Omega11(3,5,1) = 1.1029264E-02;  Omega11(3,5,2) = -2.0671266E-01; Omega11(3,5,3) = 8.2644384E+01;
-    Omega11(3,6,0) = 1.1055777E-02;  Omega11(3,6,1) = -1.6621846E-01; Omega11(3,6,2) = 1.4372166E-01;  Omega11(3,6,3) = 1.3182061E+03;
+    Omega22(3,0,0) = 0.0000000E+00;  Omega22(0,3,1) = 5.4444485E-02;  Omega22(0,3,2) = -1.2854128E+00; Omega22(0,3,3) = 1.3857556E+04;
+    Omega22(3,1,0) = -6.8237776E-03; Omega22(3,1,1) = 1.4360616E-01;  Omega22(3,1,2) = -1.1922240E+00; Omega22(3,1,3) = 1.2433086E+03;
+    Omega22(3,2,0) = -6.8508672E-03; Omega22(3,2,1) = 1.5524564E-01;  Omega22(3,2,2) = -1.3479583E+00; Omega22(3,2,3) = 2.0037890E+03;
+    Omega22(3,3,0) = -7.4942466E-03; Omega22(3,3,1) = 1.6626193E-01;  Omega22(3,3,2) = -1.4107027E+00; Omega22(3,3,3) = 2.3097604E+03;
+    Omega22(3,4,0) = -1.4719259E-03; Omega22(3,4,1) = 1.8446968E-02;  Omega22(3,4,2) = -2.6460411E-01; Omega22(3,4,3) = 1.0911124E+02;
+    Omega22(3,5,0) = -1.0066279E-03; Omega22(3,5,1) = 1.1029264E-02;  Omega22(3,5,2) = -2.0671266E-01; Omega22(3,5,3) = 8.2644384E+01;
+    Omega22(3,6,0) = 1.1055777E-02;  Omega22(3,6,1) = -1.6621846E-01; Omega22(3,6,2) = 1.4372166E-01;  Omega22(3,6,3) = 1.3182061E+03;
     //N
-    Omega11(4,0,0) = -1.0903638E-01; Omega11(4,0,1) = 2.8678381E+00;  Omega11(4,0,2) = -2.5297550E+01; Omega11(4,0,3) = 3.4838798E+33;
-    Omega11(4,1,0) = -8.3493693E-03; Omega11(4,1,1) = 1.7808911E-01;  Omega11(4,1,2) = -1.4466155E+00; Omega11(4,1,3) = 1.9324210E+03;
-    Omega11(4,2,0) = -1.0608832E-03; Omega11(4,2,1) = 1.1782595E-02;  Omega11(4,2,2) = -2.1246301E-01; Omega11(4,2,3) = 8.4561598E+01;
-    Omega11(4,3,0) = -1.4719259E-03; Omega11(4,3,1) = 1.8446968E-02;  Omega11(4,3,2) = -2.6460411E-01; Omega11(4,3,3) = 1.0911124E+02;
-    Omega11(4,4,0) = -7.7439615E-03; Omega11(4,4,1) = 1.7129007E-01;  Omega11(4,4,2) = -1.4809088E+00; Omega11(4,4,3) = 2.1284951E+03;
-    Omega11(4,5,0) = -5.0478143E-03; Omega11(4,5,1) = 1.0236186E-01;  Omega11(4,5,2) = -9.0058935E-01; Omega11(4,5,3) = 4.4472565E+02;
-    Omega11(4,6,0) = -2.1009546E-02; Omega11(4,6,1) = 5.8910426E-01;  Omega11(4,6,2) = -5.6681361E+00; Omega11(4,6,3) = 2.4486594E+09;
+    Omega22(4,0,0) = -1.0903638E-01; Omega22(4,0,1) = 2.8678381E+00;  Omega22(4,0,2) = -2.5297550E+01; Omega22(4,0,3) = 3.4838798E+33;
+    Omega22(4,1,0) = -8.3493693E-03; Omega22(4,1,1) = 1.7808911E-01;  Omega22(4,1,2) = -1.4466155E+00; Omega22(4,1,3) = 1.9324210E+03;
+    Omega22(4,2,0) = -1.0608832E-03; Omega22(4,2,1) = 1.1782595E-02;  Omega22(4,2,2) = -2.1246301E-01; Omega22(4,2,3) = 8.4561598E+01;
+    Omega22(4,3,0) = -1.4719259E-03; Omega22(4,3,1) = 1.8446968E-02;  Omega22(4,3,2) = -2.6460411E-01; Omega22(4,3,3) = 1.0911124E+02;
+    Omega22(4,4,0) = -7.7439615E-03; Omega22(4,4,1) = 1.7129007E-01;  Omega22(4,4,2) = -1.4809088E+00; Omega22(4,4,3) = 2.1284951E+03;
+    Omega22(4,5,0) = -5.0478143E-03; Omega22(4,5,1) = 1.0236186E-01;  Omega22(4,5,2) = -9.0058935E-01; Omega22(4,5,3) = 4.4472565E+02;
+    Omega22(4,6,0) = -2.1009546E-02; Omega22(4,6,1) = 5.8910426E-01;  Omega22(4,6,2) = -5.6681361E+00; Omega22(4,6,3) = 2.4486594E+09;
     //O
-    Omega11(5,0,0) = -1.7924100E-02; Omega11(5,0,1) = 4.0402656E-01;  Omega11(5,0,2) = -2.6712374E+00; Omega11(5,0,3) = 4.1447669E+02;
-    Omega11(5,1,0) = -8.3110691E-03; Omega11(5,1,1) = 1.9617877E-01;  Omega11(5,1,2) = -1.7205427E+00; Omega11(5,1,3) = 4.0812829E+03;
-    Omega11(5,2,0) = -3.7969686E-03; Omega11(5,2,1) = 7.6789981E-02;  Omega11(5,2,2) = -7.3056809E-01; Omega11(5,2,3) = 3.3958171E+02;
-    Omega11(5,3,0) = -1.0066279E-03; Omega11(5,3,1) = 1.1029264E-02;  Omega11(5,3,2) = -2.0671266E-01; Omega11(5,3,3) = 8.2644384E+01;
-    Omega11(5,4,0) = -5.0478143E-03; Omega11(5,4,1) = 1.0236186E-01;  Omega11(5,4,2) = -9.0058935E-01; Omega11(5,4,3) = 4.4472565E+02;
-    Omega11(5,5,0) = -4.2451096E-03; Omega11(5,5,1) = 9.6820337E-02;  Omega11(5,5,2) = -9.9770795E-01; Omega11(5,5,3) = 8.3320644E+02;
-    Omega11(5,6,0) = -1.5315132E-02; Omega11(5,6,1) = 4.3541627E-01;  Omega11(5,6,2) = -4.2864279E+00; Omega11(5,6,3) = 3.5125207E+07;
+    Omega22(5,0,0) = -1.7924100E-02; Omega22(5,0,1) = 4.0402656E-01;  Omega22(5,0,2) = -2.6712374E+00; Omega22(5,0,3) = 4.1447669E+02;
+    Omega22(5,1,0) = -8.3110691E-03; Omega22(5,1,1) = 1.9617877E-01;  Omega22(5,1,2) = -1.7205427E+00; Omega22(5,1,3) = 4.0812829E+03;
+    Omega22(5,2,0) = -3.7969686E-03; Omega22(5,2,1) = 7.6789981E-02;  Omega22(5,2,2) = -7.3056809E-01; Omega22(5,2,3) = 3.3958171E+02;
+    Omega22(5,3,0) = -1.0066279E-03; Omega22(5,3,1) = 1.1029264E-02;  Omega22(5,3,2) = -2.0671266E-01; Omega22(5,3,3) = 8.2644384E+01;
+    Omega22(5,4,0) = -5.0478143E-03; Omega22(5,4,1) = 1.0236186E-01;  Omega22(5,4,2) = -9.0058935E-01; Omega22(5,4,3) = 4.4472565E+02;
+    Omega22(5,5,0) = -4.2451096E-03; Omega22(5,5,1) = 9.6820337E-02;  Omega22(5,5,2) = -9.9770795E-01; Omega22(5,5,3) = 8.3320644E+02;
+    Omega22(5,6,0) = -1.5315132E-02; Omega22(5,6,1) = 4.3541627E-01;  Omega22(5,6,2) = -4.2864279E+00; Omega22(5,6,3) = 3.5125207E+07;
     //NO+
-    Omega11(6,0,0) = 1.0000000E+00;  Omega11(6,0,1) = 1.0000000E+00;  Omega11(6,0,2) = 1.0000000E+00;  Omega11(6,0,3) = 1.0000000E+00;
-    Omega11(6,1,0) = 0.0000000E+00;  Omega11(6,1,1) = 8.5112236E-02;  Omega11(6,1,2) = -1.7460044E+00; Omega11(6,1,3) = 1.4498969E+05;
-    Omega11(6,2,0) = 0.0000000E+00;  Omega11(6,2,1) = 8.4737359E-02;  Omega11(6,2,2) = -1.7290488E+00; Omega11(6,2,3) = 1.2485194E+05;
-    Omega11(6,3,0) = 1.1055777E-02;  Omega11(6,3,1) = -1.6621846E-01; Omega11(6,3,2) = 1.4372166E-01;  Omega11(6,3,3) = 1.3182061E+03;
-    Omega11(6,4,0) = -2.1009546E-02; Omega11(6,4,1) = 5.8910426E-01;  Omega11(6,4,2) = -5.6681361E+00; Omega11(6,4,3) = 2.4486594E+09;
-    Omega11(6,5,0) = -1.5315132E-02; Omega11(6,5,1) = 4.3541627E-01;  Omega11(6,5,2) = -4.2864279E+00; Omega11(6,5,3) = 3.5125207E+07;
-    Omega11(6,6,0) = -1.000000E+00;  Omega11(6,6,1) = -1.000000E+00;  Omega11(6,6,2) = -1.000000E+00;  Omega11(6,6,3) = -1.000000E+00;
+    Omega22(6,0,0) = 1.0000000E+00;  Omega22(6,0,1) = 1.0000000E+00;  Omega22(6,0,2) = 1.0000000E+00;  Omega22(6,0,3) = 1.0000000E+00;
+    Omega22(6,1,0) = 0.0000000E+00;  Omega22(6,1,1) = 8.5112236E-02;  Omega22(6,1,2) = -1.7460044E+00; Omega22(6,1,3) = 1.4498969E+05;
+    Omega22(6,2,0) = 0.0000000E+00;  Omega22(6,2,1) = 8.4737359E-02;  Omega22(6,2,2) = -1.7290488E+00; Omega22(6,2,3) = 1.2485194E+05;
+    Omega22(6,3,0) = 1.1055777E-02;  Omega22(6,3,1) = -1.6621846E-01; Omega22(6,3,2) = 1.4372166E-01;  Omega22(6,3,3) = 1.3182061E+03;
+    Omega22(6,4,0) = -2.1009546E-02; Omega22(6,4,1) = 5.8910426E-01;  Omega22(6,4,2) = -5.6681361E+00; Omega22(6,4,3) = 2.4486594E+09;
+    Omega22(6,5,0) = -1.5315132E-02; Omega22(6,5,1) = 4.3541627E-01;  Omega22(6,5,2) = -4.2864279E+00; Omega22(6,5,3) = 3.5125207E+07;
+    Omega22(6,6,0) = -1.000000E+00;  Omega22(6,6,1) = -1.000000E+00;  Omega22(6,6,2) = -1.000000E+00;  Omega22(6,6,3) = -1.000000E+00;
 
     // Creation/Destruction (+1/-1), Index of monoatomic reactants
     // Monoatomic species (N,O) recombine into diaatomic (N2, O2)
@@ -1785,11 +1785,11 @@ void CSU2TCLib::DiffusionCoeffWBE(){
     for (jSpecies = iSpecies; jSpecies < nSpecies; jSpecies++) {
       const su2double Mj = MolarMass[jSpecies]*1E-3;
 
-      /*--- Calculate the Omega^(0,0)_ij collision cross section ---*/
-      const su2double Omega_ij = 1E-20/PI_NUMBER * Omega00(iSpecies,jSpecies,3)
-          * pow(T, Omega00(iSpecies,jSpecies,0)*log(T)*log(T)
-          +  Omega00(iSpecies,jSpecies,1)*log(T)
-          +  Omega00(iSpecies,jSpecies,2));
+      /*--- Calculate the Omega^(1,1)_ij collision cross section ---*/
+      const su2double Omega_ij = 1E-20/PI_NUMBER * Omega11(iSpecies,jSpecies,3)
+          * pow(T, Omega11(iSpecies,jSpecies,0)*log(T)*log(T)
+          +  Omega11(iSpecies,jSpecies,1)*log(T)
+          +  Omega11(iSpecies,jSpecies,2));
       Dij(iSpecies,jSpecies) = 7.1613E-25*M*sqrt(T*(1/Mi+1/Mj))/(Density*Omega_ij);
       Dij(jSpecies,iSpecies) = 7.1613E-25*M*sqrt(T*(1/Mi+1/Mj))/(Density*Omega_ij);
     }
@@ -1877,7 +1877,7 @@ su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies,
 
   if (d1) {
     /*--- Check whether to use collision cross section data or Coulomb potential ---*/
-    if (Omega00(iSpecies, jSpecies, 0) == 1.0 && ionization) { // attractive potential
+    if (Omega11(iSpecies, jSpecies, 0) == 1.0 && ionization) { // attractive potential
       
       const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
       const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
@@ -1886,10 +1886,10 @@ su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies,
       const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
       const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
       
-      /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
+      /*--- Calculate the Omega^(1,1)_ij Coulomb potential ---*/
       Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);
 
-    } else if (Omega00(iSpecies, jSpecies, 0) == -1.0 && ionization) { // repulsive potential
+    } else if (Omega11(iSpecies, jSpecies, 0) == -1.0 && ionization) { // repulsive potential
 
       const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
       const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
@@ -1898,20 +1898,20 @@ su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies,
       const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
       const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
 
-      /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
+      /*--- Calculate the Omega^(1,1)_ij Coulomb potential ---*/
       Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_r*T_star*(1 - C1_r * exp(-c1_r * T_star))+1);
 
     } else {
 
-      /*--- Calculate the Omega^(0,0)_ij collision cross section ---*/
-      Omega_ij = 1E-20 * Omega00(iSpecies,jSpecies,3)
-                        * pow(T, Omega00(iSpecies,jSpecies,0)*log(T)*log(T)
-                               + Omega00(iSpecies,jSpecies,1)*log(T)
-                               + Omega00(iSpecies,jSpecies,2));
+      /*--- Calculate the Omega^(1,1)_ij collision cross section ---*/
+      Omega_ij = 1E-20 * Omega11(iSpecies,jSpecies,3)
+                        * pow(T, Omega11(iSpecies,jSpecies,0)*log(T)*log(T)
+                               + Omega11(iSpecies,jSpecies,1)*log(T)
+                               + Omega11(iSpecies,jSpecies,2));
     }  
   } else {
         /*--- Check whether to use collision cross section data or Coulomb potential ---*/
-    if (Omega11(iSpecies, jSpecies, 0) == 1.0 && ionization) { // attractive potential
+    if (Omega22(iSpecies, jSpecies, 0) == 1.0 && ionization) { // attractive potential
       
       const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
       const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
@@ -1920,10 +1920,10 @@ su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies,
       const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
       const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
       
-      /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
+      /*--- Calculate the Omega^(2,2)_ij Coulomb potential ---*/
       Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D2_a*T_star*(1 - C2_a * exp(-c2_a * T_star))+1);
 
-    } else if (Omega11(iSpecies, jSpecies, 0) == -1.0 && ionization) { // repulsive potential
+    } else if (Omega22(iSpecies, jSpecies, 0) == -1.0 && ionization) { // repulsive potential
 
       const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
       const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
@@ -1932,16 +1932,16 @@ su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies,
       const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
       const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
 
-      /*--- Calculate the Omega^(0,0)_ij Coulomb potential ---*/
+      /*--- Calculate the Omega^(2,2)_ij Coulomb potential ---*/
       Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D2_r*T_star*(1 - C2_r * exp(-c2_r * T_star))+1);
 
     } else {
 
-      /*--- Calculate the Omega^(0,0)_ij collision cross section ---*/
-      Omega_ij = 1E-20 * Omega11(iSpecies,jSpecies,3)
-                        * pow(T, Omega00(iSpecies,jSpecies,0)*log(T)*log(T)
-                               + Omega00(iSpecies,jSpecies,1)*log(T)
-                               + Omega00(iSpecies,jSpecies,2));
+      /*--- Calculate the Omega^(2,2)_ij collision cross section ---*/
+      Omega_ij = 1E-20 * Omega22(iSpecies,jSpecies,3)
+                        * pow(T, Omega22(iSpecies,jSpecies,0)*log(T)*log(T)
+                               + Omega22(iSpecies,jSpecies,1)*log(T)
+                               + Omega22(iSpecies,jSpecies,2));
     }  
   }
   

From 3e0ba63e713508b2c7dc23c8b8ab1d95c845b8c8 Mon Sep 17 00:00:00 2001
From: Jacob Needels <44848904+jtneedels@users.noreply.github.com>
Date: Tue, 17 Jan 2023 13:40:51 -0800
Subject: [PATCH 138/656] Update SU2_CFD/include/fluid/CSU2TCLib.hpp

Co-authored-by: Wally Maier <wallytmaier@gmail.com>
---
 SU2_CFD/include/fluid/CSU2TCLib.hpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/SU2_CFD/include/fluid/CSU2TCLib.hpp b/SU2_CFD/include/fluid/CSU2TCLib.hpp
index 65d91d08090..5b447ee99ec 100644
--- a/SU2_CFD/include/fluid/CSU2TCLib.hpp
+++ b/SU2_CFD/include/fluid/CSU2TCLib.hpp
@@ -273,7 +273,7 @@ class CSU2TCLib : public CNEMOGas {
    *\param[in] Mj - Molar mass of species j
    *\param[in] T - Temperature of gas
    *\param[in] d1 - Whether delta_1 or delta_2 is computed
-   *\param[out] Delta_1 or Delta_2
+   *\param[out] Delta_1 or Delta_2 - Collision term between species i and j
    */
   su2double ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies, su2double Mi, su2double Mj, su2double T, bool d1);
 

From 16845a5b10518e138376ee590275d34e0c344590 Mon Sep 17 00:00:00 2001
From: Jacob Needels <44848904+jtneedels@users.noreply.github.com>
Date: Tue, 17 Jan 2023 13:41:01 -0800
Subject: [PATCH 139/656] Update Common/src/CConfig.cpp

Co-authored-by: Wally Maier <wallytmaier@gmail.com>
---
 Common/src/CConfig.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index d25acbc61ad..60c8e7a2f66 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -6162,7 +6162,7 @@ void CConfig::SetOutput(SU2_COMPONENT val_software, unsigned short val_izone) {
         if (Kind_Regime == ENUM_REGIME::COMPRESSIBLE) cout << "Compressible two-temperature thermochemical non-equilibrium Navier-Stokes equations." << endl;
         if (Kind_FluidModel == SU2_NONEQ){
           if ((GasModel != "N2") && (GasModel != "AIR-5") && (GasModel != "AIR-7") && (GasModel != "ARGON"))
-          SU2_MPI::Error("The GAS_MODEL given is unavailble using CSU2TCLIB. Choose one of the options: N2, AIR-5, AIR-7, or ARGON.", CURRENT_FUNCTION);
+          SU2_MPI::Error("The GAS_MODEL given is unavailable using CSU2TCLIB. Choose one of the options: N2, AIR-5, AIR-7, or ARGON.", CURRENT_FUNCTION);
         }
         break;
       case MAIN_SOLVER::FEM_LES:

From d073156c48e7b3ee3a64fcd7f2d054981c28db75 Mon Sep 17 00:00:00 2001
From: Jacob Needels <44848904+jtneedels@users.noreply.github.com>
Date: Tue, 17 Jan 2023 13:41:19 -0800
Subject: [PATCH 140/656] Update Common/src/CConfig.cpp

Co-authored-by: Wally Maier <wallytmaier@gmail.com>
---
 Common/src/CConfig.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 60c8e7a2f66..1270f7a1f46 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -6155,7 +6155,7 @@ void CConfig::SetOutput(SU2_COMPONENT val_software, unsigned short val_izone) {
         if (Kind_Regime == ENUM_REGIME::COMPRESSIBLE) cout << "Compressible two-temperature thermochemical non-equilibrium Euler equations." << endl;
         if (Kind_FluidModel == SU2_NONEQ){
           if ((GasModel != "N2") && (GasModel != "AIR-5") && (GasModel != "AIR-7") && (GasModel != "ARGON"))
-            SU2_MPI::Error("The GAS_MODEL given is unavailble using CSU2TCLIB. Choose one of the options: N2, AIR-5, AIR-7, or ARGON.", CURRENT_FUNCTION);
+            SU2_MPI::Error("The GAS_MODEL given is unavailable using CSU2TCLIB. Choose one of the options: N2, AIR-5, AIR-7, or ARGON.", CURRENT_FUNCTION);
         }
         break;
       case MAIN_SOLVER::NEMO_NAVIER_STOKES:

From b0bee19fe3200d74bfc79dafdf829f2871141ea6 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 18 Jan 2023 16:14:37 +0100
Subject: [PATCH 141/656] CoDiPack update.

---
 externals/codi        | 2 +-
 meson_scripts/init.py | 2 +-
 2 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/externals/codi b/externals/codi
index 82e80e953d3..a282326f226 160000
--- a/externals/codi
+++ b/externals/codi
@@ -1 +1 @@
-Subproject commit 82e80e953d3aa1486d9879909308af51ed8159dc
+Subproject commit a282326f22612b46e2324ba9e4e5439a55ae157a
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 3326cf113f7..5fe2c669649 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -44,7 +44,7 @@ def init_submodules(method = 'auto'):
 
   # This information of the modules is used if projects was not cloned using git
   # The sha tag must be maintained manually to point to the correct commit
-  sha_version_codi = '96ac78ec5bcc5ac25b785e79b16ed76fca22d736'
+  sha_version_codi = 'a282326f22612b46e2324ba9e4e5439a55ae157a'
   github_repo_codi = 'https://github.com/scicompkl/CoDiPack'
   sha_version_medi = '6aef76912e7099c4f08c9705848797ca9e8070da'
   github_repo_medi = 'https://github.com/SciCompKL/MeDiPack'

From 1080cb64ee9e5d1438682166a78cde492ebaa471 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 18 Jan 2023 16:15:17 +0100
Subject: [PATCH 142/656] OpDiLib update.

---
 externals/opdi        | 2 +-
 meson_scripts/init.py | 2 +-
 2 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/externals/opdi b/externals/opdi
index 13350bc3b57..f33b507c24f 160000
--- a/externals/opdi
+++ b/externals/opdi
@@ -1 +1 @@
-Subproject commit 13350bc3b57d27e1845af0e8998eafee22b29593
+Subproject commit f33b507c24f7448d4cf4df16ab5c53ea254b8774
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 5fe2c669649..b5dbd2128fc 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -48,7 +48,7 @@ def init_submodules(method = 'auto'):
   github_repo_codi = 'https://github.com/scicompkl/CoDiPack'
   sha_version_medi = '6aef76912e7099c4f08c9705848797ca9e8070da'
   github_repo_medi = 'https://github.com/SciCompKL/MeDiPack'
-  sha_version_opdi = '1aabf5bd1ed77611742eb655002f2ac7a3dddef9'
+  sha_version_opdi = 'f33b507c24f7448d4cf4df16ab5c53ea254b8774'
   github_repo_opdi = 'https://github.com/SciCompKL/OpDiLib'
   sha_version_meson = '41c650a040d50e0912d268af7a903a9ce1456dfa'
   github_repo_meson = 'https://github.com/mesonbuild/meson'

From de7d49393ed83f40e2ff2846700a760840a0bd53 Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Wed, 18 Jan 2023 16:35:52 -0800
Subject: [PATCH 143/656] fix error in n_e equation

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 SU2_CFD/src/fluid/CSU2TCLib.cpp | 15 ++++++++++-----
 1 file changed, 10 insertions(+), 5 deletions(-)

diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index b9e72272621..ce19cc738fe 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1871,7 +1871,8 @@ void CSU2TCLib::ThermalConductivitiesWBE(){
 
 su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies, su2double Mi, su2double Mj, su2double T, bool d1) {
 
-  su2double pi = PI_NUMBER;
+  const su2double pi = PI_NUMBER;
+  const su2double Na = AVOGAD_CONSTANT;
 
   su2double Omega_ij;
 
@@ -1881,7 +1882,8 @@ su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies,
       
       const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
       const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
-      const su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
+
+      const su2double ne_cgs = Na * rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
         
       const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
       const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
@@ -1893,7 +1895,8 @@ su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies,
 
       const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
       const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
-      const su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
+      
+      const su2double ne_cgs = Na * rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
         
       const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
       const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
@@ -1915,7 +1918,8 @@ su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies,
       
       const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
       const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
-      const su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
+      
+      const su2double ne_cgs = Na * rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
         
       const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
       const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
@@ -1927,7 +1931,8 @@ su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies,
 
       const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
       const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
-      const su2double ne_cgs = rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
+      
+      const su2double ne_cgs = Na * rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
         
       const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
       const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));

From bdc42b1c0f4db95aafc60c808fa0b161fa4ef4fc Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Wed, 18 Jan 2023 23:21:35 -0800
Subject: [PATCH 144/656] partial fix kappa, Ds still not correct

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 SU2_CFD/src/fluid/CSU2TCLib.cpp | 14 +++++++-------
 1 file changed, 7 insertions(+), 7 deletions(-)

diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index ce19cc738fe..62e83ce3779 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1998,7 +1998,7 @@ void CSU2TCLib::DiffusionCoeffGY(){
       }
     }
     /*--- Calculate species diffusion coefficient ---*/
-    DiffusionCoeff[iSpecies] = (denom > EPS) ? (gam_t*gam_t*Mi*(1-Mi*gam_i) / denom) : su2double(0.0);
+    DiffusionCoeff[iSpecies] = (gam_t*gam_t*Mi*(1-Mi*gam_i) / denom);
   }
 }
 
@@ -2086,13 +2086,13 @@ void CSU2TCLib::ThermalConductivitiesGY(){
     }
 
     /*--- Translational contribution to thermal conductivity ---*/
-    ThermalCond_tr += (denom_t > EPS) ? ((15.0/4.0)*kb*gam_i/denom_t) : su2double(0.0);
+    ThermalCond_tr += ((15.0/4.0)*kb*gam_i/denom_t);
 
-    /*--- Translational contribution to thermal conductivity ---*/
-    if (RotationModes[iSpecies] != 0.0) ThermalCond_tr += (denom_r > EPS) ? (kb*gam_i/denom_r) : su2double(0.0);
+    /*--- Rotational contribution to thermal conductivity ---*/
+    if (RotationModes[iSpecies] != 0.0) ThermalCond_tr += (kb*gam_i/denom_r);
 
     /*--- Vibrational-electronic contribution to thermal conductivity ---*/
-    ThermalCond_ve += (denom_r > EPS) ? (kb*Cvve/R*gam_i / denom_r) : su2double(0.0);
+    ThermalCond_ve += (kb*Cvve/R*gam_i / denom_r);
   }
 
   ThermalConductivities[0] = ThermalCond_tr;
@@ -2158,8 +2158,8 @@ vector<su2double>& CSU2TCLib::ComputeTemperatures(vector<su2double>& val_rhos, s
   /*--- Set vibrational temperature algorithm parameters ---*/
   const su2double NRtol         = 1.0E-6;    // Tolerance for the Newton-Raphson method
   const su2double Btol          = 1.0E-6;    // Tolerance for the Bisection method
-  const unsigned short maxBIter = 50;        // Maximum Bisection method iterations
-  const unsigned short maxNIter = 50;        // Maximum Newton-Raphson iterations
+  const unsigned short maxBIter = 100;        // Maximum Bisection method iterations
+  const unsigned short maxNIter = 100;        // Maximum Newton-Raphson iterations
   const su2double scale         = 0.9;       // Scaling factor for Newton-Raphson step
 
   /*--- Execute a Newton-Raphson root-finding method for Tve ---*/

From ad8f4ecaabc8486af79eb0ef6356febbdc850a84 Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Thu, 19 Jan 2023 08:58:07 -0800
Subject: [PATCH 145/656] fix index error

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 SU2_CFD/src/fluid/CSU2TCLib.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 62e83ce3779..4fdcdc33b2f 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1982,7 +1982,7 @@ void CSU2TCLib::DiffusionCoeffGY(){
       if (jSpecies != iSpecies) { 
 
         const su2double Mj    = MolarMass[jSpecies];
-        const su2double gam_j = rhos[iSpecies] / (Density*Mj);
+        const su2double gam_j = rhos[jSpecies] / (Density*Mj);
 
         const su2double kb = BOLTZMANN_CONSTANT;
 

From 5352294ca4682f1e5fe4562b3d1147b3b7e425e4 Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Thu, 19 Jan 2023 16:37:51 -0800
Subject: [PATCH 146/656] cleanup

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 SU2_CFD/src/fluid/CSU2TCLib.cpp | 83 ++++++++++-----------------------
 1 file changed, 25 insertions(+), 58 deletions(-)

diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 4fdcdc33b2f..60ed6cd98da 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1875,11 +1875,11 @@ su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies,
   const su2double Na = AVOGAD_CONSTANT;
 
   su2double Omega_ij;
+  const bool coulomb1 = (d1 && ionization && (Omega11(iSpecies, jSpecies, 0) == 1.0 || Omega11(iSpecies, jSpecies, 0) == -1.0));
+  const bool coulomb2 = (d2 && ionization && (Omega22(iSpecies, jSpecies, 0) == 1.0 || Omega22(iSpecies, jSpecies, 0) == -1.0));
 
-  if (d1) {
-    /*--- Check whether to use collision cross section data or Coulomb potential ---*/
-    if (Omega11(iSpecies, jSpecies, 0) == 1.0 && ionization) { // attractive potential
-      
+  if (coulomb1 || coulomb2) {
+    
       const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
       const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
 
@@ -1887,20 +1887,17 @@ su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies,
         
       const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
       const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
-      
+  }
+
+  if (d1) {
+    /*--- Check whether to use collision cross section data or Coulomb potential ---*/
+    if (Omega11(iSpecies, jSpecies, 0) == 1.0 && ionization) { // attractive potential
+
       /*--- Calculate the Omega^(1,1)_ij Coulomb potential ---*/
       Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);
 
     } else if (Omega11(iSpecies, jSpecies, 0) == -1.0 && ionization) { // repulsive potential
 
-      const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
-      const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
-      
-      const su2double ne_cgs = Na * rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
-        
-      const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
-      const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
-
       /*--- Calculate the Omega^(1,1)_ij Coulomb potential ---*/
       Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_r*T_star*(1 - C1_r * exp(-c1_r * T_star))+1);
 
@@ -1916,27 +1913,11 @@ su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies,
         /*--- Check whether to use collision cross section data or Coulomb potential ---*/
     if (Omega22(iSpecies, jSpecies, 0) == 1.0 && ionization) { // attractive potential
       
-      const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
-      const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
-      
-      const su2double ne_cgs = Na * rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
-        
-      const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
-      const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
-      
       /*--- Calculate the Omega^(2,2)_ij Coulomb potential ---*/
       Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D2_a*T_star*(1 - C2_a * exp(-c2_a * T_star))+1);
 
     } else if (Omega22(iSpecies, jSpecies, 0) == -1.0 && ionization) { // repulsive potential
 
-      const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
-      const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
-      
-      const su2double ne_cgs = Na * rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
-        
-      const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
-      const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
-
       /*--- Calculate the Omega^(2,2)_ij Coulomb potential ---*/
       Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D2_r*T_star*(1 - C2_r * exp(-c2_r * T_star))+1);
 
@@ -1986,15 +1967,11 @@ void CSU2TCLib::DiffusionCoeffGY(){
 
         const su2double kb = BOLTZMANN_CONSTANT;
 
-        if (iSpecies == 0 && ionization) {
-          const su2double d1_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, Tve, true);
-          const su2double D_ij = kb*Tve/(Pressure*d1_ij);
-          denom += gam_j/D_ij;
-        } else {
-          const su2double d1_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T, true);
-          const su2double D_ij = kb*T/(Pressure*d1_ij);
-          denom += gam_j/D_ij;
-        }
+        const su2double T_col = (iSpecies == 0 && ionization) ? Tve : T; 
+
+        const su2double d1_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T_col, true);
+        const su2double D_ij = kb*T/(Pressure*d1_ij);
+        denom += gam_j/D_ij;
       }
     }
     /*--- Calculate species diffusion coefficient ---*/
@@ -2020,13 +1997,10 @@ void CSU2TCLib::ViscosityGY(){
       const su2double Mj    = MolarMass[jSpecies];
       const su2double gam_j = rhos[jSpecies] / (Density*Mj);
 
-      if (iSpecies == 0 && ionization) {
-          const su2double d2_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, Tve, false);
-          denom += gam_j*d2_ij;
-      } else {
-          const su2double d2_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T, false);
-          denom += gam_j*d2_ij;
-      }
+      const su2double T_col = (iSpecies == 0 && ionization) ? Tve : T; 
+
+      const su2double d2_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T_col, false);
+      denom += gam_j*d2_ij;
     }
     /*--- Calculate species laminar viscosity ---*/
     Mu += (Mi/Na * gam_i) / denom;
@@ -2069,20 +2043,13 @@ void CSU2TCLib::ThermalConductivitiesGY(){
       const su2double gam_j = rhos[iSpecies] / (Density*Mj);
       const su2double a_ij = 1.0 + (1.0 - mi/mj)*(0.45 - 2.54*mi/mj) / ((1.0 + mi/mj)*(1.0 + mi/mj));
 
-      if (iSpecies == 0 && ionization) {
-        const su2double d1_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, Tve, true);
-        const su2double d2_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, Tve, false);
+      const su2double T_col = (iSpecies == 0 && ionization) ? Tve : T; 
 
-        denom_t += a_ij*gam_j*d2_ij;
-        denom_r += gam_j*d1_ij;
-      
-      } else {
-        const su2double d1_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T, true);
-        const su2double d2_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T, false);
-      
-        denom_t += a_ij*gam_j*d2_ij;
-        denom_r += gam_j*d1_ij;
-      }
+      const su2double d1_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T_col, true);
+      const su2double d2_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T_col, false);
+    
+      denom_t += a_ij*gam_j*d2_ij;
+      denom_r += gam_j*d1_ij;
     }
 
     /*--- Translational contribution to thermal conductivity ---*/

From 927198c7d5cb761a01a3c3e6ade29d461644e2c9 Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Thu, 19 Jan 2023 16:43:39 -0800
Subject: [PATCH 147/656] fix var declaration

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 SU2_CFD/src/fluid/CSU2TCLib.cpp | 6 +++---
 1 file changed, 3 insertions(+), 3 deletions(-)

diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 60ed6cd98da..0ec8cb75600 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1879,7 +1879,7 @@ su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies,
   const bool coulomb2 = (d2 && ionization && (Omega22(iSpecies, jSpecies, 0) == 1.0 || Omega22(iSpecies, jSpecies, 0) == -1.0));
 
   if (coulomb1 || coulomb2) {
-    
+
       const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
       const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
 
@@ -1948,6 +1948,8 @@ void CSU2TCLib::DiffusionCoeffGY(){
     gam_t += rhos[iSpecies] / (Density*MolarMass[iSpecies]);
   }
 
+  const su2double kb = BOLTZMANN_CONSTANT;
+
   /*--- Mixture thermal conductivity via Gupta-Yos approximation ---*/
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
 
@@ -1965,8 +1967,6 @@ void CSU2TCLib::DiffusionCoeffGY(){
         const su2double Mj    = MolarMass[jSpecies];
         const su2double gam_j = rhos[jSpecies] / (Density*Mj);
 
-        const su2double kb = BOLTZMANN_CONSTANT;
-
         const su2double T_col = (iSpecies == 0 && ionization) ? Tve : T; 
 
         const su2double d1_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T_col, true);

From 1dc08e897c80431574d76c799b739744a95ae36b Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Thu, 19 Jan 2023 16:57:10 -0800
Subject: [PATCH 148/656] revert to clear errors

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 SU2_CFD/src/fluid/CSU2TCLib.cpp | 43 ++++++++++++++++++++++++---------
 1 file changed, 31 insertions(+), 12 deletions(-)

diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 0ec8cb75600..9a74bd5deb2 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1875,11 +1875,11 @@ su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies,
   const su2double Na = AVOGAD_CONSTANT;
 
   su2double Omega_ij;
-  const bool coulomb1 = (d1 && ionization && (Omega11(iSpecies, jSpecies, 0) == 1.0 || Omega11(iSpecies, jSpecies, 0) == -1.0));
-  const bool coulomb2 = (d2 && ionization && (Omega22(iSpecies, jSpecies, 0) == 1.0 || Omega22(iSpecies, jSpecies, 0) == -1.0));
-
-  if (coulomb1 || coulomb2) {
 
+  if (d1) {
+    /*--- Check whether to use collision cross section data or Coulomb potential ---*/
+    if (Omega11(iSpecies, jSpecies, 0) == 1.0 && ionization) { // attractive potential
+      
       const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
       const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
 
@@ -1887,17 +1887,20 @@ su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies,
         
       const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
       const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
-  }
-
-  if (d1) {
-    /*--- Check whether to use collision cross section data or Coulomb potential ---*/
-    if (Omega11(iSpecies, jSpecies, 0) == 1.0 && ionization) { // attractive potential
-
+      
       /*--- Calculate the Omega^(1,1)_ij Coulomb potential ---*/
       Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);
 
     } else if (Omega11(iSpecies, jSpecies, 0) == -1.0 && ionization) { // repulsive potential
 
+      const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
+      const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
+      
+      const su2double ne_cgs = Na * rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
+        
+      const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
+      const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
+
       /*--- Calculate the Omega^(1,1)_ij Coulomb potential ---*/
       Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_r*T_star*(1 - C1_r * exp(-c1_r * T_star))+1);
 
@@ -1913,11 +1916,27 @@ su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies,
         /*--- Check whether to use collision cross section data or Coulomb potential ---*/
     if (Omega22(iSpecies, jSpecies, 0) == 1.0 && ionization) { // attractive potential
       
+      const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
+      const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
+      
+      const su2double ne_cgs = Na * rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
+        
+      const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
+      const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
+      
       /*--- Calculate the Omega^(2,2)_ij Coulomb potential ---*/
       Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D2_a*T_star*(1 - C2_a * exp(-c2_a * T_star))+1);
 
     } else if (Omega22(iSpecies, jSpecies, 0) == -1.0 && ionization) { // repulsive potential
 
+      const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
+      const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
+      
+      const su2double ne_cgs = Na * rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
+        
+      const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
+      const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
+
       /*--- Calculate the Omega^(2,2)_ij Coulomb potential ---*/
       Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D2_r*T_star*(1 - C2_r * exp(-c2_r * T_star))+1);
 
@@ -1948,8 +1967,6 @@ void CSU2TCLib::DiffusionCoeffGY(){
     gam_t += rhos[iSpecies] / (Density*MolarMass[iSpecies]);
   }
 
-  const su2double kb = BOLTZMANN_CONSTANT;
-
   /*--- Mixture thermal conductivity via Gupta-Yos approximation ---*/
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
 
@@ -1967,6 +1984,8 @@ void CSU2TCLib::DiffusionCoeffGY(){
         const su2double Mj    = MolarMass[jSpecies];
         const su2double gam_j = rhos[jSpecies] / (Density*Mj);
 
+        const su2double kb = BOLTZMANN_CONSTANT;
+
         const su2double T_col = (iSpecies == 0 && ionization) ? Tve : T; 
 
         const su2double d1_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T_col, true);

From 7c7a436113f2d207c2df8147e78f55ec7c5f5e52 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 20 Jan 2023 11:50:21 +0100
Subject: [PATCH 149/656] Added table extrapolation method based on the two
 nearest neighbors and improved the smoothness of the quasi-3D interpolation
 process

---
 Common/include/containers/CLookUpTable.hpp |  44 ++++-
 Common/src/containers/CLookUpTable.cpp     | 194 +++++++++++++++------
 2 files changed, 183 insertions(+), 55 deletions(-)

diff --git a/Common/include/containers/CLookUpTable.hpp b/Common/include/containers/CLookUpTable.hpp
index 518f1eb36c4..db658ba871e 100644
--- a/Common/include/containers/CLookUpTable.hpp
+++ b/Common/include/containers/CLookUpTable.hpp
@@ -214,6 +214,27 @@ class CLookUpTable {
    */
   unsigned long FindNearestNeighborOnHull(su2double val_CV1, su2double val_CV2, unsigned long i_level = 0);
 
+  /*!
+   * \brief Interpolate data based on distance-weighted averaging on the nearest two table nodes.
+   * \param[in] val_CV1 - - first coordinate of point P(val_CV1,val_CV2) to check.
+   * \param[in] val_CV2 - second coordinate of point P(val_CV1,val_CV2) to check.
+   * \param[in] val_names_var - vector of string names of the variables to look up.
+   * \param[out] val_vars - pointer to the vector of stored values of the variables to look up.
+   */
+  void InterpolateToNearestNeighbors(const su2double val_CV1, const su2double val_CV2,
+                                     const std::vector<std::string>& names_var, std::vector<su2double*>& var_vals,
+                                     const unsigned long i_level = 0);
+
+  /*!
+   * \brief Interpolate data based on distance-weighted averaging on the nearest two table nodes for a single variable
+   * \param[in] val_CV1 - - first coordinate of point P(val_CV1,val_CV2) to check.
+   * \param[in] val_CV2 - second coordinate of point P(val_CV1,val_CV2) to check.
+   * \param[in] name_var - variable name to look up.
+   * \param[out] var_val - pointer to the to be interpolated variable.
+   */
+  void InterpolateToNearestNeighbors(const su2double val_CV1, const su2double val_CV2, const std::string& name_var,
+                                     su2double* var_val, const unsigned long i_level = 0);
+
   /*!
    * \brief determine if a point P(val_CV1,val_CV2) is inside the triangle val_id_triangle.
    * \param[in] val_CV1 - first coordinate of point P(val_CV1,val_CV2) to check.
@@ -237,6 +258,18 @@ class CLookUpTable {
     return abs((x1 * (y2 - y3) + x2 * (y3 - y1) + x3 * (y1 - y2)) * 0.5);
   }
 
+  /*!
+   * \brief Compute the values of the first and second controlling variable based on normalized query coordinates
+   * \param[in] inclusion_levels - Pair containing lower(first) and upper(second) table inclusion level indices.
+   * \param[in] val_CV1 - first controlling variable value.
+   * \param[in] val_CV2 - second controlling variable value.
+   * \param[in] val_CV3 - third controlling variable value.
+   * \returns array with first and second controlling variable values for the upper and lower table inclusion levels.
+   */
+  std::array<std::array<su2double, 2>, 2> ComputeNormalizedXY(std::pair<unsigned long, unsigned long>& inclusion_levels,
+                                                              const su2double val_CV1, const su2double val_CV2,
+                                                              const su2double val_CV3);
+
  public:
   CLookUpTable(const std::string& file_name_lut, const std::string& name_CV1_in, const std::string& name_CV2_in);
 
@@ -257,12 +290,11 @@ class CLookUpTable {
                           unsigned long i_level = 0);
 
   /*!
-   * \brief lookup 1 value for each of the variables in "val_name_var" using controlling variable values(val_CV1,val_CV2).
-   * \param[in] val_names_var - vector of string names of the variables to look up.
-   * \param[out] val_vars - pointer to the vector of stored values of the variables to look up.
-   * \param[in] val_CV1 - value of controlling variable 1.
-   * \param[in] val_CV2 - value of controlling variable 2.
-   * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
+   * \brief lookup 1 value for each of the variables in "val_name_var" using controlling variable
+   * values(val_CV1,val_CV2). \param[in] val_names_var - vector of string names of the variables to look up. \param[out]
+   * val_vars - pointer to the vector of stored values of the variables to look up. \param[in] val_CV1 - value of
+   * controlling variable 1. \param[in] val_CV2 - value of controlling variable 2. \returns 1 if the lookup and
+   * subsequent interpolation was a success, 0 if not.
    */
   unsigned long LookUp_XY(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars,
                           su2double val_CV1, su2double val_CV2, unsigned long i_level = 0);
diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index e9222b0b6b4..80d291899a0 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -219,8 +219,8 @@ void CLookUpTable::PrintTableInfo() {
         cout << "| Average number of triangles:" << setw(36) << right << floor(n_tria_av) << " |" << endl;
         cout << "| Average number of edges:" << setw(40) << right << floor(n_edges_av) << " |" << endl;
         cout << "+------------------------------------------------------------------+" << endl;
-        cout << "| Minimum Z:" << setw(54) << right << limits_table_z.first << " |" << endl;
-        cout << "| Maximum Z:" << setw(54) << right << limits_table_z.second << " |" << endl;
+        cout << "| Minimum Z:" << setw(54) << right << *limits_table_z.first << " |" << endl;
+        cout << "| Maximum Z:" << setw(54) << right << *limits_table_z.second << " |" << endl;
         cout << "| Minimum Y:" << setw(54) << right << min_y << " |" << endl;
         cout << "| Maximum Y:" << setw(54) << right << max_y << " |" << endl;
         cout << "| Minimum X:" << setw(54) << right << min_x << " |" << endl;
@@ -415,26 +415,32 @@ std::pair<unsigned long, unsigned long> CLookUpTable::FindInclusionLevels(const
 }
 
 unsigned long CLookUpTable::LookUp_XYZ(const std::string& val_name_var, su2double* val_var, su2double val_CV1,
-                                       su2double val_CV2, su2double val_z) {
+                                       su2double val_CV2, su2double val_CV3) {
   /*--- Perform quasi-3D interpolation for a single variable named val_name_var on a query point
         with coordinates val_CV1, val_CV2, and val_z ---*/
 
   /* 1: Find table levels directly above and below the query point (the levels that sandwhich val_z) */
-  std::pair<unsigned long, unsigned long> inclusion_levels = FindInclusionLevels(val_z);
+  std::pair<unsigned long, unsigned long> inclusion_levels = FindInclusionLevels(val_CV3);
   bool within_z_limits = (inclusion_levels.first != inclusion_levels.second);
 
   if (within_z_limits) {
-    /* 2: Perform 2D interpolations on upper and lower inclusion levels */
+    /* 2: Determine val_CV1 and val_CV2 for the inclusion table levels. */
+    std::array<std::array<su2double, 2>, 2> lower_upper_CV1_2 =
+        ComputeNormalizedXY(inclusion_levels, val_CV1, val_CV2, val_CV3);
+    su2double val_CV1_lower = lower_upper_CV1_2[0][0], val_CV2_lower = lower_upper_CV1_2[0][1],
+              val_CV1_upper = lower_upper_CV1_2[1][0], val_CV2_upper = lower_upper_CV1_2[1][1];
+
+    /* 3: Perform 2D interpolations on upper and lower inclusion levels */
     unsigned long lower_level = inclusion_levels.first;
     unsigned long upper_level = inclusion_levels.second;
 
     su2double val_var_lower, val_var_upper;
-    unsigned long exit_code_lower = LookUp_XY(val_name_var, &val_var_lower, val_CV1, val_CV2, lower_level);
-    unsigned long exit_code_upper = LookUp_XY(val_name_var, &val_var_upper, val_CV1, val_CV2, upper_level);
+    unsigned long exit_code_lower = LookUp_XY(val_name_var, &val_var_lower, val_CV1_lower, val_CV2_lower, lower_level);
+    unsigned long exit_code_upper = LookUp_XY(val_name_var, &val_var_upper, val_CV1_upper, val_CV2_upper, upper_level);
 
-    /* 3: Perform linear interpolation along the z-direction using the x-y interpolation results
+    /* 4: Perform linear interpolation along the z-direction using the x-y interpolation results
              from upper and lower trapezoidal maps */
-    Linear_Interpolation(val_z, lower_level, upper_level, val_var_lower, val_var_upper, val_var);
+    Linear_Interpolation(val_CV3, lower_level, upper_level, val_var_lower, val_var_upper, val_var);
 
     return max(exit_code_lower, exit_code_upper);
   } else {
@@ -445,28 +451,34 @@ unsigned long CLookUpTable::LookUp_XYZ(const std::string& val_name_var, su2doubl
   }
 }
 unsigned long CLookUpTable::LookUp_XYZ(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars,
-                                       su2double val_CV1, su2double val_CV2, su2double val_z) {
+                                       su2double val_CV1, su2double val_CV2, su2double val_CV3) {
   /*--- Perform quasi-3D interpolation for a vector of variables with names val_names_var
         on a query point with coordinates val_CV1, val_CV2, and val_z ---*/
 
   /* 1: Find table levels directly above and below the query point (the levels that sandwhich val_z) */
-  std::pair<unsigned long, unsigned long> inclusion_levels = FindInclusionLevels(val_z);
+  std::pair<unsigned long, unsigned long> inclusion_levels = FindInclusionLevels(val_CV3);
   bool within_z_limits = (inclusion_levels.first != inclusion_levels.second);
 
   if (within_z_limits) {
-    /* 2: Perform 2D interpolations on upper and lower inclusion levels */
+    /* 2: Determine val_CV1 and val_CV2 for the inclusion table levels. */
+    std::array<std::array<su2double, 2>, 2> lower_upper_CV1_2 =
+        ComputeNormalizedXY(inclusion_levels, val_CV1, val_CV2, val_CV3);
+    su2double val_CV1_lower = lower_upper_CV1_2[0][0], val_CV2_lower = lower_upper_CV1_2[0][1],
+              val_CV1_upper = lower_upper_CV1_2[1][0], val_CV2_upper = lower_upper_CV1_2[1][1];
+
+    /* 3: Perform 2D interpolations on upper and lower inclusion levels */
     unsigned long lower_level = inclusion_levels.first;
     unsigned long upper_level = inclusion_levels.second;
 
     std::vector<su2double> val_vars_lower, val_vars_upper;
     val_vars_lower.resize(val_vars.size());
     val_vars_upper.resize(val_vars.size());
-    unsigned long exit_code_lower = LookUp_XY(val_names_var, val_vars_lower, val_CV1, val_CV2, lower_level);
-    unsigned long exit_code_upper = LookUp_XY(val_names_var, val_vars_upper, val_CV1, val_CV2, upper_level);
+    unsigned long exit_code_lower = LookUp_XY(val_names_var, val_vars_lower, val_CV1_lower, val_CV2_lower, lower_level);
+    unsigned long exit_code_upper = LookUp_XY(val_names_var, val_vars_upper, val_CV1_upper, val_CV2_upper, upper_level);
 
-    /* 3: Perform linear interpolation along the z-direction using the x-y interpolation results
+    /* 4: Perform linear interpolation along the z-direction using the x-y interpolation results
              from upper and lower trapezoidal maps */
-    Linear_Interpolation(val_z, lower_level, upper_level, val_vars_lower, val_vars_upper, val_vars);
+    Linear_Interpolation(val_CV3, lower_level, upper_level, val_vars_lower, val_vars_upper, val_vars);
 
     return max(exit_code_lower, exit_code_upper);
   } else {
@@ -513,9 +525,54 @@ void CLookUpTable::Linear_Interpolation(const su2double val_z, const unsigned lo
   }
 }
 
-unsigned long CLookUpTable::LookUp_XY(const string& val_name_var, su2double* val_var, su2double val_CV1, su2double val_CV2,
-                                      unsigned long i_level) {
-  unsigned long exit_code = 0;
+std::array<std::array<su2double, 2>, 2> CLookUpTable::ComputeNormalizedXY(
+    std::pair<unsigned long, unsigned long>& inclusion_levels, const su2double val_CV1, const su2double val_CV2,
+    const su2double val_CV3) {
+  /* Determine the values of the controlling variables of the upper and lower table levels corresponding to the
+     normalized query point coordinates. */
+
+  unsigned long lower_level = inclusion_levels.first;
+  unsigned long upper_level = inclusion_levels.second;
+
+  /* Get the upper and lower limits of the first and second controlling variables on the inclusion levels. */
+  su2double x_min_lower = *limits_table_x[lower_level].first, x_max_lower = *limits_table_x[lower_level].second;
+  su2double x_min_upper = *limits_table_x[upper_level].first, x_max_upper = *limits_table_x[upper_level].second;
+  su2double y_min_lower = *limits_table_y[lower_level].first, y_max_lower = *limits_table_y[lower_level].second;
+  su2double y_min_upper = *limits_table_y[upper_level].first, y_max_upper = *limits_table_y[upper_level].second;
+
+  /* Interpolate the table limits to the query point coordinates. */
+  su2double x_min_q = x_min_lower + (x_min_upper - x_min_lower) * (val_CV3 - z_values_levels[lower_level]) /
+                                        (z_values_levels[upper_level] - z_values_levels[lower_level] + EPS);
+  su2double x_max_q = x_max_lower + (x_max_upper - x_max_lower) * (val_CV3 - z_values_levels[lower_level]) /
+                                        (z_values_levels[upper_level] - z_values_levels[lower_level] + EPS);
+  su2double y_min_q = y_min_lower + (y_min_upper - y_min_lower) * (val_CV3 - z_values_levels[lower_level]) /
+                                        (z_values_levels[upper_level] - z_values_levels[lower_level] + EPS);
+  su2double y_max_q = y_max_lower + (y_max_upper - y_max_lower) * (val_CV3 - z_values_levels[lower_level]) /
+                                        (z_values_levels[upper_level] - z_values_levels[lower_level] + EPS);
+
+  /* Compute the normalized first and second controlling variable values. */
+  su2double x_norm_q = (val_CV1 - x_min_q) / (x_max_q - x_min_q);
+  su2double y_norm_q = (val_CV2 - y_min_q) / (y_max_q - y_min_q);
+
+  /* De-normalize the normalized coordinates for the upper and lower table levels. */
+  su2double val_CV1_upper = x_min_upper + (x_max_upper - x_min_upper) * x_norm_q;
+  su2double val_CV2_upper = y_min_upper + (y_max_upper - y_min_upper) * y_norm_q;
+  su2double val_CV1_lower = x_min_lower + (x_max_lower - x_min_lower) * x_norm_q;
+  su2double val_CV2_lower = y_min_lower + (y_max_lower - y_min_lower) * y_norm_q;
+
+  /* Store coordinates in output */
+  std::array<std::array<su2double, 2>, 2> lower_upper_CVs;
+  lower_upper_CVs[0][0] = val_CV1_lower;
+  lower_upper_CVs[0][1] = val_CV2_lower;
+  lower_upper_CVs[1][0] = val_CV1_upper;
+  lower_upper_CVs[1][1] = val_CV2_upper;
+
+  return lower_upper_CVs;
+}
+
+unsigned long CLookUpTable::LookUp_XY(const string& val_name_var, su2double* val_var, su2double val_CV1,
+                                      su2double val_CV2, unsigned long i_level) {
+  unsigned long exit_code = 1;
 
   if (val_name_var.compare("NULL") == 0) {
     *val_var = 0.0;
@@ -540,23 +597,15 @@ unsigned long CLookUpTable::LookUp_XY(const string& val_name_var, su2double* val
 
       *val_var = Interpolate(GetDataP(val_name_var, i_level), triangle, interp_coeffs);
       exit_code = 0;
-    } else {
-      /* in bounding box but outside of table */
-      unsigned long nearest_neighbor = FindNearestNeighborOnHull(val_CV1, val_CV2, i_level);
-      *val_var = GetDataP(val_name_var, i_level)[nearest_neighbor];
-      exit_code = 1;
     }
-  } else {
-    /* lookup is outside of table bounding box */
-    unsigned long nearest_neighbor = FindNearestNeighborOnHull(val_CV1, val_CV2, i_level);
-    *val_var = GetDataP(val_name_var, i_level)[nearest_neighbor];
-    exit_code = 1;
   }
+  if (exit_code == 1) InterpolateToNearestNeighbors(val_CV1, val_CV2, val_name_var, val_var, i_level);
+
   return exit_code;
 }
 
-unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vector<su2double>& val_vars, su2double val_CV1,
-                                      su2double val_CV2, unsigned long i_level) {
+unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vector<su2double>& val_vars,
+                                      su2double val_CV1, su2double val_CV2, unsigned long i_level) {
   vector<su2double*> look_up_data(val_names_var.size());
 
   for (long unsigned int i_var = 0; i_var < val_vars.size(); ++i_var) {
@@ -587,7 +636,7 @@ unsigned long CLookUpTable::LookUp_ProgEnth(const std::vector<std::string>& val_
 
 unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vector<su2double*>& val_vars,
                                       su2double val_CV1, su2double val_CV2, unsigned long i_level) {
-  unsigned long exit_code = 0;
+  unsigned long exit_code = 1;
   unsigned long nearest_neighbor = 0;
   unsigned long id_triangle = 0;
   std::array<su2double, 3> interp_coeffs{0};
@@ -608,32 +657,24 @@ unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vecto
 
       /* exit_code 0 means point was in triangle */
       exit_code = 0;
-
-    } else {
-      /* if point is not inside a triangle (outside table domain) search nearest neighbor */
-      nearest_neighbor = FindNearestNeighborOnHull(val_CV1, val_CV2, i_level);
-      exit_code = 1;
     }
-
-  } else {
-    /* if point is outside of table ranges, find nearest neighbor */
-    nearest_neighbor = FindNearestNeighborOnHull(val_CV1, val_CV2, i_level);
-    exit_code = 1;
   }
 
   /* loop over variable names and interpolate / get values */
-  for (long unsigned int i_var = 0; i_var < val_names_var.size(); ++i_var) {
-    if (val_names_var[i_var].compare("NULL") == 0) {
-      *val_vars[i_var] = 0.0;
-    } else {
-      if (exit_code == 0) {
+  if (exit_code == 0) {
+    for (long unsigned int i_var = 0; i_var < val_names_var.size(); ++i_var) {
+      if (val_names_var[i_var].compare("NULL") == 0) {
+        *val_vars[i_var] = 0.0;
+      } else {
         /* first, copy the single triangle from the large triangle list*/
         for (int p = 0; p < 3; p++) triangle[p] = triangles[i_level][id_triangle][p];
         *val_vars[i_var] = Interpolate(GetDataP(val_names_var[i_var], i_level), triangle, interp_coeffs);
-      } else
-        *val_vars[i_var] = GetDataP(val_names_var[i_var], i_level)[nearest_neighbor];
+      }
     }
+  } else {
+    InterpolateToNearestNeighbors(val_CV1, val_CV2, val_names_var, val_vars, i_level);
   }
+
   return exit_code;
 }
 
@@ -693,6 +734,61 @@ unsigned long CLookUpTable::FindNearestNeighborOnHull(su2double val_CV1, su2doub
   return neighbor_id;
 }
 
+void CLookUpTable::InterpolateToNearestNeighbors(const su2double val_CV1, const su2double val_CV2,
+                                                 const std::vector<std::string>& names_var,
+                                                 std::vector<su2double*>& var_vals, const unsigned long i_level) {
+  /* Interpolate data using distance-weighted averaging on the two nearest table nodes. */
+
+  su2double min_distance = 1e99, second_distance = 1e99;
+  su2double norm_coeff_x = 1. / (*limits_table_x[i_level].second - *limits_table_x[i_level].first);
+  su2double norm_coeff_y = 1. / (*limits_table_y[i_level].second - *limits_table_y[i_level].first);
+  su2double val_CV1_norm = val_CV1 / (*limits_table_x[i_level].second - *limits_table_x[i_level].first);
+  su2double val_CV2_norm = val_CV2 / (*limits_table_y[i_level].second - *limits_table_y[i_level].first);
+
+  const su2double* x_table = GetDataP(name_CV1, i_level);
+  const su2double* y_table = GetDataP(name_CV2, i_level);
+  unsigned long i_nearest = 0, i_second_nearest = 0, i_third_nearest = 0;
+
+  for (unsigned long i_point = 0; i_point < n_hull_points[i_level]; ++i_point) {
+    su2double next_x_norm = x_table[hull[i_level][i_point]] * norm_coeff_x;
+    su2double next_y_norm = y_table[hull[i_level][i_point]] * norm_coeff_y;
+
+    su2double next_distance = pow(val_CV1_norm - next_x_norm, 2) + pow(val_CV2_norm - next_y_norm, 2);
+
+    /* Check if distance to node is lower than current nearest or second nearest node. */
+    if (next_distance < min_distance) {
+      second_distance = min_distance;
+      min_distance = next_distance;
+
+      i_second_nearest = i_nearest;
+      i_nearest = hull[i_level][i_point];
+    } else if ((next_distance > min_distance) && (next_distance < second_distance)) {
+      i_second_nearest = hull[i_level][i_point];
+
+      second_distance = next_distance;
+    }
+  }
+
+  min_distance = sqrt(min_distance);
+  second_distance = sqrt(second_distance);
+
+  /* Interpolate data using distance-weighted averaging */
+  su2double delimiter = (1.0 / min_distance) + (1.0 / second_distance);
+  for (auto iVar = 0u; iVar < var_vals.size(); iVar++) {
+    su2double data_nearest = GetDataP(names_var[iVar], i_level)[i_nearest],
+              data_second_nearest = GetDataP(names_var[iVar], i_level)[i_second_nearest];
+    *var_vals[iVar] = (data_nearest * (1.0 / min_distance) + data_second_nearest * (1.0 / second_distance)) / delimiter;
+  }
+}
+
+void CLookUpTable::InterpolateToNearestNeighbors(const su2double val_CV1, const su2double val_CV2,
+                                                 const std::string& name_var, su2double* var_vals,
+                                                 const unsigned long i_level) {
+  std::vector<std::string> names_var = {name_var};
+  std::vector<su2double*> val_names_var = {var_vals};
+  InterpolateToNearestNeighbors(val_CV1, val_CV2, names_var, val_names_var, i_level);
+}
+
 bool CLookUpTable::IsInTriangle(su2double val_CV1, su2double val_CV2, unsigned long val_id_triangle,
                                 unsigned long i_level) {
   su2double tri_x_0 = GetDataP(name_CV1, i_level)[triangles[i_level][val_id_triangle][0]];

From a1ad56e8861b9cbe667020786ea5f1f8e0a30f1d Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Fri, 20 Jan 2023 20:29:37 -0800
Subject: [PATCH 150/656] restructuring collision cross section

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 SU2_CFD/include/fluid/CSU2TCLib.hpp |  11 +++
 SU2_CFD/src/fluid/CSU2TCLib.cpp     | 108 +++++++++++-----------------
 2 files changed, 51 insertions(+), 68 deletions(-)

diff --git a/SU2_CFD/include/fluid/CSU2TCLib.hpp b/SU2_CFD/include/fluid/CSU2TCLib.hpp
index 5b447ee99ec..f16e649adc6 100644
--- a/SU2_CFD/include/fluid/CSU2TCLib.hpp
+++ b/SU2_CFD/include/fluid/CSU2TCLib.hpp
@@ -276,6 +276,17 @@ class CSU2TCLib : public CNEMOGas {
    *\param[out] Delta_1 or Delta_2 - Collision term between species i and j
    */
   su2double ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies, su2double Mi, su2double Mj, su2double T, bool d1);
+  
+  /*!
+   *\brief Compute the collision cross section
+   *\param[in] iSpecies - Species of gas
+   *\param[in] jSpecies - Collision partner of species i
+   *\param[in] T - Temperature of gas
+   *\param[in] d1 - Whether omega^(1,1) or omega^(2,2)
+   *\param[in] coulomb - Whether to use Coulomb potential
+   *\param[out] Omega_ij - collision cross section
+   */
+  su2double ComputeCollisionCrossSection(unsigned iSpecies, unsigned jSpecies, su2double T, bool d1, bool coulomb);
 
   /*!
    * \brief Get reference temperature.
diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 9a74bd5deb2..191b09a8ef0 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1869,93 +1869,65 @@ void CSU2TCLib::ThermalConductivitiesWBE(){
   ThermalConductivities[1] = ThermalCond_ve;
 }
 
-su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies, su2double Mi, su2double Mj, su2double T, bool d1) {
+su2double CSU2TCLib::ComputeCollisionCrossSection(unsigned iSpecies, unsigned jSpecies, su2double T, bool d1, bool coulomb) {
 
   const su2double pi = PI_NUMBER;
   const su2double Na = AVOGAD_CONSTANT;
+  
+  if (coulomb) {
+    
+    const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
+    const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
+    const su2double ne_cgs = Na * rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
+        
+    const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
+    const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
 
-  su2double Omega_ij;
+    if (Omega11(iSpecies, jSpecies, 0) == 1.0 && d1) {
 
-  if (d1) {
-    /*--- Check whether to use collision cross section data or Coulomb potential ---*/
-    if (Omega11(iSpecies, jSpecies, 0) == 1.0 && ionization) { // attractive potential
-      
-      const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
-      const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
+      return 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);
 
-      const su2double ne_cgs = Na * rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
-        
-      const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
-      const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
-      
-      /*--- Calculate the Omega^(1,1)_ij Coulomb potential ---*/
-      Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);
-
-    } else if (Omega11(iSpecies, jSpecies, 0) == -1.0 && ionization) { // repulsive potential
-
-      const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
-      const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
-      
-      const su2double ne_cgs = Na * rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
-        
-      const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
-      const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
+    } else if (Omega11(iSpecies, jSpecies, 0) == -1.0 && d1) {
+
+      return 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_r*T_star*(1 - C1_r * exp(-c1_r * T_star))+1);
+
+    } else if (Omega22(iSpecies, jSpecies, 0) == 1.0 && !d1) {
 
-      /*--- Calculate the Omega^(1,1)_ij Coulomb potential ---*/
-      Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_r*T_star*(1 - C1_r * exp(-c1_r * T_star))+1);
+      return 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D2_a*T_star*(1 - C2_a * exp(-c2_a * T_star))+1);
 
     } else {
 
-      /*--- Calculate the Omega^(1,1)_ij collision cross section ---*/
-      Omega_ij = 1E-20 * Omega11(iSpecies,jSpecies,3)
-                        * pow(T, Omega11(iSpecies,jSpecies,0)*log(T)*log(T)
-                               + Omega11(iSpecies,jSpecies,1)*log(T)
-                               + Omega11(iSpecies,jSpecies,2));
-    }  
+      return 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D2_r*T_star*(1 - C2_r * exp(-c2_r * T_star))+1);
+    }
+
   } else {
-        /*--- Check whether to use collision cross section data or Coulomb potential ---*/
-    if (Omega22(iSpecies, jSpecies, 0) == 1.0 && ionization) { // attractive potential
-      
-      const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
-      const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
-      
-      const su2double ne_cgs = Na * rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
-        
-      const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
-      const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
-      
-      /*--- Calculate the Omega^(2,2)_ij Coulomb potential ---*/
-      Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D2_a*T_star*(1 - C2_a * exp(-c2_a * T_star))+1);
-
-    } else if (Omega22(iSpecies, jSpecies, 0) == -1.0 && ionization) { // repulsive potential
-
-      const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
-      const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
-      
-      const su2double ne_cgs = Na * rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
-        
-      const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
-      const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
 
-      /*--- Calculate the Omega^(2,2)_ij Coulomb potential ---*/
-      Omega_ij = 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D2_r*T_star*(1 - C2_r * exp(-c2_r * T_star))+1);
+    if (d1) {
+
+      return 1E-20 * Omega11(iSpecies,jSpecies,3) * pow(T, Omega11(iSpecies,jSpecies,0)*log(T)*log(T) + Omega11(iSpecies,jSpecies,1)*log(T) + Omega11(iSpecies,jSpecies,2));
 
     } else {
 
-      /*--- Calculate the Omega^(2,2)_ij collision cross section ---*/
-      Omega_ij = 1E-20 * Omega22(iSpecies,jSpecies,3)
-                        * pow(T, Omega22(iSpecies,jSpecies,0)*log(T)*log(T)
-                               + Omega22(iSpecies,jSpecies,1)*log(T)
-                               + Omega22(iSpecies,jSpecies,2));
-    }  
+      return 1E-20 * Omega22(iSpecies,jSpecies,3) * pow(T, Omega22(iSpecies,jSpecies,0)*log(T)*log(T) + Omega22(iSpecies,jSpecies,1)*log(T) + Omega22(iSpecies,jSpecies,2));
+    }
   }
+}
+
+su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies, su2double Mi, su2double Mj, su2double T, bool d1) {
+
+  bool coulomb = false;
+  if (abs(Omega11(iSpecies, jSpecies, 0)) == 1.0 && ionization) {
+    coulomb = true;
+  } 
+
+  const su2double Omega_ij = ComputeCollisionCrossSection(iSpecies, jSpecies, T, d1, coulomb);
   
+  const su2double pi = PI_NUMBER;
+
   if (d1) {
-    const su2double d_ij = 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij; // d1_ij
-    return d_ij;
+    return 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij; // d1_ij
   } else {
-    const su2double d_ij = 16.0/5.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij; // d2_ij
-    return d_ij;
+    return 16.0/5.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij; // d2_ij
   }
 }
 

From 850d838ed0719fae2e312649a81e3633382a2d45 Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Sun, 22 Jan 2023 16:38:32 -0800
Subject: [PATCH 151/656] add ionization to WBE

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 SU2_CFD/src/fluid/CSU2TCLib.cpp | 22 +++++++---------------
 1 file changed, 7 insertions(+), 15 deletions(-)

diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 191b09a8ef0..d0ee31982c1 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1786,10 +1786,13 @@ void CSU2TCLib::DiffusionCoeffWBE(){
       const su2double Mj = MolarMass[jSpecies]*1E-3;
 
       /*--- Calculate the Omega^(1,1)_ij collision cross section ---*/
-      const su2double Omega_ij = 1E-20/PI_NUMBER * Omega11(iSpecies,jSpecies,3)
-          * pow(T, Omega11(iSpecies,jSpecies,0)*log(T)*log(T)
-          +  Omega11(iSpecies,jSpecies,1)*log(T)
-          +  Omega11(iSpecies,jSpecies,2));
+      bool coulomb = false;
+      if (abs(Omega11(iSpecies, jSpecies, 0)) == 1.0 && ionization) {
+        coulomb = true;
+      } 
+      const su2double T_col = (iSpecies == 0 && ionization) ? Tve : T; 
+
+      const su2double Omega_ij = ComputeCollisionCrossSection(iSpecies, jSpecies, Tcol, true, coulomb) / PI_NUMBER;
       Dij(iSpecies,jSpecies) = 7.1613E-25*M*sqrt(T*(1/Mi+1/Mj))/(Density*Omega_ij);
       Dij(jSpecies,iSpecies) = 7.1613E-25*M*sqrt(T*(1/Mi+1/Mj))/(Density*Omega_ij);
     }
@@ -1884,30 +1887,19 @@ su2double CSU2TCLib::ComputeCollisionCrossSection(unsigned iSpecies, unsigned jS
     const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
 
     if (Omega11(iSpecies, jSpecies, 0) == 1.0 && d1) {
-
       return 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);
-
     } else if (Omega11(iSpecies, jSpecies, 0) == -1.0 && d1) {
-
       return 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_r*T_star*(1 - C1_r * exp(-c1_r * T_star))+1);
-
     } else if (Omega22(iSpecies, jSpecies, 0) == 1.0 && !d1) {
-
       return 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D2_a*T_star*(1 - C2_a * exp(-c2_a * T_star))+1);
-
     } else {
-
       return 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D2_r*T_star*(1 - C2_r * exp(-c2_r * T_star))+1);
     }
 
   } else {
-
     if (d1) {
-
       return 1E-20 * Omega11(iSpecies,jSpecies,3) * pow(T, Omega11(iSpecies,jSpecies,0)*log(T)*log(T) + Omega11(iSpecies,jSpecies,1)*log(T) + Omega11(iSpecies,jSpecies,2));
-
     } else {
-
       return 1E-20 * Omega22(iSpecies,jSpecies,3) * pow(T, Omega22(iSpecies,jSpecies,0)*log(T)*log(T) + Omega22(iSpecies,jSpecies,1)*log(T) + Omega22(iSpecies,jSpecies,2));
     }
   }

From dc0c26cc3bf490eb295f73caad21330ecfd2ef43 Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Sun, 22 Jan 2023 16:51:24 -0800
Subject: [PATCH 152/656] fix var declaration

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 SU2_CFD/src/fluid/CSU2TCLib.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index d0ee31982c1..2d2516b0fbc 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1792,7 +1792,7 @@ void CSU2TCLib::DiffusionCoeffWBE(){
       } 
       const su2double T_col = (iSpecies == 0 && ionization) ? Tve : T; 
 
-      const su2double Omega_ij = ComputeCollisionCrossSection(iSpecies, jSpecies, Tcol, true, coulomb) / PI_NUMBER;
+      const su2double Omega_ij = ComputeCollisionCrossSection(iSpecies, jSpecies, T_col, true, coulomb) / PI_NUMBER;
       Dij(iSpecies,jSpecies) = 7.1613E-25*M*sqrt(T*(1/Mi+1/Mj))/(Density*Omega_ij);
       Dij(jSpecies,iSpecies) = 7.1613E-25*M*sqrt(T*(1/Mi+1/Mj))/(Density*Omega_ij);
     }

From 471fa44173c6bfb89cca2a7938a08642b807b414 Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Sun, 22 Jan 2023 19:17:17 -0800
Subject: [PATCH 153/656] clear segfault on visc ionization

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp | 16 +++++++++-------
 1 file changed, 9 insertions(+), 7 deletions(-)

diff --git a/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp b/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp
index 753ba843c08..7e0f94b6a9b 100644
--- a/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp
+++ b/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp
@@ -228,10 +228,6 @@ void CNEMONumerics::GetViscousProjFlux(const su2double *val_primvar,
                                        su2double val_therm_conductivity_ve,
                                        const CConfig *config) {
 
-  if (ionization) {
-    SU2_MPI::Error("NEED TO IMPLEMENT IONIZED FUNCTIONALITY!!!",CURRENT_FUNCTION);
-  }
-
   // Requires a slightly non-standard primitive vector:
   // Assumes -     V = [Y1, ... , Yn, T, Tve, ... ]
   // and gradient GV = [GY1, ... , GYn, GT, GTve, ... ]
@@ -261,7 +257,7 @@ void CNEMONumerics::GetViscousProjFlux(const su2double *val_primvar,
   /*--- Pre-compute mixture quantities ---*/  //TODO
   su2double Vector[MAXNDIM] = {0.0};
   for (auto iDim = 0; iDim < nDim; iDim++) {
-    for (auto iSpecies = 0; iSpecies < nHeavy; iSpecies++) {
+    for (auto iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
       Vector[iDim] += rho*Ds[iSpecies]*GV[RHOS_INDEX+iSpecies][iDim];
     }
   }
@@ -273,7 +269,7 @@ void CNEMONumerics::GetViscousProjFlux(const su2double *val_primvar,
   for (auto iDim = 0; iDim < nDim; iDim++) {
 
     /*--- Species diffusion velocity ---*/
-    for (auto iSpecies = 0; iSpecies < nHeavy; iSpecies++) {
+    for (auto iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
       Flux_Tensor[iSpecies][iDim] = rho*Ds[iSpecies]*GV[RHOS_INDEX+iSpecies][iDim]
           - V[RHOS_INDEX+iSpecies]*Vector[iDim];
     }
@@ -286,7 +282,7 @@ void CNEMONumerics::GetViscousProjFlux(const su2double *val_primvar,
     }
 
     /*--- Diffusion terms ---*/
-    for (auto iSpecies = 0; iSpecies < nHeavy; iSpecies++) {
+    for (auto iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
       Flux_Tensor[nSpecies+nDim][iDim]   += Flux_Tensor[iSpecies][iDim] * hs[iSpecies];
       Flux_Tensor[nSpecies+nDim+1][iDim] += Flux_Tensor[iSpecies][iDim] * val_eve[iSpecies];
     }
@@ -345,6 +341,12 @@ void CNEMONumerics::GetViscousProjJacs(const su2double *val_Mean_PrimVar,
     case 10:
       return COMPUTE_VISCOUS_JACS(10, 5);
 
+    case 11:
+      return COMPUTE_VISCOUS_JACS(11, 7);
+
+    case 12:
+      return COMPUTE_VISCOUS_JACS(12, 7);
+
     default:
       return COMPUTE_VISCOUS_JACS(DynamicSize,DynamicSize);
 

From 014e2d0abca61ea1123062d336d0a4b2b2fbd104 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 23 Jan 2023 14:11:28 +0100
Subject: [PATCH 154/656] Updated tutorials branch for datadriven NICFD example

---
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp |  1 +
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp     | 14 ++++++++++++++
 SU2_CFD/src/solvers/CEulerSolver.cpp       |  7 +++++--
 3 files changed, 20 insertions(+), 2 deletions(-)

diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index 4589e3a378a..109a5eafb52 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -40,6 +40,7 @@
  */
 class CDataDrivenFluid : public CFluidModel {
  protected:
+  int rank;
   unsigned short Kind_DataDriven_Method = ENUM_DATADRIVEN_METHOD::LUT;  // Interpolation method for data set evaluation
 
   size_t idx_rho,  // Interpolator index for density input
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index f82aa4f518f..de009f57fcc 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -28,14 +28,27 @@
 #include "../../include/fluid/CDataDrivenFluid.hpp"
 
 CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
+  #ifdef HAVE_MPI
+    MPI_Comm_rank(MPI_COMM_WORLD, &rank);
+  #endif
   Kind_DataDriven_Method = config->GetKind_DataDriven_Method();
 
   /*--- Set up interpolation algorithm according to data-driven method. Currently only MLP's are supported. ---*/
   switch (Kind_DataDriven_Method) {
     case ENUM_DATADRIVEN_METHOD::MLP:
+      if (rank == MASTER_NODE) {
+        cout << "***********************************************" << endl;
+        cout << "*** initializing the multi-layer perceptron ***" << endl;
+        cout << "***********************************************" << endl;
+      }
       lookup_mlp = new MLPToolbox::CLookUp_ANN(config->GetNDataDriven_Files(), config->GetDataDriven_FileNames());
       break;
     case ENUM_DATADRIVEN_METHOD::LUT:
+      if (rank == MASTER_NODE) {
+        cout << "*****************************************" << endl;
+        cout << "***   initializing the lookup table   ***" << endl;
+        cout << "*****************************************" << endl;
+      }
       lookup_table = new CLookUpTable(config->GetDataDriven_Filename(), "Density", "Energy");
       break;
     default:
@@ -372,6 +385,7 @@ unsigned long CDataDrivenFluid::Predict_MLP(su2double rho, su2double e) {
 
   /* Apply exponential transformation to the MLP outputs for the first and second
      derivative of the entropy w.r.t density */
+  // Optional:
   // dsdrho_e = -exp(dsdrho_e);
   // d2sdrho2 = exp(d2sdrho2);
 
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index 25809ad882c..ae26ecfff6e 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -791,6 +791,7 @@ void CEulerSolver::SetNondimensionalization(CConfig *config, unsigned short iMes
   bool free_stream_temp   = (config->GetKind_FreeStreamOption() == FREESTREAM_OPTION::TEMPERATURE_FS);
   bool reynolds_init      = (config->GetKind_InitOption() == REYNOLDS);
   bool aeroelastic        = config->GetAeroelastic_Simulation();
+  bool redefine_fluidmodel = true;
 
   /*--- Set temperature via the flutter speed index ---*/
   if (aeroelastic) {
@@ -857,6 +858,8 @@ void CEulerSolver::SetNondimensionalization(CConfig *config, unsigned short iMes
     case DATADRIVEN_FLUID:
 
       auxFluidModel = new CDataDrivenFluid(config);
+      redefine_fluidmodel = false;
+
       break;
     case COOLPROP:
 
@@ -1055,7 +1058,7 @@ void CEulerSolver::SetNondimensionalization(CConfig *config, unsigned short iMes
   /*--- Initialize the dimensionless Fluid Model that will be used to solve the dimensionless problem ---*/
 
   /*--- Auxilary (dimensional) FluidModel no longer needed. ---*/
-  delete auxFluidModel;
+  if(redefine_fluidmodel) delete auxFluidModel;
 
   /*--- Create one final fluid model object per OpenMP thread to be able to use them in parallel.
    *    GetFluidModel() should be used to automatically access the "right" object of each thread. ---*/
@@ -1091,7 +1094,7 @@ void CEulerSolver::SetNondimensionalization(CConfig *config, unsigned short iMes
         break;
 
       case DATADRIVEN_FLUID:
-        FluidModel[thread] = new CDataDrivenFluid(config);
+        FluidModel[thread] = auxFluidModel;
         break;
 
       case COOLPROP:

From 6037de56450f0e7c6d9350c3d5c5265bb0fc0779 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 23 Jan 2023 14:51:03 +0100
Subject: [PATCH 155/656] Fixed build error

---
 Common/src/containers/CLookUpTable.cpp | 3 +--
 1 file changed, 1 insertion(+), 2 deletions(-)

diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index 80d291899a0..acd0216d69c 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -637,7 +637,6 @@ unsigned long CLookUpTable::LookUp_ProgEnth(const std::vector<std::string>& val_
 unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vector<su2double*>& val_vars,
                                       su2double val_CV1, su2double val_CV2, unsigned long i_level) {
   unsigned long exit_code = 1;
-  unsigned long nearest_neighbor = 0;
   unsigned long id_triangle = 0;
   std::array<su2double, 3> interp_coeffs{0};
   std::array<unsigned long, 3> triangle{0};
@@ -747,7 +746,7 @@ void CLookUpTable::InterpolateToNearestNeighbors(const su2double val_CV1, const
 
   const su2double* x_table = GetDataP(name_CV1, i_level);
   const su2double* y_table = GetDataP(name_CV2, i_level);
-  unsigned long i_nearest = 0, i_second_nearest = 0, i_third_nearest = 0;
+  unsigned long i_nearest = 0, i_second_nearest = 0;
 
   for (unsigned long i_point = 0; i_point < n_hull_points[i_level]; ++i_point) {
     su2double next_x_norm = x_table[hull[i_level][i_point]] * norm_coeff_x;

From e90c9490f012eb61391fbe1c913c31b9b6857dee Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 23 Jan 2023 16:17:57 +0100
Subject: [PATCH 156/656] Changed unit test values for LUT

---
 UnitTests/Common/containers/CLookupTable_tests.cpp | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/UnitTests/Common/containers/CLookupTable_tests.cpp b/UnitTests/Common/containers/CLookupTable_tests.cpp
index b91474e33fe..05155fe9988 100644
--- a/UnitTests/Common/containers/CLookupTable_tests.cpp
+++ b/UnitTests/Common/containers/CLookupTable_tests.cpp
@@ -80,7 +80,7 @@ TEST_CASE("LUTreader", "[tabulated chemistry]") {
   enth = 1.1;
   look_up_tag = "Density";
   look_up_table.LookUp_XY(look_up_tag, &look_up_dat, prog, enth); 
-  CHECK(look_up_dat == Approx(1.2));
+  CHECK(look_up_dat == Approx(1.1738796125));
  
 }
 
@@ -131,6 +131,6 @@ TEST_CASE("LUTreader_3D", "[tabulated chemistry]") {
   mfrac = 2.0;
   look_up_tag = "Density";
   look_up_table.LookUp_XYZ(look_up_tag, &look_up_dat, prog, enth, mfrac); 
-  CHECK(look_up_dat == Approx(1.2));
+  CHECK(look_up_dat == Approx(1.1738796125));
  
 }
\ No newline at end of file

From 1040b7fa7452d0d52f7a7be66da31343e6c86c0b Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Tue, 24 Jan 2023 08:22:43 -0500
Subject: [PATCH 157/656] small comment changes

---
 SU2_CFD/src/fluid/CSU2TCLib.cpp | 15 ++++++++++-----
 1 file changed, 10 insertions(+), 5 deletions(-)

diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 2d2516b0fbc..d0dfb12cfe2 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1759,7 +1759,7 @@ void CSU2TCLib::DiffusionCoeffWBE(){
   su2double conc = 0.0;
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
     MolarFracWBE[iSpecies] = rhos[iSpecies]/MolarMass[iSpecies];
-    conc               += MolarFracWBE[iSpecies];
+    conc += MolarFracWBE[iSpecies];
   }
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
     MolarFracWBE[iSpecies] = MolarFracWBE[iSpecies]/conc;
@@ -1786,13 +1786,18 @@ void CSU2TCLib::DiffusionCoeffWBE(){
       const su2double Mj = MolarMass[jSpecies]*1E-3;
 
       /*--- Calculate the Omega^(1,1)_ij collision cross section ---*/
+
+      /*--- If collisions between electrons/ion, used Coloumb potentials ---*/
       bool coulomb = false;
-      if (abs(Omega11(iSpecies, jSpecies, 0)) == 1.0 && ionization) {
-        coulomb = true;
-      } 
+      if (abs(Omega11(iSpecies, jSpecies, 0)) == 1.0 && ionization) coulomb = true;
+
+      // Used Tve for electron collisions
       const su2double T_col = (iSpecies == 0 && ionization) ? Tve : T; 
 
+      /*--- Compute the collisional cross section (omega_ij) ---*/
       const su2double Omega_ij = ComputeCollisionCrossSection(iSpecies, jSpecies, T_col, true, coulomb) / PI_NUMBER;
+
+      /*--- Calculate and populate diffusion coefficients ---*/
       Dij(iSpecies,jSpecies) = 7.1613E-25*M*sqrt(T*(1/Mi+1/Mj))/(Density*Omega_ij);
       Dij(jSpecies,iSpecies) = 7.1613E-25*M*sqrt(T*(1/Mi+1/Mj))/(Density*Omega_ij);
     }
@@ -1819,7 +1824,7 @@ void CSU2TCLib::ViscosityWBE(){
   su2double conc = 0.0;
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
     MolarFracWBE[iSpecies] = rhos[iSpecies]/MolarMass[iSpecies];
-    conc               += MolarFracWBE[iSpecies];
+    conc += MolarFracWBE[iSpecies];
   }
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
     MolarFracWBE[iSpecies] = MolarFracWBE[iSpecies]/conc;

From 0f6c7d7847e0aca0a8c697aebbc9b0232a28feef Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Tue, 24 Jan 2023 09:08:59 -0500
Subject: [PATCH 158/656] preparing updated regressions tests

---
 .github/workflows/regression.yml              |  2 +-
 .../visc_cylinder/visc_ion_gy.cfg             | 74 ++++++++++++++++++
 .../visc_cylinder/visc_ion_wbe.cfg            | 75 +++++++++++++++++++
 .../{viscous => visc_wedge}/axi_visccone.cfg  |  0
 .../{viscous => visc_wedge}/partial_cat.cfg   |  0
 .../{viscous => visc_wedge}/super_cat.cfg     |  0
 TestCases/parallel_regression.py              | 30 +++++++-
 7 files changed, 177 insertions(+), 4 deletions(-)
 create mode 100644 TestCases/nonequilibrium/visc_cylinder/visc_ion_gy.cfg
 create mode 100644 TestCases/nonequilibrium/visc_cylinder/visc_ion_wbe.cfg
 rename TestCases/nonequilibrium/{viscous => visc_wedge}/axi_visccone.cfg (100%)
 rename TestCases/nonequilibrium/{viscous => visc_wedge}/partial_cat.cfg (100%)
 rename TestCases/nonequilibrium/{viscous => visc_wedge}/super_cat.cfg (100%)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index e749e661e70..c614f3f8f32 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c feature_NEMO_visc_ion -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
         with:
diff --git a/TestCases/nonequilibrium/visc_cylinder/visc_ion_gy.cfg b/TestCases/nonequilibrium/visc_cylinder/visc_ion_gy.cfg
new file mode 100644
index 00000000000..92ed1186935
--- /dev/null
+++ b/TestCases/nonequilibrium/visc_cylinder/visc_ion_gy.cfg
@@ -0,0 +1,74 @@
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+%                                                                              %
+% SU2 configuration file                                                       %
+% Case description: Mach 15 viscous, ionized flow over a cylinder              %
+%                   using the Gupta-Yos transport model.                       %
+%                                                                              %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
+SOLVER= NEMO_NAVIER_STOKES
+MATH_PROBLEM= DIRECT
+RESTART_SOL= YES
+AXISYMMETRIC= YES
+
+% ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
+%
+MACH_NUMBER=15
+AOA= 0.0
+SIDESLIP_ANGLE= 0.0
+FREESTREAM_PRESSURE= 21.96
+FREESTREAM_TEMPERATURE= 246.87
+FREESTREAM_TEMPERATURE_VE= 246.87
+INIT_OPTION=TD_CONDITIONS
+
+% ---- NONEQUILIBRIUM GAS, IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
+%
+FLUID_MODEL= SU2_NONEQ
+GAS_MODEL= AIR-7
+GAS_COMPOSITION= (5E-13, 0.767, 0.23, 0.001, 0.001, 0.000999999999, 5E-13)
+TRANSPORT_COEFF_MODEL= GUPTA-YOS
+
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
+MARKER_ISOTHERMAL=(wall, 300.0)
+MARKER_FAR= (far, exit)
+MARKER_SYM= (symm)
+MARKER_PLOTTING= (wall)
+MARKER_MONITORING= (wall)
+
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
+CFL_NUMBER= 3.0
+ITER= 11
+LINEAR_SOLVER= BCGSTAB
+LINEAR_SOLVER_ERROR= 1E-6
+LINEAR_SOLVER_ITER= 5
+
+% -----------------------------------------------------------------------%
+%
+CONV_NUM_METHOD_FLOW= AUSM
+MUSCL_FLOW= YES
+SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
+VENKAT_LIMITER_COEFF= 0.05
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
+CONV_RESIDUAL_MINVAL= -10
+CONV_STARTITER= 10
+
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+%
+MESH_FILENAME= visc_cyl.su2
+MESH_FORMAT= SU2
+SOLUTION_FILENAME= restart_flow_gy.dat 
+RESTART_FILENAME= restart_flow_gy.dat 
+TABULAR_FORMAT= TECPLOT
+CONV_FILENAME= convergence
+VOLUME_FILENAME= soln_volume
+SURFACE_FILENAME= soln_surface     
+OUTPUT_WRT_FREQ= 2500
+SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY_0, RMS_DENSITY_1, RMS_DENSITY_2, RMS_DENSITY_3, RMS_DENSITY_4, RMS_DENSITY_5, RMS_DENSITY_6, RMS_ENERGY, RMS_ENERGY_VE, LIFT, 
\ No newline at end of file
diff --git a/TestCases/nonequilibrium/visc_cylinder/visc_ion_wbe.cfg b/TestCases/nonequilibrium/visc_cylinder/visc_ion_wbe.cfg
new file mode 100644
index 00000000000..16a1fabd44a
--- /dev/null
+++ b/TestCases/nonequilibrium/visc_cylinder/visc_ion_wbe.cfg
@@ -0,0 +1,75 @@
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+%                                                                              %
+% SU2 configuration file                                                       %
+% Case description: Mach 15 viscous, ionized flow over a cylinder              %
+%                   using the Wilkes-Blottner-Eucken transport model.          %
+%                                                                              %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
+SOLVER= NEMO_NAVIER_STOKES
+MATH_PROBLEM= DIRECT
+RESTART_SOL= YES
+AXISYMMETRIC= YES
+
+% ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
+%
+MACH_NUMBER=15
+AOA= 0.0
+SIDESLIP_ANGLE= 0.0
+FREESTREAM_PRESSURE= 21.96
+FREESTREAM_TEMPERATURE= 246.87
+FREESTREAM_TEMPERATURE_VE= 246.87
+INIT_OPTION=TD_CONDITIONS
+
+% ---- NONEQUILIBRIUM GAS, IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
+%
+FLUID_MODEL= SU2_NONEQ
+GAS_MODEL= AIR-7
+GAS_COMPOSITION= (5E-13, 0.767, 0.23, 0.001, 0.001, 0.000999999999, 5E-13)
+TRANSPORT_COEFF_MODEL= WILKE
+
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
+MARKER_ISOTHERMAL=(wall, 300.0)
+MARKER_FAR= (far, exit)
+MARKER_SYM= (symm)
+MARKER_PLOTTING= (wall)
+MARKER_MONITORING= (wall)
+
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
+CFL_NUMBER= 3.0
+ITER= 11
+LINEAR_SOLVER= BCGSTAB
+LINEAR_SOLVER_ERROR= 1E-6
+LINEAR_SOLVER_ITER= 5
+
+% -----------------------------------------------------------------------%
+%
+CONV_NUM_METHOD_FLOW= AUSM
+MUSCL_FLOW= YES
+SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
+VENKAT_LIMITER_COEFF= 0.05
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
+CONV_RESIDUAL_MINVAL= -10
+CONV_STARTITER= 10
+
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+%
+MESH_FILENAME= visc_cyl.su2
+MESH_FORMAT= SU2
+SOLUTION_FILENAME= restart_flow_wbe.dat 
+RESTART_FILENAME= restart_flow_wbe.dat 
+TABULAR_FORMAT= TECPLOT
+CONV_FILENAME= convergence
+VOLUME_FILENAME= soln_volume
+SURFACE_FILENAME= soln_surface     
+OUTPUT_WRT_FREQ= 2500
+SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY_0, RMS_DENSITY_1, RMS_DENSITY_2, RMS_DENSITY_3, RMS_DENSITY_4, RMS_DENSITY_5, RMS_DENSITY_6, RMS_ENERGY, RMS_ENERGY_VE, LIFT, DRAG, TOTAL_HEATFLUX)
+OUTPUT_FILES= (RESTART_ASCII, PARAVIEW_ASCII)
\ No newline at end of file
diff --git a/TestCases/nonequilibrium/viscous/axi_visccone.cfg b/TestCases/nonequilibrium/visc_wedge/axi_visccone.cfg
similarity index 100%
rename from TestCases/nonequilibrium/viscous/axi_visccone.cfg
rename to TestCases/nonequilibrium/visc_wedge/axi_visccone.cfg
diff --git a/TestCases/nonequilibrium/viscous/partial_cat.cfg b/TestCases/nonequilibrium/visc_wedge/partial_cat.cfg
similarity index 100%
rename from TestCases/nonequilibrium/viscous/partial_cat.cfg
rename to TestCases/nonequilibrium/visc_wedge/partial_cat.cfg
diff --git a/TestCases/nonequilibrium/viscous/super_cat.cfg b/TestCases/nonequilibrium/visc_wedge/super_cat.cfg
similarity index 100%
rename from TestCases/nonequilibrium/viscous/super_cat.cfg
rename to TestCases/nonequilibrium/visc_wedge/super_cat.cfg
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index a72454dd5c9..b685b5e9c6c 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -132,7 +132,7 @@ def main():
 
     # Viscous single cone - axisymmetric
     visc_cone           = TestCase('visc_cone')
-    visc_cone.cfg_dir   = "nonequilibrium/viscous"
+    visc_cone.cfg_dir   = "nonequilibrium/visc_wedge"
     visc_cone.cfg_file  = "axi_visccone.cfg"
     visc_cone.test_iter = 10
     visc_cone.test_vals         = [-5.222278, -5.746529, -20.569425, -20.633787, -20.547644, 1.255759, -3.208374, -0.016010, 0.093459, 32633.000000]
@@ -151,7 +151,7 @@ def main():
 
     # Viscous single wedge - super catalytic walls
     super_cat           = TestCase('super_cat')
-    super_cat.cfg_dir   = "nonequilibrium/viscous"
+    super_cat.cfg_dir   = "nonequilibrium/visc_wedge"
     super_cat.cfg_file  = "super_cat.cfg"
     super_cat.test_iter = 10
     super_cat.test_vals = [-5.232590, -5.757884, -20.727046, -20.748136, -20.564044, 1.246889, -3.205235, -0.028406, 0.250857, 3.2459e+04]
@@ -163,7 +163,7 @@ def main():
 
     # Viscous single wedge - partially catalytic walls
     partial_cat           = TestCase('partial_cat')
-    partial_cat.cfg_dir   = "nonequilibrium/viscous"
+    partial_cat.cfg_dir   = "nonequilibrium/visc_wedge"
     partial_cat.cfg_file  = "partial_cat.cfg"
     partial_cat.test_iter = 10
     partial_cat.test_vals = [-5.210300, -5.735063, -20.880374, -20.825890, -23.475263, 1.806281, -2.813924, -0.078469, 0.496017, 2.9021e+04]
@@ -173,6 +173,30 @@ def main():
     partial_cat.tol       = 0.00001
     test_list.append(partial_cat)
 
+    # Viscous cylinder, ionization, Wilkes-Blottner-Eucken
+    partial_ion_wbe = TestCase('ion_wbe')
+    partial_ion_wbe.cfg_dir = "nonequilibrium/visc_cylinder"
+    partial_ion_wbe.cfg_file = "cyl_ion_wbe.cfg"
+    partial_ion_wbe.test_iter = 10
+    partial_ion_wbe.test_vals = [-5.210300, -5.735063, -20.880374, -20.825890, -23.475263, 1.806281, -2.813924, -0.078469, 0.496017, 2.9021e+04]
+    partial_ion_wbe.su2_exec = "mpirun -n 2 SU2_CFD"
+    partial_ion_wbe.timeout = 1600
+    partial_ion_wbe.new_output = True
+    partial_ion_wbe.tol = 0.00001
+    test_list.append(partial_ion_wbe)
+
+    # Viscous cylinder, ionization, Gupta-Yos
+    partial_ion_gy = TestCase('ion_gy')
+    partial_ion_gy.cfg_dir = "nonequilibrium/visc_cylinder"
+    partial_ion_gy.cfg_file = "cyl_ion_gy.cfg"
+    partial_ion_gy.test_iter = 10
+    partial_ion_gy.test_vals = [-5.210300, -5.735063, -20.880374, -20.825890, -23.475263, 1.806281, -2.813924, -0.078469, 0.496017, 2.9021e+04]
+    partial_ion_gy.su2_exec = "mpirun -n 2 SU2_CFD"
+    partial_ion_gy.timeout = 1600
+    partial_ion_gy.new_output = True
+    partial_ion_gy.tol = 0.00001
+    test_list.append(partial_ion_gy)
+
     ##########################
     ### Compressible Euler ###
     ##########################

From 30831d60317ce780455f28c775f8aa706a270d78 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Wed, 25 Jan 2023 13:25:59 +0100
Subject: [PATCH 159/656] Fixed bug in computation of secondary flow variables

---
 .github/workflows/regression.yml       | 2 +-
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp | 6 +++---
 2 files changed, 4 insertions(+), 4 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 003525f926c..a887c290179 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c feature_multilayer_perceptron -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t feature_multilayer_perceptron -c feature_multilayer_perceptron -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
         with:
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index de009f57fcc..8b50d60e5ae 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -137,10 +137,10 @@ void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
 
   /*--- Compute secondary flow variables ---*/
   dTde_rho = -pow(dsde_rho, -2) * d2sde2;
-  dTdrho_e = 0.0;
+  dTdrho_e = -pow(dsde_rho, -2) * d2sdedrho;
 
-  dPde_rho = -pow(rho, 2) * dTde_rho * dsdrho_e;
-  dPdrho_e = -2 * rho * Temperature * dsdrho_e - pow(rho, 2) * Temperature * d2sdrho2;
+  dPde_rho = -pow(rho, 2) * (dTde_rho * dsdrho_e + Temperature * d2sdedrho);
+  dPdrho_e = -2 * rho * Temperature * dsdrho_e - pow(rho, 2) * (dTdrho_e * dsdrho_e + Temperature * d2sdrho2);
 }
 
 void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {

From 2de9889ccaf6318eb2318f469e6cda26b688f9d4 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Wed, 25 Jan 2023 16:47:47 +0100
Subject: [PATCH 160/656] Reduced tolerances in Newton solvers to reduce
 solution variations at boundaries

---
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp | 26 +++++++++++++-------------
 1 file changed, 13 insertions(+), 13 deletions(-)

diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 8b50d60e5ae..e789de73460 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -147,8 +147,8 @@ void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
   /*--- Setting initial values for density and energy ---*/
   su2double rho = rho_start, e = e_start;
 
-  su2double tolerance_P = 0.1,  // Tolerance percentage for pressure solution
-      tolerance_T = 0.1;        // Tolerance percentage for temperature solution
+  su2double tolerance_P = 0.01,  // Tolerance percentage for pressure solution
+      tolerance_T = 0.01;        // Tolerance percentage for temperature solution
 
   bool converged = false;        // Convergence flag
   unsigned long iter_max = 500,  // Maximum number of iterations
@@ -168,7 +168,7 @@ void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
     delta_P = Pressure - P;
     delta_T = Temperature - T;
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if ((100 * abs(delta_P) / P < tolerance_P) && (100 * abs(delta_T) / T < tolerance_T)) {
+    if ((100 * abs(delta_P / P) < tolerance_P) && (100 * abs(delta_T / T) < tolerance_T)) {
       converged = true;
     } else {
       /*--- Compute step size for density and energy ---*/
@@ -202,7 +202,7 @@ void CDataDrivenFluid::SetEnergy_Prho(su2double P, su2double rho) {
   /*--- Setting initial values for energy ---*/
   su2double e = e_start;
 
-  su2double tolerance_P = 0.1;  // Tolerance percentage for pressure solution
+  su2double tolerance_P = 0.01;  // Tolerance percentage for pressure solution
 
   bool converged = false;        // Convergence flag
   unsigned long iter_max = 500,  // Maximum number of iterations
@@ -220,7 +220,7 @@ void CDataDrivenFluid::SetEnergy_Prho(su2double P, su2double rho) {
 
     su2double partial_diff = abs(delta_P) / P;
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if ((100 * partial_diff < tolerance_P)) {
+    if (100 * abs(delta_P / P) < tolerance_P) {
       converged = true;
     } else {
       /*--- Compute step size for energy ---*/
@@ -242,7 +242,7 @@ void CDataDrivenFluid::SetTDState_rhoT(su2double rho, su2double T) {
   /*--- Setting initial values for density and energy ---*/
   su2double e = e_start;
 
-  su2double tolerance_T = 0.1;  // Tolerance for temperature solution
+  su2double tolerance_T = 0.01;  // Tolerance for temperature solution
 
   bool converged = false;        // Convergence flag
   unsigned long iter_max = 500,  // Maximum number of iterations
@@ -260,7 +260,7 @@ void CDataDrivenFluid::SetTDState_rhoT(su2double rho, su2double T) {
     delta_T = Temperature - T;
 
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if (100 * abs(delta_T) / T < tolerance_T) {
+    if (100 * abs(delta_T / T) < tolerance_T) {
       converged = true;
     } else {
       delta_e = delta_T / dTde_rho;
@@ -281,8 +281,8 @@ void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
   /*--- Setting initial values for density and energy ---*/
   su2double rho = rho_start, e = e_start;
 
-  su2double tolerance_h = 0.1,  // Tolerance for enthalpy solution
-      tolerance_s = 0.1;        // Tolerance for entropy solution
+  su2double tolerance_h = 0.01,  // Tolerance for enthalpy solution
+      tolerance_s = 0.01;        // Tolerance for entropy solution
 
   bool converged = false;        // Convergence flag
   unsigned long iter_max = 500,  // Maximum number of iterations
@@ -305,7 +305,7 @@ void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
     delta_s = Entropy - s;
 
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if ((100 * abs(delta_h) / h < tolerance_h) && (100 * abs(delta_s) / s < tolerance_s)) {
+    if ((100 * abs(delta_h / h) < tolerance_h) && (100 * abs(delta_s / s) < tolerance_s)) {
       converged = true;
     } else {
       su2double dh_de = 1 + dPde_rho / rho;
@@ -331,8 +331,8 @@ void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
   /*--- Setting initial values for density and energy ---*/
   su2double rho = rho_start, e = e_start;
 
-  su2double tolerance_P = 0.1,  // Tolerance for pressure solution
-      tolerance_s = 0.1;        // Tolerance for entropy solution
+  su2double tolerance_P = 0.01,  // Tolerance for pressure solution
+      tolerance_s = 0.01;        // Tolerance for entropy solution
 
   bool converged = false;        // Convergence flag
   unsigned long iter_max = 500,  // Maximum number of iterations
@@ -354,7 +354,7 @@ void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
     delta_s = Entropy - s;
 
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if ((100 * abs(delta_P) / P < tolerance_P) && (100 * abs(delta_s) / s < tolerance_s)) {
+    if ((100 * abs(delta_P / P) < tolerance_P) && (100 * abs(delta_s / s) < tolerance_s)) {
       converged = true;
     } else {
       /*--- Compute step size for density and energy ---*/

From 1eb3a6eb30dd78f63483e43ee8da6245720b2275 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 27 Jan 2023 08:13:01 +0100
Subject: [PATCH 161/656] Reduced tolerances in datadriven fluid model for
 better convergence at boundaries

---
 .../multilayer_perceptron/CNeuralNetwork.hpp  |  3 +-
 .../multilayer_perceptron/CNeuralNetwork.cpp  | 17 ++++++
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        | 58 ++++++++++++++-----
 SU2_CFD/src/solvers/CEulerSolver.cpp          |  5 +-
 4 files changed, 67 insertions(+), 16 deletions(-)

diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
index b55cf07f7b7..42ad0bcf2c7 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
@@ -72,7 +72,8 @@ class CNeuralNetwork {
     SELU = 5,
     SIGMOID = 6,
     SWISH = 7,
-    TANH = 8
+    TANH = 8,
+    EXPONENTIAL = 9
   };
   ENUM_ACTIVATION_FUNCTION* activation_function_types;
 
diff --git a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
index 954562a7f0b..13f96878c06 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
@@ -102,6 +102,19 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double>& inputs, bool comp
             }
           }
           break;
+        case ENUM_ACTIVATION_FUNCTION::EXPONENTIAL:
+          for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
+            x = total_layers[iLayer]->getInput(iNeuron);
+            y = exp(x);
+            total_layers[iLayer]->setOutput(iNeuron, y);
+            if (compute_gradient) {
+              dy_dx = 1.0;
+              for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
+                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+              }
+            }
+          }
+          break;
         case ENUM_ACTIVATION_FUNCTION::RELU:
           for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
             x = total_layers[iLayer]->getInput(iNeuron);
@@ -320,6 +333,10 @@ void MLPToolbox::CNeuralNetwork::setActivationFunction(unsigned long i_layer, st
     activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::NONE;
     return;
   }
+  if (input.compare("exponential") == 0) {
+    activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::EXPONENTIAL;
+    return;
+  }
   SU2_MPI::Error("Unknown activation function type: " + input, CURRENT_FUNCTION);
   return;
 }
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index e789de73460..92ffc702914 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -64,6 +64,38 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
   /*--- Set initial values for density and energy based on config options ---*/
   rho_start = config->GetDensity_Init_DataDriven();
   e_start = config->GetEnergy_Init_DataDriven();
+
+  unsigned short n_streamlines = 30;
+  for(auto i_streamline=0u; i_streamline<n_streamlines+1; i_streamline++){
+    string filenamepath = "/home/evert/NICFD/Architecture_Optimization/Hyperparameter_Search/CoolProp_Streamline_"+to_string(i_streamline) + "_data.csv";
+    ifstream file;
+    file.open(filenamepath);
+    string word, line;
+    getline(file, line);
+    ofstream streamline_file;
+    streamline_file.open("SU2_Streamline_"+to_string(i_streamline)+"_data.csv");
+
+    streamline_file << "Density,Energy,Entropy,dsde,dsdrho,d2sde2,d2sdedrho,d2sdrho2,P,T,SoS,dPde,dPdrho,dTde,dTdrho" <<endl;
+    unsigned long n_steps = stoul(line);
+    for(auto j=0u; j<n_steps; j++){
+      getline(file, line);
+      stringstream str(line);
+      str >> word;
+      su2double density = stold(word);
+      str >> word;
+      su2double energy = stold(word);
+      SetTDState_rhoe(density, energy);
+      streamline_file << density << ", " << energy << ", " << Entropy << ", " << dsde_rho << ", " << dsdrho_e << ", " << d2sde2 << ", " << d2sdedrho << ", " << d2sdrho2 << ", " 
+      << Pressure << ", "
+      << Temperature << ", "
+      << sqrt(SoundSpeed2) << ", "
+      << dPde_rho << ", "
+      << dPdrho_e << ", "
+      << dTde_rho << ", "
+      << dTdrho_e << endl; 
+    }
+    streamline_file.close();
+  }
 }
 
 CDataDrivenFluid::~CDataDrivenFluid() {
@@ -147,8 +179,8 @@ void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
   /*--- Setting initial values for density and energy ---*/
   su2double rho = rho_start, e = e_start;
 
-  su2double tolerance_P = 0.01,  // Tolerance percentage for pressure solution
-      tolerance_T = 0.01;        // Tolerance percentage for temperature solution
+  su2double tolerance_P = 1e-6,  // Tolerance percentage for pressure solution
+      tolerance_T = 1e-6;        // Tolerance percentage for temperature solution
 
   bool converged = false;        // Convergence flag
   unsigned long iter_max = 500,  // Maximum number of iterations
@@ -168,7 +200,7 @@ void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
     delta_P = Pressure - P;
     delta_T = Temperature - T;
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if ((100 * abs(delta_P / P) < tolerance_P) && (100 * abs(delta_T / T) < tolerance_T)) {
+    if ((abs(delta_P / P) < tolerance_P) && (abs(delta_T / T) < tolerance_T)) {
       converged = true;
     } else {
       /*--- Compute step size for density and energy ---*/
@@ -202,7 +234,7 @@ void CDataDrivenFluid::SetEnergy_Prho(su2double P, su2double rho) {
   /*--- Setting initial values for energy ---*/
   su2double e = e_start;
 
-  su2double tolerance_P = 0.01;  // Tolerance percentage for pressure solution
+  su2double tolerance_P = 1e-6;  // Tolerance percentage for pressure solution
 
   bool converged = false;        // Convergence flag
   unsigned long iter_max = 500,  // Maximum number of iterations
@@ -220,7 +252,7 @@ void CDataDrivenFluid::SetEnergy_Prho(su2double P, su2double rho) {
 
     su2double partial_diff = abs(delta_P) / P;
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if (100 * abs(delta_P / P) < tolerance_P) {
+    if (abs(delta_P / P) < tolerance_P) {
       converged = true;
     } else {
       /*--- Compute step size for energy ---*/
@@ -242,7 +274,7 @@ void CDataDrivenFluid::SetTDState_rhoT(su2double rho, su2double T) {
   /*--- Setting initial values for density and energy ---*/
   su2double e = e_start;
 
-  su2double tolerance_T = 0.01;  // Tolerance for temperature solution
+  su2double tolerance_T = 1e-6;  // Tolerance for temperature solution
 
   bool converged = false;        // Convergence flag
   unsigned long iter_max = 500,  // Maximum number of iterations
@@ -260,7 +292,7 @@ void CDataDrivenFluid::SetTDState_rhoT(su2double rho, su2double T) {
     delta_T = Temperature - T;
 
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if (100 * abs(delta_T / T) < tolerance_T) {
+    if (abs(delta_T / T) < tolerance_T) {
       converged = true;
     } else {
       delta_e = delta_T / dTde_rho;
@@ -281,8 +313,8 @@ void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
   /*--- Setting initial values for density and energy ---*/
   su2double rho = rho_start, e = e_start;
 
-  su2double tolerance_h = 0.01,  // Tolerance for enthalpy solution
-      tolerance_s = 0.01;        // Tolerance for entropy solution
+  su2double tolerance_h = 1e-6,  // Tolerance for enthalpy solution
+      tolerance_s = 1e-6;        // Tolerance for entropy solution
 
   bool converged = false;        // Convergence flag
   unsigned long iter_max = 500,  // Maximum number of iterations
@@ -305,7 +337,7 @@ void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
     delta_s = Entropy - s;
 
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if ((100 * abs(delta_h / h) < tolerance_h) && (100 * abs(delta_s / s) < tolerance_s)) {
+    if ((abs(delta_h / h) < tolerance_h) && (abs(delta_s / s) < tolerance_s)) {
       converged = true;
     } else {
       su2double dh_de = 1 + dPde_rho / rho;
@@ -331,8 +363,8 @@ void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
   /*--- Setting initial values for density and energy ---*/
   su2double rho = rho_start, e = e_start;
 
-  su2double tolerance_P = 0.01,  // Tolerance for pressure solution
-      tolerance_s = 0.01;        // Tolerance for entropy solution
+  su2double tolerance_P = 1e-6,  // Tolerance for pressure solution
+      tolerance_s = 1e-6;        // Tolerance for entropy solution
 
   bool converged = false;        // Convergence flag
   unsigned long iter_max = 500,  // Maximum number of iterations
@@ -354,7 +386,7 @@ void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
     delta_s = Entropy - s;
 
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if ((100 * abs(delta_P / P) < tolerance_P) && (100 * abs(delta_s / s) < tolerance_s)) {
+    if ((abs(delta_P / P) < tolerance_P) && (abs(delta_s / s) < tolerance_s)) {
       converged = true;
     } else {
       /*--- Compute step size for density and energy ---*/
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index ae26ecfff6e..16ac1fb6a32 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -4688,8 +4688,9 @@ void CEulerSolver::BC_Riemann(CGeometry *geometry, CSolver **solver_container,
       GetFluidModel()->SetTDState_rhoe(Density_i, StaticEnergy_i);
 
       /*--- Set initial values for density and energy for Newton solvers in fluid model ---*/
-      GetFluidModel()->SetDensity(0.5*(Density_i + config->GetDensity_Init_DataDriven()));
-      GetFluidModel()->SetEnergy(0.5*(StaticEnergy_i + config->GetEnergy_Init_DataDriven()));
+      su2double relax_Newton = config->GetRelaxation_DataDriven();
+      GetFluidModel()->SetDensity(relax_Newton*Density_i + (1 - relax_Newton)*config->GetDensity_Init_DataDriven());
+      GetFluidModel()->SetEnergy(relax_Newton*StaticEnergy_i + (1 - relax_Newton)*config->GetEnergy_Init_DataDriven());
 
       Pressure_i = GetFluidModel()->GetPressure();
       Enthalpy_i = Energy_i + Pressure_i/Density_i;

From 5fac4f4f5260926537015722098fbf5bc3f473b4 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 27 Jan 2023 09:19:02 +0100
Subject: [PATCH 162/656] Fixed build errors

---
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp    |  13 ++-
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        | 101 +++++-------------
 .../nicf/datadriven/datadriven_nozzle.cfg     |   4 +-
 3 files changed, 36 insertions(+), 82 deletions(-)

diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index 109a5eafb52..dac2c963c7a 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -48,13 +48,16 @@ class CDataDrivenFluid : public CFluidModel {
 
   su2double Newton_Relaxation,  // Relaxation factor for Newton solvers.
       rho_start,                // Initial value for the density in Newton solver processes.
-      e_start;                  // Initial value for the energy in Newton solver processes.
+      e_start,                  // Initial value for the energy in Newton solver processes.
+      Newton_Tolerance;         // Normalized tolerance for Newton solvers.
 
-  su2double dsde_rho, dsdrho_e, d2sde2, d2sdedrho, d2sdrho2;
+  unsigned long MaxIter_Newton;  // Maximum number of iterations for Newton solvers
 
-  su2double Gamma{0.0};           /*!< \brief Ratio of Specific Heats. */
-  su2double Gamma_Minus_One{0.0}; /*!< \brief Ratio of Specific Heats Minus One. */
-  su2double Gas_Constant{0.0};    /*!< \brief Gas Constant. */
+  su2double dsde_rho, /*!< \brief Entropy derivative w.r.t. density */
+      dsdrho_e,       /*!< \brief Entropy derivative w.r.t. static energy */
+      d2sde2,         /*!< \brief Entropy second derivative w.r.t. static energy */
+      d2sdedrho,      /*!< \brief Entropy second derivative w.r.t. density and static energy */
+      d2sdrho2;       /*!< \brief Entropy second derivative w.r.t. static density */
 
   su2vector<string>
       input_names_rhoe,   // Data-driven method input variable names of the independent variables (density, energy).
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 92ffc702914..8a9797c275e 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -28,9 +28,9 @@
 #include "../../include/fluid/CDataDrivenFluid.hpp"
 
 CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
-  #ifdef HAVE_MPI
-    MPI_Comm_rank(MPI_COMM_WORLD, &rank);
-  #endif
+#ifdef HAVE_MPI
+  MPI_Comm_rank(MPI_COMM_WORLD, &rank);
+#endif
   Kind_DataDriven_Method = config->GetKind_DataDriven_Method();
 
   /*--- Set up interpolation algorithm according to data-driven method. Currently only MLP's are supported. ---*/
@@ -55,8 +55,10 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
       break;
   }
 
-  /*--- Relaxation factor for Newton solvers. ---*/
+  /*--- Relaxation factor and tolerance for Newton solvers. ---*/
   Newton_Relaxation = config->GetRelaxation_DataDriven();
+  Newton_Tolerance = 1e-8;
+  MaxIter_Newton = 500;
 
   /*--- Preprocessing of inputs and outputs for the interpolation method. ---*/
   MapInputs_to_Outputs();
@@ -64,38 +66,6 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
   /*--- Set initial values for density and energy based on config options ---*/
   rho_start = config->GetDensity_Init_DataDriven();
   e_start = config->GetEnergy_Init_DataDriven();
-
-  unsigned short n_streamlines = 30;
-  for(auto i_streamline=0u; i_streamline<n_streamlines+1; i_streamline++){
-    string filenamepath = "/home/evert/NICFD/Architecture_Optimization/Hyperparameter_Search/CoolProp_Streamline_"+to_string(i_streamline) + "_data.csv";
-    ifstream file;
-    file.open(filenamepath);
-    string word, line;
-    getline(file, line);
-    ofstream streamline_file;
-    streamline_file.open("SU2_Streamline_"+to_string(i_streamline)+"_data.csv");
-
-    streamline_file << "Density,Energy,Entropy,dsde,dsdrho,d2sde2,d2sdedrho,d2sdrho2,P,T,SoS,dPde,dPdrho,dTde,dTdrho" <<endl;
-    unsigned long n_steps = stoul(line);
-    for(auto j=0u; j<n_steps; j++){
-      getline(file, line);
-      stringstream str(line);
-      str >> word;
-      su2double density = stold(word);
-      str >> word;
-      su2double energy = stold(word);
-      SetTDState_rhoe(density, energy);
-      streamline_file << density << ", " << energy << ", " << Entropy << ", " << dsde_rho << ", " << dsdrho_e << ", " << d2sde2 << ", " << d2sdedrho << ", " << d2sdrho2 << ", " 
-      << Pressure << ", "
-      << Temperature << ", "
-      << sqrt(SoundSpeed2) << ", "
-      << dPde_rho << ", "
-      << dPdrho_e << ", "
-      << dTde_rho << ", "
-      << dTdrho_e << endl; 
-    }
-    streamline_file.close();
-  }
 }
 
 CDataDrivenFluid::~CDataDrivenFluid() {
@@ -179,12 +149,8 @@ void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
   /*--- Setting initial values for density and energy ---*/
   su2double rho = rho_start, e = e_start;
 
-  su2double tolerance_P = 1e-6,  // Tolerance percentage for pressure solution
-      tolerance_T = 1e-6;        // Tolerance percentage for temperature solution
-
-  bool converged = false;        // Convergence flag
-  unsigned long iter_max = 500,  // Maximum number of iterations
-      Iter = 0;
+  bool converged = false;  // Convergence flag
+  unsigned long Iter = 0;
 
   su2double delta_P,  // Pressure residual
       delta_T,        // Temperature residual
@@ -192,7 +158,7 @@ void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
       delta_e,        // Energy step size
       determinant;    // Jacobian determinant
   /*--- Initiating Newton solver ---*/
-  while (!converged && (Iter < iter_max)) {
+  while (!converged && (Iter < MaxIter_Newton)) {
     /*--- Determine thermodynamic state based on current density and energy*/
     SetTDState_rhoe(rho, e);
 
@@ -200,7 +166,7 @@ void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
     delta_P = Pressure - P;
     delta_T = Temperature - T;
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if ((abs(delta_P / P) < tolerance_P) && (abs(delta_T / T) < tolerance_T)) {
+    if ((abs(delta_P / P) < Newton_Tolerance) && (abs(delta_T / T) < Newton_Tolerance)) {
       converged = true;
     } else {
       /*--- Compute step size for density and energy ---*/
@@ -234,25 +200,21 @@ void CDataDrivenFluid::SetEnergy_Prho(su2double P, su2double rho) {
   /*--- Setting initial values for energy ---*/
   su2double e = e_start;
 
-  su2double tolerance_P = 1e-6;  // Tolerance percentage for pressure solution
-
-  bool converged = false;        // Convergence flag
-  unsigned long iter_max = 500,  // Maximum number of iterations
-      Iter = 0;
+  bool converged = false;  // Convergence flag
+  unsigned long Iter = 0;
 
   su2double delta_P,  // Pressure residual
       delta_e;        // Energy step size
 
-  while (!converged && (Iter < iter_max)) {
+  while (!converged && (Iter < MaxIter_Newton)) {
     /*--- Determine thermodynamic state based on current density and energy*/
     SetTDState_rhoe(rho, e);
 
     /*--- Determine pressure and temperature residuals ---*/
     delta_P = Pressure - P;
 
-    su2double partial_diff = abs(delta_P) / P;
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if (abs(delta_P / P) < tolerance_P) {
+    if (abs(delta_P / P) < Newton_Tolerance) {
       converged = true;
     } else {
       /*--- Compute step size for energy ---*/
@@ -274,17 +236,14 @@ void CDataDrivenFluid::SetTDState_rhoT(su2double rho, su2double T) {
   /*--- Setting initial values for density and energy ---*/
   su2double e = e_start;
 
-  su2double tolerance_T = 1e-6;  // Tolerance for temperature solution
-
-  bool converged = false;        // Convergence flag
-  unsigned long iter_max = 500,  // Maximum number of iterations
-      Iter = 0;
+  bool converged = false;  // Convergence flag
+  unsigned long Iter = 0;
 
   su2double delta_T,  // Temperature residual
       delta_e;        // Energy increment
 
   /*--- Initiating Newton solver ---*/
-  while (!converged && (Iter < iter_max)) {
+  while (!converged && (Iter < MaxIter_Newton)) {
     /*--- Determine thermodynamic state based on current density and energy*/
     SetTDState_rhoe(rho, e);
 
@@ -292,7 +251,7 @@ void CDataDrivenFluid::SetTDState_rhoT(su2double rho, su2double T) {
     delta_T = Temperature - T;
 
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if (abs(delta_T / T) < tolerance_T) {
+    if (abs(delta_T / T) < Newton_Tolerance) {
       converged = true;
     } else {
       delta_e = delta_T / dTde_rho;
@@ -313,12 +272,8 @@ void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
   /*--- Setting initial values for density and energy ---*/
   su2double rho = rho_start, e = e_start;
 
-  su2double tolerance_h = 1e-6,  // Tolerance for enthalpy solution
-      tolerance_s = 1e-6;        // Tolerance for entropy solution
-
-  bool converged = false;        // Convergence flag
-  unsigned long iter_max = 500,  // Maximum number of iterations
-      Iter = 0;
+  bool converged = false;  // Convergence flag
+  unsigned long Iter = 0;
 
   su2double delta_h,  // Enthalpy
       delta_s,        // Entropy residual
@@ -327,7 +282,7 @@ void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
       determinant;    // Jacobian determinant
 
   /*--- Initiating Newton solver ---*/
-  while (!converged && (Iter < iter_max)) {
+  while (!converged && (Iter < MaxIter_Newton)) {
     /*--- Determine thermodynamic state based on current density and energy*/
     SetTDState_rhoe(rho, e);
 
@@ -337,7 +292,7 @@ void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
     delta_s = Entropy - s;
 
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if ((abs(delta_h / h) < tolerance_h) && (abs(delta_s / s) < tolerance_s)) {
+    if ((abs(delta_h / h) < Newton_Tolerance) && (abs(delta_s / s) < Newton_Tolerance)) {
       converged = true;
     } else {
       su2double dh_de = 1 + dPde_rho / rho;
@@ -363,12 +318,8 @@ void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
   /*--- Setting initial values for density and energy ---*/
   su2double rho = rho_start, e = e_start;
 
-  su2double tolerance_P = 1e-6,  // Tolerance for pressure solution
-      tolerance_s = 1e-6;        // Tolerance for entropy solution
-
-  bool converged = false;        // Convergence flag
-  unsigned long iter_max = 500,  // Maximum number of iterations
-      Iter = 0;
+  bool converged = false;  // Convergence flag
+  unsigned long Iter = 0;
 
   su2double delta_P,  // Enthalpy
       delta_s,        // Entropy residual
@@ -377,7 +328,7 @@ void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
       determinant;    // Jacobian determinant
 
   /*--- Initiating Newton solver ---*/
-  while (!converged && (Iter < iter_max)) {
+  while (!converged && (Iter < MaxIter_Newton)) {
     /*--- Determine thermodynamic state based on current density and energy*/
     SetTDState_rhoe(rho, e);
 
@@ -386,7 +337,7 @@ void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
     delta_s = Entropy - s;
 
     /*--- Continue iterative process if residuals are outside tolerances ---*/
-    if ((abs(delta_P / P) < tolerance_P) && (abs(delta_s / s) < tolerance_s)) {
+    if ((abs(delta_P / P) < Newton_Tolerance) && (abs(delta_s / s) < Newton_Tolerance)) {
       converged = true;
     } else {
       /*--- Compute step size for density and energy ---*/
diff --git a/TestCases/nicf/datadriven/datadriven_nozzle.cfg b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
index e49a886c11e..e86d180f469 100644
--- a/TestCases/nicf/datadriven/datadriven_nozzle.cfg
+++ b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
@@ -38,7 +38,7 @@ REF_DIMENSIONALIZATION= DIMENSIONAL
 FLUID_MODEL = DATADRIVEN_FLUID
 INTERPOLATION_METHOD = MLP 
 FILENAMES_INTERPOLATOR = (MLP_air.mlp)
-DATADRIVEN_NEWTON_RELAXATION = 0.06
+DATADRIVEN_NEWTON_RELAXATION = 0.95
 DATADRIVEN_FLUID_INITIAL_DENSITY = 5.54548
 DATADRIVEN_FLUID_INITIAL_ENERGY = 1.8e+05
 
@@ -53,7 +53,7 @@ THERMAL_CONDUCTIVITY_CONSTANT= 0.030542828
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 MARKER_HEATFLUX= ( WALL, 0.0 )
 MARKER_SYM= ( SYMMETRY )
-MARKER_RIEMANN= ( INFLOW, TOTAL_CONDITIONS_PT,  250000.0, 400, 1.0, 0.0, 0.0, OUTFLOW, STATIC_PRESSURE, 200000.0, 0.0, 0.0, 0.0, 0.0 )
+MARKER_RIEMANN= ( INFLOW, TOTAL_CONDITIONS_PT,  904388, 542.13, 1.0, 0.0, 0.0, OUTFLOW, STATIC_PRESSURE, 200000.0, 0.0, 0.0, 0.0, 0.0 )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 NUM_METHOD_GRAD= GREEN_GAUSS

From ad2f0d7ee432fae6c5820e22bf13e02bca739f33 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 27 Jan 2023 10:22:59 +0100
Subject: [PATCH 163/656] Updated regression test values

---
 TestCases/parallel_regression.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 69bfba8ab34..933ba5f14a4 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -994,7 +994,7 @@ def main():
     datadriven_MLP.cfg_dir   = "nicf/datadriven"
     datadriven_MLP.cfg_file  = "datadriven_nozzle.cfg"
     datadriven_MLP.test_iter = 100
-    datadriven_MLP.test_vals = [-4.716703, -2.781021, 2.476446, 0.000000, 0.000000]
+    datadriven_MLP.test_vals = [-4.159241, 0.073280, 3.627716, 0.000000, 0.000000]
     test_list.append(datadriven_MLP)
 
     ######################################

From b4aec623322f2dbc4d4d2a1e0ff0169cb831f46f Mon Sep 17 00:00:00 2001
From: jtneedels <jneedels@stanford.edu>
Date: Fri, 27 Jan 2023 19:46:44 -0500
Subject: [PATCH 164/656] fix to R computation, divide by Ms

Signed-off-by: jtneedels <jneedels@stanford.edu>
---
 SU2_CFD/src/fluid/CSU2TCLib.cpp | 23 +++++++++++++++--------
 1 file changed, 15 insertions(+), 8 deletions(-)

diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 2d2516b0fbc..4a7b2bca13d 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1953,7 +1953,7 @@ void CSU2TCLib::DiffusionCoeffGY(){
         const su2double T_col = (iSpecies == 0 && ionization) ? Tve : T; 
 
         const su2double d1_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T_col, true);
-        const su2double D_ij = kb*T/(Pressure*d1_ij);
+        const su2double D_ij = kb*T_col/(Pressure*d1_ij);
         denom += gam_j/D_ij;
       }
     }
@@ -2005,7 +2005,7 @@ void CSU2TCLib::ThermalConductivitiesGY(){
   /*--- Calculate mixture gas constant ---*/
   su2double R = 0.0;
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
-    R += Ru * rhos[iSpecies]/Density;
+    R += Ru / MolarMass[iSpecies] * rhos[iSpecies]/Density;
   }
 
   /*--- Mixture thermal conductivity via Gupta-Yos approximation ---*/
@@ -2019,6 +2019,7 @@ void CSU2TCLib::ThermalConductivitiesGY(){
     const su2double gam_i   = rhos[iSpecies] / (Density*Mi);
     su2double denom_t = 0.0;
     su2double denom_r = 0.0;
+    su2double denom_re = 0.0;
 
     for (jSpecies = 0; jSpecies < nSpecies; jSpecies++) {
       const su2double Mj    = MolarMass[jSpecies];
@@ -2026,23 +2027,30 @@ void CSU2TCLib::ThermalConductivitiesGY(){
       const su2double gam_j = rhos[iSpecies] / (Density*Mj);
       const su2double a_ij = 1.0 + (1.0 - mi/mj)*(0.45 - 2.54*mi/mj) / ((1.0 + mi/mj)*(1.0 + mi/mj));
 
-      const su2double T_col = (iSpecies == 0 && ionization) ? Tve : T; 
+      const su2double T_col = ((iSpecies == 0 && ionization) || (jSpecies == 0 && ionization)) ? Tve : T; 
 
       const su2double d1_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T_col, true);
       const su2double d2_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T_col, false);
-    
-      denom_t += a_ij*gam_j*d2_ij;
+      
+      if (jSpecies == 0 && ionization) {
+        denom_t += 3.54*gam_j*d2_ij;
+      } else {
+        denom_t += a_ij*gam_j*d2_ij;
+      }
       denom_r += gam_j*d1_ij;
+      denom_re += gam_j*d2_ij;
     }
 
     /*--- Translational contribution to thermal conductivity ---*/
-    ThermalCond_tr += ((15.0/4.0)*kb*gam_i/denom_t);
+    if (!(ionization && iSpecies == 0)) ThermalCond_tr += ((15.0/4.0)*kb*gam_i/denom_t);
 
     /*--- Rotational contribution to thermal conductivity ---*/
     if (RotationModes[iSpecies] != 0.0) ThermalCond_tr += (kb*gam_i/denom_r);
 
     /*--- Vibrational-electronic contribution to thermal conductivity ---*/
-    ThermalCond_ve += (kb*Cvve/R*gam_i / denom_r);
+    if (!(ionization && iSpecies == 0) && RotationModes[iSpecies] != 0.0) ThermalCond_ve += (kb*Cvve/R*gam_i / denom_r);
+    
+    if (ionization && iSpecies == 0) ThermalCond_ve += ((15.0/4.0)*kb*gam_i/(1.45*denom_re));
   }
 
   ThermalConductivities[0] = ThermalCond_tr;
@@ -2168,7 +2176,6 @@ vector<su2double>& CSU2TCLib::ComputeTemperatures(vector<su2double>& val_rhos, s
   // If absolutely no convergence, then assign to the TR temperature
   if (!NRconvg && !Bconvg ) {
     Tve = T;
-    cout <<"Warning: temperatures did not converge, error= "<< fabs(rhoEve_t-rhoEve)<<endl;
   }
 
   temperatures[0] = T;

From 3088378be6c6ca596edfbcc44b2ca3272ee9319f Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 30 Jan 2023 09:28:01 +0100
Subject: [PATCH 165/656] Replaced 'x,y,z' with 'cv1,cv2,cv3' where it applies
 in the CLookUpTable class

---
 Common/include/containers/CLookUpTable.hpp | 26 ++++++++--------
 Common/src/containers/CLookUpTable.cpp     | 36 +++++++++++-----------
 2 files changed, 31 insertions(+), 31 deletions(-)

diff --git a/Common/include/containers/CLookUpTable.hpp b/Common/include/containers/CLookUpTable.hpp
index db658ba871e..a42770a06e3 100644
--- a/Common/include/containers/CLookUpTable.hpp
+++ b/Common/include/containers/CLookUpTable.hpp
@@ -153,12 +153,12 @@ class CLookUpTable {
 
   /*!
    * \brief compute the inverse matrix for interpolation.
-   * \param[in] vec_x - pointer to first coordinate (progress variable).
-   * \param[in] vec_y - pointer to second coordinate (enthalpy).
+   * \param[in] vec_CV1 - pointer to first coordinate (progress variable).
+   * \param[in] vec_CV2 - pointer to second coordinate (enthalpy).
    * \param[in] point_ids - single triangle data.
    * \param[out] interp_mat_inv - inverse matrix for interpolation.
    */
-  void GetInterpMatInv(const su2double* vec_x, const su2double* vec_y, std::array<unsigned long, 3>& point_ids,
+  void GetInterpMatInv(const su2double* vec_CV1, const su2double* vec_CV2, std::array<unsigned long, 3>& point_ids,
                        su2activematrix& interp_mat_inv);
 
   /*!
@@ -183,26 +183,26 @@ class CLookUpTable {
 
   /*!
    * \brief Perform linear interpolation between two table levels for a single variable.
-   * \param[in] val_z - z-coordinate of the query point.
+   * \param[in] val_CV3 - value of the third controlling variable at the query point.
    * \param[in] lower_level - Table level index of the table level directly below the query point.
    * \param[in] upper_level - Table level index of the table level directly above the query point.
    * \param[in] lower_value - Result from x-y interpolation on the lower table level.
    * \param[in] upper_value - Result from x-y interpolation on the upper table level.
    * \param[in] val_vars - Pointer to interpolation result.
    */
-  void Linear_Interpolation(const su2double val_z, const unsigned long lower_level, const unsigned long upper_level,
+  void Linear_Interpolation(const su2double val_CV3, const unsigned long lower_level, const unsigned long upper_level,
                             su2double& lower_value, su2double& upper_value, su2double*& var_vals) const;
 
   /*!
    * \brief Perform linear interpolation between two table levels for a vector of variables.
-   * \param[in] val_z - z-coordinate of the query point.
+   * \param[in] val_CV3 - value of the third controlling variable at the query point.
    * \param[in] lower_level - Table level index of the table level directly below the query point.
    * \param[in] upper_level - Table level index of the table level directly above the query point.
    * \param[in] lower_values - Results from x-y interpolation on the lower table level.
    * \param[in] upper_values - Results from x-y interpolation on the upper table level.
    * \param[in] val_vars - Pointer to interpolation results for all interpolation variables.
    */
-  void Linear_Interpolation(const su2double val_z, const unsigned long lower_level, const unsigned long upper_level,
+  void Linear_Interpolation(const su2double val_CV3, const unsigned long lower_level, const unsigned long upper_level,
                             std::vector<su2double>& lower_values, std::vector<su2double>& upper_values,
                             std::vector<su2double*>& var_vals) const;
 
@@ -357,11 +357,11 @@ class CLookUpTable {
    * \param[out] val_var - the stored value of the variable to look up.
    * \param[in] val_CV1 - value of controlling variable 1.
    * \param[in] val_CV2 - value of controlling variable 2.
-   * \param[in] val_z - value of controlling variable 3.
+   * \param[in] val_CV3 - value of controlling variable 3.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
   unsigned long LookUp_XYZ(const std::string& val_name_var, su2double* val_var, su2double val_CV1, su2double val_CV2,
-                           su2double val_z);
+                           su2double val_CV3);
 
   /*!
    * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_CV1,val_CV2,val_z).
@@ -369,19 +369,19 @@ class CLookUpTable {
    * \param[out] val_var - the stored value of the variable to look up.
    * \param[in] val_CV1 - value of controlling variable 1.
    * \param[in] val_CV2 - value of controlling variable 2.
-   * \param[in] val_z - value of controlling variable 3.
+   * \param[in] val_CV3 - value of controlling variable 3.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
   unsigned long LookUp_XYZ(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars,
-                           su2double val_CV1, su2double val_CV2, su2double val_z = 0);
+                           su2double val_CV1, su2double val_CV2, su2double val_CV3 = 0);
 
   /*!
    * \brief Find the table levels with constant z-values directly above and below query val_z.
-   * \param[in] val_z - Z-coordinate of query point.
+   * \param[in] val_CV3 - value of controlling variable 3.
    * \param[in] within_limits - Whether query point lies within table bounds.
    * \returns pair of inclusion level indices (first = lower level index, second = upper level index)
    */
-  std::pair<unsigned long, unsigned long> FindInclusionLevels(const su2double val_z);
+  std::pair<unsigned long, unsigned long> FindInclusionLevels(const su2double val_CV3);
 
   /*!
    * \brief determine the minimum and maximum value of the second controlling variable.
diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index acd0216d69c..ff5052f6e7e 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -394,19 +394,19 @@ void CLookUpTable::GetInterpMatInv(const su2double* vec_x, const su2double* vec_
   }
 }
 
-std::pair<unsigned long, unsigned long> CLookUpTable::FindInclusionLevels(const su2double val_z) {
-  /*--- Find the table levels with constant z-values directly below and above the query value val_z ---*/
+std::pair<unsigned long, unsigned long> CLookUpTable::FindInclusionLevels(const su2double val_CV3) {
+  /*--- Find the table levels with constant z-values directly below and above the query value val_CV3 ---*/
 
-  /* Check if val_z lies outside table bounds */
-  if (val_z >= *limits_table_z.second) {
+  /* Check if val_CV3 lies outside table bounds */
+  if (val_CV3 >= *limits_table_z.second) {
     return std::make_pair(n_table_levels - 1, n_table_levels - 1);
-  } else if (val_z <= *limits_table_z.first) {
+  } else if (val_CV3 <= *limits_table_z.first) {
     return std::make_pair(0, 0);
   } else {
     std::pair<unsigned long, unsigned long> inclusion_levels;
     /* Loop over table levels to find the levels directly above and below the query value */
     for (auto i_level = 0ul; i_level < n_table_levels - 1; i_level++) {
-      if ((val_z >= z_values_levels[i_level]) && (val_z < z_values_levels[i_level + 1])) {
+      if ((val_CV3 >= z_values_levels[i_level]) && (val_CV3 < z_values_levels[i_level + 1])) {
         inclusion_levels = std::make_pair(i_level, i_level + 1);
       }
     }
@@ -417,9 +417,9 @@ std::pair<unsigned long, unsigned long> CLookUpTable::FindInclusionLevels(const
 unsigned long CLookUpTable::LookUp_XYZ(const std::string& val_name_var, su2double* val_var, su2double val_CV1,
                                        su2double val_CV2, su2double val_CV3) {
   /*--- Perform quasi-3D interpolation for a single variable named val_name_var on a query point
-        with coordinates val_CV1, val_CV2, and val_z ---*/
+        with coordinates val_CV1, val_CV2, and val_CV3 ---*/
 
-  /* 1: Find table levels directly above and below the query point (the levels that sandwhich val_z) */
+  /* 1: Find table levels directly above and below the query point (the levels that sandwhich val_CV3) */
   std::pair<unsigned long, unsigned long> inclusion_levels = FindInclusionLevels(val_CV3);
   bool within_z_limits = (inclusion_levels.first != inclusion_levels.second);
 
@@ -444,7 +444,7 @@ unsigned long CLookUpTable::LookUp_XYZ(const std::string& val_name_var, su2doubl
 
     return max(exit_code_lower, exit_code_upper);
   } else {
-    /* Perform single, 2D interpolation when val_z lies outside table bounds */
+    /* Perform single, 2D interpolation when val_CV3 lies outside table bounds */
     unsigned long bound_level = inclusion_levels.first;
     LookUp_XY(val_name_var, val_var, val_CV1, val_CV2, bound_level);
     return 1;
@@ -453,9 +453,9 @@ unsigned long CLookUpTable::LookUp_XYZ(const std::string& val_name_var, su2doubl
 unsigned long CLookUpTable::LookUp_XYZ(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars,
                                        su2double val_CV1, su2double val_CV2, su2double val_CV3) {
   /*--- Perform quasi-3D interpolation for a vector of variables with names val_names_var
-        on a query point with coordinates val_CV1, val_CV2, and val_z ---*/
+        on a query point with coordinates val_CV1, val_CV2, and val_CV3 ---*/
 
-  /* 1: Find table levels directly above and below the query point (the levels that sandwhich val_z) */
+  /* 1: Find table levels directly above and below the query point (the levels that sandwhich val_CV3) */
   std::pair<unsigned long, unsigned long> inclusion_levels = FindInclusionLevels(val_CV3);
   bool within_z_limits = (inclusion_levels.first != inclusion_levels.second);
 
@@ -482,14 +482,14 @@ unsigned long CLookUpTable::LookUp_XYZ(const std::vector<std::string>& val_names
 
     return max(exit_code_lower, exit_code_upper);
   } else {
-    /* Perform single, 2D interpolation when val_z lies outside table bounds */
+    /* Perform single, 2D interpolation when val_CV3 lies outside table bounds */
     unsigned long bound_level = inclusion_levels.first;
     LookUp_XY(val_names_var, val_vars, val_CV1, val_CV2, bound_level);
     return 1;
   }
 }
 
-void CLookUpTable::Linear_Interpolation(const su2double val_z, const unsigned long lower_level,
+void CLookUpTable::Linear_Interpolation(const su2double val_CV3, const unsigned long lower_level,
                                         const unsigned long upper_level, su2double& lower_value, su2double& upper_value,
                                         su2double*& var_val) const {
   /* Perform linear interpolation along the z-direction of the table for a single variable */
@@ -499,14 +499,14 @@ void CLookUpTable::Linear_Interpolation(const su2double val_z, const unsigned lo
   su2double val_z_upper = z_values_levels[upper_level];
 
   /* Compute linear interpolation coefficients */
-  su2double factor_upper = (val_z - val_z_lower) / (val_z_upper - val_z_lower);
-  su2double factor_lower = (val_z_upper - val_z) / (val_z_upper - val_z_lower);
+  su2double factor_upper = (val_CV3 - val_z_lower) / (val_z_upper - val_z_lower);
+  su2double factor_lower = (val_z_upper - val_CV3) / (val_z_upper - val_z_lower);
 
   /* Perform linear interpolation */
   *var_val = lower_value * factor_lower + upper_value * factor_upper;
 }
 
-void CLookUpTable::Linear_Interpolation(const su2double val_z, const unsigned long lower_level,
+void CLookUpTable::Linear_Interpolation(const su2double val_CV3, const unsigned long lower_level,
                                         const unsigned long upper_level, std::vector<su2double>& lower_values,
                                         std::vector<su2double>& upper_values, std::vector<su2double*>& var_vals) const {
   /* Perform linear interpolation along the z-direction of the table for multiple variables */
@@ -516,8 +516,8 @@ void CLookUpTable::Linear_Interpolation(const su2double val_z, const unsigned lo
   su2double val_z_upper = z_values_levels[upper_level];
 
   /* Compute linear interpolation coefficients */
-  su2double factor_upper = (val_z - val_z_lower) / (val_z_upper - val_z_lower);
-  su2double factor_lower = (val_z_upper - val_z) / (val_z_upper - val_z_lower);
+  su2double factor_upper = (val_CV3 - val_z_lower) / (val_z_upper - val_z_lower);
+  su2double factor_lower = (val_z_upper - val_CV3) / (val_z_upper - val_z_lower);
 
   /* Perform linear interpolation */
   for (size_t iVar = 0; iVar < var_vals.size(); iVar++) {

From a05081f584846d38a18374560e9e58ab77f1cc87 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Tue, 31 Jan 2023 13:07:07 +0100
Subject: [PATCH 166/656] Changes for OpenMP builds.

---
 Common/include/code_config.hpp                   | 2 +-
 Common/include/parallelization/omp_structure.cpp | 2 +-
 Common/include/parallelization/omp_structure.hpp | 1 -
 meson.build                                      | 2 ++
 4 files changed, 4 insertions(+), 3 deletions(-)

diff --git a/Common/include/code_config.hpp b/Common/include/code_config.hpp
index 699afba0d2e..434e103a83e 100644
--- a/Common/include/code_config.hpp
+++ b/Common/include/code_config.hpp
@@ -90,7 +90,7 @@ FORCEINLINE Out su2staticcast_p(In ptr) {
 #include "codi/tools/data/externalFunctionUserData.hpp"
 
 #if defined(HAVE_OMP)
-using su2double = codi::RealReverseIndexParallel;
+using su2double = codi::RealReverseIndexOpenMP;
 #else
 #if defined(CODI_INDEX_TAPE)
 using su2double = codi::RealReverseIndex;
diff --git a/Common/include/parallelization/omp_structure.cpp b/Common/include/parallelization/omp_structure.cpp
index 75e29de26d6..36ada05b75d 100644
--- a/Common/include/parallelization/omp_structure.cpp
+++ b/Common/include/parallelization/omp_structure.cpp
@@ -36,7 +36,7 @@ void omp_initialize() {
 #endif
   opdi::logic = new opdi::OmpLogic;
   opdi::logic->init();
-  opdi::tool = new CoDiOpDiTool<su2double>;
+  opdi::tool = new CoDiOpDiLibTool<su2double>;
   opdi::tool->init();
 #endif
 }
diff --git a/Common/include/parallelization/omp_structure.hpp b/Common/include/parallelization/omp_structure.hpp
index d6a161ab684..6f94b22a2a9 100644
--- a/Common/include/parallelization/omp_structure.hpp
+++ b/Common/include/parallelization/omp_structure.hpp
@@ -57,7 +57,6 @@
 #else
 #include "opdi/backend/macro/macroBackend.hpp"
 #endif
-#include "codi/externals/codiOpdiTool.hpp"
 #include "opdi.hpp"
 #endif
 
diff --git a/meson.build b/meson.build
index 883383a7741..f7337fc2752 100644
--- a/meson.build
+++ b/meson.build
@@ -136,6 +136,8 @@ if omp
   # add opdi dependency
   if get_option('enable-autodiff')
     codi_dep += declare_dependency(include_directories: 'externals/opdi/include')
+    codi_rev_args += '-DCODI_EnableOpenMP'
+    codi_rev_args += '-DCODI_EnableOpDiLib'
 
     if get_option('opdi-backend') == 'macro'
       su2_cpp_args += '-DFORCE_OPDI_MACRO_BACKEND'

From e8125bf09367b843681391435fa693b4502f228d Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Tue, 31 Jan 2023 13:07:44 +0100
Subject: [PATCH 167/656] CoDiPack update.

---
 externals/codi        | 2 +-
 meson_scripts/init.py | 2 +-
 2 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/externals/codi b/externals/codi
index a282326f226..fd58ba98a93 160000
--- a/externals/codi
+++ b/externals/codi
@@ -1 +1 @@
-Subproject commit a282326f22612b46e2324ba9e4e5439a55ae157a
+Subproject commit fd58ba98a937778eed69d539c9cc9235ab38358c
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 0eed30f5283..47492bfbf18 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -44,7 +44,7 @@ def init_submodules(method = 'auto'):
 
   # This information of the modules is used if projects was not cloned using git
   # The sha tag must be maintained manually to point to the correct commit
-  sha_version_codi = 'a282326f22612b46e2324ba9e4e5439a55ae157a'
+  sha_version_codi = 'fd58ba98a937778eed69d539c9cc9235ab38358c'
   github_repo_codi = 'https://github.com/scicompkl/CoDiPack'
   sha_version_medi = '6aef76912e7099c4f08c9705848797ca9e8070da'
   github_repo_medi = 'https://github.com/SciCompKL/MeDiPack'

From e9e9bda4d65351d59c6faf74e61456a8c721d72f Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Tue, 31 Jan 2023 19:10:31 +0100
Subject: [PATCH 168/656] Use OpenMPExternalFunctionHelper for omp builds.

---
 Common/include/basic_types/ad_structure.hpp | 4 ++++
 1 file changed, 4 insertions(+)

diff --git a/Common/include/basic_types/ad_structure.hpp b/Common/include/basic_types/ad_structure.hpp
index 5aa40292727..223ee5fb73b 100644
--- a/Common/include/basic_types/ad_structure.hpp
+++ b/Common/include/basic_types/ad_structure.hpp
@@ -294,7 +294,11 @@ namespace AD{
 
   using Tape = su2double::Tape;
 
+#ifdef HAVE_OPDI
+  using ExtFuncHelper = codi::OpenMPExternalFunctionHelper<su2double>;
+#else
   using ExtFuncHelper = codi::ExternalFunctionHelper<su2double>;
+#endif
 
   extern ExtFuncHelper FuncHelper;
 

From b8d83a000ce04296ce6635d4b6cd993b769e3ab7 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Wed, 1 Feb 2023 15:05:17 +0100
Subject: [PATCH 169/656] Added function to neural network class displaying
 information on the loaded architectures

---
 .../multilayer_perceptron/CNeuralNetwork.hpp  |  8 +--
 .../multilayer_perceptron/CLookUp_ANN.cpp     |  9 ++-
 .../multilayer_perceptron/CNeuralNetwork.cpp  | 66 +++++++++++++++++--
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        | 10 ---
 4 files changed, 74 insertions(+), 19 deletions(-)

diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
index 42ad0bcf2c7..42b900783ef 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
@@ -75,8 +75,8 @@ class CNeuralNetwork {
     TANH = 8,
     EXPONENTIAL = 9
   };
-  ENUM_ACTIVATION_FUNCTION* activation_function_types;
-
+  su2vector<ENUM_ACTIVATION_FUNCTION> activation_function_types;
+  su2vector<string> activation_function_names;
  public:
   ~CNeuralNetwork() {
     delete inputLayer;
@@ -85,7 +85,6 @@ class CNeuralNetwork {
       delete total_layers[i];
     }
     delete[] ANN_outputs;
-    delete[] activation_function_types;
   };
   /*!
    * \brief Set the input layer of the network.
@@ -261,7 +260,8 @@ class CNeuralNetwork {
    * \param[in] n_layers - network layer count.
    */
   void SizeActivationFunctions(unsigned long n_layers) {
-    activation_function_types = new ENUM_ACTIVATION_FUNCTION[n_layers];
+    activation_function_types.resize(n_layers);
+    activation_function_names.resize(n_layers);
   }
 
   /*!
diff --git a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
index 71f99b4834a..496edc4d708 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
@@ -31,7 +31,7 @@
 #include <fstream>
 #include <iostream>
 #include <string>
-
+#include <iomanip>
 #include "../../../include/toolboxes/multilayer_perceptron/CIOMap.hpp"
 #include "../../../include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp"
 
@@ -46,10 +46,17 @@ MLPToolbox::CLookUp_ANN::CLookUp_ANN(const unsigned short n_inputs, const string
   number_of_variables = n_inputs;
 
   NeuralNetworks.resize(n_inputs);
+  cout << setfill(' ');
+  cout << endl;
+  cout << "+------------------------------------------------------------------+\n";
+  cout << "|                 Multi-Layer Perceptron (MLP) info                |\n";
+  cout << "+------------------------------------------------------------------+" << endl;
+  
   for (auto i_MLP = 0u; i_MLP < n_inputs; i_MLP++) {
     NeuralNetworks[i_MLP] = new CNeuralNetwork;
     if (rank == MASTER_NODE) cout << "Generating neural network for " << input_filenames[i_MLP] << endl;
     GenerateANN(NeuralNetworks[i_MLP], input_filenames[i_MLP]);
+    if (rank == MASTER_NODE) NeuralNetworks[i_MLP]->displayNetwork();
   }
 }
 
diff --git a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
index 13f96878c06..50322d31216 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
@@ -27,6 +27,7 @@
  */
 #include "../../../include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp"
 
+#include <iomanip>
 #include <iostream>
 
 #include "../../../include/toolboxes/multilayer_perceptron/CLayer.hpp"
@@ -289,14 +290,71 @@ void MLPToolbox::CNeuralNetwork::sizeWeights() {
 }
 
 void MLPToolbox::CNeuralNetwork::displayNetwork() const {
-  /*!
-  TODO:
-  find way of displaying network architectures
-  */
+  /*--- Display information on the MLP architecture ---*/
+  int display_width = 54;
+  int column_width = int(display_width / 3.0) - 1;
+
+  /*--- Input layer information ---*/
+  cout << "+" << setfill('-') << setw(display_width) << right << "+" << endl;
+  cout << setfill(' ');
+  cout << "|" << left << setw(display_width - 1) << "Input Layer Information:"
+       << "|" << endl;
+  cout << "+" << setfill('-') << setw(display_width) << right << "+" << endl;
+  cout << setfill(' ');
+  cout << "|" << left << setw(column_width) << "Input Variable:"
+       << "|" << left << setw(column_width) << "Lower limit:"
+       << "|" << left << setw(column_width) << "Upper limit:"
+       << "|" << endl;
+  cout << "+" << setfill('-') << setw(display_width) << right << "+" << endl;
+  cout << setfill(' ');
+
+  /*--- Hidden layer information ---*/
+  for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++)
+    cout << "|" << left << setw(column_width) << to_string(iInput + 1) + ": " + input_names[iInput] << "|" << right
+         << setw(column_width) << input_norm[iInput].first << "|" << right << setw(column_width)
+         << input_norm[iInput].second << "|" << endl;
+  cout << "+" << setfill('-') << setw(display_width) << right << "+" << endl;
+  cout << setfill(' ');
+  cout << "|" << left << setw(display_width - 1) << "Hidden Layers Information:"
+       << "|" << endl;
+  cout << "+" << setfill('-') << setw(display_width) << right << "+" << endl;
+  cout << setfill(' ');
+  cout << "|" << setw(column_width) << left << "Layer index"
+       << "|" << setw(column_width) << left << "Neuron count"
+       << "|" << setw(column_width) << left << "Function"
+       << "|" << endl;
+  cout << "+" << setfill('-') << setw(display_width) << right << "+" << endl;
+  cout << setfill(' ');
+  for (auto iLayer = 0u; iLayer < n_hidden_layers; iLayer++)
+    cout << "|" << setw(column_width) << right << iLayer + 1 << "|" << setw(column_width) << right
+         << hiddenLayers[iLayer]->getNNeurons() << "|" << setw(column_width) << right
+         << activation_function_names[iLayer + 1] << "|" << endl;
+  cout << "+" << setfill('-') << setw(display_width) << right << "+" << endl;
+  cout << setfill(' ');
+
+  /*--- Output layer information ---*/
+  cout << "|" << left << setw(display_width - 1) << "Output Layer Information:"
+       << "|" << endl;
+  cout << "+" << setfill('-') << setw(display_width) << right << "+" << endl;
+  cout << setfill(' ');
+  cout << "|" << left << setw(column_width) << "Output Variable:"
+       << "|" << left << setw(column_width) << "Lower limit:"
+       << "|" << left << setw(column_width) << "Upper limit:"
+       << "|" << endl;
+  cout << "+" << setfill('-') << setw(display_width) << right << "+" << endl;
+  cout << setfill(' ');
+  for (auto iOutput = 0u; iOutput < outputLayer->getNNeurons(); iOutput++)
+    cout << "|" << left << setw(column_width) << to_string(iOutput + 1) + ": " + output_names[iOutput] << "|" << right
+         << setw(column_width) << output_norm[iOutput].first << "|" << right << setw(column_width)
+         << output_norm[iOutput].second << "|" << endl;
+  cout << "+" << setfill('-') << setw(display_width) << right << "+" << endl;
+  cout << setfill(' ');
+  cout << endl;
 }
 
 void MLPToolbox::CNeuralNetwork::setActivationFunction(unsigned long i_layer, string input) {
   /*--- Translate activation function name from input file to a number ---*/
+  activation_function_names[i_layer] = input;
   if (input.compare("linear") == 0) {
     activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::LINEAR;
     return;
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 8a9797c275e..59a599fb8b3 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -36,19 +36,9 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
   /*--- Set up interpolation algorithm according to data-driven method. Currently only MLP's are supported. ---*/
   switch (Kind_DataDriven_Method) {
     case ENUM_DATADRIVEN_METHOD::MLP:
-      if (rank == MASTER_NODE) {
-        cout << "***********************************************" << endl;
-        cout << "*** initializing the multi-layer perceptron ***" << endl;
-        cout << "***********************************************" << endl;
-      }
       lookup_mlp = new MLPToolbox::CLookUp_ANN(config->GetNDataDriven_Files(), config->GetDataDriven_FileNames());
       break;
     case ENUM_DATADRIVEN_METHOD::LUT:
-      if (rank == MASTER_NODE) {
-        cout << "*****************************************" << endl;
-        cout << "***   initializing the lookup table   ***" << endl;
-        cout << "*****************************************" << endl;
-      }
       lookup_table = new CLookUpTable(config->GetDataDriven_Filename(), "Density", "Energy");
       break;
     default:

From f1140ba434100d1aff4c9c5a46d0dfad2f3fbf70 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 3 Feb 2023 17:24:49 +0100
Subject: [PATCH 170/656] Carried everything to do with the heat solver over
 from Develop as it somehow didn't do it automatically

---
 Common/include/CConfig.hpp                  |   60 +-
 Common/include/option_structure.hpp         |    6 +
 Common/src/CConfig.cpp                      |  240 ++--
 SU2_CFD/include/numerics/CNumerics.hpp      |   28 +
 SU2_CFD/include/numerics/heat.hpp           |  102 +-
 SU2_CFD/include/solvers/CHeatSolver.hpp     |  144 ++-
 SU2_CFD/include/variables/CHeatVariable.hpp |   31 +-
 SU2_CFD/obj/Makefile.am                     |    1 +
 SU2_CFD/src/drivers/CDriver.cpp             |   23 +-
 SU2_CFD/src/meson.build                     |    3 +-
 SU2_CFD/src/numerics/flow/flow_sources.cpp  |  101 +-
 SU2_CFD/src/numerics/heat.cpp               |  202 ++++
 SU2_CFD/src/solvers/CEulerSolver.cpp        |   38 +-
 SU2_CFD/src/solvers/CHeatSolver.cpp         | 1157 +++++++++++++------
 SU2_CFD/src/solvers/CNEMOEulerSolver.cpp    |  539 +++++----
 SU2_CFD/src/variables/CEulerVariable.cpp    |    6 -
 SU2_CFD/src/variables/CHeatVariable.cpp     |   37 +-
 17 files changed, 1712 insertions(+), 1006 deletions(-)
 create mode 100644 SU2_CFD/src/numerics/heat.cpp

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index 9eb9a37bef7..57a4e9af5a1 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -125,7 +125,6 @@ class CConfig {
   Low_Mach_Precon,          /*!< \brief Flag to know if we are using a low Mach number preconditioner. */
   Low_Mach_Corr,            /*!< \brief Flag to know if we are using a low Mach number correction. */
   GravityForce,             /*!< \brief Flag to know if the gravity force is incuded in the formulation. */
-  VorticityConfinement,     /*!< \brief Flag to know if the Vorticity Confinement is included in the formulation. */
   SubsonicEngine,           /*!< \brief Engine intake subsonic region. */
   Frozen_Visc_Cont,         /*!< \brief Flag for cont. adjoint problem with/without frozen viscosity. */
   Frozen_Visc_Disc,         /*!< \brief Flag for disc. adjoint problem with/without frozen viscosity. */
@@ -148,7 +147,6 @@ class CConfig {
   su2double dCMy_dCL;          /*!< \brief Fixed Cl mode derivate. */
   su2double dCMz_dCL;          /*!< \brief Fixed Cl mode derivate. */
   su2double CL_Target;         /*!< \brief Fixed Cl mode Target Cl. */
-  su2double Confinement_Param; /*!< \brief Confinement paramenter for Vorticity Confinement method. */
   TIME_MARCHING TimeMarching;        /*!< \brief Steady or unsteady (time stepping or dual time stepping) computation. */
   unsigned short Dynamic_Analysis;   /*!< \brief Static or dynamic structural analysis. */
   su2double FixAzimuthalLine;        /*!< \brief Fix an azimuthal line due to misalignments of the nearfield. */
@@ -228,7 +226,6 @@ class CConfig {
   string Inlet_Filename;        /*!< \brief Filename specifying an inlet profile. */
   su2double Inlet_Matching_Tol; /*!< \brief Tolerance used when matching a point to a point from the inlet file. */
   string ActDisk_FileName;      /*!< \brief Filename specifying an actuator disk. */
-  string MLP_filename;          /*!< \brief Filename specifying an MLP-driven fluid model. */
 
   string *Marker_Euler,           /*!< \brief Euler wall markers. */
   *Marker_FarField,               /*!< \brief Far field markers. */
@@ -287,6 +284,7 @@ class CConfig {
   su2double *Inlet_Temperature;              /*!< \brief Specified temperatures for a supersonic inlet boundaries. */
   su2double *Inlet_Pressure;                 /*!< \brief Specified static pressures for supersonic inlet boundaries. */
   su2double **Inlet_Velocity;                /*!< \brief Specified flow velocity vectors for supersonic inlet boundaries. */
+  su2double **Inlet_MassFrac;                /*!< \brief Specified Mass fraction vectors for supersonic inlet boundaries (NEMO solver). */
   su2double **Inlet_SpeciesVal;              /*!< \brief Specified species vector for inlet boundaries. */
   su2double **Inlet_TurbVal;                 /*!< \brief Specified turbulent intensity and viscosity ratio for inlet boundaries. */
   su2double *EngineInflow_Target;            /*!< \brief Specified fan face targets for nacelle boundaries. */
@@ -498,7 +496,6 @@ class CConfig {
   Kind_SlopeLimit_Turb,         /*!< \brief Slope limiter for the turbulence equation.*/
   Kind_SlopeLimit_AdjTurb,      /*!< \brief Slope limiter for the adjoint turbulent equation.*/
   Kind_SlopeLimit_AdjFlow,      /*!< \brief Slope limiter for the adjoint equation.*/
-  Kind_SlopeLimit_Heat,         /*!< \brief Slope limiter for the adjoint equation.*/
   Kind_SlopeLimit_Species;      /*!< \brief Slope limiter for the species equation.*/
   unsigned short Kind_FluidModel,  /*!< \brief Kind of the Fluid Model: Ideal, van der Waals, etc. */
   Kind_InitOption,                 /*!< \brief Kind of Init option to choose if initializing with Reynolds number or with thermodynamic conditions   */
@@ -556,7 +553,6 @@ class CConfig {
   Kind_Centered_Turb,           /*!< \brief Centered scheme for the turbulence model. */
   Kind_Centered_AdjTurb,        /*!< \brief Centered scheme for the adjoint turbulence model. */
   Kind_Centered_Species,        /*!< \brief Centered scheme for the species model. */
-  Kind_Centered_Heat,           /*!< \brief Centered scheme for the heat transfer model. */
   Kind_Centered_Template;       /*!< \brief Centered scheme for the template model. */
 
 
@@ -573,7 +569,6 @@ class CConfig {
   Kind_Upwind_Turb,             /*!< \brief Upwind scheme for the turbulence model. */
   Kind_Upwind_AdjTurb,          /*!< \brief Upwind scheme for the adjoint turbulence model. */
   Kind_Upwind_Species,          /*!< \brief Upwind scheme for the species model. */
-  Kind_Upwind_Heat,             /*!< \brief Upwind scheme for the heat transfer model. */
   Kind_Upwind_Template;         /*!< \brief Upwind scheme for the template model. */
 
   bool MUSCL,              /*!< \brief MUSCL scheme .*/
@@ -609,6 +604,7 @@ class CConfig {
   INLET_TYPE Kind_Inlet;
   INLET_TYPE *Kind_Inc_Inlet;
   INC_OUTLET_TYPE *Kind_Inc_Outlet;
+  WALL_TYPE *Kind_Wall;            /*!< \brief Type of wall treatment. */
   unsigned short nWall_Types;      /*!< \brief Number of wall treatment types listed. */
   unsigned short nInc_Inlet;       /*!< \brief Number of inlet boundary treatment types listed. */
   unsigned short nInc_Outlet;      /*!< \brief Number of inlet boundary treatment types listed. */
@@ -638,6 +634,8 @@ class CConfig {
   Kappa_1st_Flow,           /*!< \brief Lax 1st order dissipation coefficient for flow equations (coarse multigrid levels). */
   Kappa_2nd_Flow,           /*!< \brief JST 2nd order dissipation coefficient for flow equations. */
   Kappa_4th_Flow,           /*!< \brief JST 4th order dissipation coefficient for flow equations. */
+  Kappa_2nd_Heat,           /*!< \brief 2nd order dissipation coefficient for heat equation. */
+  Kappa_4th_Heat,           /*!< \brief 4th order dissipation coefficient for heat equation. */
   Cent_Jac_Fix_Factor,              /*!< \brief Multiply the dissipation contribution to the Jacobian of central schemes
                                                 by this factor to make the global matrix more diagonal dominant. */
   Cent_Inc_Jac_Fix_Factor;          /*!< \brief Multiply the dissipation contribution to the Jacobian of incompressible central schemes */
@@ -1109,6 +1107,7 @@ class CConfig {
   rampRotFrame_coeff[3], /*!< \brief ramp rotating frame coefficients for the COption class. */
   rampOutPres_coeff[3],  /*!< \brief ramp outlet pressure coefficients for the COption class. */
   jst_adj_coeff[2],      /*!< \brief artificial dissipation (adjoint) array for the COption class. */
+  ad_coeff_heat[2],      /*!< \brief artificial dissipation (heat) array for the COption class. */
   mesh_box_length[3],    /*!< \brief mesh box length for the COption class. */
   mesh_box_offset[3],    /*!< \brief mesh box offset for the COption class. */
   geo_loc[2],            /*!< \brief SU2_GEO section locations array for the COption class. */
@@ -1197,7 +1196,6 @@ class CConfig {
 
   /* other NEMO configure options*/
   unsigned short nSpecies_Cat_Wall,         /*!< \brief No. of species for a catalytic wall. */
-  nSpecies_inlet,                           /*!< \brief No. of species for NEMO inlet. */
   iWall_Catalytic,                          /*!< \brief Iterator over catalytic walls. */
   nWall_Catalytic;                          /*!< \brief No. of catalytic walls. */
   su2double *Gas_Composition,               /*!< \brief Initial mass fractions of flow [dimensionless]. */
@@ -1212,8 +1210,6 @@ class CConfig {
   *Wall_Catalytic;                          /*!< \brief Pointer to catalytic walls. */
   TRANSCOEFFMODEL   Kind_TransCoeffModel;   /*!< \brief Transport coefficient Model for NEMO solver. */
   su2double CatalyticEfficiency;            /*!< \brief Wall catalytic efficiency. */
-  su2double *Inlet_MassFrac;                /*!< \brief Specified Mass fraction vectors for NEMO inlet boundaries. */
-  su2double Inlet_Temperature_ve;           /*!< \brief Specified Tve for supersonic inlet boundaries (NEMO solver). */
 
   /*--- Additional species solver options ---*/
   bool Species_Clipping;           /*!< \brief Boolean that activates solution clipping for scalar transport. */
@@ -1595,12 +1591,6 @@ class CConfig {
    */
   su2double GetGamma(void) const { return Gamma; }
 
-  /*!
-   * \brief Get the value of the Confinement Parameter.
-   * \return Value of the constant: Confinement Parameter
-   */
-  su2double GetConfinement_Param(void) const { return Confinement_Param; }
-
   /*!
    * \brief Get the values of the CFL adaption parameters.
    * \return Value of CFL adaption parameter
@@ -2336,8 +2326,8 @@ class CConfig {
    * \param[in] val_kind_fem - If FEM, what kind of FEM discretization.
    */
   void SetKind_ConvNumScheme(unsigned short val_kind_convnumscheme, CENTERED val_kind_centered,
-                             UPWIND val_kind_upwind, LIMITER val_kind_slopelimit,
-                             bool val_muscl,  unsigned short val_kind_fem);
+                             UPWIND val_kind_upwind,        LIMITER val_kind_slopelimit,
+                             bool val_muscl,                        unsigned short val_kind_fem);
 
   /*!
    * \brief Get the value of limiter coefficient.
@@ -4386,7 +4376,7 @@ class CConfig {
    * \return Value of roughness.
    */
   su2double GethRoughness(void) const { return hRoughness; }
-
+  
   /*!
    * \brief Get the kind of the species model.
    * \return Kind of the species model.
@@ -4701,6 +4691,18 @@ class CConfig {
    */
   su2double GetKappa_4th_Flow(void) const { return Kappa_4th_Flow; }
 
+  /*!
+   * \brief Value of the calibrated constant for the JST method (center scheme).
+   * \return Calibrated constant for the JST-like method for the heat equations.
+   */
+  su2double GetKappa_2nd_Heat(void) const { return Kappa_2nd_Heat; }
+
+  /*!
+   * \brief Value of the calibrated constant for the JST-like method (center scheme).
+   * \return Calibrated constant for the JST-like method for the heat equation.
+   */
+  su2double GetKappa_4th_Heat(void) const { return Kappa_4th_Heat; }
+
   /*!
    * \brief Factor by which to multiply the dissipation contribution to Jacobians of central schemes.
    * \return The factor.
@@ -6045,12 +6047,6 @@ class CConfig {
    */
   bool GetGravityForce(void) const { return GravityForce; }
 
-  /*!
-   * \brief Get information about the Vorticity Confinement.
-   * \return <code>TRUE</code> if it uses Vorticity Confinement; otherwise <code>FALSE</code>.
-   */
-  bool GetVorticityConfinement(void) const { return VorticityConfinement; }
-
   /*!
    * \brief Get information about the body force.
    * \return <code>TRUE</code> if it uses a body force; otherwise <code>FALSE</code>.
@@ -6720,20 +6716,6 @@ class CConfig {
    */
   const su2double* GetInlet_Velocity(string val_index) const;
 
-  /*!
-   * \brief Get the mass fraction vector for a NEMO inlet boundary.
-   * \param[in] val_index - Index corresponding to the inlet boundary.
-   * \return The inlet velocity vector.
-   */
-  const su2double* GetInlet_MassFrac() const { return Inlet_MassFrac; }
-
-  /*!
-   * \brief Get the Tve value for a NEMO inlet boundary.
-   * \param[in] val_index - Index corresponding to the inlet boundary.
-   * \return The inlet velocity vector.
-   */
-  su2double GetInlet_Temperature_ve() const { return Inlet_Temperature_ve; }
-
   /*!
    * \brief Get the total pressure at an inlet boundary.
    * \param[in] val_index - Index corresponding to the inlet boundary.
@@ -7006,7 +6988,7 @@ class CConfig {
    * \param[in] val_index - Index corresponding to the boundary.
    * \return The wall type and roughness height.
    */
-  pair<WALL_TYPE,su2double> GetWallRoughnessProperties(const string& val_marker) const;
+  pair<WALL_TYPE,su2double> GetWallRoughnessProperties(string val_marker) const;
 
   /*!
    * \brief Get the target (pressure, massflow, etc) at an engine inflow boundary.
diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index 1e34f0422e8..a24a7c4960e 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -534,6 +534,12 @@ enum ENUM_SPACE {
   SPACE_UPWIND = 2,    /*!< \brief Upwind convective numerical method. */
   FINITE_ELEMENT = 3   /*!< \brief Finite element convective numerical method. */
 };
+static const MapType<std::string, ENUM_SPACE> Space_Map = {
+  MakePair("NONE", NO_CONVECTIVE)
+  MakePair("SPACE_CENTERED", SPACE_CENTERED)
+  MakePair("SPACE_UPWIND", SPACE_UPWIND)
+  MakePair("FINITE_ELEMENT", FINITE_ELEMENT)
+};
 
 /*!
  * \brief Types of fluid model
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index eee226df37e..4b60c4f62fe 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -840,6 +840,7 @@ void CConfig::SetPointersNull(void) {
   Kind_WallFunctions       = nullptr;
   IntInfo_WallFunctions    = nullptr;
   DoubleInfo_WallFunctions = nullptr;
+  Kind_Wall                = nullptr;
 
   Config_Filenames = nullptr;
 
@@ -1129,8 +1130,6 @@ void CConfig::SetConfig_Options() {
   addBoolOption("AXISYMMETRIC", Axisymmetric, false);
   /* DESCRIPTION: Add the gravity force */
   addBoolOption("GRAVITY_FORCE", GravityForce, false);
-  /* DESCRIPTION: Add the Vorticity Confinement term*/
-  addBoolOption("VORTICITY_CONFINEMENT", VorticityConfinement, false);
   /* DESCRIPTION: Apply a body force as a source term (NO, YES) */
   addBoolOption("BODY_FORCE", Body_Force, false);
   body_force[0] = 0.0; body_force[1] = 0.0; body_force[2] = 0.0;
@@ -1178,8 +1177,6 @@ void CConfig::SetConfig_Options() {
   addDoubleOption("DATADRIVEN_FLUID_INITIAL_DENSITY", DataDriven_initial_density, 1.225);
   /*!\brief DATADRIVEN_FLUID_INITIAL_ENERGY \n DESCRIPTION: Initial value for the static energy in the Newton solvers in the data-driven fluid model. \n \ingroup Config*/
   addDoubleOption("DATADRIVEN_FLUID_INITIAL_ENERGY", DataDriven_initial_energy, 1e5);
-  /*!\brief CONFINEMENT_PARAM \n DESCRIPTION: Input Confinement Parameter for Vorticity Confinement*/
-  addDoubleOption("CONFINEMENT_PARAM", Confinement_Param, 0.0);
 
   /*!\par CONFIG_CATEGORY: Freestream Conditions \ingroup Config*/
   /*--- Options related to freestream specification ---*/
@@ -1205,10 +1202,6 @@ void CConfig::SetConfig_Options() {
   addEnumOption("TRANSPORT_COEFF_MODEL", Kind_TransCoeffModel, TransCoeffModel_Map, TRANSCOEFFMODEL::WILKE);
   /* DESCRIPTION: Specify mass fraction of each species */
   addDoubleListOption("GAS_COMPOSITION", nSpecies, Gas_Composition);
-  /* DESCRIPTION: Specify mass fraction of each species for NEMO inlet*/
-  addDoubleListOption("INLET_GAS_COMPOSITION", nSpecies_inlet, Inlet_MassFrac);
-  /*!\brief INLET_TEMPERATURE_VE \n DESCRIPTION: NEMO inlet temperature_ve (K), if left 0 K, set to Ttr value \ingroup Config*/
-  addDoubleOption("INLET_TEMPERATURE_VE", Inlet_Temperature_ve, 0.0);
   /* DESCRIPTION: Specify if mixture is frozen */
   addBoolOption("FROZEN_MIXTURE", frozen, false);
   /* DESCRIPTION: Specify if there is ionization */
@@ -1517,9 +1510,6 @@ void CConfig::SetConfig_Options() {
   /*!\brief ACTDISK_FILENAME \n DESCRIPTION: Input file for a specified actuator disk (w/ extension) \n DEFAULT: actdiskinput.dat \ingroup Config*/
   addStringOption("ACTDISK_FILENAME", ActDisk_FileName, string("actdiskinput.dat"));
 
-  /*!\brief MLP_FILENAME \n DESCRIPTION: Input file for a multi-layer perceptron input file for fluid model definition. w/ extension) \n DEFAULT: MLP_collection.mlp \ingroup Config*/
-  addStringOption("MLP_FILENAME", MLP_filename, string("MLP_collection.mlp"));
-
   /*!\brief INLET_TYPE  \n DESCRIPTION: Inlet boundary type \n OPTIONS: see \link Inlet_Map \endlink \n DEFAULT: TOTAL_CONDITIONS \ingroup Config*/
   addEnumOption("INLET_TYPE", Kind_Inlet, Inlet_Map, INLET_TYPE::TOTAL_CONDITIONS);
   /*!\brief INC_INLET_TYPE \n DESCRIPTION: List of inlet types for incompressible flows. List length must match number of inlet markers. Options: VELOCITY_INLET, PRESSURE_INLET, INPUT_FILE. \ingroup Config*/
@@ -1912,6 +1902,9 @@ void CConfig::SetConfig_Options() {
   addDoubleArrayOption("JST_SENSOR_COEFF", 2, jst_coeff);
   /*!\brief LAX_SENSOR_COEFF \n DESCRIPTION: 1st order artificial dissipation coefficients for the Lax-Friedrichs method. \ingroup Config*/
   addDoubleOption("LAX_SENSOR_COEFF", Kappa_1st_Flow, 0.15);
+  ad_coeff_heat[0] = 0.5; ad_coeff_heat[1] = 0.02;
+  /*!\brief JST_SENSOR_COEFF_HEAT \n DESCRIPTION: 2nd and 4th order artificial dissipation coefficients for the JST method \ingroup Config*/
+  addDoubleArrayOption("JST_SENSOR_COEFF_HEAT", 2, ad_coeff_heat);
   /*!\brief USE_ACCURATE_FLUX_JACOBIANS \n DESCRIPTION: Use numerically computed Jacobians for AUSM+up(2) and SLAU(2) \ingroup Config*/
   addBoolOption("USE_ACCURATE_FLUX_JACOBIANS", Use_Accurate_Jacobians, false);
   /*!\brief CENTRAL_JACOBIAN_FIX_FACTOR \n DESCRIPTION: Improve the numerical properties (diagonal dominance) of the global Jacobian matrix, 3 to 4 is "optimum" (central schemes) \ingroup Config*/
@@ -1960,10 +1953,9 @@ void CConfig::SetConfig_Options() {
 
   /*!\brief MUSCL_FLOW \n DESCRIPTION: Check if the MUSCL scheme should be used \ingroup Config*/
   addBoolOption("MUSCL_HEAT", MUSCL_Heat, false);
-  /*!\brief SLOPE_LIMITER_HEAT \n DESCRIPTION: Slope limiter \n OPTIONS: See \link Limiter_Map \endlink \n DEFAULT NONE \ingroup Config*/
-  addEnumOption("SLOPE_LIMITER_HEAT", Kind_SlopeLimit_Heat, Limiter_Map, LIMITER::NONE);
-  /*!\brief CONV_NUM_METHOD_HEAT \n DESCRIPTION: Convective numerical method */
-  addConvectOption("CONV_NUM_METHOD_HEAT", Kind_ConvNumScheme_Heat, Kind_Centered_Heat, Kind_Upwind_Heat);
+  /*!\brief CONV_NUM_METHOD_HEAT
+   *  \n DESCRIPTION: Convective numerical method \n DEFAULT: UPWIND */
+  addEnumOption("CONV_NUM_METHOD_HEAT", Kind_ConvNumScheme_Heat, Space_Map, SPACE_UPWIND);
 
   /*!\par CONFIG_CATEGORY: Adjoint and Gradient \ingroup Config*/
   /*--- Options related to the adjoint and gradient ---*/
@@ -3561,20 +3553,9 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
 
   /*--- Set limiter for no MUSCL reconstructions ---*/
 
-  auto SetScalarDefaults = [](bool muscl, unsigned short& KindConvScheme, UPWIND& KindUpwind, LIMITER& KindLimiter) {
-    if (KindConvScheme == NO_CONVECTIVE) {
-      KindConvScheme = SPACE_UPWIND;
-      KindUpwind = UPWIND::SCALAR_UPWIND;
-    } else if (KindConvScheme == SPACE_CENTERED) {
-      SU2_MPI::Error("Centered schemes are not available for scalar transport", CURRENT_FUNCTION);
-    }
-    if (!muscl) KindLimiter = LIMITER::NONE;
-  };
-  SetScalarDefaults(MUSCL_Turb, Kind_ConvNumScheme_Turb, Kind_Upwind_Turb, Kind_SlopeLimit_Turb);
-  SetScalarDefaults(MUSCL_Heat, Kind_ConvNumScheme_Heat, Kind_Upwind_Heat, Kind_SlopeLimit_Heat);
-  SetScalarDefaults(MUSCL_Species, Kind_ConvNumScheme_Species, Kind_Upwind_Species, Kind_SlopeLimit_Species);
-
   if (!MUSCL_Flow || (Kind_ConvNumScheme_Flow == SPACE_CENTERED)) Kind_SlopeLimit_Flow = LIMITER::NONE;
+  if (!MUSCL_Turb || (Kind_ConvNumScheme_Turb == SPACE_CENTERED)) Kind_SlopeLimit_Turb = LIMITER::NONE;
+  if (!MUSCL_Species || (Kind_ConvNumScheme_Species == SPACE_CENTERED)) Kind_SlopeLimit_Species = LIMITER::NONE;
   if (!MUSCL_AdjFlow || (Kind_ConvNumScheme_AdjFlow == SPACE_CENTERED)) Kind_SlopeLimit_AdjFlow = LIMITER::NONE;
   if (!MUSCL_AdjTurb || (Kind_ConvNumScheme_AdjTurb == SPACE_CENTERED)) Kind_SlopeLimit_AdjTurb = LIMITER::NONE;
 
@@ -4412,6 +4393,8 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
   Kappa_4th_Flow = jst_coeff[1];
   Kappa_2nd_AdjFlow = jst_adj_coeff[0];
   Kappa_4th_AdjFlow = jst_adj_coeff[1];
+  Kappa_2nd_Heat = ad_coeff_heat[0];
+  Kappa_4th_Heat = ad_coeff_heat[1];
 
   /*--- Make the MG_PreSmooth, MG_PostSmooth, and MG_CorrecSmooth
    arrays consistent with nMGLevels ---*/
@@ -4927,18 +4910,6 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
     }
   }
 
-  /*--- Vorticity confinement feature currently not supported for incompressible or non-equilibrium model or axisymmetric flows. ---*/
-
-  if ((Kind_Solver == MAIN_SOLVER::INC_EULER
-    || Kind_Solver == MAIN_SOLVER::INC_NAVIER_STOKES
-    || Kind_Solver == MAIN_SOLVER::INC_RANS
-    || Kind_Solver == MAIN_SOLVER::NEMO_EULER
-    || Kind_Solver == MAIN_SOLVER::NEMO_NAVIER_STOKES
-    || Axisymmetric)
-    && VorticityConfinement) {
-    SU2_MPI::Error("Vorticity confinement feature currently not supported for incompressible or non-equilibrium model or axisymmetric flows.", CURRENT_FUNCTION);
-  }
-
   /*--- Check the coefficients for the polynomial models. ---*/
 
   if (Kind_Solver != MAIN_SOLVER::INC_EULER && Kind_Solver != MAIN_SOLVER::INC_NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::INC_RANS) {
@@ -5043,25 +5014,95 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
     Streamwise_Periodic_Temperature = false;
   }
 
-  if (nRough_Wall > 0) {
-    /*--- Validate name of the markers. ---*/
-    for (iMarker = 0; iMarker < nRough_Wall; ++iMarker) {
-      auto CheckMarker = [&](unsigned short nMarker, const string* markerName) {
-        for (auto jMarker = 0u; jMarker < nMarker; ++jMarker) {
-          if (markerName[jMarker].compare(Marker_RoughWall[iMarker]) == 0) {
-            return true;
-          }
-        }
-        return false;
-      };
-      if (!CheckMarker(nMarker_HeatFlux, Marker_HeatFlux) &&
-          !CheckMarker(nMarker_Isothermal, Marker_Isothermal) &&
-          !CheckMarker(nMarker_HeatTransfer, Marker_HeatTransfer) &&
-          !CheckMarker(nMarker_CHTInterface, Marker_CHTInterface)) {
-        SU2_MPI::Error("Marker " + Marker_RoughWall[iMarker] + " is not a viscous wall.", CURRENT_FUNCTION);
-      }
-    }
-  }
+  /*--- Check that if the wall roughness array are compatible and set deafult values if needed. ---*/
+   if ((nMarker_HeatFlux > 0) || (nMarker_Isothermal > 0) || (nMarker_HeatTransfer) || (nMarker_CHTInterface > 0)) {
+
+     /*--- The total number of wall markers. ---*/
+     unsigned short nWall = nMarker_HeatFlux + nMarker_Isothermal + nMarker_HeatTransfer + nMarker_CHTInterface;
+
+     /*--- If no roughness is specified all walls are assumed to be smooth. ---*/
+     if (nRough_Wall == 0) {
+
+       nRough_Wall = nWall;
+       Roughness_Height = new su2double [nWall];
+       Kind_Wall = new WALL_TYPE [nWall];
+       for (iMarker = 0; iMarker < nMarker_HeatFlux; iMarker++) {
+         Roughness_Height[iMarker] = 0.0;
+         Kind_Wall[iMarker] = WALL_TYPE::SMOOTH;
+       }
+       for (iMarker = 0; iMarker < nMarker_Isothermal; iMarker++) {
+         Roughness_Height[nMarker_HeatFlux + iMarker] = 0.0;
+         Kind_Wall[nMarker_HeatFlux + iMarker] = WALL_TYPE::SMOOTH;
+       }
+       for (iMarker = 0; iMarker < nMarker_HeatTransfer; iMarker++) {
+         Roughness_Height[nMarker_HeatFlux + nMarker_Isothermal + iMarker] = 0.0;
+         Kind_Wall[nMarker_HeatFlux + nMarker_Isothermal + iMarker] = WALL_TYPE::SMOOTH;
+       }
+       for (iMarker = 0; iMarker < nMarker_CHTInterface; iMarker++) {
+         Roughness_Height[nMarker_HeatFlux + nMarker_Isothermal + nMarker_HeatTransfer + iMarker] = 0.0;
+         Kind_Wall[nMarker_HeatFlux + nMarker_Isothermal + nMarker_HeatTransfer + iMarker] = WALL_TYPE::SMOOTH;
+       }
+
+       /*--- Check for mismatch in number of rough walls and solid walls. ---*/
+     } else if (nRough_Wall > nWall) {
+        SU2_MPI::Error("Mismatch in number of rough walls and solid walls. Number of rough walls cannot be more than solid walls.", CURRENT_FUNCTION);
+       /*--- Check name of the marker and assign the corresponding roughness. ---*/
+     } else {
+       /*--- Store roughness heights in a temp array. ---*/
+       vector<su2double> temp_rough;
+       for (iMarker = 0; iMarker < nRough_Wall; iMarker++)
+         temp_rough.push_back(Roughness_Height[iMarker]);
+
+       /*--- Reallocate the roughness arrays in case not all walls are rough. ---*/
+       delete Roughness_Height;
+       delete Kind_Wall;
+       Roughness_Height = new su2double [nWall];
+       Kind_Wall = new WALL_TYPE [nWall];
+       unsigned short jMarker, chkRough = 0;
+
+       /*--- Initialize everything to smooth. ---*/
+       for (iMarker = 0; iMarker < nWall; iMarker++) {
+         Roughness_Height[iMarker] = 0.0;
+         Kind_Wall[iMarker] = WALL_TYPE::SMOOTH;
+       }
+
+       /*--- Look through heat flux, isothermal, heat transfer and cht_interface markers and assign proper values. ---*/
+       for (iMarker = 0; iMarker < nRough_Wall; iMarker++) {
+         for (jMarker = 0; jMarker < nMarker_HeatFlux; jMarker++)
+           if (Marker_HeatFlux[jMarker].compare(Marker_RoughWall[iMarker]) == 0) {
+             Roughness_Height[jMarker] = temp_rough[iMarker];
+             chkRough++;
+           }
+
+         for (jMarker = 0; jMarker < nMarker_Isothermal; jMarker++)
+           if (Marker_Isothermal[jMarker].compare(Marker_RoughWall[iMarker]) == 0) {
+             Roughness_Height[nMarker_HeatFlux + jMarker] = temp_rough[iMarker];
+             chkRough++;
+           }
+
+         for (jMarker = 0; jMarker < nMarker_HeatTransfer; jMarker++)
+           if (Marker_HeatTransfer[jMarker].compare(Marker_RoughWall[iMarker]) == 0) {
+             Roughness_Height[nMarker_HeatFlux + nMarker_Isothermal + jMarker] = temp_rough[iMarker];
+             chkRough++;
+           }
+
+         for (jMarker = 0; jMarker < nMarker_CHTInterface; jMarker++)
+           if (Marker_CHTInterface[jMarker].compare(Marker_RoughWall[iMarker]) == 0) {
+             Roughness_Height[nMarker_HeatFlux + nMarker_Isothermal + nMarker_HeatTransfer + jMarker] = temp_rough[iMarker];
+             chkRough++;
+           }
+       }
+
+       /*--- Update kind_wall when a non zero roughness value is specified. ---*/
+       for (iMarker = 0; iMarker < nWall; iMarker++)
+         if (Roughness_Height[iMarker] != 0.0)
+           Kind_Wall[iMarker] = WALL_TYPE::ROUGH;
+
+       /*--- Check if a non solid wall marker was specified as rough. ---*/
+       if (chkRough != nRough_Wall)
+         SU2_MPI::Error("Only solid walls can be rough.", CURRENT_FUNCTION);
+     }
+   }
 
   /*--- Handle default options for topology optimization ---*/
 
@@ -6063,14 +6104,14 @@ void CConfig::SetOutput(SU2_COMPONENT val_software, unsigned short val_izone) {
         switch (Kind_Trans_Model) {
           case TURB_TRANS_MODEL::NONE:  break;
           case TURB_TRANS_MODEL::LM: {
-            cout << "Transition model: Langtry and Menter's 4 equation model";
+            cout << "Transition model: Langtry and Menter's 4 equation model"; 
             if (lmParsedOptions.LM2015) {
               cout << " w/ cross-flow corrections (2015)" << endl;
             } else {
               cout << " (2009)" << endl;
             }
-            break;
-          }
+            break; 
+          }          
         }
         if (Kind_Trans_Model == TURB_TRANS_MODEL::LM) {
 
@@ -6083,7 +6124,7 @@ void CConfig::SetOutput(SU2_COMPONENT val_software, unsigned short val_izone) {
             case TURB_TRANS_CORRELATION::MEDIDA_BAEDER: cout << "Medida and Baeder (2011)" << endl;  break;
             case TURB_TRANS_CORRELATION::MEDIDA: cout << "Medida PhD (2014)" << endl;  break;
             case TURB_TRANS_CORRELATION::MENTER_LANGTRY: cout << "Menter and Langtry (2009)" << endl;  break;
-            case TURB_TRANS_CORRELATION::DEFAULT:
+            case TURB_TRANS_CORRELATION::DEFAULT: 
               switch (Kind_Turb_Model) {
                 case TURB_MODEL::SA: cout << "Malan et al. (2009)" << endl;  break;
                 case TURB_MODEL::SST: cout << "Menter and Langtry (2009)" << endl;  break;
@@ -7969,6 +8010,8 @@ CConfig::~CConfig() {
 
   delete[] Marker_All_SendRecv;
 
+  delete[] Kind_Wall;
+
   if (DV_Value != nullptr) {
     for (iDV = 0; iDV < nDV; iDV++) delete[] DV_Value[iDV];
     delete [] DV_Value;
@@ -8358,14 +8401,6 @@ void CConfig::SetGlobalParam(MAIN_SOLVER val_solver,
     }
   };
 
-  auto SetHeatParam = [&]() {
-    if (val_system == RUNTIME_HEAT_SYS) {
-      SetKind_ConvNumScheme(Kind_ConvNumScheme_Heat, Kind_Centered_Heat,
-                            Kind_Upwind_Heat, Kind_SlopeLimit_Heat, MUSCL_Heat, NONE);
-      SetKind_TimeIntScheme(Kind_TimeIntScheme_Heat);
-    }
-  };
-
   auto SetSpeciesParam = [&]() {
     if (val_system == RUNTIME_SPECIES_SYS) {
       SetKind_ConvNumScheme(Kind_ConvNumScheme_Species, Kind_Centered_Species,
@@ -8386,21 +8421,21 @@ void CConfig::SetGlobalParam(MAIN_SOLVER val_solver,
 
   switch (val_solver) {
     case MAIN_SOLVER::EULER: case MAIN_SOLVER::INC_EULER: case MAIN_SOLVER::NEMO_EULER:
-    case MAIN_SOLVER::DISC_ADJ_EULER: case MAIN_SOLVER::DISC_ADJ_INC_EULER:
       SetFlowParam();
       break;
     case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::INC_NAVIER_STOKES: case MAIN_SOLVER::NEMO_NAVIER_STOKES:
-    case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES:
       SetFlowParam();
       SetSpeciesParam();
-      SetHeatParam();
+
+      if (val_system == RUNTIME_HEAT_SYS) {
+        SetKind_ConvNumScheme(Kind_ConvNumScheme_Heat, CENTERED::NONE, UPWIND::NONE, LIMITER::NONE, NONE, NONE);
+        SetKind_TimeIntScheme(Kind_TimeIntScheme_Heat);
+      }
       break;
     case MAIN_SOLVER::RANS: case MAIN_SOLVER::INC_RANS:
-    case MAIN_SOLVER::DISC_ADJ_RANS: case MAIN_SOLVER::DISC_ADJ_INC_RANS:
       SetFlowParam();
       SetTurbParam();
       SetSpeciesParam();
-      SetHeatParam();
 
       if (val_system == RUNTIME_TRANS_SYS) {
         SetKind_ConvNumScheme(Kind_ConvNumScheme_Turb, Kind_Centered_Turb,
@@ -8408,14 +8443,14 @@ void CConfig::SetGlobalParam(MAIN_SOLVER val_solver,
                               MUSCL_Turb, NONE);
         SetKind_TimeIntScheme(Kind_TimeIntScheme_Turb);
       }
+      if (val_system == RUNTIME_HEAT_SYS) {
+        SetKind_ConvNumScheme(Kind_ConvNumScheme_Heat, CENTERED::NONE, UPWIND::NONE, LIMITER::NONE, NONE, NONE);
+        SetKind_TimeIntScheme(Kind_TimeIntScheme_Heat);
+      }
       break;
     case MAIN_SOLVER::FEM_EULER:
     case MAIN_SOLVER::FEM_NAVIER_STOKES:
-    case MAIN_SOLVER::FEM_RANS:
     case MAIN_SOLVER::FEM_LES:
-    case MAIN_SOLVER::DISC_ADJ_FEM_EULER:
-    case MAIN_SOLVER::DISC_ADJ_FEM_NS:
-    case MAIN_SOLVER::DISC_ADJ_FEM_RANS:
       if (val_system == RUNTIME_FLOW_SYS) {
         SetKind_ConvNumScheme(Kind_ConvNumScheme_FEM_Flow, Kind_Centered_Flow,
                               Kind_Upwind_Flow, Kind_SlopeLimit_Flow,
@@ -8441,7 +8476,6 @@ void CConfig::SetGlobalParam(MAIN_SOLVER val_solver,
       }
       break;
     case MAIN_SOLVER::HEAT_EQUATION:
-    case MAIN_SOLVER::DISC_ADJ_HEAT:
       if (val_system == RUNTIME_HEAT_SYS) {
         SetKind_ConvNumScheme(NONE, CENTERED::NONE, UPWIND::NONE, LIMITER::NONE, NONE, NONE);
         SetKind_TimeIntScheme(Kind_TimeIntScheme_Heat);
@@ -8449,12 +8483,11 @@ void CConfig::SetGlobalParam(MAIN_SOLVER val_solver,
       break;
 
     case MAIN_SOLVER::FEM_ELASTICITY:
-    case MAIN_SOLVER::DISC_ADJ_FEM:
 
       Current_DynTime = static_cast<su2double>(TimeIter)*Delta_DynTime;
 
       if (val_system == RUNTIME_FEA_SYS) {
-        SetKind_ConvNumScheme(NONE, CENTERED::NONE, UPWIND::NONE, LIMITER::NONE, NONE, NONE);
+        SetKind_ConvNumScheme(NONE, CENTERED::NONE, UPWIND::NONE, LIMITER::NONE , NONE, NONE);
         SetKind_TimeIntScheme(NONE);
       }
       break;
@@ -9144,15 +9177,40 @@ su2double CConfig::GetWall_HeatTransfer_Temperature(string val_marker) const {
   return HeatTransfer_WallTemp[0];
 }
 
-pair<WALL_TYPE, su2double> CConfig::GetWallRoughnessProperties(const string& val_marker) const {
-  su2double roughness = 0.0;
-  for (auto iMarker = 0u; iMarker < nRough_Wall; iMarker++) {
-    if (val_marker.compare(Marker_RoughWall[iMarker]) == 0) {
-      roughness = Roughness_Height[iMarker];
-      break;
-    }
+pair<WALL_TYPE, su2double> CConfig::GetWallRoughnessProperties(string val_marker) const {
+  unsigned short iMarker = 0;
+  short          flag = -1;
+  pair<WALL_TYPE, su2double> WallProp;
+
+  if (nMarker_HeatFlux > 0 || nMarker_Isothermal > 0 || nMarker_HeatTransfer || nMarker_CHTInterface > 0) {
+    for (iMarker = 0; iMarker < nMarker_HeatFlux; iMarker++)
+      if (Marker_HeatFlux[iMarker] == val_marker) {
+        flag = iMarker;
+        WallProp = make_pair(Kind_Wall[flag], Roughness_Height[flag]);
+        return WallProp;
+      }
+    for (iMarker = 0; iMarker < nMarker_Isothermal; iMarker++)
+      if (Marker_Isothermal[iMarker] == val_marker) {
+        flag = nMarker_HeatFlux + iMarker;
+        WallProp = make_pair(Kind_Wall[flag], Roughness_Height[flag]);
+        return WallProp;
+      }
+    for (iMarker = 0; iMarker < nMarker_HeatTransfer; iMarker++)
+      if (Marker_HeatTransfer[iMarker] == val_marker) {
+        flag = nMarker_HeatFlux + nMarker_Isothermal + iMarker;
+        WallProp = make_pair(Kind_Wall[flag], Roughness_Height[flag]);
+        return WallProp;
+      }
+    for (iMarker = 0; iMarker < nMarker_CHTInterface; iMarker++)
+      if (Marker_CHTInterface[iMarker] == val_marker) {
+        flag = nMarker_HeatFlux + nMarker_Isothermal + nMarker_HeatTransfer + iMarker;
+        WallProp = make_pair(Kind_Wall[flag], Roughness_Height[flag]);
+        return WallProp;
+      }
   }
-  return make_pair(roughness > 0 ? WALL_TYPE::ROUGH : WALL_TYPE::SMOOTH, roughness);
+
+  WallProp = make_pair(WALL_TYPE::SMOOTH, 0.0);
+  return WallProp;
 }
 
 WALL_FUNCTIONS CConfig::GetWallFunction_Treatment(string val_marker) const {
diff --git a/SU2_CFD/include/numerics/CNumerics.hpp b/SU2_CFD/include/numerics/CNumerics.hpp
index 354ff746ec4..fed80b1af56 100644
--- a/SU2_CFD/include/numerics/CNumerics.hpp
+++ b/SU2_CFD/include/numerics/CNumerics.hpp
@@ -71,6 +71,9 @@ class CNumerics {
   Thermal_Conductivity_j,    /*!< \brief Thermal conductivity at point j. */
   Thermal_Conductivity_ve_i, /*!< \brief vibrational-electronic Thermal conductivity at point i. */
   Thermal_Conductivity_ve_j, /*!< \brief vibrational-electronic Thermal conductivity at point j. */
+  Thermal_Diffusivity_i,     /*!< \brief Thermal diffusivity at point i. */
+  Thermal_Diffusivity_j;     /*!< \brief Thermal diffusivity at point j. */
+  su2double 
   Cp_i,               /*!< \brief Cp at point i. */
   Cp_j;               /*!< \brief Cp at point j. */
   su2double
@@ -106,6 +109,9 @@ class CNumerics {
   su2double
   dist_i,  /*!< \brief Distance of point i to the nearest wall. */
   dist_j;  /*!< \brief Distance of point j to the nearest wall. */
+  su2double
+  Temp_i,  /*!< \brief Temperature at point i. */
+  Temp_j;  /*!< \brief Temperature at point j. */
   const su2double
   *Und_Lapl_i,  /*!< \brief Undivided laplacians at point i. */
   *Und_Lapl_j;  /*!< \brief Undivided laplacians at point j. */
@@ -788,6 +794,18 @@ class CNumerics {
     Thermal_Conductivity_ve_j = val_thermal_conductivity_ve_j;
   }
 
+  /*!
+   * \brief Set the thermal diffusivity (translational/rotational)
+   * \param[in] val_thermal_diffusivity_i - Value of the thermal diffusivity at point i.
+   * \param[in] val_thermal_diffusivity_j - Value of the thermal diffusivity at point j.
+   * \param[in] iSpecies - Value of the species.
+   */
+  inline void SetThermalDiffusivity(su2double val_thermal_diffusivity_i,
+                                    su2double val_thermal_diffusivity_j) {
+    Thermal_Diffusivity_i = val_thermal_diffusivity_i;
+    Thermal_Diffusivity_j = val_thermal_diffusivity_j;
+  }
+  
   /*!
    * \brief Set the specifc heat c_p.
    * \param[in] val_specific_heat_i - Value of the specific heat at point i.
@@ -920,6 +938,16 @@ class CNumerics {
     SoundSpeed_j = val_soundspeed_j;
   }
 
+  /*!
+   * \brief Set the value of the temperature.
+   * \param[in] val_temp_i - Value of the temperature at point i.
+   * \param[in] val_temp_j - Value of the temperature at point j.
+   */
+  inline void SetTemperature(su2double val_temp_i, su2double val_temp_j) {
+    Temp_i = val_temp_i;
+    Temp_j = val_temp_j;
+  }
+
   /*!
    * \brief Set the value of the enthalpy.
    * \param[in] val_enthalpy_i - Value of the enthalpy at point i.
diff --git a/SU2_CFD/include/numerics/heat.hpp b/SU2_CFD/include/numerics/heat.hpp
index a07a0fe6b97..2713c5906e6 100644
--- a/SU2_CFD/include/numerics/heat.hpp
+++ b/SU2_CFD/include/numerics/heat.hpp
@@ -27,9 +27,41 @@
 
 #pragma once
 
-#include "scalar/scalar_diffusion.hpp"
-#include "scalar/scalar_convection.hpp"
-#include "../variables/CIncEulerVariable.hpp"
+#include "CNumerics.hpp"
+
+/*!
+ * \class CCentSca_Heat
+ * \brief Class for scalar centered scheme.
+ * \ingroup ConvDiscr
+ * \author O. Burghardt
+ * \version 7.5.0 "Blackbird"
+ */
+class CCentSca_Heat : public CNumerics {
+private:
+  su2double Param_Kappa_4;         /*!< \brief Artificial dissipation parameters. */
+  bool implicit;                   /*!< \brief Implicit calculation. */
+  bool dynamic_grid;               /*!< \brief Modification for grid movement. */
+
+public:
+  /*!
+   * \brief Constructor of the class.
+   * \param[in] val_nDim - Number of dimension of the problem.
+   * \param[in] val_nVar - Number of variables of the problem.
+   * \param[in] config - Definition of the particular problem.
+   */
+  CCentSca_Heat(unsigned short val_nDim, unsigned short val_nVar, const CConfig *config);
+
+  /*!
+   * \brief Compute the flow residual using a JST method.
+   * \param[out] val_resconv - Pointer to the convective residual.
+   * \param[out] val_resvisc - Pointer to the artificial viscosity residual.
+   * \param[out] val_Jacobian_i - Jacobian of the numerical method at node i (implicit computation).
+   * \param[out] val_Jacobian_j - Jacobian of the numerical method at node j (implicit computation).
+   * \param[in] config - Definition of the particular problem.
+   */
+  void ComputeResidual(su2double *val_residual, su2double **val_Jacobian_i, su2double **val_Jacobian_j,
+                       CConfig *config) override;
+};
 
 /*!
  * \class CUpwSca_Heat
@@ -38,31 +70,27 @@
  * \author O. Burghardt.
  * \version 7.5.0 "Blackbird"
  */
-class CUpwSca_Heat final : public CUpwScalar<typename CIncEulerVariable::template CIndices<unsigned short>> {
- public:
+class CUpwSca_Heat : public CNumerics {
+private:
+  bool implicit, dynamic_grid;
+
+public:
   /*!
    * \brief Constructor of the class.
    * \param[in] val_nDim - Number of dimensions of the problem.
+   * \param[in] val_nVar - Number of variables of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  CUpwSca_Heat(unsigned short val_nDim, const CConfig *config)
-    : CUpwScalar<typename CIncEulerVariable::template CIndices<unsigned short>>(val_nDim, 1, config) {}
-
- private:
-  /*!
-   * \brief Adds extra variables to AD
-   */
-  void ExtraADPreaccIn(void) override {}
+  CUpwSca_Heat(unsigned short val_nDim, unsigned short val_nVar, const CConfig *config);
 
   /*!
-   * \brief Heat-specific specific steps in the ComputeResidual method
+   * \brief Compute the scalar upwind flux between two nodes i and j.
+   * \param[out] val_residual - Pointer to the total residual.
+   * \param[out] val_Jacobian_i - Jacobian of the numerical method at node i (implicit computation).
+   * \param[out] val_Jacobian_j - Jacobian of the numerical method at node j (implicit computation).
    * \param[in] config - Definition of the particular problem.
    */
-  void FinishResidualCalc(const CConfig* config) override {
-    Flux[0] = a0 * ScalarVar_i[0] + a1 * ScalarVar_j[0];
-    Jacobian_i[0][0] = a0;
-    Jacobian_j[0][0] = a1;
-  }
+  void ComputeResidual(su2double *val_residual, su2double **val_Jacobian_i, su2double **val_Jacobian_j, CConfig *config) override;
 };
 
 /*!
@@ -72,36 +100,26 @@ class CUpwSca_Heat final : public CUpwScalar<typename CIncEulerVariable::templat
  * \author O. Burghardt.
  * \version 7.5.0 "Blackbird"
  */
-class CAvgGrad_Heat final : public CAvgGrad_Scalar<CNoFlowIndices> {
- public:
+class CAvgGrad_Heat : public CNumerics {
+private:
+  bool implicit, correct;
+
+public:
   /*!
    * \brief Constructor of the class.
    * \param[in] val_nDim - Number of dimensions of the problem.
+   * \param[in] val_nVar - Number of variables of the problem.
    * \param[in] config - Definition of the particular problem.
-   * \param[in] correct - Whether to correct the gradient.
-   */
-  CAvgGrad_Heat(unsigned short val_nDim, const CConfig *config, bool correct)
-    : CAvgGrad_Scalar<CNoFlowIndices>(val_nDim, 1, correct, config) {}
-
- private:
-  /*!
-   * \brief Adds extra variables to AD
+   * \param[in] correct - Correct the gradient.
    */
-  void ExtraADPreaccIn(void) override {
-    AD::SetPreaccIn(*Diffusion_Coeff_i, *Diffusion_Coeff_j);
-  }
+  CAvgGrad_Heat(unsigned short val_nDim, unsigned short val_nVar, const CConfig *config, bool correct);
 
   /*!
-   * \brief Heat-specific specific steps in the ComputeResidual method
+   * \brief Compute the viscous heat residual using an average of gradients with correction.
+   * \param[out] val_residual - Pointer to the total residual.
+   * \param[out] Jacobian_i - Jacobian of the numerical method at node i (implicit computation).
+   * \param[out] Jacobian_j - Jacobian of the numerical method at node j (implicit computation).
    * \param[in] config - Definition of the particular problem.
    */
-  void FinishResidualCalc(const CConfig* config) override {
-    const su2double Thermal_Diffusivity_Mean = 0.5 * (*Diffusion_Coeff_i + *Diffusion_Coeff_j);
-
-    Flux[0] = Thermal_Diffusivity_Mean * Proj_Mean_GradScalarVar[0];
-
-    /*--- Use TSL for Jacobians. ---*/
-    Jacobian_i[0][0] = -Thermal_Diffusivity_Mean * proj_vector_ij;
-    Jacobian_j[0][0] = Thermal_Diffusivity_Mean * proj_vector_ij;
-  }
+  void ComputeResidual(su2double *val_residual, su2double **Jacobian_i, su2double **Jacobian_j, CConfig *config) override;
 };
diff --git a/SU2_CFD/include/solvers/CHeatSolver.hpp b/SU2_CFD/include/solvers/CHeatSolver.hpp
index 7f0df9a9ca8..6c99c69c26c 100644
--- a/SU2_CFD/include/solvers/CHeatSolver.hpp
+++ b/SU2_CFD/include/solvers/CHeatSolver.hpp
@@ -27,7 +27,7 @@
 
 #pragma once
 
-#include "CScalarSolver.hpp"
+#include "CSolver.hpp"
 #include "../variables/CHeatVariable.hpp"
 
 /*!
@@ -36,7 +36,7 @@
  * \author O. Burghardt
  * \version 7.5.0 "Blackbird"
  */
-class CHeatSolver final : public CScalarSolver<CHeatVariable> {
+class CHeatSolver final : public CSolver {
 protected:
   static constexpr size_t MAXNDIM = 3; /*!< \brief Max number of space dimensions, used in some static arrays. */
   static constexpr size_t MAXNVAR = 1; /*!< \brief Max number of variables, for static arrays. */
@@ -44,91 +44,27 @@ class CHeatSolver final : public CScalarSolver<CHeatVariable> {
   const bool flow; /*!< \brief Use solver as a scalar transport equation of Temperature for the inc solver. */
   const bool heat_equation; /*!< \brief use solver for heat conduction in solids. */
 
-  su2double Global_Delta_Time = 0.0, Global_Delta_UnstTimeND = 0.0;
-
-  vector<vector<su2double>> HeatFlux;
+  unsigned short nVarFlow, nMarker;
+  vector<vector<su2double> > HeatFlux;
   vector<su2double> HeatFlux_per_Marker;
   su2double Total_HeatFlux;
   su2double AllBound_HeatFlux;
   vector<su2double> AverageT_per_Marker;
   su2double Total_AverageT;
   su2double AllBound_AverageT;
+  vector<su2double>  Primitive_Flow_i;
+  vector<su2double> Primitive_Flow_j;
   vector<su2double> Surface_Areas;
   su2double Total_HeatFlux_Areas;
   su2double Total_HeatFlux_Areas_Monitor;
   vector<su2activematrix> ConjugateVar;
 
-  /*!
-   * \brief Applies an isothermal condition to a vertex of a marker.
-   */
-  void IsothermalBoundaryCondition(CGeometry *geometry, CSolver *flow_solver, const CConfig *config,
-                                   unsigned short iMarker, unsigned long iVertex, const su2double& temperature) {
-
-    const auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
-    if (!geometry->nodes->GetDomain(iPoint)) return;
-
-    const bool implicit = config->GetKind_TimeIntScheme() == EULER_IMPLICIT;
-    const su2double prandtl_lam = config->GetPrandtl_Lam();
-    const su2double const_diffusivity = config->GetThermalDiffusivity();
-
-    const auto Point_Normal = geometry->vertex[iMarker][iVertex]->GetNormal_Neighbor();
-
-    const auto* Normal = geometry->vertex[iMarker][iVertex]->GetNormal();
-    const su2double Area = GeometryToolbox::Norm(nDim, Normal);
-
-    const auto* Coord_i = geometry->nodes->GetCoord(iPoint);
-    const auto* Coord_j = geometry->nodes->GetCoord(Point_Normal);
-    const su2double dist_ij = GeometryToolbox::Distance(nDim, Coord_i, Coord_j);
-
-    const su2double dTdn = -(nodes->GetTemperature(Point_Normal) - temperature) / dist_ij;
-
-    su2double thermal_diffusivity = const_diffusivity;
-    if (flow) {
-      thermal_diffusivity = flow_solver->GetNodes()->GetLaminarViscosity(iPoint) / prandtl_lam;
-    }
-    LinSysRes(iPoint, 0) -= thermal_diffusivity * dTdn * Area;
-
-    if (implicit) {
-      su2double Jacobian_i[] = {-thermal_diffusivity / dist_ij * Area};
-      Jacobian.SubtractBlock2Diag(iPoint, &Jacobian_i);
-    }
-  }
+  CHeatVariable* nodes = nullptr;  /*!< \brief The highest level in the variable hierarchy this solver can safely use. */
 
   /*!
-   * \brief Compute the viscous flux for the scalar equation at a particular edge.
-   * \param[in] iEdge - Edge for which we want to compute the flux
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] numerics - Description of the numerical method.
-   * \param[in] config - Definition of the particular problem.
-   * \note Calls a generic implementation after defining a SolverSpecificNumerics object.
+   * \brief Return nodes to allow CSolver::base_nodes to be set.
    */
-  inline void Viscous_Residual(unsigned long iEdge, CGeometry* geometry, CSolver** solver_container,
-                                       CNumerics* numerics, CConfig* config) override {
-    const CVariable* flow_nodes = flow ? solver_container[FLOW_SOL]->GetNodes() : nullptr;
-
-    const su2double const_diffusivity = config->GetThermalDiffusivity();
-    const su2double pr_lam = config->GetPrandtl_Lam();
-    const su2double pr_turb = config->GetPrandtl_Turb();
-
-    su2double thermal_diffusivity_i{}, thermal_diffusivity_j{};
-
-    /*--- Computes the thermal diffusivity to use in the viscous numerics. ---*/
-    auto compute_thermal_diffusivity = [&](unsigned long iPoint, unsigned long jPoint) {
-      if (flow) {
-        thermal_diffusivity_i = flow_nodes->GetLaminarViscosity(iPoint) / pr_lam +
-                                flow_nodes->GetEddyViscosity(iPoint) / pr_turb;
-        thermal_diffusivity_j = flow_nodes->GetLaminarViscosity(jPoint) / pr_lam +
-                                flow_nodes->GetEddyViscosity(jPoint) / pr_turb;
-        numerics->SetDiffusionCoeff(&thermal_diffusivity_i, &thermal_diffusivity_j);
-      }
-      else {
-        numerics->SetDiffusionCoeff(&const_diffusivity, &const_diffusivity);
-      }
-    };
-    /*--- Compute residual and Jacobians. ---*/
-    Viscous_Residual_impl(compute_thermal_diffusivity, iEdge, geometry, solver_container, numerics, config);
-  }
+  inline CVariable* GetBaseClassPointerToNodes() override { return nodes; }
 
 public:
 
@@ -137,6 +73,11 @@ class CHeatSolver final : public CScalarSolver<CHeatVariable> {
    */
   CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iMesh);
 
+  /*!
+   * \brief Destructor of the class.
+   */
+  ~CHeatSolver(void) override;
+
   /*!
    * \brief Restart residual and compute gradients.
    * \param[in] geometry - Geometrical definition of the problem.
@@ -155,6 +96,18 @@ class CHeatSolver final : public CScalarSolver<CHeatVariable> {
                     unsigned short RunTime_EqSystem,
                     bool Output) override;
 
+  /*!
+   * \brief A virtual member.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] iMesh - Index of the mesh in multigrid computations.
+   */
+  void Postprocessing(CGeometry *geometry,
+                      CSolver **solver_container,
+                      CConfig *config,
+                      unsigned short iMesh) override;
+
   /*!
    * \brief Load a solution from a restart file.
    * \param[in] geometry - Geometrical definition of the problem.
@@ -169,6 +122,21 @@ class CHeatSolver final : public CScalarSolver<CHeatVariable> {
                    int val_iter,
                    bool val_update_geo) override;
 
+  /*!
+   * \brief Compute the spatial integration using a centered scheme.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] numerics_container - Description of the numerical method.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] iMesh - Index of the mesh in multigrid computations.
+   * \param[in] iRKStep - Current step of the Runge-Kutta iteration.
+   */
+  void Centered_Residual(CGeometry *geometry,
+                        CSolver **solver_container,
+                        CNumerics **numerics_container,
+                        CConfig *config,
+                        unsigned short iMesh,
+                        unsigned short iRKStep) override;
   /*!
    * \brief Compute the spatial integration using a upwind scheme.
    * \param[in] geometry - Geometrical definition of the problem.
@@ -279,6 +247,15 @@ class CHeatSolver final : public CScalarSolver<CHeatVariable> {
                                   CConfig *config,
                                   unsigned short val_marker) override;
 
+  /*!
+   * \brief Impose a periodic boundary condition by summing contributions from the complete control volume.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] numerics - Description of the numerical method.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void BC_Periodic(CGeometry* geometry, CSolver** solver_container, CNumerics* numerics, CConfig* config) final;
+
   /*!
    * \brief Set the conjugate heat variables.
    * \param[in] val_marker        - marker index
@@ -353,6 +330,26 @@ class CHeatSolver final : public CScalarSolver<CHeatVariable> {
     }
   }
 
+  /*!
+   * \brief Update the solution using an implicit solver.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void ImplicitEuler_Iteration(CGeometry *geometry,
+                               CSolver **solver_container,
+                               CConfig *config) override;
+
+  /*!
+   * \brief Update the solution using an explicit solver.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void ExplicitEuler_Iteration(CGeometry *geometry,
+                               CSolver **solver_container,
+                               CConfig *config) override;
+
   /*!
    * \brief A virtual member.
    * \param[in] geometry - Geometrical definition of the problem.
@@ -402,4 +399,5 @@ class CHeatSolver final : public CScalarSolver<CHeatVariable> {
    * \return Value of the heat flux.
    */
   inline su2double GetHeatFlux(unsigned short val_marker, unsigned long val_vertex) const override { return HeatFlux[val_marker][val_vertex]; }
+
 };
diff --git a/SU2_CFD/include/variables/CHeatVariable.hpp b/SU2_CFD/include/variables/CHeatVariable.hpp
index b093cc8f284..8daeaffbddf 100644
--- a/SU2_CFD/include/variables/CHeatVariable.hpp
+++ b/SU2_CFD/include/variables/CHeatVariable.hpp
@@ -27,7 +27,7 @@
 
 #pragma once
 
-#include "CScalarVariable.hpp"
+#include "CVariable.hpp"
 
 /*!
  * \class CHeatVariable
@@ -35,10 +35,12 @@
  * \author O. Burghardt
  * \version 7.5.0 "Blackbird"
  */
-class CHeatVariable final : public CScalarVariable {
-public:
-  static constexpr size_t MAXNVAR = 1; /*!< \brief Max number of variables, for static arrays. */
+class CHeatVariable final : public CVariable {
+protected:
+  CVectorOfMatrix& Gradient_Reconstruction;  /*!< \brief Reference to the gradient of the primitive variables for MUSCL reconstruction for the convective term */
+  CVectorOfMatrix Gradient_Aux;              /*!< \brief Auxiliary structure to store a second gradient for reconstruction, if required. */
 
+public:
   /*!
    * \brief Constructor of the class.
    * \param[in] heat - Values of the Heat solution (initialization value).
@@ -49,10 +51,29 @@ class CHeatVariable final : public CScalarVariable {
    */
   CHeatVariable(su2double heat, unsigned long npoint, unsigned long ndim, unsigned long nvar, CConfig *config);
 
+  /*!
+   * \brief Destructor of the class.
+   */
+  ~CHeatVariable() override = default;
+
+  /*!
+   * \brief Get the array of the reconstruction variables gradient at a node.
+   * \param[in] iPoint - Index of the current node.
+   * \return Array of the reconstruction variables gradient at a node.
+   */
+  inline CMatrixView<su2double> GetGradient_Reconstruction(unsigned long iPoint) final { return Gradient_Reconstruction[iPoint]; }
+
+  /*!
+   * \brief Get the reconstruction gradient for primitive variable at all points.
+   * \return Reference to variable reconstruction gradient.
+   */
+  inline CVectorOfMatrix& GetGradient_Reconstruction() final { return Gradient_Reconstruction; }
+  inline const CVectorOfMatrix& GetGradient_Reconstruction() const final { return Gradient_Reconstruction; }
+
   /*!
    * \brief Get the temperature of the point.
    * \return Value of the temperature of the point.
    */
-  inline su2double GetTemperature(unsigned long iPoint) const final { return Solution(iPoint, 0); }
+  inline su2double GetTemperature(unsigned long iPoint) const final { return Solution(iPoint,0); }
 
 };
diff --git a/SU2_CFD/obj/Makefile.am b/SU2_CFD/obj/Makefile.am
index e53ecb7c02a..87e6a9561d1 100644
--- a/SU2_CFD/obj/Makefile.am
+++ b/SU2_CFD/obj/Makefile.am
@@ -86,6 +86,7 @@ libSU2Core_sources = ../src/definition_structure.cpp \
   ../src/numerics/CNumerics.cpp \
   ../src/numerics/template.cpp \
   ../src/numerics/transition.cpp \
+  ../src/numerics/heat.cpp \
   ../src/numerics/radiation.cpp \
   ../src/numerics/CLookUpTable.cpp \
   ../src/numerics/CTrapezoidalMap.cpp \
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index dca735e062f..8b1667aad50 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -1461,6 +1461,7 @@ void CDriver::Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSol
     cout << endl <<"------------------- Numerics Preprocessing ( Zone " << config->GetiZone() <<" ) -------------------" << endl;
 
   unsigned short iMGlevel, iSol,
+
   nVar_Template         = 0,
   nVar_Flow             = 0,
   nVar_NEMO             = 0,
@@ -1472,7 +1473,8 @@ void CDriver::Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSol
   nVar_Adj_Flow         = 0,
   nVar_Adj_Turb         = 0,
   nVar_FEM              = 0,
-  nVar_Rad              = 0;
+  nVar_Rad              = 0,
+  nVar_Heat             = 0;
 
   numerics = new CNumerics***[config->GetnMGLevels()+1] ();
 
@@ -1589,6 +1591,7 @@ void CDriver::Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSol
   if (fem_ns)       nVar_Flow = solver[MESH_0][FLOW_SOL]->GetnVar();
 
   if (fem)          nVar_FEM = solver[MESH_0][FEA_SOL]->GetnVar();
+  if (heat)         nVar_Heat = solver[MESH_0][HEAT_SOL]->GetnVar();
 
   if (config->AddRadiation()) nVar_Rad = solver[MESH_0][RAD_SOL]->GetnVar();
 
@@ -1907,13 +1910,8 @@ void CDriver::Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSol
       else if ((incompressible && (config->GetKind_Streamwise_Periodic() != ENUM_STREAMWISE_PERIODIC::NONE)) &&
                (config->GetEnergy_Equation() && !config->GetStreamwise_Periodic_Temperature()))
         numerics[iMGlevel][FLOW_SOL][source_second_term] = new CSourceIncStreamwisePeriodic_Outlet(nDim, nVar_Flow, config);
-      else if (config->GetVorticityConfinement() == YES) {
-        /*--- Vorticity Confinement term as a second source term to allow the use of VC along with other source terms ---*/
-        numerics[iMGlevel][FLOW_SOL][source_second_term] = new CSourceVorticityConfinement(nDim, nVar_Flow, config);
-      }
       else
         numerics[iMGlevel][FLOW_SOL][source_second_term] = new CSourceNothing(nDim, nVar_Flow, config);
-
     }
 
   }
@@ -2116,14 +2114,19 @@ void CDriver::Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSol
     /*--- Definition of the viscous scheme for each equation and mesh level ---*/
     for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
 
-      numerics[iMGlevel][HEAT_SOL][visc_term] = new CAvgGrad_Heat(nDim, config, true);
-      numerics[iMGlevel][HEAT_SOL][visc_bound_term] = new CAvgGrad_Heat(nDim, config, false);
+      numerics[iMGlevel][HEAT_SOL][visc_term] = new CAvgGrad_Heat(nDim, nVar_Heat, config, true);
+      numerics[iMGlevel][HEAT_SOL][visc_bound_term] = new CAvgGrad_Heat(nDim, nVar_Heat, config, false);
 
       switch (config->GetKind_ConvNumScheme_Heat()) {
 
         case SPACE_UPWIND :
-          numerics[iMGlevel][HEAT_SOL][conv_term] = new CUpwSca_Heat(nDim, config);
-          numerics[iMGlevel][HEAT_SOL][conv_bound_term] = new CUpwSca_Heat(nDim, config);
+          numerics[iMGlevel][HEAT_SOL][conv_term] = new CUpwSca_Heat(nDim, nVar_Heat, config);
+          numerics[iMGlevel][HEAT_SOL][conv_bound_term] = new CUpwSca_Heat(nDim, nVar_Heat, config);
+          break;
+
+        case SPACE_CENTERED :
+          numerics[iMGlevel][HEAT_SOL][conv_term] = new CCentSca_Heat(nDim, nVar_Heat, config);
+          numerics[iMGlevel][HEAT_SOL][conv_bound_term] = new CUpwSca_Heat(nDim, nVar_Heat, config);
           break;
 
         default:
diff --git a/SU2_CFD/src/meson.build b/SU2_CFD/src/meson.build
index fa8be4fc1cd..999055decb8 100644
--- a/SU2_CFD/src/meson.build
+++ b/SU2_CFD/src/meson.build
@@ -118,7 +118,8 @@ su2_cfd_src += files(['solvers/CSolverFactory.cpp',
                       'solvers/CGradientSmoothingSolver.cpp'])
 
 su2_cfd_src += files(['numerics/CNumerics.cpp',
-                      'numerics/template.cpp',
+                      'numerics/template.cpp',                      
+                      'numerics/heat.cpp',
                       'numerics/radiation.cpp',
                       'numerics/flow/convection/roe.cpp',
                       'numerics/flow/convection/fds.cpp',
diff --git a/SU2_CFD/src/numerics/flow/flow_sources.cpp b/SU2_CFD/src/numerics/flow/flow_sources.cpp
index 8c5b737215d..fc2e3477224 100644
--- a/SU2_CFD/src/numerics/flow/flow_sources.cpp
+++ b/SU2_CFD/src/numerics/flow/flow_sources.cpp
@@ -259,8 +259,8 @@ CNumerics::ResidualType<> CSourceIncAxisymmetric_Flow::ComputeResidual(const CCo
 
     /*--- Set primitive variables at points iPoint. ---*/
 
-    const su2double Temp_i = V_i[nDim+1];
     Pressure_i    = V_i[0];
+    Temp_i        = V_i[nDim+1];
     DensityInc_i  = V_i[nDim+2];
     BetaInc2_i    = V_i[nDim+3];
     Cp_i          = V_i[nDim+7];
@@ -616,105 +616,6 @@ CNumerics::ResidualType<> CSourceIncRotatingFrame_Flow::ComputeResidual(const CC
   return ResidualType<>(residual, jacobian, nullptr);
 }
 
-CSourceVorticityConfinement::CSourceVorticityConfinement(unsigned short val_nDim, unsigned short val_nVar,
-                                                         const CConfig* config)
-    : CSourceBase_Flow(val_nDim, val_nVar, config) {
-  Gamma = config->GetGamma();
-  Gamma_Minus_One = Gamma - 1.0;
-}
-
-CNumerics::ResidualType<> CSourceVorticityConfinement::ComputeResidual(const CConfig* config) {
-  /*--- density, \rho ---*/
-  const su2double rho = V_i[nDim + 2];
-
-  /*--- velocity, U = (u, v, w) ---*/
-  su2double U[3] = {V_i[1], V_i[2], 0.0};
-  if (nDim == 3) U[2] = V_i[3];
-  const su2double U_abs = max(GeometryToolbox::Norm(3, U), 1e-12);
-
-  /*--- vorticity, \omega ---*/
-  const su2double omega[3] = {Vorticity_i[0], Vorticity_i[1], Vorticity_i[2]};
-
-  /*--- grad of the mag of vorticity, \nabla|\omega| = AuxVar_Grad_i[0] ---*/
-  const su2double omega_abs_grad_abs = max(GeometryToolbox::Norm(3, AuxVar_Grad_i[0]), 1e-12);
-
-  /*--- unit vector, n along \nabla|\omega| ---*/
-  const su2double n[3] = {
-      AuxVar_Grad_i[0][0] / omega_abs_grad_abs,
-      AuxVar_Grad_i[0][1] / omega_abs_grad_abs,
-      AuxVar_Grad_i[0][2] / omega_abs_grad_abs,
-  };
-
-  /*--- n \cross \omega ---*/
-  su2double nXomega[3] = {0.0, 0.0, 0.0};
-  GeometryToolbox::CrossProduct(n, omega, nXomega);
-  const su2double nXomega_U = GeometryToolbox::DotProduct(3, nXomega, U);
-
-  /*--- vorticity confinement parameter ---*/
-  const su2double vc_config = config->GetConfinement_Param();
-  su2double vc = vc_config * (1 + log10(pow((1 + (Volume / AvgVolume)), 1.0 / 3.0)));
-
-  /*--- correction to vc near viscous wall ---*/
-  const bool viscous = config->GetViscous();
-  if (viscous) {
-    su2double U_infty[3] = {config->GetVelocity_FreeStreamND()[0], config->GetVelocity_FreeStreamND()[1], 0.0};
-    if (nDim == 3) U_infty[2] = config->GetVelocity_FreeStreamND()[2];
-    const su2double U_infty_abs = max(GeometryToolbox::Norm(3, U_infty), 1e-12);
-    const su2double L = config->GetLength_Reynolds();
-    const su2double mu = V_i[nDim + 5];                   // viscosity
-    const su2double mu_t = V_i[nDim + 6];                 // turbulent or eddy viscosity
-    const su2double mu_eff = mu + mu_t;                   // effective or total viscosity
-    const su2double Re = rho * U_infty_abs * L / mu_eff;  // Reynolds number
-    const su2double delta = 5 * L / sqrt(Re);             // boundary layer thickness
-
-    if (dist_i <= 4 * delta) {
-      vc *= 0.0;
-    }
-  }
-
-  /*--- source terms: S / rho ---*/
-  const su2double vc_Uabs_Volume = vc * U_abs * Volume;
-  const su2double S_u_rho = -nXomega[0] * vc_Uabs_Volume;
-  const su2double S_v_rho = -nXomega[1] * vc_Uabs_Volume;
-  const su2double S_w_rho = -nXomega[2] * vc_Uabs_Volume;
-  const su2double S_E_rho = -nXomega_U * vc_Uabs_Volume;
-
-  residual[0] = 0.0;
-  residual[1] = rho * S_u_rho;
-  residual[2] = rho * S_v_rho;
-  if (nDim == 2) {
-    residual[3] = rho * S_E_rho;
-  }
-  if (nDim == 3) {
-    residual[3] = rho * S_w_rho;
-    residual[4] = rho * S_E_rho;
-  }
-
-  const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
-  if (implicit) {
-    for (unsigned iVar = 0; iVar < nVar; iVar++) {
-      for (unsigned jVar = 0; jVar < nVar; jVar++) {
-        jacobian[iVar][jVar] = 0.0;
-      }
-    }
-
-    jacobian[1][0] = S_u_rho;
-    jacobian[2][0] = S_v_rho;
-    if (nDim == 2) {
-      jacobian[3][1] = S_u_rho;
-      jacobian[3][2] = S_v_rho;
-    }
-    if (nDim == 3) {
-      jacobian[3][0] = S_w_rho;
-      jacobian[4][1] = S_u_rho;
-      jacobian[4][2] = S_v_rho;
-      jacobian[4][3] = S_w_rho;
-    }
-  }
-
-  return ResidualType<>(residual, jacobian, nullptr);
-}
-
 CSourceWindGust::CSourceWindGust(unsigned short val_nDim, unsigned short val_nVar, const CConfig* config) :
                  CSourceBase_Flow(val_nDim, val_nVar, config) { }
 
diff --git a/SU2_CFD/src/numerics/heat.cpp b/SU2_CFD/src/numerics/heat.cpp
new file mode 100644
index 00000000000..177fc0b452f
--- /dev/null
+++ b/SU2_CFD/src/numerics/heat.cpp
@@ -0,0 +1,202 @@
+/*!
+ * \file heat.cpp
+ * \brief Implementation of numerics classes for heat transfer.
+ * \author F. Palacios, T. Economon
+ * \version 7.5.0 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+
+#include "../../include/numerics/heat.hpp"
+#include "../../../Common/include/toolboxes/geometry_toolbox.hpp"
+
+CCentSca_Heat::CCentSca_Heat(unsigned short val_nDim, unsigned short val_nVar, const CConfig *config) :
+               CNumerics(val_nDim, val_nVar, config) {
+
+  implicit = (config->GetKind_TimeIntScheme_Turb() == EULER_IMPLICIT);
+  dynamic_grid = config->GetDynamic_Grid();
+  Param_Kappa_4 = config->GetKappa_4th_Heat();
+
+}
+
+void CCentSca_Heat::ComputeResidual(su2double *val_residual, su2double **val_Jacobian_i,
+                                    su2double **val_Jacobian_j, CConfig *config) {
+  AD::StartPreacc();
+  AD::SetPreaccIn(V_i, nDim+3); AD::SetPreaccIn(V_j, nDim+3);
+  AD::SetPreaccIn(Temp_i); AD::SetPreaccIn(Temp_j);
+  AD::SetPreaccIn(Und_Lapl_i, nVar); AD::SetPreaccIn(Und_Lapl_j, nVar);
+  AD::SetPreaccIn(Normal, nDim);
+  if (dynamic_grid) {
+    AD::SetPreaccIn(GridVel_i, nDim); AD::SetPreaccIn(GridVel_j, nDim);
+  }
+
+  /*--- Primitive variables at point i and j ---*/
+
+  Pressure_i =    V_i[0];       Pressure_j = V_j[0];
+  DensityInc_i =  V_i[nDim+2];  DensityInc_j = V_j[nDim+2];
+  BetaInc2_i =    V_i[nDim+3];  BetaInc2_j = V_j[nDim+3];
+
+  /*--- Projected velocities at the current edge ---*/
+
+  su2double ProjVelocity_i = 0.0;
+  su2double ProjVelocity_j = 0.0;
+
+  if (dynamic_grid) {
+    for (unsigned short iDim = 0; iDim < nDim; iDim++) {
+      su2double Velocity_i = V_i[iDim+1] - GridVel_i[iDim];
+      su2double Velocity_j = V_j[iDim+1] - GridVel_j[iDim];
+      ProjVelocity_i += Velocity_i*Normal[iDim];
+      ProjVelocity_j += Velocity_j*Normal[iDim];
+    }
+  }
+  else {
+    for (unsigned short iDim = 0; iDim < nDim; iDim++) {
+      ProjVelocity_i += V_i[iDim+1]*Normal[iDim];
+      ProjVelocity_j += V_j[iDim+1]*Normal[iDim];
+    }
+  }
+
+  /*--- Computing the second order centered scheme part ---*/
+
+  const su2double ProjVelocity = 0.5*(ProjVelocity_i+ProjVelocity_j);
+
+  val_residual[0] = 0.5*(Temp_i + Temp_j)*ProjVelocity;
+
+  if (implicit) {
+    val_Jacobian_i[0][0] = 0.5*ProjVelocity;
+    val_Jacobian_j[0][0] = 0.5*ProjVelocity;
+  }
+
+  /*--- Adding artificial dissipation to stabilize the centered scheme ---*/
+
+  const su2double Diff_Lapl = Und_Lapl_i[0]-Und_Lapl_j[0];
+  const su2double Area2 = GeometryToolbox::SquaredNorm(nDim, Normal);
+
+  const su2double SoundSpeed_i = sqrt(pow(ProjVelocity_i,2) + (BetaInc2_i/DensityInc_i)*Area2);
+  const su2double SoundSpeed_j = sqrt(pow(ProjVelocity_j,2) + (BetaInc2_j/DensityInc_j)*Area2);
+
+  const su2double Local_Lambda_i = fabs(ProjVelocity_i)+SoundSpeed_i;
+  const su2double Local_Lambda_j = fabs(ProjVelocity_j)+SoundSpeed_j;
+  const su2double MeanLambda = 0.5*(Local_Lambda_i+Local_Lambda_j);
+
+  val_residual[0] += -Param_Kappa_4*Diff_Lapl*MeanLambda;
+
+  if (implicit) {
+    const su2double cte_0 = Param_Kappa_4*su2double(Neighbor_i+1)*MeanLambda;
+    const su2double cte_1 = Param_Kappa_4*su2double(Neighbor_j+1)*MeanLambda;
+
+    val_Jacobian_i[0][0] += cte_0;
+    val_Jacobian_j[0][0] -= cte_1;
+  }
+
+  AD::SetPreaccOut(val_residual[0]);
+  AD::EndPreacc();
+
+}
+
+CUpwSca_Heat::CUpwSca_Heat(unsigned short val_nDim, unsigned short val_nVar, const CConfig *config) :
+              CNumerics(val_nDim, val_nVar, config) {
+
+  implicit = (config->GetKind_TimeIntScheme_Turb() == EULER_IMPLICIT);
+  dynamic_grid = config->GetDynamic_Grid();
+
+}
+
+void CUpwSca_Heat::ComputeResidual(su2double *val_residual, su2double **val_Jacobian_i,
+                                   su2double **val_Jacobian_j, CConfig *config) {
+
+  AD::StartPreacc();
+  AD::SetPreaccIn(V_i, nDim+1); AD::SetPreaccIn(V_j, nDim+1);
+  AD::SetPreaccIn(Temp_i); AD::SetPreaccIn(Temp_j);
+  AD::SetPreaccIn(Normal, nDim);
+  if (dynamic_grid) {
+    AD::SetPreaccIn(GridVel_i, nDim); AD::SetPreaccIn(GridVel_j, nDim);
+  }
+
+  su2double q_ij = 0.0;
+
+  if (dynamic_grid) {
+    for (unsigned short iDim = 0; iDim < nDim; iDim++) {
+      const su2double Velocity_i = V_i[iDim+1] - GridVel_i[iDim];
+      const su2double Velocity_j = V_j[iDim+1] - GridVel_j[iDim];
+      q_ij += 0.5*(Velocity_i+Velocity_j)*Normal[iDim];
+    }
+  }
+  else {
+    for (unsigned short iDim = 0; iDim < nDim; iDim++) {
+      q_ij += 0.5*(V_i[iDim+1]+V_j[iDim+1])*Normal[iDim];
+    }
+  }
+
+  const su2double a0 = 0.5*(q_ij+fabs(q_ij));
+  const su2double a1 = 0.5*(q_ij-fabs(q_ij));
+
+  val_residual[0] = a0*Temp_i+a1*Temp_j;
+
+  if (implicit) {
+    val_Jacobian_i[0][0] = a0;
+    val_Jacobian_j[0][0] = a1;
+  }
+
+  AD::SetPreaccOut(val_residual[0]);
+  AD::EndPreacc();
+
+}
+
+CAvgGrad_Heat::CAvgGrad_Heat(unsigned short val_nDim, unsigned short val_nVar,
+                             const CConfig *config, bool correct_) :
+               CNumerics(val_nDim, val_nVar, config) {
+
+  implicit = (config->GetKind_TimeIntScheme_Heat() == EULER_IMPLICIT);
+  correct = correct_;
+}
+
+void CAvgGrad_Heat::ComputeResidual(su2double *val_residual, su2double **Jacobian_i,
+                                    su2double **Jacobian_j, CConfig *config) {
+  constexpr int nVar = 1;
+
+  AD::StartPreacc();
+  AD::SetPreaccIn(Coord_i, nDim); AD::SetPreaccIn(Coord_j, nDim);
+  AD::SetPreaccIn(Normal, nDim);
+  AD::SetPreaccIn(Temp_i); AD::SetPreaccIn(Temp_j);
+  AD::SetPreaccIn(ConsVar_Grad_i[0],nDim); AD::SetPreaccIn(ConsVar_Grad_j[0],nDim);
+  AD::SetPreaccIn(Thermal_Diffusivity_i); AD::SetPreaccIn(Thermal_Conductivity_j);
+
+  su2double NormalGrad[nVar], CorrectedGrad[nVar];
+
+  auto proj_vector_ij = ComputeProjectedGradient(nDim, nVar, Normal, Coord_i, Coord_j, ConsVar_Grad_i,
+                                                 ConsVar_Grad_j, correct, &Temp_i, &Temp_j,
+                                                 NormalGrad, CorrectedGrad);
+
+  const su2double Thermal_Diffusivity_Mean = 0.5*(Thermal_Diffusivity_i + Thermal_Diffusivity_j);
+
+  val_residual[0] = Thermal_Diffusivity_Mean*CorrectedGrad[0];
+
+  /*--- For Jacobians -> Use of TSL approx. to compute derivatives of the gradients ---*/
+  if (implicit) {
+    Jacobian_i[0][0] = -Thermal_Diffusivity_Mean*proj_vector_ij;
+    Jacobian_j[0][0] = Thermal_Diffusivity_Mean*proj_vector_ij;
+  }
+
+  AD::SetPreaccOut(val_residual, nVar);
+  AD::EndPreacc();
+
+}
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index 16ac1fb6a32..f07c7b210f5 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -2030,7 +2030,6 @@ void CEulerSolver::Source_Residual(CGeometry *geometry, CSolver **solver_contain
   const bool harmonic_balance = (config->GetTime_Marching() == TIME_MARCHING::HARMONIC_BALANCE);
   const bool windgust         = config->GetWind_Gust();
   const bool body_force       = config->GetBody_Force();
-  const bool vorticity_confinement = config->GetVorticityConfinement();
   const bool ideal_gas        = (config->GetKind_FluidModel() == STANDARD_AIR) ||
                                 (config->GetKind_FluidModel() == IDEAL_GAS);
   const bool rans             = (config->GetKind_Turb_Model() != TURB_MODEL::NONE);
@@ -2229,42 +2228,6 @@ void CEulerSolver::Source_Residual(CGeometry *geometry, CSolver **solver_contain
     END_SU2_OMP_FOR
   }
 
-  if (vorticity_confinement) {
-
-    CNumerics* second_numerics = numerics_container[SOURCE_SECOND_TERM + omp_get_thread_num()*MAX_TERMS];
-
-    /*--- calculate and set the average volume ---*/
-    const su2double AvgVolume = config->GetDomainVolume() / geometry->GetGlobal_nPointDomain();
-    second_numerics->SetAvgVolume(AvgVolume);
-
-    /*--- set vorticity magnitude as auxilliary variable ---*/
-    SU2_OMP_FOR_STAT(omp_chunk_size)
-    for (iPoint = 0; iPoint < nPoint; iPoint++) {
-      const su2double VorticityMag = max(GeometryToolbox::Norm(3, nodes->GetVorticity(iPoint)), 1e-12);
-      nodes->SetAuxVar(iPoint, 0, VorticityMag);
-    }
-    END_SU2_OMP_FOR
-
-    /*--- calculate the gradient of the vorticity magnitude (AuxVarGradient) ---*/
-    SetAuxVar_Gradient_GG(geometry, config);
-
-    SU2_OMP_FOR_DYN(omp_chunk_size)
-    for (iPoint = 0; iPoint < nPointDomain; iPoint++) {
-      second_numerics->SetPrimitive(nodes->GetPrimitive(iPoint), nullptr);
-      second_numerics->SetVorticity(nodes->GetVorticity(iPoint), nullptr);
-      second_numerics->SetAuxVarGrad(nodes->GetAuxVarGradient(iPoint), nullptr);
-      second_numerics->SetDistance(geometry->nodes->GetWall_Distance(iPoint), 0);
-      second_numerics->SetVolume(geometry->nodes->GetVolume(iPoint));
-      auto residual = second_numerics->ComputeResidual(config);
-
-      LinSysRes.AddBlock(iPoint, residual);
-
-      if (implicit) Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
-    }
-    END_SU2_OMP_FOR
-
-  }
-
   /*--- Check if a verification solution is to be computed. ---*/
 
   if ( VerificationSolution ) {
@@ -4724,6 +4687,7 @@ void CEulerSolver::BC_Riemann(CGeometry *geometry, CSolver **solver_container,
         GetFluidModel()->SetTDState_PT(P_Total, T_Total);
         Enthalpy_e = GetFluidModel()->GetStaticEnergy()+ GetFluidModel()->GetPressure()/GetFluidModel()->GetDensity();
         Entropy_e = GetFluidModel()->GetEntropy();
+
         /* --- Compute the boundary state u_e --- */
         Velocity2_e = Velocity2_i;
         if (nDim == 2){
diff --git a/SU2_CFD/src/solvers/CHeatSolver.cpp b/SU2_CFD/src/solvers/CHeatSolver.cpp
index b044a1915e5..9bada16eb30 100644
--- a/SU2_CFD/src/solvers/CHeatSolver.cpp
+++ b/SU2_CFD/src/solvers/CHeatSolver.cpp
@@ -26,21 +26,17 @@
  */
 
 #include "../../include/solvers/CHeatSolver.hpp"
-#include <cstddef>
 #include "../../../Common/include/toolboxes/geometry_toolbox.hpp"
-#include "../../include/solvers/CScalarSolver.inl"
 
-/*--- Explicit instantiation of the parent class of CHeatSolver. ---*/
-template class CScalarSolver<CHeatVariable>;
+CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iMesh) : CSolver(),
+             flow(config->GetFluidProblem()), heat_equation(config->GetHeatProblem()) {
 
-CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iMesh)
-  : CScalarSolver<CHeatVariable>(geometry, config, false),
-    flow(config->GetFluidProblem()), heat_equation(config->GetHeatProblem()) {
+  /* A grid is defined as dynamic if there's rigid grid movement or grid deformation AND the problem is time domain */
+  dynamic_grid = config->GetDynamic_Grid();
 
   /*--- Dimension of the problem --> temperature is the only conservative variable ---*/
 
   nVar = 1;
-  nPrimVar = 1;
   nPoint = geometry->GetnPoint();
   nPointDomain = geometry->GetnPointDomain();
 
@@ -51,6 +47,18 @@ CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iM
   /*--- Define geometry constants in the solver structure ---*/
 
   nDim = geometry->GetnDim();
+  nMarker = config->GetnMarker_All();
+
+  /*--- Store the number of vertices on each marker for deallocation later ---*/
+
+  nVertex.resize(nMarker);
+  for (auto iMarker = 0u; iMarker < nMarker; iMarker++)
+    nVertex[iMarker] = geometry->nVertex[iMarker];
+
+  /*--- Define some auxiliary vector related with the residual ---*/
+
+  Residual = new su2double[nVar]; for (auto iVar = 0u; iVar < nVar; iVar++) Residual[iVar] = 0.0;
+  Res_Visc = new su2double[nVar]; for (auto iVar = 0u; iVar < nVar; iVar++) Res_Visc[iVar] = 0.0;
 
   /*--- Define some structures for locating max residuals ---*/
 
@@ -59,13 +67,21 @@ CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iM
   Point_Max.resize(nVar,0);
   Point_Max_Coord.resize(nVar,nDim) = su2double(0.0);
 
+  /*--- Jacobians and vector structures for implicit computations ---*/
+
+  Jacobian_i = new su2double* [nVar];
+  Jacobian_j = new su2double* [nVar];
+  for (auto iVar = 0u; iVar < nVar; iVar++) {
+    Jacobian_i[iVar] = new su2double [nVar];
+    Jacobian_j[iVar] = new su2double [nVar];
+  }
+
   /*--- Initialization of the structure of the whole Jacobian ---*/
 
   if (rank == MASTER_NODE) cout << "Initialize Jacobian structure (heat equation) MG level: " << iMesh << "." << endl;
-  Jacobian.Initialize(nPoint, nPointDomain, nVar, nVar, true, geometry, config, ReducerStrategy);
+  Jacobian.Initialize(nPoint, nPointDomain, nVar, nVar, true, geometry, config);
   LinSysSol.Initialize(nPoint, nPointDomain, nVar, 0.0);
   LinSysRes.Initialize(nPoint, nPointDomain, nVar, 0.0);
-  if (ReducerStrategy) EdgeFluxes.Initialize(geometry->GetnEdge(), geometry->GetnEdge(), nVar, nullptr);
 
   if (config->GetExtraOutput()) {
     if (nDim == 2) { nOutputVariables = 13; }
@@ -95,8 +111,7 @@ CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iM
     Temperature_Ref = config->GetInc_Temperature_Ref();
   }
   config->SetTemperature_Ref(Temperature_Ref);
-  config->SetTemperature_FreeStreamND(Temperature_FreeStream / Temperature_Ref);
-  Solution_Inf[0] = config->GetTemperature_FreeStreamND();
+  config->SetTemperature_FreeStreamND(Temperature_FreeStream/Temperature_Ref);
 
   /*--- Set the reference values for heat fluxes. If the heat solver runs stand-alone,
    *    thermal conductivity is read directly from config file ---*/
@@ -118,7 +133,7 @@ CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iM
    used for communications with donor cells ---*/
 
   const unsigned short nConjVariables = 4;
-  AllocVectorOfMatrices(nVertex, nConjVariables, ConjugateVar, Solution_Inf[0]);
+  AllocVectorOfMatrices(nVertex, nConjVariables, ConjugateVar, config->GetTemperature_FreeStreamND());
 
   /*--- Heat flux in all the markers ---*/
 
@@ -134,7 +149,7 @@ CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iM
 
   /*--- Initialize the nodes vector. ---*/
 
-  nodes = new CHeatVariable(Solution_Inf[0], nPoint, nDim, nVar, config);
+  nodes = new CHeatVariable(config->GetTemperature_FreeStreamND(), nPoint, nDim, nVar, config);
 
   SetBaseClassPointerToNodes();
 
@@ -155,52 +170,64 @@ CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iM
   InitiateComms(geometry, config, SOLUTION);
   CompleteComms(geometry, config, SOLUTION);
 
-  /*--- Store the initial CFL number for all grid points. ---*/
-
-  const su2double CFL = config->GetCFL(MGLevel) * config->GetCFLRedCoeff_Turb();
-  SU2_OMP_FOR_STAT(omp_chunk_size)
-  for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
-    nodes->SetLocalCFL(iPoint, CFL);
-  }
-  END_SU2_OMP_FOR
-  Min_CFL_Local = CFL;
-  Max_CFL_Local = CFL;
-  Avg_CFL_Local = CFL;
-
   /*--- Add the solver name (max 8 characters) ---*/
 
   SolverName = "HEAT";
 }
 
-void CHeatSolver::Preprocessing(CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh,
-                                unsigned short iRKStep, unsigned short RunTime_EqSystem, bool Output) {
-  SU2_OMP_SAFE_GLOBAL_ACCESS(config->SetGlobalParam(config->GetKind_Solver(), RunTime_EqSystem);)
-  CommonPreprocessing(geometry, config, Output);
-
-  /*--- Need to clear EdgeFluxes and Jacobian when only the viscous part is called for solid heat transfer,
-   * for the weakly coupled energy equation the convection part does this by setting instead of incrementing. ---*/
-  if (!Output && !flow && ReducerStrategy) {
-    EdgeFluxes.SetValZero();
-    if (config->GetKind_TimeIntScheme() == EULER_IMPLICIT) {
-      Jacobian.SetValZero();
-    } else {
-      SU2_OMP_BARRIER
-    }
+CHeatSolver::~CHeatSolver(void) {
+
+  delete nodes;
+}
+
+void CHeatSolver::Preprocessing(CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, unsigned short iRKStep, unsigned short RunTime_EqSystem, bool Output) {
+  SU2_OMP_MASTER
+  config->SetGlobalParam(config->GetKind_Solver(), RunTime_EqSystem);
+  END_SU2_OMP_MASTER
+
+  if (config->GetKind_ConvNumScheme_Heat() == SPACE_CENTERED) {
+    SetUndivided_Laplacian(geometry, config);
+  }
+
+  for (auto iPoint = 0ul; iPoint < nPoint; iPoint ++) {
+
+    /*--- Initialize the residual vector ---*/
+
+    LinSysRes.SetBlock_Zero(iPoint);
   }
+
+  /*--- Initialize the Jacobian matrices ---*/
+
+  Jacobian.SetValZero();
+
+  if (config->GetReconstructionGradientRequired()) {
+    if (config->GetKind_Gradient_Method_Recon() == GREEN_GAUSS)
+      SetSolution_Gradient_GG(geometry, config, true);
+    if (config->GetKind_Gradient_Method_Recon() == LEAST_SQUARES)
+      SetSolution_Gradient_LS(geometry, config, true);
+    if (config->GetKind_Gradient_Method_Recon() == WEIGHTED_LEAST_SQUARES)
+      SetSolution_Gradient_LS(geometry, config, true);
+  }
+  if (config->GetKind_Gradient_Method() == GREEN_GAUSS) SetSolution_Gradient_GG(geometry, config);
+  if (config->GetKind_Gradient_Method() == WEIGHTED_LEAST_SQUARES) SetSolution_Gradient_LS(geometry, config);
 }
 
+void CHeatSolver::Postprocessing(CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh) { }
+
 void CHeatSolver::LoadRestart(CGeometry **geometry, CSolver ***solver, CConfig *config, int val_iter,
                               bool val_update_geo) {
+  /*--- Restart the solution from file information ---*/
+
   const string restart_filename = config->GetFilename(config->GetSolution_FileName(), "", val_iter);
 
-  BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
   /*--- Skip coordinates ---*/
 
   unsigned short skipVars = nDim;
 
   if (flow) {
     // P, vx, vy (,vz)
-    skipVars += 1 + nDim;
+    if (nDim == 2) skipVars += 3;
+    if (nDim == 3) skipVars += 4;
   }
 
   /*--- Read the restart data from either an ASCII or binary SU2 file. ---*/
@@ -238,8 +265,6 @@ void CHeatSolver::LoadRestart(CGeometry **geometry, CSolver ***solver, CConfig *
     SU2_MPI::Error(string("The solution file ") + restart_filename + string(" does not match with the mesh file!\n") +
                    string("This can be caused by empty lines at the end of the file."), CURRENT_FUNCTION);
   }
-  }
-  END_SU2_OMP_SAFE_GLOBAL_ACCESS
 
   /*--- Communicate the loaded solution on the fine grid before we transfer
    it down to the coarse levels. We alo call the preprocessing routine
@@ -264,51 +289,212 @@ void CHeatSolver::LoadRestart(CGeometry **geometry, CSolver ***solver, CConfig *
 
   /*--- Delete the class memory that is used to load the restart. ---*/
 
-  BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
-    delete[] Restart_Vars;
-    Restart_Vars = nullptr;
-    delete[] Restart_Data;
-    Restart_Data = nullptr;
+  delete[] Restart_Vars;
+  Restart_Vars = nullptr;
+  delete[] Restart_Data;
+  Restart_Data = nullptr;
+}
+
+void CHeatSolver::Centered_Residual(CGeometry *geometry, CSolver **solver_container,  CNumerics **numerics_container,
+                                    CConfig *config, unsigned short iMesh, unsigned short iRKStep) {
+
+  const auto numerics = numerics_container[CONV_TERM];
+
+  if(flow) {
+
+    nVarFlow = solver_container[FLOW_SOL]->GetnVar();
+
+    for (auto iEdge = 0ul; iEdge < geometry->GetnEdge(); iEdge++) {
+
+      /*--- Points in edge ---*/
+      const auto iPoint = geometry->edges->GetNode(iEdge,0);
+      const auto jPoint = geometry->edges->GetNode(iEdge,1);
+      numerics->SetNormal(geometry->edges->GetNormal(iEdge));
+
+      /*--- Primitive variables w/o reconstruction ---*/
+      const auto V_i = solver_container[FLOW_SOL]->GetNodes()->GetPrimitive(iPoint);
+      const auto V_j = solver_container[FLOW_SOL]->GetNodes()->GetPrimitive(jPoint);
+
+      const auto Temp_i = nodes->GetTemperature(iPoint);
+      const auto Temp_j = nodes->GetTemperature(jPoint);
+
+      numerics->SetUndivided_Laplacian(nodes->GetUndivided_Laplacian(iPoint), nodes->GetUndivided_Laplacian(jPoint));
+      numerics->SetNeighbor(geometry->nodes->GetnNeighbor(iPoint), geometry->nodes->GetnNeighbor(jPoint));
+
+      numerics->SetPrimitive(V_i, V_j);
+      numerics->SetTemperature(Temp_i, Temp_j);
+
+      numerics->ComputeResidual(Residual, Jacobian_i, Jacobian_j, config);
+
+      LinSysRes.AddBlock(iPoint, Residual);
+      LinSysRes.SubtractBlock(jPoint, Residual);
+
+      /*--- Implicit part ---*/
+
+      Jacobian.UpdateBlocks(iEdge, iPoint, jPoint, Jacobian_i, Jacobian_j);
+    }
   }
-  END_SU2_OMP_SAFE_GLOBAL_ACCESS
 }
 
 void CHeatSolver::Upwind_Residual(CGeometry *geometry, CSolver **solver_container,
                                   CNumerics **numerics_container, CConfig *config, unsigned short iMesh) {
-  /*--- For solid heat transfer there is no convection. ---*/
-  if (!flow) return;
-  CScalarSolver<CHeatVariable>::Upwind_Residual(geometry, solver_container, numerics_container, config, iMesh);
+
+  CNumerics* numerics = numerics_container[CONV_TERM];
+
+  su2double *V_i, *V_j, Temp_i, Temp_i_Corrected, Temp_j, Temp_j_Corrected,
+            Project_Grad_i, Project_Grad_j, Project_Temp_i_Grad, Project_Temp_j_Grad;
+
+  su2double Vector_i[MAXNDIM] = {0};
+  su2double Vector_j[MAXNDIM] = {0};
+
+  if(flow) {
+
+    nVarFlow = solver_container[FLOW_SOL]->GetnVar();
+
+    /*--- Define some auxiliary vectors related to the primitive flow solution ---*/
+    vector<su2double> Primitive_Flow_i(nVarFlow, 0.0);
+    vector<su2double> Primitive_Flow_j(nVarFlow, 0.0);
+
+    for (auto iEdge = 0ul; iEdge < geometry->GetnEdge(); iEdge++) {
+
+      /*--- Points in edge ---*/
+      const auto iPoint = geometry->edges->GetNode(iEdge,0);
+      const auto jPoint = geometry->edges->GetNode(iEdge,1);
+      numerics->SetNormal(geometry->edges->GetNormal(iEdge));
+
+      /*--- Primitive variables w/o reconstruction ---*/
+      V_i = solver_container[FLOW_SOL]->GetNodes()->GetPrimitive(iPoint);
+      V_j = solver_container[FLOW_SOL]->GetNodes()->GetPrimitive(jPoint);
+
+      const auto Temp_i_Grad = nodes->GetGradient(iPoint);
+      const auto Temp_j_Grad = nodes->GetGradient(jPoint);
+      numerics->SetConsVarGradient(Temp_i_Grad, Temp_j_Grad);
+
+      Temp_i = nodes->GetTemperature(iPoint);
+      Temp_j = nodes->GetTemperature(jPoint);
+
+      /* Second order reconstruction */
+      if (config->GetMUSCL_Heat()) {
+
+        for (auto iDim = 0u; iDim < nDim; iDim++) {
+          Vector_i[iDim] = 0.5*(geometry->nodes->GetCoord(jPoint, iDim) - geometry->nodes->GetCoord(iPoint, iDim));
+          Vector_j[iDim] = 0.5*(geometry->nodes->GetCoord(iPoint, iDim) - geometry->nodes->GetCoord(jPoint, iDim));
+        }
+
+        const auto Gradient_i = solver_container[FLOW_SOL]->GetNodes()->GetGradient_Reconstruction(iPoint);
+        const auto Gradient_j = solver_container[FLOW_SOL]->GetNodes()->GetGradient_Reconstruction(jPoint);
+        const auto Temp_i_Grad = nodes->GetGradient_Reconstruction(iPoint);
+        const auto Temp_j_Grad = nodes->GetGradient_Reconstruction(jPoint);
+
+        /*Loop to correct the flow variables*/
+        for (auto iVar = 0u; iVar < nVarFlow; iVar++) {
+
+          /*Apply the Gradient to get the right temperature value on the edge */
+          Project_Grad_i = 0.0; Project_Grad_j = 0.0;
+          for (auto iDim = 0u; iDim < nDim; iDim++) {
+              Project_Grad_i += Vector_i[iDim]*Gradient_i[iVar][iDim];
+              Project_Grad_j += Vector_j[iDim]*Gradient_j[iVar][iDim];
+          }
+
+          Primitive_Flow_i[iVar] = V_i[iVar] + Project_Grad_i;
+          Primitive_Flow_j[iVar] = V_j[iVar] + Project_Grad_j;
+        }
+
+        /* Correct the temperature variables */
+        Project_Temp_i_Grad = 0.0; Project_Temp_j_Grad = 0.0;
+        for (auto iDim = 0u; iDim < nDim; iDim++) {
+            Project_Temp_i_Grad += Vector_i[iDim]*Temp_i_Grad[0][iDim];
+            Project_Temp_j_Grad += Vector_j[iDim]*Temp_j_Grad[0][iDim];
+        }
+
+        Temp_i_Corrected = Temp_i + Project_Temp_i_Grad;
+        Temp_j_Corrected = Temp_j + Project_Temp_j_Grad;
+
+        numerics->SetPrimitive(Primitive_Flow_i.data(), Primitive_Flow_j.data());
+        numerics->SetTemperature(Temp_i_Corrected, Temp_j_Corrected);
+      }
+
+      else {
+
+        numerics->SetPrimitive(V_i, V_j);
+        numerics->SetTemperature(Temp_i, Temp_j);
+      }
+
+      numerics->ComputeResidual(Residual, Jacobian_i, Jacobian_j, config);
+
+      LinSysRes.AddBlock(iPoint, Residual);
+      LinSysRes.SubtractBlock(jPoint, Residual);
+
+      /*--- Implicit part ---*/
+
+      Jacobian.UpdateBlocks(iEdge, iPoint, jPoint, Jacobian_i, Jacobian_j);
+    }
+  }
+
 }
 
 void CHeatSolver::Viscous_Residual(CGeometry *geometry, CSolver **solver_container, CNumerics **numerics_container,
                                    CConfig *config, unsigned short iMesh, unsigned short iRKStep) {
-  /*--- For fluid problems the viscous residual is included in the convective residual. ---*/
-  if (flow) return;
-  const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
-  CNumerics* numerics = numerics_container[VISC_TERM + omp_get_thread_num() * MAX_TERMS];
-
-  bool pausePreacc = false;
-  if (ReducerStrategy)
-    pausePreacc = AD::PausePreaccumulation();
-  else
-    AD::StartNoSharedReading();
-
-  for (auto color : EdgeColoring) {
-    SU2_OMP_FOR_DYN(nextMultiple(OMP_MIN_SIZE, color.groupSize))
-    for (auto k = 0ul; k < color.size; ++k) {
-      auto iEdge = color.indices[k];
-      Viscous_Residual(iEdge, geometry, solver_container, numerics, config);
+
+  CNumerics* numerics = numerics_container[VISC_TERM];
+
+  su2double laminar_viscosity, Prandtl_Lam, Prandtl_Turb, eddy_viscosity_i, eddy_viscosity_j,
+            thermal_diffusivity_i, thermal_diffusivity_j, Temp_i, Temp_j;
+
+  const bool turb = ((config->GetKind_Solver() == MAIN_SOLVER::INC_RANS) || (config->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_INC_RANS));
+
+  eddy_viscosity_i = 0.0;
+  eddy_viscosity_j = 0.0;
+  laminar_viscosity = config->GetMu_ConstantND();
+  Prandtl_Lam = config->GetPrandtl_Lam();
+  Prandtl_Turb = config->GetPrandtl_Turb();
+
+  for (auto iEdge = 0ul; iEdge < geometry->GetnEdge(); iEdge++) {
+
+    const auto iPoint = geometry->edges->GetNode(iEdge,0);
+    const auto jPoint = geometry->edges->GetNode(iEdge,1);
+
+    /*--- Points coordinates, and normal vector ---*/
+
+    numerics->SetCoord(geometry->nodes->GetCoord(iPoint),
+                       geometry->nodes->GetCoord(jPoint));
+    numerics->SetNormal(geometry->edges->GetNormal(iEdge));
+
+    const auto Temp_i_Grad = nodes->GetGradient(iPoint);
+    const auto Temp_j_Grad = nodes->GetGradient(jPoint);
+    numerics->SetConsVarGradient(Temp_i_Grad, Temp_j_Grad);
+
+    /*--- Primitive variables w/o reconstruction ---*/
+    Temp_i = nodes->GetTemperature(iPoint);
+    Temp_j = nodes->GetTemperature(jPoint);
+    numerics->SetTemperature(Temp_i, Temp_j);
+
+    /*--- Eddy viscosity to compute thermal conductivity ---*/
+    if (flow) {
+      if (turb) {
+        eddy_viscosity_i = solver_container[TURB_SOL]->GetNodes()->GetmuT(iPoint);
+        eddy_viscosity_j = solver_container[TURB_SOL]->GetNodes()->GetmuT(jPoint);
+      }
+      thermal_diffusivity_i = (laminar_viscosity/Prandtl_Lam) + (eddy_viscosity_i/Prandtl_Turb);
+      thermal_diffusivity_j = (laminar_viscosity/Prandtl_Lam) + (eddy_viscosity_j/Prandtl_Turb);
+    }
+    else {
+      thermal_diffusivity_i = config->GetThermalDiffusivity();
+      thermal_diffusivity_j = config->GetThermalDiffusivity();
     }
-    END_SU2_OMP_FOR
-  }
 
-  /*--- Restore preaccumulation and adjoint evaluation state. ---*/
-  AD::ResumePreaccumulation(pausePreacc);
-  if (!ReducerStrategy) AD::EndNoSharedReading();
+    numerics->SetThermalDiffusivity(thermal_diffusivity_i,thermal_diffusivity_j);
 
-  if (ReducerStrategy) {
-    SumEdgeFluxes(geometry);
-    if (implicit) Jacobian.SetDiagonalAsColumnSum();
+    /*--- Compute residual, and Jacobians ---*/
+
+    numerics->ComputeResidual(Residual, Jacobian_i, Jacobian_j, config);
+
+    /*--- Add and subtract residual, and update Jacobians ---*/
+
+    LinSysRes.SubtractBlock(iPoint, Residual);
+    LinSysRes.AddBlock(jPoint, Residual);
+
+    Jacobian.UpdateBlocksSub(iEdge, iPoint, jPoint, Jacobian_i, Jacobian_j);
   }
 }
 
@@ -367,191 +553,282 @@ void CHeatSolver::Set_Heatflux_Areas(CGeometry *geometry, CConfig *config) {
   delete[] Local_Surface_Areas;
 }
 
-void CHeatSolver::BC_Isothermal_Wall(CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics,
-                                     CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
+void CHeatSolver::BC_Isothermal_Wall(CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config,
+                                       unsigned short val_marker) {
 
-  const auto Marker_Tag = config->GetMarker_All_TagBound(val_marker);
-  su2double Twall = config->GetIsothermal_Temperature(Marker_Tag) / config->GetTemperature_Ref();
-  const bool IsPyCustom = config->GetMarker_All_PyCustom(val_marker);
+  unsigned long iPoint, Point_Normal;
+  su2double *Normal, *Coord_i, *Coord_j, Area, dist_ij, Twall, dTdn;
+  const bool implicit = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
+
+  const su2double laminar_viscosity = config->GetMu_ConstantND();
+  const su2double Prandtl_Lam = config->GetPrandtl_Lam();
+  const su2double thermal_diffusivity = flow ? laminar_viscosity/Prandtl_Lam : config->GetThermalDiffusivity();
+
+  //su2double Prandtl_Turb = config->GetPrandtl_Turb();
+  //laminar_viscosity = config->GetViscosity_FreeStreamND(); // TDE check for consistency for CHT
+
+  string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
+
+  Twall = config->GetIsothermal_Temperature(Marker_Tag)/config->GetTemperature_Ref();
 
-  SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
   for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
-    if (IsPyCustom) {
-      Twall = geometry->GetCustomBoundaryTemperature(val_marker, iVertex);
+
+    iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
+
+    if (geometry->nodes->GetDomain(iPoint)) {
+
+        Point_Normal = geometry->vertex[val_marker][iVertex]->GetNormal_Neighbor();
+
+        Normal = geometry->vertex[val_marker][iVertex]->GetNormal();
+        Area = GeometryToolbox::Norm(nDim, Normal);
+
+        Coord_i = geometry->nodes->GetCoord(iPoint);
+        Coord_j = geometry->nodes->GetCoord(Point_Normal);
+        dist_ij = 0;
+        for (auto iDim = 0u; iDim < nDim; iDim++)
+          dist_ij += (Coord_j[iDim]-Coord_i[iDim])*(Coord_j[iDim]-Coord_i[iDim]);
+        dist_ij = sqrt(dist_ij);
+
+        dTdn = -(nodes->GetTemperature(Point_Normal) - Twall)/dist_ij;
+
+        Res_Visc[0] = thermal_diffusivity*dTdn*Area;
+
+        if(implicit)
+          Jacobian_i[0][0] = -thermal_diffusivity/dist_ij * Area;
+
+        LinSysRes.SubtractBlock(iPoint, Res_Visc);
+        Jacobian.SubtractBlock2Diag(iPoint, Jacobian_i);
     }
-    IsothermalBoundaryCondition(geometry, solver_container[FLOW_SOL], config, val_marker, iVertex, Twall);
   }
-  END_SU2_OMP_FOR
 }
 
 void CHeatSolver::BC_HeatFlux_Wall(CGeometry* geometry, CSolver** solver_container, CNumerics* conv_numerics,
                                    CNumerics* visc_numerics, CConfig* config, unsigned short val_marker) {
   const auto Marker_Tag = config->GetMarker_All_TagBound(val_marker);
-  const bool IsPyCustom = config->GetMarker_All_PyCustom(val_marker);
 
   su2double Wall_HeatFlux = config->GetWall_HeatFlux(Marker_Tag) / config->GetHeat_Flux_Ref();
   if (config->GetIntegrated_HeatFlux()) {
     Wall_HeatFlux /= geometry->GetSurfaceArea(config, val_marker);
   }
 
-  SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
   for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
     const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
-    if (!geometry->nodes->GetDomain(iPoint)) continue;
 
-    if (IsPyCustom) {
-      Wall_HeatFlux = geometry->GetCustomBoundaryHeatFlux(val_marker, iVertex);
+    if (geometry->nodes->GetDomain(iPoint)) {
+      const auto Normal = geometry->vertex[val_marker][iVertex]->GetNormal();
+      const auto Area = GeometryToolbox::Norm(nDim, Normal);
+
+      Res_Visc[0] = 0.0;
+
+      Res_Visc[0] = Wall_HeatFlux * Area;
+
+      /*--- Viscous contribution to the residual at the wall ---*/
+
+      LinSysRes.SubtractBlock(iPoint, Res_Visc);
     }
-    /*--- Viscous contribution to the residual at the wall. ---*/
-    const auto* Normal = geometry->vertex[val_marker][iVertex]->GetNormal();
-    const su2double Area = GeometryToolbox::Norm(nDim, Normal);
-    const su2double flux = Wall_HeatFlux * Area;
-    LinSysRes(iPoint, 0) -= flux;
   }
-  END_SU2_OMP_FOR
 }
 
-void CHeatSolver::BC_Inlet(CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics,
-                           CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
-  if (!flow) return;
+void CHeatSolver::BC_Inlet(CGeometry *geometry, CSolver **solver_container,
+                            CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
 
-  const bool viscous = config->GetViscous();
-  const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+  unsigned short iDim;
+  unsigned long iVertex, iPoint, Point_Normal;
+  su2double Vel_Mag, *V_inlet, *V_domain;
 
-  SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
-  for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
+  bool viscous              = config->GetViscous();
+  bool implicit             = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
+  string Marker_Tag         = config->GetMarker_All_TagBound(val_marker);
 
-    const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
+  su2double Normal[MAXNDIM];
 
-    if (!geometry->nodes->GetDomain(iPoint)) continue;
+  su2double *Coord_i, *Coord_j, Area, dist_ij, laminar_viscosity, thermal_diffusivity, Twall, dTdn, Prandtl_Lam;
+  //su2double Prandtl_Turb;
+  Prandtl_Lam = config->GetPrandtl_Lam();
+//  Prandtl_Turb = config->GetPrandtl_Turb();
+  laminar_viscosity = config->GetMu_ConstantND();
+  //laminar_viscosity = config->GetViscosity_FreeStreamND(); //TDE check for consistency with CHT
 
-    su2double Normal[MAXNDIM];
-    geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
-    for (auto iDim = 0u; iDim < nDim; iDim++) Normal[iDim] = -Normal[iDim];
+  Twall = config->GetTemperature_FreeStreamND();
 
-    /*--- Normal vector for this vertex (negate for outward convention) ---*/
+  for (iVertex = 0; iVertex < geometry->nVertex[val_marker]; iVertex++) {
 
-    conv_numerics->SetNormal(Normal);
+    iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
-    /*--- Retrieve solution at this boundary node ---*/
+    if (geometry->nodes->GetDomain(iPoint)) {
 
-    const auto* V_domain = solver_container[FLOW_SOL]->GetNodes()->GetPrimitive(iPoint);
+      geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
+      for (iDim = 0; iDim < nDim; iDim++) Normal[iDim] = -Normal[iDim];
 
-    /*--- Retrieve the specified velocity for the inlet. ---*/
+      if(flow) {
 
-    const auto* V_inlet = solver_container[FLOW_SOL]->GetCharacPrimVar(val_marker, iVertex);
+        /*--- Normal vector for this vertex (negate for outward convention) ---*/
 
-    conv_numerics->SetPrimitive(V_domain, V_inlet);
+        conv_numerics->SetNormal(Normal);
 
-    if (dynamic_grid)
-      conv_numerics->SetGridVel(geometry->nodes->GetGridVel(iPoint), geometry->nodes->GetGridVel(iPoint));
+        /*--- Retrieve solution at this boundary node ---*/
 
-    const su2double Temp_i = nodes->GetTemperature(iPoint);
-    const su2double Temp_j = V_inlet[prim_idx.Temperature()];
-    conv_numerics->SetScalarVar(&Temp_i, &Temp_j);
+        V_domain = solver_container[FLOW_SOL]->GetNodes()->GetPrimitive(iPoint);
 
-    /*--- Compute the residual using an upwind scheme ---*/
+        /*--- Retrieve the specified velocity for the inlet. ---*/
 
-    auto residual = conv_numerics->ComputeResidual(config);
+        Vel_Mag  = config->GetInlet_Ptotal(Marker_Tag)/config->GetVelocity_Ref();
+        auto Flow_Dir = config->GetInlet_FlowDir(Marker_Tag);
 
-    /*--- Update residual value ---*/
+        V_inlet = solver_container[FLOW_SOL]->GetCharacPrimVar(val_marker, iVertex);
 
-    LinSysRes.AddBlock(iPoint, residual);
+        for (iDim = 0; iDim < nDim; iDim++)
+          V_inlet[iDim+1] = Vel_Mag*Flow_Dir[iDim];
 
-    /*--- Jacobian contribution for implicit integration ---*/
+        conv_numerics->SetPrimitive(V_domain, V_inlet);
 
-    if (implicit) Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
+        if (dynamic_grid)
+          conv_numerics->SetGridVel(geometry->nodes->GetGridVel(iPoint), geometry->nodes->GetGridVel(iPoint));
 
-    /*--- Viscous contribution ---*/
+        conv_numerics->SetTemperature(nodes->GetTemperature(iPoint), config->GetInlet_Ttotal(Marker_Tag)/config->GetTemperature_Ref());
+
+        /*--- Compute the residual using an upwind scheme ---*/
+
+        conv_numerics->ComputeResidual(Residual, Jacobian_i, Jacobian_j, config);
+
+        /*--- Update residual value ---*/
+
+        LinSysRes.AddBlock(iPoint, Residual);
+
+        /*--- Jacobian contribution for implicit integration ---*/
+
+        if (implicit)
+          Jacobian.AddBlock2Diag(iPoint, Jacobian_i);
+      }
+
+      /*--- Viscous contribution ---*/
+
+      if (viscous) {
+
+        Point_Normal = geometry->vertex[val_marker][iVertex]->GetNormal_Neighbor();
+
+        geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
+        Area = GeometryToolbox::Norm(nDim, Normal);
+
+        Coord_i = geometry->nodes->GetCoord(iPoint);
+        Coord_j = geometry->nodes->GetCoord(Point_Normal);
+        dist_ij = 0;
+        for (iDim = 0; iDim < nDim; iDim++)
+          dist_ij += (Coord_j[iDim]-Coord_i[iDim])*(Coord_j[iDim]-Coord_i[iDim]);
+        dist_ij = sqrt(dist_ij);
+
+        dTdn = -(nodes->GetTemperature(Point_Normal) - Twall)/dist_ij;
+
+        thermal_diffusivity = laminar_viscosity/Prandtl_Lam;
+
+        Res_Visc[0] = thermal_diffusivity*dTdn*Area;
+
+        if(implicit) {
 
-    if (viscous) {
-      IsothermalBoundaryCondition(geometry, solver_container[FLOW_SOL], config, val_marker, iVertex, Temp_j);
+          Jacobian_i[0][0] = -thermal_diffusivity/dist_ij * Area;
+        }
+        /*--- Viscous contribution to the residual at the wall ---*/
+
+        LinSysRes.SubtractBlock(iPoint, Res_Visc);
+        Jacobian.SubtractBlock2Diag(iPoint, Jacobian_i);
+      }
     }
   }
-  END_SU2_OMP_FOR
+
 }
 
 void CHeatSolver::BC_Outlet(CGeometry *geometry, CSolver **solver_container,
                              CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
-  if (!flow) return;
 
-  const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+  su2double *V_outlet, *V_domain;
+
+  bool implicit             = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
+
+  su2double Normal[MAXNDIM];
 
-  SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
   for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
 
     const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
-    if (!geometry->nodes->GetDomain(iPoint)) continue;
+    if (geometry->nodes->GetDomain(iPoint)) {
 
-    const auto Point_Normal = geometry->vertex[val_marker][iVertex]->GetNormal_Neighbor();
+      const auto Point_Normal = geometry->vertex[val_marker][iVertex]->GetNormal_Neighbor();
 
-    /*--- Normal vector for this vertex (negate for outward convention) ---*/
+      /*--- Normal vector for this vertex (negate for outward convention) ---*/
 
-    su2double Normal[MAXNDIM];
-    geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
-    for (auto iDim = 0u; iDim < nDim; iDim++) Normal[iDim] = -Normal[iDim];
+      geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
+      for (auto iDim = 0u; iDim < nDim; iDim++) Normal[iDim] = -Normal[iDim];
 
-    conv_numerics->SetNormal(Normal);
+      if(flow) {
+        conv_numerics->SetNormal(Normal);
 
-    /*--- Retrieve solution at this boundary node ---*/
+        /*--- Retrieve solution at this boundary node ---*/
 
-    const auto* V_domain = solver_container[FLOW_SOL]->GetNodes()->GetPrimitive(iPoint);
+        V_domain = solver_container[FLOW_SOL]->GetNodes()->GetPrimitive(iPoint);
 
-    /*--- Retrieve the specified velocity for the inlet. ---*/
+        /*--- Retrieve the specified velocity for the inlet. ---*/
 
-    const auto* V_outlet = solver_container[FLOW_SOL]->GetCharacPrimVar(val_marker, iVertex);
+        V_outlet = solver_container[FLOW_SOL]->GetCharacPrimVar(val_marker, iVertex);
+        for (auto iDim = 0u; iDim < nDim; iDim++)
+          V_outlet[iDim+1] = solver_container[FLOW_SOL]->GetNodes()->GetVelocity(Point_Normal, iDim);
 
-    conv_numerics->SetPrimitive(V_domain, V_outlet);
+        conv_numerics->SetPrimitive(V_domain, V_outlet);
 
-    if (dynamic_grid)
-      conv_numerics->SetGridVel(geometry->nodes->GetGridVel(iPoint), geometry->nodes->GetGridVel(iPoint));
+        if (dynamic_grid)
+          conv_numerics->SetGridVel(geometry->nodes->GetGridVel(iPoint), geometry->nodes->GetGridVel(iPoint));
 
-    const su2double Temp_i = nodes->GetTemperature(iPoint);
-    const su2double Temp_j = nodes->GetTemperature(Point_Normal);
-    conv_numerics->SetScalarVar(&Temp_i, &Temp_j);
+        conv_numerics->SetTemperature(nodes->GetTemperature(iPoint), nodes->GetTemperature(Point_Normal));
 
-    /*--- Compute the residual using an upwind scheme ---*/
+        /*--- Compute the residual using an upwind scheme ---*/
 
-    auto residual = conv_numerics->ComputeResidual(config);
+        conv_numerics->ComputeResidual(Residual, Jacobian_i, Jacobian_j, config);
 
-    /*--- Update residual value ---*/
+        /*--- Update residual value ---*/
 
-    LinSysRes.AddBlock(iPoint, residual);
+        LinSysRes.AddBlock(iPoint, Residual);
 
-    /*--- Jacobian contribution for implicit integration ---*/
+        /*--- Jacobian contribution for implicit integration ---*/
 
-    if (implicit) Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
+        if (implicit)
+          Jacobian.AddBlock2Diag(iPoint, Jacobian_i);
+      }
+    }
   }
-  END_SU2_OMP_FOR
+
 }
 
 void CHeatSolver::BC_ConjugateHeat_Interface(CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker) {
 
-  const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+  su2double thermal_diffusivity, T_Conjugate, Tinterface, Tnormal_Conjugate, HeatFluxDensity, HeatFlux, Area;
+
+  const bool implicit = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
+
   const su2double Temperature_Ref = config->GetTemperature_Ref();
-  const su2double rho_cp_solid = config->GetMaterialDensity(0) * config->GetSpecific_Heat_Cp();
+  const su2double rho_cp_solid = config->GetMaterialDensity(0)*config->GetSpecific_Heat_Cp();
 
   if (flow) {
-    SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
+
     for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
 
       const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
       if (geometry->nodes->GetDomain(iPoint)) {
-        const su2double T_Conjugate = GetConjugateHeatVariable(val_marker, iVertex, 0) / Temperature_Ref;
 
-        nodes->SetSolution_Old(iPoint, &T_Conjugate);
+        const su2double* Normal = geometry->vertex[val_marker][iVertex]->GetNormal();
+        Area = GeometryToolbox::Norm(nDim, Normal);
+
+        T_Conjugate = GetConjugateHeatVariable(val_marker, iVertex, 0)/Temperature_Ref;
+
+        nodes->SetSolution_Old(iPoint,&T_Conjugate);
         LinSysRes(iPoint, 0) = 0.0;
         nodes->SetRes_TruncErrorZero(iPoint);
 
         if (implicit) Jacobian.DeleteValsRowi(iPoint);
       }
     }
-    END_SU2_OMP_FOR
   }
   else if (heat_equation) {
-    SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
+
     for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
 
       const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
@@ -559,35 +836,49 @@ void CHeatSolver::BC_ConjugateHeat_Interface(CGeometry *geometry, CSolver **solv
       if (geometry->nodes->GetDomain(iPoint)) {
 
         su2double const* Normal = geometry->vertex[val_marker][iVertex]->GetNormal();
-        const su2double Area = GeometryToolbox::Norm(nDim, Normal);
+        Area = GeometryToolbox::Norm(nDim, Normal);
 
-        const su2double thermal_diffusivity = GetConjugateHeatVariable(val_marker, iVertex, 2) / rho_cp_solid;
-        su2double HeatFlux = 0;
+        thermal_diffusivity = GetConjugateHeatVariable(val_marker, iVertex, 2)/rho_cp_solid;
 
         if ((config->GetKind_CHT_Coupling() == CHT_COUPLING::DIRECT_TEMPERATURE_ROBIN_HEATFLUX) ||
             (config->GetKind_CHT_Coupling() == CHT_COUPLING::AVERAGED_TEMPERATURE_ROBIN_HEATFLUX)) {
 
-          const su2double Tinterface = nodes->GetTemperature(iPoint);
-          const su2double Tnormal_Conjugate = GetConjugateHeatVariable(val_marker, iVertex, 3) / Temperature_Ref;
+          Tinterface        = nodes->GetTemperature(iPoint);
+          Tnormal_Conjugate = GetConjugateHeatVariable(val_marker, iVertex, 3)/Temperature_Ref;
 
-          const su2double HeatFluxDensity = thermal_diffusivity * (Tinterface - Tnormal_Conjugate);
-          HeatFlux = HeatFluxDensity * Area;
+          HeatFluxDensity   = thermal_diffusivity*(Tinterface - Tnormal_Conjugate);
+          HeatFlux          = HeatFluxDensity * Area;
 
           if (implicit) {
-            su2double Jacobian_i[] = {-thermal_diffusivity*Area};
-            Jacobian.SubtractBlock2Diag(iPoint, &Jacobian_i);
+
+            Jacobian_i[0][0] = -thermal_diffusivity*Area;
+            Jacobian.SubtractBlock2Diag(iPoint, Jacobian_i);
           }
         }
         else {
-          const su2double HeatFluxDensity =
-              GetConjugateHeatVariable(val_marker, iVertex, 1) / config->GetHeat_Flux_Ref();
-          HeatFlux = HeatFluxDensity*Area;
+
+          HeatFluxDensity = GetConjugateHeatVariable(val_marker, iVertex, 1)/config->GetHeat_Flux_Ref();
+          HeatFlux        = HeatFluxDensity*Area;
         }
 
-        LinSysRes(iPoint, 0) += HeatFlux;
+        Res_Visc[0] = -HeatFlux;
+        LinSysRes.SubtractBlock(iPoint, Res_Visc);
       }
     }
-    END_SU2_OMP_FOR
+  }
+}
+
+void CHeatSolver::BC_Periodic(CGeometry* geometry, CSolver** solver_container, CNumerics* numerics,
+                                           CConfig* config) {
+  /*--- Complete residuals for periodic boundary conditions. We loop over
+   the periodic BCs in matching pairs so that, in the event that there are
+   adjacent periodic markers, the repeated points will have their residuals
+   accumulated corectly during the communications. For implicit calculations
+   the Jacobians and linear system are also correctly adjusted here. ---*/
+
+  for (unsigned short iPeriodic = 1; iPeriodic <= config->GetnMarker_Periodic() / 2; iPeriodic++) {
+    InitiatePeriodicComms(geometry, config, iPeriodic, PERIODIC_RESIDUAL);
+    CompletePeriodicComms(geometry, config, iPeriodic, PERIODIC_RESIDUAL);
   }
 }
 
@@ -707,215 +998,339 @@ void CHeatSolver::Heat_Fluxes(CGeometry *geometry, CSolver **solver_container, C
 void CHeatSolver::SetTime_Step(CGeometry *geometry, CSolver **solver_container, CConfig *config,
                                unsigned short iMesh, unsigned long Iteration) {
 
-  const bool implicit      = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
-  const bool time_stepping = (config->GetTime_Marching() == TIME_MARCHING::TIME_STEPPING);
-  const bool dual_time     = (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
-                             (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND);
-  const su2double K_v = 0.25;
+  unsigned long iPoint, jPoint;
+  su2double Area, Vol, laminar_viscosity, eddy_viscosity, thermal_diffusivity, Prandtl_Lam, Prandtl_Turb, Mean_ProjVel, Mean_BetaInc2, Mean_DensityInc, Mean_SoundSpeed, Lambda;
+  su2double Global_Delta_Time = 0.0, Global_Delta_UnstTimeND = 0.0, Local_Delta_Time = 0.0, Local_Delta_Time_Inv, Local_Delta_Time_Visc, CFL_Reduction, K_v = 0.25;
+  const su2double* Normal;
 
-  const su2double prandtl_lam = config->GetPrandtl_Lam();
-  const su2double prandtl_turb = config->GetPrandtl_Turb();
-  const su2double constant_thermal_diffusivity = config->GetThermalDiffusivity();
+  const bool turb = ((config->GetKind_Solver() == MAIN_SOLVER::INC_RANS) || (config->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_INC_RANS));
+  const bool dual_time = ((config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
+                    (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND));
+  const bool implicit = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
 
-  const CVariable* flow_nodes = solver_container[FLOW_SOL] ? solver_container[FLOW_SOL]->GetNodes() : nullptr;
+  eddy_viscosity    = 0.0;
+  laminar_viscosity = config->GetMu_ConstantND();
+  Prandtl_Lam = config->GetPrandtl_Lam();
+  Prandtl_Turb = config->GetPrandtl_Turb();
 
-  /*--- Init thread-shared variables to compute min/max values.
-   *    Critical sections are used for this instead of reduction
-   *    clauses for compatibility with OpenMP 2.0 (Windows...). ---*/
-  BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
-    Min_Delta_Time = 1e30;
-    Max_Delta_Time = 0.0;
-    Global_Delta_UnstTimeND = 1e30;
-  } END_SU2_OMP_SAFE_GLOBAL_ACCESS
+  thermal_diffusivity = config->GetThermalDiffusivity();
 
-  /*--- Loop domain points. ---*/
+  /*--- Compute spectral radius based on thermal conductivity ---*/
 
-  SU2_OMP_FOR_DYN(omp_chunk_size)
-  for (auto iPoint = 0ul; iPoint < nPointDomain; ++iPoint) {
+  Min_Delta_Time = 1.E30; Max_Delta_Time = 0.0;
+  CFL_Reduction = config->GetCFLRedCoeff_Turb();
 
-    /*--- Set maximum eigenvalues to zero. ---*/
+  for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
+    nodes->SetMax_Lambda_Inv(iPoint,0.0);
+    nodes->SetMax_Lambda_Visc(iPoint,0.0);
+  }
 
-    nodes->SetMax_Lambda_Visc(iPoint, 0.0);
+  /*--- Loop interior edges ---*/
 
-    /*--- Loop over the neighbors of point i. ---*/
+  for (auto iEdge = 0ul; iEdge < geometry->GetnEdge(); iEdge++) {
 
-    for (unsigned short iNeigh = 0; iNeigh < geometry->nodes->GetnPoint(iPoint); ++iNeigh) {
-      const auto jPoint = geometry->nodes->GetPoint(iPoint,iNeigh);
-      const auto iEdge = geometry->nodes->GetEdge(iPoint,iNeigh);
-      const auto* Normal = geometry->edges->GetNormal(iEdge);
-      const su2double Area2 = GeometryToolbox::SquaredNorm(nDim, Normal);
+    iPoint = geometry->edges->GetNode(iEdge,0);
+    jPoint = geometry->edges->GetNode(iEdge,1);
 
-      if (flow) {
-        const su2double laminar_viscosity = 0.5 * (flow_nodes->GetLaminarViscosity(iPoint) +
-                                                   flow_nodes->GetLaminarViscosity(jPoint));
-        const su2double eddy_viscosity = 0.5 * (flow_nodes->GetEddyViscosity(iPoint) +
-                                                flow_nodes->GetEddyViscosity(jPoint));
-
-        const su2double thermal_diffusivity = laminar_viscosity / prandtl_lam + eddy_viscosity / prandtl_turb;
-        nodes->AddMax_Lambda_Visc(iPoint, thermal_diffusivity * Area2);
-      } else {
-        nodes->AddMax_Lambda_Visc(iPoint, constant_thermal_diffusivity * Area2);
+    /*--- get the edge's normal vector to compute the edge's area ---*/
+    Normal = geometry->edges->GetNormal(iEdge);
+    Area = GeometryToolbox::Norm(nDim, Normal);
+
+    /*--- Inviscid contribution ---*/
+
+    if (flow) {
+      Mean_ProjVel = 0.5 * (solver_container[FLOW_SOL]->GetNodes()->GetProjVel(iPoint,Normal) + solver_container[FLOW_SOL]->GetNodes()->GetProjVel(jPoint,Normal));
+      Mean_BetaInc2 = 0.5 * (solver_container[FLOW_SOL]->GetNodes()->GetBetaInc2(iPoint) + solver_container[FLOW_SOL]->GetNodes()->GetBetaInc2(jPoint));
+      Mean_DensityInc = 0.5 * (solver_container[FLOW_SOL]->GetNodes()->GetDensity(iPoint) + solver_container[FLOW_SOL]->GetNodes()->GetDensity(jPoint));
+      Mean_SoundSpeed = sqrt(Mean_ProjVel*Mean_ProjVel + (Mean_BetaInc2/Mean_DensityInc)*Area*Area);
+
+      Lambda = fabs(Mean_ProjVel) + Mean_SoundSpeed;
+      if (geometry->nodes->GetDomain(iPoint)) nodes->AddMax_Lambda_Inv(iPoint, Lambda);
+      if (geometry->nodes->GetDomain(jPoint)) nodes->AddMax_Lambda_Inv(jPoint, Lambda);
+    }
+
+    /*--- Viscous contribution ---*/
+
+    thermal_diffusivity = config->GetThermalDiffusivity();
+    if(flow) {
+      if(turb) {
+        eddy_viscosity = solver_container[TURB_SOL]->GetNodes()->GetmuT(iPoint);
       }
+
+      thermal_diffusivity = laminar_viscosity/Prandtl_Lam + eddy_viscosity/Prandtl_Turb;
     }
+
+    Lambda = thermal_diffusivity*Area*Area;
+    if (geometry->nodes->GetDomain(iPoint)) nodes->AddMax_Lambda_Visc(iPoint, Lambda);
+    if (geometry->nodes->GetDomain(jPoint)) nodes->AddMax_Lambda_Visc(jPoint, Lambda);
+
   }
-  END_SU2_OMP_FOR
 
   /*--- Loop boundary edges ---*/
 
-  for (unsigned short iMarker = 0; iMarker < geometry->GetnMarker(); iMarker++) {
-    if ((config->GetMarker_All_KindBC(iMarker) != INTERNAL_BOUNDARY) &&
-        (config->GetMarker_All_KindBC(iMarker) != NEARFIELD_BOUNDARY) &&
-        (config->GetMarker_All_KindBC(iMarker) != PERIODIC_BOUNDARY)) {
+  for (auto iMarker = 0u; iMarker < geometry->GetnMarker(); iMarker++) {
+    for (auto iVertex = 0ul; iVertex < geometry->GetnVertex(iMarker); iVertex++) {
 
-      SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
-      for (auto iVertex = 0ul; iVertex < geometry->GetnVertex(iMarker); iVertex++) {
+      /*--- Point identification, Normal vector and area ---*/
 
-        /*--- Point identification, Normal vector and area ---*/
+      iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+      Normal = geometry->vertex[iMarker][iVertex]->GetNormal();
+      Area = GeometryToolbox::Norm(nDim, Normal);
 
-        const auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+      /*--- Inviscid contribution ---*/
 
-        if (!geometry->nodes->GetDomain(iPoint)) continue;
+      if (flow) {
+        Mean_ProjVel = solver_container[FLOW_SOL]->GetNodes()->GetProjVel(iPoint, Normal);
+        Mean_BetaInc2 = solver_container[FLOW_SOL]->GetNodes()->GetBetaInc2(iPoint);
+        Mean_DensityInc = solver_container[FLOW_SOL]->GetNodes()->GetDensity(iPoint);
+        Mean_SoundSpeed = sqrt(Mean_ProjVel*Mean_ProjVel + (Mean_BetaInc2/Mean_DensityInc)*Area*Area);
 
-        const auto* Normal = geometry->vertex[iMarker][iVertex]->GetNormal();
-        const su2double Area2 = GeometryToolbox::SquaredNorm(nDim, Normal);
+        Lambda = fabs(Mean_ProjVel) + Mean_SoundSpeed;
+        if (geometry->nodes->GetDomain(iPoint)) nodes->AddMax_Lambda_Inv(iPoint, Lambda);
+      }
 
-        if (flow) {
-          const su2double thermal_diffusivity = flow_nodes->GetLaminarViscosity(iPoint) / prandtl_lam +
-                                                flow_nodes->GetEddyViscosity(iPoint) / prandtl_turb;
-          nodes->AddMax_Lambda_Visc(iPoint, thermal_diffusivity * Area2);
-        } else {
-          nodes->AddMax_Lambda_Visc(iPoint, constant_thermal_diffusivity * Area2);
+      /*--- Viscous contribution ---*/
+
+      thermal_diffusivity = config->GetThermalDiffusivity();
+      if(flow) {
+        if(turb) {
+          eddy_viscosity = solver_container[TURB_SOL]->GetNodes()->GetmuT(iPoint);
         }
+
+        thermal_diffusivity = laminar_viscosity/Prandtl_Lam + eddy_viscosity/Prandtl_Turb;
       }
-      END_SU2_OMP_FOR
+
+      Lambda = thermal_diffusivity*Area*Area;
+      if (geometry->nodes->GetDomain(iPoint)) nodes->AddMax_Lambda_Visc(iPoint, Lambda);
+
     }
   }
 
-  /*--- Each element uses their own speed, steady state simulation. ---*/
-  {
-    /*--- Thread-local variables for min/max reduction. ---*/
-    su2double minDt = 1e30, maxDt = 0.0;
+  /*--- Each element uses their own speed, steady state simulation ---*/
 
-    SU2_OMP_FOR_(schedule(static,omp_chunk_size) SU2_NOWAIT)
-    for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
+  for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
 
-      su2double local_delta_time = 0.0;
-
-      const su2double Vol = geometry->nodes->GetVolume(iPoint);
-      if (Vol != 0.0) {
-        local_delta_time = nodes->GetLocalCFL(iPoint) * K_v * pow(Vol, 2) / nodes->GetMax_Lambda_Visc(iPoint);
-        if (flow) {
-          switch (config->GetKind_TimeStep_Heat()) {
-            case BYFLOW:
-            case CONVECTIVE:
-              local_delta_time = flow_nodes->GetDelta_Time(iPoint);
-              break;
-            case MINIMUM:
-              local_delta_time = min(local_delta_time, flow_nodes->GetDelta_Time(iPoint));
-              break;
-            case VISCOUS:
-              break;
-            default:
-              break;
-          }
-        }
-        minDt = min(minDt, local_delta_time);
-        maxDt = max(maxDt, local_delta_time);
+    Vol = geometry->nodes->GetVolume(iPoint);
+
+    if (Vol != 0.0) {
+
+      if(flow) {
+        Local_Delta_Time_Inv = config->GetCFL(iMesh)*Vol / nodes->GetMax_Lambda_Inv(iPoint);
+        Local_Delta_Time_Visc = config->GetCFL(iMesh)*K_v*Vol*Vol/ nodes->GetMax_Lambda_Visc(iPoint);
+      }
+      else {
+        Local_Delta_Time_Inv = config->GetMax_DeltaTime();
+        Local_Delta_Time_Visc = config->GetCFL(iMesh)*K_v*Vol*Vol/ nodes->GetMax_Lambda_Visc(iPoint);
+        //Local_Delta_Time_Visc = 100.0*K_v*Vol*Vol/ nodes->GetMax_Lambda_Visc(iPoint);
       }
-      nodes->SetDelta_Time(iPoint, local_delta_time);
+
+      /*--- Time step setting method ---*/
+
+      if (config->GetKind_TimeStep_Heat() == BYFLOW && flow) {
+        Local_Delta_Time = solver_container[FLOW_SOL]->GetNodes()->GetDelta_Time(iPoint);
+      }
+      else if (config->GetKind_TimeStep_Heat() == MINIMUM) {
+        Local_Delta_Time = min(Local_Delta_Time_Inv, Local_Delta_Time_Visc);
+      }
+      else if (config->GetKind_TimeStep_Heat() == CONVECTIVE) {
+        Local_Delta_Time = Local_Delta_Time_Inv;
+      }
+      else if (config->GetKind_TimeStep_Heat() == VISCOUS) {
+        Local_Delta_Time = Local_Delta_Time_Visc;
+      }
+
+      /*--- Min-Max-Logic ---*/
+
+      Global_Delta_Time = min(Global_Delta_Time, Local_Delta_Time);
+      Min_Delta_Time = min(Min_Delta_Time, Local_Delta_Time);
+      Max_Delta_Time = max(Max_Delta_Time, Local_Delta_Time);
+      if (Local_Delta_Time > config->GetMax_DeltaTime())
+        Local_Delta_Time = config->GetMax_DeltaTime();
+
+      nodes->SetDelta_Time(iPoint,CFL_Reduction*Local_Delta_Time);
     }
-    END_SU2_OMP_FOR
-    /*--- Min/max over threads. ---*/
-    SU2_OMP_CRITICAL
-    {
-      Min_Delta_Time = min(Min_Delta_Time, minDt);
-      Max_Delta_Time = max(Max_Delta_Time, maxDt);
-      Global_Delta_Time = Min_Delta_Time;
+    else {
+      nodes->SetDelta_Time(iPoint,0.0);
     }
-    END_SU2_OMP_CRITICAL
   }
 
-  /*--- Compute the min/max dt (in parallel, now over mpi ranks). ---*/
+  /*--- Compute the max and the min dt (in parallel) ---*/
+  if (config->GetComm_Level() == COMM_FULL) {
+#ifdef HAVE_MPI
+    su2double rbuf_time, sbuf_time;
+    sbuf_time = Min_Delta_Time;
+    SU2_MPI::Reduce(&sbuf_time, &rbuf_time, 1, MPI_DOUBLE, MPI_MIN, MASTER_NODE, SU2_MPI::GetComm());
+    SU2_MPI::Bcast(&rbuf_time, 1, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
+    Min_Delta_Time = rbuf_time;
+
+    sbuf_time = Max_Delta_Time;
+    SU2_MPI::Reduce(&sbuf_time, &rbuf_time, 1, MPI_DOUBLE, MPI_MAX, MASTER_NODE, SU2_MPI::GetComm());
+    SU2_MPI::Bcast(&rbuf_time, 1, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
+    Max_Delta_Time = rbuf_time;
+#endif
+  }
 
-  BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
-    if (config->GetComm_Level() == COMM_FULL) {
-      su2double rbuf_time;
-      SU2_MPI::Allreduce(&Min_Delta_Time, &rbuf_time, 1, MPI_DOUBLE, MPI_MIN, SU2_MPI::GetComm());
-      Min_Delta_Time = rbuf_time;
+  /*--- For exact time solution use the minimum delta time of the whole mesh ---*/
+  if (config->GetTime_Marching() == TIME_MARCHING::TIME_STEPPING) {
+#ifdef HAVE_MPI
+    su2double rbuf_time, sbuf_time;
+    sbuf_time = Global_Delta_Time;
+    SU2_MPI::Reduce(&sbuf_time, &rbuf_time, 1, MPI_DOUBLE, MPI_MIN, MASTER_NODE, SU2_MPI::GetComm());
+    SU2_MPI::Bcast(&rbuf_time, 1, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
+    Global_Delta_Time = rbuf_time;
+#endif
+    for (iPoint = 0; iPoint < nPointDomain; iPoint++)
+      nodes->SetDelta_Time(iPoint,Global_Delta_Time);
+  }
 
-      SU2_MPI::Allreduce(&Max_Delta_Time, &rbuf_time, 1, MPI_DOUBLE, MPI_MAX, SU2_MPI::GetComm());
-      Max_Delta_Time = rbuf_time;
-    }
-  } END_SU2_OMP_SAFE_GLOBAL_ACCESS
+  /*--- Recompute the unsteady time step for the dual time strategy
+   if the unsteady CFL is diferent from 0 ---*/
+  if ((dual_time) && (Iteration == 0) && (config->GetUnst_CFL() != 0.0) && (iMesh == MESH_0)) {
+    Global_Delta_UnstTimeND = config->GetUnst_CFL()*Global_Delta_Time/config->GetCFL(iMesh);
+
+#ifdef HAVE_MPI
+    su2double rbuf_time, sbuf_time;
+    sbuf_time = Global_Delta_UnstTimeND;
+    SU2_MPI::Reduce(&sbuf_time, &rbuf_time, 1, MPI_DOUBLE, MPI_MIN, MASTER_NODE, SU2_MPI::GetComm());
+    SU2_MPI::Bcast(&rbuf_time, 1, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
+    Global_Delta_UnstTimeND = rbuf_time;
+#endif
+    config->SetDelta_UnstTimeND(Global_Delta_UnstTimeND);
+  }
 
-  /*--- For exact time solution use the minimum delta time of the whole mesh. ---*/
-  if (time_stepping) {
+  /*--- The pseudo local time (explicit integration) cannot be greater than the physical time ---*/
+  if (dual_time)
+    for (iPoint = 0; iPoint < nPointDomain; iPoint++) {
+      if (!implicit) {
+        cout << "Using unsteady time: " << config->GetDelta_UnstTimeND() << endl;
+        Local_Delta_Time = min((2.0/3.0)*config->GetDelta_UnstTimeND(), nodes->GetDelta_Time(iPoint));
+        nodes->SetDelta_Time(iPoint,Local_Delta_Time);
+      }
+  }
+}
 
-    /*--- If the unsteady CFL is set to zero, it uses the defined unsteady time step,
-     *    otherwise it computes the time step based on the unsteady CFL. ---*/
+void CHeatSolver::ExplicitEuler_Iteration(CGeometry *geometry, CSolver **solver_container, CConfig *config) {
 
-    BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS
-    {
-      if (config->GetUnst_CFL() == 0.0) {
-        Global_Delta_Time = config->GetDelta_UnstTime();
-      }
-      else {
-        Global_Delta_Time = Min_Delta_Time;
-      }
-      Max_Delta_Time = Global_Delta_Time;
+  su2double *local_Residual, *local_Res_TruncError, Vol, Delta, Res;
 
-      config->SetDelta_UnstTimeND(Global_Delta_Time);
-    }
-    END_SU2_OMP_SAFE_GLOBAL_ACCESS
+  SetResToZero();
 
-    /*--- Sets the regular CFL equal to the unsteady CFL. ---*/
+  /*--- Update the solution ---*/
 
-    SU2_OMP_FOR_STAT(omp_chunk_size)
-    for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
-      nodes->SetLocalCFL(iPoint, config->GetUnst_CFL());
-      nodes->SetDelta_Time(iPoint, Global_Delta_Time);
+  for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
+    Vol = geometry->nodes->GetVolume(iPoint);
+    Delta = nodes->GetDelta_Time(iPoint) / Vol;
+
+    local_Res_TruncError = nodes->GetResTruncError(iPoint);
+    local_Residual = LinSysRes.GetBlock(iPoint);
+
+    if (!config->GetContinuous_Adjoint()) {
+      for (auto iVar = 0u; iVar < nVar; iVar++) {
+        Res = local_Residual[iVar] + local_Res_TruncError[iVar];
+        nodes->AddSolution(iPoint,iVar, -Res*Delta);
+        Residual_RMS[iVar] += Res*Res;
+        AddRes_Max(iVar, fabs(Res), geometry->nodes->GetGlobalIndex(iPoint), geometry->nodes->GetCoord(iPoint));
+      }
     }
-    END_SU2_OMP_FOR
 
   }
 
-  /*--- Recompute the unsteady time step for the dual time strategy if the unsteady CFL is diferent from 0.
-    * This is only done once because in dual time the time step cannot be variable. ---*/
+  /*--- MPI solution ---*/
 
-  if (dual_time && (Iteration == config->GetRestart_Iter()) && (config->GetUnst_CFL() != 0.0) && (iMesh == MESH_0)) {
+  InitiateComms(geometry, config, SOLUTION);
+  CompleteComms(geometry, config, SOLUTION);
 
-    /*--- Thread-local variable for reduction. ---*/
-    su2double glbDtND = 1e30;
+  /*--- Compute the root mean square residual ---*/
 
-    SU2_OMP_FOR_(schedule(static,omp_chunk_size) SU2_NOWAIT)
-    for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
-      glbDtND = min(glbDtND, config->GetUnst_CFL()*Global_Delta_Time / nodes->GetLocalCFL(iPoint));
+  SetResidual_RMS(geometry, config);
+
+}
+
+
+void CHeatSolver::ImplicitEuler_Iteration(CGeometry *geometry, CSolver **solver_container, CConfig *config) {
+
+  /*--- Set maximum residual to zero ---*/
+
+  SetResToZero();
+
+  /*--- Build implicit system ---*/
+
+  for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
+
+    /*--- Read the residual ---*/
+
+    su2double* local_Res_TruncError = nodes->GetResTruncError(iPoint);
+
+    /*--- Modify matrix diagonal to assure diagonal dominance ---*/
+
+    const su2double dt = nodes->GetDelta_Time(iPoint);
+    if (dt != 0.0) {
+      /*--- For nodes on periodic boundaries, add the respective partner volume. ---*/
+      // Identical for flow and heat
+      const su2double Vol = geometry->nodes->GetVolume(iPoint) + geometry->nodes->GetPeriodicVolume(iPoint);
+      Jacobian.AddVal2Diag(iPoint, Vol / dt);
+
+    } else {
+      Jacobian.SetVal2Diag(iPoint, 1.0);
+      for (auto iVar = 0u; iVar < nVar; iVar++) {
+        const auto total_index = iPoint*nVar + iVar;
+        LinSysRes[total_index] = 0.0;
+        local_Res_TruncError[iVar] = 0.0;
+      }
     }
-    END_SU2_OMP_FOR
-    SU2_OMP_CRITICAL
-    Global_Delta_UnstTimeND = min(Global_Delta_UnstTimeND, glbDtND);
-    END_SU2_OMP_CRITICAL
 
-    BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS
-    {
-      SU2_MPI::Allreduce(&Global_Delta_UnstTimeND, &glbDtND, 1, MPI_DOUBLE, MPI_MIN, SU2_MPI::GetComm());
-      Global_Delta_UnstTimeND = glbDtND;
+    /*--- Right hand side of the system (-Residual) and initial guess (x = 0) ---*/
 
-      config->SetDelta_UnstTimeND(Global_Delta_UnstTimeND);
+    for (auto iVar = 0; iVar < nVar; iVar++) {
+      const auto total_index = iPoint*nVar+iVar;
+      LinSysRes[total_index] = - (LinSysRes[total_index] + local_Res_TruncError[iVar]);
+      LinSysSol[total_index] = 0.0;
+      Residual_RMS[iVar] += LinSysRes[total_index]*LinSysRes[total_index];
+      AddRes_Max(iVar, fabs(LinSysRes[total_index]), geometry->nodes->GetGlobalIndex(iPoint), geometry->nodes->GetCoord(iPoint));
     }
-    END_SU2_OMP_SAFE_GLOBAL_ACCESS
   }
 
-  /*--- The pseudo local time (explicit integration) cannot be greater than the physical time ---*/
+  /*--- Initialize residual and solution at the ghost points ---*/
 
-  if (dual_time && !implicit) {
-    SU2_OMP_FOR_STAT(omp_chunk_size)
-    for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
-      su2double dt = min((2.0/3.0)*config->GetDelta_UnstTimeND(), nodes->GetDelta_Time(iPoint));
-      nodes->SetDelta_Time(iPoint, dt);
+  for (auto iPoint = nPointDomain; iPoint < nPoint; iPoint++) {
+    for (auto iVar = 0u; iVar < nVar; iVar++) {
+      const auto total_index = iPoint*nVar + iVar;
+      LinSysRes[total_index] = 0.0;
+      LinSysSol[total_index] = 0.0;
+    }
+  }
+
+  /*--- Solve or smooth the linear system ---*/
+
+  auto iter = System.Solve(Jacobian, LinSysRes, LinSysSol, geometry, config);
+
+  /*--- Store the the number of iterations of the linear solver ---*/
+  SetIterLinSolver(iter);
+
+  /*--- Store the value of the residual. ---*/
+  SetResLinSolver(System.GetResidual());
+
+  for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
+    for (auto iVar = 0u; iVar < nVar; iVar++) {
+      nodes->AddSolution(iPoint,iVar, LinSysSol[iPoint*nVar+iVar]);
     }
-    END_SU2_OMP_FOR
   }
+
+  /*--- Synchronize the solution between master and passive periodic nodes after the linear solve. ---*/
+  for (unsigned short iPeriodic = 1; iPeriodic <= config->GetnMarker_Periodic() / 2; iPeriodic++) {
+    InitiatePeriodicComms(geometry, config, iPeriodic, PERIODIC_IMPLICIT);
+    CompletePeriodicComms(geometry, config, iPeriodic, PERIODIC_IMPLICIT);
+  }
+
+  /*--- MPI solution ---*/
+
+  InitiateComms(geometry, config, SOLUTION);
+  CompleteComms(geometry, config, SOLUTION);
+
+  /*--- Compute the root mean square residual ---*/
+
+  SetResidual_RMS(geometry, config);
+
 }
 
 void CHeatSolver::SetInitialCondition(CGeometry **geometry, CSolver ***solver_container, CConfig *config, unsigned long TimeIter) {
@@ -967,57 +1382,67 @@ void CHeatSolver::SetInitialCondition(CGeometry **geometry, CSolver ***solver_co
 
 void CHeatSolver::SetResidual_DualTime(CGeometry *geometry, CSolver **solver_container, CConfig *config,
                                        unsigned short iRKStep, unsigned short iMesh, unsigned short RunTime_EqSystem) {
-  if (flow) {
-    CScalarSolver<CHeatVariable>::SetResidual_DualTime(geometry, solver_container, config, iRKStep, iMesh, RunTime_EqSystem);
-    return;
-  }
+
+  /*--- Local variables ---*/
+
+  const su2double *U_time_n, *U_time_nP1, *U_time_nM1;
+  su2double Volume_nP1;
+
   const bool first_order  = (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST);
   const bool second_order = (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND);
-  const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+  const bool implicit = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
 
   /*--- Store the physical time step ---*/
 
   const su2double TimeStep = config->GetDelta_UnstTimeND();
 
-  /*--- Compute the dual time-stepping source term ---*/
-  /*--- Loop over all nodes (excluding halos) ---*/
+  /*--- Compute the dual time-stepping source term for static meshes ---*/
 
-  AD::StartNoSharedReading();
+  if (!dynamic_grid) {
 
-  SU2_OMP_FOR_STAT(omp_chunk_size)
-  for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
+    /*--- Loop over all nodes (excluding halos) ---*/
+
+    for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
 
-    /*--- Retrieve the solution at time levels n-1, n, and n+1. Note that
-      we are currently iterating on U^n+1 and that U^n & U^n-1 are fixed,
-      previous solutions that are stored in memory. ---*/
+      /*--- Retrieve the solution at time levels n-1, n, and n+1. Note that
+       we are currently iterating on U^n+1 and that U^n & U^n-1 are fixed,
+       previous solutions that are stored in memory. ---*/
 
-    const auto* U_time_nM1 = nodes->GetSolution_time_n1(iPoint);
-    const auto* U_time_n = nodes->GetSolution_time_n(iPoint);
-    const auto* U_time_nP1 = nodes->GetSolution(iPoint);
+      U_time_nM1 = nodes->GetSolution_time_n1(iPoint);
+      U_time_n   = nodes->GetSolution_time_n(iPoint);
+      U_time_nP1 = nodes->GetSolution(iPoint);
 
-    /*--- CV volume at time n+1. As we are on a static mesh, the volume
-      of the CV will remained fixed for all time steps. ---*/
+      /*--- CV volume at time n+1. As we are on a static mesh, the volume
+       of the CV will remained fixed for all time steps. ---*/
 
-    const su2double Volume_nP1 = geometry->nodes->GetVolume(iPoint);
+      Volume_nP1 = geometry->nodes->GetVolume(iPoint);
 
-    /*--- Compute the dual time-stepping source term based on the chosen
-      time discretization scheme (1st- or 2nd-order).---*/
+      /*--- Compute the dual time-stepping source term based on the chosen
+       time discretization scheme (1st- or 2nd-order).---*/
 
-    for (auto iVar = 0u; iVar < nVar; iVar++) {
-      if (first_order)
-        LinSysRes(iPoint, iVar) += (U_time_nP1[iVar] - U_time_n[iVar]) * Volume_nP1 / TimeStep;
-      if (second_order)
-        LinSysRes(iPoint, iVar) += (3.0 * U_time_nP1[iVar] - 4.0 * U_time_n[iVar] +
-                                    1.0 * U_time_nM1[iVar]) * Volume_nP1 / (2.0 * TimeStep);
-    }
+      for (auto iVar = 0u; iVar < nVar; iVar++) {
+        if (first_order)
+          Residual[iVar] = (U_time_nP1[iVar] - U_time_n[iVar])*Volume_nP1 / TimeStep;
+        if (second_order)
+          Residual[iVar] = ( 3.0*U_time_nP1[iVar] - 4.0*U_time_n[iVar]
+                            +1.0*U_time_nM1[iVar])*Volume_nP1 / (2.0*TimeStep);
+      }
 
-    /*--- Compute the Jacobian contribution due to the dual time source term. ---*/
-    if (implicit) {
-      if (first_order) Jacobian.AddVal2Diag(iPoint, Volume_nP1 / TimeStep);
-      if (second_order) Jacobian.AddVal2Diag(iPoint, (Volume_nP1 * 3.0) / (2.0 * TimeStep));
+      /*--- Store the residual and compute the Jacobian contribution due
+       to the dual time source term. ---*/
+
+      LinSysRes.AddBlock(iPoint, Residual);
+      if (implicit) {
+        for (auto iVar = 0u; iVar < nVar; iVar++) {
+          for (auto jVar = 0u; jVar < nVar; jVar++) Jacobian_i[iVar][jVar] = 0.0;
+          if (first_order)
+            Jacobian_i[iVar][iVar] = Volume_nP1 / TimeStep;
+          if (second_order)
+            Jacobian_i[iVar][iVar] = (Volume_nP1*3.0)/(2.0*TimeStep);
+        }
+
+        Jacobian.AddBlock2Diag(iPoint, Jacobian_i);
+      }
     }
   }
-  END_SU2_OMP_FOR
-
-  AD::EndNoSharedReading();
 }
diff --git a/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp b/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
index ea4e4b60aec..147def267fa 100644
--- a/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
@@ -1,7 +1,7 @@
 /*!
  * \file CNEMOEulerSolver.cpp
  * \brief Headers of the CNEMOEulerSolver class
- * \author S. R. Copeland, F. Palacios, W. Maier, C. Garbacz, J. Needels
+ * \author S. R. Copeland, F. Palacios, W. Maier, C. Garbacz
  * \version 7.5.0 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
@@ -1503,86 +1503,90 @@ void CNEMOEulerSolver::BC_Sym_Plane(CGeometry *geometry, CSolver **solver_contai
   }
 }
 
-void CNEMOEulerSolver::BC_Far_Field(CGeometry *geometry,
-                                    CSolver **solver_container,
-                                    CNumerics *conv_numerics,
-                                    CNumerics *visc_numerics, CConfig *config,
-                                    unsigned short val_marker) {
+void CNEMOEulerSolver::BC_Far_Field(CGeometry *geometry, CSolver **solver_container,
+                                    CNumerics *conv_numerics, CNumerics *visc_numerics,
+                                    CConfig *config, unsigned short val_marker) {
+
+  unsigned short iDim;
+  unsigned long iVertex, iPoint, Point_Normal;
+
+  su2double *V_infty, *V_domain, *U_infty, *U_domain;
+
+  /*--- Set booleans from configuration parameters ---*/
+  bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+  bool viscous  = config->GetViscous();
 
   /*--- Allocate arrays ---*/
-  su2double Normal[MAXNDIM] = {0.0};
+  su2double *Normal = new su2double[nDim];
 
   /*--- Loop over all the vertices on this boundary (val_marker) ---*/
-  for (unsigned long iVertex = 0; iVertex < geometry->nVertex[val_marker];
-       iVertex++) {
-    const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
+  for (iVertex = 0; iVertex < geometry->nVertex[val_marker]; iVertex++) {
+    iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
+
+    /*--- Allocate the value at the infinity ---*/
+    V_infty = GetCharacPrimVar(val_marker, iVertex);
 
     /*--- Check if the node belongs to the domain (i.e, not a halo node) ---*/
     if (geometry->nodes->GetDomain(iPoint)) {
 
       /*--- Retrieve index of the closest interior node ---*/
-      const auto Point_Normal = geometry->vertex[val_marker][iVertex]
-              ->GetNormal_Neighbor(); // only used for implicit
+      Point_Normal = geometry->vertex[val_marker][iVertex]->GetNormal_Neighbor(); //only used for implicit
 
       /*--- Pass boundary node normal to CNumerics ---*/
       geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
-      for (unsigned short iDim = 0; iDim < nDim; iDim++)
-        Normal[iDim] = -Normal[iDim];
+      for (iDim = 0; iDim < nDim; iDim++) Normal[iDim] = -Normal[iDim];
       conv_numerics->SetNormal(Normal);
 
+      /*--- Retrieve solution at the boundary node & free-stream ---*/
+      U_domain = nodes->GetSolution(iPoint);
+      V_domain = nodes->GetPrimitive(iPoint);
+      U_infty  = node_infty->GetSolution(0);
+      V_infty  = node_infty->GetPrimitive(0);
+
       /*--- Pass conserved & primitive variables to CNumerics ---*/
-      conv_numerics->SetConservative(nodes->GetSolution(iPoint),
-                                     node_infty->GetSolution(0));
-      conv_numerics->SetPrimitive(nodes->GetPrimitive(iPoint),
-                                  node_infty->GetPrimitive(0));
+      conv_numerics->SetConservative(U_domain, U_infty);
+      conv_numerics->SetPrimitive(V_domain, V_infty);
 
       /*--- Pass supplementary information to CNumerics ---*/
-      conv_numerics->SetdPdU(nodes->GetdPdU(iPoint), node_infty->GetdPdU(0));
-      conv_numerics->SetdTdU(nodes->GetdTdU(iPoint), node_infty->GetdTdU(0));
-      conv_numerics->SetdTvedU(nodes->GetdTvedU(iPoint),
-                               node_infty->GetdTvedU(0));
-      conv_numerics->SetEve(nodes->GetEve(iPoint), node_infty->GetEve(0));
-      conv_numerics->SetCvve(nodes->GetCvve(iPoint), node_infty->GetCvve(0));
-      conv_numerics->SetGamma(nodes->GetGamma(iPoint), node_infty->GetGamma(0));
+      conv_numerics->SetdPdU  (nodes->GetdPdU(iPoint),   node_infty->GetdPdU(0));
+      conv_numerics->SetdTdU  (nodes->GetdTdU(iPoint),   node_infty->GetdTdU(0));
+      conv_numerics->SetdTvedU(nodes->GetdTvedU(iPoint), node_infty->GetdTvedU(0));
+      conv_numerics->SetEve   (nodes->GetEve(iPoint),    node_infty->GetEve(0));
+      conv_numerics->SetCvve  (nodes->GetCvve(iPoint),   node_infty->GetCvve(0));
+      conv_numerics->SetGamma (nodes->GetGamma(iPoint),  node_infty->GetGamma(0));
 
       /*--- Compute the convective residual (and Jacobian) ---*/
-      // Note: This uses the specified boundary num. method specified in
-      // driver_structure.cpp
+      // Note: This uses the specified boundary num. method specified in driver_structure.cpp
       auto residual = conv_numerics->ComputeResidual(config);
 
       /*--- Apply contribution to the linear system ---*/
       LinSysRes.AddBlock(iPoint, residual);
 
-      const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
       if (implicit)
         Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
 
       /*--- Viscous contribution ---*/
-      bool viscous = config->GetViscous();
       if (viscous) {
         su2double Coord_Reflected[MAXNDIM];
-        GeometryToolbox::PointPointReflect(
-            nDim, geometry->nodes->GetCoord(Point_Normal),
-            geometry->nodes->GetCoord(iPoint), Coord_Reflected);
-        visc_numerics->SetCoord(geometry->nodes->GetCoord(iPoint),
-                                Coord_Reflected);
+        GeometryToolbox::PointPointReflect(nDim, geometry->nodes->GetCoord(Point_Normal),
+                                                 geometry->nodes->GetCoord(iPoint), Coord_Reflected);
+        visc_numerics->SetCoord(geometry->nodes->GetCoord(iPoint), Coord_Reflected );
         visc_numerics->SetNormal(Normal);
 
         /*--- Primitive variables, and gradient ---*/
         visc_numerics->SetConservative(nodes->GetSolution(iPoint),
-                                       node_infty->GetSolution(0));
+                                       node_infty->GetSolution(0) );
         visc_numerics->SetPrimitive(nodes->GetPrimitive(iPoint),
-                                    node_infty->GetPrimitive(0));
+                                    node_infty->GetPrimitive(0) );
         visc_numerics->SetPrimVarGradient(nodes->GetGradient_Primitive(iPoint),
-                                          node_infty->GetGradient_Primitive(0));
+                                          node_infty->GetGradient_Primitive(0) );
 
         /*--- Pass supplementary information to CNumerics ---*/
-        visc_numerics->SetdPdU(nodes->GetdPdU(iPoint), node_infty->GetdPdU(0));
-        visc_numerics->SetdTdU(nodes->GetdTdU(iPoint), node_infty->GetdTdU(0));
-        visc_numerics->SetdTvedU(nodes->GetdTvedU(iPoint),
-                                 node_infty->GetdTvedU(0));
-        visc_numerics->SetEve(nodes->GetEve(iPoint), node_infty->GetEve(0));
-        visc_numerics->SetCvve(nodes->GetCvve(iPoint), node_infty->GetCvve(0));
+        visc_numerics->SetdPdU  (nodes->GetdPdU(iPoint),   node_infty->GetdPdU(0));
+        visc_numerics->SetdTdU  (nodes->GetdTdU(iPoint),   node_infty->GetdTdU(0));
+        visc_numerics->SetdTvedU(nodes->GetdTvedU(iPoint), node_infty->GetdTvedU(0));
+        visc_numerics->SetEve   (nodes->GetEve(iPoint),    node_infty->GetEve(0));
+        visc_numerics->SetCvve  (nodes->GetCvve(iPoint),   node_infty->GetCvve(0));
 
         /*--- Species diffusion coefficients ---*/
         visc_numerics->SetDiffusionCoeff(nodes->GetDiffusionCoeff(iPoint),
@@ -1597,14 +1601,12 @@ void CNEMOEulerSolver::BC_Far_Field(CGeometry *geometry,
                                         nodes->GetEddyViscosity(iPoint));
 
         /*--- Thermal conductivity ---*/
-        visc_numerics->SetThermalConductivity(
-            nodes->GetThermalConductivity(iPoint),
-            nodes->GetThermalConductivity(iPoint));
+        visc_numerics->SetThermalConductivity(nodes->GetThermalConductivity(iPoint),
+                                              nodes->GetThermalConductivity(iPoint));
 
         /*--- Vib-el. thermal conductivity ---*/
-        visc_numerics->SetThermalConductivity_ve(
-            nodes->GetThermalConductivity_ve(iPoint),
-            nodes->GetThermalConductivity_ve(iPoint));
+        visc_numerics->SetThermalConductivity_ve(nodes->GetThermalConductivity_ve(iPoint),
+                                                 nodes->GetThermalConductivity_ve(iPoint));
 
         /*--- Compute and update residual ---*/
         auto residual = visc_numerics->ComputeResidual(config);
@@ -1616,6 +1618,9 @@ void CNEMOEulerSolver::BC_Far_Field(CGeometry *geometry,
       }
     }
   }
+
+  /*--- Free locally allocated memory ---*/
+  delete [] Normal;
 }
 
 void CNEMOEulerSolver::BC_Inlet(CGeometry *geometry, CSolver **solver_container,
@@ -2143,205 +2148,281 @@ void CNEMOEulerSolver::BC_Outlet(CGeometry *geometry, CSolver **solver_container
 
 }
 
-void CNEMOEulerSolver::BC_Supersonic_Inlet(
-    CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics,
-    CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
-
-  /*--- Supersonic inlet flow: there are no outgoing characteristics,
-   so all flow variables can be imposed at the inlet.
-   First, retrieve the specified values for the primitive variables. ---*/
+void CNEMOEulerSolver::BC_Supersonic_Inlet(CGeometry *geometry, CSolver **solver_container,
+                                           CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
+
+SU2_MPI::Error("BC_SUPERSONIC_INLET: Not operational in NEMO.", CURRENT_FUNCTION);
+
+//  unsigned short iDim, iVar;
+//  unsigned long iVertex, iPoint, Point_Normal;
+//  su2double Density, Pressure, Temperature, Temperature_ve, Energy, *Velocity, Velocity2, soundspeed;
+//  su2double Gas_Constant = config->GetGas_ConstantND();
+//
+//  bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+//  bool dynamic_grid  = config->GetGrid_Movement();
+//  bool viscous              = config->GetViscous();
+//  string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
+//
+//  su2double RuSI  = UNIVERSAL_GAS_CONSTANT;
+//  su2double Ru = 1000.0*RuSI;
+//
+//  su2double *U_inlet = new su2double[nVar];     su2double *U_domain = new su2double[nVar];
+//  su2double *V_inlet = new su2double[nPrimVar]; su2double *V_domain = new su2double[nPrimVar];
+//  su2double *Normal = new su2double[nDim];
+
+/* ----------------------------------------------------------------------------- */
+/* ----------------------------------------------------------------------------- */
+/* The block of code commented below needs to be updated to use Fluidmodel class */
+/* ----------------------------------------------------------------------------- */
+/* ----------------------------------------------------------------------------- */
+
+//  /*--- Supersonic inlet flow: there are no outgoing characteristics,
+//   so all flow variables can be imposed at the inlet.
+//   First, retrieve the specified values for the primitive variables. ---*/
+//  //ASSUME TVE = T for the time being
+//  auto Mass_Frac      = config->GetInlet_MassFrac(Marker_Tag);
+//  Temperature    = config->GetInlet_Temperature(Marker_Tag);
+//  Pressure       = config->GetInlet_Pressure(Marker_Tag);
+//  Velocity       = config->GetInlet_Velocity(Marker_Tag);
+//  Temperature_ve = Temperature;
+//
+//  /*--- Compute Density and Species Densities ---*/
+//  for (iSpecies = 0; iSpecies < nHeavy; iSpecies++)
+//    denom += Mass_Frac[iSpecies] * (Ru/Ms[iSpecies]) * Temperature;
+//  for (iSpecies = 0; iSpecies < nEl; iSpecies++)
+//    denom += Mass_Frac[nSpecies-1] * (Ru/Ms[nSpecies-1]) * Temperature_ve;
+//  Density = Pressure / denom;
+//
+//  /*--- Compute Soundspeed and Velocity squared ---*/
+//  for (iSpecies = 0; iSpecies < nHeavy; iSpecies++) {
+//    conc += Mass_Frac[iSpecies]*Density/Ms[iSpecies];
+//    rhoCvtr += Density*Mass_Frac[iSpecies] * (3.0/2.0 + xi[iSpecies]/2.0) * Ru/Ms[iSpecies];
+//  }
+//  soundspeed = sqrt((1.0 + Ru/rhoCvtr*conc) * Pressure/Density);
+//
+//  Velocity2 = 0.0;
+//  for (iDim = 0; iDim < nDim; iDim++)
+//    Velocity2 += Velocity[iDim]*Velocity[iDim];
+//
+//  /*--- Non-dim. the inputs if necessary. ---*/
+//  // Need to update this portion
+//  //Temperature = Temperature/config->GetTemperature_Ref();
+//  //Pressure    = Pressure/config->GetPressure_Ref();
+//  //Density     = Density/config->GetDensity_Ref();
+//  //for (iDim = 0; iDim < nDim; iDim++)
+//  //  Velocity[iDim] = Velocity[iDim]/config->GetVelocity_Ref();
+//
+//  /*--- Compute energy (RRHO) from supplied primitive quanitites ---*/
+//  for (iSpecies = 0; iSpecies < nHeavy; iSpecies++) {
+//
+//    // Species density
+//    rhos = Mass_Frac[iSpecies]*Density;
+//
+//    // Species formation energy
+//    Ef = hf[iSpecies] - Ru/Ms[iSpecies]*Tref[iSpecies];
+//
+//    // Species vibrational energy
+//    if (thetav[iSpecies] != 0.0)
+//      Ev = Ru/Ms[iSpecies] * thetav[iSpecies] / (exp(thetav[iSpecies]/Temperature_ve)-1.0);
+//    else
+//      Ev = 0.0;
+//
+//    // Species electronic energy
+//    num = 0.0;
+//    denom = g[iSpecies][0] * exp(thetae[iSpecies][0]/Temperature_ve);
+//    for (iEl = 1; iEl < nElStates[iSpecies]; iEl++) {
+//      num   += g[iSpecies][iEl] * thetae[iSpecies][iEl] * exp(-thetae[iSpecies][iEl]/Temperature_ve);
+//      denom += g[iSpecies][iEl] * exp(-thetae[iSpecies][iEl]/Temperature_ve);
+//    }
+//    Ee = Ru/Ms[iSpecies] * (num/denom);
+//
+//    // Mixture total energy
+//    rhoE += rhos * ((3.0/2.0+xi[iSpecies]/2.0) * Ru/Ms[iSpecies] * (Temperature-Tref[iSpecies])
+//                    + Ev + Ee + Ef + 0.5*Velocity2);
+//
+//    // Mixture vibrational-electronic energy
+//    rhoEve += rhos * (Ev + Ee);
+//  }
+//
+//  /*--- Setting Conservative Variables ---*/
+//  for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+//    U_inlet[iSpecies] = Mass_Frac[iSpecies]*Density;
+//  for (iDim = 0; iDim < nDim; iDim++)
+//    U_inlet[nSpecies+iDim] = Density*Velocity[iDim];
+//  U_inlet[nVar-2] = rhoE;
+//  U_inlet[nVar-1] = rhoEve;
+//
+//  /*--- Setting Primitive Vaariables ---*/
+//  for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+//    V_inlet[iSpecies] = Mass_Frac[iSpecies]*Density;
+//  V_inlet[nSpecies] = Temperature;
+//  V_inlet[nSpecies+1] = Temperature_ve;
+//  for (iDim = 0; iDim < nDim; iDim++)
+//    V_inlet[nSpecies+2+iDim] = Velocity[iDim];
+//  V_inlet[nSpecies+2+nDim] = Pressure;
+//  V_inlet[nSpecies+3+nDim] = Density;
+//  V_inlet[nSpecies+4+nDim] = rhoE+Pressure/Density;
+//  V_inlet[nSpecies+5+nDim] = soundspeed;
+//  V_inlet[nSpecies+6+nDim] = rhoCvtr;
+
+/* ----------------------------------------------------------------------------- */
+/* ----------------------------------------------------------------------------- */
+/* The block of code that needs to be updated to use Fluidmodel class end here   */
+/* ----------------------------------------------------------------------------- */
+/* ----------------------------------------------------------------------------- */
+
+//  //This requires Newtown Raphson.....So this is not currently operational (See Deathstar)
+//  //V_inlet[nSpecies+7+nDim] = rhoCvve;
+//
+//  /*--- Loop over all the vertices on this boundary marker ---*/
+//  for(iVertex = 0; iVertex < geometry->nVertex[val_marker]; iVertex++) {
+//    iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
+//
+//    /*--- Check if the node belongs to the domain (i.e, not a halo node) ---*/
+//    if (geometry->nodes->GetDomain(iPoint)) {
+//
+//      /*--- Index of the closest interior node ---*/
+//      Point_Normal = geometry->vertex[val_marker][iVertex]->GetNormal_Neighbor();
+//
+//      /*--- Current solution at this boundary node ---*/
+//      for (iVar = 0; iVar < nVar; iVar++) U_domain[iVar] = nodes->GetSolution(iPoint,iVar);
+//      for (iVar = 0; iVar < nPrimVar; iVar++) V_domain[iVar] = nodes->GetPrimitive(iPoint,iVar);
+//
+//      /*--- Normal vector for this vertex (negate for outward convention) ---*/
+//      geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
+//      for (iDim = 0; iDim < nDim; iDim++) Normal[iDim] = -Normal[iDim];
+//
+//      su2double Area = 0.0;
+//      for (iDim = 0; iDim < nDim; iDim++)
+//        Area += Normal[iDim]*Normal[iDim];
+//      Area = sqrt (Area);
+//
+//      /*--- Set various quantities in the solver class ---*/
+//      conv_numerics->SetNormal(Normal);
+//      conv_numerics->SetConservative(U_domain, U_inlet);
+//      conv_numerics->SetPrimitive(V_domain, V_inlet);
+//
+//      /*--- Pass supplementary info to CNumerics ---*/
+//      conv_numerics->SetdPdU(nodes->GetdPdU(iPoint), node_infty->GetdPdU(0));
+//      conv_numerics->SetdTdU(nodes->GetdTdU(iPoint), node_infty->GetdTdU(0));
+//      conv_numerics->SetdTvedU(nodes->GetdTvedU(iPoint), node_infty->GetdTvedU(0));
+//      conv_numerics->SetEve(nodes->GetEve(iPoint), node_infty->GetEve(0));
+//      conv_numerics->SetCvve(nodes->GetCvve(iPoint), node_infty->GetCvve(0));
+//
+//      if (dynamic_grid)
+//        conv_numerics->SetGridVel(geometry->nodes->GetGridVel(iPoint),
+//                                  geometry->nodes->GetGridVel(iPoint));
+//
+//      /*--- Compute the residual using an upwind scheme ---*/
+//      auto residual = conv_numerics->ComputeResidual(config);
+//      LinSysRes.AddBlock(iPoint, residual);
+//
+//      /*--- Jacobian contribution for implicit integration ---*/
+//      //if (implicit)
+//      //  Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
+//
+//      /*--- Viscous contribution ---*/
+//      if (viscous) {
+//
+//        /*--- Set the normal vector and the coordinates ---*/
+//        visc_numerics->SetNormal(Normal);
+//        su2double Coord_Reflected[MAXNDIM];
+//        GeometryToolbox::PointPointReflect(nDim, geometry->nodes->GetCoord(Point_Normal),
+//                                           geometry->nodes->GetCoord(iPoint), Coord_Reflected);
+//        visc_numerics->SetCoord(geometry->nodes->GetCoord(iPoint), Coord_Reflected);
+//
+//        /*--- Primitive variables, and gradient ---*/
+//        visc_numerics->SetPrimitive(V_domain, V_inlet);
+//        visc_numerics->SetPrimVarGradient(nodes->GetGradient_Primitive(iPoint), nodes->GetGradient_Primitive(iPoint));
+//
+//        /*--- Laminar viscosity ---*/
+//        visc_numerics->SetLaminarViscosity(nodes->GetLaminarViscosity(iPoint), nodes->GetLaminarViscosity(iPoint));
+//
+//        /*--- Compute and update residual ---*/
+//        auto residual = visc_numerics->ComputeResidual(config);
+//        LinSysRes.SubtractBlock(iPoint, residual);
+//
+//        /*--- Jacobian contribution for implicit integration ---*/
+//        //if (implicit)
+//        //  Jacobian.SubtractBlock2Diag(iPoint, residual.Jacobian_i);
+//      }
+//
+//    }
+//  }
+//
+//  /*--- Free locally allocated memory ---*/
+//  delete [] U_domain;
+//  delete [] U_inlet;
+//  delete [] V_domain;
+//  delete [] V_inlet;
+//  delete [] Normal;
 
-  const string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
+}
 
-  const su2double Temperature = config->GetInlet_Temperature(Marker_Tag);
-  const su2double Pressure = config->GetInlet_Pressure(Marker_Tag);
-  const su2double *Velocity = config->GetInlet_Velocity(Marker_Tag);
-  const su2double *Mass_Frac = config->GetInlet_MassFrac();
-  su2double Temperature_ve = config->GetInlet_Temperature_ve();
+void CNEMOEulerSolver::BC_Supersonic_Outlet(CGeometry *geometry, CSolver **solver_container,
+                                            CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
+  unsigned short iDim;
+  unsigned long iVertex, iPoint;
+  su2double *V_outlet, *V_domain;
+  su2double *U_outlet, *U_domain;
 
-  /*--- If no Tve value specified (left as 0 K default), set to Ttr value ---*/
-  if (Temperature_ve == 0.0) {
-    Temperature_ve = Temperature;
-  }
+  bool implicit     = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+  string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
 
-  /*--- Set mixture state ---*/
-  FluidModel->SetTDStatePTTv(Pressure, Mass_Frac, Temperature, Temperature_ve);
+  su2double *Normal = new su2double[nDim];
 
-  /*--- Compute Ma vector for flow direction ---*/
-  const su2double soundspeed = FluidModel->ComputeSoundSpeed();
+  /*--- Supersonic outlet flow: there are no ingoing characteristics,
+   so all flow variables can should be interpolated from the domain. ---*/
 
-  su2double Mvec[MAXNDIM] = {0.0};
+  /*--- Loop over all the vertices on this boundary marker ---*/
+  for (iVertex = 0; iVertex < geometry->nVertex[val_marker]; iVertex++) {
 
-  for (unsigned short iDim = 0; iDim < nDim; iDim++)
-    Mvec[iDim] = Velocity[iDim] / soundspeed;
+    iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
-  /*--- Allocate inlet node to compute gradients for numerics ---*/
-  CNEMOEulerVariable node_inlet(Pressure, Mass_Frac, Mvec, Temperature,
-                                Temperature_ve, 1, nDim, nVar, nPrimVar,
-                                nPrimVarGrad, config, FluidModel);
-  node_inlet.SetPrimVar(0, FluidModel);
+    /*--- Check if the node belongs to the domain (i.e, not a halo node) ---*/
+    if (geometry->nodes->GetDomain(iPoint)) {
 
-  su2double Normal[MAXNDIM] = {0.0};
+      /*--- Current solution at this boundary node ---*/
+      V_domain = nodes->GetPrimitive(iPoint);
+      U_domain = nodes->GetSolution(iPoint);
 
-  /*--- Loop over all the vertices on this boundary marker ---*/
-  for (unsigned long iVertex = 0; iVertex < geometry->nVertex[val_marker];
-       iVertex++) {
-    const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
+      /*--- Allocate the value at the outlet ---*/
+      V_outlet = GetCharacPrimVar(val_marker, iVertex);
+      V_outlet = V_domain;
+      U_outlet = U_domain;
 
-    /*--- Check if the node belongs to the domain (i.e, not a halo node) ---*/
-    if (!geometry->nodes->GetDomain(iPoint))
-      continue;
-
-    /*--- Index of the closest interior node ---*/
-    const auto Point_Normal =
-        geometry->vertex[val_marker][iVertex]->GetNormal_Neighbor();
-
-    /*--- Normal vector for this vertex (negate for outward convention) ---*/
-    geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
-    for (unsigned short iDim = 0; iDim < nDim; iDim++)
-      Normal[iDim] = -Normal[iDim];
-
-    /*--- Set various quantities in the solver class ---*/
-    conv_numerics->SetNormal(Normal);
-    conv_numerics->SetConservative(nodes->GetSolution(iPoint),
-                                   node_inlet.GetSolution(0));
-    conv_numerics->SetPrimitive(nodes->GetPrimitive(iPoint),
-                                node_inlet.GetPrimitive(0));
-
-    /*--- Pass supplementary info to CNumerics ---*/
-    conv_numerics->SetdPdU(nodes->GetdPdU(iPoint), node_inlet.GetdPdU(0));
-    conv_numerics->SetdTdU(nodes->GetdTdU(iPoint), node_inlet.GetdTdU(0));
-    conv_numerics->SetdTvedU(nodes->GetdTvedU(iPoint), node_inlet.GetdTvedU(0));
-    conv_numerics->SetEve(nodes->GetEve(iPoint), node_inlet.GetEve(0));
-    conv_numerics->SetCvve(nodes->GetCvve(iPoint), node_inlet.GetCvve(0));
-
-    const bool dynamic_grid = config->GetGrid_Movement();
-    if (dynamic_grid)
-      conv_numerics->SetGridVel(geometry->nodes->GetGridVel(iPoint),
-                                geometry->nodes->GetGridVel(iPoint));
-
-    /*--- Compute the residual using an upwind scheme ---*/
-    auto residual = conv_numerics->ComputeResidual(config);
-    LinSysRes.AddBlock(iPoint, residual);
-
-    /*--- Jacobian contribution for implicit integration ---*/
-    const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
-    if (implicit)
-      Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
-
-    /*--- Viscous contribution ---*/
-    bool viscous = config->GetViscous();
-    if (viscous) {
+      /*--- Normal vector for this vertex (negate for outward convention) ---*/
+      geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
+      for (iDim = 0; iDim < nDim; iDim++) Normal[iDim] = -Normal[iDim];
 
-      /*--- Set the normal vector and the coordinates ---*/
-      su2double Coord_Reflected[MAXNDIM];
-      GeometryToolbox::PointPointReflect(
-          nDim, geometry->nodes->GetCoord(Point_Normal),
-          geometry->nodes->GetCoord(iPoint), Coord_Reflected);
-      visc_numerics->SetCoord(geometry->nodes->GetCoord(iPoint),
-                              Coord_Reflected);
-      visc_numerics->SetNormal(Normal);
-
-      /*--- Primitive variables, and gradient ---*/
-      visc_numerics->SetConservative(nodes->GetSolution(iPoint),
-                                     node_inlet.GetSolution(0));
-      visc_numerics->SetPrimitive(nodes->GetPrimitive(iPoint),
-                                  node_inlet.GetPrimitive(0));
-      visc_numerics->SetPrimVarGradient(nodes->GetGradient_Primitive(iPoint),
-                                        node_inlet.GetGradient_Primitive(0));
+      /*--- Set various quantities in the solver class ---*/
+      conv_numerics->SetNormal(Normal);
+      conv_numerics->SetPrimitive(V_domain, V_outlet);
+      conv_numerics->SetConservative(U_domain, U_outlet);
 
       /*--- Pass supplementary information to CNumerics ---*/
-      visc_numerics->SetdPdU(nodes->GetdPdU(iPoint), node_inlet.GetdPdU(0));
-      visc_numerics->SetdTdU(nodes->GetdTdU(iPoint), node_inlet.GetdTdU(0));
-      visc_numerics->SetdTvedU(nodes->GetdTvedU(iPoint),
-                               node_inlet.GetdTvedU(0));
-      visc_numerics->SetEve(nodes->GetEve(iPoint), node_inlet.GetEve(0));
-      visc_numerics->SetCvve(nodes->GetCvve(iPoint), node_inlet.GetCvve(0));
-
-      /*--- Species diffusion coefficients ---*/
-      visc_numerics->SetDiffusionCoeff(nodes->GetDiffusionCoeff(iPoint),
-                                       nodes->GetDiffusionCoeff(iPoint));
-      /*--- Laminar viscosity ---*/
-      visc_numerics->SetLaminarViscosity(nodes->GetLaminarViscosity(iPoint),
-                                         nodes->GetLaminarViscosity(iPoint));
-      /*--- Eddy viscosity ---*/
-      visc_numerics->SetEddyViscosity(nodes->GetEddyViscosity(iPoint),
-                                      nodes->GetEddyViscosity(iPoint));
-      /*--- Thermal conductivity ---*/
-      visc_numerics->SetThermalConductivity(
-          nodes->GetThermalConductivity(iPoint),
-          nodes->GetThermalConductivity(iPoint));
-      /*--- Vib-el. thermal conductivity ---*/
-      visc_numerics->SetThermalConductivity_ve(
-          nodes->GetThermalConductivity_ve(iPoint),
-          nodes->GetThermalConductivity_ve(iPoint));
-
-      /*--- Compute and update residual ---*/
-      auto residual = visc_numerics->ComputeResidual(config);
-      LinSysRes.SubtractBlock(iPoint, residual);
+      conv_numerics->SetdPdU  (nodes->GetdPdU(iPoint),   nodes->GetdPdU(iPoint));
+      conv_numerics->SetdTdU  (nodes->GetdTdU(iPoint),   nodes->GetdTdU(iPoint));
+      conv_numerics->SetdTvedU(nodes->GetdTvedU(iPoint), nodes->GetdTvedU(iPoint));
+      conv_numerics->SetEve   (nodes->GetEve(iPoint),    nodes->GetEve(iPoint));
+      conv_numerics->SetCvve  (nodes->GetCvve(iPoint),   nodes->GetCvve(iPoint));
+      conv_numerics->SetGamma (nodes->GetGamma(iPoint),  nodes->GetGamma(iPoint));
+
+      if (dynamic_grid)
+        conv_numerics->SetGridVel(geometry->nodes->GetGridVel(iPoint),
+                                  geometry->nodes->GetGridVel(iPoint));
+
+      /*--- Compute the residual using an upwind scheme ---*/
+      auto residual = conv_numerics->ComputeResidual(config);
+      LinSysRes.AddBlock(iPoint, residual);
 
       /*--- Jacobian contribution for implicit integration ---*/
       if (implicit)
-        Jacobian.SubtractBlock2Diag(iPoint, residual.jacobian_i);
+        Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
     }
   }
-}
-
-void CNEMOEulerSolver::BC_Supersonic_Outlet(
-    CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics,
-    CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
-
-  /*--- Supersonic outlet flow: there are no ingoing characteristics,
-   so all flow variables can should be interpolated from the domain. ---*/
 
-  su2double Normal[MAXNDIM] = {0.0};
-
-  const string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
-
-  /*--- Loop over all the vertices on this boundary marker ---*/
-  for (unsigned long iVertex = 0; iVertex < geometry->nVertex[val_marker];
-       iVertex++) {
-
-    const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
-
-    /*--- Check if the node belongs to the domain (i.e, not a halo node) ---*/
-    if (!geometry->nodes->GetDomain(iPoint))
-      continue;
-
-    /*--- Normal vector for this vertex (negate for outward convention) ---*/
-    geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
-    for (unsigned short iDim = 0; iDim < nDim; iDim++)
-      Normal[iDim] = -Normal[iDim];
-
-    /*--- Set various quantities in the solver class, outlet properties are
-     * equal to domain properties ---*/
-    conv_numerics->SetNormal(Normal);
-    conv_numerics->SetPrimitive(nodes->GetPrimitive(iPoint),
-                                nodes->GetPrimitive(iPoint));
-    conv_numerics->SetConservative(nodes->GetSolution(iPoint),
-                                   nodes->GetSolution(iPoint));
+  /*--- Free locally allocated memory ---*/
+  delete [] Normal;
 
-    /*--- Pass supplementary information to CNumerics ---*/
-    conv_numerics->SetdPdU(nodes->GetdPdU(iPoint), nodes->GetdPdU(iPoint));
-    conv_numerics->SetdTdU(nodes->GetdTdU(iPoint), nodes->GetdTdU(iPoint));
-    conv_numerics->SetdTvedU(nodes->GetdTvedU(iPoint),
-                             nodes->GetdTvedU(iPoint));
-    conv_numerics->SetEve(nodes->GetEve(iPoint), nodes->GetEve(iPoint));
-    conv_numerics->SetCvve(nodes->GetCvve(iPoint), nodes->GetCvve(iPoint));
-    conv_numerics->SetGamma(nodes->GetGamma(iPoint), nodes->GetGamma(iPoint));
-
-    const bool dynamic_grid = config->GetGrid_Movement();
-    if (dynamic_grid)
-      conv_numerics->SetGridVel(geometry->nodes->GetGridVel(iPoint),
-                                geometry->nodes->GetGridVel(iPoint));
-
-    /*--- Compute the residual using an upwind scheme ---*/
-    auto residual = conv_numerics->ComputeResidual(config);
-    LinSysRes.AddBlock(iPoint, residual);
-
-    /*--- Jacobian contribution for implicit integration ---*/
-    const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
-    if (implicit)
-      Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
-  }
 }
diff --git a/SU2_CFD/src/variables/CEulerVariable.cpp b/SU2_CFD/src/variables/CEulerVariable.cpp
index da046f7793a..b92de7f1f96 100644
--- a/SU2_CFD/src/variables/CEulerVariable.cpp
+++ b/SU2_CFD/src/variables/CEulerVariable.cpp
@@ -78,12 +78,6 @@ CEulerVariable::CEulerVariable(su2double density, const su2double *velocity, su2
     nIter_Newtonsolver.resize(nPoint) = 0;
     FluidEntropy.resize(nPoint) = su2double(0.0);
   }
-  
-  if (config->GetVorticityConfinement()) {
-    nAuxVar = 1;
-    Grad_AuxVar.resize(nPoint, nAuxVar, nDim, 0.0);
-    AuxVar.resize(nPoint, nAuxVar) = su2double(0.0);
-  }
 }
 
 bool CEulerVariable::SetPrimVar(unsigned long iPoint, CFluidModel *FluidModel) {
diff --git a/SU2_CFD/src/variables/CHeatVariable.cpp b/SU2_CFD/src/variables/CHeatVariable.cpp
index c5f2c58f128..a70053d4683 100644
--- a/SU2_CFD/src/variables/CHeatVariable.cpp
+++ b/SU2_CFD/src/variables/CHeatVariable.cpp
@@ -25,13 +25,16 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
+
 #include "../../include/variables/CHeatVariable.hpp"
 
+
 CHeatVariable::CHeatVariable(su2double heat, unsigned long npoint, unsigned long ndim, unsigned long nvar, CConfig *config)
-  : CScalarVariable(npoint, ndim, nvar, config) {
+  : CVariable(npoint, ndim, nvar, config), Gradient_Reconstruction(config->GetReconstructionGradientRequired() ? Gradient_Aux : Gradient) {
 
-  const bool dual_time = ((config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
-                          (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND));
+  bool low_fidelity = false;
+  bool dual_time = ((config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
+                    (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND));
 
   /*--- Initialization of heat variable ---*/
 
@@ -40,14 +43,14 @@ CHeatVariable::CHeatVariable(su2double heat, unsigned long npoint, unsigned long
 
   /*--- Allocate residual structures ---*/
 
-  Res_TruncError.resize(nPoint, nVar) = su2double(0.0);
+  Res_TruncError.resize(nPoint,nVar) = su2double(0.0);
 
   /*--- Only for residual smoothing (multigrid) ---*/
 
   for (unsigned long iMesh = 0; iMesh <= config->GetnMGLevels(); iMesh++) {
-    if (config->GetMG_CorrecSmooth(iMesh) > 0) {
-      Residual_Sum.resize(nPoint, nVar);
-      Residual_Old.resize(nPoint, nVar);
+    if ((config->GetMG_CorrecSmooth(iMesh) > 0) || low_fidelity) {
+      Residual_Sum.resize(nPoint,nVar);
+      Residual_Old.resize(nPoint,nVar);
       break;
     }
   }
@@ -58,7 +61,27 @@ CHeatVariable::CHeatVariable(su2double heat, unsigned long npoint, unsigned long
     Solution_time_n1 = heat;
   }
 
+  /*--- Gradient related fields ---*/
+  Gradient.resize(nPoint,nVar,nDim,0.0);
+
+  if (config->GetReconstructionGradientRequired()) {
+    Gradient_Aux.resize(nPoint,nVar,nDim,0.0);
+  }
+
+  if (config->GetLeastSquaresRequired()) {
+    Rmatrix.resize(nPoint,nDim,nDim,0.0);
+  }
+
+  if (config->GetKind_ConvNumScheme_Heat() == SPACE_CENTERED)
+    Undivided_Laplacian.resize(nPoint,nVar);
+
+  Max_Lambda_Inv.resize(nPoint);
   Max_Lambda_Visc.resize(nPoint);
+  Delta_Time.resize(nPoint);
+
+  /* Under-relaxation parameter. */
+  UnderRelaxation.resize(nPoint) = su2double(1.0);
+  LocalCFL.resize(nPoint) = su2double(0.0);
 
   if (config->GetMultizone_Problem())
     Set_BGSSolution_k();

From 27c62c5891ed2fdea6ba73cc2c7e013bf54eb4dc Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 3 Feb 2023 17:41:12 +0100
Subject: [PATCH 171/656] Updated test case configuration files

---
 .../disc_adj_unsteadyCHT_cylinder/solid.cfg   |  1 +
 TestCases/disc_adj_heat/disc_adj_heat.cfg     |  4 +-
 TestCases/hybrid_regression.py                | 10 +-
 .../chtPinArray_2d/of_grad_findiff.csv.ref    |  2 +-
 .../chtPinArray_3d/configSolid.cfg            |  1 +
 TestCases/nicf/coolprop/fluidModel.cfg        |  2 +-
 TestCases/nicf/coolprop/transportModel.cfg    |  2 +-
 TestCases/parallel_regression.py              | 95 +++----------------
 TestCases/parallel_regression_AD.py           | 60 ++++++------
 TestCases/serial_regression.py                |  2 +-
 TestCases/serial_regression_AD.py             | 38 ++++----
 TestCases/tutorials.py                        | 20 ----
 12 files changed, 73 insertions(+), 164 deletions(-)

diff --git a/TestCases/coupled_cht/disc_adj_unsteadyCHT_cylinder/solid.cfg b/TestCases/coupled_cht/disc_adj_unsteadyCHT_cylinder/solid.cfg
index c3d950ae259..3fb2d6bafd2 100644
--- a/TestCases/coupled_cht/disc_adj_unsteadyCHT_cylinder/solid.cfg
+++ b/TestCases/coupled_cht/disc_adj_unsteadyCHT_cylinder/solid.cfg
@@ -42,6 +42,7 @@ CONV_STARTITER= 10000
 
 % -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
 %
+CONV_NUM_METHOD_HEAT = SPACE_CENTERED
 TIME_DISCRE_HEAT= EULER_IMPLICIT
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
diff --git a/TestCases/disc_adj_heat/disc_adj_heat.cfg b/TestCases/disc_adj_heat/disc_adj_heat.cfg
index 26a502096de..78df9c1bd58 100644
--- a/TestCases/disc_adj_heat/disc_adj_heat.cfg
+++ b/TestCases/disc_adj_heat/disc_adj_heat.cfg
@@ -126,10 +126,12 @@ CFL_REDUCTION_TURB= 1.0
 
 % -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
 
-CONV_NUM_METHOD_HEAT = SCALAR_UPWIND
+CONV_NUM_METHOD_HEAT = SPACE_CENTERED
 
 MUSCL_HEAT= YES
 
+JST_SENSOR_COEFF_HEAT= ( 0.5, 0.15 )
+
 TIME_DISCRE_HEAT= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index 26d829c717c..2127f2371dd 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -248,7 +248,7 @@ def main():
     #######################################
     ### Axisymmetric Compressible RANS  ###
     #######################################
-
+    
     # Axisymmetric air nozzle (transonic)
     axi_rans_air_nozzle_restart           = TestCase('axi_rans_air_nozzle_restart')
     axi_rans_air_nozzle_restart.cfg_dir   = "axisymmetric_rans/air_nozzle"
@@ -427,14 +427,6 @@ def main():
     inc_turb_naca0012_sst_sust.test_vals = [-7.274028, 0.145888, 0.000002, 0.312014]
     test_list.append(inc_turb_naca0012_sst_sust)
 
-    # Weakly coupled heat equation
-    inc_weakly_coupled = TestCase('inc_weakly_coupled')
-    inc_weakly_coupled.cfg_dir = "disc_adj_heat"
-    inc_weakly_coupled.cfg_file = "primal.cfg"
-    inc_weakly_coupled.test_iter = 10
-    inc_weakly_coupled.test_vals = [-17.240436, -16.184455, -16.069131, -17.230730, -18.350601, -13.768070, 5.545700]
-    test_list.append(inc_weakly_coupled)
-
     ######################################
     ### Moving Wall                    ###
     ######################################
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/of_grad_findiff.csv.ref b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/of_grad_findiff.csv.ref
index 82730a5fe1e..51f3fad3680 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/of_grad_findiff.csv.ref
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/of_grad_findiff.csv.ref
@@ -1,2 +1,2 @@
 "VARIABLE"      , "AVG_DENSITY[0]", "AVG_ENTHALPY[0]", "AVG_NORMALVEL[0]", "DRAG[0]"       , "EFFICIENCY[0]" , "FORCE_X[0]"    , "FORCE_Y[0]"    , "FORCE_Z[0]"    , "LIFT[0]"       , "MOMENT_X[0]"   , "MOMENT_Y[0]"   , "MOMENT_Z[0]"   , "SIDEFORCE[0]"  , "SURFACE_MACH[0]", "SURFACE_MASSFLOW[0]", "SURFACE_MOM_DISTORTION[0]", "SURFACE_PRESSURE_DROP[0]", "SURFACE_SECONDARY[0]", "SURFACE_SECOND_OVER_UNIFORM[0]", "SURFACE_STATIC_PRESSURE[0]", "SURFACE_STATIC_TEMPERATURE[0]", "SURFACE_TOTAL_PRESSURE[0]", "SURFACE_TOTAL_TEMPERATURE[0]", "SURFACE_UNIFORMITY[0]", "AVG_TEMPERATURE[1]", "MAXIMUM_HEATFLUX[1]", "TOTAL_HEATFLUX[1]", "FINDIFF_STEP"  
-0               , 0.0             , -100000.01639127731, -1.1103000000496327e-08, 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , -0.0399999991462785, 3.3309999998872306e-08, -2.1099999997220564      , 0.0                     , 2.1799999999627673  , 3.8000000007754053            , 319.9999980552093         , -39.999997625272954          , 318.0000007318995        , -39.999997625272954         , -1.400000004814217   , -139.99999737279722, 0.0                , -540.0000077315781, 1e-08           
+0               , 0.0             , -100000.01639127731, -1.1101999999881826e-08, 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , -0.0399999991462785, 0.0                , -2.1099999997220564      , 0.0                     , 2.1799999999627673  , 3.8000000007754053            , 319.9999980552093         , -39.999997625272954          , 318.0000007318995        , -39.999997625272954         , -1.400000004814217   , -139.99999737279722, 0.0                , -540.0000077315781, 1e-08           
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configSolid.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configSolid.cfg
index 5f7f7a90b3d..6961daef9fc 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configSolid.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configSolid.cfg
@@ -64,6 +64,7 @@ CONV_STARTITER= 100
 %
 % -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
 %
+CONV_NUM_METHOD_HEAT = SPACE_CENTERED
 TIME_DISCRE_HEAT= EULER_IMPLICIT
 %
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
diff --git a/TestCases/nicf/coolprop/fluidModel.cfg b/TestCases/nicf/coolprop/fluidModel.cfg
index 44df7a39118..6b2fb858bc6 100644
--- a/TestCases/nicf/coolprop/fluidModel.cfg
+++ b/TestCases/nicf/coolprop/fluidModel.cfg
@@ -6,7 +6,7 @@
 % Author: Peng Yan, Alberto Guardone                                           %
 % Institution: Politecnico di Milano                                           %
 % Date: 2022.10.8                                                              %
-% File Version  7.5.0 Blackbird                                                %
+% File Version  7.4.0 Blackbird                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nicf/coolprop/transportModel.cfg b/TestCases/nicf/coolprop/transportModel.cfg
index 491073a2734..b4b1d9c4906 100644
--- a/TestCases/nicf/coolprop/transportModel.cfg
+++ b/TestCases/nicf/coolprop/transportModel.cfg
@@ -6,7 +6,7 @@
 % Author: Peng Yan, Alberto Guardone                                           %
 % Institution: Politecnico di Milano                                           %
 % Date: 2022.11.26                                                             %
-% File Version  7.5.0 Blackbird                                                %
+% File Version  7.4.0 Blackbird                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 933ba5f14a4..e1d8c358fb6 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -70,65 +70,15 @@ def main():
     thermalbath_frozen.new_output = True
     test_list.append(thermalbath_frozen)
 
-    # Inviscid single wedge, ausm, implicit
-    invwedge_a = TestCase('invwedge_ausm')
-    invwedge_a.cfg_dir = "nonequilibrium/invwedge"
-    invwedge_a.cfg_file = "invwedge_ausm.cfg"
-    invwedge_a.test_iter = 10
-    invwedge_a.test_vals = [-1.042842, -1.567605, -18.300680, -18.628055, -18.574084, 2.275192, 1.879772, 5.319421, 0.873699]
-    invwedge_a.test_vals_aarch64 = [-1.042842, -1.567605, -18.300025, -18.627409, -18.573428, 2.275192, 1.879772, 5.319421, 0.873699]
-    invwedge_a.new_output = True
-    test_list.append(invwedge_a)
-
-    # Inviscid single wedge, ausm+-up2, implicit
-    invwedge_ap2 = TestCase('invwedge_ap2')
-    invwedge_ap2.cfg_dir = "nonequilibrium/invwedge"
-    invwedge_ap2.cfg_file = "invwedge_ausmplusup2.cfg"
-    invwedge_ap2.test_iter = 10
-    invwedge_ap2.test_vals = [-0.952589, -1.477352, -16.736014, -17.064021, -17.009120, 2.387086, 1.287286, 5.403046, 0.956402]
-    invwedge_ap2.test_vals_aarch64 = [-0.952589, -1.477352, -16.736014, -17.064021, -17.009120, 2.387086, 1.287286, 5.403046, 0.956402]
-    invwedge_ap2.new_output = True
-    test_list.append(invwedge_ap2)
-    
-    # Inviscid single wedge, msw, implicit
-    invwedge_msw = TestCase('invwedge_msw')
-    invwedge_msw.cfg_dir = "nonequilibrium/invwedge"
-    invwedge_msw.cfg_file = "invwedge_msw.cfg"
-    invwedge_msw.test_iter = 10
-    invwedge_msw.test_vals = [-1.165957, -1.690720, -18.298756, -18.626164, -18.572159, 2.151638, 1.721236, 5.193813, 0.751584]
-    invwedge_msw.test_vals_aarch64 = [-1.165957, -1.690720, -18.298756, -18.626164, -18.572159, 2.151638, 1.721236, 5.193813, 0.751584]
-    invwedge_msw.new_output = True
-    test_list.append(invwedge_msw)
-    
-    # Inviscid single wedge, roe, implicit
-    invwedge_roe = TestCase('invwedge_roe')
-    invwedge_roe.cfg_dir = "nonequilibrium/invwedge"
-    invwedge_roe.cfg_file = "invwedge_roe.cfg"
-    invwedge_roe.test_iter = 10
-    invwedge_roe.test_vals = [-1.038582, -1.563344, -18.300307, -18.627706, -18.573706, 2.278987, 1.861307, 5.323753, 0.874900]
-    invwedge_roe.test_vals_aarch64 = [-1.038582, -1.563344, -18.300307, -18.627706, -18.573706, 2.278987, 1.861307, 5.323753, 0.874900]
-    invwedge_roe.new_output = True
-    test_list.append(invwedge_roe)
-    
-    # Inviscid single wedge, lax, implicit
-    invwedge_lax = TestCase('invwedge_lax')
-    invwedge_lax.cfg_dir = "nonequilibrium/invwedge"
-    invwedge_lax.cfg_file = "invwedge_lax.cfg"
-    invwedge_lax.test_iter = 10
-    invwedge_lax.test_vals = [-1.075662, -1.600425, -32.000000, -32.000000, -24.972431, 2.252952, 1.725158, 5.282140, 0.848823]
-    invwedge_lax.test_vals_aarch64 = [-1.075662, -1.600425, -32.000000, -32.000000, -24.972431, 2.252952, 1.725158, 5.282140, 0.848823]
-    invwedge_lax.new_output = True
-    test_list.append(invwedge_lax)
-
-    # Inviscid single wedge, implicit, NEMO supersonic inlet
-    invwedge_ss_inlet = TestCase('invwedge_ss_inlet')
-    invwedge_ss_inlet.cfg_dir = "nonequilibrium/invwedge"
-    invwedge_ss_inlet.cfg_file = "invwedge_ss_inlet.cfg"
-    invwedge_ss_inlet.test_iter = 10
-    invwedge_ss_inlet.test_vals = [-1.042718, -1.567481, -18.250175, -18.579516, -18.523248, 2.275305, 1.880068, 5.319548, 0.873821]
-    invwedge_ss_inlet.test_vals_aarch64 = [-1.042718, -1.567481, -18.250175, -18.579516, -18.523248, 2.275305, 1.880068, 5.319548, 0.873821]
-    invwedge_ss_inlet.new_output = True
-    test_list.append(invwedge_ss_inlet)
+    # Inviscid single wedge, implicit
+    invwedge           = TestCase('invwedge')
+    invwedge.cfg_dir   = "nonequilibrium/invwedge"
+    invwedge.cfg_file  = "invwedge.cfg"
+    invwedge.test_iter = 10
+    invwedge.test_vals         = [-1.042842, -1.567605, -18.300680, -18.628055, -18.574084, 2.275192, 1.879772, 5.319421, 0.873699]
+    invwedge.test_vals_aarch64 = [-1.042842, -1.567605, -18.300025, -18.627409, -18.573428, 2.275192, 1.879772, 5.319421, 0.873699]
+    invwedge.new_output = True
+    test_list.append(invwedge)
 
     # Viscous single cone - axisymmetric
     visc_cone           = TestCase('visc_cone')
@@ -352,15 +302,6 @@ def main():
     turb_oneram6.timeout   = 3200
     test_list.append(turb_oneram6)
 
-    # ONERA M6 Wing - vorticity confinement
-    turb_oneram6_vc = TestCase('turb_oneram6_vc')
-    turb_oneram6_vc.cfg_dir = "rans/oneram6"
-    turb_oneram6_vc.cfg_file = "turb_ONERAM6_vc.cfg"
-    turb_oneram6_vc.test_iter = 15
-    turb_oneram6_vc.test_vals = [-2.262387, -6.626467, 0.228393, 0.140799, -2.7107e+04]
-    turb_oneram6_vc.timeout = 3200
-    test_list.append(turb_oneram6_vc)
-
     # ONERA M6 Wing - Newton-Krylov
     turb_oneram6_nk           = TestCase('turb_oneram6_nk')
     turb_oneram6_nk.cfg_dir   = "rans/oneram6"
@@ -989,14 +930,6 @@ def main():
     coolprop_transportModel.test_vals = [-4.527922, -1.308741, 4.630469, 0.000000, 0.000000]
     test_list.append(coolprop_transportModel)
 
-    # Subsonic Q1D nozzle using an MLP for thermodynamic state evaluation
-    datadriven_MLP           = TestCase('datadriven_MLP')
-    datadriven_MLP.cfg_dir   = "nicf/datadriven"
-    datadriven_MLP.cfg_file  = "datadriven_nozzle.cfg"
-    datadriven_MLP.test_iter = 100
-    datadriven_MLP.test_vals = [-4.159241, 0.073280, 3.627716, 0.000000, 0.000000]
-    test_list.append(datadriven_MLP)
-
     ######################################
     ### Turbomachinery                 ###
     ######################################
@@ -1213,7 +1146,7 @@ def main():
     solid_periodic_pins.cfg_dir   = "solid_heat_conduction/periodic_pins"
     solid_periodic_pins.cfg_file  = "configSolid.cfg"
     solid_periodic_pins.test_iter = 750
-    solid_periodic_pins.test_vals = [-15.878977, -14.569206, 300.900000, 425.320000, 0.000000, 5.000000, -1.672737] #last 7 lines
+    solid_periodic_pins.test_vals         = [-15.878958, -14.569206, 300.900000, 425.320000, 0.000000, 5.000000, -1.672714] #last 7 lines
     solid_periodic_pins.test_vals_aarch64 = [-15.879010, -14.569206, 300.900000, 425.320000, 0.000000, 5.000000, -1.672630] #last 7 lines
     test_list.append(solid_periodic_pins)
 
@@ -1426,7 +1359,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_viscosity.test_vals = [-4.738778, -4.325766, -4.610914, -5.834431, 0.521730, -4.934375, 5.000000, -1.887191, 5.000000, -5.499917, 5.000000, -1.770845, 2.292904, 0.971941, 0.608500, 0.712464]
     species2_primitiveVenturi_mixingmodel_viscosity.new_output = True
     test_list.append(species2_primitiveVenturi_mixingmodel_viscosity)
-
+    
     # 2 species (1 eq) primitive venturi mixing using mixing model including heat capacity and mass diffusivity
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2           = TestCase('species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg')
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg_dir   = "species_transport/venturi_primitive_3species"
@@ -1438,7 +1371,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.new_output = True
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.tol       = 0.00001
     test_list.append(species2_primitiveVenturi_mixingmodel_heatcapacity_H2)
-
+    
     # 2 species (1 eq) primitive venturi mixing using mixing model including heat capacity and mass diffusivity NonDimensional case
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND           = TestCase('species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg')
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg_dir   = "species_transport/venturi_primitive_3species"
@@ -1450,7 +1383,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.new_output = True
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.tol       = 0.00001
     test_list.append(species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND)
-
+    
     # 2 species (1 eq) primitive venturi mixing
     species2_primitiveVenturi           = TestCase('species2_primitiveVenturi')
     species2_primitiveVenturi.cfg_dir   = "species_transport/venturi_primitive_3species"
@@ -1468,7 +1401,7 @@ def main():
     species_primitiveVenturi_boundedscalar.test_vals   = [-5.297585, -4.397797, -4.377086, -5.593131, -1.011782, -5.623540, 5.000000, -1.775123, 5.000000, -4.086339, 5.000000, -2.080187, 0.000424, 0.000424, 0.000000, 0.000000]
     species_primitiveVenturi_boundedscalar.new_output  = True
     test_list.append(species_primitiveVenturi_boundedscalar)
-
+    
     # 2 species (1 eq) primitive venturi mixing using mixing model including inlet markers for turbulent intensity and viscosity ratios
     species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS           = TestCase('species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg')
     species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg_dir   = "species_transport/venturi_primitive_3species"
diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index a24bfe5d844..0ab26a2dad3 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -6,8 +6,8 @@
 #  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
-#
-# The SU2 Project is maintained by the SU2 Foundation
+# 
+# The SU2 Project is maintained by the SU2 Foundation 
 # (http://su2foundation.org)
 #
 # Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
@@ -16,7 +16,7 @@
 # modify it under the terms of the GNU Lesser General Public
 # License as published by the Free Software Foundation; either
 # version 2.1 of the License, or (at your option) any later version.
-#
+# 
 # SU2 is distributed in the hope that it will be useful,
 # but WITHOUT ANY WARRANTY; without even the implied warranty of
 # MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
@@ -29,11 +29,11 @@
 from __future__ import print_function
 
 import sys
-from TestCase import TestCase
+from TestCase import TestCase    
 
 def main():
-    '''This program runs SU2 and ensures that the output matches specified values.
-       This will be used to do checks when code is pushed to github
+    '''This program runs SU2 and ensures that the output matches specified values. 
+       This will be used to do checks when code is pushed to github 
        to make sure nothing is broken. '''
 
     test_list = []
@@ -49,7 +49,7 @@ def main():
     discadj_naca0012.test_iter = 100
     discadj_naca0012.test_vals = [-3.561506, -8.926634, -0.000000, 0.005587]
     test_list.append(discadj_naca0012)
-
+   
     # Inviscid Cylinder 3D (multiple markers)
     discadj_cylinder3D           = TestCase('discadj_cylinder3D')
     discadj_cylinder3D.cfg_dir   = "disc_adj_euler/cylinder3D"
@@ -65,7 +65,7 @@ def main():
     discadj_arina2k.test_iter    = 20
     discadj_arina2k.test_vals    = [-3.111181, -3.501516, 6.8705e-02, 0]
     test_list.append(discadj_arina2k)
-
+    
     # Equivalent area NACA64-206
     ea_naca64206              = TestCase('ea_naca64206')
     ea_naca64206.cfg_dir      = "optimization_euler/equivalentarea_naca64206"
@@ -157,16 +157,16 @@ def main():
     #######################################################
     ### Unsteady Disc. adj. compressible RANS           ###
     #######################################################
-
+   
     # Turbulent Cylinder
     discadj_cylinder           = TestCase('unsteady_cylinder')
     discadj_cylinder.cfg_dir   = "disc_adj_rans/cylinder"
-    discadj_cylinder.cfg_file  = "cylinder.cfg"
+    discadj_cylinder.cfg_file  = "cylinder.cfg" 
     discadj_cylinder.test_iter = 9
     discadj_cylinder.test_vals = [3.746909, -1.544883, -0.008321, 0.000014] #last 4 columns
     discadj_cylinder.unsteady  = True
     test_list.append(discadj_cylinder)
-
+    
     ##############################################################
     ### Unsteady Disc. adj. compressible RANS Windowed Average ###
     ##############################################################
@@ -174,12 +174,12 @@ def main():
     # Turbulent Cylinder
     discadj_cylinder           = TestCase('unsteady_cylinder_windowed_average_AD')
     discadj_cylinder.cfg_dir   = "disc_adj_rans/cylinder"
-    discadj_cylinder.cfg_file  = "cylinder_Windowing_AD.cfg"
+    discadj_cylinder.cfg_file  = "cylinder_Windowing_AD.cfg" 
     discadj_cylinder.test_iter = 9
     discadj_cylinder.test_vals = [3.004406] #last column
     discadj_cylinder.unsteady  = True
     test_list.append(discadj_cylinder)
-
+    
     ##############################################################
     ### Unsteady Disc. adj. compressible RANS Windowed Average ###
     ##############################################################
@@ -187,14 +187,14 @@ def main():
     # Turbulent Cylinder
     discadj_cylinder           = TestCase('unsteady_cylinder_windowed_average')
     discadj_cylinder.cfg_dir   = "disc_adj_rans/cylinder"
-    discadj_cylinder.cfg_file  = "cylinder_Windowing.cfg"
+    discadj_cylinder.cfg_file  = "cylinder_Windowing.cfg" 
     discadj_cylinder.test_iter = 6
     discadj_cylinder.test_vals = [0.202349, -0.000119, 1.899933, -0.000050, 1.067900]
     discadj_cylinder.tol       = 0.0001
     discadj_cylinder.command   = TestCase.Command("mpirun -n 2", "SU2_CFD_DIRECTDIFF")
     discadj_cylinder.unsteady  = True
-    test_list.append(discadj_cylinder)
-
+    test_list.append(discadj_cylinder)  
+    
     ##########################################################################
     ### Unsteady Disc. adj. compressible RANS DualTimeStepping 1st order   ###
     ##########################################################################
@@ -224,27 +224,27 @@ def main():
     #######################################################
     ### Disc. adj. turbomachinery                       ###
     #######################################################
-
+    
     # Transonic Stator 2D
     discadj_trans_stator           = TestCase('transonic_stator')
     discadj_trans_stator.cfg_dir   = "disc_adj_turbomachinery/transonic_stator_2D"
-    discadj_trans_stator.cfg_file  = "transonic_stator.cfg"
+    discadj_trans_stator.cfg_file  = "transonic_stator.cfg" 
     discadj_trans_stator.test_iter = 79
     discadj_trans_stator.test_vals = [79.000000, -1.941681, -1.984570]
     test_list.append(discadj_trans_stator)
-
+    
     ###################################
     ### Structural Adjoint          ###
     ###################################
-
+   
     # Structural model
     discadj_fea           = TestCase('discadj_fea')
     discadj_fea.cfg_dir   = "disc_adj_fea"
-    discadj_fea.cfg_file  = "configAD_fem.cfg"
+    discadj_fea.cfg_file  = "configAD_fem.cfg" 
     discadj_fea.test_iter = 4
     discadj_fea.test_vals         = [-2.849774, -3.238669, -0.000364, -8.708700] #last 4 columns
     discadj_fea.test_vals_aarch64 = [-2.849726, -3.238594, -0.000364, -8.708700] #last 4 columns
-    test_list.append(discadj_fea)
+    test_list.append(discadj_fea) 
 
     ###################################
     ### Disc. adj. heat             ###
@@ -255,14 +255,14 @@ def main():
     discadj_heat.cfg_dir   = "disc_adj_heat"
     discadj_heat.cfg_file  = "disc_adj_heat.cfg"
     discadj_heat.test_iter = 10
-    discadj_heat.test_vals         = [-2.226525, 0.603989, 0.000000, -6.256200]
-    discadj_heat.test_vals_aarch64 = [-2.226525, 0.603989, 0.000000, -6.256200]
+    discadj_heat.test_vals         = [-2.280433, 0.714828, -0.743730, -6.767300]
+    discadj_heat.test_vals_aarch64 = [-2.280428, 0.714835, -0.743730, -6.767300]
     test_list.append(discadj_heat)
 
     ###################################
     ### Coupled FSI Adjoint         ###
     ###################################
-
+   
     # Legacy driver
     discadj_fsi           = TestCase('discadj_fsi')
     discadj_fsi.cfg_dir   = "disc_adj_fsi"
@@ -316,8 +316,8 @@ def main():
     da_unsteadyCHT_cylinder.cfg_dir   = "coupled_cht/disc_adj_unsteadyCHT_cylinder"
     da_unsteadyCHT_cylinder.cfg_file  = "chtMaster.cfg"
     da_unsteadyCHT_cylinder.test_iter = 2
-    da_unsteadyCHT_cylinder.test_vals         = [-3.508906, -4.317739, -4.241558, -11.836892, -12.862650, 0.000000, 3.688000, 0.295190]
-    da_unsteadyCHT_cylinder.test_vals_aarch64 = [-3.508906, -4.317739, -4.241558, -11.836892, -12.862650, 0.000000, 3.688000, 0.295190]
+    da_unsteadyCHT_cylinder.test_vals         = [-3.521358, -4.312658, -4.271025, -9.846075, -7.967741, 0.000000, 3.684000, 2.9483e-01]
+    da_unsteadyCHT_cylinder.test_vals_aarch64 = [-3.521358, -4.312658, -4.271025, -9.846075, -7.967741, 0.000000, 3.684000, 2.9483e-01]
     da_unsteadyCHT_cylinder.unsteady  = True
     da_unsteadyCHT_cylinder.multizone = True
     test_list.append(da_unsteadyCHT_cylinder)
@@ -364,7 +364,7 @@ def main():
     # NACA0012 Airfoil
     unsteady_naca0012           = TestCase('unsteady_NACA0012_restart_adjoint')
     unsteady_naca0012.cfg_dir   = "disc_adj_rans/naca0012"
-    unsteady_naca0012.cfg_file  = "naca0012.cfg"
+    unsteady_naca0012.cfg_file  = "naca0012.cfg" 
     unsteady_naca0012.test_iter = 14
     unsteady_naca0012.command   = TestCase.Command(exec = "discrete_adjoint.py", param = "-f")
     unsteady_naca0012.timeout   = 1600
@@ -373,7 +373,7 @@ def main():
     unsteady_naca0012.unsteady  = True
     pass_list.append(unsteady_naca0012.run_filediff())
     test_list.append(unsteady_naca0012)
-
+    
     ####################################################################################
     ### Unsteady Disc. adj. compressible RANS Windowed Average  only adjoint 		 ###
     ####################################################################################
@@ -381,7 +381,7 @@ def main():
     # NACA0012 Airfoil (Test depends on results of "unsteady_NACA0012_restart_adjoint")
     unsteady_naca0012           = TestCase('unsteady_NACA0012_adjoint_only')
     unsteady_naca0012.cfg_dir   = "disc_adj_rans/naca0012"
-    unsteady_naca0012.cfg_file  = "naca0012.cfg"
+    unsteady_naca0012.cfg_file  = "naca0012.cfg" 
     unsteady_naca0012.test_iter = 14
     unsteady_naca0012.command   = TestCase.Command(exec = "discrete_adjoint.py", param = "-m adj -f")
     unsteady_naca0012.timeout   = 1600
diff --git a/TestCases/serial_regression.py b/TestCases/serial_regression.py
index 1c3dc9c6994..9ff934437db 100644
--- a/TestCases/serial_regression.py
+++ b/TestCases/serial_regression.py
@@ -61,7 +61,7 @@ def main():
     # Inviscid single wedge, implicit
     invwedge           = TestCase('invwedge')
     invwedge.cfg_dir   = "nonequilibrium/invwedge"
-    invwedge.cfg_file  = "invwedge_ausm.cfg"
+    invwedge.cfg_file  = "invwedge.cfg"
     invwedge.test_iter = 10
     invwedge.test_vals         = [-1.046323, -1.571086, -18.300667, -18.628064, -18.574092, 2.271778, 1.875687, 5.315769, 0.870008]
     invwedge.test_vals_aarch64 = [-1.046323, -1.571086, -18.300012, -18.627418, -18.573436, 2.271778, 1.875687, 5.315769, 0.870008]
diff --git a/TestCases/serial_regression_AD.py b/TestCases/serial_regression_AD.py
index c3d0b926e74..536727c2d6c 100644
--- a/TestCases/serial_regression_AD.py
+++ b/TestCases/serial_regression_AD.py
@@ -6,8 +6,8 @@
 #  \version 7.5.0 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
-#
-# The SU2 Project is maintained by the SU2 Foundation
+# 
+# The SU2 Project is maintained by the SU2 Foundation 
 # (http://su2foundation.org)
 #
 # Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
@@ -16,7 +16,7 @@
 # modify it under the terms of the GNU Lesser General Public
 # License as published by the Free Software Foundation; either
 # version 2.1 of the License, or (at your option) any later version.
-#
+# 
 # SU2 is distributed in the hope that it will be useful,
 # but WITHOUT ANY WARRANTY; without even the implied warranty of
 # MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
@@ -32,8 +32,8 @@
 from TestCase import TestCase
 
 def main():
-    '''This program runs SU2 and ensures that the output matches specified values.
-       This will be used to do checks when code is pushed to github
+    '''This program runs SU2 and ensures that the output matches specified values. 
+       This will be used to do checks when code is pushed to github 
        to make sure nothing is broken. '''
 
     test_list = []
@@ -58,7 +58,7 @@ def main():
     discadj_cylinder3D.test_vals = [-3.737675, -3.842311, -0.000000, 0.000000]
     test_list.append(discadj_cylinder3D)
 
-    # Arina nozzle 2D
+    # Arina nozzle 2D  
     discadj_arina2k              = TestCase('discadj_arina2k')
     discadj_arina2k.cfg_dir      = "disc_adj_euler/arina2k"
     discadj_arina2k.cfg_file     = "Arina2KRS.cfg"
@@ -69,7 +69,7 @@ def main():
     #######################################################
     ### Disc. adj. compressible RANS                    ###
     #######################################################
-
+    
     # Adjoint turbulent NACA0012 SA
     discadj_rans_naca0012_sa           = TestCase('discadj_rans_naca0012_sa')
     discadj_rans_naca0012_sa.cfg_dir   = "disc_adj_rans/naca0012"
@@ -133,16 +133,16 @@ def main():
     #######################################################
     ### Unsteady Disc. adj. compressible RANS           ###
     #######################################################
-
+   
     # Turbulent Cylinder
     discadj_cylinder           = TestCase('unsteady_cylinder')
     discadj_cylinder.cfg_dir   = "disc_adj_rans/cylinder"
-    discadj_cylinder.cfg_file  = "cylinder.cfg"
+    discadj_cylinder.cfg_file  = "cylinder.cfg" 
     discadj_cylinder.test_iter = 9
     discadj_cylinder.test_vals = [3.746909, -1.544883, -0.008321, 0.000014] #last 4 columns
     discadj_cylinder.unsteady  = True
     test_list.append(discadj_cylinder)
-
+    
     ##########################################################################
     ### Unsteady Disc. adj. compressible RANS DualTimeStepping 1st order   ###
     ##########################################################################
@@ -181,15 +181,15 @@ def main():
     ###################################
     ### Structural Adjoint          ###
     ###################################
-
+   
     # Structural model
     discadj_fea           = TestCase('discadj_fea')
     discadj_fea.cfg_dir   = "disc_adj_fea"
-    discadj_fea.cfg_file  = "configAD_fem.cfg"
+    discadj_fea.cfg_file  = "configAD_fem.cfg" 
     discadj_fea.test_iter = 4
     discadj_fea.test_vals         = [-2.849531, -3.238474, -3.6413e-04, -8.7087] #last 4 columns
     discadj_fea.test_vals_aarch64 = [-2.849570, -3.238519, -3.6413e-04, -8.7087] #last 4 columns
-    test_list.append(discadj_fea)
+    test_list.append(discadj_fea)    
 
     ###################################
     ### Disc. adj. heat             ###
@@ -200,13 +200,13 @@ def main():
     discadj_heat.cfg_dir   = "disc_adj_heat"
     discadj_heat.cfg_file  = "disc_adj_heat.cfg"
     discadj_heat.test_iter = 10
-    discadj_heat.test_vals = [-2.227518, 0.576043, 0.000000, -7.753900] #last 4 columns
+    discadj_heat.test_vals = [-2.271569, 0.671288, -3.172000, -8.231500] #last 4 columns
     test_list.append(discadj_heat)
 
     ###################################
     ### Coupled FSI Adjoint         ###
     ###################################
-
+   
     # Structural model
     discadj_fsi           = TestCase('discadj_fsi')
     discadj_fsi.cfg_dir   = "disc_adj_fsi"
@@ -244,7 +244,7 @@ def main():
             test.tol = 0.00001
 
     pass_list = [ test.run_test() for test in test_list ]
-
+    
     ###################################
     ### Coupled RHT-CFD Adjoint     ###
     ###################################
@@ -265,7 +265,7 @@ def main():
     ######################################
     ### RUN PYTHON TESTS               ###
     ######################################
-
+    
     # test discrete_adjoint.py
     discadj_euler_py = TestCase('discadj_euler_py')
     discadj_euler_py.cfg_dir = "cont_adj_euler/naca0012"
@@ -278,7 +278,7 @@ def main():
     discadj_euler_py.test_file = "of_grad_cd.dat"
     pass_list.append(discadj_euler_py.run_filediff())
     test_list.append(discadj_euler_py)
-
+    
     # test discrete_adjoint with multiple ffd boxes
     discadj_multiple_ffd_py = TestCase('discadj_multiple_ffd_py')
     discadj_multiple_ffd_py.cfg_dir = "multiple_ffd/naca0012"
@@ -382,7 +382,7 @@ def main():
             print('  passed - %s'%test.tag)
         else:
             print('* FAILED - %s'%test.tag)
-
+    
     if all(pass_list):
         sys.exit(0)
     else:
diff --git a/TestCases/tutorials.py b/TestCases/tutorials.py
index 7d045af5ed7..5471eab7258 100644
--- a/TestCases/tutorials.py
+++ b/TestCases/tutorials.py
@@ -104,26 +104,6 @@ def main():
     DAspecies3_primitiveVenturi.command   = TestCase.Command("mpirun -n 2", "SU2_CFD_AD")
     DAspecies3_primitiveVenturi.new_output = True
     test_list.append(DAspecies3_primitiveVenturi)
-    
-    # 2 species (1 eq) kenics static mixer for composition-dependent model
-    kenics_mixer_tutorial           = TestCase('kenics_mixer_tutorial')
-    kenics_mixer_tutorial.cfg_dir   = "../Tutorials/incompressible_flow/Inc_Species_Transport_Composition_Dependent_Model"
-    kenics_mixer_tutorial.cfg_file  = "kenics_mixer_tutorial.cfg"
-    kenics_mixer_tutorial.test_iter = 10
-    kenics_mixer_tutorial.test_vals = [-7.489841, -6.823474, -6.838069, -5.157396, -7.902273, -3.174235, -7.448166, 5.000000, -1.862000, 4.000000, -5.173789, 3.000000, -6.373917, 0.025135, 0.000000, 0.025135, 0.000000, 64.095000, 8.479500, 48.089000, 7.526700]
-    kenics_mixer_tutorial.command   = TestCase.Command("mpirun -n 2", "SU2_CFD")
-    kenics_mixer_tutorial.new_output = True
-    test_list.append(kenics_mixer_tutorial)
-
-    # 90 degree pipe bend with wall functions from the experiments of Sudo et al.
-    sudo_tutorial           = TestCase('sudo_bend')
-    sudo_tutorial.cfg_dir   = "../Tutorials/incompressible_flow/Inc_Turbulent_Bend_Wallfunctions"
-    sudo_tutorial.cfg_file  = "sudo.cfg"
-    sudo_tutorial.test_iter = 10
-    sudo_tutorial.test_vals = [-13.618610, -12.647974, -12.296537, -11.658760, -13.136523, -9.550829, 15.000000, -2.369703]
-    sudo_tutorial.command   = TestCase.Command("mpirun -n 2", "SU2_CFD")
-    sudo_tutorial.new_output = True
-    test_list.append(sudo_tutorial)
 
     ### Compressible Flow
 

From c3ba96c76808d5a536804c0340a090a38f634db2 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Fri, 3 Feb 2023 21:04:49 +0100
Subject: [PATCH 172/656] Workaround for external functions.

---
 Common/src/linear_algebra/CSysSolve.cpp | 2 ++
 1 file changed, 2 insertions(+)

diff --git a/Common/src/linear_algebra/CSysSolve.cpp b/Common/src/linear_algebra/CSysSolve.cpp
index 425588c104e..76241069af6 100644
--- a/Common/src/linear_algebra/CSysSolve.cpp
+++ b/Common/src/linear_algebra/CSysSolve.cpp
@@ -980,6 +980,8 @@ unsigned long CSysSolve<ScalarType>::Solve(CSysMatrix<ScalarType> & Jacobian, co
     }
     END_SU2_OMP_SAFE_GLOBAL_ACCESS
 
+    auto placeholder = [](){};
+    AD::FuncHelper.callPrimalFuncWithADType([](){});
     AD::FuncHelper.addToTape(CSysSolve_b<ScalarType>::Solve_b);
 
     SU2_OMP_SAFE_GLOBAL_ACCESS(AD::EndExtFunc();)

From 3539882ec9a2a54dcda7eec810c077ca7209d472 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Fri, 3 Feb 2023 21:14:30 +0100
Subject: [PATCH 173/656] Fix typo.

---
 Common/src/linear_algebra/CSysSolve.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/Common/src/linear_algebra/CSysSolve.cpp b/Common/src/linear_algebra/CSysSolve.cpp
index 76241069af6..888af000957 100644
--- a/Common/src/linear_algebra/CSysSolve.cpp
+++ b/Common/src/linear_algebra/CSysSolve.cpp
@@ -981,7 +981,7 @@ unsigned long CSysSolve<ScalarType>::Solve(CSysMatrix<ScalarType> & Jacobian, co
     END_SU2_OMP_SAFE_GLOBAL_ACCESS
 
     auto placeholder = [](){};
-    AD::FuncHelper.callPrimalFuncWithADType([](){});
+    AD::FuncHelper.callPrimalFuncWithADType(placeholder);
     AD::FuncHelper.addToTape(CSysSolve_b<ScalarType>::Solve_b);
 
     SU2_OMP_SAFE_GLOBAL_ACCESS(AD::EndExtFunc();)

From 5f2e268f8da1cc211d12804de2d7dfd911b36f8f Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 5 Feb 2023 15:15:02 -0800
Subject: [PATCH 174/656] address boiler plate and return of global indices

---
 SU2_CFD/include/drivers/CDriverBase.hpp | 295 +++---------
 SU2_CFD/src/drivers/CDriverBase.cpp     | 609 +++++-------------------
 2 files changed, 172 insertions(+), 732 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index 6ff1781eb09..cb1c27f340d 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -134,36 +134,6 @@ class CDriverBase {
    */
   unsigned short GetNumberFFDBoxes() const;
 
-  /*!
-   * \brief Get the number of markers in the mesh.
-   * \return Number of markers.
-   */
-  unsigned short GetNumberMarkers() const;
-
-  /*!
-   * \brief Get all the boundary markers tags with their associated indices.
-   * \return List of boundary markers tags with their indices.
-   */
-  map<string, unsigned short> GetMarkerIndices() const;
-
-  /*!
-   * \brief Get all the boundary markers tags with their associated types.
-   * \return List of boundary markers tags with their types.
-   */
-  map<string, string> GetMarkerTypes() const;
-
-  /*!
-   * \brief Get all the boundary marker tags.
-   * \return List of boundary markers tags.
-   */
-  vector<string> GetMarkerTags() const;
-
-  /*!
-   * \brief Get all the deformable boundary marker tags.
-   * \return List of deformable boundary markers tags.
-   */
-  vector<string> GetDeformableMarkerTags() const;
-
   /*!
    * \brief Get the number of dimensions of the mesh.
    * \return Number of dimensions.
@@ -176,256 +146,144 @@ class CDriverBase {
    */
   unsigned long GetNumberElements() const;
 
-  /*!
-   * \brief Get the number of elements in the marker.
-   * \param[in] iMarker - Marker index.
-   * \return Number of elements.
-   */
-  unsigned long GetNumberMarkerElements(unsigned short iMarker) const;
-
-  /*!
-   * \brief Get the global indices of the mesh elements.
-   * \return Global element indices (nElem).
-   */
-  vector<unsigned long> GetElements() const;
-
   /*!
    * \brief Get the global index of a mesh element.
    * \param[in] iElem - Mesh element index.
    * \return Global element index.
    */
-  unsigned long GetElements(unsigned long iElem) const;
-
-  /*!
-   * \brief Get the global indices of the marker elements.
-   * \param[in] iMarker - Marker index.
-   * \return Global element indices (nElem).
-   */
-  vector<unsigned long> GetMarkerElements(unsigned short iMarker) const;
-
-  /*!
-   * \brief Get the global index of a marker element.
-   * \param[in] iMarker - Marker index.
-   * \param[in] iElem - Marker element index.
-   * \return Global element index.
-   */
-  unsigned long GetMarkerElements(unsigned short iMarker, unsigned long iElem) const;
+  unsigned long GetElementGlobalIndex(unsigned long iElem) const;
 
   /*!
-   * \brief Get the global node indices of the mesh elements.
-   * \return Element global node indices (nElem, nNode).
-   */
-  vector<vector<unsigned long>> GetElementNodes() const;
-
-  /*!
-   * \brief Get the global node indices of a mesh element.
+   * \brief Get the node indices of a mesh element.
    * \param[in] iElem - Mesh element index.
-   * \return Element global node indices (nNode).
+   * \return Element node indices (nNode).
    */
   vector<unsigned long> GetElementNodes(unsigned long iElem) const;
 
   /*!
-   * \brief Get the global node indices of the marker elements.
-   * \param[in] iMarker - Marker index.
-   * \return Element global node indices (nElem, nVertex).
-   */
-  vector<vector<unsigned long>> GetMarkerElementNodes(unsigned short iMarker) const;
-
-  /*!
-   * \brief Get the global node indices of a marker element.
-   * \param[in] iMarker - Marker index.
-   * \param[in] iElem - Marker element index.
-   * \return Element global node indices (nVertex).
-   */
-  vector<unsigned long> GetMarkerElementNodes(unsigned short iMarker, unsigned long iElem) const;
-
-  /*!
-   * \brief Get the number of nodes in the mesh.
+   * \brief Get the number of nodes in the mesh (including halos).
    * \return Number of nodes.
    */
   unsigned long GetNumberNodes() const;
 
-  /*!
-   * \brief Get the number of nodes in the marker.
-   * \param[in] iMarker - Marker index.
-   * \return Number of nodes.
-   */
-  unsigned long GetNumberMarkerNodes(unsigned short iMarker) const;
-
   /*!
    * \brief Get the number of halo nodes in the mesh.
    * \return Number of halo nodes.
    */
   unsigned long GetNumberHaloNodes() const;
 
-  /*!
-   * \brief Get the number of halo nodes in the marker.
-   * \param[in] iMarker - Marker index.
-   * \return Number of halo nodes.
-   */
-  unsigned long GetNumberMarkerHaloNodes(unsigned short iMarker) const;
-
-  /*!
-   * \brief Get the vertices of the marker.
-   * \param[in] iMarker - Marker index.
-   * \return Marker vertices (nVertex).
-   */
-  vector<unsigned long> GetMarkerVertices(unsigned short iMarker) const;
-
-  /*!
-   * \brief Get the vertex of a marker.
-   * \param[in] iMarker - Marker index.
-   * \param[in] iVertex - Marker vertex index.
-   * \return Marker vertex.
-   */
-  unsigned long GetMarkerVertices(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Get the global node indices.
-   * \return Global node indices (nNode).
-   */
-  vector<unsigned long> GetNodes() const;
-
   /*!
    * \brief Get the global node index.
    * \param[in] iPoint - Mesh node index.
    * \return Global node index.
    */
-  unsigned long GetNodes(unsigned long iPoint) const;
-
-  /*!
-   * \brief Get the global node indices of the marker vertices.
-   * \param[in] iMarker - Marker index.
-   * \return Global node indices (nVertex).
-   */
-  vector<unsigned long> GetMarkerNodes(unsigned short iMarker) const;
-
-  /*!
-   * \brief Get the global node index of a marker vertex.
-   * \param[in] iMarker - Marker index.
-   * \param[in] iVertex - Marker vertex index.
-   * \return Global node index.
-   */
-  unsigned long GetMarkerNodes(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Get the halo flags of the mesh nodes.
-   * \return Node domain flags (nNode).
-   */
-  vector<bool> GetDomain() const;
+  unsigned long GetNodeGlobalIndex(unsigned long iPoint) const;
 
   /*!
    * \brief Get the halo flag of a mesh node.
    * \param[in] iPoint - Mesh node index.
    * \return Node domain flag.
    */
-  bool GetDomain(unsigned long iPoint) const;
-
-  /*!
-   * \brief Get the halo flags of the marker vertices.
-   * \param[in] iMarker - Marker index.
-   * \return Domain flags (nVertex).
-   */
-  vector<bool> GetMarkerDomain(unsigned short iMarker) const;
+  bool GetNodeDomain(unsigned long iPoint) const;
 
   /*!
-   * \brief Get the halo flag of a marker vertex.
-   * \param[in] iMarker - Marker index.
-   * \param[in] iVertex - Marker vertex index.
-   * \return Domain flag.
+   * \brief Get the initial (un-deformed) coordinates of a mesh node.
+   * \param[in] iPoint - Mesh node index.
+   * \return Initial node coordinates (nDim).
    */
-  bool GetMarkerDomain(unsigned short iMarker, unsigned long iVertex) const;
+  vector<passivedouble> GetInitialCoordinates(unsigned long iPoint) const;
 
   /*!
-   * \brief Get the initial (un-deformed) coordinates of the mesh nodes.
-   * \return Initial node coordinates (nNode, nDim).
+   * \brief Get the current coordinates of a mesh node.
+   * \param[in] iPoint - Mesh node index.
+   * \return Node coordinates (nDim).
    */
-  vector<vector<passivedouble>> GetInitialCoordinates() const;
+  vector<passivedouble> GetCoordinates(unsigned long iPoint) const;
 
   /*!
-   * \brief Get the initial (un-deformed) coordinates of a mesh node.
+   * \brief Set the coordinates of a mesh node.
    * \param[in] iPoint - Mesh node index.
-   * \return Initial node coordinates (nDim).
+   * \param[in] values - Node coordinates (nDim).
    */
-  vector<passivedouble> GetInitialCoordinates(unsigned long iPoint) const;
+  void SetCoordinates(unsigned long iPoint, vector<passivedouble> values);
 
   /*!
-   * \brief Get the initial (un-deformed) coordinates of the marker vertices.
-   * \param[in] iMarker - Marker index.
-   * \return Initial node coordinates (nVertex, nDim).
+   * \brief Get the number of markers in the mesh.
+   * \return Number of markers.
    */
-  vector<vector<passivedouble>> GetMarkerInitialCoordinates(unsigned short iMarker) const;
+  unsigned short GetNumberMarkers() const;
 
   /*!
-   * \brief Get the initial (un-deformed) coordinates of a marker vertex.
-   * \param[in] iMarker - Marker index.
-   * \param[in] iVertex - Marker vertex index.
-   * \return Initial node coordinates (nDim).
+   * \brief Get all the boundary markers tags with their associated indices.
+   * \return Map of boundary markers tags to their indices.
    */
-  vector<passivedouble> GetMarkerInitialCoordinates(unsigned short iMarker, unsigned long iVertex) const;
+  map<string, unsigned short> GetMarkerIndices() const;
 
   /*!
-   * \brief Get the coordinates of the mesh nodes.
-   * \return Node coordinates (nNode, nDim).
+   * \brief Get all the boundary markers tags with their associated types.
+   * \return Map of boundary markers tags to their types.
    */
-  vector<vector<passivedouble>> GetCoordinates() const;
+  map<string, string> GetMarkerTypes() const;
 
   /*!
-   * \brief Get the coordinates of a mesh node.
-   * \param[in] iPoint - Mesh node index.
-   * \return Node coordinates (nDim).
+   * \brief Get all the boundary marker tags.
+   * \return List of boundary markers tags.
    */
-  vector<passivedouble> GetCoordinates(unsigned long iPoint) const;
+  vector<string> GetMarkerTags() const;
 
   /*!
-   * \brief Get the coordinates of the marker vertices.
-   * \param[in] iMarker - Marker index.
-   * \return Node coordinates (nVertex, nDim).
+   * \brief Get all the deformable boundary marker tags.
+   * \return List of deformable boundary markers tags.
    */
-  vector<vector<passivedouble>> GetMarkerCoordinates(unsigned short iMarker) const;
+  vector<string> GetDeformableMarkerTags() const;
 
   /*!
-   * \brief Get the coordinates of a marker vertex.
+   * \brief Get the number of elements in the marker.
    * \param[in] iMarker - Marker index.
-   * \param[in] iVertex - Marker vertex index.
-   * \return Node coordinates (nDim).
+   * \return Number of elements.
    */
-  vector<passivedouble> GetMarkerCoordinates(unsigned short iMarker, unsigned long iVertex) const;
+  unsigned long GetNumberMarkerElements(unsigned short iMarker) const;
 
   /*!
-   * \brief Set the coordinates of the mesh nodes.
-   * \param[in] values - Node coordinates (nNode, nDim).
+   * \brief Get the global index of a marker element.
+   * \param[in] iMarker - Marker index.
+   * \param[in] iElem - Marker element index.
+   * \return Global element index.
    */
-  void SetCoordinates(vector<vector<passivedouble>> values);
+  unsigned long GetMarkerElementGlobalIndex(unsigned short iMarker, unsigned long iElem) const;
 
   /*!
-   * \brief Set the coordinates of a mesh node.
-   * \param[in] iPoint - Mesh node index.
-   * \param[in] values - Node coordinates (nDim).
+   * \brief Get the node indices of a marker element.
+   * \param[in] iMarker - Marker index.
+   * \param[in] iElem - Marker element index.
+   * \return Element node indices.
    */
-  void SetCoordinates(unsigned long iPoint, vector<passivedouble> values);
+  vector<unsigned long> GetMarkerElementNodes(unsigned short iMarker, unsigned long iElem) const;
 
   /*!
-   * \brief Set the coordinates of the marker vertices.
+   * \brief Get the number of nodes in the marker.
    * \param[in] iMarker - Marker index.
-   * \param[in] values - Node coordinates (nVertex, nDim).
+   * \return Number of nodes.
    */
-  void SetMarkerCoordinates(unsigned short iMarker, vector<vector<passivedouble>> values);
+  unsigned long GetNumberMarkerNodes(unsigned short iMarker) const;
 
   /*!
-   * \brief Set the coordinates of a marker vertex.
+   * \brief Get the node index of a marker.
    * \param[in] iMarker - Marker index.
    * \param[in] iVertex - Marker vertex index.
-   * \param[in] values - Node coordinates (nDim).
+   * \return Marker vertex.
    */
-  void SetMarkerCoordinates(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values);
+  unsigned long GetMarkerNode(unsigned short iMarker, unsigned long iVertex) const;
 
   /*!
-   * \brief Get the displacements of the marker vertices.
+   * \brief Get the normal vector of a marker vertex.
    * \param[in] iMarker - Marker index.
-   * \return Node displacements (nVertex, nDim).
+   * \param[in] iVertex - Marker vertex index.
+   * \param[in] normalize - If true, the unit (i.e. normalized) normal vector is returned.
+   * \return Node normal vector (nDim).
    */
-  vector<vector<passivedouble>> GetMarkerDisplacements(unsigned short iMarker) const;
+  vector<passivedouble> GetMarkerVertexNormals(unsigned short iMarker, unsigned long iVertex,
+                                               bool normalize = false) const;
 
   /*!
    * \brief Get the displacements of a marker vertex.
@@ -435,13 +293,6 @@ class CDriverBase {
    */
   vector<passivedouble> GetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex) const;
 
-  /*!
-   * \brief Set the displacements of the marker vertices.
-   * \param[in] iMarker - Marker index.
-   * \param[in] values - Node displacements (nVertex, nDim).
-   */
-  void SetMarkerDisplacements(unsigned short iMarker, vector<vector<passivedouble>> values);
-
   /*!
    * \brief Set the displacements of a marker vertex.
    * \param[in] iMarker - Marker index.
@@ -450,13 +301,6 @@ class CDriverBase {
    */
   void SetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values);
 
-  /*!
-   * \brief Get the velocities of the marker vertices.
-   * \param[in] iMarker - Marker index.
-   * \return Node velocities (nVertex, nDim).
-   */
-  vector<vector<passivedouble>> GetMarkerVelocities(unsigned short iMarker) const;
-
   /*!
    * \brief Get the velocities of a marker vertex.
    * \param[in] iMarker - Marker index.
@@ -465,13 +309,6 @@ class CDriverBase {
    */
   vector<passivedouble> GetMarkerVelocities(unsigned short iMarker, unsigned long iVertex) const;
 
-  /*!
-   * \brief Set the velocities of the marker vertices.
-   * \param[in] iMarker - Marker index.
-   * \param[in] values - Node velocities (nVertex, nDim).
-   */
-  void SetMarkerVelocities(unsigned short iMarker, vector<vector<passivedouble>> values);
-
   /*!
    * \brief Set the velocities of a marker vertex.
    * \param[in] iMarker - Marker index.
@@ -480,24 +317,6 @@ class CDriverBase {
    */
   void SetMarkerVelocities(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values);
 
-  /*!
-   * \brief Get the normal vectors of the marker vertices.
-   * \param[in] iMarker - Marker index.
-   * \param[in] normalize - If true, the unit (i.e. normalized) normal vector is returned.
-   * \return Node normal vectors (nVertex, nDim).
-   */
-  vector<vector<passivedouble>> GetMarkerVertexNormals(unsigned short iMarker, bool normalize = false) const;
-
-  /*!
-   * \brief Get the normal vector of a marker vertex.
-   * \param[in] iMarker - Marker index.
-   * \param[in] iVertex - Marker vertex index.
-   * \param[in] normalize - If true, the unit (i.e. normalized) normal vector is returned.
-   * \return Node normal vector (nDim).
-   */
-  vector<passivedouble> GetMarkerVertexNormals(unsigned short iMarker, unsigned long iVertex,
-                                               bool normalize = false) const;
-
   /*!
    * \brief Communicate the boundary mesh displacements.
    */
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index fd7b2948301..5097fe345ec 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -78,6 +78,90 @@ unsigned short CDriverBase::GetNumberDesignVariables() const { return main_confi
 
 unsigned short CDriverBase::GetNumberFFDBoxes() const { return main_config->GetnFFDBox(); }
 
+unsigned long CDriverBase::GetNumberDimensions() const { return main_geometry->GetnDim(); }
+
+unsigned long CDriverBase::GetNumberElements() const { return main_geometry->GetnElem(); }
+
+unsigned long CDriverBase::GetElementGlobalIndex(unsigned long iElem) const {
+  if (iElem >= GetNumberElements()) {
+    SU2_MPI::Error("Element index exceeds size.", CURRENT_FUNCTION);
+  }
+  return main_geometry->elem[iElem]->GetGlobalIndex();
+}
+
+vector<unsigned long> CDriverBase::GetElementNodes(unsigned long iElem) const {
+  if (iElem >= GetNumberElements()) {
+    SU2_MPI::Error("Element index exceeds size.", CURRENT_FUNCTION);
+  }
+  const auto nNode = main_geometry->elem[iElem]->GetnNodes();
+  vector<unsigned long> values(nNode);
+
+  for (auto iNode = 0u; iNode < nNode; iNode++) {
+    values[iNode] = main_geometry->elem[iElem]->GetNode(iNode);
+  }
+  return values;
+}
+
+unsigned long CDriverBase::GetNumberNodes() const { return main_geometry->GetnPoint(); }
+
+unsigned long CDriverBase::GetNumberHaloNodes() const {
+  return main_geometry->GetnPoint() - main_geometry->GetnPointDomain();
+}
+
+unsigned long CDriverBase::GetNodeGlobalIndex(unsigned long iPoint) const {
+  if (iPoint >= GetNumberNodes()) {
+    SU2_MPI::Error("Node index exceeds mesh size.", CURRENT_FUNCTION);
+  }
+  return main_geometry->nodes->GetGlobalIndex(iPoint);
+}
+
+bool CDriverBase::GetNodeDomain(unsigned long iPoint) const {
+  if (iPoint >= GetNumberNodes()) {
+    SU2_MPI::Error("Node index exceeds mesh size.", CURRENT_FUNCTION);
+  }
+  return main_geometry->nodes->GetDomain(iPoint);
+}
+
+vector<passivedouble> CDriverBase::GetInitialCoordinates(unsigned long iPoint) const {
+  if (iPoint >= GetNumberNodes()) {
+    SU2_MPI::Error("Node index exceeds mesh size.", CURRENT_FUNCTION);
+  }
+  vector<passivedouble> values(nDim, 0.0);
+
+  if (main_config->GetDeform_Mesh()) {
+    for (auto iDim = 0u; iDim < nDim; iDim++) {
+      const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord(iPoint, iDim);
+      values[iDim] = SU2_TYPE::GetValue(value);
+    }
+  }
+  return values;
+}
+
+vector<passivedouble> CDriverBase::GetCoordinates(unsigned long iPoint) const {
+  if (iPoint >= GetNumberNodes()) {
+    SU2_MPI::Error("Node index exceeds mesh size.", CURRENT_FUNCTION);
+  }
+  vector<passivedouble> values;
+
+  for (auto iDim = 0u; iDim < nDim; iDim++) {
+    const su2double value = main_geometry->nodes->GetCoord(iPoint, iDim);
+    values.push_back(SU2_TYPE::GetValue(value));
+  }
+  return values;
+}
+
+void CDriverBase::SetCoordinates(unsigned long iPoint, vector<passivedouble> values) {
+  if (iPoint >= GetNumberNodes()) {
+    SU2_MPI::Error("Node index exceeds mesh size.", CURRENT_FUNCTION);
+  }
+  if (values.size() != nDim) {
+    SU2_MPI::Error("Invalid number of dimensions!", CURRENT_FUNCTION);
+  }
+  for (auto iDim = 0u; iDim < nDim; iDim++) {
+    main_geometry->nodes->SetCoord(iPoint, iDim, values[iDim]);
+  }
+}
+
 unsigned short CDriverBase::GetNumberMarkers() const { return main_config->GetnMarker_All(); }
 
 map<string, unsigned short> CDriverBase::GetMarkerIndices() const {
@@ -85,11 +169,8 @@ map<string, unsigned short> CDriverBase::GetMarkerIndices() const {
   map<string, unsigned short> indexMap;
 
   for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
-    auto tag = main_config->GetMarker_All_TagBound(iMarker);
-
-    indexMap[tag] = iMarker;
+    indexMap[main_config->GetMarker_All_TagBound(iMarker)] = iMarker;
   }
-
   return indexMap;
 }
 
@@ -160,594 +241,134 @@ map<string, string> CDriverBase::GetMarkerTypes() const {
 }
 
 vector<string> CDriverBase::GetMarkerTags() const {
-  vector<string> tags;
   const auto nMarker = main_config->GetnMarker_All();
+  vector<string> tags(nMarker);
 
   for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
-    tags.push_back(main_config->GetMarker_All_TagBound(iMarker));
+    tags[iMarker] = main_config->GetMarker_All_TagBound(iMarker);
   }
-
   return tags;
 }
 
 vector<string> CDriverBase::GetDeformableMarkerTags() const {
-  vector<string> tags;
   const auto nMarker = main_config->GetnMarker_Deform_Mesh();
+  vector<string> tags(nMarker);
 
   for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
-    tags.push_back(main_config->GetMarker_Deform_Mesh_TagBound(iMarker));
+    tags[iMarker] = main_config->GetMarker_Deform_Mesh_TagBound(iMarker);
   }
-
   return tags;
 }
 
-unsigned long CDriverBase::GetNumberDimensions() const { return main_geometry->GetnDim(); }
-
-unsigned long CDriverBase::GetNumberElements() const { return main_geometry->GetnElem(); }
-
 unsigned long CDriverBase::GetNumberMarkerElements(unsigned short iMarker) const {
   if (iMarker >= GetNumberMarkers()) {
     SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
   }
-
   return main_geometry->GetnElem_Bound(iMarker);
 }
 
-vector<unsigned long> CDriverBase::GetElements() const {
-  const auto nElem = GetNumberElements();
-
-  vector<unsigned long> values;
-
-  for (auto iElem = 0ul; iElem < nElem; iElem++) {
-    values.push_back(GetElements(iElem));
-  }
-
-  return values;
-}
-
-unsigned long CDriverBase::GetElements(unsigned long iElem) const {
-  if (iElem >= GetNumberElements()) {
-    SU2_MPI::Error("Element index exceeds size.", CURRENT_FUNCTION);
-  }
-
-  return main_geometry->elem[iElem]->GetGlobalIndex();
-}
-
-vector<unsigned long> CDriverBase::GetMarkerElements(unsigned short iMarker) const {
-  const auto nElem = GetNumberMarkerElements(iMarker);
-
-  vector<unsigned long> values;
-
-  for (auto iElem = 0ul; iElem < nElem; iElem++) {
-    values.push_back(GetMarkerElements(iMarker, iElem));
-  }
-
-  return values;
-}
-
-unsigned long CDriverBase::GetMarkerElements(unsigned short iMarker, unsigned long iElem) const {
+unsigned long CDriverBase::GetMarkerElementGlobalIndex(unsigned short iMarker, unsigned long iElem) const {
   if (iElem >= GetNumberMarkerElements(iMarker)) {
     SU2_MPI::Error("Marker element index exceeds size.", CURRENT_FUNCTION);
   }
-
   return main_geometry->bound[iMarker][iElem]->GetGlobalIndex();
 }
 
-vector<vector<unsigned long>> CDriverBase::GetElementNodes() const {
-  const auto nElem = GetNumberElements();
-
-  vector<vector<unsigned long>> values;
-
-  for (auto iElem = 0ul; iElem < nElem; iElem++) {
-    values.push_back(GetElementNodes(iElem));
-  }
-
-  return values;
-}
-
-vector<unsigned long> CDriverBase::GetElementNodes(unsigned long iElem) const {
-  if (iElem >= GetNumberElements()) {
-    SU2_MPI::Error("Element index exceeds size.", CURRENT_FUNCTION);
-  }
-
-  unsigned short nNode = main_geometry->elem[iElem]->GetnNodes();
-
-  vector<unsigned long> values;
-
-  for (auto iNode = 0u; iNode < nNode; iNode++) {
-    unsigned long iPoint = main_geometry->elem[iElem]->GetNode(iNode);
-
-    values.push_back(main_geometry->nodes->GetGlobalIndex(iPoint));
-  }
-
-  return values;
-}
-
-vector<vector<unsigned long>> CDriverBase::GetMarkerElementNodes(unsigned short iMarker) const {
-  const auto nElem = GetNumberMarkerElements(iMarker);
-
-  vector<vector<unsigned long>> values;
-
-  for (auto iElem = 0ul; iElem < nElem; iElem++) {
-    values.push_back(GetMarkerElementNodes(iMarker, iElem));
-  }
-
-  return values;
-}
-
 vector<unsigned long> CDriverBase::GetMarkerElementNodes(unsigned short iMarker, unsigned long iElem) const {
   if (iElem >= GetNumberMarkerElements(iMarker)) {
     SU2_MPI::Error("Marker element index exceeds size.", CURRENT_FUNCTION);
   }
-
   unsigned short nNode = main_geometry->bound[iMarker][iElem]->GetnNodes();
-
-  vector<unsigned long> values;
+  vector<unsigned long> values(nNode);
 
   for (auto iNode = 0u; iNode < nNode; iNode++) {
-    unsigned long iPoint = main_geometry->bound[iMarker][iElem]->GetNode(iNode);
-
-    values.push_back(main_geometry->nodes->GetGlobalIndex(iPoint));
+    values[iNode] = main_geometry->bound[iMarker][iElem]->GetNode(iNode);
   }
-
   return values;
 }
 
-unsigned long CDriverBase::GetNumberNodes() const { return main_geometry->GetnPoint(); }
-
 unsigned long CDriverBase::GetNumberMarkerNodes(unsigned short iMarker) const {
   if (iMarker >= GetNumberMarkers()) {
     SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
   }
-
   return main_geometry->GetnVertex(iMarker);
 }
 
-unsigned long CDriverBase::GetNumberHaloNodes() const {
-  const auto nPoint = GetNumberNodes();
-  unsigned long nHalo = 0;
-
-  for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
-    if (!(main_geometry->nodes->GetDomain(iPoint))) {
-      nHalo += 1;
-    }
-  }
-
-  return nHalo;
-}
-
-unsigned long CDriverBase::GetNumberMarkerHaloNodes(unsigned short iMarker) const {
-  const auto nVertex = GetNumberMarkerNodes(iMarker);
-  unsigned long nHalo = 0;
-
-  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-    auto iPoint = GetMarkerVertices(iMarker, iVertex);
-
-    if (!(main_geometry->nodes->GetDomain(iPoint))) {
-      nHalo += 1;
-    }
-  }
-
-  return nHalo;
-}
-
-vector<unsigned long> CDriverBase::GetMarkerVertices(unsigned short iMarker) const {
-  const auto nVertex = GetNumberMarkerNodes(iMarker);
-
-  vector<unsigned long> values;
-
-  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-    values.push_back(GetMarkerVertices(iMarker, iVertex));
-  }
-
-  return values;
-}
-
-unsigned long CDriverBase::GetMarkerVertices(unsigned short iMarker, unsigned long iVertex) const {
+unsigned long CDriverBase::GetMarkerNode(unsigned short iMarker, unsigned long iVertex) const {
   if (iVertex >= GetNumberMarkerNodes(iMarker)) {
     SU2_MPI::Error("Vertex index exceeds marker size.", CURRENT_FUNCTION);
   }
-
   return geometry_container[MESH_0][INST_0][ZONE_0]->vertex[iMarker][iVertex]->GetNode();
 }
 
-vector<unsigned long> CDriverBase::GetNodes() const {
-  const auto nPoint = GetNumberNodes();
-
-  vector<unsigned long> values;
-
-  for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
-    values.push_back(GetNodes(iPoint));
-  }
-
-  return values;
-}
-
-unsigned long CDriverBase::GetNodes(unsigned long iPoint) const {
-  if (iPoint >= GetNumberNodes()) {
-    SU2_MPI::Error("Node index exceeds mesh size.", CURRENT_FUNCTION);
-  }
-
-  return main_geometry->nodes->GetGlobalIndex(iPoint);
-}
-
-vector<unsigned long> CDriverBase::GetMarkerNodes(unsigned short iMarker) const {
-  const auto nVertex = GetNumberMarkerNodes(iMarker);
-
-  vector<unsigned long> values;
-
-  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-    values.push_back(GetMarkerNodes(iMarker, iVertex));
-  }
-
-  return values;
-}
-
-unsigned long CDriverBase::GetMarkerNodes(unsigned short iMarker, unsigned long iVertex) const {
-  auto iPoint = GetMarkerVertices(iMarker, iVertex);
-
-  return main_geometry->nodes->GetGlobalIndex(iPoint);
-}
-
-vector<bool> CDriverBase::GetDomain() const {
-  const auto nPoint = GetNumberNodes();
-
-  vector<bool> values;
-
-  for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
-    values.push_back(GetDomain(iPoint));
-  }
-
-  return values;
-}
-
-bool CDriverBase::GetDomain(unsigned long iPoint) const {
-  if (iPoint >= GetNumberNodes()) {
-    SU2_MPI::Error("Node index exceeds mesh size.", CURRENT_FUNCTION);
-  }
-
-  return main_geometry->nodes->GetDomain(iPoint);
-}
-
-vector<bool> CDriverBase::GetMarkerDomain(unsigned short iMarker) const {
-  const auto nVertex = GetNumberMarkerNodes(iMarker);
-
-  vector<bool> values;
-
-  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-    values.push_back(GetMarkerDomain(iMarker, iVertex));
-  }
-
-  return values;
-}
-
-bool CDriverBase::GetMarkerDomain(unsigned short iMarker, unsigned long iVertex) const {
-  auto iPoint = GetMarkerVertices(iMarker, iVertex);
-
-  return main_geometry->nodes->GetDomain(iPoint);
-}
-
-vector<vector<passivedouble>> CDriverBase::GetInitialCoordinates() const {
-  const auto nPoint = GetNumberNodes();
-
-  vector<vector<passivedouble>> values;
-
-  for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
-    values.push_back(GetInitialCoordinates(iPoint));
-  }
-
-  return values;
-}
-
-vector<passivedouble> CDriverBase::GetInitialCoordinates(unsigned long iPoint) const {
-  if (iPoint >= GetNumberNodes()) {
-    SU2_MPI::Error("Node index exceeds mesh size.", CURRENT_FUNCTION);
-  }
-
-  vector<passivedouble> values(nDim, 0.0);
-
-  if (!main_config->GetDeform_Mesh()) {
-    return values;
-  }
-
-  for (auto iDim = 0u; iDim < nDim; iDim++) {
-    const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord(iPoint, iDim);
-
-    values[iDim] = SU2_TYPE::GetValue(value);
-  }
-
-  return values;
-}
-
-vector<vector<passivedouble>> CDriverBase::GetMarkerInitialCoordinates(unsigned short iMarker) const {
-  const auto nVertex = GetNumberMarkerNodes(iMarker);
-
-  vector<vector<passivedouble>> values;
-
-  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-    values.push_back(GetMarkerInitialCoordinates(iMarker, iVertex));
+vector<passivedouble> CDriverBase::GetMarkerVertexNormals(unsigned short iMarker, unsigned long iVertex,
+                                                          bool normalize) const {
+  if (iVertex >= GetNumberMarkerNodes(iMarker)) {
+    SU2_MPI::Error("Vertex index exceeds marker size.", CURRENT_FUNCTION);
   }
-
-  return values;
-}
-
-vector<passivedouble> CDriverBase::GetMarkerInitialCoordinates(unsigned short iMarker, unsigned long iVertex) const {
-  auto iPoint = GetMarkerVertices(iMarker, iVertex);
+  const auto* normal = main_geometry->vertex[iMarker][iVertex]->GetNormal();
+  const su2double area = normalize ? GeometryToolbox::Norm(nDim, normal) : 1.0;
 
   vector<passivedouble> values(nDim, 0.0);
 
-  if (!main_config->GetDeform_Mesh()) {
-    return values;
-  }
-
-  for (auto iDim = 0u; iDim < nDim; iDim++) {
-    const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord(iPoint, iDim);
-
-    values[iDim] = SU2_TYPE::GetValue(value);
-  }
-
-  return values;
-}
-
-vector<vector<passivedouble>> CDriverBase::GetCoordinates() const {
-  const auto nPoint = GetNumberNodes();
-
-  vector<vector<passivedouble>> values;
-
-  for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
-    values.push_back(GetCoordinates(iPoint));
-  }
-
-  return values;
-}
-
-vector<passivedouble> CDriverBase::GetCoordinates(unsigned long iPoint) const {
-  if (iPoint >= GetNumberNodes()) {
-    SU2_MPI::Error("Node index exceeds mesh size.", CURRENT_FUNCTION);
-  }
-
-  vector<passivedouble> values;
-
   for (auto iDim = 0u; iDim < nDim; iDim++) {
-    const su2double value = main_geometry->nodes->GetCoord(iPoint, iDim);
-
-    values.push_back(SU2_TYPE::GetValue(value));
+    values[iDim] = SU2_TYPE::GetValue(normal[iDim] / area);
   }
-
-  return values;
-}
-
-vector<vector<passivedouble>> CDriverBase::GetMarkerCoordinates(unsigned short iMarker) const {
-  const auto nVertex = GetNumberMarkerNodes(iMarker);
-
-  vector<vector<passivedouble>> values;
-
-  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-    values.push_back(GetMarkerCoordinates(iMarker, iVertex));
-  }
-
-  return values;
-}
-
-vector<passivedouble> CDriverBase::GetMarkerCoordinates(unsigned short iMarker, unsigned long iVertex) const {
-  auto iPoint = GetMarkerVertices(iMarker, iVertex);
-
-  vector<passivedouble> values;
-
-  for (auto iDim = 0u; iDim < nDim; iDim++) {
-    const su2double value = main_geometry->nodes->GetCoord(iPoint, iDim);
-
-    values.push_back(SU2_TYPE::GetValue(value));
-  }
-
-  return values;
-}
-
-void CDriverBase::SetCoordinates(vector<vector<passivedouble>> values) {
-  const auto nPoint = GetNumberNodes();
-
-  if (values.size() != nPoint) {
-    SU2_MPI::Error("Invalid number of nodes!", CURRENT_FUNCTION);
-  }
-
-  for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
-    SetCoordinates(iPoint, values[iPoint]);
-  }
-}
-
-void CDriverBase::SetCoordinates(unsigned long iPoint, vector<passivedouble> values) {
-  if (iPoint >= GetNumberNodes()) {
-    SU2_MPI::Error("Node index exceeds mesh size.", CURRENT_FUNCTION);
-  }
-  if (values.size() != nDim) {
-    SU2_MPI::Error("Invalid number of dimensions!", CURRENT_FUNCTION);
-  }
-
-  for (auto iDim = 0u; iDim < nDim; iDim++) {
-    main_geometry->nodes->SetCoord(iPoint, iDim, values[iDim]);
-  }
-}
-
-void CDriverBase::SetMarkerCoordinates(unsigned short iMarker, vector<vector<passivedouble>> values) {
-  const auto nVertex = GetNumberMarkerNodes(iMarker);
-
-  if (values.size() != nVertex) {
-    SU2_MPI::Error("Invalid number of marker vertices!", CURRENT_FUNCTION);
-  }
-
-  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-    SetMarkerCoordinates(iMarker, iVertex, values[iVertex]);
-  }
-}
-
-void CDriverBase::SetMarkerCoordinates(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
-  auto iPoint = GetMarkerVertices(iMarker, iVertex);
-
-  if (values.size() != nDim) {
-    SU2_MPI::Error("Invalid number of dimensions!", CURRENT_FUNCTION);
-  }
-
-  for (auto iDim = 0u; iDim < nDim; iDim++) {
-    main_geometry->nodes->SetCoord(iPoint, iDim, values[iDim]);
-  }
-}
-
-vector<vector<passivedouble>> CDriverBase::GetMarkerDisplacements(unsigned short iMarker) const {
-  const auto nVertex = GetNumberMarkerNodes(iMarker);
-
-  vector<vector<passivedouble>> values;
-
-  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-    values.push_back(GetMarkerDisplacements(iMarker, iVertex));
-  }
-
   return values;
 }
 
 vector<passivedouble> CDriverBase::GetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex) const {
-  auto iPoint = GetMarkerVertices(iMarker, iVertex);
-
   vector<passivedouble> values(nDim, 0.0);
 
-  if (!main_config->GetDeform_Mesh()) {
-    return values;
-  }
-
-  for (auto iDim = 0u; iDim < nDim; iDim++) {
-    const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetBound_Disp(iPoint, iDim);
-
-    values[iDim] = SU2_TYPE::GetValue(value);
+  if (main_config->GetDeform_Mesh()) {
+    const auto iPoint = GetMarkerNode(iMarker, iVertex);
+    for (auto iDim = 0u; iDim < nDim; iDim++) {
+      const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetBound_Disp(iPoint, iDim);
+      values[iDim] = SU2_TYPE::GetValue(value);
+    }
   }
-
   return values;
 }
 
-void CDriverBase::SetMarkerDisplacements(unsigned short iMarker, vector<vector<passivedouble>> values) {
-  if (!main_config->GetDeform_Mesh()) {
-    SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
-  }
-
-  const auto nVertex = GetNumberMarkerNodes(iMarker);
-
-  if (values.size() != nVertex) {
-    SU2_MPI::Error("Invalid number of marker vertices!", CURRENT_FUNCTION);
-  }
-
-  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-    SetMarkerDisplacements(iMarker, iVertex, values[iVertex]);
-  }
-}
-
 void CDriverBase::SetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
   if (!main_config->GetDeform_Mesh()) {
     SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
   }
-
-  auto iPoint = GetMarkerVertices(iMarker, iVertex);
-
   if (values.size() != nDim) {
     SU2_MPI::Error("Invalid number of dimensions!", CURRENT_FUNCTION);
   }
+  const auto iPoint = GetMarkerNode(iMarker, iVertex);
 
   for (auto iDim = 0u; iDim < nDim; iDim++) {
     solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->SetBound_Disp(iPoint, iDim, values[iDim]);
   }
 }
 
-vector<vector<passivedouble>> CDriverBase::GetMarkerVelocities(unsigned short iMarker) const {
-  const auto nVertex = GetNumberMarkerNodes(iMarker);
-
-  vector<vector<passivedouble>> values;
-
-  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-    values.push_back(GetMarkerVelocities(iMarker, iVertex));
-  }
-
-  return values;
-}
-
 vector<passivedouble> CDriverBase::GetMarkerVelocities(unsigned short iMarker, unsigned long iVertex) const {
-  auto iPoint = GetMarkerVertices(iMarker, iVertex);
-
   vector<passivedouble> values(nDim, 0.0);
 
-  if (!main_config->GetDeform_Mesh()) {
-    return values;
-  }
-
-  for (auto iDim = 0u; iDim < nDim; iDim++) {
-    const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetBound_Vel(iPoint, iDim);
-
-    values[iDim] = SU2_TYPE::GetValue(value);
+  if (main_config->GetDeform_Mesh()) {
+    const auto iPoint = GetMarkerNode(iMarker, iVertex);
+    for (auto iDim = 0u; iDim < nDim; iDim++) {
+      const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetBound_Vel(iPoint, iDim);
+      values[iDim] = SU2_TYPE::GetValue(value);
+    }
   }
-
   return values;
 }
 
-void CDriverBase::SetMarkerVelocities(unsigned short iMarker, vector<vector<passivedouble>> values) {
-  if (!main_config->GetDeform_Mesh()) {
-    SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
-  }
-
-  const auto nVertex = GetNumberMarkerNodes(iMarker);
-
-  if (values.size() != nVertex) {
-    SU2_MPI::Error("Invalid number of marker vertices!", CURRENT_FUNCTION);
-  }
-
-  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-    SetMarkerVelocities(iMarker, iVertex, values[iVertex]);
-  }
-}
-
 void CDriverBase::SetMarkerVelocities(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
   if (!main_config->GetDeform_Mesh()) {
     SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
   }
-
-  auto iPoint = GetMarkerVertices(iMarker, iVertex);
-
   if (values.size() != nDim) {
     SU2_MPI::Error("Invalid number of dimensions!", CURRENT_FUNCTION);
   }
+  const auto iPoint = GetMarkerNode(iMarker, iVertex);
 
   for (auto iDim = 0u; iDim < nDim; iDim++) {
-    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->SetBound_Disp(iPoint, iDim, values[iDim]);
-  }
-}
-
-vector<vector<passivedouble>> CDriverBase::GetMarkerVertexNormals(unsigned short iMarker, bool normalize) const {
-  const auto nVertex = GetNumberMarkerNodes(iMarker);
-
-  vector<vector<passivedouble>> values;
-
-  for (auto iVertex = 0ul; iVertex < nVertex; iVertex++) {
-    values.push_back(GetMarkerVertexNormals(iMarker, iVertex, normalize = normalize));
+    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->SetBound_Vel(iPoint, iDim, values[iDim]);
   }
-
-  return values;
-}
-
-vector<passivedouble> CDriverBase::GetMarkerVertexNormals(unsigned short iMarker, unsigned long iVertex,
-                                                          bool normalize) const {
-  if (iVertex >= GetNumberMarkerNodes(iMarker)) {
-    SU2_MPI::Error("Vertex index exceeds marker size.", CURRENT_FUNCTION);
-  }
-
-  vector<passivedouble> values(nDim, 0.0);
-
-  auto normal = main_geometry->vertex[iMarker][iVertex]->GetNormal();
-  auto area = GeometryToolbox::Norm(nDim, normal);
-
-  for (auto iDim = 0u; iDim < nDim; iDim++) {
-    if (normalize) {
-      values[iDim] = SU2_TYPE::GetValue(normal[iDim] / area);
-    } else {
-      values[iDim] = SU2_TYPE::GetValue(normal[iDim]);
-    }
-  }
-
-  return values;
 }
 
 void CDriverBase::CommunicateMeshDisplacements(void) {

From cd1e820cde0068297a2fcb08a2917eb35e151fb4 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 5 Feb 2023 15:16:45 -0800
Subject: [PATCH 175/656] 2022 -> 2023

---
 SU2_CFD/include/drivers/CDriverBase.hpp               | 2 +-
 SU2_CFD/src/drivers/CDriverBase.cpp                   | 2 +-
 SU2_DEF/include/drivers/CDeformationDriver.hpp        | 2 +-
 SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp | 2 +-
 SU2_DEF/src/drivers/CDeformationDriver.cpp            | 2 +-
 SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp     | 2 +-
 6 files changed, 6 insertions(+), 6 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index cb1c27f340d..31e5385f802 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -9,7 +9,7 @@
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index 5097fe345ec..63c6c974013 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -9,7 +9,7 @@
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser/ General Public
diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index 01eecee0df5..ecc8b46c5cb 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -9,7 +9,7 @@
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public
diff --git a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
index 534b0cddb16..ce6ed37f4c5 100644
--- a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
@@ -9,7 +9,7 @@
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 712cd8e194d..88fa39afbff 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -9,7 +9,7 @@
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser/ General Public
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index d65f150d2a9..05d57465390 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -9,7 +9,7 @@
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public

From 46fed4fc38699d1fc2a6d621eea4b53a6a6912ea Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 5 Feb 2023 16:36:40 -0800
Subject: [PATCH 176/656] fix python scripts, remove mesh solver duplication

---
 SU2_CFD/include/drivers/CDriverBase.hpp       | 12 ++--
 SU2_CFD/include/solvers/CMeshSolver.hpp       |  9 ---
 SU2_CFD/src/solvers/CMeshSolver.cpp           | 57 -------------------
 SU2_DEF/src/drivers/CDeformationDriver.cpp    |  7 ++-
 SU2_PY/FSI_tools/FSIInterface.py              | 18 +++---
 .../launch_flatPlate_rigidMotion.py           |  9 +--
 .../launch_unsteady_CHT_FlatPlate.py          |  4 --
 .../translating_NACA0012/run_su2.py           |  5 +-
 8 files changed, 27 insertions(+), 94 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index 31e5385f802..ad647f12be8 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -95,32 +95,32 @@ class CDriverBase {
   /*!
    * \brief A virtual member.
    */
-  virtual void Preprocessing(){};
+  virtual void Preprocessing(){}
 
   /*!
    * \brief A virtual member.
    */
-  virtual void Run(){};
+  virtual void Run(){}
 
   /*!
    * \brief A virtual member.
    */
-  virtual void Update(){};
+  virtual void Update(){}
 
   /*!
    * \brief A virtual member.
    */
-  virtual void Update_Legacy(){};
+  virtual void Update_Legacy(){}
 
   /*!
    * \brief A virtual member.
    */
-  virtual void Output(){};
+  virtual void Output(){}
 
   /*!
    * \brief A virtual member.
    */
-  virtual void Postprocessing(){};
+  virtual void Postprocessing(){}
 
   /*!
    * \brief Get the number of design variables.
diff --git a/SU2_CFD/include/solvers/CMeshSolver.hpp b/SU2_CFD/include/solvers/CMeshSolver.hpp
index 02152135276..713b6a086fa 100644
--- a/SU2_CFD/include/solvers/CMeshSolver.hpp
+++ b/SU2_CFD/include/solvers/CMeshSolver.hpp
@@ -132,15 +132,6 @@ class CMeshSolver final : public CFEASolver {
                   CNumerics **numerics,
                   CConfig *config) override;
 
-  /*!
-   * \brief Grid deformation using the linear elasticity equations (no multigrid).
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] numerics - Numerics used in the solution.
-   * \param[in] config - Definition of the particular problem.
-   */
-  void DeformMesh(CGeometry *geometry,
-                  CNumerics **numerics,
-                  CConfig *config) override;
   /*!
    * \brief Set the stiffness of the mesh.
    * \param[in] numerics - Numerics used in the solution.
diff --git a/SU2_CFD/src/solvers/CMeshSolver.cpp b/SU2_CFD/src/solvers/CMeshSolver.cpp
index 970a41c7892..a4753df41cd 100644
--- a/SU2_CFD/src/solvers/CMeshSolver.cpp
+++ b/SU2_CFD/src/solvers/CMeshSolver.cpp
@@ -539,63 +539,6 @@ void CMeshSolver::DeformMesh(CGeometry **geometry, CNumerics **numerics, CConfig
 
 }
 
-void CMeshSolver::DeformMesh(CGeometry *geometry, CNumerics **numerics, CConfig *config){
-
-  if (multizone) nodes->Set_BGSSolution_k();
-
-  /*--- Capture a few MPI dependencies for AD. ---*/
-  geometry->InitiateComms(geometry, config, COORDINATES);
-  geometry->CompleteComms(geometry, config, COORDINATES);
-
-  InitiateComms(geometry, config, SOLUTION);
-  CompleteComms(geometry, config, SOLUTION);
-
-  InitiateComms(geometry, config, MESH_DISPLACEMENTS);
-  CompleteComms(geometry, config, MESH_DISPLACEMENTS);
-
-  /*--- Compute the stiffness matrix, no point recording because we clear the residual. ---*/
-
-  const bool wasActive = AD::BeginPassive();
-
-  Compute_StiffMatrix(geometry, numerics, config);
-
-  AD::EndPassive(wasActive);
-
-  /*--- Clear residual (loses AD info), we do not want an incremental solution. ---*/
-  SU2_OMP_PARALLEL {
-    LinSysRes.SetValZero();
-    if (time_domain && config->GetFSI_Simulation()) LinSysSol.SetValZero();
-  }
-  END_SU2_OMP_PARALLEL
-
-  /*--- Impose boundary conditions (all of them are ESSENTIAL BC's - displacements). ---*/
-  SetBoundaryDisplacements(geometry, config, false);
-
-  /*--- Solve the linear system. ---*/
-  Solve_System(geometry, config);
-
-  SU2_OMP_PARALLEL {
-
-  /*--- Update the grid coordinates and cell volumes using the solution
-     of the linear system (usol contains the x, y, z displacements). ---*/
-  UpdateGridCoord(geometry, config);
-
-  /*--- Update the dual grid (without multigrid). ---*/
-  geometry->InitiateComms(geometry, config, COORDINATES);
-  geometry->CompleteComms(geometry, config, COORDINATES);
-
-  geometry->SetControlVolume(config, UPDATE);
-  geometry->SetBoundControlVolume(config, UPDATE);
-  geometry->SetMaxLength(config);
-
-  /*--- Check for failed deformation (negative volumes). ---*/
-  SetMinMaxVolume(geometry, config, true);
-
-  }
-  END_SU2_OMP_PARALLEL
-
-}
-
 void CMeshSolver::UpdateGridCoord(CGeometry *geometry, const CConfig *config){
 
   /*--- Update the grid coordinates using the solution of the linear system ---*/
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 88fa39afbff..b064aaf8d62 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -309,10 +309,13 @@ void CDeformationDriver::Update() {
     solver_container[iZone][INST_0][MESH_0][MESH_SOL]->SetMesh_Stiffness(numerics_container[iZone][INST_0][MESH_0][MESH_SOL], config_container[iZone]);
 
     /*--- Deform the volume grid around the new boundary locations. ---*/
-
-    solver_container[iZone][INST_0][MESH_0][MESH_SOL]->DeformMesh(geometry_container[iZone][INST_0][MESH_0],
+    /*--- Force the number of levels to be 0 because in this driver we do not build MG levels. ---*/
+    const auto nMGLevels = config_container[iZone]->GetnMGLevels();
+    config_container[iZone]->SetMGLevels(0);
+    solver_container[iZone][INST_0][MESH_0][MESH_SOL]->DeformMesh(geometry_container[iZone][INST_0],
                                                                   numerics_container[iZone][INST_0][MESH_0][MESH_SOL],
                                                                   config_container[iZone]);
+    config_container[iZone]->SetMGLevels(nMGLevels);
   }
 }
 
diff --git a/SU2_PY/FSI_tools/FSIInterface.py b/SU2_PY/FSI_tools/FSIInterface.py
index c8d3e6bd241..21f18882d13 100644
--- a/SU2_PY/FSI_tools/FSIInterface.py
+++ b/SU2_PY/FSI_tools/FSIInterface.py
@@ -300,8 +300,9 @@ def connect(self, FSI_config, FluidSolver, SolidSolver):
         # Calculate the number of halo nodes on each partition
         self.nLocalFluidInterfaceHaloNode = 0
         for iVertex in range(self.nLocalFluidInterfaceNodes):
-            if not FluidSolver.GetMarkerDomain(self.fluidInterfaceIdentifier, iVertex):
-              GlobalIndex = FluidSolver.GetMarkerNodes(self.fluidInterfaceIdentifier, iVertex)
+            iPoint = FluidSolver.GetMarkerNode(self.fluidInterfaceIdentifier, iVertex)
+            if not FluidSolver.GetNodeDomain(iPoint):
+              GlobalIndex = FluidSolver.GetNodeGlobalIndex(iPoint)
               self.FluidHaloNodeList[GlobalIndex] = iVertex
               self.nLocalFluidInterfaceHaloNode += 1
         # Calculate the number of physical (= not halo) nodes on each partition
@@ -565,12 +566,13 @@ def interfaceMapping(self,FluidSolver, SolidSolver, FSI_config):
             # Note that the fluid solver is separated in more processors outside the python script
             # thus when, from a core, we request for the vertices on the interface, we only obtain
             # those in that core
-            GlobalIndex = FluidSolver.GetMarkerNodes(self.fluidInterfaceIdentifier, iVertex)
+            iPoint = FluidSolver.GetMarkerNode(self.fluidInterfaceIdentifier, iVertex)
+            GlobalIndex = FluidSolver.GetNodeGlobalIndex(iPoint)
             if self.nDim == 2:
-                posx, posy = FluidSolver.GetMarkerInitialCoordinates(self.fluidInterfaceIdentifier, iVertex)
+                posx, posy = FluidSolver.GetInitialCoordinates(iPoint)
                 posz = 0
             else:
-                posx, posy, posz = FluidSolver.GetMarkerInitialCoordinates(self.fluidInterfaceIdentifier, iVertex)
+                posx, posy, posz = FluidSolver.GetInitialCoordinates(iPoint)
             if GlobalIndex not in self.FluidHaloNodeList[myid].keys():
               fluidIndexing_temp[GlobalIndex] = self.__getGlobalIndex('fluid', myid, localIndex)
               self.localFluidInterface_array_X_init[localIndex] = posx
@@ -1460,7 +1462,7 @@ def getFluidInterfaceNodalForce(self, FSI_config, FluidSolver):
 
         # --- Get the fluid interface loads from the fluid solver and directly fill the corresponding PETSc vector ---
         for iVertex in range(self.nLocalFluidInterfaceNodes):
-            GlobalIndex = FluidSolver.GetMarkerNodes(self.fluidInterfaceIdentifier, iVertex)
+            GlobalIndex = FluidSolver.GetNodeGlobalIndex(FluidSolver.GetMarkerNode(self.fluidInterfaceIdentifier, iVertex))
             if GlobalIndex not in self.FluidHaloNodeList[myid].keys():
               loadX, loadY, loadZ = FluidSolver.GetFlowLoad(self.fluidInterfaceIdentifier, iVertex)
               iGlobalVertex = self.__getGlobalIndex('fluid', myid, localIndex)
@@ -1490,7 +1492,7 @@ def setFluidInterfaceVarCoord(self, FluidSolver):
         # --- Send the new fluid interface position to the fluid solver (on each partition, halo nodes included) ---
         localIndex = 0
         for iVertex in range(self.nLocalFluidInterfaceNodes):
-            GlobalIndex = FluidSolver.GetMarkerNodes(self.fluidInterfaceIdentifier, iVertex)
+            GlobalIndex = FluidSolver.GetNodeGlobalIndex(FluidSolver.GetMarkerNode(self.fluidInterfaceIdentifier, iVertex))
             if GlobalIndex in self.FluidHaloNodeList[myid].keys():
               DispX, DispY, DispZ = self.haloNodesDisplacements[GlobalIndex]
               FluidSolver.SetMarkerDisplacements(self.fluidInterfaceIdentifier, int(iVertex), np.array([DispX, DispY, DispZ]))
@@ -2151,7 +2153,7 @@ def MapModes(self, FSI_config, FluidSolver, SolidSolver):
             nz = 0
         else:
             nx, ny, nz = FluidSolver.GetMarkerVertexNormals(self.fluidInterfaceIdentifier, iVertex, False)
-        GlobalIndex = FluidSolver.GetMarkerNodes(self.fluidInterfaceIdentifier, iVertex)
+        GlobalIndex = FluidSolver.GetNodeGlobalIndex(FluidSolver.GetMarkerNode(self.fluidInterfaceIdentifier, iVertex))
         nodeNormals[GlobalIndex] = [nx, ny, nz]
 
       nodeNormals = self.comm.gather(nodeNormals, root=self.rootProcess)
diff --git a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
index fe28b4ac8dd..e3e05f7dcc1 100755
--- a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
+++ b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
@@ -87,13 +87,9 @@ def main():
 
   # Number of vertices on the specified marker (per rank)
   nVertex_MovingMarker = 0         #total number of vertices (physical + halo)
-  nVertex_MovingMarker_HALO = 0    #number of halo vertices
-  nVertex_MovingMarker_PHYS = 0    #number of physical vertices
 
   if MovingMarkerID != None:
-    nVertex_MovingMarker = SU2Driver.GetNumberMarkerNodes(MovingMarkerID)
-    nVertex_MovingMarker_HALO = SU2Driver.GetNumberMarkerHaloNodes(MovingMarkerID)
-    nVertex_MovingMarker_PHYS = nVertex_MovingMarker - nVertex_MovingMarker_HALO
+    nVertex_MovingMarker = SU2Driver.GetNumberMarkerNodes(MovingMarkerID)\
 
   # Retrieve some control parameters from the driver
   deltaT = SU2Driver.GetUnsteady_TimeStep()
@@ -105,7 +101,8 @@ def main():
   CoordX = np.zeros(nVertex_MovingMarker)
   CoordY = np.zeros(nVertex_MovingMarker)
   for iVertex in range(nVertex_MovingMarker):
-    CoordX[iVertex], CoordY[iVertex] = SU2Driver.GetMarkerInitialCoordinates(MovingMarkerID, iVertex)
+    iPoint = SU2Driver.GetMarkerNode(MovingMarkerID, iVertex)
+    CoordX[iVertex], CoordY[iVertex] = SU2Driver.GetInitialCoordinates(iPoint)
 
   # Time loop is defined in Python so that we have acces to SU2 functionalities at each time step
   if rank == 0:
diff --git a/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py b/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
index f0e692eea73..37b8ed66914 100755
--- a/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
+++ b/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
@@ -86,13 +86,9 @@ def main():
 
   # Number of vertices on the specified marker (per rank)
   nVertex_CHTMarker = 0         # total number of vertices (physical + halo)
-  nVertex_CHTMarker_HALO = 0    # number of halo vertices
-  nVertex_CHTMarker_PHYS = 0    # number of physical vertices
 
   if CHTMarkerID != None:
     nVertex_CHTMarker = SU2Driver.GetNumberMarkerNodes(CHTMarkerID)
-    nVertex_CHTMarker_HALO = SU2Driver.GetNumberMarkerHaloNodes(CHTMarkerID)
-    nVertex_CHTMarker_PHYS = nVertex_CHTMarker - nVertex_CHTMarker_HALO
 
   # Retrieve some control parameters from the driver
   deltaT = SU2Driver.GetUnsteady_TimeStep()
diff --git a/TestCases/py_wrapper/translating_NACA0012/run_su2.py b/TestCases/py_wrapper/translating_NACA0012/run_su2.py
index c8b114410ec..7d638c92b08 100644
--- a/TestCases/py_wrapper/translating_NACA0012/run_su2.py
+++ b/TestCases/py_wrapper/translating_NACA0012/run_su2.py
@@ -30,7 +30,7 @@ def run_solver(self):
         self.FluidSolver.Run()
         self.FluidSolver.Postprocess()
         # write outputs
-        self.FluidSolver.Monitor(0) 
+        self.FluidSolver.Monitor(0)
         self.FluidSolver.Output(0)
         self.comm.barrier()
 
@@ -50,7 +50,8 @@ def save_forces(self):
             n_vertices = self.FluidSolver.GetNumberMarkerNodes(solver_marker_id)
             for i_vertex in range(n_vertices):
                 fxyz = self.FluidSolver.GetFlowLoad(solver_marker_id, i_vertex)
-                GlobalIndex = self.FluidSolver.GetMarkerNodes(solver_marker_id, i_vertex)
+                iPoint = self.FluidSolver.GetMarkerNode(solver_marker_id, i_vertex)
+                GlobalIndex = self.FluidSolver.GetNodeGlobalIndex(iPoint)
                 f.write('{}, {:.2f}, {:.2f}, {:.2f}\n'.format(GlobalIndex, fxyz[0], fxyz[1], fxyz[2]))
         f.close()
 

From 2869b0ed3f8d188ebf3475a2ca20e2bad02073f6 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 6 Feb 2023 08:28:57 +0100
Subject: [PATCH 177/656] Fixed build error

---
 Common/src/containers/CFileReaderLUT.cpp      | 15 -----------
 .../Common/containers/CLookupTable_tests.cpp  | 27 -------------------
 2 files changed, 42 deletions(-)

diff --git a/Common/src/containers/CFileReaderLUT.cpp b/Common/src/containers/CFileReaderLUT.cpp
index 2f66930f902..539d60134c8 100644
--- a/Common/src/containers/CFileReaderLUT.cpp
+++ b/Common/src/containers/CFileReaderLUT.cpp
@@ -136,27 +136,12 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
 
     /*--- variable names ---*/
     if (line.compare("[Variable names]") == 0) {
-<<<<<<< HEAD
       names_var.resize(n_variables);
-<<<<<<< HEAD
-=======
-
->>>>>>> 95a84870e869ab205b5da98d0969fd732a17cf55
       for (unsigned long i = 0; i < n_variables; i++){
 
         /*--- grab a single line ---*/
         GetNextNonEmptyLine(file_stream, line);
-<<<<<<< HEAD
         names_var[i] = line.substr(line.find(":")+1); 
-=======
-        names_var.push_back(line.substr(line.find(":")+1));
->>>>>>> 95a84870e869ab205b5da98d0969fd732a17cf55
-=======
-      for (unsigned long i = 0; i < n_variables; i++) {
-        /*--- grab a single line ---*/
-        GetNextNonEmptyLine(file_stream, line);
-        names_var[i] = line.substr(line.find(":") + 1);
->>>>>>> 3088378be6c6ca596edfbcc44b2ca3272ee9319f
       }
     }
 
diff --git a/UnitTests/Common/containers/CLookupTable_tests.cpp b/UnitTests/Common/containers/CLookupTable_tests.cpp
index f649fe1a2b6..e147127e96b 100644
--- a/UnitTests/Common/containers/CLookupTable_tests.cpp
+++ b/UnitTests/Common/containers/CLookupTable_tests.cpp
@@ -53,11 +53,7 @@ TEST_CASE("LUTreader", "[tabulated chemistry]") {
   su2double enth = -0.5;
   string look_up_tag = "Density";
   su2double look_up_dat;
-<<<<<<< HEAD
   look_up_table.LookUp_XY(look_up_tag, &look_up_dat, prog, enth); 
-=======
-  look_up_table.LookUp_ProgEnth(look_up_tag, &look_up_dat, prog, enth, name_CV1, name_CV2);
->>>>>>> 95a84870e869ab205b5da98d0969fd732a17cf55
   CHECK(look_up_dat == Approx(1.02));
 
   /*--- look up a single value for viscosity ---*/
@@ -65,28 +61,14 @@ TEST_CASE("LUTreader", "[tabulated chemistry]") {
   prog = 0.6;
   enth = 0.9;
   look_up_tag = "Viscosity";
-<<<<<<< HEAD
   look_up_table.LookUp_XY(look_up_tag, &look_up_dat, prog, enth); 
   CHECK(look_up_dat == Approx(0.0000674286));
 
   /* find the table limits */
   
   auto limitsEnth = look_up_table.GetTableLimitsY();
-<<<<<<< HEAD
-=======
-  look_up_table.LookUp_ProgEnth(look_up_tag, &look_up_dat, prog, enth, name_CV1, name_CV2);
-  CHECK(look_up_dat == Approx(0.0000674286));
-
-  /* find the table limits */
-
-  auto limitsEnth = look_up_table.GetTableLimitsEnth();
->>>>>>> 95a84870e869ab205b5da98d0969fd732a17cf55
-  CHECK(limitsEnth.first == Approx(-1.0));
-  CHECK(limitsEnth.second == Approx(1.0));
-=======
   CHECK(SU2_TYPE::GetValue(*limitsEnth.first) == Approx(-1.0));
   CHECK(SU2_TYPE::GetValue(*limitsEnth.second) == Approx(1.0));
->>>>>>> 3088378be6c6ca596edfbcc44b2ca3272ee9319f
 
   auto limitsProgvar = look_up_table.GetTableLimitsX();
   CHECK(SU2_TYPE::GetValue(*limitsProgvar.first) == Approx(0.0));
@@ -97,18 +79,9 @@ TEST_CASE("LUTreader", "[tabulated chemistry]") {
   prog = 1.10;
   enth = 1.1;
   look_up_tag = "Density";
-<<<<<<< HEAD
   look_up_table.LookUp_XY(look_up_tag, &look_up_dat, prog, enth); 
-<<<<<<< HEAD
-=======
-  look_up_table.LookUp_ProgEnth(look_up_tag, &look_up_dat, prog, enth, name_CV1, name_CV2);
->>>>>>> 95a84870e869ab205b5da98d0969fd732a17cf55
   CHECK(look_up_dat == Approx(1.2));
 
-=======
-  CHECK(look_up_dat == Approx(1.1738796125));
- 
->>>>>>> 3088378be6c6ca596edfbcc44b2ca3272ee9319f
 }
 
 TEST_CASE("LUTreader_3D", "[tabulated chemistry]") {

From 2e3257ec0573206abc12d2ec7af94fcbf34c5131 Mon Sep 17 00:00:00 2001
From: Nijso <bigfootedrockmidget@hotmail.com>
Date: Mon, 6 Feb 2023 09:28:46 +0100
Subject: [PATCH 178/656] Update Common/src/containers/CLookUpTable.cpp

---
 Common/src/containers/CLookUpTable.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index c58b6387c63..8844c889e46 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -806,4 +806,4 @@ bool CLookUpTable::IsInTriangle(su2double val_CV1, su2double val_CV2, unsigned l
   su2double area_2 = TriArea(tri_x_0, tri_y_0, tri_x_1, tri_y_1, val_CV1, val_CV2);
 
   return (abs(area_tri - (area_0 + area_1 + area_2)) < area_tri * 1e-10);
-}
\ No newline at end of file
+}

From cab3bf5e417ca6c6dba0cf84a39409137cbefcd1 Mon Sep 17 00:00:00 2001
From: Nijso <bigfootedrockmidget@hotmail.com>
Date: Mon, 6 Feb 2023 09:28:57 +0100
Subject: [PATCH 179/656] Update
 UnitTests/Common/containers/CLookupTable_tests.cpp

---
 UnitTests/Common/containers/CLookupTable_tests.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/UnitTests/Common/containers/CLookupTable_tests.cpp b/UnitTests/Common/containers/CLookupTable_tests.cpp
index e147127e96b..b7f26b8f80e 100644
--- a/UnitTests/Common/containers/CLookupTable_tests.cpp
+++ b/UnitTests/Common/containers/CLookupTable_tests.cpp
@@ -133,4 +133,4 @@ TEST_CASE("LUTreader_3D", "[tabulated chemistry]") {
   look_up_table.LookUp_XYZ(look_up_tag, &look_up_dat, prog, enth, mfrac); 
   CHECK(look_up_dat == Approx(1.1738796125));
  
-}
\ No newline at end of file
+}

From 628f586a368408e2302c7fd4e4bb50474a450576 Mon Sep 17 00:00:00 2001
From: Nijso <bigfootedrockmidget@hotmail.com>
Date: Mon, 6 Feb 2023 09:29:12 +0100
Subject: [PATCH 180/656] Update Common/src/containers/CTrapezoidalMap.cpp

---
 Common/src/containers/CTrapezoidalMap.cpp | 1 -
 1 file changed, 1 deletion(-)

diff --git a/Common/src/containers/CTrapezoidalMap.cpp b/Common/src/containers/CTrapezoidalMap.cpp
index 87a112f6086..1f5f6bf1674 100644
--- a/Common/src/containers/CTrapezoidalMap.cpp
+++ b/Common/src/containers/CTrapezoidalMap.cpp
@@ -128,7 +128,6 @@ CTrapezoidalMap::CTrapezoidalMap(const su2double* samples_x, const su2double* sa
 }
 
 unsigned long CTrapezoidalMap::GetTriangle(su2double val_x, su2double val_y) {
-  // unsigned long CTrapezoidalMap::GetTriangle(su2double val_x, su2double val_y) const {
   /* find x band in which val_x sits */
   pair<unsigned long, unsigned long> band = GetBand(val_x);
 

From cf5500966aa27f9ba88aead392631070811c5bae Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 6 Feb 2023 11:05:04 +0100
Subject: [PATCH 181/656] Removed LookUp_ProgEnth aliases from CLookUpTable

---
 Common/include/containers/CLookUpTable.hpp    | 42 -------------------
 Common/src/containers/CFileReaderLUT.cpp      | 21 +++++++---
 Common/src/containers/CLookUpTable.cpp        | 17 --------
 .../Common/containers/CLookupTable_tests.cpp  |  2 +-
 4 files changed, 17 insertions(+), 65 deletions(-)

diff --git a/Common/include/containers/CLookUpTable.hpp b/Common/include/containers/CLookUpTable.hpp
index 3c6e7e713d3..e2013ae4545 100644
--- a/Common/include/containers/CLookUpTable.hpp
+++ b/Common/include/containers/CLookUpTable.hpp
@@ -309,48 +309,6 @@ class CLookUpTable {
    */
   unsigned long LookUp_XY(const std::vector<std::string>& val_names_var, std::vector<su2double>& val_vars,
                           su2double val_CV1, su2double val_CV2, unsigned long i_level = 0);
-
-  /*!
-   * \brief legacy version of the 2D lookup method for 1 value of the single variable "val_name_var"
-            using controlling variable values(val_prog,val_enth).
-   * \param[in] val_name_var - string name of the variable to look up.
-   * \param[out] val_var - the stored value of the variable to look up.
-   * \param[in] val_prog - value of the progress variable.
-   * \param[in] val_enth - value of the enthalpy.
-   * \param[in] name_prog - name of the progress variable.
-   * \param[in] name_enth - name of the enthalpy variable.
-   * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
-   */
-  unsigned long LookUp_ProgEnth(const std::string& val_name_var, su2double* val_var, su2double val_prog,
-                                su2double val_enth, std::string name_prog, std::string name_enth);
-
-  /*!
-   * \brief legacy version of the 2D lookup method for 1 value for each of the variables in "val_name_var"
-            using controlling variable values(val_CV1,val_CV2).
-   * \param[in] val_name_var - vector of string names of the variables to look up.
-   * \param[out] val_vars - pointer to the vector of stored values of the variables to look up.
-   * \param[in] val_prog - value of the progress variable.
-   * \param[in] val_enth - value of the enthalpy.
-   * \param[in] name_prog - name of the progress variable.
-   * \param[in] name_enth - name of the enthalpy variable.
-   * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
-   */
-  unsigned long LookUp_ProgEnth(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars,
-                                su2double val_prog, su2double val_enth, std::string name_prog, std::string name_enth);
-
-  /*!
-   * \brief legacy version of the 2D lookup method for 1 value for each of the variables in "val_name_var"
-            using controlling variable values(val_CV1,val_CV2).
-   * \param[in] val_name_var - vector of string names of the variables to look up.
-   * \param[out] val_vars - pointer to the vector of stored values of the variables to look up.
-   * \param[in] val_prog - value of the progress variable.
-   * \param[in] val_enth - value of the enthalpy.
-   * \param[in] name_prog - name of the progress variable.
-   * \param[in] name_enth - name of the enthalpy variable.
-   * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
-   */
-  unsigned long LookUp_ProgEnth(const std::vector<std::string>& val_names_var, std::vector<su2double>& val_vars,
-                                su2double val_CV1, su2double val_CV2, std::string name_prog, std::string name_enth);
   /*!
    * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_CV1,val_CV2,val_z).
    * \param[in] val_name_var - string name of the variable to look up.
diff --git a/Common/src/containers/CFileReaderLUT.cpp b/Common/src/containers/CFileReaderLUT.cpp
index 539d60134c8..1b27acfd82c 100644
--- a/Common/src/containers/CFileReaderLUT.cpp
+++ b/Common/src/containers/CFileReaderLUT.cpp
@@ -26,10 +26,11 @@
  */
 
 #include "../../Common/include/containers/CFileReaderLUT.hpp"
-#include "../../Common/include/option_structure.hpp"
-#include "../../Common/include/parallelization/mpi_structure.hpp"
+
 #include "../../../Common/include/linear_algebra/blas_structure.hpp"
 #include "../../../Common/include/toolboxes/CSquareMatrixCM.hpp"
+#include "../../Common/include/option_structure.hpp"
+#include "../../Common/include/parallelization/mpi_structure.hpp"
 
 using namespace std;
 
@@ -128,6 +129,17 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
         table_levels[i_level] = stod(line);
       }
     }
+
+    /*--- Checking whether table levels are ordered and appearance of duplicates ---*/
+    for (auto i_level = 0; i_level < n_levels - 1; i_level++) {
+      if (table_levels[i_level] > table_levels[i_level + 1])
+        SU2_MPI::Error("Table levels are not provided in ascending order.", CURRENT_FUNCTION);
+    }
+    const auto duplicate = adjacent_find(table_levels.begin(), table_levels.end());
+    if (duplicate != table_levels.end())
+      SU2_MPI::Error("Table level " + to_string(*duplicate) + " appears more than once in the look-up table",
+                     CURRENT_FUNCTION);
+
     /*--- number of variables in LUT ---*/
     if (line.compare("[Number of variables]") == 0) {
       GetNextNonEmptyLine(file_stream, line);
@@ -137,11 +149,10 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
     /*--- variable names ---*/
     if (line.compare("[Variable names]") == 0) {
       names_var.resize(n_variables);
-      for (unsigned long i = 0; i < n_variables; i++){
-
+      for (unsigned long i = 0; i < n_variables; i++) {
         /*--- grab a single line ---*/
         GetNextNonEmptyLine(file_stream, line);
-        names_var[i] = line.substr(line.find(":")+1); 
+        names_var[i] = line.substr(line.find(":") + 1);
       }
     }
 
diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index 8844c889e46..943bc6e633a 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -617,23 +617,6 @@ unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vecto
   return exit_code;
 }
 
-unsigned long CLookUpTable::LookUp_ProgEnth(const std::string& val_name_var, su2double* val_var, su2double val_prog,
-                                            su2double val_enth, std::string name_prog, std::string name_enth) {
-  return LookUp_XY(val_name_var, val_var, val_prog, val_enth);
-}
-
-unsigned long CLookUpTable::LookUp_ProgEnth(const std::vector<std::string>& val_names_var,
-                                            std::vector<su2double*>& val_vars, su2double val_prog, su2double val_enth,
-                                            std::string name_prog, std::string name_enth) {
-  return LookUp_XY(val_names_var, val_vars, val_prog, val_enth);
-}
-
-unsigned long CLookUpTable::LookUp_ProgEnth(const std::vector<std::string>& val_names_var,
-                                            std::vector<su2double>& val_vars, su2double val_prog, su2double val_enth,
-                                            std::string name_prog, std::string name_enth) {
-  return LookUp_XY(val_names_var, val_vars, val_prog, val_enth);
-}
-
 unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vector<su2double*>& val_vars,
                                       su2double val_CV1, su2double val_CV2, unsigned long i_level) {
   unsigned long exit_code = 1;
diff --git a/UnitTests/Common/containers/CLookupTable_tests.cpp b/UnitTests/Common/containers/CLookupTable_tests.cpp
index b7f26b8f80e..11a1f085187 100644
--- a/UnitTests/Common/containers/CLookupTable_tests.cpp
+++ b/UnitTests/Common/containers/CLookupTable_tests.cpp
@@ -80,7 +80,7 @@ TEST_CASE("LUTreader", "[tabulated chemistry]") {
   enth = 1.1;
   look_up_tag = "Density";
   look_up_table.LookUp_XY(look_up_tag, &look_up_dat, prog, enth); 
-  CHECK(look_up_dat == Approx(1.2));
+  CHECK(look_up_dat == Approx(1.1738796125));
 
 }
 

From 85281448d4fe805e9f6e769fda9d36445e5d057c Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 6 Feb 2023 11:29:23 +0100
Subject: [PATCH 182/656] Fixed build error

---
 Common/src/containers/CFileReaderLUT.cpp | 9 ++++-----
 1 file changed, 4 insertions(+), 5 deletions(-)

diff --git a/Common/src/containers/CFileReaderLUT.cpp b/Common/src/containers/CFileReaderLUT.cpp
index 1b27acfd82c..9e975b3d79f 100644
--- a/Common/src/containers/CFileReaderLUT.cpp
+++ b/Common/src/containers/CFileReaderLUT.cpp
@@ -131,14 +131,13 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
     }
 
     /*--- Checking whether table levels are ordered and appearance of duplicates ---*/
-    for (auto i_level = 0; i_level < n_levels - 1; i_level++) {
+    for (auto i_level = 0u; i_level < n_levels - 1; i_level++) {
       if (table_levels[i_level] > table_levels[i_level + 1])
         SU2_MPI::Error("Table levels are not provided in ascending order.", CURRENT_FUNCTION);
     }
-    const auto duplicate = adjacent_find(table_levels.begin(), table_levels.end());
-    if (duplicate != table_levels.end())
-      SU2_MPI::Error("Table level " + to_string(*duplicate) + " appears more than once in the look-up table",
-                     CURRENT_FUNCTION);
+    auto duplicate = adjacent_find(table_levels.begin(), table_levels.end()) != table_levels.end();
+    if (duplicate)
+      SU2_MPI::Error("Duplicate table levels are present in LUT file", CURRENT_FUNCTION);
 
     /*--- number of variables in LUT ---*/
     if (line.compare("[Number of variables]") == 0) {

From 69a432fe30e4d5ffd377e460381a73471e384e7b Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 6 Feb 2023 14:08:13 +0100
Subject: [PATCH 183/656] Fixed bug with table level checks for 3D tables

---
 Common/src/containers/CFileReaderLUT.cpp       | 18 ++++++++++--------
 .../Common/containers/CLookupTable_tests.cpp   |  4 ++--
 2 files changed, 12 insertions(+), 10 deletions(-)

diff --git a/Common/src/containers/CFileReaderLUT.cpp b/Common/src/containers/CFileReaderLUT.cpp
index 9e975b3d79f..d93ef5989fa 100644
--- a/Common/src/containers/CFileReaderLUT.cpp
+++ b/Common/src/containers/CFileReaderLUT.cpp
@@ -128,16 +128,18 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
         GetNextNonEmptyLine(file_stream, line);
         table_levels[i_level] = stod(line);
       }
-    }
 
-    /*--- Checking whether table levels are ordered and appearance of duplicates ---*/
-    for (auto i_level = 0u; i_level < n_levels - 1; i_level++) {
-      if (table_levels[i_level] > table_levels[i_level + 1])
-        SU2_MPI::Error("Table levels are not provided in ascending order.", CURRENT_FUNCTION);
+      /*--- Checking whether table levels are ordered and appearance of duplicates ---*/
+      for (auto i_level = 0u; i_level < n_levels - 1; i_level++) {
+        if (table_levels[i_level] > table_levels[i_level + 1])
+          SU2_MPI::Error("Table levels are not provided in ascending order.", CURRENT_FUNCTION);
+      }
+      auto duplicate = adjacent_find(table_levels.begin(), table_levels.end()) != table_levels.end();
+      if (duplicate)
+        SU2_MPI::Error("Duplicate table levels are present in LUT file", CURRENT_FUNCTION);
     }
-    auto duplicate = adjacent_find(table_levels.begin(), table_levels.end()) != table_levels.end();
-    if (duplicate)
-      SU2_MPI::Error("Duplicate table levels are present in LUT file", CURRENT_FUNCTION);
+
+    
 
     /*--- number of variables in LUT ---*/
     if (line.compare("[Number of variables]") == 0) {
diff --git a/UnitTests/Common/containers/CLookupTable_tests.cpp b/UnitTests/Common/containers/CLookupTable_tests.cpp
index 11a1f085187..0e040b01ffe 100644
--- a/UnitTests/Common/containers/CLookupTable_tests.cpp
+++ b/UnitTests/Common/containers/CLookupTable_tests.cpp
@@ -40,7 +40,7 @@ TEST_CASE("LUTreader", "[tabulated chemistry]") {
 
   /*--- smaller and trivial lookup table ---*/
 
-  CLookUpTable look_up_table("src/SU2/UnitTests/Common/containers/lookuptable.drg","ProgressVariable","EnthalpyTot");
+  CLookUpTable look_up_table("/home/evert/Documents/TU_Delft_administratie/PhD/SU2_general_tables/SU2/UnitTests/Common/containers/lookuptable.drg","ProgressVariable","EnthalpyTot");
 
   /*--- string names of the controlling variables ---*/
 
@@ -88,7 +88,7 @@ TEST_CASE("LUTreader_3D", "[tabulated chemistry]") {
 
   /*--- smaller and trivial lookup table ---*/
   
-  CLookUpTable look_up_table("src/SU2/UnitTests/Common/containers/lookuptable_3D.drg","ProgressVariable","EnthalpyTot");
+  CLookUpTable look_up_table("/home/evert/Documents/TU_Delft_administratie/PhD/SU2_general_tables/SU2/UnitTests/Common/containers/lookuptable_3D.drg","ProgressVariable","EnthalpyTot");
 
   /*--- string names of the controlling variables ---*/
 

From 9a7f0627247a432cbecda6914be508e1d05a22ae Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 6 Feb 2023 14:09:02 +0100
Subject: [PATCH 184/656] Fixed paths for look-up table tests

---
 UnitTests/Common/containers/CLookupTable_tests.cpp | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/UnitTests/Common/containers/CLookupTable_tests.cpp b/UnitTests/Common/containers/CLookupTable_tests.cpp
index 0e040b01ffe..11a1f085187 100644
--- a/UnitTests/Common/containers/CLookupTable_tests.cpp
+++ b/UnitTests/Common/containers/CLookupTable_tests.cpp
@@ -40,7 +40,7 @@ TEST_CASE("LUTreader", "[tabulated chemistry]") {
 
   /*--- smaller and trivial lookup table ---*/
 
-  CLookUpTable look_up_table("/home/evert/Documents/TU_Delft_administratie/PhD/SU2_general_tables/SU2/UnitTests/Common/containers/lookuptable.drg","ProgressVariable","EnthalpyTot");
+  CLookUpTable look_up_table("src/SU2/UnitTests/Common/containers/lookuptable.drg","ProgressVariable","EnthalpyTot");
 
   /*--- string names of the controlling variables ---*/
 
@@ -88,7 +88,7 @@ TEST_CASE("LUTreader_3D", "[tabulated chemistry]") {
 
   /*--- smaller and trivial lookup table ---*/
   
-  CLookUpTable look_up_table("/home/evert/Documents/TU_Delft_administratie/PhD/SU2_general_tables/SU2/UnitTests/Common/containers/lookuptable_3D.drg","ProgressVariable","EnthalpyTot");
+  CLookUpTable look_up_table("src/SU2/UnitTests/Common/containers/lookuptable_3D.drg","ProgressVariable","EnthalpyTot");
 
   /*--- string names of the controlling variables ---*/
 

From 2c44308e77d6f310d047623fd7c5346d14cf9c88 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 6 Feb 2023 15:44:26 +0100
Subject: [PATCH 185/656] Update disc_adj_fea serial regression AD values.

---
 TestCases/serial_regression_AD.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/serial_regression_AD.py b/TestCases/serial_regression_AD.py
index c3d0b926e74..ae80f972e91 100644
--- a/TestCases/serial_regression_AD.py
+++ b/TestCases/serial_regression_AD.py
@@ -187,7 +187,7 @@ def main():
     discadj_fea.cfg_dir   = "disc_adj_fea"
     discadj_fea.cfg_file  = "configAD_fem.cfg"
     discadj_fea.test_iter = 4
-    discadj_fea.test_vals         = [-2.849531, -3.238474, -3.6413e-04, -8.7087] #last 4 columns
+    discadj_fea.test_vals         = [-2.849844, -3.238713, -3.6413e-04, -8.7087] #last 4 columns
     discadj_fea.test_vals_aarch64 = [-2.849570, -3.238519, -3.6413e-04, -8.7087] #last 4 columns
     test_list.append(discadj_fea)
 

From dc52190b97b445e4d5d59ba2887f3cae9626fdf0 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 6 Feb 2023 19:02:58 +0100
Subject: [PATCH 186/656] Update disc_adj_fea parallel regression AD values.

---
 TestCases/parallel_regression_AD.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index a24bfe5d844..b65fc7657be 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -242,7 +242,7 @@ def main():
     discadj_fea.cfg_dir   = "disc_adj_fea"
     discadj_fea.cfg_file  = "configAD_fem.cfg"
     discadj_fea.test_iter = 4
-    discadj_fea.test_vals         = [-2.849774, -3.238669, -0.000364, -8.708700] #last 4 columns
+    discadj_fea.test_vals         = [-2.849453, -3.238429, -0.000364, -8.708700] #last 4 columns
     discadj_fea.test_vals_aarch64 = [-2.849726, -3.238594, -0.000364, -8.708700] #last 4 columns
     test_list.append(discadj_fea)
 

From 747225f7712424bb0bdabc33cbfd7dbea6f9b7c1 Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Tue, 7 Feb 2023 08:42:28 -0500
Subject: [PATCH 187/656] remove iterators from member function

---
 Docs/docmain.hpp                                 | 2 +-
 SU2_CFD/include/numerics/NEMO/NEMO_diffusion.hpp | 2 +-
 SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp     | 2 +-
 TestCases/nicf/coolprop/fluidModel.cfg           | 2 +-
 TestCases/nicf/coolprop/transportModel.cfg       | 2 +-
 legacy/configure.ac                              | 2 +-
 legacy/preconfigure.py                           | 2 +-
 7 files changed, 7 insertions(+), 7 deletions(-)

diff --git a/Docs/docmain.hpp b/Docs/docmain.hpp
index 1380c050559..5ea00d86ab4 100644
--- a/Docs/docmain.hpp
+++ b/Docs/docmain.hpp
@@ -9,7 +9,7 @@
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public
diff --git a/SU2_CFD/include/numerics/NEMO/NEMO_diffusion.hpp b/SU2_CFD/include/numerics/NEMO/NEMO_diffusion.hpp
index 5a8a10c128a..88701d0c79d 100644
--- a/SU2_CFD/include/numerics/NEMO/NEMO_diffusion.hpp
+++ b/SU2_CFD/include/numerics/NEMO/NEMO_diffusion.hpp
@@ -94,7 +94,7 @@ class CAvgGrad_NEMO : public CNEMONumerics {
  */
 class CAvgGradCorrected_NEMO : public CNEMONumerics {
 private:
-  unsigned short iDim, iVar,
+  unsigned short
   nPrimVar, nPrimVarGrad;       /*!< \brief Iterators in dimension an variable. */
   su2double
   *Mean_PrimVar,                /*!< \brief Mean primitive variables. */
diff --git a/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp b/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
index cc64e14d1e2..bb9874c1c06 100644
--- a/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
+++ b/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
@@ -293,7 +293,7 @@ CNumerics::ResidualType<> CAvgGradCorrected_NEMO::ComputeResidual(const CConfig
     Mean_PrimVar[iVar] = 0.5*(PrimVar_i[iVar]+PrimVar_j[iVar]);
   }
   for (auto iVar = nSpecies; iVar < nPrimVarGrad; iVar++) {
-    for (iDim = 0; iDim < nDim; iDim++) {
+    for (auto iDim = 0; iDim < nDim; iDim++) {
       Mean_GradPrimVar[iVar][iDim] = 0.5*(PrimVar_Grad_i[iVar][iDim] +
                                           PrimVar_Grad_j[iVar][iDim]);
     }
diff --git a/TestCases/nicf/coolprop/fluidModel.cfg b/TestCases/nicf/coolprop/fluidModel.cfg
index 44df7a39118..bc4e3c5bb53 100644
--- a/TestCases/nicf/coolprop/fluidModel.cfg
+++ b/TestCases/nicf/coolprop/fluidModel.cfg
@@ -6,7 +6,7 @@
 % Author: Peng Yan, Alberto Guardone                                           %
 % Institution: Politecnico di Milano                                           %
 % Date: 2022.10.8                                                              %
-% File Version  7.5.0 Blackbird                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nicf/coolprop/transportModel.cfg b/TestCases/nicf/coolprop/transportModel.cfg
index 491073a2734..eecd0cc2790 100644
--- a/TestCases/nicf/coolprop/transportModel.cfg
+++ b/TestCases/nicf/coolprop/transportModel.cfg
@@ -6,7 +6,7 @@
 % Author: Peng Yan, Alberto Guardone                                           %
 % Institution: Politecnico di Milano                                           %
 % Date: 2022.11.26                                                             %
-% File Version  7.5.0 Blackbird                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/legacy/configure.ac b/legacy/configure.ac
index 23ea882a7e3..8ab779eb8dd 100644
--- a/legacy/configure.ac
+++ b/legacy/configure.ac
@@ -338,7 +338,7 @@ AC_MSG_RESULT([
 
 -------------------------------------------------------------------------
 |    ___ _   _ ___                                                      |
-|   / __| | | |_  )   Release 7.5.0 'Blackbird'                         |
+|   / __| | | |_  )   Release 7.5.1 'Blackbird'                         |
 |   \\__ \\ |_| |/ /                                                      |
 |   |___/\\___//___|   Suite                                             |
 |                                                                       |
diff --git a/legacy/preconfigure.py b/legacy/preconfigure.py
index 6bf254ff4cb..58cdb3863d0 100755
--- a/legacy/preconfigure.py
+++ b/legacy/preconfigure.py
@@ -553,7 +553,7 @@ def header():
 
     print('-------------------------------------------------------------------------\n'\
           '|    ___ _   _ ___                                                      | \n'\
-          '|   / __| | | |_  )   Release 7.5.0 \'Blackbird\'                         | \n'\
+          '|   / __| | | |_  )   Release 7.5.1 \'Blackbird\'                         | \n'\
           '|   \__ \ |_| |/ /                                                      | \n'\
           '|   |___/\___//___|   Pre-configuration Script                          | \n'\
           '|                                                                       | \n'\

From 9965ffbb2a561d92873d71b77ed0c164115abe6c Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Tue, 7 Feb 2023 15:32:37 -0800
Subject: [PATCH 188/656] update version numbers

---
 SU2_CFD/include/drivers/CDriverBase.hpp               | 2 +-
 SU2_CFD/src/drivers/CDriverBase.cpp                   | 2 +-
 SU2_DEF/include/drivers/CDeformationDriver.hpp        | 2 +-
 SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp | 2 +-
 SU2_DEF/src/drivers/CDeformationDriver.cpp            | 2 +-
 SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp     | 2 +-
 6 files changed, 6 insertions(+), 6 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index ad647f12be8..132ee87ca71 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -2,7 +2,7 @@
  * \file CDriverBase.hpp
  * \brief Base class for all drivers.
  * \author H. Patel, A. Gastaldi
- * \version 7.5.0 "Blackbird"
+ * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index 63c6c974013..95d755c1e59 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -2,7 +2,7 @@
  * \file CDriverBase.hpp
  * \brief Base class template for all drivers.
  * \author H. Patel, A. Gastaldi
- * \version 7.5.0 "Blackbird"
+ * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index ecc8b46c5cb..a562a07c1a5 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -2,7 +2,7 @@
  * \file CDeformationDriver.hpp
  * \brief Headers of the main subroutines for driving the mesh deformation.
  * \author A. Gastaldi, H. Patel
- * \version 7.5.0 "Blackbird"
+ * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
index ce6ed37f4c5..6b28f072b98 100644
--- a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjDeformationDriver.cpp
  * \brief Headers of the main subroutines for driving the projection of sensitivities.
  * \author T. Economon, H. Kline, R. Sanchez, A. Gastaldi, H. Patel
- * \version 7.5.0 "Blackbird"
+ * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index b064aaf8d62..856450217c2 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -2,7 +2,7 @@
  * \file CDeformationDriver.cpp
  * \brief Main subroutines for driving the mesh deformation.
  * \author A. Gastaldi, H. Patel
- * \version 7.5.0 "Blackbird"
+ * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index 05d57465390..25ae73f9abd 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjDeformationDriver.cpp
  * \brief Main subroutines for driving the projection of sensitivities.
  * \author T. Economon, H. Kline, R. Sanchez, A. Gastaldi, H. Patel
- * \version 7.5.0 "Blackbird"
+ * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *

From 4907fc5f0984e9300c614534a98d0854e53fd830 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Wed, 8 Feb 2023 18:02:42 +0100
Subject: [PATCH 189/656] pulled develop

---
 Common/include/CConfig.hpp                    |  59 +-
 Common/include/option_structure.hpp           |   6 -
 Common/src/CConfig.cpp                        | 238 +++-----
 SU2_CFD/include/numerics/heat.hpp             | 102 ++--
 SU2_CFD/obj/Makefile.am                       |   1 -
 SU2_CFD/src/drivers/CDriver.cpp               |  23 +-
 SU2_CFD/src/meson.build                       |   3 +-
 SU2_CFD/src/numerics/flow/flow_sources.cpp    | 101 +++-
 SU2_CFD/src/numerics/heat.cpp                 | 202 -------
 SU2_CFD/src/solvers/CNEMOEulerSolver.cpp      | 524 ++++++++----------
 .../naca0012/inv_NACA0012_discadj.cfg         |   2 +-
 11 files changed, 502 insertions(+), 759 deletions(-)
 delete mode 100644 SU2_CFD/src/numerics/heat.cpp

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index 78921b8a790..24facfd8f3d 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -125,6 +125,7 @@ class CConfig {
   Low_Mach_Precon,          /*!< \brief Flag to know if we are using a low Mach number preconditioner. */
   Low_Mach_Corr,            /*!< \brief Flag to know if we are using a low Mach number correction. */
   GravityForce,             /*!< \brief Flag to know if the gravity force is incuded in the formulation. */
+  VorticityConfinement,     /*!< \brief Flag to know if the Vorticity Confinement is included in the formulation. */
   SubsonicEngine,           /*!< \brief Engine intake subsonic region. */
   Frozen_Visc_Cont,         /*!< \brief Flag for cont. adjoint problem with/without frozen viscosity. */
   Frozen_Visc_Disc,         /*!< \brief Flag for disc. adjoint problem with/without frozen viscosity. */
@@ -147,6 +148,7 @@ class CConfig {
   su2double dCMy_dCL;          /*!< \brief Fixed Cl mode derivate. */
   su2double dCMz_dCL;          /*!< \brief Fixed Cl mode derivate. */
   su2double CL_Target;         /*!< \brief Fixed Cl mode Target Cl. */
+  su2double Confinement_Param; /*!< \brief Confinement paramenter for Vorticity Confinement method. */
   TIME_MARCHING TimeMarching;        /*!< \brief Steady or unsteady (time stepping or dual time stepping) computation. */
   unsigned short Dynamic_Analysis;   /*!< \brief Static or dynamic structural analysis. */
   su2double FixAzimuthalLine;        /*!< \brief Fix an azimuthal line due to misalignments of the nearfield. */
@@ -284,7 +286,6 @@ class CConfig {
   su2double *Inlet_Temperature;              /*!< \brief Specified temperatures for a supersonic inlet boundaries. */
   su2double *Inlet_Pressure;                 /*!< \brief Specified static pressures for supersonic inlet boundaries. */
   su2double **Inlet_Velocity;                /*!< \brief Specified flow velocity vectors for supersonic inlet boundaries. */
-  su2double **Inlet_MassFrac;                /*!< \brief Specified Mass fraction vectors for supersonic inlet boundaries (NEMO solver). */
   su2double **Inlet_SpeciesVal;              /*!< \brief Specified species vector for inlet boundaries. */
   su2double **Inlet_TurbVal;                 /*!< \brief Specified turbulent intensity and viscosity ratio for inlet boundaries. */
   su2double *EngineInflow_Target;            /*!< \brief Specified fan face targets for nacelle boundaries. */
@@ -496,6 +497,7 @@ class CConfig {
   Kind_SlopeLimit_Turb,         /*!< \brief Slope limiter for the turbulence equation.*/
   Kind_SlopeLimit_AdjTurb,      /*!< \brief Slope limiter for the adjoint turbulent equation.*/
   Kind_SlopeLimit_AdjFlow,      /*!< \brief Slope limiter for the adjoint equation.*/
+  Kind_SlopeLimit_Heat,         /*!< \brief Slope limiter for the adjoint equation.*/
   Kind_SlopeLimit_Species;      /*!< \brief Slope limiter for the species equation.*/
   unsigned short Kind_FluidModel,  /*!< \brief Kind of the Fluid Model: Ideal, van der Waals, etc. */
   Kind_InitOption,                 /*!< \brief Kind of Init option to choose if initializing with Reynolds number or with thermodynamic conditions   */
@@ -553,6 +555,7 @@ class CConfig {
   Kind_Centered_Turb,           /*!< \brief Centered scheme for the turbulence model. */
   Kind_Centered_AdjTurb,        /*!< \brief Centered scheme for the adjoint turbulence model. */
   Kind_Centered_Species,        /*!< \brief Centered scheme for the species model. */
+  Kind_Centered_Heat,           /*!< \brief Centered scheme for the heat transfer model. */
   Kind_Centered_Template;       /*!< \brief Centered scheme for the template model. */
 
 
@@ -569,6 +572,7 @@ class CConfig {
   Kind_Upwind_Turb,             /*!< \brief Upwind scheme for the turbulence model. */
   Kind_Upwind_AdjTurb,          /*!< \brief Upwind scheme for the adjoint turbulence model. */
   Kind_Upwind_Species,          /*!< \brief Upwind scheme for the species model. */
+  Kind_Upwind_Heat,             /*!< \brief Upwind scheme for the heat transfer model. */
   Kind_Upwind_Template;         /*!< \brief Upwind scheme for the template model. */
 
   bool MUSCL,              /*!< \brief MUSCL scheme .*/
@@ -604,7 +608,6 @@ class CConfig {
   INLET_TYPE Kind_Inlet;
   INLET_TYPE *Kind_Inc_Inlet;
   INC_OUTLET_TYPE *Kind_Inc_Outlet;
-  WALL_TYPE *Kind_Wall;            /*!< \brief Type of wall treatment. */
   unsigned short nWall_Types;      /*!< \brief Number of wall treatment types listed. */
   unsigned short nInc_Inlet;       /*!< \brief Number of inlet boundary treatment types listed. */
   unsigned short nInc_Outlet;      /*!< \brief Number of inlet boundary treatment types listed. */
@@ -634,8 +637,6 @@ class CConfig {
   Kappa_1st_Flow,           /*!< \brief Lax 1st order dissipation coefficient for flow equations (coarse multigrid levels). */
   Kappa_2nd_Flow,           /*!< \brief JST 2nd order dissipation coefficient for flow equations. */
   Kappa_4th_Flow,           /*!< \brief JST 4th order dissipation coefficient for flow equations. */
-  Kappa_2nd_Heat,           /*!< \brief 2nd order dissipation coefficient for heat equation. */
-  Kappa_4th_Heat,           /*!< \brief 4th order dissipation coefficient for heat equation. */
   Cent_Jac_Fix_Factor,              /*!< \brief Multiply the dissipation contribution to the Jacobian of central schemes
                                                 by this factor to make the global matrix more diagonal dominant. */
   Cent_Inc_Jac_Fix_Factor;          /*!< \brief Multiply the dissipation contribution to the Jacobian of incompressible central schemes */
@@ -1107,7 +1108,6 @@ class CConfig {
   rampRotFrame_coeff[3], /*!< \brief ramp rotating frame coefficients for the COption class. */
   rampOutPres_coeff[3],  /*!< \brief ramp outlet pressure coefficients for the COption class. */
   jst_adj_coeff[2],      /*!< \brief artificial dissipation (adjoint) array for the COption class. */
-  ad_coeff_heat[2],      /*!< \brief artificial dissipation (heat) array for the COption class. */
   mesh_box_length[3],    /*!< \brief mesh box length for the COption class. */
   mesh_box_offset[3],    /*!< \brief mesh box offset for the COption class. */
   geo_loc[2],            /*!< \brief SU2_GEO section locations array for the COption class. */
@@ -1196,6 +1196,7 @@ class CConfig {
 
   /* other NEMO configure options*/
   unsigned short nSpecies_Cat_Wall,         /*!< \brief No. of species for a catalytic wall. */
+  nSpecies_inlet,                           /*!< \brief No. of species for NEMO inlet. */
   iWall_Catalytic,                          /*!< \brief Iterator over catalytic walls. */
   nWall_Catalytic;                          /*!< \brief No. of catalytic walls. */
   su2double *Gas_Composition,               /*!< \brief Initial mass fractions of flow [dimensionless]. */
@@ -1210,6 +1211,8 @@ class CConfig {
   *Wall_Catalytic;                          /*!< \brief Pointer to catalytic walls. */
   TRANSCOEFFMODEL   Kind_TransCoeffModel;   /*!< \brief Transport coefficient Model for NEMO solver. */
   su2double CatalyticEfficiency;            /*!< \brief Wall catalytic efficiency. */
+  su2double *Inlet_MassFrac;                /*!< \brief Specified Mass fraction vectors for NEMO inlet boundaries. */
+  su2double Inlet_Temperature_ve;           /*!< \brief Specified Tve for supersonic inlet boundaries (NEMO solver). */
 
   /*--- Additional species solver options ---*/
   bool Species_Clipping;           /*!< \brief Boolean that activates solution clipping for scalar transport. */
@@ -1591,6 +1594,12 @@ class CConfig {
    */
   su2double GetGamma(void) const { return Gamma; }
 
+  /*!
+   * \brief Get the value of the Confinement Parameter.
+   * \return Value of the constant: Confinement Parameter
+   */
+  su2double GetConfinement_Param(void) const { return Confinement_Param; }
+
   /*!
    * \brief Get the values of the CFL adaption parameters.
    * \return Value of CFL adaption parameter
@@ -2326,8 +2335,8 @@ class CConfig {
    * \param[in] val_kind_fem - If FEM, what kind of FEM discretization.
    */
   void SetKind_ConvNumScheme(unsigned short val_kind_convnumscheme, CENTERED val_kind_centered,
-                             UPWIND val_kind_upwind,        LIMITER val_kind_slopelimit,
-                             bool val_muscl,                        unsigned short val_kind_fem);
+                             UPWIND val_kind_upwind, LIMITER val_kind_slopelimit,
+                             bool val_muscl,  unsigned short val_kind_fem);
 
   /*!
    * \brief Get the value of limiter coefficient.
@@ -4376,7 +4385,7 @@ class CConfig {
    * \return Value of roughness.
    */
   su2double GethRoughness(void) const { return hRoughness; }
-  
+
   /*!
    * \brief Get the kind of the species model.
    * \return Kind of the species model.
@@ -4691,18 +4700,6 @@ class CConfig {
    */
   su2double GetKappa_4th_Flow(void) const { return Kappa_4th_Flow; }
 
-  /*!
-   * \brief Value of the calibrated constant for the JST method (center scheme).
-   * \return Calibrated constant for the JST-like method for the heat equations.
-   */
-  su2double GetKappa_2nd_Heat(void) const { return Kappa_2nd_Heat; }
-
-  /*!
-   * \brief Value of the calibrated constant for the JST-like method (center scheme).
-   * \return Calibrated constant for the JST-like method for the heat equation.
-   */
-  su2double GetKappa_4th_Heat(void) const { return Kappa_4th_Heat; }
-
   /*!
    * \brief Factor by which to multiply the dissipation contribution to Jacobians of central schemes.
    * \return The factor.
@@ -6047,6 +6044,12 @@ class CConfig {
    */
   bool GetGravityForce(void) const { return GravityForce; }
 
+  /*!
+   * \brief Get information about the Vorticity Confinement.
+   * \return <code>TRUE</code> if it uses Vorticity Confinement; otherwise <code>FALSE</code>.
+   */
+  bool GetVorticityConfinement(void) const { return VorticityConfinement; }
+
   /*!
    * \brief Get information about the body force.
    * \return <code>TRUE</code> if it uses a body force; otherwise <code>FALSE</code>.
@@ -6716,6 +6719,20 @@ class CConfig {
    */
   const su2double* GetInlet_Velocity(string val_index) const;
 
+  /*!
+   * \brief Get the mass fraction vector for a NEMO inlet boundary.
+   * \param[in] val_index - Index corresponding to the inlet boundary.
+   * \return The inlet velocity vector.
+   */
+  const su2double* GetInlet_MassFrac() const { return Inlet_MassFrac; }
+
+  /*!
+   * \brief Get the Tve value for a NEMO inlet boundary.
+   * \param[in] val_index - Index corresponding to the inlet boundary.
+   * \return The inlet velocity vector.
+   */
+  su2double GetInlet_Temperature_ve() const { return Inlet_Temperature_ve; }
+
   /*!
    * \brief Get the total pressure at an inlet boundary.
    * \param[in] val_index - Index corresponding to the inlet boundary.
@@ -6988,7 +7005,7 @@ class CConfig {
    * \param[in] val_index - Index corresponding to the boundary.
    * \return The wall type and roughness height.
    */
-  pair<WALL_TYPE,su2double> GetWallRoughnessProperties(string val_marker) const;
+  pair<WALL_TYPE,su2double> GetWallRoughnessProperties(const string& val_marker) const;
 
   /*!
    * \brief Get the target (pressure, massflow, etc) at an engine inflow boundary.
diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index e384ed6abd1..098c839a85e 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -534,12 +534,6 @@ enum ENUM_SPACE {
   SPACE_UPWIND = 2,    /*!< \brief Upwind convective numerical method. */
   FINITE_ELEMENT = 3   /*!< \brief Finite element convective numerical method. */
 };
-static const MapType<std::string, ENUM_SPACE> Space_Map = {
-  MakePair("NONE", NO_CONVECTIVE)
-  MakePair("SPACE_CENTERED", SPACE_CENTERED)
-  MakePair("SPACE_UPWIND", SPACE_UPWIND)
-  MakePair("FINITE_ELEMENT", FINITE_ELEMENT)
-};
 
 /*!
  * \brief Types of fluid model
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index f89fd1c6dd7..8fe7bfbc17d 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -840,7 +840,6 @@ void CConfig::SetPointersNull(void) {
   Kind_WallFunctions       = nullptr;
   IntInfo_WallFunctions    = nullptr;
   DoubleInfo_WallFunctions = nullptr;
-  Kind_Wall                = nullptr;
 
   Config_Filenames = nullptr;
 
@@ -1130,6 +1129,8 @@ void CConfig::SetConfig_Options() {
   addBoolOption("AXISYMMETRIC", Axisymmetric, false);
   /* DESCRIPTION: Add the gravity force */
   addBoolOption("GRAVITY_FORCE", GravityForce, false);
+  /* DESCRIPTION: Add the Vorticity Confinement term*/
+  addBoolOption("VORTICITY_CONFINEMENT", VorticityConfinement, false);
   /* DESCRIPTION: Apply a body force as a source term (NO, YES) */
   addBoolOption("BODY_FORCE", Body_Force, false);
   body_force[0] = 0.0; body_force[1] = 0.0; body_force[2] = 0.0;
@@ -1178,6 +1179,9 @@ void CConfig::SetConfig_Options() {
   /*!\brief DATADRIVEN_FLUID_INITIAL_ENERGY \n DESCRIPTION: Initial value for the static energy in the Newton solvers in the data-driven fluid model. \n \ingroup Config*/
   addDoubleOption("DATADRIVEN_FLUID_INITIAL_ENERGY", DataDriven_initial_energy, 1e5);
 
+  /*!\brief CONFINEMENT_PARAM \n DESCRIPTION: Input Confinement Parameter for Vorticity Confinement*/
+  addDoubleOption("CONFINEMENT_PARAM", Confinement_Param, 0.0);
+
   /*!\par CONFIG_CATEGORY: Freestream Conditions \ingroup Config*/
   /*--- Options related to freestream specification ---*/
 
@@ -1202,6 +1206,10 @@ void CConfig::SetConfig_Options() {
   addEnumOption("TRANSPORT_COEFF_MODEL", Kind_TransCoeffModel, TransCoeffModel_Map, TRANSCOEFFMODEL::WILKE);
   /* DESCRIPTION: Specify mass fraction of each species */
   addDoubleListOption("GAS_COMPOSITION", nSpecies, Gas_Composition);
+  /* DESCRIPTION: Specify mass fraction of each species for NEMO inlet*/
+  addDoubleListOption("INLET_GAS_COMPOSITION", nSpecies_inlet, Inlet_MassFrac);
+  /*!\brief INLET_TEMPERATURE_VE \n DESCRIPTION: NEMO inlet temperature_ve (K), if left 0 K, set to Ttr value \ingroup Config*/
+  addDoubleOption("INLET_TEMPERATURE_VE", Inlet_Temperature_ve, 0.0);
   /* DESCRIPTION: Specify if mixture is frozen */
   addBoolOption("FROZEN_MIXTURE", frozen, false);
   /* DESCRIPTION: Specify if there is ionization */
@@ -1902,9 +1910,6 @@ void CConfig::SetConfig_Options() {
   addDoubleArrayOption("JST_SENSOR_COEFF", 2, jst_coeff);
   /*!\brief LAX_SENSOR_COEFF \n DESCRIPTION: 1st order artificial dissipation coefficients for the Lax-Friedrichs method. \ingroup Config*/
   addDoubleOption("LAX_SENSOR_COEFF", Kappa_1st_Flow, 0.15);
-  ad_coeff_heat[0] = 0.5; ad_coeff_heat[1] = 0.02;
-  /*!\brief JST_SENSOR_COEFF_HEAT \n DESCRIPTION: 2nd and 4th order artificial dissipation coefficients for the JST method \ingroup Config*/
-  addDoubleArrayOption("JST_SENSOR_COEFF_HEAT", 2, ad_coeff_heat);
   /*!\brief USE_ACCURATE_FLUX_JACOBIANS \n DESCRIPTION: Use numerically computed Jacobians for AUSM+up(2) and SLAU(2) \ingroup Config*/
   addBoolOption("USE_ACCURATE_FLUX_JACOBIANS", Use_Accurate_Jacobians, false);
   /*!\brief CENTRAL_JACOBIAN_FIX_FACTOR \n DESCRIPTION: Improve the numerical properties (diagonal dominance) of the global Jacobian matrix, 3 to 4 is "optimum" (central schemes) \ingroup Config*/
@@ -1953,9 +1958,10 @@ void CConfig::SetConfig_Options() {
 
   /*!\brief MUSCL_FLOW \n DESCRIPTION: Check if the MUSCL scheme should be used \ingroup Config*/
   addBoolOption("MUSCL_HEAT", MUSCL_Heat, false);
-  /*!\brief CONV_NUM_METHOD_HEAT
-   *  \n DESCRIPTION: Convective numerical method \n DEFAULT: UPWIND */
-  addEnumOption("CONV_NUM_METHOD_HEAT", Kind_ConvNumScheme_Heat, Space_Map, SPACE_UPWIND);
+  /*!\brief SLOPE_LIMITER_HEAT \n DESCRIPTION: Slope limiter \n OPTIONS: See \link Limiter_Map \endlink \n DEFAULT NONE \ingroup Config*/
+  addEnumOption("SLOPE_LIMITER_HEAT", Kind_SlopeLimit_Heat, Limiter_Map, LIMITER::NONE);
+  /*!\brief CONV_NUM_METHOD_HEAT \n DESCRIPTION: Convective numerical method */
+  addConvectOption("CONV_NUM_METHOD_HEAT", Kind_ConvNumScheme_Heat, Kind_Centered_Heat, Kind_Upwind_Heat);
 
   /*!\par CONFIG_CATEGORY: Adjoint and Gradient \ingroup Config*/
   /*--- Options related to the adjoint and gradient ---*/
@@ -3553,9 +3559,20 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
 
   /*--- Set limiter for no MUSCL reconstructions ---*/
 
+  auto SetScalarDefaults = [](bool muscl, unsigned short& KindConvScheme, UPWIND& KindUpwind, LIMITER& KindLimiter) {
+    if (KindConvScheme == NO_CONVECTIVE) {
+      KindConvScheme = SPACE_UPWIND;
+      KindUpwind = UPWIND::SCALAR_UPWIND;
+    } else if (KindConvScheme == SPACE_CENTERED) {
+      SU2_MPI::Error("Centered schemes are not available for scalar transport", CURRENT_FUNCTION);
+    }
+    if (!muscl) KindLimiter = LIMITER::NONE;
+  };
+  SetScalarDefaults(MUSCL_Turb, Kind_ConvNumScheme_Turb, Kind_Upwind_Turb, Kind_SlopeLimit_Turb);
+  SetScalarDefaults(MUSCL_Heat, Kind_ConvNumScheme_Heat, Kind_Upwind_Heat, Kind_SlopeLimit_Heat);
+  SetScalarDefaults(MUSCL_Species, Kind_ConvNumScheme_Species, Kind_Upwind_Species, Kind_SlopeLimit_Species);
+
   if (!MUSCL_Flow || (Kind_ConvNumScheme_Flow == SPACE_CENTERED)) Kind_SlopeLimit_Flow = LIMITER::NONE;
-  if (!MUSCL_Turb || (Kind_ConvNumScheme_Turb == SPACE_CENTERED)) Kind_SlopeLimit_Turb = LIMITER::NONE;
-  if (!MUSCL_Species || (Kind_ConvNumScheme_Species == SPACE_CENTERED)) Kind_SlopeLimit_Species = LIMITER::NONE;
   if (!MUSCL_AdjFlow || (Kind_ConvNumScheme_AdjFlow == SPACE_CENTERED)) Kind_SlopeLimit_AdjFlow = LIMITER::NONE;
   if (!MUSCL_AdjTurb || (Kind_ConvNumScheme_AdjTurb == SPACE_CENTERED)) Kind_SlopeLimit_AdjTurb = LIMITER::NONE;
 
@@ -4388,8 +4405,6 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
   Kappa_4th_Flow = jst_coeff[1];
   Kappa_2nd_AdjFlow = jst_adj_coeff[0];
   Kappa_4th_AdjFlow = jst_adj_coeff[1];
-  Kappa_2nd_Heat = ad_coeff_heat[0];
-  Kappa_4th_Heat = ad_coeff_heat[1];
 
   /*--- Make the MG_PreSmooth, MG_PostSmooth, and MG_CorrecSmooth
    arrays consistent with nMGLevels ---*/
@@ -4905,6 +4920,18 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
     }
   }
 
+  /*--- Vorticity confinement feature currently not supported for incompressible or non-equilibrium model or axisymmetric flows. ---*/
+
+  if ((Kind_Solver == MAIN_SOLVER::INC_EULER
+    || Kind_Solver == MAIN_SOLVER::INC_NAVIER_STOKES
+    || Kind_Solver == MAIN_SOLVER::INC_RANS
+    || Kind_Solver == MAIN_SOLVER::NEMO_EULER
+    || Kind_Solver == MAIN_SOLVER::NEMO_NAVIER_STOKES
+    || Axisymmetric)
+    && VorticityConfinement) {
+    SU2_MPI::Error("Vorticity confinement feature currently not supported for incompressible or non-equilibrium model or axisymmetric flows.", CURRENT_FUNCTION);
+  }
+
   /*--- Check the coefficients for the polynomial models. ---*/
 
   if (Kind_Solver != MAIN_SOLVER::INC_EULER && Kind_Solver != MAIN_SOLVER::INC_NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::INC_RANS) {
@@ -5009,95 +5036,25 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
     Streamwise_Periodic_Temperature = false;
   }
 
-  /*--- Check that if the wall roughness array are compatible and set deafult values if needed. ---*/
-   if ((nMarker_HeatFlux > 0) || (nMarker_Isothermal > 0) || (nMarker_HeatTransfer) || (nMarker_CHTInterface > 0)) {
-
-     /*--- The total number of wall markers. ---*/
-     unsigned short nWall = nMarker_HeatFlux + nMarker_Isothermal + nMarker_HeatTransfer + nMarker_CHTInterface;
-
-     /*--- If no roughness is specified all walls are assumed to be smooth. ---*/
-     if (nRough_Wall == 0) {
-
-       nRough_Wall = nWall;
-       Roughness_Height = new su2double [nWall];
-       Kind_Wall = new WALL_TYPE [nWall];
-       for (iMarker = 0; iMarker < nMarker_HeatFlux; iMarker++) {
-         Roughness_Height[iMarker] = 0.0;
-         Kind_Wall[iMarker] = WALL_TYPE::SMOOTH;
-       }
-       for (iMarker = 0; iMarker < nMarker_Isothermal; iMarker++) {
-         Roughness_Height[nMarker_HeatFlux + iMarker] = 0.0;
-         Kind_Wall[nMarker_HeatFlux + iMarker] = WALL_TYPE::SMOOTH;
-       }
-       for (iMarker = 0; iMarker < nMarker_HeatTransfer; iMarker++) {
-         Roughness_Height[nMarker_HeatFlux + nMarker_Isothermal + iMarker] = 0.0;
-         Kind_Wall[nMarker_HeatFlux + nMarker_Isothermal + iMarker] = WALL_TYPE::SMOOTH;
-       }
-       for (iMarker = 0; iMarker < nMarker_CHTInterface; iMarker++) {
-         Roughness_Height[nMarker_HeatFlux + nMarker_Isothermal + nMarker_HeatTransfer + iMarker] = 0.0;
-         Kind_Wall[nMarker_HeatFlux + nMarker_Isothermal + nMarker_HeatTransfer + iMarker] = WALL_TYPE::SMOOTH;
-       }
-
-       /*--- Check for mismatch in number of rough walls and solid walls. ---*/
-     } else if (nRough_Wall > nWall) {
-        SU2_MPI::Error("Mismatch in number of rough walls and solid walls. Number of rough walls cannot be more than solid walls.", CURRENT_FUNCTION);
-       /*--- Check name of the marker and assign the corresponding roughness. ---*/
-     } else {
-       /*--- Store roughness heights in a temp array. ---*/
-       vector<su2double> temp_rough;
-       for (iMarker = 0; iMarker < nRough_Wall; iMarker++)
-         temp_rough.push_back(Roughness_Height[iMarker]);
-
-       /*--- Reallocate the roughness arrays in case not all walls are rough. ---*/
-       delete Roughness_Height;
-       delete Kind_Wall;
-       Roughness_Height = new su2double [nWall];
-       Kind_Wall = new WALL_TYPE [nWall];
-       unsigned short jMarker, chkRough = 0;
-
-       /*--- Initialize everything to smooth. ---*/
-       for (iMarker = 0; iMarker < nWall; iMarker++) {
-         Roughness_Height[iMarker] = 0.0;
-         Kind_Wall[iMarker] = WALL_TYPE::SMOOTH;
-       }
-
-       /*--- Look through heat flux, isothermal, heat transfer and cht_interface markers and assign proper values. ---*/
-       for (iMarker = 0; iMarker < nRough_Wall; iMarker++) {
-         for (jMarker = 0; jMarker < nMarker_HeatFlux; jMarker++)
-           if (Marker_HeatFlux[jMarker].compare(Marker_RoughWall[iMarker]) == 0) {
-             Roughness_Height[jMarker] = temp_rough[iMarker];
-             chkRough++;
-           }
-
-         for (jMarker = 0; jMarker < nMarker_Isothermal; jMarker++)
-           if (Marker_Isothermal[jMarker].compare(Marker_RoughWall[iMarker]) == 0) {
-             Roughness_Height[nMarker_HeatFlux + jMarker] = temp_rough[iMarker];
-             chkRough++;
-           }
-
-         for (jMarker = 0; jMarker < nMarker_HeatTransfer; jMarker++)
-           if (Marker_HeatTransfer[jMarker].compare(Marker_RoughWall[iMarker]) == 0) {
-             Roughness_Height[nMarker_HeatFlux + nMarker_Isothermal + jMarker] = temp_rough[iMarker];
-             chkRough++;
-           }
-
-         for (jMarker = 0; jMarker < nMarker_CHTInterface; jMarker++)
-           if (Marker_CHTInterface[jMarker].compare(Marker_RoughWall[iMarker]) == 0) {
-             Roughness_Height[nMarker_HeatFlux + nMarker_Isothermal + nMarker_HeatTransfer + jMarker] = temp_rough[iMarker];
-             chkRough++;
-           }
-       }
-
-       /*--- Update kind_wall when a non zero roughness value is specified. ---*/
-       for (iMarker = 0; iMarker < nWall; iMarker++)
-         if (Roughness_Height[iMarker] != 0.0)
-           Kind_Wall[iMarker] = WALL_TYPE::ROUGH;
-
-       /*--- Check if a non solid wall marker was specified as rough. ---*/
-       if (chkRough != nRough_Wall)
-         SU2_MPI::Error("Only solid walls can be rough.", CURRENT_FUNCTION);
-     }
-   }
+  if (nRough_Wall > 0) {
+    /*--- Validate name of the markers. ---*/
+    for (iMarker = 0; iMarker < nRough_Wall; ++iMarker) {
+      auto CheckMarker = [&](unsigned short nMarker, const string* markerName) {
+        for (auto jMarker = 0u; jMarker < nMarker; ++jMarker) {
+          if (markerName[jMarker].compare(Marker_RoughWall[iMarker]) == 0) {
+            return true;
+          }
+        }
+        return false;
+      };
+      if (!CheckMarker(nMarker_HeatFlux, Marker_HeatFlux) &&
+          !CheckMarker(nMarker_Isothermal, Marker_Isothermal) &&
+          !CheckMarker(nMarker_HeatTransfer, Marker_HeatTransfer) &&
+          !CheckMarker(nMarker_CHTInterface, Marker_CHTInterface)) {
+        SU2_MPI::Error("Marker " + Marker_RoughWall[iMarker] + " is not a viscous wall.", CURRENT_FUNCTION);
+      }
+    }
+  }
 
   /*--- Handle default options for topology optimization ---*/
 
@@ -6099,14 +6056,14 @@ void CConfig::SetOutput(SU2_COMPONENT val_software, unsigned short val_izone) {
         switch (Kind_Trans_Model) {
           case TURB_TRANS_MODEL::NONE:  break;
           case TURB_TRANS_MODEL::LM: {
-            cout << "Transition model: Langtry and Menter's 4 equation model"; 
+            cout << "Transition model: Langtry and Menter's 4 equation model";
             if (lmParsedOptions.LM2015) {
               cout << " w/ cross-flow corrections (2015)" << endl;
             } else {
               cout << " (2009)" << endl;
             }
-            break; 
-          }          
+            break;
+          }
         }
         if (Kind_Trans_Model == TURB_TRANS_MODEL::LM) {
 
@@ -6119,7 +6076,7 @@ void CConfig::SetOutput(SU2_COMPONENT val_software, unsigned short val_izone) {
             case TURB_TRANS_CORRELATION::MEDIDA_BAEDER: cout << "Medida and Baeder (2011)" << endl;  break;
             case TURB_TRANS_CORRELATION::MEDIDA: cout << "Medida PhD (2014)" << endl;  break;
             case TURB_TRANS_CORRELATION::MENTER_LANGTRY: cout << "Menter and Langtry (2009)" << endl;  break;
-            case TURB_TRANS_CORRELATION::DEFAULT: 
+            case TURB_TRANS_CORRELATION::DEFAULT:
               switch (Kind_Turb_Model) {
                 case TURB_MODEL::SA: cout << "Malan et al. (2009)" << endl;  break;
                 case TURB_MODEL::SST: cout << "Menter and Langtry (2009)" << endl;  break;
@@ -8005,8 +7962,6 @@ CConfig::~CConfig() {
 
   delete[] Marker_All_SendRecv;
 
-  delete[] Kind_Wall;
-
   if (DV_Value != nullptr) {
     for (iDV = 0; iDV < nDV; iDV++) delete[] DV_Value[iDV];
     delete [] DV_Value;
@@ -8396,6 +8351,14 @@ void CConfig::SetGlobalParam(MAIN_SOLVER val_solver,
     }
   };
 
+  auto SetHeatParam = [&]() {
+    if (val_system == RUNTIME_HEAT_SYS) {
+      SetKind_ConvNumScheme(Kind_ConvNumScheme_Heat, Kind_Centered_Heat,
+                            Kind_Upwind_Heat, Kind_SlopeLimit_Heat, MUSCL_Heat, NONE);
+      SetKind_TimeIntScheme(Kind_TimeIntScheme_Heat);
+    }
+  };
+
   auto SetSpeciesParam = [&]() {
     if (val_system == RUNTIME_SPECIES_SYS) {
       SetKind_ConvNumScheme(Kind_ConvNumScheme_Species, Kind_Centered_Species,
@@ -8416,21 +8379,21 @@ void CConfig::SetGlobalParam(MAIN_SOLVER val_solver,
 
   switch (val_solver) {
     case MAIN_SOLVER::EULER: case MAIN_SOLVER::INC_EULER: case MAIN_SOLVER::NEMO_EULER:
+    case MAIN_SOLVER::DISC_ADJ_EULER: case MAIN_SOLVER::DISC_ADJ_INC_EULER:
       SetFlowParam();
       break;
     case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::INC_NAVIER_STOKES: case MAIN_SOLVER::NEMO_NAVIER_STOKES:
+    case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES:
       SetFlowParam();
       SetSpeciesParam();
-
-      if (val_system == RUNTIME_HEAT_SYS) {
-        SetKind_ConvNumScheme(Kind_ConvNumScheme_Heat, CENTERED::NONE, UPWIND::NONE, LIMITER::NONE, NONE, NONE);
-        SetKind_TimeIntScheme(Kind_TimeIntScheme_Heat);
-      }
+      SetHeatParam();
       break;
     case MAIN_SOLVER::RANS: case MAIN_SOLVER::INC_RANS:
+    case MAIN_SOLVER::DISC_ADJ_RANS: case MAIN_SOLVER::DISC_ADJ_INC_RANS:
       SetFlowParam();
       SetTurbParam();
       SetSpeciesParam();
+      SetHeatParam();
 
       if (val_system == RUNTIME_TRANS_SYS) {
         SetKind_ConvNumScheme(Kind_ConvNumScheme_Turb, Kind_Centered_Turb,
@@ -8438,14 +8401,14 @@ void CConfig::SetGlobalParam(MAIN_SOLVER val_solver,
                               MUSCL_Turb, NONE);
         SetKind_TimeIntScheme(Kind_TimeIntScheme_Turb);
       }
-      if (val_system == RUNTIME_HEAT_SYS) {
-        SetKind_ConvNumScheme(Kind_ConvNumScheme_Heat, CENTERED::NONE, UPWIND::NONE, LIMITER::NONE, NONE, NONE);
-        SetKind_TimeIntScheme(Kind_TimeIntScheme_Heat);
-      }
       break;
     case MAIN_SOLVER::FEM_EULER:
     case MAIN_SOLVER::FEM_NAVIER_STOKES:
+    case MAIN_SOLVER::FEM_RANS:
     case MAIN_SOLVER::FEM_LES:
+    case MAIN_SOLVER::DISC_ADJ_FEM_EULER:
+    case MAIN_SOLVER::DISC_ADJ_FEM_NS:
+    case MAIN_SOLVER::DISC_ADJ_FEM_RANS:
       if (val_system == RUNTIME_FLOW_SYS) {
         SetKind_ConvNumScheme(Kind_ConvNumScheme_FEM_Flow, Kind_Centered_Flow,
                               Kind_Upwind_Flow, Kind_SlopeLimit_Flow,
@@ -8471,6 +8434,7 @@ void CConfig::SetGlobalParam(MAIN_SOLVER val_solver,
       }
       break;
     case MAIN_SOLVER::HEAT_EQUATION:
+    case MAIN_SOLVER::DISC_ADJ_HEAT:
       if (val_system == RUNTIME_HEAT_SYS) {
         SetKind_ConvNumScheme(NONE, CENTERED::NONE, UPWIND::NONE, LIMITER::NONE, NONE, NONE);
         SetKind_TimeIntScheme(Kind_TimeIntScheme_Heat);
@@ -8478,11 +8442,12 @@ void CConfig::SetGlobalParam(MAIN_SOLVER val_solver,
       break;
 
     case MAIN_SOLVER::FEM_ELASTICITY:
+    case MAIN_SOLVER::DISC_ADJ_FEM:
 
       Current_DynTime = static_cast<su2double>(TimeIter)*Delta_DynTime;
 
       if (val_system == RUNTIME_FEA_SYS) {
-        SetKind_ConvNumScheme(NONE, CENTERED::NONE, UPWIND::NONE, LIMITER::NONE , NONE, NONE);
+        SetKind_ConvNumScheme(NONE, CENTERED::NONE, UPWIND::NONE, LIMITER::NONE, NONE, NONE);
         SetKind_TimeIntScheme(NONE);
       }
       break;
@@ -9172,40 +9137,15 @@ su2double CConfig::GetWall_HeatTransfer_Temperature(string val_marker) const {
   return HeatTransfer_WallTemp[0];
 }
 
-pair<WALL_TYPE, su2double> CConfig::GetWallRoughnessProperties(string val_marker) const {
-  unsigned short iMarker = 0;
-  short          flag = -1;
-  pair<WALL_TYPE, su2double> WallProp;
-
-  if (nMarker_HeatFlux > 0 || nMarker_Isothermal > 0 || nMarker_HeatTransfer || nMarker_CHTInterface > 0) {
-    for (iMarker = 0; iMarker < nMarker_HeatFlux; iMarker++)
-      if (Marker_HeatFlux[iMarker] == val_marker) {
-        flag = iMarker;
-        WallProp = make_pair(Kind_Wall[flag], Roughness_Height[flag]);
-        return WallProp;
-      }
-    for (iMarker = 0; iMarker < nMarker_Isothermal; iMarker++)
-      if (Marker_Isothermal[iMarker] == val_marker) {
-        flag = nMarker_HeatFlux + iMarker;
-        WallProp = make_pair(Kind_Wall[flag], Roughness_Height[flag]);
-        return WallProp;
-      }
-    for (iMarker = 0; iMarker < nMarker_HeatTransfer; iMarker++)
-      if (Marker_HeatTransfer[iMarker] == val_marker) {
-        flag = nMarker_HeatFlux + nMarker_Isothermal + iMarker;
-        WallProp = make_pair(Kind_Wall[flag], Roughness_Height[flag]);
-        return WallProp;
-      }
-    for (iMarker = 0; iMarker < nMarker_CHTInterface; iMarker++)
-      if (Marker_CHTInterface[iMarker] == val_marker) {
-        flag = nMarker_HeatFlux + nMarker_Isothermal + nMarker_HeatTransfer + iMarker;
-        WallProp = make_pair(Kind_Wall[flag], Roughness_Height[flag]);
-        return WallProp;
-      }
+pair<WALL_TYPE, su2double> CConfig::GetWallRoughnessProperties(const string& val_marker) const {
+  su2double roughness = 0.0;
+  for (auto iMarker = 0u; iMarker < nRough_Wall; iMarker++) {
+    if (val_marker.compare(Marker_RoughWall[iMarker]) == 0) {
+      roughness = Roughness_Height[iMarker];
+      break;
+    }
   }
-
-  WallProp = make_pair(WALL_TYPE::SMOOTH, 0.0);
-  return WallProp;
+  return make_pair(roughness > 0 ? WALL_TYPE::ROUGH : WALL_TYPE::SMOOTH, roughness);
 }
 
 WALL_FUNCTIONS CConfig::GetWallFunction_Treatment(string val_marker) const {
diff --git a/SU2_CFD/include/numerics/heat.hpp b/SU2_CFD/include/numerics/heat.hpp
index fe7e8936a5f..7578a8cb842 100644
--- a/SU2_CFD/include/numerics/heat.hpp
+++ b/SU2_CFD/include/numerics/heat.hpp
@@ -27,41 +27,9 @@
 
 #pragma once
 
-#include "CNumerics.hpp"
-
-/*!
- * \class CCentSca_Heat
- * \brief Class for scalar centered scheme.
- * \ingroup ConvDiscr
- * \author O. Burghardt
- * \version 7.5.0 "Blackbird"
- */
-class CCentSca_Heat : public CNumerics {
-private:
-  su2double Param_Kappa_4;         /*!< \brief Artificial dissipation parameters. */
-  bool implicit;                   /*!< \brief Implicit calculation. */
-  bool dynamic_grid;               /*!< \brief Modification for grid movement. */
-
-public:
-  /*!
-   * \brief Constructor of the class.
-   * \param[in] val_nDim - Number of dimension of the problem.
-   * \param[in] val_nVar - Number of variables of the problem.
-   * \param[in] config - Definition of the particular problem.
-   */
-  CCentSca_Heat(unsigned short val_nDim, unsigned short val_nVar, const CConfig *config);
-
-  /*!
-   * \brief Compute the flow residual using a JST method.
-   * \param[out] val_resconv - Pointer to the convective residual.
-   * \param[out] val_resvisc - Pointer to the artificial viscosity residual.
-   * \param[out] val_Jacobian_i - Jacobian of the numerical method at node i (implicit computation).
-   * \param[out] val_Jacobian_j - Jacobian of the numerical method at node j (implicit computation).
-   * \param[in] config - Definition of the particular problem.
-   */
-  void ComputeResidual(su2double *val_residual, su2double **val_Jacobian_i, su2double **val_Jacobian_j,
-                       CConfig *config) override;
-};
+#include "scalar/scalar_diffusion.hpp"
+#include "scalar/scalar_convection.hpp"
+#include "../variables/CIncEulerVariable.hpp"
 
 /*!
  * \class CUpwSca_Heat
@@ -70,27 +38,31 @@ class CCentSca_Heat : public CNumerics {
  * \author O. Burghardt.
  * \version 7.5.1 "Blackbird"
  */
-class CUpwSca_Heat : public CNumerics {
-private:
-  bool implicit, dynamic_grid;
-
-public:
+class CUpwSca_Heat final : public CUpwScalar<typename CIncEulerVariable::template CIndices<unsigned short>> {
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] val_nDim - Number of dimensions of the problem.
-   * \param[in] val_nVar - Number of variables of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  CUpwSca_Heat(unsigned short val_nDim, unsigned short val_nVar, const CConfig *config);
+  CUpwSca_Heat(unsigned short val_nDim, const CConfig *config)
+    : CUpwScalar<typename CIncEulerVariable::template CIndices<unsigned short>>(val_nDim, 1, config) {}
+
+ private:
+  /*!
+   * \brief Adds extra variables to AD
+   */
+  void ExtraADPreaccIn(void) override {}
 
   /*!
-   * \brief Compute the scalar upwind flux between two nodes i and j.
-   * \param[out] val_residual - Pointer to the total residual.
-   * \param[out] val_Jacobian_i - Jacobian of the numerical method at node i (implicit computation).
-   * \param[out] val_Jacobian_j - Jacobian of the numerical method at node j (implicit computation).
+   * \brief Heat-specific specific steps in the ComputeResidual method
    * \param[in] config - Definition of the particular problem.
    */
-  void ComputeResidual(su2double *val_residual, su2double **val_Jacobian_i, su2double **val_Jacobian_j, CConfig *config) override;
+  void FinishResidualCalc(const CConfig* config) override {
+    Flux[0] = a0 * ScalarVar_i[0] + a1 * ScalarVar_j[0];
+    Jacobian_i[0][0] = a0;
+    Jacobian_j[0][0] = a1;
+  }
 };
 
 /*!
@@ -100,26 +72,36 @@ class CUpwSca_Heat : public CNumerics {
  * \author O. Burghardt.
  * \version 7.5.1 "Blackbird"
  */
-class CAvgGrad_Heat : public CNumerics {
-private:
-  bool implicit, correct;
-
-public:
+class CAvgGrad_Heat final : public CAvgGrad_Scalar<CNoFlowIndices> {
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] val_nDim - Number of dimensions of the problem.
-   * \param[in] val_nVar - Number of variables of the problem.
    * \param[in] config - Definition of the particular problem.
-   * \param[in] correct - Correct the gradient.
+   * \param[in] correct - Whether to correct the gradient.
+   */
+  CAvgGrad_Heat(unsigned short val_nDim, const CConfig *config, bool correct)
+    : CAvgGrad_Scalar<CNoFlowIndices>(val_nDim, 1, correct, config) {}
+
+ private:
+  /*!
+   * \brief Adds extra variables to AD
    */
-  CAvgGrad_Heat(unsigned short val_nDim, unsigned short val_nVar, const CConfig *config, bool correct);
+  void ExtraADPreaccIn(void) override {
+    AD::SetPreaccIn(*Diffusion_Coeff_i, *Diffusion_Coeff_j);
+  }
 
   /*!
-   * \brief Compute the viscous heat residual using an average of gradients with correction.
-   * \param[out] val_residual - Pointer to the total residual.
-   * \param[out] Jacobian_i - Jacobian of the numerical method at node i (implicit computation).
-   * \param[out] Jacobian_j - Jacobian of the numerical method at node j (implicit computation).
+   * \brief Heat-specific specific steps in the ComputeResidual method
    * \param[in] config - Definition of the particular problem.
    */
-  void ComputeResidual(su2double *val_residual, su2double **Jacobian_i, su2double **Jacobian_j, CConfig *config) override;
+  void FinishResidualCalc(const CConfig* config) override {
+    const su2double Thermal_Diffusivity_Mean = 0.5 * (*Diffusion_Coeff_i + *Diffusion_Coeff_j);
+
+    Flux[0] = Thermal_Diffusivity_Mean * Proj_Mean_GradScalarVar[0];
+
+    /*--- Use TSL for Jacobians. ---*/
+    Jacobian_i[0][0] = -Thermal_Diffusivity_Mean * proj_vector_ij;
+    Jacobian_j[0][0] = Thermal_Diffusivity_Mean * proj_vector_ij;
+  }
 };
diff --git a/SU2_CFD/obj/Makefile.am b/SU2_CFD/obj/Makefile.am
index ec422f7948a..5aa0df49c11 100644
--- a/SU2_CFD/obj/Makefile.am
+++ b/SU2_CFD/obj/Makefile.am
@@ -86,7 +86,6 @@ libSU2Core_sources = ../src/definition_structure.cpp \
   ../src/numerics/CNumerics.cpp \
   ../src/numerics/template.cpp \
   ../src/numerics/transition.cpp \
-  ../src/numerics/heat.cpp \
   ../src/numerics/radiation.cpp \
   ../src/numerics/CLookUpTable.cpp \
   ../src/numerics/CTrapezoidalMap.cpp \
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index 328ba44453a..121cd94e9a5 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -1459,7 +1459,6 @@ void CDriver::Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSol
     cout << endl <<"------------------- Numerics Preprocessing ( Zone " << config->GetiZone() <<" ) -------------------" << endl;
 
   unsigned short iMGlevel, iSol,
-
   nVar_Template         = 0,
   nVar_Flow             = 0,
   nVar_NEMO             = 0,
@@ -1471,8 +1470,7 @@ void CDriver::Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSol
   nVar_Adj_Flow         = 0,
   nVar_Adj_Turb         = 0,
   nVar_FEM              = 0,
-  nVar_Rad              = 0,
-  nVar_Heat             = 0;
+  nVar_Rad              = 0;
 
   numerics = new CNumerics***[config->GetnMGLevels()+1] ();
 
@@ -1589,7 +1587,6 @@ void CDriver::Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSol
   if (fem_ns)       nVar_Flow = solver[MESH_0][FLOW_SOL]->GetnVar();
 
   if (fem)          nVar_FEM = solver[MESH_0][FEA_SOL]->GetnVar();
-  if (heat)         nVar_Heat = solver[MESH_0][HEAT_SOL]->GetnVar();
 
   if (config->AddRadiation()) nVar_Rad = solver[MESH_0][RAD_SOL]->GetnVar();
 
@@ -1908,8 +1905,13 @@ void CDriver::Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSol
       else if ((incompressible && (config->GetKind_Streamwise_Periodic() != ENUM_STREAMWISE_PERIODIC::NONE)) &&
                (config->GetEnergy_Equation() && !config->GetStreamwise_Periodic_Temperature()))
         numerics[iMGlevel][FLOW_SOL][source_second_term] = new CSourceIncStreamwisePeriodic_Outlet(nDim, nVar_Flow, config);
+      else if (config->GetVorticityConfinement() == YES) {
+        /*--- Vorticity Confinement term as a second source term to allow the use of VC along with other source terms ---*/
+        numerics[iMGlevel][FLOW_SOL][source_second_term] = new CSourceVorticityConfinement(nDim, nVar_Flow, config);
+      }
       else
         numerics[iMGlevel][FLOW_SOL][source_second_term] = new CSourceNothing(nDim, nVar_Flow, config);
+
     }
 
   }
@@ -2112,19 +2114,14 @@ void CDriver::Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSol
     /*--- Definition of the viscous scheme for each equation and mesh level ---*/
     for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
 
-      numerics[iMGlevel][HEAT_SOL][visc_term] = new CAvgGrad_Heat(nDim, nVar_Heat, config, true);
-      numerics[iMGlevel][HEAT_SOL][visc_bound_term] = new CAvgGrad_Heat(nDim, nVar_Heat, config, false);
+      numerics[iMGlevel][HEAT_SOL][visc_term] = new CAvgGrad_Heat(nDim, config, true);
+      numerics[iMGlevel][HEAT_SOL][visc_bound_term] = new CAvgGrad_Heat(nDim, config, false);
 
       switch (config->GetKind_ConvNumScheme_Heat()) {
 
         case SPACE_UPWIND :
-          numerics[iMGlevel][HEAT_SOL][conv_term] = new CUpwSca_Heat(nDim, nVar_Heat, config);
-          numerics[iMGlevel][HEAT_SOL][conv_bound_term] = new CUpwSca_Heat(nDim, nVar_Heat, config);
-          break;
-
-        case SPACE_CENTERED :
-          numerics[iMGlevel][HEAT_SOL][conv_term] = new CCentSca_Heat(nDim, nVar_Heat, config);
-          numerics[iMGlevel][HEAT_SOL][conv_bound_term] = new CUpwSca_Heat(nDim, nVar_Heat, config);
+          numerics[iMGlevel][HEAT_SOL][conv_term] = new CUpwSca_Heat(nDim, config);
+          numerics[iMGlevel][HEAT_SOL][conv_bound_term] = new CUpwSca_Heat(nDim, config);
           break;
 
         default:
diff --git a/SU2_CFD/src/meson.build b/SU2_CFD/src/meson.build
index 1dc9c94ac5a..055ee26e619 100644
--- a/SU2_CFD/src/meson.build
+++ b/SU2_CFD/src/meson.build
@@ -118,8 +118,7 @@ su2_cfd_src += files(['solvers/CSolverFactory.cpp',
                       'solvers/CGradientSmoothingSolver.cpp'])
 
 su2_cfd_src += files(['numerics/CNumerics.cpp',
-                      'numerics/template.cpp',                      
-                      'numerics/heat.cpp',
+                      'numerics/template.cpp',
                       'numerics/radiation.cpp',
                       'numerics/flow/convection/roe.cpp',
                       'numerics/flow/convection/fds.cpp',
diff --git a/SU2_CFD/src/numerics/flow/flow_sources.cpp b/SU2_CFD/src/numerics/flow/flow_sources.cpp
index 766440a9cdc..2fb164f3d1f 100644
--- a/SU2_CFD/src/numerics/flow/flow_sources.cpp
+++ b/SU2_CFD/src/numerics/flow/flow_sources.cpp
@@ -259,8 +259,8 @@ CNumerics::ResidualType<> CSourceIncAxisymmetric_Flow::ComputeResidual(const CCo
 
     /*--- Set primitive variables at points iPoint. ---*/
 
+    const su2double Temp_i = V_i[nDim+1];
     Pressure_i    = V_i[0];
-    Temp_i        = V_i[nDim+1];
     DensityInc_i  = V_i[nDim+2];
     BetaInc2_i    = V_i[nDim+3];
     Cp_i          = V_i[nDim+7];
@@ -616,6 +616,105 @@ CNumerics::ResidualType<> CSourceIncRotatingFrame_Flow::ComputeResidual(const CC
   return ResidualType<>(residual, jacobian, nullptr);
 }
 
+CSourceVorticityConfinement::CSourceVorticityConfinement(unsigned short val_nDim, unsigned short val_nVar,
+                                                         const CConfig* config)
+    : CSourceBase_Flow(val_nDim, val_nVar, config) {
+  Gamma = config->GetGamma();
+  Gamma_Minus_One = Gamma - 1.0;
+}
+
+CNumerics::ResidualType<> CSourceVorticityConfinement::ComputeResidual(const CConfig* config) {
+  /*--- density, \rho ---*/
+  const su2double rho = V_i[nDim + 2];
+
+  /*--- velocity, U = (u, v, w) ---*/
+  su2double U[3] = {V_i[1], V_i[2], 0.0};
+  if (nDim == 3) U[2] = V_i[3];
+  const su2double U_abs = max(GeometryToolbox::Norm(3, U), 1e-12);
+
+  /*--- vorticity, \omega ---*/
+  const su2double omega[3] = {Vorticity_i[0], Vorticity_i[1], Vorticity_i[2]};
+
+  /*--- grad of the mag of vorticity, \nabla|\omega| = AuxVar_Grad_i[0] ---*/
+  const su2double omega_abs_grad_abs = max(GeometryToolbox::Norm(3, AuxVar_Grad_i[0]), 1e-12);
+
+  /*--- unit vector, n along \nabla|\omega| ---*/
+  const su2double n[3] = {
+      AuxVar_Grad_i[0][0] / omega_abs_grad_abs,
+      AuxVar_Grad_i[0][1] / omega_abs_grad_abs,
+      AuxVar_Grad_i[0][2] / omega_abs_grad_abs,
+  };
+
+  /*--- n \cross \omega ---*/
+  su2double nXomega[3] = {0.0, 0.0, 0.0};
+  GeometryToolbox::CrossProduct(n, omega, nXomega);
+  const su2double nXomega_U = GeometryToolbox::DotProduct(3, nXomega, U);
+
+  /*--- vorticity confinement parameter ---*/
+  const su2double vc_config = config->GetConfinement_Param();
+  su2double vc = vc_config * (1 + log10(pow((1 + (Volume / AvgVolume)), 1.0 / 3.0)));
+
+  /*--- correction to vc near viscous wall ---*/
+  const bool viscous = config->GetViscous();
+  if (viscous) {
+    su2double U_infty[3] = {config->GetVelocity_FreeStreamND()[0], config->GetVelocity_FreeStreamND()[1], 0.0};
+    if (nDim == 3) U_infty[2] = config->GetVelocity_FreeStreamND()[2];
+    const su2double U_infty_abs = max(GeometryToolbox::Norm(3, U_infty), 1e-12);
+    const su2double L = config->GetLength_Reynolds();
+    const su2double mu = V_i[nDim + 5];                   // viscosity
+    const su2double mu_t = V_i[nDim + 6];                 // turbulent or eddy viscosity
+    const su2double mu_eff = mu + mu_t;                   // effective or total viscosity
+    const su2double Re = rho * U_infty_abs * L / mu_eff;  // Reynolds number
+    const su2double delta = 5 * L / sqrt(Re);             // boundary layer thickness
+
+    if (dist_i <= 4 * delta) {
+      vc *= 0.0;
+    }
+  }
+
+  /*--- source terms: S / rho ---*/
+  const su2double vc_Uabs_Volume = vc * U_abs * Volume;
+  const su2double S_u_rho = -nXomega[0] * vc_Uabs_Volume;
+  const su2double S_v_rho = -nXomega[1] * vc_Uabs_Volume;
+  const su2double S_w_rho = -nXomega[2] * vc_Uabs_Volume;
+  const su2double S_E_rho = -nXomega_U * vc_Uabs_Volume;
+
+  residual[0] = 0.0;
+  residual[1] = rho * S_u_rho;
+  residual[2] = rho * S_v_rho;
+  if (nDim == 2) {
+    residual[3] = rho * S_E_rho;
+  }
+  if (nDim == 3) {
+    residual[3] = rho * S_w_rho;
+    residual[4] = rho * S_E_rho;
+  }
+
+  const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+  if (implicit) {
+    for (unsigned iVar = 0; iVar < nVar; iVar++) {
+      for (unsigned jVar = 0; jVar < nVar; jVar++) {
+        jacobian[iVar][jVar] = 0.0;
+      }
+    }
+
+    jacobian[1][0] = S_u_rho;
+    jacobian[2][0] = S_v_rho;
+    if (nDim == 2) {
+      jacobian[3][1] = S_u_rho;
+      jacobian[3][2] = S_v_rho;
+    }
+    if (nDim == 3) {
+      jacobian[3][0] = S_w_rho;
+      jacobian[4][1] = S_u_rho;
+      jacobian[4][2] = S_v_rho;
+      jacobian[4][3] = S_w_rho;
+    }
+  }
+
+  return ResidualType<>(residual, jacobian, nullptr);
+}
+
 CSourceWindGust::CSourceWindGust(unsigned short val_nDim, unsigned short val_nVar, const CConfig* config) :
                  CSourceBase_Flow(val_nDim, val_nVar, config) { }
 
diff --git a/SU2_CFD/src/numerics/heat.cpp b/SU2_CFD/src/numerics/heat.cpp
deleted file mode 100644
index 177fc0b452f..00000000000
--- a/SU2_CFD/src/numerics/heat.cpp
+++ /dev/null
@@ -1,202 +0,0 @@
-/*!
- * \file heat.cpp
- * \brief Implementation of numerics classes for heat transfer.
- * \author F. Palacios, T. Economon
- * \version 7.5.0 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-
-#include "../../include/numerics/heat.hpp"
-#include "../../../Common/include/toolboxes/geometry_toolbox.hpp"
-
-CCentSca_Heat::CCentSca_Heat(unsigned short val_nDim, unsigned short val_nVar, const CConfig *config) :
-               CNumerics(val_nDim, val_nVar, config) {
-
-  implicit = (config->GetKind_TimeIntScheme_Turb() == EULER_IMPLICIT);
-  dynamic_grid = config->GetDynamic_Grid();
-  Param_Kappa_4 = config->GetKappa_4th_Heat();
-
-}
-
-void CCentSca_Heat::ComputeResidual(su2double *val_residual, su2double **val_Jacobian_i,
-                                    su2double **val_Jacobian_j, CConfig *config) {
-  AD::StartPreacc();
-  AD::SetPreaccIn(V_i, nDim+3); AD::SetPreaccIn(V_j, nDim+3);
-  AD::SetPreaccIn(Temp_i); AD::SetPreaccIn(Temp_j);
-  AD::SetPreaccIn(Und_Lapl_i, nVar); AD::SetPreaccIn(Und_Lapl_j, nVar);
-  AD::SetPreaccIn(Normal, nDim);
-  if (dynamic_grid) {
-    AD::SetPreaccIn(GridVel_i, nDim); AD::SetPreaccIn(GridVel_j, nDim);
-  }
-
-  /*--- Primitive variables at point i and j ---*/
-
-  Pressure_i =    V_i[0];       Pressure_j = V_j[0];
-  DensityInc_i =  V_i[nDim+2];  DensityInc_j = V_j[nDim+2];
-  BetaInc2_i =    V_i[nDim+3];  BetaInc2_j = V_j[nDim+3];
-
-  /*--- Projected velocities at the current edge ---*/
-
-  su2double ProjVelocity_i = 0.0;
-  su2double ProjVelocity_j = 0.0;
-
-  if (dynamic_grid) {
-    for (unsigned short iDim = 0; iDim < nDim; iDim++) {
-      su2double Velocity_i = V_i[iDim+1] - GridVel_i[iDim];
-      su2double Velocity_j = V_j[iDim+1] - GridVel_j[iDim];
-      ProjVelocity_i += Velocity_i*Normal[iDim];
-      ProjVelocity_j += Velocity_j*Normal[iDim];
-    }
-  }
-  else {
-    for (unsigned short iDim = 0; iDim < nDim; iDim++) {
-      ProjVelocity_i += V_i[iDim+1]*Normal[iDim];
-      ProjVelocity_j += V_j[iDim+1]*Normal[iDim];
-    }
-  }
-
-  /*--- Computing the second order centered scheme part ---*/
-
-  const su2double ProjVelocity = 0.5*(ProjVelocity_i+ProjVelocity_j);
-
-  val_residual[0] = 0.5*(Temp_i + Temp_j)*ProjVelocity;
-
-  if (implicit) {
-    val_Jacobian_i[0][0] = 0.5*ProjVelocity;
-    val_Jacobian_j[0][0] = 0.5*ProjVelocity;
-  }
-
-  /*--- Adding artificial dissipation to stabilize the centered scheme ---*/
-
-  const su2double Diff_Lapl = Und_Lapl_i[0]-Und_Lapl_j[0];
-  const su2double Area2 = GeometryToolbox::SquaredNorm(nDim, Normal);
-
-  const su2double SoundSpeed_i = sqrt(pow(ProjVelocity_i,2) + (BetaInc2_i/DensityInc_i)*Area2);
-  const su2double SoundSpeed_j = sqrt(pow(ProjVelocity_j,2) + (BetaInc2_j/DensityInc_j)*Area2);
-
-  const su2double Local_Lambda_i = fabs(ProjVelocity_i)+SoundSpeed_i;
-  const su2double Local_Lambda_j = fabs(ProjVelocity_j)+SoundSpeed_j;
-  const su2double MeanLambda = 0.5*(Local_Lambda_i+Local_Lambda_j);
-
-  val_residual[0] += -Param_Kappa_4*Diff_Lapl*MeanLambda;
-
-  if (implicit) {
-    const su2double cte_0 = Param_Kappa_4*su2double(Neighbor_i+1)*MeanLambda;
-    const su2double cte_1 = Param_Kappa_4*su2double(Neighbor_j+1)*MeanLambda;
-
-    val_Jacobian_i[0][0] += cte_0;
-    val_Jacobian_j[0][0] -= cte_1;
-  }
-
-  AD::SetPreaccOut(val_residual[0]);
-  AD::EndPreacc();
-
-}
-
-CUpwSca_Heat::CUpwSca_Heat(unsigned short val_nDim, unsigned short val_nVar, const CConfig *config) :
-              CNumerics(val_nDim, val_nVar, config) {
-
-  implicit = (config->GetKind_TimeIntScheme_Turb() == EULER_IMPLICIT);
-  dynamic_grid = config->GetDynamic_Grid();
-
-}
-
-void CUpwSca_Heat::ComputeResidual(su2double *val_residual, su2double **val_Jacobian_i,
-                                   su2double **val_Jacobian_j, CConfig *config) {
-
-  AD::StartPreacc();
-  AD::SetPreaccIn(V_i, nDim+1); AD::SetPreaccIn(V_j, nDim+1);
-  AD::SetPreaccIn(Temp_i); AD::SetPreaccIn(Temp_j);
-  AD::SetPreaccIn(Normal, nDim);
-  if (dynamic_grid) {
-    AD::SetPreaccIn(GridVel_i, nDim); AD::SetPreaccIn(GridVel_j, nDim);
-  }
-
-  su2double q_ij = 0.0;
-
-  if (dynamic_grid) {
-    for (unsigned short iDim = 0; iDim < nDim; iDim++) {
-      const su2double Velocity_i = V_i[iDim+1] - GridVel_i[iDim];
-      const su2double Velocity_j = V_j[iDim+1] - GridVel_j[iDim];
-      q_ij += 0.5*(Velocity_i+Velocity_j)*Normal[iDim];
-    }
-  }
-  else {
-    for (unsigned short iDim = 0; iDim < nDim; iDim++) {
-      q_ij += 0.5*(V_i[iDim+1]+V_j[iDim+1])*Normal[iDim];
-    }
-  }
-
-  const su2double a0 = 0.5*(q_ij+fabs(q_ij));
-  const su2double a1 = 0.5*(q_ij-fabs(q_ij));
-
-  val_residual[0] = a0*Temp_i+a1*Temp_j;
-
-  if (implicit) {
-    val_Jacobian_i[0][0] = a0;
-    val_Jacobian_j[0][0] = a1;
-  }
-
-  AD::SetPreaccOut(val_residual[0]);
-  AD::EndPreacc();
-
-}
-
-CAvgGrad_Heat::CAvgGrad_Heat(unsigned short val_nDim, unsigned short val_nVar,
-                             const CConfig *config, bool correct_) :
-               CNumerics(val_nDim, val_nVar, config) {
-
-  implicit = (config->GetKind_TimeIntScheme_Heat() == EULER_IMPLICIT);
-  correct = correct_;
-}
-
-void CAvgGrad_Heat::ComputeResidual(su2double *val_residual, su2double **Jacobian_i,
-                                    su2double **Jacobian_j, CConfig *config) {
-  constexpr int nVar = 1;
-
-  AD::StartPreacc();
-  AD::SetPreaccIn(Coord_i, nDim); AD::SetPreaccIn(Coord_j, nDim);
-  AD::SetPreaccIn(Normal, nDim);
-  AD::SetPreaccIn(Temp_i); AD::SetPreaccIn(Temp_j);
-  AD::SetPreaccIn(ConsVar_Grad_i[0],nDim); AD::SetPreaccIn(ConsVar_Grad_j[0],nDim);
-  AD::SetPreaccIn(Thermal_Diffusivity_i); AD::SetPreaccIn(Thermal_Conductivity_j);
-
-  su2double NormalGrad[nVar], CorrectedGrad[nVar];
-
-  auto proj_vector_ij = ComputeProjectedGradient(nDim, nVar, Normal, Coord_i, Coord_j, ConsVar_Grad_i,
-                                                 ConsVar_Grad_j, correct, &Temp_i, &Temp_j,
-                                                 NormalGrad, CorrectedGrad);
-
-  const su2double Thermal_Diffusivity_Mean = 0.5*(Thermal_Diffusivity_i + Thermal_Diffusivity_j);
-
-  val_residual[0] = Thermal_Diffusivity_Mean*CorrectedGrad[0];
-
-  /*--- For Jacobians -> Use of TSL approx. to compute derivatives of the gradients ---*/
-  if (implicit) {
-    Jacobian_i[0][0] = -Thermal_Diffusivity_Mean*proj_vector_ij;
-    Jacobian_j[0][0] = Thermal_Diffusivity_Mean*proj_vector_ij;
-  }
-
-  AD::SetPreaccOut(val_residual, nVar);
-  AD::EndPreacc();
-
-}
diff --git a/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp b/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
index 636b8288310..dcca84abbeb 100644
--- a/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
@@ -1509,49 +1509,38 @@ void CNEMOEulerSolver::BC_Sym_Plane(CGeometry *geometry, CSolver **solver_contai
   }
 }
 
-void CNEMOEulerSolver::BC_Far_Field(CGeometry *geometry, CSolver **solver_container,
-                                    CNumerics *conv_numerics, CNumerics *visc_numerics,
-                                    CConfig *config, unsigned short val_marker) {
-
-  unsigned short iDim;
-  unsigned long iVertex, iPoint, Point_Normal;
-
-  su2double *V_infty, *V_domain, *U_infty, *U_domain;
-
-  /*--- Set booleans from configuration parameters ---*/
-  bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
-  bool viscous  = config->GetViscous();
+void CNEMOEulerSolver::BC_Far_Field(CGeometry *geometry,
+                                    CSolver **solver_container,
+                                    CNumerics *conv_numerics,
+                                    CNumerics *visc_numerics, CConfig *config,
+                                    unsigned short val_marker) {
 
   /*--- Allocate arrays ---*/
-  su2double *Normal = new su2double[nDim];
+  su2double Normal[MAXNDIM] = {0.0};
 
   /*--- Loop over all the vertices on this boundary (val_marker) ---*/
-  for (iVertex = 0; iVertex < geometry->nVertex[val_marker]; iVertex++) {
-    iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
-
-    /*--- Allocate the value at the infinity ---*/
-    V_infty = GetCharacPrimVar(val_marker, iVertex);
+  for (unsigned long iVertex = 0; iVertex < geometry->nVertex[val_marker];
+       iVertex++) {
+    const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
     /*--- Check if the node belongs to the domain (i.e, not a halo node) ---*/
     if (geometry->nodes->GetDomain(iPoint)) {
 
       /*--- Retrieve index of the closest interior node ---*/
-      Point_Normal = geometry->vertex[val_marker][iVertex]->GetNormal_Neighbor(); //only used for implicit
+      const auto Point_Normal = geometry->vertex[val_marker][iVertex]
+              ->GetNormal_Neighbor(); // only used for implicit
 
       /*--- Pass boundary node normal to CNumerics ---*/
       geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
-      for (iDim = 0; iDim < nDim; iDim++) Normal[iDim] = -Normal[iDim];
+      for (unsigned short iDim = 0; iDim < nDim; iDim++)
+        Normal[iDim] = -Normal[iDim];
       conv_numerics->SetNormal(Normal);
 
-      /*--- Retrieve solution at the boundary node & free-stream ---*/
-      U_domain = nodes->GetSolution(iPoint);
-      V_domain = nodes->GetPrimitive(iPoint);
-      U_infty  = node_infty->GetSolution(0);
-      V_infty  = node_infty->GetPrimitive(0);
-
       /*--- Pass conserved & primitive variables to CNumerics ---*/
-      conv_numerics->SetConservative(U_domain, U_infty);
-      conv_numerics->SetPrimitive(V_domain, V_infty);
+      conv_numerics->SetConservative(nodes->GetSolution(iPoint),
+                                     node_infty->GetSolution(0));
+      conv_numerics->SetPrimitive(nodes->GetPrimitive(iPoint),
+                                  node_infty->GetPrimitive(0));
 
       /*--- Pass supplementary information to CNumerics ---*/
       conv_numerics->SetdPdU  (nodes->GetdPdU(iPoint),   node_infty->GetdPdU(0));
@@ -1564,37 +1553,43 @@ void CNEMOEulerSolver::BC_Far_Field(CGeometry *geometry, CSolver **solver_contai
         conv_numerics->SetSensor (nodes->GetSensor(iPoint), nodes->GetSensor(iPoint));
 
       /*--- Compute the convective residual (and Jacobian) ---*/
-      // Note: This uses the specified boundary num. method specified in driver_structure.cpp
+      // Note: This uses the specified boundary num. method specified in
+      // driver_structure.cpp
       auto residual = conv_numerics->ComputeResidual(config);
 
       /*--- Apply contribution to the linear system ---*/
       LinSysRes.AddBlock(iPoint, residual);
 
+      const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
       if (implicit)
         Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
 
       /*--- Viscous contribution ---*/
+      bool viscous = config->GetViscous();
       if (viscous) {
         su2double Coord_Reflected[MAXNDIM];
-        GeometryToolbox::PointPointReflect(nDim, geometry->nodes->GetCoord(Point_Normal),
-                                                 geometry->nodes->GetCoord(iPoint), Coord_Reflected);
-        visc_numerics->SetCoord(geometry->nodes->GetCoord(iPoint), Coord_Reflected );
+        GeometryToolbox::PointPointReflect(
+            nDim, geometry->nodes->GetCoord(Point_Normal),
+            geometry->nodes->GetCoord(iPoint), Coord_Reflected);
+        visc_numerics->SetCoord(geometry->nodes->GetCoord(iPoint),
+                                Coord_Reflected);
         visc_numerics->SetNormal(Normal);
 
         /*--- Primitive variables, and gradient ---*/
         visc_numerics->SetConservative(nodes->GetSolution(iPoint),
-                                       node_infty->GetSolution(0) );
+                                       node_infty->GetSolution(0));
         visc_numerics->SetPrimitive(nodes->GetPrimitive(iPoint),
-                                    node_infty->GetPrimitive(0) );
+                                    node_infty->GetPrimitive(0));
         visc_numerics->SetPrimVarGradient(nodes->GetGradient_Primitive(iPoint),
-                                          node_infty->GetGradient_Primitive(0) );
+                                          node_infty->GetGradient_Primitive(0));
 
         /*--- Pass supplementary information to CNumerics ---*/
-        visc_numerics->SetdPdU  (nodes->GetdPdU(iPoint),   node_infty->GetdPdU(0));
-        visc_numerics->SetdTdU  (nodes->GetdTdU(iPoint),   node_infty->GetdTdU(0));
-        visc_numerics->SetdTvedU(nodes->GetdTvedU(iPoint), node_infty->GetdTvedU(0));
-        visc_numerics->SetEve   (nodes->GetEve(iPoint),    node_infty->GetEve(0));
-        visc_numerics->SetCvve  (nodes->GetCvve(iPoint),   node_infty->GetCvve(0));
+        visc_numerics->SetdPdU(nodes->GetdPdU(iPoint), node_infty->GetdPdU(0));
+        visc_numerics->SetdTdU(nodes->GetdTdU(iPoint), node_infty->GetdTdU(0));
+        visc_numerics->SetdTvedU(nodes->GetdTvedU(iPoint),
+                                 node_infty->GetdTvedU(0));
+        visc_numerics->SetEve(nodes->GetEve(iPoint), node_infty->GetEve(0));
+        visc_numerics->SetCvve(nodes->GetCvve(iPoint), node_infty->GetCvve(0));
 
         /*--- Species diffusion coefficients ---*/
         visc_numerics->SetDiffusionCoeff(nodes->GetDiffusionCoeff(iPoint),
@@ -1609,12 +1604,14 @@ void CNEMOEulerSolver::BC_Far_Field(CGeometry *geometry, CSolver **solver_contai
                                         nodes->GetEddyViscosity(iPoint));
 
         /*--- Thermal conductivity ---*/
-        visc_numerics->SetThermalConductivity(nodes->GetThermalConductivity(iPoint),
-                                              nodes->GetThermalConductivity(iPoint));
+        visc_numerics->SetThermalConductivity(
+            nodes->GetThermalConductivity(iPoint),
+            nodes->GetThermalConductivity(iPoint));
 
         /*--- Vib-el. thermal conductivity ---*/
-        visc_numerics->SetThermalConductivity_ve(nodes->GetThermalConductivity_ve(iPoint),
-                                                 nodes->GetThermalConductivity_ve(iPoint));
+        visc_numerics->SetThermalConductivity_ve(
+            nodes->GetThermalConductivity_ve(iPoint),
+            nodes->GetThermalConductivity_ve(iPoint));
 
         /*--- Compute and update residual ---*/
         auto residual = visc_numerics->ComputeResidual(config);
@@ -1626,9 +1623,6 @@ void CNEMOEulerSolver::BC_Far_Field(CGeometry *geometry, CSolver **solver_contai
       }
     }
   }
-
-  /*--- Free locally allocated memory ---*/
-  delete [] Normal;
 }
 
 void CNEMOEulerSolver::BC_Inlet(CGeometry *geometry, CSolver **solver_container,
@@ -2158,283 +2152,207 @@ void CNEMOEulerSolver::BC_Outlet(CGeometry *geometry, CSolver **solver_container
 
 }
 
-void CNEMOEulerSolver::BC_Supersonic_Inlet(CGeometry *geometry, CSolver **solver_container,
-                                           CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
-
-SU2_MPI::Error("BC_SUPERSONIC_INLET: Not operational in NEMO.", CURRENT_FUNCTION);
-
-//  unsigned short iDim, iVar;
-//  unsigned long iVertex, iPoint, Point_Normal;
-//  su2double Density, Pressure, Temperature, Temperature_ve, Energy, *Velocity, Velocity2, soundspeed;
-//  su2double Gas_Constant = config->GetGas_ConstantND();
-//
-//  bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
-//  bool dynamic_grid  = config->GetGrid_Movement();
-//  bool viscous              = config->GetViscous();
-//  string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
-//
-//  su2double RuSI  = UNIVERSAL_GAS_CONSTANT;
-//  su2double Ru = 1000.0*RuSI;
-//
-//  su2double *U_inlet = new su2double[nVar];     su2double *U_domain = new su2double[nVar];
-//  su2double *V_inlet = new su2double[nPrimVar]; su2double *V_domain = new su2double[nPrimVar];
-//  su2double *Normal = new su2double[nDim];
-
-/* ----------------------------------------------------------------------------- */
-/* ----------------------------------------------------------------------------- */
-/* The block of code commented below needs to be updated to use Fluidmodel class */
-/* ----------------------------------------------------------------------------- */
-/* ----------------------------------------------------------------------------- */
-
-//  /*--- Supersonic inlet flow: there are no outgoing characteristics,
-//   so all flow variables can be imposed at the inlet.
-//   First, retrieve the specified values for the primitive variables. ---*/
-//  //ASSUME TVE = T for the time being
-//  auto Mass_Frac      = config->GetInlet_MassFrac(Marker_Tag);
-//  Temperature    = config->GetInlet_Temperature(Marker_Tag);
-//  Pressure       = config->GetInlet_Pressure(Marker_Tag);
-//  Velocity       = config->GetInlet_Velocity(Marker_Tag);
-//  Temperature_ve = Temperature;
-//
-//  /*--- Compute Density and Species Densities ---*/
-//  for (iSpecies = 0; iSpecies < nHeavy; iSpecies++)
-//    denom += Mass_Frac[iSpecies] * (Ru/Ms[iSpecies]) * Temperature;
-//  for (iSpecies = 0; iSpecies < nEl; iSpecies++)
-//    denom += Mass_Frac[nSpecies-1] * (Ru/Ms[nSpecies-1]) * Temperature_ve;
-//  Density = Pressure / denom;
-//
-//  /*--- Compute Soundspeed and Velocity squared ---*/
-//  for (iSpecies = 0; iSpecies < nHeavy; iSpecies++) {
-//    conc += Mass_Frac[iSpecies]*Density/Ms[iSpecies];
-//    rhoCvtr += Density*Mass_Frac[iSpecies] * (3.0/2.0 + xi[iSpecies]/2.0) * Ru/Ms[iSpecies];
-//  }
-//  soundspeed = sqrt((1.0 + Ru/rhoCvtr*conc) * Pressure/Density);
-//
-//  Velocity2 = 0.0;
-//  for (iDim = 0; iDim < nDim; iDim++)
-//    Velocity2 += Velocity[iDim]*Velocity[iDim];
-//
-//  /*--- Non-dim. the inputs if necessary. ---*/
-//  // Need to update this portion
-//  //Temperature = Temperature/config->GetTemperature_Ref();
-//  //Pressure    = Pressure/config->GetPressure_Ref();
-//  //Density     = Density/config->GetDensity_Ref();
-//  //for (iDim = 0; iDim < nDim; iDim++)
-//  //  Velocity[iDim] = Velocity[iDim]/config->GetVelocity_Ref();
-//
-//  /*--- Compute energy (RRHO) from supplied primitive quanitites ---*/
-//  for (iSpecies = 0; iSpecies < nHeavy; iSpecies++) {
-//
-//    // Species density
-//    rhos = Mass_Frac[iSpecies]*Density;
-//
-//    // Species formation energy
-//    Ef = hf[iSpecies] - Ru/Ms[iSpecies]*Tref[iSpecies];
-//
-//    // Species vibrational energy
-//    if (thetav[iSpecies] != 0.0)
-//      Ev = Ru/Ms[iSpecies] * thetav[iSpecies] / (exp(thetav[iSpecies]/Temperature_ve)-1.0);
-//    else
-//      Ev = 0.0;
-//
-//    // Species electronic energy
-//    num = 0.0;
-//    denom = g[iSpecies][0] * exp(thetae[iSpecies][0]/Temperature_ve);
-//    for (iEl = 1; iEl < nElStates[iSpecies]; iEl++) {
-//      num   += g[iSpecies][iEl] * thetae[iSpecies][iEl] * exp(-thetae[iSpecies][iEl]/Temperature_ve);
-//      denom += g[iSpecies][iEl] * exp(-thetae[iSpecies][iEl]/Temperature_ve);
-//    }
-//    Ee = Ru/Ms[iSpecies] * (num/denom);
-//
-//    // Mixture total energy
-//    rhoE += rhos * ((3.0/2.0+xi[iSpecies]/2.0) * Ru/Ms[iSpecies] * (Temperature-Tref[iSpecies])
-//                    + Ev + Ee + Ef + 0.5*Velocity2);
-//
-//    // Mixture vibrational-electronic energy
-//    rhoEve += rhos * (Ev + Ee);
-//  }
-//
-//  /*--- Setting Conservative Variables ---*/
-//  for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
-//    U_inlet[iSpecies] = Mass_Frac[iSpecies]*Density;
-//  for (iDim = 0; iDim < nDim; iDim++)
-//    U_inlet[nSpecies+iDim] = Density*Velocity[iDim];
-//  U_inlet[nVar-2] = rhoE;
-//  U_inlet[nVar-1] = rhoEve;
-//
-//  /*--- Setting Primitive Vaariables ---*/
-//  for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
-//    V_inlet[iSpecies] = Mass_Frac[iSpecies]*Density;
-//  V_inlet[nSpecies] = Temperature;
-//  V_inlet[nSpecies+1] = Temperature_ve;
-//  for (iDim = 0; iDim < nDim; iDim++)
-//    V_inlet[nSpecies+2+iDim] = Velocity[iDim];
-//  V_inlet[nSpecies+2+nDim] = Pressure;
-//  V_inlet[nSpecies+3+nDim] = Density;
-//  V_inlet[nSpecies+4+nDim] = rhoE+Pressure/Density;
-//  V_inlet[nSpecies+5+nDim] = soundspeed;
-//  V_inlet[nSpecies+6+nDim] = rhoCvtr;
-
-/* ----------------------------------------------------------------------------- */
-/* ----------------------------------------------------------------------------- */
-/* The block of code that needs to be updated to use Fluidmodel class end here   */
-/* ----------------------------------------------------------------------------- */
-/* ----------------------------------------------------------------------------- */
-
-//  //This requires Newtown Raphson.....So this is not currently operational (See Deathstar)
-//  //V_inlet[nSpecies+7+nDim] = rhoCvve;
-//
-//  /*--- Loop over all the vertices on this boundary marker ---*/
-//  for(iVertex = 0; iVertex < geometry->nVertex[val_marker]; iVertex++) {
-//    iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
-//
-//    /*--- Check if the node belongs to the domain (i.e, not a halo node) ---*/
-//    if (geometry->nodes->GetDomain(iPoint)) {
-//
-//      /*--- Index of the closest interior node ---*/
-//      Point_Normal = geometry->vertex[val_marker][iVertex]->GetNormal_Neighbor();
-//
-//      /*--- Current solution at this boundary node ---*/
-//      for (iVar = 0; iVar < nVar; iVar++) U_domain[iVar] = nodes->GetSolution(iPoint,iVar);
-//      for (iVar = 0; iVar < nPrimVar; iVar++) V_domain[iVar] = nodes->GetPrimitive(iPoint,iVar);
-//
-//      /*--- Normal vector for this vertex (negate for outward convention) ---*/
-//      geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
-//      for (iDim = 0; iDim < nDim; iDim++) Normal[iDim] = -Normal[iDim];
-//
-//      su2double Area = 0.0;
-//      for (iDim = 0; iDim < nDim; iDim++)
-//        Area += Normal[iDim]*Normal[iDim];
-//      Area = sqrt (Area);
-//
-//      /*--- Set various quantities in the solver class ---*/
-//      conv_numerics->SetNormal(Normal);
-//      conv_numerics->SetConservative(U_domain, U_inlet);
-//      conv_numerics->SetPrimitive(V_domain, V_inlet);
-//
-//      /*--- Pass supplementary info to CNumerics ---*/
-//      conv_numerics->SetdPdU(nodes->GetdPdU(iPoint), node_infty->GetdPdU(0));
-//      conv_numerics->SetdTdU(nodes->GetdTdU(iPoint), node_infty->GetdTdU(0));
-//      conv_numerics->SetdTvedU(nodes->GetdTvedU(iPoint), node_infty->GetdTvedU(0));
-//      conv_numerics->SetEve(nodes->GetEve(iPoint), node_infty->GetEve(0));
-//      conv_numerics->SetCvve(nodes->GetCvve(iPoint), node_infty->GetCvve(0));
-//
-//      if (dynamic_grid)
-//        conv_numerics->SetGridVel(geometry->nodes->GetGridVel(iPoint),
-//                                  geometry->nodes->GetGridVel(iPoint));
-//
-//      /*--- Compute the residual using an upwind scheme ---*/
-//      auto residual = conv_numerics->ComputeResidual(config);
-//      LinSysRes.AddBlock(iPoint, residual);
-//
-//      /*--- Jacobian contribution for implicit integration ---*/
-//      //if (implicit)
-//      //  Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
-//
-//      /*--- Viscous contribution ---*/
-//      if (viscous) {
-//
-//        /*--- Set the normal vector and the coordinates ---*/
-//        visc_numerics->SetNormal(Normal);
-//        su2double Coord_Reflected[MAXNDIM];
-//        GeometryToolbox::PointPointReflect(nDim, geometry->nodes->GetCoord(Point_Normal),
-//                                           geometry->nodes->GetCoord(iPoint), Coord_Reflected);
-//        visc_numerics->SetCoord(geometry->nodes->GetCoord(iPoint), Coord_Reflected);
-//
-//        /*--- Primitive variables, and gradient ---*/
-//        visc_numerics->SetPrimitive(V_domain, V_inlet);
-//        visc_numerics->SetPrimVarGradient(nodes->GetGradient_Primitive(iPoint), nodes->GetGradient_Primitive(iPoint));
-//
-//        /*--- Laminar viscosity ---*/
-//        visc_numerics->SetLaminarViscosity(nodes->GetLaminarViscosity(iPoint), nodes->GetLaminarViscosity(iPoint));
-//
-//        /*--- Compute and update residual ---*/
-//        auto residual = visc_numerics->ComputeResidual(config);
-//        LinSysRes.SubtractBlock(iPoint, residual);
-//
-//        /*--- Jacobian contribution for implicit integration ---*/
-//        //if (implicit)
-//        //  Jacobian.SubtractBlock2Diag(iPoint, residual.Jacobian_i);
-//      }
-//
-//    }
-//  }
-//
-//  /*--- Free locally allocated memory ---*/
-//  delete [] U_domain;
-//  delete [] U_inlet;
-//  delete [] V_domain;
-//  delete [] V_inlet;
-//  delete [] Normal;
+void CNEMOEulerSolver::BC_Supersonic_Inlet(
+    CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics,
+    CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
 
-}
+  /*--- Supersonic inlet flow: there are no outgoing characteristics,
+   so all flow variables can be imposed at the inlet.
+   First, retrieve the specified values for the primitive variables. ---*/
 
-void CNEMOEulerSolver::BC_Supersonic_Outlet(CGeometry *geometry, CSolver **solver_container,
-                                            CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
-  unsigned short iDim;
-  unsigned long iVertex, iPoint;
-  su2double *V_outlet, *V_domain;
-  su2double *U_outlet, *U_domain;
+  const string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
 
-  bool implicit     = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
-  string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
+  const su2double Temperature = config->GetInlet_Temperature(Marker_Tag);
+  const su2double Pressure = config->GetInlet_Pressure(Marker_Tag);
+  const su2double *Velocity = config->GetInlet_Velocity(Marker_Tag);
+  const su2double *Mass_Frac = config->GetInlet_MassFrac();
+  su2double Temperature_ve = config->GetInlet_Temperature_ve();
 
-  su2double *Normal = new su2double[nDim];
+  /*--- If no Tve value specified (left as 0 K default), set to Ttr value ---*/
+  if (Temperature_ve == 0.0) {
+    Temperature_ve = Temperature;
+  }
 
-  /*--- Supersonic outlet flow: there are no ingoing characteristics,
-   so all flow variables can should be interpolated from the domain. ---*/
+  /*--- Set mixture state ---*/
+  FluidModel->SetTDStatePTTv(Pressure, Mass_Frac, Temperature, Temperature_ve);
 
-  /*--- Loop over all the vertices on this boundary marker ---*/
-  for (iVertex = 0; iVertex < geometry->nVertex[val_marker]; iVertex++) {
+  /*--- Compute Ma vector for flow direction ---*/
+  const su2double soundspeed = FluidModel->ComputeSoundSpeed();
 
-    iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
+  su2double Mvec[MAXNDIM] = {0.0};
 
-    /*--- Check if the node belongs to the domain (i.e, not a halo node) ---*/
-    if (geometry->nodes->GetDomain(iPoint)) {
-
-      /*--- Current solution at this boundary node ---*/
-      V_domain = nodes->GetPrimitive(iPoint);
-      U_domain = nodes->GetSolution(iPoint);
+  for (unsigned short iDim = 0; iDim < nDim; iDim++)
+    Mvec[iDim] = Velocity[iDim] / soundspeed;
 
-      /*--- Allocate the value at the outlet ---*/
-      V_outlet = GetCharacPrimVar(val_marker, iVertex);
-      V_outlet = V_domain;
-      U_outlet = U_domain;
+  /*--- Allocate inlet node to compute gradients for numerics ---*/
+  CNEMOEulerVariable node_inlet(Pressure, Mass_Frac, Mvec, Temperature,
+                                Temperature_ve, 1, nDim, nVar, nPrimVar,
+                                nPrimVarGrad, config, FluidModel);
+  node_inlet.SetPrimVar(0, FluidModel);
 
-      /*--- Normal vector for this vertex (negate for outward convention) ---*/
-      geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
-      for (iDim = 0; iDim < nDim; iDim++) Normal[iDim] = -Normal[iDim];
+  su2double Normal[MAXNDIM] = {0.0};
 
-      /*--- Set various quantities in the solver class ---*/
-      conv_numerics->SetNormal(Normal);
-      conv_numerics->SetPrimitive(V_domain, V_outlet);
-      conv_numerics->SetConservative(U_domain, U_outlet);
+  /*--- Loop over all the vertices on this boundary marker ---*/
+  for (unsigned long iVertex = 0; iVertex < geometry->nVertex[val_marker];
+       iVertex++) {
+    const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
-      /*--- Pass supplementary information to CNumerics ---*/
-      conv_numerics->SetdPdU  (nodes->GetdPdU(iPoint),   nodes->GetdPdU(iPoint));
-      conv_numerics->SetdTdU  (nodes->GetdTdU(iPoint),   nodes->GetdTdU(iPoint));
-      conv_numerics->SetdTvedU(nodes->GetdTvedU(iPoint), nodes->GetdTvedU(iPoint));
-      conv_numerics->SetEve   (nodes->GetEve(iPoint),    nodes->GetEve(iPoint));
-      conv_numerics->SetCvve  (nodes->GetCvve(iPoint),   nodes->GetCvve(iPoint));
-      conv_numerics->SetGamma (nodes->GetGamma(iPoint),  nodes->GetGamma(iPoint));
+    /*--- Check if the node belongs to the domain (i.e, not a halo node) ---*/
+    if (!geometry->nodes->GetDomain(iPoint))
+      continue;
+
+    /*--- Index of the closest interior node ---*/
+    const auto Point_Normal =
+        geometry->vertex[val_marker][iVertex]->GetNormal_Neighbor();
+
+    /*--- Normal vector for this vertex (negate for outward convention) ---*/
+    geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
+    for (unsigned short iDim = 0; iDim < nDim; iDim++)
+      Normal[iDim] = -Normal[iDim];
+
+    /*--- Set various quantities in the solver class ---*/
+    conv_numerics->SetNormal(Normal);
+    conv_numerics->SetConservative(nodes->GetSolution(iPoint),
+                                   node_inlet.GetSolution(0));
+    conv_numerics->SetPrimitive(nodes->GetPrimitive(iPoint),
+                                node_inlet.GetPrimitive(0));
+
+    /*--- Pass supplementary info to CNumerics ---*/
+    conv_numerics->SetdPdU(nodes->GetdPdU(iPoint), node_inlet.GetdPdU(0));
+    conv_numerics->SetdTdU(nodes->GetdTdU(iPoint), node_inlet.GetdTdU(0));
+    conv_numerics->SetdTvedU(nodes->GetdTvedU(iPoint), node_inlet.GetdTvedU(0));
+    conv_numerics->SetEve(nodes->GetEve(iPoint), node_inlet.GetEve(0));
+    conv_numerics->SetCvve(nodes->GetCvve(iPoint), node_inlet.GetCvve(0));
+
+    const bool dynamic_grid = config->GetGrid_Movement();
+    if (dynamic_grid)
+      conv_numerics->SetGridVel(geometry->nodes->GetGridVel(iPoint),
+                                geometry->nodes->GetGridVel(iPoint));
+
+    /*--- Compute the residual using an upwind scheme ---*/
+    auto residual = conv_numerics->ComputeResidual(config);
+    LinSysRes.AddBlock(iPoint, residual);
+
+    /*--- Jacobian contribution for implicit integration ---*/
+    const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+    if (implicit)
+      Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
+
+    /*--- Viscous contribution ---*/
+    bool viscous = config->GetViscous();
+    if (viscous) {
 
-      if (dynamic_grid)
-        conv_numerics->SetGridVel(geometry->nodes->GetGridVel(iPoint),
-                                  geometry->nodes->GetGridVel(iPoint));
+      /*--- Set the normal vector and the coordinates ---*/
+      su2double Coord_Reflected[MAXNDIM];
+      GeometryToolbox::PointPointReflect(
+          nDim, geometry->nodes->GetCoord(Point_Normal),
+          geometry->nodes->GetCoord(iPoint), Coord_Reflected);
+      visc_numerics->SetCoord(geometry->nodes->GetCoord(iPoint),
+                              Coord_Reflected);
+      visc_numerics->SetNormal(Normal);
+
+      /*--- Primitive variables, and gradient ---*/
+      visc_numerics->SetConservative(nodes->GetSolution(iPoint),
+                                     node_inlet.GetSolution(0));
+      visc_numerics->SetPrimitive(nodes->GetPrimitive(iPoint),
+                                  node_inlet.GetPrimitive(0));
+      visc_numerics->SetPrimVarGradient(nodes->GetGradient_Primitive(iPoint),
+                                        node_inlet.GetGradient_Primitive(0));
 
-      /*--- Compute the residual using an upwind scheme ---*/
-      auto residual = conv_numerics->ComputeResidual(config);
-      LinSysRes.AddBlock(iPoint, residual);
+      /*--- Pass supplementary information to CNumerics ---*/
+      visc_numerics->SetdPdU(nodes->GetdPdU(iPoint), node_inlet.GetdPdU(0));
+      visc_numerics->SetdTdU(nodes->GetdTdU(iPoint), node_inlet.GetdTdU(0));
+      visc_numerics->SetdTvedU(nodes->GetdTvedU(iPoint),
+                               node_inlet.GetdTvedU(0));
+      visc_numerics->SetEve(nodes->GetEve(iPoint), node_inlet.GetEve(0));
+      visc_numerics->SetCvve(nodes->GetCvve(iPoint), node_inlet.GetCvve(0));
+
+      /*--- Species diffusion coefficients ---*/
+      visc_numerics->SetDiffusionCoeff(nodes->GetDiffusionCoeff(iPoint),
+                                       nodes->GetDiffusionCoeff(iPoint));
+      /*--- Laminar viscosity ---*/
+      visc_numerics->SetLaminarViscosity(nodes->GetLaminarViscosity(iPoint),
+                                         nodes->GetLaminarViscosity(iPoint));
+      /*--- Eddy viscosity ---*/
+      visc_numerics->SetEddyViscosity(nodes->GetEddyViscosity(iPoint),
+                                      nodes->GetEddyViscosity(iPoint));
+      /*--- Thermal conductivity ---*/
+      visc_numerics->SetThermalConductivity(
+          nodes->GetThermalConductivity(iPoint),
+          nodes->GetThermalConductivity(iPoint));
+      /*--- Vib-el. thermal conductivity ---*/
+      visc_numerics->SetThermalConductivity_ve(
+          nodes->GetThermalConductivity_ve(iPoint),
+          nodes->GetThermalConductivity_ve(iPoint));
+
+      /*--- Compute and update residual ---*/
+      auto residual = visc_numerics->ComputeResidual(config);
+      LinSysRes.SubtractBlock(iPoint, residual);
 
       /*--- Jacobian contribution for implicit integration ---*/
       if (implicit)
-        Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
+        Jacobian.SubtractBlock2Diag(iPoint, residual.jacobian_i);
     }
   }
+}
 
-  /*--- Free locally allocated memory ---*/
-  delete [] Normal;
+void CNEMOEulerSolver::BC_Supersonic_Outlet(
+    CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics,
+    CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
+
+  /*--- Supersonic outlet flow: there are no ingoing characteristics,
+   so all flow variables can should be interpolated from the domain. ---*/
 
+  su2double Normal[MAXNDIM] = {0.0};
+
+  const string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
+
+  /*--- Loop over all the vertices on this boundary marker ---*/
+  for (unsigned long iVertex = 0; iVertex < geometry->nVertex[val_marker];
+       iVertex++) {
+
+    const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
+
+    /*--- Check if the node belongs to the domain (i.e, not a halo node) ---*/
+    if (!geometry->nodes->GetDomain(iPoint))
+      continue;
+
+    /*--- Normal vector for this vertex (negate for outward convention) ---*/
+    geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
+    for (unsigned short iDim = 0; iDim < nDim; iDim++)
+      Normal[iDim] = -Normal[iDim];
+
+    /*--- Set various quantities in the solver class, outlet properties are
+     * equal to domain properties ---*/
+    conv_numerics->SetNormal(Normal);
+    conv_numerics->SetPrimitive(nodes->GetPrimitive(iPoint),
+                                nodes->GetPrimitive(iPoint));
+    conv_numerics->SetConservative(nodes->GetSolution(iPoint),
+                                   nodes->GetSolution(iPoint));
+
+    /*--- Pass supplementary information to CNumerics ---*/
+    conv_numerics->SetdPdU(nodes->GetdPdU(iPoint), nodes->GetdPdU(iPoint));
+    conv_numerics->SetdTdU(nodes->GetdTdU(iPoint), nodes->GetdTdU(iPoint));
+    conv_numerics->SetdTvedU(nodes->GetdTvedU(iPoint),
+                             nodes->GetdTvedU(iPoint));
+    conv_numerics->SetEve(nodes->GetEve(iPoint), nodes->GetEve(iPoint));
+    conv_numerics->SetCvve(nodes->GetCvve(iPoint), nodes->GetCvve(iPoint));
+    conv_numerics->SetGamma(nodes->GetGamma(iPoint), nodes->GetGamma(iPoint));
+
+    const bool dynamic_grid = config->GetGrid_Movement();
+    if (dynamic_grid)
+      conv_numerics->SetGridVel(geometry->nodes->GetGridVel(iPoint),
+                                geometry->nodes->GetGridVel(iPoint));
+
+    /*--- Compute the residual using an upwind scheme ---*/
+    auto residual = conv_numerics->ComputeResidual(config);
+    LinSysRes.AddBlock(iPoint, residual);
+
+    /*--- Jacobian contribution for implicit integration ---*/
+    const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+    if (implicit)
+      Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
+  }
 }
 
 void CNEMOEulerSolver::SetPressureDiffusionSensor(CGeometry *geometry, CConfig *config) {
diff --git a/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg b/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg
index 49bda853bcd..6cceb3d0f44 100644
--- a/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg
+++ b/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg
@@ -46,7 +46,7 @@ CFL_NUMBER= 5.0
 CFL_ADAPT= NO
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-ITER= 150
+ITER= 100
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %

From 98507bc79d2c8529a8ff67e1005dd60e4253d85a Mon Sep 17 00:00:00 2001
From: Nijso <bigfootedrockmidget@hotmail.com>
Date: Sat, 11 Feb 2023 14:40:11 +0100
Subject: [PATCH 190/656] Write Z-Velocity and temperature only when solved
 (#1920)

* fix 3D and temperature output
---
 SU2_CFD/src/output/CAdjFlowCompOutput.cpp |  39 ++++----
 SU2_CFD/src/output/CAdjFlowIncOutput.cpp  | 107 +++++++++++++---------
 TestCases/parallel_regression_AD.py       |   8 +-
 TestCases/serial_regression_AD.py         |   4 +-
 4 files changed, 91 insertions(+), 67 deletions(-)

diff --git a/SU2_CFD/src/output/CAdjFlowCompOutput.cpp b/SU2_CFD/src/output/CAdjFlowCompOutput.cpp
index 3f15fdf4910..3125e783b47 100644
--- a/SU2_CFD/src/output/CAdjFlowCompOutput.cpp
+++ b/SU2_CFD/src/output/CAdjFlowCompOutput.cpp
@@ -35,14 +35,14 @@ CAdjFlowCompOutput::CAdjFlowCompOutput(CConfig *config, unsigned short nDim) : C
 
   /*--- Set the default history fields if nothing is set in the config file ---*/
 
-  if (nRequestedHistoryFields == 0){
+  if (nRequestedHistoryFields == 0) {
     requestedHistoryFields.emplace_back("ITER");
     requestedHistoryFields.emplace_back("RMS_RES");
     requestedHistoryFields.emplace_back("SENSITIVITY");
     nRequestedHistoryFields = requestedHistoryFields.size();
   }
 
-  if (nRequestedScreenFields == 0){
+  if (nRequestedScreenFields == 0) {
     if (config->GetTime_Domain()) requestedScreenFields.emplace_back("TIME_ITER");
     if (multiZone) requestedScreenFields.emplace_back("OUTER_ITER");
     requestedScreenFields.emplace_back("INNER_ITER");
@@ -53,7 +53,7 @@ CAdjFlowCompOutput::CAdjFlowCompOutput(CConfig *config, unsigned short nDim) : C
     nRequestedScreenFields = requestedScreenFields.size();
   }
 
-  if (nRequestedVolumeFields == 0){
+  if (nRequestedVolumeFields == 0) {
     requestedVolumeFields.emplace_back("COORDINATES");
     requestedVolumeFields.emplace_back("SOLUTION");
     requestedVolumeFields.emplace_back("SENSITIVITY");
@@ -93,7 +93,7 @@ CAdjFlowCompOutput::CAdjFlowCompOutput(CConfig *config, unsigned short nDim) : C
 
 CAdjFlowCompOutput::~CAdjFlowCompOutput(void) {}
 
-void CAdjFlowCompOutput::SetHistoryOutputFields(CConfig *config){
+void CAdjFlowCompOutput::SetHistoryOutputFields(CConfig *config) {
 
   /// BEGIN_GROUP: RMS_RES, DESCRIPTION: The root-mean-square residuals of the SOLUTION variables.
   /// DESCRIPTION: Root-mean square residual of the adjoint density.
@@ -103,10 +103,13 @@ void CAdjFlowCompOutput::SetHistoryOutputFields(CConfig *config){
   /// DESCRIPTION: Root-mean square residual of the adjoint momentum y-component.
   AddHistoryOutput("RMS_ADJ_MOMENTUM-Y", "rms[A_RhoV]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the adjoint momentum y-component.", HistoryFieldType::RESIDUAL);
   /// DESCRIPTION: Root-mean square residual of the adjoint momentum z-component.
-  AddHistoryOutput("RMS_ADJ_MOMENTUM-Z", "rms[A_RhoW]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the adjoint momentum z-component.", HistoryFieldType::RESIDUAL);
+  if (nDim == 3) {
+    AddHistoryOutput("RMS_ADJ_MOMENTUM-Z", "rms[A_RhoW]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the adjoint momentum z-component.", HistoryFieldType::RESIDUAL);
+  }
   /// DESCRIPTION: Root-mean square residual of the adjoint energy.
   AddHistoryOutput("RMS_ADJ_ENERGY",     "rms[A_E]",    ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the adjoint energy.", HistoryFieldType::RESIDUAL);
 
+
   AddHistoryOutputFields_AdjScalarRMS_RES(config);
   /// END_GROUP
 
@@ -118,7 +121,9 @@ void CAdjFlowCompOutput::SetHistoryOutputFields(CConfig *config){
   /// DESCRIPTION: Maximum residual of the adjoint momentum y-component
   AddHistoryOutput("MAX_ADJ_MOMENTUM-Y", "max[A_RhoV]", ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the adjoint momentum y-component", HistoryFieldType::RESIDUAL);
   /// DESCRIPTION: Maximum residual of the adjoint momentum z-component
-  AddHistoryOutput("MAX_ADJ_MOMENTUM-Z", "max[A_RhoW]", ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the adjoint momentum z-component", HistoryFieldType::RESIDUAL);
+  if (nDim == 3) {
+    AddHistoryOutput("MAX_ADJ_MOMENTUM-Z", "max[A_RhoW]", ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the adjoint momentum z-component", HistoryFieldType::RESIDUAL);
+  }
   /// DESCRIPTION: Maximum residual of the adjoint energy.
   AddHistoryOutput("MAX_ADJ_ENERGY",     "max[A_E]",    ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the adjoint energy.", HistoryFieldType::RESIDUAL);
 
@@ -134,7 +139,9 @@ void CAdjFlowCompOutput::SetHistoryOutputFields(CConfig *config){
   /// DESCRIPTION: BGS residual of the adjoint momentum y-component
   AddHistoryOutput("BGS_ADJ_MOMENTUM-Y", "bgs[A_RhoV]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the adjoint momentum y-component", HistoryFieldType::RESIDUAL);
   /// DESCRIPTION: BGS residual of the adjoint momentum z-component
-  AddHistoryOutput("BGS_ADJ_MOMENTUM-Z", "bgs[A_RhoW]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the adjoint momentum z-component", HistoryFieldType::RESIDUAL);
+  if (nDim == 3) {
+    AddHistoryOutput("BGS_ADJ_MOMENTUM-Z", "bgs[A_RhoW]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the adjoint momentum z-component", HistoryFieldType::RESIDUAL);
+  }
   /// DESCRIPTION: BGS residual of the adjoint energy.
   AddHistoryOutput("BGS_ADJ_ENERGY",     "bgs[A_E]",    ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the adjoint energy.", HistoryFieldType::RESIDUAL);
 
@@ -159,14 +166,14 @@ void CAdjFlowCompOutput::SetHistoryOutputFields(CConfig *config){
 
   AddHistoryOutputFields_AdjScalarLinsol(config);
 
-  if (config->GetDeform_Mesh()){
+  if (config->GetDeform_Mesh()) {
     AddHistoryOutput("DEFORM_ITER", "DeformIter", ScreenOutputFormat::INTEGER, "DEFORM", "Linear solver iterations for the mesh deformation");
     AddHistoryOutput("DEFORM_RESIDUAL", "DeformRes", ScreenOutputFormat::FIXED, "DEFORM", "Residual of the linear solver for the mesh deformation");
   }
 
 }
 
-void CAdjFlowCompOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, CSolver **solver){
+void CAdjFlowCompOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, CSolver **solver) {
 
   CSolver* adjflow_solver = solver[ADJFLOW_SOL];
   CSolver* mesh_solver = solver[MESH_SOL];
@@ -191,7 +198,7 @@ void CAdjFlowCompOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, C
     SetHistoryOutputValue("MAX_ADJ_ENERGY", log10(adjflow_solver->GetRes_Max(3)));
   }
 
-  if (multiZone){
+  if (multiZone) {
     SetHistoryOutputValue("BGS_ADJ_DENSITY", log10(adjflow_solver->GetRes_BGS(0)));
     SetHistoryOutputValue("BGS_ADJ_MOMENTUM-X", log10(adjflow_solver->GetRes_BGS(1)));
     SetHistoryOutputValue("BGS_ADJ_MOMENTUM-Y", log10(adjflow_solver->GetRes_BGS(2)));
@@ -220,7 +227,7 @@ void CAdjFlowCompOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, C
   LoadHistoryData_AdjScalar(config, solver);
 }
 
-void CAdjFlowCompOutput::SetVolumeOutputFields(CConfig *config){
+void CAdjFlowCompOutput::SetVolumeOutputFields(CConfig *config) {
 
   // Grid coordinates
   AddVolumeOutput("COORD-X", "x", "COORDINATES", "x-component of the coordinate vector");
@@ -274,7 +281,7 @@ void CAdjFlowCompOutput::SetVolumeOutputFields(CConfig *config){
 
 }
 
-void CAdjFlowCompOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolver **solver, unsigned long iPoint){
+void CAdjFlowCompOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolver **solver, unsigned long iPoint) {
 
   CVariable* Node_AdjFlow = solver[ADJFLOW_SOL]->GetNodes();
   CPoint*    Node_Geo     = geometry->nodes;
@@ -287,7 +294,7 @@ void CAdjFlowCompOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CS
   SetVolumeOutputValue("ADJ_DENSITY",    iPoint, Node_AdjFlow->GetSolution(iPoint, 0));
   SetVolumeOutputValue("ADJ_MOMENTUM-X", iPoint, Node_AdjFlow->GetSolution(iPoint, 1));
   SetVolumeOutputValue("ADJ_MOMENTUM-Y", iPoint, Node_AdjFlow->GetSolution(iPoint, 2));
-  if (nDim == 3){
+  if (nDim == 3) {
     SetVolumeOutputValue("ADJ_MOMENTUM-Z", iPoint, Node_AdjFlow->GetSolution(iPoint, 3));
     SetVolumeOutputValue("ADJ_ENERGY",     iPoint, Node_AdjFlow->GetSolution(iPoint, 4));
   } else {
@@ -298,7 +305,7 @@ void CAdjFlowCompOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CS
   SetVolumeOutputValue("RES_ADJ_DENSITY",    iPoint, Node_AdjFlow->GetSolution(iPoint, 0) - Node_AdjFlow->GetSolution_Old(iPoint, 0));
   SetVolumeOutputValue("RES_ADJ_MOMENTUM-X", iPoint, Node_AdjFlow->GetSolution(iPoint, 1) - Node_AdjFlow->GetSolution_Old(iPoint, 1));
   SetVolumeOutputValue("RES_ADJ_MOMENTUM-Y", iPoint, Node_AdjFlow->GetSolution(iPoint, 2) - Node_AdjFlow->GetSolution_Old(iPoint, 2));
-  if (nDim == 3){
+  if (nDim == 3) {
     SetVolumeOutputValue("RES_ADJ_MOMENTUM-Z", iPoint, Node_AdjFlow->GetSolution(iPoint, 3) - Node_AdjFlow->GetSolution_Old(iPoint, 3));
     SetVolumeOutputValue("RES_ADJ_ENERGY",     iPoint, Node_AdjFlow->GetSolution(iPoint, 4) - Node_AdjFlow->GetSolution_Old(iPoint, 4));
   } else {
@@ -313,14 +320,14 @@ void CAdjFlowCompOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CS
   LoadVolumeData_AdjScalar(config, solver, iPoint);
 }
 
-void CAdjFlowCompOutput::LoadSurfaceData(CConfig *config, CGeometry *geometry, CSolver **solver, unsigned long iPoint, unsigned short iMarker, unsigned long iVertex){
+void CAdjFlowCompOutput::LoadSurfaceData(CConfig *config, CGeometry *geometry, CSolver **solver, unsigned long iPoint, unsigned short iMarker, unsigned long iVertex) {
 
   SetVolumeOutputValue("SENSITIVITY", iPoint, solver[ADJFLOW_SOL]->GetCSensitivity(iMarker, iVertex));
 
 }
 
 
-bool CAdjFlowCompOutput::SetInit_Residuals(const CConfig *config){
+bool CAdjFlowCompOutput::SetInit_Residuals(const CConfig *config) {
 
   return ((config->GetTime_Marching() != TIME_MARCHING::STEADY) && (curInnerIter == 0)) ||
          ((config->GetTime_Marching() == TIME_MARCHING::STEADY) && (curInnerIter < 2));
diff --git a/SU2_CFD/src/output/CAdjFlowIncOutput.cpp b/SU2_CFD/src/output/CAdjFlowIncOutput.cpp
index 74dfbebcfd1..a87d03aa6cf 100644
--- a/SU2_CFD/src/output/CAdjFlowIncOutput.cpp
+++ b/SU2_CFD/src/output/CAdjFlowIncOutput.cpp
@@ -41,14 +41,14 @@ CAdjFlowIncOutput::CAdjFlowIncOutput(CConfig *config, unsigned short nDim) : CAd
 
   /*--- Set the default history fields if nothing is set in the config file ---*/
 
-  if (nRequestedHistoryFields == 0){
+  if (nRequestedHistoryFields == 0) {
     requestedHistoryFields.emplace_back("ITER");
     requestedHistoryFields.emplace_back("RMS_RES");
     requestedHistoryFields.emplace_back("SENSITIVITY");
     nRequestedHistoryFields = requestedHistoryFields.size();
   }
 
-  if (nRequestedScreenFields == 0){
+  if (nRequestedScreenFields == 0) {
     if (config->GetTime_Domain()) requestedScreenFields.emplace_back("TIME_ITER");
     if (multiZone) requestedScreenFields.emplace_back("OUTER_ITER");
     requestedScreenFields.emplace_back("INNER_ITER");
@@ -59,7 +59,7 @@ CAdjFlowIncOutput::CAdjFlowIncOutput(CConfig *config, unsigned short nDim) : CAd
     nRequestedScreenFields = requestedScreenFields.size();
   }
 
-  if (nRequestedVolumeFields == 0){
+  if (nRequestedVolumeFields == 0) {
     requestedVolumeFields.emplace_back("COORDINATES");
     requestedVolumeFields.emplace_back("SOLUTION");
     requestedVolumeFields.emplace_back("SENSITIVITY");
@@ -99,7 +99,7 @@ CAdjFlowIncOutput::CAdjFlowIncOutput(CConfig *config, unsigned short nDim) : CAd
 
 CAdjFlowIncOutput::~CAdjFlowIncOutput(void) {}
 
-void CAdjFlowIncOutput::SetHistoryOutputFields(CConfig *config){
+void CAdjFlowIncOutput::SetHistoryOutputFields(CConfig *config) {
 
   /// BEGIN_GROUP: RMS_RES, DESCRIPTION: The root-mean-square residuals of the SOLUTION variables.
   /// DESCRIPTION: Root-mean square residual of the adjoint Pressure.
@@ -109,9 +109,13 @@ void CAdjFlowIncOutput::SetHistoryOutputFields(CConfig *config){
   /// DESCRIPTION: Root-mean square residual of the adjoint Velocity y-component.
   AddHistoryOutput("RMS_ADJ_VELOCITY-Y", "rms[A_V]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the adjoint Velocity y-component.", HistoryFieldType::RESIDUAL);
   /// DESCRIPTION: Root-mean square residual of the adjoint Velocity z-component.
-  AddHistoryOutput("RMS_ADJ_VELOCITY-Z", "rms[A_W]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the adjoint Velocity z-component.", HistoryFieldType::RESIDUAL);
+  if (nDim == 3) {
+    AddHistoryOutput("RMS_ADJ_VELOCITY-Z", "rms[A_W]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the adjoint Velocity z-component.", HistoryFieldType::RESIDUAL);
+  }
   /// DESCRIPTION: Maximum residual of the temperature.
-  AddHistoryOutput("RMS_ADJ_TEMPERATURE", "rms[A_T]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the adjoint temperature.", HistoryFieldType::RESIDUAL);
+  if (heat || weakly_coupled_heat) {
+    AddHistoryOutput("RMS_ADJ_TEMPERATURE", "rms[A_T]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the adjoint temperature.", HistoryFieldType::RESIDUAL);
+  }
 
   if (config->GetKind_Streamwise_Periodic() == ENUM_STREAMWISE_PERIODIC::MASSFLOW) {
     AddHistoryOutput("ADJOINT_SOLEXTRA", "Adjoint_SolExtra", ScreenOutputFormat::FIXED, "ADJOINT_SOLEXTRA", "Adjoint value of the first extra Solution.", HistoryFieldType::COEFFICIENT);
@@ -119,7 +123,7 @@ void CAdjFlowIncOutput::SetHistoryOutputFields(CConfig *config){
 
   AddHistoryOutputFields_AdjScalarRMS_RES(config);
 
-  if (config->AddRadiation()){
+  if (config->AddRadiation()) {
     /// DESCRIPTION: Root-mean square residual of the adjoint radiative energy tilde.
     AddHistoryOutput("RMS_ADJ_RAD_ENERGY", "rms[A_P1]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the P1 radiative energy.",HistoryFieldType::RESIDUAL);
   }
@@ -133,9 +137,13 @@ void CAdjFlowIncOutput::SetHistoryOutputFields(CConfig *config){
   /// DESCRIPTION: Maximum residual of the adjoint Velocity y-component
   AddHistoryOutput("MAX_ADJ_VELOCITY-Y", "max[A_RhoV]", ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the adjoint Velocity y-component", HistoryFieldType::RESIDUAL);
   /// DESCRIPTION: Maximum residual of the adjoint Velocity z-component
-  AddHistoryOutput("MAX_ADJ_VELOCITY-Z", "max[A_RhoW]", ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the adjoint Velocity z-component", HistoryFieldType::RESIDUAL);
+  if (nDim == 3) {
+    AddHistoryOutput("MAX_ADJ_VELOCITY-Z", "max[A_RhoW]", ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the adjoint Velocity z-component", HistoryFieldType::RESIDUAL);
+  }
   /// DESCRIPTION: Maximum residual of the temperature.
-  AddHistoryOutput("MAX_ADJ_TEMPERATURE", "max[A_T]", ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the temperature.", HistoryFieldType::RESIDUAL);
+  if (heat || weakly_coupled_heat) {
+    AddHistoryOutput("MAX_ADJ_TEMPERATURE", "max[A_T]", ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the temperature.", HistoryFieldType::RESIDUAL);
+  }
 
   AddHistoryOutputFields_AdjScalarMAX_RES(config);
   /// END_GROUP
@@ -148,13 +156,17 @@ void CAdjFlowIncOutput::SetHistoryOutputFields(CConfig *config){
   /// DESCRIPTION: BGS residual of the adjoint Velocity y-component
   AddHistoryOutput("BGS_ADJ_VELOCITY-Y", "bgs[A_RhoV]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the adjoint Velocity y-component", HistoryFieldType::RESIDUAL);
   /// DESCRIPTION: BGS residual of the adjoint Velocity z-component
-  AddHistoryOutput("BGS_ADJ_VELOCITY-Z", "bgs[A_RhoW]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the adjoint Velocity z-component", HistoryFieldType::RESIDUAL);
+  if (nDim == 3) {
+    AddHistoryOutput("BGS_ADJ_VELOCITY-Z", "bgs[A_RhoW]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the adjoint Velocity z-component", HistoryFieldType::RESIDUAL);
+  }
   /// DESCRIPTION: BGS residual of the temperature.
-  AddHistoryOutput("BGS_ADJ_TEMPERATURE", "bgs[A_T]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the adjoint temperature.", HistoryFieldType::RESIDUAL);
+  if (heat || weakly_coupled_heat) {
+    AddHistoryOutput("BGS_ADJ_TEMPERATURE", "bgs[A_T]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the adjoint temperature.", HistoryFieldType::RESIDUAL);
+  }
 
   AddHistoryOutputFields_AdjScalarBGS_RES(config);
 
-  if (config->AddRadiation()){
+  if (config->AddRadiation()) {
     /// DESCRIPTION: Root-mean square residual of the adjoint radiative energy tilde.
     AddHistoryOutput("BGS_ADJ_RAD_ENERGY", "bgs[A_P1]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual  of the P1 radiative energy.",HistoryFieldType::RESIDUAL);
   }
@@ -178,7 +190,7 @@ void CAdjFlowIncOutput::SetHistoryOutputFields(CConfig *config){
 
   AddHistoryOutputFields_AdjScalarLinsol(config);
 
-  if (config->GetDeform_Mesh()){
+  if (config->GetDeform_Mesh()) {
     AddHistoryOutput("DEFORM_ITER", "DeformIter", ScreenOutputFormat::INTEGER, "DEFORM", "Linear solver iterations for the mesh deformation");
     AddHistoryOutput("DEFORM_RESIDUAL", "DeformRes", ScreenOutputFormat::FIXED, "DEFORM", "Residual of the linear solver for the mesh deformation");
   }
@@ -198,15 +210,15 @@ void CAdjFlowIncOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, CS
   if (nDim == 3) {
     SetHistoryOutputValue("RMS_ADJ_VELOCITY-Z", log10(adjflow_solver->GetRes_RMS(3)));
   }
-  if (weakly_coupled_heat){
+  if (weakly_coupled_heat) {
     SetHistoryOutputValue("RMS_ADJ_TEMPERATURE",         log10(adjheat_solver->GetRes_RMS(0)));
   }
-  if (heat){
+  if (heat) {
     if (nDim == 3) SetHistoryOutputValue("RMS_ADJ_TEMPERATURE",         log10(adjflow_solver->GetRes_RMS(4)));
     else           SetHistoryOutputValue("RMS_ADJ_TEMPERATURE",         log10(adjflow_solver->GetRes_RMS(3)));
   }
 
-  if (config->AddRadiation()){
+  if (config->AddRadiation()) {
     SetHistoryOutputValue("RMS_ADJ_RAD_ENERGY", log10(adjrad_solver->GetRes_RMS(0)));
   }
 
@@ -220,30 +232,30 @@ void CAdjFlowIncOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, CS
   if (nDim == 3) {
     SetHistoryOutputValue("MAX_ADJ_VELOCITY-Z", log10(adjflow_solver->GetRes_Max(3)));
   }
-  if (weakly_coupled_heat){
+  if (weakly_coupled_heat) {
     SetHistoryOutputValue("MAX_ADJ_TEMPERATURE",         log10(adjheat_solver->GetRes_Max(0)));
   }
-  if (heat){
+  if (heat) {
     if (nDim == 3) SetHistoryOutputValue("MAX_ADJ_TEMPERATURE",         log10(adjflow_solver->GetRes_Max(4)));
     else           SetHistoryOutputValue("MAX_ADJ_TEMPERATURE",         log10(adjflow_solver->GetRes_Max(3)));
   }
 
-  if (multiZone){
+  if (multiZone) {
     SetHistoryOutputValue("BGS_ADJ_PRESSURE", log10(adjflow_solver->GetRes_BGS(0)));
     SetHistoryOutputValue("BGS_ADJ_VELOCITY-X", log10(adjflow_solver->GetRes_BGS(1)));
     SetHistoryOutputValue("BGS_ADJ_VELOCITY-Y", log10(adjflow_solver->GetRes_BGS(2)));
     if (nDim == 3) {
       SetHistoryOutputValue("BGS_ADJ_VELOCITY-Z", log10(adjflow_solver->GetRes_BGS(3)));
     }
-    if (weakly_coupled_heat){
+    if (weakly_coupled_heat) {
       SetHistoryOutputValue("BGS_ADJ_TEMPERATURE",         log10(adjheat_solver->GetRes_BGS(0)));
     }
-    if (heat){
+    if (heat) {
       if (nDim == 3) SetHistoryOutputValue("BGS_ADJ_TEMPERATURE",         log10(adjflow_solver->GetRes_BGS(4)));
       else           SetHistoryOutputValue("BGS_ADJ_TEMPERATURE",         log10(adjflow_solver->GetRes_BGS(3)));
     }
 
-    if (config->AddRadiation()){
+    if (config->AddRadiation()) {
       SetHistoryOutputValue("BGS_ADJ_RAD_ENERGY", log10(adjrad_solver->GetRes_BGS(0)));
     }
   }
@@ -265,15 +277,15 @@ void CAdjFlowIncOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, CS
   LoadHistoryData_AdjScalar(config, solver);
 }
 
-void CAdjFlowIncOutput::SetVolumeOutputFields(CConfig *config){
+void CAdjFlowIncOutput::SetVolumeOutputFields(CConfig *config) {
 
 
   // Grid coordinates
   AddVolumeOutput("COORD-X", "x", "COORDINATES", "x-component of the coordinate vector");
   AddVolumeOutput("COORD-Y", "y", "COORDINATES", "y-component of the coordinate vector");
-  if (nDim == 3)
+  if (nDim == 3) {
     AddVolumeOutput("COORD-Z", "z", "COORDINATES", "z-component of the coordinate vector");
-
+  }
   /// BEGIN_GROUP: SOLUTION, DESCRIPTION: The SOLUTION variables of the adjoint solver.
   /// DESCRIPTION: Adjoint Pressure.
   AddVolumeOutput("ADJ_PRESSURE",    "Adjoint_Pressure",    "SOLUTION", "Adjoint pressure");
@@ -281,25 +293,26 @@ void CAdjFlowIncOutput::SetVolumeOutputFields(CConfig *config){
   AddVolumeOutput("ADJ_VELOCITY-X", "Adjoint_Velocity_x", "SOLUTION", "x-component of the adjoint velocity vector");
   /// DESCRIPTION: Adjoint Velocity y-component.
   AddVolumeOutput("ADJ_VELOCITY-Y", "Adjoint_Velocity_y", "SOLUTION", "y-component of the adjoint velocity vector");
-  if (nDim == 3)
+  if (nDim == 3) {
     /// DESCRIPTION: Adjoint Velocity z-component.
     AddVolumeOutput("ADJ_VELOCITY-Z", "Adjoint_Velocity_z", "SOLUTION", "z-component of the adjoint velocity vector");
-
+  }
   AddVolumeOutput("ADJ_TEMPERATURE", "Adjoint_Temperature", "SOLUTION",  "Adjoint temperature");
 
   SetVolumeOutputFields_AdjScalarSolution(config);
 
-  if (config->AddRadiation()){
+  if (config->AddRadiation()) {
     AddVolumeOutput("ADJ_P1_ENERGY",  "Adjoint_Energy(P1)", "SOLUTION", "Adjoint radiative energy");
   }
   /// END_GROUP
 
   // Grid velocity
-  if (config->GetDynamic_Grid()){
+  if (config->GetDynamic_Grid()) {
     AddVolumeOutput("GRID_VELOCITY-X", "Grid_Velocity_x", "GRID_VELOCITY", "x-component of the grid velocity vector");
     AddVolumeOutput("GRID_VELOCITY-Y", "Grid_Velocity_y", "GRID_VELOCITY", "y-component of the grid velocity vector");
-    if (nDim == 3 )
+    if (nDim == 3 ) {
       AddVolumeOutput("GRID_VELOCITY-Z", "Grid_Velocity_z", "GRID_VELOCITY", "z-component of the grid velocity vector");
+    }
   }
 
   /// BEGIN_GROUP: RESIDUAL, DESCRIPTION: Residuals of the SOLUTION variables.
@@ -309,15 +322,16 @@ void CAdjFlowIncOutput::SetVolumeOutputFields(CConfig *config){
   AddVolumeOutput("RES_ADJ_VELOCITY-X", "Residual_Adjoint_Velocity_x", "RESIDUAL", "Residual of the adjoint x-velocity");
   /// DESCRIPTION: Residual of the adjoint Velocity y-component.
   AddVolumeOutput("RES_ADJ_VELOCITY-Y", "Residual_Adjoint_Velocity_y", "RESIDUAL", "Residual of the adjoint y-velocity");
-  if (nDim == 3)
+  if (nDim == 3) {
     /// DESCRIPTION: Residual of the adjoint Velocity z-component.
     AddVolumeOutput("RES_ADJ_VELOCITY-Z", "Residual_Adjoint_Velocity_z", "RESIDUAL", "Residual of the adjoint z-velocity");
+  }
   /// DESCRIPTION: Residual of the adjoint energy.
   AddVolumeOutput("RES_ADJ_TEMPERATURE", "Residual_Adjoint_Heat", "RESIDUAL", "Residual of the adjoint temperature");
 
   SetVolumeOutputFields_AdjScalarResidual(config);
 
-  if (config->AddRadiation()){
+  if (config->AddRadiation()) {
     AddVolumeOutput("RES_P1_ENERGY",  "Residual_Adjoint_Energy_P1", "RESIDUAL", "Residual of adjoint radiative energy");
   }
   /// END_GROUP
@@ -327,42 +341,44 @@ void CAdjFlowIncOutput::SetVolumeOutputFields(CConfig *config){
   AddVolumeOutput("SENSITIVITY-X", "Sensitivity_x", "SENSITIVITY", "x-component of the sensitivity vector");
   /// DESCRIPTION: Sensitivity y-component.
   AddVolumeOutput("SENSITIVITY-Y", "Sensitivity_y", "SENSITIVITY", "y-component of the sensitivity vector");
-  if (nDim == 3)
+  if (nDim == 3) {
     /// DESCRIPTION: Sensitivity z-component.
     AddVolumeOutput("SENSITIVITY-Z", "Sensitivity_z", "SENSITIVITY", "z-component of the sensitivity vector");
+  }
   /// DESCRIPTION: Sensitivity in normal direction.
   AddVolumeOutput("SENSITIVITY", "Surface_Sensitivity", "SENSITIVITY", "sensitivity in normal direction");
   /// END_GROUP
 
 }
 
-void CAdjFlowIncOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolver **solver, unsigned long iPoint){
+void CAdjFlowIncOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolver **solver, unsigned long iPoint) {
 
   CVariable* Node_AdjFlow = solver[ADJFLOW_SOL]->GetNodes();
   CVariable* Node_AdjHeat = nullptr;
   CVariable* Node_AdjRad  = nullptr;
   CPoint*    Node_Geo     = geometry->nodes;
 
-  if (weakly_coupled_heat){
+  if (weakly_coupled_heat) {
     Node_AdjHeat = solver[ADJHEAT_SOL]->GetNodes();
   }
-  if (config->GetKind_RadiationModel() != RADIATION_MODEL::NONE){
+  if (config->GetKind_RadiationModel() != RADIATION_MODEL::NONE) {
     Node_AdjRad = solver[ADJRAD_SOL]->GetNodes();
   }
 
   SetVolumeOutputValue("COORD-X", iPoint,  Node_Geo->GetCoord(iPoint, 0));
   SetVolumeOutputValue("COORD-Y", iPoint,  Node_Geo->GetCoord(iPoint, 1));
-  if (nDim == 3)
+  if (nDim == 3) {
     SetVolumeOutputValue("COORD-Z", iPoint, Node_Geo->GetCoord(iPoint, 2));
+  }
 
   SetVolumeOutputValue("ADJ_PRESSURE",   iPoint, Node_AdjFlow->GetSolution(iPoint, 0));
   SetVolumeOutputValue("ADJ_VELOCITY-X", iPoint, Node_AdjFlow->GetSolution(iPoint, 1));
   SetVolumeOutputValue("ADJ_VELOCITY-Y", iPoint, Node_AdjFlow->GetSolution(iPoint, 2));
-  if (nDim == 3){
+  if (nDim == 3) {
     SetVolumeOutputValue("ADJ_VELOCITY-Z", iPoint, Node_AdjFlow->GetSolution(iPoint, 3));
   }
 
-  if (weakly_coupled_heat){
+  if (weakly_coupled_heat) {
     SetVolumeOutputValue("ADJ_TEMPERATURE", iPoint, Node_AdjHeat->GetSolution(iPoint, 0));
   }
   else {
@@ -371,7 +387,7 @@ void CAdjFlowIncOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSo
   }
 
   // Radiation
-  if (config->AddRadiation()){
+  if (config->AddRadiation()) {
     SetVolumeOutputValue("ADJ_P1_ENERGY", iPoint, Node_AdjRad->GetSolution(iPoint, 0));
   }
 
@@ -379,33 +395,34 @@ void CAdjFlowIncOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSo
   SetVolumeOutputValue("RES_ADJ_PRESSURE",   iPoint, Node_AdjFlow->GetSolution(iPoint, 0) - Node_AdjFlow->GetSolution_Old(iPoint, 0));
   SetVolumeOutputValue("RES_ADJ_VELOCITY-X", iPoint, Node_AdjFlow->GetSolution(iPoint, 1) - Node_AdjFlow->GetSolution_Old(iPoint, 1));
   SetVolumeOutputValue("RES_ADJ_VELOCITY-Y", iPoint, Node_AdjFlow->GetSolution(iPoint, 2) - Node_AdjFlow->GetSolution_Old(iPoint, 2));
-  if (nDim == 3){
+  if (nDim == 3) {
     SetVolumeOutputValue("RES_ADJ_VELOCITY-Z", iPoint, Node_AdjFlow->GetSolution(iPoint, 3) - Node_AdjFlow->GetSolution_Old(iPoint, 3));
     SetVolumeOutputValue("RES_ADJ_TEMPERATURE",     iPoint, Node_AdjFlow->GetSolution(iPoint, 4) - Node_AdjFlow->GetSolution_Old(iPoint, 4));
   } else {
     SetVolumeOutputValue("RES_ADJ_TEMPERATURE",     iPoint, Node_AdjFlow->GetSolution(iPoint, 3) - Node_AdjFlow->GetSolution_Old(iPoint, 3));
   }
 
-  if (config->AddRadiation()){
+  if (config->AddRadiation()) {
     SetVolumeOutputValue("RES_P1_ENERGY", iPoint, Node_AdjRad->GetSolution(iPoint, 0) - Node_AdjRad->GetSolution_Old(iPoint, 0));
   }
 
   SetVolumeOutputValue("SENSITIVITY-X", iPoint, Node_AdjFlow->GetSensitivity(iPoint, 0));
   SetVolumeOutputValue("SENSITIVITY-Y", iPoint, Node_AdjFlow->GetSensitivity(iPoint, 1));
-  if (nDim == 3)
+  if (nDim == 3) {
     SetVolumeOutputValue("SENSITIVITY-Z", iPoint, Node_AdjFlow->GetSensitivity(iPoint, 2));
+  }
 
   LoadVolumeData_AdjScalar(config, solver, iPoint);
 }
 
-void CAdjFlowIncOutput::LoadSurfaceData(CConfig *config, CGeometry *geometry, CSolver **solver, unsigned long iPoint, unsigned short iMarker, unsigned long iVertex){
+void CAdjFlowIncOutput::LoadSurfaceData(CConfig *config, CGeometry *geometry, CSolver **solver, unsigned long iPoint, unsigned short iMarker, unsigned long iVertex) {
 
   SetVolumeOutputValue("SENSITIVITY", iPoint, solver[ADJFLOW_SOL]->GetCSensitivity(iMarker, iVertex));
 
 }
 
 
-bool CAdjFlowIncOutput::SetInit_Residuals(const CConfig *config){
+bool CAdjFlowIncOutput::SetInit_Residuals(const CConfig *config) {
 
   return (config->GetTime_Marching() != TIME_MARCHING::STEADY && (curInnerIter == 0))||
          (config->GetTime_Marching() == TIME_MARCHING::STEADY && (curTimeIter < 2));
diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index 16051fe71fc..ad7c50042d1 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -268,7 +268,7 @@ def main():
     discadj_fsi.cfg_dir   = "disc_adj_fsi"
     discadj_fsi.cfg_file  = "config.cfg"
     discadj_fsi.test_iter = 6
-    discadj_fsi.test_vals = [6.000000, -1.559957, -3.080711, 0.000440, -1.063100]
+    discadj_fsi.test_vals = [6.000000, -1.949946, -3.080711, 0.000440, -1.063100]
     test_list.append(discadj_fsi)
 
     # Multi physics framework
@@ -276,9 +276,9 @@ def main():
     discadj_fsi2.cfg_dir   = "disc_adj_fsi/Airfoil_2d"
     discadj_fsi2.cfg_file  = "config.cfg"
     discadj_fsi2.test_iter = 8
-    discadj_fsi2.test_vals         = [-3.479484, 0.127482, -1.303589, 7.5407e-09, 2.3244]
+    discadj_fsi2.test_vals         = [-4.349355, 0.127482, -1.303589, 0.000000, 2.324400]
     discadj_fsi2.test_vals_aarch64 = [-3.479505, 0.127953, -1.303589, 7.5407e-09, 2.3244]
-    discadj_fsi2.tol       = 1e-16
+    discadj_fsi2.tol       = 0.00001
     test_list.append(discadj_fsi2)
 
     ###################################
@@ -290,7 +290,7 @@ def main():
     discadj_cht.cfg_dir   = "coupled_cht/disc_adj_incomp_2d"
     discadj_cht.cfg_file  = "cht_2d_3cylinders.cfg"
     discadj_cht.test_iter = 10
-    discadj_cht.test_vals = [-2.364408, -3.085549, -3.085516, -3.085511]
+    discadj_cht.test_vals = [-2.955510, -3.085549, -3.085516, -3.085511]
     test_list.append(discadj_cht)
 
     # 2D DA cht streamwise periodic case, 2 zones, avg temp objective
diff --git a/TestCases/serial_regression_AD.py b/TestCases/serial_regression_AD.py
index edebb37e0d1..6ce4f0b8693 100644
--- a/TestCases/serial_regression_AD.py
+++ b/TestCases/serial_regression_AD.py
@@ -212,7 +212,7 @@ def main():
     discadj_fsi.cfg_dir   = "disc_adj_fsi"
     discadj_fsi.cfg_file  = "config.cfg"
     discadj_fsi.test_iter = 6
-    discadj_fsi.test_vals = [6, -1.572702, -3.084381, 4.3990e-04, -1.0631] #last 5 columns
+    discadj_fsi.test_vals = [6.000000, -1.965877, -3.084381, 0.000440, -1.063100] #last 5 columns
     test_list.append(discadj_fsi)
 
     ###################################
@@ -224,7 +224,7 @@ def main():
     discadj_cht.cfg_dir   = "coupled_cht/disc_adj_incomp_2d"
     discadj_cht.cfg_file  = "cht_2d_3cylinders.cfg"
     discadj_cht.test_iter = 10
-    discadj_cht.test_vals = [-2.364405, -3.085551, -3.085518, -3.085513] #last 4 columns
+    discadj_cht.test_vals = [-2.955506, -3.085551, -3.085518, -3.085513] #last 4 columns
     test_list.append(discadj_cht)
 
     ######################################

From dccf66bc34c4e8f132aab8ad79d339bcbd5c8fd9 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 12 Feb 2023 17:59:02 -0800
Subject: [PATCH 191/656] re-use postprocessing

---
 SU2_CFD/include/drivers/CDriver.hpp           |   2 +
 SU2_CFD/include/drivers/CDriverBase.hpp       |   6 +-
 SU2_CFD/src/drivers/CDriverBase.cpp           |  82 +++++++-
 .../include/drivers/CDeformationDriver.hpp    |   5 -
 .../drivers/CDiscAdjDeformationDriver.hpp     | 196 +++++++++---------
 SU2_DEF/src/SU2_DEF.cpp                       |  14 +-
 SU2_DEF/src/drivers/CDeformationDriver.cpp    |  63 +-----
 .../src/drivers/CDiscAdjDeformationDriver.cpp |  83 +-------
 SU2_DOT/src/SU2_DOT.cpp                       |  14 +-
 9 files changed, 189 insertions(+), 276 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index 66fb0665aa7..92ca6370f84 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -74,6 +74,8 @@ class CDriver : public CDriverBase {
       fsi,         /*!< \brief FSI simulation flag.*/
       fem_solver;  /*!< \brief FEM fluid solver simulation flag. */
 
+  CFreeFormDefBox*** FFDBox;            /*!< \brief FFD FFDBoxes of the problem. */
+
   CIteration*** iteration_container;      /*!< \brief Container vector with all the iteration methods. */
   CIntegration**** integration_container; /*!< \brief Container vector with all the integration methods. */
   vector<vector<unique_ptr<CInterpolator>>>
diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index 132ee87ca71..3067e800baa 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -73,7 +73,6 @@ class CDriverBase {
                                            are solved). */
   CSurfaceMovement** surface_movement;  /*!< \brief Surface movement classes of the problem. */
   CVolumetricMovement*** grid_movement; /*!< \brief Volume grid movement classes of the problem. */
-  CFreeFormDefBox*** FFDBox;            /*!< \brief FFD FFDBoxes of the problem. */
 
   CConfig* main_config;     /*!< \brief Reference to base (i.e. ZONE 0) configuration (used in driver API). */
   CGeometry* main_geometry; /*!< \brief Reference to base (i.e. ZONE, INST, MESH 0) geometry (used in driver API). */
@@ -328,6 +327,11 @@ class CDriverBase {
    */
   void SetContainers_Null();
 
+  /*!
+   * \brief Delete containers.
+   */
+  void CommonPostprocessing();
+
   /*!
    * \brief Read in the config and mesh files.
    * \param[in] config - Definition of the particular problem.
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index 95d755c1e59..b9589b970f8 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -42,16 +42,6 @@ void CDriverBase::SetContainers_Null() {
    * down a hierarchy over all zones, multi-grid levels, equation sets, and equation terms as described in the comments
    * below. ---*/
 
-  config_container = nullptr;
-  output_container = nullptr;
-  geometry_container = nullptr;
-  solver_container = nullptr;
-  numerics_container = nullptr;
-
-  surface_movement = nullptr;
-  grid_movement = nullptr;
-  FFDBox = nullptr;
-
   config_container = new CConfig*[nZone]();
   output_container = new COutput*[nZone]();
   geometry_container = new CGeometry***[nZone]();
@@ -59,7 +49,6 @@ void CDriverBase::SetContainers_Null() {
   numerics_container = new CNumerics*****[nZone]();
   surface_movement = new CSurfaceMovement*[nZone]();
   grid_movement = new CVolumetricMovement**[nZone]();
-  FFDBox = new CFreeFormDefBox**[nZone]();
 
   nInst = new unsigned short[nZone];
 
@@ -74,6 +63,77 @@ void CDriverBase::SetContainers_Null() {
   main_geometry = nullptr;
 }
 
+void CDriverBase::CommonPostprocessing() {
+
+  if (numerics_container != nullptr) {
+    for (iZone = 0; iZone < nZone; iZone++) {
+      delete[] numerics_container[iZone];
+    }
+    delete[] numerics_container;
+  }
+  if (rank == MASTER_NODE) cout << "Deleted CNumerics container." << endl;
+
+  if (solver_container != nullptr) {
+    for (iZone = 0; iZone < nZone; iZone++) {
+      delete[] solver_container[iZone];
+    }
+    delete[] solver_container;
+  }
+  if (rank == MASTER_NODE) cout << "Deleted CSolver container." << endl;
+
+  if (geometry_container != nullptr) {
+    for (iZone = 0; iZone < nZone; iZone++) {
+      if (geometry_container[iZone] != nullptr) {
+        for (iInst = 0; iInst < nInst[iZone]; iInst++) {
+          delete geometry_container[iZone][iInst][MESH_0];
+          delete[] geometry_container[iZone][iInst];
+        }
+        delete[] geometry_container[iZone];
+      }
+    }
+    delete[] geometry_container;
+  }
+  if (rank == MASTER_NODE) cout << "Deleted CGeometry container." << endl;
+
+  if (surface_movement != nullptr) {
+    for (iZone = 0; iZone < nZone; iZone++) {
+      delete surface_movement[iZone];
+    }
+    delete[] surface_movement;
+  }
+  if (rank == MASTER_NODE) cout << "Deleted CSurfaceMovement class." << endl;
+
+  if (grid_movement != nullptr) {
+    for (iZone = 0; iZone < nZone; iZone++) {
+      for (iInst = 0; iInst < nInst[iZone]; iInst++) {
+        delete grid_movement[iZone][iInst];
+      }
+      delete[] grid_movement[iZone];
+    }
+    delete[] grid_movement;
+  }
+  if (rank == MASTER_NODE) cout << "Deleted CVolumetricMovement class." << endl;
+
+  if (config_container != nullptr) {
+    for (iZone = 0; iZone < nZone; iZone++) {
+      delete config_container[iZone];
+    }
+    delete[] config_container;
+  }
+  delete driver_config;
+  if (rank == MASTER_NODE) cout << "Deleted CConfig container." << endl;
+
+  if (output_container != nullptr) {
+    for (iZone = 0; iZone < nZone; iZone++) {
+      delete output_container[iZone];
+    }
+    delete[] output_container;
+  }
+  if (rank == MASTER_NODE) cout << "Deleted COutput class." << endl;
+
+  delete[] nInst;
+}
+
 unsigned short CDriverBase::GetNumberDesignVariables() const { return main_config->GetnDV(); }
 
 unsigned short CDriverBase::GetNumberFFDBoxes() const { return main_config->GetnFFDBox(); }
diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index a562a07c1a5..563221af6ee 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -48,11 +48,6 @@ class CDeformationDriver : public CDriverBase {
    */
   CDeformationDriver(char* confFile, SU2_Comm MPICommunicator);
 
-  /*!
-   * \brief Destructor of the class.
-   */
-  ~CDeformationDriver(void);
-
   /*!
    * \brief Preprocess the driver data.
    */
diff --git a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
index 6b28f072b98..24afea50a4d 100644
--- a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
@@ -33,105 +33,99 @@
 #include "../../../SU2_CFD/include/drivers/CDriverBase.hpp"
 
 class CDiscAdjDeformationDriver : public CDriverBase {
-protected:
- su2double** Gradient;
- ofstream Gradient_file;
-
-public:
- /*!
-  * \brief Constructor of the class.
-  * \param[in] confFile - Configuration file name.
-  * \param[in] MPICommunicator - MPI communicator for SU2.
-  */
- CDiscAdjDeformationDriver(char* confFile, SU2_Comm MPICommunicator);
-
- /*!
-  * \brief Destructor of the class.
-  */
- ~CDiscAdjDeformationDriver(void);
-
- /*!
-  * \brief Preprocess the driver data (includes solution allocation and initialization).
-  */
- void Preprocess();
-
- /*!
-  * \brief Launch the driver computation.
-  */
- void Run();
-
- /*!
-  * \brief Deallocation routine.
-  */
- void Postprocessing();
-
-protected:
- /*!
-  * \brief Read in the config and mesh files.
-  */
- void Input_Preprocessing();
-
- /*!
-  * \brief Construction of the edge-based data structure.
-  */
- void Geometrical_Preprocessing();
-
- /*!
-  * \brief Preprocess the output container.
-  */
- void Output_Preprocessing();
-
- /*!
-  * \brief Projection of the surface sensitivity using finite differences (FD).
-  * \param[in] geometry - Geometrical definition of the problem.
-  * \param[in] config - Definition of the particular problem.
-  * \param[in] surface_movement - Surface movement class of the problem.
-  * \param[in] Gradient_file - Output file to store the gradient data.
-  */
- void SetProjection_FD(CGeometry* geometry, CConfig* config, CSurfaceMovement* surface_movement, su2double** Gradient);
-
- /*!
-  * \brief Projection of the surface sensitivity using algorithmic differentiation (AD).
-  * \param[in] geometry - Geometrical definition of the problem.
-  * \param[in] config - Definition of the particular problem.
-  * \param[in] surface_movement - Surface movement class of the problem.
-  * \param[in] Gradient_file - Output file to store the gradient data.
-  */
- void SetProjection_AD(CGeometry* geometry, CConfig* config, CSurfaceMovement* surface_movement, su2double** Gradient);
-
- /*!
-  * \brief Prints the gradient information to a file.
-  * \param[in] Gradient - The gradient data.
-  * \param[in] config - Definition of the particular problem.
-  * \param[in] Gradient_file - Output file to store the gradient data.
-  */
- void OutputGradient(su2double** Gradient, CConfig* config, ofstream& Gradient_file);
-
- /*!
-  * \brief Write the sensitivity (including mesh sensitivity) computed with the discrete adjoint method
-  *  on the surface and in the volume to a file.
-  * \param[in] geometry - Geometrical definition of the problem.
-  * \param[in] config - Definition of the particular problem.
-  * \param[in] val_nZone - Number of Zones.
-  */
- void SetSensitivity_Files(CGeometry**** geometry, CConfig** config, unsigned short val_nZone);
-
- /*!
-  * \brief Treatment of derivatives with the Sobolev smoothing solver.
-  * \param[in] geometry - Geometrical definition of the problem.
-  * \param[in] config - Definition of the particular problem.
-  * \param[in] grid_movement - Volumetric movement class of the problem.
-  */
- void DerivativeTreatment_MeshSensitivity(CGeometry* geometry, CConfig* config, CVolumetricMovement* grid_movement);
-
- /*!
-  * \brief Treatment of derivatives with the Sobolev smoothing solver.
-  * \param[in] geometry - Geometrical definition of the problem.
-  * \param[in] config - Definition of the particular problem.
-  * \param[in] grid_movement - Volumetric movement class of the problem.
-  * \param[in] surface_movement - Surface movement class of the problem.
-  * \param[in] Gradient - Output array to store the gradient data.
-  */
- void DerivativeTreatment_Gradient(CGeometry* geometry, CConfig* config, CVolumetricMovement* grid_movement,
-                                   CSurfaceMovement* surface_movement, su2double** Gradient);
+ protected:
+  su2double** Gradient;
+
+ public:
+  /*!
+   * \brief Constructor of the class.
+   * \param[in] confFile - Configuration file name.
+   * \param[in] MPICommunicator - MPI communicator for SU2.
+   */
+  CDiscAdjDeformationDriver(char* confFile, SU2_Comm MPICommunicator);
+
+  /*!
+   * \brief Preprocess the driver data (includes solution allocation and initialization).
+   */
+  void Preprocess();
+
+  /*!
+   * \brief Launch the driver computation.
+   */
+  void Run();
+
+  /*!
+   * \brief Deallocation routine.
+   */
+  void Postprocessing();
+
+ protected:
+  /*!
+   * \brief Read in the config and mesh files.
+   */
+  void Input_Preprocessing();
+
+  /*!
+   * \brief Construction of the edge-based data structure.
+   */
+  void Geometrical_Preprocessing();
+
+  /*!
+   * \brief Preprocess the output container.
+   */
+  void Output_Preprocessing();
+
+  /*!
+   * \brief Projection of the surface sensitivity using finite differences (FD).
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] surface_movement - Surface movement class of the problem.
+   * \param[in] Gradient_file - Output file to store the gradient data.
+   */
+  void SetProjection_FD(CGeometry* geometry, CConfig* config, CSurfaceMovement* surface_movement, su2double** Gradient);
+
+  /*!
+   * \brief Projection of the surface sensitivity using algorithmic differentiation (AD).
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] surface_movement - Surface movement class of the problem.
+   * \param[in] Gradient_file - Output file to store the gradient data.
+   */
+  void SetProjection_AD(CGeometry* geometry, CConfig* config, CSurfaceMovement* surface_movement, su2double** Gradient);
+
+  /*!
+   * \brief Prints the gradient information to a file.
+   * \param[in] Gradient - The gradient data.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] Gradient_file - Output file to store the gradient data.
+   */
+  void OutputGradient(su2double** Gradient, CConfig* config, ofstream& Gradient_file);
+
+  /*!
+   * \brief Write the sensitivity (including mesh sensitivity) computed with the discrete adjoint method
+   *  on the surface and in the volume to a file.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] val_nZone - Number of Zones.
+   */
+  void SetSensitivity_Files(CGeometry**** geometry, CConfig** config, unsigned short val_nZone);
+
+  /*!
+   * \brief Treatment of derivatives with the Sobolev smoothing solver.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] grid_movement - Volumetric movement class of the problem.
+   */
+  void DerivativeTreatment_MeshSensitivity(CGeometry* geometry, CConfig* config, CVolumetricMovement* grid_movement);
+
+  /*!
+   * \brief Treatment of derivatives with the Sobolev smoothing solver.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] grid_movement - Volumetric movement class of the problem.
+   * \param[in] surface_movement - Surface movement class of the problem.
+   * \param[in] Gradient - Output array to store the gradient data.
+   */
+  void DerivativeTreatment_Gradient(CGeometry* geometry, CConfig* config, CVolumetricMovement* grid_movement,
+                                    CSurfaceMovement* surface_movement, su2double** Gradient);
 };
diff --git a/SU2_DEF/src/SU2_DEF.cpp b/SU2_DEF/src/SU2_DEF.cpp
index 49cef08b52a..2fc5041883b 100644
--- a/SU2_DEF/src/SU2_DEF.cpp
+++ b/SU2_DEF/src/SU2_DEF.cpp
@@ -33,10 +33,6 @@ int main(int argc, char* argv[]) {
 
   char config_file_name[MAX_STRING_SIZE];
 
-  /*--- Create a pointer to the main SU2_DEF Driver ---*/
-
-  CDeformationDriver* driver = nullptr;
-
   /*--- MPI initialization ---*/
 
 #if defined(HAVE_OMP) && defined(HAVE_MPI)
@@ -58,21 +54,19 @@ int main(int argc, char* argv[]) {
 
   /*--- Initialize the mesh deformation driver. ---*/
 
-  driver = new CDeformationDriver(config_file_name, comm);
+  CDeformationDriver driver(config_file_name, comm);
 
   /*--- Preprocess the solver data. ---*/
 
-  driver->Preprocess();
+  driver.Preprocess();
 
   /*--- Launch the main external loop of the solver. ---*/
 
-  driver->Run();
+  driver.Run();
 
   /*--- Postprocess all the containers, close history file, and exit SU2. ---*/
 
-  driver->Postprocessing();
-
-  delete driver;
+  driver.Postprocessing();
 
   /*--- Finalize MPI parallelization. ---*/
 
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 856450217c2..86c7fb78881 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -91,8 +91,6 @@ CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
   UsedTimeCompute = 0.0;
 }
 
-CDeformationDriver::~CDeformationDriver(void) {}
-
 void CDeformationDriver::Input_Preprocessing() {
   /*--- Initialize a char to store the zone filename. ---*/
 
@@ -525,7 +523,7 @@ void CDeformationDriver::Output() {
 
 void CDeformationDriver::Postprocessing() {
   if (rank == MASTER_NODE)
-    cout << endl << "------------------------- Solver Postprocessing -------------------------" << endl;
+    cout << "\n------------------------- Solver Postprocessing -------------------------" << endl;
 
   if (driver_config->GetDeform_Mesh()) {
     for (iZone = 0; iZone < nZone; iZone++) {
@@ -536,77 +534,26 @@ void CDeformationDriver::Postprocessing() {
           delete[] numerics_container[iZone][INST_0][MESH_0];
           delete[] numerics_container[iZone][INST_0];
         }
-        delete[] numerics_container[iZone];
       }
+      /*--- The remaining levels in the container are deleted in CommonPostprocessing ---*/
     }
-    delete[] numerics_container;
-    if (rank == MASTER_NODE) cout << "Deleted CNumerics container." << endl;
 
     for (iZone = 0; iZone < nZone; iZone++) {
       if (solver_container[iZone] != nullptr) {
         delete solver_container[iZone][INST_0][MESH_0][MESH_SOL];
         delete[] solver_container[iZone][INST_0][MESH_0];
         delete[] solver_container[iZone][INST_0];
-        delete[] solver_container[iZone];
       }
+      /*--- The remaining levels in the container are deleted in CommonPostprocessing ---*/
     }
-    delete[] solver_container;
-    if (rank == MASTER_NODE) cout << "Deleted CSolver container." << endl;
-  }
-
-  if (geometry_container != nullptr) {
-    for (iZone = 0; iZone < nZone; iZone++) {
-      delete geometry_container[iZone][INST_0][MESH_0];
-      delete[] geometry_container[iZone][INST_0];
-      delete[] geometry_container[iZone];
-    }
-    delete[] geometry_container;
-  }
-  if (rank == MASTER_NODE) cout << "Deleted CGeometry container." << endl;
-
-  delete[] FFDBox;
-  if (rank == MASTER_NODE) cout << "Deleted CFreeFormDefBox class." << endl;
-
-  if (surface_movement != nullptr) {
-    for (iZone = 0; iZone < nZone; iZone++) {
-      delete surface_movement[iZone];
-    }
-    delete[] surface_movement;
-  }
-  if (rank == MASTER_NODE) cout << "Deleted CSurfaceMovement class." << endl;
-
-  if (grid_movement != nullptr) {
-    for (iZone = 0; iZone < nZone; iZone++) {
-      delete grid_movement[iZone][INST_0];
-      delete[] grid_movement[iZone];
-    }
-    delete[] grid_movement;
-  }
-  if (rank == MASTER_NODE) cout << "Deleted CVolumetricMovement class." << endl;
-
-  if (config_container != nullptr) {
-    for (iZone = 0; iZone < nZone; iZone++) {
-      delete config_container[iZone];
-    }
-    delete[] config_container;
-  }
-  delete driver_config;
-  if (rank == MASTER_NODE) cout << "Deleted CConfig container." << endl;
-
-  if (output_container != nullptr) {
-    for (iZone = 0; iZone < nZone; iZone++) {
-      delete output_container[iZone];
-    }
-    delete[] output_container;
   }
-  if (rank == MASTER_NODE) cout << "Deleted COutput class." << endl;
 
-  if (nInst != nullptr) delete[] nInst;
+  CommonPostprocessing();
 
   /*--- Exit the solver cleanly. ---*/
 
   if (rank == MASTER_NODE)
-    cout << endl << "------------------------- Exit Success (SU2_DEF) ------------------------" << endl << endl;
+    cout << "\n------------------------- Exit Success (SU2_DEF) ------------------------" << endl << endl;
 }
 
 void CDeformationDriver::CommunicateMeshDisplacements(void) {
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index 25ae73f9abd..4b3c92be99b 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -98,8 +98,6 @@ CDiscAdjDeformationDriver::CDiscAdjDeformationDriver(char* confFile, SU2_Comm MP
   UsedTimeCompute = 0.0;
 }
 
-CDiscAdjDeformationDriver::~CDiscAdjDeformationDriver(void) {}
-
 void CDiscAdjDeformationDriver::Input_Preprocessing() {
   /*--- Initialize a char to store the zone filename. ---*/
 
@@ -334,6 +332,7 @@ void CDiscAdjDeformationDriver::Run() {
     SetSensitivity_Files(geometry_container, config_container, nZone);
   }
 
+  ofstream Gradient_file;
   Gradient_file.precision(driver_config->OptionIsSet("OUTPUT_PRECISION") ? driver_config->GetOutput_Precision() : 6);
 
   /*--- For multi-zone computations the gradient contributions are summed up and written into one file. ---*/
@@ -382,91 +381,15 @@ void CDiscAdjDeformationDriver::Postprocessing() {
   }
   delete[] Gradient;
 
-  delete driver_config;
-  driver_config = nullptr;
-
   if (rank == MASTER_NODE)
     cout << "\n------------------------- Solver Postprocessing -------------------------" << endl;
 
-  for (iZone = 0; iZone < nZone; iZone++) {
-    if (numerics_container[iZone] != nullptr) {
-      delete[] numerics_container[iZone];
-    }
-  }
-  delete[] numerics_container;
-  if (rank == MASTER_NODE) cout << "Deleted CNumerics container." << endl;
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    if (solver_container[iZone] != nullptr) {
-      delete[] solver_container[iZone];
-    }
-  }
-  delete[] solver_container;
-  if (rank == MASTER_NODE) cout << "Deleted CSolver container." << endl;
-
-  if (geometry_container != nullptr) {
-    for (iZone = 0; iZone < nZone; iZone++) {
-      if (geometry_container[iZone] != nullptr) {
-        for (iInst = 0; iInst < nInst[iZone]; iInst++) {
-          delete geometry_container[iZone][iInst][MESH_0];
-          delete[] geometry_container[iZone][iInst];
-        }
-        delete[] geometry_container[iZone];
-      }
-    }
-    delete[] geometry_container;
-  }
-  if (rank == MASTER_NODE) cout << "Deleted CGeometry container." << endl;
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    delete[] FFDBox[iZone];
-  }
-  delete[] FFDBox;
-  if (rank == MASTER_NODE) cout << "Deleted CFreeFormDefBox class." << endl;
-
-  if (surface_movement != nullptr) {
-    for (iZone = 0; iZone < nZone; iZone++) {
-      delete surface_movement[iZone];
-    }
-    delete[] surface_movement;
-  }
-  if (rank == MASTER_NODE) cout << "Deleted CSurfaceMovement class." << endl;
-
-  if (grid_movement != nullptr) {
-    for (iZone = 0; iZone < nZone; iZone++) {
-      if (grid_movement[iZone] != nullptr) {
-        for (iInst = 0; iInst < nInst[iZone]; iInst++) {
-          delete grid_movement[iZone][iInst];
-        }
-        delete[] grid_movement[iZone];
-      }
-    }
-    delete[] grid_movement;
-  }
-  if (rank == MASTER_NODE) cout << "Deleted CVolumetricMovement class." << endl;
-
-  if (config_container != nullptr) {
-    for (iZone = 0; iZone < nZone; iZone++) {
-      delete config_container[iZone];
-    }
-    delete[] config_container;
-  }
-  if (rank == MASTER_NODE) cout << "Deleted CConfig container." << endl;
-
-  if (output_container != nullptr) {
-    for (iZone = 0; iZone < nZone; iZone++) {
-      delete output_container[iZone];
-    }
-    delete[] output_container;
-  }
-  if (rank == MASTER_NODE) cout << "Deleted COutput class." << endl;
-
-  if (nInst != nullptr) delete[] nInst;
+  CommonPostprocessing();
 
   /*--- Exit the solver cleanly. ---*/
 
   if (rank == MASTER_NODE)
-    cout << endl << "------------------------- Exit Success (SU2_DEF_AD) ------------------------" << endl << endl;
+    cout << "\n------------------------- Exit Success (SU2_DOT) ------------------------" << endl << endl;
 }
 
 void CDiscAdjDeformationDriver::SetProjection_FD(CGeometry* geometry, CConfig* config,
diff --git a/SU2_DOT/src/SU2_DOT.cpp b/SU2_DOT/src/SU2_DOT.cpp
index 6c269be249c..4aa3c314538 100644
--- a/SU2_DOT/src/SU2_DOT.cpp
+++ b/SU2_DOT/src/SU2_DOT.cpp
@@ -33,10 +33,6 @@ int main(int argc, char* argv[]) {
 
   char config_file_name[MAX_STRING_SIZE];
 
-  /*--- Create a pointer to the main SU2_DEF Driver. ---*/
-
-  CDiscAdjDeformationDriver* driver = nullptr;
-
   /*--- MPI initialization. ---*/
 
 #if defined(HAVE_OMP) && defined(HAVE_MPI)
@@ -58,21 +54,19 @@ int main(int argc, char* argv[]) {
 
   /*--- Initialize the mesh deformation driver. ---*/
 
-  driver = new CDiscAdjDeformationDriver(config_file_name, comm);
+  CDiscAdjDeformationDriver driver(config_file_name, comm);
 
   /*--- Preprocess the solver data. ---*/
 
-  driver->Preprocess();
+  driver.Preprocess();
 
   /*--- Launch the main external loop of the solver. ---*/
 
-  driver->Run();
+  driver.Run();
 
   /*--- Postprocess all the containers, close history file, and exit SU2. ---*/
 
-  driver->Postprocessing();
-
-  delete driver;
+  driver.Postprocessing();
 
   /*--- Finalize MPI parallelization. ---*/
 

From dc71633395b5570079bf48891ac9b860f6001e07 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 12 Feb 2023 20:37:46 -0800
Subject: [PATCH 192/656] fix memory leaks with OpenMP

---
 SU2_CFD/src/drivers/CDriverBase.cpp        | 8 +++++---
 SU2_DEF/src/drivers/CDeformationDriver.cpp | 9 +++++----
 2 files changed, 10 insertions(+), 7 deletions(-)

diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index b9589b970f8..cfafb9d419e 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -105,10 +105,12 @@ void CDriverBase::CommonPostprocessing() {
 
   if (grid_movement != nullptr) {
     for (iZone = 0; iZone < nZone; iZone++) {
-      for (iInst = 0; iInst < nInst[iZone]; iInst++) {
-        delete grid_movement[iZone][iInst];
+      if (grid_movement[iZone] != nullptr) {
+        for (iInst = 0; iInst < nInst[iZone]; iInst++) {
+          delete grid_movement[iZone][iInst];
+        }
+        delete[] grid_movement[iZone];
       }
-      delete[] grid_movement[iZone];
     }
     delete[] grid_movement;
   }
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 86c7fb78881..03f95c3cb39 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -528,12 +528,13 @@ void CDeformationDriver::Postprocessing() {
   if (driver_config->GetDeform_Mesh()) {
     for (iZone = 0; iZone < nZone; iZone++) {
       if (numerics_container[iZone] != nullptr) {
-        for (unsigned int iTerm = 0; iTerm < MAX_TERMS * omp_get_max_threads(); iTerm++) {
+        for (int thread = 0; thread < omp_get_max_threads(); thread++) {
+          const int iTerm = FEA_TERM + thread * MAX_TERMS;
           delete numerics_container[iZone][INST_0][MESH_0][MESH_SOL][iTerm];
-          delete[] numerics_container[iZone][INST_0][MESH_0][MESH_SOL];
-          delete[] numerics_container[iZone][INST_0][MESH_0];
-          delete[] numerics_container[iZone][INST_0];
         }
+        delete[] numerics_container[iZone][INST_0][MESH_0][MESH_SOL];
+        delete[] numerics_container[iZone][INST_0][MESH_0];
+        delete[] numerics_container[iZone][INST_0];
       }
       /*--- The remaining levels in the container are deleted in CommonPostprocessing ---*/
     }

From e205c315f0de9b7b10a2b9f3b29451a538eac323 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 12 Feb 2023 20:58:36 -0800
Subject: [PATCH 193/656] remove redundant hpps for DEF and DOT

---
 SU2_DEF/include/SU2_DEF.hpp | 40 -------------------------------------
 SU2_DEF/src/SU2_DEF.cpp     |  4 +---
 SU2_DOT/include/SU2_DOT.hpp | 40 -------------------------------------
 SU2_DOT/src/SU2_DOT.cpp     |  4 +---
 4 files changed, 2 insertions(+), 86 deletions(-)
 delete mode 100644 SU2_DEF/include/SU2_DEF.hpp
 delete mode 100644 SU2_DOT/include/SU2_DOT.hpp

diff --git a/SU2_DEF/include/SU2_DEF.hpp b/SU2_DEF/include/SU2_DEF.hpp
deleted file mode 100644
index a0a9877b089..00000000000
--- a/SU2_DEF/include/SU2_DEF.hpp
+++ /dev/null
@@ -1,40 +0,0 @@
-/*!
- * \file SU2_DEF.hpp
- * \brief Headers of the main subroutines of the code SU2_DEF.
- * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-
-#pragma once
-
-#include <cmath>
-#include <cstdlib>
-#include <iomanip>
-#include <iostream>
-
-#include "../../Common/include/CConfig.hpp"
-#include "../../Common/include/parallelization/mpi_structure.hpp"
-#include "../../Common/include/parallelization/omp_structure.hpp"
-#include "drivers/CDeformationDriver.hpp"
-
-using namespace std;
diff --git a/SU2_DEF/src/SU2_DEF.cpp b/SU2_DEF/src/SU2_DEF.cpp
index 2fc5041883b..379a1a356c9 100644
--- a/SU2_DEF/src/SU2_DEF.cpp
+++ b/SU2_DEF/src/SU2_DEF.cpp
@@ -25,9 +25,7 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-#include "../include/SU2_DEF.hpp"
-
-using namespace std;
+#include "../include/drivers/CDeformationDriver.hpp"
 
 int main(int argc, char* argv[]) {
 
diff --git a/SU2_DOT/include/SU2_DOT.hpp b/SU2_DOT/include/SU2_DOT.hpp
deleted file mode 100644
index f6b6d39e508..00000000000
--- a/SU2_DOT/include/SU2_DOT.hpp
+++ /dev/null
@@ -1,40 +0,0 @@
-/*!
- * \file SU2_DOT.hpp
- * \brief Headers of the main subroutines of the code SU2_DOT.
- * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-
-#pragma once
-
-#include <cmath>
-#include <cstdlib>
-#include <iomanip>
-#include <iostream>
-
-#include "../../Common/include/CConfig.hpp"
-#include "../../Common/include/parallelization/mpi_structure.hpp"
-#include "../../Common/include/parallelization/omp_structure.hpp"
-#include "../../SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp"
-
-using namespace std;
diff --git a/SU2_DOT/src/SU2_DOT.cpp b/SU2_DOT/src/SU2_DOT.cpp
index 4aa3c314538..39e3dd34320 100644
--- a/SU2_DOT/src/SU2_DOT.cpp
+++ b/SU2_DOT/src/SU2_DOT.cpp
@@ -25,9 +25,7 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-#include "../include/SU2_DOT.hpp"
-
-using namespace std;
+#include "../../SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp"
 
 int main(int argc, char* argv[]) {
 

From 9127cfac6841484c43f993d667ecf99106ee7f29 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 12 Feb 2023 21:13:27 -0800
Subject: [PATCH 194/656] doxygen

---
 Docs/docmain.hpp                        | 35 +++++++++++++++----------
 SU2_CFD/include/drivers/CDriver.hpp     |  5 ++++
 SU2_CFD/include/drivers/CDriverBase.hpp |  4 +++
 SU2_DEF/obj/Makefile.am                 |  1 -
 SU2_DOT/obj/Makefile.am                 |  3 +--
 5 files changed, 31 insertions(+), 17 deletions(-)

diff --git a/Docs/docmain.hpp b/Docs/docmain.hpp
index 5ea00d86ab4..704f85acdcb 100644
--- a/Docs/docmain.hpp
+++ b/Docs/docmain.hpp
@@ -25,10 +25,10 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-/*! 
+/*!
  * \mainpage SU2 version 7.5.1 "Blackbird"
  * SU2 suite is an open-source collection of C++ based software tools
- * to perform PDE analysis and PDE constrained optimization.  The toolset is designed with 
+ * to perform PDE analysis and PDE constrained optimization.  The toolset is designed with
  * computational fluid dynamics and aerodynamic shape optimization in mind, but is extensible to
  * include other families of governing equations such as potential flow, electrodynamics, chemically reacting
  * flows, and many others.  SU2 is released under an open-source license.
@@ -66,43 +66,43 @@
 
 /*!
  * \defgroup ConvDiscr Discretization of the convective terms
- * \brief Group of classes which define the numerical methods for 
- *		  discretizing the convective terms of a Partial Differential Equation. 
- *		  There are methods for solving the direct, adjoint and linearized 
+ * \brief Group of classes which define the numerical methods for
+ *		  discretizing the convective terms of a Partial Differential Equation.
+ *		  There are methods for solving the direct, adjoint and linearized
  *		  systems of equations.
  */
 
 /*!
  * \defgroup ViscDiscr Discretization of the viscous terms
- * \brief Group of classes which define the numerical methods for 
- *		  discretizing the viscous terms of a Partial Differential Equation. 
- *		  There are methods for solving the direct, adjoint and linearized 
+ * \brief Group of classes which define the numerical methods for
+ *		  discretizing the viscous terms of a Partial Differential Equation.
+ *		  There are methods for solving the direct, adjoint and linearized
  *		  systems of equations.
  */
 
 /*!
  * \defgroup SourceDiscr Discretization of the source terms
- * \brief Group of classes which define the numerical methods for 
- *		  discretizing the source terms of a Partial Differential Equation. 
- *		  There are methods for solving the direct, adjoint and linearized 
+ * \brief Group of classes which define the numerical methods for
+ *		  discretizing the source terms of a Partial Differential Equation.
+ *		  There are methods for solving the direct, adjoint and linearized
  *		  systems of equations.
  */
 
 /*!
  * \defgroup Euler_Equations Solving the Euler equations
- * \brief Group of classes which define the system of Euler equations in 
+ * \brief Group of classes which define the system of Euler equations in
  *		  three formulations: direct, adjoint, and linearized.
  */
 
 /*!
  * \defgroup Navier_Stokes_Equations Solving the Navier-Stokes equations
- * \brief Group of classes which define the system of Navier-Stokes equations in 
+ * \brief Group of classes which define the system of Navier-Stokes equations in
  *		  three formulations: direct, adjoint, and linearized.
  */
 
 /*!
  * \defgroup Turbulence_Model Solving the turbulence model equations
- * \brief Group of classes which define the turbulence model in 
+ * \brief Group of classes which define the turbulence model in
  *		  three formulations: direct, adjoint, and linearized.
  */
 
@@ -130,6 +130,13 @@
  *        space and time integration. The latter use mostly the "Solvers".
  */
 
+/*!
+ * \defgroup PySU2 Python Wrapper functions
+ * \brief Functions of the driver classes (\ref Drivers) that can be used to customize SU2
+ *        via Python. For example, set custom temperature distributions at boundaries,
+ *        deform the mesh, etc.
+ */
+
 /*!
  * \defgroup Variable Storing solution variables
  * \brief Classes used to store and access the solution variables of all types of problems.
diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index 92ca6370f84..a26c841656f 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -403,6 +403,9 @@ class CDriver : public CDriverBase {
    */
   virtual void SetInitialMesh() {}
 
+/// \addtogroup PySU2
+/// \{
+
   /*!
    * \brief Process the boundary conditions and update the multi-grid structure.
    */
@@ -644,6 +647,8 @@ class CDriver : public CDriverBase {
    */
   void SetInlet_Angle(unsigned short iMarker, passivedouble alpha);
 
+/// \}
+
   /*!
    * \brief Sum the number of primal or adjoint variables for all solvers in a given zone.
    * \param[in] iZone - Index of the zone.
diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index 3067e800baa..f35c32ca07b 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -121,6 +121,9 @@ class CDriverBase {
    */
   virtual void Postprocessing(){}
 
+/// \addtogroup PySU2
+/// @{
+
   /*!
    * \brief Get the number of design variables.
    * \return Number of design variables.
@@ -320,6 +323,7 @@ class CDriverBase {
    * \brief Communicate the boundary mesh displacements.
    */
   void CommunicateMeshDisplacements(void);
+/// \}
 
  protected:
   /*!
diff --git a/SU2_DEF/obj/Makefile.am b/SU2_DEF/obj/Makefile.am
index 0704502da65..4edc38c8fd4 100644
--- a/SU2_DEF/obj/Makefile.am
+++ b/SU2_DEF/obj/Makefile.am
@@ -33,7 +33,6 @@ ACLOCAL_AMFLAGS = ${ACLOCAL_FLAGS}
 bin_PROGRAMS = ../bin/SU2_DEF
 
 ___bin_SU2_DEF_SOURCES = \
-  ../include/SU2_DEF.hpp \
   ../src/SU2_DEF.cpp
 
 
diff --git a/SU2_DOT/obj/Makefile.am b/SU2_DOT/obj/Makefile.am
index 238b66fd3a4..23c60fe972f 100644
--- a/SU2_DOT/obj/Makefile.am
+++ b/SU2_DOT/obj/Makefile.am
@@ -40,8 +40,7 @@ if BUILD_REVERSE
 bin_PROGRAMS += ../bin/SU2_DOT_AD
 endif
 
-su2_dot_sources = ../include/SU2_DOT.hpp \
-		../src/SU2_DOT.cpp
+su2_dot_sources = ../src/SU2_DOT.cpp
 
 su2_dot_ldadd =
 su2_dot_cxx_flags = -std=c++11

From 26dc856e44c94929d17ff69c073475aa1ac8ca9b Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 13 Feb 2023 13:45:26 +0100
Subject: [PATCH 195/656] pulled develop

---
 SU2_CFD/include/drivers/CDriver.hpp           |  443 ++++---
 SU2_CFD/include/numerics/CNumerics.hpp        |   28 -
 .../include/numerics/NEMO/NEMO_diffusion.hpp  |    2 +-
 SU2_CFD/include/solvers/CHeatSolver.hpp       |  144 +-
 SU2_CFD/include/solvers/CMeshSolver.hpp       |    6 +-
 SU2_CFD/include/solvers/CSolver.hpp           |   12 +-
 SU2_CFD/include/variables/CHeatVariable.hpp   |   31 +-
 SU2_CFD/src/drivers/CDriver.cpp               |   12 +-
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        |    4 +-
 SU2_CFD/src/fluid/CPengRobinson.cpp           |    1 -
 SU2_CFD/src/iteration/CIteration.cpp          |    2 +-
 SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp  |    2 +-
 SU2_CFD/src/python_wrapper_structure.cpp      |  559 +++++---
 SU2_CFD/src/solvers/CEulerSolver.cpp          |   37 +
 SU2_CFD/src/solvers/CHeatSolver.cpp           | 1157 ++++++-----------
 SU2_CFD/src/solvers/CMeshSolver.cpp           |    2 +-
 SU2_CFD/src/variables/CEulerVariable.cpp      |    6 +
 SU2_CFD/src/variables/CHeatVariable.cpp       |   37 +-
 18 files changed, 1191 insertions(+), 1294 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index 66fb0665aa7..5481a8e9a97 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -1,5 +1,5 @@
-/*!
- * \file CDriver.hpp
+/*!
+ * \file driver_structure.hpp
  * \brief Headers of the main subroutines for driving single or multi-zone problems.
  *        The subroutines and functions are in the <i>driver_structure.cpp</i> file.
  * \author T. Economon, H. Kline, R. Sanchez
@@ -28,12 +28,13 @@
 
 #pragma once
 
-#include "../../../Common/include/geometry/CGeometry.hpp"
 #include "../../../Common/include/parallelization/mpi_structure.hpp"
+
 #include "../integration/CIntegration.hpp"
-#include "../interfaces/CInterface.hpp"
 #include "../solvers/CSolver.hpp"
-#include "CDriverBase.hpp"
+#include "../interfaces/CInterface.hpp"
+
+#include "../../../Common/include/geometry/CGeometry.hpp"
 
 using namespace std;
 
@@ -48,49 +49,69 @@ class COutput;
  * \brief Parent class for driving an iteration of a single or multi-zone problem.
  * \author T. Economon
  */
-
-class CDriver : public CDriverBase {
- protected:
+class CDriver {
+protected:
+  int rank,   /*!< \brief MPI Rank. */
+  size;         /*!< \brief MPI Size. */
+  char* config_file_name;                       /*!< \brief Configuration file name of the problem.*/
   char runtime_file_name[MAX_STRING_SIZE];
-  su2double
-      UsedTimeOutput; /*!< \brief Elapsed time between Start and Stop point of the timer for tracking output phase.*/
-
-  su2double BandwidthSum =
-      0.0;                    /*!< \brief Aggregate value of the bandwidth for writing restarts (to be average later).*/
-  unsigned long IterCount,    /*!< \brief Iteration count stored for performance benchmarking.*/
-      OutputCount;            /*!< \brief Output count stored for performance benchmarking.*/
-  unsigned long DOFsPerPoint; /*!< \brief Number of unknowns at each vertex, i.e., number of equations solved. */
-  su2double Mpoints; /*!< \brief Total number of grid points in millions in the calculation (including ghost points).*/
-  su2double
-      MpointsDomain; /*!< \brief Total number of grid points in millions in the calculation (excluding ghost points).*/
-  su2double MDOFs;   /*!< \brief Total number of DOFs in millions in the calculation (including ghost points).*/
-  su2double MDOFsDomain; /*!< \brief Total number of DOFs in millions in the calculation (excluding ghost points).*/
-
-  ofstream** ConvHist_file; /*!< \brief Convergence history file.*/
-  ofstream FSIHist_file;    /*!< \brief FSI convergence history file.*/
-
-  bool StopCalc,   /*!< \brief Stop computation flag.*/
-      mixingplane, /*!< \brief mixing-plane simulation flag.*/
-      fsi,         /*!< \brief FSI simulation flag.*/
-      fem_solver;  /*!< \brief FEM fluid solver simulation flag. */
-
-  CIteration*** iteration_container;      /*!< \brief Container vector with all the iteration methods. */
-  CIntegration**** integration_container; /*!< \brief Container vector with all the integration methods. */
-  vector<vector<unique_ptr<CInterpolator>>>
-      interpolator_container; /*!< \brief Definition of the interpolation method between non-matching discretizations of
-                                 the interface. */
-  CInterface*** interface_container; /*!< \brief Definition of the interface of information and physics. */
-  bool dry_run;                      /*!< \brief Flag if SU2_CFD was started as dry-run via "SU2_CFD -d <config>.cfg" */
-
- public:
+  su2double StartTime,                          /*!< \brief Start point of the timer for performance benchmarking.*/
+            StopTime,                           /*!< \brief Stop point of the timer for performance benchmarking.*/
+            UsedTimePreproc,                    /*!< \brief Elapsed time between Start and Stop point of the timer for tracking preprocessing phase.*/
+            UsedTimeCompute,                    /*!< \brief Elapsed time between Start and Stop point of the timer for tracking compute phase.*/
+            UsedTimeOutput,                     /*!< \brief Elapsed time between Start and Stop point of the timer for tracking output phase.*/
+            UsedTime;                           /*!< \brief Elapsed time between Start and Stop point of the timer.*/
+  su2double BandwidthSum = 0.0;                 /*!< \brief Aggregate value of the bandwidth for writing restarts (to be average later).*/
+  unsigned long IterCount,                      /*!< \brief Iteration count stored for performance benchmarking.*/
+  OutputCount;                                  /*!< \brief Output count stored for performance benchmarking.*/
+  unsigned long DOFsPerPoint;                   /*!< \brief Number of unknowns at each vertex, i.e., number of equations solved. */
+  su2double Mpoints;                            /*!< \brief Total number of grid points in millions in the calculation (including ghost points).*/
+  su2double MpointsDomain;                      /*!< \brief Total number of grid points in millions in the calculation (excluding ghost points).*/
+  su2double MDOFs;                              /*!< \brief Total number of DOFs in millions in the calculation (including ghost points).*/
+  su2double MDOFsDomain;                        /*!< \brief Total number of DOFs in millions in the calculation (excluding ghost points).*/
+  unsigned long TimeIter;                       /*!< \brief External iteration.*/
+  ofstream **ConvHist_file;                     /*!< \brief Convergence history file.*/
+  ofstream FSIHist_file;                        /*!< \brief FSI convergence history file.*/
+  unsigned short iMesh,                         /*!< \brief Iterator on mesh levels.*/
+                iZone,                          /*!< \brief Iterator on zones.*/
+                nZone,                          /*!< \brief Total number of zones in the problem. */
+                nDim,                           /*!< \brief Number of dimensions.*/
+                iInst,                          /*!< \brief Iterator on instance levels.*/
+                *nInst,                         /*!< \brief Total number of instances in the problem (per zone). */
+                **interface_types;              /*!< \brief Type of coupling between the distinct (physical) zones.*/
+  bool StopCalc,                                /*!< \brief Stop computation flag.*/
+       mixingplane,                             /*!< \brief mixing-plane simulation flag.*/
+       fsi,                                     /*!< \brief FSI simulation flag.*/
+       fem_solver;                              /*!< \brief FEM fluid solver simulation flag. */
+  CIteration ***iteration_container;            /*!< \brief Container vector with all the iteration methods. */
+  COutput **output_container;                   /*!< \brief Pointer to the COutput class. */
+  CIntegration ****integration_container;       /*!< \brief Container vector with all the integration methods. */
+  CGeometry ****geometry_container;             /*!< \brief Geometrical definition of the problem. */
+  CSolver *****solver_container;                /*!< \brief Container vector with all the solutions. */
+  CNumerics ******numerics_container;           /*!< \brief Description of the numerical method (the way in which the equations are solved). */
+  CConfig **config_container;                   /*!< \brief Definition of the particular problem. */
+  CConfig *driver_config;                       /*!< \brief Definition of the driver configuration. */
+  COutput *driver_output;                       /*!< \brief Definition of the driver output. */
+  CSurfaceMovement **surface_movement;          /*!< \brief Surface movement classes of the problem. */
+  CVolumetricMovement ***grid_movement;         /*!< \brief Volume grid movement classes of the problem. */
+  CFreeFormDefBox*** FFDBox;                    /*!< \brief FFD FFDBoxes of the problem. */
+  vector<vector<unique_ptr<CInterpolator> > >
+  interpolator_container;                       /*!< \brief Definition of the interpolation method between non-matching discretizations of the interface. */
+  CInterface ***interface_container;            /*!< \brief Definition of the interface of information and physics. */
+  bool dry_run;                                 /*!< \brief Flag if SU2_CFD was started as dry-run via "SU2_CFD -d <config>.cfg" */
+
+public:
+
   /*!
    * \brief Constructor of the class.
    * \param[in] confFile - Configuration file name.
    * \param[in] val_nZone - Total number of zones.
+   * \param[in] val_nDim - Number of dimensions.
    * \param[in] MPICommunicator - MPI communicator for SU2.
-   * \param[in] dummy_geo - Dummy geometric definition of the problem.
    */
-  CDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator, bool dummy_geo);
+  CDriver(char* confFile,
+          unsigned short val_nZone,
+          SU2_Comm MPICommunicator, bool dummy_geo);
 
   /*!
    * \brief Destructor of the class.
@@ -100,9 +121,10 @@ class CDriver : public CDriverBase {
   /*!
    * \brief A virtual member.
    */
-  virtual void Run(){};
+  virtual void Run() { };
+
+protected:
 
- protected:
   /*!
    * \brief Init_Containers
    */
@@ -110,180 +132,145 @@ class CDriver : public CDriverBase {
 
   /*!
    * \brief Read in the config and mesh files.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] driver_config - Definition of the driver configuration.
    */
-  void Input_Preprocessing(CConfig**& config, CConfig*& driver_config);
+  void Input_Preprocessing(CConfig **&config, CConfig *&driver_config);
 
   /*!
-   * \brief Construction of the edge-based data structure and the multi-grid structure.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] dummy - Definition of the dummy driver.
+   * \brief Construction of the edge-based data structure and the multigrid structure.
    */
-  void Geometrical_Preprocessing(CConfig* config, CGeometry**& geometry, bool dummy);
+  void Geometrical_Preprocessing(CConfig *config, CGeometry **&geometry, bool dummy);
 
   /*!
    * \brief Do the geometrical preprocessing for the DG FEM solver.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] geometry - Geometrical definition of the problem.
    */
-  void Geometrical_Preprocessing_DGFEM(CConfig* config, CGeometry**& geometry);
+  void Geometrical_Preprocessing_DGFEM(CConfig *config, CGeometry **&geometry);
 
   /*!
    * \brief Geometrical_Preprocessing_FVM
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] geometry - Geometrical definition of the problem.
    */
-  void Geometrical_Preprocessing_FVM(CConfig* config, CGeometry**& geometry);
+  void Geometrical_Preprocessing_FVM(CConfig *config, CGeometry **&geometry);
 
   /*!
    * \brief Definition of the physics iteration class or within a single zone.
+   * \param[in] iteration_container - Pointer to the iteration container to be instantiated.
    * \param[in] config - Definition of the particular problem.
-   * \param[in] iteration - Pointer to the iteration container to be instantiated.
+   * \param[in] iZone - Index of the zone.
    */
-  void Iteration_Preprocessing(CConfig* config, CIteration*& iteration) const;
+  void Iteration_Preprocessing(CConfig *config, CIteration *&iteration) const;
 
   /*!
    * \brief Definition and allocation of all solution classes.
-   * \param[in] config - Definition of the particular problem.
+   * \param[in] solver_container - Container vector with all the solutions.
    * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] solver - Container vector with all the solutions.
+   * \param[in] config - Definition of the particular problem.
    */
-  void Solver_Preprocessing(CConfig* config, CGeometry** geometry, CSolver***& solver);
+  void Solver_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***&solver);
 
   /*!
    * \brief Restart of the solvers from the restart files.
-   * \param[in] solver - Container vector with all the solutions.
+   * \param[in] solver_container - Container vector with all the solutions.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
-   * \param[in] update_geo - Boolean to indicate if geometry should be updated.
    */
-  void Solver_Restart(CSolver*** solver, CGeometry** geometry, CConfig* config, bool update_geo);
+  void Solver_Restart(CSolver ***solver, CGeometry **geometry, CConfig *config, bool update_geo);
 
   /*!
    * \brief Definition and allocation of all solution classes.
-   * \param[in] solver - Container vector with all the solutions.
+   * \param[in] solver_container - Container vector with all the solutions.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
-   * \param[in] val_iInst - Current solver instance.
    */
-  void Solver_Postprocessing(CSolver**** solver, CGeometry** geometry, CConfig* config, unsigned short val_iInst);
+  void Solver_Postprocessing(CSolver ****solver, CGeometry **geometry, CConfig *config, unsigned short val_iInst);
 
   /*!
    * \brief Definition and allocation of all integration classes.
    * \param[in] config - Definition of the particular problem.
    * \param[in] solver - Container vector with all the solutions.
-   * \param[in] integration - Container vector with all the integration methods.
+   * \param[out] integration - Container vector with all the integration methods.
    */
-  void Integration_Preprocessing(CConfig* config, CSolver** solver, CIntegration**& integration) const;
+  void Integration_Preprocessing(CConfig *config, CSolver **solver, CIntegration **&integration) const;
 
   /*!
    * \brief Definition and allocation of all integration classes.
-   * \param[in] integration - Container vector with all the integration methods.
+   * \param[in] integration_container - Container vector with all the integration methods.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
-   * \param[in] val_iInst - Current solver instance.
    */
-  void Integration_Postprocessing(CIntegration*** integration, CGeometry** geometry, CConfig* config,
-                                  unsigned short val_iInst);
+  void Integration_Postprocessing(CIntegration ***integration, CGeometry **geometry, CConfig *config, unsigned short val_iInst);
 
   /*!
    * \brief Definition and allocation of all interface classes.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] solver - Container vector with all the solutions.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] interface_types - Type of coupling between the distinct (physical) zones.
-   * \param[in] interface - Class defining the physical transfer of information.
-   * \param[in] interpolation -  Object defining the interpolation.
    */
-  void Interface_Preprocessing(CConfig** config, CSolver***** solver, CGeometry**** geometry,
-                               unsigned short** interface_types, CInterface*** interface,
-                               vector<vector<unique_ptr<CInterpolator>>>& interpolation);
+  void Interface_Preprocessing(CConfig **config, CSolver *****solver, CGeometry ****geometry,
+                               unsigned short **interface_types, CInterface ***interface,
+                               vector<vector<unique_ptr<CInterpolator> > > &interpolation);
 
   /*!
    * \brief Definition and allocation of all solver classes.
-   * \param[in] config - Definition of the particular problem.
+   * \param[in] numerics_container - Description of the numerical method (the way in which the equations are solved).
    * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] solver - Container vector with all the solutions.
-   * \param[in] numerics - Description of the numerical method (the way in which the equations are solved).
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] config - Definition of the particular problem.
    */
-  void Numerics_Preprocessing(CConfig* config, CGeometry** geometry, CSolver*** solver, CNumerics****& numerics) const;
+  void Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***solver, CNumerics ****&numerics) const;
 
   /*!
    * \brief Helper to instantiate turbulence numerics specialized for different flow solvers.
    */
   template <class FlowIndices>
-  void InstantiateTurbulentNumerics(unsigned short nVar_Turb, int offset, const CConfig* config,
-                                    const CSolver* turb_solver, CNumerics****& numerics) const;
+  void InstantiateTurbulentNumerics(unsigned short nVar_Turb, int offset, const CConfig *config,
+                                    const CSolver* turb_solver, CNumerics ****&numerics) const;
 
   /*!
    * \brief Helper to instantiate transition numerics specialized for different flow solvers.
    */
   template <class FlowIndices>
-  void InstantiateTransitionNumerics(unsigned short nVar_Trans, int offset, const CConfig* config,
-                                     const CSolver* trans_solver, CNumerics****& numerics) const;
+  void InstantiateTransitionNumerics(unsigned short nVar_Trans, int offset, const CConfig *config,
+                                    const CSolver* trans_solver, CNumerics ****&numerics) const;
   /*!
    * \brief Helper to instantiate species transport numerics specialized for different flow solvers.
    */
   template <class FlowIndices>
-  void InstantiateSpeciesNumerics(unsigned short nVar_Species, int offset, const CConfig* config,
-                                  const CSolver* species_solver, CNumerics****& numerics) const;
+  void InstantiateSpeciesNumerics(unsigned short nVar_Species, int offset, const CConfig *config,
+                                  const CSolver* species_solver, CNumerics ****&numerics) const;
 
   /*!
    * \brief Definition and allocation of all solver classes.
-   * \param[in] numerics - Description of the numerical method (the way in which the equations are solved).
-   * \param[in] solver - Container vector with all the solutions.
+   * \param[in] numerics_container - Description of the numerical method (the way in which the equations are solved).
+   * \param[in] solver_container - Container vector with all the solutions.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
-   * \param[in] val_iInst - Current solver instance.
    */
-  void Numerics_Postprocessing(CNumerics***** numerics, CSolver*** solver, CGeometry** geometry, CConfig* config,
-                               unsigned short val_iInst);
+  void Numerics_Postprocessing(CNumerics *****numerics, CSolver ***solver, CGeometry **geometry, CConfig *config, unsigned short val_iInst);
 
   /*!
    * \brief GridMovement_Preprocessing
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] solver - Container vector with all the solutions.
-   * \param[in] iteration - Container vector with all the iteration methods.
-   * \param[in] grid_movement - Volume grid movement classes of the problem.
-   * \param[in] surface_movement - Surface movement classes of the problem.
+   * \param config
+   * \param geometry
+   * \param solver
+   * \param iteration
+   * \param grid_movement
+   * \param surface_movement
    */
-  void DynamicMesh_Preprocessing(CConfig* config, CGeometry** geometry, CSolver*** solver, CIteration* iteration,
-                                 CVolumetricMovement*& grid_movement, CSurfaceMovement*& surface_movement) const;
+  void DynamicMesh_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***solver, CIteration *iteration, CVolumetricMovement *&grid_movement, CSurfaceMovement *&surface_movement) const;
 
   /*!
    * \brief Initialize Python interface functionalities
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] solver - Container vector with all the solutions.
    */
   void PythonInterface_Preprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver);
 
   /*!
    * \brief Preprocess the output container.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] driver_config - Definition of the driver configuration.
-   * \param[in] output_container - Container vector with all the outputs.
-   * \param[in] driver_output - Definition of the driver output.
    */
-  void Output_Preprocessing(CConfig** config, CConfig* driver_config, COutput**& output_container,
-                            COutput*& driver_output);
+  void Output_Preprocessing(CConfig **config, CConfig *driver_config, COutput **&output_container, COutput *&driver_output);
 
   /*!
    * \brief Initiate value for static mesh movement such as the gridVel for the ROTATING frame.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] geometry - Geometrical definition of the problem.
    */
-  void StaticMesh_Preprocessing(const CConfig* config, CGeometry** geometry);
+  void StaticMesh_Preprocessing(const CConfig *config, CGeometry **geometry);
 
   /*!
    * \brief Initiate value for static mesh movement such as the gridVel for the ROTATING frame.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] solver - Container vector with all the solutions.
-   * \param[in] interface - Class defining the physical transfer of information.
    */
   void Turbomachinery_Preprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver,
                                     CInterface*** interface);
@@ -333,14 +320,14 @@ class CDriver : public CDriverBase {
   virtual void Relaxation_Tractions(unsigned short donorZone, unsigned short targetZone, unsigned long iOuterIter) {}
 
   /*!
-   * \brief A virtual member to run a Block Gauss-Seidel iteration in multi-zone problems.
+   * \brief A virtual member to run a Block Gauss-Seidel iteration in multizone problems.
    */
-  virtual void Run_GaussSeidel() {}
+  virtual void Run_GaussSeidel(){}
 
   /*!
-   * \brief A virtual member to run a Block-Jacobi iteration in multi-zone problems.
+   * \brief A virtual member to run a Block-Jacobi iteration in multizone problems.
    */
-  virtual void Run_Jacobi() {}
+  virtual void Run_Jacobi(){}
 
   /*!
    * \brief A virtual member.
@@ -353,7 +340,8 @@ class CDriver : public CDriverBase {
    */
   void Print_DirectResidual(RECORDING kind_recording);
 
- public:
+public:
+
   /*!
    * \brief Launch the computation for all zones and all physics.
    */
@@ -372,37 +360,35 @@ class CDriver : public CDriverBase {
   /*!
    * \brief Perform some pre-processing before an iteration of the physics.
    */
-  virtual void Preprocess(unsigned long TimeIter) {}
+  virtual void Preprocess(unsigned long TimeIter){ }
 
   /*!
    * \brief Monitor the computation.
    */
-  virtual bool Monitor(unsigned long TimeIter) { return false; }
+  virtual bool Monitor(unsigned long TimeIter){ return false; }
 
   /*!
    * \brief Output the solution in solution file.
    */
-  virtual void Output(unsigned long TimeIter) {}
+  virtual void Output(unsigned long TimeIter){ }
 
   /*!
-   * \brief Perform a dynamic mesh deformation, including grid velocity computation and update of the multi-grid
-   * structure.
+   * \brief Perform a dynamic mesh deformation, including grid velocity computation and update of the multigrid structure.
    */
-  virtual void DynamicMeshUpdate(unsigned long TimeIter) {}
+  virtual void DynamicMeshUpdate(unsigned long TimeIter) { }
 
   /*!
-   * \brief Perform a dynamic mesh deformation, including grid velocity computation and update of the multi-grid
-   * structure.
+   * \brief Perform a dynamic mesh deformation, including grid velocity computation and update of the multigrid structure.
    */
-  virtual void DynamicMeshUpdate(unsigned short val_iZone, unsigned long TimeIter) {}
+  virtual void DynamicMeshUpdate(unsigned short val_iZone, unsigned long TimeIter) { }
 
   /*!
    * \brief Perform a mesh deformation as initial condition.
    */
-  virtual void SetInitialMesh() {}
+  virtual void SetInitialMesh() { }
 
   /*!
-   * \brief Process the boundary conditions and update the multi-grid structure.
+   * \brief Process the boundary conditions and update the multigrid structure.
    */
   void BoundaryConditionsUpdate();
 
@@ -448,6 +434,28 @@ class CDriver : public CDriverBase {
    */
   passivedouble Get_LiftCoeff() const;
 
+  /*!
+   * \brief Get the number of vertices (halo nodes included) from a specified marker.
+   * \param[in] iMarker -  Marker identifier.
+   * \return Number of vertices.
+   */
+  unsigned long GetNumberVertices(unsigned short iMarker) const;
+
+  /*!
+   * \brief Get the number of halo vertices from a specified marker.
+   * \param[in] iMarker - Marker identifier.
+   * \return Number of vertices.
+   */
+  unsigned long GetNumberHaloVertices(unsigned short iMarker) const;
+
+  /*!
+   * \brief Check if a vertex is physical or not (halo node) on a specified marker.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \return True if the specified vertex is a halo node.
+   */
+  bool IsAHaloNode(unsigned short iMarker, unsigned long iVertex) const;
+
   /*!
    * \brief Get the number of external iterations.
    * \return Number of external iterations.
@@ -472,6 +480,22 @@ class CDriver : public CDriverBase {
    */
   string GetSurfaceFileName() const;
 
+  /*!
+   * \brief Get the global index of a vertex on a specified marker.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \return Vertex global index.
+   */
+  unsigned long GetVertexGlobalIndex(unsigned short iMarker, unsigned long iVertex) const;
+
+  /*!
+   * \brief Get undeformed coordinates from the mesh solver.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \return x,y,z coordinates of the vertex.
+   */
+  vector<passivedouble> GetInitialMeshCoord(unsigned short iMarker, unsigned long iVertex) const;
+
   /*!
    * \brief Get the temperature at a vertex on a specified marker.
    * \param[in] iMarker - Marker identifier.
@@ -526,19 +550,77 @@ class CDriver : public CDriverBase {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void Inlet_Preprocessing(CSolver*** solver, CGeometry** geometry, CConfig* config) const;
+  void Inlet_Preprocessing(CSolver ***solver, CGeometry **geometry, CConfig *config) const;
+
+  /*!
+   * \brief Get the normal (vector) at a vertex on a specified marker.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \param[in] unitNormal - Bool to normalise the vector.
+   * \return Normal (vector) at the vertex.
+   */
+  vector<passivedouble> GetVertexNormal(unsigned short iMarker, unsigned long iVertex, bool unitNormal = false) const;
+
+  /*!
+   * \brief Get the unit normal (vector) at a vertex on a specified marker.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \return Unit normal (vector) at the vertex.
+   */
+  inline vector<passivedouble> GetVertexUnitNormal(unsigned short iMarker, unsigned long iVertex) const {
+    return GetVertexNormal(iMarker, iVertex, true);
+  }
+
+  /*!
+   * \brief Get all the boundary markers tags.
+   * \return List of boundary markers tags.
+   */
+  vector<string> GetAllBoundaryMarkersTag() const;
+
+  /*!
+   * \brief Get all the deformable boundary marker tags.
+   * \return List of deformable boundary markers tags.
+   */
+  vector<string> GetAllDeformMeshMarkersTag() const;
 
   /*!
-   * \brief Get all the CHT boundary marker tags.
-   * \return List of CHT boundary markers tags.
+   * \brief Get all the heat transfer boundary markers tags.
+   * \return List of heat transfer boundary markers tags.
    */
-  vector<string> GetCHTMarkerTags() const;
+  vector<string> GetAllCHTMarkersTag() const;
 
   /*!
-   * \brief Get all the inlet boundary marker tags.
+   * \brief Get all the (subsonic) inlet boundary markers tags.
    * \return List of inlet boundary markers tags.
    */
-  vector<string> GetInletMarkerTags() const;
+  vector<string> GetAllInletMarkersTag() const;
+
+  /*!
+   * \brief Get all the boundary markers tags with their associated indices.
+   * \return List of boundary markers tags with their indices.
+   */
+  map<string, int> GetAllBoundaryMarkers() const;
+
+  /*!
+   * \brief Get all the boundary markers tags with their associated types.
+   * \return List of boundary markers tags with their types.
+   */
+  map<string, string> GetAllBoundaryMarkersType() const;
+
+  /*!
+   * \brief Set the mesh displacement for the elasticity mesh solver.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \param[in] DispX - Value of the mesh displacement in the direction X.
+   * \param[in] DispY - Value of the mesh displacement in the direction Y.
+   * \param[in] DispZ - Value of the mesh displacement in the direction Z.
+   */
+  void SetMeshDisplacement(unsigned short iMarker, unsigned long iVertex, passivedouble DispX, passivedouble DispY, passivedouble DispZ);
+
+  /*!
+   * \brief Communicate the boundary mesh displacements in a python call
+   */
+  void CommunicateMeshDisplacement(void);
 
   /*!
    * \brief Return the sensitivities of the mesh boundary vertices.
@@ -556,8 +638,8 @@ class CDriver : public CDriverBase {
    * \param[in] LoadX - Value of the load in the direction Y.
    * \param[in] LoadX - Value of the load in the direction Z.
    */
-  void SetFEA_Loads(unsigned short iMarker, unsigned long iVertex, passivedouble LoadX, passivedouble LoadY,
-                    passivedouble LoadZ);
+  void SetFEA_Loads(unsigned short iMarker, unsigned long iVertex, passivedouble LoadX,
+                    passivedouble LoadY, passivedouble LoadZ);
 
   /*!
    * \brief Return the displacements from the FEA solver.
@@ -611,7 +693,7 @@ class CDriver : public CDriverBase {
    * \param[in] val_AdjointZ - Value of the adjoint in the direction Z.
    */
   void SetFlowLoad_Adjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
-                           passivedouble val_AdjointY, passivedouble val_AdjointZ);
+                                    passivedouble val_AdjointY, passivedouble val_AdjointZ);
 
   /*!
    * \brief Set the adjoint of the structural displacements (from an outside source)
@@ -624,7 +706,7 @@ class CDriver : public CDriverBase {
   void SetSourceTerm_DispAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
                                  passivedouble val_AdjointY, passivedouble val_AdjointZ);
   void SetSourceTerm_VelAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
-                                passivedouble val_AdjointY, passivedouble val_AdjointZ);
+                                 passivedouble val_AdjointY, passivedouble val_AdjointZ);
 
   /*!
    * \brief Set the position of the heat source.
@@ -664,7 +746,7 @@ class CDriver : public CDriverBase {
    * \param[in] solution - Solution object with interface (iPoint,iVar).
    * \tparam Old - If true set "old solutions" instead.
    */
-  template <class Container, bool Old = false>
+  template<class Container, bool Old = false>
   void SetAllSolutions(unsigned short iZone, bool adjoint, const Container& solution) {
     const auto nPoint = geometry_container[iZone][INST_0][MESH_0]->GetnPoint();
     for (auto iSol = 0u, offset = 0u; iSol < MAX_SOLS; ++iSol) {
@@ -672,11 +754,8 @@ class CDriver : public CDriverBase {
       if (!(solver && (solver->GetAdjoint() == adjoint))) continue;
       for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint)
         for (auto iVar = 0ul; iVar < solver->GetnVar(); ++iVar)
-          if (!Old) {
-            solver->GetNodes()->SetSolution(iPoint, iVar, solution(iPoint, offset + iVar));
-          } else {
-            solver->GetNodes()->SetSolution_Old(iPoint, iVar, solution(iPoint, offset + iVar));
-          }
+          if (!Old) solver->GetNodes()->SetSolution(iPoint, iVar, solution(iPoint,offset+iVar));
+          else solver->GetNodes()->SetSolution_Old(iPoint, iVar, solution(iPoint,offset+iVar));
       offset += solver->GetnVar();
     }
   }
@@ -684,9 +763,9 @@ class CDriver : public CDriverBase {
   /*!
    * \brief Set the "old solution" of all solvers (adjoint or primal) in a zone.
    */
-  template <class Container>
+  template<class Container>
   void SetAllSolutionsOld(unsigned short iZone, bool adjoint, const Container& solution) {
-    SetAllSolutions<Container, true>(iZone, adjoint, solution);
+    SetAllSolutions<Container,true>(iZone, adjoint, solution);
   }
 
   /*!
@@ -695,7 +774,7 @@ class CDriver : public CDriverBase {
    * \param[in] adjoint - True to consider adjoint solvers instead of primal.
    * \param[out] solution - Solution object with interface (iPoint,iVar).
    */
-  template <class Container>
+  template<class Container>
   void GetAllSolutions(unsigned short iZone, bool adjoint, Container& solution) const {
     const auto nPoint = geometry_container[iZone][INST_0][MESH_0]->GetnPoint();
     for (auto iSol = 0u, offset = 0u; iSol < MAX_SOLS; ++iSol) {
@@ -704,10 +783,11 @@ class CDriver : public CDriverBase {
       const auto& sol = solver->GetNodes()->GetSolution();
       for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint)
         for (auto iVar = 0ul; iVar < solver->GetnVar(); ++iVar)
-          solution(iPoint, offset + iVar) = SU2_TYPE::GetValue(sol(iPoint, iVar));
+          solution(iPoint,offset+iVar) = SU2_TYPE::GetValue(sol(iPoint,iVar));
       offset += solver->GetnVar();
     }
   }
+
 };
 
 /*!
@@ -717,19 +797,24 @@ class CDriver : public CDriverBase {
  * \author T. Economon, G. Gori
  */
 class CFluidDriver : public CDriver {
- protected:
-  unsigned long Max_Iter;
 
- protected:
+protected:
+   unsigned long Max_Iter;
+
+protected:
+
   /*!
    * \brief Constructor of the class.
    * \param[in] confFile - Configuration file name.
    * \param[in] val_nZone - Total number of zones.
+   * \param[in] val_nDim - Number of dimensions.
    * \param[in] MPICommunicator - MPI communicator for SU2.
    */
-  CFluidDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator);
+  CFluidDriver(char* confFile,
+               unsigned short val_nZone,
+               SU2_Comm MPICommunicator);
 
- public:
+public:
   /*!
    * \brief Destructor of the class.
    */
@@ -766,8 +851,7 @@ class CFluidDriver : public CDriver {
   void Preprocess(unsigned long Iter) override;
 
   /*!
-   * \brief Perform a dynamic mesh deformation, included grid velocity computation and the update of the multi-grid
-   * structure (multiple zone).
+   * \brief Perform a dynamic mesh deformation, included grid velocity computation and the update of the multigrid structure (multiple zone).
    */
   void DynamicMeshUpdate(unsigned long TimeIter) override;
 
@@ -775,8 +859,10 @@ class CFluidDriver : public CDriver {
    * \brief Transfer data among different zones (multiple zone).
    */
   void Transfer_Data(unsigned short donorZone, unsigned short targetZone);
+
 };
 
+
 /*!
  * \class CTurbomachineryDriver
  * \ingroup Drivers
@@ -784,17 +870,22 @@ class CFluidDriver : public CDriver {
  * \author S. Vitale
  */
 class CTurbomachineryDriver : public CFluidDriver {
- private:
+private:
   COutputLegacy* output_legacy;
 
- public:
+public:
+
   /*!
    * \brief Constructor of the class.
    * \param[in] confFile - Configuration file name.
    * \param[in] val_nZone - Total number of zones.
+   * \param[in] val_nDim - Number of dimensions.
+   * \param[in] val_periodic - Bool for periodic BCs.
    * \param[in] MPICommunicator - MPI communicator for SU2.
    */
-  CTurbomachineryDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator);
+  CTurbomachineryDriver(char* confFile,
+                        unsigned short val_nZone,
+                        SU2_Comm MPICommunicator);
 
   /*!
    * \brief Destructor of the class.
@@ -821,6 +912,9 @@ class CTurbomachineryDriver : public CFluidDriver {
    * \brief Monitor the computation.
    */
   bool Monitor(unsigned long TimeIter) override;
+
+
+
 };
 
 /*!
@@ -830,19 +924,24 @@ class CTurbomachineryDriver : public CFluidDriver {
  * \author T. Economon
  */
 class CHBDriver : public CFluidDriver {
- private:
+
+private:
   COutputLegacy* output_legacy;
   unsigned short nInstHB;
-  su2double** D; /*!< \brief Harmonic Balance operator. */
+  su2double **D; /*!< \brief Harmonic Balance operator. */
+
+public:
 
- public:
   /*!
    * \brief Constructor of the class.
    * \param[in] confFile - Configuration file name.
    * \param[in] val_nZone - Total number of zones.
+   * \param[in] val_nDim - Number of dimensions.
    * \param[in] MPICommunicator - MPI communicator for SU2.
    */
-  CHBDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator);
+  CHBDriver(char* confFile,
+            unsigned short val_nZone,
+            SU2_Comm MPICommunicator);
 
   /*!
    * \brief Destructor of the class.
diff --git a/SU2_CFD/include/numerics/CNumerics.hpp b/SU2_CFD/include/numerics/CNumerics.hpp
index 194ce67557c..e8682cc8da5 100644
--- a/SU2_CFD/include/numerics/CNumerics.hpp
+++ b/SU2_CFD/include/numerics/CNumerics.hpp
@@ -71,9 +71,6 @@ class CNumerics {
   Thermal_Conductivity_j,    /*!< \brief Thermal conductivity at point j. */
   Thermal_Conductivity_ve_i, /*!< \brief vibrational-electronic Thermal conductivity at point i. */
   Thermal_Conductivity_ve_j, /*!< \brief vibrational-electronic Thermal conductivity at point j. */
-  Thermal_Diffusivity_i,     /*!< \brief Thermal diffusivity at point i. */
-  Thermal_Diffusivity_j;     /*!< \brief Thermal diffusivity at point j. */
-  su2double 
   Cp_i,               /*!< \brief Cp at point i. */
   Cp_j;               /*!< \brief Cp at point j. */
   su2double
@@ -109,9 +106,6 @@ class CNumerics {
   su2double
   dist_i,  /*!< \brief Distance of point i to the nearest wall. */
   dist_j;  /*!< \brief Distance of point j to the nearest wall. */
-  su2double
-  Temp_i,  /*!< \brief Temperature at point i. */
-  Temp_j;  /*!< \brief Temperature at point j. */
   const su2double
   *Und_Lapl_i,  /*!< \brief Undivided laplacians at point i. */
   *Und_Lapl_j;  /*!< \brief Undivided laplacians at point j. */
@@ -794,18 +788,6 @@ class CNumerics {
     Thermal_Conductivity_ve_j = val_thermal_conductivity_ve_j;
   }
 
-  /*!
-   * \brief Set the thermal diffusivity (translational/rotational)
-   * \param[in] val_thermal_diffusivity_i - Value of the thermal diffusivity at point i.
-   * \param[in] val_thermal_diffusivity_j - Value of the thermal diffusivity at point j.
-   * \param[in] iSpecies - Value of the species.
-   */
-  inline void SetThermalDiffusivity(su2double val_thermal_diffusivity_i,
-                                    su2double val_thermal_diffusivity_j) {
-    Thermal_Diffusivity_i = val_thermal_diffusivity_i;
-    Thermal_Diffusivity_j = val_thermal_diffusivity_j;
-  }
-  
   /*!
    * \brief Set the specifc heat c_p.
    * \param[in] val_specific_heat_i - Value of the specific heat at point i.
@@ -938,16 +920,6 @@ class CNumerics {
     SoundSpeed_j = val_soundspeed_j;
   }
 
-  /*!
-   * \brief Set the value of the temperature.
-   * \param[in] val_temp_i - Value of the temperature at point i.
-   * \param[in] val_temp_j - Value of the temperature at point j.
-   */
-  inline void SetTemperature(su2double val_temp_i, su2double val_temp_j) {
-    Temp_i = val_temp_i;
-    Temp_j = val_temp_j;
-  }
-
   /*!
    * \brief Set the value of the enthalpy.
    * \param[in] val_enthalpy_i - Value of the enthalpy at point i.
diff --git a/SU2_CFD/include/numerics/NEMO/NEMO_diffusion.hpp b/SU2_CFD/include/numerics/NEMO/NEMO_diffusion.hpp
index 88701d0c79d..5a8a10c128a 100644
--- a/SU2_CFD/include/numerics/NEMO/NEMO_diffusion.hpp
+++ b/SU2_CFD/include/numerics/NEMO/NEMO_diffusion.hpp
@@ -94,7 +94,7 @@ class CAvgGrad_NEMO : public CNEMONumerics {
  */
 class CAvgGradCorrected_NEMO : public CNEMONumerics {
 private:
-  unsigned short
+  unsigned short iDim, iVar,
   nPrimVar, nPrimVarGrad;       /*!< \brief Iterators in dimension an variable. */
   su2double
   *Mean_PrimVar,                /*!< \brief Mean primitive variables. */
diff --git a/SU2_CFD/include/solvers/CHeatSolver.hpp b/SU2_CFD/include/solvers/CHeatSolver.hpp
index fa78861fb19..2074d479a6a 100644
--- a/SU2_CFD/include/solvers/CHeatSolver.hpp
+++ b/SU2_CFD/include/solvers/CHeatSolver.hpp
@@ -27,7 +27,7 @@
 
 #pragma once
 
-#include "CSolver.hpp"
+#include "CScalarSolver.hpp"
 #include "../variables/CHeatVariable.hpp"
 
 /*!
@@ -36,7 +36,7 @@
  * \author O. Burghardt
  * \version 7.5.1 "Blackbird"
  */
-class CHeatSolver final : public CSolver {
+class CHeatSolver final : public CScalarSolver<CHeatVariable> {
 protected:
   static constexpr size_t MAXNDIM = 3; /*!< \brief Max number of space dimensions, used in some static arrays. */
   static constexpr size_t MAXNVAR = 1; /*!< \brief Max number of variables, for static arrays. */
@@ -44,27 +44,91 @@ class CHeatSolver final : public CSolver {
   const bool flow; /*!< \brief Use solver as a scalar transport equation of Temperature for the inc solver. */
   const bool heat_equation; /*!< \brief use solver for heat conduction in solids. */
 
-  unsigned short nVarFlow, nMarker;
-  vector<vector<su2double> > HeatFlux;
+  su2double Global_Delta_Time = 0.0, Global_Delta_UnstTimeND = 0.0;
+
+  vector<vector<su2double>> HeatFlux;
   vector<su2double> HeatFlux_per_Marker;
   su2double Total_HeatFlux;
   su2double AllBound_HeatFlux;
   vector<su2double> AverageT_per_Marker;
   su2double Total_AverageT;
   su2double AllBound_AverageT;
-  vector<su2double>  Primitive_Flow_i;
-  vector<su2double> Primitive_Flow_j;
   vector<su2double> Surface_Areas;
   su2double Total_HeatFlux_Areas;
   su2double Total_HeatFlux_Areas_Monitor;
   vector<su2activematrix> ConjugateVar;
 
-  CHeatVariable* nodes = nullptr;  /*!< \brief The highest level in the variable hierarchy this solver can safely use. */
+  /*!
+   * \brief Applies an isothermal condition to a vertex of a marker.
+   */
+  void IsothermalBoundaryCondition(CGeometry *geometry, CSolver *flow_solver, const CConfig *config,
+                                   unsigned short iMarker, unsigned long iVertex, const su2double& temperature) {
+
+    const auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+    if (!geometry->nodes->GetDomain(iPoint)) return;
+
+    const bool implicit = config->GetKind_TimeIntScheme() == EULER_IMPLICIT;
+    const su2double prandtl_lam = config->GetPrandtl_Lam();
+    const su2double const_diffusivity = config->GetThermalDiffusivity();
+
+    const auto Point_Normal = geometry->vertex[iMarker][iVertex]->GetNormal_Neighbor();
+
+    const auto* Normal = geometry->vertex[iMarker][iVertex]->GetNormal();
+    const su2double Area = GeometryToolbox::Norm(nDim, Normal);
+
+    const auto* Coord_i = geometry->nodes->GetCoord(iPoint);
+    const auto* Coord_j = geometry->nodes->GetCoord(Point_Normal);
+    const su2double dist_ij = GeometryToolbox::Distance(nDim, Coord_i, Coord_j);
+
+    const su2double dTdn = -(nodes->GetTemperature(Point_Normal) - temperature) / dist_ij;
+
+    su2double thermal_diffusivity = const_diffusivity;
+    if (flow) {
+      thermal_diffusivity = flow_solver->GetNodes()->GetLaminarViscosity(iPoint) / prandtl_lam;
+    }
+    LinSysRes(iPoint, 0) -= thermal_diffusivity * dTdn * Area;
+
+    if (implicit) {
+      su2double Jacobian_i[] = {-thermal_diffusivity / dist_ij * Area};
+      Jacobian.SubtractBlock2Diag(iPoint, &Jacobian_i);
+    }
+  }
 
   /*!
-   * \brief Return nodes to allow CSolver::base_nodes to be set.
+   * \brief Compute the viscous flux for the scalar equation at a particular edge.
+   * \param[in] iEdge - Edge for which we want to compute the flux
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] numerics - Description of the numerical method.
+   * \param[in] config - Definition of the particular problem.
+   * \note Calls a generic implementation after defining a SolverSpecificNumerics object.
    */
-  inline CVariable* GetBaseClassPointerToNodes() override { return nodes; }
+  inline void Viscous_Residual(unsigned long iEdge, CGeometry* geometry, CSolver** solver_container,
+                                       CNumerics* numerics, CConfig* config) override {
+    const CVariable* flow_nodes = flow ? solver_container[FLOW_SOL]->GetNodes() : nullptr;
+
+    const su2double const_diffusivity = config->GetThermalDiffusivity();
+    const su2double pr_lam = config->GetPrandtl_Lam();
+    const su2double pr_turb = config->GetPrandtl_Turb();
+
+    su2double thermal_diffusivity_i{}, thermal_diffusivity_j{};
+
+    /*--- Computes the thermal diffusivity to use in the viscous numerics. ---*/
+    auto compute_thermal_diffusivity = [&](unsigned long iPoint, unsigned long jPoint) {
+      if (flow) {
+        thermal_diffusivity_i = flow_nodes->GetLaminarViscosity(iPoint) / pr_lam +
+                                flow_nodes->GetEddyViscosity(iPoint) / pr_turb;
+        thermal_diffusivity_j = flow_nodes->GetLaminarViscosity(jPoint) / pr_lam +
+                                flow_nodes->GetEddyViscosity(jPoint) / pr_turb;
+        numerics->SetDiffusionCoeff(&thermal_diffusivity_i, &thermal_diffusivity_j);
+      }
+      else {
+        numerics->SetDiffusionCoeff(&const_diffusivity, &const_diffusivity);
+      }
+    };
+    /*--- Compute residual and Jacobians. ---*/
+    Viscous_Residual_impl(compute_thermal_diffusivity, iEdge, geometry, solver_container, numerics, config);
+  }
 
 public:
 
@@ -73,11 +137,6 @@ class CHeatSolver final : public CSolver {
    */
   CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iMesh);
 
-  /*!
-   * \brief Destructor of the class.
-   */
-  ~CHeatSolver(void) override;
-
   /*!
    * \brief Restart residual and compute gradients.
    * \param[in] geometry - Geometrical definition of the problem.
@@ -96,18 +155,6 @@ class CHeatSolver final : public CSolver {
                     unsigned short RunTime_EqSystem,
                     bool Output) override;
 
-  /*!
-   * \brief A virtual member.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] iMesh - Index of the mesh in multigrid computations.
-   */
-  void Postprocessing(CGeometry *geometry,
-                      CSolver **solver_container,
-                      CConfig *config,
-                      unsigned short iMesh) override;
-
   /*!
    * \brief Load a solution from a restart file.
    * \param[in] geometry - Geometrical definition of the problem.
@@ -122,21 +169,6 @@ class CHeatSolver final : public CSolver {
                    int val_iter,
                    bool val_update_geo) override;
 
-  /*!
-   * \brief Compute the spatial integration using a centered scheme.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] numerics_container - Description of the numerical method.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] iMesh - Index of the mesh in multigrid computations.
-   * \param[in] iRKStep - Current step of the Runge-Kutta iteration.
-   */
-  void Centered_Residual(CGeometry *geometry,
-                        CSolver **solver_container,
-                        CNumerics **numerics_container,
-                        CConfig *config,
-                        unsigned short iMesh,
-                        unsigned short iRKStep) override;
   /*!
    * \brief Compute the spatial integration using a upwind scheme.
    * \param[in] geometry - Geometrical definition of the problem.
@@ -247,15 +279,6 @@ class CHeatSolver final : public CSolver {
                                   CConfig *config,
                                   unsigned short val_marker) override;
 
-  /*!
-   * \brief Impose a periodic boundary condition by summing contributions from the complete control volume.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] numerics - Description of the numerical method.
-   * \param[in] config - Definition of the particular problem.
-   */
-  void BC_Periodic(CGeometry* geometry, CSolver** solver_container, CNumerics* numerics, CConfig* config) final;
-
   /*!
    * \brief Set the conjugate heat variables.
    * \param[in] val_marker        - marker index
@@ -330,26 +353,6 @@ class CHeatSolver final : public CSolver {
     }
   }
 
-  /*!
-   * \brief Update the solution using an implicit solver.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] config - Definition of the particular problem.
-   */
-  void ImplicitEuler_Iteration(CGeometry *geometry,
-                               CSolver **solver_container,
-                               CConfig *config) override;
-
-  /*!
-   * \brief Update the solution using an explicit solver.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] config - Definition of the particular problem.
-   */
-  void ExplicitEuler_Iteration(CGeometry *geometry,
-                               CSolver **solver_container,
-                               CConfig *config) override;
-
   /*!
    * \brief A virtual member.
    * \param[in] geometry - Geometrical definition of the problem.
@@ -399,5 +402,4 @@ class CHeatSolver final : public CSolver {
    * \return Value of the heat flux.
    */
   inline su2double GetHeatFlux(unsigned short val_marker, unsigned long val_vertex) const override { return HeatFlux[val_marker][val_vertex]; }
-
 };
diff --git a/SU2_CFD/include/solvers/CMeshSolver.hpp b/SU2_CFD/include/solvers/CMeshSolver.hpp
index 79876e016c1..d03a841f5e3 100644
--- a/SU2_CFD/include/solvers/CMeshSolver.hpp
+++ b/SU2_CFD/include/solvers/CMeshSolver.hpp
@@ -125,7 +125,6 @@ class CMeshSolver final : public CFEASolver {
   /*!
    * \brief Grid deformation using the linear elasticity equations.
    * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] numerics - Numerics used in the solution.
    * \param[in] config - Definition of the particular problem.
    */
   void DeformMesh(CGeometry **geometry,
@@ -134,10 +133,11 @@ class CMeshSolver final : public CFEASolver {
 
   /*!
    * \brief Set the stiffness of the mesh.
-   * \param[in] numerics - Numerics used in the solution.
+   * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetMesh_Stiffness(CNumerics **numerics,
+  void SetMesh_Stiffness(CGeometry **geometry,
+                         CNumerics **numerics,
                          CConfig *config) override;
 
   /*!
diff --git a/SU2_CFD/include/solvers/CSolver.hpp b/SU2_CFD/include/solvers/CSolver.hpp
index 954b06ad75d..f87fcf58c44 100644
--- a/SU2_CFD/include/solvers/CSolver.hpp
+++ b/SU2_CFD/include/solvers/CSolver.hpp
@@ -4167,16 +4167,8 @@ class CSolver {
    * \param[in] config - Definition of the particular problem.
    * \param[in] referenceCoord - Determine if the mesh is deformed from the reference or from the current coordinates.
    */
-  inline virtual void DeformMesh(CGeometry *geometry,
-                                 CNumerics **numerics,
-                                 CConfig *config) { }
-
-  /*!
-   * \brief A virtual member.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] referenceCoord - Determine if the mesh is deformed from the reference or from the current coordinates.
-   */
-  inline virtual void SetMesh_Stiffness(CNumerics **numerics,
+  inline virtual void SetMesh_Stiffness(CGeometry **geometry,
+                                        CNumerics **numerics,
                                         CConfig *config) { }
 
   /*!
diff --git a/SU2_CFD/include/variables/CHeatVariable.hpp b/SU2_CFD/include/variables/CHeatVariable.hpp
index 344ce4f9572..4bc2d0c1909 100644
--- a/SU2_CFD/include/variables/CHeatVariable.hpp
+++ b/SU2_CFD/include/variables/CHeatVariable.hpp
@@ -27,7 +27,7 @@
 
 #pragma once
 
-#include "CVariable.hpp"
+#include "CScalarVariable.hpp"
 
 /*!
  * \class CHeatVariable
@@ -35,12 +35,10 @@
  * \author O. Burghardt
  * \version 7.5.1 "Blackbird"
  */
-class CHeatVariable final : public CVariable {
-protected:
-  CVectorOfMatrix& Gradient_Reconstruction;  /*!< \brief Reference to the gradient of the primitive variables for MUSCL reconstruction for the convective term */
-  CVectorOfMatrix Gradient_Aux;              /*!< \brief Auxiliary structure to store a second gradient for reconstruction, if required. */
-
+class CHeatVariable final : public CScalarVariable {
 public:
+  static constexpr size_t MAXNVAR = 1; /*!< \brief Max number of variables, for static arrays. */
+
   /*!
    * \brief Constructor of the class.
    * \param[in] heat - Values of the Heat solution (initialization value).
@@ -51,29 +49,10 @@ class CHeatVariable final : public CVariable {
    */
   CHeatVariable(su2double heat, unsigned long npoint, unsigned long ndim, unsigned long nvar, CConfig *config);
 
-  /*!
-   * \brief Destructor of the class.
-   */
-  ~CHeatVariable() override = default;
-
-  /*!
-   * \brief Get the array of the reconstruction variables gradient at a node.
-   * \param[in] iPoint - Index of the current node.
-   * \return Array of the reconstruction variables gradient at a node.
-   */
-  inline CMatrixView<su2double> GetGradient_Reconstruction(unsigned long iPoint) final { return Gradient_Reconstruction[iPoint]; }
-
-  /*!
-   * \brief Get the reconstruction gradient for primitive variable at all points.
-   * \return Reference to variable reconstruction gradient.
-   */
-  inline CVectorOfMatrix& GetGradient_Reconstruction() final { return Gradient_Reconstruction; }
-  inline const CVectorOfMatrix& GetGradient_Reconstruction() const final { return Gradient_Reconstruction; }
-
   /*!
    * \brief Get the temperature of the point.
    * \return Value of the temperature of the point.
    */
-  inline su2double GetTemperature(unsigned long iPoint) const final { return Solution(iPoint,0); }
+  inline su2double GetTemperature(unsigned long iPoint) const final { return Solution(iPoint, 0); }
 
 };
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index cf69fefeddd..121cd94e9a5 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -107,9 +107,10 @@
 #include <fenv.h>
 
 CDriver::CDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator, bool dummy_geo) :
-CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false), fem_solver(false), dry_run(dummy_geo) {
+  config_file_name(confFile), StartTime(0.0), StopTime(0.0), UsedTime(0.0),
+  TimeIter(0), nZone(val_nZone), StopCalc(false), fsi(false), fem_solver(false), dry_run(dummy_geo) {
 
-    /*--- Initialize Medipack (must also be here so it is initialized from python) ---*/
+  /*--- Initialize Medipack (must also be here so it is initialized from python) ---*/
 #ifdef HAVE_MPI
   #if defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)
     SU2_MPI::Init_AMPI();
@@ -601,10 +602,6 @@ void CDriver::Input_Preprocessing(CConfig **&config, CConfig *&driver_config) {
     }
   }
 
-  /*--- Keep a reference to the main (ZONE 0) config. ---*/
-
-  main_config = config_container[ZONE_0];
-
   /*--- Determine whether or not the FEM solver is used, which decides the type of
    *    geometry classes that are instantiated. Only adapted for single-zone problems ---*/
 
@@ -709,9 +706,6 @@ void CDriver::Geometrical_Preprocessing(CConfig* config, CGeometry **&geometry,
 
   }
 
-  /*--- Keep a reference to the main (ZONE_0, INST_0, MESH_0) geometry. ---*/
-
-  main_geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 }
 
 void CDriver::Geometrical_Preprocessing_FVM(CConfig *config, CGeometry **&geometry) {
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index c9d0f8ce227..d38f5f67610 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -359,8 +359,8 @@ unsigned long CDataDrivenFluid::Predict_MLP(su2double rho, su2double e) {
   /* Apply exponential transformation to the MLP outputs for the first and second
      derivative of the entropy w.r.t density */
   // Optional:
-  // dsdrho_e = -exp(dsdrho_e);
-  // d2sdrho2 = exp(d2sdrho2);
+  dsdrho_e = -exp(dsdrho_e);
+  d2sdrho2 = exp(d2sdrho2);
 
   return exit_code;
 }
diff --git a/SU2_CFD/src/fluid/CPengRobinson.cpp b/SU2_CFD/src/fluid/CPengRobinson.cpp
index c2c89c61ca3..445854b55cb 100644
--- a/SU2_CFD/src/fluid/CPengRobinson.cpp
+++ b/SU2_CFD/src/fluid/CPengRobinson.cpp
@@ -26,7 +26,6 @@
  */
 
 #include "../../include/fluid/CPengRobinson.hpp"
-#include "../../../Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp"
 
 CPengRobinson::CPengRobinson(su2double gamma, su2double R, su2double Pstar, su2double Tstar, su2double w)
     : CIdealGas(gamma, R) {
diff --git a/SU2_CFD/src/iteration/CIteration.cpp b/SU2_CFD/src/iteration/CIteration.cpp
index 5b2eaa5cef1..337e24edaea 100644
--- a/SU2_CFD/src/iteration/CIteration.cpp
+++ b/SU2_CFD/src/iteration/CIteration.cpp
@@ -163,7 +163,7 @@ void CIteration::SetMesh_Deformation(CGeometry** geometry, CSolver** solver, CNu
 
   /*--- Set the stiffness of each element mesh into the mesh numerics ---*/
 
-  solver[MESH_SOL]->SetMesh_Stiffness(numerics[MESH_SOL], config);
+  solver[MESH_SOL]->SetMesh_Stiffness(geometry, numerics[MESH_SOL], config);
 
   /*--- Deform the volume grid around the new boundary locations ---*/
 
diff --git a/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp b/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
index bb9874c1c06..cc64e14d1e2 100644
--- a/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
+++ b/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
@@ -293,7 +293,7 @@ CNumerics::ResidualType<> CAvgGradCorrected_NEMO::ComputeResidual(const CConfig
     Mean_PrimVar[iVar] = 0.5*(PrimVar_i[iVar]+PrimVar_j[iVar]);
   }
   for (auto iVar = nSpecies; iVar < nPrimVarGrad; iVar++) {
-    for (auto iDim = 0; iDim < nDim; iDim++) {
+    for (iDim = 0; iDim < nDim; iDim++) {
       Mean_GradPrimVar[iVar][iDim] = 0.5*(PrimVar_Grad_i[iVar][iDim] +
                                           PrimVar_Grad_j[iVar][iDim]);
     }
diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index 95e8cd321f7..32672e87eef 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -25,18 +25,22 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-#include "../../Common/include/toolboxes/geometry_toolbox.hpp"
+
 #include "../include/drivers/CDriver.hpp"
 #include "../include/drivers/CSinglezoneDriver.hpp"
+#include "../../Common/include/toolboxes/geometry_toolbox.hpp"
+
+void CDriver::PythonInterface_Preprocessing(CConfig **config, CGeometry ****geometry, CSolver *****solver){
 
-void CDriver::PythonInterface_Preprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver) {
   int rank = MASTER_NODE;
   SU2_MPI::Comm_rank(SU2_MPI::GetComm(), &rank);
 
-  /* --- Initialize boundary conditions customization, this is achieved through the Python wrapper. --- */
-  for (iZone = 0; iZone < nZone; iZone++) {
-    if (config[iZone]->GetnMarker_PyCustom() > 0) {
-      if (rank == MASTER_NODE) cout << "----------------- Python Interface Preprocessing ( Zone " << iZone << " ) -----------------" << endl;
+  /* --- Initialize boundary conditions customization, this is achieve through the Python wrapper --- */
+  for(iZone=0; iZone < nZone; iZone++){
+
+    if (config[iZone]->GetnMarker_PyCustom() > 0){
+
+      if (rank == MASTER_NODE) cout << endl << "----------------- Python Interface Preprocessing ( Zone "<< iZone <<" ) -----------------" << endl;
 
       if (rank == MASTER_NODE) cout << "Setting customized boundary conditions for zone " << iZone << endl;
       for (iMesh = 0; iMesh <= config[iZone]->GetnMGLevels(); iMesh++) {
@@ -46,23 +50,21 @@ void CDriver::PythonInterface_Preprocessing(CConfig** config, CGeometry**** geom
 
       if ((config[iZone]->GetKind_Solver() == MAIN_SOLVER::EULER) ||
           (config[iZone]->GetKind_Solver() == MAIN_SOLVER::NAVIER_STOKES) ||
-          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::RANS) ||
-          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::INC_EULER) ||
-          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::INC_NAVIER_STOKES) ||
-          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::INC_RANS) ||
-          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::NEMO_EULER) ||
-          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::NEMO_NAVIER_STOKES)) {
+          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::RANS)) {
+
         solver[iZone][INST_0][MESH_0][FLOW_SOL]->UpdateCustomBoundaryConditions(geometry[iZone][INST_0], config[iZone]);
       }
     }
   }
+
 }
 
 /////////////////////////////////////////////////////////////////////////////
-/* Functions related to the global performance indices (Lift, Drag, etc.)  */
+/* Functions related to the global performance indices (Lift, Drag, ecc..) */
 /////////////////////////////////////////////////////////////////////////////
 
 passivedouble CDriver::Get_Drag() const {
+
   unsigned short val_iZone = ZONE_0;
   unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
   su2double CDrag, factor, val_Drag;
@@ -71,12 +73,13 @@ passivedouble CDriver::Get_Drag() const {
   factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
   CDrag = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CD();
 
-  val_Drag = CDrag * factor;
+  val_Drag = CDrag*factor;
 
   return SU2_TYPE::GetValue(val_Drag);
 }
 
 passivedouble CDriver::Get_Lift() const {
+
   unsigned short val_iZone = ZONE_0;
   unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
   su2double CLift, factor, val_Lift;
@@ -85,12 +88,13 @@ passivedouble CDriver::Get_Lift() const {
   factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
   CLift = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CL();
 
-  val_Lift = CLift * factor;
+  val_Lift = CLift*factor;
 
   return SU2_TYPE::GetValue(val_Lift);
 }
 
 passivedouble CDriver::Get_Mx() const {
+
   unsigned short val_iZone = ZONE_0;
   unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
   su2double CMx, RefLengthCoeff, factor, val_Mx;
@@ -101,12 +105,13 @@ passivedouble CDriver::Get_Mx() const {
   factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
   CMx = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMx();
 
-  val_Mx = CMx * factor * RefLengthCoeff;
+  val_Mx = CMx*factor*RefLengthCoeff;
 
   return SU2_TYPE::GetValue(val_Mx);
 }
 
 passivedouble CDriver::Get_My() const {
+
   unsigned short val_iZone = ZONE_0;
   unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
   su2double CMy, RefLengthCoeff, factor, val_My;
@@ -117,12 +122,13 @@ passivedouble CDriver::Get_My() const {
   factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
   CMy = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMy();
 
-  val_My = CMy * factor * RefLengthCoeff;
+  val_My = CMy*factor*RefLengthCoeff;
 
   return SU2_TYPE::GetValue(val_My);
 }
 
 passivedouble CDriver::Get_Mz() const {
+
   unsigned short val_iZone = ZONE_0;
   unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
   su2double CMz, RefLengthCoeff, factor, val_Mz;
@@ -133,12 +139,13 @@ passivedouble CDriver::Get_Mz() const {
   factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
   CMz = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMz();
 
-  val_Mz = CMz * factor * RefLengthCoeff;
+  val_Mz = CMz*factor*RefLengthCoeff;
 
   return SU2_TYPE::GetValue(val_Mz);
 }
 
 passivedouble CDriver::Get_DragCoeff() const {
+
   unsigned short val_iZone = ZONE_0;
   unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
   su2double CDrag;
@@ -149,6 +156,7 @@ passivedouble CDriver::Get_DragCoeff() const {
 }
 
 passivedouble CDriver::Get_LiftCoeff() const {
+
   unsigned short val_iZone = ZONE_0;
   unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
   su2double CLift;
@@ -158,25 +166,129 @@ passivedouble CDriver::Get_LiftCoeff() const {
   return SU2_TYPE::GetValue(CLift);
 }
 
+/////////////////////////////////////////////////////////////////////////////
+/* Functions to obtain information from the geometry/mesh                  */
+/////////////////////////////////////////////////////////////////////////////
+
+unsigned long CDriver::GetNumberVertices(unsigned short iMarker) const {
+
+  return geometry_container[ZONE_0][INST_0][MESH_0]->nVertex[iMarker];
+
+}
+
+unsigned long CDriver::GetNumberHaloVertices(unsigned short iMarker) const {
+
+  unsigned long nHaloVertices, iVertex, iPoint;
+
+  nHaloVertices = 0;
+  for(iVertex = 0; iVertex < geometry_container[ZONE_0][INST_0][MESH_0]->nVertex[iMarker]; iVertex++){
+    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+    if(!(geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint))) nHaloVertices += 1;
+  }
+
+  return nHaloVertices;
+
+}
+
+unsigned long CDriver::GetVertexGlobalIndex(unsigned short iMarker, unsigned long iVertex) const {
+
+  unsigned long iPoint, GlobalIndex;
+
+  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+  GlobalIndex = geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetGlobalIndex(iPoint);
+
+  return GlobalIndex;
+
+}
+
+bool CDriver::IsAHaloNode(unsigned short iMarker, unsigned long iVertex) const {
+
+  unsigned long iPoint;
+
+  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+  if(geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint)) return false;
+  else return true;
+
+}
+
+vector<passivedouble> CDriver::GetInitialMeshCoord(unsigned short iMarker, unsigned long iVertex) const {
+
+  vector<su2double> coord(3,0.0);
+  vector<passivedouble> coord_passive(3, 0.0);
+
+  auto iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+  for (auto iDim = 0 ; iDim < nDim ; iDim++){
+   coord[iDim] = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord(iPoint,iDim);
+  }
+
+  coord_passive[0] = SU2_TYPE::GetValue(coord[0]);
+  coord_passive[1] = SU2_TYPE::GetValue(coord[1]);
+  coord_passive[2] = SU2_TYPE::GetValue(coord[2]);
+
+  return coord_passive;
+}
+
+vector<passivedouble> CDriver::GetVertexNormal(unsigned short iMarker, unsigned long iVertex, bool unitNormal) const {
+
+  su2double *Normal;
+  su2double Area;
+  vector<su2double> ret_Normal(3, 0.0);
+  vector<passivedouble> ret_Normal_passive(3, 0.0);
+
+  Normal = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNormal();
+
+  if (!unitNormal) {
+
+    ret_Normal_passive[0] = SU2_TYPE::GetValue(Normal[0]);
+    ret_Normal_passive[1] = SU2_TYPE::GetValue(Normal[1]);
+    if(nDim>2) ret_Normal_passive[2] = SU2_TYPE::GetValue(Normal[2]);
+
+    return ret_Normal_passive;
+  }
+
+  Area = GeometryToolbox::Norm(nDim, Normal);
+
+  ret_Normal[0] = Normal[0]/Area;
+  ret_Normal[1] = Normal[1]/Area;
+  if(nDim>2) ret_Normal[2] = Normal[2]/Area;
+
+  ret_Normal_passive[0] = SU2_TYPE::GetValue(ret_Normal[0]);
+  ret_Normal_passive[1] = SU2_TYPE::GetValue(ret_Normal[1]);
+  ret_Normal_passive[2] = SU2_TYPE::GetValue(ret_Normal[2]);
+
+  return ret_Normal_passive;
+}
+
 //////////////////////////////////////////////////////////////////////////////////
-/* Functions to obtain global parameters from SU2 (time steps, delta t, etc.)   */
+/* Functions to obtain global parameters from SU2 (time steps, delta t, ecc...) */
 //////////////////////////////////////////////////////////////////////////////////
 
-unsigned long CDriver::GetnTimeIter() const { return config_container[ZONE_0]->GetnTime_Iter(); }
+unsigned long CDriver::GetnTimeIter() const {
+
+  return config_container[ZONE_0]->GetnTime_Iter();
+}
 
-unsigned long CDriver::GetTime_Iter() const { return TimeIter; }
+unsigned long CDriver::GetTime_Iter() const{
+
+  return TimeIter;
+}
 
 passivedouble CDriver::GetUnsteady_TimeStep() const {
+
   return SU2_TYPE::GetValue(config_container[ZONE_0]->GetTime_Step());
 }
 
-string CDriver::GetSurfaceFileName() const { return config_container[ZONE_0]->GetSurfCoeff_FileName(); }
+string CDriver::GetSurfaceFileName() const {
+
+  return config_container[ZONE_0]->GetSurfCoeff_FileName();
+}
 
 ///////////////////////////////////////////////////////////////////////////////
 /* Functions related to CHT solver                                           */
 ///////////////////////////////////////////////////////////////////////////////
 
 passivedouble CDriver::GetVertexTemperature(unsigned short iMarker, unsigned long iVertex) const {
+
   unsigned long iPoint;
   su2double vertexWallTemp(0.0);
 
@@ -184,40 +296,43 @@ passivedouble CDriver::GetVertexTemperature(unsigned short iMarker, unsigned lon
 
   iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
 
-  if (geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint) && compressible) {
+  if(geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint) && compressible){
     vertexWallTemp = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetTemperature(iPoint);
   }
 
   return SU2_TYPE::GetValue(vertexWallTemp);
+
 }
 
-void CDriver::SetVertexTemperature(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallTemp) {
+void CDriver::SetVertexTemperature(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallTemp){
+
   geometry_container[ZONE_0][INST_0][MESH_0]->SetCustomBoundaryTemperature(iMarker, iVertex, val_WallTemp);
 }
 
 vector<passivedouble> CDriver::GetVertexHeatFluxes(unsigned short iMarker, unsigned long iVertex) const {
+
   unsigned long iPoint;
   unsigned short iDim;
-  su2double Prandtl_Lam = config_container[ZONE_0]->GetPrandtl_Lam();
+  su2double Prandtl_Lam  = config_container[ZONE_0]->GetPrandtl_Lam();
   su2double Gas_Constant = config_container[ZONE_0]->GetGas_ConstantND();
   su2double Gamma = config_container[ZONE_0]->GetGamma();
   su2double Gamma_Minus_One = Gamma - 1.0;
   su2double Cp = (Gamma / Gamma_Minus_One) * Gas_Constant;
   su2double laminar_viscosity, thermal_conductivity;
-  vector<su2double> GradT(3, 0.0);
-  vector<su2double> HeatFlux(3, 0.0);
-  vector<passivedouble> HeatFluxPassive(3, 0.0);
+  vector<su2double> GradT (3,0.0);
+  vector<su2double> HeatFlux (3,0.0);
+  vector<passivedouble> HeatFluxPassive (3,0.0);
 
   bool compressible = (config_container[ZONE_0]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
 
   iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
 
-  if (compressible) {
-    laminar_viscosity = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
-    thermal_conductivity = Cp * (laminar_viscosity / Prandtl_Lam);
-    for (iDim = 0; iDim < nDim; iDim++) {
+  if(compressible){
+    laminar_viscosity    = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
+    thermal_conductivity = Cp * (laminar_viscosity/Prandtl_Lam);
+    for(iDim=0; iDim < nDim; iDim++){
       GradT[iDim] = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetGradient_Primitive(iPoint, 0, iDim);
-      HeatFlux[iDim] = -thermal_conductivity * GradT[iDim];
+      HeatFlux[iDim] = -thermal_conductivity*GradT[iDim];
     }
   }
 
@@ -228,18 +343,19 @@ vector<passivedouble> CDriver::GetVertexHeatFluxes(unsigned short iMarker, unsig
   return HeatFluxPassive;
 }
 
-passivedouble CDriver::GetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex) const {
+passivedouble CDriver::GetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex) const{
+
   unsigned long iPoint;
   unsigned short iDim;
   su2double vertexWallHeatFlux;
-  su2double Prandtl_Lam = config_container[ZONE_0]->GetPrandtl_Lam();
+  su2double Prandtl_Lam  = config_container[ZONE_0]->GetPrandtl_Lam();
   su2double Gas_Constant = config_container[ZONE_0]->GetGas_ConstantND();
   su2double Gamma = config_container[ZONE_0]->GetGamma();
   su2double Gamma_Minus_One = Gamma - 1.0;
   su2double Cp = (Gamma / Gamma_Minus_One) * Gas_Constant;
   su2double Area;
   su2double laminar_viscosity, thermal_conductivity, dTdn;
-  su2double *Normal, GradT[3] = {0.0, 0.0, 0.0}, UnitNormal[3] = {0.0, 0.0, 0.0};
+  su2double *Normal, GradT[3] = {0.0,0.0,0.0}, UnitNormal[3] = {0.0,0.0,0.0};
 
   bool compressible = (config_container[ZONE_0]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
 
@@ -248,34 +364,37 @@ passivedouble CDriver::GetVertexNormalHeatFlux(unsigned short iMarker, unsigned
 
   iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
 
-  if (geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint) && compressible) {
+  if(geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint) && compressible){
     Normal = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNormal();
 
     Area = GeometryToolbox::Norm(nDim, Normal);
 
-    for (iDim = 0; iDim < nDim; iDim++) UnitNormal[iDim] = Normal[iDim] / Area;
+    for (iDim = 0; iDim < nDim; iDim++)
+      UnitNormal[iDim] = Normal[iDim]/Area;
 
-    laminar_viscosity = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
-    thermal_conductivity = Cp * (laminar_viscosity / Prandtl_Lam);
+    laminar_viscosity    = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
+    thermal_conductivity = Cp * (laminar_viscosity/Prandtl_Lam);
     /*Compute wall heat flux (normal to the wall) based on computed temperature gradient*/
-    for (iDim = 0; iDim < nDim; iDim++) {
+    for(iDim=0; iDim < nDim; iDim++){
       GradT[iDim] = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetGradient_Primitive(iPoint, 0, iDim);
-      dTdn += GradT[iDim] * UnitNormal[iDim];
+      dTdn += GradT[iDim]*UnitNormal[iDim];
     }
 
-    vertexWallHeatFlux = -thermal_conductivity * dTdn;
+    vertexWallHeatFlux = -thermal_conductivity*dTdn;
   }
 
   return SU2_TYPE::GetValue(vertexWallHeatFlux);
 }
 
-void CDriver::SetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallHeatFlux) {
+void CDriver::SetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallHeatFlux){
+
   geometry_container[ZONE_0][INST_0][MESH_0]->SetCustomBoundaryHeatFlux(iMarker, iVertex, val_WallHeatFlux);
 }
 
 passivedouble CDriver::GetThermalConductivity(unsigned short iMarker, unsigned long iVertex) const {
+
   unsigned long iPoint;
-  su2double Prandtl_Lam = config_container[ZONE_0]->GetPrandtl_Lam();
+  su2double Prandtl_Lam  = config_container[ZONE_0]->GetPrandtl_Lam();
   su2double Gas_Constant = config_container[ZONE_0]->GetGas_ConstantND();
   su2double Gamma = config_container[ZONE_0]->GetGamma();
   su2double Gamma_Minus_One = Gamma - 1.0;
@@ -283,124 +402,218 @@ passivedouble CDriver::GetThermalConductivity(unsigned short iMarker, unsigned l
   su2double laminar_viscosity, thermal_conductivity;
 
   iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  laminar_viscosity = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
-  thermal_conductivity = Cp * (laminar_viscosity / Prandtl_Lam);
+  laminar_viscosity    = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
+  thermal_conductivity = Cp * (laminar_viscosity/Prandtl_Lam);
 
   return SU2_TYPE::GetValue(thermal_conductivity);
+
 }
 
 ////////////////////////////////////////////////////////////////////////////////
 /* Functions related to the management of markers                             */
 ////////////////////////////////////////////////////////////////////////////////
 
-vector<string> CDriver::GetCHTMarkerTags() const {
-  vector<string> tags;
-  const auto nMarker = config_container[ZONE_0]->GetnMarker_All();
+vector<string> CDriver::GetAllBoundaryMarkersTag() const {
+
+  vector<string> boundariesTagList;
+  unsigned short iMarker,nBoundariesMarkers;
+  string Marker_Tag;
+
+  nBoundariesMarkers = config_container[ZONE_0]->GetnMarker_All();
+  boundariesTagList.resize(nBoundariesMarkers);
+
+  for(iMarker=0; iMarker < nBoundariesMarkers; iMarker++){
+    Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
+    boundariesTagList[iMarker] = Marker_Tag;
+  }
+
+  return boundariesTagList;
+}
+
+vector<string> CDriver::GetAllDeformMeshMarkersTag() const {
+
+  vector<string> interfaceBoundariesTagList;
+  unsigned short iMarker, nBoundariesMarker;
+  string Marker_Tag;
 
-  // The CHT markers can be identified as the markers that are customizable with a BC type HEAT_FLUX or ISOTHERMAL.
-  for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
-    if ((config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == HEAT_FLUX ||
-         config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == ISOTHERMAL) &&
-        config_container[ZONE_0]->GetMarker_All_PyCustom(iMarker)) {
-      tags.push_back(config_container[ZONE_0]->GetMarker_All_TagBound(iMarker));
+  nBoundariesMarker = config_container[ZONE_0]->GetnMarker_Deform_Mesh();
+  interfaceBoundariesTagList.resize(nBoundariesMarker);
+
+  for(iMarker=0; iMarker < nBoundariesMarker; iMarker++){
+    Marker_Tag = config_container[ZONE_0]->GetMarker_Deform_Mesh_TagBound(iMarker);
+    interfaceBoundariesTagList[iMarker] = Marker_Tag;
+  }
+
+  return interfaceBoundariesTagList;
+}
+
+vector<string> CDriver::GetAllCHTMarkersTag() const {
+
+  vector<string> CHTBoundariesTagList;
+  unsigned short iMarker, nBoundariesMarker;
+  string Marker_Tag;
+
+  nBoundariesMarker = config_container[ZONE_0]->GetnMarker_All();
+
+  //The CHT markers can be identified as the markers that are customizable with a BC type HEAT_FLUX or ISOTHERMAL.
+  for(iMarker=0; iMarker<nBoundariesMarker; iMarker++){
+    if((config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == HEAT_FLUX || config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == ISOTHERMAL) && config_container[ZONE_0]->GetMarker_All_PyCustom(iMarker)){
+      Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
+      CHTBoundariesTagList.push_back(Marker_Tag);
     }
   }
 
-  return tags;
+  return CHTBoundariesTagList;
 }
 
-vector<string> CDriver::GetInletMarkerTags() const {
-  vector<string> tags;
-  const auto nMarker = config_container[ZONE_0]->GetnMarker_All();
+vector<string> CDriver::GetAllInletMarkersTag() const {
+
+  vector<string> BoundariesTagList;
+  unsigned short iMarker, nBoundariesMarker;
+  string Marker_Tag;
 
-  for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
+  nBoundariesMarker = config_container[ZONE_0]->GetnMarker_All();
+
+  for(iMarker=0; iMarker<nBoundariesMarker; iMarker++){
     bool isCustomizable = config_container[ZONE_0]->GetMarker_All_PyCustom(iMarker);
     bool isInlet = (config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == INLET_FLOW);
+    if(isCustomizable && isInlet) {
+      Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
+      BoundariesTagList.push_back(Marker_Tag);
+    }
+  }
+
+  return BoundariesTagList;
+}
+
+map<string, int> CDriver::GetAllBoundaryMarkers() const {
+
+  map<string, int>  allBoundariesMap;
+  unsigned short iMarker, nBoundaryMarkers;
+  string Marker_Tag;
+
+  nBoundaryMarkers = config_container[ZONE_0]->GetnMarker_All();
+
+  for(iMarker=0; iMarker < nBoundaryMarkers; iMarker++){
+    Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
+    allBoundariesMap[Marker_Tag] = iMarker;
+  }
+
+  return allBoundariesMap;
+}
+
+map<string, string> CDriver::GetAllBoundaryMarkersType() const {
 
-    if (isCustomizable && isInlet) {
-      tags.push_back(config_container[ZONE_0]->GetMarker_All_TagBound(iMarker));
+  map<string, string> allBoundariesTypeMap;
+  unsigned short iMarker, KindBC;
+  string Marker_Tag, Marker_Type;
+
+  for(iMarker=0; iMarker < config_container[ZONE_0]->GetnMarker_All(); iMarker++){
+    Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
+    KindBC = config_container[ZONE_0]->GetMarker_All_KindBC(iMarker);
+    switch(KindBC){
+      case EULER_WALL:
+        Marker_Type = "EULER_WALL";
+        break;
+      case FAR_FIELD:
+        Marker_Type = "FARFIELD";
+        break;
+      case ISOTHERMAL:
+        Marker_Type = "ISOTHERMAL";
+        break;
+      case HEAT_FLUX:
+        Marker_Type = "HEATFLUX";
+        break;
+      case INLET_FLOW:
+        Marker_Type = "INLET_FLOW";
+        break;
+      case OUTLET_FLOW:
+        Marker_Type = "OUTLET_FLOW";
+        break;
+      case SYMMETRY_PLANE:
+        Marker_Type = "SYMMETRY";
+        break;
+      case SEND_RECEIVE:
+        Marker_Type = "SEND_RECEIVE";
+        break;
+      default:
+        Marker_Type = "UNKNOWN_TYPE";
     }
+    allBoundariesTypeMap[Marker_Tag] = Marker_Type;
   }
 
-  return tags;
+  return allBoundariesTypeMap;
 }
 
-void CDriver::SetHeatSource_Position(passivedouble alpha, passivedouble pos_x, passivedouble pos_y,
-                                     passivedouble pos_z) {
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][RAD_SOL];
+void CDriver::SetHeatSource_Position(passivedouble alpha, passivedouble pos_x, passivedouble pos_y, passivedouble pos_z){
+
+  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][RAD_SOL];
 
   config_container[ZONE_0]->SetHeatSource_Rot_Z(alpha);
   config_container[ZONE_0]->SetHeatSource_Center(pos_x, pos_y, pos_z);
 
   solver->SetVolumetricHeatSource(geometry_container[ZONE_0][INST_0][MESH_0], config_container[ZONE_0]);
+
 }
 
-void CDriver::SetInlet_Angle(unsigned short iMarker, passivedouble alpha) {
-  su2double alpha_rad = alpha * PI_NUMBER / 180.0;
+void CDriver::SetInlet_Angle(unsigned short iMarker, passivedouble alpha){
+
+  su2double alpha_rad = alpha * PI_NUMBER/180.0;
 
   unsigned long iVertex;
 
-  for (iVertex = 0; iVertex < geometry_container[ZONE_0][INST_0][MESH_0]->nVertex[iMarker]; iVertex++) {
+  for (iVertex = 0; iVertex < geometry_container[ZONE_0][INST_0][MESH_0]->nVertex[iMarker]; iVertex++){
     solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->SetInlet_FlowDir(iMarker, iVertex, 0, cos(alpha_rad));
     solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->SetInlet_FlowDir(iMarker, iVertex, 1, sin(alpha_rad));
   }
+
 }
 
 /////////////////////////////////////////////////////////////////////////////////////////////////////////////////
-/* Functions related to simulation control, high level functions (reset convergence, set initial mesh, etc.)   */
+/* Functions related to simulation control, high level functions (reset convergence, set initial mesh, ecc...) */
 /////////////////////////////////////////////////////////////////////////////////////////////////////////////////
 
 void CDriver::ResetConvergence() {
-  for (auto iZone = 0u; iZone < nZone; iZone++) {
-    switch (main_config->GetKind_Solver()) {
-      case MAIN_SOLVER::EULER:
-      case MAIN_SOLVER::NAVIER_STOKES:
-      case MAIN_SOLVER::RANS:
-      case MAIN_SOLVER::INC_EULER:
-      case MAIN_SOLVER::INC_NAVIER_STOKES:
-      case MAIN_SOLVER::INC_RANS:
-      case MAIN_SOLVER::NEMO_EULER:
-      case MAIN_SOLVER::NEMO_NAVIER_STOKES:
-        integration_container[iZone][INST_0][FLOW_SOL]->SetConvergence(false);
-        if (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::RANS)
-          integration_container[iZone][INST_0][TURB_SOL]->SetConvergence(false);
-        if (config_container[iZone]->GetKind_Trans_Model() == TURB_TRANS_MODEL::LM)
-          integration_container[iZone][INST_0][TRANS_SOL]->SetConvergence(false);
-        break;
-
-      case MAIN_SOLVER::FEM_ELASTICITY:
-        integration_container[iZone][INST_0][FEA_SOL]->SetConvergence(false);
-        break;
-
-      case MAIN_SOLVER::ADJ_EULER:
-      case MAIN_SOLVER::ADJ_NAVIER_STOKES:
-      case MAIN_SOLVER::ADJ_RANS:
-      case MAIN_SOLVER::DISC_ADJ_EULER:
-      case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES:
-      case MAIN_SOLVER::DISC_ADJ_RANS:
-      case MAIN_SOLVER::DISC_ADJ_INC_EULER:
-      case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES:
-      case MAIN_SOLVER::DISC_ADJ_INC_RANS:
-        integration_container[iZone][INST_0][ADJFLOW_SOL]->SetConvergence(false);
-        if ((config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::ADJ_RANS) ||
-            (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_RANS))
-          integration_container[iZone][INST_0][ADJTURB_SOL]->SetConvergence(false);
-        break;
 
-      default:
-        break;
+  for(iZone = 0; iZone < nZone; iZone++) {
+    switch (config_container[iZone]->GetKind_Solver()) {
+
+    case MAIN_SOLVER::EULER: case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::RANS:
+    case MAIN_SOLVER::INC_EULER: case MAIN_SOLVER::INC_NAVIER_STOKES: case MAIN_SOLVER::INC_RANS:
+      integration_container[iZone][INST_0][FLOW_SOL]->SetConvergence(false);
+      if (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::RANS) integration_container[iZone][INST_0][TURB_SOL]->SetConvergence(false);
+      if(config_container[iZone]->GetKind_Trans_Model() == TURB_TRANS_MODEL::LM) integration_container[iZone][INST_0][TRANS_SOL]->SetConvergence(false);
+      break;
+
+    case MAIN_SOLVER::FEM_ELASTICITY:
+      integration_container[iZone][INST_0][FEA_SOL]->SetConvergence(false);
+      break;
+
+    case MAIN_SOLVER::ADJ_EULER: case MAIN_SOLVER::ADJ_NAVIER_STOKES: case MAIN_SOLVER::ADJ_RANS: case MAIN_SOLVER::DISC_ADJ_EULER: case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_RANS:
+    case MAIN_SOLVER::DISC_ADJ_INC_EULER: case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_INC_RANS:
+      integration_container[iZone][INST_0][ADJFLOW_SOL]->SetConvergence(false);
+      if( (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::ADJ_RANS) || (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_RANS) )
+        integration_container[iZone][INST_0][ADJTURB_SOL]->SetConvergence(false);
+      break;
+
+    default:
+      break;
     }
   }
+
 }
 
 void CSinglezoneDriver::SetInitialMesh() {
+
   DynamicMeshUpdate(0);
 
   SU2_OMP_PARALLEL {
-    for (iMesh = 0u; iMesh <= main_config->GetnMGLevels(); iMesh++) {
-      SU2_OMP_FOR_STAT(roundUpDiv(geometry_container[ZONE_0][INST_0][iMesh]->GetnPoint(), omp_get_max_threads()))
-      for (auto iPoint = 0ul; iPoint < geometry_container[ZONE_0][INST_0][iMesh]->GetnPoint(); iPoint++) {
-        /*--- Overwrite fictitious velocities. ---*/
+    // Overwrite fictious velocities
+    for (iMesh = 0u; iMesh <= config_container[ZONE_0]->GetnMGLevels(); iMesh++) {
+      SU2_OMP_FOR_STAT(roundUpDiv(geometry_container[ZONE_0][INST_0][iMesh]->GetnPoint(),omp_get_max_threads()))
+      for (unsigned long iPoint = 0; iPoint < geometry_container[ZONE_0][INST_0][iMesh]->GetnPoint(); iPoint++) {
+
+        /*--- Overwrite fictitious velocities ---*/
         su2double Grid_Vel[3] = {0.0, 0.0, 0.0};
 
         /*--- Set the grid velocity for this coarse node. ---*/
@@ -411,21 +624,23 @@ void CSinglezoneDriver::SetInitialMesh() {
       geometry_container[ZONE_0][INST_0][iMesh]->nodes->SetVolume_n();
       geometry_container[ZONE_0][INST_0][iMesh]->nodes->SetVolume_nM1();
     }
-    /*--- Push back the solution so that there is no fictitious velocity at the next step. ---*/
+    /*--- Push back the solution so that there is no fictious velocity at the next step. ---*/
     solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->Set_Solution_time_n();
     solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->Set_Solution_time_n1();
   }
   END_SU2_OMP_PARALLEL
 }
 
-void CDriver::BoundaryConditionsUpdate() {
+void CDriver::BoundaryConditionsUpdate(){
+
   int rank = MASTER_NODE;
+  unsigned short iZone;
 
   SU2_MPI::Comm_rank(SU2_MPI::GetComm(), &rank);
 
-  if (rank == MASTER_NODE) cout << "Updating boundary conditions." << endl;
-  for (auto iZone = 0u; iZone < nZone; iZone++) {
-    geometry_container[iZone][INST_0][MESH_0]->UpdateCustomBoundaryConditions(geometry_container[iZone][INST_0],config_container[iZone]);
+  if(rank == MASTER_NODE) cout << "Updating boundary conditions." << endl;
+  for(iZone = 0; iZone < nZone; iZone++){
+    geometry_container[iZone][INST_0][MESH_0]->UpdateCustomBoundaryConditions(geometry_container[iZone][INST_0], config_container[iZone]);
   }
 }
 
@@ -433,26 +648,29 @@ void CDriver::BoundaryConditionsUpdate() {
 /* Functions related to finite elements                                       */
 ////////////////////////////////////////////////////////////////////////////////
 
-void CDriver::SetFEA_Loads(unsigned short iMarker, unsigned long iVertex, passivedouble LoadX, passivedouble LoadY,
-                           passivedouble LoadZ) {
+void CDriver::SetFEA_Loads(unsigned short iMarker, unsigned long iVertex, passivedouble LoadX,
+                       passivedouble LoadY, passivedouble LoadZ) {
+
   unsigned long iPoint;
-  su2double NodalForce[3] = {0.0, 0.0, 0.0};
+  su2double NodalForce[3] = {0.0,0.0,0.0};
   NodalForce[0] = LoadX;
   NodalForce[1] = LoadY;
   NodalForce[2] = LoadZ;
 
   iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL]->GetNodes()->Set_FlowTraction(iPoint, NodalForce);
+  solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL]->GetNodes()->Set_FlowTraction(iPoint,NodalForce);
+
 }
 
 vector<passivedouble> CDriver::GetFEA_Displacements(unsigned short iMarker, unsigned long iVertex) const {
+
   unsigned long iPoint;
   vector<su2double> Displacements(3, 0.0);
   vector<passivedouble> Displacements_passive(3, 0.0);
 
   iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
-  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
+  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 
   Displacements[0] = solver->GetNodes()->GetSolution(iPoint, 0);
   Displacements[1] = solver->GetNodes()->GetSolution(iPoint, 1);
@@ -468,16 +686,18 @@ vector<passivedouble> CDriver::GetFEA_Displacements(unsigned short iMarker, unsi
   return Displacements_passive;
 }
 
+
 vector<passivedouble> CDriver::GetFEA_Velocity(unsigned short iMarker, unsigned long iVertex) const {
+
   unsigned long iPoint;
   vector<su2double> Velocity(3, 0.0);
-  vector<passivedouble> Velocity_passive(3, 0.0);
+  vector<passivedouble> Velocity_passive(3,0.0);
 
   iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
-  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
+  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 
-  if (config_container[ZONE_0]->GetDynamic_Analysis() == DYNAMIC) {
+  if (config_container[ZONE_0]->GetDynamic_Analysis() == DYNAMIC){
     Velocity[0] = solver->GetNodes()->GetSolution_Vel(iPoint, 0);
     Velocity[1] = solver->GetNodes()->GetSolution_Vel(iPoint, 1);
     if (geometry->GetnDim() == 3)
@@ -494,15 +714,16 @@ vector<passivedouble> CDriver::GetFEA_Velocity(unsigned short iMarker, unsigned
 }
 
 vector<passivedouble> CDriver::GetFEA_Velocity_n(unsigned short iMarker, unsigned long iVertex) const {
+
   unsigned long iPoint;
   vector<su2double> Velocity_n(3, 0.0);
   vector<passivedouble> Velocity_n_passive(3, 0.0);
 
   iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
-  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
+  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 
-  if (config_container[ZONE_0]->GetDynamic_Analysis() == DYNAMIC) {
+  if (config_container[ZONE_0]->GetDynamic_Analysis() == DYNAMIC){
     Velocity_n[0] = solver->GetNodes()->GetSolution_Vel_time_n(iPoint, 0);
     Velocity_n[1] = solver->GetNodes()->GetSolution_Vel_time_n(iPoint, 1);
     if (geometry->GetnDim() == 3)
@@ -516,6 +737,7 @@ vector<passivedouble> CDriver::GetFEA_Velocity_n(unsigned short iMarker, unsigne
   Velocity_n_passive[2] = SU2_TYPE::GetValue(Velocity_n[2]);
 
   return Velocity_n_passive;
+
 }
 
 ////////////////////////////////////////////////////////////////////////////////
@@ -523,13 +745,14 @@ vector<passivedouble> CDriver::GetFEA_Velocity_n(unsigned short iMarker, unsigne
 ////////////////////////////////////////////////////////////////////////////////
 
 vector<passivedouble> CDriver::GetMeshDisp_Sensitivity(unsigned short iMarker, unsigned long iVertex) const {
+
   unsigned long iPoint;
   vector<su2double> Disp_Sens(3, 0.0);
   vector<passivedouble> Disp_Sens_passive(3, 0.0);
 
   iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][ADJMESH_SOL];
-  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+  CSolver *solver =  solver_container[ZONE_0][INST_0][MESH_0][ADJMESH_SOL];
+  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 
   Disp_Sens[0] = solver->GetNodes()->GetBoundDisp_Sens(iPoint, 0);
   Disp_Sens[1] = solver->GetNodes()->GetBoundDisp_Sens(iPoint, 1);
@@ -543,16 +766,18 @@ vector<passivedouble> CDriver::GetMeshDisp_Sensitivity(unsigned short iMarker, u
   Disp_Sens_passive[2] = SU2_TYPE::GetValue(Disp_Sens[2]);
 
   return Disp_Sens_passive;
+
 }
 
 vector<passivedouble> CDriver::GetFlowLoad_Sensitivity(unsigned short iMarker, unsigned long iVertex) const {
+
   unsigned long iPoint;
   vector<su2double> FlowLoad_Sens(3, 0.0);
   vector<passivedouble> FlowLoad_Sens_passive(3, 0.0);
 
   iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
-  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
+  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 
   FlowLoad_Sens[0] = solver->GetNodes()->GetFlowTractionSensitivity(iPoint, 0);
   FlowLoad_Sens[1] = solver->GetNodes()->GetFlowTractionSensitivity(iPoint, 1);
@@ -566,52 +791,91 @@ vector<passivedouble> CDriver::GetFlowLoad_Sensitivity(unsigned short iMarker, u
   FlowLoad_Sens_passive[2] = SU2_TYPE::GetValue(FlowLoad_Sens[2]);
 
   return FlowLoad_Sens_passive;
+
 }
 
 void CDriver::SetFlowLoad_Adjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
                                   passivedouble val_AdjointY, passivedouble val_AdjointZ) {
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL];
-  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+
+  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL];
+  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 
   solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 0, val_AdjointX);
   solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 1, val_AdjointY);
-  if (geometry->GetnDim() == 3) solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 2, val_AdjointZ);
+  if (geometry->GetnDim() == 3)
+    solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 2, val_AdjointZ);
+
 }
 
 void CDriver::SetSourceTerm_DispAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
                                         passivedouble val_AdjointY, passivedouble val_AdjointZ) {
+
   unsigned long iPoint;
 
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
-  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
+  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
   iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
 
   solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 0, val_AdjointX);
   solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 1, val_AdjointY);
-  if (geometry->GetnDim() == 3) solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 2, val_AdjointZ);
+  if (geometry->GetnDim() == 3)
+    solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 2, val_AdjointZ);
+
 }
 
 void CDriver::SetSourceTerm_VelAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
-                                       passivedouble val_AdjointY, passivedouble val_AdjointZ) {
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
-  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+                                        passivedouble val_AdjointY, passivedouble val_AdjointZ) {
+
+  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
+  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
   const auto iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
 
   solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 0, val_AdjointX);
   solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 1, val_AdjointY);
-  if (geometry->GetnDim() == 3) solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 2, val_AdjointZ);
+  if (geometry->GetnDim() == 3)
+    solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 2, val_AdjointZ);
+
 }
 
 ////////////////////////////////////////////////////////////////////////////////
-/* Functions related to flow loads                                             */
+/* Functions related to mesh deformation */
+////////////////////////////////////////////////////////////////////////////////
+
+void CDriver::SetMeshDisplacement(unsigned short iMarker, unsigned long iVertex, passivedouble DispX, passivedouble DispY, passivedouble DispZ) {
+
+  unsigned long iPoint;
+  su2double MeshDispl[3] =  {0.0,0.0,0.0};
+
+  MeshDispl[0] = DispX;
+  MeshDispl[1] = DispY;
+  MeshDispl[2] = DispZ;
+
+  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
+
+  solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->SetBound_Disp(iPoint,MeshDispl);
+
+}
+
+void CDriver::CommunicateMeshDisplacement(void) {
+
+  solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->InitiateComms(geometry_container[ZONE_0][INST_0][MESH_0],
+                                                                    config_container[ZONE_0], MESH_DISPLACEMENTS);
+  solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->CompleteComms(geometry_container[ZONE_0][INST_0][MESH_0],
+                                                                    config_container[ZONE_0], MESH_DISPLACEMENTS);
+
+}
+
+////////////////////////////////////////////////////////////////////////////////
+/* Functions related to flow loads */
 ////////////////////////////////////////////////////////////////////////////////
 
 vector<passivedouble> CDriver::GetFlowLoad(unsigned short iMarker, unsigned long iVertex) const {
+
   vector<su2double> FlowLoad(3, 0.0);
   vector<passivedouble> FlowLoad_passive(3, 0.0);
 
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL];
-  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL];
+  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 
   if (config_container[ZONE_0]->GetSolid_Wall(iMarker)) {
     FlowLoad[0] = solver->GetVertexTractions(iMarker, iVertex, 0);
@@ -627,4 +891,5 @@ vector<passivedouble> CDriver::GetFlowLoad(unsigned short iMarker, unsigned long
   FlowLoad_passive[2] = SU2_TYPE::GetValue(FlowLoad[2]);
 
   return FlowLoad_passive;
+
 }
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index bed434e6443..ad340c2d7cd 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -2030,6 +2030,7 @@ void CEulerSolver::Source_Residual(CGeometry *geometry, CSolver **solver_contain
   const bool harmonic_balance = (config->GetTime_Marching() == TIME_MARCHING::HARMONIC_BALANCE);
   const bool windgust         = config->GetWind_Gust();
   const bool body_force       = config->GetBody_Force();
+  const bool vorticity_confinement = config->GetVorticityConfinement();
   const bool ideal_gas        = (config->GetKind_FluidModel() == STANDARD_AIR) ||
                                 (config->GetKind_FluidModel() == IDEAL_GAS);
   const bool rans             = (config->GetKind_Turb_Model() != TURB_MODEL::NONE);
@@ -2228,6 +2229,42 @@ void CEulerSolver::Source_Residual(CGeometry *geometry, CSolver **solver_contain
     END_SU2_OMP_FOR
   }
 
+  if (vorticity_confinement) {
+
+    CNumerics* second_numerics = numerics_container[SOURCE_SECOND_TERM + omp_get_thread_num()*MAX_TERMS];
+
+    /*--- calculate and set the average volume ---*/
+    const su2double AvgVolume = config->GetDomainVolume() / geometry->GetGlobal_nPointDomain();
+    second_numerics->SetAvgVolume(AvgVolume);
+
+    /*--- set vorticity magnitude as auxilliary variable ---*/
+    SU2_OMP_FOR_STAT(omp_chunk_size)
+    for (iPoint = 0; iPoint < nPoint; iPoint++) {
+      const su2double VorticityMag = max(GeometryToolbox::Norm(3, nodes->GetVorticity(iPoint)), 1e-12);
+      nodes->SetAuxVar(iPoint, 0, VorticityMag);
+    }
+    END_SU2_OMP_FOR
+
+    /*--- calculate the gradient of the vorticity magnitude (AuxVarGradient) ---*/
+    SetAuxVar_Gradient_GG(geometry, config);
+
+    SU2_OMP_FOR_DYN(omp_chunk_size)
+    for (iPoint = 0; iPoint < nPointDomain; iPoint++) {
+      second_numerics->SetPrimitive(nodes->GetPrimitive(iPoint), nullptr);
+      second_numerics->SetVorticity(nodes->GetVorticity(iPoint), nullptr);
+      second_numerics->SetAuxVarGrad(nodes->GetAuxVarGradient(iPoint), nullptr);
+      second_numerics->SetDistance(geometry->nodes->GetWall_Distance(iPoint), 0);
+      second_numerics->SetVolume(geometry->nodes->GetVolume(iPoint));
+      auto residual = second_numerics->ComputeResidual(config);
+
+      LinSysRes.AddBlock(iPoint, residual);
+
+      if (implicit) Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
+    }
+    END_SU2_OMP_FOR
+
+  }
+
   /*--- Check if a verification solution is to be computed. ---*/
 
   if ( VerificationSolution ) {
diff --git a/SU2_CFD/src/solvers/CHeatSolver.cpp b/SU2_CFD/src/solvers/CHeatSolver.cpp
index 36bb2265b8d..a7a3b1e30d3 100644
--- a/SU2_CFD/src/solvers/CHeatSolver.cpp
+++ b/SU2_CFD/src/solvers/CHeatSolver.cpp
@@ -26,17 +26,21 @@
  */
 
 #include "../../include/solvers/CHeatSolver.hpp"
+#include <cstddef>
 #include "../../../Common/include/toolboxes/geometry_toolbox.hpp"
+#include "../../include/solvers/CScalarSolver.inl"
 
-CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iMesh) : CSolver(),
-             flow(config->GetFluidProblem()), heat_equation(config->GetHeatProblem()) {
+/*--- Explicit instantiation of the parent class of CHeatSolver. ---*/
+template class CScalarSolver<CHeatVariable>;
 
-  /* A grid is defined as dynamic if there's rigid grid movement or grid deformation AND the problem is time domain */
-  dynamic_grid = config->GetDynamic_Grid();
+CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iMesh)
+  : CScalarSolver<CHeatVariable>(geometry, config, false),
+    flow(config->GetFluidProblem()), heat_equation(config->GetHeatProblem()) {
 
   /*--- Dimension of the problem --> temperature is the only conservative variable ---*/
 
   nVar = 1;
+  nPrimVar = 1;
   nPoint = geometry->GetnPoint();
   nPointDomain = geometry->GetnPointDomain();
 
@@ -47,18 +51,6 @@ CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iM
   /*--- Define geometry constants in the solver structure ---*/
 
   nDim = geometry->GetnDim();
-  nMarker = config->GetnMarker_All();
-
-  /*--- Store the number of vertices on each marker for deallocation later ---*/
-
-  nVertex.resize(nMarker);
-  for (auto iMarker = 0u; iMarker < nMarker; iMarker++)
-    nVertex[iMarker] = geometry->nVertex[iMarker];
-
-  /*--- Define some auxiliary vector related with the residual ---*/
-
-  Residual = new su2double[nVar]; for (auto iVar = 0u; iVar < nVar; iVar++) Residual[iVar] = 0.0;
-  Res_Visc = new su2double[nVar]; for (auto iVar = 0u; iVar < nVar; iVar++) Res_Visc[iVar] = 0.0;
 
   /*--- Define some structures for locating max residuals ---*/
 
@@ -67,21 +59,13 @@ CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iM
   Point_Max.resize(nVar,0);
   Point_Max_Coord.resize(nVar,nDim) = su2double(0.0);
 
-  /*--- Jacobians and vector structures for implicit computations ---*/
-
-  Jacobian_i = new su2double* [nVar];
-  Jacobian_j = new su2double* [nVar];
-  for (auto iVar = 0u; iVar < nVar; iVar++) {
-    Jacobian_i[iVar] = new su2double [nVar];
-    Jacobian_j[iVar] = new su2double [nVar];
-  }
-
   /*--- Initialization of the structure of the whole Jacobian ---*/
 
   if (rank == MASTER_NODE) cout << "Initialize Jacobian structure (heat equation) MG level: " << iMesh << "." << endl;
-  Jacobian.Initialize(nPoint, nPointDomain, nVar, nVar, true, geometry, config);
+  Jacobian.Initialize(nPoint, nPointDomain, nVar, nVar, true, geometry, config, ReducerStrategy);
   LinSysSol.Initialize(nPoint, nPointDomain, nVar, 0.0);
   LinSysRes.Initialize(nPoint, nPointDomain, nVar, 0.0);
+  if (ReducerStrategy) EdgeFluxes.Initialize(geometry->GetnEdge(), geometry->GetnEdge(), nVar, nullptr);
 
   if (config->GetExtraOutput()) {
     if (nDim == 2) { nOutputVariables = 13; }
@@ -111,7 +95,8 @@ CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iM
     Temperature_Ref = config->GetInc_Temperature_Ref();
   }
   config->SetTemperature_Ref(Temperature_Ref);
-  config->SetTemperature_FreeStreamND(Temperature_FreeStream/Temperature_Ref);
+  config->SetTemperature_FreeStreamND(Temperature_FreeStream / Temperature_Ref);
+  Solution_Inf[0] = config->GetTemperature_FreeStreamND();
 
   /*--- Set the reference values for heat fluxes. If the heat solver runs stand-alone,
    *    thermal conductivity is read directly from config file ---*/
@@ -133,7 +118,7 @@ CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iM
    used for communications with donor cells ---*/
 
   const unsigned short nConjVariables = 4;
-  AllocVectorOfMatrices(nVertex, nConjVariables, ConjugateVar, config->GetTemperature_FreeStreamND());
+  AllocVectorOfMatrices(nVertex, nConjVariables, ConjugateVar, Solution_Inf[0]);
 
   /*--- Heat flux in all the markers ---*/
 
@@ -149,7 +134,7 @@ CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iM
 
   /*--- Initialize the nodes vector. ---*/
 
-  nodes = new CHeatVariable(config->GetTemperature_FreeStreamND(), nPoint, nDim, nVar, config);
+  nodes = new CHeatVariable(Solution_Inf[0], nPoint, nDim, nVar, config);
 
   SetBaseClassPointerToNodes();
 
@@ -170,64 +155,52 @@ CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iM
   InitiateComms(geometry, config, SOLUTION);
   CompleteComms(geometry, config, SOLUTION);
 
-  /*--- Add the solver name (max 8 characters) ---*/
-
-  SolverName = "HEAT";
-}
-
-CHeatSolver::~CHeatSolver(void) {
-
-  delete nodes;
-}
-
-void CHeatSolver::Preprocessing(CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, unsigned short iRKStep, unsigned short RunTime_EqSystem, bool Output) {
-  SU2_OMP_MASTER
-  config->SetGlobalParam(config->GetKind_Solver(), RunTime_EqSystem);
-  END_SU2_OMP_MASTER
-
-  if (config->GetKind_ConvNumScheme_Heat() == SPACE_CENTERED) {
-    SetUndivided_Laplacian(geometry, config);
-  }
-
-  for (auto iPoint = 0ul; iPoint < nPoint; iPoint ++) {
-
-    /*--- Initialize the residual vector ---*/
+  /*--- Store the initial CFL number for all grid points. ---*/
 
-    LinSysRes.SetBlock_Zero(iPoint);
+  const su2double CFL = config->GetCFL(MGLevel) * config->GetCFLRedCoeff_Turb();
+  SU2_OMP_FOR_STAT(omp_chunk_size)
+  for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
+    nodes->SetLocalCFL(iPoint, CFL);
   }
+  END_SU2_OMP_FOR
+  Min_CFL_Local = CFL;
+  Max_CFL_Local = CFL;
+  Avg_CFL_Local = CFL;
 
-  /*--- Initialize the Jacobian matrices ---*/
+  /*--- Add the solver name (max 8 characters) ---*/
 
-  Jacobian.SetValZero();
+  SolverName = "HEAT";
+}
 
-  if (config->GetReconstructionGradientRequired()) {
-    if (config->GetKind_Gradient_Method_Recon() == GREEN_GAUSS)
-      SetSolution_Gradient_GG(geometry, config, true);
-    if (config->GetKind_Gradient_Method_Recon() == LEAST_SQUARES)
-      SetSolution_Gradient_LS(geometry, config, true);
-    if (config->GetKind_Gradient_Method_Recon() == WEIGHTED_LEAST_SQUARES)
-      SetSolution_Gradient_LS(geometry, config, true);
+void CHeatSolver::Preprocessing(CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh,
+                                unsigned short iRKStep, unsigned short RunTime_EqSystem, bool Output) {
+  SU2_OMP_SAFE_GLOBAL_ACCESS(config->SetGlobalParam(config->GetKind_Solver(), RunTime_EqSystem);)
+  CommonPreprocessing(geometry, config, Output);
+
+  /*--- Need to clear EdgeFluxes and Jacobian when only the viscous part is called for solid heat transfer,
+   * for the weakly coupled energy equation the convection part does this by setting instead of incrementing. ---*/
+  if (!Output && !flow && ReducerStrategy) {
+    EdgeFluxes.SetValZero();
+    if (config->GetKind_TimeIntScheme() == EULER_IMPLICIT) {
+      Jacobian.SetValZero();
+    } else {
+      SU2_OMP_BARRIER
+    }
   }
-  if (config->GetKind_Gradient_Method() == GREEN_GAUSS) SetSolution_Gradient_GG(geometry, config);
-  if (config->GetKind_Gradient_Method() == WEIGHTED_LEAST_SQUARES) SetSolution_Gradient_LS(geometry, config);
 }
 
-void CHeatSolver::Postprocessing(CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh) { }
-
 void CHeatSolver::LoadRestart(CGeometry **geometry, CSolver ***solver, CConfig *config, int val_iter,
                               bool val_update_geo) {
-  /*--- Restart the solution from file information ---*/
-
   const string restart_filename = config->GetFilename(config->GetSolution_FileName(), "", val_iter);
 
+  BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
   /*--- Skip coordinates ---*/
 
   unsigned short skipVars = nDim;
 
   if (flow) {
     // P, vx, vy (,vz)
-    if (nDim == 2) skipVars += 3;
-    if (nDim == 3) skipVars += 4;
+    skipVars += 1 + nDim;
   }
 
   /*--- Read the restart data from either an ASCII or binary SU2 file. ---*/
@@ -265,6 +238,8 @@ void CHeatSolver::LoadRestart(CGeometry **geometry, CSolver ***solver, CConfig *
     SU2_MPI::Error(string("The solution file ") + restart_filename + string(" does not match with the mesh file!\n") +
                    string("This can be caused by empty lines at the end of the file."), CURRENT_FUNCTION);
   }
+  }
+  END_SU2_OMP_SAFE_GLOBAL_ACCESS
 
   /*--- Communicate the loaded solution on the fine grid before we transfer
    it down to the coarse levels. We alo call the preprocessing routine
@@ -289,212 +264,51 @@ void CHeatSolver::LoadRestart(CGeometry **geometry, CSolver ***solver, CConfig *
 
   /*--- Delete the class memory that is used to load the restart. ---*/
 
-  delete[] Restart_Vars;
-  Restart_Vars = nullptr;
-  delete[] Restart_Data;
-  Restart_Data = nullptr;
-}
-
-void CHeatSolver::Centered_Residual(CGeometry *geometry, CSolver **solver_container,  CNumerics **numerics_container,
-                                    CConfig *config, unsigned short iMesh, unsigned short iRKStep) {
-
-  const auto numerics = numerics_container[CONV_TERM];
-
-  if(flow) {
-
-    nVarFlow = solver_container[FLOW_SOL]->GetnVar();
-
-    for (auto iEdge = 0ul; iEdge < geometry->GetnEdge(); iEdge++) {
-
-      /*--- Points in edge ---*/
-      const auto iPoint = geometry->edges->GetNode(iEdge,0);
-      const auto jPoint = geometry->edges->GetNode(iEdge,1);
-      numerics->SetNormal(geometry->edges->GetNormal(iEdge));
-
-      /*--- Primitive variables w/o reconstruction ---*/
-      const auto V_i = solver_container[FLOW_SOL]->GetNodes()->GetPrimitive(iPoint);
-      const auto V_j = solver_container[FLOW_SOL]->GetNodes()->GetPrimitive(jPoint);
-
-      const auto Temp_i = nodes->GetTemperature(iPoint);
-      const auto Temp_j = nodes->GetTemperature(jPoint);
-
-      numerics->SetUndivided_Laplacian(nodes->GetUndivided_Laplacian(iPoint), nodes->GetUndivided_Laplacian(jPoint));
-      numerics->SetNeighbor(geometry->nodes->GetnNeighbor(iPoint), geometry->nodes->GetnNeighbor(jPoint));
-
-      numerics->SetPrimitive(V_i, V_j);
-      numerics->SetTemperature(Temp_i, Temp_j);
-
-      numerics->ComputeResidual(Residual, Jacobian_i, Jacobian_j, config);
-
-      LinSysRes.AddBlock(iPoint, Residual);
-      LinSysRes.SubtractBlock(jPoint, Residual);
-
-      /*--- Implicit part ---*/
-
-      Jacobian.UpdateBlocks(iEdge, iPoint, jPoint, Jacobian_i, Jacobian_j);
-    }
+  BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
+    delete[] Restart_Vars;
+    Restart_Vars = nullptr;
+    delete[] Restart_Data;
+    Restart_Data = nullptr;
   }
+  END_SU2_OMP_SAFE_GLOBAL_ACCESS
 }
 
 void CHeatSolver::Upwind_Residual(CGeometry *geometry, CSolver **solver_container,
                                   CNumerics **numerics_container, CConfig *config, unsigned short iMesh) {
-
-  CNumerics* numerics = numerics_container[CONV_TERM];
-
-  su2double *V_i, *V_j, Temp_i, Temp_i_Corrected, Temp_j, Temp_j_Corrected,
-            Project_Grad_i, Project_Grad_j, Project_Temp_i_Grad, Project_Temp_j_Grad;
-
-  su2double Vector_i[MAXNDIM] = {0};
-  su2double Vector_j[MAXNDIM] = {0};
-
-  if(flow) {
-
-    nVarFlow = solver_container[FLOW_SOL]->GetnVar();
-
-    /*--- Define some auxiliary vectors related to the primitive flow solution ---*/
-    vector<su2double> Primitive_Flow_i(nVarFlow, 0.0);
-    vector<su2double> Primitive_Flow_j(nVarFlow, 0.0);
-
-    for (auto iEdge = 0ul; iEdge < geometry->GetnEdge(); iEdge++) {
-
-      /*--- Points in edge ---*/
-      const auto iPoint = geometry->edges->GetNode(iEdge,0);
-      const auto jPoint = geometry->edges->GetNode(iEdge,1);
-      numerics->SetNormal(geometry->edges->GetNormal(iEdge));
-
-      /*--- Primitive variables w/o reconstruction ---*/
-      V_i = solver_container[FLOW_SOL]->GetNodes()->GetPrimitive(iPoint);
-      V_j = solver_container[FLOW_SOL]->GetNodes()->GetPrimitive(jPoint);
-
-      const auto Temp_i_Grad = nodes->GetGradient(iPoint);
-      const auto Temp_j_Grad = nodes->GetGradient(jPoint);
-      numerics->SetConsVarGradient(Temp_i_Grad, Temp_j_Grad);
-
-      Temp_i = nodes->GetTemperature(iPoint);
-      Temp_j = nodes->GetTemperature(jPoint);
-
-      /* Second order reconstruction */
-      if (config->GetMUSCL_Heat()) {
-
-        for (auto iDim = 0u; iDim < nDim; iDim++) {
-          Vector_i[iDim] = 0.5*(geometry->nodes->GetCoord(jPoint, iDim) - geometry->nodes->GetCoord(iPoint, iDim));
-          Vector_j[iDim] = 0.5*(geometry->nodes->GetCoord(iPoint, iDim) - geometry->nodes->GetCoord(jPoint, iDim));
-        }
-
-        const auto Gradient_i = solver_container[FLOW_SOL]->GetNodes()->GetGradient_Reconstruction(iPoint);
-        const auto Gradient_j = solver_container[FLOW_SOL]->GetNodes()->GetGradient_Reconstruction(jPoint);
-        const auto Temp_i_Grad = nodes->GetGradient_Reconstruction(iPoint);
-        const auto Temp_j_Grad = nodes->GetGradient_Reconstruction(jPoint);
-
-        /*Loop to correct the flow variables*/
-        for (auto iVar = 0u; iVar < nVarFlow; iVar++) {
-
-          /*Apply the Gradient to get the right temperature value on the edge */
-          Project_Grad_i = 0.0; Project_Grad_j = 0.0;
-          for (auto iDim = 0u; iDim < nDim; iDim++) {
-              Project_Grad_i += Vector_i[iDim]*Gradient_i[iVar][iDim];
-              Project_Grad_j += Vector_j[iDim]*Gradient_j[iVar][iDim];
-          }
-
-          Primitive_Flow_i[iVar] = V_i[iVar] + Project_Grad_i;
-          Primitive_Flow_j[iVar] = V_j[iVar] + Project_Grad_j;
-        }
-
-        /* Correct the temperature variables */
-        Project_Temp_i_Grad = 0.0; Project_Temp_j_Grad = 0.0;
-        for (auto iDim = 0u; iDim < nDim; iDim++) {
-            Project_Temp_i_Grad += Vector_i[iDim]*Temp_i_Grad[0][iDim];
-            Project_Temp_j_Grad += Vector_j[iDim]*Temp_j_Grad[0][iDim];
-        }
-
-        Temp_i_Corrected = Temp_i + Project_Temp_i_Grad;
-        Temp_j_Corrected = Temp_j + Project_Temp_j_Grad;
-
-        numerics->SetPrimitive(Primitive_Flow_i.data(), Primitive_Flow_j.data());
-        numerics->SetTemperature(Temp_i_Corrected, Temp_j_Corrected);
-      }
-
-      else {
-
-        numerics->SetPrimitive(V_i, V_j);
-        numerics->SetTemperature(Temp_i, Temp_j);
-      }
-
-      numerics->ComputeResidual(Residual, Jacobian_i, Jacobian_j, config);
-
-      LinSysRes.AddBlock(iPoint, Residual);
-      LinSysRes.SubtractBlock(jPoint, Residual);
-
-      /*--- Implicit part ---*/
-
-      Jacobian.UpdateBlocks(iEdge, iPoint, jPoint, Jacobian_i, Jacobian_j);
-    }
-  }
-
+  /*--- For solid heat transfer there is no convection. ---*/
+  if (!flow) return;
+  CScalarSolver<CHeatVariable>::Upwind_Residual(geometry, solver_container, numerics_container, config, iMesh);
 }
 
 void CHeatSolver::Viscous_Residual(CGeometry *geometry, CSolver **solver_container, CNumerics **numerics_container,
                                    CConfig *config, unsigned short iMesh, unsigned short iRKStep) {
-
-  CNumerics* numerics = numerics_container[VISC_TERM];
-
-  su2double laminar_viscosity, Prandtl_Lam, Prandtl_Turb, eddy_viscosity_i, eddy_viscosity_j,
-            thermal_diffusivity_i, thermal_diffusivity_j, Temp_i, Temp_j;
-
-  const bool turb = ((config->GetKind_Solver() == MAIN_SOLVER::INC_RANS) || (config->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_INC_RANS));
-
-  eddy_viscosity_i = 0.0;
-  eddy_viscosity_j = 0.0;
-  laminar_viscosity = config->GetMu_ConstantND();
-  Prandtl_Lam = config->GetPrandtl_Lam();
-  Prandtl_Turb = config->GetPrandtl_Turb();
-
-  for (auto iEdge = 0ul; iEdge < geometry->GetnEdge(); iEdge++) {
-
-    const auto iPoint = geometry->edges->GetNode(iEdge,0);
-    const auto jPoint = geometry->edges->GetNode(iEdge,1);
-
-    /*--- Points coordinates, and normal vector ---*/
-
-    numerics->SetCoord(geometry->nodes->GetCoord(iPoint),
-                       geometry->nodes->GetCoord(jPoint));
-    numerics->SetNormal(geometry->edges->GetNormal(iEdge));
-
-    const auto Temp_i_Grad = nodes->GetGradient(iPoint);
-    const auto Temp_j_Grad = nodes->GetGradient(jPoint);
-    numerics->SetConsVarGradient(Temp_i_Grad, Temp_j_Grad);
-
-    /*--- Primitive variables w/o reconstruction ---*/
-    Temp_i = nodes->GetTemperature(iPoint);
-    Temp_j = nodes->GetTemperature(jPoint);
-    numerics->SetTemperature(Temp_i, Temp_j);
-
-    /*--- Eddy viscosity to compute thermal conductivity ---*/
-    if (flow) {
-      if (turb) {
-        eddy_viscosity_i = solver_container[TURB_SOL]->GetNodes()->GetmuT(iPoint);
-        eddy_viscosity_j = solver_container[TURB_SOL]->GetNodes()->GetmuT(jPoint);
-      }
-      thermal_diffusivity_i = (laminar_viscosity/Prandtl_Lam) + (eddy_viscosity_i/Prandtl_Turb);
-      thermal_diffusivity_j = (laminar_viscosity/Prandtl_Lam) + (eddy_viscosity_j/Prandtl_Turb);
+  /*--- For fluid problems the viscous residual is included in the convective residual. ---*/
+  if (flow) return;
+  const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+  CNumerics* numerics = numerics_container[VISC_TERM + omp_get_thread_num() * MAX_TERMS];
+
+  bool pausePreacc = false;
+  if (ReducerStrategy)
+    pausePreacc = AD::PausePreaccumulation();
+  else
+    AD::StartNoSharedReading();
+
+  for (auto color : EdgeColoring) {
+    SU2_OMP_FOR_DYN(nextMultiple(OMP_MIN_SIZE, color.groupSize))
+    for (auto k = 0ul; k < color.size; ++k) {
+      auto iEdge = color.indices[k];
+      Viscous_Residual(iEdge, geometry, solver_container, numerics, config);
     }
-    else {
-      thermal_diffusivity_i = config->GetThermalDiffusivity();
-      thermal_diffusivity_j = config->GetThermalDiffusivity();
-    }
-
-    numerics->SetThermalDiffusivity(thermal_diffusivity_i,thermal_diffusivity_j);
-
-    /*--- Compute residual, and Jacobians ---*/
-
-    numerics->ComputeResidual(Residual, Jacobian_i, Jacobian_j, config);
-
-    /*--- Add and subtract residual, and update Jacobians ---*/
+    END_SU2_OMP_FOR
+  }
 
-    LinSysRes.SubtractBlock(iPoint, Residual);
-    LinSysRes.AddBlock(jPoint, Residual);
+  /*--- Restore preaccumulation and adjoint evaluation state. ---*/
+  AD::ResumePreaccumulation(pausePreacc);
+  if (!ReducerStrategy) AD::EndNoSharedReading();
 
-    Jacobian.UpdateBlocksSub(iEdge, iPoint, jPoint, Jacobian_i, Jacobian_j);
+  if (ReducerStrategy) {
+    SumEdgeFluxes(geometry);
+    if (implicit) Jacobian.SetDiagonalAsColumnSum();
   }
 }
 
@@ -553,282 +367,191 @@ void CHeatSolver::Set_Heatflux_Areas(CGeometry *geometry, CConfig *config) {
   delete[] Local_Surface_Areas;
 }
 
-void CHeatSolver::BC_Isothermal_Wall(CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config,
-                                       unsigned short val_marker) {
-
-  unsigned long iPoint, Point_Normal;
-  su2double *Normal, *Coord_i, *Coord_j, Area, dist_ij, Twall, dTdn;
-  const bool implicit = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
-
-  const su2double laminar_viscosity = config->GetMu_ConstantND();
-  const su2double Prandtl_Lam = config->GetPrandtl_Lam();
-  const su2double thermal_diffusivity = flow ? laminar_viscosity/Prandtl_Lam : config->GetThermalDiffusivity();
-
-  //su2double Prandtl_Turb = config->GetPrandtl_Turb();
-  //laminar_viscosity = config->GetViscosity_FreeStreamND(); // TDE check for consistency for CHT
-
-  string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
+void CHeatSolver::BC_Isothermal_Wall(CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics,
+                                     CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
 
-  Twall = config->GetIsothermal_Temperature(Marker_Tag)/config->GetTemperature_Ref();
+  const auto Marker_Tag = config->GetMarker_All_TagBound(val_marker);
+  su2double Twall = config->GetIsothermal_Temperature(Marker_Tag) / config->GetTemperature_Ref();
+  const bool IsPyCustom = config->GetMarker_All_PyCustom(val_marker);
 
+  SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
   for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
-
-    iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
-
-    if (geometry->nodes->GetDomain(iPoint)) {
-
-        Point_Normal = geometry->vertex[val_marker][iVertex]->GetNormal_Neighbor();
-
-        Normal = geometry->vertex[val_marker][iVertex]->GetNormal();
-        Area = GeometryToolbox::Norm(nDim, Normal);
-
-        Coord_i = geometry->nodes->GetCoord(iPoint);
-        Coord_j = geometry->nodes->GetCoord(Point_Normal);
-        dist_ij = 0;
-        for (auto iDim = 0u; iDim < nDim; iDim++)
-          dist_ij += (Coord_j[iDim]-Coord_i[iDim])*(Coord_j[iDim]-Coord_i[iDim]);
-        dist_ij = sqrt(dist_ij);
-
-        dTdn = -(nodes->GetTemperature(Point_Normal) - Twall)/dist_ij;
-
-        Res_Visc[0] = thermal_diffusivity*dTdn*Area;
-
-        if(implicit)
-          Jacobian_i[0][0] = -thermal_diffusivity/dist_ij * Area;
-
-        LinSysRes.SubtractBlock(iPoint, Res_Visc);
-        Jacobian.SubtractBlock2Diag(iPoint, Jacobian_i);
+    if (IsPyCustom) {
+      Twall = geometry->GetCustomBoundaryTemperature(val_marker, iVertex);
     }
+    IsothermalBoundaryCondition(geometry, solver_container[FLOW_SOL], config, val_marker, iVertex, Twall);
   }
+  END_SU2_OMP_FOR
 }
 
 void CHeatSolver::BC_HeatFlux_Wall(CGeometry* geometry, CSolver** solver_container, CNumerics* conv_numerics,
                                    CNumerics* visc_numerics, CConfig* config, unsigned short val_marker) {
   const auto Marker_Tag = config->GetMarker_All_TagBound(val_marker);
+  const bool IsPyCustom = config->GetMarker_All_PyCustom(val_marker);
 
   su2double Wall_HeatFlux = config->GetWall_HeatFlux(Marker_Tag) / config->GetHeat_Flux_Ref();
   if (config->GetIntegrated_HeatFlux()) {
     Wall_HeatFlux /= geometry->GetSurfaceArea(config, val_marker);
   }
 
+  SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
   for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
     const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
+    if (!geometry->nodes->GetDomain(iPoint)) continue;
 
-    if (geometry->nodes->GetDomain(iPoint)) {
-      const auto Normal = geometry->vertex[val_marker][iVertex]->GetNormal();
-      const auto Area = GeometryToolbox::Norm(nDim, Normal);
-
-      Res_Visc[0] = 0.0;
-
-      Res_Visc[0] = Wall_HeatFlux * Area;
-
-      /*--- Viscous contribution to the residual at the wall ---*/
-
-      LinSysRes.SubtractBlock(iPoint, Res_Visc);
+    if (IsPyCustom) {
+      Wall_HeatFlux = geometry->GetCustomBoundaryHeatFlux(val_marker, iVertex);
     }
+    /*--- Viscous contribution to the residual at the wall. ---*/
+    const auto* Normal = geometry->vertex[val_marker][iVertex]->GetNormal();
+    const su2double Area = GeometryToolbox::Norm(nDim, Normal);
+    const su2double flux = Wall_HeatFlux * Area;
+    LinSysRes(iPoint, 0) -= flux;
   }
+  END_SU2_OMP_FOR
 }
 
-void CHeatSolver::BC_Inlet(CGeometry *geometry, CSolver **solver_container,
-                            CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
-
-  unsigned short iDim;
-  unsigned long iVertex, iPoint, Point_Normal;
-  su2double Vel_Mag, *V_inlet, *V_domain;
-
-  bool viscous              = config->GetViscous();
-  bool implicit             = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
-  string Marker_Tag         = config->GetMarker_All_TagBound(val_marker);
-
-  su2double Normal[MAXNDIM];
+void CHeatSolver::BC_Inlet(CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics,
+                           CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
+  if (!flow) return;
 
-  su2double *Coord_i, *Coord_j, Area, dist_ij, laminar_viscosity, thermal_diffusivity, Twall, dTdn, Prandtl_Lam;
-  //su2double Prandtl_Turb;
-  Prandtl_Lam = config->GetPrandtl_Lam();
-//  Prandtl_Turb = config->GetPrandtl_Turb();
-  laminar_viscosity = config->GetMu_ConstantND();
-  //laminar_viscosity = config->GetViscosity_FreeStreamND(); //TDE check for consistency with CHT
+  const bool viscous = config->GetViscous();
+  const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
 
-  Twall = config->GetTemperature_FreeStreamND();
-
-  for (iVertex = 0; iVertex < geometry->nVertex[val_marker]; iVertex++) {
-
-    iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
-
-    if (geometry->nodes->GetDomain(iPoint)) {
-
-      geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
-      for (iDim = 0; iDim < nDim; iDim++) Normal[iDim] = -Normal[iDim];
-
-      if(flow) {
-
-        /*--- Normal vector for this vertex (negate for outward convention) ---*/
-
-        conv_numerics->SetNormal(Normal);
-
-        /*--- Retrieve solution at this boundary node ---*/
-
-        V_domain = solver_container[FLOW_SOL]->GetNodes()->GetPrimitive(iPoint);
-
-        /*--- Retrieve the specified velocity for the inlet. ---*/
-
-        Vel_Mag  = config->GetInlet_Ptotal(Marker_Tag)/config->GetVelocity_Ref();
-        auto Flow_Dir = config->GetInlet_FlowDir(Marker_Tag);
-
-        V_inlet = solver_container[FLOW_SOL]->GetCharacPrimVar(val_marker, iVertex);
-
-        for (iDim = 0; iDim < nDim; iDim++)
-          V_inlet[iDim+1] = Vel_Mag*Flow_Dir[iDim];
+  SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
+  for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
 
-        conv_numerics->SetPrimitive(V_domain, V_inlet);
+    const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
-        if (dynamic_grid)
-          conv_numerics->SetGridVel(geometry->nodes->GetGridVel(iPoint), geometry->nodes->GetGridVel(iPoint));
+    if (!geometry->nodes->GetDomain(iPoint)) continue;
 
-        conv_numerics->SetTemperature(nodes->GetTemperature(iPoint), config->GetInlet_Ttotal(Marker_Tag)/config->GetTemperature_Ref());
+    su2double Normal[MAXNDIM];
+    geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
+    for (auto iDim = 0u; iDim < nDim; iDim++) Normal[iDim] = -Normal[iDim];
 
-        /*--- Compute the residual using an upwind scheme ---*/
+    /*--- Normal vector for this vertex (negate for outward convention) ---*/
 
-        conv_numerics->ComputeResidual(Residual, Jacobian_i, Jacobian_j, config);
+    conv_numerics->SetNormal(Normal);
 
-        /*--- Update residual value ---*/
+    /*--- Retrieve solution at this boundary node ---*/
 
-        LinSysRes.AddBlock(iPoint, Residual);
+    const auto* V_domain = solver_container[FLOW_SOL]->GetNodes()->GetPrimitive(iPoint);
 
-        /*--- Jacobian contribution for implicit integration ---*/
+    /*--- Retrieve the specified velocity for the inlet. ---*/
 
-        if (implicit)
-          Jacobian.AddBlock2Diag(iPoint, Jacobian_i);
-      }
+    const auto* V_inlet = solver_container[FLOW_SOL]->GetCharacPrimVar(val_marker, iVertex);
 
-      /*--- Viscous contribution ---*/
+    conv_numerics->SetPrimitive(V_domain, V_inlet);
 
-      if (viscous) {
+    if (dynamic_grid)
+      conv_numerics->SetGridVel(geometry->nodes->GetGridVel(iPoint), geometry->nodes->GetGridVel(iPoint));
 
-        Point_Normal = geometry->vertex[val_marker][iVertex]->GetNormal_Neighbor();
+    const su2double Temp_i = nodes->GetTemperature(iPoint);
+    const su2double Temp_j = V_inlet[prim_idx.Temperature()];
+    conv_numerics->SetScalarVar(&Temp_i, &Temp_j);
 
-        geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
-        Area = GeometryToolbox::Norm(nDim, Normal);
+    /*--- Compute the residual using an upwind scheme ---*/
 
-        Coord_i = geometry->nodes->GetCoord(iPoint);
-        Coord_j = geometry->nodes->GetCoord(Point_Normal);
-        dist_ij = 0;
-        for (iDim = 0; iDim < nDim; iDim++)
-          dist_ij += (Coord_j[iDim]-Coord_i[iDim])*(Coord_j[iDim]-Coord_i[iDim]);
-        dist_ij = sqrt(dist_ij);
+    auto residual = conv_numerics->ComputeResidual(config);
 
-        dTdn = -(nodes->GetTemperature(Point_Normal) - Twall)/dist_ij;
+    /*--- Update residual value ---*/
 
-        thermal_diffusivity = laminar_viscosity/Prandtl_Lam;
+    LinSysRes.AddBlock(iPoint, residual);
 
-        Res_Visc[0] = thermal_diffusivity*dTdn*Area;
+    /*--- Jacobian contribution for implicit integration ---*/
 
-        if(implicit) {
+    if (implicit) Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
 
-          Jacobian_i[0][0] = -thermal_diffusivity/dist_ij * Area;
-        }
-        /*--- Viscous contribution to the residual at the wall ---*/
+    /*--- Viscous contribution ---*/
 
-        LinSysRes.SubtractBlock(iPoint, Res_Visc);
-        Jacobian.SubtractBlock2Diag(iPoint, Jacobian_i);
-      }
+    if (viscous) {
+      IsothermalBoundaryCondition(geometry, solver_container[FLOW_SOL], config, val_marker, iVertex, Temp_j);
     }
   }
-
+  END_SU2_OMP_FOR
 }
 
 void CHeatSolver::BC_Outlet(CGeometry *geometry, CSolver **solver_container,
                              CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
+  if (!flow) return;
 
-  su2double *V_outlet, *V_domain;
-
-  bool implicit             = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
-
-  su2double Normal[MAXNDIM];
+  const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
 
+  SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
   for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
 
     const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
-    if (geometry->nodes->GetDomain(iPoint)) {
+    if (!geometry->nodes->GetDomain(iPoint)) continue;
 
-      const auto Point_Normal = geometry->vertex[val_marker][iVertex]->GetNormal_Neighbor();
+    const auto Point_Normal = geometry->vertex[val_marker][iVertex]->GetNormal_Neighbor();
 
-      /*--- Normal vector for this vertex (negate for outward convention) ---*/
+    /*--- Normal vector for this vertex (negate for outward convention) ---*/
 
-      geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
-      for (auto iDim = 0u; iDim < nDim; iDim++) Normal[iDim] = -Normal[iDim];
+    su2double Normal[MAXNDIM];
+    geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
+    for (auto iDim = 0u; iDim < nDim; iDim++) Normal[iDim] = -Normal[iDim];
 
-      if(flow) {
-        conv_numerics->SetNormal(Normal);
+    conv_numerics->SetNormal(Normal);
 
-        /*--- Retrieve solution at this boundary node ---*/
+    /*--- Retrieve solution at this boundary node ---*/
 
-        V_domain = solver_container[FLOW_SOL]->GetNodes()->GetPrimitive(iPoint);
+    const auto* V_domain = solver_container[FLOW_SOL]->GetNodes()->GetPrimitive(iPoint);
 
-        /*--- Retrieve the specified velocity for the inlet. ---*/
+    /*--- Retrieve the specified velocity for the inlet. ---*/
 
-        V_outlet = solver_container[FLOW_SOL]->GetCharacPrimVar(val_marker, iVertex);
-        for (auto iDim = 0u; iDim < nDim; iDim++)
-          V_outlet[iDim+1] = solver_container[FLOW_SOL]->GetNodes()->GetVelocity(Point_Normal, iDim);
+    const auto* V_outlet = solver_container[FLOW_SOL]->GetCharacPrimVar(val_marker, iVertex);
 
-        conv_numerics->SetPrimitive(V_domain, V_outlet);
+    conv_numerics->SetPrimitive(V_domain, V_outlet);
 
-        if (dynamic_grid)
-          conv_numerics->SetGridVel(geometry->nodes->GetGridVel(iPoint), geometry->nodes->GetGridVel(iPoint));
+    if (dynamic_grid)
+      conv_numerics->SetGridVel(geometry->nodes->GetGridVel(iPoint), geometry->nodes->GetGridVel(iPoint));
 
-        conv_numerics->SetTemperature(nodes->GetTemperature(iPoint), nodes->GetTemperature(Point_Normal));
+    const su2double Temp_i = nodes->GetTemperature(iPoint);
+    const su2double Temp_j = nodes->GetTemperature(Point_Normal);
+    conv_numerics->SetScalarVar(&Temp_i, &Temp_j);
 
-        /*--- Compute the residual using an upwind scheme ---*/
+    /*--- Compute the residual using an upwind scheme ---*/
 
-        conv_numerics->ComputeResidual(Residual, Jacobian_i, Jacobian_j, config);
+    auto residual = conv_numerics->ComputeResidual(config);
 
-        /*--- Update residual value ---*/
+    /*--- Update residual value ---*/
 
-        LinSysRes.AddBlock(iPoint, Residual);
+    LinSysRes.AddBlock(iPoint, residual);
 
-        /*--- Jacobian contribution for implicit integration ---*/
+    /*--- Jacobian contribution for implicit integration ---*/
 
-        if (implicit)
-          Jacobian.AddBlock2Diag(iPoint, Jacobian_i);
-      }
-    }
+    if (implicit) Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
   }
-
+  END_SU2_OMP_FOR
 }
 
 void CHeatSolver::BC_ConjugateHeat_Interface(CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker) {
 
-  su2double thermal_diffusivity, T_Conjugate, Tinterface, Tnormal_Conjugate, HeatFluxDensity, HeatFlux, Area;
-
-  const bool implicit = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
-
+  const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
   const su2double Temperature_Ref = config->GetTemperature_Ref();
-  const su2double rho_cp_solid = config->GetMaterialDensity(0)*config->GetSpecific_Heat_Cp();
+  const su2double rho_cp_solid = config->GetMaterialDensity(0) * config->GetSpecific_Heat_Cp();
 
   if (flow) {
-
+    SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
     for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
 
       const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
       if (geometry->nodes->GetDomain(iPoint)) {
+        const su2double T_Conjugate = GetConjugateHeatVariable(val_marker, iVertex, 0) / Temperature_Ref;
 
-        const su2double* Normal = geometry->vertex[val_marker][iVertex]->GetNormal();
-        Area = GeometryToolbox::Norm(nDim, Normal);
-
-        T_Conjugate = GetConjugateHeatVariable(val_marker, iVertex, 0)/Temperature_Ref;
-
-        nodes->SetSolution_Old(iPoint,&T_Conjugate);
+        nodes->SetSolution_Old(iPoint, &T_Conjugate);
         LinSysRes(iPoint, 0) = 0.0;
         nodes->SetRes_TruncErrorZero(iPoint);
 
         if (implicit) Jacobian.DeleteValsRowi(iPoint);
       }
     }
+    END_SU2_OMP_FOR
   }
   else if (heat_equation) {
-
+    SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
     for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
 
       const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
@@ -836,49 +559,35 @@ void CHeatSolver::BC_ConjugateHeat_Interface(CGeometry *geometry, CSolver **solv
       if (geometry->nodes->GetDomain(iPoint)) {
 
         su2double const* Normal = geometry->vertex[val_marker][iVertex]->GetNormal();
-        Area = GeometryToolbox::Norm(nDim, Normal);
+        const su2double Area = GeometryToolbox::Norm(nDim, Normal);
 
-        thermal_diffusivity = GetConjugateHeatVariable(val_marker, iVertex, 2)/rho_cp_solid;
+        const su2double thermal_diffusivity = GetConjugateHeatVariable(val_marker, iVertex, 2) / rho_cp_solid;
+        su2double HeatFlux = 0;
 
         if ((config->GetKind_CHT_Coupling() == CHT_COUPLING::DIRECT_TEMPERATURE_ROBIN_HEATFLUX) ||
             (config->GetKind_CHT_Coupling() == CHT_COUPLING::AVERAGED_TEMPERATURE_ROBIN_HEATFLUX)) {
 
-          Tinterface        = nodes->GetTemperature(iPoint);
-          Tnormal_Conjugate = GetConjugateHeatVariable(val_marker, iVertex, 3)/Temperature_Ref;
+          const su2double Tinterface = nodes->GetTemperature(iPoint);
+          const su2double Tnormal_Conjugate = GetConjugateHeatVariable(val_marker, iVertex, 3) / Temperature_Ref;
 
-          HeatFluxDensity   = thermal_diffusivity*(Tinterface - Tnormal_Conjugate);
-          HeatFlux          = HeatFluxDensity * Area;
+          const su2double HeatFluxDensity = thermal_diffusivity * (Tinterface - Tnormal_Conjugate);
+          HeatFlux = HeatFluxDensity * Area;
 
           if (implicit) {
-
-            Jacobian_i[0][0] = -thermal_diffusivity*Area;
-            Jacobian.SubtractBlock2Diag(iPoint, Jacobian_i);
+            su2double Jacobian_i[] = {-thermal_diffusivity*Area};
+            Jacobian.SubtractBlock2Diag(iPoint, &Jacobian_i);
           }
         }
         else {
-
-          HeatFluxDensity = GetConjugateHeatVariable(val_marker, iVertex, 1)/config->GetHeat_Flux_Ref();
-          HeatFlux        = HeatFluxDensity*Area;
+          const su2double HeatFluxDensity =
+              GetConjugateHeatVariable(val_marker, iVertex, 1) / config->GetHeat_Flux_Ref();
+          HeatFlux = HeatFluxDensity*Area;
         }
 
-        Res_Visc[0] = -HeatFlux;
-        LinSysRes.SubtractBlock(iPoint, Res_Visc);
+        LinSysRes(iPoint, 0) += HeatFlux;
       }
     }
-  }
-}
-
-void CHeatSolver::BC_Periodic(CGeometry* geometry, CSolver** solver_container, CNumerics* numerics,
-                                           CConfig* config) {
-  /*--- Complete residuals for periodic boundary conditions. We loop over
-   the periodic BCs in matching pairs so that, in the event that there are
-   adjacent periodic markers, the repeated points will have their residuals
-   accumulated corectly during the communications. For implicit calculations
-   the Jacobians and linear system are also correctly adjusted here. ---*/
-
-  for (unsigned short iPeriodic = 1; iPeriodic <= config->GetnMarker_Periodic() / 2; iPeriodic++) {
-    InitiatePeriodicComms(geometry, config, iPeriodic, PERIODIC_RESIDUAL);
-    CompletePeriodicComms(geometry, config, iPeriodic, PERIODIC_RESIDUAL);
+    END_SU2_OMP_FOR
   }
 }
 
@@ -998,339 +707,215 @@ void CHeatSolver::Heat_Fluxes(CGeometry *geometry, CSolver **solver_container, C
 void CHeatSolver::SetTime_Step(CGeometry *geometry, CSolver **solver_container, CConfig *config,
                                unsigned short iMesh, unsigned long Iteration) {
 
-  unsigned long iPoint, jPoint;
-  su2double Area, Vol, laminar_viscosity, eddy_viscosity, thermal_diffusivity, Prandtl_Lam, Prandtl_Turb, Mean_ProjVel, Mean_BetaInc2, Mean_DensityInc, Mean_SoundSpeed, Lambda;
-  su2double Global_Delta_Time = 0.0, Global_Delta_UnstTimeND = 0.0, Local_Delta_Time = 0.0, Local_Delta_Time_Inv, Local_Delta_Time_Visc, CFL_Reduction, K_v = 0.25;
-  const su2double* Normal;
+  const bool implicit      = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+  const bool time_stepping = (config->GetTime_Marching() == TIME_MARCHING::TIME_STEPPING);
+  const bool dual_time     = (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
+                             (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND);
+  const su2double K_v = 0.25;
 
-  const bool turb = ((config->GetKind_Solver() == MAIN_SOLVER::INC_RANS) || (config->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_INC_RANS));
-  const bool dual_time = ((config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
-                    (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND));
-  const bool implicit = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
-
-  eddy_viscosity    = 0.0;
-  laminar_viscosity = config->GetMu_ConstantND();
-  Prandtl_Lam = config->GetPrandtl_Lam();
-  Prandtl_Turb = config->GetPrandtl_Turb();
+  const su2double prandtl_lam = config->GetPrandtl_Lam();
+  const su2double prandtl_turb = config->GetPrandtl_Turb();
+  const su2double constant_thermal_diffusivity = config->GetThermalDiffusivity();
 
-  thermal_diffusivity = config->GetThermalDiffusivity();
+  const CVariable* flow_nodes = solver_container[FLOW_SOL] ? solver_container[FLOW_SOL]->GetNodes() : nullptr;
 
-  /*--- Compute spectral radius based on thermal conductivity ---*/
+  /*--- Init thread-shared variables to compute min/max values.
+   *    Critical sections are used for this instead of reduction
+   *    clauses for compatibility with OpenMP 2.0 (Windows...). ---*/
+  BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
+    Min_Delta_Time = 1e30;
+    Max_Delta_Time = 0.0;
+    Global_Delta_UnstTimeND = 1e30;
+  } END_SU2_OMP_SAFE_GLOBAL_ACCESS
 
-  Min_Delta_Time = 1.E30; Max_Delta_Time = 0.0;
-  CFL_Reduction = config->GetCFLRedCoeff_Turb();
+  /*--- Loop domain points. ---*/
 
-  for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
-    nodes->SetMax_Lambda_Inv(iPoint,0.0);
-    nodes->SetMax_Lambda_Visc(iPoint,0.0);
-  }
+  SU2_OMP_FOR_DYN(omp_chunk_size)
+  for (auto iPoint = 0ul; iPoint < nPointDomain; ++iPoint) {
 
-  /*--- Loop interior edges ---*/
+    /*--- Set maximum eigenvalues to zero. ---*/
 
-  for (auto iEdge = 0ul; iEdge < geometry->GetnEdge(); iEdge++) {
+    nodes->SetMax_Lambda_Visc(iPoint, 0.0);
 
-    iPoint = geometry->edges->GetNode(iEdge,0);
-    jPoint = geometry->edges->GetNode(iEdge,1);
+    /*--- Loop over the neighbors of point i. ---*/
 
-    /*--- get the edge's normal vector to compute the edge's area ---*/
-    Normal = geometry->edges->GetNormal(iEdge);
-    Area = GeometryToolbox::Norm(nDim, Normal);
+    for (unsigned short iNeigh = 0; iNeigh < geometry->nodes->GetnPoint(iPoint); ++iNeigh) {
+      const auto jPoint = geometry->nodes->GetPoint(iPoint,iNeigh);
+      const auto iEdge = geometry->nodes->GetEdge(iPoint,iNeigh);
+      const auto* Normal = geometry->edges->GetNormal(iEdge);
+      const su2double Area2 = GeometryToolbox::SquaredNorm(nDim, Normal);
 
-    /*--- Inviscid contribution ---*/
-
-    if (flow) {
-      Mean_ProjVel = 0.5 * (solver_container[FLOW_SOL]->GetNodes()->GetProjVel(iPoint,Normal) + solver_container[FLOW_SOL]->GetNodes()->GetProjVel(jPoint,Normal));
-      Mean_BetaInc2 = 0.5 * (solver_container[FLOW_SOL]->GetNodes()->GetBetaInc2(iPoint) + solver_container[FLOW_SOL]->GetNodes()->GetBetaInc2(jPoint));
-      Mean_DensityInc = 0.5 * (solver_container[FLOW_SOL]->GetNodes()->GetDensity(iPoint) + solver_container[FLOW_SOL]->GetNodes()->GetDensity(jPoint));
-      Mean_SoundSpeed = sqrt(Mean_ProjVel*Mean_ProjVel + (Mean_BetaInc2/Mean_DensityInc)*Area*Area);
-
-      Lambda = fabs(Mean_ProjVel) + Mean_SoundSpeed;
-      if (geometry->nodes->GetDomain(iPoint)) nodes->AddMax_Lambda_Inv(iPoint, Lambda);
-      if (geometry->nodes->GetDomain(jPoint)) nodes->AddMax_Lambda_Inv(jPoint, Lambda);
-    }
-
-    /*--- Viscous contribution ---*/
-
-    thermal_diffusivity = config->GetThermalDiffusivity();
-    if(flow) {
-      if(turb) {
-        eddy_viscosity = solver_container[TURB_SOL]->GetNodes()->GetmuT(iPoint);
+      if (flow) {
+        const su2double laminar_viscosity = 0.5 * (flow_nodes->GetLaminarViscosity(iPoint) +
+                                                   flow_nodes->GetLaminarViscosity(jPoint));
+        const su2double eddy_viscosity = 0.5 * (flow_nodes->GetEddyViscosity(iPoint) +
+                                                flow_nodes->GetEddyViscosity(jPoint));
+
+        const su2double thermal_diffusivity = laminar_viscosity / prandtl_lam + eddy_viscosity / prandtl_turb;
+        nodes->AddMax_Lambda_Visc(iPoint, thermal_diffusivity * Area2);
+      } else {
+        nodes->AddMax_Lambda_Visc(iPoint, constant_thermal_diffusivity * Area2);
       }
-
-      thermal_diffusivity = laminar_viscosity/Prandtl_Lam + eddy_viscosity/Prandtl_Turb;
     }
-
-    Lambda = thermal_diffusivity*Area*Area;
-    if (geometry->nodes->GetDomain(iPoint)) nodes->AddMax_Lambda_Visc(iPoint, Lambda);
-    if (geometry->nodes->GetDomain(jPoint)) nodes->AddMax_Lambda_Visc(jPoint, Lambda);
-
   }
+  END_SU2_OMP_FOR
 
   /*--- Loop boundary edges ---*/
 
-  for (auto iMarker = 0u; iMarker < geometry->GetnMarker(); iMarker++) {
-    for (auto iVertex = 0ul; iVertex < geometry->GetnVertex(iMarker); iVertex++) {
+  for (unsigned short iMarker = 0; iMarker < geometry->GetnMarker(); iMarker++) {
+    if ((config->GetMarker_All_KindBC(iMarker) != INTERNAL_BOUNDARY) &&
+        (config->GetMarker_All_KindBC(iMarker) != NEARFIELD_BOUNDARY) &&
+        (config->GetMarker_All_KindBC(iMarker) != PERIODIC_BOUNDARY)) {
 
-      /*--- Point identification, Normal vector and area ---*/
+      SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
+      for (auto iVertex = 0ul; iVertex < geometry->GetnVertex(iMarker); iVertex++) {
 
-      iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
-      Normal = geometry->vertex[iMarker][iVertex]->GetNormal();
-      Area = GeometryToolbox::Norm(nDim, Normal);
+        /*--- Point identification, Normal vector and area ---*/
 
-      /*--- Inviscid contribution ---*/
+        const auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
 
-      if (flow) {
-        Mean_ProjVel = solver_container[FLOW_SOL]->GetNodes()->GetProjVel(iPoint, Normal);
-        Mean_BetaInc2 = solver_container[FLOW_SOL]->GetNodes()->GetBetaInc2(iPoint);
-        Mean_DensityInc = solver_container[FLOW_SOL]->GetNodes()->GetDensity(iPoint);
-        Mean_SoundSpeed = sqrt(Mean_ProjVel*Mean_ProjVel + (Mean_BetaInc2/Mean_DensityInc)*Area*Area);
+        if (!geometry->nodes->GetDomain(iPoint)) continue;
 
-        Lambda = fabs(Mean_ProjVel) + Mean_SoundSpeed;
-        if (geometry->nodes->GetDomain(iPoint)) nodes->AddMax_Lambda_Inv(iPoint, Lambda);
-      }
+        const auto* Normal = geometry->vertex[iMarker][iVertex]->GetNormal();
+        const su2double Area2 = GeometryToolbox::SquaredNorm(nDim, Normal);
 
-      /*--- Viscous contribution ---*/
-
-      thermal_diffusivity = config->GetThermalDiffusivity();
-      if(flow) {
-        if(turb) {
-          eddy_viscosity = solver_container[TURB_SOL]->GetNodes()->GetmuT(iPoint);
+        if (flow) {
+          const su2double thermal_diffusivity = flow_nodes->GetLaminarViscosity(iPoint) / prandtl_lam +
+                                                flow_nodes->GetEddyViscosity(iPoint) / prandtl_turb;
+          nodes->AddMax_Lambda_Visc(iPoint, thermal_diffusivity * Area2);
+        } else {
+          nodes->AddMax_Lambda_Visc(iPoint, constant_thermal_diffusivity * Area2);
         }
-
-        thermal_diffusivity = laminar_viscosity/Prandtl_Lam + eddy_viscosity/Prandtl_Turb;
       }
-
-      Lambda = thermal_diffusivity*Area*Area;
-      if (geometry->nodes->GetDomain(iPoint)) nodes->AddMax_Lambda_Visc(iPoint, Lambda);
-
+      END_SU2_OMP_FOR
     }
   }
 
-  /*--- Each element uses their own speed, steady state simulation ---*/
-
-  for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
-
-    Vol = geometry->nodes->GetVolume(iPoint);
-
-    if (Vol != 0.0) {
-
-      if(flow) {
-        Local_Delta_Time_Inv = config->GetCFL(iMesh)*Vol / nodes->GetMax_Lambda_Inv(iPoint);
-        Local_Delta_Time_Visc = config->GetCFL(iMesh)*K_v*Vol*Vol/ nodes->GetMax_Lambda_Visc(iPoint);
-      }
-      else {
-        Local_Delta_Time_Inv = config->GetMax_DeltaTime();
-        Local_Delta_Time_Visc = config->GetCFL(iMesh)*K_v*Vol*Vol/ nodes->GetMax_Lambda_Visc(iPoint);
-        //Local_Delta_Time_Visc = 100.0*K_v*Vol*Vol/ nodes->GetMax_Lambda_Visc(iPoint);
-      }
+  /*--- Each element uses their own speed, steady state simulation. ---*/
+  {
+    /*--- Thread-local variables for min/max reduction. ---*/
+    su2double minDt = 1e30, maxDt = 0.0;
 
-      /*--- Time step setting method ---*/
+    SU2_OMP_FOR_(schedule(static,omp_chunk_size) SU2_NOWAIT)
+    for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
 
-      if (config->GetKind_TimeStep_Heat() == BYFLOW && flow) {
-        Local_Delta_Time = solver_container[FLOW_SOL]->GetNodes()->GetDelta_Time(iPoint);
-      }
-      else if (config->GetKind_TimeStep_Heat() == MINIMUM) {
-        Local_Delta_Time = min(Local_Delta_Time_Inv, Local_Delta_Time_Visc);
-      }
-      else if (config->GetKind_TimeStep_Heat() == CONVECTIVE) {
-        Local_Delta_Time = Local_Delta_Time_Inv;
-      }
-      else if (config->GetKind_TimeStep_Heat() == VISCOUS) {
-        Local_Delta_Time = Local_Delta_Time_Visc;
+      su2double local_delta_time = 0.0;
+
+      const su2double Vol = geometry->nodes->GetVolume(iPoint);
+      if (Vol != 0.0) {
+        local_delta_time = nodes->GetLocalCFL(iPoint) * K_v * pow(Vol, 2) / nodes->GetMax_Lambda_Visc(iPoint);
+        if (flow) {
+          switch (config->GetKind_TimeStep_Heat()) {
+            case BYFLOW:
+            case CONVECTIVE:
+              local_delta_time = flow_nodes->GetDelta_Time(iPoint);
+              break;
+            case MINIMUM:
+              local_delta_time = min(local_delta_time, flow_nodes->GetDelta_Time(iPoint));
+              break;
+            case VISCOUS:
+              break;
+            default:
+              break;
+          }
+        }
+        minDt = min(minDt, local_delta_time);
+        maxDt = max(maxDt, local_delta_time);
       }
-
-      /*--- Min-Max-Logic ---*/
-
-      Global_Delta_Time = min(Global_Delta_Time, Local_Delta_Time);
-      Min_Delta_Time = min(Min_Delta_Time, Local_Delta_Time);
-      Max_Delta_Time = max(Max_Delta_Time, Local_Delta_Time);
-      if (Local_Delta_Time > config->GetMax_DeltaTime())
-        Local_Delta_Time = config->GetMax_DeltaTime();
-
-      nodes->SetDelta_Time(iPoint,CFL_Reduction*Local_Delta_Time);
+      nodes->SetDelta_Time(iPoint, local_delta_time);
     }
-    else {
-      nodes->SetDelta_Time(iPoint,0.0);
+    END_SU2_OMP_FOR
+    /*--- Min/max over threads. ---*/
+    SU2_OMP_CRITICAL
+    {
+      Min_Delta_Time = min(Min_Delta_Time, minDt);
+      Max_Delta_Time = max(Max_Delta_Time, maxDt);
+      Global_Delta_Time = Min_Delta_Time;
     }
+    END_SU2_OMP_CRITICAL
   }
 
-  /*--- Compute the max and the min dt (in parallel) ---*/
-  if (config->GetComm_Level() == COMM_FULL) {
-#ifdef HAVE_MPI
-    su2double rbuf_time, sbuf_time;
-    sbuf_time = Min_Delta_Time;
-    SU2_MPI::Reduce(&sbuf_time, &rbuf_time, 1, MPI_DOUBLE, MPI_MIN, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Bcast(&rbuf_time, 1, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    Min_Delta_Time = rbuf_time;
-
-    sbuf_time = Max_Delta_Time;
-    SU2_MPI::Reduce(&sbuf_time, &rbuf_time, 1, MPI_DOUBLE, MPI_MAX, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Bcast(&rbuf_time, 1, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    Max_Delta_Time = rbuf_time;
-#endif
-  }
+  /*--- Compute the min/max dt (in parallel, now over mpi ranks). ---*/
 
-  /*--- For exact time solution use the minimum delta time of the whole mesh ---*/
-  if (config->GetTime_Marching() == TIME_MARCHING::TIME_STEPPING) {
-#ifdef HAVE_MPI
-    su2double rbuf_time, sbuf_time;
-    sbuf_time = Global_Delta_Time;
-    SU2_MPI::Reduce(&sbuf_time, &rbuf_time, 1, MPI_DOUBLE, MPI_MIN, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Bcast(&rbuf_time, 1, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    Global_Delta_Time = rbuf_time;
-#endif
-    for (iPoint = 0; iPoint < nPointDomain; iPoint++)
-      nodes->SetDelta_Time(iPoint,Global_Delta_Time);
-  }
+  BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
+    if (config->GetComm_Level() == COMM_FULL) {
+      su2double rbuf_time;
+      SU2_MPI::Allreduce(&Min_Delta_Time, &rbuf_time, 1, MPI_DOUBLE, MPI_MIN, SU2_MPI::GetComm());
+      Min_Delta_Time = rbuf_time;
 
-  /*--- Recompute the unsteady time step for the dual time strategy
-   if the unsteady CFL is diferent from 0 ---*/
-  if ((dual_time) && (Iteration == 0) && (config->GetUnst_CFL() != 0.0) && (iMesh == MESH_0)) {
-    Global_Delta_UnstTimeND = config->GetUnst_CFL()*Global_Delta_Time/config->GetCFL(iMesh);
-
-#ifdef HAVE_MPI
-    su2double rbuf_time, sbuf_time;
-    sbuf_time = Global_Delta_UnstTimeND;
-    SU2_MPI::Reduce(&sbuf_time, &rbuf_time, 1, MPI_DOUBLE, MPI_MIN, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Bcast(&rbuf_time, 1, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    Global_Delta_UnstTimeND = rbuf_time;
-#endif
-    config->SetDelta_UnstTimeND(Global_Delta_UnstTimeND);
-  }
+      SU2_MPI::Allreduce(&Max_Delta_Time, &rbuf_time, 1, MPI_DOUBLE, MPI_MAX, SU2_MPI::GetComm());
+      Max_Delta_Time = rbuf_time;
+    }
+  } END_SU2_OMP_SAFE_GLOBAL_ACCESS
 
-  /*--- The pseudo local time (explicit integration) cannot be greater than the physical time ---*/
-  if (dual_time)
-    for (iPoint = 0; iPoint < nPointDomain; iPoint++) {
-      if (!implicit) {
-        cout << "Using unsteady time: " << config->GetDelta_UnstTimeND() << endl;
-        Local_Delta_Time = min((2.0/3.0)*config->GetDelta_UnstTimeND(), nodes->GetDelta_Time(iPoint));
-        nodes->SetDelta_Time(iPoint,Local_Delta_Time);
-      }
-  }
-}
+  /*--- For exact time solution use the minimum delta time of the whole mesh. ---*/
+  if (time_stepping) {
 
-void CHeatSolver::ExplicitEuler_Iteration(CGeometry *geometry, CSolver **solver_container, CConfig *config) {
+    /*--- If the unsteady CFL is set to zero, it uses the defined unsteady time step,
+     *    otherwise it computes the time step based on the unsteady CFL. ---*/
 
-  su2double *local_Residual, *local_Res_TruncError, Vol, Delta, Res;
+    BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS
+    {
+      if (config->GetUnst_CFL() == 0.0) {
+        Global_Delta_Time = config->GetDelta_UnstTime();
+      }
+      else {
+        Global_Delta_Time = Min_Delta_Time;
+      }
+      Max_Delta_Time = Global_Delta_Time;
 
-  SetResToZero();
+      config->SetDelta_UnstTimeND(Global_Delta_Time);
+    }
+    END_SU2_OMP_SAFE_GLOBAL_ACCESS
 
-  /*--- Update the solution ---*/
+    /*--- Sets the regular CFL equal to the unsteady CFL. ---*/
 
-  for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
-    Vol = geometry->nodes->GetVolume(iPoint);
-    Delta = nodes->GetDelta_Time(iPoint) / Vol;
-
-    local_Res_TruncError = nodes->GetResTruncError(iPoint);
-    local_Residual = LinSysRes.GetBlock(iPoint);
-
-    if (!config->GetContinuous_Adjoint()) {
-      for (auto iVar = 0u; iVar < nVar; iVar++) {
-        Res = local_Residual[iVar] + local_Res_TruncError[iVar];
-        nodes->AddSolution(iPoint,iVar, -Res*Delta);
-        Residual_RMS[iVar] += Res*Res;
-        AddRes_Max(iVar, fabs(Res), geometry->nodes->GetGlobalIndex(iPoint), geometry->nodes->GetCoord(iPoint));
-      }
+    SU2_OMP_FOR_STAT(omp_chunk_size)
+    for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
+      nodes->SetLocalCFL(iPoint, config->GetUnst_CFL());
+      nodes->SetDelta_Time(iPoint, Global_Delta_Time);
     }
+    END_SU2_OMP_FOR
 
   }
 
-  /*--- MPI solution ---*/
-
-  InitiateComms(geometry, config, SOLUTION);
-  CompleteComms(geometry, config, SOLUTION);
-
-  /*--- Compute the root mean square residual ---*/
-
-  SetResidual_RMS(geometry, config);
-
-}
-
+  /*--- Recompute the unsteady time step for the dual time strategy if the unsteady CFL is diferent from 0.
+    * This is only done once because in dual time the time step cannot be variable. ---*/
 
-void CHeatSolver::ImplicitEuler_Iteration(CGeometry *geometry, CSolver **solver_container, CConfig *config) {
+  if (dual_time && (Iteration == config->GetRestart_Iter()) && (config->GetUnst_CFL() != 0.0) && (iMesh == MESH_0)) {
 
-  /*--- Set maximum residual to zero ---*/
+    /*--- Thread-local variable for reduction. ---*/
+    su2double glbDtND = 1e30;
 
-  SetResToZero();
-
-  /*--- Build implicit system ---*/
-
-  for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
-
-    /*--- Read the residual ---*/
-
-    su2double* local_Res_TruncError = nodes->GetResTruncError(iPoint);
-
-    /*--- Modify matrix diagonal to assure diagonal dominance ---*/
-
-    const su2double dt = nodes->GetDelta_Time(iPoint);
-    if (dt != 0.0) {
-      /*--- For nodes on periodic boundaries, add the respective partner volume. ---*/
-      // Identical for flow and heat
-      const su2double Vol = geometry->nodes->GetVolume(iPoint) + geometry->nodes->GetPeriodicVolume(iPoint);
-      Jacobian.AddVal2Diag(iPoint, Vol / dt);
-
-    } else {
-      Jacobian.SetVal2Diag(iPoint, 1.0);
-      for (auto iVar = 0u; iVar < nVar; iVar++) {
-        const auto total_index = iPoint*nVar + iVar;
-        LinSysRes[total_index] = 0.0;
-        local_Res_TruncError[iVar] = 0.0;
-      }
-    }
-
-    /*--- Right hand side of the system (-Residual) and initial guess (x = 0) ---*/
-
-    for (auto iVar = 0; iVar < nVar; iVar++) {
-      const auto total_index = iPoint*nVar+iVar;
-      LinSysRes[total_index] = - (LinSysRes[total_index] + local_Res_TruncError[iVar]);
-      LinSysSol[total_index] = 0.0;
-      Residual_RMS[iVar] += LinSysRes[total_index]*LinSysRes[total_index];
-      AddRes_Max(iVar, fabs(LinSysRes[total_index]), geometry->nodes->GetGlobalIndex(iPoint), geometry->nodes->GetCoord(iPoint));
+    SU2_OMP_FOR_(schedule(static,omp_chunk_size) SU2_NOWAIT)
+    for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
+      glbDtND = min(glbDtND, config->GetUnst_CFL()*Global_Delta_Time / nodes->GetLocalCFL(iPoint));
     }
-  }
+    END_SU2_OMP_FOR
+    SU2_OMP_CRITICAL
+    Global_Delta_UnstTimeND = min(Global_Delta_UnstTimeND, glbDtND);
+    END_SU2_OMP_CRITICAL
 
-  /*--- Initialize residual and solution at the ghost points ---*/
+    BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS
+    {
+      SU2_MPI::Allreduce(&Global_Delta_UnstTimeND, &glbDtND, 1, MPI_DOUBLE, MPI_MIN, SU2_MPI::GetComm());
+      Global_Delta_UnstTimeND = glbDtND;
 
-  for (auto iPoint = nPointDomain; iPoint < nPoint; iPoint++) {
-    for (auto iVar = 0u; iVar < nVar; iVar++) {
-      const auto total_index = iPoint*nVar + iVar;
-      LinSysRes[total_index] = 0.0;
-      LinSysSol[total_index] = 0.0;
+      config->SetDelta_UnstTimeND(Global_Delta_UnstTimeND);
     }
+    END_SU2_OMP_SAFE_GLOBAL_ACCESS
   }
 
-  /*--- Solve or smooth the linear system ---*/
-
-  auto iter = System.Solve(Jacobian, LinSysRes, LinSysSol, geometry, config);
-
-  /*--- Store the the number of iterations of the linear solver ---*/
-  SetIterLinSolver(iter);
-
-  /*--- Store the value of the residual. ---*/
-  SetResLinSolver(System.GetResidual());
+  /*--- The pseudo local time (explicit integration) cannot be greater than the physical time ---*/
 
-  for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
-    for (auto iVar = 0u; iVar < nVar; iVar++) {
-      nodes->AddSolution(iPoint,iVar, LinSysSol[iPoint*nVar+iVar]);
+  if (dual_time && !implicit) {
+    SU2_OMP_FOR_STAT(omp_chunk_size)
+    for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
+      su2double dt = min((2.0/3.0)*config->GetDelta_UnstTimeND(), nodes->GetDelta_Time(iPoint));
+      nodes->SetDelta_Time(iPoint, dt);
     }
+    END_SU2_OMP_FOR
   }
-
-  /*--- Synchronize the solution between master and passive periodic nodes after the linear solve. ---*/
-  for (unsigned short iPeriodic = 1; iPeriodic <= config->GetnMarker_Periodic() / 2; iPeriodic++) {
-    InitiatePeriodicComms(geometry, config, iPeriodic, PERIODIC_IMPLICIT);
-    CompletePeriodicComms(geometry, config, iPeriodic, PERIODIC_IMPLICIT);
-  }
-
-  /*--- MPI solution ---*/
-
-  InitiateComms(geometry, config, SOLUTION);
-  CompleteComms(geometry, config, SOLUTION);
-
-  /*--- Compute the root mean square residual ---*/
-
-  SetResidual_RMS(geometry, config);
-
 }
 
 void CHeatSolver::SetInitialCondition(CGeometry **geometry, CSolver ***solver_container, CConfig *config, unsigned long TimeIter) {
@@ -1382,67 +967,57 @@ void CHeatSolver::SetInitialCondition(CGeometry **geometry, CSolver ***solver_co
 
 void CHeatSolver::SetResidual_DualTime(CGeometry *geometry, CSolver **solver_container, CConfig *config,
                                        unsigned short iRKStep, unsigned short iMesh, unsigned short RunTime_EqSystem) {
-
-  /*--- Local variables ---*/
-
-  const su2double *U_time_n, *U_time_nP1, *U_time_nM1;
-  su2double Volume_nP1;
-
+  if (flow) {
+    CScalarSolver<CHeatVariable>::SetResidual_DualTime(geometry, solver_container, config, iRKStep, iMesh, RunTime_EqSystem);
+    return;
+  }
   const bool first_order  = (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST);
   const bool second_order = (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND);
-  const bool implicit = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
+  const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
 
   /*--- Store the physical time step ---*/
 
   const su2double TimeStep = config->GetDelta_UnstTimeND();
 
-  /*--- Compute the dual time-stepping source term for static meshes ---*/
-
-  if (!dynamic_grid) {
-
-    /*--- Loop over all nodes (excluding halos) ---*/
+  /*--- Compute the dual time-stepping source term ---*/
+  /*--- Loop over all nodes (excluding halos) ---*/
 
-    for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
+  AD::StartNoSharedReading();
 
-      /*--- Retrieve the solution at time levels n-1, n, and n+1. Note that
-       we are currently iterating on U^n+1 and that U^n & U^n-1 are fixed,
-       previous solutions that are stored in memory. ---*/
+  SU2_OMP_FOR_STAT(omp_chunk_size)
+  for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
 
-      U_time_nM1 = nodes->GetSolution_time_n1(iPoint);
-      U_time_n   = nodes->GetSolution_time_n(iPoint);
-      U_time_nP1 = nodes->GetSolution(iPoint);
+    /*--- Retrieve the solution at time levels n-1, n, and n+1. Note that
+      we are currently iterating on U^n+1 and that U^n & U^n-1 are fixed,
+      previous solutions that are stored in memory. ---*/
 
-      /*--- CV volume at time n+1. As we are on a static mesh, the volume
-       of the CV will remained fixed for all time steps. ---*/
+    const auto* U_time_nM1 = nodes->GetSolution_time_n1(iPoint);
+    const auto* U_time_n = nodes->GetSolution_time_n(iPoint);
+    const auto* U_time_nP1 = nodes->GetSolution(iPoint);
 
-      Volume_nP1 = geometry->nodes->GetVolume(iPoint);
+    /*--- CV volume at time n+1. As we are on a static mesh, the volume
+      of the CV will remained fixed for all time steps. ---*/
 
-      /*--- Compute the dual time-stepping source term based on the chosen
-       time discretization scheme (1st- or 2nd-order).---*/
+    const su2double Volume_nP1 = geometry->nodes->GetVolume(iPoint);
 
-      for (auto iVar = 0u; iVar < nVar; iVar++) {
-        if (first_order)
-          Residual[iVar] = (U_time_nP1[iVar] - U_time_n[iVar])*Volume_nP1 / TimeStep;
-        if (second_order)
-          Residual[iVar] = ( 3.0*U_time_nP1[iVar] - 4.0*U_time_n[iVar]
-                            +1.0*U_time_nM1[iVar])*Volume_nP1 / (2.0*TimeStep);
-      }
+    /*--- Compute the dual time-stepping source term based on the chosen
+      time discretization scheme (1st- or 2nd-order).---*/
 
-      /*--- Store the residual and compute the Jacobian contribution due
-       to the dual time source term. ---*/
-
-      LinSysRes.AddBlock(iPoint, Residual);
-      if (implicit) {
-        for (auto iVar = 0u; iVar < nVar; iVar++) {
-          for (auto jVar = 0u; jVar < nVar; jVar++) Jacobian_i[iVar][jVar] = 0.0;
-          if (first_order)
-            Jacobian_i[iVar][iVar] = Volume_nP1 / TimeStep;
-          if (second_order)
-            Jacobian_i[iVar][iVar] = (Volume_nP1*3.0)/(2.0*TimeStep);
-        }
+    for (auto iVar = 0u; iVar < nVar; iVar++) {
+      if (first_order)
+        LinSysRes(iPoint, iVar) += (U_time_nP1[iVar] - U_time_n[iVar]) * Volume_nP1 / TimeStep;
+      if (second_order)
+        LinSysRes(iPoint, iVar) += (3.0 * U_time_nP1[iVar] - 4.0 * U_time_n[iVar] +
+                                    1.0 * U_time_nM1[iVar]) * Volume_nP1 / (2.0 * TimeStep);
+    }
 
-        Jacobian.AddBlock2Diag(iPoint, Jacobian_i);
-      }
+    /*--- Compute the Jacobian contribution due to the dual time source term. ---*/
+    if (implicit) {
+      if (first_order) Jacobian.AddVal2Diag(iPoint, Volume_nP1 / TimeStep);
+      if (second_order) Jacobian.AddVal2Diag(iPoint, (Volume_nP1 * 3.0) / (2.0 * TimeStep));
     }
   }
+  END_SU2_OMP_FOR
+
+  AD::EndNoSharedReading();
 }
diff --git a/SU2_CFD/src/solvers/CMeshSolver.cpp b/SU2_CFD/src/solvers/CMeshSolver.cpp
index 57b4b25edb7..77470e620fb 100644
--- a/SU2_CFD/src/solvers/CMeshSolver.cpp
+++ b/SU2_CFD/src/solvers/CMeshSolver.cpp
@@ -415,7 +415,7 @@ void CMeshSolver::SetWallDistance(CGeometry *geometry, CConfig *config) {
   END_SU2_OMP_PARALLEL
 }
 
-void CMeshSolver::SetMesh_Stiffness(CNumerics **numerics, CConfig *config){
+void CMeshSolver::SetMesh_Stiffness(CGeometry **geometry, CNumerics **numerics, CConfig *config){
 
   if (stiffness_set) return;
 
diff --git a/SU2_CFD/src/variables/CEulerVariable.cpp b/SU2_CFD/src/variables/CEulerVariable.cpp
index 36d746d9bc0..255ffdfaf54 100644
--- a/SU2_CFD/src/variables/CEulerVariable.cpp
+++ b/SU2_CFD/src/variables/CEulerVariable.cpp
@@ -73,6 +73,12 @@ CEulerVariable::CEulerVariable(su2double density, const su2double *velocity, su2
     WindGustDer.resize(nPoint,nDim+1);
   }
 
+  if (config->GetVorticityConfinement()) {
+    nAuxVar = 1;
+    Grad_AuxVar.resize(nPoint, nAuxVar, nDim, 0.0);
+    AuxVar.resize(nPoint, nAuxVar) = su2double(0.0);
+  }
+  
   if (config->GetKind_FluidModel() == DATADRIVEN_FLUID){
     Dataset_Extrapolation.resize(nPoint) = 0;
     nIter_Newtonsolver.resize(nPoint) = 0;
diff --git a/SU2_CFD/src/variables/CHeatVariable.cpp b/SU2_CFD/src/variables/CHeatVariable.cpp
index a8a889d8899..f87420cea98 100644
--- a/SU2_CFD/src/variables/CHeatVariable.cpp
+++ b/SU2_CFD/src/variables/CHeatVariable.cpp
@@ -25,16 +25,13 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #include "../../include/variables/CHeatVariable.hpp"
 
-
 CHeatVariable::CHeatVariable(su2double heat, unsigned long npoint, unsigned long ndim, unsigned long nvar, CConfig *config)
-  : CVariable(npoint, ndim, nvar, config), Gradient_Reconstruction(config->GetReconstructionGradientRequired() ? Gradient_Aux : Gradient) {
+  : CScalarVariable(npoint, ndim, nvar, config) {
 
-  bool low_fidelity = false;
-  bool dual_time = ((config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
-                    (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND));
+  const bool dual_time = ((config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
+                          (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND));
 
   /*--- Initialization of heat variable ---*/
 
@@ -43,14 +40,14 @@ CHeatVariable::CHeatVariable(su2double heat, unsigned long npoint, unsigned long
 
   /*--- Allocate residual structures ---*/
 
-  Res_TruncError.resize(nPoint,nVar) = su2double(0.0);
+  Res_TruncError.resize(nPoint, nVar) = su2double(0.0);
 
   /*--- Only for residual smoothing (multigrid) ---*/
 
   for (unsigned long iMesh = 0; iMesh <= config->GetnMGLevels(); iMesh++) {
-    if ((config->GetMG_CorrecSmooth(iMesh) > 0) || low_fidelity) {
-      Residual_Sum.resize(nPoint,nVar);
-      Residual_Old.resize(nPoint,nVar);
+    if (config->GetMG_CorrecSmooth(iMesh) > 0) {
+      Residual_Sum.resize(nPoint, nVar);
+      Residual_Old.resize(nPoint, nVar);
       break;
     }
   }
@@ -61,27 +58,7 @@ CHeatVariable::CHeatVariable(su2double heat, unsigned long npoint, unsigned long
     Solution_time_n1 = heat;
   }
 
-  /*--- Gradient related fields ---*/
-  Gradient.resize(nPoint,nVar,nDim,0.0);
-
-  if (config->GetReconstructionGradientRequired()) {
-    Gradient_Aux.resize(nPoint,nVar,nDim,0.0);
-  }
-
-  if (config->GetLeastSquaresRequired()) {
-    Rmatrix.resize(nPoint,nDim,nDim,0.0);
-  }
-
-  if (config->GetKind_ConvNumScheme_Heat() == SPACE_CENTERED)
-    Undivided_Laplacian.resize(nPoint,nVar);
-
-  Max_Lambda_Inv.resize(nPoint);
   Max_Lambda_Visc.resize(nPoint);
-  Delta_Time.resize(nPoint);
-
-  /* Under-relaxation parameter. */
-  UnderRelaxation.resize(nPoint) = su2double(1.0);
-  LocalCFL.resize(nPoint) = su2double(0.0);
 
   if (config->GetMultizone_Problem())
     Set_BGSSolution_k();

From f0d8b0aab160cc90d3da0c434cae0a33eb30eadd Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Mon, 13 Feb 2023 09:27:56 -0800
Subject: [PATCH 196/656] fix multizone memory errors

---
 SU2_CFD/include/drivers/CDriverBase.hpp                   | 8 ++++----
 SU2_CFD/src/drivers/CDriverBase.cpp                       | 6 ------
 SU2_DEF/src/drivers/CDeformationDriver.cpp                | 8 ++++----
 SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp         | 8 ++++----
 .../streamwise_periodic/chtPinArray_2d/configMaster.cfg   | 2 +-
 5 files changed, 13 insertions(+), 19 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index f35c32ca07b..b7c5ca56d9f 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -62,8 +62,8 @@ class CDriverBase {
       *nInst,            /*!< \brief Total number of instances in the problem (per zone). */
       **interface_types; /*!< \brief Type of coupling between the distinct (physical) zones. */
 
-  CConfig* driver_config; /*!< \brief Definition of the driver configuration. */
-  COutput* driver_output; /*!< \brief Definition of the driver output. */
+  CConfig* driver_config = nullptr; /*!< \brief Definition of the driver configuration. */
+  COutput* driver_output = nullptr; /*!< \brief Definition of the driver output. */
 
   CConfig** config_container;           /*!< \brief Definition of the particular problem. */
   COutput** output_container;           /*!< \brief Pointer to the COutput class. */
@@ -74,8 +74,8 @@ class CDriverBase {
   CSurfaceMovement** surface_movement;  /*!< \brief Surface movement classes of the problem. */
   CVolumetricMovement*** grid_movement; /*!< \brief Volume grid movement classes of the problem. */
 
-  CConfig* main_config;     /*!< \brief Reference to base (i.e. ZONE 0) configuration (used in driver API). */
-  CGeometry* main_geometry; /*!< \brief Reference to base (i.e. ZONE, INST, MESH 0) geometry (used in driver API). */
+  CConfig* main_config = nullptr;     /*!< \brief Reference to base (i.e. ZONE 0) configuration (used in driver API). */
+  CGeometry* main_geometry = nullptr; /*!< \brief Reference to base (i.e. ZONE, INST, MESH 0) geometry (used in driver API). */
 
  public:
   /*!
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index cfafb9d419e..b13afb6e27f 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -55,12 +55,6 @@ void CDriverBase::SetContainers_Null() {
   for (iZone = 0; iZone < nZone; iZone++) {
     nInst[iZone] = 1;
   }
-
-  driver_config = nullptr;
-  driver_output = nullptr;
-
-  main_config = nullptr;
-  main_geometry = nullptr;
 }
 
 void CDriverBase::CommonPostprocessing() {
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 03f95c3cb39..d88d0048ec3 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -49,10 +49,6 @@ CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
   rank = SU2_MPI::GetRank();
   size = SU2_MPI::GetSize();
 
-  /*--- Initialize containers. --- */
-
-  SetContainers_Null();
-
   /*--- Preprocessing of the config files. ---*/
 
   Input_Preprocessing();
@@ -102,6 +98,10 @@ void CDeformationDriver::Input_Preprocessing() {
 
   nZone = driver_config->GetnZone();
 
+  /*--- Initialize containers. --- */
+
+  SetContainers_Null();
+
   /*--- Loop over all zones to initialize the various classes. In most
    cases, nZone is equal to one. This represents the solution of a partial
    differential equation on a single block, unstructured mesh. ---*/
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index 4b3c92be99b..ddab47fc4f9 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -55,10 +55,6 @@ CDiscAdjDeformationDriver::CDiscAdjDeformationDriver(char* confFile, SU2_Comm MP
   rank = SU2_MPI::GetRank();
   size = SU2_MPI::GetSize();
 
-  /*--- Initialize containers. --- */
-
-  SetContainers_Null();
-
   /*--- Preprocessing of the config files. ---*/
 
   Input_Preprocessing();
@@ -109,6 +105,10 @@ void CDiscAdjDeformationDriver::Input_Preprocessing() {
 
   nZone = driver_config->GetnZone();
 
+  /*--- Initialize containers. --- */
+
+  SetContainers_Null();
+
   /*--- Loop over all zones to initialize the various classes. In most
    * cases, nZone is equal to one. This represents the solution of a partial
    * differential equation on a single block, unstructured mesh. ---*/
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configMaster.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configMaster.cfg
index 3803a89e9b6..8e66cb0ab71 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configMaster.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configMaster.cfg
@@ -69,7 +69,7 @@ DEFORM_LINEAR_SOLVER_PREC= ILU
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
 %
 DEFORM_NONLINEAR_ITER= 1
-DEFORM_LINEAR_SOLVER_ITER= 1000
+DEFORM_LINEAR_SOLVER_ITER= 10
 %
 DEFORM_CONSOLE_OUTPUT= YES
 DEFORM_STIFFNESS_TYPE= WALL_DISTANCE

From d183ed22033280eefde5f378c9d9be47366a05c0 Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Mon, 13 Feb 2023 13:30:00 -0500
Subject: [PATCH 197/656] update regression folder names

---
 TestCases/parallel_regression.py | 6 +++---
 TestCases/serial_regression.py   | 2 +-
 2 files changed, 4 insertions(+), 4 deletions(-)

diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index c933799286e..92bba2d4460 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -142,7 +142,7 @@ def main():
 
     # Viscous single cone - axisymmetric
     visc_cone = TestCase('visc_cone')
-    visc_cone.cfg_dir = "nonequilibrium/viscous"
+    visc_cone.cfg_dir = "nonequilibrium/visc_wedge"
     visc_cone.cfg_file = "axi_visccone.cfg"
     visc_cone.test_iter = 10
     visc_cone.test_vals = [-5.222212, -5.746462, -20.569425, -20.633786, -20.547642, 1.255865, -3.208363, -0.016006, 0.093455, 32633.000000]
@@ -161,7 +161,7 @@ def main():
 
     # Viscous single wedge - super catalytic walls
     super_cat = TestCase('super_cat')
-    super_cat.cfg_dir = "nonequilibrium/viscous"
+    super_cat.cfg_dir = "nonequilibrium/visc_wedge"
     super_cat.cfg_file = "super_cat.cfg"
     super_cat.test_iter = 10
     super_cat.test_vals = [-5.232590, -5.757884, -20.727046, -20.748136, -20.564044, 1.246889, -3.205235, -0.028406, 0.250857, 3.2459e+04]
@@ -173,7 +173,7 @@ def main():
 
     # Viscous single wedge - partially catalytic walls
     partial_cat = TestCase('partial_cat')
-    partial_cat.cfg_dir = "nonequilibrium/viscous"
+    partial_cat.cfg_dir = "nonequilibrium/visc_wedge"
     partial_cat.cfg_file = "partial_cat.cfg"
     partial_cat.test_iter = 10
     partial_cat.test_vals = [-5.210300, -5.735063, -20.880374, -20.825890, -23.475263, 1.806281, -2.813924, -0.078469, 0.496017, 2.9021e+04]
diff --git a/TestCases/serial_regression.py b/TestCases/serial_regression.py
index fdd27f140ae..eac47ffd859 100644
--- a/TestCases/serial_regression.py
+++ b/TestCases/serial_regression.py
@@ -70,7 +70,7 @@ def main():
 
     # Viscous single cone - axisymmetric
     visc_cone = TestCase('visc_cone')
-    visc_cone.cfg_dir = "nonequilibrium/viscous"
+    visc_cone.cfg_dir = "nonequilibrium/visc_wedge"
     visc_cone.cfg_file = "axi_visccone.cfg"
     visc_cone.test_iter = 10
     visc_cone.test_vals = [-5.215229, -5.739368, -20.545048, -20.618699, -20.502531, 1.262784, -3.205454, -0.015696, 0.093207, 32656.000000]

From 804e6a2d4744ce60833bb8b5f5122fb351367d43 Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Mon, 13 Feb 2023 22:36:50 -0500
Subject: [PATCH 198/656] const/auto variables and loops

---
 SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp   | 143 ++++----
 SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp  |  82 ++---
 SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp    | 170 +++++-----
 .../numerics/NEMO/convection/ausm_slau.cpp    | 113 +++----
 SU2_CFD/src/numerics/NEMO/convection/lax.cpp  |  26 +-
 SU2_CFD/src/numerics/NEMO/convection/msw.cpp  |  52 +--
 SU2_CFD/src/numerics/NEMO/convection/roe.cpp  |  46 +--
 SU2_CFD/src/solvers/CNEMOEulerSolver.cpp      | 318 +++++++++---------
 SU2_CFD/src/solvers/CNEMONSSolver.cpp         | 211 ++++++------
 9 files changed, 559 insertions(+), 602 deletions(-)

diff --git a/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp b/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp
index fe2ab39173d..9fdf3f49eea 100644
--- a/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp
+++ b/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp
@@ -84,28 +84,27 @@ void CNEMONumerics::GetInviscidProjFlux(const su2double *val_U,
                                         const su2double *val_V,
                                         const su2double *val_normal,
                                         su2double *val_Proj_Flux) {
-  unsigned short iSpecies, iVar;
-  su2double rho, u, v, w, rhoEve, P, H;
+
   const su2double *rhos;
 
   /*--- Initialize vectors ---*/
-  for (iVar = 0; iVar < nVar; iVar++)
+  for (auto iVar = 0ul; iVar < nVar; iVar++)
     val_Proj_Flux[iVar] = 0.0;
 
   /*--- Rename for convienience ---*/
-  rho    = val_V[RHO_INDEX];
-  u      = val_V[VEL_INDEX];
-  v      = val_V[VEL_INDEX+1];
-  w      = val_V[VEL_INDEX+2];
-  P      = val_V[P_INDEX];
-  H      = val_V[H_INDEX];
-  rhoEve = val_U[nSpecies+nDim+1];
+  const su2double rho = val_V[RHO_INDEX];
+  const su2double u = val_V[VEL_INDEX];
+  const su2double v = val_V[VEL_INDEX+1];
+  const su2double w = val_V[VEL_INDEX+2];
+  const su2double P = val_V[P_INDEX];
+  const su2double H = val_V[H_INDEX];
+  const su2double rhoEve = val_U[nSpecies+nDim+1];
   rhos   = &val_V[RHOS_INDEX];
 
   if (nDim == 2) {
 
     /*--- iDim = 0 (x-direction) ---*/
-    for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+    for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
       val_Proj_Flux[iSpecies]  = (rhos[iSpecies]*u) * val_normal[0];
     val_Proj_Flux[nSpecies]    = (rho*u*u + P)      * val_normal[0];
     val_Proj_Flux[nSpecies+1]  = (rho*u*v)          * val_normal[0];
@@ -113,7 +112,7 @@ void CNEMONumerics::GetInviscidProjFlux(const su2double *val_U,
     val_Proj_Flux[nSpecies+3]  = (rhoEve*u)         * val_normal[0];
 
     /*---- iDim = 1 (y-direction) ---*/
-    for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+    for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
       val_Proj_Flux[iSpecies] += (rhos[iSpecies]*v) * val_normal[1];
     val_Proj_Flux[nSpecies]   += (rho*v*u)          * val_normal[1];
     val_Proj_Flux[nSpecies+1] += (rho*v*v + P)      * val_normal[1];
@@ -123,7 +122,7 @@ void CNEMONumerics::GetInviscidProjFlux(const su2double *val_U,
   else {
 
     /*--- iDim = 0 (x-direction) ---*/
-    for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+    for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
       val_Proj_Flux[iSpecies]  = (rhos[iSpecies]*u) * val_normal[0];
     val_Proj_Flux[nSpecies]    = (rho*u*u + P)      * val_normal[0];
     val_Proj_Flux[nSpecies+1]  = (rho*u*v)          * val_normal[0];
@@ -132,7 +131,7 @@ void CNEMONumerics::GetInviscidProjFlux(const su2double *val_U,
     val_Proj_Flux[nSpecies+4]  = (rhoEve*u)         * val_normal[0];
 
     /*--- iDim = 0 (y-direction) ---*/
-    for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+    for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
       val_Proj_Flux[iSpecies] += (rhos[iSpecies]*v) * val_normal[1];
     val_Proj_Flux[nSpecies]   += (rho*v*u)          * val_normal[1];
     val_Proj_Flux[nSpecies+1] += (rho*v*v + P)      * val_normal[1];
@@ -141,7 +140,7 @@ void CNEMONumerics::GetInviscidProjFlux(const su2double *val_U,
     val_Proj_Flux[nSpecies+4] += (rhoEve*v)         * val_normal[1];
 
     /*--- iDim = 0 (z-direction) ---*/
-    for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+    for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
       val_Proj_Flux[iSpecies] += (rhos[iSpecies]*w) * val_normal[2];
     val_Proj_Flux[nSpecies]   += (rho*w*u)          * val_normal[2];
     val_Proj_Flux[nSpecies+1] += (rho*w*v)          * val_normal[2];
@@ -157,33 +156,32 @@ void CNEMONumerics::GetInviscidProjJac(const su2double *val_U,    const su2doubl
                                        su2double **val_Proj_Jac_Tensor) {
 
   const su2double *rhos;
-
   rhos = &val_V[RHOS_INDEX];
 
   /*--- Initialize the Jacobian tensor ---*/
-  for (unsigned short iVar = 0; iVar < nVar; iVar++)
-    for (unsigned short jVar = 0; jVar < nVar; jVar++)
+  for (auto iVar = 0ul; iVar < nVar; iVar++)
+    for (auto jVar = 0ul; jVar < nVar; jVar++)
       val_Proj_Jac_Tensor[iVar][jVar] = 0.0;
 
   /*--- Rename for convenience ---*/
-  su2double rho    = val_V[RHO_INDEX];
-  su2double H      = val_V[H_INDEX];
-  su2double rhoEve = val_U[nSpecies+nDim+1];
+  const su2double rho = val_V[RHO_INDEX];
+  const su2double H = val_V[H_INDEX];
+  const su2double rhoEve = val_U[nSpecies+nDim+1];
 
   su2double u[MAXNDIM];
-  for (unsigned short iDim = 0; iDim < nDim; iDim++)
+  for (auto iDim = 0ul; iDim < nDim; iDim++)
     u[iDim] = val_V[VEL_INDEX+iDim];
 
   /*--- Calculate projected velocity ---*/
   su2double proj_vel = GeometryToolbox::DotProduct(nDim, u, val_normal);
 
   /*--- Species density rows ---*/
-  for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
-    for (unsigned short jSpecies = 0; jSpecies < nSpecies; jSpecies++) {
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
+    for (auto jSpecies = 0ul; jSpecies < nSpecies; jSpecies++) {
       val_Proj_Jac_Tensor[iSpecies][jSpecies] += -(rhos[iSpecies]/rho) * proj_vel;
     }
     val_Proj_Jac_Tensor[iSpecies][iSpecies]   += proj_vel;
-    for (unsigned short iDim  = 0; iDim < nDim; iDim++) {
+    for (auto iDim  = 0ul; iDim < nDim; iDim++) {
       val_Proj_Jac_Tensor[iSpecies][nSpecies+iDim] += (rhos[iSpecies]/rho) * val_normal[iDim];
       val_Proj_Jac_Tensor[nSpecies+iDim][iSpecies] += val_dPdU[iSpecies]*val_normal[iDim] - proj_vel*u[iDim];
     }
@@ -192,8 +190,8 @@ void CNEMONumerics::GetInviscidProjJac(const su2double *val_U,    const su2doubl
   }
 
   /*--- Momentum rows ---*/
-  for (unsigned short iDim = 0; iDim < nDim; iDim++) {
-    for (unsigned short jDim = 0; jDim < nDim; jDim++) {
+  for (auto iDim = 0ul; iDim < nDim; iDim++) {
+    for (auto jDim = 0ul; jDim < nDim; jDim++) {
       val_Proj_Jac_Tensor[nSpecies+iDim][nSpecies+jDim] += val_dPdU[nSpecies+jDim]*val_normal[iDim] + u[iDim]*val_normal[jDim];
     }
     val_Proj_Jac_Tensor[nSpecies+iDim][nSpecies+iDim]   += proj_vel;
@@ -202,18 +200,18 @@ void CNEMONumerics::GetInviscidProjJac(const su2double *val_U,    const su2doubl
   }
 
   /*--- Total energy row ---*/
-  for (unsigned short iDim = 0; iDim < nDim; iDim++)
+  for (auto iDim = 0ul; iDim < nDim; iDim++)
     val_Proj_Jac_Tensor[nSpecies+nDim][nSpecies+iDim] += val_dPdU[nSpecies+iDim]*proj_vel + H*val_normal[iDim];
   val_Proj_Jac_Tensor[nSpecies+nDim][nSpecies+nDim]   += (1+val_dPdU[nSpecies+nDim])*proj_vel;
   val_Proj_Jac_Tensor[nSpecies+nDim][nSpecies+nDim+1] +=  val_dPdU[nSpecies+nDim+1] *proj_vel;
 
   /*--- Vib.-el. energy row ---*/
-  for (unsigned short iDim = 0; iDim < nDim; iDim++)
+  for (auto iDim = 0ul; iDim < nDim; iDim++)
     val_Proj_Jac_Tensor[nSpecies+nDim+1][nSpecies+iDim] = rhoEve/rho*val_normal[iDim];
   val_Proj_Jac_Tensor[nSpecies+nDim+1][nSpecies+nDim+1] = proj_vel;
 
-  for (unsigned short iVar = 0; iVar < nVar; iVar++)
-    for (unsigned short jVar = 0; jVar < nVar; jVar++)
+  for (auto iVar = 0ul; iVar < nVar; iVar++)
+    for (auto jVar = 0ul; jVar < nVar; jVar++)
       val_Proj_Jac_Tensor[iVar][jVar] = val_scale * val_Proj_Jac_Tensor[iVar][jVar];
 }
 
@@ -240,17 +238,17 @@ void CNEMONumerics::GetViscousProjFlux(const su2double *val_primvar,
   su2activematrix Flux_Tensor(nVar,nDim);
 
   /*--- Initialize ---*/
-  for (auto iVar = 0; iVar < nVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
     Proj_Flux_Tensor[iVar] = 0.0;
-    for (auto iDim = 0; iDim < nDim; iDim++)
+    for (auto iDim = 0ul; iDim < nDim; iDim++)
       Flux_Tensor[iVar][iDim] = 0.0;
   }
 
   /*--- Rename variables for convenience ---*/
   const auto& Ds  = val_diffusioncoeff;
   const su2double mu  = val_lam_viscosity+val_eddy_viscosity;
-  su2double ktr = val_therm_conductivity;
-  su2double kve = val_therm_conductivity_ve;
+  const su2double ktr = val_therm_conductivity;
+  const su2double kve = val_therm_conductivity_ve;
   const su2double rho = val_primvar[RHO_INDEX];
   const su2double T = val_primvar[T_INDEX];
   const su2double Tve = val_primvar[TVE_INDEX];
@@ -260,8 +258,8 @@ void CNEMONumerics::GetViscousProjFlux(const su2double *val_primvar,
 
   /*--- Pre-compute mixture quantities ---*/  //TODO
   su2double Vector[MAXNDIM] = {0.0};
-  for (auto iDim = 0; iDim < nDim; iDim++) {
-    for (auto iSpecies = 0; iSpecies < nHeavy; iSpecies++) {
+  for (auto iDim = 0ul; iDim < nDim; iDim++) {
+    for (auto iSpecies = 0ul; iSpecies < nHeavy; iSpecies++) {
       Vector[iDim] += rho*Ds[iSpecies]*GV[RHOS_INDEX+iSpecies][iDim];
     }
   }
@@ -270,23 +268,23 @@ void CNEMONumerics::GetViscousProjFlux(const su2double *val_primvar,
   ComputeStressTensor(nDim,tau,val_gradprimvar+VEL_INDEX, mu);
 
   /*--- Populate entries in the viscous flux vector ---*/
-  for (auto iDim = 0; iDim < nDim; iDim++) {
+  for (auto iDim = 0ul; iDim < nDim; iDim++) {
 
     /*--- Species diffusion velocity ---*/
-    for (auto iSpecies = 0; iSpecies < nHeavy; iSpecies++) {
+    for (auto iSpecies = 0ul; iSpecies < nHeavy; iSpecies++) {
       Flux_Tensor[iSpecies][iDim] = rho*Ds[iSpecies]*GV[RHOS_INDEX+iSpecies][iDim]
           - V[RHOS_INDEX+iSpecies]*Vector[iDim];
     }
 
     /*--- Shear-stress/momentum related terms ---*/
     Flux_Tensor[nSpecies+nDim][iDim] = 0.0;
-    for (auto jDim = 0; jDim < nDim; jDim++) {
+    for (auto jDim = 0ul; jDim < nDim; jDim++) {
       Flux_Tensor[nSpecies+jDim][iDim]  = tau[iDim][jDim];
       Flux_Tensor[nSpecies+nDim][iDim] += tau[iDim][jDim]*val_primvar[VEL_INDEX+jDim];
     }
 
     /*--- Diffusion terms ---*/
-    for (auto iSpecies = 0; iSpecies < nHeavy; iSpecies++) {
+    for (auto iSpecies = 0ul; iSpecies < nHeavy; iSpecies++) {
       Flux_Tensor[nSpecies+nDim][iDim]   += Flux_Tensor[iSpecies][iDim] * hs[iSpecies];
       Flux_Tensor[nSpecies+nDim+1][iDim] += Flux_Tensor[iSpecies][iDim] * val_eve[iSpecies];
     }
@@ -296,8 +294,8 @@ void CNEMONumerics::GetViscousProjFlux(const su2double *val_primvar,
     Flux_Tensor[nSpecies+nDim+1][iDim] += kve*GV[TVE_INDEX][iDim];
   }
 
-  for (auto iVar = 0; iVar < nVar; iVar++) {
-    for (auto iDim = 0; iDim < nDim; iDim++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
+    for (auto iDim = 0ul; iDim < nDim; iDim++) {
       Proj_Flux_Tensor[iVar] += Flux_Tensor[iVar][iDim]*val_normal[iDim];
     }
   }
@@ -356,32 +354,27 @@ void CNEMONumerics::GetPMatrix(const su2double *U, const su2double *V, const su2
                                const su2double *val_normal, const su2double *l, const su2double *m,
                                su2double **val_p_tensor) const {
 
-  // P matrix is equivalent to the L matrix in Gnoffo
-  unsigned short iSpecies, iDim, iVar, jVar;
-  su2double sqvel, rho, a, a2, eve;
-  su2double vU, vV, vW;
-
   /*--- Initialize the P matrix to zero ---*/
-  for (iVar = 0; iVar < nVar; iVar++)
-    for (jVar = 0; jVar < nVar; jVar++)
+  for (auto iVar = 0ul; iVar < nVar; iVar++)
+    for (auto jVar = 0ul; jVar < nVar; jVar++)
       val_p_tensor[iVar][jVar] = 0.0;
 
   /*--- Pre-compute useful quantities ---*/
-  sqvel = 0.0;
-  rho = V[RHO_INDEX];
-  eve = U[nSpecies+nDim+1]/rho;
-  vU = 0.0;  vV = 0.0;  vW = 0.0;
-  for (iDim = 0; iDim < nDim; iDim++) {
+  su2double sqvel = 0.0;
+  const su2double rho = V[RHO_INDEX];
+  const su2double eve = U[nSpecies+nDim+1]/rho;
+  su2double vU = vV = vW = 0.0;
+  for (auto iDim = 0ul; iDim < nDim; iDim++) {
     vU    += V[VEL_INDEX+iDim] * val_normal[iDim];
     vV    += V[VEL_INDEX+iDim] * l[iDim];
     vW    += V[VEL_INDEX+iDim] * m[iDim];
     sqvel += V[VEL_INDEX+iDim] * V[VEL_INDEX+iDim];
   }
-  a  = V[A_INDEX];
-  a2 = V[A_INDEX]*V[A_INDEX];
+  const su2double a  = V[A_INDEX];
+  const su2double a2 = V[A_INDEX]*V[A_INDEX];
 
   if(nDim == 2) {
-    for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
+    for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
       val_p_tensor[iSpecies][iSpecies]   += 1.0/a2;
       val_p_tensor[iSpecies][nSpecies]   += 0.0;
       val_p_tensor[iSpecies][nSpecies+1] += V[RHOS_INDEX+iSpecies] / (2.0*rho*a2);
@@ -395,7 +388,7 @@ void CNEMONumerics::GetPMatrix(const su2double *U, const su2double *V, const su2
       val_p_tensor[nSpecies+3][iSpecies] += 0.0;
     }
 
-    for (iDim = 0; iDim < nDim; iDim++){
+    for (auto iDim = 0ul; iDim < nDim; iDim++){
       val_p_tensor[nSpecies+iDim][nSpecies]     += l[iDim];
       val_p_tensor[nSpecies+iDim][nSpecies+1]   += (V[VEL_INDEX+iDim]+a*val_normal[iDim]) / (2.0*a2);
       val_p_tensor[nSpecies+iDim][nSpecies+2]   += (V[VEL_INDEX+iDim]-a*val_normal[iDim]) / (2.0*a2);
@@ -414,7 +407,7 @@ void CNEMONumerics::GetPMatrix(const su2double *U, const su2double *V, const su2
 
   } else {
 
-    for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
+    for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
       val_p_tensor[iSpecies][iSpecies]   = 1.0/a2;
       val_p_tensor[iSpecies][nSpecies]   = 0.0;
       val_p_tensor[iSpecies][nSpecies+1] = 0.0;
@@ -430,7 +423,7 @@ void CNEMONumerics::GetPMatrix(const su2double *U, const su2double *V, const su2
       val_p_tensor[nSpecies+4][iSpecies] = 0.0;
     }
 
-    for (iDim = 0; iDim < nDim; iDim++){
+    for (auto iDim = 0ul; iDim < nDim; iDim++){
       val_p_tensor[nSpecies+iDim][nSpecies]     = l[iDim];
       val_p_tensor[nSpecies+iDim][nSpecies+1]   = m[iDim];
       val_p_tensor[nSpecies+iDim][nSpecies+2]   = (V[VEL_INDEX+iDim]+a*val_normal[iDim]) / (2.0*a2);
@@ -456,30 +449,26 @@ void CNEMONumerics::GetPMatrix_inv(const su2double *U, const su2double *V, const
                                    const su2double *val_normal, const su2double *l, const su2double *m,
                                    su2double **val_invp_tensor) const {
 
-  unsigned short iSpecies, jSpecies, iDim, iVar, jVar;
-  su2double rho, a, a2, eve;
-  su2double vU, vV, vW;
-
-  for (iVar = 0; iVar < nVar; iVar++)
-    for (jVar = 0; jVar < nVar; jVar++)
+  for (auto iVar = 0ul; iVar < nVar; iVar++)
+    for (auto jVar = 0ul; jVar < nVar; jVar++)
       val_invp_tensor[iVar][jVar] = 0.0;
 
   /*--- Pre-compute useful quantities ---*/
-  rho = V[RHO_INDEX];
-  eve = U[nSpecies+nDim+1]/rho;
-  vU = 0.0;  vV = 0.0;  vW = 0.0;
-  for (iDim = 0; iDim < nDim; iDim++) {
+  const su2double rho = V[RHO_INDEX];
+  const su2double eve = U[nSpecies+nDim+1]/rho;
+  su2double vU = vV = vW = 0.0;
+  for (auto iDim = 0ul; iDim < nDim; iDim++) {
     vU += V[VEL_INDEX+iDim] * val_normal[iDim];
     vV += V[VEL_INDEX+iDim] * l[iDim];
     vW += V[VEL_INDEX+iDim] * m[iDim];
   }
-  a  = V[A_INDEX];
-  a2 = V[A_INDEX]*V[A_INDEX];
+  const su2double a  = V[A_INDEX];
+  const su2double a2 = V[A_INDEX]*V[A_INDEX];
 
   if (nDim == 2) {
 
-    for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
-      for (jSpecies = 0; jSpecies < nSpecies; jSpecies++) {
+    for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
+      for (auto jSpecies = 0ul; jSpecies < nSpecies; jSpecies++) {
         val_invp_tensor[iSpecies][jSpecies] += -(V[RHOS_INDEX+iSpecies]/rho) * val_dPdU[jSpecies];
       }
       val_invp_tensor[iSpecies][iSpecies]   += a2;
@@ -516,8 +505,8 @@ void CNEMONumerics::GetPMatrix_inv(const su2double *U, const su2double *V, const
 
   } else {
 
-    for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
-      for (jSpecies = 0; jSpecies < nSpecies; jSpecies++) {
+    for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
+      for (auto jSpecies = 0ul; jSpecies < nSpecies; jSpecies++) {
         val_invp_tensor[iSpecies][jSpecies] += -(V[RHOS_INDEX+iSpecies]/rho) * val_dPdU[jSpecies];
       }
       val_invp_tensor[iSpecies][iSpecies]   += a2;
diff --git a/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp b/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
index bb9874c1c06..7f5b10f16a1 100644
--- a/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
+++ b/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
@@ -37,7 +37,7 @@ CAvgGrad_NEMO::CAvgGrad_NEMO(unsigned short val_nDim,
                                                               val_nPrimVar, val_nPrimVarGrad,
                                                               config) {
 
-  /*--- Compressible flow, primitive variables nDim+3, (T,vx,vy,vz,P,rho) ---*/
+  /*--- Compressible flow, primitive variables ---*/
   PrimVar_i    = new su2double [nPrimVar];
   PrimVar_j    = new su2double [nPrimVar];
   Mean_PrimVar = new su2double [nPrimVar];
@@ -49,23 +49,24 @@ CAvgGrad_NEMO::CAvgGrad_NEMO(unsigned short val_nDim,
   Mean_Eve    = new su2double[nSpecies];
   Mean_Cvve   = new su2double[nSpecies];
   Mean_GU     = new su2double*[nVar];
-  for (auto iVar = 0; iVar < nVar; iVar++)
+  for (auto iVar = 0ul; iVar < nVar; iVar++)
     Mean_GU[iVar] = new su2double[nDim];
 
   Mean_Diffusion_Coeff = new su2double[nSpecies];
 
-  /*--- Compressible flow, primitive gradient variables nDim+3, (T,vx,vy,vz) ---*/
+  /*--- Compressible flow, primitive gradient variables ---*/
   Mean_GradPrimVar = new su2double* [nPrimVarGrad];
-  for (auto iVar = 0; iVar < nPrimVarGrad; iVar++)
+  for (auto iVar = 0ul; iVar < nPrimVarGrad; iVar++)
     Mean_GradPrimVar[iVar] = new su2double [nDim];
 
   Flux   = new su2double[nVar];
   Jacobian_i = new su2double* [nVar];
   Jacobian_j = new su2double* [nVar];
-  for (auto iVar = 0; iVar < nVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
     Jacobian_i[iVar] = new su2double [nVar];
     Jacobian_j[iVar] = new su2double [nVar];
   }
+
 }
 
 CAvgGrad_NEMO::~CAvgGrad_NEMO(void) {
@@ -81,23 +82,24 @@ CAvgGrad_NEMO::~CAvgGrad_NEMO(void) {
   delete [] Mean_dTvedU;
   delete [] Mean_Eve;
   delete [] Mean_Cvve;
-  for (auto iVar = 0; iVar < nVar; iVar++)
+  for (auto iVar = 0ul; iVar < nVar; iVar++)
     delete [] Mean_GU[iVar];
   delete [] Mean_GU;
 
-  for (auto iVar = 0; iVar < nPrimVarGrad; iVar++)
+  for (auto iVar = 0ul; iVar < nPrimVarGrad; iVar++)
     delete [] Mean_GradPrimVar[iVar];
   delete [] Mean_GradPrimVar;
   delete [] Flux;
 
   if (Jacobian_i != nullptr) {
-    for (auto iVar = 0; iVar < nVar; iVar++) {
+    for (auto iVar = 0ul; iVar < nVar; iVar++) {
       delete [] Jacobian_i[iVar];
       delete [] Jacobian_j[iVar];
     }
     delete [] Jacobian_i;
     delete [] Jacobian_j;
   }
+
 }
 
 CNumerics::ResidualType<> CAvgGrad_NEMO::ComputeResidual(const CConfig *config) {
@@ -105,11 +107,11 @@ CNumerics::ResidualType<> CAvgGrad_NEMO::ComputeResidual(const CConfig *config)
   /*--- Normalized normal vector ---*/
   Area = GeometryToolbox::Norm(nDim, Normal);
 
-  for (auto iDim = 0; iDim < nDim; iDim++)
+  for (auto iDim = 0ul; iDim < nDim; iDim++)
     UnitNormal[iDim] = Normal[iDim]/Area;
 
   /*--- Mean transport coefficients ---*/
-  for (auto iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
     Mean_Diffusion_Coeff[iSpecies] = 0.5*(Diffusion_Coeff_i[iSpecies] +
                                           Diffusion_Coeff_j[iSpecies]);
   Mean_Laminar_Viscosity           = 0.5*(Laminar_Viscosity_i +
@@ -123,11 +125,11 @@ CNumerics::ResidualType<> CAvgGrad_NEMO::ComputeResidual(const CConfig *config)
 
   /*--- Mean gradient approximation ---*/
   // Mass fraction
-  for (auto iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
     PrimVar_i[iSpecies] = V_i[iSpecies]/V_i[RHO_INDEX];
     PrimVar_j[iSpecies] = V_j[iSpecies]/V_j[RHO_INDEX];
     Mean_PrimVar[iSpecies] = 0.5*(PrimVar_i[iSpecies] + PrimVar_j[iSpecies]);
-    for (auto iDim = 0; iDim < nDim; iDim++) {
+    for (auto iDim = 0ul; iDim < nDim; iDim++) {
       Mean_GradPrimVar[iSpecies][iDim] = 0.5*(1.0/V_i[RHO_INDEX] * (PrimVar_Grad_i[iSpecies][iDim] -
                                               PrimVar_i[iSpecies] * PrimVar_Grad_i[RHO_INDEX][iDim]) +
                                               1.0/V_j[RHO_INDEX] * (PrimVar_Grad_j[iSpecies][iDim] -
@@ -146,7 +148,7 @@ CNumerics::ResidualType<> CAvgGrad_NEMO::ComputeResidual(const CConfig *config)
                                           PrimVar_Grad_j[iVar][iDim]);
     }
   }
-  for (auto iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
     Mean_Eve[iSpecies]  = 0.5*(eve_i[iSpecies]  + eve_j[iSpecies]);
     Mean_Cvve[iSpecies] = 0.5*(Cvve_i[iSpecies] + Cvve_j[iSpecies]);
   }
@@ -159,18 +161,18 @@ CNumerics::ResidualType<> CAvgGrad_NEMO::ComputeResidual(const CConfig *config)
 
 
   /*--- Update viscous residual ---*/
-  for (auto iVar = 0; iVar < nVar; iVar++)
+  for (auto iVar = 0ul; iVar < nVar; iVar++)
     Flux[iVar] = Proj_Flux_Tensor[iVar];
 
   /*--- Compute the implicit part ---*/
   if (implicit) {
-    dist_ij = 0.0;
-    for (auto iDim = 0; iDim < nDim; iDim++)
-      dist_ij += (Coord_j[iDim]-Coord_i[iDim])*(Coord_j[iDim]-Coord_i[iDim]);
-    dist_ij = sqrt(dist_ij);
 
-    for (auto iVar = 0; iVar < nVar; iVar++) {
-      for (auto jVar = 0; jVar < nVar; jVar++) {
+  su2double dist_ij_2[nDim] = {0.0};
+  GeometryToolbox::Distance(nDim, coord_j, coord_i, dist_ij_2);    
+  dist_ij = GeometryToolbox::SquaredNorm(nDim, dist_ij_2);
+
+    for (auto iVar = 0ul; iVar < nVar; iVar++) {
+      for (auto jVar = 0ul; jVar < nVar; jVar++) {
         Jacobian_i[iVar][jVar] = 0.0;
         Jacobian_j[iVar][jVar] = 0.0;
       }
@@ -183,6 +185,7 @@ CNumerics::ResidualType<> CAvgGrad_NEMO::ComputeResidual(const CConfig *config)
   }
 
   return ResidualType<>(Flux, Jacobian_i, Jacobian_j);
+
 }
 
 CAvgGradCorrected_NEMO::CAvgGradCorrected_NEMO(unsigned short val_nDim,
@@ -200,7 +203,7 @@ CAvgGradCorrected_NEMO::CAvgGradCorrected_NEMO(unsigned short val_nDim,
   nPrimVar     = val_nPrimVar;
   nPrimVarGrad = val_nPrimVarGrad;
 
-  /*--- Compressible flow, primitive variables nDim+3, (T,vx,vy,vz,P,rho) ---*/
+  /*--- Compressible flow, primitive variables ---*/
   PrimVar_i    = new su2double [nPrimVar];
   PrimVar_j    = new su2double [nPrimVar];
   Mean_PrimVar = new su2double [nPrimVar];
@@ -210,9 +213,9 @@ CAvgGradCorrected_NEMO::CAvgGradCorrected_NEMO(unsigned short val_nDim,
 
   Mean_Diffusion_Coeff = new su2double[nSpecies];
 
-  /*--- Compressible flow, primitive gradient variables nDim+3, (T,vx,vy,vz) ---*/
+  /*--- Compressible flow, primitive gradient variables ---*/
   Mean_GradPrimVar = new su2double* [nPrimVarGrad];
-  for (auto iVar = 0; iVar < nPrimVarGrad; iVar++)
+  for (auto iVar = 0ul; iVar < nPrimVarGrad; iVar++)
     Mean_GradPrimVar[iVar] = new su2double [nDim];
 
   Proj_Mean_GradPrimVar_Edge = new su2double[nPrimVarGrad];
@@ -220,10 +223,11 @@ CAvgGradCorrected_NEMO::CAvgGradCorrected_NEMO(unsigned short val_nDim,
   Flux   = new su2double[nVar];
   Jacobian_i = new su2double* [nVar];
   Jacobian_j = new su2double* [nVar];
-  for (auto iVar = 0; iVar < nVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
     Jacobian_i[iVar] = new su2double [nVar];
     Jacobian_j[iVar] = new su2double [nVar];
   }
+
 }
 
 CAvgGradCorrected_NEMO::~CAvgGradCorrected_NEMO(void) {
@@ -237,7 +241,7 @@ CAvgGradCorrected_NEMO::~CAvgGradCorrected_NEMO(void) {
 
   delete [] Mean_Diffusion_Coeff;
 
-  for (auto iVar = 0; iVar < nPrimVarGrad; iVar++)
+  for (auto iVar = 0ul; iVar < nPrimVarGrad; iVar++)
     delete [] Mean_GradPrimVar[iVar];
   delete [] Mean_GradPrimVar;
 
@@ -246,13 +250,14 @@ CAvgGradCorrected_NEMO::~CAvgGradCorrected_NEMO(void) {
   delete [] Flux;
 
   if (Jacobian_i != nullptr) {
-    for (auto iVar = 0; iVar < nVar; iVar++) {
+    for (auto iVar = 0ul; iVar < nVar; iVar++) {
       delete [] Jacobian_i[iVar];
       delete [] Jacobian_j[iVar];
     }
   delete [] Jacobian_i;
   delete [] Jacobian_j;
   }
+
 }
 
 CNumerics::ResidualType<> CAvgGradCorrected_NEMO::ComputeResidual(const CConfig *config) {
@@ -260,23 +265,23 @@ CNumerics::ResidualType<> CAvgGradCorrected_NEMO::ComputeResidual(const CConfig
   /*--- Normalized normal vector ---*/
   Area = GeometryToolbox::Norm(nDim, Normal);
 
-  for (auto iDim = 0; iDim < nDim; iDim++)
+  for (auto iDim = 0ul; iDim < nDim; iDim++)
     UnitNormal[iDim] = Normal[iDim]/Area;
 
   /*--- Compute vector going from iPoint to jPoint ---*/
-  for (auto iDim = 0; iDim < nDim; iDim++) {
+  for (auto iDim = 0ul; iDim < nDim; iDim++) {
     Edge_Vector[iDim] = Coord_j[iDim]-Coord_i[iDim];
   }
-  su2double dist_ij_2 = GeometryToolbox::SquaredNorm(nDim, Edge_Vector);
+  const su2double dist_ij_2 = GeometryToolbox::SquaredNorm(nDim, Edge_Vector);
 
   /*--- Make a local copy of the primitive variables ---*/
   // NOTE: We are transforming the species density terms to species mass fractions
   // Mass fraction
-  for (auto iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
     PrimVar_i[iSpecies] = V_i[iSpecies]/V_i[RHO_INDEX];
     PrimVar_j[iSpecies] = V_j[iSpecies]/V_j[RHO_INDEX];
     Mean_PrimVar[iSpecies] = 0.5*(PrimVar_i[iSpecies] + PrimVar_j[iSpecies]);
-    for (auto iDim = 0; iDim < nDim; iDim++) {
+    for (auto iDim = 0ul; iDim < nDim; iDim++) {
       Mean_GradPrimVar[iSpecies][iDim] = 0.5*(1.0/V_i[RHO_INDEX] *
                                               (PrimVar_Grad_i[iSpecies][iDim] -
                                                PrimVar_i[iSpecies] *
@@ -293,18 +298,18 @@ CNumerics::ResidualType<> CAvgGradCorrected_NEMO::ComputeResidual(const CConfig
     Mean_PrimVar[iVar] = 0.5*(PrimVar_i[iVar]+PrimVar_j[iVar]);
   }
   for (auto iVar = nSpecies; iVar < nPrimVarGrad; iVar++) {
-    for (auto iDim = 0; iDim < nDim; iDim++) {
+    for (auto iDim = 0ul; iDim < nDim; iDim++) {
       Mean_GradPrimVar[iVar][iDim] = 0.5*(PrimVar_Grad_i[iVar][iDim] +
                                           PrimVar_Grad_j[iVar][iDim]);
     }
   }
-  for (auto iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
     Mean_Eve[iSpecies]  = 0.5*(eve_i[iSpecies]  + eve_j[iSpecies]);
     Mean_Cvve[iSpecies] = 0.5*(Cvve_i[iSpecies] + Cvve_j[iSpecies]);
   }
 
   /*--- Mean transport coefficients ---*/
-  for (auto iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
     Mean_Diffusion_Coeff[iSpecies] = 0.5*(Diffusion_Coeff_i[iSpecies] +
                                           Diffusion_Coeff_j[iSpecies]);
   Mean_Laminar_Viscosity           = 0.5*(Laminar_Viscosity_i +
@@ -317,9 +322,9 @@ CNumerics::ResidualType<> CAvgGradCorrected_NEMO::ComputeResidual(const CConfig
                                           Thermal_Conductivity_ve_j);
 
   /*--- Projection of the mean gradient in the direction of the edge ---*/
-  for (auto iVar = 0; iVar < nPrimVarGrad; iVar++) {
+  for (auto iVar = 0ul; iVar < nPrimVarGrad; iVar++) {
     Proj_Mean_GradPrimVar_Edge[iVar] = GeometryToolbox::DotProduct(nDim, Mean_GradPrimVar[iVar], Edge_Vector);
-    for (auto iDim = 0; iDim < nDim; iDim++) {
+    for (auto iDim = 0ul; iDim < nDim; iDim++) {
       Mean_GradPrimVar[iVar][iDim] -= (Proj_Mean_GradPrimVar_Edge[iVar] -
                                        (PrimVar_j[iVar]-PrimVar_i[iVar]))*Edge_Vector[iDim] / dist_ij_2;
     }
@@ -335,14 +340,14 @@ CNumerics::ResidualType<> CAvgGradCorrected_NEMO::ComputeResidual(const CConfig
                      config);
 
   /*--- Update viscous residual ---*/
-  for (auto iVar = 0; iVar < nVar; iVar++)
+  for (auto iVar = 0ul; iVar < nVar; iVar++)
     Flux[iVar] = Proj_Flux_Tensor[iVar];
 
   /*--- Compute the implicit part ---*/
   if (implicit) {
     dist_ij = sqrt(dist_ij_2);
 
-    for (auto iVar = 0; iVar < nVar; iVar++) {
+    for (auto iVar = 0ul; iVar < nVar; iVar++) {
       for (unsigned short jVar = 0; jVar < nVar; jVar++) {
         Jacobian_i[iVar][jVar] = 0.0;
         Jacobian_j[iVar][jVar] = 0.0;
@@ -357,4 +362,5 @@ CNumerics::ResidualType<> CAvgGradCorrected_NEMO::ComputeResidual(const CConfig
   }
 
   return ResidualType<>(Flux, Jacobian_j, Jacobian_j);
+
 }
diff --git a/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp b/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp
index 26a476f4672..1406749e1dd 100644
--- a/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp
+++ b/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp
@@ -35,36 +35,32 @@ CSource_NEMO::CSource_NEMO(unsigned short val_nDim,
                            CConfig *config) : CNEMONumerics(val_nDim, val_nVar, val_nPrimVar, val_nPrimVarGrad,
                                                           config) {
 
-  unsigned short iSpecies;
-
   /*--- Allocate arrays ---*/
   Y = new su2double[nSpecies];
 
   dYdr = new su2double*[nSpecies];
-  for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
     dYdr[iSpecies] = new su2double[nSpecies];
   }
 
   residual = new su2double[nVar]();
   jacobian = new su2double* [nVar];
-  for(unsigned short iVar = 0; iVar < nVar; ++iVar)
+  for(auto iVar = 0ul; iVar < nVar; ++iVar)
     jacobian[iVar] = new su2double [nVar]();
-
 }
 
 CSource_NEMO::~CSource_NEMO(void) {
-  unsigned short iSpecies;
 
   /*--- Deallocate arrays ---*/
 
-  for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
     delete [] dYdr[iSpecies];
   delete [] dYdr;
   delete [] Y;
 
   delete [] residual;
   if (jacobian) {
-    for(unsigned short iVar = 0; iVar < nVar; ++iVar)
+    for(auto iVar = 0ul; iVar < nVar; ++iVar)
       delete [] jacobian[iVar];
     delete [] jacobian;
   }
@@ -73,25 +69,22 @@ CSource_NEMO::~CSource_NEMO(void) {
 CNumerics::ResidualType<> CSource_NEMO::ComputeChemistry(const CConfig *config) {
 
   /*--- Nonequilibrium chemistry ---*/
-  unsigned short iSpecies, iVar;
-  unsigned short jVar;
-
   vector<su2double> rhos;
   rhos.resize(nSpecies,0.0);
 
   /*--- Initialize residual and Jacobian arrays ---*/
-  for (iVar = 0; iVar < nVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++)
     residual[iVar] = 0.0;
-  }
+
   if (implicit)
-    for (iVar = 0; iVar < nVar; iVar++)
-      for (jVar = 0; jVar < nVar; jVar++)
+    for (auto iVar = 0ul; iVar < nVar; iVar++)
+      for (auto jVar = 0ul; jVar < nVar; jVar++)
         jacobian[iVar][jVar] = 0.0;
 
   /*--- Rename for convenience ---*/
-  su2double T   = V_i[T_INDEX];
+  su2double T = V_i[T_INDEX];
   su2double Tve = V_i[TVE_INDEX];
-  for(iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
     rhos[iSpecies]=V_i[RHOS_INDEX+iSpecies];
 
   /*--- Set mixture state ---*/
@@ -101,12 +94,12 @@ CNumerics::ResidualType<> CSource_NEMO::ComputeChemistry(const CConfig *config)
   const auto& ws = fluidmodel->ComputeNetProductionRates(implicit, V_i, eve_i, Cvve_i,
                                                          dTdU_i, dTvedU_i, jacobian);
 
-  for (iSpecies = 0; iSpecies < nSpecies; iSpecies++){
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++){
     residual[iSpecies] = ws[iSpecies] * Volume;}
 
   if (implicit) {
-    for (iVar = 0; iVar<nVar; iVar++) {
-      for (jVar = 0; jVar<nVar; jVar++) {
+    for (auto iVar = 0ul; iVar<nVar; iVar++) {
+      for (auto jVar = 0ul; jVar<nVar; jVar++) {
         jacobian[iVar][jVar] *= Volume;
       }
     }
@@ -123,35 +116,33 @@ CNumerics::ResidualType<> CSource_NEMO::ComputeVibRelaxation(const CConfig *conf
   // Note: Landau-Teller formulation
   // Note: Millikan & White relaxation time (requires P in Atm.)
   // Note: Park limiting cross section
-  unsigned short iSpecies, iVar;
-  unsigned short jVar;
-  su2double res_min = -1E6;
-  su2double res_max = 1E6;
+  const su2double res_min = -1E6;
+  const su2double res_max = 1E6;
 
   vector<su2double> rhos;
   rhos.resize(nSpecies,0.0);
 
   /*--- Initialize residual and Jacobian arrays ---*/
-  for (iVar = 0; iVar < nVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
     residual[iVar] = 0.0;
   }
   if (implicit) {
-    for (iVar = 0; iVar < nVar; iVar++)
-      for (jVar = 0; jVar < nVar; jVar++)
+    for (auto iVar = 0ul; iVar < nVar; iVar++)
+      for (auto jVar = 0ul; jVar < nVar; jVar++)
         jacobian[iVar][jVar] = 0.0;
   }
 
   /*--- Rename for convenience ---*/
-  su2double T   = V_i[T_INDEX];
-  su2double Tve = V_i[TVE_INDEX];
-  for(iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+  const su2double T = V_i[T_INDEX];
+  const su2double Tve = V_i[TVE_INDEX];
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
     rhos[iSpecies]=V_i[RHOS_INDEX+iSpecies];
 
   /*--- Set fluid state ---*/
   fluidmodel->SetTDStateRhosTTv(rhos, T, Tve);
 
   /*--- Compute residual and jacobians ---*/
-  su2double VTterm = fluidmodel -> ComputeEveSourceTerm();
+  const su2double VTterm = fluidmodel -> ComputeEveSourceTerm();
   if (implicit) {
     fluidmodel->GetEveSourceTermJacobian(V_i, eve_i, Cvve_i, dTdU_i,
                                          dTvedU_i, jacobian);
@@ -160,17 +151,17 @@ CNumerics::ResidualType<> CSource_NEMO::ComputeVibRelaxation(const CConfig *conf
   residual[nSpecies+nDim+1] = VTterm * Volume;
 
   if (implicit) {
-    for (iVar = 0; iVar<nVar; iVar++) {
-      for (jVar = 0; jVar<nVar; jVar++) {
+    for (auto iVar = 0ul; iVar<nVar; iVar++) {
+      for (auto jVar = 0ul; jVar<nVar; jVar++) {
         jacobian[iVar][jVar] *= Volume;
       }
     }
   }
 
   /*--- Relax/limit vt transfer ---*/
-  if(config->GetVTTransferResidualLimiting()){
-    if(residual[nSpecies+nDim+1]>res_max) residual[nSpecies+nDim+1]=res_max;
-    if(residual[nSpecies+nDim+1]<res_min) residual[nSpecies+nDim+1]=res_min;
+  if (config->GetVTTransferResidualLimiting()) {
+    if (residual[nSpecies+nDim+1]>res_max) residual[nSpecies+nDim+1]=res_max;
+    if (residual[nSpecies+nDim+1]<res_min) residual[nSpecies+nDim+1]=res_min;
   }
 
   return ResidualType<>(residual, jacobian, nullptr);
@@ -178,31 +169,26 @@ CNumerics::ResidualType<> CSource_NEMO::ComputeVibRelaxation(const CConfig *conf
 
 CNumerics::ResidualType<> CSource_NEMO::ComputeAxisymmetric(const CConfig *config) {
 
-  unsigned short iDim, iSpecies, iVar;
-  unsigned short jSpecies, jVar;
-
   /*--- Rename for convenience ---*/
-  auto Ds = Diffusion_Coeff_i;
-  auto GV = PrimVar_Grad_i;
-  su2double ktr = Thermal_Conductivity_i;
-  su2double kve = Thermal_Conductivity_ve_i;
-  su2double rho = V_i[RHO_INDEX];
-  su2double RuSI = UNIVERSAL_GAS_CONSTANT;
-  su2double Ru = 1000.0*RuSI;
-  su2double rhou = U_i[nSpecies];
-  su2double rhov = U_i[nSpecies+1];
-  su2double H = V_i[H_INDEX];
-  su2double rhoEve = U_i[nVar-1];
+  const auto Ds = Diffusion_Coeff_i;
+  const auto GV = PrimVar_Grad_i;
+  const su2double ktr = Thermal_Conductivity_i;
+  const su2double kve = Thermal_Conductivity_ve_i;
+  const su2double rho = V_i[RHO_INDEX];
+  const su2double RuSI = UNIVERSAL_GAS_CONSTANT;
+  const su2double Ru = 1000.0*RuSI;
+  const su2double rhou = U_i[nSpecies];
+  const su2double rhov = U_i[nSpecies+1];
+  const su2double H = V_i[H_INDEX];
+  const su2double rhoEve = U_i[nVar-1];
   const auto& Ms = fluidmodel->GetSpeciesMolarMass();
   const auto& hs = fluidmodel->ComputeSpeciesEnthalpy(V_i[T_INDEX], V_i[TVE_INDEX], eve_i );
 
-  bool viscous = config->GetViscous();
-  bool rans = (config->GetKind_Turb_Model() != TURB_MODEL::NONE);
+  const bool viscous = config->GetViscous();
+  const bool rans = (config->GetKind_Turb_Model() != TURB_MODEL::NONE);
 
   /*--- Initialize residual and Jacobian arrays ---*/
-  for (iVar = 0; iVar < nVar; iVar++) {
-    residual[iVar] = 0.0;
-  }
+  for (auto iVar = 0ul; iVar < nVar; iVar++) residual[iVar] = 0.0;
 
   /*--- Calculate inverse of y coordinate ---*/
   su2double yinv = 0.0;
@@ -210,34 +196,34 @@ CNumerics::ResidualType<> CSource_NEMO::ComputeAxisymmetric(const CConfig *confi
   else yinv = 0.0;
 
   /*--- Rename for convenience ---*/
-  su2double vel2 = 0.0;
-  for (iDim = 0; iDim < nDim; iDim++)
-    vel2 += V_i[VEL_INDEX+iDim]*V_i[VEL_INDEX+iDim];
-  for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+  const su2double vel2 = GeometryToolbox::SquaredNorm(nDim, &V_i[VEL_INDEX]);
+
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
     Y[iSpecies] = V_i[RHOS_INDEX+iSpecies] / rho;
 
   /*--- Compute residual for inviscid axisym flow---*/
-  for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
     residual[iSpecies] = yinv*rhov*Y[iSpecies]*Volume;
-  residual[nSpecies]   = yinv*rhov*U_i[nSpecies]/rho*Volume;
-  residual[nSpecies+1] = yinv*rhov*U_i[nSpecies+1]/rho*Volume;
+  residual[nSpecies]   = yinv*rhov*rhou/rho*Volume;
+  residual[nSpecies+1] = yinv*rhov*rhov/rho*Volume;
   residual[nSpecies+2] = yinv*rhov*H*Volume;
-  residual[nSpecies+3] = yinv*rhov*U_i[nSpecies+nDim+1]/rho*Volume;
+  residual[nSpecies+3] = yinv*rhov*rhoEve/rho*Volume;
 
   /*---Compute Jacobian for inviscid axisym flow ---*/
   if (implicit) {
 
-    /*--- Initialize ---*/
-    for (iVar = 0; iVar < nVar; iVar++)
-      for (jVar = 0; jVar < nVar; jVar++)
+    /*--- Initialize matrices ---*/
+    for (auto iVar = 0ul; iVar < nVar; iVar++)
+      for (auto jVar = 0ul; jVar < nVar; jVar++)
         jacobian[iVar][jVar] = 0.0;
-    for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
-      for (jSpecies = 0; jSpecies < nSpecies; jSpecies++)
+
+    for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
+      for (auto jSpecies = 0ul; jSpecies < nSpecies; jSpecies++)
         dYdr[iSpecies][jSpecies] = 0.0;
 
     /*--- Calculate additional quantities ---*/
-    for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
-      for (jSpecies = 0; jSpecies < nSpecies; jSpecies++) {
+    for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
+      for (auto jSpecies = 0ul; jSpecies < nSpecies; jSpecies++) {
         dYdr[iSpecies][jSpecies] += -1/rho*Y[iSpecies];
       }
       dYdr[iSpecies][iSpecies] += 1/rho;
@@ -246,26 +232,26 @@ CNumerics::ResidualType<> CSource_NEMO::ComputeAxisymmetric(const CConfig *confi
     /*--- Populate Jacobian ---*/
 
     // Species density
-    for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
-      for (jSpecies = 0; jSpecies < nSpecies; jSpecies++) {
+    for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
+      for (auto jSpecies = 0ul; jSpecies < nSpecies; jSpecies++) {
         jacobian[iSpecies][jSpecies] = dYdr[iSpecies][jSpecies]*rhov;
       }
       jacobian[iSpecies][nSpecies+1] = Y[iSpecies];
     }
 
     // X-momentum
-    for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+    for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
       jacobian[nSpecies][iSpecies] = -rhou*rhov/(rho*rho);
     jacobian[nSpecies][nSpecies]   = rhov/rho;
     jacobian[nSpecies][nSpecies+1] = rhou/rho;
 
     // Y-momentum
-    for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+    for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
      jacobian[nSpecies+1][iSpecies] = -rhov*rhov/(rho*rho);
     jacobian[nSpecies+1][nSpecies+1] = 2*rhov/rho;
 
     // Energy
-    for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+    for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
       jacobian[nSpecies+nDim][iSpecies]      = -H*rhov/rho + dPdU_i[iSpecies]*rhov/rho;
     jacobian[nSpecies+nDim][nSpecies]        = dPdU_i[nSpecies]*rhov/rho;
     jacobian[nSpecies+nDim][nSpecies+1]      = H + dPdU_i[nSpecies+1]*rhov/rho;
@@ -273,13 +259,13 @@ CNumerics::ResidualType<> CSource_NEMO::ComputeAxisymmetric(const CConfig *confi
     jacobian[nSpecies+nDim][nSpecies+nDim+1] = dPdU_i[nSpecies+nDim+1]*rhov/rho;
 
     // Vib-el energy
-    for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+    for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
       jacobian[nSpecies+nDim+1][iSpecies] = -rhoEve*rhov/(rho*rho);
     jacobian[nSpecies+nDim+1][nSpecies+1] = rhoEve/rho;
     jacobian[nSpecies+nDim+1][nSpecies+nDim+1] = rhov/rho;
 
-    for (iVar = 0; iVar < nVar; iVar++)
-      for (jVar = 0; jVar < nVar; jVar++)
+    for (auto iVar = 0ul; iVar < nVar; iVar++)
+      for (auto jVar = 0ul; jVar < nVar; jVar++)
         jacobian[iVar][jVar] *= yinv*Volume;
   }
 
@@ -288,31 +274,29 @@ CNumerics::ResidualType<> CSource_NEMO::ComputeAxisymmetric(const CConfig *confi
     if (!rans){ turb_ke_i = 0.0; }
 
     su2double Vector = 0.0;
-    for (iSpecies = 0; iSpecies < nHeavy; iSpecies++)
+    for (auto iSpecies = 0ul; iSpecies < nHeavy; iSpecies++)
       Vector += rho*Ds[iSpecies]*GV[RHOS_INDEX+iSpecies][1];
 
-    su2double sumJhs_y  = 0.0;
-    su2double sumJeve_y = 0.0;
-    su2double Mass      = 0.0;
-
-    for (iSpecies=0; iSpecies<nSpecies; iSpecies++)
+    su2double Mass = 0.0;
+    for (auto iSpecies=0ul; iSpecies<nSpecies; iSpecies++)
       Mass += V_i[iSpecies]/rho*Ms[iSpecies];
 
-    su2double heat_capacity_cp_i   = V_i[RHOCVTR_INDEX]/rho + Ru/Mass;
-    su2double total_viscosity_i    = Laminar_Viscosity_i + Eddy_Viscosity_i;
-    su2double total_conductivity_i = ktr + kve + heat_capacity_cp_i*Eddy_Viscosity_i/Prandtl_Turb;
-    su2double u                    = V_i[VEL_INDEX];
-    su2double v                    = V_i[VEL_INDEX+1];
-    su2double qy_t                 = -total_conductivity_i*GV[T_INDEX][1];
-    su2double qy_ve                = -kve*GV[TVE_INDEX][1];
+    const su2double heat_capacity_cp_i   = V_i[RHOCVTR_INDEX]/rho + Ru/Mass;
+    const su2double total_viscosity_i    = Laminar_Viscosity_i + Eddy_Viscosity_i;
+    const su2double total_conductivity_i = ktr + kve + heat_capacity_cp_i*Eddy_Viscosity_i/Prandtl_Turb;
+    const su2double u                    = V_i[VEL_INDEX];
+    const su2double v                    = V_i[VEL_INDEX+1];
+    const su2double qy_t                 = -total_conductivity_i*GV[T_INDEX][1];
+    const su2double qy_ve                = -kve*GV[TVE_INDEX][1];
 
     /*--- Enthalpy and vib-el energy transport due to y-direction diffusion---*/
-    for (iSpecies = 0; iSpecies < nHeavy; iSpecies++) {
+    su2double sumJhs_y = sumJeve_y = 0.0;
+    for (auto iSpecies = 0ul; iSpecies < nHeavy; iSpecies++) {
       sumJhs_y  += -(rho*Ds[iSpecies]*GV[RHOS_INDEX+iSpecies][1] - V_i[RHOS_INDEX+iSpecies]*Vector) * hs[iSpecies];
       sumJeve_y += -(rho*Ds[iSpecies]*GV[RHOS_INDEX+iSpecies][1] - V_i[RHOS_INDEX+iSpecies]*Vector) * eve_i[iSpecies];
     }
 
-    for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+    for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
       residual[iSpecies] -= 0.0;
     residual[nSpecies] -= Volume*(yinv*total_viscosity_i*(GV[nSpecies+2][1]+GV[nSpecies+3][0])
                                                          -TWO3*AuxVar_Grad_i[0][0]);
diff --git a/SU2_CFD/src/numerics/NEMO/convection/ausm_slau.cpp b/SU2_CFD/src/numerics/NEMO/convection/ausm_slau.cpp
index 386850c6531..aa85f0c0a74 100644
--- a/SU2_CFD/src/numerics/NEMO/convection/ausm_slau.cpp
+++ b/SU2_CFD/src/numerics/NEMO/convection/ausm_slau.cpp
@@ -53,7 +53,7 @@ CUpwAUSM_SLAU_Base_NEMO::CUpwAUSM_SLAU_Base_NEMO(unsigned short val_nDim, unsign
   Flux = new su2double[nVar];
   Jacobian_i = new su2double*[nVar];
   Jacobian_j = new su2double*[nVar];
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
     Jacobian_i[iVar] = new su2double[nVar];
     Jacobian_j[iVar] = new su2double[nVar];
   }
@@ -73,7 +73,7 @@ CUpwAUSM_SLAU_Base_NEMO::~CUpwAUSM_SLAU_Base_NEMO(void) {
   delete[] da_R;
 
   delete[] Flux;
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
     delete[] Jacobian_i[iVar];
     delete[] Jacobian_j[iVar];
   }
@@ -98,8 +98,8 @@ void CUpwAUSM_SLAU_Base_NEMO::ComputeJacobian(su2double** val_Jacobian_i, su2dou
   rhoCvtr_j = V_j[RHOCVTR_INDEX];
 
   /*--- Initialize the Jacobians ---*/
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
-    for (unsigned short jVar = 0; jVar < nVar; jVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
+    for (auto jVar = 0ul; jVar < nVar; jVar++) {
       Jacobian_i[iVar][jVar] = 0.0;
       Jacobian_j[iVar][jVar] = 0.0;
     }
@@ -120,7 +120,7 @@ void CUpwAUSM_SLAU_Base_NEMO::ComputeJacobian(su2double** val_Jacobian_i, su2dou
   /*--- Sound speed derivatives: Species density ---*/
 
   // Electrons only
-  for (unsigned short iSpecies = 0; iSpecies < nEl; iSpecies++) {
+  for (auto iSpecies = 0ul; iSpecies < nEl; iSpecies++) {
     da_L[iSpecies] = 1.0 / (2.0 * SoundSpeed_i * Density_i) * (1 + dPdU_i[nSpecies + nDim]) *
                      (dPdU_i[iSpecies] - Pressure_i / Density_i);
     da_R[iSpecies] = 1.0 / (2.0 * SoundSpeed_j * Density_j) * (1 + dPdU_j[nSpecies + nDim]) *
@@ -128,7 +128,7 @@ void CUpwAUSM_SLAU_Base_NEMO::ComputeJacobian(su2double** val_Jacobian_i, su2dou
   }
 
   // Heavy species
-  for (unsigned short iSpecies = nEl; iSpecies < nSpecies; iSpecies++) {
+  for (auto iSpecies = nEl; iSpecies < nSpecies; iSpecies++) {
     da_L[iSpecies] =
         1.0 / (2.0 * SoundSpeed_i) *
         (1 / rhoCvtr_i * (Ru / Ms[iSpecies] - Cvtr[iSpecies] * dPdU_i[nSpecies + nDim]) * Pressure_i / Density_i +
@@ -140,7 +140,7 @@ void CUpwAUSM_SLAU_Base_NEMO::ComputeJacobian(su2double** val_Jacobian_i, su2dou
   }
 
   /*--- Sound speed derivatives: Momentum ---*/
-  for (unsigned short iDim = 0; iDim < nDim; iDim++) {
+  for (auto iDim = 0ul; iDim < nDim; iDim++) {
     da_L[nSpecies + iDim] = -1.0 / (2.0 * Density_i * SoundSpeed_i) *
                             ((1.0 + dPdU_i[nSpecies + nDim]) * dPdU_i[nSpecies + nDim]) * Velocity_i[iDim];
     da_R[nSpecies + iDim] = -1.0 / (2.0 * Density_j * SoundSpeed_j) *
@@ -162,17 +162,17 @@ void CUpwAUSM_SLAU_Base_NEMO::ComputeJacobian(su2double** val_Jacobian_i, su2dou
   /*--- Left state Jacobian ---*/
   if (M_F >= 0) {
     /*--- Jacobian contribution: dFc terms ---*/
-    for (auto iVar = 0u; iVar < nSpecies + nDim; iVar++) {
-      for (unsigned short jVar = 0; jVar < nVar; jVar++) {
+    for (auto iVar = 0ul; iVar < nSpecies + nDim; iVar++) {
+      for (auto jVar = 0ul; jVar < nVar; jVar++) {
         Jacobian_i[iVar][jVar] += M_F * Fc_L[iVar] * da_L[jVar];
       }
       Jacobian_i[iVar][iVar] += M_F * SoundSpeed_i;
     }
-    for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
+    for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
       Jacobian_i[nSpecies + nDim][iSpecies] +=
           M_F * (dPdU_i[iSpecies] * SoundSpeed_i + Density_i * Enthalpy_i * da_L[iSpecies]);
     }
-    for (unsigned short iDim = 0; iDim < nDim; iDim++) {
+    for (auto iDim = 0ul; iDim < nDim; iDim++) {
       Jacobian_i[nSpecies + nDim][nSpecies + iDim] +=
           M_F *
           (-dPdU_i[nSpecies + nDim] * Velocity_i[iDim] * SoundSpeed_i + Density_i * Enthalpy_i * da_L[nSpecies + iDim]);
@@ -181,7 +181,7 @@ void CUpwAUSM_SLAU_Base_NEMO::ComputeJacobian(su2double** val_Jacobian_i, su2dou
         M_F * ((1.0 + dPdU_i[nSpecies + nDim]) * SoundSpeed_i + Density_i * Enthalpy_i * da_L[nSpecies + nDim]);
     Jacobian_i[nSpecies + nDim][nSpecies + nDim + 1] +=
         M_F * (dPdU_i[nSpecies + nDim + 1] * SoundSpeed_i + Density_i * Enthalpy_i * da_L[nSpecies + nDim + 1]);
-    for (unsigned short jVar = 0; jVar < nVar; jVar++) {
+    for (auto jVar = 0ul; jVar < nVar; jVar++) {
       Jacobian_i[nSpecies + nDim + 1][jVar] += M_F * Fc_L[nSpecies + nDim + 1] * da_L[jVar];
     }
     Jacobian_i[nSpecies + nDim + 1][nSpecies + nDim + 1] += M_F * SoundSpeed_i;
@@ -191,11 +191,11 @@ void CUpwAUSM_SLAU_Base_NEMO::ComputeJacobian(su2double** val_Jacobian_i, su2dou
   if ((M_F >= 0) || ((M_F < 0) && (fabs(M_F) <= 1.0))) {
     if (fabs(M_L) <= 1.0) {
       /*--- Mach number ---*/
-      for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+      for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
         dM_LP[iSpecies] =
             0.5 * (M_L + 1.0) *
             (-ProjVelocity_i / (Density_i * SoundSpeed_i) - ProjVelocity_i * da_L[iSpecies] / (pow(SoundSpeed_i, 2)));
-      for (unsigned short iDim = 0; iDim < nDim; iDim++)
+      for (auto iDim = 0ul; iDim < nDim; iDim++)
         dM_LP[nSpecies + iDim] = 0.5 * (M_L + 1.0) *
                                  (-ProjVelocity_i / (pow(SoundSpeed_i, 2)) * da_L[nSpecies + iDim] +
                                   UnitNormal[iDim] / (Density_i * SoundSpeed_i));
@@ -204,14 +204,14 @@ void CUpwAUSM_SLAU_Base_NEMO::ComputeJacobian(su2double** val_Jacobian_i, su2dou
           0.5 * (M_L + 1.0) * (-ProjVelocity_i / (pow(SoundSpeed_i, 2)) * da_L[nSpecies + nDim + 1]);
 
       /*--- Pressure ---*/
-      for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+      for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
         dP_LP[iSpecies] = 0.25 * (M_L + 1.0) *
                           (dPdU_i[iSpecies] * (M_L + 1.0) * (2.0 - M_L) +
                            Pressure_i *
                                (-ProjVelocity_i / (Density_i * SoundSpeed_i) -
                                 ProjVelocity_i * da_L[iSpecies] / (pow(SoundSpeed_i, 2))) *
                                (3.0 - 3.0 * M_L));
-      for (unsigned short iDim = 0; iDim < nDim; iDim++)
+      for (auto iDim = 0ul; iDim < nDim; iDim++)
         dP_LP[nSpecies + iDim] = 0.25 * (M_L + 1.0) *
                                  (-Velocity_i[iDim] * dPdU_i[nSpecies + nDim] * (M_L + 1.0) * (2.0 - M_L) +
                                   Pressure_i *
@@ -228,33 +228,33 @@ void CUpwAUSM_SLAU_Base_NEMO::ComputeJacobian(su2double** val_Jacobian_i, su2dou
            Pressure_i * (-ProjVelocity_i / (pow(SoundSpeed_i, 2)) * da_L[nSpecies + nDim + 1]) * (3.0 - 3.0 * M_L));
     } else {
       /*--- Mach number ---*/
-      for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+      for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
         dM_LP[iSpecies] =
             -ProjVelocity_i / (Density_i * SoundSpeed_i) - ProjVelocity_i * da_L[iSpecies] / (pow(SoundSpeed_i, 2));
-      for (unsigned short iDim = 0; iDim < nDim; iDim++)
+      for (auto iDim = 0ul; iDim < nDim; iDim++)
         dM_LP[nSpecies + iDim] = -ProjVelocity_i / (pow(SoundSpeed_i, 2)) * da_L[nSpecies + iDim] +
                                  UnitNormal[iDim] / (Density_i * SoundSpeed_i);
       dM_LP[nSpecies + nDim] = -ProjVelocity_i / (pow(SoundSpeed_i, 2)) * da_L[nSpecies + nDim];
       dM_LP[nSpecies + nDim + 1] = -ProjVelocity_i / (pow(SoundSpeed_i, 2)) * da_L[nSpecies + nDim + 1];
 
       /*--- Pressure ---*/
-      for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++) dP_LP[iSpecies] = dPdU_i[iSpecies];
-      for (unsigned short iDim = 0; iDim < nDim; iDim++)
+      for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) dP_LP[iSpecies] = dPdU_i[iSpecies];
+      for (auto iDim = 0ul; iDim < nDim; iDim++)
         dP_LP[nSpecies + iDim] = (-Velocity_i[iDim] * dPdU_i[nSpecies + nDim]);
       dP_LP[nSpecies + nDim] = dPdU_i[nSpecies + nDim];
       dP_LP[nSpecies + nDim + 1] = dPdU_i[nSpecies + nDim + 1];
     }
 
     /*--- dM contribution ---*/
-    for (unsigned short iVar = 0; iVar < nVar; iVar++) {
-      for (unsigned short jVar = 0; jVar < nVar; jVar++) {
+    for (auto iVar = 0ul; iVar < nVar; iVar++) {
+      for (auto jVar = 0ul; jVar < nVar; jVar++) {
         Jacobian_i[iVar][jVar] += dM_LP[jVar] * Fc_LR[iVar] * A_LR;
       }
     }
 
     /*--- Jacobian contribution: dP terms ---*/
-    for (unsigned short iDim = 0; iDim < nDim; iDim++) {
-      for (unsigned short iVar = 0; iVar < nVar; iVar++) {
+    for (auto iDim = 0ul; iDim < nDim; iDim++) {
+      for (auto iVar = 0ul; iVar < nVar; iVar++) {
         Jacobian_i[nSpecies + iDim][iVar] += dP_LP[iVar] * UnitNormal[iDim];
       }
     }
@@ -263,17 +263,17 @@ void CUpwAUSM_SLAU_Base_NEMO::ComputeJacobian(su2double** val_Jacobian_i, su2dou
   /*--- Right state Jacobian ---*/
   if (M_F < 0) {
     /*--- Jacobian contribution: dFc terms ---*/
-    for (auto iVar = 0u; iVar < nSpecies + nDim; iVar++) {
-      for (unsigned short jVar = 0; jVar < nVar; jVar++) {
+    for (auto iVar = 0ul; iVar < nSpecies + nDim; iVar++) {
+      for (auto jVar = 0ul; jVar < nVar; jVar++) {
         Jacobian_j[iVar][jVar] += M_F * Fc_R[iVar] * da_R[jVar];
       }
       Jacobian_j[iVar][iVar] += M_F * SoundSpeed_j;
     }
-    for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
+    for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
       Jacobian_j[nSpecies + nDim][iSpecies] +=
           M_F * (dPdU_j[iSpecies] * SoundSpeed_j + Density_j * Enthalpy_j * da_R[iSpecies]);
     }
-    for (unsigned short iDim = 0; iDim < nDim; iDim++) {
+    for (auto iDim = 0ul; iDim < nDim; iDim++) {
       Jacobian_j[nSpecies + nDim][nSpecies + iDim] +=
           M_F *
           (-dPdU_j[nSpecies + nDim] * Velocity_j[iDim] * SoundSpeed_j + Density_j * Enthalpy_j * da_R[nSpecies + iDim]);
@@ -282,7 +282,7 @@ void CUpwAUSM_SLAU_Base_NEMO::ComputeJacobian(su2double** val_Jacobian_i, su2dou
         M_F * ((1.0 + dPdU_j[nSpecies + nDim]) * SoundSpeed_j + Density_j * Enthalpy_j * da_R[nSpecies + nDim]);
     Jacobian_j[nSpecies + nDim][nSpecies + nDim + 1] +=
         M_F * (dPdU_j[nSpecies + nDim + 1] * SoundSpeed_j + Density_j * Enthalpy_j * da_R[nSpecies + nDim + 1]);
-    for (unsigned short jVar = 0; jVar < nVar; jVar++) {
+    for (auto jVar = 0ul; jVar < nVar; jVar++) {
       Jacobian_j[nSpecies + nDim + 1][jVar] += M_F * Fc_R[nSpecies + nDim + 1] * da_R[jVar];
     }
     Jacobian_j[nSpecies + nDim + 1][nSpecies + nDim + 1] += M_F * SoundSpeed_j;
@@ -292,11 +292,11 @@ void CUpwAUSM_SLAU_Base_NEMO::ComputeJacobian(su2double** val_Jacobian_i, su2dou
   if ((M_F < 0) || ((M_F >= 0) && (fabs(M_F) <= 1.0))) {
     if (fabs(M_R) <= 1.0) {
       /*--- Mach ---*/
-      for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+      for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
         dM_RM[iSpecies] =
             -0.5 * (M_R - 1.0) *
             (-ProjVelocity_j / (Density_j * SoundSpeed_j) - ProjVelocity_j * da_R[iSpecies] / (pow(SoundSpeed_j, 2)));
-      for (unsigned short iDim = 0; iDim < nDim; iDim++)
+      for (auto iDim = 0ul; iDim < nDim; iDim++)
         dM_RM[nSpecies + iDim] = -0.5 * (M_R - 1.0) *
                                  (-ProjVelocity_j / (pow(SoundSpeed_j, 2)) * da_R[nSpecies + iDim] +
                                   UnitNormal[iDim] / (Density_j * SoundSpeed_j));
@@ -305,14 +305,14 @@ void CUpwAUSM_SLAU_Base_NEMO::ComputeJacobian(su2double** val_Jacobian_i, su2dou
           -0.5 * (M_R - 1.0) * (-ProjVelocity_j / (pow(SoundSpeed_j, 2)) * da_R[nSpecies + nDim + 1]);
 
       /*--- Pressure ---*/
-      for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+      for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
         dP_RM[iSpecies] = 0.25 * (M_R - 1.0) *
                           (dPdU_j[iSpecies] * (M_R - 1.0) * (2.0 + M_R) +
                            Pressure_j *
                                (-ProjVelocity_j / (Density_j * SoundSpeed_j) -
                                 ProjVelocity_j * da_R[iSpecies] / (pow(SoundSpeed_j, 2))) *
                                (3.0 + 3.0 * M_R));
-      for (unsigned short iDim = 0; iDim < nDim; iDim++)
+      for (auto iDim = 0ul; iDim < nDim; iDim++)
         dP_RM[nSpecies + iDim] = 0.25 * (M_R - 1.0) *
                                  ((-Velocity_j[iDim] * dPdU_j[nSpecies + nDim]) * (M_R - 1.0) * (2.0 + M_R) +
                                   Pressure_j *
@@ -330,41 +330,41 @@ void CUpwAUSM_SLAU_Base_NEMO::ComputeJacobian(su2double** val_Jacobian_i, su2dou
 
     } else {
       /*--- Mach ---*/
-      for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+      for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
         dM_RM[iSpecies] =
             -ProjVelocity_j / (Density_j * SoundSpeed_j) - ProjVelocity_j * da_R[iSpecies] / (pow(SoundSpeed_j, 2));
-      for (unsigned short iDim = 0; iDim < nDim; iDim++)
+      for (auto iDim = 0ul; iDim < nDim; iDim++)
         dM_RM[nSpecies + iDim] = -ProjVelocity_j / (pow(SoundSpeed_j, 2)) * da_R[nSpecies + iDim] +
                                  UnitNormal[iDim] / (Density_j * SoundSpeed_j);
       dM_RM[nSpecies + nDim] = -ProjVelocity_j / (pow(SoundSpeed_j, 2)) * da_R[nSpecies + nDim];
       dM_RM[nSpecies + nDim + 1] = -ProjVelocity_j / (pow(SoundSpeed_j, 2)) * da_R[nSpecies + nDim + 1];
 
       /*--- Pressure ---*/
-      for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++) dP_RM[iSpecies] = dPdU_j[iSpecies];
-      for (unsigned short iDim = 0; iDim < nDim; iDim++)
+      for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) dP_RM[iSpecies] = dPdU_j[iSpecies];
+      for (auto iDim = 0ul; iDim < nDim; iDim++)
         dP_RM[nSpecies + iDim] = -Velocity_j[iDim] * dPdU_j[nSpecies + nDim];
       dP_RM[nSpecies + nDim] = dPdU_j[nSpecies + nDim];
       dP_RM[nSpecies + nDim + 1] = dPdU_j[nSpecies + nDim + 1];
     }
 
     /*--- Jacobian contribution: dM terms ---*/
-    for (unsigned short iVar = 0; iVar < nVar; iVar++) {
-      for (unsigned short jVar = 0; jVar < nVar; jVar++) {
+    for (auto iVar = 0ul; iVar < nVar; iVar++) {
+      for (auto jVar = 0ul; jVar < nVar; jVar++) {
         Jacobian_j[iVar][jVar] += dM_RM[jVar] * Fc_LR[iVar] * A_LR;
       }
     }
 
     /*--- Jacobian contribution: dP terms ---*/
-    for (unsigned short iDim = 0; iDim < nDim; iDim++) {
-      for (unsigned short iVar = 0; iVar < nVar; iVar++) {
+    for (auto iDim = 0ul; iDim < nDim; iDim++) {
+      for (auto iVar = 0ul; iVar < nVar; iVar++) {
         Jacobian_j[nSpecies + iDim][iVar] += dP_RM[iVar] * UnitNormal[iDim];
       }
     }
   }
 
   /*--- Integrate over dual-face area ---*/
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
-    for (unsigned short jVar = 0; jVar < nVar; jVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
+    for (auto jVar = 0ul; jVar < nVar; jVar++) {
       Jacobian_i[iVar][jVar] *= Area;
       Jacobian_j[iVar][jVar] *= Area;
     }
@@ -375,15 +375,15 @@ CNumerics::ResidualType<> CUpwAUSM_SLAU_Base_NEMO::ComputeResidual(const CConfig
   /*--- Compute geometric quantities ---*/
   Area = GeometryToolbox::Norm(nDim, Normal);
 
-  for (unsigned short iDim = 0; iDim < nDim; iDim++) UnitNormal[iDim] = Normal[iDim] / Area;
+  for (auto iDim = 0ul; iDim < nDim; iDim++) UnitNormal[iDim] = Normal[iDim] / Area;
 
   /*--- Pull stored primitive variables ---*/
   // Primitives: [rho1,...,rhoNs, T, Tve, u, v, w, P, rho, h, a, c]
-  for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
     rhos_i[iSpecies] = V_i[RHOS_INDEX + iSpecies];
     rhos_j[iSpecies] = V_j[RHOS_INDEX + iSpecies];
   }
-  for (unsigned short iDim = 0; iDim < nDim; iDim++) {
+  for (auto iDim = 0ul; iDim < nDim; iDim++) {
     Velocity_i[iDim] = V_i[VEL_INDEX + iDim];
     Velocity_j[iDim] = V_j[VEL_INDEX + iDim];
   }
@@ -398,9 +398,8 @@ CNumerics::ResidualType<> CUpwAUSM_SLAU_Base_NEMO::ComputeResidual(const CConfig
   Density_j = V_j[RHO_INDEX];
   SoundSpeed_j = V_j[A_INDEX];
 
-  e_ve_i = 0;
-  e_ve_j = 0;
-  for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
+  e_ve_i = e_ve_j = 0;
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
     e_ve_i += (V_i[RHOS_INDEX + iSpecies] * eve_i[iSpecies]) / Density_i;
     e_ve_j += (V_j[RHOS_INDEX + iSpecies] * eve_j[iSpecies]) / Density_j;
   }
@@ -412,18 +411,18 @@ CNumerics::ResidualType<> CUpwAUSM_SLAU_Base_NEMO::ComputeResidual(const CConfig
   /*--- Compute mass and pressure fluxes of specific scheme ---*/
   ComputeInterfaceQuantities(config, PressureFlux, M_F, A_F);
 
-  su2double MassFlux_i = M_F * A_F[0];
-  su2double MassFlux_j = M_F * A_F[1];
+  const su2double MassFlux_i = M_F * A_F[0];
+  const su2double MassFlux_j = M_F * A_F[1];
 
-  su2double DissFlux_i = fabs(MassFlux_i);
-  su2double DissFlux_j = fabs(MassFlux_j);
+  const su2double DissFlux_i = fabs(MassFlux_i);
+  const su2double DissFlux_j = fabs(MassFlux_j);
 
   /*--- Assign left & right convective flux vectors ---*/
-  for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
     Fc_L[iSpecies] = rhos_i[iSpecies];
     Fc_R[iSpecies] = rhos_j[iSpecies];
   }
-  for (unsigned short iDim = 0; iDim < nDim; iDim++) {
+  for (auto iDim = 0ul; iDim < nDim; iDim++) {
     Fc_L[nSpecies + iDim] = Density_i * Velocity_i[iDim];
     Fc_R[nSpecies + iDim] = Density_j * Velocity_j[iDim];
   }
@@ -433,10 +432,10 @@ CNumerics::ResidualType<> CUpwAUSM_SLAU_Base_NEMO::ComputeResidual(const CConfig
   Fc_R[nSpecies + nDim + 1] = Density_j * e_ve_j;
 
   /*--- Compute numerical flux ---*/
-  for (unsigned short iVar = 0; iVar < nVar; iVar++)
+  for (auto iVar = 0ul; iVar < nVar; iVar++)
     Flux[iVar] = 0.5 * ((MassFlux_i + DissFlux_i) * Fc_L[iVar] + (MassFlux_j - DissFlux_j) * Fc_R[iVar]) * Area;
 
-  for (unsigned short iDim = 0; iDim < nDim; iDim++) Flux[nSpecies + iDim] += PressureFlux[iDim] * Area;
+  for (auto iDim = 0ul; iDim < nDim; iDim++) Flux[nSpecies + iDim] += PressureFlux[iDim] * Area;
 
   /*--- If required, compute Jacobians (approximated using AUSM) ---*/
   if (implicit) ComputeJacobian(Jacobian_i, Jacobian_j);
diff --git a/SU2_CFD/src/numerics/NEMO/convection/lax.cpp b/SU2_CFD/src/numerics/NEMO/convection/lax.cpp
index 482512d462b..4757897675c 100644
--- a/SU2_CFD/src/numerics/NEMO/convection/lax.cpp
+++ b/SU2_CFD/src/numerics/NEMO/convection/lax.cpp
@@ -51,7 +51,7 @@ CCentLax_NEMO::CCentLax_NEMO(unsigned short val_nDim,
 
   Jacobian_i = new su2double* [nVar];
   Jacobian_j = new su2double* [nVar];
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
     Jacobian_i[iVar] = new su2double [nVar];
     Jacobian_j[iVar] = new su2double [nVar];
   }
@@ -65,7 +65,7 @@ CCentLax_NEMO::~CCentLax_NEMO(void) {
   delete [] MeandPdU;
   delete [] ProjFlux;
   delete [] Flux;
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
     delete [] Jacobian_i[iVar];
     delete [] Jacobian_j[iVar];
   }
@@ -78,7 +78,7 @@ CNumerics::ResidualType<> CCentLax_NEMO::ComputeResidual(const CConfig *config)
   /*--- Calculate geometrical quantities ---*/
   Area = GeometryToolbox::Norm(nDim, Normal);
 
-  for (unsigned short iDim = 0; iDim < nDim; iDim++)
+  for (auto iDim = 0ul; iDim < nDim; iDim++)
     UnitNormal[iDim] = Normal[iDim]/Area;
 
   /*--- Rename for convenience ---*/
@@ -87,9 +87,9 @@ CNumerics::ResidualType<> CCentLax_NEMO::ComputeResidual(const CConfig *config)
   SoundSpeed_i = V_i[A_INDEX]; SoundSpeed_j = V_j[A_INDEX];
 
   /*--- Compute mean quantities for the variables ---*/
-  for (unsigned short iVar = 0; iVar < nVar; iVar++)
+  for (auto iVar = 0ul; iVar < nVar; iVar++)
     MeanU[iVar] = 0.5*(U_i[iVar]+U_j[iVar]);
-  for (unsigned short iVar = 0; iVar < nPrimVar; iVar++)
+  for (auto iVar = 0ul; iVar < nPrimVar; iVar++)
     MeanV[iVar] = 0.5*(V_i[iVar]+V_j[iVar]);
 
   /*--- Compute NonEq specific variables ---*/
@@ -103,8 +103,8 @@ CNumerics::ResidualType<> CCentLax_NEMO::ComputeResidual(const CConfig *config)
   if (implicit) {
     GetInviscidProjJac(MeanU, MeanV, MeandPdU, Normal, 0.5, Jacobian_i);
 
-    for (unsigned short iVar = 0; iVar < nVar; iVar++)
-      for (unsigned short jVar = 0; jVar < nVar; jVar++)
+    for (auto iVar = 0ul; iVar < nVar; iVar++)
+      for (auto jVar = 0ul; jVar < nVar; jVar++)
         Jacobian_j[iVar][jVar] = Jacobian_i[iVar][jVar];
   }
 
@@ -122,7 +122,7 @@ CNumerics::ResidualType<> CCentLax_NEMO::ComputeResidual(const CConfig *config)
   StretchingFactor = 4.0*Phi_i*Phi_j/(Phi_i+Phi_j+EPS);
 
   /*--- Computes differences btw. conservative variables ---*/
-  for (unsigned short iVar = 0; iVar < nVar; iVar++)
+  for (auto iVar = 0ul; iVar < nVar; iVar++)
     Diff_U[iVar] = U_i[iVar] - U_j[iVar];
   Diff_U[nSpecies+nDim] = Density_i*Enthalpy_i - Density_j*Enthalpy_j;
 
@@ -131,7 +131,7 @@ CNumerics::ResidualType<> CCentLax_NEMO::ComputeResidual(const CConfig *config)
   Epsilon_0 = Param_Kappa_0*sc0*su2double(nDim)/3.0;
 
   /*--- Compute viscous part of the residual ---*/
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
     Flux[iVar] = ProjFlux[iVar]+Epsilon_0*Diff_U[iVar]*StretchingFactor*MeanLambda;
   }
 
@@ -145,18 +145,18 @@ CNumerics::ResidualType<> CCentLax_NEMO::ComputeResidual(const CConfig *config)
     }
 
     /*--- Last rows: CAREFUL!! You have differences of \rho_Enthalpy, not differences of \rho_Energy ---*/
-    for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+    for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
       Jacobian_i[nSpecies+nDim][iSpecies] += cte*dPdU_i[iSpecies];
-    for (unsigned short iDim = 0; iDim < nDim; iDim++)
+    for (auto iDim = 0ul; iDim < nDim; iDim++)
       Jacobian_i[nSpecies+nDim][nSpecies+iDim]   += cte*dPdU_i[nSpecies+iDim];
     Jacobian_i[nSpecies+nDim][nSpecies+nDim]     += cte*(1+dPdU_i[nSpecies+nDim]);
     Jacobian_i[nSpecies+nDim][nSpecies+nDim+1]   += cte*dPdU_i[nSpecies+nDim+1];
     Jacobian_i[nSpecies+nDim+1][nSpecies+nDim+1] += cte;
 
     /*--- Last row of Jacobian_j ---*/
-    for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+    for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
       Jacobian_j[nSpecies+nDim][iSpecies] -= cte*dPdU_j[iSpecies];
-    for (unsigned short iDim = 0; iDim < nDim; iDim++)
+    for (auto iDim = 0ul; iDim < nDim; iDim++)
       Jacobian_j[nSpecies+nDim][nSpecies+iDim]   -= cte*dPdU_j[nSpecies+nDim];
     Jacobian_j[nSpecies+nDim][nSpecies+nDim]     -= cte*(1+dPdU_j[nSpecies+nDim]);
     Jacobian_j[nSpecies+nDim][nSpecies+nDim+1]   -= cte*dPdU_j[nSpecies+nDim+1];
diff --git a/SU2_CFD/src/numerics/NEMO/convection/msw.cpp b/SU2_CFD/src/numerics/NEMO/convection/msw.cpp
index 5f9869f9126..badd0a81fb6 100644
--- a/SU2_CFD/src/numerics/NEMO/convection/msw.cpp
+++ b/SU2_CFD/src/numerics/NEMO/convection/msw.cpp
@@ -55,7 +55,7 @@ CUpwMSW_NEMO::CUpwMSW_NEMO(unsigned short val_nDim, unsigned short val_nVar,
 
   P_Tensor    = new su2double* [nVar];
   invP_Tensor = new su2double* [nVar];
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
     P_Tensor[iVar]    = new su2double [nVar];
     invP_Tensor[iVar] = new su2double [nVar];
   }
@@ -64,7 +64,7 @@ CUpwMSW_NEMO::CUpwMSW_NEMO(unsigned short val_nDim, unsigned short val_nVar,
   Flux   = new su2double[nVar];
   Jacobian_i = new su2double* [nVar];
   Jacobian_j = new su2double* [nVar];
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
     Jacobian_i[iVar] = new su2double [nVar];
     Jacobian_j[iVar] = new su2double [nVar];
   }
@@ -91,14 +91,14 @@ CUpwMSW_NEMO::~CUpwMSW_NEMO(void) {
   delete [] dPdUst_i;
   delete [] dPdUst_j;
 
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
     delete [] P_Tensor[iVar];
     delete [] invP_Tensor[iVar];
   }
   delete [] P_Tensor;
   delete [] invP_Tensor;
   delete [] Flux;
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
     delete [] Jacobian_i[iVar];
     delete [] Jacobian_j[iVar];
   }
@@ -115,17 +115,17 @@ CNumerics::ResidualType<> CUpwMSW_NEMO::ComputeResidual(const CConfig *config) {
   /*--- Calculate supporting geometry parameters ---*/
   Area = GeometryToolbox::Norm(nDim, Normal);
 
-  for (unsigned short iDim = 0; iDim < nDim; iDim++)
+  for (auto iDim = 0ul; iDim < nDim; iDim++)
     UnitNormal[iDim] = Normal[iDim]/Area;
 
   /*--- Initialize flux & Jacobian vectors ---*/
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
     Fc_i[iVar] = 0.0;
     Fc_j[iVar] = 0.0;
   }
   if (implicit) {
-    for (unsigned short iVar = 0; iVar < nVar; iVar++) {
-      for (unsigned short jVar = 0; jVar < nVar; jVar++) {
+    for (auto iVar = 0ul; iVar < nVar; iVar++) {
+      for (auto jVar = 0ul; jVar < nVar; jVar++) {
         Jacobian_i[iVar][jVar] = 0.0;
         Jacobian_j[iVar][jVar] = 0.0;
       }
@@ -133,11 +133,11 @@ CNumerics::ResidualType<> CUpwMSW_NEMO::ComputeResidual(const CConfig *config) {
   }
 
   /*--- Load variables from nodes i & j ---*/
-  for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
     rhos_i[iSpecies] = V_i[RHOS_INDEX+iSpecies];
     rhos_j[iSpecies] = V_j[RHOS_INDEX+iSpecies];
   }
-  for (unsigned short iDim = 0; iDim < nDim; iDim++) {
+  for (auto iDim = 0ul; iDim < nDim; iDim++) {
     Velocity_i[iDim] = V_i[VEL_INDEX+iDim];
     Velocity_j[iDim] = V_j[VEL_INDEX+iDim];
   }
@@ -149,21 +149,21 @@ CNumerics::ResidualType<> CUpwMSW_NEMO::ComputeResidual(const CConfig *config) {
   ProjVelocity_j = GeometryToolbox::DotProduct(nDim, Velocity_j, UnitNormal);
 
   /*--- Calculate the state weighting function ---*/
-  su2double dp = fabs(Pressure_j-Pressure_i) / min(Pressure_j, Pressure_i);
-  su2double w = 0.5 * (1.0/(pow(alpha*dp,2.0) +1.0));
-  su2double onemw = 1.0 - w;
+  const su2double dp = fabs(Pressure_j-Pressure_i) / min(Pressure_j, Pressure_i);
+  const su2double w = 0.5 * (1.0/(pow(alpha*dp,2.0) +1.0));
+  const su2double onemw = 1.0 - w;
 
   /*--- Calculate weighted state vector (*) for i & j ---*/
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
     Ust_i[iVar] = onemw*U_i[iVar] + w*U_j[iVar];
     Ust_j[iVar] = onemw*U_j[iVar] + w*U_i[iVar];
   }
-  for (unsigned short iVar = 0; iVar < nPrimVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nPrimVar; iVar++) {
     Vst_i[iVar] = onemw*V_i[iVar] + w*V_j[iVar];
     Vst_j[iVar] = onemw*V_j[iVar] + w*V_i[iVar];
   }
-  su2double ProjVelst_i = onemw*ProjVelocity_i + w*ProjVelocity_j;
-  su2double ProjVelst_j = onemw*ProjVelocity_j + w*ProjVelocity_i;
+  const su2double ProjVelst_i = onemw*ProjVelocity_i + w*ProjVelocity_j;
+  const su2double ProjVelst_j = onemw*ProjVelocity_j + w*ProjVelocity_i;
 
   const auto& eves_st_i = fluidmodel->ComputeSpeciesEve(Vst_i[TVE_INDEX]);
   const auto& eves_st_j = fluidmodel->ComputeSpeciesEve(Vst_j[TVE_INDEX]);
@@ -172,7 +172,7 @@ CNumerics::ResidualType<> CUpwMSW_NEMO::ComputeResidual(const CConfig *config) {
   fluidmodel->ComputedPdU(Vst_j, eves_st_j, dPdUst_j);
 
   /*--- Flow eigenvalues at i (Lambda+) ---*/
-  for (unsigned short iVar = 0; iVar < nSpecies+nDim-1; iVar++)
+  for (auto iVar = 0ul; iVar < nSpecies+nDim-1; iVar++)
     Lambda_i[iVar]          = 0.5*(ProjVelst_i + sqrt(ProjVelst_i*ProjVelst_i +
                                                       epsilon*epsilon));
   Lambda_i[nSpecies+nDim-1] = 0.5*(ProjVelst_i + Vst_i[A_INDEX] +
@@ -194,12 +194,12 @@ CNumerics::ResidualType<> CUpwMSW_NEMO::ComputeResidual(const CConfig *config) {
 
   /*--- Projected flux (f+) at i ---*/
   su2double Proj_ModJac_Tensor_i;
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
-    for (unsigned short jVar = 0; jVar < nVar; jVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
+    for (auto jVar = 0ul; jVar < nVar; jVar++) {
       Proj_ModJac_Tensor_i = 0.0;
 
       /*--- Compute Proj_ModJac_Tensor = P x Lambda+ x inverse P ---*/
-      for (unsigned short kVar = 0; kVar < nVar; kVar++)
+      for (auto kVar = 0ul; kVar < nVar; kVar++)
         Proj_ModJac_Tensor_i += P_Tensor[iVar][kVar]*Lambda_i[kVar]*invP_Tensor[kVar][jVar];
       Fc_i[iVar] += Proj_ModJac_Tensor_i*U_i[jVar]*Area;
       if (implicit)
@@ -208,7 +208,7 @@ CNumerics::ResidualType<> CUpwMSW_NEMO::ComputeResidual(const CConfig *config) {
   }
 
   /*--- Flow eigenvalues at j (Lambda-) ---*/
-  for (unsigned short iVar = 0; iVar < nSpecies+nDim-1; iVar++)
+  for (auto iVar = 0ul; iVar < nSpecies+nDim-1; iVar++)
     Lambda_j[iVar]          = 0.5*(ProjVelst_j - sqrt(ProjVelst_j*ProjVelst_j +
                                                       epsilon*epsilon));
   Lambda_j[nSpecies+nDim-1] = 0.5*(ProjVelst_j + Vst_j[A_INDEX] -
@@ -229,12 +229,12 @@ CNumerics::ResidualType<> CUpwMSW_NEMO::ComputeResidual(const CConfig *config) {
 
   /*--- Projected flux (f-) ---*/
   su2double Proj_ModJac_Tensor_j;
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
-    for (unsigned short jVar = 0; jVar < nVar; jVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
+    for (auto jVar = 0ul; jVar < nVar; jVar++) {
       Proj_ModJac_Tensor_j = 0.0;
 
       /*--- Compute Proj_ModJac_Tensor = P x Lambda- x inverse P ---*/
-      for (unsigned short kVar = 0; kVar < nVar; kVar++)
+      for (auto kVar = 0ul; kVar < nVar; kVar++)
         Proj_ModJac_Tensor_j += P_Tensor[iVar][kVar]*Lambda_j[kVar]*invP_Tensor[kVar][jVar];
       Fc_j[iVar] += Proj_ModJac_Tensor_j*U_j[jVar]*Area;
       if (implicit)
@@ -243,7 +243,7 @@ CNumerics::ResidualType<> CUpwMSW_NEMO::ComputeResidual(const CConfig *config) {
   }
 
   /*--- Flux splitting ---*/
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
     Flux[iVar] = Fc_i[iVar]+Fc_j[iVar];
   }
 
diff --git a/SU2_CFD/src/numerics/NEMO/convection/roe.cpp b/SU2_CFD/src/numerics/NEMO/convection/roe.cpp
index 0adcdd8dfd1..dd200242d0b 100644
--- a/SU2_CFD/src/numerics/NEMO/convection/roe.cpp
+++ b/SU2_CFD/src/numerics/NEMO/convection/roe.cpp
@@ -44,7 +44,7 @@ CUpwRoe_NEMO::CUpwRoe_NEMO(unsigned short val_nDim, unsigned short val_nVar,
 
   P_Tensor    = new su2double* [nVar];
   invP_Tensor = new su2double* [nVar];
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
     P_Tensor[iVar]    = new su2double [nVar];
     invP_Tensor[iVar] = new su2double [nVar];
   }
@@ -56,7 +56,7 @@ CUpwRoe_NEMO::CUpwRoe_NEMO(unsigned short val_nDim, unsigned short val_nVar,
 
   Jacobian_i = new su2double* [nVar];
   Jacobian_j = new su2double* [nVar];
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
     Jacobian_i[iVar] = new su2double [nVar];
     Jacobian_j[iVar] = new su2double [nVar];
   }
@@ -71,7 +71,7 @@ CUpwRoe_NEMO::~CUpwRoe_NEMO(void) {
   delete [] Lambda;
   delete [] Epsilon;
 
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
     delete [] P_Tensor[iVar];
     delete [] invP_Tensor[iVar];
   }
@@ -81,7 +81,7 @@ CUpwRoe_NEMO::~CUpwRoe_NEMO(void) {
   delete [] ProjFlux_i;
   delete [] ProjFlux_j;
   delete [] Flux;
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
     delete [] Jacobian_i[iVar];
     delete [] Jacobian_j[iVar];
   }
@@ -95,16 +95,16 @@ CNumerics::ResidualType<> CUpwRoe_NEMO::ComputeResidual(const CConfig *config) {
   Area = GeometryToolbox::Norm(nDim, Normal);
 
   /*--- Unit Normal ---*/
-  for (unsigned short iDim = 0; iDim < nDim; iDim++)
+  for (auto iDim = 0ul; iDim < nDim; iDim++)
     UnitNormal[iDim] = Normal[iDim]/Area;
 
   /*--- Calculate Roe averaged variables ---*/
-  su2double R = sqrt(abs(V_j[RHO_INDEX]/V_i[RHO_INDEX]));
+  const su2double R = sqrt(abs(V_j[RHO_INDEX]/V_i[RHO_INDEX]));
 
-  for (unsigned short iVar = 0; iVar < nVar; iVar++)
+  for (auto iVar = 0ul; iVar < nVar; iVar++)
     RoeU[iVar] = (R*U_j[iVar] + U_i[iVar])/(R+1);
 
-  for (unsigned short iVar = 0; iVar < nPrimVar; iVar++)
+  for (auto iVar = 0ul; iVar < nPrimVar; iVar++)
     RoeV[iVar] = (R*V_j[iVar] + V_i[iVar])/(R+1);
 
   const auto& roe_eves = fluidmodel->ComputeSpeciesEve(RoeV[TVE_INDEX]);
@@ -125,18 +125,18 @@ CNumerics::ResidualType<> CUpwRoe_NEMO::ComputeResidual(const CConfig *config) {
   GetPMatrix_inv(RoeU, RoeV, RoedPdU, UnitNormal, l, m, invP_Tensor);
 
   /*--- Compute projected velocities ---*/
-  su2double ProjVelocity   = GeometryToolbox::DotProduct(nDim, &RoeV[VEL_INDEX], UnitNormal);
-  su2double ProjVelocity_i = GeometryToolbox::DotProduct(nDim, &V_i[VEL_INDEX], UnitNormal);
-  su2double ProjVelocity_j = GeometryToolbox::DotProduct(nDim, &V_j[VEL_INDEX], UnitNormal);
+  const su2double ProjVelocity   = GeometryToolbox::DotProduct(nDim, &RoeV[VEL_INDEX], UnitNormal);
+  const su2double ProjVelocity_i = GeometryToolbox::DotProduct(nDim, &V_i[VEL_INDEX], UnitNormal);
+  const su2double ProjVelocity_j = GeometryToolbox::DotProduct(nDim, &V_j[VEL_INDEX], UnitNormal);
 
-  su2double RoeSoundSpeed = sqrt((1.0+RoedPdU[nSpecies+nDim])*
-                            RoeV[P_INDEX]/RoeV[RHO_INDEX]);
+  const su2double RoeSoundSpeed = sqrt((1.0+RoedPdU[nSpecies+nDim])*
+                                  RoeV[P_INDEX]/RoeV[RHO_INDEX]);
 
   /*--- Calculate eigenvalues ---*/
-  for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
     Lambda[iSpecies] = ProjVelocity;
 
-  for (unsigned short iDim = 0; iDim < nDim-1; iDim++)
+  for (auto iDim = 0ul; iDim < nDim-1; iDim++)
     Lambda[nSpecies+iDim] = ProjVelocity;
 
   Lambda[nSpecies+nDim-1] = ProjVelocity + RoeSoundSpeed;
@@ -144,10 +144,10 @@ CNumerics::ResidualType<> CUpwRoe_NEMO::ComputeResidual(const CConfig *config) {
   Lambda[nSpecies+nDim+1] = ProjVelocity;
 
   /*--- Harten and Hyman (1983) entropy correction ---*/
-  for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
     Epsilon[iSpecies] = 4.0*max(0.0, max(Lambda[iSpecies]-ProjVelocity_i,
                                          ProjVelocity_j-Lambda[iSpecies] ));
-  for (unsigned short iDim = 0; iDim < nDim-1; iDim++)
+  for (auto iDim = 0ul; iDim < nDim-1; iDim++)
     Epsilon[nSpecies+iDim] = 4.0*max(0.0, max(Lambda[iDim]-ProjVelocity_i,
                                               ProjVelocity_j-Lambda[iDim] ));
   Epsilon[nSpecies+nDim-1] = 4.0*max(0.0, max(Lambda[nSpecies+nDim-1]-(ProjVelocity_i+V_i[A_INDEX]),
@@ -156,13 +156,13 @@ CNumerics::ResidualType<> CUpwRoe_NEMO::ComputeResidual(const CConfig *config) {
                                      (ProjVelocity_j-V_j[A_INDEX])-Lambda[nSpecies+nDim]));
   Epsilon[nSpecies+nDim+1] = 4.0*max(0.0, max(Lambda[nSpecies+nDim+1]-ProjVelocity_i,
                                               ProjVelocity_j-Lambda[nSpecies+nDim+1] ));
-  for (unsigned short iVar = 0; iVar < nVar; iVar++)
+  for (auto iVar = 0ul; iVar < nVar; iVar++)
     if ( fabs(Lambda[iVar]) < Epsilon[iVar] )
       Lambda[iVar] = (Lambda[iVar]*Lambda[iVar] + Epsilon[iVar]*Epsilon[iVar])/(2.0*Epsilon[iVar]);
     else
       Lambda[iVar] = fabs(Lambda[iVar]);
 
-  for (unsigned short iVar = 0; iVar < nVar; iVar++)
+  for (auto iVar = 0ul; iVar < nVar; iVar++)
     Lambda[iVar] = fabs(Lambda[iVar]);
 
   /*--- Calculate inviscid projected Jacobians ---*/
@@ -173,17 +173,17 @@ CNumerics::ResidualType<> CUpwRoe_NEMO::ComputeResidual(const CConfig *config) {
   }
 
   /*--- Difference of conserved variables at iPoint and jPoint ---*/
-  for (unsigned short iVar = 0; iVar < nVar; iVar++)
+  for (auto iVar = 0ul; iVar < nVar; iVar++)
     Diff_U[iVar] = U_j[iVar]-U_i[iVar];
 
   /*--- Roe's Flux approximation ---*/
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) {
     Flux[iVar] = 0.5 * (ProjFlux_i[iVar] + ProjFlux_j[iVar]);
-    for (unsigned short jVar = 0; jVar < nVar; jVar++) {
+    for (auto jVar = 0ul; jVar < nVar; jVar++) {
 
       /*--- Compute |Proj_ModJac_Tensor| = P x |Lambda| x inverse P ---*/
       Proj_ModJac_Tensor_ij = 0.0;
-      for (unsigned short kVar = 0; kVar < nVar; kVar++)
+      for (auto kVar = 0ul; kVar < nVar; kVar++)
         Proj_ModJac_Tensor_ij += P_Tensor[iVar][kVar]*Lambda[kVar]*invP_Tensor[kVar][jVar];
 
       Flux[iVar] -= 0.5*Proj_ModJac_Tensor_ij*Diff_U[jVar]*Area;
diff --git a/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp b/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
index dcca84abbeb..717f4dfb7a7 100644
--- a/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
@@ -56,8 +56,6 @@ CNEMOEulerSolver::CNEMOEulerSolver(CGeometry *geometry, CConfig *config,
   const bool adjoint = config->GetContinuous_Adjoint() || config->GetDiscrete_Adjoint();
 
   int Unst_RestartIter = 0;
-  unsigned long iMarker;
-  su2double *Mvec_Inf, Alpha, Beta;
 
   /*--- A grid is defined as dynamic if there's rigid grid movement or grid deformation AND the problem is time domain ---*/
   dynamic_grid = config->GetDynamic_Grid();
@@ -113,7 +111,7 @@ CNEMOEulerSolver::CNEMOEulerSolver(CGeometry *geometry, CConfig *config,
 
   /*--- Store the number of vertices on each marker for deallocation ---*/
   nVertex.resize(nMarker);
-  for (iMarker = 0; iMarker < nMarker; iMarker++)
+  for (auto iMarker = 0ul; iMarker < nMarker; iMarker++)
     nVertex[iMarker] = geometry->nVertex[iMarker];
 
   MassFrac_Inf = config->GetGas_Composition();
@@ -175,9 +173,10 @@ CNEMOEulerSolver::CNEMOEulerSolver(CGeometry *geometry, CConfig *config,
   SetReferenceValues(*config);
 
   /*--- Vectorize free stream Mach number based on AoA & AoS ---*/
+  su2double *Mvec_Inf;
   Mvec_Inf = new su2double[nDim];
-  Alpha    = config->GetAoA()*PI_NUMBER/180.0;
-  Beta     = config->GetAoS()*PI_NUMBER/180.0;
+  const su2double Alpha = config->GetAoA()*PI_NUMBER/180.0;
+  const su2double Beta = config->GetAoS()*PI_NUMBER/180.0;
   if (nDim == 2) {
     Mvec_Inf[0] = cos(Alpha)*Mach_Inf;
     Mvec_Inf[1] = sin(Alpha)*Mach_Inf;
@@ -240,10 +239,10 @@ CNEMOEulerSolver::~CNEMOEulerSolver(void) {
 void CNEMOEulerSolver::CommonPreprocessing(CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh,
                                            unsigned short iRKStep, unsigned short RunTime_EqSystem, bool Output) {
 
-  bool implicit         = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
-  bool center           = (config->GetKind_ConvNumScheme_Flow() == SPACE_CENTERED);
-  bool center_jst       = (config->GetKind_Centered_Flow() == CENTERED::JST) && (iMesh == MESH_0);
-  bool center_jst_ke    = (config->GetKind_Centered_Flow() == CENTERED::JST_KE) && (iMesh == MESH_0);
+  const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+  const bool center = (config->GetKind_ConvNumScheme_Flow() == SPACE_CENTERED);
+  const bool center_jst = (config->GetKind_Centered_Flow() == CENTERED::JST) && (iMesh == MESH_0);
+  const bool center_jst_ke = (config->GetKind_Centered_Flow() == CENTERED::JST_KE) && (iMesh == MESH_0);
 
   /*--- Set the primitive variables ---*/
   ompMasterAssignBarrier(ErrorCounter,0);
@@ -318,10 +317,10 @@ void CNEMOEulerSolver::Preprocessing(CGeometry *geometry, CSolver **solver_conta
 
 unsigned long CNEMOEulerSolver::SetPrimitive_Variables(CSolver **solver_container, CConfig *config, bool Output) {
 
-  unsigned long iPoint, nonPhysicalPoints = 0;
+  unsigned long nonPhysicalPoints = 0;
   bool nonphysical = true;
 
-  for (iPoint = 0; iPoint < nPoint; iPoint ++) {
+  for (auto iPoint = 0ul; iPoint < nPoint; iPoint ++) {
 
     /*--- Incompressible flow, primitive variables ---*/
 
@@ -359,27 +358,27 @@ void CNEMOEulerSolver::SetTime_Step(CGeometry *geometry, CSolver **solver_contai
   struct LambdaVisc {
     FORCEINLINE su2double lambda(su2double lamVisc, su2double eddyVisc, su2double rho, su2double k, su2double cv) const {
       /*--- Determine the viscous spectral radius and apply it to the control volume ---*/
-      su2double Lambda_1 = (4.0/3.0)*(lamVisc + eddyVisc);
+      const su2double Lambda_1 = (4.0/3.0)*(lamVisc + eddyVisc);
       return (Lambda_1 + k/cv)/rho;
     }
 
     FORCEINLINE su2double operator() (const CNEMOEulerVariable& nodes, unsigned long iPoint, unsigned long jPoint) const {
-      su2double lamVisc = 0.5*(nodes.GetLaminarViscosity(iPoint) + nodes.GetLaminarViscosity(jPoint));
-      su2double eddyVisc = 0.5*(nodes.GetEddyViscosity(iPoint) + nodes.GetEddyViscosity(jPoint));
-      su2double thermalCond = 0.5*(nodes.GetThermalConductivity(iPoint) + nodes.GetThermalConductivity(jPoint) +
+      const su2double lamVisc = 0.5*(nodes.GetLaminarViscosity(iPoint) + nodes.GetLaminarViscosity(jPoint));
+      const su2double eddyVisc = 0.5*(nodes.GetEddyViscosity(iPoint) + nodes.GetEddyViscosity(jPoint));
+      const su2double thermalCond = 0.5*(nodes.GetThermalConductivity(iPoint) + nodes.GetThermalConductivity(jPoint) +
                                    nodes.GetThermalConductivity_ve(iPoint) + nodes.GetThermalConductivity_ve(jPoint));
-      su2double density = 0.5*(nodes.GetDensity(iPoint) + nodes.GetDensity(jPoint));
-      su2double cv = 0.5*(nodes.GetRhoCv_tr(iPoint) + nodes.GetRhoCv_ve(iPoint) +
+      const su2double density = 0.5*(nodes.GetDensity(iPoint) + nodes.GetDensity(jPoint));
+      const su2double cv = 0.5*(nodes.GetRhoCv_tr(iPoint) + nodes.GetRhoCv_ve(iPoint) +
                           nodes.GetRhoCv_tr(jPoint) + nodes.GetRhoCv_ve(jPoint))/ density;
       return lambda(lamVisc, eddyVisc, density, thermalCond, cv);
     }
 
     FORCEINLINE su2double operator() (const CNEMOEulerVariable& nodes, unsigned long iPoint) const {
-      su2double lamVisc = nodes.GetLaminarViscosity(iPoint);
-      su2double eddyVisc = nodes.GetEddyViscosity(iPoint);
-      su2double thermalCond = nodes.GetThermalConductivity(iPoint) + nodes.GetThermalConductivity_ve(iPoint);
-      su2double density = nodes.GetDensity(iPoint);
-      su2double cv = (nodes.GetRhoCv_tr(iPoint) + nodes.GetRhoCv_ve(iPoint))/ density;
+      const su2double lamVisc = nodes.GetLaminarViscosity(iPoint);
+      const su2double eddyVisc = nodes.GetEddyViscosity(iPoint);
+      const su2double thermalCond = nodes.GetThermalConductivity(iPoint) + nodes.GetThermalConductivity_ve(iPoint);
+      const su2double density = nodes.GetDensity(iPoint);
+      const su2double cv = (nodes.GetRhoCv_tr(iPoint) + nodes.GetRhoCv_ve(iPoint))/ density;
       return lambda(lamVisc, eddyVisc, density, thermalCond, cv);
     }
 
@@ -413,18 +412,17 @@ void CNEMOEulerSolver::SetMax_Eigenvalue(CGeometry *geometry, CConfig *config) {
 
 void CNEMOEulerSolver::Centered_Residual(CGeometry *geometry, CSolver **solver_container, CNumerics **numerics_container,
                                          CConfig *config, unsigned short iMesh, unsigned short iRKStep) {
-  unsigned long iEdge, iPoint, jPoint;
 
   CNumerics* numerics = numerics_container[CONV_TERM];
 
   /*--- Set booleans based on config settings ---*/
-  bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+  const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
 
-  for (iEdge = 0; iEdge < geometry->GetnEdge(); iEdge++) {
+  for (auto iEdge = 0ul; iEdge < geometry->GetnEdge(); iEdge++) {
 
     /*--- Points in edge, set normal vectors, and number of neighbors ---*/
-    iPoint = geometry->edges->GetNode(iEdge, 0);
-    jPoint = geometry->edges->GetNode(iEdge, 1);
+    const auto iPoint = geometry->edges->GetNode(iEdge, 0);
+    const auto jPoint = geometry->edges->GetNode(iEdge, 1);
     numerics->SetNormal(geometry->edges->GetNormal(iEdge));
     numerics->SetNeighbor(geometry->nodes->GetnNeighbor(iPoint),
                           geometry->nodes->GetnNeighbor(jPoint));
@@ -491,18 +489,16 @@ void CNEMOEulerSolver::Upwind_Residual(CGeometry *geometry, CSolver **solver_con
   su2double Gamma_i = 0.0, Gamma_j = 0.0;
 
   /*--- Loop over edges and calculate convective fluxes ---*/
-  for(unsigned long iEdge = 0; iEdge < geometry->GetnEdge(); iEdge++) {
-
-    unsigned short iDim, iVar;
+  for(auto iEdge = 0ul; iEdge < geometry->GetnEdge(); iEdge++) {
 
     /*--- Retrieve node numbers and pass edge normal to CNumerics ---*/
-    auto iPoint = geometry->edges->GetNode(iEdge, 0);
-    auto jPoint = geometry->edges->GetNode(iEdge, 1);
+    const auto iPoint = geometry->edges->GetNode(iEdge, 0);
+    const auto jPoint = geometry->edges->GetNode(iEdge, 1);
 
     numerics->SetNormal(geometry->edges->GetNormal(iEdge));
 
-    auto Coord_i = geometry->nodes->GetCoord(iPoint);
-    auto Coord_j = geometry->nodes->GetCoord(jPoint);
+    const auto Coord_i = geometry->nodes->GetCoord(iPoint);
+    const auto Coord_j = geometry->nodes->GetCoord(jPoint);
 
     /*--- Get conserved & primitive variables from CVariable ---*/
     auto U_i = nodes->GetSolution(iPoint);   auto U_j = nodes->GetSolution(jPoint);
@@ -524,7 +520,7 @@ void CNEMOEulerSolver::Upwind_Residual(CGeometry *geometry, CSolver **solver_con
 
       /*--- High order reconstruction using MUSCL strategy ---*/
       su2double Vector_ij[MAXNDIM] = {0.0};
-      for (iDim = 0; iDim < nDim; iDim++) {
+      for (auto iDim = 0ul; iDim < nDim; iDim++) {
         Vector_ij[iDim] = 0.5*(Coord_j[iDim] - Coord_i[iDim]);
       }
 
@@ -543,10 +539,10 @@ void CNEMOEulerSolver::Upwind_Residual(CGeometry *geometry, CSolver **solver_con
       su2double lim_i = 2.0;
       su2double lim_j = 2.0;
 
-      for (iVar = 0; iVar < nPrimVarGrad; iVar++) {
+      for (auto iVar = 0ul; iVar < nPrimVarGrad; iVar++) {
         Project_Grad_i[iVar] = 0.0; Project_Grad_j[iVar] = 0.0;
 
-        for (iDim = 0; iDim < nDim; iDim++) {
+        for (auto iDim = 0ul; iDim < nDim; iDim++) {
           Project_Grad_i[iVar] += Vector_ij[iDim]*Gradient_i[iVar][iDim];
           Project_Grad_j[iVar] -= Vector_ij[iDim]*Gradient_j[iVar][iDim];
         }
@@ -568,7 +564,7 @@ void CNEMOEulerSolver::Upwind_Residual(CGeometry *geometry, CSolver **solver_con
       }
       su2double lim_ij = min(lim_i, lim_j);
 
-      for (iVar = 0; iVar < nPrimVarGrad; iVar++) {
+      for (auto iVar = 0ul; iVar < nPrimVarGrad; iVar++) {
         Primitive_i[iVar] = V_i[iVar] + lim_ij*Project_Grad_i[iVar];
         Primitive_j[iVar] = V_j[iVar] + lim_ij*Project_Grad_j[iVar];
       }
@@ -650,14 +646,13 @@ su2double CNEMOEulerSolver::ComputeConsistentExtrapolation(CNEMOGas *fluidmodel,
                                                            su2double* val_eves, su2double *val_Cvves) {
 
   //NOTE: TODO - this doesnt compute Cvves/ dPdU,etc.yet
-  su2double val_gamma;
-  vector<su2double> rhos;
 
   /*--- Rename index information ---*/
-  unsigned short T_INDEX   = nSpecies;
-  unsigned short TVE_INDEX = nSpecies+1;
+  const unsigned short T_INDEX   = nSpecies;
+  const unsigned short TVE_INDEX = nSpecies+1;
 
   /*--- Rename density vector ---*/
+  vector<su2double> rhos;
   rhos.resize(nSpecies,0.0);
   for (unsigned short iSpecies=0; iSpecies < nSpecies; iSpecies++ ){
     rhos[iSpecies] = V[iSpecies];
@@ -674,7 +669,7 @@ su2double CNEMOEulerSolver::ComputeConsistentExtrapolation(CNEMOGas *fluidmodel,
     *it = v;  ++it;
   }
 
-  val_gamma = fluidmodel->ComputeGamma();
+  const su2double val_gamma = fluidmodel->ComputeGamma();
 
   return val_gamma;
 }
@@ -686,24 +681,23 @@ void CNEMOEulerSolver::RecomputeConservativeVector(su2double *U, const su2double
   rhos.resize(nSpecies,0.0);
 
   /*--- Set Indices ---*/
-  //Make these in a general location
-  unsigned short RHO_INDEX = nodes->GetRhoIndex();
-  unsigned short T_INDEX   = nodes->GetTIndex();
-  unsigned short TVE_INDEX = nodes->GetTveIndex();
-  unsigned short VEL_INDEX = nodes->GetVelIndex();
+  //TODO: Move these to a general location
+  const unsigned short RHO_INDEX = nodes->GetRhoIndex();
+  const unsigned short T_INDEX   = nodes->GetTIndex();
+  const unsigned short TVE_INDEX = nodes->GetTveIndex();
+  const unsigned short VEL_INDEX = nodes->GetVelIndex();
 
   /*--- Set densities and mass fraction ---*/
-  for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++){
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++){
     U[iSpecies]    = V[iSpecies];
     rhos[iSpecies] = V[iSpecies];
   }
 
   /*--- Set momentum and compute v^2 ---*/
-  //TODO: geometry toolbox
   su2double sqvel = 0.0;
-  for (unsigned short iDim = 0; iDim < nDim; iDim++){
+  for (auto iDim = 0ul; iDim < nDim; iDim++){
     U[nSpecies+iDim] = V[RHO_INDEX]*V[VEL_INDEX+iDim];
-    sqvel           += V[VEL_INDEX+iDim]*V[VEL_INDEX+iDim];
+    sqvel += V[VEL_INDEX+iDim]*V[VEL_INDEX+iDim];
   }
 
   /*--- Set the fluidmodel and recompute energies ---*/
@@ -718,25 +712,23 @@ void CNEMOEulerSolver::RecomputeConservativeVector(su2double *U, const su2double
 
 bool CNEMOEulerSolver::CheckNonPhys(const su2double *V) const {
 
-  su2double Tmin, Tmax, Tvemin, Tvemax;
-
   /*--- Set booleans ---*/
   bool nonPhys = false;
 
   /*--- Set Indices ---*/
-  //Make these in a general location
-  unsigned short RHOS_INDEX = nodes->GetRhosIndex();
-  unsigned short T_INDEX    = nodes->GetTIndex();
-  unsigned short TVE_INDEX  = nodes->GetTveIndex();
-  unsigned short P_INDEX    = nodes->GetPIndex();
-  unsigned short A_INDEX    = nodes->GetAIndex();
+  //TODO: Move these to a general location
+  const unsigned short RHOS_INDEX = nodes->GetRhosIndex();
+  const unsigned short T_INDEX    = nodes->GetTIndex();
+  const unsigned short TVE_INDEX  = nodes->GetTveIndex();
+  const unsigned short P_INDEX    = nodes->GetPIndex();
+  const unsigned short A_INDEX    = nodes->GetAIndex();
 
   /*--- Set temperature clipping values ---*/
-  Tmin   = 50.0; Tmax   = 8E4;
-  Tvemin = 50.0; Tvemax = 8E4;
+  const su2double Tmin   = 50.0; const su2double Tmax   = 8E4;
+  const su2double Tvemin = 50.0; const su2double Tvemax = 8E4;
 
   /*--- Check whether state makes sense ---*/
-  for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
     if (V[RHOS_INDEX+iSpecies] < 0.0) nonPhys = true;
 
   if (V[P_INDEX] < 0.0) nonPhys = true;
@@ -753,17 +745,14 @@ bool CNEMOEulerSolver::CheckNonPhys(const su2double *V) const {
 
 void CNEMOEulerSolver::Source_Residual(CGeometry *geometry, CSolver **solver_container, CNumerics **numerics_container, CConfig *config, unsigned short iMesh) {
 
-  unsigned short iVar;
-  unsigned long iPoint;
-
   /*--- Assign booleans ---*/
   bool err        = false;
-  bool implicit   = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
-  bool frozen     = config->GetFrozen();
-  bool monoatomic = config->GetMonoatomic();
-  bool axisymm    = config->GetAxisymmetric();
-  bool viscous    = config->GetViscous();
-  bool rans       = (config->GetKind_Turb_Model() != TURB_MODEL::NONE);
+  const bool implicit   = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+  const bool frozen     = config->GetFrozen();
+  const bool monoatomic = config->GetMonoatomic();
+  const bool axisymm    = config->GetAxisymmetric();
+  const bool viscous    = config->GetViscous();
+  const bool rans       = (config->GetKind_Turb_Model() != TURB_MODEL::NONE);
 
   CNumerics* numerics = numerics_container[SOURCE_FIRST_TERM];
 
@@ -773,7 +762,7 @@ void CNEMOEulerSolver::Source_Residual(CGeometry *geometry, CSolver **solver_con
   unsigned long eVib_local = 0;
 
   /*--- Initialize the source residual to zero ---*/
-  for (iVar = 0; iVar < nVar; iVar++) Residual[iVar] = 0.0;
+  for (auto iVar = 0ul; iVar < nVar; iVar++) Residual[iVar] = 0.0;
 
   /*--- Preprocess viscous axisymm variables (if necessary) ---*/
   if (axisymm && viscous) {
@@ -784,7 +773,7 @@ void CNEMOEulerSolver::Source_Residual(CGeometry *geometry, CSolver **solver_con
 
   /*--- loop over interior points ---*/
   SU2_OMP_FOR_DYN(omp_chunk_size)
-  for (iPoint = 0; iPoint < nPointDomain; iPoint++) {
+  for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
 
     /*--- Set conserved & primitive variables  ---*/
     numerics->SetConservative(nodes->GetSolution(iPoint),  nullptr);
@@ -947,13 +936,13 @@ void CNEMOEulerSolver::ComputeUnderRelaxationFactor(const CConfig *config) {
   const su2double allowableRatio = 0.2;
 
   SU2_OMP_FOR_STAT(omp_chunk_size)
-  for (unsigned long iPoint = 0; iPoint < nPointDomain; iPoint++) {
+  for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
     su2double localUnderRelaxation = 1.0;
 
     su2double num = 0.0;
     su2double denom = 0.0;
 
-    for (unsigned short iVar = 0; iVar < nVar; iVar++) {
+    for (auto iVar = 0ul; iVar < nVar; iVar++) {
       /* We impose a limit on the maximum percentage that the
        density (sum of all species) and energy can change over a nonlinear iteration. */
 
@@ -1013,20 +1002,18 @@ void CNEMOEulerSolver::SetNondimensionalization(CConfig *config, unsigned short
 
   su2double Velocity_FreeStreamND[3] = {0.0, 0.0, 0.0};
 
-  unsigned short iDim;
-
   /*--- Local variables ---*/
-  su2double Alpha         = config->GetAoA()*PI_NUMBER/180.0;
-  su2double Beta          = config->GetAoS()*PI_NUMBER/180.0;
-  su2double Mach          = config->GetMach();
-  su2double Reynolds      = config->GetReynolds();
-
-  bool unsteady           = (config->GetTime_Marching() != TIME_MARCHING::STEADY);
-  bool viscous            = config->GetViscous();
-  bool gravity            = config->GetGravityForce();
-  bool turbulent          = false;
-  bool tkeNeeded          = ((turbulent) && (config->GetKind_Turb_Model() == TURB_MODEL::SST));
-  bool reynolds_init      = (config->GetKind_InitOption() == REYNOLDS);
+  const su2double Alpha= config->GetAoA()*PI_NUMBER/180.0;
+  const su2double Beta = config->GetAoS()*PI_NUMBER/180.0;
+  const su2double Mach = config->GetMach();
+  const su2double Reynolds = config->GetReynolds();
+
+  const bool unsteady = (config->GetTime_Marching() != TIME_MARCHING::STEADY);
+  const bool viscous  = config->GetViscous();
+  const bool gravity  = config->GetGravityForce();
+  const bool turbulent = false;
+  const bool tkeNeeded = ((turbulent) && (config->GetKind_Turb_Model() == TURB_MODEL::SST));
+  const bool reynolds_init = (config->GetKind_InitOption() == REYNOLDS);
 
   /*--- The dimensional viscosity is needed to determine the free-stream conditions.
         To accomplish this, simply set the non-dimensional coefficients to the
@@ -1086,7 +1073,7 @@ void CNEMOEulerSolver::SetNondimensionalization(CConfig *config, unsigned short
 
   /*--- Compute the modulus of the free stream velocity ---*/
   ModVel_FreeStream = 0.0;
-  for (iDim = 0; iDim < nDim; iDim++){
+  for (auto iDim = 0ul; iDim < nDim; iDim++){
     ModVel_FreeStream += config->GetVelocity_FreeStream()[iDim]*config->GetVelocity_FreeStream()[iDim];
   }
   sqvel = ModVel_FreeStream;
@@ -1186,7 +1173,7 @@ void CNEMOEulerSolver::SetNondimensionalization(CConfig *config, unsigned short
   Pressure_FreeStreamND = Pressure_FreeStream/config->GetPressure_Ref();  config->SetPressure_FreeStreamND(Pressure_FreeStreamND);
   Density_FreeStreamND  = Density_FreeStream/config->GetDensity_Ref();    config->SetDensity_FreeStreamND(Density_FreeStreamND);
 
-  for (iDim = 0; iDim < nDim; iDim++) {
+  for (auto iDim = 0ul; iDim < nDim; iDim++) {
     Velocity_FreeStreamND[iDim] = config->GetVelocity_FreeStream()[iDim]/Velocity_Ref; config->SetVelocity_FreeStreamND(Velocity_FreeStreamND[iDim], iDim);
   }
 
@@ -1195,7 +1182,7 @@ void CNEMOEulerSolver::SetNondimensionalization(CConfig *config, unsigned short
   Gas_ConstantND              = config->GetGas_Constant()/Gas_Constant_Ref;                config->SetGas_ConstantND(Gas_ConstantND);
 
   ModVel_FreeStreamND = 0.0;
-  for (iDim = 0; iDim < nDim; iDim++) ModVel_FreeStreamND += Velocity_FreeStreamND[iDim]*Velocity_FreeStreamND[iDim];
+  for (auto iDim = 0ul; iDim < nDim; iDim++) ModVel_FreeStreamND += Velocity_FreeStreamND[iDim]*Velocity_FreeStreamND[iDim];
   ModVel_FreeStreamND    = sqrt(ModVel_FreeStreamND); config->SetModVel_FreeStreamND(ModVel_FreeStreamND);
 
   Viscosity_FreeStreamND = Viscosity_FreeStream / Viscosity_Ref;   config->SetViscosity_FreeStreamND(Viscosity_FreeStreamND);
@@ -1411,17 +1398,14 @@ void CNEMOEulerSolver::SetReferenceValues(const CConfig& config) {
 void CNEMOEulerSolver::BC_Sym_Plane(CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics,
                                     CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
 
-  unsigned short iDim, jDim, iSpecies, iVar, jVar;
-  unsigned long iPoint, iVertex;
-
   /*--- Allocate the necessary vector structures ---*/
   su2double Normal[MAXNDIM] = {0.0}, UnitNormal[MAXNDIM] = {0.0};
 
-  bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+  const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
 
   /*--- Loop over all the vertices on this boundary (val_marker) ---*/
-  for (iVertex = 0; iVertex < geometry->nVertex[val_marker]; iVertex++) {
-    iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
+  for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
+    const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
     /*--- Check if the node belongs to the domain (i.e, not a halo node) ---*/
     if (geometry->nodes->GetDomain(iPoint)) {
@@ -1430,19 +1414,19 @@ void CNEMOEulerSolver::BC_Sym_Plane(CGeometry *geometry, CSolver **solver_contai
       geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
 
       /*--- Calculate parameters from the geometry ---*/
-      su2double Area = GeometryToolbox::Norm(nDim, Normal);
+      const su2double Area = GeometryToolbox::Norm(nDim, Normal);
 
-      for (iDim = 0; iDim < nDim; iDim++){
+      for (auto iDim = 0ul; iDim < nDim; iDim++){
         UnitNormal[iDim] = -Normal[iDim]/Area;
       }
 
       /*--- Retrieve the pressure on the vertex ---*/
-      su2double P = nodes->GetPressure(iPoint);
+      const su2double P = nodes->GetPressure(iPoint);
 
       /*--- Apply the flow-tangency b.c. to the convective flux ---*/
-      for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+      for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
         Residual[iSpecies] = 0.0;
-      for (iDim = 0; iDim < nDim; iDim++){
+      for (auto iDim = 0ul; iDim < nDim; iDim++){
         Residual[nSpecies+iDim] = P * UnitNormal[iDim] * Area;
       }
       Residual[nSpecies+nDim]   = 0.0;
@@ -1461,31 +1445,31 @@ void CNEMOEulerSolver::BC_Sym_Plane(CGeometry *geometry, CSolver **solver_contai
         auto& Ms = FluidModel->GetSpeciesMolarMass();
 
         /*--- Initialize Jacobian ---*/
-        for (iVar = 0; iVar < nVar; iVar++)
-          for (jVar = 0; jVar < nVar; jVar++)
+        for (auto iVar = 0ul; iVar < nVar; iVar++)
+          for (auto jVar = 0ul; jVar < nVar; jVar++)
             Jacobian_i[iVar][jVar] = 0.0;
 
         /*--- Calculate state i ---*/
-        su2double rho     = nodes->GetDensity(iPoint);
-        su2double rhoE    = nodes->GetSolution(iPoint,nSpecies+nDim);
-        su2double rhoEve  = nodes->GetSolution(iPoint,nSpecies+nDim+1);
-        auto dPdU    = nodes->GetdPdU(iPoint);
-        for (iDim = 0; iDim < nDim; iDim++)
+        const su2double rho    = nodes->GetDensity(iPoint);
+        const su2double rhoE   = nodes->GetSolution(iPoint,nSpecies+nDim);
+        const su2double rhoEve = nodes->GetSolution(iPoint,nSpecies+nDim+1);
+        const auto dPdU    = nodes->GetdPdU(iPoint);
+        for (auto iDim = 0ul; iDim < nDim; iDim++)
           Velocity[iDim] = nodes->GetVelocity(iPoint,iDim);
 
         su2double conc = 0.0;
-        for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
-          su2double cs = nodes->GetMassFraction(iPoint,iSpecies);
+        for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
+          const su2double cs = nodes->GetMassFraction(iPoint,iSpecies);
           conc += cs * rho/Ms[iSpecies];
 
-          for (iDim = 0; iDim < nDim; iDim++) {
+          for (auto iDim = 0ul; iDim < nDim; iDim++) {
             Jacobian_i[nSpecies+iDim][iSpecies] = dPdU[iSpecies] * UnitNormal[iDim];
             Jacobian_i[iSpecies][nSpecies+iDim] = cs * UnitNormal[iDim];
           }
         }
 
-        for (iDim = 0; iDim < nDim; iDim++) {
-          for (jDim = 0; jDim < nDim; jDim++) {
+        for (auto iDim = 0ul; iDim < nDim; iDim++) {
+          for (auto jDim = 0ul; jDim < nDim; jDim++) {
             Jacobian_i[nSpecies+iDim][nSpecies+jDim] = Velocity[iDim]*UnitNormal[jDim]
                 + dPdU[nSpecies+jDim]*UnitNormal[iDim];
           }
@@ -1497,8 +1481,8 @@ void CNEMOEulerSolver::BC_Sym_Plane(CGeometry *geometry, CSolver **solver_contai
         }
 
         /*--- Integrate over the dual-grid area ---*/
-        for (iVar = 0; iVar < nVar; iVar++)
-          for (jVar = 0; jVar < nVar; jVar++)
+        for (auto iVar = 0ul; iVar < nVar; iVar++)
+          for (auto jVar = 0ul; jVar < nVar; jVar++)
             Jacobian_i[iVar][jVar] = Jacobian_i[iVar][jVar] * Area;
 
         /*--- Apply the contribution to the system ---*/
@@ -1519,7 +1503,7 @@ void CNEMOEulerSolver::BC_Far_Field(CGeometry *geometry,
   su2double Normal[MAXNDIM] = {0.0};
 
   /*--- Loop over all the vertices on this boundary (val_marker) ---*/
-  for (unsigned long iVertex = 0; iVertex < geometry->nVertex[val_marker];
+  for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker];
        iVertex++) {
     const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
@@ -1532,7 +1516,7 @@ void CNEMOEulerSolver::BC_Far_Field(CGeometry *geometry,
 
       /*--- Pass boundary node normal to CNumerics ---*/
       geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
-      for (unsigned short iDim = 0; iDim < nDim; iDim++)
+      for (auto iDim = 0ul; iDim < nDim; iDim++)
         Normal[iDim] = -Normal[iDim];
       conv_numerics->SetNormal(Normal);
 
@@ -1565,7 +1549,7 @@ void CNEMOEulerSolver::BC_Far_Field(CGeometry *geometry,
         Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
 
       /*--- Viscous contribution ---*/
-      bool viscous = config->GetViscous();
+      const bool viscous = config->GetViscous();
       if (viscous) {
         su2double Coord_Reflected[MAXNDIM];
         GeometryToolbox::PointPointReflect(
@@ -1903,18 +1887,14 @@ void CNEMOEulerSolver::BC_Inlet(CGeometry *geometry, CSolver **solver_container,
 void CNEMOEulerSolver::BC_Outlet(CGeometry *geometry, CSolver **solver_container,
                                  CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
 
-  unsigned short iVar, iDim, iSpecies;
-  unsigned long iVertex, iPoint;
-  su2double Pressure, P_Exit, Velocity[3], Temperature, Tve, Velocity2, Entropy, Density,
-  Riemann, Vn, SoundSpeed, Mach_Exit, Vn_Exit, Area, UnitNormal[3];
+  su2double UnitNormal[MAXNDIM] = {0.0};
   vector<su2double> rhos;
-
   rhos.resize(nSpecies,0.0);
 
   string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
-  bool dynamic_grid = config->GetGrid_Movement();
-  bool gravity      = config->GetGravityForce();
-  bool implicit     = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+  const bool dynamic_grid = config->GetGrid_Movement();
+  const bool gravity = config->GetGravityForce();
+  const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
 
   su2double *U_domain;
   su2double *U_outlet = new su2double[nVar];
@@ -1922,19 +1902,19 @@ void CNEMOEulerSolver::BC_Outlet(CGeometry *geometry, CSolver **solver_container
   su2double *Normal   = new su2double[nDim];
   su2double *Ys       = new su2double[nSpecies];
 
-  unsigned short T_INDEX       = nodes->GetTIndex();
-  unsigned short TVE_INDEX     = nodes->GetTveIndex();
-  unsigned short VEL_INDEX     = nodes->GetVelIndex();
-  unsigned short P_INDEX       = nodes->GetPIndex();
-  unsigned short RHO_INDEX     = nodes->GetRhoIndex();
-  unsigned short H_INDEX       = nodes->GetHIndex();
-  unsigned short A_INDEX       = nodes->GetAIndex();
-  unsigned short RHOCVTR_INDEX = nodes->GetRhoCvtrIndex();
-  unsigned short RHOCVVE_INDEX = nodes->GetRhoCvveIndex();
+  const unsigned short T_INDEX       = nodes->GetTIndex();
+  const unsigned short TVE_INDEX     = nodes->GetTveIndex();
+  const unsigned short VEL_INDEX     = nodes->GetVelIndex();
+  const unsigned short P_INDEX       = nodes->GetPIndex();
+  const unsigned short RHO_INDEX     = nodes->GetRhoIndex();
+  const unsigned short H_INDEX       = nodes->GetHIndex();
+  const unsigned short A_INDEX       = nodes->GetAIndex();
+  const unsigned short RHOCVTR_INDEX = nodes->GetRhoCvtrIndex();
+  const unsigned short RHOCVVE_INDEX = nodes->GetRhoCvveIndex();
 
   /*--- Loop over all the vertices on this boundary marker ---*/
-  for (iVertex = 0; iVertex < geometry->nVertex[val_marker]; iVertex++) {
-    iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
+  for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
+    const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
     /*--- Allocate the value at the outlet ---*/
     V_outlet = GetCharacPrimVar(val_marker, iVertex);
@@ -1944,12 +1924,12 @@ void CNEMOEulerSolver::BC_Outlet(CGeometry *geometry, CSolver **solver_container
 
       /*--- Normal vector for this vertex (negate for outward convention) ---*/
       geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
-      for (iDim = 0; iDim < nDim; iDim++) Normal[iDim] = -Normal[iDim];
+      for (auto iDim = 0ul; iDim < nDim; iDim++) Normal[iDim] = -Normal[iDim];
       conv_numerics->SetNormal(Normal);
 
-      Area = GeometryToolbox::Norm(nDim, Normal);
+      const su2double Area = GeometryToolbox::Norm(nDim, Normal);
 
-      for (iDim = 0; iDim < nDim; iDim++)
+      for (auto iDim = 0ul; iDim < nDim; iDim++)
         UnitNormal[iDim] = Normal[iDim]/Area;
 
       /*--- Current solution at this boundary node ---*/
@@ -1957,8 +1937,8 @@ void CNEMOEulerSolver::BC_Outlet(CGeometry *geometry, CSolver **solver_container
       V_domain = nodes->GetPrimitive(iPoint);
 
       /*--- Initialize solution at outlet ---*/
-      for (iVar = 0; iVar < nVar; iVar++)     U_outlet[iVar] = 0.0;
-      for (iVar = 0; iVar < nPrimVar; iVar++) V_outlet[iVar] = 0.0;
+      for (auto iVar = 0ul; iVar < nVar; iVar++)     U_outlet[iVar] = 0.0;
+      for (auto iVar = 0ul; iVar < nPrimVar; iVar++) V_outlet[iVar] = 0.0;
 
       /*--- Build the fictitious intlet state based on characteristics ---*/
 
@@ -1967,6 +1947,7 @@ void CNEMOEulerSolver::BC_Outlet(CGeometry *geometry, CSolver **solver_container
       Gamma_Minus_One = Gamma - 1.0;
 
       /*--- Retrieve the specified back pressure for this outlet. ---*/
+      su2double P_Exit;
       if (gravity) P_Exit = config->GetOutlet_Pressure(Marker_Tag) - geometry->nodes->GetCoord(iPoint, nDim-1)*STANDARD_GRAVITY;
       else         P_Exit = config->GetOutlet_Pressure(Marker_Tag);
 
@@ -1975,18 +1956,19 @@ void CNEMOEulerSolver::BC_Outlet(CGeometry *geometry, CSolver **solver_container
 
       /*--- Check whether the flow is supersonic at the exit. The type
        of boundary update depends on this. ---*/
-      Density = V_domain[RHO_INDEX];
-      Velocity2 = 0.0; Vn = 0.0;
-      for (iDim = 0; iDim < nDim; iDim++) {
+      su2double Density = V_domain[RHO_INDEX];
+      su2double Velocity2 = Vn = 0.0;
+      su2double Velocity[MAXNDIM] = {0.0};
+      for (auto iDim = 0ul; iDim < nDim; iDim++) {
         Velocity[iDim] = V_domain[VEL_INDEX+iDim];
         Velocity2 += Velocity[iDim]*Velocity[iDim];
         Vn += Velocity[iDim]*UnitNormal[iDim];
       }
-      Temperature = V_domain[T_INDEX];
-      Tve         = V_domain[TVE_INDEX];
-      Pressure    = V_domain[P_INDEX];
-      SoundSpeed  = V_domain[A_INDEX];
-      Mach_Exit   = sqrt(Velocity2)/SoundSpeed;
+      su2double Temperature = V_domain[T_INDEX];
+      su2double Tve         = V_domain[TVE_INDEX];
+      su2double Pressure    = V_domain[P_INDEX];
+      su2double SoundSpeed  = V_domain[A_INDEX];
+      su2double Mach_Exit   = sqrt(Velocity2)/SoundSpeed;
 
       /*--- Compute Species Concentrations ---*/
       for (iSpecies =0; iSpecies<nSpecies;iSpecies++){
@@ -2012,8 +1994,8 @@ void CNEMOEulerSolver::BC_Outlet(CGeometry *geometry, CSolver **solver_container
          (T and Tve) and species concentraition are also assumed to be extrapolated.
          ---*/
 
-        Entropy = Pressure*pow(1.0/Density,Gamma);
-        Riemann = Vn + 2.0*SoundSpeed/Gamma_Minus_One;
+        const su2double Entropy = Pressure*pow(1.0/Density,Gamma);
+        const su2double Riemann = Vn + 2.0*SoundSpeed/Gamma_Minus_One;
 
         /*--- Compute the new fictious state at the outlet ---*/
         //     U: [rho1, ..., rhoNs, rhou, rhov, rhow, rhoe, rhoeve]^T
@@ -2023,21 +2005,21 @@ void CNEMOEulerSolver::BC_Outlet(CGeometry *geometry, CSolver **solver_container
         SoundSpeed = sqrt(Gamma*P_Exit/Density);
         Vn_Exit    = Riemann - 2.0*SoundSpeed/Gamma_Minus_One;
         Velocity2  = 0.0;
-        for (iDim = 0; iDim < nDim; iDim++) {
+        for (auto iDim = 0ul; iDim < nDim; iDim++) {
           Velocity[iDim] = Velocity[iDim] + (Vn_Exit-Vn)*UnitNormal[iDim];
           Velocity2 += Velocity[iDim]*Velocity[iDim];
         }
 
         /*--- Primitive variables, using the derived quantities ---*/
-        for (iSpecies = 0; iSpecies < nSpecies; iSpecies ++){
+        for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies ++) {
           V_outlet[iSpecies] = Ys[iSpecies]*Density;
-          rhos[iSpecies]     = V_outlet[iSpecies];
+          rhos[iSpecies] = V_outlet[iSpecies];
         }
 
-        V_outlet[T_INDEX]     = V_domain[T_INDEX];
-        V_outlet[TVE_INDEX]   = V_domain[TVE_INDEX];
+        V_outlet[T_INDEX] = V_domain[T_INDEX];
+        V_outlet[TVE_INDEX] = V_domain[TVE_INDEX];
 
-        for (iDim = 0; iDim < nDim; iDim++){
+        for (auto iDim = 0ul; iDim < nDim; iDim++){
           V_outlet[VEL_INDEX+iDim] = Velocity[iDim];
         }
 
@@ -2053,11 +2035,11 @@ void CNEMOEulerSolver::BC_Outlet(CGeometry *geometry, CSolver **solver_container
         const auto& energies = FluidModel->ComputeMixtureEnergies();
 
         /*--- Conservative variables, using the derived quantities ---*/
-        for (iSpecies = 0; iSpecies < nSpecies; iSpecies ++){
+        for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies ++){
           U_outlet[iSpecies] = V_outlet[iSpecies];
         }
 
-        for (iDim = 0; iDim < nDim; iDim++)
+        for (auto iDim = 0ul; iDim < nDim; iDim++)
           U_outlet[nSpecies+iDim] = Velocity[iDim]*Density;
 
         U_outlet[nVar-2] = (energies[0] + 0.5*Velocity2) * Density;
@@ -2181,7 +2163,7 @@ void CNEMOEulerSolver::BC_Supersonic_Inlet(
 
   su2double Mvec[MAXNDIM] = {0.0};
 
-  for (unsigned short iDim = 0; iDim < nDim; iDim++)
+  for (auto iDim = 0ul; iDim < nDim; iDim++)
     Mvec[iDim] = Velocity[iDim] / soundspeed;
 
   /*--- Allocate inlet node to compute gradients for numerics ---*/
@@ -2193,7 +2175,7 @@ void CNEMOEulerSolver::BC_Supersonic_Inlet(
   su2double Normal[MAXNDIM] = {0.0};
 
   /*--- Loop over all the vertices on this boundary marker ---*/
-  for (unsigned long iVertex = 0; iVertex < geometry->nVertex[val_marker];
+  for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker];
        iVertex++) {
     const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
@@ -2207,7 +2189,7 @@ void CNEMOEulerSolver::BC_Supersonic_Inlet(
 
     /*--- Normal vector for this vertex (negate for outward convention) ---*/
     geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
-    for (unsigned short iDim = 0; iDim < nDim; iDim++)
+    for (auto iDim = 0ul; iDim < nDim; iDim++)
       Normal[iDim] = -Normal[iDim];
 
     /*--- Set various quantities in the solver class ---*/
@@ -2308,7 +2290,7 @@ void CNEMOEulerSolver::BC_Supersonic_Outlet(
   const string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
 
   /*--- Loop over all the vertices on this boundary marker ---*/
-  for (unsigned long iVertex = 0; iVertex < geometry->nVertex[val_marker];
+  for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker];
        iVertex++) {
 
     const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
@@ -2319,7 +2301,7 @@ void CNEMOEulerSolver::BC_Supersonic_Outlet(
 
     /*--- Normal vector for this vertex (negate for outward convention) ---*/
     geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
-    for (unsigned short iDim = 0; iDim < nDim; iDim++)
+    for (auto iDim = 0ul; iDim < nDim; iDim++)
       Normal[iDim] = -Normal[iDim];
 
     /*--- Set various quantities in the solver class, outlet properties are
@@ -2359,7 +2341,7 @@ void CNEMOEulerSolver::SetPressureDiffusionSensor(CGeometry *geometry, CConfig *
 
   const auto P_INDEX = nodes->GetPIndex();
 
-  for (unsigned long iPoint = 0; iPoint < nPointDomain; iPoint++) {
+  for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
 
     su2double Sensor = 1.0;
 
diff --git a/SU2_CFD/src/solvers/CNEMONSSolver.cpp b/SU2_CFD/src/solvers/CNEMONSSolver.cpp
index 98d960b76f1..573b5aa4bae 100644
--- a/SU2_CFD/src/solvers/CNEMONSSolver.cpp
+++ b/SU2_CFD/src/solvers/CNEMONSSolver.cpp
@@ -117,7 +117,7 @@ unsigned long CNEMONSSolver::SetPrimitive_Variables(CSolver **solver_container,C
   //const bool tkeNeeded = (turb_model == TURB_MODEL::SST);
 
   SU2_OMP_FOR_STAT(omp_chunk_size)
-  for (unsigned long iPoint = 0; iPoint < nPoint; iPoint ++) {
+  for (auto iPoint = 0ul; iPoint < nPoint; iPoint ++) {
 
     /*--- Retrieve the value of the kinetic energy (if needed). ---*/
 
@@ -145,8 +145,6 @@ unsigned long CNEMONSSolver::SetPrimitive_Variables(CSolver **solver_container,C
 
 void CNEMONSSolver::SetPrimitive_Gradient_GG(CGeometry *geometry, const CConfig *config, bool reconstruction) {
 
-  unsigned long iPoint, iVar;
-  unsigned short iSpecies;
   auto& gradient = reconstruction ? nodes->GetGradient_Reconstruction() : nodes->GetGradient_Primitive();
   const auto comm = reconstruction? PRIMITIVE_GRAD_REC : PRIMITIVE_GRADIENT;
   const auto commPer = reconstruction? PERIODIC_PRIM_GG_R : PERIODIC_PRIM_GG;
@@ -156,13 +154,13 @@ void CNEMONSSolver::SetPrimitive_Gradient_GG(CGeometry *geometry, const CConfig
   const unsigned short RHO_INDEX  = nodes->GetRhoIndex();
 
   /*--- Modify species density to mass concentration ---*/
-  for ( iPoint = 0; iPoint < nPoint; iPoint++){
+  for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
     su2double primitives_aux[MAXNVAR] = {0.0};
-    for( iVar = 0; iVar < nPrimVar; iVar++)
+    for (auto iVar = 0ul; iVar < nPrimVar; iVar++)
       primitives_aux[iVar] = nodes->GetPrimitive(iPoint, iVar);
-    for ( iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+    for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
       primitives_aux[RHOS_INDEX+iSpecies] = primitives_aux[RHOS_INDEX+iSpecies]/primitives_aux[RHO_INDEX];
-    for( iVar = 0; iVar < nPrimVar; iVar++)
+    for (auto iVar = 0ul; iVar < nPrimVar; iVar++)
       nodes->SetPrimitive_Aux(iPoint, iVar, primitives_aux[iVar] );
   }
 
@@ -177,14 +175,14 @@ void CNEMONSSolver::Viscous_Residual(CGeometry *geometry,
                                      CConfig *config, unsigned short iMesh,
                                      unsigned short iRKStep) {
 
-  bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
+  const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
   CNumerics* numerics = numerics_container[VISC_TERM];
 
-  for (unsigned long iEdge = 0; iEdge < geometry->GetnEdge(); iEdge++) {
+  for (auto iEdge = 0ul; iEdge < geometry->GetnEdge(); iEdge++) {
 
     /*--- Points, coordinates and normal vector in edge ---*/
-    auto iPoint = geometry->edges->GetNode(iEdge, 0);
-    auto jPoint = geometry->edges->GetNode(iEdge, 1);
+    const auto iPoint = geometry->edges->GetNode(iEdge, 0);
+    const auto jPoint = geometry->edges->GetNode(iEdge, 1);
     numerics->SetCoord(geometry->nodes->GetCoord(iPoint),
                        geometry->nodes->GetCoord(jPoint) );
     numerics->SetNormal(geometry->edges->GetNormal(iEdge));
@@ -260,12 +258,12 @@ void CNEMONSSolver::BC_HeatFluxNonCatalytic_Wall(CGeometry *geometry,
   const su2double pcontrol = 1.0;
 
   /*--- Get the locations of the primitive variables ---*/
-  const unsigned short T_INDEX       = nodes->GetTIndex();
-  const unsigned short TVE_INDEX     = nodes->GetTveIndex();
+  const unsigned short T_INDEX = nodes->GetTIndex();
+  const unsigned short TVE_INDEX = nodes->GetTveIndex();
 
   /*--- Loop over all of the vertices on this boundary marker ---*/
   SU2_OMP_FOR_DYN(OMP_MIN_SIZE)
-  for(auto iVertex = 0u; iVertex < geometry->nVertex[val_marker]; iVertex++) {
+  for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
 
     const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
@@ -274,10 +272,10 @@ void CNEMONSSolver::BC_HeatFluxNonCatalytic_Wall(CGeometry *geometry,
 
     /*--- Compute dual-grid area and boundary normal ---*/
     const auto Normal = geometry->vertex[val_marker][iVertex]->GetNormal();
-    su2double Area = GeometryToolbox::Norm(nDim, Normal);
+    const su2double Area = GeometryToolbox::Norm(nDim, Normal);
 
     /*--- Initialize the convective & viscous residuals to zero ---*/
-    for (auto iVar = 0u; iVar < nVar; iVar++) {Res_Visc[iVar] = 0.0;}
+    for (auto iVar = 0ul; iVar < nVar; iVar++) {Res_Visc[iVar] = 0.0;}
 
     /*--- Set the residual on the boundary with the specified heat flux ---*/
     // TODO: Look into this!
@@ -286,12 +284,12 @@ void CNEMONSSolver::BC_HeatFluxNonCatalytic_Wall(CGeometry *geometry,
     const auto GradV  = nodes->GetGradient_Primitive(iPoint);
     su2double dTdn   = 0.0;
     su2double dTvedn = 0.0;
-    for (auto iDim = 0u; iDim < nDim; iDim++) {
+    for (auto iDim = 0ul; iDim < nDim; iDim++) {
       dTdn   += GradV[T_INDEX][iDim]*Normal[iDim];
       dTvedn += GradV[TVE_INDEX][iDim]*Normal[iDim];
     }
-    su2double ktr = nodes->GetThermalConductivity(iPoint);
-    su2double kve = nodes->GetThermalConductivity_ve(iPoint);
+    const su2double ktr = nodes->GetThermalConductivity(iPoint);
+    const su2double kve = nodes->GetThermalConductivity_ve(iPoint);
 
     /*--- Compute residual ---*/
     Res_Visc[nSpecies+nDim]   += pcontrol*(ktr*dTdn+kve*dTvedn) +
@@ -305,7 +303,7 @@ void CNEMONSSolver::BC_HeatFluxNonCatalytic_Wall(CGeometry *geometry,
     su2double zero[MAXNDIM] = {0.0};
     nodes->SetVelocity_Old(iPoint, zero);
 
-    for (auto iDim = 0u; iDim < nDim; iDim++)
+    for (auto iDim = 0ul; iDim < nDim; iDim++)
       LinSysRes(iPoint, nSpecies+iDim) = 0.0;
     nodes->SetVel_ResTruncError_Zero(iPoint);
 
@@ -383,11 +381,11 @@ void CNEMONSSolver::BC_HeatFluxCatalytic_Wall(CGeometry *geometry,
   /*--- Allocate arrays ---*/
   dYdn = new su2double[nSpecies];
   GradY = new su2double*[nSpecies];
-  for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+  for (iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
     GradY[iSpecies] = new su2double[nDim];
 
   /*--- Loop over all of the vertices on this boundary marker ---*/
-  for(iVertex = 0; iVertex < geometry->nVertex[val_marker]; iVertex++) {
+  for(iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
     iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
     /*--- Check if the node belongs to the domain (i.e, not a halo node) ---*/
@@ -398,17 +396,17 @@ void CNEMONSSolver::BC_HeatFluxCatalytic_Wall(CGeometry *geometry,
       Area = GeometryToolbox::Norm(nDim, Normal);
 
       /*--- Initialize the convective & viscous residuals to zero ---*/
-      for (iVar = 0; iVar < nVar; iVar++) {
+      for (iVar = 0ul; iVar < nVar; iVar++) {
         Res_Visc[iVar] = 0.0;
         Res_Sour[iVar] = 0.0;
       }
 
       /*--- Assign wall velocity to "Vector" array ---*/
-      for (iDim = 0; iDim < nDim; iDim++) Vector[iDim] = 0.0;
+      for (iDim = 0ul; iDim < nDim; iDim++) Vector[iDim] = 0.0;
 
       /*--- Set the residual, truncation error, and velocity value ---*/
       nodes->SetVelocity_Old(iPoint,Vector);
-      for (iDim = 0; iDim < nDim; iDim++) {
+      for (iDim = 0ul; iDim < nDim; iDim++) {
         LinSysRes(iPoint, nSpecies+iDim) = 0.0;
         nodes->SetVal_ResTruncError_Zero(iPoint,nSpecies+iDim);
       }
@@ -418,7 +416,7 @@ void CNEMONSSolver::BC_HeatFluxCatalytic_Wall(CGeometry *geometry,
       const auto GradV  = nodes->GetGradient_Primitive(iPoint);
       su2double dTdn   = 0.0;
       su2double dTvedn = 0.0;
-      for (iDim = 0; iDim < nDim; iDim++) {
+      for (iDim = 0ul; iDim < nDim; iDim++) {
         dTdn   += GradV[T_INDEX][iDim]*Normal[iDim];
         dTvedn += GradV[TVE_INDEX][iDim]*Normal[iDim];
       }
@@ -433,20 +431,20 @@ void CNEMONSSolver::BC_HeatFluxCatalytic_Wall(CGeometry *geometry,
         Ds  = nodes->GetDiffusionCoeff(iPoint);
 
         /*--- Calculate normal derivative of mass fraction ---*/
-        for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
+        for (iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
           Ys = V[RHOS_INDEX+iSpecies]/rho;
           dYdn[iSpecies] = 0.0;
-          for (iDim = 0; iDim < nDim; iDim++)
+          for (iDim = 0ul; iDim < nDim; iDim++)
             dYdn[iSpecies] += 1.0/rho * (GradV[RHOS_INDEX+iSpecies][iDim] -
                 Ys*GradV[RHO_INDEX][iDim])*Normal[iDim];
         }
 
         /*--- Calculate supplementary quantities ---*/
         SdYdn = 0.0;
-        for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+        for (iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
           SdYdn += rho*Ds[iSpecies]*dYdn[iSpecies];
 
-        for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
+        for (iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
           Ys   = V[RHOS_INDEX+iSpecies]/rho;
           //eves = nodes->CalcEve(config, V[TVE_INDEX], iSpecies);
           //hs   = nodes->CalcHs(config, V[T_INDEX], eves, iSpecies);
@@ -504,7 +502,7 @@ void CNEMONSSolver::BC_HeatFluxCatalytic_Wall(CGeometry *geometry,
     }
   }
 
-  for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+  for (iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
     delete [] GradY[iSpecies];
   delete [] GradY;
   delete [] dYdn;
@@ -546,18 +544,18 @@ void CNEMONSSolver::BC_IsothermalNonCatalytic_Wall(CGeometry *geometry,
   const auto Marker_Tag = config->GetMarker_All_TagBound(val_marker);
 
   /*--- Retrieve the specified wall temperature ---*/
-  su2double Twall = config->GetIsothermal_Temperature(Marker_Tag);
+  const su2double Twall = config->GetIsothermal_Temperature(Marker_Tag);
 
   su2double **Jacobian_i = nullptr;
   if (implicit) {
     Jacobian_i = new su2double* [nVar];
-    for (auto iVar = 0u; iVar < nVar; iVar++)
+    for (auto iVar = 0ul; iVar < nVar; iVar++)
       Jacobian_i[iVar] = new su2double [nVar] ();
   }
 
   /*--- Loop over boundary points to calculate energy flux ---*/
   SU2_OMP_FOR_DYN(OMP_MIN_SIZE)
-  for (auto iVertex = 0u; iVertex < geometry->nVertex[val_marker]; iVertex++) {
+  for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
 
     const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
@@ -565,8 +563,8 @@ void CNEMONSSolver::BC_IsothermalNonCatalytic_Wall(CGeometry *geometry,
 
     /*--- Compute dual-grid area and boundary normal ---*/
     const auto Normal = geometry->vertex[val_marker][iVertex]->GetNormal();
-    su2double Area = GeometryToolbox::Norm(nDim, Normal);
-    for (auto iDim = 0u; iDim < nDim; iDim++)
+    const su2double Area = GeometryToolbox::Norm(nDim, Normal);
+    for (auto iDim = 0ul; iDim < nDim; iDim++)
       UnitNormal[iDim] = Normal[iDim]/Area;
 
     /*--- Compute closest normal neighbor ---*/
@@ -576,7 +574,7 @@ void CNEMONSSolver::BC_IsothermalNonCatalytic_Wall(CGeometry *geometry,
     const auto Coord_i = geometry->nodes->GetCoord(iPoint);
     const auto Coord_j = geometry->nodes->GetCoord(Point_Normal);
 
-    su2double dist_ij = GeometryToolbox::Distance(nDim, Coord_i, Coord_j);
+    const su2double dist_ij = GeometryToolbox::Distance(nDim, Coord_i, Coord_j);
 
     /*--- Store the corrected velocity at the wall which will
      be zero (v = 0), unless there is grid motion (v = u_wall)---*/
@@ -584,21 +582,21 @@ void CNEMONSSolver::BC_IsothermalNonCatalytic_Wall(CGeometry *geometry,
     nodes->SetVelocity_Old(iPoint, zero);
 
     /*--- Initialize viscous residual to zero ---*/
-    for (auto iVar = 0u; iVar < nVar; iVar ++) {Res_Visc[iVar] = 0.0;}
+    for (auto iVar = 0ul; iVar < nVar; iVar ++) {Res_Visc[iVar] = 0.0;}
 
-    for (auto iDim = 0u; iDim < nDim; iDim++)
+    for (auto iDim = 0ul; iDim < nDim; iDim++)
       LinSysRes(iPoint, nSpecies+iDim) = 0.0;
     nodes->SetVel_ResTruncError_Zero(iPoint);
 
     /*--- Calculate the gradient of temperature ---*/
-    su2double Ti   = nodes->GetTemperature(iPoint);
-    su2double Tj   = nodes->GetTemperature(Point_Normal);
-    su2double Tvei = nodes->GetTemperature_ve(iPoint);
-    su2double Tvej = nodes->GetTemperature_ve(Point_Normal);
+    const su2double Ti   = nodes->GetTemperature(iPoint);
+    const su2double Tj   = nodes->GetTemperature(Point_Normal);
+    const su2double Tvei = nodes->GetTemperature_ve(iPoint);
+    const su2double Tvej = nodes->GetTemperature_ve(Point_Normal);
 
     /*--- Rename variables for convenience ---*/
-    su2double ktr = nodes->GetThermalConductivity(iPoint);
-    su2double kve = nodes->GetThermalConductivity_ve(iPoint);
+    const su2double ktr = nodes->GetThermalConductivity(iPoint);
+    const su2double kve = nodes->GetThermalConductivity_ve(iPoint);
 
     /*--- Apply to the linear system ---*/
     Res_Visc[nSpecies+nDim]   = ((ktr*(Ti-Tj)    + kve*(Tvei-Tvej)) +
@@ -609,8 +607,8 @@ void CNEMONSSolver::BC_IsothermalNonCatalytic_Wall(CGeometry *geometry,
     if (implicit) {
 
       /*--- Initialize Jacobian to zero ---*/
-      for (auto iVar = 0u; iVar < nVar; iVar++)
-        for (auto jVar = 0u; jVar < nVar; jVar++)
+      for (auto iVar = 0ul; iVar < nVar; iVar++)
+        for (auto jVar = 0ul; jVar < nVar; jVar++)
           Jacobian_i[iVar][jVar] = 0.0;
 
       /*--- Add contributions to the Jacobian from the weak enforcement of the energy equations. ---*/
@@ -618,7 +616,7 @@ void CNEMONSSolver::BC_IsothermalNonCatalytic_Wall(CGeometry *geometry,
       const auto dTvedU = nodes->GetdTvedU(iPoint);
       const su2double theta = GeometryToolbox::SquaredNorm(nDim, UnitNormal);
 
-      for (auto iVar = 0u; iVar < nVar; iVar++) {
+      for (auto iVar = 0ul; iVar < nVar; iVar++) {
         Jacobian_i[nSpecies+nDim][iVar]   = -(ktr*theta/dist_ij*dTdU[iVar] +
                                               kve*theta/dist_ij*dTvedU[iVar])*Area;
         Jacobian_i[nSpecies+nDim+1][iVar] = - kve*theta/dist_ij*dTvedU[iVar]*Area;
@@ -643,7 +641,7 @@ void CNEMONSSolver::BC_IsothermalNonCatalytic_Wall(CGeometry *geometry,
   END_SU2_OMP_FOR
 
   if (Jacobian_i)
-    for (auto iVar = 0u; iVar < nVar; iVar++)
+    for (auto iVar = 0ul; iVar < nVar; iVar++)
       delete [] Jacobian_i[iVar];
   delete [] Jacobian_i;
 
@@ -661,7 +659,6 @@ void CNEMONSSolver::BC_IsothermalCatalytic_Wall(CGeometry *geometry,
                                  sour_numerics, config, val_marker);
 
   /*--- Local variables ---*/
-  unsigned short iSpecies, jSpecies, iVar, jVar, kVar;
   su2double **GradY, **dVdU;
 
   /*--- Assign booleans ---*/
@@ -681,14 +678,14 @@ void CNEMONSSolver::BC_IsothermalCatalytic_Wall(CGeometry *geometry,
 
   /*--- Allocate arrays ---*/
   GradY = new su2double*[nSpecies];
-  for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
     GradY[iSpecies] = new su2double[nDim];
   dVdU = new su2double*[nVar];
-  for (iVar = 0; iVar < nVar; iVar++)
+  for (auto iVar = 0ul; iVar < nVar; iVar++)
     dVdU[iVar] = new su2double[nVar];
 
   /*--- Loop over all of the vertices on this boundary marker ---*/
-  for (auto iVertex = 0u; iVertex < geometry->nVertex[val_marker]; iVertex++) {
+  for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
 
     const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
@@ -708,7 +705,7 @@ void CNEMONSSolver::BC_IsothermalCatalytic_Wall(CGeometry *geometry,
       const su2double Area = GeometryToolbox::Norm(nDim, Normal);
 
       /*--- Initialize the viscous residual to zero ---*/
-      for (iVar = 0; iVar < nVar; iVar++) Res_Visc[iVar] = 0.0;
+      for (auto iVar = 0ul; iVar < nVar; iVar++) Res_Visc[iVar] = 0.0;
 
       /*--- Get primitive information ---*/
       const auto& Vi = nodes->GetPrimitive(iPoint);
@@ -726,21 +723,21 @@ void CNEMONSSolver::BC_IsothermalCatalytic_Wall(CGeometry *geometry,
 
         /*--- Calculate supplementary quantities ---*/
         su2double dYdn = 0.0, SdYdn = 0.0;
-        for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
+        for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
           dYdn = (Yst[iSpecies]-Vj[RHOS_INDEX+iSpecies]/Vj[RHO_INDEX])/dij;
           SdYdn += rho*Di[iSpecies]*dYdn;
         }
 
         /*--- Calculate species residual at wall ---*/
-        for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
+        for (iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
           dYdn = (Yst[iSpecies]-Vj[RHOS_INDEX+iSpecies]/Vj[RHO_INDEX])/dij;
           Res_Visc[iSpecies]  = -(-rho*Di[iSpecies]*dYdn+Yst[iSpecies]*SdYdn)*Area;
         }
 
         if (implicit) {
           /*--- Initialize the transformation matrix ---*/
-          for (iVar = 0; iVar < nVar; iVar++)
-            for (jVar = 0; jVar < nVar; jVar++) {
+          for (auto iVar = 0ul; iVar < nVar; iVar++)
+            for (auto jVar = 0ul; jVar < nVar; jVar++) {
               dVdU[iVar][jVar] = 0.0;
               Jacobian_j[iVar][jVar] = 0.0;
               Jacobian_i[iVar][jVar] = 0.0;
@@ -748,12 +745,12 @@ void CNEMONSSolver::BC_IsothermalCatalytic_Wall(CGeometry *geometry,
 
           /*--- Populate transformation matrix ---*/
           // dYsdrk
-          for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
-            for (jSpecies = 0; jSpecies < nSpecies; jSpecies++)
+          for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
+            for (auto jSpecies = 0ul; jSpecies < nSpecies; jSpecies++)
               dVdU[iSpecies][jSpecies] += -1.0/rho*Yst[iSpecies];
             dVdU[iSpecies][iSpecies] += 1.0/rho;
           }
-          for (iVar = 0; iVar < nVar; iVar++) {
+          for (auto iVar = 0ul; iVar < nVar; iVar++) {
             dVdU[nSpecies+nDim][iVar]   = dTdU[iVar];
             dVdU[nSpecies+nDim+1][iVar] = dTvedU[iVar];
           }
@@ -764,15 +761,15 @@ void CNEMONSSolver::BC_IsothermalCatalytic_Wall(CGeometry *geometry,
 
           /*--- Take the primitive var. Jacobian & store in Jac. jj ---*/
           // Species mass fraction
-          for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
-            for (jSpecies = 0; jSpecies < nSpecies; jSpecies++)
+          for (iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
+            for (jSpecies = 0ul; jSpecies < nSpecies; jSpecies++)
               Jacobian_j[iSpecies][jSpecies] += -Yst[iSpecies]*rho*Di[jSpecies]/dij;
             Jacobian_j[iSpecies][iSpecies] += rho*Di[iSpecies]/dij - SdYdn;
           }
 
           // Temperature
-          for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
-            for (jSpecies = 0; jSpecies < nSpecies; jSpecies++) {
+          for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
+            for (auto jSpecies = 0ul; jSpecies < nSpecies; jSpecies++) {
               Jacobian_j[nSpecies+nDim][iSpecies] += Jacobian_j[jSpecies][iSpecies]*hs[iSpecies];
             }
             Jacobian_j[nSpecies+nDim][nSpecies+nDim] += Res_Visc[iSpecies]/Area*(Ru/Ms[iSpecies] +
@@ -781,16 +778,16 @@ void CNEMONSSolver::BC_IsothermalCatalytic_Wall(CGeometry *geometry,
           }
 
           // Vib.-El. Temperature
-          for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
-            for (jSpecies = 0; jSpecies < nSpecies; jSpecies++)
+          for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
+            for (auto jSpecies = 0ul; jSpecies < nSpecies; jSpecies++)
               Jacobian_j[nSpecies+nDim+1][iSpecies] += Jacobian_j[jSpecies][iSpecies]*eves[iSpecies];
             Jacobian_j[nSpecies+nDim+1][nSpecies+nDim+1] += Res_Visc[iSpecies]/Area*Cvve[iSpecies];
           }
 
           /*--- Multiply by the transformation matrix and store in Jac. ii ---*/
-          for (iVar = 0; iVar < nVar; iVar++)
-            for (jVar = 0; jVar < nVar; jVar++)
-              for (kVar = 0; kVar < nVar; kVar++)
+          for (auto iVar = 0ul; iVar < nVar; iVar++)
+            for (auto jVar = 0ul; jVar < nVar; jVar++)
+              for (auto kVar = 0ul; kVar < nVar; kVar++)
                 Jacobian_i[iVar][jVar] += Jacobian_j[iVar][kVar]*dVdU[kVar][jVar]*Area;
 
           /*--- Apply to the linear system ---*/
@@ -821,13 +818,13 @@ void CNEMONSSolver::BC_IsothermalCatalytic_Wall(CGeometry *geometry,
         /*--- Compute catalytic recombination flux ---*/
         // Ref: 10.2514/6.2022-1636
         // ws = gam_s*Ys*rho_wall*sqrt(Ru*Tw/(2*Pi*M_combine)*Area
-        for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
+        for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
           int Index = SU2_TYPE::Int(RxnTable(iSpecies,1));
           Res_Visc[iSpecies] = RxnTable(iSpecies,0)*factor*Vi[Index]/Vi[RHO_INDEX]*sqrt(1/Ms[Index]);
         }
       }
 
-      for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
+      for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
         Res_Visc[nSpecies+nDim]   += (Res_Visc[iSpecies]*hs[iSpecies])*Area;
         Res_Visc[nSpecies+nDim+1] += (Res_Visc[iSpecies]*eves[iSpecies])*Area;
       }
@@ -837,10 +834,10 @@ void CNEMONSSolver::BC_IsothermalCatalytic_Wall(CGeometry *geometry,
     }
   }
 
-  for (iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
     delete [] GradY[iSpecies];
   delete [] GradY;
-  for (iVar = 0; iVar < nVar; iVar++)
+  for (auto iVar = 0ul; iVar < nVar; iVar++)
     delete [] dVdU[iVar];
   delete [] dVdU;
 }
@@ -853,26 +850,26 @@ void CNEMONSSolver::BC_Smoluchowski_Maxwell(CGeometry *geometry,
                                             unsigned short val_marker) {
 
 
-  bool ionization = config->GetIonization();
+  const bool ionization = config->GetIonization();
 
   if (ionization) {
     SU2_MPI::Error("NEED TO TAKE A CLOSER LOOK AT THE JACOBIAN W/ IONIZATION", CURRENT_FUNCTION);
   }
 
   /*--- Define 'proportional control' constant ---*/
-  su2double C = 1;
+  const su2double C = 1;
 
   /*---Define under-relaxation factors --- */
-  su2double alpha_V = 0.1;
-  su2double alpha_T = 1.0;
+  const su2double alpha_V = 0.1;
+  const su2double alpha_T = 1.0;
 
   /*--- Identify the boundary ---*/
   string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
 
   /*--- Retrieve the specified wall temperature and accomodation coefficients---*/
-  su2double Twall = config->GetIsothermal_Temperature(Marker_Tag);
-  su2double TMAC  = 1.0;
-  su2double TAC   = 1.0;
+  const su2double Twall = config->GetIsothermal_Temperature(Marker_Tag);
+  const su2double TMAC  = 1.0;
+  const su2double TAC   = 1.0;
 
   /*--- Extract necessary indices ---*/
   const unsigned short T_INDEX   = nodes->GetTIndex();
@@ -881,7 +878,7 @@ void CNEMONSSolver::BC_Smoluchowski_Maxwell(CGeometry *geometry,
 
   /*--- Loop over boundary points to calculate energy flux ---*/
   SU2_OMP_FOR_DYN(OMP_MIN_SIZE)
-  for(auto iVertex = 0u; iVertex < geometry->nVertex[val_marker]; iVertex++) {
+  for(auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
 
     const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
@@ -889,10 +886,10 @@ void CNEMONSSolver::BC_Smoluchowski_Maxwell(CGeometry *geometry,
 
     /*--- Compute dual-grid area and boundary normal ---*/
     const auto Normal = geometry->vertex[val_marker][iVertex]->GetNormal();
-    su2double Area = GeometryToolbox::Norm(nDim, Normal);
+    const su2double Area = GeometryToolbox::Norm(nDim, Normal);
 
     su2double UnitNormal[MAXNDIM] = {0.0};
-    for (auto iDim = 0u; iDim < nDim; iDim++)
+    for (auto iDim = 0ul; iDim < nDim; iDim++)
       UnitNormal[iDim] = Normal[iDim]/Area;
 
     /*--- Compute closest normal neighbor ---*/
@@ -902,42 +899,42 @@ void CNEMONSSolver::BC_Smoluchowski_Maxwell(CGeometry *geometry,
     const auto Coord_i = geometry->nodes->GetCoord(iPoint);
     const auto Coord_j = geometry->nodes->GetCoord(jPoint);
 
-    su2double dij = GeometryToolbox::Distance(nDim, Coord_i, Coord_j);
+    const su2double dij = GeometryToolbox::Distance(nDim, Coord_i, Coord_j);
 
     /*--- Calculate Pressure ---*/
-    su2double Pi   = nodes->GetPressure(iPoint);
+    const su2double Pi   = nodes->GetPressure(iPoint);
 
     /*--- Calculate the gradient of temperature ---*/
-    su2double Ti   = nodes->GetTemperature(iPoint);
-    su2double Tj   = nodes->GetTemperature(jPoint);
-    su2double Tvei = nodes->GetTemperature_ve(iPoint);
-    su2double Tvej = nodes->GetTemperature_ve(jPoint);
+    const su2double Ti   = nodes->GetTemperature(iPoint);
+    const su2double Tj   = nodes->GetTemperature(jPoint);
+    const su2double Tvei = nodes->GetTemperature_ve(iPoint);
+    const su2double Tvej = nodes->GetTemperature_ve(jPoint);
 
     /*--- Rename variables for convenience ---*/
-    su2double ktr  = nodes->GetThermalConductivity(iPoint);
-    su2double kve  = nodes->GetThermalConductivity_ve(iPoint);
+    const su2double ktr  = nodes->GetThermalConductivity(iPoint);
+    const su2double kve  = nodes->GetThermalConductivity_ve(iPoint);
 
     /*--- Retrieve Cv*density ---*/
-    su2double rhoCvtr = nodes->GetRhoCv_tr(iPoint);
-    su2double rhoCvve = nodes->GetRhoCv_ve(iPoint);
+    const su2double rhoCvtr = nodes->GetRhoCv_tr(iPoint);
+    const su2double rhoCvve = nodes->GetRhoCv_ve(iPoint);
 
     /*--- Retrieve Flow Data ---*/
-    su2double Viscosity = nodes->GetLaminarViscosity(iPoint);
-    su2double Density   = nodes->GetDensity(iPoint);
-    su2double Gamma     = nodes->GetGamma(iPoint);
+    const  su2double Viscosity = nodes->GetLaminarViscosity(iPoint);
+    const su2double Density   = nodes->GetDensity(iPoint);
+    const su2double Gamma     = nodes->GetGamma(iPoint);
 
     /*--- Retrieve Primitive Gradients ---*/
     const auto Grad_PrimVar = nodes->GetGradient_Primitive(iPoint);
 
     /*--- Calculate specific gas constant --- */
-    su2double GasConstant = FluidModel->ComputeGasConstant();
+    const su2double GasConstant = FluidModel->ComputeGasConstant();
 
     /*--- Calculate temperature gradients normal to surface---*/ //Doubt about minus sign
-    su2double dTn = GeometryToolbox::DotProduct(nDim, Grad_PrimVar[T_INDEX], UnitNormal);
-    su2double dTven = GeometryToolbox::DotProduct(nDim, Grad_PrimVar[TVE_INDEX], UnitNormal);
+    const su2double dTn = GeometryToolbox::DotProduct(nDim, Grad_PrimVar[T_INDEX], UnitNormal);
+    const su2double dTven = GeometryToolbox::DotProduct(nDim, Grad_PrimVar[TVE_INDEX], UnitNormal);
 
     /*--- Calculate molecular mean free path ---*/
-    su2double Lambda = Viscosity/Density*sqrt(PI_NUMBER/(2.0*GasConstant*Ti));
+    const su2double Lambda = Viscosity/Density*sqrt(PI_NUMBER/(2.0*GasConstant*Ti));
 
     /*--- Calculate Temperature Slip ---*/
     su2double Tslip = ((2.0-TAC)/TAC)*2.0*Gamma/(Gamma+1.0)/Prandtl_Lam*Lambda*dTn+Twall;
@@ -947,18 +944,18 @@ void CNEMONSSolver::BC_Smoluchowski_Maxwell(CGeometry *geometry,
 
     /*--- Calculate temperature gradients tangent to surface ---*/
     su2double Vector_Tangent_dT[MAXNDIM] = {0.0}, Vector_Tangent_dTve[MAXNDIM] = {0.0};
-    for (auto iDim = 0u; iDim < nDim; iDim++) {
+    for (auto iDim = 0ul; iDim < nDim; iDim++) {
       Vector_Tangent_dT[iDim]   = Grad_PrimVar[T_INDEX][iDim] - dTn * UnitNormal[iDim];
       Vector_Tangent_dTve[iDim] = Grad_PrimVar[TVE_INDEX][iDim] - dTven * UnitNormal[iDim];
     }
 
     /*--- Calculate Heatflux tangent to surface ---*/
     su2double Vector_Tangent_HF[MAXNDIM] = {0.0};
-    for (auto iDim = 0u; iDim < nDim; iDim++)
+    for (auto iDim = 0ul; iDim < nDim; iDim++)
       Vector_Tangent_HF[iDim] = -ktr*Vector_Tangent_dT[iDim]-kve*Vector_Tangent_dTve[iDim];
 
     /*--- Initialize viscous residual to zero ---*/
-    for (auto iVar = 0u; iVar < nVar; iVar ++) Res_Visc[iVar] = 0.0;
+    for (auto iVar = 0ul; iVar < nVar; iVar ++) Res_Visc[iVar] = 0.0;
 
     /*--- Compute wall shear stress (using the stress tensor) ---*/
     su2double Tau[MAXNDIM][MAXNDIM] = {{0.0}};
@@ -968,20 +965,20 @@ void CNEMONSSolver::BC_Smoluchowski_Maxwell(CGeometry *geometry,
     GeometryToolbox::TangentProjection(nDim,Tau,UnitNormal,TauTangent);
 
     /*--- Store the Slip Velocity at the wall */
-    for (auto iDim = 0u; iDim < nDim; iDim++)
+    for (auto iDim = 0ul; iDim < nDim; iDim++)
       Vector[iDim] = Lambda/Viscosity*(2.0-TMAC)/TMAC*(TauTangent[iDim])-3.0/4.0*(Gamma-1.0)/Gamma*Prandtl_Lam/Pi*Vector_Tangent_HF[iDim];
 
     /*--- Apply under-relaxation ---*/
     Tslip    = (1.0-alpha_T)*nodes->GetTemperature(iPoint)+(alpha_T)*Tslip;
     Tslip_ve = (1.0-alpha_T)*nodes->GetTemperature_ve(iPoint)+(alpha_T)*Tslip_ve;
 
-    for (auto iDim = 0u; iDim < nDim; iDim++){
+    for (auto iDim = 0ul; iDim < nDim; iDim++){
       Vector[iDim] = (1.0-alpha_V)*nodes->GetVelocity(iPoint,iDim)+(alpha_V)*Vector[iDim];
     }
 
     nodes->SetVelocity_Old(iPoint,Vector);
 
-    for (auto iDim = 0u; iDim < nDim; iDim++) {
+    for (auto iDim = 0ul; iDim < nDim; iDim++) {
       LinSysRes(iPoint, nSpecies+iDim) = 0.0;
       nodes->SetVal_ResTruncError_Zero(iPoint,nSpecies+iDim);
     }

From 3b44b82fad224917a8911b56fd2e0f6f53446c2a Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 14 Feb 2023 14:35:28 +0100
Subject: [PATCH 199/656] Pulled changes from develop

---
 SU2_CFD/include/drivers/CDriver.hpp           | 443 ++++++--------
 .../include/numerics/NEMO/NEMO_diffusion.hpp  |   2 +-
 SU2_CFD/include/solvers/CMeshSolver.hpp       |   5 +-
 SU2_CFD/include/solvers/CSolver.hpp           |  12 +-
 SU2_CFD/src/drivers/CDriver.cpp               |  12 +-
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        |   4 +-
 SU2_CFD/src/iteration/CIteration.cpp          |   2 +-
 SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp  |   2 +-
 SU2_CFD/src/python_wrapper_structure.cpp      | 559 +++++-------------
 SU2_CFD/src/solvers/CMeshSolver.cpp           |   2 +-
 .../disc_adj_unsteadyCHT_cylinder/solid.cfg   |   1 -
 TestCases/disc_adj_heat/disc_adj_heat.cfg     |   4 +-
 TestCases/hybrid_regression.py                |  10 +-
 .../chtPinArray_2d/of_grad_findiff.csv.ref    |   2 +-
 .../chtPinArray_3d/configSolid.cfg            |   1 -
 TestCases/parallel_regression.py              |  19 +-
 TestCases/parallel_regression_AD.py           |  60 +-
 17 files changed, 401 insertions(+), 739 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index 5481a8e9a97..66fb0665aa7 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -1,5 +1,5 @@
-/*!
- * \file driver_structure.hpp
+/*!
+ * \file CDriver.hpp
  * \brief Headers of the main subroutines for driving single or multi-zone problems.
  *        The subroutines and functions are in the <i>driver_structure.cpp</i> file.
  * \author T. Economon, H. Kline, R. Sanchez
@@ -28,13 +28,12 @@
 
 #pragma once
 
+#include "../../../Common/include/geometry/CGeometry.hpp"
 #include "../../../Common/include/parallelization/mpi_structure.hpp"
-
 #include "../integration/CIntegration.hpp"
-#include "../solvers/CSolver.hpp"
 #include "../interfaces/CInterface.hpp"
-
-#include "../../../Common/include/geometry/CGeometry.hpp"
+#include "../solvers/CSolver.hpp"
+#include "CDriverBase.hpp"
 
 using namespace std;
 
@@ -49,69 +48,49 @@ class COutput;
  * \brief Parent class for driving an iteration of a single or multi-zone problem.
  * \author T. Economon
  */
-class CDriver {
-protected:
-  int rank,   /*!< \brief MPI Rank. */
-  size;         /*!< \brief MPI Size. */
-  char* config_file_name;                       /*!< \brief Configuration file name of the problem.*/
-  char runtime_file_name[MAX_STRING_SIZE];
-  su2double StartTime,                          /*!< \brief Start point of the timer for performance benchmarking.*/
-            StopTime,                           /*!< \brief Stop point of the timer for performance benchmarking.*/
-            UsedTimePreproc,                    /*!< \brief Elapsed time between Start and Stop point of the timer for tracking preprocessing phase.*/
-            UsedTimeCompute,                    /*!< \brief Elapsed time between Start and Stop point of the timer for tracking compute phase.*/
-            UsedTimeOutput,                     /*!< \brief Elapsed time between Start and Stop point of the timer for tracking output phase.*/
-            UsedTime;                           /*!< \brief Elapsed time between Start and Stop point of the timer.*/
-  su2double BandwidthSum = 0.0;                 /*!< \brief Aggregate value of the bandwidth for writing restarts (to be average later).*/
-  unsigned long IterCount,                      /*!< \brief Iteration count stored for performance benchmarking.*/
-  OutputCount;                                  /*!< \brief Output count stored for performance benchmarking.*/
-  unsigned long DOFsPerPoint;                   /*!< \brief Number of unknowns at each vertex, i.e., number of equations solved. */
-  su2double Mpoints;                            /*!< \brief Total number of grid points in millions in the calculation (including ghost points).*/
-  su2double MpointsDomain;                      /*!< \brief Total number of grid points in millions in the calculation (excluding ghost points).*/
-  su2double MDOFs;                              /*!< \brief Total number of DOFs in millions in the calculation (including ghost points).*/
-  su2double MDOFsDomain;                        /*!< \brief Total number of DOFs in millions in the calculation (excluding ghost points).*/
-  unsigned long TimeIter;                       /*!< \brief External iteration.*/
-  ofstream **ConvHist_file;                     /*!< \brief Convergence history file.*/
-  ofstream FSIHist_file;                        /*!< \brief FSI convergence history file.*/
-  unsigned short iMesh,                         /*!< \brief Iterator on mesh levels.*/
-                iZone,                          /*!< \brief Iterator on zones.*/
-                nZone,                          /*!< \brief Total number of zones in the problem. */
-                nDim,                           /*!< \brief Number of dimensions.*/
-                iInst,                          /*!< \brief Iterator on instance levels.*/
-                *nInst,                         /*!< \brief Total number of instances in the problem (per zone). */
-                **interface_types;              /*!< \brief Type of coupling between the distinct (physical) zones.*/
-  bool StopCalc,                                /*!< \brief Stop computation flag.*/
-       mixingplane,                             /*!< \brief mixing-plane simulation flag.*/
-       fsi,                                     /*!< \brief FSI simulation flag.*/
-       fem_solver;                              /*!< \brief FEM fluid solver simulation flag. */
-  CIteration ***iteration_container;            /*!< \brief Container vector with all the iteration methods. */
-  COutput **output_container;                   /*!< \brief Pointer to the COutput class. */
-  CIntegration ****integration_container;       /*!< \brief Container vector with all the integration methods. */
-  CGeometry ****geometry_container;             /*!< \brief Geometrical definition of the problem. */
-  CSolver *****solver_container;                /*!< \brief Container vector with all the solutions. */
-  CNumerics ******numerics_container;           /*!< \brief Description of the numerical method (the way in which the equations are solved). */
-  CConfig **config_container;                   /*!< \brief Definition of the particular problem. */
-  CConfig *driver_config;                       /*!< \brief Definition of the driver configuration. */
-  COutput *driver_output;                       /*!< \brief Definition of the driver output. */
-  CSurfaceMovement **surface_movement;          /*!< \brief Surface movement classes of the problem. */
-  CVolumetricMovement ***grid_movement;         /*!< \brief Volume grid movement classes of the problem. */
-  CFreeFormDefBox*** FFDBox;                    /*!< \brief FFD FFDBoxes of the problem. */
-  vector<vector<unique_ptr<CInterpolator> > >
-  interpolator_container;                       /*!< \brief Definition of the interpolation method between non-matching discretizations of the interface. */
-  CInterface ***interface_container;            /*!< \brief Definition of the interface of information and physics. */
-  bool dry_run;                                 /*!< \brief Flag if SU2_CFD was started as dry-run via "SU2_CFD -d <config>.cfg" */
-
-public:
 
+class CDriver : public CDriverBase {
+ protected:
+  char runtime_file_name[MAX_STRING_SIZE];
+  su2double
+      UsedTimeOutput; /*!< \brief Elapsed time between Start and Stop point of the timer for tracking output phase.*/
+
+  su2double BandwidthSum =
+      0.0;                    /*!< \brief Aggregate value of the bandwidth for writing restarts (to be average later).*/
+  unsigned long IterCount,    /*!< \brief Iteration count stored for performance benchmarking.*/
+      OutputCount;            /*!< \brief Output count stored for performance benchmarking.*/
+  unsigned long DOFsPerPoint; /*!< \brief Number of unknowns at each vertex, i.e., number of equations solved. */
+  su2double Mpoints; /*!< \brief Total number of grid points in millions in the calculation (including ghost points).*/
+  su2double
+      MpointsDomain; /*!< \brief Total number of grid points in millions in the calculation (excluding ghost points).*/
+  su2double MDOFs;   /*!< \brief Total number of DOFs in millions in the calculation (including ghost points).*/
+  su2double MDOFsDomain; /*!< \brief Total number of DOFs in millions in the calculation (excluding ghost points).*/
+
+  ofstream** ConvHist_file; /*!< \brief Convergence history file.*/
+  ofstream FSIHist_file;    /*!< \brief FSI convergence history file.*/
+
+  bool StopCalc,   /*!< \brief Stop computation flag.*/
+      mixingplane, /*!< \brief mixing-plane simulation flag.*/
+      fsi,         /*!< \brief FSI simulation flag.*/
+      fem_solver;  /*!< \brief FEM fluid solver simulation flag. */
+
+  CIteration*** iteration_container;      /*!< \brief Container vector with all the iteration methods. */
+  CIntegration**** integration_container; /*!< \brief Container vector with all the integration methods. */
+  vector<vector<unique_ptr<CInterpolator>>>
+      interpolator_container; /*!< \brief Definition of the interpolation method between non-matching discretizations of
+                                 the interface. */
+  CInterface*** interface_container; /*!< \brief Definition of the interface of information and physics. */
+  bool dry_run;                      /*!< \brief Flag if SU2_CFD was started as dry-run via "SU2_CFD -d <config>.cfg" */
+
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] confFile - Configuration file name.
    * \param[in] val_nZone - Total number of zones.
-   * \param[in] val_nDim - Number of dimensions.
    * \param[in] MPICommunicator - MPI communicator for SU2.
+   * \param[in] dummy_geo - Dummy geometric definition of the problem.
    */
-  CDriver(char* confFile,
-          unsigned short val_nZone,
-          SU2_Comm MPICommunicator, bool dummy_geo);
+  CDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator, bool dummy_geo);
 
   /*!
    * \brief Destructor of the class.
@@ -121,10 +100,9 @@ class CDriver {
   /*!
    * \brief A virtual member.
    */
-  virtual void Run() { };
-
-protected:
+  virtual void Run(){};
 
+ protected:
   /*!
    * \brief Init_Containers
    */
@@ -132,145 +110,180 @@ class CDriver {
 
   /*!
    * \brief Read in the config and mesh files.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] driver_config - Definition of the driver configuration.
    */
-  void Input_Preprocessing(CConfig **&config, CConfig *&driver_config);
+  void Input_Preprocessing(CConfig**& config, CConfig*& driver_config);
 
   /*!
-   * \brief Construction of the edge-based data structure and the multigrid structure.
+   * \brief Construction of the edge-based data structure and the multi-grid structure.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] dummy - Definition of the dummy driver.
    */
-  void Geometrical_Preprocessing(CConfig *config, CGeometry **&geometry, bool dummy);
+  void Geometrical_Preprocessing(CConfig* config, CGeometry**& geometry, bool dummy);
 
   /*!
    * \brief Do the geometrical preprocessing for the DG FEM solver.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Geometrical definition of the problem.
    */
-  void Geometrical_Preprocessing_DGFEM(CConfig *config, CGeometry **&geometry);
+  void Geometrical_Preprocessing_DGFEM(CConfig* config, CGeometry**& geometry);
 
   /*!
    * \brief Geometrical_Preprocessing_FVM
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Geometrical definition of the problem.
    */
-  void Geometrical_Preprocessing_FVM(CConfig *config, CGeometry **&geometry);
+  void Geometrical_Preprocessing_FVM(CConfig* config, CGeometry**& geometry);
 
   /*!
    * \brief Definition of the physics iteration class or within a single zone.
-   * \param[in] iteration_container - Pointer to the iteration container to be instantiated.
    * \param[in] config - Definition of the particular problem.
-   * \param[in] iZone - Index of the zone.
+   * \param[in] iteration - Pointer to the iteration container to be instantiated.
    */
-  void Iteration_Preprocessing(CConfig *config, CIteration *&iteration) const;
+  void Iteration_Preprocessing(CConfig* config, CIteration*& iteration) const;
 
   /*!
    * \brief Definition and allocation of all solution classes.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver - Container vector with all the solutions.
    */
-  void Solver_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***&solver);
+  void Solver_Preprocessing(CConfig* config, CGeometry** geometry, CSolver***& solver);
 
   /*!
    * \brief Restart of the solvers from the restart files.
-   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] solver - Container vector with all the solutions.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
+   * \param[in] update_geo - Boolean to indicate if geometry should be updated.
    */
-  void Solver_Restart(CSolver ***solver, CGeometry **geometry, CConfig *config, bool update_geo);
+  void Solver_Restart(CSolver*** solver, CGeometry** geometry, CConfig* config, bool update_geo);
 
   /*!
    * \brief Definition and allocation of all solution classes.
-   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] solver - Container vector with all the solutions.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
+   * \param[in] val_iInst - Current solver instance.
    */
-  void Solver_Postprocessing(CSolver ****solver, CGeometry **geometry, CConfig *config, unsigned short val_iInst);
+  void Solver_Postprocessing(CSolver**** solver, CGeometry** geometry, CConfig* config, unsigned short val_iInst);
 
   /*!
    * \brief Definition and allocation of all integration classes.
    * \param[in] config - Definition of the particular problem.
    * \param[in] solver - Container vector with all the solutions.
-   * \param[out] integration - Container vector with all the integration methods.
+   * \param[in] integration - Container vector with all the integration methods.
    */
-  void Integration_Preprocessing(CConfig *config, CSolver **solver, CIntegration **&integration) const;
+  void Integration_Preprocessing(CConfig* config, CSolver** solver, CIntegration**& integration) const;
 
   /*!
    * \brief Definition and allocation of all integration classes.
-   * \param[in] integration_container - Container vector with all the integration methods.
+   * \param[in] integration - Container vector with all the integration methods.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
+   * \param[in] val_iInst - Current solver instance.
    */
-  void Integration_Postprocessing(CIntegration ***integration, CGeometry **geometry, CConfig *config, unsigned short val_iInst);
+  void Integration_Postprocessing(CIntegration*** integration, CGeometry** geometry, CConfig* config,
+                                  unsigned short val_iInst);
 
   /*!
    * \brief Definition and allocation of all interface classes.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] solver - Container vector with all the solutions.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] interface_types - Type of coupling between the distinct (physical) zones.
+   * \param[in] interface - Class defining the physical transfer of information.
+   * \param[in] interpolation -  Object defining the interpolation.
    */
-  void Interface_Preprocessing(CConfig **config, CSolver *****solver, CGeometry ****geometry,
-                               unsigned short **interface_types, CInterface ***interface,
-                               vector<vector<unique_ptr<CInterpolator> > > &interpolation);
+  void Interface_Preprocessing(CConfig** config, CSolver***** solver, CGeometry**** geometry,
+                               unsigned short** interface_types, CInterface*** interface,
+                               vector<vector<unique_ptr<CInterpolator>>>& interpolation);
 
   /*!
    * \brief Definition and allocation of all solver classes.
-   * \param[in] numerics_container - Description of the numerical method (the way in which the equations are solved).
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] solver_container - Container vector with all the solutions.
    * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver - Container vector with all the solutions.
+   * \param[in] numerics - Description of the numerical method (the way in which the equations are solved).
    */
-  void Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***solver, CNumerics ****&numerics) const;
+  void Numerics_Preprocessing(CConfig* config, CGeometry** geometry, CSolver*** solver, CNumerics****& numerics) const;
 
   /*!
    * \brief Helper to instantiate turbulence numerics specialized for different flow solvers.
    */
   template <class FlowIndices>
-  void InstantiateTurbulentNumerics(unsigned short nVar_Turb, int offset, const CConfig *config,
-                                    const CSolver* turb_solver, CNumerics ****&numerics) const;
+  void InstantiateTurbulentNumerics(unsigned short nVar_Turb, int offset, const CConfig* config,
+                                    const CSolver* turb_solver, CNumerics****& numerics) const;
 
   /*!
    * \brief Helper to instantiate transition numerics specialized for different flow solvers.
    */
   template <class FlowIndices>
-  void InstantiateTransitionNumerics(unsigned short nVar_Trans, int offset, const CConfig *config,
-                                    const CSolver* trans_solver, CNumerics ****&numerics) const;
+  void InstantiateTransitionNumerics(unsigned short nVar_Trans, int offset, const CConfig* config,
+                                     const CSolver* trans_solver, CNumerics****& numerics) const;
   /*!
    * \brief Helper to instantiate species transport numerics specialized for different flow solvers.
    */
   template <class FlowIndices>
-  void InstantiateSpeciesNumerics(unsigned short nVar_Species, int offset, const CConfig *config,
-                                  const CSolver* species_solver, CNumerics ****&numerics) const;
+  void InstantiateSpeciesNumerics(unsigned short nVar_Species, int offset, const CConfig* config,
+                                  const CSolver* species_solver, CNumerics****& numerics) const;
 
   /*!
    * \brief Definition and allocation of all solver classes.
-   * \param[in] numerics_container - Description of the numerical method (the way in which the equations are solved).
-   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] numerics - Description of the numerical method (the way in which the equations are solved).
+   * \param[in] solver - Container vector with all the solutions.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
+   * \param[in] val_iInst - Current solver instance.
    */
-  void Numerics_Postprocessing(CNumerics *****numerics, CSolver ***solver, CGeometry **geometry, CConfig *config, unsigned short val_iInst);
+  void Numerics_Postprocessing(CNumerics***** numerics, CSolver*** solver, CGeometry** geometry, CConfig* config,
+                               unsigned short val_iInst);
 
   /*!
    * \brief GridMovement_Preprocessing
-   * \param config
-   * \param geometry
-   * \param solver
-   * \param iteration
-   * \param grid_movement
-   * \param surface_movement
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver - Container vector with all the solutions.
+   * \param[in] iteration - Container vector with all the iteration methods.
+   * \param[in] grid_movement - Volume grid movement classes of the problem.
+   * \param[in] surface_movement - Surface movement classes of the problem.
    */
-  void DynamicMesh_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***solver, CIteration *iteration, CVolumetricMovement *&grid_movement, CSurfaceMovement *&surface_movement) const;
+  void DynamicMesh_Preprocessing(CConfig* config, CGeometry** geometry, CSolver*** solver, CIteration* iteration,
+                                 CVolumetricMovement*& grid_movement, CSurfaceMovement*& surface_movement) const;
 
   /*!
    * \brief Initialize Python interface functionalities
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver - Container vector with all the solutions.
    */
   void PythonInterface_Preprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver);
 
   /*!
    * \brief Preprocess the output container.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] driver_config - Definition of the driver configuration.
+   * \param[in] output_container - Container vector with all the outputs.
+   * \param[in] driver_output - Definition of the driver output.
    */
-  void Output_Preprocessing(CConfig **config, CConfig *driver_config, COutput **&output_container, COutput *&driver_output);
+  void Output_Preprocessing(CConfig** config, CConfig* driver_config, COutput**& output_container,
+                            COutput*& driver_output);
 
   /*!
    * \brief Initiate value for static mesh movement such as the gridVel for the ROTATING frame.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Geometrical definition of the problem.
    */
-  void StaticMesh_Preprocessing(const CConfig *config, CGeometry **geometry);
+  void StaticMesh_Preprocessing(const CConfig* config, CGeometry** geometry);
 
   /*!
    * \brief Initiate value for static mesh movement such as the gridVel for the ROTATING frame.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver - Container vector with all the solutions.
+   * \param[in] interface - Class defining the physical transfer of information.
    */
   void Turbomachinery_Preprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver,
                                     CInterface*** interface);
@@ -320,14 +333,14 @@ class CDriver {
   virtual void Relaxation_Tractions(unsigned short donorZone, unsigned short targetZone, unsigned long iOuterIter) {}
 
   /*!
-   * \brief A virtual member to run a Block Gauss-Seidel iteration in multizone problems.
+   * \brief A virtual member to run a Block Gauss-Seidel iteration in multi-zone problems.
    */
-  virtual void Run_GaussSeidel(){}
+  virtual void Run_GaussSeidel() {}
 
   /*!
-   * \brief A virtual member to run a Block-Jacobi iteration in multizone problems.
+   * \brief A virtual member to run a Block-Jacobi iteration in multi-zone problems.
    */
-  virtual void Run_Jacobi(){}
+  virtual void Run_Jacobi() {}
 
   /*!
    * \brief A virtual member.
@@ -340,8 +353,7 @@ class CDriver {
    */
   void Print_DirectResidual(RECORDING kind_recording);
 
-public:
-
+ public:
   /*!
    * \brief Launch the computation for all zones and all physics.
    */
@@ -360,35 +372,37 @@ class CDriver {
   /*!
    * \brief Perform some pre-processing before an iteration of the physics.
    */
-  virtual void Preprocess(unsigned long TimeIter){ }
+  virtual void Preprocess(unsigned long TimeIter) {}
 
   /*!
    * \brief Monitor the computation.
    */
-  virtual bool Monitor(unsigned long TimeIter){ return false; }
+  virtual bool Monitor(unsigned long TimeIter) { return false; }
 
   /*!
    * \brief Output the solution in solution file.
    */
-  virtual void Output(unsigned long TimeIter){ }
+  virtual void Output(unsigned long TimeIter) {}
 
   /*!
-   * \brief Perform a dynamic mesh deformation, including grid velocity computation and update of the multigrid structure.
+   * \brief Perform a dynamic mesh deformation, including grid velocity computation and update of the multi-grid
+   * structure.
    */
-  virtual void DynamicMeshUpdate(unsigned long TimeIter) { }
+  virtual void DynamicMeshUpdate(unsigned long TimeIter) {}
 
   /*!
-   * \brief Perform a dynamic mesh deformation, including grid velocity computation and update of the multigrid structure.
+   * \brief Perform a dynamic mesh deformation, including grid velocity computation and update of the multi-grid
+   * structure.
    */
-  virtual void DynamicMeshUpdate(unsigned short val_iZone, unsigned long TimeIter) { }
+  virtual void DynamicMeshUpdate(unsigned short val_iZone, unsigned long TimeIter) {}
 
   /*!
    * \brief Perform a mesh deformation as initial condition.
    */
-  virtual void SetInitialMesh() { }
+  virtual void SetInitialMesh() {}
 
   /*!
-   * \brief Process the boundary conditions and update the multigrid structure.
+   * \brief Process the boundary conditions and update the multi-grid structure.
    */
   void BoundaryConditionsUpdate();
 
@@ -434,28 +448,6 @@ class CDriver {
    */
   passivedouble Get_LiftCoeff() const;
 
-  /*!
-   * \brief Get the number of vertices (halo nodes included) from a specified marker.
-   * \param[in] iMarker -  Marker identifier.
-   * \return Number of vertices.
-   */
-  unsigned long GetNumberVertices(unsigned short iMarker) const;
-
-  /*!
-   * \brief Get the number of halo vertices from a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \return Number of vertices.
-   */
-  unsigned long GetNumberHaloVertices(unsigned short iMarker) const;
-
-  /*!
-   * \brief Check if a vertex is physical or not (halo node) on a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return True if the specified vertex is a halo node.
-   */
-  bool IsAHaloNode(unsigned short iMarker, unsigned long iVertex) const;
-
   /*!
    * \brief Get the number of external iterations.
    * \return Number of external iterations.
@@ -480,22 +472,6 @@ class CDriver {
    */
   string GetSurfaceFileName() const;
 
-  /*!
-   * \brief Get the global index of a vertex on a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Vertex global index.
-   */
-  unsigned long GetVertexGlobalIndex(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Get undeformed coordinates from the mesh solver.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return x,y,z coordinates of the vertex.
-   */
-  vector<passivedouble> GetInitialMeshCoord(unsigned short iMarker, unsigned long iVertex) const;
-
   /*!
    * \brief Get the temperature at a vertex on a specified marker.
    * \param[in] iMarker - Marker identifier.
@@ -550,77 +526,19 @@ class CDriver {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void Inlet_Preprocessing(CSolver ***solver, CGeometry **geometry, CConfig *config) const;
-
-  /*!
-   * \brief Get the normal (vector) at a vertex on a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \param[in] unitNormal - Bool to normalise the vector.
-   * \return Normal (vector) at the vertex.
-   */
-  vector<passivedouble> GetVertexNormal(unsigned short iMarker, unsigned long iVertex, bool unitNormal = false) const;
-
-  /*!
-   * \brief Get the unit normal (vector) at a vertex on a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Unit normal (vector) at the vertex.
-   */
-  inline vector<passivedouble> GetVertexUnitNormal(unsigned short iMarker, unsigned long iVertex) const {
-    return GetVertexNormal(iMarker, iVertex, true);
-  }
-
-  /*!
-   * \brief Get all the boundary markers tags.
-   * \return List of boundary markers tags.
-   */
-  vector<string> GetAllBoundaryMarkersTag() const;
-
-  /*!
-   * \brief Get all the deformable boundary marker tags.
-   * \return List of deformable boundary markers tags.
-   */
-  vector<string> GetAllDeformMeshMarkersTag() const;
+  void Inlet_Preprocessing(CSolver*** solver, CGeometry** geometry, CConfig* config) const;
 
   /*!
-   * \brief Get all the heat transfer boundary markers tags.
-   * \return List of heat transfer boundary markers tags.
+   * \brief Get all the CHT boundary marker tags.
+   * \return List of CHT boundary markers tags.
    */
-  vector<string> GetAllCHTMarkersTag() const;
+  vector<string> GetCHTMarkerTags() const;
 
   /*!
-   * \brief Get all the (subsonic) inlet boundary markers tags.
+   * \brief Get all the inlet boundary marker tags.
    * \return List of inlet boundary markers tags.
    */
-  vector<string> GetAllInletMarkersTag() const;
-
-  /*!
-   * \brief Get all the boundary markers tags with their associated indices.
-   * \return List of boundary markers tags with their indices.
-   */
-  map<string, int> GetAllBoundaryMarkers() const;
-
-  /*!
-   * \brief Get all the boundary markers tags with their associated types.
-   * \return List of boundary markers tags with their types.
-   */
-  map<string, string> GetAllBoundaryMarkersType() const;
-
-  /*!
-   * \brief Set the mesh displacement for the elasticity mesh solver.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \param[in] DispX - Value of the mesh displacement in the direction X.
-   * \param[in] DispY - Value of the mesh displacement in the direction Y.
-   * \param[in] DispZ - Value of the mesh displacement in the direction Z.
-   */
-  void SetMeshDisplacement(unsigned short iMarker, unsigned long iVertex, passivedouble DispX, passivedouble DispY, passivedouble DispZ);
-
-  /*!
-   * \brief Communicate the boundary mesh displacements in a python call
-   */
-  void CommunicateMeshDisplacement(void);
+  vector<string> GetInletMarkerTags() const;
 
   /*!
    * \brief Return the sensitivities of the mesh boundary vertices.
@@ -638,8 +556,8 @@ class CDriver {
    * \param[in] LoadX - Value of the load in the direction Y.
    * \param[in] LoadX - Value of the load in the direction Z.
    */
-  void SetFEA_Loads(unsigned short iMarker, unsigned long iVertex, passivedouble LoadX,
-                    passivedouble LoadY, passivedouble LoadZ);
+  void SetFEA_Loads(unsigned short iMarker, unsigned long iVertex, passivedouble LoadX, passivedouble LoadY,
+                    passivedouble LoadZ);
 
   /*!
    * \brief Return the displacements from the FEA solver.
@@ -693,7 +611,7 @@ class CDriver {
    * \param[in] val_AdjointZ - Value of the adjoint in the direction Z.
    */
   void SetFlowLoad_Adjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
-                                    passivedouble val_AdjointY, passivedouble val_AdjointZ);
+                           passivedouble val_AdjointY, passivedouble val_AdjointZ);
 
   /*!
    * \brief Set the adjoint of the structural displacements (from an outside source)
@@ -706,7 +624,7 @@ class CDriver {
   void SetSourceTerm_DispAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
                                  passivedouble val_AdjointY, passivedouble val_AdjointZ);
   void SetSourceTerm_VelAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
-                                 passivedouble val_AdjointY, passivedouble val_AdjointZ);
+                                passivedouble val_AdjointY, passivedouble val_AdjointZ);
 
   /*!
    * \brief Set the position of the heat source.
@@ -746,7 +664,7 @@ class CDriver {
    * \param[in] solution - Solution object with interface (iPoint,iVar).
    * \tparam Old - If true set "old solutions" instead.
    */
-  template<class Container, bool Old = false>
+  template <class Container, bool Old = false>
   void SetAllSolutions(unsigned short iZone, bool adjoint, const Container& solution) {
     const auto nPoint = geometry_container[iZone][INST_0][MESH_0]->GetnPoint();
     for (auto iSol = 0u, offset = 0u; iSol < MAX_SOLS; ++iSol) {
@@ -754,8 +672,11 @@ class CDriver {
       if (!(solver && (solver->GetAdjoint() == adjoint))) continue;
       for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint)
         for (auto iVar = 0ul; iVar < solver->GetnVar(); ++iVar)
-          if (!Old) solver->GetNodes()->SetSolution(iPoint, iVar, solution(iPoint,offset+iVar));
-          else solver->GetNodes()->SetSolution_Old(iPoint, iVar, solution(iPoint,offset+iVar));
+          if (!Old) {
+            solver->GetNodes()->SetSolution(iPoint, iVar, solution(iPoint, offset + iVar));
+          } else {
+            solver->GetNodes()->SetSolution_Old(iPoint, iVar, solution(iPoint, offset + iVar));
+          }
       offset += solver->GetnVar();
     }
   }
@@ -763,9 +684,9 @@ class CDriver {
   /*!
    * \brief Set the "old solution" of all solvers (adjoint or primal) in a zone.
    */
-  template<class Container>
+  template <class Container>
   void SetAllSolutionsOld(unsigned short iZone, bool adjoint, const Container& solution) {
-    SetAllSolutions<Container,true>(iZone, adjoint, solution);
+    SetAllSolutions<Container, true>(iZone, adjoint, solution);
   }
 
   /*!
@@ -774,7 +695,7 @@ class CDriver {
    * \param[in] adjoint - True to consider adjoint solvers instead of primal.
    * \param[out] solution - Solution object with interface (iPoint,iVar).
    */
-  template<class Container>
+  template <class Container>
   void GetAllSolutions(unsigned short iZone, bool adjoint, Container& solution) const {
     const auto nPoint = geometry_container[iZone][INST_0][MESH_0]->GetnPoint();
     for (auto iSol = 0u, offset = 0u; iSol < MAX_SOLS; ++iSol) {
@@ -783,11 +704,10 @@ class CDriver {
       const auto& sol = solver->GetNodes()->GetSolution();
       for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint)
         for (auto iVar = 0ul; iVar < solver->GetnVar(); ++iVar)
-          solution(iPoint,offset+iVar) = SU2_TYPE::GetValue(sol(iPoint,iVar));
+          solution(iPoint, offset + iVar) = SU2_TYPE::GetValue(sol(iPoint, iVar));
       offset += solver->GetnVar();
     }
   }
-
 };
 
 /*!
@@ -797,24 +717,19 @@ class CDriver {
  * \author T. Economon, G. Gori
  */
 class CFluidDriver : public CDriver {
+ protected:
+  unsigned long Max_Iter;
 
-protected:
-   unsigned long Max_Iter;
-
-protected:
-
+ protected:
   /*!
    * \brief Constructor of the class.
    * \param[in] confFile - Configuration file name.
    * \param[in] val_nZone - Total number of zones.
-   * \param[in] val_nDim - Number of dimensions.
    * \param[in] MPICommunicator - MPI communicator for SU2.
    */
-  CFluidDriver(char* confFile,
-               unsigned short val_nZone,
-               SU2_Comm MPICommunicator);
+  CFluidDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator);
 
-public:
+ public:
   /*!
    * \brief Destructor of the class.
    */
@@ -851,7 +766,8 @@ class CFluidDriver : public CDriver {
   void Preprocess(unsigned long Iter) override;
 
   /*!
-   * \brief Perform a dynamic mesh deformation, included grid velocity computation and the update of the multigrid structure (multiple zone).
+   * \brief Perform a dynamic mesh deformation, included grid velocity computation and the update of the multi-grid
+   * structure (multiple zone).
    */
   void DynamicMeshUpdate(unsigned long TimeIter) override;
 
@@ -859,10 +775,8 @@ class CFluidDriver : public CDriver {
    * \brief Transfer data among different zones (multiple zone).
    */
   void Transfer_Data(unsigned short donorZone, unsigned short targetZone);
-
 };
 
-
 /*!
  * \class CTurbomachineryDriver
  * \ingroup Drivers
@@ -870,22 +784,17 @@ class CFluidDriver : public CDriver {
  * \author S. Vitale
  */
 class CTurbomachineryDriver : public CFluidDriver {
-private:
+ private:
   COutputLegacy* output_legacy;
 
-public:
-
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] confFile - Configuration file name.
    * \param[in] val_nZone - Total number of zones.
-   * \param[in] val_nDim - Number of dimensions.
-   * \param[in] val_periodic - Bool for periodic BCs.
    * \param[in] MPICommunicator - MPI communicator for SU2.
    */
-  CTurbomachineryDriver(char* confFile,
-                        unsigned short val_nZone,
-                        SU2_Comm MPICommunicator);
+  CTurbomachineryDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator);
 
   /*!
    * \brief Destructor of the class.
@@ -912,9 +821,6 @@ class CTurbomachineryDriver : public CFluidDriver {
    * \brief Monitor the computation.
    */
   bool Monitor(unsigned long TimeIter) override;
-
-
-
 };
 
 /*!
@@ -924,24 +830,19 @@ class CTurbomachineryDriver : public CFluidDriver {
  * \author T. Economon
  */
 class CHBDriver : public CFluidDriver {
-
-private:
+ private:
   COutputLegacy* output_legacy;
   unsigned short nInstHB;
-  su2double **D; /*!< \brief Harmonic Balance operator. */
-
-public:
+  su2double** D; /*!< \brief Harmonic Balance operator. */
 
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] confFile - Configuration file name.
    * \param[in] val_nZone - Total number of zones.
-   * \param[in] val_nDim - Number of dimensions.
    * \param[in] MPICommunicator - MPI communicator for SU2.
    */
-  CHBDriver(char* confFile,
-            unsigned short val_nZone,
-            SU2_Comm MPICommunicator);
+  CHBDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator);
 
   /*!
    * \brief Destructor of the class.
diff --git a/SU2_CFD/include/numerics/NEMO/NEMO_diffusion.hpp b/SU2_CFD/include/numerics/NEMO/NEMO_diffusion.hpp
index 5a8a10c128a..88701d0c79d 100644
--- a/SU2_CFD/include/numerics/NEMO/NEMO_diffusion.hpp
+++ b/SU2_CFD/include/numerics/NEMO/NEMO_diffusion.hpp
@@ -94,7 +94,7 @@ class CAvgGrad_NEMO : public CNEMONumerics {
  */
 class CAvgGradCorrected_NEMO : public CNEMONumerics {
 private:
-  unsigned short iDim, iVar,
+  unsigned short
   nPrimVar, nPrimVarGrad;       /*!< \brief Iterators in dimension an variable. */
   su2double
   *Mean_PrimVar,                /*!< \brief Mean primitive variables. */
diff --git a/SU2_CFD/include/solvers/CMeshSolver.hpp b/SU2_CFD/include/solvers/CMeshSolver.hpp
index d03a841f5e3..18fb2a86ef3 100644
--- a/SU2_CFD/include/solvers/CMeshSolver.hpp
+++ b/SU2_CFD/include/solvers/CMeshSolver.hpp
@@ -133,11 +133,10 @@ class CMeshSolver final : public CFEASolver {
 
   /*!
    * \brief Set the stiffness of the mesh.
-   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] numerics - Numerics used in the solution.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetMesh_Stiffness(CGeometry **geometry,
-                         CNumerics **numerics,
+  void SetMesh_Stiffness(CNumerics **numerics,
                          CConfig *config) override;
 
   /*!
diff --git a/SU2_CFD/include/solvers/CSolver.hpp b/SU2_CFD/include/solvers/CSolver.hpp
index f87fcf58c44..954b06ad75d 100644
--- a/SU2_CFD/include/solvers/CSolver.hpp
+++ b/SU2_CFD/include/solvers/CSolver.hpp
@@ -4167,8 +4167,16 @@ class CSolver {
    * \param[in] config - Definition of the particular problem.
    * \param[in] referenceCoord - Determine if the mesh is deformed from the reference or from the current coordinates.
    */
-  inline virtual void SetMesh_Stiffness(CGeometry **geometry,
-                                        CNumerics **numerics,
+  inline virtual void DeformMesh(CGeometry *geometry,
+                                 CNumerics **numerics,
+                                 CConfig *config) { }
+
+  /*!
+   * \brief A virtual member.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] referenceCoord - Determine if the mesh is deformed from the reference or from the current coordinates.
+   */
+  inline virtual void SetMesh_Stiffness(CNumerics **numerics,
                                         CConfig *config) { }
 
   /*!
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index 121cd94e9a5..cf69fefeddd 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -107,10 +107,9 @@
 #include <fenv.h>
 
 CDriver::CDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator, bool dummy_geo) :
-  config_file_name(confFile), StartTime(0.0), StopTime(0.0), UsedTime(0.0),
-  TimeIter(0), nZone(val_nZone), StopCalc(false), fsi(false), fem_solver(false), dry_run(dummy_geo) {
+CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false), fem_solver(false), dry_run(dummy_geo) {
 
-  /*--- Initialize Medipack (must also be here so it is initialized from python) ---*/
+    /*--- Initialize Medipack (must also be here so it is initialized from python) ---*/
 #ifdef HAVE_MPI
   #if defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)
     SU2_MPI::Init_AMPI();
@@ -602,6 +601,10 @@ void CDriver::Input_Preprocessing(CConfig **&config, CConfig *&driver_config) {
     }
   }
 
+  /*--- Keep a reference to the main (ZONE 0) config. ---*/
+
+  main_config = config_container[ZONE_0];
+
   /*--- Determine whether or not the FEM solver is used, which decides the type of
    *    geometry classes that are instantiated. Only adapted for single-zone problems ---*/
 
@@ -706,6 +709,9 @@ void CDriver::Geometrical_Preprocessing(CConfig* config, CGeometry **&geometry,
 
   }
 
+  /*--- Keep a reference to the main (ZONE_0, INST_0, MESH_0) geometry. ---*/
+
+  main_geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 }
 
 void CDriver::Geometrical_Preprocessing_FVM(CConfig *config, CGeometry **&geometry) {
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index d38f5f67610..7511fdf3fe9 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -359,8 +359,8 @@ unsigned long CDataDrivenFluid::Predict_MLP(su2double rho, su2double e) {
   /* Apply exponential transformation to the MLP outputs for the first and second
      derivative of the entropy w.r.t density */
   // Optional:
-  dsdrho_e = -exp(dsdrho_e);
-  d2sdrho2 = exp(d2sdrho2);
+  //dsdrho_e = -exp(dsdrho_e);
+  //d2sdrho2 = exp(d2sdrho2);
 
   return exit_code;
 }
diff --git a/SU2_CFD/src/iteration/CIteration.cpp b/SU2_CFD/src/iteration/CIteration.cpp
index 337e24edaea..5b2eaa5cef1 100644
--- a/SU2_CFD/src/iteration/CIteration.cpp
+++ b/SU2_CFD/src/iteration/CIteration.cpp
@@ -163,7 +163,7 @@ void CIteration::SetMesh_Deformation(CGeometry** geometry, CSolver** solver, CNu
 
   /*--- Set the stiffness of each element mesh into the mesh numerics ---*/
 
-  solver[MESH_SOL]->SetMesh_Stiffness(geometry, numerics[MESH_SOL], config);
+  solver[MESH_SOL]->SetMesh_Stiffness(numerics[MESH_SOL], config);
 
   /*--- Deform the volume grid around the new boundary locations ---*/
 
diff --git a/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp b/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
index cc64e14d1e2..bb9874c1c06 100644
--- a/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
+++ b/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
@@ -293,7 +293,7 @@ CNumerics::ResidualType<> CAvgGradCorrected_NEMO::ComputeResidual(const CConfig
     Mean_PrimVar[iVar] = 0.5*(PrimVar_i[iVar]+PrimVar_j[iVar]);
   }
   for (auto iVar = nSpecies; iVar < nPrimVarGrad; iVar++) {
-    for (iDim = 0; iDim < nDim; iDim++) {
+    for (auto iDim = 0; iDim < nDim; iDim++) {
       Mean_GradPrimVar[iVar][iDim] = 0.5*(PrimVar_Grad_i[iVar][iDim] +
                                           PrimVar_Grad_j[iVar][iDim]);
     }
diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index 32672e87eef..95e8cd321f7 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -25,22 +25,18 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
+#include "../../Common/include/toolboxes/geometry_toolbox.hpp"
 #include "../include/drivers/CDriver.hpp"
 #include "../include/drivers/CSinglezoneDriver.hpp"
-#include "../../Common/include/toolboxes/geometry_toolbox.hpp"
-
-void CDriver::PythonInterface_Preprocessing(CConfig **config, CGeometry ****geometry, CSolver *****solver){
 
+void CDriver::PythonInterface_Preprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver) {
   int rank = MASTER_NODE;
   SU2_MPI::Comm_rank(SU2_MPI::GetComm(), &rank);
 
-  /* --- Initialize boundary conditions customization, this is achieve through the Python wrapper --- */
-  for(iZone=0; iZone < nZone; iZone++){
-
-    if (config[iZone]->GetnMarker_PyCustom() > 0){
-
-      if (rank == MASTER_NODE) cout << endl << "----------------- Python Interface Preprocessing ( Zone "<< iZone <<" ) -----------------" << endl;
+  /* --- Initialize boundary conditions customization, this is achieved through the Python wrapper. --- */
+  for (iZone = 0; iZone < nZone; iZone++) {
+    if (config[iZone]->GetnMarker_PyCustom() > 0) {
+      if (rank == MASTER_NODE) cout << "----------------- Python Interface Preprocessing ( Zone " << iZone << " ) -----------------" << endl;
 
       if (rank == MASTER_NODE) cout << "Setting customized boundary conditions for zone " << iZone << endl;
       for (iMesh = 0; iMesh <= config[iZone]->GetnMGLevels(); iMesh++) {
@@ -50,21 +46,23 @@ void CDriver::PythonInterface_Preprocessing(CConfig **config, CGeometry ****geom
 
       if ((config[iZone]->GetKind_Solver() == MAIN_SOLVER::EULER) ||
           (config[iZone]->GetKind_Solver() == MAIN_SOLVER::NAVIER_STOKES) ||
-          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::RANS)) {
-
+          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::RANS) ||
+          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::INC_EULER) ||
+          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::INC_NAVIER_STOKES) ||
+          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::INC_RANS) ||
+          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::NEMO_EULER) ||
+          (config[iZone]->GetKind_Solver() == MAIN_SOLVER::NEMO_NAVIER_STOKES)) {
         solver[iZone][INST_0][MESH_0][FLOW_SOL]->UpdateCustomBoundaryConditions(geometry[iZone][INST_0], config[iZone]);
       }
     }
   }
-
 }
 
 /////////////////////////////////////////////////////////////////////////////
-/* Functions related to the global performance indices (Lift, Drag, ecc..) */
+/* Functions related to the global performance indices (Lift, Drag, etc.)  */
 /////////////////////////////////////////////////////////////////////////////
 
 passivedouble CDriver::Get_Drag() const {
-
   unsigned short val_iZone = ZONE_0;
   unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
   su2double CDrag, factor, val_Drag;
@@ -73,13 +71,12 @@ passivedouble CDriver::Get_Drag() const {
   factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
   CDrag = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CD();
 
-  val_Drag = CDrag*factor;
+  val_Drag = CDrag * factor;
 
   return SU2_TYPE::GetValue(val_Drag);
 }
 
 passivedouble CDriver::Get_Lift() const {
-
   unsigned short val_iZone = ZONE_0;
   unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
   su2double CLift, factor, val_Lift;
@@ -88,13 +85,12 @@ passivedouble CDriver::Get_Lift() const {
   factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
   CLift = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CL();
 
-  val_Lift = CLift*factor;
+  val_Lift = CLift * factor;
 
   return SU2_TYPE::GetValue(val_Lift);
 }
 
 passivedouble CDriver::Get_Mx() const {
-
   unsigned short val_iZone = ZONE_0;
   unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
   su2double CMx, RefLengthCoeff, factor, val_Mx;
@@ -105,13 +101,12 @@ passivedouble CDriver::Get_Mx() const {
   factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
   CMx = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMx();
 
-  val_Mx = CMx*factor*RefLengthCoeff;
+  val_Mx = CMx * factor * RefLengthCoeff;
 
   return SU2_TYPE::GetValue(val_Mx);
 }
 
 passivedouble CDriver::Get_My() const {
-
   unsigned short val_iZone = ZONE_0;
   unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
   su2double CMy, RefLengthCoeff, factor, val_My;
@@ -122,13 +117,12 @@ passivedouble CDriver::Get_My() const {
   factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
   CMy = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMy();
 
-  val_My = CMy*factor*RefLengthCoeff;
+  val_My = CMy * factor * RefLengthCoeff;
 
   return SU2_TYPE::GetValue(val_My);
 }
 
 passivedouble CDriver::Get_Mz() const {
-
   unsigned short val_iZone = ZONE_0;
   unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
   su2double CMz, RefLengthCoeff, factor, val_Mz;
@@ -139,13 +133,12 @@ passivedouble CDriver::Get_Mz() const {
   factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
   CMz = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMz();
 
-  val_Mz = CMz*factor*RefLengthCoeff;
+  val_Mz = CMz * factor * RefLengthCoeff;
 
   return SU2_TYPE::GetValue(val_Mz);
 }
 
 passivedouble CDriver::Get_DragCoeff() const {
-
   unsigned short val_iZone = ZONE_0;
   unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
   su2double CDrag;
@@ -156,7 +149,6 @@ passivedouble CDriver::Get_DragCoeff() const {
 }
 
 passivedouble CDriver::Get_LiftCoeff() const {
-
   unsigned short val_iZone = ZONE_0;
   unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
   su2double CLift;
@@ -166,129 +158,25 @@ passivedouble CDriver::Get_LiftCoeff() const {
   return SU2_TYPE::GetValue(CLift);
 }
 
-/////////////////////////////////////////////////////////////////////////////
-/* Functions to obtain information from the geometry/mesh                  */
-/////////////////////////////////////////////////////////////////////////////
-
-unsigned long CDriver::GetNumberVertices(unsigned short iMarker) const {
-
-  return geometry_container[ZONE_0][INST_0][MESH_0]->nVertex[iMarker];
-
-}
-
-unsigned long CDriver::GetNumberHaloVertices(unsigned short iMarker) const {
-
-  unsigned long nHaloVertices, iVertex, iPoint;
-
-  nHaloVertices = 0;
-  for(iVertex = 0; iVertex < geometry_container[ZONE_0][INST_0][MESH_0]->nVertex[iMarker]; iVertex++){
-    iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-    if(!(geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint))) nHaloVertices += 1;
-  }
-
-  return nHaloVertices;
-
-}
-
-unsigned long CDriver::GetVertexGlobalIndex(unsigned short iMarker, unsigned long iVertex) const {
-
-  unsigned long iPoint, GlobalIndex;
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  GlobalIndex = geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetGlobalIndex(iPoint);
-
-  return GlobalIndex;
-
-}
-
-bool CDriver::IsAHaloNode(unsigned short iMarker, unsigned long iVertex) const {
-
-  unsigned long iPoint;
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  if(geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint)) return false;
-  else return true;
-
-}
-
-vector<passivedouble> CDriver::GetInitialMeshCoord(unsigned short iMarker, unsigned long iVertex) const {
-
-  vector<su2double> coord(3,0.0);
-  vector<passivedouble> coord_passive(3, 0.0);
-
-  auto iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  for (auto iDim = 0 ; iDim < nDim ; iDim++){
-   coord[iDim] = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord(iPoint,iDim);
-  }
-
-  coord_passive[0] = SU2_TYPE::GetValue(coord[0]);
-  coord_passive[1] = SU2_TYPE::GetValue(coord[1]);
-  coord_passive[2] = SU2_TYPE::GetValue(coord[2]);
-
-  return coord_passive;
-}
-
-vector<passivedouble> CDriver::GetVertexNormal(unsigned short iMarker, unsigned long iVertex, bool unitNormal) const {
-
-  su2double *Normal;
-  su2double Area;
-  vector<su2double> ret_Normal(3, 0.0);
-  vector<passivedouble> ret_Normal_passive(3, 0.0);
-
-  Normal = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNormal();
-
-  if (!unitNormal) {
-
-    ret_Normal_passive[0] = SU2_TYPE::GetValue(Normal[0]);
-    ret_Normal_passive[1] = SU2_TYPE::GetValue(Normal[1]);
-    if(nDim>2) ret_Normal_passive[2] = SU2_TYPE::GetValue(Normal[2]);
-
-    return ret_Normal_passive;
-  }
-
-  Area = GeometryToolbox::Norm(nDim, Normal);
-
-  ret_Normal[0] = Normal[0]/Area;
-  ret_Normal[1] = Normal[1]/Area;
-  if(nDim>2) ret_Normal[2] = Normal[2]/Area;
-
-  ret_Normal_passive[0] = SU2_TYPE::GetValue(ret_Normal[0]);
-  ret_Normal_passive[1] = SU2_TYPE::GetValue(ret_Normal[1]);
-  ret_Normal_passive[2] = SU2_TYPE::GetValue(ret_Normal[2]);
-
-  return ret_Normal_passive;
-}
-
 //////////////////////////////////////////////////////////////////////////////////
-/* Functions to obtain global parameters from SU2 (time steps, delta t, ecc...) */
+/* Functions to obtain global parameters from SU2 (time steps, delta t, etc.)   */
 //////////////////////////////////////////////////////////////////////////////////
 
-unsigned long CDriver::GetnTimeIter() const {
-
-  return config_container[ZONE_0]->GetnTime_Iter();
-}
+unsigned long CDriver::GetnTimeIter() const { return config_container[ZONE_0]->GetnTime_Iter(); }
 
-unsigned long CDriver::GetTime_Iter() const{
-
-  return TimeIter;
-}
+unsigned long CDriver::GetTime_Iter() const { return TimeIter; }
 
 passivedouble CDriver::GetUnsteady_TimeStep() const {
-
   return SU2_TYPE::GetValue(config_container[ZONE_0]->GetTime_Step());
 }
 
-string CDriver::GetSurfaceFileName() const {
-
-  return config_container[ZONE_0]->GetSurfCoeff_FileName();
-}
+string CDriver::GetSurfaceFileName() const { return config_container[ZONE_0]->GetSurfCoeff_FileName(); }
 
 ///////////////////////////////////////////////////////////////////////////////
 /* Functions related to CHT solver                                           */
 ///////////////////////////////////////////////////////////////////////////////
 
 passivedouble CDriver::GetVertexTemperature(unsigned short iMarker, unsigned long iVertex) const {
-
   unsigned long iPoint;
   su2double vertexWallTemp(0.0);
 
@@ -296,43 +184,40 @@ passivedouble CDriver::GetVertexTemperature(unsigned short iMarker, unsigned lon
 
   iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
 
-  if(geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint) && compressible){
+  if (geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint) && compressible) {
     vertexWallTemp = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetTemperature(iPoint);
   }
 
   return SU2_TYPE::GetValue(vertexWallTemp);
-
 }
 
-void CDriver::SetVertexTemperature(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallTemp){
-
+void CDriver::SetVertexTemperature(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallTemp) {
   geometry_container[ZONE_0][INST_0][MESH_0]->SetCustomBoundaryTemperature(iMarker, iVertex, val_WallTemp);
 }
 
 vector<passivedouble> CDriver::GetVertexHeatFluxes(unsigned short iMarker, unsigned long iVertex) const {
-
   unsigned long iPoint;
   unsigned short iDim;
-  su2double Prandtl_Lam  = config_container[ZONE_0]->GetPrandtl_Lam();
+  su2double Prandtl_Lam = config_container[ZONE_0]->GetPrandtl_Lam();
   su2double Gas_Constant = config_container[ZONE_0]->GetGas_ConstantND();
   su2double Gamma = config_container[ZONE_0]->GetGamma();
   su2double Gamma_Minus_One = Gamma - 1.0;
   su2double Cp = (Gamma / Gamma_Minus_One) * Gas_Constant;
   su2double laminar_viscosity, thermal_conductivity;
-  vector<su2double> GradT (3,0.0);
-  vector<su2double> HeatFlux (3,0.0);
-  vector<passivedouble> HeatFluxPassive (3,0.0);
+  vector<su2double> GradT(3, 0.0);
+  vector<su2double> HeatFlux(3, 0.0);
+  vector<passivedouble> HeatFluxPassive(3, 0.0);
 
   bool compressible = (config_container[ZONE_0]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
 
   iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
 
-  if(compressible){
-    laminar_viscosity    = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
-    thermal_conductivity = Cp * (laminar_viscosity/Prandtl_Lam);
-    for(iDim=0; iDim < nDim; iDim++){
+  if (compressible) {
+    laminar_viscosity = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
+    thermal_conductivity = Cp * (laminar_viscosity / Prandtl_Lam);
+    for (iDim = 0; iDim < nDim; iDim++) {
       GradT[iDim] = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetGradient_Primitive(iPoint, 0, iDim);
-      HeatFlux[iDim] = -thermal_conductivity*GradT[iDim];
+      HeatFlux[iDim] = -thermal_conductivity * GradT[iDim];
     }
   }
 
@@ -343,19 +228,18 @@ vector<passivedouble> CDriver::GetVertexHeatFluxes(unsigned short iMarker, unsig
   return HeatFluxPassive;
 }
 
-passivedouble CDriver::GetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex) const{
-
+passivedouble CDriver::GetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex) const {
   unsigned long iPoint;
   unsigned short iDim;
   su2double vertexWallHeatFlux;
-  su2double Prandtl_Lam  = config_container[ZONE_0]->GetPrandtl_Lam();
+  su2double Prandtl_Lam = config_container[ZONE_0]->GetPrandtl_Lam();
   su2double Gas_Constant = config_container[ZONE_0]->GetGas_ConstantND();
   su2double Gamma = config_container[ZONE_0]->GetGamma();
   su2double Gamma_Minus_One = Gamma - 1.0;
   su2double Cp = (Gamma / Gamma_Minus_One) * Gas_Constant;
   su2double Area;
   su2double laminar_viscosity, thermal_conductivity, dTdn;
-  su2double *Normal, GradT[3] = {0.0,0.0,0.0}, UnitNormal[3] = {0.0,0.0,0.0};
+  su2double *Normal, GradT[3] = {0.0, 0.0, 0.0}, UnitNormal[3] = {0.0, 0.0, 0.0};
 
   bool compressible = (config_container[ZONE_0]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
 
@@ -364,37 +248,34 @@ passivedouble CDriver::GetVertexNormalHeatFlux(unsigned short iMarker, unsigned
 
   iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
 
-  if(geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint) && compressible){
+  if (geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint) && compressible) {
     Normal = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNormal();
 
     Area = GeometryToolbox::Norm(nDim, Normal);
 
-    for (iDim = 0; iDim < nDim; iDim++)
-      UnitNormal[iDim] = Normal[iDim]/Area;
+    for (iDim = 0; iDim < nDim; iDim++) UnitNormal[iDim] = Normal[iDim] / Area;
 
-    laminar_viscosity    = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
-    thermal_conductivity = Cp * (laminar_viscosity/Prandtl_Lam);
+    laminar_viscosity = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
+    thermal_conductivity = Cp * (laminar_viscosity / Prandtl_Lam);
     /*Compute wall heat flux (normal to the wall) based on computed temperature gradient*/
-    for(iDim=0; iDim < nDim; iDim++){
+    for (iDim = 0; iDim < nDim; iDim++) {
       GradT[iDim] = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetGradient_Primitive(iPoint, 0, iDim);
-      dTdn += GradT[iDim]*UnitNormal[iDim];
+      dTdn += GradT[iDim] * UnitNormal[iDim];
     }
 
-    vertexWallHeatFlux = -thermal_conductivity*dTdn;
+    vertexWallHeatFlux = -thermal_conductivity * dTdn;
   }
 
   return SU2_TYPE::GetValue(vertexWallHeatFlux);
 }
 
-void CDriver::SetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallHeatFlux){
-
+void CDriver::SetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallHeatFlux) {
   geometry_container[ZONE_0][INST_0][MESH_0]->SetCustomBoundaryHeatFlux(iMarker, iVertex, val_WallHeatFlux);
 }
 
 passivedouble CDriver::GetThermalConductivity(unsigned short iMarker, unsigned long iVertex) const {
-
   unsigned long iPoint;
-  su2double Prandtl_Lam  = config_container[ZONE_0]->GetPrandtl_Lam();
+  su2double Prandtl_Lam = config_container[ZONE_0]->GetPrandtl_Lam();
   su2double Gas_Constant = config_container[ZONE_0]->GetGas_ConstantND();
   su2double Gamma = config_container[ZONE_0]->GetGamma();
   su2double Gamma_Minus_One = Gamma - 1.0;
@@ -402,218 +283,124 @@ passivedouble CDriver::GetThermalConductivity(unsigned short iMarker, unsigned l
   su2double laminar_viscosity, thermal_conductivity;
 
   iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  laminar_viscosity    = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
-  thermal_conductivity = Cp * (laminar_viscosity/Prandtl_Lam);
+  laminar_viscosity = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
+  thermal_conductivity = Cp * (laminar_viscosity / Prandtl_Lam);
 
   return SU2_TYPE::GetValue(thermal_conductivity);
-
 }
 
 ////////////////////////////////////////////////////////////////////////////////
 /* Functions related to the management of markers                             */
 ////////////////////////////////////////////////////////////////////////////////
 
-vector<string> CDriver::GetAllBoundaryMarkersTag() const {
-
-  vector<string> boundariesTagList;
-  unsigned short iMarker,nBoundariesMarkers;
-  string Marker_Tag;
-
-  nBoundariesMarkers = config_container[ZONE_0]->GetnMarker_All();
-  boundariesTagList.resize(nBoundariesMarkers);
-
-  for(iMarker=0; iMarker < nBoundariesMarkers; iMarker++){
-    Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
-    boundariesTagList[iMarker] = Marker_Tag;
-  }
-
-  return boundariesTagList;
-}
-
-vector<string> CDriver::GetAllDeformMeshMarkersTag() const {
-
-  vector<string> interfaceBoundariesTagList;
-  unsigned short iMarker, nBoundariesMarker;
-  string Marker_Tag;
+vector<string> CDriver::GetCHTMarkerTags() const {
+  vector<string> tags;
+  const auto nMarker = config_container[ZONE_0]->GetnMarker_All();
 
-  nBoundariesMarker = config_container[ZONE_0]->GetnMarker_Deform_Mesh();
-  interfaceBoundariesTagList.resize(nBoundariesMarker);
-
-  for(iMarker=0; iMarker < nBoundariesMarker; iMarker++){
-    Marker_Tag = config_container[ZONE_0]->GetMarker_Deform_Mesh_TagBound(iMarker);
-    interfaceBoundariesTagList[iMarker] = Marker_Tag;
-  }
-
-  return interfaceBoundariesTagList;
-}
-
-vector<string> CDriver::GetAllCHTMarkersTag() const {
-
-  vector<string> CHTBoundariesTagList;
-  unsigned short iMarker, nBoundariesMarker;
-  string Marker_Tag;
-
-  nBoundariesMarker = config_container[ZONE_0]->GetnMarker_All();
-
-  //The CHT markers can be identified as the markers that are customizable with a BC type HEAT_FLUX or ISOTHERMAL.
-  for(iMarker=0; iMarker<nBoundariesMarker; iMarker++){
-    if((config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == HEAT_FLUX || config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == ISOTHERMAL) && config_container[ZONE_0]->GetMarker_All_PyCustom(iMarker)){
-      Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
-      CHTBoundariesTagList.push_back(Marker_Tag);
+  // The CHT markers can be identified as the markers that are customizable with a BC type HEAT_FLUX or ISOTHERMAL.
+  for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
+    if ((config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == HEAT_FLUX ||
+         config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == ISOTHERMAL) &&
+        config_container[ZONE_0]->GetMarker_All_PyCustom(iMarker)) {
+      tags.push_back(config_container[ZONE_0]->GetMarker_All_TagBound(iMarker));
     }
   }
 
-  return CHTBoundariesTagList;
+  return tags;
 }
 
-vector<string> CDriver::GetAllInletMarkersTag() const {
-
-  vector<string> BoundariesTagList;
-  unsigned short iMarker, nBoundariesMarker;
-  string Marker_Tag;
+vector<string> CDriver::GetInletMarkerTags() const {
+  vector<string> tags;
+  const auto nMarker = config_container[ZONE_0]->GetnMarker_All();
 
-  nBoundariesMarker = config_container[ZONE_0]->GetnMarker_All();
-
-  for(iMarker=0; iMarker<nBoundariesMarker; iMarker++){
+  for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
     bool isCustomizable = config_container[ZONE_0]->GetMarker_All_PyCustom(iMarker);
     bool isInlet = (config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == INLET_FLOW);
-    if(isCustomizable && isInlet) {
-      Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
-      BoundariesTagList.push_back(Marker_Tag);
-    }
-  }
-
-  return BoundariesTagList;
-}
-
-map<string, int> CDriver::GetAllBoundaryMarkers() const {
-
-  map<string, int>  allBoundariesMap;
-  unsigned short iMarker, nBoundaryMarkers;
-  string Marker_Tag;
-
-  nBoundaryMarkers = config_container[ZONE_0]->GetnMarker_All();
-
-  for(iMarker=0; iMarker < nBoundaryMarkers; iMarker++){
-    Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
-    allBoundariesMap[Marker_Tag] = iMarker;
-  }
-
-  return allBoundariesMap;
-}
-
-map<string, string> CDriver::GetAllBoundaryMarkersType() const {
 
-  map<string, string> allBoundariesTypeMap;
-  unsigned short iMarker, KindBC;
-  string Marker_Tag, Marker_Type;
-
-  for(iMarker=0; iMarker < config_container[ZONE_0]->GetnMarker_All(); iMarker++){
-    Marker_Tag = config_container[ZONE_0]->GetMarker_All_TagBound(iMarker);
-    KindBC = config_container[ZONE_0]->GetMarker_All_KindBC(iMarker);
-    switch(KindBC){
-      case EULER_WALL:
-        Marker_Type = "EULER_WALL";
-        break;
-      case FAR_FIELD:
-        Marker_Type = "FARFIELD";
-        break;
-      case ISOTHERMAL:
-        Marker_Type = "ISOTHERMAL";
-        break;
-      case HEAT_FLUX:
-        Marker_Type = "HEATFLUX";
-        break;
-      case INLET_FLOW:
-        Marker_Type = "INLET_FLOW";
-        break;
-      case OUTLET_FLOW:
-        Marker_Type = "OUTLET_FLOW";
-        break;
-      case SYMMETRY_PLANE:
-        Marker_Type = "SYMMETRY";
-        break;
-      case SEND_RECEIVE:
-        Marker_Type = "SEND_RECEIVE";
-        break;
-      default:
-        Marker_Type = "UNKNOWN_TYPE";
+    if (isCustomizable && isInlet) {
+      tags.push_back(config_container[ZONE_0]->GetMarker_All_TagBound(iMarker));
     }
-    allBoundariesTypeMap[Marker_Tag] = Marker_Type;
   }
 
-  return allBoundariesTypeMap;
+  return tags;
 }
 
-void CDriver::SetHeatSource_Position(passivedouble alpha, passivedouble pos_x, passivedouble pos_y, passivedouble pos_z){
-
-  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][RAD_SOL];
+void CDriver::SetHeatSource_Position(passivedouble alpha, passivedouble pos_x, passivedouble pos_y,
+                                     passivedouble pos_z) {
+  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][RAD_SOL];
 
   config_container[ZONE_0]->SetHeatSource_Rot_Z(alpha);
   config_container[ZONE_0]->SetHeatSource_Center(pos_x, pos_y, pos_z);
 
   solver->SetVolumetricHeatSource(geometry_container[ZONE_0][INST_0][MESH_0], config_container[ZONE_0]);
-
 }
 
-void CDriver::SetInlet_Angle(unsigned short iMarker, passivedouble alpha){
-
-  su2double alpha_rad = alpha * PI_NUMBER/180.0;
+void CDriver::SetInlet_Angle(unsigned short iMarker, passivedouble alpha) {
+  su2double alpha_rad = alpha * PI_NUMBER / 180.0;
 
   unsigned long iVertex;
 
-  for (iVertex = 0; iVertex < geometry_container[ZONE_0][INST_0][MESH_0]->nVertex[iMarker]; iVertex++){
+  for (iVertex = 0; iVertex < geometry_container[ZONE_0][INST_0][MESH_0]->nVertex[iMarker]; iVertex++) {
     solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->SetInlet_FlowDir(iMarker, iVertex, 0, cos(alpha_rad));
     solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->SetInlet_FlowDir(iMarker, iVertex, 1, sin(alpha_rad));
   }
-
 }
 
 /////////////////////////////////////////////////////////////////////////////////////////////////////////////////
-/* Functions related to simulation control, high level functions (reset convergence, set initial mesh, ecc...) */
+/* Functions related to simulation control, high level functions (reset convergence, set initial mesh, etc.)   */
 /////////////////////////////////////////////////////////////////////////////////////////////////////////////////
 
 void CDriver::ResetConvergence() {
+  for (auto iZone = 0u; iZone < nZone; iZone++) {
+    switch (main_config->GetKind_Solver()) {
+      case MAIN_SOLVER::EULER:
+      case MAIN_SOLVER::NAVIER_STOKES:
+      case MAIN_SOLVER::RANS:
+      case MAIN_SOLVER::INC_EULER:
+      case MAIN_SOLVER::INC_NAVIER_STOKES:
+      case MAIN_SOLVER::INC_RANS:
+      case MAIN_SOLVER::NEMO_EULER:
+      case MAIN_SOLVER::NEMO_NAVIER_STOKES:
+        integration_container[iZone][INST_0][FLOW_SOL]->SetConvergence(false);
+        if (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::RANS)
+          integration_container[iZone][INST_0][TURB_SOL]->SetConvergence(false);
+        if (config_container[iZone]->GetKind_Trans_Model() == TURB_TRANS_MODEL::LM)
+          integration_container[iZone][INST_0][TRANS_SOL]->SetConvergence(false);
+        break;
+
+      case MAIN_SOLVER::FEM_ELASTICITY:
+        integration_container[iZone][INST_0][FEA_SOL]->SetConvergence(false);
+        break;
+
+      case MAIN_SOLVER::ADJ_EULER:
+      case MAIN_SOLVER::ADJ_NAVIER_STOKES:
+      case MAIN_SOLVER::ADJ_RANS:
+      case MAIN_SOLVER::DISC_ADJ_EULER:
+      case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES:
+      case MAIN_SOLVER::DISC_ADJ_RANS:
+      case MAIN_SOLVER::DISC_ADJ_INC_EULER:
+      case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES:
+      case MAIN_SOLVER::DISC_ADJ_INC_RANS:
+        integration_container[iZone][INST_0][ADJFLOW_SOL]->SetConvergence(false);
+        if ((config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::ADJ_RANS) ||
+            (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_RANS))
+          integration_container[iZone][INST_0][ADJTURB_SOL]->SetConvergence(false);
+        break;
 
-  for(iZone = 0; iZone < nZone; iZone++) {
-    switch (config_container[iZone]->GetKind_Solver()) {
-
-    case MAIN_SOLVER::EULER: case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::RANS:
-    case MAIN_SOLVER::INC_EULER: case MAIN_SOLVER::INC_NAVIER_STOKES: case MAIN_SOLVER::INC_RANS:
-      integration_container[iZone][INST_0][FLOW_SOL]->SetConvergence(false);
-      if (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::RANS) integration_container[iZone][INST_0][TURB_SOL]->SetConvergence(false);
-      if(config_container[iZone]->GetKind_Trans_Model() == TURB_TRANS_MODEL::LM) integration_container[iZone][INST_0][TRANS_SOL]->SetConvergence(false);
-      break;
-
-    case MAIN_SOLVER::FEM_ELASTICITY:
-      integration_container[iZone][INST_0][FEA_SOL]->SetConvergence(false);
-      break;
-
-    case MAIN_SOLVER::ADJ_EULER: case MAIN_SOLVER::ADJ_NAVIER_STOKES: case MAIN_SOLVER::ADJ_RANS: case MAIN_SOLVER::DISC_ADJ_EULER: case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_RANS:
-    case MAIN_SOLVER::DISC_ADJ_INC_EULER: case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_INC_RANS:
-      integration_container[iZone][INST_0][ADJFLOW_SOL]->SetConvergence(false);
-      if( (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::ADJ_RANS) || (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_RANS) )
-        integration_container[iZone][INST_0][ADJTURB_SOL]->SetConvergence(false);
-      break;
-
-    default:
-      break;
+      default:
+        break;
     }
   }
-
 }
 
 void CSinglezoneDriver::SetInitialMesh() {
-
   DynamicMeshUpdate(0);
 
   SU2_OMP_PARALLEL {
-    // Overwrite fictious velocities
-    for (iMesh = 0u; iMesh <= config_container[ZONE_0]->GetnMGLevels(); iMesh++) {
-      SU2_OMP_FOR_STAT(roundUpDiv(geometry_container[ZONE_0][INST_0][iMesh]->GetnPoint(),omp_get_max_threads()))
-      for (unsigned long iPoint = 0; iPoint < geometry_container[ZONE_0][INST_0][iMesh]->GetnPoint(); iPoint++) {
-
-        /*--- Overwrite fictitious velocities ---*/
+    for (iMesh = 0u; iMesh <= main_config->GetnMGLevels(); iMesh++) {
+      SU2_OMP_FOR_STAT(roundUpDiv(geometry_container[ZONE_0][INST_0][iMesh]->GetnPoint(), omp_get_max_threads()))
+      for (auto iPoint = 0ul; iPoint < geometry_container[ZONE_0][INST_0][iMesh]->GetnPoint(); iPoint++) {
+        /*--- Overwrite fictitious velocities. ---*/
         su2double Grid_Vel[3] = {0.0, 0.0, 0.0};
 
         /*--- Set the grid velocity for this coarse node. ---*/
@@ -624,23 +411,21 @@ void CSinglezoneDriver::SetInitialMesh() {
       geometry_container[ZONE_0][INST_0][iMesh]->nodes->SetVolume_n();
       geometry_container[ZONE_0][INST_0][iMesh]->nodes->SetVolume_nM1();
     }
-    /*--- Push back the solution so that there is no fictious velocity at the next step. ---*/
+    /*--- Push back the solution so that there is no fictitious velocity at the next step. ---*/
     solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->Set_Solution_time_n();
     solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->Set_Solution_time_n1();
   }
   END_SU2_OMP_PARALLEL
 }
 
-void CDriver::BoundaryConditionsUpdate(){
-
+void CDriver::BoundaryConditionsUpdate() {
   int rank = MASTER_NODE;
-  unsigned short iZone;
 
   SU2_MPI::Comm_rank(SU2_MPI::GetComm(), &rank);
 
-  if(rank == MASTER_NODE) cout << "Updating boundary conditions." << endl;
-  for(iZone = 0; iZone < nZone; iZone++){
-    geometry_container[iZone][INST_0][MESH_0]->UpdateCustomBoundaryConditions(geometry_container[iZone][INST_0], config_container[iZone]);
+  if (rank == MASTER_NODE) cout << "Updating boundary conditions." << endl;
+  for (auto iZone = 0u; iZone < nZone; iZone++) {
+    geometry_container[iZone][INST_0][MESH_0]->UpdateCustomBoundaryConditions(geometry_container[iZone][INST_0],config_container[iZone]);
   }
 }
 
@@ -648,29 +433,26 @@ void CDriver::BoundaryConditionsUpdate(){
 /* Functions related to finite elements                                       */
 ////////////////////////////////////////////////////////////////////////////////
 
-void CDriver::SetFEA_Loads(unsigned short iMarker, unsigned long iVertex, passivedouble LoadX,
-                       passivedouble LoadY, passivedouble LoadZ) {
-
+void CDriver::SetFEA_Loads(unsigned short iMarker, unsigned long iVertex, passivedouble LoadX, passivedouble LoadY,
+                           passivedouble LoadZ) {
   unsigned long iPoint;
-  su2double NodalForce[3] = {0.0,0.0,0.0};
+  su2double NodalForce[3] = {0.0, 0.0, 0.0};
   NodalForce[0] = LoadX;
   NodalForce[1] = LoadY;
   NodalForce[2] = LoadZ;
 
   iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL]->GetNodes()->Set_FlowTraction(iPoint,NodalForce);
-
+  solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL]->GetNodes()->Set_FlowTraction(iPoint, NodalForce);
 }
 
 vector<passivedouble> CDriver::GetFEA_Displacements(unsigned short iMarker, unsigned long iVertex) const {
-
   unsigned long iPoint;
   vector<su2double> Displacements(3, 0.0);
   vector<passivedouble> Displacements_passive(3, 0.0);
 
   iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
-  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
+  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 
   Displacements[0] = solver->GetNodes()->GetSolution(iPoint, 0);
   Displacements[1] = solver->GetNodes()->GetSolution(iPoint, 1);
@@ -686,18 +468,16 @@ vector<passivedouble> CDriver::GetFEA_Displacements(unsigned short iMarker, unsi
   return Displacements_passive;
 }
 
-
 vector<passivedouble> CDriver::GetFEA_Velocity(unsigned short iMarker, unsigned long iVertex) const {
-
   unsigned long iPoint;
   vector<su2double> Velocity(3, 0.0);
-  vector<passivedouble> Velocity_passive(3,0.0);
+  vector<passivedouble> Velocity_passive(3, 0.0);
 
   iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
-  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
+  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 
-  if (config_container[ZONE_0]->GetDynamic_Analysis() == DYNAMIC){
+  if (config_container[ZONE_0]->GetDynamic_Analysis() == DYNAMIC) {
     Velocity[0] = solver->GetNodes()->GetSolution_Vel(iPoint, 0);
     Velocity[1] = solver->GetNodes()->GetSolution_Vel(iPoint, 1);
     if (geometry->GetnDim() == 3)
@@ -714,16 +494,15 @@ vector<passivedouble> CDriver::GetFEA_Velocity(unsigned short iMarker, unsigned
 }
 
 vector<passivedouble> CDriver::GetFEA_Velocity_n(unsigned short iMarker, unsigned long iVertex) const {
-
   unsigned long iPoint;
   vector<su2double> Velocity_n(3, 0.0);
   vector<passivedouble> Velocity_n_passive(3, 0.0);
 
   iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
-  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
+  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 
-  if (config_container[ZONE_0]->GetDynamic_Analysis() == DYNAMIC){
+  if (config_container[ZONE_0]->GetDynamic_Analysis() == DYNAMIC) {
     Velocity_n[0] = solver->GetNodes()->GetSolution_Vel_time_n(iPoint, 0);
     Velocity_n[1] = solver->GetNodes()->GetSolution_Vel_time_n(iPoint, 1);
     if (geometry->GetnDim() == 3)
@@ -737,7 +516,6 @@ vector<passivedouble> CDriver::GetFEA_Velocity_n(unsigned short iMarker, unsigne
   Velocity_n_passive[2] = SU2_TYPE::GetValue(Velocity_n[2]);
 
   return Velocity_n_passive;
-
 }
 
 ////////////////////////////////////////////////////////////////////////////////
@@ -745,14 +523,13 @@ vector<passivedouble> CDriver::GetFEA_Velocity_n(unsigned short iMarker, unsigne
 ////////////////////////////////////////////////////////////////////////////////
 
 vector<passivedouble> CDriver::GetMeshDisp_Sensitivity(unsigned short iMarker, unsigned long iVertex) const {
-
   unsigned long iPoint;
   vector<su2double> Disp_Sens(3, 0.0);
   vector<passivedouble> Disp_Sens_passive(3, 0.0);
 
   iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver *solver =  solver_container[ZONE_0][INST_0][MESH_0][ADJMESH_SOL];
-  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][ADJMESH_SOL];
+  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 
   Disp_Sens[0] = solver->GetNodes()->GetBoundDisp_Sens(iPoint, 0);
   Disp_Sens[1] = solver->GetNodes()->GetBoundDisp_Sens(iPoint, 1);
@@ -766,18 +543,16 @@ vector<passivedouble> CDriver::GetMeshDisp_Sensitivity(unsigned short iMarker, u
   Disp_Sens_passive[2] = SU2_TYPE::GetValue(Disp_Sens[2]);
 
   return Disp_Sens_passive;
-
 }
 
 vector<passivedouble> CDriver::GetFlowLoad_Sensitivity(unsigned short iMarker, unsigned long iVertex) const {
-
   unsigned long iPoint;
   vector<su2double> FlowLoad_Sens(3, 0.0);
   vector<passivedouble> FlowLoad_Sens_passive(3, 0.0);
 
   iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
-  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
+  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 
   FlowLoad_Sens[0] = solver->GetNodes()->GetFlowTractionSensitivity(iPoint, 0);
   FlowLoad_Sens[1] = solver->GetNodes()->GetFlowTractionSensitivity(iPoint, 1);
@@ -791,91 +566,52 @@ vector<passivedouble> CDriver::GetFlowLoad_Sensitivity(unsigned short iMarker, u
   FlowLoad_Sens_passive[2] = SU2_TYPE::GetValue(FlowLoad_Sens[2]);
 
   return FlowLoad_Sens_passive;
-
 }
 
 void CDriver::SetFlowLoad_Adjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
                                   passivedouble val_AdjointY, passivedouble val_AdjointZ) {
-
-  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL];
-  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL];
+  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 
   solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 0, val_AdjointX);
   solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 1, val_AdjointY);
-  if (geometry->GetnDim() == 3)
-    solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 2, val_AdjointZ);
-
+  if (geometry->GetnDim() == 3) solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 2, val_AdjointZ);
 }
 
 void CDriver::SetSourceTerm_DispAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
                                         passivedouble val_AdjointY, passivedouble val_AdjointZ) {
-
   unsigned long iPoint;
 
-  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
-  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
+  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
   iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
 
   solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 0, val_AdjointX);
   solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 1, val_AdjointY);
-  if (geometry->GetnDim() == 3)
-    solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 2, val_AdjointZ);
-
+  if (geometry->GetnDim() == 3) solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 2, val_AdjointZ);
 }
 
 void CDriver::SetSourceTerm_VelAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
-                                        passivedouble val_AdjointY, passivedouble val_AdjointZ) {
-
-  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
-  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+                                       passivedouble val_AdjointY, passivedouble val_AdjointZ) {
+  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
+  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
   const auto iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
 
   solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 0, val_AdjointX);
   solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 1, val_AdjointY);
-  if (geometry->GetnDim() == 3)
-    solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 2, val_AdjointZ);
-
+  if (geometry->GetnDim() == 3) solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 2, val_AdjointZ);
 }
 
 ////////////////////////////////////////////////////////////////////////////////
-/* Functions related to mesh deformation */
-////////////////////////////////////////////////////////////////////////////////
-
-void CDriver::SetMeshDisplacement(unsigned short iMarker, unsigned long iVertex, passivedouble DispX, passivedouble DispY, passivedouble DispZ) {
-
-  unsigned long iPoint;
-  su2double MeshDispl[3] =  {0.0,0.0,0.0};
-
-  MeshDispl[0] = DispX;
-  MeshDispl[1] = DispY;
-  MeshDispl[2] = DispZ;
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-
-  solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->SetBound_Disp(iPoint,MeshDispl);
-
-}
-
-void CDriver::CommunicateMeshDisplacement(void) {
-
-  solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->InitiateComms(geometry_container[ZONE_0][INST_0][MESH_0],
-                                                                    config_container[ZONE_0], MESH_DISPLACEMENTS);
-  solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->CompleteComms(geometry_container[ZONE_0][INST_0][MESH_0],
-                                                                    config_container[ZONE_0], MESH_DISPLACEMENTS);
-
-}
-
-////////////////////////////////////////////////////////////////////////////////
-/* Functions related to flow loads */
+/* Functions related to flow loads                                             */
 ////////////////////////////////////////////////////////////////////////////////
 
 vector<passivedouble> CDriver::GetFlowLoad(unsigned short iMarker, unsigned long iVertex) const {
-
   vector<su2double> FlowLoad(3, 0.0);
   vector<passivedouble> FlowLoad_passive(3, 0.0);
 
-  CSolver *solver = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL];
-  CGeometry *geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL];
+  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 
   if (config_container[ZONE_0]->GetSolid_Wall(iMarker)) {
     FlowLoad[0] = solver->GetVertexTractions(iMarker, iVertex, 0);
@@ -891,5 +627,4 @@ vector<passivedouble> CDriver::GetFlowLoad(unsigned short iMarker, unsigned long
   FlowLoad_passive[2] = SU2_TYPE::GetValue(FlowLoad[2]);
 
   return FlowLoad_passive;
-
 }
diff --git a/SU2_CFD/src/solvers/CMeshSolver.cpp b/SU2_CFD/src/solvers/CMeshSolver.cpp
index 77470e620fb..57b4b25edb7 100644
--- a/SU2_CFD/src/solvers/CMeshSolver.cpp
+++ b/SU2_CFD/src/solvers/CMeshSolver.cpp
@@ -415,7 +415,7 @@ void CMeshSolver::SetWallDistance(CGeometry *geometry, CConfig *config) {
   END_SU2_OMP_PARALLEL
 }
 
-void CMeshSolver::SetMesh_Stiffness(CGeometry **geometry, CNumerics **numerics, CConfig *config){
+void CMeshSolver::SetMesh_Stiffness(CNumerics **numerics, CConfig *config){
 
   if (stiffness_set) return;
 
diff --git a/TestCases/coupled_cht/disc_adj_unsteadyCHT_cylinder/solid.cfg b/TestCases/coupled_cht/disc_adj_unsteadyCHT_cylinder/solid.cfg
index 3fb2d6bafd2..c3d950ae259 100644
--- a/TestCases/coupled_cht/disc_adj_unsteadyCHT_cylinder/solid.cfg
+++ b/TestCases/coupled_cht/disc_adj_unsteadyCHT_cylinder/solid.cfg
@@ -42,7 +42,6 @@ CONV_STARTITER= 10000
 
 % -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
 %
-CONV_NUM_METHOD_HEAT = SPACE_CENTERED
 TIME_DISCRE_HEAT= EULER_IMPLICIT
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
diff --git a/TestCases/disc_adj_heat/disc_adj_heat.cfg b/TestCases/disc_adj_heat/disc_adj_heat.cfg
index 9d6918ae4b7..a2509c72d08 100644
--- a/TestCases/disc_adj_heat/disc_adj_heat.cfg
+++ b/TestCases/disc_adj_heat/disc_adj_heat.cfg
@@ -126,12 +126,10 @@ CFL_REDUCTION_TURB= 1.0
 
 % -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
 
-CONV_NUM_METHOD_HEAT = SPACE_CENTERED
+CONV_NUM_METHOD_HEAT = SCALAR_UPWIND
 
 MUSCL_HEAT= YES
 
-JST_SENSOR_COEFF_HEAT= ( 0.5, 0.15 )
-
 TIME_DISCRE_HEAT= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index 40f24cb5fef..4e2094b56f6 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -248,7 +248,7 @@ def main():
     #######################################
     ### Axisymmetric Compressible RANS  ###
     #######################################
-    
+
     # Axisymmetric air nozzle (transonic)
     axi_rans_air_nozzle_restart           = TestCase('axi_rans_air_nozzle_restart')
     axi_rans_air_nozzle_restart.cfg_dir   = "axisymmetric_rans/air_nozzle"
@@ -427,6 +427,14 @@ def main():
     inc_turb_naca0012_sst_sust.test_vals = [-7.274028, 0.145888, 0.000002, 0.312014]
     test_list.append(inc_turb_naca0012_sst_sust)
 
+    # Weakly coupled heat equation
+    inc_weakly_coupled = TestCase('inc_weakly_coupled')
+    inc_weakly_coupled.cfg_dir = "disc_adj_heat"
+    inc_weakly_coupled.cfg_file = "primal.cfg"
+    inc_weakly_coupled.test_iter = 10
+    inc_weakly_coupled.test_vals = [-17.240436, -16.184455, -16.069131, -17.230730, -18.350601, -13.768070, 5.545700]
+    test_list.append(inc_weakly_coupled)
+
     ######################################
     ### Moving Wall                    ###
     ######################################
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/of_grad_findiff.csv.ref b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/of_grad_findiff.csv.ref
index 51f3fad3680..82730a5fe1e 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/of_grad_findiff.csv.ref
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/of_grad_findiff.csv.ref
@@ -1,2 +1,2 @@
 "VARIABLE"      , "AVG_DENSITY[0]", "AVG_ENTHALPY[0]", "AVG_NORMALVEL[0]", "DRAG[0]"       , "EFFICIENCY[0]" , "FORCE_X[0]"    , "FORCE_Y[0]"    , "FORCE_Z[0]"    , "LIFT[0]"       , "MOMENT_X[0]"   , "MOMENT_Y[0]"   , "MOMENT_Z[0]"   , "SIDEFORCE[0]"  , "SURFACE_MACH[0]", "SURFACE_MASSFLOW[0]", "SURFACE_MOM_DISTORTION[0]", "SURFACE_PRESSURE_DROP[0]", "SURFACE_SECONDARY[0]", "SURFACE_SECOND_OVER_UNIFORM[0]", "SURFACE_STATIC_PRESSURE[0]", "SURFACE_STATIC_TEMPERATURE[0]", "SURFACE_TOTAL_PRESSURE[0]", "SURFACE_TOTAL_TEMPERATURE[0]", "SURFACE_UNIFORMITY[0]", "AVG_TEMPERATURE[1]", "MAXIMUM_HEATFLUX[1]", "TOTAL_HEATFLUX[1]", "FINDIFF_STEP"  
-0               , 0.0             , -100000.01639127731, -1.1101999999881826e-08, 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , -0.0399999991462785, 0.0                , -2.1099999997220564      , 0.0                     , 2.1799999999627673  , 3.8000000007754053            , 319.9999980552093         , -39.999997625272954          , 318.0000007318995        , -39.999997625272954         , -1.400000004814217   , -139.99999737279722, 0.0                , -540.0000077315781, 1e-08           
+0               , 0.0             , -100000.01639127731, -1.1103000000496327e-08, 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , -0.0399999991462785, 3.3309999998872306e-08, -2.1099999997220564      , 0.0                     , 2.1799999999627673  , 3.8000000007754053            , 319.9999980552093         , -39.999997625272954          , 318.0000007318995        , -39.999997625272954         , -1.400000004814217   , -139.99999737279722, 0.0                , -540.0000077315781, 1e-08           
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configSolid.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configSolid.cfg
index 50d94b56d2f..6c78fb026ed 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configSolid.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configSolid.cfg
@@ -64,7 +64,6 @@ CONV_STARTITER= 100
 %
 % -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
 %
-CONV_NUM_METHOD_HEAT = SPACE_CENTERED
 TIME_DISCRE_HEAT= EULER_IMPLICIT
 %
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 53c54368a0b..e0fad895d88 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -362,6 +362,15 @@ def main():
     turb_oneram6.timeout   = 3200
     test_list.append(turb_oneram6)
 
+    # ONERA M6 Wing - vorticity confinement
+    turb_oneram6_vc = TestCase('turb_oneram6_vc')
+    turb_oneram6_vc.cfg_dir = "rans/oneram6"
+    turb_oneram6_vc.cfg_file = "turb_ONERAM6_vc.cfg"
+    turb_oneram6_vc.test_iter = 15
+    turb_oneram6_vc.test_vals = [-2.262387, -6.626467, 0.228393, 0.140799, -2.7107e+04]
+    turb_oneram6_vc.timeout = 3200
+    test_list.append(turb_oneram6_vc)
+
     # ONERA M6 Wing - Newton-Krylov
     turb_oneram6_nk           = TestCase('turb_oneram6_nk')
     turb_oneram6_nk.cfg_dir   = "rans/oneram6"
@@ -1206,7 +1215,7 @@ def main():
     solid_periodic_pins.cfg_dir   = "solid_heat_conduction/periodic_pins"
     solid_periodic_pins.cfg_file  = "configSolid.cfg"
     solid_periodic_pins.test_iter = 750
-    solid_periodic_pins.test_vals         = [-15.878958, -14.569206, 300.900000, 425.320000, 0.000000, 5.000000, -1.672714] #last 7 lines
+    solid_periodic_pins.test_vals = [-15.878977, -14.569206, 300.900000, 425.320000, 0.000000, 5.000000, -1.672737] #last 7 lines
     solid_periodic_pins.test_vals_aarch64 = [-15.879010, -14.569206, 300.900000, 425.320000, 0.000000, 5.000000, -1.672630] #last 7 lines
     test_list.append(solid_periodic_pins)
 
@@ -1419,7 +1428,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_viscosity.test_vals = [-4.738778, -4.325766, -4.610914, -5.834431, 0.521730, -4.934375, 5.000000, -1.887191, 5.000000, -5.499917, 5.000000, -1.770845, 2.292904, 0.971941, 0.608500, 0.712464]
     species2_primitiveVenturi_mixingmodel_viscosity.new_output = True
     test_list.append(species2_primitiveVenturi_mixingmodel_viscosity)
-    
+
     # 2 species (1 eq) primitive venturi mixing using mixing model including heat capacity and mass diffusivity
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2           = TestCase('species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg')
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg_dir   = "species_transport/venturi_primitive_3species"
@@ -1431,7 +1440,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.new_output = True
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.tol       = 0.00001
     test_list.append(species2_primitiveVenturi_mixingmodel_heatcapacity_H2)
-    
+
     # 2 species (1 eq) primitive venturi mixing using mixing model including heat capacity and mass diffusivity NonDimensional case
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND           = TestCase('species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg')
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg_dir   = "species_transport/venturi_primitive_3species"
@@ -1443,7 +1452,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.new_output = True
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.tol       = 0.00001
     test_list.append(species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND)
-    
+
     # 2 species (1 eq) primitive venturi mixing
     species2_primitiveVenturi           = TestCase('species2_primitiveVenturi')
     species2_primitiveVenturi.cfg_dir   = "species_transport/venturi_primitive_3species"
@@ -1461,7 +1470,7 @@ def main():
     species_primitiveVenturi_boundedscalar.test_vals   = [-5.297585, -4.397797, -4.377086, -5.593131, -1.011782, -5.623540, 5.000000, -1.775123, 5.000000, -4.086339, 5.000000, -2.080187, 0.000424, 0.000424, 0.000000, 0.000000]
     species_primitiveVenturi_boundedscalar.new_output  = True
     test_list.append(species_primitiveVenturi_boundedscalar)
-    
+
     # 2 species (1 eq) primitive venturi mixing using mixing model including inlet markers for turbulent intensity and viscosity ratios
     species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS           = TestCase('species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg')
     species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg_dir   = "species_transport/venturi_primitive_3species"
diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index 6e47a1a4365..ad7c50042d1 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -6,8 +6,8 @@
 #  \version 7.5.1 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
-# 
-# The SU2 Project is maintained by the SU2 Foundation 
+#
+# The SU2 Project is maintained by the SU2 Foundation
 # (http://su2foundation.org)
 #
 # Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
@@ -16,7 +16,7 @@
 # modify it under the terms of the GNU Lesser General Public
 # License as published by the Free Software Foundation; either
 # version 2.1 of the License, or (at your option) any later version.
-# 
+#
 # SU2 is distributed in the hope that it will be useful,
 # but WITHOUT ANY WARRANTY; without even the implied warranty of
 # MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
@@ -29,11 +29,11 @@
 from __future__ import print_function
 
 import sys
-from TestCase import TestCase    
+from TestCase import TestCase
 
 def main():
-    '''This program runs SU2 and ensures that the output matches specified values. 
-       This will be used to do checks when code is pushed to github 
+    '''This program runs SU2 and ensures that the output matches specified values.
+       This will be used to do checks when code is pushed to github
        to make sure nothing is broken. '''
 
     test_list = []
@@ -49,7 +49,7 @@ def main():
     discadj_naca0012.test_iter = 100
     discadj_naca0012.test_vals = [-3.561506, -8.926634, -0.000000, 0.005587]
     test_list.append(discadj_naca0012)
-   
+
     # Inviscid Cylinder 3D (multiple markers)
     discadj_cylinder3D           = TestCase('discadj_cylinder3D')
     discadj_cylinder3D.cfg_dir   = "disc_adj_euler/cylinder3D"
@@ -65,7 +65,7 @@ def main():
     discadj_arina2k.test_iter    = 20
     discadj_arina2k.test_vals    = [-3.111181, -3.501516, 6.8705e-02, 0]
     test_list.append(discadj_arina2k)
-    
+
     # Equivalent area NACA64-206
     ea_naca64206              = TestCase('ea_naca64206')
     ea_naca64206.cfg_dir      = "optimization_euler/equivalentarea_naca64206"
@@ -157,16 +157,16 @@ def main():
     #######################################################
     ### Unsteady Disc. adj. compressible RANS           ###
     #######################################################
-   
+
     # Turbulent Cylinder
     discadj_cylinder           = TestCase('unsteady_cylinder')
     discadj_cylinder.cfg_dir   = "disc_adj_rans/cylinder"
-    discadj_cylinder.cfg_file  = "cylinder.cfg" 
+    discadj_cylinder.cfg_file  = "cylinder.cfg"
     discadj_cylinder.test_iter = 9
     discadj_cylinder.test_vals = [3.746909, -1.544883, -0.008321, 0.000014] #last 4 columns
     discadj_cylinder.unsteady  = True
     test_list.append(discadj_cylinder)
-    
+
     ##############################################################
     ### Unsteady Disc. adj. compressible RANS Windowed Average ###
     ##############################################################
@@ -174,12 +174,12 @@ def main():
     # Turbulent Cylinder
     discadj_cylinder           = TestCase('unsteady_cylinder_windowed_average_AD')
     discadj_cylinder.cfg_dir   = "disc_adj_rans/cylinder"
-    discadj_cylinder.cfg_file  = "cylinder_Windowing_AD.cfg" 
+    discadj_cylinder.cfg_file  = "cylinder_Windowing_AD.cfg"
     discadj_cylinder.test_iter = 9
     discadj_cylinder.test_vals = [3.004406] #last column
     discadj_cylinder.unsteady  = True
     test_list.append(discadj_cylinder)
-    
+
     ##############################################################
     ### Unsteady Disc. adj. compressible RANS Windowed Average ###
     ##############################################################
@@ -187,14 +187,14 @@ def main():
     # Turbulent Cylinder
     discadj_cylinder           = TestCase('unsteady_cylinder_windowed_average')
     discadj_cylinder.cfg_dir   = "disc_adj_rans/cylinder"
-    discadj_cylinder.cfg_file  = "cylinder_Windowing.cfg" 
+    discadj_cylinder.cfg_file  = "cylinder_Windowing.cfg"
     discadj_cylinder.test_iter = 6
     discadj_cylinder.test_vals = [0.202349, -0.000119, 1.899933, -0.000050, 1.067900]
     discadj_cylinder.tol       = 0.0001
     discadj_cylinder.command   = TestCase.Command("mpirun -n 2", "SU2_CFD_DIRECTDIFF")
     discadj_cylinder.unsteady  = True
-    test_list.append(discadj_cylinder)  
-    
+    test_list.append(discadj_cylinder)
+
     ##########################################################################
     ### Unsteady Disc. adj. compressible RANS DualTimeStepping 1st order   ###
     ##########################################################################
@@ -224,27 +224,27 @@ def main():
     #######################################################
     ### Disc. adj. turbomachinery                       ###
     #######################################################
-    
+
     # Transonic Stator 2D
     discadj_trans_stator           = TestCase('transonic_stator')
     discadj_trans_stator.cfg_dir   = "disc_adj_turbomachinery/transonic_stator_2D"
-    discadj_trans_stator.cfg_file  = "transonic_stator.cfg" 
+    discadj_trans_stator.cfg_file  = "transonic_stator.cfg"
     discadj_trans_stator.test_iter = 79
     discadj_trans_stator.test_vals = [79.000000, -1.941681, -1.984570]
     test_list.append(discadj_trans_stator)
-    
+
     ###################################
     ### Structural Adjoint          ###
     ###################################
-   
+
     # Structural model
     discadj_fea           = TestCase('discadj_fea')
     discadj_fea.cfg_dir   = "disc_adj_fea"
-    discadj_fea.cfg_file  = "configAD_fem.cfg" 
+    discadj_fea.cfg_file  = "configAD_fem.cfg"
     discadj_fea.test_iter = 4
     discadj_fea.test_vals         = [-2.849774, -3.238669, -0.000364, -8.708700] #last 4 columns
     discadj_fea.test_vals_aarch64 = [-2.849726, -3.238594, -0.000364, -8.708700] #last 4 columns
-    test_list.append(discadj_fea) 
+    test_list.append(discadj_fea)
 
     ###################################
     ### Disc. adj. heat             ###
@@ -255,14 +255,14 @@ def main():
     discadj_heat.cfg_dir   = "disc_adj_heat"
     discadj_heat.cfg_file  = "disc_adj_heat.cfg"
     discadj_heat.test_iter = 10
-    discadj_heat.test_vals         = [-2.280433, 0.714828, -0.743730, -6.767300]
-    discadj_heat.test_vals_aarch64 = [-2.280428, 0.714835, -0.743730, -6.767300]
+    discadj_heat.test_vals         = [-2.226525, 0.603989, 0.000000, -6.256200]
+    discadj_heat.test_vals_aarch64 = [-2.226525, 0.603989, 0.000000, -6.256200]
     test_list.append(discadj_heat)
 
     ###################################
     ### Coupled FSI Adjoint         ###
     ###################################
-   
+
     # Legacy driver
     discadj_fsi           = TestCase('discadj_fsi')
     discadj_fsi.cfg_dir   = "disc_adj_fsi"
@@ -316,8 +316,8 @@ def main():
     da_unsteadyCHT_cylinder.cfg_dir   = "coupled_cht/disc_adj_unsteadyCHT_cylinder"
     da_unsteadyCHT_cylinder.cfg_file  = "chtMaster.cfg"
     da_unsteadyCHT_cylinder.test_iter = 2
-    da_unsteadyCHT_cylinder.test_vals         = [-3.521358, -4.312658, -4.271025, -9.846075, -7.967741, 0.000000, 3.684000, 2.9483e-01]
-    da_unsteadyCHT_cylinder.test_vals_aarch64 = [-3.521358, -4.312658, -4.271025, -9.846075, -7.967741, 0.000000, 3.684000, 2.9483e-01]
+    da_unsteadyCHT_cylinder.test_vals         = [-3.508906, -4.317739, -4.241558, -11.836892, -12.862650, 0.000000, 3.688000, 0.295190]
+    da_unsteadyCHT_cylinder.test_vals_aarch64 = [-3.508906, -4.317739, -4.241558, -11.836892, -12.862650, 0.000000, 3.688000, 0.295190]
     da_unsteadyCHT_cylinder.unsteady  = True
     da_unsteadyCHT_cylinder.multizone = True
     test_list.append(da_unsteadyCHT_cylinder)
@@ -364,7 +364,7 @@ def main():
     # NACA0012 Airfoil
     unsteady_naca0012           = TestCase('unsteady_NACA0012_restart_adjoint')
     unsteady_naca0012.cfg_dir   = "disc_adj_rans/naca0012"
-    unsteady_naca0012.cfg_file  = "naca0012.cfg" 
+    unsteady_naca0012.cfg_file  = "naca0012.cfg"
     unsteady_naca0012.test_iter = 14
     unsteady_naca0012.command   = TestCase.Command(exec = "discrete_adjoint.py", param = "-f")
     unsteady_naca0012.timeout   = 1600
@@ -373,7 +373,7 @@ def main():
     unsteady_naca0012.unsteady  = True
     pass_list.append(unsteady_naca0012.run_filediff())
     test_list.append(unsteady_naca0012)
-    
+
     ####################################################################################
     ### Unsteady Disc. adj. compressible RANS Windowed Average  only adjoint 		 ###
     ####################################################################################
@@ -381,7 +381,7 @@ def main():
     # NACA0012 Airfoil (Test depends on results of "unsteady_NACA0012_restart_adjoint")
     unsteady_naca0012           = TestCase('unsteady_NACA0012_adjoint_only')
     unsteady_naca0012.cfg_dir   = "disc_adj_rans/naca0012"
-    unsteady_naca0012.cfg_file  = "naca0012.cfg" 
+    unsteady_naca0012.cfg_file  = "naca0012.cfg"
     unsteady_naca0012.test_iter = 14
     unsteady_naca0012.command   = TestCase.Command(exec = "discrete_adjoint.py", param = "-m adj -f")
     unsteady_naca0012.timeout   = 1600

From d7709556e1e992bd2e7fdcb4e45489b9cebf41bc Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 14 Feb 2023 15:26:37 +0100
Subject: [PATCH 200/656] Updated AD regression file

---
 SU2_CFD/include/solvers/CMeshSolver.hpp       |  1 +
 SU2_CFD/src/solvers/CEulerSolver.cpp          |  2 +-
 SU2_CFD/src/solvers/CIncEulerSolver.cpp       |  1 +
 .../naca0012/inv_NACA0012_discadj.cfg         |  2 +-
 TestCases/serial_regression_AD.py             | 38 +++++++++----------
 5 files changed, 23 insertions(+), 21 deletions(-)

diff --git a/SU2_CFD/include/solvers/CMeshSolver.hpp b/SU2_CFD/include/solvers/CMeshSolver.hpp
index 18fb2a86ef3..79876e016c1 100644
--- a/SU2_CFD/include/solvers/CMeshSolver.hpp
+++ b/SU2_CFD/include/solvers/CMeshSolver.hpp
@@ -125,6 +125,7 @@ class CMeshSolver final : public CFEASolver {
   /*!
    * \brief Grid deformation using the linear elasticity equations.
    * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] numerics - Numerics used in the solution.
    * \param[in] config - Definition of the particular problem.
    */
   void DeformMesh(CGeometry **geometry,
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index ad340c2d7cd..b343590cafd 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -1674,7 +1674,7 @@ unsigned long CEulerSolver::SetPrimitive_Variables(CSolver **solver_container, c
     /*--- Update en---*/
     if(config->GetKind_FluidModel() == DATADRIVEN_FLUID) {
       nodes->SetDataExtrapolation(iPoint, GetFluidModel()->GetExtrapolation());
-      nodes->SetEntropy(iPoint, GetFluidModel()->GetStaticEnergy());
+      nodes->SetEntropy(iPoint, GetFluidModel()->GetEntropy());
     }
 
     /* Check for non-realizable states for reporting. */
diff --git a/SU2_CFD/src/solvers/CIncEulerSolver.cpp b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
index b6192e51a98..165f2a4230d 100644
--- a/SU2_CFD/src/solvers/CIncEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
@@ -330,6 +330,7 @@ void CIncEulerSolver::SetNondimensionalization(CConfig *config, unsigned short i
       break;
 
     case DATADRIVEN_FLUID:
+    
       auxFluidModel = new CDataDrivenFluid(config);
       auxFluidModel->SetTDState_T(Temperature_FreeStream);
       Pressure_Thermodynamic = auxFluidModel->GetPressure();
diff --git a/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg b/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg
index 6cceb3d0f44..49bda853bcd 100644
--- a/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg
+++ b/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg
@@ -46,7 +46,7 @@ CFL_NUMBER= 5.0
 CFL_ADAPT= NO
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-ITER= 100
+ITER= 150
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
diff --git a/TestCases/serial_regression_AD.py b/TestCases/serial_regression_AD.py
index 103e12d3565..6ce4f0b8693 100644
--- a/TestCases/serial_regression_AD.py
+++ b/TestCases/serial_regression_AD.py
@@ -6,8 +6,8 @@
 #  \version 7.5.1 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
-# 
-# The SU2 Project is maintained by the SU2 Foundation 
+#
+# The SU2 Project is maintained by the SU2 Foundation
 # (http://su2foundation.org)
 #
 # Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
@@ -16,7 +16,7 @@
 # modify it under the terms of the GNU Lesser General Public
 # License as published by the Free Software Foundation; either
 # version 2.1 of the License, or (at your option) any later version.
-# 
+#
 # SU2 is distributed in the hope that it will be useful,
 # but WITHOUT ANY WARRANTY; without even the implied warranty of
 # MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
@@ -32,8 +32,8 @@
 from TestCase import TestCase
 
 def main():
-    '''This program runs SU2 and ensures that the output matches specified values. 
-       This will be used to do checks when code is pushed to github 
+    '''This program runs SU2 and ensures that the output matches specified values.
+       This will be used to do checks when code is pushed to github
        to make sure nothing is broken. '''
 
     test_list = []
@@ -58,7 +58,7 @@ def main():
     discadj_cylinder3D.test_vals = [-3.737675, -3.842311, -0.000000, 0.000000]
     test_list.append(discadj_cylinder3D)
 
-    # Arina nozzle 2D  
+    # Arina nozzle 2D
     discadj_arina2k              = TestCase('discadj_arina2k')
     discadj_arina2k.cfg_dir      = "disc_adj_euler/arina2k"
     discadj_arina2k.cfg_file     = "Arina2KRS.cfg"
@@ -69,7 +69,7 @@ def main():
     #######################################################
     ### Disc. adj. compressible RANS                    ###
     #######################################################
-    
+
     # Adjoint turbulent NACA0012 SA
     discadj_rans_naca0012_sa           = TestCase('discadj_rans_naca0012_sa')
     discadj_rans_naca0012_sa.cfg_dir   = "disc_adj_rans/naca0012"
@@ -133,16 +133,16 @@ def main():
     #######################################################
     ### Unsteady Disc. adj. compressible RANS           ###
     #######################################################
-   
+
     # Turbulent Cylinder
     discadj_cylinder           = TestCase('unsteady_cylinder')
     discadj_cylinder.cfg_dir   = "disc_adj_rans/cylinder"
-    discadj_cylinder.cfg_file  = "cylinder.cfg" 
+    discadj_cylinder.cfg_file  = "cylinder.cfg"
     discadj_cylinder.test_iter = 9
     discadj_cylinder.test_vals = [3.746909, -1.544883, -0.008321, 0.000014] #last 4 columns
     discadj_cylinder.unsteady  = True
     test_list.append(discadj_cylinder)
-    
+
     ##########################################################################
     ### Unsteady Disc. adj. compressible RANS DualTimeStepping 1st order   ###
     ##########################################################################
@@ -181,15 +181,15 @@ def main():
     ###################################
     ### Structural Adjoint          ###
     ###################################
-   
+
     # Structural model
     discadj_fea           = TestCase('discadj_fea')
     discadj_fea.cfg_dir   = "disc_adj_fea"
-    discadj_fea.cfg_file  = "configAD_fem.cfg" 
+    discadj_fea.cfg_file  = "configAD_fem.cfg"
     discadj_fea.test_iter = 4
     discadj_fea.test_vals         = [-2.849531, -3.238474, -3.6413e-04, -8.7087] #last 4 columns
     discadj_fea.test_vals_aarch64 = [-2.849570, -3.238519, -3.6413e-04, -8.7087] #last 4 columns
-    test_list.append(discadj_fea)    
+    test_list.append(discadj_fea)
 
     ###################################
     ### Disc. adj. heat             ###
@@ -200,13 +200,13 @@ def main():
     discadj_heat.cfg_dir   = "disc_adj_heat"
     discadj_heat.cfg_file  = "disc_adj_heat.cfg"
     discadj_heat.test_iter = 10
-    discadj_heat.test_vals = [-2.271569, 0.671288, -3.172000, -8.231500] #last 4 columns
+    discadj_heat.test_vals = [-2.227518, 0.576043, 0.000000, -7.753900] #last 4 columns
     test_list.append(discadj_heat)
 
     ###################################
     ### Coupled FSI Adjoint         ###
     ###################################
-   
+
     # Structural model
     discadj_fsi           = TestCase('discadj_fsi')
     discadj_fsi.cfg_dir   = "disc_adj_fsi"
@@ -244,7 +244,7 @@ def main():
             test.tol = 0.00001
 
     pass_list = [ test.run_test() for test in test_list ]
-    
+
     ###################################
     ### Coupled RHT-CFD Adjoint     ###
     ###################################
@@ -265,7 +265,7 @@ def main():
     ######################################
     ### RUN PYTHON TESTS               ###
     ######################################
-    
+
     # test discrete_adjoint.py
     discadj_euler_py = TestCase('discadj_euler_py')
     discadj_euler_py.cfg_dir = "cont_adj_euler/naca0012"
@@ -278,7 +278,7 @@ def main():
     discadj_euler_py.test_file = "of_grad_cd.dat"
     pass_list.append(discadj_euler_py.run_filediff())
     test_list.append(discadj_euler_py)
-    
+
     # test discrete_adjoint with multiple ffd boxes
     discadj_multiple_ffd_py = TestCase('discadj_multiple_ffd_py')
     discadj_multiple_ffd_py.cfg_dir = "multiple_ffd/naca0012"
@@ -382,7 +382,7 @@ def main():
             print('  passed - %s'%test.tag)
         else:
             print('* FAILED - %s'%test.tag)
-    
+
     if all(pass_list):
         sys.exit(0)
     else:

From a857dbca65cd3538a6b6d616890883e975bb4b8b Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 14 Feb 2023 16:50:49 +0100
Subject: [PATCH 201/656] Added datadriven fluid model test case back

---
 TestCases/nicf/datadriven/datadriven_nozzle.cfg | 7 +++----
 TestCases/parallel_regression.py                | 8 ++++++++
 2 files changed, 11 insertions(+), 4 deletions(-)

diff --git a/TestCases/nicf/datadriven/datadriven_nozzle.cfg b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
index e86d180f469..882f310d269 100644
--- a/TestCases/nicf/datadriven/datadriven_nozzle.cfg
+++ b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
@@ -25,7 +25,7 @@ MACH_NUMBER= 1E-9
 AOA= 0.0
 SIDESLIP_ANGLE= 0.0
 INIT_OPTION= TD_CONDITIONS
-FREESTREAM_OPTION= DENSITY_FS
+FREESTREAM_OPTION= TEMPERATURE_FS
 FREESTREAM_PRESSURE= 250000.0
 %
 % Free-stream temperature (288.15 K, 518.67 R by default)
@@ -38,7 +38,7 @@ REF_DIMENSIONALIZATION= DIMENSIONAL
 FLUID_MODEL = DATADRIVEN_FLUID
 INTERPOLATION_METHOD = MLP 
 FILENAMES_INTERPOLATOR = (MLP_air.mlp)
-DATADRIVEN_NEWTON_RELAXATION = 0.95
+DATADRIVEN_NEWTON_RELAXATION = 0.8
 DATADRIVEN_FLUID_INITIAL_DENSITY = 5.54548
 DATADRIVEN_FLUID_INITIAL_ENERGY = 1.8e+05
 
@@ -51,8 +51,7 @@ CONDUCTIVITY_MODEL= CONSTANT_CONDUCTIVITY
 THERMAL_CONDUCTIVITY_CONSTANT= 0.030542828
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
-MARKER_HEATFLUX= ( WALL, 0.0 )
-MARKER_SYM= ( SYMMETRY )
+MARKER_SYM= ( SYMMETRY, WALL )
 MARKER_RIEMANN= ( INFLOW, TOTAL_CONDITIONS_PT,  904388, 542.13, 1.0, 0.0, 0.0, OUTFLOW, STATIC_PRESSURE, 200000.0, 0.0, 0.0, 0.0, 0.0 )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index e0fad895d88..a29c87b4f85 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -991,6 +991,14 @@ def main():
     coolprop_fluidModel.test_vals = [-4.525458, -1.578441, 3.439057, 0.000000, 0.000000]
     test_list.append(coolprop_fluidModel)
 
+    # Rarefaction Q1D nozzle, include CoolProp fluid model
+    datadriven_fluidModel           = TestCase('datadriven_fluidModel')
+    datadriven_fluidModel.cfg_dir   = "nicf/datadriven"
+    datadriven_fluidModel.cfg_file  = "datadriven_nozzle.cfg"
+    datadriven_fluidModel.test_iter = 20
+    datadriven_fluidModel.test_vals = [-1.873575, 0.964932, 5.467181, 0.000000, 0.000000]
+    test_list.append(datadriven_fluidModel)
+
     # Rarefaction Q1D nozzle, include CoolProp transport model
     coolprop_transportModel           = TestCase('coolprop_transportModel')
     coolprop_transportModel.cfg_dir   = "nicf/coolprop"

From 00b79eafc01a39e12c7b2c25cc422537281492e2 Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Tue, 14 Feb 2023 17:50:08 -0500
Subject: [PATCH 202/656] some changes...will still fail

---
 SU2_CFD/src/solvers/CNEMOEulerSolver.cpp | 51 ++++++++++++------------
 SU2_CFD/src/solvers/CNEMONSSolver.cpp    | 30 +++++++-------
 2 files changed, 40 insertions(+), 41 deletions(-)

diff --git a/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp b/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
index 717f4dfb7a7..8e9fbb175eb 100644
--- a/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
@@ -654,7 +654,7 @@ su2double CNEMOEulerSolver::ComputeConsistentExtrapolation(CNEMOGas *fluidmodel,
   /*--- Rename density vector ---*/
   vector<su2double> rhos;
   rhos.resize(nSpecies,0.0);
-  for (unsigned short iSpecies=0; iSpecies < nSpecies; iSpecies++ ){
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++ ){
     rhos[iSpecies] = V[iSpecies];
   }
 
@@ -1613,9 +1613,8 @@ void CNEMOEulerSolver::BC_Inlet(CGeometry *geometry, CSolver **solver_container,
                                 CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) {
   SU2_MPI::Error("BC_INLET: Not operational in NEMO.", CURRENT_FUNCTION);
 
-  unsigned short iVar, iDim, iSpecies, RHO_INDEX, nSpecies;
+  unsigned short RHO_INDEX, nSpecies;
 
-  unsigned long iVertex, iPoint;
   su2double  T_Total, P_Total, Velocity[3], Velocity2, H_Total, Temperature, Riemann,
   Pressure, Density, Energy, Mach2, SoundSpeed2, SoundSpeed_Total2, Vel_Mag,
   alpha, aa, bb, cc, dd, Area, UnitNormal[3] = {0.0};
@@ -1635,31 +1634,31 @@ void CNEMOEulerSolver::BC_Inlet(CGeometry *geometry, CSolver **solver_container,
 
   nSpecies = config->GetnSpecies();
   su2double *Spec_Density = new su2double[nSpecies];
-  for(iSpecies=0; iSpecies<nSpecies; iSpecies++)
+  for (auto iSpecies = 0ul; iSpecies<nSpecies; iSpecies++)
     Spec_Density[iSpecies] = 0.0;               /*--- To avoid a compiler warning. ---*/
 
   RHO_INDEX = nodes->GetRhoIndex();
 
   /*--- Loop over all the vertices on this boundary marker ---*/
-  for (iVertex = 0; iVertex < geometry->nVertex[val_marker]; iVertex++) {
-    iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
+  for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
+    const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
     /*--- Check if the node belongs to the domain (i.e., not a halo node) ---*/
     if (geometry->nodes->GetDomain(iPoint)) {
 
       /*--- Normal vector for this vertex (negate for outward convention) ---*/
       geometry->vertex[val_marker][iVertex]->GetNormal(Normal);
-      for (iDim = 0; iDim < nDim; iDim++) Normal[iDim] = -Normal[iDim];
+      for (auto iDim = 0ul; iDim < nDim; iDim++) Normal[iDim] = -Normal[iDim];
       conv_numerics->SetNormal(Normal);
 
       Area = GeometryToolbox::Norm(nDim, Normal);
 
-      for (iDim = 0; iDim < nDim; iDim++)
+      for (auto iDim = 0ul; iDim < nDim; iDim++)
         UnitNormal[iDim] = Normal[iDim]/Area;
 
       /*--- Retrieve solution at this boundary node ---*/
-      for (iVar = 0; iVar < nVar; iVar++)     U_domain[iVar] = nodes->GetSolution(iPoint, iVar);
-      for (iVar = 0; iVar < nPrimVar; iVar++) V_domain[iVar] = nodes->GetPrimitive(iPoint,iVar);
+      for (auto iVar = 0ul; iVar < nVar; iVar++)     U_domain[iVar] = nodes->GetSolution(iPoint, iVar);
+      for (auto iVar = 0ul; iVar < nPrimVar; iVar++) V_domain[iVar] = nodes->GetPrimitive(iPoint,iVar);
 
       /*--- Build the fictitious intlet state based on characteristics ---*/
 
@@ -1686,7 +1685,7 @@ void CNEMOEulerSolver::BC_Inlet(CGeometry *geometry, CSolver **solver_container,
 
         /*--- Store primitives and set some variables for clarity. ---*/
         Density = V_domain[RHO_INDEX];
-        for (iDim = 0; iDim < nDim; iDim++)
+        for (auto iDim = 0ul; iDim < nDim; iDim++)
           Velocity[iDim] = U_domain[nSpecies+iDim]/Density;
 
         Velocity2   = GeometryToolbox::SquaredNorm(nDim, Velocity);
@@ -1698,7 +1697,7 @@ void CNEMOEulerSolver::BC_Inlet(CGeometry *geometry, CSolver **solver_container,
         /*--- Compute the acoustic Riemann invariant that is extrapolated
            from the domain interior. ---*/
         Riemann   = 2.0*sqrt(SoundSpeed2)/Gamma_Minus_One;
-        for (iDim = 0; iDim < nDim; iDim++)
+        for (auto iDim = 0ul; iDim < nDim; iDim++)
           Riemann += Velocity[iDim]*UnitNormal[iDim];
 
         /*--- Total speed of sound ---*/
@@ -1733,7 +1732,7 @@ void CNEMOEulerSolver::BC_Inlet(CGeometry *geometry, CSolver **solver_container,
         SoundSpeed2 = SoundSpeed_Total2 - 0.5*Gamma_Minus_One*Velocity2;
 
         /*--- Compute new velocity vector at the inlet ---*/
-        for (iDim = 0; iDim < nDim; iDim++)
+        for (auto iDim = 0ul; iDim < nDim; iDim++)
           Velocity[iDim] = Vel_Mag*Flow_Dir[iDim];
 
         /*--- Static temperature from the speed of sound relation ---*/
@@ -1752,19 +1751,19 @@ void CNEMOEulerSolver::BC_Inlet(CGeometry *geometry, CSolver **solver_container,
         //NEED EVE AS WELL
 
         /*--- Conservative variables, using the derived quantities ---*/
-        for (iSpecies=0; iSpecies<nSpecies; iSpecies++)
+        for (auto iSpecies = 0ul; iSpecies<nSpecies; iSpecies++)
           U_inlet[iSpecies] = Spec_Density[iSpecies];
-        for (iDim = 0; iDim < nDim; iDim++)
+        for (auto iDim = 0ul; iDim < nDim; iDim++)
           U_inlet[nSpecies+iDim] = Velocity[iDim]*Density;
         U_inlet[nVar-2] = Energy*Density;
         //U_inlet[nVar-1]=Eve
 
         /*--- Primitive variables, using the derived quantities ---*/
-        for (iSpecies=0; iSpecies<nSpecies; iSpecies++)
+        for (auto iSpecies = 0ul; iSpecies<nSpecies; iSpecies++)
           V_inlet[iSpecies] = Spec_Density[iSpecies];
         V_inlet[nSpecies] = Temperature;
         //V_inlet[nSpecies+1] = Tve
-        for (iDim = 0; iDim < nDim; iDim++)
+        for (auto iDim = 0ul; iDim < nDim; iDim++)
           V_inlet[nSpecies+2] = Velocity[iDim];
         V_inlet[nSpecies+nDim+2] = Pressure;
         V_inlet[RHO_INDEX] = Density;
@@ -1788,7 +1787,7 @@ void CNEMOEulerSolver::BC_Inlet(CGeometry *geometry, CSolver **solver_container,
         Vel_Mag /= config->GetVelocity_Ref();
 
         /*--- Get primitives from current inlet state. ---*/
-        for (iDim = 0; iDim < nDim; iDim++)
+        for (auto iDim = 0ul; iDim < nDim; iDim++)
           Velocity[iDim] = nodes->GetVelocity(iPoint, iDim);
         Pressure    = nodes->GetPressure(iPoint);
         SoundSpeed2 = Gamma*Pressure/U_domain[0];
@@ -1796,12 +1795,12 @@ void CNEMOEulerSolver::BC_Inlet(CGeometry *geometry, CSolver **solver_container,
         /*--- Compute the acoustic Riemann invariant that is extrapolated
            from the domain interior. ---*/
         Riemann = Two_Gamma_M1*sqrt(SoundSpeed2);
-        for (iDim = 0; iDim < nDim; iDim++)
+        for (auto iDim = 0ul; iDim < nDim; iDim++)
           Riemann += Velocity[iDim]*UnitNormal[iDim];
 
         /*--- Speed of sound squared for fictitious inlet state ---*/
         SoundSpeed2 = Riemann;
-        for (iDim = 0; iDim < nDim; iDim++)
+        for (auto iDim = 0ul; iDim < nDim; iDim++)
           SoundSpeed2 -= Vel_Mag*Flow_Dir[iDim]*UnitNormal[iDim];
 
         SoundSpeed2 = max(0.0,0.5*Gamma_Minus_One*SoundSpeed2);
@@ -1815,13 +1814,13 @@ void CNEMOEulerSolver::BC_Inlet(CGeometry *geometry, CSolver **solver_container,
 
         /*--- Conservative variables, using the derived quantities ---*/
         U_inlet[0] = Density;
-        for (iDim = 0; iDim < nDim; iDim++)
+        for (auto iDim = 0ul; iDim < nDim; iDim++)
           U_inlet[iDim+1] = Vel_Mag*Flow_Dir[iDim]*Density;
         U_inlet[nDim+1] = Energy*Density;
 
         /*--- Primitive variables, using the derived quantities ---*/
         V_inlet[0] = Pressure / ( Gas_Constant * Density);
-        for (iDim = 0; iDim < nDim; iDim++)
+        for (auto iDim = 0ul; iDim < nDim; iDim++)
           V_inlet[iDim+1] = Vel_Mag*Flow_Dir[iDim];
         V_inlet[nDim+1] = Pressure;
         V_inlet[nDim+2] = Density;
@@ -1971,7 +1970,7 @@ void CNEMOEulerSolver::BC_Outlet(CGeometry *geometry, CSolver **solver_container
       su2double Mach_Exit   = sqrt(Velocity2)/SoundSpeed;
 
       /*--- Compute Species Concentrations ---*/
-      for (iSpecies =0; iSpecies<nSpecies;iSpecies++){
+      for (auto iSpecies = 0ul; iSpecies<nSpecies;iSpecies++){
         Ys[iSpecies] = V_domain[iSpecies]/Density;
       }
 
@@ -1981,8 +1980,8 @@ void CNEMOEulerSolver::BC_Outlet(CGeometry *geometry, CSolver **solver_container
         /*--- Supersonic exit flow: there are no incoming characteristics,
          so no boundary condition is necessary. Set outlet state to current
          state so that upwinding handles the direction of propagation. ---*/
-        for (iVar = 0; iVar < nVar; iVar++)     U_outlet[iVar] = U_domain[iVar];
-        for (iVar = 0; iVar < nPrimVar; iVar++) V_outlet[iVar] = V_domain[iVar];
+        for (auto iVar = 0ul; iVar < nVar; iVar++)     U_outlet[iVar] = U_domain[iVar];
+        for (auto iVar = 0ul; iVar < nPrimVar; iVar++) V_outlet[iVar] = V_domain[iVar];
 
       } else {
 
@@ -2221,7 +2220,7 @@ void CNEMOEulerSolver::BC_Supersonic_Inlet(
       Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
 
     /*--- Viscous contribution ---*/
-    bool viscous = config->GetViscous();
+    const bool viscous = config->GetViscous();
     if (viscous) {
 
       /*--- Set the normal vector and the coordinates ---*/
diff --git a/SU2_CFD/src/solvers/CNEMONSSolver.cpp b/SU2_CFD/src/solvers/CNEMONSSolver.cpp
index 573b5aa4bae..1101757271c 100644
--- a/SU2_CFD/src/solvers/CNEMONSSolver.cpp
+++ b/SU2_CFD/src/solvers/CNEMONSSolver.cpp
@@ -381,11 +381,11 @@ void CNEMONSSolver::BC_HeatFluxCatalytic_Wall(CGeometry *geometry,
   /*--- Allocate arrays ---*/
   dYdn = new su2double[nSpecies];
   GradY = new su2double*[nSpecies];
-  for (iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
     GradY[iSpecies] = new su2double[nDim];
 
   /*--- Loop over all of the vertices on this boundary marker ---*/
-  for(iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
+  for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
     iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
     /*--- Check if the node belongs to the domain (i.e, not a halo node) ---*/
@@ -396,17 +396,17 @@ void CNEMONSSolver::BC_HeatFluxCatalytic_Wall(CGeometry *geometry,
       Area = GeometryToolbox::Norm(nDim, Normal);
 
       /*--- Initialize the convective & viscous residuals to zero ---*/
-      for (iVar = 0ul; iVar < nVar; iVar++) {
+      for (auto iVar = 0ul; iVar < nVar; iVar++) {
         Res_Visc[iVar] = 0.0;
         Res_Sour[iVar] = 0.0;
       }
 
       /*--- Assign wall velocity to "Vector" array ---*/
-      for (iDim = 0ul; iDim < nDim; iDim++) Vector[iDim] = 0.0;
+      for (auto iDim = 0ul; iDim < nDim; iDim++) Vector[iDim] = 0.0;
 
       /*--- Set the residual, truncation error, and velocity value ---*/
       nodes->SetVelocity_Old(iPoint,Vector);
-      for (iDim = 0ul; iDim < nDim; iDim++) {
+      for (auto iDim = 0ul; iDim < nDim; iDim++) {
         LinSysRes(iPoint, nSpecies+iDim) = 0.0;
         nodes->SetVal_ResTruncError_Zero(iPoint,nSpecies+iDim);
       }
@@ -416,7 +416,7 @@ void CNEMONSSolver::BC_HeatFluxCatalytic_Wall(CGeometry *geometry,
       const auto GradV  = nodes->GetGradient_Primitive(iPoint);
       su2double dTdn   = 0.0;
       su2double dTvedn = 0.0;
-      for (iDim = 0ul; iDim < nDim; iDim++) {
+      for (auto iDim = 0ul; iDim < nDim; iDim++) {
         dTdn   += GradV[T_INDEX][iDim]*Normal[iDim];
         dTvedn += GradV[TVE_INDEX][iDim]*Normal[iDim];
       }
@@ -431,20 +431,20 @@ void CNEMONSSolver::BC_HeatFluxCatalytic_Wall(CGeometry *geometry,
         Ds  = nodes->GetDiffusionCoeff(iPoint);
 
         /*--- Calculate normal derivative of mass fraction ---*/
-        for (iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
+        for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
           Ys = V[RHOS_INDEX+iSpecies]/rho;
           dYdn[iSpecies] = 0.0;
-          for (iDim = 0ul; iDim < nDim; iDim++)
+          for (auto iDim = 0ul; iDim < nDim; iDim++)
             dYdn[iSpecies] += 1.0/rho * (GradV[RHOS_INDEX+iSpecies][iDim] -
                 Ys*GradV[RHO_INDEX][iDim])*Normal[iDim];
         }
 
         /*--- Calculate supplementary quantities ---*/
         SdYdn = 0.0;
-        for (iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
+        for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
           SdYdn += rho*Ds[iSpecies]*dYdn[iSpecies];
 
-        for (iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
+        for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
           Ys   = V[RHOS_INDEX+iSpecies]/rho;
           //eves = nodes->CalcEve(config, V[TVE_INDEX], iSpecies);
           //hs   = nodes->CalcHs(config, V[T_INDEX], eves, iSpecies);
@@ -493,7 +493,7 @@ void CNEMONSSolver::BC_HeatFluxCatalytic_Wall(CGeometry *geometry,
        Note that we need to add a contribution for moving walls to the Jacobian. ---*/
       if (implicit) {
         /*--- Enforce the no-slip boundary condition in a strong way ---*/
-        for (iVar = nSpecies; iVar < nSpecies+nDim; iVar++) {
+        for (auto iVar = nSpecies; iVar < nSpecies+nDim; iVar++) {
           total_index = iPoint*nVar+iVar;
           Jacobian.DeleteValsRowi(total_index);
         }
@@ -502,7 +502,7 @@ void CNEMONSSolver::BC_HeatFluxCatalytic_Wall(CGeometry *geometry,
     }
   }
 
-  for (iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
+  for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
     delete [] GradY[iSpecies];
   delete [] GradY;
   delete [] dYdn;
@@ -729,7 +729,7 @@ void CNEMONSSolver::BC_IsothermalCatalytic_Wall(CGeometry *geometry,
         }
 
         /*--- Calculate species residual at wall ---*/
-        for (iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
+        for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
           dYdn = (Yst[iSpecies]-Vj[RHOS_INDEX+iSpecies]/Vj[RHO_INDEX])/dij;
           Res_Visc[iSpecies]  = -(-rho*Di[iSpecies]*dYdn+Yst[iSpecies]*SdYdn)*Area;
         }
@@ -761,8 +761,8 @@ void CNEMONSSolver::BC_IsothermalCatalytic_Wall(CGeometry *geometry,
 
           /*--- Take the primitive var. Jacobian & store in Jac. jj ---*/
           // Species mass fraction
-          for (iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
-            for (jSpecies = 0ul; jSpecies < nSpecies; jSpecies++)
+          for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++) {
+            for (auto jSpecies = 0ul; jSpecies < nSpecies; jSpecies++)
               Jacobian_j[iSpecies][jSpecies] += -Yst[iSpecies]*rho*Di[jSpecies]/dij;
             Jacobian_j[iSpecies][iSpecies] += rho*Di[iSpecies]/dij - SdYdn;
           }

From 24ca5f8131f7d9a6c486783d3c50619cf2612cf2 Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Wed, 15 Feb 2023 11:20:16 -0500
Subject: [PATCH 203/656] Compiles now

---
 SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp  | 6 ++++--
 SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp | 2 +-
 SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp   | 3 ++-
 SU2_CFD/src/solvers/CNEMOEulerSolver.cpp     | 8 ++++----
 4 files changed, 11 insertions(+), 8 deletions(-)

diff --git a/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp b/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp
index 9fdf3f49eea..a949c249f98 100644
--- a/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp
+++ b/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp
@@ -363,7 +363,8 @@ void CNEMONumerics::GetPMatrix(const su2double *U, const su2double *V, const su2
   su2double sqvel = 0.0;
   const su2double rho = V[RHO_INDEX];
   const su2double eve = U[nSpecies+nDim+1]/rho;
-  su2double vU = vV = vW = 0.0;
+  su2double vU, vV, vW;
+  vU = vV = vW = 0.0;
   for (auto iDim = 0ul; iDim < nDim; iDim++) {
     vU    += V[VEL_INDEX+iDim] * val_normal[iDim];
     vV    += V[VEL_INDEX+iDim] * l[iDim];
@@ -456,7 +457,8 @@ void CNEMONumerics::GetPMatrix_inv(const su2double *U, const su2double *V, const
   /*--- Pre-compute useful quantities ---*/
   const su2double rho = V[RHO_INDEX];
   const su2double eve = U[nSpecies+nDim+1]/rho;
-  su2double vU = vV = vW = 0.0;
+  su2double vU, vV, vW;
+  vU = vV = vW = 0.0;
   for (auto iDim = 0ul; iDim < nDim; iDim++) {
     vU += V[VEL_INDEX+iDim] * val_normal[iDim];
     vV += V[VEL_INDEX+iDim] * l[iDim];
diff --git a/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp b/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
index 7f5b10f16a1..af99cc59fde 100644
--- a/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
+++ b/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
@@ -168,7 +168,7 @@ CNumerics::ResidualType<> CAvgGrad_NEMO::ComputeResidual(const CConfig *config)
   if (implicit) {
 
   su2double dist_ij_2[nDim] = {0.0};
-  GeometryToolbox::Distance(nDim, coord_j, coord_i, dist_ij_2);    
+  GeometryToolbox::Distance(nDim, Coord_j, Coord_i, dist_ij_2);
   dist_ij = GeometryToolbox::SquaredNorm(nDim, dist_ij_2);
 
     for (auto iVar = 0ul; iVar < nVar; iVar++) {
diff --git a/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp b/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp
index 1406749e1dd..87f4423b3f4 100644
--- a/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp
+++ b/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp
@@ -290,7 +290,8 @@ CNumerics::ResidualType<> CSource_NEMO::ComputeAxisymmetric(const CConfig *confi
     const su2double qy_ve                = -kve*GV[TVE_INDEX][1];
 
     /*--- Enthalpy and vib-el energy transport due to y-direction diffusion---*/
-    su2double sumJhs_y = sumJeve_y = 0.0;
+    su2double sumJhs_y, sumJeve_y;
+    sumJhs_y = sumJeve_y = 0.0;
     for (auto iSpecies = 0ul; iSpecies < nHeavy; iSpecies++) {
       sumJhs_y  += -(rho*Ds[iSpecies]*GV[RHOS_INDEX+iSpecies][1] - V_i[RHOS_INDEX+iSpecies]*Vector) * hs[iSpecies];
       sumJeve_y += -(rho*Ds[iSpecies]*GV[RHOS_INDEX+iSpecies][1] - V_i[RHOS_INDEX+iSpecies]*Vector) * eve_i[iSpecies];
diff --git a/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp b/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
index 8e9fbb175eb..fe00fdc4958 100644
--- a/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
@@ -1006,7 +1006,6 @@ void CNEMOEulerSolver::SetNondimensionalization(CConfig *config, unsigned short
   const su2double Alpha= config->GetAoA()*PI_NUMBER/180.0;
   const su2double Beta = config->GetAoS()*PI_NUMBER/180.0;
   const su2double Mach = config->GetMach();
-  const su2double Reynolds = config->GetReynolds();
 
   const bool unsteady = (config->GetTime_Marching() != TIME_MARCHING::STEADY);
   const bool viscous  = config->GetViscous();
@@ -1106,7 +1105,7 @@ void CNEMOEulerSolver::SetNondimensionalization(CConfig *config, unsigned short
     config->SetViscosity_FreeStream(Viscosity_FreeStream);
 
     /*--- Compute Reynolds number ---*/
-    Reynolds = (Density_FreeStream*Velocity_Reynolds*config->GetLength_Reynolds())/Viscosity_FreeStream;
+    const su2double Reynolds = (Density_FreeStream*Velocity_Reynolds*config->GetLength_Reynolds())/Viscosity_FreeStream;
     config->SetReynolds(Reynolds);
 
     /*--- Turbulence kinetic energy ---*/
@@ -1956,7 +1955,8 @@ void CNEMOEulerSolver::BC_Outlet(CGeometry *geometry, CSolver **solver_container
       /*--- Check whether the flow is supersonic at the exit. The type
        of boundary update depends on this. ---*/
       su2double Density = V_domain[RHO_INDEX];
-      su2double Velocity2 = Vn = 0.0;
+      su2double Velocity2 = 0.0;
+      su2double Vn = 0.0;
       su2double Velocity[MAXNDIM] = {0.0};
       for (auto iDim = 0ul; iDim < nDim; iDim++) {
         Velocity[iDim] = V_domain[VEL_INDEX+iDim];
@@ -2001,7 +2001,7 @@ void CNEMOEulerSolver::BC_Outlet(CGeometry *geometry, CSolver **solver_container
         //     V: [rho1, ..., rhoNs, T, Tve, u, v, w, P, rho, h, a, rhoCvtr, rhoCvve]^T
         Density    = pow(P_Exit/Entropy,1.0/Gamma);
         Pressure   = P_Exit;
-        SoundSpeed = sqrt(Gamma*P_Exit/Density);
+        const su2double SoundSpeed = sqrt(Gamma*P_Exit/Density);
         Vn_Exit    = Riemann - 2.0*SoundSpeed/Gamma_Minus_One;
         Velocity2  = 0.0;
         for (auto iDim = 0ul; iDim < nDim; iDim++) {

From bc56edc056c1eab241d2c9cbf28bc19e8cf6b770 Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Wed, 15 Feb 2023 11:56:54 -0500
Subject: [PATCH 204/656] I think I got all issues

---
 SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp | 2 +-
 SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp   | 4 +---
 SU2_CFD/src/numerics/NEMO/convection/msw.cpp | 4 ++--
 SU2_CFD/src/numerics/NEMO/convection/roe.cpp | 4 ++--
 SU2_CFD/src/solvers/CNEMOEulerSolver.cpp     | 6 +++---
 SU2_CFD/src/solvers/CNEMONSSolver.cpp        | 3 +--
 6 files changed, 10 insertions(+), 13 deletions(-)

diff --git a/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp b/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
index af99cc59fde..336093761fa 100644
--- a/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
+++ b/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
@@ -167,7 +167,7 @@ CNumerics::ResidualType<> CAvgGrad_NEMO::ComputeResidual(const CConfig *config)
   /*--- Compute the implicit part ---*/
   if (implicit) {
 
-  su2double dist_ij_2[nDim] = {0.0};
+  su2double dist_ij_2[MAXNDIM] = {0.0};
   GeometryToolbox::Distance(nDim, Coord_j, Coord_i, dist_ij_2);
   dist_ij = GeometryToolbox::SquaredNorm(nDim, dist_ij_2);
 
diff --git a/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp b/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp
index 87f4423b3f4..6f115117834 100644
--- a/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp
+++ b/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp
@@ -195,9 +195,7 @@ CNumerics::ResidualType<> CSource_NEMO::ComputeAxisymmetric(const CConfig *confi
   if (Coord_i[1]!= 0.0) yinv = 1.0/Coord_i[1];
   else yinv = 0.0;
 
-  /*--- Rename for convenience ---*/
-  const su2double vel2 = GeometryToolbox::SquaredNorm(nDim, &V_i[VEL_INDEX]);
-
+  /*--- Rename mass flux for convenience ---*/
   for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
     Y[iSpecies] = V_i[RHOS_INDEX+iSpecies] / rho;
 
diff --git a/SU2_CFD/src/numerics/NEMO/convection/msw.cpp b/SU2_CFD/src/numerics/NEMO/convection/msw.cpp
index badd0a81fb6..986ad8a0186 100644
--- a/SU2_CFD/src/numerics/NEMO/convection/msw.cpp
+++ b/SU2_CFD/src/numerics/NEMO/convection/msw.cpp
@@ -172,7 +172,7 @@ CNumerics::ResidualType<> CUpwMSW_NEMO::ComputeResidual(const CConfig *config) {
   fluidmodel->ComputedPdU(Vst_j, eves_st_j, dPdUst_j);
 
   /*--- Flow eigenvalues at i (Lambda+) ---*/
-  for (auto iVar = 0ul; iVar < nSpecies+nDim-1; iVar++)
+  for (auto iVar = 0; iVar < nSpecies+nDim-1; iVar++)
     Lambda_i[iVar]          = 0.5*(ProjVelst_i + sqrt(ProjVelst_i*ProjVelst_i +
                                                       epsilon*epsilon));
   Lambda_i[nSpecies+nDim-1] = 0.5*(ProjVelst_i + Vst_i[A_INDEX] +
@@ -208,7 +208,7 @@ CNumerics::ResidualType<> CUpwMSW_NEMO::ComputeResidual(const CConfig *config) {
   }
 
   /*--- Flow eigenvalues at j (Lambda-) ---*/
-  for (auto iVar = 0ul; iVar < nSpecies+nDim-1; iVar++)
+  for (auto iVar = 0; iVar < nSpecies+nDim-1; iVar++)
     Lambda_j[iVar]          = 0.5*(ProjVelst_j - sqrt(ProjVelst_j*ProjVelst_j +
                                                       epsilon*epsilon));
   Lambda_j[nSpecies+nDim-1] = 0.5*(ProjVelst_j + Vst_j[A_INDEX] -
diff --git a/SU2_CFD/src/numerics/NEMO/convection/roe.cpp b/SU2_CFD/src/numerics/NEMO/convection/roe.cpp
index dd200242d0b..518e1a87d1a 100644
--- a/SU2_CFD/src/numerics/NEMO/convection/roe.cpp
+++ b/SU2_CFD/src/numerics/NEMO/convection/roe.cpp
@@ -136,7 +136,7 @@ CNumerics::ResidualType<> CUpwRoe_NEMO::ComputeResidual(const CConfig *config) {
   for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
     Lambda[iSpecies] = ProjVelocity;
 
-  for (auto iDim = 0ul; iDim < nDim-1; iDim++)
+  for (auto iDim = 0; iDim < nDim-1; iDim++)
     Lambda[nSpecies+iDim] = ProjVelocity;
 
   Lambda[nSpecies+nDim-1] = ProjVelocity + RoeSoundSpeed;
@@ -147,7 +147,7 @@ CNumerics::ResidualType<> CUpwRoe_NEMO::ComputeResidual(const CConfig *config) {
   for (auto iSpecies = 0ul; iSpecies < nSpecies; iSpecies++)
     Epsilon[iSpecies] = 4.0*max(0.0, max(Lambda[iSpecies]-ProjVelocity_i,
                                          ProjVelocity_j-Lambda[iSpecies] ));
-  for (auto iDim = 0ul; iDim < nDim-1; iDim++)
+  for (auto iDim = 0; iDim < nDim-1; iDim++)
     Epsilon[nSpecies+iDim] = 4.0*max(0.0, max(Lambda[iDim]-ProjVelocity_i,
                                               ProjVelocity_j-Lambda[iDim] ));
   Epsilon[nSpecies+nDim-1] = 4.0*max(0.0, max(Lambda[nSpecies+nDim-1]-(ProjVelocity_i+V_i[A_INDEX]),
diff --git a/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp b/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
index fe00fdc4958..f02f064ff1d 100644
--- a/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
@@ -942,7 +942,7 @@ void CNEMOEulerSolver::ComputeUnderRelaxationFactor(const CConfig *config) {
     su2double num = 0.0;
     su2double denom = 0.0;
 
-    for (auto iVar = 0ul; iVar < nVar; iVar++) {
+    for (auto iVar = 0; iVar < nVar; iVar++) {
       /* We impose a limit on the maximum percentage that the
        density (sum of all species) and energy can change over a nonlinear iteration. */
 
@@ -2001,8 +2001,8 @@ void CNEMOEulerSolver::BC_Outlet(CGeometry *geometry, CSolver **solver_container
         //     V: [rho1, ..., rhoNs, T, Tve, u, v, w, P, rho, h, a, rhoCvtr, rhoCvve]^T
         Density    = pow(P_Exit/Entropy,1.0/Gamma);
         Pressure   = P_Exit;
-        const su2double SoundSpeed = sqrt(Gamma*P_Exit/Density);
-        Vn_Exit    = Riemann - 2.0*SoundSpeed/Gamma_Minus_One;
+        SoundSpeed = sqrt(Gamma*P_Exit/Density);
+        const su2double Vn_Exit    = Riemann - 2.0*SoundSpeed/Gamma_Minus_One;
         Velocity2  = 0.0;
         for (auto iDim = 0ul; iDim < nDim; iDim++) {
           Velocity[iDim] = Velocity[iDim] + (Vn_Exit-Vn)*UnitNormal[iDim];
diff --git a/SU2_CFD/src/solvers/CNEMONSSolver.cpp b/SU2_CFD/src/solvers/CNEMONSSolver.cpp
index 1101757271c..33e04b5f85f 100644
--- a/SU2_CFD/src/solvers/CNEMONSSolver.cpp
+++ b/SU2_CFD/src/solvers/CNEMONSSolver.cpp
@@ -349,8 +349,7 @@ void CNEMONSSolver::BC_HeatFluxCatalytic_Wall(CGeometry *geometry,
   SU2_MPI::Error("BC_HEATFLUX with catalytic wall: Not operational in NEMO.", CURRENT_FUNCTION);
   //TODO: SCALE WITH EDDY VISC
   /*--- Local variables ---*/
-  unsigned short iDim, iSpecies, iVar;
-  unsigned long iVertex, iPoint, total_index;
+  unsigned long iPoint, total_index;
   su2double rho, Ys;
   su2double *Normal, Area;
   su2double *Ds, *dYdn, SdYdn;

From 405db21acdcfee7063f9b2b0c98703f65bd49af4 Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Thu, 16 Feb 2023 08:46:37 -0500
Subject: [PATCH 205/656] Update regression files, attempt to fix security
 issue

---
 SU2_CFD/src/solvers/CNEMONSSolver.cpp | 2 +-
 TestCases/parallel_regression.py      | 6 +++---
 TestCases/serial_regression.py        | 4 ++--
 3 files changed, 6 insertions(+), 6 deletions(-)

diff --git a/SU2_CFD/src/solvers/CNEMONSSolver.cpp b/SU2_CFD/src/solvers/CNEMONSSolver.cpp
index 33e04b5f85f..063f1321c7b 100644
--- a/SU2_CFD/src/solvers/CNEMONSSolver.cpp
+++ b/SU2_CFD/src/solvers/CNEMONSSolver.cpp
@@ -492,7 +492,7 @@ void CNEMONSSolver::BC_HeatFluxCatalytic_Wall(CGeometry *geometry,
        Note that we need to add a contribution for moving walls to the Jacobian. ---*/
       if (implicit) {
         /*--- Enforce the no-slip boundary condition in a strong way ---*/
-        for (auto iVar = nSpecies; iVar < nSpecies+nDim; iVar++) {
+        for (unsigned short iVar = nSpecies; iVar < nSpecies+nDim; iVar++) {
           total_index = iPoint*nVar+iVar;
           Jacobian.DeleteValsRowi(total_index);
         }
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index e0fad895d88..5d5836cb164 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -145,8 +145,8 @@ def main():
     visc_cone.cfg_dir = "nonequilibrium/viscous"
     visc_cone.cfg_file = "axi_visccone.cfg"
     visc_cone.test_iter = 10
-    visc_cone.test_vals = [-5.222212, -5.746462, -20.569425, -20.633786, -20.547642, 1.255865, -3.208363, -0.016006, 0.093455, 32633.000000]
-    visc_cone.test_vals_aarch64 = [-5.222212, -5.746462, -20.569425, -20.633786, -20.547642, 1.255865, -3.208363, -0.016006, 0.093455, 32633.000000]
+    visc_cone.test_vals = [-5.222212, -5.746462, -20.559802, -20.510196, -20.439814, 1.255865, -3.208363, -0.016006, 0.093455, 32633.000000]
+    visc_cone.test_vals_aarch64 = [-5.222212, -5.746462, -20.559802, -20.510196, -20.439814, 1.255865, -3.208363, -0.016006, 0.093455, 32633.000000]
     visc_cone.new_output = True
     test_list.append(visc_cone)
 
@@ -164,7 +164,7 @@ def main():
     super_cat.cfg_dir = "nonequilibrium/viscous"
     super_cat.cfg_file = "super_cat.cfg"
     super_cat.test_iter = 10
-    super_cat.test_vals = [-5.232590, -5.757884, -20.727046, -20.748136, -20.564044, 1.246889, -3.205235, -0.028406, 0.250857, 3.2459e+04]
+    super_cat.test_vals = [-5.232590, -5.757884, -20.641547, -20.640244, -20.539243, 1.246889, -3.205235, -0.028406, 0.250857, 32459.000000]
     super_cat.su2_exec = "mpirun -n 2 SU2_CFD"
     super_cat.timeout = 1600
     super_cat.new_output = True
diff --git a/TestCases/serial_regression.py b/TestCases/serial_regression.py
index fdd27f140ae..a544062f1f1 100644
--- a/TestCases/serial_regression.py
+++ b/TestCases/serial_regression.py
@@ -73,8 +73,8 @@ def main():
     visc_cone.cfg_dir = "nonequilibrium/viscous"
     visc_cone.cfg_file = "axi_visccone.cfg"
     visc_cone.test_iter = 10
-    visc_cone.test_vals = [-5.215229, -5.739368, -20.545048, -20.618699, -20.502531, 1.262784, -3.205454, -0.015696, 0.093207, 32656.000000]
-    visc_cone.test_vals_aarch64 = [-5.215229, -5.739368, -20.545048, -20.618699, -20.502531, 1.262784, -3.205454, -0.015696, 0.093207, 32656.000000]
+    visc_cone.test_vals = [-5.215236, -5.739371, -20.556662, -20.517023, -20.436970, 1.262783, -3.205463, -0.015695, 0.093205, 32656.000000]
+    visc_cone.test_vals_aarch64 = [-5.215236, -5.739371, -20.556662, -20.517023, -20.436970, 1.262783, -3.205463, -0.015695, 0.093205, 32656.000000]
     visc_cone.new_output = True
     test_list.append(visc_cone)
 

From f14df78e41aba86383e703885ac41afe74f58a0b Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Thu, 16 Feb 2023 11:44:10 -0500
Subject: [PATCH 206/656] going back to auto

---
 SU2_CFD/src/solvers/CNEMONSSolver.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/SU2_CFD/src/solvers/CNEMONSSolver.cpp b/SU2_CFD/src/solvers/CNEMONSSolver.cpp
index 063f1321c7b..33e04b5f85f 100644
--- a/SU2_CFD/src/solvers/CNEMONSSolver.cpp
+++ b/SU2_CFD/src/solvers/CNEMONSSolver.cpp
@@ -492,7 +492,7 @@ void CNEMONSSolver::BC_HeatFluxCatalytic_Wall(CGeometry *geometry,
        Note that we need to add a contribution for moving walls to the Jacobian. ---*/
       if (implicit) {
         /*--- Enforce the no-slip boundary condition in a strong way ---*/
-        for (unsigned short iVar = nSpecies; iVar < nSpecies+nDim; iVar++) {
+        for (auto iVar = nSpecies; iVar < nSpecies+nDim; iVar++) {
           total_index = iPoint*nVar+iVar;
           Jacobian.DeleteValsRowi(total_index);
         }

From 981952d6079e76db571383fb2b0ee2164927071f Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Thu, 16 Feb 2023 12:59:44 -0500
Subject: [PATCH 207/656] address failing regressions

---
 .../visc_cylinder/visc_ion_wbe.cfg            | 75 -------------------
 TestCases/parallel_regression.py              | 32 +++-----
 2 files changed, 10 insertions(+), 97 deletions(-)
 delete mode 100644 TestCases/nonequilibrium/visc_cylinder/visc_ion_wbe.cfg

diff --git a/TestCases/nonequilibrium/visc_cylinder/visc_ion_wbe.cfg b/TestCases/nonequilibrium/visc_cylinder/visc_ion_wbe.cfg
deleted file mode 100644
index 16a1fabd44a..00000000000
--- a/TestCases/nonequilibrium/visc_cylinder/visc_ion_wbe.cfg
+++ /dev/null
@@ -1,75 +0,0 @@
-%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-%                                                                              %
-% SU2 configuration file                                                       %
-% Case description: Mach 15 viscous, ionized flow over a cylinder              %
-%                   using the Wilkes-Blottner-Eucken transport model.          %
-%                                                                              %
-%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
-% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
-%
-SOLVER= NEMO_NAVIER_STOKES
-MATH_PROBLEM= DIRECT
-RESTART_SOL= YES
-AXISYMMETRIC= YES
-
-% ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
-%
-MACH_NUMBER=15
-AOA= 0.0
-SIDESLIP_ANGLE= 0.0
-FREESTREAM_PRESSURE= 21.96
-FREESTREAM_TEMPERATURE= 246.87
-FREESTREAM_TEMPERATURE_VE= 246.87
-INIT_OPTION=TD_CONDITIONS
-
-% ---- NONEQUILIBRIUM GAS, IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
-%
-FLUID_MODEL= SU2_NONEQ
-GAS_MODEL= AIR-7
-GAS_COMPOSITION= (5E-13, 0.767, 0.23, 0.001, 0.001, 0.000999999999, 5E-13)
-TRANSPORT_COEFF_MODEL= WILKE
-
-% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
-%
-MARKER_ISOTHERMAL=(wall, 300.0)
-MARKER_FAR= (far, exit)
-MARKER_SYM= (symm)
-MARKER_PLOTTING= (wall)
-MARKER_MONITORING= (wall)
-
-% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
-%
-NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-CFL_NUMBER= 3.0
-ITER= 11
-LINEAR_SOLVER= BCGSTAB
-LINEAR_SOLVER_ERROR= 1E-6
-LINEAR_SOLVER_ITER= 5
-
-% -----------------------------------------------------------------------%
-%
-CONV_NUM_METHOD_FLOW= AUSM
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-VENKAT_LIMITER_COEFF= 0.05
-TIME_DISCRE_FLOW= EULER_IMPLICIT
-
-% --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-CONV_RESIDUAL_MINVAL= -10
-CONV_STARTITER= 10
-
-% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-%
-MESH_FILENAME= visc_cyl.su2
-MESH_FORMAT= SU2
-SOLUTION_FILENAME= restart_flow_wbe.dat 
-RESTART_FILENAME= restart_flow_wbe.dat 
-TABULAR_FORMAT= TECPLOT
-CONV_FILENAME= convergence
-VOLUME_FILENAME= soln_volume
-SURFACE_FILENAME= soln_surface     
-OUTPUT_WRT_FREQ= 2500
-SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY_0, RMS_DENSITY_1, RMS_DENSITY_2, RMS_DENSITY_3, RMS_DENSITY_4, RMS_DENSITY_5, RMS_DENSITY_6, RMS_ENERGY, RMS_ENERGY_VE, LIFT, DRAG, TOTAL_HEATFLUX)
-OUTPUT_FILES= (RESTART_ASCII, PARAVIEW_ASCII)
\ No newline at end of file
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 92bba2d4460..82dfcfe8f59 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -183,29 +183,17 @@ def main():
     partial_cat.tol = 0.00001
     test_list.append(partial_cat)
 
-    # Viscous cylinder, ionization, Wilkes-Blottner-Eucken
-    partial_ion_wbe = TestCase('ion_wbe')
-    partial_ion_wbe.cfg_dir = "nonequilibrium/visc_cylinder"
-    partial_ion_wbe.cfg_file = "cyl_ion_wbe.cfg"
-    partial_ion_wbe.test_iter = 10
-    partial_ion_wbe.test_vals = [-5.210300, -5.735063, -20.880374, -20.825890, -23.475263, 1.806281, -2.813924, -0.078469, 0.496017, 2.9021e+04]
-    partial_ion_wbe.su2_exec = "mpirun -n 2 SU2_CFD"
-    partial_ion_wbe.timeout = 1600
-    partial_ion_wbe.new_output = True
-    partial_ion_wbe.tol = 0.00001
-    test_list.append(partial_ion_wbe)
-
     # Viscous cylinder, ionization, Gupta-Yos
-    partial_ion_gy = TestCase('ion_gy')
-    partial_ion_gy.cfg_dir = "nonequilibrium/visc_cylinder"
-    partial_ion_gy.cfg_file = "cyl_ion_gy.cfg"
-    partial_ion_gy.test_iter = 10
-    partial_ion_gy.test_vals = [-5.210300, -5.735063, -20.880374, -20.825890, -23.475263, 1.806281, -2.813924, -0.078469, 0.496017, 2.9021e+04]
-    partial_ion_gy.su2_exec = "mpirun -n 2 SU2_CFD"
-    partial_ion_gy.timeout = 1600
-    partial_ion_gy.new_output = True
-    partial_ion_gy.tol = 0.00001
-    test_list.append(partial_ion_gy)
+    ion_gy = TestCase('ion_gy')
+    ion_gy.cfg_dir = "nonequilibrium/visc_cylinder"
+    ion_gy.cfg_file = "cyl_ion_gy.cfg"
+    ion_gy.test_iter = 10
+    ion_gy.test_vals = [-5.210300, -5.735063, -20.880374, -20.825890, -23.475263, 1.806281, -2.813924, -0.078469, 0.496017, 2.9021e+04]
+    ion_gy.su2_exec = "mpirun -n 2 SU2_CFD"
+    ion_gy.timeout = 1600
+    ion_gy.new_output = True
+    ion_gy.tol = 0.00001
+    test_list.append(ion_gy)
 
     ##########################
     ### Compressible Euler ###

From 1d85b5f03ed7035803b56b8793309af864972e04 Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Thu, 16 Feb 2023 13:54:30 -0500
Subject: [PATCH 208/656] renaming file

---
 .../visc_cylinder/{visc_ion_gy.cfg => cyl_ion_gy.cfg}             | 0
 1 file changed, 0 insertions(+), 0 deletions(-)
 rename TestCases/nonequilibrium/visc_cylinder/{visc_ion_gy.cfg => cyl_ion_gy.cfg} (100%)

diff --git a/TestCases/nonequilibrium/visc_cylinder/visc_ion_gy.cfg b/TestCases/nonequilibrium/visc_cylinder/cyl_ion_gy.cfg
similarity index 100%
rename from TestCases/nonequilibrium/visc_cylinder/visc_ion_gy.cfg
rename to TestCases/nonequilibrium/visc_cylinder/cyl_ion_gy.cfg

From 0663a34d04e2bc37ceda5ef4f40eaa53d9d4703c Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Fri, 17 Feb 2023 14:21:23 +0100
Subject: [PATCH 209/656] Update disc_adj_fsi parallel regression AD values.

---
 TestCases/disc_adj_fsi/dyn_fsi/grad_dv.opt.ref | 16 ++++++++--------
 TestCases/parallel_regression_AD.py            |  2 +-
 2 files changed, 9 insertions(+), 9 deletions(-)

diff --git a/TestCases/disc_adj_fsi/dyn_fsi/grad_dv.opt.ref b/TestCases/disc_adj_fsi/dyn_fsi/grad_dv.opt.ref
index 0bab88b33d0..e543b661a60 100644
--- a/TestCases/disc_adj_fsi/dyn_fsi/grad_dv.opt.ref
+++ b/TestCases/disc_adj_fsi/dyn_fsi/grad_dv.opt.ref
@@ -1,9 +1,9 @@
 INDEX	GRAD
-0	-3.461460630332286e-03
-1	-1.841786279602490e-03
-2	-7.915536035493717e-04
-3	-2.739622003666185e-04
-4	-2.734869244046031e-04
-5	-7.881162775931060e-04
-6	-1.828978353197476e-03
-7	-3.427219493292633e-03
+0	-3.461460667601001e-03
+1	-1.841786311588662e-03
+2	-7.915536257748965e-04
+3	-2.739622082729719e-04
+4	-2.734869133461108e-04
+5	-7.881162428890194e-04
+6	-1.828978290516676e-03
+7	-3.427219398258311e-03
diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index b65fc7657be..dd0bfb4cc74 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -276,7 +276,7 @@ def main():
     discadj_fsi2.cfg_dir   = "disc_adj_fsi/Airfoil_2d"
     discadj_fsi2.cfg_file  = "config.cfg"
     discadj_fsi2.test_iter = 8
-    discadj_fsi2.test_vals         = [-3.479484, 0.127482, -1.303589, 7.5407e-09, 2.3244]
+    discadj_fsi2.test_vals         = [-3.479502, 0.128475, -1.303589, 7.5407e-09, 2.3244]
     discadj_fsi2.test_vals_aarch64 = [-3.479505, 0.127953, -1.303589, 7.5407e-09, 2.3244]
     discadj_fsi2.tol       = 1e-16
     test_list.append(discadj_fsi2)

From a7f333a094e65468847cba109dc41d0785358ae1 Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Fri, 17 Feb 2023 10:23:13 -0500
Subject: [PATCH 210/656] more update to regressions

---
 Common/src/CConfig.cpp                                | 9 +++++++++
 TestCases/nonequilibrium/visc_cylinder/cyl_ion_gy.cfg | 2 +-
 TestCases/parallel_regression.py                      | 2 +-
 3 files changed, 11 insertions(+), 2 deletions(-)

diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index a3c092ecd29..4550e4fc7fc 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -3931,16 +3931,25 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
       SU2_MPI::Error("Only STANDARD_AIR fluid model can be used with US Measurement System", CURRENT_FUNCTION);
     }
 
+    /* --- Check for NEMO compatibility issues ---*/
     if (Kind_FluidModel == SU2_NONEQ && (Kind_TransCoeffModel != TRANSCOEFFMODEL::WILKE && Kind_TransCoeffModel != TRANSCOEFFMODEL::SUTHERLAND && Kind_TransCoeffModel != TRANSCOEFFMODEL::GUPTAYOS) ) {
       SU2_MPI::Error("Transport model not available for NEMO solver using SU2TCLIB. Please use the WILKE, SUTHERLAND or GUPTAYOS transport model instead.", CURRENT_FUNCTION);
     }
 
+    if (Kind_FluidModel == SU2_NONEQ && GasModel == "AIR-7" && Kind_TransCoeffModel != TRANSCOEFFMODEL::GUPTAYOS) {
+      SU2_MPI::Error("Only Gupta-Yos Transport model available for ionized flows using SU2TCLIB.", CURRENT_FUNCTION);
+    }
+
     if (Kind_FluidModel == MUTATIONPP &&
         (Kind_TransCoeffModel != TRANSCOEFFMODEL::WILKE && Kind_TransCoeffModel != TRANSCOEFFMODEL::CHAPMANN_ENSKOG)) {
       SU2_MPI::Error("Transport model not available for NEMO solver using MUTATIONPP. Please use the WILKE or CHAPMANN_ENSKOG transport model instead..",
                      CURRENT_FUNCTION);
     }
 
+    if (Kind_FluidModel == SU2_NONEQ && GasModel == "AIR-7" && nWall_Catalytic != 0) {
+      SU2_MPI::Error("Wall Catalyicity is not yet available for ionized flows in SU2_NEMO.", CURRENT_FUNCTION);
+    }
+
     if (!ideal_gas && !nemo) {
       if (Kind_Upwind_Flow != UPWIND::ROE && Kind_Upwind_Flow != UPWIND::HLLC && Kind_Centered_Flow != CENTERED::JST) {
         SU2_MPI::Error("Only ROE Upwind, HLLC Upwind scheme, and JST scheme can be used for Non-Ideal Compressible Fluids", CURRENT_FUNCTION);
diff --git a/TestCases/nonequilibrium/visc_cylinder/cyl_ion_gy.cfg b/TestCases/nonequilibrium/visc_cylinder/cyl_ion_gy.cfg
index 92ed1186935..80adfcc7941 100644
--- a/TestCases/nonequilibrium/visc_cylinder/cyl_ion_gy.cfg
+++ b/TestCases/nonequilibrium/visc_cylinder/cyl_ion_gy.cfg
@@ -71,4 +71,4 @@ CONV_FILENAME= convergence
 VOLUME_FILENAME= soln_volume
 SURFACE_FILENAME= soln_surface     
 OUTPUT_WRT_FREQ= 2500
-SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY_0, RMS_DENSITY_1, RMS_DENSITY_2, RMS_DENSITY_3, RMS_DENSITY_4, RMS_DENSITY_5, RMS_DENSITY_6, RMS_ENERGY, RMS_ENERGY_VE, LIFT, 
\ No newline at end of file
+SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY_0, RMS_DENSITY_1, RMS_DENSITY_2, RMS_DENSITY_3, RMS_DENSITY_4, RMS_DENSITY_5, RMS_DENSITY_6, RMS_ENERGY, RMS_ENERGY_VE, LIFT, DRAG, TOTAL_HEATFLUX
\ No newline at end of file
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 82dfcfe8f59..853893f2605 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -188,7 +188,7 @@ def main():
     ion_gy.cfg_dir = "nonequilibrium/visc_cylinder"
     ion_gy.cfg_file = "cyl_ion_gy.cfg"
     ion_gy.test_iter = 10
-    ion_gy.test_vals = [-5.210300, -5.735063, -20.880374, -20.825890, -23.475263, 1.806281, -2.813924, -0.078469, 0.496017, 2.9021e+04]
+    ion_gy.test_vals = [-5.210300, -5.735063, -20.880374, -20.825890, -23.475263, 1.806281, -2.813924, -0.078469, 0.496017, 2.9021e+04, 0.0, 0.0]
     ion_gy.su2_exec = "mpirun -n 2 SU2_CFD"
     ion_gy.timeout = 1600
     ion_gy.new_output = True

From 9116611eb9fa9ec6277e57c9eb823b7abdf79d4d Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Fri, 17 Feb 2023 16:36:53 +0100
Subject: [PATCH 211/656] Update disc_adj_fsi parallel regression AD values.

---
 TestCases/parallel_regression_AD.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index febf17b3876..2173b4ba3cf 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -276,7 +276,7 @@ def main():
     discadj_fsi2.cfg_dir   = "disc_adj_fsi/Airfoil_2d"
     discadj_fsi2.cfg_file  = "config.cfg"
     discadj_fsi2.test_iter = 8
-    discadj_fsi2.test_vals         = [-4.349355, 0.127482, -1.303589, 0.000000, 2.324400]
+    discadj_fsi2.test_vals         = [-4.349377, 0.128475, -1.303589, 7.5407e-09, 2.3244]
     discadj_fsi2.test_vals_aarch64 = [-3.479505, 0.127953, -1.303589, 7.5407e-09, 2.3244]
     discadj_fsi2.tol       = 0.00001
     test_list.append(discadj_fsi2)

From e3d581ad4410b3d7eb9e17cb73b1b3c81d166274 Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Fri, 17 Feb 2023 16:13:42 -0500
Subject: [PATCH 212/656] fix regressions, add errors, fix spelling mistakes

---
 Common/src/CConfig.cpp               |  4 +--
 SU2_CFD/src/fluid/CMutationTCLib.cpp | 41 ++++++++++++----------------
 SU2_CFD/src/fluid/CSU2TCLib.cpp      | 11 ++++++--
 TestCases/parallel_regression.py     |  2 +-
 4 files changed, 28 insertions(+), 30 deletions(-)

diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 4550e4fc7fc..4acdf6d2190 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -3937,7 +3937,7 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
     }
 
     if (Kind_FluidModel == SU2_NONEQ && GasModel == "AIR-7" && Kind_TransCoeffModel != TRANSCOEFFMODEL::GUPTAYOS) {
-      SU2_MPI::Error("Only Gupta-Yos Transport model available for ionized flows using SU2TCLIB.", CURRENT_FUNCTION);
+      SU2_MPI::Error("Only Gupta-Yos transport model available for ionized flows using SU2TCLIB.", CURRENT_FUNCTION);
     }
 
     if (Kind_FluidModel == MUTATIONPP &&
@@ -3947,7 +3947,7 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
     }
 
     if (Kind_FluidModel == SU2_NONEQ && GasModel == "AIR-7" && nWall_Catalytic != 0) {
-      SU2_MPI::Error("Wall Catalyicity is not yet available for ionized flows in SU2_NEMO.", CURRENT_FUNCTION);
+      SU2_MPI::Error("Catalytic wall recombination is not yet available for ionized flows in SU2_NEMO.", CURRENT_FUNCTION);
     }
 
     if (!ideal_gas && !nemo) {
diff --git a/SU2_CFD/src/fluid/CMutationTCLib.cpp b/SU2_CFD/src/fluid/CMutationTCLib.cpp
index e0ad74b04d1..59852b6a3e4 100644
--- a/SU2_CFD/src/fluid/CMutationTCLib.cpp
+++ b/SU2_CFD/src/fluid/CMutationTCLib.cpp
@@ -60,41 +60,34 @@ CMutationTCLib::CMutationTCLib(const CConfig* config, unsigned short val_nDim):
 
   for(iSpecies = 0; iSpecies < nSpecies; iSpecies++) MolarMass[iSpecies] = 1000* mix->speciesMw(iSpecies); // x1000 to have Molar Mass in kg/kmol
 
-  if (mix->hasElectrons()) {
-    if (config->GetViscous()) {
-      SU2_MPI::Error("Ionization is not yet operational for a viscous flow in the NEMO solver.", CURRENT_FUNCTION);
-    } else {
-      nHeavy = nSpecies-1;
-      nEl = 1;
-    }
-  }
-  else { nHeavy = nSpecies;   nEl = 0; }
+  if (mix->hasElectrons()) { nHeavy = nSpecies-1; nEl = 1; }
+  else { nHeavy = nSpecies; nEl = 0; }
 
   /*--- Set up catalytic recombination table. ---*/
   // Creation/Destruction (+1/-1), Index of monoatomic reactants
-  // Monoatomic species (N,O) recombine into diaatomic (N2, O2)
+  // Monoatomic species (N,O) recombine into diaatomic (N2, O2) species
   if (gas_model == "N2") {
-    CatRecombTable(0,0) =  1; CatRecombTable(0,1) = 1;
-    CatRecombTable(1,0) = -1; CatRecombTable(1,1) = 1;
+    CatRecombTable(0,0) =  1; CatRecombTable(0,1) = 1; // N2
+    CatRecombTable(1,0) = -1; CatRecombTable(1,1) = 1; // N
 
   } else if (gas_model == "air_5"){
-    CatRecombTable(0,0) = -1; CatRecombTable(0,1) = 0;
-    CatRecombTable(1,0) = -1; CatRecombTable(1,1) = 1;
-    CatRecombTable(2,0) =  0; CatRecombTable(2,1) = 4;
-    CatRecombTable(3,0) =  1; CatRecombTable(3,1) = 0;
-    CatRecombTable(4,0) =  1; CatRecombTable(4,1) = 1;
+    CatRecombTable(0,0) = -1; CatRecombTable(0,1) = 0; // N
+    CatRecombTable(1,0) = -1; CatRecombTable(1,1) = 1; // O
+    CatRecombTable(2,0) =  0; CatRecombTable(2,1) = 4; // NO
+    CatRecombTable(3,0) =  1; CatRecombTable(3,1) = 0; // N2
+    CatRecombTable(4,0) =  1; CatRecombTable(4,1) = 1; // O2
 
   } else if (gas_model == "air_6") {
-    CatRecombTable(0,0) = -1; CatRecombTable(0,1) = 0;
-    CatRecombTable(1,0) = -1; CatRecombTable(1,1) = 1;
-    CatRecombTable(2,0) =  0; CatRecombTable(2,1) = 4;
-    CatRecombTable(3,0) =  1; CatRecombTable(3,1) = 0;
-    CatRecombTable(4,0) =  1; CatRecombTable(4,1) = 1;
-    CatRecombTable(5,0) =  0; CatRecombTable(5,1) = 4;
+    CatRecombTable(0,0) = -1; CatRecombTable(0,1) = 0; // N
+    CatRecombTable(1,0) = -1; CatRecombTable(1,1) = 1; // O
+    CatRecombTable(2,0) =  0; CatRecombTable(2,1) = 4; // NO
+    CatRecombTable(3,0) =  1; CatRecombTable(3,1) = 0; // N2
+    CatRecombTable(4,0) =  1; CatRecombTable(4,1) = 1; // O2
+    CatRecombTable(5,0) =  0; CatRecombTable(5,1) = 4; // Ar
 
   } else {
     if (config->GetCatalytic())
-      SU2_MPI::Error("Cataylic wall recombination not implemented for specified Mutation gas model.", CURRENT_FUNCTION);
+      SU2_MPI::Error("Catalytic wall recombination not implemented for specified Mutation gas model.", CURRENT_FUNCTION);
   }
 
 }
diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 203189af8ec..c76c1deb069 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -111,7 +111,7 @@ CSU2TCLib::CSU2TCLib(const CConfig* config, unsigned short val_nDim, bool viscou
     ElDegeneracy(0,5) = 5;
     ElDegeneracy(0,6) = 15;
 
-    /*--- Catayltic wall table---*/
+    /*--- Catalytic wall table ---*/
     // Creation/Destruction (+1/-1), Index of monoatomic reactants.
     // Argon not used.
     CatRecombTable(0,0) = 0; CatRecombTable(0,1) = 0;
@@ -272,7 +272,7 @@ CSU2TCLib::CSU2TCLib(const CConfig* config, unsigned short val_nDim, bool viscou
     Omega22(1,0,0) = -8.3493693E-03;  Omega22(1,0,1) = 1.7808911E-01;   Omega22(1,0,2) = -1.4466155E+00;  Omega22(1,0,3) = 1.9324210E+03;
     Omega22(1,1,0) = -7.7439615E-03;  Omega22(1,1,1) = 1.7129007E-01;   Omega22(1,1,2) = -1.4809088E+00;  Omega22(1,1,3) = 2.1284951E+03;
 
-    /*--- Catayltic wall table---*/
+    /*--- Catalytic wall table ---*/
     // Creation/Destruction (+1/-1), Index of monoatomic reactants.
     // Monoatomic species (N,O) recombine into diaatomic (N2, O2)
     CatRecombTable(0,0) =  1; CatRecombTable(0,1) = 1;
@@ -1887,7 +1887,7 @@ su2double CSU2TCLib::ComputeCollisionCrossSection(unsigned iSpecies, unsigned jS
   const su2double Na = AVOGAD_CONSTANT;
   
   if (coulomb) {
-    
+
     const su2double e_cgs = FUND_ELEC_CHARGE_CGS; // CGS unit of fundamental electric charge 
     const su2double kb_cgs = BOLTZMANN_CONSTANT * 1E7; // CGS unit of Boltzmann Constant 
     const su2double ne_cgs = Na * rhos[0] / MolarMass[0] * 1E-6; // CGS unit of electron number density
@@ -1895,6 +1895,11 @@ su2double CSU2TCLib::ComputeCollisionCrossSection(unsigned iSpecies, unsigned jS
     const su2double debyeLength = sqrt(kb_cgs * T / 4 / pi / ne_cgs / pow(e_cgs,2));
     const su2double T_star = debyeLength / (pow(e_cgs,2) / (kb_cgs * T));
 
+    /*--- Compute the collisionion cross section ---*/
+    // Note: Omega11 is used for diffusion, viscosity, translational, internal, and reaction components of
+    //       thermal conductivity
+    //       Omega22 is used used for viscosity and translational component of thermal conductivity
+
     if (Omega11(iSpecies, jSpecies, 0) == 1.0 && d1) {
       return 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);
     } else if (Omega11(iSpecies, jSpecies, 0) == -1.0 && d1) {
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 853893f2605..231697f90fb 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -188,7 +188,7 @@ def main():
     ion_gy.cfg_dir = "nonequilibrium/visc_cylinder"
     ion_gy.cfg_file = "cyl_ion_gy.cfg"
     ion_gy.test_iter = 10
-    ion_gy.test_vals = [-5.210300, -5.735063, -20.880374, -20.825890, -23.475263, 1.806281, -2.813924, -0.078469, 0.496017, 2.9021e+04, 0.0, 0.0]
+    ion_gy.test_vals = [-11.629871, -4.156742, -4.692113, -4.949447, -5.146196, -4.991664, -6.893329, 5.990109, 5.990004, -0.014849, 0.000000, 90090.000000]
     ion_gy.su2_exec = "mpirun -n 2 SU2_CFD"
     ion_gy.timeout = 1600
     ion_gy.new_output = True

From ea11f823973610455d211ee72df2015663fcef1e Mon Sep 17 00:00:00 2001
From: Wally Maier <wallytmaier@gmail.com>
Date: Fri, 17 Feb 2023 16:33:59 -0500
Subject: [PATCH 213/656] Update SU2_CFD/src/fluid/CSU2TCLib.cpp

---
 SU2_CFD/src/fluid/CSU2TCLib.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index c76c1deb069..52c5ba1bda5 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1898,7 +1898,7 @@ su2double CSU2TCLib::ComputeCollisionCrossSection(unsigned iSpecies, unsigned jS
     /*--- Compute the collisionion cross section ---*/
     // Note: Omega11 is used for diffusion, viscosity, translational, internal, and reaction components of
     //       thermal conductivity
-    //       Omega22 is used used for viscosity and translational component of thermal conductivity
+    //       Omega22 is used for viscosity and translational components of thermal conductivity
 
     if (Omega11(iSpecies, jSpecies, 0) == 1.0 && d1) {
       return 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);

From 9ce7cecaf4217ff58061ee39d605d8a147f79eef Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 18 Feb 2023 18:54:35 -0800
Subject: [PATCH 214/656] do not assume that deformable markers can be straight

---
 Common/include/CConfig.hpp        | 26 ++++++++++++++------
 Common/src/CConfig.cpp            | 40 ++++++++++++-------------------
 Common/src/geometry/CGeometry.cpp |  3 ++-
 3 files changed, 36 insertions(+), 33 deletions(-)

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index f3b1abd9876..ba5190f4b24 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -6559,26 +6559,38 @@ class CConfig {
    * \brief Get the internal index for a moving boundary <i>val_marker</i>.
    * \return Internal index for a moving boundary <i>val_marker</i>.
    */
-  unsigned short GetMarker_Moving(string val_marker) const;
+  unsigned short GetMarker_Moving(const string& val_marker) const;
 
   /*!
-   * \brief Get bool if marker is moving. <i>val_marker</i>.
-   * \param[in] val_marker - String of the marker to test.
-   * \return Bool if the marker is a moving boundary <i>val_marker</i>.
+   * \brief Get a bool for whether a marker is moving. <i>val_marker</i>.
+   * \param[in] val_marker - Name of the marker to test.
+   * \return True if the marker is a moving boundary <i>val_marker</i>.
    */
-  bool GetMarker_Moving_Bool(string val_marker) const;
+  inline bool GetMarker_Moving_Bool(const string& val_marker) const {
+    return GetMarker_Moving(val_marker) < nMarker_Moving;
+  }
 
   /*!
    * \brief Get the internal index for a DEFORM_MESH boundary <i>val_marker</i>.
    * \return Internal index for a DEFORM_MESH boundary <i>val_marker</i>.
    */
-  unsigned short GetMarker_Deform_Mesh(string val_marker) const;
+  unsigned short GetMarker_Deform_Mesh(const string& val_marker) const;
 
   /*!
    * \brief Get the internal index for a DEFORM_MESH_SYM_PLANE boundary <i>val_marker</i>.
    * \return Internal index for a DEFORM_MESH_SYM_PLANE boundary <i>val_marker</i>.
    */
-  unsigned short GetMarker_Deform_Mesh_Sym_Plane(string val_marker) const;
+  unsigned short GetMarker_Deform_Mesh_Sym_Plane(const string& val_marker) const;
+
+  /*!
+   * \brief Get a bool for whether the marker is deformed. <i>val_marker</i>.
+   * \param[in] val_marker - Name of the marker to test.
+   * \return True if the marker is a deforming boundary <i>val_marker</i>.
+   */
+  inline bool GetMarker_Deform_Mesh_Bool(const string& val_marker) const {
+    return GetMarker_Deform_Mesh(val_marker) < nMarker_Deform_Mesh ||
+        GetMarker_Deform_Mesh_Sym_Plane(val_marker) < nMarker_Deform_Mesh_Sym_Plane;
+  }
 
   /*!
    * \brief Get the internal index for a Fluid_Load boundary <i>val_marker</i>.
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index f0c0d8ea91a..7f51bf5d393 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -8676,44 +8676,34 @@ bool CConfig::GetSurface_Movement(unsigned short kind_movement) const {
   return false;
 }
 
-unsigned short CConfig::GetMarker_Moving(string val_marker) const {
-  unsigned short iMarker_Moving;
+unsigned short CConfig::GetMarker_Moving(const string& val_marker) const {
+  unsigned short iMarker;
 
   /*--- Find the marker for this moving boundary. ---*/
-  for (iMarker_Moving = 0; iMarker_Moving < nMarker_Moving; iMarker_Moving++)
-    if (Marker_Moving[iMarker_Moving] == val_marker) break;
+  for (iMarker = 0; iMarker < nMarker_Moving; iMarker++)
+    if (Marker_Moving[iMarker] == val_marker) break;
 
-  return iMarker_Moving;
+  return iMarker;
 }
 
-bool CConfig::GetMarker_Moving_Bool(string val_marker) const {
-  unsigned short iMarker_Moving;
-
-  /*--- Find the marker for this moving boundary, if it exists. ---*/
-  for (iMarker_Moving = 0; iMarker_Moving < nMarker_Moving; iMarker_Moving++)
-    if (Marker_Moving[iMarker_Moving] == val_marker) return true;
-
-  return false;
-}
-
-unsigned short CConfig::GetMarker_Deform_Mesh(string val_marker) const {
-  unsigned short iMarker_Deform_Mesh;
+unsigned short CConfig::GetMarker_Deform_Mesh(const string& val_marker) const {
+  unsigned short iMarker;
 
   /*--- Find the marker for this interface boundary. ---*/
-  for (iMarker_Deform_Mesh = 0; iMarker_Deform_Mesh < nMarker_Deform_Mesh; iMarker_Deform_Mesh++)
-    if (Marker_Deform_Mesh[iMarker_Deform_Mesh] == val_marker) break;
+  for (iMarker = 0; iMarker < nMarker_Deform_Mesh; iMarker++)
+    if (Marker_Deform_Mesh[iMarker] == val_marker) break;
 
-  return iMarker_Deform_Mesh;
+  return iMarker;
 }
 
-unsigned short CConfig::GetMarker_Deform_Mesh_Sym_Plane(string val_marker) const {
-  unsigned short iMarker_Deform_Mesh_Sym_Plane;
+unsigned short CConfig::GetMarker_Deform_Mesh_Sym_Plane(const string& val_marker) const {
+  unsigned short iMarker;
 
   /*--- Find the marker for this interface boundary. ---*/
-  for (iMarker_Deform_Mesh_Sym_Plane = 0; iMarker_Deform_Mesh_Sym_Plane < nMarker_Deform_Mesh_Sym_Plane; iMarker_Deform_Mesh_Sym_Plane++)
-    if (Marker_Deform_Mesh_Sym_Plane[iMarker_Deform_Mesh_Sym_Plane] == val_marker) break;
+  for (iMarker = 0; iMarker < nMarker_Deform_Mesh_Sym_Plane; iMarker++)
+    if (Marker_Deform_Mesh_Sym_Plane[iMarker] == val_marker) break;
 
-  return iMarker_Deform_Mesh_Sym_Plane;
+  return iMarker;
 }
 
 unsigned short CConfig::GetMarker_Fluid_Load(string val_marker) const {
diff --git a/Common/src/geometry/CGeometry.cpp b/Common/src/geometry/CGeometry.cpp
index bc1e91b1682..ad15762ce5e 100644
--- a/Common/src/geometry/CGeometry.cpp
+++ b/Common/src/geometry/CGeometry.cpp
@@ -2592,7 +2592,8 @@ void CGeometry::ComputeSurf_Straightness(CConfig *config,
           other GridMovements are rigid. ---*/
     if ((config->GetMarker_All_KindBC(iMarker) == SYMMETRY_PLANE ||
          config->GetMarker_All_KindBC(iMarker) == EULER_WALL) &&
-         !config->GetMarker_Moving_Bool(Local_TagBound)) {
+         !config->GetMarker_Moving_Bool(Local_TagBound) &&
+         !config->GetMarker_Deform_Mesh_Bool(Local_TagBound)) {
 
       /*--- Loop over all global markers, and find the local-global pair via
             matching unique string tags. ---*/

From a96176f73fe6b1d14f405edcda5f4195ddea4d93 Mon Sep 17 00:00:00 2001
From: danielmayer <daniel.mayer4@us.bosch.com>
Date: Sun, 19 Feb 2023 01:21:40 -0800
Subject: [PATCH 215/656] Align Paraview multiblock output filename with other
 volume output filenames. (#1930)

---
 SU2_CFD/src/output/COutput.cpp | 5 ++---
 1 file changed, 2 insertions(+), 3 deletions(-)

diff --git a/SU2_CFD/src/output/COutput.cpp b/SU2_CFD/src/output/COutput.cpp
index 9423831de01..aa743aa0610 100644
--- a/SU2_CFD/src/output/COutput.cpp
+++ b/SU2_CFD/src/output/COutput.cpp
@@ -557,9 +557,8 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
 
         extension = CParaviewVTMFileWriter::fileExt;
 
-        /*--- The file name of the multiblock file is the case name (i.e. the config file name w/o ext.) ---*/
-
-        fileName = config->GetUnsteady_FileName(config->GetCaseName(), curTimeIter, "");
+        if (fileName.empty())
+          fileName = config->GetUnsteady_FileName(volumeFilename, curTimeIter, "");
 
         if (!config->GetWrt_Volume_Overwrite())
           filename_iter = config->GetFilename_Iter(fileName,curInnerIter, curOuterIter);

From a36e84efc82a62178a6805886f5dd0e75d0ab07a Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Mon, 20 Feb 2023 16:06:28 -0500
Subject: [PATCH 216/656] add protection for zero electron massfraction for GY

---
 Common/src/CConfig.cpp               |  6 ++--
 SU2_CFD/src/fluid/CMutationTCLib.cpp |  4 ++-
 SU2_CFD/src/fluid/CSU2TCLib.cpp      | 45 +++++++++++++++++-----------
 TestCases/parallel_regression.py     |  2 +-
 4 files changed, 35 insertions(+), 22 deletions(-)

diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 4acdf6d2190..1a14cb34f4a 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -3936,8 +3936,10 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
       SU2_MPI::Error("Transport model not available for NEMO solver using SU2TCLIB. Please use the WILKE, SUTHERLAND or GUPTAYOS transport model instead.", CURRENT_FUNCTION);
     }
 
-    if (Kind_FluidModel == SU2_NONEQ && GasModel == "AIR-7" && Kind_TransCoeffModel != TRANSCOEFFMODEL::GUPTAYOS) {
-      SU2_MPI::Error("Only Gupta-Yos transport model available for ionized flows using SU2TCLIB.", CURRENT_FUNCTION);
+    if (Kind_Solver == NEMO_NAVIER_STOKES) {
+      if (Kind_FluidModel == SU2_NONEQ && GasModel == "AIR-7" && Kind_TransCoeffModel != TRANSCOEFFMODEL::GUPTAYOS) {
+        SU2_MPI::Error("Only Gupta-Yos transport model available for ionized flows using SU2TCLIB.", CURRENT_FUNCTION);
+      }
     }
 
     if (Kind_FluidModel == MUTATIONPP &&
diff --git a/SU2_CFD/src/fluid/CMutationTCLib.cpp b/SU2_CFD/src/fluid/CMutationTCLib.cpp
index 59852b6a3e4..f23aac2b4eb 100644
--- a/SU2_CFD/src/fluid/CMutationTCLib.cpp
+++ b/SU2_CFD/src/fluid/CMutationTCLib.cpp
@@ -58,7 +58,9 @@ CMutationTCLib::CMutationTCLib(const CConfig* config, unsigned short val_nDim):
   /* Initialize mixture object */
   mix.reset(new Mutation::Mixture(opt));
 
-  for(iSpecies = 0; iSpecies < nSpecies; iSpecies++) MolarMass[iSpecies] = 1000* mix->speciesMw(iSpecies); // x1000 to have Molar Mass in kg/kmol
+  // x1000 to have Molar Mass in kg/kmol
+  for(iSpecies = 0; iSpecies < nSpecies; iSpecies++)
+    MolarMass[iSpecies] = 1000* mix->speciesMw(iSpecies);
 
   if (mix->hasElectrons()) { nHeavy = nSpecies-1; nEl = 1; }
   else { nHeavy = nSpecies; nEl = 0; }
diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 52c5ba1bda5..0e7c48dae27 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1952,21 +1952,23 @@ void CSU2TCLib::DiffusionCoeffGY(){
     DiffusionCoeff[iSpecies] = 0.0;
 
     /*--- Calculate molar concentration ---*/
-    const su2double Mi    = MolarMass[iSpecies];
+    const su2double Mi    = (MolarMass[iSpecies] + EPS);
     const su2double gam_i = rhos[iSpecies] / (Density*Mi);
     su2double denom = 0.0;
 
     for (jSpecies = 0; jSpecies < nSpecies; jSpecies++) {
       if (jSpecies != iSpecies) { 
 
-        const su2double Mj    = MolarMass[jSpecies];
+        const su2double Mj    = (MolarMass[jSpecies] + EPS);
         const su2double gam_j = rhos[jSpecies] / (Density*Mj);
 
         const su2double kb = BOLTZMANN_CONSTANT;
 
         const su2double T_col = (iSpecies == 0 && ionization) ? Tve : T; 
 
-        const su2double d1_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T_col, true);
+        su2double d1_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T_col, true);
+        if (d1_ij > 1E16) d1_ij = 1E16;
+
         const su2double D_ij = kb*T_col/(Pressure*d1_ij);
         denom += gam_j/D_ij;
       }
@@ -1987,16 +1989,18 @@ void CSU2TCLib::ViscosityGY(){
     su2double denom = 0.0;
 
     /*--- Calculate molar concentration ---*/
-    const su2double Mi    = MolarMass[iSpecies];
+    const su2double Mi    = (MolarMass[iSpecies] + EPS);
     const su2double gam_i = rhos[iSpecies] / (Density*Mi);
 
     for (jSpecies = 0; jSpecies < nSpecies; jSpecies++) {
-      const su2double Mj    = MolarMass[jSpecies];
+      const su2double Mj    = (MolarMass[jSpecies] + EPS);
       const su2double gam_j = rhos[jSpecies] / (Density*Mj);
 
       const su2double T_col = (iSpecies == 0 && ionization) ? Tve : T; 
 
-      const su2double d2_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T_col, false);
+      su2double d2_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T_col, false);
+      if (d2_ij > 1E16) d2_ij = 1E16;
+
       denom += gam_j*d2_ij;
     }
     /*--- Calculate species laminar viscosity ---*/
@@ -2028,33 +2032,38 @@ void CSU2TCLib::ThermalConductivitiesGY(){
   for (iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
 
     /*--- Calculate molar concentration ---*/
-    const su2double Mi      = MolarMass[iSpecies];
-    const su2double mi      = Mi/Na;
-    const su2double gam_i   = rhos[iSpecies] / (Density*Mi);
+    const su2double Mi    = (MolarMass[iSpecies] + EPS);
+    const su2double mi    = Mi/Na;
+    const su2double gam_i = rhos[iSpecies] / (Density*Mi);
     su2double denom_t = 0.0;
     su2double denom_r = 0.0;
     su2double denom_re = 0.0;
 
     for (jSpecies = 0; jSpecies < nSpecies; jSpecies++) {
-      const su2double Mj    = MolarMass[jSpecies];
+      const su2double Mj    = (MolarMass[jSpecies] + EPS);
       const su2double mj    = Mj/Na;
       const su2double gam_j = rhos[iSpecies] / (Density*Mj);
       const su2double a_ij = 1.0 + (1.0 - mi/mj)*(0.45 - 2.54*mi/mj) / ((1.0 + mi/mj)*(1.0 + mi/mj));
 
       const su2double T_col = ((iSpecies == 0 && ionization) || (jSpecies == 0 && ionization)) ? Tve : T; 
 
-      const su2double d1_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T_col, true);
-      const su2double d2_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T_col, false);
-      
-      if (jSpecies == 0 && ionization) {
-        denom_t += 3.54*gam_j*d2_ij;
-      } else {
-        denom_t += a_ij*gam_j*d2_ij;
-      }
+      su2double d1_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T_col, true);
+      su2double d2_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T_col, false);
+      if (d1_ij >1E16) d1_ij = 1E16;
+      if (d2_ij >1E16) d2_ij = 1E16;      
+
+      if (jSpecies == 0 && ionization) { denom_t += 3.54*gam_j*d2_ij; }
+      else { denom_t += a_ij*gam_j*d2_ij; }
+
       denom_r += gam_j*d1_ij;
       denom_re += gam_j*d2_ij;
     }
 
+    /*--- Prevent divide by 0 ---*/
+    if (denom_t == 0.0) denom_t = EPS;
+    if (denom_r == 0.0) denom_r = EPS;
+    if (denom_re == 0.0) denom_re = EPS;
+
     /*--- Translational contribution to thermal conductivity ---*/
     if (!(ionization && iSpecies == 0)) ThermalCond_tr += ((15.0/4.0)*kb*gam_i/denom_t);
 
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 548d27b38a4..4fc887ea2e2 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -188,7 +188,7 @@ def main():
     ion_gy.cfg_dir = "nonequilibrium/visc_cylinder"
     ion_gy.cfg_file = "cyl_ion_gy.cfg"
     ion_gy.test_iter = 10
-    ion_gy.test_vals = [-11.629871, -4.156742, -4.692113, -4.949447, -5.146196, -4.991664, -6.893329, 5.990109, 5.990004, -0.014849, 0.000000, 90090.000000]
+    ion_gy.test_vals = [-11.629873, -4.165563, -4.702662, -4.950351, -5.146155, -4.993878, -6.893332, 5.990109, 5.990004, -0.014849, 0.000000, 90090.000000]
     ion_gy.su2_exec = "mpirun -n 2 SU2_CFD"
     ion_gy.timeout = 1600
     ion_gy.new_output = True

From dfb8a4ef311beada32a39d9726efd2cd7b0edccf Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Mon, 20 Feb 2023 16:13:53 -0500
Subject: [PATCH 217/656] oops

---
 Common/src/CConfig.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 1a14cb34f4a..26fc77bfd54 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -3936,7 +3936,7 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
       SU2_MPI::Error("Transport model not available for NEMO solver using SU2TCLIB. Please use the WILKE, SUTHERLAND or GUPTAYOS transport model instead.", CURRENT_FUNCTION);
     }
 
-    if (Kind_Solver == NEMO_NAVIER_STOKES) {
+    if (Kind_Solver == MAIN_SOLVER::NEMO_NAVIER_STOKES) {
       if (Kind_FluidModel == SU2_NONEQ && GasModel == "AIR-7" && Kind_TransCoeffModel != TRANSCOEFFMODEL::GUPTAYOS) {
         SU2_MPI::Error("Only Gupta-Yos transport model available for ionized flows using SU2TCLIB.", CURRENT_FUNCTION);
       }

From 1580c1722551e1115890d4e7bbc0844db44238a9 Mon Sep 17 00:00:00 2001
From: Jacob Needels <44848904+jtneedels@users.noreply.github.com>
Date: Mon, 20 Feb 2023 14:20:29 -0800
Subject: [PATCH 218/656] Add comment about Coulomb potential source

---
 SU2_CFD/include/fluid/CSU2TCLib.hpp | 4 +++-
 1 file changed, 3 insertions(+), 1 deletion(-)

diff --git a/SU2_CFD/include/fluid/CSU2TCLib.hpp b/SU2_CFD/include/fluid/CSU2TCLib.hpp
index 649b05d4e1f..7412e6086e9 100644
--- a/SU2_CFD/include/fluid/CSU2TCLib.hpp
+++ b/SU2_CFD/include/fluid/CSU2TCLib.hpp
@@ -70,7 +70,9 @@ class CSU2TCLib : public CNEMOGas {
   std::array<su2double,1> Sk_ref; /*!< \brief Vector containing Sutherland's constant for thermal conductivities */
 
   const su2double T_ref_suth = 273.15; /*!<\brief Reference temperature for Sutherland's model [K] */
-
+  
+  // Coulomb potential constant values source: Scalabrin, NUMERICAL SIMULATION OF WEAKLY IONIZED HYPERSONIC
+  // FLOW OVER REENTRY CAPSULES, 2007.
   /*--- Attractive Coulombic potential constants ---*/
   const su2double D1_a = 0.784;
   const su2double C1_a = -0.476;

From 6d5618c88aa4ab93efa5cf8a644618eda482ca16 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Mon, 20 Feb 2023 15:05:06 -0800
Subject: [PATCH 219/656] add testcase

---
 TestCases/parallel_regression.py              |  10 ++
 .../deforming_bump_in_channel/config.cfg      |  72 ++++++++++++
 .../deforming_bump_in_channel/run.py          | 108 ++++++++++++++++++
 3 files changed, 190 insertions(+)
 create mode 100644 TestCases/py_wrapper/deforming_bump_in_channel/config.cfg
 create mode 100755 TestCases/py_wrapper/deforming_bump_in_channel/run.py

diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index e0fad895d88..d310f281076 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -1337,6 +1337,16 @@ def main():
     pywrapper_rigidMotion.unsteady      = True
     test_list.append(pywrapper_rigidMotion)
 
+    # Deforming Bump in Channel
+    pywrapper_deformingBump = TestCase('pywrapper deforming bump in channel')
+    pywrapper_deformingBump.cfg_dir = "py_wrapper/deforming_bump_in_channel"
+    pywrapper_deformingBump.cfg_file = "config.cfg"
+    pywrapper_deformingBump.test_iter = 2
+    pywrapper_deformingBump.test_vals = [0.5, 0, -2.55436, -1.084594, -0.024882, 2.907803, 8.785498, -0.363585]
+    pywrapper_deformingBump.command = TestCase.Command("mpirun -np 2", "python", "run.py")
+    pywrapper_deformingBump.unsteady = True
+    test_list.append(pywrapper_deformingBump)
+
     ##############################################
     ### Method of Manufactured Solutions (MMS) ###
     ##############################################
diff --git a/TestCases/py_wrapper/deforming_bump_in_channel/config.cfg b/TestCases/py_wrapper/deforming_bump_in_channel/config.cfg
new file mode 100644
index 00000000000..fcbb9a27710
--- /dev/null
+++ b/TestCases/py_wrapper/deforming_bump_in_channel/config.cfg
@@ -0,0 +1,72 @@
+% ------------------------------- SOLVER -------------------------------- %
+%
+SOLVER= EULER
+%
+% ----------------------------- FREESTREAM ------------------------------ %
+%
+MACH_NUMBER= 0.02
+AOA= 0.0
+FREESTREAM_OPTION= TEMPERATURE_FS
+FREESTREAM_PRESSURE= 101325.0
+FREESTREAM_TEMPERATURE= 288.15
+%
+% ------------------------- UNSTEADY SIMULATION ------------------------- %
+%
+TIME_DOMAIN= YES
+TIME_MARCHING= DUAL_TIME_STEPPING-1ST_ORDER
+% The time step is ~50x too large to obtain a quasi-steady solution for
+% testing.
+TIME_STEP= 0.5
+MAX_TIME= 5.0
+INNER_ITER= 500
+TIME_ITER= 2
+%
+% ------------------------- BOUNDARY CONDITIONS ------------------------- %
+%
+MARKER_EULER= ( top, slip_bottom, bottom_front, interface, bottom_rear )
+MARKER_INLET= ( inlet, 288.6, 101400.0, 1.0, 0.0, 0.0 )
+MARKER_OUTLET= ( outlet, 101100.0 )
+MARKER_PLOTTING= ( interface )
+MARKER_MONITORING= ( interface )
+%
+% -------------------------- MESH DEFORMATION --------------------------- %
+%
+DEFORM_MESH= YES
+MARKER_DEFORM_MESH = ( interface )
+DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
+DEFORM_LINEAR_SOLVER= CONJUGATE_GRADIENT
+DEFORM_LINEAR_SOLVER_PREC= ILU
+DEFORM_LINEAR_SOLVER_ITER= 200
+DEFORM_LINEAR_SOLVER_ERROR= 1e-9
+% DEFORM_CONSOLE_OUTPUT= YES
+%
+% ----------------------- SPATIAL DISCRETIZATION ------------------------ %
+%
+NUM_METHOD_GRAD= GREEN_GAUSS
+CONV_NUM_METHOD_FLOW= ROE
+MUSCL_FLOW= YES
+SLOPE_LIMITER_FLOW= NONE
+%
+% ---------- PSEUDOTIME INTEGRATION / CONVERGENCE ACCELERATION ---------- %
+%
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+CFL_NUMBER= 500
+MGLEVEL= 0
+LINEAR_SOLVER= FGMRES
+LINEAR_SOLVER_PREC= ILU
+LINEAR_SOLVER_ERROR= 0.1
+LINEAR_SOLVER_ITER= 10
+%
+% ------------------------ CONVERGENCE CRITERIA ------------------------- %
+%
+CONV_FIELD= RMS_DENSITY
+CONV_RESIDUAL_MINVAL= -8
+%
+% --------------------------- INPUT / OUTPUT ---------------------------- %
+%
+RESTART_SOL= NO
+SCREEN_OUTPUT= ( TIME_ITER, CUR_TIME, INNER_ITER, RMS_RES, LIFT, DRAG )
+MESH_FILENAME= mesh.su2
+MESH_FORMAT= SU2
+OUTPUT_WRT_FREQ= (5)
+
diff --git a/TestCases/py_wrapper/deforming_bump_in_channel/run.py b/TestCases/py_wrapper/deforming_bump_in_channel/run.py
new file mode 100755
index 00000000000..dc9a217f35e
--- /dev/null
+++ b/TestCases/py_wrapper/deforming_bump_in_channel/run.py
@@ -0,0 +1,108 @@
+#!/usr/bin/env python
+
+## \file run.py
+#  \brief Deforming bump in channel.
+#  \version 7.5.1 "Blackbird"
+#
+# SU2 Project Website: https://su2code.github.io
+#
+# The SU2 Project is maintained by the SU2 Foundation
+# (http://su2foundation.org)
+#
+# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
+#
+# SU2 is free software; you can redistribute it and/or
+# modify it under the terms of the GNU Lesser General Public
+# License as published by the Free Software Foundation; either
+# version 2.1 of the License, or (at your option) any later version.
+#
+# SU2 is distributed in the hope that it will be useful,
+# but WITHOUT ANY WARRANTY; without even the implied warranty of
+# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+# Lesser General Public License for more details.
+#
+# You should have received a copy of the GNU Lesser General Public
+# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+
+import pysu2
+from mpi4py import MPI
+import numpy as np
+
+def main():
+  comm = MPI.COMM_WORLD
+  rank = comm.Get_rank()
+
+  # Initialize the corresponding driver of SU2, this includes solver preprocessing.
+  try:
+    SU2Driver = pysu2.CSinglezoneDriver('config.cfg', 1, comm);
+  except TypeError as exception:
+    print('A TypeError occured in pysu2.CDriver : ', exception)
+    raise
+
+  # Get the ID of the marker we want to deform.
+  AllMarkerIDs = SU2Driver.GetMarkerIndices()
+  MarkerName = 'interface'
+  MarkerID = AllMarkerIDs[MarkerName] if MarkerName in AllMarkerIDs else -1
+
+  # Number of vertices on the specified marker (per rank).
+  nVertex = SU2Driver.GetNumberMarkerNodes(MarkerID) if MarkerID >= 0 else 0
+
+  # Retrieve some control parameters from the driver.
+  deltaT = SU2Driver.GetUnsteady_TimeStep()
+  TimeIter = SU2Driver.GetTime_Iter()
+  nTimeIter = SU2Driver.GetnTimeIter()
+  time = TimeIter * deltaT
+  
+  # Extract the initial position of each node on the moving marker.
+  CoordX = np.zeros(nVertex)
+  CoordY = np.zeros(nVertex)
+  for iVertex in range(nVertex):
+    iPoint = SU2Driver.GetMarkerNode(MarkerID, iVertex)
+    CoordX[iVertex], CoordY[iVertex] = SU2Driver.GetInitialCoordinates(iPoint)
+
+  if rank == 0:
+    print("\n------------------------------ Begin Solver -----------------------------\n")
+  
+  # The time loop is defined in Python so that we have acces to SU2 functionalities at each time step.
+  while (TimeIter < nTimeIter):
+    # Apply the surface deformation.
+    for iVertex in range(nVertex):
+      dy = np.real(DeformFunction(CoordX[iVertex] - 0.9, time))
+      SU2Driver.SetMarkerDisplacements(MarkerID, iVertex, (0.0, dy))
+
+    # Time iteration preprocessing.
+    SU2Driver.Preprocess(TimeIter)
+    
+    # Run one time iteration (e.g. dual-time).
+    SU2Driver.Run()
+    SU2Driver.Postprocess()
+    SU2Driver.Update()
+    
+    # Monitor the solver and output solution to file if required.
+    stopCalc = SU2Driver.Monitor(TimeIter)
+    SU2Driver.Output(TimeIter)
+
+    if (stopCalc == True):
+      break
+
+    # Update control parameters
+    TimeIter += 1
+    time += deltaT
+
+  # Postprocess the solver and exit cleanly
+  SU2Driver.Postprocessing()
+
+  if SU2Driver != None:
+    del SU2Driver
+
+# Imposed deformation
+def DeformFunction(x,t):
+  A1 = 0.016
+  L = 1.0
+  k1 = 4.730/L
+  return A1*(np.cosh(k1*x) - np.cos(k1*x) + ((np.cosh(k1*L)-np.cos(k1*L))*(np.sin(k1*x)-np.sinh(k1*x)))/(np.sinh(k1*L) - np.sin(k1*L)))*(np.exp(1j*t*2) + np.exp(-1j*t*2))
+
+
+if __name__ == '__main__':
+  main()
+

From a30ed74182b03b7e14a082b6f57ad21970c8dbdf Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Mon, 20 Feb 2023 17:21:21 -0800
Subject: [PATCH 220/656] Update TestCases/parallel_regression.py

---
 TestCases/parallel_regression.py | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 5fc1049f9c1..d5ced69b20a 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -1338,10 +1338,10 @@ def main():
     test_list.append(pywrapper_rigidMotion)
 
     # Deforming Bump in Channel
-    pywrapper_deformingBump = TestCase('pywrapper deforming bump in channel')
+    pywrapper_deformingBump = TestCase('pywrapper_deformingBump')
     pywrapper_deformingBump.cfg_dir = "py_wrapper/deforming_bump_in_channel"
     pywrapper_deformingBump.cfg_file = "config.cfg"
-    pywrapper_deformingBump.test_iter = 2
+    pywrapper_deformingBump.test_iter = 1
     pywrapper_deformingBump.test_vals = [0.5, 0, -2.55436, -1.084594, -0.024882, 2.907803, 8.785498, -0.363585]
     pywrapper_deformingBump.command = TestCase.Command("mpirun -np 2", "python", "run.py")
     pywrapper_deformingBump.unsteady = True

From cc786246281ac9e1e49aae4f100057c83fc8e731 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Mon, 20 Feb 2023 17:22:05 -0800
Subject: [PATCH 221/656] Update
 TestCases/py_wrapper/deforming_bump_in_channel/run.py

---
 TestCases/py_wrapper/deforming_bump_in_channel/run.py | 2 --
 1 file changed, 2 deletions(-)

diff --git a/TestCases/py_wrapper/deforming_bump_in_channel/run.py b/TestCases/py_wrapper/deforming_bump_in_channel/run.py
index dc9a217f35e..db7c22de31f 100755
--- a/TestCases/py_wrapper/deforming_bump_in_channel/run.py
+++ b/TestCases/py_wrapper/deforming_bump_in_channel/run.py
@@ -92,8 +92,6 @@ def main():
   # Postprocess the solver and exit cleanly
   SU2Driver.Postprocessing()
 
-  if SU2Driver != None:
-    del SU2Driver
 
 # Imposed deformation
 def DeformFunction(x,t):

From 6c04e09ab5d2fcdcdf0f3bdcffa038a2310ce647 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Mon, 20 Feb 2023 18:08:24 -0800
Subject: [PATCH 222/656] Update
 TestCases/py_wrapper/deforming_bump_in_channel/run.py

---
 TestCases/py_wrapper/deforming_bump_in_channel/run.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/py_wrapper/deforming_bump_in_channel/run.py b/TestCases/py_wrapper/deforming_bump_in_channel/run.py
index db7c22de31f..6c43adba109 100755
--- a/TestCases/py_wrapper/deforming_bump_in_channel/run.py
+++ b/TestCases/py_wrapper/deforming_bump_in_channel/run.py
@@ -34,7 +34,7 @@ def main():
 
   # Initialize the corresponding driver of SU2, this includes solver preprocessing.
   try:
-    SU2Driver = pysu2.CSinglezoneDriver('config.cfg', 1, comm);
+    SU2Driver = pysu2.CSinglezoneDriver('config.cfg', 1, comm)
   except TypeError as exception:
     print('A TypeError occured in pysu2.CDriver : ', exception)
     raise

From 9116803dd67911256a32e17c13c14eb6bc60a3c8 Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Tue, 21 Feb 2023 08:08:08 -0500
Subject: [PATCH 223/656] address PR comments

---
 SU2_CFD/src/fluid/CSU2TCLib.cpp | 17 +++++++----------
 1 file changed, 7 insertions(+), 10 deletions(-)

diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 0e7c48dae27..962426080d1 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1927,14 +1927,15 @@ su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies,
   } 
 
   const su2double Omega_ij = ComputeCollisionCrossSection(iSpecies, jSpecies, T, d1, coulomb);
-  
   const su2double pi = PI_NUMBER;
+  su2double delta = 0.0;
 
   if (d1) {
-    return 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij; // d1_ij
+    delta = 8.0/3.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij; // d1_ij
   } else {
-    return 16.0/5.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij; // d2_ij
+    delta = 16.0/5.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij; // d2_ij
   }
+  return fmin(delta, 1E16)
 }
 
 void CSU2TCLib::DiffusionCoeffGY(){
@@ -1967,7 +1968,6 @@ void CSU2TCLib::DiffusionCoeffGY(){
         const su2double T_col = (iSpecies == 0 && ionization) ? Tve : T; 
 
         su2double d1_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T_col, true);
-        if (d1_ij > 1E16) d1_ij = 1E16;
 
         const su2double D_ij = kb*T_col/(Pressure*d1_ij);
         denom += gam_j/D_ij;
@@ -1999,7 +1999,6 @@ void CSU2TCLib::ViscosityGY(){
       const su2double T_col = (iSpecies == 0 && ionization) ? Tve : T; 
 
       su2double d2_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T_col, false);
-      if (d2_ij > 1E16) d2_ij = 1E16;
 
       denom += gam_j*d2_ij;
     }
@@ -2049,8 +2048,6 @@ void CSU2TCLib::ThermalConductivitiesGY(){
 
       su2double d1_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T_col, true);
       su2double d2_ij = ComputeCollisionDelta(iSpecies, jSpecies, Mi, Mj, T_col, false);
-      if (d1_ij >1E16) d1_ij = 1E16;
-      if (d2_ij >1E16) d2_ij = 1E16;      
 
       if (jSpecies == 0 && ionization) { denom_t += 3.54*gam_j*d2_ij; }
       else { denom_t += a_ij*gam_j*d2_ij; }
@@ -2060,9 +2057,9 @@ void CSU2TCLib::ThermalConductivitiesGY(){
     }
 
     /*--- Prevent divide by 0 ---*/
-    if (denom_t == 0.0) denom_t = EPS;
-    if (denom_r == 0.0) denom_r = EPS;
-    if (denom_re == 0.0) denom_re = EPS;
+    if (denom_t <= 0.0) denom_t = EPS;
+    if (denom_r <= 0.0) denom_r = EPS;
+    if (denom_re <= 0.0) denom_re = EPS;
 
     /*--- Translational contribution to thermal conductivity ---*/
     if (!(ionization && iSpecies == 0)) ThermalCond_tr += ((15.0/4.0)*kb*gam_i/denom_t);

From a7e10eee44fefa94a01b8c029e719467c3d30226 Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Tue, 21 Feb 2023 08:20:54 -0500
Subject: [PATCH 224/656] alway forget the semicolon

---
 SU2_CFD/src/fluid/CSU2TCLib.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 962426080d1..1c0babca6b5 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1935,7 +1935,7 @@ su2double CSU2TCLib::ComputeCollisionDelta(unsigned iSpecies, unsigned jSpecies,
   } else {
     delta = 16.0/5.0 * sqrt((2.0*Mi*Mj) / (pi*Ru*T*(Mi+Mj))) * Omega_ij; // d2_ij
   }
-  return fmin(delta, 1E16)
+  return fmin(delta, 1E16);
 }
 
 void CSU2TCLib::DiffusionCoeffGY(){

From 5a0ea92a9ffdc7d85dd255b63c078e6ac85b7858 Mon Sep 17 00:00:00 2001
From: Wally Maier <wallytmaier@gmail.com>
Date: Tue, 21 Feb 2023 15:23:39 -0500
Subject: [PATCH 225/656] Update regression.yml

---
 .github/workflows/regression.yml | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index c614f3f8f32..e749e661e70 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c feature_NEMO_visc_ion -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
         with:

From 51ef1aa5652ed8825a2ea1f10cbee6594f7ad000 Mon Sep 17 00:00:00 2001
From: WallyMaier <wmaier@stanford.edu>
Date: Wed, 22 Feb 2023 08:46:33 -0800
Subject: [PATCH 226/656] update version mpp

---
 meson_scripts/init.py  | 2 +-
 subprojects/Mutationpp | 2 +-
 2 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index a5e024a1b20..b680c4465cc 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -54,7 +54,7 @@ def init_submodules(method = 'auto'):
   github_repo_meson = 'https://github.com/mesonbuild/meson'
   sha_version_ninja = '52649de2c56b63f42bc59513d51286531c595b44'
   github_repo_ninja = 'https://github.com/ninja-build/ninja'
-  sha_version_mpp = '5ff579f43781cae07411e5ab46291c9971536be6'
+  sha_version_mpp = '4cb6e3a05c15f49ffd346dc9f185ccc3459728b0'
   github_repo_mpp = 'https://github.com/mutationpp/Mutationpp'
   sha_version_coolprop = '0ce42fcf3bb2c373512bc825a4f0c1973a78f307'
   github_repo_coolprop = 'https://github.com/CoolProp/CoolProp'
diff --git a/subprojects/Mutationpp b/subprojects/Mutationpp
index 5ff579f4378..4cb6e3a05c1 160000
--- a/subprojects/Mutationpp
+++ b/subprojects/Mutationpp
@@ -1 +1 @@
-Subproject commit 5ff579f43781cae07411e5ab46291c9971536be6
+Subproject commit 4cb6e3a05c15f49ffd346dc9f185ccc3459728b0

From 0adc5c517c5e5fe78b4b36fff5c301e02335d0cf Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Wed, 22 Feb 2023 13:25:26 -0500
Subject: [PATCH 227/656] remove block on gupta yos

---
 Common/src/CConfig.cpp | 5 ++---
 1 file changed, 2 insertions(+), 3 deletions(-)

diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 8b36a1f2415..918ac0bfe26 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -3942,9 +3942,8 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
       }
     }
 
-    if (Kind_FluidModel == MUTATIONPP &&
-        (Kind_TransCoeffModel != TRANSCOEFFMODEL::WILKE && Kind_TransCoeffModel != TRANSCOEFFMODEL::CHAPMANN_ENSKOG)) {
-      SU2_MPI::Error("Transport model not available for NEMO solver using MUTATIONPP. Please use the WILKE or CHAPMANN_ENSKOG transport model instead..",
+    if (Kind_FluidModel == MUTATIONPP && (Kind_TransCoeffModel == TRANSCOEFFMODEL::SUTHERLAND)) {
+      SU2_MPI::Error("Transport model not available for NEMO solver using MUTATIONPP. Please use the WILKE, GUPTAYOS, or CHAPMANN_ENSKOG transport model instead.",
                      CURRENT_FUNCTION);
     }
 

From 1f9d2c7890d1e99bc48ce646c05d24f27726b125 Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Wed, 22 Feb 2023 14:40:03 -0500
Subject: [PATCH 228/656] Try to get mutation++ to compile

---
 .github/workflows/regression.yml | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index e749e661e70..a17a697790a 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -26,7 +26,7 @@ jobs:
         config_set: [BaseMPI, ReverseMPI, ForwardMPI, BaseNoMPI, ReverseNoMPI, ForwardNoMPI, BaseOMP, ReverseOMP, ForwardOMP]
         include:
           - config_set: BaseMPI
-            flags: '-Denable-pywrapper=true -Denable-coolprop=true -Denable-tests=true --warnlevel=2 --werror'
+            flags: '-Denable-pywrapper=true -Denable-coolprop=true -Denable-mpp=true -Denable-tests=true --warnlevel=2 --werror'
           - config_set: ReverseMPI
             flags: '-Denable-autodiff=true -Denable-normal=false -Denable-pywrapper=true -Denable-tests=true --warnlevel=3 --werror'
           - config_set: ForwardMPI

From 26f7dd5230539eff6baa150cc2b7d83cf19376be Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Thu, 23 Feb 2023 10:21:22 -0500
Subject: [PATCH 229/656] ??

---
 meson.build | 6 ++++++
 1 file changed, 6 insertions(+)

diff --git a/meson.build b/meson.build
index 84999a5476b..a6616202bce 100644
--- a/meson.build
+++ b/meson.build
@@ -230,6 +230,12 @@ catch2_dep = declare_dependency(include_directories: 'externals/catch2/')
 
 if get_option('enable-mpp')
   cmake = import('cmake')
+  if build_machine.cpu_family() == 'x86' or build_machine.cpu_family() == 'x86_64'
+    cmake_opts = cmake.subproject_options()
+      cmake_opts.add_cmake_defines({
+      'CMAKE_MAKE_PROGRAM': meson.source_root() + '/ninja',
+      'CMAKE_POSITION_INDEPENDENT_CODE': 'ON'
+  })
   mpp_subproj = cmake.subproject('Mutationpp')
   mpp_dep = mpp_subproj.dependency('mutation++')
   su2_deps     += mpp_dep

From dbb78646a48f4e3fa55230361ef82fa913fced26 Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Thu, 23 Feb 2023 10:27:19 -0500
Subject: [PATCH 230/656] missing endif

---
 meson.build | 3 ++-
 1 file changed, 2 insertions(+), 1 deletion(-)

diff --git a/meson.build b/meson.build
index a6616202bce..af4d79a063d 100644
--- a/meson.build
+++ b/meson.build
@@ -235,7 +235,8 @@ if get_option('enable-mpp')
       cmake_opts.add_cmake_defines({
       'CMAKE_MAKE_PROGRAM': meson.source_root() + '/ninja',
       'CMAKE_POSITION_INDEPENDENT_CODE': 'ON'
-  })
+      })
+  endif
   mpp_subproj = cmake.subproject('Mutationpp')
   mpp_dep = mpp_subproj.dependency('mutation++')
   su2_deps     += mpp_dep

From c48a1e1b57fbc2969cc459b318ff92f6ee7d6c62 Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Thu, 23 Feb 2023 10:33:18 -0500
Subject: [PATCH 231/656] move if statement

---
 meson.build | 10 +++++-----
 1 file changed, 5 insertions(+), 5 deletions(-)

diff --git a/meson.build b/meson.build
index af4d79a063d..5fa6ca10e94 100644
--- a/meson.build
+++ b/meson.build
@@ -229,13 +229,13 @@ endforeach
 catch2_dep = declare_dependency(include_directories: 'externals/catch2/')
 
 if get_option('enable-mpp')
-  cmake = import('cmake')
   if build_machine.cpu_family() == 'x86' or build_machine.cpu_family() == 'x86_64'
+    cmake = import('cmake')
     cmake_opts = cmake.subproject_options()
-      cmake_opts.add_cmake_defines({
-      'CMAKE_MAKE_PROGRAM': meson.source_root() + '/ninja',
-      'CMAKE_POSITION_INDEPENDENT_CODE': 'ON'
-      })
+    cmake_opts.add_cmake_defines({
+    'CMAKE_MAKE_PROGRAM': meson.source_root() + '/ninja',
+    'CMAKE_POSITION_INDEPENDENT_CODE': 'ON'
+    })
   endif
   mpp_subproj = cmake.subproject('Mutationpp')
   mpp_dep = mpp_subproj.dependency('mutation++')

From 7a342f1d37f527175f2e334b6a5a47c1906fcc03 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Thu, 23 Feb 2023 08:17:41 -0800
Subject: [PATCH 232/656] Update meson.build

---
 meson.build | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/meson.build b/meson.build
index 5fa6ca10e94..a845d412781 100644
--- a/meson.build
+++ b/meson.build
@@ -237,7 +237,7 @@ if get_option('enable-mpp')
     'CMAKE_POSITION_INDEPENDENT_CODE': 'ON'
     })
   endif
-  mpp_subproj = cmake.subproject('Mutationpp')
+  mpp_subproj = cmake.subproject('Mutationpp', options: cmake_opts)
   mpp_dep = mpp_subproj.dependency('mutation++')
   su2_deps     += mpp_dep
   su2_cpp_args += '-DHAVE_MPP'

From e31676cf0d9ecf208d0702af743f80866ef0d0bb Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Thu, 23 Feb 2023 11:43:58 -0500
Subject: [PATCH 233/656] add error override

---
 meson.build | 1 +
 1 file changed, 1 insertion(+)

diff --git a/meson.build b/meson.build
index a845d412781..5d3374f25b2 100644
--- a/meson.build
+++ b/meson.build
@@ -232,6 +232,7 @@ if get_option('enable-mpp')
   if build_machine.cpu_family() == 'x86' or build_machine.cpu_family() == 'x86_64'
     cmake = import('cmake')
     cmake_opts = cmake.subproject_options()
+    cmake_opts.set_override_option('warning_level', '0')
     cmake_opts.add_cmake_defines({
     'CMAKE_MAKE_PROGRAM': meson.source_root() + '/ninja',
     'CMAKE_POSITION_INDEPENDENT_CODE': 'ON'

From 9bc071697f0bae0bba1e5f1e1f6938f1a9c741d4 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Vo=C3=9F=2C=20Arne?= <arne.voss@dlr.de>
Date: Fri, 24 Feb 2023 12:48:27 +0100
Subject: [PATCH 234/656] Adding a new choice (Z_DIR) for parameter GUST_DIR
 and a note with respect to the wavelength of 1-cos gusts to the
 config_template.

---
 config_template.cfg | 3 ++-
 1 file changed, 2 insertions(+), 1 deletion(-)

diff --git a/config_template.cfg b/config_template.cfg
index 0463ce3357f..fb51116a546 100644
--- a/config_template.cfg
+++ b/config_template.cfg
@@ -544,10 +544,11 @@ WIND_GUST = NO
 % Type of gust (NONE, TOP_HAT, SINE, ONE_M_COSINE, VORTEX, EOG)
 GUST_TYPE = NONE
 %
-% Direction of the gust (X_DIR or Y_DIR)
+% Direction of the gust (X_DIR, Y_DIR or Z_DIR)
 GUST_DIR = Y_DIR
 %
 % Gust wavelenght (meters)
+% Note for 1-cos gusts: this is the full gust length, not the gust gradient H (half gust length) as used for example in CS-25.
 GUST_WAVELENGTH= 10.0
 %
 % Number of gust periods

From c015566dca0e3bc817188741c3c886ff7b7a2edb Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Vo=C3=9F=2C=20Arne?= <arne.voss@dlr.de>
Date: Fri, 24 Feb 2023 12:49:55 +0100
Subject: [PATCH 235/656] Implement new option Z_DIR

---
 Common/include/option_structure.hpp | 4 +++-
 1 file changed, 3 insertions(+), 1 deletion(-)

diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index 72347466647..3b6303c7fad 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -778,11 +778,13 @@ static const MapType<std::string, ENUM_GUST_TYPE> Gust_Type_Map = {
  */
 enum ENUM_GUST_DIR {
   X_DIR = 0,  /*!< \brief Gust direction-X. */
-  Y_DIR = 1   /*!< \brief Gust direction-Y. */
+  Y_DIR = 1,  /*!< \brief Gust direction-Y. */
+  Z_DIR = 2   /*!< \brief Gust direction-Z. */
 };
 static const MapType<std::string, ENUM_GUST_DIR> Gust_Dir_Map = {
   MakePair("X_DIR", X_DIR)
   MakePair("Y_DIR", Y_DIR)
+  MakePair("Z_DIR", Z_DIR)
 };
 
 // If you add to ENUM_CENTERED, you must also add the option to ENUM_CONVECTIVE

From cc353ee548a2189fc9289842cb0e0e0dabc4f7f5 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Vo=C3=9F=2C=20Arne?= <arne.voss@dlr.de>
Date: Fri, 24 Feb 2023 12:56:17 +0100
Subject: [PATCH 236/656] I think we don't need to set any source terms because
 they depend on the gust derivatives, which are zero in all implemented cases.
 This piece of code belongs to the split velocity method, which is currently
 not used as far as I understand. However, when trying to remove it, I broke
 the code elsewhere.

---
 SU2_CFD/src/numerics/flow/flow_sources.cpp | 9 +++++++--
 1 file changed, 7 insertions(+), 2 deletions(-)

diff --git a/SU2_CFD/src/numerics/flow/flow_sources.cpp b/SU2_CFD/src/numerics/flow/flow_sources.cpp
index 2fb164f3d1f..3d297157a51 100644
--- a/SU2_CFD/src/numerics/flow/flow_sources.cpp
+++ b/SU2_CFD/src/numerics/flow/flow_sources.cpp
@@ -784,8 +784,13 @@ CNumerics::ResidualType<> CSourceWindGust::ComputeResidual(const CConfig* config
     //residual[3] = smz*Volume;
     residual[3] = se*Volume;
   } else {
-    SU2_MPI::Error("You should only be in the gust source term in two dimensions", CURRENT_FUNCTION);
-  }
+	  //    SU2_MPI::Error("You should only be in the gust source term in two dimensions", CURRENT_FUNCTION);
+	  	residual[0] = 0.0;
+	  	residual[1] = 0.0;
+	  	residual[2] = 0.0;
+	  	residual[3] = 0.0;
+	  	residual[4] = 0.0;
+	    }
 
   /*--- For now the source term Jacobian is just set to zero ---*/
   //bool implicit = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);

From 3362bc14a9be007932a212ad1a95147aa238ffbb Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Fri, 24 Feb 2023 15:38:50 -0800
Subject: [PATCH 237/656] Update .github/workflows/regression.yml

---
 .github/workflows/regression.yml | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index a17a697790a..8dea4730c10 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -26,7 +26,7 @@ jobs:
         config_set: [BaseMPI, ReverseMPI, ForwardMPI, BaseNoMPI, ReverseNoMPI, ForwardNoMPI, BaseOMP, ReverseOMP, ForwardOMP]
         include:
           - config_set: BaseMPI
-            flags: '-Denable-pywrapper=true -Denable-coolprop=true -Denable-mpp=true -Denable-tests=true --warnlevel=2 --werror'
+            flags: '-Denable-pywrapper=true -Denable-coolprop=true -Denable-mpp=true -Denable-tests=true --warnlevel=2'
           - config_set: ReverseMPI
             flags: '-Denable-autodiff=true -Denable-normal=false -Denable-pywrapper=true -Denable-tests=true --warnlevel=3 --werror'
           - config_set: ForwardMPI

From 62aaee78c23725032a6bc8ac915ddc1b1c7c9a3e Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 25 Feb 2023 16:47:48 -0800
Subject: [PATCH 238/656] matrix view type to manipulate fields in python
 without copying data

---
 .../containers/CPyWrapperMatrixView.hpp       | 115 ++++++++++++++++++
 Common/src/containers/meson.build             |   2 +-
 SU2_CFD/include/drivers/CDriverBase.hpp       |  64 +++++++---
 SU2_CFD/include/output/CFlowOutput.hpp        |  70 +----------
 SU2_CFD/include/solvers/CSolver.hpp           |   4 +-
 SU2_CFD/include/variables/CEulerVariable.hpp  |   3 +
 .../include/variables/CIncEulerVariable.hpp   |   3 +
 SU2_CFD/include/variables/CMeshVariable.hpp   |   5 +
 .../include/variables/CNEMOEulerVariable.hpp  |   3 +
 .../include/variables/CPrimitiveIndices.hpp   |  42 ++++++-
 SU2_CFD/include/variables/CVariable.hpp       |   5 +
 SU2_CFD/src/drivers/CDriverBase.cpp           |  62 ++++------
 SU2_CFD/src/output/CFlowOutput.cpp            |  74 +++++++++--
 SU2_CFD/src/solvers/CAdjEulerSolver.cpp       |   1 +
 SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp     |   1 +
 SU2_CFD/src/solvers/CDiscAdjMeshSolver.cpp    |   1 +
 SU2_CFD/src/solvers/CEulerSolver.cpp          |   2 +-
 SU2_CFD/src/solvers/CFEASolver.cpp            |   2 +-
 SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp   |   4 +-
 SU2_CFD/src/solvers/CHeatSolver.cpp           |   2 +-
 SU2_CFD/src/solvers/CIncEulerSolver.cpp       |   2 +-
 SU2_CFD/src/solvers/CMeshSolver.cpp           |   2 +
 SU2_CFD/src/solvers/CNEMOEulerSolver.cpp      |   2 +-
 SU2_CFD/src/solvers/CRadP1Solver.cpp          |   1 +
 SU2_CFD/src/solvers/CSpeciesSolver.cpp        |   2 +-
 SU2_CFD/src/solvers/CTransLMSolver.cpp        |   2 +-
 SU2_CFD/src/solvers/CTurbSASolver.cpp         |   2 +-
 SU2_CFD/src/solvers/CTurbSSTSolver.cpp        |   4 +-
 SU2_PY/FSI_tools/FSIInterface.py              |   4 +-
 SU2_PY/pySU2/pySU2.i                          |   7 +-
 SU2_PY/pySU2/pySU2ad.i                        |   8 +-
 .../deforming_bump_in_channel/run.py          |  10 +-
 .../launch_flatPlate_rigidMotion.py           |   2 +-
 meson.build                                   |   8 +-
 34 files changed, 353 insertions(+), 168 deletions(-)
 create mode 100644 Common/include/containers/CPyWrapperMatrixView.hpp

diff --git a/Common/include/containers/CPyWrapperMatrixView.hpp b/Common/include/containers/CPyWrapperMatrixView.hpp
new file mode 100644
index 00000000000..2c3d6477ee4
--- /dev/null
+++ b/Common/include/containers/CPyWrapperMatrixView.hpp
@@ -0,0 +1,115 @@
+/*!
+ * \file CPyWrapperMatrixView.hpp
+ * \brief A simple matrix view to use with the python wrapper.
+ * \author P. Gomes
+ * \version 7.5.1 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+
+#pragma once
+
+#include <utility>
+#include <vector>
+#include <string>
+
+#include "C2DContainer.hpp"
+#include "../parallelization/mpi_structure.hpp"
+
+/*!
+ * \class CPyWrapperMatrixView
+ * \ingroup PySU2
+ * \brief A simple matrix view to use with the python wrapper. The accessors
+ * in this class provide a passive double interface to su2activematrix.
+ * This can be extended to allow access to derivative information of su2double.
+ */
+class CPyWrapperMatrixView {
+ private:
+  static_assert(su2activematrix::IsRowMajor, "");
+  su2double* data_ = nullptr;
+  unsigned long rows_ = 0, cols_ = 0;
+  std::string name_;
+  bool read_only_ = false;
+
+  inline const su2double& Access(unsigned long row, unsigned long col) const {
+    if (row > rows_ || col > cols_) SU2_MPI::Error(name_ + " out of bounds", "CPyWrapperMatrixView");
+    return data_[row * cols_ + col];
+  }
+  inline su2double& Access(unsigned long row, unsigned long col) {
+    if (read_only_) SU2_MPI::Error(name_ + " is read-only", "CPyWrapperMatrixView");
+    const auto& const_me = *this;
+    return const_cast<su2double&>(const_me.Access(row, col));
+  }
+
+ public:
+  CPyWrapperMatrixView() = default;
+
+  /*!
+   * \brief Construct the view of the matrix.
+   * \note "name" should be set to the variable name being returned to give better information to users.
+   * \note "read_only" can be set to true to prevent the data from being modified.
+   */
+  CPyWrapperMatrixView(su2activematrix& mat, const std::string& name, bool read_only)
+    : data_(mat.data()), rows_(mat.rows()), cols_(mat.cols()), name_(name), read_only_(read_only) {}
+
+  /*!
+   * \brief Returns the shape of the matrix.
+   */
+  std::pair<unsigned long, unsigned long> Shape() const { return std::make_pair(rows_, cols_); }
+
+  /*!
+   * \brief Returns whether the data is read-only [true] or if it can be modified [false].
+   */
+  bool IsReadOnly() const { return read_only_; }
+
+  /*!
+   * \brief Gets the value for a (row, column) pair.
+   */
+  passivedouble operator() (unsigned long row, unsigned long col) const { return Get(row, col); }
+
+  /*!
+   * \brief Gets the value for a (row, column) pair.
+   */
+  passivedouble Get(unsigned long row, unsigned long col) const { return SU2_TYPE::GetValue(Access(row, col)); }
+
+  /*!
+   * \brief Gets the values for a row of the matrix.
+   */
+  std::vector<passivedouble> Get(unsigned long row) const {
+    std::vector<passivedouble> vals(cols_);
+    for (unsigned long j = 0; j < cols_; ++j) vals[j] = Get(row, j);
+    return vals;
+  }
+
+  /*!
+   * \brief Sets the value for a (row, column) pair.
+   * \note This clears derivative information (consistently with C++ operator= with passive rhs).
+   */
+  void Set(unsigned long row, unsigned long col, passivedouble val) { Access(row, col) = val; }
+
+  /*!
+   * \brief Sets the values for a row of the matrix.
+   */
+  void Set(unsigned long row, std::vector<passivedouble> vals) {
+    unsigned long j = 0;
+    for (const auto& val : vals) Set(row, j++, val);
+  }
+};
diff --git a/Common/src/containers/meson.build b/Common/src/containers/meson.build
index 9a0fdd1a1ae..4c8d4fe618a 100644
--- a/Common/src/containers/meson.build
+++ b/Common/src/containers/meson.build
@@ -1,3 +1,3 @@
 common_src += files(['CTrapezoidalMap.cpp',
-                     'CFileReaderLUT.cpp', 
+                     'CFileReaderLUT.cpp',
                      'CLookUpTable.cpp'])
diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index b7c5ca56d9f..c83ad9bdf31 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -28,6 +28,7 @@
 #pragma once
 
 #include "../../../Common/include/CConfig.hpp"
+#include "../../../Common/include/containers/CPyWrapperMatrixView.hpp"
 #include "../numerics/CNumerics.hpp"
 #include "../output/COutput.hpp"
 #include "../solvers/CSolver.hpp"
@@ -38,7 +39,6 @@
  * \brief Base class for all drivers.
  * \author H. Patel, A. Gastaldi
  */
-
 class CDriverBase {
  protected:
   int rank,               /*!< \brief MPI Rank. */
@@ -189,25 +189,24 @@ class CDriverBase {
   bool GetNodeDomain(unsigned long iPoint) const;
 
   /*!
-   * \brief Get the initial (un-deformed) coordinates of a mesh node.
-   * \param[in] iPoint - Mesh node index.
-   * \return Initial node coordinates (nDim).
-   */
-  vector<passivedouble> GetInitialCoordinates(unsigned long iPoint) const;
-
-  /*!
-   * \brief Get the current coordinates of a mesh node.
-   * \param[in] iPoint - Mesh node index.
-   * \return Node coordinates (nDim).
+   * \brief Get a read-only view of the initial (undeformed) coordinates of all mesh nodes.
    */
-  vector<passivedouble> GetCoordinates(unsigned long iPoint) const;
+  inline CPyWrapperMatrixView InitialCoordinates() const {
+    if (!main_config->GetDeform_Mesh()) {
+      SU2_MPI::Error("Initial coordinates are only available with DEFORM_MESH= YES", CURRENT_FUNCTION);
+    }
+    auto* coords =
+        const_cast<su2activematrix*>(solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord());
+    return CPyWrapperMatrixView(*coords, "InitialCoordinates", true);
+  }
 
   /*!
-   * \brief Set the coordinates of a mesh node.
-   * \param[in] iPoint - Mesh node index.
-   * \param[in] values - Node coordinates (nDim).
+   * \brief Get a read/write view of the current coordinates of all mesh nodes.
    */
-  void SetCoordinates(unsigned long iPoint, vector<passivedouble> values);
+  inline CPyWrapperMatrixView Coordinates() {
+    auto& coords = const_cast<su2activematrix&>(main_geometry->nodes->GetCoord());
+    return CPyWrapperMatrixView(coords, "Coordinates", false);
+  }
 
   /*!
    * \brief Get the number of markers in the mesh.
@@ -323,6 +322,39 @@ class CDriverBase {
    * \brief Communicate the boundary mesh displacements.
    */
   void CommunicateMeshDisplacements(void);
+
+  /*!
+   * \brief Get all the active solver names with their associated indices (which can be used to access their data).
+   */
+  map<string, unsigned short> GetSolverIndices() const;
+
+  /*!
+   * \brief Get a read/write view of the current solution on all mesh nodes of a solver.
+   */
+  inline CPyWrapperMatrixView Solution(unsigned short iSolver) {
+    auto* solver = solver_container[ZONE_0][INST_0][MESH_0][iSolver];
+    if (solver == nullptr) SU2_MPI::Error("The selected solver does not exist.", CURRENT_FUNCTION);
+    auto& solution = solver->GetNodes()->GetSolution();
+    return CPyWrapperMatrixView(solution, "Solution of " + solver->GetSolverName(), false);
+  }
+
+  /*!
+   * \brief Get the flow solver primitive variable names with their associated indices.
+   * These correspond to the column indices in the matrix returned by Primitives.
+   */
+  map<string, unsigned short> GetPrimitiveIndices() const;
+
+  /*!
+   * \brief Get a read/write view of the current primitive variables on all mesh nodes of the flow solver.
+   * \warning Primitive variables are only available for flow solvers.
+   */
+  inline CPyWrapperMatrixView Primitives() {
+    auto* solver = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL];
+    if (solver == nullptr) SU2_MPI::Error("The flow solver does not exist.", CURRENT_FUNCTION);
+    auto& primitives = const_cast<su2activematrix&>(solver->GetNodes()->GetPrimitive());
+    return CPyWrapperMatrixView(primitives, "Primitives", false);
+  }
+
 /// \}
 
  protected:
diff --git a/SU2_CFD/include/output/CFlowOutput.hpp b/SU2_CFD/include/output/CFlowOutput.hpp
index 9f9b3e029b8..9020076486e 100644
--- a/SU2_CFD/include/output/CFlowOutput.hpp
+++ b/SU2_CFD/include/output/CFlowOutput.hpp
@@ -30,6 +30,10 @@
 #include "CFVMOutput.hpp"
 #include "../variables/CVariable.hpp"
 
+/*--- Forward declare to avoid including here. ---*/
+template <class>
+struct CPrimitiveIndices;
+
 class CFlowOutput : public CFVMOutput{
 protected:
   unsigned long lastInnerIter;
@@ -211,71 +215,7 @@ class CFlowOutput : public CFVMOutput{
    * \brief Helper for custom outputs, converts variable names to indices and pointers which are then used
    * to evaluate the custom expressions.
    */
-  template <class FlowIndices>
-  void ConvertVariableSymbolsToIndices(const FlowIndices& idx, CustomOutput& output) const {
-
-    static const auto knownVariables =
-        "TEMPERATURE, TEMPERATURE_VE, VELOCITY_X, VELOCITY_Y, VELOCITY_Z, PRESSURE,\n"
-        "DENSITY, ENTHALPY, SOUND_SPEED, LAMINAR_VISCOSITY, EDDY_VISCOSITY, THERMAL_CONDUCTIVITY\n"
-        "TURB[0,1,...], RAD[0,1,...], SPECIES[0,1,...]";
-
-    auto IndexOfVariable = [&](const FlowIndices& idx, const std::string& var) {
-      /*--- Primitives of the flow solver. ---*/
-      const auto flow_offset = FLOW_SOL * CustomOutput::MAX_VARS_PER_SOLVER;
-
-      if ("TEMPERATURE" == var) return flow_offset + idx.Temperature();
-      if ("TEMPERATURE_VE" == var) return flow_offset + idx.Temperature_ve();
-      if ("VELOCITY_X" == var) return flow_offset + idx.Velocity();
-      if ("VELOCITY_Y" == var) return flow_offset + idx.Velocity() + 1;
-      if ("VELOCITY_Z" == var) return flow_offset + idx.Velocity() + 2;
-      if ("PRESSURE" == var) return flow_offset + idx.Pressure();
-      if ("DENSITY" == var) return flow_offset + idx.Density();
-      if ("ENTHALPY" == var) return flow_offset + idx.Enthalpy();
-      if ("SOUND_SPEED" == var) return flow_offset + idx.SoundSpeed();
-      if ("LAMINAR_VISCOSITY" == var) return flow_offset + idx.LaminarViscosity();
-      if ("EDDY_VISCOSITY" == var) return flow_offset + idx.EddyViscosity();
-      if ("THERMAL_CONDUCTIVITY" == var) return flow_offset + idx.ThermalConductivity();
-
-      /*--- Index-based (no name) access to variables of other solvers. ---*/
-      auto GetIndex = [](const std::string& s, int nameLen) {
-        /*--- Extract an int from "name[int]", nameLen is the length of "name". ---*/
-        return std::stoi(std::string(s.begin() + nameLen + 1, s.end() - 1));
-      };
-      if (var.rfind("SPECIES", 0) == 0) return SPECIES_SOL * CustomOutput::MAX_VARS_PER_SOLVER + GetIndex(var, 7);
-      if (var.rfind("TURB", 0) == 0) return TURB_SOL * CustomOutput::MAX_VARS_PER_SOLVER + GetIndex(var, 4);
-      if (var.rfind("RAD", 0) == 0) return RAD_SOL * CustomOutput::MAX_VARS_PER_SOLVER + GetIndex(var, 3);
-
-      return CustomOutput::NOT_A_VARIABLE;
-    };
-
-    output.otherOutputs.clear();
-    output.varIndices.clear();
-    output.varIndices.reserve(output.varSymbols.size());
-
-    for (const auto& var : output.varSymbols) {
-      output.varIndices.push_back(IndexOfVariable(idx, var));
-
-      if (output.type == OperationType::FUNCTION && output.varIndices.back() != CustomOutput::NOT_A_VARIABLE) {
-        SU2_MPI::Error("Custom outputs of type 'Function' cannot reference solver variables.", CURRENT_FUNCTION);
-      }
-      /*--- Symbol is a valid solver variable. ---*/
-      if (output.varIndices.back() < CustomOutput::NOT_A_VARIABLE) continue;
-
-      /*--- An index above NOT_A_VARIABLE is not valid with current solver settings. ---*/
-      if (output.varIndices.back() > CustomOutput::NOT_A_VARIABLE) {
-        SU2_MPI::Error("Inactive solver variable (" + var + ") used in function " + output.name + "\n"
-                       "E.g. this may only be a variable of the compressible solver.", CURRENT_FUNCTION);
-      }
-
-      /*--- An index equal to NOT_A_VARIABLE may refer to a history output. ---*/
-      output.varIndices.back() += output.otherOutputs.size();
-      output.otherOutputs.push_back(GetPtrToHistoryOutput(var));
-      if (output.otherOutputs.back() == nullptr) {
-        SU2_MPI::Error("Invalid history output or solver variable (" + var + ") used in function " + output.name +
-                       "\nValid solvers variables: " + knownVariables, CURRENT_FUNCTION);
-      }
-    }
-  }
+  void ConvertVariableSymbolsToIndices(const CPrimitiveIndices<unsigned long>& idx, CustomOutput& output) const;
 
   /*!
    * \brief Compute value of the Q criteration for vortex idenfitication
diff --git a/SU2_CFD/include/solvers/CSolver.hpp b/SU2_CFD/include/solvers/CSolver.hpp
index 954b06ad75d..9ac3d17f6a2 100644
--- a/SU2_CFD/include/solvers/CSolver.hpp
+++ b/SU2_CFD/include/solvers/CSolver.hpp
@@ -4246,9 +4246,9 @@ class CSolver {
 
   /*!
    * \brief Retrieve the solver name for output purposes.
-   * \param[out] val_solvername - Name of the solver.
+   * \returns Name of the solver.
    */
-  inline string GetSolverName(void) {return SolverName;}
+  inline const string& GetSolverName() const  { return SolverName; }
 
   /*!
    * \brief Get the solution fields.
diff --git a/SU2_CFD/include/variables/CEulerVariable.hpp b/SU2_CFD/include/variables/CEulerVariable.hpp
index 25e992da2e1..44f07ffa0a2 100644
--- a/SU2_CFD/include/variables/CEulerVariable.hpp
+++ b/SU2_CFD/include/variables/CEulerVariable.hpp
@@ -46,6 +46,8 @@ class CEulerVariable : public CFlowVariable {
   struct CIndices {
     const IndexType nDim;
     CIndices(IndexType ndim, IndexType) : nDim(ndim) {}
+    inline IndexType NDim() const { return nDim; }
+    inline IndexType NSpecies() const { return 0; }
     inline IndexType Temperature() const { return 0; }
     inline IndexType Velocity() const { return 1; }
     inline IndexType Pressure() const { return nDim+1; }
@@ -58,6 +60,7 @@ class CEulerVariable : public CFlowVariable {
     inline IndexType CpTotal() const { return nDim+8; }
 
     /*--- For compatible interface with NEMO. ---*/
+    inline IndexType SpeciesDensities() const { return std::numeric_limits<IndexType>::max(); }
     inline IndexType Temperature_ve() const { return std::numeric_limits<IndexType>::max(); }
   };
 
diff --git a/SU2_CFD/include/variables/CIncEulerVariable.hpp b/SU2_CFD/include/variables/CIncEulerVariable.hpp
index 61341177faa..16b33d52e84 100644
--- a/SU2_CFD/include/variables/CIncEulerVariable.hpp
+++ b/SU2_CFD/include/variables/CIncEulerVariable.hpp
@@ -46,6 +46,8 @@ class CIncEulerVariable : public CFlowVariable {
   struct CIndices {
     const IndexType nDim;
     CIndices(IndexType ndim, IndexType) : nDim(ndim) {}
+    inline IndexType NDim() const { return nDim; }
+    inline IndexType NSpecies() const { return 0; }
     inline IndexType Pressure() const { return 0; }
     inline IndexType Velocity() const { return 1; }
     inline IndexType Temperature() const { return nDim+1; }
@@ -59,6 +61,7 @@ class CIncEulerVariable : public CFlowVariable {
     inline IndexType CvTotal() const { return nDim+8; }
 
     /*--- For compatible interface with NEMO. ---*/
+    inline IndexType SpeciesDensities() const { return std::numeric_limits<IndexType>::max(); }
     inline IndexType Temperature_ve() const { return std::numeric_limits<IndexType>::max(); }
     inline IndexType Enthalpy() const { return std::numeric_limits<IndexType>::max(); }
   };
diff --git a/SU2_CFD/include/variables/CMeshVariable.hpp b/SU2_CFD/include/variables/CMeshVariable.hpp
index 1c5c185c222..ce3a807885c 100644
--- a/SU2_CFD/include/variables/CMeshVariable.hpp
+++ b/SU2_CFD/include/variables/CMeshVariable.hpp
@@ -63,6 +63,11 @@ class CMeshVariable : public CVariable {
    */
   inline const su2double *GetMesh_Coord(unsigned long iPoint) const final { return Mesh_Coord[iPoint]; }
 
+  /*!
+   * \brief Get the undeformed coordinates for the entire domain.
+   */
+  inline const MatrixType* GetMesh_Coord() const final { return &Mesh_Coord; }
+
   /*!
    * \brief Set the value of the undeformed coordinates.
    * \param[in] iDim - Index of Mesh_Coord[nDim]
diff --git a/SU2_CFD/include/variables/CNEMOEulerVariable.hpp b/SU2_CFD/include/variables/CNEMOEulerVariable.hpp
index d68d90529da..246d24bf7db 100644
--- a/SU2_CFD/include/variables/CNEMOEulerVariable.hpp
+++ b/SU2_CFD/include/variables/CNEMOEulerVariable.hpp
@@ -48,6 +48,8 @@ class CNEMOEulerVariable : public CFlowVariable {
   struct CIndices {
     const IndexType nDim, nSpecies;
     CIndices(IndexType ndim, IndexType nspecies) : nDim(ndim), nSpecies(nspecies) {}
+    inline IndexType NDim() const {return nDim;}
+    inline IndexType NSpecies() const {return nSpecies;}
     inline IndexType SpeciesDensities() const {return 0;}
     inline IndexType Temperature() const {return nSpecies;}
     inline IndexType Temperature_ve() const {return nSpecies+1;}
@@ -61,6 +63,7 @@ class CNEMOEulerVariable : public CFlowVariable {
     inline IndexType LaminarViscosity() const {return nSpecies+nDim+8;}
     inline IndexType EddyViscosity() const {return nSpecies+nDim+9;}
 
+    inline IndexType CpTotal() const {return std::numeric_limits<IndexType>::max();}
     inline IndexType ThermalConductivity() const {return std::numeric_limits<IndexType>::max();}
   };
 
diff --git a/SU2_CFD/include/variables/CPrimitiveIndices.hpp b/SU2_CFD/include/variables/CPrimitiveIndices.hpp
index c07643a7139..57fbf7a48ce 100644
--- a/SU2_CFD/include/variables/CPrimitiveIndices.hpp
+++ b/SU2_CFD/include/variables/CPrimitiveIndices.hpp
@@ -28,6 +28,9 @@
 
 #include <cstdint>
 #include <cstring>
+#include <map>
+#include <string>
+
 #include "CEulerVariable.hpp"
 #include "CIncEulerVariable.hpp"
 #include "CNEMOEulerVariable.hpp"
@@ -67,6 +70,9 @@ struct CPrimitiveIndices {
       return reinterpret_cast<const CEulerVariable::template CIndices<IndexType>*>(data_)->NAME();      \
     }                                                                                                   \
   }
+  GET_INDEX_IMPL(NDim)
+  GET_INDEX_IMPL(NSpecies)
+  GET_INDEX_IMPL(SpeciesDensities)
   GET_INDEX_IMPL(Temperature)
   GET_INDEX_IMPL(Velocity)
   GET_INDEX_IMPL(Pressure)
@@ -78,6 +84,7 @@ struct CPrimitiveIndices {
   GET_INDEX_IMPL(ThermalConductivity)
   GET_INDEX_IMPL(CpTotal)
   GET_INDEX_IMPL(Temperature_ve)
+#undef GET_INDEX_IMPL
 
  private:
   template <class ConcreteIndices>
@@ -89,4 +96,37 @@ struct CPrimitiveIndices {
 
   alignas(sizeof(IndexType)) char data_[2 * sizeof(IndexType)]{};  /*!< \brief Space for the largest CIndices class. */
   uint8_t type_;
-};
\ No newline at end of file
+};
+
+/*!
+ * \brief Maps primitive variable names to their indices based on a CPrimitiveIndices object.
+ * \note The variables names we try to map here must be kept in sync with CPrimitiveIndices.
+ * All index classes should use numeric_limits::max for variables that are not available.
+ */
+template <class IndexType>
+std::map<std::string, IndexType> PrimitiveNameToIndexMap(const CPrimitiveIndices<IndexType>& idx) {
+  std::map<std::string, IndexType> nameToIndex;
+  const auto notAvailable = std::numeric_limits<IndexType>::max();
+#define INSERT_VAR_INDEX_PAIR(STRING, FUNCTION) \
+  if (idx.FUNCTION() != notAvailable) nameToIndex[STRING] = idx.FUNCTION();
+  INSERT_VAR_INDEX_PAIR("TEMPERATURE", Temperature)
+  INSERT_VAR_INDEX_PAIR("TEMPERATURE_VE", Temperature_ve)
+  INSERT_VAR_INDEX_PAIR("PRESSURE", Pressure)
+  INSERT_VAR_INDEX_PAIR("DENSITY", Density)
+  INSERT_VAR_INDEX_PAIR("ENTHALPY", Enthalpy)
+  INSERT_VAR_INDEX_PAIR("SOUND_SPEED", SoundSpeed)
+  INSERT_VAR_INDEX_PAIR("LAMINAR_VISCOSITY", LaminarViscosity)
+  INSERT_VAR_INDEX_PAIR("EDDY_VISCOSITY", EddyViscosity)
+  INSERT_VAR_INDEX_PAIR("THERMAL_CONDUCTIVITY", ThermalConductivity)
+  INSERT_VAR_INDEX_PAIR("CP_TOTAL", CpTotal)
+#undef INSERT_VAR_INDEX_PAIR
+  nameToIndex["VELOCITY_X"] = idx.Velocity();
+  nameToIndex["VELOCITY_Y"] = idx.Velocity() + 1;
+  if (idx.NDim() == 3) {
+    nameToIndex["VELOCITY_Z"] = idx.Velocity() + 2;
+  }
+  for (IndexType iSpecies = 0; iSpecies < idx.NSpecies(); ++iSpecies) {
+    nameToIndex["DENSITY_" + std::to_string(iSpecies)] = idx.SpeciesDensities() + iSpecies;
+  }
+  return nameToIndex;
+}
\ No newline at end of file
diff --git a/SU2_CFD/include/variables/CVariable.hpp b/SU2_CFD/include/variables/CVariable.hpp
index f80faebdd10..df6026a71c2 100644
--- a/SU2_CFD/include/variables/CVariable.hpp
+++ b/SU2_CFD/include/variables/CVariable.hpp
@@ -2042,6 +2042,11 @@ class CVariable {
    */
   inline virtual const su2double *GetMesh_Coord(unsigned long iPoint) const { return nullptr; }
 
+  /*!
+   * \brief A virtual member. Get the undeformed coordinates for the entire domain.
+   */
+  inline virtual const MatrixType *GetMesh_Coord() const { return nullptr; }
+
   /*!
    * \brief A virtual member. Set the value of the undeformed coordinates.
    * \param[in] iDim - Index of Mesh_Coord[nDim]
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index b13afb6e27f..c00d02c5456 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -29,6 +29,7 @@
 
 #include "../../../Common/include/geometry/CPhysicalGeometry.hpp"
 #include "../../../Common/include/toolboxes/geometry_toolbox.hpp"
+#include "../../include/variables/CPrimitiveIndices.hpp"
 
 using namespace std;
 
@@ -178,46 +179,6 @@ bool CDriverBase::GetNodeDomain(unsigned long iPoint) const {
   return main_geometry->nodes->GetDomain(iPoint);
 }
 
-vector<passivedouble> CDriverBase::GetInitialCoordinates(unsigned long iPoint) const {
-  if (iPoint >= GetNumberNodes()) {
-    SU2_MPI::Error("Node index exceeds mesh size.", CURRENT_FUNCTION);
-  }
-  vector<passivedouble> values(nDim, 0.0);
-
-  if (main_config->GetDeform_Mesh()) {
-    for (auto iDim = 0u; iDim < nDim; iDim++) {
-      const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord(iPoint, iDim);
-      values[iDim] = SU2_TYPE::GetValue(value);
-    }
-  }
-  return values;
-}
-
-vector<passivedouble> CDriverBase::GetCoordinates(unsigned long iPoint) const {
-  if (iPoint >= GetNumberNodes()) {
-    SU2_MPI::Error("Node index exceeds mesh size.", CURRENT_FUNCTION);
-  }
-  vector<passivedouble> values;
-
-  for (auto iDim = 0u; iDim < nDim; iDim++) {
-    const su2double value = main_geometry->nodes->GetCoord(iPoint, iDim);
-    values.push_back(SU2_TYPE::GetValue(value));
-  }
-  return values;
-}
-
-void CDriverBase::SetCoordinates(unsigned long iPoint, vector<passivedouble> values) {
-  if (iPoint >= GetNumberNodes()) {
-    SU2_MPI::Error("Node index exceeds mesh size.", CURRENT_FUNCTION);
-  }
-  if (values.size() != nDim) {
-    SU2_MPI::Error("Invalid number of dimensions!", CURRENT_FUNCTION);
-  }
-  for (auto iDim = 0u; iDim < nDim; iDim++) {
-    main_geometry->nodes->SetCoord(iPoint, iDim, values[iDim]);
-  }
-}
-
 unsigned short CDriverBase::GetNumberMarkers() const { return main_config->GetnMarker_All(); }
 
 map<string, unsigned short> CDriverBase::GetMarkerIndices() const {
@@ -431,3 +392,24 @@ void CDriverBase::CommunicateMeshDisplacements(void) {
   solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->InitiateComms(main_geometry, main_config, MESH_DISPLACEMENTS);
   solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->CompleteComms(main_geometry, main_config, MESH_DISPLACEMENTS);
 }
+
+map<string, unsigned short> CDriverBase::GetSolverIndices() const {
+  map<string, unsigned short> indexMap;
+  for (auto iSol = 0u; iSol < MAX_SOLS; iSol++) {
+    const auto* solver = solver_container[ZONE_0][INST_0][MESH_0][iSol];
+    if (solver != nullptr) {
+      if (solver->GetSolverName().empty()) SU2_MPI::Error("Solver name was not defined.", CURRENT_FUNCTION);
+      indexMap[solver->GetSolverName()] = iSol;
+    }
+  }
+  return indexMap;
+}
+
+map<string, unsigned short> CDriverBase::GetPrimitiveIndices() const {
+  if (solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL] == nullptr) {
+    SU2_MPI::Error("The flow solver does not exist.", CURRENT_FUNCTION);
+  }
+  return PrimitiveNameToIndexMap(CPrimitiveIndices<unsigned short>(
+      main_config->GetKind_Regime() == ENUM_REGIME::INCOMPRESSIBLE,
+      main_config->GetNEMOProblem(), nDim, main_config->GetnSpecies()));
+}
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index d24bedd03bf..ea62d779f52 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -33,9 +33,7 @@
 #include "../../../Common/include/geometry/CGeometry.hpp"
 #include "../../../Common/include/toolboxes/geometry_toolbox.hpp"
 #include "../../include/solvers/CSolver.hpp"
-#include "../../include/variables/CEulerVariable.hpp"
-#include "../../include/variables/CIncEulerVariable.hpp"
-#include "../../include/variables/CNEMOEulerVariable.hpp"
+#include "../../include/variables/CPrimitiveIndices.hpp"
 #include "../../include/fluid/CCoolProp.hpp"
 
 CFlowOutput::CFlowOutput(const CConfig *config, unsigned short nDim, bool fem_output) :
@@ -747,6 +745,63 @@ void CFlowOutput::SetAnalyzeSurface_SpeciesVariance(const CSolver* const*solver,
   SetHistoryOutputValue("SURFACE_SPECIES_VARIANCE", Tot_Surface_SpeciesVariance);
 }
 
+void CFlowOutput::ConvertVariableSymbolsToIndices(const CPrimitiveIndices<unsigned long>& idx,
+                                                  CustomOutput& output) const {
+  const auto nameToIndex = PrimitiveNameToIndexMap(idx);
+
+  std::stringstream knownVariables;
+  for (const auto& items : nameToIndex) {
+    knownVariables << items.first + '\n';
+  }
+  knownVariables << "TURB[0,1,...]\nRAD[0,1,...]\nSPECIES[0,1,...]\n";
+
+  auto IndexOfVariable = [](const map<std::string, unsigned long>& nameToIndex, const std::string& var) {
+    /*--- Primitives of the flow solver. ---*/
+    const auto flowOffset = FLOW_SOL * CustomOutput::MAX_VARS_PER_SOLVER;
+    const auto it = nameToIndex.find(var);
+    if (it != nameToIndex.end()) return flowOffset + it->second;
+
+    /*--- Index-based (no name) access to variables of other solvers. ---*/
+    auto GetIndex = [](const std::string& s, int nameLen) {
+      /*--- Extract an int from "name[int]", nameLen is the length of "name". ---*/
+      return std::stoi(std::string(s.begin() + nameLen + 1, s.end() - 1));
+    };
+    if (var.rfind("SPECIES", 0) == 0) return SPECIES_SOL * CustomOutput::MAX_VARS_PER_SOLVER + GetIndex(var, 7);
+    if (var.rfind("TURB", 0) == 0) return TURB_SOL * CustomOutput::MAX_VARS_PER_SOLVER + GetIndex(var, 4);
+    if (var.rfind("RAD", 0) == 0) return RAD_SOL * CustomOutput::MAX_VARS_PER_SOLVER + GetIndex(var, 3);
+
+    return CustomOutput::NOT_A_VARIABLE;
+  };
+
+  output.otherOutputs.clear();
+  output.varIndices.clear();
+  output.varIndices.reserve(output.varSymbols.size());
+
+  for (const auto& var : output.varSymbols) {
+    output.varIndices.push_back(IndexOfVariable(nameToIndex, var));
+
+    if (output.type == OperationType::FUNCTION && output.varIndices.back() != CustomOutput::NOT_A_VARIABLE) {
+      SU2_MPI::Error("Custom outputs of type 'Function' cannot reference solver variables.", CURRENT_FUNCTION);
+    }
+    /*--- Symbol is a valid solver variable. ---*/
+    if (output.varIndices.back() < CustomOutput::NOT_A_VARIABLE) continue;
+
+    /*--- An index above NOT_A_VARIABLE is not valid with current solver settings. ---*/
+    if (output.varIndices.back() > CustomOutput::NOT_A_VARIABLE) {
+      SU2_MPI::Error("Inactive solver variable (" + var + ") used in function " + output.name + "\n"
+                      "E.g. this may only be a variable of the compressible solver.", CURRENT_FUNCTION);
+    }
+
+    /*--- An index equal to NOT_A_VARIABLE may refer to a history output. ---*/
+    output.varIndices.back() += output.otherOutputs.size();
+    output.otherOutputs.push_back(GetPtrToHistoryOutput(var));
+    if (output.otherOutputs.back() == nullptr) {
+      SU2_MPI::Error("Invalid history output or solver variable (" + var + ") used in function " + output.name +
+                     "\nValid solvers variables:\n" + knownVariables.str(), CURRENT_FUNCTION);
+    }
+  }
+}
+
 void CFlowOutput::SetCustomOutputs(const CSolver* const* solver, const CGeometry *geometry, const CConfig *config) {
 
   const bool axisymmetric = config->GetAxisymmetric();
@@ -755,17 +810,10 @@ void CFlowOutput::SetCustomOutputs(const CSolver* const* solver, const CGeometry
   for (auto& output : customOutputs) {
     if (output.varIndices.empty()) {
       /*--- Setup indices for the symbols in the expression. ---*/
+      const auto primIdx = CPrimitiveIndices<unsigned long>(config->GetKind_Regime() == ENUM_REGIME::INCOMPRESSIBLE,
+          config->GetNEMOProblem(), nDim, config->GetnSpecies());
+      ConvertVariableSymbolsToIndices(primIdx, output);
 
-      if (config->GetNEMOProblem()) {
-        ConvertVariableSymbolsToIndices(
-            CNEMOEulerVariable::template CIndices<unsigned long>(nDim, config->GetnSpecies()), output);
-      } else if (config->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE) {
-        ConvertVariableSymbolsToIndices(CEulerVariable::template CIndices<unsigned long>(nDim, 0), output);
-      } else if (config->GetKind_Regime() == ENUM_REGIME::INCOMPRESSIBLE) {
-        ConvertVariableSymbolsToIndices(CIncEulerVariable::template CIndices<unsigned long>(nDim, 0), output);
-      } else {
-        SU2_MPI::Error("Unknown flow solver type.", CURRENT_FUNCTION);
-      }
       /*--- Convert marker names to their index (if any) in this rank. Or probe locations to nearest points. ---*/
 
       if (output.type != OperationType::PROBE) {
diff --git a/SU2_CFD/src/solvers/CAdjEulerSolver.cpp b/SU2_CFD/src/solvers/CAdjEulerSolver.cpp
index fde3afc43fa..e16446e7785 100644
--- a/SU2_CFD/src/solvers/CAdjEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CAdjEulerSolver.cpp
@@ -345,6 +345,7 @@ CAdjEulerSolver::CAdjEulerSolver(CGeometry *geometry, CConfig *config, unsigned
   InitiateComms(geometry, config, SOLUTION);
   CompleteComms(geometry, config, SOLUTION);
 
+  SolverName = "ADJ.FLOW";
 }
 
 CAdjEulerSolver::~CAdjEulerSolver(void) {
diff --git a/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp b/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
index 025cb20e82e..e82e61288a2 100644
--- a/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
+++ b/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
@@ -126,6 +126,7 @@ CDiscAdjFEASolver::CDiscAdjFEASolver(CGeometry *geometry, CConfig *config, CSolv
 
   if (fea_dv) ReadDV(config);
 
+  SolverName = "ADJ.FEA";
 }
 
 CDiscAdjFEASolver::~CDiscAdjFEASolver() { delete nodes; }
diff --git a/SU2_CFD/src/solvers/CDiscAdjMeshSolver.cpp b/SU2_CFD/src/solvers/CDiscAdjMeshSolver.cpp
index d676990d8df..ff92a04d544 100644
--- a/SU2_CFD/src/solvers/CDiscAdjMeshSolver.cpp
+++ b/SU2_CFD/src/solvers/CDiscAdjMeshSolver.cpp
@@ -80,6 +80,7 @@ CDiscAdjMeshSolver::CDiscAdjMeshSolver(CGeometry *geometry, CConfig *config, CSo
   }
   static_cast<CDiscAdjMeshBoundVariable*>(nodes)->AllocateBoundaryVariables(config);
 
+  SolverName = "ADJ.MESH";
 }
 
 CDiscAdjMeshSolver::~CDiscAdjMeshSolver() { delete nodes; }
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index f44f76817fa..97fa79e6d15 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -326,7 +326,7 @@ CEulerSolver::CEulerSolver(CGeometry *geometry, CConfig *config,
 
   CommunicateInitialState(geometry, config);
 
-  /*--- Add the solver name (max 8 characters). ---*/
+  /*--- Add the solver name.. ---*/
   SolverName = "C.FLOW";
 
   /*--- Finally, check that the static arrays will be large enough (keep this
diff --git a/SU2_CFD/src/solvers/CFEASolver.cpp b/SU2_CFD/src/solvers/CFEASolver.cpp
index 69b93a180e3..4f30cb91450 100644
--- a/SU2_CFD/src/solvers/CFEASolver.cpp
+++ b/SU2_CFD/src/solvers/CFEASolver.cpp
@@ -211,7 +211,7 @@ CFEASolver::CFEASolver(CGeometry *geometry, CConfig *config) : CFEASolverBase(ge
     Set_VertexEliminationSchedule(geometry, essentialMarkers);
   }
 
-  /*--- Add the solver name (max 8 characters) ---*/
+  /*--- Add the solver name. ---*/
   SolverName = "FEA";
 }
 
diff --git a/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp b/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
index 7acc893e986..1a12467366a 100644
--- a/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
@@ -723,8 +723,8 @@ CFEM_DG_EulerSolver::CFEM_DG_EulerSolver(CGeometry *geometry, CConfig *config, u
      the tasks to be done for one space time step. */
   SetUpTaskList(config);
 
-  /*--- Add the solver name (max 8 characters) ---*/
-  SolverName = "DG FLOW";
+  /*--- Add the solver name. ---*/
+  SolverName = "DG.FLOW";
 }
 
 CFEM_DG_EulerSolver::~CFEM_DG_EulerSolver(void) {
diff --git a/SU2_CFD/src/solvers/CHeatSolver.cpp b/SU2_CFD/src/solvers/CHeatSolver.cpp
index a7a3b1e30d3..aeefcfd75f0 100644
--- a/SU2_CFD/src/solvers/CHeatSolver.cpp
+++ b/SU2_CFD/src/solvers/CHeatSolver.cpp
@@ -167,7 +167,7 @@ CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iM
   Max_CFL_Local = CFL;
   Avg_CFL_Local = CFL;
 
-  /*--- Add the solver name (max 8 characters) ---*/
+  /*--- Add the solver name. ---*/
 
   SolverName = "HEAT";
 }
diff --git a/SU2_CFD/src/solvers/CIncEulerSolver.cpp b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
index 1749ae096f2..19b620825e1 100644
--- a/SU2_CFD/src/solvers/CIncEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
@@ -221,7 +221,7 @@ CIncEulerSolver::CIncEulerSolver(CGeometry *geometry, CConfig *config, unsigned
   if (config->GetBounded_Scalar())
     EdgeMassFluxes.resize(geometry->GetnEdge()) = su2double(0.0);
 
-  /*--- Add the solver name (max 8 characters) ---*/
+  /*--- Add the solver name. ---*/
   SolverName = "INC.FLOW";
 
   /*--- Finally, check that the static arrays will be large enough (keep this
diff --git a/SU2_CFD/src/solvers/CMeshSolver.cpp b/SU2_CFD/src/solvers/CMeshSolver.cpp
index 57b4b25edb7..d9fdecb9f06 100644
--- a/SU2_CFD/src/solvers/CMeshSolver.cpp
+++ b/SU2_CFD/src/solvers/CMeshSolver.cpp
@@ -165,6 +165,8 @@ CMeshSolver::CMeshSolver(CGeometry *geometry, CConfig *config) : CFEASolver(LINE
     }
     Set_VertexEliminationSchedule(geometry, essentialMarkers);
   }
+
+  SolverName = "MESH";
 }
 
 void CMeshSolver::SetMinMaxVolume(CGeometry *geometry, CConfig *config, bool updated) {
diff --git a/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp b/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
index f02f064ff1d..c82685c752a 100644
--- a/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
@@ -216,7 +216,7 @@ CNEMOEulerSolver::CNEMOEulerSolver(CGeometry *geometry, CConfig *config,
 
   CommunicateInitialState(geometry, config);
 
-  /*--- Add the solver name (max 8 characters) ---*/
+  /*--- Add the solver name. ---*/
   SolverName = "NEMO.FLOW";
 
   /*--- Finally, check that the static arrays will be large enough (keep this
diff --git a/SU2_CFD/src/solvers/CRadP1Solver.cpp b/SU2_CFD/src/solvers/CRadP1Solver.cpp
index f25d41fa945..e1f6ef80d1f 100644
--- a/SU2_CFD/src/solvers/CRadP1Solver.cpp
+++ b/SU2_CFD/src/solvers/CRadP1Solver.cpp
@@ -127,6 +127,7 @@ CRadP1Solver::CRadP1Solver(CGeometry* geometry, CConfig *config) : CRadSolver(ge
    SetVolumetricHeatSource(geometry, config);
   }
 
+  SolverName = "RAD";
 }
 
 CRadP1Solver::~CRadP1Solver(void) {
diff --git a/SU2_CFD/src/solvers/CSpeciesSolver.cpp b/SU2_CFD/src/solvers/CSpeciesSolver.cpp
index 690de424eee..16e069ed9bd 100644
--- a/SU2_CFD/src/solvers/CSpeciesSolver.cpp
+++ b/SU2_CFD/src/solvers/CSpeciesSolver.cpp
@@ -167,7 +167,7 @@ CSpeciesSolver::CSpeciesSolver(CGeometry* geometry, CConfig* config, unsigned sh
   Max_CFL_Local = CFL;
   Avg_CFL_Local = CFL;
 
-  /*--- Add the solver name (max 8 characters) ---*/
+  /*--- Add the solver name. ---*/
   SolverName = "SPECIES";
 }
 
diff --git a/SU2_CFD/src/solvers/CTransLMSolver.cpp b/SU2_CFD/src/solvers/CTransLMSolver.cpp
index 209f07c87c8..bd412a283a5 100644
--- a/SU2_CFD/src/solvers/CTransLMSolver.cpp
+++ b/SU2_CFD/src/solvers/CTransLMSolver.cpp
@@ -167,7 +167,7 @@ CTransLMSolver::CTransLMSolver(CGeometry *geometry, CConfig *config, unsigned sh
   Max_CFL_Local = CFL;
   Avg_CFL_Local = CFL;
 
-  /*--- Add the solver name (max 8 characters) ---*/
+  /*--- Add the solver name. ---*/
   SolverName = "LM model";
 
 }
diff --git a/SU2_CFD/src/solvers/CTurbSASolver.cpp b/SU2_CFD/src/solvers/CTurbSASolver.cpp
index adb7ac7c009..a342fa2b3a0 100644
--- a/SU2_CFD/src/solvers/CTurbSASolver.cpp
+++ b/SU2_CFD/src/solvers/CTurbSASolver.cpp
@@ -166,7 +166,7 @@ CTurbSASolver::CTurbSASolver(CGeometry *geometry, CConfig *config, unsigned shor
   Max_CFL_Local = CFL;
   Avg_CFL_Local = CFL;
 
-  /*--- Add the solver name (max 8 characters) ---*/
+  /*--- Add the solver name. ---*/
   SolverName = "SA";
 
 }
diff --git a/SU2_CFD/src/solvers/CTurbSSTSolver.cpp b/SU2_CFD/src/solvers/CTurbSSTSolver.cpp
index f9fdd16dffb..3918c07fba4 100644
--- a/SU2_CFD/src/solvers/CTurbSSTSolver.cpp
+++ b/SU2_CFD/src/solvers/CTurbSSTSolver.cpp
@@ -179,8 +179,8 @@ CTurbSSTSolver::CTurbSSTSolver(CGeometry *geometry, CConfig *config, unsigned sh
   Max_CFL_Local = CFL;
   Avg_CFL_Local = CFL;
 
-  /*--- Add the solver name (max 8 characters) ---*/
-  SolverName = "K-W SST";
+  /*--- Add the solver name. ---*/
+  SolverName = "SST";
 
 }
 
diff --git a/SU2_PY/FSI_tools/FSIInterface.py b/SU2_PY/FSI_tools/FSIInterface.py
index 99bab9afe9a..88c030ff6a0 100644
--- a/SU2_PY/FSI_tools/FSIInterface.py
+++ b/SU2_PY/FSI_tools/FSIInterface.py
@@ -569,10 +569,10 @@ def interfaceMapping(self,FluidSolver, SolidSolver, FSI_config):
             iPoint = FluidSolver.GetMarkerNode(self.fluidInterfaceIdentifier, iVertex)
             GlobalIndex = FluidSolver.GetNodeGlobalIndex(iPoint)
             if self.nDim == 2:
-                posx, posy = FluidSolver.GetInitialCoordinates(iPoint)
+                posx, posy = FluidSolver.InitialCoordinates().Get(iPoint)
                 posz = 0
             else:
-                posx, posy, posz = FluidSolver.GetInitialCoordinates(iPoint)
+                posx, posy, posz = FluidSolver.InitialCoordinates().Get(iPoint)
             if GlobalIndex not in self.FluidHaloNodeList[myid].keys():
               fluidIndexing_temp[GlobalIndex] = self.__getGlobalIndex('fluid', myid, localIndex)
               self.localFluidInterface_array_X_init[localIndex] = posx
diff --git a/SU2_PY/pySU2/pySU2.i b/SU2_PY/pySU2/pySU2.i
index a05049798b7..f783c324335 100644
--- a/SU2_PY/pySU2/pySU2.i
+++ b/SU2_PY/pySU2/pySU2.i
@@ -37,13 +37,13 @@ directors="1",
 threads="1"
 ) pysu2
 %{
+#include "../../Common/include/containers/CPyWrapperMatrixView.hpp"
 #include "../../SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CDriverBase.hpp"
 #include "../../SU2_CFD/include/drivers/CMultizoneDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
 #include "../../SU2_DEF/include/drivers/CDeformationDriver.hpp"
-
 %}
 
 // ----------- USED MODULES ------------
@@ -53,6 +53,7 @@ threads="1"
 
 %include "std_string.i"
 %include "std_vector.i"
+%include "std_pair.i"
 %include "std_map.i"
 %include "typemaps.i"
 //%include "numpy.i"
@@ -65,12 +66,11 @@ namespace std {
    %template() vector<bool>;
    %template() vector<unsigned short>;
    %template() vector<unsigned long>;
-   %template() vector<vector<unsigned long>>;
    %template() vector<double>;
-   %template() vector<vector<double>>;
    %template() vector<string>;
    %template() map<string, unsigned short>;
    %template() map<string, string>;
+   %template() pair<unsigned long, unsigned long>;
 }
 
 // ----------- API CLASSES ----------------
@@ -92,6 +92,7 @@ const unsigned int MESH_1 = 1; /*!< \brief Definition of the finest grid level.
 const unsigned int ZONE_0 = 0; /*!< \brief Definition of the first grid domain. */
 const unsigned int ZONE_1 = 1; /*!< \brief Definition of the first grid domain. */
 
+%include "../../Common/include/containers/CPyWrapperMatrixView.hpp"
 %include "../../SU2_CFD/include/drivers/CDriverBase.hpp"
 %include "../../SU2_CFD/include/drivers/CDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
diff --git a/SU2_PY/pySU2/pySU2ad.i b/SU2_PY/pySU2/pySU2ad.i
index cba62127e92..8bca85fdd2d 100644
--- a/SU2_PY/pySU2/pySU2ad.i
+++ b/SU2_PY/pySU2/pySU2ad.i
@@ -37,13 +37,13 @@ directors="1",
 threads="1"
 ) pysu2ad
 %{
+#include "../../Common/include/containers/CPyWrapperMatrixView.hpp"
 #include "../../SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CDriverBase.hpp"
 #include "../../SU2_CFD/include/drivers/CMultizoneDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
 #include "../../SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp"
-
 %}
 
 // ----------- USED MODULES ------------
@@ -53,6 +53,7 @@ threads="1"
 
 %include "std_string.i"
 %include "std_vector.i"
+%include "std_pair.i"
 %include "std_map.i"
 %include "typemaps.i"
 //%include "numpy.i"
@@ -63,13 +64,13 @@ threads="1"
 
 namespace std {
    %template() vector<bool>;
+   %template() vector<unsigned short>;
    %template() vector<unsigned long>;
-   %template() vector<vector<unsigned long>>;
    %template() vector<double>;
-   %template() vector<vector<double>>;
    %template() vector<string>;
    %template() map<string, unsigned short>;
    %template() map<string, string>;
+   %template() pair<unsigned long, unsigned long>;
 }
 
 // ----------- API CLASSES ----------------
@@ -91,6 +92,7 @@ const unsigned int MESH_1 = 1; /*!< \brief Definition of the finest grid level.
 const unsigned int ZONE_0 = 0; /*!< \brief Definition of the first grid domain. */
 const unsigned int ZONE_1 = 1; /*!< \brief Definition of the first grid domain. */
 
+%include "../../Common/include/containers/CPyWrapperMatrixView.hpp"
 %include "../../SU2_CFD/include/drivers/CDriverBase.hpp"
 %include "../../SU2_CFD/include/drivers/CDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
diff --git a/TestCases/py_wrapper/deforming_bump_in_channel/run.py b/TestCases/py_wrapper/deforming_bump_in_channel/run.py
index dc9a217f35e..80d88987977 100755
--- a/TestCases/py_wrapper/deforming_bump_in_channel/run.py
+++ b/TestCases/py_wrapper/deforming_bump_in_channel/run.py
@@ -52,17 +52,17 @@ def main():
   TimeIter = SU2Driver.GetTime_Iter()
   nTimeIter = SU2Driver.GetnTimeIter()
   time = TimeIter * deltaT
-  
+
   # Extract the initial position of each node on the moving marker.
   CoordX = np.zeros(nVertex)
   CoordY = np.zeros(nVertex)
   for iVertex in range(nVertex):
     iPoint = SU2Driver.GetMarkerNode(MarkerID, iVertex)
-    CoordX[iVertex], CoordY[iVertex] = SU2Driver.GetInitialCoordinates(iPoint)
+    CoordX[iVertex], CoordY[iVertex] = SU2Driver.InitialCoordinates().Get(iPoint)
 
   if rank == 0:
     print("\n------------------------------ Begin Solver -----------------------------\n")
-  
+
   # The time loop is defined in Python so that we have acces to SU2 functionalities at each time step.
   while (TimeIter < nTimeIter):
     # Apply the surface deformation.
@@ -72,12 +72,12 @@ def main():
 
     # Time iteration preprocessing.
     SU2Driver.Preprocess(TimeIter)
-    
+
     # Run one time iteration (e.g. dual-time).
     SU2Driver.Run()
     SU2Driver.Postprocess()
     SU2Driver.Update()
-    
+
     # Monitor the solver and output solution to file if required.
     stopCalc = SU2Driver.Monitor(TimeIter)
     SU2Driver.Output(TimeIter)
diff --git a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
index 37e7a1127f6..718fbfd8cb1 100755
--- a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
+++ b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
@@ -102,7 +102,7 @@ def main():
   CoordY = np.zeros(nVertex_MovingMarker)
   for iVertex in range(nVertex_MovingMarker):
     iPoint = SU2Driver.GetMarkerNode(MovingMarkerID, iVertex)
-    CoordX[iVertex], CoordY[iVertex] = SU2Driver.GetInitialCoordinates(iPoint)
+    CoordX[iVertex], CoordY[iVertex] = SU2Driver.InitialCoordinates().Get(iPoint)
 
   # Time loop is defined in Python so that we have acces to SU2 functionalities at each time step
   if rank == 0:
diff --git a/meson.build b/meson.build
index 84999a5476b..60b30d9ba23 100644
--- a/meson.build
+++ b/meson.build
@@ -202,10 +202,10 @@ elif get_option('enable-openblas')
 endif
 
 if get_option('enable-librom')
-   
+
    assert(get_option('librom_root')!='',
        'Must specify librom folder (-Dlibrom_root=path/to/libROM)')
-   
+
    su2_cpp_args += '-DHAVE_LIBROM'
 
    librom_root = get_option('librom_root')
@@ -292,7 +292,7 @@ message('''---------------------------------------------------------------------
          |   |___/\___//___|   Meson Configuration Summary                       |
          |                                                                       |
          -------------------------------------------------------------------------
-         
+
          Option          Value
          ---------------------
          TecIO:          @2@
@@ -336,7 +336,7 @@ if get_option('enable-librom')
   message(''' To run SU2 with libROM library, add this line to your .bashrc file:
 
           export LD_LIBRARY_PATH=@0@/build/:$LD_LIBRARY_PATH
-          
+
           '''.format(get_option('librom_root')))
 
 endif

From e296613e47328d7cf550c70decbf00637e9ae7a1 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 26 Feb 2023 14:50:12 -0800
Subject: [PATCH 239/656] extra line and update docker images

---
 .github/workflows/regression.yml               | 18 +++++++++---------
 .github/workflows/release-management.yml       |  2 +-
 .../include/variables/CPrimitiveIndices.hpp    |  2 +-
 3 files changed, 11 insertions(+), 11 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index e749e661e70..aeb1c61ce51 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -52,12 +52,12 @@ jobs:
           key: ${{ matrix.config_set }}-${{ github.sha }}
           restore-keys: ${{ matrix.config_set }}
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/build-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/build-su2:230225-2136
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
       - name: Build
-        uses: docker://ghcr.io/su2code/su2/build-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/build-su2:230225-2136
         with:
           args: -b ${{github.ref}} -f "${{matrix.flags}}"
       - name: Compress binaries
@@ -68,7 +68,7 @@ jobs:
           name: ${{ matrix.config_set }}
           path: install_bin.tgz
       - name: Post Cleanup
-        uses: docker://ghcr.io/su2code/su2/build-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/build-su2:230225-2136
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -99,7 +99,7 @@ jobs:
             tag: OMP
     steps:
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -125,12 +125,12 @@ jobs:
           chmod a+x $BIN_FOLDER/*
           ls -lahR $BIN_FOLDER
       - name: Run Tests in Container
-        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
           args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
       - name: Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -151,7 +151,7 @@ jobs:
             tag: MPI
     steps:
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -212,11 +212,11 @@ jobs:
           echo $PWD
           ls -lahR
       - name: Run Unit Tests
-        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           entrypoint: install/bin/${{matrix.testdriver}}
       - name: Post Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
diff --git a/.github/workflows/release-management.yml b/.github/workflows/release-management.yml
index 287ecdb517d..0babf1c46b2 100644
--- a/.github/workflows/release-management.yml
+++ b/.github/workflows/release-management.yml
@@ -35,7 +35,7 @@ jobs:
           key: ${{ matrix.os_bin }}-${{ github.sha }}
           restore-keys: ${{ matrix.os_bin }}
       - name: Build
-        uses: docker://ghcr.io/su2code/su2/build-su2-cross:221224-1158
+        uses: docker://ghcr.io/su2code/su2/build-su2-cross:230225-2136
         with:
           args: -b ${{ github.sha }} -f "${{matrix.flags}}"
       - name: Create Archive
diff --git a/SU2_CFD/include/variables/CPrimitiveIndices.hpp b/SU2_CFD/include/variables/CPrimitiveIndices.hpp
index 57fbf7a48ce..77878eff6cb 100644
--- a/SU2_CFD/include/variables/CPrimitiveIndices.hpp
+++ b/SU2_CFD/include/variables/CPrimitiveIndices.hpp
@@ -129,4 +129,4 @@ std::map<std::string, IndexType> PrimitiveNameToIndexMap(const CPrimitiveIndices
     nameToIndex["DENSITY_" + std::to_string(iSpecies)] = idx.SpeciesDensities() + iSpecies;
   }
   return nameToIndex;
-}
\ No newline at end of file
+}

From 5962016c99245137c724d090249ecffe8b6a997c Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 27 Feb 2023 14:50:38 +0100
Subject: [PATCH 240/656] Improved MLP classes consistency and documentation

---
 .../multilayer_perceptron/CIOMap.hpp          |   8 +-
 .../multilayer_perceptron/CLayer.hpp          |  46 +++--
 .../multilayer_perceptron/CLookUp_ANN.hpp     |  20 +-
 .../multilayer_perceptron/CNeuralNetwork.hpp  | 111 ++++++----
 .../multilayer_perceptron/CNeuron.hpp         |  33 +--
 .../CReadNeuralNetwork.hpp                    |   4 +-
 Common/lib/Makefile.am                        |   1 -
 Common/src/toolboxes/meson.build              |   1 -
 .../multilayer_perceptron/CIOMap.cpp          |  12 +-
 .../multilayer_perceptron/CLayer.cpp          |  15 +-
 .../multilayer_perceptron/CLookUp_ANN.cpp     |  73 ++++---
 .../multilayer_perceptron/CNeuralNetwork.cpp  | 191 ++++++++----------
 .../multilayer_perceptron/CNeuron.cpp         |  34 ----
 .../CReadNeuralNetwork.cpp                    |   4 +-
 Docs/docmain.hpp                              |   8 +-
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp    |   4 +-
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        |  12 +-
 .../CLookUp_ANN_tests.cpp                     |   4 +-
 18 files changed, 277 insertions(+), 304 deletions(-)
 delete mode 100644 Common/src/toolboxes/multilayer_perceptron/CNeuron.cpp

diff --git a/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp b/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
index be4613fcc3b..dfc1b4b508c 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
@@ -2,14 +2,14 @@
  * \file CIOMap.hpp
  * \brief Declaration of input-to-output mapping class for artifical neural networks
  * \author E. Bunschoten
- * \version 7.5.0 "Blackbird"
+ * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public
@@ -98,7 +98,7 @@ class CIOMap
    * \brief Set MLP index in IO map
    * \param[in] iMLP - loaded MLP index
    */
-  void Push_MLP_index(std::size_t iMLP) { MLP_indices.push_back(iMLP); }
+  void PushMLPindex(std::size_t iMLP) { MLP_indices.push_back(iMLP); }
 
   /*!
   * \brief Pair call inputs and outputs with the inputs and outputs of
@@ -177,7 +177,7 @@ class CIOMap
    * \param[in] inputs - call inputs
    * \return Vector with call inputs in the correct order of the loaded MLP
    */
-  su2vector<su2double> GetMLP_Inputs(std::size_t i_Map, su2vector<su2double>& inputs) const {
+  su2vector<su2double> GetMLPInputs(std::size_t i_Map, su2vector<su2double>& inputs) const {
     su2vector<su2double> MLP_input;
     MLP_input.resize(Input_Map[i_Map].size());
 
diff --git a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
index 920b256f156..cbce62c099d 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
@@ -2,14 +2,14 @@
  * \file CLayer.hpp
  * \brief Declaration of artificial neural network interpolation class
  * \author E. Bunschoten
- * \version 7.5.0 "Blackbird"
+ * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public
@@ -37,110 +37,116 @@
 
 namespace MLPToolbox {
 class CLayer {
+  /*!
+   *\class CLayer
+   *\brief This class functions as one of the hidden, input, or output layers in the multi-layer perceptron
+   * class. The CLayer class is used to communicate information (activation function inputs and outputs and gradients)
+   * between the CNeuralNetwork class and the CNeuron class. Currently, only a single activation function
+   * can be applied to the neuron inputs within the layer. 
+   */
  private:
   unsigned long number_of_neurons; /*!< Neuron count in current layer */
-  CNeuron* neurons;                /*!< Array of neurons in current layer */
+  su2vector<CNeuron>neurons;                /*!< Array of neurons in current layer */
   bool is_input;                   /*!< Input layer identifyer */
   std::string activation_type;     /*!< Activation function type applied to the current layer*/
  public:
   CLayer();
   CLayer(unsigned long n_neurons);
-  ~CLayer() { delete[] neurons; }
   /*!
    * \brief Set current layer neuron count
    * \param[in] n_neurons - Number of neurons in this layer
    */
-  void setNNeurons(unsigned long n_neurons);
+  void SetNNeurons(unsigned long n_neurons);
 
   /*!
    * \brief Get the current layer neuron count
    * \return Neuron count
    */
-  unsigned long getNNeurons() const { return number_of_neurons; }
+  unsigned long GetNNeurons() const { return number_of_neurons; }
 
   /*!
    * \brief Define current layer as input layer
    * \param[in] input - input layer identifyer
    */
-  void setInput(bool def) { is_input = def; }
+  void SetInput(bool def) { is_input = def; }
 
   /*!
    * \brief Get input layer identifyer
    * \return input layer identifyer
    */
-  bool isInput() const { return is_input; }
+  bool IsInput() const { return is_input; }
 
   /*!
    * \brief Set the output value of a neuron in the layer
    * \param[in] i_neuron - Neuron index
    * \param[in] output_value - Activation function output
    */
-  void setOutput(std::size_t i_neuron, su2double value) { neurons[i_neuron].setOutput(value); }
+  void SetOutput(std::size_t i_neuron, su2double value) { neurons[i_neuron].SetOutput(value); }
 
   /*!
    * \brief Get the output value of a neuron in the layer
    * \param[in] i_neuron - Neuron index
    * \return Neuron output value
    */
-  su2double getOutput(std::size_t i_neuron) const { return neurons[i_neuron].getOutput(); }
+  su2double GetOutput(std::size_t i_neuron) const { return neurons[i_neuron].GetOutput(); }
 
   /*!
    * \brief Set the input value of a neuron in the layer
    * \param[in] i_neuron - Neuron index
    * \param[in] input_value - Activation function input
    */
-  void setInput(std::size_t i_neuron, su2double value) { neurons[i_neuron].setInput(value); }
+  void SetInput(std::size_t i_neuron, su2double value) { neurons[i_neuron].SetInput(value); }
 
   /*!
    * \brief Get the input value of a neuron in the layer
    * \param[in] i_neuron - Neuron index
    * \return Neuron input value
    */
-  su2double getInput(std::size_t i_neuron) const { return neurons[i_neuron].getInput(); }
+  su2double GetInput(std::size_t i_neuron) const { return neurons[i_neuron].GetInput(); }
 
   /*!
    * \brief Set the bias value of a neuron in the layer
    * \param[in] i_neuron - Neuron index
    * \param[in] bias_value - Bias value
    */
-  void setBias(std::size_t i_neuron, su2double value) { neurons[i_neuron].setBias(value); }
+  void SetBias(std::size_t i_neuron, su2double value) { neurons[i_neuron].SetBias(value); }
 
   /*!
    * \brief Get the bias value of a neuron in the layer
    * \param[in] i_neuron - Neuron index
    * \return Neuron bias value
    */
-  su2double getBias(std::size_t i_neuron) const { return neurons[i_neuron].getBias(); }
+  su2double GetBias(std::size_t i_neuron) const { return neurons[i_neuron].GetBias(); }
 
   /*!
    * \brief Get the output-input gradient of a neuron in the layer
    * \param[in] i_neuron - Neuron index
    * \return Gradient of neuron output wrt input
    */
-  su2double getdYdX(std::size_t i_neuron, std::size_t iInput) const { return neurons[i_neuron].getGradient(iInput); }
+  su2double GetdYdX(std::size_t i_neuron, std::size_t iInput) const { return neurons[i_neuron].GetGradient(iInput); }
 
   /*!
    * \brief Get the output-input gradient of a neuron in the layer
    * \param[in] i_neuron - Neuron index
    * \return Gradient of neuron output wrt input
    */
-  void setdYdX(std::size_t i_neuron, std::size_t iInput, su2double dy_dx) {
-    neurons[i_neuron].setGradient(iInput, dy_dx);
+  void SetdYdX(std::size_t i_neuron, std::size_t iInput, su2double dy_dx) {
+    neurons[i_neuron].SetGradient(iInput, dy_dx);
   }
 
   /*!
    * \brief Size neuron output derivative wrt network inputs.
    * \param[in] nInputs - Number of network inputs.
    */
-  void sizeGradients(std::size_t nInputs) {
-    for (auto iNeuron = 0u; iNeuron < number_of_neurons; iNeuron++) neurons[iNeuron].sizeGradient(nInputs);
+  void SizeGradients(std::size_t nInputs) {
+    for (auto iNeuron = 0u; iNeuron < number_of_neurons; iNeuron++) neurons[iNeuron].SizeGradient(nInputs);
   }
 
   /*!
    * \brief Get the activation function name applied to this layer
    * \return name of the activation function
    */
-  string getActivationType() const { return activation_type; }
+  string GetActivationType() const { return activation_type; }
 };
 
 }  // namespace MLPToolbox
diff --git a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
index f17c52a92d3..d68ef0893f2 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
@@ -2,14 +2,14 @@
  * \file CLookUp_ANN.hpp
  * \brief Declaration of artificial neural network interpolation class
  * \author E. Bunschoten
- * \version 7.5.0 "Blackbird"
+ * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public
@@ -54,7 +54,7 @@ class CLookUp_ANN {
 
  private:
   int rank{0};
-  su2vector<CNeuralNetwork*> NeuralNetworks; /*!< std::vector containing all loaded neural networks. */
+  su2vector<CNeuralNetwork> NeuralNetworks; /*!< std::vector containing all loaded neural networks. */
 
   unsigned short number_of_variables; /*!< Number of loaded ANNs. */
 
@@ -63,7 +63,7 @@ class CLookUp_ANN {
    * \param[in] ANN - pointer to target NeuralNetwork class
    * \param[in] filename - filename containing ANN architecture information
    */
-  void GenerateANN(CNeuralNetwork* ANN, std::string filename);
+  void GenerateANN(CNeuralNetwork &ANN, std::string filename);
 
  public:
   /*!
@@ -80,11 +80,7 @@ class CLookUp_ANN {
    * \param[in] outputs - pointers to output variables
    * \returns Within output normalization range.
    */
-  unsigned long Predict_ANN(CIOMap* input_output_map, su2vector<su2double>& inputs, su2vector<su2double*>& outputs);
-
-  ~CLookUp_ANN() {
-    for (std::size_t i_ANN = 0; i_ANN < number_of_variables; i_ANN++) delete NeuralNetworks[i_ANN];
-  };
+  unsigned long PredictANN(CIOMap* input_output_map, su2vector<su2double>& inputs, su2vector<su2double*>& outputs);
 
   /*!
    * \brief Get number of loaded ANNs
@@ -97,14 +93,14 @@ class CLookUp_ANN {
    * \param[in] output_names - output variable names to check
    * \param[in] input_output_map - pointer to input-output map to be checked
    */
-  bool Check_Use_of_Outputs(su2vector<std::string>& output_names, CIOMap* input_output_map) const;
+  bool CheckUseOfOutputs(su2vector<std::string>& output_names, CIOMap* input_output_map) const;
 
   /*!
    * \brief Check if all input variables are present in the loaded ANNs
    * \param[in] input_names - input variable names to check
    * \param[in] input_output_map - pointer to input-output map to be checked
    */
-  bool Check_Use_of_Inputs(su2vector<std::string>& input_names, CIOMap* input_output_map) const;
+  bool CheckUseOfInputs(su2vector<std::string>& input_names, CIOMap* input_output_map) const;
 
   /*!
    * \brief Map variable names to ANN inputs or outputs
@@ -112,7 +108,7 @@ class CLookUp_ANN {
    * \param[in] variable_names - variable names to map to ANN inputs or outputs
    * \param[in] input - map to inputs (true) or outputs (false)
    */
-  std::vector<pair<std::size_t, std::size_t>> FindVariable_Indices(std::size_t i_ANN,
+  std::vector<pair<std::size_t, std::size_t>> FindVariableIndices(std::size_t i_ANN,
                                                                    su2vector<std::string> variable_names,
                                                                    bool input) const;
 };
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
index 42b900783ef..8c8c7a3edcc 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
@@ -2,14 +2,14 @@
  * \file CNeuralNetwork.hpp
  * \brief Declaration of the neural network class
  * \author E.C.Bunschoten
- * \version 7.5.0 "Blackbird"
+ * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public
@@ -32,38 +32,50 @@
 #include <cstring>
 #include <iostream>
 #include <limits>
+#include <map>
 
 #include "../../CConfig.hpp"
 #include "../../linear_algebra/blas_structure.hpp"
 #include "CLayer.hpp"
 
+
 namespace MLPToolbox {
 class CNeuralNetwork {
+  /*!
+   *\class CNeuralNetwork
+   *\brief The CNeuralNetwork class allows for the evaluation of a loaded MLP architecture for
+   * a given set of inputs. The class also contains a list of the various supported activation
+   * function types (linear, relu, elu, gelu, selu, sigmoid, swish, tanh, exp)which can be 
+   * applied to the layers in the network. Currently, only dense, feed-forward type neural 
+   * nets are supported in this implementation. 
+   */
  private:
-  su2vector<std::string> input_names,  // MLP input variable names.
-      output_names;                    // MLP output variable names.
+  su2vector<std::string> input_names,  /*!< MLP input variable names. */
+      output_names;                    /*!< MLP output variable names. */
 
-  unsigned long n_hidden_layers = 0;  // Number of hidden layers (layers between input and output layer).
+  unsigned long n_hidden_layers = 0;  /*!< Number of hidden layers (layers between input and output layer). */
 
-  CLayer *inputLayer = nullptr,  // Pointer to network input layer.
-      *outputLayer = nullptr;    // Pointer to network output layer.
+  CLayer *inputLayer = nullptr,  /*!< Pointer to network input layer. */
+      *outputLayer = nullptr;    /*!< Pointer to network output layer. */
 
-  std::vector<CLayer*> hiddenLayers;  // Hidden layer collection.
-  su2vector<CLayer*> total_layers;    // Hidden layers plus in/output layers
+  std::vector<CLayer*> hiddenLayers;  /*!< Hidden layer collection. */
+  su2vector<CLayer*> total_layers;    /*!< Hidden layers plus in/output layers */
 
-  su2vector<su2activematrix> weights_mat;  // Weights of synapses connecting layers
+  su2vector<su2activematrix> weights_mat;  /*!< Weights of synapses connecting layers */
 
-  su2vector<std::pair<su2double, su2double>> input_norm,  // Normalization factors for network inputs
-      output_norm;                                        // Normalization factors for network outputs
+  su2vector<std::pair<su2double, su2double>> input_norm,  /*!< Normalization factors for network inputs */ 
+      output_norm;                                        /*!< Normalization factors for network outputs */
 
-  su2vector<su2double> last_inputs;  // Inputs from previous lookup operation. Evaluation of the network
-                                     // is skipped if current inputs are the same as the last inputs.
+  su2vector<su2double> last_inputs;  /*!< Inputs from previous lookup operation. Evaluation of the network */
+                                     /*!< is skipped if current inputs are the same as the last inputs. */
 
-  su2double* ANN_outputs;                 // Pointer to network outputs
-  su2matrix<su2double> dOutputs_dInputs;  // Network output derivatives w.r.t inputs
+  su2double* ANN_outputs;                 /*!< Pointer to network outputs */
+  su2matrix<su2double> dOutputs_dInputs;  /*!< Network output derivatives w.r.t inputs */
 
-  /*--- Activation function types that are currently supported ---*/
-  enum ENUM_ACTIVATION_FUNCTION {
+  /*!
+   * \brief Available activation function enumeration.
+  */
+  enum class ENUM_ACTIVATION_FUNCTION {
     NONE = 0,
     LINEAR = 1,
     RELU = 2,
@@ -75,8 +87,25 @@ class CNeuralNetwork {
     TANH = 8,
     EXPONENTIAL = 9
   };
-  su2vector<ENUM_ACTIVATION_FUNCTION> activation_function_types;
-  su2vector<string> activation_function_names;
+
+  /*!
+   * \brief Available activation function map.
+  */
+  std::map<std::string, ENUM_ACTIVATION_FUNCTION> activation_function_map {
+    {"none", ENUM_ACTIVATION_FUNCTION::NONE},
+    {"linear", ENUM_ACTIVATION_FUNCTION::LINEAR},
+    {"relu", ENUM_ACTIVATION_FUNCTION::RELU},
+    {"gelu", ENUM_ACTIVATION_FUNCTION::GELU},
+    {"selu", ENUM_ACTIVATION_FUNCTION::SELU},
+    {"sigmoid", ENUM_ACTIVATION_FUNCTION::SIGMOID},
+    {"swish", ENUM_ACTIVATION_FUNCTION::SWISH},
+    {"tanh", ENUM_ACTIVATION_FUNCTION::TANH},
+    {"exponential", ENUM_ACTIVATION_FUNCTION::EXPONENTIAL}
+  };
+
+  su2vector<ENUM_ACTIVATION_FUNCTION> activation_function_types; /*!< Activation function type for each layer in the network. */
+  su2vector<string> activation_function_names;  /*!< Activation function name for each layer in the network. */
+
  public:
   ~CNeuralNetwork() {
     delete inputLayer;
@@ -90,19 +119,19 @@ class CNeuralNetwork {
    * \brief Set the input layer of the network.
    * \param[in] n_neurons - Number of inputs
    */
-  void defineInputLayer(unsigned long n_neurons);
+  void DefineInputLayer(unsigned long n_neurons);
 
   /*!
    * \brief Set the output layer of the network.
    * \param[in] n_neurons - Number of outputs
    */
-  void defineOutputLayer(unsigned long n_neurons);
+  void DefineOutputLayer(unsigned long n_neurons);
 
   /*!
    * \brief Add a hidden layer to the network
    * \param[in] n_neurons - Hidden layer size.
    */
-  void push_hidden_layer(unsigned long n_neurons);
+  void PushHiddenLayer(unsigned long n_neurons);
 
   /*!
    * \brief Set the weight value of a specific synapse.
@@ -111,7 +140,7 @@ class CNeuralNetwork {
    * \param[in] j_neuron - neuron index of connecting neuron.
    * \param[in] value - weight value.
    */
-  void setWeight(unsigned long i_layer, unsigned long i_neuron, unsigned long j_neuron, su2double value) {
+  void SetWeight(unsigned long i_layer, unsigned long i_neuron, unsigned long j_neuron, su2double value) {
     weights_mat[i_layer][j_neuron][i_neuron] = value;
   };
 
@@ -121,8 +150,8 @@ class CNeuralNetwork {
    * \param[in] i_neuron - Neuron index of current layer.
    * \param[in] value - Bias value.
    */
-  void setBias(unsigned long i_layer, unsigned long i_neuron, su2double value) {
-    total_layers[i_layer]->setBias(i_neuron, value);
+  void SetBias(unsigned long i_layer, unsigned long i_neuron, su2double value) {
+    total_layers[i_layer]->SetBias(i_neuron, value);
   }
 
   /*!
@@ -130,23 +159,23 @@ class CNeuralNetwork {
    * \param[in] i_layer - Layer index.
    * \param[in] input - Activation function name.
    */
-  void setActivationFunction(unsigned long i_layer, std::string input);
+  void SetActivationFunction(unsigned long i_layer, std::string input);
 
   /*!
    * \brief Display the network architecture in the terminal.
    */
-  void displayNetwork() const;
+  void DisplayNetwork() const;
 
   /*!
    * \brief Size the weight layers in the network according to its architecture.
    */
-  void sizeWeights();
+  void SizeWeights();
 
   /*!
    * \brief Size the vector of previous inputs.
    * \param[in] n_inputs - Number of inputs.
    */
-  void sizeInputs(unsigned long n_inputs) {
+  void SizeInputs(unsigned long n_inputs) {
     last_inputs.resize(n_inputs);
     for (unsigned long iInput = 0; iInput < n_inputs; iInput++) last_inputs[iInput] = 0.0;
   }
@@ -155,27 +184,27 @@ class CNeuralNetwork {
    * \brief Get the number of connecting regions in the network.
    * \returns number of spaces in between layers.
    */
-  unsigned long getNWeightLayers() const { return total_layers.size() - 1; }
+  unsigned long GetNWeightLayers() const { return total_layers.size() - 1; }
 
   /*!
    * \brief Get the total number of layers in the network
    * \returns number of netowork layers.
    */
-  unsigned long getNLayers() const { return total_layers.size(); }
+  unsigned long GetNLayers() const { return total_layers.size(); }
 
   /*!
    * \brief Get neuron count in a layer.
    * \param[in] iLayer - Layer index.
    * \returns number of neurons in the layer.
    */
-  unsigned long getNNeurons(unsigned long iLayer) const { return total_layers[iLayer]->getNNeurons(); }
+  unsigned long GetNNeurons(unsigned long iLayer) const { return total_layers[iLayer]->GetNNeurons(); }
 
   /*!
    * \brief Evaluate the network.
    * \param[in] inputs - Network input variable values.
    * \param[in] compute_gradient - Compute the derivatives of the outputs wrt inputs.
    */
-  void predict(su2vector<su2double>& inputs, bool compute_gradient = false);
+  void Predict(su2vector<su2double>& inputs, bool compute_gradient = false);
 
   /*!
    * \brief Set the normalization factors for the input layer
@@ -243,7 +272,7 @@ class CNeuralNetwork {
    * \param[in] iOutput - output index.
    * \returns Prediction value.
    */
-  su2double GetANN_Output(std::size_t iOutput) const { return ANN_outputs[iOutput]; }
+  su2double GetANNOutput(std::size_t iOutput) const { return ANN_outputs[iOutput]; }
 
   /*!
    * \brief Get network output derivative w.r.t specific input.
@@ -251,7 +280,7 @@ class CNeuralNetwork {
    * \param[in] iInput - input variable index.
    * \returns Output derivative w.r.t input.
    */
-  su2double GetANN_Output_Input_Derivative(std::size_t iOutput, std::size_t iInput) const {
+  su2double GetdOutputdInput(std::size_t iOutput, std::size_t iInput) const {
     return dOutputs_dInputs[iOutput][iInput];
   }
 
@@ -272,17 +301,17 @@ class CNeuralNetwork {
    */
   su2double ComputeX(std::size_t iLayer, std::size_t iNeuron) const {
     su2double x;
-    x = total_layers[iLayer]->getBias(iNeuron);
-    std::size_t nNeurons_previous = total_layers[iLayer - 1]->getNNeurons();
+    x = total_layers[iLayer]->GetBias(iNeuron);
+    std::size_t nNeurons_previous = total_layers[iLayer - 1]->GetNNeurons();
     for (std::size_t jNeuron = 0; jNeuron < nNeurons_previous; jNeuron++) {
-      x += weights_mat[iLayer - 1][iNeuron][jNeuron] * total_layers[iLayer - 1]->getOutput(jNeuron);
+      x += weights_mat[iLayer - 1][iNeuron][jNeuron] * total_layers[iLayer - 1]->GetOutput(jNeuron);
     }
     return x;
   }
   su2double ComputedOutputdInput(std::size_t iLayer, std::size_t iNeuron, std::size_t iInput) const {
     su2double doutput_dinput = 0;
-    for (auto jNeuron = 0u; jNeuron < total_layers[iLayer - 1]->getNNeurons(); jNeuron++) {
-      doutput_dinput += weights_mat[iLayer - 1][iNeuron][jNeuron] * total_layers[iLayer - 1]->getdYdX(jNeuron, iInput);
+    for (auto jNeuron = 0u; jNeuron < total_layers[iLayer - 1]->GetNNeurons(); jNeuron++) {
+      doutput_dinput += weights_mat[iLayer - 1][iNeuron][jNeuron] * total_layers[iLayer - 1]->GetdYdX(jNeuron, iInput);
     }
     return doutput_dinput;
   }
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
index 0a709a97b84..7aab3fbf5e5 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
@@ -2,14 +2,14 @@
  * \file CNeuron.hpp
  * \brief Declaration of artificial neural network perceptron class
  * \author E. Bunschoten
- * \version 7.5.0 "Blackbird"
+ * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public
@@ -35,6 +35,13 @@
 
 namespace MLPToolbox {
 class CNeuron {
+  /*!
+   *\class CNeuron
+   *\brief This class functions as a neuron within the CLayer class, making up the 
+   * CNeuralNetwork class. The CNeuron class functions as a location to store activation
+   * function inputs and outputs, as well as gradients and biases. These are accessed
+   * through the CLayer class for network evalution operations.
+   */
  private:
   unsigned long i_neuron; /*!< Neuron identification number */
   su2double output{0},    /*!< Output value of the current neuron */
@@ -48,67 +55,67 @@ class CNeuron {
    * \brief Set neuron identification number
    * \param[in] input - Identification number
    */
-  void setNumber(unsigned long input) { i_neuron = input; }
+  void SetNumber(unsigned long input) { i_neuron = input; }
 
   /*!
    * \brief Get neuron identification number
    * \return Identification number
    */
-  unsigned long getNumber() const { return i_neuron; }
+  unsigned long GetNumber() const { return i_neuron; }
 
   /*!
    * \brief Set neuron output value
    * \param[in] input - activation function output value
    */
-  void setOutput(su2double input) { output = input; }
+  void SetOutput(su2double input) { output = input; }
 
   /*!
    * \brief Get neuron output value
    * \return Output value
    */
-  su2double getOutput() const { return output; }
+  su2double GetOutput() const { return output; }
 
   /*!
    * \brief Set neuron input value
    * \param[in] input - activation function input value
    */
-  void setInput(su2double x) { input = x; }
+  void SetInput(su2double x) { input = x; }
 
   /*!
    * \brief Get neuron input value
    * \return input value
    */
-  su2double getInput() const { return input; }
+  su2double GetInput() const { return input; }
 
   /*!
    * \brief Set neuron bias
    * \param[in] input - bias value
    */
-  void setBias(su2double input) { bias = input; }
+  void SetBias(su2double input) { bias = input; }
 
   /*!
    * \brief Get neuron bias value
    * \return bias value
    */
-  su2double getBias() const { return bias; }
+  su2double GetBias() const { return bias; }
 
   /*!
    * \brief Size the derivative of the neuron output wrt MLP inputs.
    * \param[in] nInputs - Number of MLP inputs.
    */
-  void sizeGradient(std::size_t nInputs) { doutput_dinputs.resize(nInputs); }
+  void SizeGradient(std::size_t nInputs) { doutput_dinputs.resize(nInputs); }
 
   /*!
    * \brief Set neuron output gradient with respect to its input value
    * \param[in] input - Derivative of activation function with respect to input
    */
-  void setGradient(std::size_t iInput, su2double input) { doutput_dinputs[iInput] = input; }
+  void SetGradient(std::size_t iInput, su2double input) { doutput_dinputs[iInput] = input; }
 
   /*!
    * \brief Get neuron output gradient with respect to input value
    * \return output gradient wrt input value
    */
-  su2double getGradient(std::size_t iInput) const { return doutput_dinputs[iInput]; }
+  su2double GetGradient(std::size_t iInput) const { return doutput_dinputs[iInput]; }
 };
 
 }  // namespace MLPToolbox
\ No newline at end of file
diff --git a/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
index e9f930032bb..6cca01fb9dd 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
@@ -2,14 +2,14 @@
  * \file CReadNeuralNetwork.hpp
  * \brief Declaration of MLP input file reader class
  * \author E. Bunschoten
- * \version 7.5.0 "Blackbird"
+ * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public
diff --git a/Common/lib/Makefile.am b/Common/lib/Makefile.am
index 06f84826292..62f7d0faace 100644
--- a/Common/lib/Makefile.am
+++ b/Common/lib/Makefile.am
@@ -132,7 +132,6 @@ lib_sources = \
   ../src/toolboxes/multilayer_perceptron/CIOMap.cpp\
   ../src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp\
   ../src/toolboxes/multilayer_perceptron/CLayer.cpp\
-  ../src/toolboxes/multilayer_perceptron/CNeuron.cpp\
   ../src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp\
   ../src/linear_algebra/CSysVector.cpp \
   ../src/linear_algebra/CSysMatrix.cpp \
diff --git a/Common/src/toolboxes/meson.build b/Common/src/toolboxes/meson.build
index d6441390a57..4c6d76c0b1c 100644
--- a/Common/src/toolboxes/meson.build
+++ b/Common/src/toolboxes/meson.build
@@ -10,6 +10,5 @@ common_src += files(['multilayer_perceptron/CLookUp_ANN.cpp',
                      'multilayer_perceptron/CIOMap.cpp',
                      'multilayer_perceptron/CNeuralNetwork.cpp',
                      'multilayer_perceptron/CLayer.cpp',
-                     'multilayer_perceptron/CNeuron.cpp',
                      'multilayer_perceptron/CReadNeuralNetwork.cpp'])
 
diff --git a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
index 1f48f6f5292..4d28c65fff0 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
@@ -3,14 +3,14 @@
  * \brief Implementation of the input-output mapping class for the
  *      use of multi-layer perceptrons in SU2
  * \author E. Bunschoten
- * \version 7.5.0 "Blackbird"
+ * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public
@@ -46,10 +46,10 @@ MLPToolbox::CIOMap::CIOMap(CLookUp_ANN* MLP_collection, su2vector<std::string>&
   // Perform checks on input-output validity
   if (outputs.size() > 0) {
     // Check wether all call inputs are used
-    MLP_collection->Check_Use_of_Inputs(inputs, this);
+    MLP_collection->CheckUseOfInputs(inputs, this);
 
     // Check wether all call outputs are present in the MLP collection
-    MLP_collection->Check_Use_of_Outputs(outputs, this);
+    MLP_collection->CheckUseOfOutputs(outputs, this);
   }
 }
 void MLPToolbox::CIOMap::PairVariableswithMLPs(CLookUp_ANN* MLP_collection, su2vector<std::string>& inputs,
@@ -62,13 +62,13 @@ void MLPToolbox::CIOMap::PairVariableswithMLPs(CLookUp_ANN* MLP_collection, su2v
   // Looping over the loaded MLPs to check wether the MLP inputs match with the call inputs
   for (size_t iMLP = 0; iMLP < MLP_collection->GetNANNs(); iMLP++) {
     // Mapped call inputs to MLP inputs
-    std::vector<pair<size_t, size_t>> Input_Indices = MLP_collection->FindVariable_Indices(iMLP, inputs, true);
+    std::vector<pair<size_t, size_t>> Input_Indices = MLP_collection->FindVariableIndices(iMLP, inputs, true);
     isInput = Input_Indices.size() > 0;
 
     if (isInput) {
       // Only when the MLP inputs match with a portion of the call inputs are the output variable checks performed
 
-      std::vector<pair<size_t, size_t>> Output_Indices = MLP_collection->FindVariable_Indices(iMLP, outputs, false);
+      std::vector<pair<size_t, size_t>> Output_Indices = MLP_collection->FindVariableIndices(iMLP, outputs, false);
       isOutput = Output_Indices.size() > 0;
 
       if (isOutput) {
diff --git a/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp b/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp
index 82da5aa6a50..16282a23809 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp
@@ -3,14 +3,14 @@
  * \brief Implementation of the Layer class to be used in the NeuralNetwork
  *      class
  * \author E. Bunschoten
- * \version 7.5.0 "Blackbird"
+ * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public
@@ -33,18 +33,17 @@ using namespace std;
 MLPToolbox::CLayer::CLayer() : CLayer(1) {}
 
 MLPToolbox::CLayer::CLayer(unsigned long n_neurons) : number_of_neurons{n_neurons}, is_input{false} {
-  neurons = new CNeuron[n_neurons];
+  neurons.resize(n_neurons);
   for (size_t i = 0; i < number_of_neurons; i++) {
-    neurons[i].setNumber(i + 1);
+    neurons[i].SetNumber(i + 1);
   }
 }
 
-void MLPToolbox::CLayer::setNNeurons(unsigned long n_neurons) {
+void MLPToolbox::CLayer::SetNNeurons(unsigned long n_neurons) {
   if (number_of_neurons != n_neurons) {
-    delete[] neurons;
-    neurons = new CNeuron[n_neurons];
+    neurons.resize(n_neurons);
     for (size_t i = 0; i < number_of_neurons; i++) {
-      neurons[i].setNumber(i + 1);
+      neurons[i].SetNumber(i + 1);
     }
   }
 }
\ No newline at end of file
diff --git a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
index 496edc4d708..662498fc405 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
@@ -3,14 +3,14 @@
  * \brief Implementation of the multi-layer perceptron class to be
  *      used for look-up operations.
  * \author E.C.Bunschoten
- * \version 7.5.0 "Blackbird"
+ * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public
@@ -53,25 +53,24 @@ MLPToolbox::CLookUp_ANN::CLookUp_ANN(const unsigned short n_inputs, const string
   cout << "+------------------------------------------------------------------+" << endl;
   
   for (auto i_MLP = 0u; i_MLP < n_inputs; i_MLP++) {
-    NeuralNetworks[i_MLP] = new CNeuralNetwork;
     if (rank == MASTER_NODE) cout << "Generating neural network for " << input_filenames[i_MLP] << endl;
     GenerateANN(NeuralNetworks[i_MLP], input_filenames[i_MLP]);
-    if (rank == MASTER_NODE) NeuralNetworks[i_MLP]->displayNetwork();
+    if (rank == MASTER_NODE) NeuralNetworks[i_MLP].DisplayNetwork();
   }
 }
 
-vector<pair<size_t, size_t>> MLPToolbox::CLookUp_ANN::FindVariable_Indices(size_t i_ANN,
+vector<pair<size_t, size_t>> MLPToolbox::CLookUp_ANN::FindVariableIndices(size_t i_ANN,
                                                                            su2vector<string> variable_names,
                                                                            bool input) const {
   /*--- Find loaded MLPs that have the same input variable names as the variables listed in variable_names ---*/
 
   vector<pair<size_t, size_t>> variable_indices;
-  auto nVar = input ? NeuralNetworks[i_ANN]->GetnInputs() : NeuralNetworks[i_ANN]->GetnOutputs();
+  auto nVar = input ? NeuralNetworks[i_ANN].GetnInputs() : NeuralNetworks[i_ANN].GetnOutputs();
 
   for (auto iVar = 0u; iVar < nVar; iVar++) {
     for (auto jVar = 0u; jVar < variable_names.size(); jVar++) {
       string ANN_varname =
-          input ? NeuralNetworks[i_ANN]->GetInputName(iVar) : NeuralNetworks[i_ANN]->GetOutputName(iVar);
+          input ? NeuralNetworks[i_ANN].GetInputName(iVar) : NeuralNetworks[i_ANN].GetOutputName(iVar);
       if (variable_names[jVar].compare(ANN_varname) == 0) {
         variable_indices.push_back(make_pair(jVar, iVar));
       }
@@ -80,7 +79,7 @@ vector<pair<size_t, size_t>> MLPToolbox::CLookUp_ANN::FindVariable_Indices(size_
   return variable_indices;
 }
 
-unsigned long MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap* input_output_map, su2vector<su2double>& inputs,
+unsigned long MLPToolbox::CLookUp_ANN::PredictANN(CIOMap* input_output_map, su2vector<su2double>& inputs,
                                                    su2vector<su2double*>& outputs) {
   /*--- Evaluate MLP based on target input and output variables ---*/
   bool within_range,              // Within MLP training set range.
@@ -94,11 +93,11 @@ unsigned long MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap* input_output_map, su2
   for (auto i_map = 0u; i_map < input_output_map->GetNMLPs(); i_map++) {
     within_range = true;
     auto i_ANN = input_output_map->GetMLPIndex(i_map);
-    auto ANN_inputs = input_output_map->GetMLP_Inputs(i_map, inputs);
+    auto ANN_inputs = input_output_map->GetMLPInputs(i_map, inputs);
 
     su2double distance_to_query_i = 0;
     for (auto i_input = 0u; i_input < ANN_inputs.size(); i_input++) {
-      auto ANN_input_limits = NeuralNetworks[i_ANN]->GetInputNorm(i_input);
+      auto ANN_input_limits = NeuralNetworks[i_ANN].GetInputNorm(i_input);
 
       /* Check if query input lies outside MLP training range */
       if ((ANN_inputs[i_input] < ANN_input_limits.first) || (ANN_inputs[i_input] > ANN_input_limits.second)) {
@@ -113,11 +112,11 @@ unsigned long MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap* input_output_map, su2
 
     /* Evaluate MLP when query inputs lie within training data range */
     if (within_range) {
-      NeuralNetworks[i_ANN]->predict(ANN_inputs);
+      NeuralNetworks[i_ANN].Predict(ANN_inputs);
       MLP_was_evaluated = true;
       for (auto i = 0u; i < input_output_map->GetNMappedOutputs(i_map); i++) {
         *outputs[input_output_map->GetOutputIndex(i_map, i)] =
-            NeuralNetworks[i_ANN]->GetANN_Output(input_output_map->GetMLPOutputIndex(i_map, i));
+            NeuralNetworks[i_ANN].GetANNOutput(input_output_map->GetMLPOutputIndex(i_map, i));
       }
     }
 
@@ -130,11 +129,11 @@ unsigned long MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap* input_output_map, su2
   }
   /* Evaluate nearest MLP in case no query data within range is found */
   if (!MLP_was_evaluated) {
-    auto ANN_inputs = input_output_map->GetMLP_Inputs(i_map_nearest, inputs);
-    NeuralNetworks[i_ANN_nearest]->predict(ANN_inputs);
+    auto ANN_inputs = input_output_map->GetMLPInputs(i_map_nearest, inputs);
+    NeuralNetworks[i_ANN_nearest].Predict(ANN_inputs);
     for (auto i = 0u; i < input_output_map->GetNMappedOutputs(i_map_nearest); i++) {
       *outputs[input_output_map->GetOutputIndex(i_map_nearest, i)] =
-          NeuralNetworks[i_ANN_nearest]->GetANN_Output(input_output_map->GetMLPOutputIndex(i_map_nearest, i));
+          NeuralNetworks[i_ANN_nearest].GetANNOutput(input_output_map->GetMLPOutputIndex(i_map_nearest, i));
     }
   }
 
@@ -142,7 +141,7 @@ unsigned long MLPToolbox::CLookUp_ANN::Predict_ANN(CIOMap* input_output_map, su2
   return MLP_was_evaluated ? 0 : 1;
 }
 
-void MLPToolbox::CLookUp_ANN::GenerateANN(CNeuralNetwork* ANN, string fileName) {
+void MLPToolbox::CLookUp_ANN::GenerateANN(CNeuralNetwork &ANN, string fileName) {
   /*--- Generate MLP architecture based on information in MLP input file ---*/
 
   /* Read MLP input file */
@@ -152,51 +151,51 @@ void MLPToolbox::CLookUp_ANN::GenerateANN(CNeuralNetwork* ANN, string fileName)
   Reader.ReadMLPFile();
 
   /* Generate basic layer architectures */
-  ANN->defineInputLayer(Reader.GetNInputs());
-  ANN->sizeInputs(Reader.GetNInputs());
+  ANN.DefineInputLayer(Reader.GetNInputs());
+  ANN.SizeInputs(Reader.GetNInputs());
   for (auto iInput = 0u; iInput < Reader.GetNInputs(); iInput++) {
-    ANN->SetInputName(iInput, Reader.GetInputName(iInput));
+    ANN.SetInputName(iInput, Reader.GetInputName(iInput));
   }
   for (auto iLayer = 1u; iLayer < Reader.GetNlayers() - 1; iLayer++) {
-    ANN->push_hidden_layer(Reader.GetNneurons(iLayer));
+    ANN.PushHiddenLayer(Reader.GetNneurons(iLayer));
   }
-  ANN->defineOutputLayer(Reader.GetNOutputs());
+  ANN.DefineOutputLayer(Reader.GetNOutputs());
   for (auto iOutput = 0u; iOutput < Reader.GetNOutputs(); iOutput++) {
-    ANN->SetOutputName(iOutput, Reader.GetOutputName(iOutput));
+    ANN.SetOutputName(iOutput, Reader.GetOutputName(iOutput));
   }
 
   /* Size weights of each layer */
-  ANN->sizeWeights();
+  ANN.SizeWeights();
 
   /* Define weights and activation functions */
-  ANN->SizeActivationFunctions(ANN->getNWeightLayers() + 1);
-  for (auto i_layer = 0u; i_layer < ANN->getNWeightLayers(); i_layer++) {
-    ANN->setActivationFunction(i_layer, Reader.GetActivationFunction(i_layer));
-    for (auto i_neuron = 0u; i_neuron < ANN->getNNeurons(i_layer); i_neuron++) {
-      for (auto j_neuron = 0u; j_neuron < ANN->getNNeurons(i_layer + 1); j_neuron++) {
-        ANN->setWeight(i_layer, i_neuron, j_neuron, Reader.GetWeight(i_layer, i_neuron, j_neuron));
+  ANN.SizeActivationFunctions(ANN.GetNWeightLayers() + 1);
+  for (auto i_layer = 0u; i_layer < ANN.GetNWeightLayers(); i_layer++) {
+    ANN.SetActivationFunction(i_layer, Reader.GetActivationFunction(i_layer));
+    for (auto i_neuron = 0u; i_neuron < ANN.GetNNeurons(i_layer); i_neuron++) {
+      for (auto j_neuron = 0u; j_neuron < ANN.GetNNeurons(i_layer + 1); j_neuron++) {
+        ANN.SetWeight(i_layer, i_neuron, j_neuron, Reader.GetWeight(i_layer, i_neuron, j_neuron));
       }
     }
   }
-  ANN->setActivationFunction(ANN->getNWeightLayers(), Reader.GetActivationFunction(ANN->getNWeightLayers()));
+  ANN.SetActivationFunction(ANN.GetNWeightLayers(), Reader.GetActivationFunction(ANN.GetNWeightLayers()));
 
   /* Set neuron biases */
-  for (auto i_layer = 0u; i_layer < ANN->getNWeightLayers() + 1; i_layer++) {
-    for (auto i_neuron = 0u; i_neuron < ANN->getNNeurons(i_layer); i_neuron++) {
-      ANN->setBias(i_layer, i_neuron, Reader.GetBias(i_layer, i_neuron));
+  for (auto i_layer = 0u; i_layer < ANN.GetNWeightLayers() + 1; i_layer++) {
+    for (auto i_neuron = 0u; i_neuron < ANN.GetNNeurons(i_layer); i_neuron++) {
+      ANN.SetBias(i_layer, i_neuron, Reader.GetBias(i_layer, i_neuron));
     }
   }
 
   /* Define input and output layer normalization values */
   for (auto iInput = 0u; iInput < Reader.GetNInputs(); iInput++) {
-    ANN->SetInputNorm(iInput, Reader.GetInputNorm(iInput).first, Reader.GetInputNorm(iInput).second);
+    ANN.SetInputNorm(iInput, Reader.GetInputNorm(iInput).first, Reader.GetInputNorm(iInput).second);
   }
   for (auto iOutput = 0u; iOutput < Reader.GetNOutputs(); iOutput++) {
-    ANN->SetOutputNorm(iOutput, Reader.GetOutputNorm(iOutput).first, Reader.GetOutputNorm(iOutput).second);
+    ANN.SetOutputNorm(iOutput, Reader.GetOutputNorm(iOutput).first, Reader.GetOutputNorm(iOutput).second);
   }
 }
 
-bool MLPToolbox::CLookUp_ANN::Check_Use_of_Inputs(su2vector<string>& input_names, CIOMap* input_output_map) const {
+bool MLPToolbox::CLookUp_ANN::CheckUseOfInputs(su2vector<string>& input_names, CIOMap* input_output_map) const {
   /*--- Check wether all input variables are in the loaded MLPs ---*/
   vector<string> missing_inputs;
   bool inputs_are_present{true};
@@ -223,7 +222,7 @@ bool MLPToolbox::CLookUp_ANN::Check_Use_of_Inputs(su2vector<string>& input_names
   return inputs_are_present;
 }
 
-bool MLPToolbox::CLookUp_ANN::Check_Use_of_Outputs(su2vector<string>& output_names, CIOMap* input_output_map) const {
+bool MLPToolbox::CLookUp_ANN::CheckUseOfOutputs(su2vector<string>& output_names, CIOMap* input_output_map) const {
   /*--- Check wether all output variables are in the loaded MLPs ---*/
 
   vector<string> missing_outputs;
diff --git a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
index 50322d31216..16ab3f7c2a2 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
@@ -3,14 +3,14 @@
  * \brief Implementation of the NeuralNetwork class to be used
  *      for evaluation of multi-layer perceptrons.
  * \author E.C.Bunschoten
- * \version 7.5.0 "Blackbird"
+ * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public
@@ -29,25 +29,28 @@
 
 #include <iomanip>
 #include <iostream>
+#include <map>
 
 #include "../../../include/toolboxes/multilayer_perceptron/CLayer.hpp"
 #include "../../../include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp"
+#include "../../../include/option_structure.hpp"
+
 using namespace std;
 
-void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double>& inputs, bool compute_gradient) {
+void MLPToolbox::CNeuralNetwork::Predict(su2vector<su2double>& inputs, bool compute_gradient) {
   /*--- Evaluate MLP for given inputs ---*/
 
   su2double y = 0, dy_dx = 0;  // Activation function output.
   bool same_point = true;
   /* Normalize input and check if inputs are the same w.r.t last evaluation */
-  for (auto iNeuron = 0u; iNeuron < inputLayer->getNNeurons(); iNeuron++) {
+  for (auto iNeuron = 0u; iNeuron < inputLayer->GetNNeurons(); iNeuron++) {
     su2double x_norm =
         (inputs[iNeuron] - input_norm[iNeuron].first) / (input_norm[iNeuron].second - input_norm[iNeuron].first);
-    if (abs(x_norm - inputLayer->getOutput(iNeuron)) > 0) same_point = false;
-    inputLayer->setOutput(iNeuron, x_norm);
+    if (abs(x_norm - inputLayer->GetOutput(iNeuron)) > 0) same_point = false;
+    inputLayer->SetOutput(iNeuron, x_norm);
 
     if (compute_gradient)
-      inputLayer->setdYdX(iNeuron, iNeuron, 1 / (input_norm[iNeuron].second - input_norm[iNeuron].first));
+      inputLayer->SetdYdX(iNeuron, iNeuron, 1 / (input_norm[iNeuron].second - input_norm[iNeuron].first));
   }
   /* Skip evaluation process if current point is the same as during the previous evaluation */
   if (!same_point) {
@@ -55,17 +58,17 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double>& inputs, bool comp
     su2double lambda = 1.05070098;
     /* Traverse MLP and compute inputs and outputs for the neurons in each layer */
     for (auto iLayer = 1u; iLayer < n_hidden_layers + 2; iLayer++) {
-      auto nNeurons_current = total_layers[iLayer]->getNNeurons();  // Neuron count of current layer
+      auto nNeurons_current = total_layers[iLayer]->GetNNeurons();  // Neuron count of current layer
       su2double x;                                                  // Neuron input value
 
       /* Compute and store input value for each neuron */
       for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
         x = ComputeX(iLayer, iNeuron);
-        total_layers[iLayer]->setInput(iNeuron, x);
+        total_layers[iLayer]->SetInput(iNeuron, x);
         if (compute_gradient) {
-          for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
+          for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
             dy_dx = ComputedOutputdInput(iLayer, iNeuron, iInput);
-            total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx);
+            total_layers[iLayer]->SetdYdX(iNeuron, iInput, dy_dx);
           }
         }
       }
@@ -74,7 +77,7 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double>& inputs, bool comp
       switch (activation_function_types[iLayer]) {
         case ENUM_ACTIVATION_FUNCTION::ELU:
           for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
-            x = total_layers[iLayer]->getInput(iNeuron);
+            x = total_layers[iLayer]->GetInput(iNeuron);
             if (x > 0) {
               y = x;
               if (compute_gradient) dy_dx = 1.0;
@@ -82,43 +85,43 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double>& inputs, bool comp
               y = exp(x) - 1;
               if (compute_gradient) dy_dx = exp(x);
             }
-            total_layers[iLayer]->setOutput(iNeuron, y);
+            total_layers[iLayer]->SetOutput(iNeuron, y);
             if (compute_gradient) {
-              for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
-                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+              for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
+                total_layers[iLayer]->SetdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->GetdYdX(iNeuron, iInput));
               }
             }
           }
           break;
         case ENUM_ACTIVATION_FUNCTION::LINEAR:
           for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
-            x = total_layers[iLayer]->getInput(iNeuron);
+            x = total_layers[iLayer]->GetInput(iNeuron);
             y = x;
-            total_layers[iLayer]->setOutput(iNeuron, y);
+            total_layers[iLayer]->SetOutput(iNeuron, y);
             if (compute_gradient) {
               dy_dx = 1.0;
-              for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
-                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+              for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
+                total_layers[iLayer]->SetdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->GetdYdX(iNeuron, iInput));
               }
             }
           }
           break;
         case ENUM_ACTIVATION_FUNCTION::EXPONENTIAL:
           for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
-            x = total_layers[iLayer]->getInput(iNeuron);
+            x = total_layers[iLayer]->GetInput(iNeuron);
             y = exp(x);
-            total_layers[iLayer]->setOutput(iNeuron, y);
+            total_layers[iLayer]->SetOutput(iNeuron, y);
             if (compute_gradient) {
               dy_dx = 1.0;
-              for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
-                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+              for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
+                total_layers[iLayer]->SetdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->GetdYdX(iNeuron, iInput));
               }
             }
           }
           break;
         case ENUM_ACTIVATION_FUNCTION::RELU:
           for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
-            x = total_layers[iLayer]->getInput(iNeuron);
+            x = total_layers[iLayer]->GetInput(iNeuron);
             if (x > 0) {
               y = x;
               if (compute_gradient) dy_dx = 1.0;
@@ -126,56 +129,56 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double>& inputs, bool comp
               y = 0.0;
               if (compute_gradient) dy_dx = 0.0;
             }
-            total_layers[iLayer]->setOutput(iNeuron, y);
+            total_layers[iLayer]->SetOutput(iNeuron, y);
             if (compute_gradient) {
-              for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
-                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+              for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
+                total_layers[iLayer]->SetdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->GetdYdX(iNeuron, iInput));
               }
             }
           }
           break;
         case ENUM_ACTIVATION_FUNCTION::SWISH:
           for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
-            x = total_layers[iLayer]->getInput(iNeuron);
+            x = total_layers[iLayer]->GetInput(iNeuron);
             y = x / (1 + exp(-x));
-            total_layers[iLayer]->setOutput(iNeuron, y);
+            total_layers[iLayer]->SetOutput(iNeuron, y);
             if (compute_gradient) {
               dy_dx = exp(x) * (x + exp(x) + 1) / pow(exp(x) + 1, 2);
-              for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
-                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+              for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
+                total_layers[iLayer]->SetdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->GetdYdX(iNeuron, iInput));
               }
             }
           }
           break;
         case ENUM_ACTIVATION_FUNCTION::TANH:
           for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
-            x = total_layers[iLayer]->getInput(iNeuron);
+            x = total_layers[iLayer]->GetInput(iNeuron);
             y = tanh(x);
-            total_layers[iLayer]->setOutput(iNeuron, y);
+            total_layers[iLayer]->SetOutput(iNeuron, y);
             if (compute_gradient) {
               dy_dx = 1 / pow(cosh(x), 2);
-              for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
-                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+              for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
+                total_layers[iLayer]->SetdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->GetdYdX(iNeuron, iInput));
               }
             }
           }
           break;
         case ENUM_ACTIVATION_FUNCTION::SIGMOID:
           for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
-            x = total_layers[iLayer]->getInput(iNeuron);
+            x = total_layers[iLayer]->GetInput(iNeuron);
             y = 1.0 / (1 + exp(-x));
-            total_layers[iLayer]->setOutput(iNeuron, y);
+            total_layers[iLayer]->SetOutput(iNeuron, y);
             if (compute_gradient) {
               dy_dx = exp(-x) / pow(exp(-x) + 1, 2);
-              for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
-                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+              for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
+                total_layers[iLayer]->SetdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->GetdYdX(iNeuron, iInput));
               }
             }
           }
           break;
         case ENUM_ACTIVATION_FUNCTION::SELU:
           for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
-            x = total_layers[iLayer]->getInput(iNeuron);
+            x = total_layers[iLayer]->GetInput(iNeuron);
             if (x > 0.0) {
               y = lambda * x;
               if (compute_gradient) dy_dx = lambda;
@@ -183,26 +186,26 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double>& inputs, bool comp
               y = lambda * alpha * (exp(x) - 1);
               if (compute_gradient) dy_dx = lambda * alpha * exp(x);
             }
-            total_layers[iLayer]->setOutput(iNeuron, y);
+            total_layers[iLayer]->SetOutput(iNeuron, y);
             if (compute_gradient) {
-              for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
-                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+              for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
+                total_layers[iLayer]->SetdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->GetdYdX(iNeuron, iInput));
               }
             }
           }
           break;
         case ENUM_ACTIVATION_FUNCTION::GELU:
           for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
-            x = total_layers[iLayer]->getInput(iNeuron);
+            x = total_layers[iLayer]->GetInput(iNeuron);
 
             y = 0.5 * x * (1 + tanh(sqrt(2 / PI_NUMBER) * (x + 0.044715 * pow(x, 3))));
-            total_layers[iLayer]->setOutput(iNeuron, y);
+            total_layers[iLayer]->SetOutput(iNeuron, y);
             if (compute_gradient) {
               dy_dx = 0.5 * (tanh(0.0356774 * pow(x, 3) + 0.797885 * x) + (0.107032 * pow(x, 3) + 0.797885 * x) *
                                                                               pow(cosh(x), -2) *
                                                                               (0.0356774 * pow(x, 3) + 0.797885 * x));
-              for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
-                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+              for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
+                total_layers[iLayer]->SetdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->GetdYdX(iNeuron, iInput));
               }
             }
           }
@@ -210,11 +213,11 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double>& inputs, bool comp
         case ENUM_ACTIVATION_FUNCTION::NONE:
           for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
             y = 0.0;
-            total_layers[iLayer]->setOutput(iNeuron, y);
+            total_layers[iLayer]->SetOutput(iNeuron, y);
             if (compute_gradient) {
               dy_dx = 0.0;
-              for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
-                total_layers[iLayer]->setdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->getdYdX(iNeuron, iInput));
+              for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
+                total_layers[iLayer]->SetdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->GetdYdX(iNeuron, iInput));
               }
             }
           }
@@ -225,14 +228,14 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double>& inputs, bool comp
     }
   }
   /* Compute and de-normalize MLP output */
-  for (auto iNeuron = 0u; iNeuron < outputLayer->getNNeurons(); iNeuron++) {
-    su2double y_norm = outputLayer->getOutput(iNeuron);
+  for (auto iNeuron = 0u; iNeuron < outputLayer->GetNNeurons(); iNeuron++) {
+    su2double y_norm = outputLayer->GetOutput(iNeuron);
     y = y_norm * (output_norm[iNeuron].second - output_norm[iNeuron].first) + output_norm[iNeuron].first;
     if (compute_gradient) {
       dy_dx = (output_norm[iNeuron].second - output_norm[iNeuron].first);
-      for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++) {
-        outputLayer->setdYdX(iNeuron, iInput, dy_dx * outputLayer->getdYdX(iNeuron, iInput));
-        dOutputs_dInputs[iNeuron][iInput] = outputLayer->getdYdX(iNeuron, iInput);
+      for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
+        outputLayer->SetdYdX(iNeuron, iInput, dy_dx * outputLayer->GetdYdX(iNeuron, iInput));
+        dOutputs_dInputs[iNeuron][iInput] = outputLayer->GetdYdX(iNeuron, iInput);
       }
     }
     /* Storing output value */
@@ -240,31 +243,31 @@ void MLPToolbox::CNeuralNetwork::predict(su2vector<su2double>& inputs, bool comp
   }
 }
 
-void MLPToolbox::CNeuralNetwork::defineInputLayer(unsigned long n_neurons) {
+void MLPToolbox::CNeuralNetwork::DefineInputLayer(unsigned long n_neurons) {
   /*--- Define the input layer of the network ---*/
   inputLayer = new CLayer(n_neurons);
 
   /* Mark layer as input layer */
-  inputLayer->setInput(true);
+  inputLayer->SetInput(true);
   input_norm.resize(n_neurons);
   input_names.resize(n_neurons);
 }
 
-void MLPToolbox::CNeuralNetwork::defineOutputLayer(unsigned long n_neurons) {
+void MLPToolbox::CNeuralNetwork::DefineOutputLayer(unsigned long n_neurons) {
   /*--- Define the output layer of the network ---*/
   outputLayer = new CLayer(n_neurons);
   output_norm.resize(n_neurons);
   output_names.resize(n_neurons);
 }
 
-void MLPToolbox::CNeuralNetwork::push_hidden_layer(unsigned long n_neurons) {
+void MLPToolbox::CNeuralNetwork::PushHiddenLayer(unsigned long n_neurons) {
   /*--- Add a hidden layer to the network ---*/
   CLayer* newLayer = new CLayer(n_neurons);
   hiddenLayers.push_back(newLayer);
   n_hidden_layers++;
 }
 
-void MLPToolbox::CNeuralNetwork::sizeWeights() {
+void MLPToolbox::CNeuralNetwork::SizeWeights() {
   /*--- Size weight matrices based on neuron counts in each layer ---*/
 
   /* Generate vector containing input, output, and hidden layer references */
@@ -276,20 +279,20 @@ void MLPToolbox::CNeuralNetwork::sizeWeights() {
   total_layers[total_layers.size() - 1] = outputLayer;
 
   weights_mat.resize(n_hidden_layers + 1);
-  weights_mat[0].resize(hiddenLayers[0]->getNNeurons(), inputLayer->getNNeurons());
+  weights_mat[0].resize(hiddenLayers[0]->GetNNeurons(), inputLayer->GetNNeurons());
   for (auto iLayer = 1u; iLayer < n_hidden_layers; iLayer++) {
-    weights_mat[iLayer].resize(hiddenLayers[iLayer]->getNNeurons(), hiddenLayers[iLayer - 1]->getNNeurons());
+    weights_mat[iLayer].resize(hiddenLayers[iLayer]->GetNNeurons(), hiddenLayers[iLayer - 1]->GetNNeurons());
   }
-  weights_mat[n_hidden_layers].resize(outputLayer->getNNeurons(), hiddenLayers[n_hidden_layers - 1]->getNNeurons());
+  weights_mat[n_hidden_layers].resize(outputLayer->GetNNeurons(), hiddenLayers[n_hidden_layers - 1]->GetNNeurons());
 
-  ANN_outputs = new su2double[outputLayer->getNNeurons()];
-  dOutputs_dInputs.resize(outputLayer->getNNeurons(), inputLayer->getNNeurons());
+  ANN_outputs = new su2double[outputLayer->GetNNeurons()];
+  dOutputs_dInputs.resize(outputLayer->GetNNeurons(), inputLayer->GetNNeurons());
   for (auto iLayer = 0u; iLayer < n_hidden_layers + 2; iLayer++) {
-    total_layers[iLayer]->sizeGradients(inputLayer->getNNeurons());
+    total_layers[iLayer]->SizeGradients(inputLayer->GetNNeurons());
   }
 }
 
-void MLPToolbox::CNeuralNetwork::displayNetwork() const {
+void MLPToolbox::CNeuralNetwork::DisplayNetwork() const {
   /*--- Display information on the MLP architecture ---*/
   int display_width = 54;
   int column_width = int(display_width / 3.0) - 1;
@@ -309,7 +312,7 @@ void MLPToolbox::CNeuralNetwork::displayNetwork() const {
   cout << setfill(' ');
 
   /*--- Hidden layer information ---*/
-  for (auto iInput = 0u; iInput < inputLayer->getNNeurons(); iInput++)
+  for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++)
     cout << "|" << left << setw(column_width) << to_string(iInput + 1) + ": " + input_names[iInput] << "|" << right
          << setw(column_width) << input_norm[iInput].first << "|" << right << setw(column_width)
          << input_norm[iInput].second << "|" << endl;
@@ -327,7 +330,7 @@ void MLPToolbox::CNeuralNetwork::displayNetwork() const {
   cout << setfill(' ');
   for (auto iLayer = 0u; iLayer < n_hidden_layers; iLayer++)
     cout << "|" << setw(column_width) << right << iLayer + 1 << "|" << setw(column_width) << right
-         << hiddenLayers[iLayer]->getNNeurons() << "|" << setw(column_width) << right
+         << hiddenLayers[iLayer]->GetNNeurons() << "|" << setw(column_width) << right
          << activation_function_names[iLayer + 1] << "|" << endl;
   cout << "+" << setfill('-') << setw(display_width) << right << "+" << endl;
   cout << setfill(' ');
@@ -343,7 +346,7 @@ void MLPToolbox::CNeuralNetwork::displayNetwork() const {
        << "|" << endl;
   cout << "+" << setfill('-') << setw(display_width) << right << "+" << endl;
   cout << setfill(' ');
-  for (auto iOutput = 0u; iOutput < outputLayer->getNNeurons(); iOutput++)
+  for (auto iOutput = 0u; iOutput < outputLayer->GetNNeurons(); iOutput++)
     cout << "|" << left << setw(column_width) << to_string(iOutput + 1) + ": " + output_names[iOutput] << "|" << right
          << setw(column_width) << output_norm[iOutput].first << "|" << right << setw(column_width)
          << output_norm[iOutput].second << "|" << endl;
@@ -352,49 +355,13 @@ void MLPToolbox::CNeuralNetwork::displayNetwork() const {
   cout << endl;
 }
 
-void MLPToolbox::CNeuralNetwork::setActivationFunction(unsigned long i_layer, string input) {
+void MLPToolbox::CNeuralNetwork::SetActivationFunction(unsigned long i_layer, string input) {
   /*--- Translate activation function name from input file to a number ---*/
+
   activation_function_names[i_layer] = input;
-  if (input.compare("linear") == 0) {
-    activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::LINEAR;
-    return;
-  }
-  if (input.compare("relu") == 0) {
-    activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::RELU;
-    return;
-  }
-  if ((input.compare("elu") == 0)) {
-    activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::ELU;
-    return;
-  }
-  if (input.compare("swish") == 0) {
-    activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::SWISH;
-    return;
-  }
-  if (input.compare("sigmoid") == 0) {
-    activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::SIGMOID;
-    return;
-  }
-  if (input.compare("tanh") == 0) {
-    activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::TANH;
-    return;
-  }
-  if (input.compare("selu") == 0) {
-    activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::SELU;
-    return;
-  }
-  if (input.compare("gelu") == 0) {
-    activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::GELU;
-    return;
-  }
-  if (input.compare("none") == 0) {
-    activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::NONE;
-    return;
-  }
-  if (input.compare("exponential") == 0) {
-    activation_function_types[i_layer] = ENUM_ACTIVATION_FUNCTION::EXPONENTIAL;
-    return;
-  }
-  SU2_MPI::Error("Unknown activation function type: " + input, CURRENT_FUNCTION);
+
+  // Set activation function type in current layer.
+  activation_function_types[i_layer] = activation_function_map.find(input)->second;
+
   return;
 }
diff --git a/Common/src/toolboxes/multilayer_perceptron/CNeuron.cpp b/Common/src/toolboxes/multilayer_perceptron/CNeuron.cpp
deleted file mode 100644
index 2ff20a60f09..00000000000
--- a/Common/src/toolboxes/multilayer_perceptron/CNeuron.cpp
+++ /dev/null
@@ -1,34 +0,0 @@
-/*!
- * \file CNeuron.cpp
- * \brief Implementation of the neuron class to be used within the
- *      Layer class as a part of the NeuralNetwork class.
- * \author E.C.Bunschoten
- * \version 7.5.0 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-#include "../../../include/toolboxes/multilayer_perceptron/CNeuron.hpp"
-
-#include <cmath>
-#include <cstring>
-#include <iostream>
-
-using namespace std;
\ No newline at end of file
diff --git a/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
index ac31994e436..a03cf36b4bd 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
@@ -3,14 +3,14 @@
  * \brief Implementation of the reader class to read .mlp input files
  *      used to set up multi-layer perceptrons.
  * \author E.C.Bunschoten
- * \version 7.5.0 "Blackbird"
+ * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public
diff --git a/Docs/docmain.hpp b/Docs/docmain.hpp
index 704f85acdcb..ebcf272ee3f 100644
--- a/Docs/docmain.hpp
+++ b/Docs/docmain.hpp
@@ -224,4 +224,10 @@
  * \defgroup SIMD Vectorization (SIMD)
  * \brief Classes for explicit (done by the programmer) vectorization (SIMD) of computations.
  * \ingroup Toolboxes
- */
\ No newline at end of file
+ */
+
+/*!
+ * \defgroup Multi-Layer Perceptrons (MLP)
+ * \brief Data look up and interpolation via dense, feed-forward multi-layer perceptrons. 
+ * \ingroup Toolboxes
+*/
\ No newline at end of file
diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index dac2c963c7a..68b51de8d49 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -3,14 +3,14 @@
  * \brief Defines a template fluid model class using multilayer perceptrons
  *  for theromodynamic state definition
  * \author E.Bunschoten
- * \version 7.5.0 "Blackbird"
+ * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 7511fdf3fe9..0f45b74e84c 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -2,14 +2,14 @@
  * \file CDataDrivenFluid.cpp
  * \brief Source of the data-driven fluid model class
  * \author E.Bunschoten M.Mayer A.Capiello
- * \version 7.5.0 "Blackbird"
+ * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public
@@ -47,7 +47,7 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
 
   /*--- Relaxation factor and tolerance for Newton solvers. ---*/
   Newton_Relaxation = config->GetRelaxation_DataDriven();
-  Newton_Tolerance = 1e-8;
+  Newton_Tolerance = 1e-10;
   MaxIter_Newton = 500;
 
   /*--- Preprocessing of inputs and outputs for the interpolation method. ---*/
@@ -354,13 +354,13 @@ unsigned long CDataDrivenFluid::Predict_MLP(su2double rho, su2double e) {
   MLP_inputs[idx_e] = e;
 
   /* Evaluate MLP collection for the given values for density and energy */
-  unsigned long exit_code = lookup_mlp->Predict_ANN(iomap_rhoe, MLP_inputs, outputs_rhoe);
+  unsigned long exit_code = lookup_mlp->PredictANN(iomap_rhoe, MLP_inputs, outputs_rhoe);
 
   /* Apply exponential transformation to the MLP outputs for the first and second
      derivative of the entropy w.r.t density */
   // Optional:
-  //dsdrho_e = -exp(dsdrho_e);
-  //d2sdrho2 = exp(d2sdrho2);
+  dsdrho_e = -exp(dsdrho_e);
+  d2sdrho2 = exp(d2sdrho2);
 
   return exit_code;
 }
diff --git a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
index f4669364e78..de78e0875cb 100644
--- a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
+++ b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
@@ -2,14 +2,14 @@
  * \file CLookUp_ANN_tests.cpp
  * \brief Unit tests for NdFlattener template classes.
  * \author M. Aehle
- * \version 7.5.0 "Blackbird"
+ * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
  *
  * The SU2 Project is maintained by the SU2 Foundation
  * (http://su2foundation.org)
  *
- * Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
  *
  * SU2 is free software; you can redistribute it and/or
  * modify it under the terms of the GNU Lesser General Public

From a615cae5026c89def9e0931f313f4e988cff9739 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 27 Feb 2023 15:23:44 +0100
Subject: [PATCH 241/656] Fixed bug in CLookUp_ANN_tests

---
 .../toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp     | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
index de78e0875cb..7f125adb6ae 100644
--- a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
+++ b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
@@ -60,7 +60,7 @@ TEST_CASE("LookUp ANN test", "[LookUpANN]"){
 
   MLP_inputs[0] = x;
   MLP_inputs[1] = y;
-  ANN.Predict_ANN(&iomap, MLP_inputs, MLP_outputs);
+  ANN.PredictANN(&iomap, MLP_inputs, MLP_outputs);
   CHECK(z == Approx(0.344829));
 
   /*--- MLP evaluation on point outside the training data range ---*/
@@ -68,6 +68,6 @@ TEST_CASE("LookUp ANN test", "[LookUpANN]"){
   y = -10;
   MLP_inputs[0] = x;
   MLP_inputs[1] = y;
-  ANN.Predict_ANN(&iomap, MLP_inputs, MLP_outputs);
+  ANN.PredictANN(&iomap, MLP_inputs, MLP_outputs);
   CHECK(z == Approx(0.012737));
 }

From ef77c7b7c60534a4439a8b7703056c2cce8c11bb Mon Sep 17 00:00:00 2001
From: WallyMaier <wallytmaier@gmail.com>
Date: Mon, 27 Feb 2023 10:55:23 -0500
Subject: [PATCH 242/656] update docker date-time

---
 .github/workflows/regression.yml         | 18 +++++++++---------
 .github/workflows/release-management.yml |  2 +-
 2 files changed, 10 insertions(+), 10 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 8dea4730c10..ef4925a9a0c 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -52,12 +52,12 @@ jobs:
           key: ${{ matrix.config_set }}-${{ github.sha }}
           restore-keys: ${{ matrix.config_set }}
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/build-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/build-su2:230227-1421
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
       - name: Build
-        uses: docker://ghcr.io/su2code/su2/build-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/build-su2:230227-1421
         with:
           args: -b ${{github.ref}} -f "${{matrix.flags}}"
       - name: Compress binaries
@@ -68,7 +68,7 @@ jobs:
           name: ${{ matrix.config_set }}
           path: install_bin.tgz
       - name: Post Cleanup
-        uses: docker://ghcr.io/su2code/su2/build-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/build-su2:230227-1421
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -99,7 +99,7 @@ jobs:
             tag: OMP
     steps:
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/test-su2:230227-1421
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -125,12 +125,12 @@ jobs:
           chmod a+x $BIN_FOLDER/*
           ls -lahR $BIN_FOLDER
       - name: Run Tests in Container
-        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/test-su2:230227-1421
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
           args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
       - name: Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/test-su2:230227-1421
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -151,7 +151,7 @@ jobs:
             tag: MPI
     steps:
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/test-su2:230227-1421
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -212,11 +212,11 @@ jobs:
           echo $PWD
           ls -lahR
       - name: Run Unit Tests
-        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/test-su2:230227-1421
         with:
           entrypoint: install/bin/${{matrix.testdriver}}
       - name: Post Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/test-su2:230227-1421
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
diff --git a/.github/workflows/release-management.yml b/.github/workflows/release-management.yml
index 287ecdb517d..0535e2f8a89 100644
--- a/.github/workflows/release-management.yml
+++ b/.github/workflows/release-management.yml
@@ -35,7 +35,7 @@ jobs:
           key: ${{ matrix.os_bin }}-${{ github.sha }}
           restore-keys: ${{ matrix.os_bin }}
       - name: Build
-        uses: docker://ghcr.io/su2code/su2/build-su2-cross:221224-1158
+        uses: docker://ghcr.io/su2code/su2/build-su2-cross:230227-1421
         with:
           args: -b ${{ github.sha }} -f "${{matrix.flags}}"
       - name: Create Archive

From 10a09c222131d2167a2d1937edd909491c1ca9b7 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 28 Feb 2023 16:41:40 +0100
Subject: [PATCH 243/656] Fixed Giles boundary condition when using data-driven
 fluid model

---
 .../multilayer_perceptron/CLayer.hpp          |  4 +-
 .../multilayer_perceptron/CLookUp_ANN.hpp     |  6 +-
 .../multilayer_perceptron/CNeuralNetwork.hpp  | 67 +++++++++----------
 .../multilayer_perceptron/CNeuron.hpp         |  2 +-
 .../multilayer_perceptron/CIOMap.cpp          | 15 ++---
 .../multilayer_perceptron/CLookUp_ANN.cpp     | 16 ++---
 .../multilayer_perceptron/CNeuralNetwork.cpp  |  2 +-
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        | 15 ++++-
 SU2_CFD/src/solvers/CEulerSolver.cpp          |  8 +++
 9 files changed, 75 insertions(+), 60 deletions(-)

diff --git a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
index cbce62c099d..45e4304df4d 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
@@ -42,11 +42,11 @@ class CLayer {
    *\brief This class functions as one of the hidden, input, or output layers in the multi-layer perceptron
    * class. The CLayer class is used to communicate information (activation function inputs and outputs and gradients)
    * between the CNeuralNetwork class and the CNeuron class. Currently, only a single activation function
-   * can be applied to the neuron inputs within the layer. 
+   * can be applied to the neuron inputs within the layer.
    */
  private:
   unsigned long number_of_neurons; /*!< Neuron count in current layer */
-  su2vector<CNeuron>neurons;                /*!< Array of neurons in current layer */
+  su2vector<CNeuron> neurons;      /*!< Array of neurons in current layer */
   bool is_input;                   /*!< Input layer identifyer */
   std::string activation_type;     /*!< Activation function type applied to the current layer*/
  public:
diff --git a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
index d68ef0893f2..dc5b51f60e3 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
@@ -63,7 +63,7 @@ class CLookUp_ANN {
    * \param[in] ANN - pointer to target NeuralNetwork class
    * \param[in] filename - filename containing ANN architecture information
    */
-  void GenerateANN(CNeuralNetwork &ANN, std::string filename);
+  void GenerateANN(CNeuralNetwork& ANN, std::string filename);
 
  public:
   /*!
@@ -109,8 +109,8 @@ class CLookUp_ANN {
    * \param[in] input - map to inputs (true) or outputs (false)
    */
   std::vector<pair<std::size_t, std::size_t>> FindVariableIndices(std::size_t i_ANN,
-                                                                   su2vector<std::string> variable_names,
-                                                                   bool input) const;
+                                                                  su2vector<std::string> variable_names,
+                                                                  bool input) const;
 };
 
 }  // namespace MLPToolbox
\ No newline at end of file
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
index 8c8c7a3edcc..a28c60e129d 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
@@ -38,43 +38,42 @@
 #include "../../linear_algebra/blas_structure.hpp"
 #include "CLayer.hpp"
 
-
 namespace MLPToolbox {
 class CNeuralNetwork {
   /*!
    *\class CNeuralNetwork
    *\brief The CNeuralNetwork class allows for the evaluation of a loaded MLP architecture for
    * a given set of inputs. The class also contains a list of the various supported activation
-   * function types (linear, relu, elu, gelu, selu, sigmoid, swish, tanh, exp)which can be 
-   * applied to the layers in the network. Currently, only dense, feed-forward type neural 
-   * nets are supported in this implementation. 
+   * function types (linear, relu, elu, gelu, selu, sigmoid, swish, tanh, exp)which can be
+   * applied to the layers in the network. Currently, only dense, feed-forward type neural
+   * nets are supported in this implementation.
    */
  private:
-  su2vector<std::string> input_names,  /*!< MLP input variable names. */
-      output_names;                    /*!< MLP output variable names. */
+  su2vector<std::string> input_names, /*!< MLP input variable names. */
+      output_names;                   /*!< MLP output variable names. */
 
-  unsigned long n_hidden_layers = 0;  /*!< Number of hidden layers (layers between input and output layer). */
+  unsigned long n_hidden_layers = 0; /*!< Number of hidden layers (layers between input and output layer). */
 
-  CLayer *inputLayer = nullptr,  /*!< Pointer to network input layer. */
-      *outputLayer = nullptr;    /*!< Pointer to network output layer. */
+  CLayer *inputLayer = nullptr, /*!< Pointer to network input layer. */
+      *outputLayer = nullptr;   /*!< Pointer to network output layer. */
 
-  std::vector<CLayer*> hiddenLayers;  /*!< Hidden layer collection. */
-  su2vector<CLayer*> total_layers;    /*!< Hidden layers plus in/output layers */
+  std::vector<CLayer*> hiddenLayers; /*!< Hidden layer collection. */
+  su2vector<CLayer*> total_layers;   /*!< Hidden layers plus in/output layers */
 
-  su2vector<su2activematrix> weights_mat;  /*!< Weights of synapses connecting layers */
+  su2vector<su2activematrix> weights_mat; /*!< Weights of synapses connecting layers */
 
-  su2vector<std::pair<su2double, su2double>> input_norm,  /*!< Normalization factors for network inputs */ 
-      output_norm;                                        /*!< Normalization factors for network outputs */
+  su2vector<std::pair<su2double, su2double>> input_norm, /*!< Normalization factors for network inputs */
+      output_norm;                                       /*!< Normalization factors for network outputs */
 
-  su2vector<su2double> last_inputs;  /*!< Inputs from previous lookup operation. Evaluation of the network */
-                                     /*!< is skipped if current inputs are the same as the last inputs. */
+  su2vector<su2double> last_inputs; /*!< Inputs from previous lookup operation. Evaluation of the network */
+                                    /*!< is skipped if current inputs are the same as the last inputs. */
 
-  su2double* ANN_outputs;                 /*!< Pointer to network outputs */
-  su2matrix<su2double> dOutputs_dInputs;  /*!< Network output derivatives w.r.t inputs */
+  su2double* ANN_outputs;                /*!< Pointer to network outputs */
+  su2matrix<su2double> dOutputs_dInputs; /*!< Network output derivatives w.r.t inputs */
 
   /*!
    * \brief Available activation function enumeration.
-  */
+   */
   enum class ENUM_ACTIVATION_FUNCTION {
     NONE = 0,
     LINEAR = 1,
@@ -90,21 +89,21 @@ class CNeuralNetwork {
 
   /*!
    * \brief Available activation function map.
-  */
-  std::map<std::string, ENUM_ACTIVATION_FUNCTION> activation_function_map {
-    {"none", ENUM_ACTIVATION_FUNCTION::NONE},
-    {"linear", ENUM_ACTIVATION_FUNCTION::LINEAR},
-    {"relu", ENUM_ACTIVATION_FUNCTION::RELU},
-    {"gelu", ENUM_ACTIVATION_FUNCTION::GELU},
-    {"selu", ENUM_ACTIVATION_FUNCTION::SELU},
-    {"sigmoid", ENUM_ACTIVATION_FUNCTION::SIGMOID},
-    {"swish", ENUM_ACTIVATION_FUNCTION::SWISH},
-    {"tanh", ENUM_ACTIVATION_FUNCTION::TANH},
-    {"exponential", ENUM_ACTIVATION_FUNCTION::EXPONENTIAL}
-  };
-
-  su2vector<ENUM_ACTIVATION_FUNCTION> activation_function_types; /*!< Activation function type for each layer in the network. */
-  su2vector<string> activation_function_names;  /*!< Activation function name for each layer in the network. */
+   */
+  std::map<std::string, ENUM_ACTIVATION_FUNCTION> activation_function_map{
+      {"none", ENUM_ACTIVATION_FUNCTION::NONE},
+      {"linear", ENUM_ACTIVATION_FUNCTION::LINEAR},
+      {"relu", ENUM_ACTIVATION_FUNCTION::RELU},
+      {"gelu", ENUM_ACTIVATION_FUNCTION::GELU},
+      {"selu", ENUM_ACTIVATION_FUNCTION::SELU},
+      {"sigmoid", ENUM_ACTIVATION_FUNCTION::SIGMOID},
+      {"swish", ENUM_ACTIVATION_FUNCTION::SWISH},
+      {"tanh", ENUM_ACTIVATION_FUNCTION::TANH},
+      {"exponential", ENUM_ACTIVATION_FUNCTION::EXPONENTIAL}};
+
+  su2vector<ENUM_ACTIVATION_FUNCTION>
+      activation_function_types;               /*!< Activation function type for each layer in the network. */
+  su2vector<string> activation_function_names; /*!< Activation function name for each layer in the network. */
 
  public:
   ~CNeuralNetwork() {
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
index 7aab3fbf5e5..03c7a4d3212 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
@@ -37,7 +37,7 @@ namespace MLPToolbox {
 class CNeuron {
   /*!
    *\class CNeuron
-   *\brief This class functions as a neuron within the CLayer class, making up the 
+   *\brief This class functions as a neuron within the CLayer class, making up the
    * CNeuralNetwork class. The CNeuron class functions as a location to store activation
    * function inputs and outputs, as well as gradients and biases. These are accessed
    * through the CLayer class for network evalution operations.
diff --git a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
index 4d28c65fff0..78f70a4ff90 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
@@ -25,22 +25,21 @@
  * You should have received a copy of the GNU Lesser General Public
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
-#include "../../../include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp"
 #include "../../../include/toolboxes/multilayer_perceptron/CIOMap.hpp"
-#include <iostream>
-#include <string>
+
 #include <cmath>
 #include <fstream>
+#include <iostream>
+#include <string>
 
 #include "../../../include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp"
 
 MLPToolbox::CIOMap::CIOMap(CLookUp_ANN* MLP_collection, su2vector<std::string>& inputs,
                            su2vector<std::string>& outputs) {
-
-    /* Generate an input-output map given a set of call inputs and call outputs. These inputs 
-  mapped to the inputs of the loaded MLPs in the MLP_collection object. The call outputs are
-  then matched to the MLPs with matching inputs.
-  */
+  /* Generate an input-output map given a set of call inputs and call outputs. These inputs
+mapped to the inputs of the loaded MLPs in the MLP_collection object. The call outputs are
+then matched to the MLPs with matching inputs.
+*/
   PairVariableswithMLPs(MLP_collection, inputs, outputs);
 
   // Perform checks on input-output validity
diff --git a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
index 662498fc405..50c8e0cd911 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
@@ -29,9 +29,10 @@
 
 #include <cmath>
 #include <fstream>
+#include <iomanip>
 #include <iostream>
 #include <string>
-#include <iomanip>
+
 #include "../../../include/toolboxes/multilayer_perceptron/CIOMap.hpp"
 #include "../../../include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp"
 
@@ -51,7 +52,7 @@ MLPToolbox::CLookUp_ANN::CLookUp_ANN(const unsigned short n_inputs, const string
   cout << "+------------------------------------------------------------------+\n";
   cout << "|                 Multi-Layer Perceptron (MLP) info                |\n";
   cout << "+------------------------------------------------------------------+" << endl;
-  
+
   for (auto i_MLP = 0u; i_MLP < n_inputs; i_MLP++) {
     if (rank == MASTER_NODE) cout << "Generating neural network for " << input_filenames[i_MLP] << endl;
     GenerateANN(NeuralNetworks[i_MLP], input_filenames[i_MLP]);
@@ -60,8 +61,8 @@ MLPToolbox::CLookUp_ANN::CLookUp_ANN(const unsigned short n_inputs, const string
 }
 
 vector<pair<size_t, size_t>> MLPToolbox::CLookUp_ANN::FindVariableIndices(size_t i_ANN,
-                                                                           su2vector<string> variable_names,
-                                                                           bool input) const {
+                                                                          su2vector<string> variable_names,
+                                                                          bool input) const {
   /*--- Find loaded MLPs that have the same input variable names as the variables listed in variable_names ---*/
 
   vector<pair<size_t, size_t>> variable_indices;
@@ -69,8 +70,7 @@ vector<pair<size_t, size_t>> MLPToolbox::CLookUp_ANN::FindVariableIndices(size_t
 
   for (auto iVar = 0u; iVar < nVar; iVar++) {
     for (auto jVar = 0u; jVar < variable_names.size(); jVar++) {
-      string ANN_varname =
-          input ? NeuralNetworks[i_ANN].GetInputName(iVar) : NeuralNetworks[i_ANN].GetOutputName(iVar);
+      string ANN_varname = input ? NeuralNetworks[i_ANN].GetInputName(iVar) : NeuralNetworks[i_ANN].GetOutputName(iVar);
       if (variable_names[jVar].compare(ANN_varname) == 0) {
         variable_indices.push_back(make_pair(jVar, iVar));
       }
@@ -80,7 +80,7 @@ vector<pair<size_t, size_t>> MLPToolbox::CLookUp_ANN::FindVariableIndices(size_t
 }
 
 unsigned long MLPToolbox::CLookUp_ANN::PredictANN(CIOMap* input_output_map, su2vector<su2double>& inputs,
-                                                   su2vector<su2double*>& outputs) {
+                                                  su2vector<su2double*>& outputs) {
   /*--- Evaluate MLP based on target input and output variables ---*/
   bool within_range,              // Within MLP training set range.
       MLP_was_evaluated = false;  // MLP was evaluated within training set range.
@@ -141,7 +141,7 @@ unsigned long MLPToolbox::CLookUp_ANN::PredictANN(CIOMap* input_output_map, su2v
   return MLP_was_evaluated ? 0 : 1;
 }
 
-void MLPToolbox::CLookUp_ANN::GenerateANN(CNeuralNetwork &ANN, string fileName) {
+void MLPToolbox::CLookUp_ANN::GenerateANN(CNeuralNetwork& ANN, string fileName) {
   /*--- Generate MLP architecture based on information in MLP input file ---*/
 
   /* Read MLP input file */
diff --git a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
index 16ab3f7c2a2..15c68c3f161 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
@@ -31,9 +31,9 @@
 #include <iostream>
 #include <map>
 
+//#include "../../../include/option_structure.hpp"
 #include "../../../include/toolboxes/multilayer_perceptron/CLayer.hpp"
 #include "../../../include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp"
-#include "../../../include/option_structure.hpp"
 
 using namespace std;
 
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 0f45b74e84c..3358ce966e1 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -48,7 +48,7 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
   /*--- Relaxation factor and tolerance for Newton solvers. ---*/
   Newton_Relaxation = config->GetRelaxation_DataDriven();
   Newton_Tolerance = 1e-10;
-  MaxIter_Newton = 500;
+  MaxIter_Newton = 50;
 
   /*--- Preprocessing of inputs and outputs for the interpolation method. ---*/
   MapInputs_to_Outputs();
@@ -133,6 +133,15 @@ void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
 
   dPde_rho = -pow(rho, 2) * (dTde_rho * dsdrho_e + Temperature * d2sdedrho);
   dPdrho_e = -2 * rho * Temperature * dsdrho_e - pow(rho, 2) * (dTdrho_e * dsdrho_e + Temperature * d2sdrho2);
+
+  /*--- Compute enthalpy and entropy derivatives required for Giles boundary conditions ---*/
+  su2double dhdrho_e = -Pressure * pow(rho, -2) + dPdrho_e / rho;
+  su2double dhde_rho = 1 + dPde_rho / rho;
+
+  dhdrho_P = dhdrho_e - dhde_rho * (1 / dPde_rho) * dPdrho_e;
+  dhdP_rho = dhdrho_e * (1 / dPdrho_e) + dhde_rho * (1 / dPde_rho);
+  dsdrho_P = dsdrho_e - dPdrho_e * (1 / dPde_rho) * dsde_rho;
+  dsdP_rho = dsde_rho / dPde_rho;
 }
 
 void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
@@ -278,8 +287,8 @@ void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
 
     su2double Enthalpy = e + Pressure / rho;
     /*--- Determine pressure and temperature residuals ---*/
-    delta_h = Enthalpy - h;
-    delta_s = Entropy - s;
+    // delta_h = Enthalpy - h;
+    // delta_s = Entropy - s;
 
     /*--- Continue iterative process if residuals are outside tolerances ---*/
     if ((abs(delta_h / h) < Newton_Tolerance) && (abs(delta_s / s) < Newton_Tolerance)) {
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index b343590cafd..1be0b7f5732 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -6153,6 +6153,11 @@ void CEulerSolver::BC_Giles(CGeometry *geometry, CSolver **solver_container, CNu
       Energy_i = nodes->GetEnergy(iPoint);
       StaticEnergy_i = Energy_i - 0.5*Velocity2_i;
 
+      /*--- Set initial values for density and energy for Newton solvers in fluid model ---*/
+      su2double relax_Newton = config->GetRelaxation_DataDriven();
+      GetFluidModel()->SetDensity(relax_Newton*Density_i + (1 - relax_Newton)*config->GetDensity_Init_DataDriven());
+      GetFluidModel()->SetEnergy(relax_Newton*StaticEnergy_i + (1 - relax_Newton)*config->GetEnergy_Init_DataDriven());
+
       GetFluidModel()->SetTDState_rhoe(Density_i, StaticEnergy_i);
 
       Pressure_i = GetFluidModel()->GetPressure();
@@ -6502,6 +6507,9 @@ void CEulerSolver::BC_Giles(CGeometry *geometry, CSolver **solver_container, CNu
           Jacobian.SubtractBlock2Diag(iPoint, residual.jacobian_i);
 
       }
+      /*--- Store number of Newton iterations at BC ---*/
+      if(config->GetKind_FluidModel() == DATADRIVEN_FLUID)
+        GetNodes()->SetNewtonSolverIterations(iPoint, GetFluidModel()->GetnIter_Newton());
 
     }
     END_SU2_OMP_FOR

From 5d13417c10cf3197db74d4149f19ca3e9de69545 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Wed, 1 Mar 2023 01:45:33 -0800
Subject: [PATCH 244/656] Access solution and primitives via python wrapper
 (#1938)

* matrix view type to manipulate fields in python without copying data

* extra line and update docker images
---
 .github/workflows/regression.yml              |  18 +--
 .github/workflows/release-management.yml      |   2 +-
 .../containers/CPyWrapperMatrixView.hpp       | 115 ++++++++++++++++++
 Common/src/containers/meson.build             |   2 +-
 SU2_CFD/include/drivers/CDriverBase.hpp       |  64 +++++++---
 SU2_CFD/include/output/CFlowOutput.hpp        |  70 +----------
 SU2_CFD/include/solvers/CSolver.hpp           |   4 +-
 SU2_CFD/include/variables/CEulerVariable.hpp  |   3 +
 .../include/variables/CIncEulerVariable.hpp   |   3 +
 SU2_CFD/include/variables/CMeshVariable.hpp   |   5 +
 .../include/variables/CNEMOEulerVariable.hpp  |   3 +
 .../include/variables/CPrimitiveIndices.hpp   |  42 ++++++-
 SU2_CFD/include/variables/CVariable.hpp       |   5 +
 SU2_CFD/src/drivers/CDriverBase.cpp           |  62 ++++------
 SU2_CFD/src/output/CFlowOutput.cpp            |  74 +++++++++--
 SU2_CFD/src/solvers/CAdjEulerSolver.cpp       |   1 +
 SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp     |   1 +
 SU2_CFD/src/solvers/CDiscAdjMeshSolver.cpp    |   1 +
 SU2_CFD/src/solvers/CEulerSolver.cpp          |   2 +-
 SU2_CFD/src/solvers/CFEASolver.cpp            |   2 +-
 SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp   |   4 +-
 SU2_CFD/src/solvers/CHeatSolver.cpp           |   2 +-
 SU2_CFD/src/solvers/CIncEulerSolver.cpp       |   2 +-
 SU2_CFD/src/solvers/CMeshSolver.cpp           |   2 +
 SU2_CFD/src/solvers/CNEMOEulerSolver.cpp      |   2 +-
 SU2_CFD/src/solvers/CRadP1Solver.cpp          |   1 +
 SU2_CFD/src/solvers/CSpeciesSolver.cpp        |   2 +-
 SU2_CFD/src/solvers/CTransLMSolver.cpp        |   2 +-
 SU2_CFD/src/solvers/CTurbSASolver.cpp         |   2 +-
 SU2_CFD/src/solvers/CTurbSSTSolver.cpp        |   4 +-
 SU2_PY/FSI_tools/FSIInterface.py              |   4 +-
 SU2_PY/pySU2/pySU2.i                          |   7 +-
 SU2_PY/pySU2/pySU2ad.i                        |   8 +-
 .../deforming_bump_in_channel/run.py          |  10 +-
 .../launch_flatPlate_rigidMotion.py           |   2 +-
 meson.build                                   |   8 +-
 36 files changed, 363 insertions(+), 178 deletions(-)
 create mode 100644 Common/include/containers/CPyWrapperMatrixView.hpp

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index e749e661e70..aeb1c61ce51 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -52,12 +52,12 @@ jobs:
           key: ${{ matrix.config_set }}-${{ github.sha }}
           restore-keys: ${{ matrix.config_set }}
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/build-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/build-su2:230225-2136
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
       - name: Build
-        uses: docker://ghcr.io/su2code/su2/build-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/build-su2:230225-2136
         with:
           args: -b ${{github.ref}} -f "${{matrix.flags}}"
       - name: Compress binaries
@@ -68,7 +68,7 @@ jobs:
           name: ${{ matrix.config_set }}
           path: install_bin.tgz
       - name: Post Cleanup
-        uses: docker://ghcr.io/su2code/su2/build-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/build-su2:230225-2136
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -99,7 +99,7 @@ jobs:
             tag: OMP
     steps:
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -125,12 +125,12 @@ jobs:
           chmod a+x $BIN_FOLDER/*
           ls -lahR $BIN_FOLDER
       - name: Run Tests in Container
-        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
           args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
       - name: Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -151,7 +151,7 @@ jobs:
             tag: MPI
     steps:
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -212,11 +212,11 @@ jobs:
           echo $PWD
           ls -lahR
       - name: Run Unit Tests
-        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           entrypoint: install/bin/${{matrix.testdriver}}
       - name: Post Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:221224-1158
+        uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
diff --git a/.github/workflows/release-management.yml b/.github/workflows/release-management.yml
index 287ecdb517d..0babf1c46b2 100644
--- a/.github/workflows/release-management.yml
+++ b/.github/workflows/release-management.yml
@@ -35,7 +35,7 @@ jobs:
           key: ${{ matrix.os_bin }}-${{ github.sha }}
           restore-keys: ${{ matrix.os_bin }}
       - name: Build
-        uses: docker://ghcr.io/su2code/su2/build-su2-cross:221224-1158
+        uses: docker://ghcr.io/su2code/su2/build-su2-cross:230225-2136
         with:
           args: -b ${{ github.sha }} -f "${{matrix.flags}}"
       - name: Create Archive
diff --git a/Common/include/containers/CPyWrapperMatrixView.hpp b/Common/include/containers/CPyWrapperMatrixView.hpp
new file mode 100644
index 00000000000..2c3d6477ee4
--- /dev/null
+++ b/Common/include/containers/CPyWrapperMatrixView.hpp
@@ -0,0 +1,115 @@
+/*!
+ * \file CPyWrapperMatrixView.hpp
+ * \brief A simple matrix view to use with the python wrapper.
+ * \author P. Gomes
+ * \version 7.5.1 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+
+#pragma once
+
+#include <utility>
+#include <vector>
+#include <string>
+
+#include "C2DContainer.hpp"
+#include "../parallelization/mpi_structure.hpp"
+
+/*!
+ * \class CPyWrapperMatrixView
+ * \ingroup PySU2
+ * \brief A simple matrix view to use with the python wrapper. The accessors
+ * in this class provide a passive double interface to su2activematrix.
+ * This can be extended to allow access to derivative information of su2double.
+ */
+class CPyWrapperMatrixView {
+ private:
+  static_assert(su2activematrix::IsRowMajor, "");
+  su2double* data_ = nullptr;
+  unsigned long rows_ = 0, cols_ = 0;
+  std::string name_;
+  bool read_only_ = false;
+
+  inline const su2double& Access(unsigned long row, unsigned long col) const {
+    if (row > rows_ || col > cols_) SU2_MPI::Error(name_ + " out of bounds", "CPyWrapperMatrixView");
+    return data_[row * cols_ + col];
+  }
+  inline su2double& Access(unsigned long row, unsigned long col) {
+    if (read_only_) SU2_MPI::Error(name_ + " is read-only", "CPyWrapperMatrixView");
+    const auto& const_me = *this;
+    return const_cast<su2double&>(const_me.Access(row, col));
+  }
+
+ public:
+  CPyWrapperMatrixView() = default;
+
+  /*!
+   * \brief Construct the view of the matrix.
+   * \note "name" should be set to the variable name being returned to give better information to users.
+   * \note "read_only" can be set to true to prevent the data from being modified.
+   */
+  CPyWrapperMatrixView(su2activematrix& mat, const std::string& name, bool read_only)
+    : data_(mat.data()), rows_(mat.rows()), cols_(mat.cols()), name_(name), read_only_(read_only) {}
+
+  /*!
+   * \brief Returns the shape of the matrix.
+   */
+  std::pair<unsigned long, unsigned long> Shape() const { return std::make_pair(rows_, cols_); }
+
+  /*!
+   * \brief Returns whether the data is read-only [true] or if it can be modified [false].
+   */
+  bool IsReadOnly() const { return read_only_; }
+
+  /*!
+   * \brief Gets the value for a (row, column) pair.
+   */
+  passivedouble operator() (unsigned long row, unsigned long col) const { return Get(row, col); }
+
+  /*!
+   * \brief Gets the value for a (row, column) pair.
+   */
+  passivedouble Get(unsigned long row, unsigned long col) const { return SU2_TYPE::GetValue(Access(row, col)); }
+
+  /*!
+   * \brief Gets the values for a row of the matrix.
+   */
+  std::vector<passivedouble> Get(unsigned long row) const {
+    std::vector<passivedouble> vals(cols_);
+    for (unsigned long j = 0; j < cols_; ++j) vals[j] = Get(row, j);
+    return vals;
+  }
+
+  /*!
+   * \brief Sets the value for a (row, column) pair.
+   * \note This clears derivative information (consistently with C++ operator= with passive rhs).
+   */
+  void Set(unsigned long row, unsigned long col, passivedouble val) { Access(row, col) = val; }
+
+  /*!
+   * \brief Sets the values for a row of the matrix.
+   */
+  void Set(unsigned long row, std::vector<passivedouble> vals) {
+    unsigned long j = 0;
+    for (const auto& val : vals) Set(row, j++, val);
+  }
+};
diff --git a/Common/src/containers/meson.build b/Common/src/containers/meson.build
index 9a0fdd1a1ae..4c8d4fe618a 100644
--- a/Common/src/containers/meson.build
+++ b/Common/src/containers/meson.build
@@ -1,3 +1,3 @@
 common_src += files(['CTrapezoidalMap.cpp',
-                     'CFileReaderLUT.cpp', 
+                     'CFileReaderLUT.cpp',
                      'CLookUpTable.cpp'])
diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index b7c5ca56d9f..c83ad9bdf31 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -28,6 +28,7 @@
 #pragma once
 
 #include "../../../Common/include/CConfig.hpp"
+#include "../../../Common/include/containers/CPyWrapperMatrixView.hpp"
 #include "../numerics/CNumerics.hpp"
 #include "../output/COutput.hpp"
 #include "../solvers/CSolver.hpp"
@@ -38,7 +39,6 @@
  * \brief Base class for all drivers.
  * \author H. Patel, A. Gastaldi
  */
-
 class CDriverBase {
  protected:
   int rank,               /*!< \brief MPI Rank. */
@@ -189,25 +189,24 @@ class CDriverBase {
   bool GetNodeDomain(unsigned long iPoint) const;
 
   /*!
-   * \brief Get the initial (un-deformed) coordinates of a mesh node.
-   * \param[in] iPoint - Mesh node index.
-   * \return Initial node coordinates (nDim).
-   */
-  vector<passivedouble> GetInitialCoordinates(unsigned long iPoint) const;
-
-  /*!
-   * \brief Get the current coordinates of a mesh node.
-   * \param[in] iPoint - Mesh node index.
-   * \return Node coordinates (nDim).
+   * \brief Get a read-only view of the initial (undeformed) coordinates of all mesh nodes.
    */
-  vector<passivedouble> GetCoordinates(unsigned long iPoint) const;
+  inline CPyWrapperMatrixView InitialCoordinates() const {
+    if (!main_config->GetDeform_Mesh()) {
+      SU2_MPI::Error("Initial coordinates are only available with DEFORM_MESH= YES", CURRENT_FUNCTION);
+    }
+    auto* coords =
+        const_cast<su2activematrix*>(solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord());
+    return CPyWrapperMatrixView(*coords, "InitialCoordinates", true);
+  }
 
   /*!
-   * \brief Set the coordinates of a mesh node.
-   * \param[in] iPoint - Mesh node index.
-   * \param[in] values - Node coordinates (nDim).
+   * \brief Get a read/write view of the current coordinates of all mesh nodes.
    */
-  void SetCoordinates(unsigned long iPoint, vector<passivedouble> values);
+  inline CPyWrapperMatrixView Coordinates() {
+    auto& coords = const_cast<su2activematrix&>(main_geometry->nodes->GetCoord());
+    return CPyWrapperMatrixView(coords, "Coordinates", false);
+  }
 
   /*!
    * \brief Get the number of markers in the mesh.
@@ -323,6 +322,39 @@ class CDriverBase {
    * \brief Communicate the boundary mesh displacements.
    */
   void CommunicateMeshDisplacements(void);
+
+  /*!
+   * \brief Get all the active solver names with their associated indices (which can be used to access their data).
+   */
+  map<string, unsigned short> GetSolverIndices() const;
+
+  /*!
+   * \brief Get a read/write view of the current solution on all mesh nodes of a solver.
+   */
+  inline CPyWrapperMatrixView Solution(unsigned short iSolver) {
+    auto* solver = solver_container[ZONE_0][INST_0][MESH_0][iSolver];
+    if (solver == nullptr) SU2_MPI::Error("The selected solver does not exist.", CURRENT_FUNCTION);
+    auto& solution = solver->GetNodes()->GetSolution();
+    return CPyWrapperMatrixView(solution, "Solution of " + solver->GetSolverName(), false);
+  }
+
+  /*!
+   * \brief Get the flow solver primitive variable names with their associated indices.
+   * These correspond to the column indices in the matrix returned by Primitives.
+   */
+  map<string, unsigned short> GetPrimitiveIndices() const;
+
+  /*!
+   * \brief Get a read/write view of the current primitive variables on all mesh nodes of the flow solver.
+   * \warning Primitive variables are only available for flow solvers.
+   */
+  inline CPyWrapperMatrixView Primitives() {
+    auto* solver = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL];
+    if (solver == nullptr) SU2_MPI::Error("The flow solver does not exist.", CURRENT_FUNCTION);
+    auto& primitives = const_cast<su2activematrix&>(solver->GetNodes()->GetPrimitive());
+    return CPyWrapperMatrixView(primitives, "Primitives", false);
+  }
+
 /// \}
 
  protected:
diff --git a/SU2_CFD/include/output/CFlowOutput.hpp b/SU2_CFD/include/output/CFlowOutput.hpp
index 9f9b3e029b8..9020076486e 100644
--- a/SU2_CFD/include/output/CFlowOutput.hpp
+++ b/SU2_CFD/include/output/CFlowOutput.hpp
@@ -30,6 +30,10 @@
 #include "CFVMOutput.hpp"
 #include "../variables/CVariable.hpp"
 
+/*--- Forward declare to avoid including here. ---*/
+template <class>
+struct CPrimitiveIndices;
+
 class CFlowOutput : public CFVMOutput{
 protected:
   unsigned long lastInnerIter;
@@ -211,71 +215,7 @@ class CFlowOutput : public CFVMOutput{
    * \brief Helper for custom outputs, converts variable names to indices and pointers which are then used
    * to evaluate the custom expressions.
    */
-  template <class FlowIndices>
-  void ConvertVariableSymbolsToIndices(const FlowIndices& idx, CustomOutput& output) const {
-
-    static const auto knownVariables =
-        "TEMPERATURE, TEMPERATURE_VE, VELOCITY_X, VELOCITY_Y, VELOCITY_Z, PRESSURE,\n"
-        "DENSITY, ENTHALPY, SOUND_SPEED, LAMINAR_VISCOSITY, EDDY_VISCOSITY, THERMAL_CONDUCTIVITY\n"
-        "TURB[0,1,...], RAD[0,1,...], SPECIES[0,1,...]";
-
-    auto IndexOfVariable = [&](const FlowIndices& idx, const std::string& var) {
-      /*--- Primitives of the flow solver. ---*/
-      const auto flow_offset = FLOW_SOL * CustomOutput::MAX_VARS_PER_SOLVER;
-
-      if ("TEMPERATURE" == var) return flow_offset + idx.Temperature();
-      if ("TEMPERATURE_VE" == var) return flow_offset + idx.Temperature_ve();
-      if ("VELOCITY_X" == var) return flow_offset + idx.Velocity();
-      if ("VELOCITY_Y" == var) return flow_offset + idx.Velocity() + 1;
-      if ("VELOCITY_Z" == var) return flow_offset + idx.Velocity() + 2;
-      if ("PRESSURE" == var) return flow_offset + idx.Pressure();
-      if ("DENSITY" == var) return flow_offset + idx.Density();
-      if ("ENTHALPY" == var) return flow_offset + idx.Enthalpy();
-      if ("SOUND_SPEED" == var) return flow_offset + idx.SoundSpeed();
-      if ("LAMINAR_VISCOSITY" == var) return flow_offset + idx.LaminarViscosity();
-      if ("EDDY_VISCOSITY" == var) return flow_offset + idx.EddyViscosity();
-      if ("THERMAL_CONDUCTIVITY" == var) return flow_offset + idx.ThermalConductivity();
-
-      /*--- Index-based (no name) access to variables of other solvers. ---*/
-      auto GetIndex = [](const std::string& s, int nameLen) {
-        /*--- Extract an int from "name[int]", nameLen is the length of "name". ---*/
-        return std::stoi(std::string(s.begin() + nameLen + 1, s.end() - 1));
-      };
-      if (var.rfind("SPECIES", 0) == 0) return SPECIES_SOL * CustomOutput::MAX_VARS_PER_SOLVER + GetIndex(var, 7);
-      if (var.rfind("TURB", 0) == 0) return TURB_SOL * CustomOutput::MAX_VARS_PER_SOLVER + GetIndex(var, 4);
-      if (var.rfind("RAD", 0) == 0) return RAD_SOL * CustomOutput::MAX_VARS_PER_SOLVER + GetIndex(var, 3);
-
-      return CustomOutput::NOT_A_VARIABLE;
-    };
-
-    output.otherOutputs.clear();
-    output.varIndices.clear();
-    output.varIndices.reserve(output.varSymbols.size());
-
-    for (const auto& var : output.varSymbols) {
-      output.varIndices.push_back(IndexOfVariable(idx, var));
-
-      if (output.type == OperationType::FUNCTION && output.varIndices.back() != CustomOutput::NOT_A_VARIABLE) {
-        SU2_MPI::Error("Custom outputs of type 'Function' cannot reference solver variables.", CURRENT_FUNCTION);
-      }
-      /*--- Symbol is a valid solver variable. ---*/
-      if (output.varIndices.back() < CustomOutput::NOT_A_VARIABLE) continue;
-
-      /*--- An index above NOT_A_VARIABLE is not valid with current solver settings. ---*/
-      if (output.varIndices.back() > CustomOutput::NOT_A_VARIABLE) {
-        SU2_MPI::Error("Inactive solver variable (" + var + ") used in function " + output.name + "\n"
-                       "E.g. this may only be a variable of the compressible solver.", CURRENT_FUNCTION);
-      }
-
-      /*--- An index equal to NOT_A_VARIABLE may refer to a history output. ---*/
-      output.varIndices.back() += output.otherOutputs.size();
-      output.otherOutputs.push_back(GetPtrToHistoryOutput(var));
-      if (output.otherOutputs.back() == nullptr) {
-        SU2_MPI::Error("Invalid history output or solver variable (" + var + ") used in function " + output.name +
-                       "\nValid solvers variables: " + knownVariables, CURRENT_FUNCTION);
-      }
-    }
-  }
+  void ConvertVariableSymbolsToIndices(const CPrimitiveIndices<unsigned long>& idx, CustomOutput& output) const;
 
   /*!
    * \brief Compute value of the Q criteration for vortex idenfitication
diff --git a/SU2_CFD/include/solvers/CSolver.hpp b/SU2_CFD/include/solvers/CSolver.hpp
index 954b06ad75d..9ac3d17f6a2 100644
--- a/SU2_CFD/include/solvers/CSolver.hpp
+++ b/SU2_CFD/include/solvers/CSolver.hpp
@@ -4246,9 +4246,9 @@ class CSolver {
 
   /*!
    * \brief Retrieve the solver name for output purposes.
-   * \param[out] val_solvername - Name of the solver.
+   * \returns Name of the solver.
    */
-  inline string GetSolverName(void) {return SolverName;}
+  inline const string& GetSolverName() const  { return SolverName; }
 
   /*!
    * \brief Get the solution fields.
diff --git a/SU2_CFD/include/variables/CEulerVariable.hpp b/SU2_CFD/include/variables/CEulerVariable.hpp
index 25e992da2e1..44f07ffa0a2 100644
--- a/SU2_CFD/include/variables/CEulerVariable.hpp
+++ b/SU2_CFD/include/variables/CEulerVariable.hpp
@@ -46,6 +46,8 @@ class CEulerVariable : public CFlowVariable {
   struct CIndices {
     const IndexType nDim;
     CIndices(IndexType ndim, IndexType) : nDim(ndim) {}
+    inline IndexType NDim() const { return nDim; }
+    inline IndexType NSpecies() const { return 0; }
     inline IndexType Temperature() const { return 0; }
     inline IndexType Velocity() const { return 1; }
     inline IndexType Pressure() const { return nDim+1; }
@@ -58,6 +60,7 @@ class CEulerVariable : public CFlowVariable {
     inline IndexType CpTotal() const { return nDim+8; }
 
     /*--- For compatible interface with NEMO. ---*/
+    inline IndexType SpeciesDensities() const { return std::numeric_limits<IndexType>::max(); }
     inline IndexType Temperature_ve() const { return std::numeric_limits<IndexType>::max(); }
   };
 
diff --git a/SU2_CFD/include/variables/CIncEulerVariable.hpp b/SU2_CFD/include/variables/CIncEulerVariable.hpp
index 61341177faa..16b33d52e84 100644
--- a/SU2_CFD/include/variables/CIncEulerVariable.hpp
+++ b/SU2_CFD/include/variables/CIncEulerVariable.hpp
@@ -46,6 +46,8 @@ class CIncEulerVariable : public CFlowVariable {
   struct CIndices {
     const IndexType nDim;
     CIndices(IndexType ndim, IndexType) : nDim(ndim) {}
+    inline IndexType NDim() const { return nDim; }
+    inline IndexType NSpecies() const { return 0; }
     inline IndexType Pressure() const { return 0; }
     inline IndexType Velocity() const { return 1; }
     inline IndexType Temperature() const { return nDim+1; }
@@ -59,6 +61,7 @@ class CIncEulerVariable : public CFlowVariable {
     inline IndexType CvTotal() const { return nDim+8; }
 
     /*--- For compatible interface with NEMO. ---*/
+    inline IndexType SpeciesDensities() const { return std::numeric_limits<IndexType>::max(); }
     inline IndexType Temperature_ve() const { return std::numeric_limits<IndexType>::max(); }
     inline IndexType Enthalpy() const { return std::numeric_limits<IndexType>::max(); }
   };
diff --git a/SU2_CFD/include/variables/CMeshVariable.hpp b/SU2_CFD/include/variables/CMeshVariable.hpp
index 1c5c185c222..ce3a807885c 100644
--- a/SU2_CFD/include/variables/CMeshVariable.hpp
+++ b/SU2_CFD/include/variables/CMeshVariable.hpp
@@ -63,6 +63,11 @@ class CMeshVariable : public CVariable {
    */
   inline const su2double *GetMesh_Coord(unsigned long iPoint) const final { return Mesh_Coord[iPoint]; }
 
+  /*!
+   * \brief Get the undeformed coordinates for the entire domain.
+   */
+  inline const MatrixType* GetMesh_Coord() const final { return &Mesh_Coord; }
+
   /*!
    * \brief Set the value of the undeformed coordinates.
    * \param[in] iDim - Index of Mesh_Coord[nDim]
diff --git a/SU2_CFD/include/variables/CNEMOEulerVariable.hpp b/SU2_CFD/include/variables/CNEMOEulerVariable.hpp
index d68d90529da..246d24bf7db 100644
--- a/SU2_CFD/include/variables/CNEMOEulerVariable.hpp
+++ b/SU2_CFD/include/variables/CNEMOEulerVariable.hpp
@@ -48,6 +48,8 @@ class CNEMOEulerVariable : public CFlowVariable {
   struct CIndices {
     const IndexType nDim, nSpecies;
     CIndices(IndexType ndim, IndexType nspecies) : nDim(ndim), nSpecies(nspecies) {}
+    inline IndexType NDim() const {return nDim;}
+    inline IndexType NSpecies() const {return nSpecies;}
     inline IndexType SpeciesDensities() const {return 0;}
     inline IndexType Temperature() const {return nSpecies;}
     inline IndexType Temperature_ve() const {return nSpecies+1;}
@@ -61,6 +63,7 @@ class CNEMOEulerVariable : public CFlowVariable {
     inline IndexType LaminarViscosity() const {return nSpecies+nDim+8;}
     inline IndexType EddyViscosity() const {return nSpecies+nDim+9;}
 
+    inline IndexType CpTotal() const {return std::numeric_limits<IndexType>::max();}
     inline IndexType ThermalConductivity() const {return std::numeric_limits<IndexType>::max();}
   };
 
diff --git a/SU2_CFD/include/variables/CPrimitiveIndices.hpp b/SU2_CFD/include/variables/CPrimitiveIndices.hpp
index c07643a7139..77878eff6cb 100644
--- a/SU2_CFD/include/variables/CPrimitiveIndices.hpp
+++ b/SU2_CFD/include/variables/CPrimitiveIndices.hpp
@@ -28,6 +28,9 @@
 
 #include <cstdint>
 #include <cstring>
+#include <map>
+#include <string>
+
 #include "CEulerVariable.hpp"
 #include "CIncEulerVariable.hpp"
 #include "CNEMOEulerVariable.hpp"
@@ -67,6 +70,9 @@ struct CPrimitiveIndices {
       return reinterpret_cast<const CEulerVariable::template CIndices<IndexType>*>(data_)->NAME();      \
     }                                                                                                   \
   }
+  GET_INDEX_IMPL(NDim)
+  GET_INDEX_IMPL(NSpecies)
+  GET_INDEX_IMPL(SpeciesDensities)
   GET_INDEX_IMPL(Temperature)
   GET_INDEX_IMPL(Velocity)
   GET_INDEX_IMPL(Pressure)
@@ -78,6 +84,7 @@ struct CPrimitiveIndices {
   GET_INDEX_IMPL(ThermalConductivity)
   GET_INDEX_IMPL(CpTotal)
   GET_INDEX_IMPL(Temperature_ve)
+#undef GET_INDEX_IMPL
 
  private:
   template <class ConcreteIndices>
@@ -89,4 +96,37 @@ struct CPrimitiveIndices {
 
   alignas(sizeof(IndexType)) char data_[2 * sizeof(IndexType)]{};  /*!< \brief Space for the largest CIndices class. */
   uint8_t type_;
-};
\ No newline at end of file
+};
+
+/*!
+ * \brief Maps primitive variable names to their indices based on a CPrimitiveIndices object.
+ * \note The variables names we try to map here must be kept in sync with CPrimitiveIndices.
+ * All index classes should use numeric_limits::max for variables that are not available.
+ */
+template <class IndexType>
+std::map<std::string, IndexType> PrimitiveNameToIndexMap(const CPrimitiveIndices<IndexType>& idx) {
+  std::map<std::string, IndexType> nameToIndex;
+  const auto notAvailable = std::numeric_limits<IndexType>::max();
+#define INSERT_VAR_INDEX_PAIR(STRING, FUNCTION) \
+  if (idx.FUNCTION() != notAvailable) nameToIndex[STRING] = idx.FUNCTION();
+  INSERT_VAR_INDEX_PAIR("TEMPERATURE", Temperature)
+  INSERT_VAR_INDEX_PAIR("TEMPERATURE_VE", Temperature_ve)
+  INSERT_VAR_INDEX_PAIR("PRESSURE", Pressure)
+  INSERT_VAR_INDEX_PAIR("DENSITY", Density)
+  INSERT_VAR_INDEX_PAIR("ENTHALPY", Enthalpy)
+  INSERT_VAR_INDEX_PAIR("SOUND_SPEED", SoundSpeed)
+  INSERT_VAR_INDEX_PAIR("LAMINAR_VISCOSITY", LaminarViscosity)
+  INSERT_VAR_INDEX_PAIR("EDDY_VISCOSITY", EddyViscosity)
+  INSERT_VAR_INDEX_PAIR("THERMAL_CONDUCTIVITY", ThermalConductivity)
+  INSERT_VAR_INDEX_PAIR("CP_TOTAL", CpTotal)
+#undef INSERT_VAR_INDEX_PAIR
+  nameToIndex["VELOCITY_X"] = idx.Velocity();
+  nameToIndex["VELOCITY_Y"] = idx.Velocity() + 1;
+  if (idx.NDim() == 3) {
+    nameToIndex["VELOCITY_Z"] = idx.Velocity() + 2;
+  }
+  for (IndexType iSpecies = 0; iSpecies < idx.NSpecies(); ++iSpecies) {
+    nameToIndex["DENSITY_" + std::to_string(iSpecies)] = idx.SpeciesDensities() + iSpecies;
+  }
+  return nameToIndex;
+}
diff --git a/SU2_CFD/include/variables/CVariable.hpp b/SU2_CFD/include/variables/CVariable.hpp
index f80faebdd10..df6026a71c2 100644
--- a/SU2_CFD/include/variables/CVariable.hpp
+++ b/SU2_CFD/include/variables/CVariable.hpp
@@ -2042,6 +2042,11 @@ class CVariable {
    */
   inline virtual const su2double *GetMesh_Coord(unsigned long iPoint) const { return nullptr; }
 
+  /*!
+   * \brief A virtual member. Get the undeformed coordinates for the entire domain.
+   */
+  inline virtual const MatrixType *GetMesh_Coord() const { return nullptr; }
+
   /*!
    * \brief A virtual member. Set the value of the undeformed coordinates.
    * \param[in] iDim - Index of Mesh_Coord[nDim]
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index b13afb6e27f..c00d02c5456 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -29,6 +29,7 @@
 
 #include "../../../Common/include/geometry/CPhysicalGeometry.hpp"
 #include "../../../Common/include/toolboxes/geometry_toolbox.hpp"
+#include "../../include/variables/CPrimitiveIndices.hpp"
 
 using namespace std;
 
@@ -178,46 +179,6 @@ bool CDriverBase::GetNodeDomain(unsigned long iPoint) const {
   return main_geometry->nodes->GetDomain(iPoint);
 }
 
-vector<passivedouble> CDriverBase::GetInitialCoordinates(unsigned long iPoint) const {
-  if (iPoint >= GetNumberNodes()) {
-    SU2_MPI::Error("Node index exceeds mesh size.", CURRENT_FUNCTION);
-  }
-  vector<passivedouble> values(nDim, 0.0);
-
-  if (main_config->GetDeform_Mesh()) {
-    for (auto iDim = 0u; iDim < nDim; iDim++) {
-      const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord(iPoint, iDim);
-      values[iDim] = SU2_TYPE::GetValue(value);
-    }
-  }
-  return values;
-}
-
-vector<passivedouble> CDriverBase::GetCoordinates(unsigned long iPoint) const {
-  if (iPoint >= GetNumberNodes()) {
-    SU2_MPI::Error("Node index exceeds mesh size.", CURRENT_FUNCTION);
-  }
-  vector<passivedouble> values;
-
-  for (auto iDim = 0u; iDim < nDim; iDim++) {
-    const su2double value = main_geometry->nodes->GetCoord(iPoint, iDim);
-    values.push_back(SU2_TYPE::GetValue(value));
-  }
-  return values;
-}
-
-void CDriverBase::SetCoordinates(unsigned long iPoint, vector<passivedouble> values) {
-  if (iPoint >= GetNumberNodes()) {
-    SU2_MPI::Error("Node index exceeds mesh size.", CURRENT_FUNCTION);
-  }
-  if (values.size() != nDim) {
-    SU2_MPI::Error("Invalid number of dimensions!", CURRENT_FUNCTION);
-  }
-  for (auto iDim = 0u; iDim < nDim; iDim++) {
-    main_geometry->nodes->SetCoord(iPoint, iDim, values[iDim]);
-  }
-}
-
 unsigned short CDriverBase::GetNumberMarkers() const { return main_config->GetnMarker_All(); }
 
 map<string, unsigned short> CDriverBase::GetMarkerIndices() const {
@@ -431,3 +392,24 @@ void CDriverBase::CommunicateMeshDisplacements(void) {
   solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->InitiateComms(main_geometry, main_config, MESH_DISPLACEMENTS);
   solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->CompleteComms(main_geometry, main_config, MESH_DISPLACEMENTS);
 }
+
+map<string, unsigned short> CDriverBase::GetSolverIndices() const {
+  map<string, unsigned short> indexMap;
+  for (auto iSol = 0u; iSol < MAX_SOLS; iSol++) {
+    const auto* solver = solver_container[ZONE_0][INST_0][MESH_0][iSol];
+    if (solver != nullptr) {
+      if (solver->GetSolverName().empty()) SU2_MPI::Error("Solver name was not defined.", CURRENT_FUNCTION);
+      indexMap[solver->GetSolverName()] = iSol;
+    }
+  }
+  return indexMap;
+}
+
+map<string, unsigned short> CDriverBase::GetPrimitiveIndices() const {
+  if (solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL] == nullptr) {
+    SU2_MPI::Error("The flow solver does not exist.", CURRENT_FUNCTION);
+  }
+  return PrimitiveNameToIndexMap(CPrimitiveIndices<unsigned short>(
+      main_config->GetKind_Regime() == ENUM_REGIME::INCOMPRESSIBLE,
+      main_config->GetNEMOProblem(), nDim, main_config->GetnSpecies()));
+}
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index d24bedd03bf..ea62d779f52 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -33,9 +33,7 @@
 #include "../../../Common/include/geometry/CGeometry.hpp"
 #include "../../../Common/include/toolboxes/geometry_toolbox.hpp"
 #include "../../include/solvers/CSolver.hpp"
-#include "../../include/variables/CEulerVariable.hpp"
-#include "../../include/variables/CIncEulerVariable.hpp"
-#include "../../include/variables/CNEMOEulerVariable.hpp"
+#include "../../include/variables/CPrimitiveIndices.hpp"
 #include "../../include/fluid/CCoolProp.hpp"
 
 CFlowOutput::CFlowOutput(const CConfig *config, unsigned short nDim, bool fem_output) :
@@ -747,6 +745,63 @@ void CFlowOutput::SetAnalyzeSurface_SpeciesVariance(const CSolver* const*solver,
   SetHistoryOutputValue("SURFACE_SPECIES_VARIANCE", Tot_Surface_SpeciesVariance);
 }
 
+void CFlowOutput::ConvertVariableSymbolsToIndices(const CPrimitiveIndices<unsigned long>& idx,
+                                                  CustomOutput& output) const {
+  const auto nameToIndex = PrimitiveNameToIndexMap(idx);
+
+  std::stringstream knownVariables;
+  for (const auto& items : nameToIndex) {
+    knownVariables << items.first + '\n';
+  }
+  knownVariables << "TURB[0,1,...]\nRAD[0,1,...]\nSPECIES[0,1,...]\n";
+
+  auto IndexOfVariable = [](const map<std::string, unsigned long>& nameToIndex, const std::string& var) {
+    /*--- Primitives of the flow solver. ---*/
+    const auto flowOffset = FLOW_SOL * CustomOutput::MAX_VARS_PER_SOLVER;
+    const auto it = nameToIndex.find(var);
+    if (it != nameToIndex.end()) return flowOffset + it->second;
+
+    /*--- Index-based (no name) access to variables of other solvers. ---*/
+    auto GetIndex = [](const std::string& s, int nameLen) {
+      /*--- Extract an int from "name[int]", nameLen is the length of "name". ---*/
+      return std::stoi(std::string(s.begin() + nameLen + 1, s.end() - 1));
+    };
+    if (var.rfind("SPECIES", 0) == 0) return SPECIES_SOL * CustomOutput::MAX_VARS_PER_SOLVER + GetIndex(var, 7);
+    if (var.rfind("TURB", 0) == 0) return TURB_SOL * CustomOutput::MAX_VARS_PER_SOLVER + GetIndex(var, 4);
+    if (var.rfind("RAD", 0) == 0) return RAD_SOL * CustomOutput::MAX_VARS_PER_SOLVER + GetIndex(var, 3);
+
+    return CustomOutput::NOT_A_VARIABLE;
+  };
+
+  output.otherOutputs.clear();
+  output.varIndices.clear();
+  output.varIndices.reserve(output.varSymbols.size());
+
+  for (const auto& var : output.varSymbols) {
+    output.varIndices.push_back(IndexOfVariable(nameToIndex, var));
+
+    if (output.type == OperationType::FUNCTION && output.varIndices.back() != CustomOutput::NOT_A_VARIABLE) {
+      SU2_MPI::Error("Custom outputs of type 'Function' cannot reference solver variables.", CURRENT_FUNCTION);
+    }
+    /*--- Symbol is a valid solver variable. ---*/
+    if (output.varIndices.back() < CustomOutput::NOT_A_VARIABLE) continue;
+
+    /*--- An index above NOT_A_VARIABLE is not valid with current solver settings. ---*/
+    if (output.varIndices.back() > CustomOutput::NOT_A_VARIABLE) {
+      SU2_MPI::Error("Inactive solver variable (" + var + ") used in function " + output.name + "\n"
+                      "E.g. this may only be a variable of the compressible solver.", CURRENT_FUNCTION);
+    }
+
+    /*--- An index equal to NOT_A_VARIABLE may refer to a history output. ---*/
+    output.varIndices.back() += output.otherOutputs.size();
+    output.otherOutputs.push_back(GetPtrToHistoryOutput(var));
+    if (output.otherOutputs.back() == nullptr) {
+      SU2_MPI::Error("Invalid history output or solver variable (" + var + ") used in function " + output.name +
+                     "\nValid solvers variables:\n" + knownVariables.str(), CURRENT_FUNCTION);
+    }
+  }
+}
+
 void CFlowOutput::SetCustomOutputs(const CSolver* const* solver, const CGeometry *geometry, const CConfig *config) {
 
   const bool axisymmetric = config->GetAxisymmetric();
@@ -755,17 +810,10 @@ void CFlowOutput::SetCustomOutputs(const CSolver* const* solver, const CGeometry
   for (auto& output : customOutputs) {
     if (output.varIndices.empty()) {
       /*--- Setup indices for the symbols in the expression. ---*/
+      const auto primIdx = CPrimitiveIndices<unsigned long>(config->GetKind_Regime() == ENUM_REGIME::INCOMPRESSIBLE,
+          config->GetNEMOProblem(), nDim, config->GetnSpecies());
+      ConvertVariableSymbolsToIndices(primIdx, output);
 
-      if (config->GetNEMOProblem()) {
-        ConvertVariableSymbolsToIndices(
-            CNEMOEulerVariable::template CIndices<unsigned long>(nDim, config->GetnSpecies()), output);
-      } else if (config->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE) {
-        ConvertVariableSymbolsToIndices(CEulerVariable::template CIndices<unsigned long>(nDim, 0), output);
-      } else if (config->GetKind_Regime() == ENUM_REGIME::INCOMPRESSIBLE) {
-        ConvertVariableSymbolsToIndices(CIncEulerVariable::template CIndices<unsigned long>(nDim, 0), output);
-      } else {
-        SU2_MPI::Error("Unknown flow solver type.", CURRENT_FUNCTION);
-      }
       /*--- Convert marker names to their index (if any) in this rank. Or probe locations to nearest points. ---*/
 
       if (output.type != OperationType::PROBE) {
diff --git a/SU2_CFD/src/solvers/CAdjEulerSolver.cpp b/SU2_CFD/src/solvers/CAdjEulerSolver.cpp
index fde3afc43fa..e16446e7785 100644
--- a/SU2_CFD/src/solvers/CAdjEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CAdjEulerSolver.cpp
@@ -345,6 +345,7 @@ CAdjEulerSolver::CAdjEulerSolver(CGeometry *geometry, CConfig *config, unsigned
   InitiateComms(geometry, config, SOLUTION);
   CompleteComms(geometry, config, SOLUTION);
 
+  SolverName = "ADJ.FLOW";
 }
 
 CAdjEulerSolver::~CAdjEulerSolver(void) {
diff --git a/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp b/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
index 025cb20e82e..e82e61288a2 100644
--- a/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
+++ b/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
@@ -126,6 +126,7 @@ CDiscAdjFEASolver::CDiscAdjFEASolver(CGeometry *geometry, CConfig *config, CSolv
 
   if (fea_dv) ReadDV(config);
 
+  SolverName = "ADJ.FEA";
 }
 
 CDiscAdjFEASolver::~CDiscAdjFEASolver() { delete nodes; }
diff --git a/SU2_CFD/src/solvers/CDiscAdjMeshSolver.cpp b/SU2_CFD/src/solvers/CDiscAdjMeshSolver.cpp
index d676990d8df..ff92a04d544 100644
--- a/SU2_CFD/src/solvers/CDiscAdjMeshSolver.cpp
+++ b/SU2_CFD/src/solvers/CDiscAdjMeshSolver.cpp
@@ -80,6 +80,7 @@ CDiscAdjMeshSolver::CDiscAdjMeshSolver(CGeometry *geometry, CConfig *config, CSo
   }
   static_cast<CDiscAdjMeshBoundVariable*>(nodes)->AllocateBoundaryVariables(config);
 
+  SolverName = "ADJ.MESH";
 }
 
 CDiscAdjMeshSolver::~CDiscAdjMeshSolver() { delete nodes; }
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index f44f76817fa..97fa79e6d15 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -326,7 +326,7 @@ CEulerSolver::CEulerSolver(CGeometry *geometry, CConfig *config,
 
   CommunicateInitialState(geometry, config);
 
-  /*--- Add the solver name (max 8 characters). ---*/
+  /*--- Add the solver name.. ---*/
   SolverName = "C.FLOW";
 
   /*--- Finally, check that the static arrays will be large enough (keep this
diff --git a/SU2_CFD/src/solvers/CFEASolver.cpp b/SU2_CFD/src/solvers/CFEASolver.cpp
index 69b93a180e3..4f30cb91450 100644
--- a/SU2_CFD/src/solvers/CFEASolver.cpp
+++ b/SU2_CFD/src/solvers/CFEASolver.cpp
@@ -211,7 +211,7 @@ CFEASolver::CFEASolver(CGeometry *geometry, CConfig *config) : CFEASolverBase(ge
     Set_VertexEliminationSchedule(geometry, essentialMarkers);
   }
 
-  /*--- Add the solver name (max 8 characters) ---*/
+  /*--- Add the solver name. ---*/
   SolverName = "FEA";
 }
 
diff --git a/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp b/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
index 7acc893e986..1a12467366a 100644
--- a/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
@@ -723,8 +723,8 @@ CFEM_DG_EulerSolver::CFEM_DG_EulerSolver(CGeometry *geometry, CConfig *config, u
      the tasks to be done for one space time step. */
   SetUpTaskList(config);
 
-  /*--- Add the solver name (max 8 characters) ---*/
-  SolverName = "DG FLOW";
+  /*--- Add the solver name. ---*/
+  SolverName = "DG.FLOW";
 }
 
 CFEM_DG_EulerSolver::~CFEM_DG_EulerSolver(void) {
diff --git a/SU2_CFD/src/solvers/CHeatSolver.cpp b/SU2_CFD/src/solvers/CHeatSolver.cpp
index a7a3b1e30d3..aeefcfd75f0 100644
--- a/SU2_CFD/src/solvers/CHeatSolver.cpp
+++ b/SU2_CFD/src/solvers/CHeatSolver.cpp
@@ -167,7 +167,7 @@ CHeatSolver::CHeatSolver(CGeometry *geometry, CConfig *config, unsigned short iM
   Max_CFL_Local = CFL;
   Avg_CFL_Local = CFL;
 
-  /*--- Add the solver name (max 8 characters) ---*/
+  /*--- Add the solver name. ---*/
 
   SolverName = "HEAT";
 }
diff --git a/SU2_CFD/src/solvers/CIncEulerSolver.cpp b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
index 1749ae096f2..19b620825e1 100644
--- a/SU2_CFD/src/solvers/CIncEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
@@ -221,7 +221,7 @@ CIncEulerSolver::CIncEulerSolver(CGeometry *geometry, CConfig *config, unsigned
   if (config->GetBounded_Scalar())
     EdgeMassFluxes.resize(geometry->GetnEdge()) = su2double(0.0);
 
-  /*--- Add the solver name (max 8 characters) ---*/
+  /*--- Add the solver name. ---*/
   SolverName = "INC.FLOW";
 
   /*--- Finally, check that the static arrays will be large enough (keep this
diff --git a/SU2_CFD/src/solvers/CMeshSolver.cpp b/SU2_CFD/src/solvers/CMeshSolver.cpp
index 57b4b25edb7..d9fdecb9f06 100644
--- a/SU2_CFD/src/solvers/CMeshSolver.cpp
+++ b/SU2_CFD/src/solvers/CMeshSolver.cpp
@@ -165,6 +165,8 @@ CMeshSolver::CMeshSolver(CGeometry *geometry, CConfig *config) : CFEASolver(LINE
     }
     Set_VertexEliminationSchedule(geometry, essentialMarkers);
   }
+
+  SolverName = "MESH";
 }
 
 void CMeshSolver::SetMinMaxVolume(CGeometry *geometry, CConfig *config, bool updated) {
diff --git a/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp b/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
index f02f064ff1d..c82685c752a 100644
--- a/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
@@ -216,7 +216,7 @@ CNEMOEulerSolver::CNEMOEulerSolver(CGeometry *geometry, CConfig *config,
 
   CommunicateInitialState(geometry, config);
 
-  /*--- Add the solver name (max 8 characters) ---*/
+  /*--- Add the solver name. ---*/
   SolverName = "NEMO.FLOW";
 
   /*--- Finally, check that the static arrays will be large enough (keep this
diff --git a/SU2_CFD/src/solvers/CRadP1Solver.cpp b/SU2_CFD/src/solvers/CRadP1Solver.cpp
index f25d41fa945..e1f6ef80d1f 100644
--- a/SU2_CFD/src/solvers/CRadP1Solver.cpp
+++ b/SU2_CFD/src/solvers/CRadP1Solver.cpp
@@ -127,6 +127,7 @@ CRadP1Solver::CRadP1Solver(CGeometry* geometry, CConfig *config) : CRadSolver(ge
    SetVolumetricHeatSource(geometry, config);
   }
 
+  SolverName = "RAD";
 }
 
 CRadP1Solver::~CRadP1Solver(void) {
diff --git a/SU2_CFD/src/solvers/CSpeciesSolver.cpp b/SU2_CFD/src/solvers/CSpeciesSolver.cpp
index 690de424eee..16e069ed9bd 100644
--- a/SU2_CFD/src/solvers/CSpeciesSolver.cpp
+++ b/SU2_CFD/src/solvers/CSpeciesSolver.cpp
@@ -167,7 +167,7 @@ CSpeciesSolver::CSpeciesSolver(CGeometry* geometry, CConfig* config, unsigned sh
   Max_CFL_Local = CFL;
   Avg_CFL_Local = CFL;
 
-  /*--- Add the solver name (max 8 characters) ---*/
+  /*--- Add the solver name. ---*/
   SolverName = "SPECIES";
 }
 
diff --git a/SU2_CFD/src/solvers/CTransLMSolver.cpp b/SU2_CFD/src/solvers/CTransLMSolver.cpp
index 209f07c87c8..bd412a283a5 100644
--- a/SU2_CFD/src/solvers/CTransLMSolver.cpp
+++ b/SU2_CFD/src/solvers/CTransLMSolver.cpp
@@ -167,7 +167,7 @@ CTransLMSolver::CTransLMSolver(CGeometry *geometry, CConfig *config, unsigned sh
   Max_CFL_Local = CFL;
   Avg_CFL_Local = CFL;
 
-  /*--- Add the solver name (max 8 characters) ---*/
+  /*--- Add the solver name. ---*/
   SolverName = "LM model";
 
 }
diff --git a/SU2_CFD/src/solvers/CTurbSASolver.cpp b/SU2_CFD/src/solvers/CTurbSASolver.cpp
index adb7ac7c009..a342fa2b3a0 100644
--- a/SU2_CFD/src/solvers/CTurbSASolver.cpp
+++ b/SU2_CFD/src/solvers/CTurbSASolver.cpp
@@ -166,7 +166,7 @@ CTurbSASolver::CTurbSASolver(CGeometry *geometry, CConfig *config, unsigned shor
   Max_CFL_Local = CFL;
   Avg_CFL_Local = CFL;
 
-  /*--- Add the solver name (max 8 characters) ---*/
+  /*--- Add the solver name. ---*/
   SolverName = "SA";
 
 }
diff --git a/SU2_CFD/src/solvers/CTurbSSTSolver.cpp b/SU2_CFD/src/solvers/CTurbSSTSolver.cpp
index f9fdd16dffb..3918c07fba4 100644
--- a/SU2_CFD/src/solvers/CTurbSSTSolver.cpp
+++ b/SU2_CFD/src/solvers/CTurbSSTSolver.cpp
@@ -179,8 +179,8 @@ CTurbSSTSolver::CTurbSSTSolver(CGeometry *geometry, CConfig *config, unsigned sh
   Max_CFL_Local = CFL;
   Avg_CFL_Local = CFL;
 
-  /*--- Add the solver name (max 8 characters) ---*/
-  SolverName = "K-W SST";
+  /*--- Add the solver name. ---*/
+  SolverName = "SST";
 
 }
 
diff --git a/SU2_PY/FSI_tools/FSIInterface.py b/SU2_PY/FSI_tools/FSIInterface.py
index 99bab9afe9a..88c030ff6a0 100644
--- a/SU2_PY/FSI_tools/FSIInterface.py
+++ b/SU2_PY/FSI_tools/FSIInterface.py
@@ -569,10 +569,10 @@ def interfaceMapping(self,FluidSolver, SolidSolver, FSI_config):
             iPoint = FluidSolver.GetMarkerNode(self.fluidInterfaceIdentifier, iVertex)
             GlobalIndex = FluidSolver.GetNodeGlobalIndex(iPoint)
             if self.nDim == 2:
-                posx, posy = FluidSolver.GetInitialCoordinates(iPoint)
+                posx, posy = FluidSolver.InitialCoordinates().Get(iPoint)
                 posz = 0
             else:
-                posx, posy, posz = FluidSolver.GetInitialCoordinates(iPoint)
+                posx, posy, posz = FluidSolver.InitialCoordinates().Get(iPoint)
             if GlobalIndex not in self.FluidHaloNodeList[myid].keys():
               fluidIndexing_temp[GlobalIndex] = self.__getGlobalIndex('fluid', myid, localIndex)
               self.localFluidInterface_array_X_init[localIndex] = posx
diff --git a/SU2_PY/pySU2/pySU2.i b/SU2_PY/pySU2/pySU2.i
index a05049798b7..f783c324335 100644
--- a/SU2_PY/pySU2/pySU2.i
+++ b/SU2_PY/pySU2/pySU2.i
@@ -37,13 +37,13 @@ directors="1",
 threads="1"
 ) pysu2
 %{
+#include "../../Common/include/containers/CPyWrapperMatrixView.hpp"
 #include "../../SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CDriverBase.hpp"
 #include "../../SU2_CFD/include/drivers/CMultizoneDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
 #include "../../SU2_DEF/include/drivers/CDeformationDriver.hpp"
-
 %}
 
 // ----------- USED MODULES ------------
@@ -53,6 +53,7 @@ threads="1"
 
 %include "std_string.i"
 %include "std_vector.i"
+%include "std_pair.i"
 %include "std_map.i"
 %include "typemaps.i"
 //%include "numpy.i"
@@ -65,12 +66,11 @@ namespace std {
    %template() vector<bool>;
    %template() vector<unsigned short>;
    %template() vector<unsigned long>;
-   %template() vector<vector<unsigned long>>;
    %template() vector<double>;
-   %template() vector<vector<double>>;
    %template() vector<string>;
    %template() map<string, unsigned short>;
    %template() map<string, string>;
+   %template() pair<unsigned long, unsigned long>;
 }
 
 // ----------- API CLASSES ----------------
@@ -92,6 +92,7 @@ const unsigned int MESH_1 = 1; /*!< \brief Definition of the finest grid level.
 const unsigned int ZONE_0 = 0; /*!< \brief Definition of the first grid domain. */
 const unsigned int ZONE_1 = 1; /*!< \brief Definition of the first grid domain. */
 
+%include "../../Common/include/containers/CPyWrapperMatrixView.hpp"
 %include "../../SU2_CFD/include/drivers/CDriverBase.hpp"
 %include "../../SU2_CFD/include/drivers/CDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
diff --git a/SU2_PY/pySU2/pySU2ad.i b/SU2_PY/pySU2/pySU2ad.i
index cba62127e92..8bca85fdd2d 100644
--- a/SU2_PY/pySU2/pySU2ad.i
+++ b/SU2_PY/pySU2/pySU2ad.i
@@ -37,13 +37,13 @@ directors="1",
 threads="1"
 ) pysu2ad
 %{
+#include "../../Common/include/containers/CPyWrapperMatrixView.hpp"
 #include "../../SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CDriverBase.hpp"
 #include "../../SU2_CFD/include/drivers/CMultizoneDriver.hpp"
 #include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
 #include "../../SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp"
-
 %}
 
 // ----------- USED MODULES ------------
@@ -53,6 +53,7 @@ threads="1"
 
 %include "std_string.i"
 %include "std_vector.i"
+%include "std_pair.i"
 %include "std_map.i"
 %include "typemaps.i"
 //%include "numpy.i"
@@ -63,13 +64,13 @@ threads="1"
 
 namespace std {
    %template() vector<bool>;
+   %template() vector<unsigned short>;
    %template() vector<unsigned long>;
-   %template() vector<vector<unsigned long>>;
    %template() vector<double>;
-   %template() vector<vector<double>>;
    %template() vector<string>;
    %template() map<string, unsigned short>;
    %template() map<string, string>;
+   %template() pair<unsigned long, unsigned long>;
 }
 
 // ----------- API CLASSES ----------------
@@ -91,6 +92,7 @@ const unsigned int MESH_1 = 1; /*!< \brief Definition of the finest grid level.
 const unsigned int ZONE_0 = 0; /*!< \brief Definition of the first grid domain. */
 const unsigned int ZONE_1 = 1; /*!< \brief Definition of the first grid domain. */
 
+%include "../../Common/include/containers/CPyWrapperMatrixView.hpp"
 %include "../../SU2_CFD/include/drivers/CDriverBase.hpp"
 %include "../../SU2_CFD/include/drivers/CDriver.hpp"
 %include "../../SU2_CFD/include/drivers/CSinglezoneDriver.hpp"
diff --git a/TestCases/py_wrapper/deforming_bump_in_channel/run.py b/TestCases/py_wrapper/deforming_bump_in_channel/run.py
index 6c43adba109..f10932b9a13 100755
--- a/TestCases/py_wrapper/deforming_bump_in_channel/run.py
+++ b/TestCases/py_wrapper/deforming_bump_in_channel/run.py
@@ -52,17 +52,17 @@ def main():
   TimeIter = SU2Driver.GetTime_Iter()
   nTimeIter = SU2Driver.GetnTimeIter()
   time = TimeIter * deltaT
-  
+
   # Extract the initial position of each node on the moving marker.
   CoordX = np.zeros(nVertex)
   CoordY = np.zeros(nVertex)
   for iVertex in range(nVertex):
     iPoint = SU2Driver.GetMarkerNode(MarkerID, iVertex)
-    CoordX[iVertex], CoordY[iVertex] = SU2Driver.GetInitialCoordinates(iPoint)
+    CoordX[iVertex], CoordY[iVertex] = SU2Driver.InitialCoordinates().Get(iPoint)
 
   if rank == 0:
     print("\n------------------------------ Begin Solver -----------------------------\n")
-  
+
   # The time loop is defined in Python so that we have acces to SU2 functionalities at each time step.
   while (TimeIter < nTimeIter):
     # Apply the surface deformation.
@@ -72,12 +72,12 @@ def main():
 
     # Time iteration preprocessing.
     SU2Driver.Preprocess(TimeIter)
-    
+
     # Run one time iteration (e.g. dual-time).
     SU2Driver.Run()
     SU2Driver.Postprocess()
     SU2Driver.Update()
-    
+
     # Monitor the solver and output solution to file if required.
     stopCalc = SU2Driver.Monitor(TimeIter)
     SU2Driver.Output(TimeIter)
diff --git a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
index 37e7a1127f6..718fbfd8cb1 100755
--- a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
+++ b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
@@ -102,7 +102,7 @@ def main():
   CoordY = np.zeros(nVertex_MovingMarker)
   for iVertex in range(nVertex_MovingMarker):
     iPoint = SU2Driver.GetMarkerNode(MovingMarkerID, iVertex)
-    CoordX[iVertex], CoordY[iVertex] = SU2Driver.GetInitialCoordinates(iPoint)
+    CoordX[iVertex], CoordY[iVertex] = SU2Driver.InitialCoordinates().Get(iPoint)
 
   # Time loop is defined in Python so that we have acces to SU2 functionalities at each time step
   if rank == 0:
diff --git a/meson.build b/meson.build
index 84999a5476b..60b30d9ba23 100644
--- a/meson.build
+++ b/meson.build
@@ -202,10 +202,10 @@ elif get_option('enable-openblas')
 endif
 
 if get_option('enable-librom')
-   
+
    assert(get_option('librom_root')!='',
        'Must specify librom folder (-Dlibrom_root=path/to/libROM)')
-   
+
    su2_cpp_args += '-DHAVE_LIBROM'
 
    librom_root = get_option('librom_root')
@@ -292,7 +292,7 @@ message('''---------------------------------------------------------------------
          |   |___/\___//___|   Meson Configuration Summary                       |
          |                                                                       |
          -------------------------------------------------------------------------
-         
+
          Option          Value
          ---------------------
          TecIO:          @2@
@@ -336,7 +336,7 @@ if get_option('enable-librom')
   message(''' To run SU2 with libROM library, add this line to your .bashrc file:
 
           export LD_LIBRARY_PATH=@0@/build/:$LD_LIBRARY_PATH
-          
+
           '''.format(get_option('librom_root')))
 
 endif

From 9d5a0ada94ea30dea8d9956a4a088062d317f7df Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 1 Mar 2023 11:22:44 +0100
Subject: [PATCH 245/656] CoDiPack update.

---
 externals/codi        | 2 +-
 meson_scripts/init.py | 2 +-
 2 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/externals/codi b/externals/codi
index fd58ba98a93..76a63ec8805 160000
--- a/externals/codi
+++ b/externals/codi
@@ -1 +1 @@
-Subproject commit fd58ba98a937778eed69d539c9cc9235ab38358c
+Subproject commit 76a63ec8805eee146b1a5f6629676d3e78383f9e
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index ce4c67d6f88..5f4afec2522 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -44,7 +44,7 @@ def init_submodules(method = 'auto'):
 
   # This information of the modules is used if projects was not cloned using git
   # The sha tag must be maintained manually to point to the correct commit
-  sha_version_codi = 'fd58ba98a937778eed69d539c9cc9235ab38358c'
+  sha_version_codi = '76a63ec8805eee146b1a5f6629676d3e78383f9e'
   github_repo_codi = 'https://github.com/scicompkl/CoDiPack'
   sha_version_medi = '6aef76912e7099c4f08c9705848797ca9e8070da'
   github_repo_medi = 'https://github.com/SciCompKL/MeDiPack'

From 7340aa9acd1d75a8e4a30ec31056b6106dc2bdfb Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 1 Mar 2023 16:01:50 +0100
Subject: [PATCH 246/656] Restructure external function code.

---
 Common/include/basic_types/ad_structure.hpp |  26 +--
 Common/src/basic_types/ad_structure.cpp     |   9 +
 Common/src/linear_algebra/CSysSolve.cpp     | 178 ++++++++++----------
 SU2_CFD/src/SU2_CFD.cpp                     |   6 +
 SU2_DOT/src/SU2_DOT.cpp                     |   8 +
 5 files changed, 113 insertions(+), 114 deletions(-)

diff --git a/Common/include/basic_types/ad_structure.hpp b/Common/include/basic_types/ad_structure.hpp
index 4bccac805a6..445cf7c2269 100644
--- a/Common/include/basic_types/ad_structure.hpp
+++ b/Common/include/basic_types/ad_structure.hpp
@@ -185,13 +185,6 @@ namespace AD{
    */
   inline void EndPreacc() {}
 
-  /*!
-   * \brief Initializes an externally differentiated function. Input and output variables are set with SetExtFuncIn/SetExtFuncOut
-   * \param[in] storePrimalInput - Specifies whether the primal input values are stored for the reverse call of the external function.
-   * \param[in] storePrimalOutput - Specifies whether the primal output values are stored for the reverse call of the external function.
-   */
-  inline void StartExtFunc(bool storePrimalInput, bool storePrimalOutput) {}
-
   /*!
    * \brief Sets the scalar input of a externally differentiated function.
    * \param[in] data - the scalar input variable.
@@ -238,11 +231,6 @@ namespace AD{
   template<class T>
   inline void SetExtFuncOut(T&& data, const int size_x, const int size_y) {}
 
-  /*!
-   * \brief Ends an external function section by deleting the structures.
-   */
-  inline void EndExtFunc() {}
-
   /*!
    * \brief Evaluates and saves gradient data from a variable.
    * \param[in] data - variable whose gradient information will be extracted.
@@ -491,15 +479,6 @@ namespace AD{
     }
   }
 
-  FORCEINLINE void StartExtFunc(bool storePrimalInput, bool storePrimalOutput){
-    if (!storePrimalInput){
-      FuncHelper.disableInputPrimalStore();
-    }
-    if (!storePrimalOutput){
-      FuncHelper.disableOutputPrimalStore();
-    }
-  }
-
   FORCEINLINE void SetExtFuncIn(const su2double &data) {
     FuncHelper.addInput(data);
   }
@@ -551,8 +530,6 @@ namespace AD{
     checkpoint->clear();
   }
 
-  FORCEINLINE void EndExtFunc() { }
-
   FORCEINLINE bool BeginPassive() {
     if(AD::getTape().isActive()) {
       StopRecording();
@@ -590,6 +567,9 @@ namespace AD{
   }
 #endif // CODI_REVERSE_TYPE
 
+  void Initialize();
+  void Finalize();
+
 } // namespace AD
 
 
diff --git a/Common/src/basic_types/ad_structure.cpp b/Common/src/basic_types/ad_structure.cpp
index b7d3dc7c59d..90d625a5ea7 100644
--- a/Common/src/basic_types/ad_structure.cpp
+++ b/Common/src/basic_types/ad_structure.cpp
@@ -49,4 +49,13 @@ namespace AD {
   ExtFuncHelper FuncHelper;
 
 #endif
+
+  void Initialize() {
+#ifdef CODI_REVERSE_TYPE
+    FuncHelper.disableInputPrimalStore();
+    FuncHelper.disableOutputPrimalStore();
+#endif
+  }
+
+  void Finalize() {}
 }
diff --git a/Common/src/linear_algebra/CSysSolve.cpp b/Common/src/linear_algebra/CSysSolve.cpp
index 0938136a889..691ae822918 100644
--- a/Common/src/linear_algebra/CSysSolve.cpp
+++ b/Common/src/linear_algebra/CSysSolve.cpp
@@ -866,127 +866,123 @@ unsigned long CSysSolve<ScalarType>::Solve(CSysMatrix<ScalarType> & Jacobian, co
 
     TapeActive = AD::TapeActive();
 
+    /*--- Declare external function inputs, outputs, and data ---*/
     BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
-      AD::StartExtFunc(false, false);
       AD::SetExtFuncIn(&LinSysRes[0], LinSysRes.GetLocSize());
+      AD::SetExtFuncOut(&LinSysSol[0], LinSysSol.GetLocSize());
+      AD::FuncHelper.addUserData(&LinSysRes);
+      AD::FuncHelper.addUserData(&LinSysSol);
+      AD::FuncHelper.addUserData(&Jacobian);
+      AD::FuncHelper.addUserData(geometry);
+      AD::FuncHelper.addUserData(config);
+      AD::FuncHelper.addUserData(this);
     }
     END_SU2_OMP_SAFE_GLOBAL_ACCESS
-
-    AD::StopRecording();
 #endif
   }
 
-  /*--- Create matrix-vector product, preconditioner, and solve the linear system ---*/
-
-  HandleTemporariesIn(LinSysRes, LinSysSol);
-
-  auto mat_vec = CSysMatrixVectorProduct<ScalarType>(Jacobian, geometry, config);
-
-  const auto kindPrec = static_cast<ENUM_LINEAR_SOLVER_PREC>(KindPrecond);
-
-  auto precond = CPreconditioner<ScalarType>::Create(kindPrec, Jacobian, geometry, config);
-
-  /*--- Build preconditioner. ---*/
-
-  precond->Build();
-
-  /*--- Solve system. ---*/
-
   unsigned long IterLinSol = 0;
-  ScalarType residual = 0.0;
 
-  switch (KindSolver) {
-    case BCGSTAB:
-      IterLinSol = BCGSTAB_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual, ScreenOutput, config);
-      break;
-    case FGMRES:
-      IterLinSol = FGMRES_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual, ScreenOutput, config);
-      break;
-    case RESTARTED_FGMRES:
-      IterLinSol = RFGMRES_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual, ScreenOutput, config);
-      break;
-    case CONJUGATE_GRADIENT:
-      IterLinSol = CG_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual, ScreenOutput, config);
-      break;
-    case SMOOTHER:
-      IterLinSol = Smoother_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual, ScreenOutput, config);
-      break;
-    case PASTIX_LDLT : case PASTIX_LU:
-      Jacobian.BuildPastixPreconditioner(geometry, config, KindSolver);
-      Jacobian.ComputePastixPreconditioner(*LinSysRes_ptr, *LinSysSol_ptr, geometry, config);
-      IterLinSol = 1;
-      residual = 1e-20;
-      break;
-    default:
-      SU2_MPI::Error("Unknown type of linear solver.",CURRENT_FUNCTION);
-  }
+  /*--- Declaration of the external function ---*/
+  auto externalFunction = [&]() {
+    /*--- Create matrix-vector product, preconditioner, and solve the linear system ---*/
 
-  SU2_OMP_MASTER
-  {
-    Residual = residual;
-    Iterations = IterLinSol;
-  }
-  END_SU2_OMP_MASTER
+    HandleTemporariesIn(LinSysRes, LinSysSol);
 
-  HandleTemporariesOut(LinSysSol);
+    auto mat_vec = CSysMatrixVectorProduct<ScalarType>(Jacobian, geometry, config);
 
-  delete precond;
+    const auto kindPrec = static_cast<ENUM_LINEAR_SOLVER_PREC>(KindPrecond);
 
-  if(TapeActive) {
+    auto precond = CPreconditioner<ScalarType>::Create(kindPrec, Jacobian, geometry, config);
 
-    /*--- To keep the behavior of SU2_DOT, but not strictly required since jacobian is symmetric(?). ---*/
-    const bool RequiresTranspose = ((lin_sol_mode!=LINEAR_SOLVER_MODE::MESH_DEFORM) || (config->GetKind_SU2() == SU2_COMPONENT::SU2_DOT));
+    /*--- Build preconditioner. ---*/
 
-    if      (lin_sol_mode==LINEAR_SOLVER_MODE::MESH_DEFORM)   KindPrecond = config->GetKind_Deform_Linear_Solver_Prec();
-    else if (lin_sol_mode==LINEAR_SOLVER_MODE::GRADIENT_MODE) KindPrecond  = config->GetKind_Grad_Linear_Solver_Prec();
-    else    KindPrecond = config->GetKind_DiscAdj_Linear_Prec();
+    precond->Build();
 
-    /*--- Build preconditioner for the transposed Jacobian ---*/
+    /*--- Solve system. ---*/
 
-    if (RequiresTranspose) Jacobian.TransposeInPlace();
+    ScalarType residual = 0.0;
 
-    switch(KindPrecond) {
-      case ILU:
-        if (RequiresTranspose) Jacobian.BuildILUPreconditioner();
+    switch (KindSolver) {
+      case BCGSTAB:
+        IterLinSol = BCGSTAB_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual, ScreenOutput, config);
         break;
-      case JACOBI:
-      case LINELET:
-        if (RequiresTranspose) Jacobian.BuildJacobiPreconditioner();
+      case FGMRES:
+        IterLinSol = FGMRES_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual, ScreenOutput, config);
         break;
-      case LU_SGS:
-        /*--- Nothing to build. ---*/
+      case RESTARTED_FGMRES:
+        IterLinSol = RFGMRES_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual, ScreenOutput, config);
         break;
-      case PASTIX_ILU: case PASTIX_LU_P: case PASTIX_LDLT_P:
-        /*--- It was already built. ---*/
+      case CONJUGATE_GRADIENT:
+        IterLinSol = CG_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual, ScreenOutput, config);
         break;
-      default:
-        SU2_MPI::Error("The specified preconditioner is not yet implemented for the discrete adjoint method.", CURRENT_FUNCTION);
+      case SMOOTHER:
+        IterLinSol = Smoother_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual, ScreenOutput, config);
+        break;
+      case PASTIX_LDLT : case PASTIX_LU:
+        Jacobian.BuildPastixPreconditioner(geometry, config, KindSolver);
+        Jacobian.ComputePastixPreconditioner(*LinSysRes_ptr, *LinSysSol_ptr, geometry, config);
+        IterLinSol = 1;
+        residual = 1e-20;
         break;
+      default:
+        SU2_MPI::Error("Unknown type of linear solver.",CURRENT_FUNCTION);
     }
 
-    /*--- Start recording if it was stopped for the linear solver ---*/
-#ifdef CODI_REVERSE_TYPE
-    AD::StartRecording();
-
-    BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS
+    SU2_OMP_MASTER
     {
-      AD::SetExtFuncOut(&LinSysSol[0], LinSysSol.GetLocSize());
-      AD::FuncHelper.addUserData(&LinSysRes);
-      AD::FuncHelper.addUserData(&LinSysSol);
-      AD::FuncHelper.addUserData(&Jacobian);
-      AD::FuncHelper.addUserData(geometry);
-      AD::FuncHelper.addUserData(config);
-      AD::FuncHelper.addUserData(this);
+      Residual = residual;
+      Iterations = IterLinSol;
     }
-    END_SU2_OMP_SAFE_GLOBAL_ACCESS
+    END_SU2_OMP_MASTER
+
+    HandleTemporariesOut(LinSysSol);
+
+    delete precond;
+
+    if(TapeActive) {
+
+      /*--- To keep the behavior of SU2_DOT, but not strictly required since jacobian is symmetric(?). ---*/
+      const bool RequiresTranspose = ((lin_sol_mode!=LINEAR_SOLVER_MODE::MESH_DEFORM) || (config->GetKind_SU2() == SU2_COMPONENT::SU2_DOT));
+
+      if      (lin_sol_mode==LINEAR_SOLVER_MODE::MESH_DEFORM)   KindPrecond = config->GetKind_Deform_Linear_Solver_Prec();
+      else if (lin_sol_mode==LINEAR_SOLVER_MODE::GRADIENT_MODE) KindPrecond  = config->GetKind_Grad_Linear_Solver_Prec();
+      else    KindPrecond = config->GetKind_DiscAdj_Linear_Prec();
+
+      /*--- Build preconditioner for the transposed Jacobian ---*/
+
+      if (RequiresTranspose) Jacobian.TransposeInPlace();
+
+      switch(KindPrecond) {
+        case ILU:
+          if (RequiresTranspose) Jacobian.BuildILUPreconditioner();
+          break;
+        case JACOBI:
+        case LINELET:
+          if (RequiresTranspose) Jacobian.BuildJacobiPreconditioner();
+          break;
+        case LU_SGS:
+          /*--- Nothing to build. ---*/
+          break;
+        case PASTIX_ILU: case PASTIX_LU_P: case PASTIX_LDLT_P:
+          /*--- It was already built. ---*/
+          break;
+        default:
+          SU2_MPI::Error("The specified preconditioner is not yet implemented for the discrete adjoint method.", CURRENT_FUNCTION);
+          break;
+      }
+    }
+  }; /*--- Finish declaration of the external function ---*/
 
-    auto placeholder = [](){};
-    AD::FuncHelper.callPrimalFuncWithADType(placeholder);
-    AD::FuncHelper.addToTape(CSysSolve_b<ScalarType>::Solve_b);
+#ifdef CODI_REVERSE_TYPE
+  /*--- Call the external function with appropriate AD handling ---*/
+  AD::FuncHelper.callPrimalFuncWithADType(externalFunction);
 
-    SU2_OMP_SAFE_GLOBAL_ACCESS(AD::EndExtFunc();)
+  AD::FuncHelper.addToTape(CSysSolve_b<ScalarType>::Solve_b);
+#else
+  /*--- Without reverse AD, call the external function directly ---*/
+  externalFunction();
 #endif
-  }
 
   return IterLinSol;
 }
diff --git a/SU2_CFD/src/SU2_CFD.cpp b/SU2_CFD/src/SU2_CFD.cpp
index 88ea0b6314e..db29bdc1dc6 100644
--- a/SU2_CFD/src/SU2_CFD.cpp
+++ b/SU2_CFD/src/SU2_CFD.cpp
@@ -73,6 +73,9 @@ int main(int argc, char *argv[]) {
 #endif
   SU2_MPI::Comm MPICommunicator = SU2_MPI::GetComm();
 
+  /*--- AD initialization ---*/
+  AD::Initialize();
+
   /*--- Uncomment the following line if runtime NaN catching is desired. ---*/
   // feenableexcept(FE_INVALID | FE_OVERFLOW | FE_DIVBYZERO );
 
@@ -164,6 +167,9 @@ int main(int argc, char *argv[]) {
   libxsmm_finalize();
 #endif
 
+  /*--- Finalize AD. ---*/
+  AD::Finalize();
+
   /*--- Finalize MPI parallelization. ---*/
   SU2_MPI::Finalize();
 
diff --git a/SU2_DOT/src/SU2_DOT.cpp b/SU2_DOT/src/SU2_DOT.cpp
index 39e3dd34320..b8b606ca75c 100644
--- a/SU2_DOT/src/SU2_DOT.cpp
+++ b/SU2_DOT/src/SU2_DOT.cpp
@@ -41,6 +41,10 @@ int main(int argc, char* argv[]) {
 #endif
   SU2_MPI::Comm comm = SU2_MPI::GetComm();
 
+  /*--- AD initialization. ---*/
+
+  AD::Initialize();
+
   /*--- Load in the number of zones and spatial dimensions in the mesh file
    (if no config file is specified, default.cfg is used). ---*/
 
@@ -66,6 +70,10 @@ int main(int argc, char* argv[]) {
 
   driver.Postprocessing();
 
+  /*--- Finalize AD. ---*/
+
+  AD::Finalize();
+
   /*--- Finalize MPI parallelization. ---*/
 
   SU2_MPI::Finalize();

From 6bf394ac19760f1e65a629c7ef8c2f151af3784e Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Wed, 1 Mar 2023 16:47:17 +0100
Subject: [PATCH 247/656] Fixed build error

---
 .../multilayer_perceptron/CIOMap.cpp          |  2 +-
 .../multilayer_perceptron/CLookUp_ANN.cpp     | 13 ++--
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp    |  4 +-
 SU2_CFD/include/fluid/CFluidModel.hpp         |  4 +-
 SU2_CFD/include/variables/CVariable.hpp       | 67 ++++++++++---------
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        | 10 +--
 SU2_CFD/src/solvers/CEulerSolver.cpp          | 14 ++--
 SU2_CFD/src/variables/CEulerVariable.cpp      | 13 +++-
 SU2_CFD/src/variables/CNSVariable.cpp         | 13 ++++
 9 files changed, 80 insertions(+), 60 deletions(-)

diff --git a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
index 78f70a4ff90..a53247b7c5a 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
@@ -25,7 +25,6 @@
  * You should have received a copy of the GNU Lesser General Public
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
-#include "../../../include/toolboxes/multilayer_perceptron/CIOMap.hpp"
 
 #include <cmath>
 #include <fstream>
@@ -33,6 +32,7 @@
 #include <string>
 
 #include "../../../include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp"
+#include "../../../include/toolboxes/multilayer_perceptron/CIOMap.hpp"
 
 MLPToolbox::CIOMap::CIOMap(CLookUp_ANN* MLP_collection, su2vector<std::string>& inputs,
                            su2vector<std::string>& outputs) {
diff --git a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
index 50c8e0cd911..2f8281bdb4c 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
@@ -47,11 +47,14 @@ MLPToolbox::CLookUp_ANN::CLookUp_ANN(const unsigned short n_inputs, const string
   number_of_variables = n_inputs;
 
   NeuralNetworks.resize(n_inputs);
-  cout << setfill(' ');
-  cout << endl;
-  cout << "+------------------------------------------------------------------+\n";
-  cout << "|                 Multi-Layer Perceptron (MLP) info                |\n";
-  cout << "+------------------------------------------------------------------+" << endl;
+  
+  if (rank == MASTER_NODE) {
+    cout << setfill(' ');
+    cout << endl;
+    cout << "+------------------------------------------------------------------+\n";
+    cout << "|                 Multi-Layer Perceptron (MLP) info                |\n";
+    cout << "+------------------------------------------------------------------+" << endl;
+  }
 
   for (auto i_MLP = 0u; i_MLP < n_inputs; i_MLP++) {
     if (rank == MASTER_NODE) cout << "Generating neural network for " << input_filenames[i_MLP] << endl;
diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index 68b51de8d49..fe97fbe2e3f 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -163,13 +163,13 @@ class CDataDrivenFluid : public CFluidModel {
    * \brief Set the initial guess for the density in Newton solvers
    * \param[in] rho - Initial value for density.
    */
-  void SetDensity(su2double rho) override { rho_start = rho; }
+  void SetInitialDensity(su2double rho) override { rho_start = rho; }
 
   /*!
    * \brief Set the initial guess for the static energy in Newton solvers
    * \param[in] e - Initial value for static energy.
    */
-  void SetEnergy(su2double e) override { e_start = e; }
+  void SetInitialEnergy(su2double e) override { e_start = e; }
 
   /*!
    * \brief Get fluid model extrapolation instance
diff --git a/SU2_CFD/include/fluid/CFluidModel.hpp b/SU2_CFD/include/fluid/CFluidModel.hpp
index 861a0637b8a..d6f476ff10b 100644
--- a/SU2_CFD/include/fluid/CFluidModel.hpp
+++ b/SU2_CFD/include/fluid/CFluidModel.hpp
@@ -330,13 +330,13 @@ class CFluidModel {
   * \brief Set the initial guess for the density in Newton solvers
   * \param[in] rho - Initial value for density.
   */
-  virtual void SetDensity(su2double rho) {}
+  virtual void SetInitialDensity(su2double rho) {}
 
   /*!
   * \brief Set the initial guess for the static energy in Newton solvers
   * \param[in] e - Initial value for static energy.
   */
-  virtual void SetEnergy(su2double e) {}
+  virtual void SetInitialEnergy(su2double e) {}
 
   /*!
   * \brief Get fluid model extrapolation instance
diff --git a/SU2_CFD/include/variables/CVariable.hpp b/SU2_CFD/include/variables/CVariable.hpp
index e5e3b3202ef..3c80ffc5f7b 100644
--- a/SU2_CFD/include/variables/CVariable.hpp
+++ b/SU2_CFD/include/variables/CVariable.hpp
@@ -101,8 +101,9 @@ class CVariable {
 
   VectorType SolutionExtra_BGS_k; /*!< \brief Intermediate storage, enables cross term extraction as that is also pushed to Solution. */
 
-  su2vector<unsigned short> Dataset_Extrapolation; /*!< \brief Stores instances of dataset bounds violation when using datadriven fluid models. */
-  su2vector<unsigned long> nIter_Newtonsolver;    /*!< \brief Stores number of Newton solver iterations when using datadriven fluid models. */
+  bool DataDrivenFluid = false; /*!< \brief Usage of data-driven fluid model. DatasetExtrapolation and FluidEntropy will not be sized if disabled. */
+  su2vector<unsigned short> DatasetExtrapolation; /*!< \brief Stores instances of dataset bounds violation when using datadriven fluid models. */
+  su2vector<unsigned long> NIterNewtonsolver;    /*!< \brief Stores number of Newton solver iterations when using datadriven fluid models. */
   VectorType FluidEntropy;          /*!< \brief Stores the fluid entropy value as computed by the datadriven fluid model. */
 
  protected:
@@ -2303,45 +2304,47 @@ class CVariable {
   virtual su2double GetSourceTerm_VelAdjoint(unsigned long iPoint, unsigned long iDim) const { return 0.0; }
 
   /*!
-    * \brief Set fluid entropy
-    * \param[in] iPoint - Node index
-    * \param[in] entropy - fluid entropy value.
-    */
-  virtual void SetEntropy(unsigned long iPoint, su2double entropy) { FluidEntropy[iPoint] = entropy; };
+   * \brief Set fluid entropy
+   * \param[in] iPoint - Node index
+   * \param[in] entropy - fluid entropy value.
+   */
+  void SetEntropy(unsigned long iPoint, su2double entropy) { FluidEntropy[iPoint] = entropy; };
 
   /*!
-    * \brief Get fluid entropy
-    * \param[in] iPoint - Node index
-    * \return Entropy - Fluid entropy value
-    */
-  virtual su2double GetEntropy(unsigned long iPoint) const { return FluidEntropy[iPoint]; }
+   * \brief Get fluid entropy
+   * \param[in] iPoint - Node index
+   * \return Entropy - Fluid entropy value
+   */
+  su2double GetEntropy(unsigned long iPoint) const { return FluidEntropy[iPoint]; }
 
   /*!
-    * \brief Set dataset extrapolation instance
-    * \param[in] iPoint - Node index
-    * \param[in] extrapolation - Extrapolation instance (0 = within dataset, 1 = outside dataset)
-    */
-  virtual void SetDataExtrapolation(unsigned long iPoint, unsigned short extrapolation) { Dataset_Extrapolation[iPoint] = extrapolation; };
+   * \brief Set dataset extrapolation instance
+   * \param[in] iPoint - Node index
+   * \param[in] extrapolation - Extrapolation instance (0 = within dataset, 1 = outside dataset)
+   */
+  void SetDataExtrapolation(unsigned long iPoint, unsigned short extrapolation) {
+    DatasetExtrapolation[iPoint] = extrapolation;
+  };
 
   /*!
-    * \brief Get dataset extrapolation instance
-    * \param[in] iPoint - Node index
-    * \return extrapolation - Extrapolation instance (0 = within dataset, 1 = outside dataset)
-    */
-  virtual unsigned short GetDataExtrapolation(unsigned long iPoint) const { return Dataset_Extrapolation[iPoint]; }
+   * \brief Get dataset extrapolation instance
+   * \param[in] iPoint - Node index
+   * \return extrapolation - Extrapolation instance (0 = within dataset, 1 = outside dataset)
+   */
+  unsigned short GetDataExtrapolation(unsigned long iPoint) const { return DatasetExtrapolation[iPoint]; }
 
   /*!
-    * \brief Set the number of iterations required by a Newton solver used by the fluid model.
-    * \param[in] iPoint - Node index
-    * \param[in] nIter - Number of iterations evaluated by the Newton solver
-    */
-  void SetNewtonSolverIterations(unsigned long iPoint, unsigned long nIter) { nIter_Newtonsolver[iPoint] = nIter; }
+   * \brief Set the number of iterations required by a Newton solver used by the fluid model.
+   * \param[in] iPoint - Node index
+   * \param[in] nIter - Number of iterations evaluated by the Newton solver
+   */
+  void SetNewtonSolverIterations(unsigned long iPoint, unsigned long nIter) { NIterNewtonsolver[iPoint] = nIter; }
 
   /*!
-    * \brief Get the number of iterations required by a Newton solver used by the fluid model.
-    * \param[in] iPoint - Node index
-    * \return Number of iterations evaluated by the Newton solver
-    */
-  unsigned long GetNewtonSolverIterations(unsigned long iPoint) const { return nIter_Newtonsolver[iPoint]; }
+   * \brief Get the number of iterations required by a Newton solver used by the fluid model.
+   * \param[in] iPoint - Node index
+   * \return Number of iterations evaluated by the Newton solver
+   */
+  unsigned long GetNewtonSolverIterations(unsigned long iPoint) const { return NIterNewtonsolver[iPoint]; }
 
 };
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 3358ce966e1..2d2085ff67a 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -139,7 +139,7 @@ void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
   su2double dhde_rho = 1 + dPde_rho / rho;
 
   dhdrho_P = dhdrho_e - dhde_rho * (1 / dPde_rho) * dPdrho_e;
-  dhdP_rho = dhdrho_e * (1 / dPdrho_e) + dhde_rho * (1 / dPde_rho);
+  dhdP_rho = dhde_rho * (1 / dPde_rho);
   dsdrho_P = dsdrho_e - dPdrho_e * (1 / dPde_rho) * dsde_rho;
   dsdP_rho = dsde_rho / dPde_rho;
 }
@@ -287,8 +287,8 @@ void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
 
     su2double Enthalpy = e + Pressure / rho;
     /*--- Determine pressure and temperature residuals ---*/
-    // delta_h = Enthalpy - h;
-    // delta_s = Entropy - s;
+    delta_h = Enthalpy - h;
+    delta_s = Entropy - s;
 
     /*--- Continue iterative process if residuals are outside tolerances ---*/
     if ((abs(delta_h / h) < Newton_Tolerance) && (abs(delta_s / s) < Newton_Tolerance)) {
@@ -368,8 +368,8 @@ unsigned long CDataDrivenFluid::Predict_MLP(su2double rho, su2double e) {
   /* Apply exponential transformation to the MLP outputs for the first and second
      derivative of the entropy w.r.t density */
   // Optional:
-  dsdrho_e = -exp(dsdrho_e);
-  d2sdrho2 = exp(d2sdrho2);
+  // dsdrho_e = -exp(dsdrho_e);
+  // d2sdrho2 = exp(d2sdrho2);
 
   return exit_code;
 }
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index 1be0b7f5732..8b08f270b2f 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -1671,12 +1671,6 @@ unsigned long CEulerSolver::SetPrimitive_Variables(CSolver **solver_container, c
     bool physical = nodes->SetPrimVar(iPoint, GetFluidModel());
     nodes->SetSecondaryVar(iPoint, GetFluidModel());
 
-    /*--- Update en---*/
-    if(config->GetKind_FluidModel() == DATADRIVEN_FLUID) {
-      nodes->SetDataExtrapolation(iPoint, GetFluidModel()->GetExtrapolation());
-      nodes->SetEntropy(iPoint, GetFluidModel()->GetEntropy());
-    }
-
     /* Check for non-realizable states for reporting. */
 
     if (!physical) nonPhysicalPoints++;
@@ -4689,8 +4683,8 @@ void CEulerSolver::BC_Riemann(CGeometry *geometry, CSolver **solver_container,
 
       /*--- Set initial values for density and energy for Newton solvers in fluid model ---*/
       su2double relax_Newton = config->GetRelaxation_DataDriven();
-      GetFluidModel()->SetDensity(relax_Newton*Density_i + (1 - relax_Newton)*config->GetDensity_Init_DataDriven());
-      GetFluidModel()->SetEnergy(relax_Newton*StaticEnergy_i + (1 - relax_Newton)*config->GetEnergy_Init_DataDriven());
+      GetFluidModel()->SetInitialDensity(relax_Newton*Density_i + (1 - relax_Newton)*config->GetDensity_Init_DataDriven());
+      GetFluidModel()->SetInitialEnergy(relax_Newton*StaticEnergy_i + (1 - relax_Newton)*config->GetEnergy_Init_DataDriven());
 
       Pressure_i = GetFluidModel()->GetPressure();
       Enthalpy_i = Energy_i + Pressure_i/Density_i;
@@ -6155,8 +6149,8 @@ void CEulerSolver::BC_Giles(CGeometry *geometry, CSolver **solver_container, CNu
 
       /*--- Set initial values for density and energy for Newton solvers in fluid model ---*/
       su2double relax_Newton = config->GetRelaxation_DataDriven();
-      GetFluidModel()->SetDensity(relax_Newton*Density_i + (1 - relax_Newton)*config->GetDensity_Init_DataDriven());
-      GetFluidModel()->SetEnergy(relax_Newton*StaticEnergy_i + (1 - relax_Newton)*config->GetEnergy_Init_DataDriven());
+      GetFluidModel()->SetInitialDensity(relax_Newton*Density_i + (1 - relax_Newton)*config->GetDensity_Init_DataDriven());
+      GetFluidModel()->SetInitialEnergy(relax_Newton*StaticEnergy_i + (1 - relax_Newton)*config->GetEnergy_Init_DataDriven());
 
       GetFluidModel()->SetTDState_rhoe(Density_i, StaticEnergy_i);
 
diff --git a/SU2_CFD/src/variables/CEulerVariable.cpp b/SU2_CFD/src/variables/CEulerVariable.cpp
index 255ffdfaf54..b04bf23b683 100644
--- a/SU2_CFD/src/variables/CEulerVariable.cpp
+++ b/SU2_CFD/src/variables/CEulerVariable.cpp
@@ -79,9 +79,10 @@ CEulerVariable::CEulerVariable(su2double density, const su2double *velocity, su2
     AuxVar.resize(nPoint, nAuxVar) = su2double(0.0);
   }
   
-  if (config->GetKind_FluidModel() == DATADRIVEN_FLUID){
-    Dataset_Extrapolation.resize(nPoint) = 0;
-    nIter_Newtonsolver.resize(nPoint) = 0;
+  if (config->GetKind_FluidModel() == ENUM_FLUIDMODEL::DATADRIVEN_FLUID){
+    DataDrivenFluid = true;
+    DatasetExtrapolation.resize(nPoint) = 0;
+    NIterNewtonsolver.resize(nPoint) = 0;
     FluidEntropy.resize(nPoint) = su2double(0.0);
   }
 }
@@ -131,6 +132,12 @@ bool CEulerVariable::SetPrimVar(unsigned long iPoint, CFluidModel *FluidModel) {
 
   SetEnthalpy(iPoint); // Requires pressure computation.
 
+  /*--- Set look-up variables in case of data-driven fluid model ---*/
+  if (DataDrivenFluid) {
+    SetDataExtrapolation(iPoint, FluidModel->GetExtrapolation());
+    SetEntropy(iPoint, FluidModel->GetEntropy());
+  }
+
   return RightVol;
 }
 
diff --git a/SU2_CFD/src/variables/CNSVariable.cpp b/SU2_CFD/src/variables/CNSVariable.cpp
index ec278b27ae1..356ec48dac7 100644
--- a/SU2_CFD/src/variables/CNSVariable.cpp
+++ b/SU2_CFD/src/variables/CNSVariable.cpp
@@ -43,6 +43,13 @@ CNSVariable::CNSVariable(su2double density, const su2double *velocity, su2double
   Vortex_Tilting.resize(nPoint) = su2double(0.0);
   Max_Lambda_Visc.resize(nPoint) = su2double(0.0);
 
+  if (config->GetKind_FluidModel() == ENUM_FLUIDMODEL::DATADRIVEN_FLUID){
+    DataDrivenFluid = true;
+    DatasetExtrapolation.resize(nPoint) = 0;
+    NIterNewtonsolver.resize(nPoint) = 0;
+    FluidEntropy.resize(nPoint) = su2double(0.0);
+  }
+
 }
 
 void CNSVariable::SetRoe_Dissipation_NTS(unsigned long iPoint,
@@ -198,6 +205,12 @@ bool CNSVariable::SetPrimVar(unsigned long iPoint, su2double eddy_visc, su2doubl
 
   SetSpecificHeatCp(iPoint, FluidModel->GetCp());
 
+  /*--- Set look-up variables in case of data-driven fluid model ---*/
+  if (DataDrivenFluid) {
+    SetDataExtrapolation(iPoint, FluidModel->GetExtrapolation());
+    SetEntropy(iPoint, FluidModel->GetEntropy());
+  }
+
   return RightVol;
 }
 

From be3e6ddae8a4bc5713ec6d3b63a3e1f020c65734 Mon Sep 17 00:00:00 2001
From: PENGYAN777 <peng.yan@mail.polimi.it>
Date: Sat, 4 Mar 2023 08:46:56 +0100
Subject: [PATCH 248/656] single phase and away from Pc

---
 SU2_CFD/src/fluid/CCoolProp.cpp | 87 +++++++++++++++++++++------------
 1 file changed, 56 insertions(+), 31 deletions(-)

diff --git a/SU2_CFD/src/fluid/CCoolProp.cpp b/SU2_CFD/src/fluid/CCoolProp.cpp
index 8fe0103964c..78e3f454544 100644
--- a/SU2_CFD/src/fluid/CCoolProp.cpp
+++ b/SU2_CFD/src/fluid/CCoolProp.cpp
@@ -1,29 +1,29 @@
 /*!
- * \file CCoolProp.cpp
- * \brief Source of the fluid model from CoolProp.
- * \author P. Yan, G. Gori, A. Guardone
- * \version 7.5.1 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
+* \file CCoolProp.cpp
+* \brief Source of the fluid model from CoolProp.
+* \author P. Yan, G. Gori, A. Guardone
+* \version 7.4.0 "Blackbird"
+*
+* SU2 Project Website: https://su2code.github.io
+*
+* The SU2 Project is maintained by the SU2 Foundation
+* (http://su2foundation.org)
+*
+* Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+*
+* SU2 is free software; you can redistribute it and/or
+* modify it under the terms of the GNU Lesser General Public
+* License as published by the Free Software Foundation; either
+* version 2.1 of the License, or (at your option) any later version.
+*
+* SU2 is distributed in the hope that it will be useful,
+* but WITHOUT ANY WARRANTY; without even the implied warranty of
+* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+* Lesser General Public License for more details.
+*
+* You should have received a copy of the GNU Lesser General Public
+* License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+*/
 
 #include "../../include/fluid/CCoolProp.hpp"
 
@@ -56,15 +56,32 @@ void CCoolProp::SetTDState_rhoe(su2double rho, su2double e) {
   dTdrho_e = fluid_entity->first_partial_deriv(CoolProp::iT, CoolProp::iDmass, CoolProp::iUmass);
   dTde_rho = fluid_entity->first_partial_deriv(CoolProp::iT, CoolProp::iUmass, CoolProp::iDmass);
   if (fluid_entity->phase() == 6) {
+    // assume it is pure gas
+    fluid_entity->specify_phase(CoolProp::iphase_gas);
+    if(abs(Pressure/Pressure_Critical-1)<0.01){
+      // if P is very cloase to Pc, the CoolProp has issue
+      Pressure = Pressure_Critical*0.99;
+    }
+    fluid_entity->update(CoolProp::PT_INPUTS, Pressure, Temperature);
+    if(abs(fluid_entity->rhomass()/Density-1)*100 < 1){
+      // origial phase is near saturation gas, then just compute sound speed
+      SoundSpeed2 = pow(fluid_entity->speed_sound(), 2);
+    }
+    else{
+      // original phase is not near saturation gas, then specify the phase as gas phase
       fluid_entity->specify_phase(CoolProp::iphase_gas);
       SetTDState_PT(Pressure,Temperature);
+    }
   }
   else{
-      SoundSpeed2 = pow(fluid_entity->speed_sound(), 2);
+    SoundSpeed2 = pow(fluid_entity->speed_sound(), 2);
   }
 }
 
 void CCoolProp::SetTDState_PT(su2double P, su2double T) {
+  if(abs(P/Pressure_Critical-1)<0.01) {
+    P = Pressure_Critical * 0.99;
+  }
   fluid_entity->update(CoolProp::PT_INPUTS, P, T);
   su2double rho = fluid_entity->rhomass();
   su2double e = fluid_entity->umass();
@@ -72,12 +89,18 @@ void CCoolProp::SetTDState_PT(su2double P, su2double T) {
 }
 
 void CCoolProp::SetTDState_Prho(su2double P, su2double rho) {
+  if(abs(P/Pressure_Critical-1)<0.01){
+    P = Pressure_Critical*0.99;
+  }
   fluid_entity->update(CoolProp::DmassP_INPUTS, rho, P);
   su2double e = fluid_entity->umass();
   SetTDState_rhoe(rho, e);
 }
 
-void CCoolProp::SetEnergy_Prho(su2double P, su2double rho) {
+void CCoolProp::SetEnergy_Prho(su2double P, su2double rho){
+  if(abs(P/Pressure_Critical-1)<0.01){
+    P = Pressure_Critical*0.99;
+  }
   fluid_entity->update(CoolProp::DmassP_INPUTS, rho, P);
   StaticEnergy = fluid_entity->umass();
 }
@@ -90,17 +113,19 @@ void CCoolProp::SetTDState_hs(su2double h, su2double s) {
 }
 
 void  CCoolProp::SetTDState_Ps(su2double P, su2double s) {
+  if(abs(P/Pressure_Critical-1)<0.01){
+    P = Pressure_Critical*0.99;
+  }
   fluid_entity->update(CoolProp::PSmass_INPUTS, P, s);
-  su2double Rho = fluid_entity->rhomass();
+  su2double rho = fluid_entity->rhomass();
   su2double e = fluid_entity->umass();
-  SetTDState_rhoe(Rho, e);
+  SetTDState_rhoe(rho, e);
 }
 
 void CCoolProp::SetTDState_rhoT(su2double rho, su2double T) {
   fluid_entity->update(CoolProp::DmassT_INPUTS, rho, T);
-  su2double Rho = fluid_entity->rhomass();
   su2double e = fluid_entity->umass();
-  SetTDState_rhoe(Rho, e);
+  SetTDState_rhoe(rho, e);
 }
 
 void  CCoolProp::ComputeDerivativeNRBC_Prho(su2double P, su2double rho) {

From 5defc868a01d7c6eb231d976b8ed8dc32789cae2 Mon Sep 17 00:00:00 2001
From: PENGYAN777 <peng.yan@mail.polimi.it>
Date: Sat, 4 Mar 2023 09:17:30 +0100
Subject: [PATCH 249/656] run clang-format

---
 SU2_CFD/src/fluid/CCoolProp.cpp | 103 ++++++++++++++++----------------
 1 file changed, 53 insertions(+), 50 deletions(-)

diff --git a/SU2_CFD/src/fluid/CCoolProp.cpp b/SU2_CFD/src/fluid/CCoolProp.cpp
index 78e3f454544..456605f827a 100644
--- a/SU2_CFD/src/fluid/CCoolProp.cpp
+++ b/SU2_CFD/src/fluid/CCoolProp.cpp
@@ -1,39 +1,39 @@
 /*!
-* \file CCoolProp.cpp
-* \brief Source of the fluid model from CoolProp.
-* \author P. Yan, G. Gori, A. Guardone
-* \version 7.4.0 "Blackbird"
-*
-* SU2 Project Website: https://su2code.github.io
-*
-* The SU2 Project is maintained by the SU2 Foundation
-* (http://su2foundation.org)
-*
-* Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
-*
-* SU2 is free software; you can redistribute it and/or
-* modify it under the terms of the GNU Lesser General Public
-* License as published by the Free Software Foundation; either
-* version 2.1 of the License, or (at your option) any later version.
-*
-* SU2 is distributed in the hope that it will be useful,
-* but WITHOUT ANY WARRANTY; without even the implied warranty of
-* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
-* Lesser General Public License for more details.
-*
-* You should have received a copy of the GNU Lesser General Public
-* License along with SU2. If not, see <http://www.gnu.org/licenses/>.
-*/
+ * \file CCoolProp.cpp
+ * \brief Source of the fluid model from CoolProp.
+ * \author P. Yan, G. Gori, A. Guardone
+ * \version 7.5.1 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
 
 #include "../../include/fluid/CCoolProp.hpp"
 
 #ifdef USE_COOLPROP
-#include "CoolProp.h"
 #include "AbstractState.h"
+#include "CoolProp.h"
 
 CCoolProp::CCoolProp(string fluidname) : CFluidModel() {
-  fluid_entity = std::unique_ptr<CoolProp::AbstractState>(CoolProp::AbstractState::factory("HEOS",fluidname));
-  Gas_Constant = fluid_entity->gas_constant()/fluid_entity->molar_mass();
+  fluid_entity = std::unique_ptr<CoolProp::AbstractState>(CoolProp::AbstractState::factory("HEOS", fluidname));
+  Gas_Constant = fluid_entity->gas_constant() / fluid_entity->molar_mass();
   Pressure_Critical = fluid_entity->p_critical();
   Temperature_Critical = fluid_entity->T_critical();
   acentric_factor = fluid_entity->acentric_factor();
@@ -58,28 +58,28 @@ void CCoolProp::SetTDState_rhoe(su2double rho, su2double e) {
   if (fluid_entity->phase() == 6) {
     // assume it is pure gas
     fluid_entity->specify_phase(CoolProp::iphase_gas);
-    if(abs(Pressure/Pressure_Critical-1)<0.01){
+    if (abs(Pressure / Pressure_Critical - 1) < 0.01) {
       // if P is very cloase to Pc, the CoolProp has issue
-      Pressure = Pressure_Critical*0.99;
+      Pressure = Pressure_Critical * 0.99;
     }
     fluid_entity->update(CoolProp::PT_INPUTS, Pressure, Temperature);
-    if(abs(fluid_entity->rhomass()/Density-1)*100 < 1){
+    if (abs(fluid_entity->rhomass() / Density - 1) * 100 < 1) {
       // origial phase is near saturation gas, then just compute sound speed
       SoundSpeed2 = pow(fluid_entity->speed_sound(), 2);
     }
-    else{
+    else {
       // original phase is not near saturation gas, then specify the phase as gas phase
       fluid_entity->specify_phase(CoolProp::iphase_gas);
-      SetTDState_PT(Pressure,Temperature);
+      SetTDState_PT(Pressure, Temperature);
     }
   }
-  else{
+  else {
     SoundSpeed2 = pow(fluid_entity->speed_sound(), 2);
   }
 }
 
 void CCoolProp::SetTDState_PT(su2double P, su2double T) {
-  if(abs(P/Pressure_Critical-1)<0.01) {
+  if (abs(P / Pressure_Critical - 1) < 0.01) {
     P = Pressure_Critical * 0.99;
   }
   fluid_entity->update(CoolProp::PT_INPUTS, P, T);
@@ -89,17 +89,17 @@ void CCoolProp::SetTDState_PT(su2double P, su2double T) {
 }
 
 void CCoolProp::SetTDState_Prho(su2double P, su2double rho) {
-  if(abs(P/Pressure_Critical-1)<0.01){
-    P = Pressure_Critical*0.99;
+  if (abs(P / Pressure_Critical - 1) < 0.01) {
+    P = Pressure_Critical * 0.99;
   }
   fluid_entity->update(CoolProp::DmassP_INPUTS, rho, P);
   su2double e = fluid_entity->umass();
   SetTDState_rhoe(rho, e);
 }
 
-void CCoolProp::SetEnergy_Prho(su2double P, su2double rho){
-  if(abs(P/Pressure_Critical-1)<0.01){
-    P = Pressure_Critical*0.99;
+void CCoolProp::SetEnergy_Prho(su2double P, su2double rho) {
+  if (abs(P / Pressure_Critical - 1) < 0.01) {
+    P = Pressure_Critical * 0.99;
   }
   fluid_entity->update(CoolProp::DmassP_INPUTS, rho, P);
   StaticEnergy = fluid_entity->umass();
@@ -112,9 +112,9 @@ void CCoolProp::SetTDState_hs(su2double h, su2double s) {
   SetTDState_rhoe(rho, e);
 }
 
-void  CCoolProp::SetTDState_Ps(su2double P, su2double s) {
-  if(abs(P/Pressure_Critical-1)<0.01){
-    P = Pressure_Critical*0.99;
+void CCoolProp::SetTDState_Ps(su2double P, su2double s) {
+  if (abs(P / Pressure_Critical - 1) < 0.01) {
+    P = Pressure_Critical * 0.99;
   }
   fluid_entity->update(CoolProp::PSmass_INPUTS, P, s);
   su2double rho = fluid_entity->rhomass();
@@ -128,16 +128,19 @@ void CCoolProp::SetTDState_rhoT(su2double rho, su2double T) {
   SetTDState_rhoe(rho, e);
 }
 
-void  CCoolProp::ComputeDerivativeNRBC_Prho(su2double P, su2double rho) {
+void CCoolProp::ComputeDerivativeNRBC_Prho(su2double P, su2double rho) {
   SetTDState_Prho(P, rho);
-  dhdrho_P = fluid_entity->first_partial_deriv(CoolProp::iHmass,CoolProp::iDmass,CoolProp::iP);
-  dhdP_rho = fluid_entity->first_partial_deriv(CoolProp::iHmass,CoolProp::iP,CoolProp::iDmass);
-  dsdP_rho = fluid_entity->first_partial_deriv(CoolProp::iSmass,CoolProp::iP,CoolProp::iDmass);
-  dsdrho_P = fluid_entity->first_partial_deriv(CoolProp::iSmass,CoolProp::iDmass,CoolProp::iP);
+  dhdrho_P = fluid_entity->first_partial_deriv(CoolProp::iHmass, CoolProp::iDmass, CoolProp::iP);
+  dhdP_rho = fluid_entity->first_partial_deriv(CoolProp::iHmass, CoolProp::iP, CoolProp::iDmass);
+  dsdP_rho = fluid_entity->first_partial_deriv(CoolProp::iSmass, CoolProp::iP, CoolProp::iDmass);
+  dsdrho_P = fluid_entity->first_partial_deriv(CoolProp::iSmass, CoolProp::iDmass, CoolProp::iP);
 }
 
 #else
 CCoolProp::CCoolProp(string fluidname) {
-  SU2_MPI::Error("SU2 was not compiled with CoolProp (-Denable-coolprop=true). Note that CoolProp cannot be used with directdiff or autodiff", CURRENT_FUNCTION);
+  SU2_MPI::Error(
+      "SU2 was not compiled with CoolProp (-Denable-coolprop=true). Note that CoolProp cannot be used with directdiff "
+      "or autodiff",
+      CURRENT_FUNCTION);
 }
-#endif
\ No newline at end of file
+#endif

From 47d0793bb548516e3a65bdb59ae48c62b7f1b932 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 4 Mar 2023 18:08:29 -0800
Subject: [PATCH 250/656] matrix view for markers

---
 .../containers/CPyWrapperMatrixView.hpp       | 134 ++++++++++++------
 SU2_CFD/include/drivers/CDriver.hpp           |  30 +---
 SU2_CFD/include/drivers/CDriverBase.hpp       |  96 +++++++++++--
 SU2_CFD/include/variables/CVariable.hpp       |  14 +-
 SU2_CFD/src/drivers/CDriverBase.cpp           |  23 ++-
 SU2_CFD/src/python_wrapper_structure.cpp      |  79 +----------
 .../deforming_bump_in_channel/run.py          |   9 +-
 .../flow_load_sens/run_adjoint.py             |   5 +-
 .../launch_flatPlate_rigidMotion.py           |   9 +-
 .../launch_unsteady_CHT_FlatPlate.py          |   6 +-
 10 files changed, 230 insertions(+), 175 deletions(-)

diff --git a/Common/include/containers/CPyWrapperMatrixView.hpp b/Common/include/containers/CPyWrapperMatrixView.hpp
index 2c3d6477ee4..321f062738d 100644
--- a/Common/include/containers/CPyWrapperMatrixView.hpp
+++ b/Common/include/containers/CPyWrapperMatrixView.hpp
@@ -1,6 +1,6 @@
 /*!
  * \file CPyWrapperMatrixView.hpp
- * \brief A simple matrix view to use with the python wrapper.
+ * \brief Simple matrix views to use with the python wrapper.
  * \author P. Gomes
  * \version 7.5.1 "Blackbird"
  *
@@ -27,28 +27,67 @@
 
 #pragma once
 
+#include <string>
 #include <utility>
 #include <vector>
-#include <string>
 
-#include "C2DContainer.hpp"
+#include "../geometry/dual_grid/CVertex.hpp"
 #include "../parallelization/mpi_structure.hpp"
+#include "C2DContainer.hpp"
+
+/*!
+ * \brief Python wrapper matrix interface
+ * The accessors in this macro provide a passive double interface to matrix of
+ * su2double. This can be extended to allow access to derivative information.
+ * Classes that use this macro encapsulate the access to the raw data (su2double)
+ * via the functions "Access(row, col) -> su2double&" (const and non-const versions).
+ * We use a macro because it is diffult to use modern C++ idioms (e.g. CRTP) with
+ * SWIG. In addition to "Access" classes must have member variables "rows_", "cols_",
+ * and "read_only_".
+ */
+#define PY_WRAPPER_MATRIX_INTERFACE                                                                              \
+  /*! \brief Returns the shape of the matrix. */                                                                 \
+  std::pair<unsigned long, unsigned long> Shape() const { return std::make_pair(rows_, cols_); }                 \
+                                                                                                                 \
+  /*! \brief Returns whether the data is read-only [true] or if it can be modified [false]. */                   \
+  bool IsReadOnly() const { return read_only_; }                                                                 \
+                                                                                                                 \
+  /*! \brief Gets the value for a (row, column) pair. */                                                         \
+  passivedouble operator()(unsigned long row, unsigned long col) const { return Get(row, col); }                 \
+                                                                                                                 \
+  /*! \brief Gets the value for a (row, column) pair. */                                                         \
+  passivedouble Get(unsigned long row, unsigned long col) const { return SU2_TYPE::GetValue(Access(row, col)); } \
+                                                                                                                 \
+  /*! \brief Gets the values for a row of the matrix. */                                                         \
+  std::vector<passivedouble> Get(unsigned long row) const {                                                      \
+    std::vector<passivedouble> vals(cols_);                                                                      \
+    for (unsigned long j = 0; j < cols_; ++j) vals[j] = Get(row, j);                                             \
+    return vals;                                                                                                 \
+  }                                                                                                              \
+  /*! \brief Sets the value for a (row, column) pair. This clears derivative information. */                     \
+  void Set(unsigned long row, unsigned long col, passivedouble val) { Access(row, col) = val; }                  \
+                                                                                                                 \
+  /*! \brief Sets the values for a row of the matrix. */                                                         \
+  void Set(unsigned long row, std::vector<passivedouble> vals) {                                                 \
+    unsigned long j = 0;                                                                                         \
+    for (const auto& val : vals) Set(row, j++, val);                                                             \
+  }
 
 /*!
  * \class CPyWrapperMatrixView
  * \ingroup PySU2
- * \brief A simple matrix view to use with the python wrapper. The accessors
- * in this class provide a passive double interface to su2activematrix.
- * This can be extended to allow access to derivative information of su2double.
+ * \brief This class wraps su2activematrix for the python wrapper matrix interface.
+ * It is generaly used to wrap access to solver variables defined for the entire volume.
  */
 class CPyWrapperMatrixView {
- private:
+ protected:
   static_assert(su2activematrix::IsRowMajor, "");
   su2double* data_ = nullptr;
   unsigned long rows_ = 0, cols_ = 0;
   std::string name_;
   bool read_only_ = false;
 
+  /*--- Define the functions required by the interface macro. ---*/
   inline const su2double& Access(unsigned long row, unsigned long col) const {
     if (row > rows_ || col > cols_) SU2_MPI::Error(name_ + " out of bounds", "CPyWrapperMatrixView");
     return data_[row * cols_ + col];
@@ -68,48 +107,59 @@ class CPyWrapperMatrixView {
    * \note "read_only" can be set to true to prevent the data from being modified.
    */
   CPyWrapperMatrixView(su2activematrix& mat, const std::string& name, bool read_only)
-    : data_(mat.data()), rows_(mat.rows()), cols_(mat.cols()), name_(name), read_only_(read_only) {}
-
-  /*!
-   * \brief Returns the shape of the matrix.
-   */
-  std::pair<unsigned long, unsigned long> Shape() const { return std::make_pair(rows_, cols_); }
-
-  /*!
-   * \brief Returns whether the data is read-only [true] or if it can be modified [false].
-   */
-  bool IsReadOnly() const { return read_only_; }
+      : data_(mat.data()), rows_(mat.rows()), cols_(mat.cols()), name_(name), read_only_(read_only) {}
 
-  /*!
-   * \brief Gets the value for a (row, column) pair.
-   */
-  passivedouble operator() (unsigned long row, unsigned long col) const { return Get(row, col); }
+  /*--- Use the macro to generate the interface. ---*/
+  PY_WRAPPER_MATRIX_INTERFACE
+};
 
-  /*!
-   * \brief Gets the value for a (row, column) pair.
-   */
-  passivedouble Get(unsigned long row, unsigned long col) const { return SU2_TYPE::GetValue(Access(row, col)); }
+/*!
+ * \class CPyWrapperMarkerMatrixView
+ * \ingroup PySU2
+ * \brief This class wraps su2activematrix for the python wrapper matrix interface restricting it
+ * to the vertices of a given marker.
+ */
+class CPyWrapperMarkerMatrixView {
+ private:
+  static_assert(su2activematrix::IsRowMajor, "");
+  su2double* data_ = nullptr;
+  const CVertex* const* vertices_ = nullptr;
+  unsigned long rows_ = 0, cols_ = 0;
+  std::string name_;
+  bool read_only_ = false;
 
-  /*!
-   * \brief Gets the values for a row of the matrix.
-   */
-  std::vector<passivedouble> Get(unsigned long row) const {
-    std::vector<passivedouble> vals(cols_);
-    for (unsigned long j = 0; j < cols_; ++j) vals[j] = Get(row, j);
-    return vals;
+  /*--- Define the functions required by the interface macro. ---*/
+  inline const su2double& Access(unsigned long row, unsigned long col) const {
+    if (row > rows_ || col > cols_) SU2_MPI::Error(name_ + " out of bounds", "CPyWrapperMarkerMatrixView");
+    return data_[vertices_[row]->GetNode() * cols_ + col];
+  }
+  inline su2double& Access(unsigned long row, unsigned long col) {
+    if (read_only_) SU2_MPI::Error(name_ + " is read-only", "CPyWrapperMarkerMatrixView");
+    const auto& const_me = *this;
+    return const_cast<su2double&>(const_me.Access(row, col));
   }
 
-  /*!
-   * \brief Sets the value for a (row, column) pair.
-   * \note This clears derivative information (consistently with C++ operator= with passive rhs).
-   */
-  void Set(unsigned long row, unsigned long col, passivedouble val) { Access(row, col) = val; }
+ public:
+  CPyWrapperMarkerMatrixView() = default;
 
   /*!
-   * \brief Sets the values for a row of the matrix.
+   * \brief Construct the view of the matrix.
+   * \note "name" should be set to the variable name being returned to give better information to users.
+   * \note "read_only" can be set to true to prevent the data from being modified.
    */
-  void Set(unsigned long row, std::vector<passivedouble> vals) {
-    unsigned long j = 0;
-    for (const auto& val : vals) Set(row, j++, val);
+  CPyWrapperMarkerMatrixView(su2activematrix& mat, const CVertex* const* vertices, unsigned long n_vertices,
+                             const std::string& name, bool read_only)
+      : data_(mat.data()),
+        vertices_(vertices),
+        rows_(n_vertices),
+        cols_(mat.cols()),
+        name_(name),
+        read_only_(read_only) {
+    if (mat.rows() < n_vertices) {
+      SU2_MPI::Error(name + " has fewer rows than the number of vertices in the marker.", "CPyWrapperMarkerMatrixView");
+    }
   }
+
+  /*--- Use the macro to generate the interface. ---*/
+  PY_WRAPPER_MATRIX_INTERFACE
 };
diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index a26c841656f..ae50e59e2f1 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -457,19 +457,19 @@ class CDriver : public CDriverBase {
    * \brief Get the number of external iterations.
    * \return Number of external iterations.
    */
-  unsigned long GetnTimeIter() const;
+  unsigned long GetNumberTimeIter() const;
 
   /*!
    * \brief Get the current external iteration.
    * \return Current external iteration.
    */
-  unsigned long GetTime_Iter() const;
+  unsigned long GetTimeIter() const;
 
   /*!
    * \brief Get the unsteady time step.
    * \return Unsteady time step.
    */
-  passivedouble GetUnsteady_TimeStep() const;
+  passivedouble GetUnsteadyTimeStep() const;
 
   /*!
    * \brief Get the name of the output file for the surface.
@@ -564,30 +564,6 @@ class CDriver : public CDriverBase {
   void SetFEA_Loads(unsigned short iMarker, unsigned long iVertex, passivedouble LoadX, passivedouble LoadY,
                     passivedouble LoadZ);
 
-  /*!
-   * \brief Return the displacements from the FEA solver.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Vector of displacements.
-   */
-  vector<passivedouble> GetFEA_Displacements(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Return the velocities from the FEA Solver.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Vector of velocities.
-   */
-  vector<passivedouble> GetFEA_Velocity(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Return the velocities from the FEA Solver.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Vector of velocities at time n.
-   */
-  vector<passivedouble> GetFEA_Velocity_n(unsigned short iMarker, unsigned long iVertex) const;
-
   /*!
    * \brief Get the sensitivity of the flow loads for the structural solver.
    * \param[in] iMarker - Marker identifier.
diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index c83ad9bdf31..9d6c60334af 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -27,6 +27,7 @@
 
 #pragma once
 
+#include <limits>
 #include "../../../Common/include/CConfig.hpp"
 #include "../../../Common/include/containers/CPyWrapperMatrixView.hpp"
 #include "../numerics/CNumerics.hpp"
@@ -200,6 +201,21 @@ class CDriverBase {
     return CPyWrapperMatrixView(*coords, "InitialCoordinates", true);
   }
 
+  /*!
+   * \brief Get a read-only view of the initial (undeformed) coordinates of the mesh nodes of a marker.
+   */
+  inline CPyWrapperMarkerMatrixView MarkerInitialCoordinates(unsigned short iMarker) const {
+    if (!main_config->GetDeform_Mesh()) {
+      SU2_MPI::Error("Initial coordinates are only available with DEFORM_MESH= YES", CURRENT_FUNCTION);
+    }
+    if (iMarker >= GetNumberMarkers()) SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
+
+    auto* coords =
+        const_cast<su2activematrix*>(solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord());
+    return CPyWrapperMarkerMatrixView(*coords, main_geometry->vertex[iMarker], main_geometry->GetnVertex(iMarker),
+                                      "MarkerInitialCoordinates", true);
+  }
+
   /*!
    * \brief Get a read/write view of the current coordinates of all mesh nodes.
    */
@@ -208,6 +224,16 @@ class CDriverBase {
     return CPyWrapperMatrixView(coords, "Coordinates", false);
   }
 
+  /*!
+   * \brief Get a read/write view of the current coordinates of the mesh nodes of a marker.
+   */
+  inline CPyWrapperMarkerMatrixView MarkerCoordinates(unsigned short iMarker) {
+    if (iMarker >= GetNumberMarkers()) SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
+    auto& coords = const_cast<su2activematrix&>(main_geometry->nodes->GetCoord());
+    return CPyWrapperMarkerMatrixView(coords, main_geometry->vertex[iMarker], main_geometry->GetnVertex(iMarker),
+                                      "MarkerCoordinates", false);
+  }
+
   /*!
    * \brief Get the number of markers in the mesh.
    * \return Number of markers.
@@ -328,14 +354,47 @@ class CDriverBase {
    */
   map<string, unsigned short> GetSolverIndices() const;
 
+  /*!
+   * \brief Get the structural solver solution variable names with their associated indices.
+   * These correspond to the column indices in the matrix returned by e.g. Solution().
+   */
+  map<string, unsigned short> GetFEASolutionIndices() const;
+
   /*!
    * \brief Get a read/write view of the current solution on all mesh nodes of a solver.
    */
   inline CPyWrapperMatrixView Solution(unsigned short iSolver) {
-    auto* solver = solver_container[ZONE_0][INST_0][MESH_0][iSolver];
-    if (solver == nullptr) SU2_MPI::Error("The selected solver does not exist.", CURRENT_FUNCTION);
-    auto& solution = solver->GetNodes()->GetSolution();
-    return CPyWrapperMatrixView(solution, "Solution of " + solver->GetSolverName(), false);
+    auto* solver = GetSolverAndCheckMarker(iSolver);
+    return CPyWrapperMatrixView(solver->GetNodes()->GetSolution(), "Solution of " + solver->GetSolverName(), false);
+  }
+
+  /*!
+   * \brief Get a read/write view of the current solution on the mesh nodes of a marker.
+   */
+  inline CPyWrapperMarkerMatrixView MarkerSolution(unsigned short iSolver, unsigned short iMarker) {
+    auto* solver = GetSolverAndCheckMarker(iSolver, iMarker);
+    return CPyWrapperMarkerMatrixView(
+        solver->GetNodes()->GetSolution(), main_geometry->vertex[iMarker], main_geometry->GetnVertex(iMarker),
+        "MarkerSolution of " + solver->GetSolverName(), false);
+  }
+
+  /*!
+   * \brief Get a read/write view of the solution at time N on all mesh nodes of a solver.
+   */
+  inline CPyWrapperMatrixView SolutionTimeN(unsigned short iSolver) {
+    auto* solver = GetSolverAndCheckMarker(iSolver);
+    return CPyWrapperMatrixView(
+        solver->GetNodes()->GetSolution_time_n(), "SolutionTimeN of " + solver->GetSolverName(), false);
+  }
+
+  /*!
+   * \brief Get a read/write view of the solution at time N on the mesh nodes of a marker.
+   */
+  inline CPyWrapperMarkerMatrixView MarkerSolutionTimeN(unsigned short iSolver, unsigned short iMarker) {
+    auto* solver = GetSolverAndCheckMarker(iSolver, iMarker);
+    return CPyWrapperMarkerMatrixView(
+        solver->GetNodes()->GetSolution_time_n(), main_geometry->vertex[iMarker], main_geometry->GetnVertex(iMarker),
+        "MarkerSolutionTimeN of " + solver->GetSolverName(), false);
   }
 
   /*!
@@ -349,15 +408,36 @@ class CDriverBase {
    * \warning Primitive variables are only available for flow solvers.
    */
   inline CPyWrapperMatrixView Primitives() {
-    auto* solver = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL];
-    if (solver == nullptr) SU2_MPI::Error("The flow solver does not exist.", CURRENT_FUNCTION);
-    auto& primitives = const_cast<su2activematrix&>(solver->GetNodes()->GetPrimitive());
-    return CPyWrapperMatrixView(primitives, "Primitives", false);
+    auto* solver = GetSolverAndCheckMarker(FLOW_SOL);
+    return CPyWrapperMatrixView(const_cast<su2activematrix&>(solver->GetNodes()->GetPrimitive()), "Primitives", false);
   }
 
+  /*!
+   * \brief Get a read/write view of the current primitive variables on the mesh nodes of a marker.
+   * \warning Primitive variables are only available for flow solvers.
+   */
+  inline CPyWrapperMarkerMatrixView MarkerPrimitives(unsigned short iMarker) {
+    auto* solver = GetSolverAndCheckMarker(FLOW_SOL, iMarker);
+    return CPyWrapperMarkerMatrixView(
+        const_cast<su2activematrix&>(solver->GetNodes()->GetPrimitive()), main_geometry->vertex[iMarker],
+        main_geometry->GetnVertex(iMarker), "MarkerPrimitives", false);
+  }
 /// \}
 
  protected:
+  /*!
+   * \brief Automates some boilerplate of accessing solution fields for the python wrapper.
+   */
+  inline CSolver* GetSolverAndCheckMarker(unsigned short iSolver,
+                                          unsigned short iMarker = std::numeric_limits<unsigned short>::max()) {
+    if (iMarker < std::numeric_limits<unsigned short>::max() && iMarker > GetNumberMarkers()) {
+      SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
+    }
+    auto* solver = solver_container[ZONE_0][INST_0][MESH_0][iSolver];
+    if (solver == nullptr) SU2_MPI::Error("The selected solver does not exist.", CURRENT_FUNCTION);
+    return solver;
+  }
+
   /*!
    * \brief Initialize containers.
    */
diff --git a/SU2_CFD/include/variables/CVariable.hpp b/SU2_CFD/include/variables/CVariable.hpp
index df6026a71c2..13d04898bd6 100644
--- a/SU2_CFD/include/variables/CVariable.hpp
+++ b/SU2_CFD/include/variables/CVariable.hpp
@@ -492,6 +492,7 @@ class CVariable {
    * \return Pointer to the solution (at time n) vector.
    */
   inline su2double *GetSolution_time_n(unsigned long iPoint) { return Solution_time_n[iPoint]; }
+  inline MatrixType& GetSolution_time_n() { return Solution_time_n; }
 
   /*!
    * \brief Get the solution at time n-1.
@@ -1898,10 +1899,10 @@ class CVariable {
   inline virtual su2double GetSolution_Vel(unsigned long iPoint, unsigned long iVar) const { return 0.0; }
 
   /*!
-   * \brief Get the solution of the problem.
-   * \return Pointer to the solution vector.
+   * \brief Get the velocity (Structural Analysis).
+   * \return Pointer to the velocity vector at a point.
    */
-  inline virtual su2double *GetSolution_Vel(unsigned long iPoint) {return nullptr; }
+  inline virtual su2double* GetSolution_Vel(unsigned long iPoint) { return nullptr; }
 
   /*!
    * \brief Get the velocity of the nodes (Structural Analysis) at time n.
@@ -1911,11 +1912,10 @@ class CVariable {
   inline virtual su2double GetSolution_Vel_time_n(unsigned long iPoint, unsigned long iVar) const { return 0.0; }
 
   /*!
-   * \brief Get the solution at time n.
-   * \return Pointer to the solution (at time n) vector.
+   * \brief Get the velocity of the nodes (Structural Analysis) at time n.
+   * \return Pointer to the velocity vector at a point.
    */
-  inline virtual su2double *GetSolution_Vel_time_n(unsigned long iPoint) { return nullptr; }
-
+  inline virtual su2double* GetSolution_Vel_time_n(unsigned long iPoint) { return nullptr; }
 
   /*!
    * \brief Set the value of the acceleration (Structural Analysis).
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index c00d02c5456..fee7f12ab41 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -315,7 +315,7 @@ unsigned long CDriverBase::GetMarkerNode(unsigned short iMarker, unsigned long i
   if (iVertex >= GetNumberMarkerNodes(iMarker)) {
     SU2_MPI::Error("Vertex index exceeds marker size.", CURRENT_FUNCTION);
   }
-  return geometry_container[MESH_0][INST_0][ZONE_0]->vertex[iMarker][iVertex]->GetNode();
+  return main_geometry->vertex[iMarker][iVertex]->GetNode();
 }
 
 vector<passivedouble> CDriverBase::GetMarkerVertexNormals(unsigned short iMarker, unsigned long iVertex,
@@ -405,6 +405,27 @@ map<string, unsigned short> CDriverBase::GetSolverIndices() const {
   return indexMap;
 }
 
+std::map<string, unsigned short> CDriverBase::GetFEASolutionIndices() const {
+  if (solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL] == nullptr) {
+    SU2_MPI::Error("The FEA solver does not exist.", CURRENT_FUNCTION);
+  }
+  const auto nDim = main_geometry->GetnDim();
+  std::map<string, unsigned short> names;
+  names["DISPLACEMENT_X"] = 0;
+  names["DISPLACEMENT_Y"] = 1;
+  if (nDim == 3) names["DISPLACEMENT_Z"] = 2;
+
+  if (main_config->GetTime_Domain()) {
+    names["VELOCITY_X"] = nDim;
+    names["VELOCITY_Y"] = nDim + 1;
+    if (nDim == 3) names["VELOCITY_Z"] = nDim + 2;
+    names["ACCELERATION_X"] = 2 * nDim;
+    names["ACCELERATION_Y"] = 2 * nDim + 1;
+    if (nDim == 3) names["ACCELERATION_Z"] = 2 * nDim + 2;
+  }
+  return names;
+}
+
 map<string, unsigned short> CDriverBase::GetPrimitiveIndices() const {
   if (solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL] == nullptr) {
     SU2_MPI::Error("The flow solver does not exist.", CURRENT_FUNCTION);
diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index 95e8cd321f7..cc7cd689005 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -162,11 +162,11 @@ passivedouble CDriver::Get_LiftCoeff() const {
 /* Functions to obtain global parameters from SU2 (time steps, delta t, etc.)   */
 //////////////////////////////////////////////////////////////////////////////////
 
-unsigned long CDriver::GetnTimeIter() const { return config_container[ZONE_0]->GetnTime_Iter(); }
+unsigned long CDriver::GetNumberTimeIter() const { return config_container[ZONE_0]->GetnTime_Iter(); }
 
-unsigned long CDriver::GetTime_Iter() const { return TimeIter; }
+unsigned long CDriver::GetTimeIter() const { return TimeIter; }
 
-passivedouble CDriver::GetUnsteady_TimeStep() const {
+passivedouble CDriver::GetUnsteadyTimeStep() const {
   return SU2_TYPE::GetValue(config_container[ZONE_0]->GetTime_Step());
 }
 
@@ -445,79 +445,6 @@ void CDriver::SetFEA_Loads(unsigned short iMarker, unsigned long iVertex, passiv
   solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL]->GetNodes()->Set_FlowTraction(iPoint, NodalForce);
 }
 
-vector<passivedouble> CDriver::GetFEA_Displacements(unsigned short iMarker, unsigned long iVertex) const {
-  unsigned long iPoint;
-  vector<su2double> Displacements(3, 0.0);
-  vector<passivedouble> Displacements_passive(3, 0.0);
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
-  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-
-  Displacements[0] = solver->GetNodes()->GetSolution(iPoint, 0);
-  Displacements[1] = solver->GetNodes()->GetSolution(iPoint, 1);
-  if (geometry->GetnDim() == 3)
-    Displacements[2] = solver->GetNodes()->GetSolution(iPoint, 2);
-  else
-    Displacements[2] = 0.0;
-
-  Displacements_passive[0] = SU2_TYPE::GetValue(Displacements[0]);
-  Displacements_passive[1] = SU2_TYPE::GetValue(Displacements[1]);
-  Displacements_passive[2] = SU2_TYPE::GetValue(Displacements[2]);
-
-  return Displacements_passive;
-}
-
-vector<passivedouble> CDriver::GetFEA_Velocity(unsigned short iMarker, unsigned long iVertex) const {
-  unsigned long iPoint;
-  vector<su2double> Velocity(3, 0.0);
-  vector<passivedouble> Velocity_passive(3, 0.0);
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
-  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-
-  if (config_container[ZONE_0]->GetDynamic_Analysis() == DYNAMIC) {
-    Velocity[0] = solver->GetNodes()->GetSolution_Vel(iPoint, 0);
-    Velocity[1] = solver->GetNodes()->GetSolution_Vel(iPoint, 1);
-    if (geometry->GetnDim() == 3)
-      Velocity[2] = solver->GetNodes()->GetSolution_Vel(iPoint, 2);
-    else
-      Velocity[2] = 0.0;
-  }
-
-  Velocity_passive[0] = SU2_TYPE::GetValue(Velocity[0]);
-  Velocity_passive[1] = SU2_TYPE::GetValue(Velocity[1]);
-  Velocity_passive[2] = SU2_TYPE::GetValue(Velocity[2]);
-
-  return Velocity_passive;
-}
-
-vector<passivedouble> CDriver::GetFEA_Velocity_n(unsigned short iMarker, unsigned long iVertex) const {
-  unsigned long iPoint;
-  vector<su2double> Velocity_n(3, 0.0);
-  vector<passivedouble> Velocity_n_passive(3, 0.0);
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
-  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-
-  if (config_container[ZONE_0]->GetDynamic_Analysis() == DYNAMIC) {
-    Velocity_n[0] = solver->GetNodes()->GetSolution_Vel_time_n(iPoint, 0);
-    Velocity_n[1] = solver->GetNodes()->GetSolution_Vel_time_n(iPoint, 1);
-    if (geometry->GetnDim() == 3)
-      Velocity_n[2] = solver->GetNodes()->GetSolution_Vel_time_n(iPoint, 2);
-    else
-      Velocity_n[2] = 0.0;
-  }
-
-  Velocity_n_passive[0] = SU2_TYPE::GetValue(Velocity_n[0]);
-  Velocity_n_passive[1] = SU2_TYPE::GetValue(Velocity_n[1]);
-  Velocity_n_passive[2] = SU2_TYPE::GetValue(Velocity_n[2]);
-
-  return Velocity_n_passive;
-}
-
 ////////////////////////////////////////////////////////////////////////////////
 /* Functions related to adjoint simulations                                   */
 ////////////////////////////////////////////////////////////////////////////////
diff --git a/TestCases/py_wrapper/deforming_bump_in_channel/run.py b/TestCases/py_wrapper/deforming_bump_in_channel/run.py
index f10932b9a13..715e81c1cea 100755
--- a/TestCases/py_wrapper/deforming_bump_in_channel/run.py
+++ b/TestCases/py_wrapper/deforming_bump_in_channel/run.py
@@ -48,17 +48,16 @@ def main():
   nVertex = SU2Driver.GetNumberMarkerNodes(MarkerID) if MarkerID >= 0 else 0
 
   # Retrieve some control parameters from the driver.
-  deltaT = SU2Driver.GetUnsteady_TimeStep()
-  TimeIter = SU2Driver.GetTime_Iter()
-  nTimeIter = SU2Driver.GetnTimeIter()
+  deltaT = SU2Driver.GetUnsteadyTimeStep()
+  TimeIter = SU2Driver.GetTimeIter()
+  nTimeIter = SU2Driver.GetNumberTimeIter()
   time = TimeIter * deltaT
 
   # Extract the initial position of each node on the moving marker.
   CoordX = np.zeros(nVertex)
   CoordY = np.zeros(nVertex)
   for iVertex in range(nVertex):
-    iPoint = SU2Driver.GetMarkerNode(MarkerID, iVertex)
-    CoordX[iVertex], CoordY[iVertex] = SU2Driver.InitialCoordinates().Get(iPoint)
+    CoordX[iVertex], CoordY[iVertex] = SU2Driver.MarkerInitialCoordinates(MarkerID).Get(iVertex)
 
   if rank == 0:
     print("\n------------------------------ Begin Solver -----------------------------\n")
diff --git a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
index 3b33bd46d53..e254137fc27 100755
--- a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
@@ -106,7 +106,10 @@ def main():
   disp=[]
   # Recover the sensitivity
   sens.append(SU2Driver.GetFlowLoad_Sensitivity(MarkerID,5))
-  disp.append(SU2Driver.GetFEA_Displacements(MarkerID,5))
+
+  fea_sol = SU2Driver.GetSolverIndices()["FEA"]
+  marker_disp = SU2Driver.MarkerSolution(fea_sol, MarkerID)
+  disp.append(marker_disp.Get(5))
 
   print("Sens[0]\tSens[1]\tDisp[0]\tDisp[1]\t")
   print(100, 100, sens[0][0], sens[0][1], disp[0][0], disp[0][1])
diff --git a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
index 718fbfd8cb1..0efc10666df 100755
--- a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
+++ b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
@@ -92,17 +92,16 @@ def main():
     nVertex_MovingMarker = SU2Driver.GetNumberMarkerNodes(MovingMarkerID)\
 
   # Retrieve some control parameters from the driver
-  deltaT = SU2Driver.GetUnsteady_TimeStep()
-  TimeIter = SU2Driver.GetTime_Iter()
-  nTimeIter = SU2Driver.GetnTimeIter()
+  deltaT = SU2Driver.GetUnsteadyTimeStep()
+  TimeIter = SU2Driver.GetTimeIter()
+  nTimeIter = SU2Driver.GetNumberTimeIter()
   time = TimeIter*deltaT
 
   # Extract the initial position of each node on the moving marker
   CoordX = np.zeros(nVertex_MovingMarker)
   CoordY = np.zeros(nVertex_MovingMarker)
   for iVertex in range(nVertex_MovingMarker):
-    iPoint = SU2Driver.GetMarkerNode(MovingMarkerID, iVertex)
-    CoordX[iVertex], CoordY[iVertex] = SU2Driver.InitialCoordinates().Get(iPoint)
+    CoordX[iVertex], CoordY[iVertex] = SU2Driver.MarkerInitialCoordinates(MovingMarkerID).Get(iVertex)
 
   # Time loop is defined in Python so that we have acces to SU2 functionalities at each time step
   if rank == 0:
diff --git a/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py b/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
index 6a613b1fa18..2374bade7a7 100755
--- a/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
+++ b/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
@@ -91,9 +91,9 @@ def main():
     nVertex_CHTMarker = SU2Driver.GetNumberMarkerNodes(CHTMarkerID)
 
   # Retrieve some control parameters from the driver
-  deltaT = SU2Driver.GetUnsteady_TimeStep()
-  TimeIter = SU2Driver.GetTime_Iter()
-  nTimeIter = SU2Driver.GetnTimeIter()
+  deltaT = SU2Driver.GetUnsteadyTimeStep()
+  TimeIter = SU2Driver.GetTimeIter()
+  nTimeIter = SU2Driver.GetNumberTimeIter()
   time = TimeIter*deltaT
 
   # Time loop is defined in Python so that we have acces to SU2 functionalities at each time step

From a7c40fb024e1f3b180fd4f75bd862ab4eb3a8b50 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 4 Mar 2023 18:08:29 -0800
Subject: [PATCH 251/656] matrix view for markers

---
 .../containers/CPyWrapperMatrixView.hpp       | 134 ++++++++++++------
 SU2_CFD/include/drivers/CDriver.hpp           |  30 +---
 SU2_CFD/include/drivers/CDriverBase.hpp       |  96 +++++++++++--
 SU2_CFD/include/variables/CVariable.hpp       |  14 +-
 SU2_CFD/src/drivers/CDriverBase.cpp           |  23 ++-
 SU2_CFD/src/python_wrapper_structure.cpp      |  79 +----------
 .../deforming_bump_in_channel/run.py          |   9 +-
 .../flow_load_sens/run_adjoint.py             |   5 +-
 .../launch_flatPlate_rigidMotion.py           |   9 +-
 .../launch_unsteady_CHT_FlatPlate.py          |   6 +-
 10 files changed, 230 insertions(+), 175 deletions(-)

diff --git a/Common/include/containers/CPyWrapperMatrixView.hpp b/Common/include/containers/CPyWrapperMatrixView.hpp
index 2c3d6477ee4..321f062738d 100644
--- a/Common/include/containers/CPyWrapperMatrixView.hpp
+++ b/Common/include/containers/CPyWrapperMatrixView.hpp
@@ -1,6 +1,6 @@
 /*!
  * \file CPyWrapperMatrixView.hpp
- * \brief A simple matrix view to use with the python wrapper.
+ * \brief Simple matrix views to use with the python wrapper.
  * \author P. Gomes
  * \version 7.5.1 "Blackbird"
  *
@@ -27,28 +27,67 @@
 
 #pragma once
 
+#include <string>
 #include <utility>
 #include <vector>
-#include <string>
 
-#include "C2DContainer.hpp"
+#include "../geometry/dual_grid/CVertex.hpp"
 #include "../parallelization/mpi_structure.hpp"
+#include "C2DContainer.hpp"
+
+/*!
+ * \brief Python wrapper matrix interface
+ * The accessors in this macro provide a passive double interface to matrix of
+ * su2double. This can be extended to allow access to derivative information.
+ * Classes that use this macro encapsulate the access to the raw data (su2double)
+ * via the functions "Access(row, col) -> su2double&" (const and non-const versions).
+ * We use a macro because it is diffult to use modern C++ idioms (e.g. CRTP) with
+ * SWIG. In addition to "Access" classes must have member variables "rows_", "cols_",
+ * and "read_only_".
+ */
+#define PY_WRAPPER_MATRIX_INTERFACE                                                                              \
+  /*! \brief Returns the shape of the matrix. */                                                                 \
+  std::pair<unsigned long, unsigned long> Shape() const { return std::make_pair(rows_, cols_); }                 \
+                                                                                                                 \
+  /*! \brief Returns whether the data is read-only [true] or if it can be modified [false]. */                   \
+  bool IsReadOnly() const { return read_only_; }                                                                 \
+                                                                                                                 \
+  /*! \brief Gets the value for a (row, column) pair. */                                                         \
+  passivedouble operator()(unsigned long row, unsigned long col) const { return Get(row, col); }                 \
+                                                                                                                 \
+  /*! \brief Gets the value for a (row, column) pair. */                                                         \
+  passivedouble Get(unsigned long row, unsigned long col) const { return SU2_TYPE::GetValue(Access(row, col)); } \
+                                                                                                                 \
+  /*! \brief Gets the values for a row of the matrix. */                                                         \
+  std::vector<passivedouble> Get(unsigned long row) const {                                                      \
+    std::vector<passivedouble> vals(cols_);                                                                      \
+    for (unsigned long j = 0; j < cols_; ++j) vals[j] = Get(row, j);                                             \
+    return vals;                                                                                                 \
+  }                                                                                                              \
+  /*! \brief Sets the value for a (row, column) pair. This clears derivative information. */                     \
+  void Set(unsigned long row, unsigned long col, passivedouble val) { Access(row, col) = val; }                  \
+                                                                                                                 \
+  /*! \brief Sets the values for a row of the matrix. */                                                         \
+  void Set(unsigned long row, std::vector<passivedouble> vals) {                                                 \
+    unsigned long j = 0;                                                                                         \
+    for (const auto& val : vals) Set(row, j++, val);                                                             \
+  }
 
 /*!
  * \class CPyWrapperMatrixView
  * \ingroup PySU2
- * \brief A simple matrix view to use with the python wrapper. The accessors
- * in this class provide a passive double interface to su2activematrix.
- * This can be extended to allow access to derivative information of su2double.
+ * \brief This class wraps su2activematrix for the python wrapper matrix interface.
+ * It is generaly used to wrap access to solver variables defined for the entire volume.
  */
 class CPyWrapperMatrixView {
- private:
+ protected:
   static_assert(su2activematrix::IsRowMajor, "");
   su2double* data_ = nullptr;
   unsigned long rows_ = 0, cols_ = 0;
   std::string name_;
   bool read_only_ = false;
 
+  /*--- Define the functions required by the interface macro. ---*/
   inline const su2double& Access(unsigned long row, unsigned long col) const {
     if (row > rows_ || col > cols_) SU2_MPI::Error(name_ + " out of bounds", "CPyWrapperMatrixView");
     return data_[row * cols_ + col];
@@ -68,48 +107,59 @@ class CPyWrapperMatrixView {
    * \note "read_only" can be set to true to prevent the data from being modified.
    */
   CPyWrapperMatrixView(su2activematrix& mat, const std::string& name, bool read_only)
-    : data_(mat.data()), rows_(mat.rows()), cols_(mat.cols()), name_(name), read_only_(read_only) {}
-
-  /*!
-   * \brief Returns the shape of the matrix.
-   */
-  std::pair<unsigned long, unsigned long> Shape() const { return std::make_pair(rows_, cols_); }
-
-  /*!
-   * \brief Returns whether the data is read-only [true] or if it can be modified [false].
-   */
-  bool IsReadOnly() const { return read_only_; }
+      : data_(mat.data()), rows_(mat.rows()), cols_(mat.cols()), name_(name), read_only_(read_only) {}
 
-  /*!
-   * \brief Gets the value for a (row, column) pair.
-   */
-  passivedouble operator() (unsigned long row, unsigned long col) const { return Get(row, col); }
+  /*--- Use the macro to generate the interface. ---*/
+  PY_WRAPPER_MATRIX_INTERFACE
+};
 
-  /*!
-   * \brief Gets the value for a (row, column) pair.
-   */
-  passivedouble Get(unsigned long row, unsigned long col) const { return SU2_TYPE::GetValue(Access(row, col)); }
+/*!
+ * \class CPyWrapperMarkerMatrixView
+ * \ingroup PySU2
+ * \brief This class wraps su2activematrix for the python wrapper matrix interface restricting it
+ * to the vertices of a given marker.
+ */
+class CPyWrapperMarkerMatrixView {
+ private:
+  static_assert(su2activematrix::IsRowMajor, "");
+  su2double* data_ = nullptr;
+  const CVertex* const* vertices_ = nullptr;
+  unsigned long rows_ = 0, cols_ = 0;
+  std::string name_;
+  bool read_only_ = false;
 
-  /*!
-   * \brief Gets the values for a row of the matrix.
-   */
-  std::vector<passivedouble> Get(unsigned long row) const {
-    std::vector<passivedouble> vals(cols_);
-    for (unsigned long j = 0; j < cols_; ++j) vals[j] = Get(row, j);
-    return vals;
+  /*--- Define the functions required by the interface macro. ---*/
+  inline const su2double& Access(unsigned long row, unsigned long col) const {
+    if (row > rows_ || col > cols_) SU2_MPI::Error(name_ + " out of bounds", "CPyWrapperMarkerMatrixView");
+    return data_[vertices_[row]->GetNode() * cols_ + col];
+  }
+  inline su2double& Access(unsigned long row, unsigned long col) {
+    if (read_only_) SU2_MPI::Error(name_ + " is read-only", "CPyWrapperMarkerMatrixView");
+    const auto& const_me = *this;
+    return const_cast<su2double&>(const_me.Access(row, col));
   }
 
-  /*!
-   * \brief Sets the value for a (row, column) pair.
-   * \note This clears derivative information (consistently with C++ operator= with passive rhs).
-   */
-  void Set(unsigned long row, unsigned long col, passivedouble val) { Access(row, col) = val; }
+ public:
+  CPyWrapperMarkerMatrixView() = default;
 
   /*!
-   * \brief Sets the values for a row of the matrix.
+   * \brief Construct the view of the matrix.
+   * \note "name" should be set to the variable name being returned to give better information to users.
+   * \note "read_only" can be set to true to prevent the data from being modified.
    */
-  void Set(unsigned long row, std::vector<passivedouble> vals) {
-    unsigned long j = 0;
-    for (const auto& val : vals) Set(row, j++, val);
+  CPyWrapperMarkerMatrixView(su2activematrix& mat, const CVertex* const* vertices, unsigned long n_vertices,
+                             const std::string& name, bool read_only)
+      : data_(mat.data()),
+        vertices_(vertices),
+        rows_(n_vertices),
+        cols_(mat.cols()),
+        name_(name),
+        read_only_(read_only) {
+    if (mat.rows() < n_vertices) {
+      SU2_MPI::Error(name + " has fewer rows than the number of vertices in the marker.", "CPyWrapperMarkerMatrixView");
+    }
   }
+
+  /*--- Use the macro to generate the interface. ---*/
+  PY_WRAPPER_MATRIX_INTERFACE
 };
diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index a26c841656f..ae50e59e2f1 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -457,19 +457,19 @@ class CDriver : public CDriverBase {
    * \brief Get the number of external iterations.
    * \return Number of external iterations.
    */
-  unsigned long GetnTimeIter() const;
+  unsigned long GetNumberTimeIter() const;
 
   /*!
    * \brief Get the current external iteration.
    * \return Current external iteration.
    */
-  unsigned long GetTime_Iter() const;
+  unsigned long GetTimeIter() const;
 
   /*!
    * \brief Get the unsteady time step.
    * \return Unsteady time step.
    */
-  passivedouble GetUnsteady_TimeStep() const;
+  passivedouble GetUnsteadyTimeStep() const;
 
   /*!
    * \brief Get the name of the output file for the surface.
@@ -564,30 +564,6 @@ class CDriver : public CDriverBase {
   void SetFEA_Loads(unsigned short iMarker, unsigned long iVertex, passivedouble LoadX, passivedouble LoadY,
                     passivedouble LoadZ);
 
-  /*!
-   * \brief Return the displacements from the FEA solver.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Vector of displacements.
-   */
-  vector<passivedouble> GetFEA_Displacements(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Return the velocities from the FEA Solver.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Vector of velocities.
-   */
-  vector<passivedouble> GetFEA_Velocity(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Return the velocities from the FEA Solver.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Vector of velocities at time n.
-   */
-  vector<passivedouble> GetFEA_Velocity_n(unsigned short iMarker, unsigned long iVertex) const;
-
   /*!
    * \brief Get the sensitivity of the flow loads for the structural solver.
    * \param[in] iMarker - Marker identifier.
diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index c83ad9bdf31..9d6c60334af 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -27,6 +27,7 @@
 
 #pragma once
 
+#include <limits>
 #include "../../../Common/include/CConfig.hpp"
 #include "../../../Common/include/containers/CPyWrapperMatrixView.hpp"
 #include "../numerics/CNumerics.hpp"
@@ -200,6 +201,21 @@ class CDriverBase {
     return CPyWrapperMatrixView(*coords, "InitialCoordinates", true);
   }
 
+  /*!
+   * \brief Get a read-only view of the initial (undeformed) coordinates of the mesh nodes of a marker.
+   */
+  inline CPyWrapperMarkerMatrixView MarkerInitialCoordinates(unsigned short iMarker) const {
+    if (!main_config->GetDeform_Mesh()) {
+      SU2_MPI::Error("Initial coordinates are only available with DEFORM_MESH= YES", CURRENT_FUNCTION);
+    }
+    if (iMarker >= GetNumberMarkers()) SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
+
+    auto* coords =
+        const_cast<su2activematrix*>(solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord());
+    return CPyWrapperMarkerMatrixView(*coords, main_geometry->vertex[iMarker], main_geometry->GetnVertex(iMarker),
+                                      "MarkerInitialCoordinates", true);
+  }
+
   /*!
    * \brief Get a read/write view of the current coordinates of all mesh nodes.
    */
@@ -208,6 +224,16 @@ class CDriverBase {
     return CPyWrapperMatrixView(coords, "Coordinates", false);
   }
 
+  /*!
+   * \brief Get a read/write view of the current coordinates of the mesh nodes of a marker.
+   */
+  inline CPyWrapperMarkerMatrixView MarkerCoordinates(unsigned short iMarker) {
+    if (iMarker >= GetNumberMarkers()) SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
+    auto& coords = const_cast<su2activematrix&>(main_geometry->nodes->GetCoord());
+    return CPyWrapperMarkerMatrixView(coords, main_geometry->vertex[iMarker], main_geometry->GetnVertex(iMarker),
+                                      "MarkerCoordinates", false);
+  }
+
   /*!
    * \brief Get the number of markers in the mesh.
    * \return Number of markers.
@@ -328,14 +354,47 @@ class CDriverBase {
    */
   map<string, unsigned short> GetSolverIndices() const;
 
+  /*!
+   * \brief Get the structural solver solution variable names with their associated indices.
+   * These correspond to the column indices in the matrix returned by e.g. Solution().
+   */
+  map<string, unsigned short> GetFEASolutionIndices() const;
+
   /*!
    * \brief Get a read/write view of the current solution on all mesh nodes of a solver.
    */
   inline CPyWrapperMatrixView Solution(unsigned short iSolver) {
-    auto* solver = solver_container[ZONE_0][INST_0][MESH_0][iSolver];
-    if (solver == nullptr) SU2_MPI::Error("The selected solver does not exist.", CURRENT_FUNCTION);
-    auto& solution = solver->GetNodes()->GetSolution();
-    return CPyWrapperMatrixView(solution, "Solution of " + solver->GetSolverName(), false);
+    auto* solver = GetSolverAndCheckMarker(iSolver);
+    return CPyWrapperMatrixView(solver->GetNodes()->GetSolution(), "Solution of " + solver->GetSolverName(), false);
+  }
+
+  /*!
+   * \brief Get a read/write view of the current solution on the mesh nodes of a marker.
+   */
+  inline CPyWrapperMarkerMatrixView MarkerSolution(unsigned short iSolver, unsigned short iMarker) {
+    auto* solver = GetSolverAndCheckMarker(iSolver, iMarker);
+    return CPyWrapperMarkerMatrixView(
+        solver->GetNodes()->GetSolution(), main_geometry->vertex[iMarker], main_geometry->GetnVertex(iMarker),
+        "MarkerSolution of " + solver->GetSolverName(), false);
+  }
+
+  /*!
+   * \brief Get a read/write view of the solution at time N on all mesh nodes of a solver.
+   */
+  inline CPyWrapperMatrixView SolutionTimeN(unsigned short iSolver) {
+    auto* solver = GetSolverAndCheckMarker(iSolver);
+    return CPyWrapperMatrixView(
+        solver->GetNodes()->GetSolution_time_n(), "SolutionTimeN of " + solver->GetSolverName(), false);
+  }
+
+  /*!
+   * \brief Get a read/write view of the solution at time N on the mesh nodes of a marker.
+   */
+  inline CPyWrapperMarkerMatrixView MarkerSolutionTimeN(unsigned short iSolver, unsigned short iMarker) {
+    auto* solver = GetSolverAndCheckMarker(iSolver, iMarker);
+    return CPyWrapperMarkerMatrixView(
+        solver->GetNodes()->GetSolution_time_n(), main_geometry->vertex[iMarker], main_geometry->GetnVertex(iMarker),
+        "MarkerSolutionTimeN of " + solver->GetSolverName(), false);
   }
 
   /*!
@@ -349,15 +408,36 @@ class CDriverBase {
    * \warning Primitive variables are only available for flow solvers.
    */
   inline CPyWrapperMatrixView Primitives() {
-    auto* solver = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL];
-    if (solver == nullptr) SU2_MPI::Error("The flow solver does not exist.", CURRENT_FUNCTION);
-    auto& primitives = const_cast<su2activematrix&>(solver->GetNodes()->GetPrimitive());
-    return CPyWrapperMatrixView(primitives, "Primitives", false);
+    auto* solver = GetSolverAndCheckMarker(FLOW_SOL);
+    return CPyWrapperMatrixView(const_cast<su2activematrix&>(solver->GetNodes()->GetPrimitive()), "Primitives", false);
   }
 
+  /*!
+   * \brief Get a read/write view of the current primitive variables on the mesh nodes of a marker.
+   * \warning Primitive variables are only available for flow solvers.
+   */
+  inline CPyWrapperMarkerMatrixView MarkerPrimitives(unsigned short iMarker) {
+    auto* solver = GetSolverAndCheckMarker(FLOW_SOL, iMarker);
+    return CPyWrapperMarkerMatrixView(
+        const_cast<su2activematrix&>(solver->GetNodes()->GetPrimitive()), main_geometry->vertex[iMarker],
+        main_geometry->GetnVertex(iMarker), "MarkerPrimitives", false);
+  }
 /// \}
 
  protected:
+  /*!
+   * \brief Automates some boilerplate of accessing solution fields for the python wrapper.
+   */
+  inline CSolver* GetSolverAndCheckMarker(unsigned short iSolver,
+                                          unsigned short iMarker = std::numeric_limits<unsigned short>::max()) {
+    if (iMarker < std::numeric_limits<unsigned short>::max() && iMarker > GetNumberMarkers()) {
+      SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
+    }
+    auto* solver = solver_container[ZONE_0][INST_0][MESH_0][iSolver];
+    if (solver == nullptr) SU2_MPI::Error("The selected solver does not exist.", CURRENT_FUNCTION);
+    return solver;
+  }
+
   /*!
    * \brief Initialize containers.
    */
diff --git a/SU2_CFD/include/variables/CVariable.hpp b/SU2_CFD/include/variables/CVariable.hpp
index df6026a71c2..13d04898bd6 100644
--- a/SU2_CFD/include/variables/CVariable.hpp
+++ b/SU2_CFD/include/variables/CVariable.hpp
@@ -492,6 +492,7 @@ class CVariable {
    * \return Pointer to the solution (at time n) vector.
    */
   inline su2double *GetSolution_time_n(unsigned long iPoint) { return Solution_time_n[iPoint]; }
+  inline MatrixType& GetSolution_time_n() { return Solution_time_n; }
 
   /*!
    * \brief Get the solution at time n-1.
@@ -1898,10 +1899,10 @@ class CVariable {
   inline virtual su2double GetSolution_Vel(unsigned long iPoint, unsigned long iVar) const { return 0.0; }
 
   /*!
-   * \brief Get the solution of the problem.
-   * \return Pointer to the solution vector.
+   * \brief Get the velocity (Structural Analysis).
+   * \return Pointer to the velocity vector at a point.
    */
-  inline virtual su2double *GetSolution_Vel(unsigned long iPoint) {return nullptr; }
+  inline virtual su2double* GetSolution_Vel(unsigned long iPoint) { return nullptr; }
 
   /*!
    * \brief Get the velocity of the nodes (Structural Analysis) at time n.
@@ -1911,11 +1912,10 @@ class CVariable {
   inline virtual su2double GetSolution_Vel_time_n(unsigned long iPoint, unsigned long iVar) const { return 0.0; }
 
   /*!
-   * \brief Get the solution at time n.
-   * \return Pointer to the solution (at time n) vector.
+   * \brief Get the velocity of the nodes (Structural Analysis) at time n.
+   * \return Pointer to the velocity vector at a point.
    */
-  inline virtual su2double *GetSolution_Vel_time_n(unsigned long iPoint) { return nullptr; }
-
+  inline virtual su2double* GetSolution_Vel_time_n(unsigned long iPoint) { return nullptr; }
 
   /*!
    * \brief Set the value of the acceleration (Structural Analysis).
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index c00d02c5456..fee7f12ab41 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -315,7 +315,7 @@ unsigned long CDriverBase::GetMarkerNode(unsigned short iMarker, unsigned long i
   if (iVertex >= GetNumberMarkerNodes(iMarker)) {
     SU2_MPI::Error("Vertex index exceeds marker size.", CURRENT_FUNCTION);
   }
-  return geometry_container[MESH_0][INST_0][ZONE_0]->vertex[iMarker][iVertex]->GetNode();
+  return main_geometry->vertex[iMarker][iVertex]->GetNode();
 }
 
 vector<passivedouble> CDriverBase::GetMarkerVertexNormals(unsigned short iMarker, unsigned long iVertex,
@@ -405,6 +405,27 @@ map<string, unsigned short> CDriverBase::GetSolverIndices() const {
   return indexMap;
 }
 
+std::map<string, unsigned short> CDriverBase::GetFEASolutionIndices() const {
+  if (solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL] == nullptr) {
+    SU2_MPI::Error("The FEA solver does not exist.", CURRENT_FUNCTION);
+  }
+  const auto nDim = main_geometry->GetnDim();
+  std::map<string, unsigned short> names;
+  names["DISPLACEMENT_X"] = 0;
+  names["DISPLACEMENT_Y"] = 1;
+  if (nDim == 3) names["DISPLACEMENT_Z"] = 2;
+
+  if (main_config->GetTime_Domain()) {
+    names["VELOCITY_X"] = nDim;
+    names["VELOCITY_Y"] = nDim + 1;
+    if (nDim == 3) names["VELOCITY_Z"] = nDim + 2;
+    names["ACCELERATION_X"] = 2 * nDim;
+    names["ACCELERATION_Y"] = 2 * nDim + 1;
+    if (nDim == 3) names["ACCELERATION_Z"] = 2 * nDim + 2;
+  }
+  return names;
+}
+
 map<string, unsigned short> CDriverBase::GetPrimitiveIndices() const {
   if (solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL] == nullptr) {
     SU2_MPI::Error("The flow solver does not exist.", CURRENT_FUNCTION);
diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index 95e8cd321f7..cc7cd689005 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -162,11 +162,11 @@ passivedouble CDriver::Get_LiftCoeff() const {
 /* Functions to obtain global parameters from SU2 (time steps, delta t, etc.)   */
 //////////////////////////////////////////////////////////////////////////////////
 
-unsigned long CDriver::GetnTimeIter() const { return config_container[ZONE_0]->GetnTime_Iter(); }
+unsigned long CDriver::GetNumberTimeIter() const { return config_container[ZONE_0]->GetnTime_Iter(); }
 
-unsigned long CDriver::GetTime_Iter() const { return TimeIter; }
+unsigned long CDriver::GetTimeIter() const { return TimeIter; }
 
-passivedouble CDriver::GetUnsteady_TimeStep() const {
+passivedouble CDriver::GetUnsteadyTimeStep() const {
   return SU2_TYPE::GetValue(config_container[ZONE_0]->GetTime_Step());
 }
 
@@ -445,79 +445,6 @@ void CDriver::SetFEA_Loads(unsigned short iMarker, unsigned long iVertex, passiv
   solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL]->GetNodes()->Set_FlowTraction(iPoint, NodalForce);
 }
 
-vector<passivedouble> CDriver::GetFEA_Displacements(unsigned short iMarker, unsigned long iVertex) const {
-  unsigned long iPoint;
-  vector<su2double> Displacements(3, 0.0);
-  vector<passivedouble> Displacements_passive(3, 0.0);
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
-  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-
-  Displacements[0] = solver->GetNodes()->GetSolution(iPoint, 0);
-  Displacements[1] = solver->GetNodes()->GetSolution(iPoint, 1);
-  if (geometry->GetnDim() == 3)
-    Displacements[2] = solver->GetNodes()->GetSolution(iPoint, 2);
-  else
-    Displacements[2] = 0.0;
-
-  Displacements_passive[0] = SU2_TYPE::GetValue(Displacements[0]);
-  Displacements_passive[1] = SU2_TYPE::GetValue(Displacements[1]);
-  Displacements_passive[2] = SU2_TYPE::GetValue(Displacements[2]);
-
-  return Displacements_passive;
-}
-
-vector<passivedouble> CDriver::GetFEA_Velocity(unsigned short iMarker, unsigned long iVertex) const {
-  unsigned long iPoint;
-  vector<su2double> Velocity(3, 0.0);
-  vector<passivedouble> Velocity_passive(3, 0.0);
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
-  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-
-  if (config_container[ZONE_0]->GetDynamic_Analysis() == DYNAMIC) {
-    Velocity[0] = solver->GetNodes()->GetSolution_Vel(iPoint, 0);
-    Velocity[1] = solver->GetNodes()->GetSolution_Vel(iPoint, 1);
-    if (geometry->GetnDim() == 3)
-      Velocity[2] = solver->GetNodes()->GetSolution_Vel(iPoint, 2);
-    else
-      Velocity[2] = 0.0;
-  }
-
-  Velocity_passive[0] = SU2_TYPE::GetValue(Velocity[0]);
-  Velocity_passive[1] = SU2_TYPE::GetValue(Velocity[1]);
-  Velocity_passive[2] = SU2_TYPE::GetValue(Velocity[2]);
-
-  return Velocity_passive;
-}
-
-vector<passivedouble> CDriver::GetFEA_Velocity_n(unsigned short iMarker, unsigned long iVertex) const {
-  unsigned long iPoint;
-  vector<su2double> Velocity_n(3, 0.0);
-  vector<passivedouble> Velocity_n_passive(3, 0.0);
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL];
-  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-
-  if (config_container[ZONE_0]->GetDynamic_Analysis() == DYNAMIC) {
-    Velocity_n[0] = solver->GetNodes()->GetSolution_Vel_time_n(iPoint, 0);
-    Velocity_n[1] = solver->GetNodes()->GetSolution_Vel_time_n(iPoint, 1);
-    if (geometry->GetnDim() == 3)
-      Velocity_n[2] = solver->GetNodes()->GetSolution_Vel_time_n(iPoint, 2);
-    else
-      Velocity_n[2] = 0.0;
-  }
-
-  Velocity_n_passive[0] = SU2_TYPE::GetValue(Velocity_n[0]);
-  Velocity_n_passive[1] = SU2_TYPE::GetValue(Velocity_n[1]);
-  Velocity_n_passive[2] = SU2_TYPE::GetValue(Velocity_n[2]);
-
-  return Velocity_n_passive;
-}
-
 ////////////////////////////////////////////////////////////////////////////////
 /* Functions related to adjoint simulations                                   */
 ////////////////////////////////////////////////////////////////////////////////
diff --git a/TestCases/py_wrapper/deforming_bump_in_channel/run.py b/TestCases/py_wrapper/deforming_bump_in_channel/run.py
index f10932b9a13..715e81c1cea 100755
--- a/TestCases/py_wrapper/deforming_bump_in_channel/run.py
+++ b/TestCases/py_wrapper/deforming_bump_in_channel/run.py
@@ -48,17 +48,16 @@ def main():
   nVertex = SU2Driver.GetNumberMarkerNodes(MarkerID) if MarkerID >= 0 else 0
 
   # Retrieve some control parameters from the driver.
-  deltaT = SU2Driver.GetUnsteady_TimeStep()
-  TimeIter = SU2Driver.GetTime_Iter()
-  nTimeIter = SU2Driver.GetnTimeIter()
+  deltaT = SU2Driver.GetUnsteadyTimeStep()
+  TimeIter = SU2Driver.GetTimeIter()
+  nTimeIter = SU2Driver.GetNumberTimeIter()
   time = TimeIter * deltaT
 
   # Extract the initial position of each node on the moving marker.
   CoordX = np.zeros(nVertex)
   CoordY = np.zeros(nVertex)
   for iVertex in range(nVertex):
-    iPoint = SU2Driver.GetMarkerNode(MarkerID, iVertex)
-    CoordX[iVertex], CoordY[iVertex] = SU2Driver.InitialCoordinates().Get(iPoint)
+    CoordX[iVertex], CoordY[iVertex] = SU2Driver.MarkerInitialCoordinates(MarkerID).Get(iVertex)
 
   if rank == 0:
     print("\n------------------------------ Begin Solver -----------------------------\n")
diff --git a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
index 3b33bd46d53..e254137fc27 100755
--- a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
@@ -106,7 +106,10 @@ def main():
   disp=[]
   # Recover the sensitivity
   sens.append(SU2Driver.GetFlowLoad_Sensitivity(MarkerID,5))
-  disp.append(SU2Driver.GetFEA_Displacements(MarkerID,5))
+
+  fea_sol = SU2Driver.GetSolverIndices()["FEA"]
+  marker_disp = SU2Driver.MarkerSolution(fea_sol, MarkerID)
+  disp.append(marker_disp.Get(5))
 
   print("Sens[0]\tSens[1]\tDisp[0]\tDisp[1]\t")
   print(100, 100, sens[0][0], sens[0][1], disp[0][0], disp[0][1])
diff --git a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
index 718fbfd8cb1..0efc10666df 100755
--- a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
+++ b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
@@ -92,17 +92,16 @@ def main():
     nVertex_MovingMarker = SU2Driver.GetNumberMarkerNodes(MovingMarkerID)\
 
   # Retrieve some control parameters from the driver
-  deltaT = SU2Driver.GetUnsteady_TimeStep()
-  TimeIter = SU2Driver.GetTime_Iter()
-  nTimeIter = SU2Driver.GetnTimeIter()
+  deltaT = SU2Driver.GetUnsteadyTimeStep()
+  TimeIter = SU2Driver.GetTimeIter()
+  nTimeIter = SU2Driver.GetNumberTimeIter()
   time = TimeIter*deltaT
 
   # Extract the initial position of each node on the moving marker
   CoordX = np.zeros(nVertex_MovingMarker)
   CoordY = np.zeros(nVertex_MovingMarker)
   for iVertex in range(nVertex_MovingMarker):
-    iPoint = SU2Driver.GetMarkerNode(MovingMarkerID, iVertex)
-    CoordX[iVertex], CoordY[iVertex] = SU2Driver.InitialCoordinates().Get(iPoint)
+    CoordX[iVertex], CoordY[iVertex] = SU2Driver.MarkerInitialCoordinates(MovingMarkerID).Get(iVertex)
 
   # Time loop is defined in Python so that we have acces to SU2 functionalities at each time step
   if rank == 0:
diff --git a/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py b/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
index 6a613b1fa18..2374bade7a7 100755
--- a/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
+++ b/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
@@ -91,9 +91,9 @@ def main():
     nVertex_CHTMarker = SU2Driver.GetNumberMarkerNodes(CHTMarkerID)
 
   # Retrieve some control parameters from the driver
-  deltaT = SU2Driver.GetUnsteady_TimeStep()
-  TimeIter = SU2Driver.GetTime_Iter()
-  nTimeIter = SU2Driver.GetnTimeIter()
+  deltaT = SU2Driver.GetUnsteadyTimeStep()
+  TimeIter = SU2Driver.GetTimeIter()
+  nTimeIter = SU2Driver.GetNumberTimeIter()
   time = TimeIter*deltaT
 
   # Time loop is defined in Python so that we have acces to SU2 functionalities at each time step

From 267353b13c8be89bd52768938e1c10c07a6967b1 Mon Sep 17 00:00:00 2001
From: PENGYAN777 <peng.yan@mail.polimi.it>
Date: Sun, 5 Mar 2023 10:29:53 +0100
Subject: [PATCH 252/656] 5 March

---
 SU2_CFD/include/fluid/CCoolProp.hpp |  1 +
 SU2_CFD/src/fluid/CCoolProp.cpp     | 24 ++++++++++++------------
 2 files changed, 13 insertions(+), 12 deletions(-)

diff --git a/SU2_CFD/include/fluid/CCoolProp.hpp b/SU2_CFD/include/fluid/CCoolProp.hpp
index 5caec075b5e..0959271508d 100644
--- a/SU2_CFD/include/fluid/CCoolProp.hpp
+++ b/SU2_CFD/include/fluid/CCoolProp.hpp
@@ -50,6 +50,7 @@ class CCoolProp final : public CFluidModel {
   su2double acentric_factor{0.0};      /*!< \brief acentric factor */
 #ifdef USE_COOLPROP
   std::unique_ptr<CoolProp::AbstractState> fluid_entity;   /*!< \brief fluid entity */
+  su2double epsilon{0.01};  /*!< threshold for pressure */
 #endif
 
  public:
diff --git a/SU2_CFD/src/fluid/CCoolProp.cpp b/SU2_CFD/src/fluid/CCoolProp.cpp
index 456605f827a..22a37cc565a 100644
--- a/SU2_CFD/src/fluid/CCoolProp.cpp
+++ b/SU2_CFD/src/fluid/CCoolProp.cpp
@@ -55,15 +55,15 @@ void CCoolProp::SetTDState_rhoe(su2double rho, su2double e) {
   dPde_rho = fluid_entity->first_partial_deriv(CoolProp::iP, CoolProp::iUmass, CoolProp::iDmass);
   dTdrho_e = fluid_entity->first_partial_deriv(CoolProp::iT, CoolProp::iDmass, CoolProp::iUmass);
   dTde_rho = fluid_entity->first_partial_deriv(CoolProp::iT, CoolProp::iUmass, CoolProp::iDmass);
-  if (fluid_entity->phase() == 6) {
+  if (fluid_entity->phase() == CoolProp::iphase_twophase) {
     // assume it is pure gas
     fluid_entity->specify_phase(CoolProp::iphase_gas);
-    if (abs(Pressure / Pressure_Critical - 1) < 0.01) {
+    if (abs(Pressure / Pressure_Critical - 1) < epsilon) {
       // if P is very cloase to Pc, the CoolProp has issue
-      Pressure = Pressure_Critical * 0.99;
+      Pressure = Pressure_Critical * (1-epsilon);
     }
     fluid_entity->update(CoolProp::PT_INPUTS, Pressure, Temperature);
-    if (abs(fluid_entity->rhomass() / Density - 1) * 100 < 1) {
+    if (abs(fluid_entity->rhomass() / Density - 1) < epsilon) {
       // origial phase is near saturation gas, then just compute sound speed
       SoundSpeed2 = pow(fluid_entity->speed_sound(), 2);
     }
@@ -79,8 +79,8 @@ void CCoolProp::SetTDState_rhoe(su2double rho, su2double e) {
 }
 
 void CCoolProp::SetTDState_PT(su2double P, su2double T) {
-  if (abs(P / Pressure_Critical - 1) < 0.01) {
-    P = Pressure_Critical * 0.99;
+  if (abs(P / Pressure_Critical - 1) < epsilon) {
+    P = Pressure_Critical * (1-epsilon);
   }
   fluid_entity->update(CoolProp::PT_INPUTS, P, T);
   su2double rho = fluid_entity->rhomass();
@@ -89,8 +89,8 @@ void CCoolProp::SetTDState_PT(su2double P, su2double T) {
 }
 
 void CCoolProp::SetTDState_Prho(su2double P, su2double rho) {
-  if (abs(P / Pressure_Critical - 1) < 0.01) {
-    P = Pressure_Critical * 0.99;
+  if (abs(P / Pressure_Critical - 1) < epsilon) {
+    P = Pressure_Critical * (1-epsilon);
   }
   fluid_entity->update(CoolProp::DmassP_INPUTS, rho, P);
   su2double e = fluid_entity->umass();
@@ -98,8 +98,8 @@ void CCoolProp::SetTDState_Prho(su2double P, su2double rho) {
 }
 
 void CCoolProp::SetEnergy_Prho(su2double P, su2double rho) {
-  if (abs(P / Pressure_Critical - 1) < 0.01) {
-    P = Pressure_Critical * 0.99;
+  if (abs(P / Pressure_Critical - 1) < epsilon) {
+    P = Pressure_Critical * (1-epsilon);
   }
   fluid_entity->update(CoolProp::DmassP_INPUTS, rho, P);
   StaticEnergy = fluid_entity->umass();
@@ -113,8 +113,8 @@ void CCoolProp::SetTDState_hs(su2double h, su2double s) {
 }
 
 void CCoolProp::SetTDState_Ps(su2double P, su2double s) {
-  if (abs(P / Pressure_Critical - 1) < 0.01) {
-    P = Pressure_Critical * 0.99;
+  if (abs(P / Pressure_Critical - 1) < epsilon) {
+    P = Pressure_Critical * (1-epsilon);
   }
   fluid_entity->update(CoolProp::PSmass_INPUTS, P, s);
   su2double rho = fluid_entity->rhomass();

From 0fdd9a045d03eb2c757bcac577dcd85da4cff1c9 Mon Sep 17 00:00:00 2001
From: PENGYAN777 <peng.yan@mail.polimi.it>
Date: Mon, 6 Mar 2023 09:26:30 +0100
Subject: [PATCH 253/656] add switch

---
 SU2_CFD/src/fluid/CCoolProp.cpp | 36 +++++++++++++++++++++++++++------
 1 file changed, 30 insertions(+), 6 deletions(-)

diff --git a/SU2_CFD/src/fluid/CCoolProp.cpp b/SU2_CFD/src/fluid/CCoolProp.cpp
index 22a37cc565a..e59d6fe3927 100644
--- a/SU2_CFD/src/fluid/CCoolProp.cpp
+++ b/SU2_CFD/src/fluid/CCoolProp.cpp
@@ -59,8 +59,12 @@ void CCoolProp::SetTDState_rhoe(su2double rho, su2double e) {
     // assume it is pure gas
     fluid_entity->specify_phase(CoolProp::iphase_gas);
     if (abs(Pressure / Pressure_Critical - 1) < epsilon) {
-      // if P is very cloase to Pc, the CoolProp has issue
-      Pressure = Pressure_Critical * (1-epsilon);
+      if (Pressure >= Pressure_Critical){
+        Pressure = Pressure_Critical * (1 + epsilon);
+      }
+      else {
+        Pressure = Pressure_Critical * (1 - epsilon);
+      }
     }
     fluid_entity->update(CoolProp::PT_INPUTS, Pressure, Temperature);
     if (abs(fluid_entity->rhomass() / Density - 1) < epsilon) {
@@ -80,7 +84,12 @@ void CCoolProp::SetTDState_rhoe(su2double rho, su2double e) {
 
 void CCoolProp::SetTDState_PT(su2double P, su2double T) {
   if (abs(P / Pressure_Critical - 1) < epsilon) {
-    P = Pressure_Critical * (1-epsilon);
+    if (P >= Pressure_Critical){
+      P = Pressure_Critical * (1 + epsilon);
+    }
+    else {
+      P = Pressure_Critical * (1 - epsilon);
+    }
   }
   fluid_entity->update(CoolProp::PT_INPUTS, P, T);
   su2double rho = fluid_entity->rhomass();
@@ -90,7 +99,12 @@ void CCoolProp::SetTDState_PT(su2double P, su2double T) {
 
 void CCoolProp::SetTDState_Prho(su2double P, su2double rho) {
   if (abs(P / Pressure_Critical - 1) < epsilon) {
-    P = Pressure_Critical * (1-epsilon);
+    if (P >= Pressure_Critical){
+      P = Pressure_Critical * (1 + epsilon);
+    }
+    else {
+      P = Pressure_Critical * (1 - epsilon);
+    }
   }
   fluid_entity->update(CoolProp::DmassP_INPUTS, rho, P);
   su2double e = fluid_entity->umass();
@@ -99,7 +113,12 @@ void CCoolProp::SetTDState_Prho(su2double P, su2double rho) {
 
 void CCoolProp::SetEnergy_Prho(su2double P, su2double rho) {
   if (abs(P / Pressure_Critical - 1) < epsilon) {
-    P = Pressure_Critical * (1-epsilon);
+    if (P >= Pressure_Critical){
+      P = Pressure_Critical * (1 + epsilon);
+    }
+    else {
+      P = Pressure_Critical * (1 - epsilon);
+    }
   }
   fluid_entity->update(CoolProp::DmassP_INPUTS, rho, P);
   StaticEnergy = fluid_entity->umass();
@@ -114,7 +133,12 @@ void CCoolProp::SetTDState_hs(su2double h, su2double s) {
 
 void CCoolProp::SetTDState_Ps(su2double P, su2double s) {
   if (abs(P / Pressure_Critical - 1) < epsilon) {
-    P = Pressure_Critical * (1-epsilon);
+    if (P >= Pressure_Critical){
+      P = Pressure_Critical * (1 + epsilon);
+    }
+    else {
+      P = Pressure_Critical * (1 - epsilon);
+    }
   }
   fluid_entity->update(CoolProp::PSmass_INPUTS, P, s);
   su2double rho = fluid_entity->rhomass();

From a6ae8f0098413c4624669e09b08d0c6f8652e2e8 Mon Sep 17 00:00:00 2001
From: PENGYAN777 <peng.yan@mail.polimi.it>
Date: Tue, 7 Mar 2023 08:44:37 +0100
Subject: [PATCH 254/656] check pressure

---
 SU2_CFD/include/fluid/CCoolProp.hpp | 29 +++++++++++-----
 SU2_CFD/src/fluid/CCoolProp.cpp     | 51 ++++-------------------------
 2 files changed, 27 insertions(+), 53 deletions(-)

diff --git a/SU2_CFD/include/fluid/CCoolProp.hpp b/SU2_CFD/include/fluid/CCoolProp.hpp
index 0959271508d..92884294870 100644
--- a/SU2_CFD/include/fluid/CCoolProp.hpp
+++ b/SU2_CFD/include/fluid/CCoolProp.hpp
@@ -30,12 +30,11 @@
 #if defined(HAVE_COOLPROP) && !defined(CODI_FORWARD_TYPE) && !defined(CODI_REVERSE_TYPE)
 #define USE_COOLPROP
 namespace CoolProp {
-  class AbstractState;
+class AbstractState;
 }
 #endif
 #include <memory>
 
-
 /*!
  * \class CCoolProp
  * \brief Child class for defining fluid model from CoolProp library.
@@ -43,15 +42,28 @@ namespace CoolProp {
  */
 class CCoolProp final : public CFluidModel {
  private:
-  su2double Gamma{1.4};           /*!< \brief Ratio of Specific Heats. */
-  su2double Gas_Constant{297};    /*!< \brief specific Gas Constant. */
-  su2double Pressure_Critical{0.0};   /*!< \brief critical pressure */
-  su2double Temperature_Critical{0.0};    /*!< \brief critical temperature */
+  su2double Gamma{1.4};                /*!< \brief Ratio of Specific Heats. */
+  su2double Gas_Constant{297};         /*!< \brief specific Gas Constant. */
+  su2double Pressure_Critical{0.0};    /*!< \brief critical pressure */
+  su2double Temperature_Critical{0.0}; /*!< \brief critical temperature */
   su2double acentric_factor{0.0};      /*!< \brief acentric factor */
 #ifdef USE_COOLPROP
-  std::unique_ptr<CoolProp::AbstractState> fluid_entity;   /*!< \brief fluid entity */
-  su2double epsilon{0.01};  /*!< threshold for pressure */
+  std::unique_ptr<CoolProp::AbstractState> fluid_entity; /*!< \brief fluid entity */
+  su2double epsilon{0.01};                               /*!< threshold for pressure */
 #endif
+  /*!
+   * \brief Avoid critical pressure
+   * \return .
+   */
+  void Check_Pressure(su2double Pressure) {
+    if (abs(Pressure / Pressure_Critical - 1) < epsilon) {
+      if (Pressure >= Pressure_Critical) {
+        Pressure = Pressure_Critical * (1 + epsilon);
+      } else {
+        Pressure = Pressure_Critical * (1 - epsilon);
+      }
+    }
+  }
 
  public:
   /*!
@@ -146,5 +158,4 @@ class CCoolProp final : public CFluidModel {
    * \return Value of the constant: Gamma
    */
   su2double GetGamma(void) const { return Gamma; }
-
 };
diff --git a/SU2_CFD/src/fluid/CCoolProp.cpp b/SU2_CFD/src/fluid/CCoolProp.cpp
index e59d6fe3927..8205795f27d 100644
--- a/SU2_CFD/src/fluid/CCoolProp.cpp
+++ b/SU2_CFD/src/fluid/CCoolProp.cpp
@@ -58,39 +58,23 @@ void CCoolProp::SetTDState_rhoe(su2double rho, su2double e) {
   if (fluid_entity->phase() == CoolProp::iphase_twophase) {
     // assume it is pure gas
     fluid_entity->specify_phase(CoolProp::iphase_gas);
-    if (abs(Pressure / Pressure_Critical - 1) < epsilon) {
-      if (Pressure >= Pressure_Critical){
-        Pressure = Pressure_Critical * (1 + epsilon);
-      }
-      else {
-        Pressure = Pressure_Critical * (1 - epsilon);
-      }
-    }
+    Check_Pressure(Pressure);
     fluid_entity->update(CoolProp::PT_INPUTS, Pressure, Temperature);
     if (abs(fluid_entity->rhomass() / Density - 1) < epsilon) {
       // origial phase is near saturation gas, then just compute sound speed
       SoundSpeed2 = pow(fluid_entity->speed_sound(), 2);
-    }
-    else {
+    } else {
       // original phase is not near saturation gas, then specify the phase as gas phase
       fluid_entity->specify_phase(CoolProp::iphase_gas);
       SetTDState_PT(Pressure, Temperature);
     }
-  }
-  else {
+  } else {
     SoundSpeed2 = pow(fluid_entity->speed_sound(), 2);
   }
 }
 
 void CCoolProp::SetTDState_PT(su2double P, su2double T) {
-  if (abs(P / Pressure_Critical - 1) < epsilon) {
-    if (P >= Pressure_Critical){
-      P = Pressure_Critical * (1 + epsilon);
-    }
-    else {
-      P = Pressure_Critical * (1 - epsilon);
-    }
-  }
+  Check_Pressure(P);
   fluid_entity->update(CoolProp::PT_INPUTS, P, T);
   su2double rho = fluid_entity->rhomass();
   su2double e = fluid_entity->umass();
@@ -98,28 +82,14 @@ void CCoolProp::SetTDState_PT(su2double P, su2double T) {
 }
 
 void CCoolProp::SetTDState_Prho(su2double P, su2double rho) {
-  if (abs(P / Pressure_Critical - 1) < epsilon) {
-    if (P >= Pressure_Critical){
-      P = Pressure_Critical * (1 + epsilon);
-    }
-    else {
-      P = Pressure_Critical * (1 - epsilon);
-    }
-  }
+  Check_Pressure(P);
   fluid_entity->update(CoolProp::DmassP_INPUTS, rho, P);
   su2double e = fluid_entity->umass();
   SetTDState_rhoe(rho, e);
 }
 
 void CCoolProp::SetEnergy_Prho(su2double P, su2double rho) {
-  if (abs(P / Pressure_Critical - 1) < epsilon) {
-    if (P >= Pressure_Critical){
-      P = Pressure_Critical * (1 + epsilon);
-    }
-    else {
-      P = Pressure_Critical * (1 - epsilon);
-    }
-  }
+  Check_Pressure(P);
   fluid_entity->update(CoolProp::DmassP_INPUTS, rho, P);
   StaticEnergy = fluid_entity->umass();
 }
@@ -132,14 +102,7 @@ void CCoolProp::SetTDState_hs(su2double h, su2double s) {
 }
 
 void CCoolProp::SetTDState_Ps(su2double P, su2double s) {
-  if (abs(P / Pressure_Critical - 1) < epsilon) {
-    if (P >= Pressure_Critical){
-      P = Pressure_Critical * (1 + epsilon);
-    }
-    else {
-      P = Pressure_Critical * (1 - epsilon);
-    }
-  }
+  Check_Pressure(P);
   fluid_entity->update(CoolProp::PSmass_INPUTS, P, s);
   su2double rho = fluid_entity->rhomass();
   su2double e = fluid_entity->umass();

From 1c478128fda117ce467bfbfeae88ed7d7d3b5485 Mon Sep 17 00:00:00 2001
From: PENGYAN777 <peng.yan@mail.polimi.it>
Date: Tue, 7 Mar 2023 08:59:01 +0100
Subject: [PATCH 255/656] pressure threshold dp

---
 SU2_CFD/include/fluid/CCoolProp.hpp | 11 ++++++-----
 SU2_CFD/src/fluid/CCoolProp.cpp     |  2 +-
 2 files changed, 7 insertions(+), 6 deletions(-)

diff --git a/SU2_CFD/include/fluid/CCoolProp.hpp b/SU2_CFD/include/fluid/CCoolProp.hpp
index 92884294870..4ae7ba5a6ef 100644
--- a/SU2_CFD/include/fluid/CCoolProp.hpp
+++ b/SU2_CFD/include/fluid/CCoolProp.hpp
@@ -47,20 +47,21 @@ class CCoolProp final : public CFluidModel {
   su2double Pressure_Critical{0.0};    /*!< \brief critical pressure */
   su2double Temperature_Critical{0.0}; /*!< \brief critical temperature */
   su2double acentric_factor{0.0};      /*!< \brief acentric factor */
+  su2double dp{0.01};             /*!< threshold for pressure */
 #ifdef USE_COOLPROP
   std::unique_ptr<CoolProp::AbstractState> fluid_entity; /*!< \brief fluid entity */
-  su2double epsilon{0.01};                               /*!< threshold for pressure */
 #endif
   /*!
    * \brief Avoid critical pressure
    * \return .
    */
   void Check_Pressure(su2double Pressure) {
-    if (abs(Pressure / Pressure_Critical - 1) < epsilon) {
+    if (abs(Pressure / Pressure_Critical - 1) < dp) {
       if (Pressure >= Pressure_Critical) {
-        Pressure = Pressure_Critical * (1 + epsilon);
-      } else {
-        Pressure = Pressure_Critical * (1 - epsilon);
+        Pressure = Pressure_Critical * (1 + dp);
+      }
+      else {
+        Pressure = Pressure_Critical * (1 - dp);
       }
     }
   }
diff --git a/SU2_CFD/src/fluid/CCoolProp.cpp b/SU2_CFD/src/fluid/CCoolProp.cpp
index 8205795f27d..8b47339eeba 100644
--- a/SU2_CFD/src/fluid/CCoolProp.cpp
+++ b/SU2_CFD/src/fluid/CCoolProp.cpp
@@ -60,7 +60,7 @@ void CCoolProp::SetTDState_rhoe(su2double rho, su2double e) {
     fluid_entity->specify_phase(CoolProp::iphase_gas);
     Check_Pressure(Pressure);
     fluid_entity->update(CoolProp::PT_INPUTS, Pressure, Temperature);
-    if (abs(fluid_entity->rhomass() / Density - 1) < epsilon) {
+    if (abs(fluid_entity->rhomass() / Density - 1) < dp) {
       // origial phase is near saturation gas, then just compute sound speed
       SoundSpeed2 = pow(fluid_entity->speed_sound(), 2);
     } else {

From 524206717557a5072e6e7e45ac9130aae9531e05 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 7 Mar 2023 14:13:46 +0100
Subject: [PATCH 256/656] Added elu activation function to CNeuralNetwork class
 as it was missing

---
 .../include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp   | 1 +
 .../toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp       | 1 -
 .../src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp   | 1 -
 3 files changed, 1 insertion(+), 2 deletions(-)

diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
index a28c60e129d..9961a2a7d7c 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
@@ -93,6 +93,7 @@ class CNeuralNetwork {
   std::map<std::string, ENUM_ACTIVATION_FUNCTION> activation_function_map{
       {"none", ENUM_ACTIVATION_FUNCTION::NONE},
       {"linear", ENUM_ACTIVATION_FUNCTION::LINEAR},
+      {"elu", ENUM_ACTIVATION_FUNCTION::ELU},
       {"relu", ENUM_ACTIVATION_FUNCTION::RELU},
       {"gelu", ENUM_ACTIVATION_FUNCTION::GELU},
       {"selu", ENUM_ACTIVATION_FUNCTION::SELU},
diff --git a/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
index 6cca01fb9dd..af5657f0f78 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
@@ -33,7 +33,6 @@
 #include <vector>
 
 #include "../../CConfig.hpp"
-#include "../../containers/CFileReaderLUT.hpp"
 namespace MLPToolbox {
 
 class CReadNeuralNetwork {
diff --git a/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
index a03cf36b4bd..ced1a17a518 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
@@ -27,7 +27,6 @@
  */
 #include "../../../include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp"
 
-#include "../../../include/containers/CFileReaderLUT.hpp"
 using namespace std;
 
 MLPToolbox::CReadNeuralNetwork::CReadNeuralNetwork(string filename_in) { filename = filename_in; }

From 18cd9e8d285e6bca1e4f53d7b1931cc10c2f182e Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 7 Mar 2023 15:20:22 +0100
Subject: [PATCH 257/656] Implemented feedback from Pedro and code-scanner

---
 .../multilayer_perceptron/CNeuralNetwork.cpp      |  1 -
 SU2_CFD/src/solvers/CEulerSolver.cpp              | 15 +++++++++------
 2 files changed, 9 insertions(+), 7 deletions(-)

diff --git a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
index 15c68c3f161..a45c2d749fa 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
@@ -31,7 +31,6 @@
 #include <iostream>
 #include <map>
 
-//#include "../../../include/option_structure.hpp"
 #include "../../../include/toolboxes/multilayer_perceptron/CLayer.hpp"
 #include "../../../include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp"
 
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index e41fdbd8f50..7dbba2bdf5e 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -4682,10 +4682,12 @@ void CEulerSolver::BC_Riemann(CGeometry *geometry, CSolver **solver_container,
       GetFluidModel()->SetTDState_rhoe(Density_i, StaticEnergy_i);
 
       /*--- Set initial values for density and energy for Newton solvers in fluid model ---*/
-      su2double relax_Newton = config->GetRelaxation_DataDriven();
-      GetFluidModel()->SetInitialDensity(relax_Newton*Density_i + (1 - relax_Newton)*config->GetDensity_Init_DataDriven());
-      GetFluidModel()->SetInitialEnergy(relax_Newton*StaticEnergy_i + (1 - relax_Newton)*config->GetEnergy_Init_DataDriven());
-
+      if(config->GetKind_FluidModel() == DATADRIVEN_FLUID){
+        su2double relax_Newton = config->GetRelaxation_DataDriven();
+        GetFluidModel()->SetInitialDensity(relax_Newton*Density_i + (1 - relax_Newton)*config->GetDensity_Init_DataDriven());
+        GetFluidModel()->SetInitialEnergy(relax_Newton*StaticEnergy_i + (1 - relax_Newton)*config->GetEnergy_Init_DataDriven());
+      }
+      
       Pressure_i = GetFluidModel()->GetPressure();
       Enthalpy_i = Energy_i + Pressure_i/Density_i;
 
@@ -4902,8 +4904,9 @@ void CEulerSolver::BC_Riemann(CGeometry *geometry, CSolver **solver_container,
       StaticEnergy_b = Energy_b - 0.5*Velocity2_b;
       GetFluidModel()->SetTDState_rhoe(Density_b, StaticEnergy_b);
 
+      /*--- Store number of Newton iterations at BC ---*/
       if(config->GetKind_FluidModel() == DATADRIVEN_FLUID)
-        GetNodes()->SetNewtonSolverIterations(iPoint, GetFluidModel()->GetnIter_Newton());
+        nodes->SetNewtonSolverIterations(iPoint, GetFluidModel()->GetnIter_Newton());
 
       Pressure_b = GetFluidModel()->GetPressure();
       Temperature_b = GetFluidModel()->GetTemperature();
@@ -6503,7 +6506,7 @@ void CEulerSolver::BC_Giles(CGeometry *geometry, CSolver **solver_container, CNu
       }
       /*--- Store number of Newton iterations at BC ---*/
       if(config->GetKind_FluidModel() == DATADRIVEN_FLUID)
-        GetNodes()->SetNewtonSolverIterations(iPoint, GetFluidModel()->GetnIter_Newton());
+        nodes->SetNewtonSolverIterations(iPoint, GetFluidModel()->GetnIter_Newton());
 
     }
     END_SU2_OMP_FOR

From d7f3a43d4b9df354db7c9945397241b371e5dcb8 Mon Sep 17 00:00:00 2001
From: PENGYAN777 <peng.yan@mail.polimi.it>
Date: Wed, 8 Mar 2023 09:33:05 +0100
Subject: [PATCH 258/656] code review

---
 SU2_CFD/include/fluid/CCoolProp.hpp | 18 +++++++-----------
 SU2_CFD/src/fluid/CCoolProp.cpp     | 10 +++++-----
 2 files changed, 12 insertions(+), 16 deletions(-)

diff --git a/SU2_CFD/include/fluid/CCoolProp.hpp b/SU2_CFD/include/fluid/CCoolProp.hpp
index 4ae7ba5a6ef..9d241a4b000 100644
--- a/SU2_CFD/include/fluid/CCoolProp.hpp
+++ b/SU2_CFD/include/fluid/CCoolProp.hpp
@@ -47,23 +47,19 @@ class CCoolProp final : public CFluidModel {
   su2double Pressure_Critical{0.0};    /*!< \brief critical pressure */
   su2double Temperature_Critical{0.0}; /*!< \brief critical temperature */
   su2double acentric_factor{0.0};      /*!< \brief acentric factor */
-  su2double dp{0.01};             /*!< threshold for pressure */
+  const su2double dp{0.01};            /*!< threshold for pressure */
 #ifdef USE_COOLPROP
   std::unique_ptr<CoolProp::AbstractState> fluid_entity; /*!< \brief fluid entity */
 #endif
   /*!
    * \brief Avoid critical pressure
-   * \return .
+   * \param[in,out] Pressure: Modified so that it is not too close to critical pressure to avoid issues in CoolProp.
    */
-  void Check_Pressure(su2double Pressure) {
-    if (abs(Pressure / Pressure_Critical - 1) < dp) {
-      if (Pressure >= Pressure_Critical) {
-        Pressure = Pressure_Critical * (1 + dp);
-      }
-      else {
-        Pressure = Pressure_Critical * (1 - dp);
-      }
-    }
+  void CheckPressure(su2double& Pressure) const {
+    if (Pressure > Pressure_Critical)
+      Pressure = fmax(Pressure, (1 + dp) * Pressure_Critical);
+    else
+      Pressure = fmin(Pressure, (1 - dp) * Pressure_Critical);
   }
 
  public:
diff --git a/SU2_CFD/src/fluid/CCoolProp.cpp b/SU2_CFD/src/fluid/CCoolProp.cpp
index 8b47339eeba..4a3b443252b 100644
--- a/SU2_CFD/src/fluid/CCoolProp.cpp
+++ b/SU2_CFD/src/fluid/CCoolProp.cpp
@@ -58,7 +58,7 @@ void CCoolProp::SetTDState_rhoe(su2double rho, su2double e) {
   if (fluid_entity->phase() == CoolProp::iphase_twophase) {
     // assume it is pure gas
     fluid_entity->specify_phase(CoolProp::iphase_gas);
-    Check_Pressure(Pressure);
+    CheckPressure(Pressure);
     fluid_entity->update(CoolProp::PT_INPUTS, Pressure, Temperature);
     if (abs(fluid_entity->rhomass() / Density - 1) < dp) {
       // origial phase is near saturation gas, then just compute sound speed
@@ -74,7 +74,7 @@ void CCoolProp::SetTDState_rhoe(su2double rho, su2double e) {
 }
 
 void CCoolProp::SetTDState_PT(su2double P, su2double T) {
-  Check_Pressure(P);
+  CheckPressure(P);
   fluid_entity->update(CoolProp::PT_INPUTS, P, T);
   su2double rho = fluid_entity->rhomass();
   su2double e = fluid_entity->umass();
@@ -82,14 +82,14 @@ void CCoolProp::SetTDState_PT(su2double P, su2double T) {
 }
 
 void CCoolProp::SetTDState_Prho(su2double P, su2double rho) {
-  Check_Pressure(P);
+  CheckPressure(P);
   fluid_entity->update(CoolProp::DmassP_INPUTS, rho, P);
   su2double e = fluid_entity->umass();
   SetTDState_rhoe(rho, e);
 }
 
 void CCoolProp::SetEnergy_Prho(su2double P, su2double rho) {
-  Check_Pressure(P);
+  CheckPressure(P);
   fluid_entity->update(CoolProp::DmassP_INPUTS, rho, P);
   StaticEnergy = fluid_entity->umass();
 }
@@ -102,7 +102,7 @@ void CCoolProp::SetTDState_hs(su2double h, su2double s) {
 }
 
 void CCoolProp::SetTDState_Ps(su2double P, su2double s) {
-  Check_Pressure(P);
+  CheckPressure(P);
   fluid_entity->update(CoolProp::PSmass_INPUTS, P, s);
   su2double rho = fluid_entity->rhomass();
   su2double e = fluid_entity->umass();

From c6d1101aa87a87c537e204f68907ec70e546af03 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Thu, 9 Mar 2023 15:53:59 +0100
Subject: [PATCH 259/656] MeDiPack update.

---
 externals/medi        | 2 +-
 meson_scripts/init.py | 2 +-
 2 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/externals/medi b/externals/medi
index 6aef76912e7..aafc2d1966b 160000
--- a/externals/medi
+++ b/externals/medi
@@ -1 +1 @@
-Subproject commit 6aef76912e7099c4f08c9705848797ca9e8070da
+Subproject commit aafc2d1966ba1233640af737e71c77c1a86183fd
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 5f4afec2522..0ee68b6f1df 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -46,7 +46,7 @@ def init_submodules(method = 'auto'):
   # The sha tag must be maintained manually to point to the correct commit
   sha_version_codi = '76a63ec8805eee146b1a5f6629676d3e78383f9e'
   github_repo_codi = 'https://github.com/scicompkl/CoDiPack'
-  sha_version_medi = '6aef76912e7099c4f08c9705848797ca9e8070da'
+  sha_version_medi = 'aafc2d1966ba1233640af737e71c77c1a86183fd'
   github_repo_medi = 'https://github.com/SciCompKL/MeDiPack'
   sha_version_opdi = 'f33b507c24f7448d4cf4df16ab5c53ea254b8774'
   github_repo_opdi = 'https://github.com/SciCompKL/OpDiLib'

From d886e441d9a549d8789629411261bec23dd75e2d Mon Sep 17 00:00:00 2001
From: Cristopher Morales
 <98025159+Cristopher-Morales@users.noreply.github.com>
Date: Thu, 9 Mar 2023 20:56:10 +0100
Subject: [PATCH 260/656] Adding thermal conductivity, heat capacity and
 diffusivity as outputs. (#1956)

* adding Cp as a volumeoutput

* fixing laminar diffusivities

* fixing segmentation fault

* small fixings

* format fixings

* reformulating thermal conductivity

* adding thermal conductivity as output

* adding source term energy equation

* fixing source term energy equation

* fixing source term

* format fix

* changing name to effective conductivity

* spelling fix

* small fix

* cleaning up

* reducing number of variables for computing diffusivity

* fixing test case

* updating residuals

* updating multizone restart

* updating reggresion test

* pointing to develop

* Update SU2_CFD/src/output/CFlowIncOutput.cpp

Co-authored-by: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>

* addressing comments

* Apply suggestions from code review

---------

Co-authored-by: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
---
 Common/src/CConfig.cpp                             |  4 ++--
 SU2_CFD/include/fluid/CConstantDiffusivity.hpp     |  3 +--
 .../include/fluid/CConstantLewisDiffusivity.hpp    |  3 +--
 SU2_CFD/include/fluid/CConstantSchmidt.hpp         |  3 +--
 SU2_CFD/include/fluid/CDiffusivityModel.hpp        |  3 +--
 SU2_CFD/include/fluid/CFluidModel.hpp              |  2 +-
 SU2_CFD/include/fluid/CFluidScalar.hpp             | 10 ++++++++--
 SU2_CFD/include/variables/CScalarVariable.hpp      |  8 ++++++++
 SU2_CFD/include/variables/CSpeciesVariable.hpp     |  2 +-
 SU2_CFD/include/variables/CVariable.hpp            |  7 +++++++
 SU2_CFD/src/fluid/CFluidScalar.cpp                 | 13 +++++++++----
 SU2_CFD/src/output/CFlowIncOutput.cpp              |  4 ++++
 SU2_CFD/src/output/CFlowOutput.cpp                 |  8 ++++++--
 SU2_CFD/src/solvers/CSpeciesSolver.cpp             | 11 +++++++----
 SU2_CFD/src/variables/CSpeciesVariable.cpp         |  2 +-
 TestCases/parallel_regression.py                   | 14 +++++++-------
 ...mitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg |  2 +-
 TestCases/tutorials.py                             |  2 +-
 18 files changed, 67 insertions(+), 34 deletions(-)

diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 8b36a1f2415..fc312f9b1de 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -5377,10 +5377,10 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
     /*--- Check whether the number of entries of the constant Lewis number equals the number of transported scalar
        equations solved. nConstant_Lewis_Number is used because it is required for the diffusivity fluid mixing
        models--- */
-    if (Kind_Diffusivity_Model == DIFFUSIVITYMODEL::CONSTANT_LEWIS && nConstant_Lewis_Number != nSpecies_Init)
+    if (Kind_Diffusivity_Model == DIFFUSIVITYMODEL::CONSTANT_LEWIS && nConstant_Lewis_Number != nSpecies_Init + 1)
       SU2_MPI::Error(
           "The use of CONSTANT_LEWIS requires the number of entries for CONSTANT_LEWIS_NUMBER ,\n"
-          "to be equal to the number of entries of SPECIES_INIT",
+          "to be equal to the number of entries of SPECIES_INIT +1",
           CURRENT_FUNCTION);
 
     // Helper function that checks scalar variable bounds,
diff --git a/SU2_CFD/include/fluid/CConstantDiffusivity.hpp b/SU2_CFD/include/fluid/CConstantDiffusivity.hpp
index 5dd4ebeb25a..c4571084c97 100644
--- a/SU2_CFD/include/fluid/CConstantDiffusivity.hpp
+++ b/SU2_CFD/include/fluid/CConstantDiffusivity.hpp
@@ -44,6 +44,5 @@ class CConstantDiffusivity final : public CDiffusivityModel {
   /*!
    * \brief Set diffusivity.
    */
-  void SetDiffusivity(su2double T, su2double rho, su2double mu_lam, su2double mu_turb, su2double cp,
-                      su2double kt) override {}
+  void SetDiffusivity(su2double rho, su2double mu_lam, su2double cp, su2double kt) override {}
 };
diff --git a/SU2_CFD/include/fluid/CConstantLewisDiffusivity.hpp b/SU2_CFD/include/fluid/CConstantLewisDiffusivity.hpp
index 0f49225fdec..bf7f60598b5 100644
--- a/SU2_CFD/include/fluid/CConstantLewisDiffusivity.hpp
+++ b/SU2_CFD/include/fluid/CConstantLewisDiffusivity.hpp
@@ -44,8 +44,7 @@ class CConstantLewisDiffusivity final : public CDiffusivityModel {
   /*!
    * \brief Set diffusivity.
    */
-  void SetDiffusivity(su2double T, su2double rho, su2double mu_lam, su2double mu_turb, su2double cp,
-                      su2double kt) override {
+  void SetDiffusivity(su2double rho, su2double mu_lam, su2double cp, su2double kt) override {
     diff_ = kt / (Lewis_ * rho * cp);
   }
 
diff --git a/SU2_CFD/include/fluid/CConstantSchmidt.hpp b/SU2_CFD/include/fluid/CConstantSchmidt.hpp
index 966754870e6..e76a49cbcf8 100644
--- a/SU2_CFD/include/fluid/CConstantSchmidt.hpp
+++ b/SU2_CFD/include/fluid/CConstantSchmidt.hpp
@@ -45,8 +45,7 @@ class CConstantSchmidt final : public CDiffusivityModel {
   /*!
    * \brief Set diffusivity.
    */
-  void SetDiffusivity(su2double T, su2double rho, su2double mu_lam, su2double mu_turb, su2double cp,
-                      su2double kt) override {
+  void SetDiffusivity(su2double rho, su2double mu_lam, su2double cp, su2double kt) override {
     diff_ = mu_lam / (rho * sc_lam_);
   }
 
diff --git a/SU2_CFD/include/fluid/CDiffusivityModel.hpp b/SU2_CFD/include/fluid/CDiffusivityModel.hpp
index 413c970a1e2..0fee7956fd8 100644
--- a/SU2_CFD/include/fluid/CDiffusivityModel.hpp
+++ b/SU2_CFD/include/fluid/CDiffusivityModel.hpp
@@ -46,8 +46,7 @@ class CDiffusivityModel {
   /*!
    * \brief Set mass diffusivity
    */
-  virtual void SetDiffusivity(su2double T, su2double rho, su2double mu_lam, su2double mu_turb, su2double cp,
-                              su2double kt) = 0;
+  virtual void SetDiffusivity(su2double rho, su2double mu_lam, su2double cp, su2double kt) = 0;
 
  protected:
   su2double diff_{0.0}; /*!< \brief mass diffusivity. */
diff --git a/SU2_CFD/include/fluid/CFluidModel.hpp b/SU2_CFD/include/fluid/CFluidModel.hpp
index ba52958f3a9..bd8b8b4952e 100644
--- a/SU2_CFD/include/fluid/CFluidModel.hpp
+++ b/SU2_CFD/include/fluid/CFluidModel.hpp
@@ -163,7 +163,7 @@ class CFluidModel {
    * \brief Get fluid mass diffusivity.
    */
   inline virtual su2double GetMassDiffusivity(int iVar) {
-    MassDiffusivity->SetDiffusivity(Temperature, Density, Mu, Mu_Turb, Cp, Kt);
+    MassDiffusivity->SetDiffusivity(Density, Mu, Cp, Kt);
     mass_diffusivity = MassDiffusivity->GetDiffusivity();
     return mass_diffusivity;
   }
diff --git a/SU2_CFD/include/fluid/CFluidScalar.hpp b/SU2_CFD/include/fluid/CFluidScalar.hpp
index 37456084f44..f6fc2572db7 100644
--- a/SU2_CFD/include/fluid/CFluidScalar.hpp
+++ b/SU2_CFD/include/fluid/CFluidScalar.hpp
@@ -44,6 +44,7 @@ class CFluidScalar final : public CFluidModel {
   const su2double Gamma;                  /*!< \brief Ratio of specific heats of the gas. */
   const su2double Pressure_Thermodynamic; /*!< \brief Constant pressure thermodynamic. */
   const su2double GasConstant_Ref;        /*!< \brief Gas constant reference needed for Nondimensional problems. */
+  const su2double Prandtl_Number;         /*!< \brief Prandlt number.*/
 
   const bool wilke;
   const bool davidson;
@@ -96,6 +97,11 @@ class CFluidScalar final : public CFluidModel {
    */
   su2double ComputeGasConstant();
 
+  /*!
+   * \brief Compute mass diffusivity for species.
+   */
+  void ComputeMassDiffusivity();
+
  public:
   /*!
    * \brief Constructor of the class.
@@ -125,12 +131,12 @@ class CFluidScalar final : public CFluidModel {
   /*!
    * \brief Get fluid thermal conductivity.
    */
-  inline su2double GetThermalConductivity() override { return Kt; }
+  inline su2double GetThermalConductivity() override { return Kt + Mu_Turb * Cp / Prandtl_Number; }
 
   /*!
    * \brief Get fluid mass diffusivity.
    */
-  inline su2double GetMassDiffusivity(int ivar) override;
+  inline su2double GetMassDiffusivity(int ivar) override { return massDiffusivity[ivar]; }
 
   /*!
    * \brief Set the Dimensionless State using Temperature.
diff --git a/SU2_CFD/include/variables/CScalarVariable.hpp b/SU2_CFD/include/variables/CScalarVariable.hpp
index f68041d74a1..742596aedda 100644
--- a/SU2_CFD/include/variables/CScalarVariable.hpp
+++ b/SU2_CFD/include/variables/CScalarVariable.hpp
@@ -87,4 +87,12 @@ class CScalarVariable : public CVariable {
   inline su2double GetHarmonicBalance_Source(unsigned long iPoint, unsigned long iVar) const final {
     return HB_Source(iPoint, iVar);
   }
+
+  /*!
+   * \brief Get the value of the mass diffusivity
+   * \param[in] iPoint - Point index.
+   * \param[in] val_ivar - eqn. index to the mass diffusivity.
+   * \return Value of the mass diffusivity
+   */
+  inline virtual su2double GetDiffusivity(unsigned long iPoint, unsigned short val_ivar) const { return 0.0; }
 };
diff --git a/SU2_CFD/include/variables/CSpeciesVariable.hpp b/SU2_CFD/include/variables/CSpeciesVariable.hpp
index ac9b6fa4488..d668e006db2 100644
--- a/SU2_CFD/include/variables/CSpeciesVariable.hpp
+++ b/SU2_CFD/include/variables/CSpeciesVariable.hpp
@@ -65,7 +65,7 @@ class CSpeciesVariable : public CScalarVariable {
    * \param[in] val_ivar - eqn. index to the mass diffusivity.
    * \return Value of the mass diffusivity
    */
-  inline su2double GetDiffusivity(unsigned long iPoint, unsigned short val_ivar) {
+  inline su2double GetDiffusivity(unsigned long iPoint, unsigned short val_ivar) const {
     return Diffusivity(iPoint, val_ivar);
   }
 
diff --git a/SU2_CFD/include/variables/CVariable.hpp b/SU2_CFD/include/variables/CVariable.hpp
index 13d04898bd6..da68a28f051 100644
--- a/SU2_CFD/include/variables/CVariable.hpp
+++ b/SU2_CFD/include/variables/CVariable.hpp
@@ -1114,6 +1114,13 @@ class CVariable {
    */
   inline virtual su2double GetThermalConductivity(unsigned long iPoint) const { return 0.0; }
 
+  /*!
+   * \brief A virtual member.
+   * \param[in] iPoint - Point index.
+   * \return Value of the mass diffusivity.
+   */
+  inline virtual su2double GetDiffusivity(unsigned long iPoint, unsigned short val_ivar) const { return 0.0; }
+
   /*!
    * \brief A virtual member.
    * \param[in] iPoint - Point index.
diff --git a/SU2_CFD/src/fluid/CFluidScalar.cpp b/SU2_CFD/src/fluid/CFluidScalar.cpp
index 1d0700cea35..429b2c2f580 100644
--- a/SU2_CFD/src/fluid/CFluidScalar.cpp
+++ b/SU2_CFD/src/fluid/CFluidScalar.cpp
@@ -50,6 +50,7 @@ CFluidScalar::CFluidScalar(su2double val_Cp, su2double val_gas_constant, su2doub
       Gamma(config->GetGamma()),
       Pressure_Thermodynamic(value_pressure_operating),
       GasConstant_Ref(config->GetGas_Constant_Ref()),
+      Prandtl_Number(config->GetPrandtl_Turb()),
       wilke(config->GetKind_MixingViscosityModel() == MIXINGVISCOSITYMODEL::WILKE),
       davidson(config->GetKind_MixingViscosityModel() == MIXINGVISCOSITYMODEL::DAVIDSON) {
   if (n_species_mixture > ARRAYSIZE) {
@@ -63,6 +64,7 @@ CFluidScalar::CFluidScalar(su2double val_Cp, su2double val_gas_constant, su2doub
 
   SetLaminarViscosityModel(config);
   SetThermalConductivityModel(config);
+  SetMassDiffusivityModel(config);
 }
 
 void CFluidScalar::SetLaminarViscosityModel(const CConfig* config) {
@@ -83,9 +85,11 @@ void CFluidScalar::SetMassDiffusivityModel(const CConfig* config) {
   }
 }
 
-su2double CFluidScalar::GetMassDiffusivity(int iVar) {
-  MassDiffusivityPointers[iVar]->SetDiffusivity(Temperature, Density, Mu, Mu_Turb, Cp, Kt);
-  return MassDiffusivityPointers[iVar]->GetDiffusivity();
+void CFluidScalar::ComputeMassDiffusivity() {
+  for (int iVar = 0; iVar < n_species_mixture; iVar++) {
+    MassDiffusivityPointers[iVar]->SetDiffusivity(Density, Mu, Cp, Kt);
+    massDiffusivity[iVar] = MassDiffusivityPointers[iVar]->GetDiffusivity();
+  }
 }
 
 void CFluidScalar::MassToMoleFractions(const su2double* val_scalars) {
@@ -168,7 +172,7 @@ su2double CFluidScalar::DavidsonViscosity(const su2double* val_scalars) {
 su2double CFluidScalar::WilkeConductivity(const su2double* val_scalars) {
 
   for (int iVar = 0; iVar < n_species_mixture; iVar++) {
-    ThermalConductivityPointers[iVar]->SetConductivity(Temperature, Density, Mu, Mu_Turb, Cp, 0.0, 0.0);
+    ThermalConductivityPointers[iVar]->SetConductivity(Temperature, Density, Mu, 0.0, 0.0, 0.0, 0.0);
     laminarThermalConductivity[iVar] = ThermalConductivityPointers[iVar]->GetConductivity();
   }
 
@@ -227,4 +231,5 @@ void CFluidScalar::SetTDState_T(const su2double val_temperature, const su2double
   }
 
   Kt = WilkeConductivity(val_scalars);
+  ComputeMassDiffusivity();
 }
diff --git a/SU2_CFD/src/output/CFlowIncOutput.cpp b/SU2_CFD/src/output/CFlowIncOutput.cpp
index ec2b2e108d2..29aeef9e015 100644
--- a/SU2_CFD/src/output/CFlowIncOutput.cpp
+++ b/SU2_CFD/src/output/CFlowIncOutput.cpp
@@ -318,6 +318,8 @@ void CFlowIncOutput::SetVolumeOutputFields(CConfig *config){
 
   if (config->GetKind_Solver() == MAIN_SOLVER::INC_RANS || config->GetKind_Solver() == MAIN_SOLVER::INC_NAVIER_STOKES){
     AddVolumeOutput("LAMINAR_VISCOSITY", "Laminar_Viscosity", "PRIMITIVE", "Laminar viscosity");
+    AddVolumeOutput("HEAT_CAPACITY", "Heat_Capacity", "PRIMITIVE", "Heat capacity");
+    AddVolumeOutput("THERMAL_CONDUCTIVITY", "Thermal_Conductivity", "PRIMITIVE", "Thermal conductivity");
 
     AddVolumeOutput("SKIN_FRICTION-X", "Skin_Friction_Coefficient_x", "PRIMITIVE", "x-component of the skin friction vector");
     AddVolumeOutput("SKIN_FRICTION-Y", "Skin_Friction_Coefficient_y", "PRIMITIVE", "y-component of the skin friction vector");
@@ -407,6 +409,8 @@ void CFlowIncOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolve
 
   if (config->GetKind_Solver() == MAIN_SOLVER::INC_RANS || config->GetKind_Solver() == MAIN_SOLVER::INC_NAVIER_STOKES){
     SetVolumeOutputValue("LAMINAR_VISCOSITY", iPoint, Node_Flow->GetLaminarViscosity(iPoint));
+    SetVolumeOutputValue("HEAT_CAPACITY", iPoint, Node_Flow->GetSpecificHeatCp(iPoint));
+    SetVolumeOutputValue("THERMAL_CONDUCTIVITY", iPoint, Node_Flow->GetThermalConductivity(iPoint));
   }
 
   SetVolumeOutputValue("RES_PRESSURE", iPoint, solver[FLOW_SOL]->LinSysRes(iPoint, 0));
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index ea62d779f52..ed0fb0f3a16 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -1159,8 +1159,9 @@ void CFlowOutput::SetVolumeOutputFields_ScalarSolution(const CConfig* config){
   }
 
   if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
-    for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++)
+    for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
       AddVolumeOutput("SPECIES_" + std::to_string(iVar), "Species_" + std::to_string(iVar), "SOLUTION", "Species_" + std::to_string(iVar) + " mass fraction");
+    }
   }
 }
 
@@ -1190,8 +1191,10 @@ void CFlowOutput::SetVolumeOutputFields_ScalarResidual(const CConfig* config) {
   }
 
   if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
-    for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++)
+    for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++){
       AddVolumeOutput("RES_SPECIES_" + std::to_string(iVar), "Residual_Species_" + std::to_string(iVar), "RESIDUAL", "Residual of the transported species " + std::to_string(iVar));
+      AddVolumeOutput("DIFFUSIVITY_" + std::to_string(iVar), "Diffusivity_" + std::to_string(iVar), "PRIMITIVE", "Diffusivity of the transported species " + std::to_string(iVar));
+    }
   }
 }
 
@@ -1324,6 +1327,7 @@ void CFlowOutput::LoadVolumeData_Scalar(const CConfig* config, const CSolver* co
     for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
       SetVolumeOutputValue("SPECIES_" + std::to_string(iVar), iPoint, Node_Species->GetSolution(iPoint, iVar));
       SetVolumeOutputValue("RES_SPECIES_" + std::to_string(iVar), iPoint, solver[SPECIES_SOL]->LinSysRes(iPoint, iVar));
+      SetVolumeOutputValue("DIFFUSIVITY_"+ std::to_string(iVar), iPoint, Node_Species->GetDiffusivity(iPoint,iVar));
       if (config->GetKind_SlopeLimit_Species() != LIMITER::NONE)
         SetVolumeOutputValue("LIMITER_SPECIES_" + std::to_string(iVar), iPoint, Node_Species->GetLimiter(iPoint, iVar));
     }
diff --git a/SU2_CFD/src/solvers/CSpeciesSolver.cpp b/SU2_CFD/src/solvers/CSpeciesSolver.cpp
index 16e069ed9bd..b401b162f8a 100644
--- a/SU2_CFD/src/solvers/CSpeciesSolver.cpp
+++ b/SU2_CFD/src/solvers/CSpeciesSolver.cpp
@@ -116,7 +116,7 @@ CSpeciesSolver::CSpeciesSolver(CGeometry* geometry, CConfig* config, unsigned sh
   /*--- Initialize the mass diffusivity. Nondimensionalization done in the flow solver. ---*/
   SU2_OMP_FOR_STAT(omp_chunk_size)
   for (unsigned long iPoint = 0; iPoint < nPoint; iPoint++) {
-    for (auto iVar = 0u; iVar < nVar; iVar++) {
+    for (auto iVar = 0u; iVar <= nVar; iVar++) {
       const auto MassDiffusivity = config->GetDiffusivity_ConstantND();
       nodes->SetDiffusivity(iPoint, MassDiffusivity, iVar);
     }
@@ -290,9 +290,12 @@ void CSpeciesSolver::Preprocessing(CGeometry* geometry, CSolver** solver_contain
   /*--- Set the laminar mass Diffusivity for the species solver. ---*/
   SU2_OMP_FOR_STAT(omp_chunk_size)
   for (auto iPoint = 0u; iPoint < nPoint; iPoint++) {
-    for (auto iVar = 0u; iVar < nVar; iVar++) {
-      solver_container[FLOW_SOL]->GetFluidModel()->SetMassDiffusivityModel(config);
-      su2double mass_diffusivity = solver_container[FLOW_SOL]->GetFluidModel()->GetMassDiffusivity(iVar);
+    const su2double temperature = solver_container[FLOW_SOL]->GetNodes()->GetTemperature(iPoint);
+    const su2double* scalar = solver_container[SPECIES_SOL]->GetNodes()->GetSolution(iPoint);
+    solver_container[FLOW_SOL]->GetFluidModel()->SetMassDiffusivityModel(config);
+    solver_container[FLOW_SOL]->GetFluidModel()->SetTDState_T(temperature, scalar);
+    for (auto iVar = 0u; iVar <= nVar; iVar++) {
+      const su2double mass_diffusivity = solver_container[FLOW_SOL]->GetFluidModel()->GetMassDiffusivity(iVar);
       nodes->SetDiffusivity(iPoint, mass_diffusivity, iVar);
     }
 
diff --git a/SU2_CFD/src/variables/CSpeciesVariable.cpp b/SU2_CFD/src/variables/CSpeciesVariable.cpp
index 67e07ca2c88..7f903533499 100644
--- a/SU2_CFD/src/variables/CSpeciesVariable.cpp
+++ b/SU2_CFD/src/variables/CSpeciesVariable.cpp
@@ -31,7 +31,7 @@ CSpeciesVariable::CSpeciesVariable(const su2double* species_inf, unsigned long n
                                    unsigned long nvar, const CConfig* config)
     : CScalarVariable(npoint, ndim, nvar, config) {
   /*--- Allocate space for the mass diffusivity. ---*/
-  Diffusivity.resize(nPoint, nVar) = su2double(0.0);
+  Diffusivity.resize(nPoint, nVar + 1) = su2double(0.0);
 
   for (unsigned long iPoint = 0; iPoint < nPoint; iPoint++)
     for (unsigned long iVar = 0; iVar < nVar; iVar++)
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index bf0bbbb62fb..b6a7ae16b32 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -1429,7 +1429,7 @@ def main():
     species2_primitiveVenturi_mixingmodel.cfg_dir   = "species_transport/venturi_primitive_3species"
     species2_primitiveVenturi_mixingmodel.cfg_file  = "species2_primitiveVenturi_mixingmodel.cfg"
     species2_primitiveVenturi_mixingmodel.test_iter = 50
-    species2_primitiveVenturi_mixingmodel.test_vals = [-5.477236, -4.589782, -4.582531, -5.690416, -0.068943, -5.631254, 5.000000, -1.668303, 5.000000, -4.866978, 5.000000, -1.168368, 0.000425, 0.000404, 0.000021, 0.000000]
+    species2_primitiveVenturi_mixingmodel.test_vals = [-5.447741, -4.578625, -4.560889, -5.671675, -0.069655, -5.630277, 5.000000, -1.714271, 5.000000, -4.878115, 5.000000, -1.254671, 0.000418, 0.000394, 0.000024, 0.000000]
     species2_primitiveVenturi_mixingmodel.new_output = True
     test_list.append(species2_primitiveVenturi_mixingmodel)
 
@@ -1438,7 +1438,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_boundedscalar.cfg_dir   = "species_transport/venturi_primitive_3species"
     species2_primitiveVenturi_mixingmodel_boundedscalar.cfg_file  = "species2_primitiveVenturi_mixingmodel_boundedscalar.cfg"
     species2_primitiveVenturi_mixingmodel_boundedscalar.test_iter = 50
-    species2_primitiveVenturi_mixingmodel_boundedscalar.test_vals = [-5.419823, -4.490921, -4.496340, -5.724950, -0.120331, -5.693224, 5.000000, -1.766882, 5.000000, -4.958487, 5.000000, -2.150247, 0.000300, 0.000300, 0.000000, 0.000000]
+    species2_primitiveVenturi_mixingmodel_boundedscalar.test_vals = [-5.398649, -4.476373, -4.477258, -5.733271, -0.122667, -5.687136, 5.000000, -1.797791, 5.000000, -4.942913, 5.000000, -2.082842, 0.000295, 0.000295, 0.000000, 0.000000]
     species2_primitiveVenturi_mixingmodel_boundedscalar.new_output = True
     test_list.append(species2_primitiveVenturi_mixingmodel_boundedscalar)
 
@@ -1447,7 +1447,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_viscosity.cfg_dir   = "species_transport/venturi_primitive_3species"
     species2_primitiveVenturi_mixingmodel_viscosity.cfg_file  = "species2_primitiveVenturi_mixingmodel_viscosity.cfg"
     species2_primitiveVenturi_mixingmodel_viscosity.test_iter = 50
-    species2_primitiveVenturi_mixingmodel_viscosity.test_vals = [-4.738778, -4.325766, -4.610914, -5.834431, 0.521730, -4.934375, 5.000000, -1.887191, 5.000000, -5.499917, 5.000000, -1.770845, 2.292904, 0.971941, 0.608500, 0.712464]
+    species2_primitiveVenturi_mixingmodel_viscosity.test_vals = [-4.725129, -4.311366, -4.610113, -5.833264, 0.552520, -4.945381, 5.000000, -1.834845, 5.000000, -5.496023, 5.000000, -1.733470, 2.277964, 0.972376, 0.608230, 0.697358]
     species2_primitiveVenturi_mixingmodel_viscosity.new_output = True
     test_list.append(species2_primitiveVenturi_mixingmodel_viscosity)
 
@@ -1456,7 +1456,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg_dir   = "species_transport/venturi_primitive_3species"
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg_file  = "species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg"
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.test_iter = 50
-    species2_primitiveVenturi_mixingmodel_heatcapacity_H2.test_vals = [-6.105905, -4.979417, -4.870704, -7.338344, 2.435662, -5.621107, 30.000000, -5.737172, 12.000000, -8.148164, 9.000000, -8.040415, 2.084589, 1.000000, 0.600000, 0.484589]
+    species2_primitiveVenturi_mixingmodel_heatcapacity_H2.test_vals = [-6.113626, -4.989076, -4.880565, -7.351737, 2.452701, -5.627391, 30.000000, -5.721303, 11.000000, -8.001991, 10.000000, -8.813670, 2.084143, 1.000000, 0.600000, 0.484143]
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.su2_exec  = "mpirun -n 2 SU2_CFD"
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.timeout   = 1600
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.new_output = True
@@ -1468,7 +1468,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg_dir   = "species_transport/venturi_primitive_3species"
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg_file  = "species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg"
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.test_iter = 50
-    species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.test_vals = [-5.711760, -5.284237, -5.175532, -8.342082, 2.130839, -5.226944, 30.000000, -5.737157, 12.000000, -8.148020, 9.000000, -8.040460, 2.084591, 1.000000, 0.600000, 0.484591]
+    species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.test_vals = [-5.719472, -5.293846, -5.185419, -8.355307, 2.147874, -5.233215, 30.000000, -5.721396, 11.000000, -8.000062, 10.000000, -8.814100, 2.084145, 1.000000, 0.600000, 0.484145]
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.su2_exec  = "mpirun -n 2 SU2_CFD"
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.timeout   = 1600
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.new_output = True
@@ -1498,7 +1498,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg_dir   = "species_transport/venturi_primitive_3species"
     species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg_file  = "species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg"
     species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.test_iter = 50
-    species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.test_vals = [-4.019621, -1.652733, -1.414138, -0.971744, 1.590456, -3.762843, 23.000000, -5.066221, 12.000000, -5.359931, 4.000000, -6.078888, 2.000000, 1.000000, 0.000000, 1.000000]
+    species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.test_vals = [-4.012157, -1.650191, -1.405134, -0.990205, 1.619918, -3.764227, 23.000000, -5.039466, 12.000000, -5.346201, 4.000000, -6.084514, 2.000000, 1.000000, 0.000000, 1.000000]
     species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.su2_exec  = "mpirun -n 2 SU2_CFD"
     species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.timeout   = 1600
     species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.new_output = True
@@ -1530,7 +1530,7 @@ def main():
     species3_multizone_restart.cfg_dir   = "species_transport/multizone"
     species3_multizone_restart.cfg_file  = "configMaster.cfg"
     species3_multizone_restart.test_iter = 5
-    species3_multizone_restart.test_vals = [-7.169637, -6.381576]
+    species3_multizone_restart.test_vals = [-6.571720, -6.086110]
     species3_multizone_restart.new_output = True
     species3_multizone_restart.multizone = True
     test_list.append(species3_multizone_restart)
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg
index 7bef8d8c329..662646b3134 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg
@@ -104,7 +104,7 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 KIND_SCALAR_MODEL= SPECIES_TRANSPORT
 %
 DIFFUSIVITY_MODEL = CONSTANT_LEWIS
-CONSTANT_LEWIS_NUMBER = 0.365
+CONSTANT_LEWIS_NUMBER = 0.365, 0.96
 %
 CONV_NUM_METHOD_SPECIES= BOUNDED_SCALAR
 MUSCL_SPECIES= NO
diff --git a/TestCases/tutorials.py b/TestCases/tutorials.py
index e256a94c71f..af0a0039b7b 100644
--- a/TestCases/tutorials.py
+++ b/TestCases/tutorials.py
@@ -110,7 +110,7 @@ def main():
     kenics_mixer_tutorial.cfg_dir   = "../Tutorials/incompressible_flow/Inc_Species_Transport_Composition_Dependent_Model"
     kenics_mixer_tutorial.cfg_file  = "kenics_mixer_tutorial.cfg"
     kenics_mixer_tutorial.test_iter = 10
-    kenics_mixer_tutorial.test_vals = [-7.489841, -6.823474, -6.838069, -5.157396, -7.902273, -3.174235, -7.448166, 5.000000, -1.862000, 4.000000, -5.173789, 3.000000, -6.373917, 0.025135, 0.000000, 0.025135, 0.000000, 64.095000, 8.479500, 48.089000, 7.526700]
+    kenics_mixer_tutorial.test_vals = [-7.489828, -6.823474, -6.838069, -5.157396, -7.902254, -3.174210, -7.447809, 5.000000, -1.862023, 4.000000, -5.173815, 3.000000, -6.381121, 0.025490, 0.000000, 0.025490, 0.000000, 64.111000, 8.479500, 48.105000, 7.526700]
     kenics_mixer_tutorial.command   = TestCase.Command("mpirun -n 2", "SU2_CFD")
     kenics_mixer_tutorial.new_output = True
     test_list.append(kenics_mixer_tutorial)

From 12e09d330b794d6fa3c766aadbe65ef76252aaef Mon Sep 17 00:00:00 2001
From: Cristopher Morales
 <98025159+Cristopher-Morales@users.noreply.github.com>
Date: Fri, 10 Mar 2023 12:14:06 +0100
Subject: [PATCH 261/656] BC inlet for SA solver based on local conditions at
 the Inlet (#1953)

* adding turbulent markers to SA solver

* clang-format

* fixing bc.option

* updating residuals

* Update SU2_CFD/src/solvers/CTurbSASolver.cpp

Co-authored-by: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>

* Update SU2_CFD/src/solvers/CTurbSASolver.cpp

Co-authored-by: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>

* adding SA feature to existing test case

* fixing test case

* adding option in .cfg file and others

---------

Co-authored-by: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
---
 Common/src/CConfig.cpp                        | 11 +++++++-
 SU2_CFD/src/solvers/CTurbSASolver.cpp         | 27 ++++++++++++++++++-
 TestCases/hybrid_regression.py                |  4 +--
 TestCases/parallel_regression.py              |  8 +++---
 TestCases/serial_regression.py                |  6 ++---
 ...primitiveVenturi_mixingmodel_viscosity.cfg | 21 +++++++++------
 config_template.cfg                           |  3 ++-
 7 files changed, 60 insertions(+), 20 deletions(-)

diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index fc312f9b1de..0821cd6075a 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -5336,6 +5336,11 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
         "The use of MARKER_INLET_TURBULENT requires the number of entries when SST Model is used \n"
         "to be equal to 2 : Turbulent intensity and ratio turbulent to laminar viscosity",
         CURRENT_FUNCTION);
+  if (Marker_Inlet_Turb != nullptr && Kind_Turb_Model == TURB_MODEL::SA && nTurb_Properties != 1)
+    SU2_MPI::Error(
+        "The use of MARKER_INLET_TURBULENT requires the number of entries when SA Model is used \n"
+        "to be equal to 1 : ratio turbulent to laminar viscosity",
+        CURRENT_FUNCTION);
 
   /*--- Checks for additional species transport. ---*/
   if (Kind_Species_Model == SPECIES_MODEL::SPECIES_TRANSPORT) {
@@ -8826,7 +8831,11 @@ const su2double* CConfig::GetInlet_TurbVal(string val_marker) const {
   for (auto iMarker = 0u; iMarker < nMarker_Inlet_Turb; iMarker++) {
     if (Marker_Inlet_Turb[iMarker] == val_marker) return Inlet_TurbVal[iMarker];
   }
-  return TurbIntensityAndViscRatioFreeStream;
+  if (Kind_Turb_Model == TURB_MODEL::SST) {
+    return TurbIntensityAndViscRatioFreeStream;
+  } else {
+    return &NuFactor_FreeStream;
+  }
 }
 
 su2double CConfig::GetOutlet_Pressure(string val_marker) const {
diff --git a/SU2_CFD/src/solvers/CTurbSASolver.cpp b/SU2_CFD/src/solvers/CTurbSASolver.cpp
index a342fa2b3a0..fb18d50b551 100644
--- a/SU2_CFD/src/solvers/CTurbSASolver.cpp
+++ b/SU2_CFD/src/solvers/CTurbSASolver.cpp
@@ -547,7 +547,32 @@ void CTurbSASolver::BC_Inlet(CGeometry *geometry, CSolver **solver_container, CN
       su2double Inlet_Vars[MAXNVAR];
       Inlet_Vars[0] = Inlet_TurbVars[val_marker][iVertex][0];
       if (config->GetInlet_Profile_From_File()) {
-        Inlet_Vars[0] *= config->GetDensity_Ref() / config->GetViscosity_Ref();
+         Inlet_Vars[0] *= config->GetDensity_Ref() / config->GetViscosity_Ref();
+      } else {
+         /*--- Obtain fluid model for computing the nu tilde to impose at the inlet boundary. ---*/
+         CFluidModel* FluidModel = solver_container[FLOW_SOL]->GetFluidModel();
+
+         /*--- Obtain density and laminar viscosity at inlet boundary node ---*/
+
+         su2double Density_Inlet;
+         if (config->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE) {
+           Density_Inlet = V_inlet[prim_idx.Density()];
+           FluidModel->SetTDState_Prho(V_inlet[prim_idx.Pressure()], Density_Inlet);
+         } else {
+           const su2double* Scalar_Inlet = nullptr;
+           if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
+            Scalar_Inlet = config->GetInlet_SpeciesVal(config->GetMarker_All_TagBound(val_marker));
+           }
+           FluidModel->SetTDState_T(V_inlet[prim_idx.Temperature()], Scalar_Inlet);
+           Density_Inlet = FluidModel->GetDensity();
+         }
+         const su2double Laminar_Viscosity_Inlet = FluidModel->GetLaminarViscosity();
+         const su2double* Turb_Properties = config->GetInlet_TurbVal(config->GetMarker_All_TagBound(val_marker));
+         const su2double Nu_Factor = Turb_Properties[0];
+         Inlet_Vars[0] = Nu_Factor * Laminar_Viscosity_Inlet / Density_Inlet;
+         if (config->GetSAParsedOptions().bc) {
+           Inlet_Vars[0] *= 0.005;
+         }
       }
 
       /*--- Load the inlet turbulence variable (uniform by default). ---*/
diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index 4e2094b56f6..e00948e9ff7 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -182,7 +182,7 @@ def main():
     turb_flatplate.cfg_dir   = "rans/flatplate"
     turb_flatplate.cfg_file  = "turb_SA_flatplate.cfg"
     turb_flatplate.test_iter = 20
-    turb_flatplate.test_vals = [-4.157169, -6.737133, -0.176253, 0.057446]
+    turb_flatplate.test_vals = [-4.157169, -6.736698, -0.176253, 0.057446]
     test_list.append(turb_flatplate)
 
     # ONERA M6 Wing
@@ -495,7 +495,7 @@ def main():
     ddes_flatplate.cfg_dir   = "ddes/flatplate"
     ddes_flatplate.cfg_file  = "ddes_flatplate.cfg"
     ddes_flatplate.test_iter = 10
-    ddes_flatplate.test_vals = [-2.714758, -5.883004, -0.215005, 0.023783, -618.160000]
+    ddes_flatplate.test_vals = [-2.714758, -5.882733, -0.215005, 0.023783, -618.160000]
     ddes_flatplate.unsteady  = True
     test_list.append(ddes_flatplate)
 
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index b6a7ae16b32..58907af6632 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -354,7 +354,7 @@ def main():
     turb_flatplate.cfg_dir   = "rans/flatplate"
     turb_flatplate.cfg_file  = "turb_SA_flatplate.cfg"
     turb_flatplate.test_iter = 20
-    turb_flatplate.test_vals = [-4.147548, -6.729213, -0.176227, 0.057731]
+    turb_flatplate.test_vals = [-4.147548, -6.728790, -0.176227, 0.057731]
     test_list.append(turb_flatplate)
 
     # Flat plate (compressible) with species inlet
@@ -953,7 +953,7 @@ def main():
     ddes_flatplate.cfg_dir   = "ddes/flatplate"
     ddes_flatplate.cfg_file  = "ddes_flatplate.cfg"
     ddes_flatplate.test_iter = 10
-    ddes_flatplate.test_vals = [-2.714758, -5.883004, -0.215005, 0.023783, -618.160000]
+    ddes_flatplate.test_vals = [-2.714758, -5.882733, -0.215005, 0.023783, -618.160000]
     ddes_flatplate.unsteady  = True
     test_list.append(ddes_flatplate)
 
@@ -1442,12 +1442,12 @@ def main():
     species2_primitiveVenturi_mixingmodel_boundedscalar.new_output = True
     test_list.append(species2_primitiveVenturi_mixingmodel_boundedscalar)
 
-    # 2 species (1 eq) primitive venturi mixing using mixing model including viscosity and thermal conductivity
+    # 2 species (1 eq) primitive venturi mixing using mixing model including viscosity, thermal conductivity and inlet markers for SA turbulence model
     species2_primitiveVenturi_mixingmodel_viscosity           = TestCase('species2_primitiveVenturi_mixingmodel_viscosity')
     species2_primitiveVenturi_mixingmodel_viscosity.cfg_dir   = "species_transport/venturi_primitive_3species"
     species2_primitiveVenturi_mixingmodel_viscosity.cfg_file  = "species2_primitiveVenturi_mixingmodel_viscosity.cfg"
     species2_primitiveVenturi_mixingmodel_viscosity.test_iter = 50
-    species2_primitiveVenturi_mixingmodel_viscosity.test_vals = [-4.725129, -4.311366, -4.610113, -5.833264, 0.552520, -4.945381, 5.000000, -1.834845, 5.000000, -5.496023, 5.000000, -1.733470, 2.277964, 0.972376, 0.608230, 0.697358]
+    species2_primitiveVenturi_mixingmodel_viscosity.test_vals = [-4.843487, -3.585775, -3.486490, -7.560246, -5.094190, 5.000000, -1.898139, 5.000000, -3.329399, 5.000000, -2.113219, 2.482224, 0.974144, 0.607217, 0.900862]
     species2_primitiveVenturi_mixingmodel_viscosity.new_output = True
     test_list.append(species2_primitiveVenturi_mixingmodel_viscosity)
 
diff --git a/TestCases/serial_regression.py b/TestCases/serial_regression.py
index 42c60ef4388..74068920570 100644
--- a/TestCases/serial_regression.py
+++ b/TestCases/serial_regression.py
@@ -255,7 +255,7 @@ def main():
     turb_flatplate.cfg_dir   = "rans/flatplate"
     turb_flatplate.cfg_file  = "turb_SA_flatplate.cfg"
     turb_flatplate.test_iter = 20
-    turb_flatplate.test_vals = [-4.157169, -6.737133, -0.176253, 0.057446] #last 4 columns
+    turb_flatplate.test_vals = [-4.157169, -6.736698, -0.176253, 0.057446] #last 4 columns
     turb_flatplate.new_output  = True
     test_list.append(turb_flatplate)
 
@@ -854,7 +854,7 @@ def main():
     ddes_flatplate.cfg_dir   = "ddes/flatplate"
     ddes_flatplate.cfg_file  = "ddes_flatplate.cfg"
     ddes_flatplate.test_iter = 10
-    ddes_flatplate.test_vals = [-2.714758, -5.883004, -0.215005, 0.023783, -618.160000]
+    ddes_flatplate.test_vals = [-2.714758, -5.882733, -0.215005, 0.023783, -618.160000]
     ddes_flatplate.unsteady  = True
     ddes_flatplate.new_output = True
     test_list.append(ddes_flatplate)
@@ -886,7 +886,7 @@ def main():
     ls89_sa.cfg_dir   = "nicf/LS89"
     ls89_sa.cfg_file  = "turb_SA_PR.cfg"
     ls89_sa.test_iter = 20
-    ls89_sa.test_vals = [-5.050483, -13.389547, 0.174939, 0.430757] #last 4 columns
+    ls89_sa.test_vals = [-5.050483, -13.371788, 0.174939, 0.430757] #last 4 columns
     ls89_sa.new_output= True
     test_list.append(ls89_sa)
 
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_viscosity.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_viscosity.cfg
index 3be5d7a6962..dd8017ec2a6 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_viscosity.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_viscosity.cfg
@@ -3,7 +3,8 @@
 % SU2 configuration file                                                       %
 % Case description: Species mixing with 2 species, i.e. 1 transport equations  %
 %                   Including mixture dependent density, viscosity, thermal    %
-%                   conductivity                                               %
+%                   conductivity and different viscosity ratios at the inlets  %
+%                   for the SA turbulent model.                                %
 % Author: Cristopher Morales Ubal                                              %
 % Institution: Eindhoven University of Technology                              %
 % Date: 2022/06/27                                                             %
@@ -14,16 +15,16 @@
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
 SOLVER= INC_RANS
-KIND_TURB_MODEL= SST
+KIND_TURB_MODEL= SA
 %
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
 INC_DENSITY_MODEL= VARIABLE
 INC_DENSITY_INIT= 1.1766
 %
-INC_VELOCITY_INIT= ( 1.00, 0.0, 0.0 )
+INC_VELOCITY_INIT= ( 5.00, 0.0, 0.0 )
 %
-INC_ENERGY_EQUATION= YES
+INC_ENERGY_EQUATION= NO
 INC_TEMPERATURE_INIT= 300.0
 %
 INC_NONDIM= DIMENSIONAL
@@ -62,11 +63,15 @@ MARKER_SYM= ( axis )
 SPECIFIED_INLET_PROFILE= NO
 INLET_FILENAME= inlet_venturi.dat
 INC_INLET_TYPE=  VELOCITY_INLET VELOCITY_INLET
-MARKER_INLET= ( gas_inlet,       400, 1.0, 1.0,  0.0, 0.0,\
-                air_axial_inlet, 300, 1.0, 0.0, -1.0, 0.0 )
+MARKER_INLET= ( gas_inlet,       300, 5.0, 1.0,  0.0, 0.0,\
+                air_axial_inlet, 300, 3.0, 0.0, -1.0, 0.0 )
 SPECIES_USE_STRONG_BC= NO
 MARKER_INLET_SPECIES= (gas_inlet, 1.0, \          
-                       air_axial_inlet, 0.6)           
+                       air_axial_inlet, 0.6)
+%
+%
+MARKER_INLET_TURBULENT= (gas_inlet, 5.0, \          
+                       air_axial_inlet, 3.0)           
 %
 INC_OUTLET_TYPE= PRESSURE_OUTLET
 MARKER_OUTLET= ( outlet, 0.0 )
@@ -128,7 +133,7 @@ CONV_STARTITER= 10
 %
 MESH_FILENAME= primitiveVenturi.su2
 SCREEN_OUTPUT= INNER_ITER WALL_TIME \
-               RMS_PRESSURE RMS_VELOCITY-X RMS_VELOCITY-Y RMS_TKE RMS_DISSIPATION RMS_SPECIES_0 RMS_SPECIES_1 \
+               RMS_RES \
                LINSOL_ITER LINSOL_RESIDUAL \
                LINSOL_ITER_TURB LINSOL_RESIDUAL_TURB \
                LINSOL_ITER_SPECIES LINSOL_RESIDUAL_SPECIES \
diff --git a/config_template.cfg b/config_template.cfg
index 0463ce3357f..08acc5eedc7 100644
--- a/config_template.cfg
+++ b/config_template.cfg
@@ -987,7 +987,8 @@ SPATIAL_FOURIER= NO
 CATALYTIC_WALL= ( NONE )
 %
 % Inlet Turbulent boundary marker(s) with the following format:
-% (inlet_marker1, TurbIntensity1, RatioTurbLamViscosity1, inlet_marker2, TurbIntensity2, RatioTurbLamViscosity2, ...)
+% SA Model: (inlet_marker1, NuFactor1, inlet_marker2, NuFactor2, ...)
+% SST Model: (inlet_marker1, TurbIntensity1, RatioTurbLamViscosity1, inlet_marker2, TurbIntensity2, RatioTurbLamViscosity2, ...)
 MARKER_INLET_TURBULENT= (inlet1, 0.05, 15, inlet2, 0.02, ...)
 
 % ------------------------ WALL ROUGHNESS DEFINITION --------------------------%

From 3802c17838f46f5c314fc001864bdf082557419e Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 11 Mar 2023 18:39:50 -0800
Subject: [PATCH 262/656] remove legacy build files

---
 .lgtm.yml                      |     19 -
 .travis.yml                    |     90 -
 Common/lib/Makefile.am         |    169 -
 SU2_CFD/bin/.csv               |      0
 SU2_CFD/bin/.gitignore         |      2 -
 SU2_CFD/bin/.vtk               | 142079 ------------------------------
 SU2_CFD/obj/Makefile.am        |    277 -
 SU2_DEF/bin/.gitignore         |      2 -
 SU2_DEF/obj/Makefile.am        |     52 -
 SU2_DOT/bin/.gitignore         |      2 -
 SU2_DOT/obj/Makefile.am        |     80 -
 SU2_GEO/bin/.gitignore         |      2 -
 SU2_GEO/obj/Makefile.am        |     49 -
 SU2_PY/Makefile.am             |     89 -
 SU2_PY/pySU2/Makefile.am       |    134 -
 SU2_SOL/bin/.gitignore         |      2 -
 SU2_SOL/obj/Makefile.am        |     52 -
 externals/Makefile.am          |     46 -
 externals/cgns/Makefile.am     |     34 -
 externals/metis/Makefile.am    |    109 -
 externals/parmetis/Makefile.am |     68 -
 externals/tecio/Makefile.am    |     40 -
 legacy/Makefile.am             |     64 -
 legacy/bootstrap               |    151 -
 legacy/configure.ac            |    410 -
 legacy/preconfigure.py         |    590 -
 m4/ax_tls.m4                   |     74 -
 m4/cgns.m4                     |     46 -
 m4/codi.m4                     |     53 -
 m4/compiler.m4                 |     66 -
 m4/metis.m4                    |     50 -
 m4/parmetis.m4                 |     47 -
 m4/tecio.m4                    |     61 -
 33 files changed, 145009 deletions(-)
 delete mode 100644 .lgtm.yml
 delete mode 100644 .travis.yml
 delete mode 100644 Common/lib/Makefile.am
 delete mode 100644 SU2_CFD/bin/.csv
 delete mode 100644 SU2_CFD/bin/.gitignore
 delete mode 100644 SU2_CFD/bin/.vtk
 delete mode 100644 SU2_CFD/obj/Makefile.am
 delete mode 100644 SU2_DEF/bin/.gitignore
 delete mode 100644 SU2_DEF/obj/Makefile.am
 delete mode 100644 SU2_DOT/bin/.gitignore
 delete mode 100644 SU2_DOT/obj/Makefile.am
 delete mode 100644 SU2_GEO/bin/.gitignore
 delete mode 100644 SU2_GEO/obj/Makefile.am
 delete mode 100644 SU2_PY/Makefile.am
 delete mode 100644 SU2_PY/pySU2/Makefile.am
 delete mode 100644 SU2_SOL/bin/.gitignore
 delete mode 100644 SU2_SOL/obj/Makefile.am
 delete mode 100644 externals/Makefile.am
 delete mode 100644 externals/cgns/Makefile.am
 delete mode 100644 externals/metis/Makefile.am
 delete mode 100644 externals/parmetis/Makefile.am
 delete mode 100644 externals/tecio/Makefile.am
 delete mode 100644 legacy/Makefile.am
 delete mode 100755 legacy/bootstrap
 delete mode 100644 legacy/configure.ac
 delete mode 100755 legacy/preconfigure.py
 delete mode 100644 m4/ax_tls.m4
 delete mode 100644 m4/cgns.m4
 delete mode 100644 m4/codi.m4
 delete mode 100644 m4/compiler.m4
 delete mode 100644 m4/metis.m4
 delete mode 100644 m4/parmetis.m4
 delete mode 100644 m4/tecio.m4

diff --git a/.lgtm.yml b/.lgtm.yml
deleted file mode 100644
index 8489adfaea0..00000000000
--- a/.lgtm.yml
+++ /dev/null
@@ -1,19 +0,0 @@
-extraction:
-  cpp:
-     prepare:
-        packages: 
-          - libboost-all-dev
-     configure:
-        command:
-        - ./meson.py build --optimization=1
-     index:
-        build_command:
-        - ./ninja -C build
-
-path_classifiers:
-  test:
-    - TestCases/*
-  library:
-    - externals/*
-  legacy:
-    - preconfigure.py
diff --git a/.travis.yml b/.travis.yml
deleted file mode 100644
index 28481849073..00000000000
--- a/.travis.yml
+++ /dev/null
@@ -1,90 +0,0 @@
-# Continous Integration setup for SU2.
-# Tests on the develop branch in both serial and parallel.
-
-dist: xenial
-sudo: required
-
-language: c++
-
-cache: 
-    - ccache
-    - pip
-    - directories: 
-      - $HOME/.pyenv_cache
-
-compiler:
-    - gcc
-
-notifications:
-    email:
-        recipients:
-            - su2code-dev@lists.stanford.edu
-  
-branches:
-    only:
-        - develop
-
-virtualenv:
-  system_site_packages: true
-
-env:
-    matrix:
-        # Serial build and test
-        - CONFIGURE_COMMAND="./meson.py build --prefix=$TRAVIS_BUILD_DIR -Denable-pywrapper=true -Dwith-mpi=disabled"
-          TEST_SCRIPT=serial_regression.py
-
-        # Parallel build and test
-        - CONFIGURE_COMMAND="./meson.py build --prefix=$TRAVIS_BUILD_DIR -Denable-pywrapper=true"
-          TEST_SCRIPT=parallel_regression.py
-
-        # Hybrid-parallel build and test
-        - CONFIGURE_COMMAND="./meson.py build --prefix=$TRAVIS_BUILD_DIR -Dwith-omp=true -Denable-mixedprec=true -Denable-tecio=false"
-          TEST_SCRIPT=hybrid_regression.py
-
-        # Serial build and test for AD
-        - CONFIGURE_COMMAND="./meson.py build --prefix=$TRAVIS_BUILD_DIR -Denable-pywrapper=true -Dwith-mpi=disabled -Denable-autodiff=true -Denable-directdiff=true"
-          TEST_SCRIPT=serial_regression_AD.py
-
-        # Parallel build and test for AD
-        - CONFIGURE_COMMAND="./meson.py build --prefix=$TRAVIS_BUILD_DIR -Denable-pywrapper=true -Denable-autodiff=true"
-          TEST_SCRIPT=parallel_regression_AD.py
-
-before_install:
-    # Temporarily fixes Travis CI issue with paths for Python packages
-    - export PATH=/usr/bin:$PATH
-    - sudo update-alternatives --install /usr/bin/python python /usr/bin/python3 10
-    # Install the necessary packages using apt-get with sudo
-    - sudo apt-get update -qq
-    - sudo apt-get install -qq build-essential python3-numpy python3-scipy libopenmpi-dev openmpi-bin swig python3-mpi4py
-    # to avoid interference with MPI
-    - test -n $CC  && unset CC
-    - test -n $CXX && unset CXX
-
-install:
-    # build ninja
-    - echo $CONFIGURE_COMMAND
-    - $CONFIGURE_COMMAND
-    - ./meson.py build --reconfigure --optimization=2
-    - ./meson.py build --reconfigure --warnlevel=2
-    - ./ninja -C build install
-
-    # Add environmental variables according to the configure step
-    - export SU2_RUN=$TRAVIS_BUILD_DIR/bin
-    - export SU2_HOME=$TRAVIS_BUILD_DIR
-    - export PATH=$PATH:$SU2_RUN
-    - export PYTHONPATH=$PYTHONPATH:$SU2_RUN
-
-before_script:
-    # Get the test cases
-    - git clone --depth=1 -b develop https://github.com/su2code/TestCases.git ./TestData
-    - cp -R ./TestData/* ./TestCases/
-
-    # Get the tutorial cases
-    - git clone --depth=1 -b develop https://github.com/su2code/su2code.github.io ./Tutorials
-    
-    # Enter the SU2/TestCases/ directory, which is now ready to run
-    - cd TestCases/
-
-script:
-    # Run the tests via the Python scripts
-    - python $TEST_SCRIPT
diff --git a/Common/lib/Makefile.am b/Common/lib/Makefile.am
deleted file mode 100644
index 4323382ceea..00000000000
--- a/Common/lib/Makefile.am
+++ /dev/null
@@ -1,169 +0,0 @@
-################################################################################
-#
-# \file Makefile.am
-# \brief Makefile for the SU2 common library
-# \author M. Colonno, T. Economon, F. Palacios
-# \version 7.5.1 "Blackbird"
-#
-# SU2 Project Website: https://su2code.github.io
-#
-# The SU2 Project is maintained by the SU2 Foundation
-# (http://su2foundation.org)
-#
-# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
-#
-# SU2 is free software; you can redistribute it and/or
-# modify it under the terms of the GNU Lesser General Public
-# License as published by the Free Software Foundation; either
-# version 2.1 of the License, or (at your option) any later version.
-#
-# SU2 is distributed in the hope that it will be useful,
-# but WITHOUT ANY WARRANTY; without even the implied warranty of
-# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
-# Lesser General Public License for more details.
-#
-# You should have received a copy of the GNU Lesser General Public
-# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
-#
-################################################################################
-
-AUTOMAKE_OPTIONS = subdir-objects
-ACLOCAL_AMFLAGS = ${ACLOCAL_FLAGS}
-
-noinst_LIBRARIES =
-
-if BUILD_NORMAL
-noinst_LIBRARIES += libSU2.a
-endif
-
-if BUILD_DIRECTDIFF
-noinst_LIBRARIES += libSU2_DIRECTDIFF.a
-endif
-
-if BUILD_REVERSE
-noinst_LIBRARIES += libSU2_AD.a
-endif
-
-lib_sources = \
-  ../src/fem/fem_cgns_elements.cpp \
-  ../src/CConfig.cpp \
-  ../src/linear_algebra/blas_structure.cpp \
-  ../src/fem/fem_geometry_structure.cpp \
-  ../src/fem/fem_integration_rules.cpp \
-  ../src/fem/fem_standard_element.cpp \
-  ../src/fem/fem_wall_distance.cpp \
-  ../src/fem/fem_work_estimate_metis.cpp \
-  ../src/fem/geometry_structure_fem_part.cpp \
-  ../src/graph_coloring_structure.cpp \
-  ../src/grid_movement/CGridMovement.cpp \
-  ../src/grid_movement/CFreeFormBlending.cpp \
-  ../src/grid_movement/CBSplineBlending.cpp \
-  ../src/grid_movement/CBezierBlending.cpp \
-  ../src/grid_movement/CFreeFormDefBox.cpp \
-  ../src/grid_movement/CVolumetricMovement.cpp \
-  ../src/grid_movement/CSurfaceMovement.cpp \
-  ../include/parallelization/mpi_structure.cpp \
-  ../include/parallelization/omp_structure.cpp \
-  ../src/basic_types/ad_structure.cpp \
-  ../src/fem/fem_gauss_jacobi_quadrature.cpp \
-  ../src/geometry/CGeometry.cpp \
-  ../src/geometry/CPhysicalGeometry.cpp \
-  ../src/geometry/CMultiGridGeometry.cpp \
-  ../src/geometry/CMultiGridQueue.cpp \
-  ../src/geometry/CDummyGeometry.cpp \
-  ../src/geometry/elements/CElement.cpp \
-  ../src/geometry/elements/CTRIA1.cpp \
-  ../src/geometry/elements/CQUAD4.cpp \
-  ../src/geometry/elements/CTETRA1.cpp \
-  ../src/geometry/elements/CPYRAM5.cpp \
-  ../src/geometry/elements/CPRISM6.cpp \
-  ../src/geometry/elements/CHEXA8.cpp \
-  ../src/geometry/meshreader/CMeshReaderFVM.cpp \
-  ../src/geometry/meshreader/CSU2ASCIIMeshReaderFVM.cpp \
-  ../src/geometry/meshreader/CCGNSMeshReaderFVM.cpp \
-  ../src/geometry/meshreader/CRectangularMeshReaderFVM.cpp \
-  ../src/geometry/meshreader/CBoxMeshReaderFVM.cpp \
-  ../src/geometry/dual_grid/CDualGrid.cpp \
-  ../src/geometry/dual_grid/CEdge.cpp \
-  ../src/geometry/dual_grid/CPoint.cpp \
-  ../src/geometry/dual_grid/CVertex.cpp \
-  ../src/geometry/dual_grid/CTurboVertex.cpp \
-  ../src/geometry/primal_grid/CPrimalGrid.cpp \
-  ../src/geometry/primal_grid/CPrimalGridFEM.cpp \
-  ../src/geometry/primal_grid/CPrimalGridBoundFEM.cpp \
-  ../src/geometry/primal_grid/CLine.cpp \
-  ../src/geometry/primal_grid/CTriangle.cpp \
-  ../src/geometry/primal_grid/CPrism.cpp \
-  ../src/geometry/primal_grid/CPyramid.cpp \
-  ../src/geometry/primal_grid/CHexahedron.cpp \
-  ../src/geometry/primal_grid/CTetrahedron.cpp \
-  ../src/geometry/primal_grid/CQuadrilateral.cpp \
-  ../src/geometry/primal_grid/CVertexMPI.cpp \
-  ../src/interface_interpolation/CInterpolatorFactory.cpp \
-  ../src/interface_interpolation/CInterpolator.cpp \
-  ../src/interface_interpolation/CMirror.cpp \
-  ../src/interface_interpolation/CSlidingMesh.cpp \
-  ../src/interface_interpolation/CIsoparametric.cpp \
-  ../src/interface_interpolation/CNearestNeighbor.cpp \
-  ../src/interface_interpolation/CRadialBasisFunction.cpp \
-  ../src/adt/CADTBaseClass.cpp \
-  ../src/adt/CADTPointsOnlyClass.cpp \
-  ../src/adt/CADTElemClass.cpp \
-  ../src/wall_model.cpp \
-  ../src/toolboxes/printing_toolbox.cpp \
-  ../src/toolboxes/CLinearPartitioner.cpp \
-  ../src/toolboxes/C1DInterpolation.cpp \
-  ../src/toolboxes/CSymmetricMatrix.cpp \
-  ../src/toolboxes/CSquareMatrixCM.cpp \
-  ../src/toolboxes/MMS/CVerificationSolution.cpp \
-  ../src/toolboxes/MMS/CIncTGVSolution.cpp \
-  ../src/toolboxes/MMS/CInviscidVortexSolution.cpp \
-  ../src/toolboxes/MMS/CMMSIncEulerSolution.cpp \
-  ../src/toolboxes/MMS/CMMSIncNSSolution.cpp \
-  ../src/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.cpp \
-  ../src/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.cpp \
-  ../src/toolboxes/MMS/CMMSNSUnitQuadSolution.cpp \
-  ../src/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.cpp \
-  ../src/toolboxes/MMS/CNSUnitQuadSolution.cpp \
-  ../src/toolboxes/MMS/CRinglebSolution.cpp \
-  ../src/toolboxes/MMS/CTGVSolution.cpp \
-  ../src/toolboxes/MMS/CUserDefinedSolution.cpp \
-  ../src/linear_algebra/CSysVector.cpp \
-  ../src/linear_algebra/CSysMatrix.cpp \
-  ../src/linear_algebra/CSysSolve.cpp \
-  ../src/linear_algebra/CSysSolve_b.cpp \
-  ../src/linear_algebra/CPastixWrapper.cpp \
-  ../src/containers/CLookUpTable.cpp \
-  ../src/containers/CTrapezoidalMap.cpp \
-  ../src/containers/CFileReaderLUT.cpp
-
-lib_cxxflags = -fPIC -std=c++11
-lib_ldadd =
-
-# always link to built dependencies from ./externals
-lib_cxxflags += @su2_externals_INCLUDES@
-lib_ldadd += @su2_externals_LIBS@
-
-# if BUILD_MUTATIONPP
-lib_cxxflags += @MUTATIONPP_CXX@
-lib_ldadd += @MUTATIONPP_LD@
-# endif
-
-if BUILD_NORMAL
-libSU2_a_SOURCES = $(lib_sources)
-libSU2_a_CXXFLAGS = ${lib_cxxflags}
-libSU2_a_LIBADD = ${lib_ldadd}
-endif
-
-if BUILD_DIRECTDIFF
-libSU2_DIRECTDIFF_a_SOURCES = $(lib_sources)
-libSU2_DIRECTDIFF_a_CXXFLAGS = @DIRECTDIFF_CXX@ ${lib_cxxflags}
-libSU2_DIRECTDIFF_a_LIBADD =  ${lib_ldadd}
-endif
-
-if BUILD_REVERSE
-libSU2_AD_a_SOURCES = $(lib_sources)
-libSU2_AD_a_CXXFLAGS = @REVERSE_CXX@ ${lib_cxxflags}
-libSU2_AD_a_LIBADD =  ${lib_ldadd}
-endif
-
diff --git a/SU2_CFD/bin/.csv b/SU2_CFD/bin/.csv
deleted file mode 100644
index e69de29bb2d..00000000000
diff --git a/SU2_CFD/bin/.gitignore b/SU2_CFD/bin/.gitignore
deleted file mode 100644
index fe891329eff..00000000000
--- a/SU2_CFD/bin/.gitignore
+++ /dev/null
@@ -1,2 +0,0 @@
-# Do not track compiled execuatables
-SU2*
diff --git a/SU2_CFD/bin/.vtk b/SU2_CFD/bin/.vtk
deleted file mode 100644
index 900960c4d43..00000000000
--- a/SU2_CFD/bin/.vtk
+++ /dev/null
@@ -1,142079 +0,0 @@
-# vtk DataFile Version 2.0
-Visualizacion de la malla computacional
-ASCII
-DATASET UNSTRUCTURED_GRID
-POINTS 46417 float
-0.664297	0	-0.00127964
-0.654653	0	-0.00256277
-0.644559	0	-0.00388216
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diff --git a/SU2_CFD/obj/Makefile.am b/SU2_CFD/obj/Makefile.am
deleted file mode 100644
index 6926cadc38d..00000000000
--- a/SU2_CFD/obj/Makefile.am
+++ /dev/null
@@ -1,277 +0,0 @@
-################################################################################
-#
-# \file Makefile.am
-# \brief Makefile for SU2_CFD
-# \author M. Colonno, T. Economon, F. Palacios
-# \version 7.5.1 "Blackbird"
-#
-# SU2 Project Website: https://su2code.github.io
-#
-# The SU2 Project is maintained by the SU2 Foundation
-# (http://su2foundation.org)
-#
-# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
-#
-# SU2 is free software; you can redistribute it and/or
-# modify it under the terms of the GNU Lesser General Public
-# License as published by the Free Software Foundation; either
-# version 2.1 of the License, or (at your option) any later version.
-#
-# SU2 is distributed in the hope that it will be useful,
-# but WITHOUT ANY WARRANTY; without even the implied warranty of
-# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
-# Lesser General Public License for more details.
-#
-# You should have received a copy of the GNU Lesser General Public
-# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
-#
-################################################################################
-
-AUTOMAKE_OPTIONS = subdir-objects
-ACLOCAL_AMFLAGS = ${ACLOCAL_FLAGS}
-
-bin_PROGRAMS =
-noinst_LIBRARIES =
-
-if BUILD_NORMAL
-bin_PROGRAMS += ../bin/SU2_CFD
-noinst_LIBRARIES+= libSU2Core.a
-endif
-
-if BUILD_DIRECTDIFF
-bin_PROGRAMS += ../bin/SU2_CFD_DIRECTDIFF
-noinst_LIBRARIES+= libSU2Core_DIRECTDIFF.a
-endif
-
-if BUILD_REVERSE
-bin_PROGRAMS += ../bin/SU2_CFD_AD
-noinst_LIBRARIES+= libSU2Core_AD.a
-endif
-
-libSU2Core_sources = ../src/definition_structure.cpp \
-  ../src/fluid/CFluidModel.cpp \
-  ../src/fluid/CIdealGas.cpp \
-  ../src/fluid/CFluidScalar.cpp \
-  ../src/fluid/CPengRobinson.cpp \
-  ../src/fluid/CVanDerWaalsGas.cpp \
-  ../src/fluid/CCoolProp.cpp \
-  ../src/fluid/CNEMOGas.cpp \
-  ../src/fluid/CSU2TCLib.cpp \
-  ../src/fluid/CMutationTCLib.cpp \
-  ../src/integration/CIntegration.cpp \
-  ../src/integration/CSingleGridIntegration.cpp \
-  ../src/integration/CMultiGridIntegration.cpp \
-  ../src/integration/CNewtonIntegration.cpp \
-  ../src/integration/CStructuralIntegration.cpp \
-  ../src/integration/CFEM_DG_Integration.cpp \
-  ../src/integration/CIntegrationFactory.cpp \
-  ../src/drivers/CMultizoneDriver.cpp \
-  ../src/drivers/CSinglezoneDriver.cpp \
-  ../src/drivers/CDiscAdjSinglezoneDriver.cpp \
-  ../src/drivers/CDiscAdjMultizoneDriver.cpp \
-  ../src/drivers/CDriver.cpp \
-  ../src/drivers/CDummyDriver.cpp \
-  ../src/iteration/CIteration.cpp \
-  ../src/iteration/CIterationFactory.cpp \
-  ../src/iteration/CAdjFluidIteration.cpp \
-  ../src/iteration/CDiscAdjFluidIteration.cpp \
-  ../src/iteration/CDiscAdjHeatIteration.cpp \
-  ../src/iteration/CDiscAdjFEAIteration.cpp \
-  ../src/iteration/CFEAIteration.cpp \
-  ../src/iteration/CFEMFluidIteration.cpp \
-  ../src/iteration/CFluidIteration.cpp \
-  ../src/iteration/CHeatIteration.cpp \
-  ../src/iteration/CTurboIteration.cpp \
-  ../src/numerics/CNumerics.cpp \
-  ../src/numerics/template.cpp \
-  ../src/numerics/transition.cpp \
-  ../src/numerics/radiation.cpp \
-  ../src/numerics/CLookUpTable.cpp \
-  ../src/numerics/CTrapezoidalMap.cpp \
-  ../src/numerics/CFileReaderLUT.cpp \
-  ../src/numerics/flow/convection/roe.cpp \
-  ../src/numerics/flow/convection/fds.cpp \
-  ../src/numerics/flow/convection/fvs.cpp \
-  ../src/numerics/flow/convection/cusp.cpp \
-  ../src/numerics/flow/convection/hllc.cpp \
-  ../src/numerics/flow/convection/ausm_slau.cpp \
-  ../src/numerics/flow/convection/centered.cpp \
-  ../src/numerics/flow/flow_diffusion.cpp \
-  ../src/numerics/flow/flow_sources.cpp \
-  ../src/numerics/NEMO/convection/roe.cpp \
-  ../src/numerics/NEMO/convection/ausm_slau.cpp \
-  ../src/numerics/NEMO/convection/lax.cpp \
-  ../src/numerics/NEMO/convection/msw.cpp \
-  ../src/numerics/NEMO/CNEMONumerics.cpp \
-  ../src/numerics/NEMO/NEMO_diffusion.cpp \
-  ../src/numerics/NEMO/NEMO_sources.cpp \
-  ../src/numerics/continuous_adjoint/adj_convection.cpp \
-  ../src/numerics/continuous_adjoint/adj_diffusion.cpp \
-  ../src/numerics/continuous_adjoint/adj_sources.cpp \
-  ../src/numerics/scalar/scalar_sources.cpp \
-  ../src/numerics/species/species_sources.cpp \
-  ../src/numerics/elasticity/CFEAElasticity.cpp \
-  ../src/numerics/elasticity/CFEALinearElasticity.cpp \
-  ../src/numerics/elasticity/CFEANonlinearElasticity.cpp \
-  ../src/numerics/elasticity/nonlinear_models.cpp \
-  ../include/numerics_simd/CNumericsSIMD.cpp \
-  ../src/output/filewriter/CCSVFileWriter.cpp \
-  ../src/output/filewriter/CSTLFileWriter.cpp \
-  ../src/output/filewriter/CFEMDataSorter.cpp \
-  ../src/output/filewriter/CFVMDataSorter.cpp \
-  ../src/output/filewriter/CParallelDataSorter.cpp \
-  ../src/output/filewriter/CParallelFileWriter.cpp \
-  ../src/output/filewriter/CParaviewBinaryFileWriter.cpp \
-  ../src/output/filewriter/CParaviewXMLFileWriter.cpp \
-  ../src/output/filewriter/CParaviewVTMFileWriter.cpp \
-  ../src/output/filewriter/CParaviewFileWriter.cpp \
-  ../src/output/filewriter/CSurfaceFEMDataSorter.cpp \
-  ../src/output/filewriter/CSurfaceFVMDataSorter.cpp \
-  ../src/output/filewriter/CSU2BinaryFileWriter.cpp \
-  ../src/output/filewriter/CSU2FileWriter.cpp \
-  ../src/output/filewriter/CSU2MeshFileWriter.cpp \
-  ../src/output/filewriter/CTecplotFileWriter.cpp \
-  ../src/output/filewriter/CTecplotBinaryFileWriter.cpp \
-  ../src/output/filewriter/CCGNSFileWriter.cpp \
-  ../src/output/tools/CWindowingTools.cpp \
-  ../src/output/COutput.cpp \
-  ../src/output/output_physics.cpp \
-  ../src/output/CMeshOutput.cpp \
-  ../src/output/CElasticityOutput.cpp \
-  ../src/output/CFVMOutput.cpp \
-  ../src/output/CFlowOutput.cpp \
-  ../src/output/CFlowCompOutput.cpp \
-  ../src/output/CFlowCompFEMOutput.cpp \
-  ../src/output/CFlowIncOutput.cpp \
-  ../src/output/CHeatOutput.cpp \
-  ../src/output/CBaselineOutput.cpp \
-  ../src/output/CAdjElasticityOutput.cpp \
-  ../src/output/CAdjHeatOutput.cpp \
-  ../src/output/CAdjFlowOutput.cpp \
-  ../src/output/CAdjFlowCompOutput.cpp \
-  ../src/output/CAdjFlowIncOutput.cpp \
-  ../src/output/CMultizoneOutput.cpp \
-  ../src/output/CNEMOCompOutput.cpp \
-  ../src/output/COutputFactory.cpp \
-  ../src/output/output_structure_legacy.cpp \
-  ../src/python_wrapper_structure.cpp \
-  ../src/solvers/CAdjEulerSolver.cpp \
-  ../src/solvers/CAdjNSSolver.cpp \
-  ../src/solvers/CAdjTurbSolver.cpp \
-  ../src/solvers/CBaselineSolver.cpp \
-  ../src/solvers/CBaselineSolver_FEM.cpp \
-  ../src/solvers/CDiscAdjFEASolver.cpp \
-  ../src/solvers/CDiscAdjMeshSolver.cpp \
-  ../src/solvers/CDiscAdjSolver.cpp \
-  ../src/solvers/CEulerSolver.cpp \
-  ../src/solvers/CFEASolver.cpp \
-  ../src/solvers/CFEM_DG_EulerSolver.cpp \
-  ../src/solvers/CFEM_DG_NSSolver.cpp \
-  ../src/solvers/CHeatSolver.cpp \
-  ../src/solvers/CIncEulerSolver.cpp \
-  ../src/solvers/CIncNSSolver.cpp \
-  ../src/solvers/CMeshSolver.cpp \
-  ../src/solvers/CRadSolver.cpp \
-  ../src/solvers/CRadP1Solver.cpp \
-  ../src/solvers/CNEMOEulerSolver.cpp \
-  ../src/solvers/CNEMONSSolver.cpp \
-  ../src/solvers/CNSSolver.cpp \
-  ../src/solvers/CSolver.cpp \
-  ../src/solvers/CTemplateSolver.cpp \
-  ../src/solvers/CTransLMSolver.cpp \
-  ../src/solvers/CSpeciesSolver.cpp \
-  ../src/solvers/CTurbSolver.cpp \
-  ../src/solvers/CTurbSASolver.cpp \
-  ../src/solvers/CTurbSSTSolver.cpp \
-  ../src/solvers/CSolverFactory.cpp \
-  ../src/limiters/CLimiterDetails.cpp \
-  ../src/CMarkerProfileReaderFVM.cpp \
-  ../src/interfaces/CInterface.cpp \
-  ../src/interfaces/cfd/CConservativeVarsInterface.cpp \
-  ../src/interfaces/cfd/CMixingPlaneInterface.cpp \
-  ../src/interfaces/cfd/CSlidingInterface.cpp \
-  ../src/interfaces/cht/CConjugateHeatInterface.cpp \
-  ../src/interfaces/fsi/CDisplacementsInterface.cpp \
-  ../src/interfaces/fsi/CFlowTractionInterface.cpp \
-  ../src/interfaces/fsi/CDiscAdjFlowTractionInterface.cpp \
-  ../src/variables/CFEABoundVariable.cpp \
-  ../src/variables/CRadVariable.cpp \
-  ../src/variables/CRadP1Variable.cpp \
-  ../src/variables/CDiscAdjMeshBoundVariable.cpp \
-  ../src/variables/CMeshBoundVariable.cpp \
-  ../src/variables/CMeshElement.cpp \
-  ../src/variables/CMeshVariable.cpp \
-  ../src/variables/CHeatVariable.cpp \
-  ../src/variables/CVariable.cpp \
-  ../src/variables/CAdjNSVariable.cpp \
-  ../src/variables/CTurbSSTVariable.cpp \
-  ../src/variables/CAdjTurbVariable.cpp \
-  ../src/variables/CTransLMVariable.cpp \
-  ../src/variables/CDiscAdjFEABoundVariable.cpp \
-  ../src/variables/CIncEulerVariable.cpp \
-  ../src/variables/CScalarVariable.cpp \
-  ../src/variables/CSpeciesVariable.cpp \
-  ../src/variables/CTurbVariable.cpp \
-  ../src/variables/CNSVariable.cpp \
-  ../src/variables/CNEMOEulerVariable.cpp \
-  ../src/variables/CNEMONSVariable.cpp \
-  ../src/variables/CBaselineVariable.cpp \
-  ../src/variables/CTurbSAVariable.cpp \
-  ../src/variables/CFEAVariable.cpp \
-  ../src/variables/CAdjEulerVariable.cpp \
-  ../src/variables/CDiscAdjVariable.cpp \
-  ../src/variables/CIncNSVariable.cpp \
-  ../src/variables/CEulerVariable.cpp \
-  ../src/variables/CFlowVariable.cpp
-
-su2_cfd_sources = \
-  ../src/SU2_CFD.cpp
-
-libSU2Core_cxx_flags = -fPIC -std=c++11
-libSU2Core_libadd =
-
-su2_cfd_cxx_flags = -fPIC -std=c++11
-su2_cfd_ldadd =
-
-# always link to built dependencies from ./externals
-su2_cfd_cxx_flags += @su2_externals_INCLUDES@
-su2_cfd_ldadd += @su2_externals_LIBS@
-su2_cfd_ldadd += @su2_externals_LIBPTHREAD@
-libSU2Core_cxx_flags += @su2_externals_INCLUDES@
-
-# if BUILD_MUTATIONPP
-su2_cfd_cxx_flags += @MUTATIONPP_CXX@
-su2_cfd_ldadd += @MUTATIONPP_LD@
-# endif
-
-
-su2_cfd_cxx_flags += @CoolProp_CXX@
-su2_cfd_ldadd += @CoolProp_LD@
-
-
-if BUILD_NORMAL
-libSU2Core_a_SOURCES = $(libSU2Core_sources)
-libSU2Core_a_CXXFLAGS = $(libSU2Core_cxx_flags)
-libSU2Core_a_LIBADD = $(libSU2Core_libadd)
-___bin_SU2_CFD_SOURCES = $(su2_cfd_sources)
-___bin_SU2_CFD_CXXFLAGS = ${su2_cfd_cxx_flags}
-___bin_SU2_CFD_LDADD = libSU2Core.a ../../Common/lib/libSU2.a ${su2_cfd_ldadd}
-endif
-
-if BUILD_DIRECTDIFF
-libSU2Core_DIRECTDIFF_a_SOURCES = $(libSU2Core_sources)
-libSU2Core_DIRECTDIFF_a_CXXFLAGS = @DIRECTDIFF_CXX@ $(libSU2Core_cxx_flags)
-libSU2Core_DIRECTDIFF_a_LIBADD = @DIRECTDIFF_LIBS@ $(libSU2Core_libadd)
-___bin_SU2_CFD_DIRECTDIFF_SOURCES = $(su2_cfd_sources)
-___bin_SU2_CFD_DIRECTDIFF_CXXFLAGS = @DIRECTDIFF_CXX@ ${su2_cfd_cxx_flags}
-___bin_SU2_CFD_DIRECTDIFF_LDADD = libSU2Core_DIRECTDIFF.a @DIRECTDIFF_LIBS@ ../../Common/lib/libSU2_DIRECTDIFF.a ${su2_cfd_ldadd}
-endif
-
-if BUILD_REVERSE
-libSU2Core_AD_a_SOURCES = $(libSU2Core_sources)
-libSU2Core_AD_a_CXXFLAGS = @REVERSE_CXX@ $(libSU2Core_cxx_flags)
-libSU2Core_AD_a_LIBADD = @REVERSE_LIBS@ $(libSU2Core_libadd)
-___bin_SU2_CFD_AD_SOURCES = $(su2_cfd_sources)
-___bin_SU2_CFD_AD_CXXFLAGS = @REVERSE_CXX@ ${su2_cfd_cxx_flags}
-___bin_SU2_CFD_AD_LDADD = libSU2Core_AD.a @REVERSE_LIBS@ ../../Common/lib/libSU2_AD.a ${su2_cfd_ldadd}
-endif
diff --git a/SU2_DEF/bin/.gitignore b/SU2_DEF/bin/.gitignore
deleted file mode 100644
index fe891329eff..00000000000
--- a/SU2_DEF/bin/.gitignore
+++ /dev/null
@@ -1,2 +0,0 @@
-# Do not track compiled execuatables
-SU2*
diff --git a/SU2_DEF/obj/Makefile.am b/SU2_DEF/obj/Makefile.am
deleted file mode 100644
index 4edc38c8fd4..00000000000
--- a/SU2_DEF/obj/Makefile.am
+++ /dev/null
@@ -1,52 +0,0 @@
-################################################################################
-#
-# \file Makefile.am
-# \brief Makefile for SU2_DEF
-# \author M. Colonno, T. Economon, F. Palacios
-# \version 7.5.1 "Blackbird"
-#
-# SU2 Project Website: https://su2code.github.io
-#
-# The SU2 Project is maintained by the SU2 Foundation
-# (http://su2foundation.org)
-#
-# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
-#
-# SU2 is free software; you can redistribute it and/or
-# modify it under the terms of the GNU Lesser General Public
-# License as published by the Free Software Foundation; either
-# version 2.1 of the License, or (at your option) any later version.
-#
-# SU2 is distributed in the hope that it will be useful,
-# but WITHOUT ANY WARRANTY; without even the implied warranty of
-# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
-# Lesser General Public License for more details.
-#
-# You should have received a copy of the GNU Lesser General Public
-# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
-#
-################################################################################
-
-AUTOMAKE_OPTIONS = subdir-objects
-ACLOCAL_AMFLAGS = ${ACLOCAL_FLAGS}
-
-bin_PROGRAMS = ../bin/SU2_DEF
-
-___bin_SU2_DEF_SOURCES = \
-  ../src/SU2_DEF.cpp
-
-
-___bin_SU2_DEF_CXXFLAGS =
-___bin_SU2_DEF_LDADD = \
-  ../../SU2_CFD/obj/libSU2Core.a \
-  ../../Common/lib/libSU2.a
-
-# always link to built dependencies from ./externals
-___bin_SU2_DEF_CXXFLAGS += @su2_externals_INCLUDES@
-___bin_SU2_DEF_LDADD += @su2_externals_LIBS@
-___bin_SU2_DEF_LDADD += @su2_externals_LIBPTHREAD@
-
-# if BUILD_MUTATIONPP
-___bin_SU2_DEF_CXXFLAGS += @MUTATIONPP_CXX@
-___bin_SU2_DEF_LDADD += @MUTATIONPP_LD@
-# endif
diff --git a/SU2_DOT/bin/.gitignore b/SU2_DOT/bin/.gitignore
deleted file mode 100644
index fe891329eff..00000000000
--- a/SU2_DOT/bin/.gitignore
+++ /dev/null
@@ -1,2 +0,0 @@
-# Do not track compiled execuatables
-SU2*
diff --git a/SU2_DOT/obj/Makefile.am b/SU2_DOT/obj/Makefile.am
deleted file mode 100644
index 23c60fe972f..00000000000
--- a/SU2_DOT/obj/Makefile.am
+++ /dev/null
@@ -1,80 +0,0 @@
-################################################################################
-#
-# \file Makefile.am
-# \brief Makefile for SU2_DOT
-# \author M. Colonno, T. Economon, F. Palacios
-# \version 7.5.1 "Blackbird"
-#
-# SU2 Project Website: https://su2code.github.io
-#
-# The SU2 Project is maintained by the SU2 Foundation
-# (http://su2foundation.org)
-#
-# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
-#
-# SU2 is free software; you can redistribute it and/or
-# modify it under the terms of the GNU Lesser General Public
-# License as published by the Free Software Foundation; either
-# version 2.1 of the License, or (at your option) any later version.
-#
-# SU2 is distributed in the hope that it will be useful,
-# but WITHOUT ANY WARRANTY; without even the implied warranty of
-# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
-# Lesser General Public License for more details.
-#
-# You should have received a copy of the GNU Lesser General Public
-# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
-#
-################################################################################
-
-AUTOMAKE_OPTIONS = subdir-objects
-ACLOCAL_AMFLAGS = ${ACLOCAL_FLAGS}
-
-bin_PROGRAMS =
-
-if BUILD_NORMAL
-bin_PROGRAMS += ../bin/SU2_DOT
-endif
-
-if BUILD_REVERSE
-bin_PROGRAMS += ../bin/SU2_DOT_AD
-endif
-
-su2_dot_sources = ../src/SU2_DOT.cpp
-
-su2_dot_ldadd =
-su2_dot_cxx_flags = -std=c++11
-
-if BUILD_NORMAL
-su2_dot_ldadd += \
-  ../../SU2_CFD/obj/libSU2Core.a \
-  ../../Common/lib/libSU2.a
-endif
-
-if BUILD_REVERSE
-su2_dot_ldadd += \
-  ../../SU2_CFD/obj/libSU2Core_AD.a \
-  ../../Common/lib/libSU2_AD.a
-endif
-
-# always link to built dependencies from ./externals
-su2_dot_cxx_flags += @su2_externals_INCLUDES@
-su2_dot_ldadd += @su2_externals_LIBS@
-su2_dot_ldadd += @su2_externals_LIBPTHREAD@
-
-# if BUILD_MUTATIONPP
-su2_dot_cxx_flags += @MUTATIONPP_CXX@
-su2_dot_ldadd += @MUTATIONPP_LD@
-# endif
-
-if BUILD_NORMAL
-___bin_SU2_DOT_SOURCES = ${su2_dot_sources}
-___bin_SU2_DOT_CXXFLAGS = ${su2_dot_cxx_flags}
-___bin_SU2_DOT_LDADD =  ${su2_dot_ldadd}
-endif
-
-if BUILD_REVERSE
-___bin_SU2_DOT_AD_SOURCES = ${su2_dot_sources}
-___bin_SU2_DOT_AD_CXXFLAGS = @REVERSE_CXX@ ${su2_dot_cxx_flags}
-___bin_SU2_DOT_AD_LDADD = @REVERSE_LIBS@ ${su2_dot_ldadd}
-endif
diff --git a/SU2_GEO/bin/.gitignore b/SU2_GEO/bin/.gitignore
deleted file mode 100644
index fe891329eff..00000000000
--- a/SU2_GEO/bin/.gitignore
+++ /dev/null
@@ -1,2 +0,0 @@
-# Do not track compiled execuatables
-SU2*
diff --git a/SU2_GEO/obj/Makefile.am b/SU2_GEO/obj/Makefile.am
deleted file mode 100644
index 16676446325..00000000000
--- a/SU2_GEO/obj/Makefile.am
+++ /dev/null
@@ -1,49 +0,0 @@
-################################################################################
-#
-# \file Makefile.am
-# \brief Makefile for SU2_GEO
-# \author M. Colonno, T. Economon, F. Palacios
-# \version 7.5.1 "Blackbird"
-#
-# SU2 Project Website: https://su2code.github.io
-#
-# The SU2 Project is maintained by the SU2 Foundation
-# (http://su2foundation.org)
-#
-# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
-#
-# SU2 is free software; you can redistribute it and/or
-# modify it under the terms of the GNU Lesser General Public
-# License as published by the Free Software Foundation; either
-# version 2.1 of the License, or (at your option) any later version.
-#
-# SU2 is distributed in the hope that it will be useful,
-# but WITHOUT ANY WARRANTY; without even the implied warranty of
-# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
-# Lesser General Public License for more details.
-#
-# You should have received a copy of the GNU Lesser General Public
-# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
-#
-################################################################################
-
-AUTOMAKE_OPTIONS = subdir-objects
-ACLOCAL_AMFLAGS = ${ACLOCAL_FLAGS}
-
-bin_PROGRAMS = ../bin/SU2_GEO
-
-___bin_SU2_GEO_SOURCES = \
-  ../include/SU2_GEO.hpp \
-  ../src/SU2_GEO.cpp
-
-___bin_SU2_GEO_CXXFLAGS =
-___bin_SU2_GEO_LDADD = ../../Common/lib/libSU2.a
-
-# always link to built dependencies from ./externals
-___bin_SU2_GEO_CXXFLAGS += @su2_externals_INCLUDES@
-___bin_SU2_GEO_LDADD += @su2_externals_LIBS@
-
-# if BUILD_MUTATIONPP
-___bin_SU2_GEO_CXXFLAGS += @MUTATIONPP_CXX@
-___bin_SU2_GEO_LDADD += @MUTATIONPP_LD@
-# endif
diff --git a/SU2_PY/Makefile.am b/SU2_PY/Makefile.am
deleted file mode 100644
index 82985bf4202..00000000000
--- a/SU2_PY/Makefile.am
+++ /dev/null
@@ -1,89 +0,0 @@
-################################################################################
-#
-# \file Makefile.am
-# \brief Makefile for the SU2 Python framework
-# \author M. Colonno, T. Economon, F. Palacios, T. Lukaczyk
-# \version 7.5.1 "Blackbird"
-#
-# SU2 Project Website: https://su2code.github.io
-#
-# The SU2 Project is maintained by the SU2 Foundation
-# (http://su2foundation.org)
-#
-# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
-#
-# SU2 is free software; you can redistribute it and/or
-# modify it under the terms of the GNU Lesser General Public
-# License as published by the Free Software Foundation; either
-# version 2.1 of the License, or (at your option) any later version.
-#
-# SU2 is distributed in the hope that it will be useful,
-# but WITHOUT ANY WARRANTY; without even the implied warranty of
-# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
-# Lesser General Public License for more details.
-#
-# You should have received a copy of the GNU Lesser General Public
-# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
-#
-################################################################################
-
-bin_SCRIPTS = \
-    continuous_adjoint.py \
-    compute_uncertainty.py \
-    finite_differences.py \
-    mesh_deformation.py \
-    parallel_computation.py \
-    parallel_computation_fsi.py \
-    package_tests.py \
-    shape_optimization.py \
-    merge_solution.py \
-    set_ffd_design_var.py \
-    compute_polar.py \
-    compute_multipoint.py \
-    discrete_adjoint.py \
-    direct_differentiation.py \
-    fsi_computation.py \
-    SU2_CFD.py
-
-
-mypkgdir = $(prefix)/bin
-nobase_dist_mypkg_DATA= \
-    SU2/__init__.py \
-    SU2/eval/design.py \
-    SU2/eval/functions.py \
-    SU2/eval/gradients.py \
-    SU2/eval/__init__.py \
-    SU2/io/config.py \
-    SU2/io/config_options.py \
-    SU2/io/data.py \
-    SU2/io/filelock.py \
-    SU2/io/redirect.py \
-    SU2/io/state.py \
-    SU2/io/tools.py \
-    SU2/io/historyMap.py \
-    SU2/io/__init__.py \
-    SU2/opt/project.py \
-    SU2/opt/scipy_tools.py \
-    SU2/opt/__init__.py \
-    SU2/run/adjoint.py \
-    SU2/run/deform.py \
-    SU2/run/direct.py \
-    SU2/run/interface.py \
-    SU2/run/merge.py \
-    SU2/run/geometry.py \
-    SU2/run/projection.py \
-    SU2/run/__init__.py \
-    SU2/util/bunch.py \
-    SU2/util/filter_adjoint.py \
-    SU2/util/lhc_unif.py \
-    SU2/util/misc.py \
-    SU2/util/mp_eval.py \
-    SU2/util/ordered_bunch.py \
-    SU2/util/ordered_dict.py \
-    SU2/util/plot.py \
-    SU2/util/polarSweepLib.py \
-    SU2/util/switch.py \
-    SU2/util/which.py \
-    SU2/util/__init__.py
-
-EXTRA_DIST = $(bin_SCRIPTS)
diff --git a/SU2_PY/pySU2/Makefile.am b/SU2_PY/pySU2/Makefile.am
deleted file mode 100644
index a5185f54e3f..00000000000
--- a/SU2_PY/pySU2/Makefile.am
+++ /dev/null
@@ -1,134 +0,0 @@
-################################################################################
-#
-# \file Makefile.am
-# \brief Makefile for the SU2 Python wrapper.
-# \author D. Thomas
-# \version 7.5.1 "Blackbird"
-#
-# SU2 Project Website: https://su2code.github.io
-#
-# The SU2 Project is maintained by the SU2 Foundation
-# (http://su2foundation.org)
-#
-# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
-#
-# SU2 is free software; you can redistribute it and/or
-# modify it under the terms of the GNU Lesser General Public
-# License as published by the Free Software Foundation; either
-# version 2.1 of the License, or (at your option) any later version.
-#
-# SU2 is distributed in the hope that it will be useful,
-# but WITHOUT ANY WARRANTY; without even the implied warranty of
-# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
-# Lesser General Public License for more details.
-#
-# You should have received a copy of the GNU Lesser General Public
-# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
-#
-################################################################################
-
-
-CURRENT_DIR = ${abs_top_builddir}/SU2_PY/pySU2
-
-SO_EXT=so
-
-if BUILD_NORMAL
-  SWIG_SRC = ${abs_top_srcdir}/SU2_PY/pySU2/pySU2.i
-  SWIG_WRAP_REAL = SU2_APIPYTHON_wrap
-  SWIG_SO_REAL = _pysu2.${SO_EXT}
-endif
-
-if BUILD_REVERSE
-  SWIG_SRC = ${abs_top_srcdir}/SU2_PY/pySU2/pySU2ad.i
-  SWIG_WRAP_REAL = SU2_APIPYTHON_wrap_AD
-  SWIG_SO_REAL = _pysu2ad.${SO_EXT}
-endif
-
-PYTHON_SITE_PACKAGES=$(shell python -c "import site; print(site.getsitepackages()[0])")
-#NUMPY_INCLUDE = /usr/lib/python2.7/dist-packages/numpy/core/include
-MPI4PY_INCLUDE = ${HOME}/.local/lib/python2.7/site-packages/mpi4py/include \
-                 -I${PYTHON_SITE_PACKAGES}/mpi4py/include \
-                 -I/Library/Python/2.7/site-packages/mpi4py/include
-
-SWIG = swig
-
-pySU2_INCLUDE = -I${abs_top_builddir}/Common/include \
-	-I${abs_top_builddir}/SU2_CFD/include
-
-PY_INCLUDE = ${PYTHON_INCLUDE} -I${MPI4PY_INCLUDE}
-
-PY_LIB = ${PYTHON_LIBS} \
-         -L${PYTHON_EXEC_PREFIX}/lib \
-         -L/usr/lib \
-         -L/usr/lib/x86_64-linux-gnu
-
-
-SWIG_INCLUDE = ${PY_INCLUDE}
-
-SUBDIR_EXEC = ${bindir}
-
-all:
-	${MAKE} real;
-
-# List the dependencies
-real: ${SWIG_SO_REAL}
-
-if BUILD_NORMAL
-  EXTRA_CC_FLAGS = -fPIC -O3 -std=c++11
-endif
-
-if BUILD_REVERSE
-  EXTRA_CC_FLAGS = -fPIC -O3 -std=c++11 -DCODI_REVERSE_TYPE -I$(top_srcdir)/externals/codi/include -I$(top_srcdir)/externals/medi/include
-#  EXTRA_CC_FLAGS = -fPIC -g3 -std=c++11 -DCODI_REVERSE_TYPE -I$(top_srcdir)/externals/codi/include -I$(top_srcdir)/externals/medi/include
-endif
-
-#SU2_BASE lib
-if BUILD_NORMAL
-  SU2SOLVER_LIB = ${abs_top_builddir}/SU2_CFD/obj/libSU2Core.a \
-    ${abs_top_builddir}/Common/lib/libSU2.a
-  PYLIB = pysu2.py
-  SOLIB = _pysu2.so
-endif
-
-#SU2_AD lib
-if BUILD_REVERSE
-  SU2SOLVER_LIB = ${abs_top_builddir}/SU2_CFD/obj/libSU2Core_AD.a \
-    ${abs_top_builddir}/Common/lib/libSU2_AD.a
-  PYLIB = pysu2ad.py
-  SOLIB = _pysu2ad.so
-endif
-
-# Set the linking flags to use
-pySU2_LD_FLAGS = ${SU2SOLVER_LIB} @su2_externals_LIBS@ ${PY_LIB}
-
-# Set the command line flags to use for compilation
-pySU2_CC_FLAGS = ${CPPFLAGS} ${EXTRA_CC_FLAGS} @su2_externals_INCLUDES@ ${pySU2_INCLUDE}
-
-SO_LINK_FLAGS= -fPIC -shared
-
-# Default rule for creating the _wrap.cxx file from the .i file
-${SWIG_WRAP_REAL}.cxx: ${SU2SOLVER_LIB} ${SWIG_SRC}
-	${SWIG} ${CPPFLAGS} -Wall ${SWIG_INCLUDE} -outdir ./ -o ${SWIG_WRAP_REAL}.cxx -c++ -python ${SWIG_SRC}
-
-#Default rule for compiling the .o files
-${SWIG_WRAP_REAL}.o: ${SWIG_WRAP_REAL}.cxx
-	${CXX} ${pySU2_CC_FLAGS} ${PY_INCLUDE} -c ${SWIG_WRAP_REAL}.cxx -o ${SWIG_WRAP_REAL}.o
-
-#_%.${SO_EXT}: %.o
-#	${CXX} ${SO_LINK_FLAGS} -o _$*.${SO_EXT} $*_wrap.o ${pySU2_LD_FLAGS}
-
-${SWIG_SO_REAL}: ${SWIG_WRAP_REAL}.o
-	${CXX} ${SO_LINK_FLAGS} -o ${SWIG_SO_REAL} ${SWIG_WRAP_REAL}.o ${pySU2_LD_FLAGS}
-
-.SECONDARY:
-
-clean:
-	rm -f ${CURRENT_DIR}/*.cxx
-	rm -f ${CURRENT_DIR}/*.${SO_EXT}
-	rm -f ${CURRENT_DIR}/*.o
-	rm -f ${CURRENT_DIR}/*.h
-	rm -f ${CURRENT_DIR}/*.py
-
-install: all
-	${INSTALL} ${PYLIB} ${bindir}
-	${INSTALL} ${SOLIB} ${bindir}
diff --git a/SU2_SOL/bin/.gitignore b/SU2_SOL/bin/.gitignore
deleted file mode 100644
index fe891329eff..00000000000
--- a/SU2_SOL/bin/.gitignore
+++ /dev/null
@@ -1,2 +0,0 @@
-# Do not track compiled execuatables
-SU2*
diff --git a/SU2_SOL/obj/Makefile.am b/SU2_SOL/obj/Makefile.am
deleted file mode 100644
index 980499b9a53..00000000000
--- a/SU2_SOL/obj/Makefile.am
+++ /dev/null
@@ -1,52 +0,0 @@
-################################################################################
-#
-# \file Makefile.am
-# \brief Makefile for SU2_SOL
-# \author M. Colonno, T. Economon, F. Palacios
-# \version 7.5.1 "Blackbird"
-#
-# SU2 Project Website: https://su2code.github.io
-#
-# The SU2 Project is maintained by the SU2 Foundation
-# (http://su2foundation.org)
-#
-# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
-#
-# SU2 is free software; you can redistribute it and/or
-# modify it under the terms of the GNU Lesser General Public
-# License as published by the Free Software Foundation; either
-# version 2.1 of the License, or (at your option) any later version.
-#
-# SU2 is distributed in the hope that it will be useful,
-# but WITHOUT ANY WARRANTY; without even the implied warranty of
-# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
-# Lesser General Public License for more details.
-#
-# You should have received a copy of the GNU Lesser General Public
-# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
-#
-################################################################################
-
-AUTOMAKE_OPTIONS = subdir-objects
-ACLOCAL_AMFLAGS = ${ACLOCAL_FLAGS}
-
-bin_PROGRAMS = ../bin/SU2_SOL
-
-___bin_SU2_SOL_SOURCES = \
-  ../include/SU2_SOL.hpp \
-  ../src/SU2_SOL.cpp
-
-___bin_SU2_SOL_CXXFLAGS =
-___bin_SU2_SOL_LDADD = \
-  ../../SU2_CFD/obj/libSU2Core.a \
-  ../../Common/lib/libSU2.a
-
-# always link to built dependencies from ./externals
-___bin_SU2_SOL_CXXFLAGS += @su2_externals_INCLUDES@
-___bin_SU2_SOL_LDADD += @su2_externals_LIBS@
-___bin_SU2_SOL_LDADD += @su2_externals_LIBPTHREAD@
-
-# if BUILD_MUTATIONPP
-___bin_SU2_SOL_CXXFLAGS += @MUTATIONPP_CXX@
-___bin_SU2_SOL_LDADD += @MUTATIONPP_LD@
-# endif
diff --git a/externals/Makefile.am b/externals/Makefile.am
deleted file mode 100644
index 24bfed9615f..00000000000
--- a/externals/Makefile.am
+++ /dev/null
@@ -1,46 +0,0 @@
-################################################################################
-#
-# \file Makefile.am
-# \brief Makefile for external libraries
-# \author B. Kirk, T. Economon, F. Palacios
-# \version 7.5.1 "Blackbird"
-#
-# SU2 Project Website: https://su2code.github.io
-#
-# The SU2 Project is maintained by the SU2 Foundation
-# (http://su2foundation.org)
-#
-# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
-#
-# SU2 is free software; you can redistribute it and/or
-# modify it under the terms of the GNU Lesser General Public
-# License as published by the Free Software Foundation; either
-# version 2.1 of the License, or (at your option) any later version.
-#
-# SU2 is distributed in the hope that it will be useful,
-# but WITHOUT ANY WARRANTY; without even the implied warranty of
-# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
-# Lesser General Public License for more details.
-#
-# You should have received a copy of the GNU Lesser General Public
-# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
-#
-################################################################################
-
-# Build any requested libraries from the provided source
-SUBDIRS =
-
-if BUILD_TECIO
-  SUBDIRS += tecio
-endif
-
-if BUILD_METIS
-  SUBDIRS += metis
-if BUILD_PARMETIS
-  SUBDIRS += parmetis
-endif
-endif
-
-if BUILD_CGNS
-  SUBDIRS += cgns
-endif
diff --git a/externals/cgns/Makefile.am b/externals/cgns/Makefile.am
deleted file mode 100644
index 6fb3ef2bd63..00000000000
--- a/externals/cgns/Makefile.am
+++ /dev/null
@@ -1,34 +0,0 @@
-pkg_cppflags = @SU2_CGNS_CPPFLAGS@
-pkg_cppflags += -I$(srcdir) -I$(srcdir)/adf
-pkg_sources  = \
-    cgnslib.h \
-    cgns_header.h \
-    cgns_io.h \
-    cgnstypes.h \
-    cgnsconfig.h \
-    fortran_macros.h \
-    adf/ADF.h \
-    adf/ADF_fbind.h \
-    adf/ADF_internals.h \
-    cgns_error.c \
-    cgns_internals.c \
-    cgns_io.c \
-    cgnslib.c \
-    adf/ADF_interface.c \
-    adf/ADF_internals.c
-
-
-######################################################################
-AUTOMAKE_OPTIONS = subdir-objects
-
-AM_CPPFLAGS  = $(pkg_cppflags) -fPIC # any defined package-specific include paths
-AM_CFLAGS    =
-AM_CXXFLAGS  =
-AM_LDFLAGS   =
-
-noinst_LIBRARIES = libcgns.a
-
-libcgns_a_SOURCES  = $(pkg_sources)
-libcgns_a_CPPFLAGS = $(CPPFLAGS_DBG) $(AM_CPPFLAGS)
-libcgns_a_CXXFLAGS = $(CXXFLAGS_DBG)
-libcgns_a_CFLAGS   = $(CFLAGS_DBG)
diff --git a/externals/metis/Makefile.am b/externals/metis/Makefile.am
deleted file mode 100644
index 966479e188a..00000000000
--- a/externals/metis/Makefile.am
+++ /dev/null
@@ -1,109 +0,0 @@
-pkg_cppflags  = @SU2_METIS_CPPFLAGS@
-pkg_cppflags += -I$(srcdir)/include  -I$(srcdir)/GKlib -I$(srcdir)/libmetis
-pkg_sources = \
-	include/metis.h \
-	GKlib/b64.c \
-	GKlib/blas.c \
-	GKlib/csr.c \
-	GKlib/error.c \
-	GKlib/evaluate.c \
-	GKlib/fkvkselect.c \
-	GKlib/fs.c \
-	GKlib/getopt.c \
-	GKlib/gk_arch.h \
-	GKlib/gk_defs.h \
-	GKlib/gk_externs.h \
-	GKlib/gk_getopt.h \
-	GKlib/gk_macros.h \
-	GKlib/gk_mkblas.h \
-	GKlib/gk_mkmemory.h \
-	GKlib/gk_mkpqueue.h \
-	GKlib/gk_mkpqueue2.h \
-	GKlib/gk_mkrandom.h \
-	GKlib/gk_mksort.h \
-	GKlib/gk_mkutils.h \
-	GKlib/gk_proto.h \
-	GKlib/gk_struct.h \
-	GKlib/gk_types.h \
-	GKlib/GKlib.h \
-	GKlib/gkregex.c \
-	GKlib/gkregex.h \
-	GKlib/graph.c \
-	GKlib/htable.c \
-	GKlib/io.c \
-	GKlib/itemsets.c \
-	GKlib/mcore.c \
-	GKlib/memory.c \
-	GKlib/ms_inttypes.h \
-	GKlib/ms_stat.h \
-	GKlib/ms_stdint.h \
-	GKlib/omp.c \
-	GKlib/pdb.c \
-	GKlib/pqueue.c \
-	GKlib/random.c \
-	GKlib/rw.c \
-	GKlib/seq.c \
-	GKlib/sort.c \
-	GKlib/string.c \
-	GKlib/timers.c \
-	GKlib/tokenizer.c \
-	GKlib/util.c \
-	libmetis/auxapi.c \
-	libmetis/balance.c \
-	libmetis/bucketsort.c \
-	libmetis/checkgraph.c \
-	libmetis/coarsen.c \
-	libmetis/compress.c \
-	libmetis/contig.c \
-	libmetis/debug.c \
-	libmetis/defs.h \
-	libmetis/fm.c \
-	libmetis/fortran.c \
-	libmetis/frename.c \
-	libmetis/gklib.c \
-	libmetis/gklib_defs.h \
-	libmetis/gklib_rename.h \
-	libmetis/graph.c \
-	libmetis/initpart.c \
-	libmetis/kmetis.c \
-	libmetis/kwayfm.c \
-	libmetis/kwayrefine.c \
-	libmetis/macros.h \
-	libmetis/mcutil.c \
-	libmetis/mesh.c \
-	libmetis/meshpart.c \
-	libmetis/metislib.h \
-	libmetis/minconn.c \
-	libmetis/mincover.c \
-	libmetis/mmd.c \
-	libmetis/ometis.c \
-	libmetis/options.c \
-	libmetis/parmetis.c \
-	libmetis/pmetis.c \
-	libmetis/proto.h \
-	libmetis/refine.c \
-	libmetis/rename.h \
-	libmetis/separator.c \
-	libmetis/sfm.c \
-	libmetis/srefine.c \
-	libmetis/stat.c \
-	libmetis/stdheaders.h \
-	libmetis/struct.h \
-	libmetis/timing.c \
-	libmetis/util.c \
-	libmetis/wspace.c
-
-######################################################################
-AUTOMAKE_OPTIONS = subdir-objects
-
-AM_CPPFLAGS  = $(pkg_cppflags) -fPIC # any defined package-specific include paths
-AM_CFLAGS    =
-AM_CXXFLAGS  =
-AM_LDFLAGS   =
-
-noinst_LIBRARIES = libmetis.a
-
-libmetis_a_SOURCES  = $(pkg_sources)
-libmetis_a_CPPFLAGS = $(CPPFLAGS_DBG) $(AM_CPPFLAGS)
-libmetis_a_CXXFLAGS = $(CXXFLAGS_DBG)
-libmetis_a_CFLAGS   = $(CFLAGS_DBG)
diff --git a/externals/parmetis/Makefile.am b/externals/parmetis/Makefile.am
deleted file mode 100644
index 820d09fd3ea..00000000000
--- a/externals/parmetis/Makefile.am
+++ /dev/null
@@ -1,68 +0,0 @@
-# include paths - note that parmetis needs metis!
-pkg_cppflags  = @SU2_METIS_CPPFLAGS@ @SU2_PARMETIS_CPPFLAGS@
-pkg_cppflags += -I$(top_srcdir)/externals/metis/GKlib \
-                -I$(top_srcdir)/externals/metis/include \
-                -I$(srcdir)/include \
-                -I$(srcdir)/libparmetis
-pkg_sources   = \
-	include/parmetis.h \
-	libparmetis/akwayfm.c \
-	libparmetis/ametis.c \
-	libparmetis/balancemylink.c \
-	libparmetis/comm.c \
-	libparmetis/csrmatch.c \
-	libparmetis/ctrl.c \
-	libparmetis/debug.c \
-	libparmetis/defs.h \
-	libparmetis/diffutil.c \
-	libparmetis/frename.c \
-	libparmetis/gkmetis.c \
-	libparmetis/gkmpi.c \
-	libparmetis/graph.c \
-	libparmetis/initbalance.c \
-	libparmetis/initmsection.c \
-	libparmetis/initpart.c \
-	libparmetis/kmetis.c \
-	libparmetis/kwayrefine.c \
-	libparmetis/macros.h \
-	libparmetis/match.c \
-	libparmetis/mdiffusion.c \
-	libparmetis/mesh.c \
-	libparmetis/mmetis.c \
-	libparmetis/move.c \
-	libparmetis/msetup.c \
-	libparmetis/node_refine.c \
-	libparmetis/ometis.c \
-	libparmetis/parmetislib.h \
-	libparmetis/proto.h \
-	libparmetis/pspases.c \
-	libparmetis/redomylink.c \
-	libparmetis/remap.c \
-	libparmetis/rename.h \
-	libparmetis/renumber.c \
-	libparmetis/rmetis.c \
-	libparmetis/selectq.c \
-	libparmetis/serial.c \
-	libparmetis/stat.c \
-	libparmetis/struct.h \
-	libparmetis/timer.c \
-	libparmetis/util.c \
-	libparmetis/wave.c \
-	libparmetis/weird.c \
-	libparmetis/wspace.c \
-	libparmetis/xyzpart.c
-
-######################################################################
-AUTOMAKE_OPTIONS = subdir-objects
-
-AM_CPPFLAGS  = $(pkg_cppflags) -fPIC # any defined package-specific include paths
-AM_CFLAGS    =
-AM_CXXFLAGS  =
-AM_LDFLAGS   =
-
-noinst_LIBRARIES = libparmetis.a
-
-libparmetis_a_SOURCES  = $(pkg_sources)
-libparmetis_a_CPPFLAGS = $(CPPFLAGS_DBG) $(AM_CPPFLAGS)
-libparmetis_a_CXXFLAGS = $(CXXFLAGS_DBG)
-libparmetis_a_CFLAGS   = $(CFLAGS_DBG)
diff --git a/externals/tecio/Makefile.am b/externals/tecio/Makefile.am
deleted file mode 100644
index fbea331dd6c..00000000000
--- a/externals/tecio/Makefile.am
+++ /dev/null
@@ -1,40 +0,0 @@
-################################################################################
-#
-# \file Makefile.am
-# \brief Makefile for external libraries
-# \author B. Kirk, T. Economon, F. Palacios
-# \version 7.5.1 "Blackbird"
-#
-# SU2 Project Website: https://su2code.github.io
-#
-# The SU2 Project is maintained by the SU2 Foundation
-# (http://su2foundation.org)
-#
-# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
-#
-# SU2 is free software; you can redistribute it and/or
-# modify it under the terms of the GNU Lesser General Public
-# License as published by the Free Software Foundation; either
-# version 2.1 of the License, or (at your option) any later version.
-#
-# SU2 is distributed in the hope that it will be useful,
-# but WITHOUT ANY WARRANTY; without even the implied warranty of
-# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
-# Lesser General Public License for more details.
-#
-# You should have received a copy of the GNU Lesser General Public
-# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
-#
-################################################################################
-
-# Build any requested libraries from the provided source
-SUBDIRS =
-
-if BUILD_TECIO
-if BUILD_TECIOMPI
-  SUBDIRS += teciompisrc
-else
-  SUBDIRS += teciosrc
-endif
-endif
-
diff --git a/legacy/Makefile.am b/legacy/Makefile.am
deleted file mode 100644
index f99a9542973..00000000000
--- a/legacy/Makefile.am
+++ /dev/null
@@ -1,64 +0,0 @@
-################################################################################
-#
-# \file Makefile.am
-# \brief Global makefile for the SU2 project
-# \author M. Colonno, T. Economon, F. Palacios
-# \version 7.5.1 "Blackbird"
-#
-# SU2 Project Website: https://su2code.github.io
-#
-# The SU2 Project is maintained by the SU2 Foundation
-# (http://su2foundation.org)
-#
-# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
-#
-# SU2 is free software; you can redistribute it and/or
-# modify it under the terms of the GNU Lesser General Public
-# License as published by the Free Software Foundation; either
-# version 2.1 of the License, or (at your option) any later version.
-#
-# SU2 is distributed in the hope that it will be useful,
-# but WITHOUT ANY WARRANTY; without even the implied warranty of
-# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
-# Lesser General Public License for more details.
-#
-# You should have received a copy of the GNU Lesser General Public
-# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
-#
-################################################################################
-
-AUTOMAKE_OPTIONS = subdir-objects
-ACLOCAL_AMFLAGS = ${ACLOCAL_FLAGS} -I m4
-
-# build third-party optional dependencies first
-SUBDIRS = externals
-
-SUBDIRS += Common/lib
-
-if BUILD_PY
-SUBDIRS += SU2_PY
-endif
-
-if BUILD_CFD
-SUBDIRS +=SU2_CFD/obj
-endif
-
-if BUILD_DOT
-SUBDIRS +=SU2_DOT/obj
-endif
-
-if BUILD_DEF
-SUBDIRS +=SU2_DEF/obj
-endif
-
-if BUILD_SOL
-SUBDIRS +=SU2_SOL/obj
-endif
-
-if BUILD_GEO
-SUBDIRS +=SU2_GEO/obj
-endif
-
-if BUILD_PY_WRAPPER
-SUBDIRS += SU2_PY/pySU2
-endif
diff --git a/legacy/bootstrap b/legacy/bootstrap
deleted file mode 100755
index 982f4dd5656..00000000000
--- a/legacy/bootstrap
+++ /dev/null
@@ -1,151 +0,0 @@
-#! /bin/bash
-#
-# bootstrap: Utility to easy autoconf/automake toolchain setup
-#            Forcing specific tool versions.
-
-dir=`echo "$0" | sed 's,[^/]*$,,'`
-test "x${dir}" = "x" && dir='.'
-
-if (test "x`cd "${dir}" 2>/dev/null && pwd`" != "x`pwd`"); then
-    echo "This script must be executed directly from the source directory."
-    exit 1
-fi
-
-
-###############################################################################
-function check_autotool_prerequisites ()
-{
-    # prerequisite versions
-    automake_major=1
-    automake_minor=15
-
-    autoconf_major=2
-    autoconf_minor=69
-
-    build_autotools=0
-
-
-    autoreconf=`which autoreconf 2>/dev/null`
-    if (test "x$autoreconf" != "x"); then
-	if (test -x $autoreconf); then
-	    autoconf_version=`$autoreconf --version | grep " $autoconf_major\." | cut -d"." -f2`
-	    if (test $autoconf_version -lt $autoconf_minor); then
-		echo "Autoconf Version $autoconf_major.$autoconf_version too old, building a new one..."
-		build_autotools=1
-	    else
-		version_id=`$autoreconf --version 2>&1 | grep "(GNU Autoconf)"`
-		echo "Using autoconf ($version_id)"
-	    fi
-	else
-	    build_autotools=1
-	fi
-    else
-	build_autotools=1
-    fi
-
-
-    libtool=`which glibtool 2>/dev/null`
-    if (test "x$libtool" = "x"); then
-	libtool=`which libtool 2>/dev/null`
-    fi
-    if (test "x$libtool" != "x"); then
-	if (test -x $libtool); then
-	    libtool_version=`$libtool --version 2>&1 | grep "(GNU libtool)"`
-
-	    case "$libtool_version" in
-		*2.4* | *2.2*)
-		    echo "Using libtool ($libtool_version)"
-		    ;;
-		*)
-	            echo "Indaequate Libtool ($libtool_version), building a new one..."
-		    build_autotools=1
-	    esac
-	else
-	    build_autotools=1
-	fi
-    else
-	build_autotools=1
-    fi
-
-
-    automake=`which automake 2>/dev/null`
-    if (test "x$automake" != "x"); then
-	if (test -x $automake); then
-	    automake_version=`$automake --version | grep " $automake_major\." | cut -d"." -f2`
-	    if (test $automake_version -lt $automake_minor); then
-		echo "Automake Version $automake_major.$automake_version too old, building a new one..."
-		build_autotools=1
-	    else
-		version_id=`$automake --version 2>&1 | grep "(GNU automake)"`
-		echo "Using automake ($version_id)"
-	    fi
-	else
-	    build_autotools=1
-	fi
-    else
-	build_autotools=1
-    fi
-
-
-    return $build_autotools
-}
-###############################################################################
-
-
-
-check_autotool_prerequisites
-build_autotools=$?
-
-###############################################################################
-for arg in $@; do
-    if (test "x$arg" = "x--build-autotools"); then
-	echo "building autotools at user request"
-	build_autotools=1
-    fi
-done
-
-
-###############################################################################
-if (test "x$build_autotools" = "x1"); then
-    # when there is no autoreconf try to actually build one.
-    echo "Inadequate autotools in your path, I'll build new ones..."
-
-    top_srcdir=`pwd`
-    autotools_distdir=$top_srcdir/externals/autotools
-
-
-    if (test -d $autotools_distdir); then
-    # set the path to use the new tools as they are installed.
-    # for example, the new autoconf is needed to build automake.
-	PATH=$autotools_distdir/bin:$PATH
-	for tool in autoconf-2.69 automake-1.15.1 libtool-2.4.2 ; do
-	    cd $autotools_distdir
-	    echo "  building $tool in $autotools_distdir"
-	    tar zxf $tool.tar.gz
-	    cd $tool && ./configure --prefix=$autotools_distdir >/dev/null && make install >/dev/null
-	    cd .. && rm -rf $tool
-	done
-
-	cd $top_srcdir
-
-	if (test -x $autotools_distdir/bin/autoreconf -a -x $autotools_distdir/bin/automake -a -x $autotools_distdir/bin/libtool); then
-	    echo " "
-	    echo " --> successfully installed autoreconf in $autotools_distdir/bin - please update your PATH and try again!"
-	    echo " "
-	    PATH=$autotools_distdir/bin:$PATH ./$0
-	    exit 0
-	fi
-    fi
-fi
-###############################################################################
-
-
-
-autoreconf=`which autoreconf 2>/dev/null`
-# prefer autoreconf when it is available
-if (test "x$autoreconf" != "x"); then
-    if (test -x $autoreconf); then
-	$autoreconf -iv --force
-	exit 0
-    fi
-fi
diff --git a/legacy/configure.ac b/legacy/configure.ac
deleted file mode 100644
index 8ab779eb8dd..00000000000
--- a/legacy/configure.ac
+++ /dev/null
@@ -1,410 +0,0 @@
-################################################################################
-#
-# \file configure.ac
-# \brief Main file for configuring the autoconf/automake build process
-# \author M. Colonno, T. Economon, F. Palacios, B. Kirk
-# \version 7.5.1 "Blackbird"
-#
-# SU2 Project Website: https://su2code.github.io
-#
-# The SU2 Project is maintained by the SU2 Foundation
-# (http://su2foundation.org)
-#
-# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
-#
-# SU2 is free software; you can redistribute it and/or
-# modify it under the terms of the GNU Lesser General Public
-# License as published by the Free Software Foundation; either
-# version 2.1 of the License, or (at your option) any later version.
-#
-# SU2 is distributed in the hope that it will be useful,
-# but WITHOUT ANY WARRANTY; without even the implied warranty of
-# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
-# Lesser General Public License for more details.
-#
-# You should have received a copy of the GNU Lesser General Public
-# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
-#
-################################################################################
-#
-# Major Changes/Contributions:
-# METIS & TECIO integration added by Ben Kirk, 3/24/2014
-# LAPACK connection added by Teus van der Stelt, 11/13/2014
-# ParMETIS integration added by Ben Kirk & Thomas D. Economon, 2/3/2015
-# CGNS integration added by Thomas D. Economon, 8/17/2016
-#
-##########################
-
-AC_INIT([SU2], [6.2.0], [su2code-dev@lists.stanford.edu],
-        [SU2], [https://su2code.github.io])
-AC_PREREQ([2.59])
-AC_CONFIG_MACRO_DIR([m4])
-AC_CANONICAL_TARGET
-AM_INIT_AUTOMAKE([foreign])
-m4_ifdef([AM_SILENT_RULES], [AM_SILENT_RULES(yes)])
-
-# AC_CONFIG_HEADERS([config.h])
-SU2_SET_COMPILERS
-AM_PROG_CC_C_O
-AC_PROG_RANLIB
-AC_PROG_MKDIR_P
-AC_PROG_CXX
-
-# Python configuration
-AM_PATH_PYTHON
-AC_ARG_VAR([PYTHON_INCLUDE], [Include flags for python, bypassing python-config])
-AC_ARG_VAR([PYTHON_CONFIG], [Path to python-config])
-AC_ARG_VAR([PYTHON_LIB], [Python lib flags])
-AC_ARG_VAR([PYTHON_EXEC_PREFIX], [Python exec-prefix])
-AS_IF([test -z "$PYTHON_INCLUDE"], [
-  AS_IF([test -z "$PYTHON_CONFIG"], [
-    AC_PATH_PROGS([PYTHON_CONFIG],
-                  [python$PYTHON_VERSION-config python-config],
-                  [no],
-                  [`dirname $PYTHON`])
-    AS_IF([test "$PYTHON_CONFIG" = no], [AC_MSG_ERROR([cannot find python-config for $PYTHON.])])
-  ])
-  AC_MSG_CHECKING([python include flags])
-  PYTHON_INCLUDE=`$PYTHON_CONFIG --includes`
-  PYTHON_LIB=`$PYTHON_CONFIG --libs --embed`
-  PYTHON_EXEC_PREFIX=`$PYTHON_CONFIG --exec-prefix`
-  AC_MSG_RESULT([$PYTHON_INCLUDE])
-])
-
-#PKG_PROG_PKG_CONFIG
-
-# --------------------------------------------------------------
-# Check for important type sizes
-# --------------------------------------------------------------
-
-AC_CHECK_SIZEOF(short int)
-AC_CHECK_SIZEOF(int)
-AC_CHECK_SIZEOF(unsigned int)
-AC_CHECK_SIZEOF(long int)
-AC_CHECK_SIZEOF(float)
-AC_CHECK_SIZEOF(double)
-AC_CHECK_SIZEOF(void *)
-
-# optional bindings for external packages
-
-AC_ARG_WITH(Mutationpp-lib,
-    AS_HELP_STRING([--with-Mutationpp-lib[=ARG]], [Mutation++ library directory, ARG = path to libmutation++.a]),
-  [with_Mutationpp_lib=$withval], [with_Mutationpp_lib="no"])
-AC_ARG_WITH(Mutationpp-include,
-    AS_HELP_STRING([--with-Mutationpp-include[=ARG]], [Mutation++ include directory, ARG = path to mutation++.h]),
-  [with_Mutationpp_include=$withval], [with_Mutationpp_include="no"])
-
-# Check for disabling of SU2 modules
-
-AC_ARG_ENABLE(CFD,
-    AS_HELP_STRING([--disable-CFD], [build the SU2_CFD executable (default = yes)]),
-  [build_CFD=$enableval], [build_CFD="yes"])
-AC_ARG_ENABLE(DOT,
-   	AS_HELP_STRING([--disable-DOT], [build the SU2_DOT executable (default = yes)]),
-	[build_DOT=$enableval], [build_DOT="yes"])
-AC_ARG_ENABLE(DEF,
-    AS_HELP_STRING([--disable-DEF], [build the SU2_DEF executable (default = yes)]),
-  [build_DEF=$enableval], [build_DEF="yes"])
-AC_ARG_ENABLE(SOL,
-    AS_HELP_STRING([--disable-SOL], [build the SU2_SOL executable (default = yes)]),
-  [build_SOL=$enableval], [build_SOL="yes"])
-AC_ARG_ENABLE(GEO,
-    AS_HELP_STRING([--disable-GEO], [build the SU2_GEO executable (default = yes)]),
-  [build_GEO=$enableval], [build_GEO="yes"])
-AC_ARG_ENABLE(PY_WRAPPER,
-    AS_HELP_STRING([--enable-PY_WRAPPER], [wrap the SU2 code with Python (default = no)]),
-  [build_PY_WRAPPER="yes"], [build_PY_WRAPPER="no"])
-
-# Check for data types
-
-AC_ARG_ENABLE(normal,
-    AS_HELP_STRING([--disable-normal], [build executables with normal datatype (default = yes)]),
-    [build_NORMAL=$enableval], [build_NORMAL="yes"])
-
-# Check for the old MPI option so that we can throw an error
-
-AC_ARG_WITH(MPI,
-AS_HELP_STRING(),
-        [with_MPI=$withval], [with_MPI="no"])
-if test "$with_MPI" != "no"
-then
-    AC_MSG_ERROR([unsupported option --with-MPI. For MPI support, use --enable-mpi and specify your MPI implementations with --with-cc=/path/to/mpicc and --with-cxx=/path/to/mpicxx in your configure call.])
-fi
-
-# --------------------------------------------------------------
-# Build up contributed packages that we will build from source
-# --------------------------------------------------------------
-
-su2_externals_INCLUDES=""
-su2_externals_LIBS=""
-su2_externals_LIBPTHREAD=""
-
-# Tecplot
-CONFIGURE_TECIO
-if (test $enabletecio = yes); then
-  su2_externals_INCLUDES="-DHAVE_TECIO $TECIO_INCLUDE $su2_externals_INCLUDES"
-  if ( test x$have_MPI = xyes ); then
-    su2_externals_INCLUDES="-DTECIOMPI $su2_externals_INCLUDES"
-  fi
-  su2_externals_LIBS="$TECIO_LIB $su2_externals_LIBS"
-  # Check if boost directory exists, otherwise extract the sources
-  if ( ! test -d "$srcdir/externals/tecio/boost" ); then
-    AC_MSG_RESULT([Extracting boost source ...])
-    if ( ! tar -xzf $srcdir/externals/tecio/boost.tar.gz -C $srcdir/externals/tecio/ ); then
-	AC_MSG_ERROR([Extraction of boost sources to $srcdir/externals/tecio/boost using 'tar' failed ...])
-    fi
-  fi
-   # Attempt to get pthread to work
-   AC_CHECK_LIB(pthread,pthread_create,LIBPTHREAD="-lpthread")
-  su2_externals_LIBPTHREAD="$LIBPTHREAD"
-else
-  su2_externals_INCLUDES="$su2_externals_INCLUDES"
-fi
-
-AM_CONDITIONAL(BUILD_TECIO, test x$enabletecio = xyes)
-AM_CONDITIONAL(BUILD_TECIOMPI, test x$enabletecio = xyes -a x$have_MPI = xyes)
-AC_CONFIG_FILES([externals/tecio/Makefile])
-AC_CONFIG_FILES([externals/tecio/teciosrc/Makefile])
-AC_CONFIG_FILES([externals/tecio/teciompisrc/Makefile])
-
-# Metis
-CONFIGURE_METIS
-if (test $enablemetis = yes); then
-  su2_externals_INCLUDES="-DHAVE_METIS $METIS_INCLUDE $su2_externals_INCLUDES"
-  su2_externals_LIBS="$METIS_LIB $su2_externals_LIBS"
-else
-  su2_externals_INCLUDES="$su2_externals_INCLUDES"
-fi
-AM_CONDITIONAL(BUILD_METIS, test x$enablemetis = xyes)
-AC_CONFIG_FILES([externals/metis/Makefile])
-
-# Parmetis
-CONFIGURE_PARMETIS
-if (test $enableparmetis = yes); then
-  su2_externals_INCLUDES="-DHAVE_PARMETIS $PARMETIS_INCLUDE $su2_externals_INCLUDES"
-  su2_externals_LIBS="$PARMETIS_LIB $su2_externals_LIBS"
-else
-  su2_externals_INCLUDES="$su2_externals_INCLUDES"
-fi
-AM_CONDITIONAL(BUILD_PARMETIS, test x$enableparmetis = xyes)
-AC_CONFIG_FILES([externals/parmetis/Makefile])
-
-# CGNS
-CONFIGURE_CGNS
-if (test $enablecgns = yes); then
-  su2_externals_INCLUDES="-DHAVE_CGNS $CGNS_INCLUDE $su2_externals_INCLUDES"
-  su2_externals_LIBS="$CGNS_LIB $su2_externals_LIBS"
-else
-  su2_externals_INCLUDES="$su2_externals_INCLUDES"
-fi
-AM_CONDITIONAL(BUILD_CGNS, test x$enablecgns = xyes)
-AC_CONFIG_FILES([externals/cgns/Makefile])
-
-AC_SUBST([su2_externals_INCLUDES])
-AC_SUBST([su2_externals_LIBS])
-AC_SUBST([su2_externals_LIBPTHREAD])
-
-su2_externals_INCLUDES="-I\$(top_srcdir)/externals/CLI11 $su2_externals_INCLUDES"
-
-##########################
-
-# check for lib
-Mutationpplib=libmutation++.a
-Mutationppheader=mutation++.h
-have_MPP="no"
-
-if test "$with_Mutationpp_lib" != "no"
-then
-  	AC_CHECK_FILE([$with_Mutationpp_lib/$Mutationpplib],[have_MPP="yes"],[have_MPP="no"])
-	if test "$have_MPP" == "no"
-	then
-		AC_MSG_ERROR([Mutation++ requested but library file not found.])
-	fi
-fi
-
-# check for header
-if test "$have_MPP" != "no"
-then
-	if test "$with_Mutationpp_include" != "no"
-	then
-		AC_CHECK_FILE([$with_Mutationpp_include/$Mutationppheader],[have_MPP='yes'],[have_MPP='no'])
-		if test "$have_MPP" == "no"
-		then
-			AC_MSG_ERROR([Mutation++ requested but header file not found.])
-		fi
-	else
-		have_MPP="no"
-	fi
-fi
-
-if test "$have_MPP" != "no"
-then
-  	AM_CONDITIONAL(BUILD_MUTATIONPP,true,test x$enablempp = xyes -a x$have_MPP = xyes)
-	MUTATIONPP_CXX="-DHAVE_MPP -I"$with_Mutationpp_include""
-	MUTATIONPP_LD="$with_Mutationpp_lib"/$Mutationpplib
-else
-	AM_CONDITIONAL(BUILD_MUTATIONPP,false)
-	MUTATIONPP_CXX=
-	MUTATION_LD=
-fi
-AC_SUBST([MUTATIONPP_CXX])
-AC_SUBST([MUTATIONPP_LD])
-
-##########################
-
-# Check if MKL is available, enable if 2019.0 or newer.
-
-have_MKL="no"
-if test "${MKLROOT+set}" = set; then
-  FOUND_MKL_VERSION=$(grep -F "INTEL_MKL_VERSION" ${MKLROOT}/include/mkl_version.h | tr -dc '0-9')
-  REQUIRED_MKL_VERSION=20190000
-  if [[ "$FOUND_MKL_VERSION" -ge "$REQUIRED_MKL_VERSION" ]]; then
-    CPPFLAGS="-DHAVE_MKL -DMKL_DIRECT_CALL_SEQ $CPPFLAGS"
-    CXXFLAGS="-I${MKLROOT}/include $CXXFLAGS"
-    LIBS="-Wl,--start-group ${MKLROOT}/lib/intel64/libmkl_intel_lp64.a ${MKLROOT}/lib/intel64/libmkl_sequential.a ${MKLROOT}/lib/intel64/libmkl_core.a -Wl,--end-group -lpthread -lm -ldl $LIBS"
-    have_MKL="yes"
-  fi
-fi
-
-###########################
-# Determine what versions of the code to build
-
-build_PY=yes
-
-# direct differentation type
-build_DIRECTDIFF=no
-DIRECTDIFF_CXX=
-DIRECTDIFF_LIBS=
-# reverse mode type
-build_REVERSE=no
-REVERSE_CXX=
-FORWARD_CXX=
-CONFIGURE_CODI
-
-AC_SUBST([DIRECTDIFF_CXX])
-AC_SUBST([DIRECTDIFF_LIBS])
-AC_SUBST([REVERSE_CXX])
-AC_SUBST([REVERSE_LIBS])
-# Set the variables
-AM_CONDITIONAL([BUILD_NORMAL], [test $build_NORMAL != "no"])
-AM_CONDITIONAL([BUILD_DIRECTDIFF], [test $build_DIRECTDIFF != "no"])
-AM_CONDITIONAL([BUILD_REVERSE], [test $build_REVERSE != "no"])
-if test $build_NORMAL == "no"
-then
-  build_DOT=no
-  build_DEF=no
-  build_SOL=no
-  build_GEO=no
-  build_PY=no
-fi
-
-if test $build_DIRECTDIFF == "yes"
-then
-  build_PY_WRAPPER=no
-fi
-
-if test $build_REVERSE == "yes"
-then
-  build_DOT=yes
-fi
-###########################
-
-AM_CONDITIONAL([BUILD_CFD],[test $build_CFD != "no"])
-AM_CONDITIONAL([BUILD_DOT],[test $build_DOT != "no"])
-AM_CONDITIONAL([BUILD_DEF],[test $build_DEF != "no"])
-AM_CONDITIONAL([BUILD_SOL],[test $build_SOL != "no"])
-AM_CONDITIONAL([BUILD_GEO],[test $build_GEO != "no"])
-AM_CONDITIONAL([BUILD_PY],[test $build_PY != "no"])
-AM_CONDITIONAL([BUILD_PY_WRAPPER], [test $build_PY_WRAPPER != "no"])
-
-###########################
-
-AC_OUTPUT(Makefile \
-        externals/Makefile \
-	      Common/lib/Makefile \
-	      SU2_CFD/obj/Makefile \
-	      SU2_DOT/obj/Makefile \
-	      SU2_DEF/obj/Makefile \
-	      SU2_SOL/obj/Makefile \
-	      SU2_GEO/obj/Makefile \
-	      SU2_PY/Makefile \
-	      SU2_PY/pySU2/Makefile)
-
-abs_srcdir=`(cd $srcdir && pwd)`
-abs_prefix=$prefix #`(cd $prefix && pwd)`
-
-
-AC_MSG_RESULT([
-
--------------------------------------------------------------------------
-|    ___ _   _ ___                                                      |
-|   / __| | | |_  )   Release 7.5.1 'Blackbird'                         |
-|   \\__ \\ |_| |/ /                                                      |
-|   |___/\\___//___|   Suite                                             |
-|                                                                       |
--------------------------------------------------------------------------
-| SU2 Project Website: https://su2code.github.io                        |
-|                                                                       |
-| The SU2 Project is maintained by the SU2 Foundation                   |
-| (http://su2foundation.org)                                            |
--------------------------------------------------------------------------
-| Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)                |
-|                                                                       |
-| SU2 is free software; you can redistribute it and/or                  |
-| modify it under the terms of the GNU Lesser General Public            |
-| License as published by the Free Software Foundation; either          |
-| version 2.1 of the License, or (at your option) any later version.    |
-|                                                                       |
-| SU2 is distributed in the hope that it will be useful,                |
-| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
-| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
-| Lesser General Public License for more details.                       |
-|                                                                       |
-| You should have received a copy of the GNU Lesser General Public      |
-| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
--------------------------------------------------------------------------
-
-Build Configuration Summary:
-
-    Source code location: ${abs_srcdir}
-    Install location: 	  ${abs_prefix}
-    Version:              ${VERSION}
-    C++ Compiler:         ${CXX}
-    C Compiler:           ${CC}
-    Preprocessor flags:   ${CPPFLAGS}
-    Compiler flags:       ${CXXFLAGS}
-    Linker flags:         ${LDFLAGS}
-    MPI support:          $have_MPI
-    Metis support:        $enablemetis
-    Parmetis support:     $enableparmetis
-    TecIO support:        $enabletecio
-    CGNS support:         $enablecgns
-    Mutation++ support:   $have_MPP
-    MKL support:          $have_MKL
-    Datatype support:
-        double            $build_NORMAL
-        codi_reverse      $build_CODI_REVERSE
-        codi_forward      $build_CODI_FORWARD
-
-    External includes:    $su2_externals_INCLUDES
-    External libs:        $su2_externals_LIBS
-    External libpthreads: $su2_externals_LIBPTHREAD
-
-    Build SU2_CFD:        $build_CFD
-    Build SU2_DOT:        $build_DOT
-    Build SU2_DEF:        $build_DEF
-    Build SU2_SOL:        $build_SOL
-    Build SU2_GEO:        $build_GEO
-    Build Py Wrapper:     $build_PY_WRAPPER
-
-Please be sure to add the [\$]SU2_HOME and [\$]SU2_RUN environment variables,
-and update your [\$]PATH (and [\$]PYTHONPATH if applicable) with [\$]SU2_RUN.
-
-Based on the input to this configuration, add these lines to your .bashrc file:
-
-export SU2_RUN="${abs_prefix}/bin"
-export SU2_HOME="${abs_srcdir}"
-export PATH=[\$]PATH:[\$]SU2_RUN
-export PYTHONPATH=[\$]PYTHONPATH:[\$]SU2_RUN
-
-])
diff --git a/legacy/preconfigure.py b/legacy/preconfigure.py
deleted file mode 100755
index 58cdb3863d0..00000000000
--- a/legacy/preconfigure.py
+++ /dev/null
@@ -1,590 +0,0 @@
-#!/usr/bin/env python
-
-## \file configure.py
-#  \brief An extended configuration script.
-#  \author T. Albring
-#  \version 7.5.1 "Blackbird"
-#
-# SU2 Project Website: https://su2code.github.io
-#
-# The SU2 Project is maintained by the SU2 Foundation
-# (http://su2foundation.org)
-#
-# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
-#
-# SU2 is free software; you can redistribute it and/or
-# modify it under the terms of the GNU Lesser General Public
-# License as published by the Free Software Foundation; either
-# version 2.1 of the License, or (at your option) any later version.
-#
-# SU2 is distributed in the hope that it will be useful,
-# but WITHOUT ANY WARRANTY; without even the implied warranty of
-# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
-# Lesser General Public License for more details.
-#
-# You should have received a copy of the GNU Lesser General Public
-# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
-
-from __future__ import print_function, division, absolute_import
-from optparse import OptionParser, BadOptionError
-import sys,time, os, subprocess, os.path, glob, re, shutil, fileinput
-from subprocess import call
-
-# "Pass-through" option parsing -- an OptionParser that ignores
-# unknown options and lets them pile up in the leftover argument
-# list.  Useful to pass unknown arguments to the automake configure.
-class PassThroughOptionParser(OptionParser):
-
-    def _process_long_opt(self, rargs, values):
-        try:
-            OptionParser._process_long_opt(self, rargs, values)
-        except BadOptionError as err:
-            self.largs.append(err.opt_str)
-
-    def _process_short_opts(self, rargs, values):
-        try:
-            OptionParser._process_short_opts(self, rargs, values)
-        except BadOptionError as err:
-            self.largs.append(err.opt_str)
-
-def main():
-
-    # Command Line Options
-
-    usage = './preconfigure.py [options]' \
-            '\nNote: Options not listed below are passed to the automake configure.' \
-            '\n      Compiler flags must be set with \'export CFLAGS=...\' or \'export CXXFLAGS=...\' ' \
-            '\n      before calling this script.'
-
-    parser = PassThroughOptionParser(usage = usage)
-
-    parser.add_option("--enable-direct-diff", action="store_true",
-                      help="Enable direct differentiation mode support", dest="directdiff", default=False)
-    parser.add_option("--enable-autodiff", action="store_true",
-                      help="Enable Automatic Differentiation support", dest="ad_support", default=False)
-    parser.add_option("--with-ad", action="store",  type = "string",  help="AD Tool, CODI/ADOLC", default="CODI", dest="adtool")
-    parser.add_option("--enable-mpi", action="store_true",
-                      help="Enable mpi support", dest="mpi_enabled", default=False)
-    parser.add_option("--enable-PY_WRAPPER", action="store_true",
-                      help="Enable Python wrapper compilation", dest="py_wrapper_enabled", default=False)
-    parser.add_option("--disable-tecio", action="store_true",
-                      help="Disable Tecplot binary support", dest="tecio_disabled", default=False)
-    parser.add_option("--disable-normal", action="store_true",
-                      help="Disable normal mode support", dest="normal_mode", default=False)
-    parser.add_option("-c" , "--check", action="store_true",
-                      help="Check the source code for potential problems", dest="check", default=False)
-    parser.add_option("-r" , "--replace", action="store_true",
-                      help="Do a search and replace of necessary symbols. Creates back up of source files.", dest="replace", default=False)
-    parser.add_option("-d" , "--delete", action="store_true",
-                      help="Removes the back up files.", dest="remove", default=False)
-    parser.add_option("-v" , "--revert", action="store_true",
-                      help="Revert files to original state.", dest="revert", default=False)
-    parser.add_option("-u", "--update", action="store_true",
-                      help="Update and recompile submodules.", dest="update", default=False)
-    (options, args)=parser.parse_args()
-
-    options.adtool = options.adtool.upper()
-
-    if options.directdiff == False:
-        adtool_dd = ""
-    else:
-        adtool_dd = options.adtool
-    if options.ad_support == False:
-        adtool_da = ""
-    else:
-        adtool_da = options.adtool
-
-    conf_environ = os.environ
-
-    made_adolc = False
-    made_codi = False
-
-    header()
-
-    modes =  {'SU2_BASE'     : not options.normal_mode == True,
-              'SU2_DIRECTDIFF' : adtool_dd ,
-              'SU2_AD'    : adtool_da }
-
-    # Create a dictionary from the arguments
-    argument_dict = dict(zip(args[::2],args[1::2]))
-
-    # Set the default installation path (if not set with --prefix)
-    argument_dict['--prefix'] = argument_dict.get('--prefix', os.getcwd().rstrip())
-
-
-    if not options.check:
-        if any([modes["SU2_AD"] == 'CODI',  modes["SU2_DIRECTDIFF"] == 'CODI']):
-            conf_environ, made_codi  = init_codi(argument_dict,modes,options.mpi_enabled, options.update)
-
-        configure(argument_dict,
-                  conf_environ,
-                  options.mpi_enabled,
-                  options.py_wrapper_enabled,
-                  options.tecio_disabled,
-                  modes,
-                  made_adolc,
-                  made_codi)
-
-    if options.check:
-        prepare_source(options.replace, options.remove, options.revert)
-
-def prepare_source(replace = False, remove = False, revert = False):
-
-    # Directories containing the source code
-    print('Preparing source code ...')
-    dir_list = [ "Common",
-                 "SU2_CFD",
-                 "SU2_DEF",
-                 "SU2_DOT",
-                 "SU2_GEO",
-                 "SU2_SOL"]
-
-    file_list = ""
-
-    exclude_dic_lines = {}
-    exclude_dic_files = {}
-
-    exclude_file_name = 'preconf.exclude'
-
-#    # Build the dictionaries for line and file excludes that
-#    # are defined in the exlude file 'preconf.exclude'.
-#    # Syntax:
-#    # PathTo/File[:Line1,Line2,...]
-#    if os.path.exists(exclude_file_name):
-#        print 'Reading \'' + exclude_file_name + '\' ...'
-#        with open(exclude_file_name, 'r') as exclude:
-#            for line in exclude:
-#                exclude_line  = line.split(':')
-#                exclude_file = exclude_line[0].rstrip()
-#                if len(exclude_line) > 1:
-#                    exclude_lines = exclude_line[1].split(',')
-#                    for index,item in enumerate(exclude_lines):
-#                        exclude_lines[index] = int(item.rstrip())
-#                    exclude_dic_lines[exclude_line[0].rstrip()] = exclude_lines
-#                else:
-#                    exclude_dic_files[exclude_line[0].rstrip()] = [-1]
-#    else:
-#        print('Exclude file \'' + exclude_file_name + '\' not found. Checking all files.')
-
-
-    # Hardcoded files that will be skipped
-    exclude_dic_files = { 'Common/include/basic_types/datatype_structure.hpp' : [-1],
-                          'Common/include/parallelization/mpi_structure.hpp' : [-1],
-                          'Common/src/basic_types/datatype_structure.cpp': [-1],
-                          'Common/include/parallelization/mpi_structure.cpp' : [-1] }
-
-    str_double = 'double'
-
-    regex_double = re.compile(r'(^|[^\w])('+str_double+')([^\w]|$)')
-    replacement_double = r'\1su2double\3'
-    simple_replacements = {'MPI_Reduce'    : 'SU2_MPI::Reduce',
-                        'MPI_Allreduce' : 'SU2_MPI::Allreduce',
-                        'MPI_Gather'    : 'SU2_MPI::Gather',
-                        'MPI_Allgather' : 'SU2_MPI::Allgather',
-                        'MPI_Isend'     : 'SU2_MPI::Isend',
-                        'MPI_Irecv'     : 'SU2_MPI::Irecv',
-                        'MPI_Send'      : 'SU2_MPI::Send',
-                        'MPI_Wait'      : 'SU2_MPI::Wait',
-                        'MPI_Waitall'   : 'SU2_MPI::Waitall',
-                        'MPI_Waitany'   : 'SU2_MPI::Waitany',
-                        'MPI_Bsend'     : 'SU2_MPI::Bsend' ,
-                        'MPI_Bcast'     : 'SU2_MPI::Bcast',
-                        'MPI_Sendrecv'  : 'SU2_MPI::Sendrecv',
-                        'MPI_Init'      : 'SU2_MPI::Init',
-                        'MPI_Recv'      : 'SU2_MPI::Recv',
-                        'MPI_Comm_size' : 'SU2_MPI::Comm_size',
-                        'MPI_Comm_rank' : 'SU2_MPI::Comm_rank',
-                        'MPI_Init'      : 'SU2_MPI::Init',
-                        'MPI_Barrier'   : 'SU2_MPI::Barrier',
-                        'MPI_Abort'     : 'SU2_MPI::Abort',
-                        'MPI_Request'   : 'SU2_MPI::Request',
-                        'MPI_Get_count' : 'SU2_MPI::Get_count',
-                        'MPI_Finalize'  : 'SU2_MPI::Finalize',
-                        'MPI_Buffer_detach': 'SU2_MPI::Buffer_detach',
-                        'MPI_Buffer_attach': 'SU2_MPI::Buffer_attach',
-                        'MPI_Status'    : 'SU2_MPI::Status',
-                        'sprintf'       : 'SPRINTF'}
-    regex_cast_1 = re.compile(r'(^|[^\w|^\\])(int)(\s*\()')
-    replacement_cast_1 = r'\1SU2_TYPE::Int\3'
-    regex_cast_2 = re.compile(r'\(int\)\s*')
-
-    logfile = open ('preconf.log','w')
-
-    backup_ext = '.orig'
-    print('Checking for problems...')
-    # Test each source file for the occurrence of missing replacements
-    # and print the respective lines.
-    for dir in dir_list:
-        file_list = glob.glob(dir+os.path.sep+'*[src,include]'+os.path.sep+'*[.cpp,.hpp,.inl]')
-        for file in file_list:
-            if not file in exclude_dic_files.keys():
-
-                if all([not replace, revert]):
-                    # Check if back up file exists
-                    if os.path.isfile(file + backup_ext):
-                        os.remove(file);
-                        shutil.copy(file + backup_ext, file)
-                    else:
-                        print('Cannot find backup file ' + file + backup_ext)
-
-                # Remove backup files if requested
-                if all([not replace, remove]):
-                    if os.path.isfile(file + backup_ext):
-                        print('Removing' + file + backup_ext)
-                        os.remove(file + backup_ext)
-
-                if all([not remove, not revert]):
-                    num_found = 0
-                    found_line = ""
-                    ignore_line = ""
-                    new_line = ""
-                    for line in fileinput.input(file, inplace = 1, backup = backup_ext):
-                        new_line = line.rstrip('\n')
-                        if any([re.findall(regex_double, line), find_all(line, simple_replacements), re.findall(regex_cast_1, line)]):
-                            if not fileinput.lineno() in exclude_dic_lines.get(file,[]):
-                                if replace:
-                                    new_line = replace_all(new_line, simple_replacements)
-                                    new_line = re.sub(regex_double, replacement_double, new_line)
-                                    new_line = re.sub(regex_cast_1, replacement_cast_1, new_line)
-                                    found_line = found_line + '\tLine ' + str(fileinput.lineno()) +': ' + line.rstrip() + '\n\t\t => ' + new_line.rstrip() + '\n'
-                                else:
-                                    found_line = found_line + '\tLine ' + str(fileinput.lineno()) +': ' + line.rstrip() + '\n'
-                                num_found = num_found + 1
-                            else:
-                                ignore_line = ignore_line + 'Ignoring line ' + str(fileinput.lineno()) + ' in ' + file + ' (' + line.rstrip() + ')\n'
-                        print(new_line)
-                    if num_found > 0:
-                        if replace:
-                            print('Solved ' + str(num_found) + ' potential problem(s) in ' + file + '.')
-                            logfile.write('Solved ' + str(num_found) + ' potential problem(s) in ' + file + ':\n')
-                        else:
-                            print('Found ' + str(num_found) + ' potential problem(s) in ' + file + '.')
-                            logfile.write('Found ' + str(num_found) + ' potential problem(s) in ' + file + ':\n')
-                        logfile.write( found_line )
-                    else:
-                        os.remove(file + backup_ext)
-
-                    if not ignore_line == "":
-                        print(ignore_line.rstrip())
-            else:
-                print('Ignoring file ' + file)
-    print('\nPlease check preconf.log to get more information about potential problems.')
-
-def replace_all(text, dic):
-    for i, j in dic.iteritems():
-        text = text.replace(i, j)
-    return text
-
-def find_all(text, dic):
-    for i,j in dic.iteritems():
-        if not text.find(i) == -1:
-            return True
-    return False
-
-def init_codi(argument_dict, modes, mpi_support = False, update = False):
-
-    modules_failed = True
-
-    # This information of the modules is used if projects was not cloned using git
-    # The sha tag must be maintained manually to point to the correct commit
-    sha_version_codi = '3c3211fef2e225ab89680a4063b62bb3bb38a7e4'
-    github_repo_codi = 'https://github.com/scicompkl/CoDiPack'
-    sha_version_medi = '6aef76912e7099c4f08c9705848797ca9e8070da'
-    github_repo_medi = 'https://github.com/SciCompKL/MeDiPack'
-
-    medi_name = 'MeDiPack'
-    codi_name = 'CoDiPack'
-
-    alt_name_medi = 'externals/medi'
-    alt_name_codi = 'externals/codi'
-
-    # Some log and error files
-    log = open( 'preconf.log', 'w' )
-    err = open( 'preconf.err', 'w' )
-    pkg_environ = os.environ
-
-    codi_status = False
-    ampi_status = False
-
-    print("Checking the status of submodules")
-    print('=====================================================================')
-    # Remove modules if update is requested
-    if update:
-        if os.path.exists(alt_name_codi):
-            print('Removing ' + alt_name_codi)
-            shutil.rmtree(alt_name_codi)
-        if os.path.exists(alt_name_medi):
-            print('Removing ' + alt_name_medi)
-            shutil.rmtree(alt_name_medi)
-
-    submodule_check(codi_name, alt_name_codi, github_repo_codi, sha_version_codi, log, err, update)
-
-    if mpi_support:
-        submodule_check(medi_name, alt_name_medi, github_repo_medi, sha_version_medi, log, err, update)
-
-    return pkg_environ, True
-
-def submodule_check(name, alt_name, github_rep, sha_tag, log, err, update = False):
-
-    try:
-        status = submodule_status(alt_name, update)
-        if status:
-            print('Found correct version of ' + name + ' in ' + alt_name + '.')
-
-    except RuntimeError:
-        if all([os.path.exists(alt_name), not os.path.exists(alt_name + '/' + sha_tag)]):
-          print('Found an old or unspecified version of ' + name + ' in ' + alt_name + '.\nUse -u to reset module.')
-          sys.exit()
-        if not os.path.exists(alt_name):
-          print('\ngit command failed (either git is not installed or this is not a git repository).')
-          print('\nUsing fall-back method to initialize submodule ' + name)
-          download_module(name, alt_name, github_rep, sha_tag, log, err)
-        else:
-          print('Found correct version of ' + name + ' in ' + alt_name + '.')
-
-
-def submodule_status(path, update):
-
-    try:
-        status = check_output('git submodule status ' + path).decode()
-    except RuntimeError:
-        raise RuntimeError
-
-    status_indicator = status[0][0]
-
-    if status_indicator == '+':
-        sys.stderr.write('WARNING: the currently checked out submodule commit in ' + path + ' does not match the SHA-1 found in the index.\n')
-        sys.stderr.write('Use \'git submodule update --init '+ path + '\' to reset the module if necessary.\n')
-        return False
-    elif any([status_indicator == '-', update]):
-        print('Initialize submodule ' + path + ' using git ... ')
-        subprocess.check_call('git submodule update --init ' + path, shell = True)
-
-    return True
-
-def download_module(name, alt_name, git_repo, commit_sha, logfile, errorfile):
-
-    print('\nInitializing ' + name + ' \'' + commit_sha + '\'')
-    print('=====================================================================')
-    # Download package
-    try:
-        print('Downloading module from ' + git_repo)
-        subprocess.check_call('wget -N ' + git_repo + '/archive/' + commit_sha + '.zip', stdout = logfile, stderr = errorfile, shell = True )
-    except subprocess.CalledProcessError:
-        print('Download of module ' + name + ' failed. See preconf.err for more information.')
-        print('To download it manually, perform the following steps:')
-        print('\t - Download the zip at \"' + git_repo + '/archive/' + commit_sha + '.zip\"')
-        print('\t - Extract the archive to externals/' + alt_name)
-        print('\t - Execute command \'touch externals/'+ alt_name + '/' + commit_sha + '\'')
-        print('\t - Run preconfigure.py again')
-        sys.exit()
-
-    # Extract zip archive
-    try:
-        print('Extracting archive ...')
-        subprocess.check_call('unzip -u ' + commit_sha + '.zip', stdout = logfile, stderr = errorfile, shell=True)
-    except subprocess.CalledProcessError:
-        print('Extraction of module ' + name + ' failed. See preconf.err for more information.')
-        sys.exit()
-
-    # Rename folder and create a file to identify the version
-    try:
-        print('Creating identifier ...')
-        subprocess.check_call('mv '+ name + '-' + commit_sha + ' ' + alt_name + ' && touch ' + alt_name + '/' + commit_sha, stdout = logfile, stderr = errorfile, shell = True)
-    except subprocess.CalledProcessError:
-        print('Renaming of module ' + name + ' failed. See preconf.err for more information.')
-        sys.exit()
-
-    # Remove archive
-    subprocess.check_call('rm ' + commit_sha + '.zip', shell=True)
-
-def configure(argument_dict,
-              conf_environ,
-              mpi_support,
-              py_wrapper,
-              tecio,
-              modes,
-              made_adolc,
-              made_codi):
-
-    # Boostrap to generate Makefile.in
-    bootstrap_command = './bootstrap'
-    # Set the base command for running configure
-    configure_base = '../configure'
-
-    # Add the arguments to the configure command
-    for arg in argument_dict:
-        configure_base = configure_base + " " + arg + "=" + argument_dict[arg]
-
-    configure_mode = ''
-    if mpi_support:
-        configure_base = configure_base + ' --enable-mpi'
-    if py_wrapper:
-        configure_base = configure_base + ' --enable-PY_WRAPPER'
-    if tecio:
-        configure_base = configure_base + ' --disable-tecio'
-
-    build_dirs = ''
-
-    print(  '\nPreparing build environment\n' \
-            '=====================================================================')
-
-    run_command(bootstrap_command, 'bootstrap.log', 'bootstrap.err', conf_environ)
-
-    # Create the commands for the different configurations and run configure
-    for key in modes:
-        if modes[key]:
-            print('\nRunning configure in folder ' + key + ' ', end = '')
-            if modes[key] == 'CODI':
-                if key == 'SU2_DIRECTDIFF':
-                    configure_mode = '--enable-codi-forward'
-                if key == 'SU2_AD':
-                    configure_mode = '--enable-codi-reverse'
-                print('using ' + modes[key])
-            elif modes[key] == 'ADOLC':
-                if key == 'SU2_DIRECTDIFF':
-                    configure_mode = '--enable-adolc-forward'
-                if key == 'SU2_AD':
-                    configure_mode = '--enable-adolc-reverse'
-                print('using ' + modes[key])
-            elif modes[key] == 'COMPLEX':
-                configure_mode = '--enable-complex'
-                print('using ' + modes[key])
-            else:
-                configure_mode = ''
-                print('')
-
-            print('=====================================================================')
-            log = os.getcwd().rstrip() + '/conf_'+ key+'.log'
-            err = os.getcwd().rstrip() + '/conf_'+ key+'.err'
-
-            if not os.path.exists(key):
-                os.mkdir(key)
-
-            os.chdir(key)
-            run_command(configure_base + ' ' + configure_mode, log, err, conf_environ)
-            os.chdir(os.pardir)
-            build_dirs += key + ' '
-
-    write_makefile(build_dirs)
-
-    print('\nPre-configuration Summary:\n' \
-           '=====================================================================\n'\
-          '\tConfiguration sets: '+ build_dirs + '\n')
-
-    print('\tUse "make <install>" to compile (and install) all configured binaries:\n')
-    if modes['SU2_BASE']:
-        print('\tSU2_CFD            -> General solver for direct, cont. adjoint and linearized equations.\n' \
-              '\tSU2_DOT            -> Gradient Projection Code.\n' \
-              '\tSU2_DEF            -> Mesh Deformation Code.\n'  \
-              '\tSU2_SOL            -> Solution Export Code.\n' \
-              '\tSU2_GEO            -> Geometry Definition Code.\n')
-    if modes['SU2_AD']:
-        print('\tSU2_CFD_AD         -> Discrete Adjoint Solver and general AD support.')
-        print('\tSU2_DOT_AD         -> Mesh sensitivity computation and general AD support.')
-    if modes['SU2_DIRECTDIFF']:
-        print('\tSU2_CFD_DIRECTDIFF -> Direct Differentation Mode.')
-
-    print('\n')
-    print('\tPlease be sure to add the $SU2_HOME and $SU2_RUN environment variables,\n' \
-           '\tand update your $PATH (and $PYTHONPATH if applicable) with $SU2_RUN.\n' \
-           '\n' \
-           '\tBased on the input to this configuration, add these lines to your .bashrc file: \n' \
-           '\n' \
-           '\texport SU2_RUN="'+argument_dict['--prefix']+'/bin"\n' \
-           '\texport SU2_HOME="'+os.getcwd().rstrip()+'"\n' \
-           '\texport PATH=$PATH:$SU2_RUN\n' \
-           '\texport PYTHONPATH=$PYTHONPATH:$SU2_RUN\n')
-
-def run_command(command, log, err, env):
-
-    try:
-        logfile = open(log, 'w')
-        errfile = open(err, 'w')
-        print('Command: ' + command)
-        subprocess.check_call(command, env = env, stdout = logfile, stderr = errfile, shell=True)
-        print('Logfile written to ' + log)
-        logfile.close()
-        errfile.close()
-    except subprocess.CalledProcessError:
-        errfile = open(err, 'r')
-        print('\nThere was an error while running command \'' + command + '\'.')
-        print('=== Error Log ===')
-        print(errfile.read())
-        errfile.close()
-        sys.exit(1)
-
-
-def check_output(cmd):
-    std, err = subprocess.Popen([cmd], stdout=subprocess.PIPE, stderr=subprocess.PIPE, shell = True).communicate()
-    if err:
-        raise RuntimeError(err)
-    return std
-def write_makefile(build_dirs):
-    print('\nCreating Makefile ...\n')
-    makefile = open('Makefile', 'w')
-
-    makefile.writelines(['# This file is auto-generated by preconfigure.py\n',
-                         'SUBDIRS = '+ build_dirs + '\n',
-                         'INSTALLDIRS = $(SUBDIRS:%=install-%)\n',
-                         'CLEANDIRS = $(SUBDIRS:%=clean-%)\n',
-                         '\n',
-                         'subdirs: $(SUBDIRS)\n',
-                         '\n',
-                         '$(SUBDIRS):\n',
-                         '\t$(MAKE) -C $@\n',
-                         '\n',
-                         'install: $(INSTALLDIRS)\n',
-                         '$(INSTALLDIRS):\n',
-                         '\t$(MAKE) -C $(@:install-%=%) install\n',
-                         '\n',
-                         'clean: $(CLEANDIRS)\n',
-                         '$(CLEANDIRS):\n',
-                         '\t$(MAKE) -C $(@:clean-%=%) clean\n',
-                         '\n',
-                         '.PHONY: subdirs $(SUBDIRS)\n',
-                         '.PHONY: subdirs $(INSTALLDIRS)\n',
-                         '.PHONY: subdirs $(CLEANDIRS)\n',
-                         '.PHONY: install\n'])
-
-    makefile.close()
-
-def header():
-
-    print('-------------------------------------------------------------------------\n'\
-          '|    ___ _   _ ___                                                      | \n'\
-          '|   / __| | | |_  )   Release 7.5.1 \'Blackbird\'                         | \n'\
-          '|   \__ \ |_| |/ /                                                      | \n'\
-          '|   |___/\___//___|   Pre-configuration Script                          | \n'\
-          '|                                                                       | \n'\
-          '------------------------------------------------------------------------- \n'\
-          '| SU2 Project Website: https://su2code.github.io                        | \n'\
-          '|                                                                       | \n'\
-          '| The SU2 Project is maintained by the SU2 Foundation                   | \n'\
-          '| (http://su2foundation.org)                                            | \n'\
-          '------------------------------------------------------------------------- \n'\
-          '| Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)                | \n'\
-          '|                                                                       | \n'\
-          '| SU2 is free software; you can redistribute it and/or                  | \n'\
-          '| modify it under the terms of the GNU Lesser General Public            | \n'\
-          '| License as published by the Free Software Foundation; either          | \n'\
-          '| version 2.1 of the License, or (at your option) any later version.    | \n'\
-          '|                                                                       | \n'\
-          '| SU2 is distributed in the hope that it will be useful,                | \n'\
-          '| but WITHOUT ANY WARRANTY; without even the implied warranty of        | \n'\
-          '| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      | \n'\
-          '| Lesser General Public License for more details.                       | \n'\
-          '|                                                                       | \n'\
-          '| You should have received a copy of the GNU Lesser General Public      | \n'\
-          '| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   | \n'\
-          '------------------------------------------------------------------------- \n')
-
-
-
-# -------------------------------------------------------------------
-#  Run Main Program
-# -------------------------------------------------------------------
-
-# this is only accessed if running from command prompt
-if __name__ == '__main__':
-    main()
diff --git a/m4/ax_tls.m4 b/m4/ax_tls.m4
deleted file mode 100644
index 7aa3383eb8a..00000000000
--- a/m4/ax_tls.m4
+++ /dev/null
@@ -1,74 +0,0 @@
-# ===========================================================================
-#             http://www.nongnu.org/autoconf-archive/ax_tls.html
-# ===========================================================================
-#
-# SYNOPSIS
-#
-#   AX_TLS
-#
-# DESCRIPTION
-#
-#   Provides a test for the compiler support of thread local storage (TLS)
-#   extensions. Defines TLS if it is found. Currently only knows about GCC
-#   and MSVC. I think SunPro uses the same as GCC, and Borland apparently
-#   supports either.
-#
-# LICENSE
-#
-#   Copyright (c) 2008 Alan Woodland <ajw05@aber.ac.uk>
-#
-#   This program is free software: you can redistribute it and/or modify it
-#   under the terms of the GNU General Public License as published by the
-#   Free Software Foundation, either version 3 of the License, or (at your
-#   option) any later version.
-#
-#   This program is distributed in the hope that it will be useful, but
-#   WITHOUT ANY WARRANTY; without even the implied warranty of
-#   MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General
-#   Public License for more details.
-#
-#   You should have received a copy of the GNU General Public License along
-#   with this program. If not, see <http://www.gnu.org/licenses/>.
-#
-#   As a special exception, the respective Autoconf Macro's copyright owner
-#   gives unlimited permission to copy, distribute and modify the configure
-#   scripts that are the output of Autoconf when processing the Macro. You
-#   need not follow the terms of the GNU General Public License when using
-#   or distributing such scripts, even though portions of the text of the
-#   Macro appear in them. The GNU General Public License (GPL) does govern
-#   all other use of the material that constitutes the Autoconf Macro.
-#
-#   This special exception to the GPL applies to versions of the Autoconf
-#   Macro released by the Autoconf Archive. When you make and distribute a
-#   modified version of the Autoconf Macro, you may extend this special
-#   exception to the GPL to apply to your modified version as well.
-
-AC_DEFUN([AX_TLS], [
-  AC_MSG_CHECKING(for thread local storage (TLS) class)
-  AC_CACHE_VAL(ac_cv_tls, [
-    ax_tls_keywords="__thread __declspec(thread) none"
-    for ax_tls_keyword in $ax_tls_keywords; do
-       case $ax_tls_keyword in
-          none) ac_cv_tls=none ; break ;;
-	  *)
-             AC_TRY_COMPILE(
-                [#include <stdlib.h>
-                 static void
-                 foo(void) {
-                 static ] $ax_tls_keyword [ int bar;
-                 exit(1);
-                 }],
-                 [],
-                 [ac_cv_tls=$ax_tls_keyword ; break],
-                 ac_cv_tls=none
-             )
-	  esac
-    done
-])
-
-  if test "$ac_cv_tls" != "none"; then
-    dnl AC_DEFINE([TLS], [], [If the compiler supports a TLS storage class define it to that here])
-    AC_DEFINE_UNQUOTED([TLS], $ac_cv_tls, [If the compiler supports a TLS storage class define it to that here])
-  fi
-  AC_MSG_RESULT($ac_cv_tls)
-])
diff --git a/m4/cgns.m4 b/m4/cgns.m4
deleted file mode 100644
index 4a18aa06567..00000000000
--- a/m4/cgns.m4
+++ /dev/null
@@ -1,46 +0,0 @@
-# -------------------------------------------------------------
-# CGNS
-# -------------------------------------------------------------
-AC_DEFUN([CONFIGURE_CGNS],
-[
-  AC_ARG_ENABLE(cgns,
-                AC_HELP_STRING([--enable-cgns],
-                               [build with CFD General Notation System (CGNS) standard support (ADF only)]),
-		[case "${enableval}" in
-		  yes)  enablecgns=yes ;;
-		   no)  enablecgns=no ;;
- 		    *)  AC_MSG_ERROR(bad value ${enableval} for --enable-cgns) ;;
-		 esac],
-		 [enablecgns=yes])
-
-  # The CGNS lib is distributed with SU2, so we don't have to guess
-  # where it might be installed...
-  if (test $enablecgns = yes); then
-
-    # look for CGNS build cppflags by honoring the --with-cgns-cppflags="..." flag,
-    # defaulting to what we know works
-    AC_ARG_WITH([cgns-cppflags],
-                 AC_HELP_STRING([--with-cgns-cppflags="-fPIC"],
-                                [Specific CGNS C Preprocessor flags to use]),
-                 [SU2_CGNS_CPPFLAGS="$withval"],
-                 [SU2_CGNS_CPPFLAGS=""])
-
-
-     CGNS_INCLUDE="-I\$(top_srcdir)/externals/cgns -I\$(top_srcdir)/externals/cgns/adf"
-     CGNS_LIB="\$(top_builddir)/externals/cgns/libcgns.a"
-     AC_DEFINE(HAVE_CGNS, 1, [Flag indicating whether the library will be compiled with CGNS support])
-     AC_MSG_RESULT(<<< Configuring library with CGNS support >>>)
-
-     # look for thread-local storage
-     #AX_TLS
- else
-     CGNS_INCLUDE=""
-     CGNS_LIB=""
-     SU2_CGNS_CPPFLAGS=""
-     enablecgns=no
-  fi
-
-  AC_SUBST(CGNS_INCLUDE)
-  AC_SUBST(CGNS_LIB)
-  AC_SUBST(SU2_CGNS_CPPFLAGS)
-])
diff --git a/m4/codi.m4 b/m4/codi.m4
deleted file mode 100644
index 5bca5e32fb4..00000000000
--- a/m4/codi.m4
+++ /dev/null
@@ -1,53 +0,0 @@
-AC_DEFUN([CONFIGURE_CODI],
-[
-    AC_ARG_ENABLE(codi-reverse,
-        AS_HELP_STRING([--enable-codi-reverse], [build executables with codi reverse datatype (default = no)]),
-        [build_CODI_REVERSE="yes"], [build_CODI_REVERSE="no"])
-    AC_ARG_ENABLE(codi-forward,
-        AS_HELP_STRING([--enable-codi-forward], [build executables with codi forward datatype (default = no)]),
-        [build_CODI_FORWARD="yes"], [build_CODI_FORWARD="no"])
-
-        CODIheader=${srcdir}/externals/codi/include/codi.hpp
-        AMPIheader=${srcdir}/externals/medi/include/medi/medi.hpp
-
-        if test "$build_CODI_REVERSE" == "yes" || test "$build_CODI_FORWARD" == "yes"
-        then
-          AC_CHECK_FILE([$CODIheader],[have_CODI='yes'],[have_CODI='no'])
-          if test "$have_CODI" == "no"
-          then
-            AC_MSG_ERROR([CODI header was not found in externals/CoDi/include. Use 'preconfigure.py --autodiff' to download it.])
-          fi
-        fi
-
-        if test "$build_CODI_FORWARD" == "yes"
-        then
-           DIRECTDIFF_CXX="-DCODI_FORWARD_TYPE -I\$(top_srcdir)/externals/codi/include"
-           build_DIRECTDIFF=yes
-           if test "$enablempi" == "yes"
-           then
-              AC_CHECK_FILE([$AMPIheader], [have_AMPIheader='yes'], [have_AMPIheader='no'])
-              if test "$have_AMPIheader" == "no"
-              then
-                AC_MSG_ERROR([MediPack header not found in externals/medi/include.  Use 'preconfigure.py --autodiff --enable-mpi' to download it.])
-              fi
-              DIRECTDIFF_CXX=$DIRECTDIFF_CXX" -I\$(top_srcdir)/externals/medi/include -I\$(top_srcdir)/externals/medi/src"
-           fi
-           build_REVERSE=no
-           build_NORMAL=no
-        elif test "$build_CODI_REVERSE" == "yes"
-        then
-           REVERSE_CXX="-DCODI_REVERSE_TYPE -I\$(top_srcdir)/externals/codi/include"
-           if test "$enablempi" == "yes"
-           then
-              AC_CHECK_FILE([$AMPIheader], [have_AMPIheader='yes'], [have_AMPIheader='no'])
-              if test "$have_AMPIheader" == "no"
-              then
-                AC_MSG_ERROR([MediPack header not found in externals/medi/include.  Use 'preconfigure.py --autodiff --enable-mpi' to download it.])
-              fi
-              REVERSE_CXX=$REVERSE_CXX" -I\$(top_srcdir)/externals/medi/include -I\$(top_srcdir)/externals/medi/src"
-           fi
-           build_REVERSE=yes
-           build_DIRECTDIFF=no
-           build_NORMAL=no
-        fi
-])
diff --git a/m4/compiler.m4 b/m4/compiler.m4
deleted file mode 100644
index f401476404e..00000000000
--- a/m4/compiler.m4
+++ /dev/null
@@ -1,66 +0,0 @@
-# -------------------------------------------------------------
-# -------------------------------------------------------------
-AC_DEFUN([SU2_SET_COMPILERS],
-[
-  # --------------------------------------------------------------
-  # look for a decent C++ compiler or honor --with-cxx=...
-  CXX_TRY_LIST="g++ icpc icc pgCC c++"
-
-     # -------------------------------------------------------------------
-     # MPI -- disabled by default.  Check for it now so we can be somewhat
-     #                             smart about which compilers to look for
-     # -------------------------------------------------------------------
-     AC_ARG_ENABLE(mpi,
-                   AS_HELP_STRING([--enable-mpi],
-                                  [build with MPI message passing support]),
-   		   [case "${enableval}" in
-   		     yes)  enablempi=yes ;;
-   		      no)  enablempi=no ;;
-    		       *)  AC_MSG_ERROR(bad value ${enableval} for --enable-mpi) ;;
-   		    esac],
-   		    [enablempi=no])
-
-  have_MPI="no"
-
-  if  (test "$enablempi" != no) ; then
-    have_MPI="yes"
-    CPPFLAGS="-DHAVE_MPI $CPPFLAGS"
-    CXX_TRY_LIST="mpicxx mpiCC mpicc $CXX_TRY_LIST"
-  else
-    AC_MSG_RESULT(>>> MPI support disabled by default <<<)
-  fi
-
-  AC_ARG_WITH([cxx],
-  	    AS_HELP_STRING([--with-cxx=CXX],
-                             [C++ compiler to use]),
-  	    [CXX="$withval"],
-  	    [])
-
-  # --------------------------------------------------------------
-  # Determines a C++ compiler to use.  First checks if the variable CXX is
-  # already set.  If not, then searches under g++, c++, and other names.
-  # --------------------------------------------------------------
-  AC_PROG_CXX([$CXX_TRY_LIST])
-  # --------------------------------------------------------------
-
-
-
-  # --------------------------------------------------------------
-  # look for a decent C compiler or honor --with-cc=...
-  CC_TRY_LIST="gcc icc pgcc cc"
-  if  (test "$enablempi" != no) ; then
-    CC_TRY_LIST="mpicc $CC_TRY_LIST"
-  fi
-  AC_ARG_WITH([cc],
-  	    AS_HELP_STRING([--with-cc=CC],
-                             [C compiler to use]),
-  	    [CC="$withval"],
-  	    [])
-
-  # --------------------------------------------------------------
-  # Determine a C compiler to use.  If CC is not already set, checks for
-  # gcc, cc, and other C compilers.  Then sets the CC variable to the result.
-  # --------------------------------------------------------------
-  AC_PROG_CC([$CC_TRY_LIST])
-  # --------------------------------------------------------------
-])
diff --git a/m4/metis.m4 b/m4/metis.m4
deleted file mode 100644
index 9f2ee7c65f3..00000000000
--- a/m4/metis.m4
+++ /dev/null
@@ -1,50 +0,0 @@
-# -------------------------------------------------------------
-# Metis
-# -------------------------------------------------------------
-AC_DEFUN([CONFIGURE_METIS],
-[
-  AC_ARG_ENABLE(metis,
-                AC_HELP_STRING(),
-		[case "${enableval}" in
-		  yes)  enablemetis=yes ;;
-		   no)  enablemetis=no ;;
- 		    *)  AC_MSG_ERROR(bad value ${enableval} for --enable-metis) ;;
-		 esac],
-		 [enablemetis=yes])
-
-  # Trump --enable-parmetis with --disable-mpi
-  if (test "x$enablempi" = xno); then
-    enablemetis=no
-  fi
-
-  # The METIS API is distributed with SU2, so we don't have to guess
-  # where it might be installed...
-  if (test $enablemetis = yes); then
-
-    # look for METIS build cppflags by honoring the --with-metis-cppflags="..." flag,
-    # defaulting to what we know works
-    AC_ARG_WITH([metis-cppflags],
-                 AC_HELP_STRING([--with-metis-cppflags="-D_FILE_OFFSET_BITS=64 -DNDEBUG -DNDEBUG2 -DHAVE_EXECINFO_H -DHAVE_GETLINE"],
-                                [Specific METIS C Preprocessor flags to use]),
-                 [SU2_METIS_CPPFLAGS="$withval"],
-                 [SU2_METIS_CPPFLAGS="-D_FILE_OFFSET_BITS=64 -DNDEBUG -DNDEBUG2 -DHAVE_EXECINFO_H -DHAVE_GETLINE"])
-
-
-     METIS_INCLUDE="-I\$(top_srcdir)/externals/metis/include"
-     METIS_LIB="\$(top_builddir)/externals/metis/libmetis.a"
-     AC_DEFINE(HAVE_METIS, 1, [Flag indicating whether the library will be compiled with Metis support])
-     AC_MSG_RESULT(<<< Configuring library with Metis support >>>)
-
-     # look for thread-local storage
-     #AX_TLS
- else
-     METIS_INCLUDE=""
-     METIS_LIB=""
-     SU2_METIS_CPPFLAGS=""
-     enablemetis=no
-  fi
-
-  AC_SUBST(METIS_INCLUDE)
-  AC_SUBST(METIS_LIB)
-  AC_SUBST(SU2_METIS_CPPFLAGS)
-])
diff --git a/m4/parmetis.m4 b/m4/parmetis.m4
deleted file mode 100644
index 3b7443e92dd..00000000000
--- a/m4/parmetis.m4
+++ /dev/null
@@ -1,47 +0,0 @@
-# -------------------------------------------------------------
-# Parmetis
-# -------------------------------------------------------------
-AC_DEFUN([CONFIGURE_PARMETIS],
-[
-  AC_ARG_ENABLE(parmetis,
-                AS_HELP_STRING(),
-		[case "${enableval}" in
-		  yes)  enableparmetis=yes ;;
-		   no)  enableparmetis=no ;;
- 		    *)  AC_MSG_ERROR(bad value ${enableval} for --enable-parmetis) ;;
-		 esac],
-		 [enableparmetis=$enablemetis])
-
-  # Trump --enable-parmetis with --disable-mpi
-  if (test "x$enablempi" = xno); then
-    enableparmetis=no
-  fi
-
-
-  # The PARMETIS API is distributed with SU2, so we don't have to guess
-  # where it might be installed...
-  if (test $enableparmetis = yes); then
-
-    # look for PARMETIS build cppflags by honoring the --with-parmetis-cppflags="..." flag,
-    # defaulting to nothing
-    AC_ARG_WITH([parmetis-cppflags],
-                 AC_HELP_STRING([--with-parmetis-cppflags="..."],
-                                [Specific PARMETIS C Preprocessor flags to use]),
-                 [SU2_PARMETIS_CPPFLAGS="$withval"],
-                 [SU2_PARMETIS_CPPFLAGS=""])
-
-
-     PARMETIS_INCLUDE="-I\$(top_srcdir)/externals/parmetis/include"
-     PARMETIS_LIB="\$(top_builddir)/externals/parmetis/libparmetis.a"
-     AC_DEFINE(HAVE_PARMETIS, 1, [Flag indicating whether the library will be compiled with Parmetis support])
-     AC_MSG_RESULT(<<< Configuring library with Parmetis support >>>)
-  else
-     PARMETIS_INCLUDE=""
-     PARMETIS_LIB=""
-     enableparmetis=no
-  fi
-
-  AC_SUBST(PARMETIS_INCLUDE)
-  AC_SUBST(PARMETIS_LIB)
-  AC_SUBST(SU2_PARMETIS_CPPFLAGS)
-])
diff --git a/m4/tecio.m4 b/m4/tecio.m4
deleted file mode 100644
index 414bdc60470..00000000000
--- a/m4/tecio.m4
+++ /dev/null
@@ -1,61 +0,0 @@
-dnl -------------------------------------------------------------
-dnl tecio
-dnl -------------------------------------------------------------
-AC_DEFUN([CONFIGURE_TECIO],
-[
-  AC_ARG_ENABLE(tecio,
-                AC_HELP_STRING([--enable-tecio],
-                               [build with Tecplot TecIO API support (from source)]),
-		[case "${enableval}" in
-		  yes)  enabletecio=yes ;;
-		   no)  enabletecio=no ;;
- 		    *)  AC_MSG_ERROR(bad value ${enableval} for --enable-tecio) ;;
-		 esac],
-		 [enabletecio=yes])
-
-
-  # The TECIO API is distributed with libmesh, so we don't have to guess
-  # where it might be installed...
-  if (test $enabletecio = yes); then
-
-    # tecio platform-specific compiler flags
-    TECIO_CPPFLAGS=""
-    case "${host_os}" in
-      *linux*)
-	TECIO_CPPFLAGS="-DLINUX $TECIO_CPPFLAGS"
-	AC_CHECK_SIZEOF([void *])
-	if (test $ac_cv_sizeof_void_p = 8); then
-	  TECIO_CPPFLAGS="-DLINUX64 $TECIO_CPPFLAGS"
-	fi
-	;;
-
-      *darwin*)
-	TECIO_CPPFLAGS="-DDARWIN -DMAC64 $TECIO_CPPFLAGS"
-        ;;
-
-        *)
-	AC_MSG_RESULT([>>> Unrecognized TecIO platform, see externals/tecio/Runmake for hints on how to extend <<<])
-	;;
-    esac
-
-
-     if (test $have_MPI = yes); then
-         TECIO_INCLUDE="-I\$(top_srcdir)/externals/tecio/teciompisrc"
-         TECIO_LIB="\$(top_builddir)/externals/tecio/teciompisrc/libteciompi.a"
-     else
-         TECIO_INCLUDE="-I\$(top_srcdir)/externals/tecio/teciosrc"
-         TECIO_LIB="\$(top_builddir)/externals/tecio/teciosrc/libtecio.a"
-     fi
-     AC_DEFINE(HAVE_TECPLOT_API, 1, [Flag indicating whether the library will be compiled with Tecplot TecIO API support])
-     AC_DEFINE(HAVE_TECPLOT_API_112, 1, [Flag indicating tecplot API understands newer features])
-     AC_MSG_RESULT(<<< Configuring library with Tecplot TecIO support >>>)
-     have_tecio=yes
-  else
-     TECIO_INCLUDE=""
-     enabletecio=no
-     have_tecio=no
-  fi
-
-  AC_SUBST(TECIO_INCLUDE)
-  AC_SUBST(TECIO_CPPFLAGS)
-])

From 63ce2750921e408b28c6e31f269a5790eb9b9d5f Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 11 Mar 2023 19:38:51 -0800
Subject: [PATCH 263/656] check if the compiler supports the warning we disable
 for tecio

---
 externals/tecio/teciosrc/meson.build | 21 ++++++++++++---------
 1 file changed, 12 insertions(+), 9 deletions(-)

diff --git a/externals/tecio/teciosrc/meson.build b/externals/tecio/teciosrc/meson.build
index f1654fdbceb..ab7e985549b 100644
--- a/externals/tecio/teciosrc/meson.build
+++ b/externals/tecio/teciosrc/meson.build
@@ -12,14 +12,17 @@ if (host_machine.system() == 'windows')
   tecio_cpp_flags += ['-DMSWIN']
 endif
 
-if build_machine.system() != 'windows'
-  if meson.get_compiler('cpp').get_id() != 'intel'
-    tecio_cpp_flags += ['-Wno-misleading-indentation',
-                        '-Wno-uninitialized',
-                        '-Wno-placement-new',
-                        '-Wno-pedantic',
-                        '-Wno-error=deprecated-copy']
-  endif
+if build_machine.system() != 'windows' and meson.get_compiler('cpp').get_id() != 'intel'
+  desired_warnings = ['-Wno-misleading-indentation',
+                      '-Wno-uninitialized',
+                      '-Wno-placement-new',
+                      '-Wno-pedantic',
+                      '-Wno-error=deprecated-copy']
+  foreach flag : desired_warnings
+    if meson.get_compiler('cpp').has_argument(flag)
+      tecio_cpp_flags += flag
+    endif
+  endforeach
 endif
 
 tecio_include = include_directories('../', './')
@@ -97,7 +100,7 @@ tecio = static_library('tecio',
            'readValueArray.cpp',
            'TecioSZL.cpp',
            'exportSubzonePlt.cpp',
-           install : false, 
+           install : false,
 	   cpp_args: [default_warning_flags, tecio_cpp_flags],
 	   include_directories: tecio_include)
 

From 0850547c03de617984ba9562d93b5aad07a6c22c Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 11 Mar 2023 19:53:42 -0800
Subject: [PATCH 264/656] add workflow

---
 .github/workflows/require-labels.yml | 13 +++++++++++++
 1 file changed, 13 insertions(+)
 create mode 100644 .github/workflows/require-labels.yml

diff --git a/.github/workflows/require-labels.yml b/.github/workflows/require-labels.yml
new file mode 100644
index 00000000000..5e00e21e4ef
--- /dev/null
+++ b/.github/workflows/require-labels.yml
@@ -0,0 +1,13 @@
+name: Pull Request Labels
+on:
+  pull_request:
+    types: [opened, labeled, unlabeled, synchronize]
+jobs:
+  label:
+    runs-on: ubuntu-latest
+    steps:
+      - uses: mheap/github-action-required-labels@v3
+        with:
+          mode: exactly
+          count: 1
+          labels: "changelog:feature, changelog:fix, changelog:chore"

From b546b1402a31aac174b1edc641435c52ee0ea8ca Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Tue, 14 Mar 2023 16:52:25 +0100
Subject: [PATCH 265/656] CoDiPack update.

---
 externals/codi        | 2 +-
 meson_scripts/init.py | 2 +-
 2 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/externals/codi b/externals/codi
index 76a63ec8805..427c2dc754a 160000
--- a/externals/codi
+++ b/externals/codi
@@ -1 +1 @@
-Subproject commit 76a63ec8805eee146b1a5f6629676d3e78383f9e
+Subproject commit 427c2dc754a628ad3c9310c766c988ac5ce21bc7
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 0ee68b6f1df..a46079ddfc4 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -44,7 +44,7 @@ def init_submodules(method = 'auto'):
 
   # This information of the modules is used if projects was not cloned using git
   # The sha tag must be maintained manually to point to the correct commit
-  sha_version_codi = '76a63ec8805eee146b1a5f6629676d3e78383f9e'
+  sha_version_codi = '427c2dc754a628ad3c9310c766c988ac5ce21bc7'
   github_repo_codi = 'https://github.com/scicompkl/CoDiPack'
   sha_version_medi = 'aafc2d1966ba1233640af737e71c77c1a86183fd'
   github_repo_medi = 'https://github.com/SciCompKL/MeDiPack'

From 338585bcca773e8076a55571b1bc117df4c8f4be Mon Sep 17 00:00:00 2001
From: "Francesco Poli (wintermute)" <invernomuto@paranoici.org>
Date: Sun, 5 Mar 2023 12:30:55 +0100
Subject: [PATCH 266/656] allow to use Meson version later than the minimum

---
 meson.build | 5 +----
 1 file changed, 1 insertion(+), 4 deletions(-)

diff --git a/meson.build b/meson.build
index a93cdd83d5c..2bd8e4af02d 100644
--- a/meson.build
+++ b/meson.build
@@ -1,15 +1,12 @@
 project('SU2', 'c', 'cpp',
         version: '7.5.1 "Blackbird"',
+        meson_version: '>=0.61.1',
         license: 'LGPL2',
         default_options: ['buildtype=release',
                           'warning_level=0',
                           'c_std=c99',
                           'cpp_std=c++11'])
 
-if meson.version() != '0.61.1'
-  error('SU2 must be configured with the extended Meson script (./meson.py) in the SU2 root directory.')
-endif
-
 pymod = import('python')
 python = pymod.find_installation()
 

From 1c3273e6ce1b18414b4fe538e7c3d84e1195d84a Mon Sep 17 00:00:00 2001
From: "Francesco Poli (wintermute)" <invernomuto@paranoici.org>
Date: Sun, 5 Mar 2023 12:35:43 +0100
Subject: [PATCH 267/656] allow to use system-wide Meson and Ninja

See github issue [#1945] for more information on the rationale.

[#1945]: <https://github.com/su2code/SU2/issues/1945>

If a user wants to build SU2 from source and prefers to use
system-wide Meson and Ninja (assuming they are installed on the OS),
rather than SU2-specific copies, it is possible to avoid downloading
SU2-specific versions:

  $ SU2_MESON='no' ./meson.py
  $ export CXXFLAGS=<preferred_compiler_options>
  $ meson setup <preferred_config_options> build
  $ ninja -C build install

The default behavior is unchanged. If a user does not have system-wide
Meson and Ninja installed on the OS and/or prefers to use SU2-specific
copies, it is stll possible to download and use SU2-specific versions
of Meson and Ninja:

  $ export CXXFLAGS=<preferred_compiler_options>
  $ ./meson.py setup <preferred_config_options> build
  $ ./ninja -C build install
---
 meson.py              |  5 +++++
 meson_scripts/init.py | 10 ++++++----
 2 files changed, 11 insertions(+), 4 deletions(-)

diff --git a/meson.py b/meson.py
index dbeb6bfebef..6869ea28e43 100755
--- a/meson.py
+++ b/meson.py
@@ -70,6 +70,11 @@ def build_ninja():
   # Set up the build environment, i.e. clone or download all submodules
   init_submodules('auto')
 
+  # Exit after setting up submodules, if system-wide Meson and Ninja are
+  # going to be used
+  if (os.environ.get('SU2_MESON') == 'no'):
+    sys.exit(0)
+
   # Build ninja if it cannot be found
   build_ninja()
 
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index a46079ddfc4..66824e46f55 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -95,8 +95,9 @@ def init_submodules(method = 'auto'):
     submodule_status(alt_name_codi, sha_version_codi)
     submodule_status(alt_name_medi, sha_version_medi)
     submodule_status(alt_name_opdi, sha_version_opdi)
-    submodule_status(alt_name_meson, sha_version_meson)
-    submodule_status(alt_name_ninja, sha_version_ninja)
+    if (os.environ.get('SU2_MESON') != 'no'):
+      submodule_status(alt_name_meson, sha_version_meson)
+      submodule_status(alt_name_ninja, sha_version_ninja)
     submodule_status(alt_name_mpp, sha_version_mpp)
     submodule_status(alt_name_coolprop, sha_version_coolprop)
     submodule_status(alt_name_mel, sha_version_mel)
@@ -105,8 +106,9 @@ def init_submodules(method = 'auto'):
     download_module(codi_name, alt_name_codi, github_repo_codi, sha_version_codi)
     download_module(medi_name, alt_name_medi, github_repo_medi, sha_version_medi)
     download_module(opdi_name, alt_name_opdi, github_repo_opdi, sha_version_opdi)
-    download_module(meson_name, alt_name_meson, github_repo_meson, sha_version_meson)
-    download_module(ninja_name, alt_name_ninja, github_repo_ninja, sha_version_ninja)
+    if (os.environ.get('SU2_MESON') != 'no'):
+      download_module(meson_name, alt_name_meson, github_repo_meson, sha_version_meson)
+      download_module(ninja_name, alt_name_ninja, github_repo_ninja, sha_version_ninja)
     download_module(mpp_name, alt_name_mpp, github_repo_mpp, sha_version_mpp)
     download_module(coolprop_name, alt_name_coolprop, github_repo_coolprop, sha_version_coolprop)
     download_module(mel_name, alt_name_mel, github_repo_mel, sha_version_mel)

From cb9c0b7d4b5fe3c235c98a10deee5f138f41e64f Mon Sep 17 00:00:00 2001
From: "Francesco Poli (wintermute)" <invernomuto@paranoici.org>
Date: Tue, 7 Mar 2023 17:35:19 +0100
Subject: [PATCH 268/656] check that the ./meson.py script has been run

---
 .gitignore  | 3 +++
 meson.build | 5 +++++
 meson.py    | 4 ++++
 3 files changed, 12 insertions(+)

diff --git a/.gitignore b/.gitignore
index 484e0b6e38e..0a9dee961bc 100644
--- a/.gitignore
+++ b/.gitignore
@@ -97,3 +97,6 @@ ninja
 
 # Ignore vscode folder
 .vscode/
+
+# Ignore SU2 configuration timestamp created by meson.py
+su2config.timestamp
diff --git a/meson.build b/meson.build
index 2bd8e4af02d..cd9c7d66541 100644
--- a/meson.build
+++ b/meson.build
@@ -7,6 +7,11 @@ project('SU2', 'c', 'cpp',
                           'c_std=c99',
                           'cpp_std=c++11'])
 
+fsmod = import('fs')
+if not fsmod.exists('su2config.timestamp')
+  error('SU2 must be configured with the extended Meson script (./meson.py) in the SU2 root directory.')
+endif
+
 pymod = import('python')
 python = pymod.find_installation()
 
diff --git a/meson.py b/meson.py
index 6869ea28e43..a4b8d5257d8 100755
--- a/meson.py
+++ b/meson.py
@@ -26,6 +26,7 @@
 # License along with SU2. If not, see <http://www.gnu.org/licenses/>.
 
 import sys, os, subprocess, shutil, urllib.request, zipfile
+from pathlib import Path
 sys.path.append(sys.path[0] + os.path.sep + 'meson_scripts')
 from init import init_submodules
 from init import remove_file
@@ -70,6 +71,9 @@ def build_ninja():
   # Set up the build environment, i.e. clone or download all submodules
   init_submodules('auto')
 
+  # Leave a timestamp
+  Path('su2config.timestamp').touch()
+
   # Exit after setting up submodules, if system-wide Meson and Ninja are
   # going to be used
   if (os.environ.get('SU2_MESON') == 'no'):

From dda44b36ea9395327585a8b00ed2a5aeb30b6f63 Mon Sep 17 00:00:00 2001
From: "Francesco Poli (wintermute)" <invernomuto@paranoici.org>
Date: Sat, 11 Mar 2023 17:03:45 +0100
Subject: [PATCH 269/656] separate out the pre-configure step

If a user wants to build SU2 from source and prefers to use
system-wide Meson and Ninja (assuming they are installed on the OS),
rather than SU2-specific copies, it is possible to avoid downloading
SU2-specific versions:

  $ ./preconfigure.py
  $ export CXXFLAGS=<preferred_compiler_options>
  $ meson setup <preferred_config_options> build
  $ ninja -C build install

The default behavior is unchanged. If a user does not have system-wide
Meson and Ninja installed on the OS and/or prefers to use SU2-specific
copies, it is stll possible to download and use SU2-specific versions
of Meson and Ninja:

  $ export CXXFLAGS=<preferred_compiler_options>
  $ ./meson.py setup <preferred_config_options> build
  $ ./ninja -C build install
---
 .gitignore            |   4 +-
 meson.build           |   4 +-
 meson.py              |  58 ++-----------------
 meson_scripts/init.py |  51 +++++++++++------
 preconfigure.py       | 128 ++++++++++++++++++++++++++++++++++++++++++
 5 files changed, 173 insertions(+), 72 deletions(-)
 create mode 100755 preconfigure.py

diff --git a/.gitignore b/.gitignore
index 0a9dee961bc..8b56bc5e603 100644
--- a/.gitignore
+++ b/.gitignore
@@ -98,5 +98,5 @@ ninja
 # Ignore vscode folder
 .vscode/
 
-# Ignore SU2 configuration timestamp created by meson.py
-su2config.timestamp
+# Ignore SU2 pre-configuration timestamp created by preconfigure.py
+su2preconfig.timestamp
diff --git a/meson.build b/meson.build
index cd9c7d66541..2aa544f949c 100644
--- a/meson.build
+++ b/meson.build
@@ -8,8 +8,8 @@ project('SU2', 'c', 'cpp',
                           'cpp_std=c++11'])
 
 fsmod = import('fs')
-if not fsmod.exists('su2config.timestamp')
-  error('SU2 must be configured with the extended Meson script (./meson.py) in the SU2 root directory.')
+if not fsmod.exists('su2preconfig.timestamp')
+  error('SU2 must be (pre-)configured with the extended Meson script (./meson.py) or with the ./preconfigure.py script in the SU2 root directory.')
 endif
 
 pymod = import('python')
diff --git a/meson.py b/meson.py
index a4b8d5257d8..8f1659de345 100755
--- a/meson.py
+++ b/meson.py
@@ -2,7 +2,7 @@
 
 ## \file meson.py
 #  \brief An extended meson script for setting up the environment and running meson
-#  \author T. Albring
+#  \author T. Albring and F. Poli
 #  \version 7.5.1 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
@@ -25,62 +25,16 @@
 # You should have received a copy of the GNU Lesser General Public
 # License along with SU2. If not, see <http://www.gnu.org/licenses/>.
 
-import sys, os, subprocess, shutil, urllib.request, zipfile
-from pathlib import Path
-sys.path.append(sys.path[0] + os.path.sep + 'meson_scripts')
-from init import init_submodules
-from init import remove_file
-
-def build_ninja():
-
-  # If we are on windows, we don't need to compile ninja, we just download the executable
-  if os.name == 'nt':
-    ninja_exe_url = 'https://github.com/ninja-build/ninja/releases/download/v1.9.0/ninja-win.zip'
-
-    # Try to execute ninja, if it fails, download .exe from github
-    try:
-      subprocess.run([sys.path[0] + os.path.sep + 'ninja.exe', '--version'], stdout=subprocess.PIPE)
-    except OSError:
-      print ('Downloading ninja ... ')
-      try:
-        urllib.request.urlretrieve (ninja_exe_url,'ninja-win.zip')
-      except:
-        print(e)
-        print('Download of ninja executable failed.')
-        print('Get archive at ' + ninja_exe_url)
-        print('extract ninja.exe in the source code root folder.')
-        print('Run meson.py again.')
-        sys.exit(1)
-
-      zipf = zipfile.ZipFile(sys.path[0] + os.path.sep + 'ninja-win.zip')
-      zipf.extractall(sys.path[0])
-      remove_file(sys.path[0] + os.path.sep + 'ninja-win.zip')
-  else:
-    ninjapath = sys.path[0] + os.path.sep + 'externals' + os.path.sep + 'ninja'
-    try:
-      subprocess.run([sys.path[0] + os.path.sep + 'ninja', '--version'], stdout=subprocess.PIPE)
-    except OSError:
-      print("ninja executable not found. Building ...")
-      subprocess.run(['python3', 'configure.py', '--bootstrap'], cwd=ninjapath)
-      shutil.copy(ninjapath+ os.path.sep + 'ninja', '.')
+import sys, os, subprocess
+sys.path.append(sys.path[0])
+import preconfigure
 
 if __name__ == '__main__':
   if sys.version_info[0] < 3:
     raise Exception("Script must be run using Python 3")
 
-  # Set up the build environment, i.e. clone or download all submodules
-  init_submodules('auto')
-
-  # Leave a timestamp
-  Path('su2config.timestamp').touch()
-
-  # Exit after setting up submodules, if system-wide Meson and Ninja are
-  # going to be used
-  if (os.environ.get('SU2_MESON') == 'no'):
-    sys.exit(0)
-
-  # Build ninja if it cannot be found
-  build_ninja()
+  # Preconfigure
+  preconfigure.run(own_meson = True)
 
   # Add paths for meson and ninja to environment
   os.environ["NINJA"] = sys.path[0] + os.path.sep + "ninja"
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 66824e46f55..e6edac57458 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -3,7 +3,7 @@
 ## \file init.py
 #  \brief Initializes necessary dependencies for SU2 either using git or it
 #         fetches zip files.
-#  \author T. Albring
+#  \author T. Albring and F. Poli
 #  \version 7.5.1 "Blackbird"
 #
 # SU2 Project Website: https://su2code.github.io
@@ -38,7 +38,14 @@ def remove_file(path, retries=3, sleep=0.1):
       break
 
 
-def init_submodules(method = 'auto'):
+def init_submodules(method = 'auto',
+                    own_meson = False,
+                    own_codi = True,
+                    own_medi = True,
+                    own_opdi = True,
+                    own_mpp  = True,
+                    own_cool = True,
+                    own_mel  = True):
 
   cur_dir = sys.path[0]
 
@@ -92,26 +99,38 @@ def init_submodules(method = 'auto'):
   # If directory was cloned using git, use submodule feature
   # to check and initialize submodules if necessary
   if is_git:
-    submodule_status(alt_name_codi, sha_version_codi)
-    submodule_status(alt_name_medi, sha_version_medi)
-    submodule_status(alt_name_opdi, sha_version_opdi)
-    if (os.environ.get('SU2_MESON') != 'no'):
+    if own_codi:
+      submodule_status(alt_name_codi, sha_version_codi)
+    if own_medi:
+      submodule_status(alt_name_medi, sha_version_medi)
+    if own_opdi:
+      submodule_status(alt_name_opdi, sha_version_opdi)
+    if own_meson:
       submodule_status(alt_name_meson, sha_version_meson)
       submodule_status(alt_name_ninja, sha_version_ninja)
-    submodule_status(alt_name_mpp, sha_version_mpp)
-    submodule_status(alt_name_coolprop, sha_version_coolprop)
-    submodule_status(alt_name_mel, sha_version_mel)
+    if own_mpp:
+      submodule_status(alt_name_mpp, sha_version_mpp)
+    if own_cool:
+      submodule_status(alt_name_coolprop, sha_version_coolprop)
+    if own_mel:
+      submodule_status(alt_name_mel, sha_version_mel)
   # Otherwise download the zip file from git
   else:
-    download_module(codi_name, alt_name_codi, github_repo_codi, sha_version_codi)
-    download_module(medi_name, alt_name_medi, github_repo_medi, sha_version_medi)
-    download_module(opdi_name, alt_name_opdi, github_repo_opdi, sha_version_opdi)
-    if (os.environ.get('SU2_MESON') != 'no'):
+    if own_codi:
+      download_module(codi_name, alt_name_codi, github_repo_codi, sha_version_codi)
+    if own_medi:
+      download_module(medi_name, alt_name_medi, github_repo_medi, sha_version_medi)
+    if own_opdi:
+      download_module(opdi_name, alt_name_opdi, github_repo_opdi, sha_version_opdi)
+    if own_meson:
       download_module(meson_name, alt_name_meson, github_repo_meson, sha_version_meson)
       download_module(ninja_name, alt_name_ninja, github_repo_ninja, sha_version_ninja)
-    download_module(mpp_name, alt_name_mpp, github_repo_mpp, sha_version_mpp)
-    download_module(coolprop_name, alt_name_coolprop, github_repo_coolprop, sha_version_coolprop)
-    download_module(mel_name, alt_name_mel, github_repo_mel, sha_version_mel)
+    if own_mpp:
+      download_module(mpp_name, alt_name_mpp, github_repo_mpp, sha_version_mpp)
+    if own_cool:
+      download_module(coolprop_name, alt_name_coolprop, github_repo_coolprop, sha_version_coolprop)
+    if own_mel:
+      download_module(mel_name, alt_name_mel, github_repo_mel, sha_version_mel)
 
 
 def is_git_directory(path = '.'):
diff --git a/preconfigure.py b/preconfigure.py
new file mode 100755
index 00000000000..5f3d6c29182
--- /dev/null
+++ b/preconfigure.py
@@ -0,0 +1,128 @@
+#!/usr/bin/env python3
+
+## \file preconfigure.py
+#  \brief An preconfigure script for setting up the build environment
+#  \author T. Albring and F. Poli
+#  \version 7.5.1 "Blackbird"
+#
+# SU2 Project Website: https://su2code.github.io
+#
+# The SU2 Project is maintained by the SU2 Foundation
+# (http://su2foundation.org)
+#
+# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
+#
+# SU2 is free software; you can redistribute it and/or
+# modify it under the terms of the GNU Lesser General Public
+# License as published by the Free Software Foundation; either
+# version 2.1 of the License, or (at your option) any later version.
+#
+# SU2 is distributed in the hope that it will be useful,
+# but WITHOUT ANY WARRANTY; without even the implied warranty of
+# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+# Lesser General Public License for more details.
+#
+# You should have received a copy of the GNU Lesser General Public
+# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+
+import sys, os, subprocess, shutil, urllib.request, zipfile
+from pathlib import Path
+sys.path.append(sys.path[0] + os.path.sep + 'meson_scripts')
+from init import init_submodules
+from init import remove_file
+
+def build_ninja():
+
+  # If we are on windows, we don't need to compile ninja, we just download the executable
+  if os.name == 'nt':
+    ninja_exe_url = 'https://github.com/ninja-build/ninja/releases/download/v1.9.0/ninja-win.zip'
+
+    # Try to execute ninja, if it fails, download .exe from github
+    try:
+      subprocess.run([sys.path[0] + os.path.sep + 'ninja.exe', '--version'], stdout=subprocess.PIPE)
+    except OSError:
+      print ('Downloading ninja ... ')
+      try:
+        urllib.request.urlretrieve (ninja_exe_url,'ninja-win.zip')
+      except:
+        print(e)
+        print('Download of ninja executable failed.')
+        print('Get archive at ' + ninja_exe_url)
+        print('extract ninja.exe in the source code root folder.')
+        print('Run meson.py again.')
+        sys.exit(1)
+
+      zipf = zipfile.ZipFile(sys.path[0] + os.path.sep + 'ninja-win.zip')
+      zipf.extractall(sys.path[0])
+      remove_file(sys.path[0] + os.path.sep + 'ninja-win.zip')
+  else:
+    ninjapath = sys.path[0] + os.path.sep + 'externals' + os.path.sep + 'ninja'
+    try:
+      subprocess.run([sys.path[0] + os.path.sep + 'ninja', '--version'], stdout=subprocess.PIPE)
+    except OSError:
+      print("ninja executable not found. Building ...")
+      subprocess.run(['python3', 'configure.py', '--bootstrap'], cwd=ninjapath)
+      shutil.copy(ninjapath+ os.path.sep + 'ninja', '.')
+
+def run(own_meson = False,
+        own_codi = True,
+        own_medi = True,
+        own_opdi = True,
+        own_mpp  = True,
+        own_cool = True,
+        own_mel  = True):
+
+  # Set up the build environment, i.e. clone or download submodules
+  init_submodules(method = 'auto',
+                  own_meson = own_meson,
+                  own_codi = own_codi,
+                  own_medi = own_medi,
+                  own_opdi = own_opdi,
+                  own_mpp  = own_mpp ,
+                  own_cool = own_cool,
+                  own_mel  = own_mel)
+
+  # Leave a timestamp
+  Path('su2preconfig.timestamp').touch()
+
+  if (own_meson):
+    # Build ninja if it cannot be found
+    build_ninja()
+
+
+if __name__ == '__main__':
+  if sys.version_info[0] < 3:
+    raise Exception("Script must be run using Python 3")
+
+  import argparse
+  parser = argparse.ArgumentParser()
+  parser.add_argument("--with-own-meson",
+                      help="download own copies of Meson and Ninja",
+                      action="store_true")
+  parser.add_argument("--no-codi",
+                      help="do not download own copy of CoDiPack",
+                      action="store_false")
+  parser.add_argument("--no-medi",
+                      help="do not download own copy of MeDiPack",
+                      action="store_false")
+  parser.add_argument("--no-opdi",
+                      help="do not download own copy of OpDiLib",
+                      action="store_false")
+  parser.add_argument("--no-mpp",
+                      help="do not download own copy of Mutationpp",
+                      action="store_false")
+  parser.add_argument("--no-coolprop",
+                      help="do not download own copy of CoolProp",
+                      action="store_false")
+  parser.add_argument("--no-mel",
+                      help="do not download own copy of MEL",
+                      action="store_false")
+  args = parser.parse_args()
+
+  run(own_meson = args.with_own_meson,
+      own_codi = args.no_codi,
+      own_medi = args.no_medi,
+      own_opdi = args.no_opdi,
+      own_mpp  = args.no_mpp,
+      own_cool = args.no_coolprop,
+      own_mel  = args.no_mel)

From 60f85fff1b7d0b3a04a65f93987dcaa6f1ccd084 Mon Sep 17 00:00:00 2001
From: "Francesco Poli (wintermute)" <invernomuto@paranoici.org>
Date: Tue, 14 Mar 2023 23:50:21 +0100
Subject: [PATCH 270/656] create timestamp at the end of preconfigure.py

---
 preconfigure.py | 6 +++---
 1 file changed, 3 insertions(+), 3 deletions(-)

diff --git a/preconfigure.py b/preconfigure.py
index 5f3d6c29182..7e27d2e2a97 100755
--- a/preconfigure.py
+++ b/preconfigure.py
@@ -82,13 +82,13 @@ def run(own_meson = False,
                   own_cool = own_cool,
                   own_mel  = own_mel)
 
-  # Leave a timestamp
-  Path('su2preconfig.timestamp').touch()
-
   if (own_meson):
     # Build ninja if it cannot be found
     build_ninja()
 
+  # Leave a timestamp
+  Path('su2preconfig.timestamp').touch()
+
 
 if __name__ == '__main__':
   if sys.version_info[0] < 3:

From a94769c9c19e4b1cffb9d7323552849afb4b881e Mon Sep 17 00:00:00 2001
From: "Francesco Poli (wintermute)" <invernomuto@paranoici.org>
Date: Tue, 14 Mar 2023 23:51:44 +0100
Subject: [PATCH 271/656] don't import subprocess in meson.py

It's now unused in meson.py (its use has been moved to
preconfigure.py).
---
 meson.py | 3 ++-
 1 file changed, 2 insertions(+), 1 deletion(-)

diff --git a/meson.py b/meson.py
index 8f1659de345..e8601a8e599 100755
--- a/meson.py
+++ b/meson.py
@@ -25,10 +25,11 @@
 # You should have received a copy of the GNU Lesser General Public
 # License along with SU2. If not, see <http://www.gnu.org/licenses/>.
 
-import sys, os, subprocess
+import sys, os
 sys.path.append(sys.path[0])
 import preconfigure
 
+
 if __name__ == '__main__':
   if sys.version_info[0] < 3:
     raise Exception("Script must be run using Python 3")

From 7fddc7da8030cebbcd1702226724b30be91b5441 Mon Sep 17 00:00:00 2001
From: "Francesco Poli (wintermute)" <invernomuto@paranoici.org>
Date: Tue, 14 Mar 2023 23:53:30 +0100
Subject: [PATCH 272/656] add myself to the list of individual contributors

---
 AUTHORS.md | 1 +
 1 file changed, 1 insertion(+)

diff --git a/AUTHORS.md b/AUTHORS.md
index 49ce6d21fe8..85b2334d5e6 100644
--- a/AUTHORS.md
+++ b/AUTHORS.md
@@ -71,6 +71,7 @@ Eduardo Molina
 Edwin van der Weide
 Ethan Alan Hereth
 Florian Dittmann
+Francesco Poli
 Francisco D. Palacios
 Gaurav Bansal
 Giacomo Baldan

From 14ee869ba8fe81898a42e3ef31ac9d0b31a3b789 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 15 Mar 2023 11:41:33 +0100
Subject: [PATCH 273/656] Move MeDiPack initialization and MPI setup to the
 constructor of CDriverBase.

---
 SU2_CFD/src/drivers/CDriver.cpp               | 12 ----------
 SU2_CFD/src/drivers/CDriverBase.cpp           | 22 ++++++++++++++++++-
 SU2_DEF/src/drivers/CDeformationDriver.cpp    | 12 ----------
 .../src/drivers/CDiscAdjDeformationDriver.cpp | 12 ----------
 4 files changed, 21 insertions(+), 37 deletions(-)

diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index cf69fefeddd..14dc54017a4 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -109,18 +109,6 @@
 CDriver::CDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator, bool dummy_geo) :
 CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false), fem_solver(false), dry_run(dummy_geo) {
 
-    /*--- Initialize Medipack (must also be here so it is initialized from python) ---*/
-#ifdef HAVE_MPI
-  #if defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)
-    SU2_MPI::Init_AMPI();
-  #endif
-#endif
-
-  SU2_MPI::SetComm(MPICommunicator);
-
-  rank = SU2_MPI::GetRank();
-  size = SU2_MPI::GetSize();
-
   /*--- Start timer to track preprocessing for benchmarking. ---*/
 
   StartTime = SU2_MPI::Wtime();
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index fee7f12ab41..1db01069204 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -34,7 +34,27 @@
 using namespace std;
 
 CDriverBase::CDriverBase(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator)
-    : config_file_name(confFile), StartTime(0.0), StopTime(0.0), UsedTime(0.0), TimeIter(0), nZone(val_nZone) {}
+    : config_file_name(confFile), StartTime(0.0), StopTime(0.0), UsedTime(0.0), TimeIter(0), nZone(val_nZone) {
+
+  /*--- Some initializations are placed here so that they are also seen by the python wrapper. Note that the python
+   * wrapper instantiates a driver directly. ---*/
+
+  /*--- MPI is required to be initialized already, e.g, via SU2_MPI::Init, SU2_MPI::Init_thread, or via mpi4py in the
+   * python wrapper. ---*/
+
+  /*--- Initialize MeDiPack ---*/
+#ifdef HAVE_MPI
+#if defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)
+  SU2_MPI::Init_AMPI();
+#endif
+#endif
+
+  /*--- Set up MPI ---*/
+  SU2_MPI::SetComm(MPICommunicator);
+
+  rank = SU2_MPI::GetRank();
+  size = SU2_MPI::GetSize();
+}
 
 CDriverBase::~CDriverBase(void) {}
 
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index d88d0048ec3..e5f592f90db 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -37,18 +37,6 @@ using namespace std;
 CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
     : CDriverBase(confFile, 1, MPICommunicator) {
 
-/*--- Initialize MeDiPack (must also be here to initialize it from Python) ---*/
-#ifdef HAVE_MPI
-#if defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)
-  SU2_MPI::Init_AMPI();
-#endif
-#endif
-
-  SU2_MPI::SetComm(MPICommunicator);
-
-  rank = SU2_MPI::GetRank();
-  size = SU2_MPI::GetSize();
-
   /*--- Preprocessing of the config files. ---*/
 
   Input_Preprocessing();
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index ddab47fc4f9..f53ce3aa955 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -43,18 +43,6 @@ using namespace std;
 CDiscAdjDeformationDriver::CDiscAdjDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
     : CDriverBase(confFile, 1, MPICommunicator) {
 
-/*--- Initialize MeDiPack (must also be here to initialize it from Python). ---*/
-#ifdef HAVE_MPI
-#if defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)
-  SU2_MPI::Init_AMPI();
-#endif
-#endif
-
-  SU2_MPI::SetComm(MPICommunicator);
-
-  rank = SU2_MPI::GetRank();
-  size = SU2_MPI::GetSize();
-
   /*--- Preprocessing of the config files. ---*/
 
   Input_Preprocessing();

From 54af1c2500d5075607feb4b6248c149d450fc5dc Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 15 Mar 2023 11:58:05 +0100
Subject: [PATCH 274/656] Move AD initialization to the constructor of
 CDriverBase.

---
 SU2_CFD/src/SU2_CFD.cpp             | 4 ++--
 SU2_CFD/src/drivers/CDriverBase.cpp | 3 +++
 SU2_DOT/src/SU2_DOT.cpp             | 5 ++---
 3 files changed, 7 insertions(+), 5 deletions(-)

diff --git a/SU2_CFD/src/SU2_CFD.cpp b/SU2_CFD/src/SU2_CFD.cpp
index db29bdc1dc6..be34404ed79 100644
--- a/SU2_CFD/src/SU2_CFD.cpp
+++ b/SU2_CFD/src/SU2_CFD.cpp
@@ -73,8 +73,8 @@ int main(int argc, char *argv[]) {
 #endif
   SU2_MPI::Comm MPICommunicator = SU2_MPI::GetComm();
 
-  /*--- AD initialization ---*/
-  AD::Initialize();
+  /*--- Further initializations are placed in the constructor of CDriverBase, to ensure that they are also seen by the
+   python wrapper. */
 
   /*--- Uncomment the following line if runtime NaN catching is desired. ---*/
   // feenableexcept(FE_INVALID | FE_OVERFLOW | FE_DIVBYZERO );
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index 1db01069204..6f4582e2d68 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -54,6 +54,9 @@ CDriverBase::CDriverBase(char* confFile, unsigned short val_nZone, SU2_Comm MPIC
 
   rank = SU2_MPI::GetRank();
   size = SU2_MPI::GetSize();
+
+  /*--- Initialize AD ---*/
+  AD::Initialize();
 }
 
 CDriverBase::~CDriverBase(void) {}
diff --git a/SU2_DOT/src/SU2_DOT.cpp b/SU2_DOT/src/SU2_DOT.cpp
index b8b606ca75c..82d2ae5e292 100644
--- a/SU2_DOT/src/SU2_DOT.cpp
+++ b/SU2_DOT/src/SU2_DOT.cpp
@@ -41,9 +41,8 @@ int main(int argc, char* argv[]) {
 #endif
   SU2_MPI::Comm comm = SU2_MPI::GetComm();
 
-  /*--- AD initialization. ---*/
-
-  AD::Initialize();
+  /*--- Further initializations are placed in the constructor of CDriverBase, to ensure that they are also seen by the
+   python wrapper. */
 
   /*--- Load in the number of zones and spatial dimensions in the mesh file
    (if no config file is specified, default.cfg is used). ---*/

From 77d7ccea4dd835981ca1000e7a5ea2ddd2d3000f Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 15 Mar 2023 12:22:31 +0100
Subject: [PATCH 275/656] Move OpenMP initialization to the constructor of
 CDriverBase.

---
 SU2_CFD/src/SU2_CFD.cpp             | 4 +---
 SU2_CFD/src/drivers/CDriverBase.cpp | 3 +++
 2 files changed, 4 insertions(+), 3 deletions(-)

diff --git a/SU2_CFD/src/SU2_CFD.cpp b/SU2_CFD/src/SU2_CFD.cpp
index be34404ed79..11e8720cfb3 100644
--- a/SU2_CFD/src/SU2_CFD.cpp
+++ b/SU2_CFD/src/SU2_CFD.cpp
@@ -56,9 +56,7 @@ int main(int argc, char *argv[]) {
 
   CLI11_PARSE(app, argc, argv)
 
-  /*--- OpenMP initialization ---*/
-
-  omp_initialize();
+  /*--- OpenMP setup ---*/
 
   omp_set_num_threads(num_threads);
 
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index 6f4582e2d68..76ce8c42f5a 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -55,6 +55,9 @@ CDriverBase::CDriverBase(char* confFile, unsigned short val_nZone, SU2_Comm MPIC
   rank = SU2_MPI::GetRank();
   size = SU2_MPI::GetSize();
 
+  /*--- OpenMP initialization ---*/
+  omp_initialize();
+
   /*--- Initialize AD ---*/
   AD::Initialize();
 }

From 56d0f363cf0e6a02abe2919794385034b708aac1 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Thu, 16 Mar 2023 10:41:34 +0100
Subject: [PATCH 276/656] Pulled develop

---
 externals/codi | 2 +-
 externals/medi | 2 +-
 externals/opdi | 2 +-
 3 files changed, 3 insertions(+), 3 deletions(-)

diff --git a/externals/codi b/externals/codi
index 427c2dc754a..96ac78ec5bc 160000
--- a/externals/codi
+++ b/externals/codi
@@ -1 +1 @@
-Subproject commit 427c2dc754a628ad3c9310c766c988ac5ce21bc7
+Subproject commit 96ac78ec5bcc5ac25b785e79b16ed76fca22d736
diff --git a/externals/medi b/externals/medi
index aafc2d1966b..6aef76912e7 160000
--- a/externals/medi
+++ b/externals/medi
@@ -1 +1 @@
-Subproject commit aafc2d1966ba1233640af737e71c77c1a86183fd
+Subproject commit 6aef76912e7099c4f08c9705848797ca9e8070da
diff --git a/externals/opdi b/externals/opdi
index f33b507c24f..1aabf5bd1ed 160000
--- a/externals/opdi
+++ b/externals/opdi
@@ -1 +1 @@
-Subproject commit f33b507c24f7448d4cf4df16ab5c53ea254b8774
+Subproject commit 1aabf5bd1ed77611742eb655002f2ac7a3dddef9

From 16ab987418d9595f7f9a5f0ac1feaf6d33e98316 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Thu, 16 Mar 2023 10:50:52 +0100
Subject: [PATCH 277/656] Remove outdated/redundant test specifications.

---
 TestCases/parallel_regression.py | 18 ------------------
 1 file changed, 18 deletions(-)

diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 58907af6632..af2cb7ddc9f 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -165,10 +165,7 @@ def main():
     super_cat.cfg_file = "super_cat.cfg"
     super_cat.test_iter = 10
     super_cat.test_vals = [-5.232590, -5.757884, -20.641547, -20.640244, -20.539243, 1.246889, -3.205235, -0.028406, 0.250857, 32459.000000]
-    super_cat.su2_exec = "mpirun -n 2 SU2_CFD"
-    super_cat.timeout = 1600
     super_cat.new_output = True
-    super_cat.tol = 0.00001
     test_list.append(super_cat)
 
     # Viscous single wedge - partially catalytic walls
@@ -177,10 +174,7 @@ def main():
     partial_cat.cfg_file = "partial_cat.cfg"
     partial_cat.test_iter = 10
     partial_cat.test_vals = [-5.210300, -5.735063, -20.880374, -20.825890, -23.475263, 1.806281, -2.813924, -0.078469, 0.496017, 2.9021e+04]
-    partial_cat.su2_exec = "mpirun -n 2 SU2_CFD"
-    partial_cat.timeout = 1600
     partial_cat.new_output = True
-    partial_cat.tol = 0.00001
     test_list.append(partial_cat)
 
     # Viscous cylinder, ionization, Gupta-Yos
@@ -189,10 +183,7 @@ def main():
     ion_gy.cfg_file = "cyl_ion_gy.cfg"
     ion_gy.test_iter = 10
     ion_gy.test_vals = [-11.629873, -4.165563, -4.702662, -4.950351, -5.146155, -4.993878, -6.893332, 5.990109, 5.990004, -0.014849, 0.000000, 90090.000000]
-    ion_gy.su2_exec = "mpirun -n 2 SU2_CFD"
-    ion_gy.timeout = 1600
     ion_gy.new_output = True
-    ion_gy.tol = 0.00001
     test_list.append(ion_gy)
 
     ##########################
@@ -1457,10 +1448,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg_file  = "species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg"
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.test_iter = 50
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.test_vals = [-6.113626, -4.989076, -4.880565, -7.351737, 2.452701, -5.627391, 30.000000, -5.721303, 11.000000, -8.001991, 10.000000, -8.813670, 2.084143, 1.000000, 0.600000, 0.484143]
-    species2_primitiveVenturi_mixingmodel_heatcapacity_H2.su2_exec  = "mpirun -n 2 SU2_CFD"
-    species2_primitiveVenturi_mixingmodel_heatcapacity_H2.timeout   = 1600
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.new_output = True
-    species2_primitiveVenturi_mixingmodel_heatcapacity_H2.tol       = 0.00001
     test_list.append(species2_primitiveVenturi_mixingmodel_heatcapacity_H2)
 
     # 2 species (1 eq) primitive venturi mixing using mixing model including heat capacity and mass diffusivity NonDimensional case
@@ -1469,10 +1457,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg_file  = "species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg"
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.test_iter = 50
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.test_vals = [-5.719472, -5.293846, -5.185419, -8.355307, 2.147874, -5.233215, 30.000000, -5.721396, 11.000000, -8.000062, 10.000000, -8.814100, 2.084145, 1.000000, 0.600000, 0.484145]
-    species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.su2_exec  = "mpirun -n 2 SU2_CFD"
-    species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.timeout   = 1600
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.new_output = True
-    species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.tol       = 0.00001
     test_list.append(species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND)
 
     # 2 species (1 eq) primitive venturi mixing
@@ -1499,10 +1484,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg_file  = "species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg"
     species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.test_iter = 50
     species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.test_vals = [-4.012157, -1.650191, -1.405134, -0.990205, 1.619918, -3.764227, 23.000000, -5.039466, 12.000000, -5.346201, 4.000000, -6.084514, 2.000000, 1.000000, 0.000000, 1.000000]
-    species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.su2_exec  = "mpirun -n 2 SU2_CFD"
-    species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.timeout   = 1600
     species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.new_output = True
-    species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.tol       = 0.00001
     test_list.append(species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS)
 
     # 3 species (2 eq) primitive venturi mixing with inlet files.

From b4a56e4f830db7813083573c4a6cc77f29736b13 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Thu, 16 Mar 2023 11:26:31 +0100
Subject: [PATCH 278/656] Print only on rank 0 in disc_adj_flow python wrapper
 test.

---
 .../py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py      | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
index 99d32126414..69e7baccc10 100755
--- a/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
@@ -112,7 +112,7 @@ def main():
   for iVertex in range(nVertex_Marker):
     sensX, sensY, sensZ = SU2Driver.GetMeshDisp_Sensitivity(MarkerID, iVertex)
 
-    if (iVertex == 30):
+    if (iVertex == 30) and rank == 0:
       print(1000,1000,iVertex, sensX, sensY, sensZ)
 
   # Postprocess the solver and exit cleanly

From b7f5b126627f186daf2351bff4a5ab55b9a518e6 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Thu, 16 Mar 2023 13:04:35 +0100
Subject: [PATCH 279/656] Updated submodules

---
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 2d2085ff67a..e76c01013bd 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -47,7 +47,7 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
 
   /*--- Relaxation factor and tolerance for Newton solvers. ---*/
   Newton_Relaxation = config->GetRelaxation_DataDriven();
-  Newton_Tolerance = 1e-10;
+  Newton_Tolerance = 2e-10;
   MaxIter_Newton = 50;
 
   /*--- Preprocessing of inputs and outputs for the interpolation method. ---*/

From 810e3604a0e42ab348a08165851dfda7048a0e87 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Thu, 16 Mar 2023 13:35:11 +0100
Subject: [PATCH 280/656] Add disc_adj_flow python wrapper test to parallel
 regression AD.

---
 TestCases/parallel_regression_AD.py | 17 +++++++++++++++++
 1 file changed, 17 insertions(+)

diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index 2173b4ba3cf..6b953c97ec2 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -391,6 +391,23 @@ def main():
     pass_list.append(unsteady_naca0012.run_filediff())
     test_list.append(unsteady_naca0012)
 
+    ####################################################################
+    ###  Python Wrapper                                              ###
+    ####################################################################
+
+    # Flow AD Mesh Displacement Sensitivity
+    pywrapper_FEA_AD_FlowLoad               = TestCase('pywrapper_CFD_AD_MeshDisp')
+    pywrapper_FEA_AD_FlowLoad.cfg_dir       = "py_wrapper/disc_adj_flow/mesh_disp_sens"
+    pywrapper_FEA_AD_FlowLoad.cfg_file      = "configAD_flow.cfg"
+    pywrapper_FEA_AD_FlowLoad.test_iter     = 1000
+    pywrapper_FEA_AD_FlowLoad.test_vals     = [30.000000, -2.520972485907894, 1.3848377455328362, 0.000000] #last 4 columns
+    pywrapper_FEA_AD_FlowLoad.command       = TestCase.Command("mpirun -n 2", "python", "run_adjoint.py --parallel -f")
+    pywrapper_FEA_AD_FlowLoad.timeout       = 1600
+    pywrapper_FEA_AD_FlowLoad.tol           = 0.000001
+    pywrapper_FEA_AD_FlowLoad.new_output    = False
+    test_list.append(pywrapper_FEA_AD_FlowLoad)
+    pass_list.append(pywrapper_FEA_AD_FlowLoad.run_test())
+
     ####################################################################
     ###  Unsteady Disc. adj. compressible RANS restart optimization  ###
     ####################################################################

From 47457999dad410c447c1eed3d785e4f0e13dcf41 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Thu, 16 Mar 2023 14:43:18 +0100
Subject: [PATCH 281/656] Prepare disc_adj_fea python wrapper test for MPI
 parallel runs.

---
 .../flow_load_sens/run_adjoint.py             | 27 +++++++++++--------
 1 file changed, 16 insertions(+), 11 deletions(-)

diff --git a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
index e254137fc27..294d88cb48a 100755
--- a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
@@ -77,15 +77,18 @@ def main():
   if MarkerName in MarkerList and MarkerName in allMarkerIDs.keys():
     MarkerID = allMarkerIDs[MarkerName]
 
+  # Only print on the rank to which the marker belongs.
+
   # Time loop is defined in Python so that we have acces to SU2 functionalities at each time step
-  if rank == 0:
+  if MarkerID != None:
     print("\n------------------------------ Begin Solver -----------------------------\n")
   sys.stdout.flush()
   if options.with_MPI == True:
     comm.Barrier()
 
   # Define the load at the target vertex
-  SU2Driver.SetFEA_Loads(MarkerID,5,0,-0.005,0)
+  if MarkerID != None:
+    SU2Driver.SetFEA_Loads(MarkerID,5,0,-0.005,0)
 
   # Time iteration preprocessing
   SU2Driver.Preprocess(0)
@@ -102,17 +105,19 @@ def main():
   # Output the solution to file
   SU2Driver.Output(0)
 
-  sens=[]
-  disp=[]
-  # Recover the sensitivity
-  sens.append(SU2Driver.GetFlowLoad_Sensitivity(MarkerID,5))
+  if MarkerID != None:
+    sens=[]
+    disp=[]
+
+    # Recover the sensitivity
+    sens.append(SU2Driver.GetFlowLoad_Sensitivity(MarkerID,5))
 
-  fea_sol = SU2Driver.GetSolverIndices()["FEA"]
-  marker_disp = SU2Driver.MarkerSolution(fea_sol, MarkerID)
-  disp.append(marker_disp.Get(5))
+    fea_sol = SU2Driver.GetSolverIndices()["FEA"]
+    marker_disp = SU2Driver.MarkerSolution(fea_sol, MarkerID)
+    disp.append(marker_disp.Get(5))
 
-  print("Sens[0]\tSens[1]\tDisp[0]\tDisp[1]\t")
-  print(100, 100, sens[0][0], sens[0][1], disp[0][0], disp[0][1])
+    print("Sens[0]\tSens[1]\tDisp[0]\tDisp[1]\t")
+    print(100, 100, sens[0][0], sens[0][1], disp[0][0], disp[0][1])
 
   # Postprocess the solver and exit cleanly
   SU2Driver.Postprocessing()

From 121a56763f7ad0a28bb1551bb8296f9af1ba3039 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Thu, 16 Mar 2023 14:43:45 +0100
Subject: [PATCH 282/656] Add disc_adj_fea python wrapper test to parallel
 regression AD.

---
 TestCases/parallel_regression_AD.py | 13 +++++++++++++
 1 file changed, 13 insertions(+)

diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index 6b953c97ec2..00a39ccd059 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -395,6 +395,19 @@ def main():
     ###  Python Wrapper                                              ###
     ####################################################################
 
+    # FEA AD Flow Load Sensitivity
+    pywrapper_FEA_AD_FlowLoad               = TestCase('pywrapper_FEA_AD_FlowLoad')
+    pywrapper_FEA_AD_FlowLoad.cfg_dir       = "py_wrapper/disc_adj_fea/flow_load_sens"
+    pywrapper_FEA_AD_FlowLoad.cfg_file      = "configAD_fem.cfg"
+    pywrapper_FEA_AD_FlowLoad.test_iter     = 100
+    pywrapper_FEA_AD_FlowLoad.test_vals     = [-0.13945587401785386, -0.5859858866132448, -0.00036377840086080694, -0.0031005670174756366] #last 4 columns
+    pywrapper_FEA_AD_FlowLoad.command       = TestCase.Command("mpirun -n 2", "python", "run_adjoint.py --parallel -f")
+    pywrapper_FEA_AD_FlowLoad.timeout       = 1600
+    pywrapper_FEA_AD_FlowLoad.tol           = 0.000001
+    pywrapper_FEA_AD_FlowLoad.new_output    = False
+    test_list.append(pywrapper_FEA_AD_FlowLoad)
+    pass_list.append(pywrapper_FEA_AD_FlowLoad.run_test())
+
     # Flow AD Mesh Displacement Sensitivity
     pywrapper_FEA_AD_FlowLoad               = TestCase('pywrapper_CFD_AD_MeshDisp')
     pywrapper_FEA_AD_FlowLoad.cfg_dir       = "py_wrapper/disc_adj_flow/mesh_disp_sens"

From 47f5a14cbedcbae4e96b9d8062ebc1b6d3f74c35 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Thu, 16 Mar 2023 16:01:30 +0100
Subject: [PATCH 283/656] Add hybrid AD python wrapper tests.

---
 TestCases/hybrid_regression_AD.py | 31 +++++++++++++++++++++++++++++++
 1 file changed, 31 insertions(+)

diff --git a/TestCases/hybrid_regression_AD.py b/TestCases/hybrid_regression_AD.py
index 65e3ab57b24..288b3df31f8 100644
--- a/TestCases/hybrid_regression_AD.py
+++ b/TestCases/hybrid_regression_AD.py
@@ -222,6 +222,37 @@ def main():
 
     pass_list = [ test.run_test() for test in test_list ]
 
+    ###################################
+    ### Python Wrapper              ###
+    ###################################
+
+    # FEA AD Flow Load Sensitivity
+    pywrapper_FEA_AD_FlowLoad               = TestCase('pywrapper_FEA_AD_FlowLoad')
+    pywrapper_FEA_AD_FlowLoad.cfg_dir       = "py_wrapper/disc_adj_fea/flow_load_sens"
+    pywrapper_FEA_AD_FlowLoad.cfg_file      = "configAD_fem.cfg"
+    pywrapper_FEA_AD_FlowLoad.test_iter     = 100
+    pywrapper_FEA_AD_FlowLoad.test_vals     = [-0.13945587401682674, -0.5859858866082689, -0.00036377840086080753, -0.00310056701747564] #last 4 columns
+    pywrapper_FEA_AD_FlowLoad.command       = TestCase.Command(exec = "python", param = "run_adjoint.py --parallel -f")
+    pywrapper_FEA_AD_FlowLoad.timeout       = 1600
+    pywrapper_FEA_AD_FlowLoad.tol           = 0.000001
+    pywrapper_FEA_AD_FlowLoad.new_output    = False
+    test_list.append(pywrapper_FEA_AD_FlowLoad)
+    pass_list.append(pywrapper_FEA_AD_FlowLoad.run_test())
+
+    # Flow AD Mesh Displacement Sensitivity
+    pywrapper_FEA_AD_FlowLoad               = TestCase('pywrapper_CFD_AD_MeshDisp')
+    pywrapper_FEA_AD_FlowLoad.cfg_dir       = "py_wrapper/disc_adj_flow/mesh_disp_sens"
+    pywrapper_FEA_AD_FlowLoad.cfg_file      = "configAD_flow.cfg"
+    pywrapper_FEA_AD_FlowLoad.test_iter     = 1000
+    pywrapper_FEA_AD_FlowLoad.test_vals     = [30.000000, -2.5210057520523224, 1.3751902987065319, 0.000000] #last 4 columns
+    pywrapper_FEA_AD_FlowLoad.command       = TestCase.Command(exec = "python", param = "run_adjoint.py --parallel -f")
+    pywrapper_FEA_AD_FlowLoad.timeout       = 1600
+    pywrapper_FEA_AD_FlowLoad.tol           = 0.000001
+    pywrapper_FEA_AD_FlowLoad.new_output    = False
+    test_list.append(pywrapper_FEA_AD_FlowLoad)
+    pass_list.append(pywrapper_FEA_AD_FlowLoad.run_test())
+
+
     # Tests summary
     print('==================================================================')
     print('Summary of the hybrid parallel AD tests')

From 16113163ad6892b382948a53599a961ee4c653a6 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Thu, 16 Mar 2023 16:03:53 +0100
Subject: [PATCH 284/656] Fix test variable of disc_adj_flow python wrapper
 test.

---
 TestCases/hybrid_regression_AD.py   | 22 +++++++++++-----------
 TestCases/parallel_regression_AD.py | 22 +++++++++++-----------
 TestCases/serial_regression_AD.py   | 22 +++++++++++-----------
 3 files changed, 33 insertions(+), 33 deletions(-)

diff --git a/TestCases/hybrid_regression_AD.py b/TestCases/hybrid_regression_AD.py
index 288b3df31f8..a24ddb5b051 100644
--- a/TestCases/hybrid_regression_AD.py
+++ b/TestCases/hybrid_regression_AD.py
@@ -240,17 +240,17 @@ def main():
     pass_list.append(pywrapper_FEA_AD_FlowLoad.run_test())
 
     # Flow AD Mesh Displacement Sensitivity
-    pywrapper_FEA_AD_FlowLoad               = TestCase('pywrapper_CFD_AD_MeshDisp')
-    pywrapper_FEA_AD_FlowLoad.cfg_dir       = "py_wrapper/disc_adj_flow/mesh_disp_sens"
-    pywrapper_FEA_AD_FlowLoad.cfg_file      = "configAD_flow.cfg"
-    pywrapper_FEA_AD_FlowLoad.test_iter     = 1000
-    pywrapper_FEA_AD_FlowLoad.test_vals     = [30.000000, -2.5210057520523224, 1.3751902987065319, 0.000000] #last 4 columns
-    pywrapper_FEA_AD_FlowLoad.command       = TestCase.Command(exec = "python", param = "run_adjoint.py --parallel -f")
-    pywrapper_FEA_AD_FlowLoad.timeout       = 1600
-    pywrapper_FEA_AD_FlowLoad.tol           = 0.000001
-    pywrapper_FEA_AD_FlowLoad.new_output    = False
-    test_list.append(pywrapper_FEA_AD_FlowLoad)
-    pass_list.append(pywrapper_FEA_AD_FlowLoad.run_test())
+    pywrapper_CFD_AD_MeshDisp               = TestCase('pywrapper_CFD_AD_MeshDisp')
+    pywrapper_CFD_AD_MeshDisp.cfg_dir       = "py_wrapper/disc_adj_flow/mesh_disp_sens"
+    pywrapper_CFD_AD_MeshDisp.cfg_file      = "configAD_flow.cfg"
+    pywrapper_CFD_AD_MeshDisp.test_iter     = 1000
+    pywrapper_CFD_AD_MeshDisp.test_vals     = [30.000000, -2.5210057520523224, 1.3751902987065319, 0.000000] #last 4 columns
+    pywrapper_CFD_AD_MeshDisp.command       = TestCase.Command(exec = "python", param = "run_adjoint.py --parallel -f")
+    pywrapper_CFD_AD_MeshDisp.timeout       = 1600
+    pywrapper_CFD_AD_MeshDisp.tol           = 0.000001
+    pywrapper_CFD_AD_MeshDisp.new_output    = False
+    test_list.append(pywrapper_CFD_AD_MeshDisp)
+    pass_list.append(pywrapper_CFD_AD_MeshDisp.run_test())
 
 
     # Tests summary
diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index 00a39ccd059..74a991ec43b 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -409,17 +409,17 @@ def main():
     pass_list.append(pywrapper_FEA_AD_FlowLoad.run_test())
 
     # Flow AD Mesh Displacement Sensitivity
-    pywrapper_FEA_AD_FlowLoad               = TestCase('pywrapper_CFD_AD_MeshDisp')
-    pywrapper_FEA_AD_FlowLoad.cfg_dir       = "py_wrapper/disc_adj_flow/mesh_disp_sens"
-    pywrapper_FEA_AD_FlowLoad.cfg_file      = "configAD_flow.cfg"
-    pywrapper_FEA_AD_FlowLoad.test_iter     = 1000
-    pywrapper_FEA_AD_FlowLoad.test_vals     = [30.000000, -2.520972485907894, 1.3848377455328362, 0.000000] #last 4 columns
-    pywrapper_FEA_AD_FlowLoad.command       = TestCase.Command("mpirun -n 2", "python", "run_adjoint.py --parallel -f")
-    pywrapper_FEA_AD_FlowLoad.timeout       = 1600
-    pywrapper_FEA_AD_FlowLoad.tol           = 0.000001
-    pywrapper_FEA_AD_FlowLoad.new_output    = False
-    test_list.append(pywrapper_FEA_AD_FlowLoad)
-    pass_list.append(pywrapper_FEA_AD_FlowLoad.run_test())
+    pywrapper_CFD_AD_MeshDisp               = TestCase('pywrapper_CFD_AD_MeshDisp')
+    pywrapper_CFD_AD_MeshDisp.cfg_dir       = "py_wrapper/disc_adj_flow/mesh_disp_sens"
+    pywrapper_CFD_AD_MeshDisp.cfg_file      = "configAD_flow.cfg"
+    pywrapper_CFD_AD_MeshDisp.test_iter     = 1000
+    pywrapper_CFD_AD_MeshDisp.test_vals     = [30.000000, -2.520972485907894, 1.3848377455328362, 0.000000] #last 4 columns
+    pywrapper_CFD_AD_MeshDisp.command       = TestCase.Command("mpirun -n 2", "python", "run_adjoint.py --parallel -f")
+    pywrapper_CFD_AD_MeshDisp.timeout       = 1600
+    pywrapper_CFD_AD_MeshDisp.tol           = 0.000001
+    pywrapper_CFD_AD_MeshDisp.new_output    = False
+    test_list.append(pywrapper_CFD_AD_MeshDisp)
+    pass_list.append(pywrapper_CFD_AD_MeshDisp.run_test())
 
     ####################################################################
     ###  Unsteady Disc. adj. compressible RANS restart optimization  ###
diff --git a/TestCases/serial_regression_AD.py b/TestCases/serial_regression_AD.py
index 01848429ca3..d9885b1dcd1 100644
--- a/TestCases/serial_regression_AD.py
+++ b/TestCases/serial_regression_AD.py
@@ -344,17 +344,17 @@ def main():
     pass_list.append(pywrapper_FEA_AD_FlowLoad.run_test())
 
     # Flow AD Mesh Displacement Sensitivity
-    pywrapper_FEA_AD_FlowLoad               = TestCase('pywrapper_CFD_AD_MeshDisp')
-    pywrapper_FEA_AD_FlowLoad.cfg_dir       = "py_wrapper/disc_adj_flow/mesh_disp_sens"
-    pywrapper_FEA_AD_FlowLoad.cfg_file      = "configAD_flow.cfg"
-    pywrapper_FEA_AD_FlowLoad.test_iter     = 1000
-    pywrapper_FEA_AD_FlowLoad.test_vals     = [30.000000, -2.518695, 1.390150, 0.000000] #last 4 columns
-    pywrapper_FEA_AD_FlowLoad.command       = TestCase.Command(exec = "python", param = "run_adjoint.py -f")
-    pywrapper_FEA_AD_FlowLoad.timeout       = 1600
-    pywrapper_FEA_AD_FlowLoad.tol           = 0.000001
-    pywrapper_FEA_AD_FlowLoad.new_output    = False
-    test_list.append(pywrapper_FEA_AD_FlowLoad)
-    pass_list.append(pywrapper_FEA_AD_FlowLoad.run_test())
+    pywrapper_CFD_AD_MeshDisp               = TestCase('pywrapper_CFD_AD_MeshDisp')
+    pywrapper_CFD_AD_MeshDisp.cfg_dir       = "py_wrapper/disc_adj_flow/mesh_disp_sens"
+    pywrapper_CFD_AD_MeshDisp.cfg_file      = "configAD_flow.cfg"
+    pywrapper_CFD_AD_MeshDisp.test_iter     = 1000
+    pywrapper_CFD_AD_MeshDisp.test_vals     = [30.000000, -2.518695, 1.390150, 0.000000] #last 4 columns
+    pywrapper_CFD_AD_MeshDisp.command       = TestCase.Command(exec = "python", param = "run_adjoint.py -f")
+    pywrapper_CFD_AD_MeshDisp.timeout       = 1600
+    pywrapper_CFD_AD_MeshDisp.tol           = 0.000001
+    pywrapper_CFD_AD_MeshDisp.new_output    = False
+    test_list.append(pywrapper_CFD_AD_MeshDisp)
+    pass_list.append(pywrapper_CFD_AD_MeshDisp.run_test())
 
 
     ###################################

From f3da57391998e843e11d2ef0207dad6a7725d81f Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Thu, 16 Mar 2023 17:10:10 +0100
Subject: [PATCH 285/656] Enable python wrapper for OpenMP builds.

---
 .github/workflows/regression.yml | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index aeb1c61ce51..76545cdb274 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -40,9 +40,9 @@ jobs:
           - config_set: BaseOMP
             flags: '-Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
           - config_set: ReverseOMP
-            flags: '-Denable-autodiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-tecio=false --warnlevel=3 --werror'
+            flags: '-Denable-autodiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
           - config_set: ForwardOMP
-            flags: '-Denable-directdiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-tecio=false --warnlevel=3 --werror'
+            flags: '-Denable-directdiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
     runs-on: ${{ inputs.runner || 'ubuntu-latest' }}
     steps:
       - name: Cache Object Files

From c6c650094685a7af322d2b31994622f2b13e2ce0 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Thu, 16 Mar 2023 18:42:23 +0100
Subject: [PATCH 286/656] Update regression test values.

---
 TestCases/hybrid_regression_AD.py | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/TestCases/hybrid_regression_AD.py b/TestCases/hybrid_regression_AD.py
index a24ddb5b051..bf8891e91d3 100644
--- a/TestCases/hybrid_regression_AD.py
+++ b/TestCases/hybrid_regression_AD.py
@@ -231,7 +231,7 @@ def main():
     pywrapper_FEA_AD_FlowLoad.cfg_dir       = "py_wrapper/disc_adj_fea/flow_load_sens"
     pywrapper_FEA_AD_FlowLoad.cfg_file      = "configAD_fem.cfg"
     pywrapper_FEA_AD_FlowLoad.test_iter     = 100
-    pywrapper_FEA_AD_FlowLoad.test_vals     = [-0.13945587401682674, -0.5859858866082689, -0.00036377840086080753, -0.00310056701747564] #last 4 columns
+    pywrapper_FEA_AD_FlowLoad.test_vals     = [-0.131742, -0.553318, -0.000364, -0.003101] #last 4 columns
     pywrapper_FEA_AD_FlowLoad.command       = TestCase.Command(exec = "python", param = "run_adjoint.py --parallel -f")
     pywrapper_FEA_AD_FlowLoad.timeout       = 1600
     pywrapper_FEA_AD_FlowLoad.tol           = 0.000001
@@ -244,7 +244,7 @@ def main():
     pywrapper_CFD_AD_MeshDisp.cfg_dir       = "py_wrapper/disc_adj_flow/mesh_disp_sens"
     pywrapper_CFD_AD_MeshDisp.cfg_file      = "configAD_flow.cfg"
     pywrapper_CFD_AD_MeshDisp.test_iter     = 1000
-    pywrapper_CFD_AD_MeshDisp.test_vals     = [30.000000, -2.5210057520523224, 1.3751902987065319, 0.000000] #last 4 columns
+    pywrapper_CFD_AD_MeshDisp.test_vals     = [30.000000, -2.520967, 1.375188, 0.000000] #last 4 columns
     pywrapper_CFD_AD_MeshDisp.command       = TestCase.Command(exec = "python", param = "run_adjoint.py --parallel -f")
     pywrapper_CFD_AD_MeshDisp.timeout       = 1600
     pywrapper_CFD_AD_MeshDisp.tol           = 0.000001

From 5ccf3f615618d6782144c2936b945b1b6bb511ac Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Thu, 16 Mar 2023 12:10:14 -0700
Subject: [PATCH 287/656] Update
 TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py

---
 TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py | 1 +
 1 file changed, 1 insertion(+)

diff --git a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
index 294d88cb48a..bf5aa2c1fdf 100755
--- a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
@@ -78,6 +78,7 @@ def main():
     MarkerID = allMarkerIDs[MarkerName]
 
   # Only print on the rank to which the marker belongs.
+  # WARNING: We only do this for the regression test, there is no guarantee that a marker will only belong to one rank.
 
   # Time loop is defined in Python so that we have acces to SU2 functionalities at each time step
   if MarkerID != None:

From c9903490cafa8329ef6c208de936f4fdc40abdf9 Mon Sep 17 00:00:00 2001
From: Kursat Yurt <kursatyurt@gmail.com>
Date: Thu, 16 Mar 2023 23:54:35 +0100
Subject: [PATCH 288/656] Add myself to authors

---
 AUTHORS.md | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/AUTHORS.md b/AUTHORS.md
index 85b2334d5e6..2c2c9d7982e 100644
--- a/AUTHORS.md
+++ b/AUTHORS.md
@@ -94,6 +94,7 @@ Johannes Blühdorn
 JonathanSmith1936
 Josy P. Pullockara
 Kedar Naik
+Kürşat Yurt
 LaSerpe
 Lennaert Tol
 Lisa Kusch
@@ -158,4 +159,3 @@ srcopela
 tobadavid
 vfrancesmolla
 ```
-

From 2afab593b719e4030ca8e73558e1fad0284ddef6 Mon Sep 17 00:00:00 2001
From: Kursat Yurt <kursatyurt@gmail.com>
Date: Thu, 16 Mar 2023 23:54:50 +0100
Subject: [PATCH 289/656] Add python style file

---
 .pep8 | 6 ++++++
 1 file changed, 6 insertions(+)
 create mode 100644 .pep8

diff --git a/.pep8 b/.pep8
new file mode 100644
index 00000000000..998b0179c80
--- /dev/null
+++ b/.pep8
@@ -0,0 +1,6 @@
+[pycodestyle]
+max_line_length = 120
+ignore = E402
+in-place = true
+aggressive = 2
+recursive = true

From b48fe3e25aeb35b998b31bd5f4c771ddff6a8a90 Mon Sep 17 00:00:00 2001
From: Kursat Yurt <kursatyurt@gmail.com>
Date: Thu, 16 Mar 2023 23:55:13 +0100
Subject: [PATCH 290/656] Never sort the includes

---
 .clang-format | 1 +
 1 file changed, 1 insertion(+)

diff --git a/.clang-format b/.clang-format
index a0cdb6fc60c..cb363900eb6 100644
--- a/.clang-format
+++ b/.clang-format
@@ -2,3 +2,4 @@ BasedOnStyle: Google
 PointerAlignment: Left
 DerivePointerAlignment: false
 ColumnLimit: 120
+SortIncludes: Never

From 1a832351364967c34579148d6b00ad2d0e22844d Mon Sep 17 00:00:00 2001
From: Kursat Yurt <kursatyurt@gmail.com>
Date: Thu, 16 Mar 2023 23:55:32 +0100
Subject: [PATCH 291/656] Add pre-commit hooks

---
 .github/pull_request_template.md |  3 +-
 .github/workflows/code-style.yml | 30 ++++++++++++++++
 .pre-commit-config.yaml          | 62 ++++++++++++++++++++++++++++++++
 3 files changed, 94 insertions(+), 1 deletion(-)
 create mode 100644 .github/workflows/code-style.yml
 create mode 100644 .pre-commit-config.yaml

diff --git a/.github/pull_request_template.md b/.github/pull_request_template.md
index 6aab0240f56..129fb1c1723 100644
--- a/.github/pull_request_template.md
+++ b/.github/pull_request_template.md
@@ -1,6 +1,6 @@
 ## Proposed Changes
 *Give a brief overview of your contribution here in a few sentences.*
- 
+
 
 
 ## Related Work
@@ -14,5 +14,6 @@
 - [ ] I am submitting my contribution to the develop branch.
 - [ ] My contribution generates no new compiler warnings (try with --warnlevel=3 when using meson).
 - [ ] My contribution is commented and consistent with SU2 style (https://su2code.github.io/docs_v7/Style-Guide/).
+- [ ] I used the pre-commit hook to prevent dirty commits and used `pre-commit run --all` to format old commits.
 - [ ] I have added a test case that demonstrates my contribution, if necessary.
 - [ ] I have updated appropriate documentation (Tutorials, Docs Page, config_template.cpp), if necessary.
diff --git a/.github/workflows/code-style.yml b/.github/workflows/code-style.yml
new file mode 100644
index 00000000000..a0080f08981
--- /dev/null
+++ b/.github/workflows/code-style.yml
@@ -0,0 +1,30 @@
+name: Code Style
+on:
+  pull_request:
+    paths:
+      - "**.[ch]pp"
+      - "**.[ch]"
+      - "**.cfg"
+      - "**.py"
+
+jobs:
+  formatting:
+    runs-on: ubuntu-latest
+    steps:
+      - name: Checkout
+        uses: actions/checkout@v3
+      - name: Setup python
+        uses: actions/setup-python@v4
+        with:
+         python-version: '3.10'
+         check-latest: true
+      - name: Install pre-commit
+        run: pip install pre-commit
+      - name: Run checks
+        run: pre-commit run -a -v
+      - name: Git status
+        if: always()
+        run: git status
+      - name: Full diff
+        if: always()
+        run: git diff
diff --git a/.pre-commit-config.yaml b/.pre-commit-config.yaml
new file mode 100644
index 00000000000..1e55bb83a10
--- /dev/null
+++ b/.pre-commit-config.yaml
@@ -0,0 +1,62 @@
+repos:
+  # Official repo for the clang-format hook
+  - repo: https://github.com/pre-commit/mirrors-clang-format
+    rev: "v15.0.7"
+    hooks:
+      - id: clang-format
+        exclude: |
+            (?x)^(
+            ^Common/include/CConfig.hpp|
+            ^Common/include/option_structure.hpp|
+            ^Common/src/CConfig.cpp|
+            ^SU2_CFD|
+            ^externals|
+            ^subprojects|
+            ^TestCases|
+            ^legacy
+            )
+        types_or: [c++, c]
+  # black repo for python formatting
+  - repo: https://github.com/ambv/black
+    rev: 22.6.0
+    hooks:
+      - id: black
+        exclude: |
+            (?x)^(
+            ^SU2_CFD|
+            ^externals|
+            ^subprojects|
+            ^TestCases|
+            ^legacy
+            )
+  # Official repo for default hooks
+  - repo: https://github.com/pre-commit/pre-commit-hooks
+    rev: "v4.4.0"
+    hooks:
+      - id: mixed-line-ending
+        exclude: |
+            (?x)^(
+            ^SU2_CFD|
+            ^externals|
+            ^subprojects|
+            ^TestCases|
+            ^legacy
+            )
+      - id: trailing-whitespace
+        exclude: |
+            (?x)^(
+            ^SU2_CFD|
+            ^externals|
+            ^subprojects|
+            ^TestCases|
+            ^legacy
+            )
+      - id: end-of-file-fixer
+        exclude: |
+            (?x)^(
+            ^SU2_CFD|
+            ^externals|
+            ^subprojects|
+            ^TestCases|
+            ^legacy
+            )

From 7c27b228b7247a55cf82cd4f38955024f5148651 Mon Sep 17 00:00:00 2001
From: Kursat Yurt <kursatyurt@gmail.com>
Date: Thu, 16 Mar 2023 23:56:03 +0100
Subject: [PATCH 292/656] Reformat files

---
 .github/ISSUE_TEMPLATE/bug_report.md          |     1 -
 .github/release.yml                           |     1 -
 .github/workflows/release-management.yml      |     1 -
 .lgtm.yml                                     |     2 +-
 .travis.yml                                   |     8 +-
 CODE_OF_CONDUCT.md                            |     5 +-
 COPYING                                       |    18 +-
 Common/include/adt/CADTBaseClass.hpp          |    30 +-
 Common/include/adt/CADTComparePointClass.hpp  |    21 +-
 Common/include/adt/CADTElemClass.hpp          |   162 +-
 Common/include/adt/CADTNodeClass.hpp          |    19 +-
 Common/include/adt/CADTPointsOnlyClass.hpp    |    33 +-
 Common/include/adt/CBBoxTargetClass.hpp       |    33 +-
 Common/include/basic_types/ad_structure.hpp   |   914 +-
 .../basic_types/datatype_structure.hpp        |   218 +-
 Common/include/code_config.hpp                |    36 +-
 Common/include/containers/C2DContainer.hpp    |   507 +-
 .../containers/CFastFindAndEraseQueue.hpp     |    23 +-
 Common/include/containers/CVertexMap.hpp      |    24 +-
 .../containers/container_decorators.hpp       |   126 +-
 Common/include/fem/fem_cgns_elements.hpp      |   313 +-
 .../fem/fem_gauss_jacobi_quadrature.hpp       |    25 +-
 Common/include/fem/fem_geometry_structure.hpp |   991 +-
 Common/include/fem/fem_standard_element.hpp   |  1296 +-
 .../fem/geometry_structure_fem_part.hpp       |   116 +-
 Common/include/geometry/CDummyGeometry.hpp    |     9 +-
 Common/include/geometry/CGeometry.hpp         |   760 +-
 .../include/geometry/CMultiGridGeometry.hpp   |    59 +-
 Common/include/geometry/CMultiGridQueue.hpp   |    23 +-
 Common/include/geometry/CPhysicalGeometry.hpp |   424 +-
 .../include/geometry/dual_grid/CDualGrid.hpp  |    25 +-
 Common/include/geometry/dual_grid/CEdge.hpp   |    57 +-
 Common/include/geometry/dual_grid/CPoint.hpp  |   261 +-
 .../geometry/dual_grid/CTurboVertex.hpp       |    49 +-
 Common/include/geometry/dual_grid/CVertex.hpp |    74 +-
 Common/include/geometry/elements/CElement.hpp |   519 +-
 .../geometry/elements/CElementProperty.hpp    |    49 +-
 .../geometry/elements/CGaussVariable.hpp      |    24 +-
 .../geometry/meshreader/CBoxMeshReaderFVM.hpp |    14 +-
 .../meshreader/CCGNSMeshReaderFVM.hpp         |    69 +-
 .../geometry/meshreader/CMeshReaderFVM.hpp    |    83 +-
 .../meshreader/CRectangularMeshReaderFVM.hpp  |    14 +-
 .../meshreader/CSU2ASCIIMeshReaderFVM.hpp     |    41 +-
 .../geometry/primal_grid/CHexahedron.hpp      |    17 +-
 Common/include/geometry/primal_grid/CLine.hpp |    14 +-
 .../geometry/primal_grid/CPrimalGrid.hpp      |    75 +-
 .../primal_grid/CPrimalGridBoundFEM.hpp       |    75 +-
 .../geometry/primal_grid/CPrimalGridFEM.hpp   |    74 +-
 .../include/geometry/primal_grid/CPrism.hpp   |    16 +-
 .../include/geometry/primal_grid/CPyramid.hpp |    42 +-
 .../geometry/primal_grid/CQuadrilateral.hpp   |    16 +-
 .../geometry/primal_grid/CTetrahedron.hpp     |    16 +-
 .../geometry/primal_grid/CTriangle.hpp        |    19 +-
 .../geometry/primal_grid/CVertexMPI.hpp       |     6 +-
 Common/include/graph_coloring_structure.hpp   |    10 +-
 .../grid_movement/CBSplineBlending.hpp        |    21 +-
 .../include/grid_movement/CBezierBlending.hpp |    16 +-
 .../grid_movement/CFreeFormBlending.hpp       |    20 +-
 .../include/grid_movement/CFreeFormDefBox.hpp |   298 +-
 .../include/grid_movement/CGridMovement.hpp   |    12 +-
 .../grid_movement/CSurfaceMovement.hpp        |   125 +-
 .../grid_movement/CVolumetricMovement.hpp     |   109 +-
 .../interface_interpolation/CInterpolator.hpp |    52 +-
 .../CInterpolatorFactory.hpp                  |     8 +-
 .../CIsoparametric.hpp                        |    27 +-
 .../interface_interpolation/CMirror.hpp       |     9 +-
 .../CNearestNeighbor.hpp                      |    11 +-
 .../CRadialBasisFunction.hpp                  |    33 +-
 .../interface_interpolation/CSlidingMesh.hpp  |    11 +-
 .../linear_algebra/CMatrixVectorProduct.hpp   |    32 +-
 .../include/linear_algebra/CPastixWrapper.hpp |    90 +-
 .../linear_algebra/CPreconditioner.hpp        |   137 +-
 Common/include/linear_algebra/CSysMatrix.hpp  |   429 +-
 Common/include/linear_algebra/CSysMatrix.inl  |   160 +-
 Common/include/linear_algebra/CSysSolve.hpp   |   136 +-
 Common/include/linear_algebra/CSysSolve_b.hpp |     7 +-
 Common/include/linear_algebra/CSysVector.hpp  |    13 +-
 .../include/linear_algebra/blas_structure.hpp |   192 +-
 .../linear_algebra/vector_expressions.hpp     |   142 +-
 Common/include/option_structure.inl           |  1044 +-
 .../include/parallelization/mpi_structure.cpp |    76 +-
 .../include/parallelization/mpi_structure.hpp |    12 +-
 .../include/parallelization/omp_structure.hpp |    80 +-
 .../parallelization/special_vectorization.hpp |    93 +-
 .../include/parallelization/vectorization.hpp |   244 +-
 Common/include/toolboxes/C1DInterpolation.hpp |    75 +-
 .../include/toolboxes/CLinearPartitioner.hpp  |    51 +-
 .../toolboxes/CQuasiNewtonInvLeastSquares.hpp |   100 +-
 Common/include/toolboxes/CSquareMatrixCM.hpp  |    34 +-
 Common/include/toolboxes/CSymmetricMatrix.hpp |    24 +-
 .../include/toolboxes/MMS/CIncTGVSolution.hpp |    25 +-
 .../toolboxes/MMS/CInviscidVortexSolution.hpp |    43 +-
 .../toolboxes/MMS/CMMSIncEulerSolution.hpp    |    39 +-
 .../toolboxes/MMS/CMMSIncNSSolution.hpp       |    41 +-
 .../MMS/CMMSNSTwoHalfCirclesSolution.hpp      |    53 +-
 .../MMS/CMMSNSTwoHalfSpheresSolution.hpp      |    55 +-
 .../toolboxes/MMS/CMMSNSUnitQuadSolution.hpp  |    87 +-
 .../MMS/CMMSNSUnitQuadSolutionWallBC.hpp      |    44 +-
 .../toolboxes/MMS/CNSUnitQuadSolution.hpp     |    29 +-
 .../toolboxes/MMS/CRinglebSolution.hpp        |    31 +-
 Common/include/toolboxes/MMS/CTGVSolution.hpp |    29 +-
 .../toolboxes/MMS/CUserDefinedSolution.hpp    |    23 +-
 .../toolboxes/MMS/CVerificationSolution.hpp   |    61 +-
 .../include/toolboxes/allocation_toolbox.hpp  |    31 +-
 Common/include/toolboxes/geometry_toolbox.hpp |   109 +-
 Common/include/toolboxes/graph_toolbox.hpp    |   383 +-
 Common/include/toolboxes/ndflattener.hpp      |    26 +-
 Common/include/toolboxes/printing_toolbox.hpp |   105 +-
 Common/include/wall_model.hpp                 |   103 +-
 Common/lib/Makefile.am                        |     1 -
 Common/src/adt/CADTBaseClass.cpp              |   115 +-
 Common/src/adt/CADTElemClass.cpp              |  2058 +--
 Common/src/adt/CADTPointsOnlyClass.cpp        |   130 +-
 Common/src/basic_types/ad_structure.cpp       |    30 +-
 Common/src/containers/CFileReaderLUT.cpp      |     7 +-
 Common/src/fem/fem_cgns_elements.cpp          |  1474 +-
 .../src/fem/fem_gauss_jacobi_quadrature.cpp   |   549 +-
 Common/src/fem/fem_geometry_structure.cpp     |  5126 +++---
 Common/src/fem/fem_integration_rules.cpp      | 12950 ++++++++++++----
 Common/src/fem/fem_standard_element.cpp       |  2782 ++--
 Common/src/fem/fem_wall_distance.cpp          |   182 +-
 Common/src/fem/fem_work_estimate_metis.cpp    |    22 +-
 .../src/fem/geometry_structure_fem_part.cpp   |  2913 ++--
 Common/src/geometry/CDummyGeometry.cpp        |    10 +-
 Common/src/geometry/CGeometry.cpp             |  2643 ++--
 Common/src/geometry/CMultiGridGeometry.cpp    |   423 +-
 Common/src/geometry/CMultiGridQueue.cpp       |    50 +-
 Common/src/geometry/CPhysicalGeometry.cpp     |  7524 +++++----
 Common/src/geometry/dual_grid/CDualGrid.cpp   |     2 +-
 Common/src/geometry/dual_grid/CEdge.cpp       |    49 +-
 Common/src/geometry/dual_grid/CPoint.cpp      |    46 +-
 .../src/geometry/dual_grid/CTurboVertex.cpp   |    15 +-
 Common/src/geometry/dual_grid/CVertex.cpp     |    22 +-
 Common/src/geometry/elements/CElement.cpp     |    22 +-
 Common/src/geometry/elements/CHEXA8.cpp       |   217 +-
 Common/src/geometry/elements/CLINE.cpp        |    22 +-
 Common/src/geometry/elements/CPRISM6.cpp      |   161 +-
 Common/src/geometry/elements/CPYRAM5.cpp      |   119 +-
 Common/src/geometry/elements/CPYRAM6.cpp      |   203 +-
 Common/src/geometry/elements/CQUAD4.cpp       |    70 +-
 Common/src/geometry/elements/CTETRA1.cpp      |    49 +-
 Common/src/geometry/elements/CTETRA4.cpp      |    68 +-
 Common/src/geometry/elements/CTRIA1.cpp       |    42 +-
 Common/src/geometry/elements/CTRIA3.cpp       |    48 +-
 .../geometry/meshreader/CBoxMeshReaderFVM.cpp |   157 +-
 .../meshreader/CCGNSMeshReaderFVM.cpp         |   530 +-
 .../geometry/meshreader/CMeshReaderFVM.cpp    |     9 +-
 .../meshreader/CRectangularMeshReaderFVM.cpp  |    81 +-
 .../meshreader/CSU2ASCIIMeshReaderFVM.cpp     |   498 +-
 Common/src/geometry/meson.build               |     1 -
 .../src/geometry/primal_grid/CHexahedron.cpp  |    22 +-
 Common/src/geometry/primal_grid/CLine.cpp     |     6 +-
 .../src/geometry/primal_grid/CPrimalGrid.cpp  |    14 +-
 .../primal_grid/CPrimalGridBoundFEM.cpp       |    60 +-
 .../geometry/primal_grid/CPrimalGridFEM.cpp   |   224 +-
 Common/src/geometry/primal_grid/CPrism.cpp    |     8 +-
 Common/src/geometry/primal_grid/CPyramid.cpp  |    12 +-
 .../geometry/primal_grid/CQuadrilateral.cpp   |    11 +-
 .../src/geometry/primal_grid/CTetrahedron.cpp |    11 +-
 Common/src/geometry/primal_grid/CTriangle.cpp |     6 +-
 .../src/geometry/primal_grid/CVertexMPI.cpp   |     4 +-
 Common/src/graph_coloring_structure.cpp       |   103 +-
 Common/src/grid_movement/CBSplineBlending.cpp |    96 +-
 Common/src/grid_movement/CBezierBlending.cpp  |    86 +-
 .../src/grid_movement/CFreeFormBlending.cpp   |     4 +-
 Common/src/grid_movement/CFreeFormDefBox.cpp  |   955 +-
 Common/src/grid_movement/CGridMovement.cpp    |     4 +-
 Common/src/grid_movement/CSurfaceMovement.cpp |  3226 ++--
 .../src/grid_movement/CVolumetricMovement.cpp |  1589 +-
 .../interface_interpolation/CInterpolator.cpp |     6 +-
 .../CInterpolatorFactory.cpp                  |    46 +-
 .../CIsoparametric.cpp                        |   291 +-
 .../src/interface_interpolation/CMirror.cpp   |    96 +-
 .../CNearestNeighbor.cpp                      |   143 +-
 .../CRadialBasisFunction.cpp                  |   393 +-
 .../interface_interpolation/CSlidingMesh.cpp  |   746 +-
 Common/src/linear_algebra/CPastixWrapper.cpp  |   230 +-
 Common/src/linear_algebra/CSysMatrix.cpp      |   636 +-
 Common/src/linear_algebra/CSysSolve.cpp       |   490 +-
 Common/src/linear_algebra/CSysSolve_b.cpp     |     9 +-
 Common/src/linear_algebra/CSysVector.cpp      |     2 +-
 Common/src/linear_algebra/blas_structure.cpp  |   101 +-
 Common/src/meson.build                        |    22 +-
 Common/src/toolboxes/C1DInterpolation.cpp     |   181 +-
 Common/src/toolboxes/CLinearPartitioner.cpp   |    31 +-
 Common/src/toolboxes/CSquareMatrixCM.cpp      |    54 +-
 Common/src/toolboxes/CSymmetricMatrix.cpp     |   103 +-
 Common/src/toolboxes/MMS/CIncTGVSolution.cpp  |    80 +-
 .../toolboxes/MMS/CInviscidVortexSolution.cpp |   131 +-
 .../toolboxes/MMS/CMMSIncEulerSolution.cpp    |    94 +-
 .../src/toolboxes/MMS/CMMSIncNSSolution.cpp   |   111 +-
 .../MMS/CMMSNSTwoHalfCirclesSolution.cpp      |   205 +-
 .../MMS/CMMSNSTwoHalfSpheresSolution.cpp      |   238 +-
 .../toolboxes/MMS/CMMSNSUnitQuadSolution.cpp  |   265 +-
 .../MMS/CMMSNSUnitQuadSolutionWallBC.cpp      |   147 +-
 .../src/toolboxes/MMS/CNSUnitQuadSolution.cpp |   103 +-
 Common/src/toolboxes/MMS/CRinglebSolution.cpp |   160 +-
 Common/src/toolboxes/MMS/CTGVSolution.cpp     |   112 +-
 .../toolboxes/MMS/CUserDefinedSolution.cpp    |    33 +-
 .../toolboxes/MMS/CVerificationSolution.cpp   |   119 +-
 .../CMMSIncEulerSolution.py                   |    29 +-
 .../CreateMMSSourceTerms/CMMSIncNSSolution.py |    38 +-
 .../CMMSNSTwoHalfCirclesSolution.mw           |     2 +-
 .../CMMSNSTwoHalfSpheresSolution.mw           |     2 +-
 .../CMMSNSUnitQuadSolution.mw                 |     2 +-
 .../CMMSNSUnitQuadSolutionWallBC.mw           |     2 +-
 Common/src/toolboxes/printing_toolbox.cpp     |    65 +-
 Common/src/wall_model.cpp                     |   304 +-
 Docs/docmain.hpp                              |     2 +-
 QuickStart/inv_NACA0012.cfg                   |     8 +-
 SU2_DEF/src/SU2_DEF.cpp                       |     1 -
 SU2_DEF/src/drivers/CDeformationDriver.cpp    |    90 +-
 .../src/drivers/CDiscAdjDeformationDriver.cpp |    32 +-
 SU2_DOT/src/SU2_DOT.cpp                       |     1 -
 SU2_GEO/include/SU2_GEO.hpp                   |     1 -
 SU2_GEO/src/SU2_GEO.cpp                       |  1363 +-
 SU2_GEO/src/meson.build                       |     2 +-
 SU2_IDE/Eclipse/README                        |    20 +-
 SU2_PY/FSI_tools/FSIInterface.py              |  3555 +++--
 SU2_PY/FSI_tools/FSI_config.py                |   103 +-
 SU2_PY/OptimalPropeller.py                    |   245 +-
 SU2_PY/SU2/__init__.py                        |    10 +-
 SU2_PY/SU2/eval/__init__.py                   |    17 +-
 SU2_PY/SU2/eval/design.py                     |   520 +-
 SU2_PY/SU2/eval/functions.py                  |   750 +-
 SU2_PY/SU2/eval/gradients.py                  |   915 +-
 SU2_PY/SU2/io/__init__.py                     |     8 +-
 SU2_PY/SU2/io/config.py                       |  1190 +-
 SU2_PY/SU2/io/config_options.py               |   187 +-
 SU2_PY/SU2/io/data.py                         |   403 +-
 SU2_PY/SU2/io/filelock.py                     |    81 +-
 SU2_PY/SU2/io/historyMap.py                   |  3491 +++--
 SU2_PY/SU2/io/redirect.py                     |   221 +-
 SU2_PY/SU2/io/state.py                        |   385 +-
 SU2_PY/SU2/io/tools.py                        |  1164 +-
 SU2_PY/SU2/opt/project.py                     |   394 +-
 SU2_PY/SU2/opt/scipy_tools.py                 |   494 +-
 SU2_PY/SU2/run/__init__.py                    |    19 +-
 SU2_PY/SU2/run/adjoint.py                     |    83 +-
 SU2_PY/SU2/run/deform.py                      |    78 +-
 SU2_PY/SU2/run/direct.py                      |   133 +-
 SU2_PY/SU2/run/geometry.py                    |    86 +-
 SU2_PY/SU2/run/interface.py                   |   199 +-
 SU2_PY/SU2/run/merge.py                       |    60 +-
 SU2_PY/SU2/run/projection.py                  |    89 +-
 SU2_PY/SU2/util/__init__.py                   |    14 +-
 SU2_PY/SU2/util/bunch.py                      |   497 +-
 SU2_PY/SU2/util/filter_adjoint.py             |   479 +-
 SU2_PY/SU2/util/lhc_unif.py                   |   112 +-
 SU2_PY/SU2/util/misc.py                       |    17 +-
 SU2_PY/SU2/util/mp_eval.py                    |   133 +-
 SU2_PY/SU2/util/ordered_bunch.py              |   516 +-
 SU2_PY/SU2/util/ordered_dict.py               |    82 +-
 SU2_PY/SU2/util/plot.py                       |    56 +-
 SU2_PY/SU2/util/polarSweepLib.py              |  1620 +-
 SU2_PY/SU2/util/switch.py                     |    58 +-
 SU2_PY/SU2/util/which.py                      |    21 +-
 SU2_PY/SU2_CFD.py                             |   188 +-
 SU2_PY/SU2_Nastran/pysu2_nastran.py           |  2013 +--
 SU2_PY/change_version_number.py               |    99 +-
 SU2_PY/compute_multipoint.py                  |    31 +-
 SU2_PY/compute_polar.py                       |   473 +-
 SU2_PY/compute_stability.py                   |    49 +-
 SU2_PY/compute_uncertainty.py                 |    96 +-
 SU2_PY/config_gui.py                          |   550 +-
 SU2_PY/continuous_adjoint.py                  |   113 +-
 SU2_PY/convert_to_csv.py                      |    31 +-
 SU2_PY/direct_differentiation.py              |   131 +-
 SU2_PY/discrete_adjoint.py                    |   193 +-
 SU2_PY/documentation.txt                      |    50 +-
 SU2_PY/finite_differences.py                  |   107 +-
 SU2_PY/fsi_computation.py                     |   354 +-
 SU2_PY/merge_solution.py                      |    30 +-
 SU2_PY/mesh_deformation.py                    |    39 +-
 SU2_PY/package_tests.py                       |   216 +-
 SU2_PY/parallel_computation.py                |    57 +-
 SU2_PY/parallel_computation_fsi.py            |    57 +-
 SU2_PY/parse_config.py                        |   469 +-
 SU2_PY/profiling.py                           |   107 +-
 SU2_PY/pySU2/numpy.i                          |     1 -
 SU2_PY/set_ffd_design_var.py                  |   564 +-
 SU2_PY/shape_optimization.py                  |   328 +-
 SU2_PY/topology_optimization.py               |   647 +-
 SU2_PY/updateHistoryMap.py                    |    89 +-
 SU2_SOL/include/SU2_SOL.hpp                   |     5 +-
 SU2_SOL/src/SU2_SOL.cpp                       |   558 +-
 .../Common/containers/CLookupTable_tests.cpp  |    36 +-
 UnitTests/Common/geometry/CGeometry_test.cpp  |    68 +-
 .../geometry/dual_grid/CDualGrid_tests.cpp    |    26 +-
 .../primal_grid/CPrimalGrid_tests.cpp         |    50 +-
 UnitTests/Common/simple_ad_test.cpp           |     5 +-
 UnitTests/Common/simple_directdiff_test.cpp   |     4 +-
 .../toolboxes/C1DInterpolation_tests.cpp      |    18 +-
 .../CQuasiNewtonInvLeastSquares_tests.cpp     |    32 +-
 .../Common/toolboxes/ndflattener_tests.cpp    |   118 +-
 UnitTests/Common/vectorization.cpp            |    35 +-
 UnitTests/SU2_CFD/gradients.cpp               |    35 +-
 .../SU2_CFD/numerics/CNumerics_tests.cpp      |    12 +-
 UnitTests/SU2_CFD/windowing.cpp               |     8 +-
 UnitTests/UnitQuadTestCase.hpp                |     6 +-
 UnitTests/test_driver.cpp                     |     3 +-
 docker/build/Dockerfile                       |     2 +-
 docker/build/compileSU2.sh                    |     8 +-
 docker/test/runTests.sh                       |     5 +-
 doxyfile                                      |     4 +-
 meson.py                                      |    45 +-
 meson_scripts/check_dir.py                    |    14 +-
 meson_scripts/extract_file.py                 |   106 +-
 meson_scripts/init.py                         |   463 +-
 preconfigure.py                               |   208 +-
 310 files changed, 52115 insertions(+), 43626 deletions(-)

diff --git a/.github/ISSUE_TEMPLATE/bug_report.md b/.github/ISSUE_TEMPLATE/bug_report.md
index 4f53a6d0449..13c3dd26f57 100644
--- a/.github/ISSUE_TEMPLATE/bug_report.md
+++ b/.github/ISSUE_TEMPLATE/bug_report.md
@@ -26,4 +26,3 @@ assignees: ''
  - C++ compiler and version: [e.g., g++ (GCC) 4.8.5]
  - MPI implementation and version: [e.g., OpenMPI 3.0.0]
  - SU2 Version: [e.g., v6.2.0]
-
diff --git a/.github/release.yml b/.github/release.yml
index 4ec929fc17c..09557097401 100644
--- a/.github/release.yml
+++ b/.github/release.yml
@@ -17,4 +17,3 @@ changelog:
       - title: 'Other Changes'
         labels:
           - "*"
-
diff --git a/.github/workflows/release-management.yml b/.github/workflows/release-management.yml
index 0babf1c46b2..46a618f9a6c 100644
--- a/.github/workflows/release-management.yml
+++ b/.github/workflows/release-management.yml
@@ -65,4 +65,3 @@ jobs:
           asset_path: ${{matrix.os_bin}}.zip
           asset_name: SU2-${{ steps.update_release.outputs.tagname }}-${{matrix.os_bin}}.zip
           asset_content_type: application/zip
-
diff --git a/.lgtm.yml b/.lgtm.yml
index 8489adfaea0..2179d4ea710 100644
--- a/.lgtm.yml
+++ b/.lgtm.yml
@@ -1,7 +1,7 @@
 extraction:
   cpp:
      prepare:
-        packages: 
+        packages:
           - libboost-all-dev
      configure:
         command:
diff --git a/.travis.yml b/.travis.yml
index 28481849073..f10e08bc47f 100644
--- a/.travis.yml
+++ b/.travis.yml
@@ -6,10 +6,10 @@ sudo: required
 
 language: c++
 
-cache: 
+cache:
     - ccache
     - pip
-    - directories: 
+    - directories:
       - $HOME/.pyenv_cache
 
 compiler:
@@ -19,7 +19,7 @@ notifications:
     email:
         recipients:
             - su2code-dev@lists.stanford.edu
-  
+
 branches:
     only:
         - develop
@@ -81,7 +81,7 @@ before_script:
 
     # Get the tutorial cases
     - git clone --depth=1 -b develop https://github.com/su2code/su2code.github.io ./Tutorials
-    
+
     # Enter the SU2/TestCases/ directory, which is now ready to run
     - cd TestCases/
 
diff --git a/CODE_OF_CONDUCT.md b/CODE_OF_CONDUCT.md
index 174a61f6120..c22c88372a9 100644
--- a/CODE_OF_CONDUCT.md
+++ b/CODE_OF_CONDUCT.md
@@ -28,7 +28,7 @@ Examples of unacceptable behavior by participants include:
 * Trolling, insulting/derogatory comments, and personal or political attacks.
 * Public or private harassment.
 * Publishing others' private information, such as a physical or electronic
-  address, without explicit permission. 
+  address, without explicit permission.
 * Other conduct which could reasonably be considered inappropriate in a
   professional setting.
 
@@ -67,7 +67,7 @@ faith may face temporary or permanent repercussions as determined by other
 members of the project's leadership.
 
 Consequences may include:
-* Downgrade or removal of repository permissions such as admin and write 
+* Downgrade or removal of repository permissions such as admin and write
   permissions.
 * Removal from the su2code organization on Github.
 * Being blocked from the su2code repository.
@@ -79,4 +79,3 @@ This Code of Conduct is adapted from the [Contributor Covenant][homepage], versi
 available at https://www.contributor-covenant.org/version/1/4/code-of-conduct.html
 
 [homepage]: https://www.contributor-covenant.org
-
diff --git a/COPYING b/COPYING
index fe17b67bd4e..20fb9c7da21 100644
--- a/COPYING
+++ b/COPYING
@@ -55,7 +55,7 @@ modified by someone else and passed on, the recipients should know
 that what they have is not the original version, so that the original
 author's reputation will not be affected by problems that might be
 introduced by others.
-
+
   Finally, software patents pose a constant threat to the existence of
 any free program.  We wish to make sure that a company cannot
 effectively restrict the users of a free program by obtaining a
@@ -111,7 +111,7 @@ modification follow.  Pay close attention to the difference between a
 "work based on the library" and a "work that uses the library".  The
 former contains code derived from the library, whereas the latter must
 be combined with the library in order to run.
-
+
                   GNU LESSER GENERAL PUBLIC LICENSE
    TERMS AND CONDITIONS FOR COPYING, DISTRIBUTION AND MODIFICATION
 
@@ -158,7 +158,7 @@ Library.
   You may charge a fee for the physical act of transferring a copy,
 and you may at your option offer warranty protection in exchange for a
 fee.
-
+
   2. You may modify your copy or copies of the Library or any portion
 of it, thus forming a work based on the Library, and copy and
 distribute such modifications or work under the terms of Section 1
@@ -216,7 +216,7 @@ instead of to this License.  (If a newer version than version 2 of the
 ordinary GNU General Public License has appeared, then you can specify
 that version instead if you wish.)  Do not make any other change in
 these notices.
-
+
   Once this change is made in a given copy, it is irreversible for
 that copy, so the ordinary GNU General Public License applies to all
 subsequent copies and derivative works made from that copy.
@@ -267,7 +267,7 @@ Library will still fall under Section 6.)
 distribute the object code for the work under the terms of Section 6.
 Any executables containing that work also fall under Section 6,
 whether or not they are linked directly with the Library itself.
-
+
   6. As an exception to the Sections above, you may also combine or
 link a "work that uses the Library" with the Library to produce a
 work containing portions of the Library, and distribute that work
@@ -329,7 +329,7 @@ restrictions of other proprietary libraries that do not normally
 accompany the operating system.  Such a contradiction means you cannot
 use both them and the Library together in an executable that you
 distribute.
-
+
   7. You may place library facilities that are a work based on the
 Library side-by-side in a single library together with other library
 facilities not covered by this License, and distribute such a combined
@@ -370,7 +370,7 @@ subject to these terms and conditions.  You may not impose any further
 restrictions on the recipients' exercise of the rights granted herein.
 You are not responsible for enforcing compliance by third parties with
 this License.
-
+
   11. If, as a consequence of a court judgment or allegation of patent
 infringement or for any other reason (not limited to patent issues),
 conditions are imposed on you (whether by court order, agreement or
@@ -422,7 +422,7 @@ conditions either of that version or of any later version published by
 the Free Software Foundation.  If the Library does not specify a
 license version number, you may choose any version ever published by
 the Free Software Foundation.
-
+
   14. If you wish to incorporate parts of the Library into other free
 programs whose distribution conditions are incompatible with these,
 write to the author to ask for permission.  For software which is
@@ -455,4 +455,4 @@ FAILURE OF THE LIBRARY TO OPERATE WITH ANY OTHER SOFTWARE), EVEN IF
 SUCH HOLDER OR OTHER PARTY HAS BEEN ADVISED OF THE POSSIBILITY OF SUCH
 DAMAGES.
 
-                     END OF TERMS AND CONDITIONS
\ No newline at end of file
+                     END OF TERMS AND CONDITIONS
diff --git a/Common/include/adt/CADTBaseClass.hpp b/Common/include/adt/CADTBaseClass.hpp
index e1c95a5cc42..9a10f9fce54 100644
--- a/Common/include/adt/CADTBaseClass.hpp
+++ b/Common/include/adt/CADTBaseClass.hpp
@@ -43,10 +43,10 @@ using namespace std;
  * \author E. van der Weide
  */
 class CADTBaseClass {
-protected:
-  unsigned long  nLeaves;   /*!< \brief Number of leaves in the ADT. */
-  unsigned short nDimADT;   /*!< \brief Number of dimensions of the ADT. */
-  bool           isEmpty;   /*!< \brief Whether or not the ADT is empty. */
+ protected:
+  unsigned long nLeaves;  /*!< \brief Number of leaves in the ADT. */
+  unsigned short nDimADT; /*!< \brief Number of dimensions of the ADT. */
+  bool isEmpty;           /*!< \brief Whether or not the ADT is empty. */
 
   vector<CADTNodeClass> leaves; /*!< \brief Vector, which contains all the leaves of the ADT. */
 
@@ -54,23 +54,23 @@ class CADTBaseClass {
   vector<vector<unsigned long> > FrontLeaves;    /*!< \brief Vector used in the tree traversal. */
   vector<vector<unsigned long> > FrontLeavesNew; /*!< \brief Vector used in the tree traversal. */
 #else
-  array<vector<unsigned long>,1> FrontLeaves;
-  array<vector<unsigned long>,1> FrontLeavesNew;
+  array<vector<unsigned long>, 1> FrontLeaves;
+  array<vector<unsigned long>, 1> FrontLeavesNew;
 #endif
-private:
+ private:
   vector<su2double> coorMinLeaves; /*!< \brief Vector, which contains all the minimum coordinates
                                                of the leaves. */
   vector<su2double> coorMaxLeaves; /*!< \brief Vector, which contains all the maximum coordinates
                                                of the leaves. */
-protected:
+ protected:
   /*!
    * \brief Constructor of the class. Nothing to be done.
    */
   CADTBaseClass() = default;
 
   /*--- Disable copy operations ---*/
-  CADTBaseClass(const CADTBaseClass &) = delete;
-  CADTBaseClass& operator=(const CADTBaseClass &) = delete;
+  CADTBaseClass(const CADTBaseClass&) = delete;
+  CADTBaseClass& operator=(const CADTBaseClass&) = delete;
 
   /*!
    * \brief Function, which builds the ADT of the given coordinates.
@@ -78,16 +78,12 @@ class CADTBaseClass {
    * \param[in] nPoints Number of points present in the ADT.
    * \param[in] coor    Coordinates of the points.
    */
-  void BuildADT(unsigned short  nDim,
-                unsigned long   nPoints,
-                const su2double *coor);
-
-public:
+  void BuildADT(unsigned short nDim, unsigned long nPoints, const su2double* coor);
 
+ public:
   /*!
    * \brief Function, which returns whether or not the ADT is empty.
    * \return  Whether or not the ADT is empty.
    */
-  inline bool IsEmpty(void) const { return isEmpty;}
-
+  inline bool IsEmpty(void) const { return isEmpty; }
 };
diff --git a/Common/include/adt/CADTComparePointClass.hpp b/Common/include/adt/CADTComparePointClass.hpp
index 542ab2612bc..5457241b839 100644
--- a/Common/include/adt/CADTComparePointClass.hpp
+++ b/Common/include/adt/CADTComparePointClass.hpp
@@ -35,35 +35,32 @@
  * \author E. van der Weide
  */
 class CADTComparePointClass {
-private:
-  const su2double      *pointCoor;      /*!< \brief Pointer to the coordinates of the points. */
-  const unsigned short splitDirection;  /*!< \brief Split direction used in the sorting. */
-  const unsigned short nDim;            /*!< \brief Number of spatial dimensions stored in the coordinates. */
+ private:
+  const su2double* pointCoor;          /*!< \brief Pointer to the coordinates of the points. */
+  const unsigned short splitDirection; /*!< \brief Split direction used in the sorting. */
+  const unsigned short nDim;           /*!< \brief Number of spatial dimensions stored in the coordinates. */
 
-public:
+ public:
   /*!
    * \brief Constructor of the class. The member variables are initialized.
    * \param[in] coor      Pointer to the coordinates of the points.
    * \param[in] splitDir  Direction that must be used to sort the coordinates.
    * \param[in] nDimADT   Number of spatial dimensions of the ADT and coordinates.
    */
-  CADTComparePointClass(const su2double      *coor,
-                        const unsigned short splitDir,
-                        const unsigned short nDimADT) : pointCoor(coor), splitDirection(splitDir), nDim(nDimADT) {}
+  CADTComparePointClass(const su2double* coor, const unsigned short splitDir, const unsigned short nDimADT)
+      : pointCoor(coor), splitDirection(splitDir), nDim(nDimADT) {}
 
   /*!
    * \brief Operator used for the sorting of the points.
    * \param[in] p0  Index of the first point to be compared.
    * \param[in] p1  Index of the second point to be compared.
    */
-  inline bool operator()(const unsigned long p0,
-                         const unsigned long p1) const {
-    return pointCoor[nDim*p0+splitDirection] < pointCoor[nDim*p1+splitDirection];
+  inline bool operator()(const unsigned long p0, const unsigned long p1) const {
+    return pointCoor[nDim * p0 + splitDirection] < pointCoor[nDim * p1 + splitDirection];
   }
 
   /*!
    * \brief Default constructor of the class, disabled.
    */
   CADTComparePointClass() = delete;
-
 };
diff --git a/Common/include/adt/CADTElemClass.hpp b/Common/include/adt/CADTElemClass.hpp
index 1537385ca51..dd0b862be60 100644
--- a/Common/include/adt/CADTElemClass.hpp
+++ b/Common/include/adt/CADTElemClass.hpp
@@ -39,13 +39,13 @@
  * \version 7.5.1 "Blackbird"
  */
 class CADTElemClass : public CADTBaseClass {
-private:
+ private:
   unsigned short nDim; /*!< \brief Number of spatial dimensions. */
 
-  vector<su2double>     coorPoints;    /*!< \brief Vector, which contains the coordinates
-                                                   of the points in the ADT. */
-  vector<su2double>     BBoxCoor;      /*!< \brief Vector, which contains the coordinates
-                                                   of the bounding boxes of the elements. */
+  vector<su2double> coorPoints; /*!< \brief Vector, which contains the coordinates
+                                            of the points in the ADT. */
+  vector<su2double> BBoxCoor;   /*!< \brief Vector, which contains the coordinates
+                                            of the bounding boxes of the elements. */
 
   vector<unsigned short> elemVTK_Type; /*!< \brief Vector, which the type of the elements
                                                    using the VTK convention. */
@@ -58,15 +58,15 @@ class CADTElemClass : public CADTBaseClass {
                                                    of the elements in the ADT. */
   vector<unsigned long> localElemIDs;  /*!< \brief Vector, which contains the local element ID's
                                                    of the elements in the ADT. */
-  vector<int>           ranksOfElems;  /*!< \brief Vector, which contains the ranks
+  vector<int> ranksOfElems;            /*!< \brief Vector, which contains the ranks
                                                    of the elements in the ADT. */
 #ifdef HAVE_OMP
-  vector<vector<CBBoxTargetClass> >BBoxTargets; /*!< \brief Vector, used to store possible bounding box
-                                                            candidates during the nearest element search. */
+  vector<vector<CBBoxTargetClass> > BBoxTargets; /*!< \brief Vector, used to store possible bounding box
+                                                             candidates during the nearest element search. */
 #else
-  array<vector<CBBoxTargetClass>,1> BBoxTargets;
+  array<vector<CBBoxTargetClass>, 1> BBoxTargets;
 #endif
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in]     val_nDim     Number of spatial dimensions of the problem.
@@ -80,13 +80,9 @@ class CADTElemClass : public CADTBaseClass {
    * \param[in]     globalTree   Whether or not a global tree must be built. If false
                                  a local ADT is built.
    */
-  CADTElemClass(unsigned short         val_nDim,
-                vector<su2double>      &val_coor,
-                vector<unsigned long>  &val_connElem,
-                vector<unsigned short> &val_VTKElem,
-                vector<unsigned short> &val_markerID,
-                vector<unsigned long>  &val_elemID,
-                const bool             globalTree);
+  CADTElemClass(unsigned short val_nDim, vector<su2double>& val_coor, vector<unsigned long>& val_connElem,
+                vector<unsigned short>& val_VTKElem, vector<unsigned short>& val_markerID,
+                vector<unsigned long>& val_elemID, const bool globalTree);
 
   /*!
    * \brief Function, which determines the element that contains the given coordinate.
@@ -102,15 +98,11 @@ class CADTElemClass : public CADTBaseClass {
                                   which contains the coordinate.
    * \return                      True if an element is found, false if not.
    */
-  inline bool DetermineContainingElement(const su2double *coor,
-                                         unsigned short  &markerID,
-                                         unsigned long   &elemID,
-                                         int             &rankID,
-                                         su2double       *parCoor,
-                                         su2double       *weightsInterpol) {
+  inline bool DetermineContainingElement(const su2double* coor, unsigned short& markerID, unsigned long& elemID,
+                                         int& rankID, su2double* parCoor, su2double* weightsInterpol) {
     const auto iThread = omp_get_thread_num();
-    return DetermineContainingElement_impl(FrontLeaves[iThread], FrontLeavesNew[iThread],
-                                coor, markerID, elemID, rankID, parCoor, weightsInterpol);
+    return DetermineContainingElement_impl(FrontLeaves[iThread], FrontLeavesNew[iThread], coor, markerID, elemID,
+                                           rankID, parCoor, weightsInterpol);
   }
 
   /*!
@@ -123,42 +115,29 @@ class CADTElemClass : public CADTBaseClass {
    * \param[out] elemID   Local element ID of the nearest element in the ADT.
    * \param[out] rankID   Rank on which the nearest element in the ADT is stored.
    */
-  inline void DetermineNearestElement(const su2double *coor,
-                                      su2double       &dist,
-                                      unsigned short  &markerID,
-                                      unsigned long   &elemID,
-                                      int             &rankID) {
+  inline void DetermineNearestElement(const su2double* coor, su2double& dist, unsigned short& markerID,
+                                      unsigned long& elemID, int& rankID) {
     const auto iThread = omp_get_thread_num();
-    DetermineNearestElement_impl(BBoxTargets[iThread], FrontLeaves[iThread],
-              FrontLeavesNew[iThread], coor, dist, markerID, elemID, rankID);
+    DetermineNearestElement_impl(BBoxTargets[iThread], FrontLeaves[iThread], FrontLeavesNew[iThread], coor, dist,
+                                 markerID, elemID, rankID);
   }
 
-private:
+ private:
   /*!
    * \brief Implementation of DetermineContainingElement.
    * \note Working variables (first two) passed explicitly for thread safety.
    */
-  bool DetermineContainingElement_impl(vector<unsigned long>& frontLeaves,
-                                       vector<unsigned long>& frontLeavesNew,
-                                       const su2double *coor,
-                                       unsigned short  &markerID,
-                                       unsigned long   &elemID,
-                                       int             &rankID,
-                                       su2double       *parCoor,
-                                       su2double       *weightsInterpol) const;
+  bool DetermineContainingElement_impl(vector<unsigned long>& frontLeaves, vector<unsigned long>& frontLeavesNew,
+                                       const su2double* coor, unsigned short& markerID, unsigned long& elemID,
+                                       int& rankID, su2double* parCoor, su2double* weightsInterpol) const;
 
   /*!
    * \brief Implementation of DetermineNearestElement.
    * \note Working variables (first three) passed explicitly for thread safety.
    */
-  void DetermineNearestElement_impl(vector<CBBoxTargetClass>& BBoxTargets,
-                                    vector<unsigned long>& frontLeaves,
-                                    vector<unsigned long>& frontLeavesNew,
-                                    const su2double *coor,
-                                    su2double       &dist,
-                                    unsigned short  &markerID,
-                                    unsigned long   &elemID,
-                                    int             &rankID) const;
+  void DetermineNearestElement_impl(vector<CBBoxTargetClass>& BBoxTargets, vector<unsigned long>& frontLeaves,
+                                    vector<unsigned long>& frontLeavesNew, const su2double* coor, su2double& dist,
+                                    unsigned short& markerID, unsigned long& elemID, int& rankID) const;
 
   /*!
    * \brief Function, which checks whether or not the given coordinate is
@@ -172,10 +151,8 @@ class CADTElemClass : public CADTBaseClass {
                                  given element.
    * \return                     True if coor is inside the element and false otherwise.
    */
-  bool CoorInElement(const unsigned long elemID,
-                     const su2double     *coor,
-                     su2double           *parCoor,
-                     su2double           *weightsInterpol) const;
+  bool CoorInElement(const unsigned long elemID, const su2double* coor, su2double* parCoor,
+                     su2double* weightsInterpol) const;
 
   /*!
    * \brief Function, which checks whether or not the given coordinate is
@@ -189,10 +166,8 @@ class CADTElemClass : public CADTBaseClass {
                                  given quadrilateral.
    * \return                     True if coor is inside the quadrilateral and false otherwise.
    */
-  bool CoorInQuadrilateral(const unsigned long elemID,
-                           const su2double     *coor,
-                           su2double           *parCoor,
-                           su2double           *weightsInterpol) const;
+  bool CoorInQuadrilateral(const unsigned long elemID, const su2double* coor, su2double* parCoor,
+                           su2double* weightsInterpol) const;
 
   /*!
    * \brief Function, which checks whether or not the given coordinate is
@@ -206,10 +181,8 @@ class CADTElemClass : public CADTBaseClass {
                                  given triangle.
    * \return                     True if coor is inside the triangle and false otherwise.
    */
-  bool CoorInTriangle(const unsigned long elemID,
-                      const su2double     *coor,
-                      su2double           *parCoor,
-                      su2double           *weightsInterpol) const;
+  bool CoorInTriangle(const unsigned long elemID, const su2double* coor, su2double* parCoor,
+                      su2double* weightsInterpol) const;
 
   /*!
    * \brief Function, which checks whether or not the given coordinate is
@@ -223,10 +196,8 @@ class CADTElemClass : public CADTBaseClass {
                                  given hexahedron.
    * \return                     True if coor is inside the hexahedron and false otherwise.
    */
-  bool CoorInHexahedron(const unsigned long elemID,
-                        const su2double     *coor,
-                        su2double           *parCoor,
-                        su2double           *weightsInterpol) const;
+  bool CoorInHexahedron(const unsigned long elemID, const su2double* coor, su2double* parCoor,
+                        su2double* weightsInterpol) const;
 
   /*!
    * \brief Function, which checks whether or not the given coordinate is
@@ -240,10 +211,8 @@ class CADTElemClass : public CADTBaseClass {
                                  given prism.
    * \return                     True if coor is inside the prism and false otherwise.
    */
-  bool CoorInPrism(const unsigned long elemID,
-                   const su2double     *coor,
-                   su2double           *parCoor,
-                   su2double           *weightsInterpol) const;
+  bool CoorInPrism(const unsigned long elemID, const su2double* coor, su2double* parCoor,
+                   su2double* weightsInterpol) const;
 
   /*!
    * \brief Function, which checks whether or not the given coordinate is
@@ -257,10 +226,8 @@ class CADTElemClass : public CADTBaseClass {
                                  given pyramid.
    * \return                     True if coor is inside the pyramid and false otherwise.
    */
-  bool CoorInPyramid(const unsigned long elemID,
-                     const su2double     *coor,
-                     su2double           *parCoor,
-                     su2double           *weightsInterpol) const;
+  bool CoorInPyramid(const unsigned long elemID, const su2double* coor, su2double* parCoor,
+                     su2double* weightsInterpol) const;
 
   /*!
    * \brief Function, which checks whether or not the given coordinate is
@@ -274,10 +241,8 @@ class CADTElemClass : public CADTBaseClass {
                                  given tetrahedron.
    * \return                     True if coor is inside the tetrahedron and false otherwise.
    */
-  bool CoorInTetrahedron(const unsigned long elemID,
-                         const su2double     *coor,
-                         su2double           *parCoor,
-                         su2double           *weightsInterpol) const;
+  bool CoorInTetrahedron(const unsigned long elemID, const su2double* coor, su2double* parCoor,
+                         su2double* weightsInterpol) const;
 
   /*!
    * \brief Function, which provides an initial guess for the parametric coordinates
@@ -290,9 +255,8 @@ class CADTElemClass : public CADTBaseClass {
    * \return             True if the initial guess is within the hexahedron and
                          false otherwise.
    */
-  bool InitialGuessContainmentHexahedron(const su2double xRelC[3],
-                                         const su2double xRel[8][3],
-                                         su2double       *parCoor) const;
+  bool InitialGuessContainmentHexahedron(const su2double xRelC[3], const su2double xRel[8][3],
+                                         su2double* parCoor) const;
 
   /*!
    * \brief Function, which provides an initial guess for the parametric coordinates
@@ -305,9 +269,7 @@ class CADTElemClass : public CADTBaseClass {
    * \return             True if the initial guess is within the prism and
                          false otherwise.
    */
-  bool InitialGuessContainmentPrism(const su2double xRelC[3],
-                                    const su2double xRel[6][3],
-                                    su2double       *parCoor) const;
+  bool InitialGuessContainmentPrism(const su2double xRelC[3], const su2double xRel[6][3], su2double* parCoor) const;
 
   /*!
    * \brief Function, which provides an initial guess for the parametric coordinates
@@ -320,9 +282,7 @@ class CADTElemClass : public CADTBaseClass {
    * \return             True if the initial guess is within the pyramid and
                          false otherwise.
    */
-  bool InitialGuessContainmentPyramid(const su2double xRelC[3],
-                                      const su2double xRel[5][3],
-                                      su2double       *parCoor) const;
+  bool InitialGuessContainmentPyramid(const su2double xRelC[3], const su2double xRel[5][3], su2double* parCoor) const;
 
   /*!
    * \brief Function, which computes the distance squared of the given coordinate
@@ -331,9 +291,7 @@ class CADTElemClass : public CADTBaseClass {
    * \param[in]  coor      Coordinate for which the distance to the element must be determined.
    * \param[out] dist2Elem Distance squared from the coordinate to the element.
    */
-  void Dist2ToElement(const unsigned long elemID,
-                      const su2double     *coor,
-                      su2double           &dist2Elem) const;
+  void Dist2ToElement(const unsigned long elemID, const su2double* coor, su2double& dist2Elem) const;
   /*!
    * \brief Function, which computes the distance squared of the given coordinate
             to a linear line element.
@@ -344,10 +302,7 @@ class CADTElemClass : public CADTBaseClass {
    * \param[in]  coor      Coordinate for which the distance to the line must be determined.
    * \param[out] dist2Line Distance squared from the coordinate to the line.
    */
-  void Dist2ToLine(const unsigned long i0,
-                   const unsigned long i1,
-                   const su2double     *coor,
-                   su2double           &dist2Line) const;
+  void Dist2ToLine(const unsigned long i0, const unsigned long i1, const su2double* coor, su2double& dist2Line) const;
   /*!
    * \brief Function, which computes the distance squared of the given coordinate
             to a linear quadrilateral element if the projection is inside the quad.
@@ -366,14 +321,9 @@ class CADTElemClass : public CADTBaseClass {
    * \param[out] dist2Quad Distance squared from the coordinate to the quadrilateral.
    * \return     True if the projection is inside the quadrilateral and false otherwise.
    */
-  bool Dist2ToQuadrilateral(const unsigned long i0,
-                            const unsigned long i1,
-                            const unsigned long i2,
-                            const unsigned long i3,
-                            const su2double     *coor,
-                            su2double           &r,
-                            su2double           &s,
-                            su2double           &dist2Quad) const;
+  bool Dist2ToQuadrilateral(const unsigned long i0, const unsigned long i1, const unsigned long i2,
+                            const unsigned long i3, const su2double* coor, su2double& r, su2double& s,
+                            su2double& dist2Quad) const;
   /*!
    * \brief Function, which computes the distance squared of the given coordinate
             to a linear triangular element if the projection is inside the triangle.
@@ -389,16 +339,10 @@ class CADTElemClass : public CADTBaseClass {
    * \param[out] s         Parametric coordinate of the projection.
    * \return     True if the projection is inside the triangle and false otherwise.
    */
-  bool Dist2ToTriangle(const unsigned long i0,
-                       const unsigned long i1,
-                       const unsigned long i2,
-                       const su2double     *coor,
-                       su2double           &dist2Tria,
-                       su2double           &r,
-                       su2double           &s) const;
+  bool Dist2ToTriangle(const unsigned long i0, const unsigned long i1, const unsigned long i2, const su2double* coor,
+                       su2double& dist2Tria, su2double& r, su2double& s) const;
   /*!
    * \brief Default constructor of the class, disabled.
    */
   CADTElemClass() = delete;
-
 };
diff --git a/Common/include/adt/CADTNodeClass.hpp b/Common/include/adt/CADTNodeClass.hpp
index d6f1a30bcf2..28ac30696c6 100644
--- a/Common/include/adt/CADTNodeClass.hpp
+++ b/Common/include/adt/CADTNodeClass.hpp
@@ -35,15 +35,14 @@
  * \author E. van der Weide
  */
 struct CADTNodeClass {
+  bool childrenAreTerminal[2]; /*!< \brief Whether or not the child leaves are terminal. */
+  unsigned long children[2];   /*!< \brief Child leaves. If childrenAreTerminal is true the children
+                                           contain the point ID's or bounding box ID's. Note that it
+                                           is allowed that one child is termimal and the other is not. */
+  unsigned long centralNodeID; /*!< \brief ID of a node, which is near the center of the leaf. */
 
-  bool          childrenAreTerminal[2];  /*!< \brief Whether or not the child leaves are terminal. */
-  unsigned long children[2];             /*!< \brief Child leaves. If childrenAreTerminal is true the children
-                                                     contain the point ID's or bounding box ID's. Note that it
-                                                     is allowed that one child is termimal and the other is not. */
-  unsigned long centralNodeID;           /*!< \brief ID of a node, which is near the center of the leaf. */
-
-  su2double *xMin;  /*!< \brief The minimum coordinates of this leaf. It points to a position in the large
-                                vector, which contains the coordinates of all leaves. */
-  su2double *xMax;  /*!< \brief The maximum coordinates of this leaf. It points to a position in the large
-                                vector, which contains the coordinates of all leaves. */
+  su2double* xMin; /*!< \brief The minimum coordinates of this leaf. It points to a position in the large
+                               vector, which contains the coordinates of all leaves. */
+  su2double* xMax; /*!< \brief The maximum coordinates of this leaf. It points to a position in the large
+                               vector, which contains the coordinates of all leaves. */
 };
diff --git a/Common/include/adt/CADTPointsOnlyClass.hpp b/Common/include/adt/CADTPointsOnlyClass.hpp
index 68f7d3c26ed..ba5f38adc49 100644
--- a/Common/include/adt/CADTPointsOnlyClass.hpp
+++ b/Common/include/adt/CADTPointsOnlyClass.hpp
@@ -35,14 +35,14 @@
  * \author E. van der Weide
  */
 class CADTPointsOnlyClass : public CADTBaseClass {
-private:
-  vector<su2double>     coorPoints;    /*!< \brief Vector, which contains the coordinates
+ private:
+  vector<su2double> coorPoints;        /*!< \brief Vector, which contains the coordinates
                                                    of the points in the ADT. */
   vector<unsigned long> localPointIDs; /*!< \brief Vector, which contains the local point ID's
                                                    of the points in the ADT. */
-  vector<int>           ranksOfPoints; /*!< \brief Vector, which contains the ranks
+  vector<int> ranksOfPoints;           /*!< \brief Vector, which contains the ranks
                                                    of the points in the ADT. */
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] nDim       Number of spatial dimensions of the problem.
@@ -52,11 +52,8 @@ class CADTPointsOnlyClass : public CADTBaseClass {
    * \param[in] globalTree Whether or not a global tree must be built. If false
                            a local ADT is built.
    */
-  CADTPointsOnlyClass(unsigned short nDim,
-                      unsigned long  nPoints,
-                      const su2double *coor,
-                      const unsigned long *pointID,
-                      const bool     globalTree);
+  CADTPointsOnlyClass(unsigned short nDim, unsigned long nPoints, const su2double* coor, const unsigned long* pointID,
+                      const bool globalTree);
 
   /*!
    * \brief Function, which determines the nearest node in the ADT for the given coordinate.
@@ -67,13 +64,9 @@ class CADTPointsOnlyClass : public CADTBaseClass {
    * \param[out] pointID Local point ID of the nearest node in the ADT.
    * \param[out] rankID  Rank on which the nearest node in the ADT is stored.
    */
-  inline void DetermineNearestNode(const su2double *coor,
-                                   su2double       &dist,
-                                   unsigned long   &pointID,
-                                   int             &rankID) {
+  inline void DetermineNearestNode(const su2double* coor, su2double& dist, unsigned long& pointID, int& rankID) {
     const auto iThread = omp_get_thread_num();
-    DetermineNearestNode_impl(FrontLeaves[iThread], FrontLeavesNew[iThread],
-                              coor, dist, pointID, rankID);
+    DetermineNearestNode_impl(FrontLeaves[iThread], FrontLeavesNew[iThread], coor, dist, pointID, rankID);
   }
 
   /*!
@@ -81,15 +74,11 @@ class CADTPointsOnlyClass : public CADTBaseClass {
    */
   CADTPointsOnlyClass() = delete;
 
-private:
+ private:
   /*!
    * \brief Implementation of DetermineNearestNode.
    * \note Working variables (first two) passed explicitly for thread safety.
    */
-  void DetermineNearestNode_impl(vector<unsigned long>& frontLeaves,
-                                 vector<unsigned long>& frontLeavesNew,
-                                 const su2double *coor,
-                                 su2double       &dist,
-                                 unsigned long   &pointID,
-                                 int             &rankID) const;
+  void DetermineNearestNode_impl(vector<unsigned long>& frontLeaves, vector<unsigned long>& frontLeavesNew,
+                                 const su2double* coor, su2double& dist, unsigned long& pointID, int& rankID) const;
 };
diff --git a/Common/include/adt/CBBoxTargetClass.hpp b/Common/include/adt/CBBoxTargetClass.hpp
index 1a7cf37d132..405a9956e98 100644
--- a/Common/include/adt/CBBoxTargetClass.hpp
+++ b/Common/include/adt/CBBoxTargetClass.hpp
@@ -38,12 +38,11 @@
  * \version 7.5.1 "Blackbird"
  */
 struct CBBoxTargetClass {
-
-  unsigned long boundingBoxID;      /*!< \brief Corresponding bounding box ID. */
-  su2double     possibleMinDist2;   /*!< \brief Possible minimimum distance squared to the
-                                                given coordinate. */
-  su2double     guaranteedMinDist2; /*!< \brief Guaranteed minimum distance squared to the
-                                                given coordinate. */
+  unsigned long boundingBoxID;  /*!< \brief Corresponding bounding box ID. */
+  su2double possibleMinDist2;   /*!< \brief Possible minimimum distance squared to the
+                                            given coordinate. */
+  su2double guaranteedMinDist2; /*!< \brief Guaranteed minimum distance squared to the
+                                            given coordinate. */
 
   /*!
    * \brief Constructor of the class. Nothing to be done.
@@ -58,27 +57,21 @@ struct CBBoxTargetClass {
    * \param[in] val_guarDist2 - Guaranteed minimum distance squared to the target
                                 for this bounding box.
    */
-  inline CBBoxTargetClass(const unsigned long val_BBoxID,
-                          const su2double     val_posDist2,
-                          const su2double     val_guarDist2)
-                          : boundingBoxID(val_BBoxID),
-                            possibleMinDist2(val_posDist2),
-                            guaranteedMinDist2(val_guarDist2) {}
+  inline CBBoxTargetClass(const unsigned long val_BBoxID, const su2double val_posDist2, const su2double val_guarDist2)
+      : boundingBoxID(val_BBoxID), possibleMinDist2(val_posDist2), guaranteedMinDist2(val_guarDist2) {}
 
   /*!
    * \brief Less than operator. Needed for the sorting of the candidates.
    * \param[in] other  Object to which the current object must be compared.
    */
-  inline bool operator <(const CBBoxTargetClass &other) const{
-
+  inline bool operator<(const CBBoxTargetClass& other) const {
     /* Make sure that the bounding boxes with the smallest possible distances
        are stored first. */
-    if(possibleMinDist2   < other.possibleMinDist2)   return true;
-    if(possibleMinDist2   > other.possibleMinDist2)   return false;
-    if(guaranteedMinDist2 < other.guaranteedMinDist2) return true;
-    if(guaranteedMinDist2 > other.guaranteedMinDist2) return false;
-    if(boundingBoxID      < other.boundingBoxID)      return true;
+    if (possibleMinDist2 < other.possibleMinDist2) return true;
+    if (possibleMinDist2 > other.possibleMinDist2) return false;
+    if (guaranteedMinDist2 < other.guaranteedMinDist2) return true;
+    if (guaranteedMinDist2 > other.guaranteedMinDist2) return false;
+    if (boundingBoxID < other.boundingBoxID) return true;
     return false;
   }
-
 };
diff --git a/Common/include/basic_types/ad_structure.hpp b/Common/include/basic_types/ad_structure.hpp
index 445cf7c2269..c3ba75d9204 100644
--- a/Common/include/basic_types/ad_structure.hpp
+++ b/Common/include/basic_types/ad_structure.hpp
@@ -36,542 +36,534 @@
  * In case there is no reverse type configured, they have no effect at all,
  * and so the real versions of the routined are after #else.
  */
-namespace AD{
+namespace AD {
 #ifndef CODI_REVERSE_TYPE
-  /*!
-   * \brief Start the recording of the operations and involved variables.
-   * If called, the computational graph of all operations occuring after the call will be stored,
-   * starting with the variables registered with RegisterInput.
-   */
-  inline void StartRecording() {}
-
-  /*!
-   * \brief Stops the recording of the operations and variables.
-   */
-  inline void StopRecording() {}
-
-  /*!
-   * \brief Check if the tape is active
-   * \param[out] Boolean which determines whether the tape is active.
-   */
-  inline bool TapeActive() {return false;}
-
-  /*!
-   * \brief Prints out tape statistics.
-   */
-  inline void PrintStatistics() {}
-
-  /*!
-   * \brief Registers the variable as an input and saves internal data (indices). I.e. as a leaf of the computational graph.
-   * \param[in] data - The variable to be registered as input.
-   * \param[in] push_index - boolean whether we also want to push the index.
-   */
-  inline void RegisterInput(su2double &data, bool push_index = true) {}
-
-  /*!
-   * \brief Registers the variable as an output. I.e. as the root of the computational graph.
-   * \param[in] data - The variable to be registered as output.
-   */
-  inline void RegisterOutput(su2double &data) {}
-
-  /*!
-   * \brief Sets the adjoint value at index to val
-   * \param[in] index - Position in the adjoint vector.
-   * \param[in] val - adjoint value to be set.
-   */
-  inline void SetDerivative(int index, const double val) {}
-
-  /*!
-   * \brief Extracts the adjoint value at index
-   * \param[in] index - position in the adjoint vector where the derivative will be extracted.
-   * \return Derivative value.
-   */
-  inline double GetDerivative(int index) {return 0.0;}
-
-  /*!
-   * \brief Clears the currently stored adjoints but keeps the computational graph.
-   */
-  inline void ClearAdjoints() {}
-
-  /*!
-   * \brief Computes the adjoints, i.e. the derivatives of the output with respect to the input variables.
-   */
-  inline void ComputeAdjoint() {}
-
-  /*!
-   * \brief Computes the adjoints, i.e. the derivatives of the output with respect to the input variables.
-   * \param[in] enter - Position where we start evaluating the tape.
-   * \param[in] leave - Position where we stop evaluating the tape.
-   */
-  inline void ComputeAdjoint(unsigned short enter, unsigned short leave) {}
-
-  /*!
-   * \brief Computes the adjoints, i.e., the derivatives of the output with respect to the input variables, using forward tape evaluation.
-   */
-  inline void ComputeAdjointForward() {}
-
-  /*!
-   * \brief Reset the tape structure to be ready for a new recording.
-   */
-  inline void Reset() {}
-
-  /*!
-   * \brief Reset the variable (set index to zero).
-   * \param[in] data - the variable to be unregistered from the tape.
-   */
-  inline void ResetInput(su2double &data) {}
-
-  /*!
-   * \brief Sets the scalar inputs of a preaccumulation section.
-   * \param[in] data - the scalar input variables.
-   */
-  template<class... Ts>
-  inline void SetPreaccIn(Ts&&... data) {}
-
-  /*!
-   * \brief Sets the input variables of a preaccumulation section using a 1D array.
-   * \param[in] data - the input 1D array.
-   * \param[in] size - size of the array.
-   */
-  template<class T>
-  inline void SetPreaccIn(const T& data, const int size) {}
-
-  /*!
-   * \brief Sets the input variables of a preaccumulation section using a 2D array.
-   * \param[in] data - the input 2D array.
-   * \param[in] size_x - size of the array in x dimension.
-   * \param[in] size_y - size of the array in y dimension.
-   */
-  template<class T>
-  inline void SetPreaccIn(const T& data, const int size_x, const int size_y) {}
-
-  /*!
-   * \brief Starts a new preaccumulation section and sets the input variables.
-   *
-   * The idea of preaccumulation is to store only the Jacobi matrix of a code section during
-   * the taping process instead of all operations. This decreases the tape size and reduces runtime.
-   *
-   * Input/Output of the section are set with several calls to SetPreaccIn()/SetPreaccOut().
-   *
-   * Note: the call of this routine must be followed by a call of EndPreacc() and the end of the code section.
-   */
-  inline void StartPreacc() {}
-
-  /*!
-   * \brief Sets the scalar outputs of a preaccumulation section.
-   * \param[in] data - the scalar output variables.
-   */
-  template<class... Ts>
-  inline void SetPreaccOut(Ts&&... data) {}
-
-  /*!
-   * \brief Sets the output variables of a preaccumulation section using a 1D array.
-   * \param[in] data - the output 1D array.
-   */
-  template<class T>
-  inline void SetPreaccOut(T&& data, const int size) {}
-
-  /*!
-   * \brief Sets the input variables of a preaccumulation section using a 2D array.
-   * \param[in] data - the output 1D array.
-   */
-  template<class T>
-  inline void SetPreaccOut(T&& data, const int size_x, const int size_y) {}
-
-  /*!
-   * \brief Ends a preaccumulation section and computes the local Jacobi matrix
-   * of a code section using the variables set with SetLocalInput(), SetLocalOutput() and pushes a statement
-   * for each output variable to the AD tape.
-   */
-  inline void EndPreacc() {}
-
-  /*!
-   * \brief Sets the scalar input of a externally differentiated function.
-   * \param[in] data - the scalar input variable.
-   */
-  inline void SetExtFuncIn(su2double &data) {}
-
-  /*!
-   * \brief Sets the input variables of a externally differentiated function using a 1D array.
-   * \param[in] data - the input 1D array.
-   * \param[in] size - number of rows.
-   */
-  template<class T>
-  inline void SetExtFuncIn(const T& data, const int size) {}
-
-  /*!
-  * \brief  Sets the input variables of a externally differentiated function using a 2D array.
-  * \param[in] data - the input 2D array.
-  * \param[in] size_x - number of rows.
-  * \param[in] size_y - number of columns.
-  */
-  template<class T>
-  inline void SetExtFuncIn(const T& data, const int size_x, const int size_y) {}
-
-  /*!
-   * \brief Sets the scalar output of a externally differentiated function.
-   * \param[in] data - the scalar output variable.
-   */
-  inline void SetExtFuncOut(su2double &data) {}
-
-  /*!
-   * \brief Sets the output variables of a externally differentiated function using a 1D array.
-   * \param[in] data - the output 1D array.
-   * \param[in] size - number of rows.
-   */
-  template<class T>
-  inline void SetExtFuncOut(T&& data, const int size) {}
-
-  /*!
-  * \brief  Sets the output variables of a externally differentiated function using a 2D array.
-  * \param[in] data - the output 2D array.
-  * \param[in] size_x - number of rows.
-  * \param[in] size_y - number of columns.
-  */
-  template<class T>
-  inline void SetExtFuncOut(T&& data, const int size_x, const int size_y) {}
-
-  /*!
-   * \brief Evaluates and saves gradient data from a variable.
-   * \param[in] data - variable whose gradient information will be extracted.
-   * \param[in] index - where obtained gradient information will be stored.
-   */
-  inline void SetIndex(int &index, const su2double &data) {}
-
-  /*!
-   * \brief Pushes back the current tape position to the tape position's vector.
-   */
-  inline void Push_TapePosition() {}
-
-  /*!
-   * \brief Start a passive region, i.e. stop recording.
-   * \return True if tape was active.
-   */
-  inline bool BeginPassive() { return false; }
-
-  /*!
-   * \brief End a passive region, i.e. start recording if we were recording before.
-   * \param[in] wasActive - Whether we were recording before entering the passive region.
-   */
-  inline void EndPassive(bool wasActive) {}
-
-  /*!
-   * \brief Pause the use of preaccumulation.
-   * \return True if preaccumulation was active.
-   */
-  inline bool PausePreaccumulation() { return false; }
-
-  /*!
-   * \brief Resume the use of preaccumulation.
-   * \param[in] wasActive - Whether preaccumulation was active before pausing.
-   */
-  inline void ResumePreaccumulation(bool wasActive) {}
-
-  /*!
-   * \brief Begin a hybrid parallel adjoint evaluation mode that assumes an inherently safe reverse path.
-   */
-  inline void StartNoSharedReading() {}
-
-  /*!
-   * \brief End the "no shared reading" adjoint evaluation mode.
-   */
-  inline void EndNoSharedReading() {}
+/*!
+ * \brief Start the recording of the operations and involved variables.
+ * If called, the computational graph of all operations occuring after the call will be stored,
+ * starting with the variables registered with RegisterInput.
+ */
+inline void StartRecording() {}
+
+/*!
+ * \brief Stops the recording of the operations and variables.
+ */
+inline void StopRecording() {}
+
+/*!
+ * \brief Check if the tape is active
+ * \param[out] Boolean which determines whether the tape is active.
+ */
+inline bool TapeActive() { return false; }
+
+/*!
+ * \brief Prints out tape statistics.
+ */
+inline void PrintStatistics() {}
+
+/*!
+ * \brief Registers the variable as an input and saves internal data (indices). I.e. as a leaf of the computational
+ * graph. \param[in] data - The variable to be registered as input. \param[in] push_index - boolean whether we also want
+ * to push the index.
+ */
+inline void RegisterInput(su2double& data, bool push_index = true) {}
+
+/*!
+ * \brief Registers the variable as an output. I.e. as the root of the computational graph.
+ * \param[in] data - The variable to be registered as output.
+ */
+inline void RegisterOutput(su2double& data) {}
+
+/*!
+ * \brief Sets the adjoint value at index to val
+ * \param[in] index - Position in the adjoint vector.
+ * \param[in] val - adjoint value to be set.
+ */
+inline void SetDerivative(int index, const double val) {}
+
+/*!
+ * \brief Extracts the adjoint value at index
+ * \param[in] index - position in the adjoint vector where the derivative will be extracted.
+ * \return Derivative value.
+ */
+inline double GetDerivative(int index) { return 0.0; }
+
+/*!
+ * \brief Clears the currently stored adjoints but keeps the computational graph.
+ */
+inline void ClearAdjoints() {}
+
+/*!
+ * \brief Computes the adjoints, i.e. the derivatives of the output with respect to the input variables.
+ */
+inline void ComputeAdjoint() {}
+
+/*!
+ * \brief Computes the adjoints, i.e. the derivatives of the output with respect to the input variables.
+ * \param[in] enter - Position where we start evaluating the tape.
+ * \param[in] leave - Position where we stop evaluating the tape.
+ */
+inline void ComputeAdjoint(unsigned short enter, unsigned short leave) {}
+
+/*!
+ * \brief Computes the adjoints, i.e., the derivatives of the output with respect to the input variables, using forward
+ * tape evaluation.
+ */
+inline void ComputeAdjointForward() {}
+
+/*!
+ * \brief Reset the tape structure to be ready for a new recording.
+ */
+inline void Reset() {}
+
+/*!
+ * \brief Reset the variable (set index to zero).
+ * \param[in] data - the variable to be unregistered from the tape.
+ */
+inline void ResetInput(su2double& data) {}
+
+/*!
+ * \brief Sets the scalar inputs of a preaccumulation section.
+ * \param[in] data - the scalar input variables.
+ */
+template <class... Ts>
+inline void SetPreaccIn(Ts&&... data) {}
+
+/*!
+ * \brief Sets the input variables of a preaccumulation section using a 1D array.
+ * \param[in] data - the input 1D array.
+ * \param[in] size - size of the array.
+ */
+template <class T>
+inline void SetPreaccIn(const T& data, const int size) {}
+
+/*!
+ * \brief Sets the input variables of a preaccumulation section using a 2D array.
+ * \param[in] data - the input 2D array.
+ * \param[in] size_x - size of the array in x dimension.
+ * \param[in] size_y - size of the array in y dimension.
+ */
+template <class T>
+inline void SetPreaccIn(const T& data, const int size_x, const int size_y) {}
+
+/*!
+ * \brief Starts a new preaccumulation section and sets the input variables.
+ *
+ * The idea of preaccumulation is to store only the Jacobi matrix of a code section during
+ * the taping process instead of all operations. This decreases the tape size and reduces runtime.
+ *
+ * Input/Output of the section are set with several calls to SetPreaccIn()/SetPreaccOut().
+ *
+ * Note: the call of this routine must be followed by a call of EndPreacc() and the end of the code section.
+ */
+inline void StartPreacc() {}
+
+/*!
+ * \brief Sets the scalar outputs of a preaccumulation section.
+ * \param[in] data - the scalar output variables.
+ */
+template <class... Ts>
+inline void SetPreaccOut(Ts&&... data) {}
+
+/*!
+ * \brief Sets the output variables of a preaccumulation section using a 1D array.
+ * \param[in] data - the output 1D array.
+ */
+template <class T>
+inline void SetPreaccOut(T&& data, const int size) {}
+
+/*!
+ * \brief Sets the input variables of a preaccumulation section using a 2D array.
+ * \param[in] data - the output 1D array.
+ */
+template <class T>
+inline void SetPreaccOut(T&& data, const int size_x, const int size_y) {}
+
+/*!
+ * \brief Ends a preaccumulation section and computes the local Jacobi matrix
+ * of a code section using the variables set with SetLocalInput(), SetLocalOutput() and pushes a statement
+ * for each output variable to the AD tape.
+ */
+inline void EndPreacc() {}
+
+/*!
+ * \brief Sets the scalar input of a externally differentiated function.
+ * \param[in] data - the scalar input variable.
+ */
+inline void SetExtFuncIn(su2double& data) {}
+
+/*!
+ * \brief Sets the input variables of a externally differentiated function using a 1D array.
+ * \param[in] data - the input 1D array.
+ * \param[in] size - number of rows.
+ */
+template <class T>
+inline void SetExtFuncIn(const T& data, const int size) {}
+
+/*!
+ * \brief  Sets the input variables of a externally differentiated function using a 2D array.
+ * \param[in] data - the input 2D array.
+ * \param[in] size_x - number of rows.
+ * \param[in] size_y - number of columns.
+ */
+template <class T>
+inline void SetExtFuncIn(const T& data, const int size_x, const int size_y) {}
+
+/*!
+ * \brief Sets the scalar output of a externally differentiated function.
+ * \param[in] data - the scalar output variable.
+ */
+inline void SetExtFuncOut(su2double& data) {}
+
+/*!
+ * \brief Sets the output variables of a externally differentiated function using a 1D array.
+ * \param[in] data - the output 1D array.
+ * \param[in] size - number of rows.
+ */
+template <class T>
+inline void SetExtFuncOut(T&& data, const int size) {}
+
+/*!
+ * \brief  Sets the output variables of a externally differentiated function using a 2D array.
+ * \param[in] data - the output 2D array.
+ * \param[in] size_x - number of rows.
+ * \param[in] size_y - number of columns.
+ */
+template <class T>
+inline void SetExtFuncOut(T&& data, const int size_x, const int size_y) {}
+
+/*!
+ * \brief Evaluates and saves gradient data from a variable.
+ * \param[in] data - variable whose gradient information will be extracted.
+ * \param[in] index - where obtained gradient information will be stored.
+ */
+inline void SetIndex(int& index, const su2double& data) {}
+
+/*!
+ * \brief Pushes back the current tape position to the tape position's vector.
+ */
+inline void Push_TapePosition() {}
+
+/*!
+ * \brief Start a passive region, i.e. stop recording.
+ * \return True if tape was active.
+ */
+inline bool BeginPassive() { return false; }
+
+/*!
+ * \brief End a passive region, i.e. start recording if we were recording before.
+ * \param[in] wasActive - Whether we were recording before entering the passive region.
+ */
+inline void EndPassive(bool wasActive) {}
+
+/*!
+ * \brief Pause the use of preaccumulation.
+ * \return True if preaccumulation was active.
+ */
+inline bool PausePreaccumulation() { return false; }
+
+/*!
+ * \brief Resume the use of preaccumulation.
+ * \param[in] wasActive - Whether preaccumulation was active before pausing.
+ */
+inline void ResumePreaccumulation(bool wasActive) {}
+
+/*!
+ * \brief Begin a hybrid parallel adjoint evaluation mode that assumes an inherently safe reverse path.
+ */
+inline void StartNoSharedReading() {}
+
+/*!
+ * \brief End the "no shared reading" adjoint evaluation mode.
+ */
+inline void EndNoSharedReading() {}
 
 #else
-  using CheckpointHandler = codi::ExternalFunctionUserData;
+using CheckpointHandler = codi::ExternalFunctionUserData;
 
-  using Tape = su2double::Tape;
+using Tape = su2double::Tape;
 
 #ifdef HAVE_OPDI
-  using ExtFuncHelper = codi::OpenMPExternalFunctionHelper<su2double>;
+using ExtFuncHelper = codi::OpenMPExternalFunctionHelper<su2double>;
 #else
-  using ExtFuncHelper = codi::ExternalFunctionHelper<su2double>;
+using ExtFuncHelper = codi::ExternalFunctionHelper<su2double>;
 #endif
 
-  extern ExtFuncHelper FuncHelper;
+extern ExtFuncHelper FuncHelper;
 
-  extern bool PreaccActive;
+extern bool PreaccActive;
 #ifdef HAVE_OPDI
-  SU2_OMP(threadprivate(PreaccActive))
+SU2_OMP(threadprivate(PreaccActive))
 #endif
 
-  extern bool PreaccEnabled;
+extern bool PreaccEnabled;
 
 #ifdef HAVE_OPDI
-  using CoDiTapePosition = Tape::Position;
-  using OpDiState = void*;
-  using TapePosition = std::pair<CoDiTapePosition, OpDiState>;
+using CoDiTapePosition = Tape::Position;
+using OpDiState = void*;
+using TapePosition = std::pair<CoDiTapePosition, OpDiState>;
 #else
-  using TapePosition = Tape::Position;
+using TapePosition = Tape::Position;
 #endif
 
-  extern TapePosition StartPosition, EndPosition;
+extern TapePosition StartPosition, EndPosition;
 
-  extern std::vector<TapePosition> TapePositions;
+extern std::vector<TapePosition> TapePositions;
 
-  extern codi::PreaccumulationHelper<su2double> PreaccHelper;
+extern codi::PreaccumulationHelper<su2double> PreaccHelper;
 #ifdef HAVE_OPDI
-  SU2_OMP(threadprivate(PreaccHelper))
+SU2_OMP(threadprivate(PreaccHelper))
 #endif
 
-  /*--- Reference to the tape. ---*/
+/*--- Reference to the tape. ---*/
 
-  FORCEINLINE Tape& getTape() {return su2double::getTape();}
+FORCEINLINE Tape& getTape() { return su2double::getTape(); }
 
-  FORCEINLINE void RegisterInput(su2double &data) {AD::getTape().registerInput(data);}
+FORCEINLINE void RegisterInput(su2double& data) { AD::getTape().registerInput(data); }
 
-  FORCEINLINE void RegisterOutput(su2double& data) {AD::getTape().registerOutput(data);}
+FORCEINLINE void RegisterOutput(su2double& data) { AD::getTape().registerOutput(data); }
 
-  FORCEINLINE void ResetInput(su2double &data) {data = data.getValue();}
+FORCEINLINE void ResetInput(su2double& data) { data = data.getValue(); }
 
-  FORCEINLINE void StartRecording() {AD::getTape().setActive();}
+FORCEINLINE void StartRecording() { AD::getTape().setActive(); }
 
-  FORCEINLINE void StopRecording() {AD::getTape().setPassive();}
+FORCEINLINE void StopRecording() { AD::getTape().setPassive(); }
 
-  FORCEINLINE bool TapeActive() { return AD::getTape().isActive(); }
+FORCEINLINE bool TapeActive() { return AD::getTape().isActive(); }
 
-  FORCEINLINE void PrintStatistics() {AD::getTape().printStatistics();}
+FORCEINLINE void PrintStatistics() { AD::getTape().printStatistics(); }
 
-  FORCEINLINE void ClearAdjoints() {AD::getTape().clearAdjoints(); }
+FORCEINLINE void ClearAdjoints() { AD::getTape().clearAdjoints(); }
 
-  FORCEINLINE void ComputeAdjoint() {
-  #if defined(HAVE_OPDI)
-    opdi::logic->prepareEvaluate();
-  #endif
-    AD::getTape().evaluate();
-  }
+FORCEINLINE void ComputeAdjoint() {
+#if defined(HAVE_OPDI)
+  opdi::logic->prepareEvaluate();
+#endif
+  AD::getTape().evaluate();
+}
 
-  FORCEINLINE void ComputeAdjoint(unsigned short enter, unsigned short leave) {
-  #if defined(HAVE_OPDI)
-    opdi::logic->recoverState(TapePositions[enter].second);
-    opdi::logic->prepareEvaluate();
-    AD::getTape().evaluate(TapePositions[enter].first, TapePositions[leave].first);
-  #else
-    AD::getTape().evaluate(TapePositions[enter], TapePositions[leave]);
-  #endif
-  }
+FORCEINLINE void ComputeAdjoint(unsigned short enter, unsigned short leave) {
+#if defined(HAVE_OPDI)
+  opdi::logic->recoverState(TapePositions[enter].second);
+  opdi::logic->prepareEvaluate();
+  AD::getTape().evaluate(TapePositions[enter].first, TapePositions[leave].first);
+#else
+  AD::getTape().evaluate(TapePositions[enter], TapePositions[leave]);
+#endif
+}
 
-  FORCEINLINE void ComputeAdjointForward() {AD::getTape().evaluateForward();}
-
-  FORCEINLINE void Reset() {
-    AD::getTape().reset();
-  #if defined(HAVE_OPDI)
-    opdi::logic->reset();
-  #endif
-    if (TapePositions.size() != 0) {
-    #if defined(HAVE_OPDI)
-      for (TapePosition& pos : TapePositions) {
-        opdi::logic->freeState(pos.second);
-      }
-    #endif
-      TapePositions.clear();
+FORCEINLINE void ComputeAdjointForward() { AD::getTape().evaluateForward(); }
+
+FORCEINLINE void Reset() {
+  AD::getTape().reset();
+#if defined(HAVE_OPDI)
+  opdi::logic->reset();
+#endif
+  if (TapePositions.size() != 0) {
+#if defined(HAVE_OPDI)
+    for (TapePosition& pos : TapePositions) {
+      opdi::logic->freeState(pos.second);
     }
+#endif
+    TapePositions.clear();
   }
+}
 
-  FORCEINLINE void SetIndex(int &index, const su2double &data) {
-    index = data.getIdentifier();
-  }
+FORCEINLINE void SetIndex(int& index, const su2double& data) { index = data.getIdentifier(); }
 
-  FORCEINLINE void SetDerivative(int index, const double val) {
-    AD::getTape().setGradient(index, val);
-  }
+FORCEINLINE void SetDerivative(int index, const double val) { AD::getTape().setGradient(index, val); }
 
-  FORCEINLINE double GetDerivative(int index) {
-    return AD::getTape().getGradient(index);
-  }
+FORCEINLINE double GetDerivative(int index) { return AD::getTape().getGradient(index); }
 
-  FORCEINLINE bool IsIdentifierActive(su2double const& value) {
-    return getTape().isIdentifierActive(value.getIdentifier());
-  }
+FORCEINLINE bool IsIdentifierActive(su2double const& value) {
+  return getTape().isIdentifierActive(value.getIdentifier());
+}
 
-  /*--- Base case for parameter pack expansion. ---*/
-  FORCEINLINE void SetPreaccIn() {}
+/*--- Base case for parameter pack expansion. ---*/
+FORCEINLINE void SetPreaccIn() {}
 
-  template<class T, class... Ts, su2enable_if<std::is_same<T,su2double>::value> = 0>
-  FORCEINLINE void SetPreaccIn(const T& data, Ts&&... moreData) {
-    if (!PreaccActive) return;
-    if (IsIdentifierActive(data))
-      PreaccHelper.addInput(data);
-    SetPreaccIn(moreData...);
-  }
+template <class T, class... Ts, su2enable_if<std::is_same<T, su2double>::value> = 0>
+FORCEINLINE void SetPreaccIn(const T& data, Ts&&... moreData) {
+  if (!PreaccActive) return;
+  if (IsIdentifierActive(data)) PreaccHelper.addInput(data);
+  SetPreaccIn(moreData...);
+}
 
-  template<class T, class... Ts, su2enable_if<std::is_same<T,su2double>::value> = 0>
-  FORCEINLINE void SetPreaccIn(T&& data, Ts&&... moreData) {
-    static_assert(!std::is_same<T,su2double>::value, "rvalues cannot be registered");
-  }
+template <class T, class... Ts, su2enable_if<std::is_same<T, su2double>::value> = 0>
+FORCEINLINE void SetPreaccIn(T&& data, Ts&&... moreData) {
+  static_assert(!std::is_same<T, su2double>::value, "rvalues cannot be registered");
+}
 
-  template<class T>
-  FORCEINLINE void SetPreaccIn(const T& data, const int size) {
-    if (PreaccActive) {
-      for (int i = 0; i < size; i++) {
-        if (IsIdentifierActive(data[i])) {
-          PreaccHelper.addInput(data[i]);
-        }
+template <class T>
+FORCEINLINE void SetPreaccIn(const T& data, const int size) {
+  if (PreaccActive) {
+    for (int i = 0; i < size; i++) {
+      if (IsIdentifierActive(data[i])) {
+        PreaccHelper.addInput(data[i]);
       }
     }
   }
+}
 
-  template<class T>
-  FORCEINLINE void SetPreaccIn(const T& data, const int size_x, const int size_y) {
-    if (!PreaccActive) return;
-    for (int i = 0; i < size_x; i++) {
-      for (int j = 0; j < size_y; j++) {
-        if (IsIdentifierActive(data[i][j])) {
-          PreaccHelper.addInput(data[i][j]);
-        }
+template <class T>
+FORCEINLINE void SetPreaccIn(const T& data, const int size_x, const int size_y) {
+  if (!PreaccActive) return;
+  for (int i = 0; i < size_x; i++) {
+    for (int j = 0; j < size_y; j++) {
+      if (IsIdentifierActive(data[i][j])) {
+        PreaccHelper.addInput(data[i][j]);
       }
     }
   }
+}
 
-  FORCEINLINE void StartPreacc() {
-    if (AD::getTape().isActive() && PreaccEnabled) {
-      PreaccHelper.start();
-      PreaccActive = true;
-    }
+FORCEINLINE void StartPreacc() {
+  if (AD::getTape().isActive() && PreaccEnabled) {
+    PreaccHelper.start();
+    PreaccActive = true;
   }
+}
 
-  /*--- Base case for parameter pack expansion. ---*/
-  FORCEINLINE void SetPreaccOut() {}
+/*--- Base case for parameter pack expansion. ---*/
+FORCEINLINE void SetPreaccOut() {}
 
-  template<class T, class... Ts, su2enable_if<std::is_same<T,su2double>::value> = 0>
-  FORCEINLINE void SetPreaccOut(T& data, Ts&&... moreData) {
-    if (!PreaccActive) return;
-    if (IsIdentifierActive(data))
-      PreaccHelper.addOutput(data);
-    SetPreaccOut(moreData...);
-  }
+template <class T, class... Ts, su2enable_if<std::is_same<T, su2double>::value> = 0>
+FORCEINLINE void SetPreaccOut(T& data, Ts&&... moreData) {
+  if (!PreaccActive) return;
+  if (IsIdentifierActive(data)) PreaccHelper.addOutput(data);
+  SetPreaccOut(moreData...);
+}
 
-  template<class T>
-  FORCEINLINE void SetPreaccOut(T&& data, const int size) {
-    if (PreaccActive) {
-      for (int i = 0; i < size; i++) {
-        if (IsIdentifierActive(data[i])) {
-          PreaccHelper.addOutput(data[i]);
-        }
+template <class T>
+FORCEINLINE void SetPreaccOut(T&& data, const int size) {
+  if (PreaccActive) {
+    for (int i = 0; i < size; i++) {
+      if (IsIdentifierActive(data[i])) {
+        PreaccHelper.addOutput(data[i]);
       }
     }
   }
+}
 
-  template<class T>
-  FORCEINLINE void SetPreaccOut(T&& data, const int size_x, const int size_y) {
-    if (!PreaccActive) return;
-    for (int i = 0; i < size_x; i++) {
-      for (int j = 0; j < size_y; j++) {
-        if (IsIdentifierActive(data[i][j])) {
-          PreaccHelper.addOutput(data[i][j]);
-        }
+template <class T>
+FORCEINLINE void SetPreaccOut(T&& data, const int size_x, const int size_y) {
+  if (!PreaccActive) return;
+  for (int i = 0; i < size_x; i++) {
+    for (int j = 0; j < size_y; j++) {
+      if (IsIdentifierActive(data[i][j])) {
+        PreaccHelper.addOutput(data[i][j]);
       }
     }
   }
+}
 
-  FORCEINLINE void Push_TapePosition() {
-  #if defined(HAVE_OPDI)
-    TapePositions.push_back({AD::getTape().getPosition(), opdi::logic->exportState()});
-  #else
-    TapePositions.push_back(AD::getTape().getPosition());
-  #endif
-  }
+FORCEINLINE void Push_TapePosition() {
+#if defined(HAVE_OPDI)
+  TapePositions.push_back({AD::getTape().getPosition(), opdi::logic->exportState()});
+#else
+  TapePositions.push_back(AD::getTape().getPosition());
+#endif
+}
 
-  FORCEINLINE void EndPreacc(){
-    if (PreaccActive) {
-      PreaccHelper.finish(false);
-      PreaccActive = false;
-    }
+FORCEINLINE void EndPreacc() {
+  if (PreaccActive) {
+    PreaccHelper.finish(false);
+    PreaccActive = false;
   }
+}
 
-  FORCEINLINE void SetExtFuncIn(const su2double &data) {
-    FuncHelper.addInput(data);
+FORCEINLINE void SetExtFuncIn(const su2double& data) { FuncHelper.addInput(data); }
+
+template <class T>
+FORCEINLINE void SetExtFuncIn(const T& data, const int size) {
+  for (int i = 0; i < size; i++) {
+    FuncHelper.addInput(data[i]);
   }
+}
 
-  template<class T>
-  FORCEINLINE void SetExtFuncIn(const T& data, const int size) {
-    for (int i = 0; i < size; i++) {
-      FuncHelper.addInput(data[i]);
+template <class T>
+FORCEINLINE void SetExtFuncIn(const T& data, const int size_x, const int size_y) {
+  for (int i = 0; i < size_x; i++) {
+    for (int j = 0; j < size_y; j++) {
+      FuncHelper.addInput(data[i][j]);
     }
   }
+}
 
-  template<class T>
-  FORCEINLINE void SetExtFuncIn(const T& data, const int size_x, const int size_y) {
-    for (int i = 0; i < size_x; i++) {
-      for (int j = 0; j < size_y; j++) {
-        FuncHelper.addInput(data[i][j]);
-      }
-    }
+FORCEINLINE void SetExtFuncOut(su2double& data) {
+  if (AD::getTape().isActive()) {
+    FuncHelper.addOutput(data);
   }
+}
 
-  FORCEINLINE void SetExtFuncOut(su2double& data) {
+template <class T>
+FORCEINLINE void SetExtFuncOut(T&& data, const int size) {
+  for (int i = 0; i < size; i++) {
     if (AD::getTape().isActive()) {
-      FuncHelper.addOutput(data);
+      FuncHelper.addOutput(data[i]);
     }
   }
+}
 
-  template<class T>
-  FORCEINLINE void SetExtFuncOut(T&& data, const int size) {
-    for (int i = 0; i < size; i++) {
+template <class T>
+FORCEINLINE void SetExtFuncOut(T&& data, const int size_x, const int size_y) {
+  for (int i = 0; i < size_x; i++) {
+    for (int j = 0; j < size_y; j++) {
       if (AD::getTape().isActive()) {
-        FuncHelper.addOutput(data[i]);
-      }
-    }
-  }
-
-  template<class T>
-  FORCEINLINE void SetExtFuncOut(T&& data, const int size_x, const int size_y) {
-    for (int i = 0; i < size_x; i++) {
-      for (int j = 0; j < size_y; j++) {
-        if (AD::getTape().isActive()) {
-          FuncHelper.addOutput(data[i][j]);
-        }
+        FuncHelper.addOutput(data[i][j]);
       }
     }
   }
+}
 
-  FORCEINLINE void delete_handler(void *handler) {
-    CheckpointHandler *checkpoint = static_cast<CheckpointHandler*>(handler);
-    checkpoint->clear();
-  }
+FORCEINLINE void delete_handler(void* handler) {
+  CheckpointHandler* checkpoint = static_cast<CheckpointHandler*>(handler);
+  checkpoint->clear();
+}
 
-  FORCEINLINE bool BeginPassive() {
-    if(AD::getTape().isActive()) {
-      StopRecording();
-      return true;
-    }
-    return false;
+FORCEINLINE bool BeginPassive() {
+  if (AD::getTape().isActive()) {
+    StopRecording();
+    return true;
   }
+  return false;
+}
 
-  FORCEINLINE void EndPassive(bool wasActive) { if(wasActive) StartRecording(); }
+FORCEINLINE void EndPassive(bool wasActive) {
+  if (wasActive) StartRecording();
+}
 
-  FORCEINLINE bool PausePreaccumulation() {
-    const auto current = PreaccEnabled;
-    if (!current) return false;
-    SU2_OMP_SAFE_GLOBAL_ACCESS(PreaccEnabled = false;)
-    return true;
-  }
+FORCEINLINE bool PausePreaccumulation() {
+  const auto current = PreaccEnabled;
+  if (!current) return false;
+  SU2_OMP_SAFE_GLOBAL_ACCESS(PreaccEnabled = false;)
+  return true;
+}
 
-  FORCEINLINE void ResumePreaccumulation(bool wasActive) {
-    if (!wasActive) return;
-    SU2_OMP_SAFE_GLOBAL_ACCESS(PreaccEnabled = true;)
-  }
+FORCEINLINE void ResumePreaccumulation(bool wasActive) {
+  if (!wasActive) return;
+  SU2_OMP_SAFE_GLOBAL_ACCESS(PreaccEnabled = true;)
+}
 
-  FORCEINLINE void StartNoSharedReading() {
+FORCEINLINE void StartNoSharedReading() {
 #ifdef HAVE_OPDI
-    opdi::logic->setAdjointAccessMode(opdi::LogicInterface::AdjointAccessMode::Classical);
-    opdi::logic->addReverseBarrier();
+  opdi::logic->setAdjointAccessMode(opdi::LogicInterface::AdjointAccessMode::Classical);
+  opdi::logic->addReverseBarrier();
 #endif
-  }
+}
 
-  FORCEINLINE void EndNoSharedReading() {
+FORCEINLINE void EndNoSharedReading() {
 #ifdef HAVE_OPDI
-    opdi::logic->setAdjointAccessMode(opdi::LogicInterface::AdjointAccessMode::Atomic);
-    opdi::logic->addReverseBarrier();
+  opdi::logic->setAdjointAccessMode(opdi::LogicInterface::AdjointAccessMode::Atomic);
+  opdi::logic->addReverseBarrier();
 #endif
-  }
-#endif // CODI_REVERSE_TYPE
-
-  void Initialize();
-  void Finalize();
+}
+#endif  // CODI_REVERSE_TYPE
 
-} // namespace AD
+void Initialize();
+void Finalize();
 
+}  // namespace AD
 
 /*--- If we compile under OSX we have to overload some of the operators for
  *   complex numbers to avoid the use of the standard operators
@@ -579,36 +571,28 @@ namespace AD{
 
 #ifdef __APPLE__
 
-namespace std{
+namespace std {
 
-  template<>
-  inline su2double abs(const complex<su2double>& x){
-
-    return sqrt(x.real()*x.real() + x.imag()*x.imag());
-
-  }
-
-  template<>
-  inline complex<su2double> operator/(const complex<su2double>& x,
-                                      const complex<su2double>& y){
-
-    su2double d    = (y.real()*y.real() + y.imag()*y.imag());
-    su2double real = (x.real()*y.real() + x.imag()*y.imag())/d;
-    su2double imag = (x.imag()*y.real() - x.real()*y.imag())/d;
-
-    return complex<su2double>(real, imag);
-
-  }
+template <>
+inline su2double abs(const complex<su2double>& x) {
+  return sqrt(x.real() * x.real() + x.imag() * x.imag());
+}
 
-  template<>
-  inline complex<su2double> operator*(const complex<su2double>& x,
-                                      const complex<su2double>& y){
+template <>
+inline complex<su2double> operator/(const complex<su2double>& x, const complex<su2double>& y) {
+  su2double d = (y.real() * y.real() + y.imag() * y.imag());
+  su2double real = (x.real() * y.real() + x.imag() * y.imag()) / d;
+  su2double imag = (x.imag() * y.real() - x.real() * y.imag()) / d;
 
-    su2double real = (x.real()*y.real() - x.imag()*y.imag());
-    su2double imag = (x.imag()*y.real() + x.real()*y.imag());
+  return complex<su2double>(real, imag);
+}
 
-    return complex<su2double>(real, imag);
+template <>
+inline complex<su2double> operator*(const complex<su2double>& x, const complex<su2double>& y) {
+  su2double real = (x.real() * y.real() - x.imag() * y.imag());
+  su2double imag = (x.imag() * y.real() + x.real() * y.imag());
 
-  }
+  return complex<su2double>(real, imag);
 }
+}  // namespace std
 #endif
diff --git a/Common/include/basic_types/datatype_structure.hpp b/Common/include/basic_types/datatype_structure.hpp
index 1ee72ee70b7..b4bfbd47b1b 100644
--- a/Common/include/basic_types/datatype_structure.hpp
+++ b/Common/include/basic_types/datatype_structure.hpp
@@ -41,130 +41,132 @@
  * \author T. Albring
  */
 namespace SU2_TYPE {
-  /*!
-   * \brief Set the (primitive) value of the datatype (needs to be implemented for each new type).
-   * \param[in] data - The non-primitive datatype.
-   * \param[in] val - The primitive value.
-   */
-  void SetValue(su2double& data, const passivedouble &val);
-
-  /*!
-   * \brief Set the secondary value of the datatype (needs to be implemented for each new type).
-   * \param[in] data - The non-primitive datatype.
-   * \param[in] val - The primitive value.
-   */
-  void SetSecondary(su2double& data, const passivedouble &val);
-
-  /*!
-   * \brief Get the (primitive) value of the datatype (needs to be specialized for active types).
-   * \param[in] data - The non-primitive datatype.
-   * \return The primitive value.
-   */
-  passivedouble GetValue(const su2double &data);
-
-  /*!
-   * \brief Get the secondary value of the datatype (needs to be implemented for each new type).
-   * \param[in] data - The non-primitive datatype.
-   * \return The primitive value.
-   */
-  passivedouble GetSecondary(const su2double &data);
-
-  /*!
-   * \brief Get the derivative value of the datatype (needs to be implemented for each new type).
-   * \param[in] data - The non-primitive datatype.
-   * \return The derivative value.
-   */
-  passivedouble GetDerivative(const su2double &data);
-
-  /*!
-   * \brief Set the derivative value of the datatype (needs to be implemented for each new type).
-   * \param[in] data - The non-primitive datatype.
-   * \param[in] val - The value of the derivative.
-   */
-  void SetDerivative(su2double &data, const passivedouble &val);
-
-  /*--- Implementation of the above for the different types. ---*/
+/*!
+ * \brief Set the (primitive) value of the datatype (needs to be implemented for each new type).
+ * \param[in] data - The non-primitive datatype.
+ * \param[in] val - The primitive value.
+ */
+void SetValue(su2double& data, const passivedouble& val);
+
+/*!
+ * \brief Set the secondary value of the datatype (needs to be implemented for each new type).
+ * \param[in] data - The non-primitive datatype.
+ * \param[in] val - The primitive value.
+ */
+void SetSecondary(su2double& data, const passivedouble& val);
+
+/*!
+ * \brief Get the (primitive) value of the datatype (needs to be specialized for active types).
+ * \param[in] data - The non-primitive datatype.
+ * \return The primitive value.
+ */
+passivedouble GetValue(const su2double& data);
+
+/*!
+ * \brief Get the secondary value of the datatype (needs to be implemented for each new type).
+ * \param[in] data - The non-primitive datatype.
+ * \return The primitive value.
+ */
+passivedouble GetSecondary(const su2double& data);
+
+/*!
+ * \brief Get the derivative value of the datatype (needs to be implemented for each new type).
+ * \param[in] data - The non-primitive datatype.
+ * \return The derivative value.
+ */
+passivedouble GetDerivative(const su2double& data);
+
+/*!
+ * \brief Set the derivative value of the datatype (needs to be implemented for each new type).
+ * \param[in] data - The non-primitive datatype.
+ * \param[in] val - The value of the derivative.
+ */
+void SetDerivative(su2double& data, const passivedouble& val);
+
+/*--- Implementation of the above for the different types. ---*/
 
 #if defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)
 
-  FORCEINLINE void SetValue(su2double& data, const passivedouble &val) {data.setValue(val);}
+FORCEINLINE void SetValue(su2double& data, const passivedouble& val) { data.setValue(val); }
 
-  FORCEINLINE passivedouble GetValue(const su2double& data) {return data.getValue();}
+FORCEINLINE passivedouble GetValue(const su2double& data) { return data.getValue(); }
 
-  FORCEINLINE void SetSecondary(su2double& data, const passivedouble &val) {data.setGradient(val);}
+FORCEINLINE void SetSecondary(su2double& data, const passivedouble& val) { data.setGradient(val); }
 
-  FORCEINLINE void SetDerivative(su2double& data, const passivedouble &val) {data.setGradient(val);}
+FORCEINLINE void SetDerivative(su2double& data, const passivedouble& val) { data.setGradient(val); }
 
-  FORCEINLINE passivedouble GetSecondary(const su2double& data) {return data.getGradient();}
+FORCEINLINE passivedouble GetSecondary(const su2double& data) { return data.getGradient(); }
 
-  FORCEINLINE passivedouble GetDerivative(const su2double& data) {return data.getGradient();}
+FORCEINLINE passivedouble GetDerivative(const su2double& data) { return data.getGradient(); }
 
-#else // passive type, no AD
+#else  // passive type, no AD
 
-  FORCEINLINE void SetValue(su2double& data, const passivedouble &val) {data = val;}
+FORCEINLINE void SetValue(su2double& data, const passivedouble& val) { data = val; }
 
-  FORCEINLINE passivedouble GetValue(const su2double& data) {return data;}
+FORCEINLINE passivedouble GetValue(const su2double& data) { return data; }
 
-  FORCEINLINE void SetSecondary(su2double&, const passivedouble &) {}
+FORCEINLINE void SetSecondary(su2double&, const passivedouble&) {}
 
-  FORCEINLINE passivedouble GetDerivative(const su2double&) {return 0.0;}
+FORCEINLINE passivedouble GetDerivative(const su2double&) { return 0.0; }
 
-  FORCEINLINE passivedouble GetSecondary(const su2double&) {return 0.0;}
+FORCEINLINE passivedouble GetSecondary(const su2double&) { return 0.0; }
 
-  FORCEINLINE void SetDerivative(su2double &, const passivedouble &) {}
+FORCEINLINE void SetDerivative(su2double&, const passivedouble&) {}
 #endif
 
-  /*!
-   * \brief Get the passive value of any variable. For most types return directly,
-   * specialize for su2double to call GetValue.
-   * \note This is a struct instead of a function because the return type of the
-   * su2double specialization changes.
-   */
-  template <class T>
-  struct Passive {
-    FORCEINLINE static T Value(const T& val) {return val;}
-  };
-  template <>
-  struct Passive<su2double> {
-    FORCEINLINE static passivedouble Value(const su2double& val) {return GetValue(val);}
-  };
-
-  /*!
-   * \brief Casts the primitive value to int (uses GetValue, already implemented for each type).
-   * \param[in] data - The non-primitive datatype.
-   * \return - The primary value casted to int.
-   */
-  FORCEINLINE int Int(const su2double& data) {return static_cast<int>(SU2_TYPE::GetValue(data));}
-
-  /*!
-   * \brief Casts the primitive value to short (uses GetValue, already implemented for each type).
-   * \param[in] data - The non-primitive datatype.
-   * \return - The primary value casted to short.
-   */
-  FORCEINLINE short Short(const su2double& data) {return static_cast<short>(SU2_TYPE::GetValue(data));}
-
-  /*--- Special handling of the sprintf routine for non-primitive types. ---*/
-  /*--- Pass-through for built-in types. ---*/
-  template<class T, su2enable_if<std::is_trivial<T>::value> = 0>
-  FORCEINLINE const T& _printGetValue(const T& val) {return val;}
-  /*--- Overload for expressions of active types. ---*/
-  template<class T, su2enable_if<!std::is_trivial<T>::value> = 0>
-  FORCEINLINE passivedouble _printGetValue(const T& val) { return val.getValue(); }
-
-  /*!
-   * \brief Wrapper to sprintf to be able to print active types and AD expressions.
-   * \note This is for compatibility with old code, stringstreams should be the preferred way to build strings.
-   * \param[in] str - Target char buffer.
-   * \param[in] format - Format string.
-   * \param[in] args - Values to be printed to the string.
-   */
-  template<class... Ts>
-  FORCEINLINE void sprintf(char* str, const char* format, Ts&&... args) {
-    ::sprintf(str, format, SU2_TYPE::_printGetValue(args)...);
-  }
-  FORCEINLINE void sprintf(char* str, const char* literal) {
-    ::sprintf(str, "%s", literal);
-  }
+/*!
+ * \brief Get the passive value of any variable. For most types return directly,
+ * specialize for su2double to call GetValue.
+ * \note This is a struct instead of a function because the return type of the
+ * su2double specialization changes.
+ */
+template <class T>
+struct Passive {
+  FORCEINLINE static T Value(const T& val) { return val; }
+};
+template <>
+struct Passive<su2double> {
+  FORCEINLINE static passivedouble Value(const su2double& val) { return GetValue(val); }
+};
+
+/*!
+ * \brief Casts the primitive value to int (uses GetValue, already implemented for each type).
+ * \param[in] data - The non-primitive datatype.
+ * \return - The primary value casted to int.
+ */
+FORCEINLINE int Int(const su2double& data) { return static_cast<int>(SU2_TYPE::GetValue(data)); }
+
+/*!
+ * \brief Casts the primitive value to short (uses GetValue, already implemented for each type).
+ * \param[in] data - The non-primitive datatype.
+ * \return - The primary value casted to short.
+ */
+FORCEINLINE short Short(const su2double& data) { return static_cast<short>(SU2_TYPE::GetValue(data)); }
+
+/*--- Special handling of the sprintf routine for non-primitive types. ---*/
+/*--- Pass-through for built-in types. ---*/
+template <class T, su2enable_if<std::is_trivial<T>::value> = 0>
+FORCEINLINE const T& _printGetValue(const T& val) {
+  return val;
+}
+/*--- Overload for expressions of active types. ---*/
+template <class T, su2enable_if<!std::is_trivial<T>::value> = 0>
+FORCEINLINE passivedouble _printGetValue(const T& val) {
+  return val.getValue();
+}
+
+/*!
+ * \brief Wrapper to sprintf to be able to print active types and AD expressions.
+ * \note This is for compatibility with old code, stringstreams should be the preferred way to build strings.
+ * \param[in] str - Target char buffer.
+ * \param[in] format - Format string.
+ * \param[in] args - Values to be printed to the string.
+ */
+template <class... Ts>
+FORCEINLINE void sprintf(char* str, const char* format, Ts&&... args) {
+  ::sprintf(str, format, SU2_TYPE::_printGetValue(args)...);
+}
+FORCEINLINE void sprintf(char* str, const char* literal) { ::sprintf(str, "%s", literal); }
 #define SPRINTF SU2_TYPE::sprintf
 
-} // namespace SU2_TYPE
+}  // namespace SU2_TYPE
diff --git a/Common/include/code_config.hpp b/Common/include/code_config.hpp
index ab5aa8017e2..bbc5eebb76e 100644
--- a/Common/include/code_config.hpp
+++ b/Common/include/code_config.hpp
@@ -56,18 +56,24 @@
 
 /*--- Convenience SFINAE typedef to conditionally
  * enable/disable function template overloads. ---*/
-template<bool condition>
-using su2enable_if = typename std::enable_if<condition,bool>::type;
+template <bool condition>
+using su2enable_if = typename std::enable_if<condition, bool>::type;
 
 /*--- Compile-time type selection. ---*/
-template<bool B, class T, class F> struct su2conditional { using type = T; };
-template<class T, class F> struct su2conditional<false, T, F> { using type = F; };
-
-template<bool B, class T, class F>
-using su2conditional_t = typename su2conditional<B,T,F>::type;
+template <bool B, class T, class F>
+struct su2conditional {
+  using type = T;
+};
+template <class T, class F>
+struct su2conditional<false, T, F> {
+  using type = F;
+};
+
+template <bool B, class T, class F>
+using su2conditional_t = typename su2conditional<B, T, F>::type;
 
 /*! \brief Static cast "In" to "Out", in debug builds a dynamic cast is used. */
-template<class Out, class In>
+template <class Out, class In>
 FORCEINLINE Out su2staticcast_p(In ptr) {
   static_assert(std::is_pointer<In>::value, "This expects a pointer");
 #ifndef NDEBUG
@@ -85,7 +91,7 @@ FORCEINLINE Out su2staticcast_p(In ptr) {
 /*--- Depending on the datatype defined during the configuration,
  * include the correct definition, and create the main typedef. ---*/
 
-#if defined(CODI_REVERSE_TYPE) // reverse mode AD
+#if defined(CODI_REVERSE_TYPE)  // reverse mode AD
 #include "codi.hpp"
 #include "codi/tools/data/externalFunctionUserData.hpp"
 
@@ -94,19 +100,19 @@ using su2double = codi::RealReverseIndexOpenMP;
 #else
 #if defined(CODI_INDEX_TAPE)
 using su2double = codi::RealReverseIndex;
-//#elif defined(CODI_PRIMAL_TAPE)
-//using su2double = codi::RealReversePrimal;
-//#elif defined(CODI_PRIMAL_INDEX_TAPE)
-//using su2double = codi::RealReversePrimalIndex;
+// #elif defined(CODI_PRIMAL_TAPE)
+// using su2double = codi::RealReversePrimal;
+// #elif defined(CODI_PRIMAL_INDEX_TAPE)
+// using su2double = codi::RealReversePrimalIndex;
 #else
 using su2double = codi::RealReverse;
 #endif
 #endif
-#elif defined(CODI_FORWARD_TYPE) // forward mode AD
+#elif defined(CODI_FORWARD_TYPE)  // forward mode AD
 #include "codi.hpp"
 using su2double = codi::RealForward;
 
-#else // primal / direct / no AD
+#else  // primal / direct / no AD
 using su2double = double;
 #endif
 
diff --git a/Common/include/containers/C2DContainer.hpp b/Common/include/containers/C2DContainer.hpp
index 119eed0b55a..8e726ee4ef9 100644
--- a/Common/include/containers/C2DContainer.hpp
+++ b/Common/include/containers/C2DContainer.hpp
@@ -42,19 +42,17 @@
  * \brief Supported ways to flatten a matrix into an array.
  * Contiguous rows or contiguous columns respectively.
  */
-enum class StorageType {RowMajor=0, ColumnMajor=1};
+enum class StorageType { RowMajor = 0, ColumnMajor = 1 };
 
 /*!
  * \enum SizeType
  * \brief Special value "DynamicSize" to indicate a dynamic size.
  */
-enum SizeType : size_t {DynamicSize=0};
-
+enum SizeType : size_t { DynamicSize = 0 };
 
 /*--- Namespace to "hide" helper classes and
  functions used by the container class. ---*/
-namespace container_details
-{
+namespace container_details {
 /*!
  * \class AccessorImpl
  * \brief Base accessor class and version of template for both sizes known at compile time.
@@ -62,25 +60,24 @@ namespace container_details
  * The actual container inherits from this class, this is to reduce the number of
  * methods that need to be redefined with each size specialization.
  */
-template<typename Index_t, class Scalar_t, StorageType Store, size_t AlignSize, size_t StaticRows, size_t StaticCols>
-class AccessorImpl
-{
-  static_assert(!(StaticRows==1 && Store==StorageType::ColumnMajor),
-                "Row vector should have row-major storage.");
-  static_assert(!(StaticCols==1 && Store==StorageType::RowMajor),
+template <typename Index_t, class Scalar_t, StorageType Store, size_t AlignSize, size_t StaticRows, size_t StaticCols>
+class AccessorImpl {
+  static_assert(!(StaticRows == 1 && Store == StorageType::ColumnMajor), "Row vector should have row-major storage.");
+  static_assert(!(StaticCols == 1 && Store == StorageType::RowMajor),
                 "Column vector should have column-major storage.");
-protected:
+
+ protected:
   /*!
    * For static specializations AlignSize will force the alignment
    * specification of the entire class, not just the data.
    */
-  alignas(AlignSize) Scalar_t m_data[StaticRows*StaticCols];
+  alignas(AlignSize) Scalar_t m_data[StaticRows * StaticCols];
 
   /*!
    * Static size specializations use this do-nothing allocation macro.
    */
-#define DUMMY_ALLOCATOR \
-  void m_allocate(size_t sz, Index_t rows, Index_t cols) noexcept {}\
+#define DUMMY_ALLOCATOR                                              \
+  void m_allocate(size_t sz, Index_t rows, Index_t cols) noexcept {} \
   void m_destroy() noexcept {}
 
   /*!
@@ -92,26 +89,25 @@ class AccessorImpl
    * default construct the elements of non-trivial type. Such types also
    * need to be destructed explicitly before freeing the memory.
    */
-#define REAL_ALLOCATOR(EXTRA)                                           \
-  static_assert(MemoryAllocation::is_power_of_two(AlignSize),           \
-                "AlignSize is not a power of two.");                    \
-                                                                        \
-  void m_allocate(size_t sz, Index_t rows, Index_t cols) noexcept {     \
-    EXTRA;                                                              \
-    m_data = MemoryAllocation::aligned_alloc<Scalar_t>(AlignSize,sz);   \
-    if (!std::is_trivial<Scalar_t>::value)                              \
-      for (size_t i = 0; i < size(); ++i) new (m_data+i) Scalar_t();    \
-  }                                                                     \
-                                                                        \
-  void m_destroy() noexcept {                                           \
-    if (!std::is_trivial<Scalar_t>::value)                              \
-      for (size_t i = 0; i < size(); ++i) m_data[i].~Scalar_t();        \
-    MemoryAllocation::aligned_free<Scalar_t>(m_data);                   \
+#define REAL_ALLOCATOR(EXTRA)                                                                      \
+  static_assert(MemoryAllocation::is_power_of_two(AlignSize), "AlignSize is not a power of two."); \
+                                                                                                   \
+  void m_allocate(size_t sz, Index_t rows, Index_t cols) noexcept {                                \
+    EXTRA;                                                                                         \
+    m_data = MemoryAllocation::aligned_alloc<Scalar_t>(AlignSize, sz);                             \
+    if (!std::is_trivial<Scalar_t>::value)                                                         \
+      for (size_t i = 0; i < size(); ++i) new (m_data + i) Scalar_t();                             \
+  }                                                                                                \
+                                                                                                   \
+  void m_destroy() noexcept {                                                                      \
+    if (!std::is_trivial<Scalar_t>::value)                                                         \
+      for (size_t i = 0; i < size(); ++i) m_data[i].~Scalar_t();                                   \
+    MemoryAllocation::aligned_free<Scalar_t>(m_data);                                              \
   }
 
   DUMMY_ALLOCATOR
 
-public:
+ public:
   /*!
    * Dynamic types need to manage internal data as the derived class would
    * not compile if it tried to set m_data to null on static specializations.
@@ -120,241 +116,226 @@ class AccessorImpl
    * The default ctor needs to "INIT" some fields. The move ctor/assign need
    * to "MOVE" those fields, i.e. copy and set "other" appropriately.
    */
-#define CUSTOM_CTOR_AND_DTOR_BASE(INIT,MOVE)                            \
-  AccessorImpl() noexcept : m_data(nullptr) {INIT;}                     \
-                                                                        \
-  AccessorImpl(AccessorImpl&& other) noexcept                           \
-  {                                                                     \
-    MOVE; m_data=other.m_data; other.m_data=nullptr;                    \
-  }                                                                     \
-                                                                        \
-  AccessorImpl& operator= (AccessorImpl&& other) noexcept               \
-  {                                                                     \
-    m_destroy();                                                        \
-    MOVE; m_data=other.m_data; other.m_data=nullptr;                    \
-    return *this;                                                       \
-  }                                                                     \
-                                                                        \
-  ~AccessorImpl() noexcept {m_destroy();}
+#define CUSTOM_CTOR_AND_DTOR_BASE(INIT, MOVE)              \
+  AccessorImpl() noexcept : m_data(nullptr) { INIT; }      \
+                                                           \
+  AccessorImpl(AccessorImpl&& other) noexcept {            \
+    MOVE;                                                  \
+    m_data = other.m_data;                                 \
+    other.m_data = nullptr;                                \
+  }                                                        \
+                                                           \
+  AccessorImpl& operator=(AccessorImpl&& other) noexcept { \
+    m_destroy();                                           \
+    MOVE;                                                  \
+    m_data = other.m_data;                                 \
+    other.m_data = nullptr;                                \
+    return *this;                                          \
+  }                                                        \
+                                                           \
+  ~AccessorImpl() noexcept { m_destroy(); }
 
   /*!
    * Shorthand for when specialization has only one more member than m_data.
    */
-#define CUSTOM_CTOR_AND_DTOR(X) \
-  CUSTOM_CTOR_AND_DTOR_BASE(X=0, X=other.X; other.X=0)
+#define CUSTOM_CTOR_AND_DTOR(X) CUSTOM_CTOR_AND_DTOR_BASE(X = 0, X = other.X; other.X = 0)
 
   /*!
    * Universal accessors return a raw pointer to the data.
    */
-#define UNIV_ACCESSORS                                                  \
-  bool empty() const noexcept {return size()==0;}                       \
-  Scalar_t* data() noexcept {return m_data;}                            \
-  const Scalar_t* data() const noexcept {return m_data;}                \
-  Scalar_t* begin() noexcept {return data();}                           \
-  const Scalar_t* begin() const noexcept {return data();}               \
-  Scalar_t* end() noexcept {return data()+size();}                      \
-  const Scalar_t* end() const noexcept {return data()+size();}
+#define UNIV_ACCESSORS                                      \
+  bool empty() const noexcept { return size() == 0; }       \
+  Scalar_t* data() noexcept { return m_data; }              \
+  const Scalar_t* data() const noexcept { return m_data; }  \
+  Scalar_t* begin() noexcept { return data(); }             \
+  const Scalar_t* begin() const noexcept { return data(); } \
+  Scalar_t* end() noexcept { return data() + size(); }      \
+  const Scalar_t* end() const noexcept { return data() + size(); }
 
   /*!
    * Operator (,) gives pointwise access, operator [] returns a pointer to the
    * first element of the row/column of a row/column-major matrix respectively.
    */
-#define MATRIX_ACCESSORS(M,N)                                           \
-  UNIV_ACCESSORS                                                        \
-  Index_t rows() const noexcept {return M;}                             \
-  Index_t cols() const noexcept {return N;}                             \
-  size_t size() const noexcept {return M*N;}                            \
-                                                                        \
-  const Scalar_t& operator() (const Index_t i,                          \
-                              const Index_t j) const noexcept           \
-  {                                                                     \
-    assert(i>=0 && i<M && j>=0 && j<N);                                 \
-    return m_data[(Store==StorageType::RowMajor)? i*N+j : i+j*M];       \
-  }                                                                     \
-                                                                        \
-  Scalar_t& operator() (const Index_t i, const Index_t j) noexcept      \
-  {                                                                     \
-    const AccessorImpl& const_this = *this;                             \
-    return const_cast<Scalar_t&>( const_this(i,j) );                    \
-  }                                                                     \
-                                                                        \
-  const Scalar_t* operator[] (const Index_t k) const noexcept           \
-  {                                                                     \
-    if(Store == StorageType::RowMajor) {                                \
-      assert(k>=0 && k<M);                                              \
-      return &m_data[k*N];                                              \
-    } else {                                                            \
-      assert(k>=0 && k<N);                                              \
-      return &m_data[k*M];                                              \
-    }                                                                   \
-  }                                                                     \
-                                                                        \
-  Scalar_t* operator[] (const Index_t k) noexcept                       \
-  {                                                                     \
-    const AccessorImpl& const_this = *this;                             \
-    return const_cast<Scalar_t*>( const_this[k] );                      \
+#define MATRIX_ACCESSORS(M, N)                                                  \
+  UNIV_ACCESSORS                                                                \
+  Index_t rows() const noexcept { return M; }                                   \
+  Index_t cols() const noexcept { return N; }                                   \
+  size_t size() const noexcept { return M * N; }                                \
+                                                                                \
+  const Scalar_t& operator()(const Index_t i, const Index_t j) const noexcept { \
+    assert(i >= 0 && i < M && j >= 0 && j < N);                                 \
+    return m_data[(Store == StorageType::RowMajor) ? i * N + j : i + j * M];    \
+  }                                                                             \
+                                                                                \
+  Scalar_t& operator()(const Index_t i, const Index_t j) noexcept {             \
+    const AccessorImpl& const_this = *this;                                     \
+    return const_cast<Scalar_t&>(const_this(i, j));                             \
+  }                                                                             \
+                                                                                \
+  const Scalar_t* operator[](const Index_t k) const noexcept {                  \
+    if (Store == StorageType::RowMajor) {                                       \
+      assert(k >= 0 && k < M);                                                  \
+      return &m_data[k * N];                                                    \
+    } else {                                                                    \
+      assert(k >= 0 && k < N);                                                  \
+      return &m_data[k * M];                                                    \
+    }                                                                           \
+  }                                                                             \
+                                                                                \
+  Scalar_t* operator[](const Index_t k) noexcept {                              \
+    const AccessorImpl& const_this = *this;                                     \
+    return const_cast<Scalar_t*>(const_this[k]);                                \
   }
 
   /*!
    * Vectors provide both [] and () with the same behavior.
    */
-#define VECTOR_ACCESSORS(M,ROWMAJOR)                                    \
-  UNIV_ACCESSORS                                                        \
-  Index_t rows() const noexcept {return ROWMAJOR? 1 : M;}               \
-  Index_t cols() const noexcept {return ROWMAJOR? M : 1;}               \
-  size_t  size() const noexcept {return M;}                             \
-                                                                        \
-  Scalar_t& operator() (const Index_t i) noexcept                       \
-  {                                                                     \
-    assert(i>=0 && i<M);                                                \
-    return m_data[i];                                                   \
-  }                                                                     \
-                                                                        \
-  const Scalar_t& operator() (const Index_t i) const noexcept           \
-  {                                                                     \
-    assert(i>=0 && i<M);                                                \
-    return m_data[i];                                                   \
-  }                                                                     \
-                                                                        \
-  Scalar_t& operator[] (const Index_t i) noexcept                       \
-  {                                                                     \
-    assert(i>=0 && i<M);                                                \
-    return m_data[i];                                                   \
-  }                                                                     \
-                                                                        \
-  const Scalar_t& operator[] (const Index_t i) const noexcept           \
-  {                                                                     \
-    assert(i>=0 && i<M);                                                \
-    return m_data[i];                                                   \
+#define VECTOR_ACCESSORS(M, ROWMAJOR)                          \
+  UNIV_ACCESSORS                                               \
+  Index_t rows() const noexcept { return ROWMAJOR ? 1 : M; }   \
+  Index_t cols() const noexcept { return ROWMAJOR ? M : 1; }   \
+  size_t size() const noexcept { return M; }                   \
+                                                               \
+  Scalar_t& operator()(const Index_t i) noexcept {             \
+    assert(i >= 0 && i < M);                                   \
+    return m_data[i];                                          \
+  }                                                            \
+                                                               \
+  const Scalar_t& operator()(const Index_t i) const noexcept { \
+    assert(i >= 0 && i < M);                                   \
+    return m_data[i];                                          \
+  }                                                            \
+                                                               \
+  Scalar_t& operator[](const Index_t i) noexcept {             \
+    assert(i >= 0 && i < M);                                   \
+    return m_data[i];                                          \
+  }                                                            \
+                                                               \
+  const Scalar_t& operator[](const Index_t i) const noexcept { \
+    assert(i >= 0 && i < M);                                   \
+    return m_data[i];                                          \
   }
 
-  MATRIX_ACCESSORS(StaticRows,StaticCols)
+  MATRIX_ACCESSORS(StaticRows, StaticCols)
 };
 
 /*!
  * Specialization for compile-time number of columns.
  */
-template<typename Index_t, class Scalar_t, StorageType Store, size_t AlignSize, size_t StaticCols>
-class AccessorImpl<Index_t,Scalar_t,Store,AlignSize,DynamicSize,StaticCols>
-{
-  static_assert(!(StaticCols==1 && Store==StorageType::RowMajor),
+template <typename Index_t, class Scalar_t, StorageType Store, size_t AlignSize, size_t StaticCols>
+class AccessorImpl<Index_t, Scalar_t, Store, AlignSize, DynamicSize, StaticCols> {
+  static_assert(!(StaticCols == 1 && Store == StorageType::RowMajor),
                 "Column vector should have column-major storage.");
-protected:
+
+ protected:
   Index_t m_rows;
   Scalar_t* m_data;
 
-  REAL_ALLOCATOR(m_rows=rows)
+  REAL_ALLOCATOR(m_rows = rows)
 
-public:
+ public:
   CUSTOM_CTOR_AND_DTOR(m_rows)
 
-  MATRIX_ACCESSORS(m_rows,StaticCols)
+  MATRIX_ACCESSORS(m_rows, StaticCols)
 };
 
 /*!
  * Specialization for compile-time number of columns.
  */
-template<typename Index_t, class Scalar_t, StorageType Store, size_t AlignSize, size_t StaticRows>
-class AccessorImpl<Index_t,Scalar_t,Store,AlignSize,StaticRows,DynamicSize>
-{
-  static_assert(!(StaticRows==1 && Store==StorageType::ColumnMajor),
-                "Row vector should have row-major storage.");
-protected:
+template <typename Index_t, class Scalar_t, StorageType Store, size_t AlignSize, size_t StaticRows>
+class AccessorImpl<Index_t, Scalar_t, Store, AlignSize, StaticRows, DynamicSize> {
+  static_assert(!(StaticRows == 1 && Store == StorageType::ColumnMajor), "Row vector should have row-major storage.");
+
+ protected:
   Index_t m_cols;
   Scalar_t* m_data;
 
-  REAL_ALLOCATOR(m_cols=cols)
+  REAL_ALLOCATOR(m_cols = cols)
 
-public:
+ public:
   CUSTOM_CTOR_AND_DTOR(m_cols)
 
-  MATRIX_ACCESSORS(StaticRows,m_cols)
+  MATRIX_ACCESSORS(StaticRows, m_cols)
 };
 
 /*!
  * Specialization for fully dynamic sizes (generic matrix).
  */
-template<typename Index_t, class Scalar_t, StorageType Store, size_t AlignSize>
-class AccessorImpl<Index_t,Scalar_t,Store,AlignSize,DynamicSize,DynamicSize>
-{
-protected:
+template <typename Index_t, class Scalar_t, StorageType Store, size_t AlignSize>
+class AccessorImpl<Index_t, Scalar_t, Store, AlignSize, DynamicSize, DynamicSize> {
+ protected:
   Index_t m_rows, m_cols;
   Scalar_t* m_data;
 
-  REAL_ALLOCATOR(m_rows=rows; m_cols=cols)
+  REAL_ALLOCATOR(m_rows = rows; m_cols = cols)
 
-public:
-  CUSTOM_CTOR_AND_DTOR_BASE(m_rows = 0; m_cols = 0,
-                            m_rows = other.m_rows; other.m_rows = 0;
-                            m_cols = other.m_cols; other.m_cols = 0)
+ public:
+  CUSTOM_CTOR_AND_DTOR_BASE(m_rows = 0; m_cols = 0, m_rows = other.m_rows; other.m_rows = 0; m_cols = other.m_cols;
+                            other.m_cols = 0)
 
-  MATRIX_ACCESSORS(m_rows,m_cols)
+  MATRIX_ACCESSORS(m_rows, m_cols)
 };
 
 /*!
  * Specialization for static column-vector.
  */
-template<typename Index_t, class Scalar_t, size_t AlignSize, size_t StaticRows>
-class AccessorImpl<Index_t,Scalar_t,StorageType::ColumnMajor,AlignSize,StaticRows,1>
-{
-protected:
+template <typename Index_t, class Scalar_t, size_t AlignSize, size_t StaticRows>
+class AccessorImpl<Index_t, Scalar_t, StorageType::ColumnMajor, AlignSize, StaticRows, 1> {
+ protected:
   alignas(AlignSize) Scalar_t m_data[StaticRows];
 
   DUMMY_ALLOCATOR
 
-public:
-  VECTOR_ACCESSORS(StaticRows,false)
+ public:
+  VECTOR_ACCESSORS(StaticRows, false)
 };
 
 /*!
  * Specialization for dynamic column-vector.
  */
-template<typename Index_t, class Scalar_t, size_t AlignSize>
-class AccessorImpl<Index_t,Scalar_t,StorageType::ColumnMajor,AlignSize,DynamicSize,1>
-{
-protected:
+template <typename Index_t, class Scalar_t, size_t AlignSize>
+class AccessorImpl<Index_t, Scalar_t, StorageType::ColumnMajor, AlignSize, DynamicSize, 1> {
+ protected:
   Index_t m_rows;
   Scalar_t* m_data;
 
-  REAL_ALLOCATOR(m_rows=rows)
+  REAL_ALLOCATOR(m_rows = rows)
 
-public:
+ public:
   CUSTOM_CTOR_AND_DTOR(m_rows)
 
-  VECTOR_ACCESSORS(m_rows,false)
+  VECTOR_ACCESSORS(m_rows, false)
 };
 
 /*!
  * Specialization for static row-vector.
  */
-template<typename Index_t, class Scalar_t, size_t AlignSize, size_t StaticCols>
-class AccessorImpl<Index_t,Scalar_t,StorageType::RowMajor,AlignSize,1,StaticCols>
-{
-protected:
+template <typename Index_t, class Scalar_t, size_t AlignSize, size_t StaticCols>
+class AccessorImpl<Index_t, Scalar_t, StorageType::RowMajor, AlignSize, 1, StaticCols> {
+ protected:
   alignas(AlignSize) Scalar_t m_data[StaticCols];
 
   DUMMY_ALLOCATOR
 
-public:
-  VECTOR_ACCESSORS(StaticCols,true)
+ public:
+  VECTOR_ACCESSORS(StaticCols, true)
 };
 
 /*!
  * Specialization for dynamic row-vector.
  */
-template<typename Index_t, class Scalar_t, size_t AlignSize>
-class AccessorImpl<Index_t,Scalar_t,StorageType::RowMajor,AlignSize,1,DynamicSize>
-{
-protected:
+template <typename Index_t, class Scalar_t, size_t AlignSize>
+class AccessorImpl<Index_t, Scalar_t, StorageType::RowMajor, AlignSize, 1, DynamicSize> {
+ protected:
   Index_t m_cols;
   Scalar_t* m_data;
 
-  REAL_ALLOCATOR(m_cols=cols)
+  REAL_ALLOCATOR(m_cols = cols)
 
-public:
+ public:
   CUSTOM_CTOR_AND_DTOR(m_cols)
 
-  VECTOR_ACCESSORS(m_cols,true)
+  VECTOR_ACCESSORS(m_cols, true)
 };
 
 #undef CUSTOM_CTOR_AND_DTOR_BASE
@@ -364,7 +345,7 @@ class AccessorImpl<Index_t,Scalar_t,StorageType::RowMajor,AlignSize,1,DynamicSiz
 #undef MATRIX_ACCESSORS
 #undef VECTOR_ACCESSORS
 #undef UNIV_ACCESSORS
-}
+}  // namespace container_details
 
 /*!
  * \class C2DContainer
@@ -386,28 +367,28 @@ class AccessorImpl<Index_t,Scalar_t,StorageType::RowMajor,AlignSize,1,DynamicSiz
  * release compile with -DNDEBUG to avoid the associated overhead.
  *
  */
-template<typename Index_t, class Scalar_t, StorageType Store, size_t AlignSize, size_t StaticRows, size_t StaticCols>
-class C2DContainer :
-  public container_details::AccessorImpl<Index_t,Scalar_t,Store,AlignSize,StaticRows,StaticCols>
-{
-  static_assert(std::is_integral<Index_t>::value,"");
-
-private:
-  using Base = container_details::AccessorImpl<Index_t,Scalar_t,Store,AlignSize,StaticRows,StaticCols>;
-  using Base::m_data;
+template <typename Index_t, class Scalar_t, StorageType Store, size_t AlignSize, size_t StaticRows, size_t StaticCols>
+class C2DContainer
+    : public container_details::AccessorImpl<Index_t, Scalar_t, Store, AlignSize, StaticRows, StaticCols> {
+  static_assert(std::is_integral<Index_t>::value, "");
+
+ private:
+  using Base = container_details::AccessorImpl<Index_t, Scalar_t, Store, AlignSize, StaticRows, StaticCols>;
   using Base::m_allocate;
+  using Base::m_data;
   using Base::m_destroy;
-public:
-  using Base::size;
-  using Base::rows;
+
+ public:
   using Base::cols;
+  using Base::rows;
+  using Base::size;
   using Index = Index_t;
   using Scalar = Scalar_t;
   static constexpr StorageType Storage = Store;
-  static constexpr bool IsVector = (StaticRows==1) || (StaticCols==1);
-  static constexpr bool IsRowMajor = (Store==StorageType::RowMajor);
-  static constexpr bool IsColumnMajor = (Store==StorageType::ColumnMajor);
-  static constexpr size_t StaticSize = StaticRows*StaticCols;
+  static constexpr bool IsVector = (StaticRows == 1) || (StaticCols == 1);
+  static constexpr bool IsRowMajor = (Store == StorageType::RowMajor);
+  static constexpr bool IsColumnMajor = (Store == StorageType::ColumnMajor);
+  static constexpr size_t StaticSize = StaticRows * StaticCols;
 
   /*!
    * \brief Scalar iterator to the inner dimension of the container, read-only.
@@ -416,18 +397,18 @@ class C2DContainer :
    private:
     const Index m_increment;
     const Scalar* m_ptr;
+
    public:
     CInnerIter() = delete;
 
-    FORCEINLINE CInnerIter(const Scalar* ptr, Index increment) noexcept :
-      m_increment(increment),
-      m_ptr(ptr) {
-    }
+    FORCEINLINE CInnerIter(const Scalar* ptr, Index increment) noexcept : m_increment(increment), m_ptr(ptr) {}
 
-    FORCEINLINE Scalar operator* () const noexcept { return *m_ptr; }
+    FORCEINLINE Scalar operator*() const noexcept { return *m_ptr; }
 
     FORCEINLINE CInnerIter operator++(int) noexcept {
-      auto ret = *this; m_ptr += m_increment; return ret;
+      auto ret = *this;
+      m_ptr += m_increment;
+      return ret;
     }
   };
 
@@ -435,71 +416,72 @@ class C2DContainer :
    * \brief SIMD iterator to the inner dimension of the container,
    * read-only, generic non-contiguous access.
    */
-  template<class IndexSIMD_t>
+  template <class IndexSIMD_t>
   class CInnerIterGather {
    private:
-    static_assert(std::is_integral<typename IndexSIMD_t::Scalar>::value,"");
-    enum {Size = IndexSIMD_t::Size};
+    static_assert(std::is_integral<typename IndexSIMD_t::Scalar>::value, "");
+    enum { Size = IndexSIMD_t::Size };
     IndexSIMD_t m_offsets;
     const Index m_increment;
     const Scalar* const m_data;
+
    public:
     CInnerIterGather() = delete;
 
-    FORCEINLINE CInnerIterGather(const Scalar* data, Index increment, IndexSIMD_t offsets) noexcept :
-      m_offsets(offsets),
-      m_increment(increment),
-      m_data(data) {
-    }
+    FORCEINLINE CInnerIterGather(const Scalar* data, Index increment, IndexSIMD_t offsets) noexcept
+        : m_offsets(offsets), m_increment(increment), m_data(data) {}
 
-    FORCEINLINE simd::Array<Scalar,Size> operator* () const noexcept {
-      return simd::Array<Scalar,Size>(m_data, m_offsets);
+    FORCEINLINE simd::Array<Scalar, Size> operator*() const noexcept {
+      return simd::Array<Scalar, Size>(m_data, m_offsets);
     }
 
     FORCEINLINE CInnerIterGather operator++(int) noexcept {
-      auto ret = *this; m_offsets += m_increment; return ret;
+      auto ret = *this;
+      m_offsets += m_increment;
+      return ret;
     }
   };
 
-private:
+ private:
   /*!
    * \brief Logic to resize data according to arguments, a non DynamicSize cannot be changed.
    */
-  size_t m_resize(Index_t rows, Index_t cols) noexcept
-  {
+  size_t m_resize(Index_t rows, Index_t cols) noexcept {
     /*--- fully static, no allocation needed ---*/
-    if(StaticSize!=DynamicSize) return StaticSize;
+    if (StaticSize != DynamicSize) return StaticSize;
 
     /*--- dynamic row vector, swap size specification ---*/
-    if(StaticRows==1 && IsVector) {cols = rows; rows = 1;}
+    if (StaticRows == 1 && IsVector) {
+      cols = rows;
+      rows = 1;
+    }
 
     /*--- assert a static size is not being asked to change ---*/
-    if(StaticRows!=DynamicSize) assert(rows==StaticRows && "A static size was asked to change.");
-    if(StaticCols!=DynamicSize) assert(cols==StaticCols && "A static size was asked to change.");
+    if (StaticRows != DynamicSize) assert(rows == StaticRows && "A static size was asked to change.");
+    if (StaticCols != DynamicSize) assert(cols == StaticCols && "A static size was asked to change.");
 
     /*--- "rectify" sizes before continuing as asserts are usually dissabled ---*/
-    rows = (StaticRows!=DynamicSize)? StaticRows : rows;
-    cols = (StaticCols!=DynamicSize)? StaticCols : cols;
+    rows = (StaticRows != DynamicSize) ? StaticRows : rows;
+    cols = (StaticCols != DynamicSize) ? StaticCols : cols;
 
     /*--- number of requested elements ---*/
-    size_t reqSize = rows*cols;
+    size_t reqSize = rows * cols;
 
     /*--- compare with current dimensions to determine if deallocation
      is needed, also makes the container safe against self assignment
      no need to check for 0 size as the allocators handle that ---*/
-    if(rows==this->rows() && cols==this->cols())
-      return reqSize;
+    if (rows == this->rows() && cols == this->cols()) return reqSize;
 
     m_destroy();
 
     /*--- request actual allocation to base class as it needs specialization ---*/
-    size_t bytes = reqSize*sizeof(Scalar_t);
-    m_allocate(bytes,rows,cols);
+    size_t bytes = reqSize * sizeof(Scalar_t);
+    m_allocate(bytes, rows, cols);
 
     return reqSize;
   }
 
-public:
+ public:
   /*!
    * \brief Default ctor.
    */
@@ -509,27 +491,22 @@ class C2DContainer :
    * \brief Sizing ctor (no initialization of data).
    * For matrices size1 is rows and size2 columns, for vectors size1 is lenght and size2 is ignored.
    */
-  C2DContainer(const Index_t size1, const Index_t size2 = 1) noexcept : Base()
-  {
-    m_resize(size1,size2);
-  }
+  C2DContainer(const Index_t size1, const Index_t size2 = 1) noexcept : Base() { m_resize(size1, size2); }
 
   /*!
    * \brief Copy ctor.
    */
-  C2DContainer(const C2DContainer& other) noexcept : Base()
-  {
-    size_t sz = m_resize(other.rows(),other.cols());
-    for(size_t i=0; i<sz; ++i) m_data[i] = other.m_data[i];
+  C2DContainer(const C2DContainer& other) noexcept : Base() {
+    size_t sz = m_resize(other.rows(), other.cols());
+    for (size_t i = 0; i < sz; ++i) m_data[i] = other.m_data[i];
   }
 
   /*!
    * \brief Copy assignment operator, no re-allocation if sizes do not change.
    */
-  C2DContainer& operator= (const C2DContainer& other) noexcept
-  {
-    size_t sz = m_resize(other.rows(),other.cols());
-    for(size_t i=0; i<sz; ++i) m_data[i] = other.m_data[i];
+  C2DContainer& operator=(const C2DContainer& other) noexcept {
+    size_t sz = m_resize(other.rows(), other.cols());
+    for (size_t i = 0; i < sz; ++i) m_data[i] = other.m_data[i];
     return *this;
   }
 
@@ -541,13 +518,12 @@ class C2DContainer :
   /*!
    * \brief Move assign operator, implemented by base class (if fully static works as copy).
    */
-  C2DContainer& operator= (C2DContainer&&) = default;
+  C2DContainer& operator=(C2DContainer&&) = default;
 
   /*!
    * \overload Set all entries to rhs value (syntax sugar, see "resize").
    */
-  C2DContainer& operator= (const Scalar_t& value) noexcept
-  {
+  C2DContainer& operator=(const Scalar_t& value) noexcept {
     setConstant(value);
     return *this;
   }
@@ -558,35 +534,31 @@ class C2DContainer :
    * overloading ambiguities when Scalar_t = Index_t, so we do not. But it
    * is possible to assign a constant on top of resize: A.resize(m,n) = x;
    */
-  C2DContainer& resize(const Index_t size1, const Index_t size2 = 1) noexcept
-  {
-    m_resize(size1,size2);
+  C2DContainer& resize(const Index_t size1, const Index_t size2 = 1) noexcept {
+    m_resize(size1, size2);
     return *this;
   }
 
   /*!
    * \brief Set value of all entries to "value".
    */
-  void setConstant(const Scalar_t& value) noexcept
-  {
-    for(size_t i=0; i<size(); ++i) m_data[i] = value;
+  void setConstant(const Scalar_t& value) noexcept {
+    for (size_t i = 0; i < size(); ++i) m_data[i] = value;
   }
 
   /*!
    * \brief Get a scalar iterator to the inner dimension of the container.
    */
-  FORCEINLINE CInnerIter innerIter(Index_t row) const noexcept
-  {
-    return CInnerIter(&m_data[IsRowMajor? row*cols() : row], IsRowMajor? 1 : rows());
+  FORCEINLINE CInnerIter innerIter(Index_t row) const noexcept {
+    return CInnerIter(&m_data[IsRowMajor ? row * cols() : row], IsRowMajor ? 1 : rows());
   }
 
   /*!
    * \brief Get a SIMD gather iterator to the inner dimension of the container.
    */
-  template<class T, size_t N>
-  FORCEINLINE CInnerIterGather<simd::Array<T,N> > innerIter(simd::Array<T,N> row) const noexcept
-  {
-    return CInnerIterGather<simd::Array<T,N> >(m_data, IsRowMajor? 1 : rows(), IsRowMajor? row*cols() : row);
+  template <class T, size_t N>
+  FORCEINLINE CInnerIterGather<simd::Array<T, N> > innerIter(simd::Array<T, N> row) const noexcept {
+    return CInnerIterGather<simd::Array<T, N> >(m_data, IsRowMajor ? 1 : rows(), IsRowMajor ? row * cols() : row);
   }
 
   /*!
@@ -594,33 +566,31 @@ class C2DContainer :
    * \param[in] row - Row of the matrix.
    * \param[in] start - Starting column to copy the data (amount determined by container size).
    */
-  template<class StaticContainer>
-  FORCEINLINE StaticContainer get(Index_t row, Index_t start = 0) const noexcept
-  {
+  template <class StaticContainer>
+  FORCEINLINE StaticContainer get(Index_t row, Index_t start = 0) const noexcept {
     constexpr size_t Size = StaticContainer::StaticSize;
     static_assert(Size, "This method requires a static output type.");
-    assert(Size <= cols()-start);
+    assert(Size <= cols() - start);
     StaticContainer ret;
     SU2_OMP_SIMD
-    for (size_t i=0; i<Size; ++i)
-      ret.data()[i] = m_data[IsRowMajor? row*cols()+i+start : row+(i+start)*rows()];
+    for (size_t i = 0; i < Size; ++i)
+      ret.data()[i] = m_data[IsRowMajor ? row * cols() + i + start : row + (i + start) * rows()];
     return ret;
   }
 
   /*!
    * \brief Return copy of data in a static size container, SIMD version.
    */
-  template<class StaticContainer, class T, size_t N>
-  FORCEINLINE StaticContainer get(simd::Array<T,N> row, Index_t start = 0) const noexcept
-  {
+  template <class StaticContainer, class T, size_t N>
+  FORCEINLINE StaticContainer get(simd::Array<T, N> row, Index_t start = 0) const noexcept {
     constexpr size_t Size = StaticContainer::StaticSize;
     static_assert(Size, "This method requires a static output type.");
-    assert(Size <= cols()-start);
+    assert(Size <= cols() - start);
     StaticContainer ret;
-    for (size_t k=0; k<N; ++k) {
+    for (size_t k = 0; k < N; ++k) {
       SU2_OMP_SIMD_IF_NOT_AD
-      for (size_t i=0; i<Size; ++i)
-        ret.data()[i][k] = m_data[IsRowMajor? row[k]*cols()+i+start : row[k]+(i+start)*rows()];
+      for (size_t i = 0; i < Size; ++i)
+        ret.data()[i][k] = m_data[IsRowMajor ? row[k] * cols() + i + start : row[k] + (i + start) * rows()];
     }
     return ret;
   }
@@ -629,9 +599,12 @@ class C2DContainer :
 /*!
  * \brief Useful typedefs with default template parameters
  */
-template<class T> using su2vector = C2DContainer<unsigned long, T, StorageType::ColumnMajor, 64, DynamicSize, 1>;
-template<class T> using su2matrix = C2DContainer<unsigned long, T, StorageType::RowMajor,    64, DynamicSize, DynamicSize>;
-template<class T> using ColMajorMatrix = C2DContainer<unsigned long, T, StorageType::ColumnMajor, 64, DynamicSize, DynamicSize>;
+template <class T>
+using su2vector = C2DContainer<unsigned long, T, StorageType::ColumnMajor, 64, DynamicSize, 1>;
+template <class T>
+using su2matrix = C2DContainer<unsigned long, T, StorageType::RowMajor, 64, DynamicSize, DynamicSize>;
+template <class T>
+using ColMajorMatrix = C2DContainer<unsigned long, T, StorageType::ColumnMajor, 64, DynamicSize, DynamicSize>;
 
 using su2activevector = su2vector<su2double>;
 using su2activematrix = su2matrix<su2double>;
@@ -639,4 +612,4 @@ using su2activematrix = su2matrix<su2double>;
 using su2passivevector = su2vector<passivedouble>;
 using su2passivematrix = su2matrix<passivedouble>;
 
-/// @}
\ No newline at end of file
+/// @}
diff --git a/Common/include/containers/CFastFindAndEraseQueue.hpp b/Common/include/containers/CFastFindAndEraseQueue.hpp
index 01b24044e60..004500dcc86 100644
--- a/Common/include/containers/CFastFindAndEraseQueue.hpp
+++ b/Common/include/containers/CFastFindAndEraseQueue.hpp
@@ -43,19 +43,18 @@
  * \param[in] CleanupThreshold - Number of marked items that triggers full cleanup.
  * \note It would not be a good idea to use non-trivial item types.
  */
-template<typename ItemType_ = unsigned long,
-         ItemType_ ErasedValue_ = std::numeric_limits<ItemType_>::max(),
-         size_t CleanupThreshold = 8192>
+template <typename ItemType_ = unsigned long, ItemType_ ErasedValue_ = std::numeric_limits<ItemType_>::max(),
+          size_t CleanupThreshold = 8192>
 class CFastFindAndEraseQueue {
-public:
-  enum {ErasedValue = ErasedValue_};
+ public:
+  enum { ErasedValue = ErasedValue_ };
   using ItemType = ItemType_;
   using Iterator = typename std::vector<ItemType>::const_iterator;
 
-private:
+ private:
   size_t erasedCounter = 0;                     /*!< \brief How many items have been marked since last cleanup. */
   std::vector<ItemType> items;                  /*!< \brief The stored items. */
-  std::unordered_map<ItemType,size_t> indexes;  /*!< \brief Map items to their location. */
+  std::unordered_map<ItemType, size_t> indexes; /*!< \brief Map items to their location. */
 
   /*!
    * \brief Cleanup, shifts non-erased items forward, re-mapping them.
@@ -74,7 +73,7 @@ class CFastFindAndEraseQueue {
     erasedCounter = 0;
   }
 
-public:
+ public:
   /*!
    * \brief Default construct.
    */
@@ -85,7 +84,7 @@ class CFastFindAndEraseQueue {
    */
   CFastFindAndEraseQueue(size_t N) {
     items.resize(N);
-    for (size_t i=0; i<N; ++i) {
+    for (size_t i = 0; i < N; ++i) {
       items[i] = i;
       indexes[i] = i;
     }
@@ -112,7 +111,8 @@ class CFastFindAndEraseQueue {
    * \brief Get the item in front of the queue.
    */
   ItemType front() const {
-    for (auto value : items) if (value != ErasedValue) return value;
+    for (auto value : items)
+      if (value != ErasedValue) return value;
     assert(false && "Queue is empty.");
     return ErasedValue;
   }
@@ -127,7 +127,7 @@ class CFastFindAndEraseQueue {
 
     /*--- Get the item position. ---*/
     auto it = indexes.find(value);
-    if (it == indexes.end()) return false; // value is not here
+    if (it == indexes.end()) return false;  // value is not here
 
     const auto idx = it->second;
     assert(items[idx] != ErasedValue && "The item was already erased?!");
@@ -139,5 +139,4 @@ class CFastFindAndEraseQueue {
 
     return true;
   }
-
 };
diff --git a/Common/include/containers/CVertexMap.hpp b/Common/include/containers/CVertexMap.hpp
index a0152d22881..54e5ee85da0 100644
--- a/Common/include/containers/CVertexMap.hpp
+++ b/Common/include/containers/CVertexMap.hpp
@@ -49,15 +49,15 @@
  *
  * \note For efficiency use the smallest type that can fit the maximum number of vertices.
  */
-template<typename T = unsigned long>
+template <typename T = unsigned long>
 class CVertexMap {
   static_assert(std::is_unsigned<T>::value && std::is_integral<T>::value,
                 "Vertex map requires an unsigned integral type (e.g. unsigned).");
 
  private:
-  su2vector<T> Map;      /*!< \brief Map from range 0-(nPoint-1) to 1-nVertex. */
-  bool isValid = false;  /*!< \brief Set to true when it is safe to use the accessors. */
-  T nVertex = 0;         /*!< \brief Number of vertices. */
+  su2vector<T> Map;     /*!< \brief Map from range 0-(nPoint-1) to 1-nVertex. */
+  bool isValid = false; /*!< \brief Set to true when it is safe to use the accessors. */
+  T nVertex = 0;        /*!< \brief Number of vertices. */
 
  public:
   /*!
@@ -94,9 +94,7 @@ class CVertexMap {
   /*!
    * \brief Get wheter a point is marked as vertex.
    */
-  inline bool GetIsVertex(unsigned long iPoint) const {
-    return (Map(iPoint) != 0);
-  }
+  inline bool GetIsVertex(unsigned long iPoint) const { return (Map(iPoint) != 0); }
 
   /*!
    * \brief Build the point to vertex map.
@@ -108,8 +106,7 @@ class CVertexMap {
       nVertex = 0;
 
       for (unsigned long iPoint = 0; iPoint < Map.size(); ++iPoint)
-        if (Map(iPoint)!=0)
-          Map(iPoint) = ++nVertex;
+        if (Map(iPoint) != 0) Map(iPoint) = ++nVertex;
 
       isValid = true;
     }
@@ -121,12 +118,11 @@ class CVertexMap {
    * \param[in,out] iVertex - On entry point index, on exit vertex index.
    * \return True if conversion is successful (i.e. point is vertex).
    */
-  inline bool GetVertexIndex(unsigned long &iVertex) const {
+  inline bool GetVertexIndex(unsigned long& iVertex) const {
     assert(isValid && "Vertex map is not in valid state.");
     iVertex = Map(iVertex);
-    if(iVertex==0) return false; // not a vertex
-    iVertex--;    // decrement for 0 based
-    return true;  // is a vertex
+    if (iVertex == 0) return false;  // not a vertex
+    iVertex--;                       // decrement for 0 based
+    return true;                     // is a vertex
   }
-
 };
diff --git a/Common/include/containers/container_decorators.hpp b/Common/include/containers/container_decorators.hpp
index 5484a7e873e..c6c0f3f1201 100644
--- a/Common/include/containers/container_decorators.hpp
+++ b/Common/include/containers/container_decorators.hpp
@@ -36,49 +36,55 @@
 /*!
  * \brief Class to represent a matrix (without owning the data, this just wraps a pointer).
  */
-template<class T>
+template <class T>
 class CMatrixView {
-public:
+ public:
   using Scalar = typename std::remove_const<T>::type;
   using Index = unsigned long;
 
-private:
+ private:
   T* m_ptr;
   Index m_cols;
 
-public:
+ public:
   CMatrixView(T* ptr = nullptr, Index cols = 0) : m_ptr(ptr), m_cols(cols) {}
 
-  template<class U> friend class CMatrixView;
-  template<class U>
+  template <class U>
+  friend class CMatrixView;
+  template <class U>
   CMatrixView(const CMatrixView<U>& other) : m_ptr(other.m_ptr), m_cols(other.m_cols) {}
 
   explicit CMatrixView(su2matrix<Scalar>& mat) : m_ptr(mat.data()), m_cols(mat.cols()) {}
 
-  template<class U = T, su2enable_if<std::is_const<U>::value> = 0>
+  template <class U = T, su2enable_if<std::is_const<U>::value> = 0>
   explicit CMatrixView(const su2matrix<Scalar>& mat) : m_ptr(mat.data()), m_cols(mat.cols()) {}
 
-  const Scalar* operator[] (Index i) const noexcept { return &m_ptr[i*m_cols]; }
-  const Scalar& operator() (Index i, Index j) const noexcept { return m_ptr[i*m_cols + j]; }
+  const Scalar* operator[](Index i) const noexcept { return &m_ptr[i * m_cols]; }
+  const Scalar& operator()(Index i, Index j) const noexcept { return m_ptr[i * m_cols + j]; }
 
-  template<class U = T, su2enable_if<!std::is_const<U>::value> = 0>
-  Scalar* operator[] (Index i) noexcept { return &m_ptr[i*m_cols]; }
+  template <class U = T, su2enable_if<!std::is_const<U>::value> = 0>
+  Scalar* operator[](Index i) noexcept {
+    return &m_ptr[i * m_cols];
+  }
 
-  template<class U = T, su2enable_if<!std::is_const<U>::value> = 0>
-  Scalar& operator() (Index i, Index j) noexcept { return m_ptr[i*m_cols + j]; }
+  template <class U = T, su2enable_if<!std::is_const<U>::value> = 0>
+  Scalar& operator()(Index i, Index j) noexcept {
+    return m_ptr[i * m_cols + j];
+  }
 
-  friend CMatrixView operator+ (CMatrixView mv, Index incr) { return CMatrixView(mv[incr], mv.m_cols); }
+  friend CMatrixView operator+(CMatrixView mv, Index incr) { return CMatrixView(mv[incr], mv.m_cols); }
 };
 
 /*!
  * \class C3DContainerDecorator
  * \brief Decorate a matrix type (Storage) with 3 dimensions.
  */
-template<class Storage>
+template <class Storage>
 class C3DContainerDecorator {
   static_assert(!Storage::IsVector, "Storage type must be a matrix.");
   static_assert(Storage::IsRowMajor, "Storage type must be row major.");
-public:
+
+ public:
   using Scalar = typename Storage::Scalar;
   using Index = typename Storage::Index;
   static constexpr bool IsRowMajor = true;
@@ -88,14 +94,14 @@ class C3DContainerDecorator {
   using ConstMatrix = CMatrixView<const Scalar>;
 
   using CInnerIter = typename Storage::CInnerIter;
-  template<class T, size_t N>
-  using CInnerIterGather = typename Storage::template CInnerIterGather<simd::Array<T,N> >;
+  template <class T, size_t N>
+  using CInnerIterGather = typename Storage::template CInnerIterGather<simd::Array<T, N> >;
 
-private:
+ private:
   Storage m_storage;
   Index m_innerSz;
 
-public:
+ public:
   C3DContainerDecorator() = default;
 
   C3DContainerDecorator(Index length, Index rows, Index cols, Scalar value = 0) noexcept {
@@ -104,7 +110,7 @@ class C3DContainerDecorator {
 
   void resize(Index length, Index rows, Index cols, Scalar value = 0) noexcept {
     m_innerSz = cols;
-    m_storage.resize(length, rows*cols) = value;
+    m_storage.resize(length, rows * cols) = value;
   }
 
   /*!
@@ -118,34 +124,36 @@ class C3DContainerDecorator {
   /*!
    * \brief Element-wise access.
    */
-  Scalar& operator() (Index i, Index j, Index k) noexcept { return m_storage(i, j*m_innerSz + k); }
-  const Scalar& operator() (Index i, Index j, Index k) const noexcept { return m_storage(i, j*m_innerSz + k); }
+  Scalar& operator()(Index i, Index j, Index k) noexcept { return m_storage(i, j * m_innerSz + k); }
+  const Scalar& operator()(Index i, Index j, Index k) const noexcept { return m_storage(i, j * m_innerSz + k); }
 
   /*!
    * \brief Matrix access.
    */
-  Matrix operator[] (Index i) noexcept { return Matrix(m_storage[i], m_innerSz); }
-  ConstMatrix operator[] (Index i) const noexcept { return ConstMatrix(m_storage[i], m_innerSz); }
+  Matrix operator[](Index i) noexcept { return Matrix(m_storage[i], m_innerSz); }
+  ConstMatrix operator[](Index i) const noexcept { return ConstMatrix(m_storage[i], m_innerSz); }
 
   /*!
    * \brief Matrix access with an offset.
    */
-  Matrix operator() (Index i, Index j) noexcept { return Matrix(m_storage[i]+j*m_innerSz, m_innerSz); }
-  ConstMatrix operator() (Index i, Index j) const noexcept { return ConstMatrix(m_storage[i]+j*m_innerSz, m_innerSz); }
+  Matrix operator()(Index i, Index j) noexcept { return Matrix(m_storage[i] + j * m_innerSz, m_innerSz); }
+  ConstMatrix operator()(Index i, Index j) const noexcept {
+    return ConstMatrix(m_storage[i] + j * m_innerSz, m_innerSz);
+  }
 
   /*!
    * \brief Get a scalar iterator to the inner-most dimension of the container.
    */
   FORCEINLINE CInnerIter innerIter(Index i, Index j) const noexcept {
-    return CInnerIter(&m_storage(i, j*m_innerSz), 1);
+    return CInnerIter(&m_storage(i, j * m_innerSz), 1);
   }
 
   /*!
    * \brief Get a SIMD gather iterator to the inner-most dimension of the container.
    */
-  template<class T, size_t N>
-  FORCEINLINE CInnerIterGather<T,N> innerIter(simd::Array<T,N> i, Index j) const noexcept {
-    return CInnerIterGather<T,N>(m_storage.data(), 1, i*m_storage.cols() + j*m_innerSz);
+  template <class T, size_t N>
+  FORCEINLINE CInnerIterGather<T, N> innerIter(simd::Array<T, N> i, Index j) const noexcept {
+    return CInnerIterGather<T, N>(m_storage.data(), 1, i * m_storage.cols() + j * m_innerSz);
   }
 
   /*!
@@ -153,9 +161,9 @@ class C3DContainerDecorator {
    * \param[in] i - Outer index.
    * \param[in] j - Starting middle index for the copy (amount determined by container size).
    */
-  template<class StaticContainer, class Int>
+  template <class StaticContainer, class Int>
   FORCEINLINE StaticContainer get(Int i, Index j = 0) const noexcept {
-    return m_storage.template get<StaticContainer>(i, j*m_innerSz);
+    return m_storage.template get<StaticContainer>(i, j * m_innerSz);
   }
 };
 
@@ -173,9 +181,8 @@ using CVectorOfMatrix = C3DDoubleMatrix;
  * \note The constness of the object is derived from the template type, but
  *       we allways keep a reference, never a copy of the associated vector.
  */
-template<class T>
-struct C2DDummyLastView
-{
+template <class T>
+struct C2DDummyLastView {
   static_assert(T::IsVector, "This class decorates vectors.");
   using Index = typename T::Index;
   using Scalar = typename T::Scalar;
@@ -186,16 +193,12 @@ struct C2DDummyLastView
 
   C2DDummyLastView(T& ref) : data(ref) {}
 
-  template<class U = T, su2enable_if<!std::is_const<U>::value> = 0>
-  Scalar& operator() (Index i, Index) noexcept
-  {
+  template <class U = T, su2enable_if<!std::is_const<U>::value> = 0>
+  Scalar& operator()(Index i, Index) noexcept {
     return data(i);
   }
 
-  const Scalar& operator() (Index i, Index) const noexcept
-  {
-    return data(i);
-  }
+  const Scalar& operator()(Index i, Index) const noexcept { return data(i); }
 };
 
 /*!
@@ -205,9 +208,8 @@ struct C2DDummyLastView
  * \note The constness of the object is derived from the template type, but
  *       we allways keep a reference, never a copy of the associated matrix.
  */
-template<class T>
-struct C3DDummyMiddleView
-{
+template <class T>
+struct C3DDummyMiddleView {
   static_assert(!T::IsVector, "This class decorates matrices.");
   using Index = typename T::Index;
   using Scalar = typename T::Scalar;
@@ -218,16 +220,12 @@ struct C3DDummyMiddleView
 
   C3DDummyMiddleView(T& ref) : data(ref) {}
 
-  template<class U = T, su2enable_if<!std::is_const<U>::value> = 0>
-  Scalar& operator() (Index i, Index, Index k) noexcept
-  {
-    return data(i,k);
+  template <class U = T, su2enable_if<!std::is_const<U>::value> = 0>
+  Scalar& operator()(Index i, Index, Index k) noexcept {
+    return data(i, k);
   }
 
-  const Scalar& operator() (Index i, Index, Index k) const noexcept
-  {
-    return data(i,k);
-  }
+  const Scalar& operator()(Index i, Index, Index k) const noexcept { return data(i, k); }
 };
 
 /*--- Helper functions to allocate containers of containers. ---*/
@@ -241,10 +239,10 @@ struct C3DDummyMiddleView
  * \tparam IndexVector - type of N
  * \tparam VectorOfVector - type of X
  */
-template<class IndexVector, class VectorOfVector, class Scalar = int>
+template <class IndexVector, class VectorOfVector, class Scalar = int>
 inline void AllocVectorOfVectors(size_t M, const IndexVector& N, VectorOfVector& X, Scalar val = 0) {
   X.resize(M);
-  for(size_t i = 0; i < M; ++i){
+  for (size_t i = 0; i < M; ++i) {
     X[i].resize(N[i]);
     for (auto& x : X[i]) x = val;
   }
@@ -253,7 +251,7 @@ inline void AllocVectorOfVectors(size_t M, const IndexVector& N, VectorOfVector&
 /*!
  * \overload Deduce outer size from index vector.
  */
-template<class IndexVector, class VectorOfVector, class Scalar = int>
+template <class IndexVector, class VectorOfVector, class Scalar = int>
 inline void AllocVectorOfVectors(const IndexVector& N, VectorOfVector& X, Scalar val = 0) {
   auto M = N.size();
   AllocVectorOfVectors(M, N, X, val);
@@ -269,11 +267,11 @@ inline void AllocVectorOfVectors(const IndexVector& N, VectorOfVector& X, Scalar
  * \tparam IndexVector - type of N
  * \tparam VectorOfMatrix - type of X
  */
-template<class IndexVector, class VectorOfMatrix, class Scalar = int>
-inline void AllocVectorOfMatrices(size_t M, const IndexVector& N, size_t P, VectorOfMatrix& X, Scalar val=0) {
+template <class IndexVector, class VectorOfMatrix, class Scalar = int>
+inline void AllocVectorOfMatrices(size_t M, const IndexVector& N, size_t P, VectorOfMatrix& X, Scalar val = 0) {
   X.resize(M);
-  for(size_t i = 0; i < M; ++i){
-    X[i].resize(N[i],P);
+  for (size_t i = 0; i < M; ++i) {
+    X[i].resize(N[i], P);
     for (auto& x : X[i]) x = val;
   }
 }
@@ -281,10 +279,10 @@ inline void AllocVectorOfMatrices(size_t M, const IndexVector& N, size_t P, Vect
 /*!
  * \overload Deduce outer size from index vector.
  */
-template<class IndexVector, class VectorOfMatrix, class Scalar = int>
-inline void AllocVectorOfMatrices(const IndexVector& N, size_t P, VectorOfMatrix& X, Scalar val=0) {
+template <class IndexVector, class VectorOfMatrix, class Scalar = int>
+inline void AllocVectorOfMatrices(const IndexVector& N, size_t P, VectorOfMatrix& X, Scalar val = 0) {
   auto M = N.size();
   AllocVectorOfMatrices(M, N, P, X, val);
 }
 
-/// @}
\ No newline at end of file
+/// @}
diff --git a/Common/include/fem/fem_cgns_elements.hpp b/Common/include/fem/fem_cgns_elements.hpp
index 16af6f34ecc..8e9458d8d06 100644
--- a/Common/include/fem/fem_cgns_elements.hpp
+++ b/Common/include/fem/fem_cgns_elements.hpp
@@ -32,7 +32,7 @@
 #include "../parallelization/mpi_structure.hpp"
 
 #ifdef HAVE_CGNS
-  #include "cgnslib.h"
+#include "cgnslib.h"
 #endif
 
 #include "../geometry/primal_grid/CPrimalGridFEM.hpp"
@@ -49,229 +49,148 @@ class CBoundaryFace;
  */
 
 class CCGNSElementType {
-public:
-  int           connID;      /*!< \brief CGNS connectivity ID of this connectivity. */
-  ElementType_t elemType;    /*!< \brief Element type according to the CGNS convention,
-                                         possibly MIXED. */
-  cgsize_t      indBeg;      /*!< \brief Index of the first element in the CGNS connectivity. */
-  cgsize_t      indEnd;      /*!< \brief Index of the last element in the CGNS connectivity. */
-  cgsize_t      nElem;       /*!< \brief Number of elements present for this element type. */
+ public:
+  int connID;             /*!< \brief CGNS connectivity ID of this connectivity. */
+  ElementType_t elemType; /*!< \brief Element type according to the CGNS convention,
+                                      possibly MIXED. */
+  cgsize_t indBeg;        /*!< \brief Index of the first element in the CGNS connectivity. */
+  cgsize_t indEnd;        /*!< \brief Index of the last element in the CGNS connectivity. */
+  cgsize_t nElem;         /*!< \brief Number of elements present for this element type. */
 
-  std::string connName;      /*!< \brief Name of this connectivity. */
+  std::string connName; /*!< \brief Name of this connectivity. */
 
-  bool volumeConn;           /*!< \brief Whether or not this is a volume connectivity. */
-  bool surfaceConn;          /*!< \brief Whether or not this is a surface connectivity. */
+  bool volumeConn;  /*!< \brief Whether or not this is a volume connectivity. */
+  bool surfaceConn; /*!< \brief Whether or not this is a surface connectivity. */
 
   /* Standard constructor, nothing to be done. */
-  CCGNSElementType(){}
+  CCGNSElementType() {}
 
   /* Destructor, nothing to be done. */
-  ~CCGNSElementType(){}
+  ~CCGNSElementType() {}
 
   /*--- Member function, which determines the meta data for this element type. ---*/
-  void DetermineMetaData(const unsigned short nDim,
-                         const int            fn,
-                         const int            iBase,
-                         const int            iZone,
-                         const int            iConn);
+  void DetermineMetaData(const unsigned short nDim, const int fn, const int iBase, const int iZone, const int iConn);
 
   /*--- Member function, which reads the required boundary connectivity range. ---*/
-  void ReadBoundaryConnectivityRange(const int             fn,
-                                     const int             iBase,
-                                     const int             iZone,
-                                     const unsigned long   offsetRank,
-                                     const unsigned long   nBoundElemRank,
-                                     const unsigned long   startingBoundElemIDRank,
-                                     unsigned long         &locBoundElemCount,
-                                     std::vector<CBoundaryFace> &boundElems);
+  void ReadBoundaryConnectivityRange(const int fn, const int iBase, const int iZone, const unsigned long offsetRank,
+                                     const unsigned long nBoundElemRank, const unsigned long startingBoundElemIDRank,
+                                     unsigned long& locBoundElemCount, std::vector<CBoundaryFace>& boundElems);
 
   /*--- Member function, which reads the required connectivity range. ---*/
-  void ReadConnectivityRange(const int           fn,
-                             const int           iBase,
-                             const int           iZone,
-                             const unsigned long offsetRank,
-                             const unsigned long nElemRank,
-                             const unsigned long startingElemIDRank,
-                             CPrimalGrid         **&elem,
-                             unsigned long       &locElemCount,
-                             unsigned long       &nDOFsLoc);
-private:
+  void ReadConnectivityRange(const int fn, const int iBase, const int iZone, const unsigned long offsetRank,
+                             const unsigned long nElemRank, const unsigned long startingElemIDRank, CPrimalGrid**& elem,
+                             unsigned long& locElemCount, unsigned long& nDOFsLoc);
+
+ private:
   /*--- Member function, which creates the required data for the given
         element type. ---*/
-  void CreateDataElementType(const ElementType_t    typeElem,
-                             unsigned short         &VTK_Type,
-                             unsigned short         &nPoly,
-                             unsigned short         &nDOFs,
-                             std::vector<unsigned short> &SU2ToCGNS);
+  void CreateDataElementType(const ElementType_t typeElem, unsigned short& VTK_Type, unsigned short& nPoly,
+                             unsigned short& nDOFs, std::vector<unsigned short>& SU2ToCGNS);
 
   /*--- Member function, which determines the element dimension, i.e. the
         number of parametric coordinates. ---*/
-  unsigned short DetermineElementDimension(const int fn,
-                                           const int iBase,
-                                           const int iZone);
+  unsigned short DetermineElementDimension(const int fn, const int iBase, const int iZone);
 
   /*--- Member function, which determines the element dimension when the
         connectivity is mixed. ---*/
-  unsigned short DetermineElementDimensionMixed(const int fn,
-                                                const int iBase,
-                                                const int iZone);
+  unsigned short DetermineElementDimensionMixed(const int fn, const int iBase, const int iZone);
 
   /*--- Member function, which determines the corresponding index of the
         given element in the stored types. If not present, a new index
         is created. ---*/
-  unsigned short IndexInStoredTypes(const ElementType_t             typeElem,
-                                    std::vector<ElementType_t>           &CGNS_Type,
-                                    std::vector<unsigned short>          &VTK_Type,
-                                    std::vector<unsigned short>          &nPoly,
-                                    std::vector<unsigned short>          &nDOFs,
-                                    std::vector<std::vector<unsigned short> > &SU2ToCGNS);
+  unsigned short IndexInStoredTypes(const ElementType_t typeElem, std::vector<ElementType_t>& CGNS_Type,
+                                    std::vector<unsigned short>& VTK_Type, std::vector<unsigned short>& nPoly,
+                                    std::vector<unsigned short>& nDOFs,
+                                    std::vector<std::vector<unsigned short> >& SU2ToCGNS);
 
   /*--- Functions to create the conversion data from CGNS format to SU2 format
         for all the supported CGNS elements. ---*/
-  void CreateDataNODE(unsigned short         &VTK_Type,
-                      unsigned short         &nPoly,
-                      unsigned short         &nDOFs,
-                      std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataBAR_2(unsigned short         &VTK_Type,
-                       unsigned short         &nPoly,
-                       unsigned short         &nDOFs,
-                       std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataBAR_3(unsigned short         &VTK_Type,
-                       unsigned short         &nPoly,
-                       unsigned short         &nDOFs,
-                       std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataBAR_4(unsigned short         &VTK_Type,
-                       unsigned short         &nPoly,
-                       unsigned short         &nDOFs,
-                       std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataBAR_5(unsigned short         &VTK_Type,
-                       unsigned short         &nPoly,
-                       unsigned short         &nDOFs,
-                       std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataTRI_3(unsigned short         &VTK_Type,
-                       unsigned short         &nPoly,
-                       unsigned short         &nDOFs,
-                       std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataTRI_6(unsigned short         &VTK_Type,
-                       unsigned short         &nPoly,
-                       unsigned short         &nDOFs,
-                       std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataTRI_10(unsigned short         &VTK_Type,
-                        unsigned short         &nPoly,
-                        unsigned short         &nDOFs,
-                        std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataTRI_15(unsigned short         &VTK_Type,
-                        unsigned short         &nPoly,
-                        unsigned short         &nDOFs,
-                        std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataQUAD_4(unsigned short         &VTK_Type,
-                        unsigned short         &nPoly,
-                        unsigned short         &nDOFs,
-                        std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataQUAD_9(unsigned short         &VTK_Type,
-                        unsigned short         &nPoly,
-                        unsigned short         &nDOFs,
-                        std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataQUAD_16(unsigned short         &VTK_Type,
-                         unsigned short         &nPoly,
-                         unsigned short         &nDOFs,
-                         std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataQUAD_25(unsigned short         &VTK_Type,
-                         unsigned short         &nPoly,
-                         unsigned short         &nDOFs,
-                         std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataTETRA_4(unsigned short         &VTK_Type,
-                         unsigned short         &nPoly,
-                         unsigned short         &nDOFs,
-                         std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataTETRA_10(unsigned short         &VTK_Type,
-                          unsigned short         &nPoly,
-                          unsigned short         &nDOFs,
-                          std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataTETRA_20(unsigned short         &VTK_Type,
-                          unsigned short         &nPoly,
-                          unsigned short         &nDOFs,
-                          std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataTETRA_35(unsigned short         &VTK_Type,
-                          unsigned short         &nPoly,
-                          unsigned short         &nDOFs,
-                          std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataPYRA_5(unsigned short         &VTK_Type,
-                        unsigned short         &nPoly,
-                        unsigned short         &nDOFs,
-                        std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataPYRA_14(unsigned short         &VTK_Type,
-                         unsigned short         &nPoly,
-                         unsigned short         &nDOFs,
-                         std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataPYRA_30(unsigned short         &VTK_Type,
-                         unsigned short         &nPoly,
-                         unsigned short         &nDOFs,
-                         std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataPYRA_55(unsigned short         &VTK_Type,
-                         unsigned short         &nPoly,
-                         unsigned short         &nDOFs,
-                         std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataPENTA_6(unsigned short         &VTK_Type,
-                         unsigned short         &nPoly,
-                         unsigned short         &nDOFs,
-                         std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataPENTA_18(unsigned short         &VTK_Type,
-                          unsigned short         &nPoly,
-                          unsigned short         &nDOFs,
-                          std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataPENTA_40(unsigned short         &VTK_Type,
-                          unsigned short         &nPoly,
-                          unsigned short         &nDOFs,
-                          std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataPENTA_75(unsigned short         &VTK_Type,
-                          unsigned short         &nPoly,
-                          unsigned short         &nDOFs,
-                          std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataHEXA_8(unsigned short         &VTK_Type,
-                        unsigned short         &nPoly,
-                        unsigned short         &nDOFs,
-                        std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataHEXA_27(unsigned short         &VTK_Type,
-                         unsigned short         &nPoly,
-                         unsigned short         &nDOFs,
-                         std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataHEXA_64(unsigned short         &VTK_Type,
-                         unsigned short         &nPoly,
-                         unsigned short         &nDOFs,
-                         std::vector<unsigned short> &SU2ToCGNS);
-
-  void CreateDataHEXA_125(unsigned short         &VTK_Type,
-                          unsigned short         &nPoly,
-                          unsigned short         &nDOFs,
-                          std::vector<unsigned short> &SU2ToCGNS);
+  void CreateDataNODE(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                      std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataBAR_2(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                       std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataBAR_3(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                       std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataBAR_4(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                       std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataBAR_5(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                       std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataTRI_3(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                       std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataTRI_6(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                       std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataTRI_10(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                        std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataTRI_15(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                        std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataQUAD_4(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                        std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataQUAD_9(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                        std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataQUAD_16(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                         std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataQUAD_25(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                         std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataTETRA_4(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                         std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataTETRA_10(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                          std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataTETRA_20(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                          std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataTETRA_35(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                          std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataPYRA_5(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                        std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataPYRA_14(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                         std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataPYRA_30(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                         std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataPYRA_55(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                         std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataPENTA_6(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                         std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataPENTA_18(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                          std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataPENTA_40(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                          std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataPENTA_75(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                          std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataHEXA_8(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                        std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataHEXA_27(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                         std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataHEXA_64(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                         std::vector<unsigned short>& SU2ToCGNS);
+
+  void CreateDataHEXA_125(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                          std::vector<unsigned short>& SU2ToCGNS);
 };
 #endif
 #endif
diff --git a/Common/include/fem/fem_gauss_jacobi_quadrature.hpp b/Common/include/fem/fem_gauss_jacobi_quadrature.hpp
index d6ccbe227e3..04a450d8cce 100644
--- a/Common/include/fem/fem_gauss_jacobi_quadrature.hpp
+++ b/Common/include/fem/fem_gauss_jacobi_quadrature.hpp
@@ -98,7 +98,7 @@ using namespace std;
  * \version 7.5.1 "Blackbird"
  */
 class CGaussJacobiQuadrature {
-public:
+ public:
   /*!
    * \brief Function, which serves as the API to compute the integration points
             and weights.
@@ -111,30 +111,29 @@ class CGaussJacobiQuadrature {
    * \param[in,out] GJPoints  Location of the Gauss-Jacobi integration points.
    * \param[in,out] GJWeights Weights of the Gauss-Jacobi integration points.
    */
-  void GetQuadraturePoints(const passivedouble   alpha,     const passivedouble   beta,
-                           const passivedouble   a,         const passivedouble   b,
-                           vector<passivedouble> &GJPoints, vector<passivedouble> &GJWeights);
-private:
+  void GetQuadraturePoints(const passivedouble alpha, const passivedouble beta, const passivedouble a,
+                           const passivedouble b, vector<passivedouble>& GJPoints, vector<passivedouble>& GJWeights);
+
+ private:
   /*!
    * \brief Function in the original implementation of John Burkardt to compute
             the integration points of the Gauss-Jacobi quadrature rule.
    */
-  void cdgqf(int nt, int kind, passivedouble alpha, passivedouble beta, passivedouble t[],
-             passivedouble wts[]);
+  void cdgqf(int nt, int kind, passivedouble alpha, passivedouble beta, passivedouble t[], passivedouble wts[]);
 
   /*!
    * \brief Function in the original implementation of John Burkardt to compute
             the integration points of the Gauss-Jacobi quadrature rule.
    */
-  void cgqf(int nt, int kind, passivedouble alpha, passivedouble beta, passivedouble a,
-            passivedouble b, passivedouble t[], passivedouble wts[]);
+  void cgqf(int nt, int kind, passivedouble alpha, passivedouble beta, passivedouble a, passivedouble b,
+            passivedouble t[], passivedouble wts[]);
 
   /*!
    * \brief Function in the original implementation of John Burkardt to compute
             the integration points of the Gauss-Jacobi quadrature rule.
    */
-  passivedouble class_matrix(int kind, int m, passivedouble alpha, passivedouble beta,
-                             passivedouble aj[], passivedouble bj[]);
+  passivedouble class_matrix(int kind, int m, passivedouble alpha, passivedouble beta, passivedouble aj[],
+                             passivedouble bj[]);
 
   /*!
    * \brief Function in the original implementation of John Burkardt to compute
@@ -165,8 +164,8 @@ class CGaussJacobiQuadrature {
             the integration points of the Gauss-Jacobi quadrature rule.
    */
   void scqf(int nt, const passivedouble t[], const int mlt[], const passivedouble wts[], int nwts, int ndx[],
-            passivedouble swts[], passivedouble st[], int kind, passivedouble alpha,
-            passivedouble beta, passivedouble a, passivedouble b);
+            passivedouble swts[], passivedouble st[], int kind, passivedouble alpha, passivedouble beta,
+            passivedouble a, passivedouble b);
 
   /*!
    * \brief Function in the original implementation of John Burkardt to compute
diff --git a/Common/include/fem/fem_geometry_structure.hpp b/Common/include/fem/fem_geometry_structure.hpp
index 4974a6fbbc9..a6b79f276cc 100644
--- a/Common/include/fem/fem_geometry_structure.hpp
+++ b/Common/include/fem/fem_geometry_structure.hpp
@@ -44,15 +44,19 @@ using namespace std;
  * \version 7.5.1 "Blackbird"
  */
 struct CLong3T {
-  long long0 = 0;  /*!< \brief First long to store in this class. */
-  long long1 = 0;  /*!< \brief Second long to store in this class. */
-  long long2 = 0;  /*!< \brief Third long to store in this class. */
+  long long0 = 0; /*!< \brief First long to store in this class. */
+  long long1 = 0; /*!< \brief Second long to store in this class. */
+  long long2 = 0; /*!< \brief Third long to store in this class. */
 
   CLong3T() = default;
 
-  CLong3T(const long a, const long b, const long c) {long0 = a; long1 = b; long2 = c;}
+  CLong3T(const long a, const long b, const long c) {
+    long0 = a;
+    long1 = b;
+    long2 = c;
+  }
 
-  bool operator<(const CLong3T &other) const;
+  bool operator<(const CLong3T& other) const;
 };
 
 /*!
@@ -62,26 +66,23 @@ struct CLong3T {
  * \version 7.5.1 "Blackbird"
  */
 class CReorderElements {
-private:
-  unsigned long  globalElemID; /*!< \brief Global element ID of the element. */
-  unsigned short timeLevel;    /*!< \brief Time level of the element. Only relevant
-                                           for time accurate local time stepping. */
-  bool           commSolution; /*!< \brief Whether or not the solution must be
-                                           communicated to other ranks. */
-  unsigned short elemType;     /*!< \brief Short hand for the element type, Which
-                                           stored info of the VTK_Type, polynomial
-                                           degree of the solution and whether or
-                                           not the Jacobian is constant. */
-public:
+ private:
+  unsigned long globalElemID; /*!< \brief Global element ID of the element. */
+  unsigned short timeLevel;   /*!< \brief Time level of the element. Only relevant
+                                          for time accurate local time stepping. */
+  bool commSolution;          /*!< \brief Whether or not the solution must be
+                                          communicated to other ranks. */
+  unsigned short elemType;    /*!< \brief Short hand for the element type, Which
+                                          stored info of the VTK_Type, polynomial
+                                          degree of the solution and whether or
+                                          not the Jacobian is constant. */
+ public:
   /*!
    * \brief Constructor of the class, set the member variables to the arguments.
    */
-  CReorderElements(const unsigned long  val_GlobalElemID,
-                   const unsigned short val_TimeLevel,
-                   const bool           val_CommSolution,
-                   const unsigned short val_VTK_Type,
-                   const unsigned short val_nPolySol,
-                   const bool           val_JacConstant);
+  CReorderElements(const unsigned long val_GlobalElemID, const unsigned short val_TimeLevel,
+                   const bool val_CommSolution, const unsigned short val_VTK_Type, const unsigned short val_nPolySol,
+                   const bool val_JacConstant);
 
   /*!
    * \brief Default constructor of the class. Disabled.
@@ -91,7 +92,7 @@ class CReorderElements {
   /*!
    * \brief Less than operator of the class. Needed for the sorting.
    */
-  bool operator<(const CReorderElements &other) const;
+  bool operator<(const CReorderElements& other) const;
 
   /*!
    * \brief Function to make available the variable commSolution.
@@ -123,7 +124,6 @@ class CReorderElements {
    * \param[in] val_CommSolution  - value to which commSolution must be set.
    */
   inline void SetCommSolution(const bool val_CommSolution) { commSolution = val_CommSolution; }
-
 };
 
 /*!
@@ -133,21 +133,19 @@ class CReorderElements {
  * \author E. van der Weide
  * \version 7.5.1 "Blackbird"
  */
-class CVolumeElementFEM;   // Forward declaration to avoid problems.
+class CVolumeElementFEM;  // Forward declaration to avoid problems.
 class CSortFaces {
-private:
+ private:
   unsigned long nVolElemOwned; /*!< \brief Number of locally owned volume elements. */
   unsigned long nVolElemTot;   /*!< \brief Total number of local volume elements . */
 
-  const CVolumeElementFEM *volElem; /*!< \brief The locally stored volume elements. */
+  const CVolumeElementFEM* volElem; /*!< \brief The locally stored volume elements. */
 
-public:
+ public:
   /*!
    * \brief Constructor of the class. Set the values of the member variables.
    */
-  CSortFaces(unsigned long            val_nVolElemOwned,
-             unsigned long            val_nVolElemTot,
-             const CVolumeElementFEM *val_volElem) {
+  CSortFaces(unsigned long val_nVolElemOwned, unsigned long val_nVolElemTot, const CVolumeElementFEM* val_volElem) {
     nVolElemOwned = val_nVolElemOwned;
     nVolElemTot = val_nVolElemTot;
     volElem = val_volElem;
@@ -156,15 +154,14 @@ class CSortFaces {
   /*!
    * \brief Default constructor of the class. Disabled.
    */
-   CSortFaces(void) = delete;
+  CSortFaces(void) = delete;
 
- /*!
-  * \brief Operator used for the comparison.
-  * \param[in] f0 - First face in the comparison.
-  * \param[in] f1 - Second face in the comparison.
-  */
-  bool operator()(const CFaceOfElement &f0,
-                  const CFaceOfElement &f1);
+  /*!
+   * \brief Operator used for the comparison.
+   * \param[in] f0 - First face in the comparison.
+   * \param[in] f1 - Second face in the comparison.
+   */
+  bool operator()(const CFaceOfElement& f0, const CFaceOfElement& f1);
 };
 
 /*!
@@ -174,15 +171,14 @@ class CSortFaces {
  * \author E. van der Weide
  * \version 7.5.1 "Blackbird"
  */
-struct CSurfaceElementFEM;   // Forward declaration to avoid problems.
+struct CSurfaceElementFEM;  // Forward declaration to avoid problems.
 struct CSortBoundaryFaces {
- /*!
-  * \brief Operator used for the comparison.
-  * \param[in] f0 - First boundary face in the comparison.
-  * \param[in] f1 - Second boundary face in the comparison.
-  */
-  bool operator()(const CSurfaceElementFEM &f0,
-                  const CSurfaceElementFEM &f1);
+  /*!
+   * \brief Operator used for the comparison.
+   * \param[in] f0 - First boundary face in the comparison.
+   * \param[in] f1 - Second boundary face in the comparison.
+   */
+  bool operator()(const CSurfaceElementFEM& f0, const CSurfaceElementFEM& f1);
 };
 
 /*!
@@ -192,32 +188,32 @@ struct CSortBoundaryFaces {
  * \version 7.5.1 "Blackbird"
  */
 class CVolumeElementFEM {
-public:
+ public:
   bool elemIsOwned;             /*!< \brief Whether or not this is an owned element. */
   bool JacIsConsideredConstant; /*!< \brief Whether or not the Jacobian of the transformation
                                      to the standard element is considered constant. */
 
-  int rankOriginal;            /*!< \brief The rank where the original volume is stored. For
-                                    the owned volumes, this is simply the current rank. */
+  int rankOriginal; /*!< \brief The rank where the original volume is stored. For
+                         the owned volumes, this is simply the current rank. */
 
-  short periodIndexToDonor;    /*!< \brief The index of the periodic transformation to the donor
-                                    element. Only for halo elements. A -1 indicates no periodic
-                                    transformation. */
+  short periodIndexToDonor; /*!< \brief The index of the periodic transformation to the donor
+                                 element. Only for halo elements. A -1 indicates no periodic
+                                 transformation. */
 
-  unsigned short VTK_Type;     /*!< \brief Element type using the VTK convention. */
-  unsigned short nPolyGrid;    /*!< \brief Polynomial degree for the geometry of the element. */
-  unsigned short nPolySol;     /*!< \brief Polynomial degree for the solution of the element. */
-  unsigned short nDOFsGrid;    /*!< \brief Number of DOFs for the geometry of the element. */
-  unsigned short nDOFsSol;     /*!< \brief Number of DOFs for the solution of the element. */
-  unsigned short nFaces;       /*!< \brief Number of faces of the element. */
-  unsigned short timeLevel;    /*!< \brief Time level of the element when time accurate local
-                                           time stepping is employed. */
+  unsigned short VTK_Type;  /*!< \brief Element type using the VTK convention. */
+  unsigned short nPolyGrid; /*!< \brief Polynomial degree for the geometry of the element. */
+  unsigned short nPolySol;  /*!< \brief Polynomial degree for the solution of the element. */
+  unsigned short nDOFsGrid; /*!< \brief Number of DOFs for the geometry of the element. */
+  unsigned short nDOFsSol;  /*!< \brief Number of DOFs for the solution of the element. */
+  unsigned short nFaces;    /*!< \brief Number of faces of the element. */
+  unsigned short timeLevel; /*!< \brief Time level of the element when time accurate local
+                                        time stepping is employed. */
 
   unsigned short indStandardElement; /*!< \brief Index in the vector of standard elements. */
 
-  unsigned int factTimeLevel;        /*!< \brief Number of local time steps for this element
-                                                 compared to the largest time step when time
-                                                 accurate local time stepping is employed. */
+  unsigned int factTimeLevel; /*!< \brief Number of local time steps for this element
+                                          compared to the largest time step when time
+                                          accurate local time stepping is employed. */
 
   unsigned long elemIDGlobal;        /*!< \brief Global element ID of this element. */
   unsigned long offsetDOFsSolGlobal; /*!< \brief Global offset of the solution DOFs of this element. */
@@ -236,35 +232,34 @@ class CVolumeElementFEM {
 
   vector<unsigned long> nodeIDsGrid; /*!< \brief Vector with the node IDs of the grid for this element. */
 
-  su2double lenScale;                /*!< \brief Length scale of the element. */
-
-  su2double shockSensorValue;               /*!< \brief Value for sensing a shock */
-  su2double shockArtificialViscosity;       /*!< \brief Artificial viscosity for a shock */
-
-
-  vector<su2double> metricTerms;            /*!< \brief Vector of the metric terms in the
-                                                        integration points of this element. */
-  vector<su2double> metricTermsSolDOFs;     /*!< \brief Vector of the metric terms in the
-                                                        solution DOFs of this element. */
-  vector<su2double> metricTerms2ndDer;      /*!< \brief Vector of the metric terms needed for the
-                                                        computation of the 2nd derivatives in the
-                                                        integration points. Only determined when
-                                                        needed (ADER-DG with non-aliased predictor
-                                                        for the Navier-Stokes equations). */
-  vector<su2double> gridVelocities;         /*!< \brief Vector of the grid velocities in the
-                                                        integration points of this element. */
-  vector<su2double> gridVelocitiesSolDOFs;  /*!< \brief Vector of the grid velocities in the
-                                                        solution DOFs of this element. */
-  vector<su2double> massMatrix;             /*!< \brief Mass matrix for this element. */
-  vector<su2double> invMassMatrix;          /*!< \brief Inverse mass matrix for this element. */
-  vector<su2double> lumpedMassMatrix;       /*!< \brief Lumped mass matrix for this element. */
-
-  vector<su2double> coorIntegrationPoints;  /*!< \brief The coordinates of the integration points of this element. */
-  vector<su2double> coorSolDOFs;            /*!< \brief The coordinates of the solution DOFs of this element. */
-  vector<su2double> wallDistance;           /*!< \brief The wall distance to the viscous walls for
-                                                        the integration points of this element. */
-  vector<su2double> wallDistanceSolDOFs;    /*!< \brief The wall distance to the viscous walls for
-                                                        the solution DOFs of this element. */
+  su2double lenScale; /*!< \brief Length scale of the element. */
+
+  su2double shockSensorValue;         /*!< \brief Value for sensing a shock */
+  su2double shockArtificialViscosity; /*!< \brief Artificial viscosity for a shock */
+
+  vector<su2double> metricTerms;           /*!< \brief Vector of the metric terms in the
+                                                       integration points of this element. */
+  vector<su2double> metricTermsSolDOFs;    /*!< \brief Vector of the metric terms in the
+                                                       solution DOFs of this element. */
+  vector<su2double> metricTerms2ndDer;     /*!< \brief Vector of the metric terms needed for the
+                                                       computation of the 2nd derivatives in the
+                                                       integration points. Only determined when
+                                                       needed (ADER-DG with non-aliased predictor
+                                                       for the Navier-Stokes equations). */
+  vector<su2double> gridVelocities;        /*!< \brief Vector of the grid velocities in the
+                                                       integration points of this element. */
+  vector<su2double> gridVelocitiesSolDOFs; /*!< \brief Vector of the grid velocities in the
+                                                       solution DOFs of this element. */
+  vector<su2double> massMatrix;            /*!< \brief Mass matrix for this element. */
+  vector<su2double> invMassMatrix;         /*!< \brief Inverse mass matrix for this element. */
+  vector<su2double> lumpedMassMatrix;      /*!< \brief Lumped mass matrix for this element. */
+
+  vector<su2double> coorIntegrationPoints; /*!< \brief The coordinates of the integration points of this element. */
+  vector<su2double> coorSolDOFs;           /*!< \brief The coordinates of the solution DOFs of this element. */
+  vector<su2double> wallDistance;          /*!< \brief The wall distance to the viscous walls for
+                                                       the integration points of this element. */
+  vector<su2double> wallDistanceSolDOFs;   /*!< \brief The wall distance to the viscous walls for
+                                                       the solution DOFs of this element. */
 
   /*!
    * \brief Get all the corner points of all the faces of this element. It must be made sure
@@ -274,9 +269,7 @@ class CVolumeElementFEM {
    * \param[out] nPointsPerFace - Number of corner points for each of the faces.
    * \param[out] faceConn       - Global IDs of the corner points of the faces.
    */
-  void GetCornerPointsAllFaces(unsigned short &numFaces,
-                               unsigned short nPointsPerFace[],
-                               unsigned long  faceConn[6][4]);
+  void GetCornerPointsAllFaces(unsigned short& numFaces, unsigned short nPointsPerFace[], unsigned long faceConn[6][4]);
 };
 
 /*!
@@ -295,13 +288,12 @@ struct CPointFEM {
   /*!
    * \brief Less than operator of the class. Needed for the sorting.
    */
-  bool operator<(const CPointFEM &other) const;
+  bool operator<(const CPointFEM& other) const;
 
   /*!
    * \brief Equal operator of the class. Needed for the removal of double entities.
    */
-  bool operator==(const CPointFEM &other) const;
-
+  bool operator==(const CPointFEM& other) const;
 };
 
 /*!
@@ -311,42 +303,41 @@ struct CPointFEM {
  * \version 7.5.1 "Blackbird"
  */
 struct CInternalFaceElementFEM {
-  unsigned short VTK_Type;     /*!< \brief Element type using the VTK convention. */
+  unsigned short VTK_Type; /*!< \brief Element type using the VTK convention. */
 
   unsigned short indStandardElement; /*!< \brief Index in the vector of standard face elements. */
 
-  unsigned long elemID0;              /*!< \brief Element ID adjacent to side 0 of the face. */
-  unsigned long elemID1;              /*!< \brief Element ID adjacent to side 1 of the face. */
+  unsigned long elemID0; /*!< \brief Element ID adjacent to side 0 of the face. */
+  unsigned long elemID1; /*!< \brief Element ID adjacent to side 1 of the face. */
 
-  vector<unsigned long> DOFsGridFaceSide0;   /*!< \brief Vector of the grid DOFs of side 0 of the face. */
-  vector<unsigned long> DOFsGridFaceSide1;   /*!< \brief Vector of the grid DOFs of side 1 of the face. */
-  vector<unsigned long> DOFsSolFaceSide0;    /*!< \brief Vector of the solution DOFs of side 0 of the face. */
-  vector<unsigned long> DOFsSolFaceSide1;    /*!< \brief Vector of the solution DOFs of side 1 of the face. */
+  vector<unsigned long> DOFsGridFaceSide0; /*!< \brief Vector of the grid DOFs of side 0 of the face. */
+  vector<unsigned long> DOFsGridFaceSide1; /*!< \brief Vector of the grid DOFs of side 1 of the face. */
+  vector<unsigned long> DOFsSolFaceSide0;  /*!< \brief Vector of the solution DOFs of side 0 of the face. */
+  vector<unsigned long> DOFsSolFaceSide1;  /*!< \brief Vector of the solution DOFs of side 1 of the face. */
 
-  vector<unsigned long> DOFsGridElementSide0;   /*!< \brief Vector of the grid DOFs of the element of side 0. */
-  vector<unsigned long> DOFsGridElementSide1;   /*!< \brief Vector of the grid DOFs of the element of side 1. */
-  vector<unsigned long> DOFsSolElementSide0;    /*!< \brief Vector of the solution DOFs of the element of side 0. */
-  vector<unsigned long> DOFsSolElementSide1;    /*!< \brief Vector of the solution DOFs of the element of side 1. */
+  vector<unsigned long> DOFsGridElementSide0; /*!< \brief Vector of the grid DOFs of the element of side 0. */
+  vector<unsigned long> DOFsGridElementSide1; /*!< \brief Vector of the grid DOFs of the element of side 1. */
+  vector<unsigned long> DOFsSolElementSide0;  /*!< \brief Vector of the solution DOFs of the element of side 0. */
+  vector<unsigned long> DOFsSolElementSide1;  /*!< \brief Vector of the solution DOFs of the element of side 1. */
 
-  vector<su2double> metricNormalsFace;     /*!< \brief The normals in the integration points of the face.
-                                                       The normals point from side 0 to side 1. */
-  vector<su2double> metricCoorDerivFace0;  /*!< \brief The terms drdx, dsdx, etc. of side 0 in the
-                                                       integration points of the face. */
-  vector<su2double> metricCoorDerivFace1;  /*!< \brief The terms dxdr, dydr, etc. of side 1 in the
-                                                       integration points of the face. */
+  vector<su2double> metricNormalsFace;    /*!< \brief The normals in the integration points of the face.
+                                                      The normals point from side 0 to side 1. */
+  vector<su2double> metricCoorDerivFace0; /*!< \brief The terms drdx, dsdx, etc. of side 0 in the
+                                                      integration points of the face. */
+  vector<su2double> metricCoorDerivFace1; /*!< \brief The terms dxdr, dydr, etc. of side 1 in the
+                                                      integration points of the face. */
 
-  vector<su2double> coorIntegrationPoints;  /*!< \brief Coordinates for the integration points of this face. */
-  vector<su2double> gridVelocities;         /*!< \brief Grid velocities in the integration points of this face. */
-  vector<su2double> wallDistance;           /*!< \brief The wall distance to the viscous walls for
-                                                        the integration points of this face. */
+  vector<su2double> coorIntegrationPoints; /*!< \brief Coordinates for the integration points of this face. */
+  vector<su2double> gridVelocities;        /*!< \brief Grid velocities in the integration points of this face. */
+  vector<su2double> wallDistance;          /*!< \brief The wall distance to the viscous walls for
+                                                       the integration points of this face. */
 
   /*!
    * \brief Less than operator of the class. Needed for the sorting.
             The criterion for comparison are the standard element and
             adjacent volume ID's.
    */
-  bool operator<(const CInternalFaceElementFEM &other) const;
-
+  bool operator<(const CInternalFaceElementFEM& other) const;
 };
 
 /*!
@@ -356,9 +347,9 @@ struct CInternalFaceElementFEM {
  * \version 7.5.1 "Blackbird"
  */
 struct CSurfaceElementFEM {
-  unsigned short VTK_Type;     /*!< \brief Element type using the VTK convention. */
-  unsigned short nPolyGrid;    /*!< \brief Polynomial degree for the geometry of the element. */
-  unsigned short nDOFsGrid;    /*!< \brief Number of DOFs for the geometry of the element. */
+  unsigned short VTK_Type;  /*!< \brief Element type using the VTK convention. */
+  unsigned short nPolyGrid; /*!< \brief Polynomial degree for the geometry of the element. */
+  unsigned short nDOFsGrid; /*!< \brief Number of DOFs for the geometry of the element. */
 
   unsigned short indStandardElement; /*!< \brief Index in the vector of standard elements. */
 
@@ -370,45 +361,44 @@ struct CSurfaceElementFEM {
                                                  In this vector the original sequence of the grid file
                                                  is stored. */
 
-  vector<unsigned long> DOFsGridFace;   /*!< \brief Vector of the grid DOFs of the face. In principle
-                                                    the same information as nodeIDsGrid, but the sequence
-                                                    could be different. */
-  vector<unsigned long> DOFsSolFace;    /*!< \brief Vector of the solution DOFs of the face. */
+  vector<unsigned long> DOFsGridFace; /*!< \brief Vector of the grid DOFs of the face. In principle
+                                                  the same information as nodeIDsGrid, but the sequence
+                                                  could be different. */
+  vector<unsigned long> DOFsSolFace;  /*!< \brief Vector of the solution DOFs of the face. */
 
-  vector<unsigned long> DOFsGridElement;   /*!< \brief Vector of the grid DOFs of the adjacent element. */
-  vector<unsigned long> DOFsSolElement;    /*!< \brief Vector of the solution DOFs of the adjacent element. */
+  vector<unsigned long> DOFsGridElement; /*!< \brief Vector of the grid DOFs of the adjacent element. */
+  vector<unsigned long> DOFsSolElement;  /*!< \brief Vector of the solution DOFs of the adjacent element. */
 
   vector<su2double> metricNormalsFace;     /*!< \brief The normals in the integration points of the face.
                                                        The normals point out of the adjacent element. */
   vector<su2double> metricCoorDerivFace;   /*!< \brief The terms drdx, dsdx, etc. in the integration
                                                        points of the face. */
   vector<su2double> coorIntegrationPoints; /*!< \brief The coordinates of the integration points of the face. */
-  vector<su2double> gridVelocities;         /*!< \brief Grid velocities in the integration points of this face. */
+  vector<su2double> gridVelocities;        /*!< \brief Grid velocities in the integration points of this face. */
   vector<su2double> wallDistance;          /*!< \brief The wall distances of the integration points
                                                        of the face. */
 
-  vector<unsigned long>  donorsWallFunction;        /*!< \brief Local element IDs of the donors for the wall
-                                                                function treatment. These donors can be halo's. */
-  vector<unsigned short> nIntPerWallFunctionDonor;  /*!< \brief The number of integration points per donor
-                                                                element for the wall function treatment. */
-  vector<unsigned short> intPerWallFunctionDonor;   /*!< \brief The integration points per donor element
-                                                                for the wall function treatment. */
-  vector<vector<su2double> > matWallFunctionDonor;  /*!< \brief Matrices, which store the interpolation coefficients
-                                                                for the donors of the integration points.*/
+  vector<unsigned long> donorsWallFunction;        /*!< \brief Local element IDs of the donors for the wall
+                                                               function treatment. These donors can be halo's. */
+  vector<unsigned short> nIntPerWallFunctionDonor; /*!< \brief The number of integration points per donor
+                                                               element for the wall function treatment. */
+  vector<unsigned short> intPerWallFunctionDonor;  /*!< \brief The integration points per donor element
+                                                               for the wall function treatment. */
+  vector<vector<su2double> > matWallFunctionDonor; /*!< \brief Matrices, which store the interpolation coefficients
+                                                               for the donors of the integration points.*/
 
   /*!
    * \brief Less than operator of the class. Needed for the sorting.
             The criterion for comparison is the corresponding (local) volume ID.
    */
-  bool operator<(const CSurfaceElementFEM &other) const { return volElemID < other.volElemID; }
+  bool operator<(const CSurfaceElementFEM& other) const { return volElemID < other.volElemID; }
 
   /*!
    *  \brief Function, which determines the corner points of this surface element.
    *  \param[out] nPointsPerFace - Number of corner points of the face.
    *  \param[out] faceConn       - The corner points of the face.
    */
-  void GetCornerPointsFace(unsigned short &nPointsPerFace,
-                           unsigned long  faceConn[]);
+  void GetCornerPointsFace(unsigned short& nPointsPerFace, unsigned long faceConn[]);
 };
 
 /*!
@@ -418,18 +408,18 @@ struct CSurfaceElementFEM {
  * \version 7.5.1 "Blackbird"
  */
 struct CBoundaryFEM {
-  string markerTag;  /*!< \brief Marker tag of this boundary. */
+  string markerTag; /*!< \brief Marker tag of this boundary. */
 
-  bool periodicBoundary = false;     /*!< \brief Whether or not this boundary is a periodic boundary. */
-  bool haloInfoNeededForBC = false;  /*!< \brief Whether or not information of halo elements
-                                                 is needed to impose the boundary conditions. */
+  bool periodicBoundary = false;    /*!< \brief Whether or not this boundary is a periodic boundary. */
+  bool haloInfoNeededForBC = false; /*!< \brief Whether or not information of halo elements
+                                                is needed to impose the boundary conditions. */
 
   vector<unsigned long> nSurfElem; /*!< \brief Number of surface elements per time level,
                                                cumulative storage format. */
 
   vector<CSurfaceElementFEM> surfElem; /*!< \brief Vector of the local surface elements. */
 
-  CWallModel *wallModel = nullptr;     /*!< \brief Wall model for LES. */
+  CWallModel* wallModel = nullptr; /*!< \brief Wall model for LES. */
 
   ~CBoundaryFEM(void) { delete wallModel; }
 };
@@ -440,205 +430,207 @@ struct CBoundaryFEM {
  * \author E. van der Weide
  * \version 7.5.1 "Blackbird"
  */
-class CMeshFEM: public CGeometry {
-protected:
-  unsigned long nVolElemTot{0};    /*!< \brief Total number of local volume elements, including halos. */
-  unsigned long nVolElemOwned{0};  /*!< \brief Number of owned local volume elements. */
+class CMeshFEM : public CGeometry {
+ protected:
+  unsigned long nVolElemTot{0};   /*!< \brief Total number of local volume elements, including halos. */
+  unsigned long nVolElemOwned{0}; /*!< \brief Number of owned local volume elements. */
 
   vector<unsigned long> nVolElemOwnedPerTimeLevel;    /*!< \brief Number of owned local volume elements
                                                                   per time level. Cumulative storage. */
   vector<unsigned long> nVolElemInternalPerTimeLevel; /*!< \brief Number of internal local volume elements per
                                                                   time level. Internal means that the solution
                                                                   data does not need to be communicated. */
-  vector<unsigned long> nVolElemHaloPerTimeLevel;    /*!< \brief Number of local halo volume elements
-                                                                 per time level. Cumulative storage. */
+  vector<unsigned long> nVolElemHaloPerTimeLevel;     /*!< \brief Number of local halo volume elements
+                                                                  per time level. Cumulative storage. */
 
   vector<vector<unsigned long> > ownedElemAdjLowTimeLevel; /*!< \brief List of owned elements per time level that are
                                                                        adjacent to elements of the lower time level. */
-  vector<vector<unsigned long> > haloElemAdjLowTimeLevel; /*!< \brief List of halo elements per time level that are
-                                                                      adjacent to elements of the lower time level. */
+  vector<vector<unsigned long> > haloElemAdjLowTimeLevel;  /*!< \brief List of halo elements per time level that are
+                                                                       adjacent to elements of the lower time level. */
 
   vector<CVolumeElementFEM> volElem; /*!< \brief Vector of the local volume elements, including halos. */
 
-  vector<CPointFEM> meshPoints;      /*!< \brief Vector of the points of the FEM mesh. */
+  vector<CPointFEM> meshPoints; /*!< \brief Vector of the points of the FEM mesh. */
 
-  vector<CBoundaryFEM> boundaries;   /*!< \brief Vector of the boundaries of the FEM mesh. */
+  vector<CBoundaryFEM> boundaries; /*!< \brief Vector of the boundaries of the FEM mesh. */
 
-  vector<unsigned short> rotPerMarkers; /*!< \brief Vector, which contains the indices of the rotational
-                                                    periodic markers. */
+  vector<unsigned short> rotPerMarkers;       /*!< \brief Vector, which contains the indices of the rotational
+                                                          periodic markers. */
   vector<vector<unsigned long> > rotPerHalos; /*!< \brief Vector of vector, which contains the indices of
                                                           the halo elements for which a rotationally periodic
                                                           correction must be applied. */
 
-  vector<int> ranksRecv;             /*!< \brief Vector of ranks, from which this rank will receive halo
-                                                 information. Self communication is included. */
-  vector<int> ranksSend;             /*!< \brief Vector of ranks, to which this rank will send halo
-                                                 information. Self communication is included. */
+  vector<int> ranksRecv; /*!< \brief Vector of ranks, from which this rank will receive halo
+                                     information. Self communication is included. */
+  vector<int> ranksSend; /*!< \brief Vector of ranks, to which this rank will send halo
+                                     information. Self communication is included. */
 
-  vector<vector<unsigned long> > entitiesSend;    /*!< \brief Vector of vector, which contains the entities that
-                                                              must be sent. Self communication is included. For DG
-                                                              an entitity is an element, for regular FEM an entity
-                                                              is a DOF. */
+  vector<vector<unsigned long> > entitiesSend; /*!< \brief Vector of vector, which contains the entities that
+                                                           must be sent. Self communication is included. For DG
+                                                           an entitity is an element, for regular FEM an entity
+                                                           is a DOF. */
   vector<vector<unsigned long> > entitiesRecv; /*!< \brief Vector of vector, which contains the entities that
                                                            must be received. Self communication is included. For DG
                                                            an entity is an element, for regular FEM an entity
                                                            is a DOF. */
 
-  vector<CFEMStandardBoundaryFace> standardBoundaryFacesSol;  /*!< \brief Vector that contains the standard boundary
-                                                                          faces used for the solution of the DG solver. */
-  vector<CFEMStandardBoundaryFace> standardBoundaryFacesGrid; /*!< \brief Vector that contains the standard boundary
-                                                                          faces used for the geometry of the DG solver. */
+  vector<CFEMStandardBoundaryFace>
+      standardBoundaryFacesSol; /*!< \brief Vector that contains the standard boundary
+                                            faces used for the solution of the DG solver. */
+  vector<CFEMStandardBoundaryFace>
+      standardBoundaryFacesGrid; /*!< \brief Vector that contains the standard boundary
+                                             faces used for the geometry of the DG solver. */
 
-  CBlasStructure *blasFunctions{nullptr}; /*!< \brief  Pointer to the object to carry out the BLAS functionalities. */
+  CBlasStructure* blasFunctions{nullptr}; /*!< \brief  Pointer to the object to carry out the BLAS functionalities. */
 
-public:
+ public:
   /*!
-  * \brief Constructor of the class.
-  */
- CMeshFEM(void) : CGeometry() { }
+   * \brief Constructor of the class.
+   */
+  CMeshFEM(void) : CGeometry() {}
 
   /*!
-  * \overload
-  * \brief Redistributes the grid over the ranks and creates the halo layer.
-  * \param[in] geometry - The linear distributed grid that must be redistributed.
-  * \param[in] config   - Definition of the particular problem.
-  */
-  CMeshFEM(CGeometry *geometry, CConfig *config);
+   * \overload
+   * \brief Redistributes the grid over the ranks and creates the halo layer.
+   * \param[in] geometry - The linear distributed grid that must be redistributed.
+   * \param[in] config   - Definition of the particular problem.
+   */
+  CMeshFEM(CGeometry* geometry, CConfig* config);
 
   /*!
-  * \brief Destructor of the class.
-  */
+   * \brief Destructor of the class.
+   */
   ~CMeshFEM(void) override { delete blasFunctions; }
 
   /*!
-  * \brief Function, which makes available the boundaries of the local FEM mesh.
-  * \return  Pointer to the boundaries of the local FEM mesh.
-  */
-  inline CBoundaryFEM* GetBoundaries(void) {return boundaries.data();}
+   * \brief Function, which makes available the boundaries of the local FEM mesh.
+   * \return  Pointer to the boundaries of the local FEM mesh.
+   */
+  inline CBoundaryFEM* GetBoundaries(void) { return boundaries.data(); }
 
   /*!
-  * \brief Function, which makes available the mesh points of the local FEM mesh.
-  * \return  Pointer to the mesh points of the local FEM mesh.
-  */
-  inline CPointFEM *GetMeshPoints(void) {return meshPoints.data();}
+   * \brief Function, which makes available the mesh points of the local FEM mesh.
+   * \return  Pointer to the mesh points of the local FEM mesh.
+   */
+  inline CPointFEM* GetMeshPoints(void) { return meshPoints.data(); }
 
   /*!
-  * \brief Function, which makes available the number of mesh points of the local FEM mesh.
-  * \return  Number of mesh points of the local FEM mesh.
-  */
-  inline unsigned long GetNMeshPoints(void) {return meshPoints.size();}
+   * \brief Function, which makes available the number of mesh points of the local FEM mesh.
+   * \return  Number of mesh points of the local FEM mesh.
+   */
+  inline unsigned long GetNMeshPoints(void) { return meshPoints.size(); }
 
   /*!
-  * \brief Function, which makes available the number of owned volume elements in the local FEM mesh.
-  * \return  Number of owned volume elements of the local FEM mesh.
-  */
-  inline unsigned long GetNVolElemOwned(void) const {return nVolElemOwned;}
+   * \brief Function, which makes available the number of owned volume elements in the local FEM mesh.
+   * \return  Number of owned volume elements of the local FEM mesh.
+   */
+  inline unsigned long GetNVolElemOwned(void) const { return nVolElemOwned; }
 
   /*!
-  * \brief Function, which makes available the total number of volume elements in the local FEM mesh.
-  * \return  Total number of volume elements of the local FEM mesh.
-  */
-  inline unsigned long GetNVolElemTot(void) const {return nVolElemTot;}
+   * \brief Function, which makes available the total number of volume elements in the local FEM mesh.
+   * \return  Total number of volume elements of the local FEM mesh.
+   */
+  inline unsigned long GetNVolElemTot(void) const { return nVolElemTot; }
 
   /*!
-  * \brief Function, which makes available the volume elements in the local FEM mesh.
-  * \return  Pointer to the volume elements of the local FEM mesh.
-  */
-  inline CVolumeElementFEM* GetVolElem(void) {return volElem.data();}
+   * \brief Function, which makes available the volume elements in the local FEM mesh.
+   * \return  Pointer to the volume elements of the local FEM mesh.
+   */
+  inline CVolumeElementFEM* GetVolElem(void) { return volElem.data(); }
 
   /*!
-  * \brief Function, which makes available the number of owned volume elements per time level.
-  * \return  The pointer to the data of nVolElemOwnedPerTimeLevel.
-  */
-  inline unsigned long* GetNVolElemOwnedPerTimeLevel(void) {return nVolElemOwnedPerTimeLevel.data();}
+   * \brief Function, which makes available the number of owned volume elements per time level.
+   * \return  The pointer to the data of nVolElemOwnedPerTimeLevel.
+   */
+  inline unsigned long* GetNVolElemOwnedPerTimeLevel(void) { return nVolElemOwnedPerTimeLevel.data(); }
 
   /*!
-  * \brief Function, which makes available the number of internal volume elements per time level.
-  * \return  The pointer to the data of nVolElemInternalPerTimeLevel.
-  */
-  inline unsigned long* GetNVolElemInternalPerTimeLevel(void) {return nVolElemInternalPerTimeLevel.data();}
+   * \brief Function, which makes available the number of internal volume elements per time level.
+   * \return  The pointer to the data of nVolElemInternalPerTimeLevel.
+   */
+  inline unsigned long* GetNVolElemInternalPerTimeLevel(void) { return nVolElemInternalPerTimeLevel.data(); }
 
   /*!
-  * \brief Function, which makes available the number of halo volume elements per time level.
-  * \return  The pointer to the data of nVolElemHaloPerTimeLevel.
-  */
-  inline unsigned long* GetNVolElemHaloPerTimeLevel(void) {return nVolElemHaloPerTimeLevel.data();}
+   * \brief Function, which makes available the number of halo volume elements per time level.
+   * \return  The pointer to the data of nVolElemHaloPerTimeLevel.
+   */
+  inline unsigned long* GetNVolElemHaloPerTimeLevel(void) { return nVolElemHaloPerTimeLevel.data(); }
 
   /*!
   * \brief Function, which makes available the vector of vectors containing the owned element
            IDs adjacent to elements of a lower time level. Note that a copy is made.
   * \return  Copy of ownedElemAdjLowTimeLevel.
   */
-  inline vector<vector<unsigned long> > GetOwnedElemAdjLowTimeLevel(void) {return ownedElemAdjLowTimeLevel;}
+  inline vector<vector<unsigned long> > GetOwnedElemAdjLowTimeLevel(void) { return ownedElemAdjLowTimeLevel; }
 
   /*!
   * \brief Function, which makes available the vector of vectors containing the halo element
            IDs adjacent to elements of a lower time level. Note that a copy is made.
   * \return  Copy of haloElemAdjLowTimeLevel.
   */
-  inline vector<vector<unsigned long> > GetHaloElemAdjLowTimeLevel(void) {return haloElemAdjLowTimeLevel;}
+  inline vector<vector<unsigned long> > GetHaloElemAdjLowTimeLevel(void) { return haloElemAdjLowTimeLevel; }
 
   /*!
-  * \brief Function, which makes available the number of standard boundary faces of the solution.
-  * \return  Number of standard boundary faces of the solution.
-  */
-  inline unsigned short GetNStandardBoundaryFacesSol(void) {return standardBoundaryFacesSol.size();}
+   * \brief Function, which makes available the number of standard boundary faces of the solution.
+   * \return  Number of standard boundary faces of the solution.
+   */
+  inline unsigned short GetNStandardBoundaryFacesSol(void) { return standardBoundaryFacesSol.size(); }
 
   /*!
-  * \brief Function, which makes available the standard boundary faces of the solution.
-  * \return  Pointer to the standard boundary faces of the solution.
-  */
-  inline CFEMStandardBoundaryFace* GetStandardBoundaryFacesSol(void) {return standardBoundaryFacesSol.data();}
+   * \brief Function, which makes available the standard boundary faces of the solution.
+   * \return  Pointer to the standard boundary faces of the solution.
+   */
+  inline CFEMStandardBoundaryFace* GetStandardBoundaryFacesSol(void) { return standardBoundaryFacesSol.data(); }
 
   /*!
   * \brief Function, which makes available the vector of receive ranks as
            a const reference.
   * \return  Const reference to the vector of ranks.
   */
-  inline const vector<int>& GetRanksRecv(void) const {return ranksRecv;}
+  inline const vector<int>& GetRanksRecv(void) const { return ranksRecv; }
 
   /*!
   * \brief Function, which makes available the vector of send ranks as
            a const reference.
   * \return  Const reference to the vector of ranks.
   */
-  inline const vector<int>& GetRanksSend(void) const {return ranksSend;}
+  inline const vector<int>& GetRanksSend(void) const { return ranksSend; }
 
   /*!
   * \brief Function, which makes available the vector of vectors containing the receive
            entities as a const reference.
   * \return  Const reference to the vector of vectors of receive entities.
   */
-  inline const vector<vector<unsigned long> >& GetEntitiesRecv(void) const {return entitiesRecv;}
+  inline const vector<vector<unsigned long> >& GetEntitiesRecv(void) const { return entitiesRecv; }
 
   /*!
   * \brief Function, which makes available the vector of vectors containing the send
            entities as a const reference.
   * \return  Const reference to the vector of vectors of send entities.
   */
-  inline const vector<vector<unsigned long> >& GetEntitiesSend(void) const {return entitiesSend;}
+  inline const vector<vector<unsigned long> >& GetEntitiesSend(void) const { return entitiesSend; }
 
   /*!
   * \brief Function, which makes available the vector of rotational periodic markers
            as a const reference.
   * \return  Const reference to the vector with rotational periodic markers.
   */
-  inline const vector<unsigned short>& GetRotPerMarkers(void) const {return rotPerMarkers;}
+  inline const vector<unsigned short>& GetRotPerMarkers(void) const { return rotPerMarkers; }
 
   /*!
   * \brief Function, which makes available the vector of vectors containing the rotational
            periodic halos as a const reference.
   * \return  Const reference to the vector of vectors with rotational periodic halos.
   */
-  inline const vector<vector<unsigned long> >& GetRotPerHalos(void) const {return rotPerHalos;}
+  inline const vector<vector<unsigned long> >& GetRotPerHalos(void) const { return rotPerHalos; }
 
   /*!
-  * \brief Compute surface area (positive z-direction) for force coefficient non-dimensionalization.
-  * \param[in] config - Definition of the particular problem.
-  */
-  void SetPositive_ZArea(CConfig *config) override;
+   * \brief Compute surface area (positive z-direction) for force coefficient non-dimensionalization.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void SetPositive_ZArea(CConfig* config) override;
 
-protected:
+ protected:
   /*!
   * \brief Function, which computes the gradients of the parametric coordinates
            w.r.t. the Cartesian coordinates in the integration points of a face,
@@ -653,12 +645,9 @@ class CMeshFEM: public CGeometry {
   * \param[out] derivCoor      - Storage for the derivatives of the coordinates.
   *  \param[in] config         - Definition of the particular problem.
   */
-  void ComputeGradientsCoordinatesFace(const unsigned short nIntegration,
-                                       const unsigned short nDOFs,
-                                       const su2double      *matDerBasisInt,
-                                       const unsigned long  *DOFs,
-                                       su2double            *derivCoor,
-                                       CConfig              *config);
+  void ComputeGradientsCoordinatesFace(const unsigned short nIntegration, const unsigned short nDOFs,
+                                       const su2double* matDerBasisInt, const unsigned long* DOFs, su2double* derivCoor,
+                                       CConfig* config);
   /*!
   * \brief Function, which computes the gradients of the Cartesian coordinates
            w.r.t. the parametric coordinates in the given set of integration
@@ -673,12 +662,9 @@ class CMeshFEM: public CGeometry {
   * \param[out] derivCoor    - Storage for the derivatives of the coordinates.
   * \param[in] config        - Definition of the particular problem.
   */
-  void ComputeGradientsCoorWRTParam(const unsigned short nIntegration,
-                                    const unsigned short nDOFs,
-                                    const su2double      *matDerBasisInt,
-                                    const unsigned long  *DOFs,
-                                    su2double            *derivCoor,
-                                    CConfig              *config);
+  void ComputeGradientsCoorWRTParam(const unsigned short nIntegration, const unsigned short nDOFs,
+                                    const su2double* matDerBasisInt, const unsigned long* DOFs, su2double* derivCoor,
+                                    CConfig* config);
   /*!
   * \brief Function, which computes the information of the normals in the
            integration points of a face.
@@ -690,12 +676,8 @@ class CMeshFEM: public CGeometry {
   * \param[in]  DOFs         - The DOFs of the grid associated with the face.
   * \param[out] normals      - Storage for the normal information to be computed.
   */
-  void ComputeNormalsFace(const unsigned short nIntegration,
-                          const unsigned short nDOFs,
-                          const su2double      *dr,
-                          const su2double      *ds,
-                          const unsigned long  *DOFs,
-                          su2double            *normals);
+  void ComputeNormalsFace(const unsigned short nIntegration, const unsigned short nDOFs, const su2double* dr,
+                          const su2double* ds, const unsigned long* DOFs, su2double* normals);
 
   /*!
   * \brief Function, which computes the metric terms of the faces of a
@@ -704,8 +686,7 @@ class CMeshFEM: public CGeometry {
                              terms must be computed.
   * \param[in]    config   - Definition of the particular problem.
   */
-  void MetricTermsBoundaryFaces(CBoundaryFEM *boundary,
-                                CConfig      *config);
+  void MetricTermsBoundaryFaces(CBoundaryFEM* boundary, CConfig* config);
 };
 
 /*!
@@ -714,8 +695,8 @@ class CMeshFEM: public CGeometry {
  * \author E. van der Weide
  * \version 7.5.1 "Blackbird"
  */
-class CMeshFEM_DG: public CMeshFEM {
-protected:
+class CMeshFEM_DG : public CMeshFEM {
+ protected:
   vector<CFEMStandardElement> standardElementsSol;  /*!< \brief Vector that contains the standard volume elements
                                                                 used for the solution of the DG solver. */
   vector<CFEMStandardElement> standardElementsGrid; /*!< \brief Vector that contains the standard volume elements
@@ -728,159 +709,160 @@ class CMeshFEM_DG: public CMeshFEM {
                                                                           internal faces used for the geometry of
                                                                           the DG solver. */
 
-  vector<su2double> timeCoefADER_DG;                        /*!< \brief The time coefficients in the iteration matrix of
-                                                                        the ADER-DG predictor step. */
-  vector<su2double> timeInterpolDOFToIntegrationADER_DG;    /*!< \brief The interpolation matrix between the time DOFs and
-                                                                        the time integration points for ADER-DG. */
-  vector<su2double> timeInterpolAdjDOFToIntegrationADER_DG; /*!< \brief The interpolation matrix between the time DOFs of adjacent
-                                                                        elements of a higher time level and the time integration
-                                                                        points for ADER-DG. */
+  vector<su2double> timeCoefADER_DG;                     /*!< \brief The time coefficients in the iteration matrix of
+                                                                     the ADER-DG predictor step. */
+  vector<su2double> timeInterpolDOFToIntegrationADER_DG; /*!< \brief The interpolation matrix between the time DOFs and
+                                                                     the time integration points for ADER-DG. */
+  vector<su2double> timeInterpolAdjDOFToIntegrationADER_DG; /*!< \brief The interpolation matrix between the time DOFs
+                                                               of adjacent elements of a higher time level and the time
+                                                               integration points for ADER-DG. */
 
-  vector<unsigned long> nMatchingFacesInternal;          /*!< \brief Number of matching faces between between two owned elements
-                                                                     per time level. Cumulative storage format. */
-  vector<unsigned long> nMatchingFacesWithHaloElem;      /*!< \brief Number of matching faces between an owned element and a halo
-                                                                     element per time level. Cumulative storage format. */
-  vector<CInternalFaceElementFEM> matchingFaces; /*!< \brief Vector of the local matching internal faces. */
+  vector<unsigned long> nMatchingFacesInternal; /*!< \brief Number of matching faces between between two owned elements
+                                                            per time level. Cumulative storage format. */
+  vector<unsigned long> nMatchingFacesWithHaloElem; /*!< \brief Number of matching faces between an owned element and a
+                                                       halo element per time level. Cumulative storage format. */
+  vector<CInternalFaceElementFEM> matchingFaces;    /*!< \brief Vector of the local matching internal faces. */
 
   map<unsigned long, unsigned long> Global_to_Local_Point; /*!< \brief Global-local mapping for the DOFs. */
 
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    */
   CMeshFEM_DG(void) : CMeshFEM() {}
 
   /*!
-  * \overload
-  * \brief Redistributes the grid over the ranks and creates the halo layer.
-  * \param[in] geometry - The linear distributed grid that must be redistributed.
-  * \param[in] config   - Definition of the particular problem.
-  */
-  CMeshFEM_DG(CGeometry *geometry, CConfig *config);
+   * \overload
+   * \brief Redistributes the grid over the ranks and creates the halo layer.
+   * \param[in] geometry - The linear distributed grid that must be redistributed.
+   * \param[in] config   - Definition of the particular problem.
+   */
+  CMeshFEM_DG(CGeometry* geometry, CConfig* config);
 
- /*!
-  * \brief Function to compute the coordinates of the integration points.
-  */
+  /*!
+   * \brief Function to compute the coordinates of the integration points.
+   */
   void CoordinatesIntegrationPoints(void);
 
- /*!
-  * \brief Function to compute the coordinates of solution DOFs.
-  */
+  /*!
+   * \brief Function to compute the coordinates of solution DOFs.
+   */
   void CoordinatesSolDOFs(void);
 
- /*!
-  * \brief Function to create the faces used in the DG formulation.
-  * \param[in] config - Definition of the particular problem.
-  */
-  void CreateFaces(CConfig *config);
+  /*!
+   * \brief Function to create the faces used in the DG formulation.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void CreateFaces(CConfig* config);
 
- /*!
-  * \brief Function to create the standard volume elements.
-  * \param[in] config - Definition of the particular problem.
-  */
-  void CreateStandardVolumeElements(CConfig *config);
+  /*!
+   * \brief Function to create the standard volume elements.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void CreateStandardVolumeElements(CConfig* config);
 
- /*!
-  * \brief Function, which makes available the time coefficients in the
-           iteration matrix of the ADER-DG predictor step.
-  * \return  The time coefficients in the iteration matrix of ADER-DG.
-  */
-  inline su2double* GetTimeCoefADER_DG(void) {return timeCoefADER_DG.data();}
+  /*!
+   * \brief Function, which makes available the time coefficients in the
+            iteration matrix of the ADER-DG predictor step.
+   * \return  The time coefficients in the iteration matrix of ADER-DG.
+   */
+  inline su2double* GetTimeCoefADER_DG(void) { return timeCoefADER_DG.data(); }
 
- /*!
-  * \brief Function, which makes available the time interpolation matrix between
-           the time DOFs and time integration points for ADER-DG.
-  * \return  The time interpolation matrix for ADER-DG.
-  */
-  inline su2double* GetTimeInterpolDOFToIntegrationADER_DG(void) {return timeInterpolDOFToIntegrationADER_DG.data();}
+  /*!
+   * \brief Function, which makes available the time interpolation matrix between
+            the time DOFs and time integration points for ADER-DG.
+   * \return  The time interpolation matrix for ADER-DG.
+   */
+  inline su2double* GetTimeInterpolDOFToIntegrationADER_DG(void) { return timeInterpolDOFToIntegrationADER_DG.data(); }
 
- /*!
-  * \brief Function, which makes available the time interpolation matrix between
-           the adjacent time DOFs of the next time level and the time
-           integration points for ADER-DG.
-  * \return  The time interpolation matrix of adjacent time DOFs for ADER-DG.
-  */
-  inline su2double* GetTimeInterpolAdjDOFToIntegrationADER_DG(void) {return timeInterpolAdjDOFToIntegrationADER_DG.data();}
+  /*!
+   * \brief Function, which makes available the time interpolation matrix between
+            the adjacent time DOFs of the next time level and the time
+            integration points for ADER-DG.
+   * \return  The time interpolation matrix of adjacent time DOFs for ADER-DG.
+   */
+  inline su2double* GetTimeInterpolAdjDOFToIntegrationADER_DG(void) {
+    return timeInterpolAdjDOFToIntegrationADER_DG.data();
+  }
 
- /*!
-  * \brief Function, which makes available the number of matching internal faces
-           between an owned element and a halo element per time level.
-  * \return  The number of matching internal faces between these elements per time level.
-  */
-  inline unsigned long *GetNMatchingFacesWithHaloElem(void) {return nMatchingFacesWithHaloElem.data();}
+  /*!
+   * \brief Function, which makes available the number of matching internal faces
+            between an owned element and a halo element per time level.
+   * \return  The number of matching internal faces between these elements per time level.
+   */
+  inline unsigned long* GetNMatchingFacesWithHaloElem(void) { return nMatchingFacesWithHaloElem.data(); }
 
- /*!
-  * \brief Function, which makes available the number of matching internal faces
-           between two owned elements per time level.
-  * \return  The number of matching internal faces per time level.
-  */
-  inline unsigned long *GetNMatchingFacesInternal(void) {return nMatchingFacesInternal.data();}
+  /*!
+   * \brief Function, which makes available the number of matching internal faces
+            between two owned elements per time level.
+   * \return  The number of matching internal faces per time level.
+   */
+  inline unsigned long* GetNMatchingFacesInternal(void) { return nMatchingFacesInternal.data(); }
 
- /*!
-  * \brief Function, which makes available the matching internal faces.
-  * \return  Pointer to the matching internal faces.
-  */
-  inline CInternalFaceElementFEM* GetMatchingFaces(void) {return matchingFaces.data();}
+  /*!
+   * \brief Function, which makes available the matching internal faces.
+   * \return  Pointer to the matching internal faces.
+   */
+  inline CInternalFaceElementFEM* GetMatchingFaces(void) { return matchingFaces.data(); }
 
- /*!
-  * \brief Function to compute the grid velocities for static problems.
-  * \param[in] config             - Definition of the particular problem.
-  * \param[in] Kind_Grid_Movement - The type of prescribed grid motion.
-  * \param[in] iZone              - The currently active zone number.
-  */
-  void InitStaticMeshMovement(const CConfig        *config,
-                              const unsigned short Kind_Grid_Movement,
+  /*!
+   * \brief Function to compute the grid velocities for static problems.
+   * \param[in] config             - Definition of the particular problem.
+   * \param[in] Kind_Grid_Movement - The type of prescribed grid motion.
+   * \param[in] iZone              - The currently active zone number.
+   */
+  void InitStaticMeshMovement(const CConfig* config, const unsigned short Kind_Grid_Movement,
                               const unsigned short iZone);
 
- /*!
-  * \brief Function, which makes available the number of standard volume elements of the solution.
-  * \return  Number of standard volume elements of the solution.
-  */
-  inline unsigned short GetNStandardElementsSol(void) {return standardElementsSol.size();}
+  /*!
+   * \brief Function, which makes available the number of standard volume elements of the solution.
+   * \return  Number of standard volume elements of the solution.
+   */
+  inline unsigned short GetNStandardElementsSol(void) { return standardElementsSol.size(); }
 
- /*!
-  * \brief Function, which makes available the standard volume elements of the solution.
-  * \return  Pointer to the standard volume elements of the solution.
-  */
-  inline CFEMStandardElement* GetStandardElementsSol(void) {return standardElementsSol.data();}
+  /*!
+   * \brief Function, which makes available the standard volume elements of the solution.
+   * \return  Pointer to the standard volume elements of the solution.
+   */
+  inline CFEMStandardElement* GetStandardElementsSol(void) { return standardElementsSol.data(); }
 
- /*!
-  * \brief Function, which makes available the number of standard internal matching faces of the solution.
-  * \return  Number of standard internal matching faces of the solution.
-  */
-  inline unsigned short GetNStandardMatchingFacesSol(void) {return standardMatchingFacesSol.size();}
+  /*!
+   * \brief Function, which makes available the number of standard internal matching faces of the solution.
+   * \return  Number of standard internal matching faces of the solution.
+   */
+  inline unsigned short GetNStandardMatchingFacesSol(void) { return standardMatchingFacesSol.size(); }
 
- /*!
-  * \brief Function, which makes available the standard internal matching faces of the solution.
-  * \return  Pointer to the standard internal matching faces of the solution.
-  */
-  inline CFEMStandardInternalFace* GetStandardMatchingFacesSol(void) {return standardMatchingFacesSol.data();}
+  /*!
+   * \brief Function, which makes available the standard internal matching faces of the solution.
+   * \return  Pointer to the standard internal matching faces of the solution.
+   */
+  inline CFEMStandardInternalFace* GetStandardMatchingFacesSol(void) { return standardMatchingFacesSol.data(); }
 
- /*!
-  * \brief Function, which computes a length scale of the volume elements.
-  * \param[in] config - Definition of the particular problem.
-  */
+  /*!
+   * \brief Function, which computes a length scale of the volume elements.
+   * \param[in] config - Definition of the particular problem.
+   */
   void LengthScaleVolumeElements(void);
 
- /*!
-  * \brief Function, which computes the metric terms of the surface
-           elements, both internal faces and physical boundary faces.
-  * \param[in] config - Definition of the particular problem.
-  */
-  void MetricTermsSurfaceElements(CConfig *config);
+  /*!
+   * \brief Function, which computes the metric terms of the surface
+            elements, both internal faces and physical boundary faces.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void MetricTermsSurfaceElements(CConfig* config);
 
- /*!
-  * \brief Function, which computes the metric terms of the
-           volume elements.
-  * \param[in] config - Definition of the particular problem.
-  */
-  void MetricTermsVolumeElements(CConfig *config);
+  /*!
+   * \brief Function, which computes the metric terms of the
+            volume elements.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void MetricTermsVolumeElements(CConfig* config);
 
- /*!
-  * \brief Set the send receive boundaries of the grid.
-  * \param[in] config - Definition of the particular problem.
-  */
-  void SetSendReceive(const CConfig *config) override;
+  /*!
+   * \brief Set the send receive boundaries of the grid.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void SetSendReceive(const CConfig* config) override;
 
   /*!
    * \brief Set the local index that correspond with the global numbering index.
@@ -894,8 +876,7 @@ class CMeshFEM_DG: public CMeshFEM {
    */
   inline long GetGlobal_to_Local_Point(unsigned long val_ipoint) const override {
     auto it = Global_to_Local_Point.find(val_ipoint);
-    if (it != Global_to_Local_Point.cend())
-      return it->second;
+    if (it != Global_to_Local_Point.cend()) return it->second;
     return -1;
   }
 
@@ -903,44 +884,39 @@ class CMeshFEM_DG: public CMeshFEM {
    * \brief Function, which carries out the preprocessing tasks when wall functions are used.
    * \param[in] config - Definition of the particular problem.
    */
-  void WallFunctionPreprocessing(CConfig *config);
+  void WallFunctionPreprocessing(CConfig* config);
 
-protected:
- /*!
-  * \brief Function, which computes the correct sequence of the connectivities
-           of a face, such that it matches the sequence of the given corner points.
-  * \param[in]  VTK_TypeFace       - Type of the face using the VTK convention.
-  * \param[in]  cornerPointsFace   - The corner points of the face in the desired
-                                     sequence.
-  * \param[in]  VTK_TypeElem       - Type of the element using the VTK convention.
-  * \param[in]  nPolyGrid          - Polynomial degree used in the grid definition
-                                     for the face and the element.
-  * \param[in]  elemNodeIDsGrid    - The node IDs of the grid DOFs of the element,
-                                     i.e. the element connectivity.
-  * \param[in]  nPolyConn          - Polynomial degree of the connectivities to
-                                     be modified.
-  * \param[in]  connElem           - Connectivity of the adjacent volume element.
-  * \param[out] swapFaceInElement  - Whether or not the connectivity of the face must
-                                     be swapped compared to the face of the corresponding
-                                     standard element. Only relevant for triangular faces
-                                     of a pyramid and quadrilateral faces of a prism.
-                                     corresponds to the top point of the adjacent pyramid.
-  * \param[out] modConnFace        - Connectivity of the face after the renumbering.
-  * \param[out] modConnElem        - Connectivity of the element after the renumbering.
-                                     This renumbering is such that the face corresponds
-                                     to the appropriate face of the element used in the
-                                     standard faces and also the corner points match.
-  */
-  void CreateConnectivitiesFace(const unsigned short        VTK_TypeFace,
-                                const unsigned long         *cornerPointsFace,
-                                const unsigned short        VTK_TypeElem,
-                                const unsigned short        nPolyGrid,
-                                const vector<unsigned long> &elemNodeIDsGrid,
-                                const unsigned short        nPolyConn,
-                                const unsigned long         *connElem,
-                                bool                        &swapFaceInElement,
-                                unsigned long               *modConnFace,
-                                unsigned long               *modConnElem);
+ protected:
+  /*!
+   * \brief Function, which computes the correct sequence of the connectivities
+            of a face, such that it matches the sequence of the given corner points.
+   * \param[in]  VTK_TypeFace       - Type of the face using the VTK convention.
+   * \param[in]  cornerPointsFace   - The corner points of the face in the desired
+                                      sequence.
+   * \param[in]  VTK_TypeElem       - Type of the element using the VTK convention.
+   * \param[in]  nPolyGrid          - Polynomial degree used in the grid definition
+                                      for the face and the element.
+   * \param[in]  elemNodeIDsGrid    - The node IDs of the grid DOFs of the element,
+                                      i.e. the element connectivity.
+   * \param[in]  nPolyConn          - Polynomial degree of the connectivities to
+                                      be modified.
+   * \param[in]  connElem           - Connectivity of the adjacent volume element.
+   * \param[out] swapFaceInElement  - Whether or not the connectivity of the face must
+                                      be swapped compared to the face of the corresponding
+                                      standard element. Only relevant for triangular faces
+                                      of a pyramid and quadrilateral faces of a prism.
+                                      corresponds to the top point of the adjacent pyramid.
+   * \param[out] modConnFace        - Connectivity of the face after the renumbering.
+   * \param[out] modConnElem        - Connectivity of the element after the renumbering.
+                                      This renumbering is such that the face corresponds
+                                      to the appropriate face of the element used in the
+                                      standard faces and also the corner points match.
+   */
+  void CreateConnectivitiesFace(const unsigned short VTK_TypeFace, const unsigned long* cornerPointsFace,
+                                const unsigned short VTK_TypeElem, const unsigned short nPolyGrid,
+                                const vector<unsigned long>& elemNodeIDsGrid, const unsigned short nPolyConn,
+                                const unsigned long* connElem, bool& swapFaceInElement, unsigned long* modConnFace,
+                                unsigned long* modConnElem);
 
   /*!
   * \brief Function, which computes the correct sequence of the connectivities
@@ -960,14 +936,11 @@ class CMeshFEM_DG: public CMeshFEM {
                                    renumbering. This renumbering is such that the
                                    line corresponds to face 0 of the quadrilateral.
   */
-  void CreateConnectivitiesLineAdjacentQuadrilateral(
-                                  const unsigned long         *cornerPointsLine,
-                                  const unsigned short        nPolyGrid,
-                                  const vector<unsigned long> &quadNodeIDsGrid,
-                                  const unsigned short        nPolyConn,
-                                  const unsigned long         *connQuad,
-                                  unsigned long               *modConnLine,
-                                  unsigned long               *modConnQuad);
+  void CreateConnectivitiesLineAdjacentQuadrilateral(const unsigned long* cornerPointsLine,
+                                                     const unsigned short nPolyGrid,
+                                                     const vector<unsigned long>& quadNodeIDsGrid,
+                                                     const unsigned short nPolyConn, const unsigned long* connQuad,
+                                                     unsigned long* modConnLine, unsigned long* modConnQuad);
 
   /*!
   * \brief Function, which computes the correct sequence of the connectivities
@@ -987,14 +960,10 @@ class CMeshFEM_DG: public CMeshFEM {
                                    renumbering. This renumbering is such that the
                                    line corresponds to face 0 of the triangle.
   */
-  void CreateConnectivitiesLineAdjacentTriangle(
-                                  const unsigned long         *cornerPointsLine,
-                                  const unsigned short        nPolyGrid,
-                                  const vector<unsigned long> &triaNodeIDsGrid,
-                                  const unsigned short        nPolyConn,
-                                  const unsigned long         *connTria,
-                                  unsigned long               *modConnLine,
-                                  unsigned long               *modConnTria);
+  void CreateConnectivitiesLineAdjacentTriangle(const unsigned long* cornerPointsLine, const unsigned short nPolyGrid,
+                                                const vector<unsigned long>& triaNodeIDsGrid,
+                                                const unsigned short nPolyConn, const unsigned long* connTria,
+                                                unsigned long* modConnLine, unsigned long* modConnTria);
 
   /*!
   * \brief Function, which computes the correct sequence of the connectivities
@@ -1014,14 +983,12 @@ class CMeshFEM_DG: public CMeshFEM {
                                    renumbering. This renumbering is such that the
                                    quad corresponds to face 0 of the hexahedron.
   */
-  void CreateConnectivitiesQuadrilateralAdjacentHexahedron(
-                                  const unsigned long         *cornerPointsQuad,
-                                  const unsigned short        nPolyGrid,
-                                  const vector<unsigned long> &hexaNodeIDsGrid,
-                                  const unsigned short        nPolyConn,
-                                  const unsigned long         *connHexa,
-                                  unsigned long               *modConnQuad,
-                                  unsigned long               *modConnHexa);
+  void CreateConnectivitiesQuadrilateralAdjacentHexahedron(const unsigned long* cornerPointsQuad,
+                                                           const unsigned short nPolyGrid,
+                                                           const vector<unsigned long>& hexaNodeIDsGrid,
+                                                           const unsigned short nPolyConn,
+                                                           const unsigned long* connHexa, unsigned long* modConnQuad,
+                                                           unsigned long* modConnHexa);
 
   /*!
   * \brief Function, which computes the correct sequence of the connectivities
@@ -1044,15 +1011,12 @@ class CMeshFEM_DG: public CMeshFEM {
                                     renumbering. This renumbering is such that the
                                     quad corresponds to face 3 of the prism.
   */
-  void CreateConnectivitiesQuadrilateralAdjacentPrism(
-                                  const unsigned long         *cornerPointsQuad,
-                                  const unsigned short        nPolyGrid,
-                                  const vector<unsigned long> &prismNodeIDsGrid,
-                                  const unsigned short        nPolyConn,
-                                  const unsigned long         *connPrism,
-                                  bool                        &swapFaceInElement,
-                                  unsigned long               *modConnQuad,
-                                  unsigned long               *modConnPrism);
+  void CreateConnectivitiesQuadrilateralAdjacentPrism(const unsigned long* cornerPointsQuad,
+                                                      const unsigned short nPolyGrid,
+                                                      const vector<unsigned long>& prismNodeIDsGrid,
+                                                      const unsigned short nPolyConn, const unsigned long* connPrism,
+                                                      bool& swapFaceInElement, unsigned long* modConnQuad,
+                                                      unsigned long* modConnPrism);
 
   /*!
   * \brief Function, which computes the correct sequence of the connectivities
@@ -1072,14 +1036,11 @@ class CMeshFEM_DG: public CMeshFEM {
                                    renumbering. This renumbering is such that the
                                    quad corresponds to face 0 of the pyramid.
   */
-  void CreateConnectivitiesQuadrilateralAdjacentPyramid(
-                                  const unsigned long         *cornerPointsQuad,
-                                  const unsigned short        nPolyGrid,
-                                  const vector<unsigned long> &pyraNodeIDsGrid,
-                                  const unsigned short        nPolyConn,
-                                  const unsigned long         *connPyra,
-                                  unsigned long               *modConnQuad,
-                                  unsigned long               *modConnPyra);
+  void CreateConnectivitiesQuadrilateralAdjacentPyramid(const unsigned long* cornerPointsQuad,
+                                                        const unsigned short nPolyGrid,
+                                                        const vector<unsigned long>& pyraNodeIDsGrid,
+                                                        const unsigned short nPolyConn, const unsigned long* connPyra,
+                                                        unsigned long* modConnQuad, unsigned long* modConnPyra);
 
   /*!
   * \brief Function, which computes the correct sequence of the connectivities
@@ -1099,14 +1060,10 @@ class CMeshFEM_DG: public CMeshFEM {
                                    renumbering. This renumbering is such that the
                                    triangle corresponds to face 0 of the prism.
   */
-  void CreateConnectivitiesTriangleAdjacentPrism(
-                                  const unsigned long         *cornerPointsTria,
-                                  const unsigned short        nPolyGrid,
-                                  const vector<unsigned long> &prismNodeIDsGrid,
-                                  const unsigned short        nPolyConn,
-                                  const unsigned long         *connPrism,
-                                  unsigned long               *modConnTria,
-                                  unsigned long               *modConnPrism);
+  void CreateConnectivitiesTriangleAdjacentPrism(const unsigned long* cornerPointsTria, const unsigned short nPolyGrid,
+                                                 const vector<unsigned long>& prismNodeIDsGrid,
+                                                 const unsigned short nPolyConn, const unsigned long* connPrism,
+                                                 unsigned long* modConnTria, unsigned long* modConnPrism);
 
   /*!
   * \brief Function, which computes the correct sequence of the connectivities
@@ -1129,15 +1086,12 @@ class CMeshFEM_DG: public CMeshFEM {
                                      renumbering. This renumbering is such that the
                                      triangle corresponds to face 3 of the pyramid.
   */
-  void CreateConnectivitiesTriangleAdjacentPyramid(
-                                  const unsigned long         *cornerPointsTria,
-                                  const unsigned short        nPolyGrid,
-                                  const vector<unsigned long> &pyraNodeIDsGrid,
-                                  const unsigned short        nPolyConn,
-                                  const unsigned long         *connPyra,
-                                  bool                        &swapFaceInElement,
-                                  unsigned long               *modConnTria,
-                                  unsigned long               *modConnPyra);
+  void CreateConnectivitiesTriangleAdjacentPyramid(const unsigned long* cornerPointsTria,
+                                                   const unsigned short nPolyGrid,
+                                                   const vector<unsigned long>& pyraNodeIDsGrid,
+                                                   const unsigned short nPolyConn, const unsigned long* connPyra,
+                                                   bool& swapFaceInElement, unsigned long* modConnTria,
+                                                   unsigned long* modConnPyra);
 
   /*!
   * \brief Function, which computes the correct sequence of the connectivities
@@ -1157,48 +1111,42 @@ class CMeshFEM_DG: public CMeshFEM {
                                    renumbering. This renumbering is such that the
                                    triangle corresponds to face 0 of the tetrahedron.
   */
-  void CreateConnectivitiesTriangleAdjacentTetrahedron(
-                                  const unsigned long         *cornerPointsTria,
-                                  const unsigned short        nPolyGrid,
-                                  const vector<unsigned long> &tetNodeIDsGrid,
-                                  const unsigned short        nPolyConn,
-                                  const unsigned long         *connTet,
-                                  unsigned long               *modConnTria,
-                                  unsigned long               *modConnTet);
-
- /*!
-  * \brief Function, which computes the parametric coordinates of the given
-           Cartesian coordinates inside the given parent element.
-  * \param[in]  coor           - Cartesian coordinates for which the parametric
-                                 coordinates must be determined.
-  * \param[in]  parElem        - The high order parent element which contains
-                                 the point.
-  * \param[in]  subElem        - Low order sub element inside the parent element
-                                 which contains the point.
-  * \param[in]  weightsSubElem - Interpolation weights inside subElem for the
-                                 coordinates. Used for an initial guess.
-  * \param[out] parCoor        - Parametric coordinates inside the high order
-                                 parent element for the given coordinates.
-                                 These parametric coordinates must be computed.
-  */
-  void HighOrderContainmentSearch(const su2double      *coor,
-                                  const unsigned long  parElem,
-                                  const unsigned short subElem,
-                                  const su2double      *weightsSubElem,
-                                  su2double            *parCoor);
+  void CreateConnectivitiesTriangleAdjacentTetrahedron(const unsigned long* cornerPointsTria,
+                                                       const unsigned short nPolyGrid,
+                                                       const vector<unsigned long>& tetNodeIDsGrid,
+                                                       const unsigned short nPolyConn, const unsigned long* connTet,
+                                                       unsigned long* modConnTria, unsigned long* modConnTet);
+
+  /*!
+   * \brief Function, which computes the parametric coordinates of the given
+            Cartesian coordinates inside the given parent element.
+   * \param[in]  coor           - Cartesian coordinates for which the parametric
+                                  coordinates must be determined.
+   * \param[in]  parElem        - The high order parent element which contains
+                                  the point.
+   * \param[in]  subElem        - Low order sub element inside the parent element
+                                  which contains the point.
+   * \param[in]  weightsSubElem - Interpolation weights inside subElem for the
+                                  coordinates. Used for an initial guess.
+   * \param[out] parCoor        - Parametric coordinates inside the high order
+                                  parent element for the given coordinates.
+                                  These parametric coordinates must be computed.
+   */
+  void HighOrderContainmentSearch(const su2double* coor, const unsigned long parElem, const unsigned short subElem,
+                                  const su2double* weightsSubElem, su2double* parCoor);
 
   /*!
   * \brief Function, which computes the metric terms for internal
            matching faces.
   * \param[in] config - Definition of the particular problem.
   */
-  void MetricTermsMatchingFaces(CConfig *config);
+  void MetricTermsMatchingFaces(CConfig* config);
 
   /*!
-  * \brief Function, which computes the time coefficients for the ADER-DG predictor step.
-  * \param[in] config - Definition of the particular problem.
-  */
-  void TimeCoefficientsPredictorADER_DG(CConfig *config);
+   * \brief Function, which computes the time coefficients for the ADER-DG predictor step.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void TimeCoefficientsPredictorADER_DG(CConfig* config);
 
   /*!
   * \brief Function, which computes the volume metric terms for the given
@@ -1210,16 +1158,15 @@ class CMeshFEM_DG: public CMeshFEM {
                                terms must be computed.
   * \param[out] metricTerms  - Vector in which the metric terms must be stored.
   */
-  void VolumeMetricTermsFromCoorGradients(const unsigned short nEntities,
-                                          const su2double      *gradCoor,
-                                          vector<su2double>    &metricTerms);
+  void VolumeMetricTermsFromCoorGradients(const unsigned short nEntities, const su2double* gradCoor,
+                                          vector<su2double>& metricTerms);
 
   /*!
    * \brief Compute an ADT including the coordinates of all viscous markers
    * \param[in] config - Definition of the particular problem.
    * \return pointer to the ADT
    */
-  std::unique_ptr<CADTElemClass> ComputeViscousWallADT(const CConfig *config) const override;
+  std::unique_ptr<CADTElemClass> ComputeViscousWallADT(const CConfig* config) const override;
 
   /*!
    * \brief Set wall distances a specific value
@@ -1245,12 +1192,10 @@ class CMeshFEM_DG: public CMeshFEM {
  * \author T. Albring
  */
 class CDummyMeshFEM_DG : public CMeshFEM_DG {
-
-public:
+ public:
   /*!
    * \brief Constructor of the class
    * \param[in] config - Definition of the particular problem.
    */
-  CDummyMeshFEM_DG(CConfig *config);
-
+  CDummyMeshFEM_DG(CConfig* config);
 };
diff --git a/Common/include/fem/fem_standard_element.hpp b/Common/include/fem/fem_standard_element.hpp
index 6d871b0bee0..63869d7fff7 100644
--- a/Common/include/fem/fem_standard_element.hpp
+++ b/Common/include/fem/fem_standard_element.hpp
@@ -43,30 +43,32 @@ using namespace std;
  * \version 7.5.1 "Blackbird"
  */
 class CFEMStandardElementBase {
-protected:
+ protected:
   unsigned short VTK_Type;     /*!< \brief Element type using the VTK convention. */
   unsigned short orderExact;   /*!< \brief Polynomial order that must be integrated exactly by the integration rule. */
   unsigned short nIntegration; /*!< \brief Number of points used in the numerical integration. */
 
-  bool constJacobian;          /*!< \brief Whether or not the element has a constant Jacobian. */
+  bool constJacobian; /*!< \brief Whether or not the element has a constant Jacobian. */
 
   vector<su2double> rIntegration; /*!< \brief r-location of the integration points for this standard element. */
-  vector<su2double> sIntegration; /*!< \brief s-location of the integration points for this standard element, if needed. */
-  vector<su2double> tIntegration; /*!< \brief t-location of the integration points for this standard element, if needed. */
+  vector<su2double>
+      sIntegration; /*!< \brief s-location of the integration points for this standard element, if needed. */
+  vector<su2double>
+      tIntegration; /*!< \brief t-location of the integration points for this standard element, if needed. */
   vector<su2double> wIntegration; /*!< \brief The weights of the integration points for this standard element. */
 
-public:
+ public:
   /*!
-  * \brief Constructor. Nothing to be done.
-  */
+   * \brief Constructor. Nothing to be done.
+   */
   CFEMStandardElementBase() = default;
 
   /*!
-  * \brief Destructor. Nothing to be done, because the vectors are deleted automatically.
-  */
+   * \brief Destructor. Nothing to be done, because the vectors are deleted automatically.
+   */
   virtual ~CFEMStandardElementBase() = default;
 
-protected:
+ protected:
   /*!
   * \brief Alternative constructor.
   * \param[in] val_VTK_Type   - Type of the element using the VTK convention.
@@ -78,24 +80,21 @@ class CFEMStandardElementBase {
                                 be determined from the polynomial degree and the
                                 parameters in config.
   */
-  CFEMStandardElementBase(unsigned short val_VTK_Type,
-                          unsigned short val_nPoly,
-                          bool           val_constJac,
-                          CConfig        *config,
+  CFEMStandardElementBase(unsigned short val_VTK_Type, unsigned short val_nPoly, bool val_constJac, CConfig* config,
                           unsigned short val_orderExact);
 
-public:
+ public:
   /*!
-  * \brief Function, which makes available the type of the element.
-  * \return  The type of the element using the VTK convention.
-  */
-  inline unsigned short GetVTK_Type(void) const {return VTK_Type;}
+   * \brief Function, which makes available the type of the element.
+   * \return  The type of the element using the VTK convention.
+   */
+  inline unsigned short GetVTK_Type(void) const { return VTK_Type; }
 
   /*!
-  * \brief Function, which makes available the weights in the integration points.
-  * \return  The const pointer to data, which stores the weights in the integration points.
-  */
-  inline const su2double* GetWeightsIntegration(void) const {return wIntegration.data();}
+   * \brief Function, which makes available the weights in the integration points.
+   * \return  The const pointer to data, which stores the weights in the integration points.
+   */
+  inline const su2double* GetWeightsIntegration(void) const { return wIntegration.data(); }
 
   /*!
   * \brief Static function, which makes available the number of DOFs for an element
@@ -105,51 +104,45 @@ class CFEMStandardElementBase {
   * \param[in] typeErrorMessage - Default argument used to write a good error message.
   * \return The number of DOFs
   */
-  static unsigned short GetNDOFsStatic(unsigned short VTK_Type,
-                                       unsigned short nPoly,
-                                       unsigned long  typeErrorMessage = 0);
+  static unsigned short GetNDOFsStatic(unsigned short VTK_Type, unsigned short nPoly,
+                                       unsigned long typeErrorMessage = 0);
 
   /*!
-  * \brief Function, which makes available the number of integration points for this standard element.
-  * \return  The number of integration points of this standard element.
-  */
-  inline unsigned short GetNIntegration(void) const {return nIntegration;}
+   * \brief Function, which makes available the number of integration points for this standard element.
+   * \return  The number of integration points of this standard element.
+   */
+  inline unsigned short GetNIntegration(void) const { return nIntegration; }
 
   /*!
-  * \brief Function, which makes available the polynomial order that must be integrated exactly.
-  * \return  The polynomial order that must be integrated exactly.
-  */
-  inline unsigned short GetOrderExact(void) const {return orderExact;}
+   * \brief Function, which makes available the polynomial order that must be integrated exactly.
+   * \return  The polynomial order that must be integrated exactly.
+   */
+  inline unsigned short GetOrderExact(void) const { return orderExact; }
 
   /*!
-  * \brief Static function, which computes the inverse of the given square matrix.
-  * \param[in]     n - Number of rows/columns of the square matrix A.
-  * \param[in,out] A - On input the square matrix to be inverted. On output the inverse.
-  */
-  static void InverseMatrix(unsigned short    n,
-                            vector<su2double> &A);
+   * \brief Static function, which computes the inverse of the given square matrix.
+   * \param[in]     n - Number of rows/columns of the square matrix A.
+   * \param[in,out] A - On input the square matrix to be inverted. On output the inverse.
+   */
+  static void InverseMatrix(unsigned short n, vector<su2double>& A);
 
   /*!
-  * \brief Function, which computes the gradient of the Vandermonde matrix for a standard 1D edge.
-  * \param[in]  nDOFs - Number of DOFs, which in 1D is the polynomial degree + 1.
-  * \param[in]  r     - Parametric coordinates for which the gradient of the Vandermonde matrix must be computed.
-  * \param[out] VDr   - Matrix to store the gradient of the Vandermonde matrix in all r-locations.
-  */
-  void GradVandermonde1D(unsigned short          nDOFs,
-                         const vector<su2double> &r,
-                         vector<su2double>       &VDr);
+   * \brief Function, which computes the gradient of the Vandermonde matrix for a standard 1D edge.
+   * \param[in]  nDOFs - Number of DOFs, which in 1D is the polynomial degree + 1.
+   * \param[in]  r     - Parametric coordinates for which the gradient of the Vandermonde matrix must be computed.
+   * \param[out] VDr   - Matrix to store the gradient of the Vandermonde matrix in all r-locations.
+   */
+  void GradVandermonde1D(unsigned short nDOFs, const vector<su2double>& r, vector<su2double>& VDr);
 
   /*!
-  * \brief Function, which computes the Vandermonde matrix for a standard 1D edge.
-  * \param[in]  nDOFs - Number of DOFs, which in 1D is the polynomial degree + 1.
-  * \param[in]  r     - Parametric coordinates for which the Vandermonde matrix must be computed.
-  * \param[out] V     - Matrix to store the Vandermonde matrix in all r-locations.
-  */
-  void Vandermonde1D(unsigned short          nDOFs,
-                     const vector<su2double> &r,
-                     vector<su2double>       &V);
+   * \brief Function, which computes the Vandermonde matrix for a standard 1D edge.
+   * \param[in]  nDOFs - Number of DOFs, which in 1D is the polynomial degree + 1.
+   * \param[in]  r     - Parametric coordinates for which the Vandermonde matrix must be computed.
+   * \param[out] V     - Matrix to store the Vandermonde matrix in all r-locations.
+   */
+  void Vandermonde1D(unsigned short nDOFs, const vector<su2double>& r, vector<su2double>& V);
 
-protected:
+ protected:
   /*!
   * \brief Function, which checks if the sum of the given derivatives of the
            Lagrangian interpolation functions is 0 in the points.
@@ -158,9 +151,8 @@ class CFEMStandardElementBase {
   * \param[in] dLagBasisPoints - Values of the derivatives of the Lagrangian
                                  interpolation functions in the given points.
   */
-  void CheckSumDerivativesLagrangianBasisFunctions(const unsigned short    nPoints,
-                                                   const unsigned short    nDOFs,
-                                                   const vector<su2double> &dLagBasisPoints);
+  void CheckSumDerivativesLagrangianBasisFunctions(const unsigned short nPoints, const unsigned short nDOFs,
+                                                   const vector<su2double>& dLagBasisPoints);
 
   /*!
   * \brief Function, which checks if the sum of the given Lagrangian interpolation
@@ -170,15 +162,14 @@ class CFEMStandardElementBase {
   * \param[in,out] lagBasisPoints - Values of the Lagrangian interpolation
                                     functions in the given points.
   */
-  void CheckSumLagrangianBasisFunctions(const unsigned short nPoints,
-                                        const unsigned short nDOFs,
-                                        vector<su2double>    &lagBasisPoints);
+  void CheckSumLagrangianBasisFunctions(const unsigned short nPoints, const unsigned short nDOFs,
+                                        vector<su2double>& lagBasisPoints);
 
   /*!
-  * \brief Function, which copies the data of the given object into the current object.
-  * \param[in] other - Object, whose data is copied.
-  */
-  void Copy(const CFEMStandardElementBase &other);
+   * \brief Function, which copies the data of the given object into the current object.
+   * \param[in] other - Object, whose data is copied.
+   */
+  void Copy(const CFEMStandardElementBase& other);
 
   /*!
   * \brief Function, which computes the values of the derivatives of the basis functions
@@ -196,125 +187,101 @@ class CFEMStandardElementBase {
   * \param[out] dtLagBasisIntegration - t-derivatives of the basis functions in the integration points
                                         of the face.
   */
-  void DerivativesBasisFunctionsAdjacentElement(unsigned short    VTK_TypeElem,
-                                                unsigned short    nPolyElem,
-                                                const bool        swapFaceInElement,
-                                                unsigned short    &nDOFsElem,
-                                                vector<su2double> &drLagBasisIntegration,
-                                                vector<su2double> &dsLagBasisIntegration,
-                                                vector<su2double> &dtLagBasisIntegration);
-
-  /*!
-  * \brief Function, which computes the gradients of the Vandermonde matrix for a standard triangle.
-  * \param[in]  nPoly - Polynomial degree of the triangle.
-  * \param[in]  nDOFs - Number of DOFs of the triangle.
-  * \param[in]  r     - Parametric coordinate in r-direction for which the gradient of the Vandermonde matrix must be computed.
-  * \param[in]  s     - Parametric coordinate in s-direction for which the gradient of the Vandermonde matrix must be computed.
-  * \param[out] VDr   - Matrix to store the gradient in r-direction of the Vandermonde matrix in all r- and s-locations.
-  * \param[out] VDs   - Matrix to store the gradient in s-direction of the Vandermonde matrix in all r- and s-locations.
-  */
-  void GradVandermonde2D_Triangle(unsigned short          nPoly,
-                                  unsigned short          nDOFs,
-                                  const vector<su2double> &r,
-                                  const vector<su2double> &s,
-                                  vector<su2double>       &VDr,
-                                  vector<su2double>       &VDs);
-
-  /*!
-  * \brief Function, which computes the gradients of the Vandermonde matrix for a standard quadrilateral.
-  * \param[in]  nPoly - Polynomial degree of the quadrilateral.
-  * \param[in]  nDOFs - Number of DOFs of the quadrilateral.
-  * \param[in]  r     - Parametric coordinate in r-direction for which the gradient of the Vandermonde matrix must be computed.
-  * \param[in]  s     - Parametric coordinate in s-direction for which the gradient of the Vandermonde matrix must be computed.
-  * \param[out] VDr   - Matrix to store the gradient in r-direction of the Vandermonde matrix in all r- and s-locations.
-  * \param[out] VDs   - Matrix to store the gradient in s-direction of the Vandermonde matrix in all r- and s-locations.
-  */
-  void GradVandermonde2D_Quadrilateral(unsigned short          nPoly,
-                                       unsigned short          nDOFs,
-                                       const vector<su2double> &r,
-                                       const vector<su2double> &s,
-                                       vector<su2double>       &VDr,
-                                       vector<su2double>       &VDs);
-
-  /*!
-  * \brief Function, which computes the gradients of the Vandermonde matrix for a standard tetrahedron.
-  * \param[in]  nPoly - Polynomial degree of the tetrahedron.
-  * \param[in]  nDOFs - Number of DOFs of the tetrahedron.
-  * \param[in]  r     - Parametric coordinate in r-direction for which the gradient of the Vandermonde matrix must be computed.
-  * \param[in]  s     - Parametric coordinate in s-direction for which the gradient of the Vandermonde matrix must be computed.
-  * \param[in]  t     - Parametric coordinate in t-direction for which the gradient of the Vandermonde matrix must be computed.
-  * \param[out] VDr   - Matrix to store the gradient in r-direction of the Vandermonde matrix in all r-, s- and t-locations.
-  * \param[out] VDs   - Matrix to store the gradient in s-direction of the Vandermonde matrix in all r-, s- and t-locations.
-  * \param[out] VDt   - Matrix to store the gradient in t-direction of the Vandermonde matrix in all r-, s- and t-locations.
-  */
-  void GradVandermonde3D_Tetrahedron(unsigned short          nPoly,
-                                     unsigned short          nDOFs,
-                                     const vector<su2double> &r,
-                                     const vector<su2double> &s,
-                                     const vector<su2double> &t,
-                                     vector<su2double>       &VDr,
-                                     vector<su2double>       &VDs,
-                                     vector<su2double>       &VDt);
-
-  /*!
-  * \brief Function, which computes the gradients of the Vandermonde matrix for a standard pyramid.
-  * \param[in]  nPoly - Polynomial degree of the pyramid.
-  * \param[in]  nDOFs - Number of DOFs of the pyramid.
-  * \param[in]  r     - Parametric coordinate in r-direction for which the gradient of the Vandermonde matrix must be computed.
-  * \param[in]  s     - Parametric coordinate in s-direction for which the gradient of the Vandermonde matrix must be computed.
-  * \param[in]  t     - Parametric coordinate in t-direction for which the gradient of the Vandermonde matrix must be computed.
-  * \param[out] VDr   - Matrix to store the gradient in r-direction of the Vandermonde matrix in all r-, s- and t-locations.
-  * \param[out] VDs   - Matrix to store the gradient in s-direction of the Vandermonde matrix in all r-, s- and t-locations.
-  * \param[out] VDt   - Matrix to store the gradient in t-direction of the Vandermonde matrix in all r-, s- and t-locations.
-  */
-  void GradVandermonde3D_Pyramid(unsigned short          nPoly,
-                                 unsigned short          nDOFs,
-                                 const vector<su2double> &r,
-                                 const vector<su2double> &s,
-                                 const vector<su2double> &t,
-                                 vector<su2double>       &VDr,
-                                 vector<su2double>       &VDs,
-                                 vector<su2double>       &VDt);
-
-  /*!
-  * \brief Function, which computes the gradients of the Vandermonde matrix for a standard prism.
-  * \param[in]  nPoly - Polynomial degree of the prism.
-  * \param[in]  nDOFs - Number of DOFs of the prism.
-  * \param[in]  r     - Parametric coordinate in r-direction for which the gradient of the Vandermonde matrix must be computed.
-  * \param[in]  s     - Parametric coordinate in s-direction for which the gradient of the Vandermonde matrix must be computed.
-  * \param[in]  t     - Parametric coordinate in t-direction for which the gradient of the Vandermonde matrix must be computed.
-  * \param[out] VDr   - Matrix to store the gradient in r-direction of the Vandermonde matrix in all r-, s- and t-locations.
-  * \param[out] VDs   - Matrix to store the gradient in s-direction of the Vandermonde matrix in all r-, s- and t-locations.
-  * \param[out] VDt   - Matrix to store the gradient in t-direction of the Vandermonde matrix in all r-, s- and t-locations.
-  */
-  void GradVandermonde3D_Prism(unsigned short          nPoly,
-                               unsigned short          nDOFs,
-                               const vector<su2double> &r,
-                               const vector<su2double> &s,
-                               const vector<su2double> &t,
-                               vector<su2double>       &VDr,
-                               vector<su2double>       &VDs,
-                               vector<su2double>       &VDt);
-
-  /*!
-  * \brief Function, which computes the gradients of the Vandermonde matrix for a standard hexahedron.
-  * \param[in]  nPoly - Polynomial degree of the hexahedron.
-  * \param[in]  nDOFs - Number of DOFs of the hexahedron.
-  * \param[in]  r     - Parametric coordinate in r-direction for which the gradient of the Vandermonde matrix must be computed.
-  * \param[in]  s     - Parametric coordinate in s-direction for which the gradient of the Vandermonde matrix must be computed.
-  * \param[in]  t     - Parametric coordinate in t-direction for which the gradient of the Vandermonde matrix must be computed.
-  * \param[out] VDr   - Matrix to store the gradient in r-direction of the Vandermonde matrix in all r-, s- and t-locations.
-  * \param[out] VDs   - Matrix to store the gradient in s-direction of the Vandermonde matrix in all r-, s- and t-locations.
-  * \param[out] VDt   - Matrix to store the gradient in t-direction of the Vandermonde matrix in all r-, s- and t-locations.
-  */
-  void GradVandermonde3D_Hexahedron(unsigned short          nPoly,
-                                    unsigned short          nDOFs,
-                                    const vector<su2double> &r,
-                                    const vector<su2double> &s,
-                                    const vector<su2double> &t,
-                                    vector<su2double>       &VDr,
-                                    vector<su2double>       &VDs,
-                                    vector<su2double>       &VDt);
+  void DerivativesBasisFunctionsAdjacentElement(unsigned short VTK_TypeElem, unsigned short nPolyElem,
+                                                const bool swapFaceInElement, unsigned short& nDOFsElem,
+                                                vector<su2double>& drLagBasisIntegration,
+                                                vector<su2double>& dsLagBasisIntegration,
+                                                vector<su2double>& dtLagBasisIntegration);
+
+  /*!
+   * \brief Function, which computes the gradients of the Vandermonde matrix for a standard triangle.
+   * \param[in]  nPoly - Polynomial degree of the triangle.
+   * \param[in]  nDOFs - Number of DOFs of the triangle.
+   * \param[in]  r     - Parametric coordinate in r-direction for which the gradient of the Vandermonde matrix must be
+   * computed. \param[in]  s     - Parametric coordinate in s-direction for which the gradient of the Vandermonde matrix
+   * must be computed. \param[out] VDr   - Matrix to store the gradient in r-direction of the Vandermonde matrix in all
+   * r- and s-locations. \param[out] VDs   - Matrix to store the gradient in s-direction of the Vandermonde matrix in
+   * all r- and s-locations.
+   */
+  void GradVandermonde2D_Triangle(unsigned short nPoly, unsigned short nDOFs, const vector<su2double>& r,
+                                  const vector<su2double>& s, vector<su2double>& VDr, vector<su2double>& VDs);
+
+  /*!
+   * \brief Function, which computes the gradients of the Vandermonde matrix for a standard quadrilateral.
+   * \param[in]  nPoly - Polynomial degree of the quadrilateral.
+   * \param[in]  nDOFs - Number of DOFs of the quadrilateral.
+   * \param[in]  r     - Parametric coordinate in r-direction for which the gradient of the Vandermonde matrix must be
+   * computed. \param[in]  s     - Parametric coordinate in s-direction for which the gradient of the Vandermonde matrix
+   * must be computed. \param[out] VDr   - Matrix to store the gradient in r-direction of the Vandermonde matrix in all
+   * r- and s-locations. \param[out] VDs   - Matrix to store the gradient in s-direction of the Vandermonde matrix in
+   * all r- and s-locations.
+   */
+  void GradVandermonde2D_Quadrilateral(unsigned short nPoly, unsigned short nDOFs, const vector<su2double>& r,
+                                       const vector<su2double>& s, vector<su2double>& VDr, vector<su2double>& VDs);
+
+  /*!
+   * \brief Function, which computes the gradients of the Vandermonde matrix for a standard tetrahedron.
+   * \param[in]  nPoly - Polynomial degree of the tetrahedron.
+   * \param[in]  nDOFs - Number of DOFs of the tetrahedron.
+   * \param[in]  r     - Parametric coordinate in r-direction for which the gradient of the Vandermonde matrix must be
+   * computed. \param[in]  s     - Parametric coordinate in s-direction for which the gradient of the Vandermonde matrix
+   * must be computed. \param[in]  t     - Parametric coordinate in t-direction for which the gradient of the
+   * Vandermonde matrix must be computed. \param[out] VDr   - Matrix to store the gradient in r-direction of the
+   * Vandermonde matrix in all r-, s- and t-locations. \param[out] VDs   - Matrix to store the gradient in s-direction
+   * of the Vandermonde matrix in all r-, s- and t-locations. \param[out] VDt   - Matrix to store the gradient in
+   * t-direction of the Vandermonde matrix in all r-, s- and t-locations.
+   */
+  void GradVandermonde3D_Tetrahedron(unsigned short nPoly, unsigned short nDOFs, const vector<su2double>& r,
+                                     const vector<su2double>& s, const vector<su2double>& t, vector<su2double>& VDr,
+                                     vector<su2double>& VDs, vector<su2double>& VDt);
+
+  /*!
+   * \brief Function, which computes the gradients of the Vandermonde matrix for a standard pyramid.
+   * \param[in]  nPoly - Polynomial degree of the pyramid.
+   * \param[in]  nDOFs - Number of DOFs of the pyramid.
+   * \param[in]  r     - Parametric coordinate in r-direction for which the gradient of the Vandermonde matrix must be
+   * computed. \param[in]  s     - Parametric coordinate in s-direction for which the gradient of the Vandermonde matrix
+   * must be computed. \param[in]  t     - Parametric coordinate in t-direction for which the gradient of the
+   * Vandermonde matrix must be computed. \param[out] VDr   - Matrix to store the gradient in r-direction of the
+   * Vandermonde matrix in all r-, s- and t-locations. \param[out] VDs   - Matrix to store the gradient in s-direction
+   * of the Vandermonde matrix in all r-, s- and t-locations. \param[out] VDt   - Matrix to store the gradient in
+   * t-direction of the Vandermonde matrix in all r-, s- and t-locations.
+   */
+  void GradVandermonde3D_Pyramid(unsigned short nPoly, unsigned short nDOFs, const vector<su2double>& r,
+                                 const vector<su2double>& s, const vector<su2double>& t, vector<su2double>& VDr,
+                                 vector<su2double>& VDs, vector<su2double>& VDt);
+
+  /*!
+   * \brief Function, which computes the gradients of the Vandermonde matrix for a standard prism.
+   * \param[in]  nPoly - Polynomial degree of the prism.
+   * \param[in]  nDOFs - Number of DOFs of the prism.
+   * \param[in]  r     - Parametric coordinate in r-direction for which the gradient of the Vandermonde matrix must be
+   * computed. \param[in]  s     - Parametric coordinate in s-direction for which the gradient of the Vandermonde matrix
+   * must be computed. \param[in]  t     - Parametric coordinate in t-direction for which the gradient of the
+   * Vandermonde matrix must be computed. \param[out] VDr   - Matrix to store the gradient in r-direction of the
+   * Vandermonde matrix in all r-, s- and t-locations. \param[out] VDs   - Matrix to store the gradient in s-direction
+   * of the Vandermonde matrix in all r-, s- and t-locations. \param[out] VDt   - Matrix to store the gradient in
+   * t-direction of the Vandermonde matrix in all r-, s- and t-locations.
+   */
+  void GradVandermonde3D_Prism(unsigned short nPoly, unsigned short nDOFs, const vector<su2double>& r,
+                               const vector<su2double>& s, const vector<su2double>& t, vector<su2double>& VDr,
+                               vector<su2double>& VDs, vector<su2double>& VDt);
+
+  /*!
+   * \brief Function, which computes the gradients of the Vandermonde matrix for a standard hexahedron.
+   * \param[in]  nPoly - Polynomial degree of the hexahedron.
+   * \param[in]  nDOFs - Number of DOFs of the hexahedron.
+   * \param[in]  r     - Parametric coordinate in r-direction for which the gradient of the Vandermonde matrix must be
+   * computed. \param[in]  s     - Parametric coordinate in s-direction for which the gradient of the Vandermonde matrix
+   * must be computed. \param[in]  t     - Parametric coordinate in t-direction for which the gradient of the
+   * Vandermonde matrix must be computed. \param[out] VDr   - Matrix to store the gradient in r-direction of the
+   * Vandermonde matrix in all r-, s- and t-locations. \param[out] VDs   - Matrix to store the gradient in s-direction
+   * of the Vandermonde matrix in all r-, s- and t-locations. \param[out] VDt   - Matrix to store the gradient in
+   * t-direction of the Vandermonde matrix in all r-, s- and t-locations.
+   */
+  void GradVandermonde3D_Hexahedron(unsigned short nPoly, unsigned short nDOFs, const vector<su2double>& r,
+                                    const vector<su2double>& s, const vector<su2double>& t, vector<su2double>& VDr,
+                                    vector<su2double>& VDs, vector<su2double>& VDt);
 
   /*!
   * \brief Function, which determines the values of the Lagrangian interpolation
@@ -330,13 +297,11 @@ class CFEMStandardElementBase {
   * \param[out] drLagBasisPoints - Values of the r-derivatives of the Lagrangian
                                    interpolation functions in the given points.
   */
-  void LagrangianBasisFunctionAndDerivativesLine(const unsigned short    nPoly,
-                                                 const vector<su2double> &rPoints,
-                                                 unsigned short          &nDOFs,
-                                                 vector<su2double>       &rDOFs,
-                                                 vector<su2double>       &matVandermondeInv,
-                                                 vector<su2double>       &lagBasisPoints,
-                                                 vector<su2double>       &drLagBasisPoints);
+  void LagrangianBasisFunctionAndDerivativesLine(const unsigned short nPoly, const vector<su2double>& rPoints,
+                                                 unsigned short& nDOFs, vector<su2double>& rDOFs,
+                                                 vector<su2double>& matVandermondeInv,
+                                                 vector<su2double>& lagBasisPoints,
+                                                 vector<su2double>& drLagBasisPoints);
 
   /*!
   * \brief Function, which determines the values of the Lagrangian interpolation
@@ -357,16 +322,10 @@ class CFEMStandardElementBase {
   * \param[out] dsLagBasisPoints - Values of the s-derivatives of the Lagrangian
                                    interpolation functions in the given points.
   */
-  void LagrangianBasisFunctionAndDerivativesTriangle(const unsigned short    nPoly,
-                                                     const vector<su2double> &rPoints,
-                                                     const vector<su2double> &sPoints,
-                                                     unsigned short          &nDOFs,
-                                                     vector<su2double>       &rDOFs,
-                                                     vector<su2double>       &sDOFs,
-                                                     vector<su2double>       &matVandermondeInv,
-                                                     vector<su2double>       &lagBasisPoints,
-                                                     vector<su2double>       &drLagBasisPoints,
-                                                     vector<su2double>       &dsLagBasisPoints);
+  void LagrangianBasisFunctionAndDerivativesTriangle(
+      const unsigned short nPoly, const vector<su2double>& rPoints, const vector<su2double>& sPoints,
+      unsigned short& nDOFs, vector<su2double>& rDOFs, vector<su2double>& sDOFs, vector<su2double>& matVandermondeInv,
+      vector<su2double>& lagBasisPoints, vector<su2double>& drLagBasisPoints, vector<su2double>& dsLagBasisPoints);
 
   /*!
   * \brief Function, which determines the values of the Lagrangian interpolation
@@ -387,16 +346,10 @@ class CFEMStandardElementBase {
   * \param[out] dsLagBasisPoints - Values of the s-derivatives of the Lagrangian
                                    interpolation functions in the given points.
   */
-  void LagrangianBasisFunctionAndDerivativesQuadrilateral(const unsigned short    nPoly,
-                                                          const vector<su2double> &rPoints,
-                                                          const vector<su2double> &sPoints,
-                                                          unsigned short          &nDOFs,
-                                                          vector<su2double>       &rDOFs,
-                                                          vector<su2double>       &sDOFs,
-                                                          vector<su2double>       &matVandermondeInv,
-                                                          vector<su2double>       &lagBasisPoints,
-                                                          vector<su2double>       &drLagBasisPoints,
-                                                          vector<su2double>       &dsLagBasisPoints);
+  void LagrangianBasisFunctionAndDerivativesQuadrilateral(
+      const unsigned short nPoly, const vector<su2double>& rPoints, const vector<su2double>& sPoints,
+      unsigned short& nDOFs, vector<su2double>& rDOFs, vector<su2double>& sDOFs, vector<su2double>& matVandermondeInv,
+      vector<su2double>& lagBasisPoints, vector<su2double>& drLagBasisPoints, vector<su2double>& dsLagBasisPoints);
 
   /*!
   * \brief Function, which determines the values of the Lagrangian interpolation
@@ -422,19 +375,11 @@ class CFEMStandardElementBase {
   * \param[out] dtLagBasisPoints - Values of the t-derivatives of the Lagrangian
                                    interpolation functions in the given points.
   */
-  void LagrangianBasisFunctionAndDerivativesTetrahedron(const unsigned short    nPoly,
-                                                        const vector<su2double> &rPoints,
-                                                        const vector<su2double> &sPoints,
-                                                        const vector<su2double> &tPoints,
-                                                        unsigned short          &nDOFs,
-                                                        vector<su2double>       &rDOFs,
-                                                        vector<su2double>       &sDOFs,
-                                                        vector<su2double>       &tDOFs,
-                                                        vector<su2double>       &matVandermondeInv,
-                                                        vector<su2double>       &lagBasisPoints,
-                                                        vector<su2double>       &drLagBasisPoints,
-                                                        vector<su2double>       &dsLagBasisPoints,
-                                                        vector<su2double>       &dtLagBasisPoints);
+  void LagrangianBasisFunctionAndDerivativesTetrahedron(
+      const unsigned short nPoly, const vector<su2double>& rPoints, const vector<su2double>& sPoints,
+      const vector<su2double>& tPoints, unsigned short& nDOFs, vector<su2double>& rDOFs, vector<su2double>& sDOFs,
+      vector<su2double>& tDOFs, vector<su2double>& matVandermondeInv, vector<su2double>& lagBasisPoints,
+      vector<su2double>& drLagBasisPoints, vector<su2double>& dsLagBasisPoints, vector<su2double>& dtLagBasisPoints);
 
   /*!
   * \brief Function, which determines the values of the Lagrangian interpolation
@@ -460,19 +405,11 @@ class CFEMStandardElementBase {
   * \param[out] dtLagBasisPoints - Values of the t-derivatives of the Lagrangian
                                    interpolation functions in the given points.
   */
-  void LagrangianBasisFunctionAndDerivativesPyramid(const unsigned short    nPoly,
-                                                    const vector<su2double> &rPoints,
-                                                    const vector<su2double> &sPoints,
-                                                    const vector<su2double> &tPoints,
-                                                    unsigned short          &nDOFs,
-                                                    vector<su2double>       &rDOFs,
-                                                    vector<su2double>       &sDOFs,
-                                                    vector<su2double>       &tDOFs,
-                                                    vector<su2double>       &matVandermondeInv,
-                                                    vector<su2double>       &lagBasisPoints,
-                                                    vector<su2double>       &drLagBasisPoints,
-                                                    vector<su2double>       &dsLagBasisPoints,
-                                                    vector<su2double>       &dtLagBasisPoints);
+  void LagrangianBasisFunctionAndDerivativesPyramid(
+      const unsigned short nPoly, const vector<su2double>& rPoints, const vector<su2double>& sPoints,
+      const vector<su2double>& tPoints, unsigned short& nDOFs, vector<su2double>& rDOFs, vector<su2double>& sDOFs,
+      vector<su2double>& tDOFs, vector<su2double>& matVandermondeInv, vector<su2double>& lagBasisPoints,
+      vector<su2double>& drLagBasisPoints, vector<su2double>& dsLagBasisPoints, vector<su2double>& dtLagBasisPoints);
 
   /*!
   * \brief Function, which determines the values of the Lagrangian interpolation
@@ -498,19 +435,11 @@ class CFEMStandardElementBase {
   * \param[out] dtLagBasisPoints - Values of the t-derivatives of the Lagrangian
                                    interpolation functions in the given points.
   */
-  void LagrangianBasisFunctionAndDerivativesPrism(const unsigned short    nPoly,
-                                                  const vector<su2double> &rPoints,
-                                                  const vector<su2double> &sPoints,
-                                                  const vector<su2double> &tPoints,
-                                                  unsigned short          &nDOFs,
-                                                  vector<su2double>       &rDOFs,
-                                                  vector<su2double>       &sDOFs,
-                                                  vector<su2double>       &tDOFs,
-                                                  vector<su2double>       &matVandermondeInv,
-                                                  vector<su2double>       &lagBasisPoints,
-                                                  vector<su2double>       &drLagBasisPoints,
-                                                  vector<su2double>       &dsLagBasisPoints,
-                                                  vector<su2double>       &dtLagBasisPoints);
+  void LagrangianBasisFunctionAndDerivativesPrism(
+      const unsigned short nPoly, const vector<su2double>& rPoints, const vector<su2double>& sPoints,
+      const vector<su2double>& tPoints, unsigned short& nDOFs, vector<su2double>& rDOFs, vector<su2double>& sDOFs,
+      vector<su2double>& tDOFs, vector<su2double>& matVandermondeInv, vector<su2double>& lagBasisPoints,
+      vector<su2double>& drLagBasisPoints, vector<su2double>& dsLagBasisPoints, vector<su2double>& dtLagBasisPoints);
 
   /*!
   * \brief Function, which determines the values of the Lagrangian interpolation
@@ -536,19 +465,11 @@ class CFEMStandardElementBase {
   * \param[out] dtLagBasisPoints - Values of the t-derivatives of the Lagrangian
                                    interpolation functions in the given points.
   */
-  void LagrangianBasisFunctionAndDerivativesHexahedron(const unsigned short    nPoly,
-                                                       const vector<su2double> &rPoints,
-                                                       const vector<su2double> &sPoints,
-                                                       const vector<su2double> &tPoints,
-                                                       unsigned short          &nDOFs,
-                                                       vector<su2double>       &rDOFs,
-                                                       vector<su2double>       &sDOFs,
-                                                       vector<su2double>       &tDOFs,
-                                                       vector<su2double>       &matVandermondeInv,
-                                                       vector<su2double>       &lagBasisPoints,
-                                                       vector<su2double>       &drLagBasisPoints,
-                                                       vector<su2double>       &dsLagBasisPoints,
-                                                       vector<su2double>       &dtLagBasisPoints);
+  void LagrangianBasisFunctionAndDerivativesHexahedron(
+      const unsigned short nPoly, const vector<su2double>& rPoints, const vector<su2double>& sPoints,
+      const vector<su2double>& tPoints, unsigned short& nDOFs, vector<su2double>& rDOFs, vector<su2double>& sDOFs,
+      vector<su2double>& tDOFs, vector<su2double>& matVandermondeInv, vector<su2double>& lagBasisPoints,
+      vector<su2double>& drLagBasisPoints, vector<su2double>& dsLagBasisPoints, vector<su2double>& dtLagBasisPoints);
 
   /*!
   * \brief Function, which carries out a matrix matrix multiplication to obtain
@@ -564,11 +485,8 @@ class CFEMStandardElementBase {
   * \param[out] C       - Result of A*B, dimension nPoints X nDOFs. The result is stored in row
                           major order
   */
-  void MatMulRowMajor(const unsigned short nDOFs,
-                      const unsigned short nPoints,
-                      const vector<su2double> &A,
-                      const vector<su2double> &B,
-                      vector<su2double>       &C);
+  void MatMulRowMajor(const unsigned short nDOFs, const unsigned short nPoints, const vector<su2double>& A,
+                      const vector<su2double>& B, vector<su2double>& C);
 
   /*!
   * \brief Function, which computes the local connectivity of linear subelements of
@@ -576,8 +494,7 @@ class CFEMStandardElementBase {
   * \param[in]  nPoly    - Polynomial degree of the line.
   * \param[out] subConn  - The local subconnectivity of a line element.
   */
-  void SubConnForPlottingLine(const unsigned short   nPoly,
-                              vector<unsigned short> &subConn);
+  void SubConnForPlottingLine(const unsigned short nPoly, vector<unsigned short>& subConn);
 
   /*!
   * \brief Function, which computes the local connectivity of linear subelements of
@@ -585,8 +502,7 @@ class CFEMStandardElementBase {
   * \param[in]  nPoly    - Polynomial degree of the quadrilateral.
   * \param[out] subConn  - The local subconnectivity of a triangle element.
   */
-  void SubConnForPlottingQuadrilateral(const unsigned short   nPoly,
-                                       vector<unsigned short> &subConn);
+  void SubConnForPlottingQuadrilateral(const unsigned short nPoly, vector<unsigned short>& subConn);
 
   /*!
   * \brief Function, which computes the local connectivity of linear subelements of
@@ -594,8 +510,7 @@ class CFEMStandardElementBase {
   * \param[in]  nPoly    - Polynomial degree of the triangle.
   * \param[out] subConn  - The local subconnectivity of a triangle element.
   */
-  void SubConnForPlottingTriangle(const unsigned short   nPoly,
-                                  vector<unsigned short> &subConn);
+  void SubConnForPlottingTriangle(const unsigned short nPoly, vector<unsigned short>& subConn);
 
   /*!
    * \brief Function, which computes the Vandermonde matrix for a standard triangle.
@@ -604,12 +519,9 @@ class CFEMStandardElementBase {
    * \param[in]  r     - Parametric coordinates in r-direction for which the Vandermonde matrix must be computed.
    * \param[in]  s     - Parametric coordinates in s-direction for which the Vandermonde matrix must be computed.
    * \param[out] V     - Matrix to store the Vandermonde matrix in all r- and s-locations.
-  */
-  void Vandermonde2D_Triangle(unsigned short          nPoly,
-                              unsigned short          nDOFs,
-                              const vector<su2double> &r,
-                              const vector<su2double> &s,
-                              vector<su2double>       &V);
+   */
+  void Vandermonde2D_Triangle(unsigned short nPoly, unsigned short nDOFs, const vector<su2double>& r,
+                              const vector<su2double>& s, vector<su2double>& V);
 
   /*!
    * \brief Function, which computes the Vandermonde matrix for a standard quadrilateral.
@@ -618,12 +530,9 @@ class CFEMStandardElementBase {
    * \param[in]  r     - Parametric coordinates in r-direction for which the Vandermonde matrix must be computed.
    * \param[in]  s     - Parametric coordinates in s-direction for which the Vandermonde matrix must be computed.
    * \param[out] V     - Matrix to store the Vandermonde matrix in all r- and s-locations.
-  */
-  void Vandermonde2D_Quadrilateral(unsigned short          nPoly,
-                                   unsigned short          nDOFs,
-                                   const vector<su2double> &r,
-                                   const vector<su2double> &s,
-                                   vector<su2double>       &V);
+   */
+  void Vandermonde2D_Quadrilateral(unsigned short nPoly, unsigned short nDOFs, const vector<su2double>& r,
+                                   const vector<su2double>& s, vector<su2double>& V);
 
   /*!
    * \brief Function, which computes the Vandermonde matrix for a standard tetrahedron.
@@ -633,13 +542,9 @@ class CFEMStandardElementBase {
    * \param[in]  s     - Parametric coordinates in s-direction for which the Vandermonde matrix must be computed.
    * \param[in]  t     - Parametric coordinates in t-direction for which the Vandermonde matrix must be computed.
    * \param[out] V     - Matrix to store the Vandermonde matrix in all r-, s- and t-locations.
-  */
-  void Vandermonde3D_Tetrahedron(unsigned short          nPoly,
-                                 unsigned short          nDOFs,
-                                 const vector<su2double> &r,
-                                 const vector<su2double> &s,
-                                 const vector<su2double> &t,
-                                 vector<su2double>       &V);
+   */
+  void Vandermonde3D_Tetrahedron(unsigned short nPoly, unsigned short nDOFs, const vector<su2double>& r,
+                                 const vector<su2double>& s, const vector<su2double>& t, vector<su2double>& V);
 
   /*!
    * \brief Function, which computes the Vandermonde matrix for a standard pyramid.
@@ -649,13 +554,9 @@ class CFEMStandardElementBase {
    * \param[in]  s     - Parametric coordinates in s-direction for which the Vandermonde matrix must be computed.
    * \param[in]  t     - Parametric coordinates in t-direction for which the Vandermonde matrix must be computed.
    * \param[out] V     - Matrix to store the Vandermonde matrix in all r-, s- and t-locations.
-  */
-  void Vandermonde3D_Pyramid(unsigned short          nPoly,
-                             unsigned short          nDOFs,
-                             const vector<su2double> &r,
-                             const vector<su2double> &s,
-                             const vector<su2double> &t,
-                             vector<su2double>       &V);
+   */
+  void Vandermonde3D_Pyramid(unsigned short nPoly, unsigned short nDOFs, const vector<su2double>& r,
+                             const vector<su2double>& s, const vector<su2double>& t, vector<su2double>& V);
 
   /*!
    * \brief Function, which computes the Vandermonde matrix for a standard prism.
@@ -665,13 +566,9 @@ class CFEMStandardElementBase {
    * \param[in]  s     - Parametric coordinates in s-direction for which the Vandermonde matrix must be computed.
    * \param[in]  t     - Parametric coordinates in t-direction for which the Vandermonde matrix must be computed.
    * \param[out] V     - Matrix to store the Vandermonde matrix in all r-, s- and t-locations.
-  */
-  void Vandermonde3D_Prism(unsigned short          nPoly,
-                           unsigned short          nDOFs,
-                           const vector<su2double> &r,
-                           const vector<su2double> &s,
-                           const vector<su2double> &t,
-                           vector<su2double>       &V);
+   */
+  void Vandermonde3D_Prism(unsigned short nPoly, unsigned short nDOFs, const vector<su2double>& r,
+                           const vector<su2double>& s, const vector<su2double>& t, vector<su2double>& V);
 
   /*!
    * \brief Function, which computes the Vandermonde matrix for a standard hexahedron.
@@ -681,13 +578,9 @@ class CFEMStandardElementBase {
    * \param[in]  s     - Parametric coordinates in s-direction for which the Vandermonde matrix must be computed.
    * \param[in]  t     - Parametric coordinates in t-direction for which the Vandermonde matrix must be computed.
    * \param[out] V     - Matrix to store the Vandermonde matrix in all r-, s- and t-locations.
-  */
-  void Vandermonde3D_Hexahedron(unsigned short          nPoly,
-                                unsigned short          nDOFs,
-                                const vector<su2double> &r,
-                                const vector<su2double> &s,
-                                const vector<su2double> &t,
-                                vector<su2double>       &V);
+   */
+  void Vandermonde3D_Hexahedron(unsigned short nPoly, unsigned short nDOFs, const vector<su2double>& r,
+                                const vector<su2double>& s, const vector<su2double>& t, vector<su2double>& V);
 
   /*!
   * \brief Function, which computes the constant in the penalty terms for a
@@ -697,29 +590,26 @@ class CFEMStandardElementBase {
   * \param[in] nPolyElem    - The polynomial degree of the adjacent element.
   * \return                   The value of the viscous penalty parameter.
   */
-  su2double ViscousPenaltyParameter(const unsigned short VTK_TypeElem,
-                                    const unsigned short nPolyElem) const;
-private:
+  su2double ViscousPenaltyParameter(const unsigned short VTK_TypeElem, const unsigned short nPolyElem) const;
+
+ private:
   /*!
-  * \brief Function, which determines the 1D Gauss Legendre integration points and weights.
-  * \param[in,out] GLPoints  - The location of the Gauss-Legendre integration points.
-  * \param[in,out] GLWeights - The weights of the Gauss-Legendre integration points.
-  */
-  void GaussLegendrePoints1D(vector<su2double> &GLPoints,
-                             vector<su2double> &GLWeights);
+   * \brief Function, which determines the 1D Gauss Legendre integration points and weights.
+   * \param[in,out] GLPoints  - The location of the Gauss-Legendre integration points.
+   * \param[in,out] GLWeights - The weights of the Gauss-Legendre integration points.
+   */
+  void GaussLegendrePoints1D(vector<su2double>& GLPoints, vector<su2double>& GLWeights);
 
   /*!
-  * \brief Function, which computes the value of the gradient of the Jacobi polynomial for the given x-coordinate.
-  * \param[in] n     - Order of the Jacobi polynomial.
-  * \param[in] alpha - Alpha coefficient of the Jacobi polynomial.
-  * \param[in] beta  - Beta coefficient of the Jacobi polynomial.
-  * \param[in] x     - Coordinate (-1 <= x <= 1) for which the gradient of the Jacobi polynomial must be evaluated.
-  * \return            The value of the gradient of the normalized Jacobi polynomial f order n for the given value of x.
-  */
-  su2double GradNormJacobi(unsigned short n,
-                           unsigned short alpha,
-                           unsigned short beta,
-                           su2double      x);
+   * \brief Function, which computes the value of the gradient of the Jacobi polynomial for the given x-coordinate.
+   * \param[in] n     - Order of the Jacobi polynomial.
+   * \param[in] alpha - Alpha coefficient of the Jacobi polynomial.
+   * \param[in] beta  - Beta coefficient of the Jacobi polynomial.
+   * \param[in] x     - Coordinate (-1 <= x <= 1) for which the gradient of the Jacobi polynomial must be evaluated.
+   * \return            The value of the gradient of the normalized Jacobi polynomial f order n for the given value of
+   * x.
+   */
+  su2double GradNormJacobi(unsigned short n, unsigned short alpha, unsigned short beta, su2double x);
 
   /*!
   * \brief Function, which determines the integration points for a line
@@ -764,17 +654,14 @@ class CFEMStandardElementBase {
   void IntegrationPointsHexahedron(void);
 
   /*!
-  * \brief Function, which computes the value of the Jacobi polynomial for the given x-coordinate.
-  * \param[in] n     - Order of the Jacobi polynomial.
-  * \param[in] alpha - Alpha coefficient of the Jacobi polynomial.
-  * \param[in] beta  - Beta coefficient of the Jacobi polynomial.
-  * \param[in] x     - Coordinate (-1 <= x <= 1) for which the Jacobi polynomial must be evaluated.
-  * \return            The value of the normalized Jacobi polynomial f order n for the given value of x.
-  */
-  su2double NormJacobi(unsigned short n,
-                       unsigned short alpha,
-                       unsigned short beta,
-                       su2double      x);
+   * \brief Function, which computes the value of the Jacobi polynomial for the given x-coordinate.
+   * \param[in] n     - Order of the Jacobi polynomial.
+   * \param[in] alpha - Alpha coefficient of the Jacobi polynomial.
+   * \param[in] beta  - Beta coefficient of the Jacobi polynomial.
+   * \param[in] x     - Coordinate (-1 <= x <= 1) for which the Jacobi polynomial must be evaluated.
+   * \return            The value of the normalized Jacobi polynomial f order n for the given value of x.
+   */
+  su2double NormJacobi(unsigned short n, unsigned short alpha, unsigned short beta, su2double x);
 };
 
 /*!
@@ -784,50 +671,54 @@ class CFEMStandardElementBase {
  * \version 7.5.1 "Blackbird"
  */
 class CFEMStandardElement : public CFEMStandardElementBase {
-private:
-
-  unsigned short nPoly;        /*!< \brief Polynomial degree of the element. */
-  unsigned short nDOFs;        /*!< \brief Number of DOFs of the element. */
-
-  unsigned short VTK_Type1;    /*!< \brief VTK type for elements of type 1 in subConn1ForPlotting. */
-  unsigned short VTK_Type2;    /*!< \brief VTK type for elements of type 2 in subConn2ForPlotting. */
-
-  vector<su2double> rDOFs;     /*!< \brief r-location of the DOFs for this standard element. */
-  vector<su2double> sDOFs;     /*!< \brief s-location of the DOFs for this standard element, if needed. */
-  vector<su2double> tDOFs;     /*!< \brief t-location of the DOFs for this standard element, if needed. */
-
-  vector<su2double> lagBasisIntegration;       /*!< \brief Lagrangian basis functions in the integration points. */
-  vector<su2double> lagBasisIntegrationTrans;  /*!< \brief Transpose of lagBasisIntegration. It is stored such that
-                                                           in the ADER-DG predictor step the residual is obtained
-                                                           by one matrix multiplication. */
-  vector<su2double> lagBasisSolDOFs;       /*!< \brief Lagrangian basis functions in the solution DOFs. Only different
-                                                       from 1 if the polynomial degree of the grid and solution differs. */
-
-  vector<su2double> drLagBasisIntegration; /*!< \brief r-derivatives of the Lagrangian basis functions in the integration points. */
-  vector<su2double> dsLagBasisIntegration; /*!< \brief s-derivatives of the Lagrangian basis functions in the integration points. */
-  vector<su2double> dtLagBasisIntegration; /*!< \brief t-derivatives of the Lagrangian basis functions in the integration points. */
-
-  vector<su2double> matVandermondeInv;    /*!< \brief Inverse matrix of Vandermonde matrix in the DOFs for this standard element.
-                                                      This data is needed for the computation of shock sensing. */
-
-  vector<su2double> matBasisIntegration;  /*!< \brief Matrix of lagBasisIntegration, drLagBasisIntegration, dsLagBasisIntegration
-                                                      and dtLagBasisIntegration combined for efficiency when using BLAS routines. */
-  vector<su2double> matDerBasisIntTrans;  /*!< \brief Matrix of the transpose of the derivative part of matBasisIntegration. It is
-                                                      stored such that the volume residual can be computed in one matrix multiplication. */
-  vector<su2double> matDerBasisSolDOFs;   /*!< \brief Matrix of the derivatives of the Lagrangian basis functions in the solution
-                                                      DOFs. Needed to compute the metric terms in the solution DOFs. */
-  vector<su2double> matDerBasisOwnDOFs;   /*!< \brief Matrix of the derivatives of the Lagrangian basis functions in the owned
-                                                      DOFs. This differs from matDerBasisSolDOFs when the grid DOFs and the
-                                                      solution DOFs do not coincide. This data is needed for the computation
-                                                      of the derivatives of the metric terms. */
-  vector<su2double> mat2ndDerBasisInt;    /*!< \brief Matrix which contains all possible second derivatives of the basis functions
-                                                      in the integration points. As such second derivatives can be computed
-                                                      using one call to the BLAS routines. */
-
-  vector<unsigned short> connFace0; /*!< \brief Local connectivity of face 0 of the element. The numbering of the DOFs is
-                                                such that the element is to the left of the face. */
-  vector<unsigned short> connFace1; /*!< \brief Local connectivity of face 1 of the element. The numbering of the DOFs is
-                                                such that the element is to the left of the face. */
+ private:
+  unsigned short nPoly; /*!< \brief Polynomial degree of the element. */
+  unsigned short nDOFs; /*!< \brief Number of DOFs of the element. */
+
+  unsigned short VTK_Type1; /*!< \brief VTK type for elements of type 1 in subConn1ForPlotting. */
+  unsigned short VTK_Type2; /*!< \brief VTK type for elements of type 2 in subConn2ForPlotting. */
+
+  vector<su2double> rDOFs; /*!< \brief r-location of the DOFs for this standard element. */
+  vector<su2double> sDOFs; /*!< \brief s-location of the DOFs for this standard element, if needed. */
+  vector<su2double> tDOFs; /*!< \brief t-location of the DOFs for this standard element, if needed. */
+
+  vector<su2double> lagBasisIntegration;      /*!< \brief Lagrangian basis functions in the integration points. */
+  vector<su2double> lagBasisIntegrationTrans; /*!< \brief Transpose of lagBasisIntegration. It is stored such that
+                                                          in the ADER-DG predictor step the residual is obtained
+                                                          by one matrix multiplication. */
+  vector<su2double> lagBasisSolDOFs; /*!< \brief Lagrangian basis functions in the solution DOFs. Only different
+                                                 from 1 if the polynomial degree of the grid and solution differs. */
+
+  vector<su2double>
+      drLagBasisIntegration; /*!< \brief r-derivatives of the Lagrangian basis functions in the integration points. */
+  vector<su2double>
+      dsLagBasisIntegration; /*!< \brief s-derivatives of the Lagrangian basis functions in the integration points. */
+  vector<su2double>
+      dtLagBasisIntegration; /*!< \brief t-derivatives of the Lagrangian basis functions in the integration points. */
+
+  vector<su2double> matVandermondeInv; /*!< \brief Inverse matrix of Vandermonde matrix in the DOFs for this standard
+                                          element. This data is needed for the computation of shock sensing. */
+
+  vector<su2double>
+      matBasisIntegration; /*!< \brief Matrix of lagBasisIntegration, drLagBasisIntegration, dsLagBasisIntegration
+                                       and dtLagBasisIntegration combined for efficiency when using BLAS routines. */
+  vector<su2double> matDerBasisIntTrans; /*!< \brief Matrix of the transpose of the derivative part of
+                                            matBasisIntegration. It is stored such that the volume residual can be
+                                            computed in one matrix multiplication. */
+  vector<su2double> matDerBasisSolDOFs;  /*!< \brief Matrix of the derivatives of the Lagrangian basis functions in the
+                                            solution  DOFs. Needed to compute the metric terms in the solution DOFs. */
+  vector<su2double> matDerBasisOwnDOFs;  /*!< \brief Matrix of the derivatives of the Lagrangian basis functions in the
+                                            owned  DOFs. This differs from matDerBasisSolDOFs when the grid DOFs and the
+                                                     solution DOFs do not coincide. This data is needed for the
+                                            computation  of the derivatives of the metric terms. */
+  vector<su2double> mat2ndDerBasisInt;   /*!< \brief Matrix which contains all possible second derivatives of the basis
+                                            functions   in the integration points. As such second derivatives can be
+                                            computed   using one call to the BLAS routines. */
+
+  vector<unsigned short> connFace0; /*!< \brief Local connectivity of face 0 of the element. The numbering of the DOFs
+                                       is such that the element is to the left of the face. */
+  vector<unsigned short> connFace1; /*!< \brief Local connectivity of face 1 of the element. The numbering of the DOFs
+                                       is such that the element is to the left of the face. */
   vector<unsigned short> connFace2; /*!< \brief Local connectivity of face 2 of the element, if present. The numbering
                                                 of the DOFs is such that the element is to the left of the face. */
   vector<unsigned short> connFace3; /*!< \brief Local connectivity of face 3 of the element, if present. The numbering
@@ -837,11 +728,11 @@ class CFEMStandardElement : public CFEMStandardElementBase {
   vector<unsigned short> connFace5; /*!< \brief Local connectivity of face 5 of the element, if present. The numbering
                                                 of the DOFs is such that the element is to the left of the face. */
 
-  vector<unsigned short> subConn1ForPlotting; /*!< \brief Local subconnectivity of element type 1 of the high order element.
-                                                          Used for plotting. */
-  vector<unsigned short> subConn2ForPlotting; /*!< \brief Local subconnectivity of element type 2 of the high order element.
-                                                          Used for plotting. */
-public:
+  vector<unsigned short> subConn1ForPlotting; /*!< \brief Local subconnectivity of element type 1 of the high order
+                                                 element. Used for plotting. */
+  vector<unsigned short> subConn2ForPlotting; /*!< \brief Local subconnectivity of element type 2 of the high order
+                                                 element. Used for plotting. */
+ public:
   /*!
   * \brief Alternative constructor.
   * \param[in] val_VTK_Type   - Type of the element using the VTK convention.
@@ -858,26 +749,24 @@ class CFEMStandardElement : public CFEMStandardElementBase {
   * \param[in] tLocSolDOFs    - Default argument. If specified, it contains the
                                 parametric t location of the solution DOFs.
   */
-  CFEMStandardElement(unsigned short          val_VTK_Type,
-                      unsigned short          val_nPoly,
-                      bool                    val_constJac,
-                      CConfig                 *config,
-                      unsigned short          val_orderExact = 0,
-                      const vector<su2double> *rLocSolDOFs = nullptr,
-                      const vector<su2double> *sLocSolDOFs = nullptr,
-                      const vector<su2double> *tLocSolDOFs = nullptr);
+  CFEMStandardElement(unsigned short val_VTK_Type, unsigned short val_nPoly, bool val_constJac, CConfig* config,
+                      unsigned short val_orderExact = 0, const vector<su2double>* rLocSolDOFs = nullptr,
+                      const vector<su2double>* sLocSolDOFs = nullptr, const vector<su2double>* tLocSolDOFs = nullptr);
   /*!
-  * \brief Copy constructor.
-  * \param[in] other - Object, whose data must be copied.
-  */
-  CFEMStandardElement(const CFEMStandardElement &other) : CFEMStandardElementBase(other) {Copy(other);}
+   * \brief Copy constructor.
+   * \param[in] other - Object, whose data must be copied.
+   */
+  CFEMStandardElement(const CFEMStandardElement& other) : CFEMStandardElementBase(other) { Copy(other); }
 
   /*!
-  * \brief Assignment operator.
-  * \param[in] other - Object, to which this object must be assigned.
-  * \return The current object, after the member variables were assigned the correct value.
-  */
-  CFEMStandardElement& operator=(const CFEMStandardElement &other){Copy(other); return (*this);}
+   * \brief Assignment operator.
+   * \param[in] other - Object, to which this object must be assigned.
+   * \return The current object, after the member variables were assigned the correct value.
+   */
+  CFEMStandardElement& operator=(const CFEMStandardElement& other) {
+    Copy(other);
+    return (*this);
+  }
 
   /*!
   * \brief Function, which computes the Lagrangian basis functions for the
@@ -886,8 +775,7 @@ class CFEMStandardElement : public CFEMStandardElementBase {
                             and derivatives must be computed.
   * \param[out] lagBasis  - The values of the Lagrangian basis functions in parCoor.
   */
-  void BasisFunctionsInPoint(const su2double   *parCoor,
-                             vector<su2double> &lagBasis);
+  void BasisFunctionsInPoint(const su2double* parCoor, vector<su2double>& lagBasis);
   /*!
   * \brief Function, which computes the Lagrangian basis functions and its
            derivatives for the given parametric coordinates.
@@ -897,166 +785,169 @@ class CFEMStandardElement : public CFEMStandardElementBase {
   * \param[out] dLagBasis - The values of the derivatives of the basis functions
                             in parCoor.
   */
-  void BasisFunctionsAndDerivativesInPoint(const su2double            *parCoor,
-                                           vector<su2double>          &lagBasis,
-                                           vector<vector<su2double> > &dLagBasis);
+  void BasisFunctionsAndDerivativesInPoint(const su2double* parCoor, vector<su2double>& lagBasis,
+                                           vector<vector<su2double> >& dLagBasis);
 
   /*!
-  * \brief Function, which makes available the values of the basis functions in the integration points.
-  * \return The pointer to data, which stores the basis functions in the integration points.
-  */
-  inline su2double* GetBasisFunctionsIntegration(void){return lagBasisIntegration.data();}
+   * \brief Function, which makes available the values of the basis functions in the integration points.
+   * \return The pointer to data, which stores the basis functions in the integration points.
+   */
+  inline su2double* GetBasisFunctionsIntegration(void) { return lagBasisIntegration.data(); }
 
   /*!
-  * \brief Function, which makes available the transpose of the basis functions in the integration points.
-  * \return The pointer to data, which stores the transpose matrix of the basis functions.
-  */
-  inline const su2double* GetBasisFunctionsIntegrationTrans(void) const {return lagBasisIntegrationTrans.data();}
+   * \brief Function, which makes available the transpose of the basis functions in the integration points.
+   * \return The pointer to data, which stores the transpose matrix of the basis functions.
+   */
+  inline const su2double* GetBasisFunctionsIntegrationTrans(void) const { return lagBasisIntegrationTrans.data(); }
 
   /*!
-  * \brief Function, which makes available the values of the basis functions in the solution DOFs.
-  * \return The pointer to data, which stores the basis functions in the solution DOFs.
-  */
-  inline const su2double* GetBasisFunctionsSolDOFs(void) const {return lagBasisSolDOFs.data();}
+   * \brief Function, which makes available the values of the basis functions in the solution DOFs.
+   * \return The pointer to data, which stores the basis functions in the solution DOFs.
+   */
+  inline const su2double* GetBasisFunctionsSolDOFs(void) const { return lagBasisSolDOFs.data(); }
 
   /*!
-  * \brief Function, which makes available the r-derivatives of the basis functions in the integration points.
-  * \return  The pointer to data, which stores the r-derivatives of the basis functions.
-  */
-  inline su2double* GetDrBasisFunctionsIntegration(void){return drLagBasisIntegration.data();}
+   * \brief Function, which makes available the r-derivatives of the basis functions in the integration points.
+   * \return  The pointer to data, which stores the r-derivatives of the basis functions.
+   */
+  inline su2double* GetDrBasisFunctionsIntegration(void) { return drLagBasisIntegration.data(); }
 
   /*!
-  * \brief Function, which makes available the s-derivatives of the basis functions in the integration points.
-  * \return  The pointer to data, which stores the s-derivatives of the basis functions.
-  */
-  inline su2double* GetDsBasisFunctionsIntegration(void){return dsLagBasisIntegration.data();}
+   * \brief Function, which makes available the s-derivatives of the basis functions in the integration points.
+   * \return  The pointer to data, which stores the s-derivatives of the basis functions.
+   */
+  inline su2double* GetDsBasisFunctionsIntegration(void) { return dsLagBasisIntegration.data(); }
 
   /*!
-  * \brief Function, which makes available the t-derivatives of the basis functions in the integration points.
-  * \return  The pointer to data, which stores the t-derivatives of the basis functions.
-  */
-  inline su2double* GetDtBasisFunctionsIntegration(void){return dtLagBasisIntegration.data();}
+   * \brief Function, which makes available the t-derivatives of the basis functions in the integration points.
+   * \return  The pointer to data, which stores the t-derivatives of the basis functions.
+   */
+  inline su2double* GetDtBasisFunctionsIntegration(void) { return dtLagBasisIntegration.data(); }
 
   /*!
-  * \brief Function, which makes available the matrix storage of the inverse of Vandermonde matrix of solution DOFs.
-  * \return  The pointer to matVandermondeInv.
-  */
-  inline const su2double* GetMatVandermondeInv(void) const {return matVandermondeInv.data();}
+   * \brief Function, which makes available the matrix storage of the inverse of Vandermonde matrix of solution DOFs.
+   * \return  The pointer to matVandermondeInv.
+   */
+  inline const su2double* GetMatVandermondeInv(void) const { return matVandermondeInv.data(); }
 
   /*!
-  * \brief Function, which makes available the matrix storage of the basis functions in the integration points.
-  * \return  The pointer to matBasisIntegration.
-  */
-  inline const su2double* GetMatBasisFunctionsIntegration(void) const {return matBasisIntegration.data();}
+   * \brief Function, which makes available the matrix storage of the basis functions in the integration points.
+   * \return  The pointer to matBasisIntegration.
+   */
+  inline const su2double* GetMatBasisFunctionsIntegration(void) const { return matBasisIntegration.data(); }
 
   /*!
-  * \brief Function, which makes available the transpose matrix of the derivative of the basis functions in the integration points.
-  * \return  The pointer to matDerBasisIntTrans;
-  */
-  inline const su2double* GetDerMatBasisFunctionsIntTrans(void) const {return matDerBasisIntTrans.data();}
+   * \brief Function, which makes available the transpose matrix of the derivative of the basis functions in the
+   * integration points. \return  The pointer to matDerBasisIntTrans;
+   */
+  inline const su2double* GetDerMatBasisFunctionsIntTrans(void) const { return matDerBasisIntTrans.data(); }
 
   /*!
-  * \brief Function, which makes available the matrix storage of the derivative of the basis functions in the own DOFs.
-  * \return  The pointer to matDerBasisOwnDOFs.
-  */
-  inline const su2double *GetMatDerBasisFunctionsOwnDOFs(void) const {return matDerBasisOwnDOFs.data();}
+   * \brief Function, which makes available the matrix storage of the derivative of the basis functions in the own DOFs.
+   * \return  The pointer to matDerBasisOwnDOFs.
+   */
+  inline const su2double* GetMatDerBasisFunctionsOwnDOFs(void) const { return matDerBasisOwnDOFs.data(); }
 
   /*!
-  * \brief Function, which makes available the matrix storage of the derivative of the basis functions in the solution DOFs.
-  * \return  The pointer to matDerBasisSolDOFs.
-  */
-  inline const su2double *GetMatDerBasisFunctionsSolDOFs(void) const {return matDerBasisSolDOFs.data();}
+   * \brief Function, which makes available the matrix storage of the derivative of the basis functions in the solution
+   * DOFs. \return  The pointer to matDerBasisSolDOFs.
+   */
+  inline const su2double* GetMatDerBasisFunctionsSolDOFs(void) const { return matDerBasisSolDOFs.data(); }
 
   /*!
   * \brief Function, which makes available the matrix storage of the second derivativex of the basis functions
            in the integration points.
   * \return  The pointer to mat2ndDerBasisInt.
   */
-  inline const su2double *GetMat2ndDerBasisFunctionsInt(void) const {return mat2ndDerBasisInt.data();}
+  inline const su2double* GetMat2ndDerBasisFunctionsInt(void) const { return mat2ndDerBasisInt.data(); }
 
   /*!
-  * \brief Function, which makes available the connectivity of face 0.
-  * \return  The pointer to data, which stores the connectivity of face 0.
-  */
-  inline unsigned short *GetConnFace0(void) {return connFace0.data();}
+   * \brief Function, which makes available the connectivity of face 0.
+   * \return  The pointer to data, which stores the connectivity of face 0.
+   */
+  inline unsigned short* GetConnFace0(void) { return connFace0.data(); }
 
   /*!
-  * \brief Function, which makes available the connectivity of face 1.
-  * \return  The pointer to data, which stores the connectivity of face 1.
-  */
-  inline unsigned short *GetConnFace1(void) {return connFace1.data();}
+   * \brief Function, which makes available the connectivity of face 1.
+   * \return  The pointer to data, which stores the connectivity of face 1.
+   */
+  inline unsigned short* GetConnFace1(void) { return connFace1.data(); }
 
   /*!
-  * \brief Function, which makes available the connectivity of face 2.
-  * \return  The pointer to data, which stores the connectivity of face 2.
-  */
-  inline unsigned short *GetConnFace2(void) {return connFace2.data();}
+   * \brief Function, which makes available the connectivity of face 2.
+   * \return  The pointer to data, which stores the connectivity of face 2.
+   */
+  inline unsigned short* GetConnFace2(void) { return connFace2.data(); }
 
   /*!
-  * \brief Function, which makes available the connectivity of face 3.
-  * \return  The pointer to data, which stores the connectivity of face 3.
-  */
-  inline unsigned short *GetConnFace3(void) {return connFace3.data();}
+   * \brief Function, which makes available the connectivity of face 3.
+   * \return  The pointer to data, which stores the connectivity of face 3.
+   */
+  inline unsigned short* GetConnFace3(void) { return connFace3.data(); }
 
   /*!
-  * \brief Function, which makes available the connectivity of face 4.
-  * \return  The pointer to data, which stores the connectivity of face 4.
-  */
-  inline unsigned short *GetConnFace4(void) {return connFace4.data();}
+   * \brief Function, which makes available the connectivity of face 4.
+   * \return  The pointer to data, which stores the connectivity of face 4.
+   */
+  inline unsigned short* GetConnFace4(void) { return connFace4.data(); }
 
   /*!
-  * \brief Function, which makes available the connectivity of face 5.
-  * \return  The pointer to data, which stores the connectivity of face 5.
-  */
-  inline unsigned short *GetConnFace5(void) {return connFace5.data();}
+   * \brief Function, which makes available the connectivity of face 5.
+   * \return  The pointer to data, which stores the connectivity of face 5.
+   */
+  inline unsigned short* GetConnFace5(void) { return connFace5.data(); }
 
   /*!
-  * \brief Function, which makes available the number of DOFs for this standard element.
-  * \return  The number of DOFs of this standard element.
-  */
-  inline unsigned short GetNDOFs(void) const {return nDOFs;}
+   * \brief Function, which makes available the number of DOFs for this standard element.
+   * \return  The number of DOFs of this standard element.
+   */
+  inline unsigned short GetNDOFs(void) const { return nDOFs; }
 
   /*!
-  * \brief Function, which makes available the polynomial degree for this standard element.
-  * \return  The polynomial degree of this standard element.
-  */
-  inline unsigned short GetNPoly(void) const {return nPoly;}
+   * \brief Function, which makes available the polynomial degree for this standard element.
+   * \return  The polynomial degree of this standard element.
+   */
+  inline unsigned short GetNPoly(void) const { return nPoly; }
 
   /*!
    * \brief Function, which makes available the type of the element in subConn1ForPlotting.
    * \return  The type of the elements in subConn1ForPlotting using the VTK convention.
    */
-  inline unsigned short GetVTK_Type1(void) const {return VTK_Type1;}
+  inline unsigned short GetVTK_Type1(void) const { return VTK_Type1; }
 
   /*!
    * \brief Function, which makes available the number of sub-elements of type 1 for plotting.
    * \return  The number of sub-elements of type 1 for plotting.
    */
-  inline unsigned short GetNSubElemsType1(void) const {return subConn1ForPlotting.size()/GetNDOFsPerSubElem(GetVTK_Type1());}
+  inline unsigned short GetNSubElemsType1(void) const {
+    return subConn1ForPlotting.size() / GetNDOFsPerSubElem(GetVTK_Type1());
+  }
 
   /*!
    * \brief Function, which makes available the the connectivity of the linear elements of type 1 as a const pointer.
    * \return  The pointer to the local connectivity of the linear elements of type 1.
    */
-  inline const unsigned short *GetSubConnType1(void) const {return subConn1ForPlotting.data();}
+  inline const unsigned short* GetSubConnType1(void) const { return subConn1ForPlotting.data(); }
 
   /*!
    * \brief Function, which makes available the type of the element in subConn2ForPlotting.
    * \return  The type of the elements in subConn2ForPlotting using the VTK convention.
    */
-  inline unsigned short GetVTK_Type2(void) const {return VTK_Type2;}
+  inline unsigned short GetVTK_Type2(void) const { return VTK_Type2; }
 
   /*!
    * \brief Function, which makes available the number of sub-elements of type 2 for plotting.
    * \return  The number of sub-elements of type 2 for plotting.
    */
-  inline unsigned short GetNSubElemsType2(void) const {return subConn2ForPlotting.size()/GetNDOFsPerSubElem(GetVTK_Type2());}
+  inline unsigned short GetNSubElemsType2(void) const {
+    return subConn2ForPlotting.size() / GetNDOFsPerSubElem(GetVTK_Type2());
+  }
 
   /*!
    * \brief Function, which makes available the the connectivity of the linear elements of type 2 as a const pointer.
    * \return  The pointer to the local connectivity of the linear elements of type 2.
    */
-  inline const unsigned short *GetSubConnType2(void) const {return subConn2ForPlotting.data();}
+  inline const unsigned short* GetSubConnType2(void) const { return subConn2ForPlotting.data(); }
 
   /*!
    * \brief Function, which makes available the number of DOFs of a linear element, used for plotting.
@@ -1069,41 +960,39 @@ class CFEMStandardElement : public CFEMStandardElementBase {
             const pointer to the vector.
    * \return  The address of the vector, which stores the r-location of the DOFs.
    */
-  inline const vector<su2double> *GetRDOFs(void) const {return &rDOFs;}
+  inline const vector<su2double>* GetRDOFs(void) const { return &rDOFs; }
 
   /*!
    * \brief Function, which makes available the s-location of the DOFs as a
             const pointer to the vector.
    * \return  The address of the vector, which stores the s-location of the DOFs.
    */
-  inline const vector<su2double> *GetSDOFs(void) const {return &sDOFs;}
+  inline const vector<su2double>* GetSDOFs(void) const { return &sDOFs; }
 
   /*!
    * \brief Function, which makes available the t-location of the DOFs as a
             const pointer to the vector.
    * \return  The address of the vector, which stores the t-location of the DOFs.
    */
-  inline const vector<su2double> *GetTDOFs(void) const {return &tDOFs;}
+  inline const vector<su2double>* GetTDOFs(void) const { return &tDOFs; }
 
   /*!
-  * \brief Function, which checks if the function arguments correspond to this standard element.
-  * \param[in] val_VTK_Type - Type of the element using the VTK convention.
-  * \param[in] val_nPoly    - Polynomial degree of the element.
-  * \param[in] val_constJac - Whether or not the Jacobians are constant.
-  * \return Whether or not the function arguments correspond to this standard element.
-  */
-  bool SameStandardElement(unsigned short val_VTK_Type,
-                           unsigned short val_nPoly,
-                           bool           val_constJac);
+   * \brief Function, which checks if the function arguments correspond to this standard element.
+   * \param[in] val_VTK_Type - Type of the element using the VTK convention.
+   * \param[in] val_nPoly    - Polynomial degree of the element.
+   * \param[in] val_constJac - Whether or not the Jacobians are constant.
+   * \return Whether or not the function arguments correspond to this standard element.
+   */
+  bool SameStandardElement(unsigned short val_VTK_Type, unsigned short val_nPoly, bool val_constJac);
 
   /*!
   * \brief Function, which estimates the amount of work for an element of this
            type. This information is used to determine a well balanced partition.
   * \param[in] config - Object, which contains the input parameters.
   */
-  su2double WorkEstimateMetis(CConfig *config);
+  su2double WorkEstimateMetis(CConfig* config);
 
-private:
+ private:
   /*!
   * \brief Function, which changes the given quadrilateral connectivity, such that the direction coincides
            with the direction corresponding to corner vertices vert0, vert1, vert2, vert3.
@@ -1113,11 +1002,8 @@ class CFEMStandardElement : public CFEMStandardElementBase {
   * \param[in]     vert2    - Corner vertex 2 of the desired sequence.
   * \param[in]     vert3    - Corner vertex 3 of the desired sequence.
   */
-  void ChangeDirectionQuadConn(vector<unsigned short> &connQuad,
-                               unsigned short         vert0,
-                               unsigned short         vert1,
-                               unsigned short         vert2,
-                               unsigned short         vert3) const;
+  void ChangeDirectionQuadConn(vector<unsigned short>& connQuad, unsigned short vert0, unsigned short vert1,
+                               unsigned short vert2, unsigned short vert3) const;
 
   /*!
   * \brief Function, which changes the given triangular connectivity, such that the direction coincides
@@ -1127,16 +1013,14 @@ class CFEMStandardElement : public CFEMStandardElementBase {
   * \param[in]     vert1        - Corner vertex 1 of the desired sequence.
   * \param[in]     vert2        - Corner vertex 2 of the desired sequence.
   */
-  void ChangeDirectionTriangleConn(vector<unsigned short> &connTriangle,
-                                   unsigned short         vert0,
-                                   unsigned short         vert1,
-                                   unsigned short         vert2) const;
+  void ChangeDirectionTriangleConn(vector<unsigned short>& connTriangle, unsigned short vert0, unsigned short vert1,
+                                   unsigned short vert2) const;
 
   /*!
-  * \brief Function, which copies the data of the given object into the current object.
-  * \param[in] other - Object, whose data is copied.
-  */
-  void Copy(const CFEMStandardElement &other);
+   * \brief Function, which copies the data of the given object into the current object.
+   * \param[in] other - Object, whose data is copied.
+   */
+  void Copy(const CFEMStandardElement& other);
 
   /*!
   * \brief Function, which creates the basis functions and the matrix containing
@@ -1150,45 +1034,42 @@ class CFEMStandardElement : public CFEMStandardElementBase {
   * \param[out] matDerBasis  - Matrix to store the derivatives of the basis
                                functions.
   */
-  void CreateBasisFunctionsAndMatrixDerivatives(const vector<su2double> &rLoc,
-                                                const vector<su2double> &sLoc,
-                                                const vector<su2double> &tLoc,
-                                                      vector<su2double> &matVandermondeInv,
-                                                      vector<su2double> &lagBasis,
-                                                      vector<su2double> &matDerBasis);
+  void CreateBasisFunctionsAndMatrixDerivatives(const vector<su2double>& rLoc, const vector<su2double>& sLoc,
+                                                const vector<su2double>& tLoc, vector<su2double>& matVandermondeInv,
+                                                vector<su2double>& lagBasis, vector<su2double>& matDerBasis);
   /*!
-  * \brief Function, which creates all the data for a line element.
-  */
+   * \brief Function, which creates all the data for a line element.
+   */
   void DataStandardLine(void);
 
   /*!
-  * \brief Function, which creates all the data for a triangular element.
-  */
+   * \brief Function, which creates all the data for a triangular element.
+   */
   void DataStandardTriangle(void);
 
   /*!
-  * \brief Function, which creates all the data for a quadrilateral element.
-  */
+   * \brief Function, which creates all the data for a quadrilateral element.
+   */
   void DataStandardQuadrilateral(void);
 
   /*!
-  * \brief Function, which creates all the data for a tetrahedral element.
-  */
+   * \brief Function, which creates all the data for a tetrahedral element.
+   */
   void DataStandardTetrahedron(void);
 
   /*!
-  * \brief Function, which creates all the data for a pyramid element.
-  */
+   * \brief Function, which creates all the data for a pyramid element.
+   */
   void DataStandardPyramid(void);
 
   /*!
-  * \brief Function, which creates all the data for a prism element.
-  */
+   * \brief Function, which creates all the data for a prism element.
+   */
   void DataStandardPrism(void);
 
   /*!
-  * \brief Function, which creates all the data for a hexahedral element.
-  */
+   * \brief Function, which creates all the data for a hexahedral element.
+   */
   void DataStandardHexahedron(void);
 
   /*!
@@ -1223,9 +1104,9 @@ class CFEMStandardElement : public CFEMStandardElementBase {
  * \version 7.5.1 "Blackbird"
  */
 class CFEMStandardInternalFace : public CFEMStandardElementBase {
-private:
-  unsigned short nDOFsFaceSide0;    /*!< \brief Number of DOFs on side 0 of the face. */
-  unsigned short nDOFsFaceSide1;    /*!< \brief Number of DOFs on side 1 of the face. */
+ private:
+  unsigned short nDOFsFaceSide0; /*!< \brief Number of DOFs on side 0 of the face. */
+  unsigned short nDOFsFaceSide1; /*!< \brief Number of DOFs on side 1 of the face. */
 
   unsigned short nPolyElemSide0;    /*!< \brief Polynomial degree of the element on side 0 of the face. */
   unsigned short nPolyElemSide1;    /*!< \brief Polynomial degree of the element on side 1 of the face. */
@@ -1234,20 +1115,20 @@ class CFEMStandardInternalFace : public CFEMStandardElementBase {
   unsigned short VTK_TypeElemSide0; /*!< \brief Type of the element on side 0 of the face using the VTK convention. */
   unsigned short VTK_TypeElemSide1; /*!< \brief Type of the element on side 1 of the face using the VTK convention. */
 
-  bool swapFaceInElementSide0;      /*!< \brief Whether or not the connectivity of the face must
-                                                be swapped compared to the face of the corresponding
-                                                standard element on side 0 of the face. */
-  bool swapFaceInElementSide1;      /*!< \brief Whether or not the connectivity of the face must
-                                                be swapped compared to the face of the corresponding
-                                                standard element on side 1 of the face. */
+  bool swapFaceInElementSide0; /*!< \brief Whether or not the connectivity of the face must
+                                           be swapped compared to the face of the corresponding
+                                           standard element on side 0 of the face. */
+  bool swapFaceInElementSide1; /*!< \brief Whether or not the connectivity of the face must
+                                           be swapped compared to the face of the corresponding
+                                           standard element on side 1 of the face. */
 
-  su2double penaltyConstantFace;      /*!< \brief The constant of the penalty parameter of the face,
-                                                  which is used in the viscous discretization. */
+  su2double penaltyConstantFace; /*!< \brief The constant of the penalty parameter of the face,
+                                             which is used in the viscous discretization. */
 
-  vector<su2double> rDOFsFaceSide0;   /*!< \brief r-location of the DOFs on side 0 of the face. */
-  vector<su2double> rDOFsFaceSide1;   /*!< \brief r-location of the DOFs on side 1 of the face. */
-  vector<su2double> sDOFsFaceSide0;   /*!< \brief s-location of the DOFs on side 0 of the face, if needed. */
-  vector<su2double> sDOFsFaceSide1;   /*!< \brief s-location of the DOFs on side 1 of the face, if needed. */
+  vector<su2double> rDOFsFaceSide0; /*!< \brief r-location of the DOFs on side 0 of the face. */
+  vector<su2double> rDOFsFaceSide1; /*!< \brief r-location of the DOFs on side 1 of the face. */
+  vector<su2double> sDOFsFaceSide0; /*!< \brief s-location of the DOFs on side 0 of the face, if needed. */
+  vector<su2double> sDOFsFaceSide1; /*!< \brief s-location of the DOFs on side 1 of the face, if needed. */
 
   vector<su2double> lagBasisFaceIntegrationSide0; /*!< \brief Lagrangian basis functions in the integration points
                                                               of side0 of the face. */
@@ -1279,20 +1160,22 @@ class CFEMStandardInternalFace : public CFEMStandardElementBase {
   vector<su2double> dtLagBasisElemIntegrationSide1; /*!< \brief t-derivatives of the element Lagrangian basis functions
                                                                 of side 1 in the integration points. */
 
-  vector<su2double> matDerBasisElemIntegrationSide0;       /*!< \brief Matrix of drLagBasisElemIntegrationSide0, dsLagBasisElemIntegrationSide0
-                                                                       and dtLagBasisElemIntegrationSide0 combined for efficiency
-                                                                       when using BLAS routines. */
-  vector<su2double> matDerBasisElemIntegrationSide1;       /*!< \brief Matrix of drLagBasisElemIntegrationSide1, dsLagBasisElemIntegrationSide1
-                                                                       and dtLagBasisElemIntegrationSide1 combined for efficiency
-                                                                       when using BLAS routines. */
-
-  vector<su2double> matDerBasisElemIntegrationTransposeSide0; /*!< \brief Transpose of matDerBasisElemIntegrationSide0, such that
-                                                                          the residuals of the symmetrizing terms can be computed
-                                                                          with a single matrix multiplication. */
-  vector<su2double> matDerBasisElemIntegrationTransposeSide1; /*!< \brief Transpose of matDerBasisElemIntegrationSide1, such that
-                                                                          the residuals of the symmetrizing terms can be computed
-                                                                          with a single matrix multiplication. */
-public:
+  vector<su2double>
+      matDerBasisElemIntegrationSide0; /*!< \brief Matrix of drLagBasisElemIntegrationSide0,
+                                          dsLagBasisElemIntegrationSide0 and dtLagBasisElemIntegrationSide0 combined for
+                                          efficiency when using BLAS routines. */
+  vector<su2double>
+      matDerBasisElemIntegrationSide1; /*!< \brief Matrix of drLagBasisElemIntegrationSide1,
+                                          dsLagBasisElemIntegrationSide1 and dtLagBasisElemIntegrationSide1 combined for
+                                          efficiency when using BLAS routines. */
+
+  vector<su2double> matDerBasisElemIntegrationTransposeSide0; /*!< \brief Transpose of matDerBasisElemIntegrationSide0,
+                                                                 such that the residuals of the symmetrizing terms can
+                                                                 be computed with a single matrix multiplication. */
+  vector<su2double> matDerBasisElemIntegrationTransposeSide1; /*!< \brief Transpose of matDerBasisElemIntegrationSide1,
+                                                                 such that the residuals of the symmetrizing terms can
+                                                                 be computed with a single matrix multiplication. */
+ public:
   /*!
   * \brief Alternative constructor.
   * \param[in] val_VTK_TypeFace            - The type of the face using the VTK convention.
@@ -1316,84 +1199,85 @@ class CFEMStandardInternalFace : public CFEMStandardElementBase {
                                              order of the polynomials that must be integrated
                                              exactly by the integration rule.
   */
-  CFEMStandardInternalFace(unsigned short val_VTK_TypeFace,
-                           unsigned short val_VTK_TypeSide0,
-                           unsigned short val_nPolySide0,
-                           unsigned short val_VTK_TypeSide1,
-                           unsigned short val_nPolySide1,
-                           bool           val_constJac,
-                           bool           val_swapFaceInElementSide0,
-                           bool           val_swapFaceInElementSide1,
-                           CConfig        *config,
-                           unsigned short val_orderExact = 0);
+  CFEMStandardInternalFace(unsigned short val_VTK_TypeFace, unsigned short val_VTK_TypeSide0,
+                           unsigned short val_nPolySide0, unsigned short val_VTK_TypeSide1,
+                           unsigned short val_nPolySide1, bool val_constJac, bool val_swapFaceInElementSide0,
+                           bool val_swapFaceInElementSide1, CConfig* config, unsigned short val_orderExact = 0);
   /*!
-  * \brief Copy constructor.
-  * \param[in] other - Object, whose data must be copied.
-  */
-  CFEMStandardInternalFace(const CFEMStandardInternalFace &other) : CFEMStandardElementBase(other) {Copy(other);}
+   * \brief Copy constructor.
+   * \param[in] other - Object, whose data must be copied.
+   */
+  CFEMStandardInternalFace(const CFEMStandardInternalFace& other) : CFEMStandardElementBase(other) { Copy(other); }
 
   /*!
-  * \brief Assignment operator.
-  * \param[in] other - Object, to which this object must be assigned.
-  * \return The current object, after the member variables were assigned the correct value.
-  */
-  CFEMStandardInternalFace& operator=(const CFEMStandardInternalFace &other){Copy(other); return (*this);}
+   * \brief Assignment operator.
+   * \param[in] other - Object, to which this object must be assigned.
+   * \return The current object, after the member variables were assigned the correct value.
+   */
+  CFEMStandardInternalFace& operator=(const CFEMStandardInternalFace& other) {
+    Copy(other);
+    return (*this);
+  }
 
   /*!
   * \brief Function, which makes available the r-derivatives of the elements
            basis functions of side 0 in the integration points.
   * \return  The pointer to data, which stores this information.
   */
-  inline su2double *GetDrBasisElemIntegrationSide0(void) {return drLagBasisElemIntegrationSide0.data();}
+  inline su2double* GetDrBasisElemIntegrationSide0(void) { return drLagBasisElemIntegrationSide0.data(); }
 
   /*!
   * \brief Function, which makes available the r-derivatives of the elements
            basis functions of side 1 in the integration points.
   * \return  The pointer to data, which stores this information.
   */
-  inline su2double *GetDrBasisElemIntegrationSide1(void) {return drLagBasisElemIntegrationSide1.data();}
+  inline su2double* GetDrBasisElemIntegrationSide1(void) { return drLagBasisElemIntegrationSide1.data(); }
 
   /*!
   * \brief Function, which makes available the s-derivatives of the elements
            basis functions of side 0 in the integration points.
   * \return  The pointer to data, which stores this information.
   */
-  inline su2double *GetDsBasisElemIntegrationSide0(void) {return dsLagBasisElemIntegrationSide0.data();}
+  inline su2double* GetDsBasisElemIntegrationSide0(void) { return dsLagBasisElemIntegrationSide0.data(); }
 
   /*!
   * \brief Function, which makes available the s-derivatives of the elements
            basis functions of side 1 in the integration points.
   * \return  The pointer to data, which stores this information.
   */
-  inline su2double *GetDsBasisElemIntegrationSide1(void) {return dsLagBasisElemIntegrationSide1.data();}
+  inline su2double* GetDsBasisElemIntegrationSide1(void) { return dsLagBasisElemIntegrationSide1.data(); }
 
   /*!
   * \brief Function, which makes available the t-derivatives of the elements
            basis functions of side 0 in the integration points.
   * \return  The pointer to data, which stores this information.
   */
-  inline su2double *GetDtBasisElemIntegrationSide0(void) {return dtLagBasisElemIntegrationSide0.data();}
+  inline su2double* GetDtBasisElemIntegrationSide0(void) { return dtLagBasisElemIntegrationSide0.data(); }
 
   /*!
   * \brief Function, which makes available the t-derivatives of the elements
            basis functions of side 1 in the integration points.
   * \return  The pointer to data, which stores this information.
   */
-  inline su2double *GetDtBasisElemIntegrationSide1(void) {return dtLagBasisElemIntegrationSide1.data();}
+  inline su2double* GetDtBasisElemIntegrationSide1(void) { return dtLagBasisElemIntegrationSide1.data(); }
 
   /*!
   * \brief Function, which makes available the matrix with the derivatives of
            the element basis functions of side 0 in the integration points.
   * \return  The const pointer to data, which stores this information.
   */
-  inline const su2double* GetMatDerBasisElemIntegrationSide0(void) const {return matDerBasisElemIntegrationSide0.data();}
+  inline const su2double* GetMatDerBasisElemIntegrationSide0(void) const {
+    return matDerBasisElemIntegrationSide0.data();
+  }
 
   /*!
   * \brief Function, which makes available the matrix with the derivatives of
            the element basis functions of side 1 in the integration points.
   * \return  The const pointer to data, which stores this information.
   */
-  inline const su2double* GetMatDerBasisElemIntegrationSide1(void) const {return matDerBasisElemIntegrationSide1.data();}
+  inline const su2double* GetMatDerBasisElemIntegrationSide1(void) const {
+    return matDerBasisElemIntegrationSide1.data();
+  }
 
   /*!
   * \brief Function, which makes available the transpose of the matrix with
@@ -1401,7 +1285,9 @@ class CFEMStandardInternalFace : public CFEMStandardElementBase {
            integration points.
   * \return  The const pointer to data, which stores this information.
   */
-  inline const su2double* GetMatDerBasisElemIntegrationTransposeSide0(void) const {return matDerBasisElemIntegrationTransposeSide0.data();}
+  inline const su2double* GetMatDerBasisElemIntegrationTransposeSide0(void) const {
+    return matDerBasisElemIntegrationTransposeSide0.data();
+  }
 
   /*!
   * \brief Function, which makes available the transpose of the matrix with
@@ -1409,95 +1295,101 @@ class CFEMStandardInternalFace : public CFEMStandardElementBase {
            integration points.
   * \return  The const pointer to data, which stores this information.
   */
-  inline const su2double* GetMatDerBasisElemIntegrationTransposeSide1(void) const {return matDerBasisElemIntegrationTransposeSide1.data();}
+  inline const su2double* GetMatDerBasisElemIntegrationTransposeSide1(void) const {
+    return matDerBasisElemIntegrationTransposeSide1.data();
+  }
 
   /*!
   * \brief Function, which makes available the face basis functions of side 0
            in the integration points.
   * \return  The pointer to data, which stores this information.
   */
-  inline const su2double* GetBasisFaceIntegrationSide0(void) const {return lagBasisFaceIntegrationSide0.data();}
+  inline const su2double* GetBasisFaceIntegrationSide0(void) const { return lagBasisFaceIntegrationSide0.data(); }
 
   /*!
   * \brief Function, which makes available the face basis functions of side 1
            in the integration points.
   * \return  The pointer to data, which stores this information.
   */
-  inline const su2double* GetBasisFaceIntegrationSide1(void) const {return lagBasisFaceIntegrationSide1.data();}
+  inline const su2double* GetBasisFaceIntegrationSide1(void) const { return lagBasisFaceIntegrationSide1.data(); }
 
   /*!
   * \brief Function, which makes available transpose matrix of the face basis
            functions of side 0 in the integration points.
   * \return  The pointer to data, which stores this information.
   */
-  inline const su2double* GetBasisFaceIntegrationTransposeSide0(void) const {return lagBasisFaceIntegrationTransposeSide0.data();}
+  inline const su2double* GetBasisFaceIntegrationTransposeSide0(void) const {
+    return lagBasisFaceIntegrationTransposeSide0.data();
+  }
 
   /*!
   * \brief Function, which makes available transpose matrix of the face basis
            functions of side 1 in the integration points.
   * \return  The pointer to data, which stores this information.
   */
-  inline const su2double* GetBasisFaceIntegrationTransposeSide1(void) const {return lagBasisFaceIntegrationTransposeSide1.data();}
+  inline const su2double* GetBasisFaceIntegrationTransposeSide1(void) const {
+    return lagBasisFaceIntegrationTransposeSide1.data();
+  }
 
   /*!
   * \brief Function, which makes available the r-derivatives of the face basis
            functions of side 0 in the integration points.
   * \return  The pointer to data, which stores this information.
   */
-  inline su2double* GetDrBasisFaceIntegrationSide0(void) {return drLagBasisFaceIntegrationSide0.data();}
+  inline su2double* GetDrBasisFaceIntegrationSide0(void) { return drLagBasisFaceIntegrationSide0.data(); }
 
   /*!
   * \brief Function, which makes available the r-derivatives of the face basis
            functions of side 1 in the integration points.
   * \return  The pointer to data, which stores this information.
   */
-  inline su2double* GetDrBasisFaceIntegrationSide1(void) {return drLagBasisFaceIntegrationSide1.data();}
+  inline su2double* GetDrBasisFaceIntegrationSide1(void) { return drLagBasisFaceIntegrationSide1.data(); }
 
   /*!
   * \brief Function, which makes available the s-derivatives of the face basis
            functions of side 0 in the integration points.
   * \return  The pointer to data, which stores this information.
   */
-  inline su2double* GetDsBasisFaceIntegrationSide0(void) {return dsLagBasisFaceIntegrationSide0.data();}
+  inline su2double* GetDsBasisFaceIntegrationSide0(void) { return dsLagBasisFaceIntegrationSide0.data(); }
 
   /*!
   * \brief Function, which makes available the s-derivatives of the face basis
            functions of side 1 in the integration points.
   * \return  The pointer to data, which stores this information.
   */
-  inline su2double* GetDsBasisFaceIntegrationSide1(void) {return dsLagBasisFaceIntegrationSide1.data();}
+  inline su2double* GetDsBasisFaceIntegrationSide1(void) { return dsLagBasisFaceIntegrationSide1.data(); }
 
   /*!
   * \brief Function, which makes available the number of DOFs of the element
            on side 0 of the face.
   * \return  The number of DOFs of the element on side 0.
   */
-  inline unsigned short GetNDOFsElemSide0(void) const {return nDOFsElemSide0;}
+  inline unsigned short GetNDOFsElemSide0(void) const { return nDOFsElemSide0; }
 
   /*!
   * \brief Function, which makes available the number of DOFs of the element
            on side 1 of the face.
   * \return  The number of DOFs on side 1.
   */
-  inline unsigned short GetNDOFsElemSide1(void) const {return nDOFsElemSide1;}
+  inline unsigned short GetNDOFsElemSide1(void) const { return nDOFsElemSide1; }
 
   /*!
-  * \brief Function, which makes available the number of DOFs on side 0 of the face.
-  * \return  The number of DOFs on side 0.
-  */
-  inline unsigned short GetNDOFsFaceSide0(void) const {return nDOFsFaceSide0;}
+   * \brief Function, which makes available the number of DOFs on side 0 of the face.
+   * \return  The number of DOFs on side 0.
+   */
+  inline unsigned short GetNDOFsFaceSide0(void) const { return nDOFsFaceSide0; }
 
   /*!
-  * \brief Function, which makes available the number of DOFs on side 1 of the face.
-  * \return  The number of DOFs on side 1.
-  */
-  inline unsigned short GetNDOFsFaceSide1(void) const {return nDOFsFaceSide1;}
+   * \brief Function, which makes available the number of DOFs on side 1 of the face.
+   * \return  The number of DOFs on side 1.
+   */
+  inline unsigned short GetNDOFsFaceSide1(void) const { return nDOFsFaceSide1; }
 
   /*!
-  * \brief Function, which makes available the penalty constant for this standard face.
-  * \return  The penalty constant.
-  */
-  inline su2double GetPenaltyConstant(void) const {return penaltyConstantFace;}
+   * \brief Function, which makes available the penalty constant for this standard face.
+   * \return  The penalty constant.
+   */
+  inline su2double GetPenaltyConstant(void) const { return penaltyConstantFace; }
 
   /*!
   * \brief Function, which checks if the function arguments correspond to this standard face.
@@ -1518,28 +1410,24 @@ class CFEMStandardInternalFace : public CFEMStandardElementBase {
                                             be swapped w.r.t. the connectivity of face of the
                                             element on side 1.
   */
-  bool SameStandardMatchingFace(unsigned short val_VTK_TypeFace,
-                                bool           val_constJac,
-                                unsigned short val_VTK_TypeSide0,
-                                unsigned short val_nPolySide0,
-                                unsigned short val_VTK_TypeSide1,
-                                unsigned short val_nPolySide1,
-                                bool           val_swapFaceInElementSide0,
-                                bool           val_swapFaceInElementSide1);
+  bool SameStandardMatchingFace(unsigned short val_VTK_TypeFace, bool val_constJac, unsigned short val_VTK_TypeSide0,
+                                unsigned short val_nPolySide0, unsigned short val_VTK_TypeSide1,
+                                unsigned short val_nPolySide1, bool val_swapFaceInElementSide0,
+                                bool val_swapFaceInElementSide1);
 
   /*!
   * \brief Function, which estimates the amount of work for an element of this
            type. This information is used to determine a well balanced partition.
   * \param[in] config - Object, which contains the input parameters.
   */
-  su2double WorkEstimateMetis(CConfig *config);
+  su2double WorkEstimateMetis(CConfig* config);
 
-private:
+ private:
   /*!
-  * \brief Function, which copies the data of the given object into the current object.
-  * \param[in] other - Object, whose data is copied.
-  */
-  void Copy(const CFEMStandardInternalFace &other);
+   * \brief Function, which copies the data of the given object into the current object.
+   * \param[in] other - Object, whose data is copied.
+   */
+  void Copy(const CFEMStandardInternalFace& other);
 };
 
 /*!
@@ -1549,21 +1437,21 @@ class CFEMStandardInternalFace : public CFEMStandardElementBase {
  * \version 7.5.1 "Blackbird"
  */
 class CFEMStandardBoundaryFace : public CFEMStandardElementBase {
-private:
-  unsigned short nDOFsFace;    /*!< \brief Number of DOFs of the face. */
+ private:
+  unsigned short nDOFsFace; /*!< \brief Number of DOFs of the face. */
 
   unsigned short nPolyElem;    /*!< \brief Polynomial degree of the element adjacent to the face. */
   unsigned short nDOFsElem;    /*!< \brief Number of DOFs of the element adjacent element to the face. */
   unsigned short VTK_TypeElem; /*!< \brief Type of the element adjacent to the face using the VTK convention. */
 
-  bool swapFaceInElement;      /*!< \brief Whether or not the connectivity of the face must be swapped compared
-                                           to the face of the corresponding standard element adjacent to the face. */
+  bool swapFaceInElement; /*!< \brief Whether or not the connectivity of the face must be swapped compared
+                                      to the face of the corresponding standard element adjacent to the face. */
 
-  su2double penaltyConstantFace;  /*!< \brief The constant of the penalty parameter of the face,
-                                              which is used in the viscous discretization. */
+  su2double penaltyConstantFace; /*!< \brief The constant of the penalty parameter of the face,
+                                             which is used in the viscous discretization. */
 
-  vector<su2double> rDOFsFace;   /*!< \brief r-location of the DOFs of the face. */
-  vector<su2double> sDOFsFace;   /*!< \brief s-location of the DOFs of the face, if needed. */
+  vector<su2double> rDOFsFace; /*!< \brief r-location of the DOFs of the face. */
+  vector<su2double> sDOFsFace; /*!< \brief s-location of the DOFs of the face, if needed. */
 
   vector<su2double> lagBasisFaceIntegration;          /*!< \brief Lagrangian basis functions in the integration
                                                                   points of the face. */
@@ -1581,18 +1469,17 @@ class CFEMStandardBoundaryFace : public CFEMStandardElementBase {
   vector<su2double> dtLagBasisElemIntegration; /*!< \brief t-derivatives of the Lagrangian basis functions in the
                                                            integration points of the element adjacent to the face. */
 
-  vector<su2double> matDerBasisElemIntegration;       /*!< \brief Matrix of drLagBasisElemIntegration, dsLagBasisElemIntegration
-                                                                  and dtLagBasisElemIntegration combined for efficiency
-                                                                  when using BLAS routines. */
+  vector<su2double> matDerBasisElemIntegration; /*!< \brief Matrix of drLagBasisElemIntegration,
+                                                   dsLagBasisElemIntegration and dtLagBasisElemIntegration combined for
+                                                   efficiency when using BLAS routines. */
 
   vector<su2double> matDerBasisElemIntegrationTranspose; /*!< \brief Transpose of matDerBasisElemIntegration, such that
-                                                                     the residuals of the symmetrizing terms can be computed
-                                                                     with a single matrix multiplication. */
-
+                                                                     the residuals of the symmetrizing terms can be
+                                                            computed with a single matrix multiplication. */
 
   vector<unsigned short> subConnForPlotting; /*!< \brief Local subconnectivity of the high order element.
                                                          Used for plotting. */
-public:
+ public:
   /*!
   * \brief Alternative constructor.
   * \param[in] val_VTK_TypeFace       - The type of the face using the VTK convention.
@@ -1605,54 +1492,53 @@ class CFEMStandardBoundaryFace : public CFEMStandardElementBase {
   * \param[in] val_orderExact         - Default argument. If specified, it contains the order of the
                                         polynomials that must be integrated exactly by the integration rule.
   */
-  CFEMStandardBoundaryFace(unsigned short val_VTK_TypeFace,
-                           unsigned short val_VTK_TypeElem,
-                           unsigned short val_nPolyElem,
-                           bool           val_constJac,
-                           bool           val_swapFaceInElement,
-                           CConfig        *config,
+  CFEMStandardBoundaryFace(unsigned short val_VTK_TypeFace, unsigned short val_VTK_TypeElem,
+                           unsigned short val_nPolyElem, bool val_constJac, bool val_swapFaceInElement, CConfig* config,
                            unsigned short val_orderExact = 0);
 
   /*!
-  * \brief Copy constructor.
-  * \param[in] other - Object, whose data must be copied.
-  */
-  CFEMStandardBoundaryFace(const CFEMStandardBoundaryFace &other) : CFEMStandardElementBase(other) {Copy(other);}
+   * \brief Copy constructor.
+   * \param[in] other - Object, whose data must be copied.
+   */
+  CFEMStandardBoundaryFace(const CFEMStandardBoundaryFace& other) : CFEMStandardElementBase(other) { Copy(other); }
 
   /*!
-  * \brief Assignment operator.
-  * \param[in] other - Object, to which this object must be assigned.
-  * \return The current object, after the member variables were assigned the correct value.
-  */
-  CFEMStandardBoundaryFace& operator=(const CFEMStandardBoundaryFace &other){Copy(other); return (*this);}
+   * \brief Assignment operator.
+   * \param[in] other - Object, to which this object must be assigned.
+   * \return The current object, after the member variables were assigned the correct value.
+   */
+  CFEMStandardBoundaryFace& operator=(const CFEMStandardBoundaryFace& other) {
+    Copy(other);
+    return (*this);
+  }
 
   /*!
   * \brief Function, which makes available the r-derivatives of the element
            basis functions in the integration points.
   * \return  The pointer to data, which stores this information.
   */
-  inline const su2double* GetDrBasisElemIntegration(void) const {return drLagBasisElemIntegration.data();}
+  inline const su2double* GetDrBasisElemIntegration(void) const { return drLagBasisElemIntegration.data(); }
 
   /*!
   * \brief Function, which makes available the s-derivatives of the element
            basis functions in the integration points.
   * \return  The pointer to data, which stores this information.
   */
-  inline const su2double* GetDsBasisElemIntegration(void) const {return dsLagBasisElemIntegration.data();}
+  inline const su2double* GetDsBasisElemIntegration(void) const { return dsLagBasisElemIntegration.data(); }
 
   /*!
   * \brief Function, which makes available the t-derivatives of the element
            basis functions in the integration points.
   * \return  The pointer to data, which stores this information.
   */
-  inline const su2double* GetDtBasisElemIntegration(void) const {return dtLagBasisElemIntegration.data();}
+  inline const su2double* GetDtBasisElemIntegration(void) const { return dtLagBasisElemIntegration.data(); }
 
   /*!
   * \brief Function, which makes available the matrix with the derivatives of
            the element basis functions in the integration points.
   * \return  The pointer to data, which stores this information.
   */
-  inline const su2double* GetMatDerBasisElemIntegration(void) const {return matDerBasisElemIntegration.data();}
+  inline const su2double* GetMatDerBasisElemIntegration(void) const { return matDerBasisElemIntegration.data(); }
 
   /*!
   * \brief Function, which makes available the transpose of the matrix with
@@ -1660,55 +1546,59 @@ class CFEMStandardBoundaryFace : public CFEMStandardElementBase {
            points.
   * \return  The const pointer to data, which stores this information.
   */
-  inline const su2double* GetMatDerBasisElemIntegrationTranspose(void) const {return matDerBasisElemIntegrationTranspose.data();}
+  inline const su2double* GetMatDerBasisElemIntegrationTranspose(void) const {
+    return matDerBasisElemIntegrationTranspose.data();
+  }
 
   /*!
   * \brief Function, which makes available the face basis functions in the
            integration points.
   * \return  The pointer to data, which stores this information.
   */
-  inline const su2double* GetBasisFaceIntegration(void) const {return lagBasisFaceIntegration.data();}
+  inline const su2double* GetBasisFaceIntegration(void) const { return lagBasisFaceIntegration.data(); }
 
   /*!
   * \brief Function, which makes available transpose matrix of the face basis
            functions in the integration points.
   * \return  The pointer to data, which stores this information.
   */
-  inline const su2double* GetBasisFaceIntegrationTranspose(void) const {return lagBasisFaceIntegrationTranspose.data();}
+  inline const su2double* GetBasisFaceIntegrationTranspose(void) const {
+    return lagBasisFaceIntegrationTranspose.data();
+  }
 
   /*!
   * \brief Function, which makes available the r-derivatives of the face basis
            functions in the integration points.
   * \return  The pointer to data, which stores this information.
   */
-  inline const su2double* GetDrBasisFaceIntegration(void) const {return drLagBasisFaceIntegration.data();}
+  inline const su2double* GetDrBasisFaceIntegration(void) const { return drLagBasisFaceIntegration.data(); }
 
   /*!
   * \brief Function, which makes available the s-derivatives of the face basis
            functions in the integration points.
   * \return  The pointer to data, which stores this information.
   */
-  inline const su2double* GetDsBasisFaceIntegration(void) const {return dsLagBasisFaceIntegration.data();}
+  inline const su2double* GetDsBasisFaceIntegration(void) const { return dsLagBasisFaceIntegration.data(); }
 
   /*!
   * \brief Function, which makes available the number of DOFs of the
            adjacent element.
   * \return  The number of DOFs of the element.
   */
-  inline unsigned short GetNDOFsElem(void) const {return nDOFsElem;}
+  inline unsigned short GetNDOFsElem(void) const { return nDOFsElem; }
 
   /*!
-  * \brief Function, which makes available the number of DOFs of the face.
-  * \return  The number of DOFs of the face.
-  */
-  inline unsigned short GetNDOFsFace(void) const {return nDOFsFace;}
+   * \brief Function, which makes available the number of DOFs of the face.
+   * \return  The number of DOFs of the face.
+   */
+  inline unsigned short GetNDOFsFace(void) const { return nDOFsFace; }
 
   /*!
   * \brief Function, which makes available the number of linear subfaces used
            for plotting, among others.
   * \return  The number of linear subfaces of the face.
   */
-  inline unsigned short GetNSubFaces(void) const {return subConnForPlotting.size()/GetNDOFsPerSubFace();}
+  inline unsigned short GetNSubFaces(void) const { return subConnForPlotting.size() / GetNDOFsPerSubFace(); }
 
   /*!
   * \brief Function, which makes available the number of DOFs of a linear subface, used
@@ -1718,17 +1608,17 @@ class CFEMStandardBoundaryFace : public CFEMStandardElementBase {
   unsigned short GetNDOFsPerSubFace(void) const;
 
   /*!
-  * \brief Function, which makes available the penalty constant for this standard face.
-  * \return  The penalty constant.
-  */
-  inline su2double GetPenaltyConstant(void) const {return penaltyConstantFace;}
+   * \brief Function, which makes available the penalty constant for this standard face.
+   * \return  The penalty constant.
+   */
+  inline su2double GetPenaltyConstant(void) const { return penaltyConstantFace; }
 
   /*!
   * \brief Function, which makes available the the connectivity of the linear subfaces
            as a const pointer.
   * \return  The pointer to the local connectivity of the linear subfaces.
   */
-  inline const unsigned short* GetSubFaceConn(void) const {return subConnForPlotting.data();}
+  inline const unsigned short* GetSubFaceConn(void) const { return subConnForPlotting.data(); }
 
   /*!
   * \brief Function, which checks if the function arguments correspond to this standard face.
@@ -1739,17 +1629,14 @@ class CFEMStandardBoundaryFace : public CFEMStandardElementBase {
   * \param[in] val_swapFaceInElem - Whether or not the connectivity of the face must be swapped w.r.t.
                                     the connectivity of face of the adjacent element.
   */
-  bool SameStandardBoundaryFace(unsigned short val_VTK_TypeFace,
-                                bool           val_constJac,
-                                unsigned short val_VTK_TypeElem,
-                                unsigned short val_nPolyElem,
-                                bool           val_swapFaceInElem);
+  bool SameStandardBoundaryFace(unsigned short val_VTK_TypeFace, bool val_constJac, unsigned short val_VTK_TypeElem,
+                                unsigned short val_nPolyElem, bool val_swapFaceInElem);
   /*!
   * \brief Function, which estimates the amount of work for an element of this
            type. This information is used to determine a well balanced partition.
   * \param[in] config - Object, which contains the input parameters.
   */
-  su2double WorkEstimateMetis(CConfig *config);
+  su2double WorkEstimateMetis(CConfig* config);
 
   /*!
   * \brief Function, which estimates the additional amount of work for an element
@@ -1758,13 +1645,12 @@ class CFEMStandardBoundaryFace : public CFEMStandardElementBase {
   * \param[in] config    - Object, which contains the input parameters.
   * \param[in] nPointsWF - Number of points to discretize the wall model.
   */
-  su2double WorkEstimateMetisWallFunctions(CConfig              *config,
-                                           const unsigned short nPointsWF);
+  su2double WorkEstimateMetisWallFunctions(CConfig* config, const unsigned short nPointsWF);
 
-private:
+ private:
   /*!
-  * \brief Function, which copies the data of the given object into the current object.
-  * \param[in] other - Object, whose data is copied.
-  */
-  void Copy(const CFEMStandardBoundaryFace &other);
+   * \brief Function, which copies the data of the given object into the current object.
+   * \param[in] other - Object, whose data is copied.
+   */
+  void Copy(const CFEMStandardBoundaryFace& other);
 };
diff --git a/Common/include/fem/geometry_structure_fem_part.hpp b/Common/include/fem/geometry_structure_fem_part.hpp
index 332d66d3560..0791d9bfe0b 100644
--- a/Common/include/fem/geometry_structure_fem_part.hpp
+++ b/Common/include/fem/geometry_structure_fem_part.hpp
@@ -37,19 +37,17 @@
  * \brief Helper struct used to store two integral types as one entity.
  */
 struct CUnsignedLong2T {
-
-  unsigned long long0;  /*!< \brief First integer to store in this class. */
-  unsigned long long1;  /*!< \brief Second integer to store in this class. */
+  unsigned long long0; /*!< \brief First integer to store in this class. */
+  unsigned long long1; /*!< \brief Second integer to store in this class. */
 
   CUnsignedLong2T(unsigned long a = 0, unsigned long b = 0) : long0(a), long1(b) {}
 
-  inline bool operator<(const CUnsignedLong2T &other) const {
-    if(long0 != other.long0)
-      return (long0 < other.long0);
+  inline bool operator<(const CUnsignedLong2T& other) const {
+    if (long0 != other.long0) return (long0 < other.long0);
     return (long1 < other.long1);
   }
 
-  inline bool operator==(const CUnsignedLong2T &other) const {
+  inline bool operator==(const CUnsignedLong2T& other) const {
     return (long0 == other.long0) && (long1 == other.long1);
   }
 };
@@ -59,19 +57,17 @@ struct CUnsignedLong2T {
  * \brief Help struct used to store two integral types as one entity.
  */
 struct CUnsignedShort2T {
-
-  unsigned short short0;  /*!< \brief First integer to store in this class. */
-  unsigned short short1;  /*!< \brief Second integer to store in this class. */
+  unsigned short short0; /*!< \brief First integer to store in this class. */
+  unsigned short short1; /*!< \brief Second integer to store in this class. */
 
   CUnsignedShort2T(unsigned short a = 0, unsigned short b = 0) : short0(a), short1(b) {}
 
-  inline bool operator<(const CUnsignedShort2T &other) const {
-    if(short0 != other.short0)
-      return (short0 < other.short0);
+  inline bool operator<(const CUnsignedShort2T& other) const {
+    if (short0 != other.short0) return (short0 < other.short0);
     return (short1 < other.short1);
   }
 
-  inline bool operator==(const CUnsignedShort2T &other) const {
+  inline bool operator==(const CUnsignedShort2T& other) const {
     return (short0 == other.short0) && (short1 == other.short1);
   }
 };
@@ -82,16 +78,16 @@ struct CUnsignedShort2T {
           the faces of DG. It stores a face of an element.
  */
 class CFaceOfElement {
-public:
+ public:
   unsigned short nCornerPoints;          /*!< \brief Number of corner points of the face. */
-  unsigned long  cornerPoints[4];        /*!< \brief Global ID's of ther corner points. */
-  unsigned long  elemID0, elemID1;       /*!< \brief Element ID's to the left and right. */
+  unsigned long cornerPoints[4];         /*!< \brief Global ID's of ther corner points. */
+  unsigned long elemID0, elemID1;        /*!< \brief Element ID's to the left and right. */
   unsigned short nPolyGrid0, nPolyGrid1; /*!< \brief Polynomial degrees of the grid of the elements
                                                      to the left and right. */
-  unsigned short nPolySol0,  nPolySol1;  /*!< \brief Polynomial degrees of the solution of the elements
+  unsigned short nPolySol0, nPolySol1;   /*!< \brief Polynomial degrees of the solution of the elements
                                                      to the left and right. */
   unsigned short nDOFsElem0, nDOFsElem1; /*!< \brief Number of DOFs of the elements to the left and right. */
-  unsigned short elemType0,  elemType1;  /*!< \brief Type of the elements to the left and right. */
+  unsigned short elemType0, elemType1;   /*!< \brief Type of the elements to the left and right. */
   unsigned short faceID0, faceID1;       /*!< \brief The local face ID in the corresponding elements
                                                      to the left and right of the face. */
   unsigned short periodicIndex;          /*!< \brief Periodic indicator of the face. A value of 0 means no
@@ -110,35 +106,36 @@ class CFaceOfElement {
 
   /* Standard constructor and destructor. */
   CFaceOfElement();
-  ~CFaceOfElement(){}
+  ~CFaceOfElement() {}
 
   /* Alternative constructor to set the corner points. */
-  CFaceOfElement(const unsigned short VTK_Type,
-                 const unsigned short nPoly,
-                 const unsigned long  *Nodes);
+  CFaceOfElement(const unsigned short VTK_Type, const unsigned short nPoly, const unsigned long* Nodes);
 
   /* Copy constructor and assignment operator. */
-  inline CFaceOfElement(const CFaceOfElement &other) { Copy(other); }
+  inline CFaceOfElement(const CFaceOfElement& other) { Copy(other); }
 
-  inline CFaceOfElement& operator=(const CFaceOfElement &other) { Copy(other); return (*this); }
+  inline CFaceOfElement& operator=(const CFaceOfElement& other) {
+    Copy(other);
+    return (*this);
+  }
 
   /* Less than operator. Needed for the sorting and searching. */
-  bool operator<(const CFaceOfElement &other) const;
+  bool operator<(const CFaceOfElement& other) const;
 
   /* Equal operator. Needed for removing double entities. */
-  bool operator ==(const CFaceOfElement &other) const;
+  bool operator==(const CFaceOfElement& other) const;
 
   /*--- Member function, which creates a unique numbering for the corner points.
         A sort in increasing order is OK for this purpose.                       ---*/
-  inline void CreateUniqueNumbering(void) { std::sort(cornerPoints, cornerPoints+nCornerPoints); }
+  inline void CreateUniqueNumbering(void) { std::sort(cornerPoints, cornerPoints + nCornerPoints); }
 
   /*--- Member function, which creates a unique numbering for the corner points
         while the orientation is taken into account. ---*/
   void CreateUniqueNumberingWithOrientation(void);
 
-private:
+ private:
   /*--- Copy function, which copies the data of the given object into the current object. ---*/
-  void Copy(const CFaceOfElement &other);
+  void Copy(const CFaceOfElement& other);
 };
 
 /*!
@@ -147,28 +144,29 @@ class CFaceOfElement {
           It stores a boundary element.
  */
 class CBoundaryFace {
-public:
+ public:
   unsigned short VTK_Type, nPolyGrid, nDOFsGrid;
-  unsigned long  globalBoundElemID, domainElementID;
-  std::vector<unsigned long>  Nodes;
+  unsigned long globalBoundElemID, domainElementID;
+  std::vector<unsigned long> Nodes;
 
   /* Standard constructor and destructor. Nothing to be done. */
-  CBoundaryFace(){}
-  ~CBoundaryFace(){}
+  CBoundaryFace() {}
+  ~CBoundaryFace() {}
 
   /* Copy constructor and assignment operator. */
-  inline CBoundaryFace(const CBoundaryFace &other) { Copy(other); }
+  inline CBoundaryFace(const CBoundaryFace& other) { Copy(other); }
 
-  inline CBoundaryFace& operator=(const CBoundaryFace &other) { Copy(other); return (*this); }
+  inline CBoundaryFace& operator=(const CBoundaryFace& other) {
+    Copy(other);
+    return (*this);
+  }
 
   /* Less than operator. Needed for the sorting. */
-  inline bool operator<(const CBoundaryFace &other) const {
-    return (globalBoundElemID < other.globalBoundElemID);
-  }
+  inline bool operator<(const CBoundaryFace& other) const { return (globalBoundElemID < other.globalBoundElemID); }
 
-private:
+ private:
   /*--- Copy function, which copies the data of the given object into the current object. ---*/
-  void Copy(const CBoundaryFace &other);
+  void Copy(const CBoundaryFace& other);
 };
 
 /*!
@@ -176,35 +174,37 @@ class CBoundaryFace {
  * \brief Help class used to determine whether or not (periodic) faces match.
  */
 class CMatchingFace {
-public:
-  unsigned short nCornerPoints;          /*!< \brief Number of corner points of the face. */
-  unsigned short nDim;                   /*!< \brief Number of spatial dimensions. */
-  unsigned short nPoly;                  /*!< \brief Polynomial degree of the face. */
-  unsigned short nDOFsElem;              /*!< \brief Number of DOFs of the relevant adjacent element. */
-  unsigned short elemType;               /*!< \brief Type of the adjacent element. */
-  unsigned long  elemID;                 /*!< \brief The relevant adjacent element ID. */
-  su2double cornerCoor[4][3];            /*!< \brief Coordinates of the corner points of the face. */
-  su2double tolForMatching;              /*!< \brief Tolerance for this face for matching points. */
+ public:
+  unsigned short nCornerPoints; /*!< \brief Number of corner points of the face. */
+  unsigned short nDim;          /*!< \brief Number of spatial dimensions. */
+  unsigned short nPoly;         /*!< \brief Polynomial degree of the face. */
+  unsigned short nDOFsElem;     /*!< \brief Number of DOFs of the relevant adjacent element. */
+  unsigned short elemType;      /*!< \brief Type of the adjacent element. */
+  unsigned long elemID;         /*!< \brief The relevant adjacent element ID. */
+  su2double cornerCoor[4][3];   /*!< \brief Coordinates of the corner points of the face. */
+  su2double tolForMatching;     /*!< \brief Tolerance for this face for matching points. */
 
   /* Standard constructor. */
   CMatchingFace();
 
   /* Destructor, nothing to be done. */
-  ~CMatchingFace(){}
+  ~CMatchingFace() {}
 
   /* Copy constructor and assignment operator. */
-  inline CMatchingFace(const CMatchingFace &other) { Copy(other); }
+  inline CMatchingFace(const CMatchingFace& other) { Copy(other); }
 
-  inline CMatchingFace& operator=(const CMatchingFace &other) { Copy(other); return (*this); }
+  inline CMatchingFace& operator=(const CMatchingFace& other) {
+    Copy(other);
+    return (*this);
+  }
 
   /* Less than operator. Needed for the sorting and searching. */
-  bool operator<(const CMatchingFace &other) const;
+  bool operator<(const CMatchingFace& other) const;
 
   /*--- Member function, which sorts the coordinates of the face. ---*/
   void SortFaceCoordinates(void);
 
-private:
+ private:
   /*--- Copy function, which copies the data of the given object into the current object. ---*/
-  void Copy(const CMatchingFace &other);
+  void Copy(const CMatchingFace& other);
 };
-
diff --git a/Common/include/geometry/CDummyGeometry.hpp b/Common/include/geometry/CDummyGeometry.hpp
index e5ec401057e..73028f7f957 100644
--- a/Common/include/geometry/CDummyGeometry.hpp
+++ b/Common/include/geometry/CDummyGeometry.hpp
@@ -36,14 +36,11 @@
  *        going through the time-consuming mesh initialization and paritioning.
  * \author T. Albring
  */
-class CDummyGeometry final : public CGeometry{
-
-public:
+class CDummyGeometry final : public CGeometry {
+ public:
   /*!
    * \brief Constructor of the class
    * \param[in] config - Definition of the particular problem.
    */
-  CDummyGeometry(CConfig *config);
-
+  CDummyGeometry(CConfig* config);
 };
-
diff --git a/Common/include/geometry/CGeometry.hpp b/Common/include/geometry/CGeometry.hpp
index c4e5067245c..dd5f936fe49 100644
--- a/Common/include/geometry/CGeometry.hpp
+++ b/Common/include/geometry/CGeometry.hpp
@@ -74,125 +74,141 @@ using namespace std;
  */
 class CGeometry {
  protected:
-  enum : size_t {OMP_MIN_SIZE = 32}; /*!< \brief Chunk size for small loops. */
-  enum : size_t {MAXNDIM = 3};
-
-  const int size{SINGLE_NODE};    /*!< \brief MPI Size. */
-  const int rank{MASTER_NODE};    /*!< \brief MPI Rank. */
-
-  unsigned long nPoint{0},        /*!< \brief Number of points of the mesh. */
-  nPointDomain{0},                /*!< \brief Number of real points of the mesh. */
-  nPointGhost{0},                 /*!< \brief Number of ghost points of the mesh. */
-  Global_nPoint{0},               /*!< \brief Total number of nodes in a simulation across all processors (including halos). */
-  Global_nPointDomain{0},         /*!< \brief Total number of nodes in a simulation across all processors (excluding halos). */
-  nElem{0},                       /*!< \brief Number of elements of the mesh. */
-  Global_nElem{0},                /*!< \brief Total number of elements in a simulation across all processors (all types). */
-  Global_nElemDomain{0},          /*!< \brief Total number of elements in a simulation across all processors (excluding halos). */
-  nEdge{0},                       /*!< \brief Number of edges of the mesh. */
-  nFace{0},                       /*!< \brief Number of faces of the mesh. */
-  nelem_edge{0},                  /*!< \brief Number of edges in the mesh. */
-  Global_nelem_edge{0},           /*!< \brief Total number of edges in the mesh across all processors. */
-  nelem_triangle{0},              /*!< \brief Number of triangles in the mesh. */
-  Global_nelem_triangle{0},       /*!< \brief Total number of triangles in the mesh across all processors. */
-  nelem_quad{0},                  /*!< \brief Number of quadrangles in the mesh. */
-  Global_nelem_quad{0},           /*!< \brief Total number of quadrangles in the mesh across all processors. */
-  nelem_tetra{0},                 /*!< \brief Number of tetrahedra in the mesh. */
-  Global_nelem_tetra{0},          /*!< \brief Total number of tetrahedra in the mesh across all processors. */
-  nelem_hexa{0},                  /*!< \brief Number of hexahedra in the mesh. */
-  Global_nelem_hexa{0},           /*!< \brief Total number of hexahedra in the mesh across all processors. */
-  nelem_prism{0},                 /*!< \brief Number of prisms in the mesh. */
-  Global_nelem_prism{0},          /*!< \brief Total number of prisms in the mesh across all processors. */
-  nelem_pyramid{0},               /*!< \brief Number of pyramids in the mesh. */
-  Global_nelem_pyramid{0},        /*!< \brief Total number of pyramids in the mesh across all processors. */
-  nelem_edge_bound{0},            /*!< \brief Number of edges on the mesh boundaries. */
-  Global_nelem_edge_bound{0},     /*!< \brief Total number of edges on the mesh boundaries across all processors. */
-  nelem_triangle_bound{0},        /*!< \brief Number of triangles on the mesh boundaries. */
-  Global_nelem_triangle_bound{0}, /*!< \brief Total number of triangles on the mesh boundaries across all processors. */
-  nelem_quad_bound{0},            /*!< \brief Number of quads on the mesh boundaries. */
-  Global_nelem_quad_bound{0},     /*!< \brief Total number of quads on the mesh boundaries across all processors. */
-  nNonconvexElements{0};          /*!< \brief Number of nonconvex elements in the mesh. */
-
-  unsigned short nDim{0};         /*!< \brief Number of dimension of the problem. */
-  unsigned short nZone{0};        /*!< \brief Number of zones in the problem. */
-  unsigned short nMarker{0};      /*!< \brief Number of different markers of the mesh. */
-  unsigned short nCommLevel{0};   /*!< \brief Number of non-blocking communication levels. */
+  enum : size_t { OMP_MIN_SIZE = 32 }; /*!< \brief Chunk size for small loops. */
+  enum : size_t { MAXNDIM = 3 };
+
+  const int size{SINGLE_NODE}; /*!< \brief MPI Size. */
+  const int rank{MASTER_NODE}; /*!< \brief MPI Rank. */
+
+  unsigned long nPoint{0}, /*!< \brief Number of points of the mesh. */
+      nPointDomain{0},     /*!< \brief Number of real points of the mesh. */
+      nPointGhost{0},      /*!< \brief Number of ghost points of the mesh. */
+      Global_nPoint{0},    /*!< \brief Total number of nodes in a simulation across all processors (including halos). */
+      Global_nPointDomain{
+          0},          /*!< \brief Total number of nodes in a simulation across all processors (excluding halos). */
+      nElem{0},        /*!< \brief Number of elements of the mesh. */
+      Global_nElem{0}, /*!< \brief Total number of elements in a simulation across all processors (all types). */
+      Global_nElemDomain{
+          0},        /*!< \brief Total number of elements in a simulation across all processors (excluding halos). */
+      nEdge{0},      /*!< \brief Number of edges of the mesh. */
+      nFace{0},      /*!< \brief Number of faces of the mesh. */
+      nelem_edge{0}, /*!< \brief Number of edges in the mesh. */
+      Global_nelem_edge{0},       /*!< \brief Total number of edges in the mesh across all processors. */
+      nelem_triangle{0},          /*!< \brief Number of triangles in the mesh. */
+      Global_nelem_triangle{0},   /*!< \brief Total number of triangles in the mesh across all processors. */
+      nelem_quad{0},              /*!< \brief Number of quadrangles in the mesh. */
+      Global_nelem_quad{0},       /*!< \brief Total number of quadrangles in the mesh across all processors. */
+      nelem_tetra{0},             /*!< \brief Number of tetrahedra in the mesh. */
+      Global_nelem_tetra{0},      /*!< \brief Total number of tetrahedra in the mesh across all processors. */
+      nelem_hexa{0},              /*!< \brief Number of hexahedra in the mesh. */
+      Global_nelem_hexa{0},       /*!< \brief Total number of hexahedra in the mesh across all processors. */
+      nelem_prism{0},             /*!< \brief Number of prisms in the mesh. */
+      Global_nelem_prism{0},      /*!< \brief Total number of prisms in the mesh across all processors. */
+      nelem_pyramid{0},           /*!< \brief Number of pyramids in the mesh. */
+      Global_nelem_pyramid{0},    /*!< \brief Total number of pyramids in the mesh across all processors. */
+      nelem_edge_bound{0},        /*!< \brief Number of edges on the mesh boundaries. */
+      Global_nelem_edge_bound{0}, /*!< \brief Total number of edges on the mesh boundaries across all processors. */
+      nelem_triangle_bound{0},    /*!< \brief Number of triangles on the mesh boundaries. */
+      Global_nelem_triangle_bound{
+          0},                     /*!< \brief Total number of triangles on the mesh boundaries across all processors. */
+      nelem_quad_bound{0},        /*!< \brief Number of quads on the mesh boundaries. */
+      Global_nelem_quad_bound{0}, /*!< \brief Total number of quads on the mesh boundaries across all processors. */
+      nNonconvexElements{0};      /*!< \brief Number of nonconvex elements in the mesh. */
+
+  unsigned short nDim{0};       /*!< \brief Number of dimension of the problem. */
+  unsigned short nZone{0};      /*!< \brief Number of zones in the problem. */
+  unsigned short nMarker{0};    /*!< \brief Number of different markers of the mesh. */
+  unsigned short nCommLevel{0}; /*!< \brief Number of non-blocking communication levels. */
 
   unsigned short MGLevel{0};        /*!< \brief The mesh level index for the current geometry container. */
   unsigned long Max_GlobalPoint{0}; /*!< \brief Greater global point in the domain local structure. */
 
   /*--- Boundary information. ---*/
 
-  short *Marker_All_SendRecv{nullptr};   /*!< \brief MPI Marker. */
-  su2double **CustomBoundaryTemperature{nullptr};
-  su2double **CustomBoundaryHeatFlux{nullptr};
+  short* Marker_All_SendRecv{nullptr}; /*!< \brief MPI Marker. */
+  su2double** CustomBoundaryTemperature{nullptr};
+  su2double** CustomBoundaryHeatFlux{nullptr};
 
   /*--- Create vectors and distribute the values among the different planes queues ---*/
 
-  vector<vector<su2double> > Xcoord_plane;     /*!< \brief Vector containing x coordinates of new points appearing on a single plane */
-  vector<vector<su2double> > Ycoord_plane;     /*!< \brief Vector containing y coordinates of new points appearing on a single plane */
-  vector<vector<su2double> > Zcoord_plane;     /*!< \brief Vector containing z coordinates of new points appearing on a single plane */
-  vector<vector<su2double> > FaceArea_plane;   /*!< \brief Vector containing area/volume associated with  new points appearing on a single plane */
-  vector<vector<unsigned long> > Plane_points; /*!< \brief Vector containing points appearing on a single plane */
+  vector<vector<su2double>>
+      Xcoord_plane; /*!< \brief Vector containing x coordinates of new points appearing on a single plane */
+  vector<vector<su2double>>
+      Ycoord_plane; /*!< \brief Vector containing y coordinates of new points appearing on a single plane */
+  vector<vector<su2double>>
+      Zcoord_plane; /*!< \brief Vector containing z coordinates of new points appearing on a single plane */
+  vector<vector<su2double>> FaceArea_plane;   /*!< \brief Vector containing area/volume associated with  new points
+                                                 appearing on a single plane */
+  vector<vector<unsigned long>> Plane_points; /*!< \brief Vector containing points appearing on a single plane */
 
-  vector<su2double> XCoordList;              /*!< \brief Vector containing points appearing on a single plane */
+  vector<su2double> XCoordList; /*!< \brief Vector containing points appearing on a single plane */
 
 #if defined(HAVE_MPI) && defined(HAVE_PARMETIS)
-  vector<vector<unsigned long> > adj_nodes; /*!< \brief Vector of vectors holding each node's adjacency during preparation for ParMETIS. */
-  vector<idx_t> adjacency; /*!< \brief Local adjacency array to be input into ParMETIS for partitioning (idx_t is a ParMETIS type defined in their headers). */
-  vector<idx_t> xadj;      /*!< \brief Index array that points to the start of each node's adjacency in CSR format (needed to interpret the adjacency array).  */
+  vector<vector<unsigned long>>
+      adj_nodes; /*!< \brief Vector of vectors holding each node's adjacency during preparation for ParMETIS. */
+  vector<idx_t> adjacency; /*!< \brief Local adjacency array to be input into ParMETIS for partitioning (idx_t is a
+                              ParMETIS type defined in their headers). */
+  vector<idx_t> xadj; /*!< \brief Index array that points to the start of each node's adjacency in CSR format (needed to
+                         interpret the adjacency array).  */
 #endif
 
   /*--- Turbomachinery variables ---*/
 
-  unsigned short *nSpanWiseSections{nullptr};     /*!< \brief Number of Span wise section for each turbo marker, indexed by inflow/outflow */
-  unsigned short *nSpanSectionsByMarker{nullptr}; /*!< \brief Number of Span wise section for each turbo marker, indexed by marker.  Needed for deallocation.*/
+  unsigned short* nSpanWiseSections{
+      nullptr}; /*!< \brief Number of Span wise section for each turbo marker, indexed by inflow/outflow */
+  unsigned short* nSpanSectionsByMarker{nullptr}; /*!< \brief Number of Span wise section for each turbo marker, indexed
+                                                     by marker.  Needed for deallocation.*/
   unsigned short nTurboPerf{0};                   /*!< \brief Number of Span wise section for each turbo marker. */
-  su2double **SpanWiseValue{nullptr};             /*!< \brief Span wise values for each turbo marker. */
-  long **nVertexSpan{nullptr};                    /*!< \brief number of vertexes for span wise section for each marker.  */
-  unsigned long **nTotVertexSpan{nullptr};        /*!< \brief number of vertexes at each span wise section for each marker.  */
-  unsigned long nVertexSpanMax[3] = {0};          /*!< \brief max number of vertexes for each span section for each marker flag.  */
-  su2double ***AverageTurboNormal{nullptr};       /*!< \brief Average boundary normal at each span wise section for each marker in the turbomachinery frame of reference.*/
-  su2double ***AverageNormal{nullptr};            /*!< \brief Average boundary normal at each span wise section for each marker.*/
-  su2double ***AverageGridVel{nullptr};           /*!< \brief Average boundary grid velocity at each span wise section for each marker.*/
-  su2double **AverageTangGridVel{nullptr};        /*!< \brief Average tangential rotational speed at each span wise section for each marker.*/
-  su2double **SpanArea{nullptr};                  /*!< \brief Area at each span wise section for each marker.*/
-  su2double **MaxAngularCoord{nullptr};           /*!< \brief Max angular pitch at each span wise section for each marker.*/
-  su2double **MinAngularCoord{nullptr};           /*!< \brief Max angular pitch at each span wise section for each marker.*/
-  su2double **MinRelAngularCoord{nullptr};        /*!< \brief Min relative angular coord at each span wise section for each marker.*/
-  su2double **TurboRadius{nullptr};               /*!< \brief Radius at each span wise section for each marker.*/
-  su2double **TangGridVelIn{nullptr};
-  su2double **TangGridVelOut{nullptr};            /*!< \brief Average tangential rotational speed at each span wise section for each turbomachinery marker.*/
-  su2double **SpanAreaIn{nullptr};
-  su2double **SpanAreaOut{nullptr};               /*!< \brief Area at each span wise section for each turbomachinery marker.*/
-  su2double **TurboRadiusIn{nullptr};
-  su2double **TurboRadiusOut{nullptr};            /*!< \brief Radius at each span wise section for each turbomachinery marker*/
+  su2double** SpanWiseValue{nullptr};             /*!< \brief Span wise values for each turbo marker. */
+  long** nVertexSpan{nullptr};             /*!< \brief number of vertexes for span wise section for each marker.  */
+  unsigned long** nTotVertexSpan{nullptr}; /*!< \brief number of vertexes at each span wise section for each marker.  */
+  unsigned long nVertexSpanMax[3] = {
+      0}; /*!< \brief max number of vertexes for each span section for each marker flag.  */
+  su2double*** AverageTurboNormal{nullptr}; /*!< \brief Average boundary normal at each span wise section for each
+                                               marker in the turbomachinery frame of reference.*/
+  su2double*** AverageNormal{nullptr}; /*!< \brief Average boundary normal at each span wise section for each marker.*/
+  su2double*** AverageGridVel{
+      nullptr}; /*!< \brief Average boundary grid velocity at each span wise section for each marker.*/
+  su2double** AverageTangGridVel{
+      nullptr}; /*!< \brief Average tangential rotational speed at each span wise section for each marker.*/
+  su2double** SpanArea{nullptr};        /*!< \brief Area at each span wise section for each marker.*/
+  su2double** MaxAngularCoord{nullptr}; /*!< \brief Max angular pitch at each span wise section for each marker.*/
+  su2double** MinAngularCoord{nullptr}; /*!< \brief Max angular pitch at each span wise section for each marker.*/
+  su2double** MinRelAngularCoord{
+      nullptr};                     /*!< \brief Min relative angular coord at each span wise section for each marker.*/
+  su2double** TurboRadius{nullptr}; /*!< \brief Radius at each span wise section for each marker.*/
+  su2double** TangGridVelIn{nullptr};
+  su2double** TangGridVelOut{nullptr}; /*!< \brief Average tangential rotational speed at each span wise section for
+                                          each turbomachinery marker.*/
+  su2double** SpanAreaIn{nullptr};
+  su2double** SpanAreaOut{nullptr}; /*!< \brief Area at each span wise section for each turbomachinery marker.*/
+  su2double** TurboRadiusIn{nullptr};
+  su2double** TurboRadiusOut{nullptr}; /*!< \brief Radius at each span wise section for each turbomachinery marker*/
 
   /*--- Sparsity patterns associated with the geometry. ---*/
 
-  CCompressedSparsePatternUL
-  finiteVolumeCSRFill0,                  /*!< \brief 0-fill FVM sparsity. */
-  finiteVolumeCSRFillN,                  /*!< \brief N-fill FVM sparsity (e.g. for ILUn preconditioner). */
-  finiteElementCSRFill0,                 /*!< \brief 0-fill FEM sparsity. */
-  finiteElementCSRFillN;                 /*!< \brief N-fill FEM sparsity (e.g. for ILUn preconditioner). */
+  CCompressedSparsePatternUL finiteVolumeCSRFill0, /*!< \brief 0-fill FVM sparsity. */
+      finiteVolumeCSRFillN,                        /*!< \brief N-fill FVM sparsity (e.g. for ILUn preconditioner). */
+      finiteElementCSRFill0,                       /*!< \brief 0-fill FEM sparsity. */
+      finiteElementCSRFillN;                       /*!< \brief N-fill FEM sparsity (e.g. for ILUn preconditioner). */
 
-  CEdgeToNonZeroMapUL edgeToCSRMap;      /*!< \brief Map edges to CSR entries referenced by them (i,j) and (j,i). */
+  CEdgeToNonZeroMapUL edgeToCSRMap; /*!< \brief Map edges to CSR entries referenced by them (i,j) and (j,i). */
 
   /*--- Edge and element colorings. ---*/
 
-  CCompressedSparsePatternUL
-  edgeColoring,                          /*!< \brief Edge coloring structure for thread-based parallelization. */
-  elemColoring;                          /*!< \brief Element coloring structure for thread-based parallelization. */
-  unsigned long edgeColorGroupSize{1};   /*!< \brief Size of the edge groups within each color. */
-  unsigned long elemColorGroupSize{1};   /*!< \brief Size of the element groups within each color. */
+  CCompressedSparsePatternUL edgeColoring, /*!< \brief Edge coloring structure for thread-based parallelization. */
+      elemColoring;                        /*!< \brief Element coloring structure for thread-based parallelization. */
+  unsigned long edgeColorGroupSize{1};     /*!< \brief Size of the edge groups within each color. */
+  unsigned long elemColorGroupSize{1};     /*!< \brief Size of the element groups within each color. */
 
-  ColMajorMatrix<uint8_t> CoarseGridColor_;  /*!< \brief Coarse grid levels, colorized. */
+  ColMajorMatrix<uint8_t> CoarseGridColor_; /*!< \brief Coarse grid levels, colorized. */
 
  public:
   /*!< \brief Linelets (mesh lines perpendicular to stretching direction). */
   struct CLineletInfo {
     /*!< \brief Detect isotropic mesh region. */
     static passivedouble ALPHA_ISOTROPIC() { return 0.8; }
-    enum : unsigned long {MAX_LINELET_POINTS = 32}; /*!< \brief Maximum points per linelet. */
+    enum : unsigned long { MAX_LINELET_POINTS = 32 }; /*!< \brief Maximum points per linelet. */
 
     std::vector<std::vector<unsigned long>> linelets; /*!< \brief Point indices for each linelet. */
 
@@ -200,90 +216,115 @@ class CGeometry {
     std::vector<unsigned> lineletIdx;
 
     /*!< \brief Signals that a point is not on a linelet. */
-    enum : unsigned {NO_LINELET = std::numeric_limits<unsigned>::max()};
+    enum : unsigned { NO_LINELET = std::numeric_limits<unsigned>::max() };
 
     /*!< \brief Coloring for OpenMP parallelization, "linelets" is sorted by color. */
     std::vector<unsigned long> colorOffsets;
 
-    std::vector<uint8_t> lineletColor;  /*!< \brief Coloring transfered to points, for visualization. */
+    std::vector<uint8_t> lineletColor; /*!< \brief Coloring transfered to points, for visualization. */
   };
+
  protected:
   mutable CLineletInfo lineletInfo;
 
  public:
   /*--- Main geometric elements of the grid. ---*/
 
-  CPrimalGrid** elem{nullptr};           /*!< \brief Element vector (primal grid information). */
-  CPrimalGrid*** bound{nullptr};         /*!< \brief Boundary vector (primal grid information). */
-  CPoint* nodes{nullptr};                /*!< \brief Node vector (dual grid information). */
-  CEdge* edges{nullptr};                 /*!< \brief Edge vector (dual grid information). */
-  CVertex*** vertex{nullptr};            /*!< \brief Boundary Vertex vector (dual grid information). */
-  CTurboVertex**** turbovertex{nullptr}; /*!< \brief Boundary Vertex vector ordered for turbomachinery calculation(dual grid information). */
-  unsigned long *nVertex{nullptr};       /*!< \brief Number of vertex for each marker. */
-  unsigned long *nElem_Bound{nullptr};   /*!< \brief Number of elements of the boundary. */
-  string *Tag_to_Marker{nullptr};        /*!< \brief Names of boundary markers. */
-  vector<bool> bound_is_straight;        /*!< \brief Bool if boundary-marker is straight(2D)/plane(3D) for each local marker. */
-  vector<su2double> SurfaceAreaCfgFile;  /*!< \brief Total Surface area for all markers. */
+  CPrimalGrid** elem{nullptr};   /*!< \brief Element vector (primal grid information). */
+  CPrimalGrid*** bound{nullptr}; /*!< \brief Boundary vector (primal grid information). */
+  CPoint* nodes{nullptr};        /*!< \brief Node vector (dual grid information). */
+  CEdge* edges{nullptr};         /*!< \brief Edge vector (dual grid information). */
+  CVertex*** vertex{nullptr};    /*!< \brief Boundary Vertex vector (dual grid information). */
+  CTurboVertex**** turbovertex{
+      nullptr}; /*!< \brief Boundary Vertex vector ordered for turbomachinery calculation(dual grid information). */
+  unsigned long* nVertex{nullptr};     /*!< \brief Number of vertex for each marker. */
+  unsigned long* nElem_Bound{nullptr}; /*!< \brief Number of elements of the boundary. */
+  string* Tag_to_Marker{nullptr};      /*!< \brief Names of boundary markers. */
+  vector<bool>
+      bound_is_straight; /*!< \brief Bool if boundary-marker is straight(2D)/plane(3D) for each local marker. */
+  vector<su2double> SurfaceAreaCfgFile; /*!< \brief Total Surface area for all markers. */
 
   /*--- Partitioning-specific variables ---*/
 
-  unordered_map<unsigned long,unsigned long> Global_to_Local_Elem; /*!< \brief Mapping of global to local index for elements. */
-  unsigned long *beg_node{nullptr};         /*!< \brief Array containing the first node on each rank due to a linear partitioning by global index. */
-  unsigned long *end_node{nullptr};         /*!< \brief Array containing the last node on each rank due to a linear partitioning by global index. */
-  unsigned long *nPointLinear{nullptr};     /*!< \brief Array containing the total number of nodes on each rank due to a linear partioning by global index. */
-  unsigned long *nPointCumulative{nullptr}; /*!< \brief Cumulative storage array containing the total number of points on all prior ranks in the linear partitioning. */
+  unordered_map<unsigned long, unsigned long>
+      Global_to_Local_Elem;         /*!< \brief Mapping of global to local index for elements. */
+  unsigned long* beg_node{nullptr}; /*!< \brief Array containing the first node on each rank due to a linear
+                                       partitioning by global index. */
+  unsigned long* end_node{
+      nullptr}; /*!< \brief Array containing the last node on each rank due to a linear partitioning by global index. */
+  unsigned long* nPointLinear{nullptr};     /*!< \brief Array containing the total number of nodes on each rank due to a
+                                               linear partioning by global index. */
+  unsigned long* nPointCumulative{nullptr}; /*!< \brief Cumulative storage array containing the total number of points
+                                               on all prior ranks in the linear partitioning. */
 
   /*--- Data structures for point-to-point MPI communications. ---*/
 
-  int maxCountPerPoint{0};                /*!< \brief Maximum number of pieces of data sent per vertex in point-to-point comms. */
-  int nP2PSend{0};                        /*!< \brief Number of sends during point-to-point comms. */
-  int nP2PRecv{0};                        /*!< \brief Number of receives during point-to-point comms. */
-  int *nPoint_P2PSend{nullptr};           /*!< \brief Data structure holding number of vertices for each send in point-to-point comms. */
-  int *nPoint_P2PRecv{nullptr};           /*!< \brief Data structure holding number of vertices for each recv in point-to-point comms. */
-  int *Neighbors_P2PSend{nullptr};        /*!< \brief Data structure holding the ranks of the neighbors for point-to-point send comms. */
-  int *Neighbors_P2PRecv{nullptr};        /*!< \brief Data structure holding the ranks of the neighbors for point-to-point recv comms. */
-  map<int, int> P2PSend2Neighbor;         /*!< \brief Data structure holding the reverse mapping of the ranks of the neighbors for point-to-point send comms. */
-  map<int, int> P2PRecv2Neighbor;         /*!< \brief Data structure holding the reverse mapping of the ranks of the neighbors for point-to-point recv comms. */
-  unsigned long
-  *Local_Point_P2PSend{nullptr},          /*!< \brief Data structure holding the local index of all vertices to be sent in point-to-point comms. */
-  *Local_Point_P2PRecv{nullptr};          /*!< \brief Data structure holding the local index of all vertices to be received in point-to-point comms. */
-  su2double *bufD_P2PRecv{nullptr};       /*!< \brief Data structure for su2double point-to-point receive. */
-  su2double *bufD_P2PSend{nullptr};       /*!< \brief Data structure for su2double point-to-point send. */
-  unsigned short *bufS_P2PRecv{nullptr};  /*!< \brief Data structure for unsigned long point-to-point receive. */
-  unsigned short *bufS_P2PSend{nullptr};  /*!< \brief Data structure for unsigned long point-to-point send. */
-  SU2_MPI::Request *req_P2PSend{nullptr}; /*!< \brief Data structure for point-to-point send requests. */
-  SU2_MPI::Request *req_P2PRecv{nullptr}; /*!< \brief Data structure for point-to-point recv requests. */
+  int maxCountPerPoint{0}; /*!< \brief Maximum number of pieces of data sent per vertex in point-to-point comms. */
+  int nP2PSend{0};         /*!< \brief Number of sends during point-to-point comms. */
+  int nP2PRecv{0};         /*!< \brief Number of receives during point-to-point comms. */
+  int* nPoint_P2PSend{
+      nullptr}; /*!< \brief Data structure holding number of vertices for each send in point-to-point comms. */
+  int* nPoint_P2PRecv{
+      nullptr}; /*!< \brief Data structure holding number of vertices for each recv in point-to-point comms. */
+  int* Neighbors_P2PSend{
+      nullptr}; /*!< \brief Data structure holding the ranks of the neighbors for point-to-point send comms. */
+  int* Neighbors_P2PRecv{
+      nullptr}; /*!< \brief Data structure holding the ranks of the neighbors for point-to-point recv comms. */
+  map<int, int> P2PSend2Neighbor; /*!< \brief Data structure holding the reverse mapping of the ranks of the neighbors
+                                     for point-to-point send comms. */
+  map<int, int> P2PRecv2Neighbor; /*!< \brief Data structure holding the reverse mapping of the ranks of the neighbors
+                                     for point-to-point recv comms. */
+  unsigned long *Local_Point_P2PSend{nullptr}, /*!< \brief Data structure holding the local index of all vertices to be
+                                                  sent in point-to-point comms. */
+      *Local_Point_P2PRecv{nullptr}; /*!< \brief Data structure holding the local index of all vertices to be received
+                                        in point-to-point comms. */
+  su2double* bufD_P2PRecv{nullptr};  /*!< \brief Data structure for su2double point-to-point receive. */
+  su2double* bufD_P2PSend{nullptr};  /*!< \brief Data structure for su2double point-to-point send. */
+  unsigned short* bufS_P2PRecv{nullptr};  /*!< \brief Data structure for unsigned long point-to-point receive. */
+  unsigned short* bufS_P2PSend{nullptr};  /*!< \brief Data structure for unsigned long point-to-point send. */
+  SU2_MPI::Request* req_P2PSend{nullptr}; /*!< \brief Data structure for point-to-point send requests. */
+  SU2_MPI::Request* req_P2PRecv{nullptr}; /*!< \brief Data structure for point-to-point recv requests. */
 
   /*--- Data structures for periodic communications. ---*/
 
-  int maxCountPerPeriodicPoint{0};        /*!< \brief Maximum number of pieces of data sent per vertex in periodic comms. */
-  int nPeriodicSend{0};                   /*!< \brief Number of sends during periodic comms. */
-  int nPeriodicRecv{0};                   /*!< \brief Number of receives during periodic comms. */
-  int *nPoint_PeriodicSend{nullptr};      /*!< \brief Data structure holding number of vertices for each send in periodic comms. */
-  int *nPoint_PeriodicRecv{nullptr};      /*!< \brief Data structure holding number of vertices for each recv in periodic comms. */
-  int *Neighbors_PeriodicSend{nullptr};   /*!< \brief Data structure holding the ranks of the neighbors for periodic send comms. */
-  int *Neighbors_PeriodicRecv{nullptr};   /*!< \brief Data structure holding the ranks of the neighbors for periodic recv comms. */
-  map<int, int> PeriodicSend2Neighbor;    /*!< \brief Data structure holding the reverse mapping of the ranks of the neighbors for periodic send comms. */
-  map<int, int> PeriodicRecv2Neighbor;    /*!< \brief Data structure holding the reverse mapping of the ranks of the neighbors for periodic recv comms. */
-  unsigned long
-  *Local_Point_PeriodicSend{nullptr},          /*!< \brief Data structure holding the local index of all vertices to be sent in periodic comms. */
-  *Local_Point_PeriodicRecv{nullptr},          /*!< \brief Data structure holding the local index of all vertices to be received in periodic comms. */
-  *Local_Marker_PeriodicSend{nullptr},         /*!< \brief Data structure holding the local index of the periodic marker for a particular vertex to be sent in periodic comms. */
-  *Local_Marker_PeriodicRecv{nullptr};         /*!< \brief Data structure holding the local index of the periodic marker for a particular vertex to be received in periodic comms. */
-  su2double *bufD_PeriodicRecv{nullptr};       /*!< \brief Data structure for su2double periodic receive. */
-  su2double *bufD_PeriodicSend{nullptr};       /*!< \brief Data structure for su2double periodic send. */
-  unsigned short *bufS_PeriodicRecv{nullptr};  /*!< \brief Data structure for unsigned long periodic receive. */
-  unsigned short *bufS_PeriodicSend{nullptr};  /*!< \brief Data structure for unsigned long periodic send. */
-  SU2_MPI::Request *req_PeriodicSend{nullptr}; /*!< \brief Data structure for periodic send requests. */
-  SU2_MPI::Request *req_PeriodicRecv{nullptr}; /*!< \brief Data structure for periodic recv requests. */
+  int maxCountPerPeriodicPoint{0}; /*!< \brief Maximum number of pieces of data sent per vertex in periodic comms. */
+  int nPeriodicSend{0};            /*!< \brief Number of sends during periodic comms. */
+  int nPeriodicRecv{0};            /*!< \brief Number of receives during periodic comms. */
+  int* nPoint_PeriodicSend{
+      nullptr}; /*!< \brief Data structure holding number of vertices for each send in periodic comms. */
+  int* nPoint_PeriodicRecv{
+      nullptr}; /*!< \brief Data structure holding number of vertices for each recv in periodic comms. */
+  int* Neighbors_PeriodicSend{
+      nullptr}; /*!< \brief Data structure holding the ranks of the neighbors for periodic send comms. */
+  int* Neighbors_PeriodicRecv{
+      nullptr}; /*!< \brief Data structure holding the ranks of the neighbors for periodic recv comms. */
+  map<int, int> PeriodicSend2Neighbor; /*!< \brief Data structure holding the reverse mapping of the ranks of the
+                                          neighbors for periodic send comms. */
+  map<int, int> PeriodicRecv2Neighbor; /*!< \brief Data structure holding the reverse mapping of the ranks of the
+                                          neighbors for periodic recv comms. */
+  unsigned long *Local_Point_PeriodicSend{
+      nullptr}, /*!< \brief Data structure holding the local index of all vertices to be sent in periodic comms. */
+      *Local_Point_PeriodicRecv{nullptr},  /*!< \brief Data structure holding the local index of all vertices to be
+                                              received in periodic comms. */
+      *Local_Marker_PeriodicSend{nullptr}, /*!< \brief Data structure holding the local index of the periodic marker for
+                                              a particular vertex to be sent in periodic comms. */
+      *Local_Marker_PeriodicRecv{nullptr}; /*!< \brief Data structure holding the local index of the periodic marker for
+                                              a particular vertex to be received in periodic comms. */
+  su2double* bufD_PeriodicRecv{nullptr};   /*!< \brief Data structure for su2double periodic receive. */
+  su2double* bufD_PeriodicSend{nullptr};   /*!< \brief Data structure for su2double periodic send. */
+  unsigned short* bufS_PeriodicRecv{nullptr};  /*!< \brief Data structure for unsigned long periodic receive. */
+  unsigned short* bufS_PeriodicSend{nullptr};  /*!< \brief Data structure for unsigned long periodic send. */
+  SU2_MPI::Request* req_PeriodicSend{nullptr}; /*!< \brief Data structure for periodic send requests. */
+  SU2_MPI::Request* req_PeriodicRecv{nullptr}; /*!< \brief Data structure for periodic recv requests. */
 
   /*--- Mesh quality metrics. ---*/
 
-  vector<su2double> Orthogonality;       /*!< \brief Measure of dual CV orthogonality angle (0 to 90 deg., 90 being best). */
-  vector<su2double> Aspect_Ratio;        /*!< \brief Measure of dual CV aspect ratio (max face area / min face area).  */
-  vector<su2double> Volume_Ratio;        /*!< \brief Measure of dual CV volume ratio (max sub-element volume / min sub-element volume). */
+  vector<su2double> Orthogonality; /*!< \brief Measure of dual CV orthogonality angle (0 to 90 deg., 90 being best). */
+  vector<su2double> Aspect_Ratio;  /*!< \brief Measure of dual CV aspect ratio (max face area / min face area).  */
+  vector<su2double>
+      Volume_Ratio; /*!< \brief Measure of dual CV volume ratio (max sub-element volume / min sub-element volume). */
 
-  const ColMajorMatrix<uint8_t>& CoarseGridColor = CoarseGridColor_;  /*!< \brief Coarse grid levels, colorized. */
+  const ColMajorMatrix<uint8_t>& CoarseGridColor = CoarseGridColor_; /*!< \brief Coarse grid levels, colorized. */
 
   /*!
    * \brief Constructor of the class.
@@ -293,7 +334,7 @@ class CGeometry {
   /*!
    * \brief Constructor of the class.
    */
-  CGeometry(CConfig *config, unsigned short nDim);
+  CGeometry(CConfig* config, unsigned short nDim);
 
   /*!
    * \brief Destructor of the class.
@@ -307,11 +348,12 @@ class CGeometry {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void PreprocessP2PComms(CGeometry *geometry, CConfig *config);
+  void PreprocessP2PComms(CGeometry* geometry, CConfig* config);
 
   /*!
-   * \brief Routine to allocate buffers for point-to-point MPI communications. Also called to dynamically reallocate if not enough memory is found for comms during runtime.
-   * \param[in] val_countPerPoint - Maximum count of the data type per vertex in point-to-point comms, e.g., nPrimvarGrad*nDim.
+   * \brief Routine to allocate buffers for point-to-point MPI communications. Also called to dynamically reallocate if
+   * not enough memory is found for comms during runtime. \param[in] val_countPerPoint - Maximum count of the data type
+   * per vertex in point-to-point comms, e.g., nPrimvarGrad*nDim.
    */
   void AllocateP2PComms(unsigned short val_countPerPoint);
 
@@ -324,8 +366,8 @@ class CGeometry {
    * \param[in] countPerPoint - Number of variables per point.
    * \param[in] val_reverse - Boolean controlling forward or reverse communication between neighbors.
    */
-  void PostP2PRecvs(CGeometry *geometry, const CConfig *config, unsigned short commType,
-                    unsigned short countPerPoint, bool val_reverse) const;
+  void PostP2PRecvs(CGeometry* geometry, const CConfig* config, unsigned short commType, unsigned short countPerPoint,
+                    bool val_reverse) const;
 
   /*!
    * \brief Routine to launch a single non-blocking send once the buffer is loaded for a point-to-point commucation.
@@ -337,19 +379,20 @@ class CGeometry {
    * \param[in] val_iMessage - Index of the message in the order they are stored.
    * \param[in] val_reverse  - Boolean controlling forward or reverse communication between neighbors.
    */
-  void PostP2PSends(CGeometry *geometry, const CConfig *config, unsigned short commType,
-                    unsigned short countPerPoint, int val_iMessage, bool val_reverse) const;
+  void PostP2PSends(CGeometry* geometry, const CConfig* config, unsigned short commType, unsigned short countPerPoint,
+                    int val_iMessage, bool val_reverse) const;
 
   /*!
    * \brief Routine to set up persistent data structures for periodic communications.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void PreprocessPeriodicComms(CGeometry *geometry, CConfig *config);
+  void PreprocessPeriodicComms(CGeometry* geometry, CConfig* config);
 
   /*!
-   * \brief Routine to allocate buffers for periodic communications. Also called to dynamically reallocate if not enough memory is found for comms during runtime.
-   * \param[in] val_countPerPeriodicPoint - Maximum count of the data type per vertex in periodic comms, e.g., nPrimvarGrad*nDim.
+   * \brief Routine to allocate buffers for periodic communications. Also called to dynamically reallocate if not enough
+   * memory is found for comms during runtime. \param[in] val_countPerPeriodicPoint - Maximum count of the data type per
+   * vertex in periodic comms, e.g., nPrimvarGrad*nDim.
    */
   void AllocatePeriodicComms(unsigned short val_countPerPeriodicPoint);
 
@@ -361,7 +404,7 @@ class CGeometry {
    * \param[in] commType - Enumerated type for the quantity to be communicated.
    * \param[in] countPerPeriodicPoint - Number of variables per point.
    */
-  void PostPeriodicRecvs(CGeometry *geometry, const CConfig *config, unsigned short commType,
+  void PostPeriodicRecvs(CGeometry* geometry, const CConfig* config, unsigned short commType,
                          unsigned short countPerPeriodicPoint);
 
   /*!
@@ -373,7 +416,7 @@ class CGeometry {
    * \param[in] countPerPeriodicPoint - Number of variables per point.
    * \param[in] val_iMessage - Index of the message in the order they are stored.
    */
-  void PostPeriodicSends(CGeometry *geometry, const CConfig *config, unsigned short commType,
+  void PostPeriodicSends(CGeometry* geometry, const CConfig* config, unsigned short commType,
                          unsigned short countPerPeriodicPoint, int val_iMessage) const;
 
   /*!
@@ -383,10 +426,8 @@ class CGeometry {
    * \param[out] COUNT_PER_POINT - Number of communicated variables per point.
    * \param[out] MPI_TYPE - Enumerated type for the datatype of the quantity to be communicated.
    */
-  void GetCommCountAndType(const CConfig* config,
-                           unsigned short commType,
-                           unsigned short &COUNT_PER_POINT,
-                           unsigned short &MPI_TYPE) const;
+  void GetCommCountAndType(const CConfig* config, unsigned short commType, unsigned short& COUNT_PER_POINT,
+                           unsigned short& MPI_TYPE) const;
 
   /*!
    * \brief Routine to load a geometric quantity into the data structures for MPI point-to-point communication and to
@@ -395,39 +436,38 @@ class CGeometry {
    * \param[in] config   - Definition of the particular problem.
    * \param[in] commType - Enumerated type for the quantity to be communicated.
    */
-  void InitiateComms(CGeometry *geometry, const CConfig *config, unsigned short commType) const;
+  void InitiateComms(CGeometry* geometry, const CConfig* config, unsigned short commType) const;
 
   /*!
-   * \brief Routine to complete the set of non-blocking communications launched by InitiateComms() and unpacking of the data into the geometry class.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] config   - Definition of the particular problem.
-   * \param[in] commType - Enumerated type for the quantity to be unpacked.
+   * \brief Routine to complete the set of non-blocking communications launched by InitiateComms() and unpacking of the
+   * data into the geometry class. \param[in] geometry - Geometrical definition of the problem. \param[in] config   -
+   * Definition of the particular problem. \param[in] commType - Enumerated type for the quantity to be unpacked.
    */
-  void CompleteComms(CGeometry *geometry, const CConfig *config, unsigned short commType);
+  void CompleteComms(CGeometry* geometry, const CConfig* config, unsigned short commType);
 
   /*!
    * \brief Get number of coordinates.
    * \return Number of coordinates.
    */
-  inline unsigned short GetnDim() const {return nDim;}
+  inline unsigned short GetnDim() const { return nDim; }
 
   /*!
    * \brief Get number of zones.
    * \return Number of zones.
    */
-  inline unsigned short GetnZone() const {return nZone;}
+  inline unsigned short GetnZone() const { return nZone; }
 
   /*!
    * \brief Get number of points.
    * \return Number of points.
    */
-  inline unsigned long GetnPoint() const {return nPoint;}
+  inline unsigned long GetnPoint() const { return nPoint; }
 
   /*!
    * \brief Get number of real points (that belong to the domain).
    * \return Number of real points.
    */
-  inline unsigned long GetnPointDomain() const {return nPointDomain;}
+  inline unsigned long GetnPointDomain() const { return nPointDomain; }
 
   /*!
    * \brief Retrieve total number of nodes in a simulation across all processors (including halos).
@@ -445,26 +485,26 @@ class CGeometry {
    * \brief Get number of elements.
    * \return Number of elements.
    */
-  inline unsigned long GetnElem() const {return nElem;}
+  inline unsigned long GetnElem() const { return nElem; }
 
   /*!
    * \brief Get number of edges.
    * \return Number of edges.
    */
-  inline unsigned long GetnEdge() const {return nEdge;}
+  inline unsigned long GetnEdge() const { return nEdge; }
 
   /*!
    * \brief Get number of markers.
    * \return Number of markers.
    */
-  inline unsigned short GetnMarker() const {return nMarker;}
+  inline unsigned short GetnMarker() const { return nMarker; }
 
   /*!
    * \brief Get number of vertices.
    * \param[in] val_marker - Marker of the boundary.
    * \return Number of vertices.
    */
-  inline const su2double* GetSpanWiseValue(unsigned short val_marker) const { return SpanWiseValue[val_marker-1]; }
+  inline const su2double* GetSpanWiseValue(unsigned short val_marker) const { return SpanWiseValue[val_marker - 1]; }
 
   /*!
    * \brief Get number of vertices.
@@ -478,21 +518,27 @@ class CGeometry {
    * \param[in] marker_flag - flag of the turbomachinery boundary.
    * \return Number of span wise section.
    */
-  inline unsigned short GetnSpanWiseSections(unsigned short marker_flag) const { return nSpanWiseSections[marker_flag -1]; }
+  inline unsigned short GetnSpanWiseSections(unsigned short marker_flag) const {
+    return nSpanWiseSections[marker_flag - 1];
+  }
 
   /*!
    * \brief Get number of vertices.
    * \param[in] val_marker - Marker of the boundary.
    * \return Number of vertices.
    */
-  inline unsigned long GetnVertexSpan(unsigned short val_marker, unsigned short val_span) const { return nVertexSpan[val_marker][val_span]; }
+  inline unsigned long GetnVertexSpan(unsigned short val_marker, unsigned short val_span) const {
+    return nVertexSpan[val_marker][val_span];
+  }
 
   /*!
    * \brief Get number of frequencies per span for NRBC.
    * \param[in] val_marker - Marker of the boundary.
    * \return Number of frequencies for NRBC.
    */
-  inline unsigned long GetnFreqSpan(unsigned short val_marker, unsigned short val_span) const { return (nTotVertexSpan[val_marker][val_span]/2 -1); }
+  inline unsigned long GetnFreqSpan(unsigned short val_marker, unsigned short val_span) const {
+    return (nTotVertexSpan[val_marker][val_span] / 2 - 1);
+  }
 
   /*!
    * \brief Get number of vertices.
@@ -506,14 +552,18 @@ class CGeometry {
    * \param[in] marker_flag - Marker of the boundary.
    * \return Number of frequencies.
    */
-  inline unsigned long GetnFreqSpanMax(unsigned short marker_flag) const { return (nVertexSpanMax[marker_flag]/2 -1); }
+  inline unsigned long GetnFreqSpanMax(unsigned short marker_flag) const {
+    return (nVertexSpanMax[marker_flag] / 2 - 1);
+  }
 
   /*!
    * \brief Get number of vertices.
    * \param[in] val_marker - Marker of the boundary.
    * \return Number of vertices.
    */
-  inline void SetnVertexSpanMax(unsigned short marker_flag, unsigned long nVertMax) {nVertexSpanMax[marker_flag] = nVertMax;}
+  inline void SetnVertexSpanMax(unsigned short marker_flag, unsigned long nVertMax) {
+    nVertexSpanMax[marker_flag] = nVertMax;
+  }
 
   /*!
    * \brief Get the edge index from using the nodes of the edge.
@@ -553,7 +603,8 @@ class CGeometry {
    * \param[in] kCoord - Coordinates of the third point that defines the plane.
    * \return Signed distance.
    */
-  su2double Point2Plane_Distance(const su2double *Coord, const su2double *iCoord, const su2double *jCoord, const su2double *kCoord);
+  su2double Point2Plane_Distance(const su2double* Coord, const su2double* iCoord, const su2double* jCoord,
+                                 const su2double* kCoord);
 
   /*!
    * \brief Create a file for testing the geometry.
@@ -584,7 +635,9 @@ class CGeometry {
    * \param[in] val_marker - Marker of the boundary.
    * \param[in] val_index - Index of the marker.
    */
-  inline void SetMarker_Tag(unsigned short val_marker, string val_index) { Tag_to_Marker[val_marker] = std::move(val_index); }
+  inline void SetMarker_Tag(unsigned short val_marker, string val_index) {
+    Tag_to_Marker[val_marker] = std::move(val_index);
+  }
 
   /*!
    * \brief Set the number of boundary elements.
@@ -592,7 +645,7 @@ class CGeometry {
    * \param[in] val_nelem_bound - Number of boundary elements.
    */
   inline void SetnElem_Bound(unsigned short val_marker, unsigned long val_nelem_bound) {
-    nElem_Bound[val_marker]= val_nelem_bound;
+    nElem_Bound[val_marker] = val_nelem_bound;
   }
 
   /*!
@@ -637,14 +690,16 @@ class CGeometry {
    * \param[in] face_first_elem - Index of the common face for the first element.
    * \param[in] face_second_elem - Index of the common face for the second element.
    */
-  inline virtual bool FindFace(unsigned long first_elem, unsigned long second_elem, unsigned short &face_first_elem,
-                               unsigned short &face_second_elem) {return false;}
+  inline virtual bool FindFace(unsigned long first_elem, unsigned long second_elem, unsigned short& face_first_elem,
+                               unsigned short& face_second_elem) {
+    return false;
+  }
 
   /*!
    * \brief Sets area to be positive in Z direction.
    * \param[in] config - Definition of the particular problem.
    */
-  inline virtual void SetPositive_ZArea(CConfig *config) {}
+  inline virtual void SetPositive_ZArea(CConfig* config) {}
 
   /*!
    * \brief Set connectivity between points.
@@ -655,7 +710,7 @@ class CGeometry {
    * \brief Orders the RCM.
    * \param[in] config - Definition of the particular problem.
    */
-  inline virtual void SetRCM_Ordering(CConfig *config) {}
+  inline virtual void SetRCM_Ordering(CConfig* config) {}
 
   /*!
    * \brief Connects elements  .
@@ -681,7 +736,7 @@ class CGeometry {
    * \brief Sets the vertices.
    * \param[in] config - Definition of the particular problem.
    */
-  inline virtual void SetVertex(const CConfig *config) {}
+  inline virtual void SetVertex(const CConfig* config) {}
 
   /*!
    * \brief Computes the N span.
@@ -690,7 +745,8 @@ class CGeometry {
    * \param[in] marker_flag - Marker being used
    * \param[in] allocate
    */
-  inline virtual void ComputeNSpan(CConfig *config, unsigned short val_iZone, unsigned short marker_flag, bool allocate) {}
+  inline virtual void ComputeNSpan(CConfig* config, unsigned short val_iZone, unsigned short marker_flag,
+                                   bool allocate) {}
 
   /*!
    * \brief Set vertices for turbomachinery problems.
@@ -699,7 +755,8 @@ class CGeometry {
    * \param[in] marker_flag - Marker being used
    * \param[in] allocate
    */
-  inline virtual void SetTurboVertex(CConfig *config, unsigned short val_iZone, unsigned short marker_flag, bool allocate) {}
+  inline virtual void SetTurboVertex(CConfig* config, unsigned short val_iZone, unsigned short marker_flag,
+                                     bool allocate) {}
 
   /*!
    * \brief A virtual member.
@@ -707,7 +764,7 @@ class CGeometry {
    * \param[in] val_iZone - Zone of the problem
    * \param[in] marker_flag - Marker being used
    */
-  inline virtual void UpdateTurboVertex(CConfig *config, unsigned short val_iZone, unsigned short marker_flag) {}
+  inline virtual void UpdateTurboVertex(CConfig* config, unsigned short val_iZone, unsigned short marker_flag) {}
 
   /*!
    * \brief A virtual member.
@@ -716,14 +773,15 @@ class CGeometry {
    * \param[in] marker_flag - Marker being used
    * \param[in] allocate
    */
-  inline virtual void SetAvgTurboValue(CConfig *config, unsigned short val_iZone, unsigned short marker_flag, bool allocate) {}
+  inline virtual void SetAvgTurboValue(CConfig* config, unsigned short val_iZone, unsigned short marker_flag,
+                                       bool allocate) {}
 
   /*!
    * \brief A virtual member.
    * \param[in] config - Definition of the particular problem.
    * \param[in] allocate
    */
-  inline virtual void GatherInOutAverageValues(CConfig *config, bool allocate) {}
+  inline virtual void GatherInOutAverageValues(CConfig* config, bool allocate) {}
 
   /*!
    * \brief Set max length.
@@ -736,32 +794,32 @@ class CGeometry {
    * \param[in] config - Definition of the particular problem.
    * \param[in] action - Allocate or not the new elements.
    */
-  inline virtual void SetControlVolume(CConfig *config, unsigned short action) {}
+  inline virtual void SetControlVolume(CConfig* config, unsigned short action) {}
 
   /*!
    * \brief A virtual member.
    * \param[in] config - Definition of the particular problem.
    */
-  inline virtual void VisualizeControlVolume(const CConfig *config) const {}
+  inline virtual void VisualizeControlVolume(const CConfig* config) const {}
 
   /*!
    * \brief A virtual member.
    * \param[in] config - Definition of the particular problem.
    */
-  inline virtual void MatchActuator_Disk(const CConfig *config) {}
+  inline virtual void MatchActuator_Disk(const CConfig* config) {}
 
   /*!
    * \brief A virtual member.
    * \param[in] config - Definition of the particular problem.
    */
-  inline virtual void MatchPeriodic(const CConfig *config, unsigned short val_periodic) {}
+  inline virtual void MatchPeriodic(const CConfig* config, unsigned short val_periodic) {}
 
   /*!
    * \brief A virtual member.
    * \param[in] config - Definition of the particular problem.
    * \param[in] action - Allocate or not the new elements.
    */
-  inline virtual void SetBoundControlVolume(const CConfig *config, unsigned short action) {}
+  inline virtual void SetBoundControlVolume(const CConfig* config, unsigned short action) {}
 
   /*!
    * \brief A virtual member.
@@ -775,43 +833,43 @@ class CGeometry {
    * \param[in] new_file - Boolean to decide if aopen a new file or add to a old one
    * \param[in] config - Definition of the particular problem.
    */
-  inline virtual void SetBoundTecPlot(char mesh_filename[MAX_STRING_SIZE], bool new_file, CConfig *config) {}
+  inline virtual void SetBoundTecPlot(char mesh_filename[MAX_STRING_SIZE], bool new_file, CConfig* config) {}
 
   /*!
    * \brief A virtual member.
    * \param[in] config - Definition of the particular problem.
    */
-  inline virtual void Check_IntElem_Orientation(const CConfig *config) {}
+  inline virtual void Check_IntElem_Orientation(const CConfig* config) {}
 
   /*!
    * \brief A virtual member.
    * \param[in] config - Definition of the particular problem.
    */
-  inline virtual void Check_BoundElem_Orientation(const CConfig *config) {}
+  inline virtual void Check_BoundElem_Orientation(const CConfig* config) {}
 
   /*!
    * \brief A virtual member.
    * \param[in] config - Definition of the particular problem.
    */
-  inline virtual void SetColorGrid(CConfig *config) {}
+  inline virtual void SetColorGrid(CConfig* config) {}
 
   /*!
    * \brief A virtual member.
    * \param[in] config - Definition of the particular problem.
    */
-  inline virtual void SetColorGrid_Parallel(const CConfig *config) {}
+  inline virtual void SetColorGrid_Parallel(const CConfig* config) {}
 
   /*!
    * \brief A virtual member.
    * \param[in] config - Definition of the particular problem.
    */
-  inline virtual void SetColorFEMGrid_Parallel(CConfig *config) {}
+  inline virtual void SetColorFEMGrid_Parallel(CConfig* config) {}
 
   /*!
    * \brief A virtual member.
    * \param[in] config - Definition of the particular problem.
    */
-  inline virtual void DivideConnectivity(CConfig *config, unsigned short Elem_Type) {}
+  inline virtual void DivideConnectivity(CConfig* config, unsigned short Elem_Type) {}
 
   /*!
    * \brief A virtual member.
@@ -819,7 +877,7 @@ class CGeometry {
    * \param[in] config - Definition of the particular problem.
    * \param[in] val_domain - Number of domains for parallelization purposes.
    */
-  inline virtual void SetSendReceive(const CConfig *config) {}
+  inline virtual void SetSendReceive(const CConfig* config) {}
 
   /*!
    * \brief A virtual member.
@@ -827,27 +885,27 @@ class CGeometry {
    * \param[in] config - Definition of the particular problem.
    * \param[in] val_domain - Number of domains for parallelization purposes.
    */
-  inline virtual void SetBoundaries(CConfig *config) {}
+  inline virtual void SetBoundaries(CConfig* config) {}
 
   /*!
    * \brief A virtual member.
    * \param[in] fine_grid - Geometrical definition of the problem.
    */
-  inline virtual void SetCoord(const CGeometry *fine_grid) {}
+  inline virtual void SetCoord(const CGeometry* fine_grid) {}
 
   /*!
    * \brief A virtual member.
    * \param[in] fine_grid - Geometrical definition of the problem.
    * \param[in] val_marker - Index of the boundary marker.
    */
-  inline virtual void SetMultiGridWallHeatFlux(const CGeometry *fine_grid, unsigned short val_marker) {}
+  inline virtual void SetMultiGridWallHeatFlux(const CGeometry* fine_grid, unsigned short val_marker) {}
 
   /*!
    * \brief A virtual member.
    * \param[in] fine_grid - Geometrical definition of the problem.
    * \param[in] val_marker - Index of the boundary marker.
    */
-  inline virtual void SetMultiGridWallTemperature(const CGeometry *fine_grid, unsigned short val_marker) {}
+  inline virtual void SetMultiGridWallTemperature(const CGeometry* fine_grid, unsigned short val_marker) {}
 
   /*!
    * \brief A virtual member.
@@ -855,99 +913,99 @@ class CGeometry {
    * \param[in] val_smooth_coeff - Relaxation factor.
    * \param[in] config - Definition of the particular problem.
    */
-  inline virtual void SetCoord_Smoothing(unsigned short val_nSmooth, su2double val_smooth_coeff, CConfig *config) {}
+  inline virtual void SetCoord_Smoothing(unsigned short val_nSmooth, su2double val_smooth_coeff, CConfig* config) {}
 
   /*!
    * \brief A virtual member.
    * \param[in] fine_grid - Geometrical definition of the child grid (for multigrid).
    */
-  inline virtual void SetPoint_Connectivity(const CGeometry *fine_grid) {}
+  inline virtual void SetPoint_Connectivity(const CGeometry* fine_grid) {}
 
   /*!
    * \brief A virtual member.
    * \param[in] fine_grid - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  inline virtual void SetVertex(const CGeometry *fine_grid, const CConfig *config) {}
+  inline virtual void SetVertex(const CGeometry* fine_grid, const CConfig* config) {}
 
   /*!
    * \brief A virtual member.
    * \param[in] fine_grid - Geometrical definition of the problem.
    * \param[in] action - Allocate or not the new elements.
    */
-  inline virtual void SetControlVolume(const CGeometry *fine_grid, unsigned short action) {}
+  inline virtual void SetControlVolume(const CGeometry* fine_grid, unsigned short action) {}
 
   /*!
    * \brief A virtual member.
    * \param[in] fine_grid - Geometrical definition of the problem.
    * \param[in] action - Allocate or not the new elements.
    */
-  inline virtual void SetBoundControlVolume(const CGeometry *fine_grid, unsigned short action) {}
+  inline virtual void SetBoundControlVolume(const CGeometry* fine_grid, unsigned short action) {}
 
   /*!
    * \brief A virtual member.
    * \param[in] config - Definition of the particular problem.
    */
-  inline virtual void SetBoundSensitivity(CConfig *config) {}
+  inline virtual void SetBoundSensitivity(CConfig* config) {}
 
   /*!
    * \brief Set the data containers for customized boundary conditions.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetCustomBoundary(CConfig *config);
+  void SetCustomBoundary(CConfig* config);
 
   /*!
    * \brief Set cartesian grid velocity based on rotational speed and axis.
    * \param[in] config - Definition of the particular problem.
    * \param[in] print - Display information on screen.
    */
-  void SetRotationalVelocity(const CConfig *config, bool print = false);
+  void SetRotationalVelocity(const CConfig* config, bool print = false);
 
   /*!
    * \brief Set the rotational velocity of the points on the shroud markers to 0.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetShroudVelocity(const CConfig *config);
+  void SetShroudVelocity(const CConfig* config);
 
   /*!
    * \brief Set the translational velocity at each node.
    * \param[in] config - Definition of the particular problem.
    * \param[in] print - Display information on screen.
    */
-  void SetTranslationalVelocity(const CConfig *config, bool print = false);
+  void SetTranslationalVelocity(const CConfig* config, bool print = false);
 
   /*!
    * \brief Set the translational/rotational velocity for all moving walls.
    * \param[in] config - Definition of the particular problem.
    * \param[in] print - Display information on screen.
    */
-  void SetWallVelocity(const CConfig *config, bool print = false);
+  void SetWallVelocity(const CConfig* config, bool print = false);
 
   /*!
    * \brief Set the grid velocity via finite differencing at each node.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetGridVelocity(const CConfig *config);
+  void SetGridVelocity(const CConfig* config);
 
   /*!
    * \brief A virtual member.
    * \param[in] fine_grid - Geometry of the fine mesh.
    */
-  inline virtual void SetRestricted_GridVelocity(const CGeometry *fine_grid) {}
+  inline virtual void SetRestricted_GridVelocity(const CGeometry* fine_grid) {}
 
   /*!
    * \brief Compute the surface area of all global markers.
    * \param[in] config - Definition of the particular problem.
    */
-  void ComputeSurfaceAreaCfgFile(const CConfig *config);
+  void ComputeSurfaceAreaCfgFile(const CConfig* config);
 
   /*!
-  * \brief Get global Surface Area to a local marker.
-  * \param[in] config - Definition of the particular problem.
-  * \param[in] val_marker - Local surface marker.
-  * \return Global Surface Area to the local marker
-  */
-  su2double GetSurfaceArea(const CConfig *config, unsigned short val_marker) const;
+   * \brief Get global Surface Area to a local marker.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] val_marker - Local surface marker.
+   * \return Global Surface Area to the local marker
+   */
+  su2double GetSurfaceArea(const CConfig* config, unsigned short val_marker) const;
 
   /*!
    * \brief Check if a boundary is straight(2D) / plane(3D) for EULER_WALL and SYMMETRY_PLANE
@@ -956,147 +1014,172 @@ class CGeometry {
    * \param[in] config - Definition of the particular problem.
    * \param[in] print_on_screen - Boolean whether to print result on screen.
    */
-  void ComputeSurf_Straightness(CConfig *config, bool print_on_screen);
+  void ComputeSurf_Straightness(CConfig* config, bool print_on_screen);
 
   /*!
    * \brief Find and store all vertices on a sharp corner in the geometry.
    * \param[in] config - Definition of the particular problem.
    */
-  void ComputeSurf_Curvature(CConfig *config);
+  void ComputeSurf_Curvature(CConfig* config);
 
   /*!
    * \brief A virtual member.
    * \param[in] config - Definition of the particular problem.
    */
-  void ComputeAirfoil_Section(su2double *Plane_P0, su2double *Plane_Normal,
-                              su2double MinXCoord, su2double MaxXCoord,
-                              su2double MinYCoord, su2double MaxYCoord,
-                              su2double MinZCoord, su2double MaxZCoord,
-                              const su2double *FlowVariable,
-                              vector<su2double> &Xcoord_Airfoil, vector<su2double> &Ycoord_Airfoil,
-                              vector<su2double> &Zcoord_Airfoil, vector<su2double> &Variable_Airfoil,
-                              bool original_surface, CConfig *config);
+  void ComputeAirfoil_Section(su2double* Plane_P0, su2double* Plane_Normal, su2double MinXCoord, su2double MaxXCoord,
+                              su2double MinYCoord, su2double MaxYCoord, su2double MinZCoord, su2double MaxZCoord,
+                              const su2double* FlowVariable, vector<su2double>& Xcoord_Airfoil,
+                              vector<su2double>& Ycoord_Airfoil, vector<su2double>& Zcoord_Airfoil,
+                              vector<su2double>& Variable_Airfoil, bool original_surface, CConfig* config);
 
   /*!
    * \brief A virtual member.
    */
-  virtual su2double Compute_MaxThickness(su2double *Plane_P0, su2double *Plane_Normal, CConfig *config, vector<su2double> &Xcoord_Airfoil,
-                                         vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) {return 0.0;}
+  virtual su2double Compute_MaxThickness(su2double* Plane_P0, su2double* Plane_Normal, CConfig* config,
+                                         vector<su2double>& Xcoord_Airfoil, vector<su2double>& Ycoord_Airfoil,
+                                         vector<su2double>& Zcoord_Airfoil) {
+    return 0.0;
+  }
 
   /*!
    * \brief A virtual member.
    */
-  virtual su2double Compute_Twist(su2double *Plane_P0, su2double *Plane_Normal, vector<su2double> &Xcoord_Airfoil,
-                                  vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) {return 0.0;}
+  virtual su2double Compute_Twist(su2double* Plane_P0, su2double* Plane_Normal, vector<su2double>& Xcoord_Airfoil,
+                                  vector<su2double>& Ycoord_Airfoil, vector<su2double>& Zcoord_Airfoil) {
+    return 0.0;
+  }
 
   /*!
    * \brief A virtual member.
    */
-  virtual su2double Compute_Chord(su2double *Plane_P0, su2double *Plane_Normal, vector<su2double> &Xcoord_Airfoil,
-                                  vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) {return 0.0;}
+  virtual su2double Compute_Chord(su2double* Plane_P0, su2double* Plane_Normal, vector<su2double>& Xcoord_Airfoil,
+                                  vector<su2double>& Ycoord_Airfoil, vector<su2double>& Zcoord_Airfoil) {
+    return 0.0;
+  }
 
   /*!
    * \brief A virtual member.
    */
-  virtual su2double Compute_Width(su2double *Plane_P0, su2double *Plane_Normal, vector<su2double> &Xcoord_Airfoil,
-                                  vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) {return 0.0;}
+  virtual su2double Compute_Width(su2double* Plane_P0, su2double* Plane_Normal, vector<su2double>& Xcoord_Airfoil,
+                                  vector<su2double>& Ycoord_Airfoil, vector<su2double>& Zcoord_Airfoil) {
+    return 0.0;
+  }
 
   /*!
    * \brief A virtual member.
    */
-  virtual su2double Compute_WaterLineWidth(su2double *Plane_P0, su2double *Plane_Normal, CConfig *config, vector<su2double> &Xcoord_Airfoil,
-                                           vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) {return 0.0;}
+  virtual su2double Compute_WaterLineWidth(su2double* Plane_P0, su2double* Plane_Normal, CConfig* config,
+                                           vector<su2double>& Xcoord_Airfoil, vector<su2double>& Ycoord_Airfoil,
+                                           vector<su2double>& Zcoord_Airfoil) {
+    return 0.0;
+  }
 
   /*!
    * \brief A virtual member.
    */
-  virtual su2double Compute_Height(su2double *Plane_P0, su2double *Plane_Normal, vector<su2double> &Xcoord_Airfoil,
-                                   vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) {return 0.0;}
+  virtual su2double Compute_Height(su2double* Plane_P0, su2double* Plane_Normal, vector<su2double>& Xcoord_Airfoil,
+                                   vector<su2double>& Ycoord_Airfoil, vector<su2double>& Zcoord_Airfoil) {
+    return 0.0;
+  }
 
   /*!
    * \brief A virtual member.
    */
-  virtual su2double Compute_LERadius(su2double *Plane_P0, su2double *Plane_Normal, vector<su2double> &Xcoord_Airfoil,
-                                     vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) {return 0.0;}
+  virtual su2double Compute_LERadius(su2double* Plane_P0, su2double* Plane_Normal, vector<su2double>& Xcoord_Airfoil,
+                                     vector<su2double>& Ycoord_Airfoil, vector<su2double>& Zcoord_Airfoil) {
+    return 0.0;
+  }
 
   /*!
    * \brief A virtual member.
    */
-  virtual su2double Compute_Thickness(su2double *Plane_P0, su2double *Plane_Normal, su2double Location, CConfig *config,
-                                      vector<su2double> &Xcoord_Airfoil, vector<su2double> &Ycoord_Airfoil,
-                                      vector<su2double> &Zcoord_Airfoil, su2double &ZLoc) {return 0.0;}
+  virtual su2double Compute_Thickness(su2double* Plane_P0, su2double* Plane_Normal, su2double Location, CConfig* config,
+                                      vector<su2double>& Xcoord_Airfoil, vector<su2double>& Ycoord_Airfoil,
+                                      vector<su2double>& Zcoord_Airfoil, su2double& ZLoc) {
+    return 0.0;
+  }
 
   /*!
    * \brief A virtual member.
    */
-  virtual su2double Compute_Area(su2double *Plane_P0, su2double *Plane_Normal, CConfig *config, vector<su2double> &Xcoord_Airfoil,
-                                 vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) {return 0.0;}
+  virtual su2double Compute_Area(su2double* Plane_P0, su2double* Plane_Normal, CConfig* config,
+                                 vector<su2double>& Xcoord_Airfoil, vector<su2double>& Ycoord_Airfoil,
+                                 vector<su2double>& Zcoord_Airfoil) {
+    return 0.0;
+  }
 
   /*!
    * \brief A virtual member.
    */
-  virtual su2double Compute_Length(su2double *Plane_P0, su2double *Plane_Normal, CConfig *config, vector<su2double> &Xcoord_Airfoil,
-                                   vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) {return 0.0;}
+  virtual su2double Compute_Length(su2double* Plane_P0, su2double* Plane_Normal, CConfig* config,
+                                   vector<su2double>& Xcoord_Airfoil, vector<su2double>& Ycoord_Airfoil,
+                                   vector<su2double>& Zcoord_Airfoil) {
+    return 0.0;
+  }
 
   /*!
    * \brief A virtual member.
    */
-  virtual void Compute_Wing_LeadingTrailing(su2double *LeadingEdge, su2double *TrailingEdge, su2double *Plane_P0, su2double *Plane_Normal, vector<su2double>
-                                            &Xcoord_Airfoil, vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) {}
+  virtual void Compute_Wing_LeadingTrailing(su2double* LeadingEdge, su2double* TrailingEdge, su2double* Plane_P0,
+                                            su2double* Plane_Normal, vector<su2double>& Xcoord_Airfoil,
+                                            vector<su2double>& Ycoord_Airfoil, vector<su2double>& Zcoord_Airfoil) {}
 
   /*!
    * \brief A virtual member.
    */
-  virtual void Compute_Fuselage_LeadingTrailing(su2double *LeadingEdge, su2double *TrailingEdge, su2double *Plane_P0, su2double *Plane_Normal, vector<su2double>
-                                                &Xcoord_Airfoil, vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) {}
+  virtual void Compute_Fuselage_LeadingTrailing(su2double* LeadingEdge, su2double* TrailingEdge, su2double* Plane_P0,
+                                                su2double* Plane_Normal, vector<su2double>& Xcoord_Airfoil,
+                                                vector<su2double>& Ycoord_Airfoil, vector<su2double>& Zcoord_Airfoil) {}
 
   /*!
    * \brief A virtual member.
    */
-  virtual su2double Compute_Dihedral(su2double *LeadingEdge_im1, su2double *TrailingEdge_im1,
-                                     su2double *LeadingEdge_i, su2double *TrailingEdge_i) {return 0.0;}
+  virtual su2double Compute_Dihedral(su2double* LeadingEdge_im1, su2double* TrailingEdge_im1, su2double* LeadingEdge_i,
+                                     su2double* TrailingEdge_i) {
+    return 0.0;
+  }
 
   /*!
    * \brief A virtual member.
    */
-  virtual su2double Compute_Curvature(su2double *LeadingEdge_im1, su2double *TrailingEdge_im1,
-                                      su2double *LeadingEdge_i, su2double *TrailingEdge_i,
-                                      su2double *LeadingEdge_ip1, su2double *TrailingEdge_ip1) {return 0.0;}
+  virtual su2double Compute_Curvature(su2double* LeadingEdge_im1, su2double* TrailingEdge_im1, su2double* LeadingEdge_i,
+                                      su2double* TrailingEdge_i, su2double* LeadingEdge_ip1,
+                                      su2double* TrailingEdge_ip1) {
+    return 0.0;
+  }
 
   /*!
    * \brief A virtual member.
    */
-  virtual void Compute_Wing(CConfig *config, bool original_surface,
-                            su2double &Wing_Volume, su2double &Wing_MinMaxThickness, su2double &Wing_MaxMaxThickness, su2double &Wing_MinChord, su2double &Wing_MaxChord,
-                            su2double &Wing_MinLERadius, su2double &Wing_MaxLERadius,
-                            su2double &Wing_MinToC, su2double &Wing_MaxToC, su2double &Wing_ObjFun_MinToC, su2double &Wing_MaxTwist, su2double &Wing_MaxCurvature,
-                            su2double &Wing_MaxDihedral) {}
+  virtual void Compute_Wing(CConfig* config, bool original_surface, su2double& Wing_Volume,
+                            su2double& Wing_MinMaxThickness, su2double& Wing_MaxMaxThickness, su2double& Wing_MinChord,
+                            su2double& Wing_MaxChord, su2double& Wing_MinLERadius, su2double& Wing_MaxLERadius,
+                            su2double& Wing_MinToC, su2double& Wing_MaxToC, su2double& Wing_ObjFun_MinToC,
+                            su2double& Wing_MaxTwist, su2double& Wing_MaxCurvature, su2double& Wing_MaxDihedral) {}
 
   /*!
    * \brief A virtual member.
    */
-  virtual void Compute_Fuselage(CConfig *config, bool original_surface,
-                                su2double &Fuselage_Volume, su2double &Fuselage_WettedArea,
-                                su2double &Fuselage_MinWidth, su2double &Fuselage_MaxWidth,
-                                su2double &Fuselage_MinWaterLineWidth, su2double &Fuselage_MaxWaterLineWidth,
-                                su2double &Fuselage_MinHeight, su2double &Fuselage_MaxHeight,
-                                su2double &Fuselage_MaxCurvature) {}
+  virtual void Compute_Fuselage(CConfig* config, bool original_surface, su2double& Fuselage_Volume,
+                                su2double& Fuselage_WettedArea, su2double& Fuselage_MinWidth,
+                                su2double& Fuselage_MaxWidth, su2double& Fuselage_MinWaterLineWidth,
+                                su2double& Fuselage_MaxWaterLineWidth, su2double& Fuselage_MinHeight,
+                                su2double& Fuselage_MaxHeight, su2double& Fuselage_MaxCurvature) {}
 
   /*!
    * \brief A virtual member.
    */
-  virtual void Compute_Nacelle(CConfig *config, bool original_surface,
-                               su2double &Nacelle_Volume, su2double &Nacelle_MinMaxThickness, su2double &Nacelle_MaxMaxThickness,
-                               su2double &Nacelle_MinChord, su2double &Nacelle_MaxChord,
-                               su2double &Nacelle_MinLERadius, su2double &Nacelle_MaxLERadius,
-                               su2double &Nacelle_MinToC, su2double &Nacelle_MaxToC,
-                               su2double &Nacelle_ObjFun_MinToC, su2double &Nacelle_MaxTwist) {}
+  virtual void Compute_Nacelle(CConfig* config, bool original_surface, su2double& Nacelle_Volume,
+                               su2double& Nacelle_MinMaxThickness, su2double& Nacelle_MaxMaxThickness,
+                               su2double& Nacelle_MinChord, su2double& Nacelle_MaxChord, su2double& Nacelle_MinLERadius,
+                               su2double& Nacelle_MaxLERadius, su2double& Nacelle_MinToC, su2double& Nacelle_MaxToC,
+                               su2double& Nacelle_ObjFun_MinToC, su2double& Nacelle_MaxTwist) {}
 
   /*!
    * \brief A virtual member.
    * \param[in] config - Definition of the particular problem.
    */
-  inline virtual void FindNormal_Neighbor(const CConfig *config) {}
+  inline virtual void FindNormal_Neighbor(const CConfig* config) {}
 
   /*!
    * \brief A virtual member.
@@ -1209,22 +1292,22 @@ class CGeometry {
   /*!
    * \brief Get x coords of geometrical planes in the mesh
    */
-  inline vector<vector<su2double> > GetXCoord() const {return Xcoord_plane;}
+  inline vector<vector<su2double>> GetXCoord() const { return Xcoord_plane; }
 
   /*!
    * \brief Get y coords of geometrical planes in the mesh
    */
-  inline vector<vector<su2double> > GetYCoord() const {return Ycoord_plane;}
+  inline vector<vector<su2double>> GetYCoord() const { return Ycoord_plane; }
 
   /*!
    * \brief Get z coords of geometrical planes in the mesh
    */
-  inline vector<vector<su2double> > GetZCoord() const {return Zcoord_plane;}
+  inline vector<vector<su2double>> GetZCoord() const { return Zcoord_plane; }
 
   /*!
    * \brief Get all points on a geometrical plane in the mesh
    */
-  inline vector<vector<unsigned long> > GetPlanarPoints() const {return Plane_points;}
+  inline vector<vector<unsigned long>> GetPlanarPoints() const { return Plane_points; }
 
   /*!
    * \brief Compute the intersection between a segment and a plane.
@@ -1235,26 +1318,27 @@ class CGeometry {
    * \param[in] Intersection - Definition of the particular problem.
    * \return If the intersection has has been successful.
    */
-  bool SegmentIntersectsPlane(const su2double *Segment_P0, const su2double *Segment_P1, su2double Variable_P0, su2double Variable_P1,
-                              const su2double *Plane_P0, const su2double *Plane_Normal, su2double *Intersection, su2double &Variable_Interp);
+  bool SegmentIntersectsPlane(const su2double* Segment_P0, const su2double* Segment_P1, su2double Variable_P0,
+                              su2double Variable_P1, const su2double* Plane_P0, const su2double* Plane_Normal,
+                              su2double* Intersection, su2double& Variable_Interp);
 
   /*!
    * \brief Ray Intersects Triangle (Moller and Trumbore algorithm)
    */
-  bool RayIntersectsTriangle(const su2double orig[3], const su2double dir[3],
-                             const su2double vert0[3], const su2double vert1[3], const su2double vert2[3],
-                             su2double *intersect);
+  bool RayIntersectsTriangle(const su2double orig[3], const su2double dir[3], const su2double vert0[3],
+                             const su2double vert1[3], const su2double vert2[3], su2double* intersect);
 
   /*!
    * \brief Segment Intersects Triangle
    */
-  bool SegmentIntersectsTriangle(su2double point0[3], const su2double point1[3],
-                                 su2double vert0[3], su2double vert1[3], su2double vert2[3]);
+  bool SegmentIntersectsTriangle(su2double point0[3], const su2double point1[3], su2double vert0[3], su2double vert1[3],
+                                 su2double vert2[3]);
 
   /*!
    * \brief Segment Intersects Line (for 2D FFD Intersection)
    */
-  bool SegmentIntersectsLine(const su2double point0[2], const su2double point1[2], const su2double vert0[2], const su2double vert1[2]);
+  bool SegmentIntersectsLine(const su2double point0[2], const su2double point1[2], const su2double vert0[2],
+                             const su2double vert1[2]);
 
   /*!
    * \brief Register the coordinates of the mesh nodes.
@@ -1266,33 +1350,33 @@ class CGeometry {
    * \param geometry_container - Geometrical definition.
    * \param config - Config
    */
-  static void UpdateGeometry(CGeometry **geometry_container, CConfig *config);
+  static void UpdateGeometry(CGeometry** geometry_container, CConfig* config);
 
   /*!
    * \brief Update the multi-grid structure for the customized boundary conditions
    * \param geometry_container - Geometrical definition.
    * \param config - Definition of the particular problem.
    */
-  void UpdateCustomBoundaryConditions(CGeometry **geometry_container, CConfig *config);
+  void UpdateCustomBoundaryConditions(CGeometry** geometry_container, CConfig* config);
 
   /*!
    * \brief A virtual member.
    * \param config - Config
    */
-  inline virtual void SetSensitivity(CConfig *config) {}
+  inline virtual void SetSensitivity(CConfig* config) {}
 
   /*!
    * \brief A virtual member.
    * \param config - Config
    */
-  inline virtual void ReadUnorderedSensitivity(CConfig *config) {}
+  inline virtual void ReadUnorderedSensitivity(CConfig* config) {}
 
   /*!
    * \brief A virtual member.
    * \param iPoint - Point
    * \param iDim - Dimension
    */
-  inline virtual su2double GetSensitivity(unsigned long iPoint, unsigned short iDim) const {return 0.0;}
+  inline virtual su2double GetSensitivity(unsigned long iPoint, unsigned short iDim) const { return 0.0; }
 
   /*!
    * \brief A virtual member.
@@ -1515,7 +1599,7 @@ class CGeometry {
    * \brief A virtual member.
    * \param config - Config
    */
-  inline virtual void Check_Periodicity(CConfig *config) {}
+  inline virtual void Check_Periodicity(CConfig* config) {}
 
   /*!
    * \brief Get the value of the customized temperature at a specified vertex on a specified marker.
@@ -1532,7 +1616,8 @@ class CGeometry {
    * \param[in] val_vertex - Boundary vertex value
    * \param[in] val_customBoundaryTemperature - Value of the temperature.
    */
-  inline void SetCustomBoundaryTemperature(unsigned short val_marker, unsigned long val_vertex, su2double val_customBoundaryTemperature) {
+  inline void SetCustomBoundaryTemperature(unsigned short val_marker, unsigned long val_vertex,
+                                           su2double val_customBoundaryTemperature) {
     CustomBoundaryTemperature[val_marker][val_vertex] = val_customBoundaryTemperature;
   }
 
@@ -1551,7 +1636,8 @@ class CGeometry {
    * \param[in] val_vertex - Boundary vertex value
    * \param[in] val_customBoundaryHeatFlux - Value of the normal heat flux.
    */
-  inline void SetCustomBoundaryHeatFlux(unsigned short val_marker, unsigned long val_vertex, su2double val_customBoundaryHeatFlux) {
+  inline void SetCustomBoundaryHeatFlux(unsigned short val_marker, unsigned long val_vertex,
+                                        su2double val_customBoundaryHeatFlux) {
     CustomBoundaryHeatFlux[val_marker][val_vertex] = val_customBoundaryHeatFlux;
   }
 
@@ -1559,12 +1645,12 @@ class CGeometry {
    * \brief Filter values given at the element CG by performing a weighted average over a radial neighbourhood.
    * \param[in] filter_radius - Parameter defining the size of the neighbourhood.
    * \param[in] kernels - Kernel types and respective parameter, size of vector defines number of filter recursions.
-   * \param[in] search_limit - Max degree of neighborhood considered for neighbor search, avoids excessive work in fine regions.
-   * \param[in,out] values - On entry, the "raw" values, on exit, the filtered values.
+   * \param[in] search_limit - Max degree of neighborhood considered for neighbor search, avoids excessive work in fine
+   * regions. \param[in,out] values - On entry, the "raw" values, on exit, the filtered values.
    */
-  void FilterValuesAtElementCG(const vector<su2double> &filter_radius,
-                               const vector<pair<ENUM_FILTER_KERNEL,su2double> > &kernels,
-                               const unsigned short search_limit, su2double *values) const;
+  void FilterValuesAtElementCG(const vector<su2double>& filter_radius,
+                               const vector<pair<ENUM_FILTER_KERNEL, su2double>>& kernels,
+                               const unsigned short search_limit, su2double* values) const;
 
   /*!
    * \brief Build the global (entire mesh!) adjacency matrix for the elements in compressed format.
@@ -1573,23 +1659,21 @@ class CGeometry {
    *             neighbours of global element "i". Size nElemDomain+1
    * \param[out] neighbour_idx - Global index of the neighbours, mush be NULL on entry and free'd by calling function.
    */
-  void GetGlobalElementAdjacencyMatrix(vector<unsigned long> &neighbour_start, long *&neighbour_idx) const;
+  void GetGlobalElementAdjacencyMatrix(vector<unsigned long>& neighbour_start, long*& neighbour_idx) const;
 
   /*!
-   * \brief Get the neighbours of the global element in the first position of "neighbours" that are within "radius" of it.
-   * \param[in] iElem_global - Element of interest.
-   * \param[in] radius - Parameter defining the size of the neighbourhood.
-   * \param[in] search_limit - Maximum "logical radius" to consider, limits cost in refined regions, use 0 for unlimited.
-   * \param[in] neighbour_start - See GetGlobalElementAdjacencyMatrix.
-   * \param[in] neighbour_idx - See GetGlobalElementAdjacencyMatrix.
-   * \param[in] cg_elem - Global element centroid coordinates in row major format {x0,y0,x1,y1,...}. Size nDim*nElemDomain.
-   * \param[in,out] neighbours - The neighbours of iElem_global.
-   * \param[in,out] is_neighbor - Working vector of size nElemGlobal, MUST be all false on entry (if so, on exit it will be the same).
-   * \return true if the search was successful, i.e. not limited.
+   * \brief Get the neighbours of the global element in the first position of "neighbours" that are within "radius" of
+   * it. \param[in] iElem_global - Element of interest. \param[in] radius - Parameter defining the size of the
+   * neighbourhood. \param[in] search_limit - Maximum "logical radius" to consider, limits cost in refined regions, use
+   * 0 for unlimited. \param[in] neighbour_start - See GetGlobalElementAdjacencyMatrix. \param[in] neighbour_idx - See
+   * GetGlobalElementAdjacencyMatrix. \param[in] cg_elem - Global element centroid coordinates in row major format
+   * {x0,y0,x1,y1,...}. Size nDim*nElemDomain. \param[in,out] neighbours - The neighbours of iElem_global.
+   * \param[in,out] is_neighbor - Working vector of size nElemGlobal, MUST be all false on entry (if so, on exit it will
+   * be the same). \return true if the search was successful, i.e. not limited.
    */
   bool GetRadialNeighbourhood(const unsigned long iElem_global, const passivedouble radius, size_t search_limit,
-                              const vector<unsigned long> &neighbour_start, const long *neighbour_idx,
-                              const su2double *cg_elem, vector<long> &neighbours, vector<bool> &is_neighbor) const;
+                              const vector<unsigned long>& neighbour_start, const long* neighbour_idx,
+                              const su2double* cg_elem, vector<long>& neighbours, vector<bool>& is_neighbor) const;
 
   /*!
    * \brief Compute and store the volume of the primal elements.
@@ -1612,7 +1696,7 @@ class CGeometry {
    * \brief A virtual member.
    * \param config - Config
    */
-  inline virtual void ComputeMeshQualityStatistics(const CConfig *config) {}
+  inline virtual void ComputeMeshQualityStatistics(const CConfig* config) {}
 
   /*!
    * \brief Color multigrid levels for visualization.
@@ -1692,7 +1776,7 @@ class CGeometry {
    * \param[in] config - Definition of the particular problem.
    * \return pointer to the ADT
    */
-  virtual std::unique_ptr<CADTElemClass> ComputeViscousWallADT(const CConfig *config) const { return nullptr; }
+  virtual std::unique_ptr<CADTElemClass> ComputeViscousWallADT(const CConfig* config) const { return nullptr; }
 
   /*!
    * \brief Reduce the wall distance based on an previously constructed ADT.
@@ -1702,7 +1786,8 @@ class CGeometry {
    * \param[in] config - Config of this geometry (not the ADT zone's geometry)
    * \param[in] iZone - Zone whose markers made the ADT
    */
-  virtual void SetWallDistance(CADTElemClass* WallADT, const CConfig* config, unsigned short iZone = numeric_limits<unsigned short>::max()) {}
+  virtual void SetWallDistance(CADTElemClass* WallADT, const CConfig* config,
+                               unsigned short iZone = numeric_limits<unsigned short>::max()) {}
 
   /*!
    * \brief Set wall distances a specific value
@@ -1715,25 +1800,25 @@ class CGeometry {
    * \param[in] config_container - Definition of the particular problem.
    * \param[in] geometry_container - Geometrical definition of the problem.
    */
-  static void ComputeWallDistance(const CConfig * const *config_container, CGeometry ****geometry_container);
+  static void ComputeWallDistance(const CConfig* const* config_container, CGeometry**** geometry_container);
 
   /*!
    * \brief Set the amount of nonconvex elements in the mesh.
    * \param[in] nonconvex_elems - amount of nonconvex elements in the mesh
    */
-  void SetnNonconvexElements(unsigned long nonconvex_elems) {nNonconvexElements = nonconvex_elems;}
+  void SetnNonconvexElements(unsigned long nonconvex_elems) { nNonconvexElements = nonconvex_elems; }
 
   /*!
    * \brief Get the amount of nonconvex elements in the mesh.
    * \param[out] nNonconvexElements- amount of nonconvex elements in the mesh
    */
-  unsigned long GetnNonconvexElements() const {return nNonconvexElements;}
+  unsigned long GetnNonconvexElements() const { return nNonconvexElements; }
 
   /*!
    * \brief For streamwise periodicity, find & store a unique reference node on the designated periodic inlet.
    * \param[in] config - Definition of the particular problem.
    */
-  inline virtual void FindUniqueNode_PeriodicBound(const CConfig *config) {}
+  inline virtual void FindUniqueNode_PeriodicBound(const CConfig* config) {}
 
   /*!
    * \brief Get a pointer to the reference node coordinate vector.
@@ -1741,4 +1826,3 @@ class CGeometry {
    */
   inline virtual const su2double* GetStreamwise_Periodic_RefNode() const { return nullptr; }
 };
-
diff --git a/Common/include/geometry/CMultiGridGeometry.hpp b/Common/include/geometry/CMultiGridGeometry.hpp
index ab65300c5ca..6c875cc6f57 100644
--- a/Common/include/geometry/CMultiGridGeometry.hpp
+++ b/Common/include/geometry/CMultiGridGeometry.hpp
@@ -36,7 +36,7 @@
  * \author F. Palacios
  */
 class CMultiGridGeometry final : public CGeometry {
-private:
+ private:
   /*!
    * \brief Determine if a CVPoint van be agglomerated, if it have the same marker point as the seed.
    * \param[in] CVPoint - Control volume to be agglomerated.
@@ -45,8 +45,8 @@ class CMultiGridGeometry final : public CGeometry {
    * \param[in] config - Definition of the particular problem.
    * \return <code>TRUE</code> or <code>FALSE</code> depending if the control volume can be agglomerated.
    */
-  bool SetBoundAgglomeration(unsigned long CVPoint, short marker_seed, const CGeometry *fine_grid,
-                             const CConfig *config) const;
+  bool SetBoundAgglomeration(unsigned long CVPoint, short marker_seed, const CGeometry* fine_grid,
+                             const CConfig* config) const;
 
   /*!
    * \brief Determine if a can be agglomerated using geometrical criteria.
@@ -54,7 +54,7 @@ class CMultiGridGeometry final : public CGeometry {
    * \param[in] fine_grid - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  bool GeometricalCheck(unsigned long iPoint, const CGeometry *fine_grid, const CConfig *config) const;
+  bool GeometricalCheck(unsigned long iPoint, const CGeometry* fine_grid, const CConfig* config) const;
 
   /*!
    * \brief Determine if a CVPoint van be agglomerated, if it have the same marker point as the seed.
@@ -64,7 +64,7 @@ class CMultiGridGeometry final : public CGeometry {
    * \param[in] fine_grid - Geometrical definition of the problem.
    */
   void SetSuitableNeighbors(vector<unsigned long>& Suitable_Indirect_Neighbors, unsigned long iPoint,
-                            unsigned long Index_CoarseCV, const CGeometry *fine_grid) const;
+                            unsigned long Index_CoarseCV, const CGeometry* fine_grid) const;
 
   /*!
    * \brief Set a representative wall value of the agglomerated control volumes on a particular boundary marker.
@@ -73,8 +73,7 @@ class CMultiGridGeometry final : public CGeometry {
    * \param[in] wall_quantity - Object with methods Get(iVertex_fine) and Set(iVertex_coarse, val).
    */
   template <class T>
-  void SetMultiGridWallQuantity(const CGeometry *fine_grid, unsigned short val_marker, T& wall_quantity) {
-
+  void SetMultiGridWallQuantity(const CGeometry* fine_grid, unsigned short val_marker, T& wall_quantity) {
     for (auto iVertex = 0ul; iVertex < nVertex[val_marker]; iVertex++) {
       const auto Point_Coarse = vertex[val_marker][iVertex]->GetNode();
 
@@ -85,8 +84,8 @@ class CMultiGridGeometry final : public CGeometry {
       /*--- Compute area parent by taking into account only volumes that are on the marker. ---*/
       for (auto iChildren = 0u; iChildren < nodes->GetnChildren_CV(Point_Coarse); iChildren++) {
         const auto Point_Fine = nodes->GetChildren_CV(Point_Coarse, iChildren);
-        const auto isVertex = fine_grid->nodes->GetDomain(Point_Fine) &&
-                             (fine_grid->nodes->GetVertex(Point_Fine, val_marker) != -1);
+        const auto isVertex =
+            fine_grid->nodes->GetDomain(Point_Fine) && (fine_grid->nodes->GetVertex(Point_Fine, val_marker) != -1);
         if (isVertex) {
           Area_Parent += fine_grid->nodes->GetVolume(Point_Fine);
         }
@@ -97,8 +96,8 @@ class CMultiGridGeometry final : public CGeometry {
       /*--- Loop again to average coarser value. ---*/
       for (auto iChildren = 0u; iChildren < nodes->GetnChildren_CV(Point_Coarse); iChildren++) {
         const auto Point_Fine = nodes->GetChildren_CV(Point_Coarse, iChildren);
-        const auto isVertex = fine_grid->nodes->GetDomain(Point_Fine) &&
-                             (fine_grid->nodes->GetVertex(Point_Fine, val_marker) != -1);
+        const auto isVertex =
+            fine_grid->nodes->GetDomain(Point_Fine) && (fine_grid->nodes->GetVertex(Point_Fine, val_marker) != -1);
         if (isVertex) {
           const auto Vertex_Fine = fine_grid->nodes->GetVertex(Point_Fine, val_marker);
           const auto Area_Children = fine_grid->nodes->GetVolume(Point_Fine);
@@ -109,15 +108,14 @@ class CMultiGridGeometry final : public CGeometry {
       /*--- Set the value at the coarse level. ---*/
       wall_quantity.Set(iVertex, Quantity_Coarse);
     }
-
   }
 
-public:
+ public:
   /*--- This is to suppress Woverloaded-virtual, omitting it has no negative impact. ---*/
-  using CGeometry::SetVertex;
-  using CGeometry::SetControlVolume;
   using CGeometry::SetBoundControlVolume;
+  using CGeometry::SetControlVolume;
   using CGeometry::SetPoint_Connectivity;
+  using CGeometry::SetVertex;
 
   /*!
    * \brief Constructor of the class.
@@ -125,79 +123,78 @@ class CMultiGridGeometry final : public CGeometry {
    * \param[in] config - Definition of the particular problem.
    * \param[in] iMesh - Level of the multigrid.
    */
-  CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, unsigned short iMesh);
+  CMultiGridGeometry(CGeometry* fine_grid, CConfig* config, unsigned short iMesh);
 
   /*!
    * \brief Set boundary vertex.
    * \param[in] fine_grid - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetVertex(const CGeometry *fine_grid, const CConfig *config) override;
+  void SetVertex(const CGeometry* fine_grid, const CConfig* config) override;
 
   /*!
    * \brief Set points which surround a point.
    * \param[in] fine_grid - Geometrical definition of the child grid.
    */
-  void SetPoint_Connectivity(const CGeometry *fine_grid) override;
+  void SetPoint_Connectivity(const CGeometry* fine_grid) override;
 
   /*!
    * \brief Set the edge structure of the agglomerated control volume.
    * \param[in] fine_grid - Geometrical definition of the problem.
    * \param[in] action - Allocate or not the new elements.
    */
-  void SetControlVolume(const CGeometry *fine_grid, unsigned short action) override;
+  void SetControlVolume(const CGeometry* fine_grid, unsigned short action) override;
 
   /*!
    * \brief Set boundary vertex structure of the agglomerated control volume.
    * \param[in] fine_grid - Geometrical definition of the problem.
    * \param[in] action - Allocate or not the new elements.
    */
-  void SetBoundControlVolume(const CGeometry *fine_grid, unsigned short action) override;
+  void SetBoundControlVolume(const CGeometry* fine_grid, unsigned short action) override;
 
   /*!
    * \brief Set a representative coordinates of the agglomerated control volume.
    * \param[in] fine_grid - Geometrical definition of the problem.
    */
-  void SetCoord(const CGeometry *fine_grid) override;
+  void SetCoord(const CGeometry* fine_grid) override;
 
   /*!
    * \brief Set the grid velocity at each node in the coarse mesh level based
    *        on a restriction from a finer mesh.
    * \param[in] fine_grid - Geometry container for the finer mesh level.
    */
-  void SetRestricted_GridVelocity(const CGeometry *fine_grid) override;
+  void SetRestricted_GridVelocity(const CGeometry* fine_grid) override;
 
   /*!
    * \brief Find and store the closest neighbor to a vertex.
    * \param[in] config - Definition of the particular problem.
    */
-  void FindNormal_Neighbor(const CConfig *config) override;
+  void FindNormal_Neighbor(const CConfig* config) override;
 
   /*!
    * \brief Mach the near field boundary condition.
    * \param[in] config - Definition of the particular problem.
    */
-  void MatchActuator_Disk(const CConfig *config) override;
+  void MatchActuator_Disk(const CConfig* config) override;
 
   /*!
    * \brief Mach the periodic boundary conditions.
    * \param[in] config - Definition of the particular problem.
    * \param[in] val_periodic - Index of the first periodic face in a pair.
    */
-  void MatchPeriodic(const CConfig *config, unsigned short val_periodic) override;
+  void MatchPeriodic(const CConfig* config, unsigned short val_periodic) override;
 
   /*!
-   * \brief Set a representative wall normal heat flux of the agglomerated control volume on a particular boundary marker.
-   * \param[in] fine_grid - Geometrical definition of the problem.
-   * \param[in] val_marker - Index of the boundary marker.
+   * \brief Set a representative wall normal heat flux of the agglomerated control volume on a particular boundary
+   * marker. \param[in] fine_grid - Geometrical definition of the problem. \param[in] val_marker - Index of the boundary
+   * marker.
    */
-  void SetMultiGridWallHeatFlux(const CGeometry *fine_grid, unsigned short val_marker) override;
+  void SetMultiGridWallHeatFlux(const CGeometry* fine_grid, unsigned short val_marker) override;
 
   /*!
    * \brief Set a representative wall temperature of the agglomerated control volume on a particular boundary marker.
    * \param[in] fine_grid - Geometrical definition of the problem.
    * \param[in] val_marker - Index of the boundary marker.
    */
-  void SetMultiGridWallTemperature(const CGeometry *fine_grid, unsigned short val_marker) override;
-
+  void SetMultiGridWallTemperature(const CGeometry* fine_grid, unsigned short val_marker) override;
 };
diff --git a/Common/include/geometry/CMultiGridQueue.hpp b/Common/include/geometry/CMultiGridQueue.hpp
index 5865c36b687..3e75e80af1a 100644
--- a/Common/include/geometry/CMultiGridQueue.hpp
+++ b/Common/include/geometry/CMultiGridQueue.hpp
@@ -40,19 +40,21 @@ using namespace std;
  * \author F. Palacios
  */
 class CMultiGridQueue {
-private:
+ private:
   using QueueType = CFastFindAndEraseQueue<>;
-  vector<QueueType> QueueCV;        /*!< \brief Queue structure to choose the next control volume in the agglomeration process. */
-  vector<short> Priority;           /*!< \brief The priority is based on the number of pre-agglomerated neighbors. */
-  vector<char> RightCV;             /*!< \brief In the lowest priority there are some CV that can not be agglomerated, this is the way to identify them. */
-  const unsigned long nPoint = 0;   /*!< \brief Total number of points. */
+  vector<QueueType>
+      QueueCV;            /*!< \brief Queue structure to choose the next control volume in the agglomeration process. */
+  vector<short> Priority; /*!< \brief The priority is based on the number of pre-agglomerated neighbors. */
+  vector<char> RightCV;   /*!< \brief In the lowest priority there are some CV that can not be agglomerated, this is the
+                             way to identify them. */
+  const unsigned long nPoint = 0; /*!< \brief Total number of points. */
 
   /*!
    * \brief Throw error with error message that the point is not in the priority list.
    */
   void ThrowPointNotInListError(unsigned long iPoint) const;
 
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] npoint - Number of control volumes.
@@ -111,8 +113,10 @@ class CMultiGridQueue {
    * \return Index of the new control volume.
    */
   inline long NextCV(void) const {
-    if (!QueueCV.empty()) return QueueCV.back().front();
-    else return -1;
+    if (!QueueCV.empty())
+      return QueueCV.back().front();
+    else
+      return -1;
   }
 
   /*!
@@ -133,6 +137,5 @@ class CMultiGridQueue {
    * \param[in] updatePoint - Index of the new point.
    * \param[in] fineGrid - Fine grid geometry.
    */
-  void Update(unsigned long updatePoint, CGeometry *fineGrid);
-
+  void Update(unsigned long updatePoint, CGeometry* fineGrid);
 };
diff --git a/Common/include/geometry/CPhysicalGeometry.hpp b/Common/include/geometry/CPhysicalGeometry.hpp
index b69bc67da78..b02db55c0a4 100644
--- a/Common/include/geometry/CPhysicalGeometry.hpp
+++ b/Common/include/geometry/CPhysicalGeometry.hpp
@@ -31,87 +31,71 @@
 #include "meshreader/CMeshReaderFVM.hpp"
 #include "../containers/C2DContainer.hpp"
 
-
 /*!
  * \class CPhysicalGeometry
  * \brief Class for reading a defining the primal grid which is read from the grid file in .su2 or .cgns format.
  * \author F. Palacios, T. Economon, J. Alonso
  */
 class CPhysicalGeometry final : public CGeometry {
-
   unordered_map<unsigned long, unsigned long>
-  Global_to_Local_Point;                           /*!< \brief Global-local indexation for the points. */
-  long *Local_to_Global_Point{nullptr};            /*!< \brief Local-global indexation for the points. */
-  unsigned long *adj_counter{nullptr};             /*!< \brief Adjacency counter. */
-  unsigned long **adjacent_elem{nullptr};          /*!< \brief Adjacency element list. */
-  su2activematrix Sensitivity;                     /*!< \brief Matrix holding the sensitivities at each point. */
+      Global_to_Local_Point;              /*!< \brief Global-local indexation for the points. */
+  long* Local_to_Global_Point{nullptr};   /*!< \brief Local-global indexation for the points. */
+  unsigned long* adj_counter{nullptr};    /*!< \brief Adjacency counter. */
+  unsigned long** adjacent_elem{nullptr}; /*!< \brief Adjacency element list. */
+  su2activematrix Sensitivity;            /*!< \brief Matrix holding the sensitivities at each point. */
 
   vector<vector<unsigned long> > Neighbors;
   unordered_map<unsigned long, unsigned long> Color_List;
   vector<string> Marker_Tags;
-  unsigned long nLocal_Point{0},
-  nLocal_PointDomain{0},
-  nLocal_PointGhost{0},
-  nLocal_PointPeriodic{0},
-  nLocal_Elem{0},
-  nLocal_Bound_Elem{0},
-  nGlobal_Elem{0},
-  nGlobal_Bound_Elem{0},
-  nLocal_Line{0},
-  nLocal_BoundTria{0},
-  nLocal_BoundQuad{0},
-  nLinear_Line{0},
-  nLinear_BoundTria{0},
-  nLinear_BoundQuad{0},
-  nLocal_Tria{0},
-  nLocal_Quad{0},
-  nLocal_Tetr{0},
-  nLocal_Hexa{0},
-  nLocal_Pris{0},
-  nLocal_Pyra{0};
+  unsigned long nLocal_Point{0}, nLocal_PointDomain{0}, nLocal_PointGhost{0}, nLocal_PointPeriodic{0}, nLocal_Elem{0},
+      nLocal_Bound_Elem{0}, nGlobal_Elem{0}, nGlobal_Bound_Elem{0}, nLocal_Line{0}, nLocal_BoundTria{0},
+      nLocal_BoundQuad{0}, nLinear_Line{0}, nLinear_BoundTria{0}, nLinear_BoundQuad{0}, nLocal_Tria{0}, nLocal_Quad{0},
+      nLocal_Tetr{0}, nLocal_Hexa{0}, nLocal_Pris{0}, nLocal_Pyra{0};
   unsigned long nMarker_Global{0};
-  su2double *Local_Coords{nullptr};
-  unsigned long *Local_Points{nullptr};
-  unsigned long *Local_Colors{nullptr};
-  unsigned long *Conn_Line{nullptr};
-  unsigned long *Conn_BoundTria{nullptr};
-  unsigned long *Conn_BoundQuad{nullptr};
-  unsigned long *Conn_Line_Linear{nullptr};
-  unsigned long *Conn_BoundTria_Linear{nullptr};
-  unsigned long *Conn_BoundQuad_Linear{nullptr};
-  unsigned long *Conn_Tria{nullptr};
-  unsigned long *Conn_Quad{nullptr};
-  unsigned long *Conn_Tetr{nullptr};
-  unsigned long *Conn_Hexa{nullptr};
-  unsigned long *Conn_Pris{nullptr};
-  unsigned long *Conn_Pyra{nullptr};
-  unsigned long *ID_Line{nullptr};
-  unsigned long *ID_BoundTria{nullptr};
-  unsigned long *ID_BoundQuad{nullptr};
-  unsigned long *ID_Line_Linear{nullptr};
-  unsigned long *ID_BoundTria_Linear{nullptr};
-  unsigned long *ID_BoundQuad_Linear{nullptr};
-  unsigned long *ID_Tria{nullptr};
-  unsigned long *ID_Quad{nullptr};
-  unsigned long *ID_Tetr{nullptr};
-  unsigned long *ID_Hexa{nullptr};
-  unsigned long *ID_Pris{nullptr};
-  unsigned long *ID_Pyra{nullptr};
-  unsigned long *Elem_ID_Line{nullptr};
-  unsigned long *Elem_ID_BoundTria{nullptr};
-  unsigned long *Elem_ID_BoundQuad{nullptr};
-  unsigned long *Elem_ID_Line_Linear{nullptr};
-  unsigned long *Elem_ID_BoundTria_Linear{nullptr};
-  unsigned long *Elem_ID_BoundQuad_Linear{nullptr};
-
-  su2double Streamwise_Periodic_RefNode[MAXNDIM] = {0}; /*!< \brief Coordinates of the reference node [m] on the receiving periodic marker, for recovered pressure/temperature computation only.*/
-
-public:
+  su2double* Local_Coords{nullptr};
+  unsigned long* Local_Points{nullptr};
+  unsigned long* Local_Colors{nullptr};
+  unsigned long* Conn_Line{nullptr};
+  unsigned long* Conn_BoundTria{nullptr};
+  unsigned long* Conn_BoundQuad{nullptr};
+  unsigned long* Conn_Line_Linear{nullptr};
+  unsigned long* Conn_BoundTria_Linear{nullptr};
+  unsigned long* Conn_BoundQuad_Linear{nullptr};
+  unsigned long* Conn_Tria{nullptr};
+  unsigned long* Conn_Quad{nullptr};
+  unsigned long* Conn_Tetr{nullptr};
+  unsigned long* Conn_Hexa{nullptr};
+  unsigned long* Conn_Pris{nullptr};
+  unsigned long* Conn_Pyra{nullptr};
+  unsigned long* ID_Line{nullptr};
+  unsigned long* ID_BoundTria{nullptr};
+  unsigned long* ID_BoundQuad{nullptr};
+  unsigned long* ID_Line_Linear{nullptr};
+  unsigned long* ID_BoundTria_Linear{nullptr};
+  unsigned long* ID_BoundQuad_Linear{nullptr};
+  unsigned long* ID_Tria{nullptr};
+  unsigned long* ID_Quad{nullptr};
+  unsigned long* ID_Tetr{nullptr};
+  unsigned long* ID_Hexa{nullptr};
+  unsigned long* ID_Pris{nullptr};
+  unsigned long* ID_Pyra{nullptr};
+  unsigned long* Elem_ID_Line{nullptr};
+  unsigned long* Elem_ID_BoundTria{nullptr};
+  unsigned long* Elem_ID_BoundQuad{nullptr};
+  unsigned long* Elem_ID_Line_Linear{nullptr};
+  unsigned long* Elem_ID_BoundTria_Linear{nullptr};
+  unsigned long* Elem_ID_BoundQuad_Linear{nullptr};
+
+  su2double Streamwise_Periodic_RefNode[MAXNDIM] = {
+      0}; /*!< \brief Coordinates of the reference node [m] on the receiving periodic marker, for recovered
+             pressure/temperature computation only.*/
+
+ public:
   /*--- This is to suppress Woverloaded-virtual, omitting it has no negative impact. ---*/
-  using CGeometry::SetVertex;
-  using CGeometry::SetControlVolume;
   using CGeometry::SetBoundControlVolume;
+  using CGeometry::SetControlVolume;
   using CGeometry::SetPoint_Connectivity;
+  using CGeometry::SetVertex;
 
   /*!
    * \brief Constructor of the class.
@@ -128,27 +112,27 @@ class CPhysicalGeometry final : public CGeometry {
    * \param[in] val_iZone - Domain to be read from the grid file.
    * \param[in] val_nZone - Total number of domains in the grid file.
    */
-  CPhysicalGeometry(CConfig *config, unsigned short val_iZone, unsigned short val_nZone);
+  CPhysicalGeometry(CConfig* config, unsigned short val_iZone, unsigned short val_nZone);
 
   /*!
    * \overload
    * \brief Accepts a geometry container holding a linearly partitioned grid
    *        with coloring performed by ParMETIS, and this routine distributes
    *        the points and cells to all partitions based on the coloring.
-   * \param[in] geometry - Definition of the geometry container holding the initial linear partitions of the grid + coloring.
-   * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Definition of the geometry container holding the initial linear partitions of the grid +
+   * coloring. \param[in] config - Definition of the particular problem.
    */
-  CPhysicalGeometry(CGeometry *geometry, CConfig *config);
+  CPhysicalGeometry(CGeometry* geometry, CConfig* config);
 
   /*!
    * \overload
    * \brief Accepts a geometry container holding a linearly partitioned grid
    *        with coloring performed by ParMETIS, and this routine distributes
    *        the points and cells to all partitions based on the coloring.
-   * \param[in] geometry - Definition of the geometry container holding the initial linear partitions of the grid + coloring.
-   * \param[in] config - Definition of the particular problem.
+   * \param[in] geometry - Definition of the geometry container holding the initial linear partitions of the grid +
+   * coloring. \param[in] config - Definition of the particular problem.
    */
-  CPhysicalGeometry(CGeometry *geometry, CConfig *config, bool val_flag);
+  CPhysicalGeometry(CGeometry* geometry, CConfig* config, bool val_flag);
 
   /*!
    * \brief Destructor of the class.
@@ -156,18 +140,18 @@ class CPhysicalGeometry final : public CGeometry {
   ~CPhysicalGeometry(void) override;
 
   /*!
-   * \brief Distributes the coloring from ParMETIS so that each rank has complete information about the local grid points.
-   * \param[in] geometry - Definition of the geometry container holding the initial linear partitions of the grid + coloring.
-   * \param[in] config - Definition of the particular problem.
+   * \brief Distributes the coloring from ParMETIS so that each rank has complete information about the local grid
+   * points. \param[in] geometry - Definition of the geometry container holding the initial linear partitions of the
+   * grid + coloring. \param[in] config - Definition of the particular problem.
    */
-  void DistributeColoring(const CConfig *config, CGeometry *geometry);
+  void DistributeColoring(const CConfig* config, CGeometry* geometry);
 
   /*!
    * \brief Distribute the grid points, including ghost points, across all ranks based on a ParMETIS coloring.
    * \param[in] config - Definition of the particular problem.
    * \param[in] geometry - Geometrical definition of the problem.
    */
-  void DistributePoints(const CConfig *config, CGeometry *geometry);
+  void DistributePoints(const CConfig* config, CGeometry* geometry);
 
   /*!
    * \brief Distribute the connectivity for a single volume element type across all ranks based on a ParMETIS coloring.
@@ -175,22 +159,21 @@ class CPhysicalGeometry final : public CGeometry {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] Elem_Type - VTK index of the element type being distributed.
    */
-  void DistributeVolumeConnectivity(const CConfig *config, CGeometry *geometry, unsigned short Elem_Type);
+  void DistributeVolumeConnectivity(const CConfig* config, CGeometry* geometry, unsigned short Elem_Type);
 
   /*!
-   * \brief Distribute the connectivity for a single surface element type in all markers across all ranks based on a ParMETIS coloring.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] Elem_Type - VTK index of the element type being distributed.
+   * \brief Distribute the connectivity for a single surface element type in all markers across all ranks based on a
+   * ParMETIS coloring. \param[in] config - Definition of the particular problem. \param[in] geometry - Geometrical
+   * definition of the problem. \param[in] Elem_Type - VTK index of the element type being distributed.
    */
-  void DistributeSurfaceConnectivity(CConfig *config, CGeometry *geometry, unsigned short Elem_Type);
+  void DistributeSurfaceConnectivity(CConfig* config, CGeometry* geometry, unsigned short Elem_Type);
 
   /*!
    * \brief Broadcast the marker tags for all boundaries from the master rank to all other ranks.
    * \param[in] config - Definition of the particular problem.
    * \param[in] geometry - Geometrical definition of the problem.
    */
-  void DistributeMarkerTags(CConfig *config, CGeometry *geometry);
+  void DistributeMarkerTags(CConfig* config, CGeometry* geometry);
 
   /*!
    * \brief Partition the marker connectivity held on the master rank according to a linear partitioning.
@@ -198,46 +181,40 @@ class CPhysicalGeometry final : public CGeometry {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] Elem_Type - VTK index of the element type being distributed.
    */
-  void PartitionSurfaceConnectivity(CConfig *config, CGeometry *geometry, unsigned short Elem_Type);
+  void PartitionSurfaceConnectivity(CConfig* config, CGeometry* geometry, unsigned short Elem_Type);
 
   /*!
    * \brief Load the local grid points after partitioning (owned and ghost) into the geometry class objects.
    * \param[in] config - Definition of the particular problem.
    * \param[in] geometry - Geometrical definition of the problem.
    */
-  void LoadPoints(CConfig *config, CGeometry *geometry);
+  void LoadPoints(CConfig* config, CGeometry* geometry);
 
   /*!
    * \brief Load the local volume elements after partitioning (owned and ghost) into the geometry class objects.
    * \param[in] config - Definition of the particular problem.
    * \param[in] geometry - Geometrical definition of the problem.
    */
-  void LoadVolumeElements(CConfig *config, CGeometry *geometry);
+  void LoadVolumeElements(CConfig* config, CGeometry* geometry);
 
   /*!
    * \brief Load the local surface elements after partitioning (owned and ghost) into the geometry class objects.
    * \param[in] config - Definition of the particular problem.
    * \param[in] geometry - Geometrical definition of the problem.
    */
-  void LoadSurfaceElements(CConfig *config, CGeometry *geometry);
+  void LoadSurfaceElements(CConfig* config, CGeometry* geometry);
 
   /*!
    * \brief Routine to launch non-blocking sends and recvs amongst all processors.
    * \param[in] bufSend - Buffer of data to be sent.
-   * \param[in] nElemSend - Array containing the number of elements to send to other processors in cumulative storage format.
-   * \param[in] sendReq - Array of MPI send requests.
-   * \param[in] bufRecv - Buffer of data to be received.
-   * \param[in] nElemSend - Array containing the number of elements to receive from other processors in cumulative storage format.
-   * \param[in] sendReq - Array of MPI recv requests.
-   * \param[in] countPerElem - Pieces of data per element communicated.
-   */
-  void InitiateCommsAll(void *bufSend,
-                        const int *nElemSend,
-                        SU2_MPI::Request *sendReq,
-                        void *bufRecv,
-                        const int *nElemRecv,
-                        SU2_MPI::Request *recvReq,
-                        unsigned short countPerElem,
+   * \param[in] nElemSend - Array containing the number of elements to send to other processors in cumulative storage
+   * format. \param[in] sendReq - Array of MPI send requests. \param[in] bufRecv - Buffer of data to be received.
+   * \param[in] nElemSend - Array containing the number of elements to receive from other processors in cumulative
+   * storage format. \param[in] sendReq - Array of MPI recv requests. \param[in] countPerElem - Pieces of data per
+   * element communicated.
+   */
+  void InitiateCommsAll(void* bufSend, const int* nElemSend, SU2_MPI::Request* sendReq, void* bufRecv,
+                        const int* nElemRecv, SU2_MPI::Request* recvReq, unsigned short countPerElem,
                         unsigned short commType);
 
   /*!
@@ -247,10 +224,7 @@ class CPhysicalGeometry final : public CGeometry {
    * \param[in] nRecvs - Number of receives to be completed.
    * \param[in] sendReq - Array of MPI recv requests.
    */
-  void CompleteCommsAll(int nSends,
-                        SU2_MPI::Request *sendReq,
-                        int nRecvs,
-                        SU2_MPI::Request *recvReq);
+  void CompleteCommsAll(int nSends, SU2_MPI::Request* sendReq, int nRecvs, SU2_MPI::Request* recvReq);
 
   /*!
    * \brief Routine to compute the initial linear partitioning offset counts and store in persistent data structures.
@@ -269,19 +243,19 @@ class CPhysicalGeometry final : public CGeometry {
    * \brief Routine to sort the adjacency for ParMETIS for graph partitioning in parallel.
    * \param[in] config - Definition of the particular problem.
    */
-  void SortAdjacency(const CConfig *config);
+  void SortAdjacency(const CConfig* config);
 
   /*!
    * \brief Set the send receive boundaries of the grid.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetSendReceive(const CConfig *config) override;
+  void SetSendReceive(const CConfig* config) override;
 
   /*!
    * \brief Set the send receive boundaries of the grid.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetBoundaries(CConfig *config) override;
+  void SetBoundaries(CConfig* config) override;
 
   /*!
    * \brief Set the local index that correspond with the global numbering index.
@@ -295,8 +269,7 @@ class CPhysicalGeometry final : public CGeometry {
    */
   inline long GetGlobal_to_Local_Point(unsigned long val_ipoint) const override {
     auto it = Global_to_Local_Point.find(val_ipoint);
-    if (it != Global_to_Local_Point.cend())
-      return it->second;
+    if (it != Global_to_Local_Point.cend()) return it->second;
     return -1;
   }
 
@@ -309,7 +282,7 @@ class CPhysicalGeometry final : public CGeometry {
    * \param[in] val_iZone - Domain to be read from the grid file.
    * \param[in] val_nZone - Total number of domains in the grid file.
    */
-  void Read_Mesh_FVM(CConfig *config, string val_mesh_filename, unsigned short val_iZone, unsigned short val_nZone);
+  void Read_Mesh_FVM(CConfig* config, string val_mesh_filename, unsigned short val_iZone, unsigned short val_nZone);
 
   /*!
    * \brief Reads for the FEM solver the geometry of the grid and adjust the boundary
@@ -319,7 +292,8 @@ class CPhysicalGeometry final : public CGeometry {
    * \param[in] val_iZone - Domain to be read from the grid file.
    * \param[in] val_nZone - Total number of domains in the grid file.
    */
-  void Read_SU2_Format_Parallel_FEM(CConfig *config, string val_mesh_filename, unsigned short val_iZone, unsigned short val_nZone);
+  void Read_SU2_Format_Parallel_FEM(CConfig* config, string val_mesh_filename, unsigned short val_iZone,
+                                    unsigned short val_nZone);
 
   /*!
    * \brief Reads for the FEM solver the geometry of the grid and adjust the boundary
@@ -329,34 +303,35 @@ class CPhysicalGeometry final : public CGeometry {
    * \param[in] val_iZone - Domain to be read from the grid file.
    * \param[in] val_nZone - Total number of domains in the grid file.
    */
-  void Read_CGNS_Format_Parallel_FEM(CConfig *config, string val_mesh_filename, unsigned short val_iZone, unsigned short val_nZone);
+  void Read_CGNS_Format_Parallel_FEM(CConfig* config, string val_mesh_filename, unsigned short val_iZone,
+                                     unsigned short val_nZone);
 
   /*!
    * \brief Routine to load the CGNS grid points from a single zone into the proper SU2 data structures.
    * \param[in] config - definition of the particular problem.
    * \param[in] mesh   - mesh reader object containing the current zone data.
    */
-  void LoadLinearlyPartitionedPoints(CConfig *config, CMeshReaderFVM *mesh);
+  void LoadLinearlyPartitionedPoints(CConfig* config, CMeshReaderFVM* mesh);
 
   /*!
    * \brief Loads the interior volume elements from the mesh reader object into the primal element data structures.
    * \param[in] config - definition of the particular problem.
    * \param[in] mesh   - mesh reader object containing the current zone data.
    */
-  void LoadLinearlyPartitionedVolumeElements(CConfig *config, CMeshReaderFVM *mesh);
+  void LoadLinearlyPartitionedVolumeElements(CConfig* config, CMeshReaderFVM* mesh);
 
   /*!
    * \brief Loads the boundary elements (markers) from the mesh reader object into the primal element data structures.
    * \param[in] config - definition of the particular problem.
    * \param[in] mesh   - mesh reader object containing the current zone data.
    */
-  void LoadUnpartitionedSurfaceElements(CConfig *config, CMeshReaderFVM *mesh);
+  void LoadUnpartitionedSurfaceElements(CConfig* config, CMeshReaderFVM* mesh);
 
   /*!
-   * \brief Prepares the grid point adjacency based on a linearly partitioned mesh object needed by ParMETIS for graph partitioning in parallel.
-   * \param[in] config - Definition of the particular problem.
+   * \brief Prepares the grid point adjacency based on a linearly partitioned mesh object needed by ParMETIS for graph
+   * partitioning in parallel. \param[in] config - Definition of the particular problem.
    */
-  void PrepareAdjacency(const CConfig *config);
+  void PrepareAdjacency(const CConfig* config);
 
   /*!
    * \brief Find repeated nodes between two elements to identify the common face.
@@ -366,14 +341,14 @@ class CPhysicalGeometry final : public CGeometry {
    * \param[in] face_second_elem - Index of the common face for the second element.
    * \return It provides 0 or 1 depending if there is a common face or not.
    */
-  bool FindFace(unsigned long first_elem, unsigned long second_elem, unsigned short &face_first_elem,
-                unsigned short &face_second_elem) override;
+  bool FindFace(unsigned long first_elem, unsigned long second_elem, unsigned short& face_first_elem,
+                unsigned short& face_second_elem) override;
 
   /*!
    * \brief Compute surface area (positive z-direction) for force coefficient non-dimensionalization.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetPositive_ZArea(CConfig *config) override;
+  void SetPositive_ZArea(CConfig* config) override;
 
   /*!
    * \brief Set points which surround a point.
@@ -384,7 +359,7 @@ class CPhysicalGeometry final : public CGeometry {
    * \brief Set a renumbering using a Reverse Cuthill-McKee Algorithm
    * \param[in] config - Definition of the particular problem.
    */
-  void SetRCM_Ordering(CConfig *config) override;
+  void SetRCM_Ordering(CConfig* config) override;
 
   /*!
    * \brief Set elements which surround an element.
@@ -400,70 +375,70 @@ class CPhysicalGeometry final : public CGeometry {
    * \brief Set boundary vertex.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetVertex(const CConfig *config) override;
+  void SetVertex(const CConfig* config) override;
 
   /*!
    * \brief Set number of span wise level for turbomachinery computation.
    * \param[in] config - Definition of the particular problem.
    */
-  void ComputeNSpan(CConfig *config, unsigned short val_iZone, unsigned short marker_flag, bool allocate) override;
+  void ComputeNSpan(CConfig* config, unsigned short val_iZone, unsigned short marker_flag, bool allocate) override;
 
   /*!
    * \brief Set turbo boundary vertex.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetTurboVertex(CConfig *config,unsigned short val_iZone, unsigned short marker_flag, bool allocate) override;
+  void SetTurboVertex(CConfig* config, unsigned short val_iZone, unsigned short marker_flag, bool allocate) override;
 
   /*!
- * \brief update turbo boundary vertex.
- * \param[in] config - Definition of the particular problem.
- */
-  void UpdateTurboVertex(CConfig *config,unsigned short val_iZone, unsigned short marker_flag) override;
+   * \brief update turbo boundary vertex.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void UpdateTurboVertex(CConfig* config, unsigned short val_iZone, unsigned short marker_flag) override;
 
   /*!
    * \brief Set turbo boundary vertex.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetAvgTurboValue(CConfig *config, unsigned short val_iZone, unsigned short marker_flag, bool allocate) override;
+  void SetAvgTurboValue(CConfig* config, unsigned short val_iZone, unsigned short marker_flag, bool allocate) override;
 
   /*!
    * \brief Set turbo boundary vertex.
    * \param[in] config - Definition of the particular problem.
    */
-  void GatherInOutAverageValues(CConfig *config, bool allocate) override;
+  void GatherInOutAverageValues(CConfig* config, bool allocate) override;
 
   /*!
    * \brief Set the edge structure of the control volume.
    * \param[in] config - Definition of the particular problem.
    * \param[in] action - Allocate or not the new elements.
    */
-  void SetControlVolume(CConfig *config, unsigned short action) override;
+  void SetControlVolume(CConfig* config, unsigned short action) override;
 
   /*!
    * \brief Visualize the structure of the control volume(s).
    * \param[in] config - Definition of the particular problem.
    */
-  void VisualizeControlVolume(const CConfig *config) const override;
+  void VisualizeControlVolume(const CConfig* config) const override;
 
   /*!
    * \brief Mach the near field boundary condition.
    * \param[in] config - Definition of the particular problem.
    */
-  void MatchActuator_Disk(const CConfig *config) override;
+  void MatchActuator_Disk(const CConfig* config) override;
 
   /*!
    * \brief Mach the periodic boundary conditions.
    * \param[in] config - Definition of the particular problem.
    * \param[in] val_periodic - Index of the first periodic face in a pair.
    */
-  void MatchPeriodic(const CConfig *config, unsigned short val_periodic) override;
+  void MatchPeriodic(const CConfig* config, unsigned short val_periodic) override;
 
   /*!
    * \brief Set boundary vertex structure of the control volume.
    * \param[in] config - Definition of the particular problem.
    * \param[in] action - Allocate or not the new elements.
    */
-  void SetBoundControlVolume(const CConfig *config, unsigned short action) override;
+  void SetBoundControlVolume(const CConfig* config, unsigned short action) override;
 
   /*!
    * \brief Set the maximum cell-center to cell-center distance for CVs.
@@ -486,31 +461,31 @@ class CPhysicalGeometry final : public CGeometry {
    *            information is going to be stored.
    * \param[in] new_file - Create a new file.
    */
-  void SetBoundTecPlot(char mesh_filename[MAX_STRING_SIZE], bool new_file, CConfig *config) override;
+  void SetBoundTecPlot(char mesh_filename[MAX_STRING_SIZE], bool new_file, CConfig* config) override;
 
   /*!
    * \brief Check the volume element orientation.
    * \param[in] config - Definition of the particular problem.
    */
-  void Check_IntElem_Orientation(const CConfig *config) override;
+  void Check_IntElem_Orientation(const CConfig* config) override;
 
   /*!
    * \brief Check the volume element orientation.
    * \param[in] config - Definition of the particular problem.
    */
-  void Check_BoundElem_Orientation(const CConfig *config) override;
+  void Check_BoundElem_Orientation(const CConfig* config) override;
 
   /*!
    * \brief Set the domains for grid grid partitioning using ParMETIS.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetColorGrid_Parallel(const CConfig *config) override;
+  void SetColorGrid_Parallel(const CConfig* config) override;
 
   /*!
    * \brief Set the domains for FEM grid partitioning using ParMETIS.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetColorFEMGrid_Parallel(CConfig *config) override;
+  void SetColorFEMGrid_Parallel(CConfig* config) override;
 
   /*!
    * \brief Compute the weights of the FEM graph for ParMETIS.
@@ -522,45 +497,41 @@ class CPhysicalGeometry final : public CGeometry {
    * \param[out] vwgt                         - Weights of the vertices of the graph, i.e. the elements.
    * \param[out] adjwgt                       - Weights of the edges of the graph.
    */
-  void ComputeFEMGraphWeights(
-      CConfig                                    *config,
-      const vector<CFaceOfElement>               &localFaces,
-      const vector<vector<unsigned long> >       &adjacency,
-      const map<unsigned long, CUnsignedShort2T> &mapExternalElemIDToTimeLevel,
-      vector<su2double>                          &vwgt,
-      vector<vector<su2double> >                 &adjwgt);
+  void ComputeFEMGraphWeights(CConfig* config, const vector<CFaceOfElement>& localFaces,
+                              const vector<vector<unsigned long> >& adjacency,
+                              const map<unsigned long, CUnsignedShort2T>& mapExternalElemIDToTimeLevel,
+                              vector<su2double>& vwgt, vector<vector<su2double> >& adjwgt);
 
   /*!
    * \brief Determine the donor elements for the boundary elements on viscous
             wall boundaries when wall functions are used.
    * \param[in]  config - Definition of the particular problem.
    */
-  void DetermineDonorElementsWallFunctions(CConfig *config);
+  void DetermineDonorElementsWallFunctions(CConfig* config);
 
   /*!
    * \brief Determine whether or not the Jacobians of the elements and faces
             are constant and a length scale of the elements.
    * \param[in]  config - Definition of the particular problem.
    */
-  void DetermineFEMConstantJacobiansAndLenScale(CConfig *config);
+  void DetermineFEMConstantJacobiansAndLenScale(CConfig* config);
 
   /*!
    * \brief Determine the neighboring information for periodic faces of a FEM grid.
    * \param[in]     config      - Definition of the particular problem.
    * \param[in,out] localFaces  - Vector, which contains the element faces of this rank.
    */
-  void DeterminePeriodicFacesFEMGrid(CConfig                *config,
-                                     vector<CFaceOfElement> &localFaces);
+  void DeterminePeriodicFacesFEMGrid(CConfig* config, vector<CFaceOfElement>& localFaces);
 
   /*!
    * \brief Determine the time level of the elements when time accurate local time stepping is employed.
    * \param[in]  config                       - Definition of the particular problem.
    * \param[in]  localFaces                   - Vector, which contains the element faces of this rank.
-   * \param[out] mapExternalElemIDToTimeLevel - Map from the external element ID's to their time level and number of DOFs.
+   * \param[out] mapExternalElemIDToTimeLevel - Map from the external element ID's to their time level and number of
+   * DOFs.
    */
-  void DetermineTimeLevelElements(CConfig                              *config,
-                                  const vector<CFaceOfElement>         &localFaces,
-                                  map<unsigned long, CUnsignedShort2T> &mapExternalElemIDToTimeLevel);
+  void DetermineTimeLevelElements(CConfig* config, const vector<CFaceOfElement>& localFaces,
+                                  map<unsigned long, CUnsignedShort2T>& mapExternalElemIDToTimeLevel);
 
   /*!
    * \brief Do an implicit smoothing of the grid coordinates.
@@ -568,165 +539,166 @@ class CPhysicalGeometry final : public CGeometry {
    * \param[in] val_smooth_coeff - Relaxation factor.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetCoord_Smoothing(unsigned short val_nSmooth, su2double val_smooth_coeff, CConfig *config) override;
+  void SetCoord_Smoothing(unsigned short val_nSmooth, su2double val_smooth_coeff, CConfig* config) override;
 
   /*!
    * \brief Compute 3 grid quality metrics: orthogonality angle, dual cell aspect ratio, and dual cell volume ratio.
    * \param[in] config - Definition of the particular problem.
    */
-  void ComputeMeshQualityStatistics(const CConfig *config) override;
+  void ComputeMeshQualityStatistics(const CConfig* config) override;
 
   /*!
    * \brief Find and store the closest neighbor to a vertex.
    * \param[in] config - Definition of the particular problem.
    */
-  void FindNormal_Neighbor(const CConfig *config) override;
+  void FindNormal_Neighbor(const CConfig* config) override;
 
   /*!
    * \brief Read the sensitivity from an input file.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetBoundSensitivity(CConfig *config) override;
+  void SetBoundSensitivity(CConfig* config) override;
 
   /*!
    * \brief Compute the maximum thickness of an airfoil.
    * \return Maximum thickness at a particular seccion.
    */
-  su2double Compute_MaxThickness(su2double *Plane_P0, su2double *Plane_Normal, CConfig *config, vector<su2double> &Xcoord_Airfoil,
-                                 vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) override;
+  su2double Compute_MaxThickness(su2double* Plane_P0, su2double* Plane_Normal, CConfig* config,
+                                 vector<su2double>& Xcoord_Airfoil, vector<su2double>& Ycoord_Airfoil,
+                                 vector<su2double>& Zcoord_Airfoil) override;
 
   /*!
    * \brief Compute the twist of an airfoil.
    * \return Twist at a particular seccion.
    */
-  su2double Compute_Twist(su2double *Plane_P0, su2double *Plane_Normal, vector<su2double> &Xcoord_Airfoil,
-                          vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) override;
+  su2double Compute_Twist(su2double* Plane_P0, su2double* Plane_Normal, vector<su2double>& Xcoord_Airfoil,
+                          vector<su2double>& Ycoord_Airfoil, vector<su2double>& Zcoord_Airfoil) override;
 
   /*!
    * \brief Compute the leading/trailing edge location of an airfoil.
    */
-  void Compute_Wing_LeadingTrailing(su2double *LeadingEdge, su2double *TrailingEdge, su2double *Plane_P0,
-                                    su2double *Plane_Normal, vector<su2double> &Xcoord_Airfoil,
-                                    vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) override;
+  void Compute_Wing_LeadingTrailing(su2double* LeadingEdge, su2double* TrailingEdge, su2double* Plane_P0,
+                                    su2double* Plane_Normal, vector<su2double>& Xcoord_Airfoil,
+                                    vector<su2double>& Ycoord_Airfoil, vector<su2double>& Zcoord_Airfoil) override;
 
   /*!
-  * \brief Compute the leading/trailing edge location of a fuselage.
-  */
-  void Compute_Fuselage_LeadingTrailing(su2double *LeadingEdge, su2double *TrailingEdge, su2double *Plane_P0,
-                                        su2double *Plane_Normal, vector<su2double> &Xcoord_Airfoil,
-                                        vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) override;
+   * \brief Compute the leading/trailing edge location of a fuselage.
+   */
+  void Compute_Fuselage_LeadingTrailing(su2double* LeadingEdge, su2double* TrailingEdge, su2double* Plane_P0,
+                                        su2double* Plane_Normal, vector<su2double>& Xcoord_Airfoil,
+                                        vector<su2double>& Ycoord_Airfoil, vector<su2double>& Zcoord_Airfoil) override;
 
   /*!
    * \brief Compute the chord of an airfoil.
    * \return Chord of an airfoil.
    */
-  su2double Compute_Chord(su2double *Plane_P0, su2double *Plane_Normal, vector<su2double> &Xcoord_Airfoil,
-                          vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) override;
+  su2double Compute_Chord(su2double* Plane_P0, su2double* Plane_Normal, vector<su2double>& Xcoord_Airfoil,
+                          vector<su2double>& Ycoord_Airfoil, vector<su2double>& Zcoord_Airfoil) override;
 
   /*!
    * \brief Compute the chord of an airfoil.
    * \return Chord of an airfoil.
    */
-  su2double Compute_Width(su2double *Plane_P0, su2double *Plane_Normal, vector<su2double> &Xcoord_Airfoil,
-                          vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) override;
+  su2double Compute_Width(su2double* Plane_P0, su2double* Plane_Normal, vector<su2double>& Xcoord_Airfoil,
+                          vector<su2double>& Ycoord_Airfoil, vector<su2double>& Zcoord_Airfoil) override;
 
   /*!
    * \brief Compute the chord of an airfoil.
    * \return Chord of an airfoil.
    */
-  su2double Compute_WaterLineWidth(su2double *Plane_P0, su2double *Plane_Normal, CConfig *config, vector<su2double> &Xcoord_Airfoil,
-                                   vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) override;
+  su2double Compute_WaterLineWidth(su2double* Plane_P0, su2double* Plane_Normal, CConfig* config,
+                                   vector<su2double>& Xcoord_Airfoil, vector<su2double>& Ycoord_Airfoil,
+                                   vector<su2double>& Zcoord_Airfoil) override;
 
   /*!
    * \brief Compute the chord of an airfoil.
    * \return Chord of an airfoil.
    */
-  su2double Compute_Height(su2double *Plane_P0, su2double *Plane_Normal, vector<su2double> &Xcoord_Airfoil,
-                           vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) override;
+  su2double Compute_Height(su2double* Plane_P0, su2double* Plane_Normal, vector<su2double>& Xcoord_Airfoil,
+                           vector<su2double>& Ycoord_Airfoil, vector<su2double>& Zcoord_Airfoil) override;
 
   /*!
    * \brief Compute the chord of an airfoil.
    * \return Chord of an airfoil.
    */
-  su2double Compute_LERadius(su2double *Plane_P0, su2double *Plane_Normal, vector<su2double> &Xcoord_Airfoil,
-                             vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) override;
+  su2double Compute_LERadius(su2double* Plane_P0, su2double* Plane_Normal, vector<su2double>& Xcoord_Airfoil,
+                             vector<su2double>& Ycoord_Airfoil, vector<su2double>& Zcoord_Airfoil) override;
 
   /*!
    * \brief Compute the thickness of an airfoil.
    */
-  su2double Compute_Thickness(su2double *Plane_P0, su2double *Plane_Normal, su2double Location, CConfig *config, vector<su2double> &Xcoord_Airfoil,
-                              vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil, su2double &ZLoc) override;
+  su2double Compute_Thickness(su2double* Plane_P0, su2double* Plane_Normal, su2double Location, CConfig* config,
+                              vector<su2double>& Xcoord_Airfoil, vector<su2double>& Ycoord_Airfoil,
+                              vector<su2double>& Zcoord_Airfoil, su2double& ZLoc) override;
 
   /*!
    * \brief Compute the area of an airfoil.
    * \return Area of an airfoil.
    */
-  su2double Compute_Area(su2double *Plane_P0, su2double *Plane_Normal, CConfig *config, vector<su2double> &Xcoord_Airfoil,
-                         vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) override;
+  su2double Compute_Area(su2double* Plane_P0, su2double* Plane_Normal, CConfig* config,
+                         vector<su2double>& Xcoord_Airfoil, vector<su2double>& Ycoord_Airfoil,
+                         vector<su2double>& Zcoord_Airfoil) override;
 
   /*!
    * \brief Compute the length of an airfoil.
    * \return Area of an airfoil.
    */
-  su2double Compute_Length(su2double *Plane_P0, su2double *Plane_Normal, CConfig *config, vector<su2double> &Xcoord_Airfoil,
-                           vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) override;
+  su2double Compute_Length(su2double* Plane_P0, su2double* Plane_Normal, CConfig* config,
+                           vector<su2double>& Xcoord_Airfoil, vector<su2double>& Ycoord_Airfoil,
+                           vector<su2double>& Zcoord_Airfoil) override;
 
   /*!
    * \brief Compute the dihedral of a wing.
    * \return Dihedral at a particular seccion.
    */
-  su2double Compute_Dihedral(su2double *LeadingEdge_im1, su2double *TrailingEdge_im1,
-                             su2double *LeadingEdge_i, su2double *TrailingEdge_i) override;
+  su2double Compute_Dihedral(su2double* LeadingEdge_im1, su2double* TrailingEdge_im1, su2double* LeadingEdge_i,
+                             su2double* TrailingEdge_i) override;
 
   /*!
    * \brief Compute the curvature of a wing.
    */
-  su2double Compute_Curvature(su2double *LeadingEdge_im1, su2double *TrailingEdge_im1,
-                              su2double *LeadingEdge_i, su2double *TrailingEdge_i,
-                              su2double *LeadingEdge_ip1, su2double *TrailingEdge_ip1) override;
+  su2double Compute_Curvature(su2double* LeadingEdge_im1, su2double* TrailingEdge_im1, su2double* LeadingEdge_i,
+                              su2double* TrailingEdge_i, su2double* LeadingEdge_ip1,
+                              su2double* TrailingEdge_ip1) override;
 
   /*!
    * \brief Evaluate geometrical parameters of a wing.
    */
-  void Compute_Wing(CConfig *config, bool original_surface,
-                    su2double &Wing_Volume, su2double &Wing_MinMaxThickness, su2double &Wing_MaxMaxThickness,
-                    su2double &Wing_MinChord, su2double &Wing_MaxChord,
-                    su2double &Wing_MinLERadius, su2double &Wing_MaxLERadius,
-                    su2double &Wing_MinToC, su2double &Wing_MaxToC,
-                    su2double &Wing_ObjFun_MinToC, su2double &Wing_MaxTwist,
-                    su2double &Wing_MaxCurvature, su2double &Wing_MaxDihedral) override;
+  void Compute_Wing(CConfig* config, bool original_surface, su2double& Wing_Volume, su2double& Wing_MinMaxThickness,
+                    su2double& Wing_MaxMaxThickness, su2double& Wing_MinChord, su2double& Wing_MaxChord,
+                    su2double& Wing_MinLERadius, su2double& Wing_MaxLERadius, su2double& Wing_MinToC,
+                    su2double& Wing_MaxToC, su2double& Wing_ObjFun_MinToC, su2double& Wing_MaxTwist,
+                    su2double& Wing_MaxCurvature, su2double& Wing_MaxDihedral) override;
 
   /*!
    * \brief Evaluate geometrical parameters of a wing.
    */
-  void Compute_Fuselage(CConfig *config, bool original_surface,
-                        su2double &Fuselage_Volume, su2double &Fuselage_WettedArea,
-                        su2double &Fuselage_MinWidth, su2double &Fuselage_MaxWidth,
-                        su2double &Fuselage_MinWaterLineWidth, su2double &Fuselage_MaxWaterLineWidth,
-                        su2double &Fuselage_MinHeight, su2double &Fuselage_MaxHeight,
-                        su2double &Fuselage_MaxCurvature) override;
+  void Compute_Fuselage(CConfig* config, bool original_surface, su2double& Fuselage_Volume,
+                        su2double& Fuselage_WettedArea, su2double& Fuselage_MinWidth, su2double& Fuselage_MaxWidth,
+                        su2double& Fuselage_MinWaterLineWidth, su2double& Fuselage_MaxWaterLineWidth,
+                        su2double& Fuselage_MinHeight, su2double& Fuselage_MaxHeight,
+                        su2double& Fuselage_MaxCurvature) override;
 
   /*!
    * \brief Evaluate geometrical parameters of a wing.
    */
-  void Compute_Nacelle(CConfig *config, bool original_surface,
-                       su2double &Nacelle_Volume, su2double &Nacelle_MinMaxThickness, su2double &Nacelle_MaxMaxThickness,
-                       su2double &Nacelle_MinChord, su2double &Nacelle_MaxChord,
-                       su2double &Nacelle_MinLERadius, su2double &Nacelle_MaxLERadius,
-                       su2double &Nacelle_MinToC, su2double &Nacelle_MaxToC,
-                       su2double &Nacelle_ObjFun_MinToC, su2double &Nacelle_MaxTwist) override;
+  void Compute_Nacelle(CConfig* config, bool original_surface, su2double& Nacelle_Volume,
+                       su2double& Nacelle_MinMaxThickness, su2double& Nacelle_MaxMaxThickness,
+                       su2double& Nacelle_MinChord, su2double& Nacelle_MaxChord, su2double& Nacelle_MinLERadius,
+                       su2double& Nacelle_MaxLERadius, su2double& Nacelle_MinToC, su2double& Nacelle_MaxToC,
+                       su2double& Nacelle_ObjFun_MinToC, su2double& Nacelle_MaxTwist) override;
 
   /*!
    * \brief Read the sensitivity from adjoint solution file and store it.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetSensitivity(CConfig *config) override;
+  void SetSensitivity(CConfig* config) override;
 
   /*!
    * \brief Read the sensitivity from unordered ASCII adjoint solution file and store it.
    * \param[in] config - Definition of the particular problem.
    */
-  void ReadUnorderedSensitivity(CConfig *config) override;
+  void ReadUnorderedSensitivity(CConfig* config) override;
 
   /*!
    * \brief Get the Sensitivity at a specific point.
@@ -734,7 +706,9 @@ class CPhysicalGeometry final : public CGeometry {
    * \param[in] iDim - The component of the dim. vector.
    * \return The sensitivity at point iPoint and dim. iDim.
    */
-  inline su2double GetSensitivity(unsigned long iPoint, unsigned short iDim) const override { return Sensitivity(iPoint,iDim); }
+  inline su2double GetSensitivity(unsigned long iPoint, unsigned short iDim) const override {
+    return Sensitivity(iPoint, iDim);
+  }
 
   /*!
    * \brief Set the Sensitivity at a specific point.
@@ -742,20 +716,22 @@ class CPhysicalGeometry final : public CGeometry {
    * \param[in] iDim - The component of the dim. vector.
    * \param[in] val - Value of the sensitivity.
    */
-  inline void SetSensitivity(unsigned long iPoint, unsigned short iDim, su2double val) override { Sensitivity(iPoint,iDim) = val; }
+  inline void SetSensitivity(unsigned long iPoint, unsigned short iDim, su2double val) override {
+    Sensitivity(iPoint, iDim) = val;
+  }
 
   /*!
    * \brief Check the mesh for periodicity and deactivate multigrid if periodicity is found.
    * \param[in] config - Definition of the particular problem.
    */
-  void Check_Periodicity(CConfig *config) override;
+  void Check_Periodicity(CConfig* config) override;
 
   /*!
    * \brief Compute an ADT including the coordinates of all viscous markers
    * \param[in] config - Definition of the particular problem.
    * \return pointer to the ADT
    */
-  std::unique_ptr<CADTElemClass> ComputeViscousWallADT(const CConfig *config) const override;
+  std::unique_ptr<CADTElemClass> ComputeViscousWallADT(const CConfig* config) const override;
 
   /*!
    * \brief Reduce the wall distance based on an previously constructed ADT.
@@ -771,7 +747,7 @@ class CPhysicalGeometry final : public CGeometry {
    * \brief Set wall distances a specific value
    */
   void SetWallDistance(su2double val) override {
-    for (unsigned long iPoint = 0; iPoint < GetnPoint(); iPoint++){
+    for (unsigned long iPoint = 0; iPoint < GetnPoint(); iPoint++) {
       nodes->SetWall_Distance(iPoint, val);
     }
   }
@@ -780,11 +756,11 @@ class CPhysicalGeometry final : public CGeometry {
    * \brief For streamwise periodicity, find & store a unique reference node on the designated periodic inlet.
    * \param[in] config - Definition of the particular problem.
    */
-  void FindUniqueNode_PeriodicBound(const CConfig *config) final;
+  void FindUniqueNode_PeriodicBound(const CConfig* config) final;
 
   /*!
    * \brief Get a pointer to the reference node coordinate vector.
    * \return A pointer to the reference node coordinate vector.
    */
-  inline const su2double* GetStreamwise_Periodic_RefNode(void) const final { return Streamwise_Periodic_RefNode;}
+  inline const su2double* GetStreamwise_Periodic_RefNode(void) const final { return Streamwise_Periodic_RefNode; }
 };
diff --git a/Common/include/geometry/dual_grid/CDualGrid.hpp b/Common/include/geometry/dual_grid/CDualGrid.hpp
index b99e9d4a8e7..1e96d519e2c 100644
--- a/Common/include/geometry/dual_grid/CDualGrid.hpp
+++ b/Common/include/geometry/dual_grid/CDualGrid.hpp
@@ -41,12 +41,11 @@
  *        three main elements: points, edges, and vertices.
  * \author F. Palacios
  */
-class CDualGrid{
-protected:
+class CDualGrid {
+ protected:
   static unsigned short nDim; /*!< \brief Number of dimensions of the problem. */
 
-public:
-
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] val_nDim - Number of dimensions of the problem.
@@ -61,13 +60,13 @@ class CDualGrid{
   /*!
    * \brief A pure virtual member.
    */
-  virtual su2double *GetCoord(void) = 0;
+  virtual su2double* GetCoord(void) = 0;
 
   /*!
    * \brief A pure virtual member.
    * \param[in] val_coord - Coordinate of the point.
    */
-  virtual void SetCoord(const su2double *val_coord) = 0;
+  virtual void SetCoord(const su2double* val_coord) = 0;
 
   /*!
    * \brief A pure virtual member.
@@ -75,32 +74,32 @@ class CDualGrid{
    * \param[in] val_coord_FaceElem_CG - Coordinates of the centre of gravity of the face of an element.
    * \param[in] val_coord_Elem_CG - Coordinates of the centre of gravity of the element.
    */
-  virtual void SetNodes_Coord(const su2double *val_coord_Edge_CG, const su2double *val_coord_FaceElem_CG,
-                              const su2double *val_coord_Elem_CG) = 0;
+  virtual void SetNodes_Coord(const su2double* val_coord_Edge_CG, const su2double* val_coord_FaceElem_CG,
+                              const su2double* val_coord_Elem_CG) = 0;
 
   /*!
    * \overload
    * \param[in] val_coord_Edge_CG - Coordinates of the centre of gravity of the edge.
    * \param[in] val_coord_Elem_CG - Coordinates of the centre of gravity of the element.
    */
-  virtual void SetNodes_Coord(const su2double *val_coord_Edge_CG, const su2double *val_coord_Elem_CG) = 0;
+  virtual void SetNodes_Coord(const su2double* val_coord_Edge_CG, const su2double* val_coord_Elem_CG) = 0;
 
   /*!
    * \brief A pure virtual member.
    * \param[out] val_normal - Coordinates of the normal.
    */
-  virtual void GetNormal(su2double *val_normal) const = 0;
+  virtual void GetNormal(su2double* val_normal) const = 0;
 
   /*!
    * \brief A pure virtual member.
    */
-  virtual su2double *GetNormal(void) = 0;
+  virtual su2double* GetNormal(void) = 0;
 
   /*!
    * \brief A pure virtual member.
    * \param[in] val_face_normal - Coordinates of the normal.
    */
-  virtual void SetNormal(const su2double *val_face_normal) = 0;
+  virtual void SetNormal(const su2double* val_face_normal) = 0;
 
   /*!
    * \brief A pure virtual member.
@@ -116,5 +115,5 @@ class CDualGrid{
    * \brief A pure virtual member.
    * \param[in] val_face_normal - Normal vector to be added.
    */
-  virtual void AddNormal(const su2double *val_face_normal) = 0;
+  virtual void AddNormal(const su2double* val_face_normal) = 0;
 };
diff --git a/Common/include/geometry/dual_grid/CEdge.hpp b/Common/include/geometry/dual_grid/CEdge.hpp
index 84bb425cbbb..c3fbd76449b 100644
--- a/Common/include/geometry/dual_grid/CEdge.hpp
+++ b/Common/include/geometry/dual_grid/CEdge.hpp
@@ -38,17 +38,18 @@ class CPhysicalGeometry;
  */
 class CEdge {
   static_assert(su2activematrix::IsRowMajor, "Needed to return normal as pointer.");
-private:
+
+ private:
   using Index = unsigned long;
   using NodeArray = C2DContainer<Index, Index, StorageType::ColumnMajor, 64, DynamicSize, 2>;
-  NodeArray Nodes;           /*!< \brief Vector to store the node indices of the edge. */
-  su2activematrix Normal;    /*!< \brief Normal (area) of the edge. */
+  NodeArray Nodes;        /*!< \brief Vector to store the node indices of the edge. */
+  su2activematrix Normal; /*!< \brief Normal (area) of the edge. */
   const Index nEdge, nEdgeSIMD;
 
   friend class CPhysicalGeometry;
 
-public:
-  enum NodePosition : unsigned long {LEFT = 0, RIGHT = 1};
+ public:
+  enum NodePosition : unsigned long { LEFT = 0, RIGHT = 1 };
 
   /*!
    * \brief Constructor of the class.
@@ -68,14 +69,14 @@ class CEdge {
    * \param[in] iNode - Node index 0 or 1, LEFT or RIGHT.
    * \return Index of the node that composes the edge.
    */
-  inline unsigned long GetNode(unsigned long iEdge, unsigned long iNode) const { return Nodes(iEdge,iNode); }
+  inline unsigned long GetNode(unsigned long iEdge, unsigned long iNode) const { return Nodes(iEdge, iNode); }
 
   /*!
    * \brief SIMD version of GetNode, iNode returned for contiguous iEdges.
    */
-  template<class T, size_t N>
-  FORCEINLINE simd::Array<T,N> GetNode(simd::Array<T,N> iEdge, unsigned long iNode) const {
-    return simd::Array<T,N>(&Nodes(iEdge[0],iNode));
+  template <class T, size_t N>
+  FORCEINLINE simd::Array<T, N> GetNode(simd::Array<T, N> iEdge, unsigned long iNode) const {
+    return simd::Array<T, N>(&Nodes(iEdge[0], iNode));
   }
 
   /*!
@@ -116,10 +117,8 @@ class CEdge {
    * \param[in] coord_Point - Coordinates of the point that form the control volume.
    * \return Local volume associated to the edge.
    */
-  static su2double GetVolume(const su2double* coord_Edge_CG,
-                             const su2double* coord_FaceElem_CG,
-                             const su2double* coord_Elem_CG,
-                             const su2double* coord_Point);
+  static su2double GetVolume(const su2double* coord_Edge_CG, const su2double* coord_FaceElem_CG,
+                             const su2double* coord_Elem_CG, const su2double* coord_Point);
 
   /*!
    * \brief Compute the volume associated with an edge (2D version).
@@ -128,8 +127,7 @@ class CEdge {
    * \param[in] coord_Point - Coordinates of the point that form the control volume.
    * \return Local volume associated to the edge.
    */
-  static su2double GetVolume(const su2double* coord_Edge_CG,
-                             const su2double* coord_Elem_CG,
+  static su2double GetVolume(const su2double* coord_Edge_CG, const su2double* coord_Elem_CG,
                              const su2double* coord_Point);
 
   /*!
@@ -141,9 +139,7 @@ class CEdge {
    * \param[in] config - Definition of the particular problem.
    * \return Compute the normal (dimensional) to the face that makes the control volume boundaries.
    */
-  void SetNodes_Coord(unsigned long iEdge,
-                      const su2double* coord_Edge_CG,
-                      const su2double* coord_FaceElem_CG,
+  void SetNodes_Coord(unsigned long iEdge, const su2double* coord_Edge_CG, const su2double* coord_FaceElem_CG,
                       const su2double* coord_Elem_CG);
 
   /*!
@@ -154,19 +150,16 @@ class CEdge {
    * \param[in] config - Definition of the particular problem.
    * \return Compute the normal (dimensional) to the face that makes the contorl volume boundaries.
    */
-  void SetNodes_Coord(unsigned long iEdge,
-                      const su2double* coord_Edge_CG,
-                      const su2double* coord_Elem_CG);
+  void SetNodes_Coord(unsigned long iEdge, const su2double* coord_Edge_CG, const su2double* coord_Elem_CG);
 
   /*!
    * \brief Copy the the normal vector of a face.
    * \param[in] iEdge - Edge index.
    * \param[out] normal - Object into which the normal (dimensional) will be copied.
    */
-  template<class T>
+  template <class T>
   inline void GetNormal(unsigned long iEdge, T& normal) const {
-    for (auto iDim = 0ul; iDim < Normal.cols(); iDim++)
-      normal[iDim] = Normal(iEdge,iDim);
+    for (auto iDim = 0ul; iDim < Normal.cols(); iDim++) normal[iDim] = Normal(iEdge, iDim);
   }
 
   /*!
@@ -192,10 +185,9 @@ class CEdge {
    * \param[in] normal - Vector to initialize the normal vector.
    * \return Value of the normal vector.
    */
-  template<class T>
+  template <class T>
   void SetNormal(unsigned long iEdge, const T& normal) {
-    for (auto iDim = 0ul; iDim < Normal.cols(); ++iDim)
-      Normal(iEdge,iDim) = normal[iDim];
+    for (auto iDim = 0ul; iDim < Normal.cols(); ++iDim) Normal(iEdge, iDim) = normal[iDim];
   }
 
   /*!
@@ -203,10 +195,9 @@ class CEdge {
    * \param[in] iEdge - Edge index.
    * \param[in] normal - Vector to add to the normal vector.
    */
-  template<class T>
+  template <class T>
   void AddNormal(unsigned long iEdge, const T& normal) {
-    for (auto iDim = 0ul; iDim < Normal.cols(); ++iDim)
-      Normal(iEdge,iDim) += normal[iDim];
+    for (auto iDim = 0ul; iDim < Normal.cols(); ++iDim) Normal(iEdge, iDim) += normal[iDim];
   }
 
   /*!
@@ -214,10 +205,8 @@ class CEdge {
    * \param[in] iEdge - Edge index.
    * \param[in] normal - Vector to add to the normal vector.
    */
-  template<class T>
+  template <class T>
   void SubNormal(unsigned long iEdge, const T& normal) {
-    for (auto iDim = 0ul; iDim < Normal.cols(); ++iDim)
-      Normal(iEdge,iDim) -= normal[iDim];
+    for (auto iDim = 0ul; iDim < Normal.cols(); ++iDim) Normal(iEdge, iDim) -= normal[iDim];
   }
-
 };
diff --git a/Common/include/geometry/dual_grid/CPoint.hpp b/Common/include/geometry/dual_grid/CPoint.hpp
index 470dad563fd..4e78f588bfa 100644
--- a/Common/include/geometry/dual_grid/CPoint.hpp
+++ b/Common/include/geometry/dual_grid/CPoint.hpp
@@ -45,73 +45,84 @@ class CPhysicalGeometry;
  * \author F. Palacios
  */
 class CPoint {
-private:
+ private:
   friend class CPhysicalGeometry;
 
   const unsigned long nDim = 0;
 
-  su2vector<unsigned long> GlobalIndex;   /*!< \brief Global index in the parallel simulation. */
-  su2vector<unsigned long> Color;         /*!< \brief Color of the point in the partitioning strategy. */
-
-  CCompressedSparsePatternUL Point;       /*!< \brief Points surrounding the central node of the control volume. */
-  CCompressedSparsePatternL Edge;         /*!< \brief Edges that set up a control volume (same sparse structure as Point). */
-  CCompressedSparsePatternL Elem;         /*!< \brief Elements that set up a control volume around a node. */
-  vector<vector<long> > Vertex;           /*!< \brief Index of the vertex that correspond which the control volume (we need one for each marker in the same node). */
-
-  su2activevector Volume;                 /*!< \brief Volume or Area of the control volume in 3D and 2D. */
-  su2activevector Volume_n;               /*!< \brief Volume at time n. */
-  su2activevector Volume_nM1;             /*!< \brief Volume at time n-1. */
-  su2activevector Volume_Old;             /*!< \brief Old containers for Volume. */
-  su2activevector Volume_n_Old;           /*!< \brief Old containers for Volume at time n. */
-  su2activevector Volume_nM1_Old;         /*!< \brief Old containers for Volume at time n-1. */
-  su2activevector Periodic_Volume;        /*!< \brief Missing component of volume or area of a control volume on a periodic marker in 3D and 2D. */
-
-  su2vector<bool> Domain;                 /*!< \brief Indicates if a point must be computed or belong to another boundary */
-  su2vector<bool> Boundary;               /*!< \brief To see if a point belong to the boundary (including MPI). */
-  su2vector<bool> PhysicalBoundary;       /*!< \brief To see if a point belong to the physical boundary (without includin MPI). */
-  su2vector<bool> SolidBoundary;          /*!< \brief To see if a point belong to the physical boundary (without includin MPI). */
-  su2vector<bool> ViscousBoundary;        /*!< \brief To see if a point belong to the physical boundary (without includin MPI). */
-  su2vector<bool> PeriodicBoundary;       /*!< \brief To see if a point belongs to a periodic boundary (without including MPI). */
-
-  su2activematrix Coord;                  /*!< \brief vector with the coordinates of the node. */
-  su2activematrix Coord_Old;              /*!< \brief Old coordinates vector for primal solution reloading for Disc.Adj. with dynamic grid. */
-  su2activematrix Coord_Sum;              /*!< \brief Sum of coordinates vector for geometry smoothing. */
-  su2activematrix Coord_n;                /*!< \brief Coordinates at time n for use with dynamic meshes. */
-  su2activematrix Coord_n1;               /*!< \brief Coordinates at time n-1 for use with dynamic meshes. */
-  su2activematrix Coord_p1;               /*!< \brief Coordinates at time n+1 for use with dynamic meshes. */
-
-  su2activematrix GridVel;                /*!< \brief Velocity of the grid for dynamic mesh cases. */
-  CVectorOfMatrix GridVel_Grad;           /*!< \brief Gradient of the grid velocity for dynamic meshes. */
-
-  su2vector<unsigned long> Parent_CV;          /*!< \brief Index of the parent control volume in the agglomeration process. */
-  su2vector<unsigned short> nChildren_CV;      /*!< \brief Number of children in the agglomeration process. */
-  vector<vector<unsigned long> > Children_CV;  /*!< \brief Index of the children control volumes in the agglomeration process. */
-  su2vector<bool> Agglomerate_Indirect;        /*!< \brief This flag indicates if the indirect points can be agglomerated. */
-  su2vector<bool> Agglomerate;                 /*!< \brief This flag indicates if the element has been agglomerated. */
-
-  su2vector<unsigned short> nNeighbor;    /*!< \brief Number of neighbors, needed by some numerical methods. */
+  su2vector<unsigned long> GlobalIndex; /*!< \brief Global index in the parallel simulation. */
+  su2vector<unsigned long> Color;       /*!< \brief Color of the point in the partitioning strategy. */
+
+  CCompressedSparsePatternUL Point; /*!< \brief Points surrounding the central node of the control volume. */
+  CCompressedSparsePatternL Edge;   /*!< \brief Edges that set up a control volume (same sparse structure as Point). */
+  CCompressedSparsePatternL Elem;   /*!< \brief Elements that set up a control volume around a node. */
+  vector<vector<long> > Vertex; /*!< \brief Index of the vertex that correspond which the control volume (we need one
+                                   for each marker in the same node). */
+
+  su2activevector Volume;          /*!< \brief Volume or Area of the control volume in 3D and 2D. */
+  su2activevector Volume_n;        /*!< \brief Volume at time n. */
+  su2activevector Volume_nM1;      /*!< \brief Volume at time n-1. */
+  su2activevector Volume_Old;      /*!< \brief Old containers for Volume. */
+  su2activevector Volume_n_Old;    /*!< \brief Old containers for Volume at time n. */
+  su2activevector Volume_nM1_Old;  /*!< \brief Old containers for Volume at time n-1. */
+  su2activevector Periodic_Volume; /*!< \brief Missing component of volume or area of a control volume on a periodic
+                                      marker in 3D and 2D. */
+
+  su2vector<bool> Domain;   /*!< \brief Indicates if a point must be computed or belong to another boundary */
+  su2vector<bool> Boundary; /*!< \brief To see if a point belong to the boundary (including MPI). */
+  su2vector<bool>
+      PhysicalBoundary; /*!< \brief To see if a point belong to the physical boundary (without includin MPI). */
+  su2vector<bool>
+      SolidBoundary; /*!< \brief To see if a point belong to the physical boundary (without includin MPI). */
+  su2vector<bool>
+      ViscousBoundary; /*!< \brief To see if a point belong to the physical boundary (without includin MPI). */
+  su2vector<bool>
+      PeriodicBoundary; /*!< \brief To see if a point belongs to a periodic boundary (without including MPI). */
+
+  su2activematrix Coord; /*!< \brief vector with the coordinates of the node. */
+  su2activematrix
+      Coord_Old; /*!< \brief Old coordinates vector for primal solution reloading for Disc.Adj. with dynamic grid. */
+  su2activematrix Coord_Sum; /*!< \brief Sum of coordinates vector for geometry smoothing. */
+  su2activematrix Coord_n;   /*!< \brief Coordinates at time n for use with dynamic meshes. */
+  su2activematrix Coord_n1;  /*!< \brief Coordinates at time n-1 for use with dynamic meshes. */
+  su2activematrix Coord_p1;  /*!< \brief Coordinates at time n+1 for use with dynamic meshes. */
+
+  su2activematrix GridVel;      /*!< \brief Velocity of the grid for dynamic mesh cases. */
+  CVectorOfMatrix GridVel_Grad; /*!< \brief Gradient of the grid velocity for dynamic meshes. */
+
+  su2vector<unsigned long> Parent_CV; /*!< \brief Index of the parent control volume in the agglomeration process. */
+  su2vector<unsigned short> nChildren_CV; /*!< \brief Number of children in the agglomeration process. */
+  vector<vector<unsigned long> >
+      Children_CV; /*!< \brief Index of the children control volumes in the agglomeration process. */
+  su2vector<bool> Agglomerate_Indirect; /*!< \brief This flag indicates if the indirect points can be agglomerated. */
+  su2vector<bool> Agglomerate;          /*!< \brief This flag indicates if the element has been agglomerated. */
+
+  su2vector<unsigned short> nNeighbor; /*!< \brief Number of neighbors, needed by some numerical methods. */
 
   /*--- Closest element on a viscous wall, and distance to it. ---*/
-  su2activevector Wall_Distance;          /*!< \brief Distance to the nearest wall. */
-  su2vector<int> ClosestWall_Rank; /*!< \brief Rank of process holding the closest wall element. */
+  su2activevector Wall_Distance;              /*!< \brief Distance to the nearest wall. */
+  su2vector<int> ClosestWall_Rank;            /*!< \brief Rank of process holding the closest wall element. */
   su2vector<unsigned short> ClosestWall_Zone; /*!< \brief Zone index of closest wall element. */
-  su2vector<unsigned short> ClosestWall_Marker; /*!< \brief Marker index of closest wall element, for given rank and zone index. */
-  su2vector<unsigned long> ClosestWall_Elem; /*!< \brief Element index of closest wall element, for givenrank, zone and marker index. */
+  su2vector<unsigned short>
+      ClosestWall_Marker; /*!< \brief Marker index of closest wall element, for given rank and zone index. */
+  su2vector<unsigned long>
+      ClosestWall_Elem; /*!< \brief Element index of closest wall element, for givenrank, zone and marker index. */
 
-  su2activevector SharpEdge_Distance;     /*!< \brief Distance to a sharp edge. */
-  su2activevector Curvature;              /*!< \brief Value of the surface curvature (SU2_GEO). */
-  su2activevector MaxLength;              /*!< \brief The maximum cell-center to cell-center length. */
-  su2activevector RoughnessHeight;          /*!< \brief Roughness of the nearest wall. */
+  su2activevector SharpEdge_Distance; /*!< \brief Distance to a sharp edge. */
+  su2activevector Curvature;          /*!< \brief Value of the surface curvature (SU2_GEO). */
+  su2activevector MaxLength;          /*!< \brief The maximum cell-center to cell-center length. */
+  su2activevector RoughnessHeight;    /*!< \brief Roughness of the nearest wall. */
 
-  su2matrix<int> AD_InputIndex;           /*!< \brief Indices of Coord variables in the adjoint vector. */
-  su2matrix<int> AD_OutputIndex;          /*!< \brief Indices of Coord variables in the adjoint vector after having been updated. */
+  su2matrix<int> AD_InputIndex; /*!< \brief Indices of Coord variables in the adjoint vector. */
+  su2matrix<int>
+      AD_OutputIndex; /*!< \brief Indices of Coord variables in the adjoint vector after having been updated. */
 
   /*!
    * \brief Allocate fields required by the minimal constructor.
    */
   void MinimalAllocation(unsigned long npoint);
 
-public:
+ public:
   /*!
    * \brief "Full" constructor of the class.
    * \param[in] npoint - Number of points (dual volumes) in the problem.
@@ -144,14 +155,14 @@ class CPoint {
    * \param[in] iDim - Number of dimensions of the problem.
    * \return Coordinate that correspond with <i>iDim</i>.
    */
-  inline su2double GetCoord(unsigned long iPoint, unsigned long iDim) const { return Coord(iPoint,iDim); }
+  inline su2double GetCoord(unsigned long iPoint, unsigned long iDim) const { return Coord(iPoint, iDim); }
 
   /*!
    * \brief Get the coordinates of the control volume.
    * \param[in] iPoint - Index of the point.
    * \return pointer to the coordinate of the point.
    */
-  inline su2double *GetCoord(unsigned long iPoint) { return Coord[iPoint]; }
+  inline su2double* GetCoord(unsigned long iPoint) { return Coord[iPoint]; }
 
   /*!
    * \brief Get the entire matrix of coordinates of the control volumes.
@@ -164,7 +175,7 @@ class CPoint {
    * \param[in] iDim - Position to store the coordinate.
    * \param[in] coord - Coordinate for iDim.
    */
-  inline void SetCoord(unsigned long iPoint, unsigned long iDim, su2double coord) { Coord(iPoint,iDim) = coord; }
+  inline void SetCoord(unsigned long iPoint, unsigned long iDim, su2double coord) { Coord(iPoint, iDim) = coord; }
 
   /*!
    * \brief Set the coordinates for the control volume.
@@ -172,16 +183,15 @@ class CPoint {
    * \param[in] iDim - Position to store the coordinate.
    * \param[in] coord - Coordinate for iDim.
    */
-  inline void AddCoord(unsigned long iPoint, unsigned long iDim, su2double coord) { Coord(iPoint,iDim) += coord; }
+  inline void AddCoord(unsigned long iPoint, unsigned long iDim, su2double coord) { Coord(iPoint, iDim) += coord; }
 
   /*!
    * \brief Set the point coordinates.
    * \param[in] iPoint - Index of the point.
    * \param[in] coord - Coordinate of the point.
    */
-  inline void SetCoord(unsigned long iPoint, const su2double *coord) {
-    for (unsigned long iDim = 0; iDim < nDim; iDim++)
-      Coord(iPoint,iDim) = coord[iDim];
+  inline void SetCoord(unsigned long iPoint, const su2double* coord) {
+    for (unsigned long iDim = 0; iDim < nDim; iDim++) Coord(iPoint, iDim) = coord[iDim];
   }
 
   /*!
@@ -208,12 +218,16 @@ class CPoint {
    * \param[in] nelem - Position where the element is stored.
    * \return Index of the element.
    */
-  inline unsigned long GetElem(unsigned long iPoint, unsigned long nelem) const { return Elem.getInnerIdx(iPoint,nelem); }
+  inline unsigned long GetElem(unsigned long iPoint, unsigned long nelem) const {
+    return Elem.getInnerIdx(iPoint, nelem);
+  }
 
   /*!
    * \brief Get inner iterator to loop over neighbor elements.
    */
-  inline CCompressedSparsePatternL::CInnerIter GetElems(unsigned long iPoint) const { return Elem.getInnerIter(iPoint); }
+  inline CCompressedSparsePatternL::CInnerIter GetElems(unsigned long iPoint) const {
+    return Elem.getInnerIter(iPoint);
+  }
 
   /*!
    * \brief Set the points that compose the control volume.
@@ -229,7 +243,10 @@ class CPoint {
   /*!
    * \brief Reset the points that compose the control volume.
    */
-  inline void ResetPoints() { Point = CCompressedSparsePatternUL(); Edge = CCompressedSparsePatternL(); }
+  inline void ResetPoints() {
+    Point = CCompressedSparsePatternUL();
+    Edge = CCompressedSparsePatternL();
+  }
 
   /*!
    * \brief Get the number of points that compose the control volume.
@@ -244,12 +261,16 @@ class CPoint {
    * \param[in] point - Position where the point is stored.
    * \return Index of the point.
    */
-  inline unsigned long GetPoint(unsigned long iPoint, unsigned long npoint) const { return Point.getInnerIdx(iPoint,npoint); }
+  inline unsigned long GetPoint(unsigned long iPoint, unsigned long npoint) const {
+    return Point.getInnerIdx(iPoint, npoint);
+  }
 
   /*!
    * \brief Get inner iterator to loop over neighbor points.
    */
-  inline CCompressedSparsePatternUL::CInnerIter GetPoints(unsigned long iPoint) const { return Point.getInnerIter(iPoint); }
+  inline CCompressedSparsePatternUL::CInnerIter GetPoints(unsigned long iPoint) const {
+    return Point.getInnerIter(iPoint);
+  }
 
   /*!
    * \brief Set the edges that compose the control volume.
@@ -257,7 +278,9 @@ class CPoint {
    * \param[in] iedge - Edge to be added.
    * \param[in] nedge - Position in which is going to be stored the edge for each control volume.
    */
-  inline void SetEdge(unsigned long iPoint, long iedge, unsigned long nedge) { Edge.getInnerIdx(iPoint,nedge) = iedge; }
+  inline void SetEdge(unsigned long iPoint, long iedge, unsigned long nedge) {
+    Edge.getInnerIdx(iPoint, nedge) = iedge;
+  }
 
   /*!
    * \brief Get all the edges that compose the control volume.
@@ -265,12 +288,14 @@ class CPoint {
    * \param[in] nedge - Position where the edge is stored.
    * \return Index of the edge.
    */
-  inline long GetEdge(unsigned long iPoint, unsigned long nedge) const { return Edge.getInnerIdx(iPoint,nedge); }
+  inline long GetEdge(unsigned long iPoint, unsigned long nedge) const { return Edge.getInnerIdx(iPoint, nedge); }
 
   /*!
    * \brief Get inner iterator to loop over neighbor edges.
    */
-  inline CCompressedSparsePatternL::CInnerIter GetEdges(unsigned long iPoint) const { return Edge.getInnerIter(iPoint); }
+  inline CCompressedSparsePatternL::CInnerIter GetEdges(unsigned long iPoint) const {
+    return Edge.getInnerIter(iPoint);
+  }
 
   /*!
    * \brief Set the boundary vertex that compose the control volume.
@@ -289,8 +314,10 @@ class CPoint {
    * \return Index of the vertex.
    */
   inline long GetVertex(unsigned long iPoint, unsigned long iMarker) const {
-    if (Boundary(iPoint)) return Vertex[iPoint][iMarker];
-    else return -1;
+    if (Boundary(iPoint))
+      return Vertex[iPoint][iMarker];
+    else
+      return -1;
   }
 
   /*!
@@ -300,7 +327,7 @@ class CPoint {
    * \param[in] nMarker - Max number of marker.
    */
   inline void SetBoundary(unsigned long iPoint, unsigned short nMarker) {
-    if (!Boundary(iPoint)) Vertex[iPoint].resize(nMarker,-1);
+    if (!Boundary(iPoint)) Vertex[iPoint].resize(nMarker, -1);
     Boundary(iPoint) = true;
   }
 
@@ -308,7 +335,10 @@ class CPoint {
    * \brief Reset the boundary of a control volume.
    * \param[in] iPoint - Index of the point.
    */
-  inline void ResetBoundary(unsigned long iPoint) { Vertex[iPoint].clear(); Boundary(iPoint) = false; }
+  inline void ResetBoundary(unsigned long iPoint) {
+    Vertex[iPoint].clear();
+    Boundary(iPoint) = false;
+  }
 
   /*!
    * \brief Mark the point as boundary.
@@ -602,7 +632,7 @@ class CPoint {
    */
   void SetVolume_n_Old();
 
-    /*!
+  /*!
    * \brief Set the Volume_nM1 to Volume_nM1_Old.
    */
   void SetVolume_nM1_Old();
@@ -613,7 +643,8 @@ class CPoint {
    * \param[in] parent_CV - Index of the parent control volume.
    */
   inline void SetParent_CV(unsigned long iPoint, unsigned long parent_CV) {
-    Parent_CV(iPoint) = parent_CV; Agglomerate(iPoint) = true;
+    Parent_CV(iPoint) = parent_CV;
+    Agglomerate(iPoint) = true;
   }
 
   /*!
@@ -623,7 +654,7 @@ class CPoint {
    * \param[in] children_CV - Index of the children control volume.
    */
   inline void SetChildren_CV(unsigned long iPoint, unsigned long nchildren_CV, unsigned long children_CV) {
-    Children_CV[iPoint].resize(nchildren_CV+1);
+    Children_CV[iPoint].resize(nchildren_CV + 1);
     Children_CV[iPoint][nchildren_CV] = children_CV;
   }
 
@@ -663,7 +694,9 @@ class CPoint {
    * \param[in] iPoint - Index of the point.
    * \param[in] agglomerate - The indirect neigbors can be agglomerated.
    */
-  inline void SetAgglomerate_Indirect(unsigned long iPoint, bool agglomerate) { Agglomerate_Indirect(iPoint) = agglomerate; };
+  inline void SetAgglomerate_Indirect(unsigned long iPoint, bool agglomerate) {
+    Agglomerate_Indirect(iPoint) = agglomerate;
+  };
 
   /*!
    * \brief Get the number of children of an agglomerated control volume.
@@ -677,28 +710,30 @@ class CPoint {
    * \param[in] iPoint - Index of the point.
    * \param[in] nchildren_CV - Number of children of the control volume.
    */
-  inline void SetnChildren_CV(unsigned long iPoint, unsigned short nchildren_CV) { nChildren_CV(iPoint) = nchildren_CV; }
+  inline void SetnChildren_CV(unsigned long iPoint, unsigned short nchildren_CV) {
+    nChildren_CV(iPoint) = nchildren_CV;
+  }
 
   /*!
    * \brief Get the coordinates of the control volume at time n.
    * \param[in] iPoint - Index of the point.
    * \return Coordinates of the control volume at time n.
    */
-  inline su2double *GetCoord_n(unsigned long iPoint) { return Coord_n[iPoint]; }
+  inline su2double* GetCoord_n(unsigned long iPoint) { return Coord_n[iPoint]; }
 
   /*!
    * \brief Get the coordinates of the control volume at time n-1.
    * \param[in] iPoint - Index of the point.
    * \return Volume of the control volume at time n-1
    */
-  inline su2double *GetCoord_n1(unsigned long iPoint) { return Coord_n1[iPoint]; }
+  inline su2double* GetCoord_n1(unsigned long iPoint) { return Coord_n1[iPoint]; }
 
   /*!
    * \brief Get the coordinates of the control volume at time n+1.
    * \param[in] iPoint - Index of the point.
    * \return Volume of the control volume at time n+1
    */
-  inline su2double *GetCoord_p1(unsigned long iPoint) { return Coord_p1[iPoint]; }
+  inline su2double* GetCoord_p1(unsigned long iPoint) { return Coord_p1[iPoint]; }
 
   /*!
    * \brief Set the coordinates of the control volume at time n to the ones in <i>Coord</i>.
@@ -715,9 +750,8 @@ class CPoint {
    * \param[in] iPoint - Index of the point.
    * \param[in] coord - Value of the grid coordinates at time n.
    */
-  inline void SetCoord_n(unsigned long iPoint, const su2double *coord) {
-    for (unsigned long iDim = 0; iDim < nDim; iDim++)
-      Coord_n(iPoint,iDim) = coord[iDim];
+  inline void SetCoord_n(unsigned long iPoint, const su2double* coord) {
+    for (unsigned long iDim = 0; iDim < nDim; iDim++) Coord_n(iPoint, iDim) = coord[iDim];
   }
 
   /*!
@@ -725,9 +759,8 @@ class CPoint {
    * \param[in] iPoint - Index of the point.
    * \param[in] coord - Value of the grid coordinates at time n-1.
    */
-  inline void SetCoord_n1(unsigned long iPoint, const su2double *coord) {
-    for (unsigned long iDim = 0; iDim < nDim; iDim++)
-      Coord_n1(iPoint,iDim) = coord[iDim];
+  inline void SetCoord_n1(unsigned long iPoint, const su2double* coord) {
+    for (unsigned long iDim = 0; iDim < nDim; iDim++) Coord_n1(iPoint, iDim) = coord[iDim];
   }
 
   /*!
@@ -735,9 +768,8 @@ class CPoint {
    * \param[in] iPoint - Index of the point.
    * \param[in] coord - Value of the grid coordinates at time n+1.
    */
-  inline void SetCoord_p1(unsigned long iPoint, const su2double *coord) {
-    for (unsigned long iDim = 0; iDim < nDim; iDim++)
-      Coord_p1(iPoint,iDim) = coord[iDim];
+  inline void SetCoord_p1(unsigned long iPoint, const su2double* coord) {
+    for (unsigned long iDim = 0; iDim < nDim; iDim++) Coord_p1(iPoint, iDim) = coord[iDim];
   }
 
   /*!
@@ -745,16 +777,15 @@ class CPoint {
    * \param[in] iPoint - Index of the point.
    * \return Old coordinates at a point.
    */
-  inline su2double *GetCoord_Old(unsigned long iPoint) { return Coord_Old[iPoint]; }
+  inline su2double* GetCoord_Old(unsigned long iPoint) { return Coord_Old[iPoint]; }
 
   /*!
    * \brief Set the value of the vector <i>Coord_Old</i> for implicit smoothing.
    * \param[in] iPoint - Index of the point.
    * \param[in] coord_old - Value of the coordinates.
    */
-  inline void SetCoord_Old(unsigned long iPoint, const su2double *coord_old) {
-    for (unsigned long iDim = 0; iDim < nDim; iDim++)
-      Coord_Old(iPoint,iDim) = coord_old[iDim];
+  inline void SetCoord_Old(unsigned long iPoint, const su2double* coord_old) {
+    for (unsigned long iDim = 0; iDim < nDim; iDim++) Coord_Old(iPoint, iDim) = coord_old[iDim];
   }
 
   /*!
@@ -767,16 +798,15 @@ class CPoint {
    * \param[in] iPoint - Index of the point.
    * \return Sum of coordinates at a point.
    */
-  inline su2double *GetCoord_Sum(unsigned long iPoint) { return Coord_Sum[iPoint]; }
+  inline su2double* GetCoord_Sum(unsigned long iPoint) { return Coord_Sum[iPoint]; }
 
   /*!
    * \brief Add the value of the coordinates to the <i>Coord_Sum</i> vector for implicit smoothing.
    * \param[in] iPoint - Index of the point.
    * \param[in] coord_sum - Value of the coordinates to add.
    */
-  inline void AddCoord_Sum(unsigned long iPoint, const su2double *coord_sum) {
-    for (unsigned long iDim = 0; iDim < nDim; iDim++)
-      Coord_Sum(iPoint,iDim) += coord_sum[iDim];
+  inline void AddCoord_Sum(unsigned long iPoint, const su2double* coord_sum) {
+    for (unsigned long iDim = 0; iDim < nDim; iDim++) Coord_Sum(iPoint, iDim) += coord_sum[iDim];
   }
 
   /*!
@@ -789,7 +819,7 @@ class CPoint {
    * \param[in] iPoint - Index of the point.
    * \return Grid velocity at the point.
    */
-  inline su2double *GetGridVel(unsigned long iPoint) { return GridVel[iPoint]; }
+  inline su2double* GetGridVel(unsigned long iPoint) { return GridVel[iPoint]; }
 
   /*!
    * \brief Get the grid velocity matrix for the entire domain.
@@ -802,16 +832,17 @@ class CPoint {
    * \param[in] iDim - Index of the coordinate.
    * \param[in] gridvel - Value of the grid velocity.
    */
-  inline void SetGridVel(unsigned long iPoint, unsigned long iDim, su2double gridvel) { GridVel(iPoint,iDim) = gridvel; }
+  inline void SetGridVel(unsigned long iPoint, unsigned long iDim, su2double gridvel) {
+    GridVel(iPoint, iDim) = gridvel;
+  }
 
   /*!
    * \brief Set the value of the grid velocity at the point.
    * \param[in] iPoint - Index of the point.
    * \param[in] gridvel - Value of the grid velocity.
    */
-  inline void SetGridVel(unsigned long iPoint, const su2double *gridvel) {
-    for (unsigned long iDim = 0; iDim < nDim; iDim++)
-      GridVel(iPoint,iDim) = gridvel[iDim];
+  inline void SetGridVel(unsigned long iPoint, const su2double* gridvel) {
+    for (unsigned long iDim = 0; iDim < nDim; iDim++) GridVel(iPoint, iDim) = gridvel[iDim];
   }
 
   /*!
@@ -831,9 +862,9 @@ class CPoint {
    * \param[in] iPoint - Index of the point.
    * \param[in] adj_sol - Adjoint values of the Coord variables.
    */
-  inline void SetAdjointSolution(unsigned long iPoint, const su2double *adj_sol) {
+  inline void SetAdjointSolution(unsigned long iPoint, const su2double* adj_sol) {
     for (unsigned long iDim = 0; iDim < nDim; iDim++)
-      AD::SetDerivative(AD_OutputIndex(iPoint,iDim), SU2_TYPE::GetValue(adj_sol[iDim]));
+      AD::SetDerivative(AD_OutputIndex(iPoint, iDim), SU2_TYPE::GetValue(adj_sol[iDim]));
   }
 
   /*!
@@ -842,7 +873,7 @@ class CPoint {
    * \param[in] iDim - Dimension.
    */
   inline su2double GetAdjointSolution(unsigned long iPoint, unsigned long iDim) const {
-    return AD::GetDerivative(AD_InputIndex(iPoint,iDim));
+    return AD::GetDerivative(AD_InputIndex(iPoint, iDim));
   }
 
   /*!
@@ -852,13 +883,12 @@ class CPoint {
    */
   inline void RegisterCoordinates(unsigned long iPoint, bool input) {
     for (unsigned long iDim = 0; iDim < nDim; iDim++) {
-      if(input) {
-        AD::RegisterInput(Coord(iPoint,iDim));
-        AD::SetIndex(AD_InputIndex(iPoint,iDim), Coord(iPoint,iDim));
-      }
-      else {
-        AD::RegisterOutput(Coord(iPoint,iDim));
-        AD::SetIndex(AD_OutputIndex(iPoint,iDim), Coord(iPoint,iDim));
+      if (input) {
+        AD::RegisterInput(Coord(iPoint, iDim));
+        AD::SetIndex(AD_InputIndex(iPoint, iDim), Coord(iPoint, iDim));
+      } else {
+        AD::RegisterOutput(Coord(iPoint, iDim));
+        AD::SetIndex(AD_OutputIndex(iPoint, iDim), Coord(iPoint, iDim));
       }
     }
   }
@@ -867,16 +897,15 @@ class CPoint {
    * \brief Set wall roughnesses according to stored closest wall information.
    * \param[in] roughness - Mapping [rank][zone][marker] -> roughness
    */
-  template<typename Roughness_type>
-  void SetWallRoughness(Roughness_type const& roughness){
-    for (unsigned long iPoint=0; iPoint<GlobalIndex.size(); ++iPoint) {
+  template <typename Roughness_type>
+  void SetWallRoughness(Roughness_type const& roughness) {
+    for (unsigned long iPoint = 0; iPoint < GlobalIndex.size(); ++iPoint) {
       auto rankID = ClosestWall_Rank[iPoint];
       auto zoneID = ClosestWall_Zone[iPoint];
       auto markerID = ClosestWall_Marker[iPoint];
-      if(rankID >= 0){
+      if (rankID >= 0) {
         SetRoughnessHeight(iPoint, roughness[rankID][zoneID][markerID]);
       }
     }
   }
-
 };
diff --git a/Common/include/geometry/dual_grid/CTurboVertex.hpp b/Common/include/geometry/dual_grid/CTurboVertex.hpp
index 6b65d208179..47a88bfb5fd 100644
--- a/Common/include/geometry/dual_grid/CTurboVertex.hpp
+++ b/Common/include/geometry/dual_grid/CTurboVertex.hpp
@@ -36,19 +36,19 @@
  * \author S. Vitale
  */
 class CTurboVertex final : public CVertex {
-private:
-  su2double *TurboNormal;     /*!< \brief Normal for computing correct turbomachinery quantities. */
-  su2double Area;             /*!< \brief Value of the face area associated to the vertex */
+ private:
+  su2double* TurboNormal; /*!< \brief Normal for computing correct turbomachinery quantities. */
+  su2double Area;         /*!< \brief Value of the face area associated to the vertex */
   //  su2double PitchCoord;       /*!< \brief Value of the abscissa pitch wise */
-  su2double AngularCoord;     /*!< \brief Value of the angular coordinate  */
-  su2double DeltaAngularCoord;     /*!< \brief Value of the angular coordinate w.r.t. the minimum pitch point  */
-  su2double RelAngularCoord; /*!< \brief Value of the angular coordinate w.r.t. the minimum pitch point  */
+  su2double AngularCoord;      /*!< \brief Value of the angular coordinate  */
+  su2double DeltaAngularCoord; /*!< \brief Value of the angular coordinate w.r.t. the minimum pitch point  */
+  su2double RelAngularCoord;   /*!< \brief Value of the angular coordinate w.r.t. the minimum pitch point  */
 
-  unsigned long OldVertex;    /*!< \brief Value of the vertex numeration before the ordering */
-  int GlobalIndex;            /*!< \brief Value of the vertex numeration after the ordering and global with respect to MPI partinioning */
-
-public:
+  unsigned long OldVertex; /*!< \brief Value of the vertex numeration before the ordering */
+  int GlobalIndex;         /*!< \brief Value of the vertex numeration after the ordering and global with respect to MPI
+                              partinioning */
 
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] val_point - Node of the vertex.
@@ -65,17 +65,16 @@ class CTurboVertex final : public CVertex {
    * \brief set Normal in the turbomachinery frame of reference.
    * \param[in] val_normal - normal vector.
    */
-  inline void SetTurboNormal(const su2double *val_normal) {
+  inline void SetTurboNormal(const su2double* val_normal) {
     unsigned short iDim;
-    for(iDim= 0; iDim < nDim; iDim++)
-      TurboNormal[iDim] = val_normal[iDim];
+    for (iDim = 0; iDim < nDim; iDim++) TurboNormal[iDim] = val_normal[iDim];
   }
 
   /*!
    * \brief set face Area.
    * \param[in] val_area - value of the face area.
    */
-  inline void SetArea(su2double val_area){Area = val_area;}
+  inline void SetArea(su2double val_area) { Area = val_area; }
 
   /*!
    * \brief get face Area associate to the vertex.
@@ -86,22 +85,21 @@ class CTurboVertex final : public CVertex {
    * \brief Copy the the turbo normal vector of a face.
    * \param[in] val_normal - Vector where the subroutine is goint to copy the normal (dimensionaless).
    */
-  inline void GetTurboNormal(su2double *val_normal) const {
-    for (unsigned short iDim = 0; iDim < nDim; iDim++)
-      val_normal[iDim] = TurboNormal[iDim];
+  inline void GetTurboNormal(su2double* val_normal) const {
+    for (unsigned short iDim = 0; iDim < nDim; iDim++) val_normal[iDim] = TurboNormal[iDim];
   }
 
   /*!
    * \brief Get the turbo normal to a face where turboperformance are computed .
    * \return Dimensionaless normal vector, the modulus is the area of the face.
    */
-  inline su2double *GetTurboNormal(void) { return TurboNormal; }
+  inline su2double* GetTurboNormal(void) { return TurboNormal; }
 
   /*!
    * \brief set vertex value not ordered.
    * \param[in] val_vertex - value of the vertex before ordering.
    */
-  inline void SetOldVertex(unsigned long val_vertex){OldVertex = val_vertex;}
+  inline void SetOldVertex(unsigned long val_vertex) { OldVertex = val_vertex; }
 
   /*!
    * \brief retrieve vertex value not ordered.
@@ -111,17 +109,17 @@ class CTurboVertex final : public CVertex {
   /*!
    * \brief set global index for ordered span-wise turbovertex.
    */
-  inline void SetGlobalVertexIndex(int globalindex) { GlobalIndex = globalindex;}
+  inline void SetGlobalVertexIndex(int globalindex) { GlobalIndex = globalindex; }
 
   /*!
    * \brief get global index for ordered span-wise turbovertex.
    */
-  inline int GetGlobalVertexIndex(void) const {return GlobalIndex;}
+  inline int GetGlobalVertexIndex(void) const { return GlobalIndex; }
 
   /*!
    * \brief set angular coord.
    */
-  inline void SetAngularCoord(su2double angCoord) {AngularCoord = angCoord;}
+  inline void SetAngularCoord(su2double angCoord) { AngularCoord = angCoord; }
 
   /*!
    * \brief get angular coord.
@@ -131,7 +129,7 @@ class CTurboVertex final : public CVertex {
   /*!
    * \brief set angular coord.
    */
-  inline void SetDeltaAngularCoord(su2double deltaAngCoord){DeltaAngularCoord = deltaAngCoord;}
+  inline void SetDeltaAngularCoord(su2double deltaAngCoord) { DeltaAngularCoord = deltaAngCoord; }
 
   /*!
    * \brief get angular coord.
@@ -141,11 +139,10 @@ class CTurboVertex final : public CVertex {
   /*!
    * \brief set angular coord.
    */
-  inline void SetRelAngularCoord(su2double minAngCoord) {RelAngularCoord = AngularCoord - minAngCoord;}
+  inline void SetRelAngularCoord(su2double minAngCoord) { RelAngularCoord = AngularCoord - minAngCoord; }
 
   /*!
    * \brief get angular coord.
    */
-  inline su2double GetRelAngularCoord(void) const {return RelAngularCoord;}
-
+  inline su2double GetRelAngularCoord(void) const { return RelAngularCoord; }
 };
diff --git a/Common/include/geometry/dual_grid/CVertex.hpp b/Common/include/geometry/dual_grid/CVertex.hpp
index d2baf9c387b..3d18f439eef 100644
--- a/Common/include/geometry/dual_grid/CVertex.hpp
+++ b/Common/include/geometry/dual_grid/CVertex.hpp
@@ -36,19 +36,19 @@
  * \author F. Palacios
  */
 class CVertex : public CDualGrid {
-protected:
-  unsigned long Nodes[1];               /*!< \brief Vector to store the global nodes of an element. */
-  su2double Normal[3] = {0.0};          /*!< \brief Normal coordinates of the element and its center of gravity. */
-  su2double Aux_Var;                    /*!< \brief Auxiliar variable defined only on the surface. */
-  su2double CartCoord[3] = {0.0};       /*!< \brief Vertex cartesians coordinates. */
-  su2double VarCoord[3] = {0.0};        /*!< \brief Used for storing the coordinate variation due to a surface modification. */
-  long PeriodicPoint[5] = {-1};         /*!< \brief Store the periodic point of a boundary (iProcessor, iPoint) */
-  bool ActDisk_Perimeter = false;       /*!< \brief Identify nodes at the perimeter of the actuator disk */
-  short Rotation_Type;                  /*!< \brief Type of rotation associated with the vertex (MPI and periodic) */
-  unsigned long Normal_Neighbor;        /*!< \brief Index of the closest neighbor. */
-  su2double Basis_Function[3] = {0.0};  /*!< \brief Basis function values for interpolation across zones. */
-
-public:
+ protected:
+  unsigned long Nodes[1];         /*!< \brief Vector to store the global nodes of an element. */
+  su2double Normal[3] = {0.0};    /*!< \brief Normal coordinates of the element and its center of gravity. */
+  su2double Aux_Var;              /*!< \brief Auxiliar variable defined only on the surface. */
+  su2double CartCoord[3] = {0.0}; /*!< \brief Vertex cartesians coordinates. */
+  su2double VarCoord[3] = {0.0}; /*!< \brief Used for storing the coordinate variation due to a surface modification. */
+  long PeriodicPoint[5] = {-1};  /*!< \brief Store the periodic point of a boundary (iProcessor, iPoint) */
+  bool ActDisk_Perimeter = false;      /*!< \brief Identify nodes at the perimeter of the actuator disk */
+  short Rotation_Type;                 /*!< \brief Type of rotation associated with the vertex (MPI and periodic) */
+  unsigned long Normal_Neighbor;       /*!< \brief Index of the closest neighbor. */
+  su2double Basis_Function[3] = {0.0}; /*!< \brief Basis function values for interpolation across zones. */
+
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] val_point - Node of the vertex.
@@ -75,8 +75,8 @@ class CVertex : public CDualGrid {
    * \param[in] val_coord_Elem_CG - Coordinates of the centre of gravity of the element.
    * \return Compute the normal (dimensional) to the face that makes the vertex.
    */
-  void SetNodes_Coord(const su2double *val_coord_Edge_CG, const su2double *val_coord_FaceElem_CG,
-                      const su2double *val_coord_Elem_CG) override;
+  void SetNodes_Coord(const su2double* val_coord_Edge_CG, const su2double* val_coord_FaceElem_CG,
+                      const su2double* val_coord_Elem_CG) override;
 
   /*!
    * \overload
@@ -84,22 +84,21 @@ class CVertex : public CDualGrid {
    * \param[in] val_coord_Elem_CG - Coordinates of the centre of gravity of the element.
    * \return Compute the normal (dimensional) to the face that makes the vertex.
    */
-  void SetNodes_Coord(const su2double *val_coord_Edge_CG, const su2double *val_coord_Elem_CG) override;
+  void SetNodes_Coord(const su2double* val_coord_Edge_CG, const su2double* val_coord_Elem_CG) override;
 
   /*!
    * \brief Copy the the normal vector of a face.
    * \param[in] val_normal - Vector where the subroutine is goint to copy the normal (dimensional).
    */
-  inline void GetNormal(su2double *val_normal) const override {
-    for (unsigned short iDim = 0; iDim < nDim; iDim++)
-      val_normal[iDim] = Normal[iDim];
+  inline void GetNormal(su2double* val_normal) const override {
+    for (unsigned short iDim = 0; iDim < nDim; iDim++) val_normal[iDim] = Normal[iDim];
   }
 
   /*!
    * \brief Get the normal to a face of the control volume asociated with a vertex.
    * \return Dimensional normal vector, the modulus is the area of the face.
    */
-  inline su2double *GetNormal(void) override { return Normal; }
+  inline su2double* GetNormal(void) override { return Normal; }
 
   /*!
    * \brief Get the ith component of the normal.
@@ -110,8 +109,7 @@ class CVertex : public CDualGrid {
    * \brief Initialize normal vector.
    */
   inline void SetZeroValues(void) override {
-    for (unsigned short iDim = 0; iDim < nDim; iDim ++)
-      Normal[iDim] = 0.0;
+    for (unsigned short iDim = 0; iDim < nDim; iDim++) Normal[iDim] = 0.0;
   }
 
   /*!
@@ -137,58 +135,53 @@ class CVertex : public CDualGrid {
    * \param[in] val_face_normal - Vector to initialize the normal vector.
    * \return Value of the normal vector.
    */
-  inline void SetNormal(const su2double *val_face_normal) override {
-    for (unsigned short iDim = 0; iDim < nDim; iDim++)
-      Normal[iDim]=val_face_normal[iDim];
+  inline void SetNormal(const su2double* val_face_normal) override {
+    for (unsigned short iDim = 0; iDim < nDim; iDim++) Normal[iDim] = val_face_normal[iDim];
   }
 
   /*!
    * \brief Add a vector to the normal vector.
    * \param[in] val_face_normal - Vector to add to the normal vector.
    */
-  inline void AddNormal(const su2double *val_face_normal) override {
-    for(unsigned short iDim = 0; iDim < nDim; iDim++)
-      Normal[iDim] += val_face_normal[iDim];
+  inline void AddNormal(const su2double* val_face_normal) override {
+    for (unsigned short iDim = 0; iDim < nDim; iDim++) Normal[iDim] += val_face_normal[iDim];
   }
 
   /*!
    * \brief Set the value of the coordinate variation due to a surface modification.
    * \param[in] val_varcoord - Variation of the coordinate.
    */
-  inline void SetVarCoord(const su2double *val_varcoord) {
-    for (unsigned short iDim = 0; iDim < nDim; iDim++)
-      VarCoord[iDim] = val_varcoord[iDim];
+  inline void SetVarCoord(const su2double* val_varcoord) {
+    for (unsigned short iDim = 0; iDim < nDim; iDim++) VarCoord[iDim] = val_varcoord[iDim];
   }
 
   /*!
    * \brief Add the value of the coordinate variation due to a surface modification.
    * \param[in] val_varcoord - Variation of the coordinate.
    */
-  inline void AddVarCoord(const su2double *val_varcoord) {
-    for (unsigned short iDim = 0; iDim < nDim; iDim++)
-      VarCoord[iDim] += val_varcoord[iDim];
+  inline void AddVarCoord(const su2double* val_varcoord) {
+    for (unsigned short iDim = 0; iDim < nDim; iDim++) VarCoord[iDim] += val_varcoord[iDim];
   }
 
   /*!
    * \brief Get the value of the coordinate variation due to a surface modification.
    * \return Variation of the coordinate.
    */
-  inline su2double *GetVarCoord(void) { return VarCoord; }
+  inline su2double* GetVarCoord(void) { return VarCoord; }
 
   /*!
    * \brief Set the value of the cartesian coordinate for the vertex.
    * \param[in] val_coord - Value of the cartesian coordinate.
    */
-  inline void SetCoord(const su2double *val_coord) override {
-    for (unsigned short iDim = 0; iDim < nDim; iDim++)
-      CartCoord[iDim] = val_coord[iDim];
+  inline void SetCoord(const su2double* val_coord) override {
+    for (unsigned short iDim = 0; iDim < nDim; iDim++) CartCoord[iDim] = val_coord[iDim];
   }
 
   /*!
    * \brief Get the value of the cartesian coordinate for the vertex.
    * \return Value of the cartesian coordinate of the vertex.
    */
-  inline su2double *GetCoord(void) override { return CartCoord; }
+  inline su2double* GetCoord(void) override { return CartCoord; }
 
   /*!
    * \brief Get the value of the cartesian coordinate for the vertex.
@@ -293,7 +286,7 @@ class CVertex : public CDualGrid {
    * \brief Get the value of the periodic point of a vertex, and its somain
    * \return Value of the periodic point of a vertex, and the domain.
    */
-  inline long *GetPeriodicPointDomain(void) { return PeriodicPoint; }
+  inline long* GetPeriodicPointDomain(void) { return PeriodicPoint; }
 
   /*!
    * \brief Get the value of the periodic point of a vertex, and its somain
@@ -326,5 +319,4 @@ class CVertex : public CDualGrid {
    * \return Index of the closest neighbor.
    */
   inline unsigned long GetNormal_Neighbor(void) const { return Normal_Neighbor; }
-
 };
diff --git a/Common/include/geometry/elements/CElement.hpp b/Common/include/geometry/elements/CElement.hpp
index e69e1e586e6..4c057ba59b2 100644
--- a/Common/include/geometry/elements/CElement.hpp
+++ b/Common/include/geometry/elements/CElement.hpp
@@ -56,39 +56,40 @@
  * \author R. Sanchez
  */
 class CElement {
-protected:
-  enum : size_t {MAXNDIM = 3};
+ protected:
+  enum : size_t { MAXNDIM = 3 };
 
-  std::vector<CGaussVariable> GaussPoint;  /*!< \brief Vector of Gaussian Points. */
+  std::vector<CGaussVariable> GaussPoint; /*!< \brief Vector of Gaussian Points. */
 
-  su2activematrix CurrentCoord;       /*!< \brief Coordinates in the current frame. */
-  su2activematrix RefCoord;           /*!< \brief Coordinates in the reference frame. */
-  su2activevector GaussWeight;        /*!< \brief Weight of the Gaussian Points for the integration. */
-  su2activematrix NodalExtrap;        /*!< \brief Coordinates of the nodal points for Gaussian extrapolation. */
-  su2activematrix NodalStress;        /*!< \brief Stress at the nodes. */
+  su2activematrix CurrentCoord; /*!< \brief Coordinates in the current frame. */
+  su2activematrix RefCoord;     /*!< \brief Coordinates in the reference frame. */
+  su2activevector GaussWeight;  /*!< \brief Weight of the Gaussian Points for the integration. */
+  su2activematrix NodalExtrap;  /*!< \brief Coordinates of the nodal points for Gaussian extrapolation. */
+  su2activematrix NodalStress;  /*!< \brief Stress at the nodes. */
 
   /*--- Stiffness and load matrices. ---*/
-  std::vector<su2activematrix> Kab;   /*!< \brief Structure for the constitutive component of the tangent matrix. */
-  su2activematrix Mab;                /*!< \brief Structure for the nodal components of the mass matrix. */
-  su2activematrix Ks_ab;              /*!< \brief Structure for the stress component of the tangent matrix. */
-  su2activematrix Kt_a;               /*!< \brief Matrix of nodal stress terms for residual computation. */
-  su2activematrix FDL_a;              /*!< \brief Matrix of dead loads for residual computation. */
+  std::vector<su2activematrix> Kab; /*!< \brief Structure for the constitutive component of the tangent matrix. */
+  su2activematrix Mab;              /*!< \brief Structure for the nodal components of the mass matrix. */
+  su2activematrix Ks_ab;            /*!< \brief Structure for the stress component of the tangent matrix. */
+  su2activematrix Kt_a;             /*!< \brief Matrix of nodal stress terms for residual computation. */
+  su2activematrix FDL_a;            /*!< \brief Matrix of dead loads for residual computation. */
 
-  su2double el_Pressure = 0.0;        /*!< \brief Pressure in the element. */
+  su2double el_Pressure = 0.0; /*!< \brief Pressure in the element. */
 
-  unsigned long iProp = 0;            /*!< \brief ID of the Element Property. */
-  unsigned long iDV = 0;              /*!< \brief ID of the Design Variable (if it is element based). */
-  unsigned long iDe = 0;              /*!< \brief ID of the dielectric elastomer. */
+  unsigned long iProp = 0; /*!< \brief ID of the Element Property. */
+  unsigned long iDV = 0;   /*!< \brief ID of the Design Variable (if it is element based). */
+  unsigned long iDe = 0;   /*!< \brief ID of the dielectric elastomer. */
 
-  unsigned short nGaussPoints;        /*!< \brief Number of gaussian points. */
-  unsigned short nNodes;              /*!< \brief Number of geometric points. */
-  unsigned short nDim;                /*!< \brief Number of dimension of the problem. */
+  unsigned short nGaussPoints; /*!< \brief Number of gaussian points. */
+  unsigned short nNodes;       /*!< \brief Number of geometric points. */
+  unsigned short nDim;         /*!< \brief Number of dimension of the problem. */
 
-  su2activematrix HiHj = 0.0;                        /*!< \brief Scalar product of 2 ansatz functions. */
-  std::vector<std::vector<su2activematrix>> DHiDHj;  /*!< \brief Scalar product of the gradients of 2 ansatz functions. */
+  su2activematrix HiHj = 0.0; /*!< \brief Scalar product of 2 ansatz functions. */
+  std::vector<std::vector<su2activematrix>>
+      DHiDHj; /*!< \brief Scalar product of the gradients of 2 ansatz functions. */
 
-public:
-  enum FrameType {REFERENCE=1, CURRENT=2}; /*!< \brief Type of nodal coordinates. */
+ public:
+  enum FrameType { REFERENCE = 1, CURRENT = 2 }; /*!< \brief Type of nodal coordinates. */
 
   /*!
    * \brief Default constructor of the class, deleted to make sure derived
@@ -136,13 +137,13 @@ class CElement {
    * \brief Retrieve the number of nodes of the element.
    * \return Number of nodes of the element.
    */
-  inline unsigned short GetnNodes(void) const {return nNodes;}
+  inline unsigned short GetnNodes(void) const { return nNodes; }
 
   /*!
    * \brief Retrieve the number of nodes of the element.
    * \return Number of Gaussian Points of the element.
    */
-  inline unsigned short GetnGaussPoints(void) const {return nGaussPoints;}
+  inline unsigned short GetnGaussPoints(void) const { return nGaussPoints; }
 
   /*!
    * \brief Set the value of the coordinate of the nodes in the reference configuration.
@@ -151,7 +152,7 @@ class CElement {
    * \param[in] val_CoordRef - Value of the coordinate.
    */
   inline void SetRef_Coord(unsigned short iNode, unsigned short iDim, su2double val_CoordRef) {
-    RefCoord(iNode,iDim) = val_CoordRef;
+    RefCoord(iNode, iDim) = val_CoordRef;
   }
 
   /*!
@@ -161,7 +162,7 @@ class CElement {
    * \param[in] val_CoordRef - Value of the coordinate.
    */
   inline void SetCurr_Coord(unsigned short iNode, unsigned short iDim, su2double val_CoordCurr) {
-    CurrentCoord(iNode,iDim) = val_CoordCurr;
+    CurrentCoord(iNode, iDim) = val_CoordCurr;
   }
 
   /*!
@@ -170,9 +171,7 @@ class CElement {
    * \param[in] iDim - Dimension.
    * \return Reference coordinate.
    */
-  inline su2double GetRef_Coord(unsigned short iNode, unsigned short iDim) const {
-    return RefCoord(iNode,iDim);
-  }
+  inline su2double GetRef_Coord(unsigned short iNode, unsigned short iDim) const { return RefCoord(iNode, iDim); }
 
   /*!
    * \brief Get the value of the coordinate of the nodes in the current configuration.
@@ -180,36 +179,28 @@ class CElement {
    * \param[in] iDim - Dimension.
    * \return Current coordinate.
    */
-  inline su2double GetCurr_Coord(unsigned short iNode, unsigned short iDim) const {
-    return CurrentCoord(iNode,iDim);
-  }
+  inline su2double GetCurr_Coord(unsigned short iNode, unsigned short iDim) const { return CurrentCoord(iNode, iDim); }
 
   /*!
    * \brief Get the weight of the corresponding Gaussian Point.
    * \param[in] iGauss - index of the Gaussian point.
    * \return Weight.
    */
-  inline su2double GetWeight(unsigned short iGauss) const {
-    return GaussWeight(iGauss);
-  }
+  inline su2double GetWeight(unsigned short iGauss) const { return GaussWeight(iGauss); }
 
   /*!
    * \brief Get the Jacobian respect to the reference configuration for the Gaussian Point iGauss.
    * \param[in] iGauss - index of the Gaussian point.
    * \return Jacobian.
    */
-  inline su2double GetJ_X(unsigned short iGauss) const {
-    return GaussPoint[iGauss].GetJ_X();
-  }
+  inline su2double GetJ_X(unsigned short iGauss) const { return GaussPoint[iGauss].GetJ_X(); }
 
   /*!
    * \brief Get the jacobian respect to the current configuration for the Gaussian Point iGauss.
    * \param[in] iGauss - index of the Gaussian point.
    * \return Jacobian.
    */
-  inline su2double GetJ_x(unsigned short iGauss) const {
-    return GaussPoint[iGauss].GetJ_x();
-  }
+  inline su2double GetJ_x(unsigned short iGauss) const { return GaussPoint[iGauss].GetJ_x(); }
 
   /*!
    * \brief Retrieve the value of the pressure in the element for incompressible materials.
@@ -223,9 +214,7 @@ class CElement {
    * \param[in] nodeB - index of Node b.
    * \param[in] val_Ks_ab - value of the term that will constitute the diagonal of the stress contribution.
    */
-  inline void Add_Mab(unsigned short nodeA, unsigned short nodeB, su2double val_Mab) {
-    Mab(nodeA,nodeB) += val_Mab;
-  }
+  inline void Add_Mab(unsigned short nodeA, unsigned short nodeB, su2double val_Mab) { Mab(nodeA, nodeB) += val_Mab; }
 
   /*!
    * \brief Add the value of a submatrix K relating nodes a and b, for the constitutive term.
@@ -233,22 +222,19 @@ class CElement {
    * \param[in] nodeB - index of Node b.
    * \param[in] val_Kab - value of the matrix K.
    */
-  inline void Add_Kab(unsigned short nodeA, unsigned short nodeB, su2double **val_Kab) {
+  inline void Add_Kab(unsigned short nodeA, unsigned short nodeB, su2double** val_Kab) {
     for (unsigned short iDim = 0; iDim < nDim; iDim++)
-      for (unsigned short jDim = 0; jDim < nDim; jDim++)
-        Kab[nodeA](nodeB, iDim*nDim+jDim) += val_Kab[iDim][jDim];
+      for (unsigned short jDim = 0; jDim < nDim; jDim++) Kab[nodeA](nodeB, iDim * nDim + jDim) += val_Kab[iDim][jDim];
   }
 
   /*!
-   * \brief Add the value of a submatrix K relating nodes a and b, for the constitutive term (symmetric terms need transpose)
-   * \param[in] nodeA - index of Node a.
-   * \param[in] nodeB - index of Node b.
-   * \param[in] val_Kab - value of the matrix K.
+   * \brief Add the value of a submatrix K relating nodes a and b, for the constitutive term (symmetric terms need
+   * transpose) \param[in] nodeA - index of Node a. \param[in] nodeB - index of Node b. \param[in] val_Kab - value of
+   * the matrix K.
    */
-  inline void Add_Kab_T(unsigned short nodeA, unsigned short nodeB, su2double **val_Kab) {
+  inline void Add_Kab_T(unsigned short nodeA, unsigned short nodeB, su2double** val_Kab) {
     for (unsigned short iDim = 0; iDim < nDim; iDim++)
-      for (unsigned short jDim = 0; jDim < nDim; jDim++)
-        Kab[nodeA](nodeB, iDim*nDim+jDim) += val_Kab[jDim][iDim];
+      for (unsigned short jDim = 0; jDim < nDim; jDim++) Kab[nodeA](nodeB, iDim * nDim + jDim) += val_Kab[jDim][iDim];
   }
 
   /*!
@@ -258,7 +244,7 @@ class CElement {
    * \param[in] val_Ks_ab - value of the term that will constitute the diagonal of the stress contribution.
    */
   inline void Add_Ks_ab(unsigned short nodeA, unsigned short nodeB, su2double val_Ks_ab) {
-    Ks_ab(nodeA,nodeB) += val_Ks_ab;
+    Ks_ab(nodeA, nodeB) += val_Ks_ab;
   }
 
   /*!
@@ -266,9 +252,8 @@ class CElement {
    * \param[in] nodeA - index of Node a.
    * \param[in] val_Kt_a - value of the term that will constitute the diagonal of the stress contribution.
    */
-  inline void Add_Kt_a(unsigned short nodeA, const su2double *val_Kt_a) {
-    for(unsigned short iDim = 0; iDim < nDim; iDim++)
-      Kt_a(nodeA,iDim) += val_Kt_a[iDim];
+  inline void Add_Kt_a(unsigned short nodeA, const su2double* val_Kt_a) {
+    for (unsigned short iDim = 0; iDim < nDim; iDim++) Kt_a(nodeA, iDim) += val_Kt_a[iDim];
   }
 
   /*!
@@ -276,15 +261,14 @@ class CElement {
    * \param[in] nodeA - index of Node a.
    * \param[in] val_FDL_a - value of the term that will constitute the diagonal of the stress contribution.
    */
-  inline void Add_FDL_a(unsigned short nodeA, const su2double *val_FDL_a) {
-    for(unsigned short iDim = 0; iDim < nDim; iDim++)
-      FDL_a(nodeA,iDim) += val_FDL_a[iDim];
+  inline void Add_FDL_a(unsigned short nodeA, const su2double* val_FDL_a) {
+    for (unsigned short iDim = 0; iDim < nDim; iDim++) FDL_a(nodeA, iDim) += val_FDL_a[iDim];
   }
 
   /*!
    * \brief Restarts the values of stress in the element.
    */
-  inline void ClearStress(void) {NodalStress.setConstant(0.0);}
+  inline void ClearStress(void) { NodalStress.setConstant(0.0); }
 
   /*!
    * \brief Return the value of the diagonal term for the mass matrix, relating nodes a and b.
@@ -292,9 +276,7 @@ class CElement {
    * \param[in] nodeB - index of Node b.
    * \return Value of the diagonal term of Mab.
    */
-  inline su2double Get_Mab(unsigned short nodeA, unsigned short nodeB) const {
-    return Mab(nodeA,nodeB);
-  }
+  inline su2double Get_Mab(unsigned short nodeA, unsigned short nodeB) const { return Mab(nodeA, nodeB); }
 
   /*!
    * \brief Return the value of the submatrix K relating nodes a and b.
@@ -302,9 +284,7 @@ class CElement {
    * \param[in] nodeB - index of Node b.
    * \return Values of the matrix K.
    */
-  inline const su2double *Get_Kab(unsigned short nodeA, unsigned short nodeB) const {
-    return Kab[nodeA][nodeB];
-  }
+  inline const su2double* Get_Kab(unsigned short nodeA, unsigned short nodeB) const { return Kab[nodeA][nodeB]; }
 
   /*!
    * \brief Return the value of the diagonal term for the stress contribution, relating nodes a and b.
@@ -312,27 +292,21 @@ class CElement {
    * \param[in] nodeB - index of Node b.
    * \return Value of the matrix Ks.
    */
-  inline su2double Get_Ks_ab(unsigned short nodeA, unsigned short nodeB) const {
-    return Ks_ab(nodeA,nodeB);
-  }
+  inline su2double Get_Ks_ab(unsigned short nodeA, unsigned short nodeB) const { return Ks_ab(nodeA, nodeB); }
 
   /*!
    * \brief Return the values of the nodal stress components of the residual for node a.
    * \param[in] nodeA - index of Node a.
    * \return Values of the stress term.
    */
-  inline const su2double *Get_Kt_a(unsigned short nodeA) const {
-    return Kt_a[nodeA];
-  }
+  inline const su2double* Get_Kt_a(unsigned short nodeA) const { return Kt_a[nodeA]; }
 
   /*!
    * \brief Return the values of the dead load components of the residual for node a.
    * \param[in] nodeA - index of Node a.
    * \return Value of the dead loads.
    */
-  inline const su2double *Get_FDL_a(unsigned short nodeA) const {
-    return FDL_a[nodeA];
-  }
+  inline const su2double* Get_FDL_a(unsigned short nodeA) const { return FDL_a[nodeA]; }
 
   /*!
    * \brief Retrieve the value of the shape functions.
@@ -340,9 +314,7 @@ class CElement {
    * \param[in] iGauss - Index of the Gaussian Point.
    * \return Gradient of the shape function related to node iNode and evaluated at Gaussian Point iGauss
    */
-  inline su2double GetNi(unsigned short iNode, unsigned short iGauss) const {
-    return GaussPoint[iGauss].GetNi(iNode);
-  }
+  inline su2double GetNi(unsigned short iNode, unsigned short iGauss) const { return GaussPoint[iGauss].GetNi(iNode); }
 
   /*!
    * \brief Retrieve the value of the gradient of the shape functions respect to the reference configuration.
@@ -352,7 +324,7 @@ class CElement {
    * \return Gradient of the shape function related to node iNode and evaluated at Gaussian Point iGauss
    */
   inline su2double GetGradNi_X(unsigned short iNode, unsigned short iGauss, unsigned short iDim) const {
-    return GaussPoint[iGauss].GetGradNi_Xj(iNode,iDim);
+    return GaussPoint[iGauss].GetGradNi_Xj(iNode, iDim);
   }
 
   /*!
@@ -363,7 +335,7 @@ class CElement {
    * \return Gradient of the shape function related to node iNode and evaluated at Gaussian Point iGauss
    */
   inline su2double GetGradNi_x(unsigned short iNode, unsigned short iGauss, unsigned short iDim) const {
-    return GaussPoint[iGauss].GetGradNi_xj(iNode,iDim);
+    return GaussPoint[iGauss].GetGradNi_xj(iNode, iDim);
   }
 
   /*!
@@ -373,7 +345,7 @@ class CElement {
    * \return Value of the shape function at the nodes for extrapolation purposes
    */
   inline su2double GetNi_Extrap(unsigned short iNode, unsigned short iGauss) const {
-    return NodalExtrap(iNode,iGauss);
+    return NodalExtrap(iNode, iGauss);
   }
 
   /*!
@@ -383,7 +355,7 @@ class CElement {
    * \param[in] val_Stress - Value of the stress added.
    */
   inline void Add_NodalStress(unsigned short iNode, unsigned short iVar, su2double val_Stress) {
-    NodalStress(iNode,iVar) += val_Stress;
+    NodalStress(iNode, iVar) += val_Stress;
   }
 
   /*!
@@ -392,76 +364,74 @@ class CElement {
    * \param[in] iVar - Variable index.
    * \return Value of the stress.
    */
-  inline su2double Get_NodalStress(unsigned short iNode, unsigned short iVar) const {
-    return NodalStress(iNode,iVar);
-  }
+  inline su2double Get_NodalStress(unsigned short iNode, unsigned short iVar) const { return NodalStress(iNode, iVar); }
 
   /*!
    * \brief Store the values of the identifiers for element properties.
    * \param[in] element_property - element properties container.
    */
-  inline void Set_ElProperties(const CProperty *element_property) {
-    iDV   = element_property->GetDV();
+  inline void Set_ElProperties(const CProperty* element_property) {
+    iDV = element_property->GetDV();
     iProp = element_property->GetMat_Prop();
-    iDe   = element_property->GetElectric_Prop();
+    iDe = element_property->GetElectric_Prop();
   }
 
   /*!
    * \brief Store the value of the identifier for the Dielectric Elastomers.
    * \param[in] val_iDe - identifier of the DE property.
    */
-  inline void Set_iDe(unsigned long val_iDe) {iDe = val_iDe;}
+  inline void Set_iDe(unsigned long val_iDe) { iDe = val_iDe; }
 
   /*!
    * \brief Return the value of the identifier for the Dielectric Elastomers.
    * \return Identifier of the DE property.
    */
-  inline unsigned long Get_iDe(void) const {return iDe;}
+  inline unsigned long Get_iDe(void) const { return iDe; }
 
   /*!
    * \brief Return the value of the identifier for the Design Variable.
    * \return Identifier of the DV.
    */
-  inline unsigned long Get_iDV(void) const {return iDV;}
+  inline unsigned long Get_iDV(void) const { return iDV; }
 
   /*!
    * \brief Return the value of the identifier for the Element Property.
    * \return Identifier of the property.
    */
-  inline unsigned long Get_iProp(void) const {return iProp;}
+  inline unsigned long Get_iProp(void) const { return iProp; }
 
   /*!
    * \brief Compute the value of the length of the element.
    * \param[in] mode - Type of coordinates to consider in the computation.
    * \return Length of the (1D) element.
    */
-  inline virtual su2double ComputeLength(const FrameType mode = REFERENCE) const {return 0.0;}
+  inline virtual su2double ComputeLength(const FrameType mode = REFERENCE) const { return 0.0; }
 
   /*!
    * \brief Compute the value of the area of the element.
    * \param[in] mode - Type of coordinates to consider in the computation.
    * \return Area of the (2D) element.
    */
-  inline virtual su2double ComputeArea(const FrameType mode = REFERENCE) const {return 0.0;}
+  inline virtual su2double ComputeArea(const FrameType mode = REFERENCE) const { return 0.0; }
 
   /*!
    * \brief Compute the value of the volume of the element.
    * \param[in] mode - Type of coordinates to consider in the computation.
    * \return Volume of the (3D) element.
    */
-  inline virtual su2double ComputeVolume(const FrameType mode = REFERENCE) const {return 0.0;}
+  inline virtual su2double ComputeVolume(const FrameType mode = REFERENCE) const { return 0.0; }
 
   /*!
    * \brief Compute the value of the area of the element in current coordinates (wrapper to ComputeArea(CURRENT)).
    * \return Current area of the (2D) element.
    */
-  inline su2double ComputeCurrentArea(void) const {return ComputeArea(CURRENT);}
+  inline su2double ComputeCurrentArea(void) const { return ComputeArea(CURRENT); }
 
   /*!
    * \brief Compute the value of the volume of the element in current coordinates (wrapper to ComputeVolume(CURRENT)).
    * \return Current volume of the (3D) element.
    */
-  inline su2double ComputeCurrentVolume(void) const {return ComputeVolume(CURRENT);}
+  inline su2double ComputeCurrentVolume(void) const { return ComputeVolume(CURRENT); }
 
   /*!
    * \brief Register the current and reference coordinates of the element as pre-accumulation inputs
@@ -469,39 +439,32 @@ class CElement {
    * because inactive variables are ignored.
    */
   inline void SetPreaccIn_Coords(bool nonlinear = true) {
-    AD::SetPreaccIn(RefCoord.data(), nNodes*MAXNDIM);
-    if (nonlinear)
-      AD::SetPreaccIn(CurrentCoord.data(), nNodes*MAXNDIM);
+    AD::SetPreaccIn(RefCoord.data(), nNodes * MAXNDIM);
+    if (nonlinear) AD::SetPreaccIn(CurrentCoord.data(), nNodes * MAXNDIM);
   }
 
   /*!
    * \brief Register the stress residual as a pre-accumulation output. When computing the element
    * stiffness matrix this is the only term that sees its way into the RHS of the system.
    */
-  inline void SetPreaccOut_Kt_a(void) {
-    AD::SetPreaccOut(Kt_a.data(), nNodes*nDim);
-  }
+  inline void SetPreaccOut_Kt_a(void) { AD::SetPreaccOut(Kt_a.data(), nNodes * nDim); }
 
   /*!
    * \brief Register the mass matrix as a pre-accumulation output.
    */
-  inline void SetPreaccOut_Mab(void) {
-    AD::SetPreaccOut(Mab.data(), nNodes*nNodes);
-  }
+  inline void SetPreaccOut_Mab(void) { AD::SetPreaccOut(Mab.data(), nNodes * nNodes); }
 
   /*!
    * \brief Register the dead load as a pre-accumulation output.
    */
-  inline void SetPreaccOut_FDL_a(void) {
-    AD::SetPreaccOut(FDL_a.data(), nNodes*nDim);
-  }
+  inline void SetPreaccOut_FDL_a(void) { AD::SetPreaccOut(FDL_a.data(), nNodes * nDim); }
 
- /*!
-  * \brief Add the scalar product of the shape functions to the tangent matrix.
-  * \param[in] nodeA - index of Node a.
-  * \param[in] nodeB - index of Node b.
-  * \param[in] val - value of the scalar product of ansatz function.
-  */
+  /*!
+   * \brief Add the scalar product of the shape functions to the tangent matrix.
+   * \param[in] nodeA - index of Node a.
+   * \param[in] nodeB - index of Node b.
+   * \param[in] val - value of the scalar product of ansatz function.
+   */
   inline void Add_HiHj(su2double val, unsigned short nodeA, unsigned short nodeB) { HiHj[nodeA][nodeB] += val; }
 
   /*!
@@ -520,12 +483,12 @@ class CElement {
     }
   }
 
- /*!
-  * \brief Add the transposed scalar product of the gradients of shape functions to the tangent matrix.
-  * \param[in] nodeA - index of Node a.
-  * \param[in] nodeB - index of Node b.
-  * \param[in] val - value of the term that will contribute.
-  */
+  /*!
+   * \brief Add the transposed scalar product of the gradients of shape functions to the tangent matrix.
+   * \param[in] nodeA - index of Node a.
+   * \param[in] nodeB - index of Node b.
+   * \param[in] val - value of the term that will contribute.
+   */
   template <class MatrixType>
   inline void Add_DHiDHj_T(const MatrixType& val, unsigned short nodeA, unsigned short nodeB) {
     unsigned short iDim, jDim;
@@ -536,22 +499,21 @@ class CElement {
     }
   }
 
- /*!
-  * \brief Get the scalar product of the shape functions to the tangent matrix.
-  * \param[in] nodeA - index of Node a.
-  * \param[in] nodeB - index of Node b.
-  * \param[out] val - value of the scalar product of ansatz function.
-  */
- inline su2double Get_HiHj(unsigned short nodeA, unsigned short nodeB)  { return HiHj[nodeA][nodeB]; }
-
- /*!
-  * \brief Get the scalar product of the gradients of shape functions to the tangent matrix.
-  * \param[in] nodeA - index of Node a.
-  * \param[in] nodeB - index of Node b.
-  * \return val - value of the scalar product of gradients of ansatz function.
-  */
- inline su2activematrix& Get_DHiDHj(unsigned short nodeA, unsigned short nodeB) { return DHiDHj[nodeA][nodeB];}
+  /*!
+   * \brief Get the scalar product of the shape functions to the tangent matrix.
+   * \param[in] nodeA - index of Node a.
+   * \param[in] nodeB - index of Node b.
+   * \param[out] val - value of the scalar product of ansatz function.
+   */
+  inline su2double Get_HiHj(unsigned short nodeA, unsigned short nodeB) { return HiHj[nodeA][nodeB]; }
 
+  /*!
+   * \brief Get the scalar product of the gradients of shape functions to the tangent matrix.
+   * \param[in] nodeA - index of Node a.
+   * \param[in] nodeB - index of Node b.
+   * \return val - value of the scalar product of gradients of ansatz function.
+   */
+  inline su2activematrix& Get_DHiDHj(unsigned short nodeA, unsigned short nodeB) { return DHiDHj[nodeA][nodeB]; }
 };
 
 /*!
@@ -560,10 +522,9 @@ class CElement {
  * \brief Templated class to implement the computation of gradients for specific element sizes.
  * \author P. Gomes, R. Sanchez
  */
-template<unsigned short NGAUSS, unsigned short NNODE, unsigned short NDIM>
+template <unsigned short NGAUSS, unsigned short NNODE, unsigned short NDIM>
 class CElementWithKnownSizes : public CElement {
-private:
-
+ private:
   FORCEINLINE static su2double JacobianAdjoint(const su2double Jacobian[][1], su2double ad[][1]) {
     /*--- Adjoint to Jacobian, we put 1.0 here so that ad/detJac is the inverse later ---*/
     ad[0][0] = 1.0;
@@ -572,28 +533,30 @@ class CElementWithKnownSizes : public CElement {
   }
 
   FORCEINLINE static su2double JacobianAdjoint(const su2double Jacobian[][2], su2double ad[][2]) {
-    ad[0][0] =  Jacobian[1][1];  ad[0][1] = -Jacobian[0][1];
-    ad[1][0] = -Jacobian[1][0];  ad[1][1] =  Jacobian[0][0];
+    ad[0][0] = Jacobian[1][1];
+    ad[0][1] = -Jacobian[0][1];
+    ad[1][0] = -Jacobian[1][0];
+    ad[1][1] = Jacobian[0][0];
     /*--- Determinant of Jacobian ---*/
-    return ad[0][0]*ad[1][1]-ad[0][1]*ad[1][0];
+    return ad[0][0] * ad[1][1] - ad[0][1] * ad[1][0];
   }
 
   FORCEINLINE static su2double JacobianAdjoint(const su2double Jacobian[][3], su2double ad[][3]) {
-    ad[0][0] = Jacobian[1][1]*Jacobian[2][2]-Jacobian[1][2]*Jacobian[2][1];
-    ad[0][1] = Jacobian[0][2]*Jacobian[2][1]-Jacobian[0][1]*Jacobian[2][2];
-    ad[0][2] = Jacobian[0][1]*Jacobian[1][2]-Jacobian[0][2]*Jacobian[1][1];
-    ad[1][0] = Jacobian[1][2]*Jacobian[2][0]-Jacobian[1][0]*Jacobian[2][2];
-    ad[1][1] = Jacobian[0][0]*Jacobian[2][2]-Jacobian[0][2]*Jacobian[2][0];
-    ad[1][2] = Jacobian[0][2]*Jacobian[1][0]-Jacobian[0][0]*Jacobian[1][2];
-    ad[2][0] = Jacobian[1][0]*Jacobian[2][1]-Jacobian[1][1]*Jacobian[2][0];
-    ad[2][1] = Jacobian[0][1]*Jacobian[2][0]-Jacobian[0][0]*Jacobian[2][1];
-    ad[2][2] = Jacobian[0][0]*Jacobian[1][1]-Jacobian[0][1]*Jacobian[1][0];
+    ad[0][0] = Jacobian[1][1] * Jacobian[2][2] - Jacobian[1][2] * Jacobian[2][1];
+    ad[0][1] = Jacobian[0][2] * Jacobian[2][1] - Jacobian[0][1] * Jacobian[2][2];
+    ad[0][2] = Jacobian[0][1] * Jacobian[1][2] - Jacobian[0][2] * Jacobian[1][1];
+    ad[1][0] = Jacobian[1][2] * Jacobian[2][0] - Jacobian[1][0] * Jacobian[2][2];
+    ad[1][1] = Jacobian[0][0] * Jacobian[2][2] - Jacobian[0][2] * Jacobian[2][0];
+    ad[1][2] = Jacobian[0][2] * Jacobian[1][0] - Jacobian[0][0] * Jacobian[1][2];
+    ad[2][0] = Jacobian[1][0] * Jacobian[2][1] - Jacobian[1][1] * Jacobian[2][0];
+    ad[2][1] = Jacobian[0][1] * Jacobian[2][0] - Jacobian[0][0] * Jacobian[2][1];
+    ad[2][2] = Jacobian[0][0] * Jacobian[1][1] - Jacobian[0][1] * Jacobian[1][0];
     /*--- Determinant of Jacobian ---*/
-    return Jacobian[0][0]*ad[0][0]+Jacobian[0][1]*ad[1][0]+Jacobian[0][2]*ad[2][0];
+    return Jacobian[0][0] * ad[0][0] + Jacobian[0][1] * ad[1][0] + Jacobian[0][2] * ad[2][0];
   }
 
-protected:
-  static_assert(NDIM==1 || NDIM==2 || NDIM==3, "ComputeGrad_impl expects 1D, 2D or 3D");
+ protected:
+  static_assert(NDIM == 1 || NDIM == 2 || NDIM == 3, "ComputeGrad_impl expects 1D, 2D or 3D");
 
   su2double GaussCoord[NGAUSS][NDIM];   /*!< \brief Coordinates of the integration points. */
   su2double dNiXj[NGAUSS][NNODE][NDIM]; /*!< \brief Shape function derivatives evaluated at the Gauss points. */
@@ -609,31 +572,27 @@ class CElementWithKnownSizes : public CElement {
    * \brief Implementation of gradient computation leveraging the static sizes.
    * \param[in] FRAME - template, REFERENCE or CURRENT coordinates.
    */
-  template<FrameType FRAME>
+  template <FrameType FRAME>
   void ComputeGrad_impl(void) {
-
     su2double Jacobian[NDIM][NDIM], ad[NDIM][NDIM];
     unsigned short iNode, iDim, jDim, iGauss;
 
     /*--- Select the appropriate source for the nodal coordinates depending on the frame requested
           for the gradient computation, REFERENCE (undeformed) or CURRENT (deformed) ---*/
-    const su2activematrix& Coord = (FRAME==REFERENCE) ? RefCoord : CurrentCoord;
+    const su2activematrix& Coord = (FRAME == REFERENCE) ? RefCoord : CurrentCoord;
 
     for (iGauss = 0; iGauss < NGAUSS; iGauss++) {
-
       /*--- Jacobian transformation ---*/
       /*--- This does dX/dXi transpose ---*/
 
       for (iDim = 0; iDim < NDIM; iDim++)
-        for (jDim = 0; jDim < NDIM; jDim++)
-          Jacobian[iDim][jDim] = 0.0;
+        for (jDim = 0; jDim < NDIM; jDim++) Jacobian[iDim][jDim] = 0.0;
 
       for (iNode = 0; iNode < NNODE; iNode++)
         for (iDim = 0; iDim < NDIM; iDim++)
-          for (jDim = 0; jDim < NDIM; jDim++)
-            Jacobian[iDim][jDim] += Coord(iNode,jDim) * dNiXj[iGauss][iNode][iDim];
+          for (jDim = 0; jDim < NDIM; jDim++) Jacobian[iDim][jDim] += Coord(iNode, jDim) * dNiXj[iGauss][iNode][iDim];
 
-      if (NDIM==1) {
+      if (NDIM == 1) {
         /*--- Obviously the Jacobian is the slope of the line ---*/
         Jacobian[0][0] = (Coord[1][0] - Coord[0][0]);
       }
@@ -642,7 +601,7 @@ class CElementWithKnownSizes : public CElement {
 
       auto detJac = JacobianAdjoint(Jacobian, ad);
 
-      if (FRAME==REFERENCE)
+      if (FRAME == REFERENCE)
         GaussPoint[iGauss].SetJ_X(detJac);
       else
         GaussPoint[iGauss].SetJ_x(detJac);
@@ -650,92 +609,84 @@ class CElementWithKnownSizes : public CElement {
       /*--- Jacobian inverse (it was already computed as transpose) ---*/
 
       for (iDim = 0; iDim < NDIM; iDim++)
-        for (jDim = 0; jDim < NDIM; jDim++)
-          Jacobian[iDim][jDim] = ad[iDim][jDim]/detJac;
+        for (jDim = 0; jDim < NDIM; jDim++) Jacobian[iDim][jDim] = ad[iDim][jDim] / detJac;
 
       /*--- Derivatives with respect to global coordinates ---*/
 
       for (iNode = 0; iNode < NNODE; iNode++) {
         for (iDim = 0; iDim < NDIM; iDim++) {
           su2double GradNi_Xj = 0.0;
-          for (jDim = 0; jDim < NDIM; jDim++)
-            GradNi_Xj += Jacobian[iDim][jDim] * dNiXj[iGauss][iNode][jDim];
+          for (jDim = 0; jDim < NDIM; jDim++) GradNi_Xj += Jacobian[iDim][jDim] * dNiXj[iGauss][iNode][jDim];
 
-          if (FRAME==REFERENCE)
+          if (FRAME == REFERENCE)
             GaussPoint[iGauss].SetGradNi_Xj(GradNi_Xj, iDim, iNode);
           else
             GaussPoint[iGauss].SetGradNi_xj(GradNi_Xj, iDim, iNode);
         }
       }
-
     }
-
   }
 
-  template<FrameType FRAME>
+  template <FrameType FRAME>
   void ComputeGrad_impl_surf_embedded() {
-
     /*--- Select the appropriate source for the nodal coordinates depending on the frame requested
           for the gradient computation, REFERENCE (undeformed) or CURRENT (deformed) ---*/
-    const su2activematrix& Coord = (FRAME==REFERENCE) ? RefCoord : CurrentCoord;
+    const su2activematrix& Coord = (FRAME == REFERENCE) ? RefCoord : CurrentCoord;
 
-    if (NDIM==1) {
+    if (NDIM == 1) {
       unsigned short iNode, iDim, iGauss;
       su2double Jacobian[2];
       su2double val_grad;
 
       Jacobian[0] = (Coord[1][0] - Coord[0][0]);
       Jacobian[1] = (Coord[1][1] - Coord[0][1]);
-      const su2double JTJ = Jacobian[0]*Jacobian[0]+Jacobian[1]*Jacobian[1];
+      const su2double JTJ = Jacobian[0] * Jacobian[0] + Jacobian[1] * Jacobian[1];
       const su2double volJacobian = sqrt(JTJ);
 
       for (iGauss = 0; iGauss < NGAUSS; iGauss++) {
-
         GaussPoint[iGauss].SetJ_X(volJacobian);
 
         for (iNode = 0; iNode < NNODE; iNode++) {
-          for (iDim=0; iDim<NDIM+1; iDim++) {
-            val_grad = Jacobian[iDim]*dNiXj[iGauss][iNode][0]/JTJ;
-            GaussPoint[iGauss].SetGradNi_Xj( val_grad, iDim, iNode);
+          for (iDim = 0; iDim < NDIM + 1; iDim++) {
+            val_grad = Jacobian[iDim] * dNiXj[iGauss][iNode][0] / JTJ;
+            GaussPoint[iGauss].SetGradNi_Xj(val_grad, iDim, iNode);
           }
         }
       }
 
-    } else if (NDIM==2) {
-
-      su2double Jacobian[NDIM+1][NDIM], JTJ[NDIM][NDIM];
+    } else if (NDIM == 2) {
+      su2double Jacobian[NDIM + 1][NDIM], JTJ[NDIM][NDIM];
       su2double volJacobian;
       unsigned short iShape, iDim, jDim, jVertex, kDim, iGauss;
 
       for (iGauss = 0; iGauss < NGAUSS; iGauss++) {
-
         /*--- Jacobian transformation ---*/
         /*--- This does dX/dXi transpose ---*/
-        if(NNODE==3) {
-          for (iDim = 0; iDim < NDIM+1; iDim++) {
+        if (NNODE == 3) {
+          for (iDim = 0; iDim < NDIM + 1; iDim++) {
             for (jVertex = 0; jVertex < NDIM; jVertex++) {
-              Jacobian[iDim][jVertex] = Coord[jVertex+1][iDim] - Coord[0][iDim];
+              Jacobian[iDim][jVertex] = Coord[jVertex + 1][iDim] - Coord[0][iDim];
             }
           }
         }
-        if (NNODE==4) {
-          for (iDim = 0; iDim < NDIM+1; iDim++) {
-            Jacobian[iDim][0] = (Coord[1][iDim] - Coord[0][iDim])/2;
-            Jacobian[iDim][1] = (Coord[3][iDim] - Coord[0][iDim])/2;
+        if (NNODE == 4) {
+          for (iDim = 0; iDim < NDIM + 1; iDim++) {
+            Jacobian[iDim][0] = (Coord[1][iDim] - Coord[0][iDim]) / 2;
+            Jacobian[iDim][1] = (Coord[3][iDim] - Coord[0][iDim]) / 2;
           }
         }
 
         for (iDim = 0; iDim < NDIM; iDim++) {
           for (jDim = 0; jDim < NDIM; jDim++) {
             JTJ[iDim][jDim] = 0.0;
-            for (kDim = 0; kDim < NDIM+1; kDim++) {
-              JTJ[iDim][jDim] += Jacobian[kDim][iDim]*Jacobian[kDim][jDim];
+            for (kDim = 0; kDim < NDIM + 1; kDim++) {
+              JTJ[iDim][jDim] += Jacobian[kDim][iDim] * Jacobian[kDim][jDim];
             }
           }
         }
 
         /*--- matrix volume of Jacobian ---*/
-        const su2double detJacobian=JTJ[0][0]*JTJ[1][1]-JTJ[0][1]*JTJ[1][0];
+        const su2double detJacobian = JTJ[0][0] * JTJ[1][1] - JTJ[0][1] * JTJ[1][0];
 
         volJacobian = sqrt(detJacobian);
 
@@ -744,38 +695,37 @@ class CElementWithKnownSizes : public CElement {
         /*--- Derivatives with respect to global coordinates ---*/
 
         su2double JTJinv[2][2];
-        JTJinv[0][0]=JTJ[1][1]/detJacobian;
-        JTJinv[1][1]=JTJ[0][0]/detJacobian;
-        JTJinv[0][1]=-JTJ[0][1]/detJacobian;
-        JTJinv[1][0]=-JTJ[1][0]/detJacobian;
+        JTJinv[0][0] = JTJ[1][1] / detJacobian;
+        JTJinv[1][1] = JTJ[0][0] / detJacobian;
+        JTJinv[0][1] = -JTJ[0][1] / detJacobian;
+        JTJinv[1][0] = -JTJ[1][0] / detJacobian;
 
         su2double Jdagger[2][3];
 
         for (iDim = 0; iDim < NDIM; iDim++) {
-          for (jDim = 0; jDim < NDIM+1; jDim++) {
+          for (jDim = 0; jDim < NDIM + 1; jDim++) {
             Jdagger[iDim][jDim] = 0.0;
             for (kDim = 0; kDim < NDIM; kDim++) {
-              Jdagger[iDim][jDim] += JTJinv[iDim][kDim]*Jacobian[jDim][kDim];
+              Jdagger[iDim][jDim] += JTJinv[iDim][kDim] * Jacobian[jDim][kDim];
             }
           }
         }
 
-        su2double GradOut[NDIM+1];
+        su2double GradOut[NDIM + 1];
         for (iShape = 0; iShape < NNODE; iShape++) {
-          for (iDim = 0; iDim < NDIM+1; iDim++) {
+          for (iDim = 0; iDim < NDIM + 1; iDim++) {
             GradOut[iDim] = 0.0;
             for (jDim = 0; jDim < NDIM; jDim++) {
-              GradOut[iDim] += Jdagger[jDim][iDim]*dNiXj[iGauss][iShape][jDim];
+              GradOut[iDim] += Jdagger[jDim][iDim] * dNiXj[iGauss][iShape][jDim];
             }
             GaussPoint[iGauss].SetGradNi_Xj(GradOut[iDim], iDim, iShape);
           }
         }
-
       }
     }
   }
 
-public:
+ public:
   /*!
    * \brief Set the value of the gradient of the shape functions wrt the reference configuration.
    */
@@ -790,7 +740,6 @@ class CElementWithKnownSizes : public CElement {
    * \brief Overload needed for deformed 2D elements on a surface in 3D or 1D elements on a 2D curve.
    */
   void ComputeGrad_SurfaceEmbedded() final { ComputeGrad_impl_surf_embedded<REFERENCE>(); }
-
 };
 
 /*!
@@ -799,13 +748,13 @@ class CElementWithKnownSizes : public CElement {
  * \brief Tria element with 1 Gauss Points
  * \author R. Sanchez
  */
-class CTRIA1 final : public CElementWithKnownSizes<1,3,2> {
-private:
-  enum : unsigned short {NGAUSS = 1};
-  enum : unsigned short {NNODE = 3};
-  enum : unsigned short {NDIM = 2};
+class CTRIA1 final : public CElementWithKnownSizes<1, 3, 2> {
+ private:
+  enum : unsigned short { NGAUSS = 1 };
+  enum : unsigned short { NNODE = 3 };
+  enum : unsigned short { NDIM = 2 };
 
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -817,7 +766,6 @@ class CTRIA1 final : public CElementWithKnownSizes<1,3,2> {
    * \return Area of the element.
    */
   su2double ComputeArea(const FrameType mode = REFERENCE) const override;
-
 };
 
 /*!
@@ -826,13 +774,13 @@ class CTRIA1 final : public CElementWithKnownSizes<1,3,2> {
  * \brief Quadrilateral element with 4 Gauss Points
  * \author R. Sanchez
  */
-class CQUAD4 final : public CElementWithKnownSizes<4,4,2> {
-private:
-  enum : unsigned short {NGAUSS = 4};
-  enum : unsigned short {NNODE = 4};
-  enum : unsigned short {NDIM = 2};
+class CQUAD4 final : public CElementWithKnownSizes<4, 4, 2> {
+ private:
+  enum : unsigned short { NGAUSS = 4 };
+  enum : unsigned short { NNODE = 4 };
+  enum : unsigned short { NDIM = 2 };
 
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -842,20 +790,24 @@ class CQUAD4 final : public CElementWithKnownSizes<4,4,2> {
    * \brief Shape functions (Ni) evaluated at point Xi,Eta.
    */
   inline static void ShapeFunctions(su2double Xi, su2double Eta, su2double* Ni) {
-    Ni[0] = 0.25*(1.0-Xi)*(1.0-Eta);
-    Ni[1] = 0.25*(1.0+Xi)*(1.0-Eta);
-    Ni[2] = 0.25*(1.0+Xi)*(1.0+Eta);
-    Ni[3] = 0.25*(1.0-Xi)*(1.0+Eta);
+    Ni[0] = 0.25 * (1.0 - Xi) * (1.0 - Eta);
+    Ni[1] = 0.25 * (1.0 + Xi) * (1.0 - Eta);
+    Ni[2] = 0.25 * (1.0 + Xi) * (1.0 + Eta);
+    Ni[3] = 0.25 * (1.0 - Xi) * (1.0 + Eta);
   }
 
   /*!
    * \brief Shape function Jacobian (dNi) evaluated at point Xi,Eta.
    */
   inline static void ShapeFunctionJacobian(su2double Xi, su2double Eta, su2double dNi[][2]) {
-    dNi[0][0] = -0.25*(1.0-Eta);  dNi[0][1] = -0.25*(1.0-Xi);
-    dNi[1][0] =  0.25*(1.0-Eta);  dNi[1][1] = -0.25*(1.0+Xi);
-    dNi[2][0] =  0.25*(1.0+Eta);  dNi[2][1] =  0.25*(1.0+Xi);
-    dNi[3][0] = -0.25*(1.0+Eta);  dNi[3][1] =  0.25*(1.0-Xi);
+    dNi[0][0] = -0.25 * (1.0 - Eta);
+    dNi[0][1] = -0.25 * (1.0 - Xi);
+    dNi[1][0] = 0.25 * (1.0 - Eta);
+    dNi[1][1] = -0.25 * (1.0 + Xi);
+    dNi[2][0] = 0.25 * (1.0 + Eta);
+    dNi[2][1] = 0.25 * (1.0 + Xi);
+    dNi[3][0] = -0.25 * (1.0 + Eta);
+    dNi[3][1] = 0.25 * (1.0 - Xi);
   }
 
   /*!
@@ -864,7 +816,6 @@ class CQUAD4 final : public CElementWithKnownSizes<4,4,2> {
    * \return Area of the element.
    */
   su2double ComputeArea(const FrameType mode = REFERENCE) const override;
-
 };
 
 /*!
@@ -873,13 +824,13 @@ class CQUAD4 final : public CElementWithKnownSizes<4,4,2> {
  * \brief Tetrahedral element with 1 Gauss Point
  * \author R. Sanchez
  */
-class CTETRA1 final : public CElementWithKnownSizes<1,4,3> {
-private:
-  enum : unsigned short {NGAUSS = 1};
-  enum : unsigned short {NNODE = 4};
-  enum : unsigned short {NDIM = 3};
+class CTETRA1 final : public CElementWithKnownSizes<1, 4, 3> {
+ private:
+  enum : unsigned short { NGAUSS = 1 };
+  enum : unsigned short { NNODE = 4 };
+  enum : unsigned short { NDIM = 3 };
 
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -890,7 +841,6 @@ class CTETRA1 final : public CElementWithKnownSizes<1,4,3> {
    * \return Volume of the element.
    */
   su2double ComputeVolume(const FrameType mode = REFERENCE) const override;
-
 };
 
 /*!
@@ -899,13 +849,13 @@ class CTETRA1 final : public CElementWithKnownSizes<1,4,3> {
  * \brief Hexahedral element with 8 Gauss Points
  * \author R. Sanchez
  */
-class CHEXA8 final : public CElementWithKnownSizes<8,8,3> {
-private:
-  enum : unsigned short {NGAUSS = 8};
-  enum : unsigned short {NNODE = 8};
-  enum : unsigned short {NDIM = 3};
+class CHEXA8 final : public CElementWithKnownSizes<8, 8, 3> {
+ private:
+  enum : unsigned short { NGAUSS = 8 };
+  enum : unsigned short { NNODE = 8 };
+  enum : unsigned short { NDIM = 3 };
 
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -917,7 +867,6 @@ class CHEXA8 final : public CElementWithKnownSizes<8,8,3> {
    * \return Volume of the element.
    */
   su2double ComputeVolume(const FrameType mode = REFERENCE) const override;
-
 };
 
 /*!
@@ -926,13 +875,13 @@ class CHEXA8 final : public CElementWithKnownSizes<8,8,3> {
  * \brief Pyramid element with 5 Gauss Points
  * \author R. Sanchez, F. Palacios, A. Bueno, T. Economon, S. Padron.
  */
-class CPYRAM5 final : public CElementWithKnownSizes<5,5,3> {
-private:
-  enum : unsigned short {NGAUSS = 5};
-  enum : unsigned short {NNODE = 5};
-  enum : unsigned short {NDIM = 3};
+class CPYRAM5 final : public CElementWithKnownSizes<5, 5, 3> {
+ private:
+  enum : unsigned short { NGAUSS = 5 };
+  enum : unsigned short { NNODE = 5 };
+  enum : unsigned short { NDIM = 3 };
 
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -944,7 +893,6 @@ class CPYRAM5 final : public CElementWithKnownSizes<5,5,3> {
    * \return Volume of the element.
    */
   su2double ComputeVolume(const FrameType mode = REFERENCE) const override;
-
 };
 
 /*!
@@ -954,13 +902,13 @@ class CPYRAM5 final : public CElementWithKnownSizes<5,5,3> {
  * \author R. Sanchez, F. Palacios, A. Bueno, T. Economon, S. Padron.
  * \version 7.5.1 "Blackbird"
  */
-class CPRISM6 final : public CElementWithKnownSizes<6,6,3> {
-private:
-  enum : unsigned short {NGAUSS = 6};
-  enum : unsigned short {NNODE = 6};
-  enum : unsigned short {NDIM = 3};
+class CPRISM6 final : public CElementWithKnownSizes<6, 6, 3> {
+ private:
+  enum : unsigned short { NGAUSS = 6 };
+  enum : unsigned short { NNODE = 6 };
+  enum : unsigned short { NDIM = 3 };
 
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -972,7 +920,6 @@ class CPRISM6 final : public CElementWithKnownSizes<6,6,3> {
    * \return Volume of the element.
    */
   su2double ComputeVolume(const FrameType mode = REFERENCE) const override;
-
 };
 
 /*!
@@ -981,13 +928,13 @@ class CPRISM6 final : public CElementWithKnownSizes<6,6,3> {
  * \brief Tria element with 3 Gauss Points
  * \author T.Dick
  */
-class CTRIA3 final : public CElementWithKnownSizes<3,3,2> {
-private:
-  enum : unsigned short {NGAUSS = 3};
-  enum : unsigned short {NNODE = 3};
-  enum : unsigned short {NDIM = 2};
+class CTRIA3 final : public CElementWithKnownSizes<3, 3, 2> {
+ private:
+  enum : unsigned short { NGAUSS = 3 };
+  enum : unsigned short { NNODE = 3 };
+  enum : unsigned short { NDIM = 2 };
 
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -999,7 +946,6 @@ class CTRIA3 final : public CElementWithKnownSizes<3,3,2> {
    * \return Area of the element.
    */
   su2double ComputeArea(const FrameType mode = REFERENCE) const override;
-
 };
 
 /*!
@@ -1008,13 +954,13 @@ class CTRIA3 final : public CElementWithKnownSizes<3,3,2> {
  * \brief Tetrahedral element with 4 Gauss Points
  * \author T.Dick
  */
-class CTETRA4 final : public CElementWithKnownSizes<4,4,3> {
-private:
-  enum : unsigned short {NGAUSS = 4};
-  enum : unsigned short {NNODE = 4};
-  enum : unsigned short {NDIM = 3};
+class CTETRA4 final : public CElementWithKnownSizes<4, 4, 3> {
+ private:
+  enum : unsigned short { NGAUSS = 4 };
+  enum : unsigned short { NNODE = 4 };
+  enum : unsigned short { NDIM = 3 };
 
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -1026,7 +972,6 @@ class CTETRA4 final : public CElementWithKnownSizes<4,4,3> {
    * \return Area of the element.
    */
   su2double ComputeVolume(const FrameType mode = REFERENCE) const override;
-
 };
 
 /*!
@@ -1035,13 +980,13 @@ class CTETRA4 final : public CElementWithKnownSizes<4,4,3> {
  * \brief Pyramid element with 6 Gauss Points
  * \author T.Dick
  */
-class CPYRAM6 final : public CElementWithKnownSizes<6,5,3> {
-private:
-  enum : unsigned short {NGAUSS = 6};
-  enum : unsigned short {NNODE = 5};
-  enum : unsigned short {NDIM = 3};
+class CPYRAM6 final : public CElementWithKnownSizes<6, 5, 3> {
+ private:
+  enum : unsigned short { NGAUSS = 6 };
+  enum : unsigned short { NNODE = 5 };
+  enum : unsigned short { NDIM = 3 };
 
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -1053,7 +998,6 @@ class CPYRAM6 final : public CElementWithKnownSizes<6,5,3> {
    * \return Volume of the element.
    */
   su2double ComputeVolume(const FrameType mode = REFERENCE) const override;
-
 };
 
 /*!
@@ -1062,13 +1006,13 @@ class CPYRAM6 final : public CElementWithKnownSizes<6,5,3> {
  * \brief Line element with 2 Gauss Points
  * \author T.Dick
  */
-class CLINE final : public CElementWithKnownSizes<2,2,1> {
-private:
-  enum : unsigned short {NGAUSS = 2};
-  enum : unsigned short {NNODE = 2};
-  enum : unsigned short {NDIM = 1};
+class CLINE final : public CElementWithKnownSizes<2, 2, 1> {
+ private:
+  enum : unsigned short { NGAUSS = 2 };
+  enum : unsigned short { NNODE = 2 };
+  enum : unsigned short { NDIM = 1 };
 
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -1080,5 +1024,4 @@ class CLINE final : public CElementWithKnownSizes<2,2,1> {
    * \return Area of the element.
    */
   su2double ComputeLength(const FrameType mode = REFERENCE) const override;
-
 };
diff --git a/Common/include/geometry/elements/CElementProperty.hpp b/Common/include/geometry/elements/CElementProperty.hpp
index 4646ba0a7ce..fce7425694e 100644
--- a/Common/include/geometry/elements/CElementProperty.hpp
+++ b/Common/include/geometry/elements/CElementProperty.hpp
@@ -35,11 +35,10 @@
  * \version 7.5.1 "Blackbird"
  */
 class CProperty {
-protected:
+ protected:
+  unsigned long iMat_Prop = 0; /*!< \brief Index of the properties (E, Nu) for the structural model used. */
 
-  unsigned long iMat_Prop = 0;  /*!< \brief Index of the properties (E, Nu) for the structural model used. */
-
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] valMat_Prop - Index of the physical properties (E,nu,rho,rho_dead_load) assigned to the element.
@@ -102,7 +101,6 @@ class CProperty {
   inline virtual void RegisterDensity(void) {}
 };
 
-
 /*!
  * \class CElementProperty
  * \ingroup Elasticity_Equations
@@ -111,29 +109,30 @@ class CProperty {
  * \version 7.5.1 "Blackbird"
  */
 class CElementProperty final : public CProperty {
-private:
-
-  unsigned long iMat_Mod = 0;        /*!< \brief Index of the material model used. */
-  unsigned long iElectric_Prop = 0;  /*!< \brief Index of the electric properties (Em) for the structural model used. */
-  unsigned long iDV = 0;             /*!< \brief Index of the group of design variables to which the element belongs. */
-  su2double design_rho = 1.0;        /*!< \brief Value of the design density for material-based topology optimization. */
-  su2double physical_rho = 1.0;      /*!< \brief Value of the physical density for material-based topology optimization. */
-
-public:
+ private:
+  unsigned long iMat_Mod = 0;       /*!< \brief Index of the material model used. */
+  unsigned long iElectric_Prop = 0; /*!< \brief Index of the electric properties (Em) for the structural model used. */
+  unsigned long iDV = 0;            /*!< \brief Index of the group of design variables to which the element belongs. */
+  su2double design_rho = 1.0;       /*!< \brief Value of the design density for material-based topology optimization. */
+  su2double physical_rho = 1.0; /*!< \brief Value of the physical density for material-based topology optimization. */
 
+ public:
   /*!
    * \brief Constructor of the class.
-   * \param[in] valMat_Model - Type of material model (i.e. numerics) for the element, see FEA_TERM etc. in option_structure.hpp.
-   * \param[in] valMat_Prop - Index of the physical properties (E,nu,rho,rho_dead_load) assigned to the element.
-   * \param[in] valElectric_Prop - Index of the electric properties.
-   * \param[in] valDV - Index of the design variable assigned to the element (bound to a material property by "DESIGN_VARIABLE_FEA").
-   * \param[in] valDensity - Value for Design and Physical densities (topology optimization variables).
-   */
-  CElementProperty(unsigned long valMat_Model, unsigned long valMat_Prop,
-                   unsigned long valElectric_Prop, unsigned long valDV,
-                   su2double valDensity = 1.0) : CProperty(valMat_Prop),
-    iMat_Mod(valMat_Model), iElectric_Prop(valElectric_Prop),
-    iDV(valDV), design_rho(valDensity), physical_rho(valDensity) {}
+   * \param[in] valMat_Model - Type of material model (i.e. numerics) for the element, see FEA_TERM etc. in
+   * option_structure.hpp. \param[in] valMat_Prop - Index of the physical properties (E,nu,rho,rho_dead_load) assigned
+   * to the element. \param[in] valElectric_Prop - Index of the electric properties. \param[in] valDV - Index of the
+   * design variable assigned to the element (bound to a material property by "DESIGN_VARIABLE_FEA"). \param[in]
+   * valDensity - Value for Design and Physical densities (topology optimization variables).
+   */
+  CElementProperty(unsigned long valMat_Model, unsigned long valMat_Prop, unsigned long valElectric_Prop,
+                   unsigned long valDV, su2double valDensity = 1.0)
+      : CProperty(valMat_Prop),
+        iMat_Mod(valMat_Model),
+        iElectric_Prop(valElectric_Prop),
+        iDV(valDV),
+        design_rho(valDensity),
+        physical_rho(valDensity) {}
 
   /*!
    * \brief Destructor of the class.
diff --git a/Common/include/geometry/elements/CGaussVariable.hpp b/Common/include/geometry/elements/CGaussVariable.hpp
index d547d2de6a1..3ce313403b6 100644
--- a/Common/include/geometry/elements/CGaussVariable.hpp
+++ b/Common/include/geometry/elements/CGaussVariable.hpp
@@ -36,16 +36,15 @@
  * \version 7.5.1 "Blackbird"
  */
 class CGaussVariable {
-protected:
-
-  su2activematrix GradNi_Xj;      /*!< \brief Gradient of the shape functions N[i] wrt the reference configuration. */
-  su2activematrix GradNi_xj;      /*!< \brief Gradient of the shape functions N[i] wrt the current configuration. */
-  su2activevector Ni;             /*!< \brief Shape functions N[i] at the gaussian point. */
-  su2double J_X = 0.0;            /*!< \brief Element Jacobian evaluated at this Gauss Point wrt the reference configuration. */
-  su2double J_x = 0.0;            /*!< \brief Element Jacobian evaluated at this Gauss Point wrt the current configuration. */
+ protected:
+  su2activematrix GradNi_Xj; /*!< \brief Gradient of the shape functions N[i] wrt the reference configuration. */
+  su2activematrix GradNi_xj; /*!< \brief Gradient of the shape functions N[i] wrt the current configuration. */
+  su2activevector Ni;        /*!< \brief Shape functions N[i] at the gaussian point. */
+  su2double J_X = 0.0; /*!< \brief Element Jacobian evaluated at this Gauss Point wrt the reference configuration. */
+  su2double J_x = 0.0; /*!< \brief Element Jacobian evaluated at this Gauss Point wrt the current configuration. */
   unsigned short iGaussPoint = 0; /*!< \brief Identifier of the Gauss point considered. */
 
-public:
+ public:
   /*!
    * \brief Deleted default constructor as this class does not allow resizing once created.
    */
@@ -58,13 +57,11 @@ class CGaussVariable {
    * \param[in] config - Definition of the particular problem.
    */
   CGaussVariable(unsigned short val_iGauss, unsigned short val_nDim, unsigned short val_nNodes)
-    : J_X(0.0), J_x(0.0), iGaussPoint(val_iGauss)
-  {
-
+      : J_X(0.0), J_x(0.0), iGaussPoint(val_iGauss) {
     /* --- For the structural mechanics solver the dimensions (nNodes x nDim) are sufficient.
      * For the Sobolev smoothing solver dimensions (nNodes x (nDim+1)) are necessary
      * when working on a curved design surface embedded in 3D. ---*/
-    GradNi_Xj.resize(val_nNodes,val_nDim+1) = su2double(0.0);
+    GradNi_Xj.resize(val_nNodes, val_nDim + 1) = su2double(0.0);
     GradNi_xj = GradNi_Xj;
 
     Ni.resize(val_nNodes) = su2double(0.0);
@@ -89,7 +86,6 @@ class CGaussVariable {
 
   inline void SetJ_x(su2double valJ_x) { J_x = valJ_x; }
 
-
   inline su2double GetGradNi_Xj(unsigned short val_Ni, unsigned short val_iDim) const {
     return GradNi_Xj(val_Ni, val_iDim);
   }
@@ -105,6 +101,4 @@ class CGaussVariable {
   inline su2double GetJ_x(void) const { return J_x; }
 
   inline unsigned short Get_iGauss(void) const { return iGaussPoint; }
-
 };
-
diff --git a/Common/include/geometry/meshreader/CBoxMeshReaderFVM.hpp b/Common/include/geometry/meshreader/CBoxMeshReaderFVM.hpp
index a9863e424d9..58ab28752b4 100644
--- a/Common/include/geometry/meshreader/CBoxMeshReaderFVM.hpp
+++ b/Common/include/geometry/meshreader/CBoxMeshReaderFVM.hpp
@@ -35,10 +35,8 @@
  * \brief Reads a 3D box grid into linear partitions for the finite volume solver (FVM).
  * \author: T. Economon
  */
-class CBoxMeshReaderFVM: public CMeshReaderFVM {
-
-private:
-
+class CBoxMeshReaderFVM : public CMeshReaderFVM {
+ private:
   unsigned long nNode; /*!< \brief Number of grid nodes in the x-direction. */
   unsigned long mNode; /*!< \brief Number of grid nodes in the y-direction. */
   unsigned long pNode; /*!< \brief Number of grid nodes in the z-direction. */
@@ -69,18 +67,14 @@ class CBoxMeshReaderFVM: public CMeshReaderFVM {
    */
   void ComputeBoxSurfaceConnectivity();
 
-public:
-
+ public:
   /*!
    * \brief Constructor of the CBoxMeshReaderFVM class.
    */
-  CBoxMeshReaderFVM(CConfig        *val_config,
-                    unsigned short val_iZone,
-                    unsigned short val_nZone);
+  CBoxMeshReaderFVM(CConfig* val_config, unsigned short val_iZone, unsigned short val_nZone);
 
   /*!
    * \brief Destructor of the CBoxMeshReaderFVM class.
    */
   ~CBoxMeshReaderFVM(void);
-
 };
diff --git a/Common/include/geometry/meshreader/CCGNSMeshReaderFVM.hpp b/Common/include/geometry/meshreader/CCGNSMeshReaderFVM.hpp
index c5448dfa9a0..5b65f4d925b 100644
--- a/Common/include/geometry/meshreader/CCGNSMeshReaderFVM.hpp
+++ b/Common/include/geometry/meshreader/CCGNSMeshReaderFVM.hpp
@@ -39,21 +39,24 @@
  * \brief Reads a CGNS zone into linear partitions for the finite volume solver (FVM).
  * \author: T. Economon
  */
-class CCGNSMeshReaderFVM: public CMeshReaderFVM {
-
-private:
-
+class CCGNSMeshReaderFVM : public CMeshReaderFVM {
+ private:
 #ifdef HAVE_CGNS
-  int cgnsFileID; /*!< \brief CGNS file identifier. */
+  int cgnsFileID;         /*!< \brief CGNS file identifier. */
   const int cgnsBase = 1; /*!< \brief CGNS database index (the CGNS reader currently assumes a single database). */
   const int cgnsZone = 1; /*!< \brief CGNS zone index (and 1 zone in that database). */
 
-  int nSections;  /*!< \brief Total number of sections in the CGNS file. */
-
-  vector<bool> isInterior;             /*!< \brief Vector of booleans to store whether each section in the CGNS file is an interior or boundary section. */
-  vector<unsigned long> nElems;        /*!< \brief Vector containing the local number of elements found within each CGNS section. */
-  vector<unsigned long> elemOffset;    /*!< \brief Global ID offset for each interior section (i.e., the total number of global elements that came before it). */
-  vector<vector<cgsize_t> > connElems; /*!< \brief Vector containing the local element connectivity found within each CGNS section. First index is the section, second contains the connectivity in format [globalID VTK n1 n2 n3 n4 n5 n6 n7 n8] for each element. */
+  int nSections; /*!< \brief Total number of sections in the CGNS file. */
+
+  vector<bool> isInterior; /*!< \brief Vector of booleans to store whether each section in the CGNS file is an interior
+                              or boundary section. */
+  vector<unsigned long>
+      nElems; /*!< \brief Vector containing the local number of elements found within each CGNS section. */
+  vector<unsigned long> elemOffset;    /*!< \brief Global ID offset for each interior section (i.e., the total number of
+                                          global elements that came before it). */
+  vector<vector<cgsize_t> > connElems; /*!< \brief Vector containing the local element connectivity found within each
+                                          CGNS section. First index is the section, second contains the connectivity in
+                                          format [globalID VTK n1 n2 n3 n4 n5 n6 n7 n8] for each element. */
   vector<vector<char> > sectionNames;  /*!< \brief Vector for storing the names of each boundary section (marker). */
 
   /*!
@@ -78,7 +81,8 @@ class CCGNSMeshReaderFVM: public CMeshReaderFVM {
   void ReadCGNSPointCoordinates();
 
   /*!
-   * \brief Reads the metadata for each CGNS section in a zone and collect information, including the size and whether it is an interior or boundary section.
+   * \brief Reads the metadata for each CGNS section in a zone and collect information, including the size and whether
+   * it is an interior or boundary section.
    */
   void ReadCGNSSectionMetadata();
 
@@ -89,8 +93,8 @@ class CCGNSMeshReaderFVM: public CMeshReaderFVM {
   void ReadCGNSVolumeSection(int val_section);
 
   /*!
-   * \brief Reads the surface (boundary) elements from the CGNS zone. Only the master rank currently reads and stores the connectivity, which is linearly partitioned later.
-   * \param[in] val_section - CGNS section index.
+   * \brief Reads the surface (boundary) elements from the CGNS zone. Only the master rank currently reads and stores
+   * the connectivity, which is linearly partitioned later. \param[in] val_section - CGNS section index.
    */
   void ReadCGNSSurfaceSection(int val_section);
 
@@ -110,27 +114,20 @@ class CCGNSMeshReaderFVM: public CMeshReaderFVM {
    * \param[out] val_vtk_type - VTK type identifier index.
    * \returns String containing the name of the element type.
    */
-  string GetCGNSElementType(ElementType_t val_elem_type,
-                            int           &val_vtk_type);
+  string GetCGNSElementType(ElementType_t val_elem_type, int& val_vtk_type);
 #endif
 
   /*!
    * \brief Routine to launch non-blocking sends and recvs amongst all processors.
    * \param[in] bufSend - Buffer of data to be sent.
-   * \param[in] nElemSend - Array containing the number of elements to send to other processors in cumulative storage format.
-   * \param[in] sendReq - Array of MPI send requests.
-   * \param[in] bufRecv - Buffer of data to be received.
-   * \param[in] nElemSend - Array containing the number of elements to receive from other processors in cumulative storage format.
-   * \param[in] sendReq - Array of MPI recv requests.
-   * \param[in] countPerElem - Pieces of data per element communicated.
+   * \param[in] nElemSend - Array containing the number of elements to send to other processors in cumulative storage
+   * format. \param[in] sendReq - Array of MPI send requests. \param[in] bufRecv - Buffer of data to be received.
+   * \param[in] nElemSend - Array containing the number of elements to receive from other processors in cumulative
+   * storage format. \param[in] sendReq - Array of MPI recv requests. \param[in] countPerElem - Pieces of data per
+   * element communicated.
    */
-  void InitiateCommsAll(void *bufSend,
-                        const int *nElemSend,
-                        SU2_MPI::Request *sendReq,
-                        void *bufRecv,
-                        const int *nElemRecv,
-                        SU2_MPI::Request *recvReq,
-                        unsigned short countPerElem,
+  void InitiateCommsAll(void* bufSend, const int* nElemSend, SU2_MPI::Request* sendReq, void* bufRecv,
+                        const int* nElemRecv, SU2_MPI::Request* recvReq, unsigned short countPerElem,
                         unsigned short commType);
 
   /*!
@@ -140,24 +137,16 @@ class CCGNSMeshReaderFVM: public CMeshReaderFVM {
    * \param[in] nRecvs - Number of receives to be completed.
    * \param[in] sendReq - Array of MPI recv requests.
    */
-  void CompleteCommsAll(int nSends,
-                        SU2_MPI::Request *sendReq,
-                        int nRecvs,
-                        SU2_MPI::Request *recvReq);
-
-
-public:
+  void CompleteCommsAll(int nSends, SU2_MPI::Request* sendReq, int nRecvs, SU2_MPI::Request* recvReq);
 
+ public:
   /*!
    * \brief Constructor of the CCGNSMeshReaderFVM class.
    */
-  CCGNSMeshReaderFVM(CConfig        *val_config,
-                     unsigned short val_iZone,
-                     unsigned short val_nZone);
+  CCGNSMeshReaderFVM(CConfig* val_config, unsigned short val_iZone, unsigned short val_nZone);
 
   /*!
    * \brief Destructor of the CCGNSMeshReaderFVM class.
    */
   ~CCGNSMeshReaderFVM(void);
-
 };
diff --git a/Common/include/geometry/meshreader/CMeshReaderFVM.hpp b/Common/include/geometry/meshreader/CMeshReaderFVM.hpp
index 000dd0cf1e8..f4a46384e3d 100644
--- a/Common/include/geometry/meshreader/CMeshReaderFVM.hpp
+++ b/Common/include/geometry/meshreader/CMeshReaderFVM.hpp
@@ -40,62 +40,60 @@
  * \author T. Economon
  */
 class CMeshReaderFVM {
-
-protected:
-
-  const int rank;  /*!< \brief MPI Rank. */
-  const int size;  /*!< \brief MPI Size. */
+ protected:
+  const int rank; /*!< \brief MPI Rank. */
+  const int size; /*!< \brief MPI Size. */
 
   const CConfig* config = nullptr; /*!< \brief Local pointer to the config parameter object. */
 
   unsigned short dimension = 0; /*!< \brief Dimension of the problem (2 or 3). */
 
-  unsigned long numberOfLocalPoints = 0;                /*!< \brief Number of local grid points within the linear partition on this rank. */
-  unsigned long numberOfGlobalPoints = 0;               /*!< \brief Number of global grid points within the mesh file. */
-  vector<vector<passivedouble> > localPointCoordinates; /*!< \brief Vector holding the coordinates from the mesh file for the local grid points. First index is dimension, second is point index. */
+  unsigned long numberOfLocalPoints =
+      0; /*!< \brief Number of local grid points within the linear partition on this rank. */
+  unsigned long numberOfGlobalPoints = 0; /*!< \brief Number of global grid points within the mesh file. */
+  vector<vector<passivedouble> >
+      localPointCoordinates; /*!< \brief Vector holding the coordinates from the mesh file for the local grid points.
+                                First index is dimension, second is point index. */
 
-  unsigned long numberOfLocalElements = 0;              /*!< \brief Number of local elements within the linear partition on this rank. */
+  unsigned long numberOfLocalElements =
+      0; /*!< \brief Number of local elements within the linear partition on this rank. */
   unsigned long numberOfGlobalElements = 0;             /*!< \brief Number of global elements within the mesh file. */
-  vector<unsigned long> localVolumeElementConnectivity; /*!< \brief Vector containing the element connectivity from the mesh file for the local elements. */
+  vector<unsigned long> localVolumeElementConnectivity; /*!< \brief Vector containing the element connectivity from the
+                                                           mesh file for the local elements. */
 
-  unsigned long numberOfMarkers = 0;                         /*!< \brief Total number of markers contained within the mesh file. */
-  vector<string> markerNames;                                /*!< \brief String names for all markers in the mesh file. */
-  vector<vector<unsigned long> > surfaceElementConnectivity; /*!< \brief Vector containing the surface element connectivity from the mesh file on a per-marker basis. Only the master node reads and stores this connectivity. */
-
-public:
+  unsigned long numberOfMarkers = 0; /*!< \brief Total number of markers contained within the mesh file. */
+  vector<string> markerNames;        /*!< \brief String names for all markers in the mesh file. */
+  vector<vector<unsigned long> >
+      surfaceElementConnectivity; /*!< \brief Vector containing the surface element connectivity from the mesh file on a
+                                     per-marker basis. Only the master node reads and stores this connectivity. */
 
+ public:
   /*!
    * \brief Constructor of the CMeshReaderFVM class.
    * \param[in] val_config - config object for the current zone.
    * \param[in] val_iZone  - Current zone index.
    * \param[in] val_nZone  - Total number of zones.
    */
-  CMeshReaderFVM(const CConfig *val_config,
-                 unsigned short val_iZone,
-                 unsigned short val_nZone);
+  CMeshReaderFVM(const CConfig* val_config, unsigned short val_iZone, unsigned short val_nZone);
 
   /*!
    * \brief Get the physical dimension of the problem (2 or 3).
    * \returns Physical dimension of the problem.
    */
-  inline unsigned short GetDimension() const {
-    return dimension;
-  }
+  inline unsigned short GetDimension() const { return dimension; }
 
   /*!
    * \brief Get the local point coordinates (linearly partitioned).
    * \returns Local point coordinates (linear partitioned).
    */
-  inline const vector<vector<passivedouble> > &GetLocalPointCoordinates() const {
-    return localPointCoordinates;
-  }
+  inline const vector<vector<passivedouble> >& GetLocalPointCoordinates() const { return localPointCoordinates; }
 
   /*!
-   * \brief Get the surface element connectivity for the specified marker. Only the master node owns the surface connectivity.
-   * \param[in] val_iMarker - current marker index.
-   * \returns Surface element connecitivity for a marker from the master rank.
+   * \brief Get the surface element connectivity for the specified marker. Only the master node owns the surface
+   * connectivity. \param[in] val_iMarker - current marker index. \returns Surface element connecitivity for a marker
+   * from the master rank.
    */
-  inline const vector<unsigned long> &GetSurfaceElementConnectivityForMarker(int val_iMarker) const {
+  inline const vector<unsigned long>& GetSurfaceElementConnectivityForMarker(int val_iMarker) const {
     return surfaceElementConnectivity[val_iMarker];
   }
 
@@ -105,14 +103,14 @@ class CMeshReaderFVM {
    * \returns Number of surface elements for a marker.
    */
   inline unsigned long GetNumberOfSurfaceElementsForMarker(int val_iMarker) const {
-    return (unsigned long)surfaceElementConnectivity[val_iMarker].size()/SU2_CONN_SIZE;
+    return (unsigned long)surfaceElementConnectivity[val_iMarker].size() / SU2_CONN_SIZE;
   }
 
   /*!
    * \brief Get the local volume element connectivity (linearly partitioned).
    * \returns Local volume element connectivity (linearly partitioned).
    */
-  inline const vector<unsigned long> &GetLocalVolumeElementConnectivity() const {
+  inline const vector<unsigned long>& GetLocalVolumeElementConnectivity() const {
     return localVolumeElementConnectivity;
   }
 
@@ -120,48 +118,35 @@ class CMeshReaderFVM {
    * \brief Get the total number of markers in the mesh zone.
    * \returns Total number of markers in the mesh zone.
    */
-  inline unsigned long GetNumberOfMarkers() const {
-    return numberOfMarkers;
-  }
+  inline unsigned long GetNumberOfMarkers() const { return numberOfMarkers; }
 
   /*!
    * \brief Get the vector of string names for all markers in the mesh zone.
    * \returns Vector of string names for all markers in the mesh zone.
    */
-  inline const vector<string> &GetMarkerNames() const {
-    return markerNames;
-  }
+  inline const vector<string>& GetMarkerNames() const { return markerNames; }
 
   /*!
    * \brief Get the number of local grid points within the linear partition on this rank.
    * \returns Number of local grid points within the linear partition on this rank.
    */
-  inline unsigned long GetNumberOfLocalPoints() const {
-    return numberOfLocalPoints;
-  }
+  inline unsigned long GetNumberOfLocalPoints() const { return numberOfLocalPoints; }
 
   /*!
    * \brief Get the number of global grid points within the mesh file.
    * \returns Number of global grid points within the mesh file.
    */
-  inline unsigned long GetNumberOfGlobalPoints() const {
-    return numberOfGlobalPoints;
-  }
+  inline unsigned long GetNumberOfGlobalPoints() const { return numberOfGlobalPoints; }
 
   /*!
    * \brief Get the number of local elements within the linear partition on this rank.
    * \returns Number of local elements within the linear partition on this rank.
    */
-  inline unsigned long GetNumberOfLocalElements() const {
-    return numberOfLocalElements;
-  }
+  inline unsigned long GetNumberOfLocalElements() const { return numberOfLocalElements; }
 
   /*!
    * \brief Get the number of global elements within the mesh file.
    * \returns Number of global elements within the mesh file.
    */
-  inline unsigned long GetNumberOfGlobalElements() const {
-    return numberOfGlobalElements;
-  }
-
+  inline unsigned long GetNumberOfGlobalElements() const { return numberOfGlobalElements; }
 };
diff --git a/Common/include/geometry/meshreader/CRectangularMeshReaderFVM.hpp b/Common/include/geometry/meshreader/CRectangularMeshReaderFVM.hpp
index f20cf26a702..ed040f4c6b4 100644
--- a/Common/include/geometry/meshreader/CRectangularMeshReaderFVM.hpp
+++ b/Common/include/geometry/meshreader/CRectangularMeshReaderFVM.hpp
@@ -35,10 +35,8 @@
  * \brief Reads a 2D rectangular grid into linear partitions for the finite volume solver (FVM).
  * \author: T. Economon
  */
-class CRectangularMeshReaderFVM: public CMeshReaderFVM {
-
-private:
-
+class CRectangularMeshReaderFVM : public CMeshReaderFVM {
+ private:
   unsigned long nNode; /*!< \brief Number of grid nodes in the x-direction. */
   unsigned long mNode; /*!< \brief Number of grid nodes in the y-direction. */
 
@@ -66,13 +64,9 @@ class CRectangularMeshReaderFVM: public CMeshReaderFVM {
    */
   void ComputeRectangularSurfaceConnectivity();
 
-public:
-
+ public:
   /*!
    * \brief Constructor of the CRectangularMeshReaderFVM class.
    */
-  CRectangularMeshReaderFVM(const CConfig *val_config,
-                            unsigned short val_iZone,
-                            unsigned short val_nZone);
-
+  CRectangularMeshReaderFVM(const CConfig* val_config, unsigned short val_iZone, unsigned short val_nZone);
 };
diff --git a/Common/include/geometry/meshreader/CSU2ASCIIMeshReaderFVM.hpp b/Common/include/geometry/meshreader/CSU2ASCIIMeshReaderFVM.hpp
index 6be7697534f..a63f07a75d4 100644
--- a/Common/include/geometry/meshreader/CSU2ASCIIMeshReaderFVM.hpp
+++ b/Common/include/geometry/meshreader/CSU2ASCIIMeshReaderFVM.hpp
@@ -37,9 +37,8 @@
  * \brief Reads a native SU2 ASCII grid into linear partitions for the finite volume solver (FVM).
  * \author T. Economon
  */
-class CSU2ASCIIMeshReaderFVM: public CMeshReaderFVM {
-
-private:
+class CSU2ASCIIMeshReaderFVM : public CMeshReaderFVM {
+ private:
   enum class FileSection { POINTS, ELEMENTS, MARKERS }; /*!< \brief Different sections of the file. */
   std::array<FileSection, 3> SectionOrder{};            /*!< \brief Order of the sections in the file. */
 
@@ -47,11 +46,12 @@ class CSU2ASCIIMeshReaderFVM: public CMeshReaderFVM {
   const unsigned short nZones; /*!< \brief Total number of zones in the SU2 file. */
 
   const string meshFilename; /*!< \brief Name of the SU2 ASCII mesh file being read. */
-  ifstream mesh_file;  /*!< \brief File object for the SU2 ASCII mesh file. */
+  ifstream mesh_file;        /*!< \brief File object for the SU2 ASCII mesh file. */
 
   bool actuator_disk; /*!< \brief Boolean for whether we have an actuator disk to split. */
 
-  unsigned long ActDiskNewPoints = 0; /*!< \brief Total number of new grid points to add due to actuator disk splitting. */
+  unsigned long ActDiskNewPoints =
+      0; /*!< \brief Total number of new grid points to add due to actuator disk splitting. */
 
   su2double Xloc = 0.0; /*!< \brief X-coordinate of the CG of the actuator disk surface. */
   su2double Yloc = 0.0; /*!< \brief X-coordinate of the CG of the actuator disk surface. */
@@ -59,12 +59,17 @@ class CSU2ASCIIMeshReaderFVM: public CMeshReaderFVM {
 
   vector<bool> ActDisk_Bool; /*!< \brief Flag to identify the grid points on the actuator disk. */
 
-  vector<unsigned long> ActDiskPoint_Back; /*!< \brief Vector containing the global index for the new grid points added to the back of the actuator disk. */
-  vector<unsigned long> VolumePoint_Inv; /*!< \brief Vector containing the inverse mapping from the global index to the added point index for the actuator disk. */
+  vector<unsigned long> ActDiskPoint_Back; /*!< \brief Vector containing the global index for the new grid points added
+                                              to the back of the actuator disk. */
+  vector<unsigned long> VolumePoint_Inv; /*!< \brief Vector containing the inverse mapping from the global index to the
+                                            added point index for the actuator disk. */
 
-  vector<su2double> CoordXActDisk; /*!< \brief X-coordinates of the new grid points added by splitting the actuator disk (size = ActDiskNewPoints). */
-  vector<su2double> CoordYActDisk; /*!< \brief Y-coordinates of the new grid points added by splitting the actuator disk (size = ActDiskNewPoints). */
-  vector<su2double> CoordZActDisk; /*!< \brief Z-coordinates of the new grid points added by splitting the actuator disk (size = ActDiskNewPoints). */
+  vector<su2double> CoordXActDisk; /*!< \brief X-coordinates of the new grid points added by splitting the actuator disk
+                                      (size = ActDiskNewPoints). */
+  vector<su2double> CoordYActDisk; /*!< \brief Y-coordinates of the new grid points added by splitting the actuator disk
+                                      (size = ActDiskNewPoints). */
+  vector<su2double> CoordZActDisk; /*!< \brief Z-coordinates of the new grid points added by splitting the actuator disk
+                                      (size = ActDiskNewPoints). */
 
   vector<su2double> CoordXVolumePoint; /*!< \brief X-coordinates of the volume elements touching the actuator disk. */
   vector<su2double> CoordYVolumePoint; /*!< \brief Y-coordinates of the volume elements touching the actuator disk. */
@@ -72,11 +77,11 @@ class CSU2ASCIIMeshReaderFVM: public CMeshReaderFVM {
 
   /*!
    * \brief Reads all SU2 ASCII mesh metadata and checks for errors.
-   * \param[in] single_pass - Try to read the contents together with the metadata if the order allows (points before elements).
-   * \param[in,out] config - Problem configuration where some metadata is updated (e.g. AoA).
-   * \returns True if single_pass was successful.
+   * \param[in] single_pass - Try to read the contents together with the metadata if the order allows (points before
+   * elements). \param[in,out] config - Problem configuration where some metadata is updated (e.g. AoA). \returns True
+   * if single_pass was successful.
    */
-  bool ReadMetadata(const bool single_pass, CConfig *config);
+  bool ReadMetadata(const bool single_pass, CConfig* config);
 
   /*!
    * \brief Splits a single surface actuator disk boundary into two separate markers (repeated points).
@@ -103,13 +108,9 @@ class CSU2ASCIIMeshReaderFVM: public CMeshReaderFVM {
    */
   void FastForwardToMyZone();
 
-public:
-
+ public:
   /*!
    * \brief Constructor of the CSU2ASCIIMeshReaderFVM class.
    */
-  CSU2ASCIIMeshReaderFVM(CConfig *val_config,
-                         unsigned short val_iZone,
-                         unsigned short val_nZone);
-
+  CSU2ASCIIMeshReaderFVM(CConfig* val_config, unsigned short val_iZone, unsigned short val_nZone);
 };
diff --git a/Common/include/geometry/primal_grid/CHexahedron.hpp b/Common/include/geometry/primal_grid/CHexahedron.hpp
index b249559e683..b6d2da966d1 100644
--- a/Common/include/geometry/primal_grid/CHexahedron.hpp
+++ b/Common/include/geometry/primal_grid/CHexahedron.hpp
@@ -39,10 +39,12 @@ struct CHexahedronConnectivity {
   enum { nFaces = N_FACES_HEXAHEDRON };
   enum { maxNodesFace = N_POINTS_QUADRILATERAL };
   enum { VTK_Type = HEXAHEDRON };
-  static constexpr unsigned short nNodesFace[6] = {4,4,4,4,4,4};
-  static constexpr unsigned short Faces[6][4] = {{0,1,5,4},{1,2,6,5},{2,3,7,6},{3,0,4,7},{0,3,2,1},{4,5,6,7}};
-  static constexpr unsigned short nNeighbor_Nodes[8] = {3,3,3,3,3,3,3,3};
-  static constexpr unsigned short Neighbor_Nodes[8][3] = {{1,3,4},{0,2,5},{1,3,6},{0,2,7},{0,5,7},{4,6,1},{2,5,7},{4,3,6}};
+  static constexpr unsigned short nNodesFace[6] = {4, 4, 4, 4, 4, 4};
+  static constexpr unsigned short Faces[6][4] = {{0, 1, 5, 4}, {1, 2, 6, 5}, {2, 3, 7, 6},
+                                                 {3, 0, 4, 7}, {0, 3, 2, 1}, {4, 5, 6, 7}};
+  static constexpr unsigned short nNeighbor_Nodes[8] = {3, 3, 3, 3, 3, 3, 3, 3};
+  static constexpr unsigned short Neighbor_Nodes[8][3] = {{1, 3, 4}, {0, 2, 5}, {1, 3, 6}, {0, 2, 7},
+                                                          {0, 5, 7}, {4, 6, 1}, {2, 5, 7}, {4, 3, 6}};
 };
 
 /*!
@@ -51,7 +53,7 @@ struct CHexahedronConnectivity {
  * \author F. Palacios
  */
 class CHexahedron : public CPrimalGridWithConnectivity<CHexahedronConnectivity> {
-public:
+ public:
   /*!
    * \brief Constructor using the nodes and index.
    * \param[in] val_point_0 - Index of the 1st point read from the grid file.
@@ -63,9 +65,8 @@ class CHexahedron : public CPrimalGridWithConnectivity<CHexahedronConnectivity>
    * \param[in] val_point_6 - Index of the 7th point read from the grid file.
    * \param[in] val_point_7 - Index of the 8th point read from the grid file.
    */
-  CHexahedron(unsigned long val_point_0, unsigned long val_point_1,
-              unsigned long val_point_2, unsigned long val_point_3,
-              unsigned long val_point_4, unsigned long val_point_5,
+  CHexahedron(unsigned long val_point_0, unsigned long val_point_1, unsigned long val_point_2,
+              unsigned long val_point_3, unsigned long val_point_4, unsigned long val_point_5,
               unsigned long val_point_6, unsigned long val_point_7);
 
   /*!
diff --git a/Common/include/geometry/primal_grid/CLine.hpp b/Common/include/geometry/primal_grid/CLine.hpp
index 26c786e534b..49281694bc1 100644
--- a/Common/include/geometry/primal_grid/CLine.hpp
+++ b/Common/include/geometry/primal_grid/CLine.hpp
@@ -39,10 +39,10 @@ struct CLineConnectivity {
   enum { nFaces = N_FACES_LINE };
   enum { maxNodesFace = N_POINTS_LINE };
   enum { VTK_Type = LINE };
-  static constexpr unsigned short nNodesFace[1]={2};
-  static constexpr unsigned short Faces[1][2]={{0,1}};
-  static constexpr unsigned short nNeighbor_Nodes[2]={1,1};
-  static constexpr unsigned short Neighbor_Nodes[2][1]={{1},{0}};
+  static constexpr unsigned short nNodesFace[1] = {2};
+  static constexpr unsigned short Faces[1][2] = {{0, 1}};
+  static constexpr unsigned short nNeighbor_Nodes[2] = {1, 1};
+  static constexpr unsigned short Neighbor_Nodes[2][1] = {{1}, {0}};
 };
 
 /*!
@@ -51,7 +51,7 @@ struct CLineConnectivity {
  * \author F. Palacios
  */
 class CLine final : public CPrimalGridWithConnectivity<CLineConnectivity> {
-public:
+ public:
   /*!
    * \brief Constructor using the nodes and index.
    * \param[in] val_point_0 - Index of the 1st triangle point read from the grid file.
@@ -62,7 +62,5 @@ class CLine final : public CPrimalGridWithConnectivity<CLineConnectivity> {
   /*!
    * \brief Change the orientation of an element.
    */
-  inline void Change_Orientation() override {
-    std::swap(Nodes[0], Nodes[1]);
-  }
+  inline void Change_Orientation() override { std::swap(Nodes[0], Nodes[1]); }
 };
diff --git a/Common/include/geometry/primal_grid/CPrimalGrid.hpp b/Common/include/geometry/primal_grid/CPrimalGrid.hpp
index 33f10270bf6..5b5e2cdf9d3 100644
--- a/Common/include/geometry/primal_grid/CPrimalGrid.hpp
+++ b/Common/include/geometry/primal_grid/CPrimalGrid.hpp
@@ -43,29 +43,30 @@
  * \author F. Palacios, T. Economon, M. Aehle.
  */
 class CPrimalGrid {
-protected:
+ protected:
   /* If this is a domain element, stores the global index.
    * If this is a boundary element, stores the index of the adjacent domain element. */
   unsigned long GlobalIndex_DomainElement;
 
-  std::unique_ptr<unsigned long[]> Nodes;      /*!< \brief Global node indices of the element. */
-  std::unique_ptr<long[]> Neighbor_Elements;   /*!< \brief Vector to store the elements surronding this element. */
+  std::unique_ptr<unsigned long[]> Nodes;    /*!< \brief Global node indices of the element. */
+  std::unique_ptr<long[]> Neighbor_Elements; /*!< \brief Vector to store the elements surronding this element. */
 
-  su2double Coord_CG[3] = {0.0};   /*!< \brief Coordinates of the center-of-gravity of the element. */
-  su2double Volume;                /*!< \brief Volume of the element. */
-  su2double LenScale;              /*!< \brief Length scale of the element. */
+  su2double Coord_CG[3] = {0.0}; /*!< \brief Coordinates of the center-of-gravity of the element. */
+  su2double Volume;              /*!< \brief Volume of the element. */
+  su2double LenScale;            /*!< \brief Length scale of the element. */
 
   unsigned short TimeLevel; /*!< \brief Time level of the element for time accurate local time stepping. */
-  /*!< \brief Vector to store the periodic index of a neighbor, -1 indicates no periodic transformation to the neighbor. */
+  /*!< \brief Vector to store the periodic index of a neighbor, -1 indicates no periodic transformation to the neighbor.
+   */
   int8_t PeriodIndexNeighbors[N_FACES_MAXIMUM];
 
   /*! \brief Whether or not the Jacobian of the faces can be considered
    * constant in the transformation to the standard element. */
   bool JacobianFaceIsConstant[N_FACES_MAXIMUM];
-  bool ElementOwnsFace[N_FACES_MAXIMUM];    /*!< \brief Whether or not the element owns each face. */
-  const bool FEM;                           /*!< \brief Whether this is a FEM element. */
+  bool ElementOwnsFace[N_FACES_MAXIMUM]; /*!< \brief Whether or not the element owns each face. */
+  const bool FEM;                        /*!< \brief Whether this is a FEM element. */
 
-public:
+ public:
   CPrimalGrid() = delete;
 
   /*!
@@ -110,7 +111,9 @@ class CPrimalGrid {
    * \param[in] val_elem - Global index of the element.
    * \param[in] val_face - Local index of the face.
    */
-  inline void SetNeighbor_Elements(unsigned long val_elem, unsigned short val_face) { Neighbor_Elements[val_face] = val_elem; }
+  inline void SetNeighbor_Elements(unsigned long val_elem, unsigned short val_face) {
+    Neighbor_Elements[val_face] = val_elem;
+  }
 
   /*!
    * \brief Make available the length scale of the element.
@@ -190,12 +193,12 @@ class CPrimalGrid {
    * \param[in] nDim - Number of dimensions (2 or 3).
    * \param[in] val_coord - Coordinates of the element.
    */
-  template<class T>
+  template <class T>
   inline su2double* SetCoord_CG(unsigned short nDim, const T& val_coord) {
     for (unsigned short iDim = 0; iDim < nDim; iDim++) {
       Coord_CG[iDim] = 0.0;
       for (unsigned short iNode = 0; iNode < GetnNodes(); iNode++)
-        Coord_CG[iDim] += val_coord[iNode][iDim]/su2double(GetnNodes());
+        Coord_CG[iDim] += val_coord[iNode][iDim] / su2double(GetnNodes());
     }
     return Coord_CG;
   }
@@ -238,7 +241,7 @@ class CPrimalGrid {
    * \brief A virtual member.
    * \param[in] val_color - New color of the element.
    */
-  inline virtual void SetColor(unsigned long val_color) { }
+  inline virtual void SetColor(unsigned long val_color) {}
 
   /*!
    * \brief A virtual member.
@@ -267,7 +270,7 @@ class CPrimalGrid {
   /*!
    * \brief Get the index of the domain element of which this boundary element is a face.
    */
-  inline unsigned long GetDomainElement() const{ return GlobalIndex_DomainElement; }
+  inline unsigned long GetDomainElement() const { return GlobalIndex_DomainElement; }
 
   /*!
    * \brief A pure virtual member.
@@ -278,13 +281,13 @@ class CPrimalGrid {
    * \brief A pure virtual member.
    * \return Type of the element using VTK nomenclature.
    */
-  inline virtual unsigned short GetRotation_Type() const{ return 0; }
+  inline virtual unsigned short GetRotation_Type() const { return 0; }
 
   /*!
    * \brief A pure virtual member.
    * \param[in] val_rotation_type - Kind of rotation/traslation that must be applied.
    */
-  inline virtual void SetRotation_Type(unsigned short val_rotation_type) { }
+  inline virtual void SetRotation_Type(unsigned short val_rotation_type) {}
 
   /*-- The following pure virtual functions are overridden in
    * CPrimalGridWithConnectivity, except for the FEM classes. --*/
@@ -351,9 +354,8 @@ class CPrimalGrid {
    * \param[out] nPointsPerFace - Number of corner points for each of the faces.
    * \param[out] faceConn       - Global IDs of the corner points of the faces.
    */
-  inline virtual void GetCornerPointsAllFaces(unsigned short &nFaces,
-                                      unsigned short nPointsPerFace[],
-                                      unsigned long  faceConn[6][4]) const { }
+  inline virtual void GetCornerPointsAllFaces(unsigned short& nFaces, unsigned short nPointsPerFace[],
+                                              unsigned long faceConn[6][4]) const {}
 
   /*!
    * \brief Virtual function to make available the global ID of this element.
@@ -377,7 +379,7 @@ class CPrimalGrid {
    * \brief Virtual function to make available the polynomial degree of the solution.
    * \return The polynomial degree of the solution.
    */
-  inline virtual unsigned short GetNPolySol() const{ return 0; }
+  inline virtual unsigned short GetNPolySol() const { return 0; }
 
   /*!
    * \brief Virtual function to make available the number of DOFs of the grid in the element.
@@ -419,21 +421,21 @@ class CPrimalGrid {
    * \brief Virtual function to make available the number of donor elements for the wall function treatment.
    * \return The number of donor elements.
    */
-  inline virtual unsigned short GetNDonorsWallFunctions() const {return 0;}
+  inline virtual unsigned short GetNDonorsWallFunctions() const { return 0; }
 
   /*!
    * \brief Virtual function to make available the pointer to the vector for the donor elements
             for the wall function treatment.
    * \return The pointer to the data of donorElementsWallFunctions.
    */
-  inline virtual unsigned long *GetDonorsWallFunctions() {return nullptr;}
-  inline virtual const unsigned long *GetDonorsWallFunctions() const {return nullptr;}
+  inline virtual unsigned long* GetDonorsWallFunctions() { return nullptr; }
+  inline virtual const unsigned long* GetDonorsWallFunctions() const { return nullptr; }
 
   /*!
    * \brief Virtual function to set the global ID's of the donor elements for the wall function treatment.
    * \param[in] donorElements - Vector, which contain the donor elements.
    */
-  inline virtual void SetDonorsWallFunctions(const std::vector<unsigned long> &donorElements) {}
+  inline virtual void SetDonorsWallFunctions(const std::vector<unsigned long>& donorElements) {}
 
   /*!
    * \brief Virtual function to remove the multiple donors for the wall function treatment.
@@ -462,28 +464,21 @@ class CPrimalGrid {
  *
  * \tparam Connectivity - class defining the connectivity structure
  */
-template<typename Connectivity>
+template <typename Connectivity>
 class CPrimalGridWithConnectivity : public CPrimalGrid {
-public:
-
+ public:
   CPrimalGridWithConnectivity(bool FEM) : CPrimalGrid(FEM, Connectivity::nNodes, Connectivity::nFaces) {}
 
-  inline unsigned short GetnNodes() const final {
-    return Connectivity::nNodes;
-  }
+  inline unsigned short GetnNodes() const final { return Connectivity::nNodes; }
 
-  inline unsigned short GetnFaces() const final {
-    return Connectivity::nFaces;
-  }
+  inline unsigned short GetnFaces() const final { return Connectivity::nFaces; }
 
   inline unsigned short GetnNodesFace(unsigned short val_face) const final {
     assert(val_face < Connectivity::nFaces);
     return Connectivity::nNodesFace[val_face];
   }
 
-  inline unsigned short GetMaxNodesFace() const final {
-    return Connectivity::maxNodesFace;
-  }
+  inline unsigned short GetMaxNodesFace() const final { return Connectivity::maxNodesFace; }
 
   inline unsigned short GetFaces(unsigned short val_face, unsigned short val_index) const final {
     assert(val_face < GetnFaces() && val_index < GetnNodesFace(val_face));
@@ -500,9 +495,5 @@ class CPrimalGridWithConnectivity : public CPrimalGrid {
     return Connectivity::Neighbor_Nodes[val_node][val_index];
   }
 
-  inline unsigned short GetVTK_Type() const final {
-    return Connectivity::VTK_Type;
-  }
-
+  inline unsigned short GetVTK_Type() const final { return Connectivity::VTK_Type; }
 };
-
diff --git a/Common/include/geometry/primal_grid/CPrimalGridBoundFEM.hpp b/Common/include/geometry/primal_grid/CPrimalGridBoundFEM.hpp
index 2356c8a442c..e6dcf964fe9 100644
--- a/Common/include/geometry/primal_grid/CPrimalGridBoundFEM.hpp
+++ b/Common/include/geometry/primal_grid/CPrimalGridBoundFEM.hpp
@@ -35,20 +35,20 @@
  * \brief Class to define primal grid boundary element for the FEM solver.
  * \version 7.5.1 "Blackbird"
  */
-class CPrimalGridBoundFEM final: public CPrimalGrid {
-private:
-  unsigned long boundElemIDGlobal;    /*!< \brief Global boundary element ID of this element. */
+class CPrimalGridBoundFEM final : public CPrimalGrid {
+ private:
+  unsigned long boundElemIDGlobal; /*!< \brief Global boundary element ID of this element. */
 
   std::vector<unsigned long> donorElementsWallFunctions; /*!< \brief The global ID's of the donor elements
                                                                 for the wall function treatment. */
 
-  unsigned short VTK_Type;     /*!< \brief Element type using the VTK convention. */
-  unsigned short nPolyGrid;    /*!< \brief Polynomial degree for the geometry of the element. */
-  unsigned short nDOFsGrid;    /*!< \brief Number of DOFs for the geometry of the element. */
+  unsigned short VTK_Type;  /*!< \brief Element type using the VTK convention. */
+  unsigned short nPolyGrid; /*!< \brief Polynomial degree for the geometry of the element. */
+  unsigned short nDOFsGrid; /*!< \brief Number of DOFs for the geometry of the element. */
 
-  bool JacobianConsideredConstant;    /*!< \brief Whether or not the Jacobian of the transformation to
-                                                  is (almost) constant. */
-public:
+  bool JacobianConsideredConstant; /*!< \brief Whether or not the Jacobian of the transformation to
+                                               is (almost) constant. */
+ public:
   /*!
    * \brief Constructor using data to initialize the boundary element.
    * \param[in] val_elemGlobalID    - Global boundary element ID of this element.
@@ -58,19 +58,18 @@ class CPrimalGridBoundFEM final: public CPrimalGrid {
    * \param[in] val_nDOFsGrid       - Number of DOFs used to describe the geometry of the element.
    * \param[in] val_nodes           - Vector, which contains the global node IDs of the element.
    */
-  CPrimalGridBoundFEM(unsigned long         val_elemGlobalID,
-                      unsigned long         val_domainElementID,
-                      unsigned short        val_VTK_Type,
-                      unsigned short        val_nPolyGrid,
-                      unsigned short        val_nDOFsGrid,
-                      std::vector<unsigned long> &val_nodes);
+  CPrimalGridBoundFEM(unsigned long val_elemGlobalID, unsigned long val_domainElementID, unsigned short val_VTK_Type,
+                      unsigned short val_nPolyGrid, unsigned short val_nDOFsGrid,
+                      std::vector<unsigned long>& val_nodes);
 
   /*!
    * \brief Get the number of nodes that composes a face of an element.
    * \param[in] val_face - Local index of the face.
    * \return Number of nodes that composes a face of an element.
    */
-  inline unsigned short GetnNodesFace(unsigned short val_face) const override { return std::numeric_limits<unsigned short>::max(); }
+  inline unsigned short GetnNodesFace(unsigned short val_face) const override {
+    return std::numeric_limits<unsigned short>::max();
+  }
 
   /*!
    * \brief Get the face index of an element.
@@ -78,7 +77,9 @@ class CPrimalGridBoundFEM final: public CPrimalGrid {
    * \param[in] val_index - Local (to the face) index of the nodes that compose the face.
    * \return Local (to the element) index of the nodes that compose the face.
    */
-  inline unsigned short GetFaces(unsigned short val_face, unsigned short val_index) const override { return std::numeric_limits<unsigned short>::max(); }
+  inline unsigned short GetFaces(unsigned short val_face, unsigned short val_index) const override {
+    return std::numeric_limits<unsigned short>::max();
+  }
 
   /*!
    * \brief Get the local index of the neighbors to a node (given the local index).
@@ -86,7 +87,9 @@ class CPrimalGridBoundFEM final: public CPrimalGrid {
    * \param[in] val_index - Local (to the neighbor nodes of val_node) index of the nodes that are neighbor to val_node.
    * \return Local (to the element) index of the nodes that are neighbor to val_node.
    */
-  inline unsigned short GetNeighbor_Nodes(unsigned short val_node, unsigned short val_index) const override { return std::numeric_limits<unsigned short>::max(); }
+  inline unsigned short GetNeighbor_Nodes(unsigned short val_node, unsigned short val_index) const override {
+    return std::numeric_limits<unsigned short>::max();
+  }
 
   /*!
    * \brief Get the number of nodes of an element.
@@ -105,7 +108,9 @@ class CPrimalGridBoundFEM final: public CPrimalGrid {
    * \param[in] val_node - Local (to the element) index of a node.
    * \return Number if neighbors of a node val_node.
    */
-  inline unsigned short GetnNeighbor_Nodes(unsigned short val_node) const override { return std::numeric_limits<unsigned short>::max(); }
+  inline unsigned short GetnNeighbor_Nodes(unsigned short val_node) const override {
+    return std::numeric_limits<unsigned short>::max();
+  }
 
   /*!
    * \brief Change the orientation of an element.
@@ -142,9 +147,8 @@ class CPrimalGridBoundFEM final: public CPrimalGrid {
    * \param[out] nPointsPerFace - Number of corner points for each of the faces.
    * \param[out] faceConn       - Global IDs of the corner points of the faces.
    */
-  void GetCornerPointsAllFaces(unsigned short &nFaces,
-                               unsigned short nPointsPerFace[],
-                               unsigned long  faceConn[6][4]) const override;
+  void GetCornerPointsAllFaces(unsigned short& nFaces, unsigned short nPointsPerFace[],
+                               unsigned long faceConn[6][4]) const override;
 
   /*!
    * \brief Static member function to get the local the corner points of all the face
@@ -155,11 +159,8 @@ class CPrimalGridBoundFEM final: public CPrimalGrid {
    * \param[out] nPointsPerFace - Number of corner points of the face.
    * \param[out] faceConn       - Global IDs of the corner points of the face.
    */
-  static void GetLocalCornerPointsFace(unsigned short elementType,
-                                       unsigned short nPoly,
-                                       unsigned short nDOFs,
-                                       unsigned short &nPointsPerFace,
-                                       unsigned long  faceConn[]);
+  static void GetLocalCornerPointsFace(unsigned short elementType, unsigned short nPoly, unsigned short nDOFs,
+                                       unsigned short& nPointsPerFace, unsigned long faceConn[]);
 
   /*!
    * \brief Make available the global ID of this element.
@@ -171,39 +172,45 @@ class CPrimalGridBoundFEM final: public CPrimalGrid {
    * \brief Function to get whether or not the Jacobian is considered constant.
    * \return True if the Jacobian is (almost) constant and false otherwise.
    */
-  inline bool GetJacobianConsideredConstant(void) const override {return JacobianConsideredConstant;}
+  inline bool GetJacobianConsideredConstant(void) const override { return JacobianConsideredConstant; }
 
   /*!
    * \brief Function to set the value of JacobianConsideredConstant.
    * \param[in] val_JacobianConsideredConstant - The value to be set for JacobianConsideredConstant.
    */
-  inline void SetJacobianConsideredConstant(bool val_JacobianConsideredConstant) override {JacobianConsideredConstant = val_JacobianConsideredConstant;}
+  inline void SetJacobianConsideredConstant(bool val_JacobianConsideredConstant) override {
+    JacobianConsideredConstant = val_JacobianConsideredConstant;
+  }
 
   /*!
    * \brief Add the given donor ID to the donor elements for the wall function treatment.
    * \param[in] donorElement - Element to be added to donor elements.
    */
-  inline void AddDonorWallFunctions(const unsigned long donorElement) override {donorElementsWallFunctions.push_back(donorElement);}
+  inline void AddDonorWallFunctions(const unsigned long donorElement) override {
+    donorElementsWallFunctions.push_back(donorElement);
+  }
 
   /*!
    * \brief Make available the number of donor elements for the wall function treatment.
    * \return The number of donor elements.
    */
-  inline unsigned short GetNDonorsWallFunctions(void) const override {return donorElementsWallFunctions.size();}
+  inline unsigned short GetNDonorsWallFunctions(void) const override { return donorElementsWallFunctions.size(); }
 
   /*!
    * \brief Make available the pointer to the vector for the donor elements
            for the wall function treatment.
    * \return The pointer to the data of donorElementsWallFunctions.
    */
-  inline unsigned long *GetDonorsWallFunctions(void) override {return donorElementsWallFunctions.data();}
-  inline const unsigned long *GetDonorsWallFunctions(void) const override {return donorElementsWallFunctions.data();}
+  inline unsigned long* GetDonorsWallFunctions(void) override { return donorElementsWallFunctions.data(); }
+  inline const unsigned long* GetDonorsWallFunctions(void) const override { return donorElementsWallFunctions.data(); }
 
   /*!
    * \brief Set the global ID's of the donor elements for the wall function treatment.
    * \param[in] donorElements - Vector, which contain the donor elements.
    */
-  inline void SetDonorsWallFunctions(const std::vector<unsigned long> &donorElements) override {donorElementsWallFunctions = donorElements;}
+  inline void SetDonorsWallFunctions(const std::vector<unsigned long>& donorElements) override {
+    donorElementsWallFunctions = donorElements;
+  }
 
   /*!
    * \brief Function to remove the multiple donors for the wall function treatment.
diff --git a/Common/include/geometry/primal_grid/CPrimalGridFEM.hpp b/Common/include/geometry/primal_grid/CPrimalGridFEM.hpp
index 622e7915069..8a12511c2fc 100644
--- a/Common/include/geometry/primal_grid/CPrimalGridFEM.hpp
+++ b/Common/include/geometry/primal_grid/CPrimalGridFEM.hpp
@@ -36,23 +36,23 @@
  * \brief Class to define primal grid element for the FEM solver.
  * \version 7.5.1 "Blackbird"
  */
-class CPrimalGridFEM final: public CPrimalGrid {
-private:
+class CPrimalGridFEM final : public CPrimalGrid {
+ private:
   unsigned long elemIDGlobal;        /*!< \brief Global element ID of this element. */
   unsigned long offsetDOFsSolGlobal; /*!< \brief Global offset of the solution DOFs of this element. */
   unsigned long color;               /*!< \brief Color of the element in the partitioning strategy. */
 
-  unsigned short VTK_Type;      /*!< \brief Element type using the VTK convention. */
-  unsigned short nPolyGrid;     /*!< \brief Polynomial degree for the geometry of the element. */
-  unsigned short nPolySol;      /*!< \brief Polynomial degree for the solution of the element. */
-  unsigned short nDOFsGrid;     /*!< \brief Number of DOFs for the geometry of the element. */
-  unsigned short nDOFsSol;      /*!< \brief Number of DOFs for the solution of the element. */
-  unsigned short nFaces;        /*!< \brief Number of faces of the element. */
+  unsigned short VTK_Type;  /*!< \brief Element type using the VTK convention. */
+  unsigned short nPolyGrid; /*!< \brief Polynomial degree for the geometry of the element. */
+  unsigned short nPolySol;  /*!< \brief Polynomial degree for the solution of the element. */
+  unsigned short nDOFsGrid; /*!< \brief Number of DOFs for the geometry of the element. */
+  unsigned short nDOFsSol;  /*!< \brief Number of DOFs for the solution of the element. */
+  unsigned short nFaces;    /*!< \brief Number of faces of the element. */
 
-  bool JacobianConsideredConstant;   /*!< \brief Whether or not the Jacobian of the transformation to
-                                                 is (almost) constant. */
+  bool JacobianConsideredConstant; /*!< \brief Whether or not the Jacobian of the transformation to
+                                               is (almost) constant. */
 
-public:
+ public:
   /*!
    * \brief Constructor using data to initialize the element.
    * \param[in] val_elemGlobalID - Global element ID of this element.
@@ -64,10 +64,9 @@ class CPrimalGridFEM final: public CPrimalGrid {
    * \param[in] val_offDOfsSol   - Global offset of the solution DOFs of the element.
    * \param[in] elem_line        - istringstream, which contains the grid node numbers of the element.
    */
-  CPrimalGridFEM(unsigned long  val_elemGlobalID, unsigned short val_VTK_Type,
-                 unsigned short val_nPolyGrid,    unsigned short val_nPolySol,
-                 unsigned short val_nDOFsGrid,    unsigned short val_nDOFsSol,
-                 unsigned long  val_offDOfsSol,   std::istringstream  &elem_line);
+  CPrimalGridFEM(unsigned long val_elemGlobalID, unsigned short val_VTK_Type, unsigned short val_nPolyGrid,
+                 unsigned short val_nPolySol, unsigned short val_nDOFsGrid, unsigned short val_nDOFsSol,
+                 unsigned long val_offDOfsSol, std::istringstream& elem_line);
 
   /*!
    * \brief Constructor using data to initialize the element.
@@ -80,17 +79,18 @@ class CPrimalGridFEM final: public CPrimalGrid {
    * \param[in] val_offDOfsSol   - Global offset of the solution DOFs of the element.
    * \param[in] connGrid         - Array, which contains the grid node numbers of the element.
    */
-  CPrimalGridFEM(unsigned long  val_elemGlobalID, unsigned short val_VTK_Type,
-                 unsigned short val_nPolyGrid,    unsigned short val_nPolySol,
-                 unsigned short val_nDOFsGrid,    unsigned short val_nDOFsSol,
-                 unsigned long  val_offDOfsSol,   const unsigned long *connGrid);
+  CPrimalGridFEM(unsigned long val_elemGlobalID, unsigned short val_VTK_Type, unsigned short val_nPolyGrid,
+                 unsigned short val_nPolySol, unsigned short val_nDOFsGrid, unsigned short val_nDOFsSol,
+                 unsigned long val_offDOfsSol, const unsigned long* connGrid);
 
   /*!
    * \brief Get the number of nodes that composes a face of an element.
    * \param[in] val_face - Local index of the face.
    * \return Number of nodes that composes a face of an element.
    */
-  inline unsigned short GetnNodesFace(unsigned short val_face) const override { return std::numeric_limits<unsigned short>::max(); }
+  inline unsigned short GetnNodesFace(unsigned short val_face) const override {
+    return std::numeric_limits<unsigned short>::max();
+  }
 
   /*!
    * \brief Get the face index of an element.
@@ -98,7 +98,9 @@ class CPrimalGridFEM final: public CPrimalGrid {
    * \param[in] val_index - Local (to the face) index of the nodes that compose the face.
    * \return Local (to the element) index of the nodes that compose the face.
    */
-  inline unsigned short GetFaces(unsigned short val_face, unsigned short val_index) const override { return std::numeric_limits<unsigned short>::max(); }
+  inline unsigned short GetFaces(unsigned short val_face, unsigned short val_index) const override {
+    return std::numeric_limits<unsigned short>::max();
+  }
 
   /*!
    * \brief Get the local index of the neighbors to a node (given the local index).
@@ -106,7 +108,9 @@ class CPrimalGridFEM final: public CPrimalGrid {
    * \param[in] val_index - Local (to the neighbor nodes of val_node) index of the nodes that are neighbor to val_node.
    * \return Local (to the element) index of the nodes that are neighbor to val_node.
    */
-  inline unsigned short GetNeighbor_Nodes(unsigned short val_node, unsigned short val_index) const override { return std::numeric_limits<unsigned short>::max(); }
+  inline unsigned short GetNeighbor_Nodes(unsigned short val_node, unsigned short val_index) const override {
+    return std::numeric_limits<unsigned short>::max();
+  }
 
   /*!
    * \brief Get the number of nodes of an element.
@@ -125,7 +129,9 @@ class CPrimalGridFEM final: public CPrimalGrid {
    * \param[in] val_node - Local (to the element) index of a node.
    * \return Number if neighbors of a node val_node.
    */
-  inline unsigned short GetnNeighbor_Nodes(unsigned short val_node) const override { return std::numeric_limits<unsigned short>::max(); }
+  inline unsigned short GetnNeighbor_Nodes(unsigned short val_node) const override {
+    return std::numeric_limits<unsigned short>::max();
+  }
 
   /*!
    * \brief Change the orientation of an element.
@@ -188,9 +194,8 @@ class CPrimalGridFEM final: public CPrimalGrid {
    * \param[out] nPointsPerFace - Number of corner points for each of the faces.
    * \param[out] faceConn       - Global IDs of the corner points of the faces.
    */
-  void GetCornerPointsAllFaces(unsigned short &numFaces,
-                               unsigned short nPointsPerFace[],
-                               unsigned long  faceConn[6][4]) const override;
+  void GetCornerPointsAllFaces(unsigned short& numFaces, unsigned short nPointsPerFace[],
+                               unsigned long faceConn[6][4]) const override;
 
   /*!
    * \brief Static member function to get the local the corner points of all the faces
@@ -203,12 +208,9 @@ class CPrimalGridFEM final: public CPrimalGrid {
    * \param[out] nPointsPerFace - Number of corner points for each of the faces.
    * \param[out] faceConn       - Global IDs of the corner points of the faces.
    */
-  static void GetLocalCornerPointsAllFaces(unsigned short elementType,
-                                           unsigned short nPoly,
-                                           unsigned short nDOFs,
-                                           unsigned short &numFaces,
-                                           unsigned short nPointsPerFace[],
-                                           unsigned long  faceConn[6][4]);
+  static void GetLocalCornerPointsAllFaces(unsigned short elementType, unsigned short nPoly, unsigned short nDOFs,
+                                           unsigned short& numFaces, unsigned short nPointsPerFace[],
+                                           unsigned long faceConn[6][4]);
   /*!
    * \brief Function to get whether or not the Jacobian is considered constant.
    * \return True if the Jacobian is (almost) constant and false otherwise.
@@ -231,11 +233,15 @@ class CPrimalGridFEM final: public CPrimalGrid {
    * \brief Function to set the value of JacobianConsideredConstant.
    * \param[in] val_JacobianConsideredConstant - The value to be set for JacobianConsideredConstant.
    */
-  inline void SetJacobianConsideredConstant(bool val_JacobianConsideredConstant) override {JacobianConsideredConstant = val_JacobianConsideredConstant;}
+  inline void SetJacobianConsideredConstant(bool val_JacobianConsideredConstant) override {
+    JacobianConsideredConstant = val_JacobianConsideredConstant;
+  }
 
   /*!
    * \brief Function to correct the offset of the global DOFs.
    * \param[in] val_offsetRank - The offset that must be added for this rank.
    */
-  inline void AddOffsetGlobalDOFs(const unsigned long val_offsetRank) override {offsetDOFsSolGlobal += val_offsetRank;}
+  inline void AddOffsetGlobalDOFs(const unsigned long val_offsetRank) override {
+    offsetDOFsSolGlobal += val_offsetRank;
+  }
 };
diff --git a/Common/include/geometry/primal_grid/CPrism.hpp b/Common/include/geometry/primal_grid/CPrism.hpp
index 1631aee0067..75322f6005c 100644
--- a/Common/include/geometry/primal_grid/CPrism.hpp
+++ b/Common/include/geometry/primal_grid/CPrism.hpp
@@ -39,10 +39,11 @@ struct CPrismConnectivity {
   enum { nFaces = N_FACES_PRISM };
   enum { maxNodesFace = N_POINTS_QUADRILATERAL };
   enum { VTK_Type = PRISM };
-  static constexpr unsigned short nNodesFace[5] = {4,4,4,3,3};
-  static constexpr unsigned short Faces[5][4] = {{3,4,1,0},{5,2,1,4},{2,5,3,0},{0,1,2,2},{5,4,3,3}};
-  static constexpr unsigned short nNeighbor_Nodes[6] = {3,3,3,3,3,3};
-  static constexpr unsigned short Neighbor_Nodes[6][3] = {{1,2,3},{0,2,4},{1,0,5},{0,4,5},{3,5,1},{4,3,2}};
+  static constexpr unsigned short nNodesFace[5] = {4, 4, 4, 3, 3};
+  static constexpr unsigned short Faces[5][4] = {{3, 4, 1, 0}, {5, 2, 1, 4}, {2, 5, 3, 0}, {0, 1, 2, 2}, {5, 4, 3, 3}};
+  static constexpr unsigned short nNeighbor_Nodes[6] = {3, 3, 3, 3, 3, 3};
+  static constexpr unsigned short Neighbor_Nodes[6][3] = {{1, 2, 3}, {0, 2, 4}, {1, 0, 5},
+                                                          {0, 4, 5}, {3, 5, 1}, {4, 3, 2}};
 };
 
 /*!
@@ -50,8 +51,8 @@ struct CPrismConnectivity {
  * \brief Class for prism element definition.
  * \author F. Palacios
  */
-class CPrism final: public CPrimalGridWithConnectivity<CPrismConnectivity> {
-public:
+class CPrism final : public CPrimalGridWithConnectivity<CPrismConnectivity> {
+ public:
   /*!
    * \brief Constructor using the nodes and index.
    * \param[in] val_point_0 - Index of the 1st point read from the grid file.
@@ -61,8 +62,7 @@ class CPrism final: public CPrimalGridWithConnectivity<CPrismConnectivity> {
    * \param[in] val_point_4 - Index of the 5th point read from the grid file.
    * \param[in] val_point_5 - Index of the 6th point read from the grid file.
    */
-  CPrism(unsigned long val_point_0, unsigned long val_point_1,
-         unsigned long val_point_2, unsigned long val_point_3,
+  CPrism(unsigned long val_point_0, unsigned long val_point_1, unsigned long val_point_2, unsigned long val_point_3,
          unsigned long val_point_4, unsigned long val_point_5);
 
   /*!
diff --git a/Common/include/geometry/primal_grid/CPyramid.hpp b/Common/include/geometry/primal_grid/CPyramid.hpp
index 64722e8dc3b..d3da90aa269 100644
--- a/Common/include/geometry/primal_grid/CPyramid.hpp
+++ b/Common/include/geometry/primal_grid/CPyramid.hpp
@@ -39,10 +39,11 @@ struct CPyramidConnectivity {
   enum { nFaces = N_FACES_PYRAMID };
   enum { maxNodesFace = N_POINTS_QUADRILATERAL };
   enum { VTK_Type = PYRAMID };
-  static constexpr unsigned short nNodesFace[5] = {4,3,3,3,3};
-  static constexpr unsigned short Faces[5][4] = {{0,3,2,1},{4,3,0,0},{4,0,1,1},{2,4,1,1},{3,4,2,2}};
-  static constexpr unsigned short nNeighbor_Nodes[5] = {3,3,3,3,4};
-  static constexpr unsigned short Neighbor_Nodes[5][4] = {{1,3,4,4},{0,2,4,4},{1,3,4,4},{2,0,4,4},{0,1,2,3}};
+  static constexpr unsigned short nNodesFace[5] = {4, 3, 3, 3, 3};
+  static constexpr unsigned short Faces[5][4] = {{0, 3, 2, 1}, {4, 3, 0, 0}, {4, 0, 1, 1}, {2, 4, 1, 1}, {3, 4, 2, 2}};
+  static constexpr unsigned short nNeighbor_Nodes[5] = {3, 3, 3, 3, 4};
+  static constexpr unsigned short Neighbor_Nodes[5][4] = {
+      {1, 3, 4, 4}, {0, 2, 4, 4}, {1, 3, 4, 4}, {2, 0, 4, 4}, {0, 1, 2, 3}};
 };
 
 /*!
@@ -50,22 +51,21 @@ struct CPyramidConnectivity {
  * \brief Class for pyramid element definition.
  * \author F. Palacios
  */
-class CPyramid final: public CPrimalGridWithConnectivity<CPyramidConnectivity> {
-public:
- /*!
-  * \brief Constructor using the nodes and index.
-  * \param[in] val_point_0 - Index of the 1st point read from the grid file.
-  * \param[in] val_point_1 - Index of the 2nd point read from the grid file.
-  * \param[in] val_point_2 - Index of the 3th point read from the grid file.
-  * \param[in] val_point_3 - Index of the 4th point read from the grid file.
-  * \param[in] val_point_4 - Index of the 5th point read from the grid file.
-  */
- CPyramid(unsigned long val_point_0, unsigned long val_point_1,
-          unsigned long val_point_2, unsigned long val_point_3,
-          unsigned long val_point_4);
+class CPyramid final : public CPrimalGridWithConnectivity<CPyramidConnectivity> {
+ public:
+  /*!
+   * \brief Constructor using the nodes and index.
+   * \param[in] val_point_0 - Index of the 1st point read from the grid file.
+   * \param[in] val_point_1 - Index of the 2nd point read from the grid file.
+   * \param[in] val_point_2 - Index of the 3th point read from the grid file.
+   * \param[in] val_point_3 - Index of the 4th point read from the grid file.
+   * \param[in] val_point_4 - Index of the 5th point read from the grid file.
+   */
+  CPyramid(unsigned long val_point_0, unsigned long val_point_1, unsigned long val_point_2, unsigned long val_point_3,
+           unsigned long val_point_4);
 
- /*!
-  * \brief Change the orientation of an element.
-  */
- void Change_Orientation() override;
+  /*!
+   * \brief Change the orientation of an element.
+   */
+  void Change_Orientation() override;
 };
diff --git a/Common/include/geometry/primal_grid/CQuadrilateral.hpp b/Common/include/geometry/primal_grid/CQuadrilateral.hpp
index f87ff807ed8..8d96240e3d3 100644
--- a/Common/include/geometry/primal_grid/CQuadrilateral.hpp
+++ b/Common/include/geometry/primal_grid/CQuadrilateral.hpp
@@ -39,10 +39,10 @@ struct CQuadrilateralConnectivity {
   enum { nFaces = N_FACES_QUADRILATERAL };
   enum { maxNodesFace = N_POINTS_LINE };
   enum { VTK_Type = QUADRILATERAL };
-  static constexpr unsigned short nNodesFace[4] = {2,2,2,2};
-  static constexpr unsigned short Faces[4][2] = {{0,1},{1,2},{2,3},{3,0}};
-  static constexpr unsigned short nNeighbor_Nodes[4] = {2,2,2,2};
-  static constexpr unsigned short Neighbor_Nodes[4][2] = {{1,3},{2,0},{3,1},{0,2}};
+  static constexpr unsigned short nNodesFace[4] = {2, 2, 2, 2};
+  static constexpr unsigned short Faces[4][2] = {{0, 1}, {1, 2}, {2, 3}, {3, 0}};
+  static constexpr unsigned short nNeighbor_Nodes[4] = {2, 2, 2, 2};
+  static constexpr unsigned short Neighbor_Nodes[4][2] = {{1, 3}, {2, 0}, {3, 1}, {0, 2}};
 };
 
 /*!
@@ -50,8 +50,8 @@ struct CQuadrilateralConnectivity {
  * \brief Class for quadrilateral element definition.
  * \author F. Palacios
  */
-class CQuadrilateral final: public CPrimalGridWithConnectivity<CQuadrilateralConnectivity> {
-public:
+class CQuadrilateral final : public CPrimalGridWithConnectivity<CQuadrilateralConnectivity> {
+ public:
   /*!
    * \brief Constructor using the nodes and index.
    * \param[in] val_point_0 - Index of the 1st point read from the grid file.
@@ -59,8 +59,8 @@ class CQuadrilateral final: public CPrimalGridWithConnectivity<CQuadrilateralCon
    * \param[in] val_point_2 - Index of the 3th point read from the grid file.
    * \param[in] val_point_3 - Index of the 4th point read from the grid file.
    */
-  CQuadrilateral(unsigned long val_point_0, unsigned long val_point_1,
-                 unsigned long val_point_2, unsigned long val_point_3);
+  CQuadrilateral(unsigned long val_point_0, unsigned long val_point_1, unsigned long val_point_2,
+                 unsigned long val_point_3);
 
   /*!
    * \brief Change the orientation of an element.
diff --git a/Common/include/geometry/primal_grid/CTetrahedron.hpp b/Common/include/geometry/primal_grid/CTetrahedron.hpp
index 652d5461a87..17eab59670c 100644
--- a/Common/include/geometry/primal_grid/CTetrahedron.hpp
+++ b/Common/include/geometry/primal_grid/CTetrahedron.hpp
@@ -39,10 +39,10 @@ struct CTetrahedronConnectivity {
   enum { nFaces = N_FACES_TETRAHEDRON };
   enum { maxNodesFace = N_POINTS_TRIANGLE };
   enum { VTK_Type = TETRAHEDRON };
-  static constexpr unsigned short nNodesFace[4]={3,3,3,3};
-  static constexpr unsigned short Faces[4][3]={{0,2,1},{0,1,3},{0,3,2},{1,2,3}};
-  static constexpr unsigned short nNeighbor_Nodes[4]={3,3,3,3};
-  static constexpr unsigned short Neighbor_Nodes[4][3]={{1,2,3},{0,2,3},{0,1,3},{0,1,2}};
+  static constexpr unsigned short nNodesFace[4] = {3, 3, 3, 3};
+  static constexpr unsigned short Faces[4][3] = {{0, 2, 1}, {0, 1, 3}, {0, 3, 2}, {1, 2, 3}};
+  static constexpr unsigned short nNeighbor_Nodes[4] = {3, 3, 3, 3};
+  static constexpr unsigned short Neighbor_Nodes[4][3] = {{1, 2, 3}, {0, 2, 3}, {0, 1, 3}, {0, 1, 2}};
 };
 
 /*!
@@ -50,8 +50,8 @@ struct CTetrahedronConnectivity {
  * \brief Class for tetrahedron element definition.
  * \author F. Palacios
  */
-class CTetrahedron final: public CPrimalGridWithConnectivity<CTetrahedronConnectivity> {
-public:
+class CTetrahedron final : public CPrimalGridWithConnectivity<CTetrahedronConnectivity> {
+ public:
   /*!
    * \brief Constructor using the nodes and index.
    * \param[in] val_point_0 - Index of the 1st point read from the grid file.
@@ -59,8 +59,8 @@ class CTetrahedron final: public CPrimalGridWithConnectivity<CTetrahedronConnect
    * \param[in] val_point_2 - Index of the 3th point read from the grid file.
    * \param[in] val_point_3 - Index of the 4th point read from the grid file.
    */
-  CTetrahedron(unsigned long val_point_0, unsigned long val_point_1,
-               unsigned long val_point_2, unsigned long val_point_3);
+  CTetrahedron(unsigned long val_point_0, unsigned long val_point_1, unsigned long val_point_2,
+               unsigned long val_point_3);
 
   /*!
    * \brief Change the orientation of an element.
diff --git a/Common/include/geometry/primal_grid/CTriangle.hpp b/Common/include/geometry/primal_grid/CTriangle.hpp
index e29fe4f8576..9518af4c467 100644
--- a/Common/include/geometry/primal_grid/CTriangle.hpp
+++ b/Common/include/geometry/primal_grid/CTriangle.hpp
@@ -39,10 +39,10 @@ struct CTriangleConnectivity {
   enum { nFaces = N_POINTS_TRIANGLE };
   enum { maxNodesFace = N_POINTS_LINE };
   enum { VTK_Type = TRIANGLE };
-  static constexpr unsigned short nNodesFace[3] = {2,2,2};
-  static constexpr unsigned short Faces[3][2] = {{0,1},{1,2},{2,0}};
-  static constexpr unsigned short nNeighbor_Nodes[3] = {2,2,2};
-  static constexpr unsigned short Neighbor_Nodes[3][2] = {{1,2},{2,0},{0,1}};
+  static constexpr unsigned short nNodesFace[3] = {2, 2, 2};
+  static constexpr unsigned short Faces[3][2] = {{0, 1}, {1, 2}, {2, 0}};
+  static constexpr unsigned short nNeighbor_Nodes[3] = {2, 2, 2};
+  static constexpr unsigned short Neighbor_Nodes[3][2] = {{1, 2}, {2, 0}, {0, 1}};
 };
 
 /*!
@@ -50,21 +50,18 @@ struct CTriangleConnectivity {
  * \brief Class for triangle element definition.
  * \author F. Palacios
  */
-class CTriangle final: public CPrimalGridWithConnectivity<CTriangleConnectivity> {
-public:
+class CTriangle final : public CPrimalGridWithConnectivity<CTriangleConnectivity> {
+ public:
   /*!
    * \brief Constructor using the nodes and index.
    * \param[in] val_point_0 - Index of the 1st triangle point read from the grid file.
    * \param[in] val_point_1 - Index of the 2nd triangle point read from the grid file.
    * \param[in] val_point_2 - Index of the 3th triangle point read from the grid file.
    */
-  CTriangle(unsigned long val_point_0, unsigned long val_point_1,
-            unsigned long val_point_2);
+  CTriangle(unsigned long val_point_0, unsigned long val_point_1, unsigned long val_point_2);
 
   /*!
    * \brief Change the orientation of an element.
    */
-  inline void Change_Orientation() override {
-    std::swap(Nodes[0], Nodes[2]);
-  }
+  inline void Change_Orientation() override { std::swap(Nodes[0], Nodes[2]); }
 };
diff --git a/Common/include/geometry/primal_grid/CVertexMPI.hpp b/Common/include/geometry/primal_grid/CVertexMPI.hpp
index 4d3c1fc3df2..04d55760940 100644
--- a/Common/include/geometry/primal_grid/CVertexMPI.hpp
+++ b/Common/include/geometry/primal_grid/CVertexMPI.hpp
@@ -52,12 +52,12 @@ struct CVertexMPIConnectivity {
  *        of element is used in the parallelization stuff.
  * \author F. Palacios
  */
-class CVertexMPI final: public CPrimalGridWithConnectivity<CVertexMPIConnectivity> {
-private:
+class CVertexMPI final : public CPrimalGridWithConnectivity<CVertexMPIConnectivity> {
+ private:
   /*! \brief Definition of the rotation, translation of the solution at the vertex. */
   unsigned short Rotation_Type;
 
-public:
+ public:
   /*!
    * \brief Constructor using the nodes and index.
    * \param[in] val_point - Index of the 1st triangle point read from the grid file.
diff --git a/Common/include/graph_coloring_structure.hpp b/Common/include/graph_coloring_structure.hpp
index 39810948ece..1ad5103cf71 100644
--- a/Common/include/graph_coloring_structure.hpp
+++ b/Common/include/graph_coloring_structure.hpp
@@ -44,7 +44,7 @@ using namespace std;
  * \version 7.5.1 "Blackbird"
  */
 class CGraphColoringStructure {
-public:
+ public:
   /*!
    * \brief Function, which determines the colors for the vertices of the given graph.
    * \param[in]  config             - Definition of the particular problem.
@@ -55,9 +55,7 @@ class CGraphColoringStructure {
    * \param[out] nGlobalColors      - Global number of colors in the graph.
    * \param[out] colorLocalVertices - The color of the local vertices of the graph.
    */
-  void GraphVertexColoring(CConfig                              *config,
-                           const vector<unsigned long>          &nVerticesPerRank,
-                           const vector<vector<unsigned long> > &entriesVertices,
-                           int                                  &nGlobalColors,
-                           vector<int>                          &colorLocalVertices);
+  void GraphVertexColoring(CConfig* config, const vector<unsigned long>& nVerticesPerRank,
+                           const vector<vector<unsigned long> >& entriesVertices, int& nGlobalColors,
+                           vector<int>& colorLocalVertices);
 };
diff --git a/Common/include/grid_movement/CBSplineBlending.hpp b/Common/include/grid_movement/CBSplineBlending.hpp
index c93607f3d0c..6965d3d3965 100644
--- a/Common/include/grid_movement/CBSplineBlending.hpp
+++ b/Common/include/grid_movement/CBSplineBlending.hpp
@@ -38,15 +38,13 @@ using namespace std;
  * \brief Class that defines the blending using uniform BSplines.
  * \author T. Albring
  */
-class CBSplineBlending : public CFreeFormBlending{
-
-private:
-  vector<su2double>          U;  /*!< \brief The knot vector for uniform BSplines on the interval [0,1]. */
-  vector<vector<su2double> > N;  /*!< \brief The temporary matrix holding the j+p basis functions up to order p. */
-  unsigned short KnotSize;       /*!< \brief The size of the knot vector. */
-
-public:
+class CBSplineBlending : public CFreeFormBlending {
+ private:
+  vector<su2double> U;          /*!< \brief The knot vector for uniform BSplines on the interval [0,1]. */
+  vector<vector<su2double> > N; /*!< \brief The temporary matrix holding the j+p basis functions up to order p. */
+  unsigned short KnotSize;      /*!< \brief The size of the knot vector. */
 
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -58,9 +56,9 @@ class CBSplineBlending : public CFreeFormBlending{
   ~CBSplineBlending() override;
 
   /*!
-   * \brief Returns the value of the i-th basis function and stores the values of the i+p basis functions in the matrix N.
-   * \param[in] val_i - index of the basis function.
-   * \param[in] val_t - Point at which we want to evaluate the i-th basis.
+   * \brief Returns the value of the i-th basis function and stores the values of the i+p basis functions in the matrix
+   * N. \param[in] val_i - index of the basis function. \param[in] val_t - Point at which we want to evaluate the i-th
+   * basis.
    */
   su2double GetBasis(short val_i, su2double val_t) override;
 
@@ -78,5 +76,4 @@ class CBSplineBlending : public CFreeFormBlending{
    * \param[in] n_controlpoints - the new number of control points.
    */
   void SetOrder(short val_order, short n_controlpoints) override;
-
 };
diff --git a/Common/include/grid_movement/CBezierBlending.hpp b/Common/include/grid_movement/CBezierBlending.hpp
index 51c80d2233c..dba2d8a9749 100644
--- a/Common/include/grid_movement/CBezierBlending.hpp
+++ b/Common/include/grid_movement/CBezierBlending.hpp
@@ -38,10 +38,8 @@ using namespace std;
  * \brief Class that defines the blending using Bernsteinpolynomials (Bezier Curves).
  * \author F. Palacios, T. Albring
  */
-class CBezierBlending : public CFreeFormBlending{
-
-private:
-
+class CBezierBlending : public CFreeFormBlending {
+ private:
   vector<su2double> binomial; /*!< \brief Temporary vector for the Bernstein evaluation. */
 
   /*!
@@ -70,8 +68,7 @@ class CBezierBlending : public CFreeFormBlending{
    */
   su2double Binomial(unsigned short n, unsigned short m);
 
-public:
-
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] val_order - Max. order of the basis functions.
@@ -85,9 +82,9 @@ class CBezierBlending : public CFreeFormBlending{
   ~CBezierBlending() override;
 
   /*!
-   * \brief Returns the value of the i-th basis function and stores the values of the i+p basis functions in the matrix N.
-   * \param[in] val_i - index of the basis function.
-   * \param[in] val_t - Point at which we want to evaluate the i-th basis.
+   * \brief Returns the value of the i-th basis function and stores the values of the i+p basis functions in the matrix
+   * N. \param[in] val_i - index of the basis function. \param[in] val_t - Point at which we want to evaluate the i-th
+   * basis.
    */
   su2double GetBasis(short val_i, su2double val_t) override;
 
@@ -105,5 +102,4 @@ class CBezierBlending : public CFreeFormBlending{
    * \param[in] n_controlpoints - the new number of control points.
    */
   void SetOrder(short val_order, short n_controlpoints) override;
-
 };
diff --git a/Common/include/grid_movement/CFreeFormBlending.hpp b/Common/include/grid_movement/CFreeFormBlending.hpp
index 1cda93ff33b..f8e71ae2e68 100644
--- a/Common/include/grid_movement/CFreeFormBlending.hpp
+++ b/Common/include/grid_movement/CFreeFormBlending.hpp
@@ -37,14 +37,12 @@
 #include "../basic_types/datatype_structure.hpp"
 
 class CFreeFormBlending {
-
-protected:
+ protected:
   unsigned short Order, /*!< \brief Order of the polynomial basis. */
-  Degree,               /*!< \brief Degree (Order - 1) of the polynomial basis. */
-  nControl;             /*!< \brief Number of control points. */
-
-public:
+      Degree,           /*!< \brief Degree (Order - 1) of the polynomial basis. */
+      nControl;         /*!< \brief Number of control points. */
 
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -60,7 +58,7 @@ class CFreeFormBlending {
    * \param[in] val_i - index of the basis function.
    * \param[in] val_t - Point at which we want to evaluate the i-th basis.
    */
-  inline virtual su2double GetBasis(short val_i, su2double val_t){return 0.0;}
+  inline virtual su2double GetBasis(short val_i, su2double val_t) { return 0.0; }
 
   /*!
    * \brief A pure virtual member.
@@ -68,22 +66,22 @@ class CFreeFormBlending {
    * \param[in] val_t - Point at which we want to evaluate the derivative of the i-th basis.
    * \param[in] val_order - Order of the derivative.
    */
-  inline virtual su2double GetDerivative(short val_i, su2double val_t, short val_order){return 0.0;}
+  inline virtual su2double GetDerivative(short val_i, su2double val_t, short val_order) { return 0.0; }
 
   /*!
    * \brief A pure virtual member.
    * \param[in] val_order - The new order of the function.
    * \param[in] n_controlpoints - the new number of control points.
    */
-  inline virtual void SetOrder(short val_order, short n_controlpoints) { }
+  inline virtual void SetOrder(short val_order, short n_controlpoints) {}
 
   /*!
    * \brief Returns the current order of the function.
    */
-  inline su2double GetOrder() const{return Order;}
+  inline su2double GetOrder() const { return Order; }
 
   /*!
    * \brief Returns the current degree of the function.
    */
-  inline su2double GetDegree() const{return Degree;}
+  inline su2double GetDegree() const { return Degree; }
 };
diff --git a/Common/include/grid_movement/CFreeFormDefBox.hpp b/Common/include/grid_movement/CFreeFormDefBox.hpp
index 7bb489cc911..70a1d3adcec 100644
--- a/Common/include/grid_movement/CFreeFormDefBox.hpp
+++ b/Common/include/grid_movement/CFreeFormDefBox.hpp
@@ -36,48 +36,46 @@
  * \author F. Palacios & A. Galdran.
  */
 class CFreeFormDefBox : public CGridMovement {
-public:
-  unsigned short nDim;                  /*!< \brief Number of dimensions of the problem. */
-  unsigned short nCornerPoints,         /*!< \brief Number of corner points of the FFDBox. */
-  nControlPoints, nControlPoints_Copy;  /*!< \brief Number of control points of the FFDBox. */
-  su2double **Coord_Corner_Points,    /*!< \brief Coordinates of the corner points. */
-  ****Coord_Control_Points,           /*!< \brief Coordinates of the control points. */
-  ****ParCoord_Control_Points,        /*!< \brief Coordinates of the control points. */
-  ****Coord_Control_Points_Copy,      /*!< \brief Coordinates of the control points (copy). */
-  ****Coord_SupportCP{nullptr};       /*!< \brief Coordinates of the support control points. */
-  unsigned short lOrder, lOrder_Copy, /*!< \brief Order of the FFDBox in the i direction. */
-  mOrder, mOrder_Copy,        /*!< \brief Order of the FFDBox in the j direction. */
-  nOrder, nOrder_Copy;          /*!< \brief Order of the FFDBox in the k direction. */
-  unsigned short lDegree, lDegree_Copy, /*!< \brief Degree of the FFDBox in the i direction. (lOrder - 1)*/
-  mDegree, mDegree_Copy,        /*!< \brief Degree of the FFDBox in the j direction. (mOrder - 1)*/
-  nDegree, nDegree_Copy;        /*!< \brief Degree of the FFDBox in the k direction. (nOrder - 1)*/
-  su2double *ParamCoord, *ParamCoord_,  /*!< \brief Parametric coordinates of a point. */
-  *cart_coord, *cart_coord_;      /*!< \brief Cartesian coordinates of a point. */
-  su2double ObjFunc;      /*!< \brief Objective function of the point inversion process. */
-  su2double *Gradient;      /*!< \brief Gradient of the point inversion process. */
-  su2double **Hessian;          /*!< \brief Hessian of the point inversion process. */
-  su2double MaxCoord[3];    /*!< \brief Maximum coordinates of the FFDBox. */
-  su2double MinCoord[3];    /*!< \brief Minimum coordinates of the FFDBox. */
-  string Tag;         /*!< \brief Tag to identify the FFDBox. */
-  unsigned short Level;     /*!< \brief Nested level of the FFD box. */
+ public:
+  unsigned short nDim;                     /*!< \brief Number of dimensions of the problem. */
+  unsigned short nCornerPoints,            /*!< \brief Number of corner points of the FFDBox. */
+      nControlPoints, nControlPoints_Copy; /*!< \brief Number of control points of the FFDBox. */
+  su2double **Coord_Corner_Points,         /*!< \brief Coordinates of the corner points. */
+      ****Coord_Control_Points,            /*!< \brief Coordinates of the control points. */
+      ****ParCoord_Control_Points,         /*!< \brief Coordinates of the control points. */
+      ****Coord_Control_Points_Copy,       /*!< \brief Coordinates of the control points (copy). */
+      ****Coord_SupportCP{nullptr};        /*!< \brief Coordinates of the support control points. */
+  unsigned short lOrder, lOrder_Copy,      /*!< \brief Order of the FFDBox in the i direction. */
+      mOrder, mOrder_Copy,                 /*!< \brief Order of the FFDBox in the j direction. */
+      nOrder, nOrder_Copy;                 /*!< \brief Order of the FFDBox in the k direction. */
+  unsigned short lDegree, lDegree_Copy,    /*!< \brief Degree of the FFDBox in the i direction. (lOrder - 1)*/
+      mDegree, mDegree_Copy,               /*!< \brief Degree of the FFDBox in the j direction. (mOrder - 1)*/
+      nDegree, nDegree_Copy;               /*!< \brief Degree of the FFDBox in the k direction. (nOrder - 1)*/
+  su2double *ParamCoord, *ParamCoord_,     /*!< \brief Parametric coordinates of a point. */
+      *cart_coord, *cart_coord_;           /*!< \brief Cartesian coordinates of a point. */
+  su2double ObjFunc;                       /*!< \brief Objective function of the point inversion process. */
+  su2double* Gradient;                     /*!< \brief Gradient of the point inversion process. */
+  su2double** Hessian;                     /*!< \brief Hessian of the point inversion process. */
+  su2double MaxCoord[3];                   /*!< \brief Maximum coordinates of the FFDBox. */
+  su2double MinCoord[3];                   /*!< \brief Minimum coordinates of the FFDBox. */
+  string Tag;                              /*!< \brief Tag to identify the FFDBox. */
+  unsigned short Level;                    /*!< \brief Nested level of the FFD box. */
 
   vector<su2double> CartesianCoord[3];  /*!< \brief Vector with all the cartesian coordinates in the FFD FFDBox. */
   vector<su2double> ParametricCoord[3]; /*!< \brief Vector with all the parametrics coordinates in the FFD FFDBox. */
-  vector<unsigned short> MarkerIndex; /*!< \brief Vector with all markers in the FFD FFDBox. */
-  vector<unsigned long> VertexIndex;  /*!< \brief Vector with all vertex index in the FFD FFDBox. */
-  vector<unsigned long> PointIndex;   /*!< \brief Vector with all points index in the FFD FFDBox. */
-  unsigned long nSurfacePoint;      /*!< \brief Number of surfaces in the FFD FFDBox. */
-  vector<string> ParentFFDBox;      /*!< \brief Vector with all the parent FFD FFDBox. */
-  vector<string> ChildFFDBox;     /*!< \brief Vector with all the child FFD FFDBox. */
-  vector<unsigned short> Fix_IPlane;  /*!< \brief Fix FFD I plane. */
-  vector<unsigned short> Fix_JPlane;  /*!< \brief Fix FFD J plane. */
-  vector<unsigned short> Fix_KPlane;  /*!< \brief Fix FFD K plane. */
+  vector<unsigned short> MarkerIndex;   /*!< \brief Vector with all markers in the FFD FFDBox. */
+  vector<unsigned long> VertexIndex;    /*!< \brief Vector with all vertex index in the FFD FFDBox. */
+  vector<unsigned long> PointIndex;     /*!< \brief Vector with all points index in the FFD FFDBox. */
+  unsigned long nSurfacePoint;          /*!< \brief Number of surfaces in the FFD FFDBox. */
+  vector<string> ParentFFDBox;          /*!< \brief Vector with all the parent FFD FFDBox. */
+  vector<string> ChildFFDBox;           /*!< \brief Vector with all the child FFD FFDBox. */
+  vector<unsigned short> Fix_IPlane;    /*!< \brief Fix FFD I plane. */
+  vector<unsigned short> Fix_JPlane;    /*!< \brief Fix FFD J plane. */
+  vector<unsigned short> Fix_KPlane;    /*!< \brief Fix FFD K plane. */
 
   CFreeFormBlending** BlendingFunction;
 
-
-public:
-
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -172,29 +170,32 @@ class CFreeFormDefBox : public CGridMovement {
    * \brief Add to the vector of cartesian coordinates a new coordinate.
    * \param[in] val_coord - New coordinate inside the FFD box.
    */
-  inline void Set_CartesianCoord(su2double *val_coord) { CartesianCoord[0].push_back(val_coord[0]);
-                                                                      CartesianCoord[1].push_back(val_coord[1]);
-                                                                      CartesianCoord[2].push_back(val_coord[2]); }
-
+  inline void Set_CartesianCoord(su2double* val_coord) {
+    CartesianCoord[0].push_back(val_coord[0]);
+    CartesianCoord[1].push_back(val_coord[1]);
+    CartesianCoord[2].push_back(val_coord[2]);
+  }
 
   /*!
    * \brief Adds to the vector of cartesian coordinates.
    * \param[in] val_coord - New coord inside FFD box.
    * \param[in] val_iSurfacePoints - Surface points of FFD box.
    */
-  inline void Set_CartesianCoord(const su2double *val_coord, unsigned long val_iSurfacePoints) { CartesianCoord[0][val_iSurfacePoints] = val_coord[0];
-                                                                                                        CartesianCoord[1][val_iSurfacePoints] = val_coord[1];
-                                                                                                        CartesianCoord[2][val_iSurfacePoints] = val_coord[2]; }
-
+  inline void Set_CartesianCoord(const su2double* val_coord, unsigned long val_iSurfacePoints) {
+    CartesianCoord[0][val_iSurfacePoints] = val_coord[0];
+    CartesianCoord[1][val_iSurfacePoints] = val_coord[1];
+    CartesianCoord[2][val_iSurfacePoints] = val_coord[2];
+  }
 
   /*!
    * \brief Add to the vector of parametric coordinates a new coordinate.
    * \param[in] val_coord - New coordinate inside the FFD box.
    */
-  inline void Set_ParametricCoord(su2double *val_coord) { ParametricCoord[0].push_back(val_coord[0]);
-                                                                       ParametricCoord[1].push_back(val_coord[1]);
-                                                                       ParametricCoord[2].push_back(val_coord[2]); }
-
+  inline void Set_ParametricCoord(su2double* val_coord) {
+    ParametricCoord[0].push_back(val_coord[0]);
+    ParametricCoord[1].push_back(val_coord[1]);
+    ParametricCoord[2].push_back(val_coord[2]);
+  }
 
   /*!
    * \brief Add to the vector of parent FFDBoxes a new FFD FFDBox.
@@ -213,10 +214,11 @@ class CFreeFormDefBox : public CGridMovement {
    * \param[in] val_coord - New coord inside FFD box.
    * \param[in] val_iSurfacePoints - Surface points of FFD box.
    */
-  inline void Set_ParametricCoord(const su2double *val_coord, unsigned long val_iSurfacePoints) { ParametricCoord[0][val_iSurfacePoints] = val_coord[0];
-                                                                                                         ParametricCoord[1][val_iSurfacePoints] = val_coord[1];
-                                                                                                         ParametricCoord[2][val_iSurfacePoints] = val_coord[2]; }
-
+  inline void Set_ParametricCoord(const su2double* val_coord, unsigned long val_iSurfacePoints) {
+    ParametricCoord[0][val_iSurfacePoints] = val_coord[0];
+    ParametricCoord[1][val_iSurfacePoints] = val_coord[1];
+    ParametricCoord[2][val_iSurfacePoints] = val_coord[2];
+  }
 
   /*!
    * \brief Get index of the marker.
@@ -240,7 +242,7 @@ class CFreeFormDefBox : public CGridMovement {
    * \brief Get Cartesian coordinates.
    * \param[in] Get_VertexIndex - Surface points of FFD box.
    */
-  inline su2double *Get_CartesianCoord(unsigned long val_iSurfacePoints) {
+  inline su2double* Get_CartesianCoord(unsigned long val_iSurfacePoints) {
     cart_coord_[0] = CartesianCoord[0][val_iSurfacePoints];
     cart_coord_[1] = CartesianCoord[1][val_iSurfacePoints];
     cart_coord_[2] = CartesianCoord[2][val_iSurfacePoints];
@@ -251,7 +253,7 @@ class CFreeFormDefBox : public CGridMovement {
    * \brief Get parametric coordinates.
    * \param[in] Get_VertexIndex - Surface points of FFD box.
    */
-  inline su2double *Get_ParametricCoord(unsigned long val_iSurfacePoints) {
+  inline su2double* Get_ParametricCoord(unsigned long val_iSurfacePoints) {
     ParamCoord_[0] = ParametricCoord[0][val_iSurfacePoints];
     ParamCoord_[1] = ParametricCoord[1][val_iSurfacePoints];
     ParamCoord_[2] = ParametricCoord[2][val_iSurfacePoints];
@@ -265,7 +267,7 @@ class CFreeFormDefBox : public CGridMovement {
 
   /*!
    * \brief Get number of parent FFD boxes.
-  */
+   */
   inline unsigned short GetnParentFFDBox(void) const { return ParentFFDBox.size(); }
 
   /*!
@@ -290,7 +292,7 @@ class CFreeFormDefBox : public CGridMovement {
    *        and find the position of the control points for the FFDBox
    * \param[in] FFDBox - Original FFDBox where we want to compute the control points.
    */
-  void SetSupportCPChange(CFreeFormDefBox *FFDBox);
+  void SetSupportCPChange(CFreeFormDefBox* FFDBox);
 
   /*!
    * \brief Set the number of corner points.
@@ -314,7 +316,7 @@ class CFreeFormDefBox : public CGridMovement {
    * \brief Get the number of control points.
    * \return Number of control points.
    */
-  inline void SetnControlPoints(void) { nControlPoints = lOrder*mOrder*nOrder; }
+  inline void SetnControlPoints(void) { nControlPoints = lOrder * mOrder * nOrder; }
 
   /*!
    * \brief Get the number of numerical points on the surface.
@@ -332,12 +334,10 @@ class CFreeFormDefBox : public CGridMovement {
    * \param[in] val_coord - Coordinates of the corner point with index <i>val_icornerpoints</i>.
    * \param[in] val_icornerpoints - Index of the corner point.
    */
-  inline void SetCoordCornerPoints(const su2double *val_coord, unsigned short val_icornerpoints) {
-    for (unsigned short iDim = 0; iDim < nDim; iDim++)
-      Coord_Corner_Points[val_icornerpoints][iDim] = val_coord[iDim];
+  inline void SetCoordCornerPoints(const su2double* val_coord, unsigned short val_icornerpoints) {
+    for (unsigned short iDim = 0; iDim < nDim; iDim++) Coord_Corner_Points[val_icornerpoints][iDim] = val_coord[iDim];
   }
 
-
   /*!
    * \overload
    * \param[in] val_xcoord - X coordinate of the corner point with index <i>val_icornerpoints</i>.
@@ -345,13 +345,13 @@ class CFreeFormDefBox : public CGridMovement {
    * \param[in] val_zcoord - Z coordinate of the corner point with index <i>val_icornerpoints</i>.
    * \param[in] val_icornerpoints - Index of the corner point.
    */
-  inline void SetCoordCornerPoints(su2double val_xcoord, su2double val_ycoord, su2double val_zcoord, unsigned short val_icornerpoints) {
+  inline void SetCoordCornerPoints(su2double val_xcoord, su2double val_ycoord, su2double val_zcoord,
+                                   unsigned short val_icornerpoints) {
     Coord_Corner_Points[val_icornerpoints][0] = val_xcoord;
     Coord_Corner_Points[val_icornerpoints][1] = val_ycoord;
     Coord_Corner_Points[val_icornerpoints][2] = val_zcoord;
   }
 
-
   /*!
    * \brief Set the coordinates of the control points.
    * \param[in] val_coord - Coordinates of the control point.
@@ -359,13 +359,13 @@ class CFreeFormDefBox : public CGridMovement {
    * \param[in] jDegree - Index of the FFDBox, j direction.
    * \param[in] kDegree - Index of the FFDBox, k direction.
    */
-  inline void SetCoordControlPoints(const su2double *val_coord, unsigned short iDegree, unsigned short jDegree, unsigned short kDegree) {
+  inline void SetCoordControlPoints(const su2double* val_coord, unsigned short iDegree, unsigned short jDegree,
+                                    unsigned short kDegree) {
     for (unsigned short iDim = 0; iDim < nDim; iDim++) {
       Coord_Control_Points[iDegree][jDegree][kDegree][iDim] = val_coord[iDim];
     }
   }
 
-
   /*!
    * \brief Set the coordinates of the control points.
    * \param[in] val_coord - Coordinates of the control point.
@@ -373,10 +373,11 @@ class CFreeFormDefBox : public CGridMovement {
    * \param[in] jDegree - Index of the FFDBox, j direction.
    * \param[in] kDegree - Index of the FFDBox, k direction.
    */
-  inline void SetCoordControlPoints_Copy(const su2double *val_coord, unsigned short iDegree, unsigned short jDegree, unsigned short kDegree) {
+  inline void SetCoordControlPoints_Copy(const su2double* val_coord, unsigned short iDegree, unsigned short jDegree,
+                                         unsigned short kDegree) {
     for (unsigned short iDim = 0; iDim < nDim; iDim++) {
-        Coord_Control_Points_Copy[iDegree][jDegree][kDegree][iDim] = val_coord[iDim];
-      }
+      Coord_Control_Points_Copy[iDegree][jDegree][kDegree][iDim] = val_coord[iDim];
+    }
   }
 
   /*!
@@ -386,9 +387,10 @@ class CFreeFormDefBox : public CGridMovement {
    * \param[in] jDegree - Index of the FFDBox, j direction.
    * \param[in] kDegree - Index of the FFDBox, k direction.
    */
-  inline void SetParCoordControlPoints(const su2double *val_coord, unsigned short iDegree, unsigned short jDegree, unsigned short kDegree) {
+  inline void SetParCoordControlPoints(const su2double* val_coord, unsigned short iDegree, unsigned short jDegree,
+                                       unsigned short kDegree) {
     for (unsigned short iDim = 0; iDim < nDim; iDim++)
-        ParCoord_Control_Points[iDegree][jDegree][kDegree][iDim] = val_coord[iDim];
+      ParCoord_Control_Points[iDegree][jDegree][kDegree][iDim] = val_coord[iDim];
   }
 
   /*!
@@ -397,14 +399,18 @@ class CFreeFormDefBox : public CGridMovement {
    * \param[in] val_icornerpoints - Index of the corner point.
    * \return Coordinate <i>val_dim</i> of the corner point <i>val_icornerpoints</i>.
    */
-  inline su2double GetCoordCornerPoints(unsigned short val_dim, unsigned short val_icornerpoints) const { return Coord_Corner_Points[val_icornerpoints][val_dim]; }
+  inline su2double GetCoordCornerPoints(unsigned short val_dim, unsigned short val_icornerpoints) const {
+    return Coord_Corner_Points[val_icornerpoints][val_dim];
+  }
 
   /*!
    * \brief Get the coordinates of the corner points.
    * \param[in] val_icornerpoints - Index of the corner point.
    * \return Pointer to the coordinate vector of the corner point <i>val_icornerpoints</i>.
    */
-  inline su2double *GetCoordCornerPoints(unsigned short val_icornerpoints) const { return Coord_Corner_Points[val_icornerpoints]; }
+  inline su2double* GetCoordCornerPoints(unsigned short val_icornerpoints) const {
+    return Coord_Corner_Points[val_icornerpoints];
+  }
 
   /*!
    * \brief Get the coordinates of the control point.
@@ -413,7 +419,10 @@ class CFreeFormDefBox : public CGridMovement {
    * \param[in] val_kindex - Value of the local k index of the control point.
    * \return Pointer to the coordinate vector of the control point with local index (i, j, k).
    */
-  inline su2double *GetCoordControlPoints(unsigned short val_iindex, unsigned short val_jindex, unsigned short val_kindex) const { return Coord_Control_Points[val_iindex][val_jindex][val_kindex]; }
+  inline su2double* GetCoordControlPoints(unsigned short val_iindex, unsigned short val_jindex,
+                                          unsigned short val_kindex) const {
+    return Coord_Control_Points[val_iindex][val_jindex][val_kindex];
+  }
 
   /*!
    * \brief Get the parametric coordinates of the control point.
@@ -422,7 +431,10 @@ class CFreeFormDefBox : public CGridMovement {
    * \param[in] val_kindex - Value of the local k index of the control point.
    * \return Pointer to the coordinate vector of the control point with local index (i, j, k).
    */
-  inline su2double *GetParCoordControlPoints(unsigned short val_iindex, unsigned short val_jindex, unsigned short val_kindex) const { return ParCoord_Control_Points[val_iindex][val_jindex][val_kindex]; }
+  inline su2double* GetParCoordControlPoints(unsigned short val_iindex, unsigned short val_jindex,
+                                             unsigned short val_kindex) const {
+    return ParCoord_Control_Points[val_iindex][val_jindex][val_kindex];
+  }
 
   /*!
    * \brief Set the control points in a parallelepiped (hexahedron).
@@ -433,14 +445,14 @@ class CFreeFormDefBox : public CGridMovement {
    * \brief Set the control points of the final chuck in a unitary hexahedron free form.
    * \param[in] FFDBox - Original FFDBox where we want to compute the control points.
    */
-  void SetSupportCP(CFreeFormDefBox *FFDBox);
+  void SetSupportCP(CFreeFormDefBox* FFDBox);
 
   /*!
    * \brief Set the new value of the coordinates of the control points.
    * \param[in] val_index - Local index (i, j, k) of the control point.
    * \param[in] movement - Movement of the control point.
    */
-  inline void SetControlPoints(const unsigned short *val_index, const su2double *movement) {
+  inline void SetControlPoints(const unsigned short* val_index, const su2double* movement) {
     for (unsigned short iDim = 0; iDim < nDim; iDim++)
       Coord_Control_Points[val_index[0]][val_index[1]][val_index[2]][iDim] += movement[iDim];
   }
@@ -453,10 +465,15 @@ class CFreeFormDefBox : public CGridMovement {
       for (unsigned short jDegree = 0; jDegree <= mDegree_Copy; jDegree++)
         for (unsigned short kDegree = 0; kDegree <= nDegree_Copy; kDegree++)
           for (unsigned short iDim = 0; iDim < nDim; iDim++)
-            Coord_Control_Points[iDegree][jDegree][kDegree][iDim] = Coord_Control_Points_Copy[iDegree][jDegree][kDegree][iDim];
-
-    lDegree = lDegree_Copy; mDegree = mDegree_Copy; nDegree = nDegree_Copy;
-    lOrder = lOrder_Copy; mOrder = mOrder_Copy; nOrder = nOrder_Copy;
+            Coord_Control_Points[iDegree][jDegree][kDegree][iDim] =
+                Coord_Control_Points_Copy[iDegree][jDegree][kDegree][iDim];
+
+    lDegree = lDegree_Copy;
+    mDegree = mDegree_Copy;
+    nDegree = nDegree_Copy;
+    lOrder = lOrder_Copy;
+    mOrder = mOrder_Copy;
+    nOrder = nOrder_Copy;
     nControlPoints = nControlPoints_Copy;
   }
 
@@ -465,69 +482,69 @@ class CFreeFormDefBox : public CGridMovement {
    * \param[in] iFFDBox - Index of the FFD box.
    * \param[in] original - Original box (before deformation).
    */
-  void SetTecplot(CGeometry *geometry, unsigned short iFFDBox, bool original);
+  void SetTecplot(CGeometry* geometry, unsigned short iFFDBox, bool original);
 
   /*!
    * \brief Set the paraview file of the FFD chuck structure.
    * \param[in] iFFDBox - Index of the FFD box.
    * \param[in] original - Original box (before deformation).
    */
-  void SetParaview(CGeometry *geometry, unsigned short iFFDBox, bool original);
+  void SetParaview(CGeometry* geometry, unsigned short iFFDBox, bool original);
 
   /*!
    * \brief Set the CGNS file of the FFD chuck structure.
    * \param[in] iFFDBox - Index of the FFD box.
    * \param[in] original - Original box (before deformation).
    */
-  void SetCGNS(CGeometry *geometry, unsigned short iFFDBox, bool original);
+  void SetCGNS(CGeometry* geometry, unsigned short iFFDBox, bool original);
 
   /*!
    * \brief Set Cylindrical to Cartesians_ControlPoints.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetCyl2Cart_ControlPoints(CConfig *config);
+  void SetCyl2Cart_ControlPoints(CConfig* config);
 
   /*!
    * \brief Set Cartesians to Cylindrical ControlPoints.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetCart2Cyl_ControlPoints(CConfig *config);
+  void SetCart2Cyl_ControlPoints(CConfig* config);
 
   /*!
    * \brief Set Cylindrical to Cartesians_CornerPoints.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetCyl2Cart_CornerPoints(CConfig *config);
+  void SetCyl2Cart_CornerPoints(CConfig* config);
 
   /*!
    * \brief Set Cartesians to Cylindrical CornerPoints.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetCart2Cyl_CornerPoints(CConfig *config);
+  void SetCart2Cyl_CornerPoints(CConfig* config);
 
   /*!
    * \brief Set Spherical to Cartesians ControlPoints.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetSphe2Cart_ControlPoints(CConfig *config);
+  void SetSphe2Cart_ControlPoints(CConfig* config);
 
   /*!
    * \brief SetCartesians to Spherical ControlPoints.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetCart2Sphe_ControlPoints(CConfig *config);
+  void SetCart2Sphe_ControlPoints(CConfig* config);
 
   /*!
    * \brief Set Spherical to Cartesians_CornerPoints.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetSphe2Cart_CornerPoints(CConfig *config);
+  void SetSphe2Cart_CornerPoints(CConfig* config);
 
   /*!
    * \brief Set Cartesians to Spherical Corner Points.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetCart2Sphe_CornerPoints(CConfig *config);
+  void SetCart2Sphe_CornerPoints(CConfig* config);
 
   /*!
    * \brief Set the cartesian coords of a point in R^3 and convert them to the parametric coords of
@@ -535,7 +552,7 @@ class CFreeFormDefBox : public CGridMovement {
    * \param[in] cart_coord - Cartesian coordinates of a point.
    * \return Pointer to the parametric coordinates of a point.
    */
-  su2double *GetParametricCoord_Analytical(const su2double *cart_coord);
+  su2double* GetParametricCoord_Analytical(const su2double* cart_coord);
 
   /*!
    * \brief Iterative strategy for computing the parametric coordinates.
@@ -545,7 +562,8 @@ class CFreeFormDefBox : public CGridMovement {
    * \param[in] it_max - Maximal number of iterations.
    * \return Parametric coordinates of the point.
    */
-  su2double *GetParametricCoord_Iterative(unsigned long iPoint, su2double *xyz, const su2double *guess, CConfig *config);
+  su2double* GetParametricCoord_Iterative(unsigned long iPoint, su2double* xyz, const su2double* guess,
+                                          CConfig* config);
 
   /*!
    * \brief Compute the cross product.
@@ -553,10 +571,10 @@ class CFreeFormDefBox : public CGridMovement {
    * \param[in] v2 - Second input vector.
    * \param[out] v3 - Output vector wuth the cross product.
    */
-  inline void CrossProduct(const su2double *v1, const su2double *v2, su2double *v3) {
-    v3[0] = v1[1]*v2[2]-v1[2]*v2[1];
-    v3[1] = v1[2]*v2[0]-v1[0]*v2[2];
-    v3[2] = v1[0]*v2[1]-v1[1]*v2[0];
+  inline void CrossProduct(const su2double* v1, const su2double* v2, su2double* v3) {
+    v3[0] = v1[1] * v2[2] - v1[2] * v2[1];
+    v3[1] = v1[2] * v2[0] - v1[0] * v2[2];
+    v3[2] = v1[0] * v2[1] - v1[1] * v2[0];
   }
 
   /*!
@@ -565,7 +583,10 @@ class CFreeFormDefBox : public CGridMovement {
    * \param[in] v2 - Sencond input vector.
    * \return Dot product between <i>v1</i>, and <i>v2</i>.
    */
-  inline su2double DotProduct(const su2double *v1, const su2double *v2) { su2double scalar = v1[0]*v2[0]+v1[1]*v2[1]+v1[2]*v2[2]; return scalar; }
+  inline su2double DotProduct(const su2double* v1, const su2double* v2) {
+    su2double scalar = v1[0] * v2[0] + v1[1] * v2[1] + v1[2] * v2[2];
+    return scalar;
+  }
 
   /*!
    * \brief Here we take the parametric coords of a point in the box and we convert them to the
@@ -573,7 +594,7 @@ class CFreeFormDefBox : public CGridMovement {
    * \param[in] ParamCoord - Parametric coordinates of a point.
    * \return Pointer to the cartesian coordinates of a point.
    */
-  su2double *EvalCartesianCoord(su2double *ParamCoord) const;
+  su2double* EvalCartesianCoord(su2double* ParamCoord) const;
 
   /*!
    * \brief Get the order in the l direction of the FFD FFDBox.
@@ -597,19 +618,28 @@ class CFreeFormDefBox : public CGridMovement {
    * \brief Get the order in the l direction of the FFD FFDBox.
    * \return Order in the l direction of the FFD FFDBox.
    */
-  inline void SetlOrder(unsigned short val_lOrder) { lOrder = val_lOrder; lDegree = lOrder-1; }
+  inline void SetlOrder(unsigned short val_lOrder) {
+    lOrder = val_lOrder;
+    lDegree = lOrder - 1;
+  }
 
   /*!
    * \brief Get the order in the m direction of the FFD FFDBox.
    * \return Order in the m direction of the FFD FFDBox.
    */
-  inline void SetmOrder(unsigned short val_mOrder) { mOrder = val_mOrder; mDegree = mOrder-1; }
+  inline void SetmOrder(unsigned short val_mOrder) {
+    mOrder = val_mOrder;
+    mDegree = mOrder - 1;
+  }
 
   /*!
    * \brief Get the order in the n direction of the FFD FFDBox.
    * \return Order in the n direction of the FFD FFDBox.
    */
-  inline void SetnOrder(unsigned short val_nOrder) { nOrder = val_nOrder; nDegree = nOrder-1;}
+  inline void SetnOrder(unsigned short val_nOrder) {
+    nOrder = val_nOrder;
+    nDegree = nOrder - 1;
+  }
 
   /*!
    * \brief Set, at each vertex, the index of the free form FFDBox that contains the vertex.
@@ -617,7 +647,7 @@ class CFreeFormDefBox : public CGridMovement {
    * \param[in] config - Definition of the particular problem.
    * \param[in] iFFDBox - Index of the FFDBox.
    */
-  bool GetPointFFD(CGeometry *geometry, CConfig *config, unsigned long iPoint) const;
+  bool GetPointFFD(CGeometry* geometry, CConfig* config, unsigned long iPoint) const;
 
   /*!
    * \brief Set the zone of the computational domain that is going to be deformed.
@@ -626,7 +656,7 @@ class CFreeFormDefBox : public CGridMovement {
    * \param[in] iFFDBox - Index of the FFDBox.
    */
   // this routine is not used. We should consider deleting it.
-  void SetDeformationZone(CGeometry *geometry, CConfig *config, unsigned short iFFDBox) const;
+  void SetDeformationZone(CGeometry* geometry, CConfig* config, unsigned short iFFDBox) const;
 
   /*!
    * \brief The routine computes the gradient of F(u, v, w) = ||X(u, v, w)-(x, y, z)||^2  evaluated at (u, v, w).
@@ -635,7 +665,7 @@ class CFreeFormDefBox : public CGridMovement {
    * \param[in] analytical - Compute the analytical gradient.
    * \return Value of the analytical gradient.
    */
-  su2double *GetFFDGradient(su2double *val_coord, su2double *xyz);
+  su2double* GetFFDGradient(su2double* val_coord, su2double* xyz);
 
   /*!
    * \brief The routine that computes the Hessian of F(u, v, w) = ||X(u, v, w)-(x, y, z)||^2 evaluated at (u, v, w)
@@ -645,35 +675,28 @@ class CFreeFormDefBox : public CGridMovement {
    * \param[in] xyz - Cartesians coordinates of the target point to compose the functional.
    * \param[in] val_Hessian - Value of the hessian.
    */
-  void GetFFDHessian(su2double *uvw, su2double *xyz, su2double **val_Hessian);
+  void GetFFDHessian(su2double* uvw, su2double* xyz, su2double** val_Hessian);
 
   /*!
    * \brief An auxiliary routine to help us compute the gradient of F(u, v, w) = ||X(u, v, w)-(x, y, z)||^2 =
    *        (Sum_ijk^lmn P1_ijk Bi Bj Bk -x)^2+(Sum_ijk^lmn P2_ijk Bi Bj Bk -y)^2+(Sum_ijk^lmn P3_ijk Bi Bj Bk -z)^2
-   *        Input: val_t, val_diff (to identify the index of the Bernstein polynomail we differentiate), the i, j, k , l, m, n
-   *        E.G.: val_diff=2 => we differentiate w.r.t. w  (val_diff=0,1, or 2) Output: d [B_i^l*B_j^m *B_k^n] / d val_diff
-   *        (val_u, val_v, val_w).
-   * \param[in] uvw - __________.
-   * \param[in] val_diff - __________.
-   * \param[in] ijk - __________.
-   * \param[in] lmn - Degree of the FFD box.
-   * \return __________.
+   *        Input: val_t, val_diff (to identify the index of the Bernstein polynomail we differentiate), the i, j, k ,
+   * l, m, n E.G.: val_diff=2 => we differentiate w.r.t. w  (val_diff=0,1, or 2) Output: d [B_i^l*B_j^m *B_k^n] / d
+   * val_diff (val_u, val_v, val_w). \param[in] uvw - __________. \param[in] val_diff - __________. \param[in] ijk -
+   * __________. \param[in] lmn - Degree of the FFD box. \return __________.
    */
-  su2double GetDerivative1(su2double *uvw, unsigned short val_diff, unsigned short *ijk, unsigned short *lmn) const;
+  su2double GetDerivative1(su2double* uvw, unsigned short val_diff, unsigned short* ijk, unsigned short* lmn) const;
 
   /*!
    * \brief An auxiliary routine to help us compute the gradient of F(u, v, w) = ||X(u, v, w)-(x, y, z)||^2 =
    *        (Sum_ijk^lmn P1_ijk Bi Bj Bk -x)^2+(Sum_ijk^lmn P2_ijk Bi Bj Bk -y)^2+(Sum_ijk^lmn P3_ijk Bi Bj Bk -z)^2
-   *        Input: (u, v, w), dim , xyz=(x, y, z), l, m, n E.G.: dim=2 => we use the third coordinate of the control points,
-   *        and the z-coordinate of xyz  (0<=dim<=2) Output: 2* ( (Sum_{i, j, k}^l, m, n P_{ijk}[dim] B_i^l[u] B_j^m[v] B_k^n[w]) -
-   *        xyz[dim]).
-   * \param[in] uvw - __________.
-   * \param[in] dim - __________.
-   * \param[in] xyz - __________.
+   *        Input: (u, v, w), dim , xyz=(x, y, z), l, m, n E.G.: dim=2 => we use the third coordinate of the control
+   * points, and the z-coordinate of xyz  (0<=dim<=2) Output: 2* ( (Sum_{i, j, k}^l, m, n P_{ijk}[dim] B_i^l[u] B_j^m[v]
+   * B_k^n[w]) - xyz[dim]). \param[in] uvw - __________. \param[in] dim - __________. \param[in] xyz - __________.
    * \param[in] lmn - Degree of the FFD box.
    * \return __________.
    */
-  su2double GetDerivative2(su2double *uvw, unsigned short dim, const su2double *xyz, const unsigned short *lmn) const;
+  su2double GetDerivative2(su2double* uvw, unsigned short dim, const su2double* xyz, const unsigned short* lmn) const;
 
   /*!
    * \brief An auxiliary routine to help us compute the gradient of F(u, v, w) = ||X(u, v, w)-(x, y, z)||^2 =
@@ -687,25 +710,20 @@ class CFreeFormDefBox : public CGridMovement {
    *        which? diff_thiss will tell us ; E.G.: dim=2, diff_this=1 => we use the third coordinate of the control
    *        points, and derivate de v-Bersntein polynomial (use m-1 when summing!!).
    */
-  su2double GetDerivative3(su2double *uvw, unsigned short dim, unsigned short diff_this,
-                           unsigned short *lmn);
+  su2double GetDerivative3(su2double* uvw, unsigned short dim, unsigned short diff_this, unsigned short* lmn);
 
   /*!
    * \brief An auxiliary routine to help us compute the Hessian of F(u, v, w) = ||X(u, v, w)-(x, y, z)||^2 =
    *        (Sum_ijk^lmn P1_ijk Bi Bj Bk -x)^2+(Sum_ijk^lmn P2_ijk Bi Bj Bk -y)+(Sum_ijk^lmn P3_ijk Bi Bj Bk -z)
-   *        Input: val_t, val_diff, val_diff2 (to identify the index of the Bernstein polynomials we differentiate), the i, j, k , l, m, n
-   *        E.G.: val_diff=1, val_diff2=2  =>  we differentiate w.r.t. v and w  (val_diff=0,1, or 2)
-   *        E.G.: val_diff=0, val_diff2=0 => we differentiate w.r.t. u two times
-   *        Output: [d [B_i^l*B_j^m *B_k^n]/d val_diff *d [B_i^l*B_j^m *B_k^n]/d val_diff2] (val_u, val_v, val_w) .
-   * \param[in] uvw - __________.
-   * \param[in] val_diff - __________.
-   * \param[in] val_diff2 - __________.
-   * \param[in] ijk - __________.
-   * \param[in] lmn - Degree of the FFD box.
+   *        Input: val_t, val_diff, val_diff2 (to identify the index of the Bernstein polynomials we differentiate), the
+   * i, j, k , l, m, n E.G.: val_diff=1, val_diff2=2  =>  we differentiate w.r.t. v and w  (val_diff=0,1, or 2) E.G.:
+   * val_diff=0, val_diff2=0 => we differentiate w.r.t. u two times Output: [d [B_i^l*B_j^m *B_k^n]/d val_diff *d
+   * [B_i^l*B_j^m *B_k^n]/d val_diff2] (val_u, val_v, val_w) . \param[in] uvw - __________. \param[in] val_diff -
+   * __________. \param[in] val_diff2 - __________. \param[in] ijk - __________. \param[in] lmn - Degree of the FFD box.
    * \return __________.
    */
-  su2double GetDerivative4(su2double *uvw, unsigned short val_diff, unsigned short val_diff2,
-                           unsigned short *ijk, unsigned short *lmn) const;
+  su2double GetDerivative4(su2double* uvw, unsigned short val_diff, unsigned short val_diff2, unsigned short* ijk,
+                           unsigned short* lmn) const;
 
   /*!
    * \brief An auxiliary routine to help us compute the Hessian of F(u, v, w) = ||X(u, v, w)-(x, y, z)||^2 =
@@ -723,15 +741,18 @@ class CFreeFormDefBox : public CGridMovement {
    * \param[in] lmn - Degree of the FFD box.
    * \return __________.
    */
-  su2double GetDerivative5(su2double *uvw, unsigned short dim, unsigned short diff_this, unsigned short diff_this_also,
-                           unsigned short *lmn);
+  su2double GetDerivative5(su2double* uvw, unsigned short dim, unsigned short diff_this, unsigned short diff_this_also,
+                           unsigned short* lmn);
 
   /*!
    * \brief Euclidean norm of a vector.
    * \param[in] a - _______.
    * \return __________.
    */
-  inline su2double GetNorm(const su2double *a) { su2double  norm = sqrt(a[0]*a[0] + a[1]*a[1]+ a[2]*a[2]); return norm; }
+  inline su2double GetNorm(const su2double* a) {
+    su2double norm = sqrt(a[0] * a[0] + a[1] * a[1] + a[2] * a[2]);
+    return norm;
+  }
 
   /*!
    * \brief Set the tag that identify a FFDBox.
@@ -756,5 +777,4 @@ class CFreeFormDefBox : public CGridMovement {
    * \return Value of the nested level of the the FFDBox.
    */
   inline unsigned short GetLevel() const { return Level; }
-
 };
diff --git a/Common/include/grid_movement/CGridMovement.hpp b/Common/include/grid_movement/CGridMovement.hpp
index a382b58fd0f..e167dd58133 100644
--- a/Common/include/grid_movement/CGridMovement.hpp
+++ b/Common/include/grid_movement/CGridMovement.hpp
@@ -37,13 +37,11 @@
  * \author F. Palacios
  */
 class CGridMovement {
+ protected:
+  int rank, /*!< \brief MPI Rank. */
+      size; /*!< \brief MPI Size. */
 
-protected:
-  int rank,  /*!< \brief MPI Rank. */
-  size;      /*!< \brief MPI Size. */
-
-public:
-
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -60,7 +58,7 @@ class CGridMovement {
    * \param[in] config - Definition of the particular problem.
    * \return Total deformation applied, which may be less than target if intersection prevention is used.
    */
-  inline virtual vector<vector<su2double> > SetSurface_Deformation(CGeometry *geometry, CConfig *config) {
+  inline virtual vector<vector<su2double> > SetSurface_Deformation(CGeometry* geometry, CConfig* config) {
     return vector<vector<su2double> >();
   }
 };
diff --git a/Common/include/grid_movement/CSurfaceMovement.hpp b/Common/include/grid_movement/CSurfaceMovement.hpp
index 564071e9338..28eca93c343 100644
--- a/Common/include/grid_movement/CSurfaceMovement.hpp
+++ b/Common/include/grid_movement/CSurfaceMovement.hpp
@@ -36,13 +36,13 @@
  * \author F. Palacios, T. Economon.
  */
 class CSurfaceMovement : public CGridMovement {
-protected:
+ protected:
   CFreeFormDefBox** FFDBox; /*!< \brief Definition of the Free Form Deformation Box. */
-  unsigned short nFFDBox; /*!< \brief Number of FFD FFDBoxes. */
-  unsigned short nLevel;  /*!< \brief Level of the FFD FFDBoxes (parent/child). */
-  bool FFDBoxDefinition;  /*!< \brief If the FFD FFDBox has been defined in the input file. */
+  unsigned short nFFDBox;   /*!< \brief Number of FFD FFDBoxes. */
+  unsigned short nLevel;    /*!< \brief Level of the FFD FFDBoxes (parent/child). */
+  bool FFDBoxDefinition;    /*!< \brief If the FFD FFDBox has been defined in the input file. */
 
-public:
+ public:
   vector<su2double> GlobalCoordX[MAX_NUMBER_FFD];
   vector<su2double> GlobalCoordY[MAX_NUMBER_FFD];
   vector<su2double> GlobalCoordZ[MAX_NUMBER_FFD];
@@ -66,7 +66,7 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iDV - Index of the design variable.
    * \param[in] ResetDef - Reset the deformation before starting a new one.
    */
-  void SetHicksHenne(CGeometry *boundary, CConfig *config, unsigned short iDV, bool ResetDef);
+  void SetHicksHenne(CGeometry* boundary, CConfig* config, unsigned short iDV, bool ResetDef);
 
   /*!
    * \brief Set a Hicks-Henne deformation bump functions on an airfoil.
@@ -75,7 +75,7 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iDV - Index of the design variable.
    * \param[in] ResetDef - Reset the deformation before starting a new one.
    */
-  void SetSurface_Bump(CGeometry *boundary, CConfig *config, unsigned short iDV, bool ResetDef);
+  void SetSurface_Bump(CGeometry* boundary, CConfig* config, unsigned short iDV, bool ResetDef);
 
   /*!
    * \brief Set a Hicks-Henne deformation bump functions on an airfoil.
@@ -84,7 +84,7 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iDV - Index of the design variable.
    * \param[in] ResetDef - Reset the deformation before starting a new one.
    */
-  void SetAngleOfAttack(CGeometry *boundary, CConfig *config, unsigned short iDV, bool ResetDef);
+  void SetAngleOfAttack(CGeometry* boundary, CConfig* config, unsigned short iDV, bool ResetDef);
 
   /*!
    * \brief Set a deformation based on a change in the Kulfan parameters for an airfoil.
@@ -93,28 +93,28 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iDV - Index of the design variable.
    * \param[in] ResetDef - Reset the deformation before starting a new one.
    */
-  void SetCST(CGeometry *boundary, CConfig *config, unsigned short iDV, bool ResetDef);
+  void SetCST(CGeometry* boundary, CConfig* config, unsigned short iDV, bool ResetDef);
 
   /*!
    * \brief Set a NACA 4 digits airfoil family for airfoil deformation.
    * \param[in] boundary - Geometry of the boundary.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetNACA_4Digits(CGeometry *boundary, CConfig *config);
+  void SetNACA_4Digits(CGeometry* boundary, CConfig* config);
 
   /*!
    * \brief Set a parabolic family for airfoil deformation.
    * \param[in] boundary - Geometry of the boundary.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetParabolic(CGeometry *boundary, CConfig *config);
+  void SetParabolic(CGeometry* boundary, CConfig* config);
 
   /*!
    * \brief Set a obstacle in a channel.
    * \param[in] boundary - Geometry of the boundary.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetAirfoil(CGeometry *boundary, CConfig *config);
+  void SetAirfoil(CGeometry* boundary, CConfig* config);
 
   /*!
    * \brief Set a rotation for surface movement.
@@ -123,7 +123,7 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iDV - Index of the design variable.
    * \param[in] ResetDef - Reset the deformation before starting a new one.
    */
-  void SetRotation(CGeometry *boundary, CConfig *config, unsigned short iDV, bool ResetDef);
+  void SetRotation(CGeometry* boundary, CConfig* config, unsigned short iDV, bool ResetDef);
 
   /*!
    * \brief Computes the displacement of a rotating surface for a dynamic mesh simulation.
@@ -132,8 +132,7 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iter - Current physical time iteration.
    * \param[in] iZone - Zone number in the mesh.
    */
-  void HTP_Rotation(CGeometry *geometry, CConfig *config,
-                    unsigned long iter, unsigned short iZone);
+  void HTP_Rotation(CGeometry* geometry, CConfig* config, unsigned long iter, unsigned short iZone);
 
   /*!
    * \brief Unsteady aeroelastic grid movement by deforming the mesh.
@@ -144,7 +143,8 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iMarker_Monitoring - Marker we are monitoring.
    * \param[in] displacements - solution of typical section wing model.
    */
-  void AeroelasticDeform(CGeometry *geometry, CConfig *config, unsigned long TimeIter, unsigned short iMarker, unsigned short iMarker_Monitoring, vector<su2double>& displacements);
+  void AeroelasticDeform(CGeometry* geometry, CConfig* config, unsigned long TimeIter, unsigned short iMarker,
+                         unsigned short iMarker_Monitoring, vector<su2double>& displacements);
 
   /*!
    * \brief Deforms a 3-D flutter/pitching surface during an unsteady simulation.
@@ -153,15 +153,15 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iter - Current physical time iteration.
    * \param[in] iZone - Zone number in the mesh.
    */
-  void SetBoundary_Flutter3D(CGeometry *geometry, CConfig *config,
-                             CFreeFormDefBox **FFDBox, unsigned long iter, unsigned short iZone);
+  void SetBoundary_Flutter3D(CGeometry* geometry, CConfig* config, CFreeFormDefBox** FFDBox, unsigned long iter,
+                             unsigned short iZone);
 
   /*!
    * \brief Set the collective pitch for a blade surface movement.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetCollective_Pitch(CGeometry *geometry, CConfig *config);
+  void SetCollective_Pitch(CGeometry* geometry, CConfig* config);
 
   /*!
    * \brief Set any surface deformationsbased on an input file.
@@ -170,7 +170,7 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iZone - Zone number in the mesh.
    * \param[in] iter - Current physical time iteration.
    */
-  void SetExternal_Deformation(CGeometry *geometry, CConfig *config, unsigned short iZone, unsigned long iter);
+  void SetExternal_Deformation(CGeometry* geometry, CConfig* config, unsigned short iZone, unsigned long iter);
 
   /*!
    * \brief Set a displacement for surface movement.
@@ -179,7 +179,7 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iDV - Index of the design variable.
    * \param[in] ResetDef - Reset the deformation before starting a new one.
    */
-  void SetTranslation(CGeometry *boundary, CConfig *config, unsigned short iDV, bool ResetDef);
+  void SetTranslation(CGeometry* boundary, CConfig* config, unsigned short iDV, bool ResetDef);
 
   /*!
    * \brief Set a displacement for surface movement.
@@ -188,14 +188,14 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iDV - Index of the design variable.
    * \param[in] ResetDef - Reset the deformation before starting a new one.
    */
-  void SetScale(CGeometry *boundary, CConfig *config, unsigned short iDV, bool ResetDef);
+  void SetScale(CGeometry* boundary, CConfig* config, unsigned short iDV, bool ResetDef);
 
   /*!
    * \brief Copy the boundary coordinates to each vertex.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void CopyBoundary(CGeometry *geometry, CConfig *config);
+  void CopyBoundary(CGeometry* geometry, CConfig* config);
 
   /*!
    * \brief Set the surface/boundary deformation.
@@ -203,7 +203,7 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] config - Definition of the particular problem.
    * \return Total deformation applied, which may be less than target if intersection prevention is used.
    */
-  vector<vector<su2double> > SetSurface_Deformation(CGeometry *geometry, CConfig *config) override;
+  vector<vector<su2double> > SetSurface_Deformation(CGeometry* geometry, CConfig* config) override;
 
   /*!
    * \brief Compute the parametric coordinates of a grid point using a point inversion strategy
@@ -212,7 +212,7 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] config - Definition of the particular problem.
    * \param[in] FFDBox - Array with all the free forms FFDBoxes of the computation.
    */
-  void SetParametricCoord(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, unsigned short iFFDBox);
+  void SetParametricCoord(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox, unsigned short iFFDBox);
 
   /*!
    * \brief Update the parametric coordinates of a grid point using a point inversion strategy
@@ -222,7 +222,7 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] FFDBox - Array with all the free forms FFDBoxes of the computation.
    * \param[in] iFFDBox - Index of FFD box.
    */
-  void UpdateParametricCoord(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, unsigned short iFFDBox);
+  void UpdateParametricCoord(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox, unsigned short iFFDBox);
 
   /*!
    * \brief Check the intersections of the FFD with the surface
@@ -231,7 +231,7 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] FFDBox - Array with all the free forms FFDBoxes of the computation.
    * \param[in] iFFDBox - Index of FFD box.
    */
-  void CheckFFDIntersections(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, unsigned short iFFDBox);
+  void CheckFFDIntersections(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox, unsigned short iFFDBox);
 
   /*!
    * \brief Check the intersections of the FFD with the surface
@@ -240,7 +240,7 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] FFDBox - Array with all the free forms FFDBoxes of the computation.
    * \param[in] iFFDBox - Index of FFD box.
    */
-  void CheckFFDDimension(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, unsigned short iFFDBox);
+  void CheckFFDDimension(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox, unsigned short iFFDBox);
 
   /*!
    * \brief Set the Parametric coordinates.
@@ -249,7 +249,8 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] FFDBoxParent - Array with parent FFDBoxes of the computation.
    * \param[in] FFDBoxChild - Array with child FFDBoxes of the computation.
    */
-  void SetParametricCoordCP(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBoxParent, CFreeFormDefBox *FFDBoxChild);
+  void SetParametricCoordCP(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBoxParent,
+                            CFreeFormDefBox* FFDBoxChild);
 
   /*!
    * \brief Get the cartes.
@@ -258,7 +259,8 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] FFDBoxParent - Array with parent FFDBoxes of the computation.
    * \param[in] FFDBoxChild - Array with child FFDBoxes of the computation.
    */
-  void GetCartesianCoordCP(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBoxParent, CFreeFormDefBox *FFDBoxChild);
+  void GetCartesianCoordCP(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBoxParent,
+                           CFreeFormDefBox* FFDBoxChild);
 
   /*!
    * \brief Apply the design variables to the control point position
@@ -267,7 +269,7 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] FFDBox - Array with all the free forms FFDBoxes of the computation.
    * \param[in] iFFDBox - Index of FFD box.
    */
-  void ApplyDesignVariables(CGeometry *geometry, CConfig *config, CFreeFormDefBox **FFDBox, unsigned short iFFDBox);
+  void ApplyDesignVariables(CGeometry* geometry, CConfig* config, CFreeFormDefBox** FFDBox, unsigned short iFFDBox);
 
   /*!
    * \brief Recompute the cartesian coordinates using the control points position.
@@ -276,7 +278,8 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] FFDBox - Array with all the free forms FFDBoxes of the computation.
    * \param[in] iFFDBox - Index of FFD box.
    */
-  su2double SetCartesianCoord(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, unsigned short iFFDBox, bool ResetDef);
+  su2double SetCartesianCoord(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox, unsigned short iFFDBox,
+                              bool ResetDef);
 
   /*!
    * \brief Set the deformation of the Free From box using the control point position.
@@ -286,7 +289,8 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iDV - Index of the design variable.
    * \param[in] ResetDef - Reset the deformation before starting a new one.
    */
-  bool SetFFDCPChange_2D(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox, unsigned short iDV, bool ResetDef) const;
+  bool SetFFDCPChange_2D(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox, CFreeFormDefBox** ResetFFDBox,
+                         unsigned short iDV, bool ResetDef) const;
 
   /*!
    * \brief Set the deformation of the Free From box using the control point position.
@@ -296,7 +300,8 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iDV - Index of the design variable.
    * \param[in] ResetDef - Reset the deformation before starting a new one.
    */
-  bool SetFFDCPChange(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox, unsigned short iDV, bool ResetDef) const;
+  bool SetFFDCPChange(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox, CFreeFormDefBox** ResetFFDBox,
+                      unsigned short iDV, bool ResetDef) const;
 
   /*!
    * \brief Set the deformation of the Free From box using the control point position.
@@ -306,7 +311,8 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iDV - Index of the design variable.
    * \param[in] ResetDef - Reset the deformation before starting a new one.
    */
-  bool SetFFDGull(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox, unsigned short iDV, bool ResetDef) const;
+  bool SetFFDGull(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox, CFreeFormDefBox** ResetFFDBox,
+                  unsigned short iDV, bool ResetDef) const;
 
   /*!
    * \brief Set the deformation of the Free From box using the control point position.
@@ -316,7 +322,8 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iDV - Index of the design variable.
    * \param[in] ResetDef - Reset the deformation before starting a new one.
    */
-  bool SetFFDNacelle(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox, unsigned short iDV, bool ResetDef) const;
+  bool SetFFDNacelle(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox, CFreeFormDefBox** ResetFFDBox,
+                     unsigned short iDV, bool ResetDef) const;
 
   /*!
    * \brief Set a camber deformation of the Free From box using the control point position.
@@ -326,7 +333,8 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iDV - Index of the design variable.
    * \param[in] ResetDef - Reset the deformation before starting a new one.
    */
-  bool SetFFDCamber_2D(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox, unsigned short iDV, bool ResetDef) const;
+  bool SetFFDCamber_2D(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox, CFreeFormDefBox** ResetFFDBox,
+                       unsigned short iDV, bool ResetDef) const;
 
   /*!
    * \brief Set a camber deformation of the Free From box using the control point position.
@@ -336,7 +344,8 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iDV - Index of the design variable.
    * \param[in] ResetDef - Reset the deformation before starting a new one.
    */
-  bool SetFFDTwist_2D(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox, unsigned short iDV, bool ResetDef);
+  bool SetFFDTwist_2D(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox, CFreeFormDefBox** ResetFFDBox,
+                      unsigned short iDV, bool ResetDef);
 
   /*!
    * \brief Set a thickness deformation of the Free From box using the control point position.
@@ -346,7 +355,8 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iDV - Index of the design variable.
    * \param[in] ResetDef - Reset the deformation before starting a new one.
    */
-  bool SetFFDThickness_2D(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox, unsigned short iDV, bool ResetDef) const;
+  bool SetFFDThickness_2D(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox, CFreeFormDefBox** ResetFFDBox,
+                          unsigned short iDV, bool ResetDef) const;
 
   /*!
    * \brief Set a camber deformation of the Free From box using the control point position.
@@ -356,7 +366,8 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iDV - Index of the design variable.
    * \param[in] ResetDef - Reset the deformation before starting a new one.
    */
-  bool SetFFDCamber(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox, unsigned short iDV, bool ResetDef) const;
+  bool SetFFDCamber(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox, CFreeFormDefBox** ResetFFDBox,
+                    unsigned short iDV, bool ResetDef) const;
 
   /*!
    * \brief Set a thickness deformation of the Free From box using the control point position.
@@ -366,7 +377,8 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iDV - Index of the design variable.
    * \param[in] ResetDef - Reset the deformation before starting a new one.
    */
-  bool SetFFDThickness(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox, unsigned short iDV, bool ResetDef) const;
+  bool SetFFDThickness(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox, CFreeFormDefBox** ResetFFDBox,
+                       unsigned short iDV, bool ResetDef) const;
 
   /*!
    * \brief Set a thickness deformation of the Free From box using the control point position.
@@ -376,7 +388,8 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iDV - Index of the design variable.
    * \param[in] ResetDef - Reset the deformation before starting a new one.
    */
-  void SetFFDAngleOfAttack(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox, unsigned short iDV, bool ResetDef);
+  void SetFFDAngleOfAttack(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox, CFreeFormDefBox** ResetFFDBox,
+                           unsigned short iDV, bool ResetDef);
 
   /*!
    * \brief Set a twist angle deformation of the Free From box using the control point position.
@@ -386,7 +399,8 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iDV - Index of the design variable.
    * \param[in] ResetDef - Reset the deformation before starting a new one.
    */
-  bool SetFFDTwist(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox, unsigned short iDV, bool ResetDef) const;
+  bool SetFFDTwist(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox, CFreeFormDefBox** ResetFFDBox,
+                   unsigned short iDV, bool ResetDef) const;
 
   /*!
    * \brief Set a rotation angle deformation of the Free From box using the control point position.
@@ -396,7 +410,8 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iDV - Index of the design variable.
    * \param[in] ResetDef - Reset the deformation before starting a new one.
    */
-  bool SetFFDRotation(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox,CFreeFormDefBox **ResetFFDBox, unsigned short iDV, bool ResetDef) const;
+  bool SetFFDRotation(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox, CFreeFormDefBox** ResetFFDBox,
+                      unsigned short iDV, bool ResetDef) const;
 
   /*!
    * \brief Set a rotation angle deformation in a control surface of the Free From box using the control point position.
@@ -406,7 +421,8 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] iDV - Index of the design variable.
    * \param[in] ResetDef - Reset the deformation before starting a new one.
    */
-  bool SetFFDControl_Surface(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox, unsigned short iDV, bool ResetDef) const;
+  bool SetFFDControl_Surface(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox,
+                             CFreeFormDefBox** ResetFFDBox, unsigned short iDV, bool ResetDef) const;
 
   /*!
    * \brief Read the free form information from the grid input file.
@@ -417,7 +433,7 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] FFDBox - Array with all the free forms FFDBoxes of the computation.
    * \param[in] val_mesh_filename - Name of the grid input file.
    */
-  void ReadFFDInfo(CGeometry *geometry, CConfig *config, CFreeFormDefBox **FFDBox, string val_mesh_filename);
+  void ReadFFDInfo(CGeometry* geometry, CConfig* config, CFreeFormDefBox** FFDBox, string val_mesh_filename);
 
   /*!
    * \brief Read the free form information from the grid input file.
@@ -427,7 +443,7 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] FFDBox - Array with all the free forms FFDBoxes of the computation.
    */
-  void ReadFFDInfo(CGeometry *geometry, CConfig *config, CFreeFormDefBox **FFDBox);
+  void ReadFFDInfo(CGeometry* geometry, CConfig* config, CFreeFormDefBox** FFDBox);
 
   /*!
    * \brief Merge the Free Form information in the SU2 file.
@@ -435,7 +451,7 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] val_mesh_filename - Name of the grid output file.
    */
-  void MergeFFDInfo(CGeometry *geometry, CConfig *config);
+  void MergeFFDInfo(CGeometry* geometry, CConfig* config);
 
   /*!
    * \brief Write the Free Form information in the SU2 file.
@@ -443,7 +459,7 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] val_mesh_filename - Name of the grid output file.
    */
-  void WriteFFDInfo(CSurfaceMovement **surface_movement, CGeometry ****geometry, CConfig **config);
+  void WriteFFDInfo(CSurfaceMovement** surface_movement, CGeometry**** geometry, CConfig** config);
 
   /*!
    * \brief Get information about if there is a complete FFDBox definition, or it is necessary to
@@ -459,14 +475,15 @@ class CSurfaceMovement : public CGridMovement {
    * \return <code>TRUE</code> if the FFD box name referenced with DV_PARAM can be found in the FFD box definition;
    * otherwise <code>FALSE</code>.
    */
-  inline bool CheckFFDBoxDefinition(CConfig *config, unsigned short iDV) {
+  inline bool CheckFFDBoxDefinition(CConfig* config, unsigned short iDV) {
     for (unsigned short iFFDBox = 0; iFFDBox < GetnFFDBox(); iFFDBox++) {
-      if (FFDBox[iFFDBox]->GetTag() == config->GetFFDTag(iDV)) { return true;}
+      if (FFDBox[iFFDBox]->GetTag() == config->GetFFDTag(iDV)) {
+        return true;
+      }
     }
     return false;
   }
 
-
   /*!
    * \brief Obtain the number of FFDBoxes.
    * \return Number of FFD FFDBoxes.
@@ -484,7 +501,7 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetSurface_Derivative(CGeometry *geometry, CConfig *config);
+  void SetSurface_Derivative(CGeometry* geometry, CConfig* config);
 
   /*!
    * \brief Calculate the determinant of the Jacobian matrix for the FFD problem.
@@ -493,5 +510,5 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] FFDBox - Free form deformation box.
    * \return Number of points with negative Jacobian determinant.
    */
-  unsigned long calculateJacobianDeterminant(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox) const;
+  unsigned long calculateJacobianDeterminant(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox) const;
 };
diff --git a/Common/include/grid_movement/CVolumetricMovement.hpp b/Common/include/grid_movement/CVolumetricMovement.hpp
index 0a1503f6402..489f330d792 100644
--- a/Common/include/grid_movement/CVolumetricMovement.hpp
+++ b/Common/include/grid_movement/CVolumetricMovement.hpp
@@ -38,28 +38,26 @@
  * \author F. Palacios, A. Bueno, T. Economon, S. Padron.
  */
 class CVolumetricMovement : public CGridMovement {
-protected:
+ protected:
+  unsigned short nDim; /*!< \brief Number of dimensions. */
+  unsigned short nVar; /*!< \brief Number of variables. */
 
-  unsigned short nDim;    /*!< \brief Number of dimensions. */
-  unsigned short nVar;    /*!< \brief Number of variables. */
+  unsigned long nPoint;       /*!< \brief Number of points. */
+  unsigned long nPointDomain; /*!< \brief Number of points in the domain. */
 
-  unsigned long nPoint;        /*!< \brief Number of points. */
-  unsigned long nPointDomain;  /*!< \brief Number of points in the domain. */
-
-  unsigned long nIterMesh;  /*!< \brief Number of iterations in the mesh update. +*/
+  unsigned long nIterMesh; /*!< \brief Number of iterations in the mesh update. +*/
 
 #ifndef CODI_FORWARD_TYPE
   CSysMatrix<su2mixedfloat> StiffMatrix; /*!< \brief Stiffness matrix of the elasticity problem. */
-  CSysSolve<su2mixedfloat>  System;      /*!< \brief Linear solver/smoother. */
+  CSysSolve<su2mixedfloat> System;       /*!< \brief Linear solver/smoother. */
 #else
   CSysMatrix<su2double> StiffMatrix;
-  CSysSolve<su2double>  System;
+  CSysSolve<su2double> System;
 #endif
   CSysVector<su2double> LinSysSol;
   CSysVector<su2double> LinSysRes;
 
-public:
-
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -68,7 +66,7 @@ class CVolumetricMovement : public CGridMovement {
   /*!
    * \brief Constructor of the class.
    */
-  CVolumetricMovement(CGeometry *geometry, CConfig *config);
+  CVolumetricMovement(CGeometry* geometry, CConfig* config);
 
   /*!
    * \brief Destructor of the class.
@@ -80,21 +78,21 @@ class CVolumetricMovement : public CGridMovement {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void UpdateGridCoord(CGeometry *geometry, CConfig *config);
+  void UpdateGridCoord(CGeometry* geometry, CConfig* config);
 
   /*!
    * \brief Update the dual grid after the grid movement (edges and control volumes).
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void UpdateDualGrid(CGeometry *geometry, CConfig *config);
+  void UpdateDualGrid(CGeometry* geometry, CConfig* config);
 
   /*!
    * \brief Update the coarse multigrid levels after the grid movement.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void UpdateMultiGrid(CGeometry **geometry, CConfig *config);
+  void UpdateMultiGrid(CGeometry** geometry, CConfig* config);
 
   /*!
    * \brief Compute the stiffness matrix for grid deformation using spring analogy.
@@ -102,7 +100,7 @@ class CVolumetricMovement : public CGridMovement {
    * \param[in] config - Definition of the particular problem.
    * \return Value of the length of the smallest edge of the grid.
    */
-  su2double SetFEAMethodContributions_Elem(CGeometry *geometry, CConfig *config);
+  su2double SetFEAMethodContributions_Elem(CGeometry* geometry, CConfig* config);
 
   /*!
    * \brief Build the stiffness matrix for a 3-D hexahedron element. The result will be placed in StiffMatrix_Elem.
@@ -114,8 +112,9 @@ class CVolumetricMovement : public CGridMovement {
    * \param[in] nNodes - Number of nodes defining the element.
    * \param[in] scale
    */
-  void SetFEA_StiffMatrix3D(CGeometry *geometry, CConfig *config, su2double **StiffMatrix_Elem, unsigned long PointCorners[8], su2double CoordCorners[8][3],
-  unsigned short nNodes, su2double ElemVolume, su2double ElemDistance);
+  void SetFEA_StiffMatrix3D(CGeometry* geometry, CConfig* config, su2double** StiffMatrix_Elem,
+                            unsigned long PointCorners[8], su2double CoordCorners[8][3], unsigned short nNodes,
+                            su2double ElemVolume, su2double ElemDistance);
 
   /*!
    * \brief Build the stiffness matrix for a 3-D hexahedron element. The result will be placed in StiffMatrix_Elem.
@@ -127,8 +126,9 @@ class CVolumetricMovement : public CGridMovement {
    * \param[in] nNodes - Number of nodes defining the element.
    * \param[in] scale
    */
-  void SetFEA_StiffMatrix2D(CGeometry *geometry, CConfig *config, su2double **StiffMatrix_Elem, unsigned long PointCorners[8], su2double CoordCorners[8][3],
-  unsigned short nNodes, su2double ElemVolume, su2double ElemDistance);
+  void SetFEA_StiffMatrix2D(CGeometry* geometry, CConfig* config, su2double** StiffMatrix_Elem,
+                            unsigned long PointCorners[8], su2double CoordCorners[8][3], unsigned short nNodes,
+                            su2double ElemVolume, su2double ElemDistance);
 
   /*!
    * \brief Shape functions and derivative of the shape functions
@@ -138,7 +138,8 @@ class CVolumetricMovement : public CGridMovement {
    * \param[in] CoordCorners - Coordiantes of the corners.
    * \param[in] DShapeFunction - Shape function information
    */
-  su2double ShapeFunc_Hexa(su2double Xi, su2double Eta, su2double Zeta, su2double CoordCorners[8][3], su2double DShapeFunction[8][4]);
+  su2double ShapeFunc_Hexa(su2double Xi, su2double Eta, su2double Zeta, su2double CoordCorners[8][3],
+                           su2double DShapeFunction[8][4]);
 
   /*!
    * \brief Shape functions and derivative of the shape functions
@@ -148,7 +149,8 @@ class CVolumetricMovement : public CGridMovement {
    * \param[in] CoordCorners - Coordiantes of the corners.
    * \param[in] DShapeFunction - Shape function information
    */
-  su2double ShapeFunc_Tetra(su2double Xi, su2double Eta, su2double Zeta, su2double CoordCorners[8][3], su2double DShapeFunction[8][4]);
+  su2double ShapeFunc_Tetra(su2double Xi, su2double Eta, su2double Zeta, su2double CoordCorners[8][3],
+                            su2double DShapeFunction[8][4]);
 
   /*!
    * \brief Shape functions and derivative of the shape functions
@@ -158,7 +160,8 @@ class CVolumetricMovement : public CGridMovement {
    * \param[in] CoordCorners - Coordiantes of the corners.
    * \param[in] DShapeFunction - Shape function information
    */
-  su2double ShapeFunc_Pyram(su2double Xi, su2double Eta, su2double Zeta, su2double CoordCorners[8][3], su2double DShapeFunction[8][4]);
+  su2double ShapeFunc_Pyram(su2double Xi, su2double Eta, su2double Zeta, su2double CoordCorners[8][3],
+                            su2double DShapeFunction[8][4]);
 
   /*!
    * \brief Shape functions and derivative of the shape functions
@@ -168,7 +171,8 @@ class CVolumetricMovement : public CGridMovement {
    * \param[in] CoordCorners - Coordiantes of the corners.
    * \param[in] DShapeFunction - Shape function information
    */
-  su2double ShapeFunc_Prism(su2double Xi, su2double Eta, su2double Zeta, su2double CoordCorners[8][3], su2double DShapeFunction[8][4]);
+  su2double ShapeFunc_Prism(su2double Xi, su2double Eta, su2double Zeta, su2double CoordCorners[8][3],
+                            su2double DShapeFunction[8][4]);
 
   /*!
    * \brief Shape functions and derivative of the shape functions
@@ -177,7 +181,8 @@ class CVolumetricMovement : public CGridMovement {
    * \param[in] CoordCorners - Coordiantes of the corners.
    * \param[in] DShapeFunction - Shape function information
    */
-  su2double ShapeFunc_Triangle(su2double Xi, su2double Eta, su2double CoordCorners[8][3], su2double DShapeFunction[8][4]);
+  su2double ShapeFunc_Triangle(su2double Xi, su2double Eta, su2double CoordCorners[8][3],
+                               su2double DShapeFunction[8][4]);
 
   /*!
    * \brief Shape functions and derivative of the shape functions
@@ -186,7 +191,8 @@ class CVolumetricMovement : public CGridMovement {
    * \param[in] CoordCorners - Coordiantes of the corners.
    * \param[in] DShapeFunction - Shape function information
    */
-  su2double ShapeFunc_Quadrilateral(su2double Xi, su2double Eta, su2double CoordCorners[8][3], su2double DShapeFunction[8][4]);
+  su2double ShapeFunc_Quadrilateral(su2double Xi, su2double Eta, su2double CoordCorners[8][3],
+                                    su2double DShapeFunction[8][4]);
 
   /*!
    * \brief Compute the shape functions for hexahedron
@@ -225,49 +231,50 @@ class CVolumetricMovement : public CGridMovement {
   su2double GetQuadrilateral_Area(su2double CoordCorners[8][3]) const;
 
   /*!
-   * \brief Add the stiffness matrix for a 2-D triangular element to the global stiffness matrix for the entire mesh (node-based).
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] StiffMatrix_Elem - Element stiffness matrix to be filled.
-   * \param[in] PointCorners - Index values for element corners
-   * \param[in] nNodes - Number of nodes defining the element.
+   * \brief Add the stiffness matrix for a 2-D triangular element to the global stiffness matrix for the entire mesh
+   * (node-based). \param[in] geometry - Geometrical definition of the problem. \param[in] StiffMatrix_Elem - Element
+   * stiffness matrix to be filled. \param[in] PointCorners - Index values for element corners \param[in] nNodes -
+   * Number of nodes defining the element.
    */
-  void AddFEA_StiffMatrix(CGeometry *geometry, su2double **StiffMatrix_Elem, unsigned long PointCorners[8], unsigned short nNodes);
+  void AddFEA_StiffMatrix(CGeometry* geometry, su2double** StiffMatrix_Elem, unsigned long PointCorners[8],
+                          unsigned short nNodes);
 
   /*!
    * \brief Check for negative volumes (all elements) after performing grid deformation.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] Screen_Output - determines if text is written to screen
    */
-  void ComputeDeforming_Element_Volume(CGeometry *geometry, su2double &MinVolume, su2double &MaxVolume, bool Screen_Output);
+  void ComputeDeforming_Element_Volume(CGeometry* geometry, su2double& MinVolume, su2double& MaxVolume,
+                                       bool Screen_Output);
 
   /*!
    * \brief Compute amount of nonconvex elements
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] Screen_Output - determines if text is written to screen
    */
-  void ComputenNonconvexElements(CGeometry *geometry, bool Screen_Output);
-
+  void ComputenNonconvexElements(CGeometry* geometry, bool Screen_Output);
 
   /*!
    * \brief Compute the minimum distance to the nearest solid surface.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void ComputeSolid_Wall_Distance(CGeometry *geometry, CConfig *config, su2double &MinDistance, su2double &MaxDistance) const;
+  void ComputeSolid_Wall_Distance(CGeometry* geometry, CConfig* config, su2double& MinDistance,
+                                  su2double& MaxDistance) const;
 
   /*!
    * \brief Check the boundary vertex that are going to be moved.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetBoundaryDisplacements(CGeometry *geometry, CConfig *config);
+  void SetBoundaryDisplacements(CGeometry* geometry, CConfig* config);
 
   /*!
    * \brief Check the domain points vertex that are going to be moved.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetDomainDisplacements(CGeometry *geometry, CConfig *config);
+  void SetDomainDisplacements(CGeometry* geometry, CConfig* config);
 
   /*!
    * \brief Unsteady grid movement using rigid mesh rotation.
@@ -276,7 +283,7 @@ class CVolumetricMovement : public CGridMovement {
    * \param[in] iZone - Zone number in the mesh.
    * \param[in] iter - Physical time iteration number.
    */
-  void Rigid_Rotation(CGeometry *geometry, CConfig *config, unsigned short iZone, unsigned long iter);
+  void Rigid_Rotation(CGeometry* geometry, CConfig* config, unsigned short iZone, unsigned long iter);
 
   /*!
    * \brief Unsteady pitching grid movement using rigid mesh motion.
@@ -285,7 +292,7 @@ class CVolumetricMovement : public CGridMovement {
    * \param[in] iZone - Zone number in the mesh.
    * \param[in] iter - Physical time iteration number.
    */
-  void Rigid_Pitching(CGeometry *geometry, CConfig *config, unsigned short iZone, unsigned long iter);
+  void Rigid_Pitching(CGeometry* geometry, CConfig* config, unsigned short iZone, unsigned long iter);
 
   /*!
    * \brief Unsteady plunging grid movement using rigid mesh motion.
@@ -294,7 +301,7 @@ class CVolumetricMovement : public CGridMovement {
    * \param[in] iZone - Zone number in the mesh.
    * \param[in] iter - Physical time iteration number.
    */
-  void Rigid_Plunging(CGeometry *geometry, CConfig *config, unsigned short iZone, unsigned long iter);
+  void Rigid_Plunging(CGeometry* geometry, CConfig* config, unsigned short iZone, unsigned long iter);
 
   /*!
    * \brief Unsteady translational grid movement using rigid mesh motion.
@@ -303,7 +310,7 @@ class CVolumetricMovement : public CGridMovement {
    * \param[in] iZone - Zone number in the mesh.
    * \param[in] iter - Physical time iteration number.
    */
-  void Rigid_Translation(CGeometry *geometry, CConfig *config, unsigned short iZone, unsigned long iter);
+  void Rigid_Translation(CGeometry* geometry, CConfig* config, unsigned short iZone, unsigned long iter);
 
   /*!
    * \brief Scale the volume grid by a multiplicative factor.
@@ -311,7 +318,7 @@ class CVolumetricMovement : public CGridMovement {
    * \param[in] config - Definition of the particular problem.
    * \param[in] UpdateGeo - Update geometry.
    */
-  void SetVolume_Scaling(CGeometry *geometry, CConfig *config, bool UpdateGeo);
+  void SetVolume_Scaling(CGeometry* geometry, CConfig* config, bool UpdateGeo);
 
   /*!
    * \brief Translate the volume grid by a specified displacement vector.
@@ -319,7 +326,7 @@ class CVolumetricMovement : public CGridMovement {
    * \param[in] config - Definition of the particular problem.
    * \param[in] UpdateGeo - Update geometry.
    */
-  void SetVolume_Translation(CGeometry *geometry, CConfig *config, bool UpdateGeo);
+  void SetVolume_Translation(CGeometry* geometry, CConfig* config, bool UpdateGeo);
 
   /*!
    * \brief Rotate the volume grid around a specified axis and angle.
@@ -327,7 +334,7 @@ class CVolumetricMovement : public CGridMovement {
    * \param[in] config - Definition of the particular problem.
    * \param[in] UpdateGeo - Update geometry.
    */
-  void SetVolume_Rotation(CGeometry *geometry, CConfig *config, bool UpdateGeo);
+  void SetVolume_Rotation(CGeometry* geometry, CConfig* config, bool UpdateGeo);
 
   /*!
    * \brief Grid deformation using the spring analogy method.
@@ -336,7 +343,8 @@ class CVolumetricMovement : public CGridMovement {
    * \param[in] UpdateGeo - Update geometry.
    * \param[in] Derivative - Compute the derivative (disabled by default). Does not actually deform the grid if enabled.
    */
-  void SetVolume_Deformation(CGeometry *geometry, CConfig *config, bool UpdateGeo, bool Derivative = false, bool ForwardProjectionDerivative = false);
+  void SetVolume_Deformation(CGeometry* geometry, CConfig* config, bool UpdateGeo, bool Derivative = false,
+                             bool ForwardProjectionDerivative = false);
 
   /*!
    * \brief Grid deformation using the spring analogy method.
@@ -345,21 +353,22 @@ class CVolumetricMovement : public CGridMovement {
    * \param[in] UpdateGeo - Update geometry.
    * \param[in] Derivative - Compute the derivative (disabled by default). Does not actually deform the grid if enabled.
    */
-  inline virtual void SetVolume_Deformation_Elas(CGeometry *geometry, CConfig *config, bool UpdateGeo, bool screen_output, bool Derivative = false) { }
+  inline virtual void SetVolume_Deformation_Elas(CGeometry* geometry, CConfig* config, bool UpdateGeo,
+                                                 bool screen_output, bool Derivative = false) {}
 
   /*!
    * \brief Set the derivatives of the boundary nodes.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetBoundaryDerivatives(CGeometry *geometry, CConfig *config, bool ForwardProjectionDerivative);
+  void SetBoundaryDerivatives(CGeometry* geometry, CConfig* config, bool ForwardProjectionDerivative);
 
   /*!
    * \brief Update the derivatives of the coordinates after the grid movement.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void UpdateGridCoord_Derivatives(CGeometry *geometry, CConfig *config, bool ForwardProjectionDerivative);
+  void UpdateGridCoord_Derivatives(CGeometry* geometry, CConfig* config, bool ForwardProjectionDerivative);
 
   /*!
    * \brief Store the number of iterations when moving the mesh.
@@ -378,5 +387,5 @@ class CVolumetricMovement : public CGridMovement {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  inline virtual void Boundary_Dependencies(CGeometry **geometry, CConfig *config) {  }
+  inline virtual void Boundary_Dependencies(CGeometry** geometry, CConfig* config) {}
 };
diff --git a/Common/include/interface_interpolation/CInterpolator.hpp b/Common/include/interface_interpolation/CInterpolator.hpp
index 5d953f14255..e3853ae91d9 100644
--- a/Common/include/interface_interpolation/CInterpolator.hpp
+++ b/Common/include/interface_interpolation/CInterpolator.hpp
@@ -45,46 +45,47 @@ using namespace std;
  * \author H. Kline
  */
 class CInterpolator {
-protected:
+ protected:
   const int rank;            /*!< \brief MPI Rank. */
   const int size;            /*!< \brief MPI Size. */
   const unsigned donorZone;  /*!< \brief Index of donor zone. */
   const unsigned targetZone; /*!< \brief Index of target zone. */
 
-  unsigned long
-  MaxLocalVertex_Donor,              /*!< \brief Maximum vertices per processor. */
-  Buffer_Send_nVertex_Donor[1],      /*!< \brief Buffer to send number of vertices on the local processor. */
-  *Buffer_Receive_nVertex_Donor;     /*!< \brief Buffer to store the number of vertices per processor on the Donor domain. */
+  unsigned long MaxLocalVertex_Donor, /*!< \brief Maximum vertices per processor. */
+      Buffer_Send_nVertex_Donor[1],   /*!< \brief Buffer to send number of vertices on the local processor. */
+      *Buffer_Receive_nVertex_Donor;  /*!< \brief Buffer to store the number of vertices per processor on the Donor
+                                         domain. */
 
-  su2vector<unsigned long> Buffer_Send_GlobalPoint;     /*!< \brief Buffer to send global point indices. */
-  su2vector<unsigned long> Buffer_Receive_GlobalPoint;       /*!< \brief Buffer to receive global point indices. */
+  su2vector<unsigned long> Buffer_Send_GlobalPoint;    /*!< \brief Buffer to send global point indices. */
+  su2vector<unsigned long> Buffer_Receive_GlobalPoint; /*!< \brief Buffer to receive global point indices. */
 
-  su2activematrix Buffer_Send_Coord;      /*!< \brief Buffer to send coordinate values. */
-  su2activematrix Buffer_Receive_Coord;             /*!< \brief Buffer to receive coordinate values. */
+  su2activematrix Buffer_Send_Coord;    /*!< \brief Buffer to send coordinate values. */
+  su2activematrix Buffer_Receive_Coord; /*!< \brief Buffer to receive coordinate values. */
 
   /*! \brief Buffer to receive the number of surface-connected edges, for each vertex. */
   su2vector<unsigned long> Buffer_Receive_nLinkedNodes;
-  /*! \brief Buffer to receive the index of the Receive_LinkedNodes buffer where corresponding list of linked nodes begins. */
+  /*! \brief Buffer to receive the index of the Receive_LinkedNodes buffer where corresponding list of linked nodes
+   * begins. */
   su2vector<unsigned long> Buffer_Receive_StartLinkedNodes;
   /*! \brief Buffer to receive the list of surface-connected nodes, for each vertex.
-   * \details The vertices are ordered as in Buffer_Receive_nLinkedNodes and Buffer_Receive_StartLinkedNodes, but for each*/
+   * \details The vertices are ordered as in Buffer_Receive_nLinkedNodes and Buffer_Receive_StartLinkedNodes, but for
+   * each*/
   su2vector<unsigned long> Buffer_Receive_LinkedNodes;
   /*! \brief Buffer to receive the rank that owns the vertex. */
   su2vector<unsigned long> Buffer_Receive_Proc;
 
-  unsigned long
-  nGlobalVertex_Target,              /*!< \brief Global number of vertex of the target boundary. */
-  nLocalVertex_Target,               /*!< \brief Number of vertex of the target boundary owned by the thread. */
-  nGlobalVertex_Donor,               /*!< \brief Global number of vertex of the donor boundary. */
-  nLocalVertex_Donor,                /*!< \brief Number of vertex of the donor boundary owned by the thread. */
-  nGlobalVertex,                     /*!< \brief Dummy variable to temporarily store the global number of vertex of a boundary. */
-  nLocalLinkedNodes;                 /*!< \brief Dummy variable to temporarily store the number of vertex of a boundary. */
+  unsigned long nGlobalVertex_Target, /*!< \brief Global number of vertex of the target boundary. */
+      nLocalVertex_Target,            /*!< \brief Number of vertex of the target boundary owned by the thread. */
+      nGlobalVertex_Donor,            /*!< \brief Global number of vertex of the donor boundary. */
+      nLocalVertex_Donor,             /*!< \brief Number of vertex of the donor boundary owned by the thread. */
+      nGlobalVertex,     /*!< \brief Dummy variable to temporarily store the global number of vertex of a boundary. */
+      nLocalLinkedNodes; /*!< \brief Dummy variable to temporarily store the number of vertex of a boundary. */
 
-  CGeometry**** const Geometry;      /*! \brief Vector which stores n zones of geometry. */
-  CGeometry* const donor_geometry;   /*! \brief Donor geometry. */
-  CGeometry* const target_geometry;  /*! \brief Target geometry. */
+  CGeometry**** const Geometry;     /*! \brief Vector which stores n zones of geometry. */
+  CGeometry* const donor_geometry;  /*! \brief Donor geometry. */
+  CGeometry* const target_geometry; /*! \brief Target geometry. */
 
-public:
+ public:
   struct CDonorInfo {
     vector<int> processor;
     vector<unsigned long> globalPoint;
@@ -107,8 +108,7 @@ class CInterpolator {
    * \param[in] iZone - index of the donor zone.
    * \param[in] jZone - index of the target zone.
    */
-  CInterpolator(CGeometry ****geometry_container, const CConfig* const* config,
-                unsigned int iZone, unsigned int jZone);
+  CInterpolator(CGeometry**** geometry_container, const CConfig* const* config, unsigned int iZone, unsigned int jZone);
 
   /*!
    * \brief No default construction allowed to force zones and geometry to always be set.
@@ -130,7 +130,7 @@ class CInterpolator {
   /*!
    * \brief Print information about the interpolation.
    */
-  virtual void PrintStatistics(void) const { }
+  virtual void PrintStatistics(void) const {}
 
   /*!
    * \brief Check whether an interface should be processed or not, i.e. if it is part of the zones.
@@ -146,7 +146,7 @@ class CInterpolator {
    */
   static bool CheckZonesInterface(const CConfig* donor, const CConfig* target);
 
-protected:
+ protected:
   /*!
    * \brief Reconstruct the boundary connectivity from parallel partitioning and broadcasts it to all threads.
    * \param[in] val_zone   - index of the zone
diff --git a/Common/include/interface_interpolation/CInterpolatorFactory.hpp b/Common/include/interface_interpolation/CInterpolatorFactory.hpp
index a9749015ec1..f5382127232 100644
--- a/Common/include/interface_interpolation/CInterpolatorFactory.hpp
+++ b/Common/include/interface_interpolation/CInterpolatorFactory.hpp
@@ -41,9 +41,7 @@ namespace CInterpolatorFactory {
  * \param[in] verbose - If true, print information to screen.
  * \return Pointer to interpolator on the heap, caller is responsible for deletion.
  */
-CInterpolator* CreateInterpolator(CGeometry ****geometry_container,
-                                  const CConfig* const* config,
-                                  const CInterpolator* transpInterpolator,
-                                  unsigned iZone, unsigned jZone,
+CInterpolator* CreateInterpolator(CGeometry**** geometry_container, const CConfig* const* config,
+                                  const CInterpolator* transpInterpolator, unsigned iZone, unsigned jZone,
                                   bool verbose = true);
-}
+}  // namespace CInterpolatorFactory
diff --git a/Common/include/interface_interpolation/CIsoparametric.hpp b/Common/include/interface_interpolation/CIsoparametric.hpp
index 7584e61c505..7f1fc5e591a 100644
--- a/Common/include/interface_interpolation/CIsoparametric.hpp
+++ b/Common/include/interface_interpolation/CIsoparametric.hpp
@@ -33,23 +33,23 @@
  * \ingroup Interfaces
  */
 class CIsoparametric final : public CInterpolator {
-private:
+ private:
   /*--- Statistics. ---*/
   su2double MaxDistance = 0.0, ErrorRate = 0.0;
   unsigned long ErrorCounter = 0;
 
   /*! \brief Helper struct to store information about candidate donor elements. */
   struct DonorInfo {
-    su2double isoparams[4] = {0.0};  /*!< \brief Interpolation coefficients. */
-    su2double distance = 0.0;        /*!< \brief Distance from target to final mapped point on donor plane. */
-    unsigned iElem = 0;              /*!< \brief Identification of the element. */
-    int error = 0;                   /*!< \brief If the mapped point is "outside" of the donor. */
+    su2double isoparams[4] = {0.0}; /*!< \brief Interpolation coefficients. */
+    su2double distance = 0.0;       /*!< \brief Distance from target to final mapped point on donor plane. */
+    unsigned iElem = 0;             /*!< \brief Identification of the element. */
+    int error = 0;                  /*!< \brief If the mapped point is "outside" of the donor. */
 
     /*--- Best donor is one for which the mapped point is closest to target. ---*/
-    bool operator< (const DonorInfo& other) const { return distance < other.distance; }
+    bool operator<(const DonorInfo& other) const { return distance < other.distance; }
   };
 
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] geometry - Geometrical definition of the problem.
@@ -57,8 +57,8 @@ class CIsoparametric final : public CInterpolator {
    * \param[in] iZone - index of the donor zone.
    * \param[in] jZone - index of the target zone.
    */
-  CIsoparametric(CGeometry ****geometry_container, const CConfig* const* config,
-                 unsigned int iZone, unsigned int jZone);
+  CIsoparametric(CGeometry**** geometry_container, const CConfig* const* config, unsigned int iZone,
+                 unsigned int jZone);
 
   /*!
    * \brief Set up transfer matrix defining relation between two meshes
@@ -71,7 +71,7 @@ class CIsoparametric final : public CInterpolator {
    */
   void PrintStatistics(void) const override;
 
-private:
+ private:
   /*!
    * \brief Compute the isoparametric interpolation coefficients for a 2D line element.
    * \param[in] X - Coordinate matrix defining the line.
@@ -79,7 +79,7 @@ class CIsoparametric final : public CInterpolator {
    * \param[out] isoparams - Isoparametric coefficients.
    * \return 0 on success, 1 if xj is too far outside element bounds.
    */
-  static int LineIsoparameters(const su2double X[][3], const su2double *xj, su2double* isoparams);
+  static int LineIsoparameters(const su2double X[][3], const su2double* xj, su2double* isoparams);
 
   /*!
    * \brief Compute the isoparametric interpolation coefficients for a 3D triangle element.
@@ -88,7 +88,7 @@ class CIsoparametric final : public CInterpolator {
    * \param[out] isoparams - Isoparametric coefficients.
    * \return 0 on success, 1 if xj is too far outside element bounds.
    */
-  static int TriangleIsoparameters(const su2double X[][3], const su2double *xj, su2double* isoparams);
+  static int TriangleIsoparameters(const su2double X[][3], const su2double* xj, su2double* isoparams);
 
   /*!
    * \brief Compute the isoparametric interpolation coefficients for a 3D quadrilateral element.
@@ -97,6 +97,5 @@ class CIsoparametric final : public CInterpolator {
    * \param[out] isoparams - Isoparametric coefficients.
    * \return 0 on success, 1 if xj is too far outside element bounds.
    */
-  static int QuadrilateralIsoparameters(const su2double X[][3], const su2double *xj, su2double* isoparams);
-
+  static int QuadrilateralIsoparameters(const su2double X[][3], const su2double* xj, su2double* isoparams);
 };
diff --git a/Common/include/interface_interpolation/CMirror.hpp b/Common/include/interface_interpolation/CMirror.hpp
index a23626b852f..c514d2097a6 100644
--- a/Common/include/interface_interpolation/CMirror.hpp
+++ b/Common/include/interface_interpolation/CMirror.hpp
@@ -34,10 +34,10 @@
  * \ingroup Interfaces
  */
 class CMirror final : public CInterpolator {
-private:
+ private:
   const CInterpolator* const transpInterpolator; /*! \brief The transpose interpolator (from j to i). */
 
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    * \note Data is set in geometry[targetZone].
@@ -47,13 +47,12 @@ class CMirror final : public CInterpolator {
    * \param[in] iZone - First zone
    * \param[in] jZone - Second zone
    */
-  CMirror(CGeometry ****geometry_container, const CConfig* const* config,
-          const CInterpolator* interpolator, unsigned int iZone, unsigned int jZone);
+  CMirror(CGeometry**** geometry_container, const CConfig* const* config, const CInterpolator* interpolator,
+          unsigned int iZone, unsigned int jZone);
 
   /*!
    * \brief Set up transfer matrix defining relation between two meshes
    * \param[in] config - Definition of the particular problem.
    */
   void SetTransferCoeff(const CConfig* const* config) override;
-
 };
diff --git a/Common/include/interface_interpolation/CNearestNeighbor.hpp b/Common/include/interface_interpolation/CNearestNeighbor.hpp
index be97794c60f..14c12a08e07 100644
--- a/Common/include/interface_interpolation/CNearestNeighbor.hpp
+++ b/Common/include/interface_interpolation/CNearestNeighbor.hpp
@@ -36,7 +36,7 @@
  * \ingroup Interfaces
  */
 class CNearestNeighbor final : public CInterpolator {
-private:
+ private:
   su2double AvgDistance = 0.0, MaxDistance = 0.0;
 
   /*! \brief Helper struct to (partially) sort neighbours according to distance while
@@ -45,10 +45,10 @@ class CNearestNeighbor final : public CInterpolator {
     su2double dist;
     unsigned pidx;
     int proc;
-    DonorInfo(su2double d = 0.0, unsigned i = 0, int p = 0) : dist(d), pidx(i), proc(p) { }
+    DonorInfo(su2double d = 0.0, unsigned i = 0, int p = 0) : dist(d), pidx(i), proc(p) {}
   };
 
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] geometry - Geometrical definition of the problem.
@@ -56,8 +56,8 @@ class CNearestNeighbor final : public CInterpolator {
    * \param[in] iZone - index of the donor zone.
    * \param[in] jZone - index of the target zone.
    */
-  CNearestNeighbor(CGeometry ****geometry_container, const CConfig* const* config,
-                   unsigned int iZone, unsigned int jZone);
+  CNearestNeighbor(CGeometry**** geometry_container, const CConfig* const* config, unsigned int iZone,
+                   unsigned int jZone);
 
   /*!
    * \brief Set up transfer matrix defining relation between two meshes.
@@ -69,5 +69,4 @@ class CNearestNeighbor final : public CInterpolator {
    * \brief Print interpolation statistics.
    */
   void PrintStatistics(void) const override;
-
 };
diff --git a/Common/include/interface_interpolation/CRadialBasisFunction.hpp b/Common/include/interface_interpolation/CRadialBasisFunction.hpp
index 2c65cca5f18..601c96a232e 100644
--- a/Common/include/interface_interpolation/CRadialBasisFunction.hpp
+++ b/Common/include/interface_interpolation/CRadialBasisFunction.hpp
@@ -36,11 +36,12 @@
  */
 class CRadialBasisFunction final : public CInterpolator {
   static_assert(su2passivematrix::IsRowMajor, "This class relies on row major storage throughout.");
-private:
+
+ private:
   unsigned long MinDonors = 0, AvgDonors = 0, MaxDonors = 0;
   passivedouble Density = 0.0, AvgCorrection = 0.0, MaxCorrection = 0.0;
 
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] geometry - Geometrical definition of the problem.
@@ -48,8 +49,8 @@ class CRadialBasisFunction final : public CInterpolator {
    * \param[in] iZone - index of the donor zone.
    * \param[in] jZone - index of the target zone.
    */
-  CRadialBasisFunction(CGeometry ****geometry_container, const CConfig* const* config,
-                       unsigned int iZone, unsigned int jZone);
+  CRadialBasisFunction(CGeometry**** geometry_container, const CConfig* const* config, unsigned int iZone,
+                       unsigned int jZone);
 
   /*!
    * \brief Set up transfer matrix defining relation between two meshes
@@ -85,8 +86,8 @@ class CRadialBasisFunction final : public CInterpolator {
    * \param[out] C_inv_trunc - The generator matrix as described above.
    */
   static void ComputeGeneratorMatrix(RADIAL_BASIS type, bool usePolynomial, su2double radius,
-                                     const su2activematrix& coords, int& nPolynomial,
-                                     vector<int>& keepPolynomialRow, su2passivematrix& C_inv_trunc);
+                                     const su2activematrix& coords, int& nPolynomial, vector<int>& keepPolynomialRow,
+                                     su2passivematrix& C_inv_trunc);
 
   /*!
    * \brief If the polynomial term is included in the interpolation, and the points lie on a plane, the matrix
@@ -97,9 +98,9 @@ class CRadialBasisFunction final : public CInterpolator {
    * \param[in,out] P - Polynomial part of the interpolation matrix, one row may be eliminated.
    * \return n_polynomial - Size of the polynomial part on exit (in practice nDim or nDim-1).
    */
-  static int CheckPolynomialTerms(su2double max_diff_tol, vector<int>& keep_row, su2passivematrix &P);
+  static int CheckPolynomialTerms(su2double max_diff_tol, vector<int>& keep_row, su2passivematrix& P);
 
-private:
+ private:
   /*!
    * \brief Helper function, prunes (by setting to zero) small interpolation coefficients,
    * i.e. <= tolerance*max(abs(coeffs)). The vector is re-scaled such that sum(coeffs)==1.
@@ -108,25 +109,24 @@ class CRadialBasisFunction final : public CInterpolator {
    * \param[in,out] coeffs - Iterator to start of vector of interpolation coefficients.
    * \return Number of non-zero coefficients after pruning and correction factor.
    */
-  template<typename Float, typename Int, class ForwardIt>
-  static pair<Int,Float> PruneSmallCoefficients(Float tolerance, Int size, ForwardIt coeffs) {
-
+  template <typename Float, typename Int, class ForwardIt>
+  static pair<Int, Float> PruneSmallCoefficients(Float tolerance, Int size, ForwardIt coeffs) {
     /*--- Determine the pruning threshold. ---*/
     Float thresh = 0.0;
     auto end = coeffs;
-    for (Int i = 0; i < size; ++i)
-      thresh = max(thresh, fabs(*(end++)));
+    for (Int i = 0; i < size; ++i) thresh = max(thresh, fabs(*(end++)));
     thresh *= tolerance;
 
     /*--- Prune and count non-zeros. ---*/
     Int numNonZeros = 0;
     Float coeffSum = 0.0;
     for (auto it = coeffs; it != end; ++it) {
-      if (fabs(*it) > thresh) { // keep
+      if (fabs(*it) > thresh) {  // keep
         coeffSum += *it;
         ++numNonZeros;
-      }
-      else { *it = 0.0; } // prune
+      } else {
+        *it = 0.0;
+      }  // prune
     }
 
     /*--- Correct remaining coefficients, sum must be 1 for conservation. ---*/
@@ -135,5 +135,4 @@ class CRadialBasisFunction final : public CInterpolator {
 
     return make_pair(numNonZeros, correction);
   }
-
 };
diff --git a/Common/include/interface_interpolation/CSlidingMesh.hpp b/Common/include/interface_interpolation/CSlidingMesh.hpp
index b07dcef36f4..571948870ff 100644
--- a/Common/include/interface_interpolation/CSlidingMesh.hpp
+++ b/Common/include/interface_interpolation/CSlidingMesh.hpp
@@ -35,7 +35,7 @@
  * \ingroup Interfaces
  */
 class CSlidingMesh final : public CInterpolator {
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] geometry - Geometrical definition of the problem.
@@ -43,8 +43,7 @@ class CSlidingMesh final : public CInterpolator {
    * \param[in] iZone - index of the donor zone.
    * \param[in] jZone - index of the target zone.
    */
-  CSlidingMesh(CGeometry ****geometry_container, const CConfig* const* config,
-               unsigned int iZone, unsigned int jZone);
+  CSlidingMesh(CGeometry**** geometry_container, const CConfig* const* config, unsigned int iZone, unsigned int jZone);
 
   /*!
    * \brief Set up transfer matrix defining relation between two meshes
@@ -52,7 +51,7 @@ class CSlidingMesh final : public CInterpolator {
    */
   void SetTransferCoeff(const CConfig* const* config) override;
 
-private:
+ private:
   /*!
    * \brief For 3-Dimensional grids, build the dual surface element
    * \param[in] map         - array containing the index of the boundary points connected to the node
@@ -125,6 +124,6 @@ class CSlidingMesh final : public CInterpolator {
    * \param[in] T2 - second point of triangle T
    * \param[in] T3 - third  point of triangle T
    */
-  static bool CheckPointInsideTriangle(const su2double* Point, const su2double* T1,
-                                       const su2double* T2, const su2double* T3);
+  static bool CheckPointInsideTriangle(const su2double* Point, const su2double* T1, const su2double* T2,
+                                       const su2double* T3);
 };
diff --git a/Common/include/linear_algebra/CMatrixVectorProduct.hpp b/Common/include/linear_algebra/CMatrixVectorProduct.hpp
index cc48bb4670f..a3052d70d9b 100644
--- a/Common/include/linear_algebra/CMatrixVectorProduct.hpp
+++ b/Common/include/linear_algebra/CMatrixVectorProduct.hpp
@@ -26,7 +26,6 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #pragma once
 
 #include "../CConfig.hpp"
@@ -52,40 +51,37 @@
  * passed to a single implementation of the Krylov solvers.
  * This abstraction may also be used to define matrix-free products.
  */
-template<class ScalarType>
+template <class ScalarType>
 class CMatrixVectorProduct {
-public:
+ public:
   virtual ~CMatrixVectorProduct() = 0;
-  virtual void operator()(const CSysVector<ScalarType> & u, CSysVector<ScalarType> & v) const = 0;
+  virtual void operator()(const CSysVector<ScalarType>& u, CSysVector<ScalarType>& v) const = 0;
 };
-template<class ScalarType>
+template <class ScalarType>
 CMatrixVectorProduct<ScalarType>::~CMatrixVectorProduct() {}
 
-
 /*!
  * \class CSysMatrixVectorProduct
  * \ingroup SpLinSys
  * \brief Specialization of matrix-vector product that uses CSysMatrix class
  */
-template<class ScalarType>
+template <class ScalarType>
 class CSysMatrixVectorProduct final : public CMatrixVectorProduct<ScalarType> {
-private:
-  const CSysMatrix<ScalarType>& matrix;  /*!< \brief pointer to matrix that defines the product. */
-  CGeometry* geometry;                   /*!< \brief geometry associated with the matrix. */
-  const CConfig *config;                 /*!< \brief config of the problem. */
+ private:
+  const CSysMatrix<ScalarType>& matrix; /*!< \brief pointer to matrix that defines the product. */
+  CGeometry* geometry;                  /*!< \brief geometry associated with the matrix. */
+  const CConfig* config;                /*!< \brief config of the problem. */
 
-public:
+ public:
   /*!
    * \brief constructor of the class
    * \param[in] matrix_ref - matrix reference that will be used to define the products
    * \param[in] geometry_ref - geometry associated with the problem
    * \param[in] config_ref - config of the problem
    */
-  inline CSysMatrixVectorProduct(const CSysMatrix<ScalarType> & matrix_ref,
-                                 CGeometry *geometry_ref, const CConfig *config_ref) :
-    matrix(matrix_ref),
-    geometry(geometry_ref),
-    config(config_ref) {}
+  inline CSysMatrixVectorProduct(const CSysMatrix<ScalarType>& matrix_ref, CGeometry* geometry_ref,
+                                 const CConfig* config_ref)
+      : matrix(matrix_ref), geometry(geometry_ref), config(config_ref) {}
 
   /*!
    * \note This class cannot be default constructed as that would leave us with invalid pointers.
@@ -97,7 +93,7 @@ class CSysMatrixVectorProduct final : public CMatrixVectorProduct<ScalarType> {
    * \param[in] u - CSysVector that is being multiplied by the sparse matrix
    * \param[out] v - CSysVector that is the result of the product
    */
-  inline void operator()(const CSysVector<ScalarType> & u, CSysVector<ScalarType> & v) const override {
+  inline void operator()(const CSysVector<ScalarType>& u, CSysVector<ScalarType>& v) const override {
     matrix.MatrixVectorProduct(u, v, geometry, config);
   }
 };
diff --git a/Common/include/linear_algebra/CPastixWrapper.hpp b/Common/include/linear_algebra/CPastixWrapper.hpp
index 72ed9629e61..6001ec97e38 100644
--- a/Common/include/linear_algebra/CPastixWrapper.hpp
+++ b/Common/include/linear_algebra/CPastixWrapper.hpp
@@ -31,14 +31,14 @@
 #ifdef HAVE_PASTIX
 
 #ifdef CODI_FORWARD_TYPE
-  #error Cannot use PaStiX with forward mode AD
+#error Cannot use PaStiX with forward mode AD
 #endif
 
 namespace PaStiX {
 extern "C" {
 #include <pastix.h>
 }
-}
+}  // namespace PaStiX
 #include <vector>
 
 using namespace std;
@@ -52,33 +52,31 @@ class CGeometry;
  * \brief Wrapper class that converts between SU2 sparse format and PaStiX
  *        format and simplifies calls to the external solver.
  */
-template<class ScalarType>
-class CPastixWrapper
-{
-private:
-  PaStiX::pastix_data_t       *state;   /*!< \brief Internal state of the solver. */
-  PaStiX::pastix_int_t         nCols;   /*!< \brief Local number of columns. */
+template <class ScalarType>
+class CPastixWrapper {
+ private:
+  PaStiX::pastix_data_t* state;         /*!< \brief Internal state of the solver. */
+  PaStiX::pastix_int_t nCols;           /*!< \brief Local number of columns. */
   vector<PaStiX::pastix_int_t> colptr;  /*!< \brief Equiv. to our "row_ptr". */
   vector<PaStiX::pastix_int_t> rowidx;  /*!< \brief Equiv. to our "col_ind". */
-  vector<passivedouble>        values;  /*!< \brief Equiv. to our "matrix". */
+  vector<passivedouble> values;         /*!< \brief Equiv. to our "matrix". */
   vector<PaStiX::pastix_int_t> loc2glb; /*!< \brief Global index of the columns held by this rank. */
   vector<PaStiX::pastix_int_t> perm;    /*!< \brief Ordering computed by PaStiX. */
-  vector<passivedouble>        workvec; /*!< \brief RHS vector which then becomes the solution. */
+  vector<passivedouble> workvec;        /*!< \brief RHS vector which then becomes the solution. */
 
   PaStiX::pastix_int_t iparm[PaStiX::IPARM_SIZE]; /*!< \brief Integer parameters for PaStiX. */
-  passivedouble        dparm[PaStiX::DPARM_SIZE]; /*!< \brief Floating point parameters for PaStiX. */
+  passivedouble dparm[PaStiX::DPARM_SIZE];        /*!< \brief Floating point parameters for PaStiX. */
 
   struct {
     unsigned long nVar = 0;
     unsigned long nPoint = 0;
     unsigned long nPointDomain = 0;
-    const unsigned long *rowptr = nullptr;
-    const unsigned long *colidx = nullptr;
-    const ScalarType *values = nullptr;
+    const unsigned long* rowptr = nullptr;
+    const unsigned long* colidx = nullptr;
+    const ScalarType* values = nullptr;
 
-    unsigned long size_rhs() const {return nPointDomain*nVar;}
-  }
-  matrix;  /*!< \brief Pointers and sizes of the input matrix. */
+    unsigned long size_rhs() const { return nPointDomain * nVar; }
+  } matrix; /*!< \brief Pointers and sizes of the input matrix. */
 
   bool issetup;        /*!< \brief Signals that the matrix data has been provided. */
   bool isinitialized;  /*!< \brief Signals that the sparsity pattern has been set. */
@@ -87,15 +85,15 @@ class CPastixWrapper
   unsigned short verb; /*!< \brief Verbosity level. */
   const int mpi_size, mpi_rank;
 
-  vector<unsigned long>          sort_rows;  /*!< \brief List of rows with halo points. */
+  vector<unsigned long> sort_rows;           /*!< \brief List of rows with halo points. */
   vector<vector<unsigned long> > sort_order; /*!< \brief How each of those rows needs to be sorted. */
 
   /*!
    * \brief Run the external solver for the task it is currently setup to execute.
    */
   void Run() {
-    dpastix(&state, SU2_MPI::GetComm(), nCols, colptr.data(), rowidx.data(), values.data(),
-            loc2glb.data(), perm.data(), NULL, workvec.data(), 1, iparm, dparm);
+    dpastix(&state, SU2_MPI::GetComm(), nCols, colptr.data(), rowidx.data(), values.data(), loc2glb.data(), perm.data(),
+            NULL, workvec.data(), 1, iparm, dparm);
   }
 
   /*!
@@ -103,10 +101,10 @@ class CPastixWrapper
    */
   void Clean() {
     using namespace PaStiX;
-    if(isfactorized) {
+    if (isfactorized) {
       iparm[IPARM_VERBOSE] = (verb > 0) ? API_VERBOSE_NO : API_VERBOSE_NOT;
       iparm[IPARM_START_TASK] = API_TASK_CLEAN;
-      iparm[IPARM_END_TASK]   = API_TASK_CLEAN;
+      iparm[IPARM_END_TASK] = API_TASK_CLEAN;
       Run();
       isfactorized = false;
     }
@@ -115,22 +113,27 @@ class CPastixWrapper
   /*!
    * \brief Initialize the matrix format that PaStiX requires.
    */
-  void Initialize(CGeometry *geometry, const CConfig *config);
+  void Initialize(CGeometry* geometry, const CConfig* config);
 
-public:
+ public:
   /*!
    * \brief Class constructor.
    */
-  CPastixWrapper() : state(nullptr), issetup(false), isinitialized(false),
-                     isfactorized(false), iter(0), verb(0),
-                     mpi_size(SU2_MPI::GetSize()), mpi_rank(SU2_MPI::GetRank()) {
-  }
+  CPastixWrapper()
+      : state(nullptr),
+        issetup(false),
+        isinitialized(false),
+        isfactorized(false),
+        iter(0),
+        verb(0),
+        mpi_size(SU2_MPI::GetSize()),
+        mpi_rank(SU2_MPI::GetRank()) {}
 
   /*--- Move or copy is not allowed. ---*/
   CPastixWrapper(CPastixWrapper&&) = delete;
   CPastixWrapper(const CPastixWrapper&) = delete;
-  CPastixWrapper& operator= (CPastixWrapper&&) = delete;
-  CPastixWrapper& operator= (const CPastixWrapper&) = delete;
+  CPastixWrapper& operator=(CPastixWrapper&&) = delete;
+  CPastixWrapper& operator=(const CPastixWrapper&) = delete;
 
   /*!
    * \brief Class destructor.
@@ -146,13 +149,8 @@ class CPastixWrapper
    * \param[in] colidx - Non zeros column indices.
    * \param[in] values - Matrix coefficients.
    */
-  void SetMatrix(unsigned long nVar,
-                 unsigned long nPoint,
-                 unsigned long nPointDomain,
-                 const unsigned long *rowptr,
-                 const unsigned long *colidx,
-                 const ScalarType *values) {
-
+  void SetMatrix(unsigned long nVar, unsigned long nPoint, unsigned long nPointDomain, const unsigned long* rowptr,
+                 const unsigned long* colidx, const ScalarType* values) {
     if (issetup) return;
     matrix.nVar = nVar;
     matrix.nPoint = nPoint;
@@ -169,7 +167,7 @@ class CPastixWrapper
    * \param[in] config   - Definition of the particular problem.
    * \param[in] kind_fact - Type of factorization.
    */
-  void Factorize(CGeometry *geometry, const CConfig *config, unsigned short kind_fact);
+  void Factorize(CGeometry* geometry, const CConfig* config, unsigned short kind_fact);
 
   /*!
    * \brief Request solves with the transposed matrix.
@@ -178,7 +176,7 @@ class CPastixWrapper
   void SetTransposedSolve(bool transposed = true) {
     using namespace PaStiX;
     if (iparm[IPARM_SYM] == API_SYM_NO)
-      iparm[IPARM_TRANSPOSE_SOLVE] = pastix_int_t(!transposed); // negated due to CSR to CSC copy
+      iparm[IPARM_TRANSPOSE_SOLVE] = pastix_int_t(!transposed);  // negated due to CSR to CSC copy
   }
 
   /*!
@@ -186,24 +184,22 @@ class CPastixWrapper
    * \param[in]  rhs - Right hand side of the linear system.
    * \param[out] sol - Solution of the system.
    */
-  template<class T>
+  template <class T>
   void Solve(const T& rhs, T& sol) {
     using namespace PaStiX;
 
-    if (!isfactorized)
-      SU2_MPI::Error("The factorization has not been computed yet.", CURRENT_FUNCTION);
+    if (!isfactorized) SU2_MPI::Error("The factorization has not been computed yet.", CURRENT_FUNCTION);
 
     unsigned long i;
 
-    for (i=0; i < matrix.size_rhs(); ++i) workvec[i] = rhs[i];
+    for (i = 0; i < matrix.size_rhs(); ++i) workvec[i] = rhs[i];
 
-    iparm[IPARM_VERBOSE]    = API_VERBOSE_NOT;
+    iparm[IPARM_VERBOSE] = API_VERBOSE_NOT;
     iparm[IPARM_START_TASK] = API_TASK_SOLVE;
-    iparm[IPARM_END_TASK]   = API_TASK_SOLVE;
+    iparm[IPARM_END_TASK] = API_TASK_SOLVE;
     Run();
 
-    for (i=0; i < matrix.size_rhs(); ++i) sol[i] = workvec[i];
+    for (i = 0; i < matrix.size_rhs(); ++i) sol[i] = workvec[i];
   }
-
 };
 #endif
diff --git a/Common/include/linear_algebra/CPreconditioner.hpp b/Common/include/linear_algebra/CPreconditioner.hpp
index a2ebaf8ba39..b142645ff1f 100644
--- a/Common/include/linear_algebra/CPreconditioner.hpp
+++ b/Common/include/linear_algebra/CPreconditioner.hpp
@@ -44,9 +44,9 @@
  * See the remarks regarding the CMatrixVectorProduct class. The same
  * idea applies here to the preconditioning operation.
  */
-template<class ScalarType>
+template <class ScalarType>
 class CPreconditioner {
-public:
+ public:
   /*!
    * \brief Destructor of the class
    */
@@ -55,7 +55,7 @@ class CPreconditioner {
   /*!
    * \brief Overload of operator (), applies the preconditioner to "u" storing the result in "v".
    */
-  virtual void operator()(const CSysVector<ScalarType> & u, CSysVector<ScalarType> & v) const = 0;
+  virtual void operator()(const CSysVector<ScalarType>& u, CSysVector<ScalarType>& v) const = 0;
 
   /*!
    * \brief Generic "preprocessing" hook derived classes may implement to build the preconditioner.
@@ -70,36 +70,33 @@ class CPreconditioner {
   /*!
    * \brief Factory method.
    */
-  static CPreconditioner* Create(ENUM_LINEAR_SOLVER_PREC kind, CSysMatrix<ScalarType>& jacobian,
-                                 CGeometry* geometry, const CConfig* config);
+  static CPreconditioner* Create(ENUM_LINEAR_SOLVER_PREC kind, CSysMatrix<ScalarType>& jacobian, CGeometry* geometry,
+                                 const CConfig* config);
 };
-template<class ScalarType>
+template <class ScalarType>
 CPreconditioner<ScalarType>::~CPreconditioner() {}
 
-
 /*!
  * \class CJacobiPreconditioner
  * \brief Specialization of preconditioner that uses CSysMatrix class.
  */
-template<class ScalarType>
+template <class ScalarType>
 class CJacobiPreconditioner final : public CPreconditioner<ScalarType> {
-private:
+ private:
   CSysMatrix<ScalarType>& sparse_matrix; /*!< \brief Pointer to matrix that defines the preconditioner. */
   CGeometry* geometry;                   /*!< \brief Pointer to geometry associated with the matrix. */
-  const CConfig *config;                 /*!< \brief Pointer to problem configuration. */
+  const CConfig* config;                 /*!< \brief Pointer to problem configuration. */
 
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] matrix_ref - Matrix reference that will be used to define the preconditioner.
    * \param[in] geometry_ref - Geometry associated with the problem.
    * \param[in] config_ref - Config of the problem.
    */
-  inline CJacobiPreconditioner(CSysMatrix<ScalarType> & matrix_ref,
-                               CGeometry *geometry_ref, const CConfig *config_ref) :
-    sparse_matrix(matrix_ref)
-  {
-    if((geometry_ref == nullptr) || (config_ref == nullptr))
+  inline CJacobiPreconditioner(CSysMatrix<ScalarType>& matrix_ref, CGeometry* geometry_ref, const CConfig* config_ref)
+      : sparse_matrix(matrix_ref) {
+    if ((geometry_ref == nullptr) || (config_ref == nullptr))
       SU2_MPI::Error("Preconditioner needs to be built with valid references.", CURRENT_FUNCTION);
     geometry = geometry_ref;
     config = config_ref;
@@ -115,42 +112,37 @@ class CJacobiPreconditioner final : public CPreconditioner<ScalarType> {
    * \param[in] u - CSysVector that is being preconditioned
    * \param[out] v - CSysVector that is the result of the preconditioning
    */
-  inline void operator()(const CSysVector<ScalarType> & u, CSysVector<ScalarType> & v) const override {
+  inline void operator()(const CSysVector<ScalarType>& u, CSysVector<ScalarType>& v) const override {
     sparse_matrix.ComputeJacobiPreconditioner(u, v, geometry, config);
   }
 
   /*!
    * \note Request the associated matrix to build the preconditioner.
    */
-  inline void Build() override {
-    sparse_matrix.BuildJacobiPreconditioner();
-  }
+  inline void Build() override { sparse_matrix.BuildJacobiPreconditioner(); }
 };
 
-
 /*!
  * \class CILUPreconditioner
  * \brief Specialization of preconditioner that uses CSysMatrix class
  */
-template<class ScalarType>
+template <class ScalarType>
 class CILUPreconditioner final : public CPreconditioner<ScalarType> {
-private:
+ private:
   CSysMatrix<ScalarType>& sparse_matrix; /*!< \brief Pointer to matrix that defines the preconditioner. */
   CGeometry* geometry;                   /*!< \brief Pointer to geometry associated with the matrix. */
-  const CConfig *config;                 /*!< \brief Pointer to problem configuration. */
+  const CConfig* config;                 /*!< \brief Pointer to problem configuration. */
 
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] matrix_ref - Matrix reference that will be used to define the preconditioner.
    * \param[in] geometry_ref - Geometry associated with the problem.
    * \param[in] config_ref - Config of the problem.
    */
-  inline CILUPreconditioner(CSysMatrix<ScalarType> & matrix_ref,
-                            CGeometry *geometry_ref, const CConfig *config_ref) :
-    sparse_matrix(matrix_ref)
-  {
-    if((geometry_ref == nullptr) || (config_ref == nullptr))
+  inline CILUPreconditioner(CSysMatrix<ScalarType>& matrix_ref, CGeometry* geometry_ref, const CConfig* config_ref)
+      : sparse_matrix(matrix_ref) {
+    if ((geometry_ref == nullptr) || (config_ref == nullptr))
       SU2_MPI::Error("Preconditioner needs to be built with valid references.", CURRENT_FUNCTION);
     geometry = geometry_ref;
     config = config_ref;
@@ -166,43 +158,37 @@ class CILUPreconditioner final : public CPreconditioner<ScalarType> {
    * \param[in] u - CSysVector that is being preconditioned.
    * \param[out] v - CSysVector that is the result of the preconditioning.
    */
-  inline void operator()(const CSysVector<ScalarType> & u, CSysVector<ScalarType> & v) const override {
+  inline void operator()(const CSysVector<ScalarType>& u, CSysVector<ScalarType>& v) const override {
     sparse_matrix.ComputeILUPreconditioner(u, v, geometry, config);
   }
 
   /*!
    * \note Request the associated matrix to build the preconditioner.
    */
-  inline void Build() override {
-    sparse_matrix.BuildILUPreconditioner();
-  }
+  inline void Build() override { sparse_matrix.BuildILUPreconditioner(); }
 };
 
-
 /*!
  * \class CLU_SGSPreconditioner
  * \brief Specialization of preconditioner that uses CSysMatrix class.
  */
-template<class ScalarType>
+template <class ScalarType>
 class CLU_SGSPreconditioner final : public CPreconditioner<ScalarType> {
-private:
+ private:
   CSysMatrix<ScalarType>& sparse_matrix; /*!< \brief Pointer to matrix that defines the preconditioner. */
   CGeometry* geometry;                   /*!< \brief Pointer to geometry associated with the matrix. */
-  const CConfig *config;                 /*!< \brief Pointer to problem configuration. */
-
-public:
+  const CConfig* config;                 /*!< \brief Pointer to problem configuration. */
 
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] matrix_ref - Matrix reference that will be used to define the preconditioner.
    * \param[in] geometry_ref - Geometry associated with the problem.
    * \param[in] config_ref - Config of the problem.
    */
-  inline CLU_SGSPreconditioner(CSysMatrix<ScalarType> & matrix_ref,
-                               CGeometry *geometry_ref, const CConfig *config_ref) :
-    sparse_matrix(matrix_ref)
-  {
-    if((geometry_ref == nullptr) || (config_ref == nullptr))
+  inline CLU_SGSPreconditioner(CSysMatrix<ScalarType>& matrix_ref, CGeometry* geometry_ref, const CConfig* config_ref)
+      : sparse_matrix(matrix_ref) {
+    if ((geometry_ref == nullptr) || (config_ref == nullptr))
       SU2_MPI::Error("Preconditioner needs to be built with valid references.", CURRENT_FUNCTION);
     geometry = geometry_ref;
     config = config_ref;
@@ -218,35 +204,32 @@ class CLU_SGSPreconditioner final : public CPreconditioner<ScalarType> {
    * \param[in] u - CSysVector that is being preconditioned.
    * \param[out] v - CSysVector that is the result of the preconditioning.
    */
-  inline void operator()(const CSysVector<ScalarType> & u, CSysVector<ScalarType> & v) const override {
+  inline void operator()(const CSysVector<ScalarType>& u, CSysVector<ScalarType>& v) const override {
     sparse_matrix.ComputeLU_SGSPreconditioner(u, v, geometry, config);
   }
 };
 
-
 /*!
  * \class CLineletPreconditioner
  * \brief Specialization of preconditioner that uses CSysMatrix class.
  */
-template<class ScalarType>
+template <class ScalarType>
 class CLineletPreconditioner final : public CPreconditioner<ScalarType> {
-private:
+ private:
   CSysMatrix<ScalarType>& sparse_matrix; /*!< \brief Pointer to matrix that defines the preconditioner. */
   CGeometry* geometry;                   /*!< \brief Pointer to geometry associated with the matrix. */
-  const CConfig *config;                 /*!< \brief Pointer to problem configuration. */
+  const CConfig* config;                 /*!< \brief Pointer to problem configuration. */
 
-public:
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] matrix_ref - Matrix reference that will be used to define the preconditioner.
    * \param[in] geometry_ref - Geometry associated with the problem.
    * \param[in] config_ref - Config of the problem.
    */
-  inline CLineletPreconditioner(CSysMatrix<ScalarType> & matrix_ref,
-                                CGeometry *geometry_ref, const CConfig *config_ref) :
-    sparse_matrix(matrix_ref)
-  {
-    if((geometry_ref == nullptr) || (config_ref == nullptr))
+  inline CLineletPreconditioner(CSysMatrix<ScalarType>& matrix_ref, CGeometry* geometry_ref, const CConfig* config_ref)
+      : sparse_matrix(matrix_ref) {
+    if ((geometry_ref == nullptr) || (config_ref == nullptr))
       SU2_MPI::Error("Preconditioner needs to be built with valid references.", CURRENT_FUNCTION);
     geometry = geometry_ref;
     config = config_ref;
@@ -262,32 +245,29 @@ class CLineletPreconditioner final : public CPreconditioner<ScalarType> {
    * \param[in] u - CSysVector that is being preconditioned.
    * \param[out] v - CSysVector that is the result of the preconditioning.
    */
-  inline void operator()(const CSysVector<ScalarType> & u, CSysVector<ScalarType> & v) const override {
+  inline void operator()(const CSysVector<ScalarType>& u, CSysVector<ScalarType>& v) const override {
     sparse_matrix.ComputeLineletPreconditioner(u, v, geometry, config);
   }
 
   /*!
    * \note Request the associated matrix to build the preconditioner.
    */
-  inline void Build() override {
-    sparse_matrix.BuildLineletPreconditioner(geometry, config);
-  }
+  inline void Build() override { sparse_matrix.BuildLineletPreconditioner(geometry, config); }
 };
 
-
 /*!
  * \class CPastixPreconditioner
  * \brief Specialization of preconditioner that uses PaStiX to factorize a CSysMatrix.
  */
-template<class ScalarType>
+template <class ScalarType>
 class CPastixPreconditioner final : public CPreconditioner<ScalarType> {
-private:
+ private:
   CSysMatrix<ScalarType>& sparse_matrix; /*!< \brief Pointer to the matrix. */
   CGeometry* geometry;                   /*!< \brief Geometry associated with the problem. */
-  const CConfig *config;                 /*!< \brief Configuration of the problem. */
+  const CConfig* config;                 /*!< \brief Configuration of the problem. */
   unsigned short kind_fact;              /*!< \brief The type of factorization desired. */
 
-public:
+ public:
   /*!
    * \brief Constructor of the class
    * \param[in] matrix_ref - Matrix reference that will be used to define the preconditioner.
@@ -295,11 +275,10 @@ class CPastixPreconditioner final : public CPreconditioner<ScalarType> {
    * \param[in] config_ref - Problem configuration.
    * \param[in] kind_factorization - Type of factorization required.
    */
-  inline CPastixPreconditioner(CSysMatrix<ScalarType> & matrix_ref, CGeometry *geometry_ref,
-                               const CConfig *config_ref, unsigned short kind_factorization) :
-    sparse_matrix(matrix_ref)
-  {
-    if((geometry_ref == nullptr) || (config_ref == nullptr))
+  inline CPastixPreconditioner(CSysMatrix<ScalarType>& matrix_ref, CGeometry* geometry_ref, const CConfig* config_ref,
+                               unsigned short kind_factorization)
+      : sparse_matrix(matrix_ref) {
+    if ((geometry_ref == nullptr) || (config_ref == nullptr))
       SU2_MPI::Error("Preconditioner needs to be built with valid references.", CURRENT_FUNCTION);
     geometry = geometry_ref;
     config = config_ref;
@@ -316,23 +295,19 @@ class CPastixPreconditioner final : public CPreconditioner<ScalarType> {
    * \param[in] u - CSysVector that is being preconditioned.
    * \param[out] v - CSysVector that is the result of the preconditioning.
    */
-  inline void operator()(const CSysVector<ScalarType> & u, CSysVector<ScalarType> & v) const override {
+  inline void operator()(const CSysVector<ScalarType>& u, CSysVector<ScalarType>& v) const override {
     sparse_matrix.ComputePastixPreconditioner(u, v, geometry, config);
   }
 
   /*!
    * \note Request the associated matrix to build the preconditioner.
    */
-  inline void Build() override {
-    sparse_matrix.BuildPastixPreconditioner(geometry, config, kind_fact);
-  }
+  inline void Build() override { sparse_matrix.BuildPastixPreconditioner(geometry, config, kind_fact); }
 };
 
-
-template<class ScalarType>
+template <class ScalarType>
 CPreconditioner<ScalarType>* CPreconditioner<ScalarType>::Create(ENUM_LINEAR_SOLVER_PREC kind,
-                                                                 CSysMatrix<ScalarType>& jacobian,
-                                                                 CGeometry* geometry,
+                                                                 CSysMatrix<ScalarType>& jacobian, CGeometry* geometry,
                                                                  const CConfig* config) {
   CPreconditioner<ScalarType>* prec = nullptr;
 
@@ -349,7 +324,9 @@ CPreconditioner<ScalarType>* CPreconditioner<ScalarType>::Create(ENUM_LINEAR_SOL
     case ILU:
       prec = new CILUPreconditioner<ScalarType>(jacobian, geometry, config);
       break;
-    case PASTIX_ILU: case PASTIX_LU_P: case PASTIX_LDLT_P:
+    case PASTIX_ILU:
+    case PASTIX_LU_P:
+    case PASTIX_LDLT_P:
       prec = new CPastixPreconditioner<ScalarType>(jacobian, geometry, config, kind);
       break;
   }
@@ -357,4 +334,4 @@ CPreconditioner<ScalarType>* CPreconditioner<ScalarType>::Create(ENUM_LINEAR_SOL
   return prec;
 }
 
-/// @}
\ No newline at end of file
+/// @}
diff --git a/Common/include/linear_algebra/CSysMatrix.hpp b/Common/include/linear_algebra/CSysMatrix.hpp
index d140fc1e6a1..3609c260f8f 100644
--- a/Common/include/linear_algebra/CSysMatrix.hpp
+++ b/Common/include/linear_algebra/CSysMatrix.hpp
@@ -40,7 +40,7 @@
 #if defined(HAVE_MKL) && !defined(CODI_FORWARD_TYPE)
 #include "mkl.h"
 #ifndef __INTEL_MKL__
-  #error Could not determine the MKL version
+#error Could not determine the MKL version
 #endif
 /*--- JIT is only available since 2019. ---*/
 #if __INTEL_MKL__ >= 2019
@@ -50,24 +50,28 @@
  making "getrf" and "getrs" compatible with AD since they are not used as often as "gemm".
 ---*/
 #if defined(__INTEL_COMPILER) && defined(MKL_DIRECT_CALL_SEQ) && !defined(CODI_REVERSE_TYPE)
-  #define USE_MKL_LAPACK
+#define USE_MKL_LAPACK
 #endif
-template<class T>
+template <class T>
 struct mkl_jit_wrapper {
   using gemm_t = dgemm_jit_kernel_t;
-  template<class... Ts>
-  static void create_gemm(Ts&&... args) { mkl_jit_create_dgemm(args...); }
+  template <class... Ts>
+  static void create_gemm(Ts&&... args) {
+    mkl_jit_create_dgemm(args...);
+  }
   static gemm_t get_gemm(void* jitter) { return mkl_jit_get_dgemm_ptr(jitter); }
 };
-template<>
+template <>
 struct mkl_jit_wrapper<float> {
   using gemm_t = sgemm_jit_kernel_t;
-  template<class... Ts>
-  static void create_gemm(Ts&&... args) { mkl_jit_create_sgemm(args...); }
+  template <class... Ts>
+  static void create_gemm(Ts&&... args) {
+    mkl_jit_create_sgemm(args...);
+  }
   static gemm_t get_gemm(void* jitter) { return mkl_jit_get_sgemm_ptr(jitter); }
 };
 #else
-  #warning The current version of MKL does not support JIT gemm kernels
+#warning The current version of MKL does not support JIT gemm kernels
 #endif
 #endif
 
@@ -86,8 +90,8 @@ struct CSysMatrixComms {
    * \param[in] config   - Definition of the particular problem.
    * \param[in] commType - Enumerated type for the quantity to be communicated.
    */
-  template<class T>
-  static void Initiate(const CSysVector<T>& x, CGeometry *geometry, const CConfig *config,
+  template <class T>
+  static void Initiate(const CSysVector<T>& x, CGeometry* geometry, const CConfig* config,
                        unsigned short commType = SOLUTION_MATRIX);
 
   /*!
@@ -98,8 +102,8 @@ struct CSysMatrixComms {
    * \param[in] config   - Definition of the particular problem.
    * \param[in] commType - Enumerated type for the quantity to be unpacked.
    */
-  template<class T>
-  static void Complete(CSysVector<T>& x, CGeometry *geometry, const CConfig *config,
+  template <class T>
+  static void Complete(CSysVector<T>& x, CGeometry* geometry, const CConfig* config,
                        unsigned short commType = SOLUTION_MATRIX);
 };
 
@@ -108,60 +112,66 @@ struct CSysMatrixComms {
  * \ingroup SpLinSys
  * \brief Main class for defining block-compressed-row-storage sparse matrices.
  */
-template<class ScalarType>
+template <class ScalarType>
 class CSysMatrix {
-private:
+ private:
   friend struct CSysMatrixComms;
 
-  const int rank;     /*!< \brief MPI Rank. */
-  const int size;     /*!< \brief MPI Size. */
-
-  enum : size_t { MAXNVAR = 20 };   /*!< \brief Maximum number of variables the matrix can handle. The static
-                                                size is needed for fast, per-thread, static memory allocation. */
-
-  enum { OMP_MAX_SIZE_L = 8192 };   /*!< \brief Max. chunk size used in light parallel for loops. */
-  enum { OMP_MAX_SIZE_H = 512 };    /*!< \brief Max. chunk size used in heavy parallel for loops. */
-  enum { OMP_MIN_SIZE = 32 };       /*!< \brief Chunk size for finer grain operations. */
-  unsigned long omp_light_size;     /*!< \brief Actual chunk size used in light loops (e.g. over non zeros). */
-  unsigned long omp_heavy_size;     /*!< \brief Actual chunk size used in heavy loops (e.g. over rows). */
-  unsigned long omp_num_parts;      /*!< \brief Number of threads used in thread-parallel LU_SGS and ILU. */
-  unsigned long *omp_partitions;    /*!< \brief Point indexes of LU_SGS and ILU thread-parallel sub partitioning. */
-
-  unsigned long nPoint;             /*!< \brief Number of points in the grid. */
-  unsigned long nPointDomain;       /*!< \brief Number of points in the grid (excluding halos). */
-  unsigned long nVar;               /*!< \brief Number of variables (and rows of the blocks). */
-  unsigned long nEqn;               /*!< \brief Number of equations (and columns of the blocks). */
-
-  ScalarType *matrix;               /*!< \brief Entries of the sparse matrix. */
-  unsigned long nnz;                /*!< \brief Number of possible nonzero entries in the matrix. */
-  const unsigned long *row_ptr;     /*!< \brief Pointers to the first element in each row. */
-  const unsigned long *dia_ptr;     /*!< \brief Pointers to the diagonal element in each row. */
-  const unsigned long *col_ind;     /*!< \brief Column index for each of the elements in val(). */
-  const unsigned long *col_ptr;     /*!< \brief The transpose of col_ind, pointer to blocks with the same column index. */
-
-  ScalarType *ILU_matrix;           /*!< \brief Entries of the ILU sparse matrix. */
+  const int rank; /*!< \brief MPI Rank. */
+  const int size; /*!< \brief MPI Size. */
+
+  enum : size_t {
+    MAXNVAR = 20
+  }; /*!< \brief Maximum number of variables the matrix can handle. The static
+                 size is needed for fast, per-thread, static memory allocation. */
+
+  enum { OMP_MAX_SIZE_L = 8192 }; /*!< \brief Max. chunk size used in light parallel for loops. */
+  enum { OMP_MAX_SIZE_H = 512 };  /*!< \brief Max. chunk size used in heavy parallel for loops. */
+  enum { OMP_MIN_SIZE = 32 };     /*!< \brief Chunk size for finer grain operations. */
+  unsigned long omp_light_size;   /*!< \brief Actual chunk size used in light loops (e.g. over non zeros). */
+  unsigned long omp_heavy_size;   /*!< \brief Actual chunk size used in heavy loops (e.g. over rows). */
+  unsigned long omp_num_parts;    /*!< \brief Number of threads used in thread-parallel LU_SGS and ILU. */
+  unsigned long* omp_partitions;  /*!< \brief Point indexes of LU_SGS and ILU thread-parallel sub partitioning. */
+
+  unsigned long nPoint;       /*!< \brief Number of points in the grid. */
+  unsigned long nPointDomain; /*!< \brief Number of points in the grid (excluding halos). */
+  unsigned long nVar;         /*!< \brief Number of variables (and rows of the blocks). */
+  unsigned long nEqn;         /*!< \brief Number of equations (and columns of the blocks). */
+
+  ScalarType* matrix;           /*!< \brief Entries of the sparse matrix. */
+  unsigned long nnz;            /*!< \brief Number of possible nonzero entries in the matrix. */
+  const unsigned long* row_ptr; /*!< \brief Pointers to the first element in each row. */
+  const unsigned long* dia_ptr; /*!< \brief Pointers to the diagonal element in each row. */
+  const unsigned long* col_ind; /*!< \brief Column index for each of the elements in val(). */
+  const unsigned long* col_ptr; /*!< \brief The transpose of col_ind, pointer to blocks with the same column index. */
+
+  ScalarType* ILU_matrix;           /*!< \brief Entries of the ILU sparse matrix. */
   unsigned long nnz_ilu;            /*!< \brief Number of possible nonzero entries in the matrix (ILU). */
-  const unsigned long *row_ptr_ilu; /*!< \brief Pointers to the first element in each row (ILU). */
-  const unsigned long *dia_ptr_ilu; /*!< \brief Pointers to the diagonal element in each row (ILU). */
-  const unsigned long *col_ind_ilu; /*!< \brief Column index for each of the elements in val() (ILU). */
+  const unsigned long* row_ptr_ilu; /*!< \brief Pointers to the first element in each row (ILU). */
+  const unsigned long* dia_ptr_ilu; /*!< \brief Pointers to the diagonal element in each row (ILU). */
+  const unsigned long* col_ind_ilu; /*!< \brief Column index for each of the elements in val() (ILU). */
   unsigned short ilu_fill_in;       /*!< \brief Fill in level for the ILU preconditioner. */
 
-  ScalarType *invM;                 /*!< \brief Inverse of (Jacobi) preconditioner, or diagonal of ILU. */
+  ScalarType* invM; /*!< \brief Inverse of (Jacobi) preconditioner, or diagonal of ILU. */
 
   /*--- Temporary (hence mutable) working memory used in the Linelet preconditioner, outer vector is for threads ---*/
-  mutable vector<vector<const ScalarType*> > LineletUpper; /*!< \brief Pointers to the upper blocks of the tri-diag system (working memory). */
-  mutable vector<vector<ScalarType> > LineletInvDiag;      /*!< \brief Inverse of the diagonal blocks of the tri-diag system (working memory). */
-  mutable vector<vector<ScalarType> > LineletVector;       /*!< \brief Solution and RHS of the tri-diag system (working memory). */
+  mutable vector<vector<const ScalarType*> >
+      LineletUpper; /*!< \brief Pointers to the upper blocks of the tri-diag system (working memory). */
+  mutable vector<vector<ScalarType> >
+      LineletInvDiag; /*!< \brief Inverse of the diagonal blocks of the tri-diag system (working memory). */
+  mutable vector<vector<ScalarType> >
+      LineletVector; /*!< \brief Solution and RHS of the tri-diag system (working memory). */
 
 #ifdef USE_MKL
   using gemm_t = typename mkl_jit_wrapper<ScalarType>::gemm_t;
-  void * MatrixMatrixProductJitter;              /*!< \brief Jitter handle for MKL JIT based GEMM. */
+  void* MatrixMatrixProductJitter;               /*!< \brief Jitter handle for MKL JIT based GEMM. */
   gemm_t MatrixMatrixProductKernel;              /*!< \brief MKL JIT based GEMM kernel. */
-  void * MatrixVectorProductJitterBetaZero;      /*!< \brief Jitter handle for MKL JIT based GEMV. */
+  void* MatrixVectorProductJitterBetaZero;       /*!< \brief Jitter handle for MKL JIT based GEMV. */
   gemm_t MatrixVectorProductKernelBetaZero;      /*!< \brief MKL JIT based GEMV kernel. */
-  void * MatrixVectorProductJitterBetaOne;       /*!< \brief Jitter handle for MKL JIT based GEMV with BETA=1.0. */
+  void* MatrixVectorProductJitterBetaOne;        /*!< \brief Jitter handle for MKL JIT based GEMV with BETA=1.0. */
   gemm_t MatrixVectorProductKernelBetaOne;       /*!< \brief MKL JIT based GEMV kernel with BETA=1.0. */
-  void * MatrixVectorProductJitterAlphaMinusOne; /*!< \brief Jitter handle for MKL JIT based GEMV with ALPHA=-1.0 and BETA=1.0. */
+  void* MatrixVectorProductJitterAlphaMinusOne;  /*!< \brief Jitter handle for MKL JIT based GEMV with ALPHA=-1.0 and
+                                                    BETA=1.0. */
   gemm_t MatrixVectorProductKernelAlphaMinusOne; /*!< \brief MKL JIT based GEMV kernel with ALPHA=-1.0 and BETA=1.0. */
 #endif
 
@@ -173,33 +183,38 @@ class CSysMatrix {
    * \brief Auxilary object to wrap the edge map pointer used in fast block updates, i.e. without linear searches.
    */
   struct {
-    const unsigned long *ptr = nullptr;
+    const unsigned long* ptr = nullptr;
     unsigned long nEdge = 0;
 
     operator bool() { return nEdge != 0; }
 
-    inline unsigned long operator() (unsigned long edge, unsigned long node) const {
-      return ptr[2*edge+node];
-    }
-    inline unsigned long ij(unsigned long edge) const { return ptr[2*edge]; }
-    inline unsigned long ji(unsigned long edge) const { return ptr[2*edge+1]; }
+    inline unsigned long operator()(unsigned long edge, unsigned long node) const { return ptr[2 * edge + node]; }
+    inline unsigned long ij(unsigned long edge) const { return ptr[2 * edge]; }
+    inline unsigned long ji(unsigned long edge) const { return ptr[2 * edge + 1]; }
 
   } edge_ptr;
 
   /*!
-   * \brief Handle type conversion for when we Set, Add, etc. blocks, preserving derivative information (if supported by types).
+   * \brief Handle type conversion for when we Set, Add, etc. blocks, preserving derivative information (if supported by
+   * types).
    */
-  template<class DstType, class SrcType, su2enable_if<std::is_arithmetic<DstType>::value> = 0>
-  FORCEINLINE static DstType ActiveAssign(const SrcType& val) { return SU2_TYPE::GetValue(val); }
+  template <class DstType, class SrcType, su2enable_if<std::is_arithmetic<DstType>::value> = 0>
+  FORCEINLINE static DstType ActiveAssign(const SrcType& val) {
+    return SU2_TYPE::GetValue(val);
+  }
 
-  template<class DstType, class SrcType, su2enable_if<!std::is_arithmetic<DstType>::value> = 0>
-  FORCEINLINE static DstType ActiveAssign(const SrcType& val) { return val; }
+  template <class DstType, class SrcType, su2enable_if<!std::is_arithmetic<DstType>::value> = 0>
+  FORCEINLINE static DstType ActiveAssign(const SrcType& val) {
+    return val;
+  }
 
   /*!
    * \brief Handle type conversion for when we Set, Add, etc. blocks, discarding derivative information.
    */
-  template<class SrcType>
-  FORCEINLINE static ScalarType PassiveAssign(const SrcType& val) { return SU2_TYPE::GetValue(val); }
+  template <class SrcType>
+  FORCEINLINE static ScalarType PassiveAssign(const SrcType& val) {
+    return SU2_TYPE::GetValue(val);
+  }
 
   /*!
    * \brief Calculates the matrix-vector product: product = matrix*vector
@@ -207,7 +222,7 @@ class CSysMatrix {
    * \param[in] vector
    * \param[out] product
    */
-  void MatrixVectorProduct(const ScalarType *matrix, const ScalarType *vector, ScalarType *product) const;
+  void MatrixVectorProduct(const ScalarType* matrix, const ScalarType* vector, ScalarType* product) const;
 
   /*!
    * \brief Calculates the matrix-vector product: product += matrix*vector
@@ -215,7 +230,7 @@ class CSysMatrix {
    * \param[in] vector
    * \param[in,out] product
    */
-  void MatrixVectorProductAdd(const ScalarType *matrix, const ScalarType *vector, ScalarType *product) const;
+  void MatrixVectorProductAdd(const ScalarType* matrix, const ScalarType* vector, ScalarType* product) const;
 
   /*!
    * \brief Calculates the matrix-vector product: product -= matrix*vector
@@ -223,37 +238,34 @@ class CSysMatrix {
    * \param[in] vector
    * \param[in,out] product
    */
-  void MatrixVectorProductSub(const ScalarType *matrix, const ScalarType *vector, ScalarType *product) const;
+  void MatrixVectorProductSub(const ScalarType* matrix, const ScalarType* vector, ScalarType* product) const;
 
   /*!
    * \brief Calculates the matrix-matrix product
    */
-  void MatrixMatrixProduct(const ScalarType *matrix_a, const ScalarType *matrix_b, ScalarType *product) const;
+  void MatrixMatrixProduct(const ScalarType* matrix_a, const ScalarType* matrix_b, ScalarType* product) const;
 
   /*!
    * \brief Subtract b from a and store the result in c.
    */
-  FORCEINLINE void VectorSubtraction(const ScalarType *a, const ScalarType *b, ScalarType *c) const {
-    for(unsigned long iVar = 0; iVar < nVar; iVar++)
-      c[iVar] = a[iVar] - b[iVar];
+  FORCEINLINE void VectorSubtraction(const ScalarType* a, const ScalarType* b, ScalarType* c) const {
+    for (unsigned long iVar = 0; iVar < nVar; iVar++) c[iVar] = a[iVar] - b[iVar];
   }
 
   /*!
    * \brief Subtract b from a and store the result in c.
    */
-  FORCEINLINE void MatrixSubtraction(const ScalarType *a, const ScalarType *b, ScalarType *c) const {
+  FORCEINLINE void MatrixSubtraction(const ScalarType* a, const ScalarType* b, ScalarType* c) const {
     SU2_OMP_SIMD
-    for(unsigned long iVar = 0; iVar < nVar*nEqn; iVar++)
-      c[iVar] = a[iVar] - b[iVar];
+    for (unsigned long iVar = 0; iVar < nVar * nEqn; iVar++) c[iVar] = a[iVar] - b[iVar];
   }
 
   /*!
    * \brief Copy matrix src into dst, transpose if required.
    */
-  FORCEINLINE void MatrixCopy(const ScalarType *src, ScalarType *dst) const {
+  FORCEINLINE void MatrixCopy(const ScalarType* src, ScalarType* dst) const {
     SU2_OMP_SIMD
-    for(auto iVar = 0ul; iVar < nVar*nEqn; ++iVar)
-      dst[iVar] = src[iVar];
+    for (auto iVar = 0ul; iVar < nVar * nEqn; ++iVar) dst[iVar] = src[iVar];
   }
 
   /*!
@@ -268,7 +280,7 @@ class CSysMatrix {
    * \param[in,out] matrix - On entry the system matrix, on exit the factorized matrix.
    * \param[out] inverse - the matrix inverse.
    */
-  void MatrixInverse(ScalarType *matrix, ScalarType *inverse) const;
+  void MatrixInverse(ScalarType* matrix, ScalarType* inverse) const;
 
   /*!
    * \brief Performs the Gauss Elimination algorithm to solve the linear subsystem of the (i,i) subblock and rhs.
@@ -283,21 +295,21 @@ class CSysMatrix {
    * \param[in] block_i - Indexes of the block in the matrix-by-blocks structure.
    * \param[out] invBlock - Inverse block.
    */
-  inline void InverseDiagonalBlock(unsigned long block_i, ScalarType *invBlock) const;
+  inline void InverseDiagonalBlock(unsigned long block_i, ScalarType* invBlock) const;
 
   /*!
    * \brief Inverse diagonal block.
    * \param[in] block_i - Indexes of the block in the matrix-by-blocks structure.
    * \param[out] invBlock - Inverse block.
    */
-  inline void InverseDiagonalBlock_ILUMatrix(unsigned long block_i, ScalarType *invBlock) const;
+  inline void InverseDiagonalBlock_ILUMatrix(unsigned long block_i, ScalarType* invBlock) const;
 
   /*!
    * \brief Copies the block (i, j) of the matrix-by-blocks structure in the internal variable *block.
    * \param[in] block_i - Indexes of the block in the matrix-by-blocks structure.
    * \param[in] block_j - Indexes of the block in the matrix-by-blocks structure.
    */
-  inline ScalarType *GetBlock_ILUMatrix(unsigned long block_i, unsigned long block_j);
+  inline ScalarType* GetBlock_ILUMatrix(unsigned long block_i, unsigned long block_j);
 
   /*!
    * \brief Set the value of a block in the sparse matrix.
@@ -305,7 +317,7 @@ class CSysMatrix {
    * \param[in] block_j - Indexes of the block in the matrix-by-blocks structure.
    * \param[in] **val_block - Block to set to A(i, j).
    */
-  inline void SetBlock_ILUMatrix(unsigned long block_i, unsigned long block_j, ScalarType *val_block);
+  inline void SetBlock_ILUMatrix(unsigned long block_i, unsigned long block_j, ScalarType* val_block);
 
   /*!
    * \brief Performs the product of i-th row of the upper part of a sparse matrix by a vector.
@@ -314,8 +326,8 @@ class CSysMatrix {
    * \param[in] col_ub - Exclusive upper bound for column indices considered in multiplication.
    * \param[out] prod - Result of the product U(A)*vec.
    */
-  inline void UpperProduct(const CSysVector<ScalarType> & vec, unsigned long row_i,
-                           unsigned long col_ub, ScalarType *prod) const;
+  inline void UpperProduct(const CSysVector<ScalarType>& vec, unsigned long row_i, unsigned long col_ub,
+                           ScalarType* prod) const;
 
   /*!
    * \brief Performs the product of i-th row of the lower part of a sparse matrix by a vector.
@@ -324,8 +336,8 @@ class CSysMatrix {
    * \param[in] col_lb - Inclusive lower bound for column indices considered in multiplication.
    * \param[out] prod - Result of the product L(A)*vec.
    */
-  inline void LowerProduct(const CSysVector<ScalarType> & vec, unsigned long row_i,
-                           unsigned long col_lb, ScalarType *prod) const;
+  inline void LowerProduct(const CSysVector<ScalarType>& vec, unsigned long row_i, unsigned long col_lb,
+                           ScalarType* prod) const;
 
   /*!
    * \brief Performs the product of i-th row of the diagonal part of a sparse matrix by a vector.
@@ -333,7 +345,7 @@ class CSysMatrix {
    * \param[in] row_i - Row of the matrix to be multiplied by vector vec.
    * \return prod Result of the product D(A)*vec (stored at *prod_row_vector).
    */
-  inline void DiagonalProduct(const CSysVector<ScalarType> & vec, unsigned long row_i, ScalarType *prod) const;
+  inline void DiagonalProduct(const CSysVector<ScalarType>& vec, unsigned long row_i, ScalarType* prod) const;
 
   /*!
    * \brief Performs the product of i-th row of a sparse matrix by a vector.
@@ -341,10 +353,9 @@ class CSysMatrix {
    * \param[in] row_i - Row of the matrix to be multiplied by vector vec.
    * \return Result of the product (stored at *prod_row_vector).
    */
-  void RowProduct(const CSysVector<ScalarType> & vec, unsigned long row_i, ScalarType *prod) const;
-
-public:
+  void RowProduct(const CSysVector<ScalarType>& vec, unsigned long row_i, ScalarType* prod) const;
 
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -366,10 +377,9 @@ class CSysMatrix {
    * \param[in] config - Definition of the particular problem.
    * \param[in] needTranspPtr - If "col_ptr" should be created, used for "SetDiagonalAsColumnSum".
    */
-  void Initialize(unsigned long npoint, unsigned long npointdomain,
-                  unsigned short nvar, unsigned short neqn,
-                  bool EdgeConnect, CGeometry *geometry,
-                  const CConfig *config, bool needTranspPtr = false, bool grad_mode = false);
+  void Initialize(unsigned long npoint, unsigned long npointdomain, unsigned short nvar, unsigned short neqn,
+                  bool EdgeConnect, CGeometry* geometry, const CConfig* config, bool needTranspPtr = false,
+                  bool grad_mode = false);
 
   /*!
    * \brief Sets to zero all the entries of the sparse matrix.
@@ -387,21 +397,20 @@ class CSysMatrix {
    * \param[in] block_j - Column index.
    * \return Pointer to location in memory where the block starts.
    */
-  FORCEINLINE const ScalarType *GetBlock(unsigned long block_i, unsigned long block_j) const {
+  FORCEINLINE const ScalarType* GetBlock(unsigned long block_i, unsigned long block_j) const {
     /*--- The position of the diagonal block is known which allows halving the search space. ---*/
-    const auto end = (block_j<block_i)? dia_ptr[block_i] : row_ptr[block_i+1];
-    for (auto index = (block_j<block_i)? row_ptr[block_i] : dia_ptr[block_i]; index < end; ++index)
-      if (col_ind[index] == block_j)
-        return &matrix[index*nVar*nEqn];
+    const auto end = (block_j < block_i) ? dia_ptr[block_i] : row_ptr[block_i + 1];
+    for (auto index = (block_j < block_i) ? row_ptr[block_i] : dia_ptr[block_i]; index < end; ++index)
+      if (col_ind[index] == block_j) return &matrix[index * nVar * nEqn];
     return nullptr;
   }
 
   /*!
    * \brief Get a pointer to the start of block "ij", non-const version
    */
-  FORCEINLINE ScalarType *GetBlock(unsigned long block_i, unsigned long block_j) {
+  FORCEINLINE ScalarType* GetBlock(unsigned long block_i, unsigned long block_j) {
     const CSysMatrix& const_this = *this;
-    return const_cast<ScalarType*>( const_this.GetBlock(block_i, block_j) );
+    return const_cast<ScalarType*>(const_this.GetBlock(block_i, block_j));
   }
 
   /*!
@@ -412,11 +421,11 @@ class CSysMatrix {
    * \param[in] jVar - Column of the block.
    * \return Value of the block entry.
    */
-  FORCEINLINE ScalarType GetBlock(unsigned long block_i, unsigned long block_j,
-                                  unsigned short iVar, unsigned short jVar) const {
+  FORCEINLINE ScalarType GetBlock(unsigned long block_i, unsigned long block_j, unsigned short iVar,
+                                  unsigned short jVar) const {
     auto mat_ij = GetBlock(block_i, block_j);
     if (!mat_ij) return 0.0;
-    return mat_ij[iVar*nEqn+jVar];
+    return mat_ij[iVar * nEqn + jVar];
   }
 
   /*!
@@ -427,16 +436,14 @@ class CSysMatrix {
    * \param[in] val_block - Block to set to A(i, j).
    * \param[in] alpha - Scale factor.
    */
-  template<class OtherType, bool Overwrite = true,
-           su2enable_if<!is_pointer<OtherType>::value> = 0>
-  inline void SetBlock(unsigned long block_i, unsigned long block_j,
-                       const OtherType *val_block, OtherType alpha = 1.0) {
-
+  template <class OtherType, bool Overwrite = true, su2enable_if<!is_pointer<OtherType>::value> = 0>
+  inline void SetBlock(unsigned long block_i, unsigned long block_j, const OtherType* val_block,
+                       OtherType alpha = 1.0) {
     auto mat_ij = GetBlock(block_i, block_j);
     if (!mat_ij) return;
     SU2_OMP_SIMD
-    for (auto iVar = 0ul; iVar < nVar*nEqn; ++iVar) {
-      mat_ij[iVar] = (Overwrite? ScalarType(0) : mat_ij[iVar]) + PassiveAssign(alpha * val_block[iVar]);
+    for (auto iVar = 0ul; iVar < nVar * nEqn; ++iVar) {
+      mat_ij[iVar] = (Overwrite ? ScalarType(0) : mat_ij[iVar]) + PassiveAssign(alpha * val_block[iVar]);
     }
   }
 
@@ -447,10 +454,10 @@ class CSysMatrix {
    * \param[in] val_block - Block to set to A(i, j).
    * \param[in] alpha - Scale factor.
    */
-  template<class OtherType, su2enable_if<!is_pointer<OtherType>::value> = 0>
-  inline void AddBlock(unsigned long block_i, unsigned long block_j,
-                       const OtherType *val_block, OtherType alpha = 1.0) {
-    SetBlock<OtherType,false>(block_i, block_j, val_block, alpha);
+  template <class OtherType, su2enable_if<!is_pointer<OtherType>::value> = 0>
+  inline void AddBlock(unsigned long block_i, unsigned long block_j, const OtherType* val_block,
+                       OtherType alpha = 1.0) {
+    SetBlock<OtherType, false>(block_i, block_j, val_block, alpha);
   }
 
   /*!
@@ -461,15 +468,14 @@ class CSysMatrix {
    * \param[in] val_block - Block to set to A(i, j).
    * \param[in] alpha - Scale factor.
    */
-  template<class OtherType, bool Overwrite = true>
-  inline void SetBlock(unsigned long block_i, unsigned long block_j,
-                       const OtherType* const* val_block, OtherType alpha = 1.0) {
-
+  template <class OtherType, bool Overwrite = true>
+  inline void SetBlock(unsigned long block_i, unsigned long block_j, const OtherType* const* val_block,
+                       OtherType alpha = 1.0) {
     auto mat_ij = GetBlock(block_i, block_j);
     if (!mat_ij) return;
     for (auto iVar = 0ul; iVar < nVar; ++iVar) {
       for (auto jVar = 0ul; jVar < nEqn; ++jVar) {
-        *mat_ij = (Overwrite? ScalarType(0) : *mat_ij) + PassiveAssign(alpha * val_block[iVar][jVar]);
+        *mat_ij = (Overwrite ? ScalarType(0) : *mat_ij) + PassiveAssign(alpha * val_block[iVar][jVar]);
         ++mat_ij;
       }
     }
@@ -482,10 +488,10 @@ class CSysMatrix {
    * \param[in] val_block - Block to add to A(i, j).
    * \param[in] alpha - Scale factor.
    */
-  template<class OtherType>
-  inline void AddBlock(unsigned long block_i, unsigned long block_j,
-                       const OtherType* const* val_block, OtherType alpha = 1.0) {
-    SetBlock<OtherType,false>(block_i, block_j, val_block, alpha);
+  template <class OtherType>
+  inline void AddBlock(unsigned long block_i, unsigned long block_j, const OtherType* const* val_block,
+                       OtherType alpha = 1.0) {
+    SetBlock<OtherType, false>(block_i, block_j, val_block, alpha);
   }
 
   /*!
@@ -494,7 +500,7 @@ class CSysMatrix {
    * \param[in] block_j - Column index.
    * \param[in] val_block - Block to subtract to A(i, j).
    */
-  template<class OtherType>
+  template <class OtherType>
   inline void SubtractBlock(unsigned long block_i, unsigned long block_j, const OtherType* const* val_block) {
     AddBlock(block_i, block_j, val_block, OtherType(-1));
   }
@@ -545,14 +551,13 @@ class CSysMatrix {
    * \param[in] block_j - Adds to ij, subs from jj.
    * \param[in] scale - Scale blocks during update (axpy type op).
    */
-  template<class MatrixType, class OtherType = ScalarType>
-  inline void UpdateBlocks(unsigned long iEdge, unsigned long iPoint, unsigned long jPoint,
-                           const MatrixType& block_i, const MatrixType& block_j, OtherType scale = 1) {
-
-    ScalarType *bii = &matrix[dia_ptr[iPoint]*nVar*nEqn];
-    ScalarType *bjj = &matrix[dia_ptr[jPoint]*nVar*nEqn];
-    ScalarType *bij = &matrix[edge_ptr(iEdge,0)*nVar*nEqn];
-    ScalarType *bji = &matrix[edge_ptr(iEdge,1)*nVar*nEqn];
+  template <class MatrixType, class OtherType = ScalarType>
+  inline void UpdateBlocks(unsigned long iEdge, unsigned long iPoint, unsigned long jPoint, const MatrixType& block_i,
+                           const MatrixType& block_j, OtherType scale = 1) {
+    ScalarType* bii = &matrix[dia_ptr[iPoint] * nVar * nEqn];
+    ScalarType* bjj = &matrix[dia_ptr[jPoint] * nVar * nEqn];
+    ScalarType* bij = &matrix[edge_ptr(iEdge, 0) * nVar * nEqn];
+    ScalarType* bji = &matrix[edge_ptr(iEdge, 1) * nVar * nEqn];
 
     unsigned long iVar, jVar, offset = 0;
 
@@ -570,51 +575,50 @@ class CSysMatrix {
   /*!
    * \brief Short-hand for the "subtractive" version (sub from i* add to j*) of UpdateBlocks.
    */
-  template<class MatrixType>
+  template <class MatrixType>
   inline void UpdateBlocksSub(unsigned long iEdge, unsigned long iPoint, unsigned long jPoint,
                               const MatrixType& block_i, const MatrixType& block_j) {
-    UpdateBlocks<MatrixType,ScalarType>(iEdge, iPoint, jPoint, block_i, block_j, -1);
+    UpdateBlocks<MatrixType, ScalarType>(iEdge, iPoint, jPoint, block_i, block_j, -1);
   }
 
   /*!
    * \brief SIMD version, does the update for multiple edges and points.
    * \note Nothing is updated if the mask is 0.
    */
-  template<class MatTypeSIMD, size_t N, class I, class F = ScalarType>
-  FORCEINLINE void UpdateBlocks(simd::Array<I,N> iEdge, simd::Array<I,N> iPoint, simd::Array<I,N> jPoint,
-                                const MatTypeSIMD& block_i, const MatTypeSIMD& block_j, simd::Array<F,N> mask = 1) {
-
+  template <class MatTypeSIMD, size_t N, class I, class F = ScalarType>
+  FORCEINLINE void UpdateBlocks(simd::Array<I, N> iEdge, simd::Array<I, N> iPoint, simd::Array<I, N> jPoint,
+                                const MatTypeSIMD& block_i, const MatTypeSIMD& block_j, simd::Array<F, N> mask = 1) {
     static_assert(MatTypeSIMD::StaticSize, "This method requires static size blocks.");
     static_assert(MatTypeSIMD::IsRowMajor, "Block storage is not compatible with matrix.");
     constexpr size_t blkSz = MatTypeSIMD::StaticSize;
-    assert(blkSz == nVar*nEqn);
+    assert(blkSz == nVar * nEqn);
 
     /*--- "Transpose" the blocks, scale, and possibly convert types,
      * giving the compiler the chance to vectorize all of these. ---*/
     ScalarType blk_i[N][blkSz], blk_j[N][blkSz];
 
-    for (size_t i=0; i<blkSz; ++i) {
+    for (size_t i = 0; i < blkSz; ++i) {
       SU2_OMP_SIMD_IF_NOT_AD
-      for (size_t k=0; k<N; ++k) {
+      for (size_t k = 0; k < N; ++k) {
         blk_i[k][i] = PassiveAssign(-mask[k] * block_i.data()[i][k]);
         blk_j[k][i] = PassiveAssign(mask[k] * block_j.data()[i][k]);
       }
     }
 
     /*--- Update one by one skipping if mask is 0. ---*/
-    for (size_t k=0; k<N; ++k) {
-      if (mask[k]==0) continue;
+    for (size_t k = 0; k < N; ++k) {
+      if (mask[k] == 0) continue;
 
       /*--- Fetch the blocks. ---*/
-      auto bii = &matrix[dia_ptr[iPoint[k]]*blkSz];
-      auto bjj = &matrix[dia_ptr[jPoint[k]]*blkSz];
-      auto bij = &matrix[edge_ptr(iEdge[k],0)*blkSz];
-      auto bji = &matrix[edge_ptr(iEdge[k],1)*blkSz];
+      auto bii = &matrix[dia_ptr[iPoint[k]] * blkSz];
+      auto bjj = &matrix[dia_ptr[jPoint[k]] * blkSz];
+      auto bij = &matrix[edge_ptr(iEdge[k], 0) * blkSz];
+      auto bji = &matrix[edge_ptr(iEdge[k], 1) * blkSz];
 
       /*--- Update, block i was negated during transpose in the
        * hope the assignments below become non-temporal stores. ---*/
       SU2_OMP_SIMD
-      for (size_t i=0; i<blkSz; ++i) {
+      for (size_t i = 0; i < blkSz; ++i) {
         bii[i] -= blk_i[k][i];
         bjj[i] -= blk_j[k][i];
         bij[i] = blk_j[k][i];
@@ -633,19 +637,18 @@ class CSysMatrix {
    * \param[in] block_j - Adds to ij.
    * \param[in] scale - Scale blocks during update (axpy type op).
    */
-  template<class MatrixType, class OtherType = ScalarType, bool Overwrite = true>
-  inline void SetBlocks(unsigned long iEdge, const MatrixType& block_i,
-                        const MatrixType& block_j, OtherType scale = 1) {
-
-    ScalarType *bij = &matrix[edge_ptr(iEdge,0)*nVar*nEqn];
-    ScalarType *bji = &matrix[edge_ptr(iEdge,1)*nVar*nEqn];
+  template <class MatrixType, class OtherType = ScalarType, bool Overwrite = true>
+  inline void SetBlocks(unsigned long iEdge, const MatrixType& block_i, const MatrixType& block_j,
+                        OtherType scale = 1) {
+    ScalarType* bij = &matrix[edge_ptr(iEdge, 0) * nVar * nEqn];
+    ScalarType* bji = &matrix[edge_ptr(iEdge, 1) * nVar * nEqn];
 
     unsigned long iVar, jVar, offset = 0;
 
     for (iVar = 0; iVar < nVar; iVar++) {
       for (jVar = 0; jVar < nEqn; jVar++) {
-        bij[offset] = (Overwrite? ScalarType(0) : bij[offset]) + PassiveAssign(block_j[iVar][jVar] * scale);
-        bji[offset] = (Overwrite? ScalarType(0) : bji[offset]) - PassiveAssign(block_i[iVar][jVar] * scale);
+        bij[offset] = (Overwrite ? ScalarType(0) : bij[offset]) + PassiveAssign(block_j[iVar][jVar] * scale);
+        bji[offset] = (Overwrite ? ScalarType(0) : bji[offset]) - PassiveAssign(block_i[iVar][jVar] * scale);
         ++offset;
       }
     }
@@ -654,57 +657,56 @@ class CSysMatrix {
   /*!
    * \brief Short-hand for the "additive overwrite" version of SetBlocks.
    */
-  template<class MatrixType, class OtherType = ScalarType>
-  inline void UpdateBlocks(unsigned long iEdge, const MatrixType& block_i,
-                           const MatrixType& block_j, OtherType scale = 1) {
-    SetBlocks<MatrixType,OtherType,false>(iEdge, block_i, block_j, scale);
+  template <class MatrixType, class OtherType = ScalarType>
+  inline void UpdateBlocks(unsigned long iEdge, const MatrixType& block_i, const MatrixType& block_j,
+                           OtherType scale = 1) {
+    SetBlocks<MatrixType, OtherType, false>(iEdge, block_i, block_j, scale);
   }
 
   /*!
    * \brief Short-hand for the "subtractive" version (sub from i* add to j*) of SetBlocks.
    */
-  template<class MatrixType>
+  template <class MatrixType>
   inline void UpdateBlocksSub(unsigned long iEdge, const MatrixType& block_i, const MatrixType& block_j) {
-    SetBlocks<MatrixType,ScalarType,false>(iEdge, block_i, block_j, -1);
+    SetBlocks<MatrixType, ScalarType, false>(iEdge, block_i, block_j, -1);
   }
 
   /*!
    * \brief SIMD version, does the update for multiple edges.
    * \note Nothing is updated if the mask is 0.
    */
-  template<class MatTypeSIMD, size_t N, class I, class F = ScalarType>
-  FORCEINLINE void SetBlocks(simd::Array<I,N> iEdge, const MatTypeSIMD& block_i,
-                             const MatTypeSIMD& block_j, simd::Array<F,N> mask = 1) {
-
+  template <class MatTypeSIMD, size_t N, class I, class F = ScalarType>
+  FORCEINLINE void SetBlocks(simd::Array<I, N> iEdge, const MatTypeSIMD& block_i, const MatTypeSIMD& block_j,
+                             simd::Array<F, N> mask = 1) {
     static_assert(MatTypeSIMD::StaticSize, "This method requires static size blocks.");
     static_assert(MatTypeSIMD::IsRowMajor, "Block storage is not compatible with matrix.");
     constexpr size_t blkSz = MatTypeSIMD::StaticSize;
-    assert(blkSz == nVar*nEqn);
+    assert(blkSz == nVar * nEqn);
 
     /*--- "Transpose" the blocks, scale, and possibly convert types,
      * giving the compiler the chance to vectorize all of these. ---*/
     ScalarType blk_i[N][blkSz], blk_j[N][blkSz];
 
-    for (size_t i=0; i<blkSz; ++i) {
+    for (size_t i = 0; i < blkSz; ++i) {
       SU2_OMP_SIMD_IF_NOT_AD
-      for (size_t k=0; k<N; ++k) {
+      for (size_t k = 0; k < N; ++k) {
         blk_i[k][i] = PassiveAssign(-mask[k] * block_i.data()[i][k]);
         blk_j[k][i] = PassiveAssign(mask[k] * block_j.data()[i][k]);
       }
     }
 
     /*--- Update one by one skipping if mask is 0. ---*/
-    for (size_t k=0; k<N; ++k) {
-      if (mask[k]==0) continue;
+    for (size_t k = 0; k < N; ++k) {
+      if (mask[k] == 0) continue;
 
       /*--- Fetch the blocks. ---*/
-      auto bij = &matrix[edge_ptr(iEdge[k],0)*blkSz];
-      auto bji = &matrix[edge_ptr(iEdge[k],1)*blkSz];
+      auto bij = &matrix[edge_ptr(iEdge[k], 0) * blkSz];
+      auto bji = &matrix[edge_ptr(iEdge[k], 1) * blkSz];
 
       /*--- Update, block i was negated during transpose in the
        * hope the assignments below become non-temporal stores. ---*/
       SU2_OMP_SIMD
-      for (size_t i=0; i<blkSz; ++i) {
+      for (size_t i = 0; i < blkSz; ++i) {
         bij[i] = blk_j[k][i];
         bji[i] = blk_i[k][i];
       }
@@ -719,14 +721,13 @@ class CSysMatrix {
    * \param[in] val_block - Block to add to the diagonal of the matrix.
    * \param[in] alpha - Scale factor.
    */
-  template<class OtherType, bool Overwrite = true, class T = ScalarType>
+  template <class OtherType, bool Overwrite = true, class T = ScalarType>
   inline void SetBlock2Diag(unsigned long block_i, const OtherType& val_block, T alpha = 1.0) {
-
-    auto mat_ii = &matrix[dia_ptr[block_i]*nVar*nEqn];
+    auto mat_ii = &matrix[dia_ptr[block_i] * nVar * nEqn];
 
     for (auto iVar = 0ul; iVar < nVar; iVar++)
       for (auto jVar = 0ul; jVar < nEqn; jVar++) {
-        *mat_ii = (Overwrite? ScalarType(0) : *mat_ii) + PassiveAssign(alpha * val_block[iVar][jVar]);
+        *mat_ii = (Overwrite ? ScalarType(0) : *mat_ii) + PassiveAssign(alpha * val_block[iVar][jVar]);
         ++mat_ii;
       }
   }
@@ -734,15 +735,15 @@ class CSysMatrix {
   /*!
    * \brief Non overwrite version of SetBlock2Diag, also with scaling.
    */
-  template<class OtherType, class T = ScalarType>
+  template <class OtherType, class T = ScalarType>
   inline void AddBlock2Diag(unsigned long block_i, const OtherType& val_block, T alpha = 1.0) {
-    SetBlock2Diag<OtherType,false>(block_i, val_block, alpha);
+    SetBlock2Diag<OtherType, false>(block_i, val_block, alpha);
   }
 
   /*!
    * \brief Short-hand to AddBlock2Diag with alpha = -1, i.e. subtracts from the current diagonal.
    */
-  template<class OtherType>
+  template <class OtherType>
   inline void SubtractBlock2Diag(unsigned long block_i, const OtherType& val_block) {
     AddBlock2Diag(block_i, val_block, -1.0);
   }
@@ -753,10 +754,10 @@ class CSysMatrix {
    * \param[in] block_i - Diagonal index.
    * \param[in] val_matrix - Value to add to the diagonal elements of A(i, i).
    */
-  template<class OtherType>
+  template <class OtherType>
   inline void AddVal2Diag(unsigned long block_i, OtherType val_matrix) {
     for (auto iVar = 0ul; iVar < nVar; iVar++)
-      matrix[dia_ptr[block_i]*nVar*nVar + iVar*(nVar+1)] += PassiveAssign(val_matrix);
+      matrix[dia_ptr[block_i] * nVar * nVar + iVar * (nVar + 1)] += PassiveAssign(val_matrix);
   }
 
   /*!
@@ -766,9 +767,9 @@ class CSysMatrix {
    * \param[in] iVar - Variable index.
    * \param[in] val - Value to add to the diagonal elements of A(i, i).
    */
-  template<class OtherType>
+  template <class OtherType>
   inline void AddVal2Diag(unsigned long block_i, unsigned long iVar, OtherType val) {
-    matrix[dia_ptr[block_i]*nVar*nVar + iVar*(nVar+1)] += PassiveAssign(val);
+    matrix[dia_ptr[block_i] * nVar * nVar + iVar * (nVar + 1)] += PassiveAssign(val);
   }
 
   /*!
@@ -777,18 +778,15 @@ class CSysMatrix {
    * \param[in] block_i - Diagonal index.
    * \param[in] val_matrix - Value to add to the diagonal elements of A(i, i).
    */
-  template<class OtherType>
+  template <class OtherType>
   inline void SetVal2Diag(unsigned long block_i, OtherType val_matrix) {
-
-    unsigned long iVar, index = dia_ptr[block_i]*nVar*nVar;
+    unsigned long iVar, index = dia_ptr[block_i] * nVar * nVar;
 
     /*--- Clear entire block before setting its diagonal. ---*/
     SU2_OMP_SIMD
-    for (iVar = 0; iVar < nVar*nVar; iVar++)
-      matrix[index+iVar] = 0.0;
+    for (iVar = 0; iVar < nVar * nVar; iVar++) matrix[index + iVar] = 0.0;
 
-    for (iVar = 0; iVar < nVar; iVar++)
-      matrix[index+iVar*(nVar+1)] = PassiveAssign(val_matrix);
+    for (iVar = 0; iVar < nVar; iVar++) matrix[index + iVar * (nVar + 1)] = PassiveAssign(val_matrix);
   }
 
   /*!
@@ -803,14 +801,14 @@ class CSysMatrix {
    * \param[in] x_i - Values to enforce (nVar sized).
    * \param[in,out] b - The rhs vector (b := b - A_{*,i} * x_i;  b_i = x_i).
    */
-  template<class OtherType>
-  void EnforceSolutionAtNode(unsigned long node_i, const OtherType *x_i, CSysVector<OtherType> & b);
+  template <class OtherType>
+  void EnforceSolutionAtNode(unsigned long node_i, const OtherType* x_i, CSysVector<OtherType>& b);
 
   /*!
    * \brief Version of EnforceSolutionAtNode for a single degree of freedom.
    */
-  template<class OtherType>
-  void EnforceSolutionAtDOF(unsigned long node_i, unsigned long iVar, OtherType x_i, CSysVector<OtherType> & b);
+  template <class OtherType>
+  void EnforceSolutionAtDOF(unsigned long node_i, unsigned long iVar, OtherType x_i, CSysVector<OtherType>& b);
 
   /*!
    * \brief Sets the diagonal entries of the matrix as the sum of the blocks in the corresponding column.
@@ -837,8 +835,8 @@ class CSysMatrix {
    * \param[in] config - Definition of the particular problem.
    * \param[out] prod - Result of the product.
    */
-  void MatrixVectorProduct(const CSysVector<ScalarType> & vec, CSysVector<ScalarType> & prod,
-                           CGeometry *geometry, const CConfig *config) const;
+  void MatrixVectorProduct(const CSysVector<ScalarType>& vec, CSysVector<ScalarType>& prod, CGeometry* geometry,
+                           const CConfig* config) const;
 
   /*!
    * \brief Build the Jacobi preconditioner.
@@ -852,8 +850,8 @@ class CSysMatrix {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void ComputeJacobiPreconditioner(const CSysVector<ScalarType> & vec, CSysVector<ScalarType> & prod,
-                                   CGeometry *geometry, const CConfig *config) const;
+  void ComputeJacobiPreconditioner(const CSysVector<ScalarType>& vec, CSysVector<ScalarType>& prod, CGeometry* geometry,
+                                   const CConfig* config) const;
 
   /*!
    * \brief Build the ILU preconditioner.
@@ -867,31 +865,31 @@ class CSysMatrix {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void ComputeILUPreconditioner(const CSysVector<ScalarType> & vec, CSysVector<ScalarType> & prod,
-                                CGeometry *geometry, const CConfig *config) const;
+  void ComputeILUPreconditioner(const CSysVector<ScalarType>& vec, CSysVector<ScalarType>& prod, CGeometry* geometry,
+                                const CConfig* config) const;
 
   /*!
    * \brief Multiply CSysVector by the preconditioner
    * \param[in] vec - CSysVector to be multiplied by the preconditioner.
    * \param[out] prod - Result of the product A*vec.
    */
-  void ComputeLU_SGSPreconditioner(const CSysVector<ScalarType> & vec, CSysVector<ScalarType> & prod,
-                                   CGeometry *geometry, const CConfig *config) const;
+  void ComputeLU_SGSPreconditioner(const CSysVector<ScalarType>& vec, CSysVector<ScalarType>& prod, CGeometry* geometry,
+                                   const CConfig* config) const;
 
   /*!
    * \brief Build the Linelet preconditioner.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void BuildLineletPreconditioner(const CGeometry *geometry, const CConfig *config);
+  void BuildLineletPreconditioner(const CGeometry* geometry, const CConfig* config);
 
   /*!
    * \brief Multiply CSysVector by the preconditioner
    * \param[in] vec - CSysVector to be multiplied by the preconditioner.
    * \param[out] prod - Result of the product A*vec.
    */
-  void ComputeLineletPreconditioner(const CSysVector<ScalarType> & vec, CSysVector<ScalarType> & prod,
-                                    CGeometry *geometry, const CConfig *config) const;
+  void ComputeLineletPreconditioner(const CSysVector<ScalarType>& vec, CSysVector<ScalarType>& prod,
+                                    CGeometry* geometry, const CConfig* config) const;
 
   /*!
    * \brief Compute the linear residual.
@@ -899,8 +897,8 @@ class CSysMatrix {
    * \param[in] f - Right hand side (b).
    * \param[out] res - Residual (Ax-b).
    */
-  void ComputeResidual(const CSysVector<ScalarType> & sol, const CSysVector<ScalarType> & f,
-                       CSysVector<ScalarType> & res) const;
+  void ComputeResidual(const CSysVector<ScalarType>& sol, const CSysVector<ScalarType>& f,
+                       CSysVector<ScalarType>& res) const;
 
   /*!
    * \brief Factorize matrix using PaStiX.
@@ -908,7 +906,7 @@ class CSysMatrix {
    * \param[in] config - Definition of the particular problem.
    * \param[in] kind_fact - Type of factorization.
    */
-  void BuildPastixPreconditioner(CGeometry *geometry, const CConfig *config, unsigned short kind_fact);
+  void BuildPastixPreconditioner(CGeometry* geometry, const CConfig* config, unsigned short kind_fact);
 
   /*!
    * \brief Apply the PaStiX factorization to CSysVec.
@@ -917,7 +915,6 @@ class CSysMatrix {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void ComputePastixPreconditioner(const CSysVector<ScalarType> & vec, CSysVector<ScalarType> & prod,
-                                   CGeometry *geometry, const CConfig *config) const;
-
+  void ComputePastixPreconditioner(const CSysVector<ScalarType>& vec, CSysVector<ScalarType>& prod, CGeometry* geometry,
+                                   const CConfig* config) const;
 };
diff --git a/Common/include/linear_algebra/CSysMatrix.inl b/Common/include/linear_algebra/CSysMatrix.inl
index 139a6b0f45b..9fe0626119c 100644
--- a/Common/include/linear_algebra/CSysMatrix.inl
+++ b/Common/include/linear_algebra/CSysMatrix.inl
@@ -32,19 +32,18 @@
 
 #include "CSysMatrix.hpp"
 
-template<class ScalarType>
-FORCEINLINE ScalarType *CSysMatrix<ScalarType>::GetBlock_ILUMatrix(unsigned long block_i, unsigned long block_j) {
+template <class ScalarType>
+FORCEINLINE ScalarType* CSysMatrix<ScalarType>::GetBlock_ILUMatrix(unsigned long block_i, unsigned long block_j) {
   /*--- The position of the diagonal block is known which allows halving the search space. ---*/
-  const auto end = (block_j<block_i)? dia_ptr_ilu[block_i] : row_ptr_ilu[block_i+1];
-  for (auto index = (block_j<block_i)? row_ptr_ilu[block_i] : dia_ptr_ilu[block_i]; index < end; ++index)
-    if (col_ind_ilu[index] == block_j)
-      return &ILU_matrix[index*nVar*nVar];
+  const auto end = (block_j < block_i) ? dia_ptr_ilu[block_i] : row_ptr_ilu[block_i + 1];
+  for (auto index = (block_j < block_i) ? row_ptr_ilu[block_i] : dia_ptr_ilu[block_i]; index < end; ++index)
+    if (col_ind_ilu[index] == block_j) return &ILU_matrix[index * nVar * nVar];
   return nullptr;
 }
 
-template<class ScalarType>
-FORCEINLINE void CSysMatrix<ScalarType>::SetBlock_ILUMatrix(unsigned long block_i, unsigned long block_j, ScalarType *val_block) {
-
+template <class ScalarType>
+FORCEINLINE void CSysMatrix<ScalarType>::SetBlock_ILUMatrix(unsigned long block_i, unsigned long block_j,
+                                                            ScalarType* val_block) {
   auto ilu_ij = GetBlock_ILUMatrix(block_i, block_j);
   if (!ilu_ij) return;
   MatrixCopy(val_block, ilu_ij);
@@ -52,8 +51,8 @@ FORCEINLINE void CSysMatrix<ScalarType>::SetBlock_ILUMatrix(unsigned long block_
 
 namespace {
 
-template<class T, bool alpha, bool beta, bool transp>
-FORCEINLINE void gemv_impl(unsigned long n, unsigned long m, const T *a, const T *b, T *c) {
+template <class T, bool alpha, bool beta, bool transp>
+FORCEINLINE void gemv_impl(unsigned long n, unsigned long m, const T* a, const T* b, T* c) {
   /*---
    This is a templated version of GEMV with the constants as boolean
    template parameters so that they can be optimized away at compilation.
@@ -62,158 +61,151 @@ FORCEINLINE void gemv_impl(unsigned long n, unsigned long m, const T *a, const T
   if (!transp) {
     for (auto i = 0ul; i < n; i++) {
       if (!beta) c[i] = 0.0;
-      for (auto j = 0ul; j < m; j++)
-        c[i] += (alpha? 1 : -1) * a[i*m+j] * b[j];
+      for (auto j = 0ul; j < m; j++) c[i] += (alpha ? 1 : -1) * a[i * m + j] * b[j];
     }
   } else {
-    if (!beta) for (auto j = 0ul; j < m; j++) c[j] = 0.0;
+    if (!beta)
+      for (auto j = 0ul; j < m; j++) c[j] = 0.0;
     for (auto i = 0ul; i < n; i++)
-      for (auto j = 0ul; j < m; j++)
-        c[j] += (alpha? 1 : -1) * a[i*n+j] * b[i];
+      for (auto j = 0ul; j < m; j++) c[j] += (alpha ? 1 : -1) * a[i * n + j] * b[i];
   }
 }
 
-template<class T>
-FORCEINLINE void gemm_impl(unsigned long n, const T *a, const T *b, T *c) {
+template <class T>
+FORCEINLINE void gemm_impl(unsigned long n, const T* a, const T* b, T* c) {
   /*--- Same deal as for GEMV but here only the type is templated. ---*/
   unsigned long i, j, k;
   for (i = 0; i < n; i++) {
     for (j = 0; j < n; j++) {
-      c[i*n+j] = 0.0;
-      for (k = 0; k < n; k++)
-        c[i*n+j] += a[i*n+k] * b[k*n+j];
+      c[i * n + j] = 0.0;
+      for (k = 0; k < n; k++) c[i * n + j] += a[i * n + k] * b[k * n + j];
     }
   }
 }
-} // namespace
+}  // namespace
 
-#define __MATVECPROD_SIGNATURE__(TYPE,NAME) \
-FORCEINLINE void CSysMatrix<TYPE>::NAME(const TYPE *matrix, const TYPE *vector, TYPE *product) const
+#define __MATVECPROD_SIGNATURE__(TYPE, NAME) \
+  FORCEINLINE void CSysMatrix<TYPE>::NAME(const TYPE* matrix, const TYPE* vector, TYPE* product) const
 
-#define MATVECPROD_SIGNATURE(NAME) template<class ScalarType> __MATVECPROD_SIGNATURE__(ScalarType,NAME)
+#define MATVECPROD_SIGNATURE(NAME) \
+  template <class ScalarType>      \
+  __MATVECPROD_SIGNATURE__(ScalarType, NAME)
 
 #if !defined(USE_MKL)
-MATVECPROD_SIGNATURE( MatrixVectorProduct ) {
+MATVECPROD_SIGNATURE(MatrixVectorProduct) {
   /*---
    Without MKL (default) picture copying the body of gemv_impl
    here and resolving the conditionals at compilation.
   ---*/
-  gemv_impl<ScalarType,true,false,false>(nVar, nEqn, matrix, vector, product);
+  gemv_impl<ScalarType, true, false, false>(nVar, nEqn, matrix, vector, product);
 }
 
-MATVECPROD_SIGNATURE( MatrixVectorProductAdd ) {
-  gemv_impl<ScalarType,true,true,false>(nVar, nEqn, matrix, vector, product);
+MATVECPROD_SIGNATURE(MatrixVectorProductAdd) {
+  gemv_impl<ScalarType, true, true, false>(nVar, nEqn, matrix, vector, product);
 }
 
-MATVECPROD_SIGNATURE( MatrixVectorProductSub ) {
-  gemv_impl<ScalarType,false,true,false>(nVar, nEqn, matrix, vector, product);
+MATVECPROD_SIGNATURE(MatrixVectorProductSub) {
+  gemv_impl<ScalarType, false, true, false>(nVar, nEqn, matrix, vector, product);
 }
 
-template<class ScalarType>
-FORCEINLINE void CSysMatrix<ScalarType>::MatrixMatrixProduct(const ScalarType *matrix_a,
-                                                             const ScalarType *matrix_b, ScalarType *product) const {
+template <class ScalarType>
+FORCEINLINE void CSysMatrix<ScalarType>::MatrixMatrixProduct(const ScalarType* matrix_a, const ScalarType* matrix_b,
+                                                             ScalarType* product) const {
   gemm_impl<ScalarType>(nVar, matrix_a, matrix_b, product);
 }
 #else
-MATVECPROD_SIGNATURE( MatrixVectorProduct ) {
+MATVECPROD_SIGNATURE(MatrixVectorProduct) {
   /*--- With MKL we use the just-in-time kernels instead of the naive implementation. ---*/
   MatrixVectorProductKernelBetaZero(MatrixVectorProductJitterBetaZero, const_cast<ScalarType*>(vector),
-                                    const_cast<ScalarType*>(matrix), product );
+                                    const_cast<ScalarType*>(matrix), product);
 }
 
-MATVECPROD_SIGNATURE( MatrixVectorProductAdd ) {
+MATVECPROD_SIGNATURE(MatrixVectorProductAdd) {
   MatrixVectorProductKernelBetaOne(MatrixVectorProductJitterBetaOne, const_cast<ScalarType*>(vector),
-                                   const_cast<ScalarType*>(matrix), product );
+                                   const_cast<ScalarType*>(matrix), product);
 }
 
-MATVECPROD_SIGNATURE( MatrixVectorProductSub ) {
+MATVECPROD_SIGNATURE(MatrixVectorProductSub) {
   MatrixVectorProductKernelAlphaMinusOne(MatrixVectorProductJitterAlphaMinusOne, const_cast<ScalarType*>(vector),
-                                         const_cast<ScalarType*>(matrix), product );
+                                         const_cast<ScalarType*>(matrix), product);
 }
 
-template<class ScalarType>
-FORCEINLINE void CSysMatrix<ScalarType>::MatrixMatrixProduct(const ScalarType *matrix_a,
-                                                             const ScalarType *matrix_b, ScalarType *product) const {
+template <class ScalarType>
+FORCEINLINE void CSysMatrix<ScalarType>::MatrixMatrixProduct(const ScalarType* matrix_a, const ScalarType* matrix_b,
+                                                             ScalarType* product) const {
   MatrixMatrixProductKernel(MatrixMatrixProductJitter, const_cast<ScalarType*>(matrix_a),
-                            const_cast<ScalarType*>(matrix_b), product );
+                            const_cast<ScalarType*>(matrix_b), product);
 }
 #endif
 
 #undef MATVECPROD_SIGNATURE
 #undef __MATVECPROD_SIGNATURE__
 
-template<class ScalarType>
+template <class ScalarType>
 FORCEINLINE void CSysMatrix<ScalarType>::Gauss_Elimination(unsigned long block_i, ScalarType* rhs) const {
-
   /*--- Copy block, as the algorithm modifies the matrix ---*/
-  ScalarType block[MAXNVAR*MAXNVAR];
-  MatrixCopy(&matrix[dia_ptr[block_i]*nVar*nVar], block);
+  ScalarType block[MAXNVAR * MAXNVAR];
+  MatrixCopy(&matrix[dia_ptr[block_i] * nVar * nVar], block);
 
   Gauss_Elimination(block, rhs);
 }
 
-template<class ScalarType>
-FORCEINLINE void CSysMatrix<ScalarType>::InverseDiagonalBlock(unsigned long block_i, ScalarType *invBlock) const {
-
+template <class ScalarType>
+FORCEINLINE void CSysMatrix<ScalarType>::InverseDiagonalBlock(unsigned long block_i, ScalarType* invBlock) const {
   /*--- Copy block, as the algorithm modifies the matrix ---*/
-  ScalarType block[MAXNVAR*MAXNVAR];
-  MatrixCopy(&matrix[dia_ptr[block_i]*nVar*nVar], block);
+  ScalarType block[MAXNVAR * MAXNVAR];
+  MatrixCopy(&matrix[dia_ptr[block_i] * nVar * nVar], block);
 
   MatrixInverse(block, invBlock);
 }
 
-template<class ScalarType>
-FORCEINLINE void CSysMatrix<ScalarType>::InverseDiagonalBlock_ILUMatrix(unsigned long block_i, ScalarType *invBlock) const {
-
+template <class ScalarType>
+FORCEINLINE void CSysMatrix<ScalarType>::InverseDiagonalBlock_ILUMatrix(unsigned long block_i,
+                                                                        ScalarType* invBlock) const {
   /*--- Copy block, as the algorithm modifies the matrix ---*/
-  ScalarType block[MAXNVAR*MAXNVAR];
-  MatrixCopy(&ILU_matrix[dia_ptr_ilu[block_i]*nVar*nVar], block);
+  ScalarType block[MAXNVAR * MAXNVAR];
+  MatrixCopy(&ILU_matrix[dia_ptr_ilu[block_i] * nVar * nVar], block);
 
   MatrixInverse(block, invBlock);
 }
 
-template<class ScalarType>
-FORCEINLINE void CSysMatrix<ScalarType>::RowProduct(const CSysVector<ScalarType> & vec,
-                                                    unsigned long row_i, ScalarType *prod) const {
-  for (auto iVar = 0ul; iVar < nVar; iVar++)
-    prod[iVar] = 0.0;
+template <class ScalarType>
+FORCEINLINE void CSysMatrix<ScalarType>::RowProduct(const CSysVector<ScalarType>& vec, unsigned long row_i,
+                                                    ScalarType* prod) const {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) prod[iVar] = 0.0;
 
-  for (auto index = row_ptr[row_i]; index < row_ptr[row_i+1]; index++) {
+  for (auto index = row_ptr[row_i]; index < row_ptr[row_i + 1]; index++) {
     auto col_j = col_ind[index];
-    MatrixVectorProductAdd(&matrix[index*nVar*nEqn], &vec[col_j*nEqn], prod);
+    MatrixVectorProductAdd(&matrix[index * nVar * nEqn], &vec[col_j * nEqn], prod);
   }
 }
 
-template<class ScalarType>
-FORCEINLINE void CSysMatrix<ScalarType>::UpperProduct(const CSysVector<ScalarType> & vec, unsigned long row_i,
-                                                      unsigned long col_ub, ScalarType *prod) const {
-  for (auto iVar = 0ul; iVar < nVar; iVar++)
-    prod[iVar] = 0.0;
+template <class ScalarType>
+FORCEINLINE void CSysMatrix<ScalarType>::UpperProduct(const CSysVector<ScalarType>& vec, unsigned long row_i,
+                                                      unsigned long col_ub, ScalarType* prod) const {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) prod[iVar] = 0.0;
 
-  for (auto index = dia_ptr[row_i]+1; index < row_ptr[row_i+1]; index++) {
+  for (auto index = dia_ptr[row_i] + 1; index < row_ptr[row_i + 1]; index++) {
     auto col_j = col_ind[index];
     /*--- Always include halos. ---*/
     if (col_j < col_ub || col_j >= nPointDomain)
-      MatrixVectorProductAdd(&matrix[index*nVar*nEqn], &vec[col_j*nEqn], prod);
+      MatrixVectorProductAdd(&matrix[index * nVar * nEqn], &vec[col_j * nEqn], prod);
   }
 }
 
-template<class ScalarType>
-FORCEINLINE void CSysMatrix<ScalarType>::LowerProduct(const CSysVector<ScalarType> & vec, unsigned long row_i,
-                                                      unsigned long col_lb, ScalarType *prod) const {
-  for (auto iVar = 0ul; iVar < nVar; iVar++)
-    prod[iVar] = 0.0;
+template <class ScalarType>
+FORCEINLINE void CSysMatrix<ScalarType>::LowerProduct(const CSysVector<ScalarType>& vec, unsigned long row_i,
+                                                      unsigned long col_lb, ScalarType* prod) const {
+  for (auto iVar = 0ul; iVar < nVar; iVar++) prod[iVar] = 0.0;
 
   for (auto index = row_ptr[row_i]; index < dia_ptr[row_i]; index++) {
     auto col_j = col_ind[index];
-    if (col_j >= col_lb)
-      MatrixVectorProductAdd(&matrix[index*nVar*nEqn], &vec[col_j*nEqn], prod);
+    if (col_j >= col_lb) MatrixVectorProductAdd(&matrix[index * nVar * nEqn], &vec[col_j * nEqn], prod);
   }
 }
 
-template<class ScalarType>
-FORCEINLINE void CSysMatrix<ScalarType>::DiagonalProduct(const CSysVector<ScalarType> & vec,
-                                                         unsigned long row_i, ScalarType *prod) const {
-
-  MatrixVectorProduct(&matrix[dia_ptr[row_i]*nVar*nEqn], &vec[row_i*nEqn], prod);
+template <class ScalarType>
+FORCEINLINE void CSysMatrix<ScalarType>::DiagonalProduct(const CSysVector<ScalarType>& vec, unsigned long row_i,
+                                                         ScalarType* prod) const {
+  MatrixVectorProduct(&matrix[dia_ptr[row_i] * nVar * nEqn], &vec[row_i * nEqn], prod);
 }
diff --git a/Common/include/linear_algebra/CSysSolve.hpp b/Common/include/linear_algebra/CSysSolve.hpp
index 6c214ee4b29..0a5ed8f52a0 100644
--- a/Common/include/linear_algebra/CSysSolve.hpp
+++ b/Common/include/linear_algebra/CSysSolve.hpp
@@ -42,13 +42,16 @@
 
 class CConfig;
 class CGeometry;
-template<class T> class CSysMatrix;
-template<class T> class CMatrixVectorProduct;
-template<class T> class CPreconditioner;
+template <class T>
+class CSysMatrix;
+template <class T>
+class CMatrixVectorProduct;
+template <class T>
+class CPreconditioner;
 
 /*--- Relative tolerance, target residual is tol*||b-Ax||,
  *    Absolute tolerance, target residual is tol*||b||. ---*/
-enum class LinearToleranceType {RELATIVE, ABSOLUTE};
+enum class LinearToleranceType { RELATIVE, ABSOLUTE };
 
 /*!
  * \class CSysSolve
@@ -64,10 +67,9 @@ enum class LinearToleranceType {RELATIVE, ABSOLUTE};
  * Beware of writes to class member variables, for example "Residual" should only
  * be modified by one thread.
  */
-template<class ScalarType>
+template <class ScalarType>
 class CSysSolve {
-
-public:
+ public:
   /*--- Some aliases for simplicity. ---*/
   using Scalar = ScalarType;
   using VectorType = CSysVector<ScalarType>;
@@ -75,37 +77,43 @@ class CSysSolve {
   using ProductType = CMatrixVectorProduct<ScalarType>;
   using PrecondType = CPreconditioner<ScalarType>;
 
-private:
-  const ScalarType eps;      /*!< \brief Machine epsilon used in this class. */
-  ScalarType Residual=1e-20; /*!< \brief Residual at the end of a call to Solve or Solve_b. */
-  unsigned long Iterations=0;/*!< \brief Iterations done in Solve or Solve_b. */
+ private:
+  const ScalarType eps;         /*!< \brief Machine epsilon used in this class. */
+  ScalarType Residual = 1e-20;  /*!< \brief Residual at the end of a call to Solve or Solve_b. */
+  unsigned long Iterations = 0; /*!< \brief Iterations done in Solve or Solve_b. */
 
-  LINEAR_SOLVER_MODE lin_sol_mode;  /*!< \brief Type of operation for the linear system solver, changes the source of solver options. */
+  LINEAR_SOLVER_MODE
+  lin_sol_mode; /*!< \brief Type of operation for the linear system solver, changes the source of solver options. */
 
   mutable bool cg_ready;     /*!< \brief Indicate if memory used by CG is allocated. */
   mutable bool bcg_ready;    /*!< \brief Indicate if memory used by BCGSTAB is allocated. */
   mutable bool smooth_ready; /*!< \brief Indicate if memory used by SMOOTHER is allocated. */
 
-  mutable VectorType r;      /*!< \brief Residual in CG and BCGSTAB. */
-  mutable VectorType A_x;    /*!< \brief Result of matrix-vector product in CG and BCGSTAB. */
-  mutable VectorType p;      /*!< \brief Direction in CG and BCGSTAB. */
-  mutable VectorType z;      /*!< \brief Preconditioned residual/direction in CG/BCGSTAB. */
+  mutable VectorType r;   /*!< \brief Residual in CG and BCGSTAB. */
+  mutable VectorType A_x; /*!< \brief Result of matrix-vector product in CG and BCGSTAB. */
+  mutable VectorType p;   /*!< \brief Direction in CG and BCGSTAB. */
+  mutable VectorType z;   /*!< \brief Preconditioned residual/direction in CG/BCGSTAB. */
 
-  mutable VectorType r_0;    /*!< \brief The "arbitrary" vector in BCGSTAB. */
-  mutable VectorType v;      /*!< \brief BCGSTAB "v" vector (v = A * M^-1 * p). */
+  mutable VectorType r_0; /*!< \brief The "arbitrary" vector in BCGSTAB. */
+  mutable VectorType v;   /*!< \brief BCGSTAB "v" vector (v = A * M^-1 * p). */
 
-  mutable std::vector<VectorType> W;  /*!< \brief Large matrix used by FGMRES, w^i+1 = A * z^i. */
-  mutable std::vector<VectorType> Z;  /*!< \brief Large matrix used by FGMRES, preconditioned W. */
+  mutable std::vector<VectorType> W; /*!< \brief Large matrix used by FGMRES, w^i+1 = A * z^i. */
+  mutable std::vector<VectorType> Z; /*!< \brief Large matrix used by FGMRES, preconditioned W. */
 
-  VectorType  LinSysSol_tmp;        /*!< \brief Temporary used when it is necessary to interface between active and passive types. */
-  VectorType  LinSysRes_tmp;        /*!< \brief Temporary used when it is necessary to interface between active and passive types. */
-  VectorType* LinSysSol_ptr;        /*!< \brief Pointer to appropriate LinSysSol (set to original or temporary in call to Solve). */
-  const VectorType* LinSysRes_ptr;  /*!< \brief Pointer to appropriate LinSysRes (set to original or temporary in call to Solve). */
+  VectorType
+      LinSysSol_tmp; /*!< \brief Temporary used when it is necessary to interface between active and passive types. */
+  VectorType
+      LinSysRes_tmp; /*!< \brief Temporary used when it is necessary to interface between active and passive types. */
+  VectorType*
+      LinSysSol_ptr; /*!< \brief Pointer to appropriate LinSysSol (set to original or temporary in call to Solve). */
+  const VectorType*
+      LinSysRes_ptr; /*!< \brief Pointer to appropriate LinSysRes (set to original or temporary in call to Solve). */
 
-  LinearToleranceType tol_type = LinearToleranceType::ABSOLUTE; /*!< \brief How the linear solvers interpret the tolerance. */
-  bool xIsZero = false;           /*!< \brief If true assume the initial solution is always 0. */
-  bool recomputeRes = false;      /*!< \brief Recompute the residual after inner iterations, if monitoring. */
-  unsigned long monitorFreq = 10; /*!< \brief Monitoring frequency. */
+  LinearToleranceType tol_type =
+      LinearToleranceType::ABSOLUTE; /*!< \brief How the linear solvers interpret the tolerance. */
+  bool xIsZero = false;              /*!< \brief If true assume the initial solution is always 0. */
+  bool recomputeRes = false;         /*!< \brief Recompute the residual after inner iterations, if monitoring. */
+  unsigned long monitorFreq = 10;    /*!< \brief Monitoring frequency. */
 
   /*!
    * \brief sign transfer function
@@ -128,7 +136,7 @@ class CSysSolve {
    * \param[in,out] h1 - first element of 2x1 vector being transformed
    * \param[in,out] h2 - second element of 2x1 vector being transformed
    */
-  void ApplyGivens(ScalarType s, ScalarType c, ScalarType & h1, ScalarType & h2) const;
+  void ApplyGivens(ScalarType s, ScalarType c, ScalarType& h1, ScalarType& h2) const;
 
   /*!
    * \brief generates the Givens rotation matrix for a given 2-vector
@@ -140,7 +148,7 @@ class CSysSolve {
    * Based on givens() of SPARSKIT, which is based on p.202 of
    * "Matrix Computations" by Golub and van Loan.
    */
-  void GenerateGivens(ScalarType & dx, ScalarType & dy, ScalarType & s, ScalarType & c) const;
+  void GenerateGivens(ScalarType& dx, ScalarType& dy, ScalarType& s, ScalarType& c) const;
 
   /*!
    * \brief finds the solution of the upper triangular system Hsbg*x = rhs
@@ -153,8 +161,8 @@ class CSysSolve {
    * \pre the upper Hessenberg matrix has been transformed into a
    * triangular matrix.
    */
-  void SolveReduced(int n, const su2matrix<ScalarType>& Hsbg,
-                    const su2vector<ScalarType>& rhs, su2vector<ScalarType>& x) const;
+  void SolveReduced(int n, const su2matrix<ScalarType>& Hsbg, const su2vector<ScalarType>& rhs,
+                    su2vector<ScalarType>& x) const;
 
   /*!
    * \brief Modified Gram-Schmidt orthogonalization
@@ -173,7 +181,7 @@ class CSysSolve {
    * vector is kept in nrm0 and updated after operating with each vector
    *
    */
-  void ModGramSchmidt(int i, su2matrix<ScalarType>& Hsbg, std::vector<VectorType> & w) const;
+  void ModGramSchmidt(int i, su2matrix<ScalarType>& Hsbg, std::vector<VectorType>& w) const;
 
   /*!
    * \brief writes header information for a CSysSolve residual history
@@ -216,9 +224,8 @@ class CSysSolve {
    * \param[in] LinSysRes - Linear system residual
    * \param[in,out] LinSysSol - Linear system solution
    */
-  template<class OtherType, su2enable_if<std::is_same<ScalarType,OtherType>::value> = 0>
+  template <class OtherType, su2enable_if<std::is_same<ScalarType, OtherType>::value> = 0>
   void HandleTemporariesIn(const CSysVector<OtherType>& LinSysRes, CSysVector<OtherType>& LinSysSol) {
-
     /*--- Set the pointers. ---*/
     BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
       LinSysRes_ptr = &LinSysRes;
@@ -233,9 +240,8 @@ class CSysSolve {
    * \param[in] LinSysRes - Linear system residual
    * \param[in,out] LinSysSol - Linear system solution
    */
-  template<class OtherType, su2enable_if<!std::is_same<ScalarType,OtherType>::value> = 0>
+  template <class OtherType, su2enable_if<!std::is_same<ScalarType, OtherType>::value> = 0>
   void HandleTemporariesIn(const CSysVector<OtherType>& LinSysRes, CSysVector<OtherType>& LinSysSol) {
-
     /*--- Copy data, the solution is also copied as it serves as initial condition. ---*/
     LinSysRes_tmp.PassiveCopy(LinSysRes);
     LinSysSol_tmp.PassiveCopy(LinSysSol);
@@ -253,9 +259,8 @@ class CSysSolve {
    * \note Same type specialization, temporary variables are not required.
    * \param[out] LinSysSol - Linear system solution
    */
-  template<class OtherType, su2enable_if<std::is_same<ScalarType,OtherType>::value> = 0>
+  template <class OtherType, su2enable_if<std::is_same<ScalarType, OtherType>::value> = 0>
   void HandleTemporariesOut(CSysVector<OtherType>& LinSysSol) {
-
     /*--- Reset the pointers. ---*/
     BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
       LinSysRes_ptr = nullptr;
@@ -269,9 +274,8 @@ class CSysSolve {
    * \note Different type specialization, copy data from the temporary solution vector.
    * \param[out] LinSysSol - Linear system solution
    */
-  template<class OtherType, su2enable_if<!std::is_same<ScalarType,OtherType>::value> = 0>
+  template <class OtherType, su2enable_if<!std::is_same<ScalarType, OtherType>::value> = 0>
   void HandleTemporariesOut(CSysVector<OtherType>& LinSysSol) {
-
     /*--- Copy data, only the temporary solution needs to be copied. ---*/
     LinSysSol.PassiveCopy(LinSysSol_tmp);
 
@@ -283,8 +287,7 @@ class CSysSolve {
     END_SU2_OMP_SAFE_GLOBAL_ACCESS
   }
 
-public:
-
+ public:
   /*!
    * \brief default constructor of the class.
    * \param[in] linear_solver_mode - enum, to let CSysSolve know in what context it is
@@ -302,9 +305,9 @@ class CSysSolve {
    * \param[in] monitoring - turn on priting residuals from solver to screen.
    * \param[in] config - Definition of the particular problem.
    */
-  unsigned long CG_LinSolver(const VectorType & b, VectorType & x, const ProductType & mat_vec,
-                             const PrecondType & precond, ScalarType tol, unsigned long m,
-                             ScalarType & residual, bool monitoring, const CConfig *config) const;
+  unsigned long CG_LinSolver(const VectorType& b, VectorType& x, const ProductType& mat_vec, const PrecondType& precond,
+                             ScalarType tol, unsigned long m, ScalarType& residual, bool monitoring,
+                             const CConfig* config) const;
 
   /*!
    * \brief Flexible Generalized Minimal Residual method
@@ -318,16 +321,16 @@ class CSysSolve {
    * \param[in] monitoring - turn on priting residuals from solver to screen.
    * \param[in] config - Definition of the particular problem.
    */
-  unsigned long FGMRES_LinSolver(const VectorType & b, VectorType & x, const ProductType & mat_vec,
-                                 const PrecondType & precond, ScalarType tol, unsigned long m,
-                                 ScalarType & residual, bool monitoring, const CConfig *config) const;
+  unsigned long FGMRES_LinSolver(const VectorType& b, VectorType& x, const ProductType& mat_vec,
+                                 const PrecondType& precond, ScalarType tol, unsigned long m, ScalarType& residual,
+                                 bool monitoring, const CConfig* config) const;
 
   /*!
    * \brief Flexible Generalized Minimal Residual method with restarts (frequency comes from config).
    */
-  unsigned long RFGMRES_LinSolver(const VectorType & b, VectorType & x, const ProductType & mat_vec,
-                                  const PrecondType & precond, ScalarType tol, unsigned long m,
-                                  ScalarType & residual, bool monitoring, const CConfig *config);
+  unsigned long RFGMRES_LinSolver(const VectorType& b, VectorType& x, const ProductType& mat_vec,
+                                  const PrecondType& precond, ScalarType tol, unsigned long m, ScalarType& residual,
+                                  bool monitoring, const CConfig* config);
 
   /*!
    * \brief Biconjugate Gradient Stabilized Method (BCGSTAB)
@@ -341,9 +344,9 @@ class CSysSolve {
    * \param[in] monitoring - turn on priting residuals from solver to screen.
    * \param[in] config - Definition of the particular problem.
    */
-  unsigned long BCGSTAB_LinSolver(const VectorType & b, VectorType & x, const ProductType & mat_vec,
-                                  const PrecondType & precond, ScalarType tol, unsigned long m,
-                                  ScalarType & residual, bool monitoring, const CConfig *config) const;
+  unsigned long BCGSTAB_LinSolver(const VectorType& b, VectorType& x, const ProductType& mat_vec,
+                                  const PrecondType& precond, ScalarType tol, unsigned long m, ScalarType& residual,
+                                  bool monitoring, const CConfig* config) const;
 
   /*!
    * \brief Generic smoother (modified Richardson iteration with preconditioner)
@@ -357,9 +360,9 @@ class CSysSolve {
    * \param[in] monitoring - turn on priting residuals from solver to screen.
    * \param[in] config - Definition of the particular problem.
    */
-  unsigned long Smoother_LinSolver(const VectorType & b, VectorType & x, const ProductType & mat_vec,
-                                   const PrecondType & precond, ScalarType tol, unsigned long m,
-                                   ScalarType & residual, bool monitoring, const CConfig *config) const;
+  unsigned long Smoother_LinSolver(const VectorType& b, VectorType& x, const ProductType& mat_vec,
+                                   const PrecondType& precond, ScalarType tol, unsigned long m, ScalarType& residual,
+                                   bool monitoring, const CConfig* config) const;
 
   /*!
    * \brief Solve the linear system using a Krylov subspace method
@@ -369,8 +372,8 @@ class CSysSolve {
    * \param[in] geometry -  Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  unsigned long Solve(MatrixType & Jacobian, const CSysVector<su2double> & LinSysRes, CSysVector<su2double> & LinSysSol,
-                      CGeometry *geometry, const CConfig *config);
+  unsigned long Solve(MatrixType& Jacobian, const CSysVector<su2double>& LinSysRes, CSysVector<su2double>& LinSysSol,
+                      CGeometry* geometry, const CConfig* config);
 
   /*!
    * \brief Solve the adjoint linear system using a Krylov subspace method
@@ -381,8 +384,8 @@ class CSysSolve {
    * \param[in] config - Definition of the particular problem.
    * \param[in] directCall - If this method is called directly, or in AD context.
    */
-  unsigned long Solve_b(MatrixType & Jacobian, const CSysVector<su2double> & LinSysRes, CSysVector<su2double> & LinSysSol,
-                        CGeometry *geometry, const CConfig *config, const bool directCall = true);
+  unsigned long Solve_b(MatrixType& Jacobian, const CSysVector<su2double>& LinSysRes, CSysVector<su2double>& LinSysSol,
+                        CGeometry* geometry, const CConfig* config, const bool directCall = true);
 
   /*!
    * \brief Get the number of iterations.
@@ -399,21 +402,20 @@ class CSysSolve {
   /*!
    * \brief Set the type of the tolerance for stoping the linear solvers (RELATIVE or ABSOLUTE).
    */
-  inline void SetToleranceType(LinearToleranceType type) {tol_type = type;}
+  inline void SetToleranceType(LinearToleranceType type) { tol_type = type; }
 
   /*!
    * \brief Assume the initial solution is 0 to save one product, or don't.
    */
-  inline void SetxIsZero(bool isZero) {xIsZero = isZero;}
+  inline void SetxIsZero(bool isZero) { xIsZero = isZero; }
 
   /*!
    * \brief Set whether to recompute residuals at the end (while monitoring only).
    */
-  inline void SetRecomputeResidual(bool recompRes) {recomputeRes = recompRes;}
+  inline void SetRecomputeResidual(bool recompRes) { recomputeRes = recompRes; }
 
   /*!
    * \brief Set the screen output frequency during monitoring.
    */
-  inline void SetMonitoringFrequency(bool frequency) {monitorFreq = frequency;}
-
+  inline void SetMonitoringFrequency(bool frequency) { monitorFreq = frequency; }
 };
diff --git a/Common/include/linear_algebra/CSysSolve_b.hpp b/Common/include/linear_algebra/CSysSolve_b.hpp
index 7827942f14a..22a91391a32 100644
--- a/Common/include/linear_algebra/CSysSolve_b.hpp
+++ b/Common/include/linear_algebra/CSysSolve_b.hpp
@@ -30,10 +30,9 @@
 #include "../basic_types/datatype_structure.hpp"
 
 #ifdef CODI_REVERSE_TYPE
-template<class ScalarType>
+template <class ScalarType>
 struct CSysSolve_b {
-  static void Solve_b(const su2double::Real* x, su2double::Real* x_b, size_t m,
-                      const su2double::Real* y, const su2double::Real* y_b, size_t n,
-                      codi::ExternalFunctionUserData* d);
+  static void Solve_b(const su2double::Real* x, su2double::Real* x_b, size_t m, const su2double::Real* y,
+                      const su2double::Real* y_b, size_t n, codi::ExternalFunctionUserData* d);
 };
 #endif
diff --git a/Common/include/linear_algebra/CSysVector.hpp b/Common/include/linear_algebra/CSysVector.hpp
index ea6755adeae..2c20e1317b6 100644
--- a/Common/include/linear_algebra/CSysVector.hpp
+++ b/Common/include/linear_algebra/CSysVector.hpp
@@ -45,9 +45,9 @@
  */
 #ifdef HAVE_OMP
 #ifdef HAVE_OMP_SIMD
-#define CSYSVEC_PARFOR SU2_OMP_FOR_(simd schedule(static,omp_chunk_size) SU2_NOWAIT)
+#define CSYSVEC_PARFOR SU2_OMP_FOR_(simd schedule(static, omp_chunk_size) SU2_NOWAIT)
 #else
-#define CSYSVEC_PARFOR SU2_OMP_FOR_(schedule(static,omp_chunk_size) SU2_NOWAIT)
+#define CSYSVEC_PARFOR SU2_OMP_FOR_(schedule(static, omp_chunk_size) SU2_NOWAIT)
 #endif
 #define END_CSYSVEC_PARFOR END_SU2_OMP_FOR
 #else
@@ -67,9 +67,9 @@ class CSysVector : public VecExpr::CVecExpr<CSysVector<ScalarType>, ScalarType>
 
   unsigned long omp_chunk_size = OMP_MAX_SIZE; /*!< \brief Static chunk size used in loops. */
   ScalarType* vec_val = nullptr;               /*!< \brief Storage, 64 byte aligned (do not use normal new/delete). */
-  unsigned long nElm = 0;          /*!< \brief Total number of elements (or number elements on this processor). */
-  unsigned long nElmDomain = 0;    /*!< \brief Total number of elements without Ghost cells. */
-  unsigned long nVar = 1;          /*!< \brief Number of elements in a block. */
+  unsigned long nElm = 0;       /*!< \brief Total number of elements (or number elements on this processor). */
+  unsigned long nElmDomain = 0; /*!< \brief Total number of elements without Ghost cells. */
+  unsigned long nVar = 1;       /*!< \brief Number of elements in a block. */
 
   /*!
    * \brief Generic initialization from a scalar or array.
@@ -187,7 +187,8 @@ class CSysVector : public VecExpr::CVecExpr<CSysVector<ScalarType>, ScalarType>
     /*--- check if self-assignment, otherwise perform deep copy ---*/
     if ((const void*)this == (const void*)&other) return;
 
-    SU2_OMP_SAFE_GLOBAL_ACCESS(Initialize(other.GetNBlk(), other.GetNBlkDomain(), other.GetNVar(), nullptr, true, false);)
+    SU2_OMP_SAFE_GLOBAL_ACCESS(
+        Initialize(other.GetNBlk(), other.GetNBlkDomain(), other.GetNVar(), nullptr, true, false);)
 
     CSYSVEC_PARFOR
     for (auto i = 0ul; i < nElm; i++) vec_val[i] = SU2_TYPE::GetValue(other[i]);
diff --git a/Common/include/linear_algebra/blas_structure.hpp b/Common/include/linear_algebra/blas_structure.hpp
index 48358bc2ee2..3cf8142e184 100644
--- a/Common/include/linear_algebra/blas_structure.hpp
+++ b/Common/include/linear_algebra/blas_structure.hpp
@@ -44,7 +44,7 @@ class CConfig;
  * \version 7.5.1 "Blackbird"
  */
 class CBlasStructure {
-public:
+ public:
   /*!
    * \brief Constructor of the class. Initialize the constant member variables.
    */
@@ -60,9 +60,8 @@ class CBlasStructure {
    * \param[in]  B  - Input matrix in the multiplication.
    * \param[out] C  - Result of the matrix product A*B.
    */
-  void gemm(const int M,        const int N,        const int K,
-            const su2double *A, const su2double *B, su2double *C,
-            const CConfig *config);
+  void gemm(const int M, const int N, const int K, const su2double* A, const su2double* B, su2double* C,
+            const CConfig* config);
 
   /*!
    * \brief Function, which carries out a dense matrix vector product
@@ -73,8 +72,7 @@ class CBlasStructure {
    * \param[in]  x  - Input vector in the multiplication.
    * \param[out] y  - Result of the product A x.
    */
-  void gemv(const int M,        const int N,   const su2double *A,
-            const su2double *x, su2double *y);
+  void gemv(const int M, const int N, const su2double* A, const su2double* x, su2double* y);
 
   /*!
    * \brief Function, to carry out the axpy operation, i.e y += a*x.
@@ -87,55 +85,53 @@ class CBlasStructure {
                          at least 1 + (n-1)*abs(incy).
    * param[in]    incy - Specifies the increment of y.
    */
-  void axpy(const int n,    const su2double a,  const su2double *x,
-            const int incx, su2double *y,       const int incy);
+  void axpy(const int n, const su2double a, const su2double* x, const int incx, su2double* y, const int incy);
 
   /*!
    * \brief Invert a square matrix.
    * \param[in] M - Size.
    * \param[in,out] mat - Matrix, and inverse on exit.
    */
-  template<class Mat>
+  template <class Mat>
   static void inverse(const int M, Mat& mat) {
     using Scalar = typename Mat::Scalar;
 
     /*--- Copy the data from A into the augmented matrix and initialize mat with the identity. ---*/
     Mat aug = mat;
     mat = Scalar(0);
-    for(int j=0; j<M; ++j) mat(j,j) = 1;
+    for (int j = 0; j < M; ++j) mat(j, j) = 1;
 
     /*--- Outer loop of the Gauss-Jordan elimination. ---*/
-    for(int j=0; j<M; ++j) {
-
+    for (int j = 0; j < M; ++j) {
       /*--- Find the pivot in the current column. ---*/
       int jj = j;
-      Scalar valMax = fabs(aug(j,j));
-      for(int i=j+1; i<M; ++i) {
-        Scalar val = fabs(aug(i,j));
-        if(val > valMax){
+      Scalar valMax = fabs(aug(j, j));
+      for (int i = j + 1; i < M; ++i) {
+        Scalar val = fabs(aug(i, j));
+        if (val > valMax) {
           jj = i;
           valMax = val;
         }
       }
 
       /*--- Swap the rows j and jj, if needed. ---*/
-      if(jj > j) {
-        for(int k=j; k<M; ++k) std::swap(aug(j,k), aug(jj,k));
-        for(int k=0; k<M; ++k) std::swap(mat(j,k), mat(jj,k));
+      if (jj > j) {
+        for (int k = j; k < M; ++k) std::swap(aug(j, k), aug(jj, k));
+        for (int k = 0; k < M; ++k) std::swap(mat(j, k), mat(jj, k));
       }
 
       /*--- Performing row operations to form required identity
             matrix out of the input matrix.  ---*/
-      for(int i=0; i<M; ++i) {
-        if(i == j) continue;
-        valMax = aug(i,j)/aug(j,j);
-        for(int k=j; k<M; ++k) aug(i,k) -= valMax*aug(j,k);
-        for(int k=0; k<M; ++k) mat(i,k) -= valMax*mat(j,k);
+      for (int i = 0; i < M; ++i) {
+        if (i == j) continue;
+        valMax = aug(i, j) / aug(j, j);
+        for (int k = j; k < M; ++k) aug(i, k) -= valMax * aug(j, k);
+        for (int k = 0; k < M; ++k) mat(i, k) -= valMax * mat(j, k);
       }
 
-      valMax = 1.0/aug(j,j);
-      for(int k=j; k<M; ++k) aug(j,k) *= valMax;
-      for(int k=0; k<M; ++k) mat(j,k) *= valMax;
+      valMax = 1.0 / aug(j, j);
+      for (int k = j; k < M; ++k) aug(j, k) *= valMax;
+      for (int k = 0; k < M; ++k) mat(j, k) *= valMax;
     }
   }
 
@@ -174,20 +170,19 @@ class CBlasStructure {
    * \param[in,out] e: work vector
    * \param[in] n: order of matrix V
    */
-  template<class Mat, class Vec, class W>
+  template <class Mat, class Vec, class W>
   static void tred2(Mat& V, Vec& d, W& e, int n) {
     using Scalar = typename std::decay<decltype(e[0])>::type;
 
-    int i,j,k;
+    int i, j, k;
 
     for (j = 0; j < n; j++) {
-      d[j] = V[n-1][j];
+      d[j] = V[n - 1][j];
     }
 
     /* Householder reduction to tridiagonal form. */
 
-    for (i = n-1; i > 0; i--) {
-
+    for (i = n - 1; i > 0; i--) {
       /* Scale to avoid under/overflow. */
 
       Scalar scale = 0.0;
@@ -196,29 +191,27 @@ class CBlasStructure {
         scale = scale + fabs(d[k]);
       }
       if (scale == 0.0) {
-        e[i] = d[i-1];
+        e[i] = d[i - 1];
         for (j = 0; j < i; j++) {
-          d[j] = V[i-1][j];
+          d[j] = V[i - 1][j];
           V[i][j] = 0.0;
           V[j][i] = 0.0;
         }
-      }
-      else {
-
+      } else {
         /* Generate Householder vector. */
 
         for (k = 0; k < i; k++) {
           d[k] /= scale;
           h += d[k] * d[k];
         }
-        Scalar f = d[i-1];
+        Scalar f = d[i - 1];
         Scalar g = sqrt(h);
         if (f > 0) {
           g = -g;
         }
         e[i] = scale * g;
         h = h - f * g;
-        d[i-1] = f - g;
+        d[i - 1] = f - g;
         for (j = 0; j < i; j++) {
           e[j] = 0.0;
         }
@@ -229,7 +222,7 @@ class CBlasStructure {
           f = d[j];
           V[j][i] = f;
           g = e[j] + V[j][j] * f;
-          for (k = j+1; k <= i-1; k++) {
+          for (k = j + 1; k <= i - 1; k++) {
             g += V[k][j] * d[k];
             e[k] += V[k][j] * f;
           }
@@ -247,10 +240,10 @@ class CBlasStructure {
         for (j = 0; j < i; j++) {
           f = d[j];
           g = e[j];
-          for (k = j; k <= i-1; k++) {
-              V[k][j] -= (f * e[k] + g * d[k]);
+          for (k = j; k <= i - 1; k++) {
+            V[k][j] -= (f * e[k] + g * d[k]);
           }
-          d[j] = V[i-1][j];
+          d[j] = V[i - 1][j];
           V[i][j] = 0.0;
         }
       }
@@ -259,18 +252,18 @@ class CBlasStructure {
 
     /* Accumulate transformations. */
 
-    for (i = 0; i < n-1; i++) {
-      V[n-1][i] = V[i][i];
+    for (i = 0; i < n - 1; i++) {
+      V[n - 1][i] = V[i][i];
       V[i][i] = 1.0;
-      Scalar h = d[i+1];
+      Scalar h = d[i + 1];
       if (h != 0.0) {
         for (k = 0; k <= i; k++) {
-          d[k] = V[k][i+1] / h;
+          d[k] = V[k][i + 1] / h;
         }
         for (j = 0; j <= i; j++) {
           Scalar g = 0.0;
           for (k = 0; k <= i; k++) {
-            g += V[k][i+1] * V[k][j];
+            g += V[k][i + 1] * V[k][j];
           }
           for (k = 0; k <= i; k++) {
             V[k][j] -= g * d[k];
@@ -278,14 +271,14 @@ class CBlasStructure {
         }
       }
       for (k = 0; k <= i; k++) {
-        V[k][i+1] = 0.0;
+        V[k][i + 1] = 0.0;
       }
     }
     for (j = 0; j < n; j++) {
-      d[j] = V[n-1][j];
-      V[n-1][j] = 0.0;
+      d[j] = V[n - 1][j];
+      V[n - 1][j] = 0.0;
     }
-    V[n-1][n-1] = 1.0;
+    V[n - 1][n - 1] = 1.0;
     e[0] = 0.0;
   }
 
@@ -324,27 +317,26 @@ class CBlasStructure {
    * \param[in,out] e: work vector
    * \param[in] n: order of matrix V
    */
-  template<class Mat, class Vec, class W>
+  template <class Mat, class Vec, class W>
   static void tql2(Mat& V, Vec& d, W& e, int n) {
     using Scalar = typename std::decay<decltype(e[0])>::type;
 
-    int i,j,k,l;
+    int i, j, k, l;
     for (i = 1; i < n; i++) {
-      e[i-1] = e[i];
+      e[i - 1] = e[i];
     }
-    e[n-1] = 0.0;
+    e[n - 1] = 0.0;
 
     Scalar f = 0.0;
     Scalar tst1 = 0.0;
-    Scalar eps = pow(2.0,-52.0);
+    Scalar eps = pow(2.0, -52.0);
     for (l = 0; l < n; l++) {
-
       /* Find small subdiagonal element */
 
-      tst1 = max(tst1,(fabs(d[l]) + fabs(e[l])));
+      tst1 = max(tst1, (fabs(d[l]) + fabs(e[l])));
       int m = l;
       while (m < n) {
-        if (fabs(e[m]) <= eps*tst1) {
+        if (fabs(e[m]) <= eps * tst1) {
           break;
         }
         m++;
@@ -356,21 +348,21 @@ class CBlasStructure {
       if (m > l) {
         int iter = 0;
         do {
-          iter = iter + 1;  /* (Could check iteration count here.) */
+          iter = iter + 1; /* (Could check iteration count here.) */
 
           /* Compute implicit shift */
 
           Scalar g = d[l];
-          Scalar p = (d[l+1] - g) / (2.0 * e[l]);
-          Scalar r = sqrt(p*p+1.0);
+          Scalar p = (d[l + 1] - g) / (2.0 * e[l]);
+          Scalar r = sqrt(p * p + 1.0);
           if (p < 0) {
             r = -r;
           }
           d[l] = e[l] / (p + r);
-          d[l+1] = e[l] * (p + r);
-          Scalar dl1 = d[l+1];
+          d[l + 1] = e[l] * (p + r);
+          Scalar dl1 = d[l + 1];
           Scalar h = g - d[l];
-          for (i = l+2; i < n; i++) {
+          for (i = l + 2; i < n; i++) {
             d[i] -= h;
           }
           f = f + h;
@@ -381,27 +373,27 @@ class CBlasStructure {
           Scalar c = 1.0;
           Scalar c2 = c;
           Scalar c3 = c;
-          Scalar el1 = e[l+1];
+          Scalar el1 = e[l + 1];
           Scalar s = 0.0;
           Scalar s2 = 0.0;
-          for (i = m-1; i >= l; i--) {
+          for (i = m - 1; i >= l; i--) {
             c3 = c2;
             c2 = c;
             s2 = s;
             g = c * e[i];
             h = c * p;
-            r = sqrt(p*p+e[i]*e[i]);
-            e[i+1] = s * r;
+            r = sqrt(p * p + e[i] * e[i]);
+            e[i + 1] = s * r;
             s = e[i] / r;
             c = p / r;
             p = c * d[i] - s * g;
-            d[i+1] = h + s * (c * g + s * d[i]);
+            d[i + 1] = h + s * (c * g + s * d[i]);
 
             /* Accumulate transformation. */
 
             for (k = 0; k < n; k++) {
-              h = V[k][i+1];
-              V[k][i+1] = s * V[k][i] + c * h;
+              h = V[k][i + 1];
+              V[k][i + 1] = s * V[k][i] + c * h;
               V[k][i] = c * V[k][i] - s * h;
             }
           }
@@ -411,7 +403,7 @@ class CBlasStructure {
 
           /* Check for convergence. */
 
-        } while (fabs(e[l]) > eps*tst1);
+        } while (fabs(e[l]) > eps * tst1);
       }
       d[l] = d[l] + f;
       e[l] = 0.0;
@@ -419,10 +411,10 @@ class CBlasStructure {
 
     /* Sort eigenvalues and corresponding vectors. */
 
-    for (i = 0; i < n-1; i++) {
+    for (i = 0; i < n - 1; i++) {
       k = i;
       Scalar p = d[i];
-      for (j = i+1; j < n; j++) {
+      for (j = i + 1; j < n; j++) {
         if (d[j] < p) {
           k = j;
           p = d[j];
@@ -448,11 +440,11 @@ class CBlasStructure {
    * \param[in] n: order of matrix A_ij
    * \param[in,out] e: work vector
    */
-  template<class Mat, class Vec, class W>
+  template <class Mat, class Vec, class W>
   static void EigenDecomposition(const Mat& A_ij, Mat& Eig_Vec, Vec& Eig_Val, int n, W& e) {
-    for (int iDim = 0; iDim < n; iDim++){
+    for (int iDim = 0; iDim < n; iDim++) {
       e[iDim] = 0.0;
-      for (int jDim = 0; jDim < n; jDim++){
+      for (int jDim = 0; jDim < n; jDim++) {
         Eig_Vec[iDim][jDim] = A_ij[iDim][jDim];
       }
     }
@@ -467,13 +459,12 @@ class CBlasStructure {
    * \param[in] Eig_Val: eigenvalues
    * \param[in] n: order of matrix A_ij
    */
-  template<class Mat, class Vec>
+  template <class Mat, class Vec>
   static void EigenRecomposition(Mat& A_ij, const Mat& Eig_Vec, const Vec& Eig_Val, int n) {
-    for (int i = 0; i < n; i++){
-      for (int j = 0; j < n; j++){
+    for (int i = 0; i < n; i++) {
+      for (int j = 0; j < n; j++) {
         A_ij[i][j] = 0.0;
-        for (int k = 0; k < n; k++)
-          A_ij[i][j] += Eig_Vec[i][k] * Eig_Val[k] * Eig_Vec[j][k];
+        for (int k = 0; k < n; k++) A_ij[i][j] += Eig_Vec[i][k] * Eig_Val[k] * Eig_Vec[j][k];
       }
     }
   }
@@ -486,29 +477,28 @@ class CBlasStructure {
    * \param[in,out] rhs - right hand side on entry, solution on exit
    * \note Same size for all vectors. Use row index for lower and upper vector (e.g. lower[0] does not matter).
    */
-  template<class Vec, class Scalar = su2double>
+  template <class Vec, class Scalar = su2double>
   static void tdma(const Vec& lower, const Vec& main, Vec& upper, Vec& rhs) {
     const int N = main.size();
 
     upper[0] /= main[0];
     rhs[0] /= main[0];
 
-    for (int i=1; i<N; i++) {
-      const Scalar denom = 1.0 / (main[i]-lower[i]*upper[i-1]);
+    for (int i = 1; i < N; i++) {
+      const Scalar denom = 1.0 / (main[i] - lower[i] * upper[i - 1]);
       upper[i] *= denom;
-      rhs[i] = (rhs[i]-lower[i]*rhs[i-1])*denom;
+      rhs[i] = (rhs[i] - lower[i] * rhs[i - 1]) * denom;
     }
 
-    for (int i=N-2; i>=0; i--)
-      rhs[i] -= upper[i]*rhs[i+1];
+    for (int i = N - 2; i >= 0; i--) rhs[i] -= upper[i] * rhs[i + 1];
   }
 
-private:
-
-#if !(defined(HAVE_LIBXSMM) || defined(HAVE_BLAS) || defined(HAVE_MKL)) || (defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE))
-    /* Blocking parameters for the outer kernel.  We multiply mc x kc blocks of
-     the matrix A with kc x nc panels of the matrix B (this approach is referred
-     to as `gebp` in the literature). */
+ private:
+#if !(defined(HAVE_LIBXSMM) || defined(HAVE_BLAS) || defined(HAVE_MKL)) || \
+    (defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE))
+  /* Blocking parameters for the outer kernel.  We multiply mc x kc blocks of
+   the matrix A with kc x nc panels of the matrix B (this approach is referred
+   to as `gebp` in the literature). */
   const int mc;
   const int kc;
   const int nc;
@@ -522,8 +512,7 @@ class CBlasStructure {
    * \param[in]  b  - Input matrix in the multiplication.
    * \param[out] c  - Result of the matrix product a*b.
    */
-  void gemm_imp(const int m,        const int n,        const int k,
-                const su2double *a, const su2double *b, su2double *c);
+  void gemm_imp(const int m, const int n, const int k, const su2double* a, const su2double* b, su2double* c);
 
   /*!
    * \brief Compute a portion of the c matrix one block at a time.
@@ -538,8 +527,7 @@ class CBlasStructure {
    * \param[out] c   - Result of the matrix product a*b.
    * \param[in]  ldc - Leading dimension of the matrix c.
    */
-  void gemm_inner(int m, int n, int k, const su2double *a, int lda,
-                  const su2double *b, int ldb, su2double *c, int ldc);
+  void gemm_inner(int m, int n, int k, const su2double* a, int lda, const su2double* b, int ldb, su2double* c, int ldc);
 
   /*!
    * \brief Naive gemm implementation to handle arbitrary sized matrices.
@@ -553,7 +541,7 @@ class CBlasStructure {
    * \param[out] c   - Result of the matrix product a*b.
    * \param[in]  ldc - Leading dimension of the matrix c.
    */
-  void gemm_arbitrary(int m, int n, int k, const su2double *a, int lda,
-                      const su2double *b, int ldb, su2double *c, int ldc);
+  void gemm_arbitrary(int m, int n, int k, const su2double* a, int lda, const su2double* b, int ldb, su2double* c,
+                      int ldc);
 #endif
 };
diff --git a/Common/include/linear_algebra/vector_expressions.hpp b/Common/include/linear_algebra/vector_expressions.hpp
index 6164d019982..000ce3cb2d0 100644
--- a/Common/include/linear_algebra/vector_expressions.hpp
+++ b/Common/include/linear_algebra/vector_expressions.hpp
@@ -53,9 +53,9 @@ namespace VecExpr {
  * Vector classes should be stored by reference to avoid copies, especially if they
  * allocate memory dynamically.
  */
-template<class Derived, class Scalar>
+template <class Derived, class Scalar>
 class CVecExpr {
-public:
+ public:
   /*!
    * \brief Cast the expression to Derived, usually to allow evaluation via operator[].
    */
@@ -63,35 +63,45 @@ class CVecExpr {
 
   // Allowed from C++14, allows nested expression propagation without
   // manually calling derived() on the expression being evaluated.
-  //FORCEINLINE auto operator[] (size_t i) const { return derived()[i]; }
+  // FORCEINLINE auto operator[] (size_t i) const { return derived()[i]; }
 };
 
 /*!
  * \brief Expression class to broadcast a scalar value. Allows implementing
  * "vector-scalar" operations re-using "vector-vector" expressions.
  */
-template<class Scalar>
+template <class Scalar>
 class Bcast : public CVecExpr<Bcast<Scalar>, Scalar> {
   Scalar x;
-public:
+
+ public:
   static constexpr bool StoreAsRef = false;
   FORCEINLINE Bcast(const Scalar& x_) : x(x_) {}
-  FORCEINLINE const Scalar& operator[] (size_t) const { return x; }
+  FORCEINLINE const Scalar& operator[](size_t) const { return x; }
 };
 
 /*!
  * \brief std::decay_t from C++14, used to allow implicit conversions
  * between scalar types, e.g. "CVecExpr<U,double>" + "int/double/etc.".
  */
-template<class T> using decay_t = typename std::decay<T>::type;
+template <class T>
+using decay_t = typename std::decay<T>::type;
 
 /*! \brief std::remove_reference_t from C++14, removes references from some type. */
-template<class T> using remove_reference_t = typename std::remove_reference<T>::type;
+template <class T>
+using remove_reference_t = typename std::remove_reference<T>::type;
 
 /*! \brief Mechanism to conditionally (based on "StoreAsRef") add lvalue reference to a type. */
-template<class T, bool> struct add_lref_if { using type = remove_reference_t<T>; };
-template<class T> struct add_lref_if<T,true> { using type = remove_reference_t<T> &; };
-template<class T> using store_t = typename add_lref_if<T,T::StoreAsRef>::type;
+template <class T, bool>
+struct add_lref_if {
+  using type = remove_reference_t<T>;
+};
+template <class T>
+struct add_lref_if<T, true> {
+  using type = remove_reference_t<T>&;
+};
+template <class T>
+using store_t = typename add_lref_if<T, T::StoreAsRef>::type;
 
 /*--- Namespace from which the math function implementations come. ---*/
 
@@ -104,26 +114,28 @@ namespace math = ::std;
 /*--- Macro to simplify auto return type deduction in C++11, operator[] needs
  * it to allow inner expressions to propagate as the outer is evaluated.  ---*/
 
-#define RETURNS(...) ->decltype(__VA_ARGS__) { return __VA_ARGS__; }
+#define RETURNS(...) \
+  ->decltype(__VA_ARGS__) { return __VA_ARGS__; }
 
 /*--- Macro to create expression classes (EXPR) and overloads (FUN) for unary
  * functions, based on their coefficient-wise implementation (IMPL). ---*/
 
-#define MAKE_UNARY_FUN(FUN, EXPR, IMPL)                                       \
-/*!--- Expression class. ---*/                                                \
-template<class U, class Scalar>                                               \
-class EXPR : public CVecExpr<EXPR<U,Scalar>, Scalar> {                        \
-  store_t<const U> u;                                                         \
-public:                                                                       \
-  static constexpr bool StoreAsRef = false;                                   \
-  FORCEINLINE EXPR(const U& u_) : u(u_) {}                                    \
-  FORCEINLINE auto operator[] (size_t i) const RETURNS( IMPL(u[i]) )          \
-};                                                                            \
-/*!--- Function overload, returns an expression object. ---*/                 \
-template<class U, class S>                                                    \
-FORCEINLINE auto FUN(const CVecExpr<U,S>& u) RETURNS( EXPR<U,S>(u.derived()) )
-
-#define sign_impl(x) Scalar(1-2*(x<0))
+#define MAKE_UNARY_FUN(FUN, EXPR, IMPL)                             \
+  /*!--- Expression class. ---*/                                    \
+  template <class U, class Scalar>                                  \
+  class EXPR : public CVecExpr<EXPR<U, Scalar>, Scalar> {           \
+    store_t<const U> u;                                             \
+                                                                    \
+   public:                                                          \
+    static constexpr bool StoreAsRef = false;                       \
+    FORCEINLINE EXPR(const U& u_) : u(u_) {}                        \
+    FORCEINLINE auto operator[](size_t i) const RETURNS(IMPL(u[i])) \
+  };                                                                \
+  /*!--- Function overload, returns an expression object. ---*/     \
+  template <class U, class S>                                       \
+  FORCEINLINE auto FUN(const CVecExpr<U, S>& u) RETURNS(EXPR<U, S>(u.derived()))
+
+#define sign_impl(x) Scalar(1 - 2 * (x < 0))
 MAKE_UNARY_FUN(operator-, minus_, -)
 MAKE_UNARY_FUN(abs, abs_, math::abs)
 MAKE_UNARY_FUN(sqrt, sqrt_, math::sqrt)
@@ -134,32 +146,28 @@ MAKE_UNARY_FUN(sign, sign_, sign_impl)
 
 /*--- Macro to create expressions and overloads for binary functions. ---*/
 
-#define MAKE_BINARY_FUN(FUN, EXPR, IMPL)                                      \
-/*!--- Expression class. ---*/                                                \
-template<class U, class V, class Scalar>                                      \
-class EXPR : public CVecExpr<EXPR<U,V,Scalar>, Scalar> {                      \
-  store_t<const U> u;                                                         \
-  store_t<const V> v;                                                         \
-public:                                                                       \
-  static constexpr bool StoreAsRef = false;                                   \
-  FORCEINLINE EXPR(const U& u_, const V& v_) : u(u_), v(v_) {}                \
-  FORCEINLINE auto operator[] (size_t i) const RETURNS( IMPL(u[i], v[i]) )    \
-};                                                                            \
-/*!--- Vector with vector function overload. ---*/                            \
-template<class U, class V, class S>                                           \
-FORCEINLINE auto FUN(const CVecExpr<U,S>& u, const CVecExpr<V,S>& v)          \
-  RETURNS( EXPR<U,V,S>(u.derived(), v.derived())                              \
-)                                                                             \
-/*!--- Vector with scalar function overload. ---*/                            \
-template<class U, class S>                                                    \
-FORCEINLINE auto FUN(const CVecExpr<U,S>& u, decay_t<S> v)                    \
-  RETURNS( EXPR<U,Bcast<S>,S>(u.derived(), Bcast<S>(v))                       \
-)                                                                             \
-/*!--- Scalar with vector function overload. ---*/                            \
-template<class S, class V>                                                    \
-FORCEINLINE auto FUN(decay_t<S> u, const CVecExpr<V,S>& v)                    \
-  RETURNS( EXPR<Bcast<S>,V,S>(Bcast<S>(u), v.derived())                       \
-)                                                                             \
+#define MAKE_BINARY_FUN(FUN, EXPR, IMPL)                                                                             \
+  /*!--- Expression class. ---*/                                                                                     \
+  template <class U, class V, class Scalar>                                                                          \
+  class EXPR : public CVecExpr<EXPR<U, V, Scalar>, Scalar> {                                                         \
+    store_t<const U> u;                                                                                              \
+    store_t<const V> v;                                                                                              \
+                                                                                                                     \
+   public:                                                                                                           \
+    static constexpr bool StoreAsRef = false;                                                                        \
+    FORCEINLINE EXPR(const U& u_, const V& v_) : u(u_), v(v_) {}                                                     \
+    FORCEINLINE auto operator[](size_t i) const RETURNS(IMPL(u[i], v[i]))                                            \
+  };                                                                                                                 \
+  /*!--- Vector with vector function overload. ---*/                                                                 \
+  template <class U, class V, class S>                                                                               \
+  FORCEINLINE auto FUN(const CVecExpr<U, S>& u, const CVecExpr<V, S>& v)                                             \
+      RETURNS(EXPR<U, V, S>(u.derived(), v.derived())) /*!--- Vector with scalar function overload. ---*/            \
+      template <class U, class S>                                                                                    \
+      FORCEINLINE auto FUN(const CVecExpr<U, S>& u, decay_t<S> v)                                                    \
+          RETURNS(EXPR<U, Bcast<S>, S>(u.derived(), Bcast<S>(v))) /*!--- Scalar with vector function overload. ---*/ \
+      template <class S, class V>                                                                                    \
+      FORCEINLINE auto FUN(decay_t<S> u, const CVecExpr<V, S>& v)                                                    \
+          RETURNS(EXPR<Bcast<S>, V, S>(Bcast<S>(u), v.derived()))
 
 /*--- std::max/min have issues (because they return by reference).
  * fmin and fmax return by value and thus are fine, but they would force
@@ -167,9 +175,9 @@ FORCEINLINE auto FUN(decay_t<S> u, const CVecExpr<V,S>& v)                    \
  * We use int32/64 instead of int/long to avoid issues with Windows,
  * where long is 32 bits (instead of 64 bits). ---*/
 
-#define MAKE_FMINMAX_OVERLOADS(TYPE)                          \
-FORCEINLINE TYPE fmax(TYPE a, TYPE b) { return a<b? b : a; }  \
-FORCEINLINE TYPE fmin(TYPE a, TYPE b) { return a<b? a : b; }
+#define MAKE_FMINMAX_OVERLOADS(TYPE)                              \
+  FORCEINLINE TYPE fmax(TYPE a, TYPE b) { return a < b ? b : a; } \
+  FORCEINLINE TYPE fmin(TYPE a, TYPE b) { return a < b ? a : b; }
 MAKE_FMINMAX_OVERLOADS(int32_t)
 MAKE_FMINMAX_OVERLOADS(int64_t)
 MAKE_FMINMAX_OVERLOADS(uint32_t)
@@ -188,10 +196,10 @@ MAKE_BINARY_FUN(pow, pow_, math::pow)
  * conversion between different types) and creating functions for these ops
  * requires a lot of boilerplate (template args, auto return, etc.). ---*/
 
-#define add_impl(a,b) a+b
-#define sub_impl(a,b) a-b
-#define mul_impl(a,b) a*b
-#define div_impl(a,b) a/b
+#define add_impl(a, b) a + b
+#define sub_impl(a, b) a - b
+#define mul_impl(a, b) a* b
+#define div_impl(a, b) a / b
 MAKE_BINARY_FUN(operator+, add_, add_impl)
 MAKE_BINARY_FUN(operator-, sub_, sub_impl)
 MAKE_BINARY_FUN(operator*, mul_, mul_impl)
@@ -207,12 +215,12 @@ MAKE_BINARY_FUN(operator/, div_, div_impl)
  * is lost since these operators are non-differentiable. ---*/
 
 #define TO_PASSIVE(IMPL) SU2_TYPE::Passive<Scalar>::Value(IMPL)
-#define le_impl(a,b) TO_PASSIVE(a<=b)
-#define ge_impl(a,b) TO_PASSIVE(a>=b)
-#define eq_impl(a,b) TO_PASSIVE(a==b)
-#define ne_impl(a,b) TO_PASSIVE(a!=b)
-#define lt_impl(a,b) TO_PASSIVE(a<b)
-#define gt_impl(a,b) TO_PASSIVE(a>b)
+#define le_impl(a, b) TO_PASSIVE(a <= b)
+#define ge_impl(a, b) TO_PASSIVE(a >= b)
+#define eq_impl(a, b) TO_PASSIVE(a == b)
+#define ne_impl(a, b) TO_PASSIVE(a != b)
+#define lt_impl(a, b) TO_PASSIVE(a < b)
+#define gt_impl(a, b) TO_PASSIVE(a > b)
 MAKE_BINARY_FUN(operator<=, le_, le_impl)
 MAKE_BINARY_FUN(operator>=, ge_, ge_impl)
 MAKE_BINARY_FUN(operator==, eq_, eq_impl)
@@ -230,4 +238,4 @@ MAKE_BINARY_FUN(operator>, gt_, gt_impl)
 #undef MAKE_BINARY_FUN
 
 /// @}
-} // end namespace
+}  // namespace VecExpr
diff --git a/Common/include/option_structure.inl b/Common/include/option_structure.inl
index 758033da153..f017aa65e2c 100644
--- a/Common/include/option_structure.inl
+++ b/Common/include/option_structure.inl
@@ -31,21 +31,16 @@ using namespace std;
 
 template <class Tenum, class TField>
 class COptionEnum final : public COptionBase {
-
   const map<string, Tenum>& m;
-  TField& field; // Reference to the fieldname
-  const Tenum def; // Default value
-  const string name; // identifier for the option
+  TField& field;      // Reference to the fieldname
+  const Tenum def;    // Default value
+  const string name;  // identifier for the option
 
-public:
+ public:
   COptionEnum() = delete;
 
-  COptionEnum(string option_field_name, const map<string, Tenum>& m_, TField& option_field, Tenum default_value) :
-    m(m_),
-    field(option_field),
-    def(default_value),
-    name(std::move(option_field_name)) {
-  }
+  COptionEnum(string option_field_name, const map<string, Tenum>& m_, TField& option_field, Tenum default_value)
+      : m(m_), field(option_field), def(default_value), name(std::move(option_field_name)) {}
 
   string SetValue(const vector<string>& option_value) override {
     COptionBase::SetValue(option_value);
@@ -73,26 +68,19 @@ public:
   void SetDefault() override { field = def; }
 };
 
-template<typename Scalar>
+template <typename Scalar>
 class COptionScalar : public COptionBase {
-protected:
-  Scalar& field; // Reference to the fieldname
-  const Scalar def; // Default value
-  const string name; // identifier for the option
-  const string typeName; // name for the scalar type
+ protected:
+  Scalar& field;          // Reference to the fieldname
+  const Scalar def;       // Default value
+  const string name;      // identifier for the option
+  const string typeName;  // name for the scalar type
 
-public:
+ public:
   COptionScalar() = delete;
 
-  COptionScalar(const string& type_name,
-                const string& option_field_name,
-                Scalar& option_field,
-                Scalar default_value) :
-    field(option_field),
-    def(default_value),
-    name(option_field_name),
-    typeName(type_name) {
-  }
+  COptionScalar(const string& type_name, const string& option_field_name, Scalar& option_field, Scalar default_value)
+      : field(option_field), def(default_value), name(option_field_name), typeName(type_name) {}
 
   string SetValue(const vector<string>& option_value) override {
     COptionBase::SetValue(option_value);
@@ -106,63 +94,49 @@ public:
     return badValue(typeName, name);
   }
 
-  void SetDefault() final {
-    field = def;
-  }
+  void SetDefault() final { field = def; }
 };
 
 class COptionDouble final : public COptionScalar<su2double> {
-public:
-  template<class... Ts>
-  COptionDouble(Ts&&... args) :
-    COptionScalar<su2double>("su2double", args...) {
-  }
+ public:
+  template <class... Ts>
+  COptionDouble(Ts&&... args) : COptionScalar<su2double>("su2double", args...) {}
 };
 
 class COptionInt final : public COptionScalar<int> {
-public:
-  template<class... Ts>
-  COptionInt(Ts&&... args) :
-    COptionScalar<int>("int", args...) {
-  }
+ public:
+  template <class... Ts>
+  COptionInt(Ts&&... args) : COptionScalar<int>("int", args...) {}
 };
 
 class COptionULong final : public COptionScalar<unsigned long> {
-public:
-  template<class... Ts>
-  COptionULong(Ts&&... args) :
-    COptionScalar<unsigned long>("unsigned long", args...) {
-  }
+ public:
+  template <class... Ts>
+  COptionULong(Ts&&... args) : COptionScalar<unsigned long>("unsigned long", args...) {}
 };
 
 class COptionUShort final : public COptionScalar<unsigned short> {
-public:
-  template<class... Ts>
-  COptionUShort(Ts&&... args) :
-    COptionScalar<unsigned short>("unsigned short", args...) {
-  }
+ public:
+  template <class... Ts>
+  COptionUShort(Ts&&... args) : COptionScalar<unsigned short>("unsigned short", args...) {}
 };
 
 class COptionLong final : public COptionScalar<long> {
-public:
-  template<class... Ts>
-  COptionLong(Ts&&... args) :
-    COptionScalar<long>("long", args...) {
-  }
+ public:
+  template <class... Ts>
+  COptionLong(Ts&&... args) : COptionScalar<long>("long", args...) {}
 };
 
 class COptionBool final : public COptionScalar<bool> {
-public:
-  template<class... Ts>
-  COptionBool(Ts&&... args) :
-    COptionScalar<bool>("bool", args...) {
-  }
+ public:
+  template <class... Ts>
+  COptionBool(Ts&&... args) : COptionScalar<bool>("bool", args...) {}
 
   string SetValue(const vector<string>& option_value) override {
     COptionBase::SetValue(option_value);
 
     string result;
-    auto msg = COptionScalar<string>("bool",name,result,"").SetValue(option_value);
+    auto msg = COptionScalar<string>("bool", name, result, "").SetValue(option_value);
 
     if (!msg.empty()) return msg;
 
@@ -180,21 +154,16 @@ public:
 };
 
 class COptionString final : public COptionBase {
-protected:
-  string& field; // Reference to the fieldname
-  const string def; // Default value
-  const string name; // identifier for the option
+ protected:
+  string& field;      // Reference to the fieldname
+  const string def;   // Default value
+  const string name;  // identifier for the option
 
-public:
+ public:
   COptionString() = delete;
 
-  COptionString(const string& option_field_name,
-                string& option_field,
-                string default_value) :
-    field(option_field),
-    def(default_value),
-    name(option_field_name) {
-  }
+  COptionString(const string& option_field_name, string& option_field, string default_value)
+      : field(option_field), def(default_value), name(option_field_name) {}
 
   string SetValue(const vector<string>& option_value) override {
     COptionBase::SetValue(option_value);
@@ -206,32 +175,27 @@ public:
     return "";
   }
 
-  void SetDefault() override {
-    field = def;
-  }
+  void SetDefault() override { field = def; }
 };
 
 template <class Tenum, class TField>
 class COptionEnumList final : public COptionBase {
-
   const map<string, Tenum>& m;
   TField*& field;
   unsigned short& mySize;
   const string name;
 
-public:
+ public:
   COptionEnumList() = delete;
 
-  COptionEnumList(string option_field_name, const map<string,Tenum>& m_, TField*& option_field, unsigned short& list_size) :
-    m(m_),
-    field(option_field),
-    mySize(list_size),
-    name(option_field_name) {
+  COptionEnumList(string option_field_name, const map<string, Tenum>& m_, TField*& option_field,
+                  unsigned short& list_size)
+      : m(m_), field(option_field), mySize(list_size), name(option_field_name) {
     field = nullptr;
   }
 
   ~COptionEnumList() {
-    delete [] field;
+    delete[] field;
     field = nullptr;
   }
 
@@ -266,18 +230,15 @@ public:
   void SetDefault() override { mySize = 0; }
 };
 
-template<class Type>
+template <class Type>
 class COptionArray final : public COptionBase {
-  string name; // Identifier for the option
-  const int size; // Number of elements
-  Type* field; // Reference to the field
-
-public:
-  COptionArray(string option_field_name, const int list_size, Type* option_field) :
-    name(option_field_name),
-    size(list_size),
-    field(option_field) {
-  }
+  string name;     // Identifier for the option
+  const int size;  // Number of elements
+  Type* field;     // Reference to the field
+
+ public:
+  COptionArray(string option_field_name, const int list_size, Type* option_field)
+      : name(option_field_name), size(list_size), field(option_field) {}
 
   string SetValue(const vector<string>& option_value) override {
     COptionBase::SetValue(option_value);
@@ -296,7 +257,7 @@ public:
       newstring.append(" found");
       return newstring;
     }
-    for (int i  = 0; i < this->size; i++) {
+    for (int i = 0; i < this->size; i++) {
       istringstream is(option_value[i]);
       if (!(is >> field[i])) {
         return badValue(" array", this->name);
@@ -308,29 +269,24 @@ public:
   void SetDefault() override {}
 };
 
-template<typename Scalar>
+template <typename Scalar>
 class COptionScalarList : public COptionBase {
-  Scalar*& field; // reference to the field
-  const string name; // identifier for the option
-  unsigned short& mySize; // size of the list
-  const string typeName; // name of the scalar type
+  Scalar*& field;          // reference to the field
+  const string name;       // identifier for the option
+  unsigned short& mySize;  // size of the list
+  const string typeName;   // name of the scalar type
 
-public:
+ public:
   COptionScalarList() = delete;
 
-  COptionScalarList(const string& type_name,
-                    const string& option_field_name,
-                    unsigned short& list_size,
-                    Scalar*& option_field) :
-    field(option_field),
-    name(option_field_name),
-    mySize(list_size),
-    typeName(type_name) {
+  COptionScalarList(const string& type_name, const string& option_field_name, unsigned short& list_size,
+                    Scalar*& option_field)
+      : field(option_field), name(option_field_name), mySize(list_size), typeName(type_name) {
     field = nullptr;
   }
 
   ~COptionScalarList() {
-    delete [] field;
+    delete[] field;
     // prevent double free
     field = nullptr;
   }
@@ -351,7 +307,7 @@ public:
       istringstream is(option_value[i]);
       Scalar val;
       if (!(is >> val)) {
-        return badValue(typeName+" list", name);
+        return badValue(typeName + " list", name);
       }
       field[i] = std::move(val);
     }
@@ -359,59 +315,49 @@ public:
   }
 
   void SetDefault() final {
-    mySize = 0; // There is no default value for list
+    mySize = 0;  // There is no default value for list
   }
 };
 
 class COptionDoubleList final : public COptionScalarList<su2double> {
-public:
-  template<class... Ts>
-  COptionDoubleList(Ts&&... args) :
-    COptionScalarList<su2double>("su2double", args...) {
-  }
+ public:
+  template <class... Ts>
+  COptionDoubleList(Ts&&... args) : COptionScalarList<su2double>("su2double", args...) {}
 };
 
 class COptionShortList final : public COptionScalarList<short> {
-public:
-  template<class... Ts>
-  COptionShortList(Ts&&... args) :
-    COptionScalarList<short>("short", args...) {
-  }
+ public:
+  template <class... Ts>
+  COptionShortList(Ts&&... args) : COptionScalarList<short>("short", args...) {}
 };
 
 class COptionUShortList final : public COptionScalarList<unsigned short> {
-public:
-  template<class... Ts>
-  COptionUShortList(Ts&&... args) :
-    COptionScalarList<unsigned short>("unsigned short", args...) {
-  }
+ public:
+  template <class... Ts>
+  COptionUShortList(Ts&&... args) : COptionScalarList<unsigned short>("unsigned short", args...) {}
 };
 
 class COptionULongList final : public COptionScalarList<unsigned long> {
-public:
-  template<class... Ts>
-  COptionULongList(Ts&&... args) :
-    COptionScalarList<unsigned long>("unsigned long", args...) {
-  }
+ public:
+  template <class... Ts>
+  COptionULongList(Ts&&... args) : COptionScalarList<unsigned long>("unsigned long", args...) {}
 };
 
 class COptionStringList final : public COptionScalarList<string> {
-public:
-  template<class... Ts>
-  COptionStringList(Ts&&... args) :
-    COptionScalarList<string>("string", args...) {
-  }
+ public:
+  template <class... Ts>
+  COptionStringList(Ts&&... args) : COptionScalarList<string>("string", args...) {}
 };
 
 class COptionConvect : public COptionBase {
-  string name; // identifier for the option
-  unsigned short & space;
-  CENTERED & centered;
-  UPWIND & upwind;
+  string name;  // identifier for the option
+  unsigned short& space;
+  CENTERED& centered;
+  UPWIND& upwind;
 
-public:
-  COptionConvect(string option_field_name, unsigned short & space_field, CENTERED & centered_field, UPWIND & upwind_field)
-    : name(option_field_name), space(space_field), centered(centered_field), upwind(upwind_field) { }
+ public:
+  COptionConvect(string option_field_name, unsigned short& space_field, CENTERED& centered_field, UPWIND& upwind_field)
+      : name(option_field_name), space(space_field), centered(centered_field), upwind(upwind_field) {}
 
   string SetValue(const vector<string>& option_value) override {
     COptionBase::SetValue(option_value);
@@ -436,7 +382,6 @@ public:
     // Make them defined in case something weird happens
     SetDefault();
     return badValue("convect", this->name);
-
   }
 
   void SetDefault() override {
@@ -446,17 +391,18 @@ public:
   }
 };
 
-class COptionFEMConvect : public COptionBase{
-  string name; // identifier for the option
-  unsigned short & space;
-  unsigned short & fem;
+class COptionFEMConvect : public COptionBase {
+  string name;  // identifier for the option
+  unsigned short& space;
+  unsigned short& fem;
 
-public:
-  COptionFEMConvect(string option_field_name, unsigned short & space_field, unsigned short & fem_field) : space(space_field), fem(fem_field) {
+ public:
+  COptionFEMConvect(string option_field_name, unsigned short& space_field, unsigned short& fem_field)
+      : space(space_field), fem(fem_field) {
     this->name = option_field_name;
   }
 
-  ~COptionFEMConvect() override {};
+  ~COptionFEMConvect() override{};
   string SetValue(const vector<string>& option_value) override {
     COptionBase::SetValue(option_value);
 
@@ -474,56 +420,51 @@ public:
     // Make them defined in case something weird happens
     this->fem = NO_FEM;
     return badValue("convect", this->name);
-
   }
 
-  void SetDefault() override {
-    this->fem = NO_FEM;
-  }
+  void SetDefault() override { this->fem = NO_FEM; }
 };
 
 class COptionMathProblem : public COptionBase {
-  string name; // identifier for the option
-  bool & cont_adjoint;
+  string name;  // identifier for the option
+  bool& cont_adjoint;
   bool cont_adjoint_def;
-  bool & disc_adjoint;
+  bool& disc_adjoint;
   bool disc_adjoint_def;
-  bool & restart;
+  bool& restart;
   bool restart_def;
 
-public:
-  COptionMathProblem(string option_field_name, bool & cont_adjoint_field, bool cont_adjoint_default, bool & disc_adjoint_field, bool disc_adjoint_default, bool & restart_field, bool restart_default) : cont_adjoint(cont_adjoint_field), disc_adjoint(disc_adjoint_field), restart(restart_field) {
+ public:
+  COptionMathProblem(string option_field_name, bool& cont_adjoint_field, bool cont_adjoint_default,
+                     bool& disc_adjoint_field, bool disc_adjoint_default, bool& restart_field, bool restart_default)
+      : cont_adjoint(cont_adjoint_field), disc_adjoint(disc_adjoint_field), restart(restart_field) {
     name = option_field_name;
     cont_adjoint_def = cont_adjoint_default;
     disc_adjoint_def = disc_adjoint_default;
     restart_def = restart_default;
   }
 
-  ~COptionMathProblem() override {};
+  ~COptionMathProblem() override{};
   string SetValue(const vector<string>& option_value) override {
     COptionBase::SetValue(option_value);
     string out = optionCheckMultipleValues(option_value, "unsigned short", name);
     if (out.compare("") != 0) {
       return out;
-    }
-    else if (option_value[0] == "ADJOINT") {
+    } else if (option_value[0] == "ADJOINT") {
       return badValue("math problem (try CONTINUOUS_ADJOINT)", name);
-    }
-    else if (option_value[0] == "DIRECT") {
+    } else if (option_value[0] == "DIRECT") {
       cont_adjoint = false;
       disc_adjoint = false;
       restart = false;
       return "";
-    }
-    else if (option_value[0] == "CONTINUOUS_ADJOINT") {
-      cont_adjoint= true;
+    } else if (option_value[0] == "CONTINUOUS_ADJOINT") {
+      cont_adjoint = true;
       disc_adjoint = false;
-      restart= true;
+      restart = true;
       return "";
-    }
-    else if (option_value[0] == "DISCRETE_ADJOINT") {
+    } else if (option_value[0] == "DISCRETE_ADJOINT") {
       disc_adjoint = true;
-      cont_adjoint= false;
+      cont_adjoint = false;
       restart = true;
       return "";
     }
@@ -535,22 +476,23 @@ public:
     disc_adjoint = disc_adjoint_def;
     restart = restart_def;
   }
-
 };
 
 class COptionDVParam : public COptionBase {
-  string name; // identifier for the option
-  unsigned short & nDV;
-  su2double ** & paramDV;
-  string * & FFDTag;
-  unsigned short* & design_variable;
-
-public:
-  COptionDVParam(string option_field_name, unsigned short & nDV_field, su2double** & paramDV_field, string* & FFDTag_field, unsigned short * & design_variable_field) : nDV(nDV_field), paramDV(paramDV_field), FFDTag(FFDTag_field), design_variable(design_variable_field) {
+  string name;  // identifier for the option
+  unsigned short& nDV;
+  su2double**& paramDV;
+  string*& FFDTag;
+  unsigned short*& design_variable;
+
+ public:
+  COptionDVParam(string option_field_name, unsigned short& nDV_field, su2double**& paramDV_field, string*& FFDTag_field,
+                 unsigned short*& design_variable_field)
+      : nDV(nDV_field), paramDV(paramDV_field), FFDTag(FFDTag_field), design_variable(design_variable_field) {
     this->name = option_field_name;
   }
 
-  ~COptionDVParam() override {};
+  ~COptionDVParam() override{};
 
   string SetValue(const vector<string>& option_value) override {
     COptionBase::SetValue(option_value);
@@ -566,18 +508,17 @@ public:
       newstring.append(": may not have beginning semicolon");
       return newstring;
     }
-    if (option_value[option_value.size()-1].compare(";") == 0) {
+    if (option_value[option_value.size() - 1].compare(";") == 0) {
       string newstring;
       newstring.append(this->name);
       newstring.append(": may not have ending semicolon");
       return newstring;
     }
 
-
     // use the ";" token to determine the number of design variables
     // This works because semicolon is not one of the delimiters in tokenize string
     this->nDV = 0;
-    //unsigned int num_semi = 0;
+    // unsigned int num_semi = 0;
     for (unsigned int i = 0; i < static_cast<unsigned int>(option_value.size()); i++) {
       if (option_value[i].compare(";") == 0) {
         this->nDV++;
@@ -588,10 +529,12 @@ public:
     // One more design variable than semicolon
     this->nDV++;
 
-    if ( (this->nDV > 0) && (this->design_variable == nullptr) ) {
+    if ((this->nDV > 0) && (this->design_variable == nullptr)) {
       string newstring;
       newstring.append(this->name);
-      newstring.append(": Design_Variable array has not been allocated. Check that DV_KIND appears before DV_PARAM in configuration file.");
+      newstring.append(
+          ": Design_Variable array has not been allocated. Check that DV_KIND appears before DV_PARAM in configuration "
+          "file.");
       return newstring;
     }
 
@@ -602,48 +545,116 @@ public:
 
     this->FFDTag = new string[this->nDV];
 
-   vector<unsigned short> nParamDV(nDV, 0);
-   unsigned short totalnParamDV = 0;
-   stringstream ss;
-   unsigned int i = 0;
+    vector<unsigned short> nParamDV(nDV, 0);
+    unsigned short totalnParamDV = 0;
+    stringstream ss;
+    unsigned int i = 0;
 
     for (unsigned short iDV = 0; iDV < this->nDV; iDV++) {
       switch (this->design_variable[iDV]) {
-        case NO_DEFORMATION:       nParamDV[iDV] = 0; break;
-        case FFD_SETTING:          nParamDV[iDV] = 0; break;
-        case FFD_CONTROL_POINT_2D: nParamDV[iDV] = 5; break;
-        case FFD_CAMBER_2D:        nParamDV[iDV] = 2; break;
-        case FFD_THICKNESS_2D:     nParamDV[iDV] = 2; break;
-        case FFD_TWIST_2D:         nParamDV[iDV] = 3; break;
-        case HICKS_HENNE:          nParamDV[iDV] = 2; break;
-        case SURFACE_BUMP:         nParamDV[iDV] = 3; break;
-        case CST:                  nParamDV[iDV] = 3; break;
-        case ANGLE_OF_ATTACK:      nParamDV[iDV] = 1; break;
-        case SCALE:                nParamDV[iDV] = 0; break;
-        case TRANSLATION:          nParamDV[iDV] = 3; break;
-        case ROTATION:             nParamDV[iDV] = 6; break;
-        case NACA_4DIGITS:         nParamDV[iDV] = 3; break;
-        case PARABOLIC:            nParamDV[iDV] = 2; break;
-        case AIRFOIL:              nParamDV[iDV] = 2; break;
-        case FFD_CONTROL_POINT:    nParamDV[iDV] = 7; break;
-        case FFD_NACELLE:          nParamDV[iDV] = 6; break;
-        case FFD_GULL:             nParamDV[iDV] = 2; break;
-        case FFD_TWIST:            nParamDV[iDV] = 8; break;
-        case FFD_ROTATION:         nParamDV[iDV] = 7; break;
-        case FFD_CONTROL_SURFACE:  nParamDV[iDV] = 7; break;
-        case FFD_CAMBER:           nParamDV[iDV] = 3; break;
-        case FFD_THICKNESS:        nParamDV[iDV] = 3; break;
-        case FFD_ANGLE_OF_ATTACK:  nParamDV[iDV] = 2; break;
-        case SURFACE_FILE:         nParamDV[iDV] = 0; break;
-        case DV_EFIELD:            nParamDV[iDV] = 2; break;
-        case DV_YOUNG:             nParamDV[iDV] = 0; break;
-        case DV_POISSON:           nParamDV[iDV] = 0; break;
-        case DV_RHO:               nParamDV[iDV] = 0; break;
-        case DV_RHO_DL:            nParamDV[iDV] = 0; break;
-        case SCALE_GRID:           nParamDV[iDV] = 0; break;
-        case TRANSLATE_GRID:       nParamDV[iDV] = 3; break;
-        case ROTATE_GRID:          nParamDV[iDV] = 6; break;
-        default : {
+        case NO_DEFORMATION:
+          nParamDV[iDV] = 0;
+          break;
+        case FFD_SETTING:
+          nParamDV[iDV] = 0;
+          break;
+        case FFD_CONTROL_POINT_2D:
+          nParamDV[iDV] = 5;
+          break;
+        case FFD_CAMBER_2D:
+          nParamDV[iDV] = 2;
+          break;
+        case FFD_THICKNESS_2D:
+          nParamDV[iDV] = 2;
+          break;
+        case FFD_TWIST_2D:
+          nParamDV[iDV] = 3;
+          break;
+        case HICKS_HENNE:
+          nParamDV[iDV] = 2;
+          break;
+        case SURFACE_BUMP:
+          nParamDV[iDV] = 3;
+          break;
+        case CST:
+          nParamDV[iDV] = 3;
+          break;
+        case ANGLE_OF_ATTACK:
+          nParamDV[iDV] = 1;
+          break;
+        case SCALE:
+          nParamDV[iDV] = 0;
+          break;
+        case TRANSLATION:
+          nParamDV[iDV] = 3;
+          break;
+        case ROTATION:
+          nParamDV[iDV] = 6;
+          break;
+        case NACA_4DIGITS:
+          nParamDV[iDV] = 3;
+          break;
+        case PARABOLIC:
+          nParamDV[iDV] = 2;
+          break;
+        case AIRFOIL:
+          nParamDV[iDV] = 2;
+          break;
+        case FFD_CONTROL_POINT:
+          nParamDV[iDV] = 7;
+          break;
+        case FFD_NACELLE:
+          nParamDV[iDV] = 6;
+          break;
+        case FFD_GULL:
+          nParamDV[iDV] = 2;
+          break;
+        case FFD_TWIST:
+          nParamDV[iDV] = 8;
+          break;
+        case FFD_ROTATION:
+          nParamDV[iDV] = 7;
+          break;
+        case FFD_CONTROL_SURFACE:
+          nParamDV[iDV] = 7;
+          break;
+        case FFD_CAMBER:
+          nParamDV[iDV] = 3;
+          break;
+        case FFD_THICKNESS:
+          nParamDV[iDV] = 3;
+          break;
+        case FFD_ANGLE_OF_ATTACK:
+          nParamDV[iDV] = 2;
+          break;
+        case SURFACE_FILE:
+          nParamDV[iDV] = 0;
+          break;
+        case DV_EFIELD:
+          nParamDV[iDV] = 2;
+          break;
+        case DV_YOUNG:
+          nParamDV[iDV] = 0;
+          break;
+        case DV_POISSON:
+          nParamDV[iDV] = 0;
+          break;
+        case DV_RHO:
+          nParamDV[iDV] = 0;
+          break;
+        case DV_RHO_DL:
+          nParamDV[iDV] = 0;
+          break;
+        case SCALE_GRID:
+          nParamDV[iDV] = 0;
+          break;
+        case TRANSLATE_GRID:
+          nParamDV[iDV] = 3;
+          break;
+        case ROTATE_GRID:
+          nParamDV[iDV] = 6;
+          break;
+        default: {
           string newstring;
           newstring.append(this->name);
           newstring.append(": undefined design variable type found in configuration file.");
@@ -653,40 +664,31 @@ public:
       totalnParamDV += nParamDV[iDV];
     }
 
-    if (totalnParamDV > option_value.size()){
+    if (totalnParamDV > option_value.size()) {
       SU2_MPI::Error("Wrong number of arguments for DV_PARAM!", CURRENT_FUNCTION);
     }
 
     for (unsigned short iDV = 0; iDV < this->nDV; iDV++) {
       for (unsigned short iParamDV = 0; iParamDV < nParamDV[iDV]; iParamDV++) {
-
         ss << option_value[i] << " ";
 
         if ((iParamDV == 0) &&
-            ((this->design_variable[iDV] == NO_DEFORMATION) ||
-             (this->design_variable[iDV] == FFD_SETTING) ||
-             (this->design_variable[iDV] == FFD_ANGLE_OF_ATTACK)||
-             (this->design_variable[iDV] == FFD_CONTROL_POINT_2D) ||
-             (this->design_variable[iDV] == FFD_CAMBER_2D) ||
-             (this->design_variable[iDV] == FFD_TWIST_2D) ||
-             (this->design_variable[iDV] == FFD_THICKNESS_2D) ||
-             (this->design_variable[iDV] == FFD_CONTROL_POINT) ||
-             (this->design_variable[iDV] == FFD_NACELLE) ||
-             (this->design_variable[iDV] == FFD_GULL) ||
-             (this->design_variable[iDV] == FFD_TWIST) ||
-             (this->design_variable[iDV] == FFD_ROTATION) ||
-             (this->design_variable[iDV] == FFD_CONTROL_SURFACE) ||
-             (this->design_variable[iDV] == FFD_CAMBER) ||
-             (this->design_variable[iDV] == FFD_THICKNESS))) {
-              ss >> this->FFDTag[iDV];
-              this->paramDV[iDV][iParamDV] = 0;
-            }
-        else
+            ((this->design_variable[iDV] == NO_DEFORMATION) || (this->design_variable[iDV] == FFD_SETTING) ||
+             (this->design_variable[iDV] == FFD_ANGLE_OF_ATTACK) ||
+             (this->design_variable[iDV] == FFD_CONTROL_POINT_2D) || (this->design_variable[iDV] == FFD_CAMBER_2D) ||
+             (this->design_variable[iDV] == FFD_TWIST_2D) || (this->design_variable[iDV] == FFD_THICKNESS_2D) ||
+             (this->design_variable[iDV] == FFD_CONTROL_POINT) || (this->design_variable[iDV] == FFD_NACELLE) ||
+             (this->design_variable[iDV] == FFD_GULL) || (this->design_variable[iDV] == FFD_TWIST) ||
+             (this->design_variable[iDV] == FFD_ROTATION) || (this->design_variable[iDV] == FFD_CONTROL_SURFACE) ||
+             (this->design_variable[iDV] == FFD_CAMBER) || (this->design_variable[iDV] == FFD_THICKNESS))) {
+          ss >> this->FFDTag[iDV];
+          this->paramDV[iDV][iParamDV] = 0;
+        } else
           ss >> this->paramDV[iDV][iParamDV];
 
         i++;
       }
-      if (iDV < (this->nDV-1)) {
+      if (iDV < (this->nDV - 1)) {
         if (option_value[i].compare(";") != 0) {
           string newstring;
           newstring.append(this->name);
@@ -710,19 +712,25 @@ public:
 };
 
 class COptionDVValue : public COptionBase {
-  string name; // identifier for the option
-  unsigned short* & nDV_Value;
-  su2double ** & valueDV;
-  unsigned short & nDV;
-  su2double ** & paramDV;
-  unsigned short* & design_variable;
-
-public:
-  COptionDVValue(string option_field_name, unsigned short* & nDVValue_field, su2double** & valueDV_field, unsigned short & nDV_field,  su2double** & paramDV_field, unsigned short * & design_variable_field) : nDV_Value(nDVValue_field), valueDV(valueDV_field), nDV(nDV_field), paramDV(paramDV_field), design_variable(design_variable_field) {
+  string name;  // identifier for the option
+  unsigned short*& nDV_Value;
+  su2double**& valueDV;
+  unsigned short& nDV;
+  su2double**& paramDV;
+  unsigned short*& design_variable;
+
+ public:
+  COptionDVValue(string option_field_name, unsigned short*& nDVValue_field, su2double**& valueDV_field,
+                 unsigned short& nDV_field, su2double**& paramDV_field, unsigned short*& design_variable_field)
+      : nDV_Value(nDVValue_field),
+        valueDV(valueDV_field),
+        nDV(nDV_field),
+        paramDV(paramDV_field),
+        design_variable(design_variable_field) {
     this->name = option_field_name;
   }
 
-  ~COptionDVValue() override {};
+  ~COptionDVValue() override{};
 
   string SetValue(const vector<string>& option_value) override {
     COptionBase::SetValue(option_value);
@@ -731,16 +739,20 @@ public:
       return "";
     }
 
-    if ( (this->nDV > 0) && (this->design_variable == nullptr) ) {
+    if ((this->nDV > 0) && (this->design_variable == nullptr)) {
       string newstring;
       newstring.append(this->name);
-      newstring.append(": Design_Variable array has not been allocated. Check that DV_KIND appears before DV_VALUE in configuration file.");
+      newstring.append(
+          ": Design_Variable array has not been allocated. Check that DV_KIND appears before DV_VALUE in configuration "
+          "file.");
       return newstring;
     }
-    if ( (this->nDV > 0) && (this->paramDV == nullptr) ) {
+    if ((this->nDV > 0) && (this->paramDV == nullptr)) {
       string newstring;
       newstring.append(this->name);
-      newstring.append(": Design_Parameter array has not been allocated. Check that DV_PARAM appears before DV_VALUE in configuration file.");
+      newstring.append(
+          ": Design_Parameter array has not been allocated. Check that DV_PARAM appears before DV_VALUE in "
+          "configuration file.");
       return newstring;
     }
 
@@ -758,23 +770,20 @@ public:
     for (unsigned short iDV = 0; iDV < this->nDV; iDV++) {
       switch (this->design_variable[iDV]) {
         case FFD_CONTROL_POINT:
-          if((this->paramDV[iDV][4] == 0) &&
-             (this->paramDV[iDV][5] == 0) &&
-             (this->paramDV[iDV][6] == 0)) {
+          if ((this->paramDV[iDV][4] == 0) && (this->paramDV[iDV][5] == 0) && (this->paramDV[iDV][6] == 0)) {
             nValueDV = 3;
           } else {
             nValueDV = 1;
           }
           break;
         case FFD_CONTROL_POINT_2D:
-          if((this->paramDV[iDV][3] == 0) &&
-             (this->paramDV[iDV][4] == 0)) {
+          if ((this->paramDV[iDV][3] == 0) && (this->paramDV[iDV][4] == 0)) {
             nValueDV = 2;
           } else {
             nValueDV = 1;
           }
           break;
-        default :
+        default:
           nValueDV = 1;
       }
 
@@ -783,7 +792,6 @@ public:
       totalnValueDV += nValueDV;
 
       for (unsigned short iValueDV = 0; iValueDV < nValueDV; iValueDV++) {
-
         if (i >= option_value.size()) {
           string newstring;
           newstring.append(this->name);
@@ -823,12 +831,10 @@ class COptionFFDDef : public COptionBase {
   su2double**& CoordFFD;
   string*& FFDTag;
 
-public:
-  COptionFFDDef(string option_field_name, unsigned short& nFFD_field, su2double**& coordFFD_field, string*& FFDTag_field)
-    : name(option_field_name),
-      nFFD(nFFD_field),
-      CoordFFD(coordFFD_field),
-      FFDTag(FFDTag_field) {
+ public:
+  COptionFFDDef(string option_field_name, unsigned short& nFFD_field, su2double**& coordFFD_field,
+                string*& FFDTag_field)
+      : name(option_field_name), nFFD(nFFD_field), CoordFFD(coordFFD_field), FFDTag(FFDTag_field) {
     nFFD = 0;
     CoordFFD = nullptr;
     FFDTag = nullptr;
@@ -853,11 +859,10 @@ public:
     if (option_value[0].compare(";") == 0) {
       return name + ": may not have beginning semicolon";
     }
-    if (option_value[option_value.size()-1].compare(";") == 0) {
+    if (option_value[option_value.size() - 1].compare(";") == 0) {
       return name + ": may not have ending semicolon";
     }
 
-
     // use the ";" token to determine the number of design variables
     // This works because semicolon is not one of the delimiters in tokenize string
     this->nFFD = 0;
@@ -882,20 +887,20 @@ public:
     unsigned int i = 0;
 
     for (unsigned short iFFD = 0; iFFD < this->nFFD; iFFD++) {
-
       nCoordFFD = 25;
 
       for (unsigned short iCoordFFD = 0; iCoordFFD < nCoordFFD; iCoordFFD++) {
-
         ss << option_value[i] << " ";
 
-        if (iCoordFFD == 0) ss >> this->FFDTag[iFFD];
-        else ss >> this->CoordFFD[iFFD][iCoordFFD-1];
+        if (iCoordFFD == 0)
+          ss >> this->FFDTag[iFFD];
+        else
+          ss >> this->CoordFFD[iFFD][iCoordFFD - 1];
 
         i++;
       }
 
-      if (iFFD < (this->nFFD-1)) {
+      if (iFFD < (this->nFFD - 1)) {
         if (option_value[i].compare(";") != 0) {
           string newstring;
           newstring.append(this->name);
@@ -904,7 +909,6 @@ public:
         }
         i++;
       }
-
     }
 
     // Need to return something...
@@ -919,11 +923,9 @@ class COptionFFDDegree : public COptionBase {
   unsigned short& nFFD;
   unsigned short**& DegreeFFD;
 
-public:
+ public:
   COptionFFDDegree(string option_field_name, unsigned short& nFFD_field, unsigned short**& degreeFFD_field)
-    : name(option_field_name),
-      nFFD(nFFD_field),
-      DegreeFFD(degreeFFD_field) {
+      : name(option_field_name), nFFD(nFFD_field), DegreeFFD(degreeFFD_field) {
     nFFD = 0;
     DegreeFFD = nullptr;
   }
@@ -945,11 +947,10 @@ public:
     if (option_value[0].compare(";") == 0) {
       return name + ": may not have beginning semicolon";
     }
-    if (option_value[option_value.size()-1].compare(";") == 0) {
+    if (option_value[option_value.size() - 1].compare(";") == 0) {
       return name + ": may not have ending semicolon";
     }
 
-
     // use the ";" token to determine the number of design variables
     // This works because semicolon is not one of the delimiters in tokenize string
     this->nFFD = 0;
@@ -972,7 +973,6 @@ public:
     unsigned int i = 0;
 
     for (unsigned short iFFD = 0; iFFD < this->nFFD; iFFD++) {
-
       nDegreeFFD = 3;
 
       for (unsigned short iDegreeFFD = 0; iDegreeFFD < nDegreeFFD; iDegreeFFD++) {
@@ -981,7 +981,7 @@ public:
         i++;
       }
 
-      if (iFFD < (this->nFFD-1)) {
+      if (iFFD < (this->nFFD - 1)) {
         if (option_value[i].compare(";") != 0) {
           string newstring;
           newstring.append(this->name);
@@ -990,7 +990,6 @@ public:
         }
         i++;
       }
-
     }
 
     // Need to return something...
@@ -1001,22 +1000,22 @@ public:
 };
 
 class COptionInlet : public COptionBase {
-  string name; // identifier for the option
+  string name;  // identifier for the option
   unsigned short& size;
   string*& marker;
   su2double*& ttotal;
   su2double*& ptotal;
   su2double**& flowdir;
 
-public:
+ public:
   COptionInlet(string option_field_name, unsigned short& nMarker_Inlet, string*& Marker_Inlet, su2double*& Ttotal,
                su2double*& Ptotal, su2double**& FlowDir)
-    : name(option_field_name),
-      size(nMarker_Inlet),
-      marker(Marker_Inlet),
-      ttotal(Ttotal),
-      ptotal(Ptotal),
-      flowdir(FlowDir) {
+      : name(option_field_name),
+        size(nMarker_Inlet),
+        marker(Marker_Inlet),
+        ttotal(Ttotal),
+        ptotal(Ptotal),
+        flowdir(FlowDir) {
     size = 0;
     marker = nullptr;
     ttotal = nullptr;
@@ -1061,14 +1060,14 @@ public:
     bool err = false;
 
     auto getval = [&](unsigned short i, unsigned short j) {
-      istringstream ss(option_value[6*i + j]);
+      istringstream ss(option_value[6 * i + j]);
       su2double val;
       if (!(ss >> val)) err = true;
       return val;
     };
 
     for (unsigned short i = 0; i < nVals; i++) {
-      marker[i].assign(option_value[6*i]);
+      marker[i].assign(option_value[6 * i]);
       ttotal[i] = getval(i, 1);
       ptotal[i] = getval(i, 2);
       flowdir[i][0] = getval(i, 3);
@@ -1096,40 +1095,40 @@ template <class T>
 struct CStringValuesListHelper<T*> {
   static T* resize(unsigned short n) { return new T[n]; }
   static T& access(T* ptr, unsigned short i) { return ptr[i]; }
-  static void clear(T* ptr) { delete [] ptr; }
+  static void clear(T* ptr) { delete[] ptr; }
 };
 
 // Class where the option is represented by (string, N * "some type", string, N * "some type", ...)
 template <class Type>
 class COptionStringValuesList final : public COptionBase {
-  const string name;     // identifier for the option
-  unsigned short& size;  // number of string-value pairs
-  string*& strings;      // the strings in the option
-  Type*& values;         // the values per string
-  unsigned short& num_vals; // how many values per string
-  unsigned short optional_num_vals = 0; // num_vals points to this when it is not provided in the ctor.
-
-public:
-  COptionStringValuesList(string name_, unsigned short& size_, string*& strings_,
-                          Type*& values_, unsigned short& num_vals_) :
-    name(name_), size(size_), strings(strings_), values(values_), num_vals(num_vals_) {
+  const string name;                     // identifier for the option
+  unsigned short& size;                  // number of string-value pairs
+  string*& strings;                      // the strings in the option
+  Type*& values;                         // the values per string
+  unsigned short& num_vals;              // how many values per string
+  unsigned short optional_num_vals = 0;  // num_vals points to this when it is not provided in the ctor.
+
+ public:
+  COptionStringValuesList(string name_, unsigned short& size_, string*& strings_, Type*& values_,
+                          unsigned short& num_vals_)
+      : name(name_), size(size_), strings(strings_), values(values_), num_vals(num_vals_) {
     strings = nullptr;
     values = nullptr;
   }
 
-  COptionStringValuesList(string name_, unsigned short& size_, string*& strings_, Type*& values_) :
-    name(name_), size(size_), strings(strings_), values(values_), num_vals(optional_num_vals) {
+  COptionStringValuesList(string name_, unsigned short& size_, string*& strings_, Type*& values_)
+      : name(name_), size(size_), strings(strings_), values(values_), num_vals(optional_num_vals) {
     strings = nullptr;
     values = nullptr;
   }
 
   ~COptionStringValuesList() {
-    delete [] strings;
+    delete[] strings;
     strings = nullptr;
     for (unsigned short i = 0; i < size; ++i) {
       CStringValuesListHelper<Type>::clear(values[i]);
     }
-    delete [] values;
+    delete[] values;
     values = nullptr;
   }
 
@@ -1188,32 +1187,32 @@ public:
   }
 
   void SetDefault() override {
-    size = 0; // There is no default value for lists
+    size = 0;  // There is no default value for lists
     num_vals = 0;
   }
 };
 
-
 template <class Tenum>
 class COptionRiemann : public COptionBase {
-
-protected:
+ protected:
   map<string, Tenum> m;
-  string name; // identifier for the option
-  unsigned short & size;
-  string * & marker;
-  unsigned short* & field; // Reference to the field name
-  su2double * & var1;
-  su2double * & var2;
-  su2double ** & flowdir;
-
-public:
-  COptionRiemann(string option_field_name, unsigned short & nMarker_Riemann, string* & Marker_Riemann, unsigned short* & option_field, const map<string, Tenum> m, su2double* & var1, su2double* & var2, su2double** & FlowDir) : size(nMarker_Riemann),
-                  marker(Marker_Riemann), field(option_field), var1(var1), var2(var2), flowdir(FlowDir) {
+  string name;  // identifier for the option
+  unsigned short& size;
+  string*& marker;
+  unsigned short*& field;  // Reference to the field name
+  su2double*& var1;
+  su2double*& var2;
+  su2double**& flowdir;
+
+ public:
+  COptionRiemann(string option_field_name, unsigned short& nMarker_Riemann, string*& Marker_Riemann,
+                 unsigned short*& option_field, const map<string, Tenum> m, su2double*& var1, su2double*& var2,
+                 su2double**& FlowDir)
+      : size(nMarker_Riemann), marker(Marker_Riemann), field(option_field), var1(var1), var2(var2), flowdir(FlowDir) {
     this->name = option_field_name;
     this->m = m;
   }
-  ~COptionRiemann() override {};
+  ~COptionRiemann() override{};
 
   string SetValue(const vector<string>& option_value) override {
     COptionBase::SetValue(option_value);
@@ -1254,36 +1253,36 @@ public:
     }
 
     for (unsigned long i = 0; i < nVals; i++) {
-      this->marker[i].assign(option_value[7*i]);
-        // Check to see if the enum value is in the map
-    if (this->m.find(option_value[7*i + 1]) == m.end()) {
-      string str;
-      str.append(this->name);
-      str.append(": invalid option value ");
-      str.append(option_value[0]);
-      str.append(". Check current SU2 options in config_template.cfg.");
-      return str;
-    }
-      Tenum val = this->m[option_value[7*i + 1]];
+      this->marker[i].assign(option_value[7 * i]);
+      // Check to see if the enum value is in the map
+      if (this->m.find(option_value[7 * i + 1]) == m.end()) {
+        string str;
+        str.append(this->name);
+        str.append(": invalid option value ");
+        str.append(option_value[0]);
+        str.append(". Check current SU2 options in config_template.cfg.");
+        return str;
+      }
+      Tenum val = this->m[option_value[7 * i + 1]];
       this->field[i] = val;
 
-      istringstream ss_1st(option_value[7*i + 2]);
+      istringstream ss_1st(option_value[7 * i + 2]);
       if (!(ss_1st >> this->var1[i])) {
         return badValue("Riemann", this->name);
       }
-      istringstream ss_2nd(option_value[7*i + 3]);
+      istringstream ss_2nd(option_value[7 * i + 3]);
       if (!(ss_2nd >> this->var2[i])) {
         return badValue("Riemann", this->name);
       }
-      istringstream ss_3rd(option_value[7*i + 4]);
+      istringstream ss_3rd(option_value[7 * i + 4]);
       if (!(ss_3rd >> this->flowdir[i][0])) {
         return badValue("Riemann", this->name);
       }
-      istringstream ss_4th(option_value[7*i + 5]);
+      istringstream ss_4th(option_value[7 * i + 5]);
       if (!(ss_4th >> this->flowdir[i][1])) {
         return badValue("Riemann", this->name);
       }
-      istringstream ss_5th(option_value[7*i + 6]);
+      istringstream ss_5th(option_value[7 * i + 6]);
       if (!(ss_5th >> this->flowdir[i][2])) {
         return badValue("Riemann", this->name);
       }
@@ -1297,31 +1296,39 @@ public:
     this->var1 = nullptr;
     this->var2 = nullptr;
     this->flowdir = nullptr;
-    this->size = 0; // There is no default value for list
+    this->size = 0;  // There is no default value for list
   }
 };
 
 template <class Tenum>
-class COptionGiles : public COptionBase{
-
+class COptionGiles : public COptionBase {
   map<string, Tenum> m;
-  unsigned short & size;
-  string * & marker;
-  unsigned short* & field; // Reference to the fieldname
-  string name; // identifier for the option
-  su2double * & var1;
-  su2double * & var2;
-  su2double ** & flowdir;
-  su2double * & relfac1;
-  su2double * & relfac2;
-
-public:
-  COptionGiles(string option_field_name, unsigned short & nMarker_Giles, string* & Marker_Giles, unsigned short* & option_field, const map<string, Tenum> m, su2double* & var1, su2double* & var2, su2double** & FlowDir, su2double* & relfac1, su2double* & relfac2) : size(nMarker_Giles),
-               marker(Marker_Giles), field(option_field), var1(var1), var2(var2), flowdir(FlowDir), relfac1(relfac1), relfac2(relfac2) {
+  unsigned short& size;
+  string*& marker;
+  unsigned short*& field;  // Reference to the fieldname
+  string name;             // identifier for the option
+  su2double*& var1;
+  su2double*& var2;
+  su2double**& flowdir;
+  su2double*& relfac1;
+  su2double*& relfac2;
+
+ public:
+  COptionGiles(string option_field_name, unsigned short& nMarker_Giles, string*& Marker_Giles,
+               unsigned short*& option_field, const map<string, Tenum> m, su2double*& var1, su2double*& var2,
+               su2double**& FlowDir, su2double*& relfac1, su2double*& relfac2)
+      : size(nMarker_Giles),
+        marker(Marker_Giles),
+        field(option_field),
+        var1(var1),
+        var2(var2),
+        flowdir(FlowDir),
+        relfac1(relfac1),
+        relfac2(relfac2) {
     this->name = option_field_name;
     this->m = m;
   }
-  ~COptionGiles() override {};
+  ~COptionGiles() override{};
 
   string SetValue(const vector<string>& option_value) override {
     COptionBase::SetValue(option_value);
@@ -1368,44 +1375,44 @@ public:
     }
 
     for (unsigned int i = 0; i < nVals; i++) {
-      this->marker[i].assign(option_value[9*i]);
-        // Check to see if the enum value is in the map
-    if (this->m.find(option_value[9*i + 1]) == m.end()) {
-      string str;
-      str.append(this->name);
-      str.append(": invalid option value ");
-      str.append(option_value[0]);
-      str.append(". Check current SU2 options in config_template.cfg.");
-      return str;
-    }
-      Tenum val = this->m[option_value[9*i + 1]];
+      this->marker[i].assign(option_value[9 * i]);
+      // Check to see if the enum value is in the map
+      if (this->m.find(option_value[9 * i + 1]) == m.end()) {
+        string str;
+        str.append(this->name);
+        str.append(": invalid option value ");
+        str.append(option_value[0]);
+        str.append(". Check current SU2 options in config_template.cfg.");
+        return str;
+      }
+      Tenum val = this->m[option_value[9 * i + 1]];
       this->field[i] = val;
 
-      istringstream ss_1st(option_value[9*i + 2]);
+      istringstream ss_1st(option_value[9 * i + 2]);
       if (!(ss_1st >> this->var1[i])) {
         return badValue("Giles BC", this->name);
       }
-      istringstream ss_2nd(option_value[9*i + 3]);
+      istringstream ss_2nd(option_value[9 * i + 3]);
       if (!(ss_2nd >> this->var2[i])) {
         return badValue("Giles BC", this->name);
       }
-      istringstream ss_3rd(option_value[9*i + 4]);
+      istringstream ss_3rd(option_value[9 * i + 4]);
       if (!(ss_3rd >> this->flowdir[i][0])) {
         return badValue("Giles BC", this->name);
       }
-      istringstream ss_4th(option_value[9*i + 5]);
+      istringstream ss_4th(option_value[9 * i + 5]);
       if (!(ss_4th >> this->flowdir[i][1])) {
         return badValue("Giles BC", this->name);
       }
-      istringstream ss_5th(option_value[9*i + 6]);
+      istringstream ss_5th(option_value[9 * i + 6]);
       if (!(ss_5th >> this->flowdir[i][2])) {
         return badValue("Giles BC", this->name);
       }
-      istringstream ss_6th(option_value[9*i + 7]);
+      istringstream ss_6th(option_value[9 * i + 7]);
       if (!(ss_6th >> this->relfac1[i])) {
         return badValue("Giles BC", this->name);
       }
-      istringstream ss_7th(option_value[9*i + 8]);
+      istringstream ss_7th(option_value[9 * i + 8]);
       if (!(ss_7th >> this->relfac2[i])) {
         return badValue("Giles BC", this->name);
       }
@@ -1421,25 +1428,21 @@ public:
     this->relfac1 = nullptr;
     this->relfac2 = nullptr;
     this->flowdir = nullptr;
-    this->size = 0; // There is no default value for list
+    this->size = 0;  // There is no default value for list
   }
 };
 
 class COptionExhaust : public COptionBase {
-  string name; // identifier for the option
+  string name;  // identifier for the option
   unsigned short& size;
   string*& marker;
   su2double*& ttotal;
   su2double*& ptotal;
 
-public:
-  COptionExhaust(string option_field_name, unsigned short& nMarker_Exhaust, string*& Marker_Exhaust,
-                 su2double*& Ttotal, su2double*& Ptotal)
-    : name(option_field_name),
-      size(nMarker_Exhaust),
-      marker(Marker_Exhaust),
-      ttotal(Ttotal),
-      ptotal(Ptotal) {
+ public:
+  COptionExhaust(string option_field_name, unsigned short& nMarker_Exhaust, string*& Marker_Exhaust, su2double*& Ttotal,
+                 su2double*& Ptotal)
+      : name(option_field_name), size(nMarker_Exhaust), marker(Marker_Exhaust), ttotal(Ttotal), ptotal(Ptotal) {
     size = 0;
     marker = nullptr;
     ttotal = nullptr;
@@ -1472,12 +1475,12 @@ public:
     ptotal = new su2double[nVals];
 
     for (unsigned short i = 0; i < nVals; i++) {
-      this->marker[i].assign(option_value[3*i]);
+      this->marker[i].assign(option_value[3 * i]);
 
-      istringstream ss_1st(option_value[3*i + 1]);
+      istringstream ss_1st(option_value[3 * i + 1]);
       if (!(ss_1st >> ttotal[i])) return badValue("exhaust fixed", name);
 
-      istringstream ss_2nd(option_value[3*i + 2]);
+      istringstream ss_2nd(option_value[3 * i + 2]);
       if (!(ss_2nd >> ptotal[i])) return badValue("exhaust fixed", name);
     }
     return "";
@@ -1487,7 +1490,7 @@ public:
 };
 
 class COptionPeriodic : public COptionBase {
-  string name; // identifier for the option
+  string name;  // identifier for the option
   unsigned short& size;
   string*& marker_bound;
   string*& marker_donor;
@@ -1495,16 +1498,16 @@ class COptionPeriodic : public COptionBase {
   su2double**& rot_angles;
   su2double**& translation;
 
-public:
+ public:
   COptionPeriodic(const string option_field_name, unsigned short& nMarker_PerBound, string*& Marker_PerBound,
                   string*& Marker_PerDonor, su2double**& RotCenter, su2double**& RotAngles, su2double**& Translation)
-    : name(option_field_name),
-      size(nMarker_PerBound),
-      marker_bound(Marker_PerBound),
-      marker_donor(Marker_PerDonor),
-      rot_center(RotCenter),
-      rot_angles(RotAngles),
-      translation(Translation) {
+      : name(option_field_name),
+        size(nMarker_PerBound),
+        marker_bound(Marker_PerBound),
+        marker_donor(Marker_PerDonor),
+        rot_center(RotCenter),
+        rot_angles(RotAngles),
+        translation(Translation) {
     size = 0;
     COptionPeriodic::SetDefault();
   }
@@ -1535,7 +1538,7 @@ public:
       return name + ": must have a number of entries divisible by 11";
     }
 
-    const unsigned short nVals = 2 * (totalVals / mod_num); // "2" to account for periodic and donor
+    const unsigned short nVals = 2 * (totalVals / mod_num);  // "2" to account for periodic and donor
     size = nVals;
     marker_bound = new string[nVals];
     marker_donor = new string[nVals];
@@ -1548,43 +1551,43 @@ public:
       translation[i] = new su2double[3];
     }
 
-    const su2double deg2rad = PI_NUMBER/180.0;
+    const su2double deg2rad = PI_NUMBER / 180.0;
 
     bool err = false;
 
     auto getval = [&](unsigned short i, unsigned short j) {
-      istringstream ss(option_value[mod_num*i + j]);
+      istringstream ss(option_value[mod_num * i + j]);
       su2double val;
       if (!(ss >> val)) err = true;
       return val;
     };
 
     for (unsigned short i = 0; i < nVals / 2; i++) {
-      marker_bound[i].assign(option_value[mod_num*i]);
-      marker_donor[i].assign(option_value[mod_num*i+1]);
+      marker_bound[i].assign(option_value[mod_num * i]);
+      marker_donor[i].assign(option_value[mod_num * i + 1]);
       /*--- Mirror the connection between markers. ---*/
-      marker_bound[i+nVals/2] = marker_donor[i];
-      marker_donor[i+nVals/2] = marker_bound[i];
+      marker_bound[i + nVals / 2] = marker_donor[i];
+      marker_donor[i + nVals / 2] = marker_bound[i];
 
-      rot_center[i][0] = rot_center[i+nVals/2][0] = getval(i, 2);
-      rot_center[i][1] = rot_center[i+nVals/2][1] = getval(i, 3);
-      rot_center[i][2] = rot_center[i+nVals/2][2] = getval(i, 4);
+      rot_center[i][0] = rot_center[i + nVals / 2][0] = getval(i, 2);
+      rot_center[i][1] = rot_center[i + nVals / 2][1] = getval(i, 3);
+      rot_center[i][2] = rot_center[i + nVals / 2][2] = getval(i, 4);
 
-      rot_angles[i][0] = rot_angles[i+nVals/2][0] = getval(i, 5) * deg2rad;
-      rot_angles[i][1] = rot_angles[i+nVals/2][1] = getval(i, 6) * deg2rad;
-      rot_angles[i][2] = rot_angles[i+nVals/2][2] = getval(i, 7) * deg2rad;
+      rot_angles[i][0] = rot_angles[i + nVals / 2][0] = getval(i, 5) * deg2rad;
+      rot_angles[i][1] = rot_angles[i + nVals / 2][1] = getval(i, 6) * deg2rad;
+      rot_angles[i][2] = rot_angles[i + nVals / 2][2] = getval(i, 7) * deg2rad;
 
-      translation[i][0] = translation[i+nVals/2][0] = getval(i, 8);
-      translation[i][1] = translation[i+nVals/2][1] = getval(i, 9);
-      translation[i][2] = translation[i+nVals/2][2] = getval(i, 10);
+      translation[i][0] = translation[i + nVals / 2][0] = getval(i, 8);
+      translation[i][1] = translation[i + nVals / 2][1] = getval(i, 9);
+      translation[i][2] = translation[i + nVals / 2][2] = getval(i, 10);
 
       /*--- Mirror the rotational angles and translation vector (rotational center does not need to move). ---*/
-      rot_angles[i+nVals/2][0] *= -1;
-      rot_angles[i+nVals/2][1] *= -1;
-      rot_angles[i+nVals/2][2] *= -1;
-      translation[i+nVals/2][0] *= -1;
-      translation[i+nVals/2][1] *= -1;
-      translation[i+nVals/2][2] *= -1;
+      rot_angles[i + nVals / 2][0] *= -1;
+      rot_angles[i + nVals / 2][1] *= -1;
+      rot_angles[i + nVals / 2][2] *= -1;
+      translation[i + nVals / 2][0] *= -1;
+      translation[i + nVals / 2][1] *= -1;
+      translation[i + nVals / 2][2] *= -1;
 
       if (err) return badValue("periodic", name);
     }
@@ -1602,18 +1605,19 @@ public:
 };
 
 class COptionTurboPerformance : public COptionBase {
-  string name; // identifier for the option
-  unsigned short & size;
-  string * & marker_turboIn;
-  string * & marker_turboOut;
-
-public:
-  COptionTurboPerformance(const string option_field_name, unsigned short & nMarker_TurboPerf,
-                          string* & Marker_TurboBoundIn, string* & Marker_TurboBoundOut) : size(nMarker_TurboPerf), marker_turboIn(Marker_TurboBoundIn), marker_turboOut(Marker_TurboBoundOut){
+  string name;  // identifier for the option
+  unsigned short& size;
+  string*& marker_turboIn;
+  string*& marker_turboOut;
+
+ public:
+  COptionTurboPerformance(const string option_field_name, unsigned short& nMarker_TurboPerf,
+                          string*& Marker_TurboBoundIn, string*& Marker_TurboBoundOut)
+      : size(nMarker_TurboPerf), marker_turboIn(Marker_TurboBoundIn), marker_turboOut(Marker_TurboBoundOut) {
     this->name = option_field_name;
   }
 
-  ~COptionTurboPerformance() override {};
+  ~COptionTurboPerformance() override{};
   string SetValue(const vector<string>& option_value) override {
     COptionBase::SetValue(option_value);
     const int mod_num = 2;
@@ -1621,7 +1625,7 @@ public:
     unsigned long totalVals = option_value.size();
     if ((totalVals == 1) && (option_value[0].compare("NONE") == 0)) {
       this->size = 0;
-      this->marker_turboIn= nullptr;
+      this->marker_turboIn = nullptr;
       this->marker_turboOut = nullptr;
       return "";
     }
@@ -1631,8 +1635,9 @@ public:
       newstring.append(this->name);
       newstring.append(": must have a number of entries divisible by 2");
       this->size = 0;
-      this->marker_turboIn= nullptr;
-      this->marker_turboOut = nullptr;;
+      this->marker_turboIn = nullptr;
+      this->marker_turboOut = nullptr;
+      ;
       return newstring;
     }
 
@@ -1641,59 +1646,60 @@ public:
     this->marker_turboIn = new string[nVals];
     this->marker_turboOut = new string[nVals];
     for (unsigned long i = 0; i < nVals; i++) {
-      this->marker_turboIn[i].assign(option_value[mod_num*i]);
-      this->marker_turboOut[i].assign(option_value[mod_num*i+1]);
-     }
-
+      this->marker_turboIn[i].assign(option_value[mod_num * i]);
+      this->marker_turboOut[i].assign(option_value[mod_num * i + 1]);
+    }
 
     return "";
   }
 
   void SetDefault() override {
     this->size = 0;
-    this->marker_turboIn= nullptr;
+    this->marker_turboIn = nullptr;
     this->marker_turboOut = nullptr;
   }
 };
 
 class COptionPython : public COptionBase {
   string name;
-public:
-  COptionPython(const string name) {
-    this->name = name;
-  }
-  ~COptionPython() override {};
+
+ public:
+  COptionPython(const string name) { this->name = name; }
+  ~COptionPython() override{};
   // No checking happens with python options
   string SetValue(const vector<string>& option_value) override {
     COptionBase::SetValue(option_value);
     return "";
   }
   // No defaults with python options
-  void SetDefault() override {
-    return;
-  };
+  void SetDefault() override { return; };
 };
 
 class COptionActDisk : public COptionBase {
-  string name; // identifier for the option
-  unsigned short & inlet_size;
-  unsigned short & outlet_size;
-  string * & marker_inlet;
-  string * & marker_outlet;
-  su2double ** & press_jump;
-  su2double ** & temp_jump;
-  su2double ** & omega;
-
-public:
-  COptionActDisk(const string name,
-                 unsigned short & nMarker_ActDiskInlet, unsigned short & nMarker_ActDiskOutlet, string * & Marker_ActDiskInlet, string * & Marker_ActDiskOutlet,
-                 su2double ** & ActDisk_PressJump, su2double ** & ActDisk_TempJump, su2double ** & ActDisk_Omega) :
-  inlet_size(nMarker_ActDiskInlet), outlet_size(nMarker_ActDiskOutlet), marker_inlet(Marker_ActDiskInlet), marker_outlet(Marker_ActDiskOutlet),
-  press_jump(ActDisk_PressJump), temp_jump(ActDisk_TempJump), omega(ActDisk_Omega) {
+  string name;  // identifier for the option
+  unsigned short& inlet_size;
+  unsigned short& outlet_size;
+  string*& marker_inlet;
+  string*& marker_outlet;
+  su2double**& press_jump;
+  su2double**& temp_jump;
+  su2double**& omega;
+
+ public:
+  COptionActDisk(const string name, unsigned short& nMarker_ActDiskInlet, unsigned short& nMarker_ActDiskOutlet,
+                 string*& Marker_ActDiskInlet, string*& Marker_ActDiskOutlet, su2double**& ActDisk_PressJump,
+                 su2double**& ActDisk_TempJump, su2double**& ActDisk_Omega)
+      : inlet_size(nMarker_ActDiskInlet),
+        outlet_size(nMarker_ActDiskOutlet),
+        marker_inlet(Marker_ActDiskInlet),
+        marker_outlet(Marker_ActDiskOutlet),
+        press_jump(ActDisk_PressJump),
+        temp_jump(ActDisk_TempJump),
+        omega(ActDisk_Omega) {
     this->name = name;
   }
 
-  ~COptionActDisk() override {};
+  ~COptionActDisk() override{};
   string SetValue(const vector<string>& option_value) override {
     COptionBase::SetValue(option_value);
     const int mod_num = 8;
@@ -1729,29 +1735,29 @@ public:
     string tname = "actuator disk";
 
     for (int i = 0; i < this->inlet_size; i++) {
-      this->marker_inlet[i].assign(option_value[mod_num*i]);
-      this->marker_outlet[i].assign(option_value[mod_num*i+1]);
-      istringstream ss_1st(option_value[mod_num*i + 2]);
+      this->marker_inlet[i].assign(option_value[mod_num * i]);
+      this->marker_outlet[i].assign(option_value[mod_num * i + 1]);
+      istringstream ss_1st(option_value[mod_num * i + 2]);
       if (!(ss_1st >> this->press_jump[i][0])) {
         return badValue(tname, this->name);
       }
-      istringstream ss_2nd(option_value[mod_num*i + 3]);
+      istringstream ss_2nd(option_value[mod_num * i + 3]);
       if (!(ss_2nd >> this->temp_jump[i][0])) {
         return badValue(tname, this->name);
       }
-      istringstream ss_3rd(option_value[mod_num*i + 4]);
+      istringstream ss_3rd(option_value[mod_num * i + 4]);
       if (!(ss_3rd >> this->omega[i][0])) {
         return badValue(tname, this->name);
       }
-      istringstream ss_4th(option_value[mod_num*i + 5]);
+      istringstream ss_4th(option_value[mod_num * i + 5]);
       if (!(ss_4th >> this->press_jump[i][1])) {
         return badValue(tname, this->name);
       }
-      istringstream ss_5th(option_value[mod_num*i + 6]);
+      istringstream ss_5th(option_value[mod_num * i + 6]);
       if (!(ss_5th >> this->temp_jump[i][1])) {
         return badValue(tname, this->name);
       }
-      istringstream ss_6th(option_value[mod_num*i + 7]);
+      istringstream ss_6th(option_value[mod_num * i + 7]);
       if (!(ss_6th >> this->omega[i][1])) {
         return badValue(tname, this->name);
       }
@@ -1770,22 +1776,22 @@ public:
 };
 
 class COptionWallFunction : public COptionBase {
-  string name; // identifier for the option
+  string name;  // identifier for the option
   unsigned short& nMarkers;
   string*& markers;
   WALL_FUNCTIONS*& walltype;
   unsigned short**& intInfo;
   su2double**& doubleInfo;
 
-public:
+ public:
   COptionWallFunction(const string name_WF, unsigned short& nMarker_WF, string*& Marker_WF, WALL_FUNCTIONS*& type_WF,
                       unsigned short**& intInfo_WF, su2double**& doubleInfo_WF)
-    : name(name_WF),
-      nMarkers(nMarker_WF),
-      markers(Marker_WF),
-      walltype(type_WF),
-      intInfo(intInfo_WF),
-      doubleInfo(doubleInfo_WF) {
+      : name(name_WF),
+        nMarkers(nMarker_WF),
+        markers(Marker_WF),
+        walltype(type_WF),
+        intInfo(intInfo_WF),
+        doubleInfo(doubleInfo_WF) {
     nMarkers = 0;
     COptionWallFunction::SetDefault();
   }
@@ -1813,8 +1819,7 @@ public:
     /*--- Determine the number of markers, for which a wall
           function treatment has been specified. ---*/
     unsigned short counter = 0, nVals = 0;
-    while (counter < totalSize ) {
-
+    while (counter < totalSize) {
       /* Update the counter for the number of markers specified
          and store the current index for possible error messages. */
       ++nVals;
@@ -1826,17 +1831,18 @@ public:
       const unsigned short indWallType = counter;
       auto typeWF = WALL_FUNCTIONS::NONE;
       bool validWF = true;
-      if (counter == totalSize) validWF = false;
+      if (counter == totalSize)
+        validWF = false;
       else {
         map<string, WALL_FUNCTIONS>::const_iterator it;
         it = Wall_Functions_Map.find(option_value[counter]);
-        if(it == Wall_Functions_Map.end())
+        if (it == Wall_Functions_Map.end())
           validWF = false;
         else
-          typeWF  = it->second;
+          typeWF = it->second;
       }
 
-      if (!validWF ) {
+      if (!validWF) {
         string newstring;
         newstring.append(this->name);
         newstring.append(": Invalid wall function type, ");
@@ -1852,11 +1858,18 @@ public:
       /*--- For some wall function types some additional info
             must be specified. Hence the counter must be updated
             accordingly. ---*/
-      switch( typeWF ) {
-        case WALL_FUNCTIONS::EQUILIBRIUM_MODEL:    counter += 3; break;
-        case WALL_FUNCTIONS::NONEQUILIBRIUM_MODEL: counter += 2; break;
-        case WALL_FUNCTIONS::LOGARITHMIC_MODEL: counter += 3; break;
-        default: break;
+      switch (typeWF) {
+        case WALL_FUNCTIONS::EQUILIBRIUM_MODEL:
+          counter += 3;
+          break;
+        case WALL_FUNCTIONS::NONEQUILIBRIUM_MODEL:
+          counter += 2;
+          break;
+        case WALL_FUNCTIONS::LOGARITHMIC_MODEL:
+          counter += 3;
+          break;
+        default:
+          break;
       }
 
       /* In case the counter is larger than totalSize, the data for
@@ -1874,17 +1887,16 @@ public:
     }
 
     /* Allocate the memory to store the data for the wall function markers. */
-    this->nMarkers   = nVals;
-    this->markers    = new string[nVals];
-    this->walltype   = new WALL_FUNCTIONS[nVals];
-    this->intInfo    = new unsigned short*[nVals]();
+    this->nMarkers = nVals;
+    this->markers = new string[nVals];
+    this->walltype = new WALL_FUNCTIONS[nVals];
+    this->intInfo = new unsigned short*[nVals]();
     this->doubleInfo = new su2double*[nVals]();
 
     /*--- Loop over the wall markers and store the info in the
           appropriate arrays. ---*/
     counter = 0;
-    for (unsigned short i=0; i<nVals; i++) {
-
+    for (unsigned short i = 0; i < nVals; i++) {
       /* Set the name of the wall function marker. */
       this->markers[i].assign(option_value[counter++]);
 
@@ -1897,13 +1909,11 @@ public:
 
       /*--- For some wall function types, some additional info
             is needed, which is extracted from option_value. ---*/
-      switch( this->walltype[i] ) {
-
+      switch (this->walltype[i]) {
         case WALL_FUNCTIONS::EQUILIBRIUM_MODEL: {
-
           /* LES equilibrium wall model. The exchange distance, stretching
              factor and number of points in the wall model must be specified. */
-          this->intInfo[i]    = new unsigned short[1];
+          this->intInfo[i] = new unsigned short[1];
           this->doubleInfo[i] = new su2double[2];
 
           istringstream ss_1st(option_value[counter++]);
@@ -1925,24 +1935,23 @@ public:
         }
 
         case WALL_FUNCTIONS::NONEQUILIBRIUM_MODEL: {
-
           /* LES non-equilibrium model. The RANS turbulence model and
              the exchange distance need to be specified. */
-          this->intInfo[i]    = new unsigned short[1];
+          this->intInfo[i] = new unsigned short[1];
           this->doubleInfo[i] = new su2double[1];
 
           /* Check for a valid RANS turbulence model. */
           map<string, TURB_MODEL>::const_iterator iit;
           iit = Turb_Model_Map.find(option_value[counter++]);
-          if(iit == Turb_Model_Map.end()) {
+          if (iit == Turb_Model_Map.end()) {
             string newstring;
             newstring.append(this->name);
             newstring.append(", marker ");
             newstring.append(this->markers[i]);
             newstring.append(", wall function type ");
-            newstring.append(option_value[counter-2]);
+            newstring.append(option_value[counter - 2]);
             newstring.append(": Invalid RANS turbulence model, ");
-            newstring.append(option_value[counter-1]);
+            newstring.append(option_value[counter - 1]);
             newstring.append(", specified");
             return newstring;
           }
@@ -1956,10 +1965,9 @@ public:
           break;
         }
         case WALL_FUNCTIONS::LOGARITHMIC_MODEL: {
-
           /* LES Logarithmic law-of-the-wall model. The exchange distance, stretching
            factor and number of points in the wall model must be specified. */
-          this->intInfo[i]    = new unsigned short[1];
+          this->intInfo[i] = new unsigned short[1];
           this->doubleInfo[i] = new su2double[2];
 
           istringstream ss_1st(option_value[counter++]);
@@ -1980,7 +1988,7 @@ public:
           break;
         }
 
-        default: // Just to avoid a compiler warning.
+        default:  // Just to avoid a compiler warning.
           break;
       }
     }
diff --git a/Common/include/parallelization/mpi_structure.cpp b/Common/include/parallelization/mpi_structure.cpp
index cd8eae4d5f0..43b2c86a239 100644
--- a/Common/include/parallelization/mpi_structure.cpp
+++ b/Common/include/parallelization/mpi_structure.cpp
@@ -26,8 +26,7 @@
  */
 
 #include "mpi_structure.hpp"
-#include <cstring> // memcpy
-
+#include <cstring>  // memcpy
 
 /* Initialise the MPI Communicator Rank and Size */
 int CBaseMPIWrapper::Rank = 0;
@@ -41,12 +40,11 @@ CBaseMPIWrapper::Comm CBaseMPIWrapper::currentComm = 0;  // dummy value
 #endif
 
 #ifdef HAVE_MPI
-int  CBaseMPIWrapper::MinRankError;
+int CBaseMPIWrapper::MinRankError;
 bool CBaseMPIWrapper::winMinRankErrorInUse = false;
 CBaseMPIWrapper::Win CBaseMPIWrapper::winMinRankError;
 
-void CBaseMPIWrapper::Error(std::string ErrorMsg, std::string FunctionName){
-
+void CBaseMPIWrapper::Error(std::string ErrorMsg, std::string FunctionName) {
   /* Set MinRankError to Rank, as the error message is called on this rank. */
   MinRankError = Rank;
   int flag = 0;
@@ -58,13 +56,12 @@ void CBaseMPIWrapper::Error(std::string ErrorMsg, std::string FunctionName){
 
   /* Try to complete the non-blocking barrier call for a second. */
   double startTime = SU2_MPI::Wtime();
-  while( true ) {
-
+  while (true) {
     MPI_Test(&barrierRequest, &flag, MPI_STATUS_IGNORE);
-    if( flag ) break;
+    if (flag) break;
 
     double currentTime = SU2_MPI::Wtime();
-    if(currentTime > startTime + 1.0) break;
+    if (currentTime > startTime + 1.0) break;
   }
 #else
   /* MPI_Ibarrier function is not supported. Simply wait for one
@@ -76,23 +73,21 @@ void CBaseMPIWrapper::Error(std::string ErrorMsg, std::string FunctionName){
 #endif
 #endif
 
-  if( flag ) {
+  if (flag) {
     /* The barrier is completed and hence the error call is collective.
        Set MinRankError to 0. */
     MinRankError = 0;
-  }
-  else {
+  } else {
     /* The error call is not collective and the minimum rank must be
        determined by one sided communication. Loop over the lower numbered
        ranks to check if they participate in the error message. */
-    for(int i=0; i<Rank; ++i) {
-
+    for (int i = 0; i < Rank; ++i) {
       int MinRankErrorOther;
       MPI_Win_lock(MPI_LOCK_SHARED, i, 0, winMinRankError);
       MPI_Get(&MinRankErrorOther, 1, MPI_INT, i, 0, 1, MPI_INT, winMinRankError);
       MPI_Win_unlock(i, winMinRankError);
 
-      if(MinRankErrorOther < MinRankError) {
+      if (MinRankErrorOther < MinRankError) {
         MinRankError = MinRankErrorOther;
         break;
       }
@@ -100,79 +95,82 @@ void CBaseMPIWrapper::Error(std::string ErrorMsg, std::string FunctionName){
   }
 
   /* Check if this rank must write the error message and do so. */
-  if (Rank == MinRankError){
+  if (Rank == MinRankError) {
     std::cout << std::endl << std::endl;
     std::cout << "Error in \"" << FunctionName << "\": " << std::endl;
-    std::cout <<  "-------------------------------------------------------------------------" << std::endl;
+    std::cout << "-------------------------------------------------------------------------" << std::endl;
     std::cout << ErrorMsg << std::endl;
-    std::cout <<  "------------------------------ Error Exit -------------------------------" << std::endl;
+    std::cout << "------------------------------ Error Exit -------------------------------" << std::endl;
     std::cout << std::endl << std::endl;
   }
   Abort(currentComm, EXIT_FAILURE);
 }
 
-void CBaseMPIWrapper::CopyData(const void* sendbuf, void* recvbuf, int size, Datatype datatype, int recvshift, int sendshift) {
-  if(datatype==MPI_DOUBLE) {
+void CBaseMPIWrapper::CopyData(const void* sendbuf, void* recvbuf, int size, Datatype datatype, int recvshift,
+                               int sendshift) {
+  if (datatype == MPI_DOUBLE) {
     for (int i = 0; i < size; i++) {
-      static_cast<su2double*>(recvbuf)[i+recvshift] = static_cast<const su2double*>(sendbuf)[i+sendshift];
+      static_cast<su2double*>(recvbuf)[i + recvshift] = static_cast<const su2double*>(sendbuf)[i + sendshift];
     }
   } else {
     int scalarsize;
     MPI_Type_size(datatype, &scalarsize);
-    const char* src = static_cast<const char*>(sendbuf) + sendshift*static_cast<size_t>(scalarsize);
-    char* dest = static_cast<char*>(recvbuf) + recvshift*static_cast<size_t>(scalarsize);
-    std::memcpy(static_cast<void*>(dest), static_cast<const void*>(src), size*static_cast<size_t>(scalarsize));
+    const char* src = static_cast<const char*>(sendbuf) + sendshift * static_cast<size_t>(scalarsize);
+    char* dest = static_cast<char*>(recvbuf) + recvshift * static_cast<size_t>(scalarsize);
+    std::memcpy(static_cast<void*>(dest), static_cast<const void*>(src), size * static_cast<size_t>(scalarsize));
   }
 }
-#else // HAVE_MPI
+#else  // HAVE_MPI
 
-void CBaseMPIWrapper::Error(std::string ErrorMsg, std::string FunctionName){
-  if (Rank == 0){
+void CBaseMPIWrapper::Error(std::string ErrorMsg, std::string FunctionName) {
+  if (Rank == 0) {
     std::cout << std::endl << std::endl;
     std::cout << "Error in \"" << FunctionName << "\": " << std::endl;
-    std::cout <<  "-------------------------------------------------------------------------" << std::endl;
+    std::cout << "-------------------------------------------------------------------------" << std::endl;
     std::cout << ErrorMsg << std::endl;
-    std::cout <<  "------------------------------ Error Exit -------------------------------" << std::endl;
+    std::cout << "------------------------------ Error Exit -------------------------------" << std::endl;
     std::cout << std::endl << std::endl;
   }
   Abort(currentComm, 0);
 }
 
-void CBaseMPIWrapper::CopyData(const void* sendbuf, void* recvbuf, int size, Datatype datatype, int recvshift, int sendshift) {
+void CBaseMPIWrapper::CopyData(const void* sendbuf, void* recvbuf, int size, Datatype datatype, int recvshift,
+                               int sendshift) {
   switch (datatype) {
     case MPI_DOUBLE:
       for (int i = 0; i < size; i++) {
-        static_cast<su2double*>(recvbuf)[i+recvshift] = static_cast<const su2double*>(sendbuf)[i+sendshift];
+        static_cast<su2double*>(recvbuf)[i + recvshift] = static_cast<const su2double*>(sendbuf)[i + sendshift];
       }
       break;
     case MPI_UNSIGNED_LONG:
       for (int i = 0; i < size; i++) {
-        static_cast<unsigned long*>(recvbuf)[i+recvshift] = static_cast<const unsigned long*>(sendbuf)[i+sendshift];
+        static_cast<unsigned long*>(recvbuf)[i + recvshift] = static_cast<const unsigned long*>(sendbuf)[i + sendshift];
       }
       break;
     case MPI_LONG:
       for (int i = 0; i < size; i++) {
-        static_cast<long*>(recvbuf)[i+recvshift] = static_cast<const long*>(sendbuf)[i+sendshift];
+        static_cast<long*>(recvbuf)[i + recvshift] = static_cast<const long*>(sendbuf)[i + sendshift];
       }
       break;
     case MPI_UNSIGNED_SHORT:
       for (int i = 0; i < size; i++) {
-        static_cast<unsigned short*>(recvbuf)[i+recvshift] = static_cast<const unsigned short*>(sendbuf)[i+sendshift];
+        static_cast<unsigned short*>(recvbuf)[i + recvshift] =
+            static_cast<const unsigned short*>(sendbuf)[i + sendshift];
       }
       break;
     case MPI_CHAR:
       for (int i = 0; i < size; i++) {
-        static_cast<char*>(recvbuf)[i+recvshift] = static_cast<const char*>(sendbuf)[i+sendshift];
+        static_cast<char*>(recvbuf)[i + recvshift] = static_cast<const char*>(sendbuf)[i + sendshift];
       }
       break;
     case MPI_SHORT:
       for (int i = 0; i < size; i++) {
-        static_cast<short*>(recvbuf)[i+recvshift] = static_cast<const short*>(sendbuf)[i+sendshift];
+        static_cast<short*>(recvbuf)[i + recvshift] = static_cast<const short*>(sendbuf)[i + sendshift];
       }
       break;
     case MPI_INT:
       for (int i = 0; i < size; i++) {
-        static_cast<int*>(recvbuf)[i+recvshift] = static_cast<const int*>(sendbuf)[i+sendshift];
+        static_cast<int*>(recvbuf)[i + recvshift] = static_cast<const int*>(sendbuf)[i + sendshift];
       }
       break;
     default:
@@ -186,6 +184,6 @@ void CBaseMPIWrapper::CopyData(const void* sendbuf, void* recvbuf, int size, Dat
 #if defined CODI_REVERSE_TYPE || defined CODI_FORWARD_TYPE
 MediTypes* mediTypes;
 #include <medi/medi.cpp>
-#endif // defined CODI_REVERSE_TYPE || defined CODI_FORWARD_TYPE
+#endif  // defined CODI_REVERSE_TYPE || defined CODI_FORWARD_TYPE
 
-#endif // HAVE_MPI
+#endif  // HAVE_MPI
diff --git a/Common/include/parallelization/mpi_structure.hpp b/Common/include/parallelization/mpi_structure.hpp
index a18ac7bb97d..1df7281ccbd 100644
--- a/Common/include/parallelization/mpi_structure.hpp
+++ b/Common/include/parallelization/mpi_structure.hpp
@@ -105,7 +105,8 @@ class CBaseMPIWrapper {
   static Win winMinRankError;
 
  public:
-  static void CopyData(const void* sendbuf, void* recvbuf, int size, Datatype datatype, int recvshift=0, int sendshift=0);
+  static void CopyData(const void* sendbuf, void* recvbuf, int size, Datatype datatype, int recvshift = 0,
+                       int sendshift = 0);
 
   static void Error(std::string ErrorMsg, std::string FunctionName);
 
@@ -174,7 +175,7 @@ class CBaseMPIWrapper {
 
   static inline void Wait(Request* request, Status* status) { MPI_Wait(request, status); }
 
-  static inline int Request_free(Request *request) { return MPI_Request_free(request); }
+  static inline int Request_free(Request* request) { return MPI_Request_free(request); }
 
   static inline void Testall(int count, Request* array_of_requests, int* flag, Status* array_of_statuses) {
     MPI_Testall(count, array_of_requests, flag, array_of_statuses);
@@ -377,7 +378,7 @@ class CMediMPIWrapper : public CBaseMPIWrapper {
 
   static inline void Wait(SU2_MPI::Request* request, Status* status) { AMPI_Wait(request, status); }
 
-  static inline int Request_free(Request *request) { return AMPI_Request_free(request); }
+  static inline int Request_free(Request* request) { return AMPI_Request_free(request); }
 
   static inline void Testall(int count, Request* array_of_requests, int* flag, Status* array_of_statuses) {
     AMPI_Testall(count, array_of_requests, flag, array_of_statuses);
@@ -506,7 +507,8 @@ class CBaseMPIWrapper {
   static Comm currentComm;
 
  public:
-  static void CopyData(const void* sendbuf, void* recvbuf, int size, Datatype datatype, int recvshift=0, int sendshift=0);
+  static void CopyData(const void* sendbuf, void* recvbuf, int size, Datatype datatype, int recvshift = 0,
+                       int sendshift = 0);
 
   static void Error(std::string ErrorMsg, std::string FunctionName);
 
@@ -539,7 +541,7 @@ class CBaseMPIWrapper {
 
   static inline void Wait(Request* request, Status* status) {}
 
-  static inline int Request_free(Request *request) { return 0; }
+  static inline int Request_free(Request* request) { return 0; }
 
   static inline void Waitall(int nrequests, Request* request, Status* status) {}
 
diff --git a/Common/include/parallelization/omp_structure.hpp b/Common/include/parallelization/omp_structure.hpp
index 90470a0c800..de19ec1e544 100644
--- a/Common/include/parallelization/omp_structure.hpp
+++ b/Common/include/parallelization/omp_structure.hpp
@@ -63,7 +63,7 @@
 /*--- The generic start of OpenMP constructs. ---*/
 #define SU2_OMP(ARGS) PRAGMIZE(omp ARGS)
 
-#else // Compile without OpenMP
+#else  // Compile without OpenMP
 #include <ctime>
 
 /*--- Disable pragmas to quiet compilation warnings. ---*/
@@ -72,32 +72,32 @@
 /*!
  * \brief Maximum number of threads available.
  */
-inline constexpr int omp_get_max_threads() {return 1;}
+inline constexpr int omp_get_max_threads() { return 1; }
 
 /*!
  * \brief Number of threads in current team.
  */
-inline constexpr int omp_get_num_threads() {return 1;}
+inline constexpr int omp_get_num_threads() { return 1; }
 
 /*!
  * \brief Set the maximum number of threads.
  */
-inline void omp_set_num_threads(int) { }
+inline void omp_set_num_threads(int) {}
 
 /*!
  * \brief Index of current thread, akin to MPI rank.
  */
-inline constexpr int omp_get_thread_num() {return 0;}
+inline constexpr int omp_get_thread_num() { return 0; }
 
 /*!
  * \brief Returns true if inside a parallel section.
  */
-inline constexpr bool omp_in_parallel() {return false;}
+inline constexpr bool omp_in_parallel() { return false; }
 
 /*!
  * \brief Return the wall time.
  */
-inline passivedouble omp_get_wtime() {return passivedouble(clock()) / CLOCKS_PER_SEC;}
+inline passivedouble omp_get_wtime() { return passivedouble(clock()) / CLOCKS_PER_SEC; }
 
 /*!
  * \brief Dummy lock type and associated functions.
@@ -105,14 +105,14 @@ inline passivedouble omp_get_wtime() {return passivedouble(clock()) / CLOCKS_PER
 struct omp_lock_t {};
 struct DummyVectorOfLocks {
   omp_lock_t l;
-  inline omp_lock_t& operator[](int) {return l;}
+  inline omp_lock_t& operator[](int) { return l; }
 };
-inline void omp_init_lock(omp_lock_t*){}
-inline void omp_set_lock(omp_lock_t*){}
-inline void omp_unset_lock(omp_lock_t*){}
-inline void omp_destroy_lock(omp_lock_t*){}
+inline void omp_init_lock(omp_lock_t*) {}
+inline void omp_set_lock(omp_lock_t*) {}
+inline void omp_unset_lock(omp_lock_t*) {}
+inline void omp_destroy_lock(omp_lock_t*) {}
 
-#endif // end OpenMP detection
+#endif  // end OpenMP detection
 
 /*--- Initialization and finalization ---*/
 
@@ -172,8 +172,8 @@ void omp_finalize();
 #define SU2_OMP_PARALLEL_ON(NTHREADS) OPDI_PARALLEL(num_threads(NTHREADS))
 
 #define SU2_OMP_FOR_(ARGS) OPDI_FOR(ARGS)
-#define SU2_OMP_FOR_DYN(CHUNK) OPDI_FOR(schedule(dynamic,CHUNK))
-#define SU2_OMP_FOR_STAT(CHUNK) OPDI_FOR(schedule(static,CHUNK))
+#define SU2_OMP_FOR_DYN(CHUNK) OPDI_FOR(schedule(dynamic, CHUNK))
+#define SU2_OMP_FOR_STAT(CHUNK) OPDI_FOR(schedule(static, CHUNK))
 
 #define SU2_NOWAIT OPDI_NOWAIT
 
@@ -189,35 +189,28 @@ void omp_finalize();
  */
 
 #define BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS \
-  SU2_OMP_BARRIER \
+  SU2_OMP_BARRIER                        \
   SU2_OMP_MASTER
 
 #define END_SU2_OMP_SAFE_GLOBAL_ACCESS \
-  END_SU2_OMP_MASTER \
+  END_SU2_OMP_MASTER                   \
   SU2_OMP_BARRIER
 
-#define SU2_OMP_SAFE_GLOBAL_ACCESS(...) \
-  BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS \
-  { \
-    __VA_ARGS__ \
-  } \
-  END_SU2_OMP_SAFE_GLOBAL_ACCESS
+#define SU2_OMP_SAFE_GLOBAL_ACCESS(...) BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS{__VA_ARGS__} END_SU2_OMP_SAFE_GLOBAL_ACCESS
 
 /*--- Convenience functions (e.g. to compute chunk sizes). ---*/
 
 /*!
  * \brief Integer division rounding up.
  */
-inline constexpr size_t roundUpDiv(size_t numerator, size_t denominator)
-{
-  return (numerator+denominator-1)/denominator;
+inline constexpr size_t roundUpDiv(size_t numerator, size_t denominator) {
+  return (numerator + denominator - 1) / denominator;
 }
 
 /*!
  * \brief Round up to next multiple.
  */
-inline constexpr size_t nextMultiple(size_t argument, size_t multiple)
-{
+inline constexpr size_t nextMultiple(size_t argument, size_t multiple) {
   return roundUpDiv(argument, multiple) * multiple;
 }
 
@@ -229,11 +222,8 @@ inline constexpr size_t nextMultiple(size_t argument, size_t multiple)
  * \param[in] maxChunkSize - Upper bound for chunk size.
  * \return The chunkSize.
  */
-inline size_t computeStaticChunkSize(size_t totalWork,
-                                     size_t numThreads,
-                                     size_t maxChunkSize)
-{
-  if(!totalWork) return maxChunkSize;
+inline size_t computeStaticChunkSize(size_t totalWork, size_t numThreads, size_t maxChunkSize) {
+  if (!totalWork) return maxChunkSize;
   size_t workPerThread = roundUpDiv(totalWork, numThreads);
   size_t chunksPerThread = roundUpDiv(workPerThread, maxChunkSize);
   return roundUpDiv(workPerThread, chunksPerThread);
@@ -245,11 +235,10 @@ inline size_t computeStaticChunkSize(size_t totalWork,
  * \param[in] src - Source array.
  * \param[in] dst - Destination array.
  */
-template<class T, class U>
-void parallelCopy(size_t size, const T* src, U* dst)
-{
+template <class T, class U>
+void parallelCopy(size_t size, const T* src, U* dst) {
   SU2_OMP_FOR_STAT(2048)
-  for(size_t i=0; i<size; ++i) dst[i] = src[i];
+  for (size_t i = 0; i < size; ++i) dst[i] = src[i];
   END_SU2_OMP_FOR
 }
 
@@ -259,11 +248,10 @@ void parallelCopy(size_t size, const T* src, U* dst)
  * \param[in] val - Value to set.
  * \param[in] dst - Destination array.
  */
-template<class T, class U>
-void parallelSet(size_t size, T val, U* dst)
-{
+template <class T, class U>
+void parallelSet(size_t size, T val, U* dst) {
   SU2_OMP_FOR_STAT(2048)
-  for(size_t i=0; i<size; ++i) dst[i] = val;
+  for (size_t i = 0; i < size; ++i) dst[i] = val;
   END_SU2_OMP_FOR
 }
 
@@ -273,16 +261,14 @@ void parallelSet(size_t size, T val, U* dst)
  * \param[in] rhs - Local variable being added to the shared one.
  * \param[in,out] lhs - Shared variable being updated.
  */
-template<class T, su2enable_if<!std::is_arithmetic<T>::value> = 0>
-inline void atomicAdd(T rhs, T& lhs)
-{
+template <class T, su2enable_if<!std::is_arithmetic<T>::value> = 0>
+inline void atomicAdd(T rhs, T& lhs) {
   SU2_OMP_CRITICAL
   lhs += rhs;
   END_SU2_OMP_CRITICAL
 }
-template<class T, su2enable_if<std::is_arithmetic<T>::value> = 0>
-inline void atomicAdd(T rhs, T& lhs)
-{
+template <class T, su2enable_if<std::is_arithmetic<T>::value> = 0>
+inline void atomicAdd(T rhs, T& lhs) {
   SU2_OMP_ATOMIC
   lhs += rhs;
 }
diff --git a/Common/include/parallelization/special_vectorization.hpp b/Common/include/parallelization/special_vectorization.hpp
index 5ab1830dd9e..1c980fd7229 100644
--- a/Common/include/parallelization/special_vectorization.hpp
+++ b/Common/include/parallelization/special_vectorization.hpp
@@ -42,16 +42,19 @@
  * overload resolution will do the rest. The first four symbols are
  * undefined once we are done using them.
  */
-template<>
+template <>
 class ARRAY_T {
-#define FOREACH SU2_OMP_SIMD for(size_t k=0; k<Size; ++k)
-  template<class F, class S>
-  FORCEINLINE static S second(F, S s) { return s; }
-public:
+#define FOREACH SU2_OMP_SIMD for (size_t k = 0; k < Size; ++k)
+  template <class F, class S>
+  FORCEINLINE static S second(F, S s) {
+    return s;
+  }
+
+ public:
   using Scalar = SCALAR_T;
   using Register = REGISTER_T;
-  enum : size_t {Align = alignof(Register)};
-  enum : size_t {Size = sizeof(Register) / sizeof(Scalar)};
+  enum : size_t { Align = alignof(Register) };
+  enum : size_t { Size = sizeof(Register) / sizeof(Scalar) };
 
   /*--- The infamous union "hack", sue me. ---*/
   union {
@@ -76,14 +79,22 @@ class ARRAY_T {
   FORCEINLINE void store(Scalar* ptr) const { storeu_p(ptr, reg); }
   FORCEINLINE void storea(Scalar* ptr) const { store_p(ptr, reg); }
   FORCEINLINE void stream(Scalar* ptr) const { stream_p(ptr, reg); }
-  template<class T>
-  FORCEINLINE void gather(const Scalar* begin, const T& offsets) { FOREACH x_[k] = begin[offsets[k]]; }
+  template <class T>
+  FORCEINLINE void gather(const Scalar* begin, const T& offsets) {
+    FOREACH x_[k] = begin[offsets[k]];
+  }
 
   /*--- Compound assignement operators. ---*/
 
-#define MAKE_COMPOUND(OP,IMPL)\
-  FORCEINLINE Array& operator OP (Scalar x) { reg = IMPL(reg, set1_p(SIZE_TAG, x)); return *this; }\
-  FORCEINLINE Array& operator OP (const Array& other) noexcept { reg = IMPL(reg, other.reg); return *this; }
+#define MAKE_COMPOUND(OP, IMPL)                                 \
+  FORCEINLINE Array& operator OP(Scalar x) {                    \
+    reg = IMPL(reg, set1_p(SIZE_TAG, x));                       \
+    return *this;                                               \
+  }                                                             \
+  FORCEINLINE Array& operator OP(const Array& other) noexcept { \
+    reg = IMPL(reg, other.reg);                                 \
+    return *this;                                               \
+  }
   MAKE_COMPOUND(=, second)
   MAKE_COMPOUND(+=, add_p)
   MAKE_COMPOUND(-=, sub_p)
@@ -98,8 +109,8 @@ class ARRAY_T {
  * SIMD overloads, NAME is the operator or function,
  * IMPL the intrinsic function that implements it.
  */
-#define MAKE_UNARY_FUN(NAME,IMPL)\
-FORCEINLINE ARRAY_T NAME(const ARRAY_T& x) {return IMPL(x.reg);}
+#define MAKE_UNARY_FUN(NAME, IMPL) \
+  FORCEINLINE ARRAY_T NAME(const ARRAY_T& x) { return IMPL(x.reg); }
 
 MAKE_UNARY_FUN(operator-, neg_p)
 MAKE_UNARY_FUN(sqrt, sqrt_p)
@@ -108,16 +119,10 @@ MAKE_UNARY_FUN(sign, sign_p)
 
 #undef MAKE_UNARY_FUN
 
-#define MAKE_BINARY_FUN(NAME,IMPL)                              \
-FORCEINLINE ARRAY_T NAME (const ARRAY_T& a, const ARRAY_T& b) { \
-  return IMPL(a.reg, b.reg);                                    \
-}                                                               \
-FORCEINLINE ARRAY_T NAME (const ARRAY_T& a, SCALAR_T b) {       \
-  return IMPL(a.reg, set1_p(SIZE_TAG, b));                      \
-}                                                               \
-FORCEINLINE ARRAY_T NAME (SCALAR_T b, const ARRAY_T& a) {       \
-  return IMPL(set1_p(SIZE_TAG, b), a.reg);                      \
-}
+#define MAKE_BINARY_FUN(NAME, IMPL)                                                                   \
+  FORCEINLINE ARRAY_T NAME(const ARRAY_T& a, const ARRAY_T& b) { return IMPL(a.reg, b.reg); }         \
+  FORCEINLINE ARRAY_T NAME(const ARRAY_T& a, SCALAR_T b) { return IMPL(a.reg, set1_p(SIZE_TAG, b)); } \
+  FORCEINLINE ARRAY_T NAME(SCALAR_T b, const ARRAY_T& a) { return IMPL(set1_p(SIZE_TAG, b), a.reg); }
 
 MAKE_BINARY_FUN(operator+, add_p)
 MAKE_BINARY_FUN(operator-, sub_p)
@@ -137,29 +142,37 @@ MAKE_BINARY_FUN(fmin, min_p)
 /*!
  * Compatibility mode overloads, element-wise implementation.
  */
-#define FOREACH SU2_OMP_SIMD for(size_t k=0; k<ARRAY_T::Size; ++k)
+#define FOREACH SU2_OMP_SIMD for (size_t k = 0; k < ARRAY_T::Size; ++k)
 
 /*--- Functions of one (array) argument. ---*/
 
-#define MAKE_UNARY_FUN(NAME,IMPL)                             \
-FORCEINLINE ARRAY_T NAME(const ARRAY_T& x) {                  \
-  ARRAY_T res; FOREACH { res[k] = IMPL(x[k]); } return res;   \
-}
+#define MAKE_UNARY_FUN(NAME, IMPL)             \
+  FORCEINLINE ARRAY_T NAME(const ARRAY_T& x) { \
+    ARRAY_T res;                               \
+    FOREACH { res[k] = IMPL(x[k]); }           \
+    return res;                                \
+  }
 
 #undef MAKE_UNARY_FUN
 
 /*--- Functions of two arguments, with arrays and scalars. ---*/
 
-#define MAKE_BINARY_FUN(NAME,IMPL)                                    \
-FORCEINLINE ARRAY_T NAME(const ARRAY_T& a, const ARRAY_T& b) {        \
-  ARRAY_T res; FOREACH { res[k] = IMPL(a[k], b[k]); } return res;     \
-}                                                                     \
-FORCEINLINE ARRAY_T NAME(const ARRAY_T& a, SCALAR_T b) {              \
-  ARRAY_T res; FOREACH { res[k] = IMPL(a[k], b); } return res;        \
-}                                                                     \
-FORCEINLINE ARRAY_T NAME(SCALAR_T b, const ARRAY_T& a) {              \
-  ARRAY_T res; FOREACH { res[k] = IMPL(b, a[k]); } return res;        \
-}
+#define MAKE_BINARY_FUN(NAME, IMPL)                              \
+  FORCEINLINE ARRAY_T NAME(const ARRAY_T& a, const ARRAY_T& b) { \
+    ARRAY_T res;                                                 \
+    FOREACH { res[k] = IMPL(a[k], b[k]); }                       \
+    return res;                                                  \
+  }                                                              \
+  FORCEINLINE ARRAY_T NAME(const ARRAY_T& a, SCALAR_T b) {       \
+    ARRAY_T res;                                                 \
+    FOREACH { res[k] = IMPL(a[k], b); }                          \
+    return res;                                                  \
+  }                                                              \
+  FORCEINLINE ARRAY_T NAME(SCALAR_T b, const ARRAY_T& a) {       \
+    ARRAY_T res;                                                 \
+    FOREACH { res[k] = IMPL(b, a[k]); }                          \
+    return res;                                                  \
+  }
 
 MAKE_BINARY_FUN(pow, ::pow)
 
@@ -172,4 +185,4 @@ MAKE_BINARY_FUN(pow, ::pow)
 #undef REGISTER_T
 #undef SIZE_TAG
 
-/// @}
\ No newline at end of file
+/// @}
diff --git a/Common/include/parallelization/vectorization.hpp b/Common/include/parallelization/vectorization.hpp
index 2b7caaad775..eaabce00d41 100644
--- a/Common/include/parallelization/vectorization.hpp
+++ b/Common/include/parallelization/vectorization.hpp
@@ -56,10 +56,12 @@ constexpr size_t PREFERRED_SIZE = 8;
 /*!
  * \brief Convert the SIMD size (bytes) to a lenght (num elems).
  */
-template<class T>
-constexpr size_t preferredLen() { return PREFERRED_SIZE / sizeof(T); }
+template <class T>
+constexpr size_t preferredLen() {
+  return PREFERRED_SIZE / sizeof(T);
+}
 
-template<>
+template <>
 constexpr size_t preferredLen<su2double>() {
 #ifdef CODI_REVERSE_TYPE
   /*--- Use a SIMD size of 1 for reverse AD, larger sizes increase
@@ -80,54 +82,72 @@ constexpr size_t preferredLen<su2double>() {
  * specializations do not use expression templates, IF YOU NEED A NEW FUNCTION,
  * define it both in vector_expressions.hpp and in special_vectorization.hpp.
  */
-template<class Scalar_t, size_t N = preferredLen<Scalar_t>()>
-class Array : public CVecExpr<Array<Scalar_t,N>, Scalar_t> {
-#define FOREACH for(size_t k=0; k<N; ++k)
+template <class Scalar_t, size_t N = preferredLen<Scalar_t>()>
+class Array : public CVecExpr<Array<Scalar_t, N>, Scalar_t> {
+#define FOREACH for (size_t k = 0; k < N; ++k)
   static_assert(N > 0, "Invalid SIMD size");
-public:
+
+ public:
   using Scalar = Scalar_t;
-  enum : size_t {Size = N};
-  enum : size_t {Align = Size*sizeof(Scalar)};
+  enum : size_t { Size = N };
+  enum : size_t { Align = Size * sizeof(Scalar) };
   static constexpr bool StoreAsRef = true;
 
-private:
-  alignas(Size*sizeof(Scalar)) Scalar x_[N];
-
-public:
-#define ARRAY_BOILERPLATE                                                         \
-  /*!--- Access elements ---*/                                                    \
-  FORCEINLINE Scalar& operator[] (size_t k) { return x_[k]; }                     \
-  FORCEINLINE const Scalar& operator[] (size_t k) const { return x_[k]; }         \
-  /*!--- Constructors ---*/                                                       \
-  FORCEINLINE Array() = default;                                                  \
-  FORCEINLINE Array(Scalar x) { bcast(x); }                                       \
-  FORCEINLINE Array(std::initializer_list<Scalar> vals) {                         \
-    auto it = vals.begin(); FOREACH { x_[k] = *it; ++it; }                        \
-  }                                                                               \
-  FORCEINLINE Array(Scalar x0, Scalar dx) { FOREACH x_[k] = x0 + k*dx; }          \
-  FORCEINLINE Array(const Scalar* ptr) { load(ptr); }                             \
-  template<class T>                                                               \
-  FORCEINLINE Array(const Scalar* beg, const T& off) { gather(beg,off); }         \
-  /*!--- Reduction operations ---*/                                               \
-  FORCEINLINE Scalar sum() const { Scalar s(0); FOREACH { s+=x_[k]; } return s; } \
-  FORCEINLINE Scalar dot(const Array& other) const {                              \
-    Scalar s(0); FOREACH { s += x_[k] * other[k]; } return s;                     \
+ private:
+  alignas(Size * sizeof(Scalar)) Scalar x_[N];
+
+ public:
+#define ARRAY_BOILERPLATE                                                  \
+  /*!--- Access elements ---*/                                             \
+  FORCEINLINE Scalar& operator[](size_t k) { return x_[k]; }               \
+  FORCEINLINE const Scalar& operator[](size_t k) const { return x_[k]; }   \
+  /*!--- Constructors ---*/                                                \
+  FORCEINLINE Array() = default;                                           \
+  FORCEINLINE Array(Scalar x) { bcast(x); }                                \
+  FORCEINLINE Array(std::initializer_list<Scalar> vals) {                  \
+    auto it = vals.begin();                                                \
+    FOREACH {                                                              \
+      x_[k] = *it;                                                         \
+      ++it;                                                                \
+    }                                                                      \
+  }                                                                        \
+  FORCEINLINE Array(Scalar x0, Scalar dx) { FOREACH x_[k] = x0 + k * dx; } \
+  FORCEINLINE Array(const Scalar* ptr) { load(ptr); }                      \
+  template <class T>                                                       \
+  FORCEINLINE Array(const Scalar* beg, const T& off) {                     \
+    gather(beg, off);                                                      \
+  }                                                                        \
+  /*!--- Reduction operations ---*/                                        \
+  FORCEINLINE Scalar sum() const {                                         \
+    Scalar s(0);                                                           \
+    FOREACH { s += x_[k]; }                                                \
+    return s;                                                              \
+  }                                                                        \
+  FORCEINLINE Scalar dot(const Array& other) const {                       \
+    Scalar s(0);                                                           \
+    FOREACH { s += x_[k] * other[k]; }                                     \
+    return s;                                                              \
   }
 
 #if defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)
   /*--- These are not very nice but without them it would not be
    * possible to assign literals to Arrays of active types. ---*/
-  template<class U = Scalar, su2enable_if<std::is_same<U,su2double>::value> = 0>
-  FORCEINLINE Array(passivedouble x) { bcast(x); }
-  template<class U = Scalar, su2enable_if<std::is_same<U,su2double>::value> = 0>
-  FORCEINLINE Array& operator= (passivedouble x) { bcast(x); return *this; }
+  template <class U = Scalar, su2enable_if<std::is_same<U, su2double>::value> = 0>
+  FORCEINLINE Array(passivedouble x) {
+    bcast(x);
+  }
+  template <class U = Scalar, su2enable_if<std::is_same<U, su2double>::value> = 0>
+  FORCEINLINE Array& operator=(passivedouble x) {
+    bcast(x);
+    return *this;
+  }
 #endif
 
   ARRAY_BOILERPLATE
 
   /*! \brief Copy construct from expression. */
-  template<class U>
-  FORCEINLINE Array(const CVecExpr<U,Scalar>& expr) {
+  template <class U>
+  FORCEINLINE Array(const CVecExpr<U, Scalar>& expr) {
     FOREACH x_[k] = expr.derived()[k];
   }
 
@@ -139,16 +159,22 @@ class Array : public CVecExpr<Array<Scalar_t,N>, Scalar_t> {
   FORCEINLINE void store(Scalar* ptr) const { FOREACH ptr[k] = x_[k]; }
   FORCEINLINE void storea(Scalar* ptr) const { store(ptr); }
   FORCEINLINE void stream(Scalar* ptr) const { store(ptr); }
-  template<class T>
-  FORCEINLINE void gather(const Scalar* begin, const T& offsets) { FOREACH x_[k] = begin[offsets[k]]; }
+  template <class T>
+  FORCEINLINE void gather(const Scalar* begin, const T& offsets) {
+    FOREACH x_[k] = begin[offsets[k]];
+  }
 
   /*--- Compound assignment operators. ---*/
 
-#define MAKE_COMPOUND(OP)                                                             \
-  FORCEINLINE Array& operator OP (Scalar x) { FOREACH { x_[k] OP x; } return *this; } \
-  template<class U>                                                                   \
-  FORCEINLINE Array& operator OP (const CVecExpr<U,Scalar>& expr) {                   \
-    FOREACH { x_[k] OP expr.derived()[k]; } return *this;                             \
+#define MAKE_COMPOUND(OP)                                           \
+  FORCEINLINE Array& operator OP(Scalar x) {                        \
+    FOREACH { x_[k] OP x; }                                         \
+    return *this;                                                   \
+  }                                                                 \
+  template <class U>                                                \
+  FORCEINLINE Array& operator OP(const CVecExpr<U, Scalar>& expr) { \
+    FOREACH { x_[k] OP expr.derived()[k]; }                         \
+    return *this;                                                   \
   }
   MAKE_COMPOUND(=)
   MAKE_COMPOUND(+=)
@@ -166,11 +192,11 @@ class Array : public CVecExpr<Array<Scalar_t,N>, Scalar_t> {
 
 /*--- Size tags for overload resolution of some wrapper functions. ---*/
 namespace SizeTag {
-  struct TWO {};
-  struct FOUR {};
-  struct EIGHT {};
-  struct SIXTEEN {};
-}
+struct TWO {};
+struct FOUR {};
+struct EIGHT {};
+struct SIXTEEN {};
+}  // namespace SizeTag
 
 /*--- Constants for bitwise implementations. ---*/
 /*--- abs forces the sign bit to 0 ("x" & 0b0111...). ---*/
@@ -182,7 +208,7 @@ constexpr auto sign_mask_d = 0x8000000000000000L;
 /*!
  * Create specialization for array of 2 doubles (this should be always available).
  */
-#define ARRAY_T Array<double,2>
+#define ARRAY_T Array<double, 2>
 #define SCALAR_T double
 #define REGISTER_T __m128d
 #define SIZE_TAG SizeTag::TWO()
@@ -194,23 +220,23 @@ static const __m128d ones_2d = _mm_set1_pd(1);
 FORCEINLINE __m128d set1_p(SizeTag::TWO, double p) { return _mm_set1_pd(p); }
 FORCEINLINE __m128d load_p(SizeTag::TWO, const double* p) { return _mm_load_pd(p); }
 FORCEINLINE __m128d loadu_p(SizeTag::TWO, const double* p) { return _mm_loadu_pd(p); }
-FORCEINLINE void store_p(double* p, __m128d x) { _mm_store_pd(p,x); }
-FORCEINLINE void storeu_p(double* p, __m128d x) { _mm_storeu_pd(p,x); }
-FORCEINLINE void stream_p(double* p, __m128d x) { _mm_stream_pd(p,x); }
-
-FORCEINLINE __m128d add_p(__m128d a, __m128d b) { return _mm_add_pd(a,b); }
-FORCEINLINE __m128d sub_p(__m128d a, __m128d b) { return _mm_sub_pd(a,b); }
-FORCEINLINE __m128d mul_p(__m128d a, __m128d b) { return _mm_mul_pd(a,b); }
-FORCEINLINE __m128d div_p(__m128d a, __m128d b) { return _mm_div_pd(a,b); }
-FORCEINLINE __m128d max_p(__m128d a, __m128d b) { return _mm_max_pd(a,b); }
-FORCEINLINE __m128d min_p(__m128d a, __m128d b) { return _mm_min_pd(a,b); }
-
-FORCEINLINE __m128d eq_p(__m128d a, __m128d b) { return _mm_and_pd(ones_2d, _mm_cmpeq_pd(a,b)); }
-FORCEINLINE __m128d lt_p(__m128d a, __m128d b) { return _mm_and_pd(ones_2d, _mm_cmplt_pd(a,b)); }
-FORCEINLINE __m128d le_p(__m128d a, __m128d b) { return _mm_and_pd(ones_2d, _mm_cmple_pd(a,b)); }
-FORCEINLINE __m128d ne_p(__m128d a, __m128d b) { return _mm_and_pd(ones_2d, _mm_cmpneq_pd(a,b)); }
-FORCEINLINE __m128d ge_p(__m128d a, __m128d b) { return _mm_and_pd(ones_2d, _mm_cmpge_pd(a,b)); }
-FORCEINLINE __m128d gt_p(__m128d a, __m128d b) { return _mm_and_pd(ones_2d, _mm_cmpgt_pd(a,b)); }
+FORCEINLINE void store_p(double* p, __m128d x) { _mm_store_pd(p, x); }
+FORCEINLINE void storeu_p(double* p, __m128d x) { _mm_storeu_pd(p, x); }
+FORCEINLINE void stream_p(double* p, __m128d x) { _mm_stream_pd(p, x); }
+
+FORCEINLINE __m128d add_p(__m128d a, __m128d b) { return _mm_add_pd(a, b); }
+FORCEINLINE __m128d sub_p(__m128d a, __m128d b) { return _mm_sub_pd(a, b); }
+FORCEINLINE __m128d mul_p(__m128d a, __m128d b) { return _mm_mul_pd(a, b); }
+FORCEINLINE __m128d div_p(__m128d a, __m128d b) { return _mm_div_pd(a, b); }
+FORCEINLINE __m128d max_p(__m128d a, __m128d b) { return _mm_max_pd(a, b); }
+FORCEINLINE __m128d min_p(__m128d a, __m128d b) { return _mm_min_pd(a, b); }
+
+FORCEINLINE __m128d eq_p(__m128d a, __m128d b) { return _mm_and_pd(ones_2d, _mm_cmpeq_pd(a, b)); }
+FORCEINLINE __m128d lt_p(__m128d a, __m128d b) { return _mm_and_pd(ones_2d, _mm_cmplt_pd(a, b)); }
+FORCEINLINE __m128d le_p(__m128d a, __m128d b) { return _mm_and_pd(ones_2d, _mm_cmple_pd(a, b)); }
+FORCEINLINE __m128d ne_p(__m128d a, __m128d b) { return _mm_and_pd(ones_2d, _mm_cmpneq_pd(a, b)); }
+FORCEINLINE __m128d ge_p(__m128d a, __m128d b) { return _mm_and_pd(ones_2d, _mm_cmpge_pd(a, b)); }
+FORCEINLINE __m128d gt_p(__m128d a, __m128d b) { return _mm_and_pd(ones_2d, _mm_cmpgt_pd(a, b)); }
 
 FORCEINLINE __m128d sqrt_p(__m128d x) { return _mm_sqrt_pd(x); }
 FORCEINLINE __m128d abs_p(__m128d x) { return _mm_and_pd(x, abs_mask_2d); }
@@ -222,13 +248,13 @@ FORCEINLINE __m128d sign_p(__m128d x) { return _mm_or_pd(ones_2d, _mm_and_pd(x,
 
 #include "special_vectorization.hpp"
 
-#endif // __SSE2__
+#endif  // __SSE2__
 
 #ifdef __AVX__
 /*!
  * Create specialization for array of 4 doubles.
  */
-#define ARRAY_T Array<double,4>
+#define ARRAY_T Array<double, 4>
 #define SCALAR_T double
 #define REGISTER_T __m256d
 #define SIZE_TAG SizeTag::FOUR()
@@ -240,23 +266,23 @@ static const __m256d ones_4d = _mm256_set1_pd(1);
 FORCEINLINE __m256d set1_p(SizeTag::FOUR, double p) { return _mm256_set1_pd(p); }
 FORCEINLINE __m256d load_p(SizeTag::FOUR, const double* p) { return _mm256_load_pd(p); }
 FORCEINLINE __m256d loadu_p(SizeTag::FOUR, const double* p) { return _mm256_loadu_pd(p); }
-FORCEINLINE void store_p(double* p, __m256d x) { _mm256_store_pd(p,x); }
-FORCEINLINE void storeu_p(double* p, __m256d x) { _mm256_storeu_pd(p,x); }
-FORCEINLINE void stream_p(double* p, __m256d x) { _mm256_stream_pd(p,x); }
-
-FORCEINLINE __m256d add_p(__m256d a, __m256d b) { return _mm256_add_pd(a,b); }
-FORCEINLINE __m256d sub_p(__m256d a, __m256d b) { return _mm256_sub_pd(a,b); }
-FORCEINLINE __m256d mul_p(__m256d a, __m256d b) { return _mm256_mul_pd(a,b); }
-FORCEINLINE __m256d div_p(__m256d a, __m256d b) { return _mm256_div_pd(a,b); }
-FORCEINLINE __m256d max_p(__m256d a, __m256d b) { return _mm256_max_pd(a,b); }
-FORCEINLINE __m256d min_p(__m256d a, __m256d b) { return _mm256_min_pd(a,b); }
-
-FORCEINLINE __m256d eq_p(__m256d a, __m256d b) { return _mm256_and_pd(ones_4d, _mm256_cmp_pd(a,b,0)); }
-FORCEINLINE __m256d lt_p(__m256d a, __m256d b) { return _mm256_and_pd(ones_4d, _mm256_cmp_pd(a,b,1)); }
-FORCEINLINE __m256d le_p(__m256d a, __m256d b) { return _mm256_and_pd(ones_4d, _mm256_cmp_pd(a,b,2)); }
-FORCEINLINE __m256d ne_p(__m256d a, __m256d b) { return _mm256_and_pd(ones_4d, _mm256_cmp_pd(a,b,4)); }
-FORCEINLINE __m256d ge_p(__m256d a, __m256d b) { return _mm256_and_pd(ones_4d, _mm256_cmp_pd(a,b,13)); }
-FORCEINLINE __m256d gt_p(__m256d a, __m256d b) { return _mm256_and_pd(ones_4d, _mm256_cmp_pd(a,b,14)); }
+FORCEINLINE void store_p(double* p, __m256d x) { _mm256_store_pd(p, x); }
+FORCEINLINE void storeu_p(double* p, __m256d x) { _mm256_storeu_pd(p, x); }
+FORCEINLINE void stream_p(double* p, __m256d x) { _mm256_stream_pd(p, x); }
+
+FORCEINLINE __m256d add_p(__m256d a, __m256d b) { return _mm256_add_pd(a, b); }
+FORCEINLINE __m256d sub_p(__m256d a, __m256d b) { return _mm256_sub_pd(a, b); }
+FORCEINLINE __m256d mul_p(__m256d a, __m256d b) { return _mm256_mul_pd(a, b); }
+FORCEINLINE __m256d div_p(__m256d a, __m256d b) { return _mm256_div_pd(a, b); }
+FORCEINLINE __m256d max_p(__m256d a, __m256d b) { return _mm256_max_pd(a, b); }
+FORCEINLINE __m256d min_p(__m256d a, __m256d b) { return _mm256_min_pd(a, b); }
+
+FORCEINLINE __m256d eq_p(__m256d a, __m256d b) { return _mm256_and_pd(ones_4d, _mm256_cmp_pd(a, b, 0)); }
+FORCEINLINE __m256d lt_p(__m256d a, __m256d b) { return _mm256_and_pd(ones_4d, _mm256_cmp_pd(a, b, 1)); }
+FORCEINLINE __m256d le_p(__m256d a, __m256d b) { return _mm256_and_pd(ones_4d, _mm256_cmp_pd(a, b, 2)); }
+FORCEINLINE __m256d ne_p(__m256d a, __m256d b) { return _mm256_and_pd(ones_4d, _mm256_cmp_pd(a, b, 4)); }
+FORCEINLINE __m256d ge_p(__m256d a, __m256d b) { return _mm256_and_pd(ones_4d, _mm256_cmp_pd(a, b, 13)); }
+FORCEINLINE __m256d gt_p(__m256d a, __m256d b) { return _mm256_and_pd(ones_4d, _mm256_cmp_pd(a, b, 14)); }
 
 FORCEINLINE __m256d sqrt_p(__m256d x) { return _mm256_sqrt_pd(x); }
 FORCEINLINE __m256d abs_p(__m256d x) { return _mm256_and_pd(x, abs_mask_4d); }
@@ -265,13 +291,13 @@ FORCEINLINE __m256d sign_p(__m256d x) { return _mm256_or_pd(ones_4d, _mm256_and_
 
 #include "special_vectorization.hpp"
 
-#endif // __AVX__
+#endif  // __AVX__
 
 #ifdef __AVX512F__
 /*!
  * Create specialization for array of 8 doubles.
  */
-#define ARRAY_T Array<double,8>
+#define ARRAY_T Array<double, 8>
 #define SCALAR_T double
 #define REGISTER_T __m512d
 #define SIZE_TAG SizeTag::EIGHT()
@@ -283,27 +309,27 @@ static const __m512d ones_8d = _mm512_set1_pd(1);
 FORCEINLINE __m512d set1_p(SizeTag::EIGHT, double p) { return _mm512_set1_pd(p); }
 FORCEINLINE __m512d load_p(SizeTag::EIGHT, const double* p) { return _mm512_load_pd(p); }
 FORCEINLINE __m512d loadu_p(SizeTag::EIGHT, const double* p) { return _mm512_loadu_pd(p); }
-FORCEINLINE void store_p(double* p, __m512d x) { _mm512_store_pd(p,x); }
-FORCEINLINE void storeu_p(double* p, __m512d x) { _mm512_storeu_pd(p,x); }
-FORCEINLINE void stream_p(double* p, __m512d x) { _mm512_stream_pd(p,x); }
-
-FORCEINLINE __m512d add_p(__m512d a, __m512d b) { return _mm512_add_pd(a,b); }
-FORCEINLINE __m512d sub_p(__m512d a, __m512d b) { return _mm512_sub_pd(a,b); }
-FORCEINLINE __m512d mul_p(__m512d a, __m512d b) { return _mm512_mul_pd(a,b); }
-FORCEINLINE __m512d div_p(__m512d a, __m512d b) { return _mm512_div_pd(a,b); }
-FORCEINLINE __m512d max_p(__m512d a, __m512d b) { return _mm512_max_pd(a,b); }
-FORCEINLINE __m512d min_p(__m512d a, __m512d b) { return _mm512_min_pd(a,b); }
-
-template<int opCode>
+FORCEINLINE void store_p(double* p, __m512d x) { _mm512_store_pd(p, x); }
+FORCEINLINE void storeu_p(double* p, __m512d x) { _mm512_storeu_pd(p, x); }
+FORCEINLINE void stream_p(double* p, __m512d x) { _mm512_stream_pd(p, x); }
+
+FORCEINLINE __m512d add_p(__m512d a, __m512d b) { return _mm512_add_pd(a, b); }
+FORCEINLINE __m512d sub_p(__m512d a, __m512d b) { return _mm512_sub_pd(a, b); }
+FORCEINLINE __m512d mul_p(__m512d a, __m512d b) { return _mm512_mul_pd(a, b); }
+FORCEINLINE __m512d div_p(__m512d a, __m512d b) { return _mm512_div_pd(a, b); }
+FORCEINLINE __m512d max_p(__m512d a, __m512d b) { return _mm512_max_pd(a, b); }
+FORCEINLINE __m512d min_p(__m512d a, __m512d b) { return _mm512_min_pd(a, b); }
+
+template <int opCode>
 FORCEINLINE __m512d cmp_p(__m512d a, __m512d b) {
-  return _mm512_mask_blend_pd(_mm512_cmp_pd_mask(a,b,opCode), _mm512_setzero_pd(), ones_8d);
+  return _mm512_mask_blend_pd(_mm512_cmp_pd_mask(a, b, opCode), _mm512_setzero_pd(), ones_8d);
 }
-FORCEINLINE __m512d eq_p(__m512d a, __m512d b) { return cmp_p<0>(a,b); }
-FORCEINLINE __m512d lt_p(__m512d a, __m512d b) { return cmp_p<1>(a,b); }
-FORCEINLINE __m512d le_p(__m512d a, __m512d b) { return cmp_p<2>(a,b); }
-FORCEINLINE __m512d ne_p(__m512d a, __m512d b) { return cmp_p<4>(a,b); }
-FORCEINLINE __m512d ge_p(__m512d a, __m512d b) { return cmp_p<13>(a,b); }
-FORCEINLINE __m512d gt_p(__m512d a, __m512d b) { return cmp_p<14>(a,b); }
+FORCEINLINE __m512d eq_p(__m512d a, __m512d b) { return cmp_p<0>(a, b); }
+FORCEINLINE __m512d lt_p(__m512d a, __m512d b) { return cmp_p<1>(a, b); }
+FORCEINLINE __m512d le_p(__m512d a, __m512d b) { return cmp_p<2>(a, b); }
+FORCEINLINE __m512d ne_p(__m512d a, __m512d b) { return cmp_p<4>(a, b); }
+FORCEINLINE __m512d ge_p(__m512d a, __m512d b) { return cmp_p<13>(a, b); }
+FORCEINLINE __m512d gt_p(__m512d a, __m512d b) { return cmp_p<14>(a, b); }
 
 FORCEINLINE __m512d sqrt_p(__m512d x) { return _mm512_sqrt_pd(x); }
 FORCEINLINE __m512d abs_p(__m512d x) { return _mm512_and_pd(x, abs_mask_8d); }
@@ -312,9 +338,9 @@ FORCEINLINE __m512d sign_p(__m512d x) { return _mm512_or_pd(ones_8d, _mm512_and_
 
 #include "special_vectorization.hpp"
 
-#endif // __AVX512F__
+#endif  // __AVX512F__
 
 #undef ARRAY_BOILERPLATE
 
 /// @}
-} // namespace
+}  // namespace simd
diff --git a/Common/include/toolboxes/C1DInterpolation.hpp b/Common/include/toolboxes/C1DInterpolation.hpp
index 2b627f68cb2..aa00b3f2999 100644
--- a/Common/include/toolboxes/C1DInterpolation.hpp
+++ b/Common/include/toolboxes/C1DInterpolation.hpp
@@ -37,8 +37,8 @@
  * \ingroup LookUpInterp
  */
 class C1DInterpolation {
-protected:
-  std::vector<su2double> x, y;  /*!< \brief Data points. */
+ protected:
+  std::vector<su2double> x, y; /*!< \brief Data points. */
 
   /*!
    * \brief Find containing interval.
@@ -46,20 +46,19 @@ class C1DInterpolation {
    * \return The start index of the interval, or the size if the coordinate is out of bounds.
    */
   inline size_t lower_bound(su2double xi) const {
-
     if (xi <= x.front() || xi >= x.back()) return x.size();
 
-    size_t lb = 0, ub = x.size()-1;
+    size_t lb = 0, ub = x.size() - 1;
 
-    while (ub-lb > 1) {
-      size_t mid = (lb+ub)/2;
-      auto& change = (xi < x[mid])? ub : lb;
+    while (ub - lb > 1) {
+      size_t mid = (lb + ub) / 2;
+      auto& change = (xi < x[mid]) ? ub : lb;
       change = mid;
     }
     return lb;
   }
 
-public:
+ public:
   /*!
    * \brief Virtual destructor of the C1DInterpolation class.
    */
@@ -70,7 +69,7 @@ class C1DInterpolation {
    * \param[in] X - the x values.
    * \param[in] Data - the f(x) values.
    */
-  virtual void SetSpline(const std::vector<su2double> &X, const std::vector<su2double> &Data) {
+  virtual void SetSpline(const std::vector<su2double>& X, const std::vector<su2double>& Data) {
     assert(X.size() == Data.size());
     x = X;
     y = Data;
@@ -80,19 +79,18 @@ class C1DInterpolation {
    * \brief Evaluate the value of the spline at a point.
    */
   virtual su2double EvaluateSpline(su2double Point_Interp) const = 0;
-  inline su2double operator() (su2double Point_Interp) const { return EvaluateSpline(Point_Interp); }
-
+  inline su2double operator()(su2double Point_Interp) const { return EvaluateSpline(Point_Interp); }
 };
 
 /*!
  * \brief Akima 1D interpolation.
  * \ingroup LookUpInterp
  */
-class CAkimaInterpolation: public C1DInterpolation{
-protected:
-  std::vector<su2double> b,c,d;  /*!< \brief local variables for Akima spline cooefficients */
+class CAkimaInterpolation : public C1DInterpolation {
+ protected:
+  std::vector<su2double> b, c, d; /*!< \brief local variables for Akima spline cooefficients */
 
-public:
+ public:
   CAkimaInterpolation() = default;
 
   /*!
@@ -100,14 +98,14 @@ class CAkimaInterpolation: public C1DInterpolation{
    * \param[in] X - the x values (sorted low to high).
    * \param[in] Data - the f(x) values.
    */
-  CAkimaInterpolation(const std::vector<su2double> &X, const std::vector<su2double> &Data) {
-    CAkimaInterpolation::SetSpline(X,Data);
+  CAkimaInterpolation(const std::vector<su2double>& X, const std::vector<su2double>& Data) {
+    CAkimaInterpolation::SetSpline(X, Data);
   }
 
   /*!
    * \brief Build the spline.
    */
-  void SetSpline(const std::vector<su2double> &X, const std::vector<su2double> &Data) override;
+  void SetSpline(const std::vector<su2double>& X, const std::vector<su2double>& Data) override;
 
   /*!
    * \brief Evaluate the value of the spline at a point.
@@ -119,15 +117,15 @@ class CAkimaInterpolation: public C1DInterpolation{
  * \brief Cubic spline interpolation.
  * \ingroup LookUpInterp
  */
-class CCubicSpline final: public CAkimaInterpolation {
-public:
-  enum END_TYPE {SECOND, FIRST};
+class CCubicSpline final : public CAkimaInterpolation {
+ public:
+  enum END_TYPE { SECOND, FIRST };
 
-private:
+ private:
   const su2double startVal, endVal; /*!< \brief "boundary" values. */
   const END_TYPE startDer, endDer;  /*!< \brief 1st or 2nd derivative "boundary" conditions. */
 
-public:
+ public:
   CCubicSpline() = default;
 
   /*!
@@ -139,28 +137,24 @@ class CCubicSpline final: public CAkimaInterpolation {
    * \param[in] endCondition - 1st or 2nd derivative imposed at the end.
    * \param[in] endValue - value of the derivative imposed at the end.
    */
-  CCubicSpline(const std::vector<su2double> &X, const std::vector<su2double> &Data,
-               END_TYPE startCondition = SECOND, su2double startValue = 0.0,
-               END_TYPE endCondition = SECOND, su2double endValue = 0.0) :
-    startVal(startValue),
-    endVal(endValue),
-    startDer(startCondition),
-    endDer(endCondition) {
-    SetSpline(X,Data);
+  CCubicSpline(const std::vector<su2double>& X, const std::vector<su2double>& Data, END_TYPE startCondition = SECOND,
+               su2double startValue = 0.0, END_TYPE endCondition = SECOND, su2double endValue = 0.0)
+      : startVal(startValue), endVal(endValue), startDer(startCondition), endDer(endCondition) {
+    SetSpline(X, Data);
   }
 
   /*!
    * \brief Build the spline.
    */
-  void SetSpline(const std::vector<su2double> &X, const std::vector<su2double> &Data) override;
+  void SetSpline(const std::vector<su2double>& X, const std::vector<su2double>& Data) override;
 };
 
 /*!
  * \brief Linear interpolation.
  * \ingroup LookUpInterp
  */
-class CLinearInterpolation final: public C1DInterpolation {
-public:
+class CLinearInterpolation final : public C1DInterpolation {
+ public:
   CLinearInterpolation() = default;
 
   /*!
@@ -168,9 +162,7 @@ class CLinearInterpolation final: public C1DInterpolation {
    * \param[in] X - the x values (sorted low to high).
    * \param[in] Data - the f(x) values.
    */
-  CLinearInterpolation(const std::vector<su2double> &X, const std::vector<su2double> &Data) {
-    SetSpline(X,Data);
-  }
+  CLinearInterpolation(const std::vector<su2double>& X, const std::vector<su2double>& Data) { SetSpline(X, Data); }
 
   /*!
    * \brief Evaluate the value of the spline at a point.
@@ -188,12 +180,9 @@ class CLinearInterpolation final: public C1DInterpolation {
  * \param[in] ENUM_INLET_INTERPOLATIONTYPE - enum of the interpolation type to be done
  * \returns the corrected Inlet Interpolated Data.
  */
-std::vector<su2double> CorrectedInletValues(const std::vector<su2double> &Inlet_Interpolated,
-                                       su2double Theta ,
-                                       unsigned short nDim,
-                                       const su2double *Coord,
-                                       unsigned short nVar_Turb,
-                                       INLET_INTERP_TYPE Interpolation_Type);
+std::vector<su2double> CorrectedInletValues(const std::vector<su2double>& Inlet_Interpolated, su2double Theta,
+                                            unsigned short nDim, const su2double* Coord, unsigned short nVar_Turb,
+                                            INLET_INTERP_TYPE Interpolation_Type);
 
 /*!
  * \brief Prints the Inlet Interpolated Data
diff --git a/Common/include/toolboxes/CLinearPartitioner.hpp b/Common/include/toolboxes/CLinearPartitioner.hpp
index ec9ee4e6470..befb327c15a 100644
--- a/Common/include/toolboxes/CLinearPartitioner.hpp
+++ b/Common/include/toolboxes/CLinearPartitioner.hpp
@@ -41,25 +41,25 @@ using namespace std;
  * \author T. Economon
  */
 class CLinearPartitioner {
-
-protected:
-
-  int size;  /*!< \brief MPI Size. */
-
-  vector<unsigned long> firstIndex;               /*!< \brief Vector containing the first index on each rank due to a linear partitioning by global count. */
-  vector<unsigned long> lastIndex;                /*!< \brief Vector containing the last index on each rank due to a linear partitioning by global count. */
-  vector<unsigned long> sizeOnRank;               /*!< \brief Vector containing the total size of the current rank's linear partition. */
-  vector<unsigned long> cumulativeSizeBeforeRank; /*!< \brief Vector containing the cumulative size of all linear partitions before the current rank. */
-
-public:
+ protected:
+  int size; /*!< \brief MPI Size. */
+
+  vector<unsigned long> firstIndex; /*!< \brief Vector containing the first index on each rank due to a linear
+                                       partitioning by global count. */
+  vector<unsigned long> lastIndex;  /*!< \brief Vector containing the last index on each rank due to a linear
+                                       partitioning by global count. */
+  vector<unsigned long>
+      sizeOnRank; /*!< \brief Vector containing the total size of the current rank's linear partition. */
+  vector<unsigned long> cumulativeSizeBeforeRank; /*!< \brief Vector containing the cumulative size of all linear
+                                                     partitions before the current rank. */
+
+ public:
   CLinearPartitioner() = default;
 
   /*!
    * \brief Constructor of the CLinearPartitioner class, see Initialize.
    */
-  CLinearPartitioner(unsigned long global_count,
-                     unsigned long offset,
-                     bool isDisjoint = false) {
+  CLinearPartitioner(unsigned long global_count, unsigned long offset, bool isDisjoint = false) {
     Initialize(global_count, offset, isDisjoint);
   }
 
@@ -69,9 +69,7 @@ class CLinearPartitioner {
    * \param[in] offset - offset from 0 for the first index on rank 0 (typically 0).
    * \param[in] isDisjoint - boolean controlling whether the linear partitions should be disjoint (default is false).
    */
-  void Initialize(unsigned long global_count,
-                  unsigned long offset,
-                  bool isDisjoint = false);
+  void Initialize(unsigned long global_count, unsigned long offset, bool isDisjoint = false);
 
   /*!
    * \brief Get the rank that owns the index based on the linear partitioning.
@@ -85,36 +83,28 @@ class CLinearPartitioner {
    * \param[in] rank - MPI rank identifier.
    * \returns First index of the current rank's linear partition.
    */
-  inline unsigned long GetFirstIndexOnRank(int rank) const {
-    return firstIndex[rank];
-  }
+  inline unsigned long GetFirstIndexOnRank(int rank) const { return firstIndex[rank]; }
 
   /*!
    * \brief Get the last index of the current rank's linear partition.
    * \param[in] rank - MPI rank identifier.
    * \returns Last index of the current rank's linear partition.
    */
-  inline unsigned long GetLastIndexOnRank(int rank) const {
-    return lastIndex[rank];
-  }
+  inline unsigned long GetLastIndexOnRank(int rank) const { return lastIndex[rank]; }
 
   /*!
    * \brief Get the total size of the current rank's linear partition.
    * \param[in] rank - MPI rank identifier.
    * \returns Size of the current rank's linear partition.
    */
-  inline unsigned long GetSizeOnRank(int rank) const {
-    return sizeOnRank[rank];
-  }
+  inline unsigned long GetSizeOnRank(int rank) const { return sizeOnRank[rank]; }
 
   /*!
    * \brief Get the cumulative size of all linear partitions before the current rank.
    * \param[in] rank - MPI rank identifier.
    * \returns Cumulative size of all linear partitions before the current rank.
    */
-  inline unsigned long GetCumulativeSizeBeforeRank(int rank) const {
-    return cumulativeSizeBeforeRank[rank];
-  }
+  inline unsigned long GetCumulativeSizeBeforeRank(int rank) const { return cumulativeSizeBeforeRank[rank]; }
 
   /*!
    * \brief Checks if an index belongs to a rank.
@@ -123,7 +113,6 @@ class CLinearPartitioner {
    * \returns True if index is owned by rank.
    */
   bool IndexBelongsToRank(unsigned long index, int rank) const {
-    return index >= cumulativeSizeBeforeRank[rank] && index < cumulativeSizeBeforeRank[rank+1];
+    return index >= cumulativeSizeBeforeRank[rank] && index < cumulativeSizeBeforeRank[rank + 1];
   }
-
 };
diff --git a/Common/include/toolboxes/CQuasiNewtonInvLeastSquares.hpp b/Common/include/toolboxes/CQuasiNewtonInvLeastSquares.hpp
index e481d77935b..e82b41298b9 100644
--- a/Common/include/toolboxes/CQuasiNewtonInvLeastSquares.hpp
+++ b/Common/include/toolboxes/CQuasiNewtonInvLeastSquares.hpp
@@ -46,17 +46,17 @@
  * as the new input of the FP, run the FP, etc.
  * \ingroup BLAS
  */
-template<class Scalar_t, bool WithMPI = true>
+template <class Scalar_t, bool WithMPI = true>
 class CQuasiNewtonInvLeastSquares {
-public:
+ public:
   using Scalar = Scalar_t;
   using Index = typename su2matrix<Scalar>::Index;
-  static_assert(std::is_floating_point<Scalar>::value,"");
+  static_assert(std::is_floating_point<Scalar>::value, "");
 
-private:
+ private:
   using MPI_Wrapper = typename SelectMPIWrapper<Scalar>::W;
 
-  enum: size_t {BLOCK_SIZE = 1024};     /*!< \brief Loop tiling parameter. */
+  enum : size_t { BLOCK_SIZE = 1024 };  /*!< \brief Loop tiling parameter. */
   std::vector<su2matrix<Scalar> > X, R; /*!< \brief Input and residual history of the FP. */
   su2matrix<Scalar> work;               /*!< \brief Work matrix (FP result, correction, and approx solution). */
   su2vector<Scalar> mat, rhs, sol;      /*!< \brief Matrix, rhs, and solution of the normal equations. */
@@ -67,67 +67,63 @@ class CQuasiNewtonInvLeastSquares {
     for (Index i = 1; i < X.size(); ++i) {
       /*--- Swap instead of moving to re-use the memory of the first sample.
        * This is why X and R are not stored as contiguous blocks of mem. ---*/
-      std::swap(X[i-1], X[i]);
-      std::swap(R[i-1], R[i]);
+      std::swap(X[i - 1], X[i]);
+      std::swap(R[i - 1], R[i]);
     }
   }
 
   void computeNormalEquations() {
     /*--- Size for the dot products. ---*/
-    const auto end = std::min<Index>(nPtDomain,work.rows())*work.cols();
+    const auto end = std::min<Index>(nPtDomain, work.rows()) * work.cols();
 
-    mat = Scalar(0); rhs = Scalar(0);
+    mat = Scalar(0);
+    rhs = Scalar(0);
 
     /*--- Tiled part of the loop. ---*/
     Index begin = 0;
-    while (end-begin >= BLOCK_SIZE) {
+    while (end - begin >= BLOCK_SIZE) {
       computeNormalEquations<BLOCK_SIZE>(mat, rhs, begin);
       begin += BLOCK_SIZE;
     }
 
     /*--- Remainder of the loop. ---*/
     if (begin != end) {
-      computeNormalEquations<0>(mat, rhs, begin, end-begin);
+      computeNormalEquations<0>(mat, rhs, begin, end - begin);
     }
 
     /*--- MPI reduction of the dot products. ---*/
     if (WithMPI) {
-      const auto type = (sizeof(Scalar) < sizeof(double))? MPI_FLOAT : MPI_DOUBLE;
+      const auto type = (sizeof(Scalar) < sizeof(double)) ? MPI_FLOAT : MPI_DOUBLE;
 
       su2vector<Scalar> tmp(mat.size());
-      MPI_Wrapper::Allreduce(mat.data(), tmp.data(), iSample*(iSample+1)/2,
-                             type, MPI_SUM, SU2_MPI::GetComm());
+      MPI_Wrapper::Allreduce(mat.data(), tmp.data(), iSample * (iSample + 1) / 2, type, MPI_SUM, SU2_MPI::GetComm());
       mat = std::move(tmp);
 
-      MPI_Wrapper::Allreduce(rhs.data(), sol.data(), iSample,
-                             type, MPI_SUM, SU2_MPI::GetComm());
+      MPI_Wrapper::Allreduce(rhs.data(), sol.data(), iSample, type, MPI_SUM, SU2_MPI::GetComm());
       std::swap(rhs, sol);
     }
   }
 
-  template<Index StaticSize>
-  void computeNormalEquations(su2vector<Scalar>& mat,
-                              su2vector<Scalar>& vec,
-                              Index start,
-                              Index dynSize = 0) const {
+  template <Index StaticSize>
+  void computeNormalEquations(su2vector<Scalar>& mat, su2vector<Scalar>& vec, Index start, Index dynSize = 0) const {
     /*--- Select either the static or dynamic size, optimizes inner loop. ---*/
-    const auto blkSize = StaticSize? StaticSize : dynSize;
+    const auto blkSize = StaticSize ? StaticSize : dynSize;
 
     for (Index i = 0; i < iSample; ++i) {
-      const auto ri1 = R[i+1].data() + start;
+      const auto ri1 = R[i + 1].data() + start;
       const auto ri0 = R[i].data() + start;
       /*--- Off-diagonal coefficients. ---*/
       for (Index j = 0; j < i; ++j) {
-        const auto rj1 = R[j+1].data() + start;
+        const auto rj1 = R[j + 1].data() + start;
         const auto rj0 = R[j].data() + start;
         /*--- Sum of partial sums to reduce trunc. error. ---*/
         Scalar sum = 0;
         SU2_OMP_SIMD
         for (Index k = 0; k < blkSize; ++k) {
-          sum += (ri1[k]-ri0[k]) * (rj1[k]-rj0[k]);
+          sum += (ri1[k] - ri0[k]) * (rj1[k] - rj0[k]);
         }
         /*--- 1D index of (i,j) in lower triangular storage. ---*/
-        const auto iCoeff = i*(i+1)/2 + j;
+        const auto iCoeff = i * (i + 1) / 2 + j;
         mat(iCoeff) += sum;
       }
       /*--- Diagonal coeff and residual fused. ---*/
@@ -135,15 +131,15 @@ class CQuasiNewtonInvLeastSquares {
       const auto r = R[iSample].data() + start;
       SU2_OMP_SIMD
       for (Index k = 0; k < blkSize; ++k) {
-        diag += pow(ri1[k]-ri0[k], 2);
-        res += (ri1[k]-ri0[k]) * r[k];
+        diag += pow(ri1[k] - ri0[k], 2);
+        res += (ri1[k] - ri0[k]) * r[k];
       }
-      mat(i*(i+3)/2) += diag;
+      mat(i * (i + 3) / 2) += diag;
       vec(i) -= res;
     }
   }
 
-public:
+ public:
   /*! \brief Default construction without allocation. */
   CQuasiNewtonInvLeastSquares() = default;
 
@@ -160,29 +156,31 @@ class CQuasiNewtonInvLeastSquares {
    * \param[in] nptdomain - Local size (<= npt), if 0 it defaults to npt.
    */
   void resize(Index nsample, Index npt, Index nvar, Index nptdomain = 0) {
-    if (nptdomain > npt || nsample < 2)
-      SU2_MPI::Error("Invalid quasi-Newton parameters", CURRENT_FUNCTION);
+    if (nptdomain > npt || nsample < 2) SU2_MPI::Error("Invalid quasi-Newton parameters", CURRENT_FUNCTION);
     iSample = 0;
-    nPtDomain = nptdomain? nptdomain : npt;
-    work.resize(npt,nvar);
+    nPtDomain = nptdomain ? nptdomain : npt;
+    work.resize(npt, nvar);
     X.clear();
     R.clear();
     for (Index i = 0; i < nsample; ++i) {
-      X.emplace_back(npt,nvar);
-      R.emplace_back(npt,nvar);
+      X.emplace_back(npt, nvar);
+      R.emplace_back(npt, nvar);
     }
     X[0] = Scalar(0);
     /*--- Lower triangular packed storage. ---*/
-    mat.resize(nsample*(nsample-1)/2);
-    rhs.resize(nsample-1);
-    sol.resize(nsample-1);
+    mat.resize(nsample * (nsample - 1) / 2);
+    rhs.resize(nsample - 1);
+    sol.resize(nsample - 1);
   }
 
   /*! \brief Size of the object, the number of samples. */
   Index size() const { return X.size(); }
 
   /*! \brief Discard all history, keeping the current solution. */
-  void reset() { std::swap(X[0], X[iSample]); iSample = 0; }
+  void reset() {
+    std::swap(X[0], X[iSample]);
+    iSample = 0;
+  }
 
   /*!
    * \brief Access the current fixed-point result.
@@ -190,8 +188,8 @@ class CQuasiNewtonInvLeastSquares {
    */
   su2matrix<Scalar>& FPresult() { return work; }
   const su2matrix<Scalar>& FPresult() const { return work; }
-  Scalar& FPresult(Index iPt, Index iVar) { return work(iPt,iVar); }
-  const Scalar& FPresult(Index iPt, Index iVar) const { return work(iPt,iVar); }
+  Scalar& FPresult(Index iPt, Index iVar) { return work(iPt, iVar); }
+  const Scalar& FPresult(Index iPt, Index iVar) const { return work(iPt, iVar); }
 
   /*!
    * \brief Access the current solution approximation.
@@ -199,8 +197,8 @@ class CQuasiNewtonInvLeastSquares {
    */
   su2matrix<Scalar>& solution() { return X[iSample]; }
   const su2matrix<Scalar>& solution() const { return X[iSample]; }
-  Scalar& operator() (Index iPt, Index iVar) { return X[iSample](iPt,iVar); }
-  const Scalar& operator() (Index iPt, Index iVar) const { return X[iSample](iPt,iVar); }
+  Scalar& operator()(Index iPt, Index iVar) { return X[iSample](iPt, iVar); }
+  const Scalar& operator()(Index iPt, Index iVar) const { return X[iSample](iPt, iVar); }
 
   /*!
    * \brief Compute and return a new approximation.
@@ -219,35 +217,33 @@ class CQuasiNewtonInvLeastSquares {
       computeNormalEquations();
       CSymmetricMatrix pseudoInv(iSample);
       for (Index i = 0, k = 0; i < iSample; ++i)
-        for (Index j = 0; j <= i; ++j)
-          pseudoInv(i,j) = mat(k++);
+        for (Index j = 0; j <= i; ++j) pseudoInv(i, j) = mat(k++);
       pseudoInv.Invert(true);
       pseudoInv.MatVecMult(rhs.data(), sol.data());
 
       /*--- Compute correction, cleared before for less trunc. error. ---*/
       for (Index k = 0; k < iSample; ++k) {
-        const auto x1 = X[k+1].data();
-        const auto r1 = R[k+1].data();
+        const auto x1 = X[k + 1].data();
+        const auto r1 = R[k + 1].data();
         const auto x0 = X[k].data();
         const auto r0 = R[k].data();
         SU2_OMP_SIMD
         for (Index i = 0; i < work.size(); ++i) {
-          Scalar dy = r1[i]-r0[i] + x1[i]-x0[i];
+          Scalar dy = r1[i] - r0[i] + x1[i] - x0[i];
           work.data()[i] += sol(k) * dy;
         }
       }
     }
 
     /*--- Check for need to shift left. ---*/
-    if (iSample+1 == X.size()) {
+    if (iSample + 1 == X.size()) {
       shiftHistoryLeft();
       iSample--;
     }
 
     /*--- Set new solution. ---*/
     SU2_OMP_SIMD
-    for (Index i = 0; i < work.size(); ++i)
-      work.data()[i] += R[iSample].data()[i] + X[iSample].data()[i];
+    for (Index i = 0; i < work.size(); ++i) work.data()[i] += R[iSample].data()[i] + X[iSample].data()[i];
     std::swap(X[++iSample], work);
 
     return solution();
diff --git a/Common/include/toolboxes/CSquareMatrixCM.hpp b/Common/include/toolboxes/CSquareMatrixCM.hpp
index 35dd27e15f3..178417fe92f 100644
--- a/Common/include/toolboxes/CSquareMatrixCM.hpp
+++ b/Common/include/toolboxes/CSquareMatrixCM.hpp
@@ -39,11 +39,11 @@
 class CSquareMatrixCM {
   static_assert(ColMajorMatrix<passivedouble>::Storage == StorageType::ColumnMajor,
                 "Column major storage is assumed for LAPACK.");
-private:
-  ColMajorMatrix<passivedouble> mat;  /*!< \brief Storage of the actual matrix. */
 
-public:
+ private:
+  ColMajorMatrix<passivedouble> mat; /*!< \brief Storage of the actual matrix. */
 
+ public:
   /*!
    * \brief Default constructor. Nothing to be done.
    */
@@ -55,7 +55,7 @@ class CSquareMatrixCM {
    *        the matrix.
    * \param[in] N - Number of rows and colums of the matrix.
    */
-  CSquareMatrixCM(int N) {Initialize(N);}
+  CSquareMatrixCM(int N) { Initialize(N); }
 
   /*!
    * \brief Operator, which makes available the given matrix element as a reference.
@@ -63,7 +63,7 @@ class CSquareMatrixCM {
    * \param[in] j   - Column index of the matrix element.
    * \return          Reference to element (i,j).
    */
-  inline passivedouble& operator() (int i, int j) {return mat(i,j);}
+  inline passivedouble& operator()(int i, int j) { return mat(i, j); }
 
   /*!
    * \brief Operator, which makes available the given matrix element as a const reference.
@@ -71,31 +71,31 @@ class CSquareMatrixCM {
    * \param[in] j   - Column index of the matrix element.
    * \return          Constant reference to element (i,j).
    */
-  inline const passivedouble& operator() (int i, int j) const {return mat(i,j);}
+  inline const passivedouble& operator()(int i, int j) const { return mat(i, j); }
 
   /*!
    * \brief Function, which makes available a reference to the actual matrix.
    * \return A reference to mat.
    */
-  inline ColMajorMatrix<passivedouble>& GetMat() {return mat;}
+  inline ColMajorMatrix<passivedouble>& GetMat() { return mat; }
 
   /*!
    * \brief Function, which makes available a const reference to the actual matrix.
    * \return A const reference to mat.
    */
-  inline const ColMajorMatrix<passivedouble>& GetMat() const {return mat;}
+  inline const ColMajorMatrix<passivedouble>& GetMat() const { return mat; }
 
   /*!
    * \brief Function, which allocates the memory for the matrix.
    * \param[in] N - Number of rows and colums of the matrix.
    */
-  inline void Initialize(int N) {mat.resize(N,N);}
+  inline void Initialize(int N) { mat.resize(N, N); }
 
   /*!
    * \brief Function, which makes available the size of the matrix.
    * \return The number of rows, columns of the matrix.
    */
-  inline int Size() const {return mat.rows();}
+  inline int Size() const { return mat.rows(); }
 
   /*!
    * \brief Function, which carries out the matrix produc of the current matrix
@@ -104,21 +104,18 @@ class CSquareMatrixCM {
    * \param[in]  mat_in  - Matrix to be multiplied by the current matrix.
    * \param[out] mat_out - Matrix to store the result of the multiplication.
    */
-  void MatMatMult(const char                          side,
-                  const ColMajorMatrix<passivedouble> &mat_in,
-                  ColMajorMatrix<passivedouble>       &mat_out) const;
+  void MatMatMult(const char side, const ColMajorMatrix<passivedouble>& mat_in,
+                  ColMajorMatrix<passivedouble>& mat_out) const;
 
   /*!
    * \brief Naive matrix-vector multiplication with general type.
    */
-  template<class ForwardIt>
-  void MatVecMult(ForwardIt vec_in, ForwardIt vec_out) const
-  {
+  template <class ForwardIt>
+  void MatVecMult(ForwardIt vec_in, ForwardIt vec_out) const {
     for (int i = 0; i < Size(); ++i) {
       *vec_out = 0.0;
       auto vec = vec_in;
-      for (int k = 0; k < Size(); ++k)
-        *vec_out += *(vec++) * mat(i,k);
+      for (int k = 0; k < Size(); ++k) *vec_out += *(vec++) * mat(i, k);
       ++vec_out;
     }
   }
@@ -132,5 +129,4 @@ class CSquareMatrixCM {
    * \brief Function, which transposes the matrix in-place.
    */
   void Transpose();
-
 };
diff --git a/Common/include/toolboxes/CSymmetricMatrix.hpp b/Common/include/toolboxes/CSymmetricMatrix.hpp
index 717b7a45259..2dee2893e34 100644
--- a/Common/include/toolboxes/CSymmetricMatrix.hpp
+++ b/Common/include/toolboxes/CSymmetricMatrix.hpp
@@ -37,7 +37,8 @@
  */
 class CSymmetricMatrix {
   static_assert(su2passivematrix::IsRowMajor, "Row major storage is assumed for LAPACK.");
-private:
+
+ private:
   su2passivematrix mat;
 
   // Not optimized dense matrix factorization and inversion for portability.
@@ -47,30 +48,28 @@ class CSymmetricMatrix {
   void CalcInv_sytri();
   void CalcInv_potri();
 
-public:
+ public:
   CSymmetricMatrix() = default;
-  CSymmetricMatrix(int N) {Initialize(N);}
+  CSymmetricMatrix(int N) { Initialize(N); }
 
   void Initialize(int N);
 
   inline int Size() const { return mat.rows(); }
 
-  inline passivedouble Get(int i, int j) const { return mat(std::min(i,j),std::max(i,j)); }
+  inline passivedouble Get(int i, int j) const { return mat(std::min(i, j), std::max(i, j)); }
 
-  inline void Set(int i, int j, passivedouble val) { mat(std::min(i,j),std::max(i,j)) = val; }
+  inline void Set(int i, int j, passivedouble val) { mat(std::min(i, j), std::max(i, j)) = val; }
 
-  inline passivedouble& operator() (int i, int j) { return mat(std::min(i,j),std::max(i,j)); }
+  inline passivedouble& operator()(int i, int j) { return mat(std::min(i, j), std::max(i, j)); }
 
-  inline const passivedouble& operator() (int i, int j) const { return mat(std::min(i,j),std::max(i,j)); }
+  inline const passivedouble& operator()(int i, int j) const { return mat(std::min(i, j), std::max(i, j)); }
 
-  template<class ForwardIt>
-  void MatVecMult(ForwardIt vec_in, ForwardIt vec_out) const
-  {
+  template <class ForwardIt>
+  void MatVecMult(ForwardIt vec_in, ForwardIt vec_out) const {
     for (int i = 0; i < Size(); ++i) {
       *vec_out = 0.0;
       auto vec = vec_in;
-      for (int k = 0; k < Size(); ++k)
-        *vec_out += *(vec++) * Get(i,k);
+      for (int k = 0; k < Size(); ++k) *vec_out += *(vec++) * Get(i, k);
       ++vec_out;
     }
   }
@@ -80,5 +79,4 @@ class CSymmetricMatrix {
   void Invert(bool is_spd = false);
 
   su2passivematrix StealData();
-
 };
diff --git a/Common/include/toolboxes/MMS/CIncTGVSolution.hpp b/Common/include/toolboxes/MMS/CIncTGVSolution.hpp
index 972b6d4075c..2885cf863f0 100644
--- a/Common/include/toolboxes/MMS/CIncTGVSolution.hpp
+++ b/Common/include/toolboxes/MMS/CIncTGVSolution.hpp
@@ -26,7 +26,6 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #pragma once
 
 #include <cmath>
@@ -37,10 +36,8 @@
  * \brief Class to define the required data for the incompressible Taylor Green Vortex.
  * \author T. Economon, E. van der Weide
  */
-class CIncTGVSolution final: public CVerificationSolution {
-
-protected:
-
+class CIncTGVSolution final : public CVerificationSolution {
+ protected:
   /*--- TGV specific conditions. ---*/
 
   su2double tgvLength;    /*!< \brief Taylor-Green length scale. */
@@ -48,10 +45,9 @@ class CIncTGVSolution final: public CVerificationSolution {
   su2double tgvDensity;   /*!< \brief Taylor-Green density. */
   su2double tgvViscosity; /*!< \brief Taylor-Green viscosity. */
 
-  su2double Temperature;  /*!< \brief Temperature, just to be safe. */
-
-public:
+  su2double Temperature; /*!< \brief Temperature, just to be safe. */
 
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -64,10 +60,7 @@ class CIncTGVSolution final: public CVerificationSolution {
    * \param[in] val_iMesh - Multigrid level of the solver.
    * \param[in] config    - Configuration of the particular problem.
    */
-  CIncTGVSolution(unsigned short val_nDim,
-                  unsigned short val_nvar,
-                  unsigned short val_iMesh,
-                  CConfig*       config);
+  CIncTGVSolution(unsigned short val_nDim, unsigned short val_nvar, unsigned short val_iMesh, CConfig* config);
 
   /*!
    * \brief Destructor of the class.
@@ -80,9 +73,7 @@ class CIncTGVSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetSolution(const su2double *val_coords,
-                   const su2double val_t,
-                   su2double       *val_solution) const override;
+  void GetSolution(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 
   /*!
    * \brief Get the boundary conditions state for an exact solution.
@@ -90,7 +81,5 @@ class CIncTGVSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetBCState(const su2double *val_coords,
-                  const su2double val_t,
-                  su2double       *val_solution) const override;
+  void GetBCState(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 };
diff --git a/Common/include/toolboxes/MMS/CInviscidVortexSolution.hpp b/Common/include/toolboxes/MMS/CInviscidVortexSolution.hpp
index 4e2b733eeeb..f440ad9aac0 100644
--- a/Common/include/toolboxes/MMS/CInviscidVortexSolution.hpp
+++ b/Common/include/toolboxes/MMS/CInviscidVortexSolution.hpp
@@ -26,7 +26,6 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #pragma once
 
 #include <cmath>
@@ -37,26 +36,23 @@
  * \brief Class to define the required data for the Inviscid Vortex.
  * \author E. van der Weide, T. Economon
  */
-class CInviscidVortexSolution final: public CVerificationSolution {
-
-protected:
-
+class CInviscidVortexSolution final : public CVerificationSolution {
+ protected:
   /*--- Specific conditions for the inviscid vortex. ---*/
-  su2double MachVortex;     /*!< \brief Mach number of the undisturbed flow. */
-  su2double x0Vortex;       /*!< \brief Initial x-coordinate of the vortex center. */
-  su2double y0Vortex;       /*!< \brief Initial y-coordinate of the vortex center. */
-  su2double RVortex;        /*!< \brief Radius of the vortex. */
-  su2double epsVortex;      /*!< \brief Strength of the vortex. */
-  su2double thetaVortex;    /*!< \brief Advection angle (in degrees) of the vortex. */
+  su2double MachVortex;  /*!< \brief Mach number of the undisturbed flow. */
+  su2double x0Vortex;    /*!< \brief Initial x-coordinate of the vortex center. */
+  su2double y0Vortex;    /*!< \brief Initial y-coordinate of the vortex center. */
+  su2double RVortex;     /*!< \brief Radius of the vortex. */
+  su2double epsVortex;   /*!< \brief Strength of the vortex. */
+  su2double thetaVortex; /*!< \brief Advection angle (in degrees) of the vortex. */
 
   /*--- Variables involving gamma. */
-  su2double Gamma;        /*!< \brief Gamma */
-  su2double Gm1;          /*!< \brief Gamma minus 1 */
-  su2double ovGm1;        /*!< \brief 1 over Gamma minus 1 */
-  su2double gamOvGm1;     /*!< \brief Gamma over Gamma minus 1 */
-
-public:
+  su2double Gamma;    /*!< \brief Gamma */
+  su2double Gm1;      /*!< \brief Gamma minus 1 */
+  su2double ovGm1;    /*!< \brief 1 over Gamma minus 1 */
+  su2double gamOvGm1; /*!< \brief Gamma over Gamma minus 1 */
 
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -69,10 +65,7 @@ class CInviscidVortexSolution final: public CVerificationSolution {
    * \param[in] val_iMesh - Multigrid level of the solver.
    * \param[in] config    - Configuration of the particular problem.
    */
-  CInviscidVortexSolution(unsigned short val_nDim,
-                          unsigned short val_nvar,
-                          unsigned short val_iMesh,
-                          CConfig*       config);
+  CInviscidVortexSolution(unsigned short val_nDim, unsigned short val_nvar, unsigned short val_iMesh, CConfig* config);
 
   /*!
    * \brief Destructor of the class.
@@ -85,9 +78,7 @@ class CInviscidVortexSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetSolution(const su2double *val_coords,
-                   const su2double val_t,
-                   su2double       *val_solution) const override;
+  void GetSolution(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 
   /*!
    * \brief Get the boundary conditions state for an exact solution.
@@ -95,7 +86,5 @@ class CInviscidVortexSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetBCState(const su2double *val_coords,
-                  const su2double val_t,
-                  su2double       *val_solution) const override;
+  void GetBCState(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 };
diff --git a/Common/include/toolboxes/MMS/CMMSIncEulerSolution.hpp b/Common/include/toolboxes/MMS/CMMSIncEulerSolution.hpp
index 0af37d51bd6..eb71b4c5a61 100644
--- a/Common/include/toolboxes/MMS/CMMSIncEulerSolution.hpp
+++ b/Common/include/toolboxes/MMS/CMMSIncEulerSolution.hpp
@@ -26,7 +26,6 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #pragma once
 
 #include <cmath>
@@ -38,13 +37,11 @@
  *        incompressible Euler equations.
  * \author T. Economon, E. van der Weide
  */
-class CMMSIncEulerSolution final: public CVerificationSolution {
-
-protected:
-
+class CMMSIncEulerSolution final : public CVerificationSolution {
+ protected:
   /*--- Variables that define the solution and MMS source term. ---*/
-  su2double Density;      /*!< \brief Density, must be constant. */
-  su2double Temperature;  /*!< \brief Temperature, just to be safe. */
+  su2double Density;     /*!< \brief Density, must be constant. */
+  su2double Temperature; /*!< \brief Temperature, just to be safe. */
 
   /*--- Constants, which describe this manufactured solution. This is a
    solution where the primitive variables vary as a combination
@@ -52,13 +49,12 @@ class CMMSIncEulerSolution final: public CVerificationSolution {
    Knupp P, "Code verification by the method of manufactured solutions,"
    SAND 2000-1444, Sandia National Laboratories, Albuquerque, NM, 2000. ---*/
 
-  su2double P_0;      /*!< \brief Parameter for the pressure solution. */
-  su2double u_0;      /*!< \brief Parameter for the x-velocity solution. */
-  su2double v_0;      /*!< \brief Parameter for the y-velocity solution. */
-  su2double epsilon;  /*!< \brief Parameter for the velocity solutions. */
-
-public:
+  su2double P_0;     /*!< \brief Parameter for the pressure solution. */
+  su2double u_0;     /*!< \brief Parameter for the x-velocity solution. */
+  su2double v_0;     /*!< \brief Parameter for the y-velocity solution. */
+  su2double epsilon; /*!< \brief Parameter for the velocity solutions. */
 
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -71,10 +67,7 @@ class CMMSIncEulerSolution final: public CVerificationSolution {
    * \param[in] val_iMesh - Multigrid level of the solver.
    * \param[in] config    - Configuration of the particular problem.
    */
-  CMMSIncEulerSolution(unsigned short val_nDim,
-                       unsigned short val_nvar,
-                       unsigned short val_iMesh,
-                       CConfig*       config);
+  CMMSIncEulerSolution(unsigned short val_nDim, unsigned short val_nvar, unsigned short val_iMesh, CConfig* config);
 
   /*!
    * \brief Destructor of the class.
@@ -87,9 +80,7 @@ class CMMSIncEulerSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetSolution(const su2double *val_coords,
-                   const su2double val_t,
-                   su2double       *val_solution) const override;
+  void GetSolution(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 
   /*!
    * \brief Get the boundary conditions state for an exact solution.
@@ -97,9 +88,7 @@ class CMMSIncEulerSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetBCState(const su2double *val_coords,
-                  const su2double val_t,
-                  su2double       *val_solution) const override;
+  void GetBCState(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 
   /*!
    * \brief Get the source term for the manufactured solution (MMS).
@@ -107,9 +96,7 @@ class CMMSIncEulerSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetMMSSourceTerm(const su2double *val_coords,
-                        const su2double val_t,
-                        su2double       *val_source) const override;
+  void GetMMSSourceTerm(const su2double* val_coords, const su2double val_t, su2double* val_source) const override;
 
   /*!
    * \brief Whether or not this verification solution is a manufactured solution.
diff --git a/Common/include/toolboxes/MMS/CMMSIncNSSolution.hpp b/Common/include/toolboxes/MMS/CMMSIncNSSolution.hpp
index 19f58034a49..51cc3e630d9 100644
--- a/Common/include/toolboxes/MMS/CMMSIncNSSolution.hpp
+++ b/Common/include/toolboxes/MMS/CMMSIncNSSolution.hpp
@@ -26,7 +26,6 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #pragma once
 
 #include <cmath>
@@ -38,14 +37,12 @@
  *        laminar incompressible Navier-Stokes equations.
  * \author T. Economon, E. van der Weide
  */
-class CMMSIncNSSolution final: public CVerificationSolution {
-
-protected:
-
+class CMMSIncNSSolution final : public CVerificationSolution {
+ protected:
   /*--- Variables that define the solution and MMS source term. ---*/
-  su2double Viscosity;    /*!< \brief Viscosity, must be constant. */
-  su2double Density;      /*!< \brief Density, must be constant. */
-  su2double Temperature;  /*!< \brief Temperature, just to be safe. */
+  su2double Viscosity;   /*!< \brief Viscosity, must be constant. */
+  su2double Density;     /*!< \brief Density, must be constant. */
+  su2double Temperature; /*!< \brief Temperature, just to be safe. */
 
   /*--- Constants, which describe this manufactured solution. This is a
    viscous solution where the primitive variables vary as a combination
@@ -53,13 +50,12 @@ class CMMSIncNSSolution final: public CVerificationSolution {
    Knupp P, "Code verification by the method of manufactured solutions,"
    SAND 2000-1444, Sandia National Laboratories, Albuquerque, NM, 2000. ---*/
 
-  su2double P_0;      /*!< \brief Parameter for the pressure solution. */
-  su2double u_0;      /*!< \brief Parameter for the x-velocity solution. */
-  su2double v_0;      /*!< \brief Parameter for the y-velocity solution. */
-  su2double epsilon;  /*!< \brief Parameter for the velocity solutions. */
-
-public:
+  su2double P_0;     /*!< \brief Parameter for the pressure solution. */
+  su2double u_0;     /*!< \brief Parameter for the x-velocity solution. */
+  su2double v_0;     /*!< \brief Parameter for the y-velocity solution. */
+  su2double epsilon; /*!< \brief Parameter for the velocity solutions. */
 
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -72,10 +68,7 @@ class CMMSIncNSSolution final: public CVerificationSolution {
    * \param[in] val_iMesh - Multigrid level of the solver.
    * \param[in] config    - Configuration of the particular problem.
    */
-  CMMSIncNSSolution(unsigned short val_nDim,
-                    unsigned short val_nvar,
-                    unsigned short val_iMesh,
-                    CConfig*       config);
+  CMMSIncNSSolution(unsigned short val_nDim, unsigned short val_nvar, unsigned short val_iMesh, CConfig* config);
 
   /*!
    * \brief Destructor of the class.
@@ -88,9 +81,7 @@ class CMMSIncNSSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetSolution(const su2double *val_coords,
-                   const su2double val_t,
-                   su2double       *val_solution) const override;
+  void GetSolution(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 
   /*!
    * \brief Get the boundary conditions state for an exact solution.
@@ -98,9 +89,7 @@ class CMMSIncNSSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetBCState(const su2double *val_coords,
-                  const su2double val_t,
-                  su2double       *val_solution) const override;
+  void GetBCState(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 
   /*!
    * \brief Get the source term for the manufactured solution (MMS).
@@ -108,9 +97,7 @@ class CMMSIncNSSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetMMSSourceTerm(const su2double *val_coords,
-                        const su2double val_t,
-                        su2double       *val_source) const override;
+  void GetMMSSourceTerm(const su2double* val_coords, const su2double val_t, su2double* val_source) const override;
 
   /*!
    * \brief Whether or not this verification solution is a manufactured solution.
diff --git a/Common/include/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.hpp b/Common/include/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.hpp
index 3977986f43b..acb9fa3a796 100644
--- a/Common/include/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.hpp
+++ b/Common/include/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.hpp
@@ -26,7 +26,6 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #pragma once
 
 #include <cmath>
@@ -38,33 +37,31 @@
           laminar Navier-Stokes equations on the domain between two half circles.
  * \author E. van der Weide, T. Economon
  */
-class CMMSNSTwoHalfCirclesSolution final: public CVerificationSolution {
-
-protected:
+class CMMSNSTwoHalfCirclesSolution final : public CVerificationSolution {
+ protected:
   /*--- Variables that define the solution and MMS source term. ---*/
-  su2double Gamma;              /*!< \brief Specific heat ratio. */
-  su2double RGas;               /*!< \brief Gas constant. */
-  su2double Viscosity;          /*!< \brief Constant viscosity. */
-  su2double Conductivity;       /*!< \brief Constant thermal conductivity. */
-  su2double TWall;              /*!< \brief Prescribed wall temperature at the outer wall. */
+  su2double Gamma;        /*!< \brief Specific heat ratio. */
+  su2double RGas;         /*!< \brief Gas constant. */
+  su2double Viscosity;    /*!< \brief Constant viscosity. */
+  su2double Conductivity; /*!< \brief Constant thermal conductivity. */
+  su2double TWall;        /*!< \brief Prescribed wall temperature at the outer wall. */
 
-  su2double Pressure_Ref;       /*!< \brief Reference pressure for non-dimensionalization. */
-  su2double Density_Ref;        /*!< \brief Reference density for non-dimensionalization.  */
-  su2double Velocity_Ref;       /*!< \brief Reference velocity for non-dimensionalization. */
+  su2double Pressure_Ref; /*!< \brief Reference pressure for non-dimensionalization. */
+  su2double Density_Ref;  /*!< \brief Reference density for non-dimensionalization.  */
+  su2double Velocity_Ref; /*!< \brief Reference velocity for non-dimensionalization. */
 
   /*--- Constants, which describe this manufactured solution. The primitive variables
         rho, T, u, v and w are described by analytical functions in such a way that the
         inner wall is an adiabatic no-slip wall and the outer wall is an isothermal
         no-slip wall. ---*/
-  su2double rho_0;    /*!< \brief Constant density. */
-  su2double u_0;      /*!< \brief Maximum x-velocity in the domain. */
-  su2double v_0;      /*!< \brief Maximum y-velocity in the domain. */
-
-  su2double a_T1;     /*!< \brief Parameter for the temperature solution. */
-  su2double a_T2;     /*!< \brief Parameter for the temperature solution. */
+  su2double rho_0; /*!< \brief Constant density. */
+  su2double u_0;   /*!< \brief Maximum x-velocity in the domain. */
+  su2double v_0;   /*!< \brief Maximum y-velocity in the domain. */
 
-public:
+  su2double a_T1; /*!< \brief Parameter for the temperature solution. */
+  su2double a_T2; /*!< \brief Parameter for the temperature solution. */
 
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -77,10 +74,8 @@ class CMMSNSTwoHalfCirclesSolution final: public CVerificationSolution {
    * \param[in] val_iMesh - Multigrid level of the solver.
    * \param[in] config    - Configuration of the particular problem.
    */
-  CMMSNSTwoHalfCirclesSolution(unsigned short val_nDim,
-                               unsigned short val_nvar,
-                               unsigned short val_iMesh,
-                               CConfig*       config);
+  CMMSNSTwoHalfCirclesSolution(unsigned short val_nDim, unsigned short val_nvar, unsigned short val_iMesh,
+                               CConfig* config);
 
   /*!
    * \brief Destructor of the class.
@@ -93,9 +88,7 @@ class CMMSNSTwoHalfCirclesSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetSolution(const su2double *val_coords,
-                   const su2double val_t,
-                   su2double       *val_solution) const override;
+  void GetSolution(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 
   /*!
    * \brief Get the boundary conditions state for an exact solution.
@@ -103,9 +96,7 @@ class CMMSNSTwoHalfCirclesSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetBCState(const su2double *val_coords,
-                  const su2double val_t,
-                  su2double       *val_solution) const override;
+  void GetBCState(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 
   /*!
    * \brief Get the source term for the manufactured solution (MMS).
@@ -113,9 +104,7 @@ class CMMSNSTwoHalfCirclesSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetMMSSourceTerm(const su2double *val_coords,
-                        const su2double val_t,
-                        su2double       *val_source) const override;
+  void GetMMSSourceTerm(const su2double* val_coords, const su2double val_t, su2double* val_source) const override;
 
   /*!
    * \brief Whether or not this verification solution is a manufactured solution.
diff --git a/Common/include/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.hpp b/Common/include/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.hpp
index 5ae529d2251..f879b3dc177 100644
--- a/Common/include/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.hpp
+++ b/Common/include/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.hpp
@@ -26,7 +26,6 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #pragma once
 
 #include <cmath>
@@ -38,34 +37,32 @@
           laminar Navier-Stokes equations on the domain between two half spheres.
  * \author E. van der Weide, T. Economon
  */
-class CMMSNSTwoHalfSpheresSolution final: public CVerificationSolution {
-
-protected:
+class CMMSNSTwoHalfSpheresSolution final : public CVerificationSolution {
+ protected:
   /*--- Variables that define the solution and MMS source term. ---*/
-  su2double Gamma;              /*!< \brief Specific heat ratio. */
-  su2double RGas;               /*!< \brief Gas constant. */
-  su2double Viscosity;          /*!< \brief Constant viscosity. */
-  su2double Conductivity;       /*!< \brief Constant thermal conductivity. */
-  su2double TWall;              /*!< \brief Prescribed wall temperature at the outer wall. */
+  su2double Gamma;        /*!< \brief Specific heat ratio. */
+  su2double RGas;         /*!< \brief Gas constant. */
+  su2double Viscosity;    /*!< \brief Constant viscosity. */
+  su2double Conductivity; /*!< \brief Constant thermal conductivity. */
+  su2double TWall;        /*!< \brief Prescribed wall temperature at the outer wall. */
 
-  su2double Pressure_Ref;       /*!< \brief Reference pressure for non-dimensionalization. */
-  su2double Density_Ref;        /*!< \brief Reference density for non-dimensionalization.  */
-  su2double Velocity_Ref;       /*!< \brief Reference velocity for non-dimensionalization. */
+  su2double Pressure_Ref; /*!< \brief Reference pressure for non-dimensionalization. */
+  su2double Density_Ref;  /*!< \brief Reference density for non-dimensionalization.  */
+  su2double Velocity_Ref; /*!< \brief Reference velocity for non-dimensionalization. */
 
   /*--- Constants, which describe this manufactured solution. The primitive variables
         rho, T, u, v and w are described by analytical functions in such a way that the
         inner wall is an adiabatic no-slip wall and the outer wall is an isothermal
         no-slip wall. ---*/
-  su2double rho_0;    /*!< \brief Constant density. */
-  su2double u_0;      /*!< \brief Maximum x-velocity in the domain. */
-  su2double v_0;      /*!< \brief Maximum y-velocity in the domain. */
-  su2double w_0;      /*!< \brief Maximum z-velocity in the domain. */
-
-  su2double a_T1;     /*!< \brief Parameter for the temperature solution. */
-  su2double a_T2;     /*!< \brief Parameter for the temperature solution. */
+  su2double rho_0; /*!< \brief Constant density. */
+  su2double u_0;   /*!< \brief Maximum x-velocity in the domain. */
+  su2double v_0;   /*!< \brief Maximum y-velocity in the domain. */
+  su2double w_0;   /*!< \brief Maximum z-velocity in the domain. */
 
-public:
+  su2double a_T1; /*!< \brief Parameter for the temperature solution. */
+  su2double a_T2; /*!< \brief Parameter for the temperature solution. */
 
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -78,10 +75,8 @@ class CMMSNSTwoHalfSpheresSolution final: public CVerificationSolution {
    * \param[in] val_iMesh - Multigrid level of the solver.
    * \param[in] config    - Configuration of the particular problem.
    */
-  CMMSNSTwoHalfSpheresSolution(unsigned short val_nDim,
-                               unsigned short val_nvar,
-                               unsigned short val_iMesh,
-                               CConfig*       config);
+  CMMSNSTwoHalfSpheresSolution(unsigned short val_nDim, unsigned short val_nvar, unsigned short val_iMesh,
+                               CConfig* config);
 
   /*!
    * \brief Destructor of the class.
@@ -94,9 +89,7 @@ class CMMSNSTwoHalfSpheresSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetSolution(const su2double *val_coords,
-                   const su2double val_t,
-                   su2double       *val_solution) const override;
+  void GetSolution(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 
   /*!
    * \brief Get the boundary conditions state for an exact solution.
@@ -104,9 +97,7 @@ class CMMSNSTwoHalfSpheresSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetBCState(const su2double *val_coords,
-                  const su2double val_t,
-                  su2double       *val_solution) const override;
+  void GetBCState(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 
   /*!
    * \brief Get the source term for the manufactured solution (MMS).
@@ -114,9 +105,7 @@ class CMMSNSTwoHalfSpheresSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetMMSSourceTerm(const su2double *val_coords,
-                        const su2double val_t,
-                        su2double       *val_source) const override;
+  void GetMMSSourceTerm(const su2double* val_coords, const su2double val_t, su2double* val_source) const override;
 
   /*!
    * \brief Whether or not this verification solution is a manufactured solution.
diff --git a/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolution.hpp b/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolution.hpp
index c74ec885101..387fa5c78b7 100644
--- a/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolution.hpp
+++ b/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolution.hpp
@@ -26,7 +26,6 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #pragma once
 
 #include <cmath>
@@ -38,10 +37,8 @@
           laminar Navier-Stokes equations on a unit quad.
  * \author E. van der Weide, T. Economon
  */
-class CMMSNSUnitQuadSolution final: public CVerificationSolution {
-
-protected:
-
+class CMMSNSUnitQuadSolution final : public CVerificationSolution {
+ protected:
   /*--- Variables that define the solution and MMS source term. ---*/
   su2double Gamma;        /*!< \brief Specific heat ratio. */
   su2double RGas;         /*!< \brief Gas constant. */
@@ -53,38 +50,37 @@ class CMMSNSUnitQuadSolution final: public CVerificationSolution {
         combination of sine and cosine functions. The unit quad is probably not
         necessary, and an arbitrary domain should work as well. ---*/
 
-  su2double L;        /*!< \brief Length scale. */
-  su2double a_Px;     /*!< \brief Parameter for the pressure solution. */
-  su2double a_Pxy;    /*!< \brief Parameter for the pressure solution. */
-  su2double a_Py;     /*!< \brief Parameter for the pressure solution. */
-  su2double a_rhox;   /*!< \brief Parameter for the density solution. */
-  su2double a_rhoxy;  /*!< \brief Parameter for the density solution. */
-  su2double a_rhoy;   /*!< \brief Parameter for the density solution. */
-  su2double a_ux;     /*!< \brief Parameter for the x-velocity solution. */
-  su2double a_uxy;    /*!< \brief Parameter for the x-velocity solution. */
-  su2double a_uy;     /*!< \brief Parameter for the x-velocity solution. */
-  su2double a_vx;     /*!< \brief Parameter for the y-velocity solution. */
-  su2double a_vxy;    /*!< \brief Parameter for the y-velocity solution. */
-  su2double a_vy;     /*!< \brief Parameter for the y-velocity solution. */
-  su2double P_0;      /*!< \brief Parameter for the pressure solution. */
-  su2double P_x;      /*!< \brief Parameter for the pressure solution. */
-  su2double P_xy;     /*!< \brief Parameter for the pressure solution. */
-  su2double P_y;      /*!< \brief Parameter for the pressure solution. */
-  su2double rho_0;    /*!< \brief Parameter for the density solution. */
-  su2double rho_x;    /*!< \brief Parameter for the density solution. */
-  su2double rho_xy;   /*!< \brief Parameter for the density solution. */
-  su2double rho_y;    /*!< \brief Parameter for the density solution. */
-  su2double u_0;      /*!< \brief Parameter for the x-velocity solution. */
-  su2double u_x;      /*!< \brief Parameter for the x-velocity solution. */
-  su2double u_xy;     /*!< \brief Parameter for the x-velocity solution. */
-  su2double u_y;      /*!< \brief Parameter for the x-velocity solution. */
-  su2double v_0;      /*!< \brief Parameter for the y-velocity solution. */
-  su2double v_x;      /*!< \brief Parameter for the y-velocity solution. */
-  su2double v_xy;     /*!< \brief Parameter for the y-velocity solution. */
-  su2double v_y;      /*!< \brief Parameter for the y-velocity solution. */
-
-public:
-
+  su2double L;       /*!< \brief Length scale. */
+  su2double a_Px;    /*!< \brief Parameter for the pressure solution. */
+  su2double a_Pxy;   /*!< \brief Parameter for the pressure solution. */
+  su2double a_Py;    /*!< \brief Parameter for the pressure solution. */
+  su2double a_rhox;  /*!< \brief Parameter for the density solution. */
+  su2double a_rhoxy; /*!< \brief Parameter for the density solution. */
+  su2double a_rhoy;  /*!< \brief Parameter for the density solution. */
+  su2double a_ux;    /*!< \brief Parameter for the x-velocity solution. */
+  su2double a_uxy;   /*!< \brief Parameter for the x-velocity solution. */
+  su2double a_uy;    /*!< \brief Parameter for the x-velocity solution. */
+  su2double a_vx;    /*!< \brief Parameter for the y-velocity solution. */
+  su2double a_vxy;   /*!< \brief Parameter for the y-velocity solution. */
+  su2double a_vy;    /*!< \brief Parameter for the y-velocity solution. */
+  su2double P_0;     /*!< \brief Parameter for the pressure solution. */
+  su2double P_x;     /*!< \brief Parameter for the pressure solution. */
+  su2double P_xy;    /*!< \brief Parameter for the pressure solution. */
+  su2double P_y;     /*!< \brief Parameter for the pressure solution. */
+  su2double rho_0;   /*!< \brief Parameter for the density solution. */
+  su2double rho_x;   /*!< \brief Parameter for the density solution. */
+  su2double rho_xy;  /*!< \brief Parameter for the density solution. */
+  su2double rho_y;   /*!< \brief Parameter for the density solution. */
+  su2double u_0;     /*!< \brief Parameter for the x-velocity solution. */
+  su2double u_x;     /*!< \brief Parameter for the x-velocity solution. */
+  su2double u_xy;    /*!< \brief Parameter for the x-velocity solution. */
+  su2double u_y;     /*!< \brief Parameter for the x-velocity solution. */
+  su2double v_0;     /*!< \brief Parameter for the y-velocity solution. */
+  su2double v_x;     /*!< \brief Parameter for the y-velocity solution. */
+  su2double v_xy;    /*!< \brief Parameter for the y-velocity solution. */
+  su2double v_y;     /*!< \brief Parameter for the y-velocity solution. */
+
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -97,10 +93,7 @@ class CMMSNSUnitQuadSolution final: public CVerificationSolution {
    * \param[in] val_iMesh - Multigrid level of the solver.
    * \param[in] config    - Configuration of the particular problem.
    */
-  CMMSNSUnitQuadSolution(unsigned short val_nDim,
-                         unsigned short val_nvar,
-                         unsigned short val_iMesh,
-                         CConfig*       config);
+  CMMSNSUnitQuadSolution(unsigned short val_nDim, unsigned short val_nvar, unsigned short val_iMesh, CConfig* config);
 
   /*!
    * \brief Destructor of the class.
@@ -113,9 +106,7 @@ class CMMSNSUnitQuadSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetSolution(const su2double *val_coords,
-                   const su2double val_t,
-                   su2double       *val_solution) const override;
+  void GetSolution(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 
   /*!
    * \brief Get the boundary conditions state for an exact solution.
@@ -123,9 +114,7 @@ class CMMSNSUnitQuadSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetBCState(const su2double *val_coords,
-                  const su2double val_t,
-                  su2double       *val_solution) const override;
+  void GetBCState(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 
   /*!
    * \brief Get the source term for the manufactured solution (MMS).
@@ -133,9 +122,7 @@ class CMMSNSUnitQuadSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetMMSSourceTerm(const su2double *val_coords,
-                        const su2double val_t,
-                        su2double       *val_source) const override;
+  void GetMMSSourceTerm(const su2double* val_coords, const su2double val_t, su2double* val_source) const override;
 
   /*!
    * \brief Whether or not this verification solution is a manufactured solution.
diff --git a/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.hpp b/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.hpp
index 5aa25502f09..ba2135bb343 100644
--- a/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.hpp
+++ b/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.hpp
@@ -26,7 +26,6 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #pragma once
 
 #include <cmath>
@@ -38,10 +37,8 @@
           laminar Navier-Stokes equations on a unit quad with wall boundary conditions.
  * \author E. van der Weide, T. Economon
  */
-class CMMSNSUnitQuadSolutionWallBC final: public CVerificationSolution {
-
-protected:
-
+class CMMSNSUnitQuadSolutionWallBC final : public CVerificationSolution {
+ protected:
   /*--- Variables that define the solution and MMS source term. ---*/
   su2double Gamma;        /*!< \brief Specific heat ratio. */
   su2double RGas;         /*!< \brief Gas constant. */
@@ -49,23 +46,22 @@ class CMMSNSUnitQuadSolutionWallBC final: public CVerificationSolution {
   su2double Conductivity; /*!< \brief Thermal conductivity, must be constant. */
   su2double TWall;        /*!< \brief Prescribed wall temperature at the upper wall. */
 
-  su2double Pressure_Ref;       /*!< \brief Reference pressure for non-dimensionalization. */
-  su2double Density_Ref;        /*!< \brief Reference density for non-dimensionalization.  */
-  su2double Velocity_Ref;       /*!< \brief Reference velocity for non-dimensionalization. */
+  su2double Pressure_Ref; /*!< \brief Reference pressure for non-dimensionalization. */
+  su2double Density_Ref;  /*!< \brief Reference density for non-dimensionalization.  */
+  su2double Velocity_Ref; /*!< \brief Reference velocity for non-dimensionalization. */
 
   /*--- Constants, which describe this manufactured solution. The primitive variables
         rho, T, u and v are described by analytical functions in such a way that the
         lower wall is an adiabatic no-slip wall and the upper wall is an isothermal
         no-slip wall. ---*/
-  su2double rho_0;    /*!< \brief Constant density. */
-  su2double u_0;      /*!< \brief Maximum x-velocity in the domain. */
-  su2double v_0;      /*!< \brief Maximum y-velocity in the domain. */
-
-  su2double a_T1;     /*!< \brief Parameter for the temperature solution. */
-  su2double a_T2;     /*!< \brief Parameter for the temperature solution. */
+  su2double rho_0; /*!< \brief Constant density. */
+  su2double u_0;   /*!< \brief Maximum x-velocity in the domain. */
+  su2double v_0;   /*!< \brief Maximum y-velocity in the domain. */
 
-public:
+  su2double a_T1; /*!< \brief Parameter for the temperature solution. */
+  su2double a_T2; /*!< \brief Parameter for the temperature solution. */
 
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -78,10 +74,8 @@ class CMMSNSUnitQuadSolutionWallBC final: public CVerificationSolution {
    * \param[in] val_iMesh - Multigrid level of the solver.
    * \param[in] config    - Configuration of the particular problem.
    */
-  CMMSNSUnitQuadSolutionWallBC(unsigned short val_nDim,
-                               unsigned short val_nvar,
-                               unsigned short val_iMesh,
-                               CConfig*       config);
+  CMMSNSUnitQuadSolutionWallBC(unsigned short val_nDim, unsigned short val_nvar, unsigned short val_iMesh,
+                               CConfig* config);
 
   /*!
    * \brief Destructor of the class.
@@ -94,9 +88,7 @@ class CMMSNSUnitQuadSolutionWallBC final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetSolution(const su2double *val_coords,
-                   const su2double val_t,
-                   su2double       *val_solution) const override;
+  void GetSolution(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 
   /*!
    * \brief Get the boundary conditions state for an exact solution.
@@ -104,9 +96,7 @@ class CMMSNSUnitQuadSolutionWallBC final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetBCState(const su2double *val_coords,
-                  const su2double val_t,
-                  su2double       *val_solution) const override;
+  void GetBCState(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 
   /*!
    * \brief Get the source term for the manufactured solution (MMS).
@@ -114,9 +104,7 @@ class CMMSNSUnitQuadSolutionWallBC final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetMMSSourceTerm(const su2double *val_coords,
-                        const su2double val_t,
-                        su2double       *val_source) const override;
+  void GetMMSSourceTerm(const su2double* val_coords, const su2double val_t, su2double* val_source) const override;
 
   /*!
    * \brief Whether or not this verification solution is a manufactured solution.
diff --git a/Common/include/toolboxes/MMS/CNSUnitQuadSolution.hpp b/Common/include/toolboxes/MMS/CNSUnitQuadSolution.hpp
index 5bd57b60045..2d5bd8eac48 100644
--- a/Common/include/toolboxes/MMS/CNSUnitQuadSolution.hpp
+++ b/Common/include/toolboxes/MMS/CNSUnitQuadSolution.hpp
@@ -26,7 +26,6 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #pragma once
 
 #include <cmath>
@@ -38,17 +37,14 @@
           on a unit quad, heat conduction is neglected.
  * \author E. van der Weide, T. Economon
  */
-class CNSUnitQuadSolution final: public CVerificationSolution {
-
-protected:
-
+class CNSUnitQuadSolution final : public CVerificationSolution {
+ protected:
   /*--- Variables that define the soltion. ---*/
-  su2double Gm1;          /*!< \brief Gamma minus 1 */
-  su2double flowAngle;    /*!< \brief Angle of the velocity vector in radians. */
-  su2double Viscosity;    /*!< \brief Viscosity, must be constant. */
-
-public:
+  su2double Gm1;       /*!< \brief Gamma minus 1 */
+  su2double flowAngle; /*!< \brief Angle of the velocity vector in radians. */
+  su2double Viscosity; /*!< \brief Viscosity, must be constant. */
 
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -61,10 +57,7 @@ class CNSUnitQuadSolution final: public CVerificationSolution {
    * \param[in] val_iMesh - Multigrid level of the solver.
    * \param[in] config    - Configuration of the particular problem.
    */
-  CNSUnitQuadSolution(unsigned short val_nDim,
-                      unsigned short val_nvar,
-                      unsigned short val_iMesh,
-                      CConfig*       config);
+  CNSUnitQuadSolution(unsigned short val_nDim, unsigned short val_nvar, unsigned short val_iMesh, CConfig* config);
 
   /*!
    * \brief Destructor of the class.
@@ -77,9 +70,7 @@ class CNSUnitQuadSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetSolution(const su2double *val_coords,
-                   const su2double val_t,
-                   su2double       *val_solution) const override;
+  void GetSolution(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 
   /*!
    * \brief Get the boundary conditions state for an exact solution.
@@ -87,7 +78,5 @@ class CNSUnitQuadSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetBCState(const su2double *val_coords,
-                  const su2double val_t,
-                  su2double       *val_solution) const override;
+  void GetBCState(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 };
diff --git a/Common/include/toolboxes/MMS/CRinglebSolution.hpp b/Common/include/toolboxes/MMS/CRinglebSolution.hpp
index ff9a63fd62f..889b9729801 100644
--- a/Common/include/toolboxes/MMS/CRinglebSolution.hpp
+++ b/Common/include/toolboxes/MMS/CRinglebSolution.hpp
@@ -26,7 +26,6 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #pragma once
 
 #include <cmath>
@@ -37,18 +36,15 @@
  * \brief Class to define the required data for the Ringleb flow.
  * \author E. van der Weide, T. Economon
  */
-class CRinglebSolution final: public CVerificationSolution {
-
-protected:
-
+class CRinglebSolution final : public CVerificationSolution {
+ protected:
   /*--- Variables involving gamma. ---*/
-  su2double Gamma;        /*!< \brief Gamma */
-  su2double Gm1;          /*!< \brief Gamma minus 1 */
-  su2double tovGm1;       /*!< \brief 2 over Gamma minus 1 */
-  su2double tGamOvGm1;    /*!< \brief 2 Gamma over Gamma minus 1 */
-
-public:
+  su2double Gamma;     /*!< \brief Gamma */
+  su2double Gm1;       /*!< \brief Gamma minus 1 */
+  su2double tovGm1;    /*!< \brief 2 over Gamma minus 1 */
+  su2double tGamOvGm1; /*!< \brief 2 Gamma over Gamma minus 1 */
 
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -61,10 +57,7 @@ class CRinglebSolution final: public CVerificationSolution {
    * \param[in] val_iMesh - Multigrid level of the solver.
    * \param[in] config    - Configuration of the particular problem.
    */
-  CRinglebSolution(unsigned short val_nDim,
-                   unsigned short val_nvar,
-                   unsigned short val_iMesh,
-                   CConfig*       config);
+  CRinglebSolution(unsigned short val_nDim, unsigned short val_nvar, unsigned short val_iMesh, CConfig* config);
 
   /*!
    * \brief Destructor of the class.
@@ -77,9 +70,7 @@ class CRinglebSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetSolution(const su2double *val_coords,
-                   const su2double val_t,
-                   su2double       *val_solution) const override;
+  void GetSolution(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 
   /*!
    * \brief Get the boundary conditions state for an exact solution.
@@ -87,7 +78,5 @@ class CRinglebSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetBCState(const su2double *val_coords,
-                  const su2double val_t,
-                  su2double       *val_solution) const override;
+  void GetBCState(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 };
diff --git a/Common/include/toolboxes/MMS/CTGVSolution.hpp b/Common/include/toolboxes/MMS/CTGVSolution.hpp
index de8537a8846..f40b22fe530 100644
--- a/Common/include/toolboxes/MMS/CTGVSolution.hpp
+++ b/Common/include/toolboxes/MMS/CTGVSolution.hpp
@@ -26,7 +26,6 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #pragma once
 
 #include <cmath>
@@ -37,20 +36,17 @@
  * \brief Class to define the required data for the Taylor Green Vortex.
  * \author E. van der Weide, T. Economon
  */
-class CTGVSolution final: public CVerificationSolution {
-
-protected:
-
+class CTGVSolution final : public CVerificationSolution {
+ protected:
   /*--- TGV specific conditions. ---*/
 
-  su2double tgvLength;    /*!< \brief Taylor-Green length scale. */
-  su2double tgvVelocity;  /*!< \brief Taylor-Green velocity. */
-  su2double tgvDensity;   /*!< \brief Taylor-Green density. */
-  su2double tgvPressure;  /*!< \brief Taylor-Green pressure. */
-  su2double ovGm1;        /*!< \brief 1 over Gamma minus 1 */
-
-public:
+  su2double tgvLength;   /*!< \brief Taylor-Green length scale. */
+  su2double tgvVelocity; /*!< \brief Taylor-Green velocity. */
+  su2double tgvDensity;  /*!< \brief Taylor-Green density. */
+  su2double tgvPressure; /*!< \brief Taylor-Green pressure. */
+  su2double ovGm1;       /*!< \brief 1 over Gamma minus 1 */
 
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -63,10 +59,7 @@ class CTGVSolution final: public CVerificationSolution {
    * \param[in] val_iMesh - Multigrid level of the solver.
    * \param[in] config    - Configuration of the particular problem.
    */
-  CTGVSolution(unsigned short val_nDim,
-               unsigned short val_nvar,
-               unsigned short val_iMesh,
-               CConfig*       config);
+  CTGVSolution(unsigned short val_nDim, unsigned short val_nvar, unsigned short val_iMesh, CConfig* config);
 
   /*!
    * \brief Destructor of the class.
@@ -79,9 +72,7 @@ class CTGVSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetSolution(const su2double *val_coords,
-                   const su2double val_t,
-                   su2double       *val_solution) const override;
+  void GetSolution(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 
   /*!
    * \brief Whether or not the exact solution is known for this verification solution.
diff --git a/Common/include/toolboxes/MMS/CUserDefinedSolution.hpp b/Common/include/toolboxes/MMS/CUserDefinedSolution.hpp
index b6c2d1be6f5..d2b28861e0f 100644
--- a/Common/include/toolboxes/MMS/CUserDefinedSolution.hpp
+++ b/Common/include/toolboxes/MMS/CUserDefinedSolution.hpp
@@ -36,10 +36,8 @@
  * \brief Class to define the required data for a user defined solution.
  * \author E. van der Weide, T. Economon
  */
-class CUserDefinedSolution final: public CVerificationSolution {
-
-public:
-
+class CUserDefinedSolution final : public CVerificationSolution {
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -52,10 +50,7 @@ class CUserDefinedSolution final: public CVerificationSolution {
    * \param[in] val_iMesh - Multigrid level of the solver.
    * \param[in] config    - Configuration of the particular problem.
    */
-  CUserDefinedSolution(unsigned short val_nDim,
-                       unsigned short val_nvar,
-                       unsigned short val_iMesh,
-                       CConfig*       config);
+  CUserDefinedSolution(unsigned short val_nDim, unsigned short val_nvar, unsigned short val_iMesh, CConfig* config);
 
   /*!
    * \brief Destructor of the class.
@@ -68,9 +63,7 @@ class CUserDefinedSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetSolution(const su2double *val_coords,
-                   const su2double val_t,
-                   su2double       *val_solution) const override;
+  void GetSolution(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 
   /*!
    * \brief Get the boundary conditions state for an exact solution.
@@ -78,9 +71,7 @@ class CUserDefinedSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetBCState(const su2double *val_coords,
-                  const su2double val_t,
-                  su2double       *val_solution) const override;
+  void GetBCState(const su2double* val_coords, const su2double val_t, su2double* val_solution) const override;
 
   /*!
    * \brief Get the source term for the manufactured solution (MMS).
@@ -88,9 +79,7 @@ class CUserDefinedSolution final: public CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetMMSSourceTerm(const su2double *val_coords,
-                        const su2double val_t,
-                        su2double       *val_source) const override;
+  void GetMMSSourceTerm(const su2double* val_coords, const su2double val_t, su2double* val_source) const override;
 
   /*!
    * \brief Whether or not this verification solution is a manufactured solution.
diff --git a/Common/include/toolboxes/MMS/CVerificationSolution.hpp b/Common/include/toolboxes/MMS/CVerificationSolution.hpp
index c3308307b37..0802409dbc4 100644
--- a/Common/include/toolboxes/MMS/CVerificationSolution.hpp
+++ b/Common/include/toolboxes/MMS/CVerificationSolution.hpp
@@ -38,25 +38,22 @@
  * \author T. Economon, E. van der Weide
  */
 class CVerificationSolution {
+ protected:
+  int rank; /*!< \brief MPI Rank. */
+  int size; /*!< \brief MPI Size. */
 
-protected:
-  int rank;  /*!< \brief MPI Rank. */
-  int size;  /*!< \brief MPI Size. */
+  unsigned short nDim; /*!< \brief Number of dimension of the problem. */
+  unsigned short nVar; /*!< \brief Number of variables of the problem  */
 
-  unsigned short nDim;  /*!< \brief Number of dimension of the problem. */
-  unsigned short nVar;  /*!< \brief Number of variables of the problem  */
+  MAIN_SOLVER Kind_Solver; /*!< \brief The kind of solver we are running. */
 
-  MAIN_SOLVER Kind_Solver;                  /*!< \brief The kind of solver we are running. */
-
-private:
-
-  su2double *Error_RMS;                        /*!< \brief Vector with the global RMS error for each variable in a verification case. */
-  su2double *Error_Max;                        /*!< \brief Vector with the global max error for each variable in a verification case. */
-  unsigned long *Error_Point_Max;              /*!< \brief Global index for the node with the max error in a verification case. */
-  su2double **Error_Point_Max_Coord;           /*!< \brief Coordinates for the node with the max error in a verification case. */
-
-public:
+ private:
+  su2double* Error_RMS; /*!< \brief Vector with the global RMS error for each variable in a verification case. */
+  su2double* Error_Max; /*!< \brief Vector with the global max error for each variable in a verification case. */
+  unsigned long* Error_Point_Max;    /*!< \brief Global index for the node with the max error in a verification case. */
+  su2double** Error_Point_Max_Coord; /*!< \brief Coordinates for the node with the max error in a verification case. */
 
+ public:
   /*!
    * \brief Constructor of the class.
    */
@@ -69,10 +66,7 @@ class CVerificationSolution {
    * \param[in] val_iMesh - Multigrid level of the solver.
    * \param[in] config    - Definition of the particular problem.
    */
-  CVerificationSolution(unsigned short val_nDim,
-                        unsigned short val_nvar,
-                        unsigned short val_iMesh,
-                        CConfig *config);
+  CVerificationSolution(unsigned short val_nDim, unsigned short val_nvar, unsigned short val_iMesh, CConfig* config);
 
   /*!
    * \brief Destructor of the class.
@@ -85,17 +79,14 @@ class CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  virtual void GetSolution(const su2double *val_coords,
-                           const su2double val_t,
-                           su2double       *val_solution) const;
+  virtual void GetSolution(const su2double* val_coords, const su2double val_t, su2double* val_solution) const;
 
   /*!
    * \brief Get the exact solution at the current position and t = 0.
    * \param[in] val_coords   - Cartesian coordinates of the current position.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  void GetInitialCondition(const su2double *val_coords,
-                           su2double       *val_solution) const;
+  void GetInitialCondition(const su2double* val_coords, su2double* val_solution) const;
 
   /*!
    * \brief Get the boundary conditions state for an exact solution.
@@ -103,9 +94,7 @@ class CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  virtual void GetBCState(const su2double *val_coords,
-                          const su2double val_t,
-                          su2double       *val_solution) const;
+  virtual void GetBCState(const su2double* val_coords, const su2double val_t, su2double* val_solution) const;
 
   /*!
    * \brief Get the source term for the manufactured solution (MMS).
@@ -113,9 +102,7 @@ class CVerificationSolution {
    * \param[in] val_t        - Current physical time.
    * \param[in] val_solution - Array where the exact solution is stored.
    */
-  virtual void GetMMSSourceTerm(const su2double *val_coords,
-                                const su2double val_t,
-                                su2double       *val_source) const;
+  virtual void GetMMSSourceTerm(const su2double* val_coords, const su2double val_t, su2double* val_source) const;
 
   /*!
    * \brief Whether or not this verification solution is a manufactured solution.
@@ -137,10 +124,8 @@ class CVerificationSolution {
    * \param[in]  val_solution - Array where the exact solution is stored.
    * \param[out] val_error    - Array where the local error is stored.
    */
-  void GetLocalError(const su2double *val_coords,
-                     const su2double val_t,
-                     const su2double *GetLocalErrorval_solution,
-                     su2double       *val_error) const;
+  void GetLocalError(const su2double* val_coords, const su2double val_t, const su2double* GetLocalErrorval_solution,
+                     su2double* val_error) const;
 
   /*!
    * \brief Set the global RMS error for verification cases.
@@ -169,7 +154,7 @@ class CVerificationSolution {
    * \param[in] val_error - Value of the maximum error to store in the position <i>val_var</i>.
    */
   void SetError_Max(unsigned short val_var, su2double val_error, unsigned long val_point) {
-    Error_Max[val_var]       = val_error;
+    Error_Max[val_var] = val_error;
     Error_Point_Max[val_var] = val_point;
   }
 
@@ -184,8 +169,7 @@ class CVerificationSolution {
     if (val_error > Error_Max[val_var]) {
       Error_Max[val_var] = val_error;
       Error_Point_Max[val_var] = val_point;
-      for (unsigned short iDim = 0; iDim < nDim; iDim++)
-        Error_Point_Max_Coord[val_var][iDim] = val_coord[iDim];
+      for (unsigned short iDim = 0; iDim < nDim; iDim++) Error_Point_Max_Coord[val_var][iDim] = val_coord[iDim];
     }
   }
 
@@ -215,6 +199,5 @@ class CVerificationSolution {
    * \param[in] nDOFsGlobal - Global number of degrees of freedom for the current problem.
    * \param[in] config      - Definition of the particular problem.
    */
-  void SetVerificationError(unsigned long nDOFsGlobal,
-                            CConfig       *config);
+  void SetVerificationError(unsigned long nDOFsGlobal, CConfig* config);
 };
diff --git a/Common/include/toolboxes/allocation_toolbox.hpp b/Common/include/toolboxes/allocation_toolbox.hpp
index ce02fd8f857..2b0adb1f31a 100644
--- a/Common/include/toolboxes/allocation_toolbox.hpp
+++ b/Common/include/toolboxes/allocation_toolbox.hpp
@@ -40,18 +40,11 @@
 
 #include <cassert>
 
-namespace MemoryAllocation
-{
+namespace MemoryAllocation {
 
-inline constexpr bool is_power_of_two(size_t x)
-{
-  return x && !(x & (x-1));
-}
+inline constexpr bool is_power_of_two(size_t x) { return x && !(x & (x - 1)); }
 
-inline constexpr size_t round_up(size_t multiple, size_t x)
-{
-  return ((x+multiple-1)/multiple)*multiple;
-}
+inline constexpr size_t round_up(size_t multiple, size_t x) { return ((x + multiple - 1) / multiple) * multiple; }
 
 /*!
  * \brief Aligned memory allocation compatible across platforms.
@@ -60,20 +53,18 @@ inline constexpr size_t round_up(size_t multiple, size_t x)
  * \tparam ZeroInit, initialize memory to 0.
  * \return Pointer to memory, always use su2::aligned_free to deallocate.
  */
-template<class T, bool ZeroInit = false>
-inline T* aligned_alloc(size_t alignment, size_t size) noexcept
-{
+template <class T, bool ZeroInit = false>
+inline T* aligned_alloc(size_t alignment, size_t size) noexcept {
   assert(is_power_of_two(alignment));
 
-  if(alignment < alignof(void*)) alignment = alignof(void*);
+  if (alignment < alignof(void*)) alignment = alignof(void*);
 
   size = round_up(alignment, size);
 
   void* ptr = nullptr;
 
 #if defined(__APPLE__)
-  if(::posix_memalign(&ptr, alignment, size) != 0)
-  {
+  if (::posix_memalign(&ptr, alignment, size) != 0) {
     ptr = nullptr;
   }
 #elif defined(_WIN32)
@@ -89,9 +80,8 @@ inline T* aligned_alloc(size_t alignment, size_t size) noexcept
  * \brief Free memory allocated with su2::aligned_alloc.
  * \param[in] ptr, pointer to memory we want to release.
  */
-template<class T>
-inline void aligned_free(T* ptr) noexcept
-{
+template <class T>
+inline void aligned_free(T* ptr) noexcept {
 #if defined(_WIN32)
   _aligned_free(ptr);
 #else
@@ -99,5 +89,4 @@ inline void aligned_free(T* ptr) noexcept
 #endif
 }
 
-} // namespace
-
+}  // namespace MemoryAllocation
diff --git a/Common/include/toolboxes/geometry_toolbox.hpp b/Common/include/toolboxes/geometry_toolbox.hpp
index 430bc62a39d..8cb1d988df3 100644
--- a/Common/include/toolboxes/geometry_toolbox.hpp
+++ b/Common/include/toolboxes/geometry_toolbox.hpp
@@ -33,58 +33,58 @@ namespace GeometryToolbox {
 /// @{
 
 /*! \return ||a-b||^2 */
-template<class T, class U, typename Int>
+template <class T, class U, typename Int>
 inline T SquaredDistance(Int nDim, const T* a, const U* b) {
   T d(0);
-  for(Int i = 0; i < nDim; i++) d += pow(a[i]-b[i], 2);
+  for (Int i = 0; i < nDim; i++) d += pow(a[i] - b[i], 2);
   return d;
 }
 
 /*! \return ||a-b|| */
-template<class T, class U, typename Int>
+template <class T, class U, typename Int>
 inline T Distance(Int nDim, const T* a, const U* b) {
   return sqrt(SquaredDistance(nDim, a, b));
 }
 
 /*! \brief d = a-b */
-template<class T, typename Int>
+template <class T, typename Int>
 inline void Distance(Int nDim, const T* a, const T* b, T* d) {
-  for(Int i = 0; i < nDim; i++) d[i] = a[i] - b[i];
+  for (Int i = 0; i < nDim; i++) d[i] = a[i] - b[i];
 }
 
 /*! \brief Reflect a at b: c = 2*b - a
  */
-template<class T, typename Int>
-inline void PointPointReflect(Int nDim, const T* a, const T* b, T* d){
-  for(Int i = 0; i < nDim; i++) d[i] = 2 * b[i] - a[i];
+template <class T, typename Int>
+inline void PointPointReflect(Int nDim, const T* a, const T* b, T* d) {
+  for (Int i = 0; i < nDim; i++) d[i] = 2 * b[i] - a[i];
 }
 
 /*! \return a.b */
-template<class T, typename Int>
+template <class T, typename Int>
 inline T DotProduct(Int nDim, const T* a, const T* b) {
   T d(0);
-  for (Int i = 0; i < nDim; ++i) d += a[i]*b[i];
+  for (Int i = 0; i < nDim; ++i) d += a[i] * b[i];
   return d;
 }
 
 /*! \return ||a||^2 */
-template<class T, typename Int>
+template <class T, typename Int>
 inline T SquaredNorm(Int nDim, const T* a) {
   return DotProduct(nDim, a, a);
 }
 
 /*! \return ||a|| */
-template<class T, typename Int>
+template <class T, typename Int>
 inline T Norm(Int nDim, const T* a) {
   return sqrt(SquaredNorm(nDim, a));
 }
 
 /*! \brief c = a x b */
-template<class T>
+template <class T>
 inline void CrossProduct(const T* a, const T* b, T* c) {
-  c[0] = a[1]*b[2] - a[2]*b[1];
-  c[1] = a[2]*b[0] - a[0]*b[2];
-  c[2] = a[0]*b[1] - a[1]*b[0];
+  c[0] = a[1] * b[2] - a[2] * b[1];
+  c[1] = a[2] * b[0] - a[0] * b[2];
+  c[2] = a[0] * b[1] - a[1] * b[0];
 }
 
 /*!
@@ -92,14 +92,13 @@ inline void CrossProduct(const T* a, const T* b, T* c) {
  *        direction d intersects the plane defined by point p0 and normal n.
  * \return The intersection distance.
  */
-template<class T, int nDim>
+template <class T, int nDim>
 inline T LinePlaneIntersection(const T* l0, const T* d, const T* p0, const T* n, T* c) {
   T dist[nDim] = {0.0};
   Distance(nDim, p0, l0, dist);
   T alpha = DotProduct(nDim, dist, n) / DotProduct(nDim, d, n);
-  for (int iDim = 0; iDim < nDim; ++iDim)
-    c[iDim] = l0[iDim] + alpha * d[iDim];
-  return fabs(alpha) * Norm(nDim,d);
+  for (int iDim = 0; iDim < nDim; ++iDim) c[iDim] = l0[iDim] + alpha * d[iDim];
+  return fabs(alpha) * Norm(nDim, d);
 }
 
 /*!
@@ -107,22 +106,21 @@ inline T LinePlaneIntersection(const T* l0, const T* d, const T* p0, const T* n,
  *        by point p0 and normal n if projected perpendicular to it.
  * \return The normal distance.
  */
-template<class T, int nDim>
+template <class T, int nDim>
 inline T PointPlaneProjection(const T* p1, const T* p0, const T* n, T* c) {
-  return LinePlaneIntersection<T,nDim>(p1, n, p0, n, c);
+  return LinePlaneIntersection<T, nDim>(p1, n, p0, n, c);
 }
 
 /*! \brief Set U as the normal to a 2D line defined by coords[iPoint][iDim]. */
-template<class T, class U>
+template <class T, class U>
 inline void LineNormal(const T& coords, U* normal) {
   normal[0] = coords[0][1] - coords[1][1];
   normal[1] = coords[1][0] - coords[0][0];
 }
 
 /*! \brief Normal vector of a triangle, cross product of two sides. */
-template<class T, class U>
+template <class T, class U>
 inline void TriangleNormal(const T& coords, U* normal) {
-
   U a[3], b[3];
 
   for (int iDim = 0; iDim < 3; iDim++) {
@@ -131,13 +129,14 @@ inline void TriangleNormal(const T& coords, U* normal) {
   }
 
   CrossProduct(a, b, normal);
-  normal[0] *= 0.5; normal[1] *= 0.5; normal[2] *= 0.5;
+  normal[0] *= 0.5;
+  normal[1] *= 0.5;
+  normal[2] *= 0.5;
 }
 
 /*! \brief Normal vector of a quadrilateral, cross product of the two diagonals. */
-template<class T, class U>
+template <class T, class U>
 inline void QuadrilateralNormal(const T& coords, U* normal) {
-
   U a[3], b[3];
 
   for (int iDim = 0; iDim < 3; iDim++) {
@@ -146,48 +145,53 @@ inline void QuadrilateralNormal(const T& coords, U* normal) {
   }
 
   CrossProduct(a, b, normal);
-  normal[0] *= 0.5; normal[1] *= 0.5; normal[2] *= 0.5;
+  normal[0] *= 0.5;
+  normal[1] *= 0.5;
+  normal[2] *= 0.5;
 }
 
 /*!
  * \brief Compute a 3D rotation matrix.
  * \note The implicit ordering is rotation about the x, y, and then z axis.
  */
-template<class Scalar, class Matrix>
+template <class Scalar, class Matrix>
 inline void RotationMatrix(Scalar theta, Scalar phi, Scalar psi, Matrix& mat) {
+  Scalar cosTheta = cos(theta);
+  Scalar cosPhi = cos(phi);
+  Scalar cosPsi = cos(psi);
+  Scalar sinTheta = sin(theta);
+  Scalar sinPhi = sin(phi);
+  Scalar sinPsi = sin(psi);
 
-  Scalar cosTheta = cos(theta);  Scalar cosPhi = cos(phi);  Scalar cosPsi = cos(psi);
-  Scalar sinTheta = sin(theta);  Scalar sinPhi = sin(phi);  Scalar sinPsi = sin(psi);
-
-  mat[0][0] = cosPhi*cosPsi;
-  mat[1][0] = cosPhi*sinPsi;
+  mat[0][0] = cosPhi * cosPsi;
+  mat[1][0] = cosPhi * sinPsi;
   mat[2][0] = -sinPhi;
 
-  mat[0][1] = sinTheta*sinPhi*cosPsi - cosTheta*sinPsi;
-  mat[1][1] = sinTheta*sinPhi*sinPsi + cosTheta*cosPsi;
-  mat[2][1] = sinTheta*cosPhi;
+  mat[0][1] = sinTheta * sinPhi * cosPsi - cosTheta * sinPsi;
+  mat[1][1] = sinTheta * sinPhi * sinPsi + cosTheta * cosPsi;
+  mat[2][1] = sinTheta * cosPhi;
 
-  mat[0][2] = cosTheta*sinPhi*cosPsi + sinTheta*sinPsi;
-  mat[1][2] = cosTheta*sinPhi*sinPsi - sinTheta*cosPsi;
-  mat[2][2] = cosTheta*cosPhi;
+  mat[0][2] = cosTheta * sinPhi * cosPsi + sinTheta * sinPsi;
+  mat[1][2] = cosTheta * sinPhi * sinPsi - sinTheta * cosPsi;
+  mat[2][2] = cosTheta * cosPhi;
 }
 
 /*! \brief Compute a 2D rotation matrix. */
-template<class Scalar, class Matrix>
+template <class Scalar, class Matrix>
 inline void RotationMatrix(Scalar psi, Matrix& mat) {
-
   Scalar cosPsi = cos(psi);
   Scalar sinPsi = sin(psi);
 
-  mat[0][0] = cosPsi;  mat[0][1] =-sinPsi;
-  mat[1][0] = sinPsi;  mat[1][1] = cosPsi;
+  mat[0][0] = cosPsi;
+  mat[0][1] = -sinPsi;
+  mat[1][0] = sinPsi;
+  mat[1][1] = cosPsi;
 }
 
 /*! \brief Apply a rotation matrix (R) about origin (O) to a point at
  *         distance (d) from it to obtain new coordinate (c). */
-template<class Scalar, int nDim>
+template <class Scalar, int nDim>
 inline void Rotate(const Scalar R[][nDim], const Scalar* O, const Scalar* d, Scalar* c) {
-
   for (int iDim = 0; iDim < nDim; ++iDim) {
     c[iDim] = O[iDim];
     for (int k = 0; k < nDim; ++k) c[iDim] += R[iDim][k] * d[k];
@@ -195,16 +199,13 @@ inline void Rotate(const Scalar R[][nDim], const Scalar* O, const Scalar* d, Sca
 }
 
 /*! \brief Tangent projection  */
-template<class Mat, class Scalar, class Int>
+template <class Mat, class Scalar, class Int>
 inline void TangentProjection(Int nDim, const Mat& tensor, const Scalar* vector, Scalar* proj) {
-
-  for (Int iDim = 0; iDim < nDim; iDim++)
-    proj[iDim] = DotProduct(nDim, tensor[iDim], vector);
+  for (Int iDim = 0; iDim < nDim; iDim++) proj[iDim] = DotProduct(nDim, tensor[iDim], vector);
 
   auto normalProj = DotProduct(nDim, proj, vector);
 
-  for (Int iDim = 0; iDim < nDim; iDim++)
-    proj[iDim] -= normalProj * vector[iDim];
+  for (Int iDim = 0; iDim < nDim; iDim++) proj[iDim] -= normalProj * vector[iDim];
 }
 /// @}
-}
+}  // namespace GeometryToolbox
diff --git a/Common/include/toolboxes/graph_toolbox.hpp b/Common/include/toolboxes/graph_toolbox.hpp
index ef39ffaf80a..0a57ec21fd0 100644
--- a/Common/include/toolboxes/graph_toolbox.hpp
+++ b/Common/include/toolboxes/graph_toolbox.hpp
@@ -45,8 +45,7 @@
  * \brief In FVM points are connected by the edges (faces) of the grid.
  *        In FEM, two points are connected if they have an element in common.
  */
-enum class ConnectivityType {FiniteVolume=0, FiniteElement=1};
-
+enum class ConnectivityType { FiniteVolume = 0, FiniteElement = 1 };
 
 /*!
  * \class CCompressedSparsePattern
@@ -55,17 +54,17 @@ enum class ConnectivityType {FiniteVolume=0, FiniteElement=1};
  * If built for row-major storage the inner indices are column indices
  * and the pattern should be used as (row,icol), otherwise as (col,irow).
  */
-template<typename Index_t>
+template <typename Index_t>
 class CCompressedSparsePattern {
-  static_assert(std::is_integral<Index_t>::value,"");
+  static_assert(std::is_integral<Index_t>::value, "");
 
-private:
-  su2vector<Index_t> m_outerPtr; /*!< \brief Start positions of the inner indices for each outer index. */
-  su2vector<Index_t> m_innerIdx; /*!< \brief Inner indices of the non zero entries. */
-  su2vector<Index_t> m_diagPtr;  /*!< \brief Position of the diagonal entry. */
+ private:
+  su2vector<Index_t> m_outerPtr;       /*!< \brief Start positions of the inner indices for each outer index. */
+  su2vector<Index_t> m_innerIdx;       /*!< \brief Inner indices of the non zero entries. */
+  su2vector<Index_t> m_diagPtr;        /*!< \brief Position of the diagonal entry. */
   su2vector<Index_t> m_innerIdxTransp; /*!< \brief Position of the transpose non zero entries, requires symmetry. */
 
-public:
+ public:
   using IndexType = Index_t;
 
   /*!
@@ -74,9 +73,7 @@ class CCompressedSparsePattern {
   struct CInnerIter {
     const IndexType* const m_first = nullptr;
     const IndexType* const m_last = nullptr;
-    CInnerIter(const IndexType* first, const IndexType* last) :
-      m_first(first), m_last(last) {
-    }
+    CInnerIter(const IndexType* first, const IndexType* last) : m_first(first), m_last(last) {}
     const IndexType* begin() const { return m_first; }
     const IndexType* end() const { return m_last; }
   };
@@ -92,16 +89,14 @@ class CCompressedSparsePattern {
    * \param[in] outerPtrEnd - End of outer pointers.
    * \param[in] defaultInnerIdx - Default value for inner indices.
    */
-  template<class Iterator>
-  CCompressedSparsePattern(Iterator outerPtrBegin, Iterator outerPtrEnd, Index_t defaultInnerIdx)
-  {
+  template <class Iterator>
+  CCompressedSparsePattern(Iterator outerPtrBegin, Iterator outerPtrEnd, Index_t defaultInnerIdx) {
     const auto size = outerPtrEnd - outerPtrBegin;
     m_outerPtr.resize(size);
     Index_t k = 0;
-    for(auto it = outerPtrBegin; it != outerPtrEnd; ++it)
-      m_outerPtr(k++) = *it;
+    for (auto it = outerPtrBegin; it != outerPtrEnd; ++it) m_outerPtr(k++) = *it;
 
-    m_innerIdx.resize(m_outerPtr(size-1)) = defaultInnerIdx;
+    m_innerIdx.resize(m_outerPtr(size - 1)) = defaultInnerIdx;
   }
 
   /*!
@@ -110,12 +105,10 @@ class CCompressedSparsePattern {
    * \param[in] outerPtr - Outer index pointers.
    * \param[in] innerIdx - Inner indices.
    */
-  CCompressedSparsePattern(su2vector<Index_t>&& outerPtr,
-                           su2vector<Index_t>&& innerIdx) :
-    m_outerPtr(outerPtr), m_innerIdx(innerIdx)
-  {
+  CCompressedSparsePattern(su2vector<Index_t>&& outerPtr, su2vector<Index_t>&& innerIdx)
+      : m_outerPtr(outerPtr), m_innerIdx(innerIdx) {
     /*--- perform a basic sanity check ---*/
-    assert(m_innerIdx.size() == m_outerPtr(m_outerPtr.size()-1));
+    assert(m_innerIdx.size() == m_outerPtr(m_outerPtr.size() - 1));
   }
 
   /*!
@@ -124,51 +117,44 @@ class CCompressedSparsePattern {
    * \param[in] outerPtr - Outer index pointers.
    * \param[in] innerIdx - Inner indices.
    */
-  template<class T>
-  CCompressedSparsePattern(const T& outerPtr, const T& innerIdx)
-  {
+  template <class T>
+  CCompressedSparsePattern(const T& outerPtr, const T& innerIdx) {
     m_outerPtr.resize(outerPtr.size());
-    for(Index_t i=0; i<outerPtr.size(); ++i)
-      m_outerPtr(i) = outerPtr.data()[i];
+    for (Index_t i = 0; i < outerPtr.size(); ++i) m_outerPtr(i) = outerPtr.data()[i];
 
     m_innerIdx.resize(innerIdx.size());
-    for(Index_t i=0; i<innerIdx.size(); ++i)
-      m_innerIdx(i) = innerIdx.data()[i];
+    for (Index_t i = 0; i < innerIdx.size(); ++i) m_innerIdx(i) = innerIdx.data()[i];
 
     /*--- perform a basic sanity check ---*/
-    assert(m_innerIdx.size() == m_outerPtr(m_outerPtr.size()-1));
+    assert(m_innerIdx.size() == m_outerPtr(m_outerPtr.size() - 1));
   }
 
   /*!
    * \brief Build from a "list of lists" type object
    * \param[in] lil - An object with operator [][] and method "size" e.g. vector<vector<?> >.
    */
-  template<class T>
-  CCompressedSparsePattern(const T& lil)
-  {
-    m_outerPtr.resize(lil.size()+1);
+  template <class T>
+  CCompressedSparsePattern(const T& lil) {
+    m_outerPtr.resize(lil.size() + 1);
     m_outerPtr(0) = 0;
-    for(Index_t i=1; i < Index_t(m_outerPtr.size()); ++i)
-      m_outerPtr(i) = m_outerPtr(i-1) + lil[i-1].size();
+    for (Index_t i = 1; i < Index_t(m_outerPtr.size()); ++i) m_outerPtr(i) = m_outerPtr(i - 1) + lil[i - 1].size();
 
     m_innerIdx.resize(m_outerPtr(lil.size()));
     Index_t k = 0;
-    for(Index_t i=0; i < Index_t(lil.size()); ++i)
-      for(Index_t j=0; j < Index_t(lil[i].size()); ++j)
-        m_innerIdx(k++) = lil[i][j];
+    for (Index_t i = 0; i < Index_t(lil.size()); ++i)
+      for (Index_t j = 0; j < Index_t(lil[i].size()); ++j) m_innerIdx(k++) = lil[i][j];
   }
 
   /*!
    * \brief Build a list of pointers to the diagonal entries of the pattern.
    */
   void buildDiagPtr() {
-    if(!m_diagPtr.empty()) return;
+    if (!m_diagPtr.empty()) return;
 
     m_diagPtr.resize(getOuterSize());
 
     SU2_OMP_PARALLEL_(for schedule(static,roundUpDiv(getOuterSize(),omp_get_max_threads())))
-    for(Index_t k = 0; k < getOuterSize(); ++k)
-      m_diagPtr(k) = findInnerIdx(k,k);
+    for (Index_t k = 0; k < getOuterSize(); ++k) m_diagPtr(k) = findInnerIdx(k, k);
     END_SU2_OMP_PARALLEL
   }
 
@@ -176,15 +162,15 @@ class CCompressedSparsePattern {
    * \brief Build a list of pointers to the transpose entries of the pattern, requires symmetry.
    */
   void buildTransposePtr() {
-    if(!m_innerIdxTransp.empty()) return;
+    if (!m_innerIdxTransp.empty()) return;
 
     m_innerIdxTransp.resize(getNumNonZeros());
 
     SU2_OMP_PARALLEL_(for schedule(static,roundUpDiv(getOuterSize(),omp_get_max_threads())))
-    for(Index_t i = 0; i < getOuterSize(); ++i) {
-      for(Index_t k = m_outerPtr(i); k < m_outerPtr(i+1); ++k) {
+    for (Index_t i = 0; i < getOuterSize(); ++i) {
+      for (Index_t k = m_outerPtr(i); k < m_outerPtr(i + 1); ++k) {
         auto j = m_innerIdx(k);
-        m_innerIdxTransp(k) = findInnerIdx(j,i);
+        m_innerIdxTransp(k) = findInnerIdx(j, i);
         assert(m_innerIdxTransp(k) != m_innerIdx.size() && "The pattern is not symmetric.");
       }
     }
@@ -194,31 +180,23 @@ class CCompressedSparsePattern {
   /*!
    * \return True if the pattern is empty, i.e. has not been built yet.
    */
-  inline bool empty() const {
-    return m_outerPtr.empty() || m_innerIdx.empty();
-  }
+  inline bool empty() const { return m_outerPtr.empty() || m_innerIdx.empty(); }
 
   /*!
    * \return Number of rows/columns.
    */
-  inline Index_t getOuterSize() const {
-    return m_outerPtr.size()-1;
-  }
+  inline Index_t getOuterSize() const { return m_outerPtr.size() - 1; }
 
   /*!
    * \return Number of non zero entries.
    */
-  inline Index_t getNumNonZeros() const {
-    return m_innerIdx.size();
-  }
+  inline Index_t getNumNonZeros() const { return m_innerIdx.size(); }
 
   /*!
    * \param[in] iOuterIdx - Outer index.
    * \return Number of inner indices associated with the outer index.
    */
-  inline Index_t getNumNonZeros(Index_t iOuterIdx) const {
-    return m_outerPtr(iOuterIdx+1) - m_outerPtr(iOuterIdx);
-  }
+  inline Index_t getNumNonZeros(Index_t iOuterIdx) const { return m_outerPtr(iOuterIdx + 1) - m_outerPtr(iOuterIdx); }
 
   /*!
    * \param[in] iOuterIdx - Outer index.
@@ -245,8 +223,7 @@ class CCompressedSparsePattern {
    * \return Iterator to inner dimension to use in range for loops.
    */
   inline CInnerIter getInnerIter(Index_t iOuterIdx) const {
-    return CInnerIter(m_innerIdx.data()+m_outerPtr(iOuterIdx),
-                      m_innerIdx.data()+m_outerPtr(iOuterIdx+1));
+    return CInnerIter(m_innerIdx.data() + m_outerPtr(iOuterIdx), m_innerIdx.data() + m_outerPtr(iOuterIdx + 1));
   }
 
   /*!
@@ -256,8 +233,8 @@ class CCompressedSparsePattern {
    *         or NNZ if position does not belong to the pattern.
    */
   inline Index_t findInnerIdx(Index_t iOuterIdx, Index_t iInnerIdx) const {
-    for(Index_t k = m_outerPtr(iOuterIdx); k < m_outerPtr(iOuterIdx+1); ++k)
-      if(m_innerIdx(k) == iInnerIdx) return k;
+    for (Index_t k = m_outerPtr(iOuterIdx); k < m_outerPtr(iOuterIdx + 1); ++k)
+      if (m_innerIdx(k) == iInnerIdx) return k;
     return m_innerIdx.size();
   }
 
@@ -279,7 +256,7 @@ class CCompressedSparsePattern {
   inline Index_t quickFindInnerIdx(Index_t iOuterIdx, Index_t iInnerIdx) const {
     assert(isNonZero(iOuterIdx, iInnerIdx) && "Error, j does not belong to NZ(i).");
     Index_t k = m_outerPtr(iOuterIdx);
-    while(m_innerIdx(k) != iInnerIdx) ++k;
+    while (m_innerIdx(k) != iInnerIdx) ++k;
     return k;
   }
 
@@ -287,9 +264,7 @@ class CCompressedSparsePattern {
    * \param[in] iDiagIdx - Diagonal index (row == col).
    * \return Absolute position of the diagonal entry.
    */
-  inline Index_t getDiagPtr(Index_t iDiagIdx) const {
-    return m_diagPtr(iDiagIdx);
-  }
+  inline Index_t getDiagPtr(Index_t iDiagIdx) const { return m_diagPtr(iDiagIdx); }
 
   /*!
    * \return Raw pointer to the outer pointer vector.
@@ -336,8 +311,7 @@ class CCompressedSparsePattern {
    */
   Index_t getMinInnerIdx() const {
     Index_t idx = std::numeric_limits<Index_t>::max();
-    for(Index_t k=0; k<m_innerIdx.size(); ++k)
-      idx = std::min(idx, m_innerIdx(k));
+    for (Index_t k = 0; k < m_innerIdx.size(); ++k) idx = std::min(idx, m_innerIdx(k));
     return idx;
   }
 
@@ -346,8 +320,7 @@ class CCompressedSparsePattern {
    */
   Index_t getMaxInnerIdx() const {
     Index_t idx = std::numeric_limits<Index_t>::min();
-    for(Index_t k=0; k<m_innerIdx.size(); ++k)
-      idx = std::max(idx, m_innerIdx(k));
+    for (Index_t k = 0; k < m_innerIdx.size(); ++k) idx = std::max(idx, m_innerIdx(k));
     return idx;
   }
 };
@@ -357,15 +330,13 @@ class CCompressedSparsePattern {
  *        that maps the two sparse entries referenced by an edge (ij and ji) to two
  *        non zero entries of a sparse pattern.
  */
-template<typename Index_t>
+template <typename Index_t>
 using CEdgeToNonZeroMap = C2DContainer<unsigned long, Index_t, StorageType::RowMajor, 64, DynamicSize, 2>;
 
-
 using CCompressedSparsePatternUL = CCompressedSparsePattern<unsigned long>;
 using CCompressedSparsePatternL = CCompressedSparsePattern<long>;
 using CEdgeToNonZeroMapUL = CEdgeToNonZeroMap<unsigned long>;
 
-
 /*!
  * \brief Build a sparse pattern from geometry information, of type FVM or FEM,
  *        for a given fill-level. At fill-level N, the immediate neighbors of the
@@ -379,19 +350,15 @@ using CEdgeToNonZeroMapUL = CEdgeToNonZeroMap<unsigned long>;
  * \param[in] fillLvl - Target degree of neighborhood (immediate neighbors always added).
  * \return Compressed-Storage-Row sparse pattern.
  */
-template<class Geometry_t, typename Index_t>
-CCompressedSparsePattern<Index_t> buildCSRPattern(Geometry_t& geometry,
-                                                  ConnectivityType type,
-                                                  Index_t fillLvl)
-{
+template <class Geometry_t, typename Index_t>
+CCompressedSparsePattern<Index_t> buildCSRPattern(Geometry_t& geometry, ConnectivityType type, Index_t fillLvl) {
   Index_t nPoint = geometry.GetnPoint();
 
-  std::vector<Index_t> outerPtr(nPoint+1);
+  std::vector<Index_t> outerPtr(nPoint + 1);
   std::vector<Index_t> innerIdx;
-  innerIdx.reserve(nPoint); // at least this much space is needed
+  innerIdx.reserve(nPoint);  // at least this much space is needed
 
-  for(Index_t iPoint = 0; iPoint < nPoint; ++iPoint)
-  {
+  for (Index_t iPoint = 0; iPoint < nPoint; ++iPoint) {
     /*--- Inner indices for iPoint start here. ---*/
     outerPtr[iPoint] = innerIdx.size();
 
@@ -404,34 +371,28 @@ CCompressedSparsePattern<Index_t> buildCSRPattern(Geometry_t& geometry,
     /*--- Neighbors added in previous level. ---*/
     std::set<Index_t> addedNeighbors(neighbors);
 
-    for(Index_t iLevel = 0; ; ++iLevel)
-    {
+    for (Index_t iLevel = 0;; ++iLevel) {
       /*--- New points added in this level. ---*/
       std::set<Index_t> newNeighbors;
 
       /*--- For each point previously added, add its level 0
        *    neighbors, not duplicating any existing neighbor. ---*/
-      for(auto jPoint : addedNeighbors)
-      {
-        if(type == ConnectivityType::FiniteVolume)
-        {
+      for (auto jPoint : addedNeighbors) {
+        if (type == ConnectivityType::FiniteVolume) {
           /*--- For FVM we know the neighbors of point j directly. ---*/
-          for(Index_t kPoint : geometry.nodes->GetPoints(jPoint))
-            if(neighbors.count(kPoint) == 0) // no duplication
+          for (Index_t kPoint : geometry.nodes->GetPoints(jPoint))
+            if (neighbors.count(kPoint) == 0)  // no duplication
               newNeighbors.insert(kPoint);
-        }
-        else // FiniteElement
+        } else  // FiniteElement
         {
           /*--- For FEM we need the nodes of all elements that contain point j. ---*/
-          for(auto iElem : geometry.nodes->GetElems(jPoint))
-          {
+          for (auto iElem : geometry.nodes->GetElems(jPoint)) {
             auto elem = geometry.elem[iElem];
 
-            for(unsigned short iNode = 0; iNode < elem->GetnNodes(); ++iNode)
-            {
+            for (unsigned short iNode = 0; iNode < elem->GetnNodes(); ++iNode) {
               Index_t kPoint = elem->GetNode(iNode);
 
-              if(neighbors.count(kPoint) == 0) // no duplication
+              if (neighbors.count(kPoint) == 0)  // no duplication
                 newNeighbors.insert(kPoint);
             }
           }
@@ -440,7 +401,7 @@ CCompressedSparsePattern<Index_t> buildCSRPattern(Geometry_t& geometry,
 
       neighbors.insert(newNeighbors.begin(), newNeighbors.end());
 
-      if(iLevel >= fillLvl) break;
+      if (iLevel >= fillLvl) break;
 
       /*--- For the next level we get the neighbours of the new points. ---*/
       addedNeighbors = newNeighbors;
@@ -455,7 +416,6 @@ CCompressedSparsePattern<Index_t> buildCSRPattern(Geometry_t& geometry,
   return CCompressedSparsePattern<Index_t>(outerPtr, innerIdx);
 }
 
-
 /*!
  * \brief Build a lookup table of the absolute positions of the non zero entries
  *        of a compressed sparse pattern, accessed when visiting the FVM edges
@@ -465,27 +425,24 @@ CCompressedSparsePattern<Index_t> buildCSRPattern(Geometry_t& geometry,
  * \param[in] pattern - Sparse pattern.
  * \return nEdge by 2 matrix.
  */
-template<class Geometry_t, typename Index_t>
+template <class Geometry_t, typename Index_t>
 CEdgeToNonZeroMap<Index_t> mapEdgesToSparsePattern(Geometry_t& geometry,
-                                                   const CCompressedSparsePattern<Index_t>& pattern)
-{
+                                                   const CCompressedSparsePattern<Index_t>& pattern) {
   assert(!pattern.empty());
 
-  CEdgeToNonZeroMap<Index_t> edgeMap(geometry.GetnEdge(),2);
+  CEdgeToNonZeroMap<Index_t> edgeMap(geometry.GetnEdge(), 2);
 
-  for(Index_t iEdge = 0; iEdge < geometry.GetnEdge(); ++iEdge)
-  {
-    Index_t iPoint = geometry.edges->GetNode(iEdge,0);
-    Index_t jPoint = geometry.edges->GetNode(iEdge,1);
+  for (Index_t iEdge = 0; iEdge < geometry.GetnEdge(); ++iEdge) {
+    Index_t iPoint = geometry.edges->GetNode(iEdge, 0);
+    Index_t jPoint = geometry.edges->GetNode(iEdge, 1);
 
-    edgeMap(iEdge,0) = pattern.quickFindInnerIdx(iPoint,jPoint);
-    edgeMap(iEdge,1) = pattern.quickFindInnerIdx(jPoint,iPoint);
+    edgeMap(iEdge, 0) = pattern.quickFindInnerIdx(iPoint, jPoint);
+    edgeMap(iEdge, 1) = pattern.quickFindInnerIdx(jPoint, iPoint);
   }
 
   return edgeMap;
 }
 
-
 /*!
  * \brief Create the natural coloring (equivalent to the normal sequential loop
  *        order) for a given number of inner indexes.
@@ -493,10 +450,8 @@ CEdgeToNonZeroMap<Index_t> mapEdgesToSparsePattern(Geometry_t& geometry,
  * \param[in] numInnerIndexes - Number of indexes that are to be colored.
  * \return Natural (sequential) coloring of the inner indices.
  */
-template<class T = CCompressedSparsePatternUL,
-         class Index_t = typename T::IndexType>
-T createNaturalColoring(Index_t numInnerIndexes)
-{
+template <class T = CCompressedSparsePatternUL, class Index_t = typename T::IndexType>
+T createNaturalColoring(Index_t numInnerIndexes) {
   /*--- One color. ---*/
   su2vector<Index_t> outerPtr(2);
   outerPtr(0) = 0;
@@ -504,12 +459,11 @@ T createNaturalColoring(Index_t numInnerIndexes)
 
   /*--- Containing all indexes in ascending order. ---*/
   su2vector<Index_t> innerIdx(numInnerIndexes);
-  std::iota(innerIdx.data(), innerIdx.data()+numInnerIndexes, 0);
+  std::iota(innerIdx.data(), innerIdx.data() + numInnerIndexes, 0);
 
   return T(std::move(outerPtr), std::move(innerIdx));
 }
 
-
 /*!
  * \brief Color contiguous groups of outer indices of a sparse pattern such that
  *        within each color, any two groups do not have inner indices in common.
@@ -530,12 +484,11 @@ T createNaturalColoring(Index_t numInnerIndexes)
  * \param[out] indexColor - Optional, vector with colors given to the outer indices.
  * \return Coloring in the same type of the input pattern.
  */
-template<typename Color_t = char, size_t MaxColors = 64, size_t MaxMB = 128, class T>
+template <typename Color_t = char, size_t MaxColors = 64, size_t MaxMB = 128, class T>
 T colorSparsePattern(const T& pattern, size_t groupSize = 1, bool balanceColors = false,
-                     std::vector<Color_t>* indexColor = nullptr)
-{
-  static_assert(std::is_integral<Color_t>::value,"");
-  static_assert(std::numeric_limits<Color_t>::max() >= MaxColors,"");
+                     std::vector<Color_t>* indexColor = nullptr) {
+  static_assert(std::is_integral<Color_t>::value, "");
+  static_assert(std::numeric_limits<Color_t>::max() >= MaxColors, "");
 
   using Index_t = typename T::IndexType;
 
@@ -543,171 +496,161 @@ T colorSparsePattern(const T& pattern, size_t groupSize = 1, bool balanceColors
   const Index_t nOuter = pattern.getOuterSize();
 
   /*--- Trivial case. ---*/
-  if(groupSize >= nOuter) return createNaturalColoring(nOuter);
+  if (groupSize >= nOuter) return createNaturalColoring(nOuter);
 
   const Index_t minIdx = pattern.getMinInnerIdx();
-  const Index_t nInner = pattern.getMaxInnerIdx()+1-minIdx;
+  const Index_t nInner = pattern.getMaxInnerIdx() + 1 - minIdx;
 
   /*--- Check the max memory condition (<< 23 is to count bits). ---*/
-  if(size_t(nInner) > (MaxMB << 23)) return T();
+  if (size_t(nInner) > (MaxMB << 23)) return T();
 
   /*--- Vector with the color given to each outer index. ---*/
   std::vector<Color_t> idxColor(nOuter);
 
   /*--- Start with one color, with no indices assigned. ---*/
-  std::vector<Index_t> colorSize(1,0);
+  std::vector<Index_t> colorSize(1, 0);
   Color_t nColor = 1;
 
   {
-  /*--- For each color keep track of the inner indices that are in it. ---*/
-  std::vector<std::vector<bool> > innerInColor;
-  innerInColor.emplace_back(nInner, false);
+    /*--- For each color keep track of the inner indices that are in it. ---*/
+    std::vector<std::vector<bool> > innerInColor;
+    innerInColor.emplace_back(nInner, false);
 
-  /*--- Order in which we look for space in the colors to insert a new group. ---*/
-  std::vector<Color_t> searchOrder(MaxColors);
+    /*--- Order in which we look for space in the colors to insert a new group. ---*/
+    std::vector<Color_t> searchOrder(MaxColors);
 
-  auto outerPtr = pattern.outerPtr();
-  auto innerIdx = pattern.innerIdx();
+    auto outerPtr = pattern.outerPtr();
+    auto innerIdx = pattern.innerIdx();
 
-  for(Index_t iOuter = 0; iOuter < nOuter; iOuter += grpSz)
-  {
-    Index_t grpEnd = std::min(iOuter+grpSz, nOuter);
+    for (Index_t iOuter = 0; iOuter < nOuter; iOuter += grpSz) {
+      Index_t grpEnd = std::min(iOuter + grpSz, nOuter);
 
-    searchOrder.resize(nColor);
-    std::iota(searchOrder.begin(), searchOrder.end(), 0);
+      searchOrder.resize(nColor);
+      std::iota(searchOrder.begin(), searchOrder.end(), 0);
 
-    /*--- Balance sizes by looking for space in smaller colors first. ---*/
-    if(balanceColors) {
-      std::sort(searchOrder.begin(), searchOrder.end(),
-        [&colorSize](Color_t a, Color_t b){return colorSize[a] < colorSize[b];});
-    }
+      /*--- Balance sizes by looking for space in smaller colors first. ---*/
+      if (balanceColors) {
+        std::sort(searchOrder.begin(), searchOrder.end(),
+                  [&colorSize](Color_t a, Color_t b) { return colorSize[a] < colorSize[b]; });
+      }
 
-    auto it = searchOrder.begin();
+      auto it = searchOrder.begin();
 
-    for(; it != searchOrder.end(); ++it)
-    {
-      bool free = true;
-      /*--- Traverse entire group as a large outer index. ---*/
-      for(Index_t k = outerPtr[iOuter]; k < outerPtr[grpEnd] && free; ++k)
-      {
-        free = !innerInColor[*it][innerIdx[k]-minIdx];
+      for (; it != searchOrder.end(); ++it) {
+        bool free = true;
+        /*--- Traverse entire group as a large outer index. ---*/
+        for (Index_t k = outerPtr[iOuter]; k < outerPtr[grpEnd] && free; ++k) {
+          free = !innerInColor[*it][innerIdx[k] - minIdx];
+        }
+        /*--- If none of the inner indices in the group appears in
+         *    this color yet, it is assigned to the group. ---*/
+        if (free) break;
       }
-      /*--- If none of the inner indices in the group appears in
-       *    this color yet, it is assigned to the group. ---*/
-      if(free) break;
-    }
 
-    Color_t color;
+      Color_t color;
+
+      if (it != searchOrder.end()) {
+        /*--- Found a free color. ---*/
+        color = *it;
+      } else {
+        /*--- No color was free, make space for a new one. ---*/
+        color = nColor++;
+        if (nColor == MaxColors) return T();
+        colorSize.push_back(0);
+        innerInColor.emplace_back(nInner, false);
+      }
 
-    if(it != searchOrder.end())
-    {
-      /*--- Found a free color. ---*/
-      color = *it;
-    }
-    else {
-      /*--- No color was free, make space for a new one. ---*/
-      color = nColor++;
-      if(nColor == MaxColors) return T();
-      colorSize.push_back(0);
-      innerInColor.emplace_back(nInner, false);
-    }
+      /*--- Assign color to group. ---*/
+      for (Index_t k = iOuter; k < grpEnd; ++k) idxColor[k] = color;
 
-    /*--- Assign color to group. ---*/
-    for(Index_t k = iOuter; k < grpEnd; ++k) idxColor[k] = color;
+      /*--- Mark the inner indices of the group as belonging to the color. ---*/
+      for (Index_t k = outerPtr[iOuter]; k < outerPtr[grpEnd]; ++k) {
+        innerInColor[color][innerIdx[k] - minIdx] = true;
+      }
 
-    /*--- Mark the inner indices of the group as belonging to the color. ---*/
-    for(Index_t k = outerPtr[iOuter]; k < outerPtr[grpEnd]; ++k)
-    {
-      innerInColor[color][innerIdx[k]-minIdx] = true;
+      /*--- Update count for the assigned color. ---*/
+      colorSize[color] += grpEnd - iOuter;
     }
-
-    /*--- Update count for the assigned color. ---*/
-    colorSize[color] += grpEnd - iOuter;
-  }
-  } // matrix of bools goes out of scope
-
+  }  // matrix of bools goes out of scope
 
   /*--- Compress the coloring information. ---*/
 
-  su2vector<Index_t> colorPtr(nColor+1); colorPtr(0) = 0;
+  su2vector<Index_t> colorPtr(nColor + 1);
+  colorPtr(0) = 0;
   su2vector<Index_t> outerIdx(nOuter);
 
   Index_t k = 0;
-  for(Color_t color = 0; color < nColor; ++color)
-  {
-    colorPtr(color+1) = colorPtr(color)+colorSize[color];
+  for (Color_t color = 0; color < nColor; ++color) {
+    colorPtr(color + 1) = colorPtr(color) + colorSize[color];
 
-    for(Index_t iOuter = 0; iOuter < nOuter; ++iOuter)
-      if(idxColor[iOuter] == color)
-        outerIdx(k++) = iOuter;
+    for (Index_t iOuter = 0; iOuter < nOuter; ++iOuter)
+      if (idxColor[iOuter] == color) outerIdx(k++) = iOuter;
   }
 
   /*--- Optional return of the direct color information. ---*/
-  if(indexColor) *indexColor = std::move(idxColor);
+  if (indexColor) *indexColor = std::move(idxColor);
 
   /*--- Move compressed coloring into result pattern instance. ---*/
   return T(std::move(colorPtr), std::move(outerIdx));
 }
 
-
 /*!
  * \brief A way to represent one grid color that allows range-for syntax.
  */
-template<typename T = unsigned long>
-struct GridColor
-{
-  static_assert(std::is_integral<T>::value,"");
+template <typename T = unsigned long>
+struct GridColor {
+  static_assert(std::is_integral<T>::value, "");
 
   const T size;
   T groupSize;
   const T* const indices;
 
-  GridColor(const T* idx = nullptr, T sz = 0, T grp = 0) :
-    size(sz), groupSize(grp), indices(idx) { }
+  GridColor(const T* idx = nullptr, T sz = 0, T grp = 0) : size(sz), groupSize(grp), indices(idx) {}
 
-  inline const T* begin() const {return indices;}
-  inline const T* end() const {return indices+size;}
+  inline const T* begin() const { return indices; }
+  inline const T* end() const { return indices + size; }
 };
 
-
 /*!
  * \brief A way to represent natural coloring {0,1,2,...,size-1} with zero
  * overhead (behaves like looping with an integer index, after optimization...).
  */
-template<typename T = unsigned long>
-struct DummyGridColor
-{
-  static_assert(std::is_integral<T>::value,"");
+template <typename T = unsigned long>
+struct DummyGridColor {
+  static_assert(std::is_integral<T>::value, "");
 
   T size;
   struct {
-    inline T operator[] (T i) const {return i;}
-  }
-  indices;
+    inline T operator[](T i) const { return i; }
+  } indices;
 
-  DummyGridColor(T sz = 0) : size(sz) { }
+  DummyGridColor(T sz = 0) : size(sz) {}
 
   struct IteratorLikeInt {
     T i;
     inline IteratorLikeInt(T pos = 0) : i(pos) {}
-    inline IteratorLikeInt& operator++ () {++i; return *this;}
-    inline IteratorLikeInt operator++ (int) {auto j=i++; return IteratorLikeInt(j);}
-    inline T operator* () const {return i;}
-    inline T operator-> () const {return i;}
-    inline bool operator==(const IteratorLikeInt& other) const {return i==other.i;}
-    inline bool operator!=(const IteratorLikeInt& other) const {return i!=other.i;}
+    inline IteratorLikeInt& operator++() {
+      ++i;
+      return *this;
+    }
+    inline IteratorLikeInt operator++(int) {
+      auto j = i++;
+      return IteratorLikeInt(j);
+    }
+    inline T operator*() const { return i; }
+    inline T operator->() const { return i; }
+    inline bool operator==(const IteratorLikeInt& other) const { return i == other.i; }
+    inline bool operator!=(const IteratorLikeInt& other) const { return i != other.i; }
   };
-  inline IteratorLikeInt begin() const {return IteratorLikeInt(0);}
-  inline IteratorLikeInt end() const {return IteratorLikeInt(size);}
+  inline IteratorLikeInt begin() const { return IteratorLikeInt(0); }
+  inline IteratorLikeInt end() const { return IteratorLikeInt(size); }
 };
 
-
 /*!
  * \brief Computes the efficiency of a grid coloring for given number of threads and chunk size.
  */
-template<class SparsePattern>
-su2double coloringEfficiency(const SparsePattern& coloring, int numThreads, int chunkSize)
-{
+template <class SparsePattern>
+su2double coloringEfficiency(const SparsePattern& coloring, int numThreads, int chunkSize) {
   using Index_t = typename SparsePattern::IndexType;
 
   /*--- Ideally compute time is proportional to total work over number of threads. ---*/
@@ -715,10 +658,10 @@ su2double coloringEfficiency(const SparsePattern& coloring, int numThreads, int
 
   /*--- In practice the total work is quantized first by colors and then by chunks. ---*/
   Index_t real = 0;
-  for(Index_t color = 0; color < coloring.getOuterSize(); ++color)
+  for (Index_t color = 0; color < coloring.getOuterSize(); ++color)
     real += chunkSize * roundUpDiv(roundUpDiv(coloring.getNumNonZeros(color), chunkSize), numThreads);
 
   return ideal / real;
 }
 
-/// @}
\ No newline at end of file
+/// @}
diff --git a/Common/include/toolboxes/ndflattener.hpp b/Common/include/toolboxes/ndflattener.hpp
index d6c3f5c28e4..6e9a616a0e2 100644
--- a/Common/include/toolboxes/ndflattener.hpp
+++ b/Common/include/toolboxes/ndflattener.hpp
@@ -212,8 +212,9 @@ class NdFlattener;
  *  Introducing this was necessary because MPICH's Allgatherv behaved unexpectedly if there
  *  is only one MPI rank (seemingly ignoring displs[0] != 0).
  */
-static inline void SU2_MPI_Allgatherv_safe(const void* sendbuf, int sendcount, SU2_MPI::Datatype sendtype, void* recvbuf,
-                              const int* recvcounts, const int* displs, SU2_MPI::Datatype recvtype, SU2_MPI::Comm comm) {
+static inline void SU2_MPI_Allgatherv_safe(const void* sendbuf, int sendcount, SU2_MPI::Datatype sendtype,
+                                           void* recvbuf, const int* recvcounts, const int* displs,
+                                           SU2_MPI::Datatype recvtype, SU2_MPI::Comm comm) {
   if (SU2_MPI::GetSize() == 1) {
     SU2_MPI::CopyData(sendbuf, recvbuf, sendcount, sendtype, displs[0]);
   } else {
@@ -242,8 +243,7 @@ struct Nd_MPI_Environment {
   const int rank;
   const int size;
 
-  Nd_MPI_Environment(MPI_Datatype_t mpi_data = MPI_DOUBLE,
-                     MPI_Datatype_t mpi_index = MPI_UNSIGNED_LONG,
+  Nd_MPI_Environment(MPI_Datatype_t mpi_data = MPI_DOUBLE, MPI_Datatype_t mpi_index = MPI_UNSIGNED_LONG,
                      MPI_Communicator_t comm = SU2_MPI::GetComm(),
                      MPI_Allgather_t MPI_Allgather_fun = &(SU2_MPI::Allgather),
                      MPI_Allgatherv_t MPI_Allgatherv_fun = &(SU2_MPI_Allgatherv_safe))
@@ -311,19 +311,15 @@ class IndexAccumulator : public IndexAccumulator_Base<N_, Nd_t_, Check> {
 
   /*! The Base of NdFlattener<K> is NdFlattener<K-1>, but do also preserve constness.
    */
-  using Nd_Base_t = su2conditional_t<
-    std::is_const<Nd_t>::value,
-    const typename Nd_t::Base,
-    typename Nd_t::Base
-  >;
+  using Nd_Base_t = su2conditional_t<std::is_const<Nd_t>::value, const typename Nd_t::Base, typename Nd_t::Base>;
   /*! Return type of operator[]. */
   using LookupType = IndexAccumulator<N - 1, Nd_Base_t>;
   /*! Return type of operator[] const. */
   using LookupType_const = IndexAccumulator<N - 1, const typename Nd_t::Base>;
+  using Base::CheckBound;
   using Base::nd;
   using Base::offset;
   using Base::size;
-  using Base::CheckBound;
 
   /*! \brief Read one more index, checking whether it is in the range dictated by the NdFlattener and
    * previous indices. Non-const version.
@@ -359,16 +355,12 @@ class IndexAccumulator<1, Nd_t_, Check> : public IndexAccumulator_Base<1, Nd_t_,
   /*! Return type of operator[].
    * \details Data type of NdFlattener, but do also preserve constness.
    */
-  using LookupType = su2conditional_t<
-    std::is_const<Nd_t>::value,
-    const typename Nd_t::Data_t,
-    typename Nd_t::Data_t
-  >;
+  using LookupType = su2conditional_t<std::is_const<Nd_t>::value, const typename Nd_t::Data_t, typename Nd_t::Data_t>;
   using LookupType_const = const typename Nd_t::Data_t;
+  using Base::CheckBound;
   using Base::nd;
   using Base::offset;
   using Base::size;
-  using Base::CheckBound;
 
   /*! \brief Return (possibly const) reference to the corresponding data element, checking if the index is in its range.
    * Non-const version.
@@ -672,7 +664,7 @@ class NdFlattener : public NdFlattener<K_ - 1, Data_t_, Index_t_> {
   void set_g(Nd_MPI_Environment const& mpi_env, su2matrix<Index_t> const& Nodes_all,
              CurrentLayer const& local_version) {
     std::vector<int> Nodes_all_K_as_int(mpi_env.size);
-    std::vector<int> Nodes_all_k_cumulated( mpi_env.size + 1);
+    std::vector<int> Nodes_all_k_cumulated(mpi_env.size + 1);
     //< [r] is the number of nodes in the current layer, summed over all processes with rank below r, **plus one**.
     // Used as displacements in Allgatherv, as we do not want to transfer the initial zeros, but we want to transfer the
     // last element of indices, which is the local nNodes of the layer below. Note that MPI needs indices of type 'int'.
diff --git a/Common/include/toolboxes/printing_toolbox.hpp b/Common/include/toolboxes/printing_toolbox.hpp
index 7461f0465de..58c66ad4fd5 100644
--- a/Common/include/toolboxes/printing_toolbox.hpp
+++ b/Common/include/toolboxes/printing_toolbox.hpp
@@ -68,15 +68,11 @@ namespace PrintingToolbox {
  *
  * \author T. Albring
  */
-class CTablePrinter{
-public:
-  CTablePrinter(std::ostream * output, const std::string & separator = "|");
+class CTablePrinter {
+ public:
+  CTablePrinter(std::ostream* output, const std::string& separator = "|");
 
-  enum alignment {
-    CENTER,
-    LEFT,
-    RIGHT
-  };
+  enum alignment { CENTER, LEFT, RIGHT };
 
   /*!
    * \brief Get number of columns of the table
@@ -94,13 +90,13 @@ class CTablePrinter{
    * \brief Set the separator between columns (outer decoration)
    * \param[in] separator - The separation character.
    */
-  void SetSeparator(const std::string & separator);
+  void SetSeparator(const std::string& separator);
 
   /*!
    * \brief Set the separator between columns (inner decoration)
    * \param[in] separator - The separation character.
    */
-  void SetInnerSeparator(const std::string & inner_separator);
+  void SetInnerSeparator(const std::string& inner_separator);
 
   /*!
    * \brief Set the alignment of the table entries (CENTER only works for the header at the moment).
@@ -120,13 +116,12 @@ class CTablePrinter{
    */
   void SetPrintHeaderTopLine(bool print);
 
-
   /*!
    * \brief Add a column to the table by specifiying the header name and the width.
    * \param[in] header_name - The name printed in the header.
    * \param[in] column_width - The width of the column.
    */
-  void AddColumn(const std::string & header_name, int column_width);
+  void AddColumn(const std::string& header_name, int column_width);
 
   /*!
    * \brief Print the header.
@@ -143,160 +138,152 @@ class CTablePrinter{
    */
   void SetPrecision(int precision);
 
-  template<typename T> CTablePrinter& operator<<(T input){
-
+  template <typename T>
+  CTablePrinter& operator<<(T input) {
     int indent = 0;
 
     /* --- Set the left separator --- */
-    if (j_ == 0)
-      *out_stream_ << separator_;
+    if (j_ == 0) *out_stream_ << separator_;
 
     /* --- Determine and set the current alignment in the stream --- */
-    if(align_ == LEFT)
+    if (align_ == LEFT)
       *out_stream_ << std::left;
     else if (align_ == RIGHT || align_ == CENTER)
       *out_stream_ << std::right;
 
     /*--- Print the current column value to the stream --- */
-    *out_stream_ << std::setw(column_widths_.at(j_) - indent)
-                 << std::setprecision(precision_) << input;
+    *out_stream_ << std::setw(column_widths_.at(j_) - indent) << std::setprecision(precision_) << input;
 
     /*--- Reset the column counter and if it is the last column,
      * add also a line break ---*/
-    if (j_ == GetNumColumns()-1){
-      *out_stream_ << std::setw(indent+1+(int)separator_.size()) << separator_ + "\n";
+    if (j_ == GetNumColumns() - 1) {
+      *out_stream_ << std::setw(indent + 1 + (int)separator_.size()) << separator_ + "\n";
       i_ = i_ + 1;
       j_ = 0;
     } else {
-      *out_stream_ << std::setw(indent+(int)inner_separator_.size()) << inner_separator_;
+      *out_stream_ << std::setw(indent + (int)inner_separator_.size()) << inner_separator_;
       j_ = j_ + 1;
     }
 
     return *this;
   }
 
-private:
-
+ private:
   /*!
    * \brief Print a horizontal line.
    */
   void PrintHorizontalLine();
 
-  std::ostream * out_stream_;               /*< \brief The output stream. */
+  std::ostream* out_stream_;                /*< \brief The output stream. */
   std::vector<std::string> column_headers_; /*< \brief Vector of column header names. */
   std::vector<int> column_widths_;          /*< \brief Vector of column widths. */
   std::string separator_;                   /*< \brief Column separator char. */
   std::string inner_separator_;             /*< \brief Inner column separator char. */
 
-  int precision_;                           /*< \brief Floating point precision */
+  int precision_; /*< \brief Floating point precision */
 
   int i_; /*< \brief Index of the current row. */
   int j_; /*< \brief Index of the current column. */
 
-  int table_width_;  /*< \brief The total width of the table. */
-  int align_;        /*< \brief The current alignment. */
-  bool print_header_top_line_,  /*< \brief Printing the header top line. */
-  print_header_bottom_line_;   /*< \brief Printing the header bottom line. */
+  int table_width_;              /*< \brief The total width of the table. */
+  int align_;                    /*< \brief The current alignment. */
+  bool print_header_top_line_,   /*< \brief Printing the header top line. */
+      print_header_bottom_line_; /*< \brief Printing the header bottom line. */
 };
 
-
-
-inline void PrintScreenFixed(std::ostream &stream, su2double val, unsigned short field_width) {
-  stream.precision(6); stream.setf(std::ios::fixed, std::ios::floatfield); stream.width(field_width);
+inline void PrintScreenFixed(std::ostream& stream, su2double val, unsigned short field_width) {
+  stream.precision(6);
+  stream.setf(std::ios::fixed, std::ios::floatfield);
+  stream.width(field_width);
   stream << std::right << val;
   stream.unsetf(std::ios::fixed);
 }
 
-inline void PrintScreenScientific(std::ostream &stream, su2double val, unsigned short field_width) {
-  stream.precision(4); stream.setf(std::ios::scientific, std::ios::floatfield); stream.width(field_width);
+inline void PrintScreenScientific(std::ostream& stream, su2double val, unsigned short field_width) {
+  stream.precision(4);
+  stream.setf(std::ios::scientific, std::ios::floatfield);
+  stream.width(field_width);
   stream << std::right << val;
   stream.unsetf(std::ios::scientific);
 }
 
-inline void PrintScreenInteger(std::ostream &stream, unsigned long val, unsigned short field_width){
+inline void PrintScreenInteger(std::ostream& stream, unsigned long val, unsigned short field_width) {
   stream.width(field_width);
   stream << std::right << val;
 }
 
-inline void PrintScreenPercent(std::ostream &stream, su2double val, unsigned short field_width){
-  stream.precision(2); stream.setf(std::ios::fixed, std::ios::floatfield); stream.width(field_width-1);
+inline void PrintScreenPercent(std::ostream& stream, su2double val, unsigned short field_width) {
+  stream.precision(2);
+  stream.setf(std::ios::fixed, std::ios::floatfield);
+  stream.width(field_width - 1);
   stream << std::right << val << "%";
   stream.unsetf(std::ios::fixed);
 }
 
-
-inline std::vector<std::string> split(const std::string& s, char delimiter)
-{
+inline std::vector<std::string> split(const std::string& s, char delimiter) {
   std::vector<std::string> tokens;
   std::string token;
   std::istringstream tokenStream(s);
-  while (std::getline(tokenStream, token, delimiter))
-  {
+  while (std::getline(tokenStream, token, delimiter)) {
     tokens.push_back(token);
   }
   return tokens;
 }
 
-inline int stoi(const std::string s){
+inline int stoi(const std::string s) {
   std::istringstream ss(s);
   int number;
   ss >> number;
   return number;
 }
 
-inline su2double stod(const std::string s){
+inline su2double stod(const std::string s) {
   std::istringstream ss(s);
   su2double number;
   ss >> number;
   return number;
 }
 
-inline std::string to_string(const su2double number){
-
+inline std::string to_string(const su2double number) {
   std::stringstream ss;
 
   ss << number;
 
   return ss.str();
-
 }
 
 const static char* ws = " \t\n\r\f\v";
 
 // trim from end of string (right)
-inline std::string& rtrim(std::string& s, const char* t = ws){
+inline std::string& rtrim(std::string& s, const char* t = ws) {
   s.erase(s.find_last_not_of(t) + 1);
   return s;
 }
 
 // trim from beginning of string (left)
-inline std::string& ltrim(std::string& s, const char* t = ws){
+inline std::string& ltrim(std::string& s, const char* t = ws) {
   s.erase(0, s.find_first_not_of(t));
   return s;
 }
 
 // trim from both ends of string (right then left)
-inline std::string& trim(std::string& s, const char* t = ws){
-  return ltrim(rtrim(s, t), t);
-}
+inline std::string& trim(std::string& s, const char* t = ws) { return ltrim(rtrim(s, t), t); }
 
 /*!
  * \brief utility function for converting strings to uppercase
  * \param[in,out] str - string we want to convert
  */
-inline void StringToUpperCase(std::string & str) {
-  std::transform(str.begin(), str.end(), str.begin(), ::toupper);
-}
+inline void StringToUpperCase(std::string& str) { std::transform(str.begin(), str.end(), str.begin(), ::toupper); }
 
 /*!
  * \brief utility function for converting strings to uppercase
  * \param[in] str - string we want a copy of converted to uppercase
  * \return a copy of str in uppercase
  */
-inline std::string StringToUpperCase(const std::string & str) {
+inline std::string StringToUpperCase(const std::string& str) {
   std::string upp_str(str);
   std::transform(upp_str.begin(), upp_str.end(), upp_str.begin(), ::toupper);
   return upp_str;
 }
 
-}
+}  // namespace PrintingToolbox
diff --git a/Common/include/wall_model.hpp b/Common/include/wall_model.hpp
index 6369c970b11..b80f9dfcedd 100644
--- a/Common/include/wall_model.hpp
+++ b/Common/include/wall_model.hpp
@@ -45,14 +45,12 @@ class CFluidModel;
  * \version 7.5.1 "Blackbird"
  */
 class CWallModel {
-
-public:
-
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] config - Definition of the particular problem.
    */
-  CWallModel(CConfig *config);
+  CWallModel(CConfig* config);
 
   /*!
    * \brief Destructor of the class.
@@ -77,27 +75,20 @@ class CWallModel {
    * \param[out] OverCvWall             - Thermal conductivity divided by Cv at the wall,
                                           to be computed.
    */
-  virtual void WallShearStressAndHeatFlux(const su2double tExchange,
-                                          const su2double velExchange,
-                                          const su2double muExchange,
-                                          const su2double pExchange,
-                                          const su2double Wall_HeatFlux,
-                                          const bool      HeatFlux_Prescribed,
-                                          const su2double TWall,
-                                          const bool      Temperature_Prescribed,
-                                          CFluidModel     *FluidModel,
-                                          su2double       &tauWall,
-                                          su2double       &qWall,
-                                          su2double       &ViscosityWall,
-                                          su2double       &kOverCvWall);
-protected:
-
+  virtual void WallShearStressAndHeatFlux(const su2double tExchange, const su2double velExchange,
+                                          const su2double muExchange, const su2double pExchange,
+                                          const su2double Wall_HeatFlux, const bool HeatFlux_Prescribed,
+                                          const su2double TWall, const bool Temperature_Prescribed,
+                                          CFluidModel* FluidModel, su2double& tauWall, su2double& qWall,
+                                          su2double& ViscosityWall, su2double& kOverCvWall);
+
+ protected:
   su2double h_wm;    /*!< \brief The thickness of the wall model. This is also basically the exchange location */
   su2double Pr_lam;  /*!< \brief Laminar Prandtl number. */
   su2double Pr_turb; /*!< \brief Turbulent Prandtl number. */
   su2double karman;  /*!< \brief von Karman constant. */
 
-private:
+ private:
   /*!
    * \brief Default constructor of the class, disabled.
    */
@@ -105,17 +96,14 @@ class CWallModel {
 };
 
 class CWallModel1DEQ : public CWallModel {
-
-public:
-
+ public:
   /*!
    * \brief Constructor of the class.
    * \param[in] config     - Definition of the particular problem.
    * \param[in] Marker_Tag - String, which identifies the boundary marker for
                              which the wall model is used.
    */
-  CWallModel1DEQ(CConfig      *config,
-                 const string &Marker_Tag);
+  CWallModel1DEQ(CConfig* config, const string& Marker_Tag);
 
   /*!
    * \brief Function, which computes the wall shear stress and heat flux
@@ -135,27 +123,18 @@ class CWallModel1DEQ : public CWallModel {
    * \param[out] kOverCvWall             - Thermal conductivity divided by Cv at the wall,
                                           to be computed.
    */
-  void WallShearStressAndHeatFlux(const su2double tExchange,
-                                  const su2double velExchange,
-                                  const su2double muExchange,
-                                  const su2double pExchange,
-                                  const su2double Wall_HeatFlux,
-                                  const bool      HeatFlux_Prescribed,
-                                  const su2double Wall_Temperature,
-                                  const bool      Temperature_Prescribed,
-                                  CFluidModel     *FluidModel,
-                                  su2double       &tauWall,
-                                  su2double       &qWall,
-                                  su2double       &ViscosityWall,
-                                  su2double       &kOverCvWall) override;
-
-private:
-
-  su2double expansionRatio;   /*!< \brief  Stretching factor used for the wall model grid. */
-  int       numPoints;        /*!< \brief  Number of points used in the wall model grid. */
-
-  vector<su2double> y_cv;    /*!< \brief  The coordinates in normal direction of the wall model grid (control volumes). */
-  vector<su2double> y_fa;    /*!< \brief  The coordinates in normal direction of the wall model grid (faces of CV). */
+  void WallShearStressAndHeatFlux(const su2double tExchange, const su2double velExchange, const su2double muExchange,
+                                  const su2double pExchange, const su2double Wall_HeatFlux,
+                                  const bool HeatFlux_Prescribed, const su2double Wall_Temperature,
+                                  const bool Temperature_Prescribed, CFluidModel* FluidModel, su2double& tauWall,
+                                  su2double& qWall, su2double& ViscosityWall, su2double& kOverCvWall) override;
+
+ private:
+  su2double expansionRatio; /*!< \brief  Stretching factor used for the wall model grid. */
+  int numPoints;            /*!< \brief  Number of points used in the wall model grid. */
+
+  vector<su2double> y_cv; /*!< \brief  The coordinates in normal direction of the wall model grid (control volumes). */
+  vector<su2double> y_fa; /*!< \brief  The coordinates in normal direction of the wall model grid (faces of CV). */
 
   /*!
    * \brief Default constructor of the class, disabled.
@@ -164,17 +143,14 @@ class CWallModel1DEQ : public CWallModel {
 };
 
 class CWallModelLogLaw : public CWallModel {
-
-public:
-
+ public:
   /*!
    * \brief Constructor of the class, which initializes the object.
    * \param[in] config     - Definition of the particular problem.
    * \param[in] Marker_Tag - String, which identifies the boundary marker for
                              which the wall model is used.
    */
-  CWallModelLogLaw(CConfig      *config,
-                   const string &Marker_Tag);
+  CWallModelLogLaw(CConfig* config, const string& Marker_Tag);
 
   /*!
    * \brief Function, which computes the wall shear stress and heat flux
@@ -194,23 +170,14 @@ class CWallModelLogLaw : public CWallModel {
    * \param[out] kOverCvWall             - Thermal conductivity divided by Cv at the wall,
    to be computed.
    */
-  void WallShearStressAndHeatFlux(const su2double tExchange,
-                                  const su2double velExchange,
-                                  const su2double muExchange,
-                                  const su2double pExchange,
-                                  const su2double Wall_HeatFlux,
-                                  const bool      HeatFlux_Prescribed,
-                                  const su2double Wall_Temperature,
-                                  const bool      Temperature_Prescribed,
-                                  CFluidModel     *FluidModel,
-                                  su2double       &tauWall,
-                                  su2double       &qWall,
-                                  su2double       &ViscosityWall,
-                                  su2double       &kOverCvWall) override;
-
-private:
-
-  su2double C;  /*!< \brief Constant to match the Reichardt BL profile. */
+  void WallShearStressAndHeatFlux(const su2double tExchange, const su2double velExchange, const su2double muExchange,
+                                  const su2double pExchange, const su2double Wall_HeatFlux,
+                                  const bool HeatFlux_Prescribed, const su2double Wall_Temperature,
+                                  const bool Temperature_Prescribed, CFluidModel* FluidModel, su2double& tauWall,
+                                  su2double& qWall, su2double& ViscosityWall, su2double& kOverCvWall) override;
+
+ private:
+  su2double C; /*!< \brief Constant to match the Reichardt BL profile. */
 
   /*!
    * \brief Default constructor of the class, disabled.
diff --git a/Common/lib/Makefile.am b/Common/lib/Makefile.am
index 4323382ceea..1ead93f2ca7 100644
--- a/Common/lib/Makefile.am
+++ b/Common/lib/Makefile.am
@@ -166,4 +166,3 @@ libSU2_AD_a_SOURCES = $(lib_sources)
 libSU2_AD_a_CXXFLAGS = @REVERSE_CXX@ ${lib_cxxflags}
 libSU2_AD_a_LIBADD =  ${lib_ldadd}
 endif
-
diff --git a/Common/src/adt/CADTBaseClass.cpp b/Common/src/adt/CADTBaseClass.cpp
index 6be2c3f6769..0a063275541 100644
--- a/Common/src/adt/CADTBaseClass.cpp
+++ b/Common/src/adt/CADTBaseClass.cpp
@@ -31,32 +31,32 @@
 
 #include <algorithm>
 
-void CADTBaseClass::BuildADT(unsigned short  nDim,
-                             unsigned long   nPoints,
-                             const su2double *coor) {
-
+void CADTBaseClass::BuildADT(unsigned short nDim, unsigned long nPoints, const su2double* coor) {
   /*---  Determine the number of leaves. It can be proved that nLeaves equals
          nPoints-1 for an optimally balanced tree. Take the exceptional case of
          nPoints == 1 into account and return if the tree is empty. ---*/
   nDimADT = nDim;
   isEmpty = false;
-  nLeaves = nPoints -1;
-  if(nPoints <= 1) ++nLeaves;
-  if(nLeaves == 0) {isEmpty = true; return;}
+  nLeaves = nPoints - 1;
+  if (nPoints <= 1) ++nLeaves;
+  if (nLeaves == 0) {
+    isEmpty = true;
+    return;
+  }
 
   /*--- Allocate the memory for the leaves of the ADT and the minimum and
         maximum coordinates of the leaves. Note that these coordinates are
         stored in one vector, rather than that memory is allocated for the
         individual leaves. ---*/
   leaves.resize(nLeaves);
-  coorMinLeaves.resize(nDim*nLeaves);
-  coorMaxLeaves.resize(nDim*nLeaves);
+  coorMinLeaves.resize(nDim * nLeaves);
+  coorMaxLeaves.resize(nDim * nLeaves);
 
   /*--- Define the vectors, which control the subdivision of the leaves. ---*/
-  unsigned long nn = (nPoints+1)/2;
+  unsigned long nn = (nPoints + 1) / 2;
   vector<unsigned long> pointIDs(nPoints), pointIDsNew(nPoints);
-  vector<unsigned long> nPointIDs(nn+1),   nPointIDsNew(nn+1);
-  vector<unsigned long> curLeaf(nn),       curLeafNew(nn);
+  vector<unsigned long> nPointIDs(nn + 1), nPointIDsNew(nn + 1);
+  vector<unsigned long> curLeaf(nn), curLeafNew(nn);
 
   /*--------------------------------------------------------------------------*/
   /*---                 Building of the actual ADT                         ---*/
@@ -65,47 +65,45 @@ void CADTBaseClass::BuildADT(unsigned short  nDim,
   /*--- Initialize the arrays pointIDs, nPointIDs and curLeaf such that all
         points belong to the root leaf. Also set the counters nLeavesToDivide
         and nLeavesTot.  ---*/
-  nPointIDs[0] = 0; nPointIDs[1] = nPoints;
+  nPointIDs[0] = 0;
+  nPointIDs[1] = nPoints;
   curLeaf[0] = 0;
 
-  for(unsigned long i=0; i<nPoints; ++i) pointIDs[i] = i;
+  for (unsigned long i = 0; i < nPoints; ++i) pointIDs[i] = i;
 
   unsigned long nLeavesToDivide = 1, nLeavesTot = 1;
 
   /*--- Loop to subdivide the leaves. The division is such that the ADT is
         optimally balanced.  ---*/
-  for(;;) {
-
+  for (;;) {
     /* Criterion to exit the loop. */
-    if(nLeavesToDivide == 0) break;
+    if (nLeavesToDivide == 0) break;
 
     /* Initializations for the next round of subdivisions. */
     unsigned long nLeavesToDivideNew = 0;
     nPointIDsNew[0] = 0;
 
     /*--- Loop over the current number of leaves to be divided. ---*/
-    for(unsigned long i=0; i<nLeavesToDivide; ++i) {
-
+    for (unsigned long i = 0; i < nLeavesToDivide; ++i) {
       /* Store the number of points present in the leaf in nn and the
          current leaf number in mm. */
-      nn = nPointIDs[i+1] - nPointIDs[i];
+      nn = nPointIDs[i + 1] - nPointIDs[i];
       unsigned long mm = curLeaf[i];
 
       /*--- Set the pointers for the coordinates of the leaf to the correct
             locations in the vectors coorMinLeaves and coorMaxLeaves and
             determine the bounding box coordinates of this leaf. ---*/
-      leaves[mm].xMin = coorMinLeaves.data() + nDim*mm;
-      leaves[mm].xMax = coorMaxLeaves.data() + nDim*mm;
-
-      unsigned long ll = nDim*pointIDs[nPointIDs[i]];
-      for(unsigned short l=0; l<nDim; ++l)
-        leaves[mm].xMin[l] = leaves[mm].xMax[l] = coor[ll+l];
-
-      for(unsigned long j=(nPointIDs[i]+1); j<nPointIDs[i+1]; ++j) {
-        ll = nDim*pointIDs[j];
-        for(unsigned short l=0; l<nDim; ++l) {
-          leaves[mm].xMin[l] = min(leaves[mm].xMin[l], coor[ll+l]);
-          leaves[mm].xMax[l] = max(leaves[mm].xMax[l], coor[ll+l]);
+      leaves[mm].xMin = coorMinLeaves.data() + nDim * mm;
+      leaves[mm].xMax = coorMaxLeaves.data() + nDim * mm;
+
+      unsigned long ll = nDim * pointIDs[nPointIDs[i]];
+      for (unsigned short l = 0; l < nDim; ++l) leaves[mm].xMin[l] = leaves[mm].xMax[l] = coor[ll + l];
+
+      for (unsigned long j = (nPointIDs[i] + 1); j < nPointIDs[i + 1]; ++j) {
+        ll = nDim * pointIDs[j];
+        for (unsigned short l = 0; l < nDim; ++l) {
+          leaves[mm].xMin[l] = min(leaves[mm].xMin[l], coor[ll + l]);
+          leaves[mm].xMax[l] = max(leaves[mm].xMax[l], coor[ll + l]);
         }
       }
 
@@ -113,54 +111,53 @@ void CADTBaseClass::BuildADT(unsigned short  nDim,
             in such a way that isotropy is reached as quickly as possible.
             Hence the split direction is the direction of the largest dimension
             of the leaf. ---*/
-      unsigned short splitDir= 0;
+      unsigned short splitDir = 0;
       su2double distMax = -1.0;
-      for(unsigned short l=0; l<nDim; ++l) {
+      for (unsigned short l = 0; l < nDim; ++l) {
         const su2double dist = leaves[mm].xMax[l] - leaves[mm].xMin[l];
-        if(dist > distMax) {distMax = dist; splitDir = l;}
+        if (dist > distMax) {
+          distMax = dist;
+          splitDir = l;
+        }
       }
 
       /* Sort the points of the current leaf in increasing order. The sorting
          is based on the coordinate in the split direction, for which the
          functor CADTComparePointClass is used. */
-      sort(pointIDs.data() + nPointIDs[i], pointIDs.data() + nPointIDs[i+1],
+      sort(pointIDs.data() + nPointIDs[i], pointIDs.data() + nPointIDs[i + 1],
            CADTComparePointClass(coor, splitDir, nDim));
 
       /* Determine the index of the node, which is approximately central
          in this leave. */
-      leaves[mm].centralNodeID = pointIDs[nPointIDs[i] + nn/2];
+      leaves[mm].centralNodeID = pointIDs[nPointIDs[i] + nn / 2];
 
       /*--- Determine the situation of the leaf. It is either a terminal leaf
             or a leaf that must be subdivided. ---*/
-      if(nn <= 2) {
-
+      if (nn <= 2) {
         /* Terminal leaf. Store the ID's of the points as children and
            indicate that the children are terminal. */
         leaves[mm].children[0] = pointIDs[nPointIDs[i]];
-        leaves[mm].children[1] = pointIDs[nPointIDs[i+1]-1];
+        leaves[mm].children[1] = pointIDs[nPointIDs[i + 1] - 1];
 
         leaves[mm].childrenAreTerminal[0] = true;
         leaves[mm].childrenAreTerminal[1] = true;
-      }
-      else {
-
+      } else {
         /* The leaf must be divided. Determine the number of points in the
            left leaf. This number is at least 2. The actual number stored in kk
            is this number plus an offset. Also initialize the counter nfl, which
            is used to store the bounding boxes in the arrays for the new round. */
-        unsigned long kk  = (nn+1)/2 + nPointIDs[i];
+        unsigned long kk = (nn + 1) / 2 + nPointIDs[i];
         unsigned long nfl = nPointIDsNew[nLeavesToDivideNew];
 
         /* Copy the ID's of the left points into pointIDsNew. Also update the
            corresponding entry in nPointIDsNew. */
-        for(unsigned long k=nPointIDs[i]; k<kk; ++k)
-          pointIDsNew[nfl++] = pointIDs[k];
+        for (unsigned long k = nPointIDs[i]; k < kk; ++k) pointIDsNew[nfl++] = pointIDs[k];
 
-        nPointIDsNew[nLeavesToDivideNew+1] = nfl;
+        nPointIDsNew[nLeavesToDivideNew + 1] = nfl;
 
         /* Store the leaf info in the tree and in the leafs for next round and
            update nLeavesToDivideNew and nLeavesTot. */
-        leaves[mm].children[0]            = nLeavesTot;
+        leaves[mm].children[0] = nLeavesTot;
         leaves[mm].childrenAreTerminal[0] = false;
 
         curLeafNew[nLeavesToDivideNew] = nLeavesTot;
@@ -171,29 +168,25 @@ void CADTBaseClass::BuildADT(unsigned short  nDim,
               in it, i.e. if the original leaf has more than three points.
               If the new leaf only has one point in it, it is not created.
               Instead, the point is stored in the current leaf. ---*/
-        if(nn == 3)
-        {
+        if (nn == 3) {
           /* Only three points present in the current leaf. The right leaf is
              not created and the last point is stored as the second child of
              the current leaf. */
-          leaves[mm].children[1]            = pointIDs[nPointIDs[i+1]-1];
+          leaves[mm].children[1] = pointIDs[nPointIDs[i + 1] - 1];
           leaves[mm].childrenAreTerminal[1] = true;
-        }
-        else {
-
+        } else {
           /* More than 3 points are present and thus the right leaf is created.
              Copy the ID's from pointIDs into pointIDsNew and update the
              counters for the new round. */
           unsigned long nfr = nPointIDsNew[nLeavesToDivideNew];
 
-          for(unsigned long k=kk; k<nPointIDs[i+1]; ++k)
-            pointIDsNew[nfr++] = pointIDs[k];
+          for (unsigned long k = kk; k < nPointIDs[i + 1]; ++k) pointIDsNew[nfr++] = pointIDs[k];
 
-          nPointIDsNew[nLeavesToDivideNew+1] = nfr;
+          nPointIDsNew[nLeavesToDivideNew + 1] = nfr;
 
           /* Store the leaf info in the tree and in the leaves for next round and
              update nLeavesToDivideNew and nLeavesTot. */
-          leaves[mm].children[1]            = nLeavesTot;
+          leaves[mm].children[1] = nLeavesTot;
           leaves[mm].childrenAreTerminal[1] = false;
 
           curLeafNew[nLeavesToDivideNew] = nLeavesTot;
@@ -206,8 +199,8 @@ void CADTBaseClass::BuildADT(unsigned short  nDim,
     /* Set the data for the next round. */
     nLeavesToDivide = nLeavesToDivideNew;
 
-    for(unsigned long i=0; i<=nLeavesToDivide; ++i)           nPointIDs[i] = nPointIDsNew[i];
-    for(unsigned long i=0; i< nLeavesToDivide; ++i)           curLeaf[i]   = curLeafNew[i];
-    for(unsigned long i=0; i<nPointIDs[nLeavesToDivide]; ++i) pointIDs[i]  = pointIDsNew[i];
+    for (unsigned long i = 0; i <= nLeavesToDivide; ++i) nPointIDs[i] = nPointIDsNew[i];
+    for (unsigned long i = 0; i < nLeavesToDivide; ++i) curLeaf[i] = curLeafNew[i];
+    for (unsigned long i = 0; i < nPointIDs[nLeavesToDivide]; ++i) pointIDs[i] = pointIDsNew[i];
   }
 }
diff --git a/Common/src/adt/CADTElemClass.cpp b/Common/src/adt/CADTElemClass.cpp
index 7093a50b209..2c94ba5cbbe 100644
--- a/Common/src/adt/CADTElemClass.cpp
+++ b/Common/src/adt/CADTElemClass.cpp
@@ -30,18 +30,13 @@
 #include "../../include/option_structure.hpp"
 
 /* Define the tolerance to decide whether or not a point is inside an element. */
-const su2double tolInsideElem   =  1.e-10;
+const su2double tolInsideElem = 1.e-10;
 const su2double paramLowerBound = -1.0 - tolInsideElem;
-const su2double paramUpperBound =  1.0 + tolInsideElem;
-
-CADTElemClass::CADTElemClass(unsigned short         val_nDim,
-                             vector<su2double>      &val_coor,
-                             vector<unsigned long>  &val_connElem,
-                             vector<unsigned short> &val_VTKElem,
-                             vector<unsigned short> &val_markerID,
-                             vector<unsigned long>  &val_elemID,
-                             const bool             globalTree) {
+const su2double paramUpperBound = 1.0 + tolInsideElem;
 
+CADTElemClass::CADTElemClass(unsigned short val_nDim, vector<su2double>& val_coor, vector<unsigned long>& val_connElem,
+                             vector<unsigned short>& val_VTKElem, vector<unsigned short>& val_markerID,
+                             vector<unsigned long>& val_elemID, const bool globalTree) {
   /* Copy the dimension of the problem into nDim. */
   nDim = val_nDim;
 
@@ -66,8 +61,7 @@ CADTElemClass::CADTElemClass(unsigned short         val_nDim,
 #ifdef HAVE_MPI
 
   /* Parallel mode. Check whether a global or a local tree must be built. */
-  if( globalTree ) {
-
+  if (globalTree) {
     /*--- The local grids are gathered on all ranks. For very large cases this
           could become a serious memory bottleneck and a parallel version may
           be needed.  ---*/
@@ -79,35 +73,32 @@ CADTElemClass::CADTElemClass(unsigned short         val_nDim,
     SU2_MPI::Comm_size(SU2_MPI::GetComm(), &size);
 
     vector<int> recvCounts(size), displs(size);
-    int sizeLocal = (int) val_coor.size();
+    int sizeLocal = (int)val_coor.size();
 
-    SU2_MPI::Allgather(&sizeLocal, 1, MPI_INT, recvCounts.data(), 1,
-                       MPI_INT, SU2_MPI::GetComm());
+    SU2_MPI::Allgather(&sizeLocal, 1, MPI_INT, recvCounts.data(), 1, MPI_INT, SU2_MPI::GetComm());
     displs[0] = 0;
-    for(int i=1; i<size; ++i) displs[i] = displs[i-1] + recvCounts[i-1];
+    for (int i = 1; i < size; ++i) displs[i] = displs[i - 1] + recvCounts[i - 1];
 
     /*--- Correct the local connectivities with the offset of this rank,
           such that they get the correct values when all the points from
           all ranks are gathered. ---*/
-    const unsigned long offsetRank = displs[rank]/nDim;
-    for(unsigned long i=0; i<val_connElem.size(); ++i)
-      val_connElem[i] += offsetRank;
+    const unsigned long offsetRank = displs[rank] / nDim;
+    for (unsigned long i = 0; i < val_connElem.size(); ++i) val_connElem[i] += offsetRank;
 
     /*--- Gather the coordinates of the points on all ranks. ---*/
     int sizeGlobal = displs.back() + recvCounts.back();
 
     coorPoints.resize(sizeGlobal);
-    SU2_MPI::Allgatherv(val_coor.data(), sizeLocal, MPI_DOUBLE, coorPoints.data(),
-                        recvCounts.data(), displs.data(), MPI_DOUBLE, SU2_MPI::GetComm());
+    SU2_MPI::Allgatherv(val_coor.data(), sizeLocal, MPI_DOUBLE, coorPoints.data(), recvCounts.data(), displs.data(),
+                        MPI_DOUBLE, SU2_MPI::GetComm());
 
     /*--- Determine the number of elements per rank and make them
           available to all ranks. ---*/
-    sizeLocal = (int) val_VTKElem.size();
+    sizeLocal = (int)val_VTKElem.size();
 
-    SU2_MPI::Allgather(&sizeLocal, 1, MPI_INT, recvCounts.data(), 1,
-                       MPI_INT, SU2_MPI::GetComm());
+    SU2_MPI::Allgather(&sizeLocal, 1, MPI_INT, recvCounts.data(), 1, MPI_INT, SU2_MPI::GetComm());
     displs[0] = 0;
-    for(int i=1; i<size; ++i) displs[i] = displs[i-1] + recvCounts[i-1];
+    for (int i = 1; i < size; ++i) displs[i] = displs[i - 1] + recvCounts[i - 1];
 
     /*--- Gather the element type, the possible markers of these elements
           and the local element ID's on all ranks. ---*/
@@ -117,50 +108,46 @@ CADTElemClass::CADTElemClass(unsigned short         val_nDim,
     localMarkers.resize(sizeGlobal);
     localElemIDs.resize(sizeGlobal);
 
-    SU2_MPI::Allgatherv(val_VTKElem.data(), sizeLocal, MPI_UNSIGNED_SHORT, elemVTK_Type.data(),
-                        recvCounts.data(), displs.data(), MPI_UNSIGNED_SHORT, SU2_MPI::GetComm());
+    SU2_MPI::Allgatherv(val_VTKElem.data(), sizeLocal, MPI_UNSIGNED_SHORT, elemVTK_Type.data(), recvCounts.data(),
+                        displs.data(), MPI_UNSIGNED_SHORT, SU2_MPI::GetComm());
 
-    SU2_MPI::Allgatherv(val_markerID.data(), sizeLocal, MPI_UNSIGNED_SHORT, localMarkers.data(),
-                        recvCounts.data(), displs.data(), MPI_UNSIGNED_SHORT, SU2_MPI::GetComm());
+    SU2_MPI::Allgatherv(val_markerID.data(), sizeLocal, MPI_UNSIGNED_SHORT, localMarkers.data(), recvCounts.data(),
+                        displs.data(), MPI_UNSIGNED_SHORT, SU2_MPI::GetComm());
 
-    SU2_MPI::Allgatherv(val_elemID.data(), sizeLocal, MPI_UNSIGNED_LONG, localElemIDs.data(),
-                        recvCounts.data(), displs.data(), MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
+    SU2_MPI::Allgatherv(val_elemID.data(), sizeLocal, MPI_UNSIGNED_LONG, localElemIDs.data(), recvCounts.data(),
+                        displs.data(), MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
 
     /*--- Create the content of ranksOfElems, which stores the original ranks
           where the elements come from. ---*/
     ranksOfElems.resize(sizeGlobal);
 
-    for(int i=0; i<size; ++i) {
-      for(int j=0; j<recvCounts[i]; ++j)
-        ranksOfElems[displs[i]+j] = i;
+    for (int i = 0; i < size; ++i) {
+      for (int j = 0; j < recvCounts[i]; ++j) ranksOfElems[displs[i] + j] = i;
     }
 
     /*--- Determine the size of the local connectivity per rank and make them
           available to all ranks. ---*/
-    sizeLocal = (int) val_connElem.size();
+    sizeLocal = (int)val_connElem.size();
 
-    SU2_MPI::Allgather(&sizeLocal, 1, MPI_INT, recvCounts.data(), 1,
-                       MPI_INT, SU2_MPI::GetComm());
+    SU2_MPI::Allgather(&sizeLocal, 1, MPI_INT, recvCounts.data(), 1, MPI_INT, SU2_MPI::GetComm());
     displs[0] = 0;
-    for(int i=1; i<size; ++i) displs[i] = displs[i-1] + recvCounts[i-1];
+    for (int i = 1; i < size; ++i) displs[i] = displs[i - 1] + recvCounts[i - 1];
 
     /*--- Gather the element connectivity on all ranks. ---*/
     sizeGlobal = displs.back() + recvCounts.back();
 
     elemConns.resize(sizeGlobal);
 
-    SU2_MPI::Allgatherv(val_connElem.data(), sizeLocal, MPI_UNSIGNED_LONG, elemConns.data(),
-                        recvCounts.data(), displs.data(), MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
-  }
-    else {
-
+    SU2_MPI::Allgatherv(val_connElem.data(), sizeLocal, MPI_UNSIGNED_LONG, elemConns.data(), recvCounts.data(),
+                        displs.data(), MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
+  } else {
     /*--- A local tree must be built. Copy the data from the arguments into the
           member variables and set the ranks to the rank of this processor. ---*/
     int rank;
     SU2_MPI::Comm_rank(SU2_MPI::GetComm(), &rank);
 
-    coorPoints   = val_coor;
-    elemConns    = val_connElem;
+    coorPoints = val_coor;
+    elemConns = val_connElem;
     elemVTK_Type = val_VTKElem;
     localMarkers = val_markerID;
     localElemIDs = val_elemID;
@@ -171,8 +158,8 @@ CADTElemClass::CADTElemClass(unsigned short         val_nDim,
 
   /*--- Sequential mode. Copy the data from the arguments into the member
         variables and set the ranks to MASTER_NODE. ---*/
-  coorPoints   = val_coor;
-  elemConns    = val_connElem;
+  coorPoints = val_coor;
+  elemConns = val_connElem;
   elemVTK_Type = val_VTKElem;
   localMarkers = val_markerID;
   localElemIDs = val_elemID;
@@ -181,26 +168,39 @@ CADTElemClass::CADTElemClass(unsigned short         val_nDim,
 
 #endif
 
-    /*--- Determine the values of the vector nDOFsPerElem, which contains the
-        number of DOFs per element in cumulative storage format. ---*/
+  /*--- Determine the values of the vector nDOFsPerElem, which contains the
+      number of DOFs per element in cumulative storage format. ---*/
   const unsigned long nElem = elemVTK_Type.size();
-  nDOFsPerElem.resize(nElem+1);
+  nDOFsPerElem.resize(nElem + 1);
 
   nDOFsPerElem[0] = 0;
-  for(unsigned long i=0; i<nElem; ++i) {
-
+  for (unsigned long i = 0; i < nElem; ++i) {
     unsigned short nDOFs = 0;
-    switch( elemVTK_Type[i] ) {
-      case LINE:          nDOFs = 2; break;
-      case TRIANGLE:      nDOFs = 3; break;
-      case QUADRILATERAL: nDOFs = 4; break;
-      case TETRAHEDRON:   nDOFs = 4; break;
-      case PYRAMID:       nDOFs = 5; break;
-      case PRISM:         nDOFs = 6; break;
-      case HEXAHEDRON:    nDOFs = 8; break;
+    switch (elemVTK_Type[i]) {
+      case LINE:
+        nDOFs = 2;
+        break;
+      case TRIANGLE:
+        nDOFs = 3;
+        break;
+      case QUADRILATERAL:
+        nDOFs = 4;
+        break;
+      case TETRAHEDRON:
+        nDOFs = 4;
+        break;
+      case PYRAMID:
+        nDOFs = 5;
+        break;
+      case PRISM:
+        nDOFs = 6;
+        break;
+      case HEXAHEDRON:
+        nDOFs = 8;
+        break;
     }
 
-    nDOFsPerElem[i+1] = nDOFsPerElem[i] + nDOFs;
+    nDOFsPerElem[i + 1] = nDOFsPerElem[i] + nDOFs;
   }
 
   /*--------------------------------------------------------------------------*/
@@ -211,31 +211,29 @@ CADTElemClass::CADTElemClass(unsigned short         val_nDim,
   /*--------------------------------------------------------------------------*/
 
   /* Allocate the memory for the bounding boxes of the elements. */
-  BBoxCoor.resize(2*nDim*nElem);
+  BBoxCoor.resize(2 * nDim * nElem);
 
   /*--- Loop over the elements to determine the minimum and maximum coordinates
         of the elements. These coordinates completely define the bounding box,
         which can be represented as a point in 2*nDim dimensional space. ---*/
-  for(unsigned long i=0; i<nElem; ++i) {
-
+  for (unsigned long i = 0; i < nElem; ++i) {
     /* Set the pointers for the minimum and maximum coordinates for this
        bounding box. Initialize these coordinates to the first coordinate
        of the corresponding element. */
-    su2double *BBMin = BBoxCoor.data() + 2*nDim*i;
-    su2double *BBMax = BBMin + nDim;
+    su2double* BBMin = BBoxCoor.data() + 2 * nDim * i;
+    su2double* BBMax = BBMin + nDim;
 
-    unsigned long    j  = nDOFsPerElem[i];
-    const su2double *xP = coorPoints.data() + nDim*elemConns[j];
+    unsigned long j = nDOFsPerElem[i];
+    const su2double* xP = coorPoints.data() + nDim * elemConns[j];
 
-    for(unsigned short k=0; k<nDim; ++k)
-      BBMin[k] = BBMax[k] = xP[k];
+    for (unsigned short k = 0; k < nDim; ++k) BBMin[k] = BBMax[k] = xP[k];
 
     /* Loop over the other vertices of the element to determine the
        minimum and maximum coordinates of the bounding box. */
-    for(j=(nDOFsPerElem[i]+1); j<nDOFsPerElem[i+1]; ++j) {
-      xP = coorPoints.data() + nDim*elemConns[j];
+    for (j = (nDOFsPerElem[i] + 1); j < nDOFsPerElem[i + 1]; ++j) {
+      xP = coorPoints.data() + nDim * elemConns[j];
 
-      for(unsigned short k=0; k<nDim; ++k) {
+      for (unsigned short k = 0; k < nDim; ++k) {
         BBMin[k] = min(BBMin[k], xP[k]);
         BBMax[k] = max(BBMax[k], xP[k]);
       }
@@ -243,9 +241,9 @@ CADTElemClass::CADTElemClass(unsigned short         val_nDim,
 
     /* Add a tolerance to the bounding box size, such that the overlap check in
        the tree traversal does not go wrong due to round off error. */
-    for(unsigned short k=0; k<nDim; ++k) {
+    for (unsigned short k = 0; k < nDim; ++k) {
       const su2double lenScale = BBMax[k] - BBMin[k];
-      const su2double tol      = max(1.e-25, 1.e-6*lenScale);
+      const su2double tol = max(1.e-25, 1.e-6 * lenScale);
 
       BBMin[k] -= tol;
       BBMax[k] += tol;
@@ -253,7 +251,7 @@ CADTElemClass::CADTElemClass(unsigned short         val_nDim,
   }
 
   /* Build the ADT of the bounding boxes. */
-  BuildADT(2*nDim, nElem, BBoxCoor.data());
+  BuildADT(2 * nDim, nElem, BBoxCoor.data());
 
   /*--- Reserve the memory for frontLeaves, frontLeavesNew and BBoxTargets,
         which are needed during the tree search. ---*/
@@ -263,14 +261,9 @@ CADTElemClass::CADTElemClass(unsigned short         val_nDim,
 }
 
 bool CADTElemClass::DetermineContainingElement_impl(vector<unsigned long>& frontLeaves,
-                                                    vector<unsigned long>& frontLeavesNew,
-                                                    const su2double *coor,
-                                                    unsigned short  &markerID,
-                                                    unsigned long   &elemID,
-                                                    int             &rankID,
-                                                    su2double       *parCoor,
-                                                    su2double       *weightsInterpol) const {
-
+                                                    vector<unsigned long>& frontLeavesNew, const su2double* coor,
+                                                    unsigned short& markerID, unsigned long& elemID, int& rankID,
+                                                    su2double* parCoor, su2double* weightsInterpol) const {
   /* Start at the root leaf of the ADT, i.e. initialize frontLeaves such that
      it only contains the root leaf. Make sure to wipe out any data from a
      previous search. */
@@ -278,61 +271,54 @@ bool CADTElemClass::DetermineContainingElement_impl(vector<unsigned long>& front
   frontLeaves.push_back(0);
 
   /* Infinite loop of the tree traversal. */
-  for(;;) {
-
+  for (;;) {
     /* Initialize the new front, i.e. the front for the next round, to empty. */
     frontLeavesNew.clear();
 
     /* Loop over the leaves of the current front. */
-    for(unsigned long i=0; i<frontLeaves.size(); ++i) {
-
+    for (unsigned long i = 0; i < frontLeaves.size(); ++i) {
       /* Store the current leaf a bit easier in ll and loop over its children. */
       const unsigned long ll = frontLeaves[i];
-      for(unsigned short mm=0; mm<2; ++mm) {
-
+      for (unsigned short mm = 0; mm < 2; ++mm) {
         /* Determine whether this child contains a node or a leaf
            of the next level of the ADT. */
         unsigned long kk = leaves[ll].children[mm];
-        if( leaves[ll].childrenAreTerminal[mm] ) {
-
+        if (leaves[ll].childrenAreTerminal[mm]) {
           /* Child contains a bounding box. Check if the coordinate is
              inside the bounding box. */
-          const su2double *coorBBMin = BBoxCoor.data() + nDimADT*kk;
-          const su2double *coorBBMax = coorBBMin + nDim;
+          const su2double* coorBBMin = BBoxCoor.data() + nDimADT * kk;
+          const su2double* coorBBMax = coorBBMin + nDim;
 
           bool coorIsInside = true;
-          for(unsigned short k=0; k<nDim; ++k) {
-            if(coor[k] < coorBBMin[k]) coorIsInside = false;
-            if(coor[k] > coorBBMax[k]) coorIsInside = false;
+          for (unsigned short k = 0; k < nDim; ++k) {
+            if (coor[k] < coorBBMin[k]) coorIsInside = false;
+            if (coor[k] > coorBBMax[k]) coorIsInside = false;
           }
 
-          if( coorIsInside ) {
-
+          if (coorIsInside) {
             /* Coordinate is inside the bounding box. Check if it
                is also inside the corresponding element. If so,
                set the required information and return true. */
-            if( CoorInElement(kk, coor, parCoor, weightsInterpol) ) {
+            if (CoorInElement(kk, coor, parCoor, weightsInterpol)) {
               markerID = localMarkers[kk];
-              elemID   = localElemIDs[kk];
-              rankID   = ranksOfElems[kk];
+              elemID = localElemIDs[kk];
+              rankID = ranksOfElems[kk];
               return true;
             }
           }
-        }
-        else {
-
+        } else {
           /* Child contains a leaf. If the coordinate is inside the leaf
              store the leaf for the next round. */
-          const su2double *coorBBMin = leaves[kk].xMin;
-          const su2double *coorBBMax = leaves[kk].xMax + nDim;
+          const su2double* coorBBMin = leaves[kk].xMin;
+          const su2double* coorBBMax = leaves[kk].xMax + nDim;
 
           bool coorIsInside = true;
-          for(unsigned short k=0; k<nDim; ++k) {
-            if(coor[k] < coorBBMin[k]) coorIsInside = false;
-            if(coor[k] > coorBBMax[k]) coorIsInside = false;
+          for (unsigned short k = 0; k < nDim; ++k) {
+            if (coor[k] < coorBBMin[k]) coorIsInside = false;
+            if (coor[k] > coorBBMax[k]) coorIsInside = false;
           }
 
-          if( coorIsInside ) frontLeavesNew.push_back(kk);
+          if (coorIsInside) frontLeavesNew.push_back(kk);
         }
       }
     }
@@ -342,7 +328,7 @@ bool CADTElemClass::DetermineContainingElement_impl(vector<unsigned long>& front
           is empty the entire tree has been traversed and a break can be made
           from the infinite loop. ---*/
     frontLeaves = frontLeavesNew;
-    if(frontLeaves.size() == 0) break;
+    if (frontLeaves.size() == 0) break;
   }
 
   /* If this point is reached, no element is found that contains the coordinate
@@ -352,13 +338,9 @@ bool CADTElemClass::DetermineContainingElement_impl(vector<unsigned long>& front
 
 void CADTElemClass::DetermineNearestElement_impl(vector<CBBoxTargetClass>& BBoxTargets,
                                                  vector<unsigned long>& frontLeaves,
-                                                 vector<unsigned long>& frontLeavesNew,
-                                                 const su2double *coor,
-                                                 su2double       &dist,
-                                                 unsigned short  &markerID,
-                                                 unsigned long   &elemID,
-                                                 int             &rankID) const {
-
+                                                 vector<unsigned long>& frontLeavesNew, const su2double* coor,
+                                                 su2double& dist, unsigned short& markerID, unsigned long& elemID,
+                                                 int& rankID) const {
   const bool wasActive = AD::BeginPassive();
 
   /*----------------------------------------------------------------------------*/
@@ -367,16 +349,20 @@ void CADTElemClass::DetermineNearestElement_impl(vector<CBBoxTargetClass>& BBoxT
   /*----------------------------------------------------------------------------*/
 
   unsigned long kk = leaves[0].centralNodeID;
-  const su2double *coorBBMin = BBoxCoor.data() + nDimADT*kk;
-  const su2double *coorBBMax = coorBBMin + nDim;
+  const su2double* coorBBMin = BBoxCoor.data() + nDimADT * kk;
+  const su2double* coorBBMax = coorBBMin + nDim;
   unsigned long jj = 0;
 
   dist = 0.0;
   su2double ds;
-  ds = max(fabs(coor[0]-coorBBMin[0]), fabs(coor[0]-coorBBMax[0])); dist += ds*ds;
-  ds = max(fabs(coor[1]-coorBBMin[1]), fabs(coor[1]-coorBBMax[1])); dist += ds*ds;
-  if(nDim==3) {
-  ds = max(fabs(coor[2]-coorBBMin[2]), fabs(coor[2]-coorBBMax[2])); dist += ds*ds;}
+  ds = max(fabs(coor[0] - coorBBMin[0]), fabs(coor[0] - coorBBMax[0]));
+  dist += ds * ds;
+  ds = max(fabs(coor[1] - coorBBMin[1]), fabs(coor[1] - coorBBMax[1]));
+  dist += ds * ds;
+  if (nDim == 3) {
+    ds = max(fabs(coor[2] - coorBBMin[2]), fabs(coor[2] - coorBBMax[2]));
+    dist += ds * ds;
+  }
 
   /*----------------------------------------------------------------------------*/
   /*--- Step 2: Traverse the tree and store the bounding boxes for which the ---*/
@@ -393,83 +379,92 @@ void CADTElemClass::DetermineNearestElement_impl(vector<CBBoxTargetClass>& BBoxT
   frontLeaves.push_back(0);
 
   /* Infinite loop of the tree traversal. */
-  for(;;) {
-
+  for (;;) {
     /* Initialize the new front, i.e. the front for the next round, to empty. */
     frontLeavesNew.clear();
 
     /* Loop over the leaves of the current front. */
-    for(unsigned long i=0; i<frontLeaves.size(); ++i) {
-
+    for (unsigned long i = 0; i < frontLeaves.size(); ++i) {
       /* Store the current leaf a bit easier in ll and loop over its children. */
       const unsigned long ll = frontLeaves[i];
-      for(unsigned short mm=0; mm<2; ++mm) {
-
+      for (unsigned short mm = 0; mm < 2; ++mm) {
         /* Determine whether this child contains a node or a leaf
            of the next level of the ADT. */
         kk = leaves[ll].children[mm];
-        if( leaves[ll].childrenAreTerminal[mm] ) {
-
+        if (leaves[ll].childrenAreTerminal[mm]) {
           /*--- Child contains a bounding. Compute the possible distance squared
                 to this bounding box. Tf a coordinate is inside the box ds = 0. ---*/
-          coorBBMin = BBoxCoor.data() + nDimADT*kk;
+          coorBBMin = BBoxCoor.data() + nDimADT * kk;
           coorBBMax = coorBBMin + nDim;
 
           su2double posDist2 = 0.0, ds;
-          ds = min(0.0, coor[0]-coorBBMin[0]) + max(0.0, coor[0]-coorBBMax[0]); posDist2 += ds*ds;
-          ds = min(0.0, coor[1]-coorBBMin[1]) + max(0.0, coor[1]-coorBBMax[1]); posDist2 += ds*ds;
-          if(nDim==3) {
-          ds = min(0.0, coor[2]-coorBBMin[2]) + max(0.0, coor[2]-coorBBMax[2]); posDist2 += ds*ds;}
+          ds = min(0.0, coor[0] - coorBBMin[0]) + max(0.0, coor[0] - coorBBMax[0]);
+          posDist2 += ds * ds;
+          ds = min(0.0, coor[1] - coorBBMin[1]) + max(0.0, coor[1] - coorBBMax[1]);
+          posDist2 += ds * ds;
+          if (nDim == 3) {
+            ds = min(0.0, coor[2] - coorBBMin[2]) + max(0.0, coor[2] - coorBBMax[2]);
+            posDist2 += ds * ds;
+          }
 
           /* Check if the possible minimum distance is less than or equal to
              the currently stored distance. If so, this bounding box is a
              candidate for the actual minimum distance and must be stored
              in BBoxTargets. */
-          if(posDist2 <= dist) {
-
+          if (posDist2 <= dist) {
             /*--- Compute the guaranteed minimum distance for this bounding box. ---*/
             su2double guarDist2 = 0.0, ds;
-            ds = max(fabs(coor[0]-coorBBMin[0]), fabs(coor[0]-coorBBMax[0])); guarDist2 += ds*ds;
-            ds = max(fabs(coor[1]-coorBBMin[1]), fabs(coor[1]-coorBBMax[1])); guarDist2 += ds*ds;
-            if(nDim==3) {
-            ds = max(fabs(coor[2]-coorBBMin[2]), fabs(coor[2]-coorBBMax[2])); guarDist2 += ds*ds;}
+            ds = max(fabs(coor[0] - coorBBMin[0]), fabs(coor[0] - coorBBMax[0]));
+            guarDist2 += ds * ds;
+            ds = max(fabs(coor[1] - coorBBMin[1]), fabs(coor[1] - coorBBMax[1]));
+            guarDist2 += ds * ds;
+            if (nDim == 3) {
+              ds = max(fabs(coor[2] - coorBBMin[2]), fabs(coor[2] - coorBBMax[2]));
+              guarDist2 += ds * ds;
+            }
 
             /* Store this bounding box in BBoxTargets and update the currently
                stored value of the distance squared. */
             BBoxTargets.push_back(CBBoxTargetClass(kk, posDist2, guarDist2));
             dist = min(dist, guarDist2);
           }
-        }
-        else {
-
+        } else {
           /*--- Child contains a leaf. Determine the possible minimum distance
                 squared to that leaf. Same manual unroling as before. ---*/
           coorBBMin = leaves[kk].xMin;
           coorBBMax = leaves[kk].xMax + nDim;
 
           su2double posDist2 = 0.0, ds;
-          ds = min(0.0, coor[0]-coorBBMin[0]) + max(0.0, coor[0]-coorBBMax[0]); posDist2 += ds*ds;
-          ds = min(0.0, coor[1]-coorBBMin[1]) + max(0.0, coor[1]-coorBBMax[1]); posDist2 += ds*ds;
-          if(nDim==3) {
-          ds = min(0.0, coor[2]-coorBBMin[2]) + max(0.0, coor[2]-coorBBMax[2]); posDist2 += ds*ds;}
+          ds = min(0.0, coor[0] - coorBBMin[0]) + max(0.0, coor[0] - coorBBMax[0]);
+          posDist2 += ds * ds;
+          ds = min(0.0, coor[1] - coorBBMin[1]) + max(0.0, coor[1] - coorBBMax[1]);
+          posDist2 += ds * ds;
+          if (nDim == 3) {
+            ds = min(0.0, coor[2] - coorBBMin[2]) + max(0.0, coor[2] - coorBBMax[2]);
+            posDist2 += ds * ds;
+          }
 
           /* Check if the possible minimum distance is less than or equal to the currently
              stored distance. If so this leaf must be stored for the next round. */
-          if(posDist2 <= dist) {
+          if (posDist2 <= dist) {
             frontLeavesNew.push_back(kk);
 
             /*--- Determine the guaranteed minimum distance squared to the central
                   bounding box of this leaf and update the currently stored
                   minimum wall distance. Same manual unroling as before. ---*/
             kk = leaves[kk].centralNodeID;
-            coorBBMin = BBoxCoor.data() + nDimADT*kk;
+            coorBBMin = BBoxCoor.data() + nDimADT * kk;
             coorBBMax = coorBBMin + nDim;
 
             su2double guarDist2 = 0.0, ds;
-            ds = max(fabs(coor[0]-coorBBMin[0]), fabs(coor[0]-coorBBMax[0])); guarDist2 += ds*ds;
-            ds = max(fabs(coor[1]-coorBBMin[1]), fabs(coor[1]-coorBBMax[1])); guarDist2 += ds*ds;
-            if(nDim==3) {
-            ds = max(fabs(coor[2]-coorBBMin[2]), fabs(coor[2]-coorBBMax[2])); guarDist2 += ds*ds;}
+            ds = max(fabs(coor[0] - coorBBMin[0]), fabs(coor[0] - coorBBMax[0]));
+            guarDist2 += ds * ds;
+            ds = max(fabs(coor[1] - coorBBMin[1]), fabs(coor[1] - coorBBMax[1]));
+            guarDist2 += ds * ds;
+            if (nDim == 3) {
+              ds = max(fabs(coor[2] - coorBBMin[2]), fabs(coor[2] - coorBBMax[2]));
+              guarDist2 += ds * ds;
+            }
 
             dist = min(dist, guarDist2);
           }
@@ -482,7 +477,7 @@ void CADTElemClass::DetermineNearestElement_impl(vector<CBBoxTargetClass>& BBoxT
           is empty the entire tree has been traversed and a break can be made
           from the infinite loop. ---*/
     frontLeaves = frontLeavesNew;
-    if(frontLeaves.size() == 0) break;
+    if (frontLeaves.size() == 0) break;
   }
 
   /*----------------------------------------------------------------------------*/
@@ -496,14 +491,13 @@ void CADTElemClass::DetermineNearestElement_impl(vector<CBBoxTargetClass>& BBoxT
   sort(BBoxTargets.begin(), BBoxTargets.end());
 
   /* Loop over the candidate bounding boxes. */
-  for(unsigned long i=0; i<BBoxTargets.size(); ++i) {
-
+  for (unsigned long i = 0; i < BBoxTargets.size(); ++i) {
     /* Break the loop if the possible minimum distance is larger than
        the currently stored value. In that case it does not make sense to
        check the remainder of the bounding boxes, as they are sorted in
        increasing order (based on the possible minimum distance.
        Make sure that at least one bounding box is checked. */
-    if(BBoxTargets[i].possibleMinDist2 > dist) break;
+    if (BBoxTargets[i].possibleMinDist2 > dist) break;
 
     /*--- Compute the distance squared to the element that corresponds to the
           current bounding box. If this distance is less than or equal to
@@ -513,12 +507,12 @@ void CADTElemClass::DetermineNearestElement_impl(vector<CBBoxTargetClass>& BBoxT
 
     su2double dist2Elem;
     Dist2ToElement(ii, coor, dist2Elem);
-    if(dist2Elem <= dist) {
-      jj       = ii;
-      dist     = dist2Elem;
+    if (dist2Elem <= dist) {
+      jj = ii;
+      dist = dist2Elem;
       markerID = localMarkers[ii];
-      elemID   = localElemIDs[ii];
-      rankID   = ranksOfElems[ii];
+      elemID = localElemIDs[ii];
+      rankID = ranksOfElems[ii];
     }
   }
 
@@ -530,20 +524,22 @@ void CADTElemClass::DetermineNearestElement_impl(vector<CBBoxTargetClass>& BBoxT
   dist = sqrt(dist);
 }
 
-bool CADTElemClass::CoorInElement(const unsigned long elemID,
-                                  const su2double     *coor,
-                                  su2double           *parCoor,
-                                  su2double           *weightsInterpol) const {
-
+bool CADTElemClass::CoorInElement(const unsigned long elemID, const su2double* coor, su2double* parCoor,
+                                  su2double* weightsInterpol) const {
   /*--- Make a distinction between the element types. ---*/
-  switch( elemVTK_Type[elemID] ) {
-
-    case TRIANGLE:      return CoorInTriangle(elemID, coor, parCoor, weightsInterpol);
-    case QUADRILATERAL: return CoorInQuadrilateral(elemID, coor, parCoor, weightsInterpol);
-    case TETRAHEDRON:   return CoorInTetrahedron(elemID, coor, parCoor, weightsInterpol);
-    case PYRAMID:       return CoorInPyramid(elemID, coor, parCoor, weightsInterpol);
-    case PRISM:         return CoorInPrism(elemID, coor, parCoor, weightsInterpol);
-    case HEXAHEDRON:    return CoorInHexahedron(elemID, coor, parCoor, weightsInterpol);
+  switch (elemVTK_Type[elemID]) {
+    case TRIANGLE:
+      return CoorInTriangle(elemID, coor, parCoor, weightsInterpol);
+    case QUADRILATERAL:
+      return CoorInQuadrilateral(elemID, coor, parCoor, weightsInterpol);
+    case TETRAHEDRON:
+      return CoorInTetrahedron(elemID, coor, parCoor, weightsInterpol);
+    case PYRAMID:
+      return CoorInPyramid(elemID, coor, parCoor, weightsInterpol);
+    case PRISM:
+      return CoorInPrism(elemID, coor, parCoor, weightsInterpol);
+    case HEXAHEDRON:
+      return CoorInHexahedron(elemID, coor, parCoor, weightsInterpol);
 
     default:
       /* This should not happen. */
@@ -552,21 +548,17 @@ bool CADTElemClass::CoorInElement(const unsigned long elemID,
   }
 }
 
-void CADTElemClass::Dist2ToElement(const unsigned long elemID,
-                                   const su2double     *coor,
-                                   su2double           &dist2Elem) const {
-
+void CADTElemClass::Dist2ToElement(const unsigned long elemID, const su2double* coor, su2double& dist2Elem) const {
   /*--- Make a distinction between the element types. ---*/
-  switch( elemVTK_Type[elemID] ) {
-
+  switch (elemVTK_Type[elemID]) {
     case LINE: {
-
       /*--- Element is a line. The number of space dimensions can be either
             1, 2 or 3. Store the indices where the coordinates of the vertices
             are stored in i0 and i1. ---*/
       unsigned long i0 = nDOFsPerElem[elemID];
       unsigned long i1 = i0 + 1;
-      i0 = nDim*elemConns[i0]; i1 = nDim*elemConns[i1];
+      i0 = nDim * elemConns[i0];
+      i1 = nDim * elemConns[i1];
 
       /*--- Call the function Dist2ToLine to do the actual work. ---*/
       Dist2ToLine(i0, i1, coor, dist2Elem);
@@ -574,16 +566,17 @@ void CADTElemClass::Dist2ToElement(const unsigned long elemID,
       break;
     }
 
-    /*------------------------------------------------------------------------*/
+      /*------------------------------------------------------------------------*/
 
     case TRIANGLE: {
-
       /*--- Element is a triangle. The number of space dimensions can be either
             2 or 3. Store the indices where the coordinates of the vertices
             are stored in i0, i1 and i2. ---*/
       unsigned long i0 = nDOFsPerElem[elemID];
       unsigned long i1 = i0 + 1, i2 = i0 + 2;
-      i0 = nDim*elemConns[i0]; i1 = nDim*elemConns[i1]; i2 = nDim*elemConns[i2];
+      i0 = nDim * elemConns[i0];
+      i1 = nDim * elemConns[i1];
+      i2 = nDim * elemConns[i2];
 
       /*--- Call the function Dist2ToTriangle to compute the distance to the
             triangle if the projection is inside the triangle. In that case the
@@ -591,28 +584,31 @@ void CADTElemClass::Dist2ToElement(const unsigned long elemID,
             false is returned and the distance to each of the lines of the
             triangle is computed and the minimum is taken. ---*/
       su2double r, s;
-      if( !Dist2ToTriangle(i0, i1, i2, coor, dist2Elem, r, s) ) {
+      if (!Dist2ToTriangle(i0, i1, i2, coor, dist2Elem, r, s)) {
         Dist2ToLine(i0, i1, coor, dist2Elem);
 
         su2double dist2Line;
-        Dist2ToLine(i1, i2, coor, dist2Line); dist2Elem = min(dist2Elem, dist2Line);
-        Dist2ToLine(i2, i0, coor, dist2Line); dist2Elem = min(dist2Elem, dist2Line);
+        Dist2ToLine(i1, i2, coor, dist2Line);
+        dist2Elem = min(dist2Elem, dist2Line);
+        Dist2ToLine(i2, i0, coor, dist2Line);
+        dist2Elem = min(dist2Elem, dist2Line);
       }
 
       break;
     }
 
-    /*------------------------------------------------------------------------*/
+      /*------------------------------------------------------------------------*/
 
     case QUADRILATERAL: {
-
       /*--- Element is a quadrilateral. The number of space dimensions can be
             either 2 or 3. Store the indices where the coordinates of the
             vertices are stored in i0, i1, i2 and i3. ---*/
       unsigned long i0 = nDOFsPerElem[elemID];
       unsigned long i1 = i0 + 1, i2 = i0 + 2, i3 = i0 + 3;
-      i0 = nDim*elemConns[i0]; i1 = nDim*elemConns[i1];
-      i2 = nDim*elemConns[i2]; i3 = nDim*elemConns[i3];
+      i0 = nDim * elemConns[i0];
+      i1 = nDim * elemConns[i1];
+      i2 = nDim * elemConns[i2];
+      i3 = nDim * elemConns[i3];
 
       /*--- Call the function Dist2ToQuadrilateral to compute the distance to the
             quadrilateral if the projection is inside the quadrilateral. In that
@@ -620,19 +616,22 @@ void CADTElemClass::Dist2ToElement(const unsigned long elemID,
             quadrilateral, false is returned and the distance to each of the lines
             of the quadrilateral is computed and the minimum is taken. ---*/
       su2double r, s;
-      if( !Dist2ToQuadrilateral(i0, i1, i2, i3, coor, r, s, dist2Elem) ) {
+      if (!Dist2ToQuadrilateral(i0, i1, i2, i3, coor, r, s, dist2Elem)) {
         Dist2ToLine(i0, i1, coor, dist2Elem);
 
         su2double dist2Line;
-        Dist2ToLine(i1, i2, coor, dist2Line); dist2Elem = min(dist2Elem, dist2Line);
-        Dist2ToLine(i2, i3, coor, dist2Line); dist2Elem = min(dist2Elem, dist2Line);
-        Dist2ToLine(i3, i0, coor, dist2Line); dist2Elem = min(dist2Elem, dist2Line);
+        Dist2ToLine(i1, i2, coor, dist2Line);
+        dist2Elem = min(dist2Elem, dist2Line);
+        Dist2ToLine(i2, i3, coor, dist2Line);
+        dist2Elem = min(dist2Elem, dist2Line);
+        Dist2ToLine(i3, i0, coor, dist2Line);
+        dist2Elem = min(dist2Elem, dist2Line);
       }
 
       break;
     }
 
-    /*------------------------------------------------------------------------*/
+      /*------------------------------------------------------------------------*/
 
     case TETRAHEDRON:
     case PYRAMID:
@@ -643,83 +642,81 @@ void CADTElemClass::Dist2ToElement(const unsigned long elemID,
   }
 }
 
-bool CADTElemClass::CoorInTriangle(const unsigned long elemID,
-                                   const su2double     *coor,
-                                   su2double           *parCoor,
-                                   su2double           *weightsInterpol) const {
-
+bool CADTElemClass::CoorInTriangle(const unsigned long elemID, const su2double* coor, su2double* parCoor,
+                                   su2double* weightsInterpol) const {
   /* Determine the indices of the three vertices of the triangle,
      multiplied by nDim (which is 2). This gives the position in the
      coordinate array where the coordinates of these points are stored. */
   unsigned long i0 = nDOFsPerElem[elemID];
   unsigned long i1 = i0 + 1, i2 = i0 + 2;
-  i0 = nDim*elemConns[i0]; i1 = nDim*elemConns[i1]; i2 = nDim*elemConns[i2];
+  i0 = nDim * elemConns[i0];
+  i1 = nDim * elemConns[i1];
+  i2 = nDim * elemConns[i2];
 
   /* Determine the coordinates relative to the vertex 0. */
   const su2double xc = coor[0] - coorPoints[i0];
-  const su2double yc = coor[1] - coorPoints[i0+1];
+  const su2double yc = coor[1] - coorPoints[i0 + 1];
 
-  const su2double x1 = coorPoints[i1]   - coorPoints[i0];
-  const su2double y1 = coorPoints[i1+1] - coorPoints[i0+1];
+  const su2double x1 = coorPoints[i1] - coorPoints[i0];
+  const su2double y1 = coorPoints[i1 + 1] - coorPoints[i0 + 1];
 
-  const su2double x2 = coorPoints[i2]   - coorPoints[i0];
-  const su2double y2 = coorPoints[i2+1] - coorPoints[i0+1];
+  const su2double x2 = coorPoints[i2] - coorPoints[i0];
+  const su2double y2 = coorPoints[i2 + 1] - coorPoints[i0 + 1];
 
   /* The triangle is parametrized by X-X0 = (r+1)*(X1-X0)/2 + (s+1)*(X2-X0)/2,
      r, s >= -1, r+s <= 0. As this is a containment search, the number of
      dimesions is 2. As a consequence, the parametric coordinates r and s
      can be solved easily. Note that X0 is 0 in the above expression, because
      the coordinates are relative to node 0. */
-  const su2double detInv = 2.0/(x1*y2 - x2*y1);
-  parCoor[0] = detInv*(xc*y2 - yc*x2) - 1.0;
-  parCoor[1] = detInv*(yc*x1 - xc*y1) - 1.0;
+  const su2double detInv = 2.0 / (x1 * y2 - x2 * y1);
+  parCoor[0] = detInv * (xc * y2 - yc * x2) - 1.0;
+  parCoor[1] = detInv * (yc * x1 - xc * y1) - 1.0;
 
   /* Check if the point resides within the triangle and compute the
      interpolation weights if it is. */
   bool coorIsInside = false;
-  if((parCoor[0] >= paramLowerBound) && (parCoor[1] >= paramLowerBound) &&
-     ((parCoor[0]+parCoor[1]) <= tolInsideElem)) {
+  if ((parCoor[0] >= paramLowerBound) && (parCoor[1] >= paramLowerBound) &&
+      ((parCoor[0] + parCoor[1]) <= tolInsideElem)) {
     coorIsInside = true;
 
-    weightsInterpol[0] = -0.5*(parCoor[0] + parCoor[1]);
-    weightsInterpol[1] =  0.5*(parCoor[0] + 1.0);
-    weightsInterpol[2] =  0.5*(parCoor[1] + 1.0);
+    weightsInterpol[0] = -0.5 * (parCoor[0] + parCoor[1]);
+    weightsInterpol[1] = 0.5 * (parCoor[0] + 1.0);
+    weightsInterpol[2] = 0.5 * (parCoor[1] + 1.0);
   }
 
   /* Return the value of coorIsInside. */
   return coorIsInside;
 }
 
-bool CADTElemClass::CoorInQuadrilateral(const unsigned long elemID,
-                                        const su2double     *coor,
-                                        su2double           *parCoor,
-                                        su2double           *weightsInterpol) const {
-
+bool CADTElemClass::CoorInQuadrilateral(const unsigned long elemID, const su2double* coor, su2double* parCoor,
+                                        su2double* weightsInterpol) const {
   /* Definition of the maximum number of iterations in the Newton solver
      and the tolerance level. */
   const unsigned short maxIt = 50;
-  const su2double tolNewton  = 1.e-10;
+  const su2double tolNewton = 1.e-10;
 
   /* Determine the indices of the four vertices of the quadrilatral,
      multiplied by nDim (which is 2). This gives the position in the
      coordinate array where the coordinates of these points are stored. */
   unsigned long i0 = nDOFsPerElem[elemID];
-  unsigned long i1 = i0 + 1, i2 = i0 + 2, i3 = i0+3;
-  i0 = nDim*elemConns[i0]; i1 = nDim*elemConns[i1];
-  i2 = nDim*elemConns[i2]; i3 = nDim*elemConns[i3];
+  unsigned long i1 = i0 + 1, i2 = i0 + 2, i3 = i0 + 3;
+  i0 = nDim * elemConns[i0];
+  i1 = nDim * elemConns[i1];
+  i2 = nDim * elemConns[i2];
+  i3 = nDim * elemConns[i3];
 
   /* Determine the coordinates relative to the vertex 0. */
   const su2double xc = coor[0] - coorPoints[i0];
-  const su2double yc = coor[1] - coorPoints[i0+1];
+  const su2double yc = coor[1] - coorPoints[i0 + 1];
 
-  const su2double x1 = coorPoints[i1]   - coorPoints[i0];
-  const su2double y1 = coorPoints[i1+1] - coorPoints[i0+1];
+  const su2double x1 = coorPoints[i1] - coorPoints[i0];
+  const su2double y1 = coorPoints[i1 + 1] - coorPoints[i0 + 1];
 
-  const su2double x2 = coorPoints[i2]   - coorPoints[i0];
-  const su2double y2 = coorPoints[i2+1] - coorPoints[i0+1];
+  const su2double x2 = coorPoints[i2] - coorPoints[i0];
+  const su2double y2 = coorPoints[i2 + 1] - coorPoints[i0 + 1];
 
-  const su2double x3 = coorPoints[i3]   - coorPoints[i0];
-  const su2double y3 = coorPoints[i3+1] - coorPoints[i0+1];
+  const su2double x3 = coorPoints[i3] - coorPoints[i0];
+  const su2double y3 = coorPoints[i3 + 1] - coorPoints[i0 + 1];
 
   /* The parametrization of the quadrilatral is nonlinear, which requires an
      iterative algorithm. Especially for highly skewed quadrilaterals, this
@@ -727,29 +724,30 @@ bool CADTElemClass::CoorInQuadrilateral(const unsigned long elemID,
      linear triangles to check if the point is actually within the quad.
      First check the triangle i0-i1-i3. See CoorInTriangle for more details
      on this test. */
-  su2double detInv = 2.0/(x1*y3 - x3*y1);
-  parCoor[0] = detInv*(xc*y3 - yc*x3) - 1.0;
-  parCoor[1] = detInv*(yc*x1 - xc*y1) - 1.0;
+  su2double detInv = 2.0 / (x1 * y3 - x3 * y1);
+  parCoor[0] = detInv * (xc * y3 - yc * x3) - 1.0;
+  parCoor[1] = detInv * (yc * x1 - xc * y1) - 1.0;
 
   bool coorIsInside = false;
-  if((parCoor[0] >= paramLowerBound) && (parCoor[1] >= paramLowerBound) &&
-     ((parCoor[0]+parCoor[1]) <= tolInsideElem)) coorIsInside = true;
+  if ((parCoor[0] >= paramLowerBound) && (parCoor[1] >= paramLowerBound) &&
+      ((parCoor[0] + parCoor[1]) <= tolInsideElem))
+    coorIsInside = true;
 
   /* Check triangle i2-i3-i1 if the coordinate is not inside i0-i1-i3. */
-  if( !coorIsInside ) {
-
+  if (!coorIsInside) {
     /* Define the coordinates w.r.t. vertex 2 using the numbering i2-i3-i1. */
     const su2double xxc = xc - x2, yyc = yc - y2;
     const su2double xx1 = x3 - x2, yy1 = y3 - y2;
     const su2double xx3 = x1 - x2, yy3 = y1 - y2;
 
     /* Check if the coordinate is inside this triangle. */
-    detInv = 2.0/(xx1*yy3 - xx3*yy1);
-    parCoor[0] = detInv*(xxc*yy3 - yyc*xx3) - 1.0;
-    parCoor[1] = detInv*(yyc*xx1 - xxc*yy1) - 1.0;
+    detInv = 2.0 / (xx1 * yy3 - xx3 * yy1);
+    parCoor[0] = detInv * (xxc * yy3 - yyc * xx3) - 1.0;
+    parCoor[1] = detInv * (yyc * xx1 - xxc * yy1) - 1.0;
 
-    if((parCoor[0] >= paramLowerBound) && (parCoor[1] >= paramLowerBound) &&
-       ((parCoor[0]+parCoor[1]) <= tolInsideElem)) coorIsInside = true;
+    if ((parCoor[0] >= paramLowerBound) && (parCoor[1] >= paramLowerBound) &&
+        ((parCoor[0] + parCoor[1]) <= tolInsideElem))
+      coorIsInside = true;
 
     /* Convert the parametric coordinates to the ones used by the
        quadrilatral i0-i1-i2-i3. They serve as initial guess below. */
@@ -758,7 +756,7 @@ bool CADTElemClass::CoorInQuadrilateral(const unsigned long elemID,
   }
 
   /* If the coordinate is in neither triangle, return false. */
-  if( !coorIsInside ) return false;
+  if (!coorIsInside) return false;
 
   /* The coordinate is inside the quadrilatral and an initial guess has been
      obtained by splitting the quad into two triangles. Carry out a Newton
@@ -770,27 +768,26 @@ bool CADTElemClass::CoorInQuadrilateral(const unsigned long elemID,
      V0 - r*V1 - s*V2 - r*s*V3 = 0, where V0 = xc - (x1+x2+x3)/4,
      V1 = (x1+x2-x3)/4, V2 = (x2+x3-X1)/4, V3 = (x2-x1-x3)/4. First
      construct the vectors V0, V1, V2 and V3. */
-  const su2double V0x = xc - 0.25*(x1+x2+x3), V0y = yc - 0.25*(y1+y2+y3);
-  const su2double V1x =      0.25*(x1+x2-x3), V1y =      0.25*(y1+y2-y3);
-  const su2double V2x =      0.25*(x2+x3-x1), V2y =      0.25*(y2+y3-y1);
-  const su2double V3x =      0.25*(x2-x1-x3), V3y =      0.25*(y2-y1-y3);
+  const su2double V0x = xc - 0.25 * (x1 + x2 + x3), V0y = yc - 0.25 * (y1 + y2 + y3);
+  const su2double V1x = 0.25 * (x1 + x2 - x3), V1y = 0.25 * (y1 + y2 - y3);
+  const su2double V2x = 0.25 * (x2 + x3 - x1), V2y = 0.25 * (y2 + y3 - y1);
+  const su2double V3x = 0.25 * (x2 - x1 - x3), V3y = 0.25 * (y2 - y1 - y3);
 
   /* Loop over the maximum number of iterations. */
   unsigned short itCount;
-  for(itCount=0; itCount<maxIt; ++itCount) {
-
+  for (itCount = 0; itCount < maxIt; ++itCount) {
     /* Compute the values of the nonlinear functions. */
-    const su2double f0 = V0x - parCoor[0]*V1x - parCoor[1]*V2x - parCoor[0]*parCoor[1]*V3x;
-    const su2double f1 = V0y - parCoor[0]*V1y - parCoor[1]*V2y - parCoor[0]*parCoor[1]*V3y;
+    const su2double f0 = V0x - parCoor[0] * V1x - parCoor[1] * V2x - parCoor[0] * parCoor[1] * V3x;
+    const su2double f1 = V0y - parCoor[0] * V1y - parCoor[1] * V2y - parCoor[0] * parCoor[1] * V3y;
 
     /* Compute the negative of the Jacobian matrix. */
-    const su2double a00 = V1x + parCoor[1]*V3x, a01 = V2x + parCoor[0]*V3x;
-    const su2double a10 = V1y + parCoor[1]*V3y, a11 = V2y + parCoor[0]*V3y;
+    const su2double a00 = V1x + parCoor[1] * V3x, a01 = V2x + parCoor[0] * V3x;
+    const su2double a10 = V1y + parCoor[1] * V3y, a11 = V2y + parCoor[0] * V3y;
 
     /* Compute the update of the parametric coordinates. */
-    detInv = 1.0/(a00*a11 - a01*a10);
-    const su2double dr = detInv*(f0*a11 - f1*a01);
-    const su2double ds = detInv*(f1*a00 - f0*a10);
+    detInv = 1.0 / (a00 * a11 - a01 * a10);
+    const su2double dr = detInv * (f0 * a11 - f1 * a01);
+    const su2double ds = detInv * (f1 * a00 - f0 * a10);
 
     /* Update the parametric coordinates. Note that the negative of the
        Jacobian is used, so the update must be added. */
@@ -798,138 +795,136 @@ bool CADTElemClass::CoorInQuadrilateral(const unsigned long elemID,
     parCoor[1] += ds;
 
     /* Check for convergence. */
-    if(fabs(dr) <= tolNewton && fabs(ds) <= tolNewton) break;
+    if (fabs(dr) <= tolNewton && fabs(ds) <= tolNewton) break;
   }
 
   /* Terminate if the Newton algorithm did not converge. */
-  if(itCount == maxIt)
-    SU2_MPI::Error("Newton did not converge", CURRENT_FUNCTION);
+  if (itCount == maxIt) SU2_MPI::Error("Newton did not converge", CURRENT_FUNCTION);
 
   /* Check if the parametric coordinates are inside the quadrilateral.
      If not, something is seriously wrong, because the inside test has been
      done already with the triangles. */
-  if(parCoor[0] < paramLowerBound || parCoor[0] > paramUpperBound ||
-     parCoor[1] < paramLowerBound || parCoor[1] > paramUpperBound)
+  if (parCoor[0] < paramLowerBound || parCoor[0] > paramUpperBound || parCoor[1] < paramLowerBound ||
+      parCoor[1] > paramUpperBound)
     SU2_MPI::Error("Point not inside the quadrilateral.", CURRENT_FUNCTION);
 
   /* Compute the interpolation weights. */
-  const su2double omr = 0.5*(1.0-parCoor[0]), opr = 0.5*(1.0+parCoor[0]);
-  const su2double oms = 0.5*(1.0-parCoor[1]), ops = 0.5*(1.0+parCoor[1]);
+  const su2double omr = 0.5 * (1.0 - parCoor[0]), opr = 0.5 * (1.0 + parCoor[0]);
+  const su2double oms = 0.5 * (1.0 - parCoor[1]), ops = 0.5 * (1.0 + parCoor[1]);
 
-  weightsInterpol[0] = omr*oms;
-  weightsInterpol[1] = opr*oms;
-  weightsInterpol[2] = opr*ops;
-  weightsInterpol[3] = omr*ops;
+  weightsInterpol[0] = omr * oms;
+  weightsInterpol[1] = opr * oms;
+  weightsInterpol[2] = opr * ops;
+  weightsInterpol[3] = omr * ops;
 
   /* Return true, because the search was successful. */
   return true;
 }
 
-bool CADTElemClass::CoorInTetrahedron(const unsigned long elemID,
-                                      const su2double     *coor,
-                                      su2double           *parCoor,
-                                      su2double           *weightsInterpol) const {
-
+bool CADTElemClass::CoorInTetrahedron(const unsigned long elemID, const su2double* coor, su2double* parCoor,
+                                      su2double* weightsInterpol) const {
   /* Determine the indices of the four vertices of the tetrahedron,
      multiplied by nDim (which is 3). This gives the position in the
      coordinate array where the coordinates of these points are stored. */
   unsigned long i0 = nDOFsPerElem[elemID];
-  unsigned long i1 = i0 + 1, i2 = i0 + 2, i3 = i0+3;
-  i0 = nDim*elemConns[i0]; i1 = nDim*elemConns[i1];
-  i2 = nDim*elemConns[i2]; i3 = nDim*elemConns[i3];
+  unsigned long i1 = i0 + 1, i2 = i0 + 2, i3 = i0 + 3;
+  i0 = nDim * elemConns[i0];
+  i1 = nDim * elemConns[i1];
+  i2 = nDim * elemConns[i2];
+  i3 = nDim * elemConns[i3];
 
   /* Determine the coordinates relative to the vertex 0. */
   const su2double xc = coor[0] - coorPoints[i0];
-  const su2double yc = coor[1] - coorPoints[i0+1];
-  const su2double zc = coor[2] - coorPoints[i0+2];
+  const su2double yc = coor[1] - coorPoints[i0 + 1];
+  const su2double zc = coor[2] - coorPoints[i0 + 2];
 
-  const su2double x1 = coorPoints[i1]   - coorPoints[i0];
-  const su2double y1 = coorPoints[i1+1] - coorPoints[i0+1];
-  const su2double z1 = coorPoints[i1+2] - coorPoints[i0+2];
+  const su2double x1 = coorPoints[i1] - coorPoints[i0];
+  const su2double y1 = coorPoints[i1 + 1] - coorPoints[i0 + 1];
+  const su2double z1 = coorPoints[i1 + 2] - coorPoints[i0 + 2];
 
-  const su2double x2 = coorPoints[i2]   - coorPoints[i0];
-  const su2double y2 = coorPoints[i2+1] - coorPoints[i0+1];
-  const su2double z2 = coorPoints[i2+2] - coorPoints[i0+2];
+  const su2double x2 = coorPoints[i2] - coorPoints[i0];
+  const su2double y2 = coorPoints[i2 + 1] - coorPoints[i0 + 1];
+  const su2double z2 = coorPoints[i2 + 2] - coorPoints[i0 + 2];
 
-  const su2double x3 = coorPoints[i3]   - coorPoints[i0];
-  const su2double y3 = coorPoints[i3+1] - coorPoints[i0+1];
-  const su2double z3 = coorPoints[i3+2] - coorPoints[i0+2];
+  const su2double x3 = coorPoints[i3] - coorPoints[i0];
+  const su2double y3 = coorPoints[i3 + 1] - coorPoints[i0 + 1];
+  const su2double z3 = coorPoints[i3 + 2] - coorPoints[i0 + 2];
 
   /* The tetrahedron is parametrized by
      X-X0 = (r+1)*(X1-X0)/2 + (s+1)*(X2-X0)/2 + (t+1)*(X3-X0)/2,
      r, s, t >= -1, r+s+t <= -1. As a consequence, the parametric coordinates
      r, s and t can be solved easily. Note that X0 is 0 in the above expression,
      because the coordinates are relative to node 0. */
-  const su2double detInv = 2.0/(x1*y2*z3 - x1*y3*z2 - x2*y1*z3 + x2*y3*z1 + x3*y1*z2 - x3*y2*z1);
-  parCoor[0] =  detInv*(x2*y3*zc - x2*yc*z3 - x3*y2*zc + x3*yc*z2 + xc*y2*z3 - xc*y3*z2) - 1.0;
-  parCoor[1] = -detInv*(x1*y3*zc - x1*yc*z3 - x3*y1*zc + x3*yc*z1 + xc*y1*z3 - xc*y3*z1) - 1.0;
-  parCoor[2] =  detInv*(x1*y2*zc - x1*yc*z2 - x2*y1*zc + x2*yc*z1 + xc*y1*z2 - xc*y2*z1) - 1.0;
+  const su2double detInv =
+      2.0 / (x1 * y2 * z3 - x1 * y3 * z2 - x2 * y1 * z3 + x2 * y3 * z1 + x3 * y1 * z2 - x3 * y2 * z1);
+  parCoor[0] = detInv * (x2 * y3 * zc - x2 * yc * z3 - x3 * y2 * zc + x3 * yc * z2 + xc * y2 * z3 - xc * y3 * z2) - 1.0;
+  parCoor[1] =
+      -detInv * (x1 * y3 * zc - x1 * yc * z3 - x3 * y1 * zc + x3 * yc * z1 + xc * y1 * z3 - xc * y3 * z1) - 1.0;
+  parCoor[2] = detInv * (x1 * y2 * zc - x1 * yc * z2 - x2 * y1 * zc + x2 * yc * z1 + xc * y1 * z2 - xc * y2 * z1) - 1.0;
 
   /* Check if the point resides within the tetrahedron and compute the
      interpolation weights if it is. */
   bool coorIsInside = false;
-  if((parCoor[0] >= paramLowerBound) && (parCoor[1] >= paramLowerBound) &&
-     (parCoor[2] >= paramLowerBound) &&
-     ((parCoor[0]+parCoor[1]+parCoor[2]) <= paramLowerBound)) {
+  if ((parCoor[0] >= paramLowerBound) && (parCoor[1] >= paramLowerBound) && (parCoor[2] >= paramLowerBound) &&
+      ((parCoor[0] + parCoor[1] + parCoor[2]) <= paramLowerBound)) {
     coorIsInside = true;
 
-    weightsInterpol[0] = -0.5*(parCoor[0] + parCoor[1] + parCoor[2] + 1.0);
-    weightsInterpol[1] =  0.5*(parCoor[0] + 1.0);
-    weightsInterpol[2] =  0.5*(parCoor[1] + 1.0);
-    weightsInterpol[3] =  0.5*(parCoor[2] + 1.0);
+    weightsInterpol[0] = -0.5 * (parCoor[0] + parCoor[1] + parCoor[2] + 1.0);
+    weightsInterpol[1] = 0.5 * (parCoor[0] + 1.0);
+    weightsInterpol[2] = 0.5 * (parCoor[1] + 1.0);
+    weightsInterpol[3] = 0.5 * (parCoor[2] + 1.0);
   }
 
   /* Return the value of coorIsInside. */
   return coorIsInside;
 }
 
-bool CADTElemClass::CoorInPyramid(const unsigned long elemID,
-                                  const su2double     *coor,
-                                  su2double           *parCoor,
-                                  su2double           *weightsInterpol) const {
-
+bool CADTElemClass::CoorInPyramid(const unsigned long elemID, const su2double* coor, su2double* parCoor,
+                                  su2double* weightsInterpol) const {
   /* Definition of the maximum number of iterations in the Newton solver
      and the tolerance level. */
   const unsigned short maxIt = 50;
-  const su2double tolNewton  = 1.e-10;
+  const su2double tolNewton = 1.e-10;
 
   /* Determine the indices of the five vertices of the pyramid,
      multiplied by nDim (which is 3). This gives the position in the
      coordinate array where the coordinates of these points are stored. */
   unsigned long i0 = nDOFsPerElem[elemID];
-  unsigned long i1 = i0 + 1, i2 = i0 + 2, i3 = i0+3, i4 = i0+4;
-  i0 = nDim*elemConns[i0]; i1 = nDim*elemConns[i1];
-  i2 = nDim*elemConns[i2]; i3 = nDim*elemConns[i3];
-  i4 = nDim*elemConns[i4];
+  unsigned long i1 = i0 + 1, i2 = i0 + 2, i3 = i0 + 3, i4 = i0 + 4;
+  i0 = nDim * elemConns[i0];
+  i1 = nDim * elemConns[i1];
+  i2 = nDim * elemConns[i2];
+  i3 = nDim * elemConns[i3];
+  i4 = nDim * elemConns[i4];
 
   /* Determine the coordinates relative to the vertex 0. */
   su2double xRel[5][3], xc[3];
   xc[0] = coor[0] - coorPoints[i0];
-  xc[1] = coor[1] - coorPoints[i0+1];
-  xc[2] = coor[2] - coorPoints[i0+2];
+  xc[1] = coor[1] - coorPoints[i0 + 1];
+  xc[2] = coor[2] - coorPoints[i0 + 2];
 
   xRel[0][0] = xRel[0][1] = xRel[0][2] = 0.0;
 
-  xRel[1][0] = coorPoints[i1]   - coorPoints[i0];
-  xRel[1][1] = coorPoints[i1+1] - coorPoints[i0+1];
-  xRel[1][2] = coorPoints[i1+2] - coorPoints[i0+2];
+  xRel[1][0] = coorPoints[i1] - coorPoints[i0];
+  xRel[1][1] = coorPoints[i1 + 1] - coorPoints[i0 + 1];
+  xRel[1][2] = coorPoints[i1 + 2] - coorPoints[i0 + 2];
 
-  xRel[2][0] = coorPoints[i2]   - coorPoints[i0];
-  xRel[2][1] = coorPoints[i2+1] - coorPoints[i0+1];
-  xRel[2][2] = coorPoints[i2+2] - coorPoints[i0+2];
+  xRel[2][0] = coorPoints[i2] - coorPoints[i0];
+  xRel[2][1] = coorPoints[i2 + 1] - coorPoints[i0 + 1];
+  xRel[2][2] = coorPoints[i2 + 2] - coorPoints[i0 + 2];
 
-  xRel[3][0] = coorPoints[i3]   - coorPoints[i0];
-  xRel[3][1] = coorPoints[i3+1] - coorPoints[i0+1];
-  xRel[3][2] = coorPoints[i3+2] - coorPoints[i0+2];
+  xRel[3][0] = coorPoints[i3] - coorPoints[i0];
+  xRel[3][1] = coorPoints[i3 + 1] - coorPoints[i0 + 1];
+  xRel[3][2] = coorPoints[i3 + 2] - coorPoints[i0 + 2];
 
-  xRel[4][0] = coorPoints[i4]   - coorPoints[i0];
-  xRel[4][1] = coorPoints[i4+1] - coorPoints[i0+1];
-  xRel[4][2] = coorPoints[i4+2] - coorPoints[i0+2];
+  xRel[4][0] = coorPoints[i4] - coorPoints[i0];
+  xRel[4][1] = coorPoints[i4 + 1] - coorPoints[i0 + 1];
+  xRel[4][2] = coorPoints[i4 + 2] - coorPoints[i0 + 2];
 
   /* Obtain an initial guess of the parametric coordinates by splitting the
      pyramid into tetrahedra. If this approach is not successful, this means
      that the point is not inside the true pyramid and false can be returned. */
-  if( !InitialGuessContainmentPyramid(xc, xRel, parCoor) ) return false;
+  if (!InitialGuessContainmentPyramid(xc, xRel, parCoor)) return false;
 
   /* The pyramid is parametrized by X-X0 = (Xi-X0)*li, where the sum runs over
      i = 0..4, although i = 0 does not give a contribution. The Lagrangian
@@ -943,67 +938,68 @@ bool CADTElemClass::CoorInPyramid(const unsigned long elemID,
      V0 - V1*r - V2*s - V3*t - V4*r*s/(1-t)  = 0, where
      V0 = xc - (4*x4+x1+x2+x3)/8, V1 = (x1+x2-x3)/4, V2 = (x2+x3-X1)/4,
      V3 = (4*X4-x1-x2-x3)/8, V4 = (x2-x1-x3)/2. First construct these vectors. */
-  const su2double V0x = xc[0] - 0.5*xRel[4][0] - 0.125*(xRel[1][0]+xRel[2][0]+xRel[3][0]);
-  const su2double V0y = xc[1] - 0.5*xRel[4][1] - 0.125*(xRel[1][1]+xRel[2][1]+xRel[3][1]);
-  const su2double V0z = xc[2] - 0.5*xRel[4][2] - 0.125*(xRel[1][2]+xRel[2][2]+xRel[3][2]);
+  const su2double V0x = xc[0] - 0.5 * xRel[4][0] - 0.125 * (xRel[1][0] + xRel[2][0] + xRel[3][0]);
+  const su2double V0y = xc[1] - 0.5 * xRel[4][1] - 0.125 * (xRel[1][1] + xRel[2][1] + xRel[3][1]);
+  const su2double V0z = xc[2] - 0.5 * xRel[4][2] - 0.125 * (xRel[1][2] + xRel[2][2] + xRel[3][2]);
 
-  const su2double V1x = 0.25*(xRel[1][0]+xRel[2][0]-xRel[3][0]);
-  const su2double V1y = 0.25*(xRel[1][1]+xRel[2][1]-xRel[3][1]);
-  const su2double V1z = 0.25*(xRel[1][2]+xRel[2][2]-xRel[3][2]);
+  const su2double V1x = 0.25 * (xRel[1][0] + xRel[2][0] - xRel[3][0]);
+  const su2double V1y = 0.25 * (xRel[1][1] + xRel[2][1] - xRel[3][1]);
+  const su2double V1z = 0.25 * (xRel[1][2] + xRel[2][2] - xRel[3][2]);
 
-  const su2double V2x = 0.25*(xRel[2][0]+xRel[3][0]-xRel[1][0]);
-  const su2double V2y = 0.25*(xRel[2][1]+xRel[3][1]-xRel[1][1]);
-  const su2double V2z = 0.25*(xRel[2][2]+xRel[3][2]-xRel[1][2]);
+  const su2double V2x = 0.25 * (xRel[2][0] + xRel[3][0] - xRel[1][0]);
+  const su2double V2y = 0.25 * (xRel[2][1] + xRel[3][1] - xRel[1][1]);
+  const su2double V2z = 0.25 * (xRel[2][2] + xRel[3][2] - xRel[1][2]);
 
-  const su2double V3x = 0.5*xRel[4][0] - 0.125*(xRel[1][0]+xRel[2][0]+xRel[3][0]);
-  const su2double V3y = 0.5*xRel[4][1] - 0.125*(xRel[1][1]+xRel[2][1]+xRel[3][1]);
-  const su2double V3z = 0.5*xRel[4][2] - 0.125*(xRel[1][2]+xRel[2][2]+xRel[3][2]);
+  const su2double V3x = 0.5 * xRel[4][0] - 0.125 * (xRel[1][0] + xRel[2][0] + xRel[3][0]);
+  const su2double V3y = 0.5 * xRel[4][1] - 0.125 * (xRel[1][1] + xRel[2][1] + xRel[3][1]);
+  const su2double V3z = 0.5 * xRel[4][2] - 0.125 * (xRel[1][2] + xRel[2][2] + xRel[3][2]);
 
-  const su2double V4x = 0.5*(xRel[2][0]-xRel[1][0]-xRel[3][0]);
-  const su2double V4y = 0.5*(xRel[2][1]-xRel[1][1]-xRel[3][1]);
-  const su2double V4z = 0.5*(xRel[2][2]-xRel[1][2]-xRel[3][2]);
+  const su2double V4x = 0.5 * (xRel[2][0] - xRel[1][0] - xRel[3][0]);
+  const su2double V4y = 0.5 * (xRel[2][1] - xRel[1][1] - xRel[3][1]);
+  const su2double V4z = 0.5 * (xRel[2][2] - xRel[1][2] - xRel[3][2]);
 
   /* Loop over the maximum number of iterations. */
   unsigned short itCount;
-  for(itCount=0; itCount<maxIt; ++itCount) {
-
+  for (itCount = 0; itCount < maxIt; ++itCount) {
     /* Compute the values of the nonlinear functions. */
     su2double oneMinT = 1.0 - parCoor[2];
-    if(fabs(oneMinT) < 1.e-10) {
-      if(oneMinT < 0.0) oneMinT = -1.e-10;
-      else              oneMinT =  1.e-10;
+    if (fabs(oneMinT) < 1.e-10) {
+      if (oneMinT < 0.0)
+        oneMinT = -1.e-10;
+      else
+        oneMinT = 1.e-10;
     }
-    const su2double oneMinTInv = 1.0/oneMinT;
+    const su2double oneMinTInv = 1.0 / oneMinT;
 
-    const su2double f0 = V0x - parCoor[0]*V1x - parCoor[1]*V2x - parCoor[2]*V3x
-                       - parCoor[0]*parCoor[1]*V4x*oneMinTInv;
-    const su2double f1 = V0y - parCoor[0]*V1y - parCoor[1]*V2y - parCoor[2]*V3y
-                       - parCoor[0]*parCoor[1]*V4y*oneMinTInv;
-    const su2double f2 = V0z - parCoor[0]*V1z - parCoor[1]*V2z - parCoor[2]*V3z
-                       - parCoor[0]*parCoor[1]*V4z*oneMinTInv;
+    const su2double f0 =
+        V0x - parCoor[0] * V1x - parCoor[1] * V2x - parCoor[2] * V3x - parCoor[0] * parCoor[1] * V4x * oneMinTInv;
+    const su2double f1 =
+        V0y - parCoor[0] * V1y - parCoor[1] * V2y - parCoor[2] * V3y - parCoor[0] * parCoor[1] * V4y * oneMinTInv;
+    const su2double f2 =
+        V0z - parCoor[0] * V1z - parCoor[1] * V2z - parCoor[2] * V3z - parCoor[0] * parCoor[1] * V4z * oneMinTInv;
 
     /* Compute the negative of the Jacobian matrix. */
-    const su2double a00 = V1x + parCoor[1]*V4x*oneMinTInv;
-    const su2double a01 = V2x + parCoor[0]*V4x*oneMinTInv;
-    const su2double a02 = V3x + parCoor[0]*parCoor[1]*V4x*oneMinTInv*oneMinTInv;
+    const su2double a00 = V1x + parCoor[1] * V4x * oneMinTInv;
+    const su2double a01 = V2x + parCoor[0] * V4x * oneMinTInv;
+    const su2double a02 = V3x + parCoor[0] * parCoor[1] * V4x * oneMinTInv * oneMinTInv;
 
-    const su2double a10 = V1y + parCoor[1]*V4y*oneMinTInv;
-    const su2double a11 = V2y + parCoor[0]*V4y*oneMinTInv;
-    const su2double a12 = V3y + parCoor[0]*parCoor[1]*V4y*oneMinTInv*oneMinTInv;
+    const su2double a10 = V1y + parCoor[1] * V4y * oneMinTInv;
+    const su2double a11 = V2y + parCoor[0] * V4y * oneMinTInv;
+    const su2double a12 = V3y + parCoor[0] * parCoor[1] * V4y * oneMinTInv * oneMinTInv;
 
-    const su2double a20 = V1z + parCoor[1]*V4z*oneMinTInv;
-    const su2double a21 = V2z + parCoor[0]*V4z*oneMinTInv;
-    const su2double a22 = V3z + parCoor[0]*parCoor[1]*V4z*oneMinTInv*oneMinTInv;
+    const su2double a20 = V1z + parCoor[1] * V4z * oneMinTInv;
+    const su2double a21 = V2z + parCoor[0] * V4z * oneMinTInv;
+    const su2double a22 = V3z + parCoor[0] * parCoor[1] * V4z * oneMinTInv * oneMinTInv;
 
     /* Compute the update of the parametric coordinates. */
-    const su2double detInv = 1.0/(a00*a11*a22 - a00*a12*a21 - a01*a10*a22
-                           +      a01*a12*a20 + a02*a10*a21 - a02*a11*a20);
-    const su2double dr =  detInv*(a01*a12*f2 - a01*a22*f1 - a02*a11*f2
-                       +          a02*a21*f1 + a11*a22*f0 - a12*a21*f0);
-    const su2double ds = -detInv*(a00*a12*f2 - a00*a22*f1 - a02*a10*f2
-                       +          a02*a20*f1 + a10*a22*f0 - a12*a20*f0);
-    const su2double dt =  detInv*(a00*a11*f2 - a00*a21*f1 - a01*a10*f2
-                       +          a01*a20*f1 + a10*a21*f0 - a11*a20*f0);
+    const su2double detInv = 1.0 / (a00 * a11 * a22 - a00 * a12 * a21 - a01 * a10 * a22 + a01 * a12 * a20 +
+                                    a02 * a10 * a21 - a02 * a11 * a20);
+    const su2double dr =
+        detInv * (a01 * a12 * f2 - a01 * a22 * f1 - a02 * a11 * f2 + a02 * a21 * f1 + a11 * a22 * f0 - a12 * a21 * f0);
+    const su2double ds =
+        -detInv * (a00 * a12 * f2 - a00 * a22 * f1 - a02 * a10 * f2 + a02 * a20 * f1 + a10 * a22 * f0 - a12 * a20 * f0);
+    const su2double dt =
+        detInv * (a00 * a11 * f2 - a00 * a21 * f1 - a01 * a10 * f2 + a01 * a20 * f1 + a10 * a21 * f0 - a11 * a20 * f0);
 
     /* Update the parametric coordinates. Note that the negative of the
        Jacobian is used, so the update must be added. */
@@ -1012,41 +1008,42 @@ bool CADTElemClass::CoorInPyramid(const unsigned long elemID,
     parCoor[2] += dt;
 
     /* Check for convergence. */
-    if(fabs(dr) <= tolNewton && fabs(ds) <= tolNewton && fabs(dt) <= tolNewton) break;
+    if (fabs(dr) <= tolNewton && fabs(ds) <= tolNewton && fabs(dt) <= tolNewton) break;
   }
 
   /* Terminate if the Newton algorithm did not converge. */
-  if(itCount == maxIt)
-    SU2_MPI::Error("Newton did not converge", CURRENT_FUNCTION);
+  if (itCount == maxIt) SU2_MPI::Error("Newton did not converge", CURRENT_FUNCTION);
 
   /* Check if the point resides within the pyramid and compute the
      interpolation weights if it is. */
   bool coorIsInside = false;
-  if((parCoor[2] >= paramLowerBound) && (parCoor[2] <= paramUpperBound)) {
-    const su2double lowRSBound = 0.5*(parCoor[2]-1.0) - tolInsideElem;
+  if ((parCoor[2] >= paramLowerBound) && (parCoor[2] <= paramUpperBound)) {
+    const su2double lowRSBound = 0.5 * (parCoor[2] - 1.0) - tolInsideElem;
     const su2double uppRSBound = -lowRSBound;
 
-    if((parCoor[0] >= lowRSBound) && (parCoor[0] <= uppRSBound) &&
-       (parCoor[1] >= lowRSBound) && (parCoor[1] <= uppRSBound)) {
+    if ((parCoor[0] >= lowRSBound) && (parCoor[0] <= uppRSBound) && (parCoor[1] >= lowRSBound) &&
+        (parCoor[1] <= uppRSBound)) {
       coorIsInside = true;
 
       su2double oneMinT = 1.0 - parCoor[2];
-      if(fabs(oneMinT) < 1.e-10) {
-        if(oneMinT < 0.0) oneMinT = -1.e-10;
-        else              oneMinT =  1.e-10;
+      if (fabs(oneMinT) < 1.e-10) {
+        if (oneMinT < 0.0)
+          oneMinT = -1.e-10;
+        else
+          oneMinT = 1.e-10;
       }
-      const su2double oneMinTInv = 1.0/oneMinT;
-
-      const su2double omr = (1.0-parCoor[2]-2.0*parCoor[0]);
-      const su2double opr = (1.0-parCoor[2]+2.0*parCoor[0]);
-      const su2double oms = (1.0-parCoor[2]-2.0*parCoor[1]);
-      const su2double ops = (1.0-parCoor[2]+2.0*parCoor[1]);
-
-      weightsInterpol[0] = 0.125*oneMinTInv*omr*oms;
-      weightsInterpol[1] = 0.125*oneMinTInv*opr*oms;
-      weightsInterpol[2] = 0.125*oneMinTInv*opr*ops;
-      weightsInterpol[3] = 0.125*oneMinTInv*omr*ops;
-      weightsInterpol[4] = 0.5*(1.0+parCoor[2]);
+      const su2double oneMinTInv = 1.0 / oneMinT;
+
+      const su2double omr = (1.0 - parCoor[2] - 2.0 * parCoor[0]);
+      const su2double opr = (1.0 - parCoor[2] + 2.0 * parCoor[0]);
+      const su2double oms = (1.0 - parCoor[2] - 2.0 * parCoor[1]);
+      const su2double ops = (1.0 - parCoor[2] + 2.0 * parCoor[1]);
+
+      weightsInterpol[0] = 0.125 * oneMinTInv * omr * oms;
+      weightsInterpol[1] = 0.125 * oneMinTInv * opr * oms;
+      weightsInterpol[2] = 0.125 * oneMinTInv * opr * ops;
+      weightsInterpol[3] = 0.125 * oneMinTInv * omr * ops;
+      weightsInterpol[4] = 0.5 * (1.0 + parCoor[2]);
     }
   }
 
@@ -1054,9 +1051,8 @@ bool CADTElemClass::CoorInPyramid(const unsigned long elemID,
   return coorIsInside;
 }
 
-bool CADTElemClass::InitialGuessContainmentPyramid(const su2double xRelC[3],
-                                                   const su2double xRel[5][3],
-                                                   su2double       *parCoor) const {
+bool CADTElemClass::InitialGuessContainmentPyramid(const su2double xRelC[3], const su2double xRel[5][3],
+                                                   su2double* parCoor) const {
   /* Tetrahedron, 0-1-3-4.
      Create the coordinates of the tetrahedron and of the point. */
   su2double x1 = xRel[1][0], y1 = xRel[1][1], z1 = xRel[1][2];
@@ -1066,35 +1062,44 @@ bool CADTElemClass::InitialGuessContainmentPyramid(const su2double xRelC[3],
   su2double xc = xRelC[0], yc = xRelC[1], zc = xRelC[2];
 
   /* Determine the parametric coordinates inside this tetrahedron. */
-  su2double detInv = 2.0/(x1*y2*z3 - x1*y3*z2 - x2*y1*z3 + x2*y3*z1 + x3*y1*z2 - x3*y2*z1);
-  parCoor[0] =  detInv*(x2*y3*zc - x2*yc*z3 - x3*y2*zc + x3*yc*z2 + xc*y2*z3 - xc*y3*z2) - 1.0;
-  parCoor[1] = -detInv*(x1*y3*zc - x1*yc*z3 - x3*y1*zc + x3*yc*z1 + xc*y1*z3 - xc*y3*z1) - 1.0;
-  parCoor[2] =  detInv*(x1*y2*zc - x1*yc*z2 - x2*y1*zc + x2*yc*z1 + xc*y1*z2 - xc*y2*z1) - 1.0;
+  su2double detInv = 2.0 / (x1 * y2 * z3 - x1 * y3 * z2 - x2 * y1 * z3 + x2 * y3 * z1 + x3 * y1 * z2 - x3 * y2 * z1);
+  parCoor[0] = detInv * (x2 * y3 * zc - x2 * yc * z3 - x3 * y2 * zc + x3 * yc * z2 + xc * y2 * z3 - xc * y3 * z2) - 1.0;
+  parCoor[1] =
+      -detInv * (x1 * y3 * zc - x1 * yc * z3 - x3 * y1 * zc + x3 * yc * z1 + xc * y1 * z3 - xc * y3 * z1) - 1.0;
+  parCoor[2] = detInv * (x1 * y2 * zc - x1 * yc * z2 - x2 * y1 * zc + x2 * yc * z1 + xc * y1 * z2 - xc * y2 * z1) - 1.0;
 
   /* If the point is inside this tetrahedron, return true. */
-  if((parCoor[0] >= paramLowerBound) && (parCoor[1] >= paramLowerBound) &&
-     (parCoor[2] >= paramLowerBound) &&
-     ((parCoor[0]+parCoor[1]+parCoor[2]) <= paramLowerBound)) return true;
+  if ((parCoor[0] >= paramLowerBound) && (parCoor[1] >= paramLowerBound) && (parCoor[2] >= paramLowerBound) &&
+      ((parCoor[0] + parCoor[1] + parCoor[2]) <= paramLowerBound))
+    return true;
 
   /* Tetrahedron, 2-3-1-4.
      Create the coordinates of the tetrahedron and of the point. */
-  x1 = xRel[3][0]-xRel[2][0]; y1 = xRel[3][1]-xRel[2][1]; z1 = xRel[3][2]-xRel[2][2];
-  x2 = xRel[1][0]-xRel[2][0]; y2 = xRel[1][1]-xRel[2][1]; z2 = xRel[1][2]-xRel[2][2];
-  x3 = xRel[4][0]-xRel[2][0]; y3 = xRel[4][1]-xRel[2][1]; z3 = xRel[4][2]-xRel[2][2];
-
-  xc = xRelC[0]-xRel[2][0]; yc = xRelC[1]-xRel[2][1]; zc = xRelC[2]-xRel[2][2];
+  x1 = xRel[3][0] - xRel[2][0];
+  y1 = xRel[3][1] - xRel[2][1];
+  z1 = xRel[3][2] - xRel[2][2];
+  x2 = xRel[1][0] - xRel[2][0];
+  y2 = xRel[1][1] - xRel[2][1];
+  z2 = xRel[1][2] - xRel[2][2];
+  x3 = xRel[4][0] - xRel[2][0];
+  y3 = xRel[4][1] - xRel[2][1];
+  z3 = xRel[4][2] - xRel[2][2];
+
+  xc = xRelC[0] - xRel[2][0];
+  yc = xRelC[1] - xRel[2][1];
+  zc = xRelC[2] - xRel[2][2];
 
   /* Determine the parametric coordinates inside this tetrahedron. */
-  detInv = 2.0/(x1*y2*z3 - x1*y3*z2 - x2*y1*z3 + x2*y3*z1 + x3*y1*z2 - x3*y2*z1);
-  parCoor[0] =  detInv*(x2*y3*zc - x2*yc*z3 - x3*y2*zc + x3*yc*z2 + xc*y2*z3 - xc*y3*z2) - 1.0;
-  parCoor[1] = -detInv*(x1*y3*zc - x1*yc*z3 - x3*y1*zc + x3*yc*z1 + xc*y1*z3 - xc*y3*z1) - 1.0;
-  parCoor[2] =  detInv*(x1*y2*zc - x1*yc*z2 - x2*y1*zc + x2*yc*z1 + xc*y1*z2 - xc*y2*z1) - 1.0;
+  detInv = 2.0 / (x1 * y2 * z3 - x1 * y3 * z2 - x2 * y1 * z3 + x2 * y3 * z1 + x3 * y1 * z2 - x3 * y2 * z1);
+  parCoor[0] = detInv * (x2 * y3 * zc - x2 * yc * z3 - x3 * y2 * zc + x3 * yc * z2 + xc * y2 * z3 - xc * y3 * z2) - 1.0;
+  parCoor[1] =
+      -detInv * (x1 * y3 * zc - x1 * yc * z3 - x3 * y1 * zc + x3 * yc * z1 + xc * y1 * z3 - xc * y3 * z1) - 1.0;
+  parCoor[2] = detInv * (x1 * y2 * zc - x1 * yc * z2 - x2 * y1 * zc + x2 * yc * z1 + xc * y1 * z2 - xc * y2 * z1) - 1.0;
 
   /* If the point is inside this tetrahedron, adapt the parametric coordinates
      to the real pyramid and return true. */
-  if((parCoor[0] >= paramLowerBound) && (parCoor[1] >= paramLowerBound) &&
-     (parCoor[2] >= paramLowerBound) &&
-     ((parCoor[0]+parCoor[1]+parCoor[2]) <= paramLowerBound)) {
+  if ((parCoor[0] >= paramLowerBound) && (parCoor[1] >= paramLowerBound) && (parCoor[2] >= paramLowerBound) &&
+      ((parCoor[0] + parCoor[1] + parCoor[2]) <= paramLowerBound)) {
     parCoor[0] = 1.0 - parCoor[0];
     parCoor[1] = 1.0 - parCoor[1];
     return true;
@@ -1102,23 +1107,31 @@ bool CADTElemClass::InitialGuessContainmentPyramid(const su2double xRelC[3],
 
   /* Tetrahedron, 1-2-0-4.
      Create the coordinates of the tetrahedron and of the point. */
-  x1 = xRel[2][0]-xRel[1][0]; y1 = xRel[2][1]-xRel[1][1]; z1 = xRel[2][2]-xRel[1][2];
-  x2 = xRel[0][0]-xRel[1][0]; y2 = xRel[0][1]-xRel[1][1]; z2 = xRel[0][2]-xRel[1][2];
-  x3 = xRel[4][0]-xRel[1][0]; y3 = xRel[4][1]-xRel[1][1]; z3 = xRel[4][2]-xRel[1][2];
-
-  xc = xRelC[0]-xRel[1][0]; yc = xRelC[1]-xRel[1][1]; zc = xRelC[2]-xRel[1][2];
+  x1 = xRel[2][0] - xRel[1][0];
+  y1 = xRel[2][1] - xRel[1][1];
+  z1 = xRel[2][2] - xRel[1][2];
+  x2 = xRel[0][0] - xRel[1][0];
+  y2 = xRel[0][1] - xRel[1][1];
+  z2 = xRel[0][2] - xRel[1][2];
+  x3 = xRel[4][0] - xRel[1][0];
+  y3 = xRel[4][1] - xRel[1][1];
+  z3 = xRel[4][2] - xRel[1][2];
+
+  xc = xRelC[0] - xRel[1][0];
+  yc = xRelC[1] - xRel[1][1];
+  zc = xRelC[2] - xRel[1][2];
 
   /* Determine the parametric coordinates inside this tetrahedron. */
-  detInv = 2.0/(x1*y2*z3 - x1*y3*z2 - x2*y1*z3 + x2*y3*z1 + x3*y1*z2 - x3*y2*z1);
-  parCoor[0] =  detInv*(x2*y3*zc - x2*yc*z3 - x3*y2*zc + x3*yc*z2 + xc*y2*z3 - xc*y3*z2) - 1.0;
-  parCoor[1] = -detInv*(x1*y3*zc - x1*yc*z3 - x3*y1*zc + x3*yc*z1 + xc*y1*z3 - xc*y3*z1) - 1.0;
-  parCoor[2] =  detInv*(x1*y2*zc - x1*yc*z2 - x2*y1*zc + x2*yc*z1 + xc*y1*z2 - xc*y2*z1) - 1.0;
+  detInv = 2.0 / (x1 * y2 * z3 - x1 * y3 * z2 - x2 * y1 * z3 + x2 * y3 * z1 + x3 * y1 * z2 - x3 * y2 * z1);
+  parCoor[0] = detInv * (x2 * y3 * zc - x2 * yc * z3 - x3 * y2 * zc + x3 * yc * z2 + xc * y2 * z3 - xc * y3 * z2) - 1.0;
+  parCoor[1] =
+      -detInv * (x1 * y3 * zc - x1 * yc * z3 - x3 * y1 * zc + x3 * yc * z1 + xc * y1 * z3 - xc * y3 * z1) - 1.0;
+  parCoor[2] = detInv * (x1 * y2 * zc - x1 * yc * z2 - x2 * y1 * zc + x2 * yc * z1 + xc * y1 * z2 - xc * y2 * z1) - 1.0;
 
   /* If the point is inside this tetrahedron, adapt the parametric coordinates
      to the real pyramid and return true. */
-  if((parCoor[0] >= paramLowerBound) && (parCoor[1] >= paramLowerBound) &&
-     (parCoor[2] >= paramLowerBound) &&
-     ((parCoor[0]+parCoor[1]+parCoor[2]) <= paramLowerBound)) {
+  if ((parCoor[0] >= paramLowerBound) && (parCoor[1] >= paramLowerBound) && (parCoor[2] >= paramLowerBound) &&
+      ((parCoor[0] + parCoor[1] + parCoor[2]) <= paramLowerBound)) {
     const su2double r = parCoor[0];
     parCoor[0] = 1.0 - parCoor[1];
     parCoor[1] = r;
@@ -1127,23 +1140,31 @@ bool CADTElemClass::InitialGuessContainmentPyramid(const su2double xRelC[3],
 
   /* Tetrahedron, 3-0-2-4.
      Create the coordinates of the tetrahedron and of the point. */
-  x1 = xRel[0][0]-xRel[3][0]; y1 = xRel[0][1]-xRel[3][1]; z1 = xRel[0][2]-xRel[3][2];
-  x2 = xRel[2][0]-xRel[3][0]; y2 = xRel[2][1]-xRel[3][1]; z2 = xRel[2][2]-xRel[3][2];
-  x3 = xRel[4][0]-xRel[3][0]; y3 = xRel[4][1]-xRel[3][1]; z3 = xRel[4][2]-xRel[3][2];
-
-  xc = xRelC[0]-xRel[3][0]; yc = xRelC[1]-xRel[3][1]; zc = xRelC[2]-xRel[3][2];
+  x1 = xRel[0][0] - xRel[3][0];
+  y1 = xRel[0][1] - xRel[3][1];
+  z1 = xRel[0][2] - xRel[3][2];
+  x2 = xRel[2][0] - xRel[3][0];
+  y2 = xRel[2][1] - xRel[3][1];
+  z2 = xRel[2][2] - xRel[3][2];
+  x3 = xRel[4][0] - xRel[3][0];
+  y3 = xRel[4][1] - xRel[3][1];
+  z3 = xRel[4][2] - xRel[3][2];
+
+  xc = xRelC[0] - xRel[3][0];
+  yc = xRelC[1] - xRel[3][1];
+  zc = xRelC[2] - xRel[3][2];
 
   /* Determine the parametric coordinates inside this tetrahedron. */
-  detInv = 2.0/(x1*y2*z3 - x1*y3*z2 - x2*y1*z3 + x2*y3*z1 + x3*y1*z2 - x3*y2*z1);
-  parCoor[0] =  detInv*(x2*y3*zc - x2*yc*z3 - x3*y2*zc + x3*yc*z2 + xc*y2*z3 - xc*y3*z2) - 1.0;
-  parCoor[1] = -detInv*(x1*y3*zc - x1*yc*z3 - x3*y1*zc + x3*yc*z1 + xc*y1*z3 - xc*y3*z1) - 1.0;
-  parCoor[2] =  detInv*(x1*y2*zc - x1*yc*z2 - x2*y1*zc + x2*yc*z1 + xc*y1*z2 - xc*y2*z1) - 1.0;
+  detInv = 2.0 / (x1 * y2 * z3 - x1 * y3 * z2 - x2 * y1 * z3 + x2 * y3 * z1 + x3 * y1 * z2 - x3 * y2 * z1);
+  parCoor[0] = detInv * (x2 * y3 * zc - x2 * yc * z3 - x3 * y2 * zc + x3 * yc * z2 + xc * y2 * z3 - xc * y3 * z2) - 1.0;
+  parCoor[1] =
+      -detInv * (x1 * y3 * zc - x1 * yc * z3 - x3 * y1 * zc + x3 * yc * z1 + xc * y1 * z3 - xc * y3 * z1) - 1.0;
+  parCoor[2] = detInv * (x1 * y2 * zc - x1 * yc * z2 - x2 * y1 * zc + x2 * yc * z1 + xc * y1 * z2 - xc * y2 * z1) - 1.0;
 
   /* If the point is inside this tetrahedron, adapt the parametric coordinates
      to the real pyramid and return true. */
-  if((parCoor[0] >= paramLowerBound) && (parCoor[1] >= paramLowerBound) &&
-     (parCoor[2] >= paramLowerBound) &&
-     ((parCoor[0]+parCoor[1]+parCoor[2]) <= paramLowerBound)) {
+  if ((parCoor[0] >= paramLowerBound) && (parCoor[1] >= paramLowerBound) && (parCoor[2] >= paramLowerBound) &&
+      ((parCoor[0] + parCoor[1] + parCoor[2]) <= paramLowerBound)) {
     const su2double r = parCoor[0];
     parCoor[0] = parCoor[1];
     parCoor[1] = 1.0 - r;
@@ -1156,57 +1177,57 @@ bool CADTElemClass::InitialGuessContainmentPyramid(const su2double xRelC[3],
   return false;
 }
 
-bool CADTElemClass::CoorInPrism(const unsigned long elemID,
-                                const su2double     *coor,
-                                su2double           *parCoor,
-                                su2double           *weightsInterpol) const {
-
+bool CADTElemClass::CoorInPrism(const unsigned long elemID, const su2double* coor, su2double* parCoor,
+                                su2double* weightsInterpol) const {
   /* Definition of the maximum number of iterations in the Newton solver
      and the tolerance level. */
   const unsigned short maxIt = 50;
-  const su2double tolNewton  = 1.e-10;
+  const su2double tolNewton = 1.e-10;
 
   /* Determine the indices of the six vertices of the prism,
      multiplied by nDim (which is 3). This gives the position in the
      coordinate array where the coordinates of these points are stored. */
   unsigned long i0 = nDOFsPerElem[elemID];
-  unsigned long i1 = i0 + 1, i2 = i0 + 2, i3 = i0+3, i4 = i0+4, i5 = i0+5;
-  i0 = nDim*elemConns[i0]; i1 = nDim*elemConns[i1];
-  i2 = nDim*elemConns[i2]; i3 = nDim*elemConns[i3];
-  i4 = nDim*elemConns[i4]; i5 = nDim*elemConns[i5];
+  unsigned long i1 = i0 + 1, i2 = i0 + 2, i3 = i0 + 3, i4 = i0 + 4, i5 = i0 + 5;
+  i0 = nDim * elemConns[i0];
+  i1 = nDim * elemConns[i1];
+  i2 = nDim * elemConns[i2];
+  i3 = nDim * elemConns[i3];
+  i4 = nDim * elemConns[i4];
+  i5 = nDim * elemConns[i5];
 
   /* Determine the coordinates relative to the vertex 0. */
   su2double xRel[6][3], xc[3];
   xc[0] = coor[0] - coorPoints[i0];
-  xc[1] = coor[1] - coorPoints[i0+1];
-  xc[2] = coor[2] - coorPoints[i0+2];
+  xc[1] = coor[1] - coorPoints[i0 + 1];
+  xc[2] = coor[2] - coorPoints[i0 + 2];
 
   xRel[0][0] = xRel[0][1] = xRel[0][2] = 0.0;
 
-  xRel[1][0] = coorPoints[i1]   - coorPoints[i0];
-  xRel[1][1] = coorPoints[i1+1] - coorPoints[i0+1];
-  xRel[1][2] = coorPoints[i1+2] - coorPoints[i0+2];
+  xRel[1][0] = coorPoints[i1] - coorPoints[i0];
+  xRel[1][1] = coorPoints[i1 + 1] - coorPoints[i0 + 1];
+  xRel[1][2] = coorPoints[i1 + 2] - coorPoints[i0 + 2];
 
-  xRel[2][0] = coorPoints[i2]   - coorPoints[i0];
-  xRel[2][1] = coorPoints[i2+1] - coorPoints[i0+1];
-  xRel[2][2] = coorPoints[i2+2] - coorPoints[i0+2];
+  xRel[2][0] = coorPoints[i2] - coorPoints[i0];
+  xRel[2][1] = coorPoints[i2 + 1] - coorPoints[i0 + 1];
+  xRel[2][2] = coorPoints[i2 + 2] - coorPoints[i0 + 2];
 
-  xRel[3][0] = coorPoints[i3]   - coorPoints[i0];
-  xRel[3][1] = coorPoints[i3+1] - coorPoints[i0+1];
-  xRel[3][2] = coorPoints[i3+2] - coorPoints[i0+2];
+  xRel[3][0] = coorPoints[i3] - coorPoints[i0];
+  xRel[3][1] = coorPoints[i3 + 1] - coorPoints[i0 + 1];
+  xRel[3][2] = coorPoints[i3 + 2] - coorPoints[i0 + 2];
 
-  xRel[4][0] = coorPoints[i4]   - coorPoints[i0];
-  xRel[4][1] = coorPoints[i4+1] - coorPoints[i0+1];
-  xRel[4][2] = coorPoints[i4+2] - coorPoints[i0+2];
+  xRel[4][0] = coorPoints[i4] - coorPoints[i0];
+  xRel[4][1] = coorPoints[i4 + 1] - coorPoints[i0 + 1];
+  xRel[4][2] = coorPoints[i4 + 2] - coorPoints[i0 + 2];
 
-  xRel[5][0] = coorPoints[i5]   - coorPoints[i0];
-  xRel[5][1] = coorPoints[i5+1] - coorPoints[i0+1];
-  xRel[5][2] = coorPoints[i5+2] - coorPoints[i0+2];
+  xRel[5][0] = coorPoints[i5] - coorPoints[i0];
+  xRel[5][1] = coorPoints[i5 + 1] - coorPoints[i0 + 1];
+  xRel[5][2] = coorPoints[i5 + 2] - coorPoints[i0 + 2];
 
   /* Obtain an initial guess of the parametric coordinates by splitting the
      prism into tetrahedra. If this approach is not successful, this means
      that the point is not inside the true prism and false can be returned. */
-  if( !InitialGuessContainmentPrism(xc, xRel, parCoor) ) return false;
+  if (!InitialGuessContainmentPrism(xc, xRel, parCoor)) return false;
 
   /* The prism is parametrized by X-X0 = (Xi-X0)*li, where the sum runs over
      i = 0..5, although i = 0 does not give a contribution. The Lagrangian
@@ -1220,63 +1241,62 @@ bool CADTElemClass::CoorInPrism(const unsigned long elemID,
      V0 = xc - (x1+x2+x4+x5)/4, V1 = (x1+x4-x3)/4, V2 = (x2+x5-x3)/4,
      V3 = (x4+x5-x1-x2)/4, V4 = (x4-x1-x3)/4, V5 = (x5-x2-x3)/4.
      First construct these vectors. */
-  const su2double V0x = xc[0] - 0.25*(xRel[1][0]+xRel[2][0]+xRel[4][0]+xRel[5][0]);
-  const su2double V0y = xc[1] - 0.25*(xRel[1][1]+xRel[2][1]+xRel[4][1]+xRel[5][1]);
-  const su2double V0z = xc[2] - 0.25*(xRel[1][2]+xRel[2][2]+xRel[4][2]+xRel[5][2]);
+  const su2double V0x = xc[0] - 0.25 * (xRel[1][0] + xRel[2][0] + xRel[4][0] + xRel[5][0]);
+  const su2double V0y = xc[1] - 0.25 * (xRel[1][1] + xRel[2][1] + xRel[4][1] + xRel[5][1]);
+  const su2double V0z = xc[2] - 0.25 * (xRel[1][2] + xRel[2][2] + xRel[4][2] + xRel[5][2]);
 
-  const su2double V1x = 0.25*(xRel[1][0]+xRel[4][0]-xRel[3][0]);
-  const su2double V1y = 0.25*(xRel[1][1]+xRel[4][1]-xRel[3][1]);
-  const su2double V1z = 0.25*(xRel[1][2]+xRel[4][2]-xRel[3][2]);
+  const su2double V1x = 0.25 * (xRel[1][0] + xRel[4][0] - xRel[3][0]);
+  const su2double V1y = 0.25 * (xRel[1][1] + xRel[4][1] - xRel[3][1]);
+  const su2double V1z = 0.25 * (xRel[1][2] + xRel[4][2] - xRel[3][2]);
 
-  const su2double V2x = 0.25*(xRel[2][0]+xRel[5][0]-xRel[3][0]);
-  const su2double V2y = 0.25*(xRel[2][1]+xRel[5][1]-xRel[3][1]);
-  const su2double V2z = 0.25*(xRel[2][2]+xRel[5][2]-xRel[3][2]);
+  const su2double V2x = 0.25 * (xRel[2][0] + xRel[5][0] - xRel[3][0]);
+  const su2double V2y = 0.25 * (xRel[2][1] + xRel[5][1] - xRel[3][1]);
+  const su2double V2z = 0.25 * (xRel[2][2] + xRel[5][2] - xRel[3][2]);
 
-  const su2double V3x = 0.25*(xRel[4][0]+xRel[5][0]-xRel[1][0]-xRel[2][0]);
-  const su2double V3y = 0.25*(xRel[4][1]+xRel[5][1]-xRel[1][1]-xRel[2][1]);
-  const su2double V3z = 0.25*(xRel[4][2]+xRel[5][2]-xRel[1][2]-xRel[2][2]);
+  const su2double V3x = 0.25 * (xRel[4][0] + xRel[5][0] - xRel[1][0] - xRel[2][0]);
+  const su2double V3y = 0.25 * (xRel[4][1] + xRel[5][1] - xRel[1][1] - xRel[2][1]);
+  const su2double V3z = 0.25 * (xRel[4][2] + xRel[5][2] - xRel[1][2] - xRel[2][2]);
 
-  const su2double V4x = 0.25*(xRel[4][0]-xRel[1][0]-xRel[3][0]);
-  const su2double V4y = 0.25*(xRel[4][1]-xRel[1][1]-xRel[3][1]);
-  const su2double V4z = 0.25*(xRel[4][2]-xRel[1][2]-xRel[3][2]);
+  const su2double V4x = 0.25 * (xRel[4][0] - xRel[1][0] - xRel[3][0]);
+  const su2double V4y = 0.25 * (xRel[4][1] - xRel[1][1] - xRel[3][1]);
+  const su2double V4z = 0.25 * (xRel[4][2] - xRel[1][2] - xRel[3][2]);
 
-  const su2double V5x = 0.25*(xRel[5][0]-xRel[2][0]-xRel[3][0]);
-  const su2double V5y = 0.25*(xRel[5][1]-xRel[2][1]-xRel[3][1]);
-  const su2double V5z = 0.25*(xRel[5][2]-xRel[2][2]-xRel[3][2]);
+  const su2double V5x = 0.25 * (xRel[5][0] - xRel[2][0] - xRel[3][0]);
+  const su2double V5y = 0.25 * (xRel[5][1] - xRel[2][1] - xRel[3][1]);
+  const su2double V5z = 0.25 * (xRel[5][2] - xRel[2][2] - xRel[3][2]);
 
   /* Loop over the maximum number of iterations. */
   unsigned short itCount;
-  for(itCount=0; itCount<maxIt; ++itCount) {
-
-    const su2double f0 = V0x - parCoor[0]*V1x - parCoor[1]*V2x - parCoor[2]*V3x
-                       - parCoor[0]*parCoor[2]*V4x - parCoor[1]*parCoor[2]*V5x;
-    const su2double f1 = V0y - parCoor[0]*V1y - parCoor[1]*V2y - parCoor[2]*V3y
-                       - parCoor[0]*parCoor[2]*V4y - parCoor[1]*parCoor[2]*V5y;
-    const su2double f2 = V0z - parCoor[0]*V1z - parCoor[1]*V2z - parCoor[2]*V3z
-                       - parCoor[0]*parCoor[2]*V4z - parCoor[1]*parCoor[2]*V5z;
+  for (itCount = 0; itCount < maxIt; ++itCount) {
+    const su2double f0 = V0x - parCoor[0] * V1x - parCoor[1] * V2x - parCoor[2] * V3x - parCoor[0] * parCoor[2] * V4x -
+                         parCoor[1] * parCoor[2] * V5x;
+    const su2double f1 = V0y - parCoor[0] * V1y - parCoor[1] * V2y - parCoor[2] * V3y - parCoor[0] * parCoor[2] * V4y -
+                         parCoor[1] * parCoor[2] * V5y;
+    const su2double f2 = V0z - parCoor[0] * V1z - parCoor[1] * V2z - parCoor[2] * V3z - parCoor[0] * parCoor[2] * V4z -
+                         parCoor[1] * parCoor[2] * V5z;
 
     /* Compute the negative of the Jacobian matrix. */
-    const su2double a00 = V1x + parCoor[2]*V4x;
-    const su2double a01 = V2x + parCoor[2]*V5x;
-    const su2double a02 = V3x + parCoor[0]*V4x + parCoor[1]*V5x;
+    const su2double a00 = V1x + parCoor[2] * V4x;
+    const su2double a01 = V2x + parCoor[2] * V5x;
+    const su2double a02 = V3x + parCoor[0] * V4x + parCoor[1] * V5x;
 
-    const su2double a10 = V1y + parCoor[2]*V4y;
-    const su2double a11 = V2y + parCoor[2]*V5y;
-    const su2double a12 = V3y + parCoor[0]*V4y + parCoor[1]*V5y;
+    const su2double a10 = V1y + parCoor[2] * V4y;
+    const su2double a11 = V2y + parCoor[2] * V5y;
+    const su2double a12 = V3y + parCoor[0] * V4y + parCoor[1] * V5y;
 
-    const su2double a20 = V1z + parCoor[2]*V4z;
-    const su2double a21 = V2z + parCoor[2]*V5z;
-    const su2double a22 = V3z + parCoor[0]*V4z + parCoor[1]*V5z;
+    const su2double a20 = V1z + parCoor[2] * V4z;
+    const su2double a21 = V2z + parCoor[2] * V5z;
+    const su2double a22 = V3z + parCoor[0] * V4z + parCoor[1] * V5z;
 
     /* Compute the update of the parametric coordinates. */
-    const su2double detInv = 1.0/(a00*a11*a22 - a00*a12*a21 - a01*a10*a22
-                           +      a01*a12*a20 + a02*a10*a21 - a02*a11*a20);
-    const su2double dr =  detInv*(a01*a12*f2 - a01*a22*f1 - a02*a11*f2
-                       +          a02*a21*f1 + a11*a22*f0 - a12*a21*f0);
-    const su2double ds = -detInv*(a00*a12*f2 - a00*a22*f1 - a02*a10*f2
-                       +          a02*a20*f1 + a10*a22*f0 - a12*a20*f0);
-    const su2double dt =  detInv*(a00*a11*f2 - a00*a21*f1 - a01*a10*f2
-                       +          a01*a20*f1 + a10*a21*f0 - a11*a20*f0);
+    const su2double detInv = 1.0 / (a00 * a11 * a22 - a00 * a12 * a21 - a01 * a10 * a22 + a01 * a12 * a20 +
+                                    a02 * a10 * a21 - a02 * a11 * a20);
+    const su2double dr =
+        detInv * (a01 * a12 * f2 - a01 * a22 * f1 - a02 * a11 * f2 + a02 * a21 * f1 + a11 * a22 * f0 - a12 * a21 * f0);
+    const su2double ds =
+        -detInv * (a00 * a12 * f2 - a00 * a22 * f1 - a02 * a10 * f2 + a02 * a20 * f1 + a10 * a22 * f0 - a12 * a20 * f0);
+    const su2double dt =
+        detInv * (a00 * a11 * f2 - a00 * a21 * f1 - a01 * a10 * f2 + a01 * a20 * f1 + a10 * a21 * f0 - a11 * a20 * f0);
 
     /* Update the parametric coordinates. Note that the negative of the
        Jacobian is used, so the update must be added. */
@@ -1285,39 +1305,36 @@ bool CADTElemClass::CoorInPrism(const unsigned long elemID,
     parCoor[2] += dt;
 
     /* Check for convergence. */
-    if(fabs(dr) <= tolNewton && fabs(ds) <= tolNewton && fabs(dt) <= tolNewton) break;
+    if (fabs(dr) <= tolNewton && fabs(ds) <= tolNewton && fabs(dt) <= tolNewton) break;
   }
 
   /* Terminate if the Newton algorithm did not converge. */
-  if(itCount == maxIt)
-    SU2_MPI::Error("Newton did not converge", CURRENT_FUNCTION);
+  if (itCount == maxIt) SU2_MPI::Error("Newton did not converge", CURRENT_FUNCTION);
 
   /* Check if the point resides within the prism and compute the
      interpolation weights if it is. */
   bool coorIsInside = false;
-  if((parCoor[0] >= paramLowerBound) && (parCoor[1] >= paramLowerBound) &&
-     ((parCoor[0]+parCoor[1]) <= tolInsideElem) &&
-     (parCoor[2] >= paramLowerBound) && (parCoor[2] <= paramUpperBound)) {
+  if ((parCoor[0] >= paramLowerBound) && (parCoor[1] >= paramLowerBound) &&
+      ((parCoor[0] + parCoor[1]) <= tolInsideElem) && (parCoor[2] >= paramLowerBound) &&
+      (parCoor[2] <= paramUpperBound)) {
     coorIsInside = true;
 
-    const su2double omt = 0.25*(1.0-parCoor[2]), opt = 0.25*(1.0+parCoor[2]);
+    const su2double omt = 0.25 * (1.0 - parCoor[2]), opt = 0.25 * (1.0 + parCoor[2]);
 
-    weightsInterpol[0] = -omt*(parCoor[0]+parCoor[1]);
-    weightsInterpol[1] =  omt*(parCoor[0]+1.0);
-    weightsInterpol[2] =  omt*(parCoor[1]+1.0);
-    weightsInterpol[3] = -opt*(parCoor[0]+parCoor[1]);
-    weightsInterpol[4] =  opt*(parCoor[0]+1.0);
-    weightsInterpol[5] =  opt*(parCoor[1]+1.0);
+    weightsInterpol[0] = -omt * (parCoor[0] + parCoor[1]);
+    weightsInterpol[1] = omt * (parCoor[0] + 1.0);
+    weightsInterpol[2] = omt * (parCoor[1] + 1.0);
+    weightsInterpol[3] = -opt * (parCoor[0] + parCoor[1]);
+    weightsInterpol[4] = opt * (parCoor[0] + 1.0);
+    weightsInterpol[5] = opt * (parCoor[1] + 1.0);
   }
 
   /* Return the value of coorIsInside. */
   return coorIsInside;
 }
 
-bool CADTElemClass::InitialGuessContainmentPrism(const su2double xRelC[3],
-                                                 const su2double xRel[6][3],
-                                                 su2double       *parCoor) const {
-
+bool CADTElemClass::InitialGuessContainmentPrism(const su2double xRelC[3], const su2double xRel[6][3],
+                                                 su2double* parCoor) const {
   /* Tetrahedron, 0-1-2-3.
      Create the coordinates of the tetrahedron and of the point. */
   su2double x1 = xRel[1][0], y1 = xRel[1][1], z1 = xRel[1][2];
@@ -1327,126 +1344,175 @@ bool CADTElemClass::InitialGuessContainmentPrism(const su2double xRelC[3],
   su2double xc = xRelC[0], yc = xRelC[1], zc = xRelC[2];
 
   /* Determine the parametric coordinates inside this tetrahedron. */
-  su2double detInv = 2.0/(x1*y2*z3 - x1*y3*z2 - x2*y1*z3 + x2*y3*z1 + x3*y1*z2 - x3*y2*z1);
-  su2double r =  detInv*(x2*y3*zc - x2*yc*z3 - x3*y2*zc + x3*yc*z2 + xc*y2*z3 - xc*y3*z2) - 1.0;
-  su2double s = -detInv*(x1*y3*zc - x1*yc*z3 - x3*y1*zc + x3*yc*z1 + xc*y1*z3 - xc*y3*z1) - 1.0;
-  su2double t =  detInv*(x1*y2*zc - x1*yc*z2 - x2*y1*zc + x2*yc*z1 + xc*y1*z2 - xc*y2*z1) - 1.0;
+  su2double detInv = 2.0 / (x1 * y2 * z3 - x1 * y3 * z2 - x2 * y1 * z3 + x2 * y3 * z1 + x3 * y1 * z2 - x3 * y2 * z1);
+  su2double r =
+      detInv * (x2 * y3 * zc - x2 * yc * z3 - x3 * y2 * zc + x3 * yc * z2 + xc * y2 * z3 - xc * y3 * z2) - 1.0;
+  su2double s =
+      -detInv * (x1 * y3 * zc - x1 * yc * z3 - x3 * y1 * zc + x3 * yc * z1 + xc * y1 * z3 - xc * y3 * z1) - 1.0;
+  su2double t =
+      detInv * (x1 * y2 * zc - x1 * yc * z2 - x2 * y1 * zc + x2 * yc * z1 + xc * y1 * z2 - xc * y2 * z1) - 1.0;
 
   /* If the point is inside this tetrahedron, set the parametric coordinates for
      the real prism and return true. */
-  if((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) &&
-     ((r+s+t) <= paramLowerBound)) {
-    parCoor[0] = r; parCoor[1] = s; parCoor[2] = t;
+  if ((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) && ((r + s + t) <= paramLowerBound)) {
+    parCoor[0] = r;
+    parCoor[1] = s;
+    parCoor[2] = t;
     return true;
   }
 
   /* Tetrahedron, 4-1-3-2.
      Create the coordinates of the tetrahedron and of the point. */
-  x1 = xRel[1][0]-xRel[4][0]; y1 = xRel[1][1]-xRel[4][1]; z1 = xRel[1][2]-xRel[4][2];
-  x2 = xRel[3][0]-xRel[4][0]; y2 = xRel[3][1]-xRel[4][1]; z2 = xRel[3][2]-xRel[4][2];
-  x3 = xRel[2][0]-xRel[4][0]; y3 = xRel[2][1]-xRel[4][1]; z3 = xRel[2][2]-xRel[4][2];
-
-  xc = xRelC[0]-xRel[4][0]; yc = xRelC[1]-xRel[4][1]; zc = xRelC[2]-xRel[4][2];
+  x1 = xRel[1][0] - xRel[4][0];
+  y1 = xRel[1][1] - xRel[4][1];
+  z1 = xRel[1][2] - xRel[4][2];
+  x2 = xRel[3][0] - xRel[4][0];
+  y2 = xRel[3][1] - xRel[4][1];
+  z2 = xRel[3][2] - xRel[4][2];
+  x3 = xRel[2][0] - xRel[4][0];
+  y3 = xRel[2][1] - xRel[4][1];
+  z3 = xRel[2][2] - xRel[4][2];
+
+  xc = xRelC[0] - xRel[4][0];
+  yc = xRelC[1] - xRel[4][1];
+  zc = xRelC[2] - xRel[4][2];
 
   /* Determine the parametric coordinates inside this tetrahedron. */
-  detInv = 2.0/(x1*y2*z3 - x1*y3*z2 - x2*y1*z3 + x2*y3*z1 + x3*y1*z2 - x3*y2*z1);
-  r =  detInv*(x2*y3*zc - x2*yc*z3 - x3*y2*zc + x3*yc*z2 + xc*y2*z3 - xc*y3*z2) - 1.0;
-  s = -detInv*(x1*y3*zc - x1*yc*z3 - x3*y1*zc + x3*yc*z1 + xc*y1*z3 - xc*y3*z1) - 1.0;
-  t =  detInv*(x1*y2*zc - x1*yc*z2 - x2*y1*zc + x2*yc*z1 + xc*y1*z2 - xc*y2*z1) - 1.0;
+  detInv = 2.0 / (x1 * y2 * z3 - x1 * y3 * z2 - x2 * y1 * z3 + x2 * y3 * z1 + x3 * y1 * z2 - x3 * y2 * z1);
+  r = detInv * (x2 * y3 * zc - x2 * yc * z3 - x3 * y2 * zc + x3 * yc * z2 + xc * y2 * z3 - xc * y3 * z2) - 1.0;
+  s = -detInv * (x1 * y3 * zc - x1 * yc * z3 - x3 * y1 * zc + x3 * yc * z1 + xc * y1 * z3 - xc * y3 * z1) - 1.0;
+  t = detInv * (x1 * y2 * zc - x1 * yc * z2 - x2 * y1 * zc + x2 * yc * z1 + xc * y1 * z2 - xc * y2 * z1) - 1.0;
 
   /* If the point is inside this tetrahedron, set the parametric coordinates for
      the real prism and return true. */
-  if((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) &&
-     ((r+s+t) <= paramLowerBound)) {
-    parCoor[0] = 1.0 - s; parCoor[1] = t; parCoor[2] = 1.0 - r;
+  if ((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) && ((r + s + t) <= paramLowerBound)) {
+    parCoor[0] = 1.0 - s;
+    parCoor[1] = t;
+    parCoor[2] = 1.0 - r;
     return true;
   }
 
   /* Tetrahedron, 3-5-4-2.
      Create the coordinates of the tetrahedron and of the point. */
-  x1 = xRel[5][0]-xRel[3][0]; y1 = xRel[5][1]-xRel[3][1]; z1 = xRel[5][2]-xRel[3][2];
-  x2 = xRel[4][0]-xRel[3][0]; y2 = xRel[4][1]-xRel[3][1]; z2 = xRel[4][2]-xRel[3][2];
-  x3 = xRel[2][0]-xRel[3][0]; y3 = xRel[2][1]-xRel[3][1]; z3 = xRel[2][2]-xRel[3][2];
-
-  xc = xRelC[0]-xRel[3][0]; yc = xRelC[1]-xRel[3][1]; zc = xRelC[2]-xRel[3][2];
+  x1 = xRel[5][0] - xRel[3][0];
+  y1 = xRel[5][1] - xRel[3][1];
+  z1 = xRel[5][2] - xRel[3][2];
+  x2 = xRel[4][0] - xRel[3][0];
+  y2 = xRel[4][1] - xRel[3][1];
+  z2 = xRel[4][2] - xRel[3][2];
+  x3 = xRel[2][0] - xRel[3][0];
+  y3 = xRel[2][1] - xRel[3][1];
+  z3 = xRel[2][2] - xRel[3][2];
+
+  xc = xRelC[0] - xRel[3][0];
+  yc = xRelC[1] - xRel[3][1];
+  zc = xRelC[2] - xRel[3][2];
 
   /* Determine the parametric coordinates inside this tetrahedron. */
-  detInv = 2.0/(x1*y2*z3 - x1*y3*z2 - x2*y1*z3 + x2*y3*z1 + x3*y1*z2 - x3*y2*z1);
-  r =  detInv*(x2*y3*zc - x2*yc*z3 - x3*y2*zc + x3*yc*z2 + xc*y2*z3 - xc*y3*z2) - 1.0;
-  s = -detInv*(x1*y3*zc - x1*yc*z3 - x3*y1*zc + x3*yc*z1 + xc*y1*z3 - xc*y3*z1) - 1.0;
-  t =  detInv*(x1*y2*zc - x1*yc*z2 - x2*y1*zc + x2*yc*z1 + xc*y1*z2 - xc*y2*z1) - 1.0;
+  detInv = 2.0 / (x1 * y2 * z3 - x1 * y3 * z2 - x2 * y1 * z3 + x2 * y3 * z1 + x3 * y1 * z2 - x3 * y2 * z1);
+  r = detInv * (x2 * y3 * zc - x2 * yc * z3 - x3 * y2 * zc + x3 * yc * z2 + xc * y2 * z3 - xc * y3 * z2) - 1.0;
+  s = -detInv * (x1 * y3 * zc - x1 * yc * z3 - x3 * y1 * zc + x3 * yc * z1 + xc * y1 * z3 - xc * y3 * z1) - 1.0;
+  t = detInv * (x1 * y2 * zc - x1 * yc * z2 - x2 * y1 * zc + x2 * yc * z1 + xc * y1 * z2 - xc * y2 * z1) - 1.0;
 
   /* If the point is inside this tetrahedron, set the parametric coordinates for
      the real prism and return true. */
-  if((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) &&
-     ((r+s+t) <= paramLowerBound)) {
-    parCoor[0] = s; parCoor[1] = r; parCoor[2] = 1.0 - t;
+  if ((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) && ((r + s + t) <= paramLowerBound)) {
+    parCoor[0] = s;
+    parCoor[1] = r;
+    parCoor[2] = 1.0 - t;
     return true;
   }
 
   /* Tetrahedron, 3-5-4-0.
      Create the coordinates of the tetrahedron and of the point. */
-  x1 = xRel[5][0]-xRel[3][0]; y1 = xRel[5][1]-xRel[3][1]; z1 = xRel[5][2]-xRel[3][2];
-  x2 = xRel[4][0]-xRel[3][0]; y2 = xRel[4][1]-xRel[3][1]; z2 = xRel[4][2]-xRel[3][2];
-  x3 = xRel[0][0]-xRel[3][0]; y3 = xRel[0][1]-xRel[3][1]; z3 = xRel[0][2]-xRel[3][2];
-
-  xc = xRelC[0]-xRel[3][0]; yc = xRelC[1]-xRel[3][1]; zc = xRelC[2]-xRel[3][2];
+  x1 = xRel[5][0] - xRel[3][0];
+  y1 = xRel[5][1] - xRel[3][1];
+  z1 = xRel[5][2] - xRel[3][2];
+  x2 = xRel[4][0] - xRel[3][0];
+  y2 = xRel[4][1] - xRel[3][1];
+  z2 = xRel[4][2] - xRel[3][2];
+  x3 = xRel[0][0] - xRel[3][0];
+  y3 = xRel[0][1] - xRel[3][1];
+  z3 = xRel[0][2] - xRel[3][2];
+
+  xc = xRelC[0] - xRel[3][0];
+  yc = xRelC[1] - xRel[3][1];
+  zc = xRelC[2] - xRel[3][2];
 
   /* Determine the parametric coordinates inside this tetrahedron. */
-  detInv = 2.0/(x1*y2*z3 - x1*y3*z2 - x2*y1*z3 + x2*y3*z1 + x3*y1*z2 - x3*y2*z1);
-  r =  detInv*(x2*y3*zc - x2*yc*z3 - x3*y2*zc + x3*yc*z2 + xc*y2*z3 - xc*y3*z2) - 1.0;
-  s = -detInv*(x1*y3*zc - x1*yc*z3 - x3*y1*zc + x3*yc*z1 + xc*y1*z3 - xc*y3*z1) - 1.0;
-  t =  detInv*(x1*y2*zc - x1*yc*z2 - x2*y1*zc + x2*yc*z1 + xc*y1*z2 - xc*y2*z1) - 1.0;
+  detInv = 2.0 / (x1 * y2 * z3 - x1 * y3 * z2 - x2 * y1 * z3 + x2 * y3 * z1 + x3 * y1 * z2 - x3 * y2 * z1);
+  r = detInv * (x2 * y3 * zc - x2 * yc * z3 - x3 * y2 * zc + x3 * yc * z2 + xc * y2 * z3 - xc * y3 * z2) - 1.0;
+  s = -detInv * (x1 * y3 * zc - x1 * yc * z3 - x3 * y1 * zc + x3 * yc * z1 + xc * y1 * z3 - xc * y3 * z1) - 1.0;
+  t = detInv * (x1 * y2 * zc - x1 * yc * z2 - x2 * y1 * zc + x2 * yc * z1 + xc * y1 * z2 - xc * y2 * z1) - 1.0;
 
   /* If the point is inside this tetrahedron, set the parametric coordinates for
      the real prism and return true. */
-  if((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) &&
-     ((r+s+t) <= paramLowerBound)) {
-    parCoor[0] = s; parCoor[1] = r; parCoor[2] = 1.0 - t;
+  if ((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) && ((r + s + t) <= paramLowerBound)) {
+    parCoor[0] = s;
+    parCoor[1] = r;
+    parCoor[2] = 1.0 - t;
     return true;
   }
 
   /* Tetrahedron, 1-0-4-5.
      Create the coordinates of the tetrahedron and of the point. */
-  x1 = xRel[0][0]-xRel[1][0]; y1 = xRel[0][1]-xRel[1][1]; z1 = xRel[0][2]-xRel[1][2];
-  x2 = xRel[4][0]-xRel[1][0]; y2 = xRel[4][1]-xRel[1][1]; z2 = xRel[4][2]-xRel[1][2];
-  x3 = xRel[5][0]-xRel[1][0]; y3 = xRel[5][1]-xRel[1][1]; z3 = xRel[5][2]-xRel[1][2];
-
-  xc = xRelC[0]-xRel[1][0]; yc = xRelC[1]-xRel[1][1]; zc = xRelC[2]-xRel[1][2];
+  x1 = xRel[0][0] - xRel[1][0];
+  y1 = xRel[0][1] - xRel[1][1];
+  z1 = xRel[0][2] - xRel[1][2];
+  x2 = xRel[4][0] - xRel[1][0];
+  y2 = xRel[4][1] - xRel[1][1];
+  z2 = xRel[4][2] - xRel[1][2];
+  x3 = xRel[5][0] - xRel[1][0];
+  y3 = xRel[5][1] - xRel[1][1];
+  z3 = xRel[5][2] - xRel[1][2];
+
+  xc = xRelC[0] - xRel[1][0];
+  yc = xRelC[1] - xRel[1][1];
+  zc = xRelC[2] - xRel[1][2];
 
   /* Determine the parametric coordinates inside this tetrahedron. */
-  detInv = 2.0/(x1*y2*z3 - x1*y3*z2 - x2*y1*z3 + x2*y3*z1 + x3*y1*z2 - x3*y2*z1);
-  r =  detInv*(x2*y3*zc - x2*yc*z3 - x3*y2*zc + x3*yc*z2 + xc*y2*z3 - xc*y3*z2) - 1.0;
-  s = -detInv*(x1*y3*zc - x1*yc*z3 - x3*y1*zc + x3*yc*z1 + xc*y1*z3 - xc*y3*z1) - 1.0;
-  t =  detInv*(x1*y2*zc - x1*yc*z2 - x2*y1*zc + x2*yc*z1 + xc*y1*z2 - xc*y2*z1) - 1.0;
+  detInv = 2.0 / (x1 * y2 * z3 - x1 * y3 * z2 - x2 * y1 * z3 + x2 * y3 * z1 + x3 * y1 * z2 - x3 * y2 * z1);
+  r = detInv * (x2 * y3 * zc - x2 * yc * z3 - x3 * y2 * zc + x3 * yc * z2 + xc * y2 * z3 - xc * y3 * z2) - 1.0;
+  s = -detInv * (x1 * y3 * zc - x1 * yc * z3 - x3 * y1 * zc + x3 * yc * z1 + xc * y1 * z3 - xc * y3 * z1) - 1.0;
+  t = detInv * (x1 * y2 * zc - x1 * yc * z2 - x2 * y1 * zc + x2 * yc * z1 + xc * y1 * z2 - xc * y2 * z1) - 1.0;
 
   /* If the point is inside this tetrahedron, set the parametric coordinates for
      the real prism and return true. */
-  if((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) &&
-     ((r+s+t) <= paramLowerBound)) {
-    parCoor[0] = 1.0 - r; parCoor[1] = t; parCoor[2] = s;
+  if ((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) && ((r + s + t) <= paramLowerBound)) {
+    parCoor[0] = 1.0 - r;
+    parCoor[1] = t;
+    parCoor[2] = s;
     return true;
   }
 
   /* Tetrahedron, 0-1-2-5.
      Create the coordinates of the tetrahedron and of the point. */
-  x1 = xRel[1][0]; y1 = xRel[1][1]; z1 = xRel[1][2];
-  x2 = xRel[2][0]; y2 = xRel[2][1]; z2 = xRel[2][2];
-  x3 = xRel[5][0]; y3 = xRel[5][1]; z3 = xRel[5][2];
-
-  xc = xRelC[0]; yc = xRelC[1]; zc = xRelC[2];
+  x1 = xRel[1][0];
+  y1 = xRel[1][1];
+  z1 = xRel[1][2];
+  x2 = xRel[2][0];
+  y2 = xRel[2][1];
+  z2 = xRel[2][2];
+  x3 = xRel[5][0];
+  y3 = xRel[5][1];
+  z3 = xRel[5][2];
+
+  xc = xRelC[0];
+  yc = xRelC[1];
+  zc = xRelC[2];
 
   /* Determine the parametric coordinates inside this tetrahedron. */
-  detInv = 2.0/(x1*y2*z3 - x1*y3*z2 - x2*y1*z3 + x2*y3*z1 + x3*y1*z2 - x3*y2*z1);
-  r =  detInv*(x2*y3*zc - x2*yc*z3 - x3*y2*zc + x3*yc*z2 + xc*y2*z3 - xc*y3*z2) - 1.0;
-  s = -detInv*(x1*y3*zc - x1*yc*z3 - x3*y1*zc + x3*yc*z1 + xc*y1*z3 - xc*y3*z1) - 1.0;
-  t =  detInv*(x1*y2*zc - x1*yc*z2 - x2*y1*zc + x2*yc*z1 + xc*y1*z2 - xc*y2*z1) - 1.0;
+  detInv = 2.0 / (x1 * y2 * z3 - x1 * y3 * z2 - x2 * y1 * z3 + x2 * y3 * z1 + x3 * y1 * z2 - x3 * y2 * z1);
+  r = detInv * (x2 * y3 * zc - x2 * yc * z3 - x3 * y2 * zc + x3 * yc * z2 + xc * y2 * z3 - xc * y3 * z2) - 1.0;
+  s = -detInv * (x1 * y3 * zc - x1 * yc * z3 - x3 * y1 * zc + x3 * yc * z1 + xc * y1 * z3 - xc * y3 * z1) - 1.0;
+  t = detInv * (x1 * y2 * zc - x1 * yc * z2 - x2 * y1 * zc + x2 * yc * z1 + xc * y1 * z2 - xc * y2 * z1) - 1.0;
 
   /* If the point is inside this tetrahedron, set the parametric coordinates for
      the real prism and return true. */
-  if((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) &&
-     ((r+s+t) <= paramLowerBound)) {
-    parCoor[0] = r; parCoor[1] = s; parCoor[2] = t;
+  if ((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) && ((r + s + t) <= paramLowerBound)) {
+    parCoor[0] = r;
+    parCoor[1] = s;
+    parCoor[2] = t;
     return true;
   }
 
@@ -1456,66 +1522,67 @@ bool CADTElemClass::InitialGuessContainmentPrism(const su2double xRelC[3],
   return false;
 }
 
-bool CADTElemClass::CoorInHexahedron(const unsigned long elemID,
-                                     const su2double     *coor,
-                                     su2double           *parCoor,
-                                     su2double           *weightsInterpol) const {
-
+bool CADTElemClass::CoorInHexahedron(const unsigned long elemID, const su2double* coor, su2double* parCoor,
+                                     su2double* weightsInterpol) const {
   /* Definition of the maximum number of iterations in the Newton solver
      and the tolerance level. */
   const unsigned short maxIt = 50;
-  const su2double tolNewton  = 1.e-10;
+  const su2double tolNewton = 1.e-10;
 
   /* Determine the indices of the eight vertices of the hexahedron,
      multiplied by nDim (which is 3). This gives the position in the
      coordinate array where the coordinates of these points are stored. */
   unsigned long i0 = nDOFsPerElem[elemID];
-  unsigned long i1 = i0 + 1, i2 = i0 + 2, i3 = i0+3, i4 = i0+4, i5 = i0+5, i6 = i0+6, i7 = i0+7;
-  i0 = nDim*elemConns[i0]; i1 = nDim*elemConns[i1];
-  i2 = nDim*elemConns[i2]; i3 = nDim*elemConns[i3];
-  i4 = nDim*elemConns[i4]; i5 = nDim*elemConns[i5];
-  i6 = nDim*elemConns[i6]; i7 = nDim*elemConns[i7];
+  unsigned long i1 = i0 + 1, i2 = i0 + 2, i3 = i0 + 3, i4 = i0 + 4, i5 = i0 + 5, i6 = i0 + 6, i7 = i0 + 7;
+  i0 = nDim * elemConns[i0];
+  i1 = nDim * elemConns[i1];
+  i2 = nDim * elemConns[i2];
+  i3 = nDim * elemConns[i3];
+  i4 = nDim * elemConns[i4];
+  i5 = nDim * elemConns[i5];
+  i6 = nDim * elemConns[i6];
+  i7 = nDim * elemConns[i7];
 
   /* Determine the coordinates relative to the vertex 0. */
   su2double xRel[8][3], xc[3];
   xc[0] = coor[0] - coorPoints[i0];
-  xc[1] = coor[1] - coorPoints[i0+1];
-  xc[2] = coor[2] - coorPoints[i0+2];
+  xc[1] = coor[1] - coorPoints[i0 + 1];
+  xc[2] = coor[2] - coorPoints[i0 + 2];
 
   xRel[0][0] = xRel[0][1] = xRel[0][2] = 0.0;
 
-  xRel[1][0] = coorPoints[i1]   - coorPoints[i0];
-  xRel[1][1] = coorPoints[i1+1] - coorPoints[i0+1];
-  xRel[1][2] = coorPoints[i1+2] - coorPoints[i0+2];
+  xRel[1][0] = coorPoints[i1] - coorPoints[i0];
+  xRel[1][1] = coorPoints[i1 + 1] - coorPoints[i0 + 1];
+  xRel[1][2] = coorPoints[i1 + 2] - coorPoints[i0 + 2];
 
-  xRel[2][0] = coorPoints[i2]   - coorPoints[i0];
-  xRel[2][1] = coorPoints[i2+1] - coorPoints[i0+1];
-  xRel[2][2] = coorPoints[i2+2] - coorPoints[i0+2];
+  xRel[2][0] = coorPoints[i2] - coorPoints[i0];
+  xRel[2][1] = coorPoints[i2 + 1] - coorPoints[i0 + 1];
+  xRel[2][2] = coorPoints[i2 + 2] - coorPoints[i0 + 2];
 
-  xRel[3][0] = coorPoints[i3]   - coorPoints[i0];
-  xRel[3][1] = coorPoints[i3+1] - coorPoints[i0+1];
-  xRel[3][2] = coorPoints[i3+2] - coorPoints[i0+2];
+  xRel[3][0] = coorPoints[i3] - coorPoints[i0];
+  xRel[3][1] = coorPoints[i3 + 1] - coorPoints[i0 + 1];
+  xRel[3][2] = coorPoints[i3 + 2] - coorPoints[i0 + 2];
 
-  xRel[4][0] = coorPoints[i4]   - coorPoints[i0];
-  xRel[4][1] = coorPoints[i4+1] - coorPoints[i0+1];
-  xRel[4][2] = coorPoints[i4+2] - coorPoints[i0+2];
+  xRel[4][0] = coorPoints[i4] - coorPoints[i0];
+  xRel[4][1] = coorPoints[i4 + 1] - coorPoints[i0 + 1];
+  xRel[4][2] = coorPoints[i4 + 2] - coorPoints[i0 + 2];
 
-  xRel[5][0] = coorPoints[i5]   - coorPoints[i0];
-  xRel[5][1] = coorPoints[i5+1] - coorPoints[i0+1];
-  xRel[5][2] = coorPoints[i5+2] - coorPoints[i0+2];
+  xRel[5][0] = coorPoints[i5] - coorPoints[i0];
+  xRel[5][1] = coorPoints[i5 + 1] - coorPoints[i0 + 1];
+  xRel[5][2] = coorPoints[i5 + 2] - coorPoints[i0 + 2];
 
-  xRel[6][0] = coorPoints[i6]   - coorPoints[i0];
-  xRel[6][1] = coorPoints[i6+1] - coorPoints[i0+1];
-  xRel[6][2] = coorPoints[i6+2] - coorPoints[i0+2];
+  xRel[6][0] = coorPoints[i6] - coorPoints[i0];
+  xRel[6][1] = coorPoints[i6 + 1] - coorPoints[i0 + 1];
+  xRel[6][2] = coorPoints[i6 + 2] - coorPoints[i0 + 2];
 
-  xRel[7][0] = coorPoints[i7]   - coorPoints[i0];
-  xRel[7][1] = coorPoints[i7+1] - coorPoints[i0+1];
-  xRel[7][2] = coorPoints[i7+2] - coorPoints[i0+2];
+  xRel[7][0] = coorPoints[i7] - coorPoints[i0];
+  xRel[7][1] = coorPoints[i7 + 1] - coorPoints[i0 + 1];
+  xRel[7][2] = coorPoints[i7 + 2] - coorPoints[i0 + 2];
 
   /* Obtain an initial guess of the parametric coordinates by splitting the
      hexahedron into tetrahedra. If this approach is not successful, this means
      that the point is not inside the true hexahedron and false can be returned. */
-  if( !InitialGuessContainmentHexahedron(xc, xRel, parCoor) ) return false;
+  if (!InitialGuessContainmentHexahedron(xc, xRel, parCoor)) return false;
 
   /* The hexahedron is parametrized by X-X0 = (Xi-X0)*li, where the sum runs
      over i = 0..7, although i = 0 does not give a contribution. The Lagrangian
@@ -1533,74 +1600,97 @@ bool CADTElemClass::CoorInHexahedron(const unsigned long elemID,
      V4 =      (x2+x4+x6-x1-x3-x5-x7)/8, V5 = (x3+x5+x6-x1-x2-x4-x7)/8,
      V6 =      (x1+x6+x7-x2-x3-x4-x5)/8, V7 = (x1+x3+x4+x6-x2-x5-x7)/8.
      First construct these vectors. */
-  const su2double V0x = xc[0] - 0.125*(xRel[1][0]+xRel[2][0]+xRel[3][0]+xRel[4][0]+xRel[5][0]+xRel[6][0]+xRel[7][0]);
-  const su2double V0y = xc[1] - 0.125*(xRel[1][1]+xRel[2][1]+xRel[3][1]+xRel[4][1]+xRel[5][1]+xRel[6][1]+xRel[7][1]);
-  const su2double V0z = xc[2] - 0.125*(xRel[1][2]+xRel[2][2]+xRel[3][2]+xRel[4][2]+xRel[5][2]+xRel[6][2]+xRel[7][2]);
-
-  const su2double V1x = 0.125*(xRel[1][0]+xRel[2][0]-xRel[3][0]-xRel[4][0]+xRel[5][0]+xRel[6][0]-xRel[7][0]);
-  const su2double V1y = 0.125*(xRel[1][1]+xRel[2][1]-xRel[3][1]-xRel[4][1]+xRel[5][1]+xRel[6][1]-xRel[7][1]);
-  const su2double V1z = 0.125*(xRel[1][2]+xRel[2][2]-xRel[3][2]-xRel[4][2]+xRel[5][2]+xRel[6][2]-xRel[7][2]);
-
-  const su2double V2x = 0.125*(xRel[2][0]+xRel[3][0]-xRel[1][0]-xRel[4][0]-xRel[5][0]+xRel[6][0]+xRel[7][0]);
-  const su2double V2y = 0.125*(xRel[2][1]+xRel[3][1]-xRel[1][1]-xRel[4][1]-xRel[5][1]+xRel[6][1]+xRel[7][1]);
-  const su2double V2z = 0.125*(xRel[2][2]+xRel[3][2]-xRel[1][2]-xRel[4][2]-xRel[5][2]+xRel[6][2]+xRel[7][2]);
-
-  const su2double V3x = 0.125*(xRel[4][0]+xRel[5][0]+xRel[6][0]+xRel[7][0]-xRel[1][0]-xRel[2][0]-xRel[3][0]);
-  const su2double V3y = 0.125*(xRel[4][1]+xRel[5][1]+xRel[6][1]+xRel[7][1]-xRel[1][1]-xRel[2][1]-xRel[3][1]);
-  const su2double V3z = 0.125*(xRel[4][2]+xRel[5][2]+xRel[6][2]+xRel[7][2]-xRel[1][2]-xRel[2][2]-xRel[3][2]);
-
-  const su2double V4x = 0.125*(xRel[2][0]+xRel[4][0]+xRel[6][0]-xRel[1][0]-xRel[3][0]-xRel[5][0]-xRel[7][0]);
-  const su2double V4y = 0.125*(xRel[2][1]+xRel[4][1]+xRel[6][1]-xRel[1][1]-xRel[3][1]-xRel[5][1]-xRel[7][1]);
-  const su2double V4z = 0.125*(xRel[2][2]+xRel[4][2]+xRel[6][2]-xRel[1][2]-xRel[3][2]-xRel[5][2]-xRel[7][2]);
-
-  const su2double V5x = 0.125*(xRel[3][0]+xRel[5][0]+xRel[6][0]-xRel[1][0]-xRel[2][0]-xRel[4][0]-xRel[7][0]);
-  const su2double V5y = 0.125*(xRel[3][1]+xRel[5][1]+xRel[6][1]-xRel[1][1]-xRel[2][1]-xRel[4][1]-xRel[7][1]);
-  const su2double V5z = 0.125*(xRel[3][2]+xRel[5][2]+xRel[6][2]-xRel[1][2]-xRel[2][2]-xRel[4][2]-xRel[7][2]);
-
-  const su2double V6x = 0.125*(xRel[1][0]+xRel[6][0]+xRel[7][0]-xRel[2][0]-xRel[3][0]-xRel[4][0]-xRel[5][0]);
-  const su2double V6y = 0.125*(xRel[1][1]+xRel[6][1]+xRel[7][1]-xRel[2][1]-xRel[3][1]-xRel[4][1]-xRel[5][1]);
-  const su2double V6z = 0.125*(xRel[1][2]+xRel[6][2]+xRel[7][2]-xRel[2][2]-xRel[3][2]-xRel[4][2]-xRel[5][2]);
-
-  const su2double V7x = 0.125*(xRel[1][0]+xRel[3][0]+xRel[4][0]+xRel[6][0]-xRel[2][0]-xRel[5][0]-xRel[7][0]);
-  const su2double V7y = 0.125*(xRel[1][1]+xRel[3][1]+xRel[4][1]+xRel[6][1]-xRel[2][1]-xRel[5][1]-xRel[7][1]);
-  const su2double V7z = 0.125*(xRel[1][2]+xRel[3][2]+xRel[4][2]+xRel[6][2]-xRel[2][2]-xRel[5][2]-xRel[7][2]);
+  const su2double V0x =
+      xc[0] - 0.125 * (xRel[1][0] + xRel[2][0] + xRel[3][0] + xRel[4][0] + xRel[5][0] + xRel[6][0] + xRel[7][0]);
+  const su2double V0y =
+      xc[1] - 0.125 * (xRel[1][1] + xRel[2][1] + xRel[3][1] + xRel[4][1] + xRel[5][1] + xRel[6][1] + xRel[7][1]);
+  const su2double V0z =
+      xc[2] - 0.125 * (xRel[1][2] + xRel[2][2] + xRel[3][2] + xRel[4][2] + xRel[5][2] + xRel[6][2] + xRel[7][2]);
+
+  const su2double V1x =
+      0.125 * (xRel[1][0] + xRel[2][0] - xRel[3][0] - xRel[4][0] + xRel[5][0] + xRel[6][0] - xRel[7][0]);
+  const su2double V1y =
+      0.125 * (xRel[1][1] + xRel[2][1] - xRel[3][1] - xRel[4][1] + xRel[5][1] + xRel[6][1] - xRel[7][1]);
+  const su2double V1z =
+      0.125 * (xRel[1][2] + xRel[2][2] - xRel[3][2] - xRel[4][2] + xRel[5][2] + xRel[6][2] - xRel[7][2]);
+
+  const su2double V2x =
+      0.125 * (xRel[2][0] + xRel[3][0] - xRel[1][0] - xRel[4][0] - xRel[5][0] + xRel[6][0] + xRel[7][0]);
+  const su2double V2y =
+      0.125 * (xRel[2][1] + xRel[3][1] - xRel[1][1] - xRel[4][1] - xRel[5][1] + xRel[6][1] + xRel[7][1]);
+  const su2double V2z =
+      0.125 * (xRel[2][2] + xRel[3][2] - xRel[1][2] - xRel[4][2] - xRel[5][2] + xRel[6][2] + xRel[7][2]);
+
+  const su2double V3x =
+      0.125 * (xRel[4][0] + xRel[5][0] + xRel[6][0] + xRel[7][0] - xRel[1][0] - xRel[2][0] - xRel[3][0]);
+  const su2double V3y =
+      0.125 * (xRel[4][1] + xRel[5][1] + xRel[6][1] + xRel[7][1] - xRel[1][1] - xRel[2][1] - xRel[3][1]);
+  const su2double V3z =
+      0.125 * (xRel[4][2] + xRel[5][2] + xRel[6][2] + xRel[7][2] - xRel[1][2] - xRel[2][2] - xRel[3][2]);
+
+  const su2double V4x =
+      0.125 * (xRel[2][0] + xRel[4][0] + xRel[6][0] - xRel[1][0] - xRel[3][0] - xRel[5][0] - xRel[7][0]);
+  const su2double V4y =
+      0.125 * (xRel[2][1] + xRel[4][1] + xRel[6][1] - xRel[1][1] - xRel[3][1] - xRel[5][1] - xRel[7][1]);
+  const su2double V4z =
+      0.125 * (xRel[2][2] + xRel[4][2] + xRel[6][2] - xRel[1][2] - xRel[3][2] - xRel[5][2] - xRel[7][2]);
+
+  const su2double V5x =
+      0.125 * (xRel[3][0] + xRel[5][0] + xRel[6][0] - xRel[1][0] - xRel[2][0] - xRel[4][0] - xRel[7][0]);
+  const su2double V5y =
+      0.125 * (xRel[3][1] + xRel[5][1] + xRel[6][1] - xRel[1][1] - xRel[2][1] - xRel[4][1] - xRel[7][1]);
+  const su2double V5z =
+      0.125 * (xRel[3][2] + xRel[5][2] + xRel[6][2] - xRel[1][2] - xRel[2][2] - xRel[4][2] - xRel[7][2]);
+
+  const su2double V6x =
+      0.125 * (xRel[1][0] + xRel[6][0] + xRel[7][0] - xRel[2][0] - xRel[3][0] - xRel[4][0] - xRel[5][0]);
+  const su2double V6y =
+      0.125 * (xRel[1][1] + xRel[6][1] + xRel[7][1] - xRel[2][1] - xRel[3][1] - xRel[4][1] - xRel[5][1]);
+  const su2double V6z =
+      0.125 * (xRel[1][2] + xRel[6][2] + xRel[7][2] - xRel[2][2] - xRel[3][2] - xRel[4][2] - xRel[5][2]);
+
+  const su2double V7x =
+      0.125 * (xRel[1][0] + xRel[3][0] + xRel[4][0] + xRel[6][0] - xRel[2][0] - xRel[5][0] - xRel[7][0]);
+  const su2double V7y =
+      0.125 * (xRel[1][1] + xRel[3][1] + xRel[4][1] + xRel[6][1] - xRel[2][1] - xRel[5][1] - xRel[7][1]);
+  const su2double V7z =
+      0.125 * (xRel[1][2] + xRel[3][2] + xRel[4][2] + xRel[6][2] - xRel[2][2] - xRel[5][2] - xRel[7][2]);
 
   /* Loop over the maximum number of iterations. */
   unsigned short itCount;
-  for(itCount=0; itCount<maxIt; ++itCount) {
-
-    const su2double f0 = V0x - parCoor[0]*V1x - parCoor[1]*V2x - parCoor[2]*V3x
-                       - parCoor[0]*parCoor[1]*V4x - parCoor[0]*parCoor[2]*V5x
-                       - parCoor[1]*parCoor[2]*V6x - parCoor[0]*parCoor[1]*parCoor[2]*V7x;
-    const su2double f1 = V0y - parCoor[0]*V1y - parCoor[1]*V2y - parCoor[2]*V3y
-                       - parCoor[0]*parCoor[1]*V4y - parCoor[0]*parCoor[2]*V5y
-                       - parCoor[1]*parCoor[2]*V6y - parCoor[0]*parCoor[1]*parCoor[2]*V7y;
-    const su2double f2 = V0z - parCoor[0]*V1z - parCoor[1]*V2z - parCoor[2]*V3z
-                       - parCoor[0]*parCoor[1]*V4z - parCoor[0]*parCoor[2]*V5z
-                       - parCoor[1]*parCoor[2]*V6z - parCoor[0]*parCoor[1]*parCoor[2]*V7z;
+  for (itCount = 0; itCount < maxIt; ++itCount) {
+    const su2double f0 = V0x - parCoor[0] * V1x - parCoor[1] * V2x - parCoor[2] * V3x - parCoor[0] * parCoor[1] * V4x -
+                         parCoor[0] * parCoor[2] * V5x - parCoor[1] * parCoor[2] * V6x -
+                         parCoor[0] * parCoor[1] * parCoor[2] * V7x;
+    const su2double f1 = V0y - parCoor[0] * V1y - parCoor[1] * V2y - parCoor[2] * V3y - parCoor[0] * parCoor[1] * V4y -
+                         parCoor[0] * parCoor[2] * V5y - parCoor[1] * parCoor[2] * V6y -
+                         parCoor[0] * parCoor[1] * parCoor[2] * V7y;
+    const su2double f2 = V0z - parCoor[0] * V1z - parCoor[1] * V2z - parCoor[2] * V3z - parCoor[0] * parCoor[1] * V4z -
+                         parCoor[0] * parCoor[2] * V5z - parCoor[1] * parCoor[2] * V6z -
+                         parCoor[0] * parCoor[1] * parCoor[2] * V7z;
 
     /* Compute the negative of the Jacobian matrix. */
-    const su2double a00 = V1x + parCoor[1]*V4x + parCoor[2]*V5x + parCoor[1]*parCoor[2]*V7x;
-    const su2double a01 = V2x + parCoor[0]*V4x + parCoor[2]*V6x + parCoor[0]*parCoor[2]*V7x;
-    const su2double a02 = V3x + parCoor[0]*V5x + parCoor[1]*V6x + parCoor[0]*parCoor[1]*V7x;
+    const su2double a00 = V1x + parCoor[1] * V4x + parCoor[2] * V5x + parCoor[1] * parCoor[2] * V7x;
+    const su2double a01 = V2x + parCoor[0] * V4x + parCoor[2] * V6x + parCoor[0] * parCoor[2] * V7x;
+    const su2double a02 = V3x + parCoor[0] * V5x + parCoor[1] * V6x + parCoor[0] * parCoor[1] * V7x;
 
-    const su2double a10 = V1y + parCoor[1]*V4y + parCoor[2]*V5y + parCoor[1]*parCoor[2]*V7y;
-    const su2double a11 = V2y + parCoor[0]*V4y + parCoor[2]*V6y + parCoor[0]*parCoor[2]*V7y;
-    const su2double a12 = V3y + parCoor[0]*V5y + parCoor[1]*V6y + parCoor[0]*parCoor[1]*V7y;
+    const su2double a10 = V1y + parCoor[1] * V4y + parCoor[2] * V5y + parCoor[1] * parCoor[2] * V7y;
+    const su2double a11 = V2y + parCoor[0] * V4y + parCoor[2] * V6y + parCoor[0] * parCoor[2] * V7y;
+    const su2double a12 = V3y + parCoor[0] * V5y + parCoor[1] * V6y + parCoor[0] * parCoor[1] * V7y;
 
-    const su2double a20 = V1z + parCoor[1]*V4z + parCoor[2]*V5z + parCoor[1]*parCoor[2]*V7z;
-    const su2double a21 = V2z + parCoor[0]*V4z + parCoor[2]*V6z + parCoor[0]*parCoor[2]*V7z;
-    const su2double a22 = V3z + parCoor[0]*V5z + parCoor[1]*V6z + parCoor[0]*parCoor[1]*V7z;
+    const su2double a20 = V1z + parCoor[1] * V4z + parCoor[2] * V5z + parCoor[1] * parCoor[2] * V7z;
+    const su2double a21 = V2z + parCoor[0] * V4z + parCoor[2] * V6z + parCoor[0] * parCoor[2] * V7z;
+    const su2double a22 = V3z + parCoor[0] * V5z + parCoor[1] * V6z + parCoor[0] * parCoor[1] * V7z;
 
     /* Compute the update of the parametric coordinates. */
-    const su2double detInv = 1.0/(a00*a11*a22 - a00*a12*a21 - a01*a10*a22
-                           +      a01*a12*a20 + a02*a10*a21 - a02*a11*a20);
-    const su2double dr =  detInv*(a01*a12*f2 - a01*a22*f1 - a02*a11*f2
-                       +          a02*a21*f1 + a11*a22*f0 - a12*a21*f0);
-    const su2double ds = -detInv*(a00*a12*f2 - a00*a22*f1 - a02*a10*f2
-                       +          a02*a20*f1 + a10*a22*f0 - a12*a20*f0);
-    const su2double dt =  detInv*(a00*a11*f2 - a00*a21*f1 - a01*a10*f2
-                       +          a01*a20*f1 + a10*a21*f0 - a11*a20*f0);
+    const su2double detInv = 1.0 / (a00 * a11 * a22 - a00 * a12 * a21 - a01 * a10 * a22 + a01 * a12 * a20 +
+                                    a02 * a10 * a21 - a02 * a11 * a20);
+    const su2double dr =
+        detInv * (a01 * a12 * f2 - a01 * a22 * f1 - a02 * a11 * f2 + a02 * a21 * f1 + a11 * a22 * f0 - a12 * a21 * f0);
+    const su2double ds =
+        -detInv * (a00 * a12 * f2 - a00 * a22 * f1 - a02 * a10 * f2 + a02 * a20 * f1 + a10 * a22 * f0 - a12 * a20 * f0);
+    const su2double dt =
+        detInv * (a00 * a11 * f2 - a00 * a21 * f1 - a01 * a10 * f2 + a01 * a20 * f1 + a10 * a21 * f0 - a11 * a20 * f0);
 
     /* Update the parametric coordinates. Note that the negative of the
        Jacobian is used, so the update must be added. */
@@ -1609,42 +1699,39 @@ bool CADTElemClass::CoorInHexahedron(const unsigned long elemID,
     parCoor[2] += dt;
 
     /* Check for convergence. */
-    if(fabs(dr) <= tolNewton && fabs(ds) <= tolNewton && fabs(dt) <= tolNewton) break;
+    if (fabs(dr) <= tolNewton && fabs(ds) <= tolNewton && fabs(dt) <= tolNewton) break;
   }
 
   /* Terminate if the Newton algorithm did not converge. */
-  if(itCount == maxIt)
-    SU2_MPI::Error("Newton did not converge", CURRENT_FUNCTION);
+  if (itCount == maxIt) SU2_MPI::Error("Newton did not converge", CURRENT_FUNCTION);
 
   /* Check if the point resides within the hexcahedron and compute the
      interpolation weights if it is. */
   bool coorIsInside = false;
-  if((parCoor[0] >= paramLowerBound) && (parCoor[0] <= paramUpperBound) &&
-     (parCoor[1] >= paramLowerBound) && (parCoor[1] <= paramUpperBound) &&
-     (parCoor[2] >= paramLowerBound) && (parCoor[2] <= paramUpperBound)) {
+  if ((parCoor[0] >= paramLowerBound) && (parCoor[0] <= paramUpperBound) && (parCoor[1] >= paramLowerBound) &&
+      (parCoor[1] <= paramUpperBound) && (parCoor[2] >= paramLowerBound) && (parCoor[2] <= paramUpperBound)) {
     coorIsInside = true;
 
-    const su2double omr = 0.5*(1.0-parCoor[0]), opr = 0.5*(1.0+parCoor[0]);
-    const su2double oms = 0.5*(1.0-parCoor[1]), ops = 0.5*(1.0+parCoor[1]);
-    const su2double omt = 0.5*(1.0-parCoor[2]), opt = 0.5*(1.0+parCoor[2]);
-
-    weightsInterpol[0] = omr*oms*omt;
-    weightsInterpol[1] = opr*oms*omt;
-    weightsInterpol[2] = opr*ops*omt;
-    weightsInterpol[3] = omr*ops*omt;
-    weightsInterpol[4] = omr*oms*opt;
-    weightsInterpol[5] = opr*oms*opt;
-    weightsInterpol[6] = opr*ops*opt;
-    weightsInterpol[7] = omr*ops*opt;
+    const su2double omr = 0.5 * (1.0 - parCoor[0]), opr = 0.5 * (1.0 + parCoor[0]);
+    const su2double oms = 0.5 * (1.0 - parCoor[1]), ops = 0.5 * (1.0 + parCoor[1]);
+    const su2double omt = 0.5 * (1.0 - parCoor[2]), opt = 0.5 * (1.0 + parCoor[2]);
+
+    weightsInterpol[0] = omr * oms * omt;
+    weightsInterpol[1] = opr * oms * omt;
+    weightsInterpol[2] = opr * ops * omt;
+    weightsInterpol[3] = omr * ops * omt;
+    weightsInterpol[4] = omr * oms * opt;
+    weightsInterpol[5] = opr * oms * opt;
+    weightsInterpol[6] = opr * ops * opt;
+    weightsInterpol[7] = omr * ops * opt;
   }
 
   /* Return the value of coorIsInside. */
   return coorIsInside;
 }
 
-bool CADTElemClass::InitialGuessContainmentHexahedron(const su2double xRelC[3],
-                                                      const su2double xRel[8][3],
-                                                      su2double       *parCoor) const {
+bool CADTElemClass::InitialGuessContainmentHexahedron(const su2double xRelC[3], const su2double xRel[8][3],
+                                                      su2double* parCoor) const {
   /* Tetrahedron, 0-1-2-5.
      Create the coordinates of the tetrahedron and of the point. */
   su2double x1 = xRel[1][0], y1 = xRel[1][1], z1 = xRel[1][2];
@@ -1654,214 +1741,299 @@ bool CADTElemClass::InitialGuessContainmentHexahedron(const su2double xRelC[3],
   su2double xc = xRelC[0], yc = xRelC[1], zc = xRelC[2];
 
   /* Determine the parametric coordinates inside this tetrahedron. */
-  su2double detInv = 2.0/(x1*y2*z3 - x1*y3*z2 - x2*y1*z3 + x2*y3*z1 + x3*y1*z2 - x3*y2*z1);
-  su2double r =  detInv*(x2*y3*zc - x2*yc*z3 - x3*y2*zc + x3*yc*z2 + xc*y2*z3 - xc*y3*z2) - 1.0;
-  su2double s = -detInv*(x1*y3*zc - x1*yc*z3 - x3*y1*zc + x3*yc*z1 + xc*y1*z3 - xc*y3*z1) - 1.0;
-  su2double t =  detInv*(x1*y2*zc - x1*yc*z2 - x2*y1*zc + x2*yc*z1 + xc*y1*z2 - xc*y2*z1) - 1.0;
+  su2double detInv = 2.0 / (x1 * y2 * z3 - x1 * y3 * z2 - x2 * y1 * z3 + x2 * y3 * z1 + x3 * y1 * z2 - x3 * y2 * z1);
+  su2double r =
+      detInv * (x2 * y3 * zc - x2 * yc * z3 - x3 * y2 * zc + x3 * yc * z2 + xc * y2 * z3 - xc * y3 * z2) - 1.0;
+  su2double s =
+      -detInv * (x1 * y3 * zc - x1 * yc * z3 - x3 * y1 * zc + x3 * yc * z1 + xc * y1 * z3 - xc * y3 * z1) - 1.0;
+  su2double t =
+      detInv * (x1 * y2 * zc - x1 * yc * z2 - x2 * y1 * zc + x2 * yc * z1 + xc * y1 * z2 - xc * y2 * z1) - 1.0;
 
   /* If the point is inside this tetrahedron, set the parametric coordinates for
      the real hexahedron and return true. */
-  if((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) &&
-     ((r+s+t) <= paramLowerBound)) {
-    parCoor[0] = r; parCoor[1] = s; parCoor[2] = t;
+  if ((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) && ((r + s + t) <= paramLowerBound)) {
+    parCoor[0] = r;
+    parCoor[1] = s;
+    parCoor[2] = t;
     return true;
   }
 
   /* Tetrahedron, 4-7-5-0.
      Create the coordinates of the tetrahedron and of the point. */
-  x1 = xRel[7][0]-xRel[4][0]; y1 = xRel[7][1]-xRel[4][1]; z1 = xRel[7][2]-xRel[4][2];
-  x2 = xRel[5][0]-xRel[4][0]; y2 = xRel[5][1]-xRel[4][1]; z2 = xRel[5][2]-xRel[4][2];
-  x3 = xRel[0][0]-xRel[4][0]; y3 = xRel[0][1]-xRel[4][1]; z3 = xRel[0][2]-xRel[4][2];
-
-  xc = xRelC[0]-xRel[4][0]; yc = xRelC[1]-xRel[4][1]; zc = xRelC[2]-xRel[4][2];
+  x1 = xRel[7][0] - xRel[4][0];
+  y1 = xRel[7][1] - xRel[4][1];
+  z1 = xRel[7][2] - xRel[4][2];
+  x2 = xRel[5][0] - xRel[4][0];
+  y2 = xRel[5][1] - xRel[4][1];
+  z2 = xRel[5][2] - xRel[4][2];
+  x3 = xRel[0][0] - xRel[4][0];
+  y3 = xRel[0][1] - xRel[4][1];
+  z3 = xRel[0][2] - xRel[4][2];
+
+  xc = xRelC[0] - xRel[4][0];
+  yc = xRelC[1] - xRel[4][1];
+  zc = xRelC[2] - xRel[4][2];
 
   /* Determine the parametric coordinates inside this tetrahedron. */
-  detInv = 2.0/(x1*y2*z3 - x1*y3*z2 - x2*y1*z3 + x2*y3*z1 + x3*y1*z2 - x3*y2*z1);
-  r =  detInv*(x2*y3*zc - x2*yc*z3 - x3*y2*zc + x3*yc*z2 + xc*y2*z3 - xc*y3*z2) - 1.0;
-  s = -detInv*(x1*y3*zc - x1*yc*z3 - x3*y1*zc + x3*yc*z1 + xc*y1*z3 - xc*y3*z1) - 1.0;
-  t =  detInv*(x1*y2*zc - x1*yc*z2 - x2*y1*zc + x2*yc*z1 + xc*y1*z2 - xc*y2*z1) - 1.0;
+  detInv = 2.0 / (x1 * y2 * z3 - x1 * y3 * z2 - x2 * y1 * z3 + x2 * y3 * z1 + x3 * y1 * z2 - x3 * y2 * z1);
+  r = detInv * (x2 * y3 * zc - x2 * yc * z3 - x3 * y2 * zc + x3 * yc * z2 + xc * y2 * z3 - xc * y3 * z2) - 1.0;
+  s = -detInv * (x1 * y3 * zc - x1 * yc * z3 - x3 * y1 * zc + x3 * yc * z1 + xc * y1 * z3 - xc * y3 * z1) - 1.0;
+  t = detInv * (x1 * y2 * zc - x1 * yc * z2 - x2 * y1 * zc + x2 * yc * z1 + xc * y1 * z2 - xc * y2 * z1) - 1.0;
 
   /* If the point is inside this tetrahedron, set the parametric coordinates for
      the real hexahedron and return true. */
-  if((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) &&
-     ((r+s+t) <= paramLowerBound)) {
-    parCoor[0] = s; parCoor[1] = r; parCoor[2] = 1.0 - t;
+  if ((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) && ((r + s + t) <= paramLowerBound)) {
+    parCoor[0] = s;
+    parCoor[1] = r;
+    parCoor[2] = 1.0 - t;
     return true;
   }
 
   /* Tetrahedron, 6-7-5-2.
      Create the coordinates of the tetrahedron and of the point. */
-  x1 = xRel[7][0]-xRel[6][0]; y1 = xRel[7][1]-xRel[6][1]; z1 = xRel[7][2]-xRel[6][2];
-  x2 = xRel[5][0]-xRel[6][0]; y2 = xRel[5][1]-xRel[6][1]; z2 = xRel[5][2]-xRel[6][2];
-  x3 = xRel[2][0]-xRel[6][0]; y3 = xRel[2][1]-xRel[6][1]; z3 = xRel[2][2]-xRel[6][2];
-
-  xc = xRelC[0]-xRel[6][0]; yc = xRelC[1]-xRel[6][1]; zc = xRelC[2]-xRel[6][2];
+  x1 = xRel[7][0] - xRel[6][0];
+  y1 = xRel[7][1] - xRel[6][1];
+  z1 = xRel[7][2] - xRel[6][2];
+  x2 = xRel[5][0] - xRel[6][0];
+  y2 = xRel[5][1] - xRel[6][1];
+  z2 = xRel[5][2] - xRel[6][2];
+  x3 = xRel[2][0] - xRel[6][0];
+  y3 = xRel[2][1] - xRel[6][1];
+  z3 = xRel[2][2] - xRel[6][2];
+
+  xc = xRelC[0] - xRel[6][0];
+  yc = xRelC[1] - xRel[6][1];
+  zc = xRelC[2] - xRel[6][2];
 
   /* Determine the parametric coordinates inside this tetrahedron. */
-  detInv = 2.0/(x1*y2*z3 - x1*y3*z2 - x2*y1*z3 + x2*y3*z1 + x3*y1*z2 - x3*y2*z1);
-  r =  detInv*(x2*y3*zc - x2*yc*z3 - x3*y2*zc + x3*yc*z2 + xc*y2*z3 - xc*y3*z2) - 1.0;
-  s = -detInv*(x1*y3*zc - x1*yc*z3 - x3*y1*zc + x3*yc*z1 + xc*y1*z3 - xc*y3*z1) - 1.0;
-  t =  detInv*(x1*y2*zc - x1*yc*z2 - x2*y1*zc + x2*yc*z1 + xc*y1*z2 - xc*y2*z1) - 1.0;
+  detInv = 2.0 / (x1 * y2 * z3 - x1 * y3 * z2 - x2 * y1 * z3 + x2 * y3 * z1 + x3 * y1 * z2 - x3 * y2 * z1);
+  r = detInv * (x2 * y3 * zc - x2 * yc * z3 - x3 * y2 * zc + x3 * yc * z2 + xc * y2 * z3 - xc * y3 * z2) - 1.0;
+  s = -detInv * (x1 * y3 * zc - x1 * yc * z3 - x3 * y1 * zc + x3 * yc * z1 + xc * y1 * z3 - xc * y3 * z1) - 1.0;
+  t = detInv * (x1 * y2 * zc - x1 * yc * z2 - x2 * y1 * zc + x2 * yc * z1 + xc * y1 * z2 - xc * y2 * z1) - 1.0;
 
   /* If the point is inside this tetrahedron, set the parametric coordinates for
      the real hexahedron and return true. */
-  if((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) &&
-     ((r+s+t) <= paramLowerBound)) {
-    parCoor[0] = 1.0 - s; parCoor[1] = 1.0 - r; parCoor[2] = 1.0 - t;
+  if ((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) && ((r + s + t) <= paramLowerBound)) {
+    parCoor[0] = 1.0 - s;
+    parCoor[1] = 1.0 - r;
+    parCoor[2] = 1.0 - t;
     return true;
   }
 
   /* Tetrahedron, 3-0-2-7.
      Create the coordinates of the tetrahedron and of the point. */
-  x1 = xRel[0][0]-xRel[3][0]; y1 = xRel[0][1]-xRel[3][1]; z1 = xRel[0][2]-xRel[3][2];
-  x2 = xRel[2][0]-xRel[3][0]; y2 = xRel[2][1]-xRel[3][1]; z2 = xRel[2][2]-xRel[3][2];
-  x3 = xRel[7][0]-xRel[3][0]; y3 = xRel[7][1]-xRel[3][1]; z3 = xRel[7][2]-xRel[3][2];
-
-  xc = xRelC[0]-xRel[3][0]; yc = xRelC[1]-xRel[3][1]; zc = xRelC[2]-xRel[3][2];
+  x1 = xRel[0][0] - xRel[3][0];
+  y1 = xRel[0][1] - xRel[3][1];
+  z1 = xRel[0][2] - xRel[3][2];
+  x2 = xRel[2][0] - xRel[3][0];
+  y2 = xRel[2][1] - xRel[3][1];
+  z2 = xRel[2][2] - xRel[3][2];
+  x3 = xRel[7][0] - xRel[3][0];
+  y3 = xRel[7][1] - xRel[3][1];
+  z3 = xRel[7][2] - xRel[3][2];
+
+  xc = xRelC[0] - xRel[3][0];
+  yc = xRelC[1] - xRel[3][1];
+  zc = xRelC[2] - xRel[3][2];
 
   /* Determine the parametric coordinates inside this tetrahedron. */
-  detInv = 2.0/(x1*y2*z3 - x1*y3*z2 - x2*y1*z3 + x2*y3*z1 + x3*y1*z2 - x3*y2*z1);
-  r =  detInv*(x2*y3*zc - x2*yc*z3 - x3*y2*zc + x3*yc*z2 + xc*y2*z3 - xc*y3*z2) - 1.0;
-  s = -detInv*(x1*y3*zc - x1*yc*z3 - x3*y1*zc + x3*yc*z1 + xc*y1*z3 - xc*y3*z1) - 1.0;
-  t =  detInv*(x1*y2*zc - x1*yc*z2 - x2*y1*zc + x2*yc*z1 + xc*y1*z2 - xc*y2*z1) - 1.0;
+  detInv = 2.0 / (x1 * y2 * z3 - x1 * y3 * z2 - x2 * y1 * z3 + x2 * y3 * z1 + x3 * y1 * z2 - x3 * y2 * z1);
+  r = detInv * (x2 * y3 * zc - x2 * yc * z3 - x3 * y2 * zc + x3 * yc * z2 + xc * y2 * z3 - xc * y3 * z2) - 1.0;
+  s = -detInv * (x1 * y3 * zc - x1 * yc * z3 - x3 * y1 * zc + x3 * yc * z1 + xc * y1 * z3 - xc * y3 * z1) - 1.0;
+  t = detInv * (x1 * y2 * zc - x1 * yc * z2 - x2 * y1 * zc + x2 * yc * z1 + xc * y1 * z2 - xc * y2 * z1) - 1.0;
 
   /* If the point is inside this tetrahedron, set the parametric coordinates for
      the real hexahedron and return true. */
-  if((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) &&
-     ((r+s+t) <= paramLowerBound)) {
-    parCoor[0] = 1.0 - s; parCoor[1] = r; parCoor[2] = 1.0 - t;
+  if ((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) && ((r + s + t) <= paramLowerBound)) {
+    parCoor[0] = 1.0 - s;
+    parCoor[1] = r;
+    parCoor[2] = 1.0 - t;
     return true;
   }
 
   /* Tetrahedron, 0-5-2-7.
      Create the coordinates of the tetrahedron and of the point. */
-  x1 = xRel[5][0]; y1 = xRel[5][1]; z1 = xRel[5][2];
-  x2 = xRel[2][0]; y2 = xRel[2][1]; z2 = xRel[2][2];
-  x3 = xRel[7][0]; y3 = xRel[7][1]; z3 = xRel[7][2];
-
-  xc = xRelC[0]; yc = xRelC[1]; zc = xRelC[2];
+  x1 = xRel[5][0];
+  y1 = xRel[5][1];
+  z1 = xRel[5][2];
+  x2 = xRel[2][0];
+  y2 = xRel[2][1];
+  z2 = xRel[2][2];
+  x3 = xRel[7][0];
+  y3 = xRel[7][1];
+  z3 = xRel[7][2];
+
+  xc = xRelC[0];
+  yc = xRelC[1];
+  zc = xRelC[2];
 
   /* Determine the parametric coordinates inside this tetrahedron. */
-  detInv = 2.0/(x1*y2*z3 - x1*y3*z2 - x2*y1*z3 + x2*y3*z1 + x3*y1*z2 - x3*y2*z1);
-  r =  detInv*(x2*y3*zc - x2*yc*z3 - x3*y2*zc + x3*yc*z2 + xc*y2*z3 - xc*y3*z2) - 1.0;
-  s = -detInv*(x1*y3*zc - x1*yc*z3 - x3*y1*zc + x3*yc*z1 + xc*y1*z3 - xc*y3*z1) - 1.0;
-  t =  detInv*(x1*y2*zc - x1*yc*z2 - x2*y1*zc + x2*yc*z1 + xc*y1*z2 - xc*y2*z1) - 1.0;
+  detInv = 2.0 / (x1 * y2 * z3 - x1 * y3 * z2 - x2 * y1 * z3 + x2 * y3 * z1 + x3 * y1 * z2 - x3 * y2 * z1);
+  r = detInv * (x2 * y3 * zc - x2 * yc * z3 - x3 * y2 * zc + x3 * yc * z2 + xc * y2 * z3 - xc * y3 * z2) - 1.0;
+  s = -detInv * (x1 * y3 * zc - x1 * yc * z3 - x3 * y1 * zc + x3 * yc * z1 + xc * y1 * z3 - xc * y3 * z1) - 1.0;
+  t = detInv * (x1 * y2 * zc - x1 * yc * z2 - x2 * y1 * zc + x2 * yc * z1 + xc * y1 * z2 - xc * y2 * z1) - 1.0;
 
   /* If the point is inside this tetrahedron, set the parametric coordinates for
      the real hexahedron and return true. */
-  if((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) &&
-     ((r+s+t) <= paramLowerBound)) {
-    parCoor[0] = 1.0+r+s; parCoor[1] = 1.0+s+t; parCoor[2] = 1.0+r+t;
+  if ((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) && ((r + s + t) <= paramLowerBound)) {
+    parCoor[0] = 1.0 + r + s;
+    parCoor[1] = 1.0 + s + t;
+    parCoor[2] = 1.0 + r + t;
     return true;
   }
 
   /* Tetrahedron, 0-1-3-4.
      Create the coordinates of the tetrahedron and of the point. */
-  x1 = xRel[1][0]; y1 = xRel[1][1]; z1 = xRel[1][2];
-  x2 = xRel[3][0]; y2 = xRel[3][1]; z2 = xRel[3][2];
-  x3 = xRel[4][0]; y3 = xRel[4][1]; z3 = xRel[4][2];
-
-  xc = xRelC[0]; yc = xRelC[1]; zc = xRelC[2];
+  x1 = xRel[1][0];
+  y1 = xRel[1][1];
+  z1 = xRel[1][2];
+  x2 = xRel[3][0];
+  y2 = xRel[3][1];
+  z2 = xRel[3][2];
+  x3 = xRel[4][0];
+  y3 = xRel[4][1];
+  z3 = xRel[4][2];
+
+  xc = xRelC[0];
+  yc = xRelC[1];
+  zc = xRelC[2];
 
   /* Determine the parametric coordinates inside this tetrahedron. */
-  detInv = 2.0/(x1*y2*z3 - x1*y3*z2 - x2*y1*z3 + x2*y3*z1 + x3*y1*z2 - x3*y2*z1);
-  r =  detInv*(x2*y3*zc - x2*yc*z3 - x3*y2*zc + x3*yc*z2 + xc*y2*z3 - xc*y3*z2) - 1.0;
-  s = -detInv*(x1*y3*zc - x1*yc*z3 - x3*y1*zc + x3*yc*z1 + xc*y1*z3 - xc*y3*z1) - 1.0;
-  t =  detInv*(x1*y2*zc - x1*yc*z2 - x2*y1*zc + x2*yc*z1 + xc*y1*z2 - xc*y2*z1) - 1.0;
+  detInv = 2.0 / (x1 * y2 * z3 - x1 * y3 * z2 - x2 * y1 * z3 + x2 * y3 * z1 + x3 * y1 * z2 - x3 * y2 * z1);
+  r = detInv * (x2 * y3 * zc - x2 * yc * z3 - x3 * y2 * zc + x3 * yc * z2 + xc * y2 * z3 - xc * y3 * z2) - 1.0;
+  s = -detInv * (x1 * y3 * zc - x1 * yc * z3 - x3 * y1 * zc + x3 * yc * z1 + xc * y1 * z3 - xc * y3 * z1) - 1.0;
+  t = detInv * (x1 * y2 * zc - x1 * yc * z2 - x2 * y1 * zc + x2 * yc * z1 + xc * y1 * z2 - xc * y2 * z1) - 1.0;
 
   /* If the point is inside this tetrahedron, set the parametric coordinates for
      the real hexahedron and return true. */
-  if((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) &&
-     ((r+s+t) <= paramLowerBound)) {
-    parCoor[0] = r; parCoor[1] = s; parCoor[2] = t;
+  if ((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) && ((r + s + t) <= paramLowerBound)) {
+    parCoor[0] = r;
+    parCoor[1] = s;
+    parCoor[2] = t;
     return true;
   }
 
   /* Tetrahedron, 7-6-4-3.
      Create the coordinates of the tetrahedron and of the point. */
-  x1 = xRel[6][0]-xRel[7][0]; y1 = xRel[6][1]-xRel[7][1]; z1 = xRel[6][2]-xRel[7][2];
-  x2 = xRel[4][0]-xRel[7][0]; y2 = xRel[4][1]-xRel[7][1]; z2 = xRel[4][2]-xRel[7][2];
-  x3 = xRel[3][0]-xRel[7][0]; y3 = xRel[3][1]-xRel[7][1]; z3 = xRel[3][2]-xRel[7][2];
-
-  xc = xRelC[0]-xRel[7][0]; yc = xRelC[1]-xRel[7][1]; zc = xRelC[2]-xRel[7][2];
+  x1 = xRel[6][0] - xRel[7][0];
+  y1 = xRel[6][1] - xRel[7][1];
+  z1 = xRel[6][2] - xRel[7][2];
+  x2 = xRel[4][0] - xRel[7][0];
+  y2 = xRel[4][1] - xRel[7][1];
+  z2 = xRel[4][2] - xRel[7][2];
+  x3 = xRel[3][0] - xRel[7][0];
+  y3 = xRel[3][1] - xRel[7][1];
+  z3 = xRel[3][2] - xRel[7][2];
+
+  xc = xRelC[0] - xRel[7][0];
+  yc = xRelC[1] - xRel[7][1];
+  zc = xRelC[2] - xRel[7][2];
 
   /* Determine the parametric coordinates inside this tetrahedron. */
-  detInv = 2.0/(x1*y2*z3 - x1*y3*z2 - x2*y1*z3 + x2*y3*z1 + x3*y1*z2 - x3*y2*z1);
-  r =  detInv*(x2*y3*zc - x2*yc*z3 - x3*y2*zc + x3*yc*z2 + xc*y2*z3 - xc*y3*z2) - 1.0;
-  s = -detInv*(x1*y3*zc - x1*yc*z3 - x3*y1*zc + x3*yc*z1 + xc*y1*z3 - xc*y3*z1) - 1.0;
-  t =  detInv*(x1*y2*zc - x1*yc*z2 - x2*y1*zc + x2*yc*z1 + xc*y1*z2 - xc*y2*z1) - 1.0;
+  detInv = 2.0 / (x1 * y2 * z3 - x1 * y3 * z2 - x2 * y1 * z3 + x2 * y3 * z1 + x3 * y1 * z2 - x3 * y2 * z1);
+  r = detInv * (x2 * y3 * zc - x2 * yc * z3 - x3 * y2 * zc + x3 * yc * z2 + xc * y2 * z3 - xc * y3 * z2) - 1.0;
+  s = -detInv * (x1 * y3 * zc - x1 * yc * z3 - x3 * y1 * zc + x3 * yc * z1 + xc * y1 * z3 - xc * y3 * z1) - 1.0;
+  t = detInv * (x1 * y2 * zc - x1 * yc * z2 - x2 * y1 * zc + x2 * yc * z1 + xc * y1 * z2 - xc * y2 * z1) - 1.0;
 
   /* If the point is inside this tetrahedron, set the parametric coordinates for
      the real hexahedron and return true. */
-  if((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) &&
-     ((r+s+t) <= paramLowerBound)) {
-    parCoor[0] = r; parCoor[1] = 1.0 - s; parCoor[2] = 1.0 - t;
+  if ((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) && ((r + s + t) <= paramLowerBound)) {
+    parCoor[0] = r;
+    parCoor[1] = 1.0 - s;
+    parCoor[2] = 1.0 - t;
     return true;
   }
 
   /* Tetrahedron, 5-4-6-1.
      Create the coordinates of the tetrahedron and of the point. */
-  x1 = xRel[4][0]-xRel[5][0]; y1 = xRel[4][1]-xRel[5][1]; z1 = xRel[4][2]-xRel[5][2];
-  x2 = xRel[6][0]-xRel[5][0]; y2 = xRel[6][1]-xRel[5][1]; z2 = xRel[6][2]-xRel[5][2];
-  x3 = xRel[1][0]-xRel[5][0]; y3 = xRel[1][1]-xRel[5][1]; z3 = xRel[1][2]-xRel[5][2];
-
-  xc = xRelC[0]-xRel[5][0]; yc = xRelC[1]-xRel[5][1]; zc = xRelC[2]-xRel[5][2];
+  x1 = xRel[4][0] - xRel[5][0];
+  y1 = xRel[4][1] - xRel[5][1];
+  z1 = xRel[4][2] - xRel[5][2];
+  x2 = xRel[6][0] - xRel[5][0];
+  y2 = xRel[6][1] - xRel[5][1];
+  z2 = xRel[6][2] - xRel[5][2];
+  x3 = xRel[1][0] - xRel[5][0];
+  y3 = xRel[1][1] - xRel[5][1];
+  z3 = xRel[1][2] - xRel[5][2];
+
+  xc = xRelC[0] - xRel[5][0];
+  yc = xRelC[1] - xRel[5][1];
+  zc = xRelC[2] - xRel[5][2];
 
   /* Determine the parametric coordinates inside this tetrahedron. */
-  detInv = 2.0/(x1*y2*z3 - x1*y3*z2 - x2*y1*z3 + x2*y3*z1 + x3*y1*z2 - x3*y2*z1);
-  r =  detInv*(x2*y3*zc - x2*yc*z3 - x3*y2*zc + x3*yc*z2 + xc*y2*z3 - xc*y3*z2) - 1.0;
-  s = -detInv*(x1*y3*zc - x1*yc*z3 - x3*y1*zc + x3*yc*z1 + xc*y1*z3 - xc*y3*z1) - 1.0;
-  t =  detInv*(x1*y2*zc - x1*yc*z2 - x2*y1*zc + x2*yc*z1 + xc*y1*z2 - xc*y2*z1) - 1.0;
+  detInv = 2.0 / (x1 * y2 * z3 - x1 * y3 * z2 - x2 * y1 * z3 + x2 * y3 * z1 + x3 * y1 * z2 - x3 * y2 * z1);
+  r = detInv * (x2 * y3 * zc - x2 * yc * z3 - x3 * y2 * zc + x3 * yc * z2 + xc * y2 * z3 - xc * y3 * z2) - 1.0;
+  s = -detInv * (x1 * y3 * zc - x1 * yc * z3 - x3 * y1 * zc + x3 * yc * z1 + xc * y1 * z3 - xc * y3 * z1) - 1.0;
+  t = detInv * (x1 * y2 * zc - x1 * yc * z2 - x2 * y1 * zc + x2 * yc * z1 + xc * y1 * z2 - xc * y2 * z1) - 1.0;
 
   /* If the point is inside this tetrahedron, set the parametric coordinates for
      the real hexahedron and return true. */
-  if((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) &&
-     ((r+s+t) <= paramLowerBound)) {
-    parCoor[0] = 1.0 - r; parCoor[1] = s; parCoor[2] = 1.0 - t;
+  if ((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) && ((r + s + t) <= paramLowerBound)) {
+    parCoor[0] = 1.0 - r;
+    parCoor[1] = s;
+    parCoor[2] = 1.0 - t;
     return true;
   }
 
   /* Tetrahedron, 2-3-1-6.
      Create the coordinates of the tetrahedron and of the point. */
-  x1 = xRel[3][0]-xRel[2][0]; y1 = xRel[3][1]-xRel[2][1]; z1 = xRel[3][2]-xRel[2][2];
-  x2 = xRel[1][0]-xRel[2][0]; y2 = xRel[1][1]-xRel[2][1]; z2 = xRel[1][2]-xRel[2][2];
-  x3 = xRel[6][0]-xRel[2][0]; y3 = xRel[6][1]-xRel[2][1]; z3 = xRel[6][2]-xRel[2][2];
-
-  xc = xRelC[0]-xRel[2][0]; yc = xRelC[1]-xRel[2][1]; zc = xRelC[2]-xRel[2][2];
+  x1 = xRel[3][0] - xRel[2][0];
+  y1 = xRel[3][1] - xRel[2][1];
+  z1 = xRel[3][2] - xRel[2][2];
+  x2 = xRel[1][0] - xRel[2][0];
+  y2 = xRel[1][1] - xRel[2][1];
+  z2 = xRel[1][2] - xRel[2][2];
+  x3 = xRel[6][0] - xRel[2][0];
+  y3 = xRel[6][1] - xRel[2][1];
+  z3 = xRel[6][2] - xRel[2][2];
+
+  xc = xRelC[0] - xRel[2][0];
+  yc = xRelC[1] - xRel[2][1];
+  zc = xRelC[2] - xRel[2][2];
 
   /* Determine the parametric coordinates inside this tetrahedron. */
-  detInv = 2.0/(x1*y2*z3 - x1*y3*z2 - x2*y1*z3 + x2*y3*z1 + x3*y1*z2 - x3*y2*z1);
-  r =  detInv*(x2*y3*zc - x2*yc*z3 - x3*y2*zc + x3*yc*z2 + xc*y2*z3 - xc*y3*z2) - 1.0;
-  s = -detInv*(x1*y3*zc - x1*yc*z3 - x3*y1*zc + x3*yc*z1 + xc*y1*z3 - xc*y3*z1) - 1.0;
-  t =  detInv*(x1*y2*zc - x1*yc*z2 - x2*y1*zc + x2*yc*z1 + xc*y1*z2 - xc*y2*z1) - 1.0;
+  detInv = 2.0 / (x1 * y2 * z3 - x1 * y3 * z2 - x2 * y1 * z3 + x2 * y3 * z1 + x3 * y1 * z2 - x3 * y2 * z1);
+  r = detInv * (x2 * y3 * zc - x2 * yc * z3 - x3 * y2 * zc + x3 * yc * z2 + xc * y2 * z3 - xc * y3 * z2) - 1.0;
+  s = -detInv * (x1 * y3 * zc - x1 * yc * z3 - x3 * y1 * zc + x3 * yc * z1 + xc * y1 * z3 - xc * y3 * z1) - 1.0;
+  t = detInv * (x1 * y2 * zc - x1 * yc * z2 - x2 * y1 * zc + x2 * yc * z1 + xc * y1 * z2 - xc * y2 * z1) - 1.0;
 
   /* If the point is inside this tetrahedron, set the parametric coordinates for
      the real hexahedron and return true. */
-  if((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) &&
-     ((r+s+t) <= paramLowerBound)) {
-    parCoor[0] = 1.0 - r; parCoor[1] = 1.0 - s; parCoor[2] = t;
+  if ((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) && ((r + s + t) <= paramLowerBound)) {
+    parCoor[0] = 1.0 - r;
+    parCoor[1] = 1.0 - s;
+    parCoor[2] = t;
     return true;
   }
 
   /* Tetrahedron, 3-4-1-6.
      Create the coordinates of the tetrahedron and of the point. */
-  x1 = xRel[4][0]-xRel[3][0]; y1 = xRel[4][1]-xRel[3][1]; z1 = xRel[4][2]-xRel[3][2];
-  x2 = xRel[1][0]-xRel[3][0]; y2 = xRel[1][1]-xRel[3][1]; z2 = xRel[1][2]-xRel[3][2];
-  x3 = xRel[6][0]-xRel[3][0]; y3 = xRel[6][1]-xRel[3][1]; z3 = xRel[6][2]-xRel[3][2];
-
-  xc = xRelC[0]-xRel[3][0]; yc = xRelC[1]-xRel[3][1]; zc = xRelC[2]-xRel[3][2];
+  x1 = xRel[4][0] - xRel[3][0];
+  y1 = xRel[4][1] - xRel[3][1];
+  z1 = xRel[4][2] - xRel[3][2];
+  x2 = xRel[1][0] - xRel[3][0];
+  y2 = xRel[1][1] - xRel[3][1];
+  z2 = xRel[1][2] - xRel[3][2];
+  x3 = xRel[6][0] - xRel[3][0];
+  y3 = xRel[6][1] - xRel[3][1];
+  z3 = xRel[6][2] - xRel[3][2];
+
+  xc = xRelC[0] - xRel[3][0];
+  yc = xRelC[1] - xRel[3][1];
+  zc = xRelC[2] - xRel[3][2];
 
   /* Determine the parametric coordinates inside this tetrahedron. */
-  detInv = 2.0/(x1*y2*z3 - x1*y3*z2 - x2*y1*z3 + x2*y3*z1 + x3*y1*z2 - x3*y2*z1);
-  r =  detInv*(x2*y3*zc - x2*yc*z3 - x3*y2*zc + x3*yc*z2 + xc*y2*z3 - xc*y3*z2) - 1.0;
-  s = -detInv*(x1*y3*zc - x1*yc*z3 - x3*y1*zc + x3*yc*z1 + xc*y1*z3 - xc*y3*z1) - 1.0;
-  t =  detInv*(x1*y2*zc - x1*yc*z2 - x2*y1*zc + x2*yc*z1 + xc*y1*z2 - xc*y2*z1) - 1.0;
+  detInv = 2.0 / (x1 * y2 * z3 - x1 * y3 * z2 - x2 * y1 * z3 + x2 * y3 * z1 + x3 * y1 * z2 - x3 * y2 * z1);
+  r = detInv * (x2 * y3 * zc - x2 * yc * z3 - x3 * y2 * zc + x3 * yc * z2 + xc * y2 * z3 - xc * y3 * z2) - 1.0;
+  s = -detInv * (x1 * y3 * zc - x1 * yc * z3 - x3 * y1 * zc + x3 * yc * z1 + xc * y1 * z3 - xc * y3 * z1) - 1.0;
+  t = detInv * (x1 * y2 * zc - x1 * yc * z2 - x2 * y1 * zc + x2 * yc * z1 + xc * y1 * z2 - xc * y2 * z1) - 1.0;
 
   /* If the point is inside this tetrahedron, set the parametric coordinates for
      the real hexahedron and return true. */
-  if((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) &&
-     ((r+s+t) <= paramLowerBound)) {
-    parCoor[0] = 1.0+s+t; parCoor[1] = -1.0-r-s; parCoor[2] = 1.0+r+t;
+  if ((r >= paramLowerBound) && (s >= paramLowerBound) && (t >= paramLowerBound) && ((r + s + t) <= paramLowerBound)) {
+    parCoor[0] = 1.0 + s + t;
+    parCoor[1] = -1.0 - r - s;
+    parCoor[2] = 1.0 + r + t;
     return true;
   }
 
@@ -1871,20 +2043,17 @@ bool CADTElemClass::InitialGuessContainmentHexahedron(const su2double xRelC[3],
   return false;
 }
 
-void CADTElemClass::Dist2ToLine(const unsigned long i0,
-                                const unsigned long i1,
-                                const su2double     *coor,
-                                su2double           &dist2Line) const {
-
+void CADTElemClass::Dist2ToLine(const unsigned long i0, const unsigned long i1, const su2double* coor,
+                                su2double& dist2Line) const {
   /*--- The line is parametrized by X = X0 + (r+1)*(X1-X0)/2, -1 <= r <= 1.
         As a consequence the minimum distance is found where the expression
         |V0 - r*V1| has a minimum, where the vectors V0 and V1 are defined
         as: V0 = coor - (X1+X0)/2, V1 = (X1-X0)/2. First construct the
         vectors V0 and V1. ---*/
   su2double V0[3], V1[3];
-  for(unsigned short k=0; k<nDim; ++k) {
-    V0[k] = coor[k] - 0.5*(coorPoints[i1+k] + coorPoints[i0+k]);
-    V1[k] =           0.5*(coorPoints[i1+k] - coorPoints[i0+k]);
+  for (unsigned short k = 0; k < nDim; ++k) {
+    V0[k] = coor[k] - 0.5 * (coorPoints[i1 + k] + coorPoints[i0 + k]);
+    V1[k] = 0.5 * (coorPoints[i1 + k] - coorPoints[i0 + k]);
   }
 
   /*--- Determine the value of r, for which the minimum occurs. This is the
@@ -1892,30 +2061,24 @@ void CADTElemClass::Dist2ToLine(const unsigned long i0,
         limited between -1 and 1 to make sure that the projection is inside
         the line element. ---*/
   su2double dotV0V1 = 0.0, dotV1V1 = 0.0;
-  for(unsigned short k=0; k<nDim; ++k) {
-    dotV0V1 += V0[k]*V1[k];
-    dotV1V1 += V1[k]*V1[k];
+  for (unsigned short k = 0; k < nDim; ++k) {
+    dotV0V1 += V0[k] * V1[k];
+    dotV1V1 += V1[k] * V1[k];
   }
-  su2double r = dotV0V1/dotV1V1;
-  r = max(-1.0,min(1.0,r));
+  su2double r = dotV0V1 / dotV1V1;
+  r = max(-1.0, min(1.0, r));
 
   /*--- Determine the minimum distance squared. ---*/
   dist2Line = 0.0;
-  for(unsigned short k=0; k<nDim; ++k) {
-    const su2double ds = V0[k] - r*V1[k];
-    dist2Line += ds*ds;
+  for (unsigned short k = 0; k < nDim; ++k) {
+    const su2double ds = V0[k] - r * V1[k];
+    dist2Line += ds * ds;
   }
 }
 
-bool CADTElemClass::Dist2ToTriangle(const unsigned long i0,
-                                    const unsigned long i1,
-                                    const unsigned long i2,
-                                    const su2double     *coor,
-                                    su2double           &dist2Tria,
-                                    su2double           &r,
-                                    su2double           &s) const {
-
-  constexpr unsigned short nDim = 3; // boundary triangles only exist in 3D
+bool CADTElemClass::Dist2ToTriangle(const unsigned long i0, const unsigned long i1, const unsigned long i2,
+                                    const su2double* coor, su2double& dist2Tria, su2double& r, su2double& s) const {
+  constexpr unsigned short nDim = 3;  // boundary triangles only exist in 3D
 
   /*--- The triangle is parametrized by X = X0 + (r+1)*(X1-X0)/2 + (s+1)*(X2-X0)/2,
         r, s >= -1, r+s <= 0. As a consequence the minimum distance is found where
@@ -1923,38 +2086,37 @@ bool CADTElemClass::Dist2ToTriangle(const unsigned long i0,
         and V2 are defined as: V0 = coor - (X1+X2)/2, V1 = (X1-X0)/2, V2 = (X2-X0)/2.
         First construct the vectors V0, V1 and V2. ---*/
   su2double V0[3], V1[3], V2[3];
-  for(unsigned short k=0; k<nDim; ++k) {
-    V0[k] = coor[k] - 0.5*(coorPoints[i1+k] + coorPoints[i2+k]);
-    V1[k] =           0.5*(coorPoints[i1+k] - coorPoints[i0+k]);
-    V2[k] =           0.5*(coorPoints[i2+k] - coorPoints[i0+k]);
+  for (unsigned short k = 0; k < nDim; ++k) {
+    V0[k] = coor[k] - 0.5 * (coorPoints[i1 + k] + coorPoints[i2 + k]);
+    V1[k] = 0.5 * (coorPoints[i1 + k] - coorPoints[i0 + k]);
+    V2[k] = 0.5 * (coorPoints[i2 + k] - coorPoints[i0 + k]);
   }
 
   /*--- For the values of r and s where the minimum occurs the dot products V0.V1,
         V0.V2, V1.V1, V1.V2 and V2.V2 are needed. Compute these values. ---*/
   su2double dotV0V1 = 0.0, dotV0V2 = 0, dotV1V1 = 0.0, dotV1V2 = 0.0, dotV2V2 = 0.0;
-  for(unsigned short k=0; k<nDim; ++k) {
-    dotV0V1 += V0[k]*V1[k];
-    dotV0V2 += V0[k]*V2[k];
-    dotV1V1 += V1[k]*V1[k];
-    dotV1V2 += V1[k]*V2[k];
-    dotV2V2 += V2[k]*V2[k];
+  for (unsigned short k = 0; k < nDim; ++k) {
+    dotV0V1 += V0[k] * V1[k];
+    dotV0V2 += V0[k] * V2[k];
+    dotV1V1 += V1[k] * V1[k];
+    dotV1V2 += V1[k] * V2[k];
+    dotV2V2 += V2[k] * V2[k];
   }
 
   /*--- Solve the linear system for r and s. ---*/
-  const su2double detInv = 1.0/(dotV1V1*dotV2V2 - dotV1V2*dotV1V2);
+  const su2double detInv = 1.0 / (dotV1V1 * dotV2V2 - dotV1V2 * dotV1V2);
 
-  r = detInv*(dotV0V1*dotV2V2 - dotV0V2*dotV1V2);
-  s = detInv*(dotV0V2*dotV1V1 - dotV0V1*dotV1V2);
+  r = detInv * (dotV0V1 * dotV2V2 - dotV0V2 * dotV1V2);
+  s = detInv * (dotV0V2 * dotV1V1 - dotV0V1 * dotV1V2);
 
   /*--- Check if the projection is inside the triangle. ---*/
-  if((r >= paramLowerBound) && (s >= paramLowerBound) && ((r+s) <= tolInsideElem)) {
-
+  if ((r >= paramLowerBound) && (s >= paramLowerBound) && ((r + s) <= tolInsideElem)) {
     /*--- The projection of the coordinate is inside the triangle. Compute the
           minimum distance squared and return true. ---*/
     dist2Tria = 0.0;
-    for(unsigned short k=0; k<nDim; ++k) {
-      const su2double ds = V0[k] - r*V1[k] - s*V2[k];
-      dist2Tria += ds*ds;
+    for (unsigned short k = 0; k < nDim; ++k) {
+      const su2double ds = V0[k] - r * V1[k] - s * V2[k];
+      dist2Tria += ds * ds;
     }
 
     return true;
@@ -1965,21 +2127,15 @@ bool CADTElemClass::Dist2ToTriangle(const unsigned long i0,
   return false;
 }
 
-bool CADTElemClass::Dist2ToQuadrilateral(const unsigned long i0,
-                                         const unsigned long i1,
-                                         const unsigned long i2,
-                                         const unsigned long i3,
-                                         const su2double     *coor,
-                                         su2double           &r,
-                                         su2double           &s,
-                                         su2double           &dist2Quad) const {
-
-  constexpr unsigned short nDim = 3; // boundary quadrilaterals only exist in 3D
+bool CADTElemClass::Dist2ToQuadrilateral(const unsigned long i0, const unsigned long i1, const unsigned long i2,
+                                         const unsigned long i3, const su2double* coor, su2double& r, su2double& s,
+                                         su2double& dist2Quad) const {
+  constexpr unsigned short nDim = 3;  // boundary quadrilaterals only exist in 3D
 
   /* Definition of the maximum number of iterations in the iterative solver
      and the tolerance level. */
   const unsigned short maxIt = 10;
-  const su2double tolIt      = 1.e-10;
+  const su2double tolIt = 1.e-10;
 
   /*--- The quadrilateral is parametrized by
         X = {(1-r)*(1-s)*X0 + (1+r)*(1-s)*X1 + (1+r)*(1+s)*X2 + (1-r)*(1+s)*X3}/4,
@@ -1989,15 +2145,11 @@ bool CADTElemClass::Dist2ToQuadrilateral(const unsigned long i0,
         V1 = (X1+X2-X0-X3)/4, V2 = (X2+X3-X0-X1), V3 = (X0+X2-X1-X3)/4. First
         construct the vectors V0, V1, V2 and V3. ---*/
   su2double V0[3], V1[3], V2[3], V3[3];
-  for(unsigned short k=0; k<nDim; ++k) {
-    V0[k] = coor[k] - 0.25*(coorPoints[i0+k] + coorPoints[i1+k]
-          +                 coorPoints[i2+k] + coorPoints[i3+k]);
-    V1[k] =           0.25*(coorPoints[i1+k] + coorPoints[i2+k]
-          -                 coorPoints[i0+k] - coorPoints[i3+k]);
-    V2[k] =           0.25*(coorPoints[i2+k] + coorPoints[i3+k]
-          -                 coorPoints[i0+k] - coorPoints[i1+k]);
-    V3[k] =           0.25*(coorPoints[i0+k] + coorPoints[i2+k]
-          -                 coorPoints[i1+k] - coorPoints[i3+k]);
+  for (unsigned short k = 0; k < nDim; ++k) {
+    V0[k] = coor[k] - 0.25 * (coorPoints[i0 + k] + coorPoints[i1 + k] + coorPoints[i2 + k] + coorPoints[i3 + k]);
+    V1[k] = 0.25 * (coorPoints[i1 + k] + coorPoints[i2 + k] - coorPoints[i0 + k] - coorPoints[i3 + k]);
+    V2[k] = 0.25 * (coorPoints[i2 + k] + coorPoints[i3 + k] - coorPoints[i0 + k] - coorPoints[i1 + k]);
+    V3[k] = 0.25 * (coorPoints[i0 + k] + coorPoints[i2 + k] - coorPoints[i1 + k] - coorPoints[i3 + k]);
   }
 
   /*--- The minimization problem results in the following
@@ -2007,12 +2159,17 @@ bool CADTElemClass::Dist2ToQuadrilateral(const unsigned long i0,
         These equations are the gradients of the distance function squared w.r.t.
         the parametric coordinates r and s. The coefficients for these equations
         involve a couple of dot products, which are computed first.   ---*/
-  su2double V0V1 = 0.0, V0V2 = 0.0, V0V3 = 0.0, V1V1 = 0.0, V1V2 = 0.0,
-            V1V3 = 0.0, V2V2 = 0.0, V2V3 = 0.0, V3V3 = 0.0;
-  for(unsigned short k=0; k<nDim; ++k) {
-    V0V1 += V0[k]*V1[k]; V0V2 += V0[k]*V2[k]; V0V3 += V0[k]*V3[k];
-    V1V1 += V1[k]*V1[k]; V1V2 += V1[k]*V2[k]; V1V3 += V1[k]*V3[k];
-    V2V2 += V2[k]*V2[k]; V2V3 += V2[k]*V3[k]; V3V3 += V3[k]*V3[k];
+  su2double V0V1 = 0.0, V0V2 = 0.0, V0V3 = 0.0, V1V1 = 0.0, V1V2 = 0.0, V1V3 = 0.0, V2V2 = 0.0, V2V3 = 0.0, V3V3 = 0.0;
+  for (unsigned short k = 0; k < nDim; ++k) {
+    V0V1 += V0[k] * V1[k];
+    V0V2 += V0[k] * V2[k];
+    V0V3 += V0[k] * V3[k];
+    V1V1 += V1[k] * V1[k];
+    V1V2 += V1[k] * V2[k];
+    V1V3 += V1[k] * V3[k];
+    V2V2 += V2[k] * V2[k];
+    V2V3 += V2[k] * V3[k];
+    V3V3 += V3[k] * V3[k];
   }
 
   /*--- The first equation given above is linear in r and can be used to
@@ -2022,9 +2179,9 @@ bool CADTElemClass::Dist2ToQuadrilateral(const unsigned long i0,
         a fifth order equation for s is obtained, i.e.
         a5 s^5 + a4 s^4 + a3 s^3 + a2 s^2 + a1 s + a0 = 0.
         The coefficients for this equation are computed below. ---*/
-  const su2double t1  = V0V1 * V0V1;
-  const su2double t3  = V0V3 - V1V2;
-  const su2double t6  = V1V1 * V1V1;
+  const su2double t1 = V0V1 * V0V1;
+  const su2double t3 = V0V3 - V1V2;
+  const su2double t6 = V1V1 * V1V1;
   const su2double t11 = V0V1 * V2V3 * 2.0;
   const su2double t14 = V0V3 * V0V3;
   const su2double t16 = V0V3 * V1V2 * 2.0;
@@ -2036,33 +2193,36 @@ bool CADTElemClass::Dist2ToQuadrilateral(const unsigned long i0,
 
   su2double a0 = -V1V1 * t3 * V0V1 - t6 * V0V2 + V1V3 * t1;
   su2double a1 = t6 * V2V2 + V1V1 * (-4.0 * V0V2 * V1V3 + t11 - t14 + t16 - t17) + t1 * V3V3;
-  su2double a2 = -4.0 * t22 * V0V2 + V1V3 * (4.0 * V1V1 * V2V2 + t11 - t14 + t16 - t17)
-               + (V0V1 * V3V3 + 3.0 * V2V3 * V1V1) * V0V3 + V1V1 * (-3.0 * V1V2 * V2V3 - 2.0 * t34)
-               - V0V1 * V1V2 * V3V3;
-  su2double a3 = 4.0 * V2V2 * t22 + V1V3 * (4.0 * V2V3 * t3 - 4.0 * t34)
-               + 2.0 * (V2V2 * V3V3 - t50) * V1V1;
+  su2double a2 = -4.0 * t22 * V0V2 + V1V3 * (4.0 * V1V1 * V2V2 + t11 - t14 + t16 - t17) +
+                 (V0V1 * V3V3 + 3.0 * V2V3 * V1V1) * V0V3 + V1V1 * (-3.0 * V1V2 * V2V3 - 2.0 * t34) -
+                 V0V1 * V1V2 * V3V3;
+  su2double a3 = 4.0 * V2V2 * t22 + V1V3 * (4.0 * V2V3 * t3 - 4.0 * t34) + 2.0 * (V2V2 * V3V3 - t50) * V1V1;
   su2double a4 = -t55 * V0V2 + V3V3 * (4.0 * V2V2 * V1V3 + V2V3 * t3) - 3.0 * t50 * V1V3;
   su2double a5 = t55 * V2V2 - V3V3 * t50;
 
   /* Determine the maximum of these coefficients and scale them. */
-  su2double scaleFact = max(fabs(a0),  fabs(a1));
-  scaleFact           = max(scaleFact, fabs(a2));
-  scaleFact           = max(scaleFact, fabs(a3));
-  scaleFact           = max(scaleFact, fabs(a4));
-  scaleFact           = max(scaleFact, fabs(a5));
+  su2double scaleFact = max(fabs(a0), fabs(a1));
+  scaleFact = max(scaleFact, fabs(a2));
+  scaleFact = max(scaleFact, fabs(a3));
+  scaleFact = max(scaleFact, fabs(a4));
+  scaleFact = max(scaleFact, fabs(a5));
 
-  scaleFact = 1.0/scaleFact;
+  scaleFact = 1.0 / scaleFact;
 
-  a0 *= scaleFact; a1 *= scaleFact; a2 *= scaleFact;
-  a3 *= scaleFact; a4 *= scaleFact; a5 *= scaleFact;
+  a0 *= scaleFact;
+  a1 *= scaleFact;
+  a2 *= scaleFact;
+  a3 *= scaleFact;
+  a4 *= scaleFact;
+  a5 *= scaleFact;
 
   /* The coefficients that occur in the derivative of f, i.e.
      b4 s^4 + b3 s^3 + b2 s^2 + b1 s + b0. */
-  const su2double b4 = 5.0*a5;
-  const su2double b3 = 4.0*a4;
-  const su2double b2 = 3.0*a3;
-  const su2double b1 = 2.0*a2;
-  const su2double b0 =     a1;
+  const su2double b4 = 5.0 * a5;
+  const su2double b3 = 4.0 * a4;
+  const su2double b2 = 3.0 * a3;
+  const su2double b1 = 2.0 * a2;
+  const su2double b0 = a1;
 
   /* Initial guess for s. */
   s = 0.0;
@@ -2070,91 +2230,91 @@ bool CADTElemClass::Dist2ToQuadrilateral(const unsigned long i0,
   /*--- Newtons algorithm to solve the nonlinear equation
         a5 s^5 + a4 s^4 + a3 s^3 + a2 s^2 + a1 s + a0 = 0. ---*/
   unsigned short itCount;
-  for(itCount=0; itCount<maxIt; ++itCount) {
-
+  for (itCount = 0; itCount < maxIt; ++itCount) {
     /* Store the old value of s for determining the actual update. */
     const su2double sOld = s;
 
     /* Compute the values of s2 to s5. */
-    const su2double s2 = s*s;
-    const su2double s3 = s2*s;
-    const su2double s4 = s3*s;
-    const su2double s5 = s4*s;
+    const su2double s2 = s * s;
+    const su2double s3 = s2 * s;
+    const su2double s4 = s3 * s;
+    const su2double s5 = s4 * s;
 
     /* Compute the value of the function and its first derivative. */
-    const su2double  f = a5*s5 + a4*s4 + a3*s3 + a2*s2 + a1*s + a0;
-    const su2double df = b4*s4 + b3*s3 + b2*s2 + b1*s  + b0;
+    const su2double f = a5 * s5 + a4 * s4 + a3 * s3 + a2 * s2 + a1 * s + a0;
+    const su2double df = b4 * s4 + b3 * s3 + b2 * s2 + b1 * s + b0;
 
     /* Compute the value of the update and the new value of s. */
-    su2double ds = f/df;
+    su2double ds = f / df;
     s -= ds;
 
     /* Clipping, such that s is bounded to a bit outside the quadrilateral. */
     s = max(s, -1.5);
-    s = min(s,  1.5);
+    s = min(s, 1.5);
 
     /* Set the actual value of ds. */
     ds = sOld - s;
 
     /*--- Check for convergence. ---*/
-    if(fabs(ds) <= tolIt) break;
+    if (fabs(ds) <= tolIt) break;
   }
 
   /* Check if Newtons algorithm did not converge. */
-  if(itCount == maxIt) {
-
+  if (itCount == maxIt) {
     /* Newtons algorithm did not converge. The most likely reason is that there is
        no root for s on the interval paramLowerBound to paramUpperBound. Check this.
        First compute the function value for paramLowerBound. */
     s = paramLowerBound;
 
-    su2double s2 = s*s;
-    su2double s3 = s2*s;
-    su2double s4 = s3*s;
-    su2double s5 = s4*s;
+    su2double s2 = s * s;
+    su2double s3 = s2 * s;
+    su2double s4 = s3 * s;
+    su2double s5 = s4 * s;
 
-    su2double f = a5*s5 + a4*s4 + a3*s3 + a2*s2 + a1*s + a0;
+    su2double f = a5 * s5 + a4 * s4 + a3 * s3 + a2 * s2 + a1 * s + a0;
 
     /* Loop over a number of sampling points to check if the sign of f changes.
        If it does, this means that there is a root between s-ds and s. Hence
        a break from this loop can be made. */
-    const su2double ds = (paramUpperBound - paramLowerBound)*0.1;
-    for(itCount=1; itCount<=10; ++itCount) {
-
+    const su2double ds = (paramUpperBound - paramLowerBound) * 0.1;
+    for (itCount = 1; itCount <= 10; ++itCount) {
       const su2double fOld = f;
       s += ds;
 
-      s2 = s*s; s3 = s2*s; s4 = s3*s; s5 = s4*s;
-      f  = a5*s5 + a4*s4 + a3*s3 + a2*s2 + a1*s + a0;
+      s2 = s * s;
+      s3 = s2 * s;
+      s4 = s3 * s;
+      s5 = s4 * s;
+      f = a5 * s5 + a4 * s4 + a3 * s3 + a2 * s2 + a1 * s + a0;
 
-      if(f*fOld <= 0.0) break;
+      if (f * fOld <= 0.0) break;
     }
 
     /* If the end of the loop is reached this means that there is no root for s
        between the lower and upper bound. Return false. */
-    if(itCount > 10) return false;
+    if (itCount > 10) return false;
 
     /* Newtons algorithm did not converge, but there is a root. Do a crude approximation
        of the root using bisection. */
-    s -= 0.5*ds;
+    s -= 0.5 * ds;
   }
 
   /* Check if s is inside the quadrilateral. If not, return false. */
-  if(s < paramLowerBound || s > paramUpperBound) return false;
+  if (s < paramLowerBound || s > paramUpperBound) return false;
 
   /* Compute the corresponding value of r and check if it is inside the
      quadrilateral. If not return false. */
-  const su2double s2 = s*s;
+  const su2double s2 = s * s;
 
-  r = (V0V1 + (V0V3-V1V2)*s - V2V3*s2)/(V1V1 + 2.0*V1V3*s + V3V3*s2);
-  if(r < paramLowerBound || r > paramUpperBound) return false;
+  r = (V0V1 + (V0V3 - V1V2) * s - V2V3 * s2) / (V1V1 + 2.0 * V1V3 * s + V3V3 * s2);
+  if (r < paramLowerBound || r > paramUpperBound) return false;
 
   /*--- The projection is inside the quadrilateral. Determine the minimum distance
         squared and return true to indicate that the projection is inside. ---*/
   dist2Quad = 0.0;
-  for(unsigned short k=0; k<nDim; ++k) {
-    const su2double ds = V0[k] - r*V1[k] - s*V2[k] - r*s*V3[k];
-    dist2Quad += ds*ds;
+  for (unsigned short k = 0; k < nDim; ++k) {
+    const su2double ds = V0[k] - r * V1[k] - s * V2[k] - r * s * V3[k];
+    dist2Quad += ds * ds;
   }
 
   return true;
diff --git a/Common/src/adt/CADTPointsOnlyClass.cpp b/Common/src/adt/CADTPointsOnlyClass.cpp
index 9c262a47363..0503996c47c 100644
--- a/Common/src/adt/CADTPointsOnlyClass.cpp
+++ b/Common/src/adt/CADTPointsOnlyClass.cpp
@@ -29,12 +29,8 @@
 #include "../../include/parallelization/mpi_structure.hpp"
 #include "../../include/option_structure.hpp"
 
-CADTPointsOnlyClass::CADTPointsOnlyClass(unsigned short nDim,
-                                         unsigned long  nPoints,
-                                         const su2double *coor,
-                                         const unsigned long *pointID,
-                                         const bool     globalTree) {
-
+CADTPointsOnlyClass::CADTPointsOnlyClass(unsigned short nDim, unsigned long nPoints, const su2double* coor,
+                                         const unsigned long* pointID, const bool globalTree) {
   /* Allocate some thread-safe working variables if required. */
 #ifdef HAVE_OMP
   FrontLeaves.resize(omp_get_max_threads());
@@ -46,8 +42,7 @@ CADTPointsOnlyClass::CADTPointsOnlyClass(unsigned short nDim,
 #ifdef HAVE_MPI
 
   /* Parallel mode. Check whether a global or a local tree must be built. */
-  if( globalTree ) {
-
+  if (globalTree) {
     /*--- A global tree must be built. All points are gathered on all ranks.
           First determine the number of points per rank and store them in such
           a way that the info can be used directly in Allgatherv. ---*/
@@ -56,41 +51,40 @@ CADTPointsOnlyClass::CADTPointsOnlyClass(unsigned short nDim,
     SU2_MPI::Comm_size(SU2_MPI::GetComm(), &size);
 
     vector<int> recvCounts(size), displs(size);
-    int sizeLocal = (int) nPoints;
+    int sizeLocal = (int)nPoints;
 
-    SU2_MPI::Allgather(&sizeLocal, 1, MPI_INT, recvCounts.data(), 1,
-                       MPI_INT, SU2_MPI::GetComm());
+    SU2_MPI::Allgather(&sizeLocal, 1, MPI_INT, recvCounts.data(), 1, MPI_INT, SU2_MPI::GetComm());
     displs[0] = 0;
-    for(int i=1; i<size; ++i) displs[i] = displs[i-1] + recvCounts[i-1];
+    for (int i = 1; i < size; ++i) displs[i] = displs[i - 1] + recvCounts[i - 1];
 
     int sizeGlobal = displs.back() + recvCounts.back();
 
     /*--- Gather the local pointID's and the ranks of the nodes on all ranks. ---*/
     localPointIDs.resize(sizeGlobal);
-    SU2_MPI::Allgatherv(pointID, sizeLocal, MPI_UNSIGNED_LONG, localPointIDs.data(),
-                        recvCounts.data(), displs.data(), MPI_UNSIGNED_LONG,
-                        SU2_MPI::GetComm());
+    SU2_MPI::Allgatherv(pointID, sizeLocal, MPI_UNSIGNED_LONG, localPointIDs.data(), recvCounts.data(), displs.data(),
+                        MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
 
     ranksOfPoints.resize(sizeGlobal);
     vector<int> rankLocal(sizeLocal, rank);
-    SU2_MPI::Allgatherv(rankLocal.data(), sizeLocal, MPI_INT, ranksOfPoints.data(),
-                        recvCounts.data(), displs.data(), MPI_INT, SU2_MPI::GetComm());
+    SU2_MPI::Allgatherv(rankLocal.data(), sizeLocal, MPI_INT, ranksOfPoints.data(), recvCounts.data(), displs.data(),
+                        MPI_INT, SU2_MPI::GetComm());
 
     /*--- Gather the coordinates of the points on all ranks. ---*/
-    for(int i=0; i<size; ++i) {recvCounts[i] *= nDim; displs[i] *= nDim;}
-
-    coorPoints.resize(nDim*sizeGlobal);
-    SU2_MPI::Allgatherv(coor, nDim*sizeLocal, MPI_DOUBLE, coorPoints.data(),
-                        recvCounts.data(), displs.data(), MPI_DOUBLE, SU2_MPI::GetComm());
-  }
-  else {
+    for (int i = 0; i < size; ++i) {
+      recvCounts[i] *= nDim;
+      displs[i] *= nDim;
+    }
 
+    coorPoints.resize(nDim * sizeGlobal);
+    SU2_MPI::Allgatherv(coor, nDim * sizeLocal, MPI_DOUBLE, coorPoints.data(), recvCounts.data(), displs.data(),
+                        MPI_DOUBLE, SU2_MPI::GetComm());
+  } else {
     /*--- A local tree must be built. Copy the coordinates and point IDs and
           set the ranks to the rank of this processor. ---*/
     int rank;
     SU2_MPI::Comm_rank(SU2_MPI::GetComm(), &rank);
 
-    coorPoints.assign(coor, coor + nDim*nPoints);
+    coorPoints.assign(coor, coor + nDim * nPoints);
     localPointIDs.assign(pointID, pointID + nPoints);
     ranksOfPoints.assign(nPoints, rank);
   }
@@ -99,7 +93,7 @@ CADTPointsOnlyClass::CADTPointsOnlyClass(unsigned short nDim,
 
   /*--- Sequential mode. Copy the coordinates and point IDs and
         set the ranks to MASTER_NODE. ---*/
-  coorPoints.assign(coor, coor + nDim*nPoints);
+  coorPoints.assign(coor, coor + nDim * nPoints);
   localPointIDs.assign(pointID, pointID + nPoints);
   ranksOfPoints.assign(nPoints, MASTER_NODE);
 
@@ -115,12 +109,8 @@ CADTPointsOnlyClass::CADTPointsOnlyClass(unsigned short nDim,
 }
 
 void CADTPointsOnlyClass::DetermineNearestNode_impl(vector<unsigned long>& frontLeaves,
-                                                    vector<unsigned long>& frontLeavesNew,
-                                                    const su2double *coor,
-                                                    su2double       &dist,
-                                                    unsigned long   &pointID,
-                                                    int             &rankID) const {
-
+                                                    vector<unsigned long>& frontLeavesNew, const su2double* coor,
+                                                    su2double& dist, unsigned long& pointID, int& rankID) const {
   const bool wasActive = AD::BeginPassive();
 
   /*--------------------------------------------------------------------------*/
@@ -130,15 +120,15 @@ void CADTPointsOnlyClass::DetermineNearestNode_impl(vector<unsigned long>& front
   /*--------------------------------------------------------------------------*/
 
   unsigned long kk = leaves[0].centralNodeID, minIndex;
-  const su2double *coorTarget = coorPoints.data() + nDimADT*kk;
+  const su2double* coorTarget = coorPoints.data() + nDimADT * kk;
 
-  pointID  = localPointIDs[kk];
-  rankID   = ranksOfPoints[kk];
+  pointID = localPointIDs[kk];
+  rankID = ranksOfPoints[kk];
   minIndex = kk;
   dist = 0.0;
-  for(unsigned short l=0; l<nDimADT; ++l) {
+  for (unsigned short l = 0; l < nDimADT; ++l) {
     const su2double ds = coor[l] - coorTarget[l];
-    dist += ds*ds;
+    dist += ds * ds;
   }
 
   /*--------------------------------------------------------------------------*/
@@ -155,73 +145,69 @@ void CADTPointsOnlyClass::DetermineNearestNode_impl(vector<unsigned long>& front
   frontLeaves.push_back(0);
 
   /* Infinite loop of the tree traversal. */
-  for(;;) {
-
+  for (;;) {
     /* Initialize the new front, i.e. the front for the next round, to empty. */
     frontLeavesNew.clear();
 
     /* Loop over the leaves of the current front. */
-    for(unsigned long i=0; i<frontLeaves.size(); ++i) {
-
+    for (unsigned long i = 0; i < frontLeaves.size(); ++i) {
       /* Store the current leaf a bit easier in ll and loop over its children. */
       const unsigned long ll = frontLeaves[i];
-      for(unsigned short mm=0; mm<2; ++mm) {
-
+      for (unsigned short mm = 0; mm < 2; ++mm) {
         /* Determine whether this child contains a node or a leaf
            of the next level of the ADT. */
         kk = leaves[ll].children[mm];
-        if( leaves[ll].childrenAreTerminal[mm] ) {
-
+        if (leaves[ll].childrenAreTerminal[mm]) {
           /*--- Child contains a node. Compute the distance squared to this node
                 and store it if this distance squared is less than the currently
                 stored value. ---*/
-          coorTarget = coorPoints.data() + nDimADT*kk;
+          coorTarget = coorPoints.data() + nDimADT * kk;
           su2double distTarget = 0;
-          for(unsigned short l=0; l<nDimADT; ++l) {
+          for (unsigned short l = 0; l < nDimADT; ++l) {
             const su2double ds = coor[l] - coorTarget[l];
-            distTarget += ds*ds;
+            distTarget += ds * ds;
           }
 
-          if(distTarget < dist) {
-            dist     = distTarget;
-            pointID  = localPointIDs[kk];
-            rankID   = ranksOfPoints[kk];
+          if (distTarget < dist) {
+            dist = distTarget;
+            pointID = localPointIDs[kk];
+            rankID = ranksOfPoints[kk];
             minIndex = kk;
           }
-        }
-        else {
-
+        } else {
           /*--- Child contains a leaf. Determine the possible minimum distance
                 squared to that leaf. ---*/
           su2double posDist = 0.0;
-          for(unsigned short l=0; l<nDimADT; ++l) {
+          for (unsigned short l = 0; l < nDimADT; ++l) {
             su2double ds = 0.0;
-            if(     coor[l] < leaves[kk].xMin[l]) ds = coor[l] - leaves[kk].xMin[l];
-            else if(coor[l] > leaves[kk].xMax[l]) ds = coor[l] - leaves[kk].xMax[l];
+            if (coor[l] < leaves[kk].xMin[l])
+              ds = coor[l] - leaves[kk].xMin[l];
+            else if (coor[l] > leaves[kk].xMax[l])
+              ds = coor[l] - leaves[kk].xMax[l];
 
-            posDist += ds*ds;
+            posDist += ds * ds;
           }
 
           /*--- Check if the possible minimum distance is less than the currently
                 stored minimum distance. If so this leaf must be stored for the
                 next round. In that case the distance squared to the central node is
                 determined, which is used to update the currently stored value. ---*/
-          if(posDist < dist) {
+          if (posDist < dist) {
             frontLeavesNew.push_back(kk);
 
             const unsigned long jj = leaves[kk].centralNodeID;
 
-            coorTarget = coorPoints.data() + nDimADT*jj;
+            coorTarget = coorPoints.data() + nDimADT * jj;
             su2double distTarget = 0;
-            for(unsigned short l=0; l<nDimADT; ++l) {
+            for (unsigned short l = 0; l < nDimADT; ++l) {
               const su2double ds = coor[l] - coorTarget[l];
-              distTarget += ds*ds;
+              distTarget += ds * ds;
             }
 
-            if(distTarget < dist) {
-              dist     = distTarget;
-              pointID  = localPointIDs[jj];
-              rankID   = ranksOfPoints[jj];
+            if (distTarget < dist) {
+              dist = distTarget;
+              pointID = localPointIDs[jj];
+              rankID = ranksOfPoints[jj];
               minIndex = jj;
             }
           }
@@ -234,22 +220,20 @@ void CADTPointsOnlyClass::DetermineNearestNode_impl(vector<unsigned long>& front
           is empty the entire tree has been traversed and a break can be made
           from the infinite loop. ---*/
     frontLeaves = frontLeavesNew;
-    if(frontLeaves.size() == 0) break;
+    if (frontLeaves.size() == 0) break;
   }
 
   AD::EndPassive(wasActive);
 
   /* Recompute the distance to get the correct dependency if we use AD */
-  coorTarget = coorPoints.data() + nDimADT*minIndex;
+  coorTarget = coorPoints.data() + nDimADT * minIndex;
   dist = 0.0;
-  for(unsigned short l=0; l<nDimADT; ++l) {
+  for (unsigned short l = 0; l < nDimADT; ++l) {
     const su2double ds = coor[l] - coorTarget[l];
-    dist += ds*ds;
+    dist += ds * ds;
   }
 
-
   /* At the moment the distance squared to the nearest node is stored.
      Take the sqrt to obtain the correct value. */
   dist = sqrt(dist);
-
 }
diff --git a/Common/src/basic_types/ad_structure.cpp b/Common/src/basic_types/ad_structure.cpp
index 90d625a5ea7..4da61b9c57b 100644
--- a/Common/src/basic_types/ad_structure.cpp
+++ b/Common/src/basic_types/ad_structure.cpp
@@ -29,33 +29,33 @@
 
 namespace AD {
 #ifdef CODI_REVERSE_TYPE
-  /*--- Initialization of the global variables ---*/
+/*--- Initialization of the global variables ---*/
 
-  TapePosition StartPosition, EndPosition;
-  std::vector<TapePosition> TapePositions;
+TapePosition StartPosition, EndPosition;
+std::vector<TapePosition> TapePositions;
 
-  bool PreaccActive = false;
+bool PreaccActive = false;
 #ifdef HAVE_OPDI
-  SU2_OMP(threadprivate(PreaccActive))
+SU2_OMP(threadprivate(PreaccActive))
 #endif
 
-  bool PreaccEnabled = true;
+bool PreaccEnabled = true;
 
-  codi::PreaccumulationHelper<su2double> PreaccHelper;
+codi::PreaccumulationHelper<su2double> PreaccHelper;
 #ifdef HAVE_OPDI
-  SU2_OMP(threadprivate(PreaccHelper))
+SU2_OMP(threadprivate(PreaccHelper))
 #endif
 
-  ExtFuncHelper FuncHelper;
+ExtFuncHelper FuncHelper;
 
 #endif
 
-  void Initialize() {
+void Initialize() {
 #ifdef CODI_REVERSE_TYPE
-    FuncHelper.disableInputPrimalStore();
-    FuncHelper.disableOutputPrimalStore();
+  FuncHelper.disableInputPrimalStore();
+  FuncHelper.disableOutputPrimalStore();
 #endif
-  }
-
-  void Finalize() {}
 }
+
+void Finalize() {}
+}  // namespace AD
diff --git a/Common/src/containers/CFileReaderLUT.cpp b/Common/src/containers/CFileReaderLUT.cpp
index ba3f19841ee..5362a81406f 100644
--- a/Common/src/containers/CFileReaderLUT.cpp
+++ b/Common/src/containers/CFileReaderLUT.cpp
@@ -135,12 +135,9 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
           SU2_MPI::Error("Table levels are not provided in ascending order.", CURRENT_FUNCTION);
       }
       auto duplicate = adjacent_find(table_levels.begin(), table_levels.end()) != table_levels.end();
-      if (duplicate)
-        SU2_MPI::Error("Duplicate table levels are present in LUT file", CURRENT_FUNCTION);
+      if (duplicate) SU2_MPI::Error("Duplicate table levels are present in LUT file", CURRENT_FUNCTION);
     }
 
-    
-
     /*--- number of variables in LUT ---*/
     if (line.compare("[Number of variables]") == 0) {
       GetNextNonEmptyLine(file_stream, line);
@@ -367,4 +364,4 @@ bool CFileReaderLUT::GetStrippedLine(ifstream& file_stream, string& line) const
 
   /*--- return true if line is not empty, else return false ---*/
   return !line.empty();
-}
\ No newline at end of file
+}
diff --git a/Common/src/fem/fem_cgns_elements.cpp b/Common/src/fem/fem_cgns_elements.cpp
index 15f1e49256f..4069b164321 100644
--- a/Common/src/fem/fem_cgns_elements.cpp
+++ b/Common/src/fem/fem_cgns_elements.cpp
@@ -38,20 +38,16 @@ using namespace std;
 
 #if CGNS_VERSION >= 3300
 
-void CCGNSElementType::DetermineMetaData(const unsigned short nDim,
-                                         const int            fn,
-                                         const int            iBase,
-                                         const int            iZone,
-                                         const int            iConn) {
-
+void CCGNSElementType::DetermineMetaData(const unsigned short nDim, const int fn, const int iBase, const int iZone,
+                                         const int iConn) {
   /* Store the connectivity ID. */
   connID = iConn;
 
   /* Read the element type and range from the CGNS file. */
   char cgnsname[CGNS_STRING_SIZE];
   int nBndry, parentFlag;
-  if(cg_section_read(fn, iBase, iZone, iConn, cgnsname, &elemType,
-                     &indBeg, &indEnd, &nBndry, &parentFlag) != CG_OK) cg_error_exit();
+  if (cg_section_read(fn, iBase, iZone, iConn, cgnsname, &elemType, &indBeg, &indEnd, &nBndry, &parentFlag) != CG_OK)
+    cg_error_exit();
 
   /* Store the name of this connectivity. */
   connName = cgnsname;
@@ -65,46 +61,40 @@ void CCGNSElementType::DetermineMetaData(const unsigned short nDim,
      e.g. line elements for 3D. This information is not needed for the DG
      flow solver and is therefore ignored. */
   const unsigned short nDimElem = DetermineElementDimension(fn, iBase, iZone);
-  volumeConn  = (nDimElem == nDim);
-  surfaceConn = (nDimElem == nDim-1);
+  volumeConn = (nDimElem == nDim);
+  surfaceConn = (nDimElem == nDim - 1);
 }
 
-void CCGNSElementType::ReadBoundaryConnectivityRange(
-                                      const int             fn,
-                                      const int             iBase,
-                                      const int             iZone,
-                                      const unsigned long   offsetRank,
-                                      const unsigned long   nBoundElemRank,
-                                      const unsigned long   startingBoundElemIDRank,
-                                      unsigned long         &locBoundElemCount,
-                                      vector<CBoundaryFace> &boundElems) {
-
+void CCGNSElementType::ReadBoundaryConnectivityRange(const int fn, const int iBase, const int iZone,
+                                                     const unsigned long offsetRank, const unsigned long nBoundElemRank,
+                                                     const unsigned long startingBoundElemIDRank,
+                                                     unsigned long& locBoundElemCount,
+                                                     vector<CBoundaryFace>& boundElems) {
   /* Determine the index range to be read for this rank. */
   const cgsize_t iBeg = indBeg + offsetRank;
-  const cgsize_t iEnd = iBeg + nBoundElemRank -1;
+  const cgsize_t iEnd = iBeg + nBoundElemRank - 1;
 
   /* Determine the size of the vector needed to read the connectivity
      data from the CGNS file. */
   cgsize_t sizeNeeded;
-  if(cg_ElementPartialSize(fn, iBase, iZone, connID, iBeg, iEnd,
-                           &sizeNeeded) != CG_OK) cg_error_exit();
+  if (cg_ElementPartialSize(fn, iBase, iZone, connID, iBeg, iEnd, &sizeNeeded) != CG_OK) cg_error_exit();
 
   /* Allocate the memory for the connectivity and read the data. */
   vector<cgsize_t> connCGNSVec(sizeNeeded);
-  if(elemType == MIXED){
-    vector<cgsize_t> connCGNSOffsetVec(iEnd-iBeg+2);
-    if(cg_poly_elements_partial_read(fn, iBase, iZone, connID, iBeg, iEnd,
-                              connCGNSVec.data(), connCGNSOffsetVec.data(), NULL) != CG_OK)
+  if (elemType == MIXED) {
+    vector<cgsize_t> connCGNSOffsetVec(iEnd - iBeg + 2);
+    if (cg_poly_elements_partial_read(fn, iBase, iZone, connID, iBeg, iEnd, connCGNSVec.data(),
+                                      connCGNSOffsetVec.data(), NULL) != CG_OK)
       cg_error_exit();
   } else {
-    if(cg_elements_partial_read(fn, iBase, iZone, connID, iBeg, iEnd,
-                              connCGNSVec.data(), NULL) != CG_OK) cg_error_exit();
+    if (cg_elements_partial_read(fn, iBase, iZone, connID, iBeg, iEnd, connCGNSVec.data(), NULL) != CG_OK)
+      cg_error_exit();
   }
 
   /* Define the variables needed to convert the connectivities from CGNS to
      SU2 format. Note that the vectors are needed to support a connectivity
      section with mixed element types. */
-  vector<ElementType_t>  CGNS_Type;
+  vector<ElementType_t> CGNS_Type;
   vector<unsigned short> VTK_Type;
   vector<unsigned short> nPoly;
   vector<unsigned short> nDOFs;
@@ -112,25 +102,23 @@ void CCGNSElementType::ReadBoundaryConnectivityRange(
   vector<vector<unsigned short> > SU2ToCGNS;
 
   /* Definition of variables used in the loop below. */
-  cgsize_t *connCGNS = connCGNSVec.data();
+  cgsize_t* connCGNS = connCGNSVec.data();
   ElementType_t typeElem = elemType;
   vector<unsigned long> connSU2;
 
   /* Loop over the elements just read. */
-  for(unsigned long i=0; i<nBoundElemRank; ++i, ++locBoundElemCount) {
-
+  for (unsigned long i = 0; i < nBoundElemRank; ++i, ++locBoundElemCount) {
     /* Determine the element type for this element if this is a mixed
        connectivity and set the pointer to the actual connectivity data. */
-    if(elemType == MIXED) {
-      typeElem = (ElementType_t) connCGNS[0];
+    if (elemType == MIXED) {
+      typeElem = (ElementType_t)connCGNS[0];
       ++connCGNS;
     }
 
     /* Determine the index in the stored vectors (CGNS_Type, VTK_Type, etc),
        which corresponds to this element. If the type is not stored yet,
        a new entry in these vectors will be created. */
-    const unsigned short ind = IndexInStoredTypes(typeElem, CGNS_Type, VTK_Type,
-                                                  nPoly, nDOFs, SU2ToCGNS);
+    const unsigned short ind = IndexInStoredTypes(typeElem, CGNS_Type, VTK_Type, nPoly, nDOFs, SU2ToCGNS);
 
     /* Resize the connSU2 vector to the appropriate size. */
     connSU2.resize(nDOFs[ind]);
@@ -138,68 +126,59 @@ void CCGNSElementType::ReadBoundaryConnectivityRange(
     /* Create the connectivity used in SU2 by carrying out the renumbering.
        Note that in CGNS the numbering starts at 1, while in SU2 it starts
        at 0. This explains the addition of -1. */
-    for(unsigned short j=0; j<nDOFs[ind]; ++j)
-      connSU2[j] = connCGNS[SU2ToCGNS[ind][j]] - 1;
+    for (unsigned short j = 0; j < nDOFs[ind]; ++j) connSU2[j] = connCGNS[SU2ToCGNS[ind][j]] - 1;
 
     /* Set the pointer for connCGNS for the data of the next element. */
     connCGNS += nDOFs[ind];
 
     /* Determine the global boundary element ID of this element. */
-    const unsigned long globBoundElemID = startingBoundElemIDRank
-                                        + locBoundElemCount;
+    const unsigned long globBoundElemID = startingBoundElemIDRank + locBoundElemCount;
 
     /* Create an object of CBoundaryFace and store it in boundElems.
        Note that the corresponding domain element is not known yet and
        is therefore set to ULONG_MAX. */
     CBoundaryFace thisBoundFace;
-    thisBoundFace.VTK_Type          = VTK_Type[ind];
-    thisBoundFace.nPolyGrid         = nPoly[ind];
-    thisBoundFace.nDOFsGrid         = nDOFs[ind];
+    thisBoundFace.VTK_Type = VTK_Type[ind];
+    thisBoundFace.nPolyGrid = nPoly[ind];
+    thisBoundFace.nDOFsGrid = nDOFs[ind];
     thisBoundFace.globalBoundElemID = globBoundElemID;
-    thisBoundFace.domainElementID   = ULONG_MAX;
-    thisBoundFace.Nodes             = connSU2;
+    thisBoundFace.domainElementID = ULONG_MAX;
+    thisBoundFace.Nodes = connSU2;
 
     boundElems.push_back(thisBoundFace);
   }
 }
 
-void CCGNSElementType::ReadConnectivityRange(const int           fn,
-                                             const int           iBase,
-                                             const int           iZone,
-                                             const unsigned long offsetRank,
-                                             const unsigned long nElemRank,
-                                             const unsigned long startingElemIDRank,
-                                             CPrimalGrid         **&elem,
-                                             unsigned long       &locElemCount,
-                                             unsigned long       &nDOFsLoc) {
-
+void CCGNSElementType::ReadConnectivityRange(const int fn, const int iBase, const int iZone,
+                                             const unsigned long offsetRank, const unsigned long nElemRank,
+                                             const unsigned long startingElemIDRank, CPrimalGrid**& elem,
+                                             unsigned long& locElemCount, unsigned long& nDOFsLoc) {
   /* Determine the index range to be read for this rank. */
   const cgsize_t iBeg = indBeg + offsetRank;
-  const cgsize_t iEnd = iBeg + nElemRank -1;
+  const cgsize_t iEnd = iBeg + nElemRank - 1;
 
   /* Determine the size of the vector needed to read the connectivity
      data from the CGNS file. */
   cgsize_t sizeNeeded;
-  if(cg_ElementPartialSize(fn, iBase, iZone, connID, iBeg, iEnd,
-                           &sizeNeeded) != CG_OK) cg_error_exit();
+  if (cg_ElementPartialSize(fn, iBase, iZone, connID, iBeg, iEnd, &sizeNeeded) != CG_OK) cg_error_exit();
 
   /* Allocate the memory for the connectivity and read the data. */
   vector<cgsize_t> connCGNSVec(sizeNeeded);
   if (elemType == MIXED) {
-    vector<cgsize_t> connCGNSOffsetVec(iEnd-iBeg+2);
-    if(cg_poly_elements_partial_read(fn, iBase, iZone, connID, iBeg, iEnd,
-                              connCGNSVec.data(), connCGNSOffsetVec.data(), NULL) != CG_OK)
+    vector<cgsize_t> connCGNSOffsetVec(iEnd - iBeg + 2);
+    if (cg_poly_elements_partial_read(fn, iBase, iZone, connID, iBeg, iEnd, connCGNSVec.data(),
+                                      connCGNSOffsetVec.data(), NULL) != CG_OK)
       cg_error_exit();
 
   } else {
-    if(cg_elements_partial_read(fn, iBase, iZone, connID, iBeg, iEnd,
-                              connCGNSVec.data(), NULL) != CG_OK) cg_error_exit();
+    if (cg_elements_partial_read(fn, iBase, iZone, connID, iBeg, iEnd, connCGNSVec.data(), NULL) != CG_OK)
+      cg_error_exit();
   }
 
   /* Define the variables needed to convert the connectivities from CGNS to
      SU2 format. Note that the vectors are needed to support a connectivity
      section with mixed element types. */
-  vector<ElementType_t>  CGNS_Type;
+  vector<ElementType_t> CGNS_Type;
   vector<unsigned short> VTK_Type;
   vector<unsigned short> nPoly;
   vector<unsigned short> nDOFs;
@@ -207,25 +186,23 @@ void CCGNSElementType::ReadConnectivityRange(const int           fn,
   vector<vector<unsigned short> > SU2ToCGNS;
 
   /* Definition of variables used in the loop below. */
-  cgsize_t *connCGNS = connCGNSVec.data();
+  cgsize_t* connCGNS = connCGNSVec.data();
   ElementType_t typeElem = elemType;
   vector<unsigned long> connSU2;
 
   /* Loop over the elements just read. */
-  for(unsigned long i=0; i<nElemRank; ++i, ++locElemCount) {
-
+  for (unsigned long i = 0; i < nElemRank; ++i, ++locElemCount) {
     /* Determine the element type for this element if this is a mixed
        connectivity and set the pointer to the actual connectivity data. */
-    if(elemType == MIXED) {
-      typeElem = (ElementType_t) connCGNS[0];
+    if (elemType == MIXED) {
+      typeElem = (ElementType_t)connCGNS[0];
       ++connCGNS;
     }
 
     /* Determine the index in the stored vectors (CGNS_Type, VTK_Type, etc),
        which corresponds to this element. If the type is not stored yet,
        a new entry in these vectors will be created. */
-    const unsigned short ind = IndexInStoredTypes(typeElem, CGNS_Type, VTK_Type,
-                                                  nPoly, nDOFs, SU2ToCGNS);
+    const unsigned short ind = IndexInStoredTypes(typeElem, CGNS_Type, VTK_Type, nPoly, nDOFs, SU2ToCGNS);
 
     /* Resize the connSU2 vector to the appropriate size. */
     connSU2.resize(nDOFs[ind]);
@@ -233,8 +210,7 @@ void CCGNSElementType::ReadConnectivityRange(const int           fn,
     /* Create the connectivity used in SU2 by carrying out the renumbering.
        Note that in CGNS the numbering starts at 1, while in SU2 it starts
        at 0. This explains the addition of -1. */
-    for(unsigned short j=0; j<nDOFs[ind]; ++j)
-      connSU2[j] = connCGNS[SU2ToCGNS[ind][j]] - 1;
+    for (unsigned short j = 0; j < nDOFs[ind]; ++j) connSU2[j] = connCGNS[SU2ToCGNS[ind][j]] - 1;
 
     /* Set the pointer for connCGNS for the data of the next element. */
     connCGNS += nDOFs[ind];
@@ -248,8 +224,7 @@ void CCGNSElementType::ReadConnectivityRange(const int           fn,
        afterwards in CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM.
        Also note that in CGNS it is not possible (at least at the moment)
        to specify a different polynomial degree for the grid and solution. */
-    elem[locElemCount] = new CPrimalGridFEM(globElemID, VTK_Type[ind], nPoly[ind],
-                                            nPoly[ind], nDOFs[ind], nDOFs[ind],
+    elem[locElemCount] = new CPrimalGridFEM(globElemID, VTK_Type[ind], nPoly[ind], nPoly[ind], nDOFs[ind], nDOFs[ind],
                                             nDOFsLoc, connSU2.data());
 
     /* Update the counter nDOFsLoc. */
@@ -257,35 +232,69 @@ void CCGNSElementType::ReadConnectivityRange(const int           fn,
   }
 }
 
-unsigned short CCGNSElementType::DetermineElementDimension(const int fn,
-                                                           const int iBase,
-                                                           const int iZone) {
-
+unsigned short CCGNSElementType::DetermineElementDimension(const int fn, const int iBase, const int iZone) {
   /*--- Determine the element type and return the appropriate element
         dimension, i.e. the number of parametric coordinates needed to
         describe the element. ---*/
-  switch( elemType ) {
+  switch (elemType) {
     case NODE:
       return 0;
 
-    case BAR_2: case BAR_3: case BAR_4: case BAR_5:
+    case BAR_2:
+    case BAR_3:
+    case BAR_4:
+    case BAR_5:
       return 1;
 
-    case TRI_3:  case TRI_6:   case TRI_9:   case TRI_10:
-    case TRI_12: case TRI_15:  case QUAD_4:  case QUAD_8:
-    case QUAD_9: case QUAD_12: case QUAD_16: case QUAD_P4_16:
+    case TRI_3:
+    case TRI_6:
+    case TRI_9:
+    case TRI_10:
+    case TRI_12:
+    case TRI_15:
+    case QUAD_4:
+    case QUAD_8:
+    case QUAD_9:
+    case QUAD_12:
+    case QUAD_16:
+    case QUAD_P4_16:
     case QUAD_25:
       return 2;
 
-    case TETRA_4:  case TETRA_10:   case TETRA_16: case TETRA_20:
-    case TETRA_22: case TETRA_34:   case TETRA_35: case PYRA_5:
-    case PYRA_14:  case PYRA_13:    case PYRA_21:  case PYRA_29:
-    case PYRA_30:  case PYRA_P4_29: case PYRA_50:  case PYRA_55:
-    case PENTA_6:  case PENTA_15:   case PENTA_18: case PENTA_24:
-    case PENTA_38: case PENTA_40:   case PENTA_33: case PENTA_66:
-    case PENTA_75: case HEXA_8:     case HEXA_20:  case HEXA_27:
-    case HEXA_32:  case HEXA_56:    case HEXA_64:  case HEXA_44:
-    case HEXA_98:  case HEXA_125:
+    case TETRA_4:
+    case TETRA_10:
+    case TETRA_16:
+    case TETRA_20:
+    case TETRA_22:
+    case TETRA_34:
+    case TETRA_35:
+    case PYRA_5:
+    case PYRA_14:
+    case PYRA_13:
+    case PYRA_21:
+    case PYRA_29:
+    case PYRA_30:
+    case PYRA_P4_29:
+    case PYRA_50:
+    case PYRA_55:
+    case PENTA_6:
+    case PENTA_15:
+    case PENTA_18:
+    case PENTA_24:
+    case PENTA_38:
+    case PENTA_40:
+    case PENTA_33:
+    case PENTA_66:
+    case PENTA_75:
+    case HEXA_8:
+    case HEXA_20:
+    case HEXA_27:
+    case HEXA_32:
+    case HEXA_56:
+    case HEXA_64:
+    case HEXA_44:
+    case HEXA_98:
+    case HEXA_125:
       return 3;
 
     case MIXED:
@@ -302,25 +311,23 @@ unsigned short CCGNSElementType::DetermineElementDimension(const int fn,
   return 0;
 }
 
-unsigned short CCGNSElementType::DetermineElementDimensionMixed(const int fn,
-                                                                const int iBase,
-                                                                const int iZone) {
+unsigned short CCGNSElementType::DetermineElementDimensionMixed(const int fn, const int iBase, const int iZone) {
   /* Determine the required size of the vector to read the
      data of the first element of this connectivity. */
   cgsize_t sizeNeeded;
-  if(cg_ElementPartialSize(fn, iBase, iZone, connID, indBeg, indBeg,
-                           &sizeNeeded) != CG_OK) cg_error_exit();
+  if (cg_ElementPartialSize(fn, iBase, iZone, connID, indBeg, indBeg, &sizeNeeded) != CG_OK) cg_error_exit();
 
   /* Read the data of the first element in this section. */
   vector<cgsize_t> buf(sizeNeeded);
   vector<cgsize_t> buf_offset(2, 0);
-  if(cg_poly_elements_partial_read(fn, iBase, iZone, connID, indBeg, indBeg,
-                              buf.data(), buf_offset.data(), NULL) != CG_OK) cg_error_exit();
+  if (cg_poly_elements_partial_read(fn, iBase, iZone, connID, indBeg, indBeg, buf.data(), buf_offset.data(), NULL) !=
+      CG_OK)
+    cg_error_exit();
 
   /* The first entry of buf contains the element type. Copy this value
      temporarily into the member variable elemType and determine the
      element dimension of this element. */
-  elemType = (ElementType_t) buf[0];
+  elemType = (ElementType_t)buf[0];
 
   unsigned short nDimElem = DetermineElementDimension(fn, iBase, iZone);
 
@@ -329,24 +336,19 @@ unsigned short CCGNSElementType::DetermineElementDimensionMixed(const int fn,
   return nDimElem;
 }
 
-unsigned short CCGNSElementType::IndexInStoredTypes(
-                                  const ElementType_t             typeElem,
-                                  vector<ElementType_t>           &CGNS_Type,
-                                  vector<unsigned short>          &VTK_Type,
-                                  vector<unsigned short>          &nPoly,
-                                  vector<unsigned short>          &nDOFs,
-                                  vector<vector<unsigned short> > &SU2ToCGNS) {
-
+unsigned short CCGNSElementType::IndexInStoredTypes(const ElementType_t typeElem, vector<ElementType_t>& CGNS_Type,
+                                                    vector<unsigned short>& VTK_Type, vector<unsigned short>& nPoly,
+                                                    vector<unsigned short>& nDOFs,
+                                                    vector<vector<unsigned short> >& SU2ToCGNS) {
   /* Loop over the available types and check if the current type is present.
      If so, break the loop, such that the correct index is stored. */
   unsigned short ind;
-  for(ind=0; ind<CGNS_Type.size(); ++ind)
-    if(typeElem == CGNS_Type[ind]) break;
+  for (ind = 0; ind < CGNS_Type.size(); ++ind)
+    if (typeElem == CGNS_Type[ind]) break;
 
   /* If the current element type is not present yet, the data for this
      type must be created. */
-  if(ind == CGNS_Type.size()) {
-
+  if (ind == CGNS_Type.size()) {
     unsigned short VTKElem, nPolyElem, nDOFsElem;
     vector<unsigned short> SU2ToCGNSElem;
     CreateDataElementType(typeElem, VTKElem, nPolyElem, nDOFsElem, SU2ToCGNSElem);
@@ -362,46 +364,99 @@ unsigned short CCGNSElementType::IndexInStoredTypes(
   return ind;
 }
 
-void CCGNSElementType::CreateDataElementType(
-                                     const ElementType_t    typeElem,
-                                     unsigned short         &VTK_Type,
-                                     unsigned short         &nPoly,
-                                     unsigned short         &nDOFs,
-                                     vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataElementType(const ElementType_t typeElem, unsigned short& VTK_Type,
+                                             unsigned short& nPoly, unsigned short& nDOFs,
+                                             vector<unsigned short>& SU2ToCGNS) {
   /*--- Determine the element type and call the corresponding function
         to determine the actual data. ---*/
-  switch( typeElem ) {
-
-    case NODE:     CreateDataNODE(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case BAR_2:    CreateDataBAR_2(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case BAR_3:    CreateDataBAR_3(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case BAR_4:    CreateDataBAR_4(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case BAR_5:    CreateDataBAR_5(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case TRI_3:    CreateDataTRI_3(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case TRI_6:    CreateDataTRI_6(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case TRI_10:   CreateDataTRI_10(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case TRI_15:   CreateDataTRI_15(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case QUAD_4:   CreateDataQUAD_4(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case QUAD_9:   CreateDataQUAD_9(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case QUAD_16:  CreateDataQUAD_16(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case QUAD_25:  CreateDataQUAD_25(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case TETRA_4:  CreateDataTETRA_4(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case TETRA_10: CreateDataTETRA_10(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case TETRA_20: CreateDataTETRA_20(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case TETRA_35: CreateDataTETRA_35(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case PYRA_5:   CreateDataPYRA_5(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case PYRA_14:  CreateDataPYRA_14(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case PYRA_30:  CreateDataPYRA_30(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case PYRA_55:  CreateDataPYRA_55(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case PENTA_6:  CreateDataPENTA_6(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case PENTA_18: CreateDataPENTA_18(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case PENTA_40: CreateDataPENTA_40(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case PENTA_75: CreateDataPENTA_75(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case HEXA_8:   CreateDataHEXA_8(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case HEXA_27:  CreateDataHEXA_27(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case HEXA_64:  CreateDataHEXA_64(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
-    case HEXA_125: CreateDataHEXA_125(VTK_Type, nPoly, nDOFs, SU2ToCGNS); break;
+  switch (typeElem) {
+    case NODE:
+      CreateDataNODE(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case BAR_2:
+      CreateDataBAR_2(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case BAR_3:
+      CreateDataBAR_3(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case BAR_4:
+      CreateDataBAR_4(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case BAR_5:
+      CreateDataBAR_5(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case TRI_3:
+      CreateDataTRI_3(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case TRI_6:
+      CreateDataTRI_6(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case TRI_10:
+      CreateDataTRI_10(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case TRI_15:
+      CreateDataTRI_15(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case QUAD_4:
+      CreateDataQUAD_4(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case QUAD_9:
+      CreateDataQUAD_9(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case QUAD_16:
+      CreateDataQUAD_16(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case QUAD_25:
+      CreateDataQUAD_25(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case TETRA_4:
+      CreateDataTETRA_4(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case TETRA_10:
+      CreateDataTETRA_10(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case TETRA_20:
+      CreateDataTETRA_20(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case TETRA_35:
+      CreateDataTETRA_35(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case PYRA_5:
+      CreateDataPYRA_5(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case PYRA_14:
+      CreateDataPYRA_14(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case PYRA_30:
+      CreateDataPYRA_30(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case PYRA_55:
+      CreateDataPYRA_55(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case PENTA_6:
+      CreateDataPENTA_6(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case PENTA_18:
+      CreateDataPENTA_18(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case PENTA_40:
+      CreateDataPENTA_40(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case PENTA_75:
+      CreateDataPENTA_75(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case HEXA_8:
+      CreateDataHEXA_8(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case HEXA_27:
+      CreateDataHEXA_27(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case HEXA_64:
+      CreateDataHEXA_64(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
+    case HEXA_125:
+      CreateDataHEXA_125(VTK_Type, nPoly, nDOFs, SU2ToCGNS);
+      break;
 
     default:
       /* Print an error message that this element type is not supported and exit. */
@@ -416,102 +471,92 @@ void CCGNSElementType::CreateDataElementType(
 /*--- CGNS and SU2 format for the specific elements.                   ---*/
 /*------------------------------------------------------------------------*/
 
-void CCGNSElementType::CreateDataNODE(unsigned short         &VTK_Type,
-                                      unsigned short         &nPoly,
-                                      unsigned short         &nDOFs,
-                                      vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataNODE(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                      vector<unsigned short>& SU2ToCGNS) {
   /* Set the required data for a NODE. */
   VTK_Type = VERTEX;
-  nPoly    = 0;
-  nDOFs    = 1;
+  nPoly = 0;
+  nDOFs = 1;
   SU2ToCGNS.push_back(0);
 }
 
-void CCGNSElementType::CreateDataBAR_2(unsigned short         &VTK_Type,
-                                       unsigned short         &nPoly,
-                                       unsigned short         &nDOFs,
-                                       vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataBAR_2(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                       vector<unsigned short>& SU2ToCGNS) {
   /* The BAR_2 element is a linear element. The numbering of the nodes is
      the same for CGNS and SU2. */
   VTK_Type = LINE;
-  nPoly    = 1;
-  nDOFs    = 2;
+  nPoly = 1;
+  nDOFs = 2;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0] = 0; SU2ToCGNS[1] = 1;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 1;
 }
 
-void CCGNSElementType::CreateDataBAR_3(unsigned short         &VTK_Type,
-                                       unsigned short         &nPoly,
-                                       unsigned short         &nDOFs,
-                                       vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataBAR_3(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                       vector<unsigned short>& SU2ToCGNS) {
   /* The BAR_3 element is a quadratic element. SU2 numbers to nodes with
      increasing parametric value, while in CGNS the internal node is
      numbered last. */
   VTK_Type = LINE;
-  nPoly    = 2;
-  nDOFs    = 3;
+  nPoly = 2;
+  nDOFs = 3;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0] = 0; SU2ToCGNS[1] = 2; SU2ToCGNS[2] = 1;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 2;
+  SU2ToCGNS[2] = 1;
 }
 
-void CCGNSElementType::CreateDataBAR_4(unsigned short         &VTK_Type,
-                                       unsigned short         &nPoly,
-                                       unsigned short         &nDOFs,
-                                       vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataBAR_4(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                       vector<unsigned short>& SU2ToCGNS) {
   /* The BAR_4 element is a cubic element. SU2 numbers to nodes with
      increasing parametric value, while in CGNS the internal nodes are
      numbered last. */
   VTK_Type = LINE;
-  nPoly    = 3;
-  nDOFs    = 4;
+  nPoly = 3;
+  nDOFs = 4;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0] = 0; SU2ToCGNS[1] = 2; SU2ToCGNS[2] = 3; SU2ToCGNS[3] = 1;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 2;
+  SU2ToCGNS[2] = 3;
+  SU2ToCGNS[3] = 1;
 }
 
-void CCGNSElementType::CreateDataBAR_5(unsigned short         &VTK_Type,
-                                       unsigned short         &nPoly,
-                                       unsigned short         &nDOFs,
-                                       vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataBAR_5(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                       vector<unsigned short>& SU2ToCGNS) {
   /* The BAR_5 element is a quartic element. SU2 numbers to nodes with
      increasing parametric value, while in CGNS the internal nodes are
      numbered last. */
   VTK_Type = LINE;
-  nPoly    = 4;
-  nDOFs    = 5;
+  nPoly = 4;
+  nDOFs = 5;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0] = 0; SU2ToCGNS[1] = 2; SU2ToCGNS[2] = 3;
-  SU2ToCGNS[3] = 4; SU2ToCGNS[4] = 1;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 2;
+  SU2ToCGNS[2] = 3;
+  SU2ToCGNS[3] = 4;
+  SU2ToCGNS[4] = 1;
 }
 
-void CCGNSElementType::CreateDataTRI_3(unsigned short         &VTK_Type,
-                                       unsigned short         &nPoly,
-                                       unsigned short         &nDOFs,
-                                       vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataTRI_3(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                       vector<unsigned short>& SU2ToCGNS) {
   /* The TRI_3 element is a linear triangle. The node numbering is the same
      in SU2 and CGNS. */
   VTK_Type = TRIANGLE;
-  nPoly    = 1;
-  nDOFs    = 3;
+  nPoly = 1;
+  nDOFs = 3;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0] = 0; SU2ToCGNS[1] = 1; SU2ToCGNS[2] = 2;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 1;
+  SU2ToCGNS[2] = 2;
 }
 
-void CCGNSElementType::CreateDataTRI_6(unsigned short         &VTK_Type,
-                                       unsigned short         &nPoly,
-                                       unsigned short         &nDOFs,
-                                       vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataTRI_6(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                       vector<unsigned short>& SU2ToCGNS) {
   /* The TRI_6 element is a quadratic triangle. In CGNS the nodes are numbered
      as follows: - First the vertex nodes.
                  - Second the edge nodes.
@@ -520,19 +565,20 @@ void CCGNSElementType::CreateDataTRI_6(unsigned short         &VTK_Type,
      where the i-direction is defined from node 0 to 1 and the j-direction
      from node 0 along the other edge. */
   VTK_Type = TRIANGLE;
-  nPoly    = 2;
-  nDOFs    = 6;
+  nPoly = 2;
+  nDOFs = 6;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0] = 0; SU2ToCGNS[1] = 3; SU2ToCGNS[2] = 1;
-  SU2ToCGNS[3] = 5; SU2ToCGNS[4] = 4; SU2ToCGNS[5] = 2;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 3;
+  SU2ToCGNS[2] = 1;
+  SU2ToCGNS[3] = 5;
+  SU2ToCGNS[4] = 4;
+  SU2ToCGNS[5] = 2;
 }
 
-void CCGNSElementType::CreateDataTRI_10(unsigned short         &VTK_Type,
-                                        unsigned short         &nPoly,
-                                        unsigned short         &nDOFs,
-                                        vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataTRI_10(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                        vector<unsigned short>& SU2ToCGNS) {
   /* The TRI_10 element is a cubic triangle. In CGNS the nodes are numbered
      as follows: - First the vertex nodes.
                  - Second the edge nodes.
@@ -541,20 +587,24 @@ void CCGNSElementType::CreateDataTRI_10(unsigned short         &VTK_Type,
      where the i-direction is defined from node 0 to 1 and the j-direction
      from node 0 along the other edge. */
   VTK_Type = TRIANGLE;
-  nPoly    =  3;
-  nDOFs    = 10;
+  nPoly = 3;
+  nDOFs = 10;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0] = 0; SU2ToCGNS[1] = 3; SU2ToCGNS[2] = 4; SU2ToCGNS[3] = 1;
-  SU2ToCGNS[4] = 8; SU2ToCGNS[5] = 9; SU2ToCGNS[6] = 5; SU2ToCGNS[7] = 7;
-  SU2ToCGNS[8] = 6; SU2ToCGNS[9] = 2;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 3;
+  SU2ToCGNS[2] = 4;
+  SU2ToCGNS[3] = 1;
+  SU2ToCGNS[4] = 8;
+  SU2ToCGNS[5] = 9;
+  SU2ToCGNS[6] = 5;
+  SU2ToCGNS[7] = 7;
+  SU2ToCGNS[8] = 6;
+  SU2ToCGNS[9] = 2;
 }
 
-void CCGNSElementType::CreateDataTRI_15(unsigned short         &VTK_Type,
-                                        unsigned short         &nPoly,
-                                        unsigned short         &nDOFs,
-                                        vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataTRI_15(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                        vector<unsigned short>& SU2ToCGNS) {
   /* The TRI_15 element is a quartic triangle. In CGNS the nodes are numbered
      as follows: - First the vertex nodes.
                  - Second the edge nodes.
@@ -566,21 +616,29 @@ void CCGNSElementType::CreateDataTRI_15(unsigned short         &VTK_Type,
      the location for uniform spacing. This effect is currently ignored,
      i.e. it is assumed that the spacing in parameter space is uniform. */
   VTK_Type = TRIANGLE;
-  nPoly    =  4;
-  nDOFs    = 15;
+  nPoly = 4;
+  nDOFs = 15;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0]  = 0; SU2ToCGNS[1]  =  3; SU2ToCGNS[2]  =  4; SU2ToCGNS[3]  =  5;
-  SU2ToCGNS[4]  = 1; SU2ToCGNS[5]  = 11; SU2ToCGNS[6]  = 12; SU2ToCGNS[7]  = 13;
-  SU2ToCGNS[8]  = 6; SU2ToCGNS[9]  = 10; SU2ToCGNS[10] = 14; SU2ToCGNS[11] =  7;
-  SU2ToCGNS[12] = 9; SU2ToCGNS[13] =  8; SU2ToCGNS[14] =  2;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 3;
+  SU2ToCGNS[2] = 4;
+  SU2ToCGNS[3] = 5;
+  SU2ToCGNS[4] = 1;
+  SU2ToCGNS[5] = 11;
+  SU2ToCGNS[6] = 12;
+  SU2ToCGNS[7] = 13;
+  SU2ToCGNS[8] = 6;
+  SU2ToCGNS[9] = 10;
+  SU2ToCGNS[10] = 14;
+  SU2ToCGNS[11] = 7;
+  SU2ToCGNS[12] = 9;
+  SU2ToCGNS[13] = 8;
+  SU2ToCGNS[14] = 2;
 }
 
-void CCGNSElementType::CreateDataQUAD_4(unsigned short         &VTK_Type,
-                                        unsigned short         &nPoly,
-                                        unsigned short         &nDOFs,
-                                        vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataQUAD_4(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                        vector<unsigned short>& SU2ToCGNS) {
   /* The QUAD_4 element is a linear quadrilateral. In CGNS the nodes are
      numbered as follows: - First the vertex nodes.
                           - Second the edge nodes (not present for QUAD_4).
@@ -589,18 +647,18 @@ void CCGNSElementType::CreateDataQUAD_4(unsigned short         &VTK_Type,
      where the i-direction is defined from node 0 to 1 and the j-direction
      from node 0 along the other edge. */
   VTK_Type = QUADRILATERAL;
-  nPoly    = 1;
-  nDOFs    = 4;
+  nPoly = 1;
+  nDOFs = 4;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0] = 0; SU2ToCGNS[1] = 1; SU2ToCGNS[2] = 3; SU2ToCGNS[3] = 2;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 1;
+  SU2ToCGNS[2] = 3;
+  SU2ToCGNS[3] = 2;
 }
 
-void CCGNSElementType::CreateDataQUAD_9(unsigned short         &VTK_Type,
-                                        unsigned short         &nPoly,
-                                        unsigned short         &nDOFs,
-                                        vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataQUAD_9(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                        vector<unsigned short>& SU2ToCGNS) {
   /* The QUAD_9 element is a quadratic quadrilateral. In CGNS the nodes are
      numbered as follows: - First the vertex nodes.
                           - Second the edge nodes.
@@ -609,20 +667,23 @@ void CCGNSElementType::CreateDataQUAD_9(unsigned short         &VTK_Type,
      where the i-direction is defined from node 0 to 1 and the j-direction
      from node 0 along the other edge. */
   VTK_Type = QUADRILATERAL;
-  nPoly    = 2;
-  nDOFs    = 9;
+  nPoly = 2;
+  nDOFs = 9;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0] = 0; SU2ToCGNS[1] = 4; SU2ToCGNS[2] = 1; SU2ToCGNS[3] = 7;
-  SU2ToCGNS[4] = 8; SU2ToCGNS[5] = 5; SU2ToCGNS[6] = 3; SU2ToCGNS[7] = 6;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 4;
+  SU2ToCGNS[2] = 1;
+  SU2ToCGNS[3] = 7;
+  SU2ToCGNS[4] = 8;
+  SU2ToCGNS[5] = 5;
+  SU2ToCGNS[6] = 3;
+  SU2ToCGNS[7] = 6;
   SU2ToCGNS[8] = 2;
 }
 
-void CCGNSElementType::CreateDataQUAD_16(unsigned short         &VTK_Type,
-                                         unsigned short         &nPoly,
-                                         unsigned short         &nDOFs,
-                                         vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataQUAD_16(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                         vector<unsigned short>& SU2ToCGNS) {
   /* The QUAD_16 element is a cubic quadrilateral. In CGNS the nodes are
      numbered as follows: - First the vertex nodes.
                           - Second the edge nodes.
@@ -631,21 +692,30 @@ void CCGNSElementType::CreateDataQUAD_16(unsigned short         &VTK_Type,
      where the i-direction is defined from node 0 to 1 and the j-direction
      from node 0 along the other edge. */
   VTK_Type = QUADRILATERAL;
-  nPoly    =  3;
-  nDOFs    = 16;
+  nPoly = 3;
+  nDOFs = 16;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0]  =  0; SU2ToCGNS[1]  =  4; SU2ToCGNS[2]  =  5; SU2ToCGNS[3]  = 1;
-  SU2ToCGNS[4]  = 11; SU2ToCGNS[5]  = 12; SU2ToCGNS[6]  = 13; SU2ToCGNS[7]  = 6;
-  SU2ToCGNS[8]  = 10; SU2ToCGNS[9]  = 15; SU2ToCGNS[10] = 14; SU2ToCGNS[11] = 7;
-  SU2ToCGNS[12] =  3; SU2ToCGNS[13] =  9; SU2ToCGNS[14] =  8; SU2ToCGNS[15] = 2;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 4;
+  SU2ToCGNS[2] = 5;
+  SU2ToCGNS[3] = 1;
+  SU2ToCGNS[4] = 11;
+  SU2ToCGNS[5] = 12;
+  SU2ToCGNS[6] = 13;
+  SU2ToCGNS[7] = 6;
+  SU2ToCGNS[8] = 10;
+  SU2ToCGNS[9] = 15;
+  SU2ToCGNS[10] = 14;
+  SU2ToCGNS[11] = 7;
+  SU2ToCGNS[12] = 3;
+  SU2ToCGNS[13] = 9;
+  SU2ToCGNS[14] = 8;
+  SU2ToCGNS[15] = 2;
 }
 
-void CCGNSElementType::CreateDataQUAD_25(unsigned short         &VTK_Type,
-                                         unsigned short         &nPoly,
-                                         unsigned short         &nDOFs,
-                                         vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataQUAD_25(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                         vector<unsigned short>& SU2ToCGNS) {
   /* The QUAD_25 element is a quartic quadrilateral. In CGNS the nodes are
      numbered as follows: - First the vertex nodes.
                           - Second the edge nodes.
@@ -654,39 +724,54 @@ void CCGNSElementType::CreateDataQUAD_25(unsigned short         &VTK_Type,
      where the i-direction is defined from node 0 to 1 and the j-direction
      from node 0 along the other edge. */
   VTK_Type = QUADRILATERAL;
-  nPoly    =  4;
-  nDOFs    = 25;
+  nPoly = 4;
+  nDOFs = 25;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0]  =  0; SU2ToCGNS[1]  =  4; SU2ToCGNS[2]  =  5; SU2ToCGNS[3]  =  6;
-  SU2ToCGNS[4]  =  1; SU2ToCGNS[5]  = 15; SU2ToCGNS[6]  = 16; SU2ToCGNS[7]  = 17;
-  SU2ToCGNS[8]  = 18; SU2ToCGNS[9]  =  7; SU2ToCGNS[10] = 14; SU2ToCGNS[11] = 23;
-  SU2ToCGNS[12] = 24; SU2ToCGNS[13] = 19; SU2ToCGNS[14] =  8; SU2ToCGNS[15] = 13;
-  SU2ToCGNS[16] = 22; SU2ToCGNS[17] = 21; SU2ToCGNS[18] = 20; SU2ToCGNS[19] =  9;
-  SU2ToCGNS[20] =  3; SU2ToCGNS[21] = 12; SU2ToCGNS[22] = 11; SU2ToCGNS[23] = 10;
-  SU2ToCGNS[24] =  2;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 4;
+  SU2ToCGNS[2] = 5;
+  SU2ToCGNS[3] = 6;
+  SU2ToCGNS[4] = 1;
+  SU2ToCGNS[5] = 15;
+  SU2ToCGNS[6] = 16;
+  SU2ToCGNS[7] = 17;
+  SU2ToCGNS[8] = 18;
+  SU2ToCGNS[9] = 7;
+  SU2ToCGNS[10] = 14;
+  SU2ToCGNS[11] = 23;
+  SU2ToCGNS[12] = 24;
+  SU2ToCGNS[13] = 19;
+  SU2ToCGNS[14] = 8;
+  SU2ToCGNS[15] = 13;
+  SU2ToCGNS[16] = 22;
+  SU2ToCGNS[17] = 21;
+  SU2ToCGNS[18] = 20;
+  SU2ToCGNS[19] = 9;
+  SU2ToCGNS[20] = 3;
+  SU2ToCGNS[21] = 12;
+  SU2ToCGNS[22] = 11;
+  SU2ToCGNS[23] = 10;
+  SU2ToCGNS[24] = 2;
 }
 
-void CCGNSElementType::CreateDataTETRA_4(unsigned short         &VTK_Type,
-                                         unsigned short         &nPoly,
-                                         unsigned short         &nDOFs,
-                                         vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataTETRA_4(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                         vector<unsigned short>& SU2ToCGNS) {
   /* The TETRA_4 element is a linear tetrahedron. The node numbering is
      the same in SU2 and CGNS. */
   VTK_Type = TETRAHEDRON;
-  nPoly    = 1;
-  nDOFs    = 4;
+  nPoly = 1;
+  nDOFs = 4;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0] = 0; SU2ToCGNS[1] = 1; SU2ToCGNS[2] = 2; SU2ToCGNS[3] = 3;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 1;
+  SU2ToCGNS[2] = 2;
+  SU2ToCGNS[3] = 3;
 }
 
-void CCGNSElementType::CreateDataTETRA_10(unsigned short         &VTK_Type,
-                                          unsigned short         &nPoly,
-                                          unsigned short         &nDOFs,
-                                          vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataTETRA_10(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                          vector<unsigned short>& SU2ToCGNS) {
   /* The TETRA_10 element is a quadratic tetrahedron. In CGNS the nodes are
      numbered as follows: - First the vertex nodes.
                           - Second the edge nodes.
@@ -697,20 +782,24 @@ void CCGNSElementType::CreateDataTETRA_10(unsigned short         &VTK_Type,
      from node 0 along the second edge and the k-direction from node 0 along
      the third edge. */
   VTK_Type = TETRAHEDRON;
-  nPoly    =  2;
-  nDOFs    = 10;
+  nPoly = 2;
+  nDOFs = 10;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0] = 0; SU2ToCGNS[1] = 4; SU2ToCGNS[2] = 1; SU2ToCGNS[3] = 6;
-  SU2ToCGNS[4] = 5; SU2ToCGNS[5] = 2; SU2ToCGNS[6] = 7; SU2ToCGNS[7] = 8;
-  SU2ToCGNS[8] = 9; SU2ToCGNS[9] = 3;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 4;
+  SU2ToCGNS[2] = 1;
+  SU2ToCGNS[3] = 6;
+  SU2ToCGNS[4] = 5;
+  SU2ToCGNS[5] = 2;
+  SU2ToCGNS[6] = 7;
+  SU2ToCGNS[7] = 8;
+  SU2ToCGNS[8] = 9;
+  SU2ToCGNS[9] = 3;
 }
 
-void CCGNSElementType::CreateDataTETRA_20(unsigned short         &VTK_Type,
-                                          unsigned short         &nPoly,
-                                          unsigned short         &nDOFs,
-                                          vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataTETRA_20(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                          vector<unsigned short>& SU2ToCGNS) {
   /* The TETRA_20 element is a cubic tetrahedron. In CGNS the nodes are
      numbered as follows: - First the vertex nodes.
                           - Second the edge nodes.
@@ -721,22 +810,34 @@ void CCGNSElementType::CreateDataTETRA_20(unsigned short         &VTK_Type,
      from node 0 along the second edge and the k-direction from node 0 along
      the third edge. */
   VTK_Type = TETRAHEDRON;
-  nPoly    =  3;
-  nDOFs    = 20;
+  nPoly = 3;
+  nDOFs = 20;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0]  =  0; SU2ToCGNS[1]  =  4; SU2ToCGNS[2]  =  5; SU2ToCGNS[3]  =  1;
-  SU2ToCGNS[4]  =  9; SU2ToCGNS[5]  = 16; SU2ToCGNS[6]  =  6; SU2ToCGNS[7]  =  8;
-  SU2ToCGNS[8]  =  7; SU2ToCGNS[9]  =  2; SU2ToCGNS[10] = 10; SU2ToCGNS[11] = 17;
-  SU2ToCGNS[12] = 12; SU2ToCGNS[13] = 19; SU2ToCGNS[14] = 18; SU2ToCGNS[15] = 14;
-  SU2ToCGNS[16] = 11; SU2ToCGNS[17] = 13; SU2ToCGNS[18] = 15; SU2ToCGNS[19] =  3;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 4;
+  SU2ToCGNS[2] = 5;
+  SU2ToCGNS[3] = 1;
+  SU2ToCGNS[4] = 9;
+  SU2ToCGNS[5] = 16;
+  SU2ToCGNS[6] = 6;
+  SU2ToCGNS[7] = 8;
+  SU2ToCGNS[8] = 7;
+  SU2ToCGNS[9] = 2;
+  SU2ToCGNS[10] = 10;
+  SU2ToCGNS[11] = 17;
+  SU2ToCGNS[12] = 12;
+  SU2ToCGNS[13] = 19;
+  SU2ToCGNS[14] = 18;
+  SU2ToCGNS[15] = 14;
+  SU2ToCGNS[16] = 11;
+  SU2ToCGNS[17] = 13;
+  SU2ToCGNS[18] = 15;
+  SU2ToCGNS[19] = 3;
 }
 
-void CCGNSElementType::CreateDataTETRA_35(unsigned short         &VTK_Type,
-                                          unsigned short         &nPoly,
-                                          unsigned short         &nDOFs,
-                                          vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataTETRA_35(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                          vector<unsigned short>& SU2ToCGNS) {
   /* The TETRA_35 element is a quartic tetrahedron. In CGNS the nodes are
      numbered as follows: - First the vertex nodes.
                           - Second the edge nodes.
@@ -750,26 +851,49 @@ void CCGNSElementType::CreateDataTETRA_35(unsigned short         &VTK_Type,
      currently ignored, i.e. it is assumed that the spacing in parameter space
      is uniform. */
   VTK_Type = TETRAHEDRON;
-  nPoly    =  4;
-  nDOFs    = 35;
+  nPoly = 4;
+  nDOFs = 35;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0]  =  0; SU2ToCGNS[1]  =  4; SU2ToCGNS[2]  =  5; SU2ToCGNS[3]  =  6;
-  SU2ToCGNS[4]  =  1; SU2ToCGNS[5]  = 12; SU2ToCGNS[6]  = 22; SU2ToCGNS[7]  = 23;
-  SU2ToCGNS[8]  =  7; SU2ToCGNS[9]  = 11; SU2ToCGNS[10] = 24; SU2ToCGNS[11] =  8;
-  SU2ToCGNS[12] = 10; SU2ToCGNS[13] =  9; SU2ToCGNS[14] =  2; SU2ToCGNS[15] = 13;
-  SU2ToCGNS[16] = 25; SU2ToCGNS[17] = 26; SU2ToCGNS[18] = 16; SU2ToCGNS[19] = 32;
-  SU2ToCGNS[20] = 34; SU2ToCGNS[21] = 28; SU2ToCGNS[22] = 31; SU2ToCGNS[23] = 29;
-  SU2ToCGNS[24] = 19; SU2ToCGNS[25] = 14; SU2ToCGNS[26] = 27; SU2ToCGNS[27] = 17;
-  SU2ToCGNS[28] = 33; SU2ToCGNS[29] = 30; SU2ToCGNS[30] = 20; SU2ToCGNS[31] = 15;
-  SU2ToCGNS[32] = 18; SU2ToCGNS[33] = 21; SU2ToCGNS[34] =  3;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 4;
+  SU2ToCGNS[2] = 5;
+  SU2ToCGNS[3] = 6;
+  SU2ToCGNS[4] = 1;
+  SU2ToCGNS[5] = 12;
+  SU2ToCGNS[6] = 22;
+  SU2ToCGNS[7] = 23;
+  SU2ToCGNS[8] = 7;
+  SU2ToCGNS[9] = 11;
+  SU2ToCGNS[10] = 24;
+  SU2ToCGNS[11] = 8;
+  SU2ToCGNS[12] = 10;
+  SU2ToCGNS[13] = 9;
+  SU2ToCGNS[14] = 2;
+  SU2ToCGNS[15] = 13;
+  SU2ToCGNS[16] = 25;
+  SU2ToCGNS[17] = 26;
+  SU2ToCGNS[18] = 16;
+  SU2ToCGNS[19] = 32;
+  SU2ToCGNS[20] = 34;
+  SU2ToCGNS[21] = 28;
+  SU2ToCGNS[22] = 31;
+  SU2ToCGNS[23] = 29;
+  SU2ToCGNS[24] = 19;
+  SU2ToCGNS[25] = 14;
+  SU2ToCGNS[26] = 27;
+  SU2ToCGNS[27] = 17;
+  SU2ToCGNS[28] = 33;
+  SU2ToCGNS[29] = 30;
+  SU2ToCGNS[30] = 20;
+  SU2ToCGNS[31] = 15;
+  SU2ToCGNS[32] = 18;
+  SU2ToCGNS[33] = 21;
+  SU2ToCGNS[34] = 3;
 }
 
-void CCGNSElementType::CreateDataPYRA_5(unsigned short         &VTK_Type,
-                                        unsigned short         &nPoly,
-                                        unsigned short         &nDOFs,
-                                        vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataPYRA_5(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                        vector<unsigned short>& SU2ToCGNS) {
   /* The PYRA_5 element is a linear pyramid. In CGNS the nodes are
      numbered as follows: - First the vertex nodes.
                           - Second the edge nodes (not present in PYRA_5).
@@ -780,19 +904,19 @@ void CCGNSElementType::CreateDataPYRA_5(unsigned short         &VTK_Type,
      from node 0 along the second edge and the k-direction from node 0 along
      the third edge. */
   VTK_Type = PYRAMID;
-  nPoly    = 1;
-  nDOFs    = 5;
+  nPoly = 1;
+  nDOFs = 5;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0] = 0; SU2ToCGNS[1] = 1; SU2ToCGNS[2] = 3; SU2ToCGNS[3] = 2;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 1;
+  SU2ToCGNS[2] = 3;
+  SU2ToCGNS[3] = 2;
   SU2ToCGNS[4] = 4;
 }
 
-void CCGNSElementType::CreateDataPYRA_14(unsigned short         &VTK_Type,
-                                         unsigned short         &nPoly,
-                                         unsigned short         &nDOFs,
-                                         vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataPYRA_14(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                         vector<unsigned short>& SU2ToCGNS) {
   /* The PYRA_14 element is a quadratic pyramid. In CGNS the nodes are
      numbered as follows: - First the vertex nodes.
                           - Second the edge nodes.
@@ -803,21 +927,28 @@ void CCGNSElementType::CreateDataPYRA_14(unsigned short         &VTK_Type,
      from node 0 along the second edge and the k-direction from node 0 along
      the third edge. */
   VTK_Type = PYRAMID;
-  nPoly    =  2;
-  nDOFs    = 14;
+  nPoly = 2;
+  nDOFs = 14;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0]  =  0; SU2ToCGNS[1]  = 5; SU2ToCGNS[2]  =  1; SU2ToCGNS[3]  =  8;
-  SU2ToCGNS[4]  = 13; SU2ToCGNS[5]  = 6; SU2ToCGNS[6]  =  3; SU2ToCGNS[7]  =  7;
-  SU2ToCGNS[8]  =  2; SU2ToCGNS[9]  = 9; SU2ToCGNS[10] = 10; SU2ToCGNS[11] = 12;
-  SU2ToCGNS[12] = 11; SU2ToCGNS[13] = 4;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 5;
+  SU2ToCGNS[2] = 1;
+  SU2ToCGNS[3] = 8;
+  SU2ToCGNS[4] = 13;
+  SU2ToCGNS[5] = 6;
+  SU2ToCGNS[6] = 3;
+  SU2ToCGNS[7] = 7;
+  SU2ToCGNS[8] = 2;
+  SU2ToCGNS[9] = 9;
+  SU2ToCGNS[10] = 10;
+  SU2ToCGNS[11] = 12;
+  SU2ToCGNS[12] = 11;
+  SU2ToCGNS[13] = 4;
 }
 
-void CCGNSElementType::CreateDataPYRA_30(unsigned short         &VTK_Type,
-                                         unsigned short         &nPoly,
-                                         unsigned short         &nDOFs,
-                                         vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataPYRA_30(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                         vector<unsigned short>& SU2ToCGNS) {
   /* The PYRA_30 element is a cubic pyramid. In CGNS the nodes are
      numbered as follows: - First the vertex nodes.
                           - Second the edge nodes.
@@ -828,25 +959,44 @@ void CCGNSElementType::CreateDataPYRA_30(unsigned short         &VTK_Type,
      from node 0 along the second edge and the k-direction from node 0 along
      the third edge. */
   VTK_Type = PYRAMID;
-  nPoly    =  3;
-  nDOFs    = 30;
+  nPoly = 3;
+  nDOFs = 30;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0]  =  0; SU2ToCGNS[1]  =  5; SU2ToCGNS[2]  =  6; SU2ToCGNS[3]  =  1;
-  SU2ToCGNS[4]  = 12; SU2ToCGNS[5]  = 21; SU2ToCGNS[6]  = 22; SU2ToCGNS[7]  =  7;
-  SU2ToCGNS[8]  = 11; SU2ToCGNS[9]  = 24; SU2ToCGNS[10] = 23; SU2ToCGNS[11] =  8;
-  SU2ToCGNS[12] =  3; SU2ToCGNS[13] = 20; SU2ToCGNS[14] =  9; SU2ToCGNS[15] =  3;
-  SU2ToCGNS[16] = 13; SU2ToCGNS[17] = 25; SU2ToCGNS[18] = 15; SU2ToCGNS[19] = 28;
-  SU2ToCGNS[20] = 29; SU2ToCGNS[21] = 26; SU2ToCGNS[22] = 19; SU2ToCGNS[23] = 27;
-  SU2ToCGNS[24] = 17; SU2ToCGNS[25] = 14; SU2ToCGNS[26] = 16; SU2ToCGNS[27] = 20;
-  SU2ToCGNS[28] = 18; SU2ToCGNS[29] =  4;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 5;
+  SU2ToCGNS[2] = 6;
+  SU2ToCGNS[3] = 1;
+  SU2ToCGNS[4] = 12;
+  SU2ToCGNS[5] = 21;
+  SU2ToCGNS[6] = 22;
+  SU2ToCGNS[7] = 7;
+  SU2ToCGNS[8] = 11;
+  SU2ToCGNS[9] = 24;
+  SU2ToCGNS[10] = 23;
+  SU2ToCGNS[11] = 8;
+  SU2ToCGNS[12] = 3;
+  SU2ToCGNS[13] = 20;
+  SU2ToCGNS[14] = 9;
+  SU2ToCGNS[15] = 3;
+  SU2ToCGNS[16] = 13;
+  SU2ToCGNS[17] = 25;
+  SU2ToCGNS[18] = 15;
+  SU2ToCGNS[19] = 28;
+  SU2ToCGNS[20] = 29;
+  SU2ToCGNS[21] = 26;
+  SU2ToCGNS[22] = 19;
+  SU2ToCGNS[23] = 27;
+  SU2ToCGNS[24] = 17;
+  SU2ToCGNS[25] = 14;
+  SU2ToCGNS[26] = 16;
+  SU2ToCGNS[27] = 20;
+  SU2ToCGNS[28] = 18;
+  SU2ToCGNS[29] = 4;
 }
 
-void CCGNSElementType::CreateDataPYRA_55(unsigned short         &VTK_Type,
-                                         unsigned short         &nPoly,
-                                         unsigned short         &nDOFs,
-                                         vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataPYRA_55(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                         vector<unsigned short>& SU2ToCGNS) {
   /* The PYRA_55 element is a quartic pyramid. In CGNS the nodes are
      numbered as follows: - First the vertex nodes.
                           - Second the edge nodes.
@@ -860,47 +1010,86 @@ void CCGNSElementType::CreateDataPYRA_55(unsigned short         &VTK_Type,
      effect is currently ignored, i.e. it is assumed that the spacing in
      parameter space is uniform.*/
   VTK_Type = PYRAMID;
-  nPoly    =  4;
-  nDOFs    = 55;
+  nPoly = 4;
+  nDOFs = 55;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0]  =  0; SU2ToCGNS[1]  =  5; SU2ToCGNS[2]  =  6; SU2ToCGNS[3]  =  7;
-  SU2ToCGNS[4]  =  1; SU2ToCGNS[5]  = 16; SU2ToCGNS[6]  = 29; SU2ToCGNS[7]  = 30;
-  SU2ToCGNS[8]  = 31; SU2ToCGNS[9]  =  8; SU2ToCGNS[10] = 15; SU2ToCGNS[11] = 36;
-  SU2ToCGNS[12] = 37; SU2ToCGNS[13] = 32; SU2ToCGNS[14] =  9; SU2ToCGNS[15] = 14;
-  SU2ToCGNS[16] = 35; SU2ToCGNS[17] = 34; SU2ToCGNS[18] = 33; SU2ToCGNS[19] = 10;
-  SU2ToCGNS[20] =  3; SU2ToCGNS[21] = 13; SU2ToCGNS[22] = 12; SU2ToCGNS[23] = 11;
-  SU2ToCGNS[24] =  2; SU2ToCGNS[25] = 17; SU2ToCGNS[26] = 38; SU2ToCGNS[27] = 39;
-  SU2ToCGNS[28] = 20; SU2ToCGNS[29] = 48; SU2ToCGNS[30] = 50; SU2ToCGNS[31] = 51;
-  SU2ToCGNS[32] = 41; SU2ToCGNS[33] = 47; SU2ToCGNS[34] = 53; SU2ToCGNS[35] = 52;
-  SU2ToCGNS[36] = 42; SU2ToCGNS[37] = 26; SU2ToCGNS[38] = 45; SU2ToCGNS[39] = 44;
-  SU2ToCGNS[40] = 23; SU2ToCGNS[41] = 18; SU2ToCGNS[42] = 40; SU2ToCGNS[43] = 21;
-  SU2ToCGNS[44] = 49; SU2ToCGNS[45] = 54; SU2ToCGNS[46] = 43; SU2ToCGNS[47] = 27;
-  SU2ToCGNS[48] = 46; SU2ToCGNS[49] = 24; SU2ToCGNS[50] = 19; SU2ToCGNS[51] = 22;
-  SU2ToCGNS[52] = 28; SU2ToCGNS[53] = 25; SU2ToCGNS[54] =  4;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 5;
+  SU2ToCGNS[2] = 6;
+  SU2ToCGNS[3] = 7;
+  SU2ToCGNS[4] = 1;
+  SU2ToCGNS[5] = 16;
+  SU2ToCGNS[6] = 29;
+  SU2ToCGNS[7] = 30;
+  SU2ToCGNS[8] = 31;
+  SU2ToCGNS[9] = 8;
+  SU2ToCGNS[10] = 15;
+  SU2ToCGNS[11] = 36;
+  SU2ToCGNS[12] = 37;
+  SU2ToCGNS[13] = 32;
+  SU2ToCGNS[14] = 9;
+  SU2ToCGNS[15] = 14;
+  SU2ToCGNS[16] = 35;
+  SU2ToCGNS[17] = 34;
+  SU2ToCGNS[18] = 33;
+  SU2ToCGNS[19] = 10;
+  SU2ToCGNS[20] = 3;
+  SU2ToCGNS[21] = 13;
+  SU2ToCGNS[22] = 12;
+  SU2ToCGNS[23] = 11;
+  SU2ToCGNS[24] = 2;
+  SU2ToCGNS[25] = 17;
+  SU2ToCGNS[26] = 38;
+  SU2ToCGNS[27] = 39;
+  SU2ToCGNS[28] = 20;
+  SU2ToCGNS[29] = 48;
+  SU2ToCGNS[30] = 50;
+  SU2ToCGNS[31] = 51;
+  SU2ToCGNS[32] = 41;
+  SU2ToCGNS[33] = 47;
+  SU2ToCGNS[34] = 53;
+  SU2ToCGNS[35] = 52;
+  SU2ToCGNS[36] = 42;
+  SU2ToCGNS[37] = 26;
+  SU2ToCGNS[38] = 45;
+  SU2ToCGNS[39] = 44;
+  SU2ToCGNS[40] = 23;
+  SU2ToCGNS[41] = 18;
+  SU2ToCGNS[42] = 40;
+  SU2ToCGNS[43] = 21;
+  SU2ToCGNS[44] = 49;
+  SU2ToCGNS[45] = 54;
+  SU2ToCGNS[46] = 43;
+  SU2ToCGNS[47] = 27;
+  SU2ToCGNS[48] = 46;
+  SU2ToCGNS[49] = 24;
+  SU2ToCGNS[50] = 19;
+  SU2ToCGNS[51] = 22;
+  SU2ToCGNS[52] = 28;
+  SU2ToCGNS[53] = 25;
+  SU2ToCGNS[54] = 4;
 }
 
-void CCGNSElementType::CreateDataPENTA_6(unsigned short         &VTK_Type,
-                                         unsigned short         &nPoly,
-                                         unsigned short         &nDOFs,
-                                         vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataPENTA_6(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                         vector<unsigned short>& SU2ToCGNS) {
   /* The PENTA_6 element is a linear prism. The node numbering is
      the same in SU2 and CGNS. */
   VTK_Type = PRISM;
-  nPoly    = 1;
-  nDOFs    = 6;
+  nPoly = 1;
+  nDOFs = 6;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0] = 0; SU2ToCGNS[1] = 1; SU2ToCGNS[2] = 2;
-  SU2ToCGNS[3] = 3; SU2ToCGNS[4] = 4; SU2ToCGNS[5] = 5;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 1;
+  SU2ToCGNS[2] = 2;
+  SU2ToCGNS[3] = 3;
+  SU2ToCGNS[4] = 4;
+  SU2ToCGNS[5] = 5;
 }
 
-void CCGNSElementType::CreateDataPENTA_18(unsigned short         &VTK_Type,
-                                          unsigned short         &nPoly,
-                                          unsigned short         &nDOFs,
-                                          vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataPENTA_18(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                          vector<unsigned short>& SU2ToCGNS) {
   /* The PENTA_18 element is a quadratic prism. In CGNS the nodes are
      numbered as follows: - First the vertex nodes.
                           - Second the edge nodes.
@@ -911,22 +1100,32 @@ void CCGNSElementType::CreateDataPENTA_18(unsigned short         &VTK_Type,
      from node 0 along the second edge and the k-direction from node 0 along
      the third edge. */
   VTK_Type = PRISM;
-  nPoly    =  2;
-  nDOFs    = 18;
+  nPoly = 2;
+  nDOFs = 18;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0]  =  0; SU2ToCGNS[1]  =  6; SU2ToCGNS[2]  =  1; SU2ToCGNS[3]  =  8;
-  SU2ToCGNS[4]  =  7; SU2ToCGNS[5]  =  2; SU2ToCGNS[6]  =  9; SU2ToCGNS[7]  = 15;
-  SU2ToCGNS[8]  = 10; SU2ToCGNS[9]  = 17; SU2ToCGNS[10] = 16; SU2ToCGNS[11] = 11;
-  SU2ToCGNS[12] =  3; SU2ToCGNS[13] = 12; SU2ToCGNS[14] =  4; SU2ToCGNS[15] = 14;
-  SU2ToCGNS[16] = 13; SU2ToCGNS[17] =  5;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 6;
+  SU2ToCGNS[2] = 1;
+  SU2ToCGNS[3] = 8;
+  SU2ToCGNS[4] = 7;
+  SU2ToCGNS[5] = 2;
+  SU2ToCGNS[6] = 9;
+  SU2ToCGNS[7] = 15;
+  SU2ToCGNS[8] = 10;
+  SU2ToCGNS[9] = 17;
+  SU2ToCGNS[10] = 16;
+  SU2ToCGNS[11] = 11;
+  SU2ToCGNS[12] = 3;
+  SU2ToCGNS[13] = 12;
+  SU2ToCGNS[14] = 4;
+  SU2ToCGNS[15] = 14;
+  SU2ToCGNS[16] = 13;
+  SU2ToCGNS[17] = 5;
 }
 
-void CCGNSElementType::CreateDataPENTA_40(unsigned short         &VTK_Type,
-                                          unsigned short         &nPoly,
-                                          unsigned short         &nDOFs,
-                                          vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataPENTA_40(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                          vector<unsigned short>& SU2ToCGNS) {
   /* The PENTA_40 element is a cubic prism. In CGNS the nodes are
      numbered as follows: - First the vertex nodes.
                           - Second the edge nodes.
@@ -937,27 +1136,54 @@ void CCGNSElementType::CreateDataPENTA_40(unsigned short         &VTK_Type,
      from node 0 along the second edge and the k-direction from node 0 along
      the third edge. */
   VTK_Type = PRISM;
-  nPoly    =  3;
-  nDOFs    = 40;
+  nPoly = 3;
+  nDOFs = 40;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0]  =  0; SU2ToCGNS[1]  =  6; SU2ToCGNS[2]  =  7; SU2ToCGNS[3]  =  1;
-  SU2ToCGNS[4]  = 11; SU2ToCGNS[5]  = 24; SU2ToCGNS[6]  =  8; SU2ToCGNS[7]  = 10;
-  SU2ToCGNS[8]  =  9; SU2ToCGNS[9]  =  2; SU2ToCGNS[10] = 12; SU2ToCGNS[11] = 25;
-  SU2ToCGNS[12] = 26; SU2ToCGNS[13] = 14; SU2ToCGNS[14] = 34; SU2ToCGNS[15] = 38;
-  SU2ToCGNS[16] = 29; SU2ToCGNS[17] = 33; SU2ToCGNS[18] = 30; SU2ToCGNS[19] = 16;
-  SU2ToCGNS[20] = 13; SU2ToCGNS[21] = 28; SU2ToCGNS[22] = 27; SU2ToCGNS[23] = 15;
-  SU2ToCGNS[24] = 35; SU2ToCGNS[25] = 39; SU2ToCGNS[26] = 32; SU2ToCGNS[27] = 36;
-  SU2ToCGNS[28] = 31; SU2ToCGNS[29] = 17; SU2ToCGNS[30] =  3; SU2ToCGNS[31] = 18;
-  SU2ToCGNS[32] = 19; SU2ToCGNS[33] =  4; SU2ToCGNS[34] = 23; SU2ToCGNS[35] = 37;
-  SU2ToCGNS[36] = 20; SU2ToCGNS[37] = 22; SU2ToCGNS[38] = 21; SU2ToCGNS[39] =  5;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 6;
+  SU2ToCGNS[2] = 7;
+  SU2ToCGNS[3] = 1;
+  SU2ToCGNS[4] = 11;
+  SU2ToCGNS[5] = 24;
+  SU2ToCGNS[6] = 8;
+  SU2ToCGNS[7] = 10;
+  SU2ToCGNS[8] = 9;
+  SU2ToCGNS[9] = 2;
+  SU2ToCGNS[10] = 12;
+  SU2ToCGNS[11] = 25;
+  SU2ToCGNS[12] = 26;
+  SU2ToCGNS[13] = 14;
+  SU2ToCGNS[14] = 34;
+  SU2ToCGNS[15] = 38;
+  SU2ToCGNS[16] = 29;
+  SU2ToCGNS[17] = 33;
+  SU2ToCGNS[18] = 30;
+  SU2ToCGNS[19] = 16;
+  SU2ToCGNS[20] = 13;
+  SU2ToCGNS[21] = 28;
+  SU2ToCGNS[22] = 27;
+  SU2ToCGNS[23] = 15;
+  SU2ToCGNS[24] = 35;
+  SU2ToCGNS[25] = 39;
+  SU2ToCGNS[26] = 32;
+  SU2ToCGNS[27] = 36;
+  SU2ToCGNS[28] = 31;
+  SU2ToCGNS[29] = 17;
+  SU2ToCGNS[30] = 3;
+  SU2ToCGNS[31] = 18;
+  SU2ToCGNS[32] = 19;
+  SU2ToCGNS[33] = 4;
+  SU2ToCGNS[34] = 23;
+  SU2ToCGNS[35] = 37;
+  SU2ToCGNS[36] = 20;
+  SU2ToCGNS[37] = 22;
+  SU2ToCGNS[38] = 21;
+  SU2ToCGNS[39] = 5;
 }
 
-void CCGNSElementType::CreateDataPENTA_75(unsigned short         &VTK_Type,
-                                          unsigned short         &nPoly,
-                                          unsigned short         &nDOFs,
-                                          vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataPENTA_75(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                          vector<unsigned short>& SU2ToCGNS) {
   /* The PENTA_75 element is a quartic prism. In CGNS the nodes are
      numbered as follows: - First the vertex nodes.
                           - Second the edge nodes.
@@ -971,36 +1197,89 @@ void CCGNSElementType::CreateDataPENTA_75(unsigned short         &VTK_Type,
      effect is currently ignored, i.e. it is assumed that the spacing in
      parameter space is uniform. */
   VTK_Type = PRISM;
-  nPoly    =  4;
-  nDOFs    = 75;
+  nPoly = 4;
+  nDOFs = 75;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0]  =  0; SU2ToCGNS[1]  =  6; SU2ToCGNS[2]  =  7; SU2ToCGNS[3]  =  8;
-  SU2ToCGNS[4]  =  1; SU2ToCGNS[5]  = 14; SU2ToCGNS[6]  = 33; SU2ToCGNS[7]  = 34;
-  SU2ToCGNS[8]  =  9; SU2ToCGNS[9]  = 13; SU2ToCGNS[10] = 35; SU2ToCGNS[11] = 10;
-  SU2ToCGNS[12] = 12; SU2ToCGNS[13] = 11; SU2ToCGNS[14] =  2; SU2ToCGNS[15] = 15;
-  SU2ToCGNS[16] = 36; SU2ToCGNS[17] = 37; SU2ToCGNS[18] = 38; SU2ToCGNS[19] = 18;
-  SU2ToCGNS[20] = 56; SU2ToCGNS[21] = 66; SU2ToCGNS[22] = 67; SU2ToCGNS[23] = 45;
-  SU2ToCGNS[24] = 55; SU2ToCGNS[25] = 68; SU2ToCGNS[26] = 46; SU2ToCGNS[27] = 54;
-  SU2ToCGNS[28] = 47; SU2ToCGNS[29] = 21; SU2ToCGNS[30] = 16; SU2ToCGNS[31] = 43;
-  SU2ToCGNS[32] = 44; SU2ToCGNS[33] = 39; SU2ToCGNS[34] = 19; SU2ToCGNS[35] = 57;
-  SU2ToCGNS[36] = 69; SU2ToCGNS[37] = 70; SU2ToCGNS[38] = 52; SU2ToCGNS[39] = 62;
-  SU2ToCGNS[40] = 71; SU2ToCGNS[41] = 53; SU2ToCGNS[42] = 61; SU2ToCGNS[43] = 48;
-  SU2ToCGNS[44] = 22; SU2ToCGNS[45] = 17; SU2ToCGNS[46] = 42; SU2ToCGNS[47] = 41;
-  SU2ToCGNS[48] = 40; SU2ToCGNS[49] = 20; SU2ToCGNS[50] = 58; SU2ToCGNS[51] = 72;
-  SU2ToCGNS[52] = 73; SU2ToCGNS[53] = 51; SU2ToCGNS[54] = 59; SU2ToCGNS[55] = 74;
-  SU2ToCGNS[56] = 50; SU2ToCGNS[57] = 60; SU2ToCGNS[58] = 49; SU2ToCGNS[59] = 23;
-  SU2ToCGNS[60] =  3; SU2ToCGNS[61] = 24; SU2ToCGNS[62] = 25; SU2ToCGNS[63] = 26;
-  SU2ToCGNS[64] =  4; SU2ToCGNS[65] = 32; SU2ToCGNS[66] = 63; SU2ToCGNS[67] = 64;
-  SU2ToCGNS[68] = 27; SU2ToCGNS[69] = 31; SU2ToCGNS[70] = 65; SU2ToCGNS[71] = 28;
-  SU2ToCGNS[72] = 30; SU2ToCGNS[73] = 29; SU2ToCGNS[74] =  5;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 6;
+  SU2ToCGNS[2] = 7;
+  SU2ToCGNS[3] = 8;
+  SU2ToCGNS[4] = 1;
+  SU2ToCGNS[5] = 14;
+  SU2ToCGNS[6] = 33;
+  SU2ToCGNS[7] = 34;
+  SU2ToCGNS[8] = 9;
+  SU2ToCGNS[9] = 13;
+  SU2ToCGNS[10] = 35;
+  SU2ToCGNS[11] = 10;
+  SU2ToCGNS[12] = 12;
+  SU2ToCGNS[13] = 11;
+  SU2ToCGNS[14] = 2;
+  SU2ToCGNS[15] = 15;
+  SU2ToCGNS[16] = 36;
+  SU2ToCGNS[17] = 37;
+  SU2ToCGNS[18] = 38;
+  SU2ToCGNS[19] = 18;
+  SU2ToCGNS[20] = 56;
+  SU2ToCGNS[21] = 66;
+  SU2ToCGNS[22] = 67;
+  SU2ToCGNS[23] = 45;
+  SU2ToCGNS[24] = 55;
+  SU2ToCGNS[25] = 68;
+  SU2ToCGNS[26] = 46;
+  SU2ToCGNS[27] = 54;
+  SU2ToCGNS[28] = 47;
+  SU2ToCGNS[29] = 21;
+  SU2ToCGNS[30] = 16;
+  SU2ToCGNS[31] = 43;
+  SU2ToCGNS[32] = 44;
+  SU2ToCGNS[33] = 39;
+  SU2ToCGNS[34] = 19;
+  SU2ToCGNS[35] = 57;
+  SU2ToCGNS[36] = 69;
+  SU2ToCGNS[37] = 70;
+  SU2ToCGNS[38] = 52;
+  SU2ToCGNS[39] = 62;
+  SU2ToCGNS[40] = 71;
+  SU2ToCGNS[41] = 53;
+  SU2ToCGNS[42] = 61;
+  SU2ToCGNS[43] = 48;
+  SU2ToCGNS[44] = 22;
+  SU2ToCGNS[45] = 17;
+  SU2ToCGNS[46] = 42;
+  SU2ToCGNS[47] = 41;
+  SU2ToCGNS[48] = 40;
+  SU2ToCGNS[49] = 20;
+  SU2ToCGNS[50] = 58;
+  SU2ToCGNS[51] = 72;
+  SU2ToCGNS[52] = 73;
+  SU2ToCGNS[53] = 51;
+  SU2ToCGNS[54] = 59;
+  SU2ToCGNS[55] = 74;
+  SU2ToCGNS[56] = 50;
+  SU2ToCGNS[57] = 60;
+  SU2ToCGNS[58] = 49;
+  SU2ToCGNS[59] = 23;
+  SU2ToCGNS[60] = 3;
+  SU2ToCGNS[61] = 24;
+  SU2ToCGNS[62] = 25;
+  SU2ToCGNS[63] = 26;
+  SU2ToCGNS[64] = 4;
+  SU2ToCGNS[65] = 32;
+  SU2ToCGNS[66] = 63;
+  SU2ToCGNS[67] = 64;
+  SU2ToCGNS[68] = 27;
+  SU2ToCGNS[69] = 31;
+  SU2ToCGNS[70] = 65;
+  SU2ToCGNS[71] = 28;
+  SU2ToCGNS[72] = 30;
+  SU2ToCGNS[73] = 29;
+  SU2ToCGNS[74] = 5;
 }
 
-void CCGNSElementType::CreateDataHEXA_8(unsigned short         &VTK_Type,
-                                        unsigned short         &nPoly,
-                                        unsigned short         &nDOFs,
-                                        vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataHEXA_8(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                        vector<unsigned short>& SU2ToCGNS) {
   /* The HEXA_8 element is a linear hexahedron. In CGNS the nodes are
      numbered as follows: - First the vertex nodes.
                           - Second the edge nodes (not present in HEXA_8).
@@ -1011,19 +1290,22 @@ void CCGNSElementType::CreateDataHEXA_8(unsigned short         &VTK_Type,
      from node 0 along the second edge and the k-direction from node 0 along
      the third edge. */
   VTK_Type = HEXAHEDRON;
-  nPoly    = 1;
-  nDOFs    = 8;
+  nPoly = 1;
+  nDOFs = 8;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0] = 0; SU2ToCGNS[1] = 1; SU2ToCGNS[2] = 3; SU2ToCGNS[3] = 2;
-  SU2ToCGNS[4] = 4; SU2ToCGNS[5] = 5; SU2ToCGNS[6] = 7; SU2ToCGNS[7] = 6;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 1;
+  SU2ToCGNS[2] = 3;
+  SU2ToCGNS[3] = 2;
+  SU2ToCGNS[4] = 4;
+  SU2ToCGNS[5] = 5;
+  SU2ToCGNS[6] = 7;
+  SU2ToCGNS[7] = 6;
 }
 
-void CCGNSElementType::CreateDataHEXA_27(unsigned short         &VTK_Type,
-                                         unsigned short         &nPoly,
-                                         unsigned short         &nDOFs,
-                                         vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataHEXA_27(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                         vector<unsigned short>& SU2ToCGNS) {
   /* The HEXA_27 element is a quadratic hexahedron. In CGNS the nodes are
      numbered as follows: - First the vertex nodes.
                           - Second the edge nodes.
@@ -1034,24 +1316,41 @@ void CCGNSElementType::CreateDataHEXA_27(unsigned short         &VTK_Type,
      from node 0 along the second edge and the k-direction from node 0 along
      the third edge. */
   VTK_Type = HEXAHEDRON;
-  nPoly    =  2;
-  nDOFs    = 27;
+  nPoly = 2;
+  nDOFs = 27;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0]  =  0; SU2ToCGNS[1]  =  8; SU2ToCGNS[2]  =  1; SU2ToCGNS[3]  = 11;
-  SU2ToCGNS[4]  = 20; SU2ToCGNS[5]  =  9; SU2ToCGNS[6]  =  3; SU2ToCGNS[7]  = 10;
-  SU2ToCGNS[8]  =  2; SU2ToCGNS[9]  = 12; SU2ToCGNS[10] = 21; SU2ToCGNS[11] = 13;
-  SU2ToCGNS[12] = 24; SU2ToCGNS[13] = 26; SU2ToCGNS[14] = 22; SU2ToCGNS[15] = 15;
-  SU2ToCGNS[16] = 23; SU2ToCGNS[17] = 14; SU2ToCGNS[18] =  4; SU2ToCGNS[19] = 16;
-  SU2ToCGNS[20] =  5; SU2ToCGNS[21] = 19; SU2ToCGNS[22] = 25; SU2ToCGNS[23] = 17;
-  SU2ToCGNS[24] =  7; SU2ToCGNS[25] = 18; SU2ToCGNS[26] =  6;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 8;
+  SU2ToCGNS[2] = 1;
+  SU2ToCGNS[3] = 11;
+  SU2ToCGNS[4] = 20;
+  SU2ToCGNS[5] = 9;
+  SU2ToCGNS[6] = 3;
+  SU2ToCGNS[7] = 10;
+  SU2ToCGNS[8] = 2;
+  SU2ToCGNS[9] = 12;
+  SU2ToCGNS[10] = 21;
+  SU2ToCGNS[11] = 13;
+  SU2ToCGNS[12] = 24;
+  SU2ToCGNS[13] = 26;
+  SU2ToCGNS[14] = 22;
+  SU2ToCGNS[15] = 15;
+  SU2ToCGNS[16] = 23;
+  SU2ToCGNS[17] = 14;
+  SU2ToCGNS[18] = 4;
+  SU2ToCGNS[19] = 16;
+  SU2ToCGNS[20] = 5;
+  SU2ToCGNS[21] = 19;
+  SU2ToCGNS[22] = 25;
+  SU2ToCGNS[23] = 17;
+  SU2ToCGNS[24] = 7;
+  SU2ToCGNS[25] = 18;
+  SU2ToCGNS[26] = 6;
 }
 
-void CCGNSElementType::CreateDataHEXA_64(unsigned short         &VTK_Type,
-                                         unsigned short         &nPoly,
-                                         unsigned short         &nDOFs,
-                                         vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataHEXA_64(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                         vector<unsigned short>& SU2ToCGNS) {
   /* The HEXA_64 element is a cubic hexahedron. In CGNS the nodes are
      numbered as follows: - First the vertex nodes.
                           - Second the edge nodes.
@@ -1062,33 +1361,78 @@ void CCGNSElementType::CreateDataHEXA_64(unsigned short         &VTK_Type,
      from node 0 along the second edge and the k-direction from node 0 along
      the third edge. */
   VTK_Type = HEXAHEDRON;
-  nPoly    =  3;
-  nDOFs    = 64;
+  nPoly = 3;
+  nDOFs = 64;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0]  =  0; SU2ToCGNS[1]  =  8; SU2ToCGNS[2]  =  9; SU2ToCGNS[3]  =  1;
-  SU2ToCGNS[4]  = 15; SU2ToCGNS[5]  = 32; SU2ToCGNS[6]  = 33; SU2ToCGNS[7]  = 10;
-  SU2ToCGNS[8]  = 14; SU2ToCGNS[9]  = 35; SU2ToCGNS[10] = 34; SU2ToCGNS[11] = 11;
-  SU2ToCGNS[12] =  3; SU2ToCGNS[13] = 13; SU2ToCGNS[14] = 12; SU2ToCGNS[15] =  2;
-  SU2ToCGNS[16] = 16; SU2ToCGNS[17] = 36; SU2ToCGNS[18] = 37; SU2ToCGNS[19] = 18;
-  SU2ToCGNS[20] = 49; SU2ToCGNS[21] = 56; SU2ToCGNS[22] = 57; SU2ToCGNS[23] = 40;
-  SU2ToCGNS[24] = 48; SU2ToCGNS[25] = 59; SU2ToCGNS[26] = 58; SU2ToCGNS[27] = 41;
-  SU2ToCGNS[28] = 22; SU2ToCGNS[29] = 45; SU2ToCGNS[30] = 44; SU2ToCGNS[31] = 20;
-  SU2ToCGNS[32] = 17; SU2ToCGNS[33] = 39; SU2ToCGNS[34] = 38; SU2ToCGNS[35] = 19;
-  SU2ToCGNS[36] = 50; SU2ToCGNS[37] = 60; SU2ToCGNS[38] = 61; SU2ToCGNS[39] = 43;
-  SU2ToCGNS[40] = 51; SU2ToCGNS[41] = 63; SU2ToCGNS[42] = 62; SU2ToCGNS[43] = 42;
-  SU2ToCGNS[44] = 23; SU2ToCGNS[45] = 46; SU2ToCGNS[46] = 47; SU2ToCGNS[47] = 21;
-  SU2ToCGNS[48] =  4; SU2ToCGNS[49] = 24; SU2ToCGNS[50] = 25; SU2ToCGNS[51] =  5;
-  SU2ToCGNS[52] = 31; SU2ToCGNS[53] = 52; SU2ToCGNS[54] = 53; SU2ToCGNS[55] = 26;
-  SU2ToCGNS[56] = 30; SU2ToCGNS[57] = 55; SU2ToCGNS[58] = 54; SU2ToCGNS[59] = 27;
-  SU2ToCGNS[60] =  7; SU2ToCGNS[61] = 29; SU2ToCGNS[62] = 28; SU2ToCGNS[63] =  6;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 8;
+  SU2ToCGNS[2] = 9;
+  SU2ToCGNS[3] = 1;
+  SU2ToCGNS[4] = 15;
+  SU2ToCGNS[5] = 32;
+  SU2ToCGNS[6] = 33;
+  SU2ToCGNS[7] = 10;
+  SU2ToCGNS[8] = 14;
+  SU2ToCGNS[9] = 35;
+  SU2ToCGNS[10] = 34;
+  SU2ToCGNS[11] = 11;
+  SU2ToCGNS[12] = 3;
+  SU2ToCGNS[13] = 13;
+  SU2ToCGNS[14] = 12;
+  SU2ToCGNS[15] = 2;
+  SU2ToCGNS[16] = 16;
+  SU2ToCGNS[17] = 36;
+  SU2ToCGNS[18] = 37;
+  SU2ToCGNS[19] = 18;
+  SU2ToCGNS[20] = 49;
+  SU2ToCGNS[21] = 56;
+  SU2ToCGNS[22] = 57;
+  SU2ToCGNS[23] = 40;
+  SU2ToCGNS[24] = 48;
+  SU2ToCGNS[25] = 59;
+  SU2ToCGNS[26] = 58;
+  SU2ToCGNS[27] = 41;
+  SU2ToCGNS[28] = 22;
+  SU2ToCGNS[29] = 45;
+  SU2ToCGNS[30] = 44;
+  SU2ToCGNS[31] = 20;
+  SU2ToCGNS[32] = 17;
+  SU2ToCGNS[33] = 39;
+  SU2ToCGNS[34] = 38;
+  SU2ToCGNS[35] = 19;
+  SU2ToCGNS[36] = 50;
+  SU2ToCGNS[37] = 60;
+  SU2ToCGNS[38] = 61;
+  SU2ToCGNS[39] = 43;
+  SU2ToCGNS[40] = 51;
+  SU2ToCGNS[41] = 63;
+  SU2ToCGNS[42] = 62;
+  SU2ToCGNS[43] = 42;
+  SU2ToCGNS[44] = 23;
+  SU2ToCGNS[45] = 46;
+  SU2ToCGNS[46] = 47;
+  SU2ToCGNS[47] = 21;
+  SU2ToCGNS[48] = 4;
+  SU2ToCGNS[49] = 24;
+  SU2ToCGNS[50] = 25;
+  SU2ToCGNS[51] = 5;
+  SU2ToCGNS[52] = 31;
+  SU2ToCGNS[53] = 52;
+  SU2ToCGNS[54] = 53;
+  SU2ToCGNS[55] = 26;
+  SU2ToCGNS[56] = 30;
+  SU2ToCGNS[57] = 55;
+  SU2ToCGNS[58] = 54;
+  SU2ToCGNS[59] = 27;
+  SU2ToCGNS[60] = 7;
+  SU2ToCGNS[61] = 29;
+  SU2ToCGNS[62] = 28;
+  SU2ToCGNS[63] = 6;
 }
 
-void CCGNSElementType::CreateDataHEXA_125(unsigned short         &VTK_Type,
-                                          unsigned short         &nPoly,
-                                          unsigned short         &nDOFs,
-                                          vector<unsigned short> &SU2ToCGNS) {
-
+void CCGNSElementType::CreateDataHEXA_125(unsigned short& VTK_Type, unsigned short& nPoly, unsigned short& nDOFs,
+                                          vector<unsigned short>& SU2ToCGNS) {
   /* The HEXA_125 element is a quartic hexahedron. In CGNS the nodes are
      numbered as follows: - First the vertex nodes.
                           - Second the edge nodes.
@@ -1099,35 +1443,135 @@ void CCGNSElementType::CreateDataHEXA_125(unsigned short         &VTK_Type,
      from node 0 along the second edge and the k-direction from node 0 along
      the third edge. */
   VTK_Type = HEXAHEDRON;
-  nPoly    =   4;
-  nDOFs    = 125;
+  nPoly = 4;
+  nDOFs = 125;
 
   SU2ToCGNS.resize(nDOFs);
-  SU2ToCGNS[0]   =   0; SU2ToCGNS[1]   =   8; SU2ToCGNS[2]   =   9; SU2ToCGNS[3]   =  10; SU2ToCGNS[4]   =   1;
-  SU2ToCGNS[5]   =  19; SU2ToCGNS[6]   =  44; SU2ToCGNS[7]   =  45; SU2ToCGNS[8]   =  46; SU2ToCGNS[9]   =  11;
-  SU2ToCGNS[10]  =  18; SU2ToCGNS[11]  =  51; SU2ToCGNS[12]  =  52; SU2ToCGNS[13]  =  47; SU2ToCGNS[14]  =  12;
-  SU2ToCGNS[15]  =  17; SU2ToCGNS[16]  =  50; SU2ToCGNS[17]  =  49; SU2ToCGNS[18]  =  48; SU2ToCGNS[19]  =  13;
-  SU2ToCGNS[20]  =   3; SU2ToCGNS[21]  =  16; SU2ToCGNS[22]  =  15; SU2ToCGNS[23]  =  14; SU2ToCGNS[24]  =   2;
-  SU2ToCGNS[25]  =  20; SU2ToCGNS[26]  =  53; SU2ToCGNS[27]  =  54; SU2ToCGNS[28]  =  55; SU2ToCGNS[29]  =  23;
-  SU2ToCGNS[30]  =  82; SU2ToCGNS[31]  =  98; SU2ToCGNS[32]  =  99; SU2ToCGNS[33]  = 100; SU2ToCGNS[34]  =  62;
-  SU2ToCGNS[35]  =  81; SU2ToCGNS[36]  = 105; SU2ToCGNS[37]  = 106; SU2ToCGNS[38]  = 101; SU2ToCGNS[39]  =  63;
-  SU2ToCGNS[40]  =  80; SU2ToCGNS[41]  = 104; SU2ToCGNS[42]  = 103; SU2ToCGNS[43]  = 102; SU2ToCGNS[44]  =  64;
-  SU2ToCGNS[45]  =  29; SU2ToCGNS[46]  =  73; SU2ToCGNS[47]  =  72; SU2ToCGNS[48]  =  71; SU2ToCGNS[49]  =  26;
-  SU2ToCGNS[50]  =  21; SU2ToCGNS[51]  =  60; SU2ToCGNS[52]  =  61; SU2ToCGNS[53]  =  56; SU2ToCGNS[54]  =  24;
-  SU2ToCGNS[55]  =  83; SU2ToCGNS[56]  = 107; SU2ToCGNS[57]  = 108; SU2ToCGNS[58]  = 109; SU2ToCGNS[59]  =  69;
-  SU2ToCGNS[60]  =  88; SU2ToCGNS[61]  = 114; SU2ToCGNS[62]  = 115; SU2ToCGNS[63]  = 110; SU2ToCGNS[64]  =  70;
-  SU2ToCGNS[65]  =  87; SU2ToCGNS[66]  = 113; SU2ToCGNS[67]  = 112; SU2ToCGNS[68]  = 111; SU2ToCGNS[69]  =  65;
-  SU2ToCGNS[70]  =  30; SU2ToCGNS[71]  =  74; SU2ToCGNS[72]  =  79; SU2ToCGNS[73]  =  78; SU2ToCGNS[74]  =  27;
-  SU2ToCGNS[75]  =  22; SU2ToCGNS[76]  =  59; SU2ToCGNS[77]  =  58; SU2ToCGNS[78]  =  57; SU2ToCGNS[79]  =  25;
-  SU2ToCGNS[80]  =  84; SU2ToCGNS[81]  = 116; SU2ToCGNS[82]  = 117; SU2ToCGNS[83]  = 118; SU2ToCGNS[84]  =  68;
-  SU2ToCGNS[85]  =  85; SU2ToCGNS[86]  = 123; SU2ToCGNS[87]  = 124; SU2ToCGNS[88]  = 119; SU2ToCGNS[89]  =  67;
-  SU2ToCGNS[90]  =  86; SU2ToCGNS[91]  = 122; SU2ToCGNS[92]  = 121; SU2ToCGNS[93]  = 120; SU2ToCGNS[94]  =  66;
-  SU2ToCGNS[95]  =  31; SU2ToCGNS[96]  =  75; SU2ToCGNS[97]  =  76; SU2ToCGNS[98]  =  77; SU2ToCGNS[99]  =  28;
-  SU2ToCGNS[100] =   4; SU2ToCGNS[101] =  32; SU2ToCGNS[102] =  33; SU2ToCGNS[103] =  34; SU2ToCGNS[104] =   5;
-  SU2ToCGNS[105] =  43; SU2ToCGNS[106] =  89; SU2ToCGNS[107] =  90; SU2ToCGNS[108] =  91; SU2ToCGNS[109] =  35;
-  SU2ToCGNS[110] =  42; SU2ToCGNS[111] =  96; SU2ToCGNS[112] =  97; SU2ToCGNS[113] =  92; SU2ToCGNS[114] =  36;
-  SU2ToCGNS[115] =  41; SU2ToCGNS[116] =  95; SU2ToCGNS[117] =  94; SU2ToCGNS[118] =  93; SU2ToCGNS[119] =  37;
-  SU2ToCGNS[120] =   7; SU2ToCGNS[121] =  40; SU2ToCGNS[122] =  39; SU2ToCGNS[123] =  38; SU2ToCGNS[124] =   6;
+  SU2ToCGNS[0] = 0;
+  SU2ToCGNS[1] = 8;
+  SU2ToCGNS[2] = 9;
+  SU2ToCGNS[3] = 10;
+  SU2ToCGNS[4] = 1;
+  SU2ToCGNS[5] = 19;
+  SU2ToCGNS[6] = 44;
+  SU2ToCGNS[7] = 45;
+  SU2ToCGNS[8] = 46;
+  SU2ToCGNS[9] = 11;
+  SU2ToCGNS[10] = 18;
+  SU2ToCGNS[11] = 51;
+  SU2ToCGNS[12] = 52;
+  SU2ToCGNS[13] = 47;
+  SU2ToCGNS[14] = 12;
+  SU2ToCGNS[15] = 17;
+  SU2ToCGNS[16] = 50;
+  SU2ToCGNS[17] = 49;
+  SU2ToCGNS[18] = 48;
+  SU2ToCGNS[19] = 13;
+  SU2ToCGNS[20] = 3;
+  SU2ToCGNS[21] = 16;
+  SU2ToCGNS[22] = 15;
+  SU2ToCGNS[23] = 14;
+  SU2ToCGNS[24] = 2;
+  SU2ToCGNS[25] = 20;
+  SU2ToCGNS[26] = 53;
+  SU2ToCGNS[27] = 54;
+  SU2ToCGNS[28] = 55;
+  SU2ToCGNS[29] = 23;
+  SU2ToCGNS[30] = 82;
+  SU2ToCGNS[31] = 98;
+  SU2ToCGNS[32] = 99;
+  SU2ToCGNS[33] = 100;
+  SU2ToCGNS[34] = 62;
+  SU2ToCGNS[35] = 81;
+  SU2ToCGNS[36] = 105;
+  SU2ToCGNS[37] = 106;
+  SU2ToCGNS[38] = 101;
+  SU2ToCGNS[39] = 63;
+  SU2ToCGNS[40] = 80;
+  SU2ToCGNS[41] = 104;
+  SU2ToCGNS[42] = 103;
+  SU2ToCGNS[43] = 102;
+  SU2ToCGNS[44] = 64;
+  SU2ToCGNS[45] = 29;
+  SU2ToCGNS[46] = 73;
+  SU2ToCGNS[47] = 72;
+  SU2ToCGNS[48] = 71;
+  SU2ToCGNS[49] = 26;
+  SU2ToCGNS[50] = 21;
+  SU2ToCGNS[51] = 60;
+  SU2ToCGNS[52] = 61;
+  SU2ToCGNS[53] = 56;
+  SU2ToCGNS[54] = 24;
+  SU2ToCGNS[55] = 83;
+  SU2ToCGNS[56] = 107;
+  SU2ToCGNS[57] = 108;
+  SU2ToCGNS[58] = 109;
+  SU2ToCGNS[59] = 69;
+  SU2ToCGNS[60] = 88;
+  SU2ToCGNS[61] = 114;
+  SU2ToCGNS[62] = 115;
+  SU2ToCGNS[63] = 110;
+  SU2ToCGNS[64] = 70;
+  SU2ToCGNS[65] = 87;
+  SU2ToCGNS[66] = 113;
+  SU2ToCGNS[67] = 112;
+  SU2ToCGNS[68] = 111;
+  SU2ToCGNS[69] = 65;
+  SU2ToCGNS[70] = 30;
+  SU2ToCGNS[71] = 74;
+  SU2ToCGNS[72] = 79;
+  SU2ToCGNS[73] = 78;
+  SU2ToCGNS[74] = 27;
+  SU2ToCGNS[75] = 22;
+  SU2ToCGNS[76] = 59;
+  SU2ToCGNS[77] = 58;
+  SU2ToCGNS[78] = 57;
+  SU2ToCGNS[79] = 25;
+  SU2ToCGNS[80] = 84;
+  SU2ToCGNS[81] = 116;
+  SU2ToCGNS[82] = 117;
+  SU2ToCGNS[83] = 118;
+  SU2ToCGNS[84] = 68;
+  SU2ToCGNS[85] = 85;
+  SU2ToCGNS[86] = 123;
+  SU2ToCGNS[87] = 124;
+  SU2ToCGNS[88] = 119;
+  SU2ToCGNS[89] = 67;
+  SU2ToCGNS[90] = 86;
+  SU2ToCGNS[91] = 122;
+  SU2ToCGNS[92] = 121;
+  SU2ToCGNS[93] = 120;
+  SU2ToCGNS[94] = 66;
+  SU2ToCGNS[95] = 31;
+  SU2ToCGNS[96] = 75;
+  SU2ToCGNS[97] = 76;
+  SU2ToCGNS[98] = 77;
+  SU2ToCGNS[99] = 28;
+  SU2ToCGNS[100] = 4;
+  SU2ToCGNS[101] = 32;
+  SU2ToCGNS[102] = 33;
+  SU2ToCGNS[103] = 34;
+  SU2ToCGNS[104] = 5;
+  SU2ToCGNS[105] = 43;
+  SU2ToCGNS[106] = 89;
+  SU2ToCGNS[107] = 90;
+  SU2ToCGNS[108] = 91;
+  SU2ToCGNS[109] = 35;
+  SU2ToCGNS[110] = 42;
+  SU2ToCGNS[111] = 96;
+  SU2ToCGNS[112] = 97;
+  SU2ToCGNS[113] = 92;
+  SU2ToCGNS[114] = 36;
+  SU2ToCGNS[115] = 41;
+  SU2ToCGNS[116] = 95;
+  SU2ToCGNS[117] = 94;
+  SU2ToCGNS[118] = 93;
+  SU2ToCGNS[119] = 37;
+  SU2ToCGNS[120] = 7;
+  SU2ToCGNS[121] = 40;
+  SU2ToCGNS[122] = 39;
+  SU2ToCGNS[123] = 38;
+  SU2ToCGNS[124] = 6;
 }
 
 #endif
diff --git a/Common/src/fem/fem_gauss_jacobi_quadrature.cpp b/Common/src/fem/fem_gauss_jacobi_quadrature.cpp
index 47492b728e9..124a90d166b 100644
--- a/Common/src/fem/fem_gauss_jacobi_quadrature.cpp
+++ b/Common/src/fem/fem_gauss_jacobi_quadrature.cpp
@@ -79,13 +79,12 @@ Tom
 
 #include "../../include/fem/fem_gauss_jacobi_quadrature.hpp"
 
-void CGaussJacobiQuadrature::GetQuadraturePoints(const passivedouble   alpha,     const passivedouble   beta,
-                                                 const passivedouble   a,         const passivedouble   b,
-                                                 vector<passivedouble> &GJPoints, vector<passivedouble> &GJWeights) {
-
+void CGaussJacobiQuadrature::GetQuadraturePoints(const passivedouble alpha, const passivedouble beta,
+                                                 const passivedouble a, const passivedouble b,
+                                                 vector<passivedouble>& GJPoints, vector<passivedouble>& GJWeights) {
   /*--- Determine the number of integration points. Check if the number makes sense. ---*/
   unsigned int nIntPoints = (unsigned int)GJPoints.size();
-  if(nIntPoints < 1 || nIntPoints > 100)
+  if (nIntPoints < 1 || nIntPoints > 100)
     SU2_MPI::Error("Invalid number of Gauss Jacobi integration points", CURRENT_FUNCTION);
 
   /*--- Call the function cgqf to do the actual work. ---*/
@@ -95,8 +94,8 @@ void CGaussJacobiQuadrature::GetQuadraturePoints(const passivedouble   alpha,
 
 //****************************************************************************80
 
-void CGaussJacobiQuadrature::cdgqf(int nt, int kind, passivedouble alpha, passivedouble beta,
-                                   passivedouble t[], passivedouble wts[])
+void CGaussJacobiQuadrature::cdgqf(int nt, int kind, passivedouble alpha, passivedouble beta, passivedouble t[],
+                                   passivedouble wts[])
 
 //****************************************************************************80
 //
@@ -158,32 +157,32 @@ void CGaussJacobiQuadrature::cdgqf(int nt, int kind, passivedouble alpha, passiv
 //    Output, passivedouble WTS[NT], the weights.
 //
 {
-  passivedouble *aj;
-  passivedouble *bj;
+  passivedouble* aj;
+  passivedouble* bj;
   passivedouble zemu;
 
-  parchk ( kind, 2 * nt, alpha, beta );
-//
-//  Get the Jacobi matrix and zero-th moment.
-//
+  parchk(kind, 2 * nt, alpha, beta);
+  //
+  //  Get the Jacobi matrix and zero-th moment.
+  //
   aj = new passivedouble[nt];
   bj = new passivedouble[nt];
 
-  zemu = class_matrix ( kind, nt, alpha, beta, aj, bj );
-//
-//  Compute the knots and weights.
-//
-  sgqf ( nt, aj, bj, zemu, t, wts );
+  zemu = class_matrix(kind, nt, alpha, beta, aj, bj);
+  //
+  //  Compute the knots and weights.
+  //
+  sgqf(nt, aj, bj, zemu, t, wts);
 
-  delete [] aj;
-  delete [] bj;
+  delete[] aj;
+  delete[] bj;
 
   return;
 }
 //****************************************************************************80
 
-void CGaussJacobiQuadrature::cgqf(int nt, int kind, passivedouble alpha, passivedouble beta,
-                                  passivedouble a, passivedouble b, passivedouble t[], passivedouble wts[])
+void CGaussJacobiQuadrature::cgqf(int nt, int kind, passivedouble alpha, passivedouble beta, passivedouble a,
+                                  passivedouble b, passivedouble t[], passivedouble wts[])
 
 //****************************************************************************80
 //
@@ -248,38 +247,35 @@ void CGaussJacobiQuadrature::cgqf(int nt, int kind, passivedouble alpha, passive
 //
 {
   int i;
-  int *mlt;
-  int *ndx;
-//
-//  Compute the Gauss quadrature formula for default values of A and B.
-//
-  cdgqf ( nt, kind, alpha, beta, t, wts );
-//
-//  Prepare to scale the quadrature formula to other weight function with
-//  valid A and B.
-//
+  int* mlt;
+  int* ndx;
+  //
+  //  Compute the Gauss quadrature formula for default values of A and B.
+  //
+  cdgqf(nt, kind, alpha, beta, t, wts);
+  //
+  //  Prepare to scale the quadrature formula to other weight function with
+  //  valid A and B.
+  //
   mlt = new int[nt];
-  for ( i = 0; i < nt; i++ )
-  {
+  for (i = 0; i < nt; i++) {
     mlt[i] = 1;
   }
   ndx = new int[nt];
-  for ( i = 0; i < nt; i++ )
-  {
+  for (i = 0; i < nt; i++) {
     ndx[i] = i + 1;
   }
-  scqf ( nt, t, mlt, wts, nt, ndx, wts, t, kind, alpha, beta, a, b );
+  scqf(nt, t, mlt, wts, nt, ndx, wts, t, kind, alpha, beta, a, b);
 
-  delete [] mlt;
-  delete [] ndx;
+  delete[] mlt;
+  delete[] ndx;
 
   return;
 }
 //****************************************************************************80
 
-passivedouble CGaussJacobiQuadrature::class_matrix(int kind, int m, passivedouble alpha,
-                                                   passivedouble beta, passivedouble aj[],
-                                                   passivedouble bj[])
+passivedouble CGaussJacobiQuadrature::class_matrix(int kind, int m, passivedouble alpha, passivedouble beta,
+                                                   passivedouble aj[], passivedouble bj[])
 
 //****************************************************************************80
 //
@@ -358,157 +354,121 @@ passivedouble CGaussJacobiQuadrature::class_matrix(int kind, int m, passivedoubl
   passivedouble temp2;
   passivedouble zemu;
 
-  temp = r8_epsilon ( );
+  temp = r8_epsilon();
 
-  parchk ( kind, 2 * m - 1, alpha, beta );
+  parchk(kind, 2 * m - 1, alpha, beta);
 
   temp2 = 0.5;
 
-  if ( 500.0 * temp < fabs ( pow ( tgamma ( temp2 ), 2 ) - pi ) )
-  {
+  if (500.0 * temp < fabs(pow(tgamma(temp2), 2) - pi)) {
     cout << "\n";
     cout << "CLASS_MATRIX - Fatal error!\n";
     cout << "  Gamma function does not match machine parameters.\n";
-    exit ( 1 );
+    exit(1);
   }
 
-  if ( kind == 1 )
-  {
+  if (kind == 1) {
     ab = 0.0;
 
-    zemu = 2.0 / ( ab + 1.0 );
+    zemu = 2.0 / (ab + 1.0);
 
-    for ( i = 0; i < m; i++ )
-    {
+    for (i = 0; i < m; i++) {
       aj[i] = 0.0;
     }
 
-    for ( i = 1; i <= m; i++ )
-    {
-      abi = i + ab * ( i % 2 );
+    for (i = 1; i <= m; i++) {
+      abi = i + ab * (i % 2);
       abj = 2 * i + ab;
-      bj[i-1] = sqrt ( abi * abi / ( abj * abj - 1.0 ) );
+      bj[i - 1] = sqrt(abi * abi / (abj * abj - 1.0));
     }
-  }
-  else if ( kind == 2 )
-  {
+  } else if (kind == 2) {
     zemu = pi;
 
-    for ( i = 0; i < m; i++ )
-    {
+    for (i = 0; i < m; i++) {
       aj[i] = 0.0;
     }
 
-    bj[0] =  sqrt ( 0.5 );
-    for ( i = 1; i < m; i++ )
-    {
+    bj[0] = sqrt(0.5);
+    for (i = 1; i < m; i++) {
       bj[i] = 0.5;
     }
-  }
-  else if ( kind == 3 )
-  {
+  } else if (kind == 3) {
     ab = alpha * 2.0;
-    zemu = pow ( 2.0, ab + 1.0 ) * pow ( tgamma ( alpha + 1.0 ), 2 )
-      / tgamma ( ab + 2.0 );
+    zemu = pow(2.0, ab + 1.0) * pow(tgamma(alpha + 1.0), 2) / tgamma(ab + 2.0);
 
-    for ( i = 0; i < m; i++ )
-    {
+    for (i = 0; i < m; i++) {
       aj[i] = 0.0;
     }
 
-    bj[0] = sqrt ( 1.0 / ( 2.0 * alpha + 3.0 ) );
-    for ( i = 2; i <= m; i++ )
-    {
-      bj[i-1] = sqrt ( i * ( i + ab ) / ( 4.0 * pow ( i + alpha, 2 ) - 1.0 ) );
+    bj[0] = sqrt(1.0 / (2.0 * alpha + 3.0));
+    for (i = 2; i <= m; i++) {
+      bj[i - 1] = sqrt(i * (i + ab) / (4.0 * pow(i + alpha, 2) - 1.0));
     }
-  }
-  else if ( kind == 4 )
-  {
+  } else if (kind == 4) {
     ab = alpha + beta;
     abi = 2.0 + ab;
-    zemu = pow ( 2.0, ab + 1.0 ) * tgamma ( alpha + 1.0 )
-      * tgamma ( beta + 1.0 ) / tgamma ( abi );
-    aj[0] = ( beta - alpha ) / abi;
-    bj[0] = sqrt ( 4.0 * ( 1.0 + alpha ) * ( 1.0 + beta )
-      / ( ( abi + 1.0 ) * abi * abi ) );
+    zemu = pow(2.0, ab + 1.0) * tgamma(alpha + 1.0) * tgamma(beta + 1.0) / tgamma(abi);
+    aj[0] = (beta - alpha) / abi;
+    bj[0] = sqrt(4.0 * (1.0 + alpha) * (1.0 + beta) / ((abi + 1.0) * abi * abi));
     a2b2 = beta * beta - alpha * alpha;
 
-    for ( i = 2; i <= m; i++ )
-    {
+    for (i = 2; i <= m; i++) {
       abi = 2.0 * i + ab;
-      aj[i-1] = a2b2 / ( ( abi - 2.0 ) * abi );
+      aj[i - 1] = a2b2 / ((abi - 2.0) * abi);
       abi = abi * abi;
-      bj[i-1] = sqrt ( 4.0 * i * ( i + alpha ) * ( i + beta ) * ( i + ab )
-        / ( ( abi - 1.0 ) * abi ) );
+      bj[i - 1] = sqrt(4.0 * i * (i + alpha) * (i + beta) * (i + ab) / ((abi - 1.0) * abi));
     }
-  }
-  else if ( kind == 5 )
-  {
-    zemu = tgamma ( alpha + 1.0 );
+  } else if (kind == 5) {
+    zemu = tgamma(alpha + 1.0);
 
-    for ( i = 1; i <= m; i++ )
-    {
-      aj[i-1] = 2.0 * i - 1.0 + alpha;
-      bj[i-1] = sqrt ( i * ( i + alpha ) );
+    for (i = 1; i <= m; i++) {
+      aj[i - 1] = 2.0 * i - 1.0 + alpha;
+      bj[i - 1] = sqrt(i * (i + alpha));
     }
-  }
-  else if ( kind == 6 )
-  {
-    zemu = tgamma ( ( alpha + 1.0 ) / 2.0 );
+  } else if (kind == 6) {
+    zemu = tgamma((alpha + 1.0) / 2.0);
 
-    for ( i = 0; i < m; i++ )
-    {
+    for (i = 0; i < m; i++) {
       aj[i] = 0.0;
     }
 
-    for ( i = 1; i <= m; i++ )
-    {
-      bj[i-1] = sqrt ( ( i + alpha * ( i % 2 ) ) / 2.0 );
+    for (i = 1; i <= m; i++) {
+      bj[i - 1] = sqrt((i + alpha * (i % 2)) / 2.0);
     }
-  }
-  else if ( kind == 7 )
-  {
+  } else if (kind == 7) {
     ab = alpha;
-    zemu = 2.0 / ( ab + 1.0 );
+    zemu = 2.0 / (ab + 1.0);
 
-    for ( i = 0; i < m; i++ )
-    {
+    for (i = 0; i < m; i++) {
       aj[i] = 0.0;
     }
 
-    for ( i = 1; i <= m; i++ )
-    {
-      abi = i + ab * ( i % 2 );
+    for (i = 1; i <= m; i++) {
+      abi = i + ab * (i % 2);
       abj = 2 * i + ab;
-      bj[i-1] = sqrt ( abi * abi / ( abj * abj - 1.0 ) );
+      bj[i - 1] = sqrt(abi * abi / (abj * abj - 1.0));
     }
-  }
-  else   // if ( kind == 8 )
+  } else  // if ( kind == 8 )
   {
     ab = alpha + beta;
-    zemu = tgamma ( alpha + 1.0 ) * tgamma ( - ( ab + 1.0 ) )
-      / tgamma ( - beta );
+    zemu = tgamma(alpha + 1.0) * tgamma(-(ab + 1.0)) / tgamma(-beta);
     apone = alpha + 1.0;
     aba = ab * apone;
-    aj[0] = - apone / ( ab + 2.0 );
-    bj[0] = - aj[0] * ( beta + 1.0 ) / ( ab + 2.0 ) / ( ab + 3.0 );
-    for ( i = 2; i <= m; i++ )
-    {
+    aj[0] = -apone / (ab + 2.0);
+    bj[0] = -aj[0] * (beta + 1.0) / (ab + 2.0) / (ab + 3.0);
+    for (i = 2; i <= m; i++) {
       abti = ab + 2.0 * i;
-      aj[i-1] = aba + 2.0 * ( ab + i ) * ( i - 1 );
-      aj[i-1] = - aj[i-1] / abti / ( abti - 2.0 );
+      aj[i - 1] = aba + 2.0 * (ab + i) * (i - 1);
+      aj[i - 1] = -aj[i - 1] / abti / (abti - 2.0);
     }
 
-    for ( i = 2; i <= m - 1; i++ )
-    {
+    for (i = 2; i <= m - 1; i++) {
       abti = ab + 2.0 * i;
-      bj[i-1] = i * ( alpha + i ) / ( abti - 1.0 ) * ( beta + i )
-        / ( abti * abti ) * ( ab + i ) / ( abti + 1.0 );
+      bj[i - 1] = i * (alpha + i) / (abti - 1.0) * (beta + i) / (abti * abti) * (ab + i) / (abti + 1.0);
     }
-    bj[m-1] = 0.0;
-    for ( i = 0; i < m; i++ )
-    {
-      bj[i] =  sqrt ( bj[i] );
+    bj[m - 1] = 0.0;
+    for (i = 0; i < m; i++) {
+      bj[i] = sqrt(bj[i]);
     }
   }
 
@@ -596,114 +556,98 @@ void CGaussJacobiQuadrature::imtqlx(int n, passivedouble d[], passivedouble e[],
   passivedouble r;
   passivedouble s;
 
-  prec = r8_epsilon ( );
+  prec = r8_epsilon();
 
-  if ( n == 1 )
-  {
+  if (n == 1) {
     return;
   }
 
-  e[n-1] = 0.0;
+  e[n - 1] = 0.0;
 
-  for ( l = 1; l <= n; l++ )
-  {
+  for (l = 1; l <= n; l++) {
     j = 0;
-    for ( ; ; )
-    {
-      for ( m = l; m <= n; m++ )
-      {
-        if ( m == n )
-        {
+    for (;;) {
+      for (m = l; m <= n; m++) {
+        if (m == n) {
           break;
         }
 
-        if ( fabs ( e[m-1] ) <= prec * ( fabs ( d[m-1] ) + fabs ( d[m] ) ) )
-        {
+        if (fabs(e[m - 1]) <= prec * (fabs(d[m - 1]) + fabs(d[m]))) {
           break;
         }
       }
-      p = d[l-1];
-      if ( m == l )
-      {
+      p = d[l - 1];
+      if (m == l) {
         break;
       }
-      if ( itn <= j )
-      {
+      if (itn <= j) {
         cout << "\n";
         cout << "IMTQLX - Fatal error!\n";
         cout << "  Iteration limit exceeded\n";
-        exit ( 1 );
+        exit(1);
       }
       j = j + 1;
-      g = ( d[l] - p ) / ( 2.0 * e[l-1] );
-      r =  sqrt ( g * g + 1.0 );
-      g = d[m-1] - p + e[l-1] / ( g + fabs ( r ) * r8_sign ( g ) );
+      g = (d[l] - p) / (2.0 * e[l - 1]);
+      r = sqrt(g * g + 1.0);
+      g = d[m - 1] - p + e[l - 1] / (g + fabs(r) * r8_sign(g));
       s = 1.0;
       c = 1.0;
       p = 0.0;
       mml = m - l;
 
-      for ( ii = 1; ii <= mml; ii++ )
-      {
+      for (ii = 1; ii <= mml; ii++) {
         i = m - ii;
-        f = s * e[i-1];
-        b = c * e[i-1];
+        f = s * e[i - 1];
+        b = c * e[i - 1];
 
-        if ( fabs ( g ) <= fabs ( f ) )
-        {
+        if (fabs(g) <= fabs(f)) {
           c = g / f;
-          r =  sqrt ( c * c + 1.0 );
+          r = sqrt(c * c + 1.0);
           e[i] = f * r;
           s = 1.0 / r;
           c = c * s;
-        }
-        else
-        {
+        } else {
           s = f / g;
-          r =  sqrt ( s * s + 1.0 );
+          r = sqrt(s * s + 1.0);
           e[i] = g * r;
           c = 1.0 / r;
           s = s * c;
         }
         g = d[i] - p;
-        r = ( d[i-1] - g ) * s + 2.0 * c * b;
+        r = (d[i - 1] - g) * s + 2.0 * c * b;
         p = s * r;
         d[i] = g + p;
         g = c * r - b;
         f = z[i];
-        z[i] = s * z[i-1] + c * f;
-        z[i-1] = c * z[i-1] - s * f;
+        z[i] = s * z[i - 1] + c * f;
+        z[i - 1] = c * z[i - 1] - s * f;
       }
-      d[l-1] = d[l-1] - p;
-      e[l-1] = g;
-      e[m-1] = 0.0;
+      d[l - 1] = d[l - 1] - p;
+      e[l - 1] = g;
+      e[m - 1] = 0.0;
     }
   }
-//
-//  Sorting.
-//
-  for ( ii = 2; ii <= m; ii++ )
-  {
+  //
+  //  Sorting.
+  //
+  for (ii = 2; ii <= m; ii++) {
     i = ii - 1;
     k = i;
-    p = d[i-1];
-
-    for ( j = ii; j <= n; j++ )
-    {
-      if ( d[j-1] < p )
-      {
-         k = j;
-         p = d[j-1];
+    p = d[i - 1];
+
+    for (j = ii; j <= n; j++) {
+      if (d[j - 1] < p) {
+        k = j;
+        p = d[j - 1];
       }
     }
 
-    if ( k != i )
-    {
-      d[k-1] = d[i-1];
-      d[i-1] = p;
-      p = z[i-1];
-      z[i-1] = z[k-1];
-      z[k-1] = p;
+    if (k != i) {
+      d[k - 1] = d[i - 1];
+      d[i - 1] = p;
+      p = z[i - 1];
+      z[i - 1] = z[k - 1];
+      z[k - 1] = p;
     }
   }
   return;
@@ -760,52 +704,47 @@ void CGaussJacobiQuadrature::parchk(int kind, int m, passivedouble alpha, passiv
 {
   passivedouble tmp;
 
-  if ( kind <= 0 )
-  {
+  if (kind <= 0) {
     cout << "\n";
     cout << "PARCHK - Fatal error!\n";
     cout << "  KIND <= 0.\n";
-    exit ( 1 );
+    exit(1);
   }
-//
-//  Check ALPHA for Gegenbauer, Jacobi, Laguerre, Hermite, Exponential.
-//
-  if ( 3 <= kind && alpha <= -1.0 )
-  {
+  //
+  //  Check ALPHA for Gegenbauer, Jacobi, Laguerre, Hermite, Exponential.
+  //
+  if (3 <= kind && alpha <= -1.0) {
     cout << "\n";
     cout << "PARCHK - Fatal error!\n";
     cout << "  3 <= KIND and ALPHA <= -1.\n";
-    exit ( 1 );
+    exit(1);
   }
-//
-//  Check BETA for Jacobi.
-//
-  if ( kind == 4 && beta <= -1.0 )
-  {
+  //
+  //  Check BETA for Jacobi.
+  //
+  if (kind == 4 && beta <= -1.0) {
     cout << "\n";
     cout << "PARCHK - Fatal error!\n";
     cout << "  KIND == 4 and BETA <= -1.0.\n";
-    exit ( 1 );
+    exit(1);
   }
-//
-//  Check ALPHA and BETA for rational.
-//
-  if ( kind == 8 )
-  {
+  //
+  //  Check ALPHA and BETA for rational.
+  //
+  if (kind == 8) {
     tmp = alpha + beta + m + 1.0;
-    if ( 0.0 <= tmp || tmp <= beta )
-    {
+    if (0.0 <= tmp || tmp <= beta) {
       cout << "\n";
       cout << "PARCHK - Fatal error!\n";
       cout << "  KIND == 8 but condition on ALPHA and BETA fails.\n";
-      exit ( 1 );
+      exit(1);
     }
   }
   return;
 }
 //****************************************************************************80
 
-passivedouble CGaussJacobiQuadrature::r8_epsilon( )
+passivedouble CGaussJacobiQuadrature::r8_epsilon()
 
 //****************************************************************************80
 //
@@ -873,22 +812,18 @@ passivedouble CGaussJacobiQuadrature::r8_sign(passivedouble x)
 {
   passivedouble value;
 
-  if ( x < 0.0 )
-  {
+  if (x < 0.0) {
     value = -1.0;
-  }
-  else
-  {
+  } else {
     value = 1.0;
   }
   return value;
 }
 //****************************************************************************80
 
-void CGaussJacobiQuadrature::scqf(int nt, const passivedouble t[], const int mlt[], const passivedouble wts[],
-                                  int nwts, int ndx[], passivedouble swts[], passivedouble st[],
-                                  int kind, passivedouble alpha, passivedouble beta, passivedouble a,
-                                  passivedouble b)
+void CGaussJacobiQuadrature::scqf(int nt, const passivedouble t[], const int mlt[], const passivedouble wts[], int nwts,
+                                  int ndx[], passivedouble swts[], passivedouble st[], int kind, passivedouble alpha,
+                                  passivedouble beta, passivedouble a, passivedouble b)
 
 //****************************************************************************80
 //
@@ -971,150 +906,122 @@ void CGaussJacobiQuadrature::scqf(int nt, const passivedouble t[], const int mlt
   passivedouble temp;
   passivedouble tmp;
 
-  temp = r8_epsilon ( );
+  temp = r8_epsilon();
 
-  parchk ( kind, 1, alpha, beta );
+  parchk(kind, 1, alpha, beta);
 
-  if ( kind == 1 )
-  {
+  if (kind == 1) {
     al = 0.0;
     be = 0.0;
-    if ( fabs ( b - a ) <= temp )
-    {
+    if (fabs(b - a) <= temp) {
       cout << "\n";
       cout << "SCQF - Fatal error!\n";
       cout << "  |B - A| too small.\n";
-      exit ( 1 );
+      exit(1);
     }
-    shft = ( a + b ) / 2.0;
-    slp = ( b - a ) / 2.0;
-  }
-  else if ( kind == 2 )
-  {
+    shft = (a + b) / 2.0;
+    slp = (b - a) / 2.0;
+  } else if (kind == 2) {
     al = -0.5;
     be = -0.5;
-    if ( fabs ( b - a ) <= temp )
-    {
+    if (fabs(b - a) <= temp) {
       cout << "\n";
       cout << "SCQF - Fatal error!\n";
       cout << "  |B - A| too small.\n";
-      exit ( 1 );
+      exit(1);
     }
-    shft = ( a + b ) / 2.0;
-    slp = ( b - a ) / 2.0;
-  }
-  else if ( kind == 3 )
-  {
+    shft = (a + b) / 2.0;
+    slp = (b - a) / 2.0;
+  } else if (kind == 3) {
     al = alpha;
     be = alpha;
-    if ( fabs ( b - a ) <= temp )
-    {
+    if (fabs(b - a) <= temp) {
       cout << "\n";
       cout << "SCQF - Fatal error!\n";
       cout << "  |B - A| too small.\n";
-      exit ( 1 );
+      exit(1);
     }
-    shft = ( a + b ) / 2.0;
-    slp = ( b - a ) / 2.0;
-  }
-  else if ( kind == 4 )
-  {
+    shft = (a + b) / 2.0;
+    slp = (b - a) / 2.0;
+  } else if (kind == 4) {
     al = alpha;
     be = beta;
 
-    if ( fabs ( b - a ) <= temp )
-    {
+    if (fabs(b - a) <= temp) {
       cout << "\n";
       cout << "SCQF - Fatal error!\n";
       cout << "  |B - A| too small.\n";
-      exit ( 1 );
+      exit(1);
     }
-    shft = ( a + b ) / 2.0;
-    slp = ( b - a ) / 2.0;
-  }
-  else if ( kind == 5 )
-  {
-    if ( b <= 0.0 )
-    {
+    shft = (a + b) / 2.0;
+    slp = (b - a) / 2.0;
+  } else if (kind == 5) {
+    if (b <= 0.0) {
       cout << "\n";
       cout << "SCQF - Fatal error!\n";
       cout << "  B <= 0\n";
-      exit ( 1 );
+      exit(1);
     }
     shft = a;
     slp = 1.0 / b;
     al = alpha;
     be = 0.0;
-  }
-  else if ( kind == 6 )
-  {
-    if ( b <= 0.0 )
-    {
+  } else if (kind == 6) {
+    if (b <= 0.0) {
       cout << "\n";
       cout << "SCQF - Fatal error!\n";
       cout << "  B <= 0.\n";
-      exit ( 1 );
+      exit(1);
     }
     shft = a;
-    slp = 1.0 / sqrt ( b );
+    slp = 1.0 / sqrt(b);
     al = alpha;
     be = 0.0;
-  }
-  else if ( kind == 7 )
-  {
+  } else if (kind == 7) {
     al = alpha;
     be = 0.0;
-    if ( fabs ( b - a ) <= temp )
-    {
+    if (fabs(b - a) <= temp) {
       cout << "\n";
       cout << "SCQF - Fatal error!\n";
       cout << "  |B - A| too small.\n";
-      exit ( 1 );
+      exit(1);
     }
-    shft = ( a + b ) / 2.0;
-    slp = ( b - a ) / 2.0;
-  }
-  else if ( kind == 8 )
-  {
-    if ( a + b <= 0.0 )
-    {
+    shft = (a + b) / 2.0;
+    slp = (b - a) / 2.0;
+  } else if (kind == 8) {
+    if (a + b <= 0.0) {
       cout << "\n";
       cout << "SCQF - Fatal error!\n";
       cout << "  A + B <= 0.\n";
-      exit ( 1 );
+      exit(1);
     }
     shft = a;
     slp = a + b;
     al = alpha;
     be = beta;
-  }
-  else  // if ( kind == 9 )
+  } else  // if ( kind == 9 )
   {
     al = 0.5;
     be = 0.5;
-    if ( fabs ( b - a ) <= temp )
-    {
+    if (fabs(b - a) <= temp) {
       cout << "\n";
       cout << "SCQF - Fatal error!\n";
       cout << "  |B - A| too small.\n";
-      exit ( 1 );
+      exit(1);
     }
-    shft = ( a + b ) / 2.0;
-    slp = ( b - a ) / 2.0;
+    shft = (a + b) / 2.0;
+    slp = (b - a) / 2.0;
   }
 
-  p = pow ( slp, al + be + 1.0 );
+  p = pow(slp, al + be + 1.0);
 
-  for ( k = 0; k < nt; k++ )
-  {
+  for (k = 0; k < nt; k++) {
     st[k] = shft + slp * t[k];
-    l = abs ( ndx[k] );
+    l = abs(ndx[k]);
 
-    if ( l != 0 )
-    {
+    if (l != 0) {
       tmp = p;
-      for ( i = l - 1; i <= l - 1 + mlt[k] - 1; i++ )
-      {
+      for (i = l - 1; i <= l - 1 + mlt[k] - 1; i++) {
         swts[i] = wts[i] * tmp;
         tmp = tmp * slp;
       }
@@ -1124,8 +1031,8 @@ void CGaussJacobiQuadrature::scqf(int nt, const passivedouble t[], const int mlt
 }
 //****************************************************************************80
 
-void CGaussJacobiQuadrature::sgqf(int nt, const passivedouble aj[], passivedouble bj[],
-                                  passivedouble zemu, passivedouble t[], passivedouble wts[])
+void CGaussJacobiQuadrature::sgqf(int nt, const passivedouble aj[], passivedouble bj[], passivedouble zemu,
+                                  passivedouble t[], passivedouble wts[])
 
 //****************************************************************************80
 //
@@ -1177,35 +1084,31 @@ void CGaussJacobiQuadrature::sgqf(int nt, const passivedouble aj[], passivedoubl
 //
 {
   int i;
-//
-//  Exit if the zero-th moment is not positive.
-//
-  if ( zemu <= 0.0 )
-  {
+  //
+  //  Exit if the zero-th moment is not positive.
+  //
+  if (zemu <= 0.0) {
     cout << "\n";
     cout << "SGQF - Fatal error!\n";
     cout << "  ZEMU <= 0.\n";
-    exit ( 1 );
+    exit(1);
   }
-//
-//  Set up vectors for IMTQLX.
-//
-  for ( i = 0; i < nt; i++ )
-  {
+  //
+  //  Set up vectors for IMTQLX.
+  //
+  for (i = 0; i < nt; i++) {
     t[i] = aj[i];
   }
-  wts[0] = sqrt ( zemu );
-  for ( i = 1; i < nt; i++ )
-  {
+  wts[0] = sqrt(zemu);
+  for (i = 1; i < nt; i++) {
     wts[i] = 0.0;
   }
-//
-//  Diagonalize the Jacobi matrix.
-//
-  imtqlx ( nt, t, bj, wts );
+  //
+  //  Diagonalize the Jacobi matrix.
+  //
+  imtqlx(nt, t, bj, wts);
 
-  for ( i = 0; i < nt; i++ )
-  {
+  for (i = 0; i < nt; i++) {
     wts[i] = wts[i] * wts[i];
   }
 
diff --git a/Common/src/fem/fem_geometry_structure.cpp b/Common/src/fem/fem_geometry_structure.cpp
index b274989268c..375f7fefd39 100644
--- a/Common/src/fem/fem_geometry_structure.cpp
+++ b/Common/src/fem/fem_geometry_structure.cpp
@@ -32,30 +32,26 @@
 #include "../../include/adt/CADTPointsOnlyClass.hpp"
 
 /* Prototypes for Lapack functions, if MKL or LAPACK is used. */
-#if defined (HAVE_MKL) || defined(HAVE_LAPACK)
-extern "C" void dpotrf_(char *, int*, passivedouble*, int*, int*);
-extern "C" void dpotri_(char *, int*, passivedouble*, int*, int*);
+#if defined(HAVE_MKL) || defined(HAVE_LAPACK)
+extern "C" void dpotrf_(char*, int*, passivedouble*, int*, int*);
+extern "C" void dpotri_(char*, int*, passivedouble*, int*, int*);
 #endif
 
-bool CLong3T::operator<(const CLong3T &other) const {
-  if(long0 != other.long0) return (long0 < other.long0);
-  if(long1 != other.long1) return (long1 < other.long1);
-  if(long2 != other.long2) return (long2 < other.long2);
+bool CLong3T::operator<(const CLong3T& other) const {
+  if (long0 != other.long0) return (long0 < other.long0);
+  if (long1 != other.long1) return (long1 < other.long1);
+  if (long2 != other.long2) return (long2 < other.long2);
 
   return false;
 }
 
-CReorderElements::CReorderElements(const unsigned long  val_GlobalElemID,
-                                   const unsigned short val_TimeLevel,
-                                   const bool           val_CommSolution,
-                                   const unsigned short val_VTK_Type,
-                                   const unsigned short val_nPolySol,
-                                   const bool           val_JacConstant) {
-
+CReorderElements::CReorderElements(const unsigned long val_GlobalElemID, const unsigned short val_TimeLevel,
+                                   const bool val_CommSolution, const unsigned short val_VTK_Type,
+                                   const unsigned short val_nPolySol, const bool val_JacConstant) {
   /* Copy the global elment ID, time level and whether or not this element
      must be communicated. */
   globalElemID = val_GlobalElemID;
-  timeLevel    = val_TimeLevel;
+  timeLevel = val_TimeLevel;
   commSolution = val_CommSolution;
 
   /* Create the element type used in this class, which stores information of
@@ -63,38 +59,34 @@ CReorderElements::CReorderElements(const unsigned long  val_GlobalElemID,
      Jacobian of the transformation is constant. As it is possible that the
      polynomial degree of the solution is zero, this convention is different
      from the convention used in the SU2 grid file. */
-  elemType = val_VTK_Type + 100*val_nPolySol;
-  if( !val_JacConstant ) elemType += 50;
+  elemType = val_VTK_Type + 100 * val_nPolySol;
+  if (!val_JacConstant) elemType += 50;
 }
 
-bool CReorderElements::operator< (const CReorderElements &other) const {
-
+bool CReorderElements::operator<(const CReorderElements& other) const {
   /* Elements with the lowest time level are stored first. */
-  if(timeLevel != other.timeLevel) return timeLevel < other.timeLevel;
+  if (timeLevel != other.timeLevel) return timeLevel < other.timeLevel;
 
   /* Next comparison is whether or not the element must communicate its
      solution data to other ranks. Elements which do not need to do this
      are stored first. */
-  if(commSolution != other.commSolution) return other.commSolution;
+  if (commSolution != other.commSolution) return other.commSolution;
 
   /* Elements of the same element type must be stored as contiguously as
      possible to allow for the simultaneous treatment of elements in the
      matrix multiplications. */
-  if(elemType != other.elemType) return elemType < other.elemType;
+  if (elemType != other.elemType) return elemType < other.elemType;
 
   /* The final comparison is based on the global element ID. */
   return globalElemID < other.globalElemID;
 }
 
-bool CSortFaces::operator()(const CFaceOfElement &f0,
-                            const CFaceOfElement &f1) {
-
+bool CSortFaces::operator()(const CFaceOfElement& f0, const CFaceOfElement& f1) {
   /*--- Comparison in case both faces are boundary faces. ---*/
-  if(f0.faceIndicator >= 0 && f1.faceIndicator >= 0) {
-
+  if (f0.faceIndicator >= 0 && f1.faceIndicator >= 0) {
     /* Both faces are boundary faces. The first comparison is the boundary
        marker, which is stored in faceIndicator. */
-    if(f0.faceIndicator != f1.faceIndicator) return f0.faceIndicator < f1.faceIndicator;
+    if (f0.faceIndicator != f1.faceIndicator) return f0.faceIndicator < f1.faceIndicator;
 
     /* Both faces belong to the same boundary marker. The second comparison is
        based on the on the local volume ID's of the adjacent elements. As the
@@ -107,8 +99,7 @@ bool CSortFaces::operator()(const CFaceOfElement &f0,
   }
 
   /*--- Comparison in case both faces are internal faces. ---*/
-  if(f0.faceIndicator == -1 && f1.faceIndicator == -1) {
-
+  if (f0.faceIndicator == -1 && f1.faceIndicator == -1) {
     /* Both faces are internal faces. First determine the minimum and maximum
        ID of its adjacent elements.  */
     unsigned long elemIDMin0 = min(f0.elemID0, f0.elemID1);
@@ -118,8 +109,7 @@ bool CSortFaces::operator()(const CFaceOfElement &f0,
     unsigned long elemIDMax1 = max(f1.elemID0, f1.elemID1);
 
     /* Determine the situation. */
-    if(elemIDMax0 < nVolElemTot && elemIDMax1 < nVolElemTot) {
-
+    if (elemIDMax0 < nVolElemTot && elemIDMax1 < nVolElemTot) {
       /* Both faces are matching internal faces. Determine whether or not these
          faces are local faces, i.e. faces between locally owned elements. */
       const bool face0IsLocal = elemIDMax0 < nVolElemOwned;
@@ -127,45 +117,38 @@ bool CSortFaces::operator()(const CFaceOfElement &f0,
 
       /* Check if both faces have the same status, i.e. either local or
          not local. */
-      if(face0IsLocal == face1IsLocal) {
-
+      if (face0IsLocal == face1IsLocal) {
         /* Both faces are either local or not local. Determine the time level
            of the faces, which is the minimum value of the adjacent volume
            elements. */
-        const unsigned short timeLevel0 = min(volElem[elemIDMin0].timeLevel,
-                                              volElem[elemIDMax0].timeLevel);
-        const unsigned short timeLevel1 = min(volElem[elemIDMin1].timeLevel,
-                                              volElem[elemIDMax1].timeLevel);
+        const unsigned short timeLevel0 = min(volElem[elemIDMin0].timeLevel, volElem[elemIDMax0].timeLevel);
+        const unsigned short timeLevel1 = min(volElem[elemIDMin1].timeLevel, volElem[elemIDMax1].timeLevel);
 
         /* Internal faces with the same status are first sorted according to
            their time level. Faces with the smallest time level are numbered
            first. Note this is only relevant for time accurate local time
            stepping. */
-        if(timeLevel0 != timeLevel1) return timeLevel0 < timeLevel1;
+        if (timeLevel0 != timeLevel1) return timeLevel0 < timeLevel1;
 
         /* The faces belong to the same time level. They are sorted according
            to their element ID's in order to increase cache performance. */
-        if(elemIDMin0 != elemIDMin1) return elemIDMin0 < elemIDMin1;
+        if (elemIDMin0 != elemIDMin1) return elemIDMin0 < elemIDMin1;
         return elemIDMax0 < elemIDMax1;
-      }
-      else {
-
+      } else {
         /* One face is a local face and the other is not. Make sure that
            the local faces are numbered first. */
-        if( face0IsLocal ) return true;
-        else               return false;
+        if (face0IsLocal)
+          return true;
+        else
+          return false;
       }
-    }
-    else if(elemIDMax0 >= nVolElemTot && elemIDMax1 >= nVolElemTot) {
-
+    } else if (elemIDMax0 >= nVolElemTot && elemIDMax1 >= nVolElemTot) {
       /* Both faces are non-matching internal faces. Sort them according to
          their relevant element ID. The time level is not taken into account
          yet, because non-matching faces are not possible at the moment with
          time accurate local time stepping. */
       return elemIDMin0 < elemIDMin1;
-    }
-    else {
-
+    } else {
       /* One face is a matching internal face and the other face is a
          non-matching internal face. Make sure that the non-matching face
          is numbered after the matching face. This is accomplished by comparing
@@ -180,84 +163,70 @@ bool CSortFaces::operator()(const CFaceOfElement &f0,
   return f0.faceIndicator > f1.faceIndicator;
 }
 
-bool CSortBoundaryFaces::operator()(const CSurfaceElementFEM &f0,
-                                    const CSurfaceElementFEM &f1) {
-
+bool CSortBoundaryFaces::operator()(const CSurfaceElementFEM& f0, const CSurfaceElementFEM& f1) {
   /* First sorting criterion is the index of the standard element. The
      boundary faces should be sorted per standard element. Note that the
      time level is not taken into account here, because it is assumed that
      the surface elements to be sorted belong to one time level. */
-  if(f0.indStandardElement != f1.indStandardElement)
-    return f0.indStandardElement < f1.indStandardElement;
+  if (f0.indStandardElement != f1.indStandardElement) return f0.indStandardElement < f1.indStandardElement;
 
   /* The standard elements are the same. The second criterion is the
      corresponding volume IDs of the surface elements. */
   return f0.volElemID < f1.volElemID;
 }
 
-bool CPointFEM::operator< (const CPointFEM &other) const {
-  if(periodIndexToDonor != other.periodIndexToDonor)
-    return periodIndexToDonor < other.periodIndexToDonor;
+bool CPointFEM::operator<(const CPointFEM& other) const {
+  if (periodIndexToDonor != other.periodIndexToDonor) return periodIndexToDonor < other.periodIndexToDonor;
   return globalID < other.globalID;
- }
-
-bool CPointFEM::operator==(const CPointFEM &other) const {
- return (globalID           == other.globalID &&
-         periodIndexToDonor == other.periodIndexToDonor);
 }
 
-void CVolumeElementFEM::GetCornerPointsAllFaces(unsigned short &numFaces,
-                                                unsigned short nPointsPerFace[],
-                                                unsigned long  faceConn[6][4]) {
+bool CPointFEM::operator==(const CPointFEM& other) const {
+  return (globalID == other.globalID && periodIndexToDonor == other.periodIndexToDonor);
+}
 
+void CVolumeElementFEM::GetCornerPointsAllFaces(unsigned short& numFaces, unsigned short nPointsPerFace[],
+                                                unsigned long faceConn[6][4]) {
   /*--- Get the corner connectivities of the faces, local to the element. ---*/
-  CPrimalGridFEM::GetLocalCornerPointsAllFaces(VTK_Type, nPolyGrid, nDOFsGrid,
-                                               numFaces, nPointsPerFace, faceConn);
+  CPrimalGridFEM::GetLocalCornerPointsAllFaces(VTK_Type, nPolyGrid, nDOFsGrid, numFaces, nPointsPerFace, faceConn);
 
   /*--- Convert the local values of faceConn to global values. ---*/
-  for(unsigned short i=0; i<numFaces; ++i) {
-    for(unsigned short j=0; j<nPointsPerFace[i]; ++j) {
+  for (unsigned short i = 0; i < numFaces; ++i) {
+    for (unsigned short j = 0; j < nPointsPerFace[i]; ++j) {
       unsigned long nn = faceConn[i][j];
       faceConn[i][j] = nodeIDsGrid[nn];
     }
   }
 }
 
-bool CInternalFaceElementFEM::operator<(const CInternalFaceElementFEM &other) const {
-
+bool CInternalFaceElementFEM::operator<(const CInternalFaceElementFEM& other) const {
   /* First comparison is the standard element, such that elements with
      the same same standard elements are grouped together. */
-  if(indStandardElement != other.indStandardElement)
-    return indStandardElement < other.indStandardElement;
+  if (indStandardElement != other.indStandardElement) return indStandardElement < other.indStandardElement;
 
   /* The second comparison is the element ID on side 0. */
-  if(elemID0 != other.elemID0) return elemID0 < other.elemID0;
+  if (elemID0 != other.elemID0) return elemID0 < other.elemID0;
 
   /* The final comparison is the element ID on side 1. */
   return elemID1 < other.elemID1;
 }
 
-void CSurfaceElementFEM::GetCornerPointsFace(unsigned short &nPointsPerFace,
-                                             unsigned long  faceConn[]) {
-
+void CSurfaceElementFEM::GetCornerPointsFace(unsigned short& nPointsPerFace, unsigned long faceConn[]) {
   /*--- Get the corner connectivities of the face, local to the element. ---*/
-  CPrimalGridBoundFEM::GetLocalCornerPointsFace(VTK_Type, nPolyGrid, nDOFsGrid,
-                                                nPointsPerFace, faceConn);
+  CPrimalGridBoundFEM::GetLocalCornerPointsFace(VTK_Type, nPolyGrid, nDOFsGrid, nPointsPerFace, faceConn);
 
   /*--- Convert the local values of faceConn to global values. ---*/
-  for(unsigned short j=0; j<nPointsPerFace; ++j) {
+  for (unsigned short j = 0; j < nPointsPerFace; ++j) {
     unsigned long nn = faceConn[j];
     faceConn[j] = nodeIDsGrid[nn];
   }
 }
 
-CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
-
+CMeshFEM::CMeshFEM(CGeometry* geometry, CConfig* config) {
   /*--- Allocate the memory for blasFunctions. ---*/
   blasFunctions = new CBlasStructure;
 
   /*--- The new FEM mesh class has the same problem dimension/zone. ---*/
-  nDim  = geometry->GetnDim();
+  nDim = geometry->GetnDim();
   nZone = geometry->GetnZone();
 
   /*--- Determine the number of variables stored per DOF.              ---*/
@@ -267,18 +236,19 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
   /*--- for this purpose.                                              ---*/
   MAIN_SOLVER Kind_Solver = config->GetKind_Solver();
   const bool compressible = (Kind_Solver == MAIN_SOLVER::FEM_EULER) ||
-                            (Kind_Solver == MAIN_SOLVER::FEM_NAVIER_STOKES) ||
-                            (Kind_Solver == MAIN_SOLVER::FEM_RANS) ||
+                            (Kind_Solver == MAIN_SOLVER::FEM_NAVIER_STOKES) || (Kind_Solver == MAIN_SOLVER::FEM_RANS) ||
                             (Kind_Solver == MAIN_SOLVER::FEM_LES);
 
   unsigned short nVar;
-  if( compressible ) nVar = nDim + 2;
-  else               nVar = nDim + 1;
+  if (compressible)
+    nVar = nDim + 2;
+  else
+    nVar = nDim + 1;
 
   /*--- Determine a mapping from the global point ID to the local index
         of the points.            ---*/
-  map<unsigned long,unsigned long> globalPointIDToLocalInd;
-  for(unsigned long i=0; i<geometry->GetnPoint(); ++i)
+  map<unsigned long, unsigned long> globalPointIDToLocalInd;
+  for (unsigned long i = 0; i < geometry->GetnPoint(); ++i)
     globalPointIDToLocalInd[geometry->nodes->GetGlobalIndex(i)] = i;
 
   /*----------------------------------------------------------------------------*/
@@ -289,13 +259,13 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
   /*--- Determine the ranks to which I have to send my elements. ---*/
   vector<int> sendToRank(size, 0);
 
-  for(unsigned long i=0; i<geometry->GetnElem(); ++i) {
+  for (unsigned long i = 0; i < geometry->GetnElem(); ++i) {
     sendToRank[geometry->elem[i]->GetColor()] = 1;
   }
 
-  map<int,int> rankToIndCommBuf;
-  for(int i=0; i<size; ++i) {
-    if( sendToRank[i] ) {
+  map<int, int> rankToIndCommBuf;
+  for (int i = 0; i < size; ++i) {
+    if (sendToRank[i]) {
       int ind = (int)rankToIndCommBuf.size();
       rankToIndCommBuf[i] = ind;
     }
@@ -304,13 +274,13 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
   /*--- Definition of the communication buffers, used to send the element data
         to the correct ranks.                ---*/
   int nRankSend = (int)rankToIndCommBuf.size();
-  vector<vector<short> >     shortSendBuf(nRankSend,  vector<short>(0));
-  vector<vector<long>  >     longSendBuf(nRankSend,   vector<long>(0));
+  vector<vector<short> > shortSendBuf(nRankSend, vector<short>(0));
+  vector<vector<long> > longSendBuf(nRankSend, vector<long>(0));
   vector<vector<su2double> > doubleSendBuf(nRankSend, vector<su2double>(0));
 
   /*--- The first element of longSendBuf will contain the number of elements, which
         are stored in the communication buffers. Initialize this value to 0. ---*/
-  for(int i=0; i<nRankSend; ++i) longSendBuf[i].push_back(0);
+  for (int i = 0; i < nRankSend; ++i) longSendBuf[i].push_back(0);
 
   /*--- Determine the number of ranks, from which this rank will receive elements. ---*/
   int nRankRecv = nRankSend;
@@ -318,17 +288,16 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
 #ifdef HAVE_MPI
   vector<int> sizeRecv(size, 1);
 
-  SU2_MPI::Reduce_scatter(sendToRank.data(), &nRankRecv, sizeRecv.data(),
-                          MPI_INT, MPI_SUM, SU2_MPI::GetComm());
+  SU2_MPI::Reduce_scatter(sendToRank.data(), &nRankRecv, sizeRecv.data(), MPI_INT, MPI_SUM, SU2_MPI::GetComm());
 #endif
 
   /*--- Loop over the local elements to fill the communication buffers with element data. ---*/
-  for(unsigned long i=0; i<geometry->GetnElem(); ++i) {
+  for (unsigned long i = 0; i < geometry->GetnElem(); ++i) {
     int ind = (int)geometry->elem[i]->GetColor();
-    map<int,int>::const_iterator MI = rankToIndCommBuf.find(ind);
+    map<int, int>::const_iterator MI = rankToIndCommBuf.find(ind);
     ind = MI->second;
 
-    ++longSendBuf[ind][0];   /* The number of elements in the buffers must be incremented. */
+    ++longSendBuf[ind][0]; /* The number of elements in the buffers must be incremented. */
 
     shortSendBuf[ind].push_back(geometry->elem[i]->GetVTK_Type());
     shortSendBuf[ind].push_back(geometry->elem[i]->GetNPolyGrid());
@@ -337,21 +306,21 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
     shortSendBuf[ind].push_back(geometry->elem[i]->GetNDOFsSol());
     shortSendBuf[ind].push_back(geometry->elem[i]->GetnFaces());
     shortSendBuf[ind].push_back(geometry->elem[i]->GetTimeLevel());
-    shortSendBuf[ind].push_back( (short) geometry->elem[i]->GetJacobianConsideredConstant());
+    shortSendBuf[ind].push_back((short)geometry->elem[i]->GetJacobianConsideredConstant());
 
     longSendBuf[ind].push_back(geometry->elem[i]->GetGlobalElemID());
     longSendBuf[ind].push_back(geometry->elem[i]->GetGlobalOffsetDOFsSol());
 
-    for(unsigned short j=0; j<geometry->elem[i]->GetNDOFsGrid(); ++j)
+    for (unsigned short j = 0; j < geometry->elem[i]->GetNDOFsGrid(); ++j)
       longSendBuf[ind].push_back(geometry->elem[i]->GetNode(j));
 
-    for(unsigned short j=0; j<geometry->elem[i]->GetnFaces(); ++j)
+    for (unsigned short j = 0; j < geometry->elem[i]->GetnFaces(); ++j)
       longSendBuf[ind].push_back(geometry->elem[i]->GetNeighbor_Elements(j));
 
-    for(unsigned short j=0; j<geometry->elem[i]->GetnFaces(); ++j) {
+    for (unsigned short j = 0; j < geometry->elem[i]->GetnFaces(); ++j) {
       shortSendBuf[ind].push_back(geometry->elem[i]->GetPeriodicIndex(j));
-      shortSendBuf[ind].push_back( (short) geometry->elem[i]->GetJacobianConstantFace(j));
-      shortSendBuf[ind].push_back( (short) geometry->elem[i]->GetOwnerFace(j));
+      shortSendBuf[ind].push_back((short)geometry->elem[i]->GetJacobianConstantFace(j));
+      shortSendBuf[ind].push_back((short)geometry->elem[i]->GetOwnerFace(j));
     }
 
     doubleSendBuf[ind].push_back(geometry->elem[i]->GetLengthScale());
@@ -359,21 +328,19 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
 
   /*--- Determine for each rank to which I have to send elements the data of
         the corresponding nodes.   ---*/
-  for(int i=0; i<nRankSend; ++i) {
-
+  for (int i = 0; i < nRankSend; ++i) {
     /*--- Determine the vector with node IDs in the connectivity
           of the elements for this rank.   ---*/
     vector<long> nodeIDs;
 
     unsigned long indL = 3;
     unsigned long indS = 3;
-    for(long j=0; j<longSendBuf[i][0]; ++j) {
-      short nDOFsGrid = shortSendBuf[i][indS], nFaces = shortSendBuf[i][indS+2];
-      indS += 3*nFaces+8;
+    for (long j = 0; j < longSendBuf[i][0]; ++j) {
+      short nDOFsGrid = shortSendBuf[i][indS], nFaces = shortSendBuf[i][indS + 2];
+      indS += 3 * nFaces + 8;
 
-      for(short k=0; k<nDOFsGrid; ++k, ++indL)
-        nodeIDs.push_back(longSendBuf[i][indL]);
-      indL += nFaces+2;
+      for (short k = 0; k < nDOFsGrid; ++k, ++indL) nodeIDs.push_back(longSendBuf[i][indL]);
+      indL += nFaces + 2;
     }
 
     /*--- Sort nodeIDs in increasing order and remove the double entities. ---*/
@@ -386,50 +353,45 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
     longSendBuf[i].insert(longSendBuf[i].end(), nodeIDs.begin(), nodeIDs.end());
 
     /*--- Copy the coordinates to doubleSendBuf. ---*/
-    for(unsigned long j=0; j<nodeIDs.size(); ++j) {
-      map<unsigned long,unsigned long>::const_iterator LMI;
+    for (unsigned long j = 0; j < nodeIDs.size(); ++j) {
+      map<unsigned long, unsigned long>::const_iterator LMI;
       LMI = globalPointIDToLocalInd.find(nodeIDs[j]);
 
-      if(LMI == globalPointIDToLocalInd.end())
-        SU2_MPI::Error("Entry not found in map", CURRENT_FUNCTION);
+      if (LMI == globalPointIDToLocalInd.end()) SU2_MPI::Error("Entry not found in map", CURRENT_FUNCTION);
 
       unsigned long ind = LMI->second;
-      for(unsigned short l=0; l<nDim; ++l)
-        doubleSendBuf[i].push_back(geometry->nodes->GetCoord(ind, l));
+      for (unsigned short l = 0; l < nDim; ++l) doubleSendBuf[i].push_back(geometry->nodes->GetCoord(ind, l));
     }
   }
 
   /*--- Loop over the boundaries to send the boundary data to the appropriate rank. ---*/
   nMarker = geometry->GetnMarker();
-  for(unsigned short iMarker=0; iMarker<nMarker; ++iMarker) {
-
+  for (unsigned short iMarker = 0; iMarker < nMarker; ++iMarker) {
     /* Store the current indices in the longSendBuf, which are used to store the
        number of boundary elements sent to this rank. Initialize this value to 0. */
     vector<long> indLongBuf(nRankSend);
-    for(int i=0; i<nRankSend; ++i) {
+    for (int i = 0; i < nRankSend; ++i) {
       indLongBuf[i] = longSendBuf[i].size();
       longSendBuf[i].push_back(0);
     }
 
     /* Loop over the local boundary elements in geometry for this marker. */
-    for(unsigned long i=0; i<geometry->GetnElem_Bound(iMarker); ++i) {
-
+    for (unsigned long i = 0; i < geometry->GetnElem_Bound(iMarker); ++i) {
       /* Determine the local ID of the corresponding domain element. */
-      unsigned long elemID = geometry->bound[iMarker][i]->GetDomainElement()
-                           - geometry->beg_node[rank];
+      unsigned long elemID = geometry->bound[iMarker][i]->GetDomainElement() - geometry->beg_node[rank];
 
       /* Determine to which rank this boundary element must be sent.
          That is the same as its corresponding domain element.
          Update the corresponding index in longSendBuf. */
       int ind = (int)geometry->elem[elemID]->GetColor();
-      map<int,int>::const_iterator MI = rankToIndCommBuf.find(ind);
+      map<int, int>::const_iterator MI = rankToIndCommBuf.find(ind);
       ind = MI->second;
 
       ++longSendBuf[ind][indLongBuf[ind]];
 
       /* Get the donor information for the wall function treatment. */
       const unsigned short nDonors = geometry->bound[iMarker][i]->GetNDonorsWallFunctions();
-      const unsigned long  *donors = geometry->bound[iMarker][i]->GetDonorsWallFunctions();
+      const unsigned long* donors = geometry->bound[iMarker][i]->GetDonorsWallFunctions();
 
       /* Store the data for this boundary element in the communication buffers. */
       shortSendBuf[ind].push_back(geometry->bound[iMarker][i]->GetVTK_Type());
@@ -440,44 +402,41 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
       longSendBuf[ind].push_back(geometry->bound[iMarker][i]->GetDomainElement());
       longSendBuf[ind].push_back(geometry->bound[iMarker][i]->GetGlobalElemID());
 
-      for(unsigned short j=0; j<geometry->bound[iMarker][i]->GetNDOFsGrid(); ++j)
+      for (unsigned short j = 0; j < geometry->bound[iMarker][i]->GetNDOFsGrid(); ++j)
         longSendBuf[ind].push_back(geometry->bound[iMarker][i]->GetNode(j));
 
-      for(unsigned short j=0; j<nDonors; ++j)
-        longSendBuf[ind].push_back(donors[j]);
+      for (unsigned short j = 0; j < nDonors; ++j) longSendBuf[ind].push_back(donors[j]);
     }
   }
 
   /*--- Definition of the communication buffers, used to receive
         the element data from the other correct ranks.        ---*/
-  vector<vector<short> >     shortRecvBuf(nRankRecv,  vector<short>(0));
-  vector<vector<long>  >     longRecvBuf(nRankRecv,   vector<long>(0));
+  vector<vector<short> > shortRecvBuf(nRankRecv, vector<short>(0));
+  vector<vector<long> > longRecvBuf(nRankRecv, vector<long>(0));
   vector<vector<su2double> > doubleRecvBuf(nRankRecv, vector<su2double>(0));
 
   /*--- Communicate the data to the correct ranks. Make a distinction
         between parallel and sequential mode.    ---*/
-  map<int,int>::const_iterator MI;
+  map<int, int>::const_iterator MI;
 
 #ifdef HAVE_MPI
 
   /*--- Parallel mode. Send all the data using non-blocking sends. ---*/
-  vector<SU2_MPI::Request> commReqs(3*nRankSend);
+  vector<SU2_MPI::Request> commReqs(3 * nRankSend);
   MI = rankToIndCommBuf.begin();
 
-  for(int i=0; i<nRankSend; ++i, ++MI) {
-
+  for (int i = 0; i < nRankSend; ++i, ++MI) {
     int dest = MI->first;
-    SU2_MPI::Isend(shortSendBuf[i].data(), shortSendBuf[i].size(), MPI_SHORT,
-                   dest, dest, SU2_MPI::GetComm(), &commReqs[3*i]);
-    SU2_MPI::Isend(longSendBuf[i].data(), longSendBuf[i].size(), MPI_LONG,
-                   dest, dest+1, SU2_MPI::GetComm(), &commReqs[3*i+1]);
-    SU2_MPI::Isend(doubleSendBuf[i].data(), doubleSendBuf[i].size(), MPI_DOUBLE,
-                   dest, dest+2, SU2_MPI::GetComm(), &commReqs[3*i+2]);
+    SU2_MPI::Isend(shortSendBuf[i].data(), shortSendBuf[i].size(), MPI_SHORT, dest, dest, SU2_MPI::GetComm(),
+                   &commReqs[3 * i]);
+    SU2_MPI::Isend(longSendBuf[i].data(), longSendBuf[i].size(), MPI_LONG, dest, dest + 1, SU2_MPI::GetComm(),
+                   &commReqs[3 * i + 1]);
+    SU2_MPI::Isend(doubleSendBuf[i].data(), doubleSendBuf[i].size(), MPI_DOUBLE, dest, dest + 2, SU2_MPI::GetComm(),
+                   &commReqs[3 * i + 2]);
   }
 
   /* Loop over the number of ranks from which I receive data. */
-  for(int i=0; i<nRankRecv; ++i) {
-
+  for (int i = 0; i < nRankRecv; ++i) {
     /* Block until a message with shorts arrives from any processor.
        Determine the source and the size of the message.   */
     SU2_MPI::Status status;
@@ -489,29 +448,26 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
 
     /* Allocate the memory for the short receive buffer and receive the message. */
     shortRecvBuf[i].resize(sizeMess);
-    SU2_MPI::Recv(shortRecvBuf[i].data(), sizeMess, MPI_SHORT,
-                  source, rank, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Recv(shortRecvBuf[i].data(), sizeMess, MPI_SHORT, source, rank, SU2_MPI::GetComm(), &status);
 
     /* Block until the corresponding message with longs arrives, determine
        its size, allocate the memory and receive the message. */
-    SU2_MPI::Probe(source, rank+1, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Probe(source, rank + 1, SU2_MPI::GetComm(), &status);
     SU2_MPI::Get_count(&status, MPI_LONG, &sizeMess);
     longRecvBuf[i].resize(sizeMess);
 
-    SU2_MPI::Recv(longRecvBuf[i].data(), sizeMess, MPI_LONG,
-                  source, rank+1, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Recv(longRecvBuf[i].data(), sizeMess, MPI_LONG, source, rank + 1, SU2_MPI::GetComm(), &status);
 
     /* Idem for the message with doubles. */
-    SU2_MPI::Probe(source, rank+2, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Probe(source, rank + 2, SU2_MPI::GetComm(), &status);
     SU2_MPI::Get_count(&status, MPI_DOUBLE, &sizeMess);
     doubleRecvBuf[i].resize(sizeMess);
 
-    SU2_MPI::Recv(doubleRecvBuf[i].data(), sizeMess, MPI_DOUBLE,
-                  source, rank+2, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Recv(doubleRecvBuf[i].data(), sizeMess, MPI_DOUBLE, source, rank + 2, SU2_MPI::GetComm(), &status);
   }
 
   /* Complete the non-blocking sends. */
-  SU2_MPI::Waitall(3*nRankSend, commReqs.data(), MPI_STATUSES_IGNORE);
+  SU2_MPI::Waitall(3 * nRankSend, commReqs.data(), MPI_STATUSES_IGNORE);
 
   /* Wild cards have been used in the communication,
      so synchronize the ranks to avoid problems.    */
@@ -520,15 +476,15 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
 #else
 
   /*--- Sequential mode. Simply copy the buffers. ---*/
-  shortRecvBuf[0]  = shortSendBuf[0];
-  longRecvBuf[0]   = longSendBuf[0];
+  shortRecvBuf[0] = shortSendBuf[0];
+  longRecvBuf[0] = longSendBuf[0];
   doubleRecvBuf[0] = doubleSendBuf[0];
 
 #endif
 
   /*--- Release the memory of the send buffers. To make sure that all
         the memory is deleted, the swap function is used. ---*/
-  for(int i=0; i<nRankSend; ++i) {
+  for (int i = 0; i < nRankSend; ++i) {
     vector<short>().swap(shortSendBuf[i]);
     vector<long>().swap(longSendBuf[i]);
     vector<su2double>().swap(doubleSendBuf[i]);
@@ -537,41 +493,41 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
   /*--- Allocate the memory for the number of elements for every boundary
         marker and initialize them to zero.     ---*/
   nElem_Bound = new unsigned long[nMarker];
-  for(unsigned short i=0; i<nMarker; ++i)
-    nElem_Bound[i] = 0;
+  for (unsigned short i = 0; i < nMarker; ++i) nElem_Bound[i] = 0;
 
   /*--- Determine the global element ID's of the elements stored on this rank.
         Sort them in increasing order, such that an easy search can be done.
         In the same loop determine the upper bound for the local nodes (without
         halos) and the number of boundary elements for every marker. ---*/
   nElem = nPoint = 0;
-  for(int i=0; i<nRankRecv; ++i) nElem += longRecvBuf[i][0];
+  for (int i = 0; i < nRankRecv; ++i) nElem += longRecvBuf[i][0];
 
   vector<unsigned long> globalElemID;
   globalElemID.reserve(nElem);
 
-  for(int i=0; i<nRankRecv; ++i) {
+  for (int i = 0; i < nRankRecv; ++i) {
     unsigned long indL = 1, indS = 0;
-    for(long j=0; j<longRecvBuf[i][0]; ++j) {
+    for (long j = 0; j < longRecvBuf[i][0]; ++j) {
       globalElemID.push_back(longRecvBuf[i][indL]);
 
-      unsigned short nDOFsGrid = shortRecvBuf[i][indS+3];
-      unsigned short nFaces    = shortRecvBuf[i][indS+5];
-      indS += 3*nFaces + 8;
+      unsigned short nDOFsGrid = shortRecvBuf[i][indS + 3];
+      unsigned short nFaces = shortRecvBuf[i][indS + 5];
+      indS += 3 * nFaces + 8;
       indL += nDOFsGrid + nFaces + 2;
     }
 
     long nNodesThisRank = longRecvBuf[i][indL];
     nPoint += nNodesThisRank;
-    indL   += nNodesThisRank+1;
+    indL += nNodesThisRank + 1;
 
-    for(unsigned iMarker=0; iMarker<nMarker; ++iMarker) {
-      long nBoundElemThisRank = longRecvBuf[i][indL]; ++indL;
+    for (unsigned iMarker = 0; iMarker < nMarker; ++iMarker) {
+      long nBoundElemThisRank = longRecvBuf[i][indL];
+      ++indL;
       nElem_Bound[iMarker] += nBoundElemThisRank;
 
-      for(long j=0; j<nBoundElemThisRank; ++j) {
-        short nDOFsBoundElem      = shortRecvBuf[i][indS+2];
-        short nDonorsWallFunction = shortRecvBuf[i][indS+3];
+      for (long j = 0; j < nBoundElemThisRank; ++j) {
+        short nDOFsBoundElem = shortRecvBuf[i][indS + 2];
+        short nDonorsWallFunction = shortRecvBuf[i][indS + 3];
         indS += 4;
         indL += nDOFsBoundElem + nDonorsWallFunction + 2;
       }
@@ -587,32 +543,31 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
         is stored on this rank. Furthermore a vector of CReorderElements
         is created for the owned elements to be able to reorder the elements,
         see step 2 below. ---*/
-  vector<CUnsignedLong2T>  haloElements;
+  vector<CUnsignedLong2T> haloElements;
   vector<CReorderElements> ownedElements;
   unsigned short maxTimeLevelLoc = 0;
 
-  for(int i=0; i<nRankRecv; ++i) {
+  for (int i = 0; i < nRankRecv; ++i) {
     unsigned long indL = 1, indS = 0;
-    for(long j=0; j<longRecvBuf[i][0]; ++j) {
-      unsigned long  globalID    = longRecvBuf[i][indL];
-      unsigned short VTK_Type    = shortRecvBuf[i][indS];
-      unsigned short nPolySol    = shortRecvBuf[i][indS+2];
-      unsigned short nDOFsGrid   = shortRecvBuf[i][indS+3];
-      unsigned short nFaces      = shortRecvBuf[i][indS+5];
-      unsigned short timeLevel   = shortRecvBuf[i][indS+6];
-      bool           JacConstant = (bool) shortRecvBuf[i][indS+7];
-      bool           commSol     = false;
+    for (long j = 0; j < longRecvBuf[i][0]; ++j) {
+      unsigned long globalID = longRecvBuf[i][indL];
+      unsigned short VTK_Type = shortRecvBuf[i][indS];
+      unsigned short nPolySol = shortRecvBuf[i][indS + 2];
+      unsigned short nDOFsGrid = shortRecvBuf[i][indS + 3];
+      unsigned short nFaces = shortRecvBuf[i][indS + 5];
+      unsigned short timeLevel = shortRecvBuf[i][indS + 6];
+      bool JacConstant = (bool)shortRecvBuf[i][indS + 7];
+      bool commSol = false;
 
       /* If the integration rule for constant and non-constant Jacobian
          elements is the same, simply set JacConstant to false, such that
          the elements with constant and non-constant Jacobians are
          considered the same. */
-      if( JacConstant ) {
+      if (JacConstant) {
         const unsigned short orderExactStraight =
-          (unsigned short) ceil(nPolySol*config->GetQuadrature_Factor_Straight());
-        const unsigned short orderExactCurved =
-          (unsigned short) ceil(nPolySol*config->GetQuadrature_Factor_Curved());
-        if(orderExactStraight == orderExactCurved) JacConstant = false;
+            (unsigned short)ceil(nPolySol * config->GetQuadrature_Factor_Straight());
+        const unsigned short orderExactCurved = (unsigned short)ceil(nPolySol * config->GetQuadrature_Factor_Curved());
+        if (orderExactStraight == orderExactCurved) JacConstant = false;
       }
 
       /* Update the local value of the maximum time level. */
@@ -622,32 +577,27 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
             and the information needed to reorder the owned elements. ---*/
       indS += 8;
       indL += nDOFsGrid + 2;
-      for(unsigned short k=0; k<nFaces; ++k, indS+=3, ++indL) {
-
-        if(longRecvBuf[i][indL] != -1) {  /* -1 indicates a boundary face. */
+      for (unsigned short k = 0; k < nFaces; ++k, indS += 3, ++indL) {
+        if (longRecvBuf[i][indL] != -1) { /* -1 indicates a boundary face. */
 
           /* Check if the neighbor of the face is also an owned element.
              Per definition an element for which a periodic transformation
              is carried out, is a halo element, even if the parent element
              is stored locally. */
           bool neighborIsInternal = false;
-          if(shortRecvBuf[i][indS] == -1) { /* -1 indicates no periodic transformation. */
-            neighborIsInternal = binary_search(globalElemID.begin(),
-                                               globalElemID.end(),
-                                               longRecvBuf[i][indL]);
+          if (shortRecvBuf[i][indS] == -1) { /* -1 indicates no periodic transformation. */
+            neighborIsInternal = binary_search(globalElemID.begin(), globalElemID.end(), longRecvBuf[i][indL]);
           }
 
           /* Check if this neighbor is not internal and if the element owns the face. */
-          if( !neighborIsInternal ) {
-            if( shortRecvBuf[i][indS+2] ) {
-
+          if (!neighborIsInternal) {
+            if (shortRecvBuf[i][indS + 2]) {
               /* The face is owned by this element. As the neighboring element
                  is not owned, this implies that a halo element must be created. */
-              haloElements.push_back(CUnsignedLong2T(longRecvBuf[i][indL],
-                                                     shortRecvBuf[i][indS]+1));  /* The +1, because haloElements */
-            }                                                                    /* are unsigned longs.          */
+              haloElements.push_back(
+                  CUnsignedLong2T(longRecvBuf[i][indL], shortRecvBuf[i][indS] + 1)); /* The +1, because haloElements */
+            }                                                                        /* are unsigned longs.          */
             else {
-
               /* The face is not owned by this element and therefore it is owned
                  by the neighboring element on a different rank. Consequently the
                  solution of this element must be communicated. */
@@ -658,32 +608,30 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
       }
 
       /* Store the required data for this element in ownedElements. */
-      ownedElements.push_back(CReorderElements(globalID, timeLevel, commSol,
-                                               VTK_Type, nPolySol, JacConstant));
+      ownedElements.push_back(CReorderElements(globalID, timeLevel, commSol, VTK_Type, nPolySol, JacConstant));
     }
 
     /* Skip the part with the node numbers. */
     long nNodesThisRank = longRecvBuf[i][indL];
-    indL += nNodesThisRank+1;
+    indL += nNodesThisRank + 1;
 
     /* Loop over the boundary markers. */
-    for(unsigned iMarker=0; iMarker<nMarker; ++iMarker) {
-      long nBoundElemThisRank = longRecvBuf[i][indL]; ++indL;
+    for (unsigned iMarker = 0; iMarker < nMarker; ++iMarker) {
+      long nBoundElemThisRank = longRecvBuf[i][indL];
+      ++indL;
 
       /* Loop over the boundary elements coming from this rank. */
-      for(long j=0; j<nBoundElemThisRank; ++j) {
-        short nDOFsBoundElem       = shortRecvBuf[i][indS+2];
-        short nDonorsWallFunctions = shortRecvBuf[i][indS+3];
+      for (long j = 0; j < nBoundElemThisRank; ++j) {
+        short nDOFsBoundElem = shortRecvBuf[i][indS + 2];
+        short nDonorsWallFunctions = shortRecvBuf[i][indS + 3];
         indS += 4;
         indL += nDOFsBoundElem + 2;
 
         /* Loop over the donors for the wall functions. */
-        for(short k=0; k<nDonorsWallFunctions; ++k, ++indL) {
-
+        for (short k = 0; k < nDonorsWallFunctions; ++k, ++indL) {
           /* Check for an external donor. If external, store it in
              haloElements with no periodic transformation. */
-          if( !binary_search(globalElemID.begin(), globalElemID.end(),
-                             longRecvBuf[i][indL]) )
+          if (!binary_search(globalElemID.begin(), globalElemID.end(), longRecvBuf[i][indL]))
             haloElements.push_back(CUnsignedLong2T(longRecvBuf[i][indL], 0));
         }
       }
@@ -700,11 +648,10 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
   unsigned short maxTimeLevelGlob = maxTimeLevelLoc;
 
 #ifdef HAVE_MPI
-  SU2_MPI::Allreduce(&maxTimeLevelLoc, &maxTimeLevelGlob,
-                     1, MPI_UNSIGNED_SHORT, MPI_MAX, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&maxTimeLevelLoc, &maxTimeLevelGlob, 1, MPI_UNSIGNED_SHORT, MPI_MAX, SU2_MPI::GetComm());
 #endif
 
-  const unsigned short nTimeLevels = maxTimeLevelGlob+1;
+  const unsigned short nTimeLevels = maxTimeLevelGlob + 1;
   config->SetnLevels_TimeAccurateLTS(nTimeLevels);
 
   /*----------------------------------------------------------------------------*/
@@ -714,40 +661,37 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
   /* Determine the number of owned elements and the total number of
      elements stored on this rank. */
   nVolElemOwned = globalElemID.size();
-  nVolElemTot   = nVolElemOwned + haloElements.size();
+  nVolElemTot = nVolElemOwned + haloElements.size();
 
   /* Determine the map from the global element ID to the current storage
      sequence of ownedElements. */
   map<unsigned long, unsigned long> mapGlobalElemIDToInd;
-  for(unsigned long i=0; i<nVolElemOwned; ++i)
-    mapGlobalElemIDToInd[ownedElements[i].GetGlobalElemID()] = i;
+  for (unsigned long i = 0; i < nVolElemOwned; ++i) mapGlobalElemIDToInd[ownedElements[i].GetGlobalElemID()] = i;
 
   /* Determine the number of elements per rank of the originally partitioned grid
      stored in cumulative storage format. */
-  vector<unsigned long> nElemPerRankOr(size+1);
+  vector<unsigned long> nElemPerRankOr(size + 1);
 
-  for(int i=0; i<size; ++i) nElemPerRankOr[i] = geometry->beg_node[i];
-  nElemPerRankOr[size] = geometry->end_node[size-1];
+  for (int i = 0; i < size; ++i) nElemPerRankOr[i] = geometry->beg_node[i];
+  nElemPerRankOr[size] = geometry->end_node[size - 1];
 
   /* Determine to which ranks I have to send messages to find out the information
      of the halos stored on this rank. */
   sendToRank.assign(size, 0);
 
-  for(unsigned long i=0; i<haloElements.size(); ++i) {
-
+  for (unsigned long i = 0; i < haloElements.size(); ++i) {
     /* Determine the rank where this halo element was originally stored. */
     vector<unsigned long>::iterator low;
-    low = lower_bound(nElemPerRankOr.begin(), nElemPerRankOr.end(),
-                      haloElements[i].long0);
+    low = lower_bound(nElemPerRankOr.begin(), nElemPerRankOr.end(), haloElements[i].long0);
     unsigned long rankHalo = low - nElemPerRankOr.begin();
-    if(*low > haloElements[i].long0) --rankHalo;
+    if (*low > haloElements[i].long0) --rankHalo;
 
     sendToRank[rankHalo] = 1;
   }
 
   rankToIndCommBuf.clear();
-  for(int i=0; i<size; ++i) {
-    if( sendToRank[i] ) {
+  for (int i = 0; i < size; ++i) {
+    if (sendToRank[i]) {
       int ind = (int)rankToIndCommBuf.size();
       rankToIndCommBuf[i] = ind;
     }
@@ -762,19 +706,16 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
   nRankRecv = nRankSend;
 
 #ifdef HAVE_MPI
-  SU2_MPI::Reduce_scatter(sendToRank.data(), &nRankRecv, sizeRecv.data(),
-                          MPI_INT, MPI_SUM, SU2_MPI::GetComm());
+  SU2_MPI::Reduce_scatter(sendToRank.data(), &nRankRecv, sizeRecv.data(), MPI_INT, MPI_SUM, SU2_MPI::GetComm());
 #endif
 
   /* Loop over the local halo elements to fill the communication buffers. */
-  for(unsigned long i=0; i<haloElements.size(); ++i) {
-
+  for (unsigned long i = 0; i < haloElements.size(); ++i) {
     /* Determine the rank where this halo element was originally stored. */
     vector<unsigned long>::iterator low;
-    low = lower_bound(nElemPerRankOr.begin(), nElemPerRankOr.end(),
-                      haloElements[i].long0);
+    low = lower_bound(nElemPerRankOr.begin(), nElemPerRankOr.end(), haloElements[i].long0);
     unsigned long ind = low - nElemPerRankOr.begin();
-    if(*low > haloElements[i].long0) --ind;
+    if (*low > haloElements[i].long0) --ind;
 
     /* Convert this rank to the index in the send buffer. */
     MI = rankToIndCommBuf.find((int)ind);
@@ -784,7 +725,7 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
        The subtraction of 1 is there to obtain the correct periodic index.
        In haloElements a +1 is added, because this variable is of unsigned long,
        which cannot handle negative numbers. */
-    long perIndex = haloElements[i].long1 -1;
+    long perIndex = haloElements[i].long1 - 1;
 
     longSendBuf[ind].push_back(haloElements[i].long0);
     longSendBuf[ind].push_back(perIndex);
@@ -805,15 +746,14 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
   commReqs.resize(nRankSend);
   MI = rankToIndCommBuf.begin();
 
-  for(int i=0; i<nRankSend; ++i, ++MI) {
+  for (int i = 0; i < nRankSend; ++i, ++MI) {
     int dest = MI->first;
-    SU2_MPI::Isend(longSendBuf[i].data(), longSendBuf[i].size(), MPI_LONG,
-                   dest, dest, SU2_MPI::GetComm(), &commReqs[i]);
+    SU2_MPI::Isend(longSendBuf[i].data(), longSendBuf[i].size(), MPI_LONG, dest, dest, SU2_MPI::GetComm(),
+                   &commReqs[i]);
   }
 
   /* Loop over the number of ranks from which I receive data. */
-  for(int i=0; i<nRankRecv; ++i) {
-
+  for (int i = 0; i < nRankRecv; ++i) {
     /* Block until a message with longs arrives from any processor.
        Determine the source and the size of the message and receive it. */
     SU2_MPI::Status status;
@@ -824,8 +764,7 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
     SU2_MPI::Get_count(&status, MPI_LONG, &sizeMess);
 
     longSecondRecvBuf[i].resize(sizeMess);
-    SU2_MPI::Recv(longSecondRecvBuf[i].data(), sizeMess, MPI_LONG,
-                  sourceRank[i], rank, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Recv(longSecondRecvBuf[i].data(), sizeMess, MPI_LONG, sourceRank[i], rank, SU2_MPI::GetComm(), &status);
   }
 
   /* Complete the non-blocking sends. */
@@ -834,8 +773,7 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
 #else
 
   /*--- Sequential mode. Simply copy the buffer, if present at all. ---*/
-  for(int i=0; i<nRankRecv; ++i)
-    longSecondRecvBuf[i] = longSendBuf[i];
+  for (int i = 0; i < nRankRecv; ++i) longSecondRecvBuf[i] = longSendBuf[i];
 
 #endif
 
@@ -843,7 +781,7 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
         is deleted, the swap function is used. Afterwards resize the first index
         of the send buffers to nRankRecv, because this number of messages must
         be sent back to the sending ranks with halo information. ---*/
-  for(int i=0; i<nRankSend; ++i) {
+  for (int i = 0; i < nRankSend; ++i) {
     vector<long>().swap(longSendBuf[i]);
   }
 
@@ -856,24 +794,22 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
 #endif
 
   /*--- Loop over the receive buffers to fill and send the send buffers again. ---*/
-  for(int i=0; i<nRankRecv; ++i) {
-
+  for (int i = 0; i < nRankRecv; ++i) {
     /* Determine the number of elements present in longSecondRecvBuf[i] and
        reserve the memory for the send buffer. */
-    const long nElemBuf = longSecondRecvBuf[i].size()/2;
-    longSendBuf[i].reserve(3*nElemBuf);
+    const long nElemBuf = longSecondRecvBuf[i].size() / 2;
+    longSendBuf[i].reserve(3 * nElemBuf);
 
     /* Loop over the elements stored in the receive buffer. */
-    for(long j=0; j<nElemBuf; ++j) {
-
+    for (long j = 0; j < nElemBuf; ++j) {
       /* Get the global element ID and periodic index from the receive buffer. */
-      const long globalID = longSecondRecvBuf[i][2*j];
-      const long perInd   = longSecondRecvBuf[i][2*j+1];
+      const long globalID = longSecondRecvBuf[i][2 * j];
+      const long perInd = longSecondRecvBuf[i][2 * j + 1];
 
       /* Determine the local index of the element in the original partitioning.
          Check if the index is valid. */
       const long localID = globalID - geometry->beg_node[rank];
-      if(localID < 0 || localID >= (long) geometry->nPointLinear[rank]) {
+      if (localID < 0 || localID >= (long)geometry->nPointLinear[rank]) {
         ostringstream message;
         message << localID << " " << geometry->nPointLinear[rank] << endl;
         message << "Invalid local element ID";
@@ -887,15 +823,15 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
       longSendBuf[i].push_back(geometry->elem[localID]->GetColor());
     }
 
-     /* Release the memory of this receive buffer. */
+    /* Release the memory of this receive buffer. */
     vector<long>().swap(longSecondRecvBuf[i]);
 
     /*--- Send the send buffer back to the calling rank.
           Only in parallel mode of course.     ---*/
 #ifdef HAVE_MPI
     int dest = sourceRank[i];
-    SU2_MPI::Isend(longSendBuf[i].data(), longSendBuf[i].size(), MPI_LONG,
-                   dest, dest+1, SU2_MPI::GetComm(), &commReqs[i]);
+    SU2_MPI::Isend(longSendBuf[i].data(), longSendBuf[i].size(), MPI_LONG, dest, dest + 1, SU2_MPI::GetComm(),
+                   &commReqs[i]);
 #endif
   }
 
@@ -909,12 +845,11 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
 
   /* Parallel mode. Loop over the number of ranks from which I receive data
      in the return communication, i.e. nRankSend. */
-  for(int i=0; i<nRankSend; ++i) {
-
+  for (int i = 0; i < nRankSend; ++i) {
     /* Block until a message with longs arrives from any processor.
        Determine the source and the size of the message.   */
     SU2_MPI::Status status;
-    SU2_MPI::Probe(MPI_ANY_SOURCE, rank+1, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Probe(MPI_ANY_SOURCE, rank + 1, SU2_MPI::GetComm(), &status);
     int source = status.MPI_SOURCE;
 
     int sizeMess;
@@ -922,8 +857,7 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
 
     /* Allocate the memory for the long receive buffer and receive the message. */
     longSecondRecvBuf[i].resize(sizeMess);
-    SU2_MPI::Recv(longSecondRecvBuf[i].data(), sizeMess, MPI_LONG,
-                  source, rank+1, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Recv(longSecondRecvBuf[i].data(), sizeMess, MPI_LONG, source, rank + 1, SU2_MPI::GetComm(), &status);
   }
 
   /* Complete the non-blocking sends and synchronize the ranks, because
@@ -934,27 +868,24 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
 #else
 
   /*--- Sequential mode. Simply copy the buffer, if present at all. ---*/
-  for(int i=0; i<nRankRecv; ++i)
-    longSecondRecvBuf[i] = longSendBuf[i];
+  for (int i = 0; i < nRankRecv; ++i) longSecondRecvBuf[i] = longSendBuf[i];
 
 #endif
 
   /* Release the memory of the send buffers. To make sure that all
      the memory is deleted, the swap function is used. */
-  for(int i=0; i<nRankRecv; ++i)
-    vector<long>().swap(longSendBuf[i]);
+  for (int i = 0; i < nRankRecv; ++i) vector<long>().swap(longSendBuf[i]);
 
   /* Copy the data from the receive buffers into a class of CLong3T, such that
      it can be sorted in increasing order. Note that the rank of the element
      is stored first, followed by its global ID and last the periodic index. */
   vector<CLong3T> haloData;
-  for(int i=0; i<nRankSend; ++i) {
-    const long nElemBuf = longSecondRecvBuf[i].size()/3;
+  for (int i = 0; i < nRankSend; ++i) {
+    const long nElemBuf = longSecondRecvBuf[i].size() / 3;
 
-    for(long j=0; j<nElemBuf; ++j) {
-      const long j3 = 3*j;
-      haloData.push_back(CLong3T(longSecondRecvBuf[i][j3+2], longSecondRecvBuf[i][j3],
-                                 longSecondRecvBuf[i][j3+1]));
+    for (long j = 0; j < nElemBuf; ++j) {
+      const long j3 = 3 * j;
+      haloData.push_back(CLong3T(longSecondRecvBuf[i][j3 + 2], longSecondRecvBuf[i][j3], longSecondRecvBuf[i][j3 + 1]));
     }
 
     /* Release the memory of this receive buffer. */
@@ -967,23 +898,20 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
   /* Determine the number of halo elements per rank in cumulative storage.
      The first element of this vector is nVolElemOwned, such that this vector
      contains the starting position in the vector volElem. */
-  vector<unsigned long> nHaloElemPerRank(size+1, 0);
-  for(unsigned long i=0; i<haloData.size(); ++i)
-    ++nHaloElemPerRank[haloData[i].long0+1];
+  vector<unsigned long> nHaloElemPerRank(size + 1, 0);
+  for (unsigned long i = 0; i < haloData.size(); ++i) ++nHaloElemPerRank[haloData[i].long0 + 1];
 
   nHaloElemPerRank[0] = nVolElemOwned;
-  for(int i=0; i<size; ++i)
-    nHaloElemPerRank[i+1] += nHaloElemPerRank[i];
+  for (int i = 0; i < size; ++i) nHaloElemPerRank[i + 1] += nHaloElemPerRank[i];
 
-  if(nHaloElemPerRank[size] != nVolElemTot)
-    SU2_MPI::Error("Inconsistency in total number of volume elements",
-                   CURRENT_FUNCTION);
+  if (nHaloElemPerRank[size] != nVolElemTot)
+    SU2_MPI::Error("Inconsistency in total number of volume elements", CURRENT_FUNCTION);
 
   /* Determine the number of ranks to which I have to send data in this cycle. */
   sendToRank.assign(size, 0);
   rankToIndCommBuf.clear();
-  for(int i=0; i<size; ++i) {
-    if(nHaloElemPerRank[i+1] > nHaloElemPerRank[i]) {
+  for (int i = 0; i < size; ++i) {
+    if (nHaloElemPerRank[i + 1] > nHaloElemPerRank[i]) {
       sendToRank[i] = 1;
       int ind = (int)rankToIndCommBuf.size();
       rankToIndCommBuf[i] = ind;
@@ -999,17 +927,16 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
   nRankRecv = nRankSend;
 
 #ifdef HAVE_MPI
-  SU2_MPI::Reduce_scatter(sendToRank.data(), &nRankRecv, sizeRecv.data(),
-                          MPI_INT, MPI_SUM, SU2_MPI::GetComm());
+  SU2_MPI::Reduce_scatter(sendToRank.data(), &nRankRecv, sizeRecv.data(), MPI_INT, MPI_SUM, SU2_MPI::GetComm());
 #endif
 
   /* Copy the data to be sent to the send buffers. */
   longSendBuf.resize(nRankSend);
   MI = rankToIndCommBuf.begin();
 
-  for(int i=0; i<nRankSend; ++i, ++MI) {
+  for (int i = 0; i < nRankSend; ++i, ++MI) {
     int dest = MI->first;
-    for(unsigned long j=nHaloElemPerRank[dest]; j<nHaloElemPerRank[dest+1]; ++j) {
+    for (unsigned long j = nHaloElemPerRank[dest]; j < nHaloElemPerRank[dest + 1]; ++j) {
       const unsigned long jj = j - nVolElemOwned;
       longSendBuf[i].push_back(haloData[jj].long1);
       longSendBuf[i].push_back(haloData[jj].long2);
@@ -1027,18 +954,17 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
   commReqs.resize(nRankSend);
   MI = rankToIndCommBuf.begin();
 
-  for(int i=0; i<nRankSend; ++i, ++MI) {
+  for (int i = 0; i < nRankSend; ++i, ++MI) {
     int dest = MI->first;
-    SU2_MPI::Isend(longSendBuf[i].data(), longSendBuf[i].size(), MPI_LONG,
-                   dest, dest, SU2_MPI::GetComm(), &commReqs[i]);
+    SU2_MPI::Isend(longSendBuf[i].data(), longSendBuf[i].size(), MPI_LONG, dest, dest, SU2_MPI::GetComm(),
+                   &commReqs[i]);
   }
 
   /* Resize the vector to store the ranks from which the message came. */
   sourceRank.resize(nRankRecv);
 
   /* Loop over the number of ranks from which I receive data. */
-  for(int i=0; i<nRankRecv; ++i) {
-
+  for (int i = 0; i < nRankRecv; ++i) {
     /* Block until a message with longs arrives from any processor.
        Determine the source and the size of the message and receive it. */
     SU2_MPI::Status status;
@@ -1049,8 +975,7 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
     SU2_MPI::Get_count(&status, MPI_LONG, &sizeMess);
 
     longSecondRecvBuf[i].resize(sizeMess);
-    SU2_MPI::Recv(longSecondRecvBuf[i].data(), sizeMess, MPI_LONG,
-                  sourceRank[i], rank, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Recv(longSecondRecvBuf[i].data(), sizeMess, MPI_LONG, sourceRank[i], rank, SU2_MPI::GetComm(), &status);
   }
 
   /* Complete the non-blocking sends and synchronize the ranks,
@@ -1061,14 +986,13 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
 #else
 
   /*--- Sequential mode. Simply copy the buffer, if present at all. ---*/
-  for(int i=0; i<nRankSend; ++i)
-    longSecondRecvBuf[i] = longSendBuf[i];
+  for (int i = 0; i < nRankSend; ++i) longSecondRecvBuf[i] = longSendBuf[i];
 
 #endif
 
   /* Release the memory of the send buffers. To make sure that all the memory
      is deleted, the swap function is used. */
-  for(int i=0; i<nRankSend; ++i) {
+  for (int i = 0; i < nRankSend; ++i) {
     vector<long>().swap(longSendBuf[i]);
   }
 
@@ -1077,14 +1001,13 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
         do this when ownedElements are constructed, elements that are donors
         for the wall function treatment and are not direct neighbors may
         have been missed. ---*/
-  for(int i=0; i<nRankRecv; ++i) {
-
-    const unsigned long nElemBuf = longSecondRecvBuf[i].size()/2;
-    for(unsigned long j=0; j<nElemBuf; ++j) {
-      const unsigned long elemID = longSecondRecvBuf[i][2*j];
+  for (int i = 0; i < nRankRecv; ++i) {
+    const unsigned long nElemBuf = longSecondRecvBuf[i].size() / 2;
+    for (unsigned long j = 0; j < nElemBuf; ++j) {
+      const unsigned long elemID = longSecondRecvBuf[i][2 * j];
 
       map<unsigned long, unsigned long>::iterator MMI = mapGlobalElemIDToInd.find(elemID);
-      if(MMI == mapGlobalElemIDToInd.end())
+      if (MMI == mapGlobalElemIDToInd.end())
         SU2_MPI::Error("Entry not found in mapGlobalElemIDToInd", CURRENT_FUNCTION);
 
       ownedElements[MMI->second].SetCommSolution(true);
@@ -1121,15 +1044,14 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
 
   /* Determine the number of elements/faces that are treated simultaneously */
   /* in the matrix products to obtain good gemm performance.                */
-  const unsigned short nElemSimul = config->GetSizeMatMulPadding()/nVar;
+  const unsigned short nElemSimul = config->GetSizeMatMulPadding() / nVar;
 
   /* Determine the number of different element types present. */
   map<unsigned short, unsigned short> mapElemTypeToInd;
-  for(vector<CReorderElements>::iterator OEI =ownedElements.begin();
-                                         OEI!=ownedElements.end(); ++OEI) {
+  for (vector<CReorderElements>::iterator OEI = ownedElements.begin(); OEI != ownedElements.end(); ++OEI) {
     const unsigned short elType = OEI->GetElemType();
 
-    if(mapElemTypeToInd.find(elType) == mapElemTypeToInd.end()) {
+    if (mapElemTypeToInd.find(elType) == mapElemTypeToInd.end()) {
       const unsigned short ind = mapElemTypeToInd.size();
       mapElemTypeToInd[elType] = ind;
     }
@@ -1140,25 +1062,21 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
      communicated) and elements that are communicated. Later on these vectors
      will be put in cumulative storage format, which explains the +1 for
      the second index. */
-  vector<vector<unsigned long> > nInternalElem(nTimeLevels,
-                                               vector<unsigned long>(mapElemTypeToInd.size()+1));
-  vector<vector<unsigned long> > nCommElem(nTimeLevels,
-                                           vector<unsigned long>(mapElemTypeToInd.size()+1));
-  for(unsigned short i=0; i<nTimeLevels; ++i)
-  {
-    for(unsigned long j=0; j<=mapElemTypeToInd.size(); ++j) {
+  vector<vector<unsigned long> > nInternalElem(nTimeLevels, vector<unsigned long>(mapElemTypeToInd.size() + 1));
+  vector<vector<unsigned long> > nCommElem(nTimeLevels, vector<unsigned long>(mapElemTypeToInd.size() + 1));
+  for (unsigned short i = 0; i < nTimeLevels; ++i) {
+    for (unsigned long j = 0; j <= mapElemTypeToInd.size(); ++j) {
       nInternalElem[i][j] = 0;
       nCommElem[i][j] = 0;
     }
   }
 
-  for(vector<CReorderElements>::iterator OEI =ownedElements.begin();
-                                         OEI!=ownedElements.end(); ++OEI) {
+  for (vector<CReorderElements>::iterator OEI = ownedElements.begin(); OEI != ownedElements.end(); ++OEI) {
     const unsigned short elType = OEI->GetElemType();
     map<unsigned short, unsigned short>::const_iterator MI = mapElemTypeToInd.find(elType);
-    unsigned short ind = MI->second +1;
+    unsigned short ind = MI->second + 1;
 
-    if( OEI->GetCommSolution() )
+    if (OEI->GetCommSolution())
       ++nCommElem[OEI->GetTimeLevel()][ind];
     else
       ++nInternalElem[OEI->GetTimeLevel()][ind];
@@ -1167,24 +1085,21 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
   /* Loop again over the owned elements and check if elements, which do not
      have to send their solution, should be flagged as such in order to improve
      the gemm performance. */
-  for(vector<CReorderElements>::iterator OEI =ownedElements.begin();
-                                         OEI!=ownedElements.end(); ++OEI) {
-
+  for (vector<CReorderElements>::iterator OEI = ownedElements.begin(); OEI != ownedElements.end(); ++OEI) {
     /* Check for an internal element, i.e. an element for which the solution
        does not need to be communicated. */
-    if( !OEI->GetCommSolution() ) {
-
+    if (!OEI->GetCommSolution()) {
       /* Determine the time level and the index of the element type. */
       const unsigned short tLev = OEI->GetTimeLevel();
 
       const unsigned short elType = OEI->GetElemType();
       map<unsigned short, unsigned short>::const_iterator MI = mapElemTypeToInd.find(elType);
-      const unsigned short ind = MI->second +1;
+      const unsigned short ind = MI->second + 1;
 
       /* Determine whether or not this element must be moved from internal to
          comm elements to improve performance. Change the appropriate data
          when this must happen. */
-      if(nInternalElem[tLev][ind]%nElemSimul && nCommElem[tLev][ind]%nElemSimul) {
+      if (nInternalElem[tLev][ind] % nElemSimul && nCommElem[tLev][ind] % nElemSimul) {
         OEI->SetCommSolution(true);
         --nInternalElem[tLev][ind];
         ++nCommElem[tLev][ind];
@@ -1195,30 +1110,30 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
   /* Check whether there are enough elements in every partition for every
      time level to guarantee a good gemm performance. */
   unsigned long nFullChunks = 0, nPartialChunks = 0;
-  for(unsigned short tLev=0; tLev<nTimeLevels; ++tLev) {
-    for(unsigned long j=1; j<nInternalElem[tLev].size(); ++j) {
-      nFullChunks += nInternalElem[tLev][j]/nElemSimul;
-      if(nInternalElem[tLev][j]%nElemSimul) ++nPartialChunks;
+  for (unsigned short tLev = 0; tLev < nTimeLevels; ++tLev) {
+    for (unsigned long j = 1; j < nInternalElem[tLev].size(); ++j) {
+      nFullChunks += nInternalElem[tLev][j] / nElemSimul;
+      if (nInternalElem[tLev][j] % nElemSimul) ++nPartialChunks;
     }
 
-    for(unsigned long j=1; j<nCommElem[tLev].size(); ++j) {
-      nFullChunks += nCommElem[tLev][j]/nElemSimul;
-      if(nCommElem[tLev][j]%nElemSimul) ++nPartialChunks;
+    for (unsigned long j = 1; j < nCommElem[tLev].size(); ++j) {
+      nFullChunks += nCommElem[tLev][j] / nElemSimul;
+      if (nCommElem[tLev][j] % nElemSimul) ++nPartialChunks;
     }
   }
 
   unsigned long tooManyPartChunksLoc = 0;
-  if(5*nPartialChunks >= (nPartialChunks+nFullChunks)) tooManyPartChunksLoc = 1;
+  if (5 * nPartialChunks >= (nPartialChunks + nFullChunks)) tooManyPartChunksLoc = 1;
 
   /* Determine the number of ranks which contain too many partial chunks.
      The result only needs to be known on the master node. */
   unsigned long nRanksTooManyPartChunks = tooManyPartChunksLoc;
 #ifdef HAVE_MPI
-  SU2_MPI::Reduce(&tooManyPartChunksLoc, &nRanksTooManyPartChunks, 1,
-                  MPI_UNSIGNED_LONG, MPI_SUM, MASTER_NODE, SU2_MPI::GetComm());
+  SU2_MPI::Reduce(&tooManyPartChunksLoc, &nRanksTooManyPartChunks, 1, MPI_UNSIGNED_LONG, MPI_SUM, MASTER_NODE,
+                  SU2_MPI::GetComm());
 #endif
 
-  if((rank == MASTER_NODE) && (nRanksTooManyPartChunks != 0) && (size > 1)) {
+  if ((rank == MASTER_NODE) && (nRanksTooManyPartChunks != 0) && (size > 1)) {
     cout << endl << "                 WARNING" << endl;
     cout << "There are " << nRanksTooManyPartChunks << " partitions for which "
          << " the simultaneous treatment of volume elements is not optimal." << endl;
@@ -1226,14 +1141,12 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
   }
 
   /* Put nInternalElem and nCommElem in cumulative storage format. */
-  for(unsigned short tLev=0; tLev<nTimeLevels; ++tLev) {
-    if( tLev ) nInternalElem[tLev][0] = nCommElem[tLev-1].back();
-    for(unsigned long j=1; j<nInternalElem[tLev].size(); ++j)
-      nInternalElem[tLev][j] += nInternalElem[tLev][j-1];
+  for (unsigned short tLev = 0; tLev < nTimeLevels; ++tLev) {
+    if (tLev) nInternalElem[tLev][0] = nCommElem[tLev - 1].back();
+    for (unsigned long j = 1; j < nInternalElem[tLev].size(); ++j) nInternalElem[tLev][j] += nInternalElem[tLev][j - 1];
 
     nCommElem[tLev][0] = nInternalElem[tLev].back();
-    for(unsigned long j=1; j<nCommElem[tLev].size(); ++j)
-      nCommElem[tLev][j] += nCommElem[tLev][j-1];
+    for (unsigned long j = 1; j < nCommElem[tLev].size(); ++j) nCommElem[tLev][j] += nCommElem[tLev][j - 1];
   }
 
   /* In the solver only the number of elements per time level is needed.
@@ -1241,14 +1154,13 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
      cumulative storage format and can be retrieved easily from nCommElem.
      The number of internal elements per time level is stored normally and
      can be retrieved from nInternalElem. */
-  nVolElemOwnedPerTimeLevel.resize(nTimeLevels+1);
+  nVolElemOwnedPerTimeLevel.resize(nTimeLevels + 1);
   nVolElemInternalPerTimeLevel.resize(nTimeLevels);
 
   nVolElemOwnedPerTimeLevel[0] = 0;
-  for(unsigned short tLev=0; tLev<nTimeLevels; ++tLev) {
-    nVolElemOwnedPerTimeLevel[tLev+1]  = nCommElem[tLev].back();
-    nVolElemInternalPerTimeLevel[tLev] = nInternalElem[tLev].back()
-                                       - nInternalElem[tLev][0];
+  for (unsigned short tLev = 0; tLev < nTimeLevels; ++tLev) {
+    nVolElemOwnedPerTimeLevel[tLev + 1] = nCommElem[tLev].back();
+    nVolElemInternalPerTimeLevel[tLev] = nInternalElem[tLev].back() - nInternalElem[tLev][0];
   }
 
   /* Sort the elements of ownedElements in increasing order. */
@@ -1264,38 +1176,36 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
   /* Determine the map from the global element ID to the current storage
      sequence of ownedElements. */
   mapGlobalElemIDToInd.clear();
-  for(unsigned long i=0; i<nVolElemOwned; ++i)
-    mapGlobalElemIDToInd[ownedElements[i].GetGlobalElemID()] = i;
+  for (unsigned long i = 0; i < nVolElemOwned; ++i) mapGlobalElemIDToInd[ownedElements[i].GetGlobalElemID()] = i;
 
   /*--- Create the graph of local elements. The halo elements are ignored. ---*/
   vector<vector<unsigned long> > neighElem(nVolElemOwned, vector<unsigned long>(0));
 
-  nRankRecv = (int) longRecvBuf.size();
-  for(int i=0; i<nRankRecv; ++i) {
+  nRankRecv = (int)longRecvBuf.size();
+  for (int i = 0; i < nRankRecv; ++i) {
     unsigned long indL = 1, indS = 0;
-    for(long j=0; j<longRecvBuf[i][0]; ++j) {
-      unsigned long  globalID  = longRecvBuf[i][indL];
-      unsigned short nDOFsGrid = shortRecvBuf[i][indS+3];
-      unsigned short nFaces    = shortRecvBuf[i][indS+5];
+    for (long j = 0; j < longRecvBuf[i][0]; ++j) {
+      unsigned long globalID = longRecvBuf[i][indL];
+      unsigned short nDOFsGrid = shortRecvBuf[i][indS + 3];
+      unsigned short nFaces = shortRecvBuf[i][indS + 5];
 
       map<unsigned long, unsigned long>::iterator MMI = mapGlobalElemIDToInd.find(globalID);
       unsigned long ind = MMI->second;
 
       indS += 8;
       indL += nDOFsGrid + 2;
-      for(unsigned short k=0; k<nFaces; ++k, indS+=3, ++indL) {
-        if((longRecvBuf[i][indL] != -1) && (shortRecvBuf[i][indS] == -1)) { // Check for internal owned node.
+      for (unsigned short k = 0; k < nFaces; ++k, indS += 3, ++indL) {
+        if ((longRecvBuf[i][indL] != -1) && (shortRecvBuf[i][indS] == -1)) {  // Check for internal owned node.
 
           MMI = mapGlobalElemIDToInd.find(longRecvBuf[i][indL]);
-          if(MMI != mapGlobalElemIDToInd.end()) neighElem[ind].push_back(MMI->second);
+          if (MMI != mapGlobalElemIDToInd.end()) neighElem[ind].push_back(MMI->second);
         }
       }
     }
   }
 
   /* Sort the neighbors of each element in increasing order. */
-  for(unsigned long i=0; i<nVolElemOwned; ++i)
-    sort(neighElem[i].begin(), neighElem[i].end());
+  for (unsigned long i = 0; i < nVolElemOwned; ++i) sort(neighElem[i].begin(), neighElem[i].end());
 
   /* Define the vector, which contains the new numbering of the owned elements
      w.r.t. to the numbering currently stored in ownedElements. Note that signed
@@ -1307,54 +1217,50 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
         because the local partition may not be contiguous. ---*/
   unsigned long nElemRenumbered = 0;
   while (nElemRenumbered < nVolElemOwned) {
-
     /* Determine the first element in the list that has not been renumbered. */
     unsigned long indBeg;
-    for(indBeg=0; indBeg<nVolElemOwned; ++indBeg)
-      if(oldElemToNewElem[indBeg] == -1) break;
+    for (indBeg = 0; indBeg < nVolElemOwned; ++indBeg)
+      if (oldElemToNewElem[indBeg] == -1) break;
 
     /* Determine the time level and element type of the element indBeg and
        determine the element range in which the starting element for the
        renumbering must be sought. */
     unsigned short timeLevel = ownedElements[indBeg].GetTimeLevel();
-    unsigned short elType    = ownedElements[indBeg].GetElemType();
+    unsigned short elType = ownedElements[indBeg].GetElemType();
 
     map<unsigned short, unsigned short>::const_iterator MI = mapElemTypeToInd.find(elType);
     unsigned short ind = MI->second;
 
     unsigned long indEnd;
-    if( ownedElements[indBeg].GetCommSolution() )
-      indEnd = nCommElem[timeLevel][ind+1];
+    if (ownedElements[indBeg].GetCommSolution())
+      indEnd = nCommElem[timeLevel][ind + 1];
     else
-      indEnd = nInternalElem[timeLevel][ind+1];
+      indEnd = nInternalElem[timeLevel][ind + 1];
 
     /* Determine the element in the range [indBeg,indEnd) with the least number
        of neighbors that has not been renumbered yet. This is the starting
        element for the current renumbering round. */
-    for(unsigned long i=(indBeg+1); i<indEnd; ++i) {
-      if((oldElemToNewElem[i] == -1) &&
-         (neighElem[i].size() < neighElem[indBeg].size())) indBeg = i;
+    for (unsigned long i = (indBeg + 1); i < indEnd; ++i) {
+      if ((oldElemToNewElem[i] == -1) && (neighElem[i].size() < neighElem[indBeg].size())) indBeg = i;
     }
 
     /* Start of the Reverse Cuthil McKee renumbering. */
     vector<unsigned long> frontElements(1, indBeg);
-    while( frontElements.size() ) {
-
+    while (frontElements.size()) {
       /* Vector, which stores the front for the next round. */
       vector<unsigned long> frontElementsNew;
 
       /* Loop over the elements of the current front. */
-      for(unsigned long i=0; i<frontElements.size(); ++i) {
-
+      for (unsigned long i = 0; i < frontElements.size(); ++i) {
         /* Carry out the renumbering for this element. */
         const unsigned long iFront = frontElements[i];
 
         timeLevel = ownedElements[iFront].GetTimeLevel();
-        elType    = ownedElements[iFront].GetElemType();
-        MI  = mapElemTypeToInd.find(elType);
+        elType = ownedElements[iFront].GetElemType();
+        MI = mapElemTypeToInd.find(elType);
         ind = MI->second;
 
-        if( ownedElements[iFront].GetCommSolution() )
+        if (ownedElements[iFront].GetCommSolution())
           oldElemToNewElem[iFront] = nCommElem[timeLevel][ind]++;
         else
           oldElemToNewElem[iFront] = nInternalElem[timeLevel][ind]++;
@@ -1362,8 +1268,8 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
         /* Store the neighbors that have not been renumbered yet in the front
            for the next round. Set its index to -2 to indicate that the element
            is already on the new front. */
-        for(unsigned long j=0; j<neighElem[iFront].size(); ++j) {
-          if(oldElemToNewElem[neighElem[iFront][j]] == -1) {
+        for (unsigned long j = 0; j < neighElem[iFront].size(); ++j) {
+          if (oldElemToNewElem[neighElem[iFront][j]] == -1) {
             frontElementsNew.push_back(neighElem[iFront][j]);
             oldElemToNewElem[neighElem[iFront][j]] = -2;
           }
@@ -1381,32 +1287,31 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
     }
   }
 
-  if(nElemRenumbered != nVolElemOwned)
-    SU2_MPI::Error("Something went wrong in the renumbering", CURRENT_FUNCTION);
+  if (nElemRenumbered != nVolElemOwned) SU2_MPI::Error("Something went wrong in the renumbering", CURRENT_FUNCTION);
 
   /* Determine the final mapping from the global element number to the local
      entry for the owned elements. First clear mapGlobalElemIDToInd before
      it can be used to store its correct content. */
   mapGlobalElemIDToInd.clear();
-  for(unsigned long i=0; i<nVolElemOwned; ++i)
+  for (unsigned long i = 0; i < nVolElemOwned; ++i)
     mapGlobalElemIDToInd[ownedElements[i].GetGlobalElemID()] = oldElemToNewElem[i];
 
-  /*----------------------------------------------------------------------------*/
-  /*--- Step 4: Store the elements, nodes and boundary elements in the data  ---*/
-  /*---         structures used by the FEM solver.                           ---*/
-  /*----------------------------------------------------------------------------*/
+    /*----------------------------------------------------------------------------*/
+    /*--- Step 4: Store the elements, nodes and boundary elements in the data  ---*/
+    /*---         structures used by the FEM solver.                           ---*/
+    /*----------------------------------------------------------------------------*/
 
-  /*--- Check in parallel mode for empty partitions. If present, print a warning.
-        The solver is capable of handling empty partitions, but it may not be
-        efficient. ---*/
+    /*--- Check in parallel mode for empty partitions. If present, print a warning.
+          The solver is capable of handling empty partitions, but it may not be
+          efficient. ---*/
 #ifdef HAVE_MPI
   unsigned long thisPartitionEmpty = nVolElemOwned ? 0 : 1;
   unsigned long nEmptyPartitions = 0;
 
-  SU2_MPI::Reduce(&thisPartitionEmpty, &nEmptyPartitions, 1,
-                  MPI_UNSIGNED_LONG, MPI_SUM, MASTER_NODE, SU2_MPI::GetComm());
+  SU2_MPI::Reduce(&thisPartitionEmpty, &nEmptyPartitions, 1, MPI_UNSIGNED_LONG, MPI_SUM, MASTER_NODE,
+                  SU2_MPI::GetComm());
 
-  if(rank == MASTER_NODE && nEmptyPartitions) {
+  if (rank == MASTER_NODE && nEmptyPartitions) {
     cout << endl << "         WARNING" << endl;
     cout << "There are " << nEmptyPartitions << " empty partitions present." << endl;
     cout << "SU2 is able to handle this, but it may be inefficient." << endl << endl;
@@ -1419,59 +1324,55 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
   meshPoints.reserve(nPoint);
 
   boundaries.resize(nMarker);
-  for(unsigned short iMarker=0; iMarker<nMarker; ++iMarker) {
-    boundaries[iMarker].markerTag        = config->GetMarker_All_TagBound(iMarker);
+  for (unsigned short iMarker = 0; iMarker < nMarker; ++iMarker) {
+    boundaries[iMarker].markerTag = config->GetMarker_All_TagBound(iMarker);
     boundaries[iMarker].periodicBoundary = config->GetMarker_All_KindBC(iMarker) == PERIODIC_BOUNDARY;
     boundaries[iMarker].surfElem.reserve(nElem_Bound[iMarker]);
   }
 
   /*--- Copy the data from the communication buffers. ---*/
-  for(int i=0; i<nRankRecv; ++i) {
-
+  for (int i = 0; i < nRankRecv; ++i) {
     /* The data for the volume elements. Loop over these elements in the buffer. */
     unsigned long indL = 1, indS = 0, indD = 0;
-    for(long j=0; j<longRecvBuf[i][0]; ++j) {
-
+    for (long j = 0; j < longRecvBuf[i][0]; ++j) {
       /* Determine the location in volElem where this data must be stored. */
       unsigned long elemID = longRecvBuf[i][indL++];
       map<unsigned long, unsigned long>::iterator MMI = mapGlobalElemIDToInd.find(elemID);
       unsigned long ind = MMI->second;
 
       /* Store the data. */
-      volElem[ind].elemIsOwned        = true;
-      volElem[ind].rankOriginal       = rank;
+      volElem[ind].elemIsOwned = true;
+      volElem[ind].rankOriginal = rank;
       volElem[ind].periodIndexToDonor = -1;
 
-      volElem[ind].VTK_Type  = shortRecvBuf[i][indS++];
+      volElem[ind].VTK_Type = shortRecvBuf[i][indS++];
       volElem[ind].nPolyGrid = shortRecvBuf[i][indS++];
-      volElem[ind].nPolySol  = shortRecvBuf[i][indS++];
+      volElem[ind].nPolySol = shortRecvBuf[i][indS++];
       volElem[ind].nDOFsGrid = shortRecvBuf[i][indS++];
-      volElem[ind].nDOFsSol  = shortRecvBuf[i][indS++];
-      volElem[ind].nFaces    = shortRecvBuf[i][indS++];
+      volElem[ind].nDOFsSol = shortRecvBuf[i][indS++];
+      volElem[ind].nFaces = shortRecvBuf[i][indS++];
       volElem[ind].timeLevel = shortRecvBuf[i][indS++];
 
-      volElem[ind].JacIsConsideredConstant = (bool) shortRecvBuf[i][indS++];
+      volElem[ind].JacIsConsideredConstant = (bool)shortRecvBuf[i][indS++];
 
-      volElem[ind].elemIDGlobal        = elemID;
+      volElem[ind].elemIDGlobal = elemID;
       volElem[ind].offsetDOFsSolGlobal = longRecvBuf[i][indL++];
 
       volElem[ind].nodeIDsGrid.resize(volElem[ind].nDOFsGrid);
       volElem[ind].JacFacesIsConsideredConstant.resize(volElem[ind].nFaces);
       volElem[ind].ElementOwnsFaces.resize(volElem[ind].nFaces);
 
-      for(unsigned short k=0; k<volElem[ind].nDOFsGrid; ++k)
-        volElem[ind].nodeIDsGrid[k] = longRecvBuf[i][indL++];
+      for (unsigned short k = 0; k < volElem[ind].nDOFsGrid; ++k) volElem[ind].nodeIDsGrid[k] = longRecvBuf[i][indL++];
 
-      for(unsigned short k=0; k<volElem[ind].nFaces; ++k) {
+      for (unsigned short k = 0; k < volElem[ind].nFaces; ++k) {
         long neighBorID = longRecvBuf[i][indL++];
 
-        ++indS; // At this location the periodic index of the face is stored in
-                // shortRecvBuf, which is not stored in volElem.
-        volElem[ind].JacFacesIsConsideredConstant[k] = (bool) shortRecvBuf[i][indS++];
-        volElem[ind].ElementOwnsFaces[k]             = (bool) shortRecvBuf[i][indS++];
+        ++indS;  // At this location the periodic index of the face is stored in
+                 // shortRecvBuf, which is not stored in volElem.
+        volElem[ind].JacFacesIsConsideredConstant[k] = (bool)shortRecvBuf[i][indS++];
+        volElem[ind].ElementOwnsFaces[k] = (bool)shortRecvBuf[i][indS++];
 
-        if(neighBorID == -1)
-          volElem[ind].ElementOwnsFaces[k] = true;  // Boundary faces are always owned.
+        if (neighBorID == -1) volElem[ind].ElementOwnsFaces[k] = true;  // Boundary faces are always owned.
       }
 
       volElem[ind].lenScale = doubleRecvBuf[i][indD++];
@@ -1480,33 +1381,31 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
     /* The data for the nodes. Loop over these nodes in the buffer and store
        them in meshPoints. */
     unsigned long nNodesThisRank = longRecvBuf[i][indL++];
-    for(unsigned long j=0; j<nNodesThisRank; ++j) {
+    for (unsigned long j = 0; j < nNodesThisRank; ++j) {
       CPointFEM thisPoint;
       thisPoint.globalID = longRecvBuf[i][indL++];
       thisPoint.periodIndexToDonor = -1;
-      for(unsigned short k=0; k<nDim; ++k)
-        thisPoint.coor[k] = doubleRecvBuf[i][indD++];
+      for (unsigned short k = 0; k < nDim; ++k) thisPoint.coor[k] = doubleRecvBuf[i][indD++];
 
       meshPoints.push_back(thisPoint);
     }
 
     /* The data for the boundary markers. Loop over them. */
-    for(unsigned short iMarker=0; iMarker<nMarker; ++iMarker) {
-
+    for (unsigned short iMarker = 0; iMarker < nMarker; ++iMarker) {
       unsigned long nElemThisRank = longRecvBuf[i][indL++];
-      for(unsigned long j=0; j<nElemThisRank; ++j) {
+      for (unsigned long j = 0; j < nElemThisRank; ++j) {
         CSurfaceElementFEM thisSurfElem;
 
-        thisSurfElem.VTK_Type  = shortRecvBuf[i][indS++];
+        thisSurfElem.VTK_Type = shortRecvBuf[i][indS++];
         thisSurfElem.nPolyGrid = shortRecvBuf[i][indS++];
         thisSurfElem.nDOFsGrid = shortRecvBuf[i][indS++];
-        const short nDonors    = shortRecvBuf[i][indS++];
+        const short nDonors = shortRecvBuf[i][indS++];
 
-        thisSurfElem.volElemID         = longRecvBuf[i][indL++];
+        thisSurfElem.volElemID = longRecvBuf[i][indL++];
         thisSurfElem.boundElemIDGlobal = longRecvBuf[i][indL++];
 
         thisSurfElem.nodeIDsGrid.resize(thisSurfElem.nDOFsGrid);
-        for(unsigned short k=0; k<thisSurfElem.nDOFsGrid; ++k)
+        for (unsigned short k = 0; k < thisSurfElem.nDOFsGrid; ++k)
           thisSurfElem.nodeIDsGrid[k] = longRecvBuf[i][indL++];
 
         indL += nDonors;
@@ -1531,20 +1430,19 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
   /* Clear the contents of the map globalPointIDToLocalInd and fill
      it with the information present in meshPoints. */
   globalPointIDToLocalInd.clear();
-  for(unsigned long i=0; i<meshPoints.size(); ++i)
-    globalPointIDToLocalInd[meshPoints[i].globalID] = i;
+  for (unsigned long i = 0; i < meshPoints.size(); ++i) globalPointIDToLocalInd[meshPoints[i].globalID] = i;
 
   /*--- All the data from the receive buffers has been copied in the local
         data structures. Release the memory of the receive buffers. To make
         sure that all the memory is deleted, the swap function is used. ---*/
-  for(int i=0; i<nRankRecv; ++i) {
+  for (int i = 0; i < nRankRecv; ++i) {
     vector<short>().swap(shortRecvBuf[i]);
     vector<long>().swap(longRecvBuf[i]);
     vector<su2double>().swap(doubleRecvBuf[i]);
   }
 
   /*--- Sort the surface elements of the boundaries in increasing order. ---*/
-  for(unsigned short iMarker=0; iMarker<nMarker; ++iMarker)
+  for (unsigned short iMarker = 0; iMarker < nMarker; ++iMarker)
     sort(boundaries[iMarker].surfElem.begin(), boundaries[iMarker].surfElem.end());
 
   /*----------------------------------------------------------------------------*/
@@ -1556,7 +1454,7 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
   /*--- Resize the first index of the send buffers to nRankRecv, because this
         number of messages must be sent back to the sending ranks with halo
         information. ---*/
-  nRankRecv = (int) longSecondRecvBuf.size();
+  nRankRecv = (int)longSecondRecvBuf.size();
   shortSendBuf.resize(nRankRecv);
   longSendBuf.resize(nRankRecv);
   doubleSendBuf.resize(nRankRecv);
@@ -1564,29 +1462,28 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
 #ifdef HAVE_MPI
   /* Resize the vector of the communication requests to the number of messages
      to be sent by this rank. Only in parallel node. */
-  commReqs.resize(3*nRankRecv);
+  commReqs.resize(3 * nRankRecv);
 #endif
 
   /*--- Loop over the receive buffers to fill the send buffers again. ---*/
-  for(int i=0; i<nRankRecv; ++i) {
-
+  for (int i = 0; i < nRankRecv; ++i) {
     /* Loop over the elements in this receive buffer to determine the local
        index on this rank. Note that also the periodic index must be stored,
        hence use an CUnsignedLong2T for this purpose. As -1 cannot be stored
        for an unsigned long a 1 is added to the periodic transformation. */
-    const unsigned long nElemBuf = longSecondRecvBuf[i].size()/2;
+    const unsigned long nElemBuf = longSecondRecvBuf[i].size() / 2;
     vector<CUnsignedLong2T> elemBuf(nElemBuf);
 
-    for(unsigned long j=0; j<nElemBuf; ++j) {
-      const unsigned long j2 = 2*j;
+    for (unsigned long j = 0; j < nElemBuf; ++j) {
+      const unsigned long j2 = 2 * j;
 
       const unsigned long elemID = longSecondRecvBuf[i][j2];
       map<unsigned long, unsigned long>::iterator MMI = mapGlobalElemIDToInd.find(elemID);
-      if(MMI == mapGlobalElemIDToInd.end())
+      if (MMI == mapGlobalElemIDToInd.end())
         SU2_MPI::Error("Entry not found in mapGlobalElemIDToInd", CURRENT_FUNCTION);
 
       elemBuf[j].long0 = MMI->second;
-      elemBuf[j].long1 = longSecondRecvBuf[i][j2+1] + 1;
+      elemBuf[j].long1 = longSecondRecvBuf[i][j2 + 1] + 1;
     }
 
     /* Release the memory of the long receive buffer via the swap function
@@ -1604,15 +1501,14 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
     vector<CUnsignedLong2T> nodeIDs;
 
     /* Loop over the elements to fill the send buffers. */
-    for(unsigned long j=0; j<nElemBuf; ++j) {
-
+    for (unsigned long j = 0; j < nElemBuf; ++j) {
       /* Store the global element ID in the long buffer,
          the periodic index in the short send buffer and
          the length scale in the double send buffer. */
       const unsigned long indV = elemBuf[j].long0;
       longSendBuf[i].push_back(volElem[indV].elemIDGlobal);
 
-      const short perIndex = (short) elemBuf[j].long1 -1; // Note the -1.
+      const short perIndex = (short)elemBuf[j].long1 - 1;  // Note the -1.
       shortSendBuf[i].push_back(perIndex);
 
       doubleSendBuf[i].push_back(volElem[indV].lenScale);
@@ -1628,14 +1524,13 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
       shortSendBuf[i].push_back(volElem[indV].nFaces);
       shortSendBuf[i].push_back(volElem[indV].timeLevel);
 
-      for(unsigned short k=0; k<volElem[indV].nDOFsGrid; ++k) {
+      for (unsigned short k = 0; k < volElem[indV].nDOFsGrid; ++k) {
         longSendBuf[i].push_back(volElem[indV].nodeIDsGrid[k]);
-        nodeIDs.push_back(CUnsignedLong2T(volElem[indV].nodeIDsGrid[k],
-                                          elemBuf[j].long1));
+        nodeIDs.push_back(CUnsignedLong2T(volElem[indV].nodeIDsGrid[k], elemBuf[j].long1));
       }
 
-      for(unsigned short k=0; k<volElem[indV].nFaces; ++k)
-        shortSendBuf[i].push_back((short) volElem[indV].JacFacesIsConsideredConstant[k]);
+      for (unsigned short k = 0; k < volElem[indV].nFaces; ++k)
+        shortSendBuf[i].push_back((short)volElem[indV].JacFacesIsConsideredConstant[k]);
     }
 
     /* Sort nodeIDs in increasing order and remove the double entities. */
@@ -1648,34 +1543,32 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
        periodic index, because an unsigned long cannot represent -1, the
        value for the periodic index when no peridicity is present. */
     longSendBuf[i].push_back(nodeIDs.size());
-    for(unsigned long j=0; j<nodeIDs.size(); ++j) {
+    for (unsigned long j = 0; j < nodeIDs.size(); ++j) {
       longSendBuf[i].push_back(nodeIDs[j].long0);
-      shortSendBuf[i].push_back( (short) nodeIDs[j].long1-1);
+      shortSendBuf[i].push_back((short)nodeIDs[j].long1 - 1);
     }
 
     /*--- Copy the coordinates to doubleSendBuf. ---*/
-    for(unsigned long j=0; j<nodeIDs.size(); ++j) {
-      map<unsigned long,unsigned long>::const_iterator LMI;
+    for (unsigned long j = 0; j < nodeIDs.size(); ++j) {
+      map<unsigned long, unsigned long>::const_iterator LMI;
       LMI = globalPointIDToLocalInd.find(nodeIDs[j].long0);
 
-      if(LMI == globalPointIDToLocalInd.end())
-        SU2_MPI::Error("Entry not found in map", CURRENT_FUNCTION);
+      if (LMI == globalPointIDToLocalInd.end()) SU2_MPI::Error("Entry not found in map", CURRENT_FUNCTION);
 
       unsigned long ind = LMI->second;
-      for(unsigned short l=0; l<nDim; ++l)
-        doubleSendBuf[i].push_back(meshPoints[ind].coor[l]);
+      for (unsigned short l = 0; l < nDim; ++l) doubleSendBuf[i].push_back(meshPoints[ind].coor[l]);
     }
 
     /*--- Send the communication buffers back to the calling rank.
           Only in parallel mode of course.     ---*/
 #ifdef HAVE_MPI
     int dest = sourceRank[i];
-    SU2_MPI::Isend(shortSendBuf[i].data(), shortSendBuf[i].size(), MPI_SHORT,
-                   dest, dest+1, SU2_MPI::GetComm(), &commReqs[3*i]);
-    SU2_MPI::Isend(longSendBuf[i].data(), longSendBuf[i].size(), MPI_LONG,
-                   dest, dest+2, SU2_MPI::GetComm(), &commReqs[3*i+1]);
-    SU2_MPI::Isend(doubleSendBuf[i].data(), doubleSendBuf[i].size(), MPI_DOUBLE,
-                   dest, dest+3, SU2_MPI::GetComm(), &commReqs[3*i+2]);
+    SU2_MPI::Isend(shortSendBuf[i].data(), shortSendBuf[i].size(), MPI_SHORT, dest, dest + 1, SU2_MPI::GetComm(),
+                   &commReqs[3 * i]);
+    SU2_MPI::Isend(longSendBuf[i].data(), longSendBuf[i].size(), MPI_LONG, dest, dest + 2, SU2_MPI::GetComm(),
+                   &commReqs[3 * i + 1]);
+    SU2_MPI::Isend(doubleSendBuf[i].data(), doubleSendBuf[i].size(), MPI_DOUBLE, dest, dest + 3, SU2_MPI::GetComm(),
+                   &commReqs[3 * i + 2]);
 #endif
   }
 
@@ -1695,12 +1588,11 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
 
   /* Parallel mode. Loop over the number of ranks from which I receive data
      in the return communication, i.e. nRankSend. */
-  for(int i=0; i<nRankSend; ++i) {
-
+  for (int i = 0; i < nRankSend; ++i) {
     /* Block until a message with shorts arrives from any processor.
        Determine the source and the size of the message.   */
     SU2_MPI::Status status;
-    SU2_MPI::Probe(MPI_ANY_SOURCE, rank+1, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Probe(MPI_ANY_SOURCE, rank + 1, SU2_MPI::GetComm(), &status);
     sourceRank[i] = status.MPI_SOURCE;
 
     int sizeMess;
@@ -1708,29 +1600,26 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
 
     /* Allocate the memory for the short receive buffer and receive the message. */
     shortRecvBuf[i].resize(sizeMess);
-    SU2_MPI::Recv(shortRecvBuf[i].data(), sizeMess, MPI_SHORT,
-                  sourceRank[i], rank+1, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Recv(shortRecvBuf[i].data(), sizeMess, MPI_SHORT, sourceRank[i], rank + 1, SU2_MPI::GetComm(), &status);
 
     /* Block until the corresponding message with longs arrives, determine
        its size, allocate the memory and receive the message. */
-    SU2_MPI::Probe(sourceRank[i], rank+2, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Probe(sourceRank[i], rank + 2, SU2_MPI::GetComm(), &status);
     SU2_MPI::Get_count(&status, MPI_LONG, &sizeMess);
     longRecvBuf[i].resize(sizeMess);
 
-    SU2_MPI::Recv(longRecvBuf[i].data(), sizeMess, MPI_LONG,
-                  sourceRank[i], rank+2, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Recv(longRecvBuf[i].data(), sizeMess, MPI_LONG, sourceRank[i], rank + 2, SU2_MPI::GetComm(), &status);
 
     /* Idem for the message with doubles. */
-    SU2_MPI::Probe(sourceRank[i], rank+3, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Probe(sourceRank[i], rank + 3, SU2_MPI::GetComm(), &status);
     SU2_MPI::Get_count(&status, MPI_DOUBLE, &sizeMess);
     doubleRecvBuf[i].resize(sizeMess);
 
-    SU2_MPI::Recv(doubleRecvBuf[i].data(), sizeMess, MPI_DOUBLE,
-                  sourceRank[i], rank+3, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Recv(doubleRecvBuf[i].data(), sizeMess, MPI_DOUBLE, sourceRank[i], rank + 3, SU2_MPI::GetComm(), &status);
   }
 
   /* Complete the non-blocking sends. */
-  SU2_MPI::Waitall(3*nRankRecv, commReqs.data(), MPI_STATUSES_IGNORE);
+  SU2_MPI::Waitall(3 * nRankRecv, commReqs.data(), MPI_STATUSES_IGNORE);
 
   /* Wild cards have been used in the communication,
      so synchronize the ranks to avoid problems.    */
@@ -1739,10 +1628,10 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
 #else
 
   /* Sequential mode. Simply copy the buffers. Note that nRankSend is at most 1. */
-  for(int i=0; i<nRankSend; ++i) {
-    sourceRank[i]    = i;
-    shortRecvBuf[i]  = shortSendBuf[i];
-    longRecvBuf[i]   = longSendBuf[i];
+  for (int i = 0; i < nRankSend; ++i) {
+    sourceRank[i] = i;
+    shortRecvBuf[i] = shortSendBuf[i];
+    longRecvBuf[i] = longSendBuf[i];
     doubleRecvBuf[i] = doubleSendBuf[i];
   }
 
@@ -1750,7 +1639,7 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
 
   /*--- Release the memory of the send buffers. To make sure that all
         the memory is deleted, the swap function is used. ---*/
-  for(int i=0; i<nRankRecv; ++i) {
+  for (int i = 0; i < nRankRecv; ++i) {
     vector<short>().swap(shortSendBuf[i]);
     vector<long>().swap(longSendBuf[i]);
     vector<su2double>().swap(doubleSendBuf[i]);
@@ -1768,12 +1657,12 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
   vector<CLong3T> haloElemInfo;
   haloElemInfo.reserve(nVolElemTot - nVolElemOwned);
 
-  for(int i=0; i<nRankSend; ++i) {
+  for (int i = 0; i < nRankSend; ++i) {
     unsigned long indS = 0;
 
-    for(long j=0; j<longRecvBuf[i][0]; ++j) {
-      const unsigned short nFaces = shortRecvBuf[i][indS+6];
-      haloElemInfo.push_back(CLong3T(shortRecvBuf[i][indS+7], sourceRank[i], j));
+    for (long j = 0; j < longRecvBuf[i][0]; ++j) {
+      const unsigned short nFaces = shortRecvBuf[i][indS + 6];
+      haloElemInfo.push_back(CLong3T(shortRecvBuf[i][indS + 7], sourceRank[i], j));
       indS += nFaces + 8;
     }
   }
@@ -1783,18 +1672,16 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
   /*--- Loop over the receive buffers to store the information of the
         halo elements and the halo points. ---*/
   vector<CPointFEM> haloPoints;
-  for(int i=0; i<nRankSend; ++i) {
-
+  for (int i = 0; i < nRankSend; ++i) {
     /* Initialization of the indices in the communication buffers. */
     unsigned long indL = 1, indS = 0, indD = 0;
 
     /* Loop over the halo elements received from this rank. */
-    for(long j=0; j<longRecvBuf[i][0]; ++j) {
-
+    for (long j = 0; j < longRecvBuf[i][0]; ++j) {
       /* Create an object of CLong3T and search for its position
          in haloElemInfo to determine the index in volElem, where
          this element is stored. */
-      CLong3T thisElem(shortRecvBuf[i][indS+7], sourceRank[i], j);
+      CLong3T thisElem(shortRecvBuf[i][indS + 7], sourceRank[i], j);
       vector<CLong3T>::iterator low;
       low = lower_bound(haloElemInfo.begin(), haloElemInfo.end(), thisElem);
 
@@ -1806,27 +1693,27 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
       volElem[indV].rankOriginal = sourceRank[i];
 
       volElem[indV].periodIndexToDonor = shortRecvBuf[i][indS++];
-      volElem[indV].VTK_Type           = shortRecvBuf[i][indS++];
-      volElem[indV].nPolyGrid          = shortRecvBuf[i][indS++];
-      volElem[indV].nPolySol           = shortRecvBuf[i][indS++];
-      volElem[indV].nDOFsGrid          = shortRecvBuf[i][indS++];
-      volElem[indV].nDOFsSol           = shortRecvBuf[i][indS++];
-      volElem[indV].nFaces             = shortRecvBuf[i][indS++];
-      volElem[indV].timeLevel          = shortRecvBuf[i][indS++];
+      volElem[indV].VTK_Type = shortRecvBuf[i][indS++];
+      volElem[indV].nPolyGrid = shortRecvBuf[i][indS++];
+      volElem[indV].nPolySol = shortRecvBuf[i][indS++];
+      volElem[indV].nDOFsGrid = shortRecvBuf[i][indS++];
+      volElem[indV].nDOFsSol = shortRecvBuf[i][indS++];
+      volElem[indV].nFaces = shortRecvBuf[i][indS++];
+      volElem[indV].timeLevel = shortRecvBuf[i][indS++];
 
       volElem[indV].nodeIDsGrid.resize(volElem[indV].nDOFsGrid);
-      for(unsigned short k=0; k<volElem[indV].nDOFsGrid; ++k)
+      for (unsigned short k = 0; k < volElem[indV].nDOFsGrid; ++k)
         volElem[indV].nodeIDsGrid[k] = longRecvBuf[i][indL++];
 
       volElem[indV].JacFacesIsConsideredConstant.resize(volElem[indV].nFaces);
-      for(unsigned short k=0; k<volElem[indV].nFaces; ++k)
-        volElem[indV].JacFacesIsConsideredConstant[k] = (bool) shortRecvBuf[i][indS++];
+      for (unsigned short k = 0; k < volElem[indV].nFaces; ++k)
+        volElem[indV].JacFacesIsConsideredConstant[k] = (bool)shortRecvBuf[i][indS++];
 
       /* Give the member variables that are not obtained via communication their
          values. Some of these variables are not used for halo elements. */
-      volElem[indV].elemIsOwned             = false;
+      volElem[indV].elemIsOwned = false;
       volElem[indV].JacIsConsideredConstant = false;
-      volElem[indV].offsetDOFsSolGlobal     = ULONG_MAX;
+      volElem[indV].offsetDOFsSolGlobal = ULONG_MAX;
 
       /* Halo elements do not own a face per definition. */
       volElem[indV].ElementOwnsFaces.assign(volElem[indV].nFaces, false);
@@ -1837,12 +1724,11 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
 
     /* Store the information of the points in haloPoints. */
     const long nPointsThisRank = longRecvBuf[i][indL++];
-    for(long j=0; j<nPointsThisRank; ++j) {
+    for (long j = 0; j < nPointsThisRank; ++j) {
       CPointFEM thisPoint;
-      thisPoint.globalID           = longRecvBuf[i][indL++];
+      thisPoint.globalID = longRecvBuf[i][indL++];
       thisPoint.periodIndexToDonor = shortRecvBuf[i][indS++];
-      for(unsigned short l=0; l<nDim; ++l)
-        thisPoint.coor[l] = doubleRecvBuf[i][indD++];
+      for (unsigned short l = 0; l < nDim; ++l) thisPoint.coor[l] = doubleRecvBuf[i][indD++];
 
       haloPoints.push_back(thisPoint);
     }
@@ -1862,18 +1748,18 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
   /* Initialization of some variables to sort the halo points. */
   Global_nPoint = geometry->GetGlobal_nPoint();
   unsigned long InvalidPointID = Global_nPoint + 10;
-  short         InvalidPerInd  = SHRT_MAX;
+  short InvalidPerInd = SHRT_MAX;
 
   /*--- Search for the nonperiodic halo points in the local points to see
         if these points are already stored on this rank. If this is the
         case invalidate this halo and decrease the number of halo points.
         Afterwards remove the invalid halos from the vector.       ---*/
   unsigned long nHaloPoints = haloPoints.size();
-  for(unsigned long i=0; i<haloPoints.size(); ++i) {
-    if(haloPoints[i].periodIndexToDonor != -1) break;  // Test for nonperiodic.
+  for (unsigned long i = 0; i < haloPoints.size(); ++i) {
+    if (haloPoints[i].periodIndexToDonor != -1) break;  // Test for nonperiodic.
 
-    if( binary_search(meshPoints.begin(), meshPoints.end(), haloPoints[i]) ) {
-      haloPoints[i].globalID           = InvalidPointID;
+    if (binary_search(meshPoints.begin(), meshPoints.end(), haloPoints[i])) {
+      haloPoints[i].globalID = InvalidPointID;
       haloPoints[i].periodIndexToDonor = InvalidPerInd;
       --nHaloPoints;
     }
@@ -1887,8 +1773,8 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
      this is an upper bound. Add the non-periodic halo points to meshPoints. */
   meshPoints.reserve(meshPoints.size() + nHaloPoints);
 
-  for(unsigned long i=0; i<haloPoints.size(); ++i) {
-    if(haloPoints[i].periodIndexToDonor != -1) break;  // Test for nonperiodic.
+  for (unsigned long i = 0; i < haloPoints.size(); ++i) {
+    if (haloPoints[i].periodIndexToDonor != -1) break;  // Test for nonperiodic.
 
     meshPoints.push_back(haloPoints[i]);
   }
@@ -1897,22 +1783,21 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
      index in the vector meshPoints. First store the points already present
      in meshPoints. */
   map<CUnsignedLong2T, unsigned long> mapGlobalPointIDToInd;
-  for(unsigned long i=0; i<meshPoints.size(); ++i) {
+  for (unsigned long i = 0; i < meshPoints.size(); ++i) {
     CUnsignedLong2T globIndAndPer;
     globIndAndPer.long0 = meshPoints[i].globalID;
-    globIndAndPer.long1 = meshPoints[i].periodIndexToDonor+1;  // Note the +1 again.
+    globIndAndPer.long1 = meshPoints[i].periodIndexToDonor + 1;  // Note the +1 again.
 
     mapGlobalPointIDToInd[globIndAndPer] = i;
   }
 
   /*--- Convert the global indices in the boundary connectivities to local ones.
         Note that the volume ID's already contain the local number. ---*/
-  for(unsigned short iMarker=0; iMarker<nMarker; ++iMarker) {
-    for(unsigned long i=0; i<boundaries[iMarker].surfElem.size(); ++i) {
-
+  for (unsigned short iMarker = 0; iMarker < nMarker; ++iMarker) {
+    for (unsigned long i = 0; i < boundaries[iMarker].surfElem.size(); ++i) {
       /* Convert the global node ID's to local values. Note that for these node
          ID's no periodic transformation can be present. */
-      for(unsigned short j=0; j<boundaries[iMarker].surfElem[i].nDOFsGrid; ++j) {
+      for (unsigned short j = 0; j < boundaries[iMarker].surfElem[i].nDOFsGrid; ++j) {
         CUnsignedLong2T searchItem(boundaries[iMarker].surfElem[i].nodeIDsGrid[j], 0);
         map<CUnsignedLong2T, unsigned long>::const_iterator LLMI;
         LLMI = mapGlobalPointIDToInd.find(searchItem);
@@ -1924,53 +1809,46 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
   /*--- The only halo points that must be added to meshPoints are the periodic
         halo points. It must be checked whether or not the periodic points in
         haloPoints match with points in meshPoints. This is done below. ---*/
-  for(unsigned long iLow=0; iLow<haloPoints.size(); ) {
-
+  for (unsigned long iLow = 0; iLow < haloPoints.size();) {
     /* Determine the upper index for this periodic transformation. */
     unsigned long iUpp;
-    for(iUpp=iLow+1; iUpp<haloPoints.size(); ++iUpp)
-      if(haloPoints[iUpp].periodIndexToDonor != haloPoints[iLow].periodIndexToDonor) break;
+    for (iUpp = iLow + 1; iUpp < haloPoints.size(); ++iUpp)
+      if (haloPoints[iUpp].periodIndexToDonor != haloPoints[iLow].periodIndexToDonor) break;
 
     /* Check for a true periodic index. */
     short perIndex = haloPoints[iLow].periodIndexToDonor;
-    if(perIndex != -1) {
-
+    if (perIndex != -1) {
       /* Easier storage of the surface elements. */
-      vector<CSurfaceElementFEM> &surfElem = boundaries[perIndex].surfElem;
+      vector<CSurfaceElementFEM>& surfElem = boundaries[perIndex].surfElem;
 
       /*--- In the loop below the coordinates of the points of this local
             periodic boundary as well as a matching tolerance are determined.
             A vector of point ID's is also created, which is needed later on
             when it is checked whether or not a matching point is already
             stored in meshPoints. ---*/
-      vector<long>          indInPoints(meshPoints.size(), -1);
+      vector<long> indInPoints(meshPoints.size(), -1);
       vector<unsigned long> IDsPoints;
-      vector<su2double>     coordPoints;
-      vector<su2double>     tolPoints;
-
-      for(unsigned long j=0; j<surfElem.size(); ++j) {
+      vector<su2double> coordPoints;
+      vector<su2double> tolPoints;
 
+      for (unsigned long j = 0; j < surfElem.size(); ++j) {
         /* Determine the tolerance for equal points, which is a small value
            times the length scale of the adjacent volume element. */
-        const su2double tolElem = 1.e-2*volElem[surfElem[j].volElemID].lenScale;
+        const su2double tolElem = 1.e-2 * volElem[surfElem[j].volElemID].lenScale;
 
         /* Loop over the nodes of this surface grid and update the points on
            this periodic boundary. */
-        for(unsigned short k=0; k<surfElem[j].nDOFsGrid; ++k) {
+        for (unsigned short k = 0; k < surfElem[j].nDOFsGrid; ++k) {
           unsigned long nn = surfElem[j].nodeIDsGrid[k];
 
-          if(indInPoints[nn] == -1) {
-
+          if (indInPoints[nn] == -1) {
             /* Point is not stored yet in pointsBoundary. Do so now. */
             indInPoints[nn] = IDsPoints.size();
             IDsPoints.push_back(nn);
             tolPoints.push_back(tolElem);
 
-            for(unsigned short l=0; l<nDim; ++l)
-              coordPoints.push_back(meshPoints[nn].coor[l]);
-          }
-          else {
-
+            for (unsigned short l = 0; l < nDim; ++l) coordPoints.push_back(meshPoints[nn].coor[l]);
+          } else {
             /* Point is already stored. Update the tolerance. */
             nn = indInPoints[nn];
             tolPoints[nn] = min(tolPoints[nn], tolElem);
@@ -1979,27 +1857,24 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
       }
 
       /* Create a local ADT of the points on the periodic boundary. */
-      CADTPointsOnlyClass periodicADT(nDim, IDsPoints.size(), coordPoints.data(),
-                                      IDsPoints.data(), false);
+      CADTPointsOnlyClass periodicADT(nDim, IDsPoints.size(), coordPoints.data(), IDsPoints.data(), false);
 
       /* Get the data for the periodic transformation to the donor. */
       auto center = config->GetPeriodicRotCenter(config->GetMarker_All_TagBound(perIndex));
       auto angles = config->GetPeriodicRotAngles(config->GetMarker_All_TagBound(perIndex));
-      auto trans  = config->GetPeriodicTranslation(config->GetMarker_All_TagBound(perIndex));
+      auto trans = config->GetPeriodicTranslation(config->GetMarker_All_TagBound(perIndex));
 
       /*--- Compute the rotation matrix and translation vector for the
             transformation from the donor. This is the transpose of the
             transformation to the donor. ---*/
 
       /* Store (center-trans) as it is constant and will be added on. */
-      su2double translation[] = {center[0] - trans[0],
-                                 center[1] - trans[1],
-                                 center[2] - trans[2]};
+      su2double translation[] = {center[0] - trans[0], center[1] - trans[1], center[2] - trans[2]};
 
       /* Store angles separately for clarity. Compute sines/cosines. */
       su2double theta = angles[0];
-      su2double phi   = angles[1];
-      su2double psi   = angles[2];
+      su2double phi = angles[1];
+      su2double psi = angles[2];
 
       su2double cosTheta = cos(theta), cosPhi = cos(phi), cosPsi = cos(psi);
       su2double sinTheta = sin(theta), sinPhi = sin(phi), sinPsi = sin(psi);
@@ -2007,65 +1882,57 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
       /* Compute the rotation matrix. Note that the implicit
          ordering is rotation about the x-axis, y-axis, then z-axis. */
       su2double rotMatrix[3][3];
-      rotMatrix[0][0] =  cosPhi*cosPsi;
-      rotMatrix[0][1] =  cosPhi*sinPsi;
+      rotMatrix[0][0] = cosPhi * cosPsi;
+      rotMatrix[0][1] = cosPhi * sinPsi;
       rotMatrix[0][2] = -sinPhi;
 
-      rotMatrix[1][0] = sinTheta*sinPhi*cosPsi - cosTheta*sinPsi;
-      rotMatrix[1][1] = sinTheta*sinPhi*sinPsi + cosTheta*cosPsi;
-      rotMatrix[1][2] = sinTheta*cosPhi;
+      rotMatrix[1][0] = sinTheta * sinPhi * cosPsi - cosTheta * sinPsi;
+      rotMatrix[1][1] = sinTheta * sinPhi * sinPsi + cosTheta * cosPsi;
+      rotMatrix[1][2] = sinTheta * cosPhi;
 
-      rotMatrix[2][0] = cosTheta*sinPhi*cosPsi + sinTheta*sinPsi;
-      rotMatrix[2][1] = cosTheta*sinPhi*sinPsi - sinTheta*cosPsi;
-      rotMatrix[2][2] = cosTheta*cosPhi;
+      rotMatrix[2][0] = cosTheta * sinPhi * cosPsi + sinTheta * sinPsi;
+      rotMatrix[2][1] = cosTheta * sinPhi * sinPsi - sinTheta * cosPsi;
+      rotMatrix[2][2] = cosTheta * cosPhi;
 
       /* Loop over the halo points for this periodic transformation. */
-      for(unsigned long i=iLow; i<iUpp; ++i) {
-
+      for (unsigned long i = iLow; i < iUpp; ++i) {
         /* Apply the periodic transformation to the coordinates
            stored in this halo point. */
-        su2double dx =             haloPoints[i].coor[0] - center[0];
-        su2double dy =             haloPoints[i].coor[1] - center[1];
+        su2double dx = haloPoints[i].coor[0] - center[0];
+        su2double dy = haloPoints[i].coor[1] - center[1];
         su2double dz = nDim == 3 ? haloPoints[i].coor[2] - center[2] : su2double(0.0);
 
-        haloPoints[i].coor[0] = rotMatrix[0][0]*dx + rotMatrix[0][1]*dy
-                              + rotMatrix[0][2]*dz + translation[0];
-        haloPoints[i].coor[1] = rotMatrix[1][0]*dx + rotMatrix[1][1]*dy
-                              + rotMatrix[1][2]*dz + translation[1];
-        haloPoints[i].coor[2] = rotMatrix[2][0]*dx + rotMatrix[2][1]*dy
-                              + rotMatrix[2][2]*dz + translation[2];
+        haloPoints[i].coor[0] = rotMatrix[0][0] * dx + rotMatrix[0][1] * dy + rotMatrix[0][2] * dz + translation[0];
+        haloPoints[i].coor[1] = rotMatrix[1][0] * dx + rotMatrix[1][1] * dy + rotMatrix[1][2] * dz + translation[1];
+        haloPoints[i].coor[2] = rotMatrix[2][0] * dx + rotMatrix[2][1] * dy + rotMatrix[2][2] * dz + translation[2];
 
         /* Search for the nearest coordinate in the ADT. */
         su2double dist;
         unsigned long pointID;
         int rankID;
 
-        periodicADT.DetermineNearestNode(haloPoints[i].coor, dist,
-                                         pointID, rankID);
+        periodicADT.DetermineNearestNode(haloPoints[i].coor, dist, pointID, rankID);
 
         /* Check whether the distance is less equal to the tolerance for
            a matching point. */
         const unsigned long nn = indInPoints[pointID];
-        if(dist <= tolPoints[nn]) {
-
+        if (dist <= tolPoints[nn]) {
           /* The distance to the nearest point is less than the tolerance,
              hence this periodically transformed point is present on the
              boundary. Store it as such in the map mapGlobalPointIDToInd. */
           CUnsignedLong2T globIndAndPer;
           globIndAndPer.long0 = haloPoints[i].globalID;
-          globIndAndPer.long1 = haloPoints[i].periodIndexToDonor+1;  // Note the +1 again.
+          globIndAndPer.long1 = haloPoints[i].periodIndexToDonor + 1;  // Note the +1 again.
 
           mapGlobalPointIDToInd[globIndAndPer] = pointID;
-        }
-        else {
-
+        } else {
           /* The distance to the nearest point is larger than the tolerance,
              hence this periodically transformed point is not present yet on
              this rank. Store it in the mapping to the local points and
              create it in meshPoints. */
           CUnsignedLong2T globIndAndPer;
           globIndAndPer.long0 = haloPoints[i].globalID;
-          globIndAndPer.long1 = haloPoints[i].periodIndexToDonor+1;  // Note the +1 again.
+          globIndAndPer.long1 = haloPoints[i].periodIndexToDonor + 1;  // Note the +1 again.
 
           mapGlobalPointIDToInd[globIndAndPer] = meshPoints.size();
           meshPoints.push_back(haloPoints[i]);
@@ -2082,10 +1949,10 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
         of the element relative to the largest time step of an element in the mesh.
         This value can only differ from 1 when time accurate local time stepping is
         used. ---*/
-  for(unsigned long i=0; i<nVolElemTot; ++i) {
-    for(unsigned short j=0; j<volElem[i].nDOFsGrid; ++j) {
+  for (unsigned long i = 0; i < nVolElemTot; ++i) {
+    for (unsigned short j = 0; j < volElem[i].nDOFsGrid; ++j) {
       CUnsignedLong2T searchItem(volElem[i].nodeIDsGrid[j],
-                                 volElem[i].periodIndexToDonor+1); // Again the +1.
+                                 volElem[i].periodIndexToDonor + 1);  // Again the +1.
       map<CUnsignedLong2T, unsigned long>::const_iterator LLMI;
       LLMI = mapGlobalPointIDToInd.find(searchItem);
       volElem[i].nodeIDsGrid[j] = LLMI->second;
@@ -2097,91 +1964,83 @@ CMeshFEM::CMeshFEM(CGeometry *geometry, CConfig *config) {
 
   /* Determine the number of halo elements per time level in cumulative
      storage format. */
-  nVolElemHaloPerTimeLevel.assign(nTimeLevels+1, 0);
-  for(unsigned long i=nVolElemOwned; i<nVolElemTot; ++i)
-    ++nVolElemHaloPerTimeLevel[volElem[i].timeLevel+1];
+  nVolElemHaloPerTimeLevel.assign(nTimeLevels + 1, 0);
+  for (unsigned long i = nVolElemOwned; i < nVolElemTot; ++i) ++nVolElemHaloPerTimeLevel[volElem[i].timeLevel + 1];
 
   nVolElemHaloPerTimeLevel[0] = nVolElemOwned;
-  for(unsigned short i=0; i<nTimeLevels; ++i)
-    nVolElemHaloPerTimeLevel[i+1] += nVolElemHaloPerTimeLevel[i];
+  for (unsigned short i = 0; i < nTimeLevels; ++i) nVolElemHaloPerTimeLevel[i + 1] += nVolElemHaloPerTimeLevel[i];
 }
 
-void CMeshFEM::ComputeGradientsCoordinatesFace(const unsigned short nIntegration,
-                                               const unsigned short nDOFs,
-                                               const su2double      *matDerBasisInt,
-                                               const unsigned long  *DOFs,
-                                               su2double            *derivCoor,
-                                               CConfig              *config) {
-
+void CMeshFEM::ComputeGradientsCoordinatesFace(const unsigned short nIntegration, const unsigned short nDOFs,
+                                               const su2double* matDerBasisInt, const unsigned long* DOFs,
+                                               su2double* derivCoor, CConfig* config) {
   /* Allocate the memory to store the values of dxdr, dydr, etc. */
-  vector<su2double> helpDxdrVec(nIntegration*nDim*nDim);
-  su2double *dxdrVec = helpDxdrVec.data();
+  vector<su2double> helpDxdrVec(nIntegration * nDim * nDim);
+  su2double* dxdrVec = helpDxdrVec.data();
 
   /* Determine the gradients of the Cartesian coordinates w.r.t. the
      parametric coordinates. */
-  ComputeGradientsCoorWRTParam(nIntegration, nDOFs, matDerBasisInt, DOFs,
-                               dxdrVec, config);
+  ComputeGradientsCoorWRTParam(nIntegration, nDOFs, matDerBasisInt, DOFs, dxdrVec, config);
 
   /* Make a distinction between 2D and 3D to compute the derivatives drdx,
      drdy, etc. */
-  switch( nDim ) {
+  switch (nDim) {
     case 2: {
       /* 2D computation. Store the offset between the r and s derivatives. */
-      const unsigned short off = 2*nIntegration;
+      const unsigned short off = 2 * nIntegration;
 
       /* Loop over the integration points. */
       unsigned short ii = 0;
-      for(unsigned short j=0; j<nIntegration; ++j) {
-
+      for (unsigned short j = 0; j < nIntegration; ++j) {
         /* Retrieve the values of dxdr, dydr, dxds and dyds from dxdrVec
            in this integration point. */
-        const unsigned short jx = 2*j; const unsigned short jy = jx+1;
-        const su2double dxdr = dxdrVec[jx],     dydr = dxdrVec[jy];
-        const su2double dxds = dxdrVec[jx+off], dyds = dxdrVec[jy+off];
+        const unsigned short jx = 2 * j;
+        const unsigned short jy = jx + 1;
+        const su2double dxdr = dxdrVec[jx], dydr = dxdrVec[jy];
+        const su2double dxds = dxdrVec[jx + off], dyds = dxdrVec[jy + off];
 
         /* Compute the inverse relations drdx, drdy, dsdx, dsdy. */
-        const su2double Jinv = 1.0/(dxdr*dyds - dxds*dydr);
+        const su2double Jinv = 1.0 / (dxdr * dyds - dxds * dydr);
 
-        derivCoor[ii++] =  dyds*Jinv;  // drdx
-        derivCoor[ii++] = -dxds*Jinv;  // drdy
-        derivCoor[ii++] = -dydr*Jinv;  // dsdx
-        derivCoor[ii++] =  dxdr*Jinv;  // dsdy
+        derivCoor[ii++] = dyds * Jinv;   // drdx
+        derivCoor[ii++] = -dxds * Jinv;  // drdy
+        derivCoor[ii++] = -dydr * Jinv;  // dsdx
+        derivCoor[ii++] = dxdr * Jinv;   // dsdy
       }
       break;
     }
 
     case 3: {
       /* 3D computation. Store the offset between the r and s and r and t derivatives. */
-      const unsigned short offS = 3*nIntegration, offT = 6*nIntegration;
+      const unsigned short offS = 3 * nIntegration, offT = 6 * nIntegration;
 
       /* Loop over the integration points. */
       unsigned short ii = 0;
-      for(unsigned short j=0; j<nIntegration; ++j) {
-
+      for (unsigned short j = 0; j < nIntegration; ++j) {
         /* Retrieve the values of dxdr, dydr, dzdr, dxds, dyds, dzds, dxdt, dydt
            and dzdt from dxdrVec in this integration point. */
-        const unsigned short jx = 3*j; const unsigned short jy = jx+1, jz = jx+2;
-        const su2double dxdr = dxdrVec[jx],      dydr = dxdrVec[jy],      dzdr = dxdrVec[jz];
-        const su2double dxds = dxdrVec[jx+offS], dyds = dxdrVec[jy+offS], dzds = dxdrVec[jz+offS];
-        const su2double dxdt = dxdrVec[jx+offT], dydt = dxdrVec[jy+offT], dzdt = dxdrVec[jz+offT];
+        const unsigned short jx = 3 * j;
+        const unsigned short jy = jx + 1, jz = jx + 2;
+        const su2double dxdr = dxdrVec[jx], dydr = dxdrVec[jy], dzdr = dxdrVec[jz];
+        const su2double dxds = dxdrVec[jx + offS], dyds = dxdrVec[jy + offS], dzds = dxdrVec[jz + offS];
+        const su2double dxdt = dxdrVec[jx + offT], dydt = dxdrVec[jy + offT], dzdt = dxdrVec[jz + offT];
 
         /* Compute the inverse relations drdx, drdy, drdz, dsdx, dsdy, dsdz,
            dtdx, dtdy, dtdz. */
-        const su2double Jinv = 1.0/(dxdr*(dyds*dzdt - dzds*dydt)
-                             -      dxds*(dydr*dzdt - dzdr*dydt)
-                             +      dxdt*(dydr*dzds - dzdr*dyds));
+        const su2double Jinv = 1.0 / (dxdr * (dyds * dzdt - dzds * dydt) - dxds * (dydr * dzdt - dzdr * dydt) +
+                                      dxdt * (dydr * dzds - dzdr * dyds));
 
-        derivCoor[ii++] = (dyds*dzdt - dzds*dydt)*Jinv;  // drdx
-        derivCoor[ii++] = (dzds*dxdt - dxds*dzdt)*Jinv;  // drdy
-        derivCoor[ii++] = (dxds*dydt - dyds*dxdt)*Jinv;  // drdz
+        derivCoor[ii++] = (dyds * dzdt - dzds * dydt) * Jinv;  // drdx
+        derivCoor[ii++] = (dzds * dxdt - dxds * dzdt) * Jinv;  // drdy
+        derivCoor[ii++] = (dxds * dydt - dyds * dxdt) * Jinv;  // drdz
 
-        derivCoor[ii++] = (dzdr*dydt - dydr*dzdt)*Jinv;  // dsdx
-        derivCoor[ii++] = (dxdr*dzdt - dzdr*dxdt)*Jinv;  // dsdy
-        derivCoor[ii++] = (dydr*dxdt - dxdr*dydt)*Jinv;  // dsdz
+        derivCoor[ii++] = (dzdr * dydt - dydr * dzdt) * Jinv;  // dsdx
+        derivCoor[ii++] = (dxdr * dzdt - dzdr * dxdt) * Jinv;  // dsdy
+        derivCoor[ii++] = (dydr * dxdt - dxdr * dydt) * Jinv;  // dsdz
 
-        derivCoor[ii++] = (dydr*dzds - dzdr*dyds)*Jinv;  // dtdx
-        derivCoor[ii++] = (dzdr*dxds - dxdr*dzds)*Jinv;  // dtdy
-        derivCoor[ii++] = (dxdr*dyds - dydr*dxds)*Jinv;  // dtdz
+        derivCoor[ii++] = (dydr * dzds - dzdr * dyds) * Jinv;  // dtdx
+        derivCoor[ii++] = (dzdr * dxds - dxdr * dzds) * Jinv;  // dtdy
+        derivCoor[ii++] = (dxdr * dyds - dydr * dxds) * Jinv;  // dtdz
       }
 
       break;
@@ -2189,70 +2048,58 @@ void CMeshFEM::ComputeGradientsCoordinatesFace(const unsigned short nIntegration
   }
 }
 
-void CMeshFEM::ComputeGradientsCoorWRTParam(const unsigned short nIntegration,
-                                            const unsigned short nDOFs,
-                                            const su2double      *matDerBasisInt,
-                                            const unsigned long  *DOFs,
-                                            su2double            *derivCoor,
-                                            CConfig              *config) {
-
+void CMeshFEM::ComputeGradientsCoorWRTParam(const unsigned short nIntegration, const unsigned short nDOFs,
+                                            const su2double* matDerBasisInt, const unsigned long* DOFs,
+                                            su2double* derivCoor, CConfig* config) {
   /* Allocate the memory to store the coordinates as right hand side. */
-  vector<su2double> vecRHS(nDOFs*nDim);
+  vector<su2double> vecRHS(nDOFs * nDim);
 
   /* Loop over the grid DOFs of the element and copy the coordinates in
      vecRHS in row major order. */
   unsigned long ic = 0;
-  for(unsigned short j=0; j<nDOFs; ++j) {
-    for(unsigned short k=0; k<nDim; ++k, ++ic)
-      vecRHS[ic] = meshPoints[DOFs[j]].coor[k];
+  for (unsigned short j = 0; j < nDOFs; ++j) {
+    for (unsigned short k = 0; k < nDim; ++k, ++ic) vecRHS[ic] = meshPoints[DOFs[j]].coor[k];
   }
 
   /* Carry out the matrix matrix product The last argument is NULL, such
      that this gemm call is ignored in the profiling. Replace by config if
      if should be included. */
-  blasFunctions->gemm(nDim*nIntegration, nDim, nDOFs, matDerBasisInt,
-                      vecRHS.data(), derivCoor, nullptr);
+  blasFunctions->gemm(nDim * nIntegration, nDim, nDOFs, matDerBasisInt, vecRHS.data(), derivCoor, nullptr);
 }
 
-void CMeshFEM::ComputeNormalsFace(const unsigned short nIntegration,
-                                  const unsigned short nDOFs,
-                                  const su2double      *dr,
-                                  const su2double      *ds,
-                                  const unsigned long  *DOFs,
-                                  su2double            *normals) {
-
+void CMeshFEM::ComputeNormalsFace(const unsigned short nIntegration, const unsigned short nDOFs, const su2double* dr,
+                                  const su2double* ds, const unsigned long* DOFs, su2double* normals) {
   /* Initialize the counter ii to 0. ii is the index in normals where the
      information is stored. */
   unsigned int ii = 0;
 
   /* Make a distinction between 2D and 3D. */
-  switch( nDim ) {
+  switch (nDim) {
     case 2: {
       /* 2D computation. Loop over the integration points of the face. */
-      for(unsigned short j=0; j<nIntegration; ++j) {
-
+      for (unsigned short j = 0; j < nIntegration; ++j) {
         /*--- Loop over the number of DOFs of the face to compute dxdr
               and dydr. ---*/
-        const su2double *drr = &dr[j*nDOFs];
+        const su2double* drr = &dr[j * nDOFs];
         su2double dxdr = 0.0, dydr = 0.0;
-        for(unsigned short k=0; k<nDOFs; ++k) {
-          dxdr += drr[k]*meshPoints[DOFs[k]].coor[0];
-          dydr += drr[k]*meshPoints[DOFs[k]].coor[1];
+        for (unsigned short k = 0; k < nDOFs; ++k) {
+          dxdr += drr[k] * meshPoints[DOFs[k]].coor[0];
+          dydr += drr[k] * meshPoints[DOFs[k]].coor[1];
         }
 
         /* Determine the length of the tangential vector (dxdr, dydr), which
            is also the length of the corresponding normal vector. Also compute
            the inverse of the length. Make sure that a division by zero is
            avoided, although this is most likely never active. */
-        const su2double lenNorm    = sqrt(dxdr*dxdr + dydr*dydr);
-        const su2double invLenNorm = lenNorm < su2double(1.e-35) ? su2double(1.e+35) : 1.0/lenNorm;
+        const su2double lenNorm = sqrt(dxdr * dxdr + dydr * dydr);
+        const su2double invLenNorm = lenNorm < su2double(1.e-35) ? su2double(1.e+35) : 1.0 / lenNorm;
 
         /* Store the corresponding unit normal vector and its length. The
            direction of the normal vector is such that it is outward pointing
            for the element on side 0 of the face. */
-        normals[ii++] =  dydr*invLenNorm;
-        normals[ii++] = -dxdr*invLenNorm;
-        normals[ii++] =  lenNorm;
+        normals[ii++] = dydr * invLenNorm;
+        normals[ii++] = -dxdr * invLenNorm;
+        normals[ii++] = lenNorm;
       }
 
       break;
@@ -2260,33 +2107,31 @@ void CMeshFEM::ComputeNormalsFace(const unsigned short nIntegration,
 
     case 3: {
       /* 3D computation. Loop over the integration points of the face. */
-      for(unsigned short j=0; j<nIntegration; ++j) {
-
+      for (unsigned short j = 0; j < nIntegration; ++j) {
         /*--- Loop over the number of DOFs of the face to compute dxdr,
               dxds, dydr, dyds, dzdr and dzds. ---*/
-        const su2double *drr = &dr[j*nDOFs], *dss = &ds[j*nDOFs];
-        su2double dxdr = 0.0, dydr = 0.0, dzdr = 0.0,
-                  dxds = 0.0, dyds = 0.0, dzds = 0.0;
-        for(unsigned short k=0; k<nDOFs; ++k) {
-          dxdr += drr[k]*meshPoints[DOFs[k]].coor[0];
-          dydr += drr[k]*meshPoints[DOFs[k]].coor[1];
-          dzdr += drr[k]*meshPoints[DOFs[k]].coor[2];
-
-          dxds += dss[k]*meshPoints[DOFs[k]].coor[0];
-          dyds += dss[k]*meshPoints[DOFs[k]].coor[1];
-          dzds += dss[k]*meshPoints[DOFs[k]].coor[2];
+        const su2double *drr = &dr[j * nDOFs], *dss = &ds[j * nDOFs];
+        su2double dxdr = 0.0, dydr = 0.0, dzdr = 0.0, dxds = 0.0, dyds = 0.0, dzds = 0.0;
+        for (unsigned short k = 0; k < nDOFs; ++k) {
+          dxdr += drr[k] * meshPoints[DOFs[k]].coor[0];
+          dydr += drr[k] * meshPoints[DOFs[k]].coor[1];
+          dzdr += drr[k] * meshPoints[DOFs[k]].coor[2];
+
+          dxds += dss[k] * meshPoints[DOFs[k]].coor[0];
+          dyds += dss[k] * meshPoints[DOFs[k]].coor[1];
+          dzds += dss[k] * meshPoints[DOFs[k]].coor[2];
         }
 
         /* Compute the vector product dxdr X dxds, where x is the coordinate
            vector (x,y,z). Compute the length of this vector, which is an area,
            as well as the inverse.  Make sure that a division by zero is
            avoided, although this is most likely never active. */
-        const su2double nx = dydr*dzds - dyds*dzdr;
-        const su2double ny = dxds*dzdr - dxdr*dzds;
-        const su2double nz = dxdr*dyds - dxds*dydr;
+        const su2double nx = dydr * dzds - dyds * dzdr;
+        const su2double ny = dxds * dzdr - dxdr * dzds;
+        const su2double nz = dxdr * dyds - dxds * dydr;
 
-        const su2double lenNorm    = sqrt(nx*nx + ny*ny + nz*nz);
-        const su2double invLenNorm = lenNorm < su2double(1.e-35) ? su2double(1.e+35) : 1.0/lenNorm;
+        const su2double lenNorm = sqrt(nx * nx + ny * ny + nz * nz);
+        const su2double invLenNorm = lenNorm < su2double(1.e-35) ? su2double(1.e+35) : 1.0 / lenNorm;
 
         /* Store the components of the unit normal as well as its length in the
            normals. Note that the current direction of the normal is pointing
@@ -2294,25 +2139,23 @@ void CMeshFEM::ComputeNormalsFace(const unsigned short nIntegration,
            in the actual computation of the integral over the faces, it is
            assumed that the vector points in the opposite direction.
            Hence the normal vector must be reversed. */
-        normals[ii++] = -nx*invLenNorm;
-        normals[ii++] = -ny*invLenNorm;
-        normals[ii++] = -nz*invLenNorm;
-        normals[ii++] =  lenNorm;
+        normals[ii++] = -nx * invLenNorm;
+        normals[ii++] = -ny * invLenNorm;
+        normals[ii++] = -nz * invLenNorm;
+        normals[ii++] = lenNorm;
       }
       break;
     }
   }
 }
 
-void CMeshFEM::MetricTermsBoundaryFaces(CBoundaryFEM *boundary,
-                                        CConfig      *config) {
-
+void CMeshFEM::MetricTermsBoundaryFaces(CBoundaryFEM* boundary, CConfig* config) {
   /* Determine whether or not the viscous terms are needed. */
-  const bool viscousTerms = (config->GetKind_Solver() != MAIN_SOLVER::FEM_EULER && config->GetKind_Solver() != MAIN_SOLVER::DISC_ADJ_FEM_EULER);
+  const bool viscousTerms = (config->GetKind_Solver() != MAIN_SOLVER::FEM_EULER &&
+                             config->GetKind_Solver() != MAIN_SOLVER::DISC_ADJ_FEM_EULER);
 
   /*--- Loop over the boundary faces stored on this rank. ---*/
-  for(unsigned long i=0; i<boundary->surfElem.size(); ++i) {
-
+  for (unsigned long i = 0; i < boundary->surfElem.size(); ++i) {
     /*--------------------------------------------------------------------------*/
     /*--- Step 1: Allocate the memory for the face metric terms.             ---*/
     /*---         Depending on the case, not all of this memory is needed.   ---*/
@@ -2323,18 +2166,17 @@ void CMeshFEM::MetricTermsBoundaryFaces(CBoundaryFEM *boundary,
 
     /* Determine the corresponding standard face element and get the
        relevant information from it. */
-    const unsigned short ind  = boundary->surfElem[i].indStandardElement;
+    const unsigned short ind = boundary->surfElem[i].indStandardElement;
     const unsigned short nInt = standardBoundaryFacesSol[ind].GetNIntegration();
 
     /*--- Allocate the several metric terms. ---*/
-    boundary->surfElem[i].metricNormalsFace.resize(nInt*(nDim+1));
+    boundary->surfElem[i].metricNormalsFace.resize(nInt * (nDim + 1));
 
-    if( viscousTerms )
-      boundary->surfElem[i].metricCoorDerivFace.resize(nInt*nDim*nDim);
+    if (viscousTerms) boundary->surfElem[i].metricCoorDerivFace.resize(nInt * nDim * nDim);
 
     /* Allocate the memory for the grid velocities and initialize them to the
        default value of zero. */
-    boundary->surfElem[i].gridVelocities.assign(nInt*nDim, 0.0);
+    boundary->surfElem[i].gridVelocities.assign(nInt * nDim, 0.0);
 
     /*--------------------------------------------------------------------------*/
     /*--- Step 2: Determine the actual metric data in the integration points ---*/
@@ -2344,8 +2186,8 @@ void CMeshFEM::MetricTermsBoundaryFaces(CBoundaryFEM *boundary,
     /* Call the function ComputeNormalsFace to compute the unit normals and
        its corresponding area in the integration points. */
     unsigned short nDOFs = standardBoundaryFacesGrid[ind].GetNDOFsFace();
-    const su2double *dr  = standardBoundaryFacesGrid[ind].GetDrBasisFaceIntegration();
-    const su2double *ds  = standardBoundaryFacesGrid[ind].GetDsBasisFaceIntegration();
+    const su2double* dr = standardBoundaryFacesGrid[ind].GetDrBasisFaceIntegration();
+    const su2double* ds = standardBoundaryFacesGrid[ind].GetDsBasisFaceIntegration();
 
     ComputeNormalsFace(nInt, nDOFs, dr, ds, boundary->surfElem[i].DOFsGridFace.data(),
                        boundary->surfElem[i].metricNormalsFace.data());
@@ -2353,61 +2195,51 @@ void CMeshFEM::MetricTermsBoundaryFaces(CBoundaryFEM *boundary,
     /* Compute the derivatives of the parametric coordinates w.r.t. the
        Cartesian coordinates, i.e. drdx, drdy, etc. in the integration points
        of the face, if needed. */
-    if( viscousTerms ) {
+    if (viscousTerms) {
       nDOFs = standardBoundaryFacesGrid[ind].GetNDOFsElem();
-      dr    = standardBoundaryFacesGrid[ind].GetMatDerBasisElemIntegration();
+      dr = standardBoundaryFacesGrid[ind].GetMatDerBasisElemIntegration();
 
-      ComputeGradientsCoordinatesFace(nInt, nDOFs, dr,
-                                      boundary->surfElem[i].DOFsGridElement.data(),
-                                      boundary->surfElem[i].metricCoorDerivFace.data(),
-                                      config);
+      ComputeGradientsCoordinatesFace(nInt, nDOFs, dr, boundary->surfElem[i].DOFsGridElement.data(),
+                                      boundary->surfElem[i].metricCoorDerivFace.data(), config);
     }
   }
 }
 
-void CMeshFEM::SetPositive_ZArea(CConfig *config) {
-
+void CMeshFEM::SetPositive_ZArea(CConfig* config) {
   /*---------------------------------------------------------------------------*/
   /*--- Step 1: Determine the local contribution to the positive z area.    ---*/
   /*---------------------------------------------------------------------------*/
 
   /* Loop over the boundary markers. */
   su2double PositiveZArea = 0.0;
-  for(unsigned short iMarker=0; iMarker<nMarker; ++iMarker) {
-
+  for (unsigned short iMarker = 0; iMarker < nMarker; ++iMarker) {
     /* Determine whether or not this boundary contributes. */
-    const unsigned short Boundary   = config->GetMarker_All_KindBC(iMarker);
+    const unsigned short Boundary = config->GetMarker_All_KindBC(iMarker);
     const unsigned short Monitoring = config->GetMarker_All_Monitoring(iMarker);
 
-    if( ((Boundary == EULER_WALL)              ||
-         (Boundary == HEAT_FLUX)               ||
-         (Boundary == ISOTHERMAL)              ||
-         (Boundary == LOAD_BOUNDARY)           ||
-         (Boundary == DISPLACEMENT_BOUNDARY)) && (Monitoring == YES) ) {
-
+    if (((Boundary == EULER_WALL) || (Boundary == HEAT_FLUX) || (Boundary == ISOTHERMAL) ||
+         (Boundary == LOAD_BOUNDARY) || (Boundary == DISPLACEMENT_BOUNDARY)) &&
+        (Monitoring == YES)) {
       /* Easier storage of the surface elements for this marker. */
-      const vector<CSurfaceElementFEM> &surfElem = boundaries[iMarker].surfElem;
+      const vector<CSurfaceElementFEM>& surfElem = boundaries[iMarker].surfElem;
 
       /* Loop over the surface elements. */
-      for(unsigned long i=0; i<surfElem.size(); ++i) {
-
+      for (unsigned long i = 0; i < surfElem.size(); ++i) {
         /* Determine the number of integration points and their weights via
            the corresponding standard element. */
-        const unsigned short ind     = surfElem[i].indStandardElement;
-        const unsigned short nInt    = standardBoundaryFacesGrid[ind].GetNIntegration();
-        const su2double     *weights = standardBoundaryFacesGrid[ind].GetWeightsIntegration();
+        const unsigned short ind = surfElem[i].indStandardElement;
+        const unsigned short nInt = standardBoundaryFacesGrid[ind].GetNIntegration();
+        const su2double* weights = standardBoundaryFacesGrid[ind].GetWeightsIntegration();
 
         /* Loop over the integration points for this element and update PositiveZArea
            if the normal has a negative z-component. In that case it will give a
            positive contribution to PositiveZArea as this must take the normal pointing
            into the element into account. */
-        for(unsigned short j=0; j<nInt; ++j) {
-
+        for (unsigned short j = 0; j < nInt; ++j) {
           /* Store the normal data for this integration point a bit easier and update
              PositiveZArea, if needed. */
-          const su2double *normal = &surfElem[i].metricNormalsFace[j*(nDim+1)];
-          if(normal[nDim-1] < 0.0)
-            PositiveZArea -= weights[j]*normal[nDim-1]*normal[nDim];
+          const su2double* normal = &surfElem[i].metricNormalsFace[j * (nDim + 1)];
+          if (normal[nDim - 1] < 0.0) PositiveZArea -= weights[j] * normal[nDim - 1] * normal[nDim];
         }
       }
     }
@@ -2428,61 +2260,56 @@ void CMeshFEM::SetPositive_ZArea(CConfig *config) {
   /*---         a message about the projected area if I am the master.      ---*/
   /*---------------------------------------------------------------------------*/
 
-  if (config->GetRefArea() == 0.0)
-    config->SetRefArea(PositiveZArea);
+  if (config->GetRefArea() == 0.0) config->SetRefArea(PositiveZArea);
 
   if (rank == MASTER_NODE) {
-    if (nDim == 2) cout << "Area projection in the y-plane = "<< PositiveZArea << "." << endl;
-    else           cout << "Area projection in the z-plane = "<< PositiveZArea << "." << endl;
+    if (nDim == 2)
+      cout << "Area projection in the y-plane = " << PositiveZArea << "." << endl;
+    else
+      cout << "Area projection in the z-plane = " << PositiveZArea << "." << endl;
   }
 }
 
-CMeshFEM_DG::CMeshFEM_DG(CGeometry *geometry, CConfig *config)
-  : CMeshFEM(geometry, config) {
-}
+CMeshFEM_DG::CMeshFEM_DG(CGeometry* geometry, CConfig* config) : CMeshFEM(geometry, config) {}
 
 void CMeshFEM_DG::SetGlobal_to_Local_Point(void) {
   Global_to_Local_Point.clear();
   unsigned long ii = 0;
-  for(unsigned long i=0; i<nVolElemOwned; ++i) {
-    for(unsigned short j=0; j<volElem[i].nDOFsSol; ++j, ++ii) {
-      Global_to_Local_Point[volElem[i].offsetDOFsSolGlobal+j] = ii;
+  for (unsigned long i = 0; i < nVolElemOwned; ++i) {
+    for (unsigned short j = 0; j < volElem[i].nDOFsSol; ++j, ++ii) {
+      Global_to_Local_Point[volElem[i].offsetDOFsSolGlobal + j] = ii;
     }
   }
 }
 
 void CMeshFEM_DG::CoordinatesIntegrationPoints(void) {
-
   /*--------------------------------------------------------------------*/
   /*--- Step 1: The integration points of the owned volume elements. ---*/
   /*--------------------------------------------------------------------*/
 
   /*--- Loop over the owned elements to compute the coordinates
         in the integration points. ---*/
-  for(unsigned long l=0; l<nVolElemOwned; ++l) {
-
+  for (unsigned long l = 0; l < nVolElemOwned; ++l) {
     /* Get the required data from the corresponding standard element. */
-    const unsigned short ind  = volElem[l].indStandardElement;
+    const unsigned short ind = volElem[l].indStandardElement;
     const unsigned short nInt = standardElementsGrid[ind].GetNIntegration();
-    const su2double      *lag = standardElementsGrid[ind].GetBasisFunctionsIntegration();
+    const su2double* lag = standardElementsGrid[ind].GetBasisFunctionsIntegration();
 
     /* Allocate the memory for the coordinates of the integration points. */
-    volElem[l].coorIntegrationPoints.resize(nDim*nInt);
+    volElem[l].coorIntegrationPoints.resize(nDim * nInt);
 
     /* Store the grid DOFs of this element a bit easier. */
     const unsigned short nDOFs = volElem[l].nDOFsGrid;
-    const unsigned long  *DOFs = volElem[l].nodeIDsGrid.data();
+    const unsigned long* DOFs = volElem[l].nodeIDsGrid.data();
 
     /*--- Loop over the integration points of this element and compute
           the coordinates of the integration points. */
-    for(unsigned short i=0; i<nInt; ++i) {
-
-      su2double *coor = volElem[l].coorIntegrationPoints.data() + i*nDim;
-      const unsigned short jj = i*nDOFs;
-      for(unsigned short j=0; j<nDim; ++j) {
+    for (unsigned short i = 0; i < nInt; ++i) {
+      su2double* coor = volElem[l].coorIntegrationPoints.data() + i * nDim;
+      const unsigned short jj = i * nDOFs;
+      for (unsigned short j = 0; j < nDim; ++j) {
         coor[j] = 0.0;
-        for(unsigned short k=0; k<nDOFs; ++k)
-          coor[j] += lag[jj+k]*meshPoints[DOFs[k]].coor[j];
+        for (unsigned short k = 0; k < nDOFs; ++k) coor[j] += lag[jj + k] * meshPoints[DOFs[k]].coor[j];
       }
     }
   }
@@ -2493,30 +2320,27 @@ void CMeshFEM_DG::CoordinatesIntegrationPoints(void) {
 
   /*--- Loop over the internal matching faces to compute the coordinates
         in the integration points. ---*/
-  for(unsigned long l=0; l<matchingFaces.size(); ++l) {
-
+  for (unsigned long l = 0; l < matchingFaces.size(); ++l) {
     /* Get the required data from the corresponding standard element. */
-    const unsigned short ind   = matchingFaces[l].indStandardElement;
-    const unsigned short nInt  = standardMatchingFacesGrid[ind].GetNIntegration();
+    const unsigned short ind = matchingFaces[l].indStandardElement;
+    const unsigned short nInt = standardMatchingFacesGrid[ind].GetNIntegration();
     const unsigned short nDOFs = standardMatchingFacesGrid[ind].GetNDOFsFaceSide0();
-    const su2double      *lag  = standardMatchingFacesGrid[ind].GetBasisFaceIntegrationSide0();
+    const su2double* lag = standardMatchingFacesGrid[ind].GetBasisFaceIntegrationSide0();
 
     /* Allocate the memory for the coordinates of the integration points. */
-    matchingFaces[l].coorIntegrationPoints.resize(nDim*nInt);
+    matchingFaces[l].coorIntegrationPoints.resize(nDim * nInt);
 
     /* Store the grid DOFs of this face a bit easier. */
-    const unsigned long *DOFs = matchingFaces[l].DOFsGridFaceSide0.data();
+    const unsigned long* DOFs = matchingFaces[l].DOFsGridFaceSide0.data();
 
     /*--- Loop over the integration points of this face and compute
           the coordinates of the integration points. */
-    for(unsigned short i=0; i<nInt; ++i) {
-
-      su2double *coor = matchingFaces[l].coorIntegrationPoints.data() + i*nDim;
-      const unsigned short jj = i*nDOFs;
-      for(unsigned short j=0; j<nDim; ++j) {
+    for (unsigned short i = 0; i < nInt; ++i) {
+      su2double* coor = matchingFaces[l].coorIntegrationPoints.data() + i * nDim;
+      const unsigned short jj = i * nDOFs;
+      for (unsigned short j = 0; j < nDim; ++j) {
         coor[j] = 0.0;
-        for(unsigned short k=0; k<nDOFs; ++k)
-          coor[j] += lag[jj+k]*meshPoints[DOFs[k]].coor[j];
+        for (unsigned short k = 0; k < nDOFs; ++k) coor[j] += lag[jj + k] * meshPoints[DOFs[k]].coor[j];
       }
     }
   }
@@ -2527,38 +2351,34 @@ void CMeshFEM_DG::CoordinatesIntegrationPoints(void) {
 
   /*--- Loop over the boundary markers. Make sure to exclude the periodic
         boundaries, because these are not physical. ---*/
-  for(unsigned short iMarker=0; iMarker<boundaries.size(); ++iMarker) {
-    if( !boundaries[iMarker].periodicBoundary ) {
-
+  for (unsigned short iMarker = 0; iMarker < boundaries.size(); ++iMarker) {
+    if (!boundaries[iMarker].periodicBoundary) {
       /* Abbreviate the surface elements a bit easier. */
-      vector<CSurfaceElementFEM> &surfElem = boundaries[iMarker].surfElem;
+      vector<CSurfaceElementFEM>& surfElem = boundaries[iMarker].surfElem;
 
       /* Loop over the boundary faces and determine the coordinates
          in the integration points. */
-      for(unsigned long l=0; l<surfElem.size(); ++l) {
-
+      for (unsigned long l = 0; l < surfElem.size(); ++l) {
         /* Get the required data from the corresponding standard element. */
-        const unsigned short ind   = surfElem[l].indStandardElement;
-        const unsigned short nInt  = standardBoundaryFacesGrid[ind].GetNIntegration();
+        const unsigned short ind = surfElem[l].indStandardElement;
+        const unsigned short nInt = standardBoundaryFacesGrid[ind].GetNIntegration();
         const unsigned short nDOFs = surfElem[l].nDOFsGrid;
-        const su2double      *lag  = standardBoundaryFacesGrid[ind].GetBasisFaceIntegration();
+        const su2double* lag = standardBoundaryFacesGrid[ind].GetBasisFaceIntegration();
 
         /* Allocate the memory for the coordinates of the integration points. */
-        surfElem[l].coorIntegrationPoints.resize(nDim*nInt);
+        surfElem[l].coorIntegrationPoints.resize(nDim * nInt);
 
         /* Store the grid DOFs of this face a bit easier. */
-        const unsigned long *DOFs = surfElem[l].DOFsGridFace.data();
+        const unsigned long* DOFs = surfElem[l].DOFsGridFace.data();
 
         /*--- Loop over the integration points of this face and compute
               the coordinates of the integration points. */
-        for(unsigned short i=0; i<nInt; ++i) {
-
-          su2double *coor = surfElem[l].coorIntegrationPoints.data() + i*nDim;
-          const unsigned short jj = i*nDOFs;
-          for(unsigned short j=0; j<nDim; ++j) {
+        for (unsigned short i = 0; i < nInt; ++i) {
+          su2double* coor = surfElem[l].coorIntegrationPoints.data() + i * nDim;
+          const unsigned short jj = i * nDOFs;
+          for (unsigned short j = 0; j < nDim; ++j) {
             coor[j] = 0.0;
-            for(unsigned short k=0; k<nDOFs; ++k)
-              coor[j] += lag[jj+k]*meshPoints[DOFs[k]].coor[j];
+            for (unsigned short k = 0; k < nDOFs; ++k) coor[j] += lag[jj + k] * meshPoints[DOFs[k]].coor[j];
           }
         }
       }
@@ -2567,42 +2387,37 @@ void CMeshFEM_DG::CoordinatesIntegrationPoints(void) {
 }
 
 void CMeshFEM_DG::CoordinatesSolDOFs(void) {
-
   /*--- Loop over the owned elements to compute the coordinates
         of the solution DOFs. ---*/
-  for(unsigned long l=0; l<nVolElemOwned; ++l) {
-
+  for (unsigned long l = 0; l < nVolElemOwned; ++l) {
     /* Store the grid DOFs and the number of solDOFS a bit easier. */
     const unsigned short nDOFsGrid = volElem[l].nDOFsGrid;
-    const unsigned short nDOFsSol  = volElem[l].nDOFsSol;
-    const unsigned long  *DOFsGrid = volElem[l].nodeIDsGrid.data();
+    const unsigned short nDOFsSol = volElem[l].nDOFsSol;
+    const unsigned long* DOFsGrid = volElem[l].nodeIDsGrid.data();
 
     /* Get the required data from the corresponding standard element. */
     const unsigned short ind = volElem[l].indStandardElement;
-    const su2double     *lag = standardElementsGrid[ind].GetBasisFunctionsSolDOFs();
+    const su2double* lag = standardElementsGrid[ind].GetBasisFunctionsSolDOFs();
 
     /* Allocate the memory for the coordinates of the solution DOFs. */
-    volElem[l].coorSolDOFs.resize(nDim*nDOFsSol);
+    volElem[l].coorSolDOFs.resize(nDim * nDOFsSol);
 
     /*--- Loop over the solution DOFs of this element and compute the
           coordinates. Note that in case the polynomial degree of the grid
           and solution is the same the grid DOFs and solution DOFs coincide
           and the interpolation boils down to a copy of the coordinates. ---*/
-    for(unsigned short i=0; i<nDOFsSol; ++i) {
-
-      su2double *coor = volElem[l].coorSolDOFs.data() + i*nDim;
-      const unsigned short jj = i*nDOFsGrid;
-      for(unsigned short j=0; j<nDim; ++j) {
+    for (unsigned short i = 0; i < nDOFsSol; ++i) {
+      su2double* coor = volElem[l].coorSolDOFs.data() + i * nDim;
+      const unsigned short jj = i * nDOFsGrid;
+      for (unsigned short j = 0; j < nDim; ++j) {
         coor[j] = 0.0;
-        for(unsigned short k=0; k<nDOFsGrid; ++k)
-          coor[j] += lag[jj+k]*meshPoints[DOFsGrid[k]].coor[j];
+        for (unsigned short k = 0; k < nDOFsGrid; ++k) coor[j] += lag[jj + k] * meshPoints[DOFsGrid[k]].coor[j];
       }
     }
   }
 }
 
-void CMeshFEM_DG::CreateFaces(CConfig *config) {
-
+void CMeshFEM_DG::CreateFaces(CConfig* config) {
   /*---------------------------------------------------------------------------*/
   /*--- Step 1: Determine the faces of the locally stored part of the grid. ---*/
   /*---------------------------------------------------------------------------*/
@@ -2610,53 +2425,47 @@ void CMeshFEM_DG::CreateFaces(CConfig *config) {
   /*--- Loop over the volume elements stored on this rank, including the halos. ---*/
   vector<CFaceOfElement> localFaces;
 
-  for(unsigned long k=0; k<nVolElemTot; ++k) {
-
+  for (unsigned long k = 0; k < nVolElemTot; ++k) {
     /* Determine the corner points of all the faces of this element. */
     unsigned short nFaces;
     unsigned short nPointsPerFace[6];
-    unsigned long  faceConn[6][4];
+    unsigned long faceConn[6][4];
 
     volElem[k].GetCornerPointsAllFaces(nFaces, nPointsPerFace, faceConn);
 
     /* Loop over the faces of this element, set the appropriate information,
        create a unique numbering and add the faces to localFaces. */
-    for(unsigned short i=0; i<nFaces; ++i) {
+    for (unsigned short i = 0; i < nFaces; ++i) {
       CFaceOfElement thisFace;
       thisFace.nCornerPoints = nPointsPerFace[i];
-      for(unsigned short j=0; j<nPointsPerFace[i]; ++j)
-        thisFace.cornerPoints[j] = faceConn[i][j];
+      for (unsigned short j = 0; j < nPointsPerFace[i]; ++j) thisFace.cornerPoints[j] = faceConn[i][j];
 
       /* Copy the data from the volume element. */
-      thisFace.elemID0       =  k;
-      thisFace.nPolyGrid0    =  volElem[k].nPolyGrid;
-      thisFace.nPolySol0     =  volElem[k].nPolySol;
-      thisFace.nDOFsElem0    =  volElem[k].nDOFsSol;
-      thisFace.elemType0     =  volElem[k].VTK_Type;
-      thisFace.faceID0       =  i;
-      thisFace.faceIndicator = -2;   // Initialized to an invalid face.
+      thisFace.elemID0 = k;
+      thisFace.nPolyGrid0 = volElem[k].nPolyGrid;
+      thisFace.nPolySol0 = volElem[k].nPolySol;
+      thisFace.nDOFsElem0 = volElem[k].nDOFsSol;
+      thisFace.elemType0 = volElem[k].VTK_Type;
+      thisFace.faceID0 = i;
+      thisFace.faceIndicator = -2;  // Initialized to an invalid face.
 
       thisFace.JacFaceIsConsideredConstant = volElem[k].JacFacesIsConsideredConstant[i];
-      thisFace.elem0IsOwner                = volElem[k].ElementOwnsFaces[i];
+      thisFace.elem0IsOwner = volElem[k].ElementOwnsFaces[i];
 
       /* Determine whether or not the integration rule for straight and curved
          faces is the same. If that is the case, the value of JacFaceIsConsideredConstant
          is set to false. Hence it is only needed to carry out this check for faces
          with a constant Jacobian. This is done to reduce the number of standard elements. */
-      if( thisFace.JacFaceIsConsideredConstant ) {
-
+      if (thisFace.JacFaceIsConsideredConstant) {
         unsigned short orderExactStraight =
-           (unsigned short) ceil(thisFace.nPolyGrid0*config->GetQuadrature_Factor_Straight());
+            (unsigned short)ceil(thisFace.nPolyGrid0 * config->GetQuadrature_Factor_Straight());
         unsigned short orderExactCurved =
-           (unsigned short) ceil(thisFace.nPolyGrid0*config->GetQuadrature_Factor_Curved());
-
-        if(orderExactStraight == orderExactCurved) {
-          orderExactStraight =
-             (unsigned short) ceil(thisFace.nPolySol0*config->GetQuadrature_Factor_Straight());
-          orderExactCurved =
-             (unsigned short) ceil(thisFace.nPolySol0*config->GetQuadrature_Factor_Curved());
-          if(orderExactStraight == orderExactCurved)
-            thisFace.JacFaceIsConsideredConstant = false;
+            (unsigned short)ceil(thisFace.nPolyGrid0 * config->GetQuadrature_Factor_Curved());
+
+        if (orderExactStraight == orderExactCurved) {
+          orderExactStraight = (unsigned short)ceil(thisFace.nPolySol0 * config->GetQuadrature_Factor_Straight());
+          orderExactCurved = (unsigned short)ceil(thisFace.nPolySol0 * config->GetQuadrature_Factor_Curved());
+          if (orderExactStraight == orderExactCurved) thisFace.JacFaceIsConsideredConstant = false;
         }
       }
 
@@ -2672,47 +2481,42 @@ void CMeshFEM_DG::CreateFaces(CConfig *config) {
   sort(localFaces.begin(), localFaces.end());
 
   /*--- Loop over the faces to merge the matching faces. ---*/
-  for(unsigned long i=1; i<localFaces.size(); ++i) {
-
+  for (unsigned long i = 1; i < localFaces.size(); ++i) {
     /* Check for a matching face with the previous face in the vector.
        Note that the == operator only checks the node IDs. */
-    if(localFaces[i] == localFaces[i-1]) {
-
+    if (localFaces[i] == localFaces[i - 1]) {
       /* Faces are matching. Check if it should be kept, i.e. if one
          of the elements owns the face. */
-      if(localFaces[i].elem0IsOwner || localFaces[i-1].elem0IsOwner) {
-
+      if (localFaces[i].elem0IsOwner || localFaces[i - 1].elem0IsOwner) {
         /* Store the data for this matching face in faces[i-1]. */
-        if(localFaces[i].elemID0 < nVolElemTot) {
-          localFaces[i-1].elemID0      = localFaces[i].elemID0;
-          localFaces[i-1].nPolyGrid0   = localFaces[i].nPolyGrid0;
-          localFaces[i-1].nPolySol0    = localFaces[i].nPolySol0;
-          localFaces[i-1].nDOFsElem0   = localFaces[i].nDOFsElem0;
-          localFaces[i-1].elemType0    = localFaces[i].elemType0;
-          localFaces[i-1].faceID0      = localFaces[i].faceID0;
-          localFaces[i-1].elem0IsOwner = localFaces[i].elem0IsOwner;
-        }
-        else {
-          localFaces[i-1].elemID1    = localFaces[i].elemID1;
-          localFaces[i-1].nPolyGrid1 = localFaces[i].nPolyGrid1;
-          localFaces[i-1].nPolySol1  = localFaces[i].nPolySol1;
-          localFaces[i-1].nDOFsElem1 = localFaces[i].nDOFsElem1;
-          localFaces[i-1].elemType1  = localFaces[i].elemType1;
-          localFaces[i-1].faceID1    = localFaces[i].faceID1;
+        if (localFaces[i].elemID0 < nVolElemTot) {
+          localFaces[i - 1].elemID0 = localFaces[i].elemID0;
+          localFaces[i - 1].nPolyGrid0 = localFaces[i].nPolyGrid0;
+          localFaces[i - 1].nPolySol0 = localFaces[i].nPolySol0;
+          localFaces[i - 1].nDOFsElem0 = localFaces[i].nDOFsElem0;
+          localFaces[i - 1].elemType0 = localFaces[i].elemType0;
+          localFaces[i - 1].faceID0 = localFaces[i].faceID0;
+          localFaces[i - 1].elem0IsOwner = localFaces[i].elem0IsOwner;
+        } else {
+          localFaces[i - 1].elemID1 = localFaces[i].elemID1;
+          localFaces[i - 1].nPolyGrid1 = localFaces[i].nPolyGrid1;
+          localFaces[i - 1].nPolySol1 = localFaces[i].nPolySol1;
+          localFaces[i - 1].nDOFsElem1 = localFaces[i].nDOFsElem1;
+          localFaces[i - 1].elemType1 = localFaces[i].elemType1;
+          localFaces[i - 1].faceID1 = localFaces[i].faceID1;
         }
 
         /* Adapt the boolean to indicate whether or not the face has a constant
            Jacobian of the transformation, although in principle this info
            should be the same for both faces. */
-        if( !(localFaces[i-1].JacFaceIsConsideredConstant &&
-              localFaces[i].JacFaceIsConsideredConstant) ) {
-          localFaces[i-1].JacFaceIsConsideredConstant = false;
+        if (!(localFaces[i - 1].JacFaceIsConsideredConstant && localFaces[i].JacFaceIsConsideredConstant)) {
+          localFaces[i - 1].JacFaceIsConsideredConstant = false;
         }
 
         /* Set this face indicator to -1 to indicate an internal face
            and set elem0IsOwner for localFaces[i] to false. */
-        localFaces[i-1].faceIndicator = -1;
-        localFaces[i].elem0IsOwner    = false;
+        localFaces[i - 1].faceIndicator = -1;
+        localFaces[i].elem0IsOwner = false;
       }
     }
   }
@@ -2721,22 +2525,19 @@ void CMeshFEM_DG::CreateFaces(CConfig *config) {
         the corresponding faces in localFaces. These faces should be found.
         Note that periodic boundaries are skipped, because these are treated
         via the halo elements, which are already in place. ---*/
-  for(unsigned short iMarker=0; iMarker<nMarker; ++iMarker) {
-    if( !boundaries[iMarker].periodicBoundary ) {
-
-      for(unsigned long k=0; k<boundaries[iMarker].surfElem.size(); ++k) {
-
+  for (unsigned short iMarker = 0; iMarker < nMarker; ++iMarker) {
+    if (!boundaries[iMarker].periodicBoundary) {
+      for (unsigned long k = 0; k < boundaries[iMarker].surfElem.size(); ++k) {
         /* Determine the corner points of the face of this element. */
         unsigned short nPointsPerFace;
-        unsigned long  faceConn[4];
+        unsigned long faceConn[4];
 
         boundaries[iMarker].surfElem[k].GetCornerPointsFace(nPointsPerFace, faceConn);
 
         /* Create an object of CFaceOfElement to carry out the search. */
         CFaceOfElement thisFace;
         thisFace.nCornerPoints = nPointsPerFace;
-        for(unsigned short j=0; j<nPointsPerFace; ++j)
-          thisFace.cornerPoints[j] = faceConn[j];
+        for (unsigned short j = 0; j < nPointsPerFace; ++j) thisFace.cornerPoints[j] = faceConn[j];
         thisFace.CreateUniqueNumberingWithOrientation();
 
         /* Search for thisFace in localFaces. It must be found. */
@@ -2744,27 +2545,24 @@ void CMeshFEM_DG::CreateFaces(CConfig *config) {
         low = lower_bound(localFaces.begin(), localFaces.end(), thisFace);
 
         bool thisFaceFound = false;
-        if(low != localFaces.end()) {
-          if( !(thisFace < *low) ) thisFaceFound = true;
+        if (low != localFaces.end()) {
+          if (!(thisFace < *low)) thisFaceFound = true;
         }
 
-        if( thisFaceFound ) {
+        if (thisFaceFound) {
           low->faceIndicator = iMarker;
 
           /* A few additional checks. */
           bool side0IsBoundary = low->elemID0 < nVolElemTot;
-          unsigned long elemID = side0IsBoundary ? low->elemID0    : low->elemID1;
+          unsigned long elemID = side0IsBoundary ? low->elemID0 : low->elemID1;
           unsigned short nPoly = side0IsBoundary ? low->nPolyGrid0 : low->nPolyGrid1;
 
-          if(elemID != boundaries[iMarker].surfElem[k].volElemID ||
-             nPoly  != boundaries[iMarker].surfElem[k].nPolyGrid)
+          if (elemID != boundaries[iMarker].surfElem[k].volElemID || nPoly != boundaries[iMarker].surfElem[k].nPolyGrid)
             SU2_MPI::Error(string("Element ID and/or polynomial degree do not match ") +
-                           string("for this boundary element. This should not happen."),
+                               string("for this boundary element. This should not happen."),
                            CURRENT_FUNCTION);
-        }
-        else
-          SU2_MPI::Error("Boundary face not found in localFaces. This should not happen.",
-                         CURRENT_FUNCTION);
+        } else
+          SU2_MPI::Error("Boundary face not found in localFaces. This should not happen.", CURRENT_FUNCTION);
       }
     }
   }
@@ -2773,9 +2571,8 @@ void CMeshFEM_DG::CreateFaces(CConfig *config) {
         These faces are indicated by an owned face and a faceIndicator of -2.
         To avoid that these faces are removed afterwards, set their
         faceIndicator to -1. ---*/
-  for(unsigned long i=0; i<localFaces.size(); ++i) {
-    if(localFaces[i].faceIndicator == -2 && localFaces[i].elem0IsOwner)
-      localFaces[i].faceIndicator = -1;
+  for (unsigned long i = 0; i < localFaces.size(); ++i) {
+    if (localFaces[i].faceIndicator == -2 && localFaces[i].elem0IsOwner) localFaces[i].faceIndicator = -1;
   }
 
   /*--- Remove the invalid faces. This is accomplished by giving the face four
@@ -2783,8 +2580,8 @@ void CMeshFEM_DG::CreateFaces(CConfig *config) {
         ID in the grid. In this way the sorting operator puts these faces at the
         end of the vector, see also the < operator of CFaceOfElement. ---*/
   unsigned long nFacesLoc = localFaces.size();
-  for(unsigned long i=0; i<localFaces.size(); ++i) {
-    if(localFaces[i].faceIndicator == -2) {
+  for (unsigned long i = 0; i < localFaces.size(); ++i) {
+    if (localFaces[i].faceIndicator == -2) {
       unsigned long invalID = meshPoints.size();
       localFaces[i].nCornerPoints = 4;
       localFaces[i].cornerPoints[0] = invalID;
@@ -2811,8 +2608,7 @@ void CMeshFEM_DG::CreateFaces(CConfig *config) {
      functor CSortFaces is used for comparison. Within the categories
      the sorting depends on the time levels of the adjacent volume elements
      of the face. */
-  sort(localFaces.begin(), localFaces.end(),
-       CSortFaces(nVolElemOwned, nVolElemTot, volElem.data()));
+  sort(localFaces.begin(), localFaces.end(), CSortFaces(nVolElemOwned, nVolElemTot, volElem.data()));
 
   /*--- Carry out a possible swap of side 0 and side 1 of the faces. This is
         done for the following reasons (in order of importance).
@@ -2824,36 +2620,26 @@ void CMeshFEM_DG::CreateFaces(CConfig *config) {
 
         Furthermore, make sure that for boundary faces and non-matching faces
         the corresponding element is always on side 0. ---*/
-  for(unsigned long i=0; i<localFaces.size(); ++i) {
-
+  for (unsigned long i = 0; i < localFaces.size(); ++i) {
     /* Determine whether or not the ajacent elements must be swapped. */
     bool swapElements;
-    if(localFaces[i].elemID0 < nVolElemTot &&
-       localFaces[i].elemID1 < nVolElemTot) {
-
+    if (localFaces[i].elemID0 < nVolElemTot && localFaces[i].elemID1 < nVolElemTot) {
       /* This is an internal matching face. First check if one of the adjacent
          elements is not an owned element. */
-      if(localFaces[i].elemID0 >= nVolElemOwned ||
-         localFaces[i].elemID1 >= nVolElemOwned) {
-
+      if (localFaces[i].elemID0 >= nVolElemOwned || localFaces[i].elemID1 >= nVolElemOwned) {
         /* One of the element is not owned. Make sure that the owned element
            is on side 0. */
         swapElements = localFaces[i].elemID0 > localFaces[i].elemID1;
-      }
-      else if(localFaces[i].elemType0 == localFaces[i].elemType1) {
-
+      } else if (localFaces[i].elemType0 == localFaces[i].elemType1) {
         /* The same element type on both sides. Make sure that the element
            with the smallest ID is stored on side 0 of the face. */
         swapElements = localFaces[i].elemID0 > localFaces[i].elemID1;
-      }
-      else {
+      } else {
         /* Different element types. Make sure that the lowest element
            type will be stored on side 0 of the face. */
         swapElements = localFaces[i].elemType0 > localFaces[i].elemType1;
       }
-    }
-    else {
-
+    } else {
       /* Either a boundary face or a non-matching face. It must be swapped
          if the element is currently on side 1 of the face. */
       swapElements = localFaces[i].elemID1 < nVolElemTot;
@@ -2862,15 +2648,15 @@ void CMeshFEM_DG::CreateFaces(CConfig *config) {
     /* Swap the adjacent elements of the face, if needed. Note that
        also the sequence of the corner points must be altered in order
        to obey the right hand rule. */
-    if( swapElements ) {
-      swap(localFaces[i].elemID0,    localFaces[i].elemID1);
+    if (swapElements) {
+      swap(localFaces[i].elemID0, localFaces[i].elemID1);
       swap(localFaces[i].nPolyGrid0, localFaces[i].nPolyGrid1);
-      swap(localFaces[i].nPolySol0,  localFaces[i].nPolySol1);
+      swap(localFaces[i].nPolySol0, localFaces[i].nPolySol1);
       swap(localFaces[i].nDOFsElem0, localFaces[i].nDOFsElem1);
-      swap(localFaces[i].elemType0,  localFaces[i].elemType1);
-      swap(localFaces[i].faceID0,    localFaces[i].faceID1);
+      swap(localFaces[i].elemType0, localFaces[i].elemType1);
+      swap(localFaces[i].faceID0, localFaces[i].faceID1);
 
-      if(localFaces[i].nCornerPoints == 2)
+      if (localFaces[i].nCornerPoints == 2)
         swap(localFaces[i].cornerPoints[0], localFaces[i].cornerPoints[1]);
       else
         swap(localFaces[i].cornerPoints[0], localFaces[i].cornerPoints[2]);
@@ -2883,64 +2669,54 @@ void CMeshFEM_DG::CreateFaces(CConfig *config) {
         made sure that the first corner point does not coincide with the top of
         the pyramid. Otherwise it is impossible to carry the transformation to
         the standard pyramid element. ---*/
-  for(unsigned long i=0; i<localFaces.size(); ++i) {
-
+  for (unsigned long i = 0; i < localFaces.size(); ++i) {
     /* Check for a triangular face. */
-    if(localFaces[i].nCornerPoints == 3) {
-
+    if (localFaces[i].nCornerPoints == 3) {
       /* Determine if the corner points correspond to a corner point of a
          pyramid. A pyramid can in principle occur on both sides of the face. */
       bool cornerIsTopPyramid[] = {false, false, false};
 
-      if(localFaces[i].elemType0 == PYRAMID) {
+      if (localFaces[i].elemType0 == PYRAMID) {
         unsigned long topPyramid = volElem[localFaces[i].elemID0].nodeIDsGrid.back();
-        if(localFaces[i].cornerPoints[0] == topPyramid) cornerIsTopPyramid[0] = true;
-        if(localFaces[i].cornerPoints[1] == topPyramid) cornerIsTopPyramid[1] = true;
-        if(localFaces[i].cornerPoints[2] == topPyramid) cornerIsTopPyramid[2] = true;
+        if (localFaces[i].cornerPoints[0] == topPyramid) cornerIsTopPyramid[0] = true;
+        if (localFaces[i].cornerPoints[1] == topPyramid) cornerIsTopPyramid[1] = true;
+        if (localFaces[i].cornerPoints[2] == topPyramid) cornerIsTopPyramid[2] = true;
       }
 
-      if(localFaces[i].elemType1 == PYRAMID) {
+      if (localFaces[i].elemType1 == PYRAMID) {
         unsigned long topPyramid = volElem[localFaces[i].elemID1].nodeIDsGrid.back();
-        if(localFaces[i].cornerPoints[0] == topPyramid) cornerIsTopPyramid[0] = true;
-        if(localFaces[i].cornerPoints[1] == topPyramid) cornerIsTopPyramid[1] = true;
-        if(localFaces[i].cornerPoints[2] == topPyramid) cornerIsTopPyramid[2] = true;
+        if (localFaces[i].cornerPoints[0] == topPyramid) cornerIsTopPyramid[0] = true;
+        if (localFaces[i].cornerPoints[1] == topPyramid) cornerIsTopPyramid[1] = true;
+        if (localFaces[i].cornerPoints[2] == topPyramid) cornerIsTopPyramid[2] = true;
       }
 
       /* Check if the first element corresponds to the top of a pyramid. */
-      if( cornerIsTopPyramid[0] ) {
-
+      if (cornerIsTopPyramid[0]) {
         /* The sequence of the points of the face must be altered. It is done in
            such a way that the orientation remains the same. Store the original
            point numbering. */
-        unsigned long tmp[] = {localFaces[i].cornerPoints[0],
-                               localFaces[i].cornerPoints[1],
+        unsigned long tmp[] = {localFaces[i].cornerPoints[0], localFaces[i].cornerPoints[1],
                                localFaces[i].cornerPoints[2]};
 
         /* Determine the situation. */
-        if( !cornerIsTopPyramid[1] ) {
-
+        if (!cornerIsTopPyramid[1]) {
           /* cornerPoint[1] is not a top of a pyramid. Hence this will become
              the point 0 of the triangle. */
           localFaces[i].cornerPoints[0] = tmp[1];
           localFaces[i].cornerPoints[1] = tmp[2];
           localFaces[i].cornerPoints[2] = tmp[0];
-        }
-        else {
-
+        } else {
           /* Only cornerPoint[2] is not a top of a pyramid. Hence this will
              become point 0 of the triangle. */
           localFaces[i].cornerPoints[0] = tmp[2];
           localFaces[i].cornerPoints[1] = tmp[0];
           localFaces[i].cornerPoints[2] = tmp[1];
         }
-      }
-      else if(cornerIsTopPyramid[1] && !cornerIsTopPyramid[2]) {
-
+      } else if (cornerIsTopPyramid[1] && !cornerIsTopPyramid[2]) {
         /* cornerPoint[1] is a top of a pyramid and the other two corners
            are not. Change the sequence, such that cornerPoint[2] will become
            point 0 of the triangle. */
-        unsigned long tmp[] = {localFaces[i].cornerPoints[0],
-                               localFaces[i].cornerPoints[1],
+        unsigned long tmp[] = {localFaces[i].cornerPoints[0], localFaces[i].cornerPoints[1],
                                localFaces[i].cornerPoints[2]};
         localFaces[i].cornerPoints[0] = tmp[2];
         localFaces[i].cornerPoints[1] = tmp[0];
@@ -2954,26 +2730,27 @@ void CMeshFEM_DG::CreateFaces(CConfig *config) {
         and also make a distinction between internal faces and faces that
         involve a halo element. ---*/
   const unsigned short nTimeLevels = config->GetnLevels_TimeAccurateLTS();
-  nMatchingFacesInternal.assign(nTimeLevels+1, 0);
-  nMatchingFacesWithHaloElem.assign(nTimeLevels+1, 0);
+  nMatchingFacesInternal.assign(nTimeLevels + 1, 0);
+  nMatchingFacesWithHaloElem.assign(nTimeLevels + 1, 0);
 
   unsigned long nNonMatchingFaces = 0;
-  for(unsigned long i=0; i<localFaces.size(); ++i) {
-    if(localFaces[i].faceIndicator == -1) {
+  for (unsigned long i = 0; i < localFaces.size(); ++i) {
+    if (localFaces[i].faceIndicator == -1) {
       const unsigned long e0 = localFaces[i].elemID0;
       const unsigned long e1 = localFaces[i].elemID1;
 
-      if(e1 < nVolElemTot) {
-        const unsigned short timeLevel = min(volElem[e0].timeLevel,
-                                             volElem[e1].timeLevel);
-        if(e1 < nVolElemOwned) ++nMatchingFacesInternal[timeLevel+1];
-        else                   ++nMatchingFacesWithHaloElem[timeLevel+1];
-      }
-      else ++nNonMatchingFaces;
+      if (e1 < nVolElemTot) {
+        const unsigned short timeLevel = min(volElem[e0].timeLevel, volElem[e1].timeLevel);
+        if (e1 < nVolElemOwned)
+          ++nMatchingFacesInternal[timeLevel + 1];
+        else
+          ++nMatchingFacesWithHaloElem[timeLevel + 1];
+      } else
+        ++nNonMatchingFaces;
     }
   }
 
-  if( nNonMatchingFaces ) {
+  if (nNonMatchingFaces) {
     ostringstream message;
     message << nNonMatchingFaces << " non-matching internal faces found.\n"
             << "This is not supported yet." << endl;
@@ -2982,12 +2759,10 @@ void CMeshFEM_DG::CreateFaces(CConfig *config) {
 
   /* Put nMatchingFacesInternal and nMatchingFacesWithHaloElem in
      cumulative storage format. */
-  for(unsigned short i=0; i<nTimeLevels; ++i)
-    nMatchingFacesInternal[i+1] += nMatchingFacesInternal[i];
+  for (unsigned short i = 0; i < nTimeLevels; ++i) nMatchingFacesInternal[i + 1] += nMatchingFacesInternal[i];
 
   nMatchingFacesWithHaloElem[0] = nMatchingFacesInternal[nTimeLevels];
-  for(unsigned short i=0; i<nTimeLevels; ++i)
-    nMatchingFacesWithHaloElem[i+1] += nMatchingFacesWithHaloElem[i];
+  for (unsigned short i = 0; i < nTimeLevels; ++i) nMatchingFacesWithHaloElem[i + 1] += nMatchingFacesWithHaloElem[i];
 
   /*---------------------------------------------------------------------------*/
   /*--- Step 3: Create the local face based data structure for the internal ---*/
@@ -3002,7 +2777,7 @@ void CMeshFEM_DG::CreateFaces(CConfig *config) {
         of DOFs for the volume elements. Allocate the memory for the
         vector used to store the DOFs of the element.  ---*/
   unsigned short nDOFsVolMax = 0;
-  for(unsigned long i=0; i<nVolElemTot; ++i) {
+  for (unsigned long i = 0; i < nVolElemTot; ++i) {
     nDOFsVolMax = max(nDOFsVolMax, volElem[i].nDOFsGrid);
     nDOFsVolMax = max(nDOFsVolMax, volElem[i].nDOFsSol);
   }
@@ -3012,41 +2787,40 @@ void CMeshFEM_DG::CreateFaces(CConfig *config) {
   /*--- Loop over localFaces to create the connectivity information, which
         is stored in matchingFaces. ---*/
   unsigned long ii = 0;
-  for(unsigned long i=0; i<localFaces.size(); ++i) {
-    if(localFaces[i].faceIndicator == -1 && localFaces[i].elemID1 < nVolElemTot) {
-
+  for (unsigned long i = 0; i < localFaces.size(); ++i) {
+    if (localFaces[i].faceIndicator == -1 && localFaces[i].elemID1 < nVolElemTot) {
       /*--- Determine the number of DOFs on both sides of the face for both the
             grid and solution. This value depends on the face type. ---*/
       unsigned short sizeDOFsGridFaceSide0 = 0, sizeDOFsGridFaceSide1 = 0;
-      unsigned short sizeDOFsSolFaceSide0  = 0, sizeDOFsSolFaceSide1  = 0;
+      unsigned short sizeDOFsSolFaceSide0 = 0, sizeDOFsSolFaceSide1 = 0;
 
       unsigned short VTK_Type = 0;  // To avoid a compiler warning.
-      switch( localFaces[i].nCornerPoints ) {
+      switch (localFaces[i].nCornerPoints) {
         case 2:
           /* Face is a line. */
           VTK_Type = LINE;
           sizeDOFsGridFaceSide0 = localFaces[i].nPolyGrid0 + 1;
           sizeDOFsGridFaceSide1 = localFaces[i].nPolyGrid1 + 1;
-          sizeDOFsSolFaceSide0  = localFaces[i].nPolySol0  + 1;
-          sizeDOFsSolFaceSide1  = localFaces[i].nPolySol1  + 1;
+          sizeDOFsSolFaceSide0 = localFaces[i].nPolySol0 + 1;
+          sizeDOFsSolFaceSide1 = localFaces[i].nPolySol1 + 1;
           break;
 
         case 3:
           /* Face is a triangle. */
           VTK_Type = TRIANGLE;
-          sizeDOFsGridFaceSide0 = (localFaces[i].nPolyGrid0+1)*(localFaces[i].nPolyGrid0+2)/2;
-          sizeDOFsGridFaceSide1 = (localFaces[i].nPolyGrid1+1)*(localFaces[i].nPolyGrid1+2)/2;
-          sizeDOFsSolFaceSide0  = (localFaces[i].nPolySol0 +1)*(localFaces[i].nPolySol0 +2)/2;
-          sizeDOFsSolFaceSide1  = (localFaces[i].nPolySol1 +1)*(localFaces[i].nPolySol1 +2)/2;
+          sizeDOFsGridFaceSide0 = (localFaces[i].nPolyGrid0 + 1) * (localFaces[i].nPolyGrid0 + 2) / 2;
+          sizeDOFsGridFaceSide1 = (localFaces[i].nPolyGrid1 + 1) * (localFaces[i].nPolyGrid1 + 2) / 2;
+          sizeDOFsSolFaceSide0 = (localFaces[i].nPolySol0 + 1) * (localFaces[i].nPolySol0 + 2) / 2;
+          sizeDOFsSolFaceSide1 = (localFaces[i].nPolySol1 + 1) * (localFaces[i].nPolySol1 + 2) / 2;
           break;
 
         case 4:
           /* Face is a quadrilateral. */
           VTK_Type = QUADRILATERAL;
-          sizeDOFsGridFaceSide0 = (localFaces[i].nPolyGrid0+1)*(localFaces[i].nPolyGrid0+1);
-          sizeDOFsGridFaceSide1 = (localFaces[i].nPolyGrid1+1)*(localFaces[i].nPolyGrid1+1);
-          sizeDOFsSolFaceSide0  = (localFaces[i].nPolySol0 +1)*(localFaces[i].nPolySol0 +1);
-          sizeDOFsSolFaceSide1  = (localFaces[i].nPolySol1 +1)*(localFaces[i].nPolySol1 +1);
+          sizeDOFsGridFaceSide0 = (localFaces[i].nPolyGrid0 + 1) * (localFaces[i].nPolyGrid0 + 1);
+          sizeDOFsGridFaceSide1 = (localFaces[i].nPolyGrid1 + 1) * (localFaces[i].nPolyGrid1 + 1);
+          sizeDOFsSolFaceSide0 = (localFaces[i].nPolySol0 + 1) * (localFaces[i].nPolySol0 + 1);
+          sizeDOFsSolFaceSide1 = (localFaces[i].nPolySol1 + 1) * (localFaces[i].nPolySol1 + 1);
           break;
       }
 
@@ -3073,45 +2847,31 @@ void CMeshFEM_DG::CreateFaces(CConfig *config) {
             connectivities of both sides of the face are determined for the
             grid and solution. First for side 0.   ---*/
       bool swapFaceInElementSide0;
-      for(unsigned short j=0; j<volElem[v0].nDOFsSol; ++j)
-        DOFsElem[j] = volElem[v0].offsetDOFsSolLocal + j;
-
-      CreateConnectivitiesFace(VTK_Type,                localFaces[i].cornerPoints,
-                               volElem[v0].VTK_Type,    volElem[v0].nPolyGrid,
-                               volElem[v0].nodeIDsGrid, volElem[v0].nPolySol,
-                               DOFsElem.data(),         swapFaceInElementSide0,
-                               matchingFaces[ii].DOFsSolFaceSide0.data(),
-                               matchingFaces[ii].DOFsSolElementSide0.data());
-
-      for(unsigned short j=0; j<volElem[v0].nDOFsGrid; ++j)
-        DOFsElem[j] = volElem[v0].nodeIDsGrid[j];
-
-      CreateConnectivitiesFace(VTK_Type,                localFaces[i].cornerPoints,
-                               volElem[v0].VTK_Type,    volElem[v0].nPolyGrid,
-                               volElem[v0].nodeIDsGrid, volElem[v0].nPolyGrid,
-                               DOFsElem.data(),         swapFaceInElementSide0,
+      for (unsigned short j = 0; j < volElem[v0].nDOFsSol; ++j) DOFsElem[j] = volElem[v0].offsetDOFsSolLocal + j;
+
+      CreateConnectivitiesFace(VTK_Type, localFaces[i].cornerPoints, volElem[v0].VTK_Type, volElem[v0].nPolyGrid,
+                               volElem[v0].nodeIDsGrid, volElem[v0].nPolySol, DOFsElem.data(), swapFaceInElementSide0,
+                               matchingFaces[ii].DOFsSolFaceSide0.data(), matchingFaces[ii].DOFsSolElementSide0.data());
+
+      for (unsigned short j = 0; j < volElem[v0].nDOFsGrid; ++j) DOFsElem[j] = volElem[v0].nodeIDsGrid[j];
+
+      CreateConnectivitiesFace(VTK_Type, localFaces[i].cornerPoints, volElem[v0].VTK_Type, volElem[v0].nPolyGrid,
+                               volElem[v0].nodeIDsGrid, volElem[v0].nPolyGrid, DOFsElem.data(), swapFaceInElementSide0,
                                matchingFaces[ii].DOFsGridFaceSide0.data(),
                                matchingFaces[ii].DOFsGridElementSide0.data());
 
       /*--- And also for side 1 of the face. ---*/
       bool swapFaceInElementSide1;
-      for(unsigned short j=0; j<volElem[v1].nDOFsSol; ++j)
-        DOFsElem[j] = volElem[v1].offsetDOFsSolLocal + j;
-
-      CreateConnectivitiesFace(VTK_Type,                localFaces[i].cornerPoints,
-                               volElem[v1].VTK_Type,    volElem[v1].nPolyGrid,
-                               volElem[v1].nodeIDsGrid, volElem[v1].nPolySol,
-                               DOFsElem.data(),         swapFaceInElementSide1,
-                               matchingFaces[ii].DOFsSolFaceSide1.data(),
-                               matchingFaces[ii].DOFsSolElementSide1.data());
-
-      for(unsigned short j=0; j<volElem[v1].nDOFsGrid; ++j)
-        DOFsElem[j] = volElem[v1].nodeIDsGrid[j];
-
-      CreateConnectivitiesFace(VTK_Type,                localFaces[i].cornerPoints,
-                               volElem[v1].VTK_Type,    volElem[v1].nPolyGrid,
-                               volElem[v1].nodeIDsGrid, volElem[v1].nPolyGrid,
-                               DOFsElem.data(),         swapFaceInElementSide1,
+      for (unsigned short j = 0; j < volElem[v1].nDOFsSol; ++j) DOFsElem[j] = volElem[v1].offsetDOFsSolLocal + j;
+
+      CreateConnectivitiesFace(VTK_Type, localFaces[i].cornerPoints, volElem[v1].VTK_Type, volElem[v1].nPolyGrid,
+                               volElem[v1].nodeIDsGrid, volElem[v1].nPolySol, DOFsElem.data(), swapFaceInElementSide1,
+                               matchingFaces[ii].DOFsSolFaceSide1.data(), matchingFaces[ii].DOFsSolElementSide1.data());
+
+      for (unsigned short j = 0; j < volElem[v1].nDOFsGrid; ++j) DOFsElem[j] = volElem[v1].nodeIDsGrid[j];
+
+      CreateConnectivitiesFace(VTK_Type, localFaces[i].cornerPoints, volElem[v1].VTK_Type, volElem[v1].nPolyGrid,
+                               volElem[v1].nodeIDsGrid, volElem[v1].nPolyGrid, DOFsElem.data(), swapFaceInElementSide1,
                                matchingFaces[ii].DOFsGridFaceSide1.data(),
                                matchingFaces[ii].DOFsGridElementSide1.data());
 
@@ -3120,51 +2880,29 @@ void CMeshFEM_DG::CreateFaces(CConfig *config) {
             Note that both the grid and the solution representation must
             match with the standard element. ---*/
       unsigned long j;
-      for(j=0; j<standardMatchingFacesSol.size(); ++j) {
-        if(standardMatchingFacesSol[j].SameStandardMatchingFace(VTK_Type,
-                                                                localFaces[i].JacFaceIsConsideredConstant,
-                                                                localFaces[i].elemType0,
-                                                                localFaces[i].nPolySol0,
-                                                                localFaces[i].elemType1,
-                                                                localFaces[i].nPolySol1,
-                                                                swapFaceInElementSide0,
-                                                                swapFaceInElementSide1) &&
-           standardMatchingFacesGrid[j].SameStandardMatchingFace(VTK_Type,
-                                                                 localFaces[i].JacFaceIsConsideredConstant,
-                                                                 localFaces[i].elemType0,
-                                                                 localFaces[i].nPolyGrid0,
-                                                                 localFaces[i].elemType1,
-                                                                 localFaces[i].nPolyGrid1,
-                                                                 swapFaceInElementSide0,
-                                                                 swapFaceInElementSide1) ) {
+      for (j = 0; j < standardMatchingFacesSol.size(); ++j) {
+        if (standardMatchingFacesSol[j].SameStandardMatchingFace(
+                VTK_Type, localFaces[i].JacFaceIsConsideredConstant, localFaces[i].elemType0, localFaces[i].nPolySol0,
+                localFaces[i].elemType1, localFaces[i].nPolySol1, swapFaceInElementSide0, swapFaceInElementSide1) &&
+            standardMatchingFacesGrid[j].SameStandardMatchingFace(
+                VTK_Type, localFaces[i].JacFaceIsConsideredConstant, localFaces[i].elemType0, localFaces[i].nPolyGrid0,
+                localFaces[i].elemType1, localFaces[i].nPolyGrid1, swapFaceInElementSide0, swapFaceInElementSide1)) {
           matchingFaces[ii].indStandardElement = j;
           break;
         }
       }
 
       /* Create the new standard elements if no match was found. */
-      if(j == standardMatchingFacesSol.size()) {
-
-        standardMatchingFacesSol.push_back(CFEMStandardInternalFace(VTK_Type,
-                                                                    localFaces[i].elemType0,
-                                                                    localFaces[i].nPolySol0,
-                                                                    localFaces[i].elemType1,
-                                                                    localFaces[i].nPolySol1,
-                                                                    localFaces[i].JacFaceIsConsideredConstant,
-                                                                    swapFaceInElementSide0,
-                                                                    swapFaceInElementSide1,
-                                                                    config) );
-
-        standardMatchingFacesGrid.push_back(CFEMStandardInternalFace(VTK_Type,
-                                                                     localFaces[i].elemType0,
-                                                                     localFaces[i].nPolyGrid0,
-                                                                     localFaces[i].elemType1,
-                                                                     localFaces[i].nPolyGrid1,
-                                                                     localFaces[i].JacFaceIsConsideredConstant,
-                                                                     swapFaceInElementSide0,
-                                                                     swapFaceInElementSide1,
-                                                                     config,
-                                                                     standardMatchingFacesSol[j].GetOrderExact()) );
+      if (j == standardMatchingFacesSol.size()) {
+        standardMatchingFacesSol.push_back(CFEMStandardInternalFace(
+            VTK_Type, localFaces[i].elemType0, localFaces[i].nPolySol0, localFaces[i].elemType1,
+            localFaces[i].nPolySol1, localFaces[i].JacFaceIsConsideredConstant, swapFaceInElementSide0,
+            swapFaceInElementSide1, config));
+
+        standardMatchingFacesGrid.push_back(CFEMStandardInternalFace(
+            VTK_Type, localFaces[i].elemType0, localFaces[i].nPolyGrid0, localFaces[i].elemType1,
+            localFaces[i].nPolyGrid1, localFaces[i].JacFaceIsConsideredConstant, swapFaceInElementSide0,
+            swapFaceInElementSide1, config, standardMatchingFacesSol[j].GetOrderExact()));
         matchingFaces[ii].indStandardElement = j;
       }
 
@@ -3180,23 +2918,22 @@ void CMeshFEM_DG::CreateFaces(CConfig *config) {
      of faces per time level is essential for the correct functioning of the code.
      The same holds for the distinction between internal faces and faces that
      are adjacent to a halo element. */
-  for(unsigned short i=0; i<nTimeLevels; ++i) {
-    sort(matchingFaces.begin()+nMatchingFacesInternal[i],
-         matchingFaces.begin()+nMatchingFacesInternal[i+1]);
+  for (unsigned short i = 0; i < nTimeLevels; ++i) {
+    sort(matchingFaces.begin() + nMatchingFacesInternal[i], matchingFaces.begin() + nMatchingFacesInternal[i + 1]);
 
-    sort(matchingFaces.begin()+nMatchingFacesWithHaloElem[i],
-         matchingFaces.begin()+nMatchingFacesWithHaloElem[i+1]);
+    sort(matchingFaces.begin() + nMatchingFacesWithHaloElem[i],
+         matchingFaces.begin() + nMatchingFacesWithHaloElem[i + 1]);
   }
 
   /* Loop over the faces to flag the elements that share one or more faces
      with elements from a lower time level. */
   vector<bool> elemAdjLowTimeLevel(nVolElemTot, false);
-  for(unsigned long i=0; i<matchingFaces.size(); ++i) {
+  for (unsigned long i = 0; i < matchingFaces.size(); ++i) {
     const unsigned long e0 = matchingFaces[i].elemID0;
     const unsigned long e1 = matchingFaces[i].elemID1;
 
-    if(volElem[e0].timeLevel > volElem[e1].timeLevel) elemAdjLowTimeLevel[e0] = true;
-    if(volElem[e1].timeLevel > volElem[e0].timeLevel) elemAdjLowTimeLevel[e1] = true;
+    if (volElem[e0].timeLevel > volElem[e1].timeLevel) elemAdjLowTimeLevel[e0] = true;
+    if (volElem[e1].timeLevel > volElem[e0].timeLevel) elemAdjLowTimeLevel[e1] = true;
   }
 
   /* Determine the list of elements per time level, which share one or more
@@ -3205,14 +2942,12 @@ void CMeshFEM_DG::CreateFaces(CConfig *config) {
   ownedElemAdjLowTimeLevel.resize(nTimeLevels);
   haloElemAdjLowTimeLevel.resize(nTimeLevels);
 
-  for(unsigned long i=0; i<nVolElemOwned; ++i) {
-    if( elemAdjLowTimeLevel[i] )
-      ownedElemAdjLowTimeLevel[volElem[i].timeLevel].push_back(i);
+  for (unsigned long i = 0; i < nVolElemOwned; ++i) {
+    if (elemAdjLowTimeLevel[i]) ownedElemAdjLowTimeLevel[volElem[i].timeLevel].push_back(i);
   }
 
-  for(unsigned long i=nVolElemOwned; i<nVolElemTot; ++i) {
-    if( elemAdjLowTimeLevel[i] )
-      haloElemAdjLowTimeLevel[volElem[i].timeLevel].push_back(i);
+  for (unsigned long i = nVolElemOwned; i < nVolElemTot; ++i) {
+    if (elemAdjLowTimeLevel[i]) haloElemAdjLowTimeLevel[volElem[i].timeLevel].push_back(i);
   }
 
   /* Determine the offsets of the solution DOFs in the solution working vectors
@@ -3220,16 +2955,15 @@ void CMeshFEM_DG::CreateFaces(CConfig *config) {
      accurate local time stepping is employed. */
   vector<unsigned long> counterDOFs(nTimeLevels, 0);
 
-  for(unsigned long i=0; i<nVolElemTot; ++i) {
+  for (unsigned long i = 0; i < nVolElemTot; ++i) {
     const unsigned short lev = volElem[i].timeLevel;
     volElem[i].offsetDOFsSolThisTimeLevel = counterDOFs[lev];
     counterDOFs[lev] += volElem[i].nDOFsSol;
 
-    if( elemAdjLowTimeLevel[i] ) {
-      volElem[i].offsetDOFsSolPrevTimeLevel = counterDOFs[lev-1];
-      counterDOFs[lev-1] += volElem[i].nDOFsSol;
-    }
-    else {
+    if (elemAdjLowTimeLevel[i]) {
+      volElem[i].offsetDOFsSolPrevTimeLevel = counterDOFs[lev - 1];
+      counterDOFs[lev - 1] += volElem[i].nDOFsSol;
+    } else {
       volElem[i].offsetDOFsSolPrevTimeLevel = ULONG_MAX;
     }
   }
@@ -3241,64 +2975,61 @@ void CMeshFEM_DG::CreateFaces(CConfig *config) {
 
   /* Loop over the boundary markers. ---*/
   unsigned long indBegMarker = 0;
-  for(unsigned short iMarker=0; iMarker<nMarker; ++iMarker) {
-
+  for (unsigned short iMarker = 0; iMarker < nMarker; ++iMarker) {
     /* Initialize the number of surface elements per time level to zero. */
-    boundaries[iMarker].nSurfElem.assign(nTimeLevels+1, 0);
+    boundaries[iMarker].nSurfElem.assign(nTimeLevels + 1, 0);
 
     /*--- The periodic boundaries are skipped, because these are not physical
           boundaries and are treated via the halo elements. These have already
           been created. ---*/
-    if( !boundaries[iMarker].periodicBoundary ) {
-
+    if (!boundaries[iMarker].periodicBoundary) {
       /* Determine the end index for this marker in localFaces. Note that
          localFaces is sorted such that the boundary faces are first and
          also grouped per boundary, see the functor CSortFaces. */
       unsigned long indEndMarker = indBegMarker;
-      for(; indEndMarker<localFaces.size(); ++indEndMarker) {
-        if(localFaces[indEndMarker].faceIndicator != (short) iMarker) break;
+      for (; indEndMarker < localFaces.size(); ++indEndMarker) {
+        if (localFaces[indEndMarker].faceIndicator != (short)iMarker) break;
       }
 
       /* Easier storage of the surface elements for this boundary. */
-      vector<CSurfaceElementFEM> &surfElem = boundaries[iMarker].surfElem;
+      vector<CSurfaceElementFEM>& surfElem = boundaries[iMarker].surfElem;
 
       /*--- Loop over range in localFaces for this boundary marker and create
             the connectivity information, which is stored in surfElem. ---*/
-      for(unsigned long i=indBegMarker; i<indEndMarker; ++i) {
-
+      for (unsigned long i = indBegMarker; i < indEndMarker; ++i) {
         /* Determine the time level of the adjacent element and increment
            the number of surface elements for this time level. The +1 is there,
            because this vector will be put in cumulative storage format
            afterwards. */
         ii = i - indBegMarker;
         const unsigned short timeLevel = volElem[surfElem[ii].volElemID].timeLevel;
-        ++boundaries[iMarker].nSurfElem[timeLevel+1];
+        ++boundaries[iMarker].nSurfElem[timeLevel + 1];
 
         /*--- Determine the number of DOFs of the face for both the grid
               and solution. This value depends on the face type. ---*/
         unsigned short sizeDOFsGridFace = 0, sizeDOFsSolFace = 0;
 
-        unsigned short VTK_Type = 0; // To avoid a compiler warning.
-        switch( localFaces[i].nCornerPoints ) {
+        unsigned short VTK_Type = 0;  // To avoid a compiler warning.
+        switch (localFaces[i].nCornerPoints) {
           case 2:
             /* Face is a line. */
             VTK_Type = LINE;
             sizeDOFsGridFace = localFaces[i].nPolyGrid0 + 1;
-            sizeDOFsSolFace  = localFaces[i].nPolySol0  + 1;
+            sizeDOFsSolFace = localFaces[i].nPolySol0 + 1;
             break;
 
           case 3:
             /* Face is a triangle. */
             VTK_Type = TRIANGLE;
-            sizeDOFsGridFace = (localFaces[i].nPolyGrid0+1)*(localFaces[i].nPolyGrid0+2)/2;
-            sizeDOFsSolFace  = (localFaces[i].nPolySol0 +1)*(localFaces[i].nPolySol0 +2)/2;
+            sizeDOFsGridFace = (localFaces[i].nPolyGrid0 + 1) * (localFaces[i].nPolyGrid0 + 2) / 2;
+            sizeDOFsSolFace = (localFaces[i].nPolySol0 + 1) * (localFaces[i].nPolySol0 + 2) / 2;
             break;
 
           case 4:
             /* Face is a quadrilateral. */
             VTK_Type = QUADRILATERAL;
-            sizeDOFsGridFace = (localFaces[i].nPolyGrid0+1)*(localFaces[i].nPolyGrid0+1);
-            sizeDOFsSolFace  = (localFaces[i].nPolySol0 +1)*(localFaces[i].nPolySol0 +1);
+            sizeDOFsGridFace = (localFaces[i].nPolyGrid0 + 1) * (localFaces[i].nPolyGrid0 + 1);
+            sizeDOFsSolFace = (localFaces[i].nPolySol0 + 1) * (localFaces[i].nPolySol0 + 1);
             break;
         }
 
@@ -3316,64 +3047,44 @@ void CMeshFEM_DG::CreateFaces(CConfig *config) {
               sequence as well as the connectivities of the face. The
               connectivities are determined for the grid and solution. ---*/
         bool swapFaceInElement;
-        for(unsigned short j=0; j<volElem[v0].nDOFsSol; ++j)
-          DOFsElem[j] = volElem[v0].offsetDOFsSolLocal + j;
-
-        CreateConnectivitiesFace(VTK_Type,                localFaces[i].cornerPoints,
-                                 volElem[v0].VTK_Type,    volElem[v0].nPolyGrid,
-                                 volElem[v0].nodeIDsGrid, volElem[v0].nPolySol,
-                                 DOFsElem.data(),         swapFaceInElement,
-                                 surfElem[ii].DOFsSolFace.data(),
-                                 surfElem[ii].DOFsSolElement.data());
-
-        for(unsigned short j=0; j<volElem[v0].nDOFsGrid; ++j)
-          DOFsElem[j] = volElem[v0].nodeIDsGrid[j];
-
-        CreateConnectivitiesFace(VTK_Type,                localFaces[i].cornerPoints,
-                                 volElem[v0].VTK_Type,    volElem[v0].nPolyGrid,
-                                 volElem[v0].nodeIDsGrid, volElem[v0].nPolyGrid,
-                                 DOFsElem.data(),         swapFaceInElement,
-                                 surfElem[ii].DOFsGridFace.data(),
-                                 surfElem[ii].DOFsGridElement.data());
+        for (unsigned short j = 0; j < volElem[v0].nDOFsSol; ++j) DOFsElem[j] = volElem[v0].offsetDOFsSolLocal + j;
+
+        CreateConnectivitiesFace(VTK_Type, localFaces[i].cornerPoints, volElem[v0].VTK_Type, volElem[v0].nPolyGrid,
+                                 volElem[v0].nodeIDsGrid, volElem[v0].nPolySol, DOFsElem.data(), swapFaceInElement,
+                                 surfElem[ii].DOFsSolFace.data(), surfElem[ii].DOFsSolElement.data());
+
+        for (unsigned short j = 0; j < volElem[v0].nDOFsGrid; ++j) DOFsElem[j] = volElem[v0].nodeIDsGrid[j];
+
+        CreateConnectivitiesFace(VTK_Type, localFaces[i].cornerPoints, volElem[v0].VTK_Type, volElem[v0].nPolyGrid,
+                                 volElem[v0].nodeIDsGrid, volElem[v0].nPolyGrid, DOFsElem.data(), swapFaceInElement,
+                                 surfElem[ii].DOFsGridFace.data(), surfElem[ii].DOFsGridElement.data());
 
         /*--- Search in the standard elements for boundary faces for a matching
               standard element. If not found, create a new standard element.
               Note that both the grid and the solution representation must
               match with the standard element. ---*/
         unsigned long j;
-        for(j=0; j<standardBoundaryFacesSol.size(); ++j) {
-          if(standardBoundaryFacesSol[j].SameStandardBoundaryFace(VTK_Type,
-                                                                  localFaces[i].JacFaceIsConsideredConstant,
-                                                                  localFaces[i].elemType0,
-                                                                  localFaces[i].nPolySol0,
-                                                                  swapFaceInElement) &&
-             standardBoundaryFacesGrid[j].SameStandardBoundaryFace(VTK_Type,
-                                                                   localFaces[i].JacFaceIsConsideredConstant,
-                                                                   localFaces[i].elemType0,
-                                                                   localFaces[i].nPolyGrid0,
-                                                                   swapFaceInElement) ) {
+        for (j = 0; j < standardBoundaryFacesSol.size(); ++j) {
+          if (standardBoundaryFacesSol[j].SameStandardBoundaryFace(VTK_Type, localFaces[i].JacFaceIsConsideredConstant,
+                                                                   localFaces[i].elemType0, localFaces[i].nPolySol0,
+                                                                   swapFaceInElement) &&
+              standardBoundaryFacesGrid[j].SameStandardBoundaryFace(VTK_Type, localFaces[i].JacFaceIsConsideredConstant,
+                                                                    localFaces[i].elemType0, localFaces[i].nPolyGrid0,
+                                                                    swapFaceInElement)) {
             surfElem[ii].indStandardElement = j;
             break;
           }
         }
 
         /* Create the new standard elements if no match was found. */
-        if(j == standardBoundaryFacesSol.size()) {
-
-          standardBoundaryFacesSol.push_back(CFEMStandardBoundaryFace(VTK_Type,
-                                                                      localFaces[i].elemType0,
-                                                                      localFaces[i].nPolySol0,
-                                                                      localFaces[i].JacFaceIsConsideredConstant,
-                                                                      swapFaceInElement,
-                                                                      config) );
-
-          standardBoundaryFacesGrid.push_back(CFEMStandardBoundaryFace(VTK_Type,
-                                                                       localFaces[i].elemType0,
-                                                                       localFaces[i].nPolyGrid0,
-                                                                       localFaces[i].JacFaceIsConsideredConstant,
-                                                                       swapFaceInElement,
-                                                                       config,
-                                                                       standardBoundaryFacesSol[j].GetOrderExact()) );
+        if (j == standardBoundaryFacesSol.size()) {
+          standardBoundaryFacesSol.push_back(
+              CFEMStandardBoundaryFace(VTK_Type, localFaces[i].elemType0, localFaces[i].nPolySol0,
+                                       localFaces[i].JacFaceIsConsideredConstant, swapFaceInElement, config));
+
+          standardBoundaryFacesGrid.push_back(CFEMStandardBoundaryFace(
+              VTK_Type, localFaces[i].elemType0, localFaces[i].nPolyGrid0, localFaces[i].JacFaceIsConsideredConstant,
+              swapFaceInElement, config, standardBoundaryFacesSol[j].GetOrderExact()));
           surfElem[ii].indStandardElement = j;
         }
       }
@@ -3382,24 +3093,22 @@ void CMeshFEM_DG::CreateFaces(CConfig *config) {
       indBegMarker = indEndMarker;
 
       /* Put boundaries[iMarker].nSurfElem in cumulative storage. */
-      for(unsigned short i=0; i<nTimeLevels; ++i)
-        boundaries[iMarker].nSurfElem[i+1] += boundaries[iMarker].nSurfElem[i];
+      for (unsigned short i = 0; i < nTimeLevels; ++i)
+        boundaries[iMarker].nSurfElem[i + 1] += boundaries[iMarker].nSurfElem[i];
 
       /* Carry out another sort of the surface elements, such that surface elements
          belonging to the same standard element are contiguous in memory. In this
          way a simultaneous treatment of several surface elements is possible, which
          increases the performance. Note that this renumbering must happen within
          each time level. */
-      for(unsigned short i=0; i<nTimeLevels; ++i)
-        sort(surfElem.begin()+boundaries[iMarker].nSurfElem[i],
-             surfElem.begin()+boundaries[iMarker].nSurfElem[i+1],
-             CSortBoundaryFaces());
+      for (unsigned short i = 0; i < nTimeLevels; ++i)
+        sort(surfElem.begin() + boundaries[iMarker].nSurfElem[i],
+             surfElem.begin() + boundaries[iMarker].nSurfElem[i + 1], CSortBoundaryFaces());
     }
   }
 }
 
-void CMeshFEM_DG::CreateStandardVolumeElements(CConfig *config) {
-
+void CMeshFEM_DG::CreateStandardVolumeElements(CConfig* config) {
   /*--- Loop over the volume elements and create new standard elements if needed.
         Note that a new standard element is created when either the solution
         element or the grid element does not match. Note further that for the
@@ -3407,45 +3116,34 @@ void CMeshFEM_DG::CreateStandardVolumeElements(CConfig *config) {
         solution is used, such that the metric terms are computed in the correct
         integration points in case the polynomial order of the solution differs
         from that of the grid. ---*/
-  for(unsigned long i=0; i<nVolElemTot; ++i) {
-
+  for (unsigned long i = 0; i < nVolElemTot; ++i) {
     /* Check the existing standard elements in the list. */
     unsigned long j;
-    for(j=0; j<standardElementsSol.size(); ++j) {
-      if(standardElementsSol[j].SameStandardElement(volElem[i].VTK_Type,
-                                                    volElem[i].nPolySol,
-                                                    volElem[i].JacIsConsideredConstant) &&
-         standardElementsGrid[j].SameStandardElement(volElem[i].VTK_Type,
-                                                     volElem[i].nPolyGrid,
-                                                     volElem[i].JacIsConsideredConstant) ) {
-         volElem[i].indStandardElement = j;
-         break;
+    for (j = 0; j < standardElementsSol.size(); ++j) {
+      if (standardElementsSol[j].SameStandardElement(volElem[i].VTK_Type, volElem[i].nPolySol,
+                                                     volElem[i].JacIsConsideredConstant) &&
+          standardElementsGrid[j].SameStandardElement(volElem[i].VTK_Type, volElem[i].nPolyGrid,
+                                                      volElem[i].JacIsConsideredConstant)) {
+        volElem[i].indStandardElement = j;
+        break;
       }
     }
 
     /* Create the new standard elements if no match was found. */
-    if(j == standardElementsSol.size()) {
-
-      standardElementsSol.push_back(CFEMStandardElement(volElem[i].VTK_Type,
-                                                        volElem[i].nPolySol,
-                                                        volElem[i].JacIsConsideredConstant,
-                                                        config) );
-
-      standardElementsGrid.push_back(CFEMStandardElement(volElem[i].VTK_Type,
-                                                         volElem[i].nPolyGrid,
-                                                         volElem[i].JacIsConsideredConstant,
-                                                         config,
-                                                         standardElementsSol[j].GetOrderExact(),
-                                                         standardElementsSol[j].GetRDOFs(),
-                                                         standardElementsSol[j].GetSDOFs(),
-                                                         standardElementsSol[j].GetTDOFs()) );
+    if (j == standardElementsSol.size()) {
+      standardElementsSol.push_back(
+          CFEMStandardElement(volElem[i].VTK_Type, volElem[i].nPolySol, volElem[i].JacIsConsideredConstant, config));
+
+      standardElementsGrid.push_back(
+          CFEMStandardElement(volElem[i].VTK_Type, volElem[i].nPolyGrid, volElem[i].JacIsConsideredConstant, config,
+                              standardElementsSol[j].GetOrderExact(), standardElementsSol[j].GetRDOFs(),
+                              standardElementsSol[j].GetSDOFs(), standardElementsSol[j].GetTDOFs()));
       volElem[i].indStandardElement = j;
     }
   }
 }
 
-void CMeshFEM_DG::SetSendReceive(const CConfig *config) {
-
+void CMeshFEM_DG::SetSendReceive(const CConfig* config) {
   /*----------------------------------------------------------------------------*/
   /*--- Step 1: Determine the ranks from which this rank has to receive data ---*/
   /*---         during the actual communication of halo data, as well as the ---*/
@@ -3455,28 +3153,25 @@ void CMeshFEM_DG::SetSendReceive(const CConfig *config) {
   /* Determine for every element the local offset of the solution DOFs.
      The if statement in the line below is to avoid problems when the
      partition is empty. */
-  if( nVolElemTot ) volElem[0].offsetDOFsSolLocal = 0;
-  for(unsigned long i=1; i<nVolElemTot; ++i)
-    volElem[i].offsetDOFsSolLocal = volElem[i-1].offsetDOFsSolLocal
-                                  + volElem[i-1].nDOFsSol;
+  if (nVolElemTot) volElem[0].offsetDOFsSolLocal = 0;
+  for (unsigned long i = 1; i < nVolElemTot; ++i)
+    volElem[i].offsetDOFsSolLocal = volElem[i - 1].offsetDOFsSolLocal + volElem[i - 1].nDOFsSol;
 
   /* Determine the ranks from which this rank will receive halo data. */
   vector<int> recvFromRank(size, 0);
-  for(unsigned long i=nVolElemOwned; i<nVolElemTot; ++i)
-    recvFromRank[volElem[i].rankOriginal] = 1;
+  for (unsigned long i = nVolElemOwned; i < nVolElemTot; ++i) recvFromRank[volElem[i].rankOriginal] = 1;
 
-  map<int,int> rankToIndRecvBuf;
-  for(int i=0; i<size; ++i) {
-    if( recvFromRank[i] ) {
+  map<int, int> rankToIndRecvBuf;
+  for (int i = 0; i < size; ++i) {
+    if (recvFromRank[i]) {
       int ind = (int)rankToIndRecvBuf.size();
       rankToIndRecvBuf[i] = ind;
     }
   }
 
   ranksRecv.resize(rankToIndRecvBuf.size());
-  map<int,int>::const_iterator MI = rankToIndRecvBuf.begin();
-  for(unsigned long i=0; i<rankToIndRecvBuf.size(); ++i, ++MI)
-    ranksRecv[i] = MI->first;
+  map<int, int>::const_iterator MI = rankToIndRecvBuf.begin();
+  for (unsigned long i = 0; i < rankToIndRecvBuf.size(); ++i, ++MI) ranksRecv[i] = MI->first;
 
   /* Define and determine the buffers to send the global indices of my halo
      elements to the appropriate ranks and the vectors which store the
@@ -3484,7 +3179,7 @@ void CMeshFEM_DG::SetSendReceive(const CConfig *config) {
   vector<vector<unsigned long> > longBuf(rankToIndRecvBuf.size(), vector<unsigned long>(0));
   entitiesRecv.resize(rankToIndRecvBuf.size());
 
-  for(unsigned long i=nVolElemOwned; i<nVolElemTot; ++i) {
+  for (unsigned long i = nVolElemOwned; i < nVolElemTot; ++i) {
     MI = rankToIndRecvBuf.find(volElem[i].rankOriginal);
     longBuf[MI->second].push_back(volElem[i].elemIDGlobal);
 
@@ -3492,9 +3187,8 @@ void CMeshFEM_DG::SetSendReceive(const CConfig *config) {
   }
 
   /* Determine the mapping from global element ID to local owned element ID. */
-  map<unsigned long,unsigned long> globalElemIDToLocalInd;
-  for(unsigned long i=0; i<nVolElemOwned; ++i)
-    globalElemIDToLocalInd[volElem[i].elemIDGlobal] = i;
+  map<unsigned long, unsigned long> globalElemIDToLocalInd;
+  for (unsigned long i = 0; i < nVolElemOwned; ++i) globalElemIDToLocalInd[volElem[i].elemIDGlobal] = i;
 
 #ifdef HAVE_MPI
 
@@ -3503,8 +3197,7 @@ void CMeshFEM_DG::SetSendReceive(const CConfig *config) {
   int nRankSend;
   vector<int> sizeReduce(size, 1);
 
-  SU2_MPI::Reduce_scatter(recvFromRank.data(), &nRankSend, sizeReduce.data(),
-                          MPI_INT, MPI_SUM, SU2_MPI::GetComm());
+  SU2_MPI::Reduce_scatter(recvFromRank.data(), &nRankSend, sizeReduce.data(), MPI_INT, MPI_SUM, SU2_MPI::GetComm());
 
   /* Resize ranksSend and the first index of entitiesSend to the number of
      ranks to which this rank has to send data. */
@@ -3514,16 +3207,15 @@ void CMeshFEM_DG::SetSendReceive(const CConfig *config) {
   /*--- Send all the data using non-blocking sends. ---*/
   vector<SU2_MPI::Request> commReqs(ranksRecv.size());
 
-  for(unsigned long i=0; i<ranksRecv.size(); ++i) {
+  for (unsigned long i = 0; i < ranksRecv.size(); ++i) {
     int dest = ranksRecv[i];
-    SU2_MPI::Isend(longBuf[i].data(), longBuf[i].size(), MPI_UNSIGNED_LONG,
-                   dest, dest, SU2_MPI::GetComm(), &commReqs[i]);
+    SU2_MPI::Isend(longBuf[i].data(), longBuf[i].size(), MPI_UNSIGNED_LONG, dest, dest, SU2_MPI::GetComm(),
+                   &commReqs[i]);
   }
 
   /* Loop over the number of ranks from which I receive data about the
      global element ID's that I must send. */
-  for(int i=0; i<nRankSend; ++i) {
-
+  for (int i = 0; i < nRankSend; ++i) {
     /* Block until a message arrivesi and determine the source. */
     SU2_MPI::Status status;
     SU2_MPI::Probe(MPI_ANY_SOURCE, rank, SU2_MPI::GetComm(), &status);
@@ -3535,17 +3227,15 @@ void CMeshFEM_DG::SetSendReceive(const CConfig *config) {
     SU2_MPI::Get_count(&status, MPI_UNSIGNED_LONG, &sizeMess);
 
     entitiesSend[i].resize(sizeMess);
-    SU2_MPI::Recv(entitiesSend[i].data(), sizeMess, MPI_UNSIGNED_LONG,
-                  ranksSend[i], rank, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Recv(entitiesSend[i].data(), sizeMess, MPI_UNSIGNED_LONG, ranksSend[i], rank, SU2_MPI::GetComm(), &status);
 
     /* Convert the global indices currently stored in entitiesSend[i]
        to local indices. */
-    for(int j=0; j<sizeMess; ++j) {
-      map<unsigned long,unsigned long>::const_iterator LMI;
+    for (int j = 0; j < sizeMess; ++j) {
+      map<unsigned long, unsigned long>::const_iterator LMI;
       LMI = globalElemIDToLocalInd.find(entitiesSend[i][j]);
 
-      if(LMI == globalElemIDToLocalInd.end())
-        SU2_MPI::Error("This should not happen", CURRENT_FUNCTION);
+      if (LMI == globalElemIDToLocalInd.end()) SU2_MPI::Error("This should not happen", CURRENT_FUNCTION);
 
       entitiesSend[i][j] = LMI->second;
     }
@@ -3566,16 +3256,14 @@ void CMeshFEM_DG::SetSendReceive(const CConfig *config) {
   /* Convert the global element ID's of longBuf to local indices, which are
      stored in entitiesSend[0]. Note that an additional test for longBuf.size()
      is necessary to avoid problems. */
-  if( longBuf.size() ) {
-
+  if (longBuf.size()) {
     entitiesSend[0].resize(longBuf[0].size());
 
-    for(unsigned long i=0; i<longBuf[0].size(); ++i) {
-      map<unsigned long,unsigned long>::const_iterator LMI;
+    for (unsigned long i = 0; i < longBuf[0].size(); ++i) {
+      map<unsigned long, unsigned long>::const_iterator LMI;
       LMI = globalElemIDToLocalInd.find(longBuf[0][i]);
 
-      if(LMI == globalElemIDToLocalInd.end())
-        SU2_MPI::Error("This should not happen", CURRENT_FUNCTION);
+      if (LMI == globalElemIDToLocalInd.end()) SU2_MPI::Error("This should not happen", CURRENT_FUNCTION);
 
       entitiesSend[0][i] = LMI->second;
     }
@@ -3591,14 +3279,12 @@ void CMeshFEM_DG::SetSendReceive(const CConfig *config) {
   /*--- Loop over the markers and determine the mapping for the rotationally
         periodic transformations. The mapping is from the marker to the first
         index in the vectors to store the rotationally periodic halo elements. ---*/
-  map<short,unsigned short> mapRotationalPeriodicToInd;
-
-  for(unsigned short iMarker=0; iMarker<nMarker; ++iMarker) {
-    if(config->GetMarker_All_KindBC(iMarker) == PERIODIC_BOUNDARY) {
+  map<short, unsigned short> mapRotationalPeriodicToInd;
 
+  for (unsigned short iMarker = 0; iMarker < nMarker; ++iMarker) {
+    if (config->GetMarker_All_KindBC(iMarker) == PERIODIC_BOUNDARY) {
       auto angles = config->GetPeriodicRotAngles(config->GetMarker_All_TagBound(iMarker));
-      if(fabs(angles[0]) > 1.e-5 || fabs(angles[1]) > 1.e-5 || fabs(angles[2]) > 1.e-5) {
-
+      if (fabs(angles[0]) > 1.e-5 || fabs(angles[1]) > 1.e-5 || fabs(angles[2]) > 1.e-5) {
         unsigned short curSize = mapRotationalPeriodicToInd.size();
         mapRotationalPeriodicToInd[iMarker] = curSize;
       }
@@ -3607,8 +3293,8 @@ void CMeshFEM_DG::SetSendReceive(const CConfig *config) {
 
   /* Store the rotationally periodic indices in rotPerMarkers. */
   rotPerMarkers.reserve(mapRotationalPeriodicToInd.size());
-  for(map<short,unsigned short>::iterator SMI =mapRotationalPeriodicToInd.begin();
-                                          SMI!=mapRotationalPeriodicToInd.end(); ++SMI)
+  for (map<short, unsigned short>::iterator SMI = mapRotationalPeriodicToInd.begin();
+       SMI != mapRotationalPeriodicToInd.end(); ++SMI)
     rotPerMarkers.push_back(SMI->first);
 
   /* Resize the first index of rotPerHalos to the correct size. */
@@ -3616,29 +3302,21 @@ void CMeshFEM_DG::SetSendReceive(const CConfig *config) {
 
   /*--- Loop over the volume elements and store the indices of the rotationally
         periodic halo elements in rotPerHalos.     ---*/
-  for(unsigned long i=nVolElemOwned; i<nVolElemTot; ++i) {
-    if(volElem[i].periodIndexToDonor > -1) {
-      map<short,unsigned short>::const_iterator SMI;
+  for (unsigned long i = nVolElemOwned; i < nVolElemTot; ++i) {
+    if (volElem[i].periodIndexToDonor > -1) {
+      map<short, unsigned short>::const_iterator SMI;
       SMI = mapRotationalPeriodicToInd.find(volElem[i].periodIndexToDonor);
 
-      if(SMI != mapRotationalPeriodicToInd.end())
-        rotPerHalos[SMI->second].push_back(i);
+      if (SMI != mapRotationalPeriodicToInd.end()) rotPerHalos[SMI->second].push_back(i);
     }
   }
 }
 
-void CMeshFEM_DG::CreateConnectivitiesFace(
-                                const unsigned short        VTK_TypeFace,
-                                const unsigned long         *cornerPointsFace,
-                                const unsigned short        VTK_TypeElem,
-                                const unsigned short        nPolyGrid,
-                                const vector<unsigned long> &elemNodeIDsGrid,
-                                const unsigned short        nPolyConn,
-                                const unsigned long         *connElem,
-                                bool                        &swapFaceInElement,
-                                unsigned long               *modConnFace,
-                                unsigned long               *modConnElem) {
-
+void CMeshFEM_DG::CreateConnectivitiesFace(const unsigned short VTK_TypeFace, const unsigned long* cornerPointsFace,
+                                           const unsigned short VTK_TypeElem, const unsigned short nPolyGrid,
+                                           const vector<unsigned long>& elemNodeIDsGrid, const unsigned short nPolyConn,
+                                           const unsigned long* connElem, bool& swapFaceInElement,
+                                           unsigned long* modConnFace, unsigned long* modConnElem) {
   /*--- Set swapFaceInElement to false. This variable is only relevant for
         triangular faces of a pyramid and quadrilateral faces of a prism.
         Only for these situations this variable will be passed to the
@@ -3647,42 +3325,32 @@ void CMeshFEM_DG::CreateConnectivitiesFace(
 
   /*--- Make a distinction between the types of the volume element and call
         the appropriate function to do the actual job. ---*/
-  switch( VTK_TypeElem ) {
+  switch (VTK_TypeElem) {
     case TRIANGLE:
-      CreateConnectivitiesLineAdjacentTriangle(cornerPointsFace, nPolyGrid,
-                                               elemNodeIDsGrid,  nPolyConn,
-                                               connElem,         modConnFace,
-                                               modConnElem);
+      CreateConnectivitiesLineAdjacentTriangle(cornerPointsFace, nPolyGrid, elemNodeIDsGrid, nPolyConn, connElem,
+                                               modConnFace, modConnElem);
       break;
 
     case QUADRILATERAL:
-      CreateConnectivitiesLineAdjacentQuadrilateral(cornerPointsFace, nPolyGrid,
-                                                    elemNodeIDsGrid,  nPolyConn,
-                                                    connElem,         modConnFace,
-                                                    modConnElem);
+      CreateConnectivitiesLineAdjacentQuadrilateral(cornerPointsFace, nPolyGrid, elemNodeIDsGrid, nPolyConn, connElem,
+                                                    modConnFace, modConnElem);
       break;
 
     case TETRAHEDRON:
-      CreateConnectivitiesTriangleAdjacentTetrahedron(cornerPointsFace, nPolyGrid,
-                                                      elemNodeIDsGrid,  nPolyConn,
-                                                      connElem,         modConnFace,
-                                                      modConnElem);
+      CreateConnectivitiesTriangleAdjacentTetrahedron(cornerPointsFace, nPolyGrid, elemNodeIDsGrid, nPolyConn, connElem,
+                                                      modConnFace, modConnElem);
       break;
 
     case PYRAMID: {
-      switch( VTK_TypeFace ) {
+      switch (VTK_TypeFace) {
         case TRIANGLE:
-          CreateConnectivitiesTriangleAdjacentPyramid(cornerPointsFace, nPolyGrid,
-                                                      elemNodeIDsGrid,  nPolyConn,
-                                                      connElem,         swapFaceInElement,
-                                                      modConnFace,      modConnElem);
+          CreateConnectivitiesTriangleAdjacentPyramid(cornerPointsFace, nPolyGrid, elemNodeIDsGrid, nPolyConn, connElem,
+                                                      swapFaceInElement, modConnFace, modConnElem);
           break;
 
         case QUADRILATERAL:
-          CreateConnectivitiesQuadrilateralAdjacentPyramid(cornerPointsFace, nPolyGrid,
-                                                           elemNodeIDsGrid,  nPolyConn,
-                                                           connElem,         modConnFace,
-                                                           modConnElem);
+          CreateConnectivitiesQuadrilateralAdjacentPyramid(cornerPointsFace, nPolyGrid, elemNodeIDsGrid, nPolyConn,
+                                                           connElem, modConnFace, modConnElem);
           break;
       }
 
@@ -3690,19 +3358,15 @@ void CMeshFEM_DG::CreateConnectivitiesFace(
     }
 
     case PRISM: {
-      switch( VTK_TypeFace ) {
+      switch (VTK_TypeFace) {
         case TRIANGLE:
-          CreateConnectivitiesTriangleAdjacentPrism(cornerPointsFace, nPolyGrid,
-                                                    elemNodeIDsGrid,  nPolyConn,
-                                                    connElem,         modConnFace,
-                                                    modConnElem);
+          CreateConnectivitiesTriangleAdjacentPrism(cornerPointsFace, nPolyGrid, elemNodeIDsGrid, nPolyConn, connElem,
+                                                    modConnFace, modConnElem);
           break;
 
         case QUADRILATERAL:
-          CreateConnectivitiesQuadrilateralAdjacentPrism(cornerPointsFace, nPolyGrid,
-                                                         elemNodeIDsGrid,  nPolyConn,
-                                                         connElem,         swapFaceInElement,
-                                                         modConnFace,      modConnElem);
+          CreateConnectivitiesQuadrilateralAdjacentPrism(cornerPointsFace, nPolyGrid, elemNodeIDsGrid, nPolyConn,
+                                                         connElem, swapFaceInElement, modConnFace, modConnElem);
           break;
       }
 
@@ -3710,27 +3374,20 @@ void CMeshFEM_DG::CreateConnectivitiesFace(
     }
 
     case HEXAHEDRON:
-      CreateConnectivitiesQuadrilateralAdjacentHexahedron(cornerPointsFace, nPolyGrid,
-                                                          elemNodeIDsGrid,  nPolyConn,
-                                                          connElem,         modConnFace,
-                                                          modConnElem);
+      CreateConnectivitiesQuadrilateralAdjacentHexahedron(cornerPointsFace, nPolyGrid, elemNodeIDsGrid, nPolyConn,
+                                                          connElem, modConnFace, modConnElem);
       break;
   }
 }
 
 void CMeshFEM_DG::CreateConnectivitiesLineAdjacentQuadrilateral(
-                                const unsigned long         *cornerPointsLine,
-                                const unsigned short        nPolyGrid,
-                                const vector<unsigned long> &quadNodeIDsGrid,
-                                const unsigned short        nPolyConn,
-                                const unsigned long         *connQuad,
-                                unsigned long               *modConnLine,
-                                unsigned long               *modConnQuad) {
-
+    const unsigned long* cornerPointsLine, const unsigned short nPolyGrid, const vector<unsigned long>& quadNodeIDsGrid,
+    const unsigned short nPolyConn, const unsigned long* connQuad, unsigned long* modConnLine,
+    unsigned long* modConnQuad) {
   /* Determine the indices of the four corner points of the quadrilateral. */
   const unsigned short ind0 = 0;
   const unsigned short ind1 = nPolyGrid;
-  const unsigned short ind2 = (nPolyGrid+1)*(nPolyGrid+1) -1;
+  const unsigned short ind2 = (nPolyGrid + 1) * (nPolyGrid + 1) - 1;
   const unsigned short ind3 = ind2 - nPolyGrid;
 
   /* Easier storage of the two corner points of the line in the new numbering. */
@@ -3746,96 +3403,106 @@ void CMeshFEM_DG::CreateConnectivitiesLineAdjacentQuadrilateral(
         of the quad. This is determined below. The bool verticesDontMatch is
         there to check if vertices do not match. This should not happen, but
         it is checked for security. ---*/
-  signed short a=0, b=0, c=0, d=0, e=0, f=0;
+  signed short a = 0, b = 0, c = 0, d = 0, e = 0, f = 0;
   bool verticesDontMatch = false;
 
-  if(vert0 == quadNodeIDsGrid[ind0]) {
+  if (vert0 == quadNodeIDsGrid[ind0]) {
     /* Vert0 coincides with vertex 0 of the quad connectivity.
        Determine the situation for vert1. */
-    if(vert1 == quadNodeIDsGrid[ind1]){
+    if (vert1 == quadNodeIDsGrid[ind1]) {
       /* The new numbering is the same as the original numbering. */
-      a = d = 0; b = f = 1; c = e = 0;
-    }
-    else if(vert1 == quadNodeIDsGrid[ind3]) {
+      a = d = 0;
+      b = f = 1;
+      c = e = 0;
+    } else if (vert1 == quadNodeIDsGrid[ind3]) {
       /* The i and j numbering are swapped. This is a left handed transformation. */
-      a = d = 0; b = f = 0; c = e = 1;
-    }
-    else {
+      a = d = 0;
+      b = f = 0;
+      c = e = 1;
+    } else {
       verticesDontMatch = true;  // Vert1 does not match with a neigbor.
     }
-  }
-  else if(vert0 == quadNodeIDsGrid[ind1]) {
+  } else if (vert0 == quadNodeIDsGrid[ind1]) {
     /* Vert0 coincides with vertex 1 of the quad connectivity.
        Determine the situation for vert1. */
-    if(vert1 == quadNodeIDsGrid[ind2]){
+    if (vert1 == quadNodeIDsGrid[ind2]) {
       /* The i-direction of the new numbering corresponds to the j-direction
          of the original numbering, while the new j-direction is the negative
          i-direction of the original numbering. */
-      a = 0; d = nPolyConn; b = f = 0; c = 1; e = -1;
-    }
-    else if(vert1 == quadNodeIDsGrid[ind0]) {
+      a = 0;
+      d = nPolyConn;
+      b = f = 0;
+      c = 1;
+      e = -1;
+    } else if (vert1 == quadNodeIDsGrid[ind0]) {
       /* The i-direction is negated, while the j-direction coincides.
          This is a left handed transformation. */
-      a = nPolyConn; d = 0; b = -1; f = 1; c = e = 0;
-    }
-    else {
+      a = nPolyConn;
+      d = 0;
+      b = -1;
+      f = 1;
+      c = e = 0;
+    } else {
       verticesDontMatch = true;  // Vert1 does not match with a neigbor.
     }
-  }
-  else if(vert0 == quadNodeIDsGrid[ind2]) {
+  } else if (vert0 == quadNodeIDsGrid[ind2]) {
     /* Vert0 coincides with vertex 2 of the quad connectivity.
        Determine the situation for vert1. */
-    if(vert1 == quadNodeIDsGrid[ind3]){
+    if (vert1 == quadNodeIDsGrid[ind3]) {
       /* Both the i- and j-direction are negated. */
-      a = d = nPolyConn; b = f = -1; c = e = 0;
-    }
-    else if(vert1 == quadNodeIDsGrid[ind1]) {
+      a = d = nPolyConn;
+      b = f = -1;
+      c = e = 0;
+    } else if (vert1 == quadNodeIDsGrid[ind1]) {
       /* The new i-direction is the original negative j-direction, while the
          new j-direction is the original negative i-direction. This is a
          left handed transformation. */
-      a = d = nPolyConn; b = f = 0; c = e = -1;
-    }
-    else {
+      a = d = nPolyConn;
+      b = f = 0;
+      c = e = -1;
+    } else {
       verticesDontMatch = true;  // Vert1 does not match with a neigbor.
     }
-  }
-  else if(vert0 == quadNodeIDsGrid[ind3]) {
+  } else if (vert0 == quadNodeIDsGrid[ind3]) {
     /* Vert0 coincides with vertex 3 of the quad connectivity.
        Determine the situation for vert1. */
-    if(vert1 == quadNodeIDsGrid[ind0]){
+    if (vert1 == quadNodeIDsGrid[ind0]) {
       /* The new i-direction is the original negative j-direction, while the
          new j-direction is the original i-direction. */
-      a = nPolyConn; d = 0; b = f = 0; c = -1; e = 1;
-    }
-    else if(vert1 == quadNodeIDsGrid[ind2]){
+      a = nPolyConn;
+      d = 0;
+      b = f = 0;
+      c = -1;
+      e = 1;
+    } else if (vert1 == quadNodeIDsGrid[ind2]) {
       /* The i-directions coincide while the j-direction is negated.
          This is a left handed transformation. */
-      a = 0; d = nPolyConn; b = 1; f = -1; c = e = 0;
-    }
-    else {
+      a = 0;
+      d = nPolyConn;
+      b = 1;
+      f = -1;
+      c = e = 0;
+    } else {
       verticesDontMatch = true;  // Vert1 does not match with a neigbor.
     }
-  }
-  else {
+  } else {
     /* Vert0 does not match with any of the corner vertices of the quad. */
     verticesDontMatch = true;
   }
 
   /*--- If non-matching vertices have been found, terminate with an error message. ---*/
-  if( verticesDontMatch )
-    SU2_MPI::Error("Corner vertices do not match. This should not happen.", CURRENT_FUNCTION);
+  if (verticesDontMatch) SU2_MPI::Error("Corner vertices do not match. This should not happen.", CURRENT_FUNCTION);
 
   /*--- Loop over the DOFs of the original quad to create the connectivity
         of the quad that corresponds to the new numbering. ---*/
   unsigned short ind = 0;
-  for(unsigned short j=0; j<=nPolyConn; ++j) {
-    for(unsigned short i=0; i<=nPolyConn; ++i, ++ind) {
-
+  for (unsigned short j = 0; j <= nPolyConn; ++j) {
+    for (unsigned short i = 0; i <= nPolyConn; ++i, ++ind) {
       /*--- Determine the ii and jj indices of the new numbering, convert it to
             a 1D index and shore the modified index in modConnQuad. ---*/
-      unsigned short ii   = a + i*b + j*c;
-      unsigned short jj   = d + i*e + j*f;
-      unsigned short iind = jj*(nPolyConn+1) + ii;
+      unsigned short ii = a + i * b + j * c;
+      unsigned short jj = d + i * e + j * f;
+      unsigned short iind = jj * (nPolyConn + 1) + ii;
 
       modConnQuad[iind] = connQuad[ind];
     }
@@ -3844,23 +3511,19 @@ void CMeshFEM_DG::CreateConnectivitiesLineAdjacentQuadrilateral(
   /*--- The line corresponds to face 0 of the quadrilateral. Hence the first
         nPolyConn+1 entries in modConnQuad are the DOFs of the line. Copy
         these entries from modConnQuad. ---*/
-  for(unsigned short i=0; i<=nPolyConn; ++i)
-    modConnLine[i] = modConnQuad[i];
+  for (unsigned short i = 0; i <= nPolyConn; ++i) modConnLine[i] = modConnQuad[i];
 }
 
-void CMeshFEM_DG::CreateConnectivitiesLineAdjacentTriangle(
-                                const unsigned long         *cornerPointsLine,
-                                const unsigned short        nPolyGrid,
-                                const vector<unsigned long> &triaNodeIDsGrid,
-                                const unsigned short        nPolyConn,
-                                const unsigned long         *connTria,
-                                unsigned long               *modConnLine,
-                                unsigned long               *modConnTria) {
-
+void CMeshFEM_DG::CreateConnectivitiesLineAdjacentTriangle(const unsigned long* cornerPointsLine,
+                                                           const unsigned short nPolyGrid,
+                                                           const vector<unsigned long>& triaNodeIDsGrid,
+                                                           const unsigned short nPolyConn,
+                                                           const unsigned long* connTria, unsigned long* modConnLine,
+                                                           unsigned long* modConnTria) {
   /* Determine the indices of the 3 corner vertices of the triangle. */
   const unsigned short ind0 = 0;
   const unsigned short ind1 = nPolyGrid;
-  const unsigned short ind2 = (nPolyGrid+1)*(nPolyGrid+2)/2 -1;
+  const unsigned short ind2 = (nPolyGrid + 1) * (nPolyGrid + 2) / 2 - 1;
 
   /* Easier storage of the two corner points of the line in the new numbering. */
   const unsigned long vert0 = cornerPointsLine[0];
@@ -3875,81 +3538,101 @@ void CMeshFEM_DG::CreateConnectivitiesLineAdjacentTriangle(
         of the triangle. This is determined below. The bool verticesDontMatch is
         there to check if vertices do not match. This should not happen, but
         it is checked for security. ---*/
-  signed short a=0, b=0, c=0, d=0, e=0, f=0;
+  signed short a = 0, b = 0, c = 0, d = 0, e = 0, f = 0;
   bool verticesDontMatch = false;
 
-  if(vert0 == triaNodeIDsGrid[ind0]) {
+  if (vert0 == triaNodeIDsGrid[ind0]) {
     /* Vert0 coincides with vertex 0 of the triangle connectivity.
        Determine the situation for vert1. */
-    if(vert1 == triaNodeIDsGrid[ind1]){
+    if (vert1 == triaNodeIDsGrid[ind1]) {
       /* The new numbering is the same as the original numbering. */
-      a = 0; b = 1; c = 0; d = 0; e = 0; f = 1;
-    }
-    else if(vert1 == triaNodeIDsGrid[ind2]) {
+      a = 0;
+      b = 1;
+      c = 0;
+      d = 0;
+      e = 0;
+      f = 1;
+    } else if (vert1 == triaNodeIDsGrid[ind2]) {
       /* The i and j numbering are swapped. This is a left handed transformation. */
-      a = 0; b = 0; c = 1; d = 0; e = 1; f = 0;
-    }
-    else {
+      a = 0;
+      b = 0;
+      c = 1;
+      d = 0;
+      e = 1;
+      f = 0;
+    } else {
       verticesDontMatch = true;  // Vert1 does not match with a neigbor.
     }
-  }
-  else if(vert0 == triaNodeIDsGrid[ind1]) {
+  } else if (vert0 == triaNodeIDsGrid[ind1]) {
     /* Vert0 coincides with vertex 1 of the triangle connectivity.
        Determine the situation for vert1. */
-    if(vert1 == triaNodeIDsGrid[ind2]){
+    if (vert1 == triaNodeIDsGrid[ind2]) {
       /* The i-direction of the new numbering corresponds to the j-direction
          of the original numbering, while the new j-direction corresponds to
          a combination of the original i- and j-direction. */
-      a = 0; b = 0; c = 1; d = nPolyConn; e = -1; f = -1;
-    }
-    else if(vert1 == triaNodeIDsGrid[ind0]) {
+      a = 0;
+      b = 0;
+      c = 1;
+      d = nPolyConn;
+      e = -1;
+      f = -1;
+    } else if (vert1 == triaNodeIDsGrid[ind0]) {
       /* The i-direction of the new numbering corresponds to a combination of
          the original i- and j-direction, while the new j-direction corresponds
          to the j-direction of the original numbering. This is a left
          handed transformation. */
-      a = nPolyConn; b = -1; c = -1; d = 0; e = 0; f = 1;
-    }
-    else {
+      a = nPolyConn;
+      b = -1;
+      c = -1;
+      d = 0;
+      e = 0;
+      f = 1;
+    } else {
       verticesDontMatch = true;  // Vert1 does not match with a neigbor.
     }
-  }
-  else if(vert0 == triaNodeIDsGrid[ind2]) {
+  } else if (vert0 == triaNodeIDsGrid[ind2]) {
     /* Vert0 coincides with vertex 2 of the triangle connectivity.
        Determine the situation for vert1. */
-    if(vert1 == triaNodeIDsGrid[ind0]){
+    if (vert1 == triaNodeIDsGrid[ind0]) {
       /* The i-direction of the new numbering corresponds to a combination of
          the original i- and j-direction, while the new j-direction corresponds
          to the i-direction of the original numbering. */
-      a = nPolyConn; b = -1; c = -1; d = 0; e = 1; f = 0;
-    }
-    else if(vert1 == triaNodeIDsGrid[ind1]) {
+      a = nPolyConn;
+      b = -1;
+      c = -1;
+      d = 0;
+      e = 1;
+      f = 0;
+    } else if (vert1 == triaNodeIDsGrid[ind1]) {
       /* The i-direction of the new numbering corresponds to the i-direction of
          the original numbering, while the new j-direction corresponds to a
          combination of the original i- and j-direction. This is a left handed
          transformation. */
-      a = 0; b = 1; c = 0; d = nPolyConn; e = -1; f = -1;
-    }
-    else {
+      a = 0;
+      b = 1;
+      c = 0;
+      d = nPolyConn;
+      e = -1;
+      f = -1;
+    } else {
       verticesDontMatch = true;  // Vert1 does not match with a neigbor.
     }
   }
 
   /*--- If non-matching vertices have been found, terminate with an error message. ---*/
-  if( verticesDontMatch )
-    SU2_MPI::Error("Corner vertices do not match. This should not happen.", CURRENT_FUNCTION);
+  if (verticesDontMatch) SU2_MPI::Error("Corner vertices do not match. This should not happen.", CURRENT_FUNCTION);
 
   /*--- Loop over the DOFs of the original triangle to create the connectivity
         of the triangle that corresponds to the new numbering. ---*/
   unsigned short ind = 0;
-  for(unsigned short j=0; j<=nPolyConn; ++j) {
-    for(unsigned short i=0; i<=(nPolyConn-j); ++i, ++ind) {
-
+  for (unsigned short j = 0; j <= nPolyConn; ++j) {
+    for (unsigned short i = 0; i <= (nPolyConn - j); ++i, ++ind) {
       /*--- Determine the ii and jj indices of the new numbering, convert it to
             a 1D index and shore the modified index in modConnTria. ---*/
-      unsigned short ii = a + i*b + j*c;
-      unsigned short jj = d + i*e + j*f;
+      unsigned short ii = a + i * b + j * c;
+      unsigned short jj = d + i * e + j * f;
 
-      unsigned short iind = jj*(nPolyConn+1) + ii - jj*(jj-1)/2;
+      unsigned short iind = jj * (nPolyConn + 1) + ii - jj * (jj - 1) / 2;
 
       modConnTria[iind] = connTria[ind];
     }
@@ -3958,25 +3641,19 @@ void CMeshFEM_DG::CreateConnectivitiesLineAdjacentTriangle(
   /*--- The line corresponds to face 0 of the triangle. Hence the first
         nPolyConn+1 entries in modConnTria are the DOFs of the line. Copy
         these entries from modConnTria. ---*/
-  for(unsigned short i=0; i<=nPolyConn; ++i)
-    modConnLine[i] = modConnTria[i];
+  for (unsigned short i = 0; i <= nPolyConn; ++i) modConnLine[i] = modConnTria[i];
 }
 
 void CMeshFEM_DG::CreateConnectivitiesQuadrilateralAdjacentHexahedron(
-                                const unsigned long         *cornerPointsQuad,
-                                const unsigned short        nPolyGrid,
-                                const vector<unsigned long> &hexaNodeIDsGrid,
-                                const unsigned short        nPolyConn,
-                                const unsigned long         *connHexa,
-                                unsigned long               *modConnQuad,
-                                unsigned long               *modConnHexa) {
-
+    const unsigned long* cornerPointsQuad, const unsigned short nPolyGrid, const vector<unsigned long>& hexaNodeIDsGrid,
+    const unsigned short nPolyConn, const unsigned long* connHexa, unsigned long* modConnQuad,
+    unsigned long* modConnHexa) {
   /* Determine the indices of the eight corner points of the hexahedron. */
   const unsigned short ind0 = 0;
   const unsigned short ind1 = nPolyGrid;
-  const unsigned short ind2 = (nPolyGrid+1)*(nPolyGrid+1) -1;
+  const unsigned short ind2 = (nPolyGrid + 1) * (nPolyGrid + 1) - 1;
   const unsigned short ind3 = ind2 - nPolyGrid;
-  const unsigned short ind4 = (nPolyGrid+1)*(nPolyGrid+1)*nPolyGrid;
+  const unsigned short ind4 = (nPolyGrid + 1) * (nPolyGrid + 1) * nPolyGrid;
   const unsigned short ind5 = ind1 + ind4;
   const unsigned short ind6 = ind2 + ind4;
   const unsigned short ind7 = ind3 + ind4;
@@ -3997,208 +3674,245 @@ void CMeshFEM_DG::CreateConnectivitiesQuadrilateralAdjacentHexahedron(
         of the hexahedron. This is determined below. The bool verticesDontMatch is
         there to check if vertices do not match. This should not happen, but
         it is checked for security. ---*/
-  signed short a = 0, b = 0, c = 0, d = 0, e = 0, f = 0, g = 0, h = 0,
-               l = 0, m = 0, n = 0, o = 0;
+  signed short a = 0, b = 0, c = 0, d = 0, e = 0, f = 0, g = 0, h = 0, l = 0, m = 0, n = 0, o = 0;
   bool verticesDontMatch = false;
 
-  if(vert0 == hexaNodeIDsGrid[ind0] && vert1 == hexaNodeIDsGrid[ind1] &&   // ii = i.
-     vert2 == hexaNodeIDsGrid[ind2] && vert3 == hexaNodeIDsGrid[ind3]) {   // jj = j.
-    b = g = o = 1;                                                         // kk = k.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind0] && vert1 == hexaNodeIDsGrid[ind3] &&   // ii = j.
-          vert2 == hexaNodeIDsGrid[ind2] && vert3 == hexaNodeIDsGrid[ind1]) {   // jj = i.
-    c = f = o = 1;                                                              // kk = k.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind0] && vert1 == hexaNodeIDsGrid[ind1] && // ii = i.
-          vert2 == hexaNodeIDsGrid[ind5] && vert3 == hexaNodeIDsGrid[ind4]) { // jj = k.
-    b = h = n = 1;                                                            // kk = j.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind0] && vert1 == hexaNodeIDsGrid[ind4] && // ii = k.
-          vert2 == hexaNodeIDsGrid[ind5] && vert3 == hexaNodeIDsGrid[ind1]) { // jj = i.
-    d = f = n = 1;                                                            // kk = j.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind0] && vert1 == hexaNodeIDsGrid[ind3] && // ii = j.
-          vert2 == hexaNodeIDsGrid[ind7] && vert3 == hexaNodeIDsGrid[ind4]) { // jj = k.
-    c = h = m = 1;                                                            // kk = i.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind0] && vert1 == hexaNodeIDsGrid[ind4] && // ii = k.
-          vert2 == hexaNodeIDsGrid[ind7] && vert3 == hexaNodeIDsGrid[ind3]) { // jj = j.
-    d = g = m = 1;                                                            // kk = i.
-  }
-
-  else if(vert0 == hexaNodeIDsGrid[ind1] && vert1 == hexaNodeIDsGrid[ind0] && // ii = nPoly-i.
-          vert2 == hexaNodeIDsGrid[ind3] && vert3 == hexaNodeIDsGrid[ind2]) { // jj = j.
-    a = nPolyConn; b = -1; g = o = 1;                                         // kk = k.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind1] && vert1 == hexaNodeIDsGrid[ind2] && // ii = j.
-          vert2 == hexaNodeIDsGrid[ind3] && vert3 == hexaNodeIDsGrid[ind0]) { // jj = nPoly-i.
-    e = nPolyConn; f = -1; c = o = 1;                                         // kk = k.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind1] && vert1 == hexaNodeIDsGrid[ind0] && // ii = nPoly-i.
-          vert2 == hexaNodeIDsGrid[ind4] && vert3 == hexaNodeIDsGrid[ind5]) { // jj = k.
-    a = nPolyConn; b = -1; h = n = 1;                                         // kk = j.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind1] && vert1 == hexaNodeIDsGrid[ind5] && // ii = k.
-          vert2 == hexaNodeIDsGrid[ind4] && vert3 == hexaNodeIDsGrid[ind0]) { // jj = nPoly-i.
-    e = nPolyConn; f = -1; d = n = 1;                                         // kk = j.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind1] && vert1 == hexaNodeIDsGrid[ind2] && // ii = j.
-          vert2 == hexaNodeIDsGrid[ind6] && vert3 == hexaNodeIDsGrid[ind5]) { // jj = k.
-    l = nPolyConn; m = -1; c = h = 1;                                         // kk = nPoly-i.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind1] && vert1 == hexaNodeIDsGrid[ind5] && // ii = k.
-          vert2 == hexaNodeIDsGrid[ind6] && vert3 == hexaNodeIDsGrid[ind2]) { // jj = j.
-    l = nPolyConn; m = -1; d = g = 1;                                         // kk = nPoly-i.
-  }
-
-  else if(vert0 == hexaNodeIDsGrid[ind2] && vert1 == hexaNodeIDsGrid[ind1] && // ii = nPoly-j.
-          vert2 == hexaNodeIDsGrid[ind0] && vert3 == hexaNodeIDsGrid[ind3]) { // jj = nPoly-i.
-    a = e = nPolyConn; c = f = -1; o = 1;                                     // kk = k.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind2] && vert1 == hexaNodeIDsGrid[ind3] && // ii = nPoly-i.
-          vert2 == hexaNodeIDsGrid[ind0] && vert3 == hexaNodeIDsGrid[ind1]) { // jj = nPoly-j.
-    a = e = nPolyConn; b = g = -1; o = 1;                                     // kk = k.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind2] && vert1 == hexaNodeIDsGrid[ind1] && // ii = nPoly-j.
-          vert2 == hexaNodeIDsGrid[ind5] && vert3 == hexaNodeIDsGrid[ind6]) { // jj = k.
-    a = l = nPolyConn; c = m = -1; h = 1;                                     // kk = nPoly-i.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind2] && vert1 == hexaNodeIDsGrid[ind6] && // ii = k.
-          vert2 == hexaNodeIDsGrid[ind5] && vert3 == hexaNodeIDsGrid[ind1]) { // jj = nPoly-j.
-    e = l = nPolyConn; g = m = -1; d = 1;                                     // kk = nPoly-i.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind2] && vert1 == hexaNodeIDsGrid[ind3] && // ii = nPoly-i.
-          vert2 == hexaNodeIDsGrid[ind7] && vert3 == hexaNodeIDsGrid[ind6]) { // jj = k.
-    a = l = nPolyConn; b = n = -1; h = 1;                                     // kk = nPoly-j.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind2] && vert1 == hexaNodeIDsGrid[ind6] && // ii = k.
-          vert2 == hexaNodeIDsGrid[ind7] && vert3 == hexaNodeIDsGrid[ind3]) { // jj = nPoly-i.
-    e = l = nPolyConn; f = n = -1; d = 1;                                     // kk = nPoly-j.
-  }
-
-  else if(vert0 == hexaNodeIDsGrid[ind3] && vert1 == hexaNodeIDsGrid[ind0] && // ii = nPoly-j.
-          vert2 == hexaNodeIDsGrid[ind1] && vert3 == hexaNodeIDsGrid[ind2]) { // jj = i.
-    a = nPolyConn; c = -1; f = o = 1;                                         // kk = k.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind3] && vert1 == hexaNodeIDsGrid[ind2] && // ii = i.
-          vert2 == hexaNodeIDsGrid[ind1] && vert3 == hexaNodeIDsGrid[ind0]) { // jj = nPoly-j.
-    e = nPolyConn; g = -1; b = o = 1;                                         // kk = k.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind3] && vert1 == hexaNodeIDsGrid[ind0] && // ii = nPoly-j.
-          vert2 == hexaNodeIDsGrid[ind4] && vert3 == hexaNodeIDsGrid[ind7]) { // jj = k.
-    a = nPolyConn; c = -1; h = m = 1;                                         // kk = i.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind3] && vert1 == hexaNodeIDsGrid[ind7] && // ii = k.
-          vert2 == hexaNodeIDsGrid[ind4] && vert3 == hexaNodeIDsGrid[ind0]) { // jj = nPoly-j.
-    e = nPolyConn; g = -1; d = m = 1;                                         // kk = i.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind3] && vert1 == hexaNodeIDsGrid[ind2] && // ii = i.
-          vert2 == hexaNodeIDsGrid[ind6] && vert3 == hexaNodeIDsGrid[ind7]) { // jj = k.
-    l = nPolyConn; n = -1; b = h = 1;                                         // kk = nPoly-j.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind3] && vert1 == hexaNodeIDsGrid[ind7] && // ii = k.
-          vert2 == hexaNodeIDsGrid[ind6] && vert3 == hexaNodeIDsGrid[ind2]) { // jj = i.
-    l = nPolyConn; n = -1; d = f = 1;                                         // kk = nPoly-j.
-  }
-
-  else if(vert0 == hexaNodeIDsGrid[ind4] && vert1 == hexaNodeIDsGrid[ind5] && // ii = i.
-          vert2 == hexaNodeIDsGrid[ind6] && vert3 == hexaNodeIDsGrid[ind7]) { // jj = j.
-    l = nPolyConn; o = -1; b = g = 1;                                         // kk = nPoly-k.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind4] && vert1 == hexaNodeIDsGrid[ind7] && // ii = j.
-          vert2 == hexaNodeIDsGrid[ind6] && vert3 == hexaNodeIDsGrid[ind5]) { // jj = i.
-    l = nPolyConn; o = -1; c = f = 1;                                         // kk = nPoly-k.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind4] && vert1 == hexaNodeIDsGrid[ind5] && // ii = i.
-          vert2 == hexaNodeIDsGrid[ind1] && vert3 == hexaNodeIDsGrid[ind0]) { // jj = nPoly-k.
-    e = nPolyConn; h = -1; b = n = 1;                                         // kk = j.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind4] && vert1 == hexaNodeIDsGrid[ind0] && // ii = nPoly-k.
-          vert2 == hexaNodeIDsGrid[ind1] && vert3 == hexaNodeIDsGrid[ind5]) { // jj = i.
-    a = nPolyConn; d = -1; f = n = 1;                                         // kk = j.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind4] && vert1 == hexaNodeIDsGrid[ind7] && // ii = j.
-          vert2 == hexaNodeIDsGrid[ind3] && vert3 == hexaNodeIDsGrid[ind0]) { // jj = nPoly-k.
-    e = nPolyConn; h = -1; c = m = 1;                                         // kk = i.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind4] && vert1 == hexaNodeIDsGrid[ind0] && // ii = nPoly-k.
-          vert2 == hexaNodeIDsGrid[ind3] && vert3 == hexaNodeIDsGrid[ind7]) { // jj = j.
-    a = nPolyConn; d = -1; g = m = 1;                                         // kk = i.
-  }
-
-  else if(vert0 == hexaNodeIDsGrid[ind5] && vert1 == hexaNodeIDsGrid[ind6] && // ii = j.
-          vert2 == hexaNodeIDsGrid[ind7] && vert3 == hexaNodeIDsGrid[ind4]) { // jj = nPoly-i.
-    e = l = nPolyConn; f = o = -1; c = 1;                                     // kk = nPoly-k.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind5] && vert1 == hexaNodeIDsGrid[ind4] && // ii = nPoly-i.
-          vert2 == hexaNodeIDsGrid[ind7] && vert3 == hexaNodeIDsGrid[ind6]) { // jj = j.
-    a = l = nPolyConn; b = o = -1; g = 1;                                     // kk = nPoly-k.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind5] && vert1 == hexaNodeIDsGrid[ind6] && // ii = j.
-          vert2 == hexaNodeIDsGrid[ind2] && vert3 == hexaNodeIDsGrid[ind1]) { // jj = nPoly-k.
-    e = l = nPolyConn; h = m = -1; c = 1;                                     // kk = nPoly-i.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind5] && vert1 == hexaNodeIDsGrid[ind1] && // ii = nPoly-k.
-          vert2 == hexaNodeIDsGrid[ind2] && vert3 == hexaNodeIDsGrid[ind6]) { // jj = j.
-    a = l = nPolyConn; d = m = -1; g = 1;                                     // kk = nPoly-i.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind5] && vert1 == hexaNodeIDsGrid[ind1] && // ii = nPoly-k.
-          vert2 == hexaNodeIDsGrid[ind0] && vert3 == hexaNodeIDsGrid[ind4]) { // jj = nPoly-i.
-    a = e = nPolyConn; d = f = -1; n = 1;                                     // kk = j.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind5] && vert1 == hexaNodeIDsGrid[ind4] && // ii = nPoly-i.
-          vert2 == hexaNodeIDsGrid[ind0] && vert3 == hexaNodeIDsGrid[ind1]) { // jj = nPoly-k.
-    a = e = nPolyConn; b = h = -1; n = 1;                                     // kk = j.
-  }
-
-  else if(vert0 == hexaNodeIDsGrid[ind6] && vert1 == hexaNodeIDsGrid[ind7] && // ii = nPoly-i.
-          vert2 == hexaNodeIDsGrid[ind4] && vert3 == hexaNodeIDsGrid[ind5]) { // jj = nPoly-j.
-    a = e = l = nPolyConn; b = g = o = -1;                                    // kk = nPoly-k.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind6] && vert1 == hexaNodeIDsGrid[ind5] && // ii = nPoly-j.
-          vert2 == hexaNodeIDsGrid[ind4] && vert3 == hexaNodeIDsGrid[ind7]) { // jj = nPoly-i.
-    a = e = l = nPolyConn; c = f = o = -1;                                    // kk = nPoly-k.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind6] && vert1 == hexaNodeIDsGrid[ind7] && // ii = nPoly-i.
-          vert2 == hexaNodeIDsGrid[ind3] && vert3 == hexaNodeIDsGrid[ind2]) { // jj = nPoly-k.
-    a = e = l = nPolyConn; b = h = n = -1;                                    // kk = nPoly-j.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind6] && vert1 == hexaNodeIDsGrid[ind2] && // ii = nPoly-k.
-          vert2 == hexaNodeIDsGrid[ind3] && vert3 == hexaNodeIDsGrid[ind7]) { // jj = nPoly-i.
-    a = e = l = nPolyConn; d = f = n = -1;                                    // kk = nPoly-j.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind6] && vert1 == hexaNodeIDsGrid[ind2] && // ii = nPoly-k.
-          vert2 == hexaNodeIDsGrid[ind1] && vert3 == hexaNodeIDsGrid[ind5]) { // jj = nPoly-j.
-    a = e = l = nPolyConn; d = g = m = -1;                                    // kk = nPoly-i.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind6] && vert1 == hexaNodeIDsGrid[ind5] && // ii = nPoly-j.
-          vert2 == hexaNodeIDsGrid[ind1] && vert3 == hexaNodeIDsGrid[ind2]) { // jj = nPoly-k.
-    a = e = l = nPolyConn; c = h = m = -1;                                    // kk = nPoly-i.
-  }
-
-  else if(vert0 == hexaNodeIDsGrid[ind7] && vert1 == hexaNodeIDsGrid[ind4] && // ii = nPoly-j.
-          vert2 == hexaNodeIDsGrid[ind5] && vert3 == hexaNodeIDsGrid[ind6]) { // jj = i.
-    a = l = nPolyConn; c = o = -1; f = 1;                                     // kk = nPoly-k.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind7] && vert1 == hexaNodeIDsGrid[ind6] && // ii = i.
-          vert2 == hexaNodeIDsGrid[ind5] && vert3 == hexaNodeIDsGrid[ind4]) { // jj = nPoly-j.
-    e = l = nPolyConn; g = o = -1; b = 1;                                     // kk = nPoly-k.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind7] && vert1 == hexaNodeIDsGrid[ind4] && // ii = nPoly-j.
-          vert2 == hexaNodeIDsGrid[ind0] && vert3 == hexaNodeIDsGrid[ind3]) { // jj = nPoly-k.
-    a = e = nPolyConn; c = h = -1; m = 1;                                     // kk = i.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind7] && vert1 == hexaNodeIDsGrid[ind3] && // ii = nPoly-k.
-          vert2 == hexaNodeIDsGrid[ind0] && vert3 == hexaNodeIDsGrid[ind4]) { // jj = nPoly-j.
-    a = e = nPolyConn; d = g = -1; m = 1;                                     // kk = i.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind7] && vert1 == hexaNodeIDsGrid[ind6] && // ii = i.
-          vert2 == hexaNodeIDsGrid[ind2] && vert3 == hexaNodeIDsGrid[ind3]) { // jj = nPoly-k.
-    e = l = nPolyConn; h = n = -1; b = 1;                                     // kk = nPoly-j.
-  }
-  else if(vert0 == hexaNodeIDsGrid[ind7] && vert1 == hexaNodeIDsGrid[ind3] && // ii = nPoly-k.
-          vert2 == hexaNodeIDsGrid[ind2] && vert3 == hexaNodeIDsGrid[ind6]) { // jj = i.
-    a = l = nPolyConn; d = n = -1; f = 1;                                     // kk = nPoly-j.
+  if (vert0 == hexaNodeIDsGrid[ind0] && vert1 == hexaNodeIDsGrid[ind1] &&         // ii = i.
+      vert2 == hexaNodeIDsGrid[ind2] && vert3 == hexaNodeIDsGrid[ind3]) {         // jj = j.
+    b = g = o = 1;                                                                // kk = k.
+  } else if (vert0 == hexaNodeIDsGrid[ind0] && vert1 == hexaNodeIDsGrid[ind3] &&  // ii = j.
+             vert2 == hexaNodeIDsGrid[ind2] && vert3 == hexaNodeIDsGrid[ind1]) {  // jj = i.
+    c = f = o = 1;                                                                // kk = k.
+  } else if (vert0 == hexaNodeIDsGrid[ind0] && vert1 == hexaNodeIDsGrid[ind1] &&  // ii = i.
+             vert2 == hexaNodeIDsGrid[ind5] && vert3 == hexaNodeIDsGrid[ind4]) {  // jj = k.
+    b = h = n = 1;                                                                // kk = j.
+  } else if (vert0 == hexaNodeIDsGrid[ind0] && vert1 == hexaNodeIDsGrid[ind4] &&  // ii = k.
+             vert2 == hexaNodeIDsGrid[ind5] && vert3 == hexaNodeIDsGrid[ind1]) {  // jj = i.
+    d = f = n = 1;                                                                // kk = j.
+  } else if (vert0 == hexaNodeIDsGrid[ind0] && vert1 == hexaNodeIDsGrid[ind3] &&  // ii = j.
+             vert2 == hexaNodeIDsGrid[ind7] && vert3 == hexaNodeIDsGrid[ind4]) {  // jj = k.
+    c = h = m = 1;                                                                // kk = i.
+  } else if (vert0 == hexaNodeIDsGrid[ind0] && vert1 == hexaNodeIDsGrid[ind4] &&  // ii = k.
+             vert2 == hexaNodeIDsGrid[ind7] && vert3 == hexaNodeIDsGrid[ind3]) {  // jj = j.
+    d = g = m = 1;                                                                // kk = i.
+  }
+
+  else if (vert0 == hexaNodeIDsGrid[ind1] && vert1 == hexaNodeIDsGrid[ind0] &&  // ii = nPoly-i.
+           vert2 == hexaNodeIDsGrid[ind3] && vert3 == hexaNodeIDsGrid[ind2]) {  // jj = j.
+    a = nPolyConn;
+    b = -1;
+    g = o = 1;                                                                    // kk = k.
+  } else if (vert0 == hexaNodeIDsGrid[ind1] && vert1 == hexaNodeIDsGrid[ind2] &&  // ii = j.
+             vert2 == hexaNodeIDsGrid[ind3] && vert3 == hexaNodeIDsGrid[ind0]) {  // jj = nPoly-i.
+    e = nPolyConn;
+    f = -1;
+    c = o = 1;                                                                    // kk = k.
+  } else if (vert0 == hexaNodeIDsGrid[ind1] && vert1 == hexaNodeIDsGrid[ind0] &&  // ii = nPoly-i.
+             vert2 == hexaNodeIDsGrid[ind4] && vert3 == hexaNodeIDsGrid[ind5]) {  // jj = k.
+    a = nPolyConn;
+    b = -1;
+    h = n = 1;                                                                    // kk = j.
+  } else if (vert0 == hexaNodeIDsGrid[ind1] && vert1 == hexaNodeIDsGrid[ind5] &&  // ii = k.
+             vert2 == hexaNodeIDsGrid[ind4] && vert3 == hexaNodeIDsGrid[ind0]) {  // jj = nPoly-i.
+    e = nPolyConn;
+    f = -1;
+    d = n = 1;                                                                    // kk = j.
+  } else if (vert0 == hexaNodeIDsGrid[ind1] && vert1 == hexaNodeIDsGrid[ind2] &&  // ii = j.
+             vert2 == hexaNodeIDsGrid[ind6] && vert3 == hexaNodeIDsGrid[ind5]) {  // jj = k.
+    l = nPolyConn;
+    m = -1;
+    c = h = 1;                                                                    // kk = nPoly-i.
+  } else if (vert0 == hexaNodeIDsGrid[ind1] && vert1 == hexaNodeIDsGrid[ind5] &&  // ii = k.
+             vert2 == hexaNodeIDsGrid[ind6] && vert3 == hexaNodeIDsGrid[ind2]) {  // jj = j.
+    l = nPolyConn;
+    m = -1;
+    d = g = 1;  // kk = nPoly-i.
+  }
+
+  else if (vert0 == hexaNodeIDsGrid[ind2] && vert1 == hexaNodeIDsGrid[ind1] &&  // ii = nPoly-j.
+           vert2 == hexaNodeIDsGrid[ind0] && vert3 == hexaNodeIDsGrid[ind3]) {  // jj = nPoly-i.
+    a = e = nPolyConn;
+    c = f = -1;
+    o = 1;                                                                        // kk = k.
+  } else if (vert0 == hexaNodeIDsGrid[ind2] && vert1 == hexaNodeIDsGrid[ind3] &&  // ii = nPoly-i.
+             vert2 == hexaNodeIDsGrid[ind0] && vert3 == hexaNodeIDsGrid[ind1]) {  // jj = nPoly-j.
+    a = e = nPolyConn;
+    b = g = -1;
+    o = 1;                                                                        // kk = k.
+  } else if (vert0 == hexaNodeIDsGrid[ind2] && vert1 == hexaNodeIDsGrid[ind1] &&  // ii = nPoly-j.
+             vert2 == hexaNodeIDsGrid[ind5] && vert3 == hexaNodeIDsGrid[ind6]) {  // jj = k.
+    a = l = nPolyConn;
+    c = m = -1;
+    h = 1;                                                                        // kk = nPoly-i.
+  } else if (vert0 == hexaNodeIDsGrid[ind2] && vert1 == hexaNodeIDsGrid[ind6] &&  // ii = k.
+             vert2 == hexaNodeIDsGrid[ind5] && vert3 == hexaNodeIDsGrid[ind1]) {  // jj = nPoly-j.
+    e = l = nPolyConn;
+    g = m = -1;
+    d = 1;                                                                        // kk = nPoly-i.
+  } else if (vert0 == hexaNodeIDsGrid[ind2] && vert1 == hexaNodeIDsGrid[ind3] &&  // ii = nPoly-i.
+             vert2 == hexaNodeIDsGrid[ind7] && vert3 == hexaNodeIDsGrid[ind6]) {  // jj = k.
+    a = l = nPolyConn;
+    b = n = -1;
+    h = 1;                                                                        // kk = nPoly-j.
+  } else if (vert0 == hexaNodeIDsGrid[ind2] && vert1 == hexaNodeIDsGrid[ind6] &&  // ii = k.
+             vert2 == hexaNodeIDsGrid[ind7] && vert3 == hexaNodeIDsGrid[ind3]) {  // jj = nPoly-i.
+    e = l = nPolyConn;
+    f = n = -1;
+    d = 1;  // kk = nPoly-j.
+  }
+
+  else if (vert0 == hexaNodeIDsGrid[ind3] && vert1 == hexaNodeIDsGrid[ind0] &&  // ii = nPoly-j.
+           vert2 == hexaNodeIDsGrid[ind1] && vert3 == hexaNodeIDsGrid[ind2]) {  // jj = i.
+    a = nPolyConn;
+    c = -1;
+    f = o = 1;                                                                    // kk = k.
+  } else if (vert0 == hexaNodeIDsGrid[ind3] && vert1 == hexaNodeIDsGrid[ind2] &&  // ii = i.
+             vert2 == hexaNodeIDsGrid[ind1] && vert3 == hexaNodeIDsGrid[ind0]) {  // jj = nPoly-j.
+    e = nPolyConn;
+    g = -1;
+    b = o = 1;                                                                    // kk = k.
+  } else if (vert0 == hexaNodeIDsGrid[ind3] && vert1 == hexaNodeIDsGrid[ind0] &&  // ii = nPoly-j.
+             vert2 == hexaNodeIDsGrid[ind4] && vert3 == hexaNodeIDsGrid[ind7]) {  // jj = k.
+    a = nPolyConn;
+    c = -1;
+    h = m = 1;                                                                    // kk = i.
+  } else if (vert0 == hexaNodeIDsGrid[ind3] && vert1 == hexaNodeIDsGrid[ind7] &&  // ii = k.
+             vert2 == hexaNodeIDsGrid[ind4] && vert3 == hexaNodeIDsGrid[ind0]) {  // jj = nPoly-j.
+    e = nPolyConn;
+    g = -1;
+    d = m = 1;                                                                    // kk = i.
+  } else if (vert0 == hexaNodeIDsGrid[ind3] && vert1 == hexaNodeIDsGrid[ind2] &&  // ii = i.
+             vert2 == hexaNodeIDsGrid[ind6] && vert3 == hexaNodeIDsGrid[ind7]) {  // jj = k.
+    l = nPolyConn;
+    n = -1;
+    b = h = 1;                                                                    // kk = nPoly-j.
+  } else if (vert0 == hexaNodeIDsGrid[ind3] && vert1 == hexaNodeIDsGrid[ind7] &&  // ii = k.
+             vert2 == hexaNodeIDsGrid[ind6] && vert3 == hexaNodeIDsGrid[ind2]) {  // jj = i.
+    l = nPolyConn;
+    n = -1;
+    d = f = 1;  // kk = nPoly-j.
+  }
+
+  else if (vert0 == hexaNodeIDsGrid[ind4] && vert1 == hexaNodeIDsGrid[ind5] &&  // ii = i.
+           vert2 == hexaNodeIDsGrid[ind6] && vert3 == hexaNodeIDsGrid[ind7]) {  // jj = j.
+    l = nPolyConn;
+    o = -1;
+    b = g = 1;                                                                    // kk = nPoly-k.
+  } else if (vert0 == hexaNodeIDsGrid[ind4] && vert1 == hexaNodeIDsGrid[ind7] &&  // ii = j.
+             vert2 == hexaNodeIDsGrid[ind6] && vert3 == hexaNodeIDsGrid[ind5]) {  // jj = i.
+    l = nPolyConn;
+    o = -1;
+    c = f = 1;                                                                    // kk = nPoly-k.
+  } else if (vert0 == hexaNodeIDsGrid[ind4] && vert1 == hexaNodeIDsGrid[ind5] &&  // ii = i.
+             vert2 == hexaNodeIDsGrid[ind1] && vert3 == hexaNodeIDsGrid[ind0]) {  // jj = nPoly-k.
+    e = nPolyConn;
+    h = -1;
+    b = n = 1;                                                                    // kk = j.
+  } else if (vert0 == hexaNodeIDsGrid[ind4] && vert1 == hexaNodeIDsGrid[ind0] &&  // ii = nPoly-k.
+             vert2 == hexaNodeIDsGrid[ind1] && vert3 == hexaNodeIDsGrid[ind5]) {  // jj = i.
+    a = nPolyConn;
+    d = -1;
+    f = n = 1;                                                                    // kk = j.
+  } else if (vert0 == hexaNodeIDsGrid[ind4] && vert1 == hexaNodeIDsGrid[ind7] &&  // ii = j.
+             vert2 == hexaNodeIDsGrid[ind3] && vert3 == hexaNodeIDsGrid[ind0]) {  // jj = nPoly-k.
+    e = nPolyConn;
+    h = -1;
+    c = m = 1;                                                                    // kk = i.
+  } else if (vert0 == hexaNodeIDsGrid[ind4] && vert1 == hexaNodeIDsGrid[ind0] &&  // ii = nPoly-k.
+             vert2 == hexaNodeIDsGrid[ind3] && vert3 == hexaNodeIDsGrid[ind7]) {  // jj = j.
+    a = nPolyConn;
+    d = -1;
+    g = m = 1;  // kk = i.
+  }
+
+  else if (vert0 == hexaNodeIDsGrid[ind5] && vert1 == hexaNodeIDsGrid[ind6] &&  // ii = j.
+           vert2 == hexaNodeIDsGrid[ind7] && vert3 == hexaNodeIDsGrid[ind4]) {  // jj = nPoly-i.
+    e = l = nPolyConn;
+    f = o = -1;
+    c = 1;                                                                        // kk = nPoly-k.
+  } else if (vert0 == hexaNodeIDsGrid[ind5] && vert1 == hexaNodeIDsGrid[ind4] &&  // ii = nPoly-i.
+             vert2 == hexaNodeIDsGrid[ind7] && vert3 == hexaNodeIDsGrid[ind6]) {  // jj = j.
+    a = l = nPolyConn;
+    b = o = -1;
+    g = 1;                                                                        // kk = nPoly-k.
+  } else if (vert0 == hexaNodeIDsGrid[ind5] && vert1 == hexaNodeIDsGrid[ind6] &&  // ii = j.
+             vert2 == hexaNodeIDsGrid[ind2] && vert3 == hexaNodeIDsGrid[ind1]) {  // jj = nPoly-k.
+    e = l = nPolyConn;
+    h = m = -1;
+    c = 1;                                                                        // kk = nPoly-i.
+  } else if (vert0 == hexaNodeIDsGrid[ind5] && vert1 == hexaNodeIDsGrid[ind1] &&  // ii = nPoly-k.
+             vert2 == hexaNodeIDsGrid[ind2] && vert3 == hexaNodeIDsGrid[ind6]) {  // jj = j.
+    a = l = nPolyConn;
+    d = m = -1;
+    g = 1;                                                                        // kk = nPoly-i.
+  } else if (vert0 == hexaNodeIDsGrid[ind5] && vert1 == hexaNodeIDsGrid[ind1] &&  // ii = nPoly-k.
+             vert2 == hexaNodeIDsGrid[ind0] && vert3 == hexaNodeIDsGrid[ind4]) {  // jj = nPoly-i.
+    a = e = nPolyConn;
+    d = f = -1;
+    n = 1;                                                                        // kk = j.
+  } else if (vert0 == hexaNodeIDsGrid[ind5] && vert1 == hexaNodeIDsGrid[ind4] &&  // ii = nPoly-i.
+             vert2 == hexaNodeIDsGrid[ind0] && vert3 == hexaNodeIDsGrid[ind1]) {  // jj = nPoly-k.
+    a = e = nPolyConn;
+    b = h = -1;
+    n = 1;  // kk = j.
+  }
+
+  else if (vert0 == hexaNodeIDsGrid[ind6] && vert1 == hexaNodeIDsGrid[ind7] &&  // ii = nPoly-i.
+           vert2 == hexaNodeIDsGrid[ind4] && vert3 == hexaNodeIDsGrid[ind5]) {  // jj = nPoly-j.
+    a = e = l = nPolyConn;
+    b = g = o = -1;                                                               // kk = nPoly-k.
+  } else if (vert0 == hexaNodeIDsGrid[ind6] && vert1 == hexaNodeIDsGrid[ind5] &&  // ii = nPoly-j.
+             vert2 == hexaNodeIDsGrid[ind4] && vert3 == hexaNodeIDsGrid[ind7]) {  // jj = nPoly-i.
+    a = e = l = nPolyConn;
+    c = f = o = -1;                                                               // kk = nPoly-k.
+  } else if (vert0 == hexaNodeIDsGrid[ind6] && vert1 == hexaNodeIDsGrid[ind7] &&  // ii = nPoly-i.
+             vert2 == hexaNodeIDsGrid[ind3] && vert3 == hexaNodeIDsGrid[ind2]) {  // jj = nPoly-k.
+    a = e = l = nPolyConn;
+    b = h = n = -1;                                                               // kk = nPoly-j.
+  } else if (vert0 == hexaNodeIDsGrid[ind6] && vert1 == hexaNodeIDsGrid[ind2] &&  // ii = nPoly-k.
+             vert2 == hexaNodeIDsGrid[ind3] && vert3 == hexaNodeIDsGrid[ind7]) {  // jj = nPoly-i.
+    a = e = l = nPolyConn;
+    d = f = n = -1;                                                               // kk = nPoly-j.
+  } else if (vert0 == hexaNodeIDsGrid[ind6] && vert1 == hexaNodeIDsGrid[ind2] &&  // ii = nPoly-k.
+             vert2 == hexaNodeIDsGrid[ind1] && vert3 == hexaNodeIDsGrid[ind5]) {  // jj = nPoly-j.
+    a = e = l = nPolyConn;
+    d = g = m = -1;                                                               // kk = nPoly-i.
+  } else if (vert0 == hexaNodeIDsGrid[ind6] && vert1 == hexaNodeIDsGrid[ind5] &&  // ii = nPoly-j.
+             vert2 == hexaNodeIDsGrid[ind1] && vert3 == hexaNodeIDsGrid[ind2]) {  // jj = nPoly-k.
+    a = e = l = nPolyConn;
+    c = h = m = -1;  // kk = nPoly-i.
+  }
+
+  else if (vert0 == hexaNodeIDsGrid[ind7] && vert1 == hexaNodeIDsGrid[ind4] &&  // ii = nPoly-j.
+           vert2 == hexaNodeIDsGrid[ind5] && vert3 == hexaNodeIDsGrid[ind6]) {  // jj = i.
+    a = l = nPolyConn;
+    c = o = -1;
+    f = 1;                                                                        // kk = nPoly-k.
+  } else if (vert0 == hexaNodeIDsGrid[ind7] && vert1 == hexaNodeIDsGrid[ind6] &&  // ii = i.
+             vert2 == hexaNodeIDsGrid[ind5] && vert3 == hexaNodeIDsGrid[ind4]) {  // jj = nPoly-j.
+    e = l = nPolyConn;
+    g = o = -1;
+    b = 1;                                                                        // kk = nPoly-k.
+  } else if (vert0 == hexaNodeIDsGrid[ind7] && vert1 == hexaNodeIDsGrid[ind4] &&  // ii = nPoly-j.
+             vert2 == hexaNodeIDsGrid[ind0] && vert3 == hexaNodeIDsGrid[ind3]) {  // jj = nPoly-k.
+    a = e = nPolyConn;
+    c = h = -1;
+    m = 1;                                                                        // kk = i.
+  } else if (vert0 == hexaNodeIDsGrid[ind7] && vert1 == hexaNodeIDsGrid[ind3] &&  // ii = nPoly-k.
+             vert2 == hexaNodeIDsGrid[ind0] && vert3 == hexaNodeIDsGrid[ind4]) {  // jj = nPoly-j.
+    a = e = nPolyConn;
+    d = g = -1;
+    m = 1;                                                                        // kk = i.
+  } else if (vert0 == hexaNodeIDsGrid[ind7] && vert1 == hexaNodeIDsGrid[ind6] &&  // ii = i.
+             vert2 == hexaNodeIDsGrid[ind2] && vert3 == hexaNodeIDsGrid[ind3]) {  // jj = nPoly-k.
+    e = l = nPolyConn;
+    h = n = -1;
+    b = 1;                                                                        // kk = nPoly-j.
+  } else if (vert0 == hexaNodeIDsGrid[ind7] && vert1 == hexaNodeIDsGrid[ind3] &&  // ii = nPoly-k.
+             vert2 == hexaNodeIDsGrid[ind2] && vert3 == hexaNodeIDsGrid[ind6]) {  // jj = i.
+    a = l = nPolyConn;
+    d = n = -1;
+    f = 1;  // kk = nPoly-j.
   }
 
   else {
@@ -4206,23 +3920,21 @@ void CMeshFEM_DG::CreateConnectivitiesQuadrilateralAdjacentHexahedron(
   }
 
   /*--- If non-matching vertices have been found, terminate with an error message. ---*/
-  if( verticesDontMatch )
-    SU2_MPI::Error("Corner vertices do not match. This should not happen.", CURRENT_FUNCTION);
+  if (verticesDontMatch) SU2_MPI::Error("Corner vertices do not match. This should not happen.", CURRENT_FUNCTION);
 
   /*--- Loop over the DOFs of the original hexahedron to create the connectivity
         of the hexahedron that corresponds to the new numbering. ---*/
-  const unsigned short nn2 = (nPolyConn+1)*(nPolyConn+1);
+  const unsigned short nn2 = (nPolyConn + 1) * (nPolyConn + 1);
   unsigned short ind = 0;
-  for(unsigned short k=0; k<=nPolyConn; ++k) {
-    for(unsigned short j=0; j<=nPolyConn; ++j) {
-      for(unsigned short i=0; i<=nPolyConn; ++i, ++ind) {
-
+  for (unsigned short k = 0; k <= nPolyConn; ++k) {
+    for (unsigned short j = 0; j <= nPolyConn; ++j) {
+      for (unsigned short i = 0; i <= nPolyConn; ++i, ++ind) {
         /*--- Determine the ii, jj and kk indices of the new numbering, convert it to
               a 1D index and shore the modified index in modConnHexa. ---*/
-        unsigned short ii   = a + i*b + j*c + k*d;
-        unsigned short jj   = e + i*f + j*g + k*h;
-        unsigned short kk   = l + i*m + j*n + k*o;
-        unsigned short iind = kk*nn2 + jj*(nPolyConn+1) + ii;
+        unsigned short ii = a + i * b + j * c + k * d;
+        unsigned short jj = e + i * f + j * g + k * h;
+        unsigned short kk = l + i * m + j * n + k * o;
+        unsigned short iind = kk * nn2 + jj * (nPolyConn + 1) + ii;
 
         modConnHexa[iind] = connHexa[ind];
       }
@@ -4232,25 +3944,18 @@ void CMeshFEM_DG::CreateConnectivitiesQuadrilateralAdjacentHexahedron(
   /*--- The quad corresponds to face 0 of the hexahedron. Hence the first
         nn2 entries in modConnHexa are the DOFs of the quad. Copy
         these entries from modConnHexa. ---*/
-  for(unsigned short i=0; i<nn2; ++i)
-    modConnQuad[i] = modConnHexa[i];
+  for (unsigned short i = 0; i < nn2; ++i) modConnQuad[i] = modConnHexa[i];
 }
 
 void CMeshFEM_DG::CreateConnectivitiesQuadrilateralAdjacentPrism(
-                                const unsigned long         *cornerPointsQuad,
-                                const unsigned short        nPolyGrid,
-                                const vector<unsigned long> &prismNodeIDsGrid,
-                                const unsigned short        nPolyConn,
-                                const unsigned long         *connPrism,
-                                bool                        &swapFaceInElement,
-                                unsigned long               *modConnQuad,
-                                unsigned long               *modConnPrism) {
-
+    const unsigned long* cornerPointsQuad, const unsigned short nPolyGrid,
+    const vector<unsigned long>& prismNodeIDsGrid, const unsigned short nPolyConn, const unsigned long* connPrism,
+    bool& swapFaceInElement, unsigned long* modConnQuad, unsigned long* modConnPrism) {
   /* Determine the indices of the six corner points of the prism. */
   const unsigned short ind0 = 0;
   const unsigned short ind1 = nPolyGrid;
-  const unsigned short ind2 = (nPolyGrid+1)*(nPolyGrid+2)/2 -1;
-  const unsigned short ind3 = (nPolyGrid+1)*(nPolyGrid+2)*nPolyGrid/2;
+  const unsigned short ind2 = (nPolyGrid + 1) * (nPolyGrid + 2) / 2 - 1;
+  const unsigned short ind3 = (nPolyGrid + 1) * (nPolyGrid + 2) * nPolyGrid / 2;
   const unsigned short ind4 = ind1 + ind3;
   const unsigned short ind5 = ind2 + ind3;
 
@@ -4276,106 +3981,152 @@ void CMeshFEM_DG::CreateConnectivitiesQuadrilateralAdjacentPrism(
   signed short a = 0, b = 0, c = 0, d = 0, e = 0, f = 0, g = 0, h = 0;
   bool verticesDontMatch = false;
 
-  if(vert0 == prismNodeIDsGrid[ind0] && vert1 == prismNodeIDsGrid[ind1] &&   // ii = i.
-     vert2 == prismNodeIDsGrid[ind4] && vert3 == prismNodeIDsGrid[ind3]) {   // jj = j.
-    b = f = h = 1; swapFaceInElement = false;                                // kk = k.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind0] && vert1 == prismNodeIDsGrid[ind3] &&   // ii = i.
-          vert2 == prismNodeIDsGrid[ind4] && vert3 == prismNodeIDsGrid[ind1]) {   // jj = j.
-    b = f = h = 1; swapFaceInElement = true;                                      // kk = k. Plus swap.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind0] && vert1 == prismNodeIDsGrid[ind2] &&   // ii = j.
-          vert2 == prismNodeIDsGrid[ind5] && vert3 == prismNodeIDsGrid[ind3]) {   // jj = i.
-    c = e = h = 1; swapFaceInElement = false;                                     // kk = k.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind0] && vert1 == prismNodeIDsGrid[ind3] &&   // ii = j.
-          vert2 == prismNodeIDsGrid[ind5] && vert3 == prismNodeIDsGrid[ind2]) {   // jj = i.
-    c = e = h = 1; swapFaceInElement = true;                                      // kk = k. Plus swap.
-  }
-
-  else if(vert0 == prismNodeIDsGrid[ind1] && vert1 == prismNodeIDsGrid[ind0] &&   // ii = nPoly-i-j.
-          vert2 == prismNodeIDsGrid[ind3] && vert3 == prismNodeIDsGrid[ind4]) {   // jj = j.
-    a = nPolyConn; b = c = -1; f = h = 1; swapFaceInElement = false;              // kk = k.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind1] && vert1 == prismNodeIDsGrid[ind4] &&   // ii = nPoly-i-j.
-          vert2 == prismNodeIDsGrid[ind3] && vert3 == prismNodeIDsGrid[ind0]) {   // jj = j.
-    a = nPolyConn; b = c = -1; f = h = 1; swapFaceInElement = true;               // kk = k. Plus swap.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind1] && vert1 == prismNodeIDsGrid[ind2] &&   // ii = j.
-          vert2 == prismNodeIDsGrid[ind5] && vert3 == prismNodeIDsGrid[ind4]) {   // jj = nPoly-i-j.
-    d = nPolyConn; e = f = -1; c = h = 1; swapFaceInElement = false;              // kk = k.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind1] && vert1 == prismNodeIDsGrid[ind4] &&   // ii = j.
-          vert2 == prismNodeIDsGrid[ind5] && vert3 == prismNodeIDsGrid[ind2]) {   // jj = nPoly-i-j.
-    d = nPolyConn; e = f = -1; c = h = 1; swapFaceInElement = true;               // kk = k. Plus swap.
-  }
-
-  else if(vert0 == prismNodeIDsGrid[ind2] && vert1 == prismNodeIDsGrid[ind0] &&   // ii = nPoly-i-j.
-          vert2 == prismNodeIDsGrid[ind3] && vert3 == prismNodeIDsGrid[ind5]) {   // jj = i.
-    a = nPolyConn; b = c = -1; e = h = 1; swapFaceInElement = false;              // kk = k.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind2] && vert1 == prismNodeIDsGrid[ind5] &&   // ii = nPoly-i-j.
-          vert2 == prismNodeIDsGrid[ind3] && vert3 == prismNodeIDsGrid[ind0]) {   // jj = i.
-    a = nPolyConn; b = c = -1; e = h = 1; swapFaceInElement = true;               // kk = k. Plus swap.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind2] && vert1 == prismNodeIDsGrid[ind1] &&   // ii = i.
-          vert2 == prismNodeIDsGrid[ind4] && vert3 == prismNodeIDsGrid[ind5]) {   // jj = nPoly-i-j.
-    d = nPolyConn; e = f = -1; b = h = 1; swapFaceInElement = false;              // kk = k.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind2] && vert1 == prismNodeIDsGrid[ind5] &&   // ii = i.
-          vert2 == prismNodeIDsGrid[ind4] && vert3 == prismNodeIDsGrid[ind1]) {   // jj = nPoly-i-j.
-    d = nPolyConn; e = f = -1; b = h = 1; swapFaceInElement = true;               // kk = k. Plus swap.
-  }
-
-  else if(vert0 == prismNodeIDsGrid[ind3] && vert1 == prismNodeIDsGrid[ind4] &&   // ii = i.
-          vert2 == prismNodeIDsGrid[ind1] && vert3 == prismNodeIDsGrid[ind0]) {   // jj = j.
-    g = nPolyConn; b = f = 1; h = -1; swapFaceInElement = false;                  // kk = nPoly-k.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind3] && vert1 == prismNodeIDsGrid[ind0] &&   // ii = i.
-          vert2 == prismNodeIDsGrid[ind1] && vert3 == prismNodeIDsGrid[ind4]) {   // jj = j.
-    g = nPolyConn; b = f = 1; h = -1; swapFaceInElement = true;                   // kk = nPoly-k. Plus swap.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind3] && vert1 == prismNodeIDsGrid[ind5] &&   // ii = j.
-          vert2 == prismNodeIDsGrid[ind2] && vert3 == prismNodeIDsGrid[ind0]) {   // jj = i.
-    g = nPolyConn; c = e = 1; h = -1; swapFaceInElement = false;                  // kk = nPoly-k.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind3] && vert1 == prismNodeIDsGrid[ind0] &&   // ii = j.
-          vert2 == prismNodeIDsGrid[ind2] && vert3 == prismNodeIDsGrid[ind5]) {   // jj = i.
-    g = nPolyConn; c = e = 1; h = -1; swapFaceInElement = true;                   // kk = nPoly-k. Plus swap.
-  }
-
-  else if(vert0 == prismNodeIDsGrid[ind4] && vert1 == prismNodeIDsGrid[ind3] &&   // ii = nPoly-i-j.
-          vert2 == prismNodeIDsGrid[ind0] && vert3 == prismNodeIDsGrid[ind1]) {   // jj = j.
-    a = g = nPolyConn; b = c = h = -1; f = 1; swapFaceInElement = false;          // kk = nPoly-k.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind4] && vert1 == prismNodeIDsGrid[ind1] &&   // ii = nPoly-i-j.
-          vert2 == prismNodeIDsGrid[ind0] && vert3 == prismNodeIDsGrid[ind3]) {   // jj = j.
-    a = g = nPolyConn; b = c = h = -1; f = 1; swapFaceInElement = true;           // kk = nPoly-k. Plus swap.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind4] && vert1 == prismNodeIDsGrid[ind5] &&   // ii = j.
-          vert2 == prismNodeIDsGrid[ind2] && vert3 == prismNodeIDsGrid[ind1]) {   // jj = nPoly-i-j.
-    d = g = nPolyConn; e = f = h = -1; c = 1; swapFaceInElement = false;          // kk = nPoly-k.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind4] && vert1 == prismNodeIDsGrid[ind1] &&   // ii = j.
-          vert2 == prismNodeIDsGrid[ind2] && vert3 == prismNodeIDsGrid[ind5]) {   // jj = nPoly-i-j.
-    d = g = nPolyConn; e = f = h = -1; c = 1; swapFaceInElement = true;           // kk = nPoly-k. Plus swap.
-  }
-
-  else if(vert0 == prismNodeIDsGrid[ind5] && vert1 == prismNodeIDsGrid[ind3] &&   // ii = nPoly-i-j.
-          vert2 == prismNodeIDsGrid[ind0] && vert3 == prismNodeIDsGrid[ind2]) {   // jj = i.
-    a = g = nPolyConn; b = c = h = -1; e = 1; swapFaceInElement = false;          // kk = nPoly-k.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind5] && vert1 == prismNodeIDsGrid[ind2] &&   // ii = nPoly-i-j.
-          vert2 == prismNodeIDsGrid[ind0] && vert3 == prismNodeIDsGrid[ind3]) {   // jj = i.
-    a = g = nPolyConn; b = c = h = -1; e = 1; swapFaceInElement = true;           // kk = nPoly-k. Plus swap.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind5] && vert1 == prismNodeIDsGrid[ind4] &&   // ii = i.
-          vert2 == prismNodeIDsGrid[ind1] && vert3 == prismNodeIDsGrid[ind2]) {   // jj = nPoly-i-j.
-    d = g = nPolyConn; e = f = h = -1; b = 1; swapFaceInElement = false;          // kk = nPoly-k.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind5] && vert1 == prismNodeIDsGrid[ind2] &&   // ii = i.
-          vert2 == prismNodeIDsGrid[ind1] && vert3 == prismNodeIDsGrid[ind4]) {   // jj = nPoly-i-j.
-    d = g = nPolyConn; e = f = h = -1; b = 1; swapFaceInElement = true;           // kk = nPoly-k. Plus swap.
+  if (vert0 == prismNodeIDsGrid[ind0] && vert1 == prismNodeIDsGrid[ind1] &&  // ii = i.
+      vert2 == prismNodeIDsGrid[ind4] && vert3 == prismNodeIDsGrid[ind3]) {  // jj = j.
+    b = f = h = 1;
+    swapFaceInElement = false;                                                      // kk = k.
+  } else if (vert0 == prismNodeIDsGrid[ind0] && vert1 == prismNodeIDsGrid[ind3] &&  // ii = i.
+             vert2 == prismNodeIDsGrid[ind4] && vert3 == prismNodeIDsGrid[ind1]) {  // jj = j.
+    b = f = h = 1;
+    swapFaceInElement = true;                                                       // kk = k. Plus swap.
+  } else if (vert0 == prismNodeIDsGrid[ind0] && vert1 == prismNodeIDsGrid[ind2] &&  // ii = j.
+             vert2 == prismNodeIDsGrid[ind5] && vert3 == prismNodeIDsGrid[ind3]) {  // jj = i.
+    c = e = h = 1;
+    swapFaceInElement = false;                                                      // kk = k.
+  } else if (vert0 == prismNodeIDsGrid[ind0] && vert1 == prismNodeIDsGrid[ind3] &&  // ii = j.
+             vert2 == prismNodeIDsGrid[ind5] && vert3 == prismNodeIDsGrid[ind2]) {  // jj = i.
+    c = e = h = 1;
+    swapFaceInElement = true;  // kk = k. Plus swap.
+  }
+
+  else if (vert0 == prismNodeIDsGrid[ind1] && vert1 == prismNodeIDsGrid[ind0] &&  // ii = nPoly-i-j.
+           vert2 == prismNodeIDsGrid[ind3] && vert3 == prismNodeIDsGrid[ind4]) {  // jj = j.
+    a = nPolyConn;
+    b = c = -1;
+    f = h = 1;
+    swapFaceInElement = false;                                                      // kk = k.
+  } else if (vert0 == prismNodeIDsGrid[ind1] && vert1 == prismNodeIDsGrid[ind4] &&  // ii = nPoly-i-j.
+             vert2 == prismNodeIDsGrid[ind3] && vert3 == prismNodeIDsGrid[ind0]) {  // jj = j.
+    a = nPolyConn;
+    b = c = -1;
+    f = h = 1;
+    swapFaceInElement = true;                                                       // kk = k. Plus swap.
+  } else if (vert0 == prismNodeIDsGrid[ind1] && vert1 == prismNodeIDsGrid[ind2] &&  // ii = j.
+             vert2 == prismNodeIDsGrid[ind5] && vert3 == prismNodeIDsGrid[ind4]) {  // jj = nPoly-i-j.
+    d = nPolyConn;
+    e = f = -1;
+    c = h = 1;
+    swapFaceInElement = false;                                                      // kk = k.
+  } else if (vert0 == prismNodeIDsGrid[ind1] && vert1 == prismNodeIDsGrid[ind4] &&  // ii = j.
+             vert2 == prismNodeIDsGrid[ind5] && vert3 == prismNodeIDsGrid[ind2]) {  // jj = nPoly-i-j.
+    d = nPolyConn;
+    e = f = -1;
+    c = h = 1;
+    swapFaceInElement = true;  // kk = k. Plus swap.
+  }
+
+  else if (vert0 == prismNodeIDsGrid[ind2] && vert1 == prismNodeIDsGrid[ind0] &&  // ii = nPoly-i-j.
+           vert2 == prismNodeIDsGrid[ind3] && vert3 == prismNodeIDsGrid[ind5]) {  // jj = i.
+    a = nPolyConn;
+    b = c = -1;
+    e = h = 1;
+    swapFaceInElement = false;                                                      // kk = k.
+  } else if (vert0 == prismNodeIDsGrid[ind2] && vert1 == prismNodeIDsGrid[ind5] &&  // ii = nPoly-i-j.
+             vert2 == prismNodeIDsGrid[ind3] && vert3 == prismNodeIDsGrid[ind0]) {  // jj = i.
+    a = nPolyConn;
+    b = c = -1;
+    e = h = 1;
+    swapFaceInElement = true;                                                       // kk = k. Plus swap.
+  } else if (vert0 == prismNodeIDsGrid[ind2] && vert1 == prismNodeIDsGrid[ind1] &&  // ii = i.
+             vert2 == prismNodeIDsGrid[ind4] && vert3 == prismNodeIDsGrid[ind5]) {  // jj = nPoly-i-j.
+    d = nPolyConn;
+    e = f = -1;
+    b = h = 1;
+    swapFaceInElement = false;                                                      // kk = k.
+  } else if (vert0 == prismNodeIDsGrid[ind2] && vert1 == prismNodeIDsGrid[ind5] &&  // ii = i.
+             vert2 == prismNodeIDsGrid[ind4] && vert3 == prismNodeIDsGrid[ind1]) {  // jj = nPoly-i-j.
+    d = nPolyConn;
+    e = f = -1;
+    b = h = 1;
+    swapFaceInElement = true;  // kk = k. Plus swap.
+  }
+
+  else if (vert0 == prismNodeIDsGrid[ind3] && vert1 == prismNodeIDsGrid[ind4] &&  // ii = i.
+           vert2 == prismNodeIDsGrid[ind1] && vert3 == prismNodeIDsGrid[ind0]) {  // jj = j.
+    g = nPolyConn;
+    b = f = 1;
+    h = -1;
+    swapFaceInElement = false;                                                      // kk = nPoly-k.
+  } else if (vert0 == prismNodeIDsGrid[ind3] && vert1 == prismNodeIDsGrid[ind0] &&  // ii = i.
+             vert2 == prismNodeIDsGrid[ind1] && vert3 == prismNodeIDsGrid[ind4]) {  // jj = j.
+    g = nPolyConn;
+    b = f = 1;
+    h = -1;
+    swapFaceInElement = true;                                                       // kk = nPoly-k. Plus swap.
+  } else if (vert0 == prismNodeIDsGrid[ind3] && vert1 == prismNodeIDsGrid[ind5] &&  // ii = j.
+             vert2 == prismNodeIDsGrid[ind2] && vert3 == prismNodeIDsGrid[ind0]) {  // jj = i.
+    g = nPolyConn;
+    c = e = 1;
+    h = -1;
+    swapFaceInElement = false;                                                      // kk = nPoly-k.
+  } else if (vert0 == prismNodeIDsGrid[ind3] && vert1 == prismNodeIDsGrid[ind0] &&  // ii = j.
+             vert2 == prismNodeIDsGrid[ind2] && vert3 == prismNodeIDsGrid[ind5]) {  // jj = i.
+    g = nPolyConn;
+    c = e = 1;
+    h = -1;
+    swapFaceInElement = true;  // kk = nPoly-k. Plus swap.
+  }
+
+  else if (vert0 == prismNodeIDsGrid[ind4] && vert1 == prismNodeIDsGrid[ind3] &&  // ii = nPoly-i-j.
+           vert2 == prismNodeIDsGrid[ind0] && vert3 == prismNodeIDsGrid[ind1]) {  // jj = j.
+    a = g = nPolyConn;
+    b = c = h = -1;
+    f = 1;
+    swapFaceInElement = false;                                                      // kk = nPoly-k.
+  } else if (vert0 == prismNodeIDsGrid[ind4] && vert1 == prismNodeIDsGrid[ind1] &&  // ii = nPoly-i-j.
+             vert2 == prismNodeIDsGrid[ind0] && vert3 == prismNodeIDsGrid[ind3]) {  // jj = j.
+    a = g = nPolyConn;
+    b = c = h = -1;
+    f = 1;
+    swapFaceInElement = true;                                                       // kk = nPoly-k. Plus swap.
+  } else if (vert0 == prismNodeIDsGrid[ind4] && vert1 == prismNodeIDsGrid[ind5] &&  // ii = j.
+             vert2 == prismNodeIDsGrid[ind2] && vert3 == prismNodeIDsGrid[ind1]) {  // jj = nPoly-i-j.
+    d = g = nPolyConn;
+    e = f = h = -1;
+    c = 1;
+    swapFaceInElement = false;                                                      // kk = nPoly-k.
+  } else if (vert0 == prismNodeIDsGrid[ind4] && vert1 == prismNodeIDsGrid[ind1] &&  // ii = j.
+             vert2 == prismNodeIDsGrid[ind2] && vert3 == prismNodeIDsGrid[ind5]) {  // jj = nPoly-i-j.
+    d = g = nPolyConn;
+    e = f = h = -1;
+    c = 1;
+    swapFaceInElement = true;  // kk = nPoly-k. Plus swap.
+  }
+
+  else if (vert0 == prismNodeIDsGrid[ind5] && vert1 == prismNodeIDsGrid[ind3] &&  // ii = nPoly-i-j.
+           vert2 == prismNodeIDsGrid[ind0] && vert3 == prismNodeIDsGrid[ind2]) {  // jj = i.
+    a = g = nPolyConn;
+    b = c = h = -1;
+    e = 1;
+    swapFaceInElement = false;                                                      // kk = nPoly-k.
+  } else if (vert0 == prismNodeIDsGrid[ind5] && vert1 == prismNodeIDsGrid[ind2] &&  // ii = nPoly-i-j.
+             vert2 == prismNodeIDsGrid[ind0] && vert3 == prismNodeIDsGrid[ind3]) {  // jj = i.
+    a = g = nPolyConn;
+    b = c = h = -1;
+    e = 1;
+    swapFaceInElement = true;                                                       // kk = nPoly-k. Plus swap.
+  } else if (vert0 == prismNodeIDsGrid[ind5] && vert1 == prismNodeIDsGrid[ind4] &&  // ii = i.
+             vert2 == prismNodeIDsGrid[ind1] && vert3 == prismNodeIDsGrid[ind2]) {  // jj = nPoly-i-j.
+    d = g = nPolyConn;
+    e = f = h = -1;
+    b = 1;
+    swapFaceInElement = false;                                                      // kk = nPoly-k.
+  } else if (vert0 == prismNodeIDsGrid[ind5] && vert1 == prismNodeIDsGrid[ind2] &&  // ii = i.
+             vert2 == prismNodeIDsGrid[ind1] && vert3 == prismNodeIDsGrid[ind4]) {  // jj = nPoly-i-j.
+    d = g = nPolyConn;
+    e = f = h = -1;
+    b = 1;
+    swapFaceInElement = true;  // kk = nPoly-k. Plus swap.
   }
 
   else {
@@ -4383,24 +4134,22 @@ void CMeshFEM_DG::CreateConnectivitiesQuadrilateralAdjacentPrism(
   }
 
   /*--- If non-matching vertices have been found, terminate with an error message. ---*/
-  if( verticesDontMatch )
-    SU2_MPI::Error("Corner vertices do not match. This should not happen.", CURRENT_FUNCTION);
+  if (verticesDontMatch) SU2_MPI::Error("Corner vertices do not match. This should not happen.", CURRENT_FUNCTION);
 
   /*--- Loop over the DOFs of the original prism to create the connectivity
         of the prism that corresponds to the new numbering. ---*/
-  const unsigned short kOff = (nPolyConn+1)*(nPolyConn+2)/2;
+  const unsigned short kOff = (nPolyConn + 1) * (nPolyConn + 2) / 2;
   unsigned short ind = 0;
-  for(unsigned short k=0; k<=nPolyConn; ++k) {
-    for(unsigned short j=0; j<=nPolyConn; ++j) {
+  for (unsigned short k = 0; k <= nPolyConn; ++k) {
+    for (unsigned short j = 0; j <= nPolyConn; ++j) {
       unsigned short uppBoundI = nPolyConn - j;
-      for(unsigned short i=0; i<=uppBoundI; ++i, ++ind) {
-
+      for (unsigned short i = 0; i <= uppBoundI; ++i, ++ind) {
         /*--- Determine the ii, jj and kk indices of the new numbering, convert it to
               a 1D index and shore the modified index in modConnPrism. ---*/
-        unsigned short ii   = a + i*b + j*c;
-        unsigned short jj   = d + i*e + j*f;
-        unsigned short kk   = g + h*k;
-        unsigned short iind = kk*kOff + jj*(nPolyConn+1) + ii - jj*(jj-1)/2;
+        unsigned short ii = a + i * b + j * c;
+        unsigned short jj = d + i * e + j * f;
+        unsigned short kk = g + h * k;
+        unsigned short iind = kk * kOff + jj * (nPolyConn + 1) + ii - jj * (jj - 1) / 2;
 
         modConnPrism[iind] = connPrism[ind];
       }
@@ -4408,49 +4157,42 @@ void CMeshFEM_DG::CreateConnectivitiesQuadrilateralAdjacentPrism(
   }
 
   /*--- Determine the connectivity of the quadrilateral face. ---*/
-  if( swapFaceInElement ) {
-
+  if (swapFaceInElement) {
     /*--- The parametric coordinates r and s of the quad must be swapped
           w.r.t. to the parametric coordinates of the face of the prism.
           This means that the coordinate r of the quad runs from the base
           triangle to the top triangle of the prism. This corresponds to
           the k-direction of the prism. Hence the s-direction of the quad
           corresponds to the i-direction of the prism. ---*/
-    for(unsigned short k=0; k<=nPolyConn; ++k) {
-      for(unsigned short i=0; i<=nPolyConn; ++i) {
-        const unsigned short iind = i*(nPolyConn+1) + k;
-        modConnQuad[iind] = modConnPrism[k*kOff+i];
+    for (unsigned short k = 0; k <= nPolyConn; ++k) {
+      for (unsigned short i = 0; i <= nPolyConn; ++i) {
+        const unsigned short iind = i * (nPolyConn + 1) + k;
+        modConnQuad[iind] = modConnPrism[k * kOff + i];
       }
     }
-  }
-  else {
+  } else {
     /*--- The parametric coordinates r and s of the quad correspond to the
           parametric coordinates in i- and k-direction of the face of the
           prism. So an easy copy can be made. ---*/
     unsigned short iind = 0;
-    for(unsigned short k=0; k<=nPolyConn; ++k) {
-      for(unsigned short i=0; i<=nPolyConn; ++i, ++iind) {
-        modConnQuad[iind] = modConnPrism[k*kOff+i];
+    for (unsigned short k = 0; k <= nPolyConn; ++k) {
+      for (unsigned short i = 0; i <= nPolyConn; ++i, ++iind) {
+        modConnQuad[iind] = modConnPrism[k * kOff + i];
       }
     }
   }
 }
 
 void CMeshFEM_DG::CreateConnectivitiesQuadrilateralAdjacentPyramid(
-                                const unsigned long         *cornerPointsQuad,
-                                const unsigned short        nPolyGrid,
-                                const vector<unsigned long> &pyraNodeIDsGrid,
-                                const unsigned short        nPolyConn,
-                                const unsigned long         *connPyra,
-                                unsigned long               *modConnQuad,
-                                unsigned long               *modConnPyra) {
-
+    const unsigned long* cornerPointsQuad, const unsigned short nPolyGrid, const vector<unsigned long>& pyraNodeIDsGrid,
+    const unsigned short nPolyConn, const unsigned long* connPyra, unsigned long* modConnQuad,
+    unsigned long* modConnPyra) {
   /* Determine the indices of the four corner points of the quadrilateral
      base of the pyramid. Note that the top of the pyramid is not needed
      in the comparison, because only triangular faces are attached to it. */
   const unsigned short ind0 = 0;
   const unsigned short ind1 = nPolyGrid;
-  const unsigned short ind2 = (nPolyGrid+1)*(nPolyGrid+1) -1;
+  const unsigned short ind2 = (nPolyGrid + 1) * (nPolyGrid + 1) - 1;
   const unsigned short ind3 = ind2 - nPolyGrid;
 
   /* Easier storage of the four corner points of the quad in the new numbering. */
@@ -4474,40 +4216,46 @@ void CMeshFEM_DG::CreateConnectivitiesQuadrilateralAdjacentPyramid(
   signed short a = 0, b = 0, c = 0, d = 0, e = 0, f = 0;
   bool verticesDontMatch = false;
 
-  if(vert0 == pyraNodeIDsGrid[ind0] && vert1 == pyraNodeIDsGrid[ind1] &&   // ii = i.
-     vert2 == pyraNodeIDsGrid[ind2] && vert3 == pyraNodeIDsGrid[ind3]) {   // jj = j.
+  if (vert0 == pyraNodeIDsGrid[ind0] && vert1 == pyraNodeIDsGrid[ind1] &&  // ii = i.
+      vert2 == pyraNodeIDsGrid[ind2] && vert3 == pyraNodeIDsGrid[ind3]) {  // jj = j.
     b = f = 1;
-  }
-  else if(vert0 == pyraNodeIDsGrid[ind0] && vert1 == pyraNodeIDsGrid[ind3] &&   // ii = j.
-          vert2 == pyraNodeIDsGrid[ind2] && vert3 == pyraNodeIDsGrid[ind1]) {   // jj = i.
+  } else if (vert0 == pyraNodeIDsGrid[ind0] && vert1 == pyraNodeIDsGrid[ind3] &&  // ii = j.
+             vert2 == pyraNodeIDsGrid[ind2] && vert3 == pyraNodeIDsGrid[ind1]) {  // jj = i.
     c = e = 1;
   }
 
-  else if(vert0 == pyraNodeIDsGrid[ind1] && vert1 == pyraNodeIDsGrid[ind2] &&   // ii = j.
-          vert2 == pyraNodeIDsGrid[ind3] && vert3 == pyraNodeIDsGrid[ind0]) {   // jj = nPoly-i.
-    d = nPolyConn; c = 1; e = -1;
-  }
-  else if(vert0 == pyraNodeIDsGrid[ind1] && vert1 == pyraNodeIDsGrid[ind0] &&   // ii = nPoly-i.
-          vert2 == pyraNodeIDsGrid[ind3] && vert3 == pyraNodeIDsGrid[ind2]) {   // jj = j.
-    a = nPolyConn; b = -1; f = 1;
-  }
-
-  else if(vert0 == pyraNodeIDsGrid[ind2] && vert1 == pyraNodeIDsGrid[ind3] &&   // ii = nPoly-i.
-          vert2 == pyraNodeIDsGrid[ind0] && vert3 == pyraNodeIDsGrid[ind1]) {   // jj = nPoly-j.
-    a = d = nPolyConn; b = f = -1;
-  }
-  else if(vert0 == pyraNodeIDsGrid[ind2] && vert1 == pyraNodeIDsGrid[ind1] &&   // ii = nPoly-j.
-          vert2 == pyraNodeIDsGrid[ind0] && vert3 == pyraNodeIDsGrid[ind3]) {   // jj = nPoly-i.
-    a = d = nPolyConn; c = e = -1;
-  }
-
-  else if(vert0 == pyraNodeIDsGrid[ind3] && vert1 == pyraNodeIDsGrid[ind0] &&   // ii = nPoly-j.
-          vert2 == pyraNodeIDsGrid[ind1] && vert3 == pyraNodeIDsGrid[ind2]) {   // jj = i.
-    a = nPolyConn; c = -1; e = 1;
-  }
-  else if(vert0 == pyraNodeIDsGrid[ind3] && vert1 == pyraNodeIDsGrid[ind2] &&   // ii = i.
-          vert2 == pyraNodeIDsGrid[ind1] && vert3 == pyraNodeIDsGrid[ind0]) {   // jj = nPoly-j.
-    d = nPolyConn; b = 1; f = -1;
+  else if (vert0 == pyraNodeIDsGrid[ind1] && vert1 == pyraNodeIDsGrid[ind2] &&  // ii = j.
+           vert2 == pyraNodeIDsGrid[ind3] && vert3 == pyraNodeIDsGrid[ind0]) {  // jj = nPoly-i.
+    d = nPolyConn;
+    c = 1;
+    e = -1;
+  } else if (vert0 == pyraNodeIDsGrid[ind1] && vert1 == pyraNodeIDsGrid[ind0] &&  // ii = nPoly-i.
+             vert2 == pyraNodeIDsGrid[ind3] && vert3 == pyraNodeIDsGrid[ind2]) {  // jj = j.
+    a = nPolyConn;
+    b = -1;
+    f = 1;
+  }
+
+  else if (vert0 == pyraNodeIDsGrid[ind2] && vert1 == pyraNodeIDsGrid[ind3] &&  // ii = nPoly-i.
+           vert2 == pyraNodeIDsGrid[ind0] && vert3 == pyraNodeIDsGrid[ind1]) {  // jj = nPoly-j.
+    a = d = nPolyConn;
+    b = f = -1;
+  } else if (vert0 == pyraNodeIDsGrid[ind2] && vert1 == pyraNodeIDsGrid[ind1] &&  // ii = nPoly-j.
+             vert2 == pyraNodeIDsGrid[ind0] && vert3 == pyraNodeIDsGrid[ind3]) {  // jj = nPoly-i.
+    a = d = nPolyConn;
+    c = e = -1;
+  }
+
+  else if (vert0 == pyraNodeIDsGrid[ind3] && vert1 == pyraNodeIDsGrid[ind0] &&  // ii = nPoly-j.
+           vert2 == pyraNodeIDsGrid[ind1] && vert3 == pyraNodeIDsGrid[ind2]) {  // jj = i.
+    a = nPolyConn;
+    c = -1;
+    e = 1;
+  } else if (vert0 == pyraNodeIDsGrid[ind3] && vert1 == pyraNodeIDsGrid[ind2] &&  // ii = i.
+             vert2 == pyraNodeIDsGrid[ind1] && vert3 == pyraNodeIDsGrid[ind0]) {  // jj = nPoly-j.
+    d = nPolyConn;
+    b = 1;
+    f = -1;
   }
 
   else {
@@ -4515,16 +4263,15 @@ void CMeshFEM_DG::CreateConnectivitiesQuadrilateralAdjacentPyramid(
   }
 
   /*--- If non-matching vertices have been found, terminate with an error message. ---*/
-  if( verticesDontMatch )
-    SU2_MPI::Error("Corner vertices do not match. This should not happen.", CURRENT_FUNCTION);
+  if (verticesDontMatch) SU2_MPI::Error("Corner vertices do not match. This should not happen.", CURRENT_FUNCTION);
 
   /*--- Loop over the DOFs of the original pyramid to create the connectivity
         of the pyramid that corresponds to the new numbering. Note that the
         outer k-loop is the same for both numberings. ---*/
-  unsigned short mPoly    = nPolyConn;
+  unsigned short mPoly = nPolyConn;
   unsigned short offLevel = 0;
 
-  for(unsigned short k=0; k<=nPolyConn; ++k, --mPoly) {
+  for (unsigned short k = 0; k <= nPolyConn; ++k, --mPoly) {
     unsigned short ind = offLevel;
 
     /* The variables of a and d in the transformation are actually flexible. */
@@ -4533,45 +4280,40 @@ void CMeshFEM_DG::CreateConnectivitiesQuadrilateralAdjacentPyramid(
     const signed short dd = d ? mPoly : 0;
 
     /* Loop over the DOFs of the current quadrilateral. */
-    for(unsigned short j=0; j<=mPoly; ++j) {
-      for(unsigned short i=0; i<=mPoly; ++i, ++ind) {
-
+    for (unsigned short j = 0; j <= mPoly; ++j) {
+      for (unsigned short i = 0; i <= mPoly; ++i, ++ind) {
         /*--- Determine the ii and jj indices of the new numbering, convert it
               to a 1D index and shore the modified index in modConnPyra. ---*/
-        unsigned short ii   = aa + i*b + j*c;
-        unsigned short jj   = dd + i*e + j*f;
-        unsigned short iind = offLevel + jj*(mPoly+1) + ii;
+        unsigned short ii = aa + i * b + j * c;
+        unsigned short jj = dd + i * e + j * f;
+        unsigned short iind = offLevel + jj * (mPoly + 1) + ii;
 
         modConnPyra[iind] = connPyra[ind];
       }
     }
 
     /* Update offLevel for the next quadrilateral level of the pyramid. */
-    offLevel += (mPoly+1)*(mPoly+1);
+    offLevel += (mPoly + 1) * (mPoly + 1);
   }
 
   /*--- The quad corresponds to face 0 of the pyramid. Hence the first
         nn2 entries in modConnPyra are the DOFs of the quad. Copy
         these entries from modConnPyra. ---*/
-  const unsigned short nn2 = (nPolyConn+1)*(nPolyConn+1);
-  for(unsigned short i=0; i<nn2; ++i)
-    modConnQuad[i] = modConnPyra[i];
+  const unsigned short nn2 = (nPolyConn + 1) * (nPolyConn + 1);
+  for (unsigned short i = 0; i < nn2; ++i) modConnQuad[i] = modConnPyra[i];
 }
 
-void CMeshFEM_DG::CreateConnectivitiesTriangleAdjacentPrism(
-                                const unsigned long         *cornerPointsTria,
-                                const unsigned short        nPolyGrid,
-                                const vector<unsigned long> &prismNodeIDsGrid,
-                                const unsigned short        nPolyConn,
-                                const unsigned long         *connPrism,
-                                unsigned long               *modConnTria,
-                                unsigned long               *modConnPrism) {
-
+void CMeshFEM_DG::CreateConnectivitiesTriangleAdjacentPrism(const unsigned long* cornerPointsTria,
+                                                            const unsigned short nPolyGrid,
+                                                            const vector<unsigned long>& prismNodeIDsGrid,
+                                                            const unsigned short nPolyConn,
+                                                            const unsigned long* connPrism, unsigned long* modConnTria,
+                                                            unsigned long* modConnPrism) {
   /* Determine the indices of the six corner points of the prism. */
   const unsigned short ind0 = 0;
   const unsigned short ind1 = nPolyGrid;
-  const unsigned short ind2 = (nPolyGrid+1)*(nPolyGrid+2)/2 -1;
-  const unsigned short ind3 = (nPolyGrid+1)*(nPolyGrid+2)*nPolyGrid/2;
+  const unsigned short ind2 = (nPolyGrid + 1) * (nPolyGrid + 2) / 2 - 1;
+  const unsigned short ind3 = (nPolyGrid + 1) * (nPolyGrid + 2) * nPolyGrid / 2;
   const unsigned short ind4 = ind1 + ind3;
   const unsigned short ind5 = ind2 + ind3;
 
@@ -4594,58 +4336,72 @@ void CMeshFEM_DG::CreateConnectivitiesTriangleAdjacentPrism(
   signed short a = 0, b = 0, c = 0, d = 0, e = 0, f = 0, g = 0, h = 0;
   bool verticesDontMatch = false;
 
-  if(vert0 == prismNodeIDsGrid[ind0] && vert1 == prismNodeIDsGrid[ind1] &&   // ii = i.
-     vert2 == prismNodeIDsGrid[ind2]) {                                      // jj = j.
-    b = f = h = 1;                                                           // kk = k.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind0] && vert1 == prismNodeIDsGrid[ind2] &&   // ii = j.
-          vert2 == prismNodeIDsGrid[ind1]) {                                      // jj = i.
-    c = e = h = 1;                                                                // kk = k.
-  }
-
-  else if(vert0 == prismNodeIDsGrid[ind1] && vert1 == prismNodeIDsGrid[ind0] &&   // ii = nPoly-i-j.
-          vert2 == prismNodeIDsGrid[ind2]) {                                      // jj = j.
-    a = nPolyConn; b = c = -1; f = h = 1;                                         // kk = k.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind1] && vert1 == prismNodeIDsGrid[ind2] &&   // ii = j.
-          vert2 == prismNodeIDsGrid[ind0]) {                                      // jj = nPoly-i-j.
-    d = nPolyConn; e = f = -1; c = h = 1;                                         // kk = k.
-  }
-
-  else if(vert0 == prismNodeIDsGrid[ind2] && vert1 == prismNodeIDsGrid[ind0] &&   // ii = nPoly-i-j.
-          vert2 == prismNodeIDsGrid[ind1]) {                                      // jj = i.
-    a = nPolyConn; b = c = -1; e = h = 1;                                         // kk = k.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind2] && vert1 == prismNodeIDsGrid[ind1] &&   // ii = i.
-          vert2 == prismNodeIDsGrid[ind0]) {                                      // jj = nPoly-i-j.
-    d = nPolyConn; e = f = -1; b = h = 1;                                         // kk = k.
-  }
-
-  else if(vert0 == prismNodeIDsGrid[ind3] && vert1 == prismNodeIDsGrid[ind4] &&   // ii = i.
-     vert2 == prismNodeIDsGrid[ind5]) {                                           // jj = j.
-    g = nPolyConn; b = f = 1; h = -1;                                             // kk = nPoly-k.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind3] && vert1 == prismNodeIDsGrid[ind5] &&   // ii = j.
-          vert2 == prismNodeIDsGrid[ind4]) {                                      // jj = i.
-    g = nPolyConn; c = e = 1; h = -1;                                             // kk = nPoly-k.
+  if (vert0 == prismNodeIDsGrid[ind0] && vert1 == prismNodeIDsGrid[ind1] &&         // ii = i.
+      vert2 == prismNodeIDsGrid[ind2]) {                                            // jj = j.
+    b = f = h = 1;                                                                  // kk = k.
+  } else if (vert0 == prismNodeIDsGrid[ind0] && vert1 == prismNodeIDsGrid[ind2] &&  // ii = j.
+             vert2 == prismNodeIDsGrid[ind1]) {                                     // jj = i.
+    c = e = h = 1;                                                                  // kk = k.
+  }
+
+  else if (vert0 == prismNodeIDsGrid[ind1] && vert1 == prismNodeIDsGrid[ind0] &&  // ii = nPoly-i-j.
+           vert2 == prismNodeIDsGrid[ind2]) {                                     // jj = j.
+    a = nPolyConn;
+    b = c = -1;
+    f = h = 1;                                                                      // kk = k.
+  } else if (vert0 == prismNodeIDsGrid[ind1] && vert1 == prismNodeIDsGrid[ind2] &&  // ii = j.
+             vert2 == prismNodeIDsGrid[ind0]) {                                     // jj = nPoly-i-j.
+    d = nPolyConn;
+    e = f = -1;
+    c = h = 1;  // kk = k.
+  }
+
+  else if (vert0 == prismNodeIDsGrid[ind2] && vert1 == prismNodeIDsGrid[ind0] &&  // ii = nPoly-i-j.
+           vert2 == prismNodeIDsGrid[ind1]) {                                     // jj = i.
+    a = nPolyConn;
+    b = c = -1;
+    e = h = 1;                                                                      // kk = k.
+  } else if (vert0 == prismNodeIDsGrid[ind2] && vert1 == prismNodeIDsGrid[ind1] &&  // ii = i.
+             vert2 == prismNodeIDsGrid[ind0]) {                                     // jj = nPoly-i-j.
+    d = nPolyConn;
+    e = f = -1;
+    b = h = 1;  // kk = k.
+  }
+
+  else if (vert0 == prismNodeIDsGrid[ind3] && vert1 == prismNodeIDsGrid[ind4] &&  // ii = i.
+           vert2 == prismNodeIDsGrid[ind5]) {                                     // jj = j.
+    g = nPolyConn;
+    b = f = 1;
+    h = -1;                                                                         // kk = nPoly-k.
+  } else if (vert0 == prismNodeIDsGrid[ind3] && vert1 == prismNodeIDsGrid[ind5] &&  // ii = j.
+             vert2 == prismNodeIDsGrid[ind4]) {                                     // jj = i.
+    g = nPolyConn;
+    c = e = 1;
+    h = -1;  // kk = nPoly-k.
   }
 
-  else if(vert0 == prismNodeIDsGrid[ind4] && vert1 == prismNodeIDsGrid[ind3] &&   // ii = nPoly-i-j.
-          vert2 == prismNodeIDsGrid[ind5]) {                                      // jj = j.
-    a = g = nPolyConn; b = c = h = -1; f = 1;                                     // kk = nPoly-k.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind4] && vert1 == prismNodeIDsGrid[ind5] &&   // ii = j.
-          vert2 == prismNodeIDsGrid[ind3]) {                                      // jj = nPoly-i-j.
-    d = g = nPolyConn; e = f = h = -1; c = 1;                                     // kk = nPoly-k.
+  else if (vert0 == prismNodeIDsGrid[ind4] && vert1 == prismNodeIDsGrid[ind3] &&  // ii = nPoly-i-j.
+           vert2 == prismNodeIDsGrid[ind5]) {                                     // jj = j.
+    a = g = nPolyConn;
+    b = c = h = -1;
+    f = 1;                                                                          // kk = nPoly-k.
+  } else if (vert0 == prismNodeIDsGrid[ind4] && vert1 == prismNodeIDsGrid[ind5] &&  // ii = j.
+             vert2 == prismNodeIDsGrid[ind3]) {                                     // jj = nPoly-i-j.
+    d = g = nPolyConn;
+    e = f = h = -1;
+    c = 1;  // kk = nPoly-k.
   }
 
-  else if(vert0 == prismNodeIDsGrid[ind5] && vert1 == prismNodeIDsGrid[ind3] &&   // ii = nPoly-i-j.
-          vert2 == prismNodeIDsGrid[ind4]) {                                      // jj = i.
-    a = g = nPolyConn; b = c = h = -1; e = 1;                                     // kk = nPoly-k.
-  }
-  else if(vert0 == prismNodeIDsGrid[ind5] && vert1 == prismNodeIDsGrid[ind4] &&   // ii = i.
-          vert2 == prismNodeIDsGrid[ind3]) {                                      // jj = nPoly-i-j.
-    d = g = nPolyConn; e = f = h = -1; b = 1;                                     // kk = nPoly-k.
+  else if (vert0 == prismNodeIDsGrid[ind5] && vert1 == prismNodeIDsGrid[ind3] &&  // ii = nPoly-i-j.
+           vert2 == prismNodeIDsGrid[ind4]) {                                     // jj = i.
+    a = g = nPolyConn;
+    b = c = h = -1;
+    e = 1;                                                                          // kk = nPoly-k.
+  } else if (vert0 == prismNodeIDsGrid[ind5] && vert1 == prismNodeIDsGrid[ind4] &&  // ii = i.
+             vert2 == prismNodeIDsGrid[ind3]) {                                     // jj = nPoly-i-j.
+    d = g = nPolyConn;
+    e = f = h = -1;
+    b = 1;  // kk = nPoly-k.
   }
 
   else {
@@ -4653,24 +4409,22 @@ void CMeshFEM_DG::CreateConnectivitiesTriangleAdjacentPrism(
   }
 
   /*--- If non-matching vertices have been found, terminate with an error message. ---*/
-  if( verticesDontMatch )
-    SU2_MPI::Error("Corner vertices do not match. This should not happen.", CURRENT_FUNCTION);
+  if (verticesDontMatch) SU2_MPI::Error("Corner vertices do not match. This should not happen.", CURRENT_FUNCTION);
 
   /*--- Loop over the DOFs of the original prism to create the connectivity
         of the prism that corresponds to the new numbering. ---*/
-  const unsigned short kOff = (nPolyConn+1)*(nPolyConn+2)/2;
+  const unsigned short kOff = (nPolyConn + 1) * (nPolyConn + 2) / 2;
   unsigned short ind = 0;
-  for(unsigned short k=0; k<=nPolyConn; ++k) {
-    for(unsigned short j=0; j<=nPolyConn; ++j) {
+  for (unsigned short k = 0; k <= nPolyConn; ++k) {
+    for (unsigned short j = 0; j <= nPolyConn; ++j) {
       unsigned short uppBoundI = nPolyConn - j;
-      for(unsigned short i=0; i<=uppBoundI; ++i, ++ind) {
-
+      for (unsigned short i = 0; i <= uppBoundI; ++i, ++ind) {
         /*--- Determine the ii, jj and kk indices of the new numbering, convert it to
               a 1D index and shore the modified index in modConnPrism. ---*/
-        unsigned short ii   = a + i*b + j*c;
-        unsigned short jj   = d + i*e + j*f;
-        unsigned short kk   = g + h*k;
-        unsigned short iind = kk*kOff + jj*(nPolyConn+1) + ii - jj*(jj-1)/2;
+        unsigned short ii = a + i * b + j * c;
+        unsigned short jj = d + i * e + j * f;
+        unsigned short kk = g + h * k;
+        unsigned short iind = kk * kOff + jj * (nPolyConn + 1) + ii - jj * (jj - 1) / 2;
 
         modConnPrism[iind] = connPrism[ind];
       }
@@ -4680,34 +4434,32 @@ void CMeshFEM_DG::CreateConnectivitiesTriangleAdjacentPrism(
   /*--- The triangle corresponds to face 0 of the prism. Hence the first
         kOff entries in modConnPrism are the DOFs of the triangle. Copy
         these entries from modConnPrism. ---*/
-  for(unsigned short i=0; i<kOff; ++i)
-    modConnTria[i] = modConnPrism[i];
+  for (unsigned short i = 0; i < kOff; ++i) modConnTria[i] = modConnPrism[i];
 }
 
-void CMeshFEM_DG::CreateConnectivitiesTriangleAdjacentPyramid(
-                                const unsigned long         *cornerPointsTria,
-                                const unsigned short        nPolyGrid,
-                                const vector<unsigned long> &pyraNodeIDsGrid,
-                                const unsigned short        nPolyConn,
-                                const unsigned long         *connPyra,
-                                bool                        &swapFaceInElement,
-                                unsigned long               *modConnTria,
-                                unsigned long               *modConnPyra) {
-
+void CMeshFEM_DG::CreateConnectivitiesTriangleAdjacentPyramid(const unsigned long* cornerPointsTria,
+                                                              const unsigned short nPolyGrid,
+                                                              const vector<unsigned long>& pyraNodeIDsGrid,
+                                                              const unsigned short nPolyConn,
+                                                              const unsigned long* connPyra, bool& swapFaceInElement,
+                                                              unsigned long* modConnTria, unsigned long* modConnPyra) {
   /* Determine the indices of the five corner points of the pyramid. */
   const unsigned short ind0 = 0;
   const unsigned short ind1 = nPolyGrid;
-  const unsigned short ind2 = (nPolyGrid+1)*(nPolyGrid+1) -1;
+  const unsigned short ind2 = (nPolyGrid + 1) * (nPolyGrid + 1) - 1;
   const unsigned short ind3 = ind2 - nPolyGrid;
-  const unsigned short ind4 = (nPolyGrid+1)*(nPolyGrid+2)*(2*nPolyGrid+3)/6 -1;
+  const unsigned short ind4 = (nPolyGrid + 1) * (nPolyGrid + 2) * (2 * nPolyGrid + 3) / 6 - 1;
 
   /* Check if the top of the pyramid coincides with either corner point 1 or
      corner point 2 of the triangle. Set swapFaceInElement accordingly. */
-  if(     cornerPointsTria[1] == pyraNodeIDsGrid[ind4]) swapFaceInElement = true;
-  else if(cornerPointsTria[2] == pyraNodeIDsGrid[ind4]) swapFaceInElement = false;
+  if (cornerPointsTria[1] == pyraNodeIDsGrid[ind4])
+    swapFaceInElement = true;
+  else if (cornerPointsTria[2] == pyraNodeIDsGrid[ind4])
+    swapFaceInElement = false;
   else
     SU2_MPI::Error(string("Top of the pyramid does not coincide with either corner point 1 or 2.\n") +
-                   string("This should not happen"), CURRENT_FUNCTION);
+                       string("This should not happen"),
+                   CURRENT_FUNCTION);
 
   /* Easier storage of the two other corner points of the triangle in the new numbering.
      vert0 always corresponds to cornerPointsTria[0], while vert1 contains the other
@@ -4728,32 +4480,38 @@ void CMeshFEM_DG::CreateConnectivitiesTriangleAdjacentPyramid(
   signed short a = 0, b = 0, c = 0, d = 0, e = 0, f = 0;
   bool verticesDontMatch = false;
 
-  if(vert0 == pyraNodeIDsGrid[ind0] && vert1 == pyraNodeIDsGrid[ind1]) {   // ii = i.
-    b = f = 1;                                                             // jj = j.
-  }
-  else if(vert0 == pyraNodeIDsGrid[ind0] && vert1 == pyraNodeIDsGrid[ind3]) {   // ii = j.
-    c = e = 1;                                                                  // jj = i.
+  if (vert0 == pyraNodeIDsGrid[ind0] && vert1 == pyraNodeIDsGrid[ind1]) {         // ii = i.
+    b = f = 1;                                                                    // jj = j.
+  } else if (vert0 == pyraNodeIDsGrid[ind0] && vert1 == pyraNodeIDsGrid[ind3]) {  // ii = j.
+    c = e = 1;                                                                    // jj = i.
   }
 
-  else if(vert0 == pyraNodeIDsGrid[ind1] && vert1 == pyraNodeIDsGrid[ind2]) {   // ii = j.
-    d = nPolyConn; c = 1; e = -1;                                               // jj = nPoly-i.
-  }
-  else if(vert0 == pyraNodeIDsGrid[ind1] && vert1 == pyraNodeIDsGrid[ind0]) {   // ii = nPoly-i.
-    a = nPolyConn; b = -1; f = 1;                                               // jj = j.
+  else if (vert0 == pyraNodeIDsGrid[ind1] && vert1 == pyraNodeIDsGrid[ind2]) {  // ii = j.
+    d = nPolyConn;
+    c = 1;
+    e = -1;                                                                       // jj = nPoly-i.
+  } else if (vert0 == pyraNodeIDsGrid[ind1] && vert1 == pyraNodeIDsGrid[ind0]) {  // ii = nPoly-i.
+    a = nPolyConn;
+    b = -1;
+    f = 1;  // jj = j.
   }
 
-  else if(vert0 == pyraNodeIDsGrid[ind2] && vert1 == pyraNodeIDsGrid[ind3]) {   // ii = nPoly-i.
-    a = d = nPolyConn; b = f = -1;                                              // jj = nPoly-j.
-  }
-  else if(vert0 == pyraNodeIDsGrid[ind2] && vert1 == pyraNodeIDsGrid[ind1]) {   // ii = nPoly-j.
-    a = d = nPolyConn; c = e = -1;                                              // jj = nPoly-i.
+  else if (vert0 == pyraNodeIDsGrid[ind2] && vert1 == pyraNodeIDsGrid[ind3]) {  // ii = nPoly-i.
+    a = d = nPolyConn;
+    b = f = -1;                                                                   // jj = nPoly-j.
+  } else if (vert0 == pyraNodeIDsGrid[ind2] && vert1 == pyraNodeIDsGrid[ind1]) {  // ii = nPoly-j.
+    a = d = nPolyConn;
+    c = e = -1;  // jj = nPoly-i.
   }
 
-  else if(vert0 == pyraNodeIDsGrid[ind3] && vert1 == pyraNodeIDsGrid[ind0]) {   // ii = nPoly-j.
-    a = nPolyConn; c = -1; e = 1;                                               // jj = i.
-  }
-  else if(vert0 == pyraNodeIDsGrid[ind3] && vert1 == pyraNodeIDsGrid[ind2]) {   // ii = i.
-    d = nPolyConn; b = 1; f = -1;                                               // jj = nPoly-j.
+  else if (vert0 == pyraNodeIDsGrid[ind3] && vert1 == pyraNodeIDsGrid[ind0]) {  // ii = nPoly-j.
+    a = nPolyConn;
+    c = -1;
+    e = 1;                                                                        // jj = i.
+  } else if (vert0 == pyraNodeIDsGrid[ind3] && vert1 == pyraNodeIDsGrid[ind2]) {  // ii = i.
+    d = nPolyConn;
+    b = 1;
+    f = -1;  // jj = nPoly-j.
   }
 
   else {
@@ -4761,16 +4519,15 @@ void CMeshFEM_DG::CreateConnectivitiesTriangleAdjacentPyramid(
   }
 
   /*--- If non-matching vertices have been found, terminate with an error message. ---*/
-  if( verticesDontMatch )
-    SU2_MPI::Error("Corner vertices do not match. This should not happen.", CURRENT_FUNCTION);
+  if (verticesDontMatch) SU2_MPI::Error("Corner vertices do not match. This should not happen.", CURRENT_FUNCTION);
 
   /*--- Loop over the DOFs of the original pyramid to create the connectivity
         of the pyramid that corresponds to the new numbering. Note that the
         outer k-loop is the same for both numberings. ---*/
-  unsigned short mPoly    = nPolyConn;
+  unsigned short mPoly = nPolyConn;
   unsigned short offLevel = 0;
 
-  for(unsigned short k=0; k<=nPolyConn; ++k, --mPoly) {
+  for (unsigned short k = 0; k <= nPolyConn; ++k, --mPoly) {
     unsigned short ind = offLevel;
 
     /* The variables of a and d in the transformation are actually flexible. */
@@ -4779,72 +4536,64 @@ void CMeshFEM_DG::CreateConnectivitiesTriangleAdjacentPyramid(
     const signed short dd = d ? mPoly : 0;
 
     /* Loop over the DOFs of the current quadrilateral. */
-    for(unsigned short j=0; j<=mPoly; ++j) {
-      for(unsigned short i=0; i<=mPoly; ++i, ++ind) {
-
+    for (unsigned short j = 0; j <= mPoly; ++j) {
+      for (unsigned short i = 0; i <= mPoly; ++i, ++ind) {
         /*--- Determine the ii and jj indices of the new numbering, convert it
               to a 1D index and shore the modified index in modConnPyra. ---*/
-        unsigned short ii   = aa + i*b + j*c;
-        unsigned short jj   = dd + i*e + j*f;
-        unsigned short iind = offLevel + jj*(mPoly+1) + ii;
+        unsigned short ii = aa + i * b + j * c;
+        unsigned short jj = dd + i * e + j * f;
+        unsigned short iind = offLevel + jj * (mPoly + 1) + ii;
 
         modConnPyra[iind] = connPyra[ind];
       }
     }
 
     /* Update offLevel for the next quadrilateral level of the pyramid. */
-    offLevel += (mPoly+1)*(mPoly+1);
+    offLevel += (mPoly + 1) * (mPoly + 1);
   }
 
   /*--- Determine the connectivity of the triangular face. ---*/
-  if( swapFaceInElement ) {
-
+  if (swapFaceInElement) {
     /*--- The parametric coordinates r and s of the triangle must be swapped
           w.r.t. to the parametric coordinates of the face of the pyramid.
           This means that the coordinate r of the triangle runs from the base
           to the top of the pyramid. This corresponds to the k-direction of the
           pyramid. Hence the s-direction of the triangle corresponds to the
           i-direction of the pyramid. ---*/
-    mPoly    = nPolyConn;
+    mPoly = nPolyConn;
     offLevel = 0;
-    for(unsigned short k=0; k<=nPolyConn; ++k, --mPoly) {
-      for(unsigned short i=0; i<=mPoly; ++i) {
-        unsigned short iind = i*(nPolyConn+1) + k - i*(i-1)/2;
-        modConnTria[iind] = modConnPyra[offLevel+i];
+    for (unsigned short k = 0; k <= nPolyConn; ++k, --mPoly) {
+      for (unsigned short i = 0; i <= mPoly; ++i) {
+        unsigned short iind = i * (nPolyConn + 1) + k - i * (i - 1) / 2;
+        modConnTria[iind] = modConnPyra[offLevel + i];
       }
-      offLevel += (mPoly+1)*(mPoly+1);
+      offLevel += (mPoly + 1) * (mPoly + 1);
     }
-  }
-  else {
+  } else {
     /*--- The parametric coordinates r and s of the triangle correspond to the
           parametric coordinates in i- and k-direction of the face of the
           pyramid. So an easy copy can be made. ---*/
-    mPoly    = nPolyConn;
+    mPoly = nPolyConn;
     offLevel = 0;
     unsigned short iind = 0;
-    for(unsigned short k=0; k<=nPolyConn; ++k, --mPoly) {
-      for(unsigned short i=0; i<=mPoly; ++i, ++iind) {
-        modConnTria[iind] = modConnPyra[offLevel+i];
+    for (unsigned short k = 0; k <= nPolyConn; ++k, --mPoly) {
+      for (unsigned short i = 0; i <= mPoly; ++i, ++iind) {
+        modConnTria[iind] = modConnPyra[offLevel + i];
       }
-      offLevel += (mPoly+1)*(mPoly+1);
+      offLevel += (mPoly + 1) * (mPoly + 1);
     }
   }
 }
 
 void CMeshFEM_DG::CreateConnectivitiesTriangleAdjacentTetrahedron(
-                                const unsigned long         *cornerPointsTria,
-                                const unsigned short        nPolyGrid,
-                                const vector<unsigned long> &tetNodeIDsGrid,
-                                const unsigned short        nPolyConn,
-                                const unsigned long         *connTet,
-                                unsigned long               *modConnTria,
-                                unsigned long               *modConnTet) {
-
+    const unsigned long* cornerPointsTria, const unsigned short nPolyGrid, const vector<unsigned long>& tetNodeIDsGrid,
+    const unsigned short nPolyConn, const unsigned long* connTet, unsigned long* modConnTria,
+    unsigned long* modConnTet) {
   /* Determine the indices of the four corner points of the tetrahedron. */
   const unsigned short ind0 = 0;
   const unsigned short ind1 = nPolyGrid;
-  const unsigned short ind2 = (nPolyGrid+1)*(nPolyGrid+2)/2 -1;
-  const unsigned short ind3 = (nPolyGrid+1)*(nPolyGrid+2)*(nPolyGrid+3)/6 -1;
+  const unsigned short ind2 = (nPolyGrid + 1) * (nPolyGrid + 2) / 2 - 1;
+  const unsigned short ind3 = (nPolyGrid + 1) * (nPolyGrid + 2) * (nPolyGrid + 3) / 6 - 1;
 
   /* Easier storage of the three corner points of the triangle in the new numbering. */
   const unsigned long vert0 = cornerPointsTria[0];
@@ -4861,112 +4610,128 @@ void CMeshFEM_DG::CreateConnectivitiesTriangleAdjacentTetrahedron(
         of the tetrahedron. This is determined below. The bool verticesDontMatch is
         there to check if vertices do not match. This should not happen, but
         it is checked for security. ---*/
-  signed short a = 0, b = 0, c = 0, d = 0, e = 0, f = 0, g = 0, h = 0,
-               l = 0, m = 0, n = 0, o = 0;
+  signed short a = 0, b = 0, c = 0, d = 0, e = 0, f = 0, g = 0, h = 0, l = 0, m = 0, n = 0, o = 0;
   bool verticesDontMatch = false;
 
-  if(vert0 == tetNodeIDsGrid[ind0] && vert1 == tetNodeIDsGrid[ind1] &&   // ii = i.
-     vert2 == tetNodeIDsGrid[ind2]) {                                    // jj = j.
-    b = g = o = 1;                                                       // kk = k.
-  }
-  else if(vert0 == tetNodeIDsGrid[ind0] && vert1 == tetNodeIDsGrid[ind2] &&   // ii = j.
-          vert2 == tetNodeIDsGrid[ind1]) {                                    // jj = i.
-    c = f = o = 1;                                                            // kk = k.
-  }
-  else if(vert0 == tetNodeIDsGrid[ind0] && vert1 == tetNodeIDsGrid[ind1] &&   // ii = i.
-          vert2 == tetNodeIDsGrid[ind3]) {                                    // jj = k.
-    b = h = n = 1;                                                            // kk = j.
-  }
-  else if(vert0 == tetNodeIDsGrid[ind0] && vert1 == tetNodeIDsGrid[ind3] &&   // ii = k.
-          vert2 == tetNodeIDsGrid[ind1]) {                                    // jj = i.
-    d = f = n = 1;                                                            // kk = j.
-  }
-  else if(vert0 == tetNodeIDsGrid[ind0] && vert1 == tetNodeIDsGrid[ind2] &&   // ii = j.
-          vert2 == tetNodeIDsGrid[ind3]) {                                    // jj = k.
-    c = h = m = 1;                                                            // kk = i.
-  }
-  else if(vert0 == tetNodeIDsGrid[ind0] && vert1 == tetNodeIDsGrid[ind3] &&   // ii = k.
-          vert2 == tetNodeIDsGrid[ind2]) {                                    // jj = j.
-    d = g = m = 1;                                                            // kk = i.
-  }
-
-  else if(vert0 == tetNodeIDsGrid[ind1] && vert1 == tetNodeIDsGrid[ind0] &&   // ii = nPoly-i-j-k.
-          vert2 == tetNodeIDsGrid[ind2]) {                                    // jj = j.
-    a = nPolyConn; b = c = d = -1; g = o = 1;                                 // kk = k.
-  }
-  else if(vert0 == tetNodeIDsGrid[ind1] && vert1 == tetNodeIDsGrid[ind2] &&   // ii = j.
-          vert2 == tetNodeIDsGrid[ind0]) {                                    // jj = nPoly-i-j-k.
-    e = nPolyConn; f = g = h = -1; c = o = 1;                                 // kk = k.
-  }
-  else if(vert0 == tetNodeIDsGrid[ind1] && vert1 == tetNodeIDsGrid[ind0] &&   // ii = nPoly-i-j-k.
-          vert2 == tetNodeIDsGrid[ind3]) {                                    // jj = k.
-    a = nPolyConn; b = c = d = -1; h = n = 1;                                 // kk = j.
-  }
-  else if(vert0 == tetNodeIDsGrid[ind1] && vert1 == tetNodeIDsGrid[ind3] &&   // ii = k.
-          vert2 == tetNodeIDsGrid[ind0]) {                                    // jj = nPoly-i-j-k.
-    e = nPolyConn; f = g = h = -1; d = n = 1;                                 // kk = j.
-  }
-  else if(vert0 == tetNodeIDsGrid[ind1] && vert1 == tetNodeIDsGrid[ind2] &&   // ii = j.
-          vert2 == tetNodeIDsGrid[ind3]) {                                    // jj = k.
-    l = nPolyConn; m = n = o = -1; c = h = 1;                                 // kk = nPoly-i-j-k.
-  }
-  else if(vert0 == tetNodeIDsGrid[ind1] && vert1 == tetNodeIDsGrid[ind3] &&   // ii = k.
-          vert2 == tetNodeIDsGrid[ind2]) {                                    // jj = j.
-    l = nPolyConn; m = n = o = -1; d = g = 1;                                 // kk = nPoly-i-j-k.
-  }
-
-  else if(vert0 == tetNodeIDsGrid[ind2] && vert1 == tetNodeIDsGrid[ind0] &&   // ii = nPoly-i-j-k.
-          vert2 == tetNodeIDsGrid[ind1]) {                                    // jj = i.
-    a = nPolyConn; b = c = d = -1; f = o = 1;                                 // kk = k.
-  }
-  else if(vert0 == tetNodeIDsGrid[ind2] && vert1 == tetNodeIDsGrid[ind1] &&   // ii = i.
-          vert2 == tetNodeIDsGrid[ind0]) {                                    // jj = nPoly-i-j-k.
-    e = nPolyConn; f = g = h = -1; b = o = 1;                                 // kk = k.
-  }
-  else if(vert0 == tetNodeIDsGrid[ind2] && vert1 == tetNodeIDsGrid[ind0] &&   // ii = nPoly-i-j-k.
-          vert2 == tetNodeIDsGrid[ind3]) {                                    // jj = k.
-    a = nPolyConn; b = c = d = -1; h = m = 1;                                 // kk = i.
-  }
-  else if(vert0 == tetNodeIDsGrid[ind2] && vert1 == tetNodeIDsGrid[ind3] &&   // ii = k.
-          vert2 == tetNodeIDsGrid[ind0]) {                                    // jj = nPoly-i-j-k.
-    e = nPolyConn; f = g = h = -1; d = m = 1;                                 // kk = i.
-  }
-  else if(vert0 == tetNodeIDsGrid[ind2] && vert1 == tetNodeIDsGrid[ind0] &&   // ii = nPoly-i-j-k.
-          vert2 == tetNodeIDsGrid[ind3]) {                                    // jj = k.
-    a = nPolyConn; b = c = d = -1; h = m = 1;                                 // kk = i.
-  }
-  else if(vert0 == tetNodeIDsGrid[ind2] && vert1 == tetNodeIDsGrid[ind1] &&   // ii = i.
-          vert2 == tetNodeIDsGrid[ind3]) {                                    // jj = k.
-    l = nPolyConn; m = n = o = -1; b = h = 1;                                 // kk = nPoly-i-j-k.
-  }
-  else if(vert0 == tetNodeIDsGrid[ind2] && vert1 == tetNodeIDsGrid[ind3] &&   // ii = k.
-          vert2 == tetNodeIDsGrid[ind1]) {                                    // jj = i.
-    l = nPolyConn; m = n = o = -1; d = f = 1;                                 // kk = nPoly-i-j-k.
-  }
-
-  else if(vert0 == tetNodeIDsGrid[ind3] && vert1 == tetNodeIDsGrid[ind0] &&   // ii = nPoly-i-j-k.
-          vert2 == tetNodeIDsGrid[ind1]) {                                    // jj = i.
-    a = nPolyConn; b = c = d = -1; f = n = 1;                                 // kk = j.
-  }
-  else if(vert0 == tetNodeIDsGrid[ind3] && vert1 == tetNodeIDsGrid[ind1] &&   // ii = i.
-          vert2 == tetNodeIDsGrid[ind0]) {                                    // jj = nPoly-i-j-k.
-    e = nPolyConn; f = g = h = -1; b = n = 1;                                 // kk = j.
-  }
-  else if(vert0 == tetNodeIDsGrid[ind3] && vert1 == tetNodeIDsGrid[ind0] &&   // ii = nPoly-i-j-k.
-          vert2 == tetNodeIDsGrid[ind2]) {                                    // jj = j.
-    a = nPolyConn; b = c = d = -1; g = m = 1;                                 // kk = i.
-  }
-  else if(vert0 == tetNodeIDsGrid[ind3] && vert1 == tetNodeIDsGrid[ind2] &&   // ii = j.
-          vert2 == tetNodeIDsGrid[ind0]) {                                    // jj = nPoly-i-j-k.
-    e = nPolyConn; f = g = h = -1; c = m = 1;                                 // kk = i.
-  }
-  else if(vert0 == tetNodeIDsGrid[ind3] && vert1 == tetNodeIDsGrid[ind1] &&   // ii = i.
-          vert2 == tetNodeIDsGrid[ind2]) {                                    // jj = j.
-    l = nPolyConn; m = n = o = -1; b = g = 1;                                 // kk = nPoly-i-j-k.
-  }
-  else if(vert0 == tetNodeIDsGrid[ind3] && vert1 == tetNodeIDsGrid[ind2] &&   // ii = j.
-          vert2 == tetNodeIDsGrid[ind1]) {                                    // jj = i.
-    l = nPolyConn; m = n = o = -1; c = f = 1;                                 // kk = nPoly-i-j-k.
+  if (vert0 == tetNodeIDsGrid[ind0] && vert1 == tetNodeIDsGrid[ind1] &&         // ii = i.
+      vert2 == tetNodeIDsGrid[ind2]) {                                          // jj = j.
+    b = g = o = 1;                                                              // kk = k.
+  } else if (vert0 == tetNodeIDsGrid[ind0] && vert1 == tetNodeIDsGrid[ind2] &&  // ii = j.
+             vert2 == tetNodeIDsGrid[ind1]) {                                   // jj = i.
+    c = f = o = 1;                                                              // kk = k.
+  } else if (vert0 == tetNodeIDsGrid[ind0] && vert1 == tetNodeIDsGrid[ind1] &&  // ii = i.
+             vert2 == tetNodeIDsGrid[ind3]) {                                   // jj = k.
+    b = h = n = 1;                                                              // kk = j.
+  } else if (vert0 == tetNodeIDsGrid[ind0] && vert1 == tetNodeIDsGrid[ind3] &&  // ii = k.
+             vert2 == tetNodeIDsGrid[ind1]) {                                   // jj = i.
+    d = f = n = 1;                                                              // kk = j.
+  } else if (vert0 == tetNodeIDsGrid[ind0] && vert1 == tetNodeIDsGrid[ind2] &&  // ii = j.
+             vert2 == tetNodeIDsGrid[ind3]) {                                   // jj = k.
+    c = h = m = 1;                                                              // kk = i.
+  } else if (vert0 == tetNodeIDsGrid[ind0] && vert1 == tetNodeIDsGrid[ind3] &&  // ii = k.
+             vert2 == tetNodeIDsGrid[ind2]) {                                   // jj = j.
+    d = g = m = 1;                                                              // kk = i.
+  }
+
+  else if (vert0 == tetNodeIDsGrid[ind1] && vert1 == tetNodeIDsGrid[ind0] &&  // ii = nPoly-i-j-k.
+           vert2 == tetNodeIDsGrid[ind2]) {                                   // jj = j.
+    a = nPolyConn;
+    b = c = d = -1;
+    g = o = 1;                                                                  // kk = k.
+  } else if (vert0 == tetNodeIDsGrid[ind1] && vert1 == tetNodeIDsGrid[ind2] &&  // ii = j.
+             vert2 == tetNodeIDsGrid[ind0]) {                                   // jj = nPoly-i-j-k.
+    e = nPolyConn;
+    f = g = h = -1;
+    c = o = 1;                                                                  // kk = k.
+  } else if (vert0 == tetNodeIDsGrid[ind1] && vert1 == tetNodeIDsGrid[ind0] &&  // ii = nPoly-i-j-k.
+             vert2 == tetNodeIDsGrid[ind3]) {                                   // jj = k.
+    a = nPolyConn;
+    b = c = d = -1;
+    h = n = 1;                                                                  // kk = j.
+  } else if (vert0 == tetNodeIDsGrid[ind1] && vert1 == tetNodeIDsGrid[ind3] &&  // ii = k.
+             vert2 == tetNodeIDsGrid[ind0]) {                                   // jj = nPoly-i-j-k.
+    e = nPolyConn;
+    f = g = h = -1;
+    d = n = 1;                                                                  // kk = j.
+  } else if (vert0 == tetNodeIDsGrid[ind1] && vert1 == tetNodeIDsGrid[ind2] &&  // ii = j.
+             vert2 == tetNodeIDsGrid[ind3]) {                                   // jj = k.
+    l = nPolyConn;
+    m = n = o = -1;
+    c = h = 1;                                                                  // kk = nPoly-i-j-k.
+  } else if (vert0 == tetNodeIDsGrid[ind1] && vert1 == tetNodeIDsGrid[ind3] &&  // ii = k.
+             vert2 == tetNodeIDsGrid[ind2]) {                                   // jj = j.
+    l = nPolyConn;
+    m = n = o = -1;
+    d = g = 1;  // kk = nPoly-i-j-k.
+  }
+
+  else if (vert0 == tetNodeIDsGrid[ind2] && vert1 == tetNodeIDsGrid[ind0] &&  // ii = nPoly-i-j-k.
+           vert2 == tetNodeIDsGrid[ind1]) {                                   // jj = i.
+    a = nPolyConn;
+    b = c = d = -1;
+    f = o = 1;                                                                  // kk = k.
+  } else if (vert0 == tetNodeIDsGrid[ind2] && vert1 == tetNodeIDsGrid[ind1] &&  // ii = i.
+             vert2 == tetNodeIDsGrid[ind0]) {                                   // jj = nPoly-i-j-k.
+    e = nPolyConn;
+    f = g = h = -1;
+    b = o = 1;                                                                  // kk = k.
+  } else if (vert0 == tetNodeIDsGrid[ind2] && vert1 == tetNodeIDsGrid[ind0] &&  // ii = nPoly-i-j-k.
+             vert2 == tetNodeIDsGrid[ind3]) {                                   // jj = k.
+    a = nPolyConn;
+    b = c = d = -1;
+    h = m = 1;                                                                  // kk = i.
+  } else if (vert0 == tetNodeIDsGrid[ind2] && vert1 == tetNodeIDsGrid[ind3] &&  // ii = k.
+             vert2 == tetNodeIDsGrid[ind0]) {                                   // jj = nPoly-i-j-k.
+    e = nPolyConn;
+    f = g = h = -1;
+    d = m = 1;                                                                  // kk = i.
+  } else if (vert0 == tetNodeIDsGrid[ind2] && vert1 == tetNodeIDsGrid[ind0] &&  // ii = nPoly-i-j-k.
+             vert2 == tetNodeIDsGrid[ind3]) {                                   // jj = k.
+    a = nPolyConn;
+    b = c = d = -1;
+    h = m = 1;                                                                  // kk = i.
+  } else if (vert0 == tetNodeIDsGrid[ind2] && vert1 == tetNodeIDsGrid[ind1] &&  // ii = i.
+             vert2 == tetNodeIDsGrid[ind3]) {                                   // jj = k.
+    l = nPolyConn;
+    m = n = o = -1;
+    b = h = 1;                                                                  // kk = nPoly-i-j-k.
+  } else if (vert0 == tetNodeIDsGrid[ind2] && vert1 == tetNodeIDsGrid[ind3] &&  // ii = k.
+             vert2 == tetNodeIDsGrid[ind1]) {                                   // jj = i.
+    l = nPolyConn;
+    m = n = o = -1;
+    d = f = 1;  // kk = nPoly-i-j-k.
+  }
+
+  else if (vert0 == tetNodeIDsGrid[ind3] && vert1 == tetNodeIDsGrid[ind0] &&  // ii = nPoly-i-j-k.
+           vert2 == tetNodeIDsGrid[ind1]) {                                   // jj = i.
+    a = nPolyConn;
+    b = c = d = -1;
+    f = n = 1;                                                                  // kk = j.
+  } else if (vert0 == tetNodeIDsGrid[ind3] && vert1 == tetNodeIDsGrid[ind1] &&  // ii = i.
+             vert2 == tetNodeIDsGrid[ind0]) {                                   // jj = nPoly-i-j-k.
+    e = nPolyConn;
+    f = g = h = -1;
+    b = n = 1;                                                                  // kk = j.
+  } else if (vert0 == tetNodeIDsGrid[ind3] && vert1 == tetNodeIDsGrid[ind0] &&  // ii = nPoly-i-j-k.
+             vert2 == tetNodeIDsGrid[ind2]) {                                   // jj = j.
+    a = nPolyConn;
+    b = c = d = -1;
+    g = m = 1;                                                                  // kk = i.
+  } else if (vert0 == tetNodeIDsGrid[ind3] && vert1 == tetNodeIDsGrid[ind2] &&  // ii = j.
+             vert2 == tetNodeIDsGrid[ind0]) {                                   // jj = nPoly-i-j-k.
+    e = nPolyConn;
+    f = g = h = -1;
+    c = m = 1;                                                                  // kk = i.
+  } else if (vert0 == tetNodeIDsGrid[ind3] && vert1 == tetNodeIDsGrid[ind1] &&  // ii = i.
+             vert2 == tetNodeIDsGrid[ind2]) {                                   // jj = j.
+    l = nPolyConn;
+    m = n = o = -1;
+    b = g = 1;                                                                  // kk = nPoly-i-j-k.
+  } else if (vert0 == tetNodeIDsGrid[ind3] && vert1 == tetNodeIDsGrid[ind2] &&  // ii = j.
+             vert2 == tetNodeIDsGrid[ind1]) {                                   // jj = i.
+    l = nPolyConn;
+    m = n = o = -1;
+    c = f = 1;  // kk = nPoly-i-j-k.
   }
 
   else {
@@ -4974,30 +4739,28 @@ void CMeshFEM_DG::CreateConnectivitiesTriangleAdjacentTetrahedron(
   }
 
   /*--- If non-matching vertices have been found, terminate with an error message. ---*/
-  if( verticesDontMatch )
-    SU2_MPI::Error("Corner vertices do not match. This should not happen.", CURRENT_FUNCTION);
+  if (verticesDontMatch) SU2_MPI::Error("Corner vertices do not match. This should not happen.", CURRENT_FUNCTION);
 
   /*--- Some constants to convert the (ii,jj,kk) indices to a 1D index. ---*/
-  const unsigned short abv1 = (11 + 12*nPolyConn + 3*nPolyConn*nPolyConn);
-  const unsigned short abv2 = (2*nPolyConn + 3)*3;
-  const unsigned short abv3 = (nPolyConn + 2)*3;
+  const unsigned short abv1 = (11 + 12 * nPolyConn + 3 * nPolyConn * nPolyConn);
+  const unsigned short abv2 = (2 * nPolyConn + 3) * 3;
+  const unsigned short abv3 = (nPolyConn + 2) * 3;
 
   /*--- Loop over the DOFs of the original tetrahedron to create the connectivity
         of the tetrahedron that corresponds to the new numbering. ---*/
   unsigned short ind = 0;
-  for(unsigned short k=0; k<=nPolyConn; ++k) {
+  for (unsigned short k = 0; k <= nPolyConn; ++k) {
     unsigned short uppBoundJ = nPolyConn - k;
-    for(unsigned short j=0; j<=uppBoundJ; ++j) {
+    for (unsigned short j = 0; j <= uppBoundJ; ++j) {
       unsigned short uppBoundI = nPolyConn - k - j;
-      for(unsigned short i=0; i<=uppBoundI; ++i, ++ind) {
-
+      for (unsigned short i = 0; i <= uppBoundI; ++i, ++ind) {
         /*--- Determine the ii, jj and kk indices of the new numbering, convert it to
               a 1D index and shore the modified index in modConnTet. ---*/
-        unsigned short ii   = a + i*b + j*c + k*d;
-        unsigned short jj   = e + i*f + j*g + k*h;
-        unsigned short kk   = l + i*m + j*n + k*o;
-        unsigned short iind = (abv1*kk + abv2*jj + 6*ii - abv3*kk*kk
-                            -  6*kk*jj - 3*jj*jj + kk*kk*kk)/6;
+        unsigned short ii = a + i * b + j * c + k * d;
+        unsigned short jj = e + i * f + j * g + k * h;
+        unsigned short kk = l + i * m + j * n + k * o;
+        unsigned short iind =
+            (abv1 * kk + abv2 * jj + 6 * ii - abv3 * kk * kk - 6 * kk * jj - 3 * jj * jj + kk * kk * kk) / 6;
 
         modConnTet[iind] = connTet[ind];
       }
@@ -5007,19 +4770,17 @@ void CMeshFEM_DG::CreateConnectivitiesTriangleAdjacentTetrahedron(
   /*--- The triangle corresponds to face 0 of the tetrahedron. Hence the first
         nn2 entries in modConnTet are the DOFs of the triangle. Copy these
         entries from modConnTet. ---*/
-  const unsigned short nn2 = (nPolyConn+1)*(nPolyConn+2)/2;
-  for(unsigned short i=0; i<nn2; ++i)
-    modConnTria[i] = modConnTet[i];
+  const unsigned short nn2 = (nPolyConn + 1) * (nPolyConn + 2) / 2;
+  for (unsigned short i = 0; i < nn2; ++i) modConnTria[i] = modConnTet[i];
 }
 
-void CMeshFEM_DG::MetricTermsMatchingFaces(CConfig *config) {
-
+void CMeshFEM_DG::MetricTermsMatchingFaces(CConfig* config) {
   /* Determine whether or not the viscous terms are needed. */
-  bool viscousTerms = (config->GetKind_Solver() != MAIN_SOLVER::FEM_EULER && config->GetKind_Solver() != MAIN_SOLVER::DISC_ADJ_FEM_EULER);
+  bool viscousTerms = (config->GetKind_Solver() != MAIN_SOLVER::FEM_EULER &&
+                       config->GetKind_Solver() != MAIN_SOLVER::DISC_ADJ_FEM_EULER);
 
   /* Loop over the internal matching faces. */
-  for(unsigned long i=0; i<matchingFaces.size(); ++i) {
-
+  for (unsigned long i = 0; i < matchingFaces.size(); ++i) {
     /*--------------------------------------------------------------------------*/
     /*--- Step 1: Allocate the memory for the face metric terms.             ---*/
     /*---         Depending on the case, not all of this memory is needed.   ---*/
@@ -5031,21 +4792,21 @@ void CMeshFEM_DG::MetricTermsMatchingFaces(CConfig *config) {
 
     /* Determine the corresponding standard face element and get the
        relevant information from it. */
-    const unsigned short ind  = matchingFaces[i].indStandardElement;
+    const unsigned short ind = matchingFaces[i].indStandardElement;
     const unsigned short nInt = standardMatchingFacesSol[ind].GetNIntegration();
 
     /* Allocate the memory for the vectors to store the different face
        metric terms. */
-    matchingFaces[i].metricNormalsFace.resize(nInt*(nDim+1));
+    matchingFaces[i].metricNormalsFace.resize(nInt * (nDim + 1));
 
-    if( viscousTerms ) {
-      matchingFaces[i].metricCoorDerivFace0.resize(nInt*nDim*nDim);
-      matchingFaces[i].metricCoorDerivFace1.resize(nInt*nDim*nDim);
+    if (viscousTerms) {
+      matchingFaces[i].metricCoorDerivFace0.resize(nInt * nDim * nDim);
+      matchingFaces[i].metricCoorDerivFace1.resize(nInt * nDim * nDim);
     }
 
     /* Allocate the memory for the grid velocities and initialize them to the
        default value of zero. */
-    matchingFaces[i].gridVelocities.assign(nInt*nDim, 0.0);
+    matchingFaces[i].gridVelocities.assign(nInt * nDim, 0.0);
 
     /*--------------------------------------------------------------------------*/
     /*--- Step 2: Determine the actual metric data in the integration points ---*/
@@ -5056,45 +4817,38 @@ void CMeshFEM_DG::MetricTermsMatchingFaces(CConfig *config) {
        its corresponding area in the integration points. The data from side 0
        is used, but the data from side 1 should give the same result. */
     unsigned short nDOFs = standardMatchingFacesGrid[ind].GetNDOFsFaceSide0();
-    const su2double *dr = standardMatchingFacesGrid[ind].GetDrBasisFaceIntegrationSide0();
-    const su2double *ds = standardMatchingFacesGrid[ind].GetDsBasisFaceIntegrationSide0();
+    const su2double* dr = standardMatchingFacesGrid[ind].GetDrBasisFaceIntegrationSide0();
+    const su2double* ds = standardMatchingFacesGrid[ind].GetDsBasisFaceIntegrationSide0();
 
     ComputeNormalsFace(nInt, nDOFs, dr, ds, matchingFaces[i].DOFsGridFaceSide0.data(),
                        matchingFaces[i].metricNormalsFace.data());
 
     /* Check whether the viscous terms are needed in the discretization. */
-    if( viscousTerms ) {
-
+    if (viscousTerms) {
       /* Compute the derivatives of the parametric coordinates w.r.t. the
          Cartesian coordinates, i.e. drdx, drdy, etc. in the integration points
          on side 0 of the face. */
       nDOFs = standardMatchingFacesGrid[ind].GetNDOFsElemSide0();
-      dr    = standardMatchingFacesGrid[ind].GetMatDerBasisElemIntegrationSide0();
+      dr = standardMatchingFacesGrid[ind].GetMatDerBasisElemIntegrationSide0();
 
-      ComputeGradientsCoordinatesFace(nInt, nDOFs, dr,
-                                      matchingFaces[i].DOFsGridElementSide0.data(),
-                                      matchingFaces[i].metricCoorDerivFace0.data(),
-                                      config);
+      ComputeGradientsCoordinatesFace(nInt, nDOFs, dr, matchingFaces[i].DOFsGridElementSide0.data(),
+                                      matchingFaces[i].metricCoorDerivFace0.data(), config);
 
       /* Compute the derivatives of the parametric coordinates w.r.t. the
          Cartesian coordinates, i.e. drdx, drdy, etc. in the integration points
          on side 1 of the face. */
       nDOFs = standardMatchingFacesGrid[ind].GetNDOFsElemSide1();
-      dr    = standardMatchingFacesGrid[ind].GetMatDerBasisElemIntegrationSide1();
+      dr = standardMatchingFacesGrid[ind].GetMatDerBasisElemIntegrationSide1();
 
-      ComputeGradientsCoordinatesFace(nInt, nDOFs, dr,
-                                      matchingFaces[i].DOFsGridElementSide1.data(),
-                                      matchingFaces[i].metricCoorDerivFace1.data(),
-                                      config);
+      ComputeGradientsCoordinatesFace(nInt, nDOFs, dr, matchingFaces[i].DOFsGridElementSide1.data(),
+                                      matchingFaces[i].metricCoorDerivFace1.data(), config);
     }
   }
 }
 
 void CMeshFEM_DG::LengthScaleVolumeElements(void) {
-
   /* Initialize the length scale of the elements to zero. */
-  for(unsigned long i=0; i<nVolElemTot; ++i)
-    volElem[i].lenScale = 0.0;
+  for (unsigned long i = 0; i < nVolElemTot; ++i) volElem[i].lenScale = 0.0;
 
   /*-------------------------------------------------------------------*/
   /*--- Step 1: Determine the maximum value of the Jacobians of the ---*/
@@ -5102,46 +4856,43 @@ void CMeshFEM_DG::LengthScaleVolumeElements(void) {
   /*-------------------------------------------------------------------*/
 
   /*--- First the physical boundaries. Loop over them. ---*/
-  for(unsigned short j=0; j<boundaries.size(); ++j) {
-    if( !boundaries[j].periodicBoundary ) {
-      for(unsigned long i=0; i<boundaries[j].surfElem.size(); ++i) {
-
+  for (unsigned short j = 0; j < boundaries.size(); ++j) {
+    if (!boundaries[j].periodicBoundary) {
+      for (unsigned long i = 0; i < boundaries[j].surfElem.size(); ++i) {
         /* Easier storage of corresponding volume element and the metric data
            for the normals of this surface element, determine the number of
            integration points for this surface element and loop over them. */
-        const unsigned long  volInd   = boundaries[j].surfElem[i].volElemID;
-        const su2double      *normals = boundaries[j].surfElem[i].metricNormalsFace.data();
-        const unsigned short ind      = boundaries[j].surfElem[i].indStandardElement;
-        const unsigned short nInt     = standardBoundaryFacesSol[ind].GetNIntegration();
+        const unsigned long volInd = boundaries[j].surfElem[i].volElemID;
+        const su2double* normals = boundaries[j].surfElem[i].metricNormalsFace.data();
+        const unsigned short ind = boundaries[j].surfElem[i].indStandardElement;
+        const unsigned short nInt = standardBoundaryFacesSol[ind].GetNIntegration();
 
         /* Loop over the integration points and determine the maximum area
            scale for this face. This is stored in the variable lenScale of
            the corresponding volume element. */
-        for(unsigned short k=0; k<nInt; ++k)
-          volElem[volInd].lenScale = max(volElem[volInd].lenScale,
-                                         normals[k*(nDim+1)+nDim]);
+        for (unsigned short k = 0; k < nInt; ++k)
+          volElem[volInd].lenScale = max(volElem[volInd].lenScale, normals[k * (nDim + 1) + nDim]);
       }
     }
   }
 
   /*--- Loop over the matching internal faces to update the maximum Jacobian
         of the surrounding faces. ---*/
-  for(unsigned long i=0; i<matchingFaces.size(); ++i) {
-
+  for (unsigned long i = 0; i < matchingFaces.size(); ++i) {
     /* Easier storage of the ID's of the two adjacent elements, determine the
        corresponding standard face element, the number of integration points
        and store the metric data of the face a bit easier. */
-    const unsigned long  v0       = matchingFaces[i].elemID0;
-    const unsigned long  v1       = matchingFaces[i].elemID1;
-    const su2double      *normals = matchingFaces[i].metricNormalsFace.data();
-    const unsigned short ind      = matchingFaces[i].indStandardElement;
-    const unsigned short nInt     = standardMatchingFacesSol[ind].GetNIntegration();
+    const unsigned long v0 = matchingFaces[i].elemID0;
+    const unsigned long v1 = matchingFaces[i].elemID1;
+    const su2double* normals = matchingFaces[i].metricNormalsFace.data();
+    const unsigned short ind = matchingFaces[i].indStandardElement;
+    const unsigned short nInt = standardMatchingFacesSol[ind].GetNIntegration();
 
     /* Loop over the integration points and determine the maximum area
        scale for this face. This is stored in the variable lenScale of
        the neigbhoring volume elements. */
-    for(unsigned short k=0; k<nInt; ++k) {
-      const su2double area = normals[k*(nDim+1)+nDim];
+    for (unsigned short k = 0; k < nInt; ++k) {
+      const su2double area = normals[k * (nDim + 1) + nDim];
       volElem[v0].lenScale = max(volElem[v0].lenScale, area);
       volElem[v1].lenScale = max(volElem[v1].lenScale, area);
     }
@@ -5165,35 +4916,30 @@ void CMeshFEM_DG::LengthScaleVolumeElements(void) {
         Note that the inverse communication pattern must be used for this
         purpose.  ---*/
   unsigned long nRecvRequests = 0;
-  for(unsigned long i=0; i<ranksRecv.size(); ++i) {
-    if(ranksRecv[i] != rank) {
-
+  for (unsigned long i = 0; i < ranksRecv.size(); ++i) {
+    if (ranksRecv[i] != rank) {
       /* Allocate the memory for communication buffer. */
       recvBuf[i].resize(entitiesRecv[i].size());
 
       /* Fill the buffer to be sent, which is the receive
          information of the original communication pattern. */
-      for(unsigned long j=0; j<entitiesRecv[i].size(); ++j)
-        recvBuf[i][j] = volElem[entitiesRecv[i][j]].lenScale;
+      for (unsigned long j = 0; j < entitiesRecv[i].size(); ++j) recvBuf[i][j] = volElem[entitiesRecv[i][j]].lenScale;
 
       /* Send the data. */
-      SU2_MPI::Isend(recvBuf[i].data(), recvBuf[i].size(), MPI_DOUBLE,
-                     ranksRecv[i], ranksRecv[i]+10, SU2_MPI::GetComm(),
-                     &recvRequests[nRecvRequests++]);
+      SU2_MPI::Isend(recvBuf[i].data(), recvBuf[i].size(), MPI_DOUBLE, ranksRecv[i], ranksRecv[i] + 10,
+                     SU2_MPI::GetComm(), &recvRequests[nRecvRequests++]);
     }
   }
 
   /*--- Post the receives using non-blocking receives. Exclude self communication.
         Also here the inverse communication pattern must be used.  ---*/
   unsigned long nSendRequests = 0;
-  for(unsigned long i=0; i<ranksSend.size(); ++i) {
-    if(ranksSend[i] != rank)  {
-
+  for (unsigned long i = 0; i < ranksSend.size(); ++i) {
+    if (ranksSend[i] != rank) {
       /* Allocate the memory for communication buffer and post the receive. */
       sendBuf[i].resize(entitiesSend[i].size());
 
-      SU2_MPI::Irecv(sendBuf[i].data(), sendBuf[i].size(), MPI_DOUBLE,
-                     ranksSend[i], rank+10, SU2_MPI::GetComm(),
+      SU2_MPI::Irecv(sendBuf[i].data(), sendBuf[i].size(), MPI_DOUBLE, ranksSend[i], rank + 10, SU2_MPI::GetComm(),
                      &sendRequests[nSendRequests++]);
     }
   }
@@ -5205,8 +4951,8 @@ void CMeshFEM_DG::LengthScaleVolumeElements(void) {
         takes place at all. ---*/
   bool selfComm = false;
   unsigned long selfRecvInd, selfSendInd = 0;
-  for(selfRecvInd=0; selfRecvInd<ranksRecv.size(); ++selfRecvInd) {
-    if(ranksRecv[selfRecvInd] == rank) {
+  for (selfRecvInd = 0; selfRecvInd < ranksRecv.size(); ++selfRecvInd) {
+    if (ranksRecv[selfRecvInd] == rank) {
       selfComm = true;
       break;
     }
@@ -5215,12 +4961,12 @@ void CMeshFEM_DG::LengthScaleVolumeElements(void) {
   /*--- Determine the send index for self communication and update the
         data of the owners with the halo data, if self communication
         takes place. ---*/
-  if( selfComm ) {
-    for(selfSendInd=0; selfSendInd<ranksSend.size(); ++selfSendInd) {
-      if(ranksSend[selfSendInd] == rank) break;
+  if (selfComm) {
+    for (selfSendInd = 0; selfSendInd < ranksSend.size(); ++selfSendInd) {
+      if (ranksSend[selfSendInd] == rank) break;
     }
 
-    for(unsigned long j=0; j<entitiesSend[selfSendInd].size(); ++j) {
+    for (unsigned long j = 0; j < entitiesSend[selfSendInd].size(); ++j) {
       const unsigned long v0 = entitiesSend[selfSendInd][j];
       const unsigned long v1 = entitiesRecv[selfRecvInd][j];
 
@@ -5236,9 +4982,9 @@ void CMeshFEM_DG::LengthScaleVolumeElements(void) {
 
   /*--- Update the variable currently stored in lenScale for the
         owned elements. ---*/
-  for(unsigned long i=0; i<ranksSend.size(); ++i) {
-    if(ranksSend[i] != rank) {
-      for(unsigned long j=0; j<entitiesSend[i].size(); ++j) {
+  for (unsigned long i = 0; i < ranksSend.size(); ++i) {
+    if (ranksSend[i] != rank) {
+      for (unsigned long j = 0; j < entitiesSend[i].size(); ++j) {
         const unsigned long ind = entitiesSend[i][j];
         volElem[ind].lenScale = max(volElem[ind].lenScale, sendBuf[i][j]);
       }
@@ -5255,28 +5001,26 @@ void CMeshFEM_DG::LengthScaleVolumeElements(void) {
 
   /* Determine the number of metric terms per integration point.
      This depends on the number of spatial dimensions of the problem. */
-  const unsigned short nMetricPerPoint = nDim*nDim + 1;
+  const unsigned short nMetricPerPoint = nDim * nDim + 1;
 
   /* Loop over the owned volume elements. */
-  for(unsigned long i=0; i<nVolElemOwned; ++i) {
-
+  for (unsigned long i = 0; i < nVolElemOwned; ++i) {
     /* Easier storage of the metric terms and determine the number of
        integration points for this element. */
-    const su2double      *metric = volElem[i].metricTerms.data();
-    const unsigned short ind     = volElem[i].indStandardElement;
-    const unsigned short nInt    = standardElementsSol[ind].GetNIntegration();
+    const su2double* metric = volElem[i].metricTerms.data();
+    const unsigned short ind = volElem[i].indStandardElement;
+    const unsigned short nInt = standardElementsSol[ind].GetNIntegration();
 
     /* Loop over the integration points and determine the minimum Jacobian
        for this element. Note that the Jacobian is the first variable stored
        in the metric terms of the integration points. */
     su2double minJacElem = metric[0];
-    for(unsigned short k=1; k<nInt; ++k)
-      minJacElem = min(minJacElem, metric[k*nMetricPerPoint]);
+    for (unsigned short k = 1; k < nInt; ++k) minJacElem = min(minJacElem, metric[k * nMetricPerPoint]);
 
     /* Determine the length scale of the element, for which the length
        scale of the reference element, 2.0, must be taken into account. */
     const su2double maxJacFaces = volElem[i].lenScale;
-    volElem[i].lenScale         = 2.0*minJacElem/maxJacFaces;
+    volElem[i].lenScale = 2.0 * minJacElem / maxJacFaces;
   }
 
   /*-------------------------------------------------------------------*/
@@ -5287,29 +5031,24 @@ void CMeshFEM_DG::LengthScaleVolumeElements(void) {
 
   /*--- Send the data using non-blocking sends. Exclude self communication. ---*/
   nSendRequests = 0;
-  for(unsigned long i=0; i<ranksSend.size(); ++i) {
-    if(ranksSend[i] != rank) {
-
+  for (unsigned long i = 0; i < ranksSend.size(); ++i) {
+    if (ranksSend[i] != rank) {
       /* Fill the send buffer. */
-      for(unsigned long j=0; j<entitiesSend[i].size(); ++j)
-        sendBuf[i][j] = volElem[entitiesSend[i][j]].lenScale;
+      for (unsigned long j = 0; j < entitiesSend[i].size(); ++j) sendBuf[i][j] = volElem[entitiesSend[i][j]].lenScale;
 
       /* Send the data. */
-      SU2_MPI::Isend(sendBuf[i].data(), sendBuf[i].size(), MPI_DOUBLE,
-                     ranksSend[i], ranksSend[i]+20, SU2_MPI::GetComm(),
-                     &sendRequests[nSendRequests++]);
+      SU2_MPI::Isend(sendBuf[i].data(), sendBuf[i].size(), MPI_DOUBLE, ranksSend[i], ranksSend[i] + 20,
+                     SU2_MPI::GetComm(), &sendRequests[nSendRequests++]);
     }
   }
 
   /*--- Post the receives using non-blocking receives.
         Exclude self communication. ---*/
   nRecvRequests = 0;
-  for(unsigned long i=0; i<ranksRecv.size(); ++i) {
-    if(ranksRecv[i] != rank) {
-
+  for (unsigned long i = 0; i < ranksRecv.size(); ++i) {
+    if (ranksRecv[i] != rank) {
       /* Post the nonblocking receive. */
-      SU2_MPI::Irecv(recvBuf[i].data(), recvBuf[i].size(), MPI_DOUBLE,
-                     ranksRecv[i], rank+20, SU2_MPI::GetComm(),
+      SU2_MPI::Irecv(recvBuf[i].data(), recvBuf[i].size(), MPI_DOUBLE, ranksRecv[i], rank + 20, SU2_MPI::GetComm(),
                      &recvRequests[nRecvRequests++]);
     }
   }
@@ -5318,8 +5057,8 @@ void CMeshFEM_DG::LengthScaleVolumeElements(void) {
 
   /*--- Carry out the self communication, if needed. Note that this part
         is outside the MPI part. ---*/
-  if( selfComm ) {
-    for(unsigned long j=0; j<entitiesSend[selfSendInd].size(); ++j) {
+  if (selfComm) {
+    for (unsigned long j = 0; j < entitiesSend[selfSendInd].size(); ++j) {
       const unsigned long v0 = entitiesSend[selfSendInd][j];
       const unsigned long v1 = entitiesRecv[selfRecvInd][j];
       volElem[v1].lenScale = volElem[v0].lenScale;
@@ -5333,31 +5072,27 @@ void CMeshFEM_DG::LengthScaleVolumeElements(void) {
   SU2_MPI::Waitall(nRecvRequests, recvRequests.data(), MPI_STATUSES_IGNORE);
 
   /*--- Copy the data from the receive buffers into the volElem. ---*/
-  for(unsigned long i=0; i<ranksRecv.size(); ++i) {
-    if(ranksRecv[i] != rank) {
-      for(unsigned long j=0; j<entitiesRecv[i].size(); ++j)
-        volElem[entitiesRecv[i][j]].lenScale = recvBuf[i][j];
+  for (unsigned long i = 0; i < ranksRecv.size(); ++i) {
+    if (ranksRecv[i] != rank) {
+      for (unsigned long j = 0; j < entitiesRecv[i].size(); ++j) volElem[entitiesRecv[i][j]].lenScale = recvBuf[i][j];
     }
   }
 
 #endif
 }
 
-void CMeshFEM_DG::MetricTermsSurfaceElements(CConfig *config) {
-
+void CMeshFEM_DG::MetricTermsSurfaceElements(CConfig* config) {
   /*--- Compute the metric terms of the internal matching faces. ---*/
   MetricTermsMatchingFaces(config);
 
   /*--- Loop over the physical boundaries and compute the metric
         terms of the boundary. ---*/
-  for(unsigned short i=0; i<boundaries.size(); ++i) {
-    if( !boundaries[i].periodicBoundary )
-      MetricTermsBoundaryFaces(&boundaries[i], config);
+  for (unsigned short i = 0; i < boundaries.size(); ++i) {
+    if (!boundaries[i].periodicBoundary) MetricTermsBoundaryFaces(&boundaries[i], config);
   }
 }
 
-void CMeshFEM_DG::MetricTermsVolumeElements(CConfig *config) {
-
+void CMeshFEM_DG::MetricTermsVolumeElements(CConfig* config) {
   /* Find out whether or not the full, inverse of the full and the lumped mass
      matrices are needed. In principle always the full mass matrix is used,
      unless the user explicitly indices to use the lumped mass matrix for
@@ -5367,32 +5102,33 @@ void CMeshFEM_DG::MetricTermsVolumeElements(CConfig *config) {
      metric terms are needed for the computation of the 2nd derivatives. */
   const bool UseLumpedMassMatrix = config->GetUse_Lumped_MassMatrix_DGFEM();
 
-  bool FullMassMatrix   = false, FullInverseMassMatrix = false;
+  bool FullMassMatrix = false, FullInverseMassMatrix = false;
   bool LumpedMassMatrix = false, DerMetricTerms = false;
 
-  if(config->GetTime_Marching() == TIME_MARCHING::STEADY ||
-     config->GetTime_Marching() == TIME_MARCHING::ROTATIONAL_FRAME) {
-    if( UseLumpedMassMatrix) LumpedMassMatrix      = true;
-    else                     FullInverseMassMatrix = true;
-  }
-  else if(config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST ||
-          config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND ||
-          config->GetTime_Marching() == TIME_MARCHING::HARMONIC_BALANCE) {
-    if( UseLumpedMassMatrix ) FullMassMatrix = LumpedMassMatrix = true;
-    else                      FullInverseMassMatrix = true;
-  }
-  else {
-
+  if (config->GetTime_Marching() == TIME_MARCHING::STEADY ||
+      config->GetTime_Marching() == TIME_MARCHING::ROTATIONAL_FRAME) {
+    if (UseLumpedMassMatrix)
+      LumpedMassMatrix = true;
+    else
+      FullInverseMassMatrix = true;
+  } else if (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST ||
+             config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND ||
+             config->GetTime_Marching() == TIME_MARCHING::HARMONIC_BALANCE) {
+    if (UseLumpedMassMatrix)
+      FullMassMatrix = LumpedMassMatrix = true;
+    else
+      FullInverseMassMatrix = true;
+  } else {
     /* Time accurate explicit time integration scheme. */
-    FullMassMatrix        = LumpedMassMatrix = false;
+    FullMassMatrix = LumpedMassMatrix = false;
     FullInverseMassMatrix = true;
 
     /* For ADER-DG, check if the derivative of the metric terms are needed. */
-    if(config->GetKind_TimeIntScheme_Flow() == ADER_DG) {
+    if (config->GetKind_TimeIntScheme_Flow() == ADER_DG) {
       MAIN_SOLVER solver = config->GetKind_Solver();
-      if(solver == MAIN_SOLVER::FEM_NAVIER_STOKES || solver == MAIN_SOLVER::FEM_RANS || solver == MAIN_SOLVER::FEM_LES) {
-        if(config->GetKind_ADER_Predictor() == ADER_NON_ALIASED_PREDICTOR)
-          DerMetricTerms = true;
+      if (solver == MAIN_SOLVER::FEM_NAVIER_STOKES || solver == MAIN_SOLVER::FEM_RANS ||
+          solver == MAIN_SOLVER::FEM_LES) {
+        if (config->GetKind_ADER_Predictor() == ADER_NON_ALIASED_PREDICTOR) DerMetricTerms = true;
       }
     }
   }
@@ -5401,8 +5137,8 @@ void CMeshFEM_DG::MetricTermsVolumeElements(CConfig *config) {
      This depends on the number of spatial dimensions of the problem.
      Also determine the additional number of metric terms per integration
      point for the computation of the second derivatives. */
-  const unsigned short nMetricPerPoint       = nDim*nDim + 1;
-  const unsigned short nMetric2ndDerPerPoint = nDim*(nDim + nDim*(nDim-1)/2);
+  const unsigned short nMetricPerPoint = nDim * nDim + 1;
+  const unsigned short nMetric2ndDerPerPoint = nDim * (nDim + nDim * (nDim - 1) / 2);
 
   /*--------------------------------------------------------------------------*/
   /*--- Step 1: Determine the metric terms, drdx, drdy, drdz, dsdx, etc.   ---*/
@@ -5411,75 +5147,68 @@ void CMeshFEM_DG::MetricTermsVolumeElements(CConfig *config) {
   /*--------------------------------------------------------------------------*/
 
   /* Loop over the owned volume elements. */
-  for(unsigned long i=0; i<nVolElemOwned; ++i) {
-
+  for (unsigned long i = 0; i < nVolElemOwned; ++i) {
     /* Easier storage of the index of the corresponding standard element
        and determine the number of integration points as well as the number
        of DOFs for the grid and solution. */
-    const unsigned short ind       = volElem[i].indStandardElement;
-    const unsigned short nInt      = standardElementsGrid[ind].GetNIntegration();
+    const unsigned short ind = volElem[i].indStandardElement;
+    const unsigned short nInt = standardElementsGrid[ind].GetNIntegration();
     const unsigned short nDOFsGrid = volElem[i].nDOFsGrid;
-    const unsigned short nDOFsSol  = volElem[i].nDOFsSol;
+    const unsigned short nDOFsSol = volElem[i].nDOFsSol;
 
     /* Allocate the memory for the grid velocities. They are initialized to
        zero as default value, i.e. not moving. */
-    volElem[i].gridVelocities.assign(nDim*nInt, 0.0);
-    volElem[i].gridVelocitiesSolDOFs.assign(nDim*nDOFsSol, 0.0);
+    volElem[i].gridVelocities.assign(nDim * nInt, 0.0);
+    volElem[i].gridVelocitiesSolDOFs.assign(nDim * nDOFsSol, 0.0);
 
     /* Allocate the memory for the metric terms of this element. */
-    volElem[i].metricTerms.resize(nMetricPerPoint*nInt);
-    volElem[i].metricTermsSolDOFs.resize(nMetricPerPoint*nDOFsSol);
+    volElem[i].metricTerms.resize(nMetricPerPoint * nInt);
+    volElem[i].metricTermsSolDOFs.resize(nMetricPerPoint * nDOFsSol);
 
     /* Get the pointer to the matrix storage of the basis functions
        and its derivatives. The first nDOFsGrid*nInt entries of this matrix
        correspond to the interpolation data to the integration points
        and are not needed. Hence this part is skipped. */
-    const su2double *matBasisInt    = standardElementsGrid[ind].GetMatBasisFunctionsIntegration();
-    const su2double *matDerBasisInt = matBasisInt + nDOFsGrid*nInt;
+    const su2double* matBasisInt = standardElementsGrid[ind].GetMatBasisFunctionsIntegration();
+    const su2double* matDerBasisInt = matBasisInt + nDOFsGrid * nInt;
 
     /* Also get the pointer to the matrix storage of the derivatives of the
        basis functions in the sol DOFs. */
-    const su2double *matDerBasisSolDOFs = standardElementsGrid[ind].GetMatDerBasisFunctionsSolDOFs();
+    const su2double* matDerBasisSolDOFs = standardElementsGrid[ind].GetMatDerBasisFunctionsSolDOFs();
 
     /* Allocate the memory for the result vectors. */
-    vector<su2double> helpVecResultInt(nInt*nDim*nDim);
-    vector<su2double> helpVecResultDOFsSol(nDOFsSol*nDim*nDim);
-    su2double *vecResultInt     = helpVecResultInt.data();
-    su2double *vecResultDOFsSol = helpVecResultDOFsSol.data();
+    vector<su2double> helpVecResultInt(nInt * nDim * nDim);
+    vector<su2double> helpVecResultDOFsSol(nDOFsSol * nDim * nDim);
+    su2double* vecResultInt = helpVecResultInt.data();
+    su2double* vecResultDOFsSol = helpVecResultDOFsSol.data();
 
     /* Compute the gradient of the coordinates w.r.t. the parametric
        coordinates for this element in the integration points. */
-    ComputeGradientsCoorWRTParam(nInt, nDOFsGrid, matDerBasisInt,
-                                 volElem[i].nodeIDsGrid.data(),
-                                 vecResultInt, config);
+    ComputeGradientsCoorWRTParam(nInt, nDOFsGrid, matDerBasisInt, volElem[i].nodeIDsGrid.data(), vecResultInt, config);
 
     /* Compute the gradient of the coordinates w.r.t. the parametric
        coordinates for this element in the solution DOFs. */
-    ComputeGradientsCoorWRTParam(nDOFsSol, nDOFsGrid, matDerBasisSolDOFs,
-                                 volElem[i].nodeIDsGrid.data(),
+    ComputeGradientsCoorWRTParam(nDOFsSol, nDOFsGrid, matDerBasisSolDOFs, volElem[i].nodeIDsGrid.data(),
                                  vecResultDOFsSol, config);
 
     /* Convert the values of dxdr, dydr, etc. to the required metric terms
        for both the integration points and the solution DOFs. */
-    VolumeMetricTermsFromCoorGradients(nInt, vecResultInt,
-                                       volElem[i].metricTerms);
+    VolumeMetricTermsFromCoorGradients(nInt, vecResultInt, volElem[i].metricTerms);
 
-    VolumeMetricTermsFromCoorGradients(nDOFsSol, vecResultDOFsSol,
-                                       volElem[i].metricTermsSolDOFs);
+    VolumeMetricTermsFromCoorGradients(nDOFsSol, vecResultDOFsSol, volElem[i].metricTermsSolDOFs);
 
     /* Check for negative Jacobians in the integrations points and at the
        location of the solution DOFs. */
     bool negJacobian = false;
-    for(unsigned short j=0; j<nInt; ++j) {
-      if(volElem[i].metricTerms[nMetricPerPoint*j] <= 0.0) negJacobian = true;
+    for (unsigned short j = 0; j < nInt; ++j) {
+      if (volElem[i].metricTerms[nMetricPerPoint * j] <= 0.0) negJacobian = true;
     }
 
-    for(unsigned short j=0; j<nDOFsSol; ++j) {
-      if(volElem[i].metricTermsSolDOFs[nMetricPerPoint*j] <= 0.0) negJacobian = true;
+    for (unsigned short j = 0; j < nDOFsSol; ++j) {
+      if (volElem[i].metricTermsSolDOFs[nMetricPerPoint * j] <= 0.0) negJacobian = true;
     }
 
-    if( negJacobian )
-      SU2_MPI::Error("Negative Jacobian found.", CURRENT_FUNCTION);
+    if (negJacobian) SU2_MPI::Error("Negative Jacobian found.", CURRENT_FUNCTION);
   }
 
   /*--------------------------------------------------------------------------*/
@@ -5487,98 +5216,89 @@ void CMeshFEM_DG::MetricTermsVolumeElements(CConfig *config) {
   /*---         integration points, if needed.                             ---*/
   /*--------------------------------------------------------------------------*/
 
-  if( DerMetricTerms ) {
-
+  if (DerMetricTerms) {
     /* Loop over the owned volume elements. */
-    for(unsigned long i=0; i<nVolElemOwned; ++i) {
-
+    for (unsigned long i = 0; i < nVolElemOwned; ++i) {
       /* Easier storage of the index of the corresponding standard element
          and determine the number of integration points as well as the number
          of DOFs for the grid. */
-      const unsigned short ind       = volElem[i].indStandardElement;
-      const unsigned short nInt      = standardElementsGrid[ind].GetNIntegration();
+      const unsigned short ind = volElem[i].indStandardElement;
+      const unsigned short nInt = standardElementsGrid[ind].GetNIntegration();
       const unsigned short nDOFsGrid = volElem[i].nDOFsGrid;
 
       /* Get the pointer to the matrix storage of the basis functions
          and its derivatives. The first nDOFsGrid*nInt entries of this matrix
          correspond to the interpolation data to the integration points
          and are not needed. Hence this part is skipped. */
-      const su2double *matBasisInt    = standardElementsGrid[ind].GetMatBasisFunctionsIntegration();
-      const su2double *matDerBasisInt = matBasisInt + nDOFsGrid*nInt;
+      const su2double* matBasisInt = standardElementsGrid[ind].GetMatBasisFunctionsIntegration();
+      const su2double* matDerBasisInt = matBasisInt + nDOFsGrid * nInt;
 
       /* Also get the pointer to the matrix storage of the derivatives of the
          basis functions in the owned DOFs, i.e. the grid DOFs. */
-      const su2double *matDerBasisGridDOFs = standardElementsGrid[ind].GetMatDerBasisFunctionsOwnDOFs();
+      const su2double* matDerBasisGridDOFs = standardElementsGrid[ind].GetMatDerBasisFunctionsOwnDOFs();
 
       /* Compute the gradient of the coordinates w.r.t. the parametric
          coordinates for this element in the solution DOFs. */
-      vector<su2double> helpVecResultGridDOFs(nDOFsGrid*nDim*nDim);
-      su2double *vecResultGridDOFs = helpVecResultGridDOFs.data();
+      vector<su2double> helpVecResultGridDOFs(nDOFsGrid * nDim * nDim);
+      su2double* vecResultGridDOFs = helpVecResultGridDOFs.data();
 
-      ComputeGradientsCoorWRTParam(nDOFsGrid, nDOFsGrid, matDerBasisGridDOFs,
-                                   volElem[i].nodeIDsGrid.data(),
+      ComputeGradientsCoorWRTParam(nDOFsGrid, nDOFsGrid, matDerBasisGridDOFs, volElem[i].nodeIDsGrid.data(),
                                    vecResultGridDOFs, config);
 
       /* Convert the values of dxdr, dydr, etc. to the required metric terms
          in the grid DOFs. */
-      vector<su2double> metricGridDOFs(nDOFsGrid*nMetricPerPoint);
-      VolumeMetricTermsFromCoorGradients(nDOFsGrid, vecResultGridDOFs,
-                                         metricGridDOFs);
+      vector<su2double> metricGridDOFs(nDOFsGrid * nMetricPerPoint);
+      VolumeMetricTermsFromCoorGradients(nDOFsGrid, vecResultGridDOFs, metricGridDOFs);
 
       /*--- The metric terms currently stored in metricGridDOFs are scaled
             with the Jacobian and also the Jacobian is part of the metric
             terms. For the derivatives of the metric terms, the Jacobian
             is not needed, but the original unscaled terms are needed.
             This is done in the loop below. ---*/
-      for(unsigned short j=0; j<nDOFsGrid; ++j) {
-        su2double *metOld = metricGridDOFs.data() + j*nMetricPerPoint;
-        su2double *metNew = metricGridDOFs.data() + j*(nMetricPerPoint-1);
+      for (unsigned short j = 0; j < nDOFsGrid; ++j) {
+        su2double* metOld = metricGridDOFs.data() + j * nMetricPerPoint;
+        su2double* metNew = metricGridDOFs.data() + j * (nMetricPerPoint - 1);
 
-        const su2double JacInv = 1.0/metOld[0];
-        for(unsigned short k=1; k<nMetricPerPoint; ++k)
-          metNew[k-1] = JacInv*metOld[k];
+        const su2double JacInv = 1.0 / metOld[0];
+        for (unsigned short k = 1; k < nMetricPerPoint; ++k) metNew[k - 1] = JacInv * metOld[k];
       }
 
       /* Compute the derivatives of the metric terms w.r.t. the
          parametric coordinates in the integration points.
          First allocate the memory to store the results. */
-      vector<su2double> helpVecDerMetrics(nDim*nInt*(nMetricPerPoint-1));
-      su2double *vecDerMetrics = helpVecDerMetrics.data();
+      vector<su2double> helpVecDerMetrics(nDim * nInt * (nMetricPerPoint - 1));
+      su2double* vecDerMetrics = helpVecDerMetrics.data();
 
       /* Carry out the matrix multiplication. The last argument is NULL, such
          that this gemm call is ignored in the profiling. Replace by config if
          it should be included. */
-      blasFunctions->gemm(nDim*nInt, nMetricPerPoint-1, nDOFsGrid, matDerBasisInt,
-                          metricGridDOFs.data(), vecDerMetrics, nullptr);
+      blasFunctions->gemm(nDim * nInt, nMetricPerPoint - 1, nDOFsGrid, matDerBasisInt, metricGridDOFs.data(),
+                          vecDerMetrics, nullptr);
 
       /* Allocate the memory for the additional metric terms needed to
          compute the second derivatives. */
-      volElem[i].metricTerms2ndDer.resize(nInt*nMetric2ndDerPerPoint);
+      volElem[i].metricTerms2ndDer.resize(nInt * nMetric2ndDerPerPoint);
 
       /*--- Loop over the integration points to compute the additional metric
             terms needed for the second derivatives. This is a combination of
             the original metric terms and derivatives of these terms.
             Make a distinction between 2D and 3D. ---*/
-      switch( nDim ) {
+      switch (nDim) {
         case 2: {
-
           /* 2D computation. Loop over the integration points. */
-          for(unsigned short j=0; j<nInt; ++j) {
-
+          for (unsigned short j = 0; j < nInt; ++j) {
             /* Set the pointers where the data for this integration
                point starts. */
-            const su2double *metric       = volElem[i].metricTerms.data()
-                                          + j*nMetricPerPoint;
-            const su2double *rDerMetric   = vecDerMetrics + j*(nMetricPerPoint-1);
-            const su2double *sDerMetric   = rDerMetric + nInt*(nMetricPerPoint-1);
-            su2double       *metric2ndDer = volElem[i].metricTerms2ndDer.data()
-                                          + j*nMetric2ndDerPerPoint;
+            const su2double* metric = volElem[i].metricTerms.data() + j * nMetricPerPoint;
+            const su2double* rDerMetric = vecDerMetrics + j * (nMetricPerPoint - 1);
+            const su2double* sDerMetric = rDerMetric + nInt * (nMetricPerPoint - 1);
+            su2double* metric2ndDer = volElem[i].metricTerms2ndDer.data() + j * nMetric2ndDerPerPoint;
 
             /* More readable abbreviations for the metric terms
                and its derivatives. */
-            const su2double JacInv = 1.0/metric[0];
-            const su2double drdx   = JacInv*metric[1], drdy = JacInv*metric[2];
-            const su2double dsdx   = JacInv*metric[3], dsdy = JacInv*metric[4];
+            const su2double JacInv = 1.0 / metric[0];
+            const su2double drdx = JacInv * metric[1], drdy = JacInv * metric[2];
+            const su2double dsdx = JacInv * metric[3], dsdy = JacInv * metric[4];
 
             const su2double ddrdx_dr = rDerMetric[0], ddrdy_dr = rDerMetric[1];
             const su2double ddsdx_dr = rDerMetric[2], ddsdy_dr = rDerMetric[3];
@@ -5589,42 +5309,36 @@ void CMeshFEM_DG::MetricTermsVolumeElements(CConfig *config) {
             /* Compute the metric terms needed to compute the Cartesian 2nd
                derivatives. Note that for the cross derivatives an average of
                the two possibilities is taken. */
-            metric2ndDer[0] = drdx*ddrdx_dr + dsdx*ddrdx_ds;
-            metric2ndDer[1] = drdx*ddsdx_dr + dsdx*ddsdx_ds;
+            metric2ndDer[0] = drdx * ddrdx_dr + dsdx * ddrdx_ds;
+            metric2ndDer[1] = drdx * ddsdx_dr + dsdx * ddsdx_ds;
 
-            metric2ndDer[2] = 0.5*(drdx*ddrdy_dr + dsdx*ddrdy_ds
-                            +      drdy*ddrdx_dr + dsdy*ddrdx_ds);
-            metric2ndDer[3] = 0.5*(drdx*ddsdy_dr + dsdx*ddsdy_ds
-                            +      drdy*ddsdx_dr + dsdy*ddsdx_ds);
+            metric2ndDer[2] = 0.5 * (drdx * ddrdy_dr + dsdx * ddrdy_ds + drdy * ddrdx_dr + dsdy * ddrdx_ds);
+            metric2ndDer[3] = 0.5 * (drdx * ddsdy_dr + dsdx * ddsdy_ds + drdy * ddsdx_dr + dsdy * ddsdx_ds);
 
-            metric2ndDer[4] = drdy*ddrdy_dr + dsdy*ddrdy_ds;
-            metric2ndDer[5] = drdy*ddsdy_dr + dsdy*ddsdy_ds;
+            metric2ndDer[4] = drdy * ddrdy_dr + dsdy * ddrdy_ds;
+            metric2ndDer[5] = drdy * ddsdy_dr + dsdy * ddsdy_ds;
           }
 
           break;
         }
 
         case 3: {
-
           /* 3D computation. Loop over the integration points. */
-          for(unsigned short j=0; j<nInt; ++j) {
-
+          for (unsigned short j = 0; j < nInt; ++j) {
             /* Set the pointers where the data for this integration
                point starts. */
-            const su2double *metric       = volElem[i].metricTerms.data()
-                                          + j*nMetricPerPoint;
-            const su2double *rDerMetric   = vecDerMetrics + j*(nMetricPerPoint-1);
-            const su2double *sDerMetric   = rDerMetric + nInt*(nMetricPerPoint-1);
-            const su2double *tDerMetric   = sDerMetric + nInt*(nMetricPerPoint-1);
-            su2double       *metric2ndDer = volElem[i].metricTerms2ndDer.data()
-                                          + j*nMetric2ndDerPerPoint;
+            const su2double* metric = volElem[i].metricTerms.data() + j * nMetricPerPoint;
+            const su2double* rDerMetric = vecDerMetrics + j * (nMetricPerPoint - 1);
+            const su2double* sDerMetric = rDerMetric + nInt * (nMetricPerPoint - 1);
+            const su2double* tDerMetric = sDerMetric + nInt * (nMetricPerPoint - 1);
+            su2double* metric2ndDer = volElem[i].metricTerms2ndDer.data() + j * nMetric2ndDerPerPoint;
 
             /* More readable abbreviations for the metric terms
                and its derivatives. */
-            const su2double JacInv = 1.0/metric[0];
-            const su2double drdx   = JacInv*metric[1], drdy = JacInv*metric[2], drdz = JacInv*metric[3];
-            const su2double dsdx   = JacInv*metric[4], dsdy = JacInv*metric[5], dsdz = JacInv*metric[6];
-            const su2double dtdx   = JacInv*metric[7], dtdy = JacInv*metric[8], dtdz = JacInv*metric[9];
+            const su2double JacInv = 1.0 / metric[0];
+            const su2double drdx = JacInv * metric[1], drdy = JacInv * metric[2], drdz = JacInv * metric[3];
+            const su2double dsdx = JacInv * metric[4], dsdy = JacInv * metric[5], dsdz = JacInv * metric[6];
+            const su2double dtdx = JacInv * metric[7], dtdy = JacInv * metric[8], dtdz = JacInv * metric[9];
 
             const su2double ddrdx_dr = rDerMetric[0], ddrdy_dr = rDerMetric[1], ddrdz_dr = rDerMetric[2];
             const su2double ddsdx_dr = rDerMetric[3], ddsdy_dr = rDerMetric[4], ddsdz_dr = rDerMetric[5];
@@ -5641,38 +5355,38 @@ void CMeshFEM_DG::MetricTermsVolumeElements(CConfig *config) {
             /* Compute the metric terms needed to compute the Cartesian 2nd
                derivatives. Note that for the cross derivatives an average of
                the two possibilities is taken. */
-            metric2ndDer[0] = drdx*ddrdx_dr + dsdx*ddrdx_ds + dtdx*ddrdx_dt;
-            metric2ndDer[1] = drdx*ddsdx_dr + dsdx*ddsdx_ds + dtdx*ddsdx_dt;
-            metric2ndDer[2] = drdx*ddtdx_dr + dsdx*ddtdx_ds + dtdx*ddtdx_dt;
-
-            metric2ndDer[3] = 0.5*(drdx*ddrdy_dr + dsdx*ddrdy_ds + dtdx*ddrdy_dt
-                            +      drdy*ddrdx_dr + dsdy*ddrdx_ds + dtdy*ddrdx_dt);
-            metric2ndDer[4] = 0.5*(drdx*ddsdy_dr + dsdx*ddsdy_ds + dtdx*ddsdy_dt
-                            +      drdy*ddsdx_dr + dsdy*ddsdx_ds + dtdy*ddsdx_dt);
-            metric2ndDer[5] = 0.5*(drdx*ddtdy_dr + dsdx*ddtdy_ds + dtdx*ddtdy_dt
-                            +      drdy*ddtdx_dr + dsdy*ddtdx_ds + dtdy*ddtdx_dt);
-
-            metric2ndDer[6] = drdy*ddrdy_dr + dsdy*ddrdy_ds + dtdy*ddrdy_dt;
-            metric2ndDer[7] = drdy*ddsdy_dr + dsdy*ddsdy_ds + dtdy*ddsdy_dt;
-            metric2ndDer[8] = drdy*ddtdy_dr + dsdy*ddtdy_ds + dtdy*ddtdy_dt;
-
-            metric2ndDer[9]  = 0.5*(drdx*ddrdz_dr + dsdx*ddrdz_ds + dtdx*ddrdz_dt
-                             +      drdz*ddrdx_dr + dsdz*ddrdx_ds + dtdz*ddrdx_dt);
-            metric2ndDer[10] = 0.5*(drdx*ddsdz_dr + dsdx*ddsdz_ds + dtdx*ddsdz_dt
-                             +      drdz*ddsdx_dr + dsdz*ddsdx_ds + dtdz*ddsdx_dt);
-            metric2ndDer[11] = 0.5*(drdx*ddtdz_dr + dsdx*ddtdz_ds + dtdx*ddtdz_dt
-                             +      drdz*ddtdx_dr + dsdz*ddtdx_ds + dtdz*ddtdx_dt);
-
-            metric2ndDer[12] = 0.5*(drdy*ddrdz_dr + dsdy*ddrdz_ds + dtdy*ddrdz_dt
-                             +      drdz*ddrdy_dr + dsdz*ddrdy_ds + dtdz*ddrdy_dt);
-            metric2ndDer[13] = 0.5*(drdy*ddsdz_dr + dsdy*ddsdz_ds + dtdy*ddsdz_dt
-                             +      drdz*ddsdy_dr + dsdz*ddsdy_ds + dtdz*ddsdy_dt);
-            metric2ndDer[14] = 0.5*(drdy*ddtdz_dr + dsdy*ddtdz_ds + dtdy*ddtdz_dt
-                             +      drdz*ddtdy_dr + dsdz*ddtdy_ds + dtdz*ddtdy_dt);
-
-            metric2ndDer[15] = drdz*ddrdz_dr + dsdz*ddrdz_ds + dtdz*ddrdz_dt;
-            metric2ndDer[16] = drdz*ddsdz_dr + dsdz*ddsdz_ds + dtdz*ddsdz_dt;
-            metric2ndDer[17] = drdz*ddtdz_dr + dsdz*ddtdz_ds + dtdz*ddtdz_dt;
+            metric2ndDer[0] = drdx * ddrdx_dr + dsdx * ddrdx_ds + dtdx * ddrdx_dt;
+            metric2ndDer[1] = drdx * ddsdx_dr + dsdx * ddsdx_ds + dtdx * ddsdx_dt;
+            metric2ndDer[2] = drdx * ddtdx_dr + dsdx * ddtdx_ds + dtdx * ddtdx_dt;
+
+            metric2ndDer[3] = 0.5 * (drdx * ddrdy_dr + dsdx * ddrdy_ds + dtdx * ddrdy_dt + drdy * ddrdx_dr +
+                                     dsdy * ddrdx_ds + dtdy * ddrdx_dt);
+            metric2ndDer[4] = 0.5 * (drdx * ddsdy_dr + dsdx * ddsdy_ds + dtdx * ddsdy_dt + drdy * ddsdx_dr +
+                                     dsdy * ddsdx_ds + dtdy * ddsdx_dt);
+            metric2ndDer[5] = 0.5 * (drdx * ddtdy_dr + dsdx * ddtdy_ds + dtdx * ddtdy_dt + drdy * ddtdx_dr +
+                                     dsdy * ddtdx_ds + dtdy * ddtdx_dt);
+
+            metric2ndDer[6] = drdy * ddrdy_dr + dsdy * ddrdy_ds + dtdy * ddrdy_dt;
+            metric2ndDer[7] = drdy * ddsdy_dr + dsdy * ddsdy_ds + dtdy * ddsdy_dt;
+            metric2ndDer[8] = drdy * ddtdy_dr + dsdy * ddtdy_ds + dtdy * ddtdy_dt;
+
+            metric2ndDer[9] = 0.5 * (drdx * ddrdz_dr + dsdx * ddrdz_ds + dtdx * ddrdz_dt + drdz * ddrdx_dr +
+                                     dsdz * ddrdx_ds + dtdz * ddrdx_dt);
+            metric2ndDer[10] = 0.5 * (drdx * ddsdz_dr + dsdx * ddsdz_ds + dtdx * ddsdz_dt + drdz * ddsdx_dr +
+                                      dsdz * ddsdx_ds + dtdz * ddsdx_dt);
+            metric2ndDer[11] = 0.5 * (drdx * ddtdz_dr + dsdx * ddtdz_ds + dtdx * ddtdz_dt + drdz * ddtdx_dr +
+                                      dsdz * ddtdx_ds + dtdz * ddtdx_dt);
+
+            metric2ndDer[12] = 0.5 * (drdy * ddrdz_dr + dsdy * ddrdz_ds + dtdy * ddrdz_dt + drdz * ddrdy_dr +
+                                      dsdz * ddrdy_ds + dtdz * ddrdy_dt);
+            metric2ndDer[13] = 0.5 * (drdy * ddsdz_dr + dsdy * ddsdz_ds + dtdy * ddsdz_dt + drdz * ddsdy_dr +
+                                      dsdz * ddsdy_ds + dtdz * ddsdy_dt);
+            metric2ndDer[14] = 0.5 * (drdy * ddtdz_dr + dsdy * ddtdz_ds + dtdy * ddtdz_dt + drdz * ddtdy_dr +
+                                      dsdz * ddtdy_ds + dtdz * ddtdy_dt);
+
+            metric2ndDer[15] = drdz * ddrdz_dr + dsdz * ddrdz_ds + dtdz * ddrdz_dt;
+            metric2ndDer[16] = drdz * ddsdz_dr + dsdz * ddsdz_ds + dtdz * ddsdz_dt;
+            metric2ndDer[17] = drdz * ddtdz_dr + dsdz * ddtdz_ds + dtdz * ddtdz_dt;
           }
 
           break;
@@ -5688,8 +5402,7 @@ void CMeshFEM_DG::MetricTermsVolumeElements(CConfig *config) {
 
   /* Determine the time coefficients in the iteration matrix of the ADER-DG
      predictor step. */
-  if(config->GetKind_TimeIntScheme_Flow() == ADER_DG)
-    TimeCoefficientsPredictorADER_DG(config);
+  if (config->GetKind_TimeIntScheme_Flow() == ADER_DG) TimeCoefficientsPredictorADER_DG(config);
 
   /* Define the double vector to define the values of the mass matrix
      contributions of the standard element in the integration points. */
@@ -5697,44 +5410,41 @@ void CMeshFEM_DG::MetricTermsVolumeElements(CConfig *config) {
   valMMInt.resize(standardElementsSol.size());
 
   /* Loop over the different standard elements. */
-  for(unsigned long i=0; i<standardElementsSol.size(); ++i) {
-
+  for (unsigned long i = 0; i < standardElementsSol.size(); ++i) {
     /* Get the required data from the standard element. */
-    const unsigned short nInt  = standardElementsSol[i].GetNIntegration();
+    const unsigned short nInt = standardElementsSol[i].GetNIntegration();
     const unsigned short nDOFs = standardElementsSol[i].GetNDOFs();
-    const su2double      *lag  = standardElementsSol[i].GetBasisFunctionsIntegration();
-    const su2double      *w    = standardElementsSol[i].GetWeightsIntegration();
+    const su2double* lag = standardElementsSol[i].GetBasisFunctionsIntegration();
+    const su2double* w = standardElementsSol[i].GetWeightsIntegration();
 
     /* Allocate the memory for valMMInt[i]. */
-    valMMInt[i].resize(nDOFs*nDOFs*nInt);
+    valMMInt[i].resize(nDOFs * nDOFs * nInt);
 
     /* Create the values of valMMInt[i], which is a matrix of size
        nDOFs2XnInt stored in row major order. */
     unsigned int ll = 0;
-    for(unsigned short k=0; k<nDOFs; ++k)
-      for(unsigned short j=0; j<nDOFs; ++j)
-        for(unsigned short l=0; l<nInt; ++l, ++ll)
-          valMMInt[i][ll] = w[l]*lag[l*nDOFs+k]*lag[l*nDOFs+j];
+    for (unsigned short k = 0; k < nDOFs; ++k)
+      for (unsigned short j = 0; j < nDOFs; ++j)
+        for (unsigned short l = 0; l < nInt; ++l, ++ll)
+          valMMInt[i][ll] = w[l] * lag[l * nDOFs + k] * lag[l * nDOFs + j];
   }
 
   /* Loop over the owned volume elements. */
-  for(unsigned long i=0; i<nVolElemOwned; ++i) {
-
+  for (unsigned long i = 0; i < nVolElemOwned; ++i) {
     /* Easier storage of the index of the corresponding standard element and
        get the necessary information from it. */
-    const unsigned short ind    = volElem[i].indStandardElement;
-    const unsigned short nInt   = standardElementsSol[ind].GetNIntegration();
-    const unsigned short nDOFs  = volElem[i].nDOFsSol;
-    const unsigned int   nDOFs2 = nDOFs*nDOFs;
-    const su2double     *valInt = valMMInt[ind].data();
+    const unsigned short ind = volElem[i].indStandardElement;
+    const unsigned short nInt = standardElementsSol[ind].GetNIntegration();
+    const unsigned short nDOFs = volElem[i].nDOFsSol;
+    const unsigned int nDOFs2 = nDOFs * nDOFs;
+    const su2double* valInt = valMMInt[ind].data();
 
     /* Copy the data of the Jacobian in the integration points in
        a separate vector. */
     vector<su2double> JacVec(nInt);
-    su2double *Jac = JacVec.data();
+    su2double* Jac = JacVec.data();
 
-    for(unsigned short l=0; l<nInt; ++l)
-      Jac[l] = volElem[i].metricTerms[l*nMetricPerPoint];
+    for (unsigned short l = 0; l < nInt; ++l) Jac[l] = volElem[i].metricTerms[l * nMetricPerPoint];
 
     /* Allocate the memory for working vector for the construction
        of the mass matrix. */
@@ -5744,26 +5454,23 @@ void CMeshFEM_DG::MetricTermsVolumeElements(CConfig *config) {
     blasFunctions->gemv(nDOFs2, nInt, valInt, Jac, massMat.data());
 
     /* Store the full mass matrix in volElem[i], if needed. */
-    if( FullMassMatrix ) volElem[i].massMatrix = massMat;
+    if (FullMassMatrix) volElem[i].massMatrix = massMat;
 
     /*--- Check if the lumped mass matrix is needed. ---*/
-    if( LumpedMassMatrix ) {
-
+    if (LumpedMassMatrix) {
       /* Allocate the memory for the lumped mass matrix and initialize them to zero.. */
       volElem[i].lumpedMassMatrix.assign(nDOFs, 0.0);
 
       /* Loop over the DOFs to compute the elements of the local lumped mass
          matrix. It is the sum of the absolute values of the row. */
-      for(unsigned short j=0; j<nDOFs; ++j) {
-        const su2double *val = massMat.data() + j*nDOFs;
-        for(unsigned short k=0; k<nDOFs; ++k)
-          volElem[i].lumpedMassMatrix[j] += fabs(val[k]);
+      for (unsigned short j = 0; j < nDOFs; ++j) {
+        const su2double* val = massMat.data() + j * nDOFs;
+        for (unsigned short k = 0; k < nDOFs; ++k) volElem[i].lumpedMassMatrix[j] += fabs(val[k]);
       }
     }
 
     /*--- Check if the inverse of mass matrix is needed. ---*/
-    if( FullInverseMassMatrix ) {
-
+    if (FullInverseMassMatrix) {
       /*--- Check if LAPACK/MKL can be used to compute the inverse. ---*/
 
 #if (defined(HAVE_MKL) || defined(HAVE_LAPACK)) && !(defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE))
@@ -5773,15 +5480,13 @@ void CMeshFEM_DG::MetricTermsVolumeElements(CConfig *config) {
          Cholesky decomposition is used, which is much more efficient
          than a standard inverse. */
       char uplo = 'L';
-      int  NN = nDOFs, errorCode;
+      int NN = nDOFs, errorCode;
       dpotrf_(&uplo, &NN, massMat.data(), &NN, &errorCode);
-      if(errorCode != 0) {
+      if (errorCode != 0) {
         ostringstream message;
-        if(errorCode < 0)  {
-          message << "Something wrong when calling dpotrf. Error code: "
-                  << errorCode;
-        }
-        else {
+        if (errorCode < 0) {
+          message << "Something wrong when calling dpotrf. Error code: " << errorCode;
+        } else {
           message << "Mass matrix not positive definite. " << endl;
           message << "This is most likely caused by a too low accuracy of the quadrature rule," << endl;
           message << "possibly combined with a low quality element." << endl;
@@ -5792,13 +5497,11 @@ void CMeshFEM_DG::MetricTermsVolumeElements(CConfig *config) {
       }
 
       dpotri_(&uplo, &NN, massMat.data(), &NN, &errorCode);
-      if(errorCode != 0) {
+      if (errorCode != 0) {
         ostringstream message;
-        if(errorCode < 0) {
-          message << "Something wrong when calling dpotri. Error code: "
-                  << errorCode;
-        }
-        else {
+        if (errorCode < 0) {
+          message << "Something wrong when calling dpotri. Error code: " << errorCode;
+        } else {
           message << "Mass matrix is singular. " << endl;
           message << "The is most likely caused by a too low accuracy of the quadrature rule, " << endl;
           message << "possibly combined with a low quality element." << endl;
@@ -5810,9 +5513,9 @@ void CMeshFEM_DG::MetricTermsVolumeElements(CConfig *config) {
 
       /* The Lapack routines for a Cholesky decomposition only store the upper
          part of the matrix. Copy the data to the lower part. */
-      for(unsigned short k=0; k<nDOFs; ++k) {
-        for(unsigned short j=(k+1); j<nDOFs; ++j) {
-          massMat[j*nDOFs+k] = massMat[k*nDOFs+j];
+      for (unsigned short k = 0; k < nDOFs; ++k) {
+        for (unsigned short j = (k + 1); j < nDOFs; ++j) {
+          massMat[j * nDOFs + k] = massMat[k * nDOFs + j];
         }
       }
 #else
@@ -5826,8 +5529,7 @@ void CMeshFEM_DG::MetricTermsVolumeElements(CConfig *config) {
   }
 }
 
-void CMeshFEM_DG::TimeCoefficientsPredictorADER_DG(CConfig *config) {
-
+void CMeshFEM_DG::TimeCoefficientsPredictorADER_DG(CConfig* config) {
   /*--------------------------------------------------------------------------*/
   /*--- Determine the coefficients that appear in the iteration matrix of  ---*/
   /*--- the prediction step of ADER-DG.                                    ---*/
@@ -5836,13 +5538,13 @@ void CMeshFEM_DG::TimeCoefficientsPredictorADER_DG(CConfig *config) {
   /* Determine the number of time DOFs in the predictor step of ADER as well
      as their location on the interval [-1..1]. */
   const unsigned short nTimeDOFs = config->GetnTimeDOFsADER_DG();
-  const su2double      *TimeDOFs = config->GetTimeDOFsADER_DG();
+  const su2double* TimeDOFs = config->GetTimeDOFsADER_DG();
 
   /* Compute the Vandermonde matrix and its inverse in the time DOFs. */
   vector<su2double> rTimeDOFs(nTimeDOFs);
-  for(unsigned short i=0; i<nTimeDOFs; ++i) rTimeDOFs[i] = TimeDOFs[i];
+  for (unsigned short i = 0; i < nTimeDOFs; ++i) rTimeDOFs[i] = TimeDOFs[i];
 
-  vector<su2double> V(nTimeDOFs*nTimeDOFs);
+  vector<su2double> V(nTimeDOFs * nTimeDOFs);
   CFEMStandardElementBase timeElement;
   timeElement.Vandermonde1D(nTimeDOFs, rTimeDOFs, V);
 
@@ -5850,75 +5552,71 @@ void CMeshFEM_DG::TimeCoefficientsPredictorADER_DG(CConfig *config) {
   timeElement.InverseMatrix(nTimeDOFs, VInv);
 
   /* Compute the Vandermonde matrix for r = 1, i.e. the end of the interval. */
-  vector<su2double> rEnd(1); rEnd[0] = 1.0;
+  vector<su2double> rEnd(1);
+  rEnd[0] = 1.0;
   vector<su2double> VEnd(nTimeDOFs);
   timeElement.Vandermonde1D(nTimeDOFs, rEnd, VEnd);
 
   /*--- Determine the matrix products VEnd*VInv to get the correct expression
         for the values of the Lagrangian interpolation functions for r = 1. ---*/
   vector<su2double> lEnd(nTimeDOFs, 0.0);
-  for(unsigned short j=0; j<nTimeDOFs; ++j) {
-    for(unsigned short k=0; k<nTimeDOFs; ++k)
-      lEnd[j] += VEnd[k]*VInv[j*nTimeDOFs+k];
+  for (unsigned short j = 0; j < nTimeDOFs; ++j) {
+    for (unsigned short k = 0; k < nTimeDOFs; ++k) lEnd[j] += VEnd[k] * VInv[j * nTimeDOFs + k];
   }
 
   /*--- To reduce the error due to round off, make sure that the row sum is 1.
         Also check if the difference is not too large to be solely caused by
         roundoff.  ---*/
   su2double val = 0.0;
-  for(unsigned short j=0; j<nTimeDOFs; ++j) val += lEnd[j];
+  for (unsigned short j = 0; j < nTimeDOFs; ++j) val += lEnd[j];
 
-  if(fabs(val-1.0) > 1.e-6)
-    SU2_MPI::Error( "Difference is too large to be caused by roundoff", CURRENT_FUNCTION);
+  if (fabs(val - 1.0) > 1.e-6) SU2_MPI::Error("Difference is too large to be caused by roundoff", CURRENT_FUNCTION);
 
-  val = 1.0/val;
-  for(unsigned short j=0; j<nTimeDOFs; ++j) lEnd[j] *= val;
+  val = 1.0 / val;
+  for (unsigned short j = 0; j < nTimeDOFs; ++j) lEnd[j] *= val;
 
   /*--- Compute the mass matrix in time, which is the inverse of V^T V. Note that
         this definition is different from the one used in Hesthaven, because their
         V is our V^T. Furthermore note that the mass matrix should be a diagonal
         matrix, due to the choice of the DOFs (Gauss Legendre points). ---*/
-  vector<su2double> MassTime(nTimeDOFs*nTimeDOFs, 0.0);
-  for(unsigned short j=0; j<nTimeDOFs; ++j) {
-    for(unsigned short i=0; i<nTimeDOFs; ++i) {
-      const unsigned short ji = j*nTimeDOFs + i;
-      for(unsigned short k=0; k<nTimeDOFs; ++k)
-        MassTime[ji] += V[k*nTimeDOFs+j]*V[k*nTimeDOFs+i];
+  vector<su2double> MassTime(nTimeDOFs * nTimeDOFs, 0.0);
+  for (unsigned short j = 0; j < nTimeDOFs; ++j) {
+    for (unsigned short i = 0; i < nTimeDOFs; ++i) {
+      const unsigned short ji = j * nTimeDOFs + i;
+      for (unsigned short k = 0; k < nTimeDOFs; ++k) MassTime[ji] += V[k * nTimeDOFs + j] * V[k * nTimeDOFs + i];
     }
   }
 
   timeElement.InverseMatrix(nTimeDOFs, MassTime);
 
   /* Compute the gradient of the Vandermonde matrix in the time DOFs. */
-  vector<su2double> VDr(nTimeDOFs*nTimeDOFs);
+  vector<su2double> VDr(nTimeDOFs * nTimeDOFs);
   timeElement.GradVandermonde1D(nTimeDOFs, rTimeDOFs, VDr);
 
   /* Compute the product VDr VInv. Store the result in V. Note that in both
      matrices the transpose is stored compared to the definition of Hesthaven. */
-  for(unsigned short j=0; j<nTimeDOFs; ++j) {
-    for(unsigned short i=0; i<nTimeDOFs; ++i) {
-      const unsigned short ji = j*nTimeDOFs + i;
+  for (unsigned short j = 0; j < nTimeDOFs; ++j) {
+    for (unsigned short i = 0; i < nTimeDOFs; ++i) {
+      const unsigned short ji = j * nTimeDOFs + i;
       V[ji] = 0.0;
-      for(unsigned short k=0; k<nTimeDOFs; ++k)
-        V[ji] += VDr[k*nTimeDOFs+j]*VInv[i*nTimeDOFs+k];
+      for (unsigned short k = 0; k < nTimeDOFs; ++k) V[ji] += VDr[k * nTimeDOFs + j] * VInv[i * nTimeDOFs + k];
     }
   }
 
   /* Compute the time stiffness matrix S = M Dr. */
-  vector<su2double> S(nTimeDOFs*nTimeDOFs, 0.0);
-  for(unsigned short j=0; j<nTimeDOFs; ++j) {
-    for(unsigned short i=0; i<nTimeDOFs; ++i) {
-      const unsigned short ji = j*nTimeDOFs + i;
-      for(unsigned short k=0; k<nTimeDOFs; ++k)
-        S[ji] += MassTime[j*nTimeDOFs+k]*V[k*nTimeDOFs+i];
+  vector<su2double> S(nTimeDOFs * nTimeDOFs, 0.0);
+  for (unsigned short j = 0; j < nTimeDOFs; ++j) {
+    for (unsigned short i = 0; i < nTimeDOFs; ++i) {
+      const unsigned short ji = j * nTimeDOFs + i;
+      for (unsigned short k = 0; k < nTimeDOFs; ++k) S[ji] += MassTime[j * nTimeDOFs + k] * V[k * nTimeDOFs + i];
     }
   }
 
   /* Compute the time coefficients of the iteration matrix in the predictor step. */
-  timeCoefADER_DG.assign(nTimeDOFs*nTimeDOFs, 0.0);
-  for(unsigned short j=0; j<nTimeDOFs; ++j) {
-    for(unsigned short i=0; i<nTimeDOFs; ++i)
-      timeCoefADER_DG[j*nTimeDOFs+i] = lEnd[j]*lEnd[i] - S[i*nTimeDOFs+j];
+  timeCoefADER_DG.assign(nTimeDOFs * nTimeDOFs, 0.0);
+  for (unsigned short j = 0; j < nTimeDOFs; ++j) {
+    for (unsigned short i = 0; i < nTimeDOFs; ++i)
+      timeCoefADER_DG[j * nTimeDOFs + i] = lEnd[j] * lEnd[i] - S[i * nTimeDOFs + j];
   }
 
   /* Determine the inverse of timeCoefADER_DG, because this is needed in the
@@ -5934,34 +5632,33 @@ void CMeshFEM_DG::TimeCoefficientsPredictorADER_DG(CConfig *config) {
 
   /* Determine the number of time integration points of ADER as well
      as their location on the interval [-1..1]. */
-  unsigned short  nTimeIntegrationPoints = config->GetnTimeIntegrationADER_DG();
-  const su2double *TimeIntegrationPoints = config->GetTimeIntegrationADER_DG();
+  unsigned short nTimeIntegrationPoints = config->GetnTimeIntegrationADER_DG();
+  const su2double* TimeIntegrationPoints = config->GetTimeIntegrationADER_DG();
 
   /* Compute the Vandermonde matrix for the time integration points. */
   vector<su2double> rTimeIntPoints(nTimeIntegrationPoints);
-  for(unsigned short i=0; i<nTimeIntegrationPoints; ++i)
-    rTimeIntPoints[i] = TimeIntegrationPoints[i];
+  for (unsigned short i = 0; i < nTimeIntegrationPoints; ++i) rTimeIntPoints[i] = TimeIntegrationPoints[i];
 
-  V.resize(nTimeIntegrationPoints*nTimeDOFs);
+  V.resize(nTimeIntegrationPoints * nTimeDOFs);
   timeElement.Vandermonde1D(nTimeDOFs, rTimeIntPoints, V);
 
   /* Allocate the memory for the time interpolation coefficients and initialize
      them to zero. */
-  timeInterpolDOFToIntegrationADER_DG.assign(nTimeIntegrationPoints*nTimeDOFs, 0.0);
+  timeInterpolDOFToIntegrationADER_DG.assign(nTimeIntegrationPoints * nTimeDOFs, 0.0);
 
   /* Determine the matrix products V*VInv to get the correct expression for
      mTimeInterpolDOFToIntegration. Note that from mathematical point of view the
      transpose of V*VInv is stored, because in this way the interpolation data
      for a time integration point is contiguous in memory. */
-  for(unsigned short j=0; j<nTimeDOFs; ++j) {
-    for(unsigned short i=0; i<nTimeIntegrationPoints; ++i) {
-      const unsigned short ii = i*nTimeDOFs + j;
+  for (unsigned short j = 0; j < nTimeDOFs; ++j) {
+    for (unsigned short i = 0; i < nTimeIntegrationPoints; ++i) {
+      const unsigned short ii = i * nTimeDOFs + j;
 
-      for(unsigned short k=0; k<nTimeDOFs; ++k) {
-        const unsigned short indV    = k*nTimeIntegrationPoints + i;
-        const unsigned short indVInv = j*nTimeDOFs + k;
+      for (unsigned short k = 0; k < nTimeDOFs; ++k) {
+        const unsigned short indV = k * nTimeIntegrationPoints + i;
+        const unsigned short indVInv = j * nTimeDOFs + k;
 
-        timeInterpolDOFToIntegrationADER_DG[ii] += V[indV]*VInv[indVInv];
+        timeInterpolDOFToIntegrationADER_DG[ii] += V[indV] * VInv[indVInv];
       }
     }
   }
@@ -5969,19 +5666,16 @@ void CMeshFEM_DG::TimeCoefficientsPredictorADER_DG(CConfig *config) {
   /*--- To reduce the error due to round off, make sure that the row sum is 1.
         Also check if the difference is not too large to be solely caused by
         roundoff.  ---*/
-  for(unsigned short j=0; j<nTimeIntegrationPoints; ++j) {
-    const unsigned short jj = j*nTimeDOFs;
+  for (unsigned short j = 0; j < nTimeIntegrationPoints; ++j) {
+    const unsigned short jj = j * nTimeDOFs;
 
     val = 0.0;
-    for(unsigned short i=0; i<nTimeDOFs; ++i)
-      val += timeInterpolDOFToIntegrationADER_DG[jj+i];
+    for (unsigned short i = 0; i < nTimeDOFs; ++i) val += timeInterpolDOFToIntegrationADER_DG[jj + i];
 
-    if(fabs(val-1.0) > 1.e-6)
-      SU2_MPI::Error( "Difference is too large to be caused by roundoff", CURRENT_FUNCTION);
+    if (fabs(val - 1.0) > 1.e-6) SU2_MPI::Error("Difference is too large to be caused by roundoff", CURRENT_FUNCTION);
 
-    val = 1.0/val;
-    for(unsigned short i=0; i<nTimeDOFs; ++i)
-      timeInterpolDOFToIntegrationADER_DG[jj+i] *= val;
+    val = 1.0 / val;
+    for (unsigned short i = 0; i < nTimeDOFs; ++i) timeInterpolDOFToIntegrationADER_DG[jj + i] *= val;
   }
 
   /*--------------------------------------------------------------------------*/
@@ -5996,38 +5690,38 @@ void CMeshFEM_DG::TimeCoefficientsPredictorADER_DG(CConfig *config) {
      hence the number of integration points double and the position is
      determined via the transformation xxi = 0.5(xi-1) and xi varies between
      -1 and 3. */
-  rTimeIntPoints.resize(2*nTimeIntegrationPoints);
-  for(unsigned short i=0; i<nTimeIntegrationPoints; ++i)
-    rTimeIntPoints[i] = 0.5*(TimeIntegrationPoints[i]-1.0);
+  rTimeIntPoints.resize(2 * nTimeIntegrationPoints);
+  for (unsigned short i = 0; i < nTimeIntegrationPoints; ++i)
+    rTimeIntPoints[i] = 0.5 * (TimeIntegrationPoints[i] - 1.0);
 
-  for(unsigned short i=0; i<nTimeIntegrationPoints; ++i) {
+  for (unsigned short i = 0; i < nTimeIntegrationPoints; ++i) {
     const unsigned short ii = i + nTimeIntegrationPoints;
-    rTimeIntPoints[ii] = 0.5*(TimeIntegrationPoints[i]+1.0);
+    rTimeIntPoints[ii] = 0.5 * (TimeIntegrationPoints[i] + 1.0);
   }
 
   nTimeIntegrationPoints *= 2;
 
   /* Compute the Vandermonde matrix for these time integration points. */
-  V.resize(nTimeIntegrationPoints*nTimeDOFs);
+  V.resize(nTimeIntegrationPoints * nTimeDOFs);
   timeElement.Vandermonde1D(nTimeDOFs, rTimeIntPoints, V);
 
   /* Allocate the memory for the time interpolation coefficients and initialize
      them to zero. */
-  timeInterpolAdjDOFToIntegrationADER_DG.assign(nTimeIntegrationPoints*nTimeDOFs, 0.0);
+  timeInterpolAdjDOFToIntegrationADER_DG.assign(nTimeIntegrationPoints * nTimeDOFs, 0.0);
 
   /* Determine the matrix products V*VInv to get the correct expression for
      mTimeInterpolAdjDOFToIntegration. Note that from mathematical point of view
      the transpose of V*VInv is stored, because in this way the interpolation
      data for a time integration point is contiguous in memory. */
-  for(unsigned short j=0; j<nTimeDOFs; ++j) {
-    for(unsigned short i=0; i<nTimeIntegrationPoints; ++i) {
-      const unsigned short ii = i*nTimeDOFs + j;
+  for (unsigned short j = 0; j < nTimeDOFs; ++j) {
+    for (unsigned short i = 0; i < nTimeIntegrationPoints; ++i) {
+      const unsigned short ii = i * nTimeDOFs + j;
 
-      for(unsigned short k=0; k<nTimeDOFs; ++k) {
-        const unsigned short indV    = k*nTimeIntegrationPoints + i;
-        const unsigned short indVInv = j*nTimeDOFs + k;
+      for (unsigned short k = 0; k < nTimeDOFs; ++k) {
+        const unsigned short indV = k * nTimeIntegrationPoints + i;
+        const unsigned short indVInv = j * nTimeDOFs + k;
 
-        timeInterpolAdjDOFToIntegrationADER_DG[ii] += V[indV]*VInv[indVInv];
+        timeInterpolAdjDOFToIntegrationADER_DG[ii] += V[indV] * VInv[indVInv];
       }
     }
   }
@@ -6035,47 +5729,41 @@ void CMeshFEM_DG::TimeCoefficientsPredictorADER_DG(CConfig *config) {
   /*--- To reduce the error due to round off, make sure that the row sum is 1.
         Also check if the difference is not too large to be solely caused by
         roundoff.  ---*/
-  for(unsigned short j=0; j<nTimeIntegrationPoints; ++j) {
-    const unsigned short jj = j*nTimeDOFs;
+  for (unsigned short j = 0; j < nTimeIntegrationPoints; ++j) {
+    const unsigned short jj = j * nTimeDOFs;
 
     val = 0.0;
-    for(unsigned short i=0; i<nTimeDOFs; ++i)
-      val += timeInterpolAdjDOFToIntegrationADER_DG[jj+i];
+    for (unsigned short i = 0; i < nTimeDOFs; ++i) val += timeInterpolAdjDOFToIntegrationADER_DG[jj + i];
 
-    if(fabs(val-1.0) > 1.e-6)
-      SU2_MPI::Error( "Difference is too large to be caused by roundoff", CURRENT_FUNCTION);
+    if (fabs(val - 1.0) > 1.e-6) SU2_MPI::Error("Difference is too large to be caused by roundoff", CURRENT_FUNCTION);
 
-    val = 1.0/val;
-    for(unsigned short i=0; i<nTimeDOFs; ++i)
-      timeInterpolAdjDOFToIntegrationADER_DG[jj+i] *= val;
+    val = 1.0 / val;
+    for (unsigned short i = 0; i < nTimeDOFs; ++i) timeInterpolAdjDOFToIntegrationADER_DG[jj + i] *= val;
   }
 }
 
-void CMeshFEM_DG::VolumeMetricTermsFromCoorGradients(
-                                       const unsigned short nEntities,
-                                       const su2double      *gradCoor,
-                                       vector<su2double>    &metricTerms) {
-
+void CMeshFEM_DG::VolumeMetricTermsFromCoorGradients(const unsigned short nEntities, const su2double* gradCoor,
+                                                     vector<su2double>& metricTerms) {
   /*--- Convert the dxdr, dydr, etc., stored in coorGradients, to the
         required metric terms. Make a distinction between 2D and 3D. ---*/
-  switch( nDim ) {
+  switch (nDim) {
     case 2: {
-
       /* 2D computation. Store the offset between the r and s derivatives. */
-      const unsigned short off = 2*nEntities;
+      const unsigned short off = 2 * nEntities;
 
       /* Loop over the entities and store the metric terms. */
       unsigned short ii = 0;
-      for(unsigned short j=0; j<nEntities; ++j) {
-        const unsigned short jx = 2*j; const unsigned short jy = jx+1;
-        const su2double dxdr = gradCoor[jx],     dydr = gradCoor[jy];
-        const su2double dxds = gradCoor[jx+off], dyds = gradCoor[jy+off];
-
-        metricTerms[ii++] =  dxdr*dyds - dxds*dydr; // J
-        metricTerms[ii++] =  dyds;   // J drdx
-        metricTerms[ii++] = -dxds;   // J drdy
-        metricTerms[ii++] = -dydr;   // J dsdx
-        metricTerms[ii++] =  dxdr;   // J dsdy
+      for (unsigned short j = 0; j < nEntities; ++j) {
+        const unsigned short jx = 2 * j;
+        const unsigned short jy = jx + 1;
+        const su2double dxdr = gradCoor[jx], dydr = gradCoor[jy];
+        const su2double dxds = gradCoor[jx + off], dyds = gradCoor[jy + off];
+
+        metricTerms[ii++] = dxdr * dyds - dxds * dydr;  // J
+        metricTerms[ii++] = dyds;                       // J drdx
+        metricTerms[ii++] = -dxds;                      // J drdy
+        metricTerms[ii++] = -dydr;                      // J dsdx
+        metricTerms[ii++] = dxdr;                       // J dsdy
       }
 
       break;
@@ -6083,31 +5771,31 @@ void CMeshFEM_DG::VolumeMetricTermsFromCoorGradients(
 
     case 3: {
       /* 3D computation. Store the offset between the r and s and r and t derivatives. */
-      unsigned short offS = 3*nEntities, offT = 6*nEntities;
+      unsigned short offS = 3 * nEntities, offT = 6 * nEntities;
 
       /* Loop over the entities and store the metric terms. */
       unsigned short ii = 0;
-      for(unsigned short j=0; j<nEntities; ++j) {
-        const unsigned short jx = 3*j; const unsigned short jy = jx+1, jz = jx+2;
-        const su2double dxdr = gradCoor[jx],      dydr = gradCoor[jy],      dzdr = gradCoor[jz];
-        const su2double dxds = gradCoor[jx+offS], dyds = gradCoor[jy+offS], dzds = gradCoor[jz+offS];
-        const su2double dxdt = gradCoor[jx+offT], dydt = gradCoor[jy+offT], dzdt = gradCoor[jz+offT];
-
-        metricTerms[ii++] = dxdr*(dyds*dzdt - dzds*dydt)
-                          - dxds*(dydr*dzdt - dzdr*dydt)
-                          + dxdt*(dydr*dzds - dzdr*dyds); // J
-
-        metricTerms[ii++] = dyds*dzdt - dzds*dydt;  // J drdx
-        metricTerms[ii++] = dzds*dxdt - dxds*dzdt;  // J drdy
-        metricTerms[ii++] = dxds*dydt - dyds*dxdt;  // J drdz
-
-        metricTerms[ii++] = dzdr*dydt - dydr*dzdt;  // J dsdx
-        metricTerms[ii++] = dxdr*dzdt - dzdr*dxdt;  // J dsdy
-        metricTerms[ii++] = dydr*dxdt - dxdr*dydt;  // J dsdz
-
-        metricTerms[ii++] = dydr*dzds - dzdr*dyds;  // J dtdx
-        metricTerms[ii++] = dzdr*dxds - dxdr*dzds;  // J dtdy
-        metricTerms[ii++] = dxdr*dyds - dydr*dxds;  // J dtdz
+      for (unsigned short j = 0; j < nEntities; ++j) {
+        const unsigned short jx = 3 * j;
+        const unsigned short jy = jx + 1, jz = jx + 2;
+        const su2double dxdr = gradCoor[jx], dydr = gradCoor[jy], dzdr = gradCoor[jz];
+        const su2double dxds = gradCoor[jx + offS], dyds = gradCoor[jy + offS], dzds = gradCoor[jz + offS];
+        const su2double dxdt = gradCoor[jx + offT], dydt = gradCoor[jy + offT], dzdt = gradCoor[jz + offT];
+
+        metricTerms[ii++] = dxdr * (dyds * dzdt - dzds * dydt) - dxds * (dydr * dzdt - dzdr * dydt) +
+                            dxdt * (dydr * dzds - dzdr * dyds);  // J
+
+        metricTerms[ii++] = dyds * dzdt - dzds * dydt;  // J drdx
+        metricTerms[ii++] = dzds * dxdt - dxds * dzdt;  // J drdy
+        metricTerms[ii++] = dxds * dydt - dyds * dxdt;  // J drdz
+
+        metricTerms[ii++] = dzdr * dydt - dydr * dzdt;  // J dsdx
+        metricTerms[ii++] = dxdr * dzdt - dzdr * dxdt;  // J dsdy
+        metricTerms[ii++] = dydr * dxdt - dxdr * dydt;  // J dsdz
+
+        metricTerms[ii++] = dydr * dzds - dzdr * dyds;  // J dtdx
+        metricTerms[ii++] = dzdr * dxds - dxdr * dzds;  // J dtdy
+        metricTerms[ii++] = dxdr * dyds - dydr * dxds;  // J dtdz
       }
 
       break;
@@ -6115,31 +5803,28 @@ void CMeshFEM_DG::VolumeMetricTermsFromCoorGradients(
   }
 }
 
-void CMeshFEM_DG::WallFunctionPreprocessing(CConfig *config) {
-
+void CMeshFEM_DG::WallFunctionPreprocessing(CConfig* config) {
   /*--------------------------------------------------------------------------*/
   /*--- Step 1: Check whether wall functions are used at all.              ---*/
   /*--------------------------------------------------------------------------*/
 
   bool wallFunctions = false;
-  for(unsigned short iMarker=0; iMarker<nMarker; ++iMarker) {
-
+  for (unsigned short iMarker = 0; iMarker < nMarker; ++iMarker) {
     switch (config->GetMarker_All_KindBC(iMarker)) {
       case ISOTHERMAL:
       case HEAT_FLUX: {
         const string Marker_Tag = config->GetMarker_All_TagBound(iMarker);
-        if(config->GetWallFunction_Treatment(Marker_Tag) != WALL_FUNCTIONS::NONE)
-          wallFunctions = true;
+        if (config->GetWallFunction_Treatment(Marker_Tag) != WALL_FUNCTIONS::NONE) wallFunctions = true;
         break;
       }
-      default:  /* Just to avoid a compiler warning. */
+      default: /* Just to avoid a compiler warning. */
         break;
     }
   }
 
   /* If no wall functions are used, nothing needs to be done and a
      return can be made. */
-  if( !wallFunctions ) return;
+  if (!wallFunctions) return;
 
   /*--------------------------------------------------------------------------*/
   /*--- Step 2. Build the local ADT of the volume elements. The halo       ---*/
@@ -6153,66 +5838,61 @@ void CMeshFEM_DG::WallFunctionPreprocessing(CConfig *config) {
   /* Define the vectors, which store the mapping from the subelement to the
      parent element, subelement ID within the parent element, the element
      type and the connectivity of the subelements. */
-  vector<unsigned long>  parentElement;
+  vector<unsigned long> parentElement;
   vector<unsigned short> subElementIDInParent;
   vector<unsigned short> VTK_TypeElem;
-  vector<unsigned long>  elemConn;
+  vector<unsigned long> elemConn;
 
   /* Loop over the locally stored volume elements (including halo elements)
      to create the connectivity of the subelements. */
-  for(unsigned long l=0; l<nVolElemTot; ++l) {
-
+  for (unsigned long l = 0; l < nVolElemTot; ++l) {
     /* Determine the necessary data from the corresponding standard element. */
     const unsigned short ind = volElem[l].indStandardElement;
 
-    unsigned short VTK_Type[]  = {standardElementsGrid[ind].GetVTK_Type1(),
-                                  standardElementsGrid[ind].GetVTK_Type2()};
+    unsigned short VTK_Type[] = {standardElementsGrid[ind].GetVTK_Type1(), standardElementsGrid[ind].GetVTK_Type2()};
     unsigned short nSubElems[] = {0, 0};
     unsigned short nDOFsPerSubElem[] = {0, 0};
-    const unsigned short *connSubElems[] = {nullptr, nullptr};
+    const unsigned short* connSubElems[] = {nullptr, nullptr};
 
-    if(VTK_Type[0] != NONE) {
-      nSubElems[0]       = standardElementsGrid[ind].GetNSubElemsType1();
+    if (VTK_Type[0] != NONE) {
+      nSubElems[0] = standardElementsGrid[ind].GetNSubElemsType1();
       nDOFsPerSubElem[0] = standardElementsGrid[ind].GetNDOFsPerSubElem(VTK_Type[0]);
-      connSubElems[0]    = standardElementsGrid[ind].GetSubConnType1();
+      connSubElems[0] = standardElementsGrid[ind].GetSubConnType1();
     }
 
-    if(VTK_Type[1] != NONE) {
-      nSubElems[1]       = standardElementsGrid[ind].GetNSubElemsType2();
+    if (VTK_Type[1] != NONE) {
+      nSubElems[1] = standardElementsGrid[ind].GetNSubElemsType2();
       nDOFsPerSubElem[1] = standardElementsGrid[ind].GetNDOFsPerSubElem(VTK_Type[1]);
-      connSubElems[1]    = standardElementsGrid[ind].GetSubConnType2();
+      connSubElems[1] = standardElementsGrid[ind].GetSubConnType2();
     }
 
     /* Abbreviate the grid DOFs of this element a bit easier. */
-    const unsigned long *DOFs = volElem[l].nodeIDsGrid.data();
+    const unsigned long* DOFs = volElem[l].nodeIDsGrid.data();
 
     /* Loop over the number of subelements and store the required data. */
     unsigned short jj = 0;
-    for(unsigned short i=0; i<2; ++i) {
+    for (unsigned short i = 0; i < 2; ++i) {
       unsigned short kk = 0;
-      for(unsigned short j=0; j<nSubElems[i]; ++j, ++jj) {
+      for (unsigned short j = 0; j < nSubElems[i]; ++j, ++jj) {
         parentElement.push_back(l);
         subElementIDInParent.push_back(jj);
         VTK_TypeElem.push_back(VTK_Type[i]);
 
-        for(unsigned short k=0; k<nDOFsPerSubElem[i]; ++k, ++kk)
-          elemConn.push_back(DOFs[connSubElems[i][kk]]);
+        for (unsigned short k = 0; k < nDOFsPerSubElem[i]; ++k, ++kk) elemConn.push_back(DOFs[connSubElems[i][kk]]);
       }
     }
   }
 
   /* Copy the coordinates in a vector that can be used by the ADT. */
   vector<su2double> volCoor;
-  volCoor.reserve(nDim*meshPoints.size());
+  volCoor.reserve(nDim * meshPoints.size());
 
-  for(unsigned long l=0; l<meshPoints.size(); ++l) {
-    for(unsigned short k=0; k<nDim; ++k)
-      volCoor.push_back(meshPoints[l].coor[k]);
+  for (unsigned long l = 0; l < meshPoints.size(); ++l) {
+    for (unsigned short k = 0; k < nDim; ++k) volCoor.push_back(meshPoints[l].coor[k]);
   }
 
   /* Build the local ADT. */
-  CADTElemClass localVolumeADT(nDim, volCoor, elemConn, VTK_TypeElem,
-                               subElementIDInParent, parentElement, false);
+  CADTElemClass localVolumeADT(nDim, volCoor, elemConn, VTK_TypeElem, subElementIDInParent, parentElement, false);
 
   /* Release the memory of the vectors used to build the ADT. To make sure
      that all the memory is deleted, the swap function is used. */
@@ -6229,27 +5909,25 @@ void CMeshFEM_DG::WallFunctionPreprocessing(CConfig *config) {
 
   /* Loop over the markers and select the ones for which a wall function
      treatment must be carried out. */
-  for(unsigned short iMarker=0; iMarker<nMarker; ++iMarker) {
-
+  for (unsigned short iMarker = 0; iMarker < nMarker; ++iMarker) {
     switch (config->GetMarker_All_KindBC(iMarker)) {
       case ISOTHERMAL:
       case HEAT_FLUX: {
         const string Marker_Tag = config->GetMarker_All_TagBound(iMarker);
-        if(config->GetWallFunction_Treatment(Marker_Tag) != WALL_FUNCTIONS::NONE) {
-
+        if (config->GetWallFunction_Treatment(Marker_Tag) != WALL_FUNCTIONS::NONE) {
           /* An LES wall model is used for this boundary marker. Determine
              which wall model and allocate the memory for the member variable. */
-          switch (config->GetWallFunction_Treatment(Marker_Tag) ) {
+          switch (config->GetWallFunction_Treatment(Marker_Tag)) {
             case WALL_FUNCTIONS::EQUILIBRIUM_MODEL: {
-              if(rank == MASTER_NODE)
-                cout << "Marker " << Marker_Tag << " uses an Equilibrium Wall Model." << endl;
+              if (rank == MASTER_NODE) cout << "Marker " << Marker_Tag << " uses an Equilibrium Wall Model." << endl;
 
               boundaries[iMarker].wallModel = new CWallModel1DEQ(config, Marker_Tag);
               break;
             }
             case WALL_FUNCTIONS::LOGARITHMIC_MODEL: {
-              if(rank == MASTER_NODE)
-                cout << "Marker " << Marker_Tag << " uses the Reichardt and Kader analytical laws for the Wall Model." << endl;
+              if (rank == MASTER_NODE)
+                cout << "Marker " << Marker_Tag << " uses the Reichardt and Kader analytical laws for the Wall Model."
+                     << endl;
 
               boundaries[iMarker].wallModel = new CWallModelLogLaw(config, Marker_Tag);
               break;
@@ -6261,68 +5939,57 @@ void CMeshFEM_DG::WallFunctionPreprocessing(CConfig *config) {
 
           /* Retrieve the double information for this wall model. The height
              of the exchange location is the first element of this array. */
-          const su2double *doubleInfo = config->GetWallFunction_DoubleInfo(Marker_Tag);
+          const su2double* doubleInfo = config->GetWallFunction_DoubleInfo(Marker_Tag);
 
           /* Easier storage of the surface elements and loop over them. */
-          vector<CSurfaceElementFEM> &surfElem = boundaries[iMarker].surfElem;
-          for(unsigned long l=0; l<surfElem.size(); ++l) {
-
+          vector<CSurfaceElementFEM>& surfElem = boundaries[iMarker].surfElem;
+          for (unsigned long l = 0; l < surfElem.size(); ++l) {
             /* Determine the corresponding standard face element and get the
                relevant information from it. Note that the standard element
                of the solution must be taken and not of the grid. */
-            const unsigned short ind  = surfElem[l].indStandardElement;
+            const unsigned short ind = surfElem[l].indStandardElement;
             const unsigned short nInt = standardBoundaryFacesSol[ind].GetNIntegration();
 
             /* Allocate the memory for the memory to store the donors and
                the parametric weights. The donor elements are stored in an
                CUnsignedLong2T, such that they can be sorted. */
             vector<CUnsignedLong2T> donorElements(nInt);
-            vector<su2double>       parCoorInDonor(nInt*nDim);
+            vector<su2double> parCoorInDonor(nInt * nDim);
 
             /* Loop over the integration points. */
-            for(unsigned short i=0; i<nInt; ++i) {
-
+            for (unsigned short i = 0; i < nInt; ++i) {
               /* Easier storage of the normals and coordinates of this
                  integration point. */
-              const su2double *normals = surfElem[l].metricNormalsFace.data()
-                                       + i*(nDim+1);
-              const su2double *Coord   = surfElem[l].coorIntegrationPoints.data()
-                                       + i*nDim;
+              const su2double* normals = surfElem[l].metricNormalsFace.data() + i * (nDim + 1);
+              const su2double* Coord = surfElem[l].coorIntegrationPoints.data() + i * nDim;
 
               /* Determine the coordinates of the exchange location. Note that the normals
                  point out of the domain, so the normals must be subtracted. */
               su2double coorExchange[] = {0.0, 0.0, 0.0};  // To avoid a compiler warning.
-              for(unsigned short iDim=0; iDim<nDim; ++iDim)
-                coorExchange[iDim] = Coord[iDim] - doubleInfo[0]*normals[iDim];
+              for (unsigned short iDim = 0; iDim < nDim; ++iDim)
+                coorExchange[iDim] = Coord[iDim] - doubleInfo[0] * normals[iDim];
 
               /* Search for the element, which contains the exchange location. */
               unsigned short subElem;
-              unsigned long  parElem;
-              int            rank;
-              su2double      parCoor[3], weightsInterpol[8];
-              if( localVolumeADT.DetermineContainingElement(coorExchange, subElem,
-                                                            parElem, rank, parCoor,
-                                                            weightsInterpol) ) {
-
+              unsigned long parElem;
+              int rank;
+              su2double parCoor[3], weightsInterpol[8];
+              if (localVolumeADT.DetermineContainingElement(coorExchange, subElem, parElem, rank, parCoor,
+                                                            weightsInterpol)) {
                 /* Subelement found that contains the exchange location. However,
                    what is needed is the location in the high order parent element.
                    Determine this. */
-                HighOrderContainmentSearch(coorExchange, parElem, subElem,
-                                           weightsInterpol, parCoor);
+                HighOrderContainmentSearch(coorExchange, parElem, subElem, weightsInterpol, parCoor);
 
                 /* Store the info in donorElements and parCoorInDonor. */
                 donorElements[i].long0 = parElem;
                 donorElements[i].long1 = i;
-                for(unsigned short iDim=0; iDim<nDim; ++iDim)
-                  parCoorInDonor[nDim*i+iDim] = parCoor[iDim];
-              }
-              else {
-
+                for (unsigned short iDim = 0; iDim < nDim; ++iDim) parCoorInDonor[nDim * i + iDim] = parCoor[iDim];
+              } else {
                 /* No subelement found that contains the exchange location.
                    The partitioning is done such that this should not happen.
                    Print an error message and exit. */
-                SU2_MPI::Error("Exchange location not found in ADT",
-                               CURRENT_FUNCTION);
+                SU2_MPI::Error("Exchange location not found in ADT", CURRENT_FUNCTION);
               }
             }
 
@@ -6336,8 +6003,8 @@ void CMeshFEM_DG::WallFunctionPreprocessing(CConfig *config) {
             surfElem[l].intPerWallFunctionDonor.resize(nInt);
             surfElem[l].intPerWallFunctionDonor[0] = donorElements[0].long1;
 
-            for(unsigned short i=1; i<nInt; ++i) {
-              if(donorElements[i].long0 != surfElem[l].donorsWallFunction.back()) {
+            for (unsigned short i = 1; i < nInt; ++i) {
+              if (donorElements[i].long0 != surfElem[l].donorsWallFunction.back()) {
                 surfElem[l].donorsWallFunction.push_back(donorElements[i].long0);
                 surfElem[l].nIntPerWallFunctionDonor.push_back(i);
               }
@@ -6350,44 +6017,41 @@ void CMeshFEM_DG::WallFunctionPreprocessing(CConfig *config) {
                the boundary conditions for this surface. If needed, set
                haloInfoNeededForBC of the boundary to true. As DonorsWallFunction
                is sorted in increasing order, it suffices to check the last element. */
-            if(surfElem[l].donorsWallFunction.back() >= nVolElemOwned)
-              boundaries[iMarker].haloInfoNeededForBC = true;
+            if (surfElem[l].donorsWallFunction.back() >= nVolElemOwned) boundaries[iMarker].haloInfoNeededForBC = true;
 
             /* Allocate the memory of the first index of the interpolation
                matrices for the donordata. */
             surfElem[l].matWallFunctionDonor.resize(surfElem[l].donorsWallFunction.size());
 
             /* Loop over the different donors for the wall function data. */
-            for(unsigned long j=0; j<surfElem[l].donorsWallFunction.size(); ++j) {
-
+            for (unsigned long j = 0; j < surfElem[l].donorsWallFunction.size(); ++j) {
               /* Easier storage of the donor and the vector for the
                  interpolation data for this donor. */
-              const unsigned long donor   = surfElem[l].donorsWallFunction[j];
-              vector<su2double> &matDonor = surfElem[l].matWallFunctionDonor[j];
+              const unsigned long donor = surfElem[l].donorsWallFunction[j];
+              vector<su2double>& matDonor = surfElem[l].matWallFunctionDonor[j];
 
               /* Determine the number of DOFs in the donor element. Note that
                  the standard element of the solution must be used for this
                  purpose. */
-              const unsigned short ind   = volElem[donor].indStandardElement;
+              const unsigned short ind = volElem[donor].indStandardElement;
               const unsigned short nDOFs = standardElementsSol[ind].GetNDOFs();
 
               /* Allocate the memory for the vector used to compute the
                  Lagrangian interpolation functions in the parametric coordinates,
                  i.e. the interpolation weights, and for matDonor, which stores
                  all these weights. */
-              const unsigned short nIntThisDonor = surfElem[l].nIntPerWallFunctionDonor[j+1]
-                                                 - surfElem[l].nIntPerWallFunctionDonor[j];
+              const unsigned short nIntThisDonor =
+                  surfElem[l].nIntPerWallFunctionDonor[j + 1] - surfElem[l].nIntPerWallFunctionDonor[j];
               vector<su2double> lagBasis(nDOFs);
-              matDonor.reserve(nIntThisDonor*nDOFs);
+              matDonor.reserve(nIntThisDonor * nDOFs);
 
               /* Loop over the integration points for this donor element. */
-              for(unsigned short i=surfElem[l].nIntPerWallFunctionDonor[j];
-                                 i<surfElem[l].nIntPerWallFunctionDonor[j+1]; ++i) {
-
+              for (unsigned short i = surfElem[l].nIntPerWallFunctionDonor[j];
+                   i < surfElem[l].nIntPerWallFunctionDonor[j + 1]; ++i) {
                 /* Determine the pointer to the parametric coordinates of the
                    donor point of this integration point. */
-                const unsigned short ii  = surfElem[l].intPerWallFunctionDonor[i];
-                const su2double *parCoor = parCoorInDonor.data() + ii*nDim;
+                const unsigned short ii = surfElem[l].intPerWallFunctionDonor[i];
+                const su2double* parCoor = parCoorInDonor.data() + ii * nDim;
 
                 /* Determine the interpolation weights for this point and
                    store it in matDonor. */
@@ -6400,22 +6064,19 @@ void CMeshFEM_DG::WallFunctionPreprocessing(CConfig *config) {
 
         break;
       }
-      default:  /* Just to avoid a compiler warning. */
+      default: /* Just to avoid a compiler warning. */
         break;
     }
   }
 }
 
-void CMeshFEM_DG::HighOrderContainmentSearch(const su2double      *coor,
-                                             const unsigned long  parElem,
-                                             const unsigned short subElem,
-                                             const su2double      *weightsSubElem,
-                                             su2double            *parCoor) {
-
+void CMeshFEM_DG::HighOrderContainmentSearch(const su2double* coor, const unsigned long parElem,
+                                             const unsigned short subElem, const su2double* weightsSubElem,
+                                             su2double* parCoor) {
   /* Definition of the maximum number of iterations in the Newton solver
      and the tolerance level. */
   const unsigned short maxIt = 50;
-  const su2double tolNewton  = 1.e-10;
+  const su2double tolNewton = 1.e-10;
 
   /*--------------------------------------------------------------------------*/
   /* Step 1: Create an initial guess for the parametric coordinates from      */
@@ -6428,58 +6089,77 @@ void CMeshFEM_DG::HighOrderContainmentSearch(const su2double      *coor,
   /* Define the variables to store the number of DOFs and the connectivity
      of the sub element in which the given coordinate resides. */
   unsigned short nDOFsPerSubElem = 0;
-  const unsigned short *connSubElems;
+  const unsigned short* connSubElems;
 
   /* Check if the sub element is of the first sub-element type. */
   const unsigned short nSubElemType1 = standardElementsGrid[ind].GetNSubElemsType1();
-  if(subElem < nSubElemType1) {
-
+  if (subElem < nSubElemType1) {
     /* Determine the element type and set nDOFsPerSubElem. */
-    switch( standardElementsGrid[ind].GetVTK_Type1() ) {
-      case TRIANGLE:      nDOFsPerSubElem = 3; break;
-      case QUADRILATERAL: nDOFsPerSubElem = 4; break;
-      case TETRAHEDRON:   nDOFsPerSubElem = 4; break;
-      case PYRAMID:       nDOFsPerSubElem = 5; break;
-      case PRISM:         nDOFsPerSubElem = 6; break;
-      case HEXAHEDRON:    nDOFsPerSubElem = 8; break;
-      default: break; /* Just to avoid a compiler warning. */
+    switch (standardElementsGrid[ind].GetVTK_Type1()) {
+      case TRIANGLE:
+        nDOFsPerSubElem = 3;
+        break;
+      case QUADRILATERAL:
+        nDOFsPerSubElem = 4;
+        break;
+      case TETRAHEDRON:
+        nDOFsPerSubElem = 4;
+        break;
+      case PYRAMID:
+        nDOFsPerSubElem = 5;
+        break;
+      case PRISM:
+        nDOFsPerSubElem = 6;
+        break;
+      case HEXAHEDRON:
+        nDOFsPerSubElem = 8;
+        break;
+      default:
+        break; /* Just to avoid a compiler warning. */
     }
 
     /* Set the connectivity for the correct subelement. */
-    connSubElems = standardElementsGrid[ind].GetSubConnType1()
-                 + subElem*nDOFsPerSubElem;
-  }
-  else {
-
+    connSubElems = standardElementsGrid[ind].GetSubConnType1() + subElem * nDOFsPerSubElem;
+  } else {
     /* The sub-element is of the second sub-element type. Determine the
        element type and set nDOFsPerSubElem. */
-    switch( standardElementsGrid[ind].GetVTK_Type2() ) {
-      case TRIANGLE:      nDOFsPerSubElem = 3; break;
-      case QUADRILATERAL: nDOFsPerSubElem = 4; break;
-      case TETRAHEDRON:   nDOFsPerSubElem = 4; break;
-      case PYRAMID:       nDOFsPerSubElem = 5; break;
-      case PRISM:         nDOFsPerSubElem = 6; break;
-      case HEXAHEDRON:    nDOFsPerSubElem = 8; break;
-      default: break; /* Just to avoid a compiler warning. */
+    switch (standardElementsGrid[ind].GetVTK_Type2()) {
+      case TRIANGLE:
+        nDOFsPerSubElem = 3;
+        break;
+      case QUADRILATERAL:
+        nDOFsPerSubElem = 4;
+        break;
+      case TETRAHEDRON:
+        nDOFsPerSubElem = 4;
+        break;
+      case PYRAMID:
+        nDOFsPerSubElem = 5;
+        break;
+      case PRISM:
+        nDOFsPerSubElem = 6;
+        break;
+      case HEXAHEDRON:
+        nDOFsPerSubElem = 8;
+        break;
+      default:
+        break; /* Just to avoid a compiler warning. */
     }
 
     /* Set the connectivity for the correct subelement. */
-    connSubElems = standardElementsGrid[ind].GetSubConnType2()
-                 + (subElem-nSubElemType1)*nDOFsPerSubElem;
+    connSubElems = standardElementsGrid[ind].GetSubConnType2() + (subElem - nSubElemType1) * nDOFsPerSubElem;
   }
 
   /* Get the parametric coordinates of the DOFs from the standard element. */
-  const vector<su2double> *locDOFs[] = {standardElementsGrid[ind].GetRDOFs(),
-                                        standardElementsGrid[ind].GetSDOFs(),
+  const vector<su2double>* locDOFs[] = {standardElementsGrid[ind].GetRDOFs(), standardElementsGrid[ind].GetSDOFs(),
                                         standardElementsGrid[ind].GetTDOFs()};
 
   /* Create the initial guess of the parametric coordinates by interpolation
      in the sub-element. */
-  for(unsigned short iDim=0; iDim<nDim; ++iDim) {
+  for (unsigned short iDim = 0; iDim < nDim; ++iDim) {
     parCoor[iDim] = 0.0;
-    const su2double *coorDOFs = locDOFs[iDim]->data();
-    for(unsigned short i=0; i<nDOFsPerSubElem; ++i)
-      parCoor[iDim] += weightsSubElem[i]*coorDOFs[connSubElems[i]];
+    const su2double* coorDOFs = locDOFs[iDim]->data();
+    for (unsigned short i = 0; i < nDOFsPerSubElem; ++i) parCoor[iDim] += weightsSubElem[i] * coorDOFs[connSubElems[i]];
   }
 
   /*--------------------------------------------------------------------------*/
@@ -6495,47 +6175,48 @@ void CMeshFEM_DG::HighOrderContainmentSearch(const su2double      *coor,
   vector<vector<su2double> > dLagBasis(nDim, vector<su2double>(nDOFs));
 
   /* Abbreviate the grid DOFs of this element a bit easier. */
-  const unsigned long *DOFs = volElem[parElem].nodeIDsGrid.data();
+  const unsigned long* DOFs = volElem[parElem].nodeIDsGrid.data();
 
   /* Loop over the maximum number of iterations. */
   unsigned short itCount;
-  for(itCount=0; itCount<maxIt; ++itCount) {
-
+  for (itCount = 0; itCount < maxIt; ++itCount) {
     /* Compute the Lagrangian basis functions and its derivatives in
        the current parametric coordinate. */
-    standardElementsGrid[ind].BasisFunctionsAndDerivativesInPoint(parCoor, lagBasis,
-                                                                  dLagBasis);
+    standardElementsGrid[ind].BasisFunctionsAndDerivativesInPoint(parCoor, lagBasis, dLagBasis);
 
     /* Make a distinction between 2D and 3D in order to have the most
        efficient code. */
     bool converged = false;
-    switch( nDim ) {
+    switch (nDim) {
       case 2: {
         /* Two dimensional computation. Compute the values of the function
            and minus the Jacobian matrix. */
         su2double f0 = coor[0], f1 = coor[1];
         su2double a00 = 0.0, a01 = 0.0, a10 = 0.0, a11 = 0.0;
-        for(unsigned short i=0; i<nDOFs; ++i) {
+        for (unsigned short i = 0; i < nDOFs; ++i) {
           const su2double x = meshPoints[DOFs[i]].coor[0];
           const su2double y = meshPoints[DOFs[i]].coor[1];
 
-          f0 -= x*lagBasis[i]; f1 -= y*lagBasis[i];
+          f0 -= x * lagBasis[i];
+          f1 -= y * lagBasis[i];
 
-          a00 += x*dLagBasis[0][i]; a01 += x*dLagBasis[1][i];
-          a10 += y*dLagBasis[0][i]; a11 += y*dLagBasis[1][i];
+          a00 += x * dLagBasis[0][i];
+          a01 += x * dLagBasis[1][i];
+          a10 += y * dLagBasis[0][i];
+          a11 += y * dLagBasis[1][i];
         }
 
         /* Compute the updates of the parametric values. As minus the
            Jacobian is computed, the updates should be added to parCoor. */
-        const su2double detInv = 1.0/(a00*a11 - a01*a10);
-        const su2double dr = detInv*(f0*a11 - f1*a01);
-        const su2double ds = detInv*(f1*a00 - f0*a10);
+        const su2double detInv = 1.0 / (a00 * a11 - a01 * a10);
+        const su2double dr = detInv * (f0 * a11 - f1 * a01);
+        const su2double ds = detInv * (f1 * a00 - f0 * a10);
 
         parCoor[0] += dr;
         parCoor[1] += ds;
 
         /* Check for convergence. */
-        if(fabs(dr) <= tolNewton && fabs(ds) <= tolNewton) converged = true;
+        if (fabs(dr) <= tolNewton && fabs(ds) <= tolNewton) converged = true;
         break;
       }
 
@@ -6547,173 +6228,162 @@ void CMeshFEM_DG::HighOrderContainmentSearch(const su2double      *coor,
         su2double a10 = 0.0, a11 = 0.0, a12 = 0.0;
         su2double a20 = 0.0, a21 = 0.0, a22 = 0.0;
 
-        for(unsigned short i=0; i<nDOFs; ++i) {
+        for (unsigned short i = 0; i < nDOFs; ++i) {
           const su2double x = meshPoints[DOFs[i]].coor[0];
           const su2double y = meshPoints[DOFs[i]].coor[1];
           const su2double z = meshPoints[DOFs[i]].coor[2];
 
-          f0 -= x*lagBasis[i]; f1 -= y*lagBasis[i]; f2 -= z*lagBasis[i];
-
-          a00 += x*dLagBasis[0][i]; a01 += x*dLagBasis[1][i]; a02 += x*dLagBasis[2][i];
-          a10 += y*dLagBasis[0][i]; a11 += y*dLagBasis[1][i]; a12 += y*dLagBasis[2][i];
-          a20 += z*dLagBasis[0][i]; a21 += z*dLagBasis[1][i]; a22 += z*dLagBasis[2][i];
+          f0 -= x * lagBasis[i];
+          f1 -= y * lagBasis[i];
+          f2 -= z * lagBasis[i];
+
+          a00 += x * dLagBasis[0][i];
+          a01 += x * dLagBasis[1][i];
+          a02 += x * dLagBasis[2][i];
+          a10 += y * dLagBasis[0][i];
+          a11 += y * dLagBasis[1][i];
+          a12 += y * dLagBasis[2][i];
+          a20 += z * dLagBasis[0][i];
+          a21 += z * dLagBasis[1][i];
+          a22 += z * dLagBasis[2][i];
         }
 
         /* Compute the updates of the parametric values. As minus the
            Jacobian is computed, the updates should be added to parCoor. */
-        const su2double detInv = 1.0/(a00*a11*a22 - a00*a12*a21 - a01*a10*a22
-                               +      a01*a12*a20 + a02*a10*a21 - a02*a11*a20);
-        const su2double dr =  detInv*(a01*a12*f2 - a01*a22*f1 - a02*a11*f2
-                           +          a02*a21*f1 + a11*a22*f0 - a12*a21*f0);
-        const su2double ds = -detInv*(a00*a12*f2 - a00*a22*f1 - a02*a10*f2
-                           +          a02*a20*f1 + a10*a22*f0 - a12*a20*f0);
-        const su2double dt =  detInv*(a00*a11*f2 - a00*a21*f1 - a01*a10*f2
-                           +          a01*a20*f1 + a10*a21*f0 - a11*a20*f0);
+        const su2double detInv = 1.0 / (a00 * a11 * a22 - a00 * a12 * a21 - a01 * a10 * a22 + a01 * a12 * a20 +
+                                        a02 * a10 * a21 - a02 * a11 * a20);
+        const su2double dr = detInv * (a01 * a12 * f2 - a01 * a22 * f1 - a02 * a11 * f2 + a02 * a21 * f1 +
+                                       a11 * a22 * f0 - a12 * a21 * f0);
+        const su2double ds = -detInv * (a00 * a12 * f2 - a00 * a22 * f1 - a02 * a10 * f2 + a02 * a20 * f1 +
+                                        a10 * a22 * f0 - a12 * a20 * f0);
+        const su2double dt = detInv * (a00 * a11 * f2 - a00 * a21 * f1 - a01 * a10 * f2 + a01 * a20 * f1 +
+                                       a10 * a21 * f0 - a11 * a20 * f0);
         parCoor[0] += dr;
         parCoor[1] += ds;
         parCoor[2] += dt;
 
         /* Check for convergence. */
-        if(fabs(dr) <= tolNewton && fabs(ds) <= tolNewton && fabs(dt) <= tolNewton)
-          converged = true;
+        if (fabs(dr) <= tolNewton && fabs(ds) <= tolNewton && fabs(dt) <= tolNewton) converged = true;
         break;
       }
     }
 
     /* Break the loop if the Newton algorithm converged. */
-    if( converged ) break;
+    if (converged) break;
   }
 
   /* Terminate if the Newton algorithm did not converge. */
-  if(itCount == maxIt)
-    SU2_MPI::Error("Newton did not converge", CURRENT_FUNCTION);
+  if (itCount == maxIt) SU2_MPI::Error("Newton did not converge", CURRENT_FUNCTION);
 }
 
-void CMeshFEM_DG::InitStaticMeshMovement(const CConfig        *config,
-                                         const unsigned short Kind_Grid_Movement,
+void CMeshFEM_DG::InitStaticMeshMovement(const CConfig* config, const unsigned short Kind_Grid_Movement,
                                          const unsigned short iZone) {
-
   /*--- Get the reference values for the non-dimensionalization of the
         prescribed velocities. ---*/
-  const su2double L_Ref     = config->GetLength_Ref();
+  const su2double L_Ref = config->GetLength_Ref();
   const su2double Omega_Ref = config->GetOmega_Ref();
-  const su2double Vel_Ref   = config->GetVelocity_Ref();
+  const su2double Vel_Ref = config->GetVelocity_Ref();
 
   /*--- Make a distinction between the possibilities. ---*/
-  switch( Kind_Grid_Movement ) {
-
-    /*-------------------------------------------------------------------------------------*/
+  switch (Kind_Grid_Movement) {
+      /*-------------------------------------------------------------------------------------*/
 
     case ROTATING_FRAME: {
-
       /* Get the rotation rate and rotation center from config. */
-    const su2double Center[] = {config->GetMotion_Origin(0),
-                                config->GetMotion_Origin(1),
-                                config->GetMotion_Origin(2)};
-    const su2double Omega[]  = {config->GetRotation_Rate(0)/Omega_Ref,
-                                config->GetRotation_Rate(1)/Omega_Ref,
-                                config->GetRotation_Rate(2)/Omega_Ref};
+      const su2double Center[] = {config->GetMotion_Origin(0), config->GetMotion_Origin(1),
+                                  config->GetMotion_Origin(2)};
+      const su2double Omega[] = {config->GetRotation_Rate(0) / Omega_Ref, config->GetRotation_Rate(1) / Omega_Ref,
+                                 config->GetRotation_Rate(2) / Omega_Ref};
 
       /* Array used to store the distance to the rotation center. */
       su2double dist[] = {0.0, 0.0, 0.0};
 
       /* Loop over the owned volume elements. */
-      for(unsigned long l=0; l<nVolElemOwned; ++l) {
-
+      for (unsigned long l = 0; l < nVolElemOwned; ++l) {
         /* Get the number of DOFs and integration points for this element. */
-        const unsigned short ind   = volElem[l].indStandardElement;
-        const unsigned short nInt  = standardElementsSol[ind].GetNIntegration();
+        const unsigned short ind = volElem[l].indStandardElement;
+        const unsigned short nInt = standardElementsSol[ind].GetNIntegration();
         const unsigned short nDOFs = volElem[l].nDOFsSol;
 
         /* Determine the grid velocities in the integration points. */
-        for(unsigned short i=0; i<nInt; ++i) {
-          const su2double *coor    = volElem[l].coorIntegrationPoints.data() + i*nDim;
-          su2double       *gridVel = volElem[l].gridVelocities.data() + i*nDim;
+        for (unsigned short i = 0; i < nInt; ++i) {
+          const su2double* coor = volElem[l].coorIntegrationPoints.data() + i * nDim;
+          su2double* gridVel = volElem[l].gridVelocities.data() + i * nDim;
 
-          for(unsigned short iDim=0; iDim<nDim; ++iDim)
-            dist[iDim] = (coor[iDim]-Center[iDim])/L_Ref;
+          for (unsigned short iDim = 0; iDim < nDim; ++iDim) dist[iDim] = (coor[iDim] - Center[iDim]) / L_Ref;
 
-          gridVel[0] = Omega[1]*dist[2] - Omega[2]*dist[1];
-          gridVel[1] = Omega[2]*dist[0] - Omega[0]*dist[2];
-          if(nDim == 3) gridVel[2] = Omega[0]*dist[1] - Omega[1]*dist[0];
+          gridVel[0] = Omega[1] * dist[2] - Omega[2] * dist[1];
+          gridVel[1] = Omega[2] * dist[0] - Omega[0] * dist[2];
+          if (nDim == 3) gridVel[2] = Omega[0] * dist[1] - Omega[1] * dist[0];
         }
 
         /* Determine the grid velocities in the solution DOFs. */
-        for(unsigned short i=0; i<nDOFs; ++i) {
-          const su2double *coor    = volElem[l].coorSolDOFs.data() + i*nDim;
-          su2double       *gridVel = volElem[l].gridVelocitiesSolDOFs.data() + i*nDim;
+        for (unsigned short i = 0; i < nDOFs; ++i) {
+          const su2double* coor = volElem[l].coorSolDOFs.data() + i * nDim;
+          su2double* gridVel = volElem[l].gridVelocitiesSolDOFs.data() + i * nDim;
 
-          for(unsigned short iDim=0; iDim<nDim; ++iDim)
-            dist[iDim] = (coor[iDim]-Center[iDim])/L_Ref;
+          for (unsigned short iDim = 0; iDim < nDim; ++iDim) dist[iDim] = (coor[iDim] - Center[iDim]) / L_Ref;
 
-          gridVel[0] = Omega[1]*dist[2] - Omega[2]*dist[1];
-          gridVel[1] = Omega[2]*dist[0] - Omega[0]*dist[2];
-          if(nDim == 3) gridVel[2] = Omega[0]*dist[1] - Omega[1]*dist[0];
+          gridVel[0] = Omega[1] * dist[2] - Omega[2] * dist[1];
+          gridVel[1] = Omega[2] * dist[0] - Omega[0] * dist[2];
+          if (nDim == 3) gridVel[2] = Omega[0] * dist[1] - Omega[1] * dist[0];
         }
       }
 
       /* Loop over the internal matching faces. */
-      for(unsigned long l=0; l<matchingFaces.size(); ++l) {
-
+      for (unsigned long l = 0; l < matchingFaces.size(); ++l) {
         /* Get the number of integration points. */
-        const unsigned short ind  = matchingFaces[l].indStandardElement;
+        const unsigned short ind = matchingFaces[l].indStandardElement;
         const unsigned short nInt = standardMatchingFacesSol[ind].GetNIntegration();
 
         /* Determine the grid velocity in the integration points. */
-        for(unsigned short i=0; i<nInt; ++i) {
-          const su2double *coor    = matchingFaces[l].coorIntegrationPoints.data() + i*nDim;
-          su2double       *gridVel = matchingFaces[l].gridVelocities.data() + i*nDim;
+        for (unsigned short i = 0; i < nInt; ++i) {
+          const su2double* coor = matchingFaces[l].coorIntegrationPoints.data() + i * nDim;
+          su2double* gridVel = matchingFaces[l].gridVelocities.data() + i * nDim;
 
-          for(unsigned short iDim=0; iDim<nDim; ++iDim)
-            dist[iDim] = (coor[iDim]-Center[iDim])/L_Ref;
+          for (unsigned short iDim = 0; iDim < nDim; ++iDim) dist[iDim] = (coor[iDim] - Center[iDim]) / L_Ref;
 
-          gridVel[0] = Omega[1]*dist[2] - Omega[2]*dist[1];
-          gridVel[1] = Omega[2]*dist[0] - Omega[0]*dist[2];
-          if(nDim == 3) gridVel[2] = Omega[0]*dist[1] - Omega[1]*dist[0];
+          gridVel[0] = Omega[1] * dist[2] - Omega[2] * dist[1];
+          gridVel[1] = Omega[2] * dist[0] - Omega[0] * dist[2];
+          if (nDim == 3) gridVel[2] = Omega[0] * dist[1] - Omega[1] * dist[0];
         }
       }
 
       /* Loop over the physical boundaries. Exclude periodic boundaries. */
-      for(unsigned short iMarker=0; iMarker<boundaries.size(); ++iMarker) {
-        if( !boundaries[iMarker].periodicBoundary ) {
-
+      for (unsigned short iMarker = 0; iMarker < boundaries.size(); ++iMarker) {
+        if (!boundaries[iMarker].periodicBoundary) {
           /* Abbreviate the surface elements a bit easier. */
-          vector<CSurfaceElementFEM> &surfElem = boundaries[iMarker].surfElem;
+          vector<CSurfaceElementFEM>& surfElem = boundaries[iMarker].surfElem;
 
           /* Check if this is a shroud boundary. */
           bool shroudBoundary = false;
-          for(unsigned short iShroud=0; iShroud<config->GetnMarker_Shroud(); ++iShroud) {
-            if(boundaries[iMarker].markerTag == config->GetMarker_Shroud(iShroud)) {
+          for (unsigned short iShroud = 0; iShroud < config->GetnMarker_Shroud(); ++iShroud) {
+            if (boundaries[iMarker].markerTag == config->GetMarker_Shroud(iShroud)) {
               shroudBoundary = true;
               break;
             }
           }
 
           /* Loop over the boundary faces of this marker. */
-          for(unsigned long l=0; l<surfElem.size(); ++l) {
-
+          for (unsigned long l = 0; l < surfElem.size(); ++l) {
             /* Get the number of integration points. */
-            const unsigned short ind  = surfElem[l].indStandardElement;
+            const unsigned short ind = surfElem[l].indStandardElement;
             const unsigned short nInt = standardBoundaryFacesGrid[ind].GetNIntegration();
 
             /* For a shroud boundary the grid velocities must be set to zero. */
-            if( shroudBoundary ) {
-              for(unsigned short i=0; i<(nInt*nDim); ++i)
-                surfElem[l].gridVelocities[i] = 0.0;
-            }
-            else {
-
+            if (shroudBoundary) {
+              for (unsigned short i = 0; i < (nInt * nDim); ++i) surfElem[l].gridVelocities[i] = 0.0;
+            } else {
               /* Normal boundary. Determine the grid velocity in the integration points. */
-              for(unsigned short i=0; i<nInt; ++i) {
-                const su2double *coor    = surfElem[l].coorIntegrationPoints.data() + i*nDim;
-                su2double       *gridVel = surfElem[l].gridVelocities.data() + i*nDim;
+              for (unsigned short i = 0; i < nInt; ++i) {
+                const su2double* coor = surfElem[l].coorIntegrationPoints.data() + i * nDim;
+                su2double* gridVel = surfElem[l].gridVelocities.data() + i * nDim;
 
-                for(unsigned short iDim=0; iDim<nDim; ++iDim)
-                  dist[iDim] = (coor[iDim]-Center[iDim])/L_Ref;
+                for (unsigned short iDim = 0; iDim < nDim; ++iDim) dist[iDim] = (coor[iDim] - Center[iDim]) / L_Ref;
 
-                gridVel[0] = Omega[1]*dist[2] - Omega[2]*dist[1];
-                gridVel[1] = Omega[2]*dist[0] - Omega[0]*dist[2];
-                if(nDim == 3) gridVel[2] = Omega[0]*dist[1] - Omega[1]*dist[0];
+                gridVel[0] = Omega[1] * dist[2] - Omega[2] * dist[1];
+                gridVel[1] = Omega[2] * dist[0] - Omega[0] * dist[2];
+                if (nDim == 3) gridVel[2] = Omega[0] * dist[1] - Omega[1] * dist[0];
               }
             }
           }
@@ -6723,72 +6393,62 @@ void CMeshFEM_DG::InitStaticMeshMovement(const CConfig        *config,
       break;
     }
 
-    /*-------------------------------------------------------------------------------------*/
+      /*-------------------------------------------------------------------------------------*/
 
     case STEADY_TRANSLATION: {
-
       /* Get the translation velocity from config. */
-    const su2double vTrans[] = {config->GetTranslation_Rate(0)/Vel_Ref,
-                                config->GetTranslation_Rate(1)/Vel_Ref,
-                                config->GetTranslation_Rate(2)/Vel_Ref};
+      const su2double vTrans[] = {config->GetTranslation_Rate(0) / Vel_Ref, config->GetTranslation_Rate(1) / Vel_Ref,
+                                  config->GetTranslation_Rate(2) / Vel_Ref};
 
       /* Loop over the owned volume elements. */
-      for(unsigned long l=0; l<nVolElemOwned; ++l) {
-
+      for (unsigned long l = 0; l < nVolElemOwned; ++l) {
         /* Get the number of DOFs and integration points for this element. */
-        const unsigned short ind   = volElem[l].indStandardElement;
-        const unsigned short nInt  = standardElementsSol[ind].GetNIntegration();
+        const unsigned short ind = volElem[l].indStandardElement;
+        const unsigned short nInt = standardElementsSol[ind].GetNIntegration();
         const unsigned short nDOFs = volElem[l].nDOFsSol;
 
         /* Set the grid velocity in both the integration points and
            the sol DOFs. */
-        for(unsigned short i=0; i<nInt; ++i) {
-          su2double *gridVel = volElem[l].gridVelocities.data() + i*nDim;
-          for(unsigned short iDim=0; iDim<nDim; ++iDim)
-            gridVel[iDim] = vTrans[iDim];
+        for (unsigned short i = 0; i < nInt; ++i) {
+          su2double* gridVel = volElem[l].gridVelocities.data() + i * nDim;
+          for (unsigned short iDim = 0; iDim < nDim; ++iDim) gridVel[iDim] = vTrans[iDim];
         }
 
-        for(unsigned short i=0; i<nDOFs; ++i) {
-          su2double *gridVel = volElem[l].gridVelocitiesSolDOFs.data() + i*nDim;
-          for(unsigned short iDim=0; iDim<nDim; ++iDim)
-            gridVel[iDim] = vTrans[iDim];
+        for (unsigned short i = 0; i < nDOFs; ++i) {
+          su2double* gridVel = volElem[l].gridVelocitiesSolDOFs.data() + i * nDim;
+          for (unsigned short iDim = 0; iDim < nDim; ++iDim) gridVel[iDim] = vTrans[iDim];
         }
       }
 
       /* Loop over the internal matching faces. */
-      for(unsigned long l=0; l<matchingFaces.size(); ++l) {
-
+      for (unsigned long l = 0; l < matchingFaces.size(); ++l) {
         /* Get the number of integration points. */
-        const unsigned short ind  = matchingFaces[l].indStandardElement;
+        const unsigned short ind = matchingFaces[l].indStandardElement;
         const unsigned short nInt = standardMatchingFacesSol[ind].GetNIntegration();
 
         /* Set the grid velocity in the integration points. */
-        for(unsigned short i=0; i<nInt; ++i) {
-          su2double *gridVel = matchingFaces[l].gridVelocities.data() + i*nDim;
-          for(unsigned short iDim=0; iDim<nDim; ++iDim)
-            gridVel[iDim] = vTrans[iDim];
+        for (unsigned short i = 0; i < nInt; ++i) {
+          su2double* gridVel = matchingFaces[l].gridVelocities.data() + i * nDim;
+          for (unsigned short iDim = 0; iDim < nDim; ++iDim) gridVel[iDim] = vTrans[iDim];
         }
       }
 
       /* Loop over the physical boundaries. Exclude periodic boundaries. */
-      for(unsigned short iMarker=0; iMarker<boundaries.size(); ++iMarker) {
-        if( !boundaries[iMarker].periodicBoundary ) {
-
+      for (unsigned short iMarker = 0; iMarker < boundaries.size(); ++iMarker) {
+        if (!boundaries[iMarker].periodicBoundary) {
           /* Abbreviate the surface elements a bit easier. */
-          vector<CSurfaceElementFEM> &surfElem = boundaries[iMarker].surfElem;
+          vector<CSurfaceElementFEM>& surfElem = boundaries[iMarker].surfElem;
 
           /* Loop over the boundary faces of this marker. */
-          for(unsigned long l=0; l<surfElem.size(); ++l) {
-
+          for (unsigned long l = 0; l < surfElem.size(); ++l) {
             /* Get the number of integration points. */
-            const unsigned short ind  = surfElem[l].indStandardElement;
+            const unsigned short ind = surfElem[l].indStandardElement;
             const unsigned short nInt = standardBoundaryFacesGrid[ind].GetNIntegration();
 
             /* Set the grid velocity in the integration points. */
-            for(unsigned short i=0; i<nInt; ++i) {
-              su2double *gridVel = surfElem[l].gridVelocities.data() + i*nDim;
-              for(unsigned short iDim=0; iDim<nDim; ++iDim)
-                gridVel[iDim] = vTrans[iDim];
+            for (unsigned short i = 0; i < nInt; ++i) {
+              su2double* gridVel = surfElem[l].gridVelocities.data() + i * nDim;
+              for (unsigned short iDim = 0; iDim < nDim; ++iDim) gridVel[iDim] = vTrans[iDim];
             }
           }
         }
@@ -6797,67 +6457,59 @@ void CMeshFEM_DG::InitStaticMeshMovement(const CConfig        *config,
       break;
     }
 
-    /*-------------------------------------------------------------------------------------*/
+      /*-------------------------------------------------------------------------------------*/
 
-    default:  /* Just to avoid a compiler warning. */
+    default: /* Just to avoid a compiler warning. */
       break;
   }
 
-  if (config->GetSurface_Movement(MOVING_WALL)){
+  if (config->GetSurface_Movement(MOVING_WALL)) {
     /*--- Loop over the physical boundaries. Skip the periodic boundaries. ---*/
-    for(unsigned short i=0; i<boundaries.size(); ++i) {
-      if( !boundaries[i].periodicBoundary ) {
-
+    for (unsigned short i = 0; i < boundaries.size(); ++i) {
+      if (!boundaries[i].periodicBoundary) {
         /* Check if for this boundary a motion has been specified. */
         if (config->GetMarker_All_Moving(i) == YES) {
-
           /* Determine the prescribed translation velocity, rotation rate
                and rotation center. */
-          const su2double Center[] = {config->GetMotion_Origin(0),
-                                      config->GetMotion_Origin(1),
+          const su2double Center[] = {config->GetMotion_Origin(0), config->GetMotion_Origin(1),
                                       config->GetMotion_Origin(2)};
-          const su2double Omega[]  = {config->GetRotation_Rate(0)/Omega_Ref,
-                                      config->GetRotation_Rate(1)/Omega_Ref,
-                                      config->GetRotation_Rate(2)/Omega_Ref};
-          const su2double vTrans[] = {config->GetTranslation_Rate(0)/Vel_Ref,
-                                      config->GetTranslation_Rate(1)/Vel_Ref,
-                                      config->GetTranslation_Rate(2)/Vel_Ref};
+          const su2double Omega[] = {config->GetRotation_Rate(0) / Omega_Ref, config->GetRotation_Rate(1) / Omega_Ref,
+                                     config->GetRotation_Rate(2) / Omega_Ref};
+          const su2double vTrans[] = {config->GetTranslation_Rate(0) / Vel_Ref,
+                                      config->GetTranslation_Rate(1) / Vel_Ref,
+                                      config->GetTranslation_Rate(2) / Vel_Ref};
 
           /* Easier storage of the surface elements and loop over them. */
-          vector<CSurfaceElementFEM> &surfElem = boundaries[i].surfElem;
-
-          for(unsigned long l=0; l<surfElem.size(); ++l) {
+          vector<CSurfaceElementFEM>& surfElem = boundaries[i].surfElem;
 
+          for (unsigned long l = 0; l < surfElem.size(); ++l) {
             /* Determine the corresponding standard face element and get the
                  relevant information from it. Note that the standard element
                  of the solution must be taken and not of the grid. */
-            const unsigned short ind  = surfElem[l].indStandardElement;
+            const unsigned short ind = surfElem[l].indStandardElement;
             const unsigned short nInt = standardBoundaryFacesSol[ind].GetNIntegration();
 
             /* Loop over the number of integration points. */
-            for(unsigned short j=0; j<nInt; ++j) {
-
+            for (unsigned short j = 0; j < nInt; ++j) {
               /* Set the pointers for the coordinates and grid velocities
                    for this integration points. */
-              const su2double *Coord = surfElem[l].coorIntegrationPoints.data() + j*nDim;
-              su2double *gridVel     = surfElem[l].gridVelocities.data() + j*nDim;
+              const su2double* Coord = surfElem[l].coorIntegrationPoints.data() + j * nDim;
+              su2double* gridVel = surfElem[l].gridVelocities.data() + j * nDim;
 
               /* Calculate non-dim. position from rotation center. */
               su2double r[] = {0.0, 0.0, 0.0};
-              for(unsigned short iDim=0; iDim<nDim; ++iDim)
-                r[iDim] = (Coord[iDim]-Center[iDim])/L_Ref;
+              for (unsigned short iDim = 0; iDim < nDim; ++iDim) r[iDim] = (Coord[iDim] - Center[iDim]) / L_Ref;
 
               /* Cross Product of angular velocity and distance from center to
                    get the rotational velocity. Note that we are adding on the
                    velocity due to pure translation as well. Note that for the
                    2D case only Omega[2] can be non-zero. */
-              su2double velGrid[] = {vTrans[0] + Omega[1]*r[2] - Omega[2]*r[1],
-                                     vTrans[1] + Omega[2]*r[0] - Omega[0]*r[2],
-                                     vTrans[2] + Omega[0]*r[1] - Omega[1]*r[0]};
+              su2double velGrid[] = {vTrans[0] + Omega[1] * r[2] - Omega[2] * r[1],
+                                     vTrans[1] + Omega[2] * r[0] - Omega[0] * r[2],
+                                     vTrans[2] + Omega[0] * r[1] - Omega[1] * r[0]};
 
               /* Store the grid velocities. */
-              for(unsigned short iDim=0; iDim<nDim; ++iDim)
-                gridVel[iDim] = velGrid[iDim];
+              for (unsigned short iDim = 0; iDim < nDim; ++iDim) gridVel[iDim] = velGrid[iDim];
             }
           }
         }
@@ -6866,23 +6518,21 @@ void CMeshFEM_DG::InitStaticMeshMovement(const CConfig        *config,
   }
 }
 
-CDummyMeshFEM_DG::CDummyMeshFEM_DG(CConfig *config): CMeshFEM_DG() {
-
+CDummyMeshFEM_DG::CDummyMeshFEM_DG(CConfig* config) : CMeshFEM_DG() {
   nZone = config->GetnZone();
 
-  nPoint_P2PSend = new int[size] ();
-  nPoint_P2PRecv = new int[size] ();
+  nPoint_P2PSend = new int[size]();
+  nPoint_P2PRecv = new int[size]();
 
-  nVertex = new unsigned long[config->GetnMarker_All()] ();
+  nVertex = new unsigned long[config->GetnMarker_All()]();
 
   Tag_to_Marker = new string[config->GetnMarker_All()];
 
-  for (unsigned short i=0; i <= config->GetnLevels_TimeAccurateLTS(); i++){
+  for (unsigned short i = 0; i <= config->GetnLevels_TimeAccurateLTS(); i++) {
     nMatchingFacesWithHaloElem.push_back(0);
   }
 
   boundaries.resize(config->GetnMarker_All());
 
   nDim = CConfig::GetnDim(config->GetMesh_FileName(), config->GetMesh_FileFormat());
-
 }
diff --git a/Common/src/fem/fem_integration_rules.cpp b/Common/src/fem/fem_integration_rules.cpp
index 6f80ee16bf7..0335b3f62cc 100644
--- a/Common/src/fem/fem_integration_rules.cpp
+++ b/Common/src/fem/fem_integration_rules.cpp
@@ -33,10 +33,9 @@
 /*----------------------------------------------------------------------------------*/
 
 void CFEMStandardElementBase::IntegrationPointsLine(void) {
-
   /*--- Allocate the memory for the integration points
         and weights and determine them.                ---*/
-  nIntegration = orderExact/2 + 1;
+  nIntegration = orderExact / 2 + 1;
   rIntegration.resize(nIntegration);
   wIntegration.resize(nIntegration);
 
@@ -44,39 +43,37 @@ void CFEMStandardElementBase::IntegrationPointsLine(void) {
 }
 
 void CFEMStandardElementBase::IntegrationPointsQuadrilateral(void) {
-
   /*--- The 2D quadrature rule is a tensor product of the 1D Gauss-Legendre
         quadrature rule. First determine the number of integration points in 1D,
         which is stored in M, and determine them.                    ---*/
-  unsigned short M = orderExact/2 + 1;
+  unsigned short M = orderExact / 2 + 1;
 
   vector<su2double> GLPoints(M), GLWeights(M);
   GaussLegendrePoints1D(GLPoints, GLWeights);
 
   /*--- Allocate the memory for the integration points
         and weights and determine them.                ---*/
-  nIntegration = M*M;
+  nIntegration = M * M;
   rIntegration.resize(nIntegration);
   sIntegration.resize(nIntegration);
   wIntegration.resize(nIntegration);
 
   unsigned int ii = 0;
-  for(unsigned short j=0; j<M; ++j) {
-    for(unsigned short i=0; i<M; ++i, ++ii) {
+  for (unsigned short j = 0; j < M; ++j) {
+    for (unsigned short i = 0; i < M; ++i, ++ii) {
       rIntegration[ii] = GLPoints[i];
       sIntegration[ii] = GLPoints[j];
-      wIntegration[ii] = GLWeights[i]*GLWeights[j];
+      wIntegration[ii] = GLWeights[i] * GLWeights[j];
     }
   }
 }
 
 void CFEMStandardElementBase::IntegrationPointsPrism(void) {
-
   /*--- The 3D quadrature rule for a prism is a tensor product of the 1D Gauss-Legendre
         quadrature rule with the triangle quadrature rule. Determine the number of
         integration points in 1D, which is stored in M, and the actual integration
         1D integration points. ---*/
-  unsigned short M = orderExact/2 + 1;
+  unsigned short M = orderExact / 2 + 1;
 
   vector<su2double> GLPoints(M), GLWeights(M);
   GaussLegendrePoints1D(GLPoints, GLWeights);
@@ -84,95 +81,147 @@ void CFEMStandardElementBase::IntegrationPointsPrism(void) {
   /*--- Also determine the integration rule for a triangle. ---*/
   IntegrationPointsTriangle();
 
-  unsigned short    nIntTriangle = nIntegration;
-  vector<su2double> rTriangle    = rIntegration;
-  vector<su2double> sTriangle    = sIntegration;
-  vector<su2double> wTriangle    = wIntegration;
+  unsigned short nIntTriangle = nIntegration;
+  vector<su2double> rTriangle = rIntegration;
+  vector<su2double> sTriangle = sIntegration;
+  vector<su2double> wTriangle = wIntegration;
 
   /*--- Allocate the memory for the integration points and weights
         of the prism and determine them.                ---*/
-  nIntegration = M*nIntTriangle;
+  nIntegration = M * nIntTriangle;
   rIntegration.resize(nIntegration);
   sIntegration.resize(nIntegration);
   tIntegration.resize(nIntegration);
   wIntegration.resize(nIntegration);
 
   unsigned int ii = 0;
-  for(unsigned short k=0; k<M; ++k) {
-    for(unsigned short j=0; j<nIntTriangle; ++j, ++ii) {
+  for (unsigned short k = 0; k < M; ++k) {
+    for (unsigned short j = 0; j < nIntTriangle; ++j, ++ii) {
       rIntegration[ii] = rTriangle[j];
       sIntegration[ii] = sTriangle[j];
       tIntegration[ii] = GLPoints[k];
-      wIntegration[ii] = wTriangle[j]*GLWeights[k];
+      wIntegration[ii] = wTriangle[j] * GLWeights[k];
     }
   }
 }
 
 void CFEMStandardElementBase::IntegrationPointsHexahedron(void) {
-
   /*--- The 3D quadrature rule is a tensor product of the 1D Gauss-Legendre
         quadrature rule. Determine the number of integration points in 1D, which
         is stored in M, and the actual integration 1D integration points. ---*/
-  unsigned short M = orderExact/2 + 1;
+  unsigned short M = orderExact / 2 + 1;
 
   vector<su2double> GLPoints(M), GLWeights(M);
   GaussLegendrePoints1D(GLPoints, GLWeights);
 
   /*--- Allocate the memory for the integration points and weights
         of the hexahedron and determine them.                ---*/
-  nIntegration = M*M*M;
+  nIntegration = M * M * M;
   rIntegration.resize(nIntegration);
   sIntegration.resize(nIntegration);
   tIntegration.resize(nIntegration);
   wIntegration.resize(nIntegration);
 
   unsigned int ii = 0;
-  for(unsigned short k=0; k<M; ++k) {
-    for(unsigned short j=0; j<M; ++j) {
-      for(unsigned short i=0; i<M; ++i, ++ii) {
+  for (unsigned short k = 0; k < M; ++k) {
+    for (unsigned short j = 0; j < M; ++j) {
+      for (unsigned short i = 0; i < M; ++i, ++ii) {
         rIntegration[ii] = GLPoints[i];
         sIntegration[ii] = GLPoints[j];
         tIntegration[ii] = GLPoints[k];
-        wIntegration[ii] = GLWeights[i]*GLWeights[j]*GLWeights[k];
+        wIntegration[ii] = GLWeights[i] * GLWeights[j] * GLWeights[k];
       }
     }
   }
 }
 
 void CFEMStandardElementBase::IntegrationPointsTriangle(void) {
-
   /*--- Set the number of integration points, depending on the order of
         polynomials that must be integrated exactly. ---*/
-  switch( orderExact ) {
-    case  0:
-    case  1: nIntegration =   1; break;
-    case  2: nIntegration =   3; break;
-    case  3:
-    case  4: nIntegration =   6; break;
-    case  5: nIntegration =   7; break;
-    case  6: nIntegration =  12; break;
-    case  7: nIntegration =  15; break;
-    case  8: nIntegration =  16; break;
-    case  9: nIntegration =  19; break;
-    case 10: nIntegration =  25; break;
-    case 11: nIntegration =  28; break;
-    case 12: nIntegration =  36; break;
-    case 13: nIntegration =  40; break;
-    case 14: nIntegration =  46; break;
-    case 15: nIntegration =  54; break;
-    case 16: nIntegration =  58; break;
-    case 17: nIntegration =  66; break;
-    case 18: nIntegration =  73; break;
-    case 19: nIntegration =  82; break;
-    case 20: nIntegration =  85; break;
-    case 21: nIntegration =  93; break;
-    case 22: nIntegration = 100; break;
-    case 23: nIntegration = 106; break;
-    case 24: nIntegration = 118; break;
-    case 25: nIntegration = 126; break;
-    case 26: nIntegration = 138; break;
-    case 27: nIntegration = 145; break;
-    case 28: nIntegration = 225; break;
+  switch (orderExact) {
+    case 0:
+    case 1:
+      nIntegration = 1;
+      break;
+    case 2:
+      nIntegration = 3;
+      break;
+    case 3:
+    case 4:
+      nIntegration = 6;
+      break;
+    case 5:
+      nIntegration = 7;
+      break;
+    case 6:
+      nIntegration = 12;
+      break;
+    case 7:
+      nIntegration = 15;
+      break;
+    case 8:
+      nIntegration = 16;
+      break;
+    case 9:
+      nIntegration = 19;
+      break;
+    case 10:
+      nIntegration = 25;
+      break;
+    case 11:
+      nIntegration = 28;
+      break;
+    case 12:
+      nIntegration = 36;
+      break;
+    case 13:
+      nIntegration = 40;
+      break;
+    case 14:
+      nIntegration = 46;
+      break;
+    case 15:
+      nIntegration = 54;
+      break;
+    case 16:
+      nIntegration = 58;
+      break;
+    case 17:
+      nIntegration = 66;
+      break;
+    case 18:
+      nIntegration = 73;
+      break;
+    case 19:
+      nIntegration = 82;
+      break;
+    case 20:
+      nIntegration = 85;
+      break;
+    case 21:
+      nIntegration = 93;
+      break;
+    case 22:
+      nIntegration = 100;
+      break;
+    case 23:
+      nIntegration = 106;
+      break;
+    case 24:
+      nIntegration = 118;
+      break;
+    case 25:
+      nIntegration = 126;
+      break;
+    case 26:
+      nIntegration = 138;
+      break;
+    case 27:
+      nIntegration = 145;
+      break;
+    case 28:
+      nIntegration = 225;
+      break;
     default:
       SU2_MPI::Error("Polynomial order not supported", CURRENT_FUNCTION);
   }
@@ -184,1845 +233,5291 @@ void CFEMStandardElementBase::IntegrationPointsTriangle(void) {
 
   /*--- Set the pointers to the data arrays of the variables just allocated, such
         that the names are shorter. This is useful for the code below. ---*/
-  su2double *r = rIntegration.data();
-  su2double *s = sIntegration.data();
-  su2double *w = wIntegration.data();
+  su2double* r = rIntegration.data();
+  su2double* s = sIntegration.data();
+  su2double* w = wIntegration.data();
 
   /*--- Set the data for the integration points, depending on the order.
         These integration rules come from the Matlab codes corresponding to
         the book "Nodal Discontinuous Methods: Algorithms, Analysis, and Applications"
         by Jan S. Hesthaven and Tim Warburton. ---*/
-  switch( orderExact ) {
-    case  0:
-    case  1: {
-      r[0] = -0.333333333333333; s[0] = -0.333333333333333; w[0] = 2.000000000000000;
+  switch (orderExact) {
+    case 0:
+    case 1: {
+      r[0] = -0.333333333333333;
+      s[0] = -0.333333333333333;
+      w[0] = 2.000000000000000;
 
       break;
     }
-    case  2: {
-      r[0] = -0.666666666666667; s[0] = -0.666666666666667; w[0] = 0.666666666666667;
-      r[1] =  0.333333333333333; s[1] = -0.666666666666667; w[1] = 0.666666666666667;
-      r[2] = -0.666666666666667; s[2] =  0.333333333333333; w[2] = 0.666666666666667;
+    case 2: {
+      r[0] = -0.666666666666667;
+      s[0] = -0.666666666666667;
+      w[0] = 0.666666666666667;
+      r[1] = 0.333333333333333;
+      s[1] = -0.666666666666667;
+      w[1] = 0.666666666666667;
+      r[2] = -0.666666666666667;
+      s[2] = 0.333333333333333;
+      w[2] = 0.666666666666667;
 
       break;
     }
-    case  3:
-    case  4: {
-      r[0] = -0.816847572980458; s[0] = -0.816847572980458; w[0] = 0.219903487310644;
-      r[1] =  0.633695145960917; s[1] = -0.816847572980459; w[1] = 0.219903487310644;
-      r[2] = -0.816847572980459; s[2] =  0.633695145960917; w[2] = 0.219903487310644;
-      r[3] = -0.108103018168070; s[3] = -0.108103018168070; w[3] = 0.446763179356023;
-      r[4] = -0.783793963663860; s[4] = -0.108103018168070; w[4] = 0.446763179356023;
-      r[5] = -0.108103018168070; s[5] = -0.783793963663860; w[5] = 0.446763179356023;
+    case 3:
+    case 4: {
+      r[0] = -0.816847572980458;
+      s[0] = -0.816847572980458;
+      w[0] = 0.219903487310644;
+      r[1] = 0.633695145960917;
+      s[1] = -0.816847572980459;
+      w[1] = 0.219903487310644;
+      r[2] = -0.816847572980459;
+      s[2] = 0.633695145960917;
+      w[2] = 0.219903487310644;
+      r[3] = -0.108103018168070;
+      s[3] = -0.108103018168070;
+      w[3] = 0.446763179356023;
+      r[4] = -0.783793963663860;
+      s[4] = -0.108103018168070;
+      w[4] = 0.446763179356023;
+      r[5] = -0.108103018168070;
+      s[5] = -0.783793963663860;
+      w[5] = 0.446763179356023;
 
       break;
     }
-    case  5: {
-      r[0] = -0.333333333333333; s[0] = -0.333333333333333; w[0] = 0.450000000000000;
-      r[1] = -0.059715871789770; s[1] = -0.059715871789770; w[1] = 0.264788305577012;
-      r[2] = -0.880568256420460; s[2] = -0.059715871789770; w[2] = 0.264788305577012;
-      r[3] = -0.059715871789770; s[3] = -0.880568256420460; w[3] = 0.264788305577012;
-      r[4] = -0.797426985353087; s[4] = -0.797426985353087; w[4] = 0.251878361089654;
-      r[5] =  0.594853970706175; s[5] = -0.797426985353087; w[5] = 0.251878361089654;
-      r[6] = -0.797426985353087; s[6] =  0.594853970706175; w[6] = 0.251878361089654;
+    case 5: {
+      r[0] = -0.333333333333333;
+      s[0] = -0.333333333333333;
+      w[0] = 0.450000000000000;
+      r[1] = -0.059715871789770;
+      s[1] = -0.059715871789770;
+      w[1] = 0.264788305577012;
+      r[2] = -0.880568256420460;
+      s[2] = -0.059715871789770;
+      w[2] = 0.264788305577012;
+      r[3] = -0.059715871789770;
+      s[3] = -0.880568256420460;
+      w[3] = 0.264788305577012;
+      r[4] = -0.797426985353087;
+      s[4] = -0.797426985353087;
+      w[4] = 0.251878361089654;
+      r[5] = 0.594853970706175;
+      s[5] = -0.797426985353087;
+      w[5] = 0.251878361089654;
+      r[6] = -0.797426985353087;
+      s[6] = 0.594853970706175;
+      w[6] = 0.251878361089654;
 
       break;
     }
-    case  6: {
-      r[0]  = -0.501426509658179; s[0]  = -0.501426509658179; w[0]  = 0.233572551452759;
-      r[1]  =  0.002853019316358; s[1]  = -0.501426509658179; w[1]  = 0.233572551452759;
-      r[2]  = -0.501426509658179; s[2]  =  0.002853019316358; w[2]  = 0.233572551452759;
-      r[3]  = -0.873821971016996; s[3]  = -0.873821971016996; w[3]  = 0.101689812740414;
-      r[4]  =  0.747643942033991; s[4]  = -0.873821971016996; w[4]  = 0.101689812740414;
-      r[5]  = -0.873821971016996; s[5]  =  0.747643942033991; w[5]  = 0.101689812740414;
-      r[6]  = -0.379295097932431; s[6]  = -0.893709900310366; w[6]  = 0.165702151236747;
-      r[7]  = -0.893709900310366; s[7]  = -0.379295097932431; w[7]  = 0.165702151236747;
-      r[8]  =  0.273004998242797; s[8]  = -0.893709900310366; w[8]  = 0.165702151236747;
-      r[9]  = -0.893709900310366; s[9]  =  0.273004998242797; w[9]  = 0.165702151236747;
-      r[10] =  0.273004998242797; s[10] = -0.379295097932431; w[10] = 0.165702151236747;
-      r[11] = -0.379295097932431; s[11] =  0.273004998242797; w[11] = 0.165702151236747;
+    case 6: {
+      r[0] = -0.501426509658179;
+      s[0] = -0.501426509658179;
+      w[0] = 0.233572551452759;
+      r[1] = 0.002853019316358;
+      s[1] = -0.501426509658179;
+      w[1] = 0.233572551452759;
+      r[2] = -0.501426509658179;
+      s[2] = 0.002853019316358;
+      w[2] = 0.233572551452759;
+      r[3] = -0.873821971016996;
+      s[3] = -0.873821971016996;
+      w[3] = 0.101689812740414;
+      r[4] = 0.747643942033991;
+      s[4] = -0.873821971016996;
+      w[4] = 0.101689812740414;
+      r[5] = -0.873821971016996;
+      s[5] = 0.747643942033991;
+      w[5] = 0.101689812740414;
+      r[6] = -0.379295097932431;
+      s[6] = -0.893709900310366;
+      w[6] = 0.165702151236747;
+      r[7] = -0.893709900310366;
+      s[7] = -0.379295097932431;
+      w[7] = 0.165702151236747;
+      r[8] = 0.273004998242797;
+      s[8] = -0.893709900310366;
+      w[8] = 0.165702151236747;
+      r[9] = -0.893709900310366;
+      s[9] = 0.273004998242797;
+      w[9] = 0.165702151236747;
+      r[10] = 0.273004998242797;
+      s[10] = -0.379295097932431;
+      w[10] = 0.165702151236747;
+      r[11] = -0.379295097932431;
+      s[11] = 0.273004998242797;
+      w[11] = 0.165702151236747;
 
       break;
     }
-    case  7: {
-      r[0]  = -0.158765070723907; s[0]  = -0.158765070723907; w[0]  = 0.278402959350494;
-      r[1]  = -0.682469858552186; s[1]  = -0.158765070723907; w[1]  = 0.278402959350494;
-      r[2]  = -0.158765070723907; s[2]  = -0.682469858552186; w[2]  = 0.278402959350494;
-      r[3]  = -0.901937632421608; s[3]  = -0.901937632421608; w[3]  = 0.063653882657145;
-      r[4]  =  0.803875264843215; s[4]  = -0.901937632421608; w[4]  = 0.063653882657145;
-      r[5]  = -0.901937632421608; s[5]  =  0.803875264843215; w[5]  = 0.063653882657145;
-      r[6]  = -0.696696002590528; s[6]  = -0.696696002590528; w[6]  = 0.168642646759703;
-      r[7]  =  0.393392005181056; s[7]  = -0.696696002590528; w[7]  = 0.168642646759703;
-      r[8]  = -0.696696002590528; s[8]  =  0.393392005181056; w[8]  = 0.168642646759703;
-      r[9]  =  0.348275575962283; s[9]  = -0.375762055856278; w[9]  = 0.077983588949662;
-      r[10] = -0.375762055856278; s[10] =  0.348275575962283; w[10] = 0.077983588949662;
-      r[11] = -0.972513520106005; s[11] = -0.375762055856278; w[11] = 0.077983588949662;
-      r[12] = -0.375762055856278; s[12] = -0.972513520106005; w[12] = 0.077983588949662;
-      r[13] = -0.972513520106005; s[13] =  0.348275575962283; w[13] = 0.077983588949662;
-      r[14] =  0.348275575962283; s[14] = -0.972513520106005; w[14] = 0.077983588949662;
+    case 7: {
+      r[0] = -0.158765070723907;
+      s[0] = -0.158765070723907;
+      w[0] = 0.278402959350494;
+      r[1] = -0.682469858552186;
+      s[1] = -0.158765070723907;
+      w[1] = 0.278402959350494;
+      r[2] = -0.158765070723907;
+      s[2] = -0.682469858552186;
+      w[2] = 0.278402959350494;
+      r[3] = -0.901937632421608;
+      s[3] = -0.901937632421608;
+      w[3] = 0.063653882657145;
+      r[4] = 0.803875264843215;
+      s[4] = -0.901937632421608;
+      w[4] = 0.063653882657145;
+      r[5] = -0.901937632421608;
+      s[5] = 0.803875264843215;
+      w[5] = 0.063653882657145;
+      r[6] = -0.696696002590528;
+      s[6] = -0.696696002590528;
+      w[6] = 0.168642646759703;
+      r[7] = 0.393392005181056;
+      s[7] = -0.696696002590528;
+      w[7] = 0.168642646759703;
+      r[8] = -0.696696002590528;
+      s[8] = 0.393392005181056;
+      w[8] = 0.168642646759703;
+      r[9] = 0.348275575962283;
+      s[9] = -0.375762055856278;
+      w[9] = 0.077983588949662;
+      r[10] = -0.375762055856278;
+      s[10] = 0.348275575962283;
+      w[10] = 0.077983588949662;
+      r[11] = -0.972513520106005;
+      s[11] = -0.375762055856278;
+      w[11] = 0.077983588949662;
+      r[12] = -0.375762055856278;
+      s[12] = -0.972513520106005;
+      w[12] = 0.077983588949662;
+      r[13] = -0.972513520106005;
+      s[13] = 0.348275575962283;
+      w[13] = 0.077983588949662;
+      r[14] = 0.348275575962283;
+      s[14] = -0.972513520106005;
+      w[14] = 0.077983588949662;
 
       break;
     }
-    case  8: {
-      r[0]  = -0.333333333333333; s[0]  = -0.333333333333333; w[0]  = 0.288631215355574;
-      r[1]  = -0.081414823414554; s[1]  = -0.081414823414554; w[1]  = 0.190183268534569;
-      r[2]  = -0.837170353170893; s[2]  = -0.081414823414554; w[2]  = 0.190183268534569;
-      r[3]  = -0.081414823414554; s[3]  = -0.837170353170893; w[3]  = 0.190183268534569;
-      r[4]  = -0.658861384496480; s[4]  = -0.658861384496480; w[4]  = 0.206434741069437;
-      r[5]  =  0.317722768992959; s[5]  = -0.658861384496480; w[5]  = 0.206434741069437;
-      r[6]  = -0.658861384496480; s[6]  =  0.317722768992959; w[6]  = 0.206434741069437;
-      r[7]  = -0.898905543365938; s[7]  = -0.898905543365938; w[7]  = 0.064916995246396;
-      r[8]  =  0.797811086731876; s[8]  = -0.898905543365938; w[8]  = 0.064916995246396;
-      r[9]  = -0.898905543365938; s[9]  =  0.797811086731876; w[9]  = 0.064916995246396;
-      r[10] = -0.473774340730724; s[10] =  0.456984785910809; w[10] = 0.054460628348870;
-      r[11] =  0.456984785910809; s[11] = -0.473774340730724; w[11] = 0.054460628348870;
-      r[12] = -0.983210445180085; s[12] =  0.456984785910809; w[12] = 0.054460628348870;
-      r[13] =  0.456984785910809; s[13] = -0.983210445180085; w[13] = 0.054460628348870;
-      r[14] = -0.983210445180085; s[14] = -0.473774340730724; w[14] = 0.054460628348870;
-      r[15] = -0.473774340730724; s[15] = -0.983210445180085; w[15] = 0.054460628348870;
+    case 8: {
+      r[0] = -0.333333333333333;
+      s[0] = -0.333333333333333;
+      w[0] = 0.288631215355574;
+      r[1] = -0.081414823414554;
+      s[1] = -0.081414823414554;
+      w[1] = 0.190183268534569;
+      r[2] = -0.837170353170893;
+      s[2] = -0.081414823414554;
+      w[2] = 0.190183268534569;
+      r[3] = -0.081414823414554;
+      s[3] = -0.837170353170893;
+      w[3] = 0.190183268534569;
+      r[4] = -0.658861384496480;
+      s[4] = -0.658861384496480;
+      w[4] = 0.206434741069437;
+      r[5] = 0.317722768992959;
+      s[5] = -0.658861384496480;
+      w[5] = 0.206434741069437;
+      r[6] = -0.658861384496480;
+      s[6] = 0.317722768992959;
+      w[6] = 0.206434741069437;
+      r[7] = -0.898905543365938;
+      s[7] = -0.898905543365938;
+      w[7] = 0.064916995246396;
+      r[8] = 0.797811086731876;
+      s[8] = -0.898905543365938;
+      w[8] = 0.064916995246396;
+      r[9] = -0.898905543365938;
+      s[9] = 0.797811086731876;
+      w[9] = 0.064916995246396;
+      r[10] = -0.473774340730724;
+      s[10] = 0.456984785910809;
+      w[10] = 0.054460628348870;
+      r[11] = 0.456984785910809;
+      s[11] = -0.473774340730724;
+      w[11] = 0.054460628348870;
+      r[12] = -0.983210445180085;
+      s[12] = 0.456984785910809;
+      w[12] = 0.054460628348870;
+      r[13] = 0.456984785910809;
+      s[13] = -0.983210445180085;
+      w[13] = 0.054460628348870;
+      r[14] = -0.983210445180085;
+      s[14] = -0.473774340730724;
+      w[14] = 0.054460628348870;
+      r[15] = -0.473774340730724;
+      s[15] = -0.983210445180085;
+      w[15] = 0.054460628348870;
 
       break;
     }
-    case  9: {
-      r[0]  = -0.333333333333333; s[0]  = -0.333333333333333; w[0]  = 0.194271592565598;
-      r[1]  = -0.020634961602525; s[1]  = -0.020634961602525; w[1]  = 0.062669400454278;
-      r[2]  = -0.958730076794950; s[2]  = -0.020634961602525; w[2]  = 0.062669400454278;
-      r[3]  = -0.020634961602525; s[3]  = -0.958730076794950; w[3]  = 0.062669400454278;
-      r[4]  = -0.125820817014127; s[4]  = -0.125820817014127; w[4]  = 0.155655082009549;
-      r[5]  = -0.748358365971746; s[5]  = -0.125820817014127; w[5]  = 0.155655082009549;
-      r[6]  = -0.125820817014127; s[6]  = -0.748358365971746; w[6]  = 0.155655082009549;
-      r[7]  = -0.623592928761935; s[7]  = -0.623592928761935; w[7]  = 0.159295477854420;
-      r[8]  =  0.247185857523869; s[8]  = -0.623592928761935; w[8]  = 0.159295477854420;
-      r[9]  = -0.623592928761935; s[9]  =  0.247185857523869; w[9]  = 0.159295477854420;
-      r[10] = -0.910540973211095; s[10] = -0.910540973211095; w[10] = 0.051155351317396;
-      r[11] =  0.821081946422189; s[11] = -0.910540973211095; w[11] = 0.051155351317396;
-      r[12] = -0.910540973211095; s[12] =  0.821081946422189; w[12] = 0.051155351317396;
-      r[13] =  0.482397197568996; s[13] = -0.556074021678469; w[13] = 0.086567078754579;
-      r[14] = -0.556074021678469; s[14] =  0.482397197568996; w[14] = 0.086567078754579;
-      r[15] = -0.926323175890527; s[15] = -0.556074021678469; w[15] = 0.086567078754579;
-      r[16] = -0.556074021678469; s[16] = -0.926323175890527; w[16] = 0.086567078754579;
-      r[17] = -0.926323175890527; s[17] =  0.482397197568996; w[17] = 0.086567078754579;
-      r[18] =  0.482397197568996; s[18] = -0.926323175890527; w[18] = 0.086567078754579;
+    case 9: {
+      r[0] = -0.333333333333333;
+      s[0] = -0.333333333333333;
+      w[0] = 0.194271592565598;
+      r[1] = -0.020634961602525;
+      s[1] = -0.020634961602525;
+      w[1] = 0.062669400454278;
+      r[2] = -0.958730076794950;
+      s[2] = -0.020634961602525;
+      w[2] = 0.062669400454278;
+      r[3] = -0.020634961602525;
+      s[3] = -0.958730076794950;
+      w[3] = 0.062669400454278;
+      r[4] = -0.125820817014127;
+      s[4] = -0.125820817014127;
+      w[4] = 0.155655082009549;
+      r[5] = -0.748358365971746;
+      s[5] = -0.125820817014127;
+      w[5] = 0.155655082009549;
+      r[6] = -0.125820817014127;
+      s[6] = -0.748358365971746;
+      w[6] = 0.155655082009549;
+      r[7] = -0.623592928761935;
+      s[7] = -0.623592928761935;
+      w[7] = 0.159295477854420;
+      r[8] = 0.247185857523869;
+      s[8] = -0.623592928761935;
+      w[8] = 0.159295477854420;
+      r[9] = -0.623592928761935;
+      s[9] = 0.247185857523869;
+      w[9] = 0.159295477854420;
+      r[10] = -0.910540973211095;
+      s[10] = -0.910540973211095;
+      w[10] = 0.051155351317396;
+      r[11] = 0.821081946422189;
+      s[11] = -0.910540973211095;
+      w[11] = 0.051155351317396;
+      r[12] = -0.910540973211095;
+      s[12] = 0.821081946422189;
+      w[12] = 0.051155351317396;
+      r[13] = 0.482397197568996;
+      s[13] = -0.556074021678469;
+      w[13] = 0.086567078754579;
+      r[14] = -0.556074021678469;
+      s[14] = 0.482397197568996;
+      w[14] = 0.086567078754579;
+      r[15] = -0.926323175890527;
+      s[15] = -0.556074021678469;
+      w[15] = 0.086567078754579;
+      r[16] = -0.556074021678469;
+      s[16] = -0.926323175890527;
+      w[16] = 0.086567078754579;
+      r[17] = -0.926323175890527;
+      s[17] = 0.482397197568996;
+      w[17] = 0.086567078754579;
+      r[18] = 0.482397197568996;
+      s[18] = -0.926323175890527;
+      w[18] = 0.086567078754579;
 
       break;
     }
     case 10: {
-      r[0]  = -0.333333333333333; s[0]  = -0.333333333333333; w[0]  = 0.167046799610393;
-      r[1]  = -0.004269134091050; s[1]  = -0.004269134091050; w[1]  = 0.014459701184113;
-      r[2]  = -0.991461731817899; s[2]  = -0.004269134091050; w[2]  = 0.014459701184113;
-      r[3]  = -0.004269134091050; s[3]  = -0.991461731817899; w[3]  = 0.014459701184113;
-      r[4]  = -0.143975100541888; s[4]  = -0.143975100541888; w[4]  = 0.148984355841961;
-      r[5]  = -0.712049798916225; s[5]  = -0.143975100541888; w[5]  = 0.148984355841961;
-      r[6]  = -0.143975100541888; s[6]  = -0.712049798916225; w[6]  = 0.148984355841961;
-      r[7]  = -0.630487174513551; s[7]  = -0.630487174513551; w[7]  = 0.157292946806217;
-      r[8]  =  0.260974349027102; s[8]  = -0.630487174513551; w[8]  = 0.157292946806217;
-      r[9]  = -0.630487174513551; s[9]  =  0.260974349027102; w[9]  = 0.157292946806217;
-      r[10] = -0.959037562856645; s[10] = -0.959037562856645; w[10] = 0.013856646174215;
-      r[11] =  0.918075125713290; s[11] = -0.959037562856645; w[11] = 0.013856646174215;
-      r[12] = -0.959037562856645; s[12] =  0.918075125713290; w[12] = 0.013856646174215;
-      r[13] = -0.726852847487933; s[13] =  0.656846867693389; w[13] = 0.059036640669559;
-      r[14] =  0.656846867693389; s[14] = -0.726852847487933; w[14] = 0.059036640669559;
-      r[15] = -0.929994020205456; s[15] =  0.656846867693389; w[15] = 0.059036640669559;
-      r[16] =  0.656846867693389; s[16] = -0.929994020205456; w[16] = 0.059036640669559;
-      r[17] = -0.929994020205456; s[17] = -0.726852847487933; w[17] = 0.059036640669559;
-      r[18] = -0.726852847487933; s[18] = -0.929994020205456; w[18] = 0.059036640669559;
-      r[19] = -0.334512798822723; s[19] =  0.259414658305837; w[19] = 0.079158734392122;
-      r[20] =  0.259414658305837; s[20] = -0.334512798822723; w[20] = 0.079158734392122;
-      r[21] = -0.924901859483115; s[21] =  0.259414658305837; w[21] = 0.079158734392122;
-      r[22] =  0.259414658305837; s[22] = -0.924901859483115; w[22] = 0.079158734392122;
-      r[23] = -0.924901859483115; s[23] = -0.334512798822723; w[23] = 0.079158734392122;
-      r[24] = -0.334512798822723; s[24] = -0.924901859483115; w[24] = 0.079158734392122;
+      r[0] = -0.333333333333333;
+      s[0] = -0.333333333333333;
+      w[0] = 0.167046799610393;
+      r[1] = -0.004269134091050;
+      s[1] = -0.004269134091050;
+      w[1] = 0.014459701184113;
+      r[2] = -0.991461731817899;
+      s[2] = -0.004269134091050;
+      w[2] = 0.014459701184113;
+      r[3] = -0.004269134091050;
+      s[3] = -0.991461731817899;
+      w[3] = 0.014459701184113;
+      r[4] = -0.143975100541888;
+      s[4] = -0.143975100541888;
+      w[4] = 0.148984355841961;
+      r[5] = -0.712049798916225;
+      s[5] = -0.143975100541888;
+      w[5] = 0.148984355841961;
+      r[6] = -0.143975100541888;
+      s[6] = -0.712049798916225;
+      w[6] = 0.148984355841961;
+      r[7] = -0.630487174513551;
+      s[7] = -0.630487174513551;
+      w[7] = 0.157292946806217;
+      r[8] = 0.260974349027102;
+      s[8] = -0.630487174513551;
+      w[8] = 0.157292946806217;
+      r[9] = -0.630487174513551;
+      s[9] = 0.260974349027102;
+      w[9] = 0.157292946806217;
+      r[10] = -0.959037562856645;
+      s[10] = -0.959037562856645;
+      w[10] = 0.013856646174215;
+      r[11] = 0.918075125713290;
+      s[11] = -0.959037562856645;
+      w[11] = 0.013856646174215;
+      r[12] = -0.959037562856645;
+      s[12] = 0.918075125713290;
+      w[12] = 0.013856646174215;
+      r[13] = -0.726852847487933;
+      s[13] = 0.656846867693389;
+      w[13] = 0.059036640669559;
+      r[14] = 0.656846867693389;
+      s[14] = -0.726852847487933;
+      w[14] = 0.059036640669559;
+      r[15] = -0.929994020205456;
+      s[15] = 0.656846867693389;
+      w[15] = 0.059036640669559;
+      r[16] = 0.656846867693389;
+      s[16] = -0.929994020205456;
+      w[16] = 0.059036640669559;
+      r[17] = -0.929994020205456;
+      s[17] = -0.726852847487933;
+      w[17] = 0.059036640669559;
+      r[18] = -0.726852847487933;
+      s[18] = -0.929994020205456;
+      w[18] = 0.059036640669559;
+      r[19] = -0.334512798822723;
+      s[19] = 0.259414658305837;
+      w[19] = 0.079158734392122;
+      r[20] = 0.259414658305837;
+      s[20] = -0.334512798822723;
+      w[20] = 0.079158734392122;
+      r[21] = -0.924901859483115;
+      s[21] = 0.259414658305837;
+      w[21] = 0.079158734392122;
+      r[22] = 0.259414658305837;
+      s[22] = -0.924901859483115;
+      w[22] = 0.079158734392122;
+      r[23] = -0.924901859483115;
+      s[23] = -0.334512798822723;
+      w[23] = 0.079158734392122;
+      r[24] = -0.334512798822723;
+      s[24] = -0.924901859483115;
+      w[24] = 0.079158734392122;
 
       break;
     }
     case 11: {
-      r[0]  = -0.333333333333333; s[0]  = -0.333333333333333; w[0]  = 0.171542269659139;
-      r[1]  = -0.008227986519701; s[1]  = -0.008227986519701; w[1]  = 0.033232309648099;
-      r[2]  = -0.983544026960598; s[2]  = -0.008227986519701; w[2]  = 0.033232309648099;
-      r[3]  = -0.008227986519701; s[3]  = -0.983544026960598; w[3]  = 0.033232309648099;
-      r[4]  = -0.123062767323470; s[4]  = -0.123062767323470; w[4]  = 0.134650934561697;
-      r[5]  = -0.753874465353061; s[5]  = -0.123062767323470; w[5]  = 0.134650934561697;
-      r[6]  = -0.123062767323470; s[6]  = -0.753874465353061; w[6]  = 0.134650934561697;
-      r[7]  = -0.579583807314522; s[7]  = -0.579583807314522; w[7]  = 0.141045284213931;
-      r[8]  =  0.159167614629044; s[8]  = -0.579583807314522; w[8]  = 0.141045284213931;
-      r[9]  = -0.579583807314522; s[9]  =  0.159167614629044; w[9]  = 0.141045284213931;
-      r[10] = -0.794793191450311; s[10] = -0.794793191450311; w[10] = 0.077255352409353;
-      r[11] =  0.589586382900622; s[11] = -0.794793191450311; w[11] = 0.077255352409353;
-      r[12] = -0.794793191450311; s[12] =  0.589586382900622; w[12] = 0.077255352409353;
-      r[13] = -0.943045809035533; s[13] = -0.943045809035533; w[13] = 0.020851693311810;
-      r[14] =  0.886091618071066; s[14] = -0.943045809035533; w[14] = 0.020851693311810;
-      r[15] = -0.943045809035533; s[15] =  0.886091618071066; w[15] = 0.020851693311810;
-      r[16] = -0.701412405190965; s[16] =  0.686811031831200; w[16] = 0.020556454130106;
-      r[17] =  0.686811031831200; s[17] = -0.701412405190965; w[17] = 0.020556454130106;
-      r[18] = -0.985398626640235; s[18] =  0.686811031831200; w[18] = 0.020556454130106;
-      r[19] =  0.686811031831200; s[19] = -0.985398626640235; w[19] = 0.020556454130106;
-      r[20] = -0.985398626640235; s[20] = -0.701412405190966; w[20] = 0.020556454130106;
-      r[21] = -0.701412405190966; s[21] = -0.985398626640235; w[21] = 0.020556454130106;
-      r[22] = -0.420944470627256; s[22] =  0.328932876191794; w[22] = 0.080668713854259;
-      r[23] =  0.328932876191794; s[23] = -0.420944470627256; w[23] = 0.080668713854259;
-      r[24] = -0.907988405564538; s[24] =  0.328932876191794; w[24] = 0.080668713854259;
-      r[25] =  0.328932876191794; s[25] = -0.907988405564538; w[25] = 0.080668713854259;
-      r[26] = -0.907988405564538; s[26] = -0.420944470627256; w[26] = 0.080668713854259;
-      r[27] = -0.420944470627256; s[27] = -0.907988405564538; w[27] = 0.080668713854259;
+      r[0] = -0.333333333333333;
+      s[0] = -0.333333333333333;
+      w[0] = 0.171542269659139;
+      r[1] = -0.008227986519701;
+      s[1] = -0.008227986519701;
+      w[1] = 0.033232309648099;
+      r[2] = -0.983544026960598;
+      s[2] = -0.008227986519701;
+      w[2] = 0.033232309648099;
+      r[3] = -0.008227986519701;
+      s[3] = -0.983544026960598;
+      w[3] = 0.033232309648099;
+      r[4] = -0.123062767323470;
+      s[4] = -0.123062767323470;
+      w[4] = 0.134650934561697;
+      r[5] = -0.753874465353061;
+      s[5] = -0.123062767323470;
+      w[5] = 0.134650934561697;
+      r[6] = -0.123062767323470;
+      s[6] = -0.753874465353061;
+      w[6] = 0.134650934561697;
+      r[7] = -0.579583807314522;
+      s[7] = -0.579583807314522;
+      w[7] = 0.141045284213931;
+      r[8] = 0.159167614629044;
+      s[8] = -0.579583807314522;
+      w[8] = 0.141045284213931;
+      r[9] = -0.579583807314522;
+      s[9] = 0.159167614629044;
+      w[9] = 0.141045284213931;
+      r[10] = -0.794793191450311;
+      s[10] = -0.794793191450311;
+      w[10] = 0.077255352409353;
+      r[11] = 0.589586382900622;
+      s[11] = -0.794793191450311;
+      w[11] = 0.077255352409353;
+      r[12] = -0.794793191450311;
+      s[12] = 0.589586382900622;
+      w[12] = 0.077255352409353;
+      r[13] = -0.943045809035533;
+      s[13] = -0.943045809035533;
+      w[13] = 0.020851693311810;
+      r[14] = 0.886091618071066;
+      s[14] = -0.943045809035533;
+      w[14] = 0.020851693311810;
+      r[15] = -0.943045809035533;
+      s[15] = 0.886091618071066;
+      w[15] = 0.020851693311810;
+      r[16] = -0.701412405190965;
+      s[16] = 0.686811031831200;
+      w[16] = 0.020556454130106;
+      r[17] = 0.686811031831200;
+      s[17] = -0.701412405190965;
+      w[17] = 0.020556454130106;
+      r[18] = -0.985398626640235;
+      s[18] = 0.686811031831200;
+      w[18] = 0.020556454130106;
+      r[19] = 0.686811031831200;
+      s[19] = -0.985398626640235;
+      w[19] = 0.020556454130106;
+      r[20] = -0.985398626640235;
+      s[20] = -0.701412405190966;
+      w[20] = 0.020556454130106;
+      r[21] = -0.701412405190966;
+      s[21] = -0.985398626640235;
+      w[21] = 0.020556454130106;
+      r[22] = -0.420944470627256;
+      s[22] = 0.328932876191794;
+      w[22] = 0.080668713854259;
+      r[23] = 0.328932876191794;
+      s[23] = -0.420944470627256;
+      w[23] = 0.080668713854259;
+      r[24] = -0.907988405564538;
+      s[24] = 0.328932876191794;
+      w[24] = 0.080668713854259;
+      r[25] = 0.328932876191794;
+      s[25] = -0.907988405564538;
+      w[25] = 0.080668713854259;
+      r[26] = -0.907988405564538;
+      s[26] = -0.420944470627256;
+      w[26] = 0.080668713854259;
+      r[27] = -0.420944470627256;
+      s[27] = -0.907988405564538;
+      w[27] = 0.080668713854259;
 
       break;
     }
     case 12: {
-      r[0]  = -0.115127288420454; s[0]  = -0.115127288420454; w[0]  = 0.088694050812375;
-      r[1]  = -0.769745423159092; s[1]  = -0.115127288420454; w[1]  = 0.088694050812375;
-      r[2]  = -0.115127288420454; s[2]  = -0.769745423159092; w[2]  = 0.088694050812375;
-      r[3]  = -0.241326933740970; s[3]  = -0.241326933740970; w[3]  = 0.083486638970495;
-      r[4]  = -0.517346132518060; s[4]  = -0.241326933740970; w[4]  = 0.083486638970495;
-      r[5]  = -0.241326933740970; s[5]  = -0.517346132518060; w[5]  = 0.083486638970495;
-      r[6]  = -0.773435586772427; s[6]  = -0.773435586772427; w[6]  = 0.061949370456958;
-      r[7]  =  0.546871173544855; s[7]  = -0.773435586772427; w[7]  = 0.061949370456958;
-      r[8]  = -0.773435586772427; s[8]  =  0.546871173544855; w[8]  = 0.061949370456958;
-      r[9]  = -0.550360151853422; s[9]  = -0.550360151853422; w[9]  = 0.096926744607805;
-      r[10] =  0.100720303706844; s[10] = -0.550360151853422; w[10] = 0.096926744607805;
-      r[11] = -0.550360151853422; s[11] =  0.100720303706844; w[11] = 0.096926744607805;
-      r[12] = -0.949850839686919; s[12] = -0.949850839686919; w[12] = 0.016284715813394;
-      r[13] =  0.899701679373837; s[13] = -0.949850839686919; w[13] = 0.016284715813394;
-      r[14] = -0.949850839686919; s[14] =  0.899701679373837; w[14] = 0.016284715813394;
-      r[15] = -0.023247583079632; s[15] = -0.023247583079632; w[15] = 0.047730162209543;
-      r[16] = -0.953504833840737; s[16] = -0.023247583079632; w[16] = 0.047730162209543;
-      r[17] = -0.023247583079632; s[17] = -0.953504833840737; w[17] = 0.047730162209543;
-      r[18] =  0.701114686742190; s[18] = -0.956341185792092; w[18] = 0.030740478172077;
-      r[19] = -0.956341185792092; s[19] =  0.701114686742190; w[19] = 0.030740478172077;
-      r[20] = -0.744773500950097; s[20] = -0.956341185792092; w[20] = 0.030740478172077;
-      r[21] = -0.956341185792092; s[21] = -0.744773500950097; w[21] = 0.030740478172077;
-      r[22] = -0.744773500950097; s[22] =  0.701114686742189; w[22] = 0.030740478172077;
-      r[23] =  0.701114686742189; s[23] = -0.744773500950097; w[23] = 0.030740478172077;
-      r[24] =  0.280974603820889; s[24] = -0.820754518409649; w[24] = 0.073364295183933;
-      r[25] = -0.820754518409649; s[25] =  0.280974603820889; w[25] = 0.073364295183933;
-      r[26] = -0.460220085411240; s[26] = -0.820754518409649; w[26] = 0.073364295183933;
-      r[27] = -0.820754518409649; s[27] = -0.460220085411240; w[27] = 0.073364295183933;
-      r[28] = -0.460220085411240; s[28] =  0.280974603820889; w[28] = 0.073364295183933;
-      r[29] =  0.280974603820889; s[29] = -0.460220085411240; w[29] = 0.073364295183933;
-      r[30] =  0.380092839755442; s[30] = -0.412599349012509; w[30] = 0.031692718542038;
-      r[31] = -0.412599349012509; s[31] =  0.380092839755442; w[31] = 0.031692718542038;
-      r[32] = -0.967493490742933; s[32] = -0.412599349012509; w[32] = 0.031692718542038;
-      r[33] = -0.412599349012509; s[33] = -0.967493490742933; w[33] = 0.031692718542038;
-      r[34] = -0.967493490742933; s[34] =  0.380092839755442; w[34] = 0.031692718542038;
-      r[35] =  0.380092839755442; s[35] = -0.967493490742933; w[35] = 0.031692718542038;
+      r[0] = -0.115127288420454;
+      s[0] = -0.115127288420454;
+      w[0] = 0.088694050812375;
+      r[1] = -0.769745423159092;
+      s[1] = -0.115127288420454;
+      w[1] = 0.088694050812375;
+      r[2] = -0.115127288420454;
+      s[2] = -0.769745423159092;
+      w[2] = 0.088694050812375;
+      r[3] = -0.241326933740970;
+      s[3] = -0.241326933740970;
+      w[3] = 0.083486638970495;
+      r[4] = -0.517346132518060;
+      s[4] = -0.241326933740970;
+      w[4] = 0.083486638970495;
+      r[5] = -0.241326933740970;
+      s[5] = -0.517346132518060;
+      w[5] = 0.083486638970495;
+      r[6] = -0.773435586772427;
+      s[6] = -0.773435586772427;
+      w[6] = 0.061949370456958;
+      r[7] = 0.546871173544855;
+      s[7] = -0.773435586772427;
+      w[7] = 0.061949370456958;
+      r[8] = -0.773435586772427;
+      s[8] = 0.546871173544855;
+      w[8] = 0.061949370456958;
+      r[9] = -0.550360151853422;
+      s[9] = -0.550360151853422;
+      w[9] = 0.096926744607805;
+      r[10] = 0.100720303706844;
+      s[10] = -0.550360151853422;
+      w[10] = 0.096926744607805;
+      r[11] = -0.550360151853422;
+      s[11] = 0.100720303706844;
+      w[11] = 0.096926744607805;
+      r[12] = -0.949850839686919;
+      s[12] = -0.949850839686919;
+      w[12] = 0.016284715813394;
+      r[13] = 0.899701679373837;
+      s[13] = -0.949850839686919;
+      w[13] = 0.016284715813394;
+      r[14] = -0.949850839686919;
+      s[14] = 0.899701679373837;
+      w[14] = 0.016284715813394;
+      r[15] = -0.023247583079632;
+      s[15] = -0.023247583079632;
+      w[15] = 0.047730162209543;
+      r[16] = -0.953504833840737;
+      s[16] = -0.023247583079632;
+      w[16] = 0.047730162209543;
+      r[17] = -0.023247583079632;
+      s[17] = -0.953504833840737;
+      w[17] = 0.047730162209543;
+      r[18] = 0.701114686742190;
+      s[18] = -0.956341185792092;
+      w[18] = 0.030740478172077;
+      r[19] = -0.956341185792092;
+      s[19] = 0.701114686742190;
+      w[19] = 0.030740478172077;
+      r[20] = -0.744773500950097;
+      s[20] = -0.956341185792092;
+      w[20] = 0.030740478172077;
+      r[21] = -0.956341185792092;
+      s[21] = -0.744773500950097;
+      w[21] = 0.030740478172077;
+      r[22] = -0.744773500950097;
+      s[22] = 0.701114686742189;
+      w[22] = 0.030740478172077;
+      r[23] = 0.701114686742189;
+      s[23] = -0.744773500950097;
+      w[23] = 0.030740478172077;
+      r[24] = 0.280974603820889;
+      s[24] = -0.820754518409649;
+      w[24] = 0.073364295183933;
+      r[25] = -0.820754518409649;
+      s[25] = 0.280974603820889;
+      w[25] = 0.073364295183933;
+      r[26] = -0.460220085411240;
+      s[26] = -0.820754518409649;
+      w[26] = 0.073364295183933;
+      r[27] = -0.820754518409649;
+      s[27] = -0.460220085411240;
+      w[27] = 0.073364295183933;
+      r[28] = -0.460220085411240;
+      s[28] = 0.280974603820889;
+      w[28] = 0.073364295183933;
+      r[29] = 0.280974603820889;
+      s[29] = -0.460220085411240;
+      w[29] = 0.073364295183933;
+      r[30] = 0.380092839755442;
+      s[30] = -0.412599349012509;
+      w[30] = 0.031692718542038;
+      r[31] = -0.412599349012509;
+      s[31] = 0.380092839755442;
+      w[31] = 0.031692718542038;
+      r[32] = -0.967493490742933;
+      s[32] = -0.412599349012509;
+      w[32] = 0.031692718542038;
+      r[33] = -0.412599349012509;
+      s[33] = -0.967493490742933;
+      w[33] = 0.031692718542038;
+      r[34] = -0.967493490742933;
+      s[34] = 0.380092839755442;
+      w[34] = 0.031692718542038;
+      r[35] = 0.380092839755442;
+      s[35] = -0.967493490742933;
+      w[35] = 0.031692718542038;
 
       break;
     }
     case 13: {
-      r[0]  = -0.333333333333333; s[0]  = -0.333333333333333; w[0]  = 0.097649880256618;
-      r[1]  = -0.178369512906405; s[1]  = -0.178369512906405; w[1]  = 0.090830392435257;
-      r[2]  = -0.643260974187191; s[2]  = -0.178369512906405; w[2]  = 0.090830392435257;
-      r[3]  = -0.178369512906405; s[3]  = -0.643260974187191; w[3]  = 0.090830392435257;
-      r[4]  = -0.542160866418819; s[4]  = -0.542160866418819; w[4]  = 0.093688172298398;
-      r[5]  =  0.084321732837639; s[5]  = -0.542160866418819; w[5]  = 0.093688172298398;
-      r[6]  = -0.542160866418819; s[6]  =  0.084321732837639; w[6]  = 0.093688172298398;
-      r[7]  = -0.771083702251175; s[7]  = -0.771083702251175; w[7]  = 0.062636625766914;
-      r[8]  =  0.542167404502350; s[8]  = -0.771083702251175; w[8]  = 0.062636625766914;
-      r[9]  = -0.771083702251175; s[9]  =  0.542167404502350; w[9]  = 0.062636625766914;
-      r[10] = -0.951222762153923; s[10] = -0.951222762153923; w[10] = 0.015384123058757;
-      r[11] =  0.902445524307847; s[11] = -0.951222762153923; w[11] = 0.015384123058757;
-      r[12] = -0.951222762153923; s[12] =  0.902445524307847; w[12] = 0.015384123058757;
-      r[13] = -0.071124044893491; s[13] = -0.071124044893491; w[13] = 0.063336411850675;
-      r[14] = -0.857751910213018; s[14] = -0.071124044893491; w[14] = 0.063336411850675;
-      r[15] = -0.071124044893491; s[15] = -0.857751910213018; w[15] = 0.063336411850675;
-      r[16] =  0.089497598920545; s[16] = -0.972567007080596; w[16] = 0.017363112895214;
-      r[17] = -0.972567007080596; s[17] =  0.089497598920545; w[17] = 0.017363112895214;
-      r[18] = -0.116930591839948; s[18] = -0.972567007080596; w[18] = 0.017363112895214;
-      r[19] = -0.972567007080596; s[19] = -0.116930591839948; w[19] = 0.017363112895214;
-      r[20] = -0.116930591839948; s[20] =  0.089497598920545; w[20] = 0.017363112895214;
-      r[21] =  0.089497598920545; s[21] = -0.116930591839948; w[21] = 0.017363112895214;
-      r[22] =  0.708303576893352; s[22] = -0.752827405974001; w[22] = 0.030203519313196;
-      r[23] = -0.752827405974001; s[23] =  0.708303576893352; w[23] = 0.030203519313196;
-      r[24] = -0.955476170919351; s[24] = -0.752827405974001; w[24] = 0.030203519313196;
-      r[25] = -0.752827405974001; s[25] = -0.955476170919351; w[25] = 0.030203519313196;
-      r[26] = -0.955476170919351; s[26] =  0.708303576893352; w[26] = 0.030203519313196;
-      r[27] =  0.708303576893352; s[27] = -0.955476170919351; w[27] = 0.030203519313196;
-      r[28] =  0.400693795223418; s[28] = -0.438009873048077; w[28] = 0.032954120635442;
-      r[29] = -0.438009873048077; s[29] =  0.400693795223418; w[29] = 0.032954120635442;
-      r[30] = -0.962683922175342; s[30] = -0.438009873048076; w[30] = 0.032954120635442;
-      r[31] = -0.438009873048076; s[31] = -0.962683922175342; w[31] = 0.032954120635442;
-      r[32] = -0.962683922175342; s[32] =  0.400693795223419; w[32] = 0.032954120635442;
-      r[33] =  0.400693795223419; s[33] = -0.962683922175342; w[33] = 0.032954120635442;
-      r[34] = -0.461147708177324; s[34] = -0.809703416305633; w[34] = 0.073599737741711;
-      r[35] = -0.809703416305633; s[35] = -0.461147708177324; w[35] = 0.073599737741711;
-      r[36] =  0.270851124482956; s[36] = -0.809703416305633; w[36] = 0.073599737741711;
-      r[37] = -0.809703416305633; s[37] =  0.270851124482956; w[37] = 0.073599737741711;
-      r[38] =  0.270851124482956; s[38] = -0.461147708177324; w[38] = 0.073599737741711;
-      r[39] = -0.461147708177324; s[39] =  0.270851124482956; w[39] = 0.073599737741711;
+      r[0] = -0.333333333333333;
+      s[0] = -0.333333333333333;
+      w[0] = 0.097649880256618;
+      r[1] = -0.178369512906405;
+      s[1] = -0.178369512906405;
+      w[1] = 0.090830392435257;
+      r[2] = -0.643260974187191;
+      s[2] = -0.178369512906405;
+      w[2] = 0.090830392435257;
+      r[3] = -0.178369512906405;
+      s[3] = -0.643260974187191;
+      w[3] = 0.090830392435257;
+      r[4] = -0.542160866418819;
+      s[4] = -0.542160866418819;
+      w[4] = 0.093688172298398;
+      r[5] = 0.084321732837639;
+      s[5] = -0.542160866418819;
+      w[5] = 0.093688172298398;
+      r[6] = -0.542160866418819;
+      s[6] = 0.084321732837639;
+      w[6] = 0.093688172298398;
+      r[7] = -0.771083702251175;
+      s[7] = -0.771083702251175;
+      w[7] = 0.062636625766914;
+      r[8] = 0.542167404502350;
+      s[8] = -0.771083702251175;
+      w[8] = 0.062636625766914;
+      r[9] = -0.771083702251175;
+      s[9] = 0.542167404502350;
+      w[9] = 0.062636625766914;
+      r[10] = -0.951222762153923;
+      s[10] = -0.951222762153923;
+      w[10] = 0.015384123058757;
+      r[11] = 0.902445524307847;
+      s[11] = -0.951222762153923;
+      w[11] = 0.015384123058757;
+      r[12] = -0.951222762153923;
+      s[12] = 0.902445524307847;
+      w[12] = 0.015384123058757;
+      r[13] = -0.071124044893491;
+      s[13] = -0.071124044893491;
+      w[13] = 0.063336411850675;
+      r[14] = -0.857751910213018;
+      s[14] = -0.071124044893491;
+      w[14] = 0.063336411850675;
+      r[15] = -0.071124044893491;
+      s[15] = -0.857751910213018;
+      w[15] = 0.063336411850675;
+      r[16] = 0.089497598920545;
+      s[16] = -0.972567007080596;
+      w[16] = 0.017363112895214;
+      r[17] = -0.972567007080596;
+      s[17] = 0.089497598920545;
+      w[17] = 0.017363112895214;
+      r[18] = -0.116930591839948;
+      s[18] = -0.972567007080596;
+      w[18] = 0.017363112895214;
+      r[19] = -0.972567007080596;
+      s[19] = -0.116930591839948;
+      w[19] = 0.017363112895214;
+      r[20] = -0.116930591839948;
+      s[20] = 0.089497598920545;
+      w[20] = 0.017363112895214;
+      r[21] = 0.089497598920545;
+      s[21] = -0.116930591839948;
+      w[21] = 0.017363112895214;
+      r[22] = 0.708303576893352;
+      s[22] = -0.752827405974001;
+      w[22] = 0.030203519313196;
+      r[23] = -0.752827405974001;
+      s[23] = 0.708303576893352;
+      w[23] = 0.030203519313196;
+      r[24] = -0.955476170919351;
+      s[24] = -0.752827405974001;
+      w[24] = 0.030203519313196;
+      r[25] = -0.752827405974001;
+      s[25] = -0.955476170919351;
+      w[25] = 0.030203519313196;
+      r[26] = -0.955476170919351;
+      s[26] = 0.708303576893352;
+      w[26] = 0.030203519313196;
+      r[27] = 0.708303576893352;
+      s[27] = -0.955476170919351;
+      w[27] = 0.030203519313196;
+      r[28] = 0.400693795223418;
+      s[28] = -0.438009873048077;
+      w[28] = 0.032954120635442;
+      r[29] = -0.438009873048077;
+      s[29] = 0.400693795223418;
+      w[29] = 0.032954120635442;
+      r[30] = -0.962683922175342;
+      s[30] = -0.438009873048076;
+      w[30] = 0.032954120635442;
+      r[31] = -0.438009873048076;
+      s[31] = -0.962683922175342;
+      w[31] = 0.032954120635442;
+      r[32] = -0.962683922175342;
+      s[32] = 0.400693795223419;
+      w[32] = 0.032954120635442;
+      r[33] = 0.400693795223419;
+      s[33] = -0.962683922175342;
+      w[33] = 0.032954120635442;
+      r[34] = -0.461147708177324;
+      s[34] = -0.809703416305633;
+      w[34] = 0.073599737741711;
+      r[35] = -0.809703416305633;
+      s[35] = -0.461147708177324;
+      w[35] = 0.073599737741711;
+      r[36] = 0.270851124482956;
+      s[36] = -0.809703416305633;
+      w[36] = 0.073599737741711;
+      r[37] = -0.809703416305633;
+      s[37] = 0.270851124482956;
+      w[37] = 0.073599737741711;
+      r[38] = 0.270851124482956;
+      s[38] = -0.461147708177324;
+      w[38] = 0.073599737741711;
+      r[39] = -0.461147708177324;
+      s[39] = 0.270851124482956;
+      w[39] = 0.073599737741711;
 
       break;
     }
     case 14: {
-      r[0]  = -0.333333333333333; s[0]  = -0.333333333333333; w[0]  = 0.086016161940337;
-      r[1]  = -0.031437623162377; s[1]  = -0.031437623162377; w[1]  = 0.020861042581505;
-      r[2]  = -0.937124753675245; s[2]  = -0.031437623162377; w[2]  = 0.020861042581505;
-      r[3]  = -0.031437623162377; s[3]  = -0.937124753675245; w[3]  = 0.020861042581505;
-      r[4]  = -0.190179067155837; s[4]  = -0.190179067155837; w[4]  = 0.084906577433761;
-      r[5]  = -0.619641865688325; s[5]  = -0.190179067155837; w[5]  = 0.084906577433761;
-      r[6]  = -0.190179067155837; s[6]  = -0.619641865688325; w[6]  = 0.084906577433761;
-      r[7]  = -0.544945017724160; s[7]  = -0.544945017724160; w[7]  = 0.094412955694385;
-      r[8]  =  0.089890035448320; s[8]  = -0.544945017724160; w[8]  = 0.094412955694385;
-      r[9]  = -0.544945017724160; s[9]  =  0.089890035448320; w[9]  = 0.094412955694385;
-      r[10] = -0.829084434528895; s[10] = -0.829084434528895; w[10] = 0.036931420530108;
-      r[11] =  0.658168869057790; s[11] = -0.829084434528895; w[11] = 0.036931420530108;
-      r[12] = -0.829084434528895; s[12] =  0.658168869057790; w[12] = 0.036931420530108;
-      r[13] = -0.961731843229187; s[13] = -0.961731843229187; w[13] = 0.009566859223433;
-      r[14] =  0.923463686458374; s[14] = -0.961731843229187; w[14] = 0.009566859223433;
-      r[15] = -0.961731843229187; s[15] =  0.923463686458374; w[15] = 0.009566859223433;
-      r[16] = -0.228055909294146; s[16] =  0.200257489743243; w[16] = 0.023873332102599;
-      r[17] =  0.200257489743243; s[17] = -0.228055909294146; w[17] = 0.023873332102599;
-      r[18] = -0.972201580449098; s[18] =  0.200257489743243; w[18] = 0.023873332102599;
-      r[19] =  0.200257489743243; s[19] = -0.972201580449098; w[19] = 0.023873332102599;
-      r[20] = -0.972201580449097; s[20] = -0.228055909294146; w[20] = 0.023873332102599;
-      r[21] = -0.228055909294146; s[21] = -0.972201580449097; w[21] = 0.023873332102599;
-      r[22] = -0.801926305237733; s[22] =  0.769518568627872; w[22] = 0.018006541968931;
-      r[23] =  0.769518568627872; s[23] = -0.801926305237733; w[23] = 0.018006541968931;
-      r[24] = -0.967592263390139; s[24] =  0.769518568627872; w[24] = 0.018006541968931;
-      r[25] =  0.769518568627872; s[25] = -0.967592263390139; w[25] = 0.018006541968931;
-      r[26] = -0.967592263390139; s[26] = -0.801926305237733; w[26] = 0.018006541968931;
-      r[27] = -0.801926305237733; s[27] = -0.967592263390139; w[27] = 0.018006541968931;
-      r[28] = -0.544893784145096; s[28] =  0.504355701557747; w[28] = 0.030117913357456;
-      r[29] =  0.504355701557747; s[29] = -0.544893784145096; w[29] = 0.030117913357456;
-      r[30] = -0.959461917412651; s[30] =  0.504355701557747; w[30] = 0.030117913357456;
-      r[31] =  0.504355701557747; s[31] = -0.959461917412651; w[31] = 0.030117913357456;
-      r[32] = -0.959461917412651; s[32] = -0.544893784145095; w[32] = 0.030117913357456;
-      r[33] = -0.544893784145095; s[33] = -0.959461917412651; w[33] = 0.030117913357456;
-      r[34] = -0.288429073961769; s[34] =  0.109399611316741; w[34] = 0.067035335144205;
-      r[35] =  0.109399611316741; s[35] = -0.288429073961769; w[35] = 0.067035335144205;
-      r[36] = -0.820970537354972; s[36] =  0.109399611316741; w[36] = 0.067035335144205;
-      r[37] =  0.109399611316741; s[37] = -0.820970537354972; w[37] = 0.067035335144205;
-      r[38] = -0.820970537354972; s[38] = -0.288429073961769; w[38] = 0.067035335144205;
-      r[39] = -0.288429073961769; s[39] = -0.820970537354972; w[39] = 0.067035335144205;
-      r[40] = -0.593507885280605; s[40] =  0.397658756992448; w[40] = 0.056624756038490;
-      r[41] =  0.397658756992448; s[41] = -0.593507885280605; w[41] = 0.056624756038490;
-      r[42] = -0.804150871711842; s[42] =  0.397658756992447; w[42] = 0.056624756038490;
-      r[43] =  0.397658756992447; s[43] = -0.804150871711842; w[43] = 0.056624756038490;
-      r[44] = -0.804150871711842; s[44] = -0.593507885280605; w[44] = 0.056624756038490;
-      r[45] = -0.593507885280605; s[45] = -0.804150871711842; w[45] = 0.056624756038490;
+      r[0] = -0.333333333333333;
+      s[0] = -0.333333333333333;
+      w[0] = 0.086016161940337;
+      r[1] = -0.031437623162377;
+      s[1] = -0.031437623162377;
+      w[1] = 0.020861042581505;
+      r[2] = -0.937124753675245;
+      s[2] = -0.031437623162377;
+      w[2] = 0.020861042581505;
+      r[3] = -0.031437623162377;
+      s[3] = -0.937124753675245;
+      w[3] = 0.020861042581505;
+      r[4] = -0.190179067155837;
+      s[4] = -0.190179067155837;
+      w[4] = 0.084906577433761;
+      r[5] = -0.619641865688325;
+      s[5] = -0.190179067155837;
+      w[5] = 0.084906577433761;
+      r[6] = -0.190179067155837;
+      s[6] = -0.619641865688325;
+      w[6] = 0.084906577433761;
+      r[7] = -0.544945017724160;
+      s[7] = -0.544945017724160;
+      w[7] = 0.094412955694385;
+      r[8] = 0.089890035448320;
+      s[8] = -0.544945017724160;
+      w[8] = 0.094412955694385;
+      r[9] = -0.544945017724160;
+      s[9] = 0.089890035448320;
+      w[9] = 0.094412955694385;
+      r[10] = -0.829084434528895;
+      s[10] = -0.829084434528895;
+      w[10] = 0.036931420530108;
+      r[11] = 0.658168869057790;
+      s[11] = -0.829084434528895;
+      w[11] = 0.036931420530108;
+      r[12] = -0.829084434528895;
+      s[12] = 0.658168869057790;
+      w[12] = 0.036931420530108;
+      r[13] = -0.961731843229187;
+      s[13] = -0.961731843229187;
+      w[13] = 0.009566859223433;
+      r[14] = 0.923463686458374;
+      s[14] = -0.961731843229187;
+      w[14] = 0.009566859223433;
+      r[15] = -0.961731843229187;
+      s[15] = 0.923463686458374;
+      w[15] = 0.009566859223433;
+      r[16] = -0.228055909294146;
+      s[16] = 0.200257489743243;
+      w[16] = 0.023873332102599;
+      r[17] = 0.200257489743243;
+      s[17] = -0.228055909294146;
+      w[17] = 0.023873332102599;
+      r[18] = -0.972201580449098;
+      s[18] = 0.200257489743243;
+      w[18] = 0.023873332102599;
+      r[19] = 0.200257489743243;
+      s[19] = -0.972201580449098;
+      w[19] = 0.023873332102599;
+      r[20] = -0.972201580449097;
+      s[20] = -0.228055909294146;
+      w[20] = 0.023873332102599;
+      r[21] = -0.228055909294146;
+      s[21] = -0.972201580449097;
+      w[21] = 0.023873332102599;
+      r[22] = -0.801926305237733;
+      s[22] = 0.769518568627872;
+      w[22] = 0.018006541968931;
+      r[23] = 0.769518568627872;
+      s[23] = -0.801926305237733;
+      w[23] = 0.018006541968931;
+      r[24] = -0.967592263390139;
+      s[24] = 0.769518568627872;
+      w[24] = 0.018006541968931;
+      r[25] = 0.769518568627872;
+      s[25] = -0.967592263390139;
+      w[25] = 0.018006541968931;
+      r[26] = -0.967592263390139;
+      s[26] = -0.801926305237733;
+      w[26] = 0.018006541968931;
+      r[27] = -0.801926305237733;
+      s[27] = -0.967592263390139;
+      w[27] = 0.018006541968931;
+      r[28] = -0.544893784145096;
+      s[28] = 0.504355701557747;
+      w[28] = 0.030117913357456;
+      r[29] = 0.504355701557747;
+      s[29] = -0.544893784145096;
+      w[29] = 0.030117913357456;
+      r[30] = -0.959461917412651;
+      s[30] = 0.504355701557747;
+      w[30] = 0.030117913357456;
+      r[31] = 0.504355701557747;
+      s[31] = -0.959461917412651;
+      w[31] = 0.030117913357456;
+      r[32] = -0.959461917412651;
+      s[32] = -0.544893784145095;
+      w[32] = 0.030117913357456;
+      r[33] = -0.544893784145095;
+      s[33] = -0.959461917412651;
+      w[33] = 0.030117913357456;
+      r[34] = -0.288429073961769;
+      s[34] = 0.109399611316741;
+      w[34] = 0.067035335144205;
+      r[35] = 0.109399611316741;
+      s[35] = -0.288429073961769;
+      w[35] = 0.067035335144205;
+      r[36] = -0.820970537354972;
+      s[36] = 0.109399611316741;
+      w[36] = 0.067035335144205;
+      r[37] = 0.109399611316741;
+      s[37] = -0.820970537354972;
+      w[37] = 0.067035335144205;
+      r[38] = -0.820970537354972;
+      s[38] = -0.288429073961769;
+      w[38] = 0.067035335144205;
+      r[39] = -0.288429073961769;
+      s[39] = -0.820970537354972;
+      w[39] = 0.067035335144205;
+      r[40] = -0.593507885280605;
+      s[40] = 0.397658756992448;
+      w[40] = 0.056624756038490;
+      r[41] = 0.397658756992448;
+      s[41] = -0.593507885280605;
+      w[41] = 0.056624756038490;
+      r[42] = -0.804150871711842;
+      s[42] = 0.397658756992447;
+      w[42] = 0.056624756038490;
+      r[43] = 0.397658756992447;
+      s[43] = -0.804150871711842;
+      w[43] = 0.056624756038490;
+      r[44] = -0.804150871711842;
+      s[44] = -0.593507885280605;
+      w[44] = 0.056624756038490;
+      r[45] = -0.593507885280605;
+      s[45] = -0.804150871711842;
+      w[45] = 0.056624756038490;
 
       break;
     }
     case 15: {
-      r[0]  = -0.083438407261750; s[0]  = -0.083438407261750; w[0]  = 0.065323637697611;
-      r[1]  = -0.833123185476500; s[1]  = -0.083438407261750; w[1]  = 0.065323637697611;
-      r[2]  = -0.083438407261750; s[2]  = -0.833123185476500; w[2]  = 0.065323637697611;
-      r[3]  = -0.192779070841739; s[3]  = -0.192779070841739; w[3]  = 0.054825636062729;
-      r[4]  = -0.614441858316522; s[4]  = -0.192779070841739; w[4]  = 0.054825636062729;
-      r[5]  = -0.192779070841739; s[5]  = -0.614441858316522; w[5]  = 0.054825636062729;
-      r[6]  = -0.413605664173949; s[6]  = -0.413605664173949; w[6]  = 0.053020073197407;
-      r[7]  = -0.172788671652101; s[7]  = -0.413605664173949; w[7]  = 0.053020073197407;
-      r[8]  = -0.413605664173949; s[8]  = -0.172788671652101; w[8]  = 0.053020073197407;
-      r[9]  = -0.707064426114454; s[9]  = -0.707064426114454; w[9]  = 0.058431924272972;
-      r[10] =  0.414128852228908; s[10] = -0.707064426114454; w[10] = 0.058431924272972;
-      r[11] = -0.707064426114454; s[11] =  0.414128852228908; w[11] = 0.058431924272972;
-      r[12] = -0.887274264668793; s[12] = -0.887274264668793; w[12] = 0.021169216132488;
-      r[13] =  0.774548529337586; s[13] = -0.887274264668793; w[13] = 0.021169216132488;
-      r[14] = -0.887274264668793; s[14] =  0.774548529337586; w[14] = 0.021169216132488;
-      r[15] = -0.966849746283259; s[15] = -0.966849746283259; w[15] = 0.007229286128184;
-      r[16] =  0.933699492566519; s[16] = -0.966849746283259; w[16] = 0.007229286128184;
-      r[17] = -0.966849746283259; s[17] =  0.933699492566519; w[17] = 0.007229286128184;
-      r[18] = -0.520930891690411; s[18] =  0.501106485071962; w[18] = 0.017055496203419;
-      r[19] =  0.501106485071962; s[19] = -0.520930891690411; w[19] = 0.017055496203419;
-      r[20] = -0.980175593381550; s[20] =  0.501106485071962; w[20] = 0.017055496203419;
-      r[21] =  0.501106485071962; s[21] = -0.980175593381550; w[21] = 0.017055496203419;
-      r[22] = -0.980175593381550; s[22] = -0.520930891690411; w[22] = 0.017055496203419;
-      r[23] = -0.520930891690411; s[23] = -0.980175593381550; w[23] = 0.017055496203419;
-      r[24] = -0.190242385363320; s[24] =  0.158634844102864; w[24] = 0.027832353033384;
-      r[25] =  0.158634844102864; s[25] = -0.190242385363320; w[25] = 0.027832353033384;
-      r[26] = -0.968392458739544; s[26] =  0.158634844102864; w[26] = 0.027832353033384;
-      r[27] =  0.158634844102864; s[27] = -0.968392458739544; w[27] = 0.027832353033384;
-      r[28] = -0.968392458739544; s[28] = -0.190242385363320; w[28] = 0.027832353033384;
-      r[29] = -0.190242385363320; s[29] = -0.968392458739544; w[29] = 0.027832353033384;
-      r[30] = -0.809995773773910; s[30] =  0.799708556139969; w[30] = 0.008583865881470;
-      r[31] =  0.799708556139969; s[31] = -0.809995773773910; w[31] = 0.008583865881470;
-      r[32] = -0.989712782366059; s[32] =  0.799708556139969; w[32] = 0.008583865881470;
-      r[33] =  0.799708556139969; s[33] = -0.989712782366059; w[33] = 0.008583865881470;
-      r[34] = -0.989712782366059; s[34] = -0.809995773773910; w[34] = 0.008583865881470;
-      r[35] = -0.809995773773910; s[35] = -0.989712782366059; w[35] = 0.008583865881470;
-      r[36] = -0.700493785355452; s[36] =  0.602649133849474; w[36] = 0.032470658563550;
-      r[37] =  0.602649133849474; s[37] = -0.700493785355452; w[37] = 0.032470658563550;
-      r[38] = -0.902155348494022; s[38] =  0.602649133849474; w[38] = 0.032470658563550;
-      r[39] =  0.602649133849474; s[39] = -0.902155348494022; w[39] = 0.032470658563550;
-      r[40] = -0.902155348494023; s[40] = -0.700493785355452; w[40] = 0.032470658563550;
-      r[41] = -0.700493785355452; s[41] = -0.902155348494023; w[41] = 0.032470658563550;
-      r[42] = -0.426160775117330; s[42] =  0.288623277852292; w[42] = 0.051214681842525;
-      r[43] =  0.288623277852292; s[43] = -0.426160775117330; w[43] = 0.051214681842525;
-      r[44] = -0.862462502734962; s[44] =  0.288623277852292; w[44] = 0.051214681842525;
-      r[45] =  0.288623277852292; s[45] = -0.862462502734962; w[45] = 0.051214681842525;
-      r[46] = -0.862462502734962; s[46] = -0.426160775117330; w[46] = 0.051214681842525;
-      r[47] = -0.426160775117330; s[47] = -0.862462502734962; w[47] = 0.051214681842525;
-      r[48] = -0.436328663801831; s[48] =  0.099519827552432; w[48] = 0.066176391063291;
-      r[49] =  0.099519827552432; s[49] = -0.436328663801831; w[49] = 0.066176391063291;
-      r[50] = -0.663191163750602; s[50] =  0.099519827552432; w[50] = 0.066176391063291;
-      r[51] =  0.099519827552432; s[51] = -0.663191163750602; w[51] = 0.066176391063291;
-      r[52] = -0.663191163750602; s[52] = -0.436328663801831; w[52] = 0.066176391063291;
-      r[53] = -0.436328663801831; s[53] = -0.663191163750602; w[53] = 0.066176391063291;
+      r[0] = -0.083438407261750;
+      s[0] = -0.083438407261750;
+      w[0] = 0.065323637697611;
+      r[1] = -0.833123185476500;
+      s[1] = -0.083438407261750;
+      w[1] = 0.065323637697611;
+      r[2] = -0.083438407261750;
+      s[2] = -0.833123185476500;
+      w[2] = 0.065323637697611;
+      r[3] = -0.192779070841739;
+      s[3] = -0.192779070841739;
+      w[3] = 0.054825636062729;
+      r[4] = -0.614441858316522;
+      s[4] = -0.192779070841739;
+      w[4] = 0.054825636062729;
+      r[5] = -0.192779070841739;
+      s[5] = -0.614441858316522;
+      w[5] = 0.054825636062729;
+      r[6] = -0.413605664173949;
+      s[6] = -0.413605664173949;
+      w[6] = 0.053020073197407;
+      r[7] = -0.172788671652101;
+      s[7] = -0.413605664173949;
+      w[7] = 0.053020073197407;
+      r[8] = -0.413605664173949;
+      s[8] = -0.172788671652101;
+      w[8] = 0.053020073197407;
+      r[9] = -0.707064426114454;
+      s[9] = -0.707064426114454;
+      w[9] = 0.058431924272972;
+      r[10] = 0.414128852228908;
+      s[10] = -0.707064426114454;
+      w[10] = 0.058431924272972;
+      r[11] = -0.707064426114454;
+      s[11] = 0.414128852228908;
+      w[11] = 0.058431924272972;
+      r[12] = -0.887274264668793;
+      s[12] = -0.887274264668793;
+      w[12] = 0.021169216132488;
+      r[13] = 0.774548529337586;
+      s[13] = -0.887274264668793;
+      w[13] = 0.021169216132488;
+      r[14] = -0.887274264668793;
+      s[14] = 0.774548529337586;
+      w[14] = 0.021169216132488;
+      r[15] = -0.966849746283259;
+      s[15] = -0.966849746283259;
+      w[15] = 0.007229286128184;
+      r[16] = 0.933699492566519;
+      s[16] = -0.966849746283259;
+      w[16] = 0.007229286128184;
+      r[17] = -0.966849746283259;
+      s[17] = 0.933699492566519;
+      w[17] = 0.007229286128184;
+      r[18] = -0.520930891690411;
+      s[18] = 0.501106485071962;
+      w[18] = 0.017055496203419;
+      r[19] = 0.501106485071962;
+      s[19] = -0.520930891690411;
+      w[19] = 0.017055496203419;
+      r[20] = -0.980175593381550;
+      s[20] = 0.501106485071962;
+      w[20] = 0.017055496203419;
+      r[21] = 0.501106485071962;
+      s[21] = -0.980175593381550;
+      w[21] = 0.017055496203419;
+      r[22] = -0.980175593381550;
+      s[22] = -0.520930891690411;
+      w[22] = 0.017055496203419;
+      r[23] = -0.520930891690411;
+      s[23] = -0.980175593381550;
+      w[23] = 0.017055496203419;
+      r[24] = -0.190242385363320;
+      s[24] = 0.158634844102864;
+      w[24] = 0.027832353033384;
+      r[25] = 0.158634844102864;
+      s[25] = -0.190242385363320;
+      w[25] = 0.027832353033384;
+      r[26] = -0.968392458739544;
+      s[26] = 0.158634844102864;
+      w[26] = 0.027832353033384;
+      r[27] = 0.158634844102864;
+      s[27] = -0.968392458739544;
+      w[27] = 0.027832353033384;
+      r[28] = -0.968392458739544;
+      s[28] = -0.190242385363320;
+      w[28] = 0.027832353033384;
+      r[29] = -0.190242385363320;
+      s[29] = -0.968392458739544;
+      w[29] = 0.027832353033384;
+      r[30] = -0.809995773773910;
+      s[30] = 0.799708556139969;
+      w[30] = 0.008583865881470;
+      r[31] = 0.799708556139969;
+      s[31] = -0.809995773773910;
+      w[31] = 0.008583865881470;
+      r[32] = -0.989712782366059;
+      s[32] = 0.799708556139969;
+      w[32] = 0.008583865881470;
+      r[33] = 0.799708556139969;
+      s[33] = -0.989712782366059;
+      w[33] = 0.008583865881470;
+      r[34] = -0.989712782366059;
+      s[34] = -0.809995773773910;
+      w[34] = 0.008583865881470;
+      r[35] = -0.809995773773910;
+      s[35] = -0.989712782366059;
+      w[35] = 0.008583865881470;
+      r[36] = -0.700493785355452;
+      s[36] = 0.602649133849474;
+      w[36] = 0.032470658563550;
+      r[37] = 0.602649133849474;
+      s[37] = -0.700493785355452;
+      w[37] = 0.032470658563550;
+      r[38] = -0.902155348494022;
+      s[38] = 0.602649133849474;
+      w[38] = 0.032470658563550;
+      r[39] = 0.602649133849474;
+      s[39] = -0.902155348494022;
+      w[39] = 0.032470658563550;
+      r[40] = -0.902155348494023;
+      s[40] = -0.700493785355452;
+      w[40] = 0.032470658563550;
+      r[41] = -0.700493785355452;
+      s[41] = -0.902155348494023;
+      w[41] = 0.032470658563550;
+      r[42] = -0.426160775117330;
+      s[42] = 0.288623277852292;
+      w[42] = 0.051214681842525;
+      r[43] = 0.288623277852292;
+      s[43] = -0.426160775117330;
+      w[43] = 0.051214681842525;
+      r[44] = -0.862462502734962;
+      s[44] = 0.288623277852292;
+      w[44] = 0.051214681842525;
+      r[45] = 0.288623277852292;
+      s[45] = -0.862462502734962;
+      w[45] = 0.051214681842525;
+      r[46] = -0.862462502734962;
+      s[46] = -0.426160775117330;
+      w[46] = 0.051214681842525;
+      r[47] = -0.426160775117330;
+      s[47] = -0.862462502734962;
+      w[47] = 0.051214681842525;
+      r[48] = -0.436328663801831;
+      s[48] = 0.099519827552432;
+      w[48] = 0.066176391063291;
+      r[49] = 0.099519827552432;
+      s[49] = -0.436328663801831;
+      w[49] = 0.066176391063291;
+      r[50] = -0.663191163750602;
+      s[50] = 0.099519827552432;
+      w[50] = 0.066176391063291;
+      r[51] = 0.099519827552432;
+      s[51] = -0.663191163750602;
+      w[51] = 0.066176391063291;
+      r[52] = -0.663191163750602;
+      s[52] = -0.436328663801831;
+      w[52] = 0.066176391063291;
+      r[53] = -0.436328663801831;
+      s[53] = -0.663191163750602;
+      w[53] = 0.066176391063291;
 
       break;
     }
     case 16: {
-      r[0]  = -0.333333333333333; s[0]  = -0.333333333333333; w[0]  = 0.092421202321849;
-      r[1]  = -0.015796436959213; s[1]  = -0.015796436959213; w[1]  = 0.027991652734724;
-      r[2]  = -0.968407126081574; s[2]  = -0.015796436959213; w[2]  = 0.027991652734724;
-      r[3]  = -0.015796436959213; s[3]  = -0.968407126081574; w[3]  = 0.027991652734724;
-      r[4]  = -0.087376299046785; s[4]  = -0.087376299046785; w[4]  = 0.036406763596424;
-      r[5]  = -0.825247401906431; s[5]  = -0.087376299046785; w[5]  = 0.036406763596424;
-      r[6]  = -0.087376299046785; s[6]  = -0.825247401906431; w[6]  = 0.036406763596424;
-      r[7]  = -0.640498098534045; s[7]  = -0.640498098534045; w[7]  = 0.062729423327251;
-      r[8]  =  0.280996197068091; s[8]  = -0.640498098534045; w[8]  = 0.062729423327251;
-      r[9]  = -0.640498098534045; s[9]  =  0.280996197068091; w[9]  = 0.062729423327251;
-      r[10] = -0.828211591878549; s[10] = -0.828211591878549; w[10] = 0.032217170192673;
-      r[11] =  0.656423183757099; s[11] = -0.828211591878549; w[11] = 0.032217170192673;
-      r[12] = -0.828211591878549; s[12] =  0.656423183757099; w[12] = 0.032217170192673;
-      r[13] = -0.977882767295650; s[13] = -0.977882767295650; w[13] = 0.003676792575648;
-      r[14] =  0.955765534591299; s[14] = -0.977882767295650; w[14] = 0.003676792575648;
-      r[15] = -0.977882767295650; s[15] =  0.955765534591299; w[15] = 0.003676792575648;
-      r[16] = -0.648594849699253; s[16] =  0.619534954455185; w[16] = 0.019075686313307;
-      r[17] =  0.619534954455185; s[17] = -0.648594849699253; w[17] = 0.019075686313307;
-      r[18] = -0.970940104755933; s[18] =  0.619534954455185; w[18] = 0.019075686313307;
-      r[19] =  0.619534954455185; s[19] = -0.970940104755933; w[19] = 0.019075686313307;
-      r[20] = -0.970940104755933; s[20] = -0.648594849699253; w[20] = 0.019075686313307;
-      r[21] = -0.648594849699253; s[21] = -0.970940104755933; w[21] = 0.019075686313307;
-      r[22] = -0.355089058161032; s[22] =  0.324703448463838; w[22] = 0.025111336723323;
-      r[23] =  0.324703448463838; s[23] = -0.355089058161032; w[23] = 0.025111336723323;
-      r[24] = -0.969614390302806; s[24] =  0.324703448463838; w[24] = 0.025111336723323;
-      r[25] =  0.324703448463838; s[25] = -0.969614390302806; w[25] = 0.025111336723323;
-      r[26] = -0.969614390302806; s[26] = -0.355089058161032; w[26] = 0.025111336723323;
-      r[27] = -0.355089058161032; s[27] = -0.969614390302806; w[27] = 0.025111336723323;
-      r[28] = -0.863082725186344; s[28] =  0.829810165174004; w[28] = 0.014134510743040;
-      r[29] =  0.829810165174004; s[29] = -0.863082725186344; w[29] = 0.014134510743040;
-      r[30] = -0.966727439987660; s[30] =  0.829810165174004; w[30] = 0.014134510743040;
-      r[31] =  0.829810165174004; s[31] = -0.966727439987660; w[31] = 0.014134510743040;
-      r[32] = -0.966727439987660; s[32] = -0.863082725186344; w[32] = 0.014134510743040;
-      r[33] = -0.863082725186344; s[33] = -0.966727439987660; w[33] = 0.014134510743040;
-      r[34] = -0.650110471151428; s[34] =  0.511910525190604; w[34] = 0.025255543672496;
-      r[35] =  0.511910525190604; s[35] = -0.650110471151428; w[35] = 0.025255543672496;
-      r[36] = -0.861800054039176; s[36] =  0.511910525190604; w[36] = 0.025255543672496;
-      r[37] =  0.511910525190604; s[37] = -0.861800054039176; w[37] = 0.025255543672496;
-      r[38] = -0.861800054039176; s[38] = -0.650110471151428; w[38] = 0.025255543672496;
-      r[39] = -0.650110471151428; s[39] = -0.861800054039176; w[39] = 0.025255543672496;
-      r[40] = -0.282624366842035; s[40] =  0.131065359625217; w[40] = 0.038432852520849;
-      r[41] =  0.131065359625217; s[41] = -0.282624366842035; w[41] = 0.038432852520849;
-      r[42] = -0.848440992783182; s[42] =  0.131065359625217; w[42] = 0.038432852520849;
-      r[43] =  0.131065359625217; s[43] = -0.848440992783182; w[43] = 0.038432852520849;
-      r[44] = -0.848440992783182; s[44] = -0.282624366842035; w[44] = 0.038432852520849;
-      r[45] = -0.282624366842035; s[45] = -0.848440992783182; w[45] = 0.038432852520849;
-      r[46] = -0.500121711290305; s[46] =  0.333566061453817; w[46] = 0.032993291211606;
-      r[47] =  0.333566061453817; s[47] = -0.500121711290305; w[47] = 0.032993291211606;
-      r[48] = -0.833444350163512; s[48] =  0.333566061453817; w[48] = 0.032993291211606;
-      r[49] =  0.333566061453817; s[49] = -0.833444350163512; w[49] = 0.032993291211606;
-      r[50] = -0.833444350163512; s[50] = -0.500121711290305; w[50] = 0.032993291211606;
-      r[51] = -0.500121711290305; s[51] = -0.833444350163512; w[51] = 0.032993291211606;
-      r[52] = -0.353308953197778; s[52] = -0.027538833736648; w[52] = 0.081415677215044;
-      r[53] = -0.027538833736648; s[53] = -0.353308953197778; w[53] = 0.081415677215044;
-      r[54] = -0.619152213065573; s[54] = -0.027538833736648; w[54] = 0.081415677215044;
-      r[55] = -0.027538833736648; s[55] = -0.619152213065573; w[55] = 0.081415677215044;
-      r[56] = -0.619152213065573; s[56] = -0.353308953197778; w[56] = 0.081415677215044;
-      r[57] = -0.353308953197778; s[57] = -0.619152213065573; w[57] = 0.081415677215044;
+      r[0] = -0.333333333333333;
+      s[0] = -0.333333333333333;
+      w[0] = 0.092421202321849;
+      r[1] = -0.015796436959213;
+      s[1] = -0.015796436959213;
+      w[1] = 0.027991652734724;
+      r[2] = -0.968407126081574;
+      s[2] = -0.015796436959213;
+      w[2] = 0.027991652734724;
+      r[3] = -0.015796436959213;
+      s[3] = -0.968407126081574;
+      w[3] = 0.027991652734724;
+      r[4] = -0.087376299046785;
+      s[4] = -0.087376299046785;
+      w[4] = 0.036406763596424;
+      r[5] = -0.825247401906431;
+      s[5] = -0.087376299046785;
+      w[5] = 0.036406763596424;
+      r[6] = -0.087376299046785;
+      s[6] = -0.825247401906431;
+      w[6] = 0.036406763596424;
+      r[7] = -0.640498098534045;
+      s[7] = -0.640498098534045;
+      w[7] = 0.062729423327251;
+      r[8] = 0.280996197068091;
+      s[8] = -0.640498098534045;
+      w[8] = 0.062729423327251;
+      r[9] = -0.640498098534045;
+      s[9] = 0.280996197068091;
+      w[9] = 0.062729423327251;
+      r[10] = -0.828211591878549;
+      s[10] = -0.828211591878549;
+      w[10] = 0.032217170192673;
+      r[11] = 0.656423183757099;
+      s[11] = -0.828211591878549;
+      w[11] = 0.032217170192673;
+      r[12] = -0.828211591878549;
+      s[12] = 0.656423183757099;
+      w[12] = 0.032217170192673;
+      r[13] = -0.977882767295650;
+      s[13] = -0.977882767295650;
+      w[13] = 0.003676792575648;
+      r[14] = 0.955765534591299;
+      s[14] = -0.977882767295650;
+      w[14] = 0.003676792575648;
+      r[15] = -0.977882767295650;
+      s[15] = 0.955765534591299;
+      w[15] = 0.003676792575648;
+      r[16] = -0.648594849699253;
+      s[16] = 0.619534954455185;
+      w[16] = 0.019075686313307;
+      r[17] = 0.619534954455185;
+      s[17] = -0.648594849699253;
+      w[17] = 0.019075686313307;
+      r[18] = -0.970940104755933;
+      s[18] = 0.619534954455185;
+      w[18] = 0.019075686313307;
+      r[19] = 0.619534954455185;
+      s[19] = -0.970940104755933;
+      w[19] = 0.019075686313307;
+      r[20] = -0.970940104755933;
+      s[20] = -0.648594849699253;
+      w[20] = 0.019075686313307;
+      r[21] = -0.648594849699253;
+      s[21] = -0.970940104755933;
+      w[21] = 0.019075686313307;
+      r[22] = -0.355089058161032;
+      s[22] = 0.324703448463838;
+      w[22] = 0.025111336723323;
+      r[23] = 0.324703448463838;
+      s[23] = -0.355089058161032;
+      w[23] = 0.025111336723323;
+      r[24] = -0.969614390302806;
+      s[24] = 0.324703448463838;
+      w[24] = 0.025111336723323;
+      r[25] = 0.324703448463838;
+      s[25] = -0.969614390302806;
+      w[25] = 0.025111336723323;
+      r[26] = -0.969614390302806;
+      s[26] = -0.355089058161032;
+      w[26] = 0.025111336723323;
+      r[27] = -0.355089058161032;
+      s[27] = -0.969614390302806;
+      w[27] = 0.025111336723323;
+      r[28] = -0.863082725186344;
+      s[28] = 0.829810165174004;
+      w[28] = 0.014134510743040;
+      r[29] = 0.829810165174004;
+      s[29] = -0.863082725186344;
+      w[29] = 0.014134510743040;
+      r[30] = -0.966727439987660;
+      s[30] = 0.829810165174004;
+      w[30] = 0.014134510743040;
+      r[31] = 0.829810165174004;
+      s[31] = -0.966727439987660;
+      w[31] = 0.014134510743040;
+      r[32] = -0.966727439987660;
+      s[32] = -0.863082725186344;
+      w[32] = 0.014134510743040;
+      r[33] = -0.863082725186344;
+      s[33] = -0.966727439987660;
+      w[33] = 0.014134510743040;
+      r[34] = -0.650110471151428;
+      s[34] = 0.511910525190604;
+      w[34] = 0.025255543672496;
+      r[35] = 0.511910525190604;
+      s[35] = -0.650110471151428;
+      w[35] = 0.025255543672496;
+      r[36] = -0.861800054039176;
+      s[36] = 0.511910525190604;
+      w[36] = 0.025255543672496;
+      r[37] = 0.511910525190604;
+      s[37] = -0.861800054039176;
+      w[37] = 0.025255543672496;
+      r[38] = -0.861800054039176;
+      s[38] = -0.650110471151428;
+      w[38] = 0.025255543672496;
+      r[39] = -0.650110471151428;
+      s[39] = -0.861800054039176;
+      w[39] = 0.025255543672496;
+      r[40] = -0.282624366842035;
+      s[40] = 0.131065359625217;
+      w[40] = 0.038432852520849;
+      r[41] = 0.131065359625217;
+      s[41] = -0.282624366842035;
+      w[41] = 0.038432852520849;
+      r[42] = -0.848440992783182;
+      s[42] = 0.131065359625217;
+      w[42] = 0.038432852520849;
+      r[43] = 0.131065359625217;
+      s[43] = -0.848440992783182;
+      w[43] = 0.038432852520849;
+      r[44] = -0.848440992783182;
+      s[44] = -0.282624366842035;
+      w[44] = 0.038432852520849;
+      r[45] = -0.282624366842035;
+      s[45] = -0.848440992783182;
+      w[45] = 0.038432852520849;
+      r[46] = -0.500121711290305;
+      s[46] = 0.333566061453817;
+      w[46] = 0.032993291211606;
+      r[47] = 0.333566061453817;
+      s[47] = -0.500121711290305;
+      w[47] = 0.032993291211606;
+      r[48] = -0.833444350163512;
+      s[48] = 0.333566061453817;
+      w[48] = 0.032993291211606;
+      r[49] = 0.333566061453817;
+      s[49] = -0.833444350163512;
+      w[49] = 0.032993291211606;
+      r[50] = -0.833444350163512;
+      s[50] = -0.500121711290305;
+      w[50] = 0.032993291211606;
+      r[51] = -0.500121711290305;
+      s[51] = -0.833444350163512;
+      w[51] = 0.032993291211606;
+      r[52] = -0.353308953197778;
+      s[52] = -0.027538833736648;
+      w[52] = 0.081415677215044;
+      r[53] = -0.027538833736648;
+      s[53] = -0.353308953197778;
+      w[53] = 0.081415677215044;
+      r[54] = -0.619152213065573;
+      s[54] = -0.027538833736648;
+      w[54] = 0.081415677215044;
+      r[55] = -0.027538833736648;
+      s[55] = -0.619152213065573;
+      w[55] = 0.081415677215044;
+      r[56] = -0.619152213065573;
+      s[56] = -0.353308953197778;
+      w[56] = 0.081415677215044;
+      r[57] = -0.353308953197778;
+      s[57] = -0.619152213065573;
+      w[57] = 0.081415677215044;
 
       break;
     }
     case 17: {
-      r[0]  = -0.013565183960096; s[0]  = -0.013565183960096; w[0]  = 0.022448424077156;
-      r[1]  = -0.972869632079808; s[1]  = -0.013565183960096; w[1]  = 0.022448424077156;
-      r[2]  = -0.013565183960096; s[2]  = -0.972869632079808; w[2]  = 0.022448424077156;
-      r[3]  = -0.918012666387151; s[3]  = -0.918012666387151; w[3]  = 0.011377816766740;
-      r[4]  =  0.836025332774302; s[4]  = -0.918012666387151; w[4]  = 0.011377816766740;
-      r[5]  = -0.918012666387151; s[5]  =  0.836025332774302; w[5]  = 0.011377816766740;
-      r[6]  = -0.469265478050798; s[6]  = -0.469265478050798; w[6]  = 0.056148078797670;
-      r[7]  = -0.061469043898404; s[7]  = -0.469265478050798; w[7]  = 0.056148078797670;
-      r[8]  = -0.469265478050798; s[8]  = -0.061469043898404; w[8]  = 0.056148078797670;
-      r[9]  = -0.278161974512876; s[9]  = -0.278161974512876; w[9]  = 0.031804753050686;
-      r[10] = -0.443676050974249; s[10] = -0.278161974512876; w[10] = 0.031804753050686;
-      r[11] = -0.278161974512876; s[11] = -0.443676050974249; w[11] = 0.031804753050686;
-      r[12] = -0.743831619059579; s[12] = -0.743831619059579; w[12] = 0.042944604159838;
-      r[13] =  0.487663238119159; s[13] = -0.743831619059579; w[13] = 0.042944604159838;
-      r[14] = -0.743831619059579; s[14] =  0.487663238119159; w[14] = 0.042944604159838;
-      r[15] = -0.975086972700342; s[15] = -0.975086972700342; w[15] = 0.004138336267131;
-      r[16] =  0.950173945400684; s[16] = -0.975086972700342; w[16] = 0.004138336267131;
-      r[17] = -0.975086972700342; s[17] =  0.950173945400684; w[17] = 0.004138336267131;
-      r[18] = -0.331485915788080; s[18] =  0.305875449252880; w[18] = 0.020094111670483;
-      r[19] =  0.305875449252880; s[19] = -0.331485915788080; w[19] = 0.020094111670483;
-      r[20] = -0.974389533464800; s[20] =  0.305875449252880; w[20] = 0.020094111670483;
-      r[21] =  0.305875449252880; s[21] = -0.974389533464800; w[21] = 0.020094111670483;
-      r[22] = -0.974389533464800; s[22] = -0.331485915788080; w[22] = 0.020094111670483;
-      r[23] = -0.331485915788080; s[23] = -0.974389533464800; w[23] = 0.020094111670483;
-      r[24] = -0.617368143234940; s[24] =  0.598534426856625; w[24] = 0.013023443943004;
-      r[25] =  0.598534426856625; s[25] = -0.617368143234940; w[25] = 0.013023443943004;
-      r[26] = -0.981166283621686; s[26] =  0.598534426856625; w[26] = 0.013023443943004;
-      r[27] =  0.598534426856625; s[27] = -0.981166283621686; w[27] = 0.013023443943004;
-      r[28] = -0.981166283621686; s[28] = -0.617368143234940; w[28] = 0.013023443943004;
-      r[29] = -0.617368143234940; s[29] = -0.981166283621686; w[29] = 0.013023443943004;
-      r[30] = -0.846737941679184; s[30] =  0.837351785097968; w[30] = 0.005856954369545;
-      r[31] =  0.837351785097968; s[31] = -0.846737941679184; w[31] = 0.005856954369545;
-      r[32] = -0.990613843418784; s[32] =  0.837351785097968; w[32] = 0.005856954369545;
-      r[33] =  0.837351785097968; s[33] = -0.990613843418784; w[33] = 0.005856954369545;
-      r[34] = -0.990613843418784; s[34] = -0.846737941679184; w[34] = 0.005856954369545;
-      r[35] = -0.846737941679184; s[35] = -0.990613843418784; w[35] = 0.005856954369545;
-      r[36] = -0.530582382227094; s[36] =  0.412831673770520; w[36] = 0.037746172643499;
-      r[37] =  0.412831673770520; s[37] = -0.530582382227094; w[37] = 0.037746172643499;
-      r[38] = -0.882249291543426; s[38] =  0.412831673770520; w[38] = 0.037746172643499;
-      r[39] =  0.412831673770520; s[39] = -0.882249291543426; w[39] = 0.037746172643499;
-      r[40] = -0.882249291543426; s[40] = -0.530582382227094; w[40] = 0.037746172643499;
-      r[41] = -0.530582382227094; s[41] = -0.882249291543426; w[41] = 0.037746172643499;
-      r[42] = -0.230167008731505; s[42] =  0.092655855430620; w[42] = 0.048362752988591;
-      r[43] =  0.092655855430620; s[43] = -0.230167008731505; w[43] = 0.048362752988591;
-      r[44] = -0.862488846699115; s[44] =  0.092655855430620; w[44] = 0.048362752988591;
-      r[45] =  0.092655855430620; s[45] = -0.862488846699115; w[45] = 0.048362752988591;
-      r[46] = -0.862488846699115; s[46] = -0.230167008731505; w[46] = 0.048362752988591;
-      r[47] = -0.230167008731505; s[47] = -0.862488846699115; w[47] = 0.048362752988591;
-      r[48] = -0.769841956364772; s[48] =  0.681416462088999; w[48] = 0.023467126169388;
-      r[49] =  0.681416462088999; s[49] = -0.769841956364772; w[49] = 0.023467126169388;
-      r[50] = -0.911574505724228; s[50] =  0.681416462088999; w[50] = 0.023467126169388;
-      r[51] =  0.681416462088999; s[51] = -0.911574505724228; w[51] = 0.023467126169388;
-      r[52] = -0.911574505724228; s[52] = -0.769841956364772; w[52] = 0.023467126169388;
-      r[53] = -0.769841956364772; s[53] = -0.911574505724228; w[53] = 0.023467126169388;
-      r[54] = -0.502901760016855; s[54] =  0.206946937904245; w[54] = 0.054703428836887;
-      r[55] =  0.206946937904245; s[55] = -0.502901760016855; w[55] = 0.054703428836887;
-      r[56] = -0.704045177887389; s[56] =  0.206946937904245; w[56] = 0.054703428836887;
-      r[57] =  0.206946937904245; s[57] = -0.704045177887389; w[57] = 0.054703428836887;
-      r[58] = -0.704045177887389; s[58] = -0.502901760016855; w[58] = 0.054703428836887;
-      r[59] = -0.502901760016855; s[59] = -0.704045177887389; w[59] = 0.054703428836887;
-      r[60] = -0.258115377755090; s[60] = -0.067105414124881; w[60] = 0.045648336152327;
-      r[61] = -0.067105414124881; s[61] = -0.258115377755090; w[61] = 0.045648336152327;
-      r[62] = -0.674779208120030; s[62] = -0.067105414124880; w[62] = 0.045648336152327;
-      r[63] = -0.067105414124880; s[63] = -0.674779208120030; w[63] = 0.045648336152327;
-      r[64] = -0.674779208120030; s[64] = -0.258115377755090; w[64] = 0.045648336152327;
-      r[65] = -0.258115377755090; s[65] = -0.674779208120030; w[65] = 0.045648336152327;
+      r[0] = -0.013565183960096;
+      s[0] = -0.013565183960096;
+      w[0] = 0.022448424077156;
+      r[1] = -0.972869632079808;
+      s[1] = -0.013565183960096;
+      w[1] = 0.022448424077156;
+      r[2] = -0.013565183960096;
+      s[2] = -0.972869632079808;
+      w[2] = 0.022448424077156;
+      r[3] = -0.918012666387151;
+      s[3] = -0.918012666387151;
+      w[3] = 0.011377816766740;
+      r[4] = 0.836025332774302;
+      s[4] = -0.918012666387151;
+      w[4] = 0.011377816766740;
+      r[5] = -0.918012666387151;
+      s[5] = 0.836025332774302;
+      w[5] = 0.011377816766740;
+      r[6] = -0.469265478050798;
+      s[6] = -0.469265478050798;
+      w[6] = 0.056148078797670;
+      r[7] = -0.061469043898404;
+      s[7] = -0.469265478050798;
+      w[7] = 0.056148078797670;
+      r[8] = -0.469265478050798;
+      s[8] = -0.061469043898404;
+      w[8] = 0.056148078797670;
+      r[9] = -0.278161974512876;
+      s[9] = -0.278161974512876;
+      w[9] = 0.031804753050686;
+      r[10] = -0.443676050974249;
+      s[10] = -0.278161974512876;
+      w[10] = 0.031804753050686;
+      r[11] = -0.278161974512876;
+      s[11] = -0.443676050974249;
+      w[11] = 0.031804753050686;
+      r[12] = -0.743831619059579;
+      s[12] = -0.743831619059579;
+      w[12] = 0.042944604159838;
+      r[13] = 0.487663238119159;
+      s[13] = -0.743831619059579;
+      w[13] = 0.042944604159838;
+      r[14] = -0.743831619059579;
+      s[14] = 0.487663238119159;
+      w[14] = 0.042944604159838;
+      r[15] = -0.975086972700342;
+      s[15] = -0.975086972700342;
+      w[15] = 0.004138336267131;
+      r[16] = 0.950173945400684;
+      s[16] = -0.975086972700342;
+      w[16] = 0.004138336267131;
+      r[17] = -0.975086972700342;
+      s[17] = 0.950173945400684;
+      w[17] = 0.004138336267131;
+      r[18] = -0.331485915788080;
+      s[18] = 0.305875449252880;
+      w[18] = 0.020094111670483;
+      r[19] = 0.305875449252880;
+      s[19] = -0.331485915788080;
+      w[19] = 0.020094111670483;
+      r[20] = -0.974389533464800;
+      s[20] = 0.305875449252880;
+      w[20] = 0.020094111670483;
+      r[21] = 0.305875449252880;
+      s[21] = -0.974389533464800;
+      w[21] = 0.020094111670483;
+      r[22] = -0.974389533464800;
+      s[22] = -0.331485915788080;
+      w[22] = 0.020094111670483;
+      r[23] = -0.331485915788080;
+      s[23] = -0.974389533464800;
+      w[23] = 0.020094111670483;
+      r[24] = -0.617368143234940;
+      s[24] = 0.598534426856625;
+      w[24] = 0.013023443943004;
+      r[25] = 0.598534426856625;
+      s[25] = -0.617368143234940;
+      w[25] = 0.013023443943004;
+      r[26] = -0.981166283621686;
+      s[26] = 0.598534426856625;
+      w[26] = 0.013023443943004;
+      r[27] = 0.598534426856625;
+      s[27] = -0.981166283621686;
+      w[27] = 0.013023443943004;
+      r[28] = -0.981166283621686;
+      s[28] = -0.617368143234940;
+      w[28] = 0.013023443943004;
+      r[29] = -0.617368143234940;
+      s[29] = -0.981166283621686;
+      w[29] = 0.013023443943004;
+      r[30] = -0.846737941679184;
+      s[30] = 0.837351785097968;
+      w[30] = 0.005856954369545;
+      r[31] = 0.837351785097968;
+      s[31] = -0.846737941679184;
+      w[31] = 0.005856954369545;
+      r[32] = -0.990613843418784;
+      s[32] = 0.837351785097968;
+      w[32] = 0.005856954369545;
+      r[33] = 0.837351785097968;
+      s[33] = -0.990613843418784;
+      w[33] = 0.005856954369545;
+      r[34] = -0.990613843418784;
+      s[34] = -0.846737941679184;
+      w[34] = 0.005856954369545;
+      r[35] = -0.846737941679184;
+      s[35] = -0.990613843418784;
+      w[35] = 0.005856954369545;
+      r[36] = -0.530582382227094;
+      s[36] = 0.412831673770520;
+      w[36] = 0.037746172643499;
+      r[37] = 0.412831673770520;
+      s[37] = -0.530582382227094;
+      w[37] = 0.037746172643499;
+      r[38] = -0.882249291543426;
+      s[38] = 0.412831673770520;
+      w[38] = 0.037746172643499;
+      r[39] = 0.412831673770520;
+      s[39] = -0.882249291543426;
+      w[39] = 0.037746172643499;
+      r[40] = -0.882249291543426;
+      s[40] = -0.530582382227094;
+      w[40] = 0.037746172643499;
+      r[41] = -0.530582382227094;
+      s[41] = -0.882249291543426;
+      w[41] = 0.037746172643499;
+      r[42] = -0.230167008731505;
+      s[42] = 0.092655855430620;
+      w[42] = 0.048362752988591;
+      r[43] = 0.092655855430620;
+      s[43] = -0.230167008731505;
+      w[43] = 0.048362752988591;
+      r[44] = -0.862488846699115;
+      s[44] = 0.092655855430620;
+      w[44] = 0.048362752988591;
+      r[45] = 0.092655855430620;
+      s[45] = -0.862488846699115;
+      w[45] = 0.048362752988591;
+      r[46] = -0.862488846699115;
+      s[46] = -0.230167008731505;
+      w[46] = 0.048362752988591;
+      r[47] = -0.230167008731505;
+      s[47] = -0.862488846699115;
+      w[47] = 0.048362752988591;
+      r[48] = -0.769841956364772;
+      s[48] = 0.681416462088999;
+      w[48] = 0.023467126169388;
+      r[49] = 0.681416462088999;
+      s[49] = -0.769841956364772;
+      w[49] = 0.023467126169388;
+      r[50] = -0.911574505724228;
+      s[50] = 0.681416462088999;
+      w[50] = 0.023467126169388;
+      r[51] = 0.681416462088999;
+      s[51] = -0.911574505724228;
+      w[51] = 0.023467126169388;
+      r[52] = -0.911574505724228;
+      s[52] = -0.769841956364772;
+      w[52] = 0.023467126169388;
+      r[53] = -0.769841956364772;
+      s[53] = -0.911574505724228;
+      w[53] = 0.023467126169388;
+      r[54] = -0.502901760016855;
+      s[54] = 0.206946937904245;
+      w[54] = 0.054703428836887;
+      r[55] = 0.206946937904245;
+      s[55] = -0.502901760016855;
+      w[55] = 0.054703428836887;
+      r[56] = -0.704045177887389;
+      s[56] = 0.206946937904245;
+      w[56] = 0.054703428836887;
+      r[57] = 0.206946937904245;
+      s[57] = -0.704045177887389;
+      w[57] = 0.054703428836887;
+      r[58] = -0.704045177887389;
+      s[58] = -0.502901760016855;
+      w[58] = 0.054703428836887;
+      r[59] = -0.502901760016855;
+      s[59] = -0.704045177887389;
+      w[59] = 0.054703428836887;
+      r[60] = -0.258115377755090;
+      s[60] = -0.067105414124881;
+      w[60] = 0.045648336152327;
+      r[61] = -0.067105414124881;
+      s[61] = -0.258115377755090;
+      w[61] = 0.045648336152327;
+      r[62] = -0.674779208120030;
+      s[62] = -0.067105414124880;
+      w[62] = 0.045648336152327;
+      r[63] = -0.067105414124880;
+      s[63] = -0.674779208120030;
+      w[63] = 0.045648336152327;
+      r[64] = -0.674779208120030;
+      s[64] = -0.258115377755090;
+      w[64] = 0.045648336152327;
+      r[65] = -0.258115377755090;
+      s[65] = -0.674779208120030;
+      w[65] = 0.045648336152327;
 
       break;
     }
     case 18: {
-      r[0]  = -0.333333333333333; s[0]  = -0.333333333333333; w[0]  = 0.044365924378076;
-      r[1]  = -0.012131216528029; s[1]  = -0.012131216528029; w[1]  = 0.019118866558615;
-      r[2]  = -0.975737566943942; s[2]  = -0.012131216528029; w[2]  = 0.019118866558615;
-      r[3]  = -0.012131216528029; s[3]  = -0.975737566943942; w[3]  = 0.019118866558615;
-      r[4]  = -0.230136518749796; s[4]  = -0.230136518749796; w[4]  = 0.049294282264207;
-      r[5]  = -0.539726962500408; s[5]  = -0.230136518749796; w[5]  = 0.049294282264207;
-      r[6]  = -0.230136518749796; s[6]  = -0.539726962500408; w[6]  = 0.049294282264207;
-      r[7]  = -0.499402807850562; s[7]  = -0.499402807850562; w[7]  = 0.060654125981259;
-      r[8]  = -0.001194384298875; s[8]  = -0.499402807850563; w[8]  = 0.060654125981259;
-      r[9]  = -0.499402807850563; s[9]  = -0.001194384298875; w[9]  = 0.060654125981259;
-      r[10] = -0.710045241598598; s[10] = -0.710045241598598; w[10] = 0.031366231844497;
-      r[11] =  0.420090483197196; s[11] = -0.710045241598598; w[11] = 0.031366231844497;
-      r[12] = -0.710045241598598; s[12] =  0.420090483197196; w[12] = 0.031366231844497;
-      r[13] = -0.903019171569391; s[13] = -0.903019171569391; w[13] = 0.016173035699059;
-      r[14] =  0.806038343138783; s[14] = -0.903019171569391; w[14] = 0.016173035699059;
-      r[15] = -0.903019171569391; s[15] =  0.806038343138783; w[15] = 0.016173035699059;
-      r[16] = -0.972866921676664; s[16] = -0.972866921676664; w[16] = 0.004750076743416;
-      r[17] =  0.945733843353328; s[17] = -0.972866921676664; w[17] = 0.004750076743416;
-      r[18] = -0.972866921676664; s[18] =  0.945733843353328; w[18] = 0.004750076743416;
-      r[19] = -0.859848143426920; s[19] =  0.852682278520227; w[19] = 0.004329998364046;
-      r[20] =  0.852682278520227; s[20] = -0.859848143426920; w[20] = 0.004329998364046;
-      r[21] = -0.992834135093306; s[21] =  0.852682278520227; w[21] = 0.004329998364046;
-      r[22] =  0.852682278520227; s[22] = -0.992834135093306; w[22] = 0.004329998364046;
-      r[23] = -0.992834135093306; s[23] = -0.859848143426920; w[23] = 0.004329998364046;
-      r[24] = -0.859848143426920; s[24] = -0.992834135093306; w[24] = 0.004329998364046;
-      r[25] = -0.592208428296456; s[25] =  0.573110619333459; w[25] = 0.012300136592151;
-      r[26] =  0.573110619333459; s[26] = -0.592208428296456; w[26] = 0.012300136592151;
-      r[27] = -0.980902191037003; s[27] =  0.573110619333459; w[27] = 0.012300136592151;
-      r[28] =  0.573110619333459; s[28] = -0.980902191037003; w[28] = 0.012300136592151;
-      r[29] = -0.980902191037003; s[29] = -0.592208428296456; w[29] = 0.012300136592151;
-      r[30] = -0.592208428296456; s[30] = -0.980902191037003; w[30] = 0.012300136592151;
-      r[31] = -0.316660705097116; s[31] =  0.294011442575493; w[31] = 0.017146550496094;
-      r[32] =  0.294011442575493; s[32] = -0.316660705097116; w[32] = 0.017146550496094;
-      r[33] = -0.977350737478378; s[33] =  0.294011442575493; w[33] = 0.017146550496094;
-      r[34] =  0.294011442575493; s[34] = -0.977350737478378; w[34] = 0.017146550496094;
-      r[35] = -0.977350737478378; s[35] = -0.316660705097116; w[35] = 0.017146550496094;
-      r[36] = -0.316660705097116; s[36] = -0.977350737478378; w[36] = 0.017146550496094;
-      r[37] = -0.762708275393600; s[37] =  0.720805143081058; w[37] = 0.010992784367686;
-      r[38] =  0.720805143081058; s[38] = -0.762708275393600; w[38] = 0.010992784367686;
-      r[39] = -0.958096867687458; s[39] =  0.720805143081058; w[39] = 0.010992784367686;
-      r[40] =  0.720805143081058; s[40] = -0.958096867687458; w[40] = 0.010992784367686;
-      r[41] = -0.958096867687458; s[41] = -0.762708275393600; w[41] = 0.010992784367686;
-      r[42] = -0.762708275393600; s[42] = -0.958096867687458; w[42] = 0.010992784367686;
-      r[43] = -0.499464753852078; s[43] =  0.389673957377540; w[43] = 0.033988423627451;
-      r[44] =  0.389673957377540; s[44] = -0.499464753852078; w[44] = 0.033988423627451;
-      r[45] = -0.890209203525462; s[45] =  0.389673957377540; w[45] = 0.033988423627451;
-      r[46] =  0.389673957377540; s[46] = -0.890209203525462; w[46] = 0.033988423627451;
-      r[47] = -0.890209203525462; s[47] = -0.499464753852078; w[47] = 0.033988423627451;
-      r[48] = -0.499464753852078; s[48] = -0.890209203525462; w[48] = 0.033988423627451;
-      r[49] = -0.730193961187213; s[49] =  0.595225312221749; w[49] = 0.025768775250048;
-      r[50] =  0.595225312221749; s[50] = -0.730193961187213; w[50] = 0.025768775250048;
-      r[51] = -0.865031351034536; s[51] =  0.595225312221749; w[51] = 0.025768775250048;
-      r[52] =  0.595225312221749; s[52] = -0.865031351034536; w[52] = 0.025768775250048;
-      r[53] = -0.865031351034535; s[53] = -0.730193961187213; w[53] = 0.025768775250048;
-      r[54] = -0.730193961187213; s[54] = -0.865031351034535; w[54] = 0.025768775250048;
-      r[55] = -0.213662181077459; s[55] =  0.092159471784540; w[55] = 0.040023698716305;
-      r[56] =  0.092159471784540; s[56] = -0.213662181077459; w[56] = 0.040023698716305;
-      r[57] = -0.878497290707081; s[57] =  0.092159471784540; w[57] = 0.040023698716305;
-      r[58] =  0.092159471784540; s[58] = -0.878497290707081; w[58] = 0.040023698716305;
-      r[59] = -0.878497290707081; s[59] = -0.213662181077459; w[59] = 0.040023698716305;
-      r[60] = -0.213662181077459; s[60] = -0.878497290707081; w[60] = 0.040023698716305;
-      r[61] = -0.268906542375276; s[61] = -0.010964677486621; w[61] = 0.045277248097616;
-      r[62] = -0.010964677486621; s[62] = -0.268906542375276; w[62] = 0.045277248097616;
-      r[63] = -0.720128780138103; s[63] = -0.010964677486621; w[63] = 0.045277248097616;
-      r[64] = -0.010964677486621; s[64] = -0.720128780138103; w[64] = 0.045277248097616;
-      r[65] = -0.720128780138103; s[65] = -0.268906542375276; w[65] = 0.045277248097616;
-      r[66] = -0.268906542375276; s[66] = -0.720128780138103; w[66] = 0.045277248097616;
-      r[67] = -0.507963230765286; s[67] =  0.233062121320884; w[67] = 0.045433087546729;
-      r[68] =  0.233062121320884; s[68] = -0.507963230765286; w[68] = 0.045433087546729;
-      r[69] = -0.725098890555598; s[69] =  0.233062121320884; w[69] = 0.045433087546729;
-      r[70] =  0.233062121320884; s[70] = -0.725098890555598; w[70] = 0.045433087546729;
-      r[71] = -0.725098890555598; s[71] = -0.507963230765286; w[71] = 0.045433087546729;
-      r[72] = -0.507963230765286; s[72] = -0.725098890555598; w[72] = 0.045433087546729;
+      r[0] = -0.333333333333333;
+      s[0] = -0.333333333333333;
+      w[0] = 0.044365924378076;
+      r[1] = -0.012131216528029;
+      s[1] = -0.012131216528029;
+      w[1] = 0.019118866558615;
+      r[2] = -0.975737566943942;
+      s[2] = -0.012131216528029;
+      w[2] = 0.019118866558615;
+      r[3] = -0.012131216528029;
+      s[3] = -0.975737566943942;
+      w[3] = 0.019118866558615;
+      r[4] = -0.230136518749796;
+      s[4] = -0.230136518749796;
+      w[4] = 0.049294282264207;
+      r[5] = -0.539726962500408;
+      s[5] = -0.230136518749796;
+      w[5] = 0.049294282264207;
+      r[6] = -0.230136518749796;
+      s[6] = -0.539726962500408;
+      w[6] = 0.049294282264207;
+      r[7] = -0.499402807850562;
+      s[7] = -0.499402807850562;
+      w[7] = 0.060654125981259;
+      r[8] = -0.001194384298875;
+      s[8] = -0.499402807850563;
+      w[8] = 0.060654125981259;
+      r[9] = -0.499402807850563;
+      s[9] = -0.001194384298875;
+      w[9] = 0.060654125981259;
+      r[10] = -0.710045241598598;
+      s[10] = -0.710045241598598;
+      w[10] = 0.031366231844497;
+      r[11] = 0.420090483197196;
+      s[11] = -0.710045241598598;
+      w[11] = 0.031366231844497;
+      r[12] = -0.710045241598598;
+      s[12] = 0.420090483197196;
+      w[12] = 0.031366231844497;
+      r[13] = -0.903019171569391;
+      s[13] = -0.903019171569391;
+      w[13] = 0.016173035699059;
+      r[14] = 0.806038343138783;
+      s[14] = -0.903019171569391;
+      w[14] = 0.016173035699059;
+      r[15] = -0.903019171569391;
+      s[15] = 0.806038343138783;
+      w[15] = 0.016173035699059;
+      r[16] = -0.972866921676664;
+      s[16] = -0.972866921676664;
+      w[16] = 0.004750076743416;
+      r[17] = 0.945733843353328;
+      s[17] = -0.972866921676664;
+      w[17] = 0.004750076743416;
+      r[18] = -0.972866921676664;
+      s[18] = 0.945733843353328;
+      w[18] = 0.004750076743416;
+      r[19] = -0.859848143426920;
+      s[19] = 0.852682278520227;
+      w[19] = 0.004329998364046;
+      r[20] = 0.852682278520227;
+      s[20] = -0.859848143426920;
+      w[20] = 0.004329998364046;
+      r[21] = -0.992834135093306;
+      s[21] = 0.852682278520227;
+      w[21] = 0.004329998364046;
+      r[22] = 0.852682278520227;
+      s[22] = -0.992834135093306;
+      w[22] = 0.004329998364046;
+      r[23] = -0.992834135093306;
+      s[23] = -0.859848143426920;
+      w[23] = 0.004329998364046;
+      r[24] = -0.859848143426920;
+      s[24] = -0.992834135093306;
+      w[24] = 0.004329998364046;
+      r[25] = -0.592208428296456;
+      s[25] = 0.573110619333459;
+      w[25] = 0.012300136592151;
+      r[26] = 0.573110619333459;
+      s[26] = -0.592208428296456;
+      w[26] = 0.012300136592151;
+      r[27] = -0.980902191037003;
+      s[27] = 0.573110619333459;
+      w[27] = 0.012300136592151;
+      r[28] = 0.573110619333459;
+      s[28] = -0.980902191037003;
+      w[28] = 0.012300136592151;
+      r[29] = -0.980902191037003;
+      s[29] = -0.592208428296456;
+      w[29] = 0.012300136592151;
+      r[30] = -0.592208428296456;
+      s[30] = -0.980902191037003;
+      w[30] = 0.012300136592151;
+      r[31] = -0.316660705097116;
+      s[31] = 0.294011442575493;
+      w[31] = 0.017146550496094;
+      r[32] = 0.294011442575493;
+      s[32] = -0.316660705097116;
+      w[32] = 0.017146550496094;
+      r[33] = -0.977350737478378;
+      s[33] = 0.294011442575493;
+      w[33] = 0.017146550496094;
+      r[34] = 0.294011442575493;
+      s[34] = -0.977350737478378;
+      w[34] = 0.017146550496094;
+      r[35] = -0.977350737478378;
+      s[35] = -0.316660705097116;
+      w[35] = 0.017146550496094;
+      r[36] = -0.316660705097116;
+      s[36] = -0.977350737478378;
+      w[36] = 0.017146550496094;
+      r[37] = -0.762708275393600;
+      s[37] = 0.720805143081058;
+      w[37] = 0.010992784367686;
+      r[38] = 0.720805143081058;
+      s[38] = -0.762708275393600;
+      w[38] = 0.010992784367686;
+      r[39] = -0.958096867687458;
+      s[39] = 0.720805143081058;
+      w[39] = 0.010992784367686;
+      r[40] = 0.720805143081058;
+      s[40] = -0.958096867687458;
+      w[40] = 0.010992784367686;
+      r[41] = -0.958096867687458;
+      s[41] = -0.762708275393600;
+      w[41] = 0.010992784367686;
+      r[42] = -0.762708275393600;
+      s[42] = -0.958096867687458;
+      w[42] = 0.010992784367686;
+      r[43] = -0.499464753852078;
+      s[43] = 0.389673957377540;
+      w[43] = 0.033988423627451;
+      r[44] = 0.389673957377540;
+      s[44] = -0.499464753852078;
+      w[44] = 0.033988423627451;
+      r[45] = -0.890209203525462;
+      s[45] = 0.389673957377540;
+      w[45] = 0.033988423627451;
+      r[46] = 0.389673957377540;
+      s[46] = -0.890209203525462;
+      w[46] = 0.033988423627451;
+      r[47] = -0.890209203525462;
+      s[47] = -0.499464753852078;
+      w[47] = 0.033988423627451;
+      r[48] = -0.499464753852078;
+      s[48] = -0.890209203525462;
+      w[48] = 0.033988423627451;
+      r[49] = -0.730193961187213;
+      s[49] = 0.595225312221749;
+      w[49] = 0.025768775250048;
+      r[50] = 0.595225312221749;
+      s[50] = -0.730193961187213;
+      w[50] = 0.025768775250048;
+      r[51] = -0.865031351034536;
+      s[51] = 0.595225312221749;
+      w[51] = 0.025768775250048;
+      r[52] = 0.595225312221749;
+      s[52] = -0.865031351034536;
+      w[52] = 0.025768775250048;
+      r[53] = -0.865031351034535;
+      s[53] = -0.730193961187213;
+      w[53] = 0.025768775250048;
+      r[54] = -0.730193961187213;
+      s[54] = -0.865031351034535;
+      w[54] = 0.025768775250048;
+      r[55] = -0.213662181077459;
+      s[55] = 0.092159471784540;
+      w[55] = 0.040023698716305;
+      r[56] = 0.092159471784540;
+      s[56] = -0.213662181077459;
+      w[56] = 0.040023698716305;
+      r[57] = -0.878497290707081;
+      s[57] = 0.092159471784540;
+      w[57] = 0.040023698716305;
+      r[58] = 0.092159471784540;
+      s[58] = -0.878497290707081;
+      w[58] = 0.040023698716305;
+      r[59] = -0.878497290707081;
+      s[59] = -0.213662181077459;
+      w[59] = 0.040023698716305;
+      r[60] = -0.213662181077459;
+      s[60] = -0.878497290707081;
+      w[60] = 0.040023698716305;
+      r[61] = -0.268906542375276;
+      s[61] = -0.010964677486621;
+      w[61] = 0.045277248097616;
+      r[62] = -0.010964677486621;
+      s[62] = -0.268906542375276;
+      w[62] = 0.045277248097616;
+      r[63] = -0.720128780138103;
+      s[63] = -0.010964677486621;
+      w[63] = 0.045277248097616;
+      r[64] = -0.010964677486621;
+      s[64] = -0.720128780138103;
+      w[64] = 0.045277248097616;
+      r[65] = -0.720128780138103;
+      s[65] = -0.268906542375276;
+      w[65] = 0.045277248097616;
+      r[66] = -0.268906542375276;
+      s[66] = -0.720128780138103;
+      w[66] = 0.045277248097616;
+      r[67] = -0.507963230765286;
+      s[67] = 0.233062121320884;
+      w[67] = 0.045433087546729;
+      r[68] = 0.233062121320884;
+      s[68] = -0.507963230765286;
+      w[68] = 0.045433087546729;
+      r[69] = -0.725098890555598;
+      s[69] = 0.233062121320884;
+      w[69] = 0.045433087546729;
+      r[70] = 0.233062121320884;
+      s[70] = -0.725098890555598;
+      w[70] = 0.045433087546729;
+      r[71] = -0.725098890555598;
+      s[71] = -0.507963230765286;
+      w[71] = 0.045433087546729;
+      r[72] = -0.507963230765286;
+      s[72] = -0.725098890555598;
+      w[72] = 0.045433087546729;
 
       break;
     }
     case 19: {
-      r[0]  = -0.333333333333333; s[0]  = -0.333333333333333; w[0]  = 0.041424760048010;
-      r[1]  = -0.121193890022463; s[1]  = -0.121193890022463; w[1]  = 0.031784855337689;
-      r[2]  = -0.757612219955075; s[2]  = -0.121193890022463; w[2]  = 0.031784855337689;
-      r[3]  = -0.121193890022463; s[3]  = -0.757612219955075; w[3]  = 0.031784855337689;
-      r[4]  = -0.227921589064499; s[4]  = -0.227921589064499; w[4]  = 0.048406599909930;
-      r[5]  = -0.544156821871001; s[5]  = -0.227921589064499; w[5]  = 0.048406599909930;
-      r[6]  = -0.227921589064499; s[6]  = -0.544156821871001; w[6]  = 0.048406599909930;
-      r[7]  = -0.480832787187258; s[7]  = -0.480832787187258; w[7]  = 0.048177661858475;
-      r[8]  = -0.038334425625484; s[8]  = -0.480832787187258; w[8]  = 0.048177661858475;
-      r[9]  = -0.480832787187258; s[9]  = -0.038334425625484; w[9]  = 0.048177661858475;
-      r[10] = -0.607587000462791; s[10] = -0.607587000462791; w[10] = 0.042691162490028;
-      r[11] =  0.215174000925582; s[11] = -0.607587000462791; w[11] = 0.042691162490028;
-      r[12] = -0.607587000462791; s[12] =  0.215174000925582; w[12] = 0.042691162490028;
-      r[13] = -0.728032884013154; s[13] = -0.728032884013154; w[13] = 0.031889013978028;
-      r[14] =  0.456065768026307; s[14] = -0.728032884013154; w[14] = 0.031889013978028;
-      r[15] = -0.728032884013154; s[15] =  0.456065768026307; w[15] = 0.031889013978028;
-      r[16] = -0.884999963315497; s[16] = -0.884999963315497; w[16] = 0.015529272923518;
-      r[17] =  0.769999926630994; s[17] = -0.884999963315497; w[17] = 0.015529272923518;
-      r[18] = -0.884999963315497; s[18] =  0.769999926630994; w[18] = 0.015529272923518;
-      r[19] = -0.973927705240279; s[19] = -0.973927705240279; w[19] = 0.004442852871415;
-      r[20] =  0.947855410480559; s[20] = -0.973927705240279; w[20] = 0.004442852871415;
-      r[21] = -0.973927705240279; s[21] =  0.947855410480559; w[21] = 0.004442852871415;
-      r[22] = -0.419340397282846; s[22] =  0.418549313572482; w[22] = 0.004599409024561;
-      r[23] =  0.418549313572482; s[23] = -0.419340397282846; w[23] = 0.004599409024561;
-      r[24] = -0.999208916289636; s[24] =  0.418549313572482; w[24] = 0.004599409024561;
-      r[25] =  0.418549313572482; s[25] = -0.999208916289636; w[25] = 0.004599409024561;
-      r[26] = -0.999208916289636; s[26] = -0.419340397282846; w[26] = 0.004599409024561;
-      r[27] = -0.419340397282846; s[27] = -0.999208916289636; w[27] = 0.004599409024561;
-      r[28] = -0.154285565801825; s[28] =  0.131285016869205; w[28] = 0.016608327001253;
-      r[29] =  0.131285016869205; s[29] = -0.154285565801825; w[29] = 0.016608327001253;
-      r[30] = -0.976999451067380; s[30] =  0.131285016869205; w[30] = 0.016608327001253;
-      r[31] =  0.131285016869205; s[31] = -0.976999451067380; w[31] = 0.016608327001253;
-      r[32] = -0.976999451067380; s[32] = -0.154285565801825; w[32] = 0.016608327001253;
-      r[33] = -0.154285565801825; s[33] = -0.976999451067380; w[33] = 0.016608327001253;
-      r[34] = -0.864328042937615; s[34] =  0.842262778125134; w[34] = 0.008508350664254;
-      r[35] =  0.842262778125134; s[35] = -0.864328042937615; w[35] = 0.008508350664254;
-      r[36] = -0.977934735187519; s[36] =  0.842262778125134; w[36] = 0.008508350664254;
-      r[37] =  0.842262778125134; s[37] = -0.977934735187519; w[37] = 0.008508350664254;
-      r[38] = -0.977934735187519; s[38] = -0.864328042937615; w[38] = 0.008508350664254;
-      r[39] = -0.864328042937615; s[39] = -0.977934735187519; w[39] = 0.008508350664254;
-      r[40] = -0.676980679779850; s[40] =  0.654351228666662; w[40] = 0.012752760516072;
-      r[41] =  0.654351228666662; s[41] = -0.676980679779850; w[41] = 0.012752760516072;
-      r[42] = -0.977370548886812; s[42] =  0.654351228666662; w[42] = 0.012752760516072;
-      r[43] =  0.654351228666662; s[43] = -0.977370548886812; w[43] = 0.012752760516072;
-      r[44] = -0.977370548886812; s[44] = -0.676980679779850; w[44] = 0.012752760516072;
-      r[45] = -0.676980679779850; s[45] = -0.977370548886812; w[45] = 0.012752760516072;
-      r[46] = -0.451038034994882; s[46] =  0.391933493150074; w[46] = 0.024864731137205;
-      r[47] =  0.391933493150074; s[47] = -0.451038034994882; w[47] = 0.024864731137205;
-      r[48] = -0.940895458155192; s[48] =  0.391933493150074; w[48] = 0.024864731137205;
-      r[49] =  0.391933493150074; s[49] = -0.940895458155192; w[49] = 0.024864731137205;
-      r[50] = -0.940895458155192; s[50] = -0.451038034994882; w[50] = 0.024864731137205;
-      r[51] = -0.451038034994882; s[51] = -0.940895458155192; w[51] = 0.024864731137205;
-      r[52] = -0.755079003035426; s[52] =  0.643775758022122; w[52] = 0.012779469878381;
-      r[53] =  0.643775758022122; s[53] = -0.755079003035426; w[53] = 0.012779469878381;
-      r[54] = -0.888696754986697; s[54] =  0.643775758022122; w[54] = 0.012779469878381;
-      r[55] =  0.643775758022122; s[55] = -0.888696754986697; w[55] = 0.012779469878381;
-      r[56] = -0.888696754986697; s[56] = -0.755079003035426; w[56] = 0.012779469878381;
-      r[57] = -0.755079003035426; s[57] = -0.888696754986697; w[57] = 0.012779469878381;
-      r[58] = -0.668500025831376; s[58] =  0.544622467980326; w[58] = 0.017801502950615;
-      r[59] =  0.544622467980326; s[59] = -0.668500025831376; w[59] = 0.017801502950615;
-      r[60] = -0.876122442148950; s[60] =  0.544622467980326; w[60] = 0.017801502950615;
-      r[61] =  0.544622467980326; s[61] = -0.876122442148950; w[61] = 0.017801502950615;
-      r[62] = -0.876122442148950; s[62] = -0.668500025831376; w[62] = 0.017801502950615;
-      r[63] = -0.668500025831376; s[63] = -0.876122442148950; w[63] = 0.017801502950615;
-      r[64] = -0.205954158284095; s[64] =  0.090524206162520; w[64] = 0.035738233266717;
-      r[65] =  0.090524206162520; s[65] = -0.205954158284095; w[65] = 0.035738233266717;
-      r[66] = -0.884570047878425; s[66] =  0.090524206162520; w[66] = 0.035738233266717;
-      r[67] =  0.090524206162520; s[67] = -0.884570047878425; w[67] = 0.035738233266717;
-      r[68] = -0.884570047878425; s[68] = -0.205954158284095; w[68] = 0.035738233266717;
-      r[69] = -0.205954158284095; s[69] = -0.884570047878425; w[69] = 0.035738233266717;
-      r[70] = -0.488476686471250; s[70] =  0.295757669634562; w[70] = 0.038344199404453;
-      r[71] =  0.295757669634562; s[71] = -0.488476686471250; w[71] = 0.038344199404453;
-      r[72] = -0.807280983163311; s[72] =  0.295757669634562; w[72] = 0.038344199404453;
-      r[73] =  0.295757669634562; s[73] = -0.807280983163311; w[73] = 0.038344199404453;
-      r[74] = -0.807280983163311; s[74] = -0.488476686471250; w[74] = 0.038344199404453;
-      r[75] = -0.488476686471250; s[75] = -0.807280983163311; w[75] = 0.038344199404453;
-      r[76] = -0.342507806805715; s[76] =  0.042214391480752; w[76] = 0.042971513130613;
-      r[77] =  0.042214391480752; s[77] = -0.342507806805715; w[77] = 0.042971513130613;
-      r[78] = -0.699706584675037; s[78] =  0.042214391480751; w[78] = 0.042971513130613;
-      r[79] =  0.042214391480751; s[79] = -0.699706584675037; w[79] = 0.042971513130613;
-      r[80] = -0.699706584675037; s[80] = -0.342507806805715; w[80] = 0.042971513130613;
-      r[81] = -0.342507806805715; s[81] = -0.699706584675037; w[81] = 0.042971513130613;
+      r[0] = -0.333333333333333;
+      s[0] = -0.333333333333333;
+      w[0] = 0.041424760048010;
+      r[1] = -0.121193890022463;
+      s[1] = -0.121193890022463;
+      w[1] = 0.031784855337689;
+      r[2] = -0.757612219955075;
+      s[2] = -0.121193890022463;
+      w[2] = 0.031784855337689;
+      r[3] = -0.121193890022463;
+      s[3] = -0.757612219955075;
+      w[3] = 0.031784855337689;
+      r[4] = -0.227921589064499;
+      s[4] = -0.227921589064499;
+      w[4] = 0.048406599909930;
+      r[5] = -0.544156821871001;
+      s[5] = -0.227921589064499;
+      w[5] = 0.048406599909930;
+      r[6] = -0.227921589064499;
+      s[6] = -0.544156821871001;
+      w[6] = 0.048406599909930;
+      r[7] = -0.480832787187258;
+      s[7] = -0.480832787187258;
+      w[7] = 0.048177661858475;
+      r[8] = -0.038334425625484;
+      s[8] = -0.480832787187258;
+      w[8] = 0.048177661858475;
+      r[9] = -0.480832787187258;
+      s[9] = -0.038334425625484;
+      w[9] = 0.048177661858475;
+      r[10] = -0.607587000462791;
+      s[10] = -0.607587000462791;
+      w[10] = 0.042691162490028;
+      r[11] = 0.215174000925582;
+      s[11] = -0.607587000462791;
+      w[11] = 0.042691162490028;
+      r[12] = -0.607587000462791;
+      s[12] = 0.215174000925582;
+      w[12] = 0.042691162490028;
+      r[13] = -0.728032884013154;
+      s[13] = -0.728032884013154;
+      w[13] = 0.031889013978028;
+      r[14] = 0.456065768026307;
+      s[14] = -0.728032884013154;
+      w[14] = 0.031889013978028;
+      r[15] = -0.728032884013154;
+      s[15] = 0.456065768026307;
+      w[15] = 0.031889013978028;
+      r[16] = -0.884999963315497;
+      s[16] = -0.884999963315497;
+      w[16] = 0.015529272923518;
+      r[17] = 0.769999926630994;
+      s[17] = -0.884999963315497;
+      w[17] = 0.015529272923518;
+      r[18] = -0.884999963315497;
+      s[18] = 0.769999926630994;
+      w[18] = 0.015529272923518;
+      r[19] = -0.973927705240279;
+      s[19] = -0.973927705240279;
+      w[19] = 0.004442852871415;
+      r[20] = 0.947855410480559;
+      s[20] = -0.973927705240279;
+      w[20] = 0.004442852871415;
+      r[21] = -0.973927705240279;
+      s[21] = 0.947855410480559;
+      w[21] = 0.004442852871415;
+      r[22] = -0.419340397282846;
+      s[22] = 0.418549313572482;
+      w[22] = 0.004599409024561;
+      r[23] = 0.418549313572482;
+      s[23] = -0.419340397282846;
+      w[23] = 0.004599409024561;
+      r[24] = -0.999208916289636;
+      s[24] = 0.418549313572482;
+      w[24] = 0.004599409024561;
+      r[25] = 0.418549313572482;
+      s[25] = -0.999208916289636;
+      w[25] = 0.004599409024561;
+      r[26] = -0.999208916289636;
+      s[26] = -0.419340397282846;
+      w[26] = 0.004599409024561;
+      r[27] = -0.419340397282846;
+      s[27] = -0.999208916289636;
+      w[27] = 0.004599409024561;
+      r[28] = -0.154285565801825;
+      s[28] = 0.131285016869205;
+      w[28] = 0.016608327001253;
+      r[29] = 0.131285016869205;
+      s[29] = -0.154285565801825;
+      w[29] = 0.016608327001253;
+      r[30] = -0.976999451067380;
+      s[30] = 0.131285016869205;
+      w[30] = 0.016608327001253;
+      r[31] = 0.131285016869205;
+      s[31] = -0.976999451067380;
+      w[31] = 0.016608327001253;
+      r[32] = -0.976999451067380;
+      s[32] = -0.154285565801825;
+      w[32] = 0.016608327001253;
+      r[33] = -0.154285565801825;
+      s[33] = -0.976999451067380;
+      w[33] = 0.016608327001253;
+      r[34] = -0.864328042937615;
+      s[34] = 0.842262778125134;
+      w[34] = 0.008508350664254;
+      r[35] = 0.842262778125134;
+      s[35] = -0.864328042937615;
+      w[35] = 0.008508350664254;
+      r[36] = -0.977934735187519;
+      s[36] = 0.842262778125134;
+      w[36] = 0.008508350664254;
+      r[37] = 0.842262778125134;
+      s[37] = -0.977934735187519;
+      w[37] = 0.008508350664254;
+      r[38] = -0.977934735187519;
+      s[38] = -0.864328042937615;
+      w[38] = 0.008508350664254;
+      r[39] = -0.864328042937615;
+      s[39] = -0.977934735187519;
+      w[39] = 0.008508350664254;
+      r[40] = -0.676980679779850;
+      s[40] = 0.654351228666662;
+      w[40] = 0.012752760516072;
+      r[41] = 0.654351228666662;
+      s[41] = -0.676980679779850;
+      w[41] = 0.012752760516072;
+      r[42] = -0.977370548886812;
+      s[42] = 0.654351228666662;
+      w[42] = 0.012752760516072;
+      r[43] = 0.654351228666662;
+      s[43] = -0.977370548886812;
+      w[43] = 0.012752760516072;
+      r[44] = -0.977370548886812;
+      s[44] = -0.676980679779850;
+      w[44] = 0.012752760516072;
+      r[45] = -0.676980679779850;
+      s[45] = -0.977370548886812;
+      w[45] = 0.012752760516072;
+      r[46] = -0.451038034994882;
+      s[46] = 0.391933493150074;
+      w[46] = 0.024864731137205;
+      r[47] = 0.391933493150074;
+      s[47] = -0.451038034994882;
+      w[47] = 0.024864731137205;
+      r[48] = -0.940895458155192;
+      s[48] = 0.391933493150074;
+      w[48] = 0.024864731137205;
+      r[49] = 0.391933493150074;
+      s[49] = -0.940895458155192;
+      w[49] = 0.024864731137205;
+      r[50] = -0.940895458155192;
+      s[50] = -0.451038034994882;
+      w[50] = 0.024864731137205;
+      r[51] = -0.451038034994882;
+      s[51] = -0.940895458155192;
+      w[51] = 0.024864731137205;
+      r[52] = -0.755079003035426;
+      s[52] = 0.643775758022122;
+      w[52] = 0.012779469878381;
+      r[53] = 0.643775758022122;
+      s[53] = -0.755079003035426;
+      w[53] = 0.012779469878381;
+      r[54] = -0.888696754986697;
+      s[54] = 0.643775758022122;
+      w[54] = 0.012779469878381;
+      r[55] = 0.643775758022122;
+      s[55] = -0.888696754986697;
+      w[55] = 0.012779469878381;
+      r[56] = -0.888696754986697;
+      s[56] = -0.755079003035426;
+      w[56] = 0.012779469878381;
+      r[57] = -0.755079003035426;
+      s[57] = -0.888696754986697;
+      w[57] = 0.012779469878381;
+      r[58] = -0.668500025831376;
+      s[58] = 0.544622467980326;
+      w[58] = 0.017801502950615;
+      r[59] = 0.544622467980326;
+      s[59] = -0.668500025831376;
+      w[59] = 0.017801502950615;
+      r[60] = -0.876122442148950;
+      s[60] = 0.544622467980326;
+      w[60] = 0.017801502950615;
+      r[61] = 0.544622467980326;
+      s[61] = -0.876122442148950;
+      w[61] = 0.017801502950615;
+      r[62] = -0.876122442148950;
+      s[62] = -0.668500025831376;
+      w[62] = 0.017801502950615;
+      r[63] = -0.668500025831376;
+      s[63] = -0.876122442148950;
+      w[63] = 0.017801502950615;
+      r[64] = -0.205954158284095;
+      s[64] = 0.090524206162520;
+      w[64] = 0.035738233266717;
+      r[65] = 0.090524206162520;
+      s[65] = -0.205954158284095;
+      w[65] = 0.035738233266717;
+      r[66] = -0.884570047878425;
+      s[66] = 0.090524206162520;
+      w[66] = 0.035738233266717;
+      r[67] = 0.090524206162520;
+      s[67] = -0.884570047878425;
+      w[67] = 0.035738233266717;
+      r[68] = -0.884570047878425;
+      s[68] = -0.205954158284095;
+      w[68] = 0.035738233266717;
+      r[69] = -0.205954158284095;
+      s[69] = -0.884570047878425;
+      w[69] = 0.035738233266717;
+      r[70] = -0.488476686471250;
+      s[70] = 0.295757669634562;
+      w[70] = 0.038344199404453;
+      r[71] = 0.295757669634562;
+      s[71] = -0.488476686471250;
+      w[71] = 0.038344199404453;
+      r[72] = -0.807280983163311;
+      s[72] = 0.295757669634562;
+      w[72] = 0.038344199404453;
+      r[73] = 0.295757669634562;
+      s[73] = -0.807280983163311;
+      w[73] = 0.038344199404453;
+      r[74] = -0.807280983163311;
+      s[74] = -0.488476686471250;
+      w[74] = 0.038344199404453;
+      r[75] = -0.488476686471250;
+      s[75] = -0.807280983163311;
+      w[75] = 0.038344199404453;
+      r[76] = -0.342507806805715;
+      s[76] = 0.042214391480752;
+      w[76] = 0.042971513130613;
+      r[77] = 0.042214391480752;
+      s[77] = -0.342507806805715;
+      w[77] = 0.042971513130613;
+      r[78] = -0.699706584675037;
+      s[78] = 0.042214391480751;
+      w[78] = 0.042971513130613;
+      r[79] = 0.042214391480751;
+      s[79] = -0.699706584675037;
+      w[79] = 0.042971513130613;
+      r[80] = -0.699706584675037;
+      s[80] = -0.342507806805715;
+      w[80] = 0.042971513130613;
+      r[81] = -0.342507806805715;
+      s[81] = -0.699706584675037;
+      w[81] = 0.042971513130613;
 
       break;
     }
     case 20: {
-      r[0]  = -0.333333333333333; s[0]  = -0.333333333333333; w[0]  = 0.055220853995399;
-      r[1]  = -0.001500649324429; s[1]  = -0.001500649324429; w[1]  = 0.003558059094653;
-      r[2]  = -0.996998701351142; s[2]  = -0.001500649324429; w[2]  = 0.003558059094653;
-      r[3]  = -0.001500649324429; s[3]  = -0.996998701351142; w[3]  = 0.003558059094653;
-      r[4]  = -0.094139751938951; s[4]  = -0.094139751938951; w[4]  = 0.040224796227922;
-      r[5]  = -0.811720496122098; s[5]  = -0.094139751938951; w[5]  = 0.040224796227922;
-      r[6]  = -0.094139751938951; s[6]  = -0.811720496122098; w[6]  = 0.040224796227922;
-      r[7]  = -0.204472124089526; s[7]  = -0.204472124089526; w[7]  = 0.053635694518663;
-      r[8]  = -0.591055751820947; s[8]  = -0.204472124089526; w[8]  = 0.053635694518663;
-      r[9]  = -0.204472124089526; s[9]  = -0.591055751820947; w[9]  = 0.053635694518663;
-      r[10] = -0.470999594934425; s[10] = -0.470999594934425; w[10] = 0.049046267603004;
-      r[11] = -0.058000810131149; s[11] = -0.470999594934425; w[11] = 0.049046267603004;
-      r[12] = -0.470999594934425; s[12] = -0.058000810131149; w[12] = 0.049046267603004;
-      r[13] = -0.577962071815846; s[13] = -0.577962071815846; w[13] = 0.032789156821391;
-      r[14] =  0.155924143631693; s[14] = -0.577962071815846; w[14] = 0.032789156821391;
-      r[15] = -0.577962071815846; s[15] =  0.155924143631693; w[15] = 0.032789156821391;
-      r[16] = -0.784528785657457; s[16] = -0.784528785657457; w[16] = 0.029591814797299;
-      r[17] =  0.569057571314915; s[17] = -0.784528785657457; w[17] = 0.029591814797299;
-      r[18] = -0.784528785657457; s[18] =  0.569057571314915; w[18] = 0.029591814797299;
-      r[19] = -0.921861824324395; s[19] = -0.921861824324395; w[19] = 0.009158564555409;
-      r[20] =  0.843723648648789; s[20] = -0.921861824324395; w[20] = 0.009158564555409;
-      r[21] = -0.921861824324395; s[21] =  0.843723648648789; w[21] = 0.009158564555409;
-      r[22] = -0.977651240541341; s[22] = -0.977651240541341; w[22] = 0.003303653031152;
-      r[23] =  0.955302481082681; s[23] = -0.977651240541341; w[23] = 0.003303653031152;
-      r[24] = -0.977651240541341; s[24] =  0.955302481082681; w[24] = 0.003303653031152;
-      r[25] = -0.872900668183296; s[25] =  0.862201431808621; w[25] = 0.004698341817151;
-      r[26] =  0.862201431808621; s[26] = -0.872900668183296; w[26] = 0.004698341817151;
-      r[27] = -0.989300763625325; s[27] =  0.862201431808621; w[27] = 0.004698341817151;
-      r[28] =  0.862201431808621; s[28] = -0.989300763625325; w[28] = 0.004698341817151;
-      r[29] = -0.989300763625325; s[29] = -0.872900668183295; w[29] = 0.004698341817151;
-      r[30] = -0.872900668183295; s[30] = -0.989300763625325; w[30] = 0.004698341817151;
-      r[31] = -0.685786162118586; s[31] =  0.669876527986188; w[31] = 0.008931851508364;
-      r[32] =  0.669876527986188; s[32] = -0.685786162118586; w[32] = 0.008931851508364;
-      r[33] = -0.984090365867602; s[33] =  0.669876527986188; w[33] = 0.008931851508364;
-      r[34] =  0.669876527986188; s[34] = -0.984090365867602; w[34] = 0.008931851508364;
-      r[35] = -0.984090365867602; s[35] = -0.685786162118586; w[35] = 0.008931851508364;
-      r[36] = -0.685786162118586; s[36] = -0.984090365867602; w[36] = 0.008931851508364;
-      r[37] = -0.208715771271252; s[37] =  0.187870974708724; w[37] = 0.012199133615816;
-      r[38] =  0.187870974708724; s[38] = -0.208715771271252; w[38] = 0.012199133615816;
-      r[39] = -0.979155203437472; s[39] =  0.187870974708724; w[39] = 0.012199133615816;
-      r[40] =  0.187870974708724; s[40] = -0.979155203437472; w[40] = 0.012199133615816;
-      r[41] = -0.979155203437472; s[41] = -0.208715771271252; w[41] = 0.012199133615816;
-      r[42] = -0.208715771271252; s[42] = -0.979155203437472; w[42] = 0.012199133615816;
-      r[43] = -0.453664858574179; s[43] =  0.431736028981932; w[43] = 0.013782162654376;
-      r[44] =  0.431736028981932; s[44] = -0.453664858574179; w[44] = 0.013782162654376;
-      r[45] = -0.978071170407753; s[45] =  0.431736028981932; w[45] = 0.013782162654376;
-      r[46] =  0.431736028981932; s[46] = -0.978071170407753; w[46] = 0.013782162654376;
-      r[47] = -0.978071170407753; s[47] = -0.453664858574179; w[47] = 0.013782162654376;
-      r[48] = -0.453664858574179; s[48] = -0.978071170407753; w[48] = 0.013782162654376;
-      r[49] = -0.796429235029966; s[49] =  0.719295810859041; w[49] = 0.015994950144956;
-      r[50] =  0.719295810859041; s[50] = -0.796429235029966; w[50] = 0.015994950144956;
-      r[51] = -0.922866575829075; s[51] =  0.719295810859041; w[51] = 0.015994950144956;
-      r[52] =  0.719295810859041; s[52] = -0.922866575829075; w[52] = 0.015994950144956;
-      r[53] = -0.922866575829075; s[53] = -0.796429235029966; w[53] = 0.015994950144956;
-      r[54] = -0.796429235029966; s[54] = -0.922866575829075; w[54] = 0.015994950144956;
-      r[55] = -0.106682901647172; s[55] =  0.035521886012736; w[55] = 0.014772268570672;
-      r[56] =  0.035521886012736; s[56] = -0.106682901647172; w[56] = 0.014772268570672;
-      r[57] = -0.928838984365563; s[57] =  0.035521886012736; w[57] = 0.014772268570672;
-      r[58] =  0.035521886012736; s[58] = -0.928838984365563; w[58] = 0.014772268570672;
-      r[59] = -0.928838984365564; s[59] = -0.106682901647172; w[59] = 0.014772268570672;
-      r[60] = -0.106682901647172; s[60] = -0.928838984365564; w[60] = 0.014772268570672;
-      r[61] = -0.601978411700994; s[61] =  0.502636778975466; w[61] = 0.025598663757297;
-      r[62] =  0.502636778975466; s[62] = -0.601978411700994; w[62] = 0.025598663757297;
-      r[63] = -0.900658367274472; s[63] =  0.502636778975466; w[63] = 0.025598663757297;
-      r[64] =  0.502636778975466; s[64] = -0.900658367274472; w[64] = 0.025598663757297;
-      r[65] = -0.900658367274472; s[65] = -0.601978411700994; w[65] = 0.025598663757297;
-      r[66] = -0.601978411700994; s[66] = -0.900658367274472; w[66] = 0.025598663757297;
-      r[67] = -0.351477632615435; s[67] =  0.234438182446771; w[67] = 0.034516142351393;
-      r[68] =  0.234438182446771; s[68] = -0.351477632615435; w[68] = 0.034516142351393;
-      r[69] = -0.882960549831337; s[69] =  0.234438182446771; w[69] = 0.034516142351393;
-      r[70] =  0.234438182446771; s[70] = -0.882960549831337; w[70] = 0.034516142351393;
-      r[71] = -0.882960549831337; s[71] = -0.351477632615435; w[71] = 0.034516142351393;
-      r[72] = -0.351477632615435; s[72] = -0.882960549831337; w[72] = 0.034516142351393;
-      r[73] = -0.582937273579734; s[73] =  0.339941699570946; w[73] = 0.037345891805871;
-      r[74] =  0.339941699570946; s[74] = -0.582937273579734; w[74] = 0.037345891805871;
-      r[75] = -0.757004425991211; s[75] =  0.339941699570946; w[75] = 0.037345891805871;
-      r[76] =  0.339941699570946; s[76] = -0.757004425991211; w[76] = 0.037345891805871;
-      r[77] = -0.757004425991211; s[77] = -0.582937273579734; w[77] = 0.037345891805871;
-      r[78] = -0.582937273579734; s[78] = -0.757004425991211; w[78] = 0.037345891805871;
-      r[79] = -0.353658866927485; s[79] =  0.072237177039608; w[79] = 0.045636448116791;
-      r[80] =  0.072237177039608; s[80] = -0.353658866927485; w[80] = 0.045636448116791;
-      r[81] = -0.718578310112123; s[81] =  0.072237177039608; w[81] = 0.045636448116791;
-      r[82] =  0.072237177039608; s[82] = -0.718578310112123; w[82] = 0.045636448116791;
-      r[83] = -0.718578310112123; s[83] = -0.353658866927485; w[83] = 0.045636448116791;
-      r[84] = -0.353658866927485; s[84] = -0.718578310112123; w[84] = 0.045636448116791;
+      r[0] = -0.333333333333333;
+      s[0] = -0.333333333333333;
+      w[0] = 0.055220853995399;
+      r[1] = -0.001500649324429;
+      s[1] = -0.001500649324429;
+      w[1] = 0.003558059094653;
+      r[2] = -0.996998701351142;
+      s[2] = -0.001500649324429;
+      w[2] = 0.003558059094653;
+      r[3] = -0.001500649324429;
+      s[3] = -0.996998701351142;
+      w[3] = 0.003558059094653;
+      r[4] = -0.094139751938951;
+      s[4] = -0.094139751938951;
+      w[4] = 0.040224796227922;
+      r[5] = -0.811720496122098;
+      s[5] = -0.094139751938951;
+      w[5] = 0.040224796227922;
+      r[6] = -0.094139751938951;
+      s[6] = -0.811720496122098;
+      w[6] = 0.040224796227922;
+      r[7] = -0.204472124089526;
+      s[7] = -0.204472124089526;
+      w[7] = 0.053635694518663;
+      r[8] = -0.591055751820947;
+      s[8] = -0.204472124089526;
+      w[8] = 0.053635694518663;
+      r[9] = -0.204472124089526;
+      s[9] = -0.591055751820947;
+      w[9] = 0.053635694518663;
+      r[10] = -0.470999594934425;
+      s[10] = -0.470999594934425;
+      w[10] = 0.049046267603004;
+      r[11] = -0.058000810131149;
+      s[11] = -0.470999594934425;
+      w[11] = 0.049046267603004;
+      r[12] = -0.470999594934425;
+      s[12] = -0.058000810131149;
+      w[12] = 0.049046267603004;
+      r[13] = -0.577962071815846;
+      s[13] = -0.577962071815846;
+      w[13] = 0.032789156821391;
+      r[14] = 0.155924143631693;
+      s[14] = -0.577962071815846;
+      w[14] = 0.032789156821391;
+      r[15] = -0.577962071815846;
+      s[15] = 0.155924143631693;
+      w[15] = 0.032789156821391;
+      r[16] = -0.784528785657457;
+      s[16] = -0.784528785657457;
+      w[16] = 0.029591814797299;
+      r[17] = 0.569057571314915;
+      s[17] = -0.784528785657457;
+      w[17] = 0.029591814797299;
+      r[18] = -0.784528785657457;
+      s[18] = 0.569057571314915;
+      w[18] = 0.029591814797299;
+      r[19] = -0.921861824324395;
+      s[19] = -0.921861824324395;
+      w[19] = 0.009158564555409;
+      r[20] = 0.843723648648789;
+      s[20] = -0.921861824324395;
+      w[20] = 0.009158564555409;
+      r[21] = -0.921861824324395;
+      s[21] = 0.843723648648789;
+      w[21] = 0.009158564555409;
+      r[22] = -0.977651240541341;
+      s[22] = -0.977651240541341;
+      w[22] = 0.003303653031152;
+      r[23] = 0.955302481082681;
+      s[23] = -0.977651240541341;
+      w[23] = 0.003303653031152;
+      r[24] = -0.977651240541341;
+      s[24] = 0.955302481082681;
+      w[24] = 0.003303653031152;
+      r[25] = -0.872900668183296;
+      s[25] = 0.862201431808621;
+      w[25] = 0.004698341817151;
+      r[26] = 0.862201431808621;
+      s[26] = -0.872900668183296;
+      w[26] = 0.004698341817151;
+      r[27] = -0.989300763625325;
+      s[27] = 0.862201431808621;
+      w[27] = 0.004698341817151;
+      r[28] = 0.862201431808621;
+      s[28] = -0.989300763625325;
+      w[28] = 0.004698341817151;
+      r[29] = -0.989300763625325;
+      s[29] = -0.872900668183295;
+      w[29] = 0.004698341817151;
+      r[30] = -0.872900668183295;
+      s[30] = -0.989300763625325;
+      w[30] = 0.004698341817151;
+      r[31] = -0.685786162118586;
+      s[31] = 0.669876527986188;
+      w[31] = 0.008931851508364;
+      r[32] = 0.669876527986188;
+      s[32] = -0.685786162118586;
+      w[32] = 0.008931851508364;
+      r[33] = -0.984090365867602;
+      s[33] = 0.669876527986188;
+      w[33] = 0.008931851508364;
+      r[34] = 0.669876527986188;
+      s[34] = -0.984090365867602;
+      w[34] = 0.008931851508364;
+      r[35] = -0.984090365867602;
+      s[35] = -0.685786162118586;
+      w[35] = 0.008931851508364;
+      r[36] = -0.685786162118586;
+      s[36] = -0.984090365867602;
+      w[36] = 0.008931851508364;
+      r[37] = -0.208715771271252;
+      s[37] = 0.187870974708724;
+      w[37] = 0.012199133615816;
+      r[38] = 0.187870974708724;
+      s[38] = -0.208715771271252;
+      w[38] = 0.012199133615816;
+      r[39] = -0.979155203437472;
+      s[39] = 0.187870974708724;
+      w[39] = 0.012199133615816;
+      r[40] = 0.187870974708724;
+      s[40] = -0.979155203437472;
+      w[40] = 0.012199133615816;
+      r[41] = -0.979155203437472;
+      s[41] = -0.208715771271252;
+      w[41] = 0.012199133615816;
+      r[42] = -0.208715771271252;
+      s[42] = -0.979155203437472;
+      w[42] = 0.012199133615816;
+      r[43] = -0.453664858574179;
+      s[43] = 0.431736028981932;
+      w[43] = 0.013782162654376;
+      r[44] = 0.431736028981932;
+      s[44] = -0.453664858574179;
+      w[44] = 0.013782162654376;
+      r[45] = -0.978071170407753;
+      s[45] = 0.431736028981932;
+      w[45] = 0.013782162654376;
+      r[46] = 0.431736028981932;
+      s[46] = -0.978071170407753;
+      w[46] = 0.013782162654376;
+      r[47] = -0.978071170407753;
+      s[47] = -0.453664858574179;
+      w[47] = 0.013782162654376;
+      r[48] = -0.453664858574179;
+      s[48] = -0.978071170407753;
+      w[48] = 0.013782162654376;
+      r[49] = -0.796429235029966;
+      s[49] = 0.719295810859041;
+      w[49] = 0.015994950144956;
+      r[50] = 0.719295810859041;
+      s[50] = -0.796429235029966;
+      w[50] = 0.015994950144956;
+      r[51] = -0.922866575829075;
+      s[51] = 0.719295810859041;
+      w[51] = 0.015994950144956;
+      r[52] = 0.719295810859041;
+      s[52] = -0.922866575829075;
+      w[52] = 0.015994950144956;
+      r[53] = -0.922866575829075;
+      s[53] = -0.796429235029966;
+      w[53] = 0.015994950144956;
+      r[54] = -0.796429235029966;
+      s[54] = -0.922866575829075;
+      w[54] = 0.015994950144956;
+      r[55] = -0.106682901647172;
+      s[55] = 0.035521886012736;
+      w[55] = 0.014772268570672;
+      r[56] = 0.035521886012736;
+      s[56] = -0.106682901647172;
+      w[56] = 0.014772268570672;
+      r[57] = -0.928838984365563;
+      s[57] = 0.035521886012736;
+      w[57] = 0.014772268570672;
+      r[58] = 0.035521886012736;
+      s[58] = -0.928838984365563;
+      w[58] = 0.014772268570672;
+      r[59] = -0.928838984365564;
+      s[59] = -0.106682901647172;
+      w[59] = 0.014772268570672;
+      r[60] = -0.106682901647172;
+      s[60] = -0.928838984365564;
+      w[60] = 0.014772268570672;
+      r[61] = -0.601978411700994;
+      s[61] = 0.502636778975466;
+      w[61] = 0.025598663757297;
+      r[62] = 0.502636778975466;
+      s[62] = -0.601978411700994;
+      w[62] = 0.025598663757297;
+      r[63] = -0.900658367274472;
+      s[63] = 0.502636778975466;
+      w[63] = 0.025598663757297;
+      r[64] = 0.502636778975466;
+      s[64] = -0.900658367274472;
+      w[64] = 0.025598663757297;
+      r[65] = -0.900658367274472;
+      s[65] = -0.601978411700994;
+      w[65] = 0.025598663757297;
+      r[66] = -0.601978411700994;
+      s[66] = -0.900658367274472;
+      w[66] = 0.025598663757297;
+      r[67] = -0.351477632615435;
+      s[67] = 0.234438182446771;
+      w[67] = 0.034516142351393;
+      r[68] = 0.234438182446771;
+      s[68] = -0.351477632615435;
+      w[68] = 0.034516142351393;
+      r[69] = -0.882960549831337;
+      s[69] = 0.234438182446771;
+      w[69] = 0.034516142351393;
+      r[70] = 0.234438182446771;
+      s[70] = -0.882960549831337;
+      w[70] = 0.034516142351393;
+      r[71] = -0.882960549831337;
+      s[71] = -0.351477632615435;
+      w[71] = 0.034516142351393;
+      r[72] = -0.351477632615435;
+      s[72] = -0.882960549831337;
+      w[72] = 0.034516142351393;
+      r[73] = -0.582937273579734;
+      s[73] = 0.339941699570946;
+      w[73] = 0.037345891805871;
+      r[74] = 0.339941699570946;
+      s[74] = -0.582937273579734;
+      w[74] = 0.037345891805871;
+      r[75] = -0.757004425991211;
+      s[75] = 0.339941699570946;
+      w[75] = 0.037345891805871;
+      r[76] = 0.339941699570946;
+      s[76] = -0.757004425991211;
+      w[76] = 0.037345891805871;
+      r[77] = -0.757004425991211;
+      s[77] = -0.582937273579734;
+      w[77] = 0.037345891805871;
+      r[78] = -0.582937273579734;
+      s[78] = -0.757004425991211;
+      w[78] = 0.037345891805871;
+      r[79] = -0.353658866927485;
+      s[79] = 0.072237177039608;
+      w[79] = 0.045636448116791;
+      r[80] = 0.072237177039608;
+      s[80] = -0.353658866927485;
+      w[80] = 0.045636448116791;
+      r[81] = -0.718578310112123;
+      s[81] = 0.072237177039608;
+      w[81] = 0.045636448116791;
+      r[82] = 0.072237177039608;
+      s[82] = -0.718578310112123;
+      w[82] = 0.045636448116791;
+      r[83] = -0.718578310112123;
+      s[83] = -0.353658866927485;
+      w[83] = 0.045636448116791;
+      r[84] = -0.353658866927485;
+      s[84] = -0.718578310112123;
+      w[84] = 0.045636448116791;
 
       break;
     }
     case 21: {
-      r[0]  = -0.006427416686680; s[0]  = -0.006427416686680; w[0]  = 0.009411977990382;
-      r[1]  = -0.987145166626641; s[1]  = -0.006427416686680; w[1]  = 0.009411977990382;
-      r[2]  = -0.006427416686680; s[2]  = -0.987145166626641; w[2]  = 0.009411977990382;
-      r[3]  = -0.037371238381685; s[3]  = -0.037371238381685; w[3]  = 0.023551229711283;
-      r[4]  = -0.925257523236629; s[4]  = -0.037371238381685; w[4]  = 0.023551229711283;
-      r[5]  = -0.037371238381685; s[5]  = -0.925257523236629; w[5]  = 0.023551229711283;
-      r[6]  = -0.101972641308225; s[6]  = -0.101972641308225; w[6]  = 0.041353961937512;
-      r[7]  = -0.796054717383551; s[7]  = -0.101972641308225; w[7]  = 0.041353961937512;
-      r[8]  = -0.101972641308225; s[8]  = -0.796054717383551; w[8]  = 0.041353961937512;
-      r[9]  = -0.405469125577621; s[9]  = -0.405469125577621; w[9]  = 0.045947520102707;
-      r[10] = -0.189061748844758; s[10] = -0.405469125577621; w[10] = 0.045947520102707;
-      r[11] = -0.405469125577621; s[11] = -0.189061748844758; w[11] = 0.045947520102707;
-      r[12] = -0.556282620757932; s[12] = -0.556282620757932; w[12] = 0.047724273523632;
-      r[13] =  0.112565241515865; s[13] = -0.556282620757932; w[13] = 0.047724273523632;
-      r[14] = -0.556282620757932; s[14] =  0.112565241515865; w[14] = 0.047724273523632;
-      r[15] = -0.787490889149774; s[15] = -0.787490889149774; w[15] = 0.019906824503099;
-      r[16] =  0.574981778299548; s[16] = -0.787490889149774; w[16] = 0.019906824503099;
-      r[17] = -0.787490889149774; s[17] =  0.574981778299548; w[17] = 0.019906824503099;
-      r[18] = -0.892713038713217; s[18] = -0.892713038713217; w[18] = 0.014287994054933;
-      r[19] =  0.785426077426434; s[19] = -0.892713038713217; w[19] = 0.014287994054933;
-      r[20] = -0.892713038713217; s[20] =  0.785426077426434; w[20] = 0.014287994054933;
-      r[21] = -0.975095902008750; s[21] =  0.956581360464913; w[21] = 0.001538784565604;
-      r[22] =  0.956581360464913; s[22] = -0.975095902008750; w[22] = 0.001538784565604;
-      r[23] = -0.981485458456163; s[23] =  0.956581360464913; w[23] = 0.001538784565604;
-      r[24] =  0.956581360464913; s[24] = -0.981485458456163; w[24] = 0.001538784565604;
-      r[25] = -0.981485458456163; s[25] = -0.975095902008750; w[25] = 0.001538784565604;
-      r[26] = -0.975095902008750; s[26] = -0.981485458456163; w[26] = 0.001538784565604;
-      r[27] = -0.734190363492767; s[27] =  0.718759150923754; w[27] = 0.007257720730941;
-      r[28] =  0.718759150923754; s[28] = -0.734190363492767; w[28] = 0.007257720730941;
-      r[29] = -0.984568787430988; s[29] =  0.718759150923754; w[29] = 0.007257720730941;
-      r[30] =  0.718759150923754; s[30] = -0.984568787430988; w[30] = 0.007257720730941;
-      r[31] = -0.984568787430988; s[31] = -0.734190363492767; w[31] = 0.007257720730941;
-      r[32] = -0.734190363492767; s[32] = -0.984568787430988; w[32] = 0.007257720730941;
-      r[33] = -0.279909645448207; s[33] =  0.260066127858194; w[33] = 0.013303360825119;
-      r[34] =  0.260066127858194; s[34] = -0.279909645448207; w[34] = 0.013303360825119;
-      r[35] = -0.980156482409987; s[35] =  0.260066127858194; w[35] = 0.013303360825119;
-      r[36] =  0.260066127858194; s[36] = -0.980156482409987; w[36] = 0.013303360825119;
-      r[37] = -0.980156482409987; s[37] = -0.279909645448207; w[37] = 0.013303360825119;
-      r[38] = -0.279909645448207; s[38] = -0.980156482409987; w[38] = 0.013303360825119;
-      r[39] = -0.527626383829046; s[39] =  0.508213994286434; w[39] = 0.011413497063052;
-      r[40] =  0.508213994286434; s[40] = -0.527626383829046; w[40] = 0.011413497063052;
-      r[41] = -0.980587610457388; s[41] =  0.508213994286434; w[41] = 0.011413497063052;
-      r[42] =  0.508213994286434; s[42] = -0.980587610457388; w[42] = 0.011413497063052;
-      r[43] = -0.980587610457388; s[43] = -0.527626383829046; w[43] = 0.011413497063052;
-      r[44] = -0.527626383829046; s[44] = -0.980587610457388; w[44] = 0.011413497063052;
-      r[45] = -0.887945885434766; s[45] =  0.867094084690673; w[45] = 0.006552521291655;
-      r[46] =  0.867094084690673; s[46] = -0.887945885434766; w[46] = 0.006552521291655;
-      r[47] = -0.979148199255907; s[47] =  0.867094084690673; w[47] = 0.006552521291655;
-      r[48] =  0.867094084690673; s[48] = -0.979148199255907; w[48] = 0.006552521291655;
-      r[49] = -0.979148199255907; s[49] = -0.887945885434766; w[49] = 0.006552521291655;
-      r[50] = -0.887945885434766; s[50] = -0.979148199255907; w[50] = 0.006552521291655;
-      r[51] = -0.738154400021390; s[51] =  0.655149643679198; w[51] = 0.017432381135646;
-      r[52] =  0.655149643679198; s[52] = -0.738154400021390; w[52] = 0.017432381135646;
-      r[53] = -0.916995243657807; s[53] =  0.655149643679198; w[53] = 0.017432381135646;
-      r[54] =  0.655149643679198; s[54] = -0.916995243657807; w[54] = 0.017432381135646;
-      r[55] = -0.916995243657807; s[55] = -0.738154400021390; w[55] = 0.017432381135646;
-      r[56] = -0.738154400021390; s[56] = -0.916995243657807; w[56] = 0.017432381135646;
-      r[57] = -0.296840355384531; s[57] =  0.194393499586184; w[57] = 0.027402609499462;
-      r[58] =  0.194393499586184; s[58] = -0.296840355384531; w[58] = 0.027402609499462;
-      r[59] = -0.897553144201652; s[59] =  0.194393499586184; w[59] = 0.027402609499462;
-      r[60] =  0.194393499586184; s[60] = -0.897553144201652; w[60] = 0.027402609499462;
-      r[61] = -0.897553144201652; s[61] = -0.296840355384531; w[61] = 0.027402609499462;
-      r[62] = -0.296840355384531; s[62] = -0.897553144201652; w[62] = 0.027402609499462;
-      r[63] = -0.531632641825188; s[63] =  0.431035654635683; w[63] = 0.025014173853794;
-      r[64] =  0.431035654635683; s[64] = -0.531632641825188; w[64] = 0.025014173853794;
-      r[65] = -0.899403012810496; s[65] =  0.431035654635683; w[65] = 0.025014173853794;
-      r[66] =  0.431035654635683; s[66] = -0.899403012810496; w[66] = 0.025014173853794;
-      r[67] = -0.899403012810496; s[67] = -0.531632641825188; w[67] = 0.025014173853794;
-      r[68] = -0.531632641825188; s[68] = -0.899403012810496; w[68] = 0.025014173853794;
-      r[69] = -0.682130525363537; s[69] =  0.500223407469218; w[69] = 0.008690112508894;
-      r[70] =  0.500223407469218; s[70] = -0.682130525363537; w[70] = 0.008690112508894;
-      r[71] = -0.818092882105681; s[71] =  0.500223407469218; w[71] = 0.008690112508894;
-      r[72] =  0.500223407469218; s[72] = -0.818092882105681; w[72] = 0.008690112508894;
-      r[73] = -0.818092882105681; s[73] = -0.682130525363537; w[73] = 0.008690112508894;
-      r[74] = -0.682130525363537; s[74] = -0.818092882105681; w[74] = 0.008690112508894;
-      r[75] = -0.376270450471865; s[75] =  0.138207573987544; w[75] = 0.037386369243416;
-      r[76] =  0.138207573987544; s[76] = -0.376270450471865; w[76] = 0.037386369243416;
-      r[77] = -0.761937123515678; s[77] =  0.138207573987544; w[77] = 0.037386369243416;
-      r[78] =  0.138207573987544; s[78] = -0.761937123515678; w[78] = 0.037386369243416;
-      r[79] = -0.761937123515678; s[79] = -0.376270450471865; w[79] = 0.037386369243416;
-      r[80] = -0.376270450471865; s[80] = -0.761937123515678; w[80] = 0.037386369243416;
-      r[81] = -0.590719081005038; s[81] =  0.339375331943743; w[81] = 0.032509611084921;
-      r[82] =  0.339375331943743; s[82] = -0.590719081005038; w[82] = 0.032509611084921;
-      r[83] = -0.748656250938705; s[83] =  0.339375331943743; w[83] = 0.032509611084921;
-      r[84] =  0.339375331943743; s[84] = -0.748656250938705; w[84] = 0.032509611084921;
-      r[85] = -0.748656250938705; s[85] = -0.590719081005038; w[85] = 0.032509611084921;
-      r[86] = -0.590719081005038; s[86] = -0.748656250938705; w[86] = 0.032509611084921;
-      r[87] = -0.305527033262063; s[87] = -0.081590222620926; w[87] = 0.043740300619054;
-      r[88] = -0.081590222620926; s[88] = -0.305527033262063; w[88] = 0.043740300619054;
-      r[89] = -0.612882744117011; s[89] = -0.081590222620926; w[89] = 0.043740300619054;
-      r[90] = -0.081590222620926; s[90] = -0.612882744117011; w[90] = 0.043740300619054;
-      r[91] = -0.612882744117011; s[91] = -0.305527033262063; w[91] = 0.043740300619054;
-      r[92] = -0.305527033262063; s[92] = -0.612882744117011; w[92] = 0.043740300619054;
+      r[0] = -0.006427416686680;
+      s[0] = -0.006427416686680;
+      w[0] = 0.009411977990382;
+      r[1] = -0.987145166626641;
+      s[1] = -0.006427416686680;
+      w[1] = 0.009411977990382;
+      r[2] = -0.006427416686680;
+      s[2] = -0.987145166626641;
+      w[2] = 0.009411977990382;
+      r[3] = -0.037371238381685;
+      s[3] = -0.037371238381685;
+      w[3] = 0.023551229711283;
+      r[4] = -0.925257523236629;
+      s[4] = -0.037371238381685;
+      w[4] = 0.023551229711283;
+      r[5] = -0.037371238381685;
+      s[5] = -0.925257523236629;
+      w[5] = 0.023551229711283;
+      r[6] = -0.101972641308225;
+      s[6] = -0.101972641308225;
+      w[6] = 0.041353961937512;
+      r[7] = -0.796054717383551;
+      s[7] = -0.101972641308225;
+      w[7] = 0.041353961937512;
+      r[8] = -0.101972641308225;
+      s[8] = -0.796054717383551;
+      w[8] = 0.041353961937512;
+      r[9] = -0.405469125577621;
+      s[9] = -0.405469125577621;
+      w[9] = 0.045947520102707;
+      r[10] = -0.189061748844758;
+      s[10] = -0.405469125577621;
+      w[10] = 0.045947520102707;
+      r[11] = -0.405469125577621;
+      s[11] = -0.189061748844758;
+      w[11] = 0.045947520102707;
+      r[12] = -0.556282620757932;
+      s[12] = -0.556282620757932;
+      w[12] = 0.047724273523632;
+      r[13] = 0.112565241515865;
+      s[13] = -0.556282620757932;
+      w[13] = 0.047724273523632;
+      r[14] = -0.556282620757932;
+      s[14] = 0.112565241515865;
+      w[14] = 0.047724273523632;
+      r[15] = -0.787490889149774;
+      s[15] = -0.787490889149774;
+      w[15] = 0.019906824503099;
+      r[16] = 0.574981778299548;
+      s[16] = -0.787490889149774;
+      w[16] = 0.019906824503099;
+      r[17] = -0.787490889149774;
+      s[17] = 0.574981778299548;
+      w[17] = 0.019906824503099;
+      r[18] = -0.892713038713217;
+      s[18] = -0.892713038713217;
+      w[18] = 0.014287994054933;
+      r[19] = 0.785426077426434;
+      s[19] = -0.892713038713217;
+      w[19] = 0.014287994054933;
+      r[20] = -0.892713038713217;
+      s[20] = 0.785426077426434;
+      w[20] = 0.014287994054933;
+      r[21] = -0.975095902008750;
+      s[21] = 0.956581360464913;
+      w[21] = 0.001538784565604;
+      r[22] = 0.956581360464913;
+      s[22] = -0.975095902008750;
+      w[22] = 0.001538784565604;
+      r[23] = -0.981485458456163;
+      s[23] = 0.956581360464913;
+      w[23] = 0.001538784565604;
+      r[24] = 0.956581360464913;
+      s[24] = -0.981485458456163;
+      w[24] = 0.001538784565604;
+      r[25] = -0.981485458456163;
+      s[25] = -0.975095902008750;
+      w[25] = 0.001538784565604;
+      r[26] = -0.975095902008750;
+      s[26] = -0.981485458456163;
+      w[26] = 0.001538784565604;
+      r[27] = -0.734190363492767;
+      s[27] = 0.718759150923754;
+      w[27] = 0.007257720730941;
+      r[28] = 0.718759150923754;
+      s[28] = -0.734190363492767;
+      w[28] = 0.007257720730941;
+      r[29] = -0.984568787430988;
+      s[29] = 0.718759150923754;
+      w[29] = 0.007257720730941;
+      r[30] = 0.718759150923754;
+      s[30] = -0.984568787430988;
+      w[30] = 0.007257720730941;
+      r[31] = -0.984568787430988;
+      s[31] = -0.734190363492767;
+      w[31] = 0.007257720730941;
+      r[32] = -0.734190363492767;
+      s[32] = -0.984568787430988;
+      w[32] = 0.007257720730941;
+      r[33] = -0.279909645448207;
+      s[33] = 0.260066127858194;
+      w[33] = 0.013303360825119;
+      r[34] = 0.260066127858194;
+      s[34] = -0.279909645448207;
+      w[34] = 0.013303360825119;
+      r[35] = -0.980156482409987;
+      s[35] = 0.260066127858194;
+      w[35] = 0.013303360825119;
+      r[36] = 0.260066127858194;
+      s[36] = -0.980156482409987;
+      w[36] = 0.013303360825119;
+      r[37] = -0.980156482409987;
+      s[37] = -0.279909645448207;
+      w[37] = 0.013303360825119;
+      r[38] = -0.279909645448207;
+      s[38] = -0.980156482409987;
+      w[38] = 0.013303360825119;
+      r[39] = -0.527626383829046;
+      s[39] = 0.508213994286434;
+      w[39] = 0.011413497063052;
+      r[40] = 0.508213994286434;
+      s[40] = -0.527626383829046;
+      w[40] = 0.011413497063052;
+      r[41] = -0.980587610457388;
+      s[41] = 0.508213994286434;
+      w[41] = 0.011413497063052;
+      r[42] = 0.508213994286434;
+      s[42] = -0.980587610457388;
+      w[42] = 0.011413497063052;
+      r[43] = -0.980587610457388;
+      s[43] = -0.527626383829046;
+      w[43] = 0.011413497063052;
+      r[44] = -0.527626383829046;
+      s[44] = -0.980587610457388;
+      w[44] = 0.011413497063052;
+      r[45] = -0.887945885434766;
+      s[45] = 0.867094084690673;
+      w[45] = 0.006552521291655;
+      r[46] = 0.867094084690673;
+      s[46] = -0.887945885434766;
+      w[46] = 0.006552521291655;
+      r[47] = -0.979148199255907;
+      s[47] = 0.867094084690673;
+      w[47] = 0.006552521291655;
+      r[48] = 0.867094084690673;
+      s[48] = -0.979148199255907;
+      w[48] = 0.006552521291655;
+      r[49] = -0.979148199255907;
+      s[49] = -0.887945885434766;
+      w[49] = 0.006552521291655;
+      r[50] = -0.887945885434766;
+      s[50] = -0.979148199255907;
+      w[50] = 0.006552521291655;
+      r[51] = -0.738154400021390;
+      s[51] = 0.655149643679198;
+      w[51] = 0.017432381135646;
+      r[52] = 0.655149643679198;
+      s[52] = -0.738154400021390;
+      w[52] = 0.017432381135646;
+      r[53] = -0.916995243657807;
+      s[53] = 0.655149643679198;
+      w[53] = 0.017432381135646;
+      r[54] = 0.655149643679198;
+      s[54] = -0.916995243657807;
+      w[54] = 0.017432381135646;
+      r[55] = -0.916995243657807;
+      s[55] = -0.738154400021390;
+      w[55] = 0.017432381135646;
+      r[56] = -0.738154400021390;
+      s[56] = -0.916995243657807;
+      w[56] = 0.017432381135646;
+      r[57] = -0.296840355384531;
+      s[57] = 0.194393499586184;
+      w[57] = 0.027402609499462;
+      r[58] = 0.194393499586184;
+      s[58] = -0.296840355384531;
+      w[58] = 0.027402609499462;
+      r[59] = -0.897553144201652;
+      s[59] = 0.194393499586184;
+      w[59] = 0.027402609499462;
+      r[60] = 0.194393499586184;
+      s[60] = -0.897553144201652;
+      w[60] = 0.027402609499462;
+      r[61] = -0.897553144201652;
+      s[61] = -0.296840355384531;
+      w[61] = 0.027402609499462;
+      r[62] = -0.296840355384531;
+      s[62] = -0.897553144201652;
+      w[62] = 0.027402609499462;
+      r[63] = -0.531632641825188;
+      s[63] = 0.431035654635683;
+      w[63] = 0.025014173853794;
+      r[64] = 0.431035654635683;
+      s[64] = -0.531632641825188;
+      w[64] = 0.025014173853794;
+      r[65] = -0.899403012810496;
+      s[65] = 0.431035654635683;
+      w[65] = 0.025014173853794;
+      r[66] = 0.431035654635683;
+      s[66] = -0.899403012810496;
+      w[66] = 0.025014173853794;
+      r[67] = -0.899403012810496;
+      s[67] = -0.531632641825188;
+      w[67] = 0.025014173853794;
+      r[68] = -0.531632641825188;
+      s[68] = -0.899403012810496;
+      w[68] = 0.025014173853794;
+      r[69] = -0.682130525363537;
+      s[69] = 0.500223407469218;
+      w[69] = 0.008690112508894;
+      r[70] = 0.500223407469218;
+      s[70] = -0.682130525363537;
+      w[70] = 0.008690112508894;
+      r[71] = -0.818092882105681;
+      s[71] = 0.500223407469218;
+      w[71] = 0.008690112508894;
+      r[72] = 0.500223407469218;
+      s[72] = -0.818092882105681;
+      w[72] = 0.008690112508894;
+      r[73] = -0.818092882105681;
+      s[73] = -0.682130525363537;
+      w[73] = 0.008690112508894;
+      r[74] = -0.682130525363537;
+      s[74] = -0.818092882105681;
+      w[74] = 0.008690112508894;
+      r[75] = -0.376270450471865;
+      s[75] = 0.138207573987544;
+      w[75] = 0.037386369243416;
+      r[76] = 0.138207573987544;
+      s[76] = -0.376270450471865;
+      w[76] = 0.037386369243416;
+      r[77] = -0.761937123515678;
+      s[77] = 0.138207573987544;
+      w[77] = 0.037386369243416;
+      r[78] = 0.138207573987544;
+      s[78] = -0.761937123515678;
+      w[78] = 0.037386369243416;
+      r[79] = -0.761937123515678;
+      s[79] = -0.376270450471865;
+      w[79] = 0.037386369243416;
+      r[80] = -0.376270450471865;
+      s[80] = -0.761937123515678;
+      w[80] = 0.037386369243416;
+      r[81] = -0.590719081005038;
+      s[81] = 0.339375331943743;
+      w[81] = 0.032509611084921;
+      r[82] = 0.339375331943743;
+      s[82] = -0.590719081005038;
+      w[82] = 0.032509611084921;
+      r[83] = -0.748656250938705;
+      s[83] = 0.339375331943743;
+      w[83] = 0.032509611084921;
+      r[84] = 0.339375331943743;
+      s[84] = -0.748656250938705;
+      w[84] = 0.032509611084921;
+      r[85] = -0.748656250938705;
+      s[85] = -0.590719081005038;
+      w[85] = 0.032509611084921;
+      r[86] = -0.590719081005038;
+      s[86] = -0.748656250938705;
+      w[86] = 0.032509611084921;
+      r[87] = -0.305527033262063;
+      s[87] = -0.081590222620926;
+      w[87] = 0.043740300619054;
+      r[88] = -0.081590222620926;
+      s[88] = -0.305527033262063;
+      w[88] = 0.043740300619054;
+      r[89] = -0.612882744117011;
+      s[89] = -0.081590222620926;
+      w[89] = 0.043740300619054;
+      r[90] = -0.081590222620926;
+      s[90] = -0.612882744117011;
+      w[90] = 0.043740300619054;
+      r[91] = -0.612882744117011;
+      s[91] = -0.305527033262063;
+      w[91] = 0.043740300619054;
+      r[92] = -0.305527033262063;
+      s[92] = -0.612882744117011;
+      w[92] = 0.043740300619054;
 
       break;
     }
     case 22: {
-      r[0]   = -0.333333333333333; s[0]   = -0.333333333333333; w[0]   = 0.052134891986775;
-      r[1]   = -0.005980679319437; s[1]   = -0.005980679319437; w[1]   = 0.002127559342619;
-      r[2]   = -0.988038641361126; s[2]   = -0.005980679319437; w[2]   = 0.002127559342619;
-      r[3]   = -0.005980679319437; s[3]   = -0.988038641361126; w[3]   = 0.002127559342619;
-      r[4]   = -0.112289615572167; s[4]   = -0.112289615572167; w[4]   = 0.040243429730281;
-      r[5]   = -0.775420768855665; s[5]   = -0.112289615572167; w[5]   = 0.040243429730281;
-      r[6]   = -0.112289615572167; s[6]   = -0.775420768855665; w[6]   = 0.040243429730281;
-      r[7]   = -0.209082673923590; s[7]   = -0.209082673923590; w[7]   = 0.048340550896214;
-      r[8]   = -0.581834652152820; s[8]   = -0.209082673923590; w[8]   = 0.048340550896214;
-      r[9]   = -0.209082673923590; s[9]   = -0.581834652152820; w[9]   = 0.048340550896214;
-      r[10]  = -0.467712894350161; s[10]  = -0.467712894350161; w[10]  = 0.047378470721283;
-      r[11]  = -0.064574211299679; s[11]  = -0.467712894350161; w[11]  = 0.047378470721283;
-      r[12]  = -0.467712894350161; s[12]  = -0.064574211299679; w[12]  = 0.047378470721283;
-      r[13]  = -0.616276252022817; s[13]  = -0.616276252022817; w[13]  = 0.040231109011798;
-      r[14]  =  0.232552504045635; s[14]  = -0.616276252022817; w[14]  = 0.040231109011798;
-      r[15]  = -0.616276252022817; s[15]  =  0.232552504045635; w[15]  = 0.040231109011798;
-      r[16]  = -0.755246756631224; s[16]  = -0.755246756631224; w[16]  = 0.027899919845537;
-      r[17]  =  0.510493513262448; s[17]  = -0.755246756631224; w[17]  = 0.027899919845537;
-      r[18]  = -0.755246756631224; s[18]  =  0.510493513262448; w[18]  = 0.027899919845537;
-      r[19]  = -0.893562558892192; s[19]  = -0.893562558892192; w[19]  = 0.012350949744993;
-      r[20]  =  0.787125117784384; s[20]  = -0.893562558892192; w[20]  = 0.012350949744993;
-      r[21]  = -0.893562558892192; s[21]  =  0.787125117784384; w[21]  = 0.012350949744993;
-      r[22]  = -0.943105536827199; s[22]  = -0.943105536827199; w[22]  = 0.003039705316805;
-      r[23]  =  0.886211073654399; s[23]  = -0.943105536827199; w[23]  = 0.003039705316805;
-      r[24]  = -0.943105536827199; s[24]  =  0.886211073654399; w[24]  = 0.003039705316805;
-      r[25]  = -0.991786296535875; s[25]  = -0.991786296535875; w[25]  = 0.000691671630889;
-      r[26]  =  0.983572593071750; s[26]  = -0.991786296535875; w[26]  = 0.000691671630889;
-      r[27]  = -0.991786296535875; s[27]  =  0.983572593071750; w[27]  = 0.000691671630889;
-      r[28]  = -0.413667191986728; s[28]  =  0.401491377065593; w[28]  = 0.008022198405286;
-      r[29]  =  0.401491377065593; s[29]  = -0.413667191986728; w[29]  = 0.008022198405286;
-      r[30]  = -0.987824185078864; s[30]  =  0.401491377065593; w[30]  = 0.008022198405286;
-      r[31]  =  0.401491377065593; s[31]  = -0.987824185078864; w[31]  = 0.008022198405286;
-      r[32]  = -0.987824185078865; s[32]  = -0.413667191986728; w[32]  = 0.008022198405286;
-      r[33]  = -0.413667191986728; s[33]  = -0.987824185078865; w[33]  = 0.008022198405286;
-      r[34]  = -0.932052869826067; s[34]  =  0.918490219898898; w[34]  = 0.003090974933637;
-      r[35]  =  0.918490219898898; s[35]  = -0.932052869826067; w[35]  = 0.003090974933637;
-      r[36]  = -0.986437350072830; s[36]  =  0.918490219898898; w[36]  = 0.003090974933637;
-      r[37]  =  0.918490219898898; s[37]  = -0.986437350072830; w[37]  = 0.003090974933637;
-      r[38]  = -0.986437350072830; s[38]  = -0.932052869826067; w[38]  = 0.003090974933637;
-      r[39]  = -0.932052869826067; s[39]  = -0.986437350072830; w[39]  = 0.003090974933637;
-      r[40]  = -0.640599464469824; s[40]  =  0.623868058857117; w[40]  = 0.008631214056178;
-      r[41]  =  0.623868058857117; s[41]  = -0.640599464469824; w[41]  = 0.008631214056178;
-      r[42]  = -0.983268594387293; s[42]  =  0.623868058857116; w[42]  = 0.008631214056178;
-      r[43]  =  0.623868058857116; s[43]  = -0.983268594387293; w[43]  = 0.008631214056178;
-      r[44]  = -0.983268594387293; s[44]  = -0.640599464469824; w[44]  = 0.008631214056178;
-      r[45]  = -0.640599464469824; s[45]  = -0.983268594387293; w[45]  = 0.008631214056178;
-      r[46]  = -0.158411570812104; s[46]  =  0.140890429939385; w[46]  = 0.010897457944070;
-      r[47]  =  0.140890429939385; s[47]  = -0.158411570812104; w[47]  = 0.010897457944070;
-      r[48]  = -0.982478859127282; s[48]  =  0.140890429939385; w[48]  = 0.010897457944070;
-      r[49]  =  0.140890429939385; s[49]  = -0.982478859127282; w[49]  = 0.010897457944070;
-      r[50]  = -0.982478859127282; s[50]  = -0.158411570812104; w[50]  = 0.010897457944070;
-      r[51]  = -0.158411570812104; s[51]  = -0.982478859127282; w[51]  = 0.010897457944070;
-      r[52]  = -0.814806216564922; s[52]  =  0.793459188393794; w[52]  = 0.008001551263950;
-      r[53]  =  0.793459188393794; s[53]  = -0.814806216564922; w[53]  = 0.008001551263950;
-      r[54]  = -0.978652971828873; s[54]  =  0.793459188393795; w[54]  = 0.008001551263950;
-      r[55]  =  0.793459188393795; s[55]  = -0.978652971828873; w[55]  = 0.008001551263950;
-      r[56]  = -0.978652971828873; s[56]  = -0.814806216564922; w[56]  = 0.008001551263950;
-      r[57]  = -0.814806216564922; s[57]  = -0.978652971828873; w[57]  = 0.008001551263950;
-      r[58]  = -0.363960589331557; s[58]  =  0.295112627690632; w[58]  = 0.017745434082141;
-      r[59]  =  0.295112627690632; s[59]  = -0.363960589331557; w[59]  = 0.017745434082141;
-      r[60]  = -0.931152038359075; s[60]  =  0.295112627690632; w[60]  = 0.017745434082141;
-      r[61]  =  0.295112627690632; s[61]  = -0.931152038359075; w[61]  = 0.017745434082141;
-      r[62]  = -0.931152038359075; s[62]  = -0.363960589331557; w[62]  = 0.017745434082141;
-      r[63]  = -0.363960589331557; s[63]  = -0.931152038359075; w[63]  = 0.017745434082141;
-      r[64]  = -0.570323384314285; s[64]  =  0.491002374048080; w[64]  = 0.017950672107247;
-      r[65]  =  0.491002374048080; s[65]  = -0.570323384314285; w[65]  = 0.017950672107247;
-      r[66]  = -0.920678989733795; s[66]  =  0.491002374048080; w[66]  = 0.017950672107247;
-      r[67]  =  0.491002374048080; s[67]  = -0.920678989733795; w[67]  = 0.017950672107247;
-      r[68]  = -0.920678989733795; s[68]  = -0.570323384314285; w[68]  = 0.017950672107247;
-      r[69]  = -0.570323384314285; s[69]  = -0.920678989733795; w[69]  = 0.017950672107247;
-      r[70]  = -0.134636707603169; s[70]  =  0.047157943371727; w[70]  = 0.019228676191702;
-      r[71]  =  0.047157943371727; s[71]  = -0.134636707603169; w[71]  = 0.019228676191702;
-      r[72]  = -0.912521235768557; s[72]  =  0.047157943371727; w[72]  = 0.019228676191702;
-      r[73]  =  0.047157943371727; s[73]  = -0.912521235768557; w[73]  = 0.019228676191702;
-      r[74]  = -0.912521235768557; s[74]  = -0.134636707603169; w[74]  = 0.019228676191702;
-      r[75]  = -0.134636707603169; s[75]  = -0.912521235768557; w[75]  = 0.019228676191702;
-      r[76]  = -0.752804662376914; s[76]  =  0.649201355096884; w[76]  = 0.019100455942623;
-      r[77]  =  0.649201355096884; s[77]  = -0.752804662376914; w[77]  = 0.019100455942623;
-      r[78]  = -0.896396692719970; s[78]  =  0.649201355096884; w[78]  = 0.019100455942623;
-      r[79]  =  0.649201355096884; s[79]  = -0.896396692719970; w[79]  = 0.019100455942623;
-      r[80]  = -0.896396692719970; s[80]  = -0.752804662376914; w[80]  = 0.019100455942623;
-      r[81]  = -0.752804662376914; s[81]  = -0.896396692719970; w[81]  = 0.019100455942623;
-      r[82]  = -0.328638645186542; s[82]  =  0.161176552903625; w[82]  = 0.028083739150636;
-      r[83]  =  0.161176552903625; s[83]  = -0.328638645186542; w[83]  = 0.028083739150636;
-      r[84]  = -0.832537907717083; s[84]  =  0.161176552903625; w[84]  = 0.028083739150636;
-      r[85]  =  0.161176552903625; s[85]  = -0.832537907717083; w[85]  = 0.028083739150636;
-      r[86]  = -0.832537907717083; s[86]  = -0.328638645186542; w[86]  = 0.028083739150636;
-      r[87]  = -0.328638645186542; s[87]  = -0.832537907717083; w[87]  = 0.028083739150636;
-      r[88]  = -0.559939069093864; s[88]  =  0.361861076343249; w[88]  = 0.031874915632607;
-      r[89]  =  0.361861076343249; s[89]  = -0.559939069093864; w[89]  = 0.031874915632607;
-      r[90]  = -0.801922007249385; s[90]  =  0.361861076343249; w[90]  = 0.031874915632607;
-      r[91]  =  0.361861076343249; s[91]  = -0.801922007249385; w[91]  = 0.031874915632607;
-      r[92]  = -0.801922007249385; s[92]  = -0.559939069093864; w[92]  = 0.031874915632607;
-      r[93]  = -0.559939069093864; s[93]  = -0.801922007249385; w[93]  = 0.031874915632607;
-      r[94]  = -0.388196135129182; s[94]  =  0.068617773977901; w[94]  = 0.040865211838584;
-      r[95]  =  0.068617773977901; s[95]  = -0.388196135129182; w[95]  = 0.040865211838584;
-      r[96]  = -0.680421638848718; s[96]  =  0.068617773977901; w[96]  = 0.040865211838584;
-      r[97]  =  0.068617773977901; s[97]  = -0.680421638848718; w[97]  = 0.040865211838584;
-      r[98]  = -0.680421638848718; s[98]  = -0.388196135129182; w[98]  = 0.040865211838584;
-      r[99]  = -0.388196135129182; s[99]  = -0.680421638848718; w[99]  = 0.040865211838584;
+      r[0] = -0.333333333333333;
+      s[0] = -0.333333333333333;
+      w[0] = 0.052134891986775;
+      r[1] = -0.005980679319437;
+      s[1] = -0.005980679319437;
+      w[1] = 0.002127559342619;
+      r[2] = -0.988038641361126;
+      s[2] = -0.005980679319437;
+      w[2] = 0.002127559342619;
+      r[3] = -0.005980679319437;
+      s[3] = -0.988038641361126;
+      w[3] = 0.002127559342619;
+      r[4] = -0.112289615572167;
+      s[4] = -0.112289615572167;
+      w[4] = 0.040243429730281;
+      r[5] = -0.775420768855665;
+      s[5] = -0.112289615572167;
+      w[5] = 0.040243429730281;
+      r[6] = -0.112289615572167;
+      s[6] = -0.775420768855665;
+      w[6] = 0.040243429730281;
+      r[7] = -0.209082673923590;
+      s[7] = -0.209082673923590;
+      w[7] = 0.048340550896214;
+      r[8] = -0.581834652152820;
+      s[8] = -0.209082673923590;
+      w[8] = 0.048340550896214;
+      r[9] = -0.209082673923590;
+      s[9] = -0.581834652152820;
+      w[9] = 0.048340550896214;
+      r[10] = -0.467712894350161;
+      s[10] = -0.467712894350161;
+      w[10] = 0.047378470721283;
+      r[11] = -0.064574211299679;
+      s[11] = -0.467712894350161;
+      w[11] = 0.047378470721283;
+      r[12] = -0.467712894350161;
+      s[12] = -0.064574211299679;
+      w[12] = 0.047378470721283;
+      r[13] = -0.616276252022817;
+      s[13] = -0.616276252022817;
+      w[13] = 0.040231109011798;
+      r[14] = 0.232552504045635;
+      s[14] = -0.616276252022817;
+      w[14] = 0.040231109011798;
+      r[15] = -0.616276252022817;
+      s[15] = 0.232552504045635;
+      w[15] = 0.040231109011798;
+      r[16] = -0.755246756631224;
+      s[16] = -0.755246756631224;
+      w[16] = 0.027899919845537;
+      r[17] = 0.510493513262448;
+      s[17] = -0.755246756631224;
+      w[17] = 0.027899919845537;
+      r[18] = -0.755246756631224;
+      s[18] = 0.510493513262448;
+      w[18] = 0.027899919845537;
+      r[19] = -0.893562558892192;
+      s[19] = -0.893562558892192;
+      w[19] = 0.012350949744993;
+      r[20] = 0.787125117784384;
+      s[20] = -0.893562558892192;
+      w[20] = 0.012350949744993;
+      r[21] = -0.893562558892192;
+      s[21] = 0.787125117784384;
+      w[21] = 0.012350949744993;
+      r[22] = -0.943105536827199;
+      s[22] = -0.943105536827199;
+      w[22] = 0.003039705316805;
+      r[23] = 0.886211073654399;
+      s[23] = -0.943105536827199;
+      w[23] = 0.003039705316805;
+      r[24] = -0.943105536827199;
+      s[24] = 0.886211073654399;
+      w[24] = 0.003039705316805;
+      r[25] = -0.991786296535875;
+      s[25] = -0.991786296535875;
+      w[25] = 0.000691671630889;
+      r[26] = 0.983572593071750;
+      s[26] = -0.991786296535875;
+      w[26] = 0.000691671630889;
+      r[27] = -0.991786296535875;
+      s[27] = 0.983572593071750;
+      w[27] = 0.000691671630889;
+      r[28] = -0.413667191986728;
+      s[28] = 0.401491377065593;
+      w[28] = 0.008022198405286;
+      r[29] = 0.401491377065593;
+      s[29] = -0.413667191986728;
+      w[29] = 0.008022198405286;
+      r[30] = -0.987824185078864;
+      s[30] = 0.401491377065593;
+      w[30] = 0.008022198405286;
+      r[31] = 0.401491377065593;
+      s[31] = -0.987824185078864;
+      w[31] = 0.008022198405286;
+      r[32] = -0.987824185078865;
+      s[32] = -0.413667191986728;
+      w[32] = 0.008022198405286;
+      r[33] = -0.413667191986728;
+      s[33] = -0.987824185078865;
+      w[33] = 0.008022198405286;
+      r[34] = -0.932052869826067;
+      s[34] = 0.918490219898898;
+      w[34] = 0.003090974933637;
+      r[35] = 0.918490219898898;
+      s[35] = -0.932052869826067;
+      w[35] = 0.003090974933637;
+      r[36] = -0.986437350072830;
+      s[36] = 0.918490219898898;
+      w[36] = 0.003090974933637;
+      r[37] = 0.918490219898898;
+      s[37] = -0.986437350072830;
+      w[37] = 0.003090974933637;
+      r[38] = -0.986437350072830;
+      s[38] = -0.932052869826067;
+      w[38] = 0.003090974933637;
+      r[39] = -0.932052869826067;
+      s[39] = -0.986437350072830;
+      w[39] = 0.003090974933637;
+      r[40] = -0.640599464469824;
+      s[40] = 0.623868058857117;
+      w[40] = 0.008631214056178;
+      r[41] = 0.623868058857117;
+      s[41] = -0.640599464469824;
+      w[41] = 0.008631214056178;
+      r[42] = -0.983268594387293;
+      s[42] = 0.623868058857116;
+      w[42] = 0.008631214056178;
+      r[43] = 0.623868058857116;
+      s[43] = -0.983268594387293;
+      w[43] = 0.008631214056178;
+      r[44] = -0.983268594387293;
+      s[44] = -0.640599464469824;
+      w[44] = 0.008631214056178;
+      r[45] = -0.640599464469824;
+      s[45] = -0.983268594387293;
+      w[45] = 0.008631214056178;
+      r[46] = -0.158411570812104;
+      s[46] = 0.140890429939385;
+      w[46] = 0.010897457944070;
+      r[47] = 0.140890429939385;
+      s[47] = -0.158411570812104;
+      w[47] = 0.010897457944070;
+      r[48] = -0.982478859127282;
+      s[48] = 0.140890429939385;
+      w[48] = 0.010897457944070;
+      r[49] = 0.140890429939385;
+      s[49] = -0.982478859127282;
+      w[49] = 0.010897457944070;
+      r[50] = -0.982478859127282;
+      s[50] = -0.158411570812104;
+      w[50] = 0.010897457944070;
+      r[51] = -0.158411570812104;
+      s[51] = -0.982478859127282;
+      w[51] = 0.010897457944070;
+      r[52] = -0.814806216564922;
+      s[52] = 0.793459188393794;
+      w[52] = 0.008001551263950;
+      r[53] = 0.793459188393794;
+      s[53] = -0.814806216564922;
+      w[53] = 0.008001551263950;
+      r[54] = -0.978652971828873;
+      s[54] = 0.793459188393795;
+      w[54] = 0.008001551263950;
+      r[55] = 0.793459188393795;
+      s[55] = -0.978652971828873;
+      w[55] = 0.008001551263950;
+      r[56] = -0.978652971828873;
+      s[56] = -0.814806216564922;
+      w[56] = 0.008001551263950;
+      r[57] = -0.814806216564922;
+      s[57] = -0.978652971828873;
+      w[57] = 0.008001551263950;
+      r[58] = -0.363960589331557;
+      s[58] = 0.295112627690632;
+      w[58] = 0.017745434082141;
+      r[59] = 0.295112627690632;
+      s[59] = -0.363960589331557;
+      w[59] = 0.017745434082141;
+      r[60] = -0.931152038359075;
+      s[60] = 0.295112627690632;
+      w[60] = 0.017745434082141;
+      r[61] = 0.295112627690632;
+      s[61] = -0.931152038359075;
+      w[61] = 0.017745434082141;
+      r[62] = -0.931152038359075;
+      s[62] = -0.363960589331557;
+      w[62] = 0.017745434082141;
+      r[63] = -0.363960589331557;
+      s[63] = -0.931152038359075;
+      w[63] = 0.017745434082141;
+      r[64] = -0.570323384314285;
+      s[64] = 0.491002374048080;
+      w[64] = 0.017950672107247;
+      r[65] = 0.491002374048080;
+      s[65] = -0.570323384314285;
+      w[65] = 0.017950672107247;
+      r[66] = -0.920678989733795;
+      s[66] = 0.491002374048080;
+      w[66] = 0.017950672107247;
+      r[67] = 0.491002374048080;
+      s[67] = -0.920678989733795;
+      w[67] = 0.017950672107247;
+      r[68] = -0.920678989733795;
+      s[68] = -0.570323384314285;
+      w[68] = 0.017950672107247;
+      r[69] = -0.570323384314285;
+      s[69] = -0.920678989733795;
+      w[69] = 0.017950672107247;
+      r[70] = -0.134636707603169;
+      s[70] = 0.047157943371727;
+      w[70] = 0.019228676191702;
+      r[71] = 0.047157943371727;
+      s[71] = -0.134636707603169;
+      w[71] = 0.019228676191702;
+      r[72] = -0.912521235768557;
+      s[72] = 0.047157943371727;
+      w[72] = 0.019228676191702;
+      r[73] = 0.047157943371727;
+      s[73] = -0.912521235768557;
+      w[73] = 0.019228676191702;
+      r[74] = -0.912521235768557;
+      s[74] = -0.134636707603169;
+      w[74] = 0.019228676191702;
+      r[75] = -0.134636707603169;
+      s[75] = -0.912521235768557;
+      w[75] = 0.019228676191702;
+      r[76] = -0.752804662376914;
+      s[76] = 0.649201355096884;
+      w[76] = 0.019100455942623;
+      r[77] = 0.649201355096884;
+      s[77] = -0.752804662376914;
+      w[77] = 0.019100455942623;
+      r[78] = -0.896396692719970;
+      s[78] = 0.649201355096884;
+      w[78] = 0.019100455942623;
+      r[79] = 0.649201355096884;
+      s[79] = -0.896396692719970;
+      w[79] = 0.019100455942623;
+      r[80] = -0.896396692719970;
+      s[80] = -0.752804662376914;
+      w[80] = 0.019100455942623;
+      r[81] = -0.752804662376914;
+      s[81] = -0.896396692719970;
+      w[81] = 0.019100455942623;
+      r[82] = -0.328638645186542;
+      s[82] = 0.161176552903625;
+      w[82] = 0.028083739150636;
+      r[83] = 0.161176552903625;
+      s[83] = -0.328638645186542;
+      w[83] = 0.028083739150636;
+      r[84] = -0.832537907717083;
+      s[84] = 0.161176552903625;
+      w[84] = 0.028083739150636;
+      r[85] = 0.161176552903625;
+      s[85] = -0.832537907717083;
+      w[85] = 0.028083739150636;
+      r[86] = -0.832537907717083;
+      s[86] = -0.328638645186542;
+      w[86] = 0.028083739150636;
+      r[87] = -0.328638645186542;
+      s[87] = -0.832537907717083;
+      w[87] = 0.028083739150636;
+      r[88] = -0.559939069093864;
+      s[88] = 0.361861076343249;
+      w[88] = 0.031874915632607;
+      r[89] = 0.361861076343249;
+      s[89] = -0.559939069093864;
+      w[89] = 0.031874915632607;
+      r[90] = -0.801922007249385;
+      s[90] = 0.361861076343249;
+      w[90] = 0.031874915632607;
+      r[91] = 0.361861076343249;
+      s[91] = -0.801922007249385;
+      w[91] = 0.031874915632607;
+      r[92] = -0.801922007249385;
+      s[92] = -0.559939069093864;
+      w[92] = 0.031874915632607;
+      r[93] = -0.559939069093864;
+      s[93] = -0.801922007249385;
+      w[93] = 0.031874915632607;
+      r[94] = -0.388196135129182;
+      s[94] = 0.068617773977901;
+      w[94] = 0.040865211838584;
+      r[95] = 0.068617773977901;
+      s[95] = -0.388196135129182;
+      w[95] = 0.040865211838584;
+      r[96] = -0.680421638848718;
+      s[96] = 0.068617773977901;
+      w[96] = 0.040865211838584;
+      r[97] = 0.068617773977901;
+      s[97] = -0.680421638848718;
+      w[97] = 0.040865211838584;
+      r[98] = -0.680421638848718;
+      s[98] = -0.388196135129182;
+      w[98] = 0.040865211838584;
+      r[99] = -0.388196135129182;
+      s[99] = -0.680421638848718;
+      w[99] = 0.040865211838584;
 
       break;
     }
     case 23: {
-      r[0]   = -0.333333333333333; s[0]   = -0.333333333333333; w[0]   = 0.049993627092845;
-      r[1]   = -0.023538910955543; s[1]   = -0.023538910955543; w[1]   = 0.008227775544650;
-      r[2]   = -0.952922178088914; s[2]   = -0.023538910955543; w[2]   = 0.008227775544650;
-      r[3]   = -0.023538910955543; s[3]   = -0.952922178088914; w[3]   = 0.008227775544650;
-      r[4]   = -0.112255282121933; s[4]   = -0.112255282121933; w[4]   = 0.037662477311797;
-      r[5]   = -0.775489435756134; s[5]   = -0.112255282121933; w[5]   = 0.037662477311797;
-      r[6]   = -0.112255282121933; s[6]   = -0.775489435756134; w[6]   = 0.037662477311797;
-      r[7]   = -0.212088442838205; s[7]   = -0.212088442838205; w[7]   = 0.046916667243031;
-      r[8]   = -0.575823114323591; s[8]   = -0.212088442838205; w[8]   = 0.046916667243031;
-      r[9]   = -0.212088442838205; s[9]   = -0.575823114323591; w[9]   = 0.046916667243031;
-      r[10]  = -0.467032671065063; s[10]  = -0.467032671065063; w[10]  = 0.047191879210718;
-      r[11]  = -0.065934657869875; s[11]  = -0.467032671065063; w[11]  = 0.047191879210718;
-      r[12]  = -0.467032671065063; s[12]  = -0.065934657869875; w[12]  = 0.047191879210718;
-      r[13]  = -0.602458675644835; s[13]  = -0.602458675644835; w[13]  = 0.039689081561875;
-      r[14]  =  0.204917351289670; s[14]  = -0.602458675644835; w[14]  = 0.039689081561875;
-      r[15]  = -0.602458675644835; s[15]  =  0.204917351289670; w[15]  = 0.039689081561875;
-      r[16]  = -0.729340080155585; s[16]  = -0.729340080155585; w[16]  = 0.029223692430473;
-      r[17]  =  0.458680160311169; s[17]  = -0.729340080155585; w[17]  = 0.029223692430473;
-      r[18]  = -0.729340080155585; s[18]  =  0.458680160311169; w[18]  = 0.029223692430473;
-      r[19]  = -0.835032835950571; s[19]  = -0.835032835950571; w[19]  = 0.018566057479642;
-      r[20]  =  0.670065671901142; s[20]  = -0.835032835950571; w[20]  = 0.018566057479642;
-      r[21]  = -0.835032835950571; s[21]  =  0.670065671901142; w[21]  = 0.018566057479642;
-      r[22]  = -0.916650365183127; s[22]  = -0.916650365183127; w[22]  = 0.008784960019827;
-      r[23]  =  0.833300730366254; s[23]  = -0.916650365183127; w[23]  = 0.008784960019827;
-      r[24]  = -0.916650365183127; s[24]  =  0.833300730366254; w[24]  = 0.008784960019827;
-      r[25]  = -0.982250743407210; s[25]  = -0.982250743407210; w[25]  = 0.002061552741126;
-      r[26]  =  0.964501486814420; s[26]  = -0.982250743407210; w[26]  = 0.002061552741126;
-      r[27]  = -0.982250743407210; s[27]  =  0.964501486814420; w[27]  = 0.002061552741126;
-      r[28]  = -0.105601712649592; s[28]  =  0.098292547426640; w[28]  = 0.004448377162851;
-      r[29]  =  0.098292547426640; s[29]  = -0.105601712649592; w[29]  = 0.004448377162851;
-      r[30]  = -0.992690834777047; s[30]  =  0.098292547426640; w[30]  = 0.004448377162851;
-      r[31]  =  0.098292547426640; s[31]  = -0.992690834777047; w[31]  = 0.004448377162851;
-      r[32]  = -0.992690834777047; s[32]  = -0.105601712649592; w[32]  = 0.004448377162851;
-      r[33]  = -0.105601712649592; s[33]  = -0.992690834777047; w[33]  = 0.004448377162851;
-      r[34]  = -0.775227228315076; s[34]  =  0.773362241907340; w[34]  = 0.002318973002522;
-      r[35]  =  0.773362241907340; s[35]  = -0.775227228315076; w[35]  = 0.002318973002522;
-      r[36]  = -0.998135013592264; s[36]  =  0.773362241907340; w[36]  = 0.002318973002522;
-      r[37]  =  0.773362241907340; s[37]  = -0.998135013592264; w[37]  = 0.002318973002522;
-      r[38]  = -0.998135013592264; s[38]  = -0.775227228315076; w[38]  = 0.002318973002522;
-      r[39]  = -0.775227228315076; s[39]  = -0.998135013592264; w[39]  = 0.002318973002522;
-      r[40]  = -0.399056075238285; s[40]  =  0.392811698367078; w[40]  = 0.005127488569570;
-      r[41]  =  0.392811698367078; s[41]  = -0.399056075238285; w[41]  = 0.005127488569570;
-      r[42]  = -0.993755623128794; s[42]  =  0.392811698367078; w[42]  = 0.005127488569570;
-      r[43]  =  0.392811698367078; s[43]  = -0.993755623128794; w[43]  = 0.005127488569570;
-      r[44]  = -0.993755623128794; s[44]  = -0.399056075238285; w[44]  = 0.005127488569570;
-      r[45]  = -0.399056075238285; s[45]  = -0.993755623128794; w[45]  = 0.005127488569570;
-      r[46]  = -0.907633572417643; s[46]  =  0.891831436837026; w[46]  = 0.004167853762943;
-      r[47]  =  0.891831436837026; s[47]  = -0.907633572417643; w[47]  = 0.004167853762943;
-      r[48]  = -0.984197864419384; s[48]  =  0.891831436837026; w[48]  = 0.004167853762943;
-      r[49]  =  0.891831436837026; s[49]  = -0.984197864419384; w[49]  = 0.004167853762943;
-      r[50]  = -0.984197864419383; s[50]  = -0.907633572417642; w[50]  = 0.004167853762943;
-      r[51]  = -0.907633572417642; s[51]  = -0.984197864419383; w[51]  = 0.004167853762943;
-      r[52]  = -0.610008084404048; s[52]  =  0.588812673873118; w[52]  = 0.010245094978581;
-      r[53]  =  0.588812673873118; s[53]  = -0.610008084404048; w[53]  = 0.010245094978581;
-      r[54]  = -0.978804589469070; s[54]  =  0.588812673873118; w[54]  = 0.010245094978581;
-      r[55]  =  0.588812673873118; s[55]  = -0.978804589469070; w[55]  = 0.010245094978581;
-      r[56]  = -0.978804589469070; s[56]  = -0.610008084404048; w[56]  = 0.010245094978581;
-      r[57]  = -0.610008084404048; s[57]  = -0.978804589469070; w[57]  = 0.010245094978581;
-      r[58]  = -0.243171741354056; s[58]  =  0.207960140279272; w[58]  = 0.012823590639281;
-      r[59]  =  0.207960140279272; s[59]  = -0.243171741354056; w[59]  = 0.012823590639281;
-      r[60]  = -0.964788398925216; s[60]  =  0.207960140279272; w[60]  = 0.012823590639281;
-      r[61]  =  0.207960140279272; s[61]  = -0.964788398925216; w[61]  = 0.012823590639281;
-      r[62]  = -0.964788398925216; s[62]  = -0.243171741354055; w[62]  = 0.012823590639281;
-      r[63]  = -0.243171741354055; s[63]  = -0.964788398925216; w[63]  = 0.012823590639281;
-      r[64]  = -0.789506197850739; s[64]  =  0.739925802118596; w[64]  = 0.011635516794817;
-      r[65]  =  0.739925802118596; s[65]  = -0.789506197850739; w[65]  = 0.011635516794817;
-      r[66]  = -0.950419604267857; s[66]  =  0.739925802118596; w[66]  = 0.011635516794817;
-      r[67]  =  0.739925802118596; s[67]  = -0.950419604267857; w[67]  = 0.011635516794817;
-      r[68]  = -0.950419604267857; s[68]  = -0.789506197850739; w[68]  = 0.011635516794817;
-      r[69]  = -0.789506197850739; s[69]  = -0.950419604267857; w[69]  = 0.011635516794817;
-      r[70]  = -0.455884762353173; s[70]  =  0.385117794610837; w[70]  = 0.019844273900077;
-      r[71]  =  0.385117794610837; s[71]  = -0.455884762353173; w[71]  = 0.019844273900077;
-      r[72]  = -0.929233032257664; s[72]  =  0.385117794610837; w[72]  = 0.019844273900077;
-      r[73]  =  0.385117794610837; s[73]  = -0.929233032257664; w[73]  = 0.019844273900077;
-      r[74]  = -0.929233032257664; s[74]  = -0.455884762353173; w[74]  = 0.019844273900077;
-      r[75]  = -0.455884762353173; s[75]  = -0.929233032257664; w[75]  = 0.019844273900077;
-      r[76]  = -0.112482048478797; s[76]  =  0.019740291196956; w[76]  = 0.011754407449188;
-      r[77]  =  0.019740291196956; s[77]  = -0.112482048478797; w[77]  = 0.011754407449188;
-      r[78]  = -0.907258242718159; s[78]  =  0.019740291196956; w[78]  = 0.011754407449188;
-      r[79]  =  0.019740291196956; s[79]  = -0.907258242718159; w[79]  = 0.011754407449188;
-      r[80]  = -0.907258242718159; s[80]  = -0.112482048478797; w[80]  = 0.011754407449188;
-      r[81]  = -0.112482048478797; s[81]  = -0.907258242718159; w[81]  = 0.011754407449188;
-      r[82]  = -0.664205324633765; s[82]  =  0.550530931038120; w[82]  = 0.021600208906600;
-      r[83]  =  0.550530931038120; s[83]  = -0.664205324633765; w[83]  = 0.021600208906600;
-      r[84]  = -0.886325606404355; s[84]  =  0.550530931038120; w[84]  = 0.021600208906600;
-      r[85]  =  0.550530931038120; s[85]  = -0.886325606404355; w[85]  = 0.021600208906600;
-      r[86]  = -0.886325606404354; s[86]  = -0.664205324633765; w[86]  = 0.021600208906600;
-      r[87]  = -0.664205324633765; s[87]  = -0.886325606404354; w[87]  = 0.021600208906600;
-      r[88]  = -0.295594853518405; s[88]  =  0.152149871080588; w[88]  = 0.028495796363599;
-      r[89]  =  0.152149871080588; s[89]  = -0.295594853518405; w[89]  = 0.028495796363599;
-      r[90]  = -0.856555017562183; s[90]  =  0.152149871080588; w[90]  = 0.028495796363599;
-      r[91]  =  0.152149871080588; s[91]  = -0.856555017562183; w[91]  = 0.028495796363599;
-      r[92]  = -0.856555017562183; s[92]  = -0.295594853518405; w[92]  = 0.028495796363599;
-      r[93]  = -0.295594853518405; s[93]  = -0.856555017562183; w[93]  = 0.028495796363599;
-      r[94]  = -0.525935282564036; s[94]  =  0.319991164262401; w[94]  = 0.031988381018369;
-      r[95]  =  0.319991164262401; s[95]  = -0.525935282564036; w[95]  = 0.031988381018369;
-      r[96]  = -0.794055881698366; s[96]  =  0.319991164262401; w[96]  = 0.031988381018369;
-      r[97]  =  0.319991164262401; s[97]  = -0.794055881698366; w[97]  = 0.031988381018369;
-      r[98]  = -0.794055881698366; s[98]  = -0.525935282564036; w[98]  = 0.031988381018369;
-      r[99]  = -0.525935282564036; s[99]  = -0.794055881698366; w[99]  = 0.031988381018369;
-      r[100] = -0.368673747852155; s[100] =  0.056982821883363; w[100] = 0.041389027831224;
-      r[101] =  0.056982821883363; s[101] = -0.368673747852155; w[101] = 0.041389027831224;
-      r[102] = -0.688309074031208; s[102] =  0.056982821883363; w[102] = 0.041389027831224;
-      r[103] =  0.056982821883363; s[103] = -0.688309074031208; w[103] = 0.041389027831224;
-      r[104] = -0.688309074031208; s[104] = -0.368673747852155; w[104] = 0.041389027831224;
-      r[105] = -0.368673747852155; s[105] = -0.688309074031208; w[105] = 0.041389027831224;
+      r[0] = -0.333333333333333;
+      s[0] = -0.333333333333333;
+      w[0] = 0.049993627092845;
+      r[1] = -0.023538910955543;
+      s[1] = -0.023538910955543;
+      w[1] = 0.008227775544650;
+      r[2] = -0.952922178088914;
+      s[2] = -0.023538910955543;
+      w[2] = 0.008227775544650;
+      r[3] = -0.023538910955543;
+      s[3] = -0.952922178088914;
+      w[3] = 0.008227775544650;
+      r[4] = -0.112255282121933;
+      s[4] = -0.112255282121933;
+      w[4] = 0.037662477311797;
+      r[5] = -0.775489435756134;
+      s[5] = -0.112255282121933;
+      w[5] = 0.037662477311797;
+      r[6] = -0.112255282121933;
+      s[6] = -0.775489435756134;
+      w[6] = 0.037662477311797;
+      r[7] = -0.212088442838205;
+      s[7] = -0.212088442838205;
+      w[7] = 0.046916667243031;
+      r[8] = -0.575823114323591;
+      s[8] = -0.212088442838205;
+      w[8] = 0.046916667243031;
+      r[9] = -0.212088442838205;
+      s[9] = -0.575823114323591;
+      w[9] = 0.046916667243031;
+      r[10] = -0.467032671065063;
+      s[10] = -0.467032671065063;
+      w[10] = 0.047191879210718;
+      r[11] = -0.065934657869875;
+      s[11] = -0.467032671065063;
+      w[11] = 0.047191879210718;
+      r[12] = -0.467032671065063;
+      s[12] = -0.065934657869875;
+      w[12] = 0.047191879210718;
+      r[13] = -0.602458675644835;
+      s[13] = -0.602458675644835;
+      w[13] = 0.039689081561875;
+      r[14] = 0.204917351289670;
+      s[14] = -0.602458675644835;
+      w[14] = 0.039689081561875;
+      r[15] = -0.602458675644835;
+      s[15] = 0.204917351289670;
+      w[15] = 0.039689081561875;
+      r[16] = -0.729340080155585;
+      s[16] = -0.729340080155585;
+      w[16] = 0.029223692430473;
+      r[17] = 0.458680160311169;
+      s[17] = -0.729340080155585;
+      w[17] = 0.029223692430473;
+      r[18] = -0.729340080155585;
+      s[18] = 0.458680160311169;
+      w[18] = 0.029223692430473;
+      r[19] = -0.835032835950571;
+      s[19] = -0.835032835950571;
+      w[19] = 0.018566057479642;
+      r[20] = 0.670065671901142;
+      s[20] = -0.835032835950571;
+      w[20] = 0.018566057479642;
+      r[21] = -0.835032835950571;
+      s[21] = 0.670065671901142;
+      w[21] = 0.018566057479642;
+      r[22] = -0.916650365183127;
+      s[22] = -0.916650365183127;
+      w[22] = 0.008784960019827;
+      r[23] = 0.833300730366254;
+      s[23] = -0.916650365183127;
+      w[23] = 0.008784960019827;
+      r[24] = -0.916650365183127;
+      s[24] = 0.833300730366254;
+      w[24] = 0.008784960019827;
+      r[25] = -0.982250743407210;
+      s[25] = -0.982250743407210;
+      w[25] = 0.002061552741126;
+      r[26] = 0.964501486814420;
+      s[26] = -0.982250743407210;
+      w[26] = 0.002061552741126;
+      r[27] = -0.982250743407210;
+      s[27] = 0.964501486814420;
+      w[27] = 0.002061552741126;
+      r[28] = -0.105601712649592;
+      s[28] = 0.098292547426640;
+      w[28] = 0.004448377162851;
+      r[29] = 0.098292547426640;
+      s[29] = -0.105601712649592;
+      w[29] = 0.004448377162851;
+      r[30] = -0.992690834777047;
+      s[30] = 0.098292547426640;
+      w[30] = 0.004448377162851;
+      r[31] = 0.098292547426640;
+      s[31] = -0.992690834777047;
+      w[31] = 0.004448377162851;
+      r[32] = -0.992690834777047;
+      s[32] = -0.105601712649592;
+      w[32] = 0.004448377162851;
+      r[33] = -0.105601712649592;
+      s[33] = -0.992690834777047;
+      w[33] = 0.004448377162851;
+      r[34] = -0.775227228315076;
+      s[34] = 0.773362241907340;
+      w[34] = 0.002318973002522;
+      r[35] = 0.773362241907340;
+      s[35] = -0.775227228315076;
+      w[35] = 0.002318973002522;
+      r[36] = -0.998135013592264;
+      s[36] = 0.773362241907340;
+      w[36] = 0.002318973002522;
+      r[37] = 0.773362241907340;
+      s[37] = -0.998135013592264;
+      w[37] = 0.002318973002522;
+      r[38] = -0.998135013592264;
+      s[38] = -0.775227228315076;
+      w[38] = 0.002318973002522;
+      r[39] = -0.775227228315076;
+      s[39] = -0.998135013592264;
+      w[39] = 0.002318973002522;
+      r[40] = -0.399056075238285;
+      s[40] = 0.392811698367078;
+      w[40] = 0.005127488569570;
+      r[41] = 0.392811698367078;
+      s[41] = -0.399056075238285;
+      w[41] = 0.005127488569570;
+      r[42] = -0.993755623128794;
+      s[42] = 0.392811698367078;
+      w[42] = 0.005127488569570;
+      r[43] = 0.392811698367078;
+      s[43] = -0.993755623128794;
+      w[43] = 0.005127488569570;
+      r[44] = -0.993755623128794;
+      s[44] = -0.399056075238285;
+      w[44] = 0.005127488569570;
+      r[45] = -0.399056075238285;
+      s[45] = -0.993755623128794;
+      w[45] = 0.005127488569570;
+      r[46] = -0.907633572417643;
+      s[46] = 0.891831436837026;
+      w[46] = 0.004167853762943;
+      r[47] = 0.891831436837026;
+      s[47] = -0.907633572417643;
+      w[47] = 0.004167853762943;
+      r[48] = -0.984197864419384;
+      s[48] = 0.891831436837026;
+      w[48] = 0.004167853762943;
+      r[49] = 0.891831436837026;
+      s[49] = -0.984197864419384;
+      w[49] = 0.004167853762943;
+      r[50] = -0.984197864419383;
+      s[50] = -0.907633572417642;
+      w[50] = 0.004167853762943;
+      r[51] = -0.907633572417642;
+      s[51] = -0.984197864419383;
+      w[51] = 0.004167853762943;
+      r[52] = -0.610008084404048;
+      s[52] = 0.588812673873118;
+      w[52] = 0.010245094978581;
+      r[53] = 0.588812673873118;
+      s[53] = -0.610008084404048;
+      w[53] = 0.010245094978581;
+      r[54] = -0.978804589469070;
+      s[54] = 0.588812673873118;
+      w[54] = 0.010245094978581;
+      r[55] = 0.588812673873118;
+      s[55] = -0.978804589469070;
+      w[55] = 0.010245094978581;
+      r[56] = -0.978804589469070;
+      s[56] = -0.610008084404048;
+      w[56] = 0.010245094978581;
+      r[57] = -0.610008084404048;
+      s[57] = -0.978804589469070;
+      w[57] = 0.010245094978581;
+      r[58] = -0.243171741354056;
+      s[58] = 0.207960140279272;
+      w[58] = 0.012823590639281;
+      r[59] = 0.207960140279272;
+      s[59] = -0.243171741354056;
+      w[59] = 0.012823590639281;
+      r[60] = -0.964788398925216;
+      s[60] = 0.207960140279272;
+      w[60] = 0.012823590639281;
+      r[61] = 0.207960140279272;
+      s[61] = -0.964788398925216;
+      w[61] = 0.012823590639281;
+      r[62] = -0.964788398925216;
+      s[62] = -0.243171741354055;
+      w[62] = 0.012823590639281;
+      r[63] = -0.243171741354055;
+      s[63] = -0.964788398925216;
+      w[63] = 0.012823590639281;
+      r[64] = -0.789506197850739;
+      s[64] = 0.739925802118596;
+      w[64] = 0.011635516794817;
+      r[65] = 0.739925802118596;
+      s[65] = -0.789506197850739;
+      w[65] = 0.011635516794817;
+      r[66] = -0.950419604267857;
+      s[66] = 0.739925802118596;
+      w[66] = 0.011635516794817;
+      r[67] = 0.739925802118596;
+      s[67] = -0.950419604267857;
+      w[67] = 0.011635516794817;
+      r[68] = -0.950419604267857;
+      s[68] = -0.789506197850739;
+      w[68] = 0.011635516794817;
+      r[69] = -0.789506197850739;
+      s[69] = -0.950419604267857;
+      w[69] = 0.011635516794817;
+      r[70] = -0.455884762353173;
+      s[70] = 0.385117794610837;
+      w[70] = 0.019844273900077;
+      r[71] = 0.385117794610837;
+      s[71] = -0.455884762353173;
+      w[71] = 0.019844273900077;
+      r[72] = -0.929233032257664;
+      s[72] = 0.385117794610837;
+      w[72] = 0.019844273900077;
+      r[73] = 0.385117794610837;
+      s[73] = -0.929233032257664;
+      w[73] = 0.019844273900077;
+      r[74] = -0.929233032257664;
+      s[74] = -0.455884762353173;
+      w[74] = 0.019844273900077;
+      r[75] = -0.455884762353173;
+      s[75] = -0.929233032257664;
+      w[75] = 0.019844273900077;
+      r[76] = -0.112482048478797;
+      s[76] = 0.019740291196956;
+      w[76] = 0.011754407449188;
+      r[77] = 0.019740291196956;
+      s[77] = -0.112482048478797;
+      w[77] = 0.011754407449188;
+      r[78] = -0.907258242718159;
+      s[78] = 0.019740291196956;
+      w[78] = 0.011754407449188;
+      r[79] = 0.019740291196956;
+      s[79] = -0.907258242718159;
+      w[79] = 0.011754407449188;
+      r[80] = -0.907258242718159;
+      s[80] = -0.112482048478797;
+      w[80] = 0.011754407449188;
+      r[81] = -0.112482048478797;
+      s[81] = -0.907258242718159;
+      w[81] = 0.011754407449188;
+      r[82] = -0.664205324633765;
+      s[82] = 0.550530931038120;
+      w[82] = 0.021600208906600;
+      r[83] = 0.550530931038120;
+      s[83] = -0.664205324633765;
+      w[83] = 0.021600208906600;
+      r[84] = -0.886325606404355;
+      s[84] = 0.550530931038120;
+      w[84] = 0.021600208906600;
+      r[85] = 0.550530931038120;
+      s[85] = -0.886325606404355;
+      w[85] = 0.021600208906600;
+      r[86] = -0.886325606404354;
+      s[86] = -0.664205324633765;
+      w[86] = 0.021600208906600;
+      r[87] = -0.664205324633765;
+      s[87] = -0.886325606404354;
+      w[87] = 0.021600208906600;
+      r[88] = -0.295594853518405;
+      s[88] = 0.152149871080588;
+      w[88] = 0.028495796363599;
+      r[89] = 0.152149871080588;
+      s[89] = -0.295594853518405;
+      w[89] = 0.028495796363599;
+      r[90] = -0.856555017562183;
+      s[90] = 0.152149871080588;
+      w[90] = 0.028495796363599;
+      r[91] = 0.152149871080588;
+      s[91] = -0.856555017562183;
+      w[91] = 0.028495796363599;
+      r[92] = -0.856555017562183;
+      s[92] = -0.295594853518405;
+      w[92] = 0.028495796363599;
+      r[93] = -0.295594853518405;
+      s[93] = -0.856555017562183;
+      w[93] = 0.028495796363599;
+      r[94] = -0.525935282564036;
+      s[94] = 0.319991164262401;
+      w[94] = 0.031988381018369;
+      r[95] = 0.319991164262401;
+      s[95] = -0.525935282564036;
+      w[95] = 0.031988381018369;
+      r[96] = -0.794055881698366;
+      s[96] = 0.319991164262401;
+      w[96] = 0.031988381018369;
+      r[97] = 0.319991164262401;
+      s[97] = -0.794055881698366;
+      w[97] = 0.031988381018369;
+      r[98] = -0.794055881698366;
+      s[98] = -0.525935282564036;
+      w[98] = 0.031988381018369;
+      r[99] = -0.525935282564036;
+      s[99] = -0.794055881698366;
+      w[99] = 0.031988381018369;
+      r[100] = -0.368673747852155;
+      s[100] = 0.056982821883363;
+      w[100] = 0.041389027831224;
+      r[101] = 0.056982821883363;
+      s[101] = -0.368673747852155;
+      w[101] = 0.041389027831224;
+      r[102] = -0.688309074031208;
+      s[102] = 0.056982821883363;
+      w[102] = 0.041389027831224;
+      r[103] = 0.056982821883363;
+      s[103] = -0.688309074031208;
+      w[103] = 0.041389027831224;
+      r[104] = -0.688309074031208;
+      s[104] = -0.368673747852155;
+      w[104] = 0.041389027831224;
+      r[105] = -0.368673747852155;
+      s[105] = -0.688309074031208;
+      w[105] = 0.041389027831224;
 
       break;
     }
     case 24: {
-      r[0]   = -0.333333333333333; s[0]   = -0.333333333333333; w[0]   = 0.031330242175782;
-      r[1]   = -0.031382760283421; s[1]   = -0.031382760283421; w[1]   = 0.014717653847587;
-      r[2]   = -0.937234479433159; s[2]   = -0.031382760283421; w[2]   = 0.014717653847587;
-      r[3]   = -0.031382760283421; s[3]   = -0.937234479433159; w[3]   = 0.014717653847587;
-      r[4]   = -0.120096233850662; s[4]   = -0.120096233850662; w[4]   = 0.030963348398970;
-      r[5]   = -0.759807532298676; s[5]   = -0.120096233850662; w[5]   = 0.030963348398970;
-      r[6]   = -0.120096233850662; s[6]   = -0.759807532298676; w[6]   = 0.030963348398970;
-      r[7]   = -0.217343938317536; s[7]   = -0.217343938317536; w[7]   = 0.037986940843648;
-      r[8]   = -0.565312123364928; s[8]   = -0.217343938317536; w[8]   = 0.037986940843648;
-      r[9]   = -0.217343938317536; s[9]   = -0.565312123364928; w[9]   = 0.037986940843648;
-      r[10]  = -0.429818284439074; s[10]  = -0.429818284439074; w[10]  = 0.033466254011049;
-      r[11]  = -0.140363431121852; s[11]  = -0.429818284439074; w[11]  = 0.033466254011049;
-      r[12]  = -0.429818284439074; s[12]  = -0.140363431121852; w[12]  = 0.033466254011049;
-      r[13]  = -0.522392801883300; s[13]  = -0.522392801883300; w[13]  = 0.029203686754054;
-      r[14]  =  0.044785603766601; s[14]  = -0.522392801883300; w[14]  = 0.029203686754054;
-      r[15]  = -0.522392801883300; s[15]  =  0.044785603766601; w[15]  = 0.029203686754054;
-      r[16]  = -0.704274510649686; s[16]  = -0.704274510649686; w[16]  = 0.022147482605586;
-      r[17]  =  0.408549021299373; s[17]  = -0.704274510649686; w[17]  = 0.022147482605586;
-      r[18]  = -0.704274510649686; s[18]  =  0.408549021299373; w[18]  = 0.022147482605586;
-      r[19]  = -0.843105586121546; s[19]  = -0.843105586121546; w[19]  = 0.015827753677335;
-      r[20]  =  0.686211172243092; s[20]  = -0.843105586121546; w[20]  = 0.015827753677335;
-      r[21]  = -0.843105586121546; s[21]  =  0.686211172243092; w[21]  = 0.015827753677335;
-      r[22]  = -0.936285318267427; s[22]  = -0.936285318267427; w[22]  = 0.005897827695084;
-      r[23]  =  0.872570636534854; s[23]  = -0.936285318267427; w[23]  = 0.005897827695084;
-      r[24]  = -0.936285318267427; s[24]  =  0.872570636534854; w[24]  = 0.005897827695084;
-      r[25]  = -0.983008712604130; s[25]  = -0.983008712604130; w[25]  = 0.001905131297570;
-      r[26]  =  0.966017425208259; s[26]  = -0.983008712604130; w[26]  = 0.001905131297570;
-      r[27]  = -0.983008712604130; s[27]  =  0.966017425208259; w[27]  = 0.001905131297570;
-      r[28]  = -0.133936561710478; s[28]  =  0.120327965916980; w[28]  = 0.008627443386199;
-      r[29]  =  0.120327965916980; s[29]  = -0.133936561710478; w[29]  = 0.008627443386199;
-      r[30]  = -0.986391404206501; s[30]  =  0.120327965916980; w[30]  = 0.008627443386199;
-      r[31]  =  0.120327965916980; s[31]  = -0.986391404206501; w[31]  = 0.008627443386199;
-      r[32]  = -0.986391404206501; s[32]  = -0.133936561710478; w[32]  = 0.008627443386199;
-      r[33]  = -0.133936561710478; s[33]  = -0.986391404206501; w[33]  = 0.008627443386199;
-      r[34]  = -0.589559941056661; s[34]  =  0.574991625876557; w[34]  = 0.007292016855628;
-      r[35]  =  0.574991625876557; s[35]  = -0.589559941056661; w[35]  = 0.007292016855628;
-      r[36]  = -0.985431684819897; s[36]  =  0.574991625876557; w[36]  = 0.007292016855628;
-      r[37]  =  0.574991625876557; s[37]  = -0.985431684819897; w[37]  = 0.007292016855628;
-      r[38]  = -0.985431684819897; s[38]  = -0.589559941056661; w[38]  = 0.007292016855628;
-      r[39]  = -0.589559941056661; s[39]  = -0.985431684819897; w[39]  = 0.007292016855628;
-      r[40]  = -0.375079684130172; s[40]  =  0.361371712031196; w[40]  = 0.008117703702749;
-      r[41]  =  0.361371712031196; s[41]  = -0.375079684130172; w[41]  = 0.008117703702749;
-      r[42]  = -0.986292027901024; s[42]  =  0.361371712031196; w[42]  = 0.008117703702749;
-      r[43]  =  0.361371712031196; s[43]  = -0.986292027901024; w[43]  = 0.008117703702749;
-      r[44]  = -0.986292027901024; s[44]  = -0.375079684130172; w[44]  = 0.008117703702749;
-      r[45]  = -0.375079684130172; s[45]  = -0.986292027901024; w[45]  = 0.008117703702749;
-      r[46]  = -0.906832105591067; s[46]  =  0.897244066241012; w[46]  = 0.002858359515171;
-      r[47]  =  0.897244066241012; s[47]  = -0.906832105591067; w[47]  = 0.002858359515171;
-      r[48]  = -0.990411960649945; s[48]  =  0.897244066241012; w[48]  = 0.002858359515171;
-      r[49]  =  0.897244066241012; s[49]  = -0.990411960649945; w[49]  = 0.002858359515171;
-      r[50]  = -0.990411960649945; s[50]  = -0.906832105591067; w[50]  = 0.002858359515171;
-      r[51]  = -0.906832105591067; s[51]  = -0.990411960649945; w[51]  = 0.002858359515171;
-      r[52]  = -0.768281564078976; s[52]  =  0.757477531703546; w[52]  = 0.004596788633153;
-      r[53]  =  0.757477531703546; s[53]  = -0.768281564078976; w[53]  = 0.004596788633153;
-      r[54]  = -0.989195967624570; s[54]  =  0.757477531703546; w[54]  = 0.004596788633153;
-      r[55]  =  0.757477531703546; s[55]  = -0.989195967624570; w[55]  = 0.004596788633153;
-      r[56]  = -0.989195967624570; s[56]  = -0.768281564078975; w[56]  = 0.004596788633153;
-      r[57]  = -0.768281564078975; s[57]  = -0.989195967624570; w[57]  = 0.004596788633153;
-      r[58]  = -0.498678726055310; s[58]  =  0.424585822926150; w[58]  = 0.017097477649229;
-      r[59]  =  0.424585822926150; s[59]  = -0.498678726055310; w[59]  = 0.017097477649229;
-      r[60]  = -0.925907096870839; s[60]  =  0.424585822926150; w[60]  = 0.017097477649229;
-      r[61]  =  0.424585822926150; s[61]  = -0.925907096870839; w[61]  = 0.017097477649229;
-      r[62]  = -0.925907096870839; s[62]  = -0.498678726055310; w[62]  = 0.017097477649229;
-      r[63]  = -0.498678726055310; s[63]  = -0.925907096870839; w[63]  = 0.017097477649229;
-      r[64]  = -0.279607664483490; s[64]  =  0.208396882316209; w[64]  = 0.018575372163249;
-      r[65]  =  0.208396882316209; s[65]  = -0.279607664483490; w[65]  = 0.018575372163249;
-      r[66]  = -0.928789217832719; s[66]  =  0.208396882316209; w[66]  = 0.018575372163249;
-      r[67]  =  0.208396882316209; s[67]  = -0.928789217832719; w[67]  = 0.018575372163249;
-      r[68]  = -0.928789217832719; s[68]  = -0.279607664483490; w[68]  = 0.018575372163249;
-      r[69]  = -0.279607664483490; s[69]  = -0.928789217832719; w[69]  = 0.018575372163249;
-      r[70]  = -0.837737372642508; s[70]  =  0.780926628976898; w[70]  = 0.008711688567270;
-      r[71]  =  0.780926628976898; s[71]  = -0.837737372642508; w[71]  = 0.008711688567270;
-      r[72]  = -0.943189256334389; s[72]  =  0.780926628976898; w[72]  = 0.008711688567270;
-      r[73]  =  0.780926628976898; s[73]  = -0.943189256334389; w[73]  = 0.008711688567270;
-      r[74]  = -0.943189256334389; s[74]  = -0.837737372642508; w[74]  = 0.008711688567270;
-      r[75]  = -0.837737372642508; s[75]  = -0.943189256334389; w[75]  = 0.008711688567270;
-      r[76]  = -0.693711793201882; s[76]  =  0.625024627714433; w[76]  = 0.013292883787775;
-      r[77]  =  0.625024627714433; s[77]  = -0.693711793201882; w[77]  = 0.013292883787775;
-      r[78]  = -0.931312834512551; s[78]  =  0.625024627714433; w[78]  = 0.013292883787775;
-      r[79]  =  0.625024627714433; s[79]  = -0.931312834512551; w[79]  = 0.013292883787775;
-      r[80]  = -0.931312834512551; s[80]  = -0.693711793201882; w[80]  = 0.013292883787775;
-      r[81]  = -0.693711793201882; s[81]  = -0.931312834512551; w[81]  = 0.013292883787775;
-      r[82]  =  0.004700993829951; s[82]  = -0.135567929734853; w[82]  = 0.012281001510740;
-      r[83]  = -0.135567929734853; s[83]  =  0.004700993829951; w[83]  = 0.012281001510740;
-      r[84]  = -0.869133064095098; s[84]  = -0.135567929734853; w[84]  = 0.012281001510740;
-      r[85]  = -0.135567929734853; s[85]  = -0.869133064095098; w[85]  = 0.012281001510740;
-      r[86]  = -0.869133064095098; s[86]  =  0.004700993829951; w[86]  = 0.012281001510740;
-      r[87]  =  0.004700993829951; s[87]  = -0.869133064095098; w[87]  = 0.012281001510740;
-      r[88]  = -0.521976982650353; s[88]  =  0.349105045944945; w[88]  = 0.021820885555420;
-      r[89]  =  0.349105045944945; s[89]  = -0.521976982650353; w[89]  = 0.021820885555420;
-      r[90]  = -0.827128063294591; s[90]  =  0.349105045944945; w[90]  = 0.021820885555420;
-      r[91]  =  0.349105045944945; s[91]  = -0.827128063294591; w[91]  = 0.021820885555420;
-      r[92]  = -0.827128063294591; s[92]  = -0.521976982650353; w[92]  = 0.021820885555420;
-      r[93]  = -0.521976982650353; s[93]  = -0.827128063294591; w[93]  = 0.021820885555420;
-      r[94]  = -0.326968721136217; s[94]  =  0.144732602043697; w[94]  = 0.027371090249668;
-      r[95]  =  0.144732602043697; s[95]  = -0.326968721136217; w[95]  = 0.027371090249668;
-      r[96]  = -0.817763880907480; s[96]  =  0.144732602043697; w[96]  = 0.027371090249668;
-      r[97]  =  0.144732602043697; s[97]  = -0.817763880907480; w[97]  = 0.027371090249668;
-      r[98]  = -0.817763880907480; s[98]  = -0.326968721136217; w[98]  = 0.027371090249668;
-      r[99]  = -0.326968721136217; s[99]  = -0.817763880907480; w[99]  = 0.027371090249668;
-      r[100] = -0.696116803866709; s[100] =  0.531011336134871; w[100] = 0.018737543889147;
-      r[101] =  0.531011336134871; s[101] = -0.696116803866709; w[101] = 0.018737543889147;
-      r[102] = -0.834894532268162; s[102] =  0.531011336134871; w[102] = 0.018737543889147;
-      r[103] =  0.531011336134871; s[103] = -0.834894532268162; w[103] = 0.018737543889147;
-      r[104] = -0.834894532268162; s[104] = -0.696116803866709; w[104] = 0.018737543889147;
-      r[105] = -0.696116803866709; s[105] = -0.834894532268162; w[105] = 0.018737543889147;
-      r[106] = -0.536404917748559; s[106] =  0.226734558438523; w[106] = 0.028700757241388;
-      r[107] =  0.226734558438523; s[107] = -0.536404917748559; w[107] = 0.028700757241388;
-      r[108] = -0.690329640689964; s[108] =  0.226734558438523; w[108] = 0.028700757241388;
-      r[109] =  0.226734558438523; s[109] = -0.690329640689964; w[109] = 0.028700757241388;
-      r[110] = -0.690329640689964; s[110] = -0.536404917748559; w[110] = 0.028700757241388;
-      r[111] = -0.536404917748559; s[111] = -0.690329640689964; w[111] = 0.028700757241388;
-      r[112] = -0.344489563789357; s[112] =  0.009282127094255; w[112] = 0.033972574031807;
-      r[113] =  0.009282127094255; s[113] = -0.344489563789357; w[113] = 0.033972574031807;
-      r[114] = -0.664792563304898; s[114] =  0.009282127094255; w[114] = 0.033972574031807;
-      r[115] =  0.009282127094255; s[115] = -0.664792563304898; w[115] = 0.033972574031807;
-      r[116] = -0.664792563304898; s[116] = -0.344489563789357; w[116] = 0.033972574031807;
-      r[117] = -0.344489563789357; s[117] = -0.664792563304898; w[117] = 0.033972574031807;
+      r[0] = -0.333333333333333;
+      s[0] = -0.333333333333333;
+      w[0] = 0.031330242175782;
+      r[1] = -0.031382760283421;
+      s[1] = -0.031382760283421;
+      w[1] = 0.014717653847587;
+      r[2] = -0.937234479433159;
+      s[2] = -0.031382760283421;
+      w[2] = 0.014717653847587;
+      r[3] = -0.031382760283421;
+      s[3] = -0.937234479433159;
+      w[3] = 0.014717653847587;
+      r[4] = -0.120096233850662;
+      s[4] = -0.120096233850662;
+      w[4] = 0.030963348398970;
+      r[5] = -0.759807532298676;
+      s[5] = -0.120096233850662;
+      w[5] = 0.030963348398970;
+      r[6] = -0.120096233850662;
+      s[6] = -0.759807532298676;
+      w[6] = 0.030963348398970;
+      r[7] = -0.217343938317536;
+      s[7] = -0.217343938317536;
+      w[7] = 0.037986940843648;
+      r[8] = -0.565312123364928;
+      s[8] = -0.217343938317536;
+      w[8] = 0.037986940843648;
+      r[9] = -0.217343938317536;
+      s[9] = -0.565312123364928;
+      w[9] = 0.037986940843648;
+      r[10] = -0.429818284439074;
+      s[10] = -0.429818284439074;
+      w[10] = 0.033466254011049;
+      r[11] = -0.140363431121852;
+      s[11] = -0.429818284439074;
+      w[11] = 0.033466254011049;
+      r[12] = -0.429818284439074;
+      s[12] = -0.140363431121852;
+      w[12] = 0.033466254011049;
+      r[13] = -0.522392801883300;
+      s[13] = -0.522392801883300;
+      w[13] = 0.029203686754054;
+      r[14] = 0.044785603766601;
+      s[14] = -0.522392801883300;
+      w[14] = 0.029203686754054;
+      r[15] = -0.522392801883300;
+      s[15] = 0.044785603766601;
+      w[15] = 0.029203686754054;
+      r[16] = -0.704274510649686;
+      s[16] = -0.704274510649686;
+      w[16] = 0.022147482605586;
+      r[17] = 0.408549021299373;
+      s[17] = -0.704274510649686;
+      w[17] = 0.022147482605586;
+      r[18] = -0.704274510649686;
+      s[18] = 0.408549021299373;
+      w[18] = 0.022147482605586;
+      r[19] = -0.843105586121546;
+      s[19] = -0.843105586121546;
+      w[19] = 0.015827753677335;
+      r[20] = 0.686211172243092;
+      s[20] = -0.843105586121546;
+      w[20] = 0.015827753677335;
+      r[21] = -0.843105586121546;
+      s[21] = 0.686211172243092;
+      w[21] = 0.015827753677335;
+      r[22] = -0.936285318267427;
+      s[22] = -0.936285318267427;
+      w[22] = 0.005897827695084;
+      r[23] = 0.872570636534854;
+      s[23] = -0.936285318267427;
+      w[23] = 0.005897827695084;
+      r[24] = -0.936285318267427;
+      s[24] = 0.872570636534854;
+      w[24] = 0.005897827695084;
+      r[25] = -0.983008712604130;
+      s[25] = -0.983008712604130;
+      w[25] = 0.001905131297570;
+      r[26] = 0.966017425208259;
+      s[26] = -0.983008712604130;
+      w[26] = 0.001905131297570;
+      r[27] = -0.983008712604130;
+      s[27] = 0.966017425208259;
+      w[27] = 0.001905131297570;
+      r[28] = -0.133936561710478;
+      s[28] = 0.120327965916980;
+      w[28] = 0.008627443386199;
+      r[29] = 0.120327965916980;
+      s[29] = -0.133936561710478;
+      w[29] = 0.008627443386199;
+      r[30] = -0.986391404206501;
+      s[30] = 0.120327965916980;
+      w[30] = 0.008627443386199;
+      r[31] = 0.120327965916980;
+      s[31] = -0.986391404206501;
+      w[31] = 0.008627443386199;
+      r[32] = -0.986391404206501;
+      s[32] = -0.133936561710478;
+      w[32] = 0.008627443386199;
+      r[33] = -0.133936561710478;
+      s[33] = -0.986391404206501;
+      w[33] = 0.008627443386199;
+      r[34] = -0.589559941056661;
+      s[34] = 0.574991625876557;
+      w[34] = 0.007292016855628;
+      r[35] = 0.574991625876557;
+      s[35] = -0.589559941056661;
+      w[35] = 0.007292016855628;
+      r[36] = -0.985431684819897;
+      s[36] = 0.574991625876557;
+      w[36] = 0.007292016855628;
+      r[37] = 0.574991625876557;
+      s[37] = -0.985431684819897;
+      w[37] = 0.007292016855628;
+      r[38] = -0.985431684819897;
+      s[38] = -0.589559941056661;
+      w[38] = 0.007292016855628;
+      r[39] = -0.589559941056661;
+      s[39] = -0.985431684819897;
+      w[39] = 0.007292016855628;
+      r[40] = -0.375079684130172;
+      s[40] = 0.361371712031196;
+      w[40] = 0.008117703702749;
+      r[41] = 0.361371712031196;
+      s[41] = -0.375079684130172;
+      w[41] = 0.008117703702749;
+      r[42] = -0.986292027901024;
+      s[42] = 0.361371712031196;
+      w[42] = 0.008117703702749;
+      r[43] = 0.361371712031196;
+      s[43] = -0.986292027901024;
+      w[43] = 0.008117703702749;
+      r[44] = -0.986292027901024;
+      s[44] = -0.375079684130172;
+      w[44] = 0.008117703702749;
+      r[45] = -0.375079684130172;
+      s[45] = -0.986292027901024;
+      w[45] = 0.008117703702749;
+      r[46] = -0.906832105591067;
+      s[46] = 0.897244066241012;
+      w[46] = 0.002858359515171;
+      r[47] = 0.897244066241012;
+      s[47] = -0.906832105591067;
+      w[47] = 0.002858359515171;
+      r[48] = -0.990411960649945;
+      s[48] = 0.897244066241012;
+      w[48] = 0.002858359515171;
+      r[49] = 0.897244066241012;
+      s[49] = -0.990411960649945;
+      w[49] = 0.002858359515171;
+      r[50] = -0.990411960649945;
+      s[50] = -0.906832105591067;
+      w[50] = 0.002858359515171;
+      r[51] = -0.906832105591067;
+      s[51] = -0.990411960649945;
+      w[51] = 0.002858359515171;
+      r[52] = -0.768281564078976;
+      s[52] = 0.757477531703546;
+      w[52] = 0.004596788633153;
+      r[53] = 0.757477531703546;
+      s[53] = -0.768281564078976;
+      w[53] = 0.004596788633153;
+      r[54] = -0.989195967624570;
+      s[54] = 0.757477531703546;
+      w[54] = 0.004596788633153;
+      r[55] = 0.757477531703546;
+      s[55] = -0.989195967624570;
+      w[55] = 0.004596788633153;
+      r[56] = -0.989195967624570;
+      s[56] = -0.768281564078975;
+      w[56] = 0.004596788633153;
+      r[57] = -0.768281564078975;
+      s[57] = -0.989195967624570;
+      w[57] = 0.004596788633153;
+      r[58] = -0.498678726055310;
+      s[58] = 0.424585822926150;
+      w[58] = 0.017097477649229;
+      r[59] = 0.424585822926150;
+      s[59] = -0.498678726055310;
+      w[59] = 0.017097477649229;
+      r[60] = -0.925907096870839;
+      s[60] = 0.424585822926150;
+      w[60] = 0.017097477649229;
+      r[61] = 0.424585822926150;
+      s[61] = -0.925907096870839;
+      w[61] = 0.017097477649229;
+      r[62] = -0.925907096870839;
+      s[62] = -0.498678726055310;
+      w[62] = 0.017097477649229;
+      r[63] = -0.498678726055310;
+      s[63] = -0.925907096870839;
+      w[63] = 0.017097477649229;
+      r[64] = -0.279607664483490;
+      s[64] = 0.208396882316209;
+      w[64] = 0.018575372163249;
+      r[65] = 0.208396882316209;
+      s[65] = -0.279607664483490;
+      w[65] = 0.018575372163249;
+      r[66] = -0.928789217832719;
+      s[66] = 0.208396882316209;
+      w[66] = 0.018575372163249;
+      r[67] = 0.208396882316209;
+      s[67] = -0.928789217832719;
+      w[67] = 0.018575372163249;
+      r[68] = -0.928789217832719;
+      s[68] = -0.279607664483490;
+      w[68] = 0.018575372163249;
+      r[69] = -0.279607664483490;
+      s[69] = -0.928789217832719;
+      w[69] = 0.018575372163249;
+      r[70] = -0.837737372642508;
+      s[70] = 0.780926628976898;
+      w[70] = 0.008711688567270;
+      r[71] = 0.780926628976898;
+      s[71] = -0.837737372642508;
+      w[71] = 0.008711688567270;
+      r[72] = -0.943189256334389;
+      s[72] = 0.780926628976898;
+      w[72] = 0.008711688567270;
+      r[73] = 0.780926628976898;
+      s[73] = -0.943189256334389;
+      w[73] = 0.008711688567270;
+      r[74] = -0.943189256334389;
+      s[74] = -0.837737372642508;
+      w[74] = 0.008711688567270;
+      r[75] = -0.837737372642508;
+      s[75] = -0.943189256334389;
+      w[75] = 0.008711688567270;
+      r[76] = -0.693711793201882;
+      s[76] = 0.625024627714433;
+      w[76] = 0.013292883787775;
+      r[77] = 0.625024627714433;
+      s[77] = -0.693711793201882;
+      w[77] = 0.013292883787775;
+      r[78] = -0.931312834512551;
+      s[78] = 0.625024627714433;
+      w[78] = 0.013292883787775;
+      r[79] = 0.625024627714433;
+      s[79] = -0.931312834512551;
+      w[79] = 0.013292883787775;
+      r[80] = -0.931312834512551;
+      s[80] = -0.693711793201882;
+      w[80] = 0.013292883787775;
+      r[81] = -0.693711793201882;
+      s[81] = -0.931312834512551;
+      w[81] = 0.013292883787775;
+      r[82] = 0.004700993829951;
+      s[82] = -0.135567929734853;
+      w[82] = 0.012281001510740;
+      r[83] = -0.135567929734853;
+      s[83] = 0.004700993829951;
+      w[83] = 0.012281001510740;
+      r[84] = -0.869133064095098;
+      s[84] = -0.135567929734853;
+      w[84] = 0.012281001510740;
+      r[85] = -0.135567929734853;
+      s[85] = -0.869133064095098;
+      w[85] = 0.012281001510740;
+      r[86] = -0.869133064095098;
+      s[86] = 0.004700993829951;
+      w[86] = 0.012281001510740;
+      r[87] = 0.004700993829951;
+      s[87] = -0.869133064095098;
+      w[87] = 0.012281001510740;
+      r[88] = -0.521976982650353;
+      s[88] = 0.349105045944945;
+      w[88] = 0.021820885555420;
+      r[89] = 0.349105045944945;
+      s[89] = -0.521976982650353;
+      w[89] = 0.021820885555420;
+      r[90] = -0.827128063294591;
+      s[90] = 0.349105045944945;
+      w[90] = 0.021820885555420;
+      r[91] = 0.349105045944945;
+      s[91] = -0.827128063294591;
+      w[91] = 0.021820885555420;
+      r[92] = -0.827128063294591;
+      s[92] = -0.521976982650353;
+      w[92] = 0.021820885555420;
+      r[93] = -0.521976982650353;
+      s[93] = -0.827128063294591;
+      w[93] = 0.021820885555420;
+      r[94] = -0.326968721136217;
+      s[94] = 0.144732602043697;
+      w[94] = 0.027371090249668;
+      r[95] = 0.144732602043697;
+      s[95] = -0.326968721136217;
+      w[95] = 0.027371090249668;
+      r[96] = -0.817763880907480;
+      s[96] = 0.144732602043697;
+      w[96] = 0.027371090249668;
+      r[97] = 0.144732602043697;
+      s[97] = -0.817763880907480;
+      w[97] = 0.027371090249668;
+      r[98] = -0.817763880907480;
+      s[98] = -0.326968721136217;
+      w[98] = 0.027371090249668;
+      r[99] = -0.326968721136217;
+      s[99] = -0.817763880907480;
+      w[99] = 0.027371090249668;
+      r[100] = -0.696116803866709;
+      s[100] = 0.531011336134871;
+      w[100] = 0.018737543889147;
+      r[101] = 0.531011336134871;
+      s[101] = -0.696116803866709;
+      w[101] = 0.018737543889147;
+      r[102] = -0.834894532268162;
+      s[102] = 0.531011336134871;
+      w[102] = 0.018737543889147;
+      r[103] = 0.531011336134871;
+      s[103] = -0.834894532268162;
+      w[103] = 0.018737543889147;
+      r[104] = -0.834894532268162;
+      s[104] = -0.696116803866709;
+      w[104] = 0.018737543889147;
+      r[105] = -0.696116803866709;
+      s[105] = -0.834894532268162;
+      w[105] = 0.018737543889147;
+      r[106] = -0.536404917748559;
+      s[106] = 0.226734558438523;
+      w[106] = 0.028700757241388;
+      r[107] = 0.226734558438523;
+      s[107] = -0.536404917748559;
+      w[107] = 0.028700757241388;
+      r[108] = -0.690329640689964;
+      s[108] = 0.226734558438523;
+      w[108] = 0.028700757241388;
+      r[109] = 0.226734558438523;
+      s[109] = -0.690329640689964;
+      w[109] = 0.028700757241388;
+      r[110] = -0.690329640689964;
+      s[110] = -0.536404917748559;
+      w[110] = 0.028700757241388;
+      r[111] = -0.536404917748559;
+      s[111] = -0.690329640689964;
+      w[111] = 0.028700757241388;
+      r[112] = -0.344489563789357;
+      s[112] = 0.009282127094255;
+      w[112] = 0.033972574031807;
+      r[113] = 0.009282127094255;
+      s[113] = -0.344489563789357;
+      w[113] = 0.033972574031807;
+      r[114] = -0.664792563304898;
+      s[114] = 0.009282127094255;
+      w[114] = 0.033972574031807;
+      r[115] = 0.009282127094255;
+      s[115] = -0.664792563304898;
+      w[115] = 0.033972574031807;
+      r[116] = -0.664792563304898;
+      s[116] = -0.344489563789357;
+      w[116] = 0.033972574031807;
+      r[117] = -0.344489563789357;
+      s[117] = -0.664792563304898;
+      w[117] = 0.033972574031807;
 
       break;
     }
     case 25: {
-      r[0]   = -0.027946483073174; s[0]   = -0.027946483073174; w[0]   = 0.016011163760041;
-      r[1]   = -0.944107033853652; s[1]   = -0.027946483073174; w[1]   = 0.016011163760041;
-      r[2]   = -0.027946483073174; s[2]   = -0.944107033853652; w[2]   = 0.016011163760041;
-      r[3]   = -0.131178601327651; s[3]   = -0.131178601327651; w[3]   = 0.031894153664781;
-      r[4]   = -0.737642797344697; s[4]   = -0.131178601327651; w[4]   = 0.031894153664781;
-      r[5]   = -0.131178601327651; s[5]   = -0.737642797344697; w[5]   = 0.031894153664781;
-      r[6]   = -0.220221729512072; s[6]   = -0.220221729512072; w[6]   = 0.026218282461591;
-      r[7]   = -0.559556540975855; s[7]   = -0.220221729512072; w[7]   = 0.026218282461591;
-      r[8]   = -0.220221729512072; s[8]   = -0.559556540975855; w[8]   = 0.026218282461591;
-      r[9]   = -0.403113531960391; s[9]   = -0.403113531960391; w[9]   = 0.039166001931271;
-      r[10]  = -0.193772936079218; s[10]  = -0.403113531960391; w[10]  = 0.039166001931271;
-      r[11]  = -0.403113531960391; s[11]  = -0.193772936079218; w[11]  = 0.039166001931271;
-      r[12]  = -0.531911655325256; s[12]  = -0.531911655325256; w[12]  = 0.032941770883075;
-      r[13]  =  0.063823310650513; s[13]  = -0.531911655325256; w[13]  = 0.032941770883075;
-      r[14]  = -0.531911655325256; s[14]  =  0.063823310650513; w[14]  = 0.032941770883075;
-      r[15]  = -0.697063330781965; s[15]  = -0.697063330781965; w[15]  = 0.017094558148184;
-      r[16]  =  0.394126661563930; s[16]  = -0.697063330781965; w[16]  = 0.017094558148184;
-      r[17]  = -0.697063330781965; s[17]  =  0.394126661563930; w[17]  = 0.017094558148184;
-      r[18]  = -0.774532212908013; s[18]  = -0.774532212908013; w[18]  = 0.016323771714453;
-      r[19]  =  0.549064425816026; s[19]  = -0.774532212908013; w[19]  = 0.016323771714453;
-      r[20]  = -0.774532212908013; s[20]  =  0.549064425816026; w[20]  = 0.016323771714453;
-      r[21]  = -0.844568615816947; s[21]  = -0.844568615816947; w[21]  = 0.012242293079968;
-      r[22]  =  0.689137231633895; s[22]  = -0.844568615816948; w[22]  = 0.012242293079968;
-      r[23]  = -0.844568615816948; s[23]  =  0.689137231633895; w[23]  = 0.012242293079968;
-      r[24]  = -0.930213812771406; s[24]  = -0.930213812771406; w[24]  = 0.005816996529873;
-      r[25]  =  0.860427625542812; s[25]  = -0.930213812771406; w[25]  = 0.005816996529873;
-      r[26]  = -0.930213812771406; s[26]  =  0.860427625542812; w[26]  = 0.005816996529873;
-      r[27]  = -0.985483630758135; s[27]  = -0.985483630758135; w[27]  = 0.001384550491324;
-      r[28]  =  0.970967261516271; s[28]  = -0.985483630758135; w[28]  = 0.001384550491324;
-      r[29]  = -0.985483630758135; s[29]  =  0.970967261516271; w[29]  = 0.001384550491324;
-      r[30]  = -0.545571095693272; s[30]  =  0.542986390284387; w[30]  = 0.002496578398555;
-      r[31]  =  0.542986390284387; s[31]  = -0.545571095693272; w[31]  = 0.002496578398555;
-      r[32]  = -0.997415294591116; s[32]  =  0.542986390284387; w[32]  = 0.002496578398555;
-      r[33]  =  0.542986390284387; s[33]  = -0.997415294591116; w[33]  = 0.002496578398555;
-      r[34]  = -0.997415294591116; s[34]  = -0.545571095693272; w[34]  = 0.002496578398555;
-      r[35]  = -0.545571095693272; s[35]  = -0.997415294591116; w[35]  = 0.002496578398555;
-      r[36]  = -0.129978890292857; s[36]  =  0.119179487748624; w[36]  = 0.006809505817606;
-      r[37]  =  0.119179487748624; s[37]  = -0.129978890292857; w[37]  = 0.006809505817606;
-      r[38]  = -0.989200597455768; s[38]  =  0.119179487748624; w[38]  = 0.006809505817606;
-      r[39]  =  0.119179487748624; s[39]  = -0.989200597455768; w[39]  = 0.006809505817606;
-      r[40]  = -0.989200597455768; s[40]  = -0.129978890292857; w[40]  = 0.006809505817606;
-      r[41]  = -0.129978890292857; s[41]  = -0.989200597455768; w[41]  = 0.006809505817606;
-      r[42]  = -0.359380801455591; s[42]  =  0.346612795387641; w[42]  = 0.006719308652128;
-      r[43]  =  0.346612795387641; s[43]  = -0.359380801455591; w[43]  = 0.006719308652128;
-      r[44]  = -0.987231993932050; s[44]  =  0.346612795387641; w[44]  = 0.006719308652128;
-      r[45]  =  0.346612795387641; s[45]  = -0.987231993932050; w[45]  = 0.006719308652128;
-      r[46]  = -0.987231993932050; s[46]  = -0.359380801455591; w[46]  = 0.006719308652128;
-      r[47]  = -0.359380801455591; s[47]  = -0.987231993932050; w[47]  = 0.006719308652128;
-      r[48]  = -0.816499355439990; s[48]  =  0.806442932436004; w[48]  = 0.003432313078994;
-      r[49]  =  0.806442932436004; s[49]  = -0.816499355439990; w[49]  = 0.003432313078994;
-      r[50]  = -0.989943576996014; s[50]  =  0.806442932436004; w[50]  = 0.003432313078994;
-      r[51]  =  0.806442932436004; s[51]  = -0.989943576996014; w[51]  = 0.003432313078994;
-      r[52]  = -0.989943576996014; s[52]  = -0.816499355439990; w[52]  = 0.003432313078994;
-      r[53]  = -0.816499355439990; s[53]  = -0.989943576996014; w[53]  = 0.003432313078994;
-      r[54]  = -0.923978328282551; s[54]  =  0.910324811038988; w[54]  = 0.002961712633431;
-      r[55]  =  0.910324811038988; s[55]  = -0.923978328282551; w[55]  = 0.002961712633431;
-      r[56]  = -0.986346482756436; s[56]  =  0.910324811038988; w[56]  = 0.002961712633431;
-      r[57]  =  0.910324811038988; s[57]  = -0.986346482756436; w[57]  = 0.002961712633431;
-      r[58]  = -0.986346482756436; s[58]  = -0.923978328282551; w[58]  = 0.002961712633431;
-      r[59]  = -0.923978328282551; s[59]  = -0.986346482756436; w[59]  = 0.002961712633431;
-      r[60]  = -0.685149563029377; s[60]  =  0.665117163749518; w[60]  = 0.007022625221457;
-      r[61]  =  0.665117163749518; s[61]  = -0.685149563029377; w[61]  = 0.007022625221457;
-      r[62]  = -0.979967600720141; s[62]  =  0.665117163749517; w[62]  = 0.007022625221457;
-      r[63]  =  0.665117163749517; s[63]  = -0.979967600720141; w[63]  = 0.007022625221457;
-      r[64]  = -0.979967600720141; s[64]  = -0.685149563029376; w[64]  = 0.007022625221457;
-      r[65]  = -0.685149563029376; s[65]  = -0.979967600720141; w[65]  = 0.007022625221457;
-      r[66]  = -0.520220680442934; s[66]  =  0.468705054096154; w[66]  = 0.014787100299413;
-      r[67]  =  0.468705054096154; s[67]  = -0.520220680442934; w[67]  = 0.014787100299413;
-      r[68]  = -0.948484373653220; s[68]  =  0.468705054096154; w[68]  = 0.014787100299413;
-      r[69]  =  0.468705054096154; s[69]  = -0.948484373653220; w[69]  = 0.014787100299413;
-      r[70]  = -0.948484373653220; s[70]  = -0.520220680442934; w[70]  = 0.014787100299413;
-      r[71]  = -0.520220680442934; s[71]  = -0.948484373653220; w[71]  = 0.014787100299413;
-      r[72]  = -0.276113763747879; s[72]  =  0.215657967508047; w[72]  = 0.015966174954753;
-      r[73]  =  0.215657967508047; s[73]  = -0.276113763747879; w[73]  = 0.015966174954753;
-      r[74]  = -0.939544203760168; s[74]  =  0.215657967508047; w[74]  = 0.015966174954753;
-      r[75]  =  0.215657967508047; s[75]  = -0.939544203760168; w[75]  = 0.015966174954753;
-      r[76]  = -0.939544203760168; s[76]  = -0.276113763747879; w[76]  = 0.015966174954753;
-      r[77]  = -0.276113763747879; s[77]  = -0.939544203760168; w[77]  = 0.015966174954753;
-      r[78]  = -0.832896078090343; s[78]  =  0.771886097876019; w[78]  = 0.008711925226316;
-      r[79]  =  0.771886097876019; s[79]  = -0.832896078090343; w[79]  = 0.008711925226316;
-      r[80]  = -0.938990019785676; s[80]  =  0.771886097876019; w[80]  = 0.008711925226316;
-      r[81]  =  0.771886097876019; s[81]  = -0.938990019785676; w[81]  = 0.008711925226316;
-      r[82]  = -0.938990019785676; s[82]  = -0.832896078090343; w[82]  = 0.008711925226316;
-      r[83]  = -0.832896078090343; s[83]  = -0.938990019785676; w[83]  = 0.008711925226316;
-      r[84]  = -0.703113558535164; s[84]  =  0.611200463810025; w[84]  = 0.014730113402836;
-      r[85]  =  0.611200463810025; s[85]  = -0.703113558535164; w[85]  = 0.014730113402836;
-      r[86]  = -0.908086905274861; s[86]  =  0.611200463810025; w[86]  = 0.014730113402836;
-      r[87]  =  0.611200463810025; s[87]  = -0.908086905274861; w[87]  = 0.014730113402836;
-      r[88]  = -0.908086905274861; s[88]  = -0.703113558535164; w[88]  = 0.014730113402836;
-      r[89]  = -0.703113558535164; s[89]  = -0.908086905274861; w[89]  = 0.014730113402836;
-      r[90]  = -0.432520582544930; s[90]  =  0.297634981464375; w[90]  = 0.021927145692839;
-      r[91]  =  0.297634981464375; s[91]  = -0.432520582544930; w[91]  = 0.021927145692839;
-      r[92]  = -0.865114398919445; s[92]  =  0.297634981464375; w[92]  = 0.021927145692839;
-      r[93]  =  0.297634981464375; s[93]  = -0.865114398919445; w[93]  = 0.021927145692839;
-      r[94]  = -0.865114398919445; s[94]  = -0.432520582544930; w[94]  = 0.021927145692839;
-      r[95]  = -0.432520582544930; s[95]  = -0.865114398919445; w[95]  = 0.021927145692839;
-      r[96]  = -0.186201249762425; s[96]  =  0.046111066930604; w[96]  = 0.023499923487082;
-      r[97]  =  0.046111066930604; s[97]  = -0.186201249762425; w[97]  = 0.023499923487082;
-      r[98]  = -0.859909817168179; s[98]  =  0.046111066930604; w[98]  = 0.023499923487082;
-      r[99]  =  0.046111066930604; s[99]  = -0.859909817168179; w[99]  = 0.023499923487082;
-      r[100] = -0.859909817168179; s[100] = -0.186201249762425; w[100] = 0.023499923487082;
-      r[101] = -0.186201249762425; s[101] = -0.859909817168179; w[101] = 0.023499923487082;
-      r[102] = -0.611772025950215; s[102] =  0.443948976669982; w[102] = 0.020031201427597;
-      r[103] =  0.443948976669982; s[103] = -0.611772025950215; w[103] = 0.020031201427597;
-      r[104] = -0.832176950719767; s[104] =  0.443948976669982; w[104] = 0.020031201427597;
-      r[105] =  0.443948976669982; s[105] = -0.832176950719767; w[105] = 0.020031201427597;
-      r[106] = -0.832176950719767; s[106] = -0.611772025950215; w[106] = 0.020031201427597;
-      r[107] = -0.611772025950215; s[107] = -0.832176950719767; w[107] = 0.020031201427597;
-      r[108] = -0.351731305998594; s[108] =  0.110980234644288; w[108] = 0.026619281575257;
-      r[109] =  0.110980234644288; s[109] = -0.351731305998594; w[109] = 0.026619281575257;
-      r[110] = -0.759248928645695; s[110] =  0.110980234644288; w[110] = 0.026619281575257;
-      r[111] =  0.110980234644288; s[111] = -0.759248928645695; w[111] = 0.026619281575257;
-      r[112] = -0.759248928645695; s[112] = -0.351731305998594; w[112] = 0.026619281575257;
-      r[113] = -0.351731305998594; s[113] = -0.759248928645695; w[113] = 0.026619281575257;
-      r[114] = -0.541445032888038; s[114] =  0.245311234573305; w[114] = 0.028308893010452;
-      r[115] =  0.245311234573305; s[115] = -0.541445032888038; w[115] = 0.028308893010452;
-      r[116] = -0.703866201685267; s[116] =  0.245311234573305; w[116] = 0.028308893010452;
-      r[117] =  0.245311234573305; s[117] = -0.703866201685267; w[117] = 0.028308893010452;
-      r[118] = -0.703866201685267; s[118] = -0.541445032888038; w[118] = 0.028308893010452;
-      r[119] = -0.541445032888038; s[119] = -0.703866201685267; w[119] = 0.028308893010452;
-      r[120] = -0.348763754808032; s[120] = -0.034779976926618; w[120] = 0.029762759122336;
-      r[121] = -0.034779976926618; s[121] = -0.348763754808032; w[121] = 0.029762759122336;
-      r[122] = -0.616456268265350; s[122] = -0.034779976926618; w[122] = 0.029762759122336;
-      r[123] = -0.034779976926618; s[123] = -0.616456268265350; w[123] = 0.029762759122336;
-      r[124] = -0.616456268265350; s[124] = -0.348763754808032; w[124] = 0.029762759122336;
-      r[125] = -0.348763754808032; s[125] = -0.616456268265350; w[125] = 0.029762759122336;
+      r[0] = -0.027946483073174;
+      s[0] = -0.027946483073174;
+      w[0] = 0.016011163760041;
+      r[1] = -0.944107033853652;
+      s[1] = -0.027946483073174;
+      w[1] = 0.016011163760041;
+      r[2] = -0.027946483073174;
+      s[2] = -0.944107033853652;
+      w[2] = 0.016011163760041;
+      r[3] = -0.131178601327651;
+      s[3] = -0.131178601327651;
+      w[3] = 0.031894153664781;
+      r[4] = -0.737642797344697;
+      s[4] = -0.131178601327651;
+      w[4] = 0.031894153664781;
+      r[5] = -0.131178601327651;
+      s[5] = -0.737642797344697;
+      w[5] = 0.031894153664781;
+      r[6] = -0.220221729512072;
+      s[6] = -0.220221729512072;
+      w[6] = 0.026218282461591;
+      r[7] = -0.559556540975855;
+      s[7] = -0.220221729512072;
+      w[7] = 0.026218282461591;
+      r[8] = -0.220221729512072;
+      s[8] = -0.559556540975855;
+      w[8] = 0.026218282461591;
+      r[9] = -0.403113531960391;
+      s[9] = -0.403113531960391;
+      w[9] = 0.039166001931271;
+      r[10] = -0.193772936079218;
+      s[10] = -0.403113531960391;
+      w[10] = 0.039166001931271;
+      r[11] = -0.403113531960391;
+      s[11] = -0.193772936079218;
+      w[11] = 0.039166001931271;
+      r[12] = -0.531911655325256;
+      s[12] = -0.531911655325256;
+      w[12] = 0.032941770883075;
+      r[13] = 0.063823310650513;
+      s[13] = -0.531911655325256;
+      w[13] = 0.032941770883075;
+      r[14] = -0.531911655325256;
+      s[14] = 0.063823310650513;
+      w[14] = 0.032941770883075;
+      r[15] = -0.697063330781965;
+      s[15] = -0.697063330781965;
+      w[15] = 0.017094558148184;
+      r[16] = 0.394126661563930;
+      s[16] = -0.697063330781965;
+      w[16] = 0.017094558148184;
+      r[17] = -0.697063330781965;
+      s[17] = 0.394126661563930;
+      w[17] = 0.017094558148184;
+      r[18] = -0.774532212908013;
+      s[18] = -0.774532212908013;
+      w[18] = 0.016323771714453;
+      r[19] = 0.549064425816026;
+      s[19] = -0.774532212908013;
+      w[19] = 0.016323771714453;
+      r[20] = -0.774532212908013;
+      s[20] = 0.549064425816026;
+      w[20] = 0.016323771714453;
+      r[21] = -0.844568615816947;
+      s[21] = -0.844568615816947;
+      w[21] = 0.012242293079968;
+      r[22] = 0.689137231633895;
+      s[22] = -0.844568615816948;
+      w[22] = 0.012242293079968;
+      r[23] = -0.844568615816948;
+      s[23] = 0.689137231633895;
+      w[23] = 0.012242293079968;
+      r[24] = -0.930213812771406;
+      s[24] = -0.930213812771406;
+      w[24] = 0.005816996529873;
+      r[25] = 0.860427625542812;
+      s[25] = -0.930213812771406;
+      w[25] = 0.005816996529873;
+      r[26] = -0.930213812771406;
+      s[26] = 0.860427625542812;
+      w[26] = 0.005816996529873;
+      r[27] = -0.985483630758135;
+      s[27] = -0.985483630758135;
+      w[27] = 0.001384550491324;
+      r[28] = 0.970967261516271;
+      s[28] = -0.985483630758135;
+      w[28] = 0.001384550491324;
+      r[29] = -0.985483630758135;
+      s[29] = 0.970967261516271;
+      w[29] = 0.001384550491324;
+      r[30] = -0.545571095693272;
+      s[30] = 0.542986390284387;
+      w[30] = 0.002496578398555;
+      r[31] = 0.542986390284387;
+      s[31] = -0.545571095693272;
+      w[31] = 0.002496578398555;
+      r[32] = -0.997415294591116;
+      s[32] = 0.542986390284387;
+      w[32] = 0.002496578398555;
+      r[33] = 0.542986390284387;
+      s[33] = -0.997415294591116;
+      w[33] = 0.002496578398555;
+      r[34] = -0.997415294591116;
+      s[34] = -0.545571095693272;
+      w[34] = 0.002496578398555;
+      r[35] = -0.545571095693272;
+      s[35] = -0.997415294591116;
+      w[35] = 0.002496578398555;
+      r[36] = -0.129978890292857;
+      s[36] = 0.119179487748624;
+      w[36] = 0.006809505817606;
+      r[37] = 0.119179487748624;
+      s[37] = -0.129978890292857;
+      w[37] = 0.006809505817606;
+      r[38] = -0.989200597455768;
+      s[38] = 0.119179487748624;
+      w[38] = 0.006809505817606;
+      r[39] = 0.119179487748624;
+      s[39] = -0.989200597455768;
+      w[39] = 0.006809505817606;
+      r[40] = -0.989200597455768;
+      s[40] = -0.129978890292857;
+      w[40] = 0.006809505817606;
+      r[41] = -0.129978890292857;
+      s[41] = -0.989200597455768;
+      w[41] = 0.006809505817606;
+      r[42] = -0.359380801455591;
+      s[42] = 0.346612795387641;
+      w[42] = 0.006719308652128;
+      r[43] = 0.346612795387641;
+      s[43] = -0.359380801455591;
+      w[43] = 0.006719308652128;
+      r[44] = -0.987231993932050;
+      s[44] = 0.346612795387641;
+      w[44] = 0.006719308652128;
+      r[45] = 0.346612795387641;
+      s[45] = -0.987231993932050;
+      w[45] = 0.006719308652128;
+      r[46] = -0.987231993932050;
+      s[46] = -0.359380801455591;
+      w[46] = 0.006719308652128;
+      r[47] = -0.359380801455591;
+      s[47] = -0.987231993932050;
+      w[47] = 0.006719308652128;
+      r[48] = -0.816499355439990;
+      s[48] = 0.806442932436004;
+      w[48] = 0.003432313078994;
+      r[49] = 0.806442932436004;
+      s[49] = -0.816499355439990;
+      w[49] = 0.003432313078994;
+      r[50] = -0.989943576996014;
+      s[50] = 0.806442932436004;
+      w[50] = 0.003432313078994;
+      r[51] = 0.806442932436004;
+      s[51] = -0.989943576996014;
+      w[51] = 0.003432313078994;
+      r[52] = -0.989943576996014;
+      s[52] = -0.816499355439990;
+      w[52] = 0.003432313078994;
+      r[53] = -0.816499355439990;
+      s[53] = -0.989943576996014;
+      w[53] = 0.003432313078994;
+      r[54] = -0.923978328282551;
+      s[54] = 0.910324811038988;
+      w[54] = 0.002961712633431;
+      r[55] = 0.910324811038988;
+      s[55] = -0.923978328282551;
+      w[55] = 0.002961712633431;
+      r[56] = -0.986346482756436;
+      s[56] = 0.910324811038988;
+      w[56] = 0.002961712633431;
+      r[57] = 0.910324811038988;
+      s[57] = -0.986346482756436;
+      w[57] = 0.002961712633431;
+      r[58] = -0.986346482756436;
+      s[58] = -0.923978328282551;
+      w[58] = 0.002961712633431;
+      r[59] = -0.923978328282551;
+      s[59] = -0.986346482756436;
+      w[59] = 0.002961712633431;
+      r[60] = -0.685149563029377;
+      s[60] = 0.665117163749518;
+      w[60] = 0.007022625221457;
+      r[61] = 0.665117163749518;
+      s[61] = -0.685149563029377;
+      w[61] = 0.007022625221457;
+      r[62] = -0.979967600720141;
+      s[62] = 0.665117163749517;
+      w[62] = 0.007022625221457;
+      r[63] = 0.665117163749517;
+      s[63] = -0.979967600720141;
+      w[63] = 0.007022625221457;
+      r[64] = -0.979967600720141;
+      s[64] = -0.685149563029376;
+      w[64] = 0.007022625221457;
+      r[65] = -0.685149563029376;
+      s[65] = -0.979967600720141;
+      w[65] = 0.007022625221457;
+      r[66] = -0.520220680442934;
+      s[66] = 0.468705054096154;
+      w[66] = 0.014787100299413;
+      r[67] = 0.468705054096154;
+      s[67] = -0.520220680442934;
+      w[67] = 0.014787100299413;
+      r[68] = -0.948484373653220;
+      s[68] = 0.468705054096154;
+      w[68] = 0.014787100299413;
+      r[69] = 0.468705054096154;
+      s[69] = -0.948484373653220;
+      w[69] = 0.014787100299413;
+      r[70] = -0.948484373653220;
+      s[70] = -0.520220680442934;
+      w[70] = 0.014787100299413;
+      r[71] = -0.520220680442934;
+      s[71] = -0.948484373653220;
+      w[71] = 0.014787100299413;
+      r[72] = -0.276113763747879;
+      s[72] = 0.215657967508047;
+      w[72] = 0.015966174954753;
+      r[73] = 0.215657967508047;
+      s[73] = -0.276113763747879;
+      w[73] = 0.015966174954753;
+      r[74] = -0.939544203760168;
+      s[74] = 0.215657967508047;
+      w[74] = 0.015966174954753;
+      r[75] = 0.215657967508047;
+      s[75] = -0.939544203760168;
+      w[75] = 0.015966174954753;
+      r[76] = -0.939544203760168;
+      s[76] = -0.276113763747879;
+      w[76] = 0.015966174954753;
+      r[77] = -0.276113763747879;
+      s[77] = -0.939544203760168;
+      w[77] = 0.015966174954753;
+      r[78] = -0.832896078090343;
+      s[78] = 0.771886097876019;
+      w[78] = 0.008711925226316;
+      r[79] = 0.771886097876019;
+      s[79] = -0.832896078090343;
+      w[79] = 0.008711925226316;
+      r[80] = -0.938990019785676;
+      s[80] = 0.771886097876019;
+      w[80] = 0.008711925226316;
+      r[81] = 0.771886097876019;
+      s[81] = -0.938990019785676;
+      w[81] = 0.008711925226316;
+      r[82] = -0.938990019785676;
+      s[82] = -0.832896078090343;
+      w[82] = 0.008711925226316;
+      r[83] = -0.832896078090343;
+      s[83] = -0.938990019785676;
+      w[83] = 0.008711925226316;
+      r[84] = -0.703113558535164;
+      s[84] = 0.611200463810025;
+      w[84] = 0.014730113402836;
+      r[85] = 0.611200463810025;
+      s[85] = -0.703113558535164;
+      w[85] = 0.014730113402836;
+      r[86] = -0.908086905274861;
+      s[86] = 0.611200463810025;
+      w[86] = 0.014730113402836;
+      r[87] = 0.611200463810025;
+      s[87] = -0.908086905274861;
+      w[87] = 0.014730113402836;
+      r[88] = -0.908086905274861;
+      s[88] = -0.703113558535164;
+      w[88] = 0.014730113402836;
+      r[89] = -0.703113558535164;
+      s[89] = -0.908086905274861;
+      w[89] = 0.014730113402836;
+      r[90] = -0.432520582544930;
+      s[90] = 0.297634981464375;
+      w[90] = 0.021927145692839;
+      r[91] = 0.297634981464375;
+      s[91] = -0.432520582544930;
+      w[91] = 0.021927145692839;
+      r[92] = -0.865114398919445;
+      s[92] = 0.297634981464375;
+      w[92] = 0.021927145692839;
+      r[93] = 0.297634981464375;
+      s[93] = -0.865114398919445;
+      w[93] = 0.021927145692839;
+      r[94] = -0.865114398919445;
+      s[94] = -0.432520582544930;
+      w[94] = 0.021927145692839;
+      r[95] = -0.432520582544930;
+      s[95] = -0.865114398919445;
+      w[95] = 0.021927145692839;
+      r[96] = -0.186201249762425;
+      s[96] = 0.046111066930604;
+      w[96] = 0.023499923487082;
+      r[97] = 0.046111066930604;
+      s[97] = -0.186201249762425;
+      w[97] = 0.023499923487082;
+      r[98] = -0.859909817168179;
+      s[98] = 0.046111066930604;
+      w[98] = 0.023499923487082;
+      r[99] = 0.046111066930604;
+      s[99] = -0.859909817168179;
+      w[99] = 0.023499923487082;
+      r[100] = -0.859909817168179;
+      s[100] = -0.186201249762425;
+      w[100] = 0.023499923487082;
+      r[101] = -0.186201249762425;
+      s[101] = -0.859909817168179;
+      w[101] = 0.023499923487082;
+      r[102] = -0.611772025950215;
+      s[102] = 0.443948976669982;
+      w[102] = 0.020031201427597;
+      r[103] = 0.443948976669982;
+      s[103] = -0.611772025950215;
+      w[103] = 0.020031201427597;
+      r[104] = -0.832176950719767;
+      s[104] = 0.443948976669982;
+      w[104] = 0.020031201427597;
+      r[105] = 0.443948976669982;
+      s[105] = -0.832176950719767;
+      w[105] = 0.020031201427597;
+      r[106] = -0.832176950719767;
+      s[106] = -0.611772025950215;
+      w[106] = 0.020031201427597;
+      r[107] = -0.611772025950215;
+      s[107] = -0.832176950719767;
+      w[107] = 0.020031201427597;
+      r[108] = -0.351731305998594;
+      s[108] = 0.110980234644288;
+      w[108] = 0.026619281575257;
+      r[109] = 0.110980234644288;
+      s[109] = -0.351731305998594;
+      w[109] = 0.026619281575257;
+      r[110] = -0.759248928645695;
+      s[110] = 0.110980234644288;
+      w[110] = 0.026619281575257;
+      r[111] = 0.110980234644288;
+      s[111] = -0.759248928645695;
+      w[111] = 0.026619281575257;
+      r[112] = -0.759248928645695;
+      s[112] = -0.351731305998594;
+      w[112] = 0.026619281575257;
+      r[113] = -0.351731305998594;
+      s[113] = -0.759248928645695;
+      w[113] = 0.026619281575257;
+      r[114] = -0.541445032888038;
+      s[114] = 0.245311234573305;
+      w[114] = 0.028308893010452;
+      r[115] = 0.245311234573305;
+      s[115] = -0.541445032888038;
+      w[115] = 0.028308893010452;
+      r[116] = -0.703866201685267;
+      s[116] = 0.245311234573305;
+      w[116] = 0.028308893010452;
+      r[117] = 0.245311234573305;
+      s[117] = -0.703866201685267;
+      w[117] = 0.028308893010452;
+      r[118] = -0.703866201685267;
+      s[118] = -0.541445032888038;
+      w[118] = 0.028308893010452;
+      r[119] = -0.541445032888038;
+      s[119] = -0.703866201685267;
+      w[119] = 0.028308893010452;
+      r[120] = -0.348763754808032;
+      s[120] = -0.034779976926618;
+      w[120] = 0.029762759122336;
+      r[121] = -0.034779976926618;
+      s[121] = -0.348763754808032;
+      w[121] = 0.029762759122336;
+      r[122] = -0.616456268265350;
+      s[122] = -0.034779976926618;
+      w[122] = 0.029762759122336;
+      r[123] = -0.034779976926618;
+      s[123] = -0.616456268265350;
+      w[123] = 0.029762759122336;
+      r[124] = -0.616456268265350;
+      s[124] = -0.348763754808032;
+      w[124] = 0.029762759122336;
+      r[125] = -0.348763754808032;
+      s[125] = -0.616456268265350;
+      w[125] = 0.029762759122336;
 
       break;
     }
     case 26: {
-      r[0]   = -0.027285103318006; s[0]   = -0.027285103318006; w[0]   = 0.005361616431413;
-      r[1]   = -0.945429793363989; s[1]   = -0.027285103318006; w[1]   = 0.005361616431413;
-      r[2]   = -0.027285103318006; s[2]   = -0.945429793363989; w[2]   = 0.005361616431413;
-      r[3]   = -0.068629018183452; s[3]   = -0.068629018183452; w[3]   = 0.012732191427031;
-      r[4]   = -0.862741963633096; s[4]   = -0.068629018183452; w[4]   = 0.012732191427031;
-      r[5]   = -0.068629018183452; s[5]   = -0.862741963633096; w[5]   = 0.012732191427031;
-      r[6]   = -0.136174624247252; s[6]   = -0.136174624247252; w[6]   = 0.029707048808635;
-      r[7]   = -0.727650751505495; s[7]   = -0.136174624247252; w[7]   = 0.029707048808635;
-      r[8]   = -0.136174624247252; s[8]   = -0.727650751505495; w[8]   = 0.029707048808635;
-      r[9]   = -0.214440393597162; s[9]   = -0.214440393597162; w[9]   = 0.026709487358142;
-      r[10]  = -0.571119212805675; s[10]  = -0.214440393597162; w[10]  = 0.026709487358142;
-      r[11]  = -0.214440393597162; s[11]  = -0.571119212805675; w[11]  = 0.026709487358142;
-      r[12]  = -0.392927303733924; s[12]  = -0.392927303733924; w[12]  = 0.031691197689589;
-      r[13]  = -0.214145392532152; s[13]  = -0.392927303733924; w[13]  = 0.031691197689589;
-      r[14]  = -0.392927303733924; s[14]  = -0.214145392532152; w[14]  = 0.031691197689589;
-      r[15]  = -0.541283541373341; s[15]  = -0.541283541373341; w[15]  = 0.028281596577704;
-      r[16]  =  0.082567082746682; s[16]  = -0.541283541373341; w[16]  = 0.028281596577704;
-      r[17]  = -0.541283541373341; s[17]  =  0.082567082746682; w[17]  = 0.028281596577704;
-      r[18]  = -0.710171670270578; s[18]  = -0.710171670270578; w[18]  = 0.022460561269283;
-      r[19]  =  0.420343340541156; s[19]  = -0.710171670270578; w[19]  = 0.022460561269283;
-      r[20]  = -0.710171670270578; s[20]  =  0.420343340541156; w[20]  = 0.022460561269283;
-      r[21]  = -0.832251071789951; s[21]  = -0.832251071789951; w[21]  = 0.013160382318625;
-      r[22]  =  0.664502143579902; s[22]  = -0.832251071789951; w[22]  = 0.013160382318625;
-      r[23]  = -0.832251071789951; s[23]  =  0.664502143579902; w[23]  = 0.013160382318625;
-      r[24]  = -0.931928355163542; s[24]  = -0.931928355163542; w[24]  = 0.005828465225510;
-      r[25]  =  0.863856710327084; s[25]  = -0.931928355163542; w[25]  = 0.005828465225510;
-      r[26]  = -0.931928355163542; s[26]  =  0.863856710327084; w[26]  = 0.005828465225510;
-      r[27]  = -0.987078078630829; s[27]  = -0.987078078630829; w[27]  = 0.001098762787251;
-      r[28]  =  0.974156157261657; s[28]  = -0.987078078630829; w[28]  = 0.001098762787251;
-      r[29]  = -0.987078078630829; s[29]  =  0.974156157261657; w[29]  = 0.001098762787251;
-      r[30]  = -0.932113855389598; s[30]  =  0.919072286067742; w[30]  = 0.002557622023150;
-      r[31]  =  0.919072286067742; s[31]  = -0.932113855389598; w[31]  = 0.002557622023150;
-      r[32]  = -0.986958430678145; s[32]  =  0.919072286067742; w[32]  = 0.002557622023150;
-      r[33]  =  0.919072286067742; s[33]  = -0.986958430678145; w[33]  = 0.002557622023150;
-      r[34]  = -0.986958430678145; s[34]  = -0.932113855389597; w[34]  = 0.002557622023150;
-      r[35]  = -0.932113855389597; s[35]  = -0.986958430678145; w[35]  = 0.002557622023150;
-      r[36]  = -0.331832115907669; s[36]  =  0.318412220533634; w[36]  = 0.007088900226242;
-      r[37]  =  0.318412220533634; s[37]  = -0.331832115907669; w[37]  = 0.007088900226242;
-      r[38]  = -0.986580104625965; s[38]  =  0.318412220533634; w[38]  = 0.007088900226242;
-      r[39]  =  0.318412220533634; s[39]  = -0.986580104625965; w[39]  = 0.007088900226242;
-      r[40]  = -0.986580104625965; s[40]  = -0.331832115907669; w[40]  = 0.007088900226242;
-      r[41]  = -0.331832115907669; s[41]  = -0.986580104625965; w[41]  = 0.007088900226242;
-      r[42]  = -0.117284648816543; s[42]  =  0.105635324925259; w[42]  = 0.006588000446609;
-      r[43]  =  0.105635324925259; s[43]  = -0.117284648816543; w[43]  = 0.006588000446609;
-      r[44]  = -0.988350676108717; s[44]  =  0.105635324925259; w[44]  = 0.006588000446609;
-      r[45]  =  0.105635324925259; s[45]  = -0.988350676108717; w[45]  = 0.006588000446609;
-      r[46]  = -0.988350676108717; s[46]  = -0.117284648816543; w[46]  = 0.006588000446609;
-      r[47]  = -0.117284648816543; s[47]  = -0.988350676108717; w[47]  = 0.006588000446609;
-      r[48]  = -0.528179583523521; s[48]  =  0.515363521190658; w[48]  = 0.006069708653929;
-      r[49]  =  0.515363521190658; s[49]  = -0.528179583523521; w[49]  = 0.006069708653929;
-      r[50]  = -0.987183937667137; s[50]  =  0.515363521190658; w[50]  = 0.006069708653929;
-      r[51]  =  0.515363521190658; s[51]  = -0.987183937667137; w[51]  = 0.006069708653929;
-      r[52]  = -0.987183937667137; s[52]  = -0.528179583523521; w[52]  = 0.006069708653929;
-      r[53]  = -0.528179583523521; s[53]  = -0.987183937667137; w[53]  = 0.006069708653929;
-      r[54]  = -0.698183069548291; s[54]  =  0.685666877859863; w[54]  = 0.004942128706706;
-      r[55]  =  0.685666877859863; s[55]  = -0.698183069548291; w[55]  = 0.004942128706706;
-      r[56]  = -0.987483808311572; s[56]  =  0.685666877859863; w[56]  = 0.004942128706706;
-      r[57]  =  0.685666877859863; s[57]  = -0.987483808311572; w[57]  = 0.004942128706706;
-      r[58]  = -0.987483808311572; s[58]  = -0.698183069548291; w[58]  = 0.004942128706706;
-      r[59]  = -0.698183069548291; s[59]  = -0.987483808311572; w[59]  = 0.004942128706706;
-      r[60]  = -0.834663613179069; s[60]  =  0.821127985248516; w[60]  = 0.004076340070443;
-      r[61]  =  0.821127985248516; s[61]  = -0.834663613179069; w[61]  = 0.004076340070443;
-      r[62]  = -0.986464372069447; s[62]  =  0.821127985248516; w[62]  = 0.004076340070443;
-      r[63]  =  0.821127985248516; s[63]  = -0.986464372069447; w[63]  = 0.004076340070443;
-      r[64]  = -0.986464372069447; s[64]  = -0.834663613179069; w[64]  = 0.004076340070443;
-      r[65]  = -0.834663613179069; s[65]  = -0.986464372069447; w[65]  = 0.004076340070443;
-      r[66]  = -0.700166221086294; s[66]  =  0.634916644768372; w[66]  = 0.011120280239045;
-      r[67]  =  0.634916644768372; s[67]  = -0.700166221086294; w[67]  = 0.011120280239045;
-      r[68]  = -0.934750423682077; s[68]  =  0.634916644768372; w[68]  = 0.011120280239045;
-      r[69]  =  0.634916644768372; s[69]  = -0.934750423682077; w[69]  = 0.011120280239045;
-      r[70]  = -0.934750423682078; s[70]  = -0.700166221086294; w[70]  = 0.011120280239045;
-      r[71]  = -0.700166221086294; s[71]  = -0.934750423682078; w[71]  = 0.011120280239045;
-      r[72]  = -0.160245113591115; s[72]  =  0.096801406370527; w[72]  = 0.012755358640694;
-      r[73]  =  0.096801406370527; s[73]  = -0.160245113591115; w[73]  = 0.012755358640694;
-      r[74]  = -0.936556292779412; s[74]  =  0.096801406370527; w[74]  = 0.012755358640694;
-      r[75]  =  0.096801406370527; s[75]  = -0.936556292779412; w[75]  = 0.012755358640694;
-      r[76]  = -0.936556292779412; s[76]  = -0.160245113591115; w[76]  = 0.012755358640694;
-      r[77]  = -0.160245113591115; s[77]  = -0.936556292779412; w[77]  = 0.012755358640694;
-      r[78]  = -0.348814552390868; s[78]  =  0.279444440434072; w[78]  = 0.014549157045387;
-      r[79]  =  0.279444440434072; s[79]  = -0.348814552390868; w[79]  = 0.014549157045387;
-      r[80]  = -0.930629888043204; s[80]  =  0.279444440434072; w[80]  = 0.014549157045387;
-      r[81]  =  0.279444440434072; s[81]  = -0.930629888043204; w[81]  = 0.014549157045387;
-      r[82]  = -0.930629888043204; s[82]  = -0.348814552390868; w[82]  = 0.014549157045387;
-      r[83]  = -0.348814552390868; s[83]  = -0.930629888043204; w[83]  = 0.014549157045387;
-      r[84]  = -0.835149343614232; s[84]  =  0.764834325997890; w[84]  = 0.009121880355576;
-      r[85]  =  0.764834325997890; s[85]  = -0.835149343614232; w[85]  = 0.009121880355576;
-      r[86]  = -0.929684982383659; s[86]  =  0.764834325997890; w[86]  = 0.009121880355576;
-      r[87]  =  0.764834325997890; s[87]  = -0.929684982383659; w[87]  = 0.009121880355576;
-      r[88]  = -0.929684982383659; s[88]  = -0.835149343614232; w[88]  = 0.009121880355576;
-      r[89]  = -0.835149343614232; s[89]  = -0.929684982383659; w[89]  = 0.009121880355576;
-      r[90]  = -0.534046892746188; s[90]  =  0.466663082505331; w[90]  = 0.013582808914065;
-      r[91]  =  0.466663082505331; s[91]  = -0.534046892746188; w[91]  = 0.013582808914065;
-      r[92]  = -0.932616189759143; s[92]  =  0.466663082505331; w[92]  = 0.013582808914065;
-      r[93]  =  0.466663082505331; s[93]  = -0.932616189759143; w[93]  = 0.013582808914065;
-      r[94]  = -0.932616189759143; s[94]  = -0.534046892746188; w[94]  = 0.013582808914065;
-      r[95]  = -0.534046892746188; s[95]  = -0.932616189759143; w[95]  = 0.013582808914065;
-      r[96]  = -0.704373154566392; s[96]  =  0.546726033293271; w[96]  = 0.015585248954434;
-      r[97]  =  0.546726033293271; s[97]  = -0.704373154566392; w[97]  = 0.015585248954434;
-      r[98]  = -0.842352878726879; s[98]  =  0.546726033293271; w[98]  = 0.015585248954434;
-      r[99]  =  0.546726033293271; s[99]  = -0.842352878726879; w[99]  = 0.015585248954434;
-      r[100] = -0.842352878726879; s[100] = -0.704373154566392; w[100] = 0.015585248954434;
-      r[101] = -0.704373154566392; s[101] = -0.842352878726879; w[101] = 0.015585248954434;
-      r[102] = -0.220224863280788; s[102] =  0.060870104244893; w[102] = 0.018960151369388;
-      r[103] =  0.060870104244893; s[103] = -0.220224863280788; w[103] = 0.018960151369388;
-      r[104] = -0.840645240964104; s[104] =  0.060870104244893; w[104] = 0.018960151369388;
-      r[105] =  0.060870104244893; s[105] = -0.840645240964104; w[105] = 0.018960151369388;
-      r[106] = -0.840645240964104; s[106] = -0.220224863280788; w[106] = 0.018960151369388;
-      r[107] = -0.220224863280788; s[107] = -0.840645240964104; w[107] = 0.018960151369388;
-      r[108] = -0.394989254221112; s[108] =  0.230609434358343; w[108] = 0.019206200353033;
-      r[109] =  0.230609434358343; s[109] = -0.394989254221112; w[109] = 0.019206200353033;
-      r[110] = -0.835620180137232; s[110] =  0.230609434358343; w[110] = 0.019206200353033;
-      r[111] =  0.230609434358343; s[111] = -0.835620180137232; w[111] = 0.019206200353033;
-      r[112] = -0.835620180137232; s[112] = -0.394989254221112; w[112] = 0.019206200353033;
-      r[113] = -0.394989254221112; s[113] = -0.835620180137232; w[113] = 0.019206200353033;
-      r[114] = -0.557563751773578; s[114] =  0.393274056332418; w[114] = 0.018121839059318;
-      r[115] =  0.393274056332418; s[115] = -0.557563751773578; w[115] = 0.018121839059318;
-      r[116] = -0.835710304558840; s[116] =  0.393274056332418; w[116] = 0.018121839059318;
-      r[117] =  0.393274056332418; s[117] = -0.835710304558840; w[117] = 0.018121839059318;
-      r[118] = -0.835710304558840; s[118] = -0.557563751773578; w[118] = 0.018121839059318;
-      r[119] = -0.557563751773578; s[119] = -0.835710304558840; w[119] = 0.018121839059318;
-      r[120] = -0.350522450436603; s[120] =  0.060630141977535; w[120] = 0.028403705951863;
-      r[121] =  0.060630141977535; s[121] = -0.350522450436603; w[121] = 0.028403705951863;
-      r[122] = -0.710107691540932; s[122] =  0.060630141977535; w[122] = 0.028403705951863;
-      r[123] =  0.060630141977535; s[123] = -0.710107691540932; w[123] = 0.028403705951863;
-      r[124] = -0.710107691540932; s[124] = -0.350522450436603; w[124] = 0.028403705951863;
-      r[125] = -0.350522450436603; s[125] = -0.710107691540932; w[125] = 0.028403705951863;
-      r[126] = -0.544246685468649; s[126] =  0.246315777233803; w[126] = 0.026986162760930;
-      r[127] =  0.246315777233803; s[127] = -0.544246685468649; w[127] = 0.026986162760930;
-      r[128] = -0.702069091765154; s[128] =  0.246315777233803; w[128] = 0.026986162760930;
-      r[129] =  0.246315777233803; s[129] = -0.702069091765154; w[129] = 0.026986162760930;
-      r[130] = -0.702069091765154; s[130] = -0.544246685468649; w[130] = 0.026986162760930;
-      r[131] = -0.544246685468649; s[131] = -0.702069091765154; w[131] = 0.026986162760930;
-      r[132] = -0.373996265063702; s[132] = -0.064072130507071; w[132] = 0.025102184615930;
-      r[133] = -0.064072130507071; s[133] = -0.373996265063702; w[133] = 0.025102184615930;
-      r[134] = -0.561931604429227; s[134] = -0.064072130507071; w[134] = 0.025102184615930;
-      r[135] = -0.064072130507071; s[135] = -0.561931604429227; w[135] = 0.025102184615930;
-      r[136] = -0.561931604429227; s[136] = -0.373996265063702; w[136] = 0.025102184615930;
-      r[137] = -0.373996265063702; s[137] = -0.561931604429227; w[137] = 0.025102184615930;
+      r[0] = -0.027285103318006;
+      s[0] = -0.027285103318006;
+      w[0] = 0.005361616431413;
+      r[1] = -0.945429793363989;
+      s[1] = -0.027285103318006;
+      w[1] = 0.005361616431413;
+      r[2] = -0.027285103318006;
+      s[2] = -0.945429793363989;
+      w[2] = 0.005361616431413;
+      r[3] = -0.068629018183452;
+      s[3] = -0.068629018183452;
+      w[3] = 0.012732191427031;
+      r[4] = -0.862741963633096;
+      s[4] = -0.068629018183452;
+      w[4] = 0.012732191427031;
+      r[5] = -0.068629018183452;
+      s[5] = -0.862741963633096;
+      w[5] = 0.012732191427031;
+      r[6] = -0.136174624247252;
+      s[6] = -0.136174624247252;
+      w[6] = 0.029707048808635;
+      r[7] = -0.727650751505495;
+      s[7] = -0.136174624247252;
+      w[7] = 0.029707048808635;
+      r[8] = -0.136174624247252;
+      s[8] = -0.727650751505495;
+      w[8] = 0.029707048808635;
+      r[9] = -0.214440393597162;
+      s[9] = -0.214440393597162;
+      w[9] = 0.026709487358142;
+      r[10] = -0.571119212805675;
+      s[10] = -0.214440393597162;
+      w[10] = 0.026709487358142;
+      r[11] = -0.214440393597162;
+      s[11] = -0.571119212805675;
+      w[11] = 0.026709487358142;
+      r[12] = -0.392927303733924;
+      s[12] = -0.392927303733924;
+      w[12] = 0.031691197689589;
+      r[13] = -0.214145392532152;
+      s[13] = -0.392927303733924;
+      w[13] = 0.031691197689589;
+      r[14] = -0.392927303733924;
+      s[14] = -0.214145392532152;
+      w[14] = 0.031691197689589;
+      r[15] = -0.541283541373341;
+      s[15] = -0.541283541373341;
+      w[15] = 0.028281596577704;
+      r[16] = 0.082567082746682;
+      s[16] = -0.541283541373341;
+      w[16] = 0.028281596577704;
+      r[17] = -0.541283541373341;
+      s[17] = 0.082567082746682;
+      w[17] = 0.028281596577704;
+      r[18] = -0.710171670270578;
+      s[18] = -0.710171670270578;
+      w[18] = 0.022460561269283;
+      r[19] = 0.420343340541156;
+      s[19] = -0.710171670270578;
+      w[19] = 0.022460561269283;
+      r[20] = -0.710171670270578;
+      s[20] = 0.420343340541156;
+      w[20] = 0.022460561269283;
+      r[21] = -0.832251071789951;
+      s[21] = -0.832251071789951;
+      w[21] = 0.013160382318625;
+      r[22] = 0.664502143579902;
+      s[22] = -0.832251071789951;
+      w[22] = 0.013160382318625;
+      r[23] = -0.832251071789951;
+      s[23] = 0.664502143579902;
+      w[23] = 0.013160382318625;
+      r[24] = -0.931928355163542;
+      s[24] = -0.931928355163542;
+      w[24] = 0.005828465225510;
+      r[25] = 0.863856710327084;
+      s[25] = -0.931928355163542;
+      w[25] = 0.005828465225510;
+      r[26] = -0.931928355163542;
+      s[26] = 0.863856710327084;
+      w[26] = 0.005828465225510;
+      r[27] = -0.987078078630829;
+      s[27] = -0.987078078630829;
+      w[27] = 0.001098762787251;
+      r[28] = 0.974156157261657;
+      s[28] = -0.987078078630829;
+      w[28] = 0.001098762787251;
+      r[29] = -0.987078078630829;
+      s[29] = 0.974156157261657;
+      w[29] = 0.001098762787251;
+      r[30] = -0.932113855389598;
+      s[30] = 0.919072286067742;
+      w[30] = 0.002557622023150;
+      r[31] = 0.919072286067742;
+      s[31] = -0.932113855389598;
+      w[31] = 0.002557622023150;
+      r[32] = -0.986958430678145;
+      s[32] = 0.919072286067742;
+      w[32] = 0.002557622023150;
+      r[33] = 0.919072286067742;
+      s[33] = -0.986958430678145;
+      w[33] = 0.002557622023150;
+      r[34] = -0.986958430678145;
+      s[34] = -0.932113855389597;
+      w[34] = 0.002557622023150;
+      r[35] = -0.932113855389597;
+      s[35] = -0.986958430678145;
+      w[35] = 0.002557622023150;
+      r[36] = -0.331832115907669;
+      s[36] = 0.318412220533634;
+      w[36] = 0.007088900226242;
+      r[37] = 0.318412220533634;
+      s[37] = -0.331832115907669;
+      w[37] = 0.007088900226242;
+      r[38] = -0.986580104625965;
+      s[38] = 0.318412220533634;
+      w[38] = 0.007088900226242;
+      r[39] = 0.318412220533634;
+      s[39] = -0.986580104625965;
+      w[39] = 0.007088900226242;
+      r[40] = -0.986580104625965;
+      s[40] = -0.331832115907669;
+      w[40] = 0.007088900226242;
+      r[41] = -0.331832115907669;
+      s[41] = -0.986580104625965;
+      w[41] = 0.007088900226242;
+      r[42] = -0.117284648816543;
+      s[42] = 0.105635324925259;
+      w[42] = 0.006588000446609;
+      r[43] = 0.105635324925259;
+      s[43] = -0.117284648816543;
+      w[43] = 0.006588000446609;
+      r[44] = -0.988350676108717;
+      s[44] = 0.105635324925259;
+      w[44] = 0.006588000446609;
+      r[45] = 0.105635324925259;
+      s[45] = -0.988350676108717;
+      w[45] = 0.006588000446609;
+      r[46] = -0.988350676108717;
+      s[46] = -0.117284648816543;
+      w[46] = 0.006588000446609;
+      r[47] = -0.117284648816543;
+      s[47] = -0.988350676108717;
+      w[47] = 0.006588000446609;
+      r[48] = -0.528179583523521;
+      s[48] = 0.515363521190658;
+      w[48] = 0.006069708653929;
+      r[49] = 0.515363521190658;
+      s[49] = -0.528179583523521;
+      w[49] = 0.006069708653929;
+      r[50] = -0.987183937667137;
+      s[50] = 0.515363521190658;
+      w[50] = 0.006069708653929;
+      r[51] = 0.515363521190658;
+      s[51] = -0.987183937667137;
+      w[51] = 0.006069708653929;
+      r[52] = -0.987183937667137;
+      s[52] = -0.528179583523521;
+      w[52] = 0.006069708653929;
+      r[53] = -0.528179583523521;
+      s[53] = -0.987183937667137;
+      w[53] = 0.006069708653929;
+      r[54] = -0.698183069548291;
+      s[54] = 0.685666877859863;
+      w[54] = 0.004942128706706;
+      r[55] = 0.685666877859863;
+      s[55] = -0.698183069548291;
+      w[55] = 0.004942128706706;
+      r[56] = -0.987483808311572;
+      s[56] = 0.685666877859863;
+      w[56] = 0.004942128706706;
+      r[57] = 0.685666877859863;
+      s[57] = -0.987483808311572;
+      w[57] = 0.004942128706706;
+      r[58] = -0.987483808311572;
+      s[58] = -0.698183069548291;
+      w[58] = 0.004942128706706;
+      r[59] = -0.698183069548291;
+      s[59] = -0.987483808311572;
+      w[59] = 0.004942128706706;
+      r[60] = -0.834663613179069;
+      s[60] = 0.821127985248516;
+      w[60] = 0.004076340070443;
+      r[61] = 0.821127985248516;
+      s[61] = -0.834663613179069;
+      w[61] = 0.004076340070443;
+      r[62] = -0.986464372069447;
+      s[62] = 0.821127985248516;
+      w[62] = 0.004076340070443;
+      r[63] = 0.821127985248516;
+      s[63] = -0.986464372069447;
+      w[63] = 0.004076340070443;
+      r[64] = -0.986464372069447;
+      s[64] = -0.834663613179069;
+      w[64] = 0.004076340070443;
+      r[65] = -0.834663613179069;
+      s[65] = -0.986464372069447;
+      w[65] = 0.004076340070443;
+      r[66] = -0.700166221086294;
+      s[66] = 0.634916644768372;
+      w[66] = 0.011120280239045;
+      r[67] = 0.634916644768372;
+      s[67] = -0.700166221086294;
+      w[67] = 0.011120280239045;
+      r[68] = -0.934750423682077;
+      s[68] = 0.634916644768372;
+      w[68] = 0.011120280239045;
+      r[69] = 0.634916644768372;
+      s[69] = -0.934750423682077;
+      w[69] = 0.011120280239045;
+      r[70] = -0.934750423682078;
+      s[70] = -0.700166221086294;
+      w[70] = 0.011120280239045;
+      r[71] = -0.700166221086294;
+      s[71] = -0.934750423682078;
+      w[71] = 0.011120280239045;
+      r[72] = -0.160245113591115;
+      s[72] = 0.096801406370527;
+      w[72] = 0.012755358640694;
+      r[73] = 0.096801406370527;
+      s[73] = -0.160245113591115;
+      w[73] = 0.012755358640694;
+      r[74] = -0.936556292779412;
+      s[74] = 0.096801406370527;
+      w[74] = 0.012755358640694;
+      r[75] = 0.096801406370527;
+      s[75] = -0.936556292779412;
+      w[75] = 0.012755358640694;
+      r[76] = -0.936556292779412;
+      s[76] = -0.160245113591115;
+      w[76] = 0.012755358640694;
+      r[77] = -0.160245113591115;
+      s[77] = -0.936556292779412;
+      w[77] = 0.012755358640694;
+      r[78] = -0.348814552390868;
+      s[78] = 0.279444440434072;
+      w[78] = 0.014549157045387;
+      r[79] = 0.279444440434072;
+      s[79] = -0.348814552390868;
+      w[79] = 0.014549157045387;
+      r[80] = -0.930629888043204;
+      s[80] = 0.279444440434072;
+      w[80] = 0.014549157045387;
+      r[81] = 0.279444440434072;
+      s[81] = -0.930629888043204;
+      w[81] = 0.014549157045387;
+      r[82] = -0.930629888043204;
+      s[82] = -0.348814552390868;
+      w[82] = 0.014549157045387;
+      r[83] = -0.348814552390868;
+      s[83] = -0.930629888043204;
+      w[83] = 0.014549157045387;
+      r[84] = -0.835149343614232;
+      s[84] = 0.764834325997890;
+      w[84] = 0.009121880355576;
+      r[85] = 0.764834325997890;
+      s[85] = -0.835149343614232;
+      w[85] = 0.009121880355576;
+      r[86] = -0.929684982383659;
+      s[86] = 0.764834325997890;
+      w[86] = 0.009121880355576;
+      r[87] = 0.764834325997890;
+      s[87] = -0.929684982383659;
+      w[87] = 0.009121880355576;
+      r[88] = -0.929684982383659;
+      s[88] = -0.835149343614232;
+      w[88] = 0.009121880355576;
+      r[89] = -0.835149343614232;
+      s[89] = -0.929684982383659;
+      w[89] = 0.009121880355576;
+      r[90] = -0.534046892746188;
+      s[90] = 0.466663082505331;
+      w[90] = 0.013582808914065;
+      r[91] = 0.466663082505331;
+      s[91] = -0.534046892746188;
+      w[91] = 0.013582808914065;
+      r[92] = -0.932616189759143;
+      s[92] = 0.466663082505331;
+      w[92] = 0.013582808914065;
+      r[93] = 0.466663082505331;
+      s[93] = -0.932616189759143;
+      w[93] = 0.013582808914065;
+      r[94] = -0.932616189759143;
+      s[94] = -0.534046892746188;
+      w[94] = 0.013582808914065;
+      r[95] = -0.534046892746188;
+      s[95] = -0.932616189759143;
+      w[95] = 0.013582808914065;
+      r[96] = -0.704373154566392;
+      s[96] = 0.546726033293271;
+      w[96] = 0.015585248954434;
+      r[97] = 0.546726033293271;
+      s[97] = -0.704373154566392;
+      w[97] = 0.015585248954434;
+      r[98] = -0.842352878726879;
+      s[98] = 0.546726033293271;
+      w[98] = 0.015585248954434;
+      r[99] = 0.546726033293271;
+      s[99] = -0.842352878726879;
+      w[99] = 0.015585248954434;
+      r[100] = -0.842352878726879;
+      s[100] = -0.704373154566392;
+      w[100] = 0.015585248954434;
+      r[101] = -0.704373154566392;
+      s[101] = -0.842352878726879;
+      w[101] = 0.015585248954434;
+      r[102] = -0.220224863280788;
+      s[102] = 0.060870104244893;
+      w[102] = 0.018960151369388;
+      r[103] = 0.060870104244893;
+      s[103] = -0.220224863280788;
+      w[103] = 0.018960151369388;
+      r[104] = -0.840645240964104;
+      s[104] = 0.060870104244893;
+      w[104] = 0.018960151369388;
+      r[105] = 0.060870104244893;
+      s[105] = -0.840645240964104;
+      w[105] = 0.018960151369388;
+      r[106] = -0.840645240964104;
+      s[106] = -0.220224863280788;
+      w[106] = 0.018960151369388;
+      r[107] = -0.220224863280788;
+      s[107] = -0.840645240964104;
+      w[107] = 0.018960151369388;
+      r[108] = -0.394989254221112;
+      s[108] = 0.230609434358343;
+      w[108] = 0.019206200353033;
+      r[109] = 0.230609434358343;
+      s[109] = -0.394989254221112;
+      w[109] = 0.019206200353033;
+      r[110] = -0.835620180137232;
+      s[110] = 0.230609434358343;
+      w[110] = 0.019206200353033;
+      r[111] = 0.230609434358343;
+      s[111] = -0.835620180137232;
+      w[111] = 0.019206200353033;
+      r[112] = -0.835620180137232;
+      s[112] = -0.394989254221112;
+      w[112] = 0.019206200353033;
+      r[113] = -0.394989254221112;
+      s[113] = -0.835620180137232;
+      w[113] = 0.019206200353033;
+      r[114] = -0.557563751773578;
+      s[114] = 0.393274056332418;
+      w[114] = 0.018121839059318;
+      r[115] = 0.393274056332418;
+      s[115] = -0.557563751773578;
+      w[115] = 0.018121839059318;
+      r[116] = -0.835710304558840;
+      s[116] = 0.393274056332418;
+      w[116] = 0.018121839059318;
+      r[117] = 0.393274056332418;
+      s[117] = -0.835710304558840;
+      w[117] = 0.018121839059318;
+      r[118] = -0.835710304558840;
+      s[118] = -0.557563751773578;
+      w[118] = 0.018121839059318;
+      r[119] = -0.557563751773578;
+      s[119] = -0.835710304558840;
+      w[119] = 0.018121839059318;
+      r[120] = -0.350522450436603;
+      s[120] = 0.060630141977535;
+      w[120] = 0.028403705951863;
+      r[121] = 0.060630141977535;
+      s[121] = -0.350522450436603;
+      w[121] = 0.028403705951863;
+      r[122] = -0.710107691540932;
+      s[122] = 0.060630141977535;
+      w[122] = 0.028403705951863;
+      r[123] = 0.060630141977535;
+      s[123] = -0.710107691540932;
+      w[123] = 0.028403705951863;
+      r[124] = -0.710107691540932;
+      s[124] = -0.350522450436603;
+      w[124] = 0.028403705951863;
+      r[125] = -0.350522450436603;
+      s[125] = -0.710107691540932;
+      w[125] = 0.028403705951863;
+      r[126] = -0.544246685468649;
+      s[126] = 0.246315777233803;
+      w[126] = 0.026986162760930;
+      r[127] = 0.246315777233803;
+      s[127] = -0.544246685468649;
+      w[127] = 0.026986162760930;
+      r[128] = -0.702069091765154;
+      s[128] = 0.246315777233803;
+      w[128] = 0.026986162760930;
+      r[129] = 0.246315777233803;
+      s[129] = -0.702069091765154;
+      w[129] = 0.026986162760930;
+      r[130] = -0.702069091765154;
+      s[130] = -0.544246685468649;
+      w[130] = 0.026986162760930;
+      r[131] = -0.544246685468649;
+      s[131] = -0.702069091765154;
+      w[131] = 0.026986162760930;
+      r[132] = -0.373996265063702;
+      s[132] = -0.064072130507071;
+      w[132] = 0.025102184615930;
+      r[133] = -0.064072130507071;
+      s[133] = -0.373996265063702;
+      w[133] = 0.025102184615930;
+      r[134] = -0.561931604429227;
+      s[134] = -0.064072130507071;
+      w[134] = 0.025102184615930;
+      r[135] = -0.064072130507071;
+      s[135] = -0.561931604429227;
+      w[135] = 0.025102184615930;
+      r[136] = -0.561931604429227;
+      s[136] = -0.373996265063702;
+      w[136] = 0.025102184615930;
+      r[137] = -0.373996265063702;
+      s[137] = -0.561931604429227;
+      w[137] = 0.025102184615930;
 
       break;
     }
     case 27: {
-      r[0]   = -0.333333333333333; s[0]   = -0.333333333333333; w[0]   = 0.029215421142604;
-      r[1]   = -0.029244446609137; s[1]   = -0.029244446609137; w[1]   = 0.013615273717612;
-      r[2]   = -0.941511106781726; s[2]   = -0.029244446609137; w[2]   = 0.013615273717612;
-      r[3]   = -0.029244446609137; s[3]   = -0.941511106781726; w[3]   = 0.013615273717612;
-      r[4]   = -0.132843721814340; s[4]   = -0.132843721814340; w[4]   = 0.030951102870660;
-      r[5]   = -0.734312556371321; s[5]   = -0.132843721814340; w[5]   = 0.030951102870660;
-      r[6]   = -0.132843721814340; s[6]   = -0.734312556371321; w[6]   = 0.030951102870660;
-      r[7]   = -0.224940014502969; s[7]   = -0.224940014502969; w[7]   = 0.031733186724762;
-      r[8]   = -0.550119970994063; s[8]   = -0.224940014502969; w[8]   = 0.031733186724762;
-      r[9]   = -0.224940014502969; s[9]   = -0.550119970994063; w[9]   = 0.031733186724762;
-      r[10]  = -0.427786783949924; s[10]  = -0.427786783949924; w[10]  = 0.031559855928489;
-      r[11]  = -0.144426432100151; s[11]  = -0.427786783949924; w[11]  = 0.031559855928489;
-      r[12]  = -0.427786783949924; s[12]  = -0.144426432100151; w[12]  = 0.031559855928489;
-      r[13]  = -0.532776206162091; s[13]  = -0.532776206162091; w[13]  = 0.027863700370354;
-      r[14]  =  0.065552412324182; s[14]  = -0.532776206162091; w[14]  = 0.027863700370354;
-      r[15]  = -0.532776206162091; s[15]  =  0.065552412324182; w[15]  = 0.027863700370354;
-      r[16]  = -0.690368113175391; s[16]  = -0.690368113175391; w[16]  = 0.019750305737275;
-      r[17]  =  0.380736226350782; s[17]  = -0.690368113175391; w[17]  = 0.019750305737275;
-      r[18]  = -0.690368113175391; s[18]  =  0.380736226350782; w[18]  = 0.019750305737275;
-      r[19]  = -0.781499070170348; s[19]  = -0.781499070170348; w[19]  = 0.015635498945203;
-      r[20]  =  0.562998140340695; s[20]  = -0.781499070170348; w[20]  = 0.015635498945203;
-      r[21]  = -0.781499070170348; s[21]  =  0.562998140340695; w[21]  = 0.015635498945203;
-      r[22]  = -0.862704525220276; s[22]  = -0.862704525220276; w[22]  = 0.010432865446986;
-      r[23]  =  0.725409050440551; s[23]  = -0.862704525220276; w[23]  = 0.010432865446986;
-      r[24]  = -0.862704525220276; s[24]  =  0.725409050440551; w[24]  = 0.010432865446986;
-      r[25]  = -0.932961091535336; s[25]  = -0.932961091535336; w[25]  = 0.005852724472600;
-      r[26]  =  0.865922183070671; s[26]  = -0.932961091535336; w[26]  = 0.005852724472600;
-      r[27]  = -0.932961091535336; s[27]  =  0.865922183070671; w[27]  = 0.005852724472600;
-      r[28]  = -0.986811381964774; s[28]  = -0.986811381964774; w[28]  = 0.001134879007165;
-      r[29]  =  0.973622763929549; s[29]  = -0.986811381964774; w[29]  = 0.001134879007165;
-      r[30]  = -0.986811381964774; s[30]  =  0.973622763929549; w[30]  = 0.001134879007165;
-      r[31]  = -0.717055503863097; s[31]  =  0.716419063026126; w[31]  = 0.001375795459783;
-      r[32]  =  0.716419063026126; s[32]  = -0.717055503863097; w[32]  = 0.001375795459783;
-      r[33]  = -0.999363559163030; s[33]  =  0.716419063026126; w[33]  = 0.001375795459783;
-      r[34]  =  0.716419063026126; s[34]  = -0.999363559163030; w[34]  = 0.001375795459783;
-      r[35]  = -0.999363559163030; s[35]  = -0.717055503863097; w[35]  = 0.001375795459783;
-      r[36]  = -0.717055503863097; s[36]  = -0.999363559163030; w[36]  = 0.001375795459783;
-      r[37]  = -0.838822221132805; s[37]  =  0.827544031058903; w[37]  = 0.003088879415937;
-      r[38]  =  0.827544031058903; s[38]  = -0.838822221132805; w[38]  = 0.003088879415937;
-      r[39]  = -0.988721809926098; s[39]  =  0.827544031058903; w[39]  = 0.003088879415937;
-      r[40]  =  0.827544031058903; s[40]  = -0.988721809926098; w[40]  = 0.003088879415937;
-      r[41]  = -0.988721809926098; s[41]  = -0.838822221132805; w[41]  = 0.003088879415937;
-      r[42]  = -0.838822221132805; s[42]  = -0.988721809926098; w[42]  = 0.003088879415937;
-      r[43]  = -0.537630806497654; s[43]  =  0.526128943172145; w[43]  = 0.005625149324346;
-      r[44]  =  0.526128943172145; s[44]  = -0.537630806497654; w[44]  = 0.005625149324346;
-      r[45]  = -0.988498136674491; s[45]  =  0.526128943172145; w[45]  = 0.005625149324346;
-      r[46]  =  0.526128943172145; s[46]  = -0.988498136674491; w[46]  = 0.005625149324346;
-      r[47]  = -0.988498136674491; s[47]  = -0.537630806497654; w[47]  = 0.005625149324346;
-      r[48]  = -0.537630806497654; s[48]  = -0.988498136674491; w[48]  = 0.005625149324346;
-      r[49]  = -0.113842988120976; s[49]  =  0.103273580134309; w[49]  = 0.005913105372899;
-      r[50]  =  0.103273580134309; s[50]  = -0.113842988120976; w[50]  = 0.005913105372899;
-      r[51]  = -0.989430592013333; s[51]  =  0.103273580134310; w[51]  = 0.005913105372899;
-      r[52]  =  0.103273580134310; s[52]  = -0.989430592013333; w[52]  = 0.005913105372899;
-      r[53]  = -0.989430592013333; s[53]  = -0.113842988120976; w[53]  = 0.005913105372899;
-      r[54]  = -0.113842988120976; s[54]  = -0.989430592013333; w[54]  = 0.005913105372899;
-      r[55]  = -0.330849908839651; s[55]  =  0.320515152715889; w[55]  = 0.005565783438844;
-      r[56]  =  0.320515152715889; s[56]  = -0.330849908839651; w[56]  = 0.005565783438844;
-      r[57]  = -0.989665243876238; s[57]  =  0.320515152715889; w[57]  = 0.005565783438844;
-      r[58]  =  0.320515152715889; s[58]  = -0.989665243876238; w[58]  = 0.005565783438844;
-      r[59]  = -0.989665243876238; s[59]  = -0.330849908839651; w[59]  = 0.005565783438844;
-      r[60]  = -0.330849908839651; s[60]  = -0.989665243876238; w[60]  = 0.005565783438844;
-      r[61]  = -0.931869179489789; s[61]  =  0.919222453867072; w[61]  = 0.002449540456172;
-      r[62]  =  0.919222453867072; s[62]  = -0.931869179489789; w[62]  = 0.002449540456172;
-      r[63]  = -0.987353274377283; s[63]  =  0.919222453867072; w[63]  = 0.002449540456172;
-      r[64]  =  0.919222453867072; s[64]  = -0.987353274377283; w[64]  = 0.002449540456172;
-      r[65]  = -0.987353274377283; s[65]  = -0.931869179489789; w[65]  = 0.002449540456172;
-      r[66]  = -0.931869179489789; s[66]  = -0.987353274377283; w[66]  = 0.002449540456172;
-      r[67]  = -0.695123977280935; s[67]  =  0.663705924287710; w[67]  = 0.007906643758942;
-      r[68]  =  0.663705924287710; s[68]  = -0.695123977280935; w[68]  = 0.007906643758942;
-      r[69]  = -0.968581947006775; s[69]  =  0.663705924287710; w[69]  = 0.007906643758942;
-      r[70]  =  0.663705924287710; s[70]  = -0.968581947006775; w[70]  = 0.007906643758942;
-      r[71]  = -0.968581947006775; s[71]  = -0.695123977280935; w[71]  = 0.007906643758942;
-      r[72]  = -0.695123977280935; s[72]  = -0.968581947006775; w[72]  = 0.007906643758942;
-      r[73]  = -0.831869809255826; s[73]  =  0.777736654895860; w[73]  = 0.007221969465327;
-      r[74]  =  0.777736654895860; s[74]  = -0.831869809255826; w[74]  = 0.007221969465327;
-      r[75]  = -0.945866845640035; s[75]  =  0.777736654895860; w[75]  = 0.007221969465327;
-      r[76]  =  0.777736654895860; s[76]  = -0.945866845640035; w[76]  = 0.007221969465327;
-      r[77]  = -0.945866845640035; s[77]  = -0.831869809255826; w[77]  = 0.007221969465327;
-      r[78]  = -0.831869809255826; s[78]  = -0.945866845640035; w[78]  = 0.007221969465327;
-      r[79]  = -0.423211420319719; s[79]  =  0.374995160760160; w[79]  = 0.008707930088036;
-      r[80]  =  0.374995160760160; s[80]  = -0.423211420319719; w[80]  = 0.008707930088036;
-      r[81]  = -0.951783740440441; s[81]  =  0.374995160760160; w[81]  = 0.008707930088036;
-      r[82]  =  0.374995160760160; s[82]  = -0.951783740440441; w[82]  = 0.008707930088036;
-      r[83]  = -0.951783740440441; s[83]  = -0.423211420319719; w[83]  = 0.008707930088036;
-      r[84]  = -0.423211420319719; s[84]  = -0.951783740440441; w[84]  = 0.008707930088036;
-      r[85]  = -0.223962554104902; s[85]  =  0.171509638849087; w[85]  = 0.011256464740666;
-      r[86]  =  0.171509638849087; s[86]  = -0.223962554104902; w[86]  = 0.011256464740666;
-      r[87]  = -0.947547084744185; s[87]  =  0.171509638849087; w[87]  = 0.011256464740666;
-      r[88]  =  0.171509638849087; s[88]  = -0.947547084744185; w[88]  = 0.011256464740666;
-      r[89]  = -0.947547084744185; s[89]  = -0.223962554104902; w[89]  = 0.011256464740666;
-      r[90]  = -0.223962554104902; s[90]  = -0.947547084744185; w[90]  = 0.011256464740666;
-      r[91]  = -0.566926820194262; s[91]  =  0.490923426439871; w[91]  = 0.013269437724243;
-      r[92]  =  0.490923426439871; s[92]  = -0.566926820194262; w[92]  = 0.013269437724243;
-      r[93]  = -0.923996606245609; s[93]  =  0.490923426439871; w[93]  = 0.013269437724243;
-      r[94]  =  0.490923426439871; s[94]  = -0.923996606245609; w[94]  = 0.013269437724243;
-      r[95]  = -0.923996606245609; s[95]  = -0.566926820194262; w[95]  = 0.013269437724243;
-      r[96]  = -0.566926820194262; s[96]  = -0.923996606245609; w[96]  = 0.013269437724243;
-      r[97]  = -0.350787336349322; s[97]  =  0.245677528944182; w[97]  = 0.013046146795576;
-      r[98]  =  0.245677528944182; s[98]  = -0.350787336349322; w[98]  = 0.013046146795576;
-      r[99]  = -0.894890192594860; s[99]  =  0.245677528944182; w[99]  = 0.013046146795576;
-      r[100] =  0.245677528944182; s[100] = -0.894890192594860; w[100] = 0.013046146795576;
-      r[101] = -0.894890192594860; s[101] = -0.350787336349322; w[101] = 0.013046146795576;
-      r[102] = -0.350787336349322; s[102] = -0.894890192594860; w[102] = 0.013046146795576;
-      r[103] = -0.729613610936203; s[103] =  0.622255871516285; w[103] = 0.012947418329903;
-      r[104] =  0.622255871516285; s[104] = -0.729613610936203; w[104] = 0.012947418329903;
-      r[105] = -0.892642260580081; s[105] =  0.622255871516285; w[105] = 0.012947418329903;
-      r[106] =  0.622255871516285; s[106] = -0.892642260580081; w[106] = 0.012947418329903;
-      r[107] = -0.892642260580081; s[107] = -0.729613610936203; w[107] = 0.012947418329903;
-      r[108] = -0.729613610936203; s[108] = -0.892642260580081; w[108] = 0.012947418329903;
-      r[109] = -0.176209680235251; s[109] =  0.035410146457445; w[109] = 0.021313811627966;
-      r[110] =  0.035410146457445; s[110] = -0.176209680235251; w[110] = 0.021313811627966;
-      r[111] = -0.859200466222194; s[111] =  0.035410146457445; w[111] = 0.021313811627966;
-      r[112] =  0.035410146457445; s[112] = -0.859200466222194; w[112] = 0.021313811627966;
-      r[113] = -0.859200466222194; s[113] = -0.176209680235251; w[113] = 0.021313811627966;
-      r[114] = -0.176209680235251; s[114] = -0.859200466222194; w[114] = 0.021313811627966;
-      r[115] = -0.469171656648510; s[115] =  0.304686011244002; w[115] = 0.017176891528936;
-      r[116] =  0.304686011244002; s[116] = -0.469171656648510; w[116] = 0.017176891528936;
-      r[117] = -0.835514354595492; s[117] =  0.304686011244002; w[117] = 0.017176891528936;
-      r[118] =  0.304686011244002; s[118] = -0.835514354595492; w[118] = 0.017176891528936;
-      r[119] = -0.835514354595492; s[119] = -0.469171656648510; w[119] = 0.017176891528936;
-      r[120] = -0.469171656648510; s[120] = -0.835514354595492; w[120] = 0.017176891528936;
-      r[121] = -0.623736093891471; s[121] =  0.443479545725970; w[121] = 0.017763399981969;
-      r[122] =  0.443479545725970; s[122] = -0.623736093891471; w[122] = 0.017763399981969;
-      r[123] = -0.819743451834499; s[123] =  0.443479545725970; w[123] = 0.017763399981969;
-      r[124] =  0.443479545725970; s[124] = -0.819743451834499; w[124] = 0.017763399981969;
-      r[125] = -0.819743451834499; s[125] = -0.623736093891471; w[125] = 0.017763399981969;
-      r[126] = -0.623736093891471; s[126] = -0.819743451834499; w[126] = 0.017763399981969;
-      r[127] = -0.336632062394500; s[127] =  0.104847567508036; w[127] = 0.023828398561090;
-      r[128] =  0.104847567508036; s[128] = -0.336632062394500; w[128] = 0.023828398561090;
-      r[129] = -0.768215505113536; s[129] =  0.104847567508036; w[129] = 0.023828398561090;
-      r[130] =  0.104847567508036; s[130] = -0.768215505113536; w[130] = 0.023828398561090;
-      r[131] = -0.768215505113536; s[131] = -0.336632062394500; w[131] = 0.023828398561090;
-      r[132] = -0.336632062394500; s[132] = -0.768215505113536; w[132] = 0.023828398561090;
-      r[133] = -0.530404689974552; s[133] =  0.224195004863778; w[133] = 0.026764788789016;
-      r[134] =  0.224195004863778; s[134] = -0.530404689974552; w[134] = 0.026764788789016;
-      r[135] = -0.693790314889227; s[135] =  0.224195004863778; w[135] = 0.026764788789016;
-      r[136] =  0.224195004863778; s[136] = -0.693790314889227; w[136] = 0.026764788789016;
-      r[137] = -0.693790314889227; s[137] = -0.530404689974552; w[137] = 0.026764788789016;
-      r[138] = -0.530404689974552; s[138] = -0.693790314889227; w[138] = 0.026764788789016;
-      r[139] = -0.350831684137242; s[139] = -0.019508133770036; w[139] = 0.028977845006028;
-      r[140] = -0.019508133770036; s[140] = -0.350831684137242; w[140] = 0.028977845006028;
-      r[141] = -0.629660182092722; s[141] = -0.019508133770036; w[141] = 0.028977845006028;
-      r[142] = -0.019508133770036; s[142] = -0.629660182092722; w[142] = 0.028977845006028;
-      r[143] = -0.629660182092722; s[143] = -0.350831684137242; w[143] = 0.028977845006028;
-      r[144] = -0.350831684137242; s[144] = -0.629660182092722; w[144] = 0.028977845006028;
+      r[0] = -0.333333333333333;
+      s[0] = -0.333333333333333;
+      w[0] = 0.029215421142604;
+      r[1] = -0.029244446609137;
+      s[1] = -0.029244446609137;
+      w[1] = 0.013615273717612;
+      r[2] = -0.941511106781726;
+      s[2] = -0.029244446609137;
+      w[2] = 0.013615273717612;
+      r[3] = -0.029244446609137;
+      s[3] = -0.941511106781726;
+      w[3] = 0.013615273717612;
+      r[4] = -0.132843721814340;
+      s[4] = -0.132843721814340;
+      w[4] = 0.030951102870660;
+      r[5] = -0.734312556371321;
+      s[5] = -0.132843721814340;
+      w[5] = 0.030951102870660;
+      r[6] = -0.132843721814340;
+      s[6] = -0.734312556371321;
+      w[6] = 0.030951102870660;
+      r[7] = -0.224940014502969;
+      s[7] = -0.224940014502969;
+      w[7] = 0.031733186724762;
+      r[8] = -0.550119970994063;
+      s[8] = -0.224940014502969;
+      w[8] = 0.031733186724762;
+      r[9] = -0.224940014502969;
+      s[9] = -0.550119970994063;
+      w[9] = 0.031733186724762;
+      r[10] = -0.427786783949924;
+      s[10] = -0.427786783949924;
+      w[10] = 0.031559855928489;
+      r[11] = -0.144426432100151;
+      s[11] = -0.427786783949924;
+      w[11] = 0.031559855928489;
+      r[12] = -0.427786783949924;
+      s[12] = -0.144426432100151;
+      w[12] = 0.031559855928489;
+      r[13] = -0.532776206162091;
+      s[13] = -0.532776206162091;
+      w[13] = 0.027863700370354;
+      r[14] = 0.065552412324182;
+      s[14] = -0.532776206162091;
+      w[14] = 0.027863700370354;
+      r[15] = -0.532776206162091;
+      s[15] = 0.065552412324182;
+      w[15] = 0.027863700370354;
+      r[16] = -0.690368113175391;
+      s[16] = -0.690368113175391;
+      w[16] = 0.019750305737275;
+      r[17] = 0.380736226350782;
+      s[17] = -0.690368113175391;
+      w[17] = 0.019750305737275;
+      r[18] = -0.690368113175391;
+      s[18] = 0.380736226350782;
+      w[18] = 0.019750305737275;
+      r[19] = -0.781499070170348;
+      s[19] = -0.781499070170348;
+      w[19] = 0.015635498945203;
+      r[20] = 0.562998140340695;
+      s[20] = -0.781499070170348;
+      w[20] = 0.015635498945203;
+      r[21] = -0.781499070170348;
+      s[21] = 0.562998140340695;
+      w[21] = 0.015635498945203;
+      r[22] = -0.862704525220276;
+      s[22] = -0.862704525220276;
+      w[22] = 0.010432865446986;
+      r[23] = 0.725409050440551;
+      s[23] = -0.862704525220276;
+      w[23] = 0.010432865446986;
+      r[24] = -0.862704525220276;
+      s[24] = 0.725409050440551;
+      w[24] = 0.010432865446986;
+      r[25] = -0.932961091535336;
+      s[25] = -0.932961091535336;
+      w[25] = 0.005852724472600;
+      r[26] = 0.865922183070671;
+      s[26] = -0.932961091535336;
+      w[26] = 0.005852724472600;
+      r[27] = -0.932961091535336;
+      s[27] = 0.865922183070671;
+      w[27] = 0.005852724472600;
+      r[28] = -0.986811381964774;
+      s[28] = -0.986811381964774;
+      w[28] = 0.001134879007165;
+      r[29] = 0.973622763929549;
+      s[29] = -0.986811381964774;
+      w[29] = 0.001134879007165;
+      r[30] = -0.986811381964774;
+      s[30] = 0.973622763929549;
+      w[30] = 0.001134879007165;
+      r[31] = -0.717055503863097;
+      s[31] = 0.716419063026126;
+      w[31] = 0.001375795459783;
+      r[32] = 0.716419063026126;
+      s[32] = -0.717055503863097;
+      w[32] = 0.001375795459783;
+      r[33] = -0.999363559163030;
+      s[33] = 0.716419063026126;
+      w[33] = 0.001375795459783;
+      r[34] = 0.716419063026126;
+      s[34] = -0.999363559163030;
+      w[34] = 0.001375795459783;
+      r[35] = -0.999363559163030;
+      s[35] = -0.717055503863097;
+      w[35] = 0.001375795459783;
+      r[36] = -0.717055503863097;
+      s[36] = -0.999363559163030;
+      w[36] = 0.001375795459783;
+      r[37] = -0.838822221132805;
+      s[37] = 0.827544031058903;
+      w[37] = 0.003088879415937;
+      r[38] = 0.827544031058903;
+      s[38] = -0.838822221132805;
+      w[38] = 0.003088879415937;
+      r[39] = -0.988721809926098;
+      s[39] = 0.827544031058903;
+      w[39] = 0.003088879415937;
+      r[40] = 0.827544031058903;
+      s[40] = -0.988721809926098;
+      w[40] = 0.003088879415937;
+      r[41] = -0.988721809926098;
+      s[41] = -0.838822221132805;
+      w[41] = 0.003088879415937;
+      r[42] = -0.838822221132805;
+      s[42] = -0.988721809926098;
+      w[42] = 0.003088879415937;
+      r[43] = -0.537630806497654;
+      s[43] = 0.526128943172145;
+      w[43] = 0.005625149324346;
+      r[44] = 0.526128943172145;
+      s[44] = -0.537630806497654;
+      w[44] = 0.005625149324346;
+      r[45] = -0.988498136674491;
+      s[45] = 0.526128943172145;
+      w[45] = 0.005625149324346;
+      r[46] = 0.526128943172145;
+      s[46] = -0.988498136674491;
+      w[46] = 0.005625149324346;
+      r[47] = -0.988498136674491;
+      s[47] = -0.537630806497654;
+      w[47] = 0.005625149324346;
+      r[48] = -0.537630806497654;
+      s[48] = -0.988498136674491;
+      w[48] = 0.005625149324346;
+      r[49] = -0.113842988120976;
+      s[49] = 0.103273580134309;
+      w[49] = 0.005913105372899;
+      r[50] = 0.103273580134309;
+      s[50] = -0.113842988120976;
+      w[50] = 0.005913105372899;
+      r[51] = -0.989430592013333;
+      s[51] = 0.103273580134310;
+      w[51] = 0.005913105372899;
+      r[52] = 0.103273580134310;
+      s[52] = -0.989430592013333;
+      w[52] = 0.005913105372899;
+      r[53] = -0.989430592013333;
+      s[53] = -0.113842988120976;
+      w[53] = 0.005913105372899;
+      r[54] = -0.113842988120976;
+      s[54] = -0.989430592013333;
+      w[54] = 0.005913105372899;
+      r[55] = -0.330849908839651;
+      s[55] = 0.320515152715889;
+      w[55] = 0.005565783438844;
+      r[56] = 0.320515152715889;
+      s[56] = -0.330849908839651;
+      w[56] = 0.005565783438844;
+      r[57] = -0.989665243876238;
+      s[57] = 0.320515152715889;
+      w[57] = 0.005565783438844;
+      r[58] = 0.320515152715889;
+      s[58] = -0.989665243876238;
+      w[58] = 0.005565783438844;
+      r[59] = -0.989665243876238;
+      s[59] = -0.330849908839651;
+      w[59] = 0.005565783438844;
+      r[60] = -0.330849908839651;
+      s[60] = -0.989665243876238;
+      w[60] = 0.005565783438844;
+      r[61] = -0.931869179489789;
+      s[61] = 0.919222453867072;
+      w[61] = 0.002449540456172;
+      r[62] = 0.919222453867072;
+      s[62] = -0.931869179489789;
+      w[62] = 0.002449540456172;
+      r[63] = -0.987353274377283;
+      s[63] = 0.919222453867072;
+      w[63] = 0.002449540456172;
+      r[64] = 0.919222453867072;
+      s[64] = -0.987353274377283;
+      w[64] = 0.002449540456172;
+      r[65] = -0.987353274377283;
+      s[65] = -0.931869179489789;
+      w[65] = 0.002449540456172;
+      r[66] = -0.931869179489789;
+      s[66] = -0.987353274377283;
+      w[66] = 0.002449540456172;
+      r[67] = -0.695123977280935;
+      s[67] = 0.663705924287710;
+      w[67] = 0.007906643758942;
+      r[68] = 0.663705924287710;
+      s[68] = -0.695123977280935;
+      w[68] = 0.007906643758942;
+      r[69] = -0.968581947006775;
+      s[69] = 0.663705924287710;
+      w[69] = 0.007906643758942;
+      r[70] = 0.663705924287710;
+      s[70] = -0.968581947006775;
+      w[70] = 0.007906643758942;
+      r[71] = -0.968581947006775;
+      s[71] = -0.695123977280935;
+      w[71] = 0.007906643758942;
+      r[72] = -0.695123977280935;
+      s[72] = -0.968581947006775;
+      w[72] = 0.007906643758942;
+      r[73] = -0.831869809255826;
+      s[73] = 0.777736654895860;
+      w[73] = 0.007221969465327;
+      r[74] = 0.777736654895860;
+      s[74] = -0.831869809255826;
+      w[74] = 0.007221969465327;
+      r[75] = -0.945866845640035;
+      s[75] = 0.777736654895860;
+      w[75] = 0.007221969465327;
+      r[76] = 0.777736654895860;
+      s[76] = -0.945866845640035;
+      w[76] = 0.007221969465327;
+      r[77] = -0.945866845640035;
+      s[77] = -0.831869809255826;
+      w[77] = 0.007221969465327;
+      r[78] = -0.831869809255826;
+      s[78] = -0.945866845640035;
+      w[78] = 0.007221969465327;
+      r[79] = -0.423211420319719;
+      s[79] = 0.374995160760160;
+      w[79] = 0.008707930088036;
+      r[80] = 0.374995160760160;
+      s[80] = -0.423211420319719;
+      w[80] = 0.008707930088036;
+      r[81] = -0.951783740440441;
+      s[81] = 0.374995160760160;
+      w[81] = 0.008707930088036;
+      r[82] = 0.374995160760160;
+      s[82] = -0.951783740440441;
+      w[82] = 0.008707930088036;
+      r[83] = -0.951783740440441;
+      s[83] = -0.423211420319719;
+      w[83] = 0.008707930088036;
+      r[84] = -0.423211420319719;
+      s[84] = -0.951783740440441;
+      w[84] = 0.008707930088036;
+      r[85] = -0.223962554104902;
+      s[85] = 0.171509638849087;
+      w[85] = 0.011256464740666;
+      r[86] = 0.171509638849087;
+      s[86] = -0.223962554104902;
+      w[86] = 0.011256464740666;
+      r[87] = -0.947547084744185;
+      s[87] = 0.171509638849087;
+      w[87] = 0.011256464740666;
+      r[88] = 0.171509638849087;
+      s[88] = -0.947547084744185;
+      w[88] = 0.011256464740666;
+      r[89] = -0.947547084744185;
+      s[89] = -0.223962554104902;
+      w[89] = 0.011256464740666;
+      r[90] = -0.223962554104902;
+      s[90] = -0.947547084744185;
+      w[90] = 0.011256464740666;
+      r[91] = -0.566926820194262;
+      s[91] = 0.490923426439871;
+      w[91] = 0.013269437724243;
+      r[92] = 0.490923426439871;
+      s[92] = -0.566926820194262;
+      w[92] = 0.013269437724243;
+      r[93] = -0.923996606245609;
+      s[93] = 0.490923426439871;
+      w[93] = 0.013269437724243;
+      r[94] = 0.490923426439871;
+      s[94] = -0.923996606245609;
+      w[94] = 0.013269437724243;
+      r[95] = -0.923996606245609;
+      s[95] = -0.566926820194262;
+      w[95] = 0.013269437724243;
+      r[96] = -0.566926820194262;
+      s[96] = -0.923996606245609;
+      w[96] = 0.013269437724243;
+      r[97] = -0.350787336349322;
+      s[97] = 0.245677528944182;
+      w[97] = 0.013046146795576;
+      r[98] = 0.245677528944182;
+      s[98] = -0.350787336349322;
+      w[98] = 0.013046146795576;
+      r[99] = -0.894890192594860;
+      s[99] = 0.245677528944182;
+      w[99] = 0.013046146795576;
+      r[100] = 0.245677528944182;
+      s[100] = -0.894890192594860;
+      w[100] = 0.013046146795576;
+      r[101] = -0.894890192594860;
+      s[101] = -0.350787336349322;
+      w[101] = 0.013046146795576;
+      r[102] = -0.350787336349322;
+      s[102] = -0.894890192594860;
+      w[102] = 0.013046146795576;
+      r[103] = -0.729613610936203;
+      s[103] = 0.622255871516285;
+      w[103] = 0.012947418329903;
+      r[104] = 0.622255871516285;
+      s[104] = -0.729613610936203;
+      w[104] = 0.012947418329903;
+      r[105] = -0.892642260580081;
+      s[105] = 0.622255871516285;
+      w[105] = 0.012947418329903;
+      r[106] = 0.622255871516285;
+      s[106] = -0.892642260580081;
+      w[106] = 0.012947418329903;
+      r[107] = -0.892642260580081;
+      s[107] = -0.729613610936203;
+      w[107] = 0.012947418329903;
+      r[108] = -0.729613610936203;
+      s[108] = -0.892642260580081;
+      w[108] = 0.012947418329903;
+      r[109] = -0.176209680235251;
+      s[109] = 0.035410146457445;
+      w[109] = 0.021313811627966;
+      r[110] = 0.035410146457445;
+      s[110] = -0.176209680235251;
+      w[110] = 0.021313811627966;
+      r[111] = -0.859200466222194;
+      s[111] = 0.035410146457445;
+      w[111] = 0.021313811627966;
+      r[112] = 0.035410146457445;
+      s[112] = -0.859200466222194;
+      w[112] = 0.021313811627966;
+      r[113] = -0.859200466222194;
+      s[113] = -0.176209680235251;
+      w[113] = 0.021313811627966;
+      r[114] = -0.176209680235251;
+      s[114] = -0.859200466222194;
+      w[114] = 0.021313811627966;
+      r[115] = -0.469171656648510;
+      s[115] = 0.304686011244002;
+      w[115] = 0.017176891528936;
+      r[116] = 0.304686011244002;
+      s[116] = -0.469171656648510;
+      w[116] = 0.017176891528936;
+      r[117] = -0.835514354595492;
+      s[117] = 0.304686011244002;
+      w[117] = 0.017176891528936;
+      r[118] = 0.304686011244002;
+      s[118] = -0.835514354595492;
+      w[118] = 0.017176891528936;
+      r[119] = -0.835514354595492;
+      s[119] = -0.469171656648510;
+      w[119] = 0.017176891528936;
+      r[120] = -0.469171656648510;
+      s[120] = -0.835514354595492;
+      w[120] = 0.017176891528936;
+      r[121] = -0.623736093891471;
+      s[121] = 0.443479545725970;
+      w[121] = 0.017763399981969;
+      r[122] = 0.443479545725970;
+      s[122] = -0.623736093891471;
+      w[122] = 0.017763399981969;
+      r[123] = -0.819743451834499;
+      s[123] = 0.443479545725970;
+      w[123] = 0.017763399981969;
+      r[124] = 0.443479545725970;
+      s[124] = -0.819743451834499;
+      w[124] = 0.017763399981969;
+      r[125] = -0.819743451834499;
+      s[125] = -0.623736093891471;
+      w[125] = 0.017763399981969;
+      r[126] = -0.623736093891471;
+      s[126] = -0.819743451834499;
+      w[126] = 0.017763399981969;
+      r[127] = -0.336632062394500;
+      s[127] = 0.104847567508036;
+      w[127] = 0.023828398561090;
+      r[128] = 0.104847567508036;
+      s[128] = -0.336632062394500;
+      w[128] = 0.023828398561090;
+      r[129] = -0.768215505113536;
+      s[129] = 0.104847567508036;
+      w[129] = 0.023828398561090;
+      r[130] = 0.104847567508036;
+      s[130] = -0.768215505113536;
+      w[130] = 0.023828398561090;
+      r[131] = -0.768215505113536;
+      s[131] = -0.336632062394500;
+      w[131] = 0.023828398561090;
+      r[132] = -0.336632062394500;
+      s[132] = -0.768215505113536;
+      w[132] = 0.023828398561090;
+      r[133] = -0.530404689974552;
+      s[133] = 0.224195004863778;
+      w[133] = 0.026764788789016;
+      r[134] = 0.224195004863778;
+      s[134] = -0.530404689974552;
+      w[134] = 0.026764788789016;
+      r[135] = -0.693790314889227;
+      s[135] = 0.224195004863778;
+      w[135] = 0.026764788789016;
+      r[136] = 0.224195004863778;
+      s[136] = -0.693790314889227;
+      w[136] = 0.026764788789016;
+      r[137] = -0.693790314889227;
+      s[137] = -0.530404689974552;
+      w[137] = 0.026764788789016;
+      r[138] = -0.530404689974552;
+      s[138] = -0.693790314889227;
+      w[138] = 0.026764788789016;
+      r[139] = -0.350831684137242;
+      s[139] = -0.019508133770036;
+      w[139] = 0.028977845006028;
+      r[140] = -0.019508133770036;
+      s[140] = -0.350831684137242;
+      w[140] = 0.028977845006028;
+      r[141] = -0.629660182092722;
+      s[141] = -0.019508133770036;
+      w[141] = 0.028977845006028;
+      r[142] = -0.019508133770036;
+      s[142] = -0.629660182092722;
+      w[142] = 0.028977845006028;
+      r[143] = -0.629660182092722;
+      s[143] = -0.350831684137242;
+      w[143] = 0.028977845006028;
+      r[144] = -0.350831684137242;
+      s[144] = -0.629660182092722;
+      w[144] = 0.028977845006028;
 
       break;
     }
     case 28: {
-      r[0]   = -0.988064607832230; s[0]   =  0.987992518020485; w[0]   = 0.000005678109445;
-      r[1]   = -0.937649986705898; s[1]   =  0.937273392400706; w[1]   = 0.000067869690329;
-      r[2]   = -0.849117911767581; s[2]   =  0.848206583410427; w[2]   = 0.000250117104238;
-      r[3]   = -0.726072255922453; s[3]   =  0.724417731360170; w[3]   = 0.000591434111178;
-      r[4]   = -0.573547944561595; s[4]   =  0.570972172608539; w[4]   = 0.001096877668021;
-      r[5]   = -0.397788705468703; s[5]   =  0.394151347077563; w[5]   = 0.001734258212849;
-      r[6]   = -0.205989917758162; s[6]   =  0.201194093997435; w[6]   = 0.002437321168702;
-      r[7]   = -0.006003740989757; s[7]   =  0.000000000000000; w[7]   = 0.003114968848543;
-      r[8]   =  0.193982435778648; s[8]   = -0.201194093997435; w[8]   = 0.003665090319212;
-      r[9]   =  0.385781223489189; s[9]   = -0.394151347077563; w[9]   = 0.003990796070869;
-      r[10]  =  0.561540462582081; s[10]  = -0.570972172608539; w[10]  = 0.004016439454972;
-      r[11]  =  0.714064773942939; s[11]  = -0.724417731360170; w[11]  = 0.003700816722647;
-      r[12]  =  0.837110429788067; s[12]  = -0.848206583410427; w[12]  = 0.003045376334904;
-      r[13]  =  0.925642504726384; s[13]  = -0.937273392400706; w[13]  = 0.002096114396383;
-      r[14]  =  0.976057125852715; s[14]  = -0.987992518020485; w[14]  = 0.000940083783827;
-      r[15]  = -0.988369112325678; s[15]  =  0.987992518020485; w[15]  = 0.000012991999963;
-      r[16]  = -0.939240706051164; s[16]  =  0.937273392400706; w[16]  = 0.000155291655212;
-      r[17]  = -0.852967326449712; s[17]  =  0.848206583410427; w[17]  = 0.000572289322752;
-      r[18]  = -0.733060901773317; s[18]  =  0.724417731360170; w[18]  = 0.001353251821662;
-      r[19]  = -0.584427902697520; s[19]  =  0.570972172608539; w[19]  = 0.002509749901695;
-      r[20]  = -0.413152762435777; s[20]  =  0.394151347077563; w[20]  = 0.003968131092565;
-      r[21]  = -0.226247286304345; s[21]  =  0.201194093997435; w[21]  = 0.005576799256556;
-      r[22]  = -0.031363303799647; s[22]  =  0.000000000000000; w[22]  = 0.007127315095696;
-      r[23]  =  0.163520678705051; s[23]  = -0.201194093997435; w[23]  = 0.008386040063107;
-      r[24]  =  0.350426154836483; s[24]  = -0.394151347077563; w[24]  = 0.009131282674963;
-      r[25]  =  0.521701295098226; s[25]  = -0.570972172608539; w[25]  = 0.009189956930633;
-      r[26]  =  0.670334294174023; s[26]  = -0.724417731360170; w[26]  = 0.008467785129237;
-      r[27]  =  0.790240718850418; s[27]  = -0.848206583410427; w[27]  = 0.006968081473429;
-      r[28]  =  0.876514098451870; s[28]  = -0.937273392400706; w[28]  = 0.004796088983887;
-      r[29]  =  0.925642504726384; s[29]  = -0.987992518020485; w[29]  = 0.002150992086750;
-      r[30]  = -0.988903846377640; s[30]  =  0.987992518020485; w[30]  = 0.000019785289042;
-      r[31]  = -0.942034135439991; s[31]  =  0.937273392400706; w[31]  = 0.000236490940043;
-      r[32]  = -0.859727204070395; s[32]  =  0.848206583410427; w[32]  = 0.000871529379538;
-      r[33]  = -0.745333518414343; s[33]  =  0.724417731360170; w[33]  = 0.002060843481789;
-      r[34]  = -0.603533972474414; s[34]  =  0.570972172608539; w[34]  = 0.003822054138805;
-      r[35]  = -0.440133265559207; s[35]  =  0.394151347077563; w[35]  = 0.006042997294437;
-      r[36]  = -0.261820832829464; s[36]  =  0.201194093997435; w[36]  = 0.008492809847469;
-      r[37]  = -0.075896708294786; s[37]  =  0.000000000000000; w[37]  = 0.010854063244177;
-      r[38]  =  0.110027416239891; s[38]  = -0.201194093997435; w[38]  = 0.012770953436328;
-      r[39]  =  0.288339848969634; s[39]  = -0.394151347077563; w[39]  = 0.013905870348620;
-      r[40]  =  0.451740555884842; s[40]  = -0.570972172608539; w[40]  = 0.013995224344240;
-      r[41]  =  0.593540101824770; s[41]  = -0.724417731360170; w[41]  = 0.012895441564853;
-      r[42]  =  0.707933787480822; s[42]  = -0.848206583410427; w[42]  = 0.010611569151594;
-      r[43]  =  0.790240718850418; s[43]  = -0.937273392400706; w[43]  = 0.007303879856139;
-      r[44]  =  0.837110429788067; s[44]  = -0.987992518020485; w[44]  = 0.003275708150100;
-      r[45]  = -0.989647042582769; s[45]  =  0.987992518020485; w[45]  = 0.000025769562269;
-      r[46]  = -0.945916562813853; s[46]  =  0.937273392400706; w[46]  = 0.000308020165519;
-      r[47]  = -0.869122370464600; s[47]  =  0.848206583410427; w[47]  = 0.001135132803359;
-      r[48]  = -0.762390524754508; s[48]  =  0.724417731360170; w[48]  = 0.002684167732828;
-      r[49]  = -0.630088403599617; s[49]  =  0.570972172608539; w[49]  = 0.004978075474027;
-      r[50]  = -0.477631920189938; s[50]  =  0.394151347077563; w[50]  = 0.007870766747028;
-      r[51]  = -0.311262465886975; s[51]  =  0.201194093997435; w[51]  = 0.011061551425453;
-      r[52]  = -0.137791134319915; s[52]  =  0.000000000000000; w[52]  = 0.014136991279319;
-      r[53]  =  0.035680197247145; s[53]  = -0.201194093997435; w[53]  = 0.016633665503545;
-      r[54]  =  0.202049651550108; s[54]  = -0.394151347077563; w[54]  = 0.018111850228555;
-      r[55]  =  0.354506134959787; s[55]  = -0.570972172608539; w[55]  = 0.018228230300094;
-      r[56]  =  0.486808256114678; s[56]  = -0.724417731360170; w[56]  = 0.016795806403939;
-      r[57]  =  0.593540101824770; s[57]  = -0.848206583410427; w[57]  = 0.013821152243283;
-      r[58]  =  0.670334294174023; s[58]  = -0.937273392400706; w[58]  = 0.009513016785380;
-      r[59]  =  0.714064773942939; s[59]  = -0.987992518020485; w[59]  = 0.004266481271556;
-      r[60]  = -0.990568289973542; s[60]  =  0.987992518020485; w[60]  = 0.000030699031605;
-      r[61]  = -0.950729122489687; s[61]  =  0.937273392400706; w[61]  = 0.000366941459749;
-      r[62]  = -0.880768383276303; s[62]  =  0.848206583410427; w[62]  = 0.001352272787635;
-      r[63]  = -0.783533962351248; s[63]  =  0.724417731360170; w[63]  = 0.003197623195991;
-      r[64]  = -0.663004610946658; s[64]  =  0.570972172608539; w[64]  = 0.005930333418609;
-      r[65]  = -0.524114312723242; s[65]  =  0.394151347077563; w[65]  = 0.009376368701824;
-      r[66]  = -0.372549075177309; s[66]  =  0.201194093997435; w[66]  = 0.013177519790991;
-      r[67]  = -0.214513913695731; s[67]  =  0.000000000000000; w[67]  = 0.016841261700383;
-      r[68]  = -0.056478752214152; s[68]  = -0.201194093997435; w[68]  = 0.019815525683434;
-      r[69]  =  0.095086485331781; s[69]  = -0.394151347077563; w[69]  = 0.021576472924861;
-      r[70]  =  0.233976783555196; s[70]  = -0.570972172608539; w[70]  = 0.021715115384404;
-      r[71]  =  0.354506134959787; s[71]  = -0.724417731360170; w[71]  = 0.020008682578130;
-      r[72]  =  0.451740555884842; s[72]  = -0.848206583410427; w[72]  = 0.016465005695410;
-      r[73]  =  0.521701295098226; s[73]  = -0.937273392400706; w[73]  = 0.011332765372579;
-      r[74]  =  0.561540462582081; s[74]  = -0.987992518020485; w[74]  = 0.005082618091388;
-      r[75]  = -0.991629876411625; s[75]  =  0.987992518020485; w[75]  = 0.000034371743072;
-      r[76]  = -0.956274807758919; s[76]  =  0.937273392400706; w[76]  = 0.000410840893588;
-      r[77]  = -0.894188501892071; s[77]  =  0.848206583410427; w[77]  = 0.001514053388316;
-      r[78]  = -0.807898304472545; s[78]  =  0.724417731360170; w[78]  = 0.003580174265665;
-      r[79]  = -0.700935138254217; s[79]  =  0.570972172608539; w[79]  = 0.006639815197344;
-      r[80]  = -0.577677642201529; s[80]  =  0.394151347077563; w[80]  = 0.010498120595869;
-      r[81]  = -0.443171835046505; s[81]  =  0.201194093997435; w[81]  = 0.014754026459451;
-      r[82]  = -0.302924326461218; s[82]  =  0.000000000000000; w[82]  = 0.018856084049129;
-      r[83]  = -0.162676817875932; s[83]  = -0.201194093997435; w[83]  = 0.022186177283618;
-      r[84]  = -0.028171010720908; s[84]  = -0.394151347077563; w[84]  = 0.024157797330925;
-      r[85]  =  0.095086485331781; s[85]  = -0.570972172608539; w[85]  = 0.024313026429341;
-      r[86]  =  0.202049651550108; s[86]  = -0.724417731360170; w[86]  = 0.022402442709917;
-      r[87]  =  0.288339848969634; s[87]  = -0.848206583410427; w[87]  = 0.018434814254740;
-      r[88]  =  0.350426154836483; s[88]  = -0.937273392400706; w[88]  = 0.012688572873940;
-      r[89]  =  0.385781223489189; s[89]  = -0.987992518020485; w[89]  = 0.005690682540646;
-      r[90]  = -0.992788341781213; s[90]  =  0.987992518020485; w[90]  = 0.000036637297986;
-      r[91]  = -0.962326584707617; s[91]  =  0.937273392400706; w[91]  = 0.000437920771488;
-      r[92]  = -0.908833322242456; s[92]  =  0.848206583410427; w[92]  = 0.001613849639200;
-      r[93]  = -0.834486103249711; s[93]  =  0.724417731360170; w[93]  = 0.003816155355883;
-      r[94]  = -0.742327153788413; s[94]  =  0.570972172608539; w[94]  = 0.007077467309460;
-      r[95]  = -0.636129088126634; s[95]  =  0.394151347077563; w[95]  = 0.011190086338209;
-      r[96]  = -0.520239531729724; s[96]  =  0.201194093997435; w[96]  = 0.015726512989614;
-      r[97]  = -0.399402953001283; s[97]  =  0.000000000000000; w[97]  = 0.020098950720122;
-      r[98]  = -0.278566374272841; s[98]  = -0.201194093997435; w[98]  = 0.023648541379510;
-      r[99]  = -0.162676817875932; s[99]  = -0.394151347077563; w[99]  = 0.025750117404859;
-      r[100] = -0.056478752214152; s[100] = -0.570972172608539; w[100] = 0.025915578164965;
-      r[101] =  0.035680197247145; s[101] = -0.724417731360170; w[101] = 0.023879061573116;
-      r[102] =  0.110027416239891; s[102] = -0.848206583410427; w[102] = 0.019649913644597;
-      r[103] =  0.163520678705051; s[103] = -0.937273392400706; w[103] = 0.013524918548175;
-      r[104] =  0.193982435778648; s[104] = -0.987992518020485; w[104] = 0.006065774189928;
-      r[105] = -0.993996259010243; s[105] =  0.987992518020485; w[105] = 0.000037402932316;
-      r[106] = -0.968636696200353; s[106] =  0.937273392400706; w[106] = 0.000447072297244;
-      r[107] = -0.924103291705214; s[107] =  0.848206583410427; w[107] = 0.001647575343713;
-      r[108] = -0.862208865680085; s[108] =  0.724417731360170; w[108] = 0.003895904128496;
-      r[109] = -0.785486086304269; s[109] =  0.570972172608539; w[109] = 0.007225369917846;
-      r[110] = -0.697075673538782; s[110] =  0.394151347077563; w[110] = 0.011423933120557;
-      r[111] = -0.600597046998717; s[111] =  0.201194093997435; w[111] = 0.016055160539688;
-      r[112] = -0.500000000000000; s[112] =  0.000000000000000; w[112] = 0.020518972050826;
-      r[113] = -0.399402953001283; s[113] = -0.201194093997435; w[113] = 0.024142740900556;
-      r[114] = -0.302924326461218; s[114] = -0.394151347077563; w[114] = 0.026288234977700;
-      r[115] = -0.214513913695731; s[115] = -0.570972172608539; w[115] = 0.026457153482920;
-      r[116] = -0.137791134319915; s[116] = -0.724417731360170; w[116] = 0.024378078430143;
-      r[117] = -0.075896708294786; s[117] = -0.848206583410427; w[117] = 0.020060551144640;
-      r[118] = -0.031363303799647; s[118] = -0.937273392400706; w[118] = 0.013807557894147;
-      r[119] = -0.006003740989757; s[119] = -0.987992518020485; w[119] = 0.006192534764769;
-      r[120] = -0.995204176239272; s[120] =  0.987992518020485; w[120] = 0.000036637297986;
-      r[121] = -0.974946807693089; s[121] =  0.937273392400706; w[121] = 0.000437920771488;
-      r[122] = -0.939373261167971; s[122] =  0.848206583410427; w[122] = 0.001613849639200;
-      r[123] = -0.889931628110459; s[123] =  0.724417731360170; w[123] = 0.003816155355883;
-      r[124] = -0.828645018820126; s[124] =  0.570972172608539; w[124] = 0.007077467309460;
-      r[125] = -0.758022258950930; s[125] =  0.394151347077563; w[125] = 0.011190086338209;
-      r[126] = -0.680954562267710; s[126] =  0.201194093997435; w[126] = 0.015726512989614;
-      r[127] = -0.600597046998717; s[127] =  0.000000000000000; w[127] = 0.020098950720122;
-      r[128] = -0.520239531729724; s[128] = -0.201194093997435; w[128] = 0.023648541379510;
-      r[129] = -0.443171835046505; s[129] = -0.394151347077563; w[129] = 0.025750117404859;
-      r[130] = -0.372549075177309; s[130] = -0.570972172608539; w[130] = 0.025915578164965;
-      r[131] = -0.311262465886975; s[131] = -0.724417731360170; w[131] = 0.023879061573116;
-      r[132] = -0.261820832829464; s[132] = -0.848206583410427; w[132] = 0.019649913644597;
-      r[133] = -0.226247286304345; s[133] = -0.937273392400706; w[133] = 0.013524918548175;
-      r[134] = -0.205989917758162; s[134] = -0.987992518020485; w[134] = 0.006065774189928;
-      r[135] = -0.996362641608860; s[135] =  0.987992518020485; w[135] = 0.000034371743072;
-      r[136] = -0.980998584641787; s[136] =  0.937273392400706; w[136] = 0.000410840893588;
-      r[137] = -0.954018081518357; s[137] =  0.848206583410427; w[137] = 0.001514053388316;
-      r[138] = -0.916519426887625; s[138] =  0.724417731360170; w[138] = 0.003580174265665;
-      r[139] = -0.870037034354322; s[139] =  0.570972172608539; w[139] = 0.006639815197344;
-      r[140] = -0.816473704876034; s[140] =  0.394151347077563; w[140] = 0.010498120595869;
-      r[141] = -0.758022258950930; s[141] =  0.201194093997435; w[141] = 0.014754026459451;
-      r[142] = -0.697075673538782; s[142] =  0.000000000000000; w[142] = 0.018856084049129;
-      r[143] = -0.636129088126634; s[143] = -0.201194093997435; w[143] = 0.022186177283618;
-      r[144] = -0.577677642201529; s[144] = -0.394151347077563; w[144] = 0.024157797330925;
-      r[145] = -0.524114312723242; s[145] = -0.570972172608539; w[145] = 0.024313026429341;
-      r[146] = -0.477631920189938; s[146] = -0.724417731360170; w[146] = 0.022402442709917;
-      r[147] = -0.440133265559207; s[147] = -0.848206583410427; w[147] = 0.018434814254740;
-      r[148] = -0.413152762435777; s[148] = -0.937273392400706; w[148] = 0.012688572873940;
-      r[149] = -0.397788705468703; s[149] = -0.987992518020485; w[149] = 0.005690682540646;
-      r[150] = -0.997424228046943; s[150] =  0.987992518020485; w[150] = 0.000030699031605;
-      r[151] = -0.986544269911019; s[151] =  0.937273392400706; w[151] = 0.000366941459749;
-      r[152] = -0.967438200134124; s[152] =  0.848206583410427; w[152] = 0.001352272787635;
-      r[153] = -0.940883769008922; s[153] =  0.724417731360170; w[153] = 0.003197623195991;
-      r[154] = -0.907967561661881; s[154] =  0.570972172608539; w[154] = 0.005930333418609;
-      r[155] = -0.870037034354322; s[155] =  0.394151347077563; w[155] = 0.009376368701824;
-      r[156] = -0.828645018820126; s[156] =  0.201194093997435; w[156] = 0.013177519790991;
-      r[157] = -0.785486086304269; s[157] =  0.000000000000000; w[157] = 0.016841261700383;
-      r[158] = -0.742327153788413; s[158] = -0.201194093997435; w[158] = 0.019815525683434;
-      r[159] = -0.700935138254217; s[159] = -0.394151347077563; w[159] = 0.021576472924861;
-      r[160] = -0.663004610946658; s[160] = -0.570972172608539; w[160] = 0.021715115384404;
-      r[161] = -0.630088403599617; s[161] = -0.724417731360170; w[161] = 0.020008682578130;
-      r[162] = -0.603533972474414; s[162] = -0.848206583410427; w[162] = 0.016465005695410;
-      r[163] = -0.584427902697520; s[163] = -0.937273392400706; w[163] = 0.011332765372579;
-      r[164] = -0.573547944561595; s[164] = -0.987992518020485; w[164] = 0.005082618091388;
-      r[165] = -0.998345475437717; s[165] =  0.987992518020485; w[165] = 0.000025769562269;
-      r[166] = -0.991356829586853; s[166] =  0.937273392400706; w[166] = 0.000308020165519;
-      r[167] = -0.979084212945827; s[167] =  0.848206583410427; w[167] = 0.001135132803359;
-      r[168] = -0.962027206605662; s[168] =  0.724417731360170; w[168] = 0.002684167732828;
-      r[169] = -0.940883769008922; s[169] =  0.570972172608539; w[169] = 0.004978075474027;
-      r[170] = -0.916519426887625; s[170] =  0.394151347077563; w[170] = 0.007870766747028;
-      r[171] = -0.889931628110459; s[171] =  0.201194093997435; w[171] = 0.011061551425453;
-      r[172] = -0.862208865680085; s[172] =  0.000000000000000; w[172] = 0.014136991279319;
-      r[173] = -0.834486103249711; s[173] = -0.201194093997435; w[173] = 0.016633665503545;
-      r[174] = -0.807898304472545; s[174] = -0.394151347077563; w[174] = 0.018111850228555;
-      r[175] = -0.783533962351248; s[175] = -0.570972172608539; w[175] = 0.018228230300094;
-      r[176] = -0.762390524754508; s[176] = -0.724417731360170; w[176] = 0.016795806403939;
-      r[177] = -0.745333518414343; s[177] = -0.848206583410427; w[177] = 0.013821152243283;
-      r[178] = -0.733060901773317; s[178] = -0.937273392400706; w[178] = 0.009513016785380;
-      r[179] = -0.726072255922453; s[179] = -0.987992518020485; w[179] = 0.004266481271556;
-      r[180] = -0.999088671642846; s[180] =  0.987992518020485; w[180] = 0.000019785289042;
-      r[181] = -0.995239256960715; s[181] =  0.937273392400706; w[181] = 0.000236490940043;
-      r[182] = -0.988479379340032; s[182] =  0.848206583410427; w[182] = 0.000871529379538;
-      r[183] = -0.979084212945827; s[183] =  0.724417731360170; w[183] = 0.002060843481789;
-      r[184] = -0.967438200134124; s[184] =  0.570972172608539; w[184] = 0.003822054138805;
-      r[185] = -0.954018081518357; s[185] =  0.394151347077563; w[185] = 0.006042997294437;
-      r[186] = -0.939373261167971; s[186] =  0.201194093997435; w[186] = 0.008492809847469;
-      r[187] = -0.924103291705214; s[187] =  0.000000000000000; w[187] = 0.010854063244177;
-      r[188] = -0.908833322242456; s[188] = -0.201194093997435; w[188] = 0.012770953436328;
-      r[189] = -0.894188501892071; s[189] = -0.394151347077563; w[189] = 0.013905870348620;
-      r[190] = -0.880768383276303; s[190] = -0.570972172608539; w[190] = 0.013995224344240;
-      r[191] = -0.869122370464600; s[191] = -0.724417731360170; w[191] = 0.012895441564853;
-      r[192] = -0.859727204070395; s[192] = -0.848206583410427; w[192] = 0.010611569151594;
-      r[193] = -0.852967326449712; s[193] = -0.937273392400706; w[193] = 0.007303879856139;
-      r[194] = -0.849117911767581; s[194] = -0.987992518020485; w[194] = 0.003275708150100;
-      r[195] = -0.999623405694808; s[195] =  0.987992518020485; w[195] = 0.000012991999963;
-      r[196] = -0.998032686349542; s[196] =  0.937273392400706; w[196] = 0.000155291655212;
-      r[197] = -0.995239256960715; s[197] =  0.848206583410427; w[197] = 0.000572289322752;
-      r[198] = -0.991356829586853; s[198] =  0.724417731360170; w[198] = 0.001353251821662;
-      r[199] = -0.986544269911019; s[199] =  0.570972172608539; w[199] = 0.002509749901695;
-      r[200] = -0.980998584641787; s[200] =  0.394151347077563; w[200] = 0.003968131092565;
-      r[201] = -0.974946807693089; s[201] =  0.201194093997435; w[201] = 0.005576799256556;
-      r[202] = -0.968636696200353; s[202] =  0.000000000000000; w[202] = 0.007127315095696;
-      r[203] = -0.962326584707617; s[203] = -0.201194093997435; w[203] = 0.008386040063107;
-      r[204] = -0.956274807758919; s[204] = -0.394151347077563; w[204] = 0.009131282674963;
-      r[205] = -0.950729122489687; s[205] = -0.570972172608539; w[205] = 0.009189956930633;
-      r[206] = -0.945916562813853; s[206] = -0.724417731360170; w[206] = 0.008467785129237;
-      r[207] = -0.942034135439991; s[207] = -0.848206583410427; w[207] = 0.006968081473429;
-      r[208] = -0.939240706051164; s[208] = -0.937273392400706; w[208] = 0.004796088983887;
-      r[209] = -0.937649986705898; s[209] = -0.987992518020485; w[209] = 0.002150992086750;
-      r[210] = -0.999927910188256; s[210] =  0.987992518020485; w[210] = 0.000005678109445;
-      r[211] = -0.999623405694808; s[211] =  0.937273392400706; w[211] = 0.000067869690329;
-      r[212] = -0.999088671642846; s[212] =  0.848206583410427; w[212] = 0.000250117104238;
-      r[213] = -0.998345475437717; s[213] =  0.724417731360170; w[213] = 0.000591434111178;
-      r[214] = -0.997424228046943; s[214] =  0.570972172608539; w[214] = 0.001096877668021;
-      r[215] = -0.996362641608860; s[215] =  0.394151347077563; w[215] = 0.001734258212849;
-      r[216] = -0.995204176239272; s[216] =  0.201194093997435; w[216] = 0.002437321168702;
-      r[217] = -0.993996259010243; s[217] =  0.000000000000000; w[217] = 0.003114968848543;
-      r[218] = -0.992788341781213; s[218] = -0.201194093997435; w[218] = 0.003665090319212;
-      r[219] = -0.991629876411625; s[219] = -0.394151347077563; w[219] = 0.003990796070869;
-      r[220] = -0.990568289973542; s[220] = -0.570972172608539; w[220] = 0.004016439454972;
-      r[221] = -0.989647042582769; s[221] = -0.724417731360170; w[221] = 0.003700816722647;
-      r[222] = -0.988903846377640; s[222] = -0.848206583410427; w[222] = 0.003045376334904;
-      r[223] = -0.988369112325678; s[223] = -0.937273392400706; w[223] = 0.002096114396383;
-      r[224] = -0.988064607832230; s[224] = -0.987992518020485; w[224] = 0.000940083783827;
+      r[0] = -0.988064607832230;
+      s[0] = 0.987992518020485;
+      w[0] = 0.000005678109445;
+      r[1] = -0.937649986705898;
+      s[1] = 0.937273392400706;
+      w[1] = 0.000067869690329;
+      r[2] = -0.849117911767581;
+      s[2] = 0.848206583410427;
+      w[2] = 0.000250117104238;
+      r[3] = -0.726072255922453;
+      s[3] = 0.724417731360170;
+      w[3] = 0.000591434111178;
+      r[4] = -0.573547944561595;
+      s[4] = 0.570972172608539;
+      w[4] = 0.001096877668021;
+      r[5] = -0.397788705468703;
+      s[5] = 0.394151347077563;
+      w[5] = 0.001734258212849;
+      r[6] = -0.205989917758162;
+      s[6] = 0.201194093997435;
+      w[6] = 0.002437321168702;
+      r[7] = -0.006003740989757;
+      s[7] = 0.000000000000000;
+      w[7] = 0.003114968848543;
+      r[8] = 0.193982435778648;
+      s[8] = -0.201194093997435;
+      w[8] = 0.003665090319212;
+      r[9] = 0.385781223489189;
+      s[9] = -0.394151347077563;
+      w[9] = 0.003990796070869;
+      r[10] = 0.561540462582081;
+      s[10] = -0.570972172608539;
+      w[10] = 0.004016439454972;
+      r[11] = 0.714064773942939;
+      s[11] = -0.724417731360170;
+      w[11] = 0.003700816722647;
+      r[12] = 0.837110429788067;
+      s[12] = -0.848206583410427;
+      w[12] = 0.003045376334904;
+      r[13] = 0.925642504726384;
+      s[13] = -0.937273392400706;
+      w[13] = 0.002096114396383;
+      r[14] = 0.976057125852715;
+      s[14] = -0.987992518020485;
+      w[14] = 0.000940083783827;
+      r[15] = -0.988369112325678;
+      s[15] = 0.987992518020485;
+      w[15] = 0.000012991999963;
+      r[16] = -0.939240706051164;
+      s[16] = 0.937273392400706;
+      w[16] = 0.000155291655212;
+      r[17] = -0.852967326449712;
+      s[17] = 0.848206583410427;
+      w[17] = 0.000572289322752;
+      r[18] = -0.733060901773317;
+      s[18] = 0.724417731360170;
+      w[18] = 0.001353251821662;
+      r[19] = -0.584427902697520;
+      s[19] = 0.570972172608539;
+      w[19] = 0.002509749901695;
+      r[20] = -0.413152762435777;
+      s[20] = 0.394151347077563;
+      w[20] = 0.003968131092565;
+      r[21] = -0.226247286304345;
+      s[21] = 0.201194093997435;
+      w[21] = 0.005576799256556;
+      r[22] = -0.031363303799647;
+      s[22] = 0.000000000000000;
+      w[22] = 0.007127315095696;
+      r[23] = 0.163520678705051;
+      s[23] = -0.201194093997435;
+      w[23] = 0.008386040063107;
+      r[24] = 0.350426154836483;
+      s[24] = -0.394151347077563;
+      w[24] = 0.009131282674963;
+      r[25] = 0.521701295098226;
+      s[25] = -0.570972172608539;
+      w[25] = 0.009189956930633;
+      r[26] = 0.670334294174023;
+      s[26] = -0.724417731360170;
+      w[26] = 0.008467785129237;
+      r[27] = 0.790240718850418;
+      s[27] = -0.848206583410427;
+      w[27] = 0.006968081473429;
+      r[28] = 0.876514098451870;
+      s[28] = -0.937273392400706;
+      w[28] = 0.004796088983887;
+      r[29] = 0.925642504726384;
+      s[29] = -0.987992518020485;
+      w[29] = 0.002150992086750;
+      r[30] = -0.988903846377640;
+      s[30] = 0.987992518020485;
+      w[30] = 0.000019785289042;
+      r[31] = -0.942034135439991;
+      s[31] = 0.937273392400706;
+      w[31] = 0.000236490940043;
+      r[32] = -0.859727204070395;
+      s[32] = 0.848206583410427;
+      w[32] = 0.000871529379538;
+      r[33] = -0.745333518414343;
+      s[33] = 0.724417731360170;
+      w[33] = 0.002060843481789;
+      r[34] = -0.603533972474414;
+      s[34] = 0.570972172608539;
+      w[34] = 0.003822054138805;
+      r[35] = -0.440133265559207;
+      s[35] = 0.394151347077563;
+      w[35] = 0.006042997294437;
+      r[36] = -0.261820832829464;
+      s[36] = 0.201194093997435;
+      w[36] = 0.008492809847469;
+      r[37] = -0.075896708294786;
+      s[37] = 0.000000000000000;
+      w[37] = 0.010854063244177;
+      r[38] = 0.110027416239891;
+      s[38] = -0.201194093997435;
+      w[38] = 0.012770953436328;
+      r[39] = 0.288339848969634;
+      s[39] = -0.394151347077563;
+      w[39] = 0.013905870348620;
+      r[40] = 0.451740555884842;
+      s[40] = -0.570972172608539;
+      w[40] = 0.013995224344240;
+      r[41] = 0.593540101824770;
+      s[41] = -0.724417731360170;
+      w[41] = 0.012895441564853;
+      r[42] = 0.707933787480822;
+      s[42] = -0.848206583410427;
+      w[42] = 0.010611569151594;
+      r[43] = 0.790240718850418;
+      s[43] = -0.937273392400706;
+      w[43] = 0.007303879856139;
+      r[44] = 0.837110429788067;
+      s[44] = -0.987992518020485;
+      w[44] = 0.003275708150100;
+      r[45] = -0.989647042582769;
+      s[45] = 0.987992518020485;
+      w[45] = 0.000025769562269;
+      r[46] = -0.945916562813853;
+      s[46] = 0.937273392400706;
+      w[46] = 0.000308020165519;
+      r[47] = -0.869122370464600;
+      s[47] = 0.848206583410427;
+      w[47] = 0.001135132803359;
+      r[48] = -0.762390524754508;
+      s[48] = 0.724417731360170;
+      w[48] = 0.002684167732828;
+      r[49] = -0.630088403599617;
+      s[49] = 0.570972172608539;
+      w[49] = 0.004978075474027;
+      r[50] = -0.477631920189938;
+      s[50] = 0.394151347077563;
+      w[50] = 0.007870766747028;
+      r[51] = -0.311262465886975;
+      s[51] = 0.201194093997435;
+      w[51] = 0.011061551425453;
+      r[52] = -0.137791134319915;
+      s[52] = 0.000000000000000;
+      w[52] = 0.014136991279319;
+      r[53] = 0.035680197247145;
+      s[53] = -0.201194093997435;
+      w[53] = 0.016633665503545;
+      r[54] = 0.202049651550108;
+      s[54] = -0.394151347077563;
+      w[54] = 0.018111850228555;
+      r[55] = 0.354506134959787;
+      s[55] = -0.570972172608539;
+      w[55] = 0.018228230300094;
+      r[56] = 0.486808256114678;
+      s[56] = -0.724417731360170;
+      w[56] = 0.016795806403939;
+      r[57] = 0.593540101824770;
+      s[57] = -0.848206583410427;
+      w[57] = 0.013821152243283;
+      r[58] = 0.670334294174023;
+      s[58] = -0.937273392400706;
+      w[58] = 0.009513016785380;
+      r[59] = 0.714064773942939;
+      s[59] = -0.987992518020485;
+      w[59] = 0.004266481271556;
+      r[60] = -0.990568289973542;
+      s[60] = 0.987992518020485;
+      w[60] = 0.000030699031605;
+      r[61] = -0.950729122489687;
+      s[61] = 0.937273392400706;
+      w[61] = 0.000366941459749;
+      r[62] = -0.880768383276303;
+      s[62] = 0.848206583410427;
+      w[62] = 0.001352272787635;
+      r[63] = -0.783533962351248;
+      s[63] = 0.724417731360170;
+      w[63] = 0.003197623195991;
+      r[64] = -0.663004610946658;
+      s[64] = 0.570972172608539;
+      w[64] = 0.005930333418609;
+      r[65] = -0.524114312723242;
+      s[65] = 0.394151347077563;
+      w[65] = 0.009376368701824;
+      r[66] = -0.372549075177309;
+      s[66] = 0.201194093997435;
+      w[66] = 0.013177519790991;
+      r[67] = -0.214513913695731;
+      s[67] = 0.000000000000000;
+      w[67] = 0.016841261700383;
+      r[68] = -0.056478752214152;
+      s[68] = -0.201194093997435;
+      w[68] = 0.019815525683434;
+      r[69] = 0.095086485331781;
+      s[69] = -0.394151347077563;
+      w[69] = 0.021576472924861;
+      r[70] = 0.233976783555196;
+      s[70] = -0.570972172608539;
+      w[70] = 0.021715115384404;
+      r[71] = 0.354506134959787;
+      s[71] = -0.724417731360170;
+      w[71] = 0.020008682578130;
+      r[72] = 0.451740555884842;
+      s[72] = -0.848206583410427;
+      w[72] = 0.016465005695410;
+      r[73] = 0.521701295098226;
+      s[73] = -0.937273392400706;
+      w[73] = 0.011332765372579;
+      r[74] = 0.561540462582081;
+      s[74] = -0.987992518020485;
+      w[74] = 0.005082618091388;
+      r[75] = -0.991629876411625;
+      s[75] = 0.987992518020485;
+      w[75] = 0.000034371743072;
+      r[76] = -0.956274807758919;
+      s[76] = 0.937273392400706;
+      w[76] = 0.000410840893588;
+      r[77] = -0.894188501892071;
+      s[77] = 0.848206583410427;
+      w[77] = 0.001514053388316;
+      r[78] = -0.807898304472545;
+      s[78] = 0.724417731360170;
+      w[78] = 0.003580174265665;
+      r[79] = -0.700935138254217;
+      s[79] = 0.570972172608539;
+      w[79] = 0.006639815197344;
+      r[80] = -0.577677642201529;
+      s[80] = 0.394151347077563;
+      w[80] = 0.010498120595869;
+      r[81] = -0.443171835046505;
+      s[81] = 0.201194093997435;
+      w[81] = 0.014754026459451;
+      r[82] = -0.302924326461218;
+      s[82] = 0.000000000000000;
+      w[82] = 0.018856084049129;
+      r[83] = -0.162676817875932;
+      s[83] = -0.201194093997435;
+      w[83] = 0.022186177283618;
+      r[84] = -0.028171010720908;
+      s[84] = -0.394151347077563;
+      w[84] = 0.024157797330925;
+      r[85] = 0.095086485331781;
+      s[85] = -0.570972172608539;
+      w[85] = 0.024313026429341;
+      r[86] = 0.202049651550108;
+      s[86] = -0.724417731360170;
+      w[86] = 0.022402442709917;
+      r[87] = 0.288339848969634;
+      s[87] = -0.848206583410427;
+      w[87] = 0.018434814254740;
+      r[88] = 0.350426154836483;
+      s[88] = -0.937273392400706;
+      w[88] = 0.012688572873940;
+      r[89] = 0.385781223489189;
+      s[89] = -0.987992518020485;
+      w[89] = 0.005690682540646;
+      r[90] = -0.992788341781213;
+      s[90] = 0.987992518020485;
+      w[90] = 0.000036637297986;
+      r[91] = -0.962326584707617;
+      s[91] = 0.937273392400706;
+      w[91] = 0.000437920771488;
+      r[92] = -0.908833322242456;
+      s[92] = 0.848206583410427;
+      w[92] = 0.001613849639200;
+      r[93] = -0.834486103249711;
+      s[93] = 0.724417731360170;
+      w[93] = 0.003816155355883;
+      r[94] = -0.742327153788413;
+      s[94] = 0.570972172608539;
+      w[94] = 0.007077467309460;
+      r[95] = -0.636129088126634;
+      s[95] = 0.394151347077563;
+      w[95] = 0.011190086338209;
+      r[96] = -0.520239531729724;
+      s[96] = 0.201194093997435;
+      w[96] = 0.015726512989614;
+      r[97] = -0.399402953001283;
+      s[97] = 0.000000000000000;
+      w[97] = 0.020098950720122;
+      r[98] = -0.278566374272841;
+      s[98] = -0.201194093997435;
+      w[98] = 0.023648541379510;
+      r[99] = -0.162676817875932;
+      s[99] = -0.394151347077563;
+      w[99] = 0.025750117404859;
+      r[100] = -0.056478752214152;
+      s[100] = -0.570972172608539;
+      w[100] = 0.025915578164965;
+      r[101] = 0.035680197247145;
+      s[101] = -0.724417731360170;
+      w[101] = 0.023879061573116;
+      r[102] = 0.110027416239891;
+      s[102] = -0.848206583410427;
+      w[102] = 0.019649913644597;
+      r[103] = 0.163520678705051;
+      s[103] = -0.937273392400706;
+      w[103] = 0.013524918548175;
+      r[104] = 0.193982435778648;
+      s[104] = -0.987992518020485;
+      w[104] = 0.006065774189928;
+      r[105] = -0.993996259010243;
+      s[105] = 0.987992518020485;
+      w[105] = 0.000037402932316;
+      r[106] = -0.968636696200353;
+      s[106] = 0.937273392400706;
+      w[106] = 0.000447072297244;
+      r[107] = -0.924103291705214;
+      s[107] = 0.848206583410427;
+      w[107] = 0.001647575343713;
+      r[108] = -0.862208865680085;
+      s[108] = 0.724417731360170;
+      w[108] = 0.003895904128496;
+      r[109] = -0.785486086304269;
+      s[109] = 0.570972172608539;
+      w[109] = 0.007225369917846;
+      r[110] = -0.697075673538782;
+      s[110] = 0.394151347077563;
+      w[110] = 0.011423933120557;
+      r[111] = -0.600597046998717;
+      s[111] = 0.201194093997435;
+      w[111] = 0.016055160539688;
+      r[112] = -0.500000000000000;
+      s[112] = 0.000000000000000;
+      w[112] = 0.020518972050826;
+      r[113] = -0.399402953001283;
+      s[113] = -0.201194093997435;
+      w[113] = 0.024142740900556;
+      r[114] = -0.302924326461218;
+      s[114] = -0.394151347077563;
+      w[114] = 0.026288234977700;
+      r[115] = -0.214513913695731;
+      s[115] = -0.570972172608539;
+      w[115] = 0.026457153482920;
+      r[116] = -0.137791134319915;
+      s[116] = -0.724417731360170;
+      w[116] = 0.024378078430143;
+      r[117] = -0.075896708294786;
+      s[117] = -0.848206583410427;
+      w[117] = 0.020060551144640;
+      r[118] = -0.031363303799647;
+      s[118] = -0.937273392400706;
+      w[118] = 0.013807557894147;
+      r[119] = -0.006003740989757;
+      s[119] = -0.987992518020485;
+      w[119] = 0.006192534764769;
+      r[120] = -0.995204176239272;
+      s[120] = 0.987992518020485;
+      w[120] = 0.000036637297986;
+      r[121] = -0.974946807693089;
+      s[121] = 0.937273392400706;
+      w[121] = 0.000437920771488;
+      r[122] = -0.939373261167971;
+      s[122] = 0.848206583410427;
+      w[122] = 0.001613849639200;
+      r[123] = -0.889931628110459;
+      s[123] = 0.724417731360170;
+      w[123] = 0.003816155355883;
+      r[124] = -0.828645018820126;
+      s[124] = 0.570972172608539;
+      w[124] = 0.007077467309460;
+      r[125] = -0.758022258950930;
+      s[125] = 0.394151347077563;
+      w[125] = 0.011190086338209;
+      r[126] = -0.680954562267710;
+      s[126] = 0.201194093997435;
+      w[126] = 0.015726512989614;
+      r[127] = -0.600597046998717;
+      s[127] = 0.000000000000000;
+      w[127] = 0.020098950720122;
+      r[128] = -0.520239531729724;
+      s[128] = -0.201194093997435;
+      w[128] = 0.023648541379510;
+      r[129] = -0.443171835046505;
+      s[129] = -0.394151347077563;
+      w[129] = 0.025750117404859;
+      r[130] = -0.372549075177309;
+      s[130] = -0.570972172608539;
+      w[130] = 0.025915578164965;
+      r[131] = -0.311262465886975;
+      s[131] = -0.724417731360170;
+      w[131] = 0.023879061573116;
+      r[132] = -0.261820832829464;
+      s[132] = -0.848206583410427;
+      w[132] = 0.019649913644597;
+      r[133] = -0.226247286304345;
+      s[133] = -0.937273392400706;
+      w[133] = 0.013524918548175;
+      r[134] = -0.205989917758162;
+      s[134] = -0.987992518020485;
+      w[134] = 0.006065774189928;
+      r[135] = -0.996362641608860;
+      s[135] = 0.987992518020485;
+      w[135] = 0.000034371743072;
+      r[136] = -0.980998584641787;
+      s[136] = 0.937273392400706;
+      w[136] = 0.000410840893588;
+      r[137] = -0.954018081518357;
+      s[137] = 0.848206583410427;
+      w[137] = 0.001514053388316;
+      r[138] = -0.916519426887625;
+      s[138] = 0.724417731360170;
+      w[138] = 0.003580174265665;
+      r[139] = -0.870037034354322;
+      s[139] = 0.570972172608539;
+      w[139] = 0.006639815197344;
+      r[140] = -0.816473704876034;
+      s[140] = 0.394151347077563;
+      w[140] = 0.010498120595869;
+      r[141] = -0.758022258950930;
+      s[141] = 0.201194093997435;
+      w[141] = 0.014754026459451;
+      r[142] = -0.697075673538782;
+      s[142] = 0.000000000000000;
+      w[142] = 0.018856084049129;
+      r[143] = -0.636129088126634;
+      s[143] = -0.201194093997435;
+      w[143] = 0.022186177283618;
+      r[144] = -0.577677642201529;
+      s[144] = -0.394151347077563;
+      w[144] = 0.024157797330925;
+      r[145] = -0.524114312723242;
+      s[145] = -0.570972172608539;
+      w[145] = 0.024313026429341;
+      r[146] = -0.477631920189938;
+      s[146] = -0.724417731360170;
+      w[146] = 0.022402442709917;
+      r[147] = -0.440133265559207;
+      s[147] = -0.848206583410427;
+      w[147] = 0.018434814254740;
+      r[148] = -0.413152762435777;
+      s[148] = -0.937273392400706;
+      w[148] = 0.012688572873940;
+      r[149] = -0.397788705468703;
+      s[149] = -0.987992518020485;
+      w[149] = 0.005690682540646;
+      r[150] = -0.997424228046943;
+      s[150] = 0.987992518020485;
+      w[150] = 0.000030699031605;
+      r[151] = -0.986544269911019;
+      s[151] = 0.937273392400706;
+      w[151] = 0.000366941459749;
+      r[152] = -0.967438200134124;
+      s[152] = 0.848206583410427;
+      w[152] = 0.001352272787635;
+      r[153] = -0.940883769008922;
+      s[153] = 0.724417731360170;
+      w[153] = 0.003197623195991;
+      r[154] = -0.907967561661881;
+      s[154] = 0.570972172608539;
+      w[154] = 0.005930333418609;
+      r[155] = -0.870037034354322;
+      s[155] = 0.394151347077563;
+      w[155] = 0.009376368701824;
+      r[156] = -0.828645018820126;
+      s[156] = 0.201194093997435;
+      w[156] = 0.013177519790991;
+      r[157] = -0.785486086304269;
+      s[157] = 0.000000000000000;
+      w[157] = 0.016841261700383;
+      r[158] = -0.742327153788413;
+      s[158] = -0.201194093997435;
+      w[158] = 0.019815525683434;
+      r[159] = -0.700935138254217;
+      s[159] = -0.394151347077563;
+      w[159] = 0.021576472924861;
+      r[160] = -0.663004610946658;
+      s[160] = -0.570972172608539;
+      w[160] = 0.021715115384404;
+      r[161] = -0.630088403599617;
+      s[161] = -0.724417731360170;
+      w[161] = 0.020008682578130;
+      r[162] = -0.603533972474414;
+      s[162] = -0.848206583410427;
+      w[162] = 0.016465005695410;
+      r[163] = -0.584427902697520;
+      s[163] = -0.937273392400706;
+      w[163] = 0.011332765372579;
+      r[164] = -0.573547944561595;
+      s[164] = -0.987992518020485;
+      w[164] = 0.005082618091388;
+      r[165] = -0.998345475437717;
+      s[165] = 0.987992518020485;
+      w[165] = 0.000025769562269;
+      r[166] = -0.991356829586853;
+      s[166] = 0.937273392400706;
+      w[166] = 0.000308020165519;
+      r[167] = -0.979084212945827;
+      s[167] = 0.848206583410427;
+      w[167] = 0.001135132803359;
+      r[168] = -0.962027206605662;
+      s[168] = 0.724417731360170;
+      w[168] = 0.002684167732828;
+      r[169] = -0.940883769008922;
+      s[169] = 0.570972172608539;
+      w[169] = 0.004978075474027;
+      r[170] = -0.916519426887625;
+      s[170] = 0.394151347077563;
+      w[170] = 0.007870766747028;
+      r[171] = -0.889931628110459;
+      s[171] = 0.201194093997435;
+      w[171] = 0.011061551425453;
+      r[172] = -0.862208865680085;
+      s[172] = 0.000000000000000;
+      w[172] = 0.014136991279319;
+      r[173] = -0.834486103249711;
+      s[173] = -0.201194093997435;
+      w[173] = 0.016633665503545;
+      r[174] = -0.807898304472545;
+      s[174] = -0.394151347077563;
+      w[174] = 0.018111850228555;
+      r[175] = -0.783533962351248;
+      s[175] = -0.570972172608539;
+      w[175] = 0.018228230300094;
+      r[176] = -0.762390524754508;
+      s[176] = -0.724417731360170;
+      w[176] = 0.016795806403939;
+      r[177] = -0.745333518414343;
+      s[177] = -0.848206583410427;
+      w[177] = 0.013821152243283;
+      r[178] = -0.733060901773317;
+      s[178] = -0.937273392400706;
+      w[178] = 0.009513016785380;
+      r[179] = -0.726072255922453;
+      s[179] = -0.987992518020485;
+      w[179] = 0.004266481271556;
+      r[180] = -0.999088671642846;
+      s[180] = 0.987992518020485;
+      w[180] = 0.000019785289042;
+      r[181] = -0.995239256960715;
+      s[181] = 0.937273392400706;
+      w[181] = 0.000236490940043;
+      r[182] = -0.988479379340032;
+      s[182] = 0.848206583410427;
+      w[182] = 0.000871529379538;
+      r[183] = -0.979084212945827;
+      s[183] = 0.724417731360170;
+      w[183] = 0.002060843481789;
+      r[184] = -0.967438200134124;
+      s[184] = 0.570972172608539;
+      w[184] = 0.003822054138805;
+      r[185] = -0.954018081518357;
+      s[185] = 0.394151347077563;
+      w[185] = 0.006042997294437;
+      r[186] = -0.939373261167971;
+      s[186] = 0.201194093997435;
+      w[186] = 0.008492809847469;
+      r[187] = -0.924103291705214;
+      s[187] = 0.000000000000000;
+      w[187] = 0.010854063244177;
+      r[188] = -0.908833322242456;
+      s[188] = -0.201194093997435;
+      w[188] = 0.012770953436328;
+      r[189] = -0.894188501892071;
+      s[189] = -0.394151347077563;
+      w[189] = 0.013905870348620;
+      r[190] = -0.880768383276303;
+      s[190] = -0.570972172608539;
+      w[190] = 0.013995224344240;
+      r[191] = -0.869122370464600;
+      s[191] = -0.724417731360170;
+      w[191] = 0.012895441564853;
+      r[192] = -0.859727204070395;
+      s[192] = -0.848206583410427;
+      w[192] = 0.010611569151594;
+      r[193] = -0.852967326449712;
+      s[193] = -0.937273392400706;
+      w[193] = 0.007303879856139;
+      r[194] = -0.849117911767581;
+      s[194] = -0.987992518020485;
+      w[194] = 0.003275708150100;
+      r[195] = -0.999623405694808;
+      s[195] = 0.987992518020485;
+      w[195] = 0.000012991999963;
+      r[196] = -0.998032686349542;
+      s[196] = 0.937273392400706;
+      w[196] = 0.000155291655212;
+      r[197] = -0.995239256960715;
+      s[197] = 0.848206583410427;
+      w[197] = 0.000572289322752;
+      r[198] = -0.991356829586853;
+      s[198] = 0.724417731360170;
+      w[198] = 0.001353251821662;
+      r[199] = -0.986544269911019;
+      s[199] = 0.570972172608539;
+      w[199] = 0.002509749901695;
+      r[200] = -0.980998584641787;
+      s[200] = 0.394151347077563;
+      w[200] = 0.003968131092565;
+      r[201] = -0.974946807693089;
+      s[201] = 0.201194093997435;
+      w[201] = 0.005576799256556;
+      r[202] = -0.968636696200353;
+      s[202] = 0.000000000000000;
+      w[202] = 0.007127315095696;
+      r[203] = -0.962326584707617;
+      s[203] = -0.201194093997435;
+      w[203] = 0.008386040063107;
+      r[204] = -0.956274807758919;
+      s[204] = -0.394151347077563;
+      w[204] = 0.009131282674963;
+      r[205] = -0.950729122489687;
+      s[205] = -0.570972172608539;
+      w[205] = 0.009189956930633;
+      r[206] = -0.945916562813853;
+      s[206] = -0.724417731360170;
+      w[206] = 0.008467785129237;
+      r[207] = -0.942034135439991;
+      s[207] = -0.848206583410427;
+      w[207] = 0.006968081473429;
+      r[208] = -0.939240706051164;
+      s[208] = -0.937273392400706;
+      w[208] = 0.004796088983887;
+      r[209] = -0.937649986705898;
+      s[209] = -0.987992518020485;
+      w[209] = 0.002150992086750;
+      r[210] = -0.999927910188256;
+      s[210] = 0.987992518020485;
+      w[210] = 0.000005678109445;
+      r[211] = -0.999623405694808;
+      s[211] = 0.937273392400706;
+      w[211] = 0.000067869690329;
+      r[212] = -0.999088671642846;
+      s[212] = 0.848206583410427;
+      w[212] = 0.000250117104238;
+      r[213] = -0.998345475437717;
+      s[213] = 0.724417731360170;
+      w[213] = 0.000591434111178;
+      r[214] = -0.997424228046943;
+      s[214] = 0.570972172608539;
+      w[214] = 0.001096877668021;
+      r[215] = -0.996362641608860;
+      s[215] = 0.394151347077563;
+      w[215] = 0.001734258212849;
+      r[216] = -0.995204176239272;
+      s[216] = 0.201194093997435;
+      w[216] = 0.002437321168702;
+      r[217] = -0.993996259010243;
+      s[217] = 0.000000000000000;
+      w[217] = 0.003114968848543;
+      r[218] = -0.992788341781213;
+      s[218] = -0.201194093997435;
+      w[218] = 0.003665090319212;
+      r[219] = -0.991629876411625;
+      s[219] = -0.394151347077563;
+      w[219] = 0.003990796070869;
+      r[220] = -0.990568289973542;
+      s[220] = -0.570972172608539;
+      w[220] = 0.004016439454972;
+      r[221] = -0.989647042582769;
+      s[221] = -0.724417731360170;
+      w[221] = 0.003700816722647;
+      r[222] = -0.988903846377640;
+      s[222] = -0.848206583410427;
+      w[222] = 0.003045376334904;
+      r[223] = -0.988369112325678;
+      s[223] = -0.937273392400706;
+      w[223] = 0.002096114396383;
+      r[224] = -0.988064607832230;
+      s[224] = -0.987992518020485;
+      w[224] = 0.000940083783827;
 
       break;
     }
@@ -2030,26 +5525,57 @@ void CFEMStandardElementBase::IntegrationPointsTriangle(void) {
 }
 
 void CFEMStandardElementBase::IntegrationPointsTetrahedron(void) {
-
   /*--- Set the number of integration points, depending on the order of
         polynomials that must be integrated exactly. ---*/
-  switch( orderExact ) {
-    case  0: nIntegration =   1; break;
-    case  1: nIntegration =   1; break;
-    case  2: nIntegration =   4; break;
-    case  3: nIntegration =   8; break;
-    case  4: nIntegration =  14; break;
-    case  5: nIntegration =  14; break;
-    case  6: nIntegration =  24; break;
-    case  7: nIntegration =  35; break;
-    case  8: nIntegration =  46; break;
-    case  9: nIntegration =  59; break;
-    case 10: nIntegration =  81; break;
-    case 11: nIntegration = 105; break;
-    case 12: nIntegration = 132; break;
-    case 13: nIntegration = 163; break;
-    case 14: nIntegration = 214; break;
-    case 15: nIntegration = 264; break;
+  switch (orderExact) {
+    case 0:
+      nIntegration = 1;
+      break;
+    case 1:
+      nIntegration = 1;
+      break;
+    case 2:
+      nIntegration = 4;
+      break;
+    case 3:
+      nIntegration = 8;
+      break;
+    case 4:
+      nIntegration = 14;
+      break;
+    case 5:
+      nIntegration = 14;
+      break;
+    case 6:
+      nIntegration = 24;
+      break;
+    case 7:
+      nIntegration = 35;
+      break;
+    case 8:
+      nIntegration = 46;
+      break;
+    case 9:
+      nIntegration = 59;
+      break;
+    case 10:
+      nIntegration = 81;
+      break;
+    case 11:
+      nIntegration = 105;
+      break;
+    case 12:
+      nIntegration = 132;
+      break;
+    case 13:
+      nIntegration = 163;
+      break;
+    case 14:
+      nIntegration = 214;
+      break;
+    case 15:
+      nIntegration = 264;
+      break;
     default:
       SU2_MPI::Error("Polynomial order not supported", CURRENT_FUNCTION);
   }
@@ -2062,1221 +5588,4670 @@ void CFEMStandardElementBase::IntegrationPointsTetrahedron(void) {
 
   /*--- Set the pointers to the data arrays of the variables just allocated, such
         that the names are shorter. This is useful for the code below. ---*/
-  su2double *r = rIntegration.data();
-  su2double *s = sIntegration.data();
-  su2double *t = tIntegration.data();
-  su2double *w = wIntegration.data();
+  su2double* r = rIntegration.data();
+  su2double* s = sIntegration.data();
+  su2double* t = tIntegration.data();
+  su2double* w = wIntegration.data();
 
   /*--- Set the data for the integration points, depending on the order.
         These integration rules are obtained with the open source program
         Polyquad, developed by Freddie Witherden.           ---*/
-  switch( orderExact )
-  {
-    case  0:
-    case  1: {
-      r[0] = -0.500000000000000; s[0] = -0.500000000000000; t[0] = -0.500000000000000; w[0] = 1.333333333333333;
+  switch (orderExact) {
+    case 0:
+    case 1: {
+      r[0] = -0.500000000000000;
+      s[0] = -0.500000000000000;
+      t[0] = -0.500000000000000;
+      w[0] = 1.333333333333333;
 
       break;
     }
-    case  2: {
-      r[0] =-0.723606797749979; s[0] = -0.723606797749979; t[0] = 0.1708203932499369; w[0] = 0.3333333333333333;
-      r[1] =-0.723606797749979; s[1] = 0.1708203932499369; t[1] = -0.723606797749979; w[1] = 0.3333333333333333;
-      r[2] = 0.170820393249937; s[2] = -0.723606797749979; t[2] = -0.723606797749979; w[2] = 0.3333333333333333;
-      r[3] =-0.723606797749979; s[3] = -0.723606797749979; t[3] = -0.723606797749979; w[3] = 0.3333333333333333;
+    case 2: {
+      r[0] = -0.723606797749979;
+      s[0] = -0.723606797749979;
+      t[0] = 0.1708203932499369;
+      w[0] = 0.3333333333333333;
+      r[1] = -0.723606797749979;
+      s[1] = 0.1708203932499369;
+      t[1] = -0.723606797749979;
+      w[1] = 0.3333333333333333;
+      r[2] = 0.170820393249937;
+      s[2] = -0.723606797749979;
+      t[2] = -0.723606797749979;
+      w[2] = 0.3333333333333333;
+      r[3] = -0.723606797749979;
+      s[3] = -0.723606797749979;
+      t[3] = -0.723606797749979;
+      w[3] = 0.3333333333333333;
 
       break;
     }
-    case  3: {
-      r[0] =-0.7860119704589262; s[0] =-0.7860119704589262; t[0] = 0.3580359113767786; w[0] = 0.1487451997767295;
-      r[1] =-0.7860119704589262; s[1] = 0.3580359113767786; t[1] =-0.7860119704589262; w[1] = 0.1487451997767295;
-      r[2] = 0.3580359113767786; s[2] =-0.7860119704589262; t[2] =-0.7860119704589262; w[2] = 0.1487451997767295;
-      r[3] =-0.7860119704589262; s[3] =-0.7860119704589262; t[3] =-0.7860119704589262; w[3] = 0.1487451997767295;
-      r[4] =-0.3438828566749746; s[4] =-0.3438828566749746; t[4] =-0.9683514299750762; w[4] = 0.1845881335566038;
-      r[5] =-0.3438828566749746; s[5] =-0.9683514299750762; t[5] =-0.3438828566749746; w[5] = 0.1845881335566038;
-      r[6] =-0.9683514299750762; s[6] =-0.3438828566749746; t[6] =-0.3438828566749746; w[6] = 0.1845881335566038;
-      r[7] =-0.3438828566749746; s[7] =-0.3438828566749746; t[7] =-0.3438828566749746; w[7] = 0.1845881335566038;
+    case 3: {
+      r[0] = -0.7860119704589262;
+      s[0] = -0.7860119704589262;
+      t[0] = 0.3580359113767786;
+      w[0] = 0.1487451997767295;
+      r[1] = -0.7860119704589262;
+      s[1] = 0.3580359113767786;
+      t[1] = -0.7860119704589262;
+      w[1] = 0.1487451997767295;
+      r[2] = 0.3580359113767786;
+      s[2] = -0.7860119704589262;
+      t[2] = -0.7860119704589262;
+      w[2] = 0.1487451997767295;
+      r[3] = -0.7860119704589262;
+      s[3] = -0.7860119704589262;
+      t[3] = -0.7860119704589262;
+      w[3] = 0.1487451997767295;
+      r[4] = -0.3438828566749746;
+      s[4] = -0.3438828566749746;
+      t[4] = -0.9683514299750762;
+      w[4] = 0.1845881335566038;
+      r[5] = -0.3438828566749746;
+      s[5] = -0.9683514299750762;
+      t[5] = -0.3438828566749746;
+      w[5] = 0.1845881335566038;
+      r[6] = -0.9683514299750762;
+      s[6] = -0.3438828566749746;
+      t[6] = -0.3438828566749746;
+      w[6] = 0.1845881335566038;
+      r[7] = -0.3438828566749746;
+      s[7] = -0.3438828566749746;
+      t[7] = -0.3438828566749746;
+      w[7] = 0.1845881335566038;
 
       break;
     }
-    case  4:
-    case  5: {
-      r[0]   = -0.8145294993782175; s[0]  = -0.8145294993782175; t[0]  =  0.4435884981346525; w[0]  = 0.09799072415514934;
-      r[1]   = -0.8145294993782175; s[1]  =  0.4435884981346525; t[1]  = -0.8145294993782175; w[1]  = 0.09799072415514934;
-      r[2]   =  0.4435884981346525; s[2]  = -0.8145294993782175; t[2]  = -0.8145294993782175; w[2]  = 0.09799072415514934;
-      r[3]   = -0.8145294993782175; s[3]  = -0.8145294993782175; t[3]  = -0.8145294993782175; w[3]  = 0.09799072415514934;
-      r[4]   = -0.3782281614733985; s[4]  = -0.3782281614733985; t[4]  = -0.8653155155798045; w[4]  =  0.1502505676240211;
-      r[5]   = -0.3782281614733985; s[5]  = -0.8653155155798045; t[5]  = -0.3782281614733985; w[5]  =  0.1502505676240211;
-      r[6]   = -0.8653155155798045; s[6]  = -0.3782281614733985; t[6]  = -0.3782281614733985; w[6]  =  0.1502505676240211;
-      r[7]   = -0.3782281614733985; s[7]  = -0.3782281614733985; t[7]  = -0.3782281614733985; w[7]  =  0.1502505676240211;
-      r[8]   =  -0.908992591748701; s[8]  =-0.09100740825129899; t[8]  =-0.09100740825129899; w[8]  =  0.0567280277027752;
-      r[9]   =-0.09100740825129902; s[9]  =  -0.908992591748701; t[9]  =-0.09100740825129902; w[9]  =  0.0567280277027752;
-      r[10]  =  -0.908992591748701; s[10] =  -0.908992591748701; t[10] =-0.09100740825129905; w[10] =  0.0567280277027752;
-      r[11]  =  -0.908992591748701; s[11] =-0.09100740825129905; t[11] =  -0.908992591748701; w[11] =  0.0567280277027752;
-      r[12]  =-0.09100740825129899; s[12] =  -0.908992591748701; t[12] =  -0.908992591748701; w[12] =  0.0567280277027752;
-      r[13]  =-0.09100740825129902; s[13] =-0.09100740825129902; t[13] =  -0.908992591748701; w[13] =  0.0567280277027752;
+    case 4:
+    case 5: {
+      r[0] = -0.8145294993782175;
+      s[0] = -0.8145294993782175;
+      t[0] = 0.4435884981346525;
+      w[0] = 0.09799072415514934;
+      r[1] = -0.8145294993782175;
+      s[1] = 0.4435884981346525;
+      t[1] = -0.8145294993782175;
+      w[1] = 0.09799072415514934;
+      r[2] = 0.4435884981346525;
+      s[2] = -0.8145294993782175;
+      t[2] = -0.8145294993782175;
+      w[2] = 0.09799072415514934;
+      r[3] = -0.8145294993782175;
+      s[3] = -0.8145294993782175;
+      t[3] = -0.8145294993782175;
+      w[3] = 0.09799072415514934;
+      r[4] = -0.3782281614733985;
+      s[4] = -0.3782281614733985;
+      t[4] = -0.8653155155798045;
+      w[4] = 0.1502505676240211;
+      r[5] = -0.3782281614733985;
+      s[5] = -0.8653155155798045;
+      t[5] = -0.3782281614733985;
+      w[5] = 0.1502505676240211;
+      r[6] = -0.8653155155798045;
+      s[6] = -0.3782281614733985;
+      t[6] = -0.3782281614733985;
+      w[6] = 0.1502505676240211;
+      r[7] = -0.3782281614733985;
+      s[7] = -0.3782281614733985;
+      t[7] = -0.3782281614733985;
+      w[7] = 0.1502505676240211;
+      r[8] = -0.908992591748701;
+      s[8] = -0.09100740825129899;
+      t[8] = -0.09100740825129899;
+      w[8] = 0.0567280277027752;
+      r[9] = -0.09100740825129902;
+      s[9] = -0.908992591748701;
+      t[9] = -0.09100740825129902;
+      w[9] = 0.0567280277027752;
+      r[10] = -0.908992591748701;
+      s[10] = -0.908992591748701;
+      t[10] = -0.09100740825129905;
+      w[10] = 0.0567280277027752;
+      r[11] = -0.908992591748701;
+      s[11] = -0.09100740825129905;
+      t[11] = -0.908992591748701;
+      w[11] = 0.0567280277027752;
+      r[12] = -0.09100740825129899;
+      s[12] = -0.908992591748701;
+      t[12] = -0.908992591748701;
+      w[12] = 0.0567280277027752;
+      r[13] = -0.09100740825129902;
+      s[13] = -0.09100740825129902;
+      t[13] = -0.908992591748701;
+      w[13] = 0.0567280277027752;
 
       break;
     }
-    case  6: {
-      r[0]  =-0.5707942574816954; s[0]  =-0.5707942574816954; t[0]  =  -0.2876172275549138; w[0]  =  0.05323033367755636;
-      r[1]  =-0.5707942574816954; s[1]  =-0.2876172275549138; t[1]  =  -0.5707942574816954; w[1]  =  0.05323033367755636;
-      r[2]  =-0.2876172275549138; s[2]  =-0.5707942574816954; t[2]  =  -0.5707942574816954; w[2]  =  0.05323033367755636;
-      r[3]  =-0.5707942574816954; s[3]  =-0.5707942574816954; t[3]  =  -0.5707942574816954; w[3]  =  0.05323033367755636;
-      r[4]  =-0.3553242197154491; s[4]  =-0.3553242197154491; t[4]  =  -0.9340273408536528; w[4]  =  0.07380957539153983;
-      r[5]  =-0.3553242197154491; s[5]  =-0.9340273408536528; t[5]  =  -0.3553242197154491; w[5]  =  0.07380957539153983;
-      r[6]  =-0.9340273408536528; s[6]  =-0.3553242197154491; t[6]  =  -0.3553242197154491; w[6]  =  0.07380957539153983;
-      r[7]  =-0.3553242197154491; s[7]  =-0.3553242197154491; t[7]  =  -0.3553242197154491; w[7]  =  0.07380957539153983;
-      r[8]  =-0.9186520829307774; s[8]  =-0.9186520829307774; t[8]  =   0.7559562487923321; w[8]  =  0.01343628140709418;
-      r[9]  =-0.9186520829307774; s[9]  = 0.7559562487923321; t[9]  =  -0.9186520829307774; w[9]  =  0.01343628140709418;
-      r[10] = 0.7559562487923321; s[10] =-0.9186520829307774; t[10] =  -0.9186520829307774; w[10] =  0.01343628140709418;
-      r[11] =-0.9186520829307774; s[11] =-0.9186520829307774; t[11] =  -0.9186520829307774; w[11] =  0.01343628140709418;
-      r[12] = 0.2060113295832982; s[12] =-0.8726779962499649; t[12] =  -0.4606553370833684; w[12] =  0.06428571428571428;
-      r[13] = 0.2060113295832982; s[13] =-0.8726779962499649; t[13] =  -0.8726779962499649; w[13] =  0.06428571428571428;
-      r[14] =-0.8726779962499649; s[14] =-0.8726779962499649; t[14] =   0.2060113295832982; w[14] =  0.06428571428571428;
-      r[15] =-0.4606553370833684; s[15] = 0.2060113295832982; t[15] =  -0.8726779962499649; w[15] =  0.06428571428571428;
-      r[16] =-0.8726779962499649; s[16] =-0.4606553370833684; t[16] =   0.2060113295832982; w[16] =  0.06428571428571428;
-      r[17] =-0.8726779962499649; s[17] = 0.2060113295832982; t[17] =  -0.8726779962499649; w[17] =  0.06428571428571428;
-      r[18] =-0.4606553370833684; s[18] =-0.8726779962499649; t[18] =   0.2060113295832982; w[18] =  0.06428571428571428;
-      r[19] =-0.8726779962499649; s[19] =-0.4606553370833684; t[19] =  -0.8726779962499649; w[19] =  0.06428571428571428;
-      r[20] =-0.8726779962499649; s[20] =-0.8726779962499649; t[20] =  -0.4606553370833684; w[20] =  0.06428571428571428;
-      r[21] =-0.8726779962499649; s[21] = 0.2060113295832982; t[21] =  -0.4606553370833684; w[21] =  0.06428571428571428;
-      r[22] =-0.4606553370833684; s[22] =-0.8726779962499649; t[22] =  -0.8726779962499649; w[22] =  0.06428571428571428;
-      r[23] = 0.2060113295832982; s[23] =-0.4606553370833684; t[23] =  -0.8726779962499649; w[23] =  0.06428571428571428;
+    case 6: {
+      r[0] = -0.5707942574816954;
+      s[0] = -0.5707942574816954;
+      t[0] = -0.2876172275549138;
+      w[0] = 0.05323033367755636;
+      r[1] = -0.5707942574816954;
+      s[1] = -0.2876172275549138;
+      t[1] = -0.5707942574816954;
+      w[1] = 0.05323033367755636;
+      r[2] = -0.2876172275549138;
+      s[2] = -0.5707942574816954;
+      t[2] = -0.5707942574816954;
+      w[2] = 0.05323033367755636;
+      r[3] = -0.5707942574816954;
+      s[3] = -0.5707942574816954;
+      t[3] = -0.5707942574816954;
+      w[3] = 0.05323033367755636;
+      r[4] = -0.3553242197154491;
+      s[4] = -0.3553242197154491;
+      t[4] = -0.9340273408536528;
+      w[4] = 0.07380957539153983;
+      r[5] = -0.3553242197154491;
+      s[5] = -0.9340273408536528;
+      t[5] = -0.3553242197154491;
+      w[5] = 0.07380957539153983;
+      r[6] = -0.9340273408536528;
+      s[6] = -0.3553242197154491;
+      t[6] = -0.3553242197154491;
+      w[6] = 0.07380957539153983;
+      r[7] = -0.3553242197154491;
+      s[7] = -0.3553242197154491;
+      t[7] = -0.3553242197154491;
+      w[7] = 0.07380957539153983;
+      r[8] = -0.9186520829307774;
+      s[8] = -0.9186520829307774;
+      t[8] = 0.7559562487923321;
+      w[8] = 0.01343628140709418;
+      r[9] = -0.9186520829307774;
+      s[9] = 0.7559562487923321;
+      t[9] = -0.9186520829307774;
+      w[9] = 0.01343628140709418;
+      r[10] = 0.7559562487923321;
+      s[10] = -0.9186520829307774;
+      t[10] = -0.9186520829307774;
+      w[10] = 0.01343628140709418;
+      r[11] = -0.9186520829307774;
+      s[11] = -0.9186520829307774;
+      t[11] = -0.9186520829307774;
+      w[11] = 0.01343628140709418;
+      r[12] = 0.2060113295832982;
+      s[12] = -0.8726779962499649;
+      t[12] = -0.4606553370833684;
+      w[12] = 0.06428571428571428;
+      r[13] = 0.2060113295832982;
+      s[13] = -0.8726779962499649;
+      t[13] = -0.8726779962499649;
+      w[13] = 0.06428571428571428;
+      r[14] = -0.8726779962499649;
+      s[14] = -0.8726779962499649;
+      t[14] = 0.2060113295832982;
+      w[14] = 0.06428571428571428;
+      r[15] = -0.4606553370833684;
+      s[15] = 0.2060113295832982;
+      t[15] = -0.8726779962499649;
+      w[15] = 0.06428571428571428;
+      r[16] = -0.8726779962499649;
+      s[16] = -0.4606553370833684;
+      t[16] = 0.2060113295832982;
+      w[16] = 0.06428571428571428;
+      r[17] = -0.8726779962499649;
+      s[17] = 0.2060113295832982;
+      t[17] = -0.8726779962499649;
+      w[17] = 0.06428571428571428;
+      r[18] = -0.4606553370833684;
+      s[18] = -0.8726779962499649;
+      t[18] = 0.2060113295832982;
+      w[18] = 0.06428571428571428;
+      r[19] = -0.8726779962499649;
+      s[19] = -0.4606553370833684;
+      t[19] = -0.8726779962499649;
+      w[19] = 0.06428571428571428;
+      r[20] = -0.8726779962499649;
+      s[20] = -0.8726779962499649;
+      t[20] = -0.4606553370833684;
+      w[20] = 0.06428571428571428;
+      r[21] = -0.8726779962499649;
+      s[21] = 0.2060113295832982;
+      t[21] = -0.4606553370833684;
+      w[21] = 0.06428571428571428;
+      r[22] = -0.4606553370833684;
+      s[22] = -0.8726779962499649;
+      t[22] = -0.8726779962499649;
+      w[22] = 0.06428571428571428;
+      r[23] = 0.2060113295832982;
+      s[23] = -0.4606553370833684;
+      t[23] = -0.8726779962499649;
+      w[23] = 0.06428571428571428;
 
       break;
     }
-    case  7: {
-      r[0]  =               -0.5; s[0]  =               -0.5; t[0]  =               -0.5; w[0]  =  0.1273137192855079;
-      r[1]  =-0.3685977004435944; s[1]  =-0.3685977004435944; t[1]  =-0.8942068986692169; w[1]  = 0.05643944161328927;
-      r[2]  =-0.3685977004435944; s[2]  =-0.8942068986692169; t[2]  =-0.3685977004435944; w[2]  = 0.05643944161328927;
-      r[3]  =-0.8942068986692169; s[3]  =-0.3685977004435944; t[3]  =-0.3685977004435944; w[3]  = 0.05643944161328927;
-      r[4]  =-0.3685977004435944; s[4]  =-0.3685977004435944; t[4]  =-0.3685977004435944; w[4]  = 0.05643944161328927;
-      r[5]  =-0.1009796451967928; s[5]  =-0.8990203548032072; t[5]  =-0.8990203548032072; w[5]  = 0.04252923711047679;
-      r[6]  =-0.8990203548032072; s[6]  =-0.1009796451967928; t[6]  =-0.8990203548032072; w[6]  = 0.04252923711047679;
-      r[7]  =-0.1009796451967928; s[7]  =-0.1009796451967928; t[7]  =-0.8990203548032072; w[7]  = 0.04252923711047679;
-      r[8]  =-0.1009796451967928; s[8]  =-0.8990203548032072; t[8]  =-0.1009796451967928; w[8]  = 0.04252923711047679;
-      r[9]  =-0.8990203548032072; s[9]  =-0.1009796451967928; t[9]  =-0.1009796451967928; w[9]  = 0.04252923711047679;
-      r[10] =-0.8990203548032072; s[10] =-0.8990203548032072; t[10] =-0.1009796451967928; w[10] = 0.04252923711047679;
-      r[11] = 0.6216604821970968; s[11] =-0.9574690549170335; t[11] =-0.7067223723630298; w[11] = 0.01081436110653779;
-      r[12] = 0.6216604821970968; s[12] =-0.9574690549170335; t[12] =-0.9574690549170335; w[12] = 0.01081436110653779;
-      r[13] =-0.9574690549170335; s[13] =-0.9574690549170335; t[13] = 0.6216604821970968; w[13] = 0.01081436110653779;
-      r[14] =-0.7067223723630298; s[14] = 0.6216604821970968; t[14] =-0.9574690549170335; w[14] = 0.01081436110653779;
-      r[15] =-0.9574690549170335; s[15] =-0.7067223723630298; t[15] = 0.6216604821970968; w[15] = 0.01081436110653779;
-      r[16] =-0.9574690549170335; s[16] = 0.6216604821970968; t[16] =-0.9574690549170335; w[16] = 0.01081436110653779;
-      r[17] =-0.7067223723630298; s[17] =-0.9574690549170335; t[17] = 0.6216604821970968; w[17] = 0.01081436110653779;
-      r[18] =-0.9574690549170335; s[18] =-0.7067223723630298; t[18] =-0.9574690549170335; w[18] = 0.01081436110653779;
-      r[19] =-0.9574690549170335; s[19] =-0.9574690549170335; t[19] =-0.7067223723630298; w[19] = 0.01081436110653779;
-      r[20] =-0.9574690549170335; s[20] = 0.6216604821970968; t[20] =-0.7067223723630298; w[20] = 0.01081436110653779;
-      r[21] =-0.7067223723630298; s[21] =-0.9574690549170335; t[21] =-0.9574690549170335; w[21] = 0.01081436110653779;
-      r[22] = 0.6216604821970968; s[22] =-0.7067223723630298; t[22] =-0.9574690549170335; w[22] = 0.01081436110653779;
-      r[23] = 0.1503432751739998; s[23] =-0.6223323379479977; t[23] =-0.9056785992780041; w[23] = 0.04960950763777947;
-      r[24] = 0.1503432751739997; s[24] =-0.6223323379479978; t[24] =-0.6223323379479978; w[24] = 0.04960950763777947;
-      r[25] =-0.6223323379479977; s[25] =-0.6223323379479978; t[25] = 0.1503432751739997; w[25] = 0.04960950763777947;
-      r[26] =-0.9056785992780041; s[26] = 0.1503432751739997; t[26] =-0.6223323379479978; w[26] = 0.04960950763777947;
-      r[27] =-0.6223323379479978; s[27] =-0.9056785992780041; t[27] = 0.1503432751739997; w[27] = 0.04960950763777947;
-      r[28] =-0.6223323379479977; s[28] = 0.1503432751739997; t[28] =-0.6223323379479978; w[28] = 0.04960950763777947;
-      r[29] =-0.9056785992780041; s[29] =-0.6223323379479978; t[29] = 0.1503432751739997; w[29] = 0.04960950763777947;
-      r[30] =-0.6223323379479978; s[30] =-0.9056785992780041; t[30] =-0.6223323379479978; w[30] = 0.04960950763777947;
-      r[31] =-0.6223323379479978; s[31] =-0.6223323379479978; t[31] =-0.9056785992780041; w[31] = 0.04960950763777947;
-      r[32] =-0.6223323379479978; s[32] = 0.1503432751739997; t[32] =-0.9056785992780041; w[32] = 0.04960950763777947;
-      r[33] =-0.9056785992780041; s[33] =-0.6223323379479978; t[33] =-0.6223323379479978; w[33] = 0.04960950763777947;
-      r[34] = 0.1503432751739998; s[34] =-0.9056785992780041; t[34] =-0.6223323379479977; w[34] = 0.04960950763777947;
+    case 7: {
+      r[0] = -0.5;
+      s[0] = -0.5;
+      t[0] = -0.5;
+      w[0] = 0.1273137192855079;
+      r[1] = -0.3685977004435944;
+      s[1] = -0.3685977004435944;
+      t[1] = -0.8942068986692169;
+      w[1] = 0.05643944161328927;
+      r[2] = -0.3685977004435944;
+      s[2] = -0.8942068986692169;
+      t[2] = -0.3685977004435944;
+      w[2] = 0.05643944161328927;
+      r[3] = -0.8942068986692169;
+      s[3] = -0.3685977004435944;
+      t[3] = -0.3685977004435944;
+      w[3] = 0.05643944161328927;
+      r[4] = -0.3685977004435944;
+      s[4] = -0.3685977004435944;
+      t[4] = -0.3685977004435944;
+      w[4] = 0.05643944161328927;
+      r[5] = -0.1009796451967928;
+      s[5] = -0.8990203548032072;
+      t[5] = -0.8990203548032072;
+      w[5] = 0.04252923711047679;
+      r[6] = -0.8990203548032072;
+      s[6] = -0.1009796451967928;
+      t[6] = -0.8990203548032072;
+      w[6] = 0.04252923711047679;
+      r[7] = -0.1009796451967928;
+      s[7] = -0.1009796451967928;
+      t[7] = -0.8990203548032072;
+      w[7] = 0.04252923711047679;
+      r[8] = -0.1009796451967928;
+      s[8] = -0.8990203548032072;
+      t[8] = -0.1009796451967928;
+      w[8] = 0.04252923711047679;
+      r[9] = -0.8990203548032072;
+      s[9] = -0.1009796451967928;
+      t[9] = -0.1009796451967928;
+      w[9] = 0.04252923711047679;
+      r[10] = -0.8990203548032072;
+      s[10] = -0.8990203548032072;
+      t[10] = -0.1009796451967928;
+      w[10] = 0.04252923711047679;
+      r[11] = 0.6216604821970968;
+      s[11] = -0.9574690549170335;
+      t[11] = -0.7067223723630298;
+      w[11] = 0.01081436110653779;
+      r[12] = 0.6216604821970968;
+      s[12] = -0.9574690549170335;
+      t[12] = -0.9574690549170335;
+      w[12] = 0.01081436110653779;
+      r[13] = -0.9574690549170335;
+      s[13] = -0.9574690549170335;
+      t[13] = 0.6216604821970968;
+      w[13] = 0.01081436110653779;
+      r[14] = -0.7067223723630298;
+      s[14] = 0.6216604821970968;
+      t[14] = -0.9574690549170335;
+      w[14] = 0.01081436110653779;
+      r[15] = -0.9574690549170335;
+      s[15] = -0.7067223723630298;
+      t[15] = 0.6216604821970968;
+      w[15] = 0.01081436110653779;
+      r[16] = -0.9574690549170335;
+      s[16] = 0.6216604821970968;
+      t[16] = -0.9574690549170335;
+      w[16] = 0.01081436110653779;
+      r[17] = -0.7067223723630298;
+      s[17] = -0.9574690549170335;
+      t[17] = 0.6216604821970968;
+      w[17] = 0.01081436110653779;
+      r[18] = -0.9574690549170335;
+      s[18] = -0.7067223723630298;
+      t[18] = -0.9574690549170335;
+      w[18] = 0.01081436110653779;
+      r[19] = -0.9574690549170335;
+      s[19] = -0.9574690549170335;
+      t[19] = -0.7067223723630298;
+      w[19] = 0.01081436110653779;
+      r[20] = -0.9574690549170335;
+      s[20] = 0.6216604821970968;
+      t[20] = -0.7067223723630298;
+      w[20] = 0.01081436110653779;
+      r[21] = -0.7067223723630298;
+      s[21] = -0.9574690549170335;
+      t[21] = -0.9574690549170335;
+      w[21] = 0.01081436110653779;
+      r[22] = 0.6216604821970968;
+      s[22] = -0.7067223723630298;
+      t[22] = -0.9574690549170335;
+      w[22] = 0.01081436110653779;
+      r[23] = 0.1503432751739998;
+      s[23] = -0.6223323379479977;
+      t[23] = -0.9056785992780041;
+      w[23] = 0.04960950763777947;
+      r[24] = 0.1503432751739997;
+      s[24] = -0.6223323379479978;
+      t[24] = -0.6223323379479978;
+      w[24] = 0.04960950763777947;
+      r[25] = -0.6223323379479977;
+      s[25] = -0.6223323379479978;
+      t[25] = 0.1503432751739997;
+      w[25] = 0.04960950763777947;
+      r[26] = -0.9056785992780041;
+      s[26] = 0.1503432751739997;
+      t[26] = -0.6223323379479978;
+      w[26] = 0.04960950763777947;
+      r[27] = -0.6223323379479978;
+      s[27] = -0.9056785992780041;
+      t[27] = 0.1503432751739997;
+      w[27] = 0.04960950763777947;
+      r[28] = -0.6223323379479977;
+      s[28] = 0.1503432751739997;
+      t[28] = -0.6223323379479978;
+      w[28] = 0.04960950763777947;
+      r[29] = -0.9056785992780041;
+      s[29] = -0.6223323379479978;
+      t[29] = 0.1503432751739997;
+      w[29] = 0.04960950763777947;
+      r[30] = -0.6223323379479978;
+      s[30] = -0.9056785992780041;
+      t[30] = -0.6223323379479978;
+      w[30] = 0.04960950763777947;
+      r[31] = -0.6223323379479978;
+      s[31] = -0.6223323379479978;
+      t[31] = -0.9056785992780041;
+      w[31] = 0.04960950763777947;
+      r[32] = -0.6223323379479978;
+      s[32] = 0.1503432751739997;
+      t[32] = -0.9056785992780041;
+      w[32] = 0.04960950763777947;
+      r[33] = -0.9056785992780041;
+      s[33] = -0.6223323379479978;
+      t[33] = -0.6223323379479978;
+      w[33] = 0.04960950763777947;
+      r[34] = 0.1503432751739998;
+      s[34] = -0.9056785992780041;
+      t[34] = -0.6223323379479977;
+      w[34] = 0.04960950763777947;
 
       break;
     }
-    case  8: {
-      r[0]  =-0.6320721895815339; s[0]  =-0.6320721895815339; t[0]  =-0.1037834312553985; w[0]  =  0.07440058157405982;
-      r[1]  =-0.6320721895815339; s[1]  =-0.1037834312553985; t[1]  =-0.6320721895815339; w[1]  =  0.07440058157405982;
-      r[2]  =-0.1037834312553985; s[2]  =-0.6320721895815339; t[2]  =-0.6320721895815339; w[2]  =  0.07440058157405982;
-      r[3]  =-0.6320721895815339; s[3]  =-0.6320721895815339; t[3]  =-0.6320721895815339; w[3]  =  0.07440058157405982;
-      r[4]  = -0.923300199653955; s[4]  = -0.923300199653955; t[4]  = 0.7699005989618649; w[4]  = 0.007857765854252971;
-      r[5]  = -0.923300199653955; s[5]  = 0.7699005989618649; t[5]  = -0.923300199653955; w[5]  = 0.007857765854252971;
-      r[6]  =  0.769900598961865; s[6]  = -0.923300199653955; t[6]  = -0.923300199653955; w[6]  = 0.007857765854252971;
-      r[7]  = -0.923300199653955; s[7]  = -0.923300199653955; t[7]  = -0.923300199653955; w[7]  = 0.007857765854252971;
-      r[8]  =-0.8009956129757766; s[8]  =-0.8009956129757766; t[8]  = 0.4029868389273299; w[8]  =  0.03149884873824373;
-      r[9]  =-0.8009956129757766; s[9]  = 0.4029868389273299; t[9]  =-0.8009956129757766; w[9]  =  0.03149884873824373;
-      r[10] = 0.4029868389273298; s[10] =-0.8009956129757766; t[10] =-0.8009956129757766; w[10] =  0.03149884873824373;
-      r[11] =-0.8009956129757766; s[11] =-0.8009956129757766; t[11] =-0.8009956129757766; w[11] =  0.03149884873824373;
-      r[12] =-0.3707849034682734; s[12] =-0.3707849034682734; t[12] =-0.8876452895951799; w[12] =  0.05270161842714149;
-      r[13] =-0.3707849034682734; s[13] =-0.8876452895951799; t[13] =-0.3707849034682734; w[13] =  0.05270161842714149;
-      r[14] =-0.8876452895951799; s[14] =-0.3707849034682734; t[14] =-0.3707849034682734; w[14] =  0.05270161842714149;
-      r[15] =-0.3707849034682734; s[15] =-0.3707849034682734; t[15] =-0.3707849034682734; w[15] =  0.05270161842714149;
-      r[16] =-0.1260500583716688; s[16] =-0.8739499416283312; t[16] =-0.8739499416283312; w[16] =  0.04730584876233031;
-      r[17] =-0.8739499416283312; s[17] =-0.1260500583716688; t[17] =-0.8739499416283312; w[17] =  0.04730584876233031;
-      r[18] =-0.1260500583716688; s[18] =-0.1260500583716688; t[18] =-0.8739499416283312; w[18] =  0.04730584876233031;
-      r[19] =-0.1260500583716688; s[19] =-0.8739499416283312; t[19] =-0.1260500583716688; w[19] =  0.04730584876233031;
-      r[20] =-0.8739499416283312; s[20] =-0.1260500583716688; t[20] =-0.1260500583716688; w[20] =  0.04730584876233031;
-      r[21] =-0.8739499416283312; s[21] =-0.8739499416283312; t[21] =-0.1260500583716688; w[21] =  0.04730584876233031;
-      r[22] = 0.1583084315814429; s[22] =-0.5906770163268148; t[22] =-0.9769543989278133; w[22] =   0.0223681938462459;
-      r[23] = 0.1583084315814429; s[23] =-0.5906770163268148; t[23] =-0.5906770163268148; w[23] =   0.0223681938462459;
-      r[24] =-0.5906770163268148; s[24] =-0.5906770163268148; t[24] = 0.1583084315814429; w[24] =   0.0223681938462459;
-      r[25] =-0.9769543989278133; s[25] = 0.1583084315814429; t[25] =-0.5906770163268148; w[25] =   0.0223681938462459;
-      r[26] =-0.5906770163268148; s[26] =-0.9769543989278133; t[26] = 0.1583084315814429; w[26] =   0.0223681938462459;
-      r[27] =-0.5906770163268148; s[27] = 0.1583084315814429; t[27] =-0.5906770163268148; w[27] =   0.0223681938462459;
-      r[28] =-0.9769543989278133; s[28] =-0.5906770163268148; t[28] = 0.1583084315814429; w[28] =   0.0223681938462459;
-      r[29] =-0.5906770163268148; s[29] =-0.9769543989278133; t[29] =-0.5906770163268148; w[29] =   0.0223681938462459;
-      r[30] =-0.5906770163268148; s[30] =-0.5906770163268148; t[30] =-0.9769543989278133; w[30] =   0.0223681938462459;
-      r[31] =-0.5906770163268148; s[31] = 0.1583084315814429; t[31] =-0.9769543989278133; w[31] =   0.0223681938462459;
-      r[32] =-0.9769543989278133; s[32] =-0.5906770163268148; t[32] =-0.5906770163268148; w[32] =   0.0223681938462459;
-      r[33] = 0.1583084315814429; s[33] =-0.9769543989278133; t[33] =-0.5906770163268148; w[33] =   0.0223681938462459;
-      r[34] = 0.4419106530449903; s[34] =-0.9563482048314847; t[34] =-0.5292142433820209; w[34] = 0.009603721352467381;
-      r[35] = 0.4419106530449903; s[35] =-0.9563482048314847; t[35] =-0.9563482048314847; w[35] = 0.009603721352467381;
-      r[36] =-0.9563482048314847; s[36] =-0.9563482048314847; t[36] = 0.4419106530449902; w[36] = 0.009603721352467381;
-      r[37] =-0.5292142433820209; s[37] = 0.4419106530449903; t[37] =-0.9563482048314847; w[37] = 0.009603721352467381;
-      r[38] =-0.9563482048314847; s[38] =-0.5292142433820209; t[38] = 0.4419106530449903; w[38] = 0.009603721352467381;
-      r[39] =-0.9563482048314847; s[39] = 0.4419106530449902; t[39] =-0.9563482048314847; w[39] = 0.009603721352467381;
-      r[40] =-0.5292142433820209; s[40] =-0.9563482048314847; t[40] = 0.4419106530449903; w[40] = 0.009603721352467381;
-      r[41] =-0.9563482048314849; s[41] =-0.5292142433820208; t[41] =-0.9563482048314847; w[41] = 0.009603721352467381;
-      r[42] =-0.9563482048314849; s[42] =-0.9563482048314847; t[42] =-0.5292142433820208; w[42] = 0.009603721352467381;
-      r[43] =-0.9563482048314847; s[43] = 0.4419106530449903; t[43] =-0.5292142433820209; w[43] = 0.009603721352467381;
-      r[44] =-0.5292142433820208; s[44] =-0.9563482048314847; t[44] =-0.9563482048314847; w[44] = 0.009603721352467381;
-      r[45] = 0.4419106530449903; s[45] =-0.5292142433820209; t[45] =-0.9563482048314847; w[45] = 0.009603721352467381;
+    case 8: {
+      r[0] = -0.6320721895815339;
+      s[0] = -0.6320721895815339;
+      t[0] = -0.1037834312553985;
+      w[0] = 0.07440058157405982;
+      r[1] = -0.6320721895815339;
+      s[1] = -0.1037834312553985;
+      t[1] = -0.6320721895815339;
+      w[1] = 0.07440058157405982;
+      r[2] = -0.1037834312553985;
+      s[2] = -0.6320721895815339;
+      t[2] = -0.6320721895815339;
+      w[2] = 0.07440058157405982;
+      r[3] = -0.6320721895815339;
+      s[3] = -0.6320721895815339;
+      t[3] = -0.6320721895815339;
+      w[3] = 0.07440058157405982;
+      r[4] = -0.923300199653955;
+      s[4] = -0.923300199653955;
+      t[4] = 0.7699005989618649;
+      w[4] = 0.007857765854252971;
+      r[5] = -0.923300199653955;
+      s[5] = 0.7699005989618649;
+      t[5] = -0.923300199653955;
+      w[5] = 0.007857765854252971;
+      r[6] = 0.769900598961865;
+      s[6] = -0.923300199653955;
+      t[6] = -0.923300199653955;
+      w[6] = 0.007857765854252971;
+      r[7] = -0.923300199653955;
+      s[7] = -0.923300199653955;
+      t[7] = -0.923300199653955;
+      w[7] = 0.007857765854252971;
+      r[8] = -0.8009956129757766;
+      s[8] = -0.8009956129757766;
+      t[8] = 0.4029868389273299;
+      w[8] = 0.03149884873824373;
+      r[9] = -0.8009956129757766;
+      s[9] = 0.4029868389273299;
+      t[9] = -0.8009956129757766;
+      w[9] = 0.03149884873824373;
+      r[10] = 0.4029868389273298;
+      s[10] = -0.8009956129757766;
+      t[10] = -0.8009956129757766;
+      w[10] = 0.03149884873824373;
+      r[11] = -0.8009956129757766;
+      s[11] = -0.8009956129757766;
+      t[11] = -0.8009956129757766;
+      w[11] = 0.03149884873824373;
+      r[12] = -0.3707849034682734;
+      s[12] = -0.3707849034682734;
+      t[12] = -0.8876452895951799;
+      w[12] = 0.05270161842714149;
+      r[13] = -0.3707849034682734;
+      s[13] = -0.8876452895951799;
+      t[13] = -0.3707849034682734;
+      w[13] = 0.05270161842714149;
+      r[14] = -0.8876452895951799;
+      s[14] = -0.3707849034682734;
+      t[14] = -0.3707849034682734;
+      w[14] = 0.05270161842714149;
+      r[15] = -0.3707849034682734;
+      s[15] = -0.3707849034682734;
+      t[15] = -0.3707849034682734;
+      w[15] = 0.05270161842714149;
+      r[16] = -0.1260500583716688;
+      s[16] = -0.8739499416283312;
+      t[16] = -0.8739499416283312;
+      w[16] = 0.04730584876233031;
+      r[17] = -0.8739499416283312;
+      s[17] = -0.1260500583716688;
+      t[17] = -0.8739499416283312;
+      w[17] = 0.04730584876233031;
+      r[18] = -0.1260500583716688;
+      s[18] = -0.1260500583716688;
+      t[18] = -0.8739499416283312;
+      w[18] = 0.04730584876233031;
+      r[19] = -0.1260500583716688;
+      s[19] = -0.8739499416283312;
+      t[19] = -0.1260500583716688;
+      w[19] = 0.04730584876233031;
+      r[20] = -0.8739499416283312;
+      s[20] = -0.1260500583716688;
+      t[20] = -0.1260500583716688;
+      w[20] = 0.04730584876233031;
+      r[21] = -0.8739499416283312;
+      s[21] = -0.8739499416283312;
+      t[21] = -0.1260500583716688;
+      w[21] = 0.04730584876233031;
+      r[22] = 0.1583084315814429;
+      s[22] = -0.5906770163268148;
+      t[22] = -0.9769543989278133;
+      w[22] = 0.0223681938462459;
+      r[23] = 0.1583084315814429;
+      s[23] = -0.5906770163268148;
+      t[23] = -0.5906770163268148;
+      w[23] = 0.0223681938462459;
+      r[24] = -0.5906770163268148;
+      s[24] = -0.5906770163268148;
+      t[24] = 0.1583084315814429;
+      w[24] = 0.0223681938462459;
+      r[25] = -0.9769543989278133;
+      s[25] = 0.1583084315814429;
+      t[25] = -0.5906770163268148;
+      w[25] = 0.0223681938462459;
+      r[26] = -0.5906770163268148;
+      s[26] = -0.9769543989278133;
+      t[26] = 0.1583084315814429;
+      w[26] = 0.0223681938462459;
+      r[27] = -0.5906770163268148;
+      s[27] = 0.1583084315814429;
+      t[27] = -0.5906770163268148;
+      w[27] = 0.0223681938462459;
+      r[28] = -0.9769543989278133;
+      s[28] = -0.5906770163268148;
+      t[28] = 0.1583084315814429;
+      w[28] = 0.0223681938462459;
+      r[29] = -0.5906770163268148;
+      s[29] = -0.9769543989278133;
+      t[29] = -0.5906770163268148;
+      w[29] = 0.0223681938462459;
+      r[30] = -0.5906770163268148;
+      s[30] = -0.5906770163268148;
+      t[30] = -0.9769543989278133;
+      w[30] = 0.0223681938462459;
+      r[31] = -0.5906770163268148;
+      s[31] = 0.1583084315814429;
+      t[31] = -0.9769543989278133;
+      w[31] = 0.0223681938462459;
+      r[32] = -0.9769543989278133;
+      s[32] = -0.5906770163268148;
+      t[32] = -0.5906770163268148;
+      w[32] = 0.0223681938462459;
+      r[33] = 0.1583084315814429;
+      s[33] = -0.9769543989278133;
+      t[33] = -0.5906770163268148;
+      w[33] = 0.0223681938462459;
+      r[34] = 0.4419106530449903;
+      s[34] = -0.9563482048314847;
+      t[34] = -0.5292142433820209;
+      w[34] = 0.009603721352467381;
+      r[35] = 0.4419106530449903;
+      s[35] = -0.9563482048314847;
+      t[35] = -0.9563482048314847;
+      w[35] = 0.009603721352467381;
+      r[36] = -0.9563482048314847;
+      s[36] = -0.9563482048314847;
+      t[36] = 0.4419106530449902;
+      w[36] = 0.009603721352467381;
+      r[37] = -0.5292142433820209;
+      s[37] = 0.4419106530449903;
+      t[37] = -0.9563482048314847;
+      w[37] = 0.009603721352467381;
+      r[38] = -0.9563482048314847;
+      s[38] = -0.5292142433820209;
+      t[38] = 0.4419106530449903;
+      w[38] = 0.009603721352467381;
+      r[39] = -0.9563482048314847;
+      s[39] = 0.4419106530449902;
+      t[39] = -0.9563482048314847;
+      w[39] = 0.009603721352467381;
+      r[40] = -0.5292142433820209;
+      s[40] = -0.9563482048314847;
+      t[40] = 0.4419106530449903;
+      w[40] = 0.009603721352467381;
+      r[41] = -0.9563482048314849;
+      s[41] = -0.5292142433820208;
+      t[41] = -0.9563482048314847;
+      w[41] = 0.009603721352467381;
+      r[42] = -0.9563482048314849;
+      s[42] = -0.9563482048314847;
+      t[42] = -0.5292142433820208;
+      w[42] = 0.009603721352467381;
+      r[43] = -0.9563482048314847;
+      s[43] = 0.4419106530449903;
+      t[43] = -0.5292142433820209;
+      w[43] = 0.009603721352467381;
+      r[44] = -0.5292142433820208;
+      s[44] = -0.9563482048314847;
+      t[44] = -0.9563482048314847;
+      w[44] = 0.009603721352467381;
+      r[45] = 0.4419106530449903;
+      s[45] = -0.5292142433820209;
+      t[45] = -0.9563482048314847;
+      w[45] = 0.009603721352467381;
 
       break;
     }
-    case  9: {
-      r[0]  =                -0.5; s[0]  =                -0.5; t[0]  =                -0.5; w[0]  =  0.07327761647615459;
-      r[1]  = -0.8198449760801311; s[1]  = -0.8198449760801311; t[1]  =   0.459534928240393; w[1]  = 0.002848036499465571;
-      r[2]  = -0.8198449760801311; s[2]  =   0.459534928240393; t[2]  = -0.8198449760801311; w[2]  = 0.002848036499465571;
-      r[3]  =   0.459534928240393; s[3]  = -0.8198449760801311; t[3]  = -0.8198449760801311; w[3]  = 0.002848036499465571;
-      r[4]  = -0.8198449760801311; s[4]  = -0.8198449760801311; t[4]  = -0.8198449760801311; w[4]  = 0.002848036499465571;
-      r[5]  = -0.9160617305090143; s[5]  = -0.9160617305090143; t[5]  =  0.7481851915270431; w[5]  =  0.00957623445188957;
-      r[6]  = -0.9160617305090143; s[6]  =  0.7481851915270431; t[6]  = -0.9160617305090143; w[6]  =  0.00957623445188957;
-      r[7]  =  0.7481851915270431; s[7]  = -0.9160617305090143; t[7]  = -0.9160617305090143; w[7]  =  0.00957623445188957;
-      r[8]  = -0.9160617305090143; s[8]  = -0.9160617305090143; t[8]  = -0.9160617305090143; w[8]  =  0.00957623445188957;
-      r[9]  = -0.3560564433877504; s[9]  = -0.3560564433877504; t[9]  = -0.9318306698367487; w[9]  =  0.04059381195379974;
-      r[10] = -0.3560564433877504; s[10] = -0.9318306698367487; t[10] = -0.3560564433877504; w[10] =  0.04059381195379974;
-      r[11] = -0.9318306698367487; s[11] = -0.3560564433877504; t[11] = -0.3560564433877504; w[11] =  0.04059381195379974;
-      r[12] = -0.3560564433877504; s[12] = -0.3560564433877504; t[12] = -0.3560564433877504; w[12] =  0.04059381195379974;
-      r[13] =  -0.658427438836176; s[13] =  -0.658427438836176; t[13] =-0.02471768349147202; w[13] =  0.03397956979508031;
-      r[14] =  -0.658427438836176; s[14] =-0.02471768349147202; t[14] =  -0.658427438836176; w[14] =  0.03397956979508031;
-      r[15] =-0.02471768349147199; s[15] =  -0.658427438836176; t[15] =  -0.658427438836176; w[15] =  0.03397956979508031;
-      r[16] =  -0.658427438836176; s[16] =  -0.658427438836176; t[16] =  -0.658427438836176; w[16] =  0.03397956979508031;
-      r[17] = -0.2129618822280694; s[17] = -0.7870381177719306; t[17] = -0.7870381177719306; w[17] =  0.04875647105046832;
-      r[18] = -0.7870381177719306; s[18] = -0.2129618822280694; t[18] = -0.7870381177719306; w[18] =  0.04875647105046832;
-      r[19] = -0.2129618822280694; s[19] = -0.2129618822280694; t[19] = -0.7870381177719306; w[19] =  0.04875647105046832;
-      r[20] = -0.2129618822280694; s[20] = -0.7870381177719306; t[20] = -0.2129618822280694; w[20] =  0.04875647105046832;
-      r[21] = -0.7870381177719306; s[21] = -0.2129618822280694; t[21] = -0.2129618822280694; w[21] =  0.04875647105046832;
-      r[22] = -0.7870381177719306; s[22] = -0.7870381177719306; t[22] = -0.2129618822280694; w[22] =  0.04875647105046832;
-      r[23] =                -1.0; s[23] =-0.07906724107645879; t[23] = -0.8418655178470824; w[23] =  0.01022387218776507;
-      r[24] =                -1.0; s[24] =-0.07906724107645879; t[24] =-0.07906724107645879; w[24] =  0.01022387218776507;
-      r[25] =-0.07906724107645879; s[25] =-0.07906724107645879; t[25] =                -1.0; w[25] =  0.01022387218776507;
-      r[26] = -0.8418655178470824; s[26] =                -1.0; t[26] =-0.07906724107645879; w[26] =  0.01022387218776507;
-      r[27] =-0.07906724107645879; s[27] = -0.8418655178470824; t[27] =                -1.0; w[27] =  0.01022387218776507;
-      r[28] =-0.07906724107645879; s[28] =                -1.0; t[28] =-0.07906724107645879; w[28] =  0.01022387218776507;
-      r[29] = -0.8418655178470824; s[29] =-0.07906724107645879; t[29] =                -1.0; w[29] =  0.01022387218776507;
-      r[30] =-0.07906724107645879; s[30] = -0.8418655178470824; t[30] =-0.07906724107645879; w[30] =  0.01022387218776507;
-      r[31] =-0.07906724107645879; s[31] =-0.07906724107645879; t[31] = -0.8418655178470824; w[31] =  0.01022387218776507;
-      r[32] =-0.07906724107645879; s[32] =                -1.0; t[32] = -0.8418655178470824; w[32] =  0.01022387218776507;
-      r[33] = -0.8418655178470824; s[33] =-0.07906724107645879; t[33] =-0.07906724107645879; w[33] =  0.01022387218776507;
-      r[34] =                -1.0; s[34] = -0.8418655178470824; t[34] =-0.07906724107645879; w[34] =  0.01022387218776507;
-      r[35] =  0.1968616506697061; s[35] = -0.6334882372417514; t[35] = -0.9298851761862033; w[35] =  0.02791006448800061;
-      r[36] =  0.1968616506697061; s[36] = -0.6334882372417514; t[36] = -0.6334882372417514; w[36] =  0.02791006448800061;
-      r[37] = -0.6334882372417514; s[37] = -0.6334882372417514; t[37] =  0.1968616506697061; w[37] =  0.02791006448800061;
-      r[38] = -0.9298851761862033; s[38] =  0.1968616506697061; t[38] = -0.6334882372417514; w[38] =  0.02791006448800061;
-      r[39] = -0.6334882372417514; s[39] = -0.9298851761862033; t[39] =  0.1968616506697061; w[39] =  0.02791006448800061;
-      r[40] = -0.6334882372417514; s[40] =  0.1968616506697061; t[40] = -0.6334882372417514; w[40] =  0.02791006448800061;
-      r[41] = -0.9298851761862033; s[41] = -0.6334882372417514; t[41] =  0.1968616506697061; w[41] =  0.02791006448800061;
-      r[42] = -0.6334882372417514; s[42] = -0.9298851761862033; t[42] = -0.6334882372417514; w[42] =  0.02791006448800061;
-      r[43] = -0.6334882372417514; s[43] = -0.6334882372417514; t[43] = -0.9298851761862033; w[43] =  0.02791006448800061;
-      r[44] = -0.6334882372417514; s[44] =  0.1968616506697061; t[44] = -0.9298851761862033; w[44] =  0.02791006448800061;
-      r[45] = -0.9298851761862033; s[45] = -0.6334882372417514; t[45] = -0.6334882372417514; w[45] =  0.02791006448800061;
-      r[46] =  0.1968616506697061; s[46] = -0.9298851761862033; t[46] = -0.6334882372417514; w[46] =  0.02791006448800061;
-      r[47] =  0.4372341714004844; s[47] = -0.9329857011557074; t[47] = -0.5712627690890695; w[47] =  0.01349325330368666;
-      r[48] =  0.4372341714004844; s[48] = -0.9329857011557074; t[48] = -0.9329857011557074; w[48] =  0.01349325330368666;
-      r[49] = -0.9329857011557074; s[49] = -0.9329857011557074; t[49] =  0.4372341714004844; w[49] =  0.01349325330368666;
-      r[50] = -0.5712627690890695; s[50] =  0.4372341714004844; t[50] = -0.9329857011557074; w[50] =  0.01349325330368666;
-      r[51] = -0.9329857011557074; s[51] = -0.5712627690890695; t[51] =  0.4372341714004844; w[51] =  0.01349325330368666;
-      r[52] = -0.9329857011557074; s[52] =  0.4372341714004844; t[52] = -0.9329857011557074; w[52] =  0.01349325330368666;
-      r[53] = -0.5712627690890695; s[53] = -0.9329857011557074; t[53] =  0.4372341714004844; w[53] =  0.01349325330368666;
-      r[54] = -0.9329857011557074; s[54] = -0.5712627690890695; t[54] = -0.9329857011557074; w[54] =  0.01349325330368666;
-      r[55] = -0.9329857011557074; s[55] = -0.9329857011557074; t[55] = -0.5712627690890695; w[55] =  0.01349325330368666;
-      r[56] = -0.9329857011557074; s[56] =  0.4372341714004844; t[56] = -0.5712627690890695; w[56] =  0.01349325330368666;
-      r[57] = -0.5712627690890695; s[57] = -0.9329857011557074; t[57] = -0.9329857011557074; w[57] =  0.01349325330368666;
-      r[58] =  0.4372341714004844; s[58] = -0.5712627690890695; t[58] = -0.9329857011557074; w[58] =  0.01349325330368666;
+    case 9: {
+      r[0] = -0.5;
+      s[0] = -0.5;
+      t[0] = -0.5;
+      w[0] = 0.07327761647615459;
+      r[1] = -0.8198449760801311;
+      s[1] = -0.8198449760801311;
+      t[1] = 0.459534928240393;
+      w[1] = 0.002848036499465571;
+      r[2] = -0.8198449760801311;
+      s[2] = 0.459534928240393;
+      t[2] = -0.8198449760801311;
+      w[2] = 0.002848036499465571;
+      r[3] = 0.459534928240393;
+      s[3] = -0.8198449760801311;
+      t[3] = -0.8198449760801311;
+      w[3] = 0.002848036499465571;
+      r[4] = -0.8198449760801311;
+      s[4] = -0.8198449760801311;
+      t[4] = -0.8198449760801311;
+      w[4] = 0.002848036499465571;
+      r[5] = -0.9160617305090143;
+      s[5] = -0.9160617305090143;
+      t[5] = 0.7481851915270431;
+      w[5] = 0.00957623445188957;
+      r[6] = -0.9160617305090143;
+      s[6] = 0.7481851915270431;
+      t[6] = -0.9160617305090143;
+      w[6] = 0.00957623445188957;
+      r[7] = 0.7481851915270431;
+      s[7] = -0.9160617305090143;
+      t[7] = -0.9160617305090143;
+      w[7] = 0.00957623445188957;
+      r[8] = -0.9160617305090143;
+      s[8] = -0.9160617305090143;
+      t[8] = -0.9160617305090143;
+      w[8] = 0.00957623445188957;
+      r[9] = -0.3560564433877504;
+      s[9] = -0.3560564433877504;
+      t[9] = -0.9318306698367487;
+      w[9] = 0.04059381195379974;
+      r[10] = -0.3560564433877504;
+      s[10] = -0.9318306698367487;
+      t[10] = -0.3560564433877504;
+      w[10] = 0.04059381195379974;
+      r[11] = -0.9318306698367487;
+      s[11] = -0.3560564433877504;
+      t[11] = -0.3560564433877504;
+      w[11] = 0.04059381195379974;
+      r[12] = -0.3560564433877504;
+      s[12] = -0.3560564433877504;
+      t[12] = -0.3560564433877504;
+      w[12] = 0.04059381195379974;
+      r[13] = -0.658427438836176;
+      s[13] = -0.658427438836176;
+      t[13] = -0.02471768349147202;
+      w[13] = 0.03397956979508031;
+      r[14] = -0.658427438836176;
+      s[14] = -0.02471768349147202;
+      t[14] = -0.658427438836176;
+      w[14] = 0.03397956979508031;
+      r[15] = -0.02471768349147199;
+      s[15] = -0.658427438836176;
+      t[15] = -0.658427438836176;
+      w[15] = 0.03397956979508031;
+      r[16] = -0.658427438836176;
+      s[16] = -0.658427438836176;
+      t[16] = -0.658427438836176;
+      w[16] = 0.03397956979508031;
+      r[17] = -0.2129618822280694;
+      s[17] = -0.7870381177719306;
+      t[17] = -0.7870381177719306;
+      w[17] = 0.04875647105046832;
+      r[18] = -0.7870381177719306;
+      s[18] = -0.2129618822280694;
+      t[18] = -0.7870381177719306;
+      w[18] = 0.04875647105046832;
+      r[19] = -0.2129618822280694;
+      s[19] = -0.2129618822280694;
+      t[19] = -0.7870381177719306;
+      w[19] = 0.04875647105046832;
+      r[20] = -0.2129618822280694;
+      s[20] = -0.7870381177719306;
+      t[20] = -0.2129618822280694;
+      w[20] = 0.04875647105046832;
+      r[21] = -0.7870381177719306;
+      s[21] = -0.2129618822280694;
+      t[21] = -0.2129618822280694;
+      w[21] = 0.04875647105046832;
+      r[22] = -0.7870381177719306;
+      s[22] = -0.7870381177719306;
+      t[22] = -0.2129618822280694;
+      w[22] = 0.04875647105046832;
+      r[23] = -1.0;
+      s[23] = -0.07906724107645879;
+      t[23] = -0.8418655178470824;
+      w[23] = 0.01022387218776507;
+      r[24] = -1.0;
+      s[24] = -0.07906724107645879;
+      t[24] = -0.07906724107645879;
+      w[24] = 0.01022387218776507;
+      r[25] = -0.07906724107645879;
+      s[25] = -0.07906724107645879;
+      t[25] = -1.0;
+      w[25] = 0.01022387218776507;
+      r[26] = -0.8418655178470824;
+      s[26] = -1.0;
+      t[26] = -0.07906724107645879;
+      w[26] = 0.01022387218776507;
+      r[27] = -0.07906724107645879;
+      s[27] = -0.8418655178470824;
+      t[27] = -1.0;
+      w[27] = 0.01022387218776507;
+      r[28] = -0.07906724107645879;
+      s[28] = -1.0;
+      t[28] = -0.07906724107645879;
+      w[28] = 0.01022387218776507;
+      r[29] = -0.8418655178470824;
+      s[29] = -0.07906724107645879;
+      t[29] = -1.0;
+      w[29] = 0.01022387218776507;
+      r[30] = -0.07906724107645879;
+      s[30] = -0.8418655178470824;
+      t[30] = -0.07906724107645879;
+      w[30] = 0.01022387218776507;
+      r[31] = -0.07906724107645879;
+      s[31] = -0.07906724107645879;
+      t[31] = -0.8418655178470824;
+      w[31] = 0.01022387218776507;
+      r[32] = -0.07906724107645879;
+      s[32] = -1.0;
+      t[32] = -0.8418655178470824;
+      w[32] = 0.01022387218776507;
+      r[33] = -0.8418655178470824;
+      s[33] = -0.07906724107645879;
+      t[33] = -0.07906724107645879;
+      w[33] = 0.01022387218776507;
+      r[34] = -1.0;
+      s[34] = -0.8418655178470824;
+      t[34] = -0.07906724107645879;
+      w[34] = 0.01022387218776507;
+      r[35] = 0.1968616506697061;
+      s[35] = -0.6334882372417514;
+      t[35] = -0.9298851761862033;
+      w[35] = 0.02791006448800061;
+      r[36] = 0.1968616506697061;
+      s[36] = -0.6334882372417514;
+      t[36] = -0.6334882372417514;
+      w[36] = 0.02791006448800061;
+      r[37] = -0.6334882372417514;
+      s[37] = -0.6334882372417514;
+      t[37] = 0.1968616506697061;
+      w[37] = 0.02791006448800061;
+      r[38] = -0.9298851761862033;
+      s[38] = 0.1968616506697061;
+      t[38] = -0.6334882372417514;
+      w[38] = 0.02791006448800061;
+      r[39] = -0.6334882372417514;
+      s[39] = -0.9298851761862033;
+      t[39] = 0.1968616506697061;
+      w[39] = 0.02791006448800061;
+      r[40] = -0.6334882372417514;
+      s[40] = 0.1968616506697061;
+      t[40] = -0.6334882372417514;
+      w[40] = 0.02791006448800061;
+      r[41] = -0.9298851761862033;
+      s[41] = -0.6334882372417514;
+      t[41] = 0.1968616506697061;
+      w[41] = 0.02791006448800061;
+      r[42] = -0.6334882372417514;
+      s[42] = -0.9298851761862033;
+      t[42] = -0.6334882372417514;
+      w[42] = 0.02791006448800061;
+      r[43] = -0.6334882372417514;
+      s[43] = -0.6334882372417514;
+      t[43] = -0.9298851761862033;
+      w[43] = 0.02791006448800061;
+      r[44] = -0.6334882372417514;
+      s[44] = 0.1968616506697061;
+      t[44] = -0.9298851761862033;
+      w[44] = 0.02791006448800061;
+      r[45] = -0.9298851761862033;
+      s[45] = -0.6334882372417514;
+      t[45] = -0.6334882372417514;
+      w[45] = 0.02791006448800061;
+      r[46] = 0.1968616506697061;
+      s[46] = -0.9298851761862033;
+      t[46] = -0.6334882372417514;
+      w[46] = 0.02791006448800061;
+      r[47] = 0.4372341714004844;
+      s[47] = -0.9329857011557074;
+      t[47] = -0.5712627690890695;
+      w[47] = 0.01349325330368666;
+      r[48] = 0.4372341714004844;
+      s[48] = -0.9329857011557074;
+      t[48] = -0.9329857011557074;
+      w[48] = 0.01349325330368666;
+      r[49] = -0.9329857011557074;
+      s[49] = -0.9329857011557074;
+      t[49] = 0.4372341714004844;
+      w[49] = 0.01349325330368666;
+      r[50] = -0.5712627690890695;
+      s[50] = 0.4372341714004844;
+      t[50] = -0.9329857011557074;
+      w[50] = 0.01349325330368666;
+      r[51] = -0.9329857011557074;
+      s[51] = -0.5712627690890695;
+      t[51] = 0.4372341714004844;
+      w[51] = 0.01349325330368666;
+      r[52] = -0.9329857011557074;
+      s[52] = 0.4372341714004844;
+      t[52] = -0.9329857011557074;
+      w[52] = 0.01349325330368666;
+      r[53] = -0.5712627690890695;
+      s[53] = -0.9329857011557074;
+      t[53] = 0.4372341714004844;
+      w[53] = 0.01349325330368666;
+      r[54] = -0.9329857011557074;
+      s[54] = -0.5712627690890695;
+      t[54] = -0.9329857011557074;
+      w[54] = 0.01349325330368666;
+      r[55] = -0.9329857011557074;
+      s[55] = -0.9329857011557074;
+      t[55] = -0.5712627690890695;
+      w[55] = 0.01349325330368666;
+      r[56] = -0.9329857011557074;
+      s[56] = 0.4372341714004844;
+      t[56] = -0.5712627690890695;
+      w[56] = 0.01349325330368666;
+      r[57] = -0.5712627690890695;
+      s[57] = -0.9329857011557074;
+      t[57] = -0.9329857011557074;
+      w[57] = 0.01349325330368666;
+      r[58] = 0.4372341714004844;
+      s[58] = -0.5712627690890695;
+      t[58] = -0.9329857011557074;
+      w[58] = 0.01349325330368666;
 
       break;
     }
     case 10: {
-      r[0]  =                -0.5; s[0]  =                -0.5; t[0]  =                -0.5; w[0]  =  0.06111729903668942;
-      r[1]  = -0.3902379693282467; s[1]  = -0.3902379693282467; t[1]  =   -0.82928609201526; w[1]  =  0.03648653859255376;
-      r[2]  = -0.3902379693282467; s[2]  =   -0.82928609201526; t[2]  = -0.3902379693282467; w[2]  =  0.03648653859255376;
-      r[3]  =   -0.82928609201526; s[3]  = -0.3902379693282467; t[3]  = -0.3902379693282467; w[3]  =  0.03648653859255376;
-      r[4]  = -0.3902379693282467; s[4]  = -0.3902379693282467; t[4]  = -0.3902379693282467; w[4]  =  0.03648653859255376;
-      r[5]  = -0.8646773501288808; s[5]  = -0.8646773501288808; t[5]  =  0.5940320503866422; w[5]  =  0.01772043697176758;
-      r[6]  = -0.8646773501288808; s[6]  =  0.5940320503866422; t[6]  = -0.8646773501288808; w[6]  =  0.01772043697176758;
-      r[7]  =  0.5940320503866422; s[7]  = -0.8646773501288808; t[7]  = -0.8646773501288808; w[7]  =  0.01772043697176758;
-      r[8]  = -0.8646773501288808; s[8]  = -0.8646773501288808; t[8]  = -0.8646773501288808; w[8]  =  0.01772043697176758;
-      r[9]  = -0.9473346828260848; s[9]  =-0.05266531717391518; t[9]  =-0.05266531717391518; w[9]  =  0.00811057586155056;
-      r[10] =-0.05266531717391519; s[10] = -0.9473346828260848; t[10] =-0.05266531717391519; w[10] =  0.00811057586155056;
-      r[11] = -0.9473346828260848; s[11] = -0.9473346828260848; t[11] = -0.0526653171739152; w[11] =  0.00811057586155056;
-      r[12] = -0.9473346828260848; s[12] = -0.0526653171739152; t[12] = -0.9473346828260848; w[12] =  0.00811057586155056;
-      r[13] =-0.05266531717391515; s[13] = -0.9473346828260848; t[13] = -0.9473346828260848; w[13] =  0.00811057586155056;
-      r[14] =-0.05266531717391519; s[14] =-0.05266531717391519; t[14] = -0.9473346828260848; w[14] =  0.00811057586155056;
-      r[15] = -0.2038789111878272; s[15] = -0.7961210888121728; t[15] = -0.7961210888121728; w[15] =  0.03066711559292157;
-      r[16] = -0.7961210888121728; s[16] = -0.2038789111878272; t[16] = -0.7961210888121728; w[16] =  0.03066711559292157;
-      r[17] = -0.2038789111878272; s[17] = -0.2038789111878272; t[17] = -0.7961210888121728; w[17] =  0.03066711559292157;
-      r[18] = -0.2038789111878272; s[18] = -0.7961210888121728; t[18] = -0.2038789111878272; w[18] =  0.03066711559292157;
-      r[19] = -0.7961210888121728; s[19] = -0.2038789111878272; t[19] = -0.2038789111878272; w[19] =  0.03066711559292157;
-      r[20] = -0.7961210888121728; s[20] = -0.7961210888121728; t[20] = -0.2038789111878272; w[20] =  0.03066711559292157;
-      r[21] = 0.06411454763598279; s[21] = -0.6048469883044114; t[21] =   -0.85442057102716; w[21] =  0.03277830640502917;
-      r[22] = 0.06411454763598282; s[22] = -0.6048469883044114; t[22] = -0.6048469883044114; w[22] =  0.03277830640502917;
-      r[23] = -0.6048469883044114; s[23] = -0.6048469883044114; t[23] = 0.06411454763598282; w[23] =  0.03277830640502917;
-      r[24] =   -0.85442057102716; s[24] = 0.06411454763598279; t[24] = -0.6048469883044114; w[24] =  0.03277830640502917;
-      r[25] = -0.6048469883044114; s[25] =   -0.85442057102716; t[25] = 0.06411454763598279; w[25] =  0.03277830640502917;
-      r[26] = -0.6048469883044114; s[26] = 0.06411454763598282; t[26] = -0.6048469883044114; w[26] =  0.03277830640502917;
-      r[27] =   -0.85442057102716; s[27] = -0.6048469883044114; t[27] = 0.06411454763598279; w[27] =  0.03277830640502917;
-      r[28] = -0.6048469883044114; s[28] =   -0.85442057102716; t[28] = -0.6048469883044114; w[28] =  0.03277830640502917;
-      r[29] = -0.6048469883044114; s[29] = -0.6048469883044114; t[29] =   -0.85442057102716; w[29] =  0.03277830640502917;
-      r[30] = -0.6048469883044114; s[30] = 0.06411454763598279; t[30] =   -0.85442057102716; w[30] =  0.03277830640502917;
-      r[31] =   -0.85442057102716; s[31] = -0.6048469883044114; t[31] = -0.6048469883044114; w[31] =  0.03277830640502917;
-      r[32] = 0.06411454763598279; s[32] =   -0.85442057102716; t[32] = -0.6048469883044114; w[32] =  0.03277830640502917;
-      r[33] =  0.8117588817115982; s[33] =                -1.0; t[33] = -0.8117588817115982; w[33] = 0.001276432944056112;
-      r[34] =  0.8117588817115982; s[34] =                -1.0; t[34] =                -1.0; w[34] = 0.001276432944056112;
-      r[35] =                -1.0; s[35] =                -1.0; t[35] =  0.8117588817115982; w[35] = 0.001276432944056112;
-      r[36] = -0.8117588817115982; s[36] =  0.8117588817115982; t[36] =                -1.0; w[36] = 0.001276432944056112;
-      r[37] =                -1.0; s[37] = -0.8117588817115982; t[37] =  0.8117588817115982; w[37] = 0.001276432944056112;
-      r[38] =                -1.0; s[38] =  0.8117588817115982; t[38] =                -1.0; w[38] = 0.001276432944056112;
-      r[39] = -0.8117588817115982; s[39] =                -1.0; t[39] =  0.8117588817115982; w[39] = 0.001276432944056112;
-      r[40] =                -1.0; s[40] = -0.8117588817115982; t[40] =                -1.0; w[40] = 0.001276432944056112;
-      r[41] =                -1.0; s[41] =                -1.0; t[41] = -0.8117588817115982; w[41] = 0.001276432944056112;
-      r[42] =                -1.0; s[42] =  0.8117588817115982; t[42] = -0.8117588817115982; w[42] = 0.001276432944056112;
-      r[43] = -0.8117588817115982; s[43] =                -1.0; t[43] =                -1.0; w[43] = 0.001276432944056112;
-      r[44] =  0.8117588817115982; s[44] = -0.8117588817115982; t[44] =                -1.0; w[44] = 0.001276432944056112;
-      r[45] =  0.3854615068170896; s[45] = -0.6928701162511337; t[45] = -0.9997212743148225; w[45] = 0.006560363793425748;
-      r[46] =  0.3854615068170896; s[46] = -0.6928701162511336; t[46] = -0.6928701162511336; w[46] = 0.006560363793425748;
-      r[47] = -0.6928701162511337; s[47] = -0.6928701162511335; t[47] =  0.3854615068170896; w[47] = 0.006560363793425748;
-      r[48] = -0.9997212743148225; s[48] =  0.3854615068170896; t[48] = -0.6928701162511335; w[48] = 0.006560363793425748;
-      r[49] = -0.6928701162511335; s[49] = -0.9997212743148225; t[49] =  0.3854615068170896; w[49] = 0.006560363793425748;
-      r[50] = -0.6928701162511337; s[50] =  0.3854615068170896; t[50] = -0.6928701162511335; w[50] = 0.006560363793425748;
-      r[51] = -0.9997212743148225; s[51] = -0.6928701162511335; t[51] =  0.3854615068170896; w[51] = 0.006560363793425748;
-      r[52] = -0.6928701162511337; s[52] = -0.9997212743148225; t[52] = -0.6928701162511337; w[52] = 0.006560363793425748;
-      r[53] = -0.6928701162511337; s[53] = -0.6928701162511337; t[53] = -0.9997212743148225; w[53] = 0.006560363793425748;
-      r[54] = -0.6928701162511335; s[54] =  0.3854615068170896; t[54] = -0.9997212743148225; w[54] = 0.006560363793425748;
-      r[55] = -0.9997212743148225; s[55] = -0.6928701162511336; t[55] = -0.6928701162511336; w[55] = 0.006560363793425748;
-      r[56] =  0.3854615068170896; s[56] = -0.9997212743148225; t[56] = -0.6928701162511337; w[56] = 0.006560363793425748;
-      r[57] = -0.6460142846738401; s[57] = -0.1823369737573523; t[57] = -0.9893117678114551; w[57] =  0.01289761909705229;
-      r[58] = -0.6460142846738401; s[58] = -0.1823369737573524; t[58] = -0.1823369737573524; w[58] =  0.01289761909705229;
-      r[59] = -0.1823369737573524; s[59] = -0.1823369737573524; t[59] = -0.6460142846738401; w[59] =  0.01289761909705229;
-      r[60] = -0.9893117678114551; s[60] = -0.6460142846738401; t[60] = -0.1823369737573524; w[60] =  0.01289761909705229;
-      r[61] = -0.1823369737573524; s[61] = -0.9893117678114551; t[61] = -0.6460142846738401; w[61] =  0.01289761909705229;
-      r[62] = -0.1823369737573524; s[62] = -0.6460142846738401; t[62] = -0.1823369737573524; w[62] =  0.01289761909705229;
-      r[63] = -0.9893117678114551; s[63] = -0.1823369737573524; t[63] = -0.6460142846738401; w[63] =  0.01289761909705229;
-      r[64] = -0.1823369737573523; s[64] = -0.9893117678114551; t[64] = -0.1823369737573523; w[64] =  0.01289761909705229;
-      r[65] = -0.1823369737573523; s[65] = -0.1823369737573523; t[65] = -0.9893117678114551; w[65] =  0.01289761909705229;
-      r[66] = -0.1823369737573524; s[66] = -0.6460142846738401; t[66] = -0.9893117678114551; w[66] =  0.01289761909705229;
-      r[67] = -0.9893117678114551; s[67] = -0.1823369737573524; t[67] = -0.1823369737573524; w[67] =  0.01289761909705229;
-      r[68] = -0.6460142846738401; s[68] = -0.9893117678114551; t[68] = -0.1823369737573523; w[68] =  0.01289761909705229;
-      r[69] =  0.3166885452555603; s[69] = -0.9215201459821879; t[69] = -0.4736482532911847; w[69] =  0.01504744303648042;
-      r[70] =  0.3166885452555603; s[70] = -0.9215201459821878; t[70] = -0.9215201459821878; w[70] =  0.01504744303648042;
-      r[71] = -0.9215201459821878; s[71] = -0.9215201459821878; t[71] =  0.3166885452555603; w[71] =  0.01504744303648042;
-      r[72] = -0.4736482532911847; s[72] =  0.3166885452555603; t[72] = -0.9215201459821878; w[72] =  0.01504744303648042;
-      r[73] = -0.9215201459821878; s[73] = -0.4736482532911847; t[73] =  0.3166885452555603; w[73] =  0.01504744303648042;
-      r[74] = -0.9215201459821878; s[74] =  0.3166885452555603; t[74] = -0.9215201459821878; w[74] =  0.01504744303648042;
-      r[75] = -0.4736482532911847; s[75] = -0.9215201459821878; t[75] =  0.3166885452555603; w[75] =  0.01504744303648042;
-      r[76] = -0.9215201459821878; s[76] = -0.4736482532911847; t[76] = -0.9215201459821878; w[76] =  0.01504744303648042;
-      r[77] = -0.9215201459821878; s[77] = -0.9215201459821878; t[77] = -0.4736482532911847; w[77] =  0.01504744303648042;
-      r[78] = -0.9215201459821878; s[78] =  0.3166885452555603; t[78] = -0.4736482532911847; w[78] =  0.01504744303648042;
-      r[79] = -0.4736482532911847; s[79] = -0.9215201459821878; t[79] = -0.9215201459821878; w[79] =  0.01504744303648042;
-      r[80] =  0.3166885452555603; s[80] = -0.4736482532911847; t[80] = -0.9215201459821879; w[80] =  0.01504744303648042;
+      r[0] = -0.5;
+      s[0] = -0.5;
+      t[0] = -0.5;
+      w[0] = 0.06111729903668942;
+      r[1] = -0.3902379693282467;
+      s[1] = -0.3902379693282467;
+      t[1] = -0.82928609201526;
+      w[1] = 0.03648653859255376;
+      r[2] = -0.3902379693282467;
+      s[2] = -0.82928609201526;
+      t[2] = -0.3902379693282467;
+      w[2] = 0.03648653859255376;
+      r[3] = -0.82928609201526;
+      s[3] = -0.3902379693282467;
+      t[3] = -0.3902379693282467;
+      w[3] = 0.03648653859255376;
+      r[4] = -0.3902379693282467;
+      s[4] = -0.3902379693282467;
+      t[4] = -0.3902379693282467;
+      w[4] = 0.03648653859255376;
+      r[5] = -0.8646773501288808;
+      s[5] = -0.8646773501288808;
+      t[5] = 0.5940320503866422;
+      w[5] = 0.01772043697176758;
+      r[6] = -0.8646773501288808;
+      s[6] = 0.5940320503866422;
+      t[6] = -0.8646773501288808;
+      w[6] = 0.01772043697176758;
+      r[7] = 0.5940320503866422;
+      s[7] = -0.8646773501288808;
+      t[7] = -0.8646773501288808;
+      w[7] = 0.01772043697176758;
+      r[8] = -0.8646773501288808;
+      s[8] = -0.8646773501288808;
+      t[8] = -0.8646773501288808;
+      w[8] = 0.01772043697176758;
+      r[9] = -0.9473346828260848;
+      s[9] = -0.05266531717391518;
+      t[9] = -0.05266531717391518;
+      w[9] = 0.00811057586155056;
+      r[10] = -0.05266531717391519;
+      s[10] = -0.9473346828260848;
+      t[10] = -0.05266531717391519;
+      w[10] = 0.00811057586155056;
+      r[11] = -0.9473346828260848;
+      s[11] = -0.9473346828260848;
+      t[11] = -0.0526653171739152;
+      w[11] = 0.00811057586155056;
+      r[12] = -0.9473346828260848;
+      s[12] = -0.0526653171739152;
+      t[12] = -0.9473346828260848;
+      w[12] = 0.00811057586155056;
+      r[13] = -0.05266531717391515;
+      s[13] = -0.9473346828260848;
+      t[13] = -0.9473346828260848;
+      w[13] = 0.00811057586155056;
+      r[14] = -0.05266531717391519;
+      s[14] = -0.05266531717391519;
+      t[14] = -0.9473346828260848;
+      w[14] = 0.00811057586155056;
+      r[15] = -0.2038789111878272;
+      s[15] = -0.7961210888121728;
+      t[15] = -0.7961210888121728;
+      w[15] = 0.03066711559292157;
+      r[16] = -0.7961210888121728;
+      s[16] = -0.2038789111878272;
+      t[16] = -0.7961210888121728;
+      w[16] = 0.03066711559292157;
+      r[17] = -0.2038789111878272;
+      s[17] = -0.2038789111878272;
+      t[17] = -0.7961210888121728;
+      w[17] = 0.03066711559292157;
+      r[18] = -0.2038789111878272;
+      s[18] = -0.7961210888121728;
+      t[18] = -0.2038789111878272;
+      w[18] = 0.03066711559292157;
+      r[19] = -0.7961210888121728;
+      s[19] = -0.2038789111878272;
+      t[19] = -0.2038789111878272;
+      w[19] = 0.03066711559292157;
+      r[20] = -0.7961210888121728;
+      s[20] = -0.7961210888121728;
+      t[20] = -0.2038789111878272;
+      w[20] = 0.03066711559292157;
+      r[21] = 0.06411454763598279;
+      s[21] = -0.6048469883044114;
+      t[21] = -0.85442057102716;
+      w[21] = 0.03277830640502917;
+      r[22] = 0.06411454763598282;
+      s[22] = -0.6048469883044114;
+      t[22] = -0.6048469883044114;
+      w[22] = 0.03277830640502917;
+      r[23] = -0.6048469883044114;
+      s[23] = -0.6048469883044114;
+      t[23] = 0.06411454763598282;
+      w[23] = 0.03277830640502917;
+      r[24] = -0.85442057102716;
+      s[24] = 0.06411454763598279;
+      t[24] = -0.6048469883044114;
+      w[24] = 0.03277830640502917;
+      r[25] = -0.6048469883044114;
+      s[25] = -0.85442057102716;
+      t[25] = 0.06411454763598279;
+      w[25] = 0.03277830640502917;
+      r[26] = -0.6048469883044114;
+      s[26] = 0.06411454763598282;
+      t[26] = -0.6048469883044114;
+      w[26] = 0.03277830640502917;
+      r[27] = -0.85442057102716;
+      s[27] = -0.6048469883044114;
+      t[27] = 0.06411454763598279;
+      w[27] = 0.03277830640502917;
+      r[28] = -0.6048469883044114;
+      s[28] = -0.85442057102716;
+      t[28] = -0.6048469883044114;
+      w[28] = 0.03277830640502917;
+      r[29] = -0.6048469883044114;
+      s[29] = -0.6048469883044114;
+      t[29] = -0.85442057102716;
+      w[29] = 0.03277830640502917;
+      r[30] = -0.6048469883044114;
+      s[30] = 0.06411454763598279;
+      t[30] = -0.85442057102716;
+      w[30] = 0.03277830640502917;
+      r[31] = -0.85442057102716;
+      s[31] = -0.6048469883044114;
+      t[31] = -0.6048469883044114;
+      w[31] = 0.03277830640502917;
+      r[32] = 0.06411454763598279;
+      s[32] = -0.85442057102716;
+      t[32] = -0.6048469883044114;
+      w[32] = 0.03277830640502917;
+      r[33] = 0.8117588817115982;
+      s[33] = -1.0;
+      t[33] = -0.8117588817115982;
+      w[33] = 0.001276432944056112;
+      r[34] = 0.8117588817115982;
+      s[34] = -1.0;
+      t[34] = -1.0;
+      w[34] = 0.001276432944056112;
+      r[35] = -1.0;
+      s[35] = -1.0;
+      t[35] = 0.8117588817115982;
+      w[35] = 0.001276432944056112;
+      r[36] = -0.8117588817115982;
+      s[36] = 0.8117588817115982;
+      t[36] = -1.0;
+      w[36] = 0.001276432944056112;
+      r[37] = -1.0;
+      s[37] = -0.8117588817115982;
+      t[37] = 0.8117588817115982;
+      w[37] = 0.001276432944056112;
+      r[38] = -1.0;
+      s[38] = 0.8117588817115982;
+      t[38] = -1.0;
+      w[38] = 0.001276432944056112;
+      r[39] = -0.8117588817115982;
+      s[39] = -1.0;
+      t[39] = 0.8117588817115982;
+      w[39] = 0.001276432944056112;
+      r[40] = -1.0;
+      s[40] = -0.8117588817115982;
+      t[40] = -1.0;
+      w[40] = 0.001276432944056112;
+      r[41] = -1.0;
+      s[41] = -1.0;
+      t[41] = -0.8117588817115982;
+      w[41] = 0.001276432944056112;
+      r[42] = -1.0;
+      s[42] = 0.8117588817115982;
+      t[42] = -0.8117588817115982;
+      w[42] = 0.001276432944056112;
+      r[43] = -0.8117588817115982;
+      s[43] = -1.0;
+      t[43] = -1.0;
+      w[43] = 0.001276432944056112;
+      r[44] = 0.8117588817115982;
+      s[44] = -0.8117588817115982;
+      t[44] = -1.0;
+      w[44] = 0.001276432944056112;
+      r[45] = 0.3854615068170896;
+      s[45] = -0.6928701162511337;
+      t[45] = -0.9997212743148225;
+      w[45] = 0.006560363793425748;
+      r[46] = 0.3854615068170896;
+      s[46] = -0.6928701162511336;
+      t[46] = -0.6928701162511336;
+      w[46] = 0.006560363793425748;
+      r[47] = -0.6928701162511337;
+      s[47] = -0.6928701162511335;
+      t[47] = 0.3854615068170896;
+      w[47] = 0.006560363793425748;
+      r[48] = -0.9997212743148225;
+      s[48] = 0.3854615068170896;
+      t[48] = -0.6928701162511335;
+      w[48] = 0.006560363793425748;
+      r[49] = -0.6928701162511335;
+      s[49] = -0.9997212743148225;
+      t[49] = 0.3854615068170896;
+      w[49] = 0.006560363793425748;
+      r[50] = -0.6928701162511337;
+      s[50] = 0.3854615068170896;
+      t[50] = -0.6928701162511335;
+      w[50] = 0.006560363793425748;
+      r[51] = -0.9997212743148225;
+      s[51] = -0.6928701162511335;
+      t[51] = 0.3854615068170896;
+      w[51] = 0.006560363793425748;
+      r[52] = -0.6928701162511337;
+      s[52] = -0.9997212743148225;
+      t[52] = -0.6928701162511337;
+      w[52] = 0.006560363793425748;
+      r[53] = -0.6928701162511337;
+      s[53] = -0.6928701162511337;
+      t[53] = -0.9997212743148225;
+      w[53] = 0.006560363793425748;
+      r[54] = -0.6928701162511335;
+      s[54] = 0.3854615068170896;
+      t[54] = -0.9997212743148225;
+      w[54] = 0.006560363793425748;
+      r[55] = -0.9997212743148225;
+      s[55] = -0.6928701162511336;
+      t[55] = -0.6928701162511336;
+      w[55] = 0.006560363793425748;
+      r[56] = 0.3854615068170896;
+      s[56] = -0.9997212743148225;
+      t[56] = -0.6928701162511337;
+      w[56] = 0.006560363793425748;
+      r[57] = -0.6460142846738401;
+      s[57] = -0.1823369737573523;
+      t[57] = -0.9893117678114551;
+      w[57] = 0.01289761909705229;
+      r[58] = -0.6460142846738401;
+      s[58] = -0.1823369737573524;
+      t[58] = -0.1823369737573524;
+      w[58] = 0.01289761909705229;
+      r[59] = -0.1823369737573524;
+      s[59] = -0.1823369737573524;
+      t[59] = -0.6460142846738401;
+      w[59] = 0.01289761909705229;
+      r[60] = -0.9893117678114551;
+      s[60] = -0.6460142846738401;
+      t[60] = -0.1823369737573524;
+      w[60] = 0.01289761909705229;
+      r[61] = -0.1823369737573524;
+      s[61] = -0.9893117678114551;
+      t[61] = -0.6460142846738401;
+      w[61] = 0.01289761909705229;
+      r[62] = -0.1823369737573524;
+      s[62] = -0.6460142846738401;
+      t[62] = -0.1823369737573524;
+      w[62] = 0.01289761909705229;
+      r[63] = -0.9893117678114551;
+      s[63] = -0.1823369737573524;
+      t[63] = -0.6460142846738401;
+      w[63] = 0.01289761909705229;
+      r[64] = -0.1823369737573523;
+      s[64] = -0.9893117678114551;
+      t[64] = -0.1823369737573523;
+      w[64] = 0.01289761909705229;
+      r[65] = -0.1823369737573523;
+      s[65] = -0.1823369737573523;
+      t[65] = -0.9893117678114551;
+      w[65] = 0.01289761909705229;
+      r[66] = -0.1823369737573524;
+      s[66] = -0.6460142846738401;
+      t[66] = -0.9893117678114551;
+      w[66] = 0.01289761909705229;
+      r[67] = -0.9893117678114551;
+      s[67] = -0.1823369737573524;
+      t[67] = -0.1823369737573524;
+      w[67] = 0.01289761909705229;
+      r[68] = -0.6460142846738401;
+      s[68] = -0.9893117678114551;
+      t[68] = -0.1823369737573523;
+      w[68] = 0.01289761909705229;
+      r[69] = 0.3166885452555603;
+      s[69] = -0.9215201459821879;
+      t[69] = -0.4736482532911847;
+      w[69] = 0.01504744303648042;
+      r[70] = 0.3166885452555603;
+      s[70] = -0.9215201459821878;
+      t[70] = -0.9215201459821878;
+      w[70] = 0.01504744303648042;
+      r[71] = -0.9215201459821878;
+      s[71] = -0.9215201459821878;
+      t[71] = 0.3166885452555603;
+      w[71] = 0.01504744303648042;
+      r[72] = -0.4736482532911847;
+      s[72] = 0.3166885452555603;
+      t[72] = -0.9215201459821878;
+      w[72] = 0.01504744303648042;
+      r[73] = -0.9215201459821878;
+      s[73] = -0.4736482532911847;
+      t[73] = 0.3166885452555603;
+      w[73] = 0.01504744303648042;
+      r[74] = -0.9215201459821878;
+      s[74] = 0.3166885452555603;
+      t[74] = -0.9215201459821878;
+      w[74] = 0.01504744303648042;
+      r[75] = -0.4736482532911847;
+      s[75] = -0.9215201459821878;
+      t[75] = 0.3166885452555603;
+      w[75] = 0.01504744303648042;
+      r[76] = -0.9215201459821878;
+      s[76] = -0.4736482532911847;
+      t[76] = -0.9215201459821878;
+      w[76] = 0.01504744303648042;
+      r[77] = -0.9215201459821878;
+      s[77] = -0.9215201459821878;
+      t[77] = -0.4736482532911847;
+      w[77] = 0.01504744303648042;
+      r[78] = -0.9215201459821878;
+      s[78] = 0.3166885452555603;
+      t[78] = -0.4736482532911847;
+      w[78] = 0.01504744303648042;
+      r[79] = -0.4736482532911847;
+      s[79] = -0.9215201459821878;
+      t[79] = -0.9215201459821878;
+      w[79] = 0.01504744303648042;
+      r[80] = 0.3166885452555603;
+      s[80] = -0.4736482532911847;
+      t[80] = -0.9215201459821879;
+      w[80] = 0.01504744303648042;
 
       break;
     }
     case 11: {
-      r[0]   =                -0.5; s[0]   =                -0.5; t[0]   =                -0.5; w[0]   =  0.03784683898277254;
-      r[1]   =  -0.397380485851065; s[1]   =  -0.397380485851065; t[1]   =  -0.807858542446805; w[1]   =  0.03166744105497066;
-      r[2]   =  -0.397380485851065; s[2]   =  -0.807858542446805; t[2]   =  -0.397380485851065; w[2]   =  0.03166744105497066;
-      r[3]   =  -0.807858542446805; s[3]   =  -0.397380485851065; t[3]   =  -0.397380485851065; w[3]   =  0.03166744105497066;
-      r[4]   =  -0.397380485851065; s[4]   =  -0.397380485851065; t[4]   =  -0.397380485851065; w[4]   =  0.03166744105497066;
-      r[5]   = -0.3448885483183461; s[5]   = -0.3448885483183461; t[5]   = -0.9653343550449618; w[5]   =  0.01522419400512382;
-      r[6]   = -0.3448885483183461; s[6]   = -0.9653343550449618; t[6]   = -0.3448885483183461; w[6]   =  0.01522419400512382;
-      r[7]   = -0.9653343550449618; s[7]   = -0.3448885483183461; t[7]   = -0.3448885483183461; w[7]   =  0.01522419400512382;
-      r[8]   = -0.3448885483183461; s[8]   = -0.3448885483183461; t[8]   = -0.3448885483183461; w[8]   =  0.01522419400512382;
-      r[9]   = -0.9428094459201933; s[9]   = -0.0571905540798067; t[9]   = -0.0571905540798067; w[9]   = 0.009963593188767755;
-      r[10]  =-0.05719055407980668; s[10]  = -0.9428094459201934; t[10]  =-0.05719055407980668; w[10]  = 0.009963593188767755;
-      r[11]  = -0.9428094459201933; s[11]  = -0.9428094459201933; t[11]  =-0.05719055407980667; w[11]  = 0.009963593188767755;
-      r[12]  = -0.9428094459201933; s[12]  =-0.05719055407980667; t[12]  = -0.9428094459201933; w[12]  = 0.009963593188767755;
-      r[13]  =-0.05719055407980672; s[13]  = -0.9428094459201933; t[13]  = -0.9428094459201933; w[13]  = 0.009963593188767755;
-      r[14]  =-0.05719055407980668; s[14]  =-0.05719055407980668; t[14]  = -0.9428094459201934; w[14]  = 0.009963593188767755;
-      r[15]  = -0.2544420245972532; s[15]  = -0.7455579754027468; t[15]  = -0.7455579754027468; w[15]  =  0.02286217079043096;
-      r[16]  = -0.7455579754027468; s[16]  = -0.2544420245972532; t[16]  = -0.7455579754027468; w[16]  =  0.02286217079043096;
-      r[17]  = -0.2544420245972532; s[17]  = -0.2544420245972532; t[17]  = -0.7455579754027468; w[17]  =  0.02286217079043096;
-      r[18]  = -0.2544420245972532; s[18]  = -0.7455579754027468; t[18]  = -0.2544420245972532; w[18]  =  0.02286217079043096;
-      r[19]  = -0.7455579754027468; s[19]  = -0.2544420245972532; t[19]  = -0.2544420245972532; w[19]  =  0.02286217079043096;
-      r[20]  = -0.7455579754027468; s[20]  = -0.7455579754027468; t[20]  = -0.2544420245972532; w[20]  =  0.02286217079043096;
-      r[21]  =  0.5227647114364038; s[21]  = -0.7755897474786564; t[21]  =  -0.971585216479091; w[21]  = 0.004639621843157262;
-      r[22]  =  0.5227647114364038; s[22]  = -0.7755897474786564; t[22]  = -0.7755897474786564; w[22]  = 0.004639621843157262;
-      r[23]  = -0.7755897474786564; s[23]  = -0.7755897474786564; t[23]  =  0.5227647114364038; w[23]  = 0.004639621843157262;
-      r[24]  =  -0.971585216479091; s[24]  =  0.5227647114364038; t[24]  = -0.7755897474786564; w[24]  = 0.004639621843157262;
-      r[25]  = -0.7755897474786564; s[25]  =  -0.971585216479091; t[25]  =  0.5227647114364038; w[25]  = 0.004639621843157262;
-      r[26]  = -0.7755897474786564; s[26]  =  0.5227647114364038; t[26]  = -0.7755897474786564; w[26]  = 0.004639621843157262;
-      r[27]  =  -0.971585216479091; s[27]  = -0.7755897474786564; t[27]  =  0.5227647114364038; w[27]  = 0.004639621843157262;
-      r[28]  = -0.7755897474786564; s[28]  =  -0.971585216479091; t[28]  = -0.7755897474786564; w[28]  = 0.004639621843157262;
-      r[29]  = -0.7755897474786564; s[29]  = -0.7755897474786564; t[29]  =  -0.971585216479091; w[29]  = 0.004639621843157262;
-      r[30]  = -0.7755897474786564; s[30]  =  0.5227647114364038; t[30]  =  -0.971585216479091; w[30]  = 0.004639621843157262;
-      r[31]  =  -0.971585216479091; s[31]  = -0.7755897474786564; t[31]  = -0.7755897474786564; w[31]  = 0.004639621843157262;
-      r[32]  =  0.5227647114364038; s[32]  =  -0.971585216479091; t[32]  = -0.7755897474786564; w[32]  = 0.004639621843157262;
-      r[33]  =  0.7831995665077649; s[33]  = -0.9669551040900525; t[33]  = -0.8492893583276598; w[33]  = 0.002112278397796427;
-      r[34]  =  0.7831995665077649; s[34]  = -0.9669551040900525; t[34]  = -0.9669551040900525; w[34]  = 0.002112278397796427;
-      r[35]  = -0.9669551040900525; s[35]  = -0.9669551040900525; t[35]  =   0.783199566507765; w[35]  = 0.002112278397796427;
-      r[36]  = -0.8492893583276598; s[36]  =   0.783199566507765; t[36]  = -0.9669551040900525; w[36]  = 0.002112278397796427;
-      r[37]  = -0.9669551040900525; s[37]  = -0.8492893583276598; t[37]  =   0.783199566507765; w[37]  = 0.002112278397796427;
-      r[38]  = -0.9669551040900525; s[38]  =   0.783199566507765; t[38]  = -0.9669551040900525; w[38]  = 0.002112278397796427;
-      r[39]  = -0.8492893583276598; s[39]  = -0.9669551040900525; t[39]  =   0.783199566507765; w[39]  = 0.002112278397796427;
-      r[40]  = -0.9669551040900525; s[40]  = -0.8492893583276598; t[40]  = -0.9669551040900525; w[40]  = 0.002112278397796427;
-      r[41]  = -0.9669551040900525; s[41]  = -0.9669551040900525; t[41]  = -0.8492893583276598; w[41]  = 0.002112278397796427;
-      r[42]  = -0.9669551040900525; s[42]  =   0.783199566507765; t[42]  = -0.8492893583276598; w[42]  = 0.002112278397796427;
-      r[43]  = -0.8492893583276598; s[43]  = -0.9669551040900525; t[43]  = -0.9669551040900525; w[43]  = 0.002112278397796427;
-      r[44]  =  0.7831995665077649; s[44]  = -0.8492893583276598; t[44]  = -0.9669551040900525; w[44]  = 0.002112278397796427;
-      r[45]  =  0.4152874915976885; s[45]  = -0.7537734583743153; t[45]  = -0.9077405748490578; w[45]  = 0.008720212321831882;
-      r[46]  =  0.4152874915976886; s[46]  = -0.7537734583743154; t[46]  = -0.7537734583743154; w[46]  = 0.008720212321831882;
-      r[47]  = -0.7537734583743154; s[47]  = -0.7537734583743154; t[47]  =  0.4152874915976886; w[47]  = 0.008720212321831882;
-      r[48]  = -0.9077405748490577; s[48]  =  0.4152874915976885; t[48]  = -0.7537734583743154; w[48]  = 0.008720212321831882;
-      r[49]  = -0.7537734583743154; s[49]  = -0.9077405748490577; t[49]  =  0.4152874915976885; w[49]  = 0.008720212321831882;
-      r[50]  = -0.7537734583743154; s[50]  =  0.4152874915976886; t[50]  = -0.7537734583743154; w[50]  = 0.008720212321831882;
-      r[51]  = -0.9077405748490577; s[51]  = -0.7537734583743154; t[51]  =  0.4152874915976885; w[51]  = 0.008720212321831882;
-      r[52]  = -0.7537734583743154; s[52]  = -0.9077405748490577; t[52]  = -0.7537734583743154; w[52]  = 0.008720212321831882;
-      r[53]  = -0.7537734583743154; s[53]  = -0.7537734583743154; t[53]  = -0.9077405748490577; w[53]  = 0.008720212321831882;
-      r[54]  = -0.7537734583743154; s[54]  =  0.4152874915976885; t[54]  = -0.9077405748490577; w[54]  = 0.008720212321831882;
-      r[55]  = -0.9077405748490578; s[55]  = -0.7537734583743154; t[55]  = -0.7537734583743154; w[55]  = 0.008720212321831882;
-      r[56]  =  0.4152874915976885; s[56]  = -0.9077405748490578; t[56]  = -0.7537734583743153; w[56]  = 0.008720212321831882;
-      r[57]  = 0.02508211404942551; s[57]  = -0.7430319617668262; t[57]  = -0.5390181905157732; w[57]  =  0.01923782271792721;
-      r[58]  = 0.02508211404942554; s[58]  = -0.7430319617668262; t[58]  = -0.7430319617668262; w[58]  =  0.01923782271792721;
-      r[59]  = -0.7430319617668262; s[59]  = -0.7430319617668262; t[59]  = 0.02508211404942554; w[59]  =  0.01923782271792721;
-      r[60]  = -0.5390181905157732; s[60]  = 0.02508211404942554; t[60]  = -0.7430319617668262; w[60]  =  0.01923782271792721;
-      r[61]  = -0.7430319617668262; s[61]  = -0.5390181905157732; t[61]  = 0.02508211404942551; w[61]  =  0.01923782271792721;
-      r[62]  = -0.7430319617668262; s[62]  = 0.02508211404942554; t[62]  = -0.7430319617668262; w[62]  =  0.01923782271792721;
-      r[63]  = -0.5390181905157732; s[63]  = -0.7430319617668262; t[63]  = 0.02508211404942554; w[63]  =  0.01923782271792721;
-      r[64]  = -0.7430319617668262; s[64]  = -0.5390181905157732; t[64]  = -0.7430319617668262; w[64]  =  0.01923782271792721;
-      r[65]  = -0.7430319617668262; s[65]  = -0.7430319617668262; t[65]  = -0.5390181905157732; w[65]  =  0.01923782271792721;
-      r[66]  = -0.7430319617668262; s[66]  = 0.02508211404942551; t[66]  = -0.5390181905157732; w[66]  =  0.01923782271792721;
-      r[67]  = -0.5390181905157732; s[67]  = -0.7430319617668262; t[67]  = -0.7430319617668262; w[67]  =  0.01923782271792721;
-      r[68]  = 0.02508211404942551; s[68]  = -0.5390181905157732; t[68]  = -0.7430319617668262; w[68]  =  0.01923782271792721;
-      r[69]  =  0.4045657634046023; s[69]  = -0.9481462410143495; t[69]  = -0.5082732813759032; w[69]  = 0.007336665507925923;
-      r[70]  =  0.4045657634046023; s[70]  = -0.9481462410143495; t[70]  = -0.9481462410143495; w[70]  = 0.007336665507925923;
-      r[71]  = -0.9481462410143495; s[71]  = -0.9481462410143495; t[71]  =  0.4045657634046023; w[71]  = 0.007336665507925923;
-      r[72]  = -0.5082732813759032; s[72]  =  0.4045657634046023; t[72]  = -0.9481462410143495; w[72]  = 0.007336665507925923;
-      r[73]  = -0.9481462410143495; s[73]  = -0.5082732813759032; t[73]  =  0.4045657634046023; w[73]  = 0.007336665507925923;
-      r[74]  = -0.9481462410143495; s[74]  =  0.4045657634046023; t[74]  = -0.9481462410143495; w[74]  = 0.007336665507925923;
-      r[75]  = -0.5082732813759032; s[75]  = -0.9481462410143495; t[75]  =  0.4045657634046023; w[75]  = 0.007336665507925923;
-      r[76]  = -0.9481462410143495; s[76]  = -0.5082732813759032; t[76]  = -0.9481462410143495; w[76]  = 0.007336665507925923;
-      r[77]  = -0.9481462410143495; s[77]  = -0.9481462410143495; t[77]  = -0.5082732813759032; w[77]  = 0.007336665507925923;
-      r[78]  = -0.9481462410143495; s[78]  =  0.4045657634046023; t[78]  = -0.5082732813759032; w[78]  = 0.007336665507925923;
-      r[79]  = -0.5082732813759032; s[79]  = -0.9481462410143495; t[79]  = -0.9481462410143495; w[79]  = 0.007336665507925923;
-      r[80]  =  0.4045657634046023; s[80]  = -0.5082732813759032; t[80]  = -0.9481462410143495; w[80]  = 0.007336665507925923;
-      r[81]  = 0.06079123224408745; s[81]  = -0.9501658362591827; t[81]  = -0.7183474030028485; w[81]  =  0.01693359003213852;
-      r[82]  = -0.9501658362591827; s[82]  = -0.7183474030028485; t[82]  =  0.0607912322440875; w[82]  =  0.01693359003213852;
-      r[83]  = -0.9501658362591827; s[83]  =  0.0607912322440875; t[83]  = -0.7183474030028485; w[83]  =  0.01693359003213852;
-      r[84]  = -0.7183474030028484; s[84]  = 0.06079123224408749; t[84]  = -0.3922779929820564; w[84]  =  0.01693359003213852;
-      r[85]  = -0.7183474030028485; s[85]  =  0.0607912322440875; t[85]  = -0.9501658362591828; w[85]  =  0.01693359003213852;
-      r[86]  = -0.3922779929820563; s[86]  = 0.06079123224408749; t[86]  = -0.7183474030028484; w[86]  =  0.01693359003213852;
-      r[87]  = -0.7183474030028485; s[87]  = -0.9501658362591827; t[87]  = -0.3922779929820564; w[87]  =  0.01693359003213852;
-      r[88]  = -0.7183474030028484; s[88]  = -0.3922779929820564; t[88]  = 0.06079123224408749; w[88]  =  0.01693359003213852;
-      r[89]  = -0.3922779929820565; s[89]  = -0.9501658362591827; t[89]  = -0.7183474030028485; w[89]  =  0.01693359003213852;
-      r[90]  =  0.0607912322440875; s[90]  = -0.9501658362591827; t[90]  = -0.3922779929820564; w[90]  =  0.01693359003213852;
-      r[91]  = -0.3922779929820564; s[91]  =  0.0607912322440875; t[91]  = -0.9501658362591827; w[91]  =  0.01693359003213852;
-      r[92]  = -0.7183474030028485; s[92]  = -0.9501658362591828; t[92]  =  0.0607912322440875; w[92]  =  0.01693359003213852;
-      r[93]  = -0.3922779929820564; s[93]  = -0.9501658362591827; t[93]  =  0.0607912322440875; w[93]  =  0.01693359003213852;
-      r[94]  = 0.06079123224408749; s[94]  = -0.3922779929820564; t[94]  = -0.7183474030028484; w[94]  =  0.01693359003213852;
-      r[95]  = -0.7183474030028485; s[95]  = -0.3922779929820564; t[95]  = -0.9501658362591827; w[95]  =  0.01693359003213852;
-      r[96]  = -0.9501658362591827; s[96]  = -0.3922779929820565; t[96]  = -0.7183474030028485; w[96]  =  0.01693359003213852;
-      r[97]  =  0.0607912322440875; s[97]  = -0.3922779929820564; t[97]  = -0.9501658362591827; w[97]  =  0.01693359003213852;
-      r[98]  = -0.9501658362591827; s[98]  = -0.3922779929820564; t[98]  = 0.06079123224408747; w[98]  =  0.01693359003213852;
-      r[99]  = -0.9501658362591827; s[99]  = 0.06079123224408747; t[99]  = -0.3922779929820564; w[99]  =  0.01693359003213852;
-      r[100] = -0.3922779929820563; s[100] = -0.7183474030028484; t[100] = 0.06079123224408749; w[100] =  0.01693359003213852;
-      r[101] = 0.06079123224408749; s[101] = -0.7183474030028484; t[101] = -0.3922779929820564; w[101] =  0.01693359003213852;
-      r[102] = 0.06079123224408745; s[102] = -0.7183474030028485; t[102] = -0.9501658362591827; w[102] =  0.01693359003213852;
-      r[103] = -0.9501658362591827; s[103] = -0.7183474030028485; t[103] = -0.3922779929820565; w[103] =  0.01693359003213852;
-      r[104] = -0.3922779929820565; s[104] = -0.7183474030028485; t[104] = -0.9501658362591827; w[104] =  0.01693359003213852;
+      r[0] = -0.5;
+      s[0] = -0.5;
+      t[0] = -0.5;
+      w[0] = 0.03784683898277254;
+      r[1] = -0.397380485851065;
+      s[1] = -0.397380485851065;
+      t[1] = -0.807858542446805;
+      w[1] = 0.03166744105497066;
+      r[2] = -0.397380485851065;
+      s[2] = -0.807858542446805;
+      t[2] = -0.397380485851065;
+      w[2] = 0.03166744105497066;
+      r[3] = -0.807858542446805;
+      s[3] = -0.397380485851065;
+      t[3] = -0.397380485851065;
+      w[3] = 0.03166744105497066;
+      r[4] = -0.397380485851065;
+      s[4] = -0.397380485851065;
+      t[4] = -0.397380485851065;
+      w[4] = 0.03166744105497066;
+      r[5] = -0.3448885483183461;
+      s[5] = -0.3448885483183461;
+      t[5] = -0.9653343550449618;
+      w[5] = 0.01522419400512382;
+      r[6] = -0.3448885483183461;
+      s[6] = -0.9653343550449618;
+      t[6] = -0.3448885483183461;
+      w[6] = 0.01522419400512382;
+      r[7] = -0.9653343550449618;
+      s[7] = -0.3448885483183461;
+      t[7] = -0.3448885483183461;
+      w[7] = 0.01522419400512382;
+      r[8] = -0.3448885483183461;
+      s[8] = -0.3448885483183461;
+      t[8] = -0.3448885483183461;
+      w[8] = 0.01522419400512382;
+      r[9] = -0.9428094459201933;
+      s[9] = -0.0571905540798067;
+      t[9] = -0.0571905540798067;
+      w[9] = 0.009963593188767755;
+      r[10] = -0.05719055407980668;
+      s[10] = -0.9428094459201934;
+      t[10] = -0.05719055407980668;
+      w[10] = 0.009963593188767755;
+      r[11] = -0.9428094459201933;
+      s[11] = -0.9428094459201933;
+      t[11] = -0.05719055407980667;
+      w[11] = 0.009963593188767755;
+      r[12] = -0.9428094459201933;
+      s[12] = -0.05719055407980667;
+      t[12] = -0.9428094459201933;
+      w[12] = 0.009963593188767755;
+      r[13] = -0.05719055407980672;
+      s[13] = -0.9428094459201933;
+      t[13] = -0.9428094459201933;
+      w[13] = 0.009963593188767755;
+      r[14] = -0.05719055407980668;
+      s[14] = -0.05719055407980668;
+      t[14] = -0.9428094459201934;
+      w[14] = 0.009963593188767755;
+      r[15] = -0.2544420245972532;
+      s[15] = -0.7455579754027468;
+      t[15] = -0.7455579754027468;
+      w[15] = 0.02286217079043096;
+      r[16] = -0.7455579754027468;
+      s[16] = -0.2544420245972532;
+      t[16] = -0.7455579754027468;
+      w[16] = 0.02286217079043096;
+      r[17] = -0.2544420245972532;
+      s[17] = -0.2544420245972532;
+      t[17] = -0.7455579754027468;
+      w[17] = 0.02286217079043096;
+      r[18] = -0.2544420245972532;
+      s[18] = -0.7455579754027468;
+      t[18] = -0.2544420245972532;
+      w[18] = 0.02286217079043096;
+      r[19] = -0.7455579754027468;
+      s[19] = -0.2544420245972532;
+      t[19] = -0.2544420245972532;
+      w[19] = 0.02286217079043096;
+      r[20] = -0.7455579754027468;
+      s[20] = -0.7455579754027468;
+      t[20] = -0.2544420245972532;
+      w[20] = 0.02286217079043096;
+      r[21] = 0.5227647114364038;
+      s[21] = -0.7755897474786564;
+      t[21] = -0.971585216479091;
+      w[21] = 0.004639621843157262;
+      r[22] = 0.5227647114364038;
+      s[22] = -0.7755897474786564;
+      t[22] = -0.7755897474786564;
+      w[22] = 0.004639621843157262;
+      r[23] = -0.7755897474786564;
+      s[23] = -0.7755897474786564;
+      t[23] = 0.5227647114364038;
+      w[23] = 0.004639621843157262;
+      r[24] = -0.971585216479091;
+      s[24] = 0.5227647114364038;
+      t[24] = -0.7755897474786564;
+      w[24] = 0.004639621843157262;
+      r[25] = -0.7755897474786564;
+      s[25] = -0.971585216479091;
+      t[25] = 0.5227647114364038;
+      w[25] = 0.004639621843157262;
+      r[26] = -0.7755897474786564;
+      s[26] = 0.5227647114364038;
+      t[26] = -0.7755897474786564;
+      w[26] = 0.004639621843157262;
+      r[27] = -0.971585216479091;
+      s[27] = -0.7755897474786564;
+      t[27] = 0.5227647114364038;
+      w[27] = 0.004639621843157262;
+      r[28] = -0.7755897474786564;
+      s[28] = -0.971585216479091;
+      t[28] = -0.7755897474786564;
+      w[28] = 0.004639621843157262;
+      r[29] = -0.7755897474786564;
+      s[29] = -0.7755897474786564;
+      t[29] = -0.971585216479091;
+      w[29] = 0.004639621843157262;
+      r[30] = -0.7755897474786564;
+      s[30] = 0.5227647114364038;
+      t[30] = -0.971585216479091;
+      w[30] = 0.004639621843157262;
+      r[31] = -0.971585216479091;
+      s[31] = -0.7755897474786564;
+      t[31] = -0.7755897474786564;
+      w[31] = 0.004639621843157262;
+      r[32] = 0.5227647114364038;
+      s[32] = -0.971585216479091;
+      t[32] = -0.7755897474786564;
+      w[32] = 0.004639621843157262;
+      r[33] = 0.7831995665077649;
+      s[33] = -0.9669551040900525;
+      t[33] = -0.8492893583276598;
+      w[33] = 0.002112278397796427;
+      r[34] = 0.7831995665077649;
+      s[34] = -0.9669551040900525;
+      t[34] = -0.9669551040900525;
+      w[34] = 0.002112278397796427;
+      r[35] = -0.9669551040900525;
+      s[35] = -0.9669551040900525;
+      t[35] = 0.783199566507765;
+      w[35] = 0.002112278397796427;
+      r[36] = -0.8492893583276598;
+      s[36] = 0.783199566507765;
+      t[36] = -0.9669551040900525;
+      w[36] = 0.002112278397796427;
+      r[37] = -0.9669551040900525;
+      s[37] = -0.8492893583276598;
+      t[37] = 0.783199566507765;
+      w[37] = 0.002112278397796427;
+      r[38] = -0.9669551040900525;
+      s[38] = 0.783199566507765;
+      t[38] = -0.9669551040900525;
+      w[38] = 0.002112278397796427;
+      r[39] = -0.8492893583276598;
+      s[39] = -0.9669551040900525;
+      t[39] = 0.783199566507765;
+      w[39] = 0.002112278397796427;
+      r[40] = -0.9669551040900525;
+      s[40] = -0.8492893583276598;
+      t[40] = -0.9669551040900525;
+      w[40] = 0.002112278397796427;
+      r[41] = -0.9669551040900525;
+      s[41] = -0.9669551040900525;
+      t[41] = -0.8492893583276598;
+      w[41] = 0.002112278397796427;
+      r[42] = -0.9669551040900525;
+      s[42] = 0.783199566507765;
+      t[42] = -0.8492893583276598;
+      w[42] = 0.002112278397796427;
+      r[43] = -0.8492893583276598;
+      s[43] = -0.9669551040900525;
+      t[43] = -0.9669551040900525;
+      w[43] = 0.002112278397796427;
+      r[44] = 0.7831995665077649;
+      s[44] = -0.8492893583276598;
+      t[44] = -0.9669551040900525;
+      w[44] = 0.002112278397796427;
+      r[45] = 0.4152874915976885;
+      s[45] = -0.7537734583743153;
+      t[45] = -0.9077405748490578;
+      w[45] = 0.008720212321831882;
+      r[46] = 0.4152874915976886;
+      s[46] = -0.7537734583743154;
+      t[46] = -0.7537734583743154;
+      w[46] = 0.008720212321831882;
+      r[47] = -0.7537734583743154;
+      s[47] = -0.7537734583743154;
+      t[47] = 0.4152874915976886;
+      w[47] = 0.008720212321831882;
+      r[48] = -0.9077405748490577;
+      s[48] = 0.4152874915976885;
+      t[48] = -0.7537734583743154;
+      w[48] = 0.008720212321831882;
+      r[49] = -0.7537734583743154;
+      s[49] = -0.9077405748490577;
+      t[49] = 0.4152874915976885;
+      w[49] = 0.008720212321831882;
+      r[50] = -0.7537734583743154;
+      s[50] = 0.4152874915976886;
+      t[50] = -0.7537734583743154;
+      w[50] = 0.008720212321831882;
+      r[51] = -0.9077405748490577;
+      s[51] = -0.7537734583743154;
+      t[51] = 0.4152874915976885;
+      w[51] = 0.008720212321831882;
+      r[52] = -0.7537734583743154;
+      s[52] = -0.9077405748490577;
+      t[52] = -0.7537734583743154;
+      w[52] = 0.008720212321831882;
+      r[53] = -0.7537734583743154;
+      s[53] = -0.7537734583743154;
+      t[53] = -0.9077405748490577;
+      w[53] = 0.008720212321831882;
+      r[54] = -0.7537734583743154;
+      s[54] = 0.4152874915976885;
+      t[54] = -0.9077405748490577;
+      w[54] = 0.008720212321831882;
+      r[55] = -0.9077405748490578;
+      s[55] = -0.7537734583743154;
+      t[55] = -0.7537734583743154;
+      w[55] = 0.008720212321831882;
+      r[56] = 0.4152874915976885;
+      s[56] = -0.9077405748490578;
+      t[56] = -0.7537734583743153;
+      w[56] = 0.008720212321831882;
+      r[57] = 0.02508211404942551;
+      s[57] = -0.7430319617668262;
+      t[57] = -0.5390181905157732;
+      w[57] = 0.01923782271792721;
+      r[58] = 0.02508211404942554;
+      s[58] = -0.7430319617668262;
+      t[58] = -0.7430319617668262;
+      w[58] = 0.01923782271792721;
+      r[59] = -0.7430319617668262;
+      s[59] = -0.7430319617668262;
+      t[59] = 0.02508211404942554;
+      w[59] = 0.01923782271792721;
+      r[60] = -0.5390181905157732;
+      s[60] = 0.02508211404942554;
+      t[60] = -0.7430319617668262;
+      w[60] = 0.01923782271792721;
+      r[61] = -0.7430319617668262;
+      s[61] = -0.5390181905157732;
+      t[61] = 0.02508211404942551;
+      w[61] = 0.01923782271792721;
+      r[62] = -0.7430319617668262;
+      s[62] = 0.02508211404942554;
+      t[62] = -0.7430319617668262;
+      w[62] = 0.01923782271792721;
+      r[63] = -0.5390181905157732;
+      s[63] = -0.7430319617668262;
+      t[63] = 0.02508211404942554;
+      w[63] = 0.01923782271792721;
+      r[64] = -0.7430319617668262;
+      s[64] = -0.5390181905157732;
+      t[64] = -0.7430319617668262;
+      w[64] = 0.01923782271792721;
+      r[65] = -0.7430319617668262;
+      s[65] = -0.7430319617668262;
+      t[65] = -0.5390181905157732;
+      w[65] = 0.01923782271792721;
+      r[66] = -0.7430319617668262;
+      s[66] = 0.02508211404942551;
+      t[66] = -0.5390181905157732;
+      w[66] = 0.01923782271792721;
+      r[67] = -0.5390181905157732;
+      s[67] = -0.7430319617668262;
+      t[67] = -0.7430319617668262;
+      w[67] = 0.01923782271792721;
+      r[68] = 0.02508211404942551;
+      s[68] = -0.5390181905157732;
+      t[68] = -0.7430319617668262;
+      w[68] = 0.01923782271792721;
+      r[69] = 0.4045657634046023;
+      s[69] = -0.9481462410143495;
+      t[69] = -0.5082732813759032;
+      w[69] = 0.007336665507925923;
+      r[70] = 0.4045657634046023;
+      s[70] = -0.9481462410143495;
+      t[70] = -0.9481462410143495;
+      w[70] = 0.007336665507925923;
+      r[71] = -0.9481462410143495;
+      s[71] = -0.9481462410143495;
+      t[71] = 0.4045657634046023;
+      w[71] = 0.007336665507925923;
+      r[72] = -0.5082732813759032;
+      s[72] = 0.4045657634046023;
+      t[72] = -0.9481462410143495;
+      w[72] = 0.007336665507925923;
+      r[73] = -0.9481462410143495;
+      s[73] = -0.5082732813759032;
+      t[73] = 0.4045657634046023;
+      w[73] = 0.007336665507925923;
+      r[74] = -0.9481462410143495;
+      s[74] = 0.4045657634046023;
+      t[74] = -0.9481462410143495;
+      w[74] = 0.007336665507925923;
+      r[75] = -0.5082732813759032;
+      s[75] = -0.9481462410143495;
+      t[75] = 0.4045657634046023;
+      w[75] = 0.007336665507925923;
+      r[76] = -0.9481462410143495;
+      s[76] = -0.5082732813759032;
+      t[76] = -0.9481462410143495;
+      w[76] = 0.007336665507925923;
+      r[77] = -0.9481462410143495;
+      s[77] = -0.9481462410143495;
+      t[77] = -0.5082732813759032;
+      w[77] = 0.007336665507925923;
+      r[78] = -0.9481462410143495;
+      s[78] = 0.4045657634046023;
+      t[78] = -0.5082732813759032;
+      w[78] = 0.007336665507925923;
+      r[79] = -0.5082732813759032;
+      s[79] = -0.9481462410143495;
+      t[79] = -0.9481462410143495;
+      w[79] = 0.007336665507925923;
+      r[80] = 0.4045657634046023;
+      s[80] = -0.5082732813759032;
+      t[80] = -0.9481462410143495;
+      w[80] = 0.007336665507925923;
+      r[81] = 0.06079123224408745;
+      s[81] = -0.9501658362591827;
+      t[81] = -0.7183474030028485;
+      w[81] = 0.01693359003213852;
+      r[82] = -0.9501658362591827;
+      s[82] = -0.7183474030028485;
+      t[82] = 0.0607912322440875;
+      w[82] = 0.01693359003213852;
+      r[83] = -0.9501658362591827;
+      s[83] = 0.0607912322440875;
+      t[83] = -0.7183474030028485;
+      w[83] = 0.01693359003213852;
+      r[84] = -0.7183474030028484;
+      s[84] = 0.06079123224408749;
+      t[84] = -0.3922779929820564;
+      w[84] = 0.01693359003213852;
+      r[85] = -0.7183474030028485;
+      s[85] = 0.0607912322440875;
+      t[85] = -0.9501658362591828;
+      w[85] = 0.01693359003213852;
+      r[86] = -0.3922779929820563;
+      s[86] = 0.06079123224408749;
+      t[86] = -0.7183474030028484;
+      w[86] = 0.01693359003213852;
+      r[87] = -0.7183474030028485;
+      s[87] = -0.9501658362591827;
+      t[87] = -0.3922779929820564;
+      w[87] = 0.01693359003213852;
+      r[88] = -0.7183474030028484;
+      s[88] = -0.3922779929820564;
+      t[88] = 0.06079123224408749;
+      w[88] = 0.01693359003213852;
+      r[89] = -0.3922779929820565;
+      s[89] = -0.9501658362591827;
+      t[89] = -0.7183474030028485;
+      w[89] = 0.01693359003213852;
+      r[90] = 0.0607912322440875;
+      s[90] = -0.9501658362591827;
+      t[90] = -0.3922779929820564;
+      w[90] = 0.01693359003213852;
+      r[91] = -0.3922779929820564;
+      s[91] = 0.0607912322440875;
+      t[91] = -0.9501658362591827;
+      w[91] = 0.01693359003213852;
+      r[92] = -0.7183474030028485;
+      s[92] = -0.9501658362591828;
+      t[92] = 0.0607912322440875;
+      w[92] = 0.01693359003213852;
+      r[93] = -0.3922779929820564;
+      s[93] = -0.9501658362591827;
+      t[93] = 0.0607912322440875;
+      w[93] = 0.01693359003213852;
+      r[94] = 0.06079123224408749;
+      s[94] = -0.3922779929820564;
+      t[94] = -0.7183474030028484;
+      w[94] = 0.01693359003213852;
+      r[95] = -0.7183474030028485;
+      s[95] = -0.3922779929820564;
+      t[95] = -0.9501658362591827;
+      w[95] = 0.01693359003213852;
+      r[96] = -0.9501658362591827;
+      s[96] = -0.3922779929820565;
+      t[96] = -0.7183474030028485;
+      w[96] = 0.01693359003213852;
+      r[97] = 0.0607912322440875;
+      s[97] = -0.3922779929820564;
+      t[97] = -0.9501658362591827;
+      w[97] = 0.01693359003213852;
+      r[98] = -0.9501658362591827;
+      s[98] = -0.3922779929820564;
+      t[98] = 0.06079123224408747;
+      w[98] = 0.01693359003213852;
+      r[99] = -0.9501658362591827;
+      s[99] = 0.06079123224408747;
+      t[99] = -0.3922779929820564;
+      w[99] = 0.01693359003213852;
+      r[100] = -0.3922779929820563;
+      s[100] = -0.7183474030028484;
+      t[100] = 0.06079123224408749;
+      w[100] = 0.01693359003213852;
+      r[101] = 0.06079123224408749;
+      s[101] = -0.7183474030028484;
+      t[101] = -0.3922779929820564;
+      w[101] = 0.01693359003213852;
+      r[102] = 0.06079123224408745;
+      s[102] = -0.7183474030028485;
+      t[102] = -0.9501658362591827;
+      w[102] = 0.01693359003213852;
+      r[103] = -0.9501658362591827;
+      s[103] = -0.7183474030028485;
+      t[103] = -0.3922779929820565;
+      w[103] = 0.01693359003213852;
+      r[104] = -0.3922779929820565;
+      s[104] = -0.7183474030028485;
+      t[104] = -0.9501658362591827;
+      w[104] = 0.01693359003213852;
 
       break;
     }
     case 12: {
-      r[0]   = -0.4191163350517226; s[0]   = -0.4191163350517226; t[0]   = -0.7426509948448321; w[0]   =   0.03722586152357994;
-      r[1]   = -0.4191163350517226; s[1]   = -0.7426509948448321; t[1]   = -0.4191163350517226; w[1]   =   0.03722586152357994;
-      r[2]   = -0.7426509948448321; s[2]   = -0.4191163350517226; t[2]   = -0.4191163350517226; w[2]   =   0.03722586152357994;
-      r[3]   = -0.4191163350517226; s[3]   = -0.4191163350517226; t[3]   = -0.4191163350517226; w[3]   =   0.03722586152357994;
-      r[4]   = -0.8117896607688906; s[4]   = -0.8117896607688906; t[4]   =  0.4353689823066721; w[4]   =   0.01079833060340124;
-      r[5]   = -0.8117896607688906; s[5]   =  0.4353689823066721; t[5]   = -0.8117896607688906; w[5]   =   0.01079833060340124;
-      r[6]   =   0.435368982306672; s[6]   = -0.8117896607688906; t[6]   = -0.8117896607688906; w[6]   =   0.01079833060340124;
-      r[7]   = -0.8117896607688906; s[7]   = -0.8117896607688906; t[7]   = -0.8117896607688906; w[7]   =   0.01079833060340124;
-      r[8]   = -0.6487514080793829; s[8]   = -0.6487514080793829; t[8]   =-0.05374577576185108; w[8]   =   0.02817918150655735;
-      r[9]   = -0.6487514080793829; s[9]   =-0.05374577576185108; t[9]   = -0.6487514080793829; w[9]   =   0.02817918150655735;
-      r[10]  =-0.05374577576185111; s[10]  = -0.6487514080793829; t[10]  = -0.6487514080793829; w[10]  =   0.02817918150655735;
-      r[11]  = -0.6487514080793829; s[11]  = -0.6487514080793829; t[11]  = -0.6487514080793829; w[11]  =   0.02817918150655735;
-      r[12]  = -0.2083097004570116; s[12]  = -0.7916902995429884; t[12]  = -0.7916902995429884; w[12]  =   0.02834338756489718;
-      r[13]  = -0.7916902995429884; s[13]  = -0.2083097004570116; t[13]  = -0.7916902995429884; w[13]  =   0.02834338756489718;
-      r[14]  = -0.2083097004570116; s[14]  = -0.2083097004570116; t[14]  = -0.7916902995429884; w[14]  =   0.02834338756489718;
-      r[15]  = -0.2083097004570116; s[15]  = -0.7916902995429884; t[15]  = -0.2083097004570116; w[15]  =   0.02834338756489718;
-      r[16]  = -0.7916902995429884; s[16]  = -0.2083097004570116; t[16]  = -0.2083097004570116; w[16]  =   0.02834338756489718;
-      r[17]  = -0.7916902995429884; s[17]  = -0.7916902995429884; t[17]  = -0.2083097004570116; w[17]  =   0.02834338756489718;
-      r[18]  = -0.9454374073009324; s[18]  =-0.05456259269906756; t[18]  =-0.05456259269906756; w[18]  =   0.00762096465940687;
-      r[19]  =-0.05456259269906758; s[19]  = -0.9454374073009324; t[19]  =-0.05456259269906758; w[19]  =   0.00762096465940687;
-      r[20]  = -0.9454374073009324; s[20]  = -0.9454374073009324; t[20]  = -0.0545625926990676; w[20]  =   0.00762096465940687;
-      r[21]  = -0.9454374073009324; s[21]  = -0.0545625926990676; t[21]  = -0.9454374073009324; w[21]  =   0.00762096465940687;
-      r[22]  =-0.05456259269906755; s[22]  = -0.9454374073009324; t[22]  = -0.9454374073009324; w[22]  =   0.00762096465940687;
-      r[23]  =-0.05456259269906758; s[23]  =-0.05456259269906758; t[23]  = -0.9454374073009324; w[23]  =   0.00762096465940687;
-      r[24]  = -0.5426252783987343; s[24]  = -0.2484192605435968; t[24]  = -0.9605362005140723; w[24]  =  0.009941214894086916;
-      r[25]  = -0.5426252783987343; s[25]  = -0.2484192605435968; t[25]  = -0.2484192605435968; w[25]  =  0.009941214894086916;
-      r[26]  = -0.2484192605435968; s[26]  = -0.2484192605435968; t[26]  = -0.5426252783987343; w[26]  =  0.009941214894086916;
-      r[27]  = -0.9605362005140721; s[27]  = -0.5426252783987343; t[27]  = -0.2484192605435968; w[27]  =  0.009941214894086916;
-      r[28]  = -0.2484192605435968; s[28]  = -0.9605362005140723; t[28]  = -0.5426252783987343; w[28]  =  0.009941214894086916;
-      r[29]  = -0.2484192605435968; s[29]  = -0.5426252783987343; t[29]  = -0.2484192605435968; w[29]  =  0.009941214894086916;
-      r[30]  = -0.9605362005140721; s[30]  = -0.2484192605435968; t[30]  = -0.5426252783987343; w[30]  =  0.009941214894086916;
-      r[31]  = -0.2484192605435968; s[31]  = -0.9605362005140721; t[31]  = -0.2484192605435968; w[31]  =  0.009941214894086916;
-      r[32]  = -0.2484192605435968; s[32]  = -0.2484192605435968; t[32]  = -0.9605362005140721; w[32]  =  0.009941214894086916;
-      r[33]  = -0.2484192605435968; s[33]  = -0.5426252783987343; t[33]  = -0.9605362005140723; w[33]  =  0.009941214894086916;
-      r[34]  = -0.9605362005140721; s[34]  = -0.2484192605435968; t[34]  = -0.2484192605435968; w[34]  =  0.009941214894086916;
-      r[35]  = -0.5426252783987343; s[35]  = -0.9605362005140723; t[35]  = -0.2484192605435968; w[35]  =  0.009941214894086916;
-      r[36]  = 0.02514623497982801; s[36]  = -0.5646581404659121; t[36]  = -0.8958299540480037; w[36]  =   0.01791292763274642;
-      r[37]  =   0.025146234979828; s[37]  = -0.5646581404659121; t[37]  = -0.5646581404659121; w[37]  =   0.01791292763274642;
-      r[38]  = -0.5646581404659121; s[38]  = -0.5646581404659121; t[38]  = 0.02514623497982797; w[38]  =   0.01791292763274642;
-      r[39]  = -0.8958299540480037; s[39]  = 0.02514623497982796; t[39]  = -0.5646581404659121; w[39]  =   0.01791292763274642;
-      r[40]  = -0.5646581404659121; s[40]  = -0.8958299540480037; t[40]  = 0.02514623497982799; w[40]  =   0.01791292763274642;
-      r[41]  = -0.5646581404659121; s[41]  = 0.02514623497982797; t[41]  = -0.5646581404659121; w[41]  =   0.01791292763274642;
-      r[42]  = -0.8958299540480037; s[42]  = -0.5646581404659121; t[42]  = 0.02514623497982796; w[42]  =   0.01791292763274642;
-      r[43]  = -0.5646581404659121; s[43]  = -0.8958299540480037; t[43]  = -0.5646581404659121; w[43]  =   0.01791292763274642;
-      r[44]  = -0.5646581404659121; s[44]  = -0.5646581404659121; t[44]  = -0.8958299540480037; w[44]  =   0.01791292763274642;
-      r[45]  = -0.5646581404659121; s[45]  = 0.02514623497982799; t[45]  = -0.8958299540480037; w[45]  =   0.01791292763274642;
-      r[46]  = -0.8958299540480037; s[46]  = -0.5646581404659121; t[46]  = -0.5646581404659121; w[46]  =   0.01791292763274642;
-      r[47]  = 0.02514623497982801; s[47]  = -0.8958299540480037; t[47]  = -0.5646581404659121; w[47]  =   0.01791292763274642;
-      r[48]  =  0.3827353334438319; s[48]  = -0.9651564497171329; t[48]  = -0.4524224340095662; w[48]  =  0.003515981327063368;
-      r[49]  =  0.3827353334438319; s[49]  = -0.9651564497171329; t[49]  = -0.9651564497171329; w[49]  =  0.003515981327063368;
-      r[50]  = -0.9651564497171329; s[50]  = -0.9651564497171329; t[50]  =   0.382735333443832; w[50]  =  0.003515981327063368;
-      r[51]  = -0.4524224340095661; s[51]  =   0.382735333443832; t[51]  = -0.9651564497171329; w[51]  =  0.003515981327063368;
-      r[52]  = -0.9651564497171329; s[52]  = -0.4524224340095662; t[52]  =  0.3827353334438319; w[52]  =  0.003515981327063368;
-      r[53]  = -0.9651564497171329; s[53]  =   0.382735333443832; t[53]  = -0.9651564497171329; w[53]  =  0.003515981327063368;
-      r[54]  = -0.4524224340095661; s[54]  = -0.9651564497171329; t[54]  =   0.382735333443832; w[54]  =  0.003515981327063368;
-      r[55]  = -0.9651564497171329; s[55]  = -0.4524224340095662; t[55]  = -0.9651564497171329; w[55]  =  0.003515981327063368;
-      r[56]  = -0.9651564497171329; s[56]  = -0.9651564497171329; t[56]  = -0.4524224340095662; w[56]  =  0.003515981327063368;
-      r[57]  = -0.9651564497171329; s[57]  =  0.3827353334438319; t[57]  = -0.4524224340095662; w[57]  =  0.003515981327063368;
-      r[58]  = -0.4524224340095661; s[58]  = -0.9651564497171329; t[58]  = -0.9651564497171329; w[58]  =  0.003515981327063368;
-      r[59]  =  0.3827353334438319; s[59]  = -0.4524224340095662; t[59]  = -0.9651564497171329; w[59]  =  0.003515981327063368;
-      r[60]  =  0.2761393513413102; s[60]  =  -0.860260573663048; t[60]  = -0.5556182040152142; w[60]  =   0.01316564240019808;
-      r[61]  =  0.2761393513413101; s[61]  =  -0.860260573663048; t[61]  =  -0.860260573663048; w[61]  =   0.01316564240019808;
-      r[62]  =  -0.860260573663048; s[62]  =  -0.860260573663048; t[62]  =  0.2761393513413102; w[62]  =   0.01316564240019808;
-      r[63]  = -0.5556182040152142; s[63]  =  0.2761393513413102; t[63]  =  -0.860260573663048; w[63]  =   0.01316564240019808;
-      r[64]  =  -0.860260573663048; s[64]  = -0.5556182040152142; t[64]  =  0.2761393513413102; w[64]  =   0.01316564240019808;
-      r[65]  =  -0.860260573663048; s[65]  =  0.2761393513413102; t[65]  =  -0.860260573663048; w[65]  =   0.01316564240019808;
-      r[66]  = -0.5556182040152142; s[66]  =  -0.860260573663048; t[66]  =  0.2761393513413102; w[66]  =   0.01316564240019808;
-      r[67]  =  -0.860260573663048; s[67]  = -0.5556182040152142; t[67]  =  -0.860260573663048; w[67]  =   0.01316564240019808;
-      r[68]  =  -0.860260573663048; s[68]  =  -0.860260573663048; t[68]  = -0.5556182040152142; w[68]  =   0.01316564240019808;
-      r[69]  =  -0.860260573663048; s[69]  =  0.2761393513413102; t[69]  = -0.5556182040152142; w[69]  =   0.01316564240019808;
-      r[70]  = -0.5556182040152142; s[70]  =  -0.860260573663048; t[70]  =  -0.860260573663048; w[70]  =   0.01316564240019808;
-      r[71]  =  0.2761393513413102; s[71]  = -0.5556182040152142; t[71]  =  -0.860260573663048; w[71]  =   0.01316564240019808;
-      r[72]  =  0.6774764765813509; s[72]  =  -0.948908768728992; t[72]  = -0.7796589391233667; w[72]  =   0.00421031530337885;
-      r[73]  =  0.6774764765813508; s[73]  =  -0.948908768728992; t[73]  =  -0.948908768728992; w[73]  =   0.00421031530337885;
-      r[74]  =  -0.948908768728992; s[74]  =  -0.948908768728992; t[74]  =  0.6774764765813509; w[74]  =   0.00421031530337885;
-      r[75]  = -0.7796589391233667; s[75]  =  0.6774764765813509; t[75]  =  -0.948908768728992; w[75]  =   0.00421031530337885;
-      r[76]  =  -0.948908768728992; s[76]  = -0.7796589391233667; t[76]  =  0.6774764765813509; w[76]  =   0.00421031530337885;
-      r[77]  =  -0.948908768728992; s[77]  =  0.6774764765813509; t[77]  =  -0.948908768728992; w[77]  =   0.00421031530337885;
-      r[78]  = -0.7796589391233667; s[78]  =  -0.948908768728992; t[78]  =  0.6774764765813509; w[78]  =   0.00421031530337885;
-      r[79]  =  -0.948908768728992; s[79]  = -0.7796589391233668; t[79]  =  -0.948908768728992; w[79]  =   0.00421031530337885;
-      r[80]  =  -0.948908768728992; s[80]  =  -0.948908768728992; t[80]  = -0.7796589391233668; w[80]  =   0.00421031530337885;
-      r[81]  =  -0.948908768728992; s[81]  =  0.6774764765813509; t[81]  = -0.7796589391233667; w[81]  =   0.00421031530337885;
-      r[82]  = -0.7796589391233668; s[82]  =  -0.948908768728992; t[82]  =  -0.948908768728992; w[82]  =   0.00421031530337885;
-      r[83]  =  0.6774764765813509; s[83]  = -0.7796589391233667; t[83]  =  -0.948908768728992; w[83]  =   0.00421031530337885;
-      r[84]  =  0.4516899137328004; s[84]  = -0.7307456223061921; t[84]  = -0.9901986691204159; w[84]  =  0.004750818519930626;
-      r[85]  =  0.4516899137328003; s[85]  = -0.7307456223061922; t[85]  = -0.7307456223061922; w[85]  =  0.004750818519930626;
-      r[86]  = -0.7307456223061921; s[86]  = -0.7307456223061923; t[86]  =  0.4516899137328004; w[86]  =  0.004750818519930626;
-      r[87]  = -0.9901986691204159; s[87]  =  0.4516899137328004; t[87]  = -0.7307456223061923; w[87]  =  0.004750818519930626;
-      r[88]  = -0.7307456223061923; s[88]  = -0.9901986691204159; t[88]  =  0.4516899137328004; w[88]  =  0.004750818519930626;
-      r[89]  = -0.7307456223061921; s[89]  =  0.4516899137328004; t[89]  = -0.7307456223061923; w[89]  =  0.004750818519930626;
-      r[90]  = -0.9901986691204159; s[90]  = -0.7307456223061923; t[90]  =  0.4516899137328004; w[90]  =  0.004750818519930626;
-      r[91]  = -0.7307456223061922; s[91]  = -0.9901986691204159; t[91]  = -0.7307456223061922; w[91]  =  0.004750818519930626;
-      r[92]  = -0.7307456223061922; s[92]  = -0.7307456223061922; t[92]  = -0.9901986691204159; w[92]  =  0.004750818519930626;
-      r[93]  = -0.7307456223061923; s[93]  =  0.4516899137328004; t[93]  = -0.9901986691204159; w[93]  =  0.004750818519930626;
-      r[94]  = -0.9901986691204159; s[94]  = -0.7307456223061922; t[94]  = -0.7307456223061922; w[94]  =  0.004750818519930626;
-      r[95]  =  0.4516899137328004; s[95]  = -0.9901986691204159; t[95]  = -0.7307456223061921; w[95]  =  0.004750818519930626;
-      r[96]  =  0.8845962806133972; s[96]  = -0.9719492361359849; t[96]  = -0.9406978083414277; w[96]  = 0.0003599363171224237;
-      r[97]  =  0.8845962806133973; s[97]  = -0.9719492361359848; t[97]  = -0.9719492361359848; w[97]  = 0.0003599363171224237;
-      r[98]  = -0.9719492361359848; s[98]  = -0.9719492361359848; t[98]  =  0.8845962806133972; w[98]  = 0.0003599363171224237;
-      r[99]  = -0.9406978083414278; s[99]  =  0.8845962806133972; t[99]  = -0.9719492361359848; w[99]  = 0.0003599363171224237;
-      r[100] = -0.9719492361359848; s[100] = -0.9406978083414278; t[100] =  0.8845962806133972; w[100] = 0.0003599363171224237;
-      r[101] = -0.9719492361359848; s[101] =  0.8845962806133972; t[101] = -0.9719492361359848; w[101] = 0.0003599363171224237;
-      r[102] = -0.9406978083414278; s[102] = -0.9719492361359848; t[102] =  0.8845962806133972; w[102] = 0.0003599363171224237;
-      r[103] = -0.9719492361359848; s[103] = -0.9406978083414277; t[103] = -0.9719492361359848; w[103] = 0.0003599363171224237;
-      r[104] = -0.9719492361359848; s[104] = -0.9719492361359848; t[104] = -0.9406978083414277; w[104] = 0.0003599363171224237;
-      r[105] = -0.9719492361359848; s[105] =  0.8845962806133972; t[105] = -0.9406978083414278; w[105] = 0.0003599363171224237;
-      r[106] = -0.9406978083414277; s[106] = -0.9719492361359848; t[106] = -0.9719492361359848; w[106] = 0.0003599363171224237;
-      r[107] =  0.8845962806133972; s[107] = -0.9406978083414277; t[107] = -0.9719492361359849; w[107] = 0.0003599363171224237;
-      r[108] =  0.1011535049643996; s[108] = -0.3535634288145484; t[108] = -0.9763709473096609; w[108] =  0.006935487029959765;
-      r[109] = -0.3535634288145484; s[109] = -0.9763709473096609; t[109] =  0.1011535049643997; w[109] =  0.006935487029959765;
-      r[110] = -0.3535634288145484; s[110] =  0.1011535049643997; t[110] = -0.9763709473096609; w[110] =  0.006935487029959765;
-      r[111] = -0.9763709473096609; s[111] =  0.1011535049643996; t[111] = -0.7712191288401904; w[111] =  0.006935487029959765;
-      r[112] = -0.9763709473096609; s[112] =  0.1011535049643996; t[112] = -0.3535634288145484; w[112] =  0.006935487029959765;
-      r[113] = -0.7712191288401904; s[113] =  0.1011535049643997; t[113] = -0.9763709473096609; w[113] =  0.006935487029959765;
-      r[114] = -0.9763709473096609; s[114] = -0.3535634288145484; t[114] = -0.7712191288401904; w[114] =  0.006935487029959765;
-      r[115] = -0.9763709473096609; s[115] = -0.7712191288401904; t[115] =  0.1011535049643996; w[115] =  0.006935487029959765;
-      r[116] = -0.7712191288401904; s[116] = -0.3535634288145484; t[116] = -0.9763709473096609; w[116] =  0.006935487029959765;
-      r[117] =  0.1011535049643996; s[117] = -0.3535634288145484; t[117] = -0.7712191288401904; w[117] =  0.006935487029959765;
-      r[118] = -0.7712191288401904; s[118] =  0.1011535049643996; t[118] = -0.3535634288145484; w[118] =  0.006935487029959765;
-      r[119] = -0.9763709473096609; s[119] = -0.3535634288145484; t[119] =  0.1011535049643996; w[119] =  0.006935487029959765;
-      r[120] = -0.7712191288401904; s[120] = -0.3535634288145484; t[120] =  0.1011535049643996; w[120] =  0.006935487029959765;
-      r[121] =  0.1011535049643997; s[121] = -0.7712191288401904; t[121] = -0.9763709473096609; w[121] =  0.006935487029959765;
-      r[122] = -0.9763709473096609; s[122] = -0.7712191288401904; t[122] = -0.3535634288145484; w[122] =  0.006935487029959765;
-      r[123] = -0.3535634288145484; s[123] = -0.7712191288401904; t[123] = -0.9763709473096609; w[123] =  0.006935487029959765;
-      r[124] =  0.1011535049643996; s[124] = -0.7712191288401904; t[124] = -0.3535634288145484; w[124] =  0.006935487029959765;
-      r[125] = -0.3535634288145484; s[125] = -0.7712191288401904; t[125] =  0.1011535049643996; w[125] =  0.006935487029959765;
-      r[126] = -0.3535634288145484; s[126] =  0.1011535049643996; t[126] = -0.7712191288401904; w[126] =  0.006935487029959765;
-      r[127] = -0.7712191288401904; s[127] = -0.9763709473096609; t[127] =  0.1011535049643997; w[127] =  0.006935487029959765;
-      r[128] =  0.1011535049643997; s[128] = -0.9763709473096609; t[128] = -0.7712191288401904; w[128] =  0.006935487029959765;
-      r[129] =  0.1011535049643996; s[129] = -0.9763709473096609; t[129] = -0.3535634288145484; w[129] =  0.006935487029959765;
-      r[130] = -0.3535634288145484; s[130] = -0.9763709473096609; t[130] = -0.7712191288401904; w[130] =  0.006935487029959765;
-      r[131] = -0.7712191288401904; s[131] = -0.9763709473096609; t[131] = -0.3535634288145484; w[131] =  0.006935487029959765;
+      r[0] = -0.4191163350517226;
+      s[0] = -0.4191163350517226;
+      t[0] = -0.7426509948448321;
+      w[0] = 0.03722586152357994;
+      r[1] = -0.4191163350517226;
+      s[1] = -0.7426509948448321;
+      t[1] = -0.4191163350517226;
+      w[1] = 0.03722586152357994;
+      r[2] = -0.7426509948448321;
+      s[2] = -0.4191163350517226;
+      t[2] = -0.4191163350517226;
+      w[2] = 0.03722586152357994;
+      r[3] = -0.4191163350517226;
+      s[3] = -0.4191163350517226;
+      t[3] = -0.4191163350517226;
+      w[3] = 0.03722586152357994;
+      r[4] = -0.8117896607688906;
+      s[4] = -0.8117896607688906;
+      t[4] = 0.4353689823066721;
+      w[4] = 0.01079833060340124;
+      r[5] = -0.8117896607688906;
+      s[5] = 0.4353689823066721;
+      t[5] = -0.8117896607688906;
+      w[5] = 0.01079833060340124;
+      r[6] = 0.435368982306672;
+      s[6] = -0.8117896607688906;
+      t[6] = -0.8117896607688906;
+      w[6] = 0.01079833060340124;
+      r[7] = -0.8117896607688906;
+      s[7] = -0.8117896607688906;
+      t[7] = -0.8117896607688906;
+      w[7] = 0.01079833060340124;
+      r[8] = -0.6487514080793829;
+      s[8] = -0.6487514080793829;
+      t[8] = -0.05374577576185108;
+      w[8] = 0.02817918150655735;
+      r[9] = -0.6487514080793829;
+      s[9] = -0.05374577576185108;
+      t[9] = -0.6487514080793829;
+      w[9] = 0.02817918150655735;
+      r[10] = -0.05374577576185111;
+      s[10] = -0.6487514080793829;
+      t[10] = -0.6487514080793829;
+      w[10] = 0.02817918150655735;
+      r[11] = -0.6487514080793829;
+      s[11] = -0.6487514080793829;
+      t[11] = -0.6487514080793829;
+      w[11] = 0.02817918150655735;
+      r[12] = -0.2083097004570116;
+      s[12] = -0.7916902995429884;
+      t[12] = -0.7916902995429884;
+      w[12] = 0.02834338756489718;
+      r[13] = -0.7916902995429884;
+      s[13] = -0.2083097004570116;
+      t[13] = -0.7916902995429884;
+      w[13] = 0.02834338756489718;
+      r[14] = -0.2083097004570116;
+      s[14] = -0.2083097004570116;
+      t[14] = -0.7916902995429884;
+      w[14] = 0.02834338756489718;
+      r[15] = -0.2083097004570116;
+      s[15] = -0.7916902995429884;
+      t[15] = -0.2083097004570116;
+      w[15] = 0.02834338756489718;
+      r[16] = -0.7916902995429884;
+      s[16] = -0.2083097004570116;
+      t[16] = -0.2083097004570116;
+      w[16] = 0.02834338756489718;
+      r[17] = -0.7916902995429884;
+      s[17] = -0.7916902995429884;
+      t[17] = -0.2083097004570116;
+      w[17] = 0.02834338756489718;
+      r[18] = -0.9454374073009324;
+      s[18] = -0.05456259269906756;
+      t[18] = -0.05456259269906756;
+      w[18] = 0.00762096465940687;
+      r[19] = -0.05456259269906758;
+      s[19] = -0.9454374073009324;
+      t[19] = -0.05456259269906758;
+      w[19] = 0.00762096465940687;
+      r[20] = -0.9454374073009324;
+      s[20] = -0.9454374073009324;
+      t[20] = -0.0545625926990676;
+      w[20] = 0.00762096465940687;
+      r[21] = -0.9454374073009324;
+      s[21] = -0.0545625926990676;
+      t[21] = -0.9454374073009324;
+      w[21] = 0.00762096465940687;
+      r[22] = -0.05456259269906755;
+      s[22] = -0.9454374073009324;
+      t[22] = -0.9454374073009324;
+      w[22] = 0.00762096465940687;
+      r[23] = -0.05456259269906758;
+      s[23] = -0.05456259269906758;
+      t[23] = -0.9454374073009324;
+      w[23] = 0.00762096465940687;
+      r[24] = -0.5426252783987343;
+      s[24] = -0.2484192605435968;
+      t[24] = -0.9605362005140723;
+      w[24] = 0.009941214894086916;
+      r[25] = -0.5426252783987343;
+      s[25] = -0.2484192605435968;
+      t[25] = -0.2484192605435968;
+      w[25] = 0.009941214894086916;
+      r[26] = -0.2484192605435968;
+      s[26] = -0.2484192605435968;
+      t[26] = -0.5426252783987343;
+      w[26] = 0.009941214894086916;
+      r[27] = -0.9605362005140721;
+      s[27] = -0.5426252783987343;
+      t[27] = -0.2484192605435968;
+      w[27] = 0.009941214894086916;
+      r[28] = -0.2484192605435968;
+      s[28] = -0.9605362005140723;
+      t[28] = -0.5426252783987343;
+      w[28] = 0.009941214894086916;
+      r[29] = -0.2484192605435968;
+      s[29] = -0.5426252783987343;
+      t[29] = -0.2484192605435968;
+      w[29] = 0.009941214894086916;
+      r[30] = -0.9605362005140721;
+      s[30] = -0.2484192605435968;
+      t[30] = -0.5426252783987343;
+      w[30] = 0.009941214894086916;
+      r[31] = -0.2484192605435968;
+      s[31] = -0.9605362005140721;
+      t[31] = -0.2484192605435968;
+      w[31] = 0.009941214894086916;
+      r[32] = -0.2484192605435968;
+      s[32] = -0.2484192605435968;
+      t[32] = -0.9605362005140721;
+      w[32] = 0.009941214894086916;
+      r[33] = -0.2484192605435968;
+      s[33] = -0.5426252783987343;
+      t[33] = -0.9605362005140723;
+      w[33] = 0.009941214894086916;
+      r[34] = -0.9605362005140721;
+      s[34] = -0.2484192605435968;
+      t[34] = -0.2484192605435968;
+      w[34] = 0.009941214894086916;
+      r[35] = -0.5426252783987343;
+      s[35] = -0.9605362005140723;
+      t[35] = -0.2484192605435968;
+      w[35] = 0.009941214894086916;
+      r[36] = 0.02514623497982801;
+      s[36] = -0.5646581404659121;
+      t[36] = -0.8958299540480037;
+      w[36] = 0.01791292763274642;
+      r[37] = 0.025146234979828;
+      s[37] = -0.5646581404659121;
+      t[37] = -0.5646581404659121;
+      w[37] = 0.01791292763274642;
+      r[38] = -0.5646581404659121;
+      s[38] = -0.5646581404659121;
+      t[38] = 0.02514623497982797;
+      w[38] = 0.01791292763274642;
+      r[39] = -0.8958299540480037;
+      s[39] = 0.02514623497982796;
+      t[39] = -0.5646581404659121;
+      w[39] = 0.01791292763274642;
+      r[40] = -0.5646581404659121;
+      s[40] = -0.8958299540480037;
+      t[40] = 0.02514623497982799;
+      w[40] = 0.01791292763274642;
+      r[41] = -0.5646581404659121;
+      s[41] = 0.02514623497982797;
+      t[41] = -0.5646581404659121;
+      w[41] = 0.01791292763274642;
+      r[42] = -0.8958299540480037;
+      s[42] = -0.5646581404659121;
+      t[42] = 0.02514623497982796;
+      w[42] = 0.01791292763274642;
+      r[43] = -0.5646581404659121;
+      s[43] = -0.8958299540480037;
+      t[43] = -0.5646581404659121;
+      w[43] = 0.01791292763274642;
+      r[44] = -0.5646581404659121;
+      s[44] = -0.5646581404659121;
+      t[44] = -0.8958299540480037;
+      w[44] = 0.01791292763274642;
+      r[45] = -0.5646581404659121;
+      s[45] = 0.02514623497982799;
+      t[45] = -0.8958299540480037;
+      w[45] = 0.01791292763274642;
+      r[46] = -0.8958299540480037;
+      s[46] = -0.5646581404659121;
+      t[46] = -0.5646581404659121;
+      w[46] = 0.01791292763274642;
+      r[47] = 0.02514623497982801;
+      s[47] = -0.8958299540480037;
+      t[47] = -0.5646581404659121;
+      w[47] = 0.01791292763274642;
+      r[48] = 0.3827353334438319;
+      s[48] = -0.9651564497171329;
+      t[48] = -0.4524224340095662;
+      w[48] = 0.003515981327063368;
+      r[49] = 0.3827353334438319;
+      s[49] = -0.9651564497171329;
+      t[49] = -0.9651564497171329;
+      w[49] = 0.003515981327063368;
+      r[50] = -0.9651564497171329;
+      s[50] = -0.9651564497171329;
+      t[50] = 0.382735333443832;
+      w[50] = 0.003515981327063368;
+      r[51] = -0.4524224340095661;
+      s[51] = 0.382735333443832;
+      t[51] = -0.9651564497171329;
+      w[51] = 0.003515981327063368;
+      r[52] = -0.9651564497171329;
+      s[52] = -0.4524224340095662;
+      t[52] = 0.3827353334438319;
+      w[52] = 0.003515981327063368;
+      r[53] = -0.9651564497171329;
+      s[53] = 0.382735333443832;
+      t[53] = -0.9651564497171329;
+      w[53] = 0.003515981327063368;
+      r[54] = -0.4524224340095661;
+      s[54] = -0.9651564497171329;
+      t[54] = 0.382735333443832;
+      w[54] = 0.003515981327063368;
+      r[55] = -0.9651564497171329;
+      s[55] = -0.4524224340095662;
+      t[55] = -0.9651564497171329;
+      w[55] = 0.003515981327063368;
+      r[56] = -0.9651564497171329;
+      s[56] = -0.9651564497171329;
+      t[56] = -0.4524224340095662;
+      w[56] = 0.003515981327063368;
+      r[57] = -0.9651564497171329;
+      s[57] = 0.3827353334438319;
+      t[57] = -0.4524224340095662;
+      w[57] = 0.003515981327063368;
+      r[58] = -0.4524224340095661;
+      s[58] = -0.9651564497171329;
+      t[58] = -0.9651564497171329;
+      w[58] = 0.003515981327063368;
+      r[59] = 0.3827353334438319;
+      s[59] = -0.4524224340095662;
+      t[59] = -0.9651564497171329;
+      w[59] = 0.003515981327063368;
+      r[60] = 0.2761393513413102;
+      s[60] = -0.860260573663048;
+      t[60] = -0.5556182040152142;
+      w[60] = 0.01316564240019808;
+      r[61] = 0.2761393513413101;
+      s[61] = -0.860260573663048;
+      t[61] = -0.860260573663048;
+      w[61] = 0.01316564240019808;
+      r[62] = -0.860260573663048;
+      s[62] = -0.860260573663048;
+      t[62] = 0.2761393513413102;
+      w[62] = 0.01316564240019808;
+      r[63] = -0.5556182040152142;
+      s[63] = 0.2761393513413102;
+      t[63] = -0.860260573663048;
+      w[63] = 0.01316564240019808;
+      r[64] = -0.860260573663048;
+      s[64] = -0.5556182040152142;
+      t[64] = 0.2761393513413102;
+      w[64] = 0.01316564240019808;
+      r[65] = -0.860260573663048;
+      s[65] = 0.2761393513413102;
+      t[65] = -0.860260573663048;
+      w[65] = 0.01316564240019808;
+      r[66] = -0.5556182040152142;
+      s[66] = -0.860260573663048;
+      t[66] = 0.2761393513413102;
+      w[66] = 0.01316564240019808;
+      r[67] = -0.860260573663048;
+      s[67] = -0.5556182040152142;
+      t[67] = -0.860260573663048;
+      w[67] = 0.01316564240019808;
+      r[68] = -0.860260573663048;
+      s[68] = -0.860260573663048;
+      t[68] = -0.5556182040152142;
+      w[68] = 0.01316564240019808;
+      r[69] = -0.860260573663048;
+      s[69] = 0.2761393513413102;
+      t[69] = -0.5556182040152142;
+      w[69] = 0.01316564240019808;
+      r[70] = -0.5556182040152142;
+      s[70] = -0.860260573663048;
+      t[70] = -0.860260573663048;
+      w[70] = 0.01316564240019808;
+      r[71] = 0.2761393513413102;
+      s[71] = -0.5556182040152142;
+      t[71] = -0.860260573663048;
+      w[71] = 0.01316564240019808;
+      r[72] = 0.6774764765813509;
+      s[72] = -0.948908768728992;
+      t[72] = -0.7796589391233667;
+      w[72] = 0.00421031530337885;
+      r[73] = 0.6774764765813508;
+      s[73] = -0.948908768728992;
+      t[73] = -0.948908768728992;
+      w[73] = 0.00421031530337885;
+      r[74] = -0.948908768728992;
+      s[74] = -0.948908768728992;
+      t[74] = 0.6774764765813509;
+      w[74] = 0.00421031530337885;
+      r[75] = -0.7796589391233667;
+      s[75] = 0.6774764765813509;
+      t[75] = -0.948908768728992;
+      w[75] = 0.00421031530337885;
+      r[76] = -0.948908768728992;
+      s[76] = -0.7796589391233667;
+      t[76] = 0.6774764765813509;
+      w[76] = 0.00421031530337885;
+      r[77] = -0.948908768728992;
+      s[77] = 0.6774764765813509;
+      t[77] = -0.948908768728992;
+      w[77] = 0.00421031530337885;
+      r[78] = -0.7796589391233667;
+      s[78] = -0.948908768728992;
+      t[78] = 0.6774764765813509;
+      w[78] = 0.00421031530337885;
+      r[79] = -0.948908768728992;
+      s[79] = -0.7796589391233668;
+      t[79] = -0.948908768728992;
+      w[79] = 0.00421031530337885;
+      r[80] = -0.948908768728992;
+      s[80] = -0.948908768728992;
+      t[80] = -0.7796589391233668;
+      w[80] = 0.00421031530337885;
+      r[81] = -0.948908768728992;
+      s[81] = 0.6774764765813509;
+      t[81] = -0.7796589391233667;
+      w[81] = 0.00421031530337885;
+      r[82] = -0.7796589391233668;
+      s[82] = -0.948908768728992;
+      t[82] = -0.948908768728992;
+      w[82] = 0.00421031530337885;
+      r[83] = 0.6774764765813509;
+      s[83] = -0.7796589391233667;
+      t[83] = -0.948908768728992;
+      w[83] = 0.00421031530337885;
+      r[84] = 0.4516899137328004;
+      s[84] = -0.7307456223061921;
+      t[84] = -0.9901986691204159;
+      w[84] = 0.004750818519930626;
+      r[85] = 0.4516899137328003;
+      s[85] = -0.7307456223061922;
+      t[85] = -0.7307456223061922;
+      w[85] = 0.004750818519930626;
+      r[86] = -0.7307456223061921;
+      s[86] = -0.7307456223061923;
+      t[86] = 0.4516899137328004;
+      w[86] = 0.004750818519930626;
+      r[87] = -0.9901986691204159;
+      s[87] = 0.4516899137328004;
+      t[87] = -0.7307456223061923;
+      w[87] = 0.004750818519930626;
+      r[88] = -0.7307456223061923;
+      s[88] = -0.9901986691204159;
+      t[88] = 0.4516899137328004;
+      w[88] = 0.004750818519930626;
+      r[89] = -0.7307456223061921;
+      s[89] = 0.4516899137328004;
+      t[89] = -0.7307456223061923;
+      w[89] = 0.004750818519930626;
+      r[90] = -0.9901986691204159;
+      s[90] = -0.7307456223061923;
+      t[90] = 0.4516899137328004;
+      w[90] = 0.004750818519930626;
+      r[91] = -0.7307456223061922;
+      s[91] = -0.9901986691204159;
+      t[91] = -0.7307456223061922;
+      w[91] = 0.004750818519930626;
+      r[92] = -0.7307456223061922;
+      s[92] = -0.7307456223061922;
+      t[92] = -0.9901986691204159;
+      w[92] = 0.004750818519930626;
+      r[93] = -0.7307456223061923;
+      s[93] = 0.4516899137328004;
+      t[93] = -0.9901986691204159;
+      w[93] = 0.004750818519930626;
+      r[94] = -0.9901986691204159;
+      s[94] = -0.7307456223061922;
+      t[94] = -0.7307456223061922;
+      w[94] = 0.004750818519930626;
+      r[95] = 0.4516899137328004;
+      s[95] = -0.9901986691204159;
+      t[95] = -0.7307456223061921;
+      w[95] = 0.004750818519930626;
+      r[96] = 0.8845962806133972;
+      s[96] = -0.9719492361359849;
+      t[96] = -0.9406978083414277;
+      w[96] = 0.0003599363171224237;
+      r[97] = 0.8845962806133973;
+      s[97] = -0.9719492361359848;
+      t[97] = -0.9719492361359848;
+      w[97] = 0.0003599363171224237;
+      r[98] = -0.9719492361359848;
+      s[98] = -0.9719492361359848;
+      t[98] = 0.8845962806133972;
+      w[98] = 0.0003599363171224237;
+      r[99] = -0.9406978083414278;
+      s[99] = 0.8845962806133972;
+      t[99] = -0.9719492361359848;
+      w[99] = 0.0003599363171224237;
+      r[100] = -0.9719492361359848;
+      s[100] = -0.9406978083414278;
+      t[100] = 0.8845962806133972;
+      w[100] = 0.0003599363171224237;
+      r[101] = -0.9719492361359848;
+      s[101] = 0.8845962806133972;
+      t[101] = -0.9719492361359848;
+      w[101] = 0.0003599363171224237;
+      r[102] = -0.9406978083414278;
+      s[102] = -0.9719492361359848;
+      t[102] = 0.8845962806133972;
+      w[102] = 0.0003599363171224237;
+      r[103] = -0.9719492361359848;
+      s[103] = -0.9406978083414277;
+      t[103] = -0.9719492361359848;
+      w[103] = 0.0003599363171224237;
+      r[104] = -0.9719492361359848;
+      s[104] = -0.9719492361359848;
+      t[104] = -0.9406978083414277;
+      w[104] = 0.0003599363171224237;
+      r[105] = -0.9719492361359848;
+      s[105] = 0.8845962806133972;
+      t[105] = -0.9406978083414278;
+      w[105] = 0.0003599363171224237;
+      r[106] = -0.9406978083414277;
+      s[106] = -0.9719492361359848;
+      t[106] = -0.9719492361359848;
+      w[106] = 0.0003599363171224237;
+      r[107] = 0.8845962806133972;
+      s[107] = -0.9406978083414277;
+      t[107] = -0.9719492361359849;
+      w[107] = 0.0003599363171224237;
+      r[108] = 0.1011535049643996;
+      s[108] = -0.3535634288145484;
+      t[108] = -0.9763709473096609;
+      w[108] = 0.006935487029959765;
+      r[109] = -0.3535634288145484;
+      s[109] = -0.9763709473096609;
+      t[109] = 0.1011535049643997;
+      w[109] = 0.006935487029959765;
+      r[110] = -0.3535634288145484;
+      s[110] = 0.1011535049643997;
+      t[110] = -0.9763709473096609;
+      w[110] = 0.006935487029959765;
+      r[111] = -0.9763709473096609;
+      s[111] = 0.1011535049643996;
+      t[111] = -0.7712191288401904;
+      w[111] = 0.006935487029959765;
+      r[112] = -0.9763709473096609;
+      s[112] = 0.1011535049643996;
+      t[112] = -0.3535634288145484;
+      w[112] = 0.006935487029959765;
+      r[113] = -0.7712191288401904;
+      s[113] = 0.1011535049643997;
+      t[113] = -0.9763709473096609;
+      w[113] = 0.006935487029959765;
+      r[114] = -0.9763709473096609;
+      s[114] = -0.3535634288145484;
+      t[114] = -0.7712191288401904;
+      w[114] = 0.006935487029959765;
+      r[115] = -0.9763709473096609;
+      s[115] = -0.7712191288401904;
+      t[115] = 0.1011535049643996;
+      w[115] = 0.006935487029959765;
+      r[116] = -0.7712191288401904;
+      s[116] = -0.3535634288145484;
+      t[116] = -0.9763709473096609;
+      w[116] = 0.006935487029959765;
+      r[117] = 0.1011535049643996;
+      s[117] = -0.3535634288145484;
+      t[117] = -0.7712191288401904;
+      w[117] = 0.006935487029959765;
+      r[118] = -0.7712191288401904;
+      s[118] = 0.1011535049643996;
+      t[118] = -0.3535634288145484;
+      w[118] = 0.006935487029959765;
+      r[119] = -0.9763709473096609;
+      s[119] = -0.3535634288145484;
+      t[119] = 0.1011535049643996;
+      w[119] = 0.006935487029959765;
+      r[120] = -0.7712191288401904;
+      s[120] = -0.3535634288145484;
+      t[120] = 0.1011535049643996;
+      w[120] = 0.006935487029959765;
+      r[121] = 0.1011535049643997;
+      s[121] = -0.7712191288401904;
+      t[121] = -0.9763709473096609;
+      w[121] = 0.006935487029959765;
+      r[122] = -0.9763709473096609;
+      s[122] = -0.7712191288401904;
+      t[122] = -0.3535634288145484;
+      w[122] = 0.006935487029959765;
+      r[123] = -0.3535634288145484;
+      s[123] = -0.7712191288401904;
+      t[123] = -0.9763709473096609;
+      w[123] = 0.006935487029959765;
+      r[124] = 0.1011535049643996;
+      s[124] = -0.7712191288401904;
+      t[124] = -0.3535634288145484;
+      w[124] = 0.006935487029959765;
+      r[125] = -0.3535634288145484;
+      s[125] = -0.7712191288401904;
+      t[125] = 0.1011535049643996;
+      w[125] = 0.006935487029959765;
+      r[126] = -0.3535634288145484;
+      s[126] = 0.1011535049643996;
+      t[126] = -0.7712191288401904;
+      w[126] = 0.006935487029959765;
+      r[127] = -0.7712191288401904;
+      s[127] = -0.9763709473096609;
+      t[127] = 0.1011535049643997;
+      w[127] = 0.006935487029959765;
+      r[128] = 0.1011535049643997;
+      s[128] = -0.9763709473096609;
+      t[128] = -0.7712191288401904;
+      w[128] = 0.006935487029959765;
+      r[129] = 0.1011535049643996;
+      s[129] = -0.9763709473096609;
+      t[129] = -0.3535634288145484;
+      w[129] = 0.006935487029959765;
+      r[130] = -0.3535634288145484;
+      s[130] = -0.9763709473096609;
+      t[130] = -0.7712191288401904;
+      w[130] = 0.006935487029959765;
+      r[131] = -0.7712191288401904;
+      s[131] = -0.9763709473096609;
+      t[131] = -0.3535634288145484;
+      w[131] = 0.006935487029959765;
 
       break;
     }
     case 13: {
-      r[0]   =                 -0.5; s[0]   =                  -0.5; t[0]   =                  -0.5; w[0]   =   0.02570257046255168;
-      r[1]   =  -0.6329110087029203; s[1]   =   -0.6329110087029203; t[1]   =   -0.1012669738912393; w[1]   =     0.025755118605889;
-      r[2]   =  -0.6329110087029203; s[2]   =   -0.1012669738912393; t[2]   =   -0.6329110087029203; w[2]   =     0.025755118605889;
-      r[3]   =  -0.1012669738912393; s[3]   =   -0.6329110087029203; t[3]   =   -0.6329110087029203; w[3]   =     0.025755118605889;
-      r[4]   =  -0.6329110087029203; s[4]   =   -0.6329110087029203; t[4]   =   -0.6329110087029203; w[4]   =     0.025755118605889;
-      r[5]   =  -0.4045365578147406; s[5]   =   -0.4045365578147406; t[5]   =   -0.7863903265557781; w[5]   =   0.02596652605859084;
-      r[6]   =  -0.4045365578147406; s[6]   =   -0.7863903265557781; t[6]   =   -0.4045365578147406; w[6]   =   0.02596652605859084;
-      r[7]   =  -0.7863903265557781; s[7]   =   -0.4045365578147406; t[7]   =   -0.4045365578147406; w[7]   =   0.02596652605859084;
-      r[8]   =  -0.4045365578147406; s[8]   =   -0.4045365578147406; t[8]   =   -0.4045365578147406; w[8]   =   0.02596652605859084;
-      r[9]   =  -0.9646777838400239; s[9]   =   -0.9646777838400239; t[9]   =    0.8940333515200715; w[9]   = 0.0007544935237094989;
-      r[10]  =  -0.9646777838400239; s[10]  =    0.8940333515200715; t[10]  =   -0.9646777838400239; w[10]  = 0.0007544935237094989;
-      r[11]  =   0.8940333515200715; s[11]  =   -0.9646777838400239; t[11]  =   -0.9646777838400239; w[11]  = 0.0007544935237094989;
-      r[12]  =  -0.9646777838400239; s[12]  =   -0.9646777838400239; t[12]  =   -0.9646777838400239; w[12]  = 0.0007544935237094989;
-      r[13]  = -0.08904461651389284; s[13]  =   -0.9109553834861072; t[13]  =   -0.9109553834861072; w[13]  =   0.01010100489376552;
-      r[14]  =  -0.9109553834861072; s[14]  =  -0.08904461651389284; t[14]  =   -0.9109553834861072; w[14]  =   0.01010100489376552;
-      r[15]  = -0.08904461651389284; s[15]  =  -0.08904461651389284; t[15]  =   -0.9109553834861071; w[15]  =   0.01010100489376552;
-      r[16]  = -0.08904461651389284; s[16]  =   -0.9109553834861071; t[16]  =  -0.08904461651389284; w[16]  =   0.01010100489376552;
-      r[17]  =  -0.9109553834861071; s[17]  =  -0.08904461651389284; t[17]  =  -0.08904461651389284; w[17]  =   0.01010100489376552;
-      r[18]  =  -0.9109553834861072; s[18]  =   -0.9109553834861072; t[18]  =  -0.08904461651389284; w[18]  =   0.01010100489376552;
-      r[19]  =   0.1160327366305325; s[19]  =   -0.5846173877234908; t[19]  =   -0.9467979611835509; w[19]  =   0.01116031414450733;
-      r[20]  =   0.1160327366305325; s[20]  =   -0.5846173877234908; t[20]  =   -0.5846173877234908; w[20]  =   0.01116031414450733;
-      r[21]  =  -0.5846173877234908; s[21]  =   -0.5846173877234908; t[21]  =    0.1160327366305325; w[21]  =   0.01116031414450733;
-      r[22]  =  -0.9467979611835509; s[22]  =    0.1160327366305325; t[22]  =   -0.5846173877234908; w[22]  =   0.01116031414450733;
-      r[23]  =  -0.5846173877234908; s[23]  =   -0.9467979611835509; t[23]  =    0.1160327366305325; w[23]  =   0.01116031414450733;
-      r[24]  =  -0.5846173877234908; s[24]  =    0.1160327366305325; t[24]  =   -0.5846173877234908; w[24]  =   0.01116031414450733;
-      r[25]  =  -0.9467979611835509; s[25]  =   -0.5846173877234908; t[25]  =    0.1160327366305325; w[25]  =   0.01116031414450733;
-      r[26]  =  -0.5846173877234908; s[26]  =   -0.9467979611835509; t[26]  =   -0.5846173877234908; w[26]  =   0.01116031414450733;
-      r[27]  =  -0.5846173877234908; s[27]  =   -0.5846173877234908; t[27]  =   -0.9467979611835509; w[27]  =   0.01116031414450733;
-      r[28]  =  -0.5846173877234908; s[28]  =    0.1160327366305325; t[28]  =   -0.9467979611835509; w[28]  =   0.01116031414450733;
-      r[29]  =  -0.9467979611835509; s[29]  =   -0.5846173877234908; t[29]  =   -0.5846173877234908; w[29]  =   0.01116031414450733;
-      r[30]  =   0.1160327366305325; s[30]  =   -0.9467979611835509; t[30]  =   -0.5846173877234908; w[30]  =   0.01116031414450733;
-      r[31]  =   0.5400622913680578; s[31]  =   -0.8483461038575444; t[31]  =   -0.8433700836529689; w[31]  =  0.002501306177499892;
-      r[32]  =   0.5400622913680577; s[32]  =   -0.8483461038575444; t[32]  =   -0.8483461038575444; w[32]  =  0.002501306177499892;
-      r[33]  =  -0.8483461038575444; s[33]  =   -0.8483461038575444; t[33]  =    0.5400622913680577; w[33]  =  0.002501306177499892;
-      r[34]  =  -0.8433700836529689; s[34]  =    0.5400622913680577; t[34]  =   -0.8483461038575444; w[34]  =  0.002501306177499892;
-      r[35]  =  -0.8483461038575444; s[35]  =   -0.8433700836529689; t[35]  =    0.5400622913680577; w[35]  =  0.002501306177499892;
-      r[36]  =  -0.8483461038575444; s[36]  =    0.5400622913680577; t[36]  =   -0.8483461038575444; w[36]  =  0.002501306177499892;
-      r[37]  =  -0.8433700836529689; s[37]  =   -0.8483461038575444; t[37]  =    0.5400622913680577; w[37]  =  0.002501306177499892;
-      r[38]  =  -0.8483461038575444; s[38]  =   -0.8433700836529689; t[38]  =   -0.8483461038575444; w[38]  =  0.002501306177499892;
-      r[39]  =  -0.8483461038575444; s[39]  =   -0.8483461038575444; t[39]  =   -0.8433700836529689; w[39]  =  0.002501306177499892;
-      r[40]  =  -0.8483461038575444; s[40]  =    0.5400622913680577; t[40]  =   -0.8433700836529689; w[40]  =  0.002501306177499892;
-      r[41]  =  -0.8433700836529689; s[41]  =   -0.8483461038575444; t[41]  =   -0.8483461038575444; w[41]  =  0.002501306177499892;
-      r[42]  =   0.5400622913680578; s[42]  =   -0.8433700836529689; t[42]  =   -0.8483461038575444; w[42]  =  0.002501306177499892;
-      r[43]  =   0.4961756588167157; s[43]  =   -0.7568863921423576; t[43]  =   -0.9824028745320004; w[43]  =  0.004661475475166795;
-      r[44]  =   0.4961756588167155; s[44]  =   -0.7568863921423576; t[44]  =   -0.7568863921423576; w[44]  =  0.004661475475166795;
-      r[45]  =  -0.7568863921423576; s[45]  =   -0.7568863921423576; t[45]  =    0.4961756588167157; w[45]  =  0.004661475475166795;
-      r[46]  =  -0.9824028745320004; s[46]  =    0.4961756588167157; t[46]  =   -0.7568863921423576; w[46]  =  0.004661475475166795;
-      r[47]  =  -0.7568863921423576; s[47]  =   -0.9824028745320004; t[47]  =    0.4961756588167157; w[47]  =  0.004661475475166795;
-      r[48]  =  -0.7568863921423576; s[48]  =    0.4961756588167157; t[48]  =   -0.7568863921423576; w[48]  =  0.004661475475166795;
-      r[49]  =  -0.9824028745320004; s[49]  =   -0.7568863921423576; t[49]  =    0.4961756588167157; w[49]  =  0.004661475475166795;
-      r[50]  =  -0.7568863921423576; s[50]  =   -0.9824028745320004; t[50]  =   -0.7568863921423576; w[50]  =  0.004661475475166795;
-      r[51]  =  -0.7568863921423576; s[51]  =   -0.7568863921423576; t[51]  =   -0.9824028745320004; w[51]  =  0.004661475475166795;
-      r[52]  =  -0.7568863921423576; s[52]  =    0.4961756588167157; t[52]  =   -0.9824028745320004; w[52]  =  0.004661475475166795;
-      r[53]  =  -0.9824028745320004; s[53]  =   -0.7568863921423576; t[53]  =   -0.7568863921423576; w[53]  =  0.004661475475166795;
-      r[54]  =   0.4961756588167157; s[54]  =   -0.9824028745320004; t[54]  =   -0.7568863921423576; w[54]  =  0.004661475475166795;
-      r[55]  =   0.7273541110818488; s[55]  =   -0.9597087051542637; t[55]  =   -0.8079367007733216; w[55]  =  0.002445605512977689;
-      r[56]  =   0.7273541110818489; s[56]  =   -0.9597087051542637; t[56]  =   -0.9597087051542637; w[56]  =  0.002445605512977689;
-      r[57]  =  -0.9597087051542637; s[57]  =   -0.9597087051542637; t[57]  =    0.7273541110818489; w[57]  =  0.002445605512977689;
-      r[58]  =  -0.8079367007733216; s[58]  =    0.7273541110818489; t[58]  =   -0.9597087051542637; w[58]  =  0.002445605512977689;
-      r[59]  =  -0.9597087051542637; s[59]  =   -0.8079367007733216; t[59]  =    0.7273541110818489; w[59]  =  0.002445605512977689;
-      r[60]  =  -0.9597087051542637; s[60]  =    0.7273541110818489; t[60]  =   -0.9597087051542637; w[60]  =  0.002445605512977689;
-      r[61]  =  -0.8079367007733216; s[61]  =   -0.9597087051542637; t[61]  =    0.7273541110818489; w[61]  =  0.002445605512977689;
-      r[62]  =  -0.9597087051542637; s[62]  =   -0.8079367007733216; t[62]  =   -0.9597087051542637; w[62]  =  0.002445605512977689;
-      r[63]  =  -0.9597087051542637; s[63]  =   -0.9597087051542637; t[63]  =   -0.8079367007733216; w[63]  =  0.002445605512977689;
-      r[64]  =  -0.9597087051542637; s[64]  =    0.7273541110818489; t[64]  =   -0.8079367007733216; w[64]  =  0.002445605512977689;
-      r[65]  =  -0.8079367007733216; s[65]  =   -0.9597087051542637; t[65]  =   -0.9597087051542637; w[65]  =  0.002445605512977689;
-      r[66]  =   0.7273541110818488; s[66]  =   -0.8079367007733216; t[66]  =   -0.9597087051542637; w[66]  =  0.002445605512977689;
-      r[67]  =  -0.9671310349065154; s[67]  =   -0.2352788816640514; t[67]  =   -0.5623112017653817; w[67]  =  0.009916060005751849;
-      r[68]  =  -0.9671310349065154; s[68]  =   -0.2352788816640514; t[68]  =   -0.2352788816640514; w[68]  =  0.009916060005751849;
-      r[69]  =  -0.2352788816640514; s[69]  =   -0.2352788816640514; t[69]  =   -0.9671310349065154; w[69]  =  0.009916060005751849;
-      r[70]  =  -0.5623112017653817; s[70]  =   -0.9671310349065154; t[70]  =   -0.2352788816640514; w[70]  =  0.009916060005751849;
-      r[71]  =  -0.2352788816640514; s[71]  =   -0.5623112017653817; t[71]  =   -0.9671310349065153; w[71]  =  0.009916060005751849;
-      r[72]  =  -0.2352788816640514; s[72]  =   -0.9671310349065154; t[72]  =   -0.2352788816640514; w[72]  =  0.009916060005751849;
-      r[73]  =  -0.5623112017653817; s[73]  =   -0.2352788816640514; t[73]  =   -0.9671310349065154; w[73]  =  0.009916060005751849;
-      r[74]  =  -0.2352788816640514; s[74]  =   -0.5623112017653817; t[74]  =   -0.2352788816640514; w[74]  =  0.009916060005751849;
-      r[75]  =  -0.2352788816640514; s[75]  =   -0.2352788816640514; t[75]  =   -0.5623112017653817; w[75]  =  0.009916060005751849;
-      r[76]  =  -0.2352788816640514; s[76]  =   -0.9671310349065153; t[76]  =   -0.5623112017653817; w[76]  =  0.009916060005751849;
-      r[77]  =  -0.5623112017653817; s[77]  =   -0.2352788816640514; t[77]  =   -0.2352788816640514; w[77]  =  0.009916060005751849;
-      r[78]  =  -0.9671310349065154; s[78]  =   -0.5623112017653817; t[78]  =   -0.2352788816640514; w[78]  =  0.009916060005751849;
-      r[79]  =   0.1759133631658635; s[79]  =   -0.9999999160158975; t[79]  =   -0.1759135311340684; w[79]  = 0.0006021025520830907;
-      r[80]  =   0.1759133631658635; s[80]  =   -0.9999999160158977; t[80]  =   -0.9999999160158977; w[80]  = 0.0006021025520830907;
-      r[81]  =  -0.9999999160158977; s[81]  =   -0.9999999160158977; t[81]  =    0.1759133631658636; w[81]  = 0.0006021025520830907;
-      r[82]  =  -0.1759135311340684; s[82]  =    0.1759133631658636; t[82]  =   -0.9999999160158977; w[82]  = 0.0006021025520830907;
-      r[83]  =  -0.9999999160158977; s[83]  =   -0.1759135311340684; t[83]  =    0.1759133631658635; w[83]  = 0.0006021025520830907;
-      r[84]  =  -0.9999999160158977; s[84]  =    0.1759133631658636; t[84]  =   -0.9999999160158977; w[84]  = 0.0006021025520830907;
-      r[85]  =  -0.1759135311340684; s[85]  =   -0.9999999160158977; t[85]  =    0.1759133631658636; w[85]  = 0.0006021025520830907;
-      r[86]  =  -0.9999999160158977; s[86]  =   -0.1759135311340684; t[86]  =   -0.9999999160158977; w[86]  = 0.0006021025520830907;
-      r[87]  =  -0.9999999160158977; s[87]  =   -0.9999999160158977; t[87]  =   -0.1759135311340684; w[87]  = 0.0006021025520830907;
-      r[88]  =  -0.9999999160158977; s[88]  =    0.1759133631658635; t[88]  =   -0.1759135311340684; w[88]  = 0.0006021025520830907;
-      r[89]  =  -0.1759135311340684; s[89]  =   -0.9999999160158977; t[89]  =   -0.9999999160158977; w[89]  = 0.0006021025520830907;
-      r[90]  =   0.1759133631658635; s[90]  =   -0.1759135311340684; t[90]  =   -0.9999999160158975; w[90]  = 0.0006021025520830907;
-      r[91]  =   0.2530466848028199; s[91]  =    -0.831586279456956; t[91]  =    -0.589874125888908; w[91]  =   0.01402602083723675;
-      r[92]  =   0.2530466848028199; s[92]  =    -0.831586279456956; t[92]  =    -0.831586279456956; w[92]  =   0.01402602083723675;
-      r[93]  =   -0.831586279456956; s[93]  =    -0.831586279456956; t[93]  =    0.2530466848028199; w[93]  =   0.01402602083723675;
-      r[94]  =   -0.589874125888908; s[94]  =    0.2530466848028199; t[94]  =    -0.831586279456956; w[94]  =   0.01402602083723675;
-      r[95]  =   -0.831586279456956; s[95]  =    -0.589874125888908; t[95]  =    0.2530466848028199; w[95]  =   0.01402602083723675;
-      r[96]  =   -0.831586279456956; s[96]  =    0.2530466848028199; t[96]  =    -0.831586279456956; w[96]  =   0.01402602083723675;
-      r[97]  =   -0.589874125888908; s[97]  =    -0.831586279456956; t[97]  =    0.2530466848028199; w[97]  =   0.01402602083723675;
-      r[98]  =   -0.831586279456956; s[98]  =    -0.589874125888908; t[98]  =    -0.831586279456956; w[98]  =   0.01402602083723675;
-      r[99]  =   -0.831586279456956; s[99]  =    -0.831586279456956; t[99]  =    -0.589874125888908; w[99]  =   0.01402602083723675;
-      r[100] =   -0.831586279456956; s[100] =    0.2530466848028199; t[100] =    -0.589874125888908; w[100] =   0.01402602083723675;
-      r[101] =   -0.589874125888908; s[101] =    -0.831586279456956; t[101] =    -0.831586279456956; w[101] =   0.01402602083723675;
-      r[102] =   0.2530466848028199; s[102] =    -0.589874125888908; t[102] =    -0.831586279456956; w[102] =   0.01402602083723675;
-      r[103] =   0.4427772816839441; s[103] =   -0.9504935036420215; t[103] =   -0.5417902743999015; w[103] =  0.004713294756390646;
-      r[104] =   0.4427772816839441; s[104] =   -0.9504935036420213; t[104] =   -0.9504935036420213; w[104] =  0.004713294756390646;
-      r[105] =  -0.9504935036420213; s[105] =   -0.9504935036420213; t[105] =     0.442777281683944; w[105] =  0.004713294756390646;
-      r[106] =  -0.5417902743999015; s[106] =    0.4427772816839441; t[106] =   -0.9504935036420212; w[106] =  0.004713294756390646;
-      r[107] =  -0.9504935036420215; s[107] =   -0.5417902743999015; t[107] =    0.4427772816839441; w[107] =  0.004713294756390646;
-      r[108] =  -0.9504935036420213; s[108] =     0.442777281683944; t[108] =   -0.9504935036420213; w[108] =  0.004713294756390646;
-      r[109] =  -0.5417902743999015; s[109] =   -0.9504935036420212; t[109] =    0.4427772816839441; w[109] =  0.004713294756390646;
-      r[110] =  -0.9504935036420215; s[110] =   -0.5417902743999015; t[110] =   -0.9504935036420213; w[110] =  0.004713294756390646;
-      r[111] =  -0.9504935036420215; s[111] =   -0.9504935036420213; t[111] =   -0.5417902743999015; w[111] =  0.004713294756390646;
-      r[112] =  -0.9504935036420215; s[112] =    0.4427772816839441; t[112] =   -0.5417902743999015; w[112] =  0.004713294756390646;
-      r[113] =  -0.5417902743999015; s[113] =   -0.9504935036420213; t[113] =   -0.9504935036420213; w[113] =  0.004713294756390646;
-      r[114] =   0.4427772816839441; s[114] =   -0.5417902743999015; t[114] =   -0.9504935036420215; w[114] =  0.004713294756390646;
-      r[115] =   -0.368542015595983; s[115] =   -0.1027697847087988; t[115] =   -0.8393942724781172; w[115] =   0.01264454161650734;
-      r[116] =  -0.1027697847087988; s[116] =   -0.8393942724781172; t[116] =   -0.3685420155959831; w[116] =   0.01264454161650734;
-      r[117] =  -0.1027697847087988; s[117] =   -0.3685420155959831; t[117] =   -0.8393942724781172; w[117] =   0.01264454161650734;
-      r[118] =  -0.8393942724781172; s[118] =    -0.368542015595983; t[118] =   -0.6892939272171009; w[118] =   0.01264454161650734;
-      r[119] =   -0.839394272478117; s[119] =   -0.3685420155959831; t[119] =   -0.1027697847087988; w[119] =   0.01264454161650734;
-      r[120] =  -0.6892939272171009; s[120] =   -0.3685420155959831; t[120] =   -0.8393942724781172; w[120] =   0.01264454161650734;
-      r[121] =  -0.8393942724781172; s[121] =   -0.1027697847087988; t[121] =   -0.6892939272171009; w[121] =   0.01264454161650734;
-      r[122] =  -0.8393942724781172; s[122] =   -0.6892939272171009; t[122] =    -0.368542015595983; w[122] =   0.01264454161650734;
-      r[123] =  -0.6892939272171009; s[123] =   -0.1027697847087988; t[123] =   -0.8393942724781172; w[123] =   0.01264454161650734;
-      r[124] =  -0.3685420155959831; s[124] =   -0.1027697847087988; t[124] =   -0.6892939272171009; w[124] =   0.01264454161650734;
-      r[125] =  -0.6892939272171009; s[125] =   -0.3685420155959831; t[125] =   -0.1027697847087988; w[125] =   0.01264454161650734;
-      r[126] =   -0.839394272478117; s[126] =   -0.1027697847087988; t[126] =   -0.3685420155959831; w[126] =   0.01264454161650734;
-      r[127] =  -0.6892939272171009; s[127] =   -0.1027697847087988; t[127] =   -0.3685420155959831; w[127] =   0.01264454161650734;
-      r[128] =   -0.368542015595983; s[128] =   -0.6892939272171009; t[128] =   -0.8393942724781172; w[128] =   0.01264454161650734;
-      r[129] =  -0.8393942724781172; s[129] =   -0.6892939272171009; t[129] =   -0.1027697847087988; w[129] =   0.01264454161650734;
-      r[130] =  -0.1027697847087988; s[130] =   -0.6892939272171009; t[130] =   -0.8393942724781172; w[130] =   0.01264454161650734;
-      r[131] =  -0.3685420155959831; s[131] =   -0.6892939272171009; t[131] =   -0.1027697847087988; w[131] =   0.01264454161650734;
-      r[132] =  -0.1027697847087988; s[132] =   -0.6892939272171009; t[132] =   -0.3685420155959831; w[132] =   0.01264454161650734;
-      r[133] =  -0.1027697847087988; s[133] =   -0.3685420155959831; t[133] =   -0.6892939272171009; w[133] =   0.01264454161650734;
-      r[134] =  -0.6892939272171009; s[134] =   -0.8393942724781172; t[134] =   -0.3685420155959831; w[134] =   0.01264454161650734;
-      r[135] =   -0.368542015595983; s[135] =   -0.8393942724781172; t[135] =   -0.6892939272171009; w[135] =   0.01264454161650734;
-      r[136] =   -0.368542015595983; s[136] =   -0.8393942724781172; t[136] =   -0.1027697847087988; w[136] =   0.01264454161650734;
-      r[137] =  -0.1027697847087988; s[137] =   -0.8393942724781172; t[137] =   -0.6892939272171009; w[137] =   0.01264454161650734;
-      r[138] =  -0.6892939272171009; s[138] =   -0.8393942724781172; t[138] =   -0.1027697847087988; w[138] =   0.01264454161650734;
-      r[139] =   0.1413168803104978; s[139] =   -0.3372367253999866; t[139] =   -0.9796911310165592; w[139] =  0.005555709517495258;
-      r[140] =  -0.3372367253999866; s[140] =   -0.9796911310165592; t[140] =    0.1413168803104978; w[140] =  0.005555709517495258;
-      r[141] =  -0.3372367253999866; s[141] =    0.1413168803104978; t[141] =   -0.9796911310165592; w[141] =  0.005555709517495258;
-      r[142] =  -0.9796911310165592; s[142] =    0.1413168803104978; t[142] =    -0.824389023893952; w[142] =  0.005555709517495258;
-      r[143] =  -0.9796911310165592; s[143] =    0.1413168803104978; t[143] =   -0.3372367253999866; w[143] =  0.005555709517495258;
-      r[144] =   -0.824389023893952; s[144] =    0.1413168803104978; t[144] =   -0.9796911310165592; w[144] =  0.005555709517495258;
-      r[145] =  -0.9796911310165592; s[145] =   -0.3372367253999866; t[145] =    -0.824389023893952; w[145] =  0.005555709517495258;
-      r[146] =  -0.9796911310165592; s[146] =    -0.824389023893952; t[146] =    0.1413168803104978; w[146] =  0.005555709517495258;
-      r[147] =   -0.824389023893952; s[147] =   -0.3372367253999866; t[147] =   -0.9796911310165592; w[147] =  0.005555709517495258;
-      r[148] =   0.1413168803104978; s[148] =   -0.3372367253999866; t[148] =    -0.824389023893952; w[148] =  0.005555709517495258;
-      r[149] =   -0.824389023893952; s[149] =    0.1413168803104978; t[149] =   -0.3372367253999866; w[149] =  0.005555709517495258;
-      r[150] =  -0.9796911310165592; s[150] =   -0.3372367253999866; t[150] =    0.1413168803104978; w[150] =  0.005555709517495258;
-      r[151] =   -0.824389023893952; s[151] =   -0.3372367253999866; t[151] =    0.1413168803104978; w[151] =  0.005555709517495258;
-      r[152] =   0.1413168803104978; s[152] =    -0.824389023893952; t[152] =   -0.9796911310165592; w[152] =  0.005555709517495258;
-      r[153] =  -0.9796911310165592; s[153] =    -0.824389023893952; t[153] =   -0.3372367253999866; w[153] =  0.005555709517495258;
-      r[154] =  -0.3372367253999866; s[154] =    -0.824389023893952; t[154] =   -0.9796911310165592; w[154] =  0.005555709517495258;
-      r[155] =   0.1413168803104978; s[155] =    -0.824389023893952; t[155] =   -0.3372367253999866; w[155] =  0.005555709517495258;
-      r[156] =  -0.3372367253999866; s[156] =    -0.824389023893952; t[156] =    0.1413168803104978; w[156] =  0.005555709517495258;
-      r[157] =  -0.3372367253999866; s[157] =    0.1413168803104978; t[157] =    -0.824389023893952; w[157] =  0.005555709517495258;
-      r[158] =   -0.824389023893952; s[158] =   -0.9796911310165592; t[158] =    0.1413168803104978; w[158] =  0.005555709517495258;
-      r[159] =   0.1413168803104978; s[159] =   -0.9796911310165592; t[159] =    -0.824389023893952; w[159] =  0.005555709517495258;
-      r[160] =   0.1413168803104978; s[160] =   -0.9796911310165592; t[160] =   -0.3372367253999866; w[160] =  0.005555709517495258;
-      r[161] =  -0.3372367253999866; s[161] =   -0.9796911310165592; t[161] =    -0.824389023893952; w[161] =  0.005555709517495258;
-      r[162] =   -0.824389023893952; s[162] =   -0.9796911310165592; t[162] =   -0.3372367253999866; w[162] =  0.005555709517495258;
+      r[0] = -0.5;
+      s[0] = -0.5;
+      t[0] = -0.5;
+      w[0] = 0.02570257046255168;
+      r[1] = -0.6329110087029203;
+      s[1] = -0.6329110087029203;
+      t[1] = -0.1012669738912393;
+      w[1] = 0.025755118605889;
+      r[2] = -0.6329110087029203;
+      s[2] = -0.1012669738912393;
+      t[2] = -0.6329110087029203;
+      w[2] = 0.025755118605889;
+      r[3] = -0.1012669738912393;
+      s[3] = -0.6329110087029203;
+      t[3] = -0.6329110087029203;
+      w[3] = 0.025755118605889;
+      r[4] = -0.6329110087029203;
+      s[4] = -0.6329110087029203;
+      t[4] = -0.6329110087029203;
+      w[4] = 0.025755118605889;
+      r[5] = -0.4045365578147406;
+      s[5] = -0.4045365578147406;
+      t[5] = -0.7863903265557781;
+      w[5] = 0.02596652605859084;
+      r[6] = -0.4045365578147406;
+      s[6] = -0.7863903265557781;
+      t[6] = -0.4045365578147406;
+      w[6] = 0.02596652605859084;
+      r[7] = -0.7863903265557781;
+      s[7] = -0.4045365578147406;
+      t[7] = -0.4045365578147406;
+      w[7] = 0.02596652605859084;
+      r[8] = -0.4045365578147406;
+      s[8] = -0.4045365578147406;
+      t[8] = -0.4045365578147406;
+      w[8] = 0.02596652605859084;
+      r[9] = -0.9646777838400239;
+      s[9] = -0.9646777838400239;
+      t[9] = 0.8940333515200715;
+      w[9] = 0.0007544935237094989;
+      r[10] = -0.9646777838400239;
+      s[10] = 0.8940333515200715;
+      t[10] = -0.9646777838400239;
+      w[10] = 0.0007544935237094989;
+      r[11] = 0.8940333515200715;
+      s[11] = -0.9646777838400239;
+      t[11] = -0.9646777838400239;
+      w[11] = 0.0007544935237094989;
+      r[12] = -0.9646777838400239;
+      s[12] = -0.9646777838400239;
+      t[12] = -0.9646777838400239;
+      w[12] = 0.0007544935237094989;
+      r[13] = -0.08904461651389284;
+      s[13] = -0.9109553834861072;
+      t[13] = -0.9109553834861072;
+      w[13] = 0.01010100489376552;
+      r[14] = -0.9109553834861072;
+      s[14] = -0.08904461651389284;
+      t[14] = -0.9109553834861072;
+      w[14] = 0.01010100489376552;
+      r[15] = -0.08904461651389284;
+      s[15] = -0.08904461651389284;
+      t[15] = -0.9109553834861071;
+      w[15] = 0.01010100489376552;
+      r[16] = -0.08904461651389284;
+      s[16] = -0.9109553834861071;
+      t[16] = -0.08904461651389284;
+      w[16] = 0.01010100489376552;
+      r[17] = -0.9109553834861071;
+      s[17] = -0.08904461651389284;
+      t[17] = -0.08904461651389284;
+      w[17] = 0.01010100489376552;
+      r[18] = -0.9109553834861072;
+      s[18] = -0.9109553834861072;
+      t[18] = -0.08904461651389284;
+      w[18] = 0.01010100489376552;
+      r[19] = 0.1160327366305325;
+      s[19] = -0.5846173877234908;
+      t[19] = -0.9467979611835509;
+      w[19] = 0.01116031414450733;
+      r[20] = 0.1160327366305325;
+      s[20] = -0.5846173877234908;
+      t[20] = -0.5846173877234908;
+      w[20] = 0.01116031414450733;
+      r[21] = -0.5846173877234908;
+      s[21] = -0.5846173877234908;
+      t[21] = 0.1160327366305325;
+      w[21] = 0.01116031414450733;
+      r[22] = -0.9467979611835509;
+      s[22] = 0.1160327366305325;
+      t[22] = -0.5846173877234908;
+      w[22] = 0.01116031414450733;
+      r[23] = -0.5846173877234908;
+      s[23] = -0.9467979611835509;
+      t[23] = 0.1160327366305325;
+      w[23] = 0.01116031414450733;
+      r[24] = -0.5846173877234908;
+      s[24] = 0.1160327366305325;
+      t[24] = -0.5846173877234908;
+      w[24] = 0.01116031414450733;
+      r[25] = -0.9467979611835509;
+      s[25] = -0.5846173877234908;
+      t[25] = 0.1160327366305325;
+      w[25] = 0.01116031414450733;
+      r[26] = -0.5846173877234908;
+      s[26] = -0.9467979611835509;
+      t[26] = -0.5846173877234908;
+      w[26] = 0.01116031414450733;
+      r[27] = -0.5846173877234908;
+      s[27] = -0.5846173877234908;
+      t[27] = -0.9467979611835509;
+      w[27] = 0.01116031414450733;
+      r[28] = -0.5846173877234908;
+      s[28] = 0.1160327366305325;
+      t[28] = -0.9467979611835509;
+      w[28] = 0.01116031414450733;
+      r[29] = -0.9467979611835509;
+      s[29] = -0.5846173877234908;
+      t[29] = -0.5846173877234908;
+      w[29] = 0.01116031414450733;
+      r[30] = 0.1160327366305325;
+      s[30] = -0.9467979611835509;
+      t[30] = -0.5846173877234908;
+      w[30] = 0.01116031414450733;
+      r[31] = 0.5400622913680578;
+      s[31] = -0.8483461038575444;
+      t[31] = -0.8433700836529689;
+      w[31] = 0.002501306177499892;
+      r[32] = 0.5400622913680577;
+      s[32] = -0.8483461038575444;
+      t[32] = -0.8483461038575444;
+      w[32] = 0.002501306177499892;
+      r[33] = -0.8483461038575444;
+      s[33] = -0.8483461038575444;
+      t[33] = 0.5400622913680577;
+      w[33] = 0.002501306177499892;
+      r[34] = -0.8433700836529689;
+      s[34] = 0.5400622913680577;
+      t[34] = -0.8483461038575444;
+      w[34] = 0.002501306177499892;
+      r[35] = -0.8483461038575444;
+      s[35] = -0.8433700836529689;
+      t[35] = 0.5400622913680577;
+      w[35] = 0.002501306177499892;
+      r[36] = -0.8483461038575444;
+      s[36] = 0.5400622913680577;
+      t[36] = -0.8483461038575444;
+      w[36] = 0.002501306177499892;
+      r[37] = -0.8433700836529689;
+      s[37] = -0.8483461038575444;
+      t[37] = 0.5400622913680577;
+      w[37] = 0.002501306177499892;
+      r[38] = -0.8483461038575444;
+      s[38] = -0.8433700836529689;
+      t[38] = -0.8483461038575444;
+      w[38] = 0.002501306177499892;
+      r[39] = -0.8483461038575444;
+      s[39] = -0.8483461038575444;
+      t[39] = -0.8433700836529689;
+      w[39] = 0.002501306177499892;
+      r[40] = -0.8483461038575444;
+      s[40] = 0.5400622913680577;
+      t[40] = -0.8433700836529689;
+      w[40] = 0.002501306177499892;
+      r[41] = -0.8433700836529689;
+      s[41] = -0.8483461038575444;
+      t[41] = -0.8483461038575444;
+      w[41] = 0.002501306177499892;
+      r[42] = 0.5400622913680578;
+      s[42] = -0.8433700836529689;
+      t[42] = -0.8483461038575444;
+      w[42] = 0.002501306177499892;
+      r[43] = 0.4961756588167157;
+      s[43] = -0.7568863921423576;
+      t[43] = -0.9824028745320004;
+      w[43] = 0.004661475475166795;
+      r[44] = 0.4961756588167155;
+      s[44] = -0.7568863921423576;
+      t[44] = -0.7568863921423576;
+      w[44] = 0.004661475475166795;
+      r[45] = -0.7568863921423576;
+      s[45] = -0.7568863921423576;
+      t[45] = 0.4961756588167157;
+      w[45] = 0.004661475475166795;
+      r[46] = -0.9824028745320004;
+      s[46] = 0.4961756588167157;
+      t[46] = -0.7568863921423576;
+      w[46] = 0.004661475475166795;
+      r[47] = -0.7568863921423576;
+      s[47] = -0.9824028745320004;
+      t[47] = 0.4961756588167157;
+      w[47] = 0.004661475475166795;
+      r[48] = -0.7568863921423576;
+      s[48] = 0.4961756588167157;
+      t[48] = -0.7568863921423576;
+      w[48] = 0.004661475475166795;
+      r[49] = -0.9824028745320004;
+      s[49] = -0.7568863921423576;
+      t[49] = 0.4961756588167157;
+      w[49] = 0.004661475475166795;
+      r[50] = -0.7568863921423576;
+      s[50] = -0.9824028745320004;
+      t[50] = -0.7568863921423576;
+      w[50] = 0.004661475475166795;
+      r[51] = -0.7568863921423576;
+      s[51] = -0.7568863921423576;
+      t[51] = -0.9824028745320004;
+      w[51] = 0.004661475475166795;
+      r[52] = -0.7568863921423576;
+      s[52] = 0.4961756588167157;
+      t[52] = -0.9824028745320004;
+      w[52] = 0.004661475475166795;
+      r[53] = -0.9824028745320004;
+      s[53] = -0.7568863921423576;
+      t[53] = -0.7568863921423576;
+      w[53] = 0.004661475475166795;
+      r[54] = 0.4961756588167157;
+      s[54] = -0.9824028745320004;
+      t[54] = -0.7568863921423576;
+      w[54] = 0.004661475475166795;
+      r[55] = 0.7273541110818488;
+      s[55] = -0.9597087051542637;
+      t[55] = -0.8079367007733216;
+      w[55] = 0.002445605512977689;
+      r[56] = 0.7273541110818489;
+      s[56] = -0.9597087051542637;
+      t[56] = -0.9597087051542637;
+      w[56] = 0.002445605512977689;
+      r[57] = -0.9597087051542637;
+      s[57] = -0.9597087051542637;
+      t[57] = 0.7273541110818489;
+      w[57] = 0.002445605512977689;
+      r[58] = -0.8079367007733216;
+      s[58] = 0.7273541110818489;
+      t[58] = -0.9597087051542637;
+      w[58] = 0.002445605512977689;
+      r[59] = -0.9597087051542637;
+      s[59] = -0.8079367007733216;
+      t[59] = 0.7273541110818489;
+      w[59] = 0.002445605512977689;
+      r[60] = -0.9597087051542637;
+      s[60] = 0.7273541110818489;
+      t[60] = -0.9597087051542637;
+      w[60] = 0.002445605512977689;
+      r[61] = -0.8079367007733216;
+      s[61] = -0.9597087051542637;
+      t[61] = 0.7273541110818489;
+      w[61] = 0.002445605512977689;
+      r[62] = -0.9597087051542637;
+      s[62] = -0.8079367007733216;
+      t[62] = -0.9597087051542637;
+      w[62] = 0.002445605512977689;
+      r[63] = -0.9597087051542637;
+      s[63] = -0.9597087051542637;
+      t[63] = -0.8079367007733216;
+      w[63] = 0.002445605512977689;
+      r[64] = -0.9597087051542637;
+      s[64] = 0.7273541110818489;
+      t[64] = -0.8079367007733216;
+      w[64] = 0.002445605512977689;
+      r[65] = -0.8079367007733216;
+      s[65] = -0.9597087051542637;
+      t[65] = -0.9597087051542637;
+      w[65] = 0.002445605512977689;
+      r[66] = 0.7273541110818488;
+      s[66] = -0.8079367007733216;
+      t[66] = -0.9597087051542637;
+      w[66] = 0.002445605512977689;
+      r[67] = -0.9671310349065154;
+      s[67] = -0.2352788816640514;
+      t[67] = -0.5623112017653817;
+      w[67] = 0.009916060005751849;
+      r[68] = -0.9671310349065154;
+      s[68] = -0.2352788816640514;
+      t[68] = -0.2352788816640514;
+      w[68] = 0.009916060005751849;
+      r[69] = -0.2352788816640514;
+      s[69] = -0.2352788816640514;
+      t[69] = -0.9671310349065154;
+      w[69] = 0.009916060005751849;
+      r[70] = -0.5623112017653817;
+      s[70] = -0.9671310349065154;
+      t[70] = -0.2352788816640514;
+      w[70] = 0.009916060005751849;
+      r[71] = -0.2352788816640514;
+      s[71] = -0.5623112017653817;
+      t[71] = -0.9671310349065153;
+      w[71] = 0.009916060005751849;
+      r[72] = -0.2352788816640514;
+      s[72] = -0.9671310349065154;
+      t[72] = -0.2352788816640514;
+      w[72] = 0.009916060005751849;
+      r[73] = -0.5623112017653817;
+      s[73] = -0.2352788816640514;
+      t[73] = -0.9671310349065154;
+      w[73] = 0.009916060005751849;
+      r[74] = -0.2352788816640514;
+      s[74] = -0.5623112017653817;
+      t[74] = -0.2352788816640514;
+      w[74] = 0.009916060005751849;
+      r[75] = -0.2352788816640514;
+      s[75] = -0.2352788816640514;
+      t[75] = -0.5623112017653817;
+      w[75] = 0.009916060005751849;
+      r[76] = -0.2352788816640514;
+      s[76] = -0.9671310349065153;
+      t[76] = -0.5623112017653817;
+      w[76] = 0.009916060005751849;
+      r[77] = -0.5623112017653817;
+      s[77] = -0.2352788816640514;
+      t[77] = -0.2352788816640514;
+      w[77] = 0.009916060005751849;
+      r[78] = -0.9671310349065154;
+      s[78] = -0.5623112017653817;
+      t[78] = -0.2352788816640514;
+      w[78] = 0.009916060005751849;
+      r[79] = 0.1759133631658635;
+      s[79] = -0.9999999160158975;
+      t[79] = -0.1759135311340684;
+      w[79] = 0.0006021025520830907;
+      r[80] = 0.1759133631658635;
+      s[80] = -0.9999999160158977;
+      t[80] = -0.9999999160158977;
+      w[80] = 0.0006021025520830907;
+      r[81] = -0.9999999160158977;
+      s[81] = -0.9999999160158977;
+      t[81] = 0.1759133631658636;
+      w[81] = 0.0006021025520830907;
+      r[82] = -0.1759135311340684;
+      s[82] = 0.1759133631658636;
+      t[82] = -0.9999999160158977;
+      w[82] = 0.0006021025520830907;
+      r[83] = -0.9999999160158977;
+      s[83] = -0.1759135311340684;
+      t[83] = 0.1759133631658635;
+      w[83] = 0.0006021025520830907;
+      r[84] = -0.9999999160158977;
+      s[84] = 0.1759133631658636;
+      t[84] = -0.9999999160158977;
+      w[84] = 0.0006021025520830907;
+      r[85] = -0.1759135311340684;
+      s[85] = -0.9999999160158977;
+      t[85] = 0.1759133631658636;
+      w[85] = 0.0006021025520830907;
+      r[86] = -0.9999999160158977;
+      s[86] = -0.1759135311340684;
+      t[86] = -0.9999999160158977;
+      w[86] = 0.0006021025520830907;
+      r[87] = -0.9999999160158977;
+      s[87] = -0.9999999160158977;
+      t[87] = -0.1759135311340684;
+      w[87] = 0.0006021025520830907;
+      r[88] = -0.9999999160158977;
+      s[88] = 0.1759133631658635;
+      t[88] = -0.1759135311340684;
+      w[88] = 0.0006021025520830907;
+      r[89] = -0.1759135311340684;
+      s[89] = -0.9999999160158977;
+      t[89] = -0.9999999160158977;
+      w[89] = 0.0006021025520830907;
+      r[90] = 0.1759133631658635;
+      s[90] = -0.1759135311340684;
+      t[90] = -0.9999999160158975;
+      w[90] = 0.0006021025520830907;
+      r[91] = 0.2530466848028199;
+      s[91] = -0.831586279456956;
+      t[91] = -0.589874125888908;
+      w[91] = 0.01402602083723675;
+      r[92] = 0.2530466848028199;
+      s[92] = -0.831586279456956;
+      t[92] = -0.831586279456956;
+      w[92] = 0.01402602083723675;
+      r[93] = -0.831586279456956;
+      s[93] = -0.831586279456956;
+      t[93] = 0.2530466848028199;
+      w[93] = 0.01402602083723675;
+      r[94] = -0.589874125888908;
+      s[94] = 0.2530466848028199;
+      t[94] = -0.831586279456956;
+      w[94] = 0.01402602083723675;
+      r[95] = -0.831586279456956;
+      s[95] = -0.589874125888908;
+      t[95] = 0.2530466848028199;
+      w[95] = 0.01402602083723675;
+      r[96] = -0.831586279456956;
+      s[96] = 0.2530466848028199;
+      t[96] = -0.831586279456956;
+      w[96] = 0.01402602083723675;
+      r[97] = -0.589874125888908;
+      s[97] = -0.831586279456956;
+      t[97] = 0.2530466848028199;
+      w[97] = 0.01402602083723675;
+      r[98] = -0.831586279456956;
+      s[98] = -0.589874125888908;
+      t[98] = -0.831586279456956;
+      w[98] = 0.01402602083723675;
+      r[99] = -0.831586279456956;
+      s[99] = -0.831586279456956;
+      t[99] = -0.589874125888908;
+      w[99] = 0.01402602083723675;
+      r[100] = -0.831586279456956;
+      s[100] = 0.2530466848028199;
+      t[100] = -0.589874125888908;
+      w[100] = 0.01402602083723675;
+      r[101] = -0.589874125888908;
+      s[101] = -0.831586279456956;
+      t[101] = -0.831586279456956;
+      w[101] = 0.01402602083723675;
+      r[102] = 0.2530466848028199;
+      s[102] = -0.589874125888908;
+      t[102] = -0.831586279456956;
+      w[102] = 0.01402602083723675;
+      r[103] = 0.4427772816839441;
+      s[103] = -0.9504935036420215;
+      t[103] = -0.5417902743999015;
+      w[103] = 0.004713294756390646;
+      r[104] = 0.4427772816839441;
+      s[104] = -0.9504935036420213;
+      t[104] = -0.9504935036420213;
+      w[104] = 0.004713294756390646;
+      r[105] = -0.9504935036420213;
+      s[105] = -0.9504935036420213;
+      t[105] = 0.442777281683944;
+      w[105] = 0.004713294756390646;
+      r[106] = -0.5417902743999015;
+      s[106] = 0.4427772816839441;
+      t[106] = -0.9504935036420212;
+      w[106] = 0.004713294756390646;
+      r[107] = -0.9504935036420215;
+      s[107] = -0.5417902743999015;
+      t[107] = 0.4427772816839441;
+      w[107] = 0.004713294756390646;
+      r[108] = -0.9504935036420213;
+      s[108] = 0.442777281683944;
+      t[108] = -0.9504935036420213;
+      w[108] = 0.004713294756390646;
+      r[109] = -0.5417902743999015;
+      s[109] = -0.9504935036420212;
+      t[109] = 0.4427772816839441;
+      w[109] = 0.004713294756390646;
+      r[110] = -0.9504935036420215;
+      s[110] = -0.5417902743999015;
+      t[110] = -0.9504935036420213;
+      w[110] = 0.004713294756390646;
+      r[111] = -0.9504935036420215;
+      s[111] = -0.9504935036420213;
+      t[111] = -0.5417902743999015;
+      w[111] = 0.004713294756390646;
+      r[112] = -0.9504935036420215;
+      s[112] = 0.4427772816839441;
+      t[112] = -0.5417902743999015;
+      w[112] = 0.004713294756390646;
+      r[113] = -0.5417902743999015;
+      s[113] = -0.9504935036420213;
+      t[113] = -0.9504935036420213;
+      w[113] = 0.004713294756390646;
+      r[114] = 0.4427772816839441;
+      s[114] = -0.5417902743999015;
+      t[114] = -0.9504935036420215;
+      w[114] = 0.004713294756390646;
+      r[115] = -0.368542015595983;
+      s[115] = -0.1027697847087988;
+      t[115] = -0.8393942724781172;
+      w[115] = 0.01264454161650734;
+      r[116] = -0.1027697847087988;
+      s[116] = -0.8393942724781172;
+      t[116] = -0.3685420155959831;
+      w[116] = 0.01264454161650734;
+      r[117] = -0.1027697847087988;
+      s[117] = -0.3685420155959831;
+      t[117] = -0.8393942724781172;
+      w[117] = 0.01264454161650734;
+      r[118] = -0.8393942724781172;
+      s[118] = -0.368542015595983;
+      t[118] = -0.6892939272171009;
+      w[118] = 0.01264454161650734;
+      r[119] = -0.839394272478117;
+      s[119] = -0.3685420155959831;
+      t[119] = -0.1027697847087988;
+      w[119] = 0.01264454161650734;
+      r[120] = -0.6892939272171009;
+      s[120] = -0.3685420155959831;
+      t[120] = -0.8393942724781172;
+      w[120] = 0.01264454161650734;
+      r[121] = -0.8393942724781172;
+      s[121] = -0.1027697847087988;
+      t[121] = -0.6892939272171009;
+      w[121] = 0.01264454161650734;
+      r[122] = -0.8393942724781172;
+      s[122] = -0.6892939272171009;
+      t[122] = -0.368542015595983;
+      w[122] = 0.01264454161650734;
+      r[123] = -0.6892939272171009;
+      s[123] = -0.1027697847087988;
+      t[123] = -0.8393942724781172;
+      w[123] = 0.01264454161650734;
+      r[124] = -0.3685420155959831;
+      s[124] = -0.1027697847087988;
+      t[124] = -0.6892939272171009;
+      w[124] = 0.01264454161650734;
+      r[125] = -0.6892939272171009;
+      s[125] = -0.3685420155959831;
+      t[125] = -0.1027697847087988;
+      w[125] = 0.01264454161650734;
+      r[126] = -0.839394272478117;
+      s[126] = -0.1027697847087988;
+      t[126] = -0.3685420155959831;
+      w[126] = 0.01264454161650734;
+      r[127] = -0.6892939272171009;
+      s[127] = -0.1027697847087988;
+      t[127] = -0.3685420155959831;
+      w[127] = 0.01264454161650734;
+      r[128] = -0.368542015595983;
+      s[128] = -0.6892939272171009;
+      t[128] = -0.8393942724781172;
+      w[128] = 0.01264454161650734;
+      r[129] = -0.8393942724781172;
+      s[129] = -0.6892939272171009;
+      t[129] = -0.1027697847087988;
+      w[129] = 0.01264454161650734;
+      r[130] = -0.1027697847087988;
+      s[130] = -0.6892939272171009;
+      t[130] = -0.8393942724781172;
+      w[130] = 0.01264454161650734;
+      r[131] = -0.3685420155959831;
+      s[131] = -0.6892939272171009;
+      t[131] = -0.1027697847087988;
+      w[131] = 0.01264454161650734;
+      r[132] = -0.1027697847087988;
+      s[132] = -0.6892939272171009;
+      t[132] = -0.3685420155959831;
+      w[132] = 0.01264454161650734;
+      r[133] = -0.1027697847087988;
+      s[133] = -0.3685420155959831;
+      t[133] = -0.6892939272171009;
+      w[133] = 0.01264454161650734;
+      r[134] = -0.6892939272171009;
+      s[134] = -0.8393942724781172;
+      t[134] = -0.3685420155959831;
+      w[134] = 0.01264454161650734;
+      r[135] = -0.368542015595983;
+      s[135] = -0.8393942724781172;
+      t[135] = -0.6892939272171009;
+      w[135] = 0.01264454161650734;
+      r[136] = -0.368542015595983;
+      s[136] = -0.8393942724781172;
+      t[136] = -0.1027697847087988;
+      w[136] = 0.01264454161650734;
+      r[137] = -0.1027697847087988;
+      s[137] = -0.8393942724781172;
+      t[137] = -0.6892939272171009;
+      w[137] = 0.01264454161650734;
+      r[138] = -0.6892939272171009;
+      s[138] = -0.8393942724781172;
+      t[138] = -0.1027697847087988;
+      w[138] = 0.01264454161650734;
+      r[139] = 0.1413168803104978;
+      s[139] = -0.3372367253999866;
+      t[139] = -0.9796911310165592;
+      w[139] = 0.005555709517495258;
+      r[140] = -0.3372367253999866;
+      s[140] = -0.9796911310165592;
+      t[140] = 0.1413168803104978;
+      w[140] = 0.005555709517495258;
+      r[141] = -0.3372367253999866;
+      s[141] = 0.1413168803104978;
+      t[141] = -0.9796911310165592;
+      w[141] = 0.005555709517495258;
+      r[142] = -0.9796911310165592;
+      s[142] = 0.1413168803104978;
+      t[142] = -0.824389023893952;
+      w[142] = 0.005555709517495258;
+      r[143] = -0.9796911310165592;
+      s[143] = 0.1413168803104978;
+      t[143] = -0.3372367253999866;
+      w[143] = 0.005555709517495258;
+      r[144] = -0.824389023893952;
+      s[144] = 0.1413168803104978;
+      t[144] = -0.9796911310165592;
+      w[144] = 0.005555709517495258;
+      r[145] = -0.9796911310165592;
+      s[145] = -0.3372367253999866;
+      t[145] = -0.824389023893952;
+      w[145] = 0.005555709517495258;
+      r[146] = -0.9796911310165592;
+      s[146] = -0.824389023893952;
+      t[146] = 0.1413168803104978;
+      w[146] = 0.005555709517495258;
+      r[147] = -0.824389023893952;
+      s[147] = -0.3372367253999866;
+      t[147] = -0.9796911310165592;
+      w[147] = 0.005555709517495258;
+      r[148] = 0.1413168803104978;
+      s[148] = -0.3372367253999866;
+      t[148] = -0.824389023893952;
+      w[148] = 0.005555709517495258;
+      r[149] = -0.824389023893952;
+      s[149] = 0.1413168803104978;
+      t[149] = -0.3372367253999866;
+      w[149] = 0.005555709517495258;
+      r[150] = -0.9796911310165592;
+      s[150] = -0.3372367253999866;
+      t[150] = 0.1413168803104978;
+      w[150] = 0.005555709517495258;
+      r[151] = -0.824389023893952;
+      s[151] = -0.3372367253999866;
+      t[151] = 0.1413168803104978;
+      w[151] = 0.005555709517495258;
+      r[152] = 0.1413168803104978;
+      s[152] = -0.824389023893952;
+      t[152] = -0.9796911310165592;
+      w[152] = 0.005555709517495258;
+      r[153] = -0.9796911310165592;
+      s[153] = -0.824389023893952;
+      t[153] = -0.3372367253999866;
+      w[153] = 0.005555709517495258;
+      r[154] = -0.3372367253999866;
+      s[154] = -0.824389023893952;
+      t[154] = -0.9796911310165592;
+      w[154] = 0.005555709517495258;
+      r[155] = 0.1413168803104978;
+      s[155] = -0.824389023893952;
+      t[155] = -0.3372367253999866;
+      w[155] = 0.005555709517495258;
+      r[156] = -0.3372367253999866;
+      s[156] = -0.824389023893952;
+      t[156] = 0.1413168803104978;
+      w[156] = 0.005555709517495258;
+      r[157] = -0.3372367253999866;
+      s[157] = 0.1413168803104978;
+      t[157] = -0.824389023893952;
+      w[157] = 0.005555709517495258;
+      r[158] = -0.824389023893952;
+      s[158] = -0.9796911310165592;
+      t[158] = 0.1413168803104978;
+      w[158] = 0.005555709517495258;
+      r[159] = 0.1413168803104978;
+      s[159] = -0.9796911310165592;
+      t[159] = -0.824389023893952;
+      w[159] = 0.005555709517495258;
+      r[160] = 0.1413168803104978;
+      s[160] = -0.9796911310165592;
+      t[160] = -0.3372367253999866;
+      w[160] = 0.005555709517495258;
+      r[161] = -0.3372367253999866;
+      s[161] = -0.9796911310165592;
+      t[161] = -0.824389023893952;
+      w[161] = 0.005555709517495258;
+      r[162] = -0.824389023893952;
+      s[162] = -0.9796911310165592;
+      t[162] = -0.3372367253999866;
+      w[162] = 0.005555709517495258;
 
       break;
     }
     case 14: {
-      r[0]   =  -0.9153144959134277; s[0]   =   -0.9153144959134277; t[0]   =     0.745943487740283; w[0]   =  0.003176684382984782;
-      r[1]   =  -0.9153144959134277; s[1]   =     0.745943487740283; t[1]   =   -0.9153144959134277; w[1]   =  0.003176684382984782;
-      r[2]   =   0.7459434877402831; s[2]   =   -0.9153144959134277; t[2]   =   -0.9153144959134277; w[2]   =  0.003176684382984782;
-      r[3]   =  -0.9153144959134277; s[3]   =   -0.9153144959134277; t[3]   =   -0.9153144959134277; w[3]   =  0.003176684382984782;
-      r[4]   =  -0.7292035608164203; s[4]   =   -0.7292035608164203; t[4]   =    0.1876106824492612; w[4]   =  0.008958793406037778;
-      r[5]   =  -0.7292035608164203; s[5]   =    0.1876106824492612; t[5]   =   -0.7292035608164203; w[5]   =  0.008958793406037778;
-      r[6]   =   0.1876106824492612; s[6]   =   -0.7292035608164203; t[6]   =   -0.7292035608164203; w[6]   =  0.008958793406037778;
-      r[7]   =  -0.7292035608164203; s[7]   =   -0.7292035608164203; t[7]   =   -0.7292035608164203; w[7]   =  0.008958793406037778;
-      r[8]   =  -0.3709271370554474; s[8]   =   -0.3709271370554474; t[8]   =   -0.8872185888336577; w[8]   =   0.01117598049100474;
-      r[9]   =  -0.3709271370554474; s[9]   =   -0.8872185888336577; t[9]   =   -0.3709271370554474; w[9]   =   0.01117598049100474;
-      r[10]  =  -0.8872185888336577; s[10]  =   -0.3709271370554474; t[10]  =   -0.3709271370554474; w[10]  =   0.01117598049100474;
-      r[11]  =  -0.3709271370554474; s[11]  =   -0.3709271370554474; t[11]  =   -0.3709271370554474; w[11]  =   0.01117598049100474;
-      r[12]  =  -0.8344757841485797; s[12]  =   -0.8344757841485797; t[12]  =    0.5034273524457391; w[12]  =  0.006677534058303564;
-      r[13]  =  -0.8344757841485797; s[13]  =    0.5034273524457391; t[13]  =   -0.8344757841485797; w[13]  =  0.006677534058303564;
-      r[14]  =   0.5034273524457391; s[14]  =   -0.8344757841485797; t[14]  =   -0.8344757841485797; w[14]  =  0.006677534058303564;
-      r[15]  =  -0.8344757841485797; s[15]  =   -0.8344757841485797; t[15]  =   -0.8344757841485797; w[15]  =  0.006677534058303564;
-      r[16]  =  -0.1663704866153568; s[16]  =   -0.8336295133846432; t[16]  =   -0.8336295133846432; w[16]  =  0.008908689779326269;
-      r[17]  =  -0.8336295133846432; s[17]  =   -0.1663704866153568; t[17]  =   -0.8336295133846432; w[17]  =  0.008908689779326269;
-      r[18]  =  -0.1663704866153568; s[18]  =   -0.1663704866153568; t[18]  =   -0.8336295133846432; w[18]  =  0.008908689779326269;
-      r[19]  =  -0.1663704866153568; s[19]  =   -0.8336295133846432; t[19]  =   -0.1663704866153568; w[19]  =  0.008908689779326269;
-      r[20]  =  -0.8336295133846432; s[20]  =   -0.1663704866153568; t[20]  =   -0.1663704866153568; w[20]  =  0.008908689779326269;
-      r[21]  =  -0.8336295133846432; s[21]  =   -0.8336295133846432; t[21]  =   -0.1663704866153568; w[21]  =  0.008908689779326269;
-      r[22]  = -0.03464142965362016; s[22]  =   -0.9653585703463798; t[22]  =   -0.9653585703463798; w[22]  =   0.00328555582848326;
-      r[23]  =  -0.9653585703463798; s[23]  =  -0.03464142965362016; t[23]  =   -0.9653585703463798; w[23]  =   0.00328555582848326;
-      r[24]  = -0.03464142965362016; s[24]  =  -0.03464142965362016; t[24]  =   -0.9653585703463798; w[24]  =   0.00328555582848326;
-      r[25]  = -0.03464142965362016; s[25]  =   -0.9653585703463798; t[25]  =  -0.03464142965362016; w[25]  =   0.00328555582848326;
-      r[26]  =  -0.9653585703463798; s[26]  =  -0.03464142965362016; t[26]  =  -0.03464142965362016; w[26]  =   0.00328555582848326;
-      r[27]  =  -0.9653585703463798; s[27]  =   -0.9653585703463798; t[27]  =  -0.03464142965362016; w[27]  =   0.00328555582848326;
-      r[28]  =  -0.4789374311664119; s[28]  =   -0.5210625688335881; t[28]  =   -0.5210625688335881; w[28]  =  0.003034768187464438;
-      r[29]  =  -0.5210625688335881; s[29]  =   -0.4789374311664119; t[29]  =   -0.5210625688335881; w[29]  =  0.003034768187464438;
-      r[30]  =  -0.4789374311664119; s[30]  =   -0.4789374311664119; t[30]  =   -0.5210625688335881; w[30]  =  0.003034768187464438;
-      r[31]  =  -0.4789374311664119; s[31]  =   -0.5210625688335881; t[31]  =   -0.4789374311664119; w[31]  =  0.003034768187464438;
-      r[32]  =  -0.5210625688335881; s[32]  =   -0.4789374311664119; t[32]  =   -0.4789374311664119; w[32]  =  0.003034768187464438;
-      r[33]  =  -0.5210625688335881; s[33]  =   -0.5210625688335881; t[33]  =   -0.4789374311664119; w[33]  =  0.003034768187464438;
-      r[34]  =  -0.6648466287055623; s[34]  =    -0.234103305514385; t[34]  =   -0.8669467602656677; w[34]  =  0.009394571537633017;
-      r[35]  =  -0.6648466287055623; s[35]  =    -0.234103305514385; t[35]  =    -0.234103305514385; w[35]  =  0.009394571537633017;
-      r[36]  =   -0.234103305514385; s[36]  =    -0.234103305514385; t[36]  =   -0.6648466287055623; w[36]  =  0.009394571537633017;
-      r[37]  =  -0.8669467602656677; s[37]  =   -0.6648466287055623; t[37]  =    -0.234103305514385; w[37]  =  0.009394571537633017;
-      r[38]  =   -0.234103305514385; s[38]  =   -0.8669467602656677; t[38]  =   -0.6648466287055623; w[38]  =  0.009394571537633017;
-      r[39]  =   -0.234103305514385; s[39]  =   -0.6648466287055623; t[39]  =    -0.234103305514385; w[39]  =  0.009394571537633017;
-      r[40]  =  -0.8669467602656677; s[40]  =    -0.234103305514385; t[40]  =   -0.6648466287055623; w[40]  =  0.009394571537633017;
-      r[41]  =   -0.234103305514385; s[41]  =   -0.8669467602656677; t[41]  =    -0.234103305514385; w[41]  =  0.009394571537633017;
-      r[42]  =   -0.234103305514385; s[42]  =    -0.234103305514385; t[42]  =   -0.8669467602656677; w[42]  =  0.009394571537633017;
-      r[43]  =   -0.234103305514385; s[43]  =   -0.6648466287055623; t[43]  =   -0.8669467602656677; w[43]  =  0.009394571537633017;
-      r[44]  =  -0.8669467602656677; s[44]  =    -0.234103305514385; t[44]  =    -0.234103305514385; w[44]  =  0.009394571537633017;
-      r[45]  =  -0.6648466287055623; s[45]  =   -0.8669467602656677; t[45]  =    -0.234103305514385; w[45]  =  0.009394571537633017;
-      r[46]  =  -0.5658650959714019; s[46]  =   -0.2277398552115068; t[46]  =   -0.9786551936055847; w[46]  =  0.006724249255682279;
-      r[47]  =  -0.5658650959714018; s[47]  =   -0.2277398552115067; t[47]  =   -0.2277398552115067; w[47]  =  0.006724249255682279;
-      r[48]  =  -0.2277398552115067; s[48]  =   -0.2277398552115067; t[48]  =   -0.5658650959714018; w[48]  =  0.006724249255682279;
-      r[49]  =  -0.9786551936055847; s[49]  =   -0.5658650959714018; t[49]  =   -0.2277398552115067; w[49]  =  0.006724249255682279;
-      r[50]  =  -0.2277398552115067; s[50]  =   -0.9786551936055847; t[50]  =   -0.5658650959714018; w[50]  =  0.006724249255682279;
-      r[51]  =  -0.2277398552115067; s[51]  =   -0.5658650959714018; t[51]  =   -0.2277398552115067; w[51]  =  0.006724249255682279;
-      r[52]  =  -0.9786551936055847; s[52]  =   -0.2277398552115067; t[52]  =   -0.5658650959714018; w[52]  =  0.006724249255682279;
-      r[53]  =  -0.2277398552115068; s[53]  =   -0.9786551936055846; t[53]  =   -0.2277398552115068; w[53]  =  0.006724249255682279;
-      r[54]  =  -0.2277398552115068; s[54]  =   -0.2277398552115068; t[54]  =   -0.9786551936055846; w[54]  =  0.006724249255682279;
-      r[55]  =  -0.2277398552115067; s[55]  =   -0.5658650959714018; t[55]  =   -0.9786551936055847; w[55]  =  0.006724249255682279;
-      r[56]  =  -0.9786551936055847; s[56]  =   -0.2277398552115067; t[56]  =   -0.2277398552115067; w[56]  =  0.006724249255682279;
-      r[57]  =  -0.5658650959714019; s[57]  =   -0.9786551936055847; t[57]  =   -0.2277398552115068; w[57]  =  0.006724249255682279;
-      r[58]  =   0.8987448413516816; s[58]  =   -0.9881033648300827; t[58]  =   -0.9225381116915164; w[58]  = 0.0002384711012816958;
-      r[59]  =   0.8987448413516816; s[59]  =   -0.9881033648300825; t[59]  =   -0.9881033648300825; w[59]  = 0.0002384711012816958;
-      r[60]  =  -0.9881033648300825; s[60]  =   -0.9881033648300825; t[60]  =    0.8987448413516816; w[60]  = 0.0002384711012816958;
-      r[61]  =  -0.9225381116915166; s[61]  =    0.8987448413516816; t[61]  =   -0.9881033648300825; w[61]  = 0.0002384711012816958;
-      r[62]  =  -0.9881033648300825; s[62]  =   -0.9225381116915166; t[62]  =    0.8987448413516816; w[62]  = 0.0002384711012816958;
-      r[63]  =  -0.9881033648300825; s[63]  =    0.8987448413516816; t[63]  =   -0.9881033648300825; w[63]  = 0.0002384711012816958;
-      r[64]  =  -0.9225381116915166; s[64]  =   -0.9881033648300825; t[64]  =    0.8987448413516816; w[64]  = 0.0002384711012816958;
-      r[65]  =  -0.9881033648300825; s[65]  =   -0.9225381116915164; t[65]  =   -0.9881033648300825; w[65]  = 0.0002384711012816958;
-      r[66]  =  -0.9881033648300825; s[66]  =   -0.9881033648300825; t[66]  =   -0.9225381116915164; w[66]  = 0.0002384711012816958;
-      r[67]  =  -0.9881033648300825; s[67]  =    0.8987448413516816; t[67]  =   -0.9225381116915166; w[67]  = 0.0002384711012816958;
-      r[68]  =  -0.9225381116915164; s[68]  =   -0.9881033648300825; t[68]  =   -0.9881033648300825; w[68]  = 0.0002384711012816958;
-      r[69]  =   0.8987448413516816; s[69]  =   -0.9225381116915164; t[69]  =   -0.9881033648300827; w[69]  = 0.0002384711012816958;
-      r[70]  =   0.1272273908999288; s[70]  =   -0.8038931758108054; t[70]  =    -0.519441039278318; w[70]  =    0.0126767254277136;
-      r[71]  =   0.1272273908999288; s[71]  =   -0.8038931758108054; t[71]  =   -0.8038931758108054; w[71]  =    0.0126767254277136;
-      r[72]  =  -0.8038931758108054; s[72]  =   -0.8038931758108054; t[72]  =    0.1272273908999288; w[72]  =    0.0126767254277136;
-      r[73]  =   -0.519441039278318; s[73]  =    0.1272273908999288; t[73]  =   -0.8038931758108054; w[73]  =    0.0126767254277136;
-      r[74]  =  -0.8038931758108054; s[74]  =    -0.519441039278318; t[74]  =    0.1272273908999288; w[74]  =    0.0126767254277136;
-      r[75]  =  -0.8038931758108054; s[75]  =    0.1272273908999288; t[75]  =   -0.8038931758108054; w[75]  =    0.0126767254277136;
-      r[76]  =   -0.519441039278318; s[76]  =   -0.8038931758108054; t[76]  =    0.1272273908999288; w[76]  =    0.0126767254277136;
-      r[77]  =  -0.8038931758108054; s[77]  =    -0.519441039278318; t[77]  =   -0.8038931758108054; w[77]  =    0.0126767254277136;
-      r[78]  =  -0.8038931758108054; s[78]  =   -0.8038931758108054; t[78]  =    -0.519441039278318; w[78]  =    0.0126767254277136;
-      r[79]  =  -0.8038931758108054; s[79]  =    0.1272273908999288; t[79]  =    -0.519441039278318; w[79]  =    0.0126767254277136;
-      r[80]  =   -0.519441039278318; s[80]  =   -0.8038931758108054; t[80]  =   -0.8038931758108054; w[80]  =    0.0126767254277136;
-      r[81]  =   0.1272273908999288; s[81]  =    -0.519441039278318; t[81]  =   -0.8038931758108054; w[81]  =    0.0126767254277136;
-      r[82]  =    0.167041309150224; s[82]  =   -0.5900208986445075; t[82]  =   -0.9869995118612092; w[82]  =  0.003746993853374758;
-      r[83]  =    0.167041309150224; s[83]  =   -0.5900208986445075; t[83]  =   -0.5900208986445075; w[83]  =  0.003746993853374758;
-      r[84]  =  -0.5900208986445075; s[84]  =   -0.5900208986445075; t[84]  =     0.167041309150224; w[84]  =  0.003746993853374758;
-      r[85]  =  -0.9869995118612092; s[85]  =     0.167041309150224; t[85]  =   -0.5900208986445076; w[85]  =  0.003746993853374758;
-      r[86]  =  -0.5900208986445075; s[86]  =   -0.9869995118612092; t[86]  =    0.1670413091502241; w[86]  =  0.003746993853374758;
-      r[87]  =  -0.5900208986445075; s[87]  =     0.167041309150224; t[87]  =   -0.5900208986445075; w[87]  =  0.003746993853374758;
-      r[88]  =  -0.9869995118612092; s[88]  =   -0.5900208986445076; t[88]  =     0.167041309150224; w[88]  =  0.003746993853374758;
-      r[89]  =  -0.5900208986445075; s[89]  =   -0.9869995118612092; t[89]  =   -0.5900208986445075; w[89]  =  0.003746993853374758;
-      r[90]  =  -0.5900208986445075; s[90]  =   -0.5900208986445075; t[90]  =   -0.9869995118612092; w[90]  =  0.003746993853374758;
-      r[91]  =  -0.5900208986445075; s[91]  =    0.1670413091502241; t[91]  =   -0.9869995118612092; w[91]  =  0.003746993853374758;
-      r[92]  =  -0.9869995118612092; s[92]  =   -0.5900208986445075; t[92]  =   -0.5900208986445075; w[92]  =  0.003746993853374758;
-      r[93]  =    0.167041309150224; s[93]  =   -0.9869995118612092; t[93]  =   -0.5900208986445075; w[93]  =  0.003746993853374758;
-      r[94]  =   0.3769078559207375; s[94]  =   -0.9679000455085793; t[94]  =   -0.4411077649035788; w[94]  =  0.002647148326943714;
-      r[95]  =   0.3769078559207375; s[95]  =   -0.9679000455085793; t[95]  =   -0.9679000455085793; w[95]  =  0.002647148326943714;
-      r[96]  =  -0.9679000455085793; s[96]  =   -0.9679000455085793; t[96]  =    0.3769078559207375; w[96]  =  0.002647148326943714;
-      r[97]  =  -0.4411077649035788; s[97]  =    0.3769078559207375; t[97]  =   -0.9679000455085793; w[97]  =  0.002647148326943714;
-      r[98]  =  -0.9679000455085793; s[98]  =   -0.4411077649035788; t[98]  =    0.3769078559207375; w[98]  =  0.002647148326943714;
-      r[99]  =  -0.9679000455085793; s[99]  =    0.3769078559207375; t[99]  =   -0.9679000455085793; w[99]  =  0.002647148326943714;
-      r[100] =  -0.4411077649035788; s[100] =   -0.9679000455085793; t[100] =    0.3769078559207375; w[100] =  0.002647148326943714;
-      r[101] =  -0.9679000455085793; s[101] =   -0.4411077649035788; t[101] =   -0.9679000455085793; w[101] =  0.002647148326943714;
-      r[102] =  -0.9679000455085793; s[102] =   -0.9679000455085793; t[102] =   -0.4411077649035788; w[102] =  0.002647148326943714;
-      r[103] =  -0.9679000455085793; s[103] =    0.3769078559207375; t[103] =   -0.4411077649035788; w[103] =  0.002647148326943714;
-      r[104] =  -0.4411077649035788; s[104] =   -0.9679000455085793; t[104] =   -0.9679000455085793; w[104] =  0.002647148326943714;
-      r[105] =   0.3769078559207375; s[105] =   -0.4411077649035788; t[105] =   -0.9679000455085793; w[105] =  0.002647148326943714;
-      r[106] =  0.02049804457700402; s[106] =   -0.5571196390838979; t[106] =   -0.9062587664092081; w[106] =   0.01128950360189216;
-      r[107] =  0.02049804457700401; s[107] =   -0.5571196390838979; t[107] =   -0.5571196390838979; w[107] =   0.01128950360189216;
-      r[108] =  -0.5571196390838979; s[108] =   -0.5571196390838979; t[108] =   0.02049804457700399; w[108] =   0.01128950360189216;
-      r[109] =  -0.9062587664092081; s[109] =   0.02049804457700399; t[109] =   -0.5571196390838979; w[109] =   0.01128950360189216;
-      r[110] =  -0.5571196390838979; s[110] =    -0.906258766409208; t[110] =   0.02049804457700399; w[110] =   0.01128950360189216;
-      r[111] =  -0.5571196390838979; s[111] =   0.02049804457700399; t[111] =   -0.5571196390838979; w[111] =   0.01128950360189216;
-      r[112] =  -0.9062587664092081; s[112] =   -0.5571196390838979; t[112] =   0.02049804457700399; w[112] =   0.01128950360189216;
-      r[113] =  -0.5571196390838979; s[113] =    -0.906258766409208; t[113] =   -0.5571196390838979; w[113] =   0.01128950360189216;
-      r[114] =  -0.5571196390838979; s[114] =   -0.5571196390838979; t[114] =    -0.906258766409208; w[114] =   0.01128950360189216;
-      r[115] =  -0.5571196390838979; s[115] =   0.02049804457700399; t[115] =    -0.906258766409208; w[115] =   0.01128950360189216;
-      r[116] =   -0.906258766409208; s[116] =   -0.5571196390838979; t[116] =   -0.5571196390838979; w[116] =   0.01128950360189216;
-      r[117] =  0.02049804457700402; s[117] =   -0.9062587664092081; t[117] =   -0.5571196390838979; w[117] =   0.01128950360189216;
-      r[118] =  -0.2105599201328233; s[118] =   -0.5894853260438491; t[118] =   -0.4677734198382106; w[118] =  0.009255870808126791;
-      r[119] =  -0.5894853260438491; s[119] =   -0.4677734198382106; t[119] =   -0.2105599201328233; w[119] =  0.009255870808126791;
-      r[120] =  -0.5894853260438491; s[120] =   -0.2105599201328233; t[120] =   -0.4677734198382106; w[120] =  0.009255870808126791;
-      r[121] =  -0.4677734198382106; s[121] =   -0.2105599201328233; t[121] =   -0.7321813339851169; w[121] =  0.009255870808126791;
-      r[122] =  -0.4677734198382106; s[122] =   -0.2105599201328233; t[122] =   -0.5894853260438491; w[122] =  0.009255870808126791;
-      r[123] =  -0.7321813339851166; s[123] =   -0.2105599201328233; t[123] =   -0.4677734198382107; w[123] =  0.009255870808126791;
-      r[124] =  -0.4677734198382107; s[124] =   -0.5894853260438491; t[124] =   -0.7321813339851168; w[124] =  0.009255870808126791;
-      r[125] =  -0.4677734198382106; s[125] =   -0.7321813339851169; t[125] =   -0.2105599201328233; w[125] =  0.009255870808126791;
-      r[126] =  -0.7321813339851168; s[126] =   -0.5894853260438491; t[126] =   -0.4677734198382106; w[126] =  0.009255870808126791;
-      r[127] =  -0.2105599201328234; s[127] =   -0.5894853260438491; t[127] =   -0.7321813339851166; w[127] =  0.009255870808126791;
-      r[128] =  -0.7321813339851166; s[128] =   -0.2105599201328233; t[128] =   -0.5894853260438491; w[128] =  0.009255870808126791;
-      r[129] =  -0.4677734198382106; s[129] =   -0.5894853260438491; t[129] =   -0.2105599201328233; w[129] =  0.009255870808126791;
-      r[130] =  -0.7321813339851166; s[130] =   -0.5894853260438491; t[130] =   -0.2105599201328233; w[130] =  0.009255870808126791;
-      r[131] =  -0.2105599201328234; s[131] =   -0.7321813339851166; t[131] =   -0.4677734198382107; w[131] =  0.009255870808126791;
-      r[132] =  -0.4677734198382107; s[132] =   -0.7321813339851168; t[132] =   -0.5894853260438491; w[132] =  0.009255870808126791;
-      r[133] =  -0.5894853260438491; s[133] =   -0.7321813339851168; t[133] =   -0.4677734198382106; w[133] =  0.009255870808126791;
-      r[134] =  -0.2105599201328234; s[134] =   -0.7321813339851166; t[134] =   -0.5894853260438491; w[134] =  0.009255870808126791;
-      r[135] =  -0.5894853260438491; s[135] =   -0.7321813339851168; t[135] =   -0.2105599201328233; w[135] =  0.009255870808126791;
-      r[136] =  -0.5894853260438491; s[136] =   -0.2105599201328233; t[136] =   -0.7321813339851168; w[136] =  0.009255870808126791;
-      r[137] =  -0.7321813339851166; s[137] =   -0.4677734198382107; t[137] =   -0.2105599201328233; w[137] =  0.009255870808126791;
-      r[138] =  -0.2105599201328234; s[138] =   -0.4677734198382107; t[138] =   -0.7321813339851166; w[138] =  0.009255870808126791;
-      r[139] =  -0.2105599201328233; s[139] =   -0.4677734198382106; t[139] =   -0.5894853260438491; w[139] =  0.009255870808126791;
-      r[140] =  -0.5894853260438491; s[140] =   -0.4677734198382106; t[140] =   -0.7321813339851168; w[140] =  0.009255870808126791;
-      r[141] =  -0.7321813339851168; s[141] =   -0.4677734198382106; t[141] =   -0.5894853260438491; w[141] =  0.009255870808126791;
-      r[142] =   0.4187537170452442; s[142] =   -0.8257019301996555; t[142] =   -0.6417530716753372; w[142] =  0.005856256384098688;
-      r[143] =  -0.8257019301996555; s[143] =   -0.6417530716753372; t[143] =    0.4187537170452442; w[143] =  0.005856256384098688;
-      r[144] =  -0.8257019301996555; s[144] =    0.4187537170452442; t[144] =   -0.6417530716753372; w[144] =  0.005856256384098688;
-      r[145] =  -0.6417530716753372; s[145] =    0.4187537170452442; t[145] =   -0.9512987151702514; w[145] =  0.005856256384098688;
-      r[146] =  -0.6417530716753372; s[146] =    0.4187537170452442; t[146] =   -0.8257019301996555; w[146] =  0.005856256384098688;
-      r[147] =  -0.9512987151702514; s[147] =    0.4187537170452442; t[147] =   -0.6417530716753372; w[147] =  0.005856256384098688;
-      r[148] =  -0.6417530716753372; s[148] =   -0.8257019301996555; t[148] =   -0.9512987151702514; w[148] =  0.005856256384098688;
-      r[149] =  -0.6417530716753372; s[149] =   -0.9512987151702514; t[149] =    0.4187537170452442; w[149] =  0.005856256384098688;
-      r[150] =  -0.9512987151702514; s[150] =   -0.8257019301996555; t[150] =   -0.6417530716753372; w[150] =  0.005856256384098688;
-      r[151] =   0.4187537170452442; s[151] =   -0.8257019301996555; t[151] =   -0.9512987151702514; w[151] =  0.005856256384098688;
-      r[152] =  -0.9512987151702514; s[152] =    0.4187537170452442; t[152] =   -0.8257019301996555; w[152] =  0.005856256384098688;
-      r[153] =  -0.6417530716753372; s[153] =   -0.8257019301996555; t[153] =    0.4187537170452442; w[153] =  0.005856256384098688;
-      r[154] =  -0.9512987151702514; s[154] =   -0.8257019301996555; t[154] =    0.4187537170452442; w[154] =  0.005856256384098688;
-      r[155] =   0.4187537170452442; s[155] =   -0.9512987151702514; t[155] =   -0.6417530716753372; w[155] =  0.005856256384098688;
-      r[156] =  -0.6417530716753372; s[156] =   -0.9512987151702514; t[156] =   -0.8257019301996555; w[156] =  0.005856256384098688;
-      r[157] =  -0.8257019301996555; s[157] =   -0.9512987151702514; t[157] =   -0.6417530716753372; w[157] =  0.005856256384098688;
-      r[158] =   0.4187537170452442; s[158] =   -0.9512987151702514; t[158] =   -0.8257019301996555; w[158] =  0.005856256384098688;
-      r[159] =  -0.8257019301996555; s[159] =   -0.9512987151702514; t[159] =    0.4187537170452442; w[159] =  0.005856256384098688;
-      r[160] =  -0.8257019301996555; s[160] =    0.4187537170452442; t[160] =   -0.9512987151702514; w[160] =  0.005856256384098688;
-      r[161] =  -0.9512987151702514; s[161] =   -0.6417530716753372; t[161] =    0.4187537170452442; w[161] =  0.005856256384098688;
-      r[162] =   0.4187537170452442; s[162] =   -0.6417530716753372; t[162] =   -0.9512987151702514; w[162] =  0.005856256384098688;
-      r[163] =   0.4187537170452442; s[163] =   -0.6417530716753372; t[163] =   -0.8257019301996555; w[163] =  0.005856256384098688;
-      r[164] =  -0.8257019301996555; s[164] =   -0.6417530716753372; t[164] =   -0.9512987151702514; w[164] =  0.005856256384098688;
-      r[165] =  -0.9512987151702514; s[165] =   -0.6417530716753372; t[165] =   -0.8257019301996555; w[165] =  0.005856256384098688;
-      r[166] =   0.6760206216666895; s[166] =   -0.9243451288222915; t[166] =     -0.75826562740743; w[166] =  0.001287935899077956;
-      r[167] =  -0.9243451288222915; s[167] =     -0.75826562740743; t[167] =    0.6760206216666895; w[167] =  0.001287935899077956;
-      r[168] =  -0.9243451288222915; s[168] =    0.6760206216666895; t[168] =     -0.75826562740743; w[168] =  0.001287935899077956;
-      r[169] =    -0.75826562740743; s[169] =    0.6760206216666895; t[169] =   -0.9934098654369681; w[169] =  0.001287935899077956;
-      r[170] =    -0.75826562740743; s[170] =    0.6760206216666895; t[170] =   -0.9243451288222915; w[170] =  0.001287935899077956;
-      r[171] =  -0.9934098654369681; s[171] =    0.6760206216666895; t[171] =     -0.75826562740743; w[171] =  0.001287935899077956;
-      r[172] =    -0.75826562740743; s[172] =   -0.9243451288222915; t[172] =    -0.993409865436968; w[172] =  0.001287935899077956;
-      r[173] =    -0.75826562740743; s[173] =   -0.9934098654369681; t[173] =    0.6760206216666895; w[173] =  0.001287935899077956;
-      r[174] =   -0.993409865436968; s[174] =   -0.9243451288222915; t[174] =     -0.75826562740743; w[174] =  0.001287935899077956;
-      r[175] =   0.6760206216666895; s[175] =   -0.9243451288222916; t[175] =    -0.993409865436968; w[175] =  0.001287935899077956;
-      r[176] =  -0.9934098654369681; s[176] =    0.6760206216666895; t[176] =   -0.9243451288222915; w[176] =  0.001287935899077956;
-      r[177] =    -0.75826562740743; s[177] =   -0.9243451288222915; t[177] =    0.6760206216666895; w[177] =  0.001287935899077956;
-      r[178] =  -0.9934098654369681; s[178] =   -0.9243451288222915; t[178] =    0.6760206216666895; w[178] =  0.001287935899077956;
-      r[179] =   0.6760206216666895; s[179] =   -0.9934098654369681; t[179] =     -0.75826562740743; w[179] =  0.001287935899077956;
-      r[180] =    -0.75826562740743; s[180] =    -0.993409865436968; t[180] =   -0.9243451288222915; w[180] =  0.001287935899077956;
-      r[181] =  -0.9243451288222915; s[181] =    -0.993409865436968; t[181] =     -0.75826562740743; w[181] =  0.001287935899077956;
-      r[182] =   0.6760206216666895; s[182] =    -0.993409865436968; t[182] =   -0.9243451288222916; w[182] =  0.001287935899077956;
-      r[183] =  -0.9243451288222915; s[183] =   -0.9934098654369681; t[183] =    0.6760206216666895; w[183] =  0.001287935899077956;
-      r[184] =  -0.9243451288222915; s[184] =    0.6760206216666895; t[184] =   -0.9934098654369681; w[184] =  0.001287935899077956;
-      r[185] =  -0.9934098654369681; s[185] =     -0.75826562740743; t[185] =    0.6760206216666895; w[185] =  0.001287935899077956;
-      r[186] =   0.6760206216666895; s[186] =     -0.75826562740743; t[186] =   -0.9934098654369681; w[186] =  0.001287935899077956;
-      r[187] =   0.6760206216666895; s[187] =     -0.75826562740743; t[187] =   -0.9243451288222915; w[187] =  0.001287935899077956;
-      r[188] =  -0.9243451288222915; s[188] =     -0.75826562740743; t[188] =    -0.993409865436968; w[188] =  0.001287935899077956;
-      r[189] =   -0.993409865436968; s[189] =     -0.75826562740743; t[189] =   -0.9243451288222915; w[189] =  0.001287935899077956;
-      r[190] =   0.0969456158451746; s[190] =   -0.3090604280187177; t[190] =   -0.8233513951196885; w[190] =    0.0069912420734512;
-      r[191] =  -0.3090604280187177; s[191] =   -0.8233513951196885; t[191] =    0.0969456158451746; w[191] =    0.0069912420734512;
-      r[192] =  -0.3090604280187177; s[192] =    0.0969456158451746; t[192] =   -0.8233513951196885; w[192] =    0.0069912420734512;
-      r[193] =  -0.8233513951196885; s[193] =   0.09694561584517464; t[193] =   -0.9645337927067685; w[193] =    0.0069912420734512;
-      r[194] =  -0.8233513951196886; s[194] =   0.09694561584517458; t[194] =   -0.3090604280187177; w[194] =    0.0069912420734512;
-      r[195] =  -0.9645337927067685; s[195] =   0.09694561584517458; t[195] =   -0.8233513951196886; w[195] =    0.0069912420734512;
-      r[196] =  -0.8233513951196886; s[196] =   -0.3090604280187177; t[196] =   -0.9645337927067685; w[196] =    0.0069912420734512;
-      r[197] =  -0.8233513951196885; s[197] =   -0.9645337927067685; t[197] =   0.09694561584517464; w[197] =    0.0069912420734512;
-      r[198] =  -0.9645337927067685; s[198] =   -0.3090604280187177; t[198] =   -0.8233513951196886; w[198] =    0.0069912420734512;
-      r[199] =  0.09694561584517457; s[199] =   -0.3090604280187177; t[199] =   -0.9645337927067685; w[199] =    0.0069912420734512;
-      r[200] =  -0.9645337927067686; s[200] =    0.0969456158451746; t[200] =   -0.3090604280187177; w[200] =    0.0069912420734512;
-      r[201] =  -0.8233513951196886; s[201] =   -0.3090604280187177; t[201] =   0.09694561584517458; w[201] =    0.0069912420734512;
-      r[202] =  -0.9645337927067686; s[202] =   -0.3090604280187177; t[202] =    0.0969456158451746; w[202] =    0.0069912420734512;
-      r[203] =  0.09694561584517458; s[203] =   -0.9645337927067685; t[203] =   -0.8233513951196885; w[203] =    0.0069912420734512;
-      r[204] =  -0.8233513951196886; s[204] =   -0.9645337927067685; t[204] =   -0.3090604280187177; w[204] =    0.0069912420734512;
-      r[205] =  -0.3090604280187177; s[205] =   -0.9645337927067685; t[205] =   -0.8233513951196886; w[205] =    0.0069912420734512;
-      r[206] =  0.09694561584517457; s[206] =   -0.9645337927067685; t[206] =   -0.3090604280187177; w[206] =    0.0069912420734512;
-      r[207] =  -0.3090604280187176; s[207] =   -0.9645337927067686; t[207] =   0.09694561584517462; w[207] =    0.0069912420734512;
-      r[208] =  -0.3090604280187176; s[208] =   0.09694561584517462; t[208] =   -0.9645337927067686; w[208] =    0.0069912420734512;
-      r[209] =  -0.9645337927067685; s[209] =   -0.8233513951196886; t[209] =   0.09694561584517458; w[209] =    0.0069912420734512;
-      r[210] =  0.09694561584517458; s[210] =   -0.8233513951196885; t[210] =   -0.9645337927067685; w[210] =    0.0069912420734512;
-      r[211] =   0.0969456158451746; s[211] =   -0.8233513951196885; t[211] =   -0.3090604280187177; w[211] =    0.0069912420734512;
-      r[212] =  -0.3090604280187177; s[212] =   -0.8233513951196886; t[212] =   -0.9645337927067685; w[212] =    0.0069912420734512;
-      r[213] =  -0.9645337927067685; s[213] =   -0.8233513951196886; t[213] =   -0.3090604280187177; w[213] =    0.0069912420734512;
+      r[0] = -0.9153144959134277;
+      s[0] = -0.9153144959134277;
+      t[0] = 0.745943487740283;
+      w[0] = 0.003176684382984782;
+      r[1] = -0.9153144959134277;
+      s[1] = 0.745943487740283;
+      t[1] = -0.9153144959134277;
+      w[1] = 0.003176684382984782;
+      r[2] = 0.7459434877402831;
+      s[2] = -0.9153144959134277;
+      t[2] = -0.9153144959134277;
+      w[2] = 0.003176684382984782;
+      r[3] = -0.9153144959134277;
+      s[3] = -0.9153144959134277;
+      t[3] = -0.9153144959134277;
+      w[3] = 0.003176684382984782;
+      r[4] = -0.7292035608164203;
+      s[4] = -0.7292035608164203;
+      t[4] = 0.1876106824492612;
+      w[4] = 0.008958793406037778;
+      r[5] = -0.7292035608164203;
+      s[5] = 0.1876106824492612;
+      t[5] = -0.7292035608164203;
+      w[5] = 0.008958793406037778;
+      r[6] = 0.1876106824492612;
+      s[6] = -0.7292035608164203;
+      t[6] = -0.7292035608164203;
+      w[6] = 0.008958793406037778;
+      r[7] = -0.7292035608164203;
+      s[7] = -0.7292035608164203;
+      t[7] = -0.7292035608164203;
+      w[7] = 0.008958793406037778;
+      r[8] = -0.3709271370554474;
+      s[8] = -0.3709271370554474;
+      t[8] = -0.8872185888336577;
+      w[8] = 0.01117598049100474;
+      r[9] = -0.3709271370554474;
+      s[9] = -0.8872185888336577;
+      t[9] = -0.3709271370554474;
+      w[9] = 0.01117598049100474;
+      r[10] = -0.8872185888336577;
+      s[10] = -0.3709271370554474;
+      t[10] = -0.3709271370554474;
+      w[10] = 0.01117598049100474;
+      r[11] = -0.3709271370554474;
+      s[11] = -0.3709271370554474;
+      t[11] = -0.3709271370554474;
+      w[11] = 0.01117598049100474;
+      r[12] = -0.8344757841485797;
+      s[12] = -0.8344757841485797;
+      t[12] = 0.5034273524457391;
+      w[12] = 0.006677534058303564;
+      r[13] = -0.8344757841485797;
+      s[13] = 0.5034273524457391;
+      t[13] = -0.8344757841485797;
+      w[13] = 0.006677534058303564;
+      r[14] = 0.5034273524457391;
+      s[14] = -0.8344757841485797;
+      t[14] = -0.8344757841485797;
+      w[14] = 0.006677534058303564;
+      r[15] = -0.8344757841485797;
+      s[15] = -0.8344757841485797;
+      t[15] = -0.8344757841485797;
+      w[15] = 0.006677534058303564;
+      r[16] = -0.1663704866153568;
+      s[16] = -0.8336295133846432;
+      t[16] = -0.8336295133846432;
+      w[16] = 0.008908689779326269;
+      r[17] = -0.8336295133846432;
+      s[17] = -0.1663704866153568;
+      t[17] = -0.8336295133846432;
+      w[17] = 0.008908689779326269;
+      r[18] = -0.1663704866153568;
+      s[18] = -0.1663704866153568;
+      t[18] = -0.8336295133846432;
+      w[18] = 0.008908689779326269;
+      r[19] = -0.1663704866153568;
+      s[19] = -0.8336295133846432;
+      t[19] = -0.1663704866153568;
+      w[19] = 0.008908689779326269;
+      r[20] = -0.8336295133846432;
+      s[20] = -0.1663704866153568;
+      t[20] = -0.1663704866153568;
+      w[20] = 0.008908689779326269;
+      r[21] = -0.8336295133846432;
+      s[21] = -0.8336295133846432;
+      t[21] = -0.1663704866153568;
+      w[21] = 0.008908689779326269;
+      r[22] = -0.03464142965362016;
+      s[22] = -0.9653585703463798;
+      t[22] = -0.9653585703463798;
+      w[22] = 0.00328555582848326;
+      r[23] = -0.9653585703463798;
+      s[23] = -0.03464142965362016;
+      t[23] = -0.9653585703463798;
+      w[23] = 0.00328555582848326;
+      r[24] = -0.03464142965362016;
+      s[24] = -0.03464142965362016;
+      t[24] = -0.9653585703463798;
+      w[24] = 0.00328555582848326;
+      r[25] = -0.03464142965362016;
+      s[25] = -0.9653585703463798;
+      t[25] = -0.03464142965362016;
+      w[25] = 0.00328555582848326;
+      r[26] = -0.9653585703463798;
+      s[26] = -0.03464142965362016;
+      t[26] = -0.03464142965362016;
+      w[26] = 0.00328555582848326;
+      r[27] = -0.9653585703463798;
+      s[27] = -0.9653585703463798;
+      t[27] = -0.03464142965362016;
+      w[27] = 0.00328555582848326;
+      r[28] = -0.4789374311664119;
+      s[28] = -0.5210625688335881;
+      t[28] = -0.5210625688335881;
+      w[28] = 0.003034768187464438;
+      r[29] = -0.5210625688335881;
+      s[29] = -0.4789374311664119;
+      t[29] = -0.5210625688335881;
+      w[29] = 0.003034768187464438;
+      r[30] = -0.4789374311664119;
+      s[30] = -0.4789374311664119;
+      t[30] = -0.5210625688335881;
+      w[30] = 0.003034768187464438;
+      r[31] = -0.4789374311664119;
+      s[31] = -0.5210625688335881;
+      t[31] = -0.4789374311664119;
+      w[31] = 0.003034768187464438;
+      r[32] = -0.5210625688335881;
+      s[32] = -0.4789374311664119;
+      t[32] = -0.4789374311664119;
+      w[32] = 0.003034768187464438;
+      r[33] = -0.5210625688335881;
+      s[33] = -0.5210625688335881;
+      t[33] = -0.4789374311664119;
+      w[33] = 0.003034768187464438;
+      r[34] = -0.6648466287055623;
+      s[34] = -0.234103305514385;
+      t[34] = -0.8669467602656677;
+      w[34] = 0.009394571537633017;
+      r[35] = -0.6648466287055623;
+      s[35] = -0.234103305514385;
+      t[35] = -0.234103305514385;
+      w[35] = 0.009394571537633017;
+      r[36] = -0.234103305514385;
+      s[36] = -0.234103305514385;
+      t[36] = -0.6648466287055623;
+      w[36] = 0.009394571537633017;
+      r[37] = -0.8669467602656677;
+      s[37] = -0.6648466287055623;
+      t[37] = -0.234103305514385;
+      w[37] = 0.009394571537633017;
+      r[38] = -0.234103305514385;
+      s[38] = -0.8669467602656677;
+      t[38] = -0.6648466287055623;
+      w[38] = 0.009394571537633017;
+      r[39] = -0.234103305514385;
+      s[39] = -0.6648466287055623;
+      t[39] = -0.234103305514385;
+      w[39] = 0.009394571537633017;
+      r[40] = -0.8669467602656677;
+      s[40] = -0.234103305514385;
+      t[40] = -0.6648466287055623;
+      w[40] = 0.009394571537633017;
+      r[41] = -0.234103305514385;
+      s[41] = -0.8669467602656677;
+      t[41] = -0.234103305514385;
+      w[41] = 0.009394571537633017;
+      r[42] = -0.234103305514385;
+      s[42] = -0.234103305514385;
+      t[42] = -0.8669467602656677;
+      w[42] = 0.009394571537633017;
+      r[43] = -0.234103305514385;
+      s[43] = -0.6648466287055623;
+      t[43] = -0.8669467602656677;
+      w[43] = 0.009394571537633017;
+      r[44] = -0.8669467602656677;
+      s[44] = -0.234103305514385;
+      t[44] = -0.234103305514385;
+      w[44] = 0.009394571537633017;
+      r[45] = -0.6648466287055623;
+      s[45] = -0.8669467602656677;
+      t[45] = -0.234103305514385;
+      w[45] = 0.009394571537633017;
+      r[46] = -0.5658650959714019;
+      s[46] = -0.2277398552115068;
+      t[46] = -0.9786551936055847;
+      w[46] = 0.006724249255682279;
+      r[47] = -0.5658650959714018;
+      s[47] = -0.2277398552115067;
+      t[47] = -0.2277398552115067;
+      w[47] = 0.006724249255682279;
+      r[48] = -0.2277398552115067;
+      s[48] = -0.2277398552115067;
+      t[48] = -0.5658650959714018;
+      w[48] = 0.006724249255682279;
+      r[49] = -0.9786551936055847;
+      s[49] = -0.5658650959714018;
+      t[49] = -0.2277398552115067;
+      w[49] = 0.006724249255682279;
+      r[50] = -0.2277398552115067;
+      s[50] = -0.9786551936055847;
+      t[50] = -0.5658650959714018;
+      w[50] = 0.006724249255682279;
+      r[51] = -0.2277398552115067;
+      s[51] = -0.5658650959714018;
+      t[51] = -0.2277398552115067;
+      w[51] = 0.006724249255682279;
+      r[52] = -0.9786551936055847;
+      s[52] = -0.2277398552115067;
+      t[52] = -0.5658650959714018;
+      w[52] = 0.006724249255682279;
+      r[53] = -0.2277398552115068;
+      s[53] = -0.9786551936055846;
+      t[53] = -0.2277398552115068;
+      w[53] = 0.006724249255682279;
+      r[54] = -0.2277398552115068;
+      s[54] = -0.2277398552115068;
+      t[54] = -0.9786551936055846;
+      w[54] = 0.006724249255682279;
+      r[55] = -0.2277398552115067;
+      s[55] = -0.5658650959714018;
+      t[55] = -0.9786551936055847;
+      w[55] = 0.006724249255682279;
+      r[56] = -0.9786551936055847;
+      s[56] = -0.2277398552115067;
+      t[56] = -0.2277398552115067;
+      w[56] = 0.006724249255682279;
+      r[57] = -0.5658650959714019;
+      s[57] = -0.9786551936055847;
+      t[57] = -0.2277398552115068;
+      w[57] = 0.006724249255682279;
+      r[58] = 0.8987448413516816;
+      s[58] = -0.9881033648300827;
+      t[58] = -0.9225381116915164;
+      w[58] = 0.0002384711012816958;
+      r[59] = 0.8987448413516816;
+      s[59] = -0.9881033648300825;
+      t[59] = -0.9881033648300825;
+      w[59] = 0.0002384711012816958;
+      r[60] = -0.9881033648300825;
+      s[60] = -0.9881033648300825;
+      t[60] = 0.8987448413516816;
+      w[60] = 0.0002384711012816958;
+      r[61] = -0.9225381116915166;
+      s[61] = 0.8987448413516816;
+      t[61] = -0.9881033648300825;
+      w[61] = 0.0002384711012816958;
+      r[62] = -0.9881033648300825;
+      s[62] = -0.9225381116915166;
+      t[62] = 0.8987448413516816;
+      w[62] = 0.0002384711012816958;
+      r[63] = -0.9881033648300825;
+      s[63] = 0.8987448413516816;
+      t[63] = -0.9881033648300825;
+      w[63] = 0.0002384711012816958;
+      r[64] = -0.9225381116915166;
+      s[64] = -0.9881033648300825;
+      t[64] = 0.8987448413516816;
+      w[64] = 0.0002384711012816958;
+      r[65] = -0.9881033648300825;
+      s[65] = -0.9225381116915164;
+      t[65] = -0.9881033648300825;
+      w[65] = 0.0002384711012816958;
+      r[66] = -0.9881033648300825;
+      s[66] = -0.9881033648300825;
+      t[66] = -0.9225381116915164;
+      w[66] = 0.0002384711012816958;
+      r[67] = -0.9881033648300825;
+      s[67] = 0.8987448413516816;
+      t[67] = -0.9225381116915166;
+      w[67] = 0.0002384711012816958;
+      r[68] = -0.9225381116915164;
+      s[68] = -0.9881033648300825;
+      t[68] = -0.9881033648300825;
+      w[68] = 0.0002384711012816958;
+      r[69] = 0.8987448413516816;
+      s[69] = -0.9225381116915164;
+      t[69] = -0.9881033648300827;
+      w[69] = 0.0002384711012816958;
+      r[70] = 0.1272273908999288;
+      s[70] = -0.8038931758108054;
+      t[70] = -0.519441039278318;
+      w[70] = 0.0126767254277136;
+      r[71] = 0.1272273908999288;
+      s[71] = -0.8038931758108054;
+      t[71] = -0.8038931758108054;
+      w[71] = 0.0126767254277136;
+      r[72] = -0.8038931758108054;
+      s[72] = -0.8038931758108054;
+      t[72] = 0.1272273908999288;
+      w[72] = 0.0126767254277136;
+      r[73] = -0.519441039278318;
+      s[73] = 0.1272273908999288;
+      t[73] = -0.8038931758108054;
+      w[73] = 0.0126767254277136;
+      r[74] = -0.8038931758108054;
+      s[74] = -0.519441039278318;
+      t[74] = 0.1272273908999288;
+      w[74] = 0.0126767254277136;
+      r[75] = -0.8038931758108054;
+      s[75] = 0.1272273908999288;
+      t[75] = -0.8038931758108054;
+      w[75] = 0.0126767254277136;
+      r[76] = -0.519441039278318;
+      s[76] = -0.8038931758108054;
+      t[76] = 0.1272273908999288;
+      w[76] = 0.0126767254277136;
+      r[77] = -0.8038931758108054;
+      s[77] = -0.519441039278318;
+      t[77] = -0.8038931758108054;
+      w[77] = 0.0126767254277136;
+      r[78] = -0.8038931758108054;
+      s[78] = -0.8038931758108054;
+      t[78] = -0.519441039278318;
+      w[78] = 0.0126767254277136;
+      r[79] = -0.8038931758108054;
+      s[79] = 0.1272273908999288;
+      t[79] = -0.519441039278318;
+      w[79] = 0.0126767254277136;
+      r[80] = -0.519441039278318;
+      s[80] = -0.8038931758108054;
+      t[80] = -0.8038931758108054;
+      w[80] = 0.0126767254277136;
+      r[81] = 0.1272273908999288;
+      s[81] = -0.519441039278318;
+      t[81] = -0.8038931758108054;
+      w[81] = 0.0126767254277136;
+      r[82] = 0.167041309150224;
+      s[82] = -0.5900208986445075;
+      t[82] = -0.9869995118612092;
+      w[82] = 0.003746993853374758;
+      r[83] = 0.167041309150224;
+      s[83] = -0.5900208986445075;
+      t[83] = -0.5900208986445075;
+      w[83] = 0.003746993853374758;
+      r[84] = -0.5900208986445075;
+      s[84] = -0.5900208986445075;
+      t[84] = 0.167041309150224;
+      w[84] = 0.003746993853374758;
+      r[85] = -0.9869995118612092;
+      s[85] = 0.167041309150224;
+      t[85] = -0.5900208986445076;
+      w[85] = 0.003746993853374758;
+      r[86] = -0.5900208986445075;
+      s[86] = -0.9869995118612092;
+      t[86] = 0.1670413091502241;
+      w[86] = 0.003746993853374758;
+      r[87] = -0.5900208986445075;
+      s[87] = 0.167041309150224;
+      t[87] = -0.5900208986445075;
+      w[87] = 0.003746993853374758;
+      r[88] = -0.9869995118612092;
+      s[88] = -0.5900208986445076;
+      t[88] = 0.167041309150224;
+      w[88] = 0.003746993853374758;
+      r[89] = -0.5900208986445075;
+      s[89] = -0.9869995118612092;
+      t[89] = -0.5900208986445075;
+      w[89] = 0.003746993853374758;
+      r[90] = -0.5900208986445075;
+      s[90] = -0.5900208986445075;
+      t[90] = -0.9869995118612092;
+      w[90] = 0.003746993853374758;
+      r[91] = -0.5900208986445075;
+      s[91] = 0.1670413091502241;
+      t[91] = -0.9869995118612092;
+      w[91] = 0.003746993853374758;
+      r[92] = -0.9869995118612092;
+      s[92] = -0.5900208986445075;
+      t[92] = -0.5900208986445075;
+      w[92] = 0.003746993853374758;
+      r[93] = 0.167041309150224;
+      s[93] = -0.9869995118612092;
+      t[93] = -0.5900208986445075;
+      w[93] = 0.003746993853374758;
+      r[94] = 0.3769078559207375;
+      s[94] = -0.9679000455085793;
+      t[94] = -0.4411077649035788;
+      w[94] = 0.002647148326943714;
+      r[95] = 0.3769078559207375;
+      s[95] = -0.9679000455085793;
+      t[95] = -0.9679000455085793;
+      w[95] = 0.002647148326943714;
+      r[96] = -0.9679000455085793;
+      s[96] = -0.9679000455085793;
+      t[96] = 0.3769078559207375;
+      w[96] = 0.002647148326943714;
+      r[97] = -0.4411077649035788;
+      s[97] = 0.3769078559207375;
+      t[97] = -0.9679000455085793;
+      w[97] = 0.002647148326943714;
+      r[98] = -0.9679000455085793;
+      s[98] = -0.4411077649035788;
+      t[98] = 0.3769078559207375;
+      w[98] = 0.002647148326943714;
+      r[99] = -0.9679000455085793;
+      s[99] = 0.3769078559207375;
+      t[99] = -0.9679000455085793;
+      w[99] = 0.002647148326943714;
+      r[100] = -0.4411077649035788;
+      s[100] = -0.9679000455085793;
+      t[100] = 0.3769078559207375;
+      w[100] = 0.002647148326943714;
+      r[101] = -0.9679000455085793;
+      s[101] = -0.4411077649035788;
+      t[101] = -0.9679000455085793;
+      w[101] = 0.002647148326943714;
+      r[102] = -0.9679000455085793;
+      s[102] = -0.9679000455085793;
+      t[102] = -0.4411077649035788;
+      w[102] = 0.002647148326943714;
+      r[103] = -0.9679000455085793;
+      s[103] = 0.3769078559207375;
+      t[103] = -0.4411077649035788;
+      w[103] = 0.002647148326943714;
+      r[104] = -0.4411077649035788;
+      s[104] = -0.9679000455085793;
+      t[104] = -0.9679000455085793;
+      w[104] = 0.002647148326943714;
+      r[105] = 0.3769078559207375;
+      s[105] = -0.4411077649035788;
+      t[105] = -0.9679000455085793;
+      w[105] = 0.002647148326943714;
+      r[106] = 0.02049804457700402;
+      s[106] = -0.5571196390838979;
+      t[106] = -0.9062587664092081;
+      w[106] = 0.01128950360189216;
+      r[107] = 0.02049804457700401;
+      s[107] = -0.5571196390838979;
+      t[107] = -0.5571196390838979;
+      w[107] = 0.01128950360189216;
+      r[108] = -0.5571196390838979;
+      s[108] = -0.5571196390838979;
+      t[108] = 0.02049804457700399;
+      w[108] = 0.01128950360189216;
+      r[109] = -0.9062587664092081;
+      s[109] = 0.02049804457700399;
+      t[109] = -0.5571196390838979;
+      w[109] = 0.01128950360189216;
+      r[110] = -0.5571196390838979;
+      s[110] = -0.906258766409208;
+      t[110] = 0.02049804457700399;
+      w[110] = 0.01128950360189216;
+      r[111] = -0.5571196390838979;
+      s[111] = 0.02049804457700399;
+      t[111] = -0.5571196390838979;
+      w[111] = 0.01128950360189216;
+      r[112] = -0.9062587664092081;
+      s[112] = -0.5571196390838979;
+      t[112] = 0.02049804457700399;
+      w[112] = 0.01128950360189216;
+      r[113] = -0.5571196390838979;
+      s[113] = -0.906258766409208;
+      t[113] = -0.5571196390838979;
+      w[113] = 0.01128950360189216;
+      r[114] = -0.5571196390838979;
+      s[114] = -0.5571196390838979;
+      t[114] = -0.906258766409208;
+      w[114] = 0.01128950360189216;
+      r[115] = -0.5571196390838979;
+      s[115] = 0.02049804457700399;
+      t[115] = -0.906258766409208;
+      w[115] = 0.01128950360189216;
+      r[116] = -0.906258766409208;
+      s[116] = -0.5571196390838979;
+      t[116] = -0.5571196390838979;
+      w[116] = 0.01128950360189216;
+      r[117] = 0.02049804457700402;
+      s[117] = -0.9062587664092081;
+      t[117] = -0.5571196390838979;
+      w[117] = 0.01128950360189216;
+      r[118] = -0.2105599201328233;
+      s[118] = -0.5894853260438491;
+      t[118] = -0.4677734198382106;
+      w[118] = 0.009255870808126791;
+      r[119] = -0.5894853260438491;
+      s[119] = -0.4677734198382106;
+      t[119] = -0.2105599201328233;
+      w[119] = 0.009255870808126791;
+      r[120] = -0.5894853260438491;
+      s[120] = -0.2105599201328233;
+      t[120] = -0.4677734198382106;
+      w[120] = 0.009255870808126791;
+      r[121] = -0.4677734198382106;
+      s[121] = -0.2105599201328233;
+      t[121] = -0.7321813339851169;
+      w[121] = 0.009255870808126791;
+      r[122] = -0.4677734198382106;
+      s[122] = -0.2105599201328233;
+      t[122] = -0.5894853260438491;
+      w[122] = 0.009255870808126791;
+      r[123] = -0.7321813339851166;
+      s[123] = -0.2105599201328233;
+      t[123] = -0.4677734198382107;
+      w[123] = 0.009255870808126791;
+      r[124] = -0.4677734198382107;
+      s[124] = -0.5894853260438491;
+      t[124] = -0.7321813339851168;
+      w[124] = 0.009255870808126791;
+      r[125] = -0.4677734198382106;
+      s[125] = -0.7321813339851169;
+      t[125] = -0.2105599201328233;
+      w[125] = 0.009255870808126791;
+      r[126] = -0.7321813339851168;
+      s[126] = -0.5894853260438491;
+      t[126] = -0.4677734198382106;
+      w[126] = 0.009255870808126791;
+      r[127] = -0.2105599201328234;
+      s[127] = -0.5894853260438491;
+      t[127] = -0.7321813339851166;
+      w[127] = 0.009255870808126791;
+      r[128] = -0.7321813339851166;
+      s[128] = -0.2105599201328233;
+      t[128] = -0.5894853260438491;
+      w[128] = 0.009255870808126791;
+      r[129] = -0.4677734198382106;
+      s[129] = -0.5894853260438491;
+      t[129] = -0.2105599201328233;
+      w[129] = 0.009255870808126791;
+      r[130] = -0.7321813339851166;
+      s[130] = -0.5894853260438491;
+      t[130] = -0.2105599201328233;
+      w[130] = 0.009255870808126791;
+      r[131] = -0.2105599201328234;
+      s[131] = -0.7321813339851166;
+      t[131] = -0.4677734198382107;
+      w[131] = 0.009255870808126791;
+      r[132] = -0.4677734198382107;
+      s[132] = -0.7321813339851168;
+      t[132] = -0.5894853260438491;
+      w[132] = 0.009255870808126791;
+      r[133] = -0.5894853260438491;
+      s[133] = -0.7321813339851168;
+      t[133] = -0.4677734198382106;
+      w[133] = 0.009255870808126791;
+      r[134] = -0.2105599201328234;
+      s[134] = -0.7321813339851166;
+      t[134] = -0.5894853260438491;
+      w[134] = 0.009255870808126791;
+      r[135] = -0.5894853260438491;
+      s[135] = -0.7321813339851168;
+      t[135] = -0.2105599201328233;
+      w[135] = 0.009255870808126791;
+      r[136] = -0.5894853260438491;
+      s[136] = -0.2105599201328233;
+      t[136] = -0.7321813339851168;
+      w[136] = 0.009255870808126791;
+      r[137] = -0.7321813339851166;
+      s[137] = -0.4677734198382107;
+      t[137] = -0.2105599201328233;
+      w[137] = 0.009255870808126791;
+      r[138] = -0.2105599201328234;
+      s[138] = -0.4677734198382107;
+      t[138] = -0.7321813339851166;
+      w[138] = 0.009255870808126791;
+      r[139] = -0.2105599201328233;
+      s[139] = -0.4677734198382106;
+      t[139] = -0.5894853260438491;
+      w[139] = 0.009255870808126791;
+      r[140] = -0.5894853260438491;
+      s[140] = -0.4677734198382106;
+      t[140] = -0.7321813339851168;
+      w[140] = 0.009255870808126791;
+      r[141] = -0.7321813339851168;
+      s[141] = -0.4677734198382106;
+      t[141] = -0.5894853260438491;
+      w[141] = 0.009255870808126791;
+      r[142] = 0.4187537170452442;
+      s[142] = -0.8257019301996555;
+      t[142] = -0.6417530716753372;
+      w[142] = 0.005856256384098688;
+      r[143] = -0.8257019301996555;
+      s[143] = -0.6417530716753372;
+      t[143] = 0.4187537170452442;
+      w[143] = 0.005856256384098688;
+      r[144] = -0.8257019301996555;
+      s[144] = 0.4187537170452442;
+      t[144] = -0.6417530716753372;
+      w[144] = 0.005856256384098688;
+      r[145] = -0.6417530716753372;
+      s[145] = 0.4187537170452442;
+      t[145] = -0.9512987151702514;
+      w[145] = 0.005856256384098688;
+      r[146] = -0.6417530716753372;
+      s[146] = 0.4187537170452442;
+      t[146] = -0.8257019301996555;
+      w[146] = 0.005856256384098688;
+      r[147] = -0.9512987151702514;
+      s[147] = 0.4187537170452442;
+      t[147] = -0.6417530716753372;
+      w[147] = 0.005856256384098688;
+      r[148] = -0.6417530716753372;
+      s[148] = -0.8257019301996555;
+      t[148] = -0.9512987151702514;
+      w[148] = 0.005856256384098688;
+      r[149] = -0.6417530716753372;
+      s[149] = -0.9512987151702514;
+      t[149] = 0.4187537170452442;
+      w[149] = 0.005856256384098688;
+      r[150] = -0.9512987151702514;
+      s[150] = -0.8257019301996555;
+      t[150] = -0.6417530716753372;
+      w[150] = 0.005856256384098688;
+      r[151] = 0.4187537170452442;
+      s[151] = -0.8257019301996555;
+      t[151] = -0.9512987151702514;
+      w[151] = 0.005856256384098688;
+      r[152] = -0.9512987151702514;
+      s[152] = 0.4187537170452442;
+      t[152] = -0.8257019301996555;
+      w[152] = 0.005856256384098688;
+      r[153] = -0.6417530716753372;
+      s[153] = -0.8257019301996555;
+      t[153] = 0.4187537170452442;
+      w[153] = 0.005856256384098688;
+      r[154] = -0.9512987151702514;
+      s[154] = -0.8257019301996555;
+      t[154] = 0.4187537170452442;
+      w[154] = 0.005856256384098688;
+      r[155] = 0.4187537170452442;
+      s[155] = -0.9512987151702514;
+      t[155] = -0.6417530716753372;
+      w[155] = 0.005856256384098688;
+      r[156] = -0.6417530716753372;
+      s[156] = -0.9512987151702514;
+      t[156] = -0.8257019301996555;
+      w[156] = 0.005856256384098688;
+      r[157] = -0.8257019301996555;
+      s[157] = -0.9512987151702514;
+      t[157] = -0.6417530716753372;
+      w[157] = 0.005856256384098688;
+      r[158] = 0.4187537170452442;
+      s[158] = -0.9512987151702514;
+      t[158] = -0.8257019301996555;
+      w[158] = 0.005856256384098688;
+      r[159] = -0.8257019301996555;
+      s[159] = -0.9512987151702514;
+      t[159] = 0.4187537170452442;
+      w[159] = 0.005856256384098688;
+      r[160] = -0.8257019301996555;
+      s[160] = 0.4187537170452442;
+      t[160] = -0.9512987151702514;
+      w[160] = 0.005856256384098688;
+      r[161] = -0.9512987151702514;
+      s[161] = -0.6417530716753372;
+      t[161] = 0.4187537170452442;
+      w[161] = 0.005856256384098688;
+      r[162] = 0.4187537170452442;
+      s[162] = -0.6417530716753372;
+      t[162] = -0.9512987151702514;
+      w[162] = 0.005856256384098688;
+      r[163] = 0.4187537170452442;
+      s[163] = -0.6417530716753372;
+      t[163] = -0.8257019301996555;
+      w[163] = 0.005856256384098688;
+      r[164] = -0.8257019301996555;
+      s[164] = -0.6417530716753372;
+      t[164] = -0.9512987151702514;
+      w[164] = 0.005856256384098688;
+      r[165] = -0.9512987151702514;
+      s[165] = -0.6417530716753372;
+      t[165] = -0.8257019301996555;
+      w[165] = 0.005856256384098688;
+      r[166] = 0.6760206216666895;
+      s[166] = -0.9243451288222915;
+      t[166] = -0.75826562740743;
+      w[166] = 0.001287935899077956;
+      r[167] = -0.9243451288222915;
+      s[167] = -0.75826562740743;
+      t[167] = 0.6760206216666895;
+      w[167] = 0.001287935899077956;
+      r[168] = -0.9243451288222915;
+      s[168] = 0.6760206216666895;
+      t[168] = -0.75826562740743;
+      w[168] = 0.001287935899077956;
+      r[169] = -0.75826562740743;
+      s[169] = 0.6760206216666895;
+      t[169] = -0.9934098654369681;
+      w[169] = 0.001287935899077956;
+      r[170] = -0.75826562740743;
+      s[170] = 0.6760206216666895;
+      t[170] = -0.9243451288222915;
+      w[170] = 0.001287935899077956;
+      r[171] = -0.9934098654369681;
+      s[171] = 0.6760206216666895;
+      t[171] = -0.75826562740743;
+      w[171] = 0.001287935899077956;
+      r[172] = -0.75826562740743;
+      s[172] = -0.9243451288222915;
+      t[172] = -0.993409865436968;
+      w[172] = 0.001287935899077956;
+      r[173] = -0.75826562740743;
+      s[173] = -0.9934098654369681;
+      t[173] = 0.6760206216666895;
+      w[173] = 0.001287935899077956;
+      r[174] = -0.993409865436968;
+      s[174] = -0.9243451288222915;
+      t[174] = -0.75826562740743;
+      w[174] = 0.001287935899077956;
+      r[175] = 0.6760206216666895;
+      s[175] = -0.9243451288222916;
+      t[175] = -0.993409865436968;
+      w[175] = 0.001287935899077956;
+      r[176] = -0.9934098654369681;
+      s[176] = 0.6760206216666895;
+      t[176] = -0.9243451288222915;
+      w[176] = 0.001287935899077956;
+      r[177] = -0.75826562740743;
+      s[177] = -0.9243451288222915;
+      t[177] = 0.6760206216666895;
+      w[177] = 0.001287935899077956;
+      r[178] = -0.9934098654369681;
+      s[178] = -0.9243451288222915;
+      t[178] = 0.6760206216666895;
+      w[178] = 0.001287935899077956;
+      r[179] = 0.6760206216666895;
+      s[179] = -0.9934098654369681;
+      t[179] = -0.75826562740743;
+      w[179] = 0.001287935899077956;
+      r[180] = -0.75826562740743;
+      s[180] = -0.993409865436968;
+      t[180] = -0.9243451288222915;
+      w[180] = 0.001287935899077956;
+      r[181] = -0.9243451288222915;
+      s[181] = -0.993409865436968;
+      t[181] = -0.75826562740743;
+      w[181] = 0.001287935899077956;
+      r[182] = 0.6760206216666895;
+      s[182] = -0.993409865436968;
+      t[182] = -0.9243451288222916;
+      w[182] = 0.001287935899077956;
+      r[183] = -0.9243451288222915;
+      s[183] = -0.9934098654369681;
+      t[183] = 0.6760206216666895;
+      w[183] = 0.001287935899077956;
+      r[184] = -0.9243451288222915;
+      s[184] = 0.6760206216666895;
+      t[184] = -0.9934098654369681;
+      w[184] = 0.001287935899077956;
+      r[185] = -0.9934098654369681;
+      s[185] = -0.75826562740743;
+      t[185] = 0.6760206216666895;
+      w[185] = 0.001287935899077956;
+      r[186] = 0.6760206216666895;
+      s[186] = -0.75826562740743;
+      t[186] = -0.9934098654369681;
+      w[186] = 0.001287935899077956;
+      r[187] = 0.6760206216666895;
+      s[187] = -0.75826562740743;
+      t[187] = -0.9243451288222915;
+      w[187] = 0.001287935899077956;
+      r[188] = -0.9243451288222915;
+      s[188] = -0.75826562740743;
+      t[188] = -0.993409865436968;
+      w[188] = 0.001287935899077956;
+      r[189] = -0.993409865436968;
+      s[189] = -0.75826562740743;
+      t[189] = -0.9243451288222915;
+      w[189] = 0.001287935899077956;
+      r[190] = 0.0969456158451746;
+      s[190] = -0.3090604280187177;
+      t[190] = -0.8233513951196885;
+      w[190] = 0.0069912420734512;
+      r[191] = -0.3090604280187177;
+      s[191] = -0.8233513951196885;
+      t[191] = 0.0969456158451746;
+      w[191] = 0.0069912420734512;
+      r[192] = -0.3090604280187177;
+      s[192] = 0.0969456158451746;
+      t[192] = -0.8233513951196885;
+      w[192] = 0.0069912420734512;
+      r[193] = -0.8233513951196885;
+      s[193] = 0.09694561584517464;
+      t[193] = -0.9645337927067685;
+      w[193] = 0.0069912420734512;
+      r[194] = -0.8233513951196886;
+      s[194] = 0.09694561584517458;
+      t[194] = -0.3090604280187177;
+      w[194] = 0.0069912420734512;
+      r[195] = -0.9645337927067685;
+      s[195] = 0.09694561584517458;
+      t[195] = -0.8233513951196886;
+      w[195] = 0.0069912420734512;
+      r[196] = -0.8233513951196886;
+      s[196] = -0.3090604280187177;
+      t[196] = -0.9645337927067685;
+      w[196] = 0.0069912420734512;
+      r[197] = -0.8233513951196885;
+      s[197] = -0.9645337927067685;
+      t[197] = 0.09694561584517464;
+      w[197] = 0.0069912420734512;
+      r[198] = -0.9645337927067685;
+      s[198] = -0.3090604280187177;
+      t[198] = -0.8233513951196886;
+      w[198] = 0.0069912420734512;
+      r[199] = 0.09694561584517457;
+      s[199] = -0.3090604280187177;
+      t[199] = -0.9645337927067685;
+      w[199] = 0.0069912420734512;
+      r[200] = -0.9645337927067686;
+      s[200] = 0.0969456158451746;
+      t[200] = -0.3090604280187177;
+      w[200] = 0.0069912420734512;
+      r[201] = -0.8233513951196886;
+      s[201] = -0.3090604280187177;
+      t[201] = 0.09694561584517458;
+      w[201] = 0.0069912420734512;
+      r[202] = -0.9645337927067686;
+      s[202] = -0.3090604280187177;
+      t[202] = 0.0969456158451746;
+      w[202] = 0.0069912420734512;
+      r[203] = 0.09694561584517458;
+      s[203] = -0.9645337927067685;
+      t[203] = -0.8233513951196885;
+      w[203] = 0.0069912420734512;
+      r[204] = -0.8233513951196886;
+      s[204] = -0.9645337927067685;
+      t[204] = -0.3090604280187177;
+      w[204] = 0.0069912420734512;
+      r[205] = -0.3090604280187177;
+      s[205] = -0.9645337927067685;
+      t[205] = -0.8233513951196886;
+      w[205] = 0.0069912420734512;
+      r[206] = 0.09694561584517457;
+      s[206] = -0.9645337927067685;
+      t[206] = -0.3090604280187177;
+      w[206] = 0.0069912420734512;
+      r[207] = -0.3090604280187176;
+      s[207] = -0.9645337927067686;
+      t[207] = 0.09694561584517462;
+      w[207] = 0.0069912420734512;
+      r[208] = -0.3090604280187176;
+      s[208] = 0.09694561584517462;
+      t[208] = -0.9645337927067686;
+      w[208] = 0.0069912420734512;
+      r[209] = -0.9645337927067685;
+      s[209] = -0.8233513951196886;
+      t[209] = 0.09694561584517458;
+      w[209] = 0.0069912420734512;
+      r[210] = 0.09694561584517458;
+      s[210] = -0.8233513951196885;
+      t[210] = -0.9645337927067685;
+      w[210] = 0.0069912420734512;
+      r[211] = 0.0969456158451746;
+      s[211] = -0.8233513951196885;
+      t[211] = -0.3090604280187177;
+      w[211] = 0.0069912420734512;
+      r[212] = -0.3090604280187177;
+      s[212] = -0.8233513951196886;
+      t[212] = -0.9645337927067685;
+      w[212] = 0.0069912420734512;
+      r[213] = -0.9645337927067685;
+      s[213] = -0.8233513951196886;
+      t[213] = -0.3090604280187177;
+      w[213] = 0.0069912420734512;
 
       break;
     }
     case 15: {
-      r[0]   =  -0.9076368170586709; s[0]   =  -0.09236318294132902; t[0]   =  -0.09236318294132902; w[0]   =  0.003624777463188084;
-      r[1]   = -0.09236318294132903; s[1]   =   -0.9076368170586708; t[1]   =  -0.09236318294132903; w[1]   =  0.003624777463188084;
-      r[2]   =  -0.9076368170586709; s[2]   =   -0.9076368170586709; t[2]   =  -0.09236318294132906; w[2]   =  0.003624777463188084;
-      r[3]   =  -0.9076368170586709; s[3]   =  -0.09236318294132906; t[3]   =   -0.9076368170586709; w[3]   =  0.003624777463188084;
-      r[4]   =   -0.092363182941329; s[4]   =   -0.9076368170586709; t[4]   =   -0.9076368170586709; w[4]   =  0.003624777463188084;
-      r[5]   = -0.09236318294132903; s[5]   =  -0.09236318294132903; t[5]   =   -0.9076368170586708; w[5]   =  0.003624777463188084;
-      r[6]   =   -0.370992993579241; s[6]   =    -0.629007006420759; t[6]   =    -0.629007006420759; w[6]   =   0.01433106071621348;
-      r[7]   =   -0.629007006420759; s[7]   =    -0.370992993579241; t[7]   =    -0.629007006420759; w[7]   =   0.01433106071621348;
-      r[8]   =   -0.370992993579241; s[8]   =    -0.370992993579241; t[8]   =    -0.629007006420759; w[8]   =   0.01433106071621348;
-      r[9]   =   -0.370992993579241; s[9]   =    -0.629007006420759; t[9]   =    -0.370992993579241; w[9]   =   0.01433106071621348;
-      r[10]  =   -0.629007006420759; s[10]  =    -0.370992993579241; t[10]  =    -0.370992993579241; w[10]  =   0.01433106071621348;
-      r[11]  =   -0.629007006420759; s[11]  =    -0.629007006420759; t[11]  =    -0.370992993579241; w[11]  =   0.01433106071621348;
-      r[12]  =   -0.976731889985617; s[12]  =  -0.09868672016609403; t[12]  =   -0.8258946696821948; w[12]  =  0.004367279354518188;
-      r[13]  =   -0.976731889985617; s[13]  =  -0.09868672016609403; t[13]  =  -0.09868672016609403; w[13]  =  0.004367279354518188;
-      r[14]  = -0.09868672016609402; s[14]  =  -0.09868672016609402; t[14]  =    -0.976731889985617; w[14]  =  0.004367279354518188;
-      r[15]  =  -0.8258946696821948; s[15]  =    -0.976731889985617; t[15]  =  -0.09868672016609403; w[15]  =  0.004367279354518188;
-      r[16]  = -0.09868672016609403; s[16]  =   -0.8258946696821949; t[16]  =    -0.976731889985617; w[16]  =  0.004367279354518188;
-      r[17]  = -0.09868672016609402; s[17]  =    -0.976731889985617; t[17]  =  -0.09868672016609402; w[17]  =  0.004367279354518188;
-      r[18]  =  -0.8258946696821948; s[18]  =  -0.09868672016609403; t[18]  =    -0.976731889985617; w[18]  =  0.004367279354518188;
-      r[19]  = -0.09868672016609405; s[19]  =   -0.8258946696821948; t[19]  =  -0.09868672016609405; w[19]  =  0.004367279354518188;
-      r[20]  = -0.09868672016609405; s[20]  =  -0.09868672016609405; t[20]  =   -0.8258946696821948; w[20]  =  0.004367279354518188;
-      r[21]  = -0.09868672016609403; s[21]  =    -0.976731889985617; t[21]  =   -0.8258946696821949; w[21]  =  0.004367279354518188;
-      r[22]  =  -0.8258946696821949; s[22]  =  -0.09868672016609403; t[22]  =  -0.09868672016609403; w[22]  =  0.004367279354518188;
-      r[23]  =   -0.976731889985617; s[23]  =   -0.8258946696821948; t[23]  =  -0.09868672016609403; w[23]  =  0.004367279354518188;
-      r[24]  =   0.1352990708252919; s[24]  =   -0.6485414254839078; t[24]  =   -0.8382162198574763; w[24]  =   0.01284507309970654;
-      r[25]  =   0.1352990708252919; s[25]  =   -0.6485414254839078; t[25]  =   -0.6485414254839078; w[25]  =   0.01284507309970654;
-      r[26]  =  -0.6485414254839079; s[26]  =   -0.6485414254839078; t[26]  =    0.1352990708252919; w[26]  =   0.01284507309970654;
-      r[27]  =  -0.8382162198574763; s[27]  =    0.1352990708252919; t[27]  =   -0.6485414254839078; w[27]  =   0.01284507309970654;
-      r[28]  =  -0.6485414254839078; s[28]  =   -0.8382162198574763; t[28]  =    0.1352990708252919; w[28]  =   0.01284507309970654;
-      r[29]  =  -0.6485414254839079; s[29]  =    0.1352990708252919; t[29]  =   -0.6485414254839078; w[29]  =   0.01284507309970654;
-      r[30]  =  -0.8382162198574763; s[30]  =   -0.6485414254839078; t[30]  =    0.1352990708252919; w[30]  =   0.01284507309970654;
-      r[31]  =  -0.6485414254839078; s[31]  =   -0.8382162198574763; t[31]  =   -0.6485414254839078; w[31]  =   0.01284507309970654;
-      r[32]  =  -0.6485414254839078; s[32]  =   -0.6485414254839078; t[32]  =   -0.8382162198574763; w[32]  =   0.01284507309970654;
-      r[33]  =  -0.6485414254839078; s[33]  =    0.1352990708252919; t[33]  =   -0.8382162198574763; w[33]  =   0.01284507309970654;
-      r[34]  =  -0.8382162198574763; s[34]  =   -0.6485414254839078; t[34]  =   -0.6485414254839078; w[34]  =   0.01284507309970654;
-      r[35]  =   0.1352990708252919; s[35]  =   -0.8382162198574763; t[35]  =   -0.6485414254839078; w[35]  =   0.01284507309970654;
-      r[36]  =  -0.1713948686362624; s[36]  =   -0.5320754445652878; t[36]  =   -0.7644542422331619; w[36]  =   0.01322318197056493;
-      r[37]  =  -0.1713948686362624; s[37]  =   -0.5320754445652878; t[37]  =   -0.5320754445652878; w[37]  =   0.01322318197056493;
-      r[38]  =  -0.5320754445652878; s[38]  =   -0.5320754445652878; t[38]  =   -0.1713948686362624; w[38]  =   0.01322318197056493;
-      r[39]  =  -0.7644542422331619; s[39]  =   -0.1713948686362624; t[39]  =   -0.5320754445652878; w[39]  =   0.01322318197056493;
-      r[40]  =  -0.5320754445652878; s[40]  =   -0.7644542422331619; t[40]  =   -0.1713948686362625; w[40]  =   0.01322318197056493;
-      r[41]  =  -0.5320754445652878; s[41]  =   -0.1713948686362624; t[41]  =   -0.5320754445652878; w[41]  =   0.01322318197056493;
-      r[42]  =  -0.7644542422331619; s[42]  =   -0.5320754445652878; t[42]  =   -0.1713948686362624; w[42]  =   0.01322318197056493;
-      r[43]  =  -0.5320754445652878; s[43]  =   -0.7644542422331619; t[43]  =   -0.5320754445652878; w[43]  =   0.01322318197056493;
-      r[44]  =  -0.5320754445652878; s[44]  =   -0.5320754445652878; t[44]  =   -0.7644542422331619; w[44]  =   0.01322318197056493;
-      r[45]  =  -0.5320754445652878; s[45]  =   -0.1713948686362625; t[45]  =   -0.7644542422331619; w[45]  =   0.01322318197056493;
-      r[46]  =  -0.7644542422331619; s[46]  =   -0.5320754445652878; t[46]  =   -0.5320754445652878; w[46]  =   0.01322318197056493;
-      r[47]  =  -0.1713948686362624; s[47]  =   -0.7644542422331619; t[47]  =   -0.5320754445652878; w[47]  =   0.01322318197056493;
-      r[48]  =   0.5928931760523802; s[48]  =   -0.9680223460032426; t[48]  =   -0.6568484840458949; w[48]  =  0.001737921774909094;
-      r[49]  =   0.5928931760523801; s[49]  =   -0.9680223460032426; t[49]  =   -0.9680223460032426; w[49]  =  0.001737921774909094;
-      r[50]  =  -0.9680223460032426; s[50]  =   -0.9680223460032426; t[50]  =    0.5928931760523802; w[50]  =  0.001737921774909094;
-      r[51]  =  -0.6568484840458949; s[51]  =    0.5928931760523802; t[51]  =   -0.9680223460032426; w[51]  =  0.001737921774909094;
-      r[52]  =  -0.9680223460032426; s[52]  =   -0.6568484840458949; t[52]  =    0.5928931760523802; w[52]  =  0.001737921774909094;
-      r[53]  =  -0.9680223460032426; s[53]  =    0.5928931760523802; t[53]  =   -0.9680223460032426; w[53]  =  0.001737921774909094;
-      r[54]  =  -0.6568484840458949; s[54]  =   -0.9680223460032426; t[54]  =    0.5928931760523802; w[54]  =  0.001737921774909094;
-      r[55]  =  -0.9680223460032426; s[55]  =    -0.656848484045895; t[55]  =   -0.9680223460032426; w[55]  =  0.001737921774909094;
-      r[56]  =  -0.9680223460032426; s[56]  =   -0.9680223460032426; t[56]  =    -0.656848484045895; w[56]  =  0.001737921774909094;
-      r[57]  =  -0.9680223460032426; s[57]  =    0.5928931760523802; t[57]  =   -0.6568484840458949; w[57]  =  0.001737921774909094;
-      r[58]  =   -0.656848484045895; s[58]  =   -0.9680223460032426; t[58]  =   -0.9680223460032426; w[58]  =  0.001737921774909094;
-      r[59]  =   0.5928931760523802; s[59]  =   -0.6568484840458949; t[59]  =   -0.9680223460032426; w[59]  =  0.001737921774909094;
-      r[60]  =   0.7288561343388752; s[60]  =   -0.9422902775923775; t[60]  =     -0.84427557915412; w[60]  =    0.0016942693217037;
-      r[61]  =   0.7288561343388751; s[61]  =   -0.9422902775923776; t[61]  =   -0.9422902775923776; w[61]  =    0.0016942693217037;
-      r[62]  =  -0.9422902775923776; s[62]  =   -0.9422902775923776; t[62]  =    0.7288561343388751; w[62]  =    0.0016942693217037;
-      r[63]  =    -0.84427557915412; s[63]  =    0.7288561343388752; t[63]  =   -0.9422902775923775; w[63]  =    0.0016942693217037;
-      r[64]  =  -0.9422902775923776; s[64]  =   -0.8442755791541199; t[64]  =    0.7288561343388751; w[64]  =    0.0016942693217037;
-      r[65]  =  -0.9422902775923776; s[65]  =    0.7288561343388751; t[65]  =   -0.9422902775923776; w[65]  =    0.0016942693217037;
-      r[66]  =    -0.84427557915412; s[66]  =   -0.9422902775923775; t[66]  =    0.7288561343388752; w[66]  =    0.0016942693217037;
-      r[67]  =  -0.9422902775923776; s[67]  =   -0.8442755791541199; t[67]  =   -0.9422902775923776; w[67]  =    0.0016942693217037;
-      r[68]  =  -0.9422902775923776; s[68]  =   -0.9422902775923776; t[68]  =   -0.8442755791541199; w[68]  =    0.0016942693217037;
-      r[69]  =  -0.9422902775923776; s[69]  =    0.7288561343388751; t[69]  =   -0.8442755791541199; w[69]  =    0.0016942693217037;
-      r[70]  =  -0.8442755791541199; s[70]  =   -0.9422902775923776; t[70]  =   -0.9422902775923776; w[70]  =    0.0016942693217037;
-      r[71]  =   0.7288561343388752; s[71]  =     -0.84427557915412; t[71]  =   -0.9422902775923775; w[71]  =    0.0016942693217037;
-      r[72]  =   0.1583485928795491; s[72]  =    -0.971858294245413; t[72]  =    -0.214632004388723; w[72]  =  0.001940446590642878;
-      r[73]  =   0.1583485928795491; s[73]  =    -0.971858294245413; t[73]  =    -0.971858294245413; w[73]  =  0.001940446590642878;
-      r[74]  =   -0.971858294245413; s[74]  =    -0.971858294245413; t[74]  =    0.1583485928795491; w[74]  =  0.001940446590642878;
-      r[75]  =   -0.214632004388723; s[75]  =    0.1583485928795491; t[75]  =    -0.971858294245413; w[75]  =  0.001940446590642878;
-      r[76]  =   -0.971858294245413; s[76]  =    -0.214632004388723; t[76]  =    0.1583485928795491; w[76]  =  0.001940446590642878;
-      r[77]  =   -0.971858294245413; s[77]  =    0.1583485928795491; t[77]  =    -0.971858294245413; w[77]  =  0.001940446590642878;
-      r[78]  =   -0.214632004388723; s[78]  =    -0.971858294245413; t[78]  =    0.1583485928795491; w[78]  =  0.001940446590642878;
-      r[79]  =   -0.971858294245413; s[79]  =    -0.214632004388723; t[79]  =    -0.971858294245413; w[79]  =  0.001940446590642878;
-      r[80]  =   -0.971858294245413; s[80]  =    -0.971858294245413; t[80]  =    -0.214632004388723; w[80]  =  0.001940446590642878;
-      r[81]  =   -0.971858294245413; s[81]  =    0.1583485928795491; t[81]  =    -0.214632004388723; w[81]  =  0.001940446590642878;
-      r[82]  =   -0.214632004388723; s[82]  =    -0.971858294245413; t[82]  =    -0.971858294245413; w[82]  =  0.001940446590642878;
-      r[83]  =   0.1583485928795491; s[83]  =    -0.214632004388723; t[83]  =    -0.971858294245413; w[83]  =  0.001940446590642878;
-      r[84]  =   0.8829223301854611; s[84]  =   -0.9875744948028141; t[84]  =   -0.9077733405798326; w[84]  = 0.0003305107661392797;
-      r[85]  =    0.882922330185461; s[85]  =   -0.9875744948028141; t[85]  =   -0.9875744948028141; w[85]  = 0.0003305107661392797;
-      r[86]  =  -0.9875744948028141; s[86]  =   -0.9875744948028141; t[86]  =    0.8829223301854611; w[86]  = 0.0003305107661392797;
-      r[87]  =  -0.9077733405798326; s[87]  =    0.8829223301854611; t[87]  =   -0.9875744948028141; w[87]  = 0.0003305107661392797;
-      r[88]  =  -0.9875744948028141; s[88]  =   -0.9077733405798326; t[88]  =    0.8829223301854611; w[88]  = 0.0003305107661392797;
-      r[89]  =  -0.9875744948028141; s[89]  =    0.8829223301854611; t[89]  =   -0.9875744948028141; w[89]  = 0.0003305107661392797;
-      r[90]  =  -0.9077733405798326; s[90]  =   -0.9875744948028141; t[90]  =    0.8829223301854611; w[90]  = 0.0003305107661392797;
-      r[91]  =  -0.9875744948028141; s[91]  =   -0.9077733405798327; t[91]  =   -0.9875744948028141; w[91]  = 0.0003305107661392797;
-      r[92]  =  -0.9875744948028141; s[92]  =   -0.9875744948028141; t[92]  =   -0.9077733405798327; w[92]  = 0.0003305107661392797;
-      r[93]  =  -0.9875744948028141; s[93]  =    0.8829223301854611; t[93]  =   -0.9077733405798326; w[93]  = 0.0003305107661392797;
-      r[94]  =  -0.9077733405798327; s[94]  =   -0.9875744948028141; t[94]  =   -0.9875744948028141; w[94]  = 0.0003305107661392797;
-      r[95]  =   0.8829223301854611; s[95]  =   -0.9077733405798326; t[95]  =   -0.9875744948028141; w[95]  = 0.0003305107661392797;
-      r[96]  =   0.4508479895270611; s[96]  =   -0.8735622137514976; t[96]  =   -0.7037235620240663; w[96]  =  0.007011534793568188;
-      r[97]  =   0.4508479895270612; s[97]  =   -0.8735622137514975; t[97]  =   -0.8735622137514975; w[97]  =  0.007011534793568188;
-      r[98]  =  -0.8735622137514975; s[98]  =   -0.8735622137514975; t[98]  =    0.4508479895270611; w[98]  =  0.007011534793568188;
-      r[99]  =  -0.7037235620240664; s[99]  =    0.4508479895270611; t[99]  =   -0.8735622137514975; w[99]  =  0.007011534793568188;
-      r[100] =  -0.8735622137514975; s[100] =   -0.7037235620240664; t[100] =    0.4508479895270611; w[100] =  0.007011534793568188;
-      r[101] =  -0.8735622137514975; s[101] =    0.4508479895270611; t[101] =   -0.8735622137514975; w[101] =  0.007011534793568188;
-      r[102] =  -0.7037235620240664; s[102] =   -0.8735622137514975; t[102] =    0.4508479895270611; w[102] =  0.007011534793568188;
-      r[103] =  -0.8735622137514976; s[103] =   -0.7037235620240663; t[103] =   -0.8735622137514975; w[103] =  0.007011534793568188;
-      r[104] =  -0.8735622137514976; s[104] =   -0.8735622137514975; t[104] =   -0.7037235620240663; w[104] =  0.007011534793568188;
-      r[105] =  -0.8735622137514975; s[105] =    0.4508479895270611; t[105] =   -0.7037235620240664; w[105] =  0.007011534793568188;
-      r[106] =  -0.7037235620240663; s[106] =   -0.8735622137514975; t[106] =   -0.8735622137514975; w[106] =  0.007011534793568188;
-      r[107] =   0.4508479895270611; s[107] =   -0.7037235620240663; t[107] =   -0.8735622137514976; w[107] =  0.007011534793568188;
-      r[108] =  -0.5516925700125669; s[108] =   -0.2744088656233612; t[108] =   -0.8994896987407107; w[108] =   0.01172667523349425;
-      r[109] =   -0.551692570012567; s[109] =   -0.2744088656233612; t[109] =   -0.2744088656233612; w[109] =   0.01172667523349425;
-      r[110] =  -0.2744088656233611; s[110] =   -0.2744088656233612; t[110] =    -0.551692570012567; w[110] =   0.01172667523349425;
-      r[111] =  -0.8994896987407106; s[111] =   -0.5516925700125669; t[111] =   -0.2744088656233612; w[111] =   0.01172667523349425;
-      r[112] =  -0.2744088656233612; s[112] =   -0.8994896987407107; t[112] =   -0.5516925700125669; w[112] =   0.01172667523349425;
-      r[113] =  -0.2744088656233611; s[113] =    -0.551692570012567; t[113] =   -0.2744088656233612; w[113] =   0.01172667523349425;
-      r[114] =  -0.8994896987407106; s[114] =   -0.2744088656233612; t[114] =   -0.5516925700125669; w[114] =   0.01172667523349425;
-      r[115] =  -0.2744088656233612; s[115] =   -0.8994896987407106; t[115] =   -0.2744088656233612; w[115] =   0.01172667523349425;
-      r[116] =  -0.2744088656233612; s[116] =   -0.2744088656233612; t[116] =   -0.8994896987407106; w[116] =   0.01172667523349425;
-      r[117] =  -0.2744088656233612; s[117] =   -0.5516925700125669; t[117] =   -0.8994896987407107; w[117] =   0.01172667523349425;
-      r[118] =  -0.8994896987407106; s[118] =   -0.2744088656233612; t[118] =   -0.2744088656233612; w[118] =   0.01172667523349425;
-      r[119] =  -0.5516925700125669; s[119] =   -0.8994896987407107; t[119] =   -0.2744088656233612; w[119] =   0.01172667523349425;
-      r[120] =  -0.2705478352359212; s[120] =   -0.3647260823842446; t[120] =   -0.9999999999955895; w[120] =  0.001230402051446423;
-      r[121] =  -0.2705478352359212; s[121] =   -0.3647260823842446; t[121] =   -0.3647260823842446; w[121] =  0.001230402051446423;
-      r[122] =  -0.3647260823842446; s[122] =   -0.3647260823842446; t[122] =   -0.2705478352359212; w[122] =  0.001230402051446423;
-      r[123] =  -0.9999999999955895; s[123] =   -0.2705478352359212; t[123] =   -0.3647260823842446; w[123] =  0.001230402051446423;
-      r[124] =  -0.3647260823842446; s[124] =   -0.9999999999955895; t[124] =   -0.2705478352359212; w[124] =  0.001230402051446423;
-      r[125] =  -0.3647260823842446; s[125] =   -0.2705478352359212; t[125] =   -0.3647260823842446; w[125] =  0.001230402051446423;
-      r[126] =  -0.9999999999955895; s[126] =   -0.3647260823842446; t[126] =   -0.2705478352359212; w[126] =  0.001230402051446423;
-      r[127] =  -0.3647260823842446; s[127] =   -0.9999999999955895; t[127] =   -0.3647260823842446; w[127] =  0.001230402051446423;
-      r[128] =  -0.3647260823842446; s[128] =   -0.3647260823842446; t[128] =   -0.9999999999955895; w[128] =  0.001230402051446423;
-      r[129] =  -0.3647260823842446; s[129] =   -0.2705478352359212; t[129] =   -0.9999999999955895; w[129] =  0.001230402051446423;
-      r[130] =  -0.9999999999955895; s[130] =   -0.3647260823842446; t[130] =   -0.3647260823842446; w[130] =  0.001230402051446423;
-      r[131] =  -0.2705478352359212; s[131] =   -0.9999999999955895; t[131] =   -0.3647260823842446; w[131] =  0.001230402051446423;
-      r[132] =    0.626731105538749; s[132] =   -0.8180945156497114; t[132] =   -0.9905420742393262; w[132] =  0.001646474664995799;
-      r[133] =    0.626731105538749; s[133] =   -0.8180945156497114; t[133] =   -0.8180945156497114; w[133] =  0.001646474664995799;
-      r[134] =  -0.8180945156497114; s[134] =   -0.8180945156497114; t[134] =    0.6267311055387491; w[134] =  0.001646474664995799;
-      r[135] =  -0.9905420742393262; s[135] =    0.6267311055387491; t[135] =   -0.8180945156497114; w[135] =  0.001646474664995799;
-      r[136] =  -0.8180945156497114; s[136] =   -0.9905420742393262; t[136] =    0.6267311055387491; w[136] =  0.001646474664995799;
-      r[137] =  -0.8180945156497114; s[137] =    0.6267311055387491; t[137] =   -0.8180945156497114; w[137] =  0.001646474664995799;
-      r[138] =  -0.9905420742393262; s[138] =   -0.8180945156497114; t[138] =    0.6267311055387491; w[138] =  0.001646474664995799;
-      r[139] =  -0.8180945156497114; s[139] =   -0.9905420742393263; t[139] =   -0.8180945156497114; w[139] =  0.001646474664995799;
-      r[140] =  -0.8180945156497114; s[140] =   -0.8180945156497114; t[140] =   -0.9905420742393263; w[140] =  0.001646474664995799;
-      r[141] =  -0.8180945156497114; s[141] =    0.6267311055387491; t[141] =   -0.9905420742393262; w[141] =  0.001646474664995799;
-      r[142] =  -0.9905420742393263; s[142] =   -0.8180945156497114; t[142] =   -0.8180945156497114; w[142] =  0.001646474664995799;
-      r[143] =    0.626731105538749; s[143] =   -0.9905420742393262; t[143] =   -0.8180945156497114; w[143] =  0.001646474664995799;
-      r[144] =   0.3792076436253303; s[144] =      -0.9999981170571; t[144] =   -0.4718864927921055; w[144] =  0.001073960061199892;
-      r[145] =     -0.9999981170571; s[145] =   -0.4718864927921055; t[145] =    0.3792076436253303; w[145] =  0.001073960061199892;
-      r[146] =     -0.9999981170571; s[146] =    0.3792076436253303; t[146] =   -0.4718864927921055; w[146] =  0.001073960061199892;
-      r[147] =  -0.4718864927921055; s[147] =    0.3792076436253303; t[147] =    -0.907323033776125; w[147] =  0.001073960061199892;
-      r[148] =  -0.4718864927921054; s[148] =    0.3792076436253304; t[148] =      -0.9999981170571; w[148] =  0.001073960061199892;
-      r[149] =   -0.907323033776125; s[149] =    0.3792076436253303; t[149] =   -0.4718864927921055; w[149] =  0.001073960061199892;
-      r[150] =  -0.4718864927921055; s[150] =      -0.9999981170571; t[150] =   -0.9073230337761251; w[150] =  0.001073960061199892;
-      r[151] =  -0.4718864927921055; s[151] =    -0.907323033776125; t[151] =    0.3792076436253303; w[151] =  0.001073960061199892;
-      r[152] =  -0.9073230337761251; s[152] =      -0.9999981170571; t[152] =   -0.4718864927921055; w[152] =  0.001073960061199892;
-      r[153] =   0.3792076436253303; s[153] =      -0.9999981170571; t[153] =   -0.9073230337761251; w[153] =  0.001073960061199892;
-      r[154] =  -0.9073230337761251; s[154] =    0.3792076436253304; t[154] =      -0.9999981170571; w[154] =  0.001073960061199892;
-      r[155] =  -0.4718864927921054; s[155] =      -0.9999981170571; t[155] =    0.3792076436253304; w[155] =  0.001073960061199892;
-      r[156] =  -0.9073230337761251; s[156] =      -0.9999981170571; t[156] =    0.3792076436253304; w[156] =  0.001073960061199892;
-      r[157] =   0.3792076436253303; s[157] =    -0.907323033776125; t[157] =   -0.4718864927921055; w[157] =  0.001073960061199892;
-      r[158] =  -0.4718864927921055; s[158] =   -0.9073230337761251; t[158] =      -0.9999981170571; w[158] =  0.001073960061199892;
-      r[159] =     -0.9999981170571; s[159] =   -0.9073230337761251; t[159] =   -0.4718864927921055; w[159] =  0.001073960061199892;
-      r[160] =   0.3792076436253303; s[160] =   -0.9073230337761251; t[160] =      -0.9999981170571; w[160] =  0.001073960061199892;
-      r[161] =  -0.9999981170571001; s[161] =    -0.907323033776125; t[161] =    0.3792076436253303; w[161] =  0.001073960061199892;
-      r[162] =  -0.9999981170571001; s[162] =    0.3792076436253303; t[162] =    -0.907323033776125; w[162] =  0.001073960061199892;
-      r[163] =   -0.907323033776125; s[163] =   -0.4718864927921055; t[163] =    0.3792076436253303; w[163] =  0.001073960061199892;
-      r[164] =   0.3792076436253303; s[164] =   -0.4718864927921055; t[164] =    -0.907323033776125; w[164] =  0.001073960061199892;
-      r[165] =   0.3792076436253303; s[165] =   -0.4718864927921055; t[165] =      -0.9999981170571; w[165] =  0.001073960061199892;
-      r[166] =     -0.9999981170571; s[166] =   -0.4718864927921055; t[166] =   -0.9073230337761251; w[166] =  0.001073960061199892;
-      r[167] =  -0.9073230337761251; s[167] =   -0.4718864927921055; t[167] =      -0.9999981170571; w[167] =  0.001073960061199892;
-      r[168] = 0.009243726856787898; s[168] =    -0.967668650055743; t[168] =   -0.3971580998740936; w[168] =  0.006581160094433206;
-      r[169] =  -0.9676686500557431; s[169] =   -0.3971580998740936; t[169] =  0.009243726856787898; w[169] =  0.006581160094433206;
-      r[170] =  -0.9676686500557431; s[170] =  0.009243726856787898; t[170] =   -0.3971580998740936; w[170] =  0.006581160094433206;
-      r[171] =  -0.3971580998740935; s[171] =  0.009243726856787933; t[171] =   -0.6444169769269515; w[171] =  0.006581160094433206;
-      r[172] =  -0.3971580998740936; s[172] =  0.009243726856787898; t[172] =    -0.967668650055743; w[172] =  0.006581160094433206;
-      r[173] =  -0.6444169769269515; s[173] =  0.009243726856787905; t[173] =   -0.3971580998740936; w[173] =  0.006581160094433206;
-      r[174] =  -0.3971580998740936; s[174] =   -0.9676686500557431; t[174] =   -0.6444169769269514; w[174] =  0.006581160094433206;
-      r[175] =  -0.3971580998740935; s[175] =   -0.6444169769269515; t[175] =  0.009243726856787933; w[175] =  0.006581160094433206;
-      r[176] =  -0.6444169769269514; s[176] =   -0.9676686500557431; t[176] =   -0.3971580998740936; w[176] =  0.006581160094433206;
-      r[177] = 0.009243726856787926; s[177] =    -0.967668650055743; t[177] =   -0.6444169769269514; w[177] =  0.006581160094433206;
-      r[178] =  -0.6444169769269514; s[178] =  0.009243726856787926; t[178] =    -0.967668650055743; w[178] =  0.006581160094433206;
-      r[179] =  -0.3971580998740936; s[179] =    -0.967668650055743; t[179] =  0.009243726856787898; w[179] =  0.006581160094433206;
-      r[180] =  -0.6444169769269514; s[180] =    -0.967668650055743; t[180] =  0.009243726856787926; w[180] =  0.006581160094433206;
-      r[181] = 0.009243726856787877; s[181] =   -0.6444169769269514; t[181] =   -0.3971580998740936; w[181] =  0.006581160094433206;
-      r[182] =  -0.3971580998740936; s[182] =   -0.6444169769269514; t[182] =   -0.9676686500557431; w[182] =  0.006581160094433206;
-      r[183] =  -0.9676686500557431; s[183] =   -0.6444169769269514; t[183] =   -0.3971580998740936; w[183] =  0.006581160094433206;
-      r[184] = 0.009243726856787926; s[184] =   -0.6444169769269514; t[184] =    -0.967668650055743; w[184] =  0.006581160094433206;
-      r[185] =   -0.967668650055743; s[185] =   -0.6444169769269514; t[185] =  0.009243726856787926; w[185] =  0.006581160094433206;
-      r[186] =   -0.967668650055743; s[186] =  0.009243726856787926; t[186] =   -0.6444169769269514; w[186] =  0.006581160094433206;
-      r[187] =  -0.6444169769269515; s[187] =   -0.3971580998740936; t[187] =  0.009243726856787905; w[187] =  0.006581160094433206;
-      r[188] = 0.009243726856787877; s[188] =   -0.3971580998740936; t[188] =   -0.6444169769269514; w[188] =  0.006581160094433206;
-      r[189] = 0.009243726856787898; s[189] =   -0.3971580998740936; t[189] =    -0.967668650055743; w[189] =  0.006581160094433206;
-      r[190] =  -0.9676686500557431; s[190] =   -0.3971580998740936; t[190] =   -0.6444169769269514; w[190] =  0.006581160094433206;
-      r[191] =  -0.6444169769269514; s[191] =   -0.3971580998740936; t[191] =   -0.9676686500557431; w[191] =  0.006581160094433206;
-      r[192] = -0.05167635714627374; s[192] =    -0.777238506336745; t[192] =   -0.3482370284980628; w[192] =   0.00689920931058941;
-      r[193] =   -0.777238506336745; s[193] =   -0.3482370284980628; t[193] =  -0.05167635714627372; w[193] =   0.00689920931058941;
-      r[194] =   -0.777238506336745; s[194] =  -0.05167635714627372; t[194] =   -0.3482370284980628; w[194] =   0.00689920931058941;
-      r[195] =  -0.3482370284980628; s[195] =  -0.05167635714627371; t[195] =   -0.8228481080189185; w[195] =   0.00689920931058941;
-      r[196] =  -0.3482370284980628; s[196] =  -0.05167635714627374; t[196] =    -0.777238506336745; w[196] =   0.00689920931058941;
-      r[197] =  -0.8228481080189184; s[197] =  -0.05167635714627372; t[197] =   -0.3482370284980628; w[197] =   0.00689920931058941;
-      r[198] =  -0.3482370284980628; s[198] =    -0.777238506336745; t[198] =   -0.8228481080189185; w[198] =   0.00689920931058941;
-      r[199] =  -0.3482370284980628; s[199] =   -0.8228481080189185; t[199] =  -0.05167635714627371; w[199] =   0.00689920931058941;
-      r[200] =  -0.8228481080189185; s[200] =    -0.777238506336745; t[200] =   -0.3482370284980628; w[200] =   0.00689920931058941;
-      r[201] = -0.05167635714627372; s[201] =   -0.7772385063367451; t[201] =   -0.8228481080189185; w[201] =   0.00689920931058941;
-      r[202] =  -0.8228481080189185; s[202] =  -0.05167635714627372; t[202] =    -0.777238506336745; w[202] =   0.00689920931058941;
-      r[203] =  -0.3482370284980628; s[203] =    -0.777238506336745; t[203] =  -0.05167635714627374; w[203] =   0.00689920931058941;
-      r[204] =  -0.8228481080189185; s[204] =    -0.777238506336745; t[204] =  -0.05167635714627372; w[204] =   0.00689920931058941;
-      r[205] = -0.05167635714627371; s[205] =   -0.8228481080189185; t[205] =   -0.3482370284980628; w[205] =   0.00689920931058941;
-      r[206] =  -0.3482370284980628; s[206] =   -0.8228481080189185; t[206] =    -0.777238506336745; w[206] =   0.00689920931058941;
-      r[207] =   -0.777238506336745; s[207] =   -0.8228481080189185; t[207] =   -0.3482370284980628; w[207] =   0.00689920931058941;
-      r[208] = -0.05167635714627372; s[208] =   -0.8228481080189185; t[208] =   -0.7772385063367451; w[208] =   0.00689920931058941;
-      r[209] =   -0.777238506336745; s[209] =   -0.8228481080189185; t[209] =  -0.05167635714627372; w[209] =   0.00689920931058941;
-      r[210] =   -0.777238506336745; s[210] =  -0.05167635714627372; t[210] =   -0.8228481080189185; w[210] =   0.00689920931058941;
-      r[211] =  -0.8228481080189184; s[211] =   -0.3482370284980628; t[211] =  -0.05167635714627372; w[211] =   0.00689920931058941;
-      r[212] = -0.05167635714627371; s[212] =   -0.3482370284980628; t[212] =   -0.8228481080189185; w[212] =   0.00689920931058941;
-      r[213] = -0.05167635714627374; s[213] =   -0.3482370284980628; t[213] =    -0.777238506336745; w[213] =   0.00689920931058941;
-      r[214] =   -0.777238506336745; s[214] =   -0.3482370284980628; t[214] =   -0.8228481080189185; w[214] =   0.00689920931058941;
-      r[215] =  -0.8228481080189185; s[215] =   -0.3482370284980628; t[215] =    -0.777238506336745; w[215] =   0.00689920931058941;
-      r[216] =   0.3406917485192568; s[216] =   -0.7452186729085513; t[216] =   -0.6245753999478341; w[216] =  0.002901831405233198;
-      r[217] =  -0.7452186729085513; s[217] =   -0.6245753999478341; t[217] =    0.3406917485192569; w[217] =  0.002901831405233198;
-      r[218] =  -0.7452186729085513; s[218] =    0.3406917485192569; t[218] =   -0.6245753999478341; w[218] =  0.002901831405233198;
-      r[219] =  -0.6245753999478341; s[219] =    0.3406917485192569; t[219] =   -0.9708976756628716; w[219] =  0.002901831405233198;
-      r[220] =  -0.6245753999478341; s[220] =    0.3406917485192569; t[220] =   -0.7452186729085513; w[220] =  0.002901831405233198;
-      r[221] =  -0.9708976756628716; s[221] =    0.3406917485192569; t[221] =   -0.6245753999478341; w[221] =  0.002901831405233198;
-      r[222] =  -0.6245753999478341; s[222] =   -0.7452186729085513; t[222] =   -0.9708976756628716; w[222] =  0.002901831405233198;
-      r[223] =  -0.6245753999478341; s[223] =   -0.9708976756628716; t[223] =    0.3406917485192569; w[223] =  0.002901831405233198;
-      r[224] =  -0.9708976756628716; s[224] =   -0.7452186729085513; t[224] =   -0.6245753999478341; w[224] =  0.002901831405233198;
-      r[225] =   0.3406917485192569; s[225] =   -0.7452186729085513; t[225] =   -0.9708976756628716; w[225] =  0.002901831405233198;
-      r[226] =  -0.9708976756628716; s[226] =    0.3406917485192569; t[226] =   -0.7452186729085513; w[226] =  0.002901831405233198;
-      r[227] =  -0.6245753999478341; s[227] =   -0.7452186729085513; t[227] =    0.3406917485192569; w[227] =  0.002901831405233198;
-      r[228] =  -0.9708976756628716; s[228] =   -0.7452186729085513; t[228] =    0.3406917485192569; w[228] =  0.002901831405233198;
-      r[229] =   0.3406917485192569; s[229] =   -0.9708976756628716; t[229] =   -0.6245753999478341; w[229] =  0.002901831405233198;
-      r[230] =  -0.6245753999478341; s[230] =   -0.9708976756628716; t[230] =   -0.7452186729085513; w[230] =  0.002901831405233198;
-      r[231] =  -0.7452186729085513; s[231] =   -0.9708976756628716; t[231] =   -0.6245753999478341; w[231] =  0.002901831405233198;
-      r[232] =   0.3406917485192569; s[232] =   -0.9708976756628716; t[232] =   -0.7452186729085513; w[232] =  0.002901831405233198;
-      r[233] =  -0.7452186729085513; s[233] =   -0.9708976756628716; t[233] =    0.3406917485192569; w[233] =  0.002901831405233198;
-      r[234] =  -0.7452186729085513; s[234] =    0.3406917485192569; t[234] =   -0.9708976756628716; w[234] =  0.002901831405233198;
-      r[235] =  -0.9708976756628716; s[235] =   -0.6245753999478341; t[235] =    0.3406917485192569; w[235] =  0.002901831405233198;
-      r[236] =   0.3406917485192569; s[236] =   -0.6245753999478341; t[236] =   -0.9708976756628716; w[236] =  0.002901831405233198;
-      r[237] =   0.3406917485192568; s[237] =   -0.6245753999478341; t[237] =   -0.7452186729085513; w[237] =  0.002901831405233198;
-      r[238] =  -0.7452186729085513; s[238] =   -0.6245753999478341; t[238] =   -0.9708976756628716; w[238] =  0.002901831405233198;
-      r[239] =  -0.9708976756628716; s[239] =   -0.6245753999478341; t[239] =   -0.7452186729085513; w[239] =  0.002901831405233198;
-      r[240] =   0.2189863676757071; s[240] =   -0.8497429545848707; t[240] =   -0.9379540563954483; w[240] =  0.004733550328404792;
-      r[241] =  -0.8497429545848707; s[241] =   -0.9379540563954483; t[241] =    0.2189863676757071; w[241] =  0.004733550328404792;
-      r[242] =  -0.8497429545848707; s[242] =    0.2189863676757071; t[242] =   -0.9379540563954483; w[242] =  0.004733550328404792;
-      r[243] =  -0.9379540563954483; s[243] =    0.2189863676757071; t[243] =   -0.4312893566953881; w[243] =  0.004733550328404792;
-      r[244] =  -0.9379540563954483; s[244] =    0.2189863676757071; t[244] =   -0.8497429545848707; w[244] =  0.004733550328404792;
-      r[245] =  -0.4312893566953881; s[245] =    0.2189863676757071; t[245] =   -0.9379540563954483; w[245] =  0.004733550328404792;
-      r[246] =  -0.9379540563954483; s[246] =   -0.8497429545848707; t[246] =   -0.4312893566953881; w[246] =  0.004733550328404792;
-      r[247] =  -0.9379540563954483; s[247] =   -0.4312893566953881; t[247] =    0.2189863676757071; w[247] =  0.004733550328404792;
-      r[248] =  -0.4312893566953881; s[248] =   -0.8497429545848707; t[248] =   -0.9379540563954483; w[248] =  0.004733550328404792;
-      r[249] =   0.2189863676757071; s[249] =   -0.8497429545848707; t[249] =   -0.4312893566953881; w[249] =  0.004733550328404792;
-      r[250] =  -0.4312893566953881; s[250] =    0.2189863676757071; t[250] =   -0.8497429545848707; w[250] =  0.004733550328404792;
-      r[251] =  -0.9379540563954483; s[251] =   -0.8497429545848707; t[251] =    0.2189863676757071; w[251] =  0.004733550328404792;
-      r[252] =  -0.4312893566953881; s[252] =   -0.8497429545848707; t[252] =    0.2189863676757071; w[252] =  0.004733550328404792;
-      r[253] =   0.2189863676757071; s[253] =   -0.4312893566953881; t[253] =   -0.9379540563954483; w[253] =  0.004733550328404792;
-      r[254] =  -0.9379540563954483; s[254] =   -0.4312893566953881; t[254] =   -0.8497429545848707; w[254] =  0.004733550328404792;
-      r[255] =  -0.8497429545848707; s[255] =   -0.4312893566953881; t[255] =   -0.9379540563954483; w[255] =  0.004733550328404792;
-      r[256] =   0.2189863676757071; s[256] =   -0.4312893566953881; t[256] =   -0.8497429545848707; w[256] =  0.004733550328404792;
-      r[257] =  -0.8497429545848707; s[257] =   -0.4312893566953881; t[257] =    0.2189863676757071; w[257] =  0.004733550328404792;
-      r[258] =  -0.8497429545848707; s[258] =    0.2189863676757071; t[258] =   -0.4312893566953881; w[258] =  0.004733550328404792;
-      r[259] =  -0.4312893566953881; s[259] =   -0.9379540563954483; t[259] =    0.2189863676757071; w[259] =  0.004733550328404792;
-      r[260] =   0.2189863676757071; s[260] =   -0.9379540563954483; t[260] =   -0.4312893566953881; w[260] =  0.004733550328404792;
-      r[261] =   0.2189863676757071; s[261] =   -0.9379540563954483; t[261] =   -0.8497429545848707; w[261] =  0.004733550328404792;
-      r[262] =  -0.8497429545848707; s[262] =   -0.9379540563954483; t[262] =   -0.4312893566953881; w[262] =  0.004733550328404792;
-      r[263] =  -0.4312893566953881; s[263] =   -0.9379540563954483; t[263] =   -0.8497429545848707; w[263] =  0.004733550328404792;
+      r[0] = -0.9076368170586709;
+      s[0] = -0.09236318294132902;
+      t[0] = -0.09236318294132902;
+      w[0] = 0.003624777463188084;
+      r[1] = -0.09236318294132903;
+      s[1] = -0.9076368170586708;
+      t[1] = -0.09236318294132903;
+      w[1] = 0.003624777463188084;
+      r[2] = -0.9076368170586709;
+      s[2] = -0.9076368170586709;
+      t[2] = -0.09236318294132906;
+      w[2] = 0.003624777463188084;
+      r[3] = -0.9076368170586709;
+      s[3] = -0.09236318294132906;
+      t[3] = -0.9076368170586709;
+      w[3] = 0.003624777463188084;
+      r[4] = -0.092363182941329;
+      s[4] = -0.9076368170586709;
+      t[4] = -0.9076368170586709;
+      w[4] = 0.003624777463188084;
+      r[5] = -0.09236318294132903;
+      s[5] = -0.09236318294132903;
+      t[5] = -0.9076368170586708;
+      w[5] = 0.003624777463188084;
+      r[6] = -0.370992993579241;
+      s[6] = -0.629007006420759;
+      t[6] = -0.629007006420759;
+      w[6] = 0.01433106071621348;
+      r[7] = -0.629007006420759;
+      s[7] = -0.370992993579241;
+      t[7] = -0.629007006420759;
+      w[7] = 0.01433106071621348;
+      r[8] = -0.370992993579241;
+      s[8] = -0.370992993579241;
+      t[8] = -0.629007006420759;
+      w[8] = 0.01433106071621348;
+      r[9] = -0.370992993579241;
+      s[9] = -0.629007006420759;
+      t[9] = -0.370992993579241;
+      w[9] = 0.01433106071621348;
+      r[10] = -0.629007006420759;
+      s[10] = -0.370992993579241;
+      t[10] = -0.370992993579241;
+      w[10] = 0.01433106071621348;
+      r[11] = -0.629007006420759;
+      s[11] = -0.629007006420759;
+      t[11] = -0.370992993579241;
+      w[11] = 0.01433106071621348;
+      r[12] = -0.976731889985617;
+      s[12] = -0.09868672016609403;
+      t[12] = -0.8258946696821948;
+      w[12] = 0.004367279354518188;
+      r[13] = -0.976731889985617;
+      s[13] = -0.09868672016609403;
+      t[13] = -0.09868672016609403;
+      w[13] = 0.004367279354518188;
+      r[14] = -0.09868672016609402;
+      s[14] = -0.09868672016609402;
+      t[14] = -0.976731889985617;
+      w[14] = 0.004367279354518188;
+      r[15] = -0.8258946696821948;
+      s[15] = -0.976731889985617;
+      t[15] = -0.09868672016609403;
+      w[15] = 0.004367279354518188;
+      r[16] = -0.09868672016609403;
+      s[16] = -0.8258946696821949;
+      t[16] = -0.976731889985617;
+      w[16] = 0.004367279354518188;
+      r[17] = -0.09868672016609402;
+      s[17] = -0.976731889985617;
+      t[17] = -0.09868672016609402;
+      w[17] = 0.004367279354518188;
+      r[18] = -0.8258946696821948;
+      s[18] = -0.09868672016609403;
+      t[18] = -0.976731889985617;
+      w[18] = 0.004367279354518188;
+      r[19] = -0.09868672016609405;
+      s[19] = -0.8258946696821948;
+      t[19] = -0.09868672016609405;
+      w[19] = 0.004367279354518188;
+      r[20] = -0.09868672016609405;
+      s[20] = -0.09868672016609405;
+      t[20] = -0.8258946696821948;
+      w[20] = 0.004367279354518188;
+      r[21] = -0.09868672016609403;
+      s[21] = -0.976731889985617;
+      t[21] = -0.8258946696821949;
+      w[21] = 0.004367279354518188;
+      r[22] = -0.8258946696821949;
+      s[22] = -0.09868672016609403;
+      t[22] = -0.09868672016609403;
+      w[22] = 0.004367279354518188;
+      r[23] = -0.976731889985617;
+      s[23] = -0.8258946696821948;
+      t[23] = -0.09868672016609403;
+      w[23] = 0.004367279354518188;
+      r[24] = 0.1352990708252919;
+      s[24] = -0.6485414254839078;
+      t[24] = -0.8382162198574763;
+      w[24] = 0.01284507309970654;
+      r[25] = 0.1352990708252919;
+      s[25] = -0.6485414254839078;
+      t[25] = -0.6485414254839078;
+      w[25] = 0.01284507309970654;
+      r[26] = -0.6485414254839079;
+      s[26] = -0.6485414254839078;
+      t[26] = 0.1352990708252919;
+      w[26] = 0.01284507309970654;
+      r[27] = -0.8382162198574763;
+      s[27] = 0.1352990708252919;
+      t[27] = -0.6485414254839078;
+      w[27] = 0.01284507309970654;
+      r[28] = -0.6485414254839078;
+      s[28] = -0.8382162198574763;
+      t[28] = 0.1352990708252919;
+      w[28] = 0.01284507309970654;
+      r[29] = -0.6485414254839079;
+      s[29] = 0.1352990708252919;
+      t[29] = -0.6485414254839078;
+      w[29] = 0.01284507309970654;
+      r[30] = -0.8382162198574763;
+      s[30] = -0.6485414254839078;
+      t[30] = 0.1352990708252919;
+      w[30] = 0.01284507309970654;
+      r[31] = -0.6485414254839078;
+      s[31] = -0.8382162198574763;
+      t[31] = -0.6485414254839078;
+      w[31] = 0.01284507309970654;
+      r[32] = -0.6485414254839078;
+      s[32] = -0.6485414254839078;
+      t[32] = -0.8382162198574763;
+      w[32] = 0.01284507309970654;
+      r[33] = -0.6485414254839078;
+      s[33] = 0.1352990708252919;
+      t[33] = -0.8382162198574763;
+      w[33] = 0.01284507309970654;
+      r[34] = -0.8382162198574763;
+      s[34] = -0.6485414254839078;
+      t[34] = -0.6485414254839078;
+      w[34] = 0.01284507309970654;
+      r[35] = 0.1352990708252919;
+      s[35] = -0.8382162198574763;
+      t[35] = -0.6485414254839078;
+      w[35] = 0.01284507309970654;
+      r[36] = -0.1713948686362624;
+      s[36] = -0.5320754445652878;
+      t[36] = -0.7644542422331619;
+      w[36] = 0.01322318197056493;
+      r[37] = -0.1713948686362624;
+      s[37] = -0.5320754445652878;
+      t[37] = -0.5320754445652878;
+      w[37] = 0.01322318197056493;
+      r[38] = -0.5320754445652878;
+      s[38] = -0.5320754445652878;
+      t[38] = -0.1713948686362624;
+      w[38] = 0.01322318197056493;
+      r[39] = -0.7644542422331619;
+      s[39] = -0.1713948686362624;
+      t[39] = -0.5320754445652878;
+      w[39] = 0.01322318197056493;
+      r[40] = -0.5320754445652878;
+      s[40] = -0.7644542422331619;
+      t[40] = -0.1713948686362625;
+      w[40] = 0.01322318197056493;
+      r[41] = -0.5320754445652878;
+      s[41] = -0.1713948686362624;
+      t[41] = -0.5320754445652878;
+      w[41] = 0.01322318197056493;
+      r[42] = -0.7644542422331619;
+      s[42] = -0.5320754445652878;
+      t[42] = -0.1713948686362624;
+      w[42] = 0.01322318197056493;
+      r[43] = -0.5320754445652878;
+      s[43] = -0.7644542422331619;
+      t[43] = -0.5320754445652878;
+      w[43] = 0.01322318197056493;
+      r[44] = -0.5320754445652878;
+      s[44] = -0.5320754445652878;
+      t[44] = -0.7644542422331619;
+      w[44] = 0.01322318197056493;
+      r[45] = -0.5320754445652878;
+      s[45] = -0.1713948686362625;
+      t[45] = -0.7644542422331619;
+      w[45] = 0.01322318197056493;
+      r[46] = -0.7644542422331619;
+      s[46] = -0.5320754445652878;
+      t[46] = -0.5320754445652878;
+      w[46] = 0.01322318197056493;
+      r[47] = -0.1713948686362624;
+      s[47] = -0.7644542422331619;
+      t[47] = -0.5320754445652878;
+      w[47] = 0.01322318197056493;
+      r[48] = 0.5928931760523802;
+      s[48] = -0.9680223460032426;
+      t[48] = -0.6568484840458949;
+      w[48] = 0.001737921774909094;
+      r[49] = 0.5928931760523801;
+      s[49] = -0.9680223460032426;
+      t[49] = -0.9680223460032426;
+      w[49] = 0.001737921774909094;
+      r[50] = -0.9680223460032426;
+      s[50] = -0.9680223460032426;
+      t[50] = 0.5928931760523802;
+      w[50] = 0.001737921774909094;
+      r[51] = -0.6568484840458949;
+      s[51] = 0.5928931760523802;
+      t[51] = -0.9680223460032426;
+      w[51] = 0.001737921774909094;
+      r[52] = -0.9680223460032426;
+      s[52] = -0.6568484840458949;
+      t[52] = 0.5928931760523802;
+      w[52] = 0.001737921774909094;
+      r[53] = -0.9680223460032426;
+      s[53] = 0.5928931760523802;
+      t[53] = -0.9680223460032426;
+      w[53] = 0.001737921774909094;
+      r[54] = -0.6568484840458949;
+      s[54] = -0.9680223460032426;
+      t[54] = 0.5928931760523802;
+      w[54] = 0.001737921774909094;
+      r[55] = -0.9680223460032426;
+      s[55] = -0.656848484045895;
+      t[55] = -0.9680223460032426;
+      w[55] = 0.001737921774909094;
+      r[56] = -0.9680223460032426;
+      s[56] = -0.9680223460032426;
+      t[56] = -0.656848484045895;
+      w[56] = 0.001737921774909094;
+      r[57] = -0.9680223460032426;
+      s[57] = 0.5928931760523802;
+      t[57] = -0.6568484840458949;
+      w[57] = 0.001737921774909094;
+      r[58] = -0.656848484045895;
+      s[58] = -0.9680223460032426;
+      t[58] = -0.9680223460032426;
+      w[58] = 0.001737921774909094;
+      r[59] = 0.5928931760523802;
+      s[59] = -0.6568484840458949;
+      t[59] = -0.9680223460032426;
+      w[59] = 0.001737921774909094;
+      r[60] = 0.7288561343388752;
+      s[60] = -0.9422902775923775;
+      t[60] = -0.84427557915412;
+      w[60] = 0.0016942693217037;
+      r[61] = 0.7288561343388751;
+      s[61] = -0.9422902775923776;
+      t[61] = -0.9422902775923776;
+      w[61] = 0.0016942693217037;
+      r[62] = -0.9422902775923776;
+      s[62] = -0.9422902775923776;
+      t[62] = 0.7288561343388751;
+      w[62] = 0.0016942693217037;
+      r[63] = -0.84427557915412;
+      s[63] = 0.7288561343388752;
+      t[63] = -0.9422902775923775;
+      w[63] = 0.0016942693217037;
+      r[64] = -0.9422902775923776;
+      s[64] = -0.8442755791541199;
+      t[64] = 0.7288561343388751;
+      w[64] = 0.0016942693217037;
+      r[65] = -0.9422902775923776;
+      s[65] = 0.7288561343388751;
+      t[65] = -0.9422902775923776;
+      w[65] = 0.0016942693217037;
+      r[66] = -0.84427557915412;
+      s[66] = -0.9422902775923775;
+      t[66] = 0.7288561343388752;
+      w[66] = 0.0016942693217037;
+      r[67] = -0.9422902775923776;
+      s[67] = -0.8442755791541199;
+      t[67] = -0.9422902775923776;
+      w[67] = 0.0016942693217037;
+      r[68] = -0.9422902775923776;
+      s[68] = -0.9422902775923776;
+      t[68] = -0.8442755791541199;
+      w[68] = 0.0016942693217037;
+      r[69] = -0.9422902775923776;
+      s[69] = 0.7288561343388751;
+      t[69] = -0.8442755791541199;
+      w[69] = 0.0016942693217037;
+      r[70] = -0.8442755791541199;
+      s[70] = -0.9422902775923776;
+      t[70] = -0.9422902775923776;
+      w[70] = 0.0016942693217037;
+      r[71] = 0.7288561343388752;
+      s[71] = -0.84427557915412;
+      t[71] = -0.9422902775923775;
+      w[71] = 0.0016942693217037;
+      r[72] = 0.1583485928795491;
+      s[72] = -0.971858294245413;
+      t[72] = -0.214632004388723;
+      w[72] = 0.001940446590642878;
+      r[73] = 0.1583485928795491;
+      s[73] = -0.971858294245413;
+      t[73] = -0.971858294245413;
+      w[73] = 0.001940446590642878;
+      r[74] = -0.971858294245413;
+      s[74] = -0.971858294245413;
+      t[74] = 0.1583485928795491;
+      w[74] = 0.001940446590642878;
+      r[75] = -0.214632004388723;
+      s[75] = 0.1583485928795491;
+      t[75] = -0.971858294245413;
+      w[75] = 0.001940446590642878;
+      r[76] = -0.971858294245413;
+      s[76] = -0.214632004388723;
+      t[76] = 0.1583485928795491;
+      w[76] = 0.001940446590642878;
+      r[77] = -0.971858294245413;
+      s[77] = 0.1583485928795491;
+      t[77] = -0.971858294245413;
+      w[77] = 0.001940446590642878;
+      r[78] = -0.214632004388723;
+      s[78] = -0.971858294245413;
+      t[78] = 0.1583485928795491;
+      w[78] = 0.001940446590642878;
+      r[79] = -0.971858294245413;
+      s[79] = -0.214632004388723;
+      t[79] = -0.971858294245413;
+      w[79] = 0.001940446590642878;
+      r[80] = -0.971858294245413;
+      s[80] = -0.971858294245413;
+      t[80] = -0.214632004388723;
+      w[80] = 0.001940446590642878;
+      r[81] = -0.971858294245413;
+      s[81] = 0.1583485928795491;
+      t[81] = -0.214632004388723;
+      w[81] = 0.001940446590642878;
+      r[82] = -0.214632004388723;
+      s[82] = -0.971858294245413;
+      t[82] = -0.971858294245413;
+      w[82] = 0.001940446590642878;
+      r[83] = 0.1583485928795491;
+      s[83] = -0.214632004388723;
+      t[83] = -0.971858294245413;
+      w[83] = 0.001940446590642878;
+      r[84] = 0.8829223301854611;
+      s[84] = -0.9875744948028141;
+      t[84] = -0.9077733405798326;
+      w[84] = 0.0003305107661392797;
+      r[85] = 0.882922330185461;
+      s[85] = -0.9875744948028141;
+      t[85] = -0.9875744948028141;
+      w[85] = 0.0003305107661392797;
+      r[86] = -0.9875744948028141;
+      s[86] = -0.9875744948028141;
+      t[86] = 0.8829223301854611;
+      w[86] = 0.0003305107661392797;
+      r[87] = -0.9077733405798326;
+      s[87] = 0.8829223301854611;
+      t[87] = -0.9875744948028141;
+      w[87] = 0.0003305107661392797;
+      r[88] = -0.9875744948028141;
+      s[88] = -0.9077733405798326;
+      t[88] = 0.8829223301854611;
+      w[88] = 0.0003305107661392797;
+      r[89] = -0.9875744948028141;
+      s[89] = 0.8829223301854611;
+      t[89] = -0.9875744948028141;
+      w[89] = 0.0003305107661392797;
+      r[90] = -0.9077733405798326;
+      s[90] = -0.9875744948028141;
+      t[90] = 0.8829223301854611;
+      w[90] = 0.0003305107661392797;
+      r[91] = -0.9875744948028141;
+      s[91] = -0.9077733405798327;
+      t[91] = -0.9875744948028141;
+      w[91] = 0.0003305107661392797;
+      r[92] = -0.9875744948028141;
+      s[92] = -0.9875744948028141;
+      t[92] = -0.9077733405798327;
+      w[92] = 0.0003305107661392797;
+      r[93] = -0.9875744948028141;
+      s[93] = 0.8829223301854611;
+      t[93] = -0.9077733405798326;
+      w[93] = 0.0003305107661392797;
+      r[94] = -0.9077733405798327;
+      s[94] = -0.9875744948028141;
+      t[94] = -0.9875744948028141;
+      w[94] = 0.0003305107661392797;
+      r[95] = 0.8829223301854611;
+      s[95] = -0.9077733405798326;
+      t[95] = -0.9875744948028141;
+      w[95] = 0.0003305107661392797;
+      r[96] = 0.4508479895270611;
+      s[96] = -0.8735622137514976;
+      t[96] = -0.7037235620240663;
+      w[96] = 0.007011534793568188;
+      r[97] = 0.4508479895270612;
+      s[97] = -0.8735622137514975;
+      t[97] = -0.8735622137514975;
+      w[97] = 0.007011534793568188;
+      r[98] = -0.8735622137514975;
+      s[98] = -0.8735622137514975;
+      t[98] = 0.4508479895270611;
+      w[98] = 0.007011534793568188;
+      r[99] = -0.7037235620240664;
+      s[99] = 0.4508479895270611;
+      t[99] = -0.8735622137514975;
+      w[99] = 0.007011534793568188;
+      r[100] = -0.8735622137514975;
+      s[100] = -0.7037235620240664;
+      t[100] = 0.4508479895270611;
+      w[100] = 0.007011534793568188;
+      r[101] = -0.8735622137514975;
+      s[101] = 0.4508479895270611;
+      t[101] = -0.8735622137514975;
+      w[101] = 0.007011534793568188;
+      r[102] = -0.7037235620240664;
+      s[102] = -0.8735622137514975;
+      t[102] = 0.4508479895270611;
+      w[102] = 0.007011534793568188;
+      r[103] = -0.8735622137514976;
+      s[103] = -0.7037235620240663;
+      t[103] = -0.8735622137514975;
+      w[103] = 0.007011534793568188;
+      r[104] = -0.8735622137514976;
+      s[104] = -0.8735622137514975;
+      t[104] = -0.7037235620240663;
+      w[104] = 0.007011534793568188;
+      r[105] = -0.8735622137514975;
+      s[105] = 0.4508479895270611;
+      t[105] = -0.7037235620240664;
+      w[105] = 0.007011534793568188;
+      r[106] = -0.7037235620240663;
+      s[106] = -0.8735622137514975;
+      t[106] = -0.8735622137514975;
+      w[106] = 0.007011534793568188;
+      r[107] = 0.4508479895270611;
+      s[107] = -0.7037235620240663;
+      t[107] = -0.8735622137514976;
+      w[107] = 0.007011534793568188;
+      r[108] = -0.5516925700125669;
+      s[108] = -0.2744088656233612;
+      t[108] = -0.8994896987407107;
+      w[108] = 0.01172667523349425;
+      r[109] = -0.551692570012567;
+      s[109] = -0.2744088656233612;
+      t[109] = -0.2744088656233612;
+      w[109] = 0.01172667523349425;
+      r[110] = -0.2744088656233611;
+      s[110] = -0.2744088656233612;
+      t[110] = -0.551692570012567;
+      w[110] = 0.01172667523349425;
+      r[111] = -0.8994896987407106;
+      s[111] = -0.5516925700125669;
+      t[111] = -0.2744088656233612;
+      w[111] = 0.01172667523349425;
+      r[112] = -0.2744088656233612;
+      s[112] = -0.8994896987407107;
+      t[112] = -0.5516925700125669;
+      w[112] = 0.01172667523349425;
+      r[113] = -0.2744088656233611;
+      s[113] = -0.551692570012567;
+      t[113] = -0.2744088656233612;
+      w[113] = 0.01172667523349425;
+      r[114] = -0.8994896987407106;
+      s[114] = -0.2744088656233612;
+      t[114] = -0.5516925700125669;
+      w[114] = 0.01172667523349425;
+      r[115] = -0.2744088656233612;
+      s[115] = -0.8994896987407106;
+      t[115] = -0.2744088656233612;
+      w[115] = 0.01172667523349425;
+      r[116] = -0.2744088656233612;
+      s[116] = -0.2744088656233612;
+      t[116] = -0.8994896987407106;
+      w[116] = 0.01172667523349425;
+      r[117] = -0.2744088656233612;
+      s[117] = -0.5516925700125669;
+      t[117] = -0.8994896987407107;
+      w[117] = 0.01172667523349425;
+      r[118] = -0.8994896987407106;
+      s[118] = -0.2744088656233612;
+      t[118] = -0.2744088656233612;
+      w[118] = 0.01172667523349425;
+      r[119] = -0.5516925700125669;
+      s[119] = -0.8994896987407107;
+      t[119] = -0.2744088656233612;
+      w[119] = 0.01172667523349425;
+      r[120] = -0.2705478352359212;
+      s[120] = -0.3647260823842446;
+      t[120] = -0.9999999999955895;
+      w[120] = 0.001230402051446423;
+      r[121] = -0.2705478352359212;
+      s[121] = -0.3647260823842446;
+      t[121] = -0.3647260823842446;
+      w[121] = 0.001230402051446423;
+      r[122] = -0.3647260823842446;
+      s[122] = -0.3647260823842446;
+      t[122] = -0.2705478352359212;
+      w[122] = 0.001230402051446423;
+      r[123] = -0.9999999999955895;
+      s[123] = -0.2705478352359212;
+      t[123] = -0.3647260823842446;
+      w[123] = 0.001230402051446423;
+      r[124] = -0.3647260823842446;
+      s[124] = -0.9999999999955895;
+      t[124] = -0.2705478352359212;
+      w[124] = 0.001230402051446423;
+      r[125] = -0.3647260823842446;
+      s[125] = -0.2705478352359212;
+      t[125] = -0.3647260823842446;
+      w[125] = 0.001230402051446423;
+      r[126] = -0.9999999999955895;
+      s[126] = -0.3647260823842446;
+      t[126] = -0.2705478352359212;
+      w[126] = 0.001230402051446423;
+      r[127] = -0.3647260823842446;
+      s[127] = -0.9999999999955895;
+      t[127] = -0.3647260823842446;
+      w[127] = 0.001230402051446423;
+      r[128] = -0.3647260823842446;
+      s[128] = -0.3647260823842446;
+      t[128] = -0.9999999999955895;
+      w[128] = 0.001230402051446423;
+      r[129] = -0.3647260823842446;
+      s[129] = -0.2705478352359212;
+      t[129] = -0.9999999999955895;
+      w[129] = 0.001230402051446423;
+      r[130] = -0.9999999999955895;
+      s[130] = -0.3647260823842446;
+      t[130] = -0.3647260823842446;
+      w[130] = 0.001230402051446423;
+      r[131] = -0.2705478352359212;
+      s[131] = -0.9999999999955895;
+      t[131] = -0.3647260823842446;
+      w[131] = 0.001230402051446423;
+      r[132] = 0.626731105538749;
+      s[132] = -0.8180945156497114;
+      t[132] = -0.9905420742393262;
+      w[132] = 0.001646474664995799;
+      r[133] = 0.626731105538749;
+      s[133] = -0.8180945156497114;
+      t[133] = -0.8180945156497114;
+      w[133] = 0.001646474664995799;
+      r[134] = -0.8180945156497114;
+      s[134] = -0.8180945156497114;
+      t[134] = 0.6267311055387491;
+      w[134] = 0.001646474664995799;
+      r[135] = -0.9905420742393262;
+      s[135] = 0.6267311055387491;
+      t[135] = -0.8180945156497114;
+      w[135] = 0.001646474664995799;
+      r[136] = -0.8180945156497114;
+      s[136] = -0.9905420742393262;
+      t[136] = 0.6267311055387491;
+      w[136] = 0.001646474664995799;
+      r[137] = -0.8180945156497114;
+      s[137] = 0.6267311055387491;
+      t[137] = -0.8180945156497114;
+      w[137] = 0.001646474664995799;
+      r[138] = -0.9905420742393262;
+      s[138] = -0.8180945156497114;
+      t[138] = 0.6267311055387491;
+      w[138] = 0.001646474664995799;
+      r[139] = -0.8180945156497114;
+      s[139] = -0.9905420742393263;
+      t[139] = -0.8180945156497114;
+      w[139] = 0.001646474664995799;
+      r[140] = -0.8180945156497114;
+      s[140] = -0.8180945156497114;
+      t[140] = -0.9905420742393263;
+      w[140] = 0.001646474664995799;
+      r[141] = -0.8180945156497114;
+      s[141] = 0.6267311055387491;
+      t[141] = -0.9905420742393262;
+      w[141] = 0.001646474664995799;
+      r[142] = -0.9905420742393263;
+      s[142] = -0.8180945156497114;
+      t[142] = -0.8180945156497114;
+      w[142] = 0.001646474664995799;
+      r[143] = 0.626731105538749;
+      s[143] = -0.9905420742393262;
+      t[143] = -0.8180945156497114;
+      w[143] = 0.001646474664995799;
+      r[144] = 0.3792076436253303;
+      s[144] = -0.9999981170571;
+      t[144] = -0.4718864927921055;
+      w[144] = 0.001073960061199892;
+      r[145] = -0.9999981170571;
+      s[145] = -0.4718864927921055;
+      t[145] = 0.3792076436253303;
+      w[145] = 0.001073960061199892;
+      r[146] = -0.9999981170571;
+      s[146] = 0.3792076436253303;
+      t[146] = -0.4718864927921055;
+      w[146] = 0.001073960061199892;
+      r[147] = -0.4718864927921055;
+      s[147] = 0.3792076436253303;
+      t[147] = -0.907323033776125;
+      w[147] = 0.001073960061199892;
+      r[148] = -0.4718864927921054;
+      s[148] = 0.3792076436253304;
+      t[148] = -0.9999981170571;
+      w[148] = 0.001073960061199892;
+      r[149] = -0.907323033776125;
+      s[149] = 0.3792076436253303;
+      t[149] = -0.4718864927921055;
+      w[149] = 0.001073960061199892;
+      r[150] = -0.4718864927921055;
+      s[150] = -0.9999981170571;
+      t[150] = -0.9073230337761251;
+      w[150] = 0.001073960061199892;
+      r[151] = -0.4718864927921055;
+      s[151] = -0.907323033776125;
+      t[151] = 0.3792076436253303;
+      w[151] = 0.001073960061199892;
+      r[152] = -0.9073230337761251;
+      s[152] = -0.9999981170571;
+      t[152] = -0.4718864927921055;
+      w[152] = 0.001073960061199892;
+      r[153] = 0.3792076436253303;
+      s[153] = -0.9999981170571;
+      t[153] = -0.9073230337761251;
+      w[153] = 0.001073960061199892;
+      r[154] = -0.9073230337761251;
+      s[154] = 0.3792076436253304;
+      t[154] = -0.9999981170571;
+      w[154] = 0.001073960061199892;
+      r[155] = -0.4718864927921054;
+      s[155] = -0.9999981170571;
+      t[155] = 0.3792076436253304;
+      w[155] = 0.001073960061199892;
+      r[156] = -0.9073230337761251;
+      s[156] = -0.9999981170571;
+      t[156] = 0.3792076436253304;
+      w[156] = 0.001073960061199892;
+      r[157] = 0.3792076436253303;
+      s[157] = -0.907323033776125;
+      t[157] = -0.4718864927921055;
+      w[157] = 0.001073960061199892;
+      r[158] = -0.4718864927921055;
+      s[158] = -0.9073230337761251;
+      t[158] = -0.9999981170571;
+      w[158] = 0.001073960061199892;
+      r[159] = -0.9999981170571;
+      s[159] = -0.9073230337761251;
+      t[159] = -0.4718864927921055;
+      w[159] = 0.001073960061199892;
+      r[160] = 0.3792076436253303;
+      s[160] = -0.9073230337761251;
+      t[160] = -0.9999981170571;
+      w[160] = 0.001073960061199892;
+      r[161] = -0.9999981170571001;
+      s[161] = -0.907323033776125;
+      t[161] = 0.3792076436253303;
+      w[161] = 0.001073960061199892;
+      r[162] = -0.9999981170571001;
+      s[162] = 0.3792076436253303;
+      t[162] = -0.907323033776125;
+      w[162] = 0.001073960061199892;
+      r[163] = -0.907323033776125;
+      s[163] = -0.4718864927921055;
+      t[163] = 0.3792076436253303;
+      w[163] = 0.001073960061199892;
+      r[164] = 0.3792076436253303;
+      s[164] = -0.4718864927921055;
+      t[164] = -0.907323033776125;
+      w[164] = 0.001073960061199892;
+      r[165] = 0.3792076436253303;
+      s[165] = -0.4718864927921055;
+      t[165] = -0.9999981170571;
+      w[165] = 0.001073960061199892;
+      r[166] = -0.9999981170571;
+      s[166] = -0.4718864927921055;
+      t[166] = -0.9073230337761251;
+      w[166] = 0.001073960061199892;
+      r[167] = -0.9073230337761251;
+      s[167] = -0.4718864927921055;
+      t[167] = -0.9999981170571;
+      w[167] = 0.001073960061199892;
+      r[168] = 0.009243726856787898;
+      s[168] = -0.967668650055743;
+      t[168] = -0.3971580998740936;
+      w[168] = 0.006581160094433206;
+      r[169] = -0.9676686500557431;
+      s[169] = -0.3971580998740936;
+      t[169] = 0.009243726856787898;
+      w[169] = 0.006581160094433206;
+      r[170] = -0.9676686500557431;
+      s[170] = 0.009243726856787898;
+      t[170] = -0.3971580998740936;
+      w[170] = 0.006581160094433206;
+      r[171] = -0.3971580998740935;
+      s[171] = 0.009243726856787933;
+      t[171] = -0.6444169769269515;
+      w[171] = 0.006581160094433206;
+      r[172] = -0.3971580998740936;
+      s[172] = 0.009243726856787898;
+      t[172] = -0.967668650055743;
+      w[172] = 0.006581160094433206;
+      r[173] = -0.6444169769269515;
+      s[173] = 0.009243726856787905;
+      t[173] = -0.3971580998740936;
+      w[173] = 0.006581160094433206;
+      r[174] = -0.3971580998740936;
+      s[174] = -0.9676686500557431;
+      t[174] = -0.6444169769269514;
+      w[174] = 0.006581160094433206;
+      r[175] = -0.3971580998740935;
+      s[175] = -0.6444169769269515;
+      t[175] = 0.009243726856787933;
+      w[175] = 0.006581160094433206;
+      r[176] = -0.6444169769269514;
+      s[176] = -0.9676686500557431;
+      t[176] = -0.3971580998740936;
+      w[176] = 0.006581160094433206;
+      r[177] = 0.009243726856787926;
+      s[177] = -0.967668650055743;
+      t[177] = -0.6444169769269514;
+      w[177] = 0.006581160094433206;
+      r[178] = -0.6444169769269514;
+      s[178] = 0.009243726856787926;
+      t[178] = -0.967668650055743;
+      w[178] = 0.006581160094433206;
+      r[179] = -0.3971580998740936;
+      s[179] = -0.967668650055743;
+      t[179] = 0.009243726856787898;
+      w[179] = 0.006581160094433206;
+      r[180] = -0.6444169769269514;
+      s[180] = -0.967668650055743;
+      t[180] = 0.009243726856787926;
+      w[180] = 0.006581160094433206;
+      r[181] = 0.009243726856787877;
+      s[181] = -0.6444169769269514;
+      t[181] = -0.3971580998740936;
+      w[181] = 0.006581160094433206;
+      r[182] = -0.3971580998740936;
+      s[182] = -0.6444169769269514;
+      t[182] = -0.9676686500557431;
+      w[182] = 0.006581160094433206;
+      r[183] = -0.9676686500557431;
+      s[183] = -0.6444169769269514;
+      t[183] = -0.3971580998740936;
+      w[183] = 0.006581160094433206;
+      r[184] = 0.009243726856787926;
+      s[184] = -0.6444169769269514;
+      t[184] = -0.967668650055743;
+      w[184] = 0.006581160094433206;
+      r[185] = -0.967668650055743;
+      s[185] = -0.6444169769269514;
+      t[185] = 0.009243726856787926;
+      w[185] = 0.006581160094433206;
+      r[186] = -0.967668650055743;
+      s[186] = 0.009243726856787926;
+      t[186] = -0.6444169769269514;
+      w[186] = 0.006581160094433206;
+      r[187] = -0.6444169769269515;
+      s[187] = -0.3971580998740936;
+      t[187] = 0.009243726856787905;
+      w[187] = 0.006581160094433206;
+      r[188] = 0.009243726856787877;
+      s[188] = -0.3971580998740936;
+      t[188] = -0.6444169769269514;
+      w[188] = 0.006581160094433206;
+      r[189] = 0.009243726856787898;
+      s[189] = -0.3971580998740936;
+      t[189] = -0.967668650055743;
+      w[189] = 0.006581160094433206;
+      r[190] = -0.9676686500557431;
+      s[190] = -0.3971580998740936;
+      t[190] = -0.6444169769269514;
+      w[190] = 0.006581160094433206;
+      r[191] = -0.6444169769269514;
+      s[191] = -0.3971580998740936;
+      t[191] = -0.9676686500557431;
+      w[191] = 0.006581160094433206;
+      r[192] = -0.05167635714627374;
+      s[192] = -0.777238506336745;
+      t[192] = -0.3482370284980628;
+      w[192] = 0.00689920931058941;
+      r[193] = -0.777238506336745;
+      s[193] = -0.3482370284980628;
+      t[193] = -0.05167635714627372;
+      w[193] = 0.00689920931058941;
+      r[194] = -0.777238506336745;
+      s[194] = -0.05167635714627372;
+      t[194] = -0.3482370284980628;
+      w[194] = 0.00689920931058941;
+      r[195] = -0.3482370284980628;
+      s[195] = -0.05167635714627371;
+      t[195] = -0.8228481080189185;
+      w[195] = 0.00689920931058941;
+      r[196] = -0.3482370284980628;
+      s[196] = -0.05167635714627374;
+      t[196] = -0.777238506336745;
+      w[196] = 0.00689920931058941;
+      r[197] = -0.8228481080189184;
+      s[197] = -0.05167635714627372;
+      t[197] = -0.3482370284980628;
+      w[197] = 0.00689920931058941;
+      r[198] = -0.3482370284980628;
+      s[198] = -0.777238506336745;
+      t[198] = -0.8228481080189185;
+      w[198] = 0.00689920931058941;
+      r[199] = -0.3482370284980628;
+      s[199] = -0.8228481080189185;
+      t[199] = -0.05167635714627371;
+      w[199] = 0.00689920931058941;
+      r[200] = -0.8228481080189185;
+      s[200] = -0.777238506336745;
+      t[200] = -0.3482370284980628;
+      w[200] = 0.00689920931058941;
+      r[201] = -0.05167635714627372;
+      s[201] = -0.7772385063367451;
+      t[201] = -0.8228481080189185;
+      w[201] = 0.00689920931058941;
+      r[202] = -0.8228481080189185;
+      s[202] = -0.05167635714627372;
+      t[202] = -0.777238506336745;
+      w[202] = 0.00689920931058941;
+      r[203] = -0.3482370284980628;
+      s[203] = -0.777238506336745;
+      t[203] = -0.05167635714627374;
+      w[203] = 0.00689920931058941;
+      r[204] = -0.8228481080189185;
+      s[204] = -0.777238506336745;
+      t[204] = -0.05167635714627372;
+      w[204] = 0.00689920931058941;
+      r[205] = -0.05167635714627371;
+      s[205] = -0.8228481080189185;
+      t[205] = -0.3482370284980628;
+      w[205] = 0.00689920931058941;
+      r[206] = -0.3482370284980628;
+      s[206] = -0.8228481080189185;
+      t[206] = -0.777238506336745;
+      w[206] = 0.00689920931058941;
+      r[207] = -0.777238506336745;
+      s[207] = -0.8228481080189185;
+      t[207] = -0.3482370284980628;
+      w[207] = 0.00689920931058941;
+      r[208] = -0.05167635714627372;
+      s[208] = -0.8228481080189185;
+      t[208] = -0.7772385063367451;
+      w[208] = 0.00689920931058941;
+      r[209] = -0.777238506336745;
+      s[209] = -0.8228481080189185;
+      t[209] = -0.05167635714627372;
+      w[209] = 0.00689920931058941;
+      r[210] = -0.777238506336745;
+      s[210] = -0.05167635714627372;
+      t[210] = -0.8228481080189185;
+      w[210] = 0.00689920931058941;
+      r[211] = -0.8228481080189184;
+      s[211] = -0.3482370284980628;
+      t[211] = -0.05167635714627372;
+      w[211] = 0.00689920931058941;
+      r[212] = -0.05167635714627371;
+      s[212] = -0.3482370284980628;
+      t[212] = -0.8228481080189185;
+      w[212] = 0.00689920931058941;
+      r[213] = -0.05167635714627374;
+      s[213] = -0.3482370284980628;
+      t[213] = -0.777238506336745;
+      w[213] = 0.00689920931058941;
+      r[214] = -0.777238506336745;
+      s[214] = -0.3482370284980628;
+      t[214] = -0.8228481080189185;
+      w[214] = 0.00689920931058941;
+      r[215] = -0.8228481080189185;
+      s[215] = -0.3482370284980628;
+      t[215] = -0.777238506336745;
+      w[215] = 0.00689920931058941;
+      r[216] = 0.3406917485192568;
+      s[216] = -0.7452186729085513;
+      t[216] = -0.6245753999478341;
+      w[216] = 0.002901831405233198;
+      r[217] = -0.7452186729085513;
+      s[217] = -0.6245753999478341;
+      t[217] = 0.3406917485192569;
+      w[217] = 0.002901831405233198;
+      r[218] = -0.7452186729085513;
+      s[218] = 0.3406917485192569;
+      t[218] = -0.6245753999478341;
+      w[218] = 0.002901831405233198;
+      r[219] = -0.6245753999478341;
+      s[219] = 0.3406917485192569;
+      t[219] = -0.9708976756628716;
+      w[219] = 0.002901831405233198;
+      r[220] = -0.6245753999478341;
+      s[220] = 0.3406917485192569;
+      t[220] = -0.7452186729085513;
+      w[220] = 0.002901831405233198;
+      r[221] = -0.9708976756628716;
+      s[221] = 0.3406917485192569;
+      t[221] = -0.6245753999478341;
+      w[221] = 0.002901831405233198;
+      r[222] = -0.6245753999478341;
+      s[222] = -0.7452186729085513;
+      t[222] = -0.9708976756628716;
+      w[222] = 0.002901831405233198;
+      r[223] = -0.6245753999478341;
+      s[223] = -0.9708976756628716;
+      t[223] = 0.3406917485192569;
+      w[223] = 0.002901831405233198;
+      r[224] = -0.9708976756628716;
+      s[224] = -0.7452186729085513;
+      t[224] = -0.6245753999478341;
+      w[224] = 0.002901831405233198;
+      r[225] = 0.3406917485192569;
+      s[225] = -0.7452186729085513;
+      t[225] = -0.9708976756628716;
+      w[225] = 0.002901831405233198;
+      r[226] = -0.9708976756628716;
+      s[226] = 0.3406917485192569;
+      t[226] = -0.7452186729085513;
+      w[226] = 0.002901831405233198;
+      r[227] = -0.6245753999478341;
+      s[227] = -0.7452186729085513;
+      t[227] = 0.3406917485192569;
+      w[227] = 0.002901831405233198;
+      r[228] = -0.9708976756628716;
+      s[228] = -0.7452186729085513;
+      t[228] = 0.3406917485192569;
+      w[228] = 0.002901831405233198;
+      r[229] = 0.3406917485192569;
+      s[229] = -0.9708976756628716;
+      t[229] = -0.6245753999478341;
+      w[229] = 0.002901831405233198;
+      r[230] = -0.6245753999478341;
+      s[230] = -0.9708976756628716;
+      t[230] = -0.7452186729085513;
+      w[230] = 0.002901831405233198;
+      r[231] = -0.7452186729085513;
+      s[231] = -0.9708976756628716;
+      t[231] = -0.6245753999478341;
+      w[231] = 0.002901831405233198;
+      r[232] = 0.3406917485192569;
+      s[232] = -0.9708976756628716;
+      t[232] = -0.7452186729085513;
+      w[232] = 0.002901831405233198;
+      r[233] = -0.7452186729085513;
+      s[233] = -0.9708976756628716;
+      t[233] = 0.3406917485192569;
+      w[233] = 0.002901831405233198;
+      r[234] = -0.7452186729085513;
+      s[234] = 0.3406917485192569;
+      t[234] = -0.9708976756628716;
+      w[234] = 0.002901831405233198;
+      r[235] = -0.9708976756628716;
+      s[235] = -0.6245753999478341;
+      t[235] = 0.3406917485192569;
+      w[235] = 0.002901831405233198;
+      r[236] = 0.3406917485192569;
+      s[236] = -0.6245753999478341;
+      t[236] = -0.9708976756628716;
+      w[236] = 0.002901831405233198;
+      r[237] = 0.3406917485192568;
+      s[237] = -0.6245753999478341;
+      t[237] = -0.7452186729085513;
+      w[237] = 0.002901831405233198;
+      r[238] = -0.7452186729085513;
+      s[238] = -0.6245753999478341;
+      t[238] = -0.9708976756628716;
+      w[238] = 0.002901831405233198;
+      r[239] = -0.9708976756628716;
+      s[239] = -0.6245753999478341;
+      t[239] = -0.7452186729085513;
+      w[239] = 0.002901831405233198;
+      r[240] = 0.2189863676757071;
+      s[240] = -0.8497429545848707;
+      t[240] = -0.9379540563954483;
+      w[240] = 0.004733550328404792;
+      r[241] = -0.8497429545848707;
+      s[241] = -0.9379540563954483;
+      t[241] = 0.2189863676757071;
+      w[241] = 0.004733550328404792;
+      r[242] = -0.8497429545848707;
+      s[242] = 0.2189863676757071;
+      t[242] = -0.9379540563954483;
+      w[242] = 0.004733550328404792;
+      r[243] = -0.9379540563954483;
+      s[243] = 0.2189863676757071;
+      t[243] = -0.4312893566953881;
+      w[243] = 0.004733550328404792;
+      r[244] = -0.9379540563954483;
+      s[244] = 0.2189863676757071;
+      t[244] = -0.8497429545848707;
+      w[244] = 0.004733550328404792;
+      r[245] = -0.4312893566953881;
+      s[245] = 0.2189863676757071;
+      t[245] = -0.9379540563954483;
+      w[245] = 0.004733550328404792;
+      r[246] = -0.9379540563954483;
+      s[246] = -0.8497429545848707;
+      t[246] = -0.4312893566953881;
+      w[246] = 0.004733550328404792;
+      r[247] = -0.9379540563954483;
+      s[247] = -0.4312893566953881;
+      t[247] = 0.2189863676757071;
+      w[247] = 0.004733550328404792;
+      r[248] = -0.4312893566953881;
+      s[248] = -0.8497429545848707;
+      t[248] = -0.9379540563954483;
+      w[248] = 0.004733550328404792;
+      r[249] = 0.2189863676757071;
+      s[249] = -0.8497429545848707;
+      t[249] = -0.4312893566953881;
+      w[249] = 0.004733550328404792;
+      r[250] = -0.4312893566953881;
+      s[250] = 0.2189863676757071;
+      t[250] = -0.8497429545848707;
+      w[250] = 0.004733550328404792;
+      r[251] = -0.9379540563954483;
+      s[251] = -0.8497429545848707;
+      t[251] = 0.2189863676757071;
+      w[251] = 0.004733550328404792;
+      r[252] = -0.4312893566953881;
+      s[252] = -0.8497429545848707;
+      t[252] = 0.2189863676757071;
+      w[252] = 0.004733550328404792;
+      r[253] = 0.2189863676757071;
+      s[253] = -0.4312893566953881;
+      t[253] = -0.9379540563954483;
+      w[253] = 0.004733550328404792;
+      r[254] = -0.9379540563954483;
+      s[254] = -0.4312893566953881;
+      t[254] = -0.8497429545848707;
+      w[254] = 0.004733550328404792;
+      r[255] = -0.8497429545848707;
+      s[255] = -0.4312893566953881;
+      t[255] = -0.9379540563954483;
+      w[255] = 0.004733550328404792;
+      r[256] = 0.2189863676757071;
+      s[256] = -0.4312893566953881;
+      t[256] = -0.8497429545848707;
+      w[256] = 0.004733550328404792;
+      r[257] = -0.8497429545848707;
+      s[257] = -0.4312893566953881;
+      t[257] = 0.2189863676757071;
+      w[257] = 0.004733550328404792;
+      r[258] = -0.8497429545848707;
+      s[258] = 0.2189863676757071;
+      t[258] = -0.4312893566953881;
+      w[258] = 0.004733550328404792;
+      r[259] = -0.4312893566953881;
+      s[259] = -0.9379540563954483;
+      t[259] = 0.2189863676757071;
+      w[259] = 0.004733550328404792;
+      r[260] = 0.2189863676757071;
+      s[260] = -0.9379540563954483;
+      t[260] = -0.4312893566953881;
+      w[260] = 0.004733550328404792;
+      r[261] = 0.2189863676757071;
+      s[261] = -0.9379540563954483;
+      t[261] = -0.8497429545848707;
+      w[261] = 0.004733550328404792;
+      r[262] = -0.8497429545848707;
+      s[262] = -0.9379540563954483;
+      t[262] = -0.4312893566953881;
+      w[262] = 0.004733550328404792;
+      r[263] = -0.4312893566953881;
+      s[263] = -0.9379540563954483;
+      t[263] = -0.8497429545848707;
+      w[263] = 0.004733550328404792;
 
       break;
     }
@@ -3284,7 +10259,6 @@ void CFEMStandardElementBase::IntegrationPointsTetrahedron(void) {
 }
 
 void CFEMStandardElementBase::IntegrationPointsPyramid(void) {
-
   /*--- The 3D quadrature rule for a pyramid is obtained by transforming the
         standard pyramid into a standard hexahedron by means of the Duffy
         transformation. On the created hexahedron a tensor product rule is used,
@@ -3294,7 +10268,7 @@ void CFEMStandardElementBase::IntegrationPointsPyramid(void) {
         is 0.25*(1-t)^2, which explains the alpha = 2 in the Gauss-Jacobi.
         Determine the number of integration points in 1D, which is stored in M,
         and the actual integration 1D integration points. ---*/
-  unsigned short M = orderExact/2 + 1;
+  unsigned short M = orderExact / 2 + 1;
 
   vector<su2double> GLPoints(M), GLWeights(M);
   GaussLegendrePoints1D(GLPoints, GLWeights);
@@ -3305,23 +10279,23 @@ void CFEMStandardElementBase::IntegrationPointsPyramid(void) {
 
   /*--- Allocate the memory for the integration points and weights
         of the pyramid and determine them.                ---*/
-  nIntegration = M*M*M;
+  nIntegration = M * M * M;
   rIntegration.resize(nIntegration);
   sIntegration.resize(nIntegration);
   tIntegration.resize(nIntegration);
   wIntegration.resize(nIntegration);
 
   unsigned int ii = 0;
-  for(unsigned short k=0; k<M; ++k) {
-    for(unsigned short j=0; j<M; ++j) {
-      for(unsigned short i=0; i<M; ++i, ++ii) {
-        const su2double xi   = GLPoints[i];
-        const su2double eta  = GLPoints[j];
+  for (unsigned short k = 0; k < M; ++k) {
+    for (unsigned short j = 0; j < M; ++j) {
+      for (unsigned short i = 0; i < M; ++i, ++ii) {
+        const su2double xi = GLPoints[i];
+        const su2double eta = GLPoints[j];
         const su2double zeta = GJPoints[k];
-        rIntegration[ii] = 0.5*(1.0-zeta)*xi;
-        sIntegration[ii] = 0.5*(1.0-zeta)*eta;
+        rIntegration[ii] = 0.5 * (1.0 - zeta) * xi;
+        sIntegration[ii] = 0.5 * (1.0 - zeta) * eta;
         tIntegration[ii] = zeta;
-        wIntegration[ii] = 0.25*GLWeights[i]*GLWeights[j]*GJWeights[k];
+        wIntegration[ii] = 0.25 * GLWeights[i] * GLWeights[j] * GJWeights[k];
       }
     }
   }
diff --git a/Common/src/fem/fem_standard_element.cpp b/Common/src/fem/fem_standard_element.cpp
index b03f1ab929c..84d0103f699 100644
--- a/Common/src/fem/fem_standard_element.cpp
+++ b/Common/src/fem/fem_standard_element.cpp
@@ -33,157 +33,137 @@
 /*          Public member functions of CFEMStandardElementBase.                     */
 /*----------------------------------------------------------------------------------*/
 
-unsigned short CFEMStandardElementBase::GetNDOFsStatic(unsigned short VTK_Type,
-                                                       unsigned short nPoly,
-                                                       unsigned long  typeErrorMessage) {
+unsigned short CFEMStandardElementBase::GetNDOFsStatic(unsigned short VTK_Type, unsigned short nPoly,
+                                                       unsigned long typeErrorMessage) {
   unsigned short nDOFsEdge = nPoly + 1;
-  unsigned short nDOFs = 0;    // To avoid a compiler warning.
-
-  switch(VTK_Type) {
+  unsigned short nDOFs = 0;  // To avoid a compiler warning.
 
+  switch (VTK_Type) {
     case LINE:
       nDOFs = nDOFsEdge;
       break;
 
     case TRIANGLE:
-      nDOFs = nDOFsEdge*(nDOFsEdge+1)/2;
+      nDOFs = nDOFsEdge * (nDOFsEdge + 1) / 2;
       break;
 
     case QUADRILATERAL:
-      nDOFs = nDOFsEdge*nDOFsEdge;
+      nDOFs = nDOFsEdge * nDOFsEdge;
       break;
 
     case TETRAHEDRON:
-      nDOFs = nDOFsEdge*(nDOFsEdge+1)*(nDOFsEdge+2)/6;
+      nDOFs = nDOFsEdge * (nDOFsEdge + 1) * (nDOFsEdge + 2) / 6;
       break;
 
     case HEXAHEDRON:
-      nDOFs = nDOFsEdge*nDOFsEdge*nDOFsEdge;
+      nDOFs = nDOFsEdge * nDOFsEdge * nDOFsEdge;
       break;
 
     case PRISM:
-      nDOFs = nDOFsEdge*nDOFsEdge*(nDOFsEdge+1)/2;
+      nDOFs = nDOFsEdge * nDOFsEdge * (nDOFsEdge + 1) / 2;
       break;
 
     case PYRAMID:
-      nDOFs = nDOFsEdge*(nDOFsEdge+1)*(2*nDOFsEdge+1)/6;
+      nDOFs = nDOFsEdge * (nDOFsEdge + 1) * (2 * nDOFsEdge + 1) / 6;
       break;
 
     default:
       ostringstream message;
-      message << "Unknown FEM element type, " << typeErrorMessage
-              << ", encountered.";
+      message << "Unknown FEM element type, " << typeErrorMessage << ", encountered.";
       SU2_MPI::Error(message.str(), CURRENT_FUNCTION);
   }
 
   return nDOFs;
 }
 
-
-void CFEMStandardElementBase::InverseMatrix(unsigned short    n,
-                                            vector<su2double> &A) {
-
- /*--- Check the dimensions of A. ---*/
- unsigned long nEntities = n*n;
- if(A.size() != nEntities)
-   SU2_MPI::Error("Wrong size of the A matrix in InverseMatrix", CURRENT_FUNCTION);
+void CFEMStandardElementBase::InverseMatrix(unsigned short n, vector<su2double>& A) {
+  /*--- Check the dimensions of A. ---*/
+  unsigned long nEntities = n * n;
+  if (A.size() != nEntities) SU2_MPI::Error("Wrong size of the A matrix in InverseMatrix", CURRENT_FUNCTION);
 
   /*--- Create a local matrix to carry out the actual inversion. ---*/
-  vector<vector<su2double> > augmentedmatrix(n, vector<su2double>(2*n));
+  vector<vector<su2double> > augmentedmatrix(n, vector<su2double>(2 * n));
 
   /*--- Copy the data from A into the first part of augmentedmatrix. Note
         that A is stored in column major order, such that also Lapack
         routines can be used to invert the matrix.       ---*/
   unsigned int ii = 0;
-  for(unsigned short j=0; j<n; ++j)
-    for(unsigned short i=0; i<n; ++i, ++ii)
-      augmentedmatrix[i][j] = A[ii];
+  for (unsigned short j = 0; j < n; ++j)
+    for (unsigned short i = 0; i < n; ++i, ++ii) augmentedmatrix[i][j] = A[ii];
 
   /*--- Augmenting with identity matrix of similar dimensions ---*/
-  for(unsigned short j=0; j<n; ++j)
-    for(unsigned short i=0; i<n; ++i)
-      augmentedmatrix[i][j+n] = i == j ? 1 : 0;
+  for (unsigned short j = 0; j < n; ++j)
+    for (unsigned short i = 0; i < n; ++i) augmentedmatrix[i][j + n] = i == j ? 1 : 0;
 
   /*--- Outer loop of the Gauss-Jordan elimination. ---*/
-  for(unsigned short j=0; j<n; ++j) {
-
+  for (unsigned short j = 0; j < n; ++j) {
     /*--- Find the pivot in the current column. ---*/
     unsigned short jj = j;
-    su2double  valMax = fabs(augmentedmatrix[j][j]);
-    for(unsigned short i=j+1; i<n; ++i) {
+    su2double valMax = fabs(augmentedmatrix[j][j]);
+    for (unsigned short i = j + 1; i < n; ++i) {
       su2double val = fabs(augmentedmatrix[i][j]);
-      if(val > valMax){
+      if (val > valMax) {
         jj = i;
         valMax = val;
       }
     }
 
     /* Swap the rows j and jj, if needed. */
-    if(jj > j) {
-      for(unsigned short k=j; k<2*n; ++k) {
-        su2double valTmp       = augmentedmatrix[j][k];
-        augmentedmatrix[j][k]  = augmentedmatrix[jj][k];
+    if (jj > j) {
+      for (unsigned short k = j; k < 2 * n; ++k) {
+        su2double valTmp = augmentedmatrix[j][k];
+        augmentedmatrix[j][k] = augmentedmatrix[jj][k];
         augmentedmatrix[jj][k] = valTmp;
       }
     }
 
     /*--- Performing row operations to form required identity matrix out
           of the input matrix.              ---*/
-    for(unsigned short i=0; i<n; ++i) {
-      if(i != j) {
-        valMax = augmentedmatrix[i][j]/augmentedmatrix[j][j];
-        for(unsigned short k=j; k<2*n; ++k)
-          augmentedmatrix[i][k] -= valMax*augmentedmatrix[j][k];
+    for (unsigned short i = 0; i < n; ++i) {
+      if (i != j) {
+        valMax = augmentedmatrix[i][j] / augmentedmatrix[j][j];
+        for (unsigned short k = j; k < 2 * n; ++k) augmentedmatrix[i][k] -= valMax * augmentedmatrix[j][k];
       }
     }
 
-    valMax = 1.0/augmentedmatrix[j][j];
-    for(unsigned short k=j; k<2*n; ++k)
-      augmentedmatrix[j][k] *= valMax;
+    valMax = 1.0 / augmentedmatrix[j][j];
+    for (unsigned short k = j; k < 2 * n; ++k) augmentedmatrix[j][k] *= valMax;
   }
 
   /*--- Store the inverse in A. Again column major order is used. ---*/
   ii = 0;
-  for(unsigned short j=0; j<n; ++j)
-    for(unsigned short i=0; i<n; ++i, ++ii)
-      A[ii] = augmentedmatrix[i][j+n];
+  for (unsigned short j = 0; j < n; ++j)
+    for (unsigned short i = 0; i < n; ++i, ++ii) A[ii] = augmentedmatrix[i][j + n];
 }
 
-void CFEMStandardElementBase::Vandermonde1D(unsigned short          nDOFs,
-                                            const vector<su2double> &r,
-                                            vector<su2double>       &V) {
-
+void CFEMStandardElementBase::Vandermonde1D(unsigned short nDOFs, const vector<su2double>& r, vector<su2double>& V) {
   /*--- Determine the number or rows of the Vandermonde matrix and check
         if the dimension of V is correct.     ---*/
   unsigned short nRows = r.size();
-  unsigned long  nEntities = nRows*nDOFs;
-  if(V.size() != nEntities)
-    SU2_MPI::Error("Wrong size of the V matrix", CURRENT_FUNCTION);
+  unsigned long nEntities = nRows * nDOFs;
+  if (V.size() != nEntities) SU2_MPI::Error("Wrong size of the V matrix", CURRENT_FUNCTION);
 
   /*--- Compute the Vandermonde matrix. ---*/
   unsigned int ii = 0;
-  for(unsigned short i=0; i<nDOFs; ++i) {
-    for(unsigned short k=0; k<nRows; ++k, ++ii) {
+  for (unsigned short i = 0; i < nDOFs; ++i) {
+    for (unsigned short k = 0; k < nRows; ++k, ++ii) {
       V[ii] = NormJacobi(i, 0, 0, r[k]);
     }
   }
 }
 
-void CFEMStandardElementBase::GradVandermonde1D(unsigned short          nDOFs,
-                                                const vector<su2double> &r,
-                                                vector<su2double>       &VDr) {
-
+void CFEMStandardElementBase::GradVandermonde1D(unsigned short nDOFs, const vector<su2double>& r,
+                                                vector<su2double>& VDr) {
   /*--- Determine the number or rows of the gradient of the Vandermonde matrix
         and check if the dimension of VDr is correct.     ---*/
   unsigned short nRows = r.size();
-  unsigned long  nEntities = nRows*nDOFs;
-  if(VDr.size() != nEntities)
-    SU2_MPI::Error("Wrong size of the VDr matrix", CURRENT_FUNCTION);
+  unsigned long nEntities = nRows * nDOFs;
+  if (VDr.size() != nEntities) SU2_MPI::Error("Wrong size of the VDr matrix", CURRENT_FUNCTION);
 
   /*--- Compute the gradient of the Vandermonde matrix. ---*/
   unsigned int ii = 0;
-  for(unsigned short i=0; i<nDOFs; ++i) {
-    for(unsigned short k=0; k<nRows; ++k, ++ii) {
+  for (unsigned short i = 0; i < nDOFs; ++i) {
+    for (unsigned short k = 0; k < nRows; ++k, ++ii) {
       VDr[ii] = GradNormJacobi(i, 0, 0, r[k]);
     }
   }
@@ -193,87 +173,85 @@ void CFEMStandardElementBase::GradVandermonde1D(unsigned short          nDOFs,
 /*         Protected member functions of CFEMStandardElementBase.                   */
 /*----------------------------------------------------------------------------------*/
 
-CFEMStandardElementBase::CFEMStandardElementBase(unsigned short val_VTK_Type,
-                                                 unsigned short val_nPoly,
-                                                 bool           val_constJac,
-                                                 CConfig        *config,
-                                                 unsigned short val_orderExact) {
-
+CFEMStandardElementBase::CFEMStandardElementBase(unsigned short val_VTK_Type, unsigned short val_nPoly,
+                                                 bool val_constJac, CConfig* config, unsigned short val_orderExact) {
   /*--- Copy the function arguments that must be stored in the member variables. ---*/
-  VTK_Type      = val_VTK_Type;
+  VTK_Type = val_VTK_Type;
   constJacobian = val_constJac;
 
   /*--- Determine the polynomial degree that must be integrated exactly by the
         integration rule. If this degree is specified in the argument, just
         copy that value. Otherwise, determine its value. ---*/
-  if(val_orderExact > 0) {
+  if (val_orderExact > 0) {
     orderExact = val_orderExact;
-  }
-  else {
-    if( constJacobian )
-      orderExact = (unsigned short) ceil(val_nPoly*config->GetQuadrature_Factor_Straight());
+  } else {
+    if (constJacobian)
+      orderExact = (unsigned short)ceil(val_nPoly * config->GetQuadrature_Factor_Straight());
     else
-      orderExact = (unsigned short) ceil(val_nPoly*config->GetQuadrature_Factor_Curved());
+      orderExact = (unsigned short)ceil(val_nPoly * config->GetQuadrature_Factor_Curved());
   }
 
   /*--- Determine the integration points. This depends on the element type. ---*/
-  switch( VTK_Type ) {
-    case LINE:          IntegrationPointsLine();          break;
-    case TRIANGLE:      IntegrationPointsTriangle();      break;
-    case QUADRILATERAL: IntegrationPointsQuadrilateral(); break;
-    case TETRAHEDRON:   IntegrationPointsTetrahedron();   break;
-    case PYRAMID:       IntegrationPointsPyramid();       break;
-    case PRISM:         IntegrationPointsPrism();         break;
-    case HEXAHEDRON:    IntegrationPointsHexahedron();    break;
+  switch (VTK_Type) {
+    case LINE:
+      IntegrationPointsLine();
+      break;
+    case TRIANGLE:
+      IntegrationPointsTriangle();
+      break;
+    case QUADRILATERAL:
+      IntegrationPointsQuadrilateral();
+      break;
+    case TETRAHEDRON:
+      IntegrationPointsTetrahedron();
+      break;
+    case PYRAMID:
+      IntegrationPointsPyramid();
+      break;
+    case PRISM:
+      IntegrationPointsPrism();
+      break;
+    case HEXAHEDRON:
+      IntegrationPointsHexahedron();
+      break;
   }
 }
 
-void CFEMStandardElementBase::CheckSumDerivativesLagrangianBasisFunctions(
-                                          const unsigned short    nPoints,
-                                          const unsigned short    nDOFs,
-                                          const vector<su2double> &dLagBasisPoints) {
-
+void CFEMStandardElementBase::CheckSumDerivativesLagrangianBasisFunctions(const unsigned short nPoints,
+                                                                          const unsigned short nDOFs,
+                                                                          const vector<su2double>& dLagBasisPoints) {
   /*--- Check for a zero sum of the derivatives in the given points. ---*/
-  for(unsigned short j=0; j<nPoints; ++j) {
-    unsigned int jj = j*nDOFs;
-    su2double val  = 0.0;
-    for(unsigned short i=0; i<nDOFs; ++i)
-      val += dLagBasisPoints[jj+i];
+  for (unsigned short j = 0; j < nPoints; ++j) {
+    unsigned int jj = j * nDOFs;
+    su2double val = 0.0;
+    for (unsigned short i = 0; i < nDOFs; ++i) val += dLagBasisPoints[jj + i];
 
-    if(fabs(val) > 1.e-6)
-      SU2_MPI::Error("Difference is too large to be caused by roundoff", CURRENT_FUNCTION);
+    if (fabs(val) > 1.e-6) SU2_MPI::Error("Difference is too large to be caused by roundoff", CURRENT_FUNCTION);
   }
 }
 
-void CFEMStandardElementBase::CheckSumLagrangianBasisFunctions(
-                                          const unsigned short nPoints,
-                                          const unsigned short nDOFs,
-                                          vector<su2double>    &lagBasisPoints) {
-
+void CFEMStandardElementBase::CheckSumLagrangianBasisFunctions(const unsigned short nPoints, const unsigned short nDOFs,
+                                                               vector<su2double>& lagBasisPoints) {
   /*--- To reduce the error due to round off in the Lagrangian basis functions,
         make sure that the row sum is 1. Also check if the difference is not
         too large to be solely caused by roundoff.   ---*/
-  for(unsigned short j=0; j<nPoints; ++j) {
-    unsigned int jj = j*nDOFs;
-    su2double val   = 0.0;
-    for(unsigned short i=0; i<nDOFs; ++i)
-      val += lagBasisPoints[jj+i];
+  for (unsigned short j = 0; j < nPoints; ++j) {
+    unsigned int jj = j * nDOFs;
+    su2double val = 0.0;
+    for (unsigned short i = 0; i < nDOFs; ++i) val += lagBasisPoints[jj + i];
 
-    if(fabs(val-1.0) > 1.e-6)
-      SU2_MPI::Error("Difference is too large to be caused by roundoff", CURRENT_FUNCTION);
+    if (fabs(val - 1.0) > 1.e-6) SU2_MPI::Error("Difference is too large to be caused by roundoff", CURRENT_FUNCTION);
 
-    val = 1.0/val;
-    for(unsigned short i=0; i<nDOFs; ++i)
-      lagBasisPoints[jj+i] *= val;
+    val = 1.0 / val;
+    for (unsigned short i = 0; i < nDOFs; ++i) lagBasisPoints[jj + i] *= val;
   }
 }
 
-void CFEMStandardElementBase::Copy(const CFEMStandardElementBase &other) {
-
-  VTK_Type      = other.VTK_Type;
-  nIntegration  = other.nIntegration;
+void CFEMStandardElementBase::Copy(const CFEMStandardElementBase& other) {
+  VTK_Type = other.VTK_Type;
+  nIntegration = other.nIntegration;
   constJacobian = other.constJacobian;
-  orderExact    = other.orderExact;
+  orderExact = other.orderExact;
 
   rIntegration = other.rIntegration;
   sIntegration = other.sIntegration;
@@ -282,23 +260,16 @@ void CFEMStandardElementBase::Copy(const CFEMStandardElementBase &other) {
 }
 
 void CFEMStandardElementBase::DerivativesBasisFunctionsAdjacentElement(
-                                        unsigned short    VTK_TypeElem,
-                                        unsigned short    nPolyElem,
-                                        const bool        swapFaceInElement,
-                                        unsigned short    &nDOFsElem,
-                                        vector<su2double> &drLagBasisIntegration,
-                                        vector<su2double> &dsLagBasisIntegration,
-                                        vector<su2double> &dtLagBasisIntegration) {
-
+    unsigned short VTK_TypeElem, unsigned short nPolyElem, const bool swapFaceInElement, unsigned short& nDOFsElem,
+    vector<su2double>& drLagBasisIntegration, vector<su2double>& dsLagBasisIntegration,
+    vector<su2double>& dtLagBasisIntegration) {
   /*--- Define a number of dummy variables, such that the general functions
         to compute the gradients of the basis functions can be used. ---*/
   vector<su2double> rDOFsDummy, sDOFsDummy, tDOFsDummy, matVandermondeInvDummy, lagBasisPointsDummy;
 
   /*--- Determine the type of the face. ---*/
-  switch( VTK_Type ) {
-
+  switch (VTK_Type) {
     case LINE: {
-
       /*--- The face element is a line. The adjacent element can be either a
             triangle or a quadrilateral. In order to use the member functions
             LagrangianBasisFunctionAndDerivativesTriangle and
@@ -308,25 +279,17 @@ void CFEMStandardElementBase::DerivativesBasisFunctionsAdjacentElement(
             face is face 0 of standard element, which corresponds to s = -1. ---*/
       vector<su2double> sInt(nIntegration, -1.0);
 
-      switch( VTK_TypeElem ) {
+      switch (VTK_TypeElem) {
         case TRIANGLE:
-          LagrangianBasisFunctionAndDerivativesTriangle(nPolyElem,  rIntegration,
-                                                        sInt,       nDOFsElem,
-                                                        rDOFsDummy, sDOFsDummy,
-                                                        matVandermondeInvDummy,
-                                                        lagBasisPointsDummy,
-                                                        drLagBasisIntegration,
-                                                        dsLagBasisIntegration);
+          LagrangianBasisFunctionAndDerivativesTriangle(nPolyElem, rIntegration, sInt, nDOFsElem, rDOFsDummy,
+                                                        sDOFsDummy, matVandermondeInvDummy, lagBasisPointsDummy,
+                                                        drLagBasisIntegration, dsLagBasisIntegration);
           break;
 
         case QUADRILATERAL:
-          LagrangianBasisFunctionAndDerivativesQuadrilateral(nPolyElem,  rIntegration,
-                                                             sInt,       nDOFsElem,
-                                                             rDOFsDummy, sDOFsDummy,
-                                                             matVandermondeInvDummy,
-                                                             lagBasisPointsDummy,
-                                                             drLagBasisIntegration,
-                                                             dsLagBasisIntegration);
+          LagrangianBasisFunctionAndDerivativesQuadrilateral(nPolyElem, rIntegration, sInt, nDOFsElem, rDOFsDummy,
+                                                             sDOFsDummy, matVandermondeInvDummy, lagBasisPointsDummy,
+                                                             drLagBasisIntegration, dsLagBasisIntegration);
           break;
       }
 
@@ -334,7 +297,6 @@ void CFEMStandardElementBase::DerivativesBasisFunctionsAdjacentElement(
     }
 
     case TRIANGLE: {
-
       /*---- The face element is a triangle. The adjacent element can be a tetrahedron,
              a pyramid or a prism. For the tetrahedron and the prism the convention is
              that the face is face 0 of these elements, which corresponds to a
@@ -345,64 +307,46 @@ void CFEMStandardElementBase::DerivativesBasisFunctionsAdjacentElement(
              case, also the parametric coordinates of the integration points must be
              swapped in order to get the correct behavior. ---*/
 
-      switch( VTK_TypeElem ) {
-
+      switch (VTK_TypeElem) {
         case TETRAHEDRON: {
           vector<su2double> tInt(nIntegration, -1.0);
 
-          LagrangianBasisFunctionAndDerivativesTetrahedron(nPolyElem,    rIntegration,
-                                                           sIntegration, tInt,
-                                                           nDOFsElem,    rDOFsDummy,
-                                                           sDOFsDummy,   tDOFsDummy,
-                                                           matVandermondeInvDummy,
-                                                           lagBasisPointsDummy,
-                                                           drLagBasisIntegration,
-                                                           dsLagBasisIntegration,
-                                                           dtLagBasisIntegration);
+          LagrangianBasisFunctionAndDerivativesTetrahedron(nPolyElem, rIntegration, sIntegration, tInt, nDOFsElem,
+                                                           rDOFsDummy, sDOFsDummy, tDOFsDummy, matVandermondeInvDummy,
+                                                           lagBasisPointsDummy, drLagBasisIntegration,
+                                                           dsLagBasisIntegration, dtLagBasisIntegration);
           break;
         }
 
         case PRISM: {
           vector<su2double> tInt(nIntegration, -1.0);
 
-          LagrangianBasisFunctionAndDerivativesPrism(nPolyElem,    rIntegration,
-                                                     sIntegration, tInt,
-                                                     nDOFsElem,    rDOFsDummy,
-                                                     sDOFsDummy,   tDOFsDummy,
-                                                     matVandermondeInvDummy,
-                                                     lagBasisPointsDummy,
-                                                     drLagBasisIntegration,
-                                                     dsLagBasisIntegration,
+          LagrangianBasisFunctionAndDerivativesPrism(nPolyElem, rIntegration, sIntegration, tInt, nDOFsElem, rDOFsDummy,
+                                                     sDOFsDummy, tDOFsDummy, matVandermondeInvDummy,
+                                                     lagBasisPointsDummy, drLagBasisIntegration, dsLagBasisIntegration,
                                                      dtLagBasisIntegration);
           break;
         }
 
         case PYRAMID: {
           vector<su2double> rInt(nIntegration), sInt(nIntegration), tInt(nIntegration);
-          if( swapFaceInElement ) {
-            for(unsigned short i=0; i<nIntegration; ++i) {
-              rInt[i] = sIntegration[i] + 0.5*(rIntegration[i]+1.0);
-              sInt[i] = 0.5*(rIntegration[i]-1.0);
+          if (swapFaceInElement) {
+            for (unsigned short i = 0; i < nIntegration; ++i) {
+              rInt[i] = sIntegration[i] + 0.5 * (rIntegration[i] + 1.0);
+              sInt[i] = 0.5 * (rIntegration[i] - 1.0);
               tInt[i] = rIntegration[i];
             }
-          }
-          else {
-            for(unsigned short i=0; i<nIntegration; ++i) {
-              rInt[i] = rIntegration[i] + 0.5*(sIntegration[i]+1.0);
-              sInt[i] = 0.5*(sIntegration[i]-1.0);
+          } else {
+            for (unsigned short i = 0; i < nIntegration; ++i) {
+              rInt[i] = rIntegration[i] + 0.5 * (sIntegration[i] + 1.0);
+              sInt[i] = 0.5 * (sIntegration[i] - 1.0);
               tInt[i] = sIntegration[i];
             }
           }
 
-          LagrangianBasisFunctionAndDerivativesPyramid(nPolyElem,  rInt,
-                                                       sInt,       tInt,
-                                                       nDOFsElem,  rDOFsDummy,
-                                                       sDOFsDummy, tDOFsDummy,
-                                                       matVandermondeInvDummy,
-                                                       lagBasisPointsDummy,
-                                                       drLagBasisIntegration,
-                                                       dsLagBasisIntegration,
-                                                       dtLagBasisIntegration);
+          LagrangianBasisFunctionAndDerivativesPyramid(
+              nPolyElem, rInt, sInt, tInt, nDOFsElem, rDOFsDummy, sDOFsDummy, tDOFsDummy, matVandermondeInvDummy,
+              lagBasisPointsDummy, drLagBasisIntegration, dsLagBasisIntegration, dtLagBasisIntegration);
           break;
         }
       }
@@ -411,7 +355,6 @@ void CFEMStandardElementBase::DerivativesBasisFunctionsAdjacentElement(
     }
 
     case QUADRILATERAL: {
-
       /*--- The face element is a quadrilateral. The adjacent element can be a pyramid,
             a prism or a hexahedron. For the pyramid and the hexahedron the convention
             is that the face is face 0 of these elements, which corresponds to a
@@ -422,53 +365,41 @@ void CFEMStandardElementBase::DerivativesBasisFunctionsAdjacentElement(
             the desired sequence. If that is the case, also the integration points of
             the quadrilateral face must be swapped. ---*/
 
-      switch( VTK_TypeElem ) {
-
+      switch (VTK_TypeElem) {
         case HEXAHEDRON: {
           vector<su2double> tInt(nIntegration, -1.0);
 
-          LagrangianBasisFunctionAndDerivativesHexahedron(nPolyElem,    rIntegration,
-                                                          sIntegration, tInt,
-                                                          nDOFsElem,    rDOFsDummy,
-                                                          sDOFsDummy,   tDOFsDummy,
-                                                          matVandermondeInvDummy,
-                                                          lagBasisPointsDummy,
-                                                          drLagBasisIntegration,
-                                                          dsLagBasisIntegration,
-                                                          dtLagBasisIntegration);
+          LagrangianBasisFunctionAndDerivativesHexahedron(nPolyElem, rIntegration, sIntegration, tInt, nDOFsElem,
+                                                          rDOFsDummy, sDOFsDummy, tDOFsDummy, matVandermondeInvDummy,
+                                                          lagBasisPointsDummy, drLagBasisIntegration,
+                                                          dsLagBasisIntegration, dtLagBasisIntegration);
           break;
         }
 
         case PRISM: {
           vector<su2double> sInt(nIntegration, -1.0), rInt, tInt;
 
-          if( swapFaceInElement ) {rInt = sIntegration; tInt = rIntegration;}
-          else                    {rInt = rIntegration; tInt = sIntegration;}
-
-          LagrangianBasisFunctionAndDerivativesPrism(nPolyElem,  rInt,
-                                                     sInt,       tInt,
-                                                     nDOFsElem,  rDOFsDummy,
-                                                     sDOFsDummy, tDOFsDummy,
-                                                     matVandermondeInvDummy,
-                                                     lagBasisPointsDummy,
-                                                     drLagBasisIntegration,
-                                                     dsLagBasisIntegration,
-                                                     dtLagBasisIntegration);
+          if (swapFaceInElement) {
+            rInt = sIntegration;
+            tInt = rIntegration;
+          } else {
+            rInt = rIntegration;
+            tInt = sIntegration;
+          }
+
+          LagrangianBasisFunctionAndDerivativesPrism(
+              nPolyElem, rInt, sInt, tInt, nDOFsElem, rDOFsDummy, sDOFsDummy, tDOFsDummy, matVandermondeInvDummy,
+              lagBasisPointsDummy, drLagBasisIntegration, dsLagBasisIntegration, dtLagBasisIntegration);
           break;
         }
 
         case PYRAMID: {
           vector<su2double> tInt(nIntegration, -1.0);
 
-          LagrangianBasisFunctionAndDerivativesPyramid(nPolyElem,    rIntegration,
-                                                       sIntegration, tInt,
-                                                       nDOFsElem,    rDOFsDummy,
-                                                       sDOFsDummy,   tDOFsDummy,
-                                                       matVandermondeInvDummy,
-                                                       lagBasisPointsDummy,
-                                                       drLagBasisIntegration,
-                                                       dsLagBasisIntegration,
-                                                       dtLagBasisIntegration);
+          LagrangianBasisFunctionAndDerivativesPyramid(nPolyElem, rIntegration, sIntegration, tInt, nDOFsElem,
+                                                       rDOFsDummy, sDOFsDummy, tDOFsDummy, matVandermondeInvDummy,
+                                                       lagBasisPointsDummy, drLagBasisIntegration,
+                                                       dsLagBasisIntegration, dtLagBasisIntegration);
           break;
         }
       }
@@ -479,14 +410,8 @@ void CFEMStandardElementBase::DerivativesBasisFunctionsAdjacentElement(
 }
 
 void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesLine(
-                                       const unsigned short    nPoly,
-                                       const vector<su2double> &rPoints,
-                                       unsigned short          &nDOFs,
-                                       vector<su2double>       &rDOFs,
-                                       vector<su2double>       &matVandermondeInv,
-                                       vector<su2double>       &lagBasisPoints,
-                                       vector<su2double>       &drLagBasisPoints) {
-
+    const unsigned short nPoly, const vector<su2double>& rPoints, unsigned short& nDOFs, vector<su2double>& rDOFs,
+    vector<su2double>& matVandermondeInv, vector<su2double>& lagBasisPoints, vector<su2double>& drLagBasisPoints) {
   /*--- Determine the number of points in which the functions must
         be determined. ---*/
   const unsigned short nPoints = rPoints.size();
@@ -495,14 +420,13 @@ void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesLine(
   nDOFs = nPoly + 1;
   rDOFs.resize(nDOFs);
 
-  su2double dh = 2.0/nPoly;
-  for(unsigned i=0; i<nDOFs; ++i)
-    rDOFs[i] = -1.0 + i*dh;
+  su2double dh = 2.0 / nPoly;
+  for (unsigned i = 0; i < nDOFs; ++i) rDOFs[i] = -1.0 + i * dh;
 
   /*--- Compute the inverse of the Vandermonde matrix in the DOFs and
         compute the Vandermonde matrix in the given points. ---*/
-  vector<su2double> V(nDOFs*nPoints);
-  matVandermondeInv.resize(nDOFs*nDOFs);
+  vector<su2double> V(nDOFs * nPoints);
+  matVandermondeInv.resize(nDOFs * nDOFs);
 
   Vandermonde1D(nDOFs, rDOFs, matVandermondeInv);
   InverseMatrix(nDOFs, matVandermondeInv);
@@ -515,7 +439,7 @@ void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesLine(
         obtained from the matrix product V*Vinv. Note that the result is stored
         in row major order, because in this way the interpolation data for a
         point is contiguous in memory.        ---*/
-  lagBasisPoints.resize(nDOFs*nPoints);
+  lagBasisPoints.resize(nDOFs * nPoints);
   MatMulRowMajor(nDOFs, nPoints, V, matVandermondeInv, lagBasisPoints);
 
   /*--- Compute the gradients of the 1D Vandermonde matrix in the
@@ -528,48 +452,40 @@ void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesLine(
         obtained from the matrix product V*Vinv. Note that the result is stored
         in row major order, because in this way the gradient data for a point
         is contiguous in memory.  ---*/
-  drLagBasisPoints.resize(nDOFs*nPoints);
+  drLagBasisPoints.resize(nDOFs * nPoints);
   MatMulRowMajor(nDOFs, nPoints, V, matVandermondeInv, drLagBasisPoints);
 }
 
 void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesTriangle(
-                                       const unsigned short    nPoly,
-                                       const vector<su2double> &rPoints,
-                                       const vector<su2double> &sPoints,
-                                       unsigned short          &nDOFs,
-                                       vector<su2double>       &rDOFs,
-                                       vector<su2double>       &sDOFs,
-                                       vector<su2double>       &matVandermondeInv,
-                                       vector<su2double>       &lagBasisPoints,
-                                       vector<su2double>       &drLagBasisPoints,
-                                       vector<su2double>       &dsLagBasisPoints) {
-
+    const unsigned short nPoly, const vector<su2double>& rPoints, const vector<su2double>& sPoints,
+    unsigned short& nDOFs, vector<su2double>& rDOFs, vector<su2double>& sDOFs, vector<su2double>& matVandermondeInv,
+    vector<su2double>& lagBasisPoints, vector<su2double>& drLagBasisPoints, vector<su2double>& dsLagBasisPoints) {
   /*--- Determine the number of points in which the functions must
         be determined. ---*/
   const unsigned short nPoints = rPoints.size();
 
   /*--- Determine the location of the DOFs of the standard triangle. ---*/
-  nDOFs = (nPoly+1)*(nPoly+2)/2;
+  nDOFs = (nPoly + 1) * (nPoly + 2) / 2;
   rDOFs.resize(nDOFs);
   sDOFs.resize(nDOFs);
 
-  su2double dh = 2.0/nPoly;
+  su2double dh = 2.0 / nPoly;
 
   unsigned int ii = 0;
-  for(unsigned short j=0; j<=nPoly; ++j) {
-    su2double s = -1.0 + j*dh;
+  for (unsigned short j = 0; j <= nPoly; ++j) {
+    su2double s = -1.0 + j * dh;
     unsigned short uppBoundI = nPoly - j;
-    for(unsigned short i=0; i<=uppBoundI; ++i, ++ii) {
-      su2double r = -1.0 + i*dh;
-      rDOFs[ii]   = r;
-      sDOFs[ii]   = s;
+    for (unsigned short i = 0; i <= uppBoundI; ++i, ++ii) {
+      su2double r = -1.0 + i * dh;
+      rDOFs[ii] = r;
+      sDOFs[ii] = s;
     }
   }
 
   /*--- Compute the inverse of the Vandermonde matrix in the DOFs and
         compute the Vandermonde matrix in the points. ---*/
-  vector<su2double> V(nDOFs*nPoints);
-  matVandermondeInv.resize(nDOFs*nDOFs);
+  vector<su2double> V(nDOFs * nPoints);
+  matVandermondeInv.resize(nDOFs * nDOFs);
 
   Vandermonde2D_Triangle(nPoly, nDOFs, rDOFs, sDOFs, matVandermondeInv);
   InverseMatrix(nDOFs, matVandermondeInv);
@@ -581,11 +497,11 @@ void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesTriangle(
         coefficients from the DOFs to the points and are obtained from the matrix
         product V*Vinv. Note that the result is stored in row major order, because
         in this way the interpolation data for a point is contiguous in memory. ---*/
-  lagBasisPoints.resize(nDOFs*nPoints);
+  lagBasisPoints.resize(nDOFs * nPoints);
   MatMulRowMajor(nDOFs, nPoints, V, matVandermondeInv, lagBasisPoints);
 
   /*--- Compute the gradients of the 2D Vandermonde matrix in the points. ---*/
-  vector<su2double> VDr(nDOFs*nPoints), VDs(nDOFs*nPoints);
+  vector<su2double> VDr(nDOFs * nPoints), VDs(nDOFs * nPoints);
   GradVandermonde2D_Triangle(nPoly, nDOFs, rPoints, sPoints, VDr, VDs);
 
   /*--- Allocate the memory to store the derivatives in r- and s-direction of the
@@ -594,52 +510,42 @@ void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesTriangle(
         product VDr*Vinv and VDs*Vinv. Note that the result is stored in row major
         order, because in this way the gradient data for a point is contiguous
         in memory. ---*/
-  drLagBasisPoints.resize(nDOFs*nPoints);
-  dsLagBasisPoints.resize(nDOFs*nPoints);
+  drLagBasisPoints.resize(nDOFs * nPoints);
+  dsLagBasisPoints.resize(nDOFs * nPoints);
 
   MatMulRowMajor(nDOFs, nPoints, VDr, matVandermondeInv, drLagBasisPoints);
   MatMulRowMajor(nDOFs, nPoints, VDs, matVandermondeInv, dsLagBasisPoints);
 }
 
 void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesQuadrilateral(
-                                       const unsigned short    nPoly,
-                                       const vector<su2double> &rPoints,
-                                       const vector<su2double> &sPoints,
-                                       unsigned short          &nDOFs,
-                                       vector<su2double>       &rDOFs,
-                                       vector<su2double>       &sDOFs,
-                                       vector<su2double>       &matVandermondeInv,
-                                       vector<su2double>       &lagBasisPoints,
-                                       vector<su2double>       &drLagBasisPoints,
-                                       vector<su2double>       &dsLagBasisPoints) {
-
+    const unsigned short nPoly, const vector<su2double>& rPoints, const vector<su2double>& sPoints,
+    unsigned short& nDOFs, vector<su2double>& rDOFs, vector<su2double>& sDOFs, vector<su2double>& matVandermondeInv,
+    vector<su2double>& lagBasisPoints, vector<su2double>& drLagBasisPoints, vector<su2double>& dsLagBasisPoints) {
   /*--- Determine the number of points in which the functions must
         be determined. ---*/
   const unsigned short nPoints = rPoints.size();
 
   /*--- Determine the location of the DOFs of the standard quadrilateral. ---*/
-  nDOFs = (nPoly+1)*(nPoly+1);
+  nDOFs = (nPoly + 1) * (nPoly + 1);
   rDOFs.resize(nDOFs);
   sDOFs.resize(nDOFs);
 
-  su2double dh = 2.0/nPoly;
+  su2double dh = 2.0 / nPoly;
 
   unsigned int ii = 0;
-  for(unsigned short j=0; j<=nPoly; ++j)
-  {
-    su2double s = -1.0 + j*dh;
-    for(unsigned short i=0; i<=nPoly; ++i, ++ii)
-    {
-      su2double r = -1.0 + i*dh;
-      rDOFs[ii]   = r;
-      sDOFs[ii]   = s;
+  for (unsigned short j = 0; j <= nPoly; ++j) {
+    su2double s = -1.0 + j * dh;
+    for (unsigned short i = 0; i <= nPoly; ++i, ++ii) {
+      su2double r = -1.0 + i * dh;
+      rDOFs[ii] = r;
+      sDOFs[ii] = s;
     }
   }
 
   /*--- Compute the inverse of the Vandermonde matrix in the DOFs and
         compute the Vandermonde matrix in the points. ---*/
-  vector<su2double> V(nDOFs*nPoints);
-  matVandermondeInv.resize(nDOFs*nDOFs);
+  vector<su2double> V(nDOFs * nPoints);
+  matVandermondeInv.resize(nDOFs * nDOFs);
 
   Vandermonde2D_Quadrilateral(nPoly, nDOFs, rDOFs, sDOFs, matVandermondeInv);
   InverseMatrix(nDOFs, matVandermondeInv);
@@ -651,11 +557,11 @@ void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesQuadrilateral
         coefficients from the DOFs to the points and are obtained from the matrix
         product V*Vinv. Note that the result is stored in row major order, because
         in this way the interpolation data for a point is contiguous in memory. ---*/
-  lagBasisPoints.resize(nDOFs*nPoints);
+  lagBasisPoints.resize(nDOFs * nPoints);
   MatMulRowMajor(nDOFs, nPoints, V, matVandermondeInv, lagBasisPoints);
 
   /*--- Compute the gradients of the 2D Vandermonde matrix in the points. ---*/
-  vector<su2double> VDr(nDOFs*nPoints), VDs(nDOFs*nPoints);
+  vector<su2double> VDr(nDOFs * nPoints), VDs(nDOFs * nPoints);
   GradVandermonde2D_Quadrilateral(nPoly, nDOFs, rPoints, sPoints, VDr, VDs);
 
   /*--- Allocate the memory to store the derivatives in r- and s-direction of the
@@ -664,49 +570,39 @@ void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesQuadrilateral
         product VDr*Vinv and VDr*Vinv. Note that the result is stored in row major
         order, because in this way the gradient data for a point is contiguous
         in memory. ---*/
-  drLagBasisPoints.resize(nDOFs*nPoints);
-  dsLagBasisPoints.resize(nDOFs*nPoints);
+  drLagBasisPoints.resize(nDOFs * nPoints);
+  dsLagBasisPoints.resize(nDOFs * nPoints);
 
   MatMulRowMajor(nDOFs, nPoints, VDr, matVandermondeInv, drLagBasisPoints);
   MatMulRowMajor(nDOFs, nPoints, VDs, matVandermondeInv, dsLagBasisPoints);
 }
 
 void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesTetrahedron(
-                                       const unsigned short    nPoly,
-                                       const vector<su2double> &rPoints,
-                                       const vector<su2double> &sPoints,
-                                       const vector<su2double> &tPoints,
-                                       unsigned short          &nDOFs,
-                                       vector<su2double>       &rDOFs,
-                                       vector<su2double>       &sDOFs,
-                                       vector<su2double>       &tDOFs,
-                                       vector<su2double>       &matVandermondeInv,
-                                       vector<su2double>       &lagBasisPoints,
-                                       vector<su2double>       &drLagBasisPoints,
-                                       vector<su2double>       &dsLagBasisPoints,
-                                       vector<su2double>       &dtLagBasisPoints)
-{
+    const unsigned short nPoly, const vector<su2double>& rPoints, const vector<su2double>& sPoints,
+    const vector<su2double>& tPoints, unsigned short& nDOFs, vector<su2double>& rDOFs, vector<su2double>& sDOFs,
+    vector<su2double>& tDOFs, vector<su2double>& matVandermondeInv, vector<su2double>& lagBasisPoints,
+    vector<su2double>& drLagBasisPoints, vector<su2double>& dsLagBasisPoints, vector<su2double>& dtLagBasisPoints) {
   /*--- Determine the number of points in which the functions must
         be determined. ---*/
   const unsigned short nPoints = rPoints.size();
 
   /*--- Determine the location of the DOFs of the standard tetrahedron. ---*/
-  nDOFs = (nPoly+1)*(nPoly+2)*(nPoly+3)/6;
+  nDOFs = (nPoly + 1) * (nPoly + 2) * (nPoly + 3) / 6;
   rDOFs.resize(nDOFs);
   sDOFs.resize(nDOFs);
   tDOFs.resize(nDOFs);
 
-  su2double dh = 2.0/nPoly;
+  su2double dh = 2.0 / nPoly;
 
   unsigned int ii = 0;
-  for(unsigned short k=0; k<=nPoly; ++k) {
-    su2double t = -1.0 + k*dh;
+  for (unsigned short k = 0; k <= nPoly; ++k) {
+    su2double t = -1.0 + k * dh;
     unsigned short uppBoundJ = nPoly - k;
-    for(unsigned short j=0; j<=uppBoundJ; ++j) {
-      su2double s = -1.0 + j*dh;
+    for (unsigned short j = 0; j <= uppBoundJ; ++j) {
+      su2double s = -1.0 + j * dh;
       unsigned short uppBoundI = nPoly - k - j;
-      for(unsigned short i=0; i<=uppBoundI; ++i, ++ii) {
-        su2double r = -1.0 + i*dh;
+      for (unsigned short i = 0; i <= uppBoundI; ++i, ++ii) {
+        su2double r = -1.0 + i * dh;
         rDOFs[ii] = r;
         sDOFs[ii] = s;
         tDOFs[ii] = t;
@@ -716,10 +612,10 @@ void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesTetrahedron(
 
   /*--- Compute the inverse of the Vandermonde matrix in the DOFs and
         compute the Vandermonde matrix in the points. ---*/
-  vector<su2double> V(nDOFs*nPoints);
-  matVandermondeInv.resize(nDOFs*nDOFs);
+  vector<su2double> V(nDOFs * nPoints);
+  matVandermondeInv.resize(nDOFs * nDOFs);
 
-  Vandermonde3D_Tetrahedron(nPoly, nDOFs, rDOFs, sDOFs, tDOFs, matVandermondeInv );
+  Vandermonde3D_Tetrahedron(nPoly, nDOFs, rDOFs, sDOFs, tDOFs, matVandermondeInv);
   InverseMatrix(nDOFs, matVandermondeInv);
 
   Vandermonde3D_Tetrahedron(nPoly, nDOFs, rPoints, sPoints, tPoints, V);
@@ -729,13 +625,12 @@ void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesTetrahedron(
         coefficients from the DOFs to the points and are obtained from the matrix
         product V*Vinv. Note that the result is stored in row major order, because
         in this way the interpolation data for a point is contiguous in memory. ---*/
-  lagBasisPoints.resize(nDOFs*nPoints);
+  lagBasisPoints.resize(nDOFs * nPoints);
   MatMulRowMajor(nDOFs, nPoints, V, matVandermondeInv, lagBasisPoints);
 
   /*--- Compute the gradients of the 3D Vandermonde matrix in the points. ---*/
-  vector<su2double> VDr(nDOFs*nPoints), VDs(nDOFs*nPoints), VDt(nDOFs*nPoints);
-  GradVandermonde3D_Tetrahedron(nPoly, nDOFs, rPoints, sPoints,
-                                tPoints, VDr, VDs, VDt);
+  vector<su2double> VDr(nDOFs * nPoints), VDs(nDOFs * nPoints), VDt(nDOFs * nPoints);
+  GradVandermonde3D_Tetrahedron(nPoly, nDOFs, rPoints, sPoints, tPoints, VDr, VDs, VDt);
 
   /*--- Allocate the memory to store the derivatives in r-, s- and t-direction
         of the Lagrange basis functions in the points and determine them. The
@@ -743,9 +638,9 @@ void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesTetrahedron(
         from the matrix product VDr*Vinv, VDr*Vinv and VDt*Vinv. Note that the
         result is stored in row major order, because in this way the gradient
         data for a point is contiguous in memory. ---*/
-  drLagBasisPoints.resize(nDOFs*nPoints);
-  dsLagBasisPoints.resize(nDOFs*nPoints);
-  dtLagBasisPoints.resize(nDOFs*nPoints);
+  drLagBasisPoints.resize(nDOFs * nPoints);
+  dsLagBasisPoints.resize(nDOFs * nPoints);
+  dtLagBasisPoints.resize(nDOFs * nPoints);
 
   MatMulRowMajor(nDOFs, nPoints, VDr, matVandermondeInv, drLagBasisPoints);
   MatMulRowMajor(nDOFs, nPoints, VDs, matVandermondeInv, dsLagBasisPoints);
@@ -753,54 +648,43 @@ void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesTetrahedron(
 }
 
 void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesPyramid(
-                                       const unsigned short    nPoly,
-                                       const vector<su2double> &rPoints,
-                                       const vector<su2double> &sPoints,
-                                       const vector<su2double> &tPoints,
-                                       unsigned short          &nDOFs,
-                                       vector<su2double>       &rDOFs,
-                                       vector<su2double>       &sDOFs,
-                                       vector<su2double>       &tDOFs,
-                                       vector<su2double>       &matVandermondeInv,
-                                       vector<su2double>       &lagBasisPoints,
-                                       vector<su2double>       &drLagBasisPoints,
-                                       vector<su2double>       &dsLagBasisPoints,
-                                       vector<su2double>       &dtLagBasisPoints)
-{
+    const unsigned short nPoly, const vector<su2double>& rPoints, const vector<su2double>& sPoints,
+    const vector<su2double>& tPoints, unsigned short& nDOFs, vector<su2double>& rDOFs, vector<su2double>& sDOFs,
+    vector<su2double>& tDOFs, vector<su2double>& matVandermondeInv, vector<su2double>& lagBasisPoints,
+    vector<su2double>& drLagBasisPoints, vector<su2double>& dsLagBasisPoints, vector<su2double>& dtLagBasisPoints) {
   /*--- Determine the number of points in which the functions must
         be determined. ---*/
   const unsigned short nPoints = rPoints.size();
 
   /*--- Allocate the memory for the DOFs of the standard pyramid. ---*/
-  unsigned short nDOFsEdge = nPoly+1;
-  nDOFs = nDOFsEdge*(nDOFsEdge+1)*(2*nDOFsEdge+1)/6;
+  unsigned short nDOFsEdge = nPoly + 1;
+  nDOFs = nDOFsEdge * (nDOFsEdge + 1) * (2 * nDOFsEdge + 1) / 6;
   rDOFs.resize(nDOFs);
   sDOFs.resize(nDOFs);
   tDOFs.resize(nDOFs);
 
   /*--- Determine the location of the DOFs of the standard pyramid.
         The outer loop is in the k-direction, which is from base to top. ---*/
-  su2double dt         = 2.0/nPoly;
+  su2double dt = 2.0 / nPoly;
   unsigned short mPoly = nPoly;
-  unsigned int   ii = 0;
-
-  for(unsigned short k=0; k<=nPoly; ++k, --mPoly) {
+  unsigned int ii = 0;
 
+  for (unsigned short k = 0; k <= nPoly; ++k, --mPoly) {
     /*--- Determine the minimum and maximum value for r and s for this t-value. ---*/
-    su2double t     = -1.0 + k*dt;
-    su2double rsMin =  0.5*(t-1.0);
+    su2double t = -1.0 + k * dt;
+    su2double rsMin = 0.5 * (t - 1.0);
     su2double rsMax = -rsMin;
 
     /*--- Determine the step size along the edges of the current quad.
           Take the exceptional situation mPoly == 0 into account to avoid a
           division by zero.     ---*/
-    su2double dh = mPoly ? (rsMax-rsMin)/mPoly : su2double(0.0);
+    su2double dh = mPoly ? (rsMax - rsMin) / mPoly : su2double(0.0);
 
     /*--- Loop over the vertices of the current quadrilateral. ---*/
-    for(unsigned short j=0; j<=mPoly; ++j) {
-      su2double s = rsMin + j*dh;
-      for(unsigned short i=0; i<=mPoly; ++i, ++ii) {
-        su2double r = rsMin + i*dh;
+    for (unsigned short j = 0; j <= mPoly; ++j) {
+      su2double s = rsMin + j * dh;
+      for (unsigned short i = 0; i <= mPoly; ++i, ++ii) {
+        su2double r = rsMin + i * dh;
         rDOFs[ii] = r;
         sDOFs[ii] = s;
         tDOFs[ii] = t;
@@ -810,8 +694,8 @@ void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesPyramid(
 
   /*--- Compute the inverse of the Vandermonde matrix in the DOFs and
         compute the Vandermonde matrix in the points. ---*/
-  vector<su2double> V(nDOFs*nPoints);
-  matVandermondeInv.resize(nDOFs*nDOFs);
+  vector<su2double> V(nDOFs * nPoints);
+  matVandermondeInv.resize(nDOFs * nDOFs);
 
   Vandermonde3D_Pyramid(nPoly, nDOFs, rDOFs, sDOFs, tDOFs, matVandermondeInv);
   InverseMatrix(nDOFs, matVandermondeInv);
@@ -823,11 +707,11 @@ void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesPyramid(
         coefficients from the DOFs to the points and are obtained from the matrix
         product V*Vinv. Note that the result is stored in row major order, because
         in this way the interpolation data for a point is contiguous in memory.  ---*/
-  lagBasisPoints.resize(nDOFs*nPoints);
+  lagBasisPoints.resize(nDOFs * nPoints);
   MatMulRowMajor(nDOFs, nPoints, V, matVandermondeInv, lagBasisPoints);
 
   /*--- Compute the gradients of the 3D Vandermonde matrix in the points. ---*/
-  vector<su2double> VDr(nDOFs*nPoints), VDs(nDOFs*nPoints), VDt(nDOFs*nPoints);
+  vector<su2double> VDr(nDOFs * nPoints), VDs(nDOFs * nPoints), VDt(nDOFs * nPoints);
   GradVandermonde3D_Pyramid(nPoly, nDOFs, rPoints, sPoints, tPoints, VDr, VDs, VDt);
 
   /*--- Allocate the memory to store the derivatives in r-, s- and t-direction
@@ -836,9 +720,9 @@ void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesPyramid(
         from the matrix product VDr*Vinv, VDr*Vinv and VDt*Vinv. Note that the
         result is stored in row major order, because in this way the gradient
         data for a point is contiguous in memory. ---*/
-  drLagBasisPoints.resize(nDOFs*nPoints);
-  dsLagBasisPoints.resize(nDOFs*nPoints);
-  dtLagBasisPoints.resize(nDOFs*nPoints);
+  drLagBasisPoints.resize(nDOFs * nPoints);
+  dsLagBasisPoints.resize(nDOFs * nPoints);
+  dtLagBasisPoints.resize(nDOFs * nPoints);
 
   MatMulRowMajor(nDOFs, nPoints, VDr, matVandermondeInv, drLagBasisPoints);
   MatMulRowMajor(nDOFs, nPoints, VDs, matVandermondeInv, dsLagBasisPoints);
@@ -846,43 +730,33 @@ void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesPyramid(
 }
 
 void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesPrism(
-                                       const unsigned short    nPoly,
-                                       const vector<su2double> &rPoints,
-                                       const vector<su2double> &sPoints,
-                                       const vector<su2double> &tPoints,
-                                       unsigned short          &nDOFs,
-                                       vector<su2double>       &rDOFs,
-                                       vector<su2double>       &sDOFs,
-                                       vector<su2double>       &tDOFs,
-                                       vector<su2double>       &matVandermondeInv,
-                                       vector<su2double>       &lagBasisPoints,
-                                       vector<su2double>       &drLagBasisPoints,
-                                       vector<su2double>       &dsLagBasisPoints,
-                                       vector<su2double>       &dtLagBasisPoints)
-{
+    const unsigned short nPoly, const vector<su2double>& rPoints, const vector<su2double>& sPoints,
+    const vector<su2double>& tPoints, unsigned short& nDOFs, vector<su2double>& rDOFs, vector<su2double>& sDOFs,
+    vector<su2double>& tDOFs, vector<su2double>& matVandermondeInv, vector<su2double>& lagBasisPoints,
+    vector<su2double>& drLagBasisPoints, vector<su2double>& dsLagBasisPoints, vector<su2double>& dtLagBasisPoints) {
   /*--- Determine the number of points in which the functions must
         be determined. ---*/
   const unsigned short nPoints = rPoints.size();
 
   /*--- Allocate the memory for the DOFs of the standard prism
         and determine its locations. ---*/
-  unsigned short nDOFsEdge = nPoly+1;
-  nDOFs = nDOFsEdge*nDOFsEdge*(nDOFsEdge+1)/2;
+  unsigned short nDOFsEdge = nPoly + 1;
+  nDOFs = nDOFsEdge * nDOFsEdge * (nDOFsEdge + 1) / 2;
   rDOFs.resize(nDOFs);
   sDOFs.resize(nDOFs);
   tDOFs.resize(nDOFs);
 
-  su2double dh = 2.0/nPoly;
+  su2double dh = 2.0 / nPoly;
 
   unsigned short ii = 0;
-  for(unsigned short k=0; k<=nPoly; ++k) {
-    const su2double t = -1.0 + k*dh;
+  for (unsigned short k = 0; k <= nPoly; ++k) {
+    const su2double t = -1.0 + k * dh;
 
-    for(unsigned short j=0; j<=nPoly; ++j) {
-      su2double s = -1.0 + j*dh;
+    for (unsigned short j = 0; j <= nPoly; ++j) {
+      su2double s = -1.0 + j * dh;
       unsigned short uppBoundI = nPoly - j;
-      for(unsigned short i=0; i<=uppBoundI; ++i, ++ii) {
-        su2double r = -1.0 + i*dh;
+      for (unsigned short i = 0; i <= uppBoundI; ++i, ++ii) {
+        su2double r = -1.0 + i * dh;
         rDOFs[ii] = r;
         sDOFs[ii] = s;
         tDOFs[ii] = t;
@@ -892,8 +766,8 @@ void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesPrism(
 
   /*--- Compute the inverse of the Vandermonde matrix in the DOFs and
         compute the Vandermonde matrix in the points. ---*/
-  vector<su2double> V(nDOFs*nPoints);
-  matVandermondeInv.resize(nDOFs*nDOFs);
+  vector<su2double> V(nDOFs * nPoints);
+  matVandermondeInv.resize(nDOFs * nDOFs);
 
   Vandermonde3D_Prism(nPoly, nDOFs, rDOFs, sDOFs, tDOFs, matVandermondeInv);
   InverseMatrix(nDOFs, matVandermondeInv);
@@ -905,12 +779,12 @@ void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesPrism(
         coefficients from the DOFs to the points and are obtained from the matrix
         product V*Vinv. Note that the result is stored in row major order, because
         in this way the interpolation data for a point is contiguous in memory.  ---*/
-  lagBasisPoints.resize(nDOFs*nPoints);
+  lagBasisPoints.resize(nDOFs * nPoints);
   MatMulRowMajor(nDOFs, nPoints, V, matVandermondeInv, lagBasisPoints);
 
   /*--- Compute the gradients of the 3D Vandermonde matrix in the points. ---*/
-  vector<su2double> VDr(nDOFs*nPoints), VDs(nDOFs*nPoints), VDt(nDOFs*nPoints);
-  GradVandermonde3D_Prism(nPoly, nDOFs,rPoints, sPoints, tPoints, VDr, VDs, VDt);
+  vector<su2double> VDr(nDOFs * nPoints), VDs(nDOFs * nPoints), VDt(nDOFs * nPoints);
+  GradVandermonde3D_Prism(nPoly, nDOFs, rPoints, sPoints, tPoints, VDr, VDs, VDt);
 
   /*--- Allocate the memory to store the derivatives in r-, s- and t-direction
         of the Lagrange basis functions in the points and determine them. The
@@ -918,9 +792,9 @@ void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesPrism(
         from the matrix product VDr*Vinv, VDr*Vinv and VDt*Vinv. Note that the
         the result is stored in row major order, because in this way the gradient
         data for a point is contiguous in memory. ---*/
-  drLagBasisPoints.resize(nDOFs*nPoints);
-  dsLagBasisPoints.resize(nDOFs*nPoints);
-  dtLagBasisPoints.resize(nDOFs*nPoints);
+  drLagBasisPoints.resize(nDOFs * nPoints);
+  dsLagBasisPoints.resize(nDOFs * nPoints);
+  dtLagBasisPoints.resize(nDOFs * nPoints);
 
   MatMulRowMajor(nDOFs, nPoints, VDr, matVandermondeInv, drLagBasisPoints);
   MatMulRowMajor(nDOFs, nPoints, VDs, matVandermondeInv, dsLagBasisPoints);
@@ -928,41 +802,31 @@ void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesPrism(
 }
 
 void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesHexahedron(
-                                       const unsigned short    nPoly,
-                                       const vector<su2double> &rPoints,
-                                       const vector<su2double> &sPoints,
-                                       const vector<su2double> &tPoints,
-                                       unsigned short          &nDOFs,
-                                       vector<su2double>       &rDOFs,
-                                       vector<su2double>       &sDOFs,
-                                       vector<su2double>       &tDOFs,
-                                       vector<su2double>       &matVandermondeInv,
-                                       vector<su2double>       &lagBasisPoints,
-                                       vector<su2double>       &drLagBasisPoints,
-                                       vector<su2double>       &dsLagBasisPoints,
-                                       vector<su2double>       &dtLagBasisPoints)
-{
+    const unsigned short nPoly, const vector<su2double>& rPoints, const vector<su2double>& sPoints,
+    const vector<su2double>& tPoints, unsigned short& nDOFs, vector<su2double>& rDOFs, vector<su2double>& sDOFs,
+    vector<su2double>& tDOFs, vector<su2double>& matVandermondeInv, vector<su2double>& lagBasisPoints,
+    vector<su2double>& drLagBasisPoints, vector<su2double>& dsLagBasisPoints, vector<su2double>& dtLagBasisPoints) {
   /*--- Determine the number of points in which the functions must
         be determined. ---*/
   const unsigned short nPoints = rPoints.size();
 
   /*--- Allocate the memory for the DOFs of the standard hexahedron
         and determine its locations. ---*/
-  unsigned short nDOFsEdge = nPoly+1;
-  nDOFs = nDOFsEdge*nDOFsEdge*nDOFsEdge;
+  unsigned short nDOFsEdge = nPoly + 1;
+  nDOFs = nDOFsEdge * nDOFsEdge * nDOFsEdge;
   rDOFs.resize(nDOFs);
   sDOFs.resize(nDOFs);
   tDOFs.resize(nDOFs);
 
-  su2double dh = 2.0/nPoly;
+  su2double dh = 2.0 / nPoly;
 
   unsigned short ii = 0;
-  for(unsigned short k=0; k<=nPoly; ++k) {
-    su2double t = -1.0 + k*dh;
-    for(unsigned short j=0; j<=nPoly; ++j) {
-      su2double s = -1.0 + j*dh;
-      for(unsigned short i=0; i<=nPoly; ++i, ++ii) {
-        su2double r = -1.0 + i*dh;
+  for (unsigned short k = 0; k <= nPoly; ++k) {
+    su2double t = -1.0 + k * dh;
+    for (unsigned short j = 0; j <= nPoly; ++j) {
+      su2double s = -1.0 + j * dh;
+      for (unsigned short i = 0; i <= nPoly; ++i, ++ii) {
+        su2double r = -1.0 + i * dh;
         rDOFs[ii] = r;
         sDOFs[ii] = s;
         tDOFs[ii] = t;
@@ -972,8 +836,8 @@ void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesHexahedron(
 
   /*--- Compute the inverse of the Vandermonde matrix in the DOFs and
         compute the Vandermonde matrix in the points. ---*/
-  vector<su2double> V(nDOFs*nPoints);
-  matVandermondeInv.resize(nDOFs*nDOFs);
+  vector<su2double> V(nDOFs * nPoints);
+  matVandermondeInv.resize(nDOFs * nDOFs);
 
   Vandermonde3D_Hexahedron(nPoly, nDOFs, rDOFs, sDOFs, tDOFs, matVandermondeInv);
   InverseMatrix(nDOFs, matVandermondeInv);
@@ -985,11 +849,11 @@ void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesHexahedron(
         coefficients from the DOFs to the points and are obtained from the matrix
         product V*Vinv. Note that the result is stored in row major order, because
         in this way the interpolation data for a point is contiguous in memory.  ---*/
-  lagBasisPoints.resize(nDOFs*nPoints);
+  lagBasisPoints.resize(nDOFs * nPoints);
   MatMulRowMajor(nDOFs, nPoints, V, matVandermondeInv, lagBasisPoints);
 
   /*--- Compute the gradients of the 3D Vandermonde matrix in the points. ---*/
-  vector<su2double> VDr(nDOFs*nPoints), VDs(nDOFs*nPoints), VDt(nDOFs*nPoints);
+  vector<su2double> VDr(nDOFs * nPoints), VDs(nDOFs * nPoints), VDt(nDOFs * nPoints);
   GradVandermonde3D_Hexahedron(nPoly, nDOFs, rPoints, sPoints, tPoints, VDr, VDs, VDt);
 
   /*--- Allocate the memory to store the derivatives in r-, s- and t-direction
@@ -998,97 +862,88 @@ void CFEMStandardElementBase::LagrangianBasisFunctionAndDerivativesHexahedron(
         from the matrix product VDr*Vinv, VDr*Vinv and VDt*Vinv. Note that the
         the result is stored in row major order, because in this way the gradient
         data for a point is contiguous in memory. ---*/
-  drLagBasisPoints.resize(nDOFs*nPoints);
-  dsLagBasisPoints.resize(nDOFs*nPoints);
-  dtLagBasisPoints.resize(nDOFs*nPoints);
+  drLagBasisPoints.resize(nDOFs * nPoints);
+  dsLagBasisPoints.resize(nDOFs * nPoints);
+  dtLagBasisPoints.resize(nDOFs * nPoints);
 
   MatMulRowMajor(nDOFs, nPoints, VDr, matVandermondeInv, drLagBasisPoints);
   MatMulRowMajor(nDOFs, nPoints, VDs, matVandermondeInv, dsLagBasisPoints);
   MatMulRowMajor(nDOFs, nPoints, VDt, matVandermondeInv, dtLagBasisPoints);
 }
 
-void CFEMStandardElementBase::MatMulRowMajor(const unsigned short nDOFs,
-                                             const unsigned short nPoints,
-                                             const vector<su2double> &A,
-                                             const vector<su2double> &B,
-                                             vector<su2double>       &C) {
-
+void CFEMStandardElementBase::MatMulRowMajor(const unsigned short nDOFs, const unsigned short nPoints,
+                                             const vector<su2double>& A, const vector<su2double>& B,
+                                             vector<su2double>& C) {
   /*--- Check if the dimensions of the matrices correspond to the
         assumptions made in this function.                    ---*/
-  const unsigned int dimA = nDOFs*nPoints;
-  const unsigned int dimB = nDOFs*nDOFs;
+  const unsigned int dimA = nDOFs * nPoints;
+  const unsigned int dimB = nDOFs * nDOFs;
 
-  if(A.size() != dimA || B.size() != dimB || C.size() != dimA)
+  if (A.size() != dimA || B.size() != dimB || C.size() != dimA)
     SU2_MPI::Error("Unexpected size of the matrices", CURRENT_FUNCTION);
 
   /*--- Carry out the actual matrix matrix multiplication and store the result
         in row major order (the matrices A and B are in column major order).  ---*/
-  for(unsigned short j=0; j<nDOFs; ++j) {
-    for(unsigned short i=0; i<nPoints; ++i) {
-      const unsigned int ii = i*nDOFs + j;
+  for (unsigned short j = 0; j < nDOFs; ++j) {
+    for (unsigned short i = 0; i < nPoints; ++i) {
+      const unsigned int ii = i * nDOFs + j;
       C[ii] = 0.0;
 
-      for(unsigned short k=0; k<nDOFs; ++k) {
-        const unsigned int indA = k*nPoints + i;
-        const unsigned int indB = j*nDOFs + k;
+      for (unsigned short k = 0; k < nDOFs; ++k) {
+        const unsigned int indA = k * nPoints + i;
+        const unsigned int indB = j * nDOFs + k;
 
-        C[ii] += A[indA]*B[indB];
+        C[ii] += A[indA] * B[indB];
       }
     }
   }
 }
 
-void CFEMStandardElementBase::SubConnForPlottingLine(
-                                         const unsigned short   nPoly,
-                                         vector<unsigned short> &subConn) {
-
+void CFEMStandardElementBase::SubConnForPlottingLine(const unsigned short nPoly, vector<unsigned short>& subConn) {
   /*--- Determine the local subconnectivity of the line element used for plotting
         purposes. This is rather trivial, because the line element is subdivided
         into nPoly linear line elements.                    ---*/
-  unsigned short nnPoly = max(nPoly,(unsigned short) 1);
-  for(unsigned short i=0; i<nnPoly; ++i) {
+  unsigned short nnPoly = max(nPoly, (unsigned short)1);
+  for (unsigned short i = 0; i < nnPoly; ++i) {
     subConn.push_back(i);
-    subConn.push_back(i+1);
+    subConn.push_back(i + 1);
   }
 }
 
-void CFEMStandardElementBase::SubConnForPlottingQuadrilateral(
-                                         const unsigned short   nPoly,
-                                         vector<unsigned short> &subConn) {
-
+void CFEMStandardElementBase::SubConnForPlottingQuadrilateral(const unsigned short nPoly,
+                                                              vector<unsigned short>& subConn) {
   /*--- Determine the local subconnectivity of the quadrilateral element used for
         plotting purposes. Note that the connectivity of the linear subelements
         obey the VTK connectivity rule of a quadrilateral, which is different
         from the connectivity for the high order quadrilateral. ---*/
-  unsigned short nnPoly = max(nPoly,(unsigned short) 1);
-  for(unsigned short j=0; j<nnPoly; ++j) {
-    unsigned short jj = j*(nnPoly+1);
-    for(unsigned short i=0; i<nnPoly; ++i) {
-      const unsigned short n0 = jj + i;        subConn.push_back(n0);
-      const unsigned short n1 = n0 + 1;        subConn.push_back(n1);
-      const unsigned short n2 = n1 + nPoly+1;  subConn.push_back(n2);
-      const unsigned short n3 = n2 - 1;        subConn.push_back(n3);
+  unsigned short nnPoly = max(nPoly, (unsigned short)1);
+  for (unsigned short j = 0; j < nnPoly; ++j) {
+    unsigned short jj = j * (nnPoly + 1);
+    for (unsigned short i = 0; i < nnPoly; ++i) {
+      const unsigned short n0 = jj + i;
+      subConn.push_back(n0);
+      const unsigned short n1 = n0 + 1;
+      subConn.push_back(n1);
+      const unsigned short n2 = n1 + nPoly + 1;
+      subConn.push_back(n2);
+      const unsigned short n3 = n2 - 1;
+      subConn.push_back(n3);
     }
   }
 }
 
-void CFEMStandardElementBase::SubConnForPlottingTriangle(
-                                         const unsigned short   nPoly,
-                                         vector<unsigned short> &subConn) {
-
+void CFEMStandardElementBase::SubConnForPlottingTriangle(const unsigned short nPoly, vector<unsigned short>& subConn) {
   /*--- Determine the local subconnectivity of the triangular element used for
         plotting purposes. ---*/
   unsigned short jj = 0;
 
   /*--- Loop over subedges of the left boundary of the standard triangle. ---*/
-  for(unsigned short j=0; j<nPoly; ++j) {
-
+  for (unsigned short j = 0; j < nPoly; ++j) {
     /*--- Check if the "down" elements must be written. ---*/
-    if( j ) {
+    if (j) {
+      unsigned short kk = jj - (nPoly + 1 - j);  // Offset of the relevant DOF on the previous row.
 
-      unsigned short kk = jj - (nPoly + 1 - j); // Offset of the relevant DOF on the previous row.
-
-      for(unsigned short i=0; i<(nPoly-j); ++i) {
+      for (unsigned short i = 0; i < (nPoly - j); ++i) {
         unsigned short n0 = jj + i;
         unsigned short n1 = kk + i;
         unsigned short n2 = n0 + 1;
@@ -1103,7 +958,7 @@ void CFEMStandardElementBase::SubConnForPlottingTriangle(
           Determine the offset of the DOF on the next row. ---*/
     unsigned short kk = jj + (nPoly + 1 - j);
 
-    for(unsigned short i=0; i<(nPoly-j); ++i) {
+    for (unsigned short i = 0; i < (nPoly - j); ++i) {
       unsigned short n0 = jj + i;
       unsigned short n1 = n0 + 1;
       unsigned short n2 = kk + i;
@@ -1118,141 +973,125 @@ void CFEMStandardElementBase::SubConnForPlottingTriangle(
   }
 }
 
-
-void CFEMStandardElementBase::Vandermonde2D_Triangle(unsigned short          nPoly,
-                                                     unsigned short          nDOFs,
-                                                     const vector<su2double> &r,
-                                                     const vector<su2double> &s,
-                                                     vector<su2double>       &V) {
-
+void CFEMStandardElementBase::Vandermonde2D_Triangle(unsigned short nPoly, unsigned short nDOFs,
+                                                     const vector<su2double>& r, const vector<su2double>& s,
+                                                     vector<su2double>& V) {
   /*--- Determine the number or rows of the Vandermonde matrix and check
         if the dimension of V is correct.     ---*/
   unsigned short nRows = r.size();
-  unsigned long  nEntities = nRows*nDOFs;
-  if(V.size() != nEntities)
-    SU2_MPI::Error("Wrong size of the V matrix", CURRENT_FUNCTION);
+  unsigned long nEntities = nRows * nDOFs;
+  if (V.size() != nEntities) SU2_MPI::Error("Wrong size of the V matrix", CURRENT_FUNCTION);
 
   /*--- For a triangle the orthogonal basis for the reference element is obtained
         by a combination of a Jacobi polynomial and a Legendre polynomial. This
         is the result of the orthonormalization of the monomial basis. ---*/
   unsigned int ii = 0;
-  for(unsigned short i=0; i<=nPoly; ++i) {
-    for(unsigned short j=0; j<=(nPoly-i); ++j) {
-      for(unsigned short k=0; k<nRows; ++k, ++ii) {
-
+  for (unsigned short i = 0; i <= nPoly; ++i) {
+    for (unsigned short j = 0; j <= (nPoly - i); ++j) {
+      for (unsigned short k = 0; k < nRows; ++k, ++ii) {
         /*--- Determine the coefficients a and b. ---*/
         su2double a;
-        if(fabs(s[k]-1.0) < 1.e-8) a = -1.0;
-        else a = 2.0*(1.0+r[k])/(1.0-s[k]) - 1.0;
+        if (fabs(s[k] - 1.0) < 1.e-8)
+          a = -1.0;
+        else
+          a = 2.0 * (1.0 + r[k]) / (1.0 - s[k]) - 1.0;
 
         su2double b = s[k];
 
         /*--- Determine the value of the current basis function in this point. ---*/
         su2double tmp = 1.0;
-        if( i ) tmp = pow((1.0-b),i);
-        V[ii] = sqrt(2.0)*tmp*NormJacobi(i,0,0,a)*NormJacobi(j,2*i+1,0,b);
+        if (i) tmp = pow((1.0 - b), i);
+        V[ii] = sqrt(2.0) * tmp * NormJacobi(i, 0, 0, a) * NormJacobi(j, 2 * i + 1, 0, b);
       }
     }
   }
 }
 
-void CFEMStandardElementBase::GradVandermonde2D_Triangle(unsigned short          nPoly,
-                                                         unsigned short          nDOFs,
-                                                         const vector<su2double> &r,
-                                                         const vector<su2double> &s,
-                                                         vector<su2double>       &VDr,
-                                                         vector<su2double>       &VDs) {
-
+void CFEMStandardElementBase::GradVandermonde2D_Triangle(unsigned short nPoly, unsigned short nDOFs,
+                                                         const vector<su2double>& r, const vector<su2double>& s,
+                                                         vector<su2double>& VDr, vector<su2double>& VDs) {
   /*--- Determine the number or rows of the gradient of the Vandermonde matrix
         and check if the dimensions of VDr and VDs are correct.     ---*/
   unsigned short nRows = r.size();
-  unsigned long  nEntities = nRows*nDOFs;
-  if(VDr.size() != nEntities || VDs.size() != nEntities)
+  unsigned long nEntities = nRows * nDOFs;
+  if (VDr.size() != nEntities || VDs.size() != nEntities)
     SU2_MPI::Error("Wrong size of the VDr and/or VDs matrices", CURRENT_FUNCTION);
 
   /*--- For a triangle the orthogonal basis for the reference element is obtained
         by a combination of a Jacobi polynomial and a Legendre polynomial. This
         is the result of the orthonormalization of the monomial basis. ---*/
   unsigned int ii = 0;
-  for(unsigned short i=0; i<=nPoly; ++i) {
-    for(unsigned short j=0; j<=(nPoly-i); ++j) {
-      for(unsigned k=0; k<nRows; ++k, ++ii) {
-
+  for (unsigned short i = 0; i <= nPoly; ++i) {
+    for (unsigned short j = 0; j <= (nPoly - i); ++j) {
+      for (unsigned k = 0; k < nRows; ++k, ++ii) {
         /*--- Determine the coefficients a and b. ---*/
         su2double a;
-        if(fabs(s[k]-1.0) < 1.e-8) a = -1.0;
-        else a = 2.0*(1.0+r[k])/(1.0-s[k]) - 1.0;
+        if (fabs(s[k] - 1.0) < 1.e-8)
+          a = -1.0;
+        else
+          a = 2.0 * (1.0 + r[k]) / (1.0 - s[k]) - 1.0;
 
         su2double b = s[k];
 
         /*--- Determine the value of the two 1D contributions to the 2D
               basis functions as well as the gradients of these basis
               functions w.r.t. to their arguments. ---*/
-        su2double fa  = NormJacobi(i,0,    0,a);
-        su2double gb  = NormJacobi(j,2*i+1,0,b);
-        su2double dfa = GradNormJacobi(i,0,    0,a);
-        su2double dgb = GradNormJacobi(j,2*i+1,0,b);
+        su2double fa = NormJacobi(i, 0, 0, a);
+        su2double gb = NormJacobi(j, 2 * i + 1, 0, b);
+        su2double dfa = GradNormJacobi(i, 0, 0, a);
+        su2double dgb = GradNormJacobi(j, 2 * i + 1, 0, b);
 
         /*--- Determine the gradients of the basis functions w.r.t. the
               coordinates r and s. The product rule must be used in order
               to change the derivative of a to the derivative of r and s. ---*/
-        VDr[ii] = sqrt(2.0)*dfa*gb;
+        VDr[ii] = sqrt(2.0) * dfa * gb;
         VDs[ii] = VDr[ii];
-        if(i > 0)
-        {
+        if (i > 0) {
           su2double tmp = 1.0;
-          if( i-1 ) tmp = pow((1.0-b), (i-1));
+          if (i - 1) tmp = pow((1.0 - b), (i - 1));
 
-          VDr[ii] = 2.0*tmp*VDr[ii];
-          VDs[ii] = (a+1.0)*tmp*VDs[ii] - i*tmp*sqrt(2.0)*fa*gb;
+          VDr[ii] = 2.0 * tmp * VDr[ii];
+          VDs[ii] = (a + 1.0) * tmp * VDs[ii] - i * tmp * sqrt(2.0) * fa * gb;
         }
 
         su2double tmp = 1.0;
-        if( i ) tmp = pow((1.0-b), i);
-        VDs[ii] += sqrt(2.0)*fa*dgb*tmp;
+        if (i) tmp = pow((1.0 - b), i);
+        VDs[ii] += sqrt(2.0) * fa * dgb * tmp;
       }
     }
   }
 }
 
-void CFEMStandardElementBase::Vandermonde2D_Quadrilateral(unsigned short          nPoly,
-                                                          unsigned short          nDOFs,
-                                                          const vector<su2double> &r,
-                                                          const vector<su2double> &s,
-                                                          vector<su2double>       &V) {
-
+void CFEMStandardElementBase::Vandermonde2D_Quadrilateral(unsigned short nPoly, unsigned short nDOFs,
+                                                          const vector<su2double>& r, const vector<su2double>& s,
+                                                          vector<su2double>& V) {
   /*--- Determine the number or rows of the Vandermonde matrix and check
         if the dimension of V is correct.     ---*/
   unsigned short nRows = r.size();
-  unsigned long  nEntities = nRows*nDOFs;
-  if(V.size() != nEntities)
-    SU2_MPI::Error("Wrong size of the V matrix", CURRENT_FUNCTION);
+  unsigned long nEntities = nRows * nDOFs;
+  if (V.size() != nEntities) SU2_MPI::Error("Wrong size of the V matrix", CURRENT_FUNCTION);
 
   /*--- For a quadrilateral the basis functions are the product of the 1D
         basis functions, which are the normalized Legendre polynomials.
         The Legendre polynomials are implemented via Jacobi polynomials. ---*/
   unsigned int ii = 0;
-  for(unsigned short i=0; i<=nPoly; ++i) {
-    for(unsigned short j=0; j<=nPoly; ++j) {
-      for(unsigned short k=0; k<nRows; ++k, ++ii) {
-        V[ii] = NormJacobi(i,0,0,r[k])*NormJacobi(j,0,0,s[k]);
+  for (unsigned short i = 0; i <= nPoly; ++i) {
+    for (unsigned short j = 0; j <= nPoly; ++j) {
+      for (unsigned short k = 0; k < nRows; ++k, ++ii) {
+        V[ii] = NormJacobi(i, 0, 0, r[k]) * NormJacobi(j, 0, 0, s[k]);
       }
     }
   }
 }
 
-void CFEMStandardElementBase::GradVandermonde2D_Quadrilateral(unsigned short          nPoly,
-                                                              unsigned short          nDOFs,
-                                                              const vector<su2double> &r,
-                                                              const vector<su2double> &s,
-                                                              vector<su2double>       &VDr,
-                                                              vector<su2double>       &VDs) {
-
+void CFEMStandardElementBase::GradVandermonde2D_Quadrilateral(unsigned short nPoly, unsigned short nDOFs,
+                                                              const vector<su2double>& r, const vector<su2double>& s,
+                                                              vector<su2double>& VDr, vector<su2double>& VDs) {
   /*--- Determine the number or rows of the gradient of the Vandermonde matrix
         and check if the dimensions of VDr and VDs are correct.     ---*/
   unsigned short nRows = r.size();
-  unsigned long  nEntities = nRows*nDOFs;
-  if(VDr.size() != nEntities || VDs.size() != nEntities)
+  unsigned long nEntities = nRows * nDOFs;
+  if (VDr.size() != nEntities || VDs.size() != nEntities)
     SU2_MPI::Error("Wrong size of the VDr and/or VDs matrices", CURRENT_FUNCTION);
 
   /*--- For a quadrilateral the basis functions are the product of the 1D
@@ -1260,80 +1099,73 @@ void CFEMStandardElementBase::GradVandermonde2D_Quadrilateral(unsigned short
         The Legendre polynomials are implemented via Jacobi polynomials.
         Hence the derivatives in r- and s-direction can be computed easily. ---*/
   unsigned int ii = 0;
-  for(unsigned short i=0; i<=nPoly; ++i) {
-    for(unsigned short j=0; j<=nPoly; ++j) {
-      for(unsigned short k=0; k<nRows; ++k, ++ii) {
-        VDr[ii] = GradNormJacobi(i,0,0,r[k])*NormJacobi(j,0,0,s[k]);
-        VDs[ii] = GradNormJacobi(j,0,0,s[k])*NormJacobi(i,0,0,r[k]);
+  for (unsigned short i = 0; i <= nPoly; ++i) {
+    for (unsigned short j = 0; j <= nPoly; ++j) {
+      for (unsigned short k = 0; k < nRows; ++k, ++ii) {
+        VDr[ii] = GradNormJacobi(i, 0, 0, r[k]) * NormJacobi(j, 0, 0, s[k]);
+        VDs[ii] = GradNormJacobi(j, 0, 0, s[k]) * NormJacobi(i, 0, 0, r[k]);
       }
     }
   }
 }
 
-void CFEMStandardElementBase::Vandermonde3D_Tetrahedron(unsigned short          nPoly,
-                                                        unsigned short          nDOFs,
-                                                        const vector<su2double> &r,
-                                                        const vector<su2double> &s,
-                                                        const vector<su2double> &t,
-                                                        vector<su2double>       &V) {
-
+void CFEMStandardElementBase::Vandermonde3D_Tetrahedron(unsigned short nPoly, unsigned short nDOFs,
+                                                        const vector<su2double>& r, const vector<su2double>& s,
+                                                        const vector<su2double>& t, vector<su2double>& V) {
   /*--- Determine the number or rows of the Vandermonde matrix and check
         if the dimension of V is correct.     ---*/
   unsigned short nRows = r.size();
-  unsigned long  nEntities = nRows*nDOFs;
-  if(V.size() != nEntities)
-    SU2_MPI::Error("Wrong size of the V matrix", CURRENT_FUNCTION);
+  unsigned long nEntities = nRows * nDOFs;
+  if (V.size() != nEntities) SU2_MPI::Error("Wrong size of the V matrix", CURRENT_FUNCTION);
 
   /*--- For a tetrahedron the orthogonal basis for the reference element is obtained by a
         combination of Jacobi polynomials (of which the Legendre polynomials is a special
         case). This is the result of the orthonormalization of the monomial basis. ---*/
   unsigned int ii = 0;
-  for(unsigned short i=0; i<=nPoly; ++i) {
-    for(unsigned short j=0; j<=(nPoly-i); ++j) {
-      for(unsigned short k=0; k<=(nPoly-i-j); ++k) {
-        for(unsigned short l=0; l<nRows; ++l, ++ii) {
-
+  for (unsigned short i = 0; i <= nPoly; ++i) {
+    for (unsigned short j = 0; j <= (nPoly - i); ++j) {
+      for (unsigned short k = 0; k <= (nPoly - i - j); ++k) {
+        for (unsigned short l = 0; l < nRows; ++l, ++ii) {
           /*--- Determine the coefficients a, b and c. ---*/
           su2double a, b;
           su2double tmp = s[l] + t[l];
-          if(fabs(tmp) < 1.e-8) a = -1.0;
-          else                  a = -1.0 - 2.0*(1.0+r[l])/tmp;
+          if (fabs(tmp) < 1.e-8)
+            a = -1.0;
+          else
+            a = -1.0 - 2.0 * (1.0 + r[l]) / tmp;
 
           tmp = 1.0 - t[l];
-          if(fabs(tmp) < 1.e-8) b = -1.0;
-          else                  b = -1.0 + 2.0*(1.0+s[l])/tmp;
+          if (fabs(tmp) < 1.e-8)
+            b = -1.0;
+          else
+            b = -1.0 + 2.0 * (1.0 + s[l]) / tmp;
 
           su2double c = t[l];
 
           /*--- Determine the value of the current basis function in this point. ---*/
           su2double tmpb = 1.0;
-          if( i )   tmpb = pow((1.0-b),i);
+          if (i) tmpb = pow((1.0 - b), i);
 
           su2double tmpc = 1.0;
-          if( i+j ) tmpc = pow((1.0-c),i+j);
+          if (i + j) tmpc = pow((1.0 - c), i + j);
 
-          V[ii] = sqrt(8.0)*tmpb*tmpc*NormJacobi(i,0,0,a)*NormJacobi(j,2*i+1,0,b)
-                * NormJacobi(k,2*(i+j+1),0,c);
+          V[ii] = sqrt(8.0) * tmpb * tmpc * NormJacobi(i, 0, 0, a) * NormJacobi(j, 2 * i + 1, 0, b) *
+                  NormJacobi(k, 2 * (i + j + 1), 0, c);
         }
       }
     }
   }
 }
 
-void CFEMStandardElementBase::GradVandermonde3D_Tetrahedron(unsigned short          nPoly,
-                                                            unsigned short          nDOFs,
-                                                            const vector<su2double> &r,
-                                                            const vector<su2double> &s,
-                                                            const vector<su2double> &t,
-                                                            vector<su2double>       &VDr,
-                                                            vector<su2double>       &VDs,
-                                                            vector<su2double>       &VDt) {
-
+void CFEMStandardElementBase::GradVandermonde3D_Tetrahedron(unsigned short nPoly, unsigned short nDOFs,
+                                                            const vector<su2double>& r, const vector<su2double>& s,
+                                                            const vector<su2double>& t, vector<su2double>& VDr,
+                                                            vector<su2double>& VDs, vector<su2double>& VDt) {
   /*--- Determine the number or rows of the gradient of the Vandermonde matrix
         and check if the dimensions of VDr, VDs and VDt are correct.     ---*/
   unsigned short nRows = r.size();
-  unsigned long  nEntities = nRows*nDOFs;
-  if(VDr.size() != nEntities || VDs.size() != nEntities || VDt.size() != nEntities)
+  unsigned long nEntities = nRows * nDOFs;
+  if (VDr.size() != nEntities || VDs.size() != nEntities || VDt.size() != nEntities)
     SU2_MPI::Error("Wrong size of the VDr, VDs and VDt matrices", CURRENT_FUNCTION);
 
   /*--- For a tetrahedron the orthogonal basis for the reference element is obtained by a
@@ -1342,43 +1174,46 @@ void CFEMStandardElementBase::GradVandermonde3D_Tetrahedron(unsigned short
         Note that the sequence of the i, j and k loop must be identical to
         the evaluation of the Vandermonde matrix itself.                ---*/
   unsigned int ii = 0;
-  for(unsigned short i=0; i<=nPoly; ++i) {
-    for(unsigned short j=0; j<=(nPoly-i); ++j) {
-      for(unsigned short k=0; k<=(nPoly-i-j); ++k) {
-        for(unsigned short l=0; l<nRows; ++l, ++ii) {
-
+  for (unsigned short i = 0; i <= nPoly; ++i) {
+    for (unsigned short j = 0; j <= (nPoly - i); ++j) {
+      for (unsigned short k = 0; k <= (nPoly - i - j); ++k) {
+        for (unsigned short l = 0; l < nRows; ++l, ++ii) {
           /*--- Determine the coefficients a, b and c. */
           su2double a, b;
           su2double tmp = s[l] + t[l];
-          if(fabs(tmp) < 1.e-8) a = -1.0;
-          else                  a = -1.0 - 2.0*(1.0+r[l])/tmp;
+          if (fabs(tmp) < 1.e-8)
+            a = -1.0;
+          else
+            a = -1.0 - 2.0 * (1.0 + r[l]) / tmp;
 
           tmp = 1.0 - t[l];
-          if(fabs(tmp) < 1.e-8) b = -1.0;
-          else                  b = -1.0 + 2.0*(1.0+s[l])/tmp;
+          if (fabs(tmp) < 1.e-8)
+            b = -1.0;
+          else
+            b = -1.0 + 2.0 * (1.0 + s[l]) / tmp;
 
           su2double c = t[l];
 
           /*--- Determine the value of the three 1D contributions to the 3D basis functions as
                 well as the gradients of these basis functions w.r.t. to their arguments. ---*/
-          su2double fa  = NormJacobi(i,0,    0,a);
-          su2double gb  = NormJacobi(j,2*i+1,0,b);
-          su2double hc  = NormJacobi(k,2*(i+j+1),0,c);
-          su2double dfa = GradNormJacobi(i,0,    0,a);
-          su2double dgb = GradNormJacobi(j,2*i+1,0,b);
-          su2double dhc = GradNormJacobi(k,2*(i+j+1),0,c);
+          su2double fa = NormJacobi(i, 0, 0, a);
+          su2double gb = NormJacobi(j, 2 * i + 1, 0, b);
+          su2double hc = NormJacobi(k, 2 * (i + j + 1), 0, c);
+          su2double dfa = GradNormJacobi(i, 0, 0, a);
+          su2double dgb = GradNormJacobi(j, 2 * i + 1, 0, b);
+          su2double dhc = GradNormJacobi(k, 2 * (i + j + 1), 0, c);
 
           /*--- Compute the derivative of the basis function w.r.t. r. As r is only present in
                 the parameter a the derivative of the basis function w.r.t. a is multiplied by
                 dadr. Note that the implementation is such that all possible singularities are
                 divided out of the expression.                                  ---*/
-          VDr[ii] = sqrt(8.0)*dfa*gb*hc;
-          if(i > 0) {
+          VDr[ii] = sqrt(8.0) * dfa * gb * hc;
+          if (i > 0) {
             VDr[ii] *= 4.0;
-            if(i > 1 ) VDr[ii] *= pow((1.0-b), (i-1));
+            if (i > 1) VDr[ii] *= pow((1.0 - b), (i - 1));
           }
 
-          if(i+j > 1) VDr[ii] *= pow((1.0-c), (i+j-1));
+          if (i + j > 1) VDr[ii] *= pow((1.0 - c), (i + j - 1));
 
           /*--- Compute the derivative of the basis function w.r.t. s. As s is present in both
                 the parameters a and b, both variables must be taken into account when the
@@ -1387,24 +1222,24 @@ void CFEMStandardElementBase::GradVandermonde3D_Tetrahedron(unsigned short
                 of the basis function w.r.t. b multiplied by dbds. This value is stored, because
                 it is needed later on to compute the derivative w.r.t. t.       ---*/
           VDs[ii] = dgb;
-          if( i ) VDs[ii] *= pow((1.0-b), i);
+          if (i) VDs[ii] *= pow((1.0 - b), i);
 
-          if(i > 0) {
-            tmp = i*gb;
-            if(i > 1) tmp *= pow((1.0-b), (i-1));
+          if (i > 0) {
+            tmp = i * gb;
+            if (i > 1) tmp *= pow((1.0 - b), (i - 1));
             VDs[ii] -= tmp;
           }
 
-          if(i+j > 0) {
-            VDs[ii] *= 2.0*sqrt(8.0)*fa*hc;
-            if(i+j > 1) VDs[ii] *= pow((1.0-c), (i+j-1));
+          if (i + j > 0) {
+            VDs[ii] *= 2.0 * sqrt(8.0) * fa * hc;
+            if (i + j > 1) VDs[ii] *= pow((1.0 - c), (i + j - 1));
           }
 
           su2double dPsidbXdbds = VDs[ii];
 
           /*--- Add the contribution from the derivative of the basis function
                 w.r.t. a multiplied by dads.           ---*/
-          VDs[ii] += 0.5*(a+1.0)*VDr[ii];
+          VDs[ii] += 0.5 * (a + 1.0) * VDr[ii];
 
           /*--- Compute the derivative of the basis function w.r.t. t. As t is present in a, b and c,
                 all parameters must be taken into account when the derivative is computed. Note that
@@ -1412,60 +1247,55 @@ void CFEMStandardElementBase::GradVandermonde3D_Tetrahedron(unsigned short
                 expression. The first part is the derivative of the basis function w.r.t. c,
                 which is equal to t.                                     ---*/
           VDt[ii] = dhc;
-          if(i+j > 0) {
-            VDt[ii] *= pow((1.0-c), (i+j));
+          if (i + j > 0) {
+            VDt[ii] *= pow((1.0 - c), (i + j));
 
-            tmp = (i+j)*hc;
-            if(i+j > 1) tmp *= pow((1.0-c), (i+j-1));
+            tmp = (i + j) * hc;
+            if (i + j > 1) tmp *= pow((1.0 - c), (i + j - 1));
 
             VDt[ii] -= tmp;
           }
 
-          VDt[ii] *= sqrt(8.0)*fa*gb;
-          if( i) VDt[ii] *= pow((1.0-b), i);
+          VDt[ii] *= sqrt(8.0) * fa * gb;
+          if (i) VDt[ii] *= pow((1.0 - b), i);
 
           /*--- Add the contribution from the derivative of the basis function w.r.t. a multiplied
                 by dadt and the derivative w.r.t. b multiplied by dbdt.           ---*/
-          VDt[ii] += 0.5*(a+1.0)*VDr[ii] + 0.5*(b+1.0)*dPsidbXdbds;
+          VDt[ii] += 0.5 * (a + 1.0) * VDr[ii] + 0.5 * (b + 1.0) * dPsidbXdbds;
         }
       }
     }
   }
 }
 
-void CFEMStandardElementBase::Vandermonde3D_Pyramid(unsigned short          nPoly,
-                                                    unsigned short          nDOFs,
-                                                    const vector<su2double> &r,
-                                                    const vector<su2double> &s,
-                                                    const vector<su2double> &t,
-                                                    vector<su2double>       &V) {
-
+void CFEMStandardElementBase::Vandermonde3D_Pyramid(unsigned short nPoly, unsigned short nDOFs,
+                                                    const vector<su2double>& r, const vector<su2double>& s,
+                                                    const vector<su2double>& t, vector<su2double>& V) {
   /*--- Determine the number or rows of the Vandermonde matrix and check
         if the dimension of V is correct.     ---*/
   unsigned short nRows = r.size();
-  unsigned long  nEntities = nRows*nDOFs;
-  if(V.size() != nEntities)
-    SU2_MPI::Error("Wrong size of the V matrix", CURRENT_FUNCTION);
+  unsigned long nEntities = nRows * nDOFs;
+  if (V.size() != nEntities) SU2_MPI::Error("Wrong size of the V matrix", CURRENT_FUNCTION);
 
   /*--- For a pyramid the orthogonal basis for the reference element is
         obtained by a combination of Jacobi polynomials (of which the Legendre
         polynomials is a special case). This is the result of the
         orthonormalization of the monomial basis. ---*/
   unsigned int ii = 0;
-  for(unsigned short i=0; i<=nPoly; ++i) {
-    for(unsigned short j=0; j<=nPoly; ++j) {
-      unsigned short muij = max(i,j);
-      const su2double scaleFact = pow(2,muij+1);
-      for(unsigned short k=0; k<=(nPoly-muij); ++k) {
-        for(unsigned short l=0; l<nRows; ++l, ++ii) {
-
+  for (unsigned short i = 0; i <= nPoly; ++i) {
+    for (unsigned short j = 0; j <= nPoly; ++j) {
+      unsigned short muij = max(i, j);
+      const su2double scaleFact = pow(2, muij + 1);
+      for (unsigned short k = 0; k <= (nPoly - muij); ++k) {
+        for (unsigned short l = 0; l < nRows; ++l, ++ii) {
           /*--- Determine the coefficients a, b and c. ---*/
           su2double a, b;
-          su2double tmp = 0.5*(1.0-t[l]);
-          if(fabs(tmp) < 1.e-8) a = b = 0.0;
+          su2double tmp = 0.5 * (1.0 - t[l]);
+          if (fabs(tmp) < 1.e-8)
+            a = b = 0.0;
           else {
-            a = r[l]/tmp;
-            b = s[l]/tmp;
+            a = r[l] / tmp;
+            b = s[l] / tmp;
           }
 
           su2double c = t[l];
@@ -1475,30 +1305,25 @@ void CFEMStandardElementBase::Vandermonde3D_Pyramid(unsigned short          nPol
                 formulation is derived in literature for a t coordinate between
                 0 and 1, while in this code t varies between -1 and 1. ---*/
           su2double tmpt = 1.0;
-          if( muij ) tmpt = pow(tmp,muij);
+          if (muij) tmpt = pow(tmp, muij);
 
-          V[ii] = scaleFact*tmpt*NormJacobi(i,0,0,a)*NormJacobi(j,0,0,b)
-                * NormJacobi(k,2*(muij+1),0,c);
+          V[ii] =
+              scaleFact * tmpt * NormJacobi(i, 0, 0, a) * NormJacobi(j, 0, 0, b) * NormJacobi(k, 2 * (muij + 1), 0, c);
         }
       }
     }
   }
 }
 
-void CFEMStandardElementBase::GradVandermonde3D_Pyramid(unsigned short          nPoly,
-                                                        unsigned short          nDOFs,
-                                                        const vector<su2double> &r,
-                                                        const vector<su2double> &s,
-                                                        const vector<su2double> &t,
-                                                        vector<su2double>       &VDr,
-                                                        vector<su2double>       &VDs,
-                                                        vector<su2double>       &VDt) {
-
+void CFEMStandardElementBase::GradVandermonde3D_Pyramid(unsigned short nPoly, unsigned short nDOFs,
+                                                        const vector<su2double>& r, const vector<su2double>& s,
+                                                        const vector<su2double>& t, vector<su2double>& VDr,
+                                                        vector<su2double>& VDs, vector<su2double>& VDt) {
   /*--- Determine the number or rows of the gradient of the Vandermonde matrix
         and check if the dimensions of VDr, VDs and VDt are correct.     ---*/
   unsigned short nRows = r.size();
-  unsigned long  nEntities = nRows*nDOFs;
-  if(VDr.size() != nEntities || VDs.size() != nEntities || VDt.size() != nEntities)
+  unsigned long nEntities = nRows * nDOFs;
+  if (VDr.size() != nEntities || VDs.size() != nEntities || VDt.size() != nEntities)
     SU2_MPI::Error("Wrong size of the VDr, VDs and VDt matrices", CURRENT_FUNCTION);
 
   /*--- For a pyramid the orthogonal basis for the reference element is
@@ -1508,20 +1333,20 @@ void CFEMStandardElementBase::GradVandermonde3D_Pyramid(unsigned short
         Note that the sequence of the i, j and k loop must be identical to
         the evaluation of the Vandermonde matrix itself.  ---*/
   unsigned int ii = 0;
-  for(unsigned short i=0; i<=nPoly; ++i) {
-    for(unsigned short j=0; j<=nPoly; ++j) {
-      unsigned short muij = max(i,j);
-      const su2double scaleFact = pow(2,muij+1);
-      for(unsigned short k=0; k<=(nPoly-muij); ++k) {
-        for(unsigned short l=0; l<nRows; ++l, ++ii) {
-
+  for (unsigned short i = 0; i <= nPoly; ++i) {
+    for (unsigned short j = 0; j <= nPoly; ++j) {
+      unsigned short muij = max(i, j);
+      const su2double scaleFact = pow(2, muij + 1);
+      for (unsigned short k = 0; k <= (nPoly - muij); ++k) {
+        for (unsigned short l = 0; l < nRows; ++l, ++ii) {
           /*--- Determine the coefficients a, b and c. ---*/
           su2double a, b;
-          su2double tmp = 0.5*(1.0-t[l]);
-          if(fabs(tmp) < 1.e-8) a = b = 0.0;
+          su2double tmp = 0.5 * (1.0 - t[l]);
+          if (fabs(tmp) < 1.e-8)
+            a = b = 0.0;
           else {
-            a = r[l]/tmp;
-            b = s[l]/tmp;
+            a = r[l] / tmp;
+            b = s[l] / tmp;
           }
 
           su2double c = t[l];
@@ -1529,12 +1354,12 @@ void CFEMStandardElementBase::GradVandermonde3D_Pyramid(unsigned short
           /*--- Determine the value of the three 1D contributions to the 3D
                 basis functions as well as the gradients of these basis
                 functions w.r.t. to their arguments. ---*/
-          su2double fa  = NormJacobi(i,0,         0,a);
-          su2double gb  = NormJacobi(j,0,         0,b);
-          su2double hc  = NormJacobi(k,2*(muij+1),0,c);
-          su2double dfa = GradNormJacobi(i,0,         0,a);
-          su2double dgb = GradNormJacobi(j,0,         0,b);
-          su2double dhc = GradNormJacobi(k,2*(muij+1),0,c);
+          su2double fa = NormJacobi(i, 0, 0, a);
+          su2double gb = NormJacobi(j, 0, 0, b);
+          su2double hc = NormJacobi(k, 2 * (muij + 1), 0, c);
+          su2double dfa = GradNormJacobi(i, 0, 0, a);
+          su2double dgb = GradNormJacobi(j, 0, 0, b);
+          su2double dhc = GradNormJacobi(k, 2 * (muij + 1), 0, c);
 
           /*--- Compute the derivative of the basis function w.r.t. r and s.
                 As r is only present in the parameter a the derivative of
@@ -1542,11 +1367,10 @@ void CFEMStandardElementBase::GradVandermonde3D_Pyramid(unsigned short
                 argument holds for s, which is only present in the parameter b.
                 Note that the implementation is such that all possible
                 singularities are divided out of the expression.  ---*/
-          VDr[ii] = dfa*gb*hc;
-          VDs[ii] = fa*dgb*hc;
-          if(muij > 1)
-          {
-            su2double tmpt = pow(tmp, (muij-1));
+          VDr[ii] = dfa * gb * hc;
+          VDs[ii] = fa * dgb * hc;
+          if (muij > 1) {
+            su2double tmpt = pow(tmp, (muij - 1));
             VDr[ii] *= tmpt;
             VDs[ii] *= tmpt;
           }
@@ -1559,20 +1383,20 @@ void CFEMStandardElementBase::GradVandermonde3D_Pyramid(unsigned short
                 The first part is the derivative of the basis function w.r.t. c,
                 which is equal to t.       --*/
           VDt[ii] = dhc;
-          if(muij > 0) VDt[ii] *= pow(tmp, muij);
+          if (muij > 0) VDt[ii] *= pow(tmp, muij);
 
-          if(muij > 0) {
-            su2double tmpt = 0.5*muij*hc;
-            if(muij > 1) tmpt *= pow(tmp, (muij-1));
+          if (muij > 0) {
+            su2double tmpt = 0.5 * muij * hc;
+            if (muij > 1) tmpt *= pow(tmp, (muij - 1));
             VDt[ii] -= tmpt;
           }
 
-          VDt[ii] *= fa*gb;
+          VDt[ii] *= fa * gb;
 
           /*--- Add the contribution from the derivative of the basis function
                 w.r.t. a multiplied by dadt and the derivative w.r.t. b multiplied
                 by dbdt.                      ---*/
-          VDt[ii] += 0.5*a*VDr[ii] + 0.5*b*VDs[ii];
+          VDt[ii] += 0.5 * a * VDr[ii] + 0.5 * b * VDs[ii];
 
           /*--- Multiply the three derivatives with the scale factor to
                 obtain the correct answers. See Vandermonde3D_Pyramid for
@@ -1586,19 +1410,14 @@ void CFEMStandardElementBase::GradVandermonde3D_Pyramid(unsigned short
   }
 }
 
-void CFEMStandardElementBase::Vandermonde3D_Prism(unsigned short          nPoly,
-                                                  unsigned short          nDOFs,
-                                                  const vector<su2double> &r,
-                                                  const vector<su2double> &s,
-                                                  const vector<su2double> &t,
-                                                  vector<su2double>       &V) {
-
+void CFEMStandardElementBase::Vandermonde3D_Prism(unsigned short nPoly, unsigned short nDOFs,
+                                                  const vector<su2double>& r, const vector<su2double>& s,
+                                                  const vector<su2double>& t, vector<su2double>& V) {
   /*--- Determine the number or rows of the Vandermonde matrix and check
         if the dimension of V is correct.     ---*/
   unsigned short nRows = r.size();
-  unsigned long  nEntities = nRows*nDOFs;
-  if(V.size() != nEntities)
-    SU2_MPI::Error("Wrong size of the V matrix", CURRENT_FUNCTION);
+  unsigned long nEntities = nRows * nDOFs;
+  if (V.size() != nEntities) SU2_MPI::Error("Wrong size of the V matrix", CURRENT_FUNCTION);
 
   /*--- For a prism the orthogonal basis for the reference element is a tensor
         product of the 1D basis functions in the structured direction of the prism
@@ -1607,44 +1426,39 @@ void CFEMStandardElementBase::Vandermonde3D_Prism(unsigned short          nPoly,
         polynomial. This is the result of the orthonormalization of the
         monomial basis.                   ---*/
   unsigned int ii = 0;
-  for(unsigned short i=0; i<=nPoly; ++i) {
-    for(unsigned short j=0; j<=(nPoly-i); ++j) {
-      for(unsigned short k=0; k<=nPoly; ++k) {
-        for(unsigned short l=0; l<nRows; ++l, ++ii) {
-
+  for (unsigned short i = 0; i <= nPoly; ++i) {
+    for (unsigned short j = 0; j <= (nPoly - i); ++j) {
+      for (unsigned short k = 0; k <= nPoly; ++k) {
+        for (unsigned short l = 0; l < nRows; ++l, ++ii) {
           /*--- Determine the coefficients a and b. ---*/
           su2double a;
-          if(fabs(s[l]-1.0) < 1.e-8) a = -1.0;
-          else a = 2.0*(1.0+r[l])/(1.0-s[l]) - 1.0;
+          if (fabs(s[l] - 1.0) < 1.e-8)
+            a = -1.0;
+          else
+            a = 2.0 * (1.0 + r[l]) / (1.0 - s[l]) - 1.0;
 
           su2double b = s[l];
 
           /*--- Determine the value of the current basis function in this point. ---*/
           su2double tmp = 1.0;
-          if( i ) tmp = pow((1.0-b),i);
+          if (i) tmp = pow((1.0 - b), i);
 
-          V[ii] = sqrt(2.0)*tmp*NormJacobi(i,0,0,a)*NormJacobi(j,2*i+1,0,b)
-                * NormJacobi(k,0,0,t[l]);
+          V[ii] = sqrt(2.0) * tmp * NormJacobi(i, 0, 0, a) * NormJacobi(j, 2 * i + 1, 0, b) * NormJacobi(k, 0, 0, t[l]);
         }
       }
     }
   }
 }
 
-void CFEMStandardElementBase::GradVandermonde3D_Prism(unsigned short          nPoly,
-                                                      unsigned short          nDOFs,
-                                                      const vector<su2double> &r,
-                                                      const vector<su2double> &s,
-                                                      const vector<su2double> &t,
-                                                      vector<su2double>       &VDr,
-                                                      vector<su2double>       &VDs,
-                                                      vector<su2double>       &VDt) {
-
+void CFEMStandardElementBase::GradVandermonde3D_Prism(unsigned short nPoly, unsigned short nDOFs,
+                                                      const vector<su2double>& r, const vector<su2double>& s,
+                                                      const vector<su2double>& t, vector<su2double>& VDr,
+                                                      vector<su2double>& VDs, vector<su2double>& VDt) {
   /*--- Determine the number or rows of the gradient of the Vandermonde matrix
         and check if the dimensions of VDr, VDs and VDt are correct.     ---*/
   unsigned short nRows = r.size();
-  unsigned long  nEntities = nRows*nDOFs;
-  if(VDr.size() != nEntities || VDs.size() != nEntities || VDt.size() != nEntities)
+  unsigned long nEntities = nRows * nDOFs;
+  if (VDr.size() != nEntities || VDs.size() != nEntities || VDt.size() != nEntities)
     SU2_MPI::Error("Wrong size of the VDr, VDs and VDt matrices", CURRENT_FUNCTION);
 
   /*--- For a prism the orthogonal basis for the reference element is a tensor
@@ -1654,103 +1468,92 @@ void CFEMStandardElementBase::GradVandermonde3D_Prism(unsigned short          nP
         Note that the sequence of the i, j and k loop must be identical to
         the evaluation of the Vandermonde matrix itself.          ---*/
   unsigned int ii = 0;
-  for(unsigned short i=0; i<=nPoly; ++i) {
-    for(unsigned short j=0; j<=(nPoly-i); ++j) {
-      for(unsigned short k=0; k<=nPoly; ++k) {
-        for(unsigned short l=0; l<nRows; ++l, ++ii) {
-
+  for (unsigned short i = 0; i <= nPoly; ++i) {
+    for (unsigned short j = 0; j <= (nPoly - i); ++j) {
+      for (unsigned short k = 0; k <= nPoly; ++k) {
+        for (unsigned short l = 0; l < nRows; ++l, ++ii) {
           /*--- Determine the coefficients a and b. ---*/
           su2double a;
-          if(fabs(s[l]-1.0) < 1.e-8) a = -1.0;
-          else a = 2.0*(1.0+r[l])/(1.0-s[l]) - 1.0;
+          if (fabs(s[l] - 1.0) < 1.e-8)
+            a = -1.0;
+          else
+            a = 2.0 * (1.0 + r[l]) / (1.0 - s[l]) - 1.0;
 
           su2double b = s[l];
 
           /*--- Determine the value of the two 1D contributions to the 2D
                 basis functions of the triangle as well as the gradients of
                 these basis functions w.r.t. to its argument. ---*/
-          su2double fa  = NormJacobi(i,0,    0,a);
-          su2double gb  = NormJacobi(j,2*i+1,0,b);
-          su2double dfa = GradNormJacobi(i,0,    0,a);
-          su2double dgb = GradNormJacobi(j,2*i+1,0,b);
+          su2double fa = NormJacobi(i, 0, 0, a);
+          su2double gb = NormJacobi(j, 2 * i + 1, 0, b);
+          su2double dfa = GradNormJacobi(i, 0, 0, a);
+          su2double dgb = GradNormJacobi(j, 2 * i + 1, 0, b);
 
           /*--- Determine the gradients of the basis functions w.r.t. the
                 coordinates r and s. The product rule must be used in order
                 to change the derivative of a to the derivative of r and s. ---*/
-          VDr[ii] = sqrt(2.0)*dfa*gb;
+          VDr[ii] = sqrt(2.0) * dfa * gb;
           VDs[ii] = VDr[ii];
-          if(i > 0)
-          {
+          if (i > 0) {
             su2double tmp = 1.0;
-            if(i > 1) tmp = pow((1.0-b), (i-1));
+            if (i > 1) tmp = pow((1.0 - b), (i - 1));
 
-            VDr[ii] = 2.0*tmp*VDr[ii];
-            VDs[ii] = (a+1.0)*tmp*VDs[ii] - i*tmp*sqrt(2.0)*fa*gb;
+            VDr[ii] = 2.0 * tmp * VDr[ii];
+            VDs[ii] = (a + 1.0) * tmp * VDs[ii] - i * tmp * sqrt(2.0) * fa * gb;
           }
 
           su2double tmp = 1.0;
-          if(i > 0) tmp = pow((1.0-b), i);
+          if (i > 0) tmp = pow((1.0 - b), i);
 
-          VDs[ii] += sqrt(2.0)*fa*dgb*tmp;
+          VDs[ii] += sqrt(2.0) * fa * dgb * tmp;
 
           /*--- Multiply VDr and VDs with the contribution from the structured
                 direction of the prism.                 ---*/
-          VDr[ii] *= NormJacobi(k,0,0,t[l]);
-          VDs[ii] *= NormJacobi(k,0,0,t[l]);
+          VDr[ii] *= NormJacobi(k, 0, 0, t[l]);
+          VDs[ii] *= NormJacobi(k, 0, 0, t[l]);
 
           /*--- Compute the derivative of the basis function in the t-direction,
                 which is the structured direction.             ---*/
-          VDt[ii] = sqrt(2.0)*tmp*fa*gb*GradNormJacobi(k,0,0,t[l]);
+          VDt[ii] = sqrt(2.0) * tmp * fa * gb * GradNormJacobi(k, 0, 0, t[l]);
         }
       }
     }
   }
 }
 
-void CFEMStandardElementBase::Vandermonde3D_Hexahedron(unsigned short          nPoly,
-                                                       unsigned short          nDOFs,
-                                                       const vector<su2double> &r,
-                                                       const vector<su2double> &s,
-                                                       const vector<su2double> &t,
-                                                       vector<su2double>       &V) {
-
+void CFEMStandardElementBase::Vandermonde3D_Hexahedron(unsigned short nPoly, unsigned short nDOFs,
+                                                       const vector<su2double>& r, const vector<su2double>& s,
+                                                       const vector<su2double>& t, vector<su2double>& V) {
   /*--- Determine the number or rows of the Vandermonde matrix and check
         if the dimension of V is correct.     ---*/
   unsigned short nRows = r.size();
-  unsigned long  nEntities = nRows*nDOFs;
-  if(V.size() != nEntities)
-    SU2_MPI::Error("Wrong size of the V matrix", CURRENT_FUNCTION);
+  unsigned long nEntities = nRows * nDOFs;
+  if (V.size() != nEntities) SU2_MPI::Error("Wrong size of the V matrix", CURRENT_FUNCTION);
 
   /*--- For a hexahedron the basis functions are the tensor product of the 1D
         basis functions, which are the normalized Legendre polynomials. Note
         that the Legendre polynomials are a special kind of Jacobi polynomials. ---*/
   unsigned int ii = 0;
-  for(unsigned short i=0; i<=nPoly; ++i) {
-    for(unsigned short j=0; j<=nPoly; ++j) {
-      for(unsigned short k=0; k<=nPoly; ++k) {
-        for(unsigned short l=0; l<nRows; ++l, ++ii) {
-          V[ii] = NormJacobi(i,0,0,r[l])*NormJacobi(j,0,0,s[l])
-                * NormJacobi(k,0,0,t[l]);
+  for (unsigned short i = 0; i <= nPoly; ++i) {
+    for (unsigned short j = 0; j <= nPoly; ++j) {
+      for (unsigned short k = 0; k <= nPoly; ++k) {
+        for (unsigned short l = 0; l < nRows; ++l, ++ii) {
+          V[ii] = NormJacobi(i, 0, 0, r[l]) * NormJacobi(j, 0, 0, s[l]) * NormJacobi(k, 0, 0, t[l]);
         }
       }
     }
   }
 }
 
-void CFEMStandardElementBase::GradVandermonde3D_Hexahedron(unsigned short          nPoly,
-                                                           unsigned short          nDOFs,
-                                                           const vector<su2double> &r,
-                                                           const vector<su2double> &s,
-                                                           const vector<su2double> &t,
-                                                           vector<su2double>       &VDr,
-                                                           vector<su2double>       &VDs,
-                                                           vector<su2double>       &VDt) {
-
+void CFEMStandardElementBase::GradVandermonde3D_Hexahedron(unsigned short nPoly, unsigned short nDOFs,
+                                                           const vector<su2double>& r, const vector<su2double>& s,
+                                                           const vector<su2double>& t, vector<su2double>& VDr,
+                                                           vector<su2double>& VDs, vector<su2double>& VDt) {
   /*--- Determine the number or rows of the gradient of the Vandermonde matrix
         and check if the dimensions of VDr, VDs and VDt are correct.     ---*/
   unsigned short nRows = r.size();
-  unsigned long  nEntities = nRows*nDOFs;
-  if(VDr.size() != nEntities || VDs.size() != nEntities || VDt.size() != nEntities)
+  unsigned long nEntities = nRows * nDOFs;
+  if (VDr.size() != nEntities || VDs.size() != nEntities || VDt.size() != nEntities)
     SU2_MPI::Error("Wrong size of the VDr, VDs and VDt matrices", CURRENT_FUNCTION);
 
   /*--- For a hexahedron the basis functions are the tensor product of the 1D
@@ -1760,50 +1563,49 @@ void CFEMStandardElementBase::GradVandermonde3D_Hexahedron(unsigned short
         Also note that the sequence of the i, j and k loop must be identical to
         the evaluation of the Vandermonde matrix itself.      ---*/
   unsigned int ii = 0;
-  for(unsigned short i=0; i<=nPoly; ++i) {
-    for(unsigned short j=0; j<=nPoly; ++j) {
-      for(unsigned short k=0; k<=nPoly; ++k) {
-        for(unsigned short l=0; l<nRows; ++l, ++ii) {
-          VDr[ii] = NormJacobi(j,0,0,s[l])*NormJacobi(k,0,0,t[l])
-                  * GradNormJacobi(i,0,0,r[l]);
-          VDs[ii] = NormJacobi(i,0,0,r[l])*NormJacobi(k,0,0,t[l])
-                  * GradNormJacobi(j,0,0,s[l]);
-          VDt[ii] = NormJacobi(i,0,0,r[l])*NormJacobi(j,0,0,s[l])
-                  * GradNormJacobi(k,0,0,t[l]);
+  for (unsigned short i = 0; i <= nPoly; ++i) {
+    for (unsigned short j = 0; j <= nPoly; ++j) {
+      for (unsigned short k = 0; k <= nPoly; ++k) {
+        for (unsigned short l = 0; l < nRows; ++l, ++ii) {
+          VDr[ii] = NormJacobi(j, 0, 0, s[l]) * NormJacobi(k, 0, 0, t[l]) * GradNormJacobi(i, 0, 0, r[l]);
+          VDs[ii] = NormJacobi(i, 0, 0, r[l]) * NormJacobi(k, 0, 0, t[l]) * GradNormJacobi(j, 0, 0, s[l]);
+          VDt[ii] = NormJacobi(i, 0, 0, r[l]) * NormJacobi(j, 0, 0, s[l]) * GradNormJacobi(k, 0, 0, t[l]);
         }
       }
     }
   }
 }
 
-su2double CFEMStandardElementBase::ViscousPenaltyParameter(
-                                       const unsigned short VTK_TypeElem,
-                                       const unsigned short nPolyElem) const {
-
+su2double CFEMStandardElementBase::ViscousPenaltyParameter(const unsigned short VTK_TypeElem,
+                                                           const unsigned short nPolyElem) const {
   /*--- Determine the element type and set the value of the penalty
         parameter accordingly. ---*/
   su2double penParam = 0;  // To avoid a compiler warning.
 
-  switch( VTK_TypeElem ) {
+  switch (VTK_TypeElem) {
     case TRIANGLE:
-      penParam = (nPolyElem+1)*(nPolyElem+2)*0.5;
+      penParam = (nPolyElem + 1) * (nPolyElem + 2) * 0.5;
       break;
     case QUADRILATERAL:
-      penParam = (nPolyElem+1)*(nPolyElem+1);
+      penParam = (nPolyElem + 1) * (nPolyElem + 1);
       break;
     case TETRAHEDRON:
-      penParam = (nPolyElem+1)*(nPolyElem+3)/3.0;
+      penParam = (nPolyElem + 1) * (nPolyElem + 3) / 3.0;
       break;
     case PYRAMID:
-      if(VTK_Type == TRIANGLE) penParam = (nPolyElem+1)*(2*nPolyElem+3)*1.05/3.0;
-      else                     penParam = (nPolyElem+1)*(nPolyElem+3)/3.0;
+      if (VTK_Type == TRIANGLE)
+        penParam = (nPolyElem + 1) * (2 * nPolyElem + 3) * 1.05 / 3.0;
+      else
+        penParam = (nPolyElem + 1) * (nPolyElem + 3) / 3.0;
       break;
     case PRISM:
-      if(VTK_Type == TRIANGLE) penParam = (nPolyElem+1)*(nPolyElem+1);
-      else                     penParam = (nPolyElem+1)*(nPolyElem+2)*0.5;
+      if (VTK_Type == TRIANGLE)
+        penParam = (nPolyElem + 1) * (nPolyElem + 1);
+      else
+        penParam = (nPolyElem + 1) * (nPolyElem + 2) * 0.5;
       break;
     case HEXAHEDRON:
-      penParam = (nPolyElem+1)*(nPolyElem+1);
+      penParam = (nPolyElem + 1) * (nPolyElem + 1);
       break;
   }
 
@@ -1815,9 +1617,7 @@ su2double CFEMStandardElementBase::ViscousPenaltyParameter(
 /*          Private member functions of CFEMStandardElementBase.                    */
 /*----------------------------------------------------------------------------------*/
 
-void CFEMStandardElementBase::GaussLegendrePoints1D(vector<su2double> &GLPoints,
-                                                    vector<su2double> &GLWeights) {
-
+void CFEMStandardElementBase::GaussLegendrePoints1D(vector<su2double>& GLPoints, vector<su2double>& GLWeights) {
   /* The class used to determine the integration points operate on passivedoubles.
      Allocate the memory for the help vectors. */
   vector<passivedouble> GLPointsPas(GLPoints.size());
@@ -1829,61 +1629,56 @@ void CFEMStandardElementBase::GaussLegendrePoints1D(vector<su2double> &GLPoints,
   GaussJacobi.GetQuadraturePoints(0.0, 0.0, -1.0, 1.0, GLPointsPas, GLWeightsPas);
 
   /* Copy the data back into GLPoints and GLWeights. */
-  for(unsigned long i=0; i<GLPoints.size(); ++i) {
-    GLPoints[i]  = GLPointsPas[i];
+  for (unsigned long i = 0; i < GLPoints.size(); ++i) {
+    GLPoints[i] = GLPointsPas[i];
     GLWeights[i] = GLWeightsPas[i];
   }
 }
 
-su2double CFEMStandardElementBase::NormJacobi(unsigned short n,
-                                              unsigned short alpha,
-                                              unsigned short beta,
-                                              su2double      x) {
+su2double CFEMStandardElementBase::NormJacobi(unsigned short n, unsigned short alpha, unsigned short beta,
+                                              su2double x) {
   /*--- Some abbreviations. ---*/
-  su2double ap1   = alpha + 1;
-  su2double bp1   = beta  + 1;
-  su2double apb   = alpha + beta;
+  su2double ap1 = alpha + 1;
+  su2double bp1 = beta + 1;
+  su2double apb = alpha + beta;
   su2double apbp1 = apb + 1;
   su2double apbp2 = apb + 2;
   su2double apbp3 = apb + 3;
-  su2double b2ma2 = beta*beta - alpha*alpha;
+  su2double b2ma2 = beta * beta - alpha * alpha;
 
   /*--- Determine the term, which involves the gamma function for P0. As the
         arguments are integers, this term can be computed easily, because
         Gamma(n+1) = n!. ---*/
   su2double Gamap1 = 1.0, Gambp1 = 1.0, Gamapbp2 = 1.0;
-  for(unsigned short i=2; i<=alpha; ++i)          Gamap1   *= i;
-  for(unsigned short i=2; i<=beta; ++i)           Gambp1   *= i;
-  for(unsigned short i=2; i<=(alpha+beta+1); ++i) Gamapbp2 *= i;
+  for (unsigned short i = 2; i <= alpha; ++i) Gamap1 *= i;
+  for (unsigned short i = 2; i <= beta; ++i) Gambp1 *= i;
+  for (unsigned short i = 2; i <= (alpha + beta + 1); ++i) Gamapbp2 *= i;
 
   /*--- Initialize the normalized polynomials. ---*/
-  su2double Pnm1 = sqrt(pow(0.5,apbp1)*Gamapbp2/(Gamap1*Gambp1));
-  su2double Pn   = 0.5*Pnm1*(apbp2*x + alpha - beta)*sqrt(apbp3/(ap1*bp1));
+  su2double Pnm1 = sqrt(pow(0.5, apbp1) * Gamapbp2 / (Gamap1 * Gambp1));
+  su2double Pn = 0.5 * Pnm1 * (apbp2 * x + alpha - beta) * sqrt(apbp3 / (ap1 * bp1));
 
   /*--- Take care of the special situation of n == 0. ---*/
-  if(n == 0) Pn = Pnm1;
-  else
-  {
+  if (n == 0)
+    Pn = Pnm1;
+  else {
     /*--- The value of the normalized Jacobi polynomial must be obtained via recursion. ---*/
-    for(unsigned short i=2; i<=n; ++i)
-    {
+    for (unsigned short i = 2; i <= n; ++i) {
       /*--- Compute the coefficients a for i and i-1 and the coefficient bi. ---*/
-      unsigned short j = i-1;
-      su2double   tmp  = 2*j + apb;
-      su2double   aim1 = 2.0*sqrt(j*(j+apb)*(j+alpha)*(j+beta)/((tmp-1.0)*(tmp+1.0)))
-                       / tmp;
+      unsigned short j = i - 1;
+      su2double tmp = 2 * j + apb;
+      su2double aim1 = 2.0 * sqrt(j * (j + apb) * (j + alpha) * (j + beta) / ((tmp - 1.0) * (tmp + 1.0))) / tmp;
 
-      su2double bi = b2ma2/(tmp*(tmp+2.0));
+      su2double bi = b2ma2 / (tmp * (tmp + 2.0));
 
-      tmp          = 2*i + apb;
-      su2double ai = 2.0*sqrt(i*(i+apb)*(i+alpha)*(i+beta)/((tmp-1.0)*(tmp+1.0)))
-                   / tmp;
+      tmp = 2 * i + apb;
+      su2double ai = 2.0 * sqrt(i * (i + apb) * (i + alpha) * (i + beta) / ((tmp - 1.0) * (tmp + 1.0))) / tmp;
 
       /*--- Compute the new value of Pn and make sure to store Pnm1 correctly. ---*/
-      tmp  = Pnm1;
+      tmp = Pnm1;
       Pnm1 = Pn;
 
-      Pn = ((x-bi)*Pn - aim1*tmp)/ai;
+      Pn = ((x - bi) * Pn - aim1 * tmp) / ai;
     }
   }
 
@@ -1891,19 +1686,16 @@ su2double CFEMStandardElementBase::NormJacobi(unsigned short n,
   return Pn;
 }
 
-su2double CFEMStandardElementBase::GradNormJacobi(unsigned short n,
-                                                  unsigned short alpha,
-                                                  unsigned short beta,
-                                                  su2double      x) {
-
+su2double CFEMStandardElementBase::GradNormJacobi(unsigned short n, unsigned short alpha, unsigned short beta,
+                                                  su2double x) {
   /*--- Make a distinction for n == 0 and n > 0. For n == 0 the derivative is
         zero, because the polynomial itself is constant. ---*/
   su2double grad;
-  if(n == 0) grad = 0.0;
-  else
-  {
-    su2double tmp = n*(n+alpha+beta+1.0);
-    grad          = sqrt(tmp)*NormJacobi(n-1, alpha+1, beta+1, x);
+  if (n == 0)
+    grad = 0.0;
+  else {
+    su2double tmp = n * (n + alpha + beta + 1.0);
+    grad = sqrt(tmp) * NormJacobi(n - 1, alpha + 1, beta + 1, x);
   }
 
   /*--- Return the gradient. ---*/
@@ -1914,30 +1706,38 @@ su2double CFEMStandardElementBase::GradNormJacobi(unsigned short n,
 /*           Public member functions of CFEMStandardElement.                        */
 /*----------------------------------------------------------------------------------*/
 
-CFEMStandardElement::CFEMStandardElement(unsigned short          val_VTK_Type,
-                                         unsigned short          val_nPoly,
-                                         bool                    val_constJac,
-                                         CConfig                 *config,
-                                         unsigned short          val_orderExact,
-                                         const vector<su2double> *rLocSolDOFs,
-                                         const vector<su2double> *sLocSolDOFs,
-                                         const vector<su2double> *tLocSolDOFs)
-
-  : CFEMStandardElementBase(val_VTK_Type, val_nPoly, val_constJac,
-                            config, val_orderExact) {
+CFEMStandardElement::CFEMStandardElement(unsigned short val_VTK_Type, unsigned short val_nPoly, bool val_constJac,
+                                         CConfig* config, unsigned short val_orderExact,
+                                         const vector<su2double>* rLocSolDOFs, const vector<su2double>* sLocSolDOFs,
+                                         const vector<su2double>* tLocSolDOFs)
 
+    : CFEMStandardElementBase(val_VTK_Type, val_nPoly, val_constJac, config, val_orderExact) {
   /*--- Copy the function arguments to the member variables. ---*/
   nPoly = val_nPoly;
 
   /*--- Determine the element type and compute the other member variables. ---*/
-  switch( VTK_Type ) {
-    case LINE:          DataStandardLine();          break;
-    case TRIANGLE:      DataStandardTriangle();      break;
-    case QUADRILATERAL: DataStandardQuadrilateral(); break;
-    case TETRAHEDRON:   DataStandardTetrahedron();   break;
-    case PYRAMID:       DataStandardPyramid();       break;
-    case PRISM:         DataStandardPrism();         break;
-    case HEXAHEDRON:    DataStandardHexahedron();    break;
+  switch (VTK_Type) {
+    case LINE:
+      DataStandardLine();
+      break;
+    case TRIANGLE:
+      DataStandardTriangle();
+      break;
+    case QUADRILATERAL:
+      DataStandardQuadrilateral();
+      break;
+    case TETRAHEDRON:
+      DataStandardTetrahedron();
+      break;
+    case PYRAMID:
+      DataStandardPyramid();
+      break;
+    case PRISM:
+      DataStandardPrism();
+      break;
+    case HEXAHEDRON:
+      DataStandardHexahedron();
+      break;
   }
 
   /*--------------------------------------------------------------------------*/
@@ -1949,24 +1749,21 @@ CFEMStandardElement::CFEMStandardElement(unsigned short          val_VTK_Type,
   CheckSumLagrangianBasisFunctions(nIntegration, nDOFs, lagBasisIntegration);
 
   /*--- Check the sum of the derivatives of the Lagrangian basis functions. ---*/
-  if( !drLagBasisIntegration.empty() )
-    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFs,
-                                                drLagBasisIntegration);
-  if( !dsLagBasisIntegration.empty() )
-    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFs,
-                                                dsLagBasisIntegration);
-  if( !dtLagBasisIntegration.empty() )
-    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFs,
-                                                dtLagBasisIntegration);
+  if (!drLagBasisIntegration.empty())
+    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFs, drLagBasisIntegration);
+  if (!dsLagBasisIntegration.empty())
+    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFs, dsLagBasisIntegration);
+  if (!dtLagBasisIntegration.empty())
+    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFs, dtLagBasisIntegration);
 
   /*--- Create the transpose of lagBasisIntegration. This is needed for the
         efficient residual computation for the ADER-DG predictor step. ---*/
   lagBasisIntegrationTrans.resize(lagBasisIntegration.size());
 
   unsigned int ii = 0;
-  for(unsigned short j=0; j<nDOFs; ++j) {
-    for(unsigned short i=0; i<nIntegration; ++i, ++ii) {
-      const unsigned int ind = i*nDOFs + j;
+  for (unsigned short j = 0; j < nDOFs; ++j) {
+    for (unsigned short i = 0; i < nIntegration; ++i, ++ii) {
+      const unsigned int ind = i * nDOFs + j;
       lagBasisIntegrationTrans[ii] = lagBasisIntegration[ind];
     }
   }
@@ -1974,25 +1771,23 @@ CFEMStandardElement::CFEMStandardElement(unsigned short          val_VTK_Type,
   /*--- For efficiency reasons it is beneficial to store lagBasisIntegration,
         drLagBasisIntegration, dsLagBasisIntegration and dtLagBasisIntegration in
         one array. ---*/
-  const unsigned long sizeDerMat = drLagBasisIntegration.size()
-                                 + dsLagBasisIntegration.size()
-                                 + dtLagBasisIntegration.size();
-  const unsigned long sizeMat    = lagBasisIntegration.size() + sizeDerMat;
+  const unsigned long sizeDerMat =
+      drLagBasisIntegration.size() + dsLagBasisIntegration.size() + dtLagBasisIntegration.size();
+  const unsigned long sizeMat = lagBasisIntegration.size() + sizeDerMat;
 
   matBasisIntegration.resize(sizeMat);
   matDerBasisIntTrans.resize(sizeDerMat);
 
   ii = 0;
-  for(unsigned long i=0; i<lagBasisIntegration.size(); ++i, ++ii)
-    matBasisIntegration[ii] = lagBasisIntegration[i];
+  for (unsigned long i = 0; i < lagBasisIntegration.size(); ++i, ++ii) matBasisIntegration[ii] = lagBasisIntegration[i];
 
-  for(unsigned long i=0; i<drLagBasisIntegration.size(); ++i, ++ii)
+  for (unsigned long i = 0; i < drLagBasisIntegration.size(); ++i, ++ii)
     matBasisIntegration[ii] = drLagBasisIntegration[i];
 
-  for(unsigned long i=0; i<dsLagBasisIntegration.size(); ++i, ++ii)
+  for (unsigned long i = 0; i < dsLagBasisIntegration.size(); ++i, ++ii)
     matBasisIntegration[ii] = dsLagBasisIntegration[i];
 
-  for(unsigned long i=0; i<dtLagBasisIntegration.size(); ++i, ++ii)
+  for (unsigned long i = 0; i < dtLagBasisIntegration.size(); ++i, ++ii)
     matBasisIntegration[ii] = dtLagBasisIntegration[i];
 
   /* The transpose of the matrix containing the derivative information is needed
@@ -2000,15 +1795,18 @@ CFEMStandardElement::CFEMStandardElement(unsigned short          val_VTK_Type,
      residual can be computed with one matrix multiplication when the fluxes
      are known. */
   unsigned short nDim;
-  if(      dtLagBasisIntegration.size() ) nDim = 3;
-  else if( dsLagBasisIntegration.size() ) nDim = 2;
-  else                                    nDim = 1;
+  if (dtLagBasisIntegration.size())
+    nDim = 3;
+  else if (dsLagBasisIntegration.size())
+    nDim = 2;
+  else
+    nDim = 1;
 
   ii = 0;
-  for(unsigned short j=0; j<nDOFs; ++j) {
-    for(unsigned short i=0; i<nIntegration; ++i) {
-      for(unsigned short iDim=0; iDim<nDim; ++iDim, ++ii) {
-        const unsigned int ind = (iDim+1)*nDOFs*nIntegration + i*nDOFs + j;
+  for (unsigned short j = 0; j < nDOFs; ++j) {
+    for (unsigned short i = 0; i < nIntegration; ++i) {
+      for (unsigned short iDim = 0; iDim < nDim; ++iDim, ++ii) {
+        const unsigned int ind = (iDim + 1) * nDOFs * nIntegration + i * nDOFs + j;
         matDerBasisIntTrans[ii] = matBasisIntegration[ind];
       }
     }
@@ -2027,8 +1825,8 @@ CFEMStandardElement::CFEMStandardElement(unsigned short          val_VTK_Type,
 
   /* Create the basis functions and the matrix to store the derivatives in
      the basis functions in the solution DOFs. */
-  CreateBasisFunctionsAndMatrixDerivatives(rSolDOFs, sSolDOFs, tSolDOFs,
-                                           matVandermondeInv, lagBasisSolDOFs, matDerBasisSolDOFs);
+  CreateBasisFunctionsAndMatrixDerivatives(rSolDOFs, sSolDOFs, tSolDOFs, matVandermondeInv, lagBasisSolDOFs,
+                                           matDerBasisSolDOFs);
 
   /*--------------------------------------------------------------------------*/
   /*--- Create the data of the derivatives of the basis functions in the   ---*/
@@ -2039,8 +1837,7 @@ CFEMStandardElement::CFEMStandardElement(unsigned short          val_VTK_Type,
 
   vector<su2double> dummyLagBasis;
   vector<su2double> dummyMatVandermondeInv;
-  CreateBasisFunctionsAndMatrixDerivatives(rDOFs, sDOFs, tDOFs,
-                                           dummyMatVandermondeInv, dummyLagBasis,
+  CreateBasisFunctionsAndMatrixDerivatives(rDOFs, sDOFs, tDOFs, dummyMatVandermondeInv, dummyLagBasis,
                                            matDerBasisOwnDOFs);
 
   /*--------------------------------------------------------------------------*/
@@ -2056,19 +1853,18 @@ CFEMStandardElement::CFEMStandardElement(unsigned short          val_VTK_Type,
 
   /* Easier storage of the offset between the derivatives for matBasisIntegration
      and matDerBasisSolDOFs. */
-  const unsigned long offsetDerInt  = nDOFs*nIntegration;
-  const unsigned long offsetDerDOFs = nDOFs*nDOFs;
+  const unsigned long offsetDerInt = nDOFs * nIntegration;
+  const unsigned long offsetDerDOFs = nDOFs * nDOFs;
 
   /* Determine the size of the vector to store the second derivatives of the
      basis functions in the integration points. */
-  const unsigned long sizeMat2ndDer = offsetDerInt*nDim*(nDim+1)/2;
+  const unsigned long sizeMat2ndDer = offsetDerInt * nDim * (nDim + 1) / 2;
   mat2ndDerBasisInt.resize(sizeMat2ndDer);
 
   /* Loop over the number of dimensions to carry out the matrix multiplications. */
-  const su2double *matDerBasisInt = matBasisIntegration.data();
-  su2double       *mat2ndDerBasisIntPoint = mat2ndDerBasisInt.data();
-  for(unsigned short jDim=0; jDim<nDim; ++jDim) {
-
+  const su2double* matDerBasisInt = matBasisIntegration.data();
+  su2double* mat2ndDerBasisIntPoint = mat2ndDerBasisInt.data();
+  for (unsigned short jDim = 0; jDim < nDim; ++jDim) {
     /* Update the pointer matDerBasisInt to point to the correct derivative.
        As in matBasisIntegration also the interpolation data is stored, this
        update must happen before the matrix multiplication. */
@@ -2076,13 +1872,11 @@ CFEMStandardElement::CFEMStandardElement(unsigned short          val_VTK_Type,
 
     /* Second loop over the dimensions. Note that this loop only runs until
        iDim, because the Hessian is symmetric. */
-    for(unsigned short iDim=0; iDim<=jDim; iDim++)
-    {
+    for (unsigned short iDim = 0; iDim <= jDim; iDim++) {
       /* Carry out the matrix multiplication. The last argument is NULL, such
          that this gemm call is ignored in the profiling. Replace by config if
          if should be included. */
-      blasFunctions.gemm(nIntegration, nDOFs, nDOFs, matDerBasisInt,
-                         matDerBasisSolDOFs.data() + iDim*offsetDerDOFs,
+      blasFunctions.gemm(nIntegration, nDOFs, nDOFs, matDerBasisInt, matDerBasisSolDOFs.data() + iDim * offsetDerDOFs,
                          mat2ndDerBasisIntPoint, nullptr);
 
       /* Update the pointer to the position where the next second
@@ -2092,20 +1886,24 @@ CFEMStandardElement::CFEMStandardElement(unsigned short          val_VTK_Type,
   }
 }
 
-void CFEMStandardElement::BasisFunctionsInPoint(const su2double   *parCoor,
-                                                vector<su2double> &lagBasis) {
-
+void CFEMStandardElement::BasisFunctionsInPoint(const su2double* parCoor, vector<su2double>& lagBasis) {
   /* Determine the number of parametric dimensions, depending on the
      element type. */
   unsigned short nDimPar = 0;
-  switch(VTK_Type) {
-    case LINE:          nDimPar = 1; break;
+  switch (VTK_Type) {
+    case LINE:
+      nDimPar = 1;
+      break;
     case TRIANGLE:
-    case QUADRILATERAL: nDimPar = 2; break;
+    case QUADRILATERAL:
+      nDimPar = 2;
+      break;
     case TETRAHEDRON:
     case PYRAMID:
     case PRISM:
-    case HEXAHEDRON:    nDimPar = 3; break;
+    case HEXAHEDRON:
+      nDimPar = 3;
+      break;
   }
 
   /* Allocate the memory for the help vectors for computing the Vandermonde
@@ -2115,12 +1913,11 @@ void CFEMStandardElement::BasisFunctionsInPoint(const su2double   *parCoor,
 
   /* Copy the parametric coordinates in rPoints, such that the functions to
      compute the Vandermonde matrices can be used. */
-  for(unsigned long i=0; i<rPoints.size(); ++i)
-    rPoints[i][0] = parCoor[i];
+  for (unsigned long i = 0; i < rPoints.size(); ++i) rPoints[i][0] = parCoor[i];
 
   /* Determine the element type and call the appropriate function to compute
      the Vandermonde matrix. */
-  switch(VTK_Type) {
+  switch (VTK_Type) {
     case LINE:
       Vandermonde1D(nDOFs, rPoints[0], V);
       break;
@@ -2155,11 +1952,8 @@ void CFEMStandardElement::BasisFunctionsInPoint(const su2double   *parCoor,
   MatMulRowMajor(nDOFs, 1, V, matVandermondeInv, lagBasis);
 }
 
-void CFEMStandardElement::BasisFunctionsAndDerivativesInPoint(
-                                           const su2double            *parCoor,
-                                           vector<su2double>          &lagBasis,
-                                           vector<vector<su2double> > &dLagBasis) {
-
+void CFEMStandardElement::BasisFunctionsAndDerivativesInPoint(const su2double* parCoor, vector<su2double>& lagBasis,
+                                                              vector<vector<su2double> >& dLagBasis) {
   /* Allocate the memory for the help vectors for computing the Vandermonde
      matrices and its derivatives. */
   vector<vector<su2double> > rPoints(dLagBasis.size(), vector<su2double>(1));
@@ -2169,12 +1963,11 @@ void CFEMStandardElement::BasisFunctionsAndDerivativesInPoint(
 
   /* Copy the parametric coordinates in rPoints, such that the functions to
      compute the Vandermonde matrices can be used. */
-  for(unsigned long i=0; i<rPoints.size(); ++i)
-    rPoints[i][0] = parCoor[i];
+  for (unsigned long i = 0; i < rPoints.size(); ++i) rPoints[i][0] = parCoor[i];
 
   /* Determine the element type and call the appropriate function to compute
      the Vandermonde matrix and the derivative of the Vandermonde matrix. */
-  switch(VTK_Type) {
+  switch (VTK_Type) {
     case LINE:
       Vandermonde1D(nDOFs, rPoints[0], V);
       GradVandermonde1D(nDOFs, rPoints[0], VDr[0]);
@@ -2192,26 +1985,22 @@ void CFEMStandardElement::BasisFunctionsAndDerivativesInPoint(
 
     case TETRAHEDRON:
       Vandermonde3D_Tetrahedron(nPoly, nDOFs, rPoints[0], rPoints[1], rPoints[2], V);
-      GradVandermonde3D_Tetrahedron(nPoly, nDOFs, rPoints[0], rPoints[1], rPoints[2],
-                                    VDr[0], VDr[1], VDr[2]);
+      GradVandermonde3D_Tetrahedron(nPoly, nDOFs, rPoints[0], rPoints[1], rPoints[2], VDr[0], VDr[1], VDr[2]);
       break;
 
     case PYRAMID:
       Vandermonde3D_Pyramid(nPoly, nDOFs, rPoints[0], rPoints[1], rPoints[2], V);
-      GradVandermonde3D_Pyramid(nPoly, nDOFs, rPoints[0], rPoints[1], rPoints[2],
-                                VDr[0], VDr[1], VDr[2]);
+      GradVandermonde3D_Pyramid(nPoly, nDOFs, rPoints[0], rPoints[1], rPoints[2], VDr[0], VDr[1], VDr[2]);
       break;
 
     case PRISM:
       Vandermonde3D_Prism(nPoly, nDOFs, rPoints[0], rPoints[1], rPoints[2], V);
-      GradVandermonde3D_Prism(nPoly, nDOFs, rPoints[0], rPoints[1], rPoints[2],
-                              VDr[0], VDr[1], VDr[2]);
+      GradVandermonde3D_Prism(nPoly, nDOFs, rPoints[0], rPoints[1], rPoints[2], VDr[0], VDr[1], VDr[2]);
       break;
 
     case HEXAHEDRON:
       Vandermonde3D_Hexahedron(nPoly, nDOFs, rPoints[0], rPoints[1], rPoints[2], V);
-      GradVandermonde3D_Hexahedron(nPoly, nDOFs, rPoints[0], rPoints[1], rPoints[2],
-                                   VDr[0], VDr[1], VDr[2]);
+      GradVandermonde3D_Hexahedron(nPoly, nDOFs, rPoints[0], rPoints[1], rPoints[2], VDr[0], VDr[1], VDr[2]);
       break;
   }
 
@@ -2219,16 +2008,15 @@ void CFEMStandardElement::BasisFunctionsAndDerivativesInPoint(
      basis functions and its derivatives in the given parametric coordinate. */
   MatMulRowMajor(nDOFs, 1, V, matVandermondeInv, lagBasis);
 
-  for(unsigned long i=0; i<dLagBasis.size(); ++i)
+  for (unsigned long i = 0; i < dLagBasis.size(); ++i)
     MatMulRowMajor(nDOFs, 1, VDr[i], matVandermondeInv, dLagBasis[i]);
 }
 
-bool CFEMStandardElement::SameStandardElement(unsigned short val_VTK_Type,
-                                              unsigned short val_nPoly,
-                                              bool           val_constJac) {
-  if(val_VTK_Type != VTK_Type)      return false;
-  if(val_nPoly    != nPoly)         return false;
-  if(val_constJac != constJacobian) return false;
+bool CFEMStandardElement::SameStandardElement(unsigned short val_VTK_Type, unsigned short val_nPoly,
+                                              bool val_constJac) {
+  if (val_VTK_Type != VTK_Type) return false;
+  if (val_nPoly != nPoly) return false;
+  if (val_constJac != constJacobian) return false;
 
   return true;
 }
@@ -2237,8 +2025,7 @@ bool CFEMStandardElement::SameStandardElement(unsigned short val_VTK_Type,
 /*           Private member functions of CFEMStandardElement.                       */
 /*----------------------------------------------------------------------------------*/
 
-void CFEMStandardElement::Copy(const CFEMStandardElement &other) {
-
+void CFEMStandardElement::Copy(const CFEMStandardElement& other) {
   CFEMStandardElementBase::Copy(other);
 
   nPoly = other.nPoly;
@@ -2251,9 +2038,9 @@ void CFEMStandardElement::Copy(const CFEMStandardElement &other) {
   sDOFs = other.sDOFs;
   tDOFs = other.tDOFs;
 
-  lagBasisIntegration      = other.lagBasisIntegration;
+  lagBasisIntegration = other.lagBasisIntegration;
   lagBasisIntegrationTrans = other.lagBasisIntegrationTrans;
-  lagBasisSolDOFs          = other.lagBasisSolDOFs;
+  lagBasisSolDOFs = other.lagBasisSolDOFs;
 
   drLagBasisIntegration = other.drLagBasisIntegration;
   dsLagBasisIntegration = other.dsLagBasisIntegration;
@@ -2269,99 +2056,64 @@ void CFEMStandardElement::Copy(const CFEMStandardElement &other) {
   subConn1ForPlotting = other.subConn1ForPlotting;
   subConn2ForPlotting = other.subConn2ForPlotting;
 
-  matVandermondeInv   = other.matVandermondeInv;
+  matVandermondeInv = other.matVandermondeInv;
   matBasisIntegration = other.matBasisIntegration;
   matDerBasisIntTrans = other.matDerBasisIntTrans;
-  matDerBasisSolDOFs  = other.matDerBasisSolDOFs;
-  matDerBasisOwnDOFs  = other.matDerBasisOwnDOFs;
-  mat2ndDerBasisInt   = other.mat2ndDerBasisInt;
+  matDerBasisSolDOFs = other.matDerBasisSolDOFs;
+  matDerBasisOwnDOFs = other.matDerBasisOwnDOFs;
+  mat2ndDerBasisInt = other.mat2ndDerBasisInt;
 }
 
 void CFEMStandardElement::CreateBasisFunctionsAndMatrixDerivatives(
-                                       const vector<su2double> &rLoc,
-                                       const vector<su2double> &sLoc,
-                                       const vector<su2double> &tLoc,
-                                             vector<su2double> &matVandermondeInv,
-                                             vector<su2double> &lagBasis,
-                                             vector<su2double> &matDerBasis) {
-
+    const vector<su2double>& rLoc, const vector<su2double>& sLoc, const vector<su2double>& tLoc,
+    vector<su2double>& matVandermondeInv, vector<su2double>& lagBasis, vector<su2double>& matDerBasis) {
   /* Define the variables, such that the general functions to compute
      the gradients of the basis functions can be used. Note that some
      of these variables are dummy variables. */
-  unsigned short    nDOFsDummy;
+  unsigned short nDOFsDummy;
   vector<su2double> rDOFsDummy, sDOFsDummy, tDOFsDummy;
   vector<su2double> drLagBasisLoc, dsLagBasisLoc, dtLagBasisLoc;
 
   /*--- Determine the element type and compute the basis functions and the
         gradients of the basis functions in the given DOFs. ---*/
-  switch( VTK_Type ) {
+  switch (VTK_Type) {
     case LINE:
-      LagrangianBasisFunctionAndDerivativesLine(nPoly,      rLoc,
-                                                nDOFsDummy, rDOFsDummy,
-                                                matVandermondeInv,
-                                                lagBasis,   drLagBasisLoc);
+      LagrangianBasisFunctionAndDerivativesLine(nPoly, rLoc, nDOFsDummy, rDOFsDummy, matVandermondeInv, lagBasis,
+                                                drLagBasisLoc);
       break;
 
     case TRIANGLE:
-      LagrangianBasisFunctionAndDerivativesTriangle(nPoly,      rLoc,
-                                                    sLoc,       nDOFsDummy,
-                                                    rDOFsDummy, sDOFsDummy,
-                                                    matVandermondeInv,
-                                                    lagBasis,   drLagBasisLoc,
-                                                    dsLagBasisLoc);
+      LagrangianBasisFunctionAndDerivativesTriangle(nPoly, rLoc, sLoc, nDOFsDummy, rDOFsDummy, sDOFsDummy,
+                                                    matVandermondeInv, lagBasis, drLagBasisLoc, dsLagBasisLoc);
       break;
 
     case QUADRILATERAL:
-      LagrangianBasisFunctionAndDerivativesQuadrilateral(nPoly,      rLoc,
-                                                         sLoc,       nDOFsDummy,
-                                                         rDOFsDummy, sDOFsDummy,
-                                                         matVandermondeInv,
-                                                         lagBasis,   drLagBasisLoc,
-                                                         dsLagBasisLoc);
+      LagrangianBasisFunctionAndDerivativesQuadrilateral(nPoly, rLoc, sLoc, nDOFsDummy, rDOFsDummy, sDOFsDummy,
+                                                         matVandermondeInv, lagBasis, drLagBasisLoc, dsLagBasisLoc);
       break;
 
     case TETRAHEDRON:
-      LagrangianBasisFunctionAndDerivativesTetrahedron(nPoly,      rLoc,
-                                                       sLoc,       tLoc,
-                                                       nDOFsDummy, rDOFsDummy,
-                                                       sDOFsDummy, tDOFsDummy,
-                                                       matVandermondeInv,
-                                                       lagBasis,   drLagBasisLoc,
-                                                       dsLagBasisLoc,
-                                                       dtLagBasisLoc);
+      LagrangianBasisFunctionAndDerivativesTetrahedron(nPoly, rLoc, sLoc, tLoc, nDOFsDummy, rDOFsDummy, sDOFsDummy,
+                                                       tDOFsDummy, matVandermondeInv, lagBasis, drLagBasisLoc,
+                                                       dsLagBasisLoc, dtLagBasisLoc);
       break;
 
     case PYRAMID:
-      LagrangianBasisFunctionAndDerivativesPyramid(nPoly,      rLoc,
-                                                   sLoc,       tLoc,
-                                                   nDOFsDummy, rDOFsDummy,
-                                                   sDOFsDummy, tDOFsDummy,
-                                                   matVandermondeInv,
-                                                   lagBasis,   drLagBasisLoc,
-                                                   dsLagBasisLoc,
-                                                   dtLagBasisLoc);
+      LagrangianBasisFunctionAndDerivativesPyramid(nPoly, rLoc, sLoc, tLoc, nDOFsDummy, rDOFsDummy, sDOFsDummy,
+                                                   tDOFsDummy, matVandermondeInv, lagBasis, drLagBasisLoc,
+                                                   dsLagBasisLoc, dtLagBasisLoc);
       break;
 
     case PRISM:
-      LagrangianBasisFunctionAndDerivativesPrism(nPoly,      rLoc,
-                                                 sLoc,       tLoc,
-                                                 nDOFsDummy, rDOFsDummy,
-                                                 sDOFsDummy, tDOFsDummy,
-                                                 matVandermondeInv,
-                                                 lagBasis,   drLagBasisLoc,
-                                                 dsLagBasisLoc,
+      LagrangianBasisFunctionAndDerivativesPrism(nPoly, rLoc, sLoc, tLoc, nDOFsDummy, rDOFsDummy, sDOFsDummy,
+                                                 tDOFsDummy, matVandermondeInv, lagBasis, drLagBasisLoc, dsLagBasisLoc,
                                                  dtLagBasisLoc);
       break;
 
     case HEXAHEDRON:
-      LagrangianBasisFunctionAndDerivativesHexahedron(nPoly,      rLoc,
-                                                      sLoc,       tLoc,
-                                                      nDOFsDummy, rDOFsDummy,
-                                                      sDOFsDummy, tDOFsDummy,
-                                                      matVandermondeInv,
-                                                      lagBasis,   drLagBasisLoc,
-                                                      dsLagBasisLoc,
-                                                      dtLagBasisLoc);
+      LagrangianBasisFunctionAndDerivativesHexahedron(nPoly, rLoc, sLoc, tLoc, nDOFsDummy, rDOFsDummy, sDOFsDummy,
+                                                      tDOFsDummy, matVandermondeInv, lagBasis, drLagBasisLoc,
+                                                      dsLagBasisLoc, dtLagBasisLoc);
       break;
   }
 
@@ -2371,48 +2123,37 @@ void CFEMStandardElement::CreateBasisFunctionsAndMatrixDerivatives(
 
   CheckSumLagrangianBasisFunctions(nLoc, nDOFs, lagBasis);
 
-  if( !drLagBasisLoc.empty() )
-    CheckSumDerivativesLagrangianBasisFunctions(nLoc, nDOFs,
-                                                drLagBasisLoc);
-  if( !dsLagBasisLoc.empty() )
-    CheckSumDerivativesLagrangianBasisFunctions(nLoc, nDOFs,
-                                                dsLagBasisLoc);
-  if( !dtLagBasisLoc.empty() )
-    CheckSumDerivativesLagrangianBasisFunctions(nLoc, nDOFs,
-                                                dtLagBasisLoc);
+  if (!drLagBasisLoc.empty()) CheckSumDerivativesLagrangianBasisFunctions(nLoc, nDOFs, drLagBasisLoc);
+  if (!dsLagBasisLoc.empty()) CheckSumDerivativesLagrangianBasisFunctions(nLoc, nDOFs, dsLagBasisLoc);
+  if (!dtLagBasisLoc.empty()) CheckSumDerivativesLagrangianBasisFunctions(nLoc, nDOFs, dtLagBasisLoc);
 
   /*--- For efficiency reasons drLagBasisLoc, dsLagBasisLoc and
         dtLagBasisLoc are stored in matDerBasis. ---*/
-  const unsigned long sizeDerMat = drLagBasisLoc.size() + dsLagBasisLoc.size()
-                                 + dtLagBasisLoc.size();
+  const unsigned long sizeDerMat = drLagBasisLoc.size() + dsLagBasisLoc.size() + dtLagBasisLoc.size();
 
   matDerBasis.resize(sizeDerMat);
 
   unsigned int ii = 0;
-  for(unsigned long i=0; i<drLagBasisLoc.size(); ++i, ++ii)
-    matDerBasis[ii] = drLagBasisLoc[i];
+  for (unsigned long i = 0; i < drLagBasisLoc.size(); ++i, ++ii) matDerBasis[ii] = drLagBasisLoc[i];
 
-  for(unsigned long i=0; i<dsLagBasisLoc.size(); ++i, ++ii)
-    matDerBasis[ii] = dsLagBasisLoc[i];
+  for (unsigned long i = 0; i < dsLagBasisLoc.size(); ++i, ++ii) matDerBasis[ii] = dsLagBasisLoc[i];
 
-  for(unsigned long i=0; i<dtLagBasisLoc.size(); ++i, ++ii)
-    matDerBasis[ii] = dtLagBasisLoc[i];
+  for (unsigned long i = 0; i < dtLagBasisLoc.size(); ++i, ++ii) matDerBasis[ii] = dtLagBasisLoc[i];
 }
 
 void CFEMStandardElement::DataStandardLine(void) {
-
   /*--- Determine the Lagrangian basis functions and its derivatives
         in the integration points. ---*/
   vector<su2double> matVandermondeInvDummy;
-  LagrangianBasisFunctionAndDerivativesLine(nPoly, rIntegration, nDOFs, rDOFs,
-                                            matVandermondeInvDummy,
-                                            lagBasisIntegration,
-                                            drLagBasisIntegration);
+  LagrangianBasisFunctionAndDerivativesLine(nPoly, rIntegration, nDOFs, rDOFs, matVandermondeInvDummy,
+                                            lagBasisIntegration, drLagBasisIntegration);
 
   /*--- Determine the local connectivity of the two "faces" of the line element.
         For a line element the faces are just points.   ---*/
-  connFace0.reserve(1); connFace0.push_back(0);
-  connFace1.reserve(1); connFace1.push_back(nPoly);
+  connFace0.reserve(1);
+  connFace0.push_back(0);
+  connFace1.reserve(1);
+  connFace1.push_back(nPoly);
 
   /*--- Determine the local subconnectivity used for plotting purposes. ---*/
   SubConnForPlottingLine(nPoly, subConn1ForPlotting);
@@ -2423,25 +2164,23 @@ void CFEMStandardElement::DataStandardLine(void) {
 }
 
 void CFEMStandardElement::DataStandardTriangle(void) {
-
   /*--- Determine the Lagrangian basis functions and its derivatives
         in the integration points. ---*/
   vector<su2double> matVandermondeInvDummy;
-  LagrangianBasisFunctionAndDerivativesTriangle(nPoly, rIntegration, sIntegration,
-                                                nDOFs, rDOFs, sDOFs,
-                                                matVandermondeInvDummy,
-                                                lagBasisIntegration,
-                                                drLagBasisIntegration,
+  LagrangianBasisFunctionAndDerivativesTriangle(nPoly, rIntegration, sIntegration, nDOFs, rDOFs, sDOFs,
+                                                matVandermondeInvDummy, lagBasisIntegration, drLagBasisIntegration,
                                                 dsLagBasisIntegration);
 
   /*--- Determine the local connectivity of the three "faces" of the triangle.
         For a triangular element the faces are just lines. Make sure that the
         element is to the left of the face. ---*/
-  connFace0.reserve(nPoly+1); connFace1.reserve(nPoly+1); connFace2.reserve(nPoly+1);
+  connFace0.reserve(nPoly + 1);
+  connFace1.reserve(nPoly + 1);
+  connFace2.reserve(nPoly + 1);
 
-  for(signed short i=0; i<=nPoly; ++i) connFace0.push_back(i);
-  for(signed short i=0; i<=nPoly; ++i) connFace1.push_back((i+1)*(nPoly+1) - i*(i+1)/2 -1);
-  for(signed short i=nPoly; i>=0; --i) connFace2.push_back(i*(nPoly+1) - i*(i-1)/2);
+  for (signed short i = 0; i <= nPoly; ++i) connFace0.push_back(i);
+  for (signed short i = 0; i <= nPoly; ++i) connFace1.push_back((i + 1) * (nPoly + 1) - i * (i + 1) / 2 - 1);
+  for (signed short i = nPoly; i >= 0; --i) connFace2.push_back(i * (nPoly + 1) - i * (i - 1) / 2);
 
   /*--- Determine the local subconnectivity of the triangular element used for
         plotting purposes. ---*/
@@ -2453,30 +2192,27 @@ void CFEMStandardElement::DataStandardTriangle(void) {
 }
 
 void CFEMStandardElement::DataStandardQuadrilateral(void) {
-
   /*--- Determine the Lagrangian basis functions and its derivatives
         in the integration points. ---*/
   vector<su2double> matVandermondeInvDummy;
-  LagrangianBasisFunctionAndDerivativesQuadrilateral(nPoly, rIntegration,
-                                                     sIntegration,
-                                                     nDOFs, rDOFs, sDOFs,
-                                                     matVandermondeInvDummy,
-                                                     lagBasisIntegration,
-                                                     drLagBasisIntegration,
+  LagrangianBasisFunctionAndDerivativesQuadrilateral(nPoly, rIntegration, sIntegration, nDOFs, rDOFs, sDOFs,
+                                                     matVandermondeInvDummy, lagBasisIntegration, drLagBasisIntegration,
                                                      dsLagBasisIntegration);
 
   /*--- Determine the local connectivity of the four "faces" of the quad element.
         For a quad element the faces are just lines. Make sure that the element
         is to the left of the face. ---*/
-  connFace0.reserve(nPoly+1); connFace1.reserve(nPoly+1);
-  connFace2.reserve(nPoly+1); connFace3.reserve(nPoly+1);
+  connFace0.reserve(nPoly + 1);
+  connFace1.reserve(nPoly + 1);
+  connFace2.reserve(nPoly + 1);
+  connFace3.reserve(nPoly + 1);
 
-  unsigned short n0 = 0, n1 = nPoly, n2 = nDOFs-1, n3 = nPoly*(nPoly+1);
+  unsigned short n0 = 0, n1 = nPoly, n2 = nDOFs - 1, n3 = nPoly * (nPoly + 1);
 
-  for(signed short i=n0; i<=n1; ++i)          connFace0.push_back(i);
-  for(signed short i=n1; i<=n2; i+=(nPoly+1)) connFace1.push_back(i);
-  for(signed short i=n2; i>=n3; --i)          connFace2.push_back(i);
-  for(signed short i=n3; i>=n0; i-=(nPoly+1)) connFace3.push_back(i);
+  for (signed short i = n0; i <= n1; ++i) connFace0.push_back(i);
+  for (signed short i = n1; i <= n2; i += (nPoly + 1)) connFace1.push_back(i);
+  for (signed short i = n2; i >= n3; --i) connFace2.push_back(i);
+  for (signed short i = n3; i >= n0; i -= (nPoly + 1)) connFace3.push_back(i);
 
   /*--- Determine the local subconnectivity of the quadrilateral element used for
         plotting purposes. ---*/
@@ -2488,35 +2224,31 @@ void CFEMStandardElement::DataStandardQuadrilateral(void) {
 }
 
 void CFEMStandardElement::DataStandardTetrahedron(void) {
-
   /*--- Determine the Lagrangian basis functions and its derivatives
         in the integration points. ---*/
   vector<su2double> matVandermondeInvDummy;
-  LagrangianBasisFunctionAndDerivativesTetrahedron(nPoly, rIntegration,
-                                                   sIntegration, tIntegration,
-                                                   nDOFs, rDOFs, sDOFs, tDOFs,
-                                                   matVandermondeInvDummy,
-                                                   lagBasisIntegration,
-                                                   drLagBasisIntegration,
-                                                   dsLagBasisIntegration,
-                                                   dtLagBasisIntegration);
+  LagrangianBasisFunctionAndDerivativesTetrahedron(nPoly, rIntegration, sIntegration, tIntegration, nDOFs, rDOFs, sDOFs,
+                                                   tDOFs, matVandermondeInvDummy, lagBasisIntegration,
+                                                   drLagBasisIntegration, dsLagBasisIntegration, dtLagBasisIntegration);
 
   /*--- Determine the local connectivity of the four faces of the tetrahedron.
         For a tetrahedron the faces are triangles. ---*/
-  unsigned short nDOFsTriangle = (nPoly+1)*(nPoly+2)/2;
-  connFace0.reserve(nDOFsTriangle); connFace1.reserve(nDOFsTriangle);
-  connFace2.reserve(nDOFsTriangle); connFace3.reserve(nDOFsTriangle);
+  unsigned short nDOFsTriangle = (nPoly + 1) * (nPoly + 2) / 2;
+  connFace0.reserve(nDOFsTriangle);
+  connFace1.reserve(nDOFsTriangle);
+  connFace2.reserve(nDOFsTriangle);
+  connFace3.reserve(nDOFsTriangle);
 
   unsigned int ii = 0;
-  for(unsigned short k=0; k<=nPoly; ++k) {
+  for (unsigned short k = 0; k <= nPoly; ++k) {
     unsigned short uppBoundJ = nPoly - k;
-    for(unsigned short j=0; j<=uppBoundJ; ++j) {
+    for (unsigned short j = 0; j <= uppBoundJ; ++j) {
       unsigned short uppBoundI = nPoly - k - j;
-      for(unsigned short i=0; i<=uppBoundI; ++i, ++ii) {
-        if(k == 0)           connFace0.push_back(ii);
-        if(j == 0)           connFace1.push_back(ii);
-        if(i == 0)           connFace2.push_back(ii);
-        if((i+j+k) == nPoly) connFace3.push_back(ii);
+      for (unsigned short i = 0; i <= uppBoundI; ++i, ++ii) {
+        if (k == 0) connFace0.push_back(ii);
+        if (j == 0) connFace1.push_back(ii);
+        if (i == 0) connFace2.push_back(ii);
+        if ((i + j + k) == nPoly) connFace3.push_back(ii);
       }
     }
   }
@@ -2524,8 +2256,8 @@ void CFEMStandardElement::DataStandardTetrahedron(void) {
   /*--- Make sure that the element is to the left of the faces. ---*/
   unsigned short n0 = 0;
   unsigned short n1 = nPoly;
-  unsigned short n2 = nDOFsTriangle -1;
-  unsigned short n3 = nDOFs -1;
+  unsigned short n2 = nDOFsTriangle - 1;
+  unsigned short n3 = nDOFs - 1;
 
   ChangeDirectionTriangleConn(connFace0, n0, n1, n2);
   ChangeDirectionTriangleConn(connFace1, n0, n3, n1);
@@ -2543,23 +2275,17 @@ void CFEMStandardElement::DataStandardTetrahedron(void) {
 }
 
 void CFEMStandardElement::DataStandardPyramid(void) {
-
   /*--- Determine the Lagrangian basis functions and its derivatives
         in the integration points. ---*/
   vector<su2double> matVandermondeInvDummy;
-  LagrangianBasisFunctionAndDerivativesPyramid(nPoly, rIntegration,
-                                               sIntegration, tIntegration,
-                                               nDOFs, rDOFs, sDOFs, tDOFs,
-                                               matVandermondeInvDummy,
-                                               lagBasisIntegration,
-                                               drLagBasisIntegration,
-                                               dsLagBasisIntegration,
-                                               dtLagBasisIntegration);
+  LagrangianBasisFunctionAndDerivativesPyramid(nPoly, rIntegration, sIntegration, tIntegration, nDOFs, rDOFs, sDOFs,
+                                               tDOFs, matVandermondeInvDummy, lagBasisIntegration,
+                                               drLagBasisIntegration, dsLagBasisIntegration, dtLagBasisIntegration);
 
   /*--- Determine the local connectivity of the five faces of the pyramid.
         For a pyramid there are four triangular faces and one quadrilateral face. ---*/
-  unsigned short nDOFsQuad     = (nPoly+1)*(nPoly+1);
-  unsigned short nDOFsTriangle = (nPoly+1)*(nPoly+2)/2;
+  unsigned short nDOFsQuad = (nPoly + 1) * (nPoly + 1);
+  unsigned short nDOFsTriangle = (nPoly + 1) * (nPoly + 2) / 2;
 
   connFace0.reserve(nDOFsQuad);
   connFace1.reserve(nDOFsTriangle);
@@ -2569,14 +2295,14 @@ void CFEMStandardElement::DataStandardPyramid(void) {
 
   unsigned short mPoly = nPoly;
   unsigned int ii = 0;
-  for(unsigned short k=0; k<=nPoly; ++k, --mPoly) {
-    for(unsigned short j=0; j<=mPoly; ++j) {
-      for(unsigned short i=0; i<=mPoly; ++i, ++ii) {
-        if(k == 0)     connFace0.push_back(ii);
-        if(j == 0)     connFace1.push_back(ii);
-        if(j == mPoly) connFace2.push_back(ii);
-        if(i == 0)     connFace3.push_back(ii);
-        if(i == mPoly) connFace4.push_back(ii);
+  for (unsigned short k = 0; k <= nPoly; ++k, --mPoly) {
+    for (unsigned short j = 0; j <= mPoly; ++j) {
+      for (unsigned short i = 0; i <= mPoly; ++i, ++ii) {
+        if (k == 0) connFace0.push_back(ii);
+        if (j == 0) connFace1.push_back(ii);
+        if (j == mPoly) connFace2.push_back(ii);
+        if (i == 0) connFace3.push_back(ii);
+        if (i == mPoly) connFace4.push_back(ii);
       }
     }
   }
@@ -2584,9 +2310,9 @@ void CFEMStandardElement::DataStandardPyramid(void) {
   /*--- Make sure that the element is to the left of the faces. ---*/
   unsigned short n0 = 0;
   unsigned short n1 = nPoly;
-  unsigned short n2 = nDOFsQuad -1;
+  unsigned short n2 = nDOFsQuad - 1;
   unsigned short n3 = n2 - nPoly;
-  unsigned short n4 = nDOFs -1;
+  unsigned short n4 = nDOFs - 1;
 
   ChangeDirectionQuadConn(connFace0, n0, n1, n2, n3);
   ChangeDirectionTriangleConn(connFace1, n0, n4, n1);
@@ -2605,23 +2331,17 @@ void CFEMStandardElement::DataStandardPyramid(void) {
 }
 
 void CFEMStandardElement::DataStandardPrism(void) {
-
   /*--- Determine the Lagrangian basis functions and its derivatives
         in the integration points. ---*/
   vector<su2double> matVandermondeInvDummy;
-  LagrangianBasisFunctionAndDerivativesPrism(nPoly, rIntegration,
-                                             sIntegration, tIntegration,
-                                             nDOFs, rDOFs, sDOFs, tDOFs,
-                                             matVandermondeInvDummy,
-                                             lagBasisIntegration,
-                                             drLagBasisIntegration,
-                                             dsLagBasisIntegration,
-                                             dtLagBasisIntegration);
+  LagrangianBasisFunctionAndDerivativesPrism(nPoly, rIntegration, sIntegration, tIntegration, nDOFs, rDOFs, sDOFs,
+                                             tDOFs, matVandermondeInvDummy, lagBasisIntegration, drLagBasisIntegration,
+                                             dsLagBasisIntegration, dtLagBasisIntegration);
 
   /*--- Determine the local connectivity of the five faces of the prism.
         For a prism there are two triangular faces and three quadrilateral faces. ---*/
-  unsigned short nDOFsQuad     = (nPoly+1)*(nPoly+1);
-  unsigned short nDOFsTriangle = (nPoly+1)*(nPoly+2)/2;
+  unsigned short nDOFsQuad = (nPoly + 1) * (nPoly + 1);
+  unsigned short nDOFsTriangle = (nPoly + 1) * (nPoly + 2) / 2;
 
   connFace0.reserve(nDOFsTriangle);
   connFace1.reserve(nDOFsTriangle);
@@ -2630,15 +2350,15 @@ void CFEMStandardElement::DataStandardPrism(void) {
   connFace4.reserve(nDOFsQuad);
 
   unsigned int ii = 0;
-  for(unsigned short k=0; k<=nPoly; ++k) {
-    for(unsigned short j=0; j<=nPoly; ++j) {
+  for (unsigned short k = 0; k <= nPoly; ++k) {
+    for (unsigned short j = 0; j <= nPoly; ++j) {
       unsigned short uppBoundI = nPoly - j;
-      for(unsigned short i=0; i<=uppBoundI; ++i, ++ii) {
-        if(k == 0)         connFace0.push_back(ii);
-        if(k == nPoly)     connFace1.push_back(ii);
-        if(j == 0)         connFace2.push_back(ii);
-        if(i == 0)         connFace3.push_back(ii);
-        if((i+j) == nPoly) connFace4.push_back(ii);
+      for (unsigned short i = 0; i <= uppBoundI; ++i, ++ii) {
+        if (k == 0) connFace0.push_back(ii);
+        if (k == nPoly) connFace1.push_back(ii);
+        if (j == 0) connFace2.push_back(ii);
+        if (i == 0) connFace3.push_back(ii);
+        if ((i + j) == nPoly) connFace4.push_back(ii);
       }
     }
   }
@@ -2646,10 +2366,10 @@ void CFEMStandardElement::DataStandardPrism(void) {
   /*--- Make sure that the element is to the left of the faces. ---*/
   unsigned short n0 = 0;
   unsigned short n1 = nPoly;
-  unsigned short n2 = nDOFsTriangle -1;
-  unsigned short n3 = n0 + nDOFsTriangle*nPoly;
-  unsigned short n4 = n1 + nDOFsTriangle*nPoly;
-  unsigned short n5 = n2 + nDOFsTriangle*nPoly;
+  unsigned short n2 = nDOFsTriangle - 1;
+  unsigned short n3 = n0 + nDOFsTriangle * nPoly;
+  unsigned short n4 = n1 + nDOFsTriangle * nPoly;
+  unsigned short n5 = n2 + nDOFsTriangle * nPoly;
 
   ChangeDirectionTriangleConn(connFace0, n0, n1, n2);
   ChangeDirectionTriangleConn(connFace1, n3, n5, n4);
@@ -2668,22 +2388,16 @@ void CFEMStandardElement::DataStandardPrism(void) {
 }
 
 void CFEMStandardElement::DataStandardHexahedron(void) {
-
   /*--- Determine the Lagrangian basis functions and its derivatives
         in the integration points. ---*/
   vector<su2double> matVandermondeInvDummy;
-  LagrangianBasisFunctionAndDerivativesHexahedron(nPoly, rIntegration,
-                                                  sIntegration, tIntegration,
-                                                  nDOFs, rDOFs, sDOFs, tDOFs,
-                                                  matVandermondeInvDummy,
-                                                  lagBasisIntegration,
-                                                  drLagBasisIntegration,
-                                                  dsLagBasisIntegration,
-                                                  dtLagBasisIntegration);
+  LagrangianBasisFunctionAndDerivativesHexahedron(nPoly, rIntegration, sIntegration, tIntegration, nDOFs, rDOFs, sDOFs,
+                                                  tDOFs, matVandermondeInvDummy, lagBasisIntegration,
+                                                  drLagBasisIntegration, dsLagBasisIntegration, dtLagBasisIntegration);
 
   /*--- Determine the local connectivity of the six faces of the hexahedron.
         For a hexahedron the faces are all quadrilateral faces. ---*/
-  unsigned short nDOFsQuad = (nPoly+1)*(nPoly+1);
+  unsigned short nDOFsQuad = (nPoly + 1) * (nPoly + 1);
 
   connFace0.reserve(nDOFsQuad);
   connFace1.reserve(nDOFsQuad);
@@ -2693,15 +2407,15 @@ void CFEMStandardElement::DataStandardHexahedron(void) {
   connFace5.reserve(nDOFsQuad);
 
   unsigned int ii = 0;
-  for(unsigned short k=0; k<=nPoly; ++k) {
-    for(unsigned short j=0; j<=nPoly; ++j) {
-      for(unsigned short i=0; i<=nPoly; ++i, ++ii) {
-        if(k == 0)     connFace0.push_back(ii);
-        if(k == nPoly) connFace1.push_back(ii);
-        if(j == 0)     connFace2.push_back(ii);
-        if(j == nPoly) connFace3.push_back(ii);
-        if(i == 0)     connFace4.push_back(ii);
-        if(i == nPoly) connFace5.push_back(ii);
+  for (unsigned short k = 0; k <= nPoly; ++k) {
+    for (unsigned short j = 0; j <= nPoly; ++j) {
+      for (unsigned short i = 0; i <= nPoly; ++i, ++ii) {
+        if (k == 0) connFace0.push_back(ii);
+        if (k == nPoly) connFace1.push_back(ii);
+        if (j == 0) connFace2.push_back(ii);
+        if (j == nPoly) connFace3.push_back(ii);
+        if (i == 0) connFace4.push_back(ii);
+        if (i == nPoly) connFace5.push_back(ii);
       }
     }
   }
@@ -2709,12 +2423,12 @@ void CFEMStandardElement::DataStandardHexahedron(void) {
   /*--- Make sure that the element is to the left of the faces. ---*/
   unsigned short n0 = 0;
   unsigned short n1 = nPoly;
-  unsigned short n2 = nDOFsQuad -1;
+  unsigned short n2 = nDOFsQuad - 1;
   unsigned short n3 = n2 - nPoly;
-  unsigned short n4 = n0 + nDOFsQuad*nPoly;
-  unsigned short n5 = n1 + nDOFsQuad*nPoly;
-  unsigned short n6 = n2 + nDOFsQuad*nPoly;
-  unsigned short n7 = n3 + nDOFsQuad*nPoly;
+  unsigned short n4 = n0 + nDOFsQuad * nPoly;
+  unsigned short n5 = n1 + nDOFsQuad * nPoly;
+  unsigned short n6 = n2 + nDOFsQuad * nPoly;
+  unsigned short n7 = n3 + nDOFsQuad * nPoly;
 
   ChangeDirectionQuadConn(connFace0, n0, n1, n2, n3);
   ChangeDirectionQuadConn(connFace1, n4, n7, n6, n5);
@@ -2734,20 +2448,17 @@ void CFEMStandardElement::DataStandardHexahedron(void) {
 }
 
 void CFEMStandardElement::SubConnTetrahedron(void) {
-
   /*--- Initialize the number of DOFs for the current edges to the number of
         DOFs of the edges present in the tetrahedron. Also initialize the
         current k offset to zero.    ---*/
   unsigned short nDOFsCurrentEdges = nPoly + 1;
-  unsigned short offCurrentK       = 0;
+  unsigned short offCurrentK = 0;
 
   /*--- Loop in the k-direction of the tetrahedron, which is along the edge
         from the first vertex to the last vertex of the tet.    ---*/
-  for(unsigned short k=0; k<nPoly; ++k) {
-
+  for (unsigned short k = 0; k < nPoly; ++k) {
     /*--- Determine the offset for the next k. ---*/
-    unsigned short offNextK = offCurrentK
-                            + nDOFsCurrentEdges*(nDOFsCurrentEdges+1)/2;
+    unsigned short offNextK = offCurrentK + nDOFsCurrentEdges * (nDOFsCurrentEdges + 1) / 2;
 
     /*--------------------------------------------------------------------------
        Step 1: The tetrahedron at the end of the current i-edge.
@@ -2768,40 +2479,39 @@ void CFEMStandardElement::SubConnTetrahedron(void) {
                just created. These prisms are subdivided into tetrahedra.
       ------------------------------------------------------------------------*/
 
-    for(unsigned short i=0; i<(nDOFsCurrentEdges-2); ++i) {
-
+    for (unsigned short i = 0; i < (nDOFsCurrentEdges - 2); ++i) {
       /*--- Determine the lowest j-index on the current i-line that contributes
             to the subprism. Convert that index to the local vertex number in
             the tetrahedron.     ---*/
-      unsigned short j = nDOFsCurrentEdges-2 -i;
-      n0 = j*nDOFsCurrentEdges + i - j*(j-1)/2 + offCurrentK;
+      unsigned short j = nDOFsCurrentEdges - 2 - i;
+      n0 = j * nDOFsCurrentEdges + i - j * (j - 1) / 2 + offCurrentK;
 
       /*--- Increment the j index to obtain the n1 vertex of the subprism. ---*/
       ++j;
-      n1 = j*nDOFsCurrentEdges + i - j*(j-1)/2 + offCurrentK;
+      n1 = j * nDOFsCurrentEdges + i - j * (j - 1) / 2 + offCurrentK;
 
       /*--- The n2 vertex of the prism is located on the next k-level.
             The i-index remains the same, but the j index must be adapted, because
             the number of DOFs on the edges on the next k-level is one less. ---*/
-      j  = nDOFsCurrentEdges-2 -i;
-      n2 = j*(nDOFsCurrentEdges-1) + i - j*(j-1)/2 + offNextK;
+      j = nDOFsCurrentEdges - 2 - i;
+      n2 = j * (nDOFsCurrentEdges - 1) + i - j * (j - 1) / 2 + offNextK;
 
       /*--- The n3 vertex is part of the upper triangle of the prism. Hence the
             i-index must be incremented by one, stored in ii. The j-index must
             be computed accordingly and converted to the 1D numbering. ---*/
-      unsigned short ii = i+1;
-      j  = nDOFsCurrentEdges-2 -ii;
-      n3 = j*nDOFsCurrentEdges + ii - j*(j-1)/2 + offCurrentK;
+      unsigned short ii = i + 1;
+      j = nDOFsCurrentEdges - 2 - ii;
+      n3 = j * nDOFsCurrentEdges + ii - j * (j - 1) / 2 + offCurrentK;
 
       /*--- Increment the j index to obtain the n4 vertex of the subprism. ---*/
       ++j;
-      unsigned short n4 = j*nDOFsCurrentEdges + ii - j*(j-1)/2 + offCurrentK;
+      unsigned short n4 = j * nDOFsCurrentEdges + ii - j * (j - 1) / 2 + offCurrentK;
 
       /*--- The n5 vertex of the prism is located on the next k-level.
             The i-index remains the same, but the j index must be adapted, because
             the number of DOFs on the edges on the next k-level is one less. ---*/
-      j  = nDOFsCurrentEdges-2 -ii;
-      unsigned short n5 = j*(nDOFsCurrentEdges-1) + ii - j*(j-1)/2 + offNextK;
+      j = nDOFsCurrentEdges - 2 - ii;
+      unsigned short n5 = j * (nDOFsCurrentEdges - 1) + ii - j * (j - 1) / 2 + offNextK;
 
       /*--- Divide the subprism into 3 subtetrahedra. ---*/
       subConn1ForPlotting.push_back(n0);
@@ -2825,26 +2535,29 @@ void CFEMStandardElement::SubConnTetrahedron(void) {
                hexas. These are subdivided into tetrahedra again.
       ------------------------------------------------------------------------*/
 
-    for(unsigned short i=0; i<(nDOFsCurrentEdges-2); ++i) {
-
+    for (unsigned short i = 0; i < (nDOFsCurrentEdges - 2); ++i) {
       /*--- Define the variables n4 to n7, because these indices will be used
             again for the prism treated after the hexahedra. ---*/
       unsigned short n4, n5, n6, n7;
 
       /*--- Initialize n3, n2, n7 and n6 to the quad on the line j = 0. ---*/
-      n3 = offCurrentK + i; n2 = n3 + 1;
-      n7 = offNextK    + i; n6 = n7 + 1;
+      n3 = offCurrentK + i;
+      n2 = n3 + 1;
+      n7 = offNextK + i;
+      n6 = n7 + 1;
 
       /*--- Loop in the j-direction for the hexahedra on this i-row. ---*/
-      for(unsigned short j=0; j<(nDOFsCurrentEdges-3-i); ++j) {
-
+      for (unsigned short j = 0; j < (nDOFsCurrentEdges - 3 - i); ++j) {
         /*--- Set the values of n0, n1, n4 and n5 from the previous hex. ---*/
-        n0 = n3; n1 = n2; n4 = n7; n5 = n6;
+        n0 = n3;
+        n1 = n2;
+        n4 = n7;
+        n5 = n6;
 
         /*--- Nodes n3 and n7 are the j-neighbors of n0 and n4 respectively.
               Convert these (i,j,k) indices to the 1D index again. ---*/
-        n3 = (j+1)*nDOFsCurrentEdges + i - j*(j+1)/2 + offCurrentK;
-        n7 = (j+1)*(nDOFsCurrentEdges-1) + i - j*(j+1)/2 + offNextK;
+        n3 = (j + 1) * nDOFsCurrentEdges + i - j * (j + 1) / 2 + offCurrentK;
+        n7 = (j + 1) * (nDOFsCurrentEdges - 1) + i - j * (j + 1) / 2 + offNextK;
 
         /*--- Nodes n2 and n6 are the i-neighbors of n3 and n7 respectively.
               Just add an offset of 1 in the 1D numbering. ---*/
@@ -2896,10 +2609,10 @@ void CFEMStandardElement::SubConnTetrahedron(void) {
 
       /*--- Determine the j-index of the two remaining vertices and convert
             the (i,j,k) indices to the 1D index.     ---*/
-      unsigned short j = nDOFsCurrentEdges-2-i;
+      unsigned short j = nDOFsCurrentEdges - 2 - i;
 
-      n2 = j*nDOFsCurrentEdges + i - j*(j-1)/2 + offCurrentK;
-      n5 = j*(nDOFsCurrentEdges-1) + i - j*(j-1)/2 + offNextK;
+      n2 = j * nDOFsCurrentEdges + i - j * (j - 1) / 2 + offCurrentK;
+      n5 = j * (nDOFsCurrentEdges - 1) + i - j * (j - 1) / 2 + offNextK;
 
       /*--- Divide the prism in 3 tetrahedra and add their connectivity
             to the vector to store the subtetrahedra.     ---*/
@@ -2927,33 +2640,29 @@ void CFEMStandardElement::SubConnTetrahedron(void) {
 }
 
 void CFEMStandardElement::SubConnPyramid(void) {
-
   /*--- Initialize the number of DOFs for the current edges to the number of
         DOFs of the edges on the base of the pyramid. Also initialize the
         current k offset to zero.     ---*/
   unsigned short nDOFsCurrentEdges = nPoly + 1;
-  unsigned short offCurrentK       = 0;
+  unsigned short offCurrentK = 0;
 
   /*--- Loop in the k-direction of the pyramid. ---*/
-  for(unsigned short k=0; k<nPoly; ++k) {
-
+  for (unsigned short k = 0; k < nPoly; ++k) {
     /*--------------------------------------------------------------------------
        Sub-pyramids in the same direction as the original pyramid.
       ------------------------------------------------------------------------*/
 
     /*--- Determine the index of the first vertex of the quadrilateral of the
           next k value.    ---*/
-    unsigned short kk = offCurrentK + nDOFsCurrentEdges*nDOFsCurrentEdges;
+    unsigned short kk = offCurrentK + nDOFsCurrentEdges * nDOFsCurrentEdges;
 
     // Loop in j-direction of the current quad.
-    for(unsigned short j=0; j<(nDOFsCurrentEdges-1); ++j) {
-
+    for (unsigned short j = 0; j < (nDOFsCurrentEdges - 1); ++j) {
       /*--- Index of the first vertex along the j-row of the current quad. ---*/
-      unsigned short jj = offCurrentK + j*nDOFsCurrentEdges;
+      unsigned short jj = offCurrentK + j * nDOFsCurrentEdges;
 
       /*--- Loop in i-direction of the current quad. ---*/
-      for(unsigned short i=0; i<(nDOFsCurrentEdges-1); ++i) {
-
+      for (unsigned short i = 0; i < (nDOFsCurrentEdges - 1); ++i) {
         /*--- Determine the local indices of the corners of the quadrilateral
               of this subpyramid as well as the top of the subpyramid.
               Store the connectivity in subConn1ForPlotting.  ---*/
@@ -2980,24 +2689,22 @@ void CFEMStandardElement::SubConnPyramid(void) {
 
     /*--- Reset the value of kk to the index of the first vertex of the
           quadrilateral of the next k-plane.       ---*/
-    kk = offCurrentK + nDOFsCurrentEdges*nDOFsCurrentEdges;
+    kk = offCurrentK + nDOFsCurrentEdges * nDOFsCurrentEdges;
 
     /*--- Loop in j-direction of the current quad. Note that the starting index
           of this loop is 1.                       ---*/
-    for(unsigned short j=1; j<(nDOFsCurrentEdges-1); ++j) {
-
+    for (unsigned short j = 1; j < (nDOFsCurrentEdges - 1); ++j) {
       /*--- Index of the first vertex along the j-row of the current quad. ---*/
-      unsigned short jj = offCurrentK + j*nDOFsCurrentEdges;
+      unsigned short jj = offCurrentK + j * nDOFsCurrentEdges;
 
       /*--- Loop in the i-direction of this quad. Again the starting index is 1. ---*/
-      for(unsigned short i=1; i<(nDOFsCurrentEdges-1); ++i) {
-
+      for (unsigned short i = 1; i < (nDOFsCurrentEdges - 1); ++i) {
         /*--- Determine the local indices of the corners of the quadrilateral
               of this subpyramid as well as the top of the subpyramid.  ---*/
         unsigned short n0 = kk + i - 1;
         unsigned short n1 = n0 + 1;
-        unsigned short n2 = n1 + nDOFsCurrentEdges-1;
-        unsigned short n3 = n0 + nDOFsCurrentEdges-1;
+        unsigned short n2 = n1 + nDOFsCurrentEdges - 1;
+        unsigned short n3 = n0 + nDOFsCurrentEdges - 1;
         unsigned short n4 = jj + i;
 
         /*--- Store the connectivity of this subpyramid. Note that n1 and n3 are
@@ -3019,21 +2726,19 @@ void CFEMStandardElement::SubConnPyramid(void) {
       ------------------------------------------------------------------------*/
 
     /*--- Reset the value of kk again. ---*/
-    kk = offCurrentK + nDOFsCurrentEdges*nDOFsCurrentEdges;
+    kk = offCurrentK + nDOFsCurrentEdges * nDOFsCurrentEdges;
 
     /*--- Loop in the i-direction of the current quad. Note that the starting
           index must be 1.                         ---*/
-    for(unsigned short i=1; i<(nDOFsCurrentEdges-1); ++i) {
-
+    for (unsigned short i = 1; i < (nDOFsCurrentEdges - 1); ++i) {
       /*--- Loop in the j-direction of the current quad. This loop starts at 0. ---*/
-      for(unsigned short j=0; j<(nDOFsCurrentEdges-1); ++j) {
-
+      for (unsigned short j = 0; j < (nDOFsCurrentEdges - 1); ++j) {
         /*--- Determine the local indices of the 4 corner points of this tet.
               Its connectivity is stored in subConn2ForPlotting, because in
               subConn1ForPlotting the pyramids are stored. ---*/
-        unsigned short n0 = kk + i-1 + j*(nDOFsCurrentEdges-1);
+        unsigned short n0 = kk + i - 1 + j * (nDOFsCurrentEdges - 1);
         unsigned short n1 = n0 + 1;
-        unsigned short n2 = offCurrentK + i + j*nDOFsCurrentEdges;
+        unsigned short n2 = offCurrentK + i + j * nDOFsCurrentEdges;
         unsigned short n3 = n2 + nDOFsCurrentEdges;
 
         subConn2ForPlotting.push_back(n0);
@@ -3049,19 +2754,17 @@ void CFEMStandardElement::SubConnPyramid(void) {
 
     /*--- Loop in the j-direction of the current quad. Note that the starting
           index must be 1.                          ---*/
-    for(unsigned short j=1; j<(nDOFsCurrentEdges-1); ++j) {
-
+    for (unsigned short j = 1; j < (nDOFsCurrentEdges - 1); ++j) {
       /*--- Index of the first vertex along the j-row of the current quad. ---*/
-      unsigned short jj = offCurrentK + j*nDOFsCurrentEdges;
+      unsigned short jj = offCurrentK + j * nDOFsCurrentEdges;
 
       /*--- Loop in the i-direction of the current quad. This loop starts at 0. ---*/
-      for(unsigned short i=0; i<(nDOFsCurrentEdges-1); ++i) {
-
+      for (unsigned short i = 0; i < (nDOFsCurrentEdges - 1); ++i) {
         /*--- Determine the local indices of the 4 corner points of this tet
               and store its connectivity in subConn2ForPlotting.   ---*/
         unsigned short n0 = kk + i;
         unsigned short n1 = jj + i;
-        unsigned short n2 = n0 + nDOFsCurrentEdges-1;
+        unsigned short n2 = n0 + nDOFsCurrentEdges - 1;
         unsigned short n3 = n1 + 1;
 
         subConn2ForPlotting.push_back(n0);
@@ -3077,37 +2780,32 @@ void CFEMStandardElement::SubConnPyramid(void) {
     /*--- Update the value of offCurrentK with the amounts of DOFs present in the
           current quadrilateral plane and decrement nDOFsCurrentEdges, such that it
           contains the number of DOFs along an edge of the next quadrilateral plane. ---*/
-    offCurrentK += nDOFsCurrentEdges*nDOFsCurrentEdges;
+    offCurrentK += nDOFsCurrentEdges * nDOFsCurrentEdges;
     --nDOFsCurrentEdges;
   }
 }
 
 void CFEMStandardElement::SubConnPrism(void) {
-
   /*--- Determine the number of DOFs for a triangle. This is the offset in
         k-direction, the structured direction of a prisms.    ---*/
-  unsigned short nDOFTria = (nPoly+1)*(nPoly+2)/2;
+  unsigned short nDOFTria = (nPoly + 1) * (nPoly + 2) / 2;
 
   /*--- Loop in k-direction, which is the structured direction of the prism. ---*/
-  for(unsigned short k=0; k<nPoly; ++k) {
-
+  for (unsigned short k = 0; k < nPoly; ++k) {
     /*--- Initialize the counter jj to the ID of the first vertex for this
           k-value. jj contains the ID of the first vertex on the "0-2 edge"
           of the current bottom triangle.                 ---*/
-    unsigned short jj = k*nDOFTria;
+    unsigned short jj = k * nDOFTria;
 
     /*--- Loop over subedges of the left boundary of the standard triangle. ---*/
-    for(unsigned short j=0; j<nPoly; ++j) {
-
+    for (unsigned short j = 0; j < nPoly; ++j) {
       /*--- Check if the "down" elements must be written. ---*/
-      if( j ) {
-
+      if (j) {
         /*--- Determine the offset of the relevant DOF on the previous row. ---*/
         unsigned short kk = jj - (nPoly + 1 - j);
 
         /*--- Loop over the edges of this row. ---*/
-        for(unsigned short i=0; i<(nPoly-j); ++i) {
-
+        for (unsigned short i = 0; i < (nPoly - j); ++i) {
           /*--- Determine the local connectivity of this subelement and add
                 it to subConn1ForPlotting.           ---*/
           unsigned short n0 = jj + i;
@@ -3131,8 +2829,7 @@ void CFEMStandardElement::SubConnPrism(void) {
       unsigned short kk = jj + (nPoly + 1 - j);
 
       /*--- Loop over the edges of this row. ---*/
-      for(unsigned short i=0; i<(nPoly-j); ++i) {
-
+      for (unsigned short i = 0; i < (nPoly - j); ++i) {
         /*--- Determine the local connectivity of this subelement and add
               it to subConn1ForPlotting.           ---*/
         unsigned short n0 = jj + i;
@@ -3157,26 +2854,22 @@ void CFEMStandardElement::SubConnPrism(void) {
 }
 
 void CFEMStandardElement::SubConnHexahedron(void) {
-
   /*--- Determine the nodal offset in j- and k-direction. ---*/
-  unsigned short jOff = nPoly+1;
-  unsigned short kOff = jOff*jOff;
+  unsigned short jOff = nPoly + 1;
+  unsigned short kOff = jOff * jOff;
 
   /*--- Loop over the subelements in k-direction. ---*/
-  for(unsigned short k=0; k<nPoly; ++k) {
-
+  for (unsigned short k = 0; k < nPoly; ++k) {
     /*--- Abbreviate the offset in k-direction used in the connectivity. ---*/
-    unsigned short kk = k*kOff;
+    unsigned short kk = k * kOff;
 
     /*--- Loop over the subelements in j-direction. ---*/
-    for(unsigned short j=0; j<nPoly; ++j) {
-
+    for (unsigned short j = 0; j < nPoly; ++j) {
       /*--- Abbreviate the offset in j-direction used in the connectivity. ---*/
-      unsigned short jj = j*jOff;
+      unsigned short jj = j * jOff;
 
       /*--- Loop over the subelements in i-direction. ---*/
-      for(unsigned short i=0; i<nPoly; ++i) {
-
+      for (unsigned short i = 0; i < nPoly; ++i) {
         /*--- Determine the 8 vertices of this subhexahedron and store
               them in subConn1ForPlotting.           ---*/
         unsigned short n0 = kk + jj + i;
@@ -3202,23 +2895,37 @@ void CFEMStandardElement::SubConnHexahedron(void) {
 }
 
 unsigned short CFEMStandardElement::GetNDOFsPerSubElem(unsigned short val_VTK_Type) const {
-
   /*--- Distinguish between the possible element types for a linear
    sub-element and set the nDOFs accordingly. ---*/
-  unsigned short nDOFsSubElem = 0;   // To avoid a compiler warning.
-  switch( val_VTK_Type ) {
-    case NONE:          nDOFsSubElem = 0; break;
-    case LINE:          nDOFsSubElem = 2; break;
-    case TRIANGLE:      nDOFsSubElem = 3; break;
-    case QUADRILATERAL: nDOFsSubElem = 4; break;
-    case TETRAHEDRON:   nDOFsSubElem = 4; break;
-    case PYRAMID:       nDOFsSubElem = 5; break;
-    case PRISM:         nDOFsSubElem = 6; break;
-    case HEXAHEDRON:    nDOFsSubElem = 8; break;
+  unsigned short nDOFsSubElem = 0;  // To avoid a compiler warning.
+  switch (val_VTK_Type) {
+    case NONE:
+      nDOFsSubElem = 0;
+      break;
+    case LINE:
+      nDOFsSubElem = 2;
+      break;
+    case TRIANGLE:
+      nDOFsSubElem = 3;
+      break;
+    case QUADRILATERAL:
+      nDOFsSubElem = 4;
+      break;
+    case TETRAHEDRON:
+      nDOFsSubElem = 4;
+      break;
+    case PYRAMID:
+      nDOFsSubElem = 5;
+      break;
+    case PRISM:
+      nDOFsSubElem = 6;
+      break;
+    case HEXAHEDRON:
+      nDOFsSubElem = 8;
+      break;
     default:
       ostringstream message;
-      message << "Impossible FEM sub element type, " << val_VTK_Type
-              << ", encountered.";
+      message << "Impossible FEM sub element type, " << val_VTK_Type << ", encountered.";
       SU2_MPI::Error(message.str(), CURRENT_FUNCTION);
   }
 
@@ -3226,16 +2933,13 @@ unsigned short CFEMStandardElement::GetNDOFsPerSubElem(unsigned short val_VTK_Ty
   return nDOFsSubElem;
 }
 
-void CFEMStandardElement::ChangeDirectionQuadConn(vector<unsigned short> &connQuad,
-                                                  unsigned short         vert0,
-                                                  unsigned short         vert1,
-                                                  unsigned short         vert2,
-                                                  unsigned short         vert3) const {
-
+void CFEMStandardElement::ChangeDirectionQuadConn(vector<unsigned short>& connQuad, unsigned short vert0,
+                                                  unsigned short vert1, unsigned short vert2,
+                                                  unsigned short vert3) const {
   /*--- Determine the indices of the 4 corner vertices of the quad. ---*/
   unsigned short ind0 = 0;
   unsigned short ind1 = nPoly;
-  unsigned short ind2 = (nPoly+1)*(nPoly+1) -1;
+  unsigned short ind2 = (nPoly + 1) * (nPoly + 1) - 1;
   unsigned short ind3 = ind2 - nPoly;
 
   /*--- There exists a linear mapping from the indices of the numbering used in the
@@ -3247,125 +2951,113 @@ void CFEMStandardElement::ChangeDirectionQuadConn(vector<unsigned short> &connQu
         determined below. The bool verticesDontMatch is there to check if vertices
         do not match. This should not happen, but it is checked for security. ---*/
 
-  signed short a=0, b=0, c=0, d=0, e=0, f=0;  // Initialization to avoid a compiler warning.
+  signed short a = 0, b = 0, c = 0, d = 0, e = 0, f = 0;  // Initialization to avoid a compiler warning.
   bool verticesDontMatch = false;
 
-  if(vert0 == connQuad[ind0]) {
-
+  if (vert0 == connQuad[ind0]) {
     /*--- Vert0 coincides with the first vertex of the face connectivity.
           Set the coefficients a and d accordingly.   ---*/
     a = d = 0;
-    if(vert2 != connQuad[ind2]) verticesDontMatch = true;
+    if (vert2 != connQuad[ind2]) verticesDontMatch = true;
 
     /*--- Check the situation for the neighboring vertices. ---*/
-    if(vert1 == connQuad[ind1]) {
-
+    if (vert1 == connQuad[ind1]) {
       /*--- The vertex numbering is the same for both faces. ---*/
-      if(vert3 != connQuad[ind3]) verticesDontMatch = true;
-
-      b = f = 1; c = e = 0;
-    }
-    else if(vert1 == connQuad[ind3]) {
+      if (vert3 != connQuad[ind3]) verticesDontMatch = true;
 
+      b = f = 1;
+      c = e = 0;
+    } else if (vert1 == connQuad[ind3]) {
       /*--- The i and j numbering are swapped. ---*/
-      if(vert3 != connQuad[ind1]) verticesDontMatch = true;
+      if (vert3 != connQuad[ind1]) verticesDontMatch = true;
 
-      b = f = 0; c = e = 1;
-    }
-    else {
+      b = f = 0;
+      c = e = 1;
+    } else {
       verticesDontMatch = true;
     }
-  }
-  else if(vert1 == connQuad[ind0]) {
-
+  } else if (vert1 == connQuad[ind0]) {
     /*--- Vert1 coincides with the first vertex of the face connectivity.
           Set the coefficients a and d accordingly.  ---*/
-    a = nPoly; d = 0;
-    if(vert3 != connQuad[ind2]) verticesDontMatch = true;
+    a = nPoly;
+    d = 0;
+    if (vert3 != connQuad[ind2]) verticesDontMatch = true;
 
     /*--- Check the situation for the neighboring vertices. ---*/
-    if(vert0 == connQuad[ind1]) {
-
+    if (vert0 == connQuad[ind1]) {
       /*--- The i-direction is negated while the j-direction coincides. ---*/
-      if(vert2 != connQuad[ind3]) verticesDontMatch = true;
-
-      b = -1; f = 1; c = e = 0;
-    }
-    else if(vert0 == connQuad[ind3]) {
+      if (vert2 != connQuad[ind3]) verticesDontMatch = true;
 
+      b = -1;
+      f = 1;
+      c = e = 0;
+    } else if (vert0 == connQuad[ind3]) {
       /*--- The j-direction of the current face corresponds with the negative
             i-direction of the target, while the i-direction coincides with
             the j-direction of the target.     ---*/
-      if(vert2 != connQuad[ind1]) verticesDontMatch = true;
+      if (vert2 != connQuad[ind1]) verticesDontMatch = true;
 
-      b = f = 0; c = -1; e = 1;
-    }
-    else {
+      b = f = 0;
+      c = -1;
+      e = 1;
+    } else {
       verticesDontMatch = true;
     }
-  }
-  else if(vert2 == connQuad[ind0]) {
-
+  } else if (vert2 == connQuad[ind0]) {
     /*--- Vert2 coincides with the first vertex of the face connectivity.
           Set the coefficients a and d accordingly.  ---*/
     a = d = nPoly;
-    if(vert0 != connQuad[ind2]) verticesDontMatch = true;
+    if (vert0 != connQuad[ind2]) verticesDontMatch = true;
 
     /*--- Check the situation for the neighboring vertices. ---*/
-    if(vert1 == connQuad[ind3]) {
-
+    if (vert1 == connQuad[ind3]) {
       /*--- Both the i and j-direction are negated. ---*/
-      if(vert3 != connQuad[ind1]) verticesDontMatch = true;
-
-      b = f = -1; c = e = 0;
-    }
-    else if(vert1 == connQuad[ind1]) {
+      if (vert3 != connQuad[ind1]) verticesDontMatch = true;
 
+      b = f = -1;
+      c = e = 0;
+    } else if (vert1 == connQuad[ind1]) {
       /*--- The i and j-direction are negated and swapped. ---*/
-      if(vert3 != connQuad[ind3]) verticesDontMatch = true;
+      if (vert3 != connQuad[ind3]) verticesDontMatch = true;
 
-      b = f = 0; c = e = -1;
-    }
-    else {
+      b = f = 0;
+      c = e = -1;
+    } else {
       verticesDontMatch = true;
     }
-  }
-  else if(vert3 == connQuad[ind0]) {
-
+  } else if (vert3 == connQuad[ind0]) {
     /*--- Vert3 coincides with the first vertex of the face connectivity.
           Set the coefficients a and d accordingly.  ---*/
-    a = 0; d = nPoly;
-    if(vert1 != connQuad[ind2]) verticesDontMatch = true;
+    a = 0;
+    d = nPoly;
+    if (vert1 != connQuad[ind2]) verticesDontMatch = true;
 
     /*--- Check the situation for the neighboring vertices. ---*/
-    if(vert0 == connQuad[ind3]) {
-
+    if (vert0 == connQuad[ind3]) {
       /*--- The i-direction coincides while the j-direction is negated. ---*/
-      if(vert2 != connQuad[ind1]) verticesDontMatch = true;
-
-      b = 1; f = -1; c = e = 0;
-    }
-    else if(vert0 == connQuad[ind1]) {
+      if (vert2 != connQuad[ind1]) verticesDontMatch = true;
 
+      b = 1;
+      f = -1;
+      c = e = 0;
+    } else if (vert0 == connQuad[ind1]) {
       /*--- The j-direction of the current face corresponds with the i-direction
             of the target, while the i-direction coincides with the negative
             j-direction of the target.    ---*/
-      if(vert2 != connQuad[ind3]) verticesDontMatch = true;
+      if (vert2 != connQuad[ind3]) verticesDontMatch = true;
 
-      b = f = 0; c = 1; e = -1;
-    }
-    else {
+      b = f = 0;
+      c = 1;
+      e = -1;
+    } else {
       verticesDontMatch = true;
     }
-  }
-  else {
+  } else {
     verticesDontMatch = true;
   }
 
   /*--- If non-matching vertices have been found, terminate with an error message. ---*/
-  if( verticesDontMatch )
-    SU2_MPI::Error("Corner vertices do not match. This should not happen.",
-                   CURRENT_FUNCTION);
+  if (verticesDontMatch) SU2_MPI::Error("Corner vertices do not match. This should not happen.", CURRENT_FUNCTION);
 
   /*--- Copy the connectivity, such that things works out correctly when carrying
         out the renumbering.      ---*/
@@ -3373,30 +3065,26 @@ void CFEMStandardElement::ChangeDirectionQuadConn(vector<unsigned short> &connQu
 
   /*--- Loop over the vertices of the original face to copy the connectivity data. ---*/
   unsigned short ind = 0;
-  for(unsigned short j=0; j<=nPoly; ++j) {
-    for(unsigned short i=0; i<=nPoly; ++i, ++ind) {
-
+  for (unsigned short j = 0; j <= nPoly; ++j) {
+    for (unsigned short i = 0; i <= nPoly; ++i, ++ind) {
       /*--- Determine the ii and jj indices of the target, convert it to
             a 1D index and shore the modified index in connQuad. ---*/
-      unsigned short ii = a + i*b + j*c;
-      unsigned short jj = d + i*e + j*f;
+      unsigned short ii = a + i * b + j * c;
+      unsigned short jj = d + i * e + j * f;
 
-      unsigned short iind = jj*(nPoly+1) + ii;
+      unsigned short iind = jj * (nPoly + 1) + ii;
 
       connQuad[iind] = connQuadOr[ind];
     }
   }
 }
 
-void CFEMStandardElement::ChangeDirectionTriangleConn(vector<unsigned short> &connTriangle,
-                                                      unsigned short         vert0,
-                                                      unsigned short         vert1,
-                                                      unsigned short         vert2) const {
-
+void CFEMStandardElement::ChangeDirectionTriangleConn(vector<unsigned short>& connTriangle, unsigned short vert0,
+                                                      unsigned short vert1, unsigned short vert2) const {
   /*--- Determine the indices of the 3 corner vertices of the triangle. ---*/
   unsigned short ind0 = 0;
   unsigned short ind1 = nPoly;
-  unsigned short ind2 = (nPoly+1)*(nPoly+2)/2 -1;
+  unsigned short ind2 = (nPoly + 1) * (nPoly + 2) / 2 - 1;
 
   /*--- There exists a linear mapping from the indices of the numbering used in the
         connectivity of this face to the indices of the target numbering. This
@@ -3406,88 +3094,98 @@ void CFEMStandardElement::ChangeDirectionTriangleConn(vector<unsigned short> &co
         depend on how the corner points coincide with each other. This is
         determined below. The bool verticesDontMatch is there to check if vertices
         do not match. This should not happen, but it is checked for security. ---*/
-  signed short a=0, b=0, c=0, d=0, e=0, f=0;
+  signed short a = 0, b = 0, c = 0, d = 0, e = 0, f = 0;
   bool verticesDontMatch = false;
 
-  if(vert0 == connTriangle[ind0]) {
-
+  if (vert0 == connTriangle[ind0]) {
     /*--- Vert0 coincides with the first vertex of the face connectivity.
           Check the situation for the neighboring vertices.  ---*/
-    if(vert1 == connTriangle[ind1]) {
-
+    if (vert1 == connTriangle[ind1]) {
       /*--- The vertex numbering is the same for both faces. ---*/
-      if(vert2 != connTriangle[ind2]) verticesDontMatch = true;
-
-      a = 0; b = 1; c = 0; d = 0; e = 0; f = 1;
-    }
-    else if(vert1 == connTriangle[ind2]) {
-
+      if (vert2 != connTriangle[ind2]) verticesDontMatch = true;
+
+      a = 0;
+      b = 1;
+      c = 0;
+      d = 0;
+      e = 0;
+      f = 1;
+    } else if (vert1 == connTriangle[ind2]) {
       /*--- The ii-index corresponds to the j-index and the
             jj-index corresponds to i-index.    ---*/
-      if(vert2 != connTriangle[ind1]) verticesDontMatch = true;
-
-      a = 0; b = 0; c = 1; d = 0; e = 1; f = 0;
-    }
-    else {
+      if (vert2 != connTriangle[ind1]) verticesDontMatch = true;
+
+      a = 0;
+      b = 0;
+      c = 1;
+      d = 0;
+      e = 1;
+      f = 0;
+    } else {
       verticesDontMatch = true;
     }
-  }
-  else if(vert0 == connTriangle[ind1]) {
-
+  } else if (vert0 == connTriangle[ind1]) {
     /*--- Vert0 coincides with the second vertex of the face connectivity.
           Check the situation for the neighboring vertices.    ---*/
-    if(vert1 == connTriangle[ind0]) {
-
+    if (vert1 == connTriangle[ind0]) {
       /*--- The ii-index corresponds to a combination of the i and j index
             and the jj-index corresponds to the j-index.   ---*/
-      if(vert2 != connTriangle[ind2]) verticesDontMatch = true;
-
-      a = nPoly; b = -1; c = -1; d = 0; e = 0; f = 1;
-    }
-    else if(vert1 == connTriangle[ind2]) {
-
+      if (vert2 != connTriangle[ind2]) verticesDontMatch = true;
+
+      a = nPoly;
+      b = -1;
+      c = -1;
+      d = 0;
+      e = 0;
+      f = 1;
+    } else if (vert1 == connTriangle[ind2]) {
       /*--- The jj-index corresponds to a combination of the i and j index
             and the ii-index corresponds to the j-index.  ---*/
-      if(vert2 != connTriangle[ind0]) verticesDontMatch = true;
-
-      a = 0; b = 0; c = 1; d = nPoly; e = -1; f = -1;
-    }
-    else {
+      if (vert2 != connTriangle[ind0]) verticesDontMatch = true;
+
+      a = 0;
+      b = 0;
+      c = 1;
+      d = nPoly;
+      e = -1;
+      f = -1;
+    } else {
       verticesDontMatch = true;
     }
-  }
-  else if(vert0 == connTriangle[ind2]) {
-
+  } else if (vert0 == connTriangle[ind2]) {
     /*--- Vert0 coincides with the third vertex of the face connectivity.
           Check the situation for the neighboring vertices.    ---*/
-    if(vert1 == connTriangle[ind0]) {
-
+    if (vert1 == connTriangle[ind0]) {
       /*--- The ii-index corresponds to a combination of the i and j index
             and the jj-index corresponds with the i-index.  ---*/
-      if(vert2 != connTriangle[ind1]) verticesDontMatch = true;
-
-      a = nPoly; b = -1; c = -1; d = 0; e = 1; f = 0;
-    }
-    else if(vert1 == connTriangle[ind1]) {
-
+      if (vert2 != connTriangle[ind1]) verticesDontMatch = true;
+
+      a = nPoly;
+      b = -1;
+      c = -1;
+      d = 0;
+      e = 1;
+      f = 0;
+    } else if (vert1 == connTriangle[ind1]) {
       /*--- The jj-index corresponds to a combination of the i and j index
             and the ii-index corresponds with the i-index.   ---*/
-      if(vert2 != connTriangle[ind0]) verticesDontMatch = true;
-
-      a = 0; b = 1; c = 0; d = nPoly; e = -1; f = -1;
-    }
-    else {
+      if (vert2 != connTriangle[ind0]) verticesDontMatch = true;
+
+      a = 0;
+      b = 1;
+      c = 0;
+      d = nPoly;
+      e = -1;
+      f = -1;
+    } else {
       verticesDontMatch = true;
     }
-  }
-  else {
+  } else {
     verticesDontMatch = true;
   }
 
   /*--- If non-matching vertices have been found, terminate with an error message. ---*/
-  if( verticesDontMatch )
-    SU2_MPI::Error("Corner vertices do not match. This should not happen.",
-                   CURRENT_FUNCTION);
+  if (verticesDontMatch) SU2_MPI::Error("Corner vertices do not match. This should not happen.", CURRENT_FUNCTION);
 
   /*--- Copy the connectivity, such that things works out correctly when carrying
         out the renumbering.  ---*/
@@ -3495,15 +3193,14 @@ void CFEMStandardElement::ChangeDirectionTriangleConn(vector<unsigned short> &co
 
   /*--- Loop over the vertices of the original face to copy the connectivity data. ---*/
   unsigned short ind = 0;
-  for(unsigned short j=0; j<=nPoly; ++j) {
-    for(unsigned short i=0; i<=(nPoly-j); ++i, ++ind) {
-
+  for (unsigned short j = 0; j <= nPoly; ++j) {
+    for (unsigned short i = 0; i <= (nPoly - j); ++i, ++ind) {
       /*--- Determine the ii and jj indices of the target, convert it to
             a 1D index and shore the modified index in connTriangle. ---*/
-      unsigned short ii = a + i*b + j*c;
-      unsigned short jj = d + i*e + j*f;
+      unsigned short ii = a + i * b + j * c;
+      unsigned short jj = d + i * e + j * f;
 
-      unsigned short iind = jj*(nPoly+1) + ii - jj*(jj-1)/2;
+      unsigned short iind = jj * (nPoly + 1) + ii - jj * (jj - 1) / 2;
 
       connTriangle[iind] = connTriangleOr[ind];
     }
@@ -3514,25 +3211,19 @@ void CFEMStandardElement::ChangeDirectionTriangleConn(vector<unsigned short> &co
 /*         Public member functions of CFEMStandardInternalFace.                     */
 /*----------------------------------------------------------------------------------*/
 
-CFEMStandardInternalFace::CFEMStandardInternalFace(unsigned short val_VTK_TypeFace,
-                                                   unsigned short val_VTK_TypeSide0,
-                                                   unsigned short val_nPolySide0,
-                                                   unsigned short val_VTK_TypeSide1,
-                                                   unsigned short val_nPolySide1,
-                                                   bool           val_constJac,
-                                                   bool           val_swapFaceInElementSide0,
-                                                   bool           val_swapFaceInElementSide1,
-                                                   CConfig        *config,
-                                                   unsigned short val_orderExact)
-
-  : CFEMStandardElementBase(val_VTK_TypeFace, max(val_nPolySide0, val_nPolySide1),
-                            val_constJac, config, val_orderExact) {
+CFEMStandardInternalFace::CFEMStandardInternalFace(unsigned short val_VTK_TypeFace, unsigned short val_VTK_TypeSide0,
+                                                   unsigned short val_nPolySide0, unsigned short val_VTK_TypeSide1,
+                                                   unsigned short val_nPolySide1, bool val_constJac,
+                                                   bool val_swapFaceInElementSide0, bool val_swapFaceInElementSide1,
+                                                   CConfig* config, unsigned short val_orderExact)
 
+    : CFEMStandardElementBase(val_VTK_TypeFace, max(val_nPolySide0, val_nPolySide1), val_constJac, config,
+                              val_orderExact) {
   /*--- Copy the function arguments to the member variables. ---*/
-  nPolyElemSide0         = val_nPolySide0;
-  VTK_TypeElemSide0      = val_VTK_TypeSide0;
-  nPolyElemSide1         = val_nPolySide1;
-  VTK_TypeElemSide1      = val_VTK_TypeSide1;
+  nPolyElemSide0 = val_nPolySide0;
+  VTK_TypeElemSide0 = val_VTK_TypeSide0;
+  nPolyElemSide1 = val_nPolySide1;
+  VTK_TypeElemSide1 = val_VTK_TypeSide1;
   swapFaceInElementSide0 = val_swapFaceInElementSide0;
   swapFaceInElementSide1 = val_swapFaceInElementSide1;
 
@@ -3549,49 +3240,35 @@ CFEMStandardInternalFace::CFEMStandardInternalFace(unsigned short val_VTK_TypeFa
 
   /*--- Determine the Lagrangian basis functions and its gradients in the
         integration points for both sides of the face. ---*/
-  switch( VTK_Type ) {
+  switch (VTK_Type) {
     case LINE:
-      LagrangianBasisFunctionAndDerivativesLine(nPolyElemSide0, rIntegration, nDOFsFaceSide0,
-                                                rDOFsFaceSide0, matVandermondeInvDummy,
-                                                lagBasisFaceIntegrationSide0,
+      LagrangianBasisFunctionAndDerivativesLine(nPolyElemSide0, rIntegration, nDOFsFaceSide0, rDOFsFaceSide0,
+                                                matVandermondeInvDummy, lagBasisFaceIntegrationSide0,
                                                 drLagBasisFaceIntegrationSide0);
-      LagrangianBasisFunctionAndDerivativesLine(nPolyElemSide1, rIntegration, nDOFsFaceSide1,
-                                                rDOFsFaceSide1, matVandermondeInvDummy,
-                                                lagBasisFaceIntegrationSide1,
+      LagrangianBasisFunctionAndDerivativesLine(nPolyElemSide1, rIntegration, nDOFsFaceSide1, rDOFsFaceSide1,
+                                                matVandermondeInvDummy, lagBasisFaceIntegrationSide1,
                                                 drLagBasisFaceIntegrationSide1);
       break;
 
     case TRIANGLE:
-      LagrangianBasisFunctionAndDerivativesTriangle(nPolyElemSide0, rIntegration,
-                                                    sIntegration,   nDOFsFaceSide0,
-                                                    rDOFsFaceSide0, sDOFsFaceSide0,
-                                                    matVandermondeInvDummy,
-                                                    lagBasisFaceIntegrationSide0,
-                                                    drLagBasisFaceIntegrationSide0,
+      LagrangianBasisFunctionAndDerivativesTriangle(nPolyElemSide0, rIntegration, sIntegration, nDOFsFaceSide0,
+                                                    rDOFsFaceSide0, sDOFsFaceSide0, matVandermondeInvDummy,
+                                                    lagBasisFaceIntegrationSide0, drLagBasisFaceIntegrationSide0,
                                                     dsLagBasisFaceIntegrationSide0);
-      LagrangianBasisFunctionAndDerivativesTriangle(nPolyElemSide1, rIntegration,
-                                                    sIntegration,   nDOFsFaceSide1,
-                                                    rDOFsFaceSide1, sDOFsFaceSide1,
-                                                    matVandermondeInvDummy,
-                                                    lagBasisFaceIntegrationSide1,
-                                                    drLagBasisFaceIntegrationSide1,
+      LagrangianBasisFunctionAndDerivativesTriangle(nPolyElemSide1, rIntegration, sIntegration, nDOFsFaceSide1,
+                                                    rDOFsFaceSide1, sDOFsFaceSide1, matVandermondeInvDummy,
+                                                    lagBasisFaceIntegrationSide1, drLagBasisFaceIntegrationSide1,
                                                     dsLagBasisFaceIntegrationSide1);
       break;
 
     case QUADRILATERAL:
-      LagrangianBasisFunctionAndDerivativesQuadrilateral(nPolyElemSide0, rIntegration,
-                                                         sIntegration,   nDOFsFaceSide0,
-                                                         rDOFsFaceSide0, sDOFsFaceSide0,
-                                                         matVandermondeInvDummy,
-                                                         lagBasisFaceIntegrationSide0,
-                                                         drLagBasisFaceIntegrationSide0,
+      LagrangianBasisFunctionAndDerivativesQuadrilateral(nPolyElemSide0, rIntegration, sIntegration, nDOFsFaceSide0,
+                                                         rDOFsFaceSide0, sDOFsFaceSide0, matVandermondeInvDummy,
+                                                         lagBasisFaceIntegrationSide0, drLagBasisFaceIntegrationSide0,
                                                          dsLagBasisFaceIntegrationSide0);
-      LagrangianBasisFunctionAndDerivativesQuadrilateral(nPolyElemSide1, rIntegration,
-                                                         sIntegration,   nDOFsFaceSide1,
-                                                         rDOFsFaceSide0, sDOFsFaceSide1,
-                                                         matVandermondeInvDummy,
-                                                         lagBasisFaceIntegrationSide1,
-                                                         drLagBasisFaceIntegrationSide1,
+      LagrangianBasisFunctionAndDerivativesQuadrilateral(nPolyElemSide1, rIntegration, sIntegration, nDOFsFaceSide1,
+                                                         rDOFsFaceSide0, sDOFsFaceSide1, matVandermondeInvDummy,
+                                                         lagBasisFaceIntegrationSide1, drLagBasisFaceIntegrationSide1,
                                                          dsLagBasisFaceIntegrationSide1);
       break;
   }
@@ -3603,85 +3280,67 @@ CFEMStandardInternalFace::CFEMStandardInternalFace(unsigned short val_VTK_TypeFa
   /*--- Create the transpose versions of lagBasisFaceIntegrationSide0 and
         lagBasisFaceIntegrationSide1. These are needed for an efficient computation
         of the residual of the faces. ---*/
-  lagBasisFaceIntegrationTransposeSide0.resize(nIntegration*nDOFsFaceSide0);
-  lagBasisFaceIntegrationTransposeSide1.resize(nIntegration*nDOFsFaceSide1);
+  lagBasisFaceIntegrationTransposeSide0.resize(nIntegration * nDOFsFaceSide0);
+  lagBasisFaceIntegrationTransposeSide1.resize(nIntegration * nDOFsFaceSide1);
 
   unsigned int ii = 0;
-  for(unsigned short j=0; j<nDOFsFaceSide0; ++j) {
-    for(unsigned short i=0; i<nIntegration; ++i, ++ii) {
-      const unsigned int ind = i*nDOFsFaceSide0 + j;
+  for (unsigned short j = 0; j < nDOFsFaceSide0; ++j) {
+    for (unsigned short i = 0; i < nIntegration; ++i, ++ii) {
+      const unsigned int ind = i * nDOFsFaceSide0 + j;
       lagBasisFaceIntegrationTransposeSide0[ii] = lagBasisFaceIntegrationSide0[ind];
     }
   }
 
   ii = 0;
-  for(unsigned short j=0; j<nDOFsFaceSide1; ++j) {
-    for(unsigned short i=0; i<nIntegration; ++i, ++ii) {
-      const unsigned int ind = i*nDOFsFaceSide1 + j;
+  for (unsigned short j = 0; j < nDOFsFaceSide1; ++j) {
+    for (unsigned short i = 0; i < nIntegration; ++i, ++ii) {
+      const unsigned int ind = i * nDOFsFaceSide1 + j;
       lagBasisFaceIntegrationTransposeSide1[ii] = lagBasisFaceIntegrationSide1[ind];
     }
   }
 
   /*--- Check the sum of the derivatives of the Lagrangian basis functions. ---*/
-  if( !drLagBasisFaceIntegrationSide0.empty() )
-    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsFaceSide0,
-                                                drLagBasisFaceIntegrationSide0);
-  if( !dsLagBasisFaceIntegrationSide0.empty() )
-    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsFaceSide0,
-                                                dsLagBasisFaceIntegrationSide0);
-  if( !drLagBasisFaceIntegrationSide1.empty() )
-    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsFaceSide1,
-                                                drLagBasisFaceIntegrationSide1);
-  if( !dsLagBasisFaceIntegrationSide1.empty() )
-    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsFaceSide1,
-                                                dsLagBasisFaceIntegrationSide1);
+  if (!drLagBasisFaceIntegrationSide0.empty())
+    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsFaceSide0, drLagBasisFaceIntegrationSide0);
+  if (!dsLagBasisFaceIntegrationSide0.empty())
+    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsFaceSide0, dsLagBasisFaceIntegrationSide0);
+  if (!drLagBasisFaceIntegrationSide1.empty())
+    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsFaceSide1, drLagBasisFaceIntegrationSide1);
+  if (!dsLagBasisFaceIntegrationSide1.empty())
+    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsFaceSide1, dsLagBasisFaceIntegrationSide1);
 
   /*--- Determine the derivatives of the Lagrangian basis functions of the
         adjacent elements in the integration points of the face for both sides
         of the face. ---*/
-  DerivativesBasisFunctionsAdjacentElement(VTK_TypeElemSide0, nPolyElemSide0,
-                                           swapFaceInElementSide0,
-                                           nDOFsElemSide0,
-                                           drLagBasisElemIntegrationSide0,
-                                           dsLagBasisElemIntegrationSide0,
+  DerivativesBasisFunctionsAdjacentElement(VTK_TypeElemSide0, nPolyElemSide0, swapFaceInElementSide0, nDOFsElemSide0,
+                                           drLagBasisElemIntegrationSide0, dsLagBasisElemIntegrationSide0,
                                            dtLagBasisElemIntegrationSide0);
 
-  DerivativesBasisFunctionsAdjacentElement(VTK_TypeElemSide1, nPolyElemSide1,
-                                           swapFaceInElementSide1,
-                                           nDOFsElemSide1,
-                                           drLagBasisElemIntegrationSide1,
-                                           dsLagBasisElemIntegrationSide1,
+  DerivativesBasisFunctionsAdjacentElement(VTK_TypeElemSide1, nPolyElemSide1, swapFaceInElementSide1, nDOFsElemSide1,
+                                           drLagBasisElemIntegrationSide1, dsLagBasisElemIntegrationSide1,
                                            dtLagBasisElemIntegrationSide1);
 
   /*--- Check the sum of the derivatives of the Lagrangian basis functions. ---*/
-  if( !drLagBasisElemIntegrationSide0.empty() )
-    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsElemSide0,
-                                                drLagBasisElemIntegrationSide0);
-  if( !dsLagBasisElemIntegrationSide0.empty() )
-    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsElemSide0,
-                                                dsLagBasisElemIntegrationSide0);
-  if( !dtLagBasisElemIntegrationSide0.empty() )
-    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsElemSide0,
-                                                dtLagBasisElemIntegrationSide0);
-
-  if( !drLagBasisElemIntegrationSide1.empty() )
-    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsElemSide1,
-                                                drLagBasisElemIntegrationSide1);
-  if( !dsLagBasisElemIntegrationSide1.empty() )
-    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsElemSide1,
-                                                dsLagBasisElemIntegrationSide1);
-  if( !dtLagBasisElemIntegrationSide1.empty() )
-    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsElemSide1,
-                                                dtLagBasisElemIntegrationSide1);
+  if (!drLagBasisElemIntegrationSide0.empty())
+    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsElemSide0, drLagBasisElemIntegrationSide0);
+  if (!dsLagBasisElemIntegrationSide0.empty())
+    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsElemSide0, dsLagBasisElemIntegrationSide0);
+  if (!dtLagBasisElemIntegrationSide0.empty())
+    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsElemSide0, dtLagBasisElemIntegrationSide0);
+
+  if (!drLagBasisElemIntegrationSide1.empty())
+    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsElemSide1, drLagBasisElemIntegrationSide1);
+  if (!dsLagBasisElemIntegrationSide1.empty())
+    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsElemSide1, dsLagBasisElemIntegrationSide1);
+  if (!dtLagBasisElemIntegrationSide1.empty())
+    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsElemSide1, dtLagBasisElemIntegrationSide1);
 
   /*--- If the BLAS routines are used it is beneficial to store all the
         derivatives of the element basis functions in one array. ---*/
-  unsigned long sizeMatSide0 = drLagBasisElemIntegrationSide0.size()
-                             + dsLagBasisElemIntegrationSide0.size()
-                             + dtLagBasisElemIntegrationSide0.size();
-  unsigned long sizeMatSide1 = drLagBasisElemIntegrationSide1.size()
-                             + dsLagBasisElemIntegrationSide1.size()
-                             + dtLagBasisElemIntegrationSide1.size();
+  unsigned long sizeMatSide0 = drLagBasisElemIntegrationSide0.size() + dsLagBasisElemIntegrationSide0.size() +
+                               dtLagBasisElemIntegrationSide0.size();
+  unsigned long sizeMatSide1 = drLagBasisElemIntegrationSide1.size() + dsLagBasisElemIntegrationSide1.size() +
+                               dtLagBasisElemIntegrationSide1.size();
 
   matDerBasisElemIntegrationSide0.resize(sizeMatSide0);
   matDerBasisElemIntegrationSide1.resize(sizeMatSide1);
@@ -3690,23 +3349,23 @@ CFEMStandardInternalFace::CFEMStandardInternalFace(unsigned short val_VTK_TypeFa
   matDerBasisElemIntegrationTransposeSide1.resize(sizeMatSide1);
 
   ii = 0;
-  for(unsigned long i=0; i<drLagBasisElemIntegrationSide0.size(); ++i, ++ii)
+  for (unsigned long i = 0; i < drLagBasisElemIntegrationSide0.size(); ++i, ++ii)
     matDerBasisElemIntegrationSide0[ii] = drLagBasisElemIntegrationSide0[i];
 
-  for(unsigned long i=0; i<dsLagBasisElemIntegrationSide0.size(); ++i, ++ii)
+  for (unsigned long i = 0; i < dsLagBasisElemIntegrationSide0.size(); ++i, ++ii)
     matDerBasisElemIntegrationSide0[ii] = dsLagBasisElemIntegrationSide0[i];
 
-  for(unsigned long i=0; i<dtLagBasisElemIntegrationSide0.size(); ++i, ++ii)
+  for (unsigned long i = 0; i < dtLagBasisElemIntegrationSide0.size(); ++i, ++ii)
     matDerBasisElemIntegrationSide0[ii] = dtLagBasisElemIntegrationSide0[i];
 
   ii = 0;
-  for(unsigned long i=0; i<drLagBasisElemIntegrationSide1.size(); ++i, ++ii)
+  for (unsigned long i = 0; i < drLagBasisElemIntegrationSide1.size(); ++i, ++ii)
     matDerBasisElemIntegrationSide1[ii] = drLagBasisElemIntegrationSide1[i];
 
-  for(unsigned long i=0; i<dsLagBasisElemIntegrationSide1.size(); ++i, ++ii)
+  for (unsigned long i = 0; i < dsLagBasisElemIntegrationSide1.size(); ++i, ++ii)
     matDerBasisElemIntegrationSide1[ii] = dsLagBasisElemIntegrationSide1[i];
 
-  for(unsigned long i=0; i<dtLagBasisElemIntegrationSide1.size(); ++i, ++ii)
+  for (unsigned long i = 0; i < dtLagBasisElemIntegrationSide1.size(); ++i, ++ii)
     matDerBasisElemIntegrationSide1[ii] = dtLagBasisElemIntegrationSide1[i];
 
   /*--- Also create the transpose of the matDerBasisElemIntegrationSide0 and
@@ -3715,42 +3374,39 @@ CFEMStandardInternalFace::CFEMStandardInternalFace(unsigned short val_VTK_TypeFa
   const unsigned short nDim = dtLagBasisElemIntegrationSide0.size() ? 3 : 2;
 
   ii = 0;
-  for(unsigned short j=0; j<nDOFsElemSide0; ++j) {
-    for(unsigned short i=0; i<nIntegration; ++i) {
-      for(unsigned short iDim=0; iDim<nDim; ++iDim, ++ii) {
-        const unsigned int ind = iDim*nDOFsElemSide0*nIntegration + i*nDOFsElemSide0 + j;
+  for (unsigned short j = 0; j < nDOFsElemSide0; ++j) {
+    for (unsigned short i = 0; i < nIntegration; ++i) {
+      for (unsigned short iDim = 0; iDim < nDim; ++iDim, ++ii) {
+        const unsigned int ind = iDim * nDOFsElemSide0 * nIntegration + i * nDOFsElemSide0 + j;
         matDerBasisElemIntegrationTransposeSide0[ii] = matDerBasisElemIntegrationSide0[ind];
       }
     }
   }
 
   ii = 0;
-  for(unsigned short j=0; j<nDOFsElemSide1; ++j) {
-    for(unsigned short i=0; i<nIntegration; ++i) {
-      for(unsigned short iDim=0; iDim<nDim; ++iDim, ++ii) {
-        const unsigned int ind = iDim*nDOFsElemSide1*nIntegration + i*nDOFsElemSide1 + j;
+  for (unsigned short j = 0; j < nDOFsElemSide1; ++j) {
+    for (unsigned short i = 0; i < nIntegration; ++i) {
+      for (unsigned short iDim = 0; iDim < nDim; ++iDim, ++ii) {
+        const unsigned int ind = iDim * nDOFsElemSide1 * nIntegration + i * nDOFsElemSide1 + j;
         matDerBasisElemIntegrationTransposeSide1[ii] = matDerBasisElemIntegrationSide1[ind];
       }
     }
   }
 }
 
-bool CFEMStandardInternalFace::SameStandardMatchingFace(unsigned short val_VTK_TypeFace,
-                                                        bool           val_constJac,
-                                                        unsigned short val_VTK_TypeSide0,
-                                                        unsigned short val_nPolySide0,
-                                                        unsigned short val_VTK_TypeSide1,
-                                                        unsigned short val_nPolySide1,
-                                                        bool           val_swapFaceInElementSide0,
-                                                        bool           val_swapFaceInElementSide1) {
-  if(val_VTK_TypeFace           != VTK_Type)               return false;
-  if(val_constJac               != constJacobian)          return false;
-  if(val_VTK_TypeSide0          != VTK_TypeElemSide0)      return false;
-  if(val_nPolySide0             != nPolyElemSide0)         return false;
-  if(val_VTK_TypeSide1          != VTK_TypeElemSide1)      return false;
-  if(val_nPolySide1             != nPolyElemSide1)         return false;
-  if(val_swapFaceInElementSide0 != swapFaceInElementSide0) return false;
-  if(val_swapFaceInElementSide1 != swapFaceInElementSide1) return false;
+bool CFEMStandardInternalFace::SameStandardMatchingFace(unsigned short val_VTK_TypeFace, bool val_constJac,
+                                                        unsigned short val_VTK_TypeSide0, unsigned short val_nPolySide0,
+                                                        unsigned short val_VTK_TypeSide1, unsigned short val_nPolySide1,
+                                                        bool val_swapFaceInElementSide0,
+                                                        bool val_swapFaceInElementSide1) {
+  if (val_VTK_TypeFace != VTK_Type) return false;
+  if (val_constJac != constJacobian) return false;
+  if (val_VTK_TypeSide0 != VTK_TypeElemSide0) return false;
+  if (val_nPolySide0 != nPolyElemSide0) return false;
+  if (val_VTK_TypeSide1 != VTK_TypeElemSide1) return false;
+  if (val_nPolySide1 != nPolyElemSide1) return false;
+  if (val_swapFaceInElementSide0 != swapFaceInElementSide0) return false;
+  if (val_swapFaceInElementSide1 != swapFaceInElementSide1) return false;
 
   return true;
 }
@@ -3759,8 +3415,7 @@ bool CFEMStandardInternalFace::SameStandardMatchingFace(unsigned short val_VTK_T
 /*        Private member functions of CFEMStandardInternalFace.                     */
 /*----------------------------------------------------------------------------------*/
 
-void CFEMStandardInternalFace::Copy(const CFEMStandardInternalFace &other) {
-
+void CFEMStandardInternalFace::Copy(const CFEMStandardInternalFace& other) {
   CFEMStandardElementBase::Copy(other);
 
   nDOFsFaceSide0 = other.nDOFsFaceSide0;
@@ -3802,10 +3457,10 @@ void CFEMStandardInternalFace::Copy(const CFEMStandardInternalFace &other) {
   dtLagBasisElemIntegrationSide0 = other.dtLagBasisElemIntegrationSide0;
   dtLagBasisElemIntegrationSide1 = other.dtLagBasisElemIntegrationSide1;
 
-  matDerBasisElemIntegrationSide0          = other.matDerBasisElemIntegrationSide0;
+  matDerBasisElemIntegrationSide0 = other.matDerBasisElemIntegrationSide0;
   matDerBasisElemIntegrationTransposeSide0 = other.matDerBasisElemIntegrationTransposeSide0;
 
-  matDerBasisElemIntegrationSide1          = other.matDerBasisElemIntegrationSide1;
+  matDerBasisElemIntegrationSide1 = other.matDerBasisElemIntegrationSide1;
   matDerBasisElemIntegrationTransposeSide1 = other.matDerBasisElemIntegrationTransposeSide1;
 }
 
@@ -3813,20 +3468,15 @@ void CFEMStandardInternalFace::Copy(const CFEMStandardInternalFace &other) {
 /*         Public member functions of CFEMStandardBoundaryFace.                     */
 /*----------------------------------------------------------------------------------*/
 
-CFEMStandardBoundaryFace::CFEMStandardBoundaryFace(unsigned short val_VTK_TypeFace,
-                                                   unsigned short val_VTK_TypeElem,
-                                                   unsigned short val_nPolyElem,
-                                                   bool           val_constJac,
-                                                   bool           val_swapFaceInElement,
-                                                   CConfig        *config,
+CFEMStandardBoundaryFace::CFEMStandardBoundaryFace(unsigned short val_VTK_TypeFace, unsigned short val_VTK_TypeElem,
+                                                   unsigned short val_nPolyElem, bool val_constJac,
+                                                   bool val_swapFaceInElement, CConfig* config,
                                                    unsigned short val_orderExact)
 
-  : CFEMStandardElementBase(val_VTK_TypeFace, val_nPolyElem,
-                            val_constJac, config, val_orderExact) {
-
+    : CFEMStandardElementBase(val_VTK_TypeFace, val_nPolyElem, val_constJac, config, val_orderExact) {
   /*--- Copy the function arguments to the member variables. ---*/
-  nPolyElem         = val_nPolyElem;
-  VTK_TypeElem      = val_VTK_TypeElem;
+  nPolyElem = val_nPolyElem;
+  VTK_TypeElem = val_VTK_TypeElem;
   swapFaceInElement = val_swapFaceInElement;
 
   /*--- Create dummy variable to store inverse of Vandermonde matrix temporarily. ---*/
@@ -3840,34 +3490,24 @@ CFEMStandardBoundaryFace::CFEMStandardBoundaryFace(unsigned short val_VTK_TypeFa
   /*--- Determine the Lagrangian basis functions in the integration
         points of the face and the subconnectivity of the linear elements
         used for plotting. ---*/
-  switch( VTK_Type ) {
+  switch (VTK_Type) {
     case LINE:
-      LagrangianBasisFunctionAndDerivativesLine(nPolyElem, rIntegration, nDOFsFace,
-                                                rDOFsFace, matVandermondeInvDummy,
-                                                lagBasisFaceIntegration,
-                                                drLagBasisFaceIntegration);
+      LagrangianBasisFunctionAndDerivativesLine(nPolyElem, rIntegration, nDOFsFace, rDOFsFace, matVandermondeInvDummy,
+                                                lagBasisFaceIntegration, drLagBasisFaceIntegration);
       SubConnForPlottingLine(nPolyElem, subConnForPlotting);
       break;
 
     case TRIANGLE:
-      LagrangianBasisFunctionAndDerivativesTriangle(nPolyElem,    rIntegration,
-                                                    sIntegration, nDOFsFace,
-                                                    rDOFsFace,    sDOFsFace,
-                                                    matVandermondeInvDummy,
-                                                    lagBasisFaceIntegration,
-                                                    drLagBasisFaceIntegration,
-                                                    dsLagBasisFaceIntegration);
+      LagrangianBasisFunctionAndDerivativesTriangle(nPolyElem, rIntegration, sIntegration, nDOFsFace, rDOFsFace,
+                                                    sDOFsFace, matVandermondeInvDummy, lagBasisFaceIntegration,
+                                                    drLagBasisFaceIntegration, dsLagBasisFaceIntegration);
       SubConnForPlottingTriangle(nPolyElem, subConnForPlotting);
       break;
 
     case QUADRILATERAL:
-      LagrangianBasisFunctionAndDerivativesQuadrilateral(nPolyElem,    rIntegration,
-                                                         sIntegration, nDOFsFace,
-                                                         rDOFsFace,    sDOFsFace,
-                                                         matVandermondeInvDummy,
-                                                         lagBasisFaceIntegration,
-                                                         drLagBasisFaceIntegration,
-                                                         dsLagBasisFaceIntegration);
+      LagrangianBasisFunctionAndDerivativesQuadrilateral(nPolyElem, rIntegration, sIntegration, nDOFsFace, rDOFsFace,
+                                                         sDOFsFace, matVandermondeInvDummy, lagBasisFaceIntegration,
+                                                         drLagBasisFaceIntegration, dsLagBasisFaceIntegration);
       SubConnForPlottingQuadrilateral(nPolyElem, subConnForPlotting);
       break;
   }
@@ -3877,72 +3517,63 @@ CFEMStandardBoundaryFace::CFEMStandardBoundaryFace(unsigned short val_VTK_TypeFa
 
   /*--- Create the transpose version of lagBasisFaceIntegration. This is needed
         for an efficient computation of the residual of the faces. ---*/
-  lagBasisFaceIntegrationTranspose.resize(nIntegration*nDOFsFace);
+  lagBasisFaceIntegrationTranspose.resize(nIntegration * nDOFsFace);
 
   unsigned int ii = 0;
-  for(unsigned short j=0; j<nDOFsFace; ++j) {
-    for(unsigned short i=0; i<nIntegration; ++i, ++ii) {
-      const unsigned int ind = i*nDOFsFace + j;
+  for (unsigned short j = 0; j < nDOFsFace; ++j) {
+    for (unsigned short i = 0; i < nIntegration; ++i, ++ii) {
+      const unsigned int ind = i * nDOFsFace + j;
       lagBasisFaceIntegrationTranspose[ii] = lagBasisFaceIntegration[ind];
     }
   }
 
   /*--- Check the sum of the derivatives of the Lagrangian basis functions. ---*/
-  if( !drLagBasisFaceIntegration.empty() )
-    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsFace,
-                                                drLagBasisFaceIntegration);
-  if( !dsLagBasisFaceIntegration.empty() )
-    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsFace,
-                                                dsLagBasisFaceIntegration);
+  if (!drLagBasisFaceIntegration.empty())
+    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsFace, drLagBasisFaceIntegration);
+  if (!dsLagBasisFaceIntegration.empty())
+    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsFace, dsLagBasisFaceIntegration);
 
   /*--- Determine the derivatives of the Lagrangian basis functions of the
         adjacent element in the integration points of the face. ---*/
-  DerivativesBasisFunctionsAdjacentElement(VTK_TypeElem, nPolyElem,
-                                           swapFaceInElement,
-                                           nDOFsElem, drLagBasisElemIntegration,
-                                           dsLagBasisElemIntegration,
+  DerivativesBasisFunctionsAdjacentElement(VTK_TypeElem, nPolyElem, swapFaceInElement, nDOFsElem,
+                                           drLagBasisElemIntegration, dsLagBasisElemIntegration,
                                            dtLagBasisElemIntegration);
 
   /*--- Check the sum of the derivatives of the Lagrangian basis functions. ---*/
-  if( !drLagBasisElemIntegration.empty() )
-    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsElem,
-                                                drLagBasisElemIntegration);
-  if( !dsLagBasisElemIntegration.empty() )
-    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsElem,
-                                                dsLagBasisElemIntegration);
-  if( !dtLagBasisElemIntegration.empty() )
-    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsElem,
-                                                dtLagBasisElemIntegration);
+  if (!drLagBasisElemIntegration.empty())
+    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsElem, drLagBasisElemIntegration);
+  if (!dsLagBasisElemIntegration.empty())
+    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsElem, dsLagBasisElemIntegration);
+  if (!dtLagBasisElemIntegration.empty())
+    CheckSumDerivativesLagrangianBasisFunctions(nIntegration, nDOFsElem, dtLagBasisElemIntegration);
 
   /*--- If the BLAS routines are used it is beneficial to store all the
         derivatives of the element basis functions in one array. ---*/
-  unsigned long sizeMat = drLagBasisElemIntegration.size()
-                        + dsLagBasisElemIntegration.size()
-                        + dtLagBasisElemIntegration.size();
+  unsigned long sizeMat =
+      drLagBasisElemIntegration.size() + dsLagBasisElemIntegration.size() + dtLagBasisElemIntegration.size();
 
   matDerBasisElemIntegration.resize(sizeMat);
   matDerBasisElemIntegrationTranspose.resize(sizeMat);
 
   ii = 0;
-  for(unsigned long i=0; i<drLagBasisElemIntegration.size(); ++i, ++ii)
+  for (unsigned long i = 0; i < drLagBasisElemIntegration.size(); ++i, ++ii)
     matDerBasisElemIntegration[ii] = drLagBasisElemIntegration[i];
 
-  for(unsigned long i=0; i<dsLagBasisElemIntegration.size(); ++i, ++ii)
+  for (unsigned long i = 0; i < dsLagBasisElemIntegration.size(); ++i, ++ii)
     matDerBasisElemIntegration[ii] = dsLagBasisElemIntegration[i];
 
-  for(unsigned long i=0; i<dtLagBasisElemIntegration.size(); ++i, ++ii)
+  for (unsigned long i = 0; i < dtLagBasisElemIntegration.size(); ++i, ++ii)
     matDerBasisElemIntegration[ii] = dtLagBasisElemIntegration[i];
 
-
   /*--- Also create the transpose of the matDerBasisElemIntegration, such that
         the residual of the symmetrizing terms can be computed efficiently. ---*/
   const unsigned short nDim = dtLagBasisElemIntegration.size() ? 3 : 2;
 
   ii = 0;
-  for(unsigned short j=0; j<nDOFsElem; ++j) {
-    for(unsigned short i=0; i<nIntegration; ++i) {
-      for(unsigned short iDim=0; iDim<nDim; ++iDim, ++ii) {
-        const unsigned int ind = iDim*nDOFsElem*nIntegration + i*nDOFsElem + j;
+  for (unsigned short j = 0; j < nDOFsElem; ++j) {
+    for (unsigned short i = 0; i < nIntegration; ++i) {
+      for (unsigned short iDim = 0; iDim < nDim; ++iDim, ++ii) {
+        const unsigned int ind = iDim * nDOFsElem * nIntegration + i * nDOFsElem + j;
         matDerBasisElemIntegrationTranspose[ii] = matDerBasisElemIntegration[ind];
       }
     }
@@ -3950,18 +3581,22 @@ CFEMStandardBoundaryFace::CFEMStandardBoundaryFace(unsigned short val_VTK_TypeFa
 }
 
 unsigned short CFEMStandardBoundaryFace::GetNDOFsPerSubFace(void) const {
-
   /*--- Distinguish between the possible element types for a boundary surface
         and set the number nDOFs for a subface accordingly. ---*/
   unsigned short nDOFsSubface = 0;
-  switch( VTK_Type ) {
-    case LINE:          nDOFsSubface = 2; break;
-    case TRIANGLE:      nDOFsSubface = 3; break;
-    case QUADRILATERAL: nDOFsSubface = 4; break;
+  switch (VTK_Type) {
+    case LINE:
+      nDOFsSubface = 2;
+      break;
+    case TRIANGLE:
+      nDOFsSubface = 3;
+      break;
+    case QUADRILATERAL:
+      nDOFsSubface = 4;
+      break;
     default:
       ostringstream message;
-      message << "Impossible FEM surface element type, " << VTK_Type
-              << ", encountered.";
+      message << "Impossible FEM surface element type, " << VTK_Type << ", encountered.";
       SU2_MPI::Error(message.str(), CURRENT_FUNCTION);
   }
 
@@ -3969,16 +3604,14 @@ unsigned short CFEMStandardBoundaryFace::GetNDOFsPerSubFace(void) const {
   return nDOFsSubface;
 }
 
-bool CFEMStandardBoundaryFace::SameStandardBoundaryFace(unsigned short val_VTK_TypeFace,
-                                                        bool           val_constJac,
-                                                        unsigned short val_VTK_TypeElem,
-                                                        unsigned short val_nPolyElem,
-                                                        bool           val_swapFaceInElem) {
-  if(val_VTK_TypeFace   != VTK_Type)          return false;
-  if(val_constJac       != constJacobian)     return false;
-  if(val_VTK_TypeElem   != VTK_TypeElem)      return false;
-  if(val_nPolyElem      != nPolyElem)         return false;
-  if(val_swapFaceInElem != swapFaceInElement) return false;
+bool CFEMStandardBoundaryFace::SameStandardBoundaryFace(unsigned short val_VTK_TypeFace, bool val_constJac,
+                                                        unsigned short val_VTK_TypeElem, unsigned short val_nPolyElem,
+                                                        bool val_swapFaceInElem) {
+  if (val_VTK_TypeFace != VTK_Type) return false;
+  if (val_constJac != constJacobian) return false;
+  if (val_VTK_TypeElem != VTK_TypeElem) return false;
+  if (val_nPolyElem != nPolyElem) return false;
+  if (val_swapFaceInElem != swapFaceInElement) return false;
 
   return true;
 }
@@ -3987,14 +3620,13 @@ bool CFEMStandardBoundaryFace::SameStandardBoundaryFace(unsigned short val_VTK_T
 /*        Private member functions of CFEMStandardBoundaryFace.                     */
 /*----------------------------------------------------------------------------------*/
 
-void CFEMStandardBoundaryFace::Copy(const CFEMStandardBoundaryFace &other) {
-
+void CFEMStandardBoundaryFace::Copy(const CFEMStandardBoundaryFace& other) {
   CFEMStandardElementBase::Copy(other);
 
-  nDOFsFace         = other.nDOFsFace;
-  nPolyElem         = other.nPolyElem;
-  nDOFsElem         = other.nDOFsElem;
-  VTK_TypeElem      = other.VTK_TypeElem;
+  nDOFsFace = other.nDOFsFace;
+  nPolyElem = other.nPolyElem;
+  nDOFsElem = other.nDOFsElem;
+  VTK_TypeElem = other.VTK_TypeElem;
   swapFaceInElement = other.swapFaceInElement;
 
   penaltyConstantFace = other.penaltyConstantFace;
@@ -4002,16 +3634,16 @@ void CFEMStandardBoundaryFace::Copy(const CFEMStandardBoundaryFace &other) {
   rDOFsFace = other.rDOFsFace;
   sDOFsFace = other.sDOFsFace;
 
-  lagBasisFaceIntegration          = other.lagBasisFaceIntegration;
+  lagBasisFaceIntegration = other.lagBasisFaceIntegration;
   lagBasisFaceIntegrationTranspose = other.lagBasisFaceIntegrationTranspose;
-  drLagBasisFaceIntegration        = other.drLagBasisFaceIntegration;
-  dsLagBasisFaceIntegration        = other.dsLagBasisFaceIntegration;
+  drLagBasisFaceIntegration = other.drLagBasisFaceIntegration;
+  dsLagBasisFaceIntegration = other.dsLagBasisFaceIntegration;
 
   drLagBasisElemIntegration = other.drLagBasisElemIntegration;
   dsLagBasisElemIntegration = other.dsLagBasisElemIntegration;
   dtLagBasisElemIntegration = other.dtLagBasisElemIntegration;
 
-  matDerBasisElemIntegration          = other.matDerBasisElemIntegration;
+  matDerBasisElemIntegration = other.matDerBasisElemIntegration;
   matDerBasisElemIntegrationTranspose = other.matDerBasisElemIntegrationTranspose;
 
   subConnForPlotting = other.subConnForPlotting;
diff --git a/Common/src/fem/fem_wall_distance.cpp b/Common/src/fem/fem_wall_distance.cpp
index df4bd85391c..cd9920927e3 100644
--- a/Common/src/fem/fem_wall_distance.cpp
+++ b/Common/src/fem/fem_wall_distance.cpp
@@ -28,8 +28,7 @@
 #include "../../include/fem/fem_geometry_structure.hpp"
 #include "../../include/adt/CADTElemClass.hpp"
 
-std::unique_ptr<CADTElemClass> CMeshFEM_DG::ComputeViscousWallADT(const CConfig *config) const {
-
+std::unique_ptr<CADTElemClass> CMeshFEM_DG::ComputeViscousWallADT(const CConfig* config) const {
   /*--------------------------------------------------------------------------*/
   /*--- Step 1: Create the coordinates and connectivity of the linear      ---*/
   /*---         subelements of the local boundaries that must be taken     ---*/
@@ -50,38 +49,34 @@ std::unique_ptr<CADTElemClass> CMeshFEM_DG::ComputeViscousWallADT(const CConfig
   vector<unsigned short> markerIDs;
 
   /* Loop over the boundary markers. */
-  for(unsigned short iMarker=0; iMarker<boundaries.size(); ++iMarker) {
-    if( !boundaries[iMarker].periodicBoundary ) {
-
+  for (unsigned short iMarker = 0; iMarker < boundaries.size(); ++iMarker) {
+    if (!boundaries[iMarker].periodicBoundary) {
       /* Check for a viscous wall. */
-      if( (config->GetMarker_All_KindBC(iMarker) == HEAT_FLUX) ||
-          (config->GetMarker_All_KindBC(iMarker) == ISOTHERMAL) ) {
-
+      if ((config->GetMarker_All_KindBC(iMarker) == HEAT_FLUX) ||
+          (config->GetMarker_All_KindBC(iMarker) == ISOTHERMAL)) {
         /* Loop over the surface elements of this marker. */
-        const vector<CSurfaceElementFEM> &surfElem = boundaries[iMarker].surfElem;
-        for(unsigned long i=0; i<surfElem.size(); ++i) {
-
+        const vector<CSurfaceElementFEM>& surfElem = boundaries[iMarker].surfElem;
+        for (unsigned long i = 0; i < surfElem.size(); ++i) {
           /* Set the flag of the mesh points on this surface to true. */
-          for(unsigned short j=0; j<surfElem[i].nDOFsGrid; ++j)
-            meshToSurface[surfElem[i].DOFsGridFace[j]] = 1;
+          for (unsigned short j = 0; j < surfElem[i].nDOFsGrid; ++j) meshToSurface[surfElem[i].DOFsGridFace[j]] = 1;
 
           /* Determine the necessary data from the corresponding standard face,
              such as the number of linear subfaces, the number of DOFs per
              linear subface and the corresponding local connectivity. */
-          const unsigned short ind           = surfElem[i].indStandardElement;
-          const unsigned short VTK_Type      = standardBoundaryFacesGrid[ind].GetVTK_Type();
-          const unsigned short nSubFaces     = standardBoundaryFacesGrid[ind].GetNSubFaces();
-          const unsigned short nDOFsPerFace  = standardBoundaryFacesGrid[ind].GetNDOFsPerSubFace();
-          const unsigned short *connSubFaces = standardBoundaryFacesGrid[ind].GetSubFaceConn();
+          const unsigned short ind = surfElem[i].indStandardElement;
+          const unsigned short VTK_Type = standardBoundaryFacesGrid[ind].GetVTK_Type();
+          const unsigned short nSubFaces = standardBoundaryFacesGrid[ind].GetNSubFaces();
+          const unsigned short nDOFsPerFace = standardBoundaryFacesGrid[ind].GetNDOFsPerSubFace();
+          const unsigned short* connSubFaces = standardBoundaryFacesGrid[ind].GetSubFaceConn();
 
           /* Loop over the number of subfaces and store the required data. */
           unsigned short ii = 0;
-          for(unsigned short j=0; j<nSubFaces; ++j) {
+          for (unsigned short j = 0; j < nSubFaces; ++j) {
             markerIDs.push_back(iMarker);
             VTK_TypeElem.push_back(VTK_Type);
             elemIDs.push_back(i);
 
-            for(unsigned short k=0; k<nDOFsPerFace; ++k, ++ii)
+            for (unsigned short k = 0; k < nDOFsPerFace; ++k, ++ii)
               surfaceConn.push_back(surfElem[i].DOFsGridFace[connSubFaces[ii]]);
           }
         }
@@ -95,19 +90,17 @@ std::unique_ptr<CADTElemClass> CMeshFEM_DG::ComputeViscousWallADT(const CConfig
   vector<su2double> surfaceCoor;
   unsigned long nVertex_SolidWall = 0;
 
-  for(unsigned long i=0; i<meshPoints.size(); ++i) {
-    if( meshToSurface[i] ) {
+  for (unsigned long i = 0; i < meshPoints.size(); ++i) {
+    if (meshToSurface[i]) {
       meshToSurface[i] = nVertex_SolidWall++;
 
-      for(unsigned short k=0; k<nDim; ++k)
-        surfaceCoor.push_back(meshPoints[i].coor[k]);
+      for (unsigned short k = 0; k < nDim; ++k) surfaceCoor.push_back(meshPoints[i].coor[k]);
     }
   }
 
   /*--- Change the surface connectivity, such that it corresponds to
         the entries in surfaceCoor rather than in meshPoints. ---*/
-  for(unsigned long i=0; i<surfaceConn.size(); ++i)
-    surfaceConn[i] = meshToSurface[surfaceConn[i]];
+  for (unsigned long i = 0; i < surfaceConn.size(); ++i) surfaceConn[i] = meshToSurface[surfaceConn[i]];
 
   /*--------------------------------------------------------------------------*/
   /*--- Step 2: Build the ADT, which is an ADT of bounding boxes of the    ---*/
@@ -117,53 +110,47 @@ std::unique_ptr<CADTElemClass> CMeshFEM_DG::ComputeViscousWallADT(const CConfig
   /*--------------------------------------------------------------------------*/
 
   /* Build the ADT. */
-  std::unique_ptr<CADTElemClass> WallADT(new CADTElemClass(nDim, surfaceCoor, surfaceConn, VTK_TypeElem,
-                                                           markerIDs, elemIDs, true));
+  std::unique_ptr<CADTElemClass> WallADT(
+      new CADTElemClass(nDim, surfaceCoor, surfaceConn, VTK_TypeElem, markerIDs, elemIDs, true));
 
   return WallADT;
-
 }
 
 /*!
  * \brief Set wall distances a specific value
  */
-void CMeshFEM_DG::SetWallDistance(su2double val){
-
-  for(unsigned long l=0; l<nVolElemOwned; ++l) {
-
+void CMeshFEM_DG::SetWallDistance(su2double val) {
+  for (unsigned long l = 0; l < nVolElemOwned; ++l) {
     /* Get the required data from the corresponding standard element. */
-    const unsigned short ind  = volElem[l].indStandardElement;
+    const unsigned short ind = volElem[l].indStandardElement;
     const unsigned short nInt = standardElementsGrid[ind].GetNIntegration();
 
     /* Store the number of solDOFS a bit easier. */
-    const unsigned short nDOFsSol  = volElem[l].nDOFsSol;
+    const unsigned short nDOFsSol = volElem[l].nDOFsSol;
 
     /* Allocate the memory for the wall distance of this element. */
     volElem[l].wallDistance.resize(nInt, val);
     volElem[l].wallDistanceSolDOFs.resize(nDOFsSol, val);
-
   }
 
-  for(unsigned long l=0; l<matchingFaces.size(); ++l) {
+  for (unsigned long l = 0; l < matchingFaces.size(); ++l) {
     /* Get the required data from the corresponding standard element. */
-    const unsigned short ind   = matchingFaces[l].indStandardElement;
-    const unsigned short nInt  = standardMatchingFacesGrid[ind].GetNIntegration();
+    const unsigned short ind = matchingFaces[l].indStandardElement;
+    const unsigned short nInt = standardMatchingFacesGrid[ind].GetNIntegration();
 
     /* Allocate the memory for the wall distance for this matching face. */
     matchingFaces[l].wallDistance.resize(nInt, val);
   }
 
-  for(unsigned short iMarker=0; iMarker<boundaries.size(); ++iMarker) {
-    if( !boundaries[iMarker].periodicBoundary ) {
-
+  for (unsigned short iMarker = 0; iMarker < boundaries.size(); ++iMarker) {
+    if (!boundaries[iMarker].periodicBoundary) {
       /* Loop over the boundary faces and determine the wall distances
          in the integration points. */
-      vector<CSurfaceElementFEM> &surfElem = boundaries[iMarker].surfElem;
-      for(unsigned long l=0; l<surfElem.size(); ++l) {
-
+      vector<CSurfaceElementFEM>& surfElem = boundaries[iMarker].surfElem;
+      for (unsigned long l = 0; l < surfElem.size(); ++l) {
         /* Get the required data from the corresponding standard element. */
-        const unsigned short ind   = surfElem[l].indStandardElement;
-        const unsigned short nInt  = standardBoundaryFacesGrid[ind].GetNIntegration();
+        const unsigned short ind = surfElem[l].indStandardElement;
+        const unsigned short nInt = standardBoundaryFacesGrid[ind].GetNIntegration();
 
         /* Allocate the memory for the wall distance for this boundary face. */
         surfElem[l].wallDistance.resize(nInt, val);
@@ -172,8 +159,7 @@ void CMeshFEM_DG::SetWallDistance(su2double val){
   }
 }
 
-void CMeshFEM_DG::SetWallDistance(CADTElemClass *WallADT, const CConfig* config, unsigned short iZone){
-
+void CMeshFEM_DG::SetWallDistance(CADTElemClass* WallADT, const CConfig* config, unsigned short iZone) {
   /*--------------------------------------------------------------------------*/
   /*--- Step 3: Determine the wall distance of the integration points of   ---*/
   /*---         locally owned volume elements.                             ---*/
@@ -181,26 +167,23 @@ void CMeshFEM_DG::SetWallDistance(CADTElemClass *WallADT, const CConfig* config,
 
   /*--- Loop over the owned elements to compute the wall distance
         in the integration points. ---*/
-  for(unsigned long l=0; l<nVolElemOwned; ++l) {
-
+  for (unsigned long l = 0; l < nVolElemOwned; ++l) {
     /* Get the required data from the corresponding standard element. */
-    const unsigned short ind  = volElem[l].indStandardElement;
+    const unsigned short ind = volElem[l].indStandardElement;
     const unsigned short nInt = standardElementsGrid[ind].GetNIntegration();
 
     /* Allocate the memory for the wall distance of this element. */
     volElem[l].wallDistance.resize(nInt);
 
-    if( !WallADT->IsEmpty() ) {
-
+    if (!WallADT->IsEmpty()) {
       /*--- The tree is not empty. Loop over the integration points
             and determine the wall distance. ---*/
-      for(unsigned short i=0; i<nInt; ++i) {
-
-        const su2double *coor = volElem[l].coorIntegrationPoints.data() + i*nDim;
+      for (unsigned short i = 0; i < nInt; ++i) {
+        const su2double* coor = volElem[l].coorIntegrationPoints.data() + i * nDim;
         unsigned short markerID;
-        unsigned long  elemID;
-        int            rankID;
-        su2double      dist;
+        unsigned long elemID;
+        int rankID;
+        su2double dist;
         WallADT->DetermineNearestElement(coor, dist, markerID, elemID, rankID);
 
         volElem[l].wallDistance[i] = dist;
@@ -215,25 +198,22 @@ void CMeshFEM_DG::SetWallDistance(CADTElemClass *WallADT, const CConfig* config,
 
   /*--- Loop over the owned elements to compute the wall distance
         in the integration points. ---*/
-  for(unsigned long l=0; l<nVolElemOwned; ++l) {
-
+  for (unsigned long l = 0; l < nVolElemOwned; ++l) {
     /* Store the number of solDOFS a bit easier. */
-    const unsigned short nDOFsSol  = volElem[l].nDOFsSol;
+    const unsigned short nDOFsSol = volElem[l].nDOFsSol;
 
     /* Allocate the memory for the wall distance of the solution DOFs. */
     volElem[l].wallDistanceSolDOFs.resize(nDOFsSol);
 
-    if( !WallADT->IsEmpty() ) {
-
+    if (!WallADT->IsEmpty()) {
       /*--- The tree is not empty. Loop over the solution DOFs
             and determine the wall distance. ---*/
-      for(unsigned short i=0; i<nDOFsSol; ++i) {
-
-        const su2double *coor = volElem[l].coorSolDOFs.data() + i*nDim;
+      for (unsigned short i = 0; i < nDOFsSol; ++i) {
+        const su2double* coor = volElem[l].coorSolDOFs.data() + i * nDim;
         unsigned short markerID;
-        unsigned long  elemID;
-        int            rankID;
-        su2double      dist;
+        unsigned long elemID;
+        int rankID;
+        su2double dist;
         WallADT->DetermineNearestElement(coor, dist, markerID, elemID, rankID);
 
         volElem[l].wallDistanceSolDOFs[i] = dist;
@@ -246,27 +226,23 @@ void CMeshFEM_DG::SetWallDistance(CADTElemClass *WallADT, const CConfig* config,
   /*---         the internal matching faces.                               ---*/
   /*--------------------------------------------------------------------------*/
 
-  for(unsigned long l=0; l<matchingFaces.size(); ++l) {
-
+  for (unsigned long l = 0; l < matchingFaces.size(); ++l) {
     /* Get the required data from the corresponding standard element. */
-    const unsigned short ind   = matchingFaces[l].indStandardElement;
-    const unsigned short nInt  = standardMatchingFacesGrid[ind].GetNIntegration();
+    const unsigned short ind = matchingFaces[l].indStandardElement;
+    const unsigned short nInt = standardMatchingFacesGrid[ind].GetNIntegration();
 
     /* Allocate the memory for the wall distance for this matching face. */
     matchingFaces[l].wallDistance.resize(nInt);
 
-    if( !WallADT->IsEmpty() ) {
-
+    if (!WallADT->IsEmpty()) {
       /*--- The tree is not empty. Loop over the integration points
             and determine the wall distance. */
-      for(unsigned short i=0; i<nInt; ++i) {
-
-        const su2double *coor = matchingFaces[l].coorIntegrationPoints.data()
-                              + i*nDim;
+      for (unsigned short i = 0; i < nInt; ++i) {
+        const su2double* coor = matchingFaces[l].coorIntegrationPoints.data() + i * nDim;
         unsigned short markerID;
-        unsigned long  elemID;
-        int            rankID;
-        su2double      dist;
+        unsigned long elemID;
+        int rankID;
+        su2double dist;
         WallADT->DetermineNearestElement(coor, dist, markerID, elemID, rankID);
 
         matchingFaces[l].wallDistance[i] = dist;
@@ -281,44 +257,38 @@ void CMeshFEM_DG::SetWallDistance(CADTElemClass *WallADT, const CConfig* config,
 
   /*--- Loop over the boundary markers. Make sure to exclude the periodic
         boundaries, because these are not physical. ---*/
-  for(unsigned short iMarker=0; iMarker<boundaries.size(); ++iMarker) {
-    if( !boundaries[iMarker].periodicBoundary ) {
-
+  for (unsigned short iMarker = 0; iMarker < boundaries.size(); ++iMarker) {
+    if (!boundaries[iMarker].periodicBoundary) {
       /* Determine whether or not this is a viscous wall boundary. */
-      const bool viscousWall = config->GetMarker_All_KindBC(iMarker) == HEAT_FLUX ||
-                               config->GetMarker_All_KindBC(iMarker) == ISOTHERMAL;
+      const bool viscousWall =
+          config->GetMarker_All_KindBC(iMarker) == HEAT_FLUX || config->GetMarker_All_KindBC(iMarker) == ISOTHERMAL;
 
       /* Loop over the boundary faces and determine the wall distances
          in the integration points. */
-      vector<CSurfaceElementFEM> &surfElem = boundaries[iMarker].surfElem;
-      for(unsigned long l=0; l<surfElem.size(); ++l) {
-
+      vector<CSurfaceElementFEM>& surfElem = boundaries[iMarker].surfElem;
+      for (unsigned long l = 0; l < surfElem.size(); ++l) {
         /* Get the required data from the corresponding standard element. */
-        const unsigned short ind   = surfElem[l].indStandardElement;
-        const unsigned short nInt  = standardBoundaryFacesGrid[ind].GetNIntegration();
+        const unsigned short ind = surfElem[l].indStandardElement;
+        const unsigned short nInt = standardBoundaryFacesGrid[ind].GetNIntegration();
 
         /* Allocate the memory for the wall distance for this boundary face. */
         surfElem[l].wallDistance.resize(nInt);
 
         /* Check for an empty tree or a viscous wall.
            In those case the wall distance is set to zero. */
-        if(viscousWall) {
-
+        if (viscousWall) {
           /* Wall distance must be set to zero. */
-          for(unsigned short i=0; i<nInt; ++i)
-            surfElem[l].wallDistance[i] = 0.0;
-        }
-        else if ( !WallADT->IsEmpty() ) {
+          for (unsigned short i = 0; i < nInt; ++i) surfElem[l].wallDistance[i] = 0.0;
+        } else if (!WallADT->IsEmpty()) {
           /*--- Not a viscous wall boundary, while viscous walls are present.
                 The distance must be computed. Loop over the integration points
                 and do so. ---*/
-          for(unsigned short i=0; i<nInt; ++i) {
-
-            const su2double *coor = surfElem[l].coorIntegrationPoints.data() + i*nDim;
+          for (unsigned short i = 0; i < nInt; ++i) {
+            const su2double* coor = surfElem[l].coorIntegrationPoints.data() + i * nDim;
             unsigned short markerID;
-            unsigned long  elemID;
-            int            rankID;
-            su2double      dist;
+            unsigned long elemID;
+            int rankID;
+            su2double dist;
             WallADT->DetermineNearestElement(coor, dist, markerID, elemID, rankID);
 
             surfElem[l].wallDistance[i] = dist;
diff --git a/Common/src/fem/fem_work_estimate_metis.cpp b/Common/src/fem/fem_work_estimate_metis.cpp
index 9476452d252..e00f89bf98f 100644
--- a/Common/src/fem/fem_work_estimate_metis.cpp
+++ b/Common/src/fem/fem_work_estimate_metis.cpp
@@ -28,28 +28,22 @@
 
 #include "../../include/fem/fem_standard_element.hpp"
 
-su2double CFEMStandardElement::WorkEstimateMetis(CConfig *config) {
-
+su2double CFEMStandardElement::WorkEstimateMetis(CConfig* config) {
   /* TEMPORARY IMPLEMENTATION. */
-  return nIntegration + 0.1*nDOFs;
+  return nIntegration + 0.1 * nDOFs;
 }
 
-su2double CFEMStandardInternalFace::WorkEstimateMetis(CConfig *config) {
-
+su2double CFEMStandardInternalFace::WorkEstimateMetis(CConfig* config) {
   /* TEMPORARY IMPLEMENTATION. */
-  return 2.0*nIntegration + 0.05*(nDOFsFaceSide0 + nDOFsFaceSide1);
+  return 2.0 * nIntegration + 0.05 * (nDOFsFaceSide0 + nDOFsFaceSide1);
 }
 
-su2double CFEMStandardBoundaryFace::WorkEstimateMetis(CConfig *config) {
-
+su2double CFEMStandardBoundaryFace::WorkEstimateMetis(CConfig* config) {
   /* TEMPORARY IMPLEMENTATION. */
-  return nIntegration + 0.05*nDOFsFace;
+  return nIntegration + 0.05 * nDOFsFace;
 }
 
-su2double CFEMStandardBoundaryFace::WorkEstimateMetisWallFunctions(
-                                           CConfig              *config,
-                                           const unsigned short nPointsWF) {
-
+su2double CFEMStandardBoundaryFace::WorkEstimateMetisWallFunctions(CConfig* config, const unsigned short nPointsWF) {
   /* TEMPORARY IMPLEMENTATION. */
-  return 0.25*nIntegration*nPointsWF;
+  return 0.25 * nIntegration * nPointsWF;
 }
diff --git a/Common/src/fem/geometry_structure_fem_part.cpp b/Common/src/fem/geometry_structure_fem_part.cpp
index d6871e9c863..3e6853176d8 100644
--- a/Common/src/fem/geometry_structure_fem_part.cpp
+++ b/Common/src/fem/geometry_structure_fem_part.cpp
@@ -41,54 +41,50 @@
 #include <sys/stat.h>
 /*--- Epsilon definition ---*/
 
-
 CFaceOfElement::CFaceOfElement() {
-  nCornerPoints   = 0;
+  nCornerPoints = 0;
   cornerPoints[0] = cornerPoints[1] = cornerPoints[2] = cornerPoints[3] = ULONG_MAX;
-  elemID0         = elemID1 = ULONG_MAX;
-  nPolyGrid0      = nPolyGrid1 = 0;
-  nPolySol0       = nPolySol1  = 0;
-  nDOFsElem0      = nDOFsElem1 = 0;
-  elemType0       = elemType1  = 0;
-  faceID0         = faceID1    = 0;
-  periodicIndex   = periodicIndexDonor = 0;
-  faceIndicator   = 0;
+  elemID0 = elemID1 = ULONG_MAX;
+  nPolyGrid0 = nPolyGrid1 = 0;
+  nPolySol0 = nPolySol1 = 0;
+  nDOFsElem0 = nDOFsElem1 = 0;
+  elemType0 = elemType1 = 0;
+  faceID0 = faceID1 = 0;
+  periodicIndex = periodicIndexDonor = 0;
+  faceIndicator = 0;
 
   JacFaceIsConsideredConstant = false;
-  elem0IsOwner                = false;
+  elem0IsOwner = false;
 }
 
-CFaceOfElement::CFaceOfElement(const unsigned short VTK_Type,
-                               const unsigned short nPoly,
-                               const unsigned long  *Nodes) {
-
+CFaceOfElement::CFaceOfElement(const unsigned short VTK_Type, const unsigned short nPoly, const unsigned long* Nodes) {
   /* Set the default values of the member variables. */
-  nCornerPoints   = 0;
+  nCornerPoints = 0;
   cornerPoints[0] = cornerPoints[1] = cornerPoints[2] = cornerPoints[3] = ULONG_MAX;
-  elemID0         = elemID1 = ULONG_MAX;
-  nPolyGrid0      = nPolyGrid1 = 0;
-  nPolySol0       = nPolySol1  = 0;
-  nDOFsElem0      = nDOFsElem1 = 0;
-  elemType0       = elemType1  = 0;
-  faceID0         = faceID1    = 0;
-  periodicIndex   = periodicIndexDonor = 0;
-  faceIndicator   = 0;
+  elemID0 = elemID1 = ULONG_MAX;
+  nPolyGrid0 = nPolyGrid1 = 0;
+  nPolySol0 = nPolySol1 = 0;
+  nDOFsElem0 = nDOFsElem1 = 0;
+  elemType0 = elemType1 = 0;
+  faceID0 = faceID1 = 0;
+  periodicIndex = periodicIndexDonor = 0;
+  faceIndicator = 0;
 
   JacFaceIsConsideredConstant = false;
-  elem0IsOwner                = false;
+  elem0IsOwner = false;
 
   /* Determine the face element type and set the corner points accordingly. */
-  switch( VTK_Type ) {
+  switch (VTK_Type) {
     case LINE: {
-      nCornerPoints   = 2;
+      nCornerPoints = 2;
       cornerPoints[0] = Nodes[0];
       cornerPoints[1] = Nodes[nPoly];
       break;
     }
 
     case TRIANGLE: {
-      const unsigned short ind2 = (nPoly+1)*(nPoly+2)/2 -1;
-      nCornerPoints   = 3;
+      const unsigned short ind2 = (nPoly + 1) * (nPoly + 2) / 2 - 1;
+      nCornerPoints = 3;
       cornerPoints[0] = Nodes[0];
       cornerPoints[1] = Nodes[nPoly];
       cornerPoints[2] = Nodes[ind2];
@@ -96,9 +92,9 @@ CFaceOfElement::CFaceOfElement(const unsigned short VTK_Type,
     }
 
     case QUADRILATERAL: {
-      const unsigned short ind2 = nPoly*(nPoly+1);
-      const unsigned short ind3 = (nPoly+1)*(nPoly+1) -1;
-      nCornerPoints   = 4;
+      const unsigned short ind2 = nPoly * (nPoly + 1);
+      const unsigned short ind3 = (nPoly + 1) * (nPoly + 1) - 1;
+      nCornerPoints = 4;
       cornerPoints[0] = Nodes[0];
       cornerPoints[1] = Nodes[nPoly];
       cornerPoints[2] = Nodes[ind2];
@@ -114,62 +110,60 @@ CFaceOfElement::CFaceOfElement(const unsigned short VTK_Type,
   }
 }
 
-bool CFaceOfElement::operator<(const CFaceOfElement &other) const {
-  if(nCornerPoints != other.nCornerPoints) return nCornerPoints < other.nCornerPoints;
+bool CFaceOfElement::operator<(const CFaceOfElement& other) const {
+  if (nCornerPoints != other.nCornerPoints) return nCornerPoints < other.nCornerPoints;
 
-  for(unsigned short i=0; i<nCornerPoints; ++i)
-    if(cornerPoints[i] != other.cornerPoints[i]) return cornerPoints[i] < other.cornerPoints[i];
+  for (unsigned short i = 0; i < nCornerPoints; ++i)
+    if (cornerPoints[i] != other.cornerPoints[i]) return cornerPoints[i] < other.cornerPoints[i];
 
   return false;
 }
 
-bool CFaceOfElement::operator ==(const CFaceOfElement &other) const {
-  if(nCornerPoints != other.nCornerPoints) return false;
-  for(unsigned short i=0; i<nCornerPoints; ++i)
-    if(cornerPoints[i] != other.cornerPoints[i]) return false;
+bool CFaceOfElement::operator==(const CFaceOfElement& other) const {
+  if (nCornerPoints != other.nCornerPoints) return false;
+  for (unsigned short i = 0; i < nCornerPoints; ++i)
+    if (cornerPoints[i] != other.cornerPoints[i]) return false;
 
   return true;
 }
 
-void CFaceOfElement::Copy(const CFaceOfElement &other) {
+void CFaceOfElement::Copy(const CFaceOfElement& other) {
   nCornerPoints = other.nCornerPoints;
-  for(unsigned short i=0; i<nCornerPoints; ++i) cornerPoints[i] = other.cornerPoints[i];
-  for(unsigned short i=nCornerPoints; i<4; ++i) cornerPoints[i] = ULONG_MAX;
+  for (unsigned short i = 0; i < nCornerPoints; ++i) cornerPoints[i] = other.cornerPoints[i];
+  for (unsigned short i = nCornerPoints; i < 4; ++i) cornerPoints[i] = ULONG_MAX;
 
   elemID0 = other.elemID0;
   elemID1 = other.elemID1;
 
   nPolyGrid0 = other.nPolyGrid0;
   nPolyGrid1 = other.nPolyGrid1;
-  nPolySol0  = other.nPolySol0;
-  nPolySol1  = other.nPolySol1;
+  nPolySol0 = other.nPolySol0;
+  nPolySol1 = other.nPolySol1;
 
   nDOFsElem0 = other.nDOFsElem0;
   nDOFsElem1 = other.nDOFsElem1;
-  elemType0  = other.elemType0;
-  elemType1  = other.elemType1;
-  faceID0    = other.faceID0;
-  faceID1    = other.faceID1;
+  elemType0 = other.elemType0;
+  elemType1 = other.elemType1;
+  faceID0 = other.faceID0;
+  faceID1 = other.faceID1;
 
-  periodicIndex      = other.periodicIndex;
+  periodicIndex = other.periodicIndex;
   periodicIndexDonor = other.periodicIndexDonor;
-  faceIndicator      = other.faceIndicator;
+  faceIndicator = other.faceIndicator;
 
   JacFaceIsConsideredConstant = other.JacFaceIsConsideredConstant;
-  elem0IsOwner                = other.elem0IsOwner;
+  elem0IsOwner = other.elem0IsOwner;
 }
 
 void CFaceOfElement::CreateUniqueNumberingWithOrientation(void) {
-
   /*--- Determine the element type and create the unique numbering accordingly. ---*/
   bool swapElements = false;
-  switch( nCornerPoints ) {
-
+  switch (nCornerPoints) {
     case 2: {
       /* Element is a line. Check if the node numbering must be swapped. If so
          also the element information must be swapped, because element 0 is to
          the left of the face and element 1 to the right. */
-      if(cornerPoints[1] < cornerPoints[0]) {
+      if (cornerPoints[1] < cornerPoints[0]) {
         swap(cornerPoints[0], cornerPoints[1]);
         swapElements = true;
       }
@@ -183,28 +177,25 @@ void CFaceOfElement::CreateUniqueNumberingWithOrientation(void) {
          element 0 is to the left of the face and element 1 to the right. */
       unsigned long nn[] = {cornerPoints[0], cornerPoints[1], cornerPoints[2]};
       unsigned short ind = 0;
-      if(nn[1] < nn[ind]) ind = 1;
-      if(nn[2] < nn[ind]) ind = 2;
-
-      unsigned short indm1 = ind==0 ? 2 : ind - 1;   // Next lower index.
-      unsigned short indp1 = ind==2 ? 0 : ind + 1;   // Next upper index.
+      if (nn[1] < nn[ind]) ind = 1;
+      if (nn[2] < nn[ind]) ind = 2;
 
-      if(nn[indp1] < nn[indm1]) {
+      unsigned short indm1 = ind == 0 ? 2 : ind - 1;  // Next lower index.
+      unsigned short indp1 = ind == 2 ? 0 : ind + 1;  // Next upper index.
 
+      if (nn[indp1] < nn[indm1]) {
         /* The orientation of the triangle remains the same.
            Store the new sorted node numbering. */
         cornerPoints[0] = nn[ind];
         cornerPoints[1] = nn[indp1];
         cornerPoints[2] = nn[indm1];
-      }
-      else {
-
+      } else {
         /* The orientation of the triangle changes. Store the new
            sorted node numbering and set swapElements to true. */
         cornerPoints[0] = nn[ind];
         cornerPoints[1] = nn[indm1];
         cornerPoints[2] = nn[indp1];
-        swapElements    = true;
+        swapElements = true;
       }
 
       break;
@@ -216,35 +207,31 @@ void CFaceOfElement::CreateUniqueNumberingWithOrientation(void) {
          sequence of the new numbering is opposite to the current
          numbering, the element information must be exchanged, because
          element 0 is to the left of the face and element 1 to the right. */
-      unsigned long nn[] = {cornerPoints[0], cornerPoints[1],
-                            cornerPoints[2], cornerPoints[3]};
+      unsigned long nn[] = {cornerPoints[0], cornerPoints[1], cornerPoints[2], cornerPoints[3]};
       unsigned short ind = 0;
-      if(nn[1] < nn[ind]) ind = 1;
-      if(nn[2] < nn[ind]) ind = 2;
-      if(nn[3] < nn[ind]) ind = 3;
-
-      unsigned short indm1 = ind==0 ?       3 : ind - 1; // Next lower index.
-      unsigned short indp1 = ind==3 ?       0 : ind + 1; // Next upper index.
-      unsigned short indp2 = ind>=2 ? ind - 2 : ind + 2; // Opposite index.
+      if (nn[1] < nn[ind]) ind = 1;
+      if (nn[2] < nn[ind]) ind = 2;
+      if (nn[3] < nn[ind]) ind = 3;
 
-      if(nn[indp1] < nn[indm1]) {
+      unsigned short indm1 = ind == 0 ? 3 : ind - 1;        // Next lower index.
+      unsigned short indp1 = ind == 3 ? 0 : ind + 1;        // Next upper index.
+      unsigned short indp2 = ind >= 2 ? ind - 2 : ind + 2;  // Opposite index.
 
+      if (nn[indp1] < nn[indm1]) {
         /* The orientation of the quadrilateral remains the same.
            Store the new sorted node numbering. */
         cornerPoints[0] = nn[ind];
         cornerPoints[1] = nn[indp1];
         cornerPoints[2] = nn[indp2];
         cornerPoints[3] = nn[indm1];
-      }
-      else {
-
+      } else {
         /* The orientation of the quadrilateral changes. Store the new
            sorted node numbering and set swapElements to true. */
         cornerPoints[0] = nn[ind];
         cornerPoints[1] = nn[indm1];
         cornerPoints[2] = nn[indp2];
         cornerPoints[3] = nn[indp1];
-        swapElements    = true;
+        swapElements = true;
       }
 
       break;
@@ -252,39 +239,38 @@ void CFaceOfElement::CreateUniqueNumberingWithOrientation(void) {
 
     default: {
       ostringstream message;
-      message << "Unknown surface element type with " << nCornerPoints
-              << " corners." << endl;
+      message << "Unknown surface element type with " << nCornerPoints << " corners." << endl;
       SU2_MPI::Error(message.str(), CURRENT_FUNCTION);
     }
   }
 
   /* Swap the element information, if needed. */
-  if( swapElements ) {
-    swap(elemID0,    elemID1);
+  if (swapElements) {
+    swap(elemID0, elemID1);
     swap(nPolyGrid0, nPolyGrid1);
-    swap(nPolySol0,  nPolySol1);
+    swap(nPolySol0, nPolySol1);
     swap(nDOFsElem0, nDOFsElem1);
-    swap(elemType0,  elemType1);
-    swap(faceID0,    faceID1);
+    swap(elemType0, elemType1);
+    swap(faceID0, faceID1);
   }
 }
 
-void CBoundaryFace::Copy(const CBoundaryFace &other) {
-  VTK_Type          = other.VTK_Type;
-  nPolyGrid         = other.nPolyGrid;
-  nDOFsGrid         = other.nDOFsGrid;
+void CBoundaryFace::Copy(const CBoundaryFace& other) {
+  VTK_Type = other.VTK_Type;
+  nPolyGrid = other.nPolyGrid;
+  nDOFsGrid = other.nDOFsGrid;
   globalBoundElemID = other.globalBoundElemID;
-  domainElementID   = other.domainElementID;
-  Nodes             = other.Nodes;
+  domainElementID = other.domainElementID;
+  Nodes = other.Nodes;
 }
 
 CMatchingFace::CMatchingFace() {
   nCornerPoints = 0;
-  nDim          = 0;
-  nPoly         = 0;
-  nDOFsElem     = 0;
-  elemType      = 0;
-  elemID        = 0;
+  nDim = 0;
+  nPoly = 0;
+  nDOFsElem = 0;
+  elemType = 0;
+  elemID = 0;
 
   cornerCoor[0][0] = cornerCoor[0][1] = cornerCoor[0][2] = 0.0;
   cornerCoor[1][0] = cornerCoor[1][1] = cornerCoor[1][2] = 0.0;
@@ -294,10 +280,9 @@ CMatchingFace::CMatchingFace() {
   tolForMatching = 0.0;
 }
 
-bool CMatchingFace::operator<(const CMatchingFace &other) const {
-
+bool CMatchingFace::operator<(const CMatchingFace& other) const {
   /* First compare the number of corner points. ---*/
-  if(nCornerPoints != other.nCornerPoints) return nCornerPoints < other.nCornerPoints;
+  if (nCornerPoints != other.nCornerPoints) return nCornerPoints < other.nCornerPoints;
 
   /*--- Determine the tolerance for comparing both objects. ---*/
   const su2double tol = min(tolForMatching, other.tolForMatching);
@@ -305,10 +290,9 @@ bool CMatchingFace::operator<(const CMatchingFace &other) const {
   /*--- Loop over the number of corner points and dimensions and compare the
         coordinates. If considered different, return true if the current face
         is considered smaller and false otherwise.            ---*/
-  for(unsigned short k=0; k<nCornerPoints; ++k) {
-    for(unsigned short l=0; l<nDim; ++l) {
-      if(fabs(cornerCoor[k][l] - other.cornerCoor[k][l]) > tol)
-        return cornerCoor[k][l] < other.cornerCoor[k][l];
+  for (unsigned short k = 0; k < nCornerPoints; ++k) {
+    for (unsigned short l = 0; l < nDim; ++l) {
+      if (fabs(cornerCoor[k][l] - other.cornerCoor[k][l]) > tol) return cornerCoor[k][l] < other.cornerCoor[k][l];
     }
   }
 
@@ -317,21 +301,22 @@ bool CMatchingFace::operator<(const CMatchingFace &other) const {
 }
 
 void CMatchingFace::SortFaceCoordinates(void) {
-
   /*--- Determine the tolerance for a matching point for this face. This is
         accomplished by computing the minimum distance between the points of
         the face, multiplied by a relative tolerance.        ---*/
-  for(unsigned short k=0; k<nCornerPoints; ++k) {
-    for(unsigned short j=(k+1); j<nCornerPoints; ++j) {
+  for (unsigned short k = 0; k < nCornerPoints; ++k) {
+    for (unsigned short j = (k + 1); j < nCornerPoints; ++j) {
       su2double dist = 0.0;
-      for(unsigned short l=0; l<nDim; ++l) {
+      for (unsigned short l = 0; l < nDim; ++l) {
         su2double ds = cornerCoor[k][l] - cornerCoor[j][l];
-        dist += ds*ds;
+        dist += ds * ds;
       }
       dist = sqrt(dist);
 
-      if(k==0 && j==1) tolForMatching = dist;
-      else             tolForMatching = min(tolForMatching, dist);
+      if (k == 0 && j == 1)
+        tolForMatching = dist;
+      else
+        tolForMatching = min(tolForMatching, dist);
     }
   }
 
@@ -340,39 +325,37 @@ void CMatchingFace::SortFaceCoordinates(void) {
   /*--- Sort the points in increasing order based on the coordinates.
         An insertion sort algorithm is used, which is quite efficient
         for at most four corner points.                        ---*/
-  for(unsigned short k=1; k<nCornerPoints; ++k) {
-    for(unsigned short j=k; j>0; --j) {
-
+  for (unsigned short k = 1; k < nCornerPoints; ++k) {
+    for (unsigned short j = k; j > 0; --j) {
       /* Check if cornerCoor[j] is considered less than cornerCoor[j-1]. */
       bool lessThan = false;
-      for(unsigned short l=0; l<nDim; ++l) {
-        if(fabs(cornerCoor[j][l] - cornerCoor[j-1][l]) > tolForMatching) {
-          lessThan = cornerCoor[j][l] < cornerCoor[j-1][l];
+      for (unsigned short l = 0; l < nDim; ++l) {
+        if (fabs(cornerCoor[j][l] - cornerCoor[j - 1][l]) > tolForMatching) {
+          lessThan = cornerCoor[j][l] < cornerCoor[j - 1][l];
           break;
         }
       }
 
       /* If cornerCoor[j] is less than cornerCoor[j-1] they must be swapped.
          Otherwise an exit can be made from the j-loop.         */
-      if( lessThan ) {
-        for(unsigned short l=0; l<nDim; ++l)
-          swap(cornerCoor[j][l], cornerCoor[j-1][l]);
-      }
-      else break;
+      if (lessThan) {
+        for (unsigned short l = 0; l < nDim; ++l) swap(cornerCoor[j][l], cornerCoor[j - 1][l]);
+      } else
+        break;
     }
   }
 }
 
-void CMatchingFace::Copy(const CMatchingFace &other) {
+void CMatchingFace::Copy(const CMatchingFace& other) {
   nCornerPoints = other.nCornerPoints;
-  nDim          = other.nDim;
-  nPoly         = other.nPoly;
-  nDOFsElem     = other.nDOFsElem;
-  elemType      = other.elemType;
-  elemID        = other.elemID;
-
-  for(unsigned short k=0; k<nCornerPoints; ++k) {
-    for(unsigned l=0; l<nDim; ++l) {
+  nDim = other.nDim;
+  nPoly = other.nPoly;
+  nDOFsElem = other.nDOFsElem;
+  elemType = other.elemType;
+  elemID = other.elemID;
+
+  for (unsigned short k = 0; k < nCornerPoints; ++k) {
+    for (unsigned l = 0; l < nDim; ++l) {
       cornerCoor[k][l] = other.cornerCoor[k][l];
     }
   }
@@ -380,35 +363,42 @@ void CMatchingFace::Copy(const CMatchingFace &other) {
   tolForMatching = other.tolForMatching;
 }
 
-void CPhysicalGeometry::Read_SU2_Format_Parallel_FEM(CConfig        *config,
-                                                     string         val_mesh_filename,
-                                                     unsigned short val_iZone,
-                                                     unsigned short val_nZone) {
+void CPhysicalGeometry::Read_SU2_Format_Parallel_FEM(CConfig* config, string val_mesh_filename,
+                                                     unsigned short val_iZone, unsigned short val_nZone) {
   string text_line, Marker_Tag;
   ifstream mesh_file;
   string::size_type position;
   unsigned long nDOFsGrid_Local = 0, loc_element_count = 0;
-  bool domain_flag   = false;
+  bool domain_flag = false;
   bool time_spectral = config->GetTime_Marching() == TIME_MARCHING::HARMONIC_BALANCE;
   unsigned short nMarker_Max = config->GetnMarker_Max();
   nZone = val_nZone;
 
   /*--- Initialize counters for local/global points & elements ---*/
-  Global_nPoint  = 0; Global_nPointDomain   = 0; Global_nElem = 0;
-  nelem_edge     = 0; Global_nelem_edge     = 0;
-  nelem_triangle = 0; Global_nelem_triangle = 0;
-  nelem_quad     = 0; Global_nelem_quad     = 0;
-  nelem_tetra    = 0; Global_nelem_tetra    = 0;
-  nelem_hexa     = 0; Global_nelem_hexa     = 0;
-  nelem_prism    = 0; Global_nelem_prism    = 0;
-  nelem_pyramid  = 0; Global_nelem_pyramid  = 0;
+  Global_nPoint = 0;
+  Global_nPointDomain = 0;
+  Global_nElem = 0;
+  nelem_edge = 0;
+  Global_nelem_edge = 0;
+  nelem_triangle = 0;
+  Global_nelem_triangle = 0;
+  nelem_quad = 0;
+  Global_nelem_quad = 0;
+  nelem_tetra = 0;
+  Global_nelem_tetra = 0;
+  nelem_hexa = 0;
+  Global_nelem_hexa = 0;
+  nelem_prism = 0;
+  Global_nelem_prism = 0;
+  nelem_pyramid = 0;
+  Global_nelem_pyramid = 0;
 
   /*--- Allocate memory for the linear partition of the elements of the mesh.
         These arrays are the size of the number of ranks. ---*/
 
   beg_node = new unsigned long[size];
   end_node = new unsigned long[size];
-  nPointLinear  = new unsigned long[size];
+  nPointLinear = new unsigned long[size];
 
   /*--- Open grid file ---*/
 
@@ -417,23 +407,22 @@ void CPhysicalGeometry::Read_SU2_Format_Parallel_FEM(CConfig        *config,
   /*--- Check the grid ---*/
 
   if (mesh_file.fail())
-    SU2_MPI::Error(string("There is no mesh file (CPhysicalGeometry)!! ") + val_mesh_filename,
-                   CURRENT_FUNCTION);
+    SU2_MPI::Error(string("There is no mesh file (CPhysicalGeometry)!! ") + val_mesh_filename, CURRENT_FUNCTION);
 
   /*--- If more than one, find the zone in the mesh file ---*/
 
   if (val_nZone > 1 || time_spectral) {
     if (time_spectral) {
-      if (rank == MASTER_NODE) cout << "Reading time spectral instance " << val_iZone+1 << ":" << endl;
+      if (rank == MASTER_NODE) cout << "Reading time spectral instance " << val_iZone + 1 << ":" << endl;
     } else {
-      while (getline (mesh_file,text_line)) {
+      while (getline(mesh_file, text_line)) {
         /*--- Search for the current domain ---*/
-        position = text_line.find ("IZONE=",0);
+        position = text_line.find("IZONE=", 0);
         if (position != string::npos) {
-          text_line.erase (0,6);
+          text_line.erase(0, 6);
           unsigned short jDomain = atoi(text_line.c_str());
-          if (jDomain == val_iZone+1) {
-            if (rank == MASTER_NODE) cout << "Reading zone " << val_iZone+1 << " points:" << endl;
+          if (jDomain == val_iZone + 1) {
+            if (rank == MASTER_NODE) cout << "Reading zone " << val_iZone + 1 << " points:" << endl;
             break;
           }
         }
@@ -443,27 +432,29 @@ void CPhysicalGeometry::Read_SU2_Format_Parallel_FEM(CConfig        *config,
 
   /*--- Read grid file with format SU2 ---*/
 
-  while (getline (mesh_file, text_line)) {
-
+  while (getline(mesh_file, text_line)) {
     /*--- Read the dimension of the problem ---*/
 
-    position = text_line.find ("NDIME=",0);
+    position = text_line.find("NDIME=", 0);
     if (position != string::npos) {
       if (domain_flag == false) {
-        text_line.erase (0,6); nDim = atoi(text_line.c_str());
+        text_line.erase(0, 6);
+        nDim = atoi(text_line.c_str());
         if (rank == MASTER_NODE) {
           if (nDim == 2) cout << "Two dimensional problem." << endl;
           if (nDim == 3) cout << "Three dimensional problem." << endl;
         }
         domain_flag = true;
-      } else { break; }
+      } else {
+        break;
+      }
     }
 
     /*--- Read the information about inner elements ---*/
 
-    position = text_line.find ("NELEM=",0);
+    position = text_line.find("NELEM=", 0);
     if (position != string::npos) {
-      text_line.erase (0,6);
+      text_line.erase(0, 6);
       stringstream stream_line(text_line);
       stream_line >> Global_nElem;
 
@@ -473,8 +464,8 @@ void CPhysicalGeometry::Read_SU2_Format_Parallel_FEM(CConfig        *config,
       /*--- Check if the number of cores used is larger than the number of
             elements. Terminate if this is the case, because it does not make
             sense to do this. ---*/
-      unsigned long nCores = size;   // Correct for the number of cores per rank.
-      if(nCores > Global_nElem) {
+      unsigned long nCores = size;  // Correct for the number of cores per rank.
+      if (nCores > Global_nElem) {
         ostringstream message;
         message << "The number of cores, " << nCores;
         message << ", is larger than the number of elements, " << Global_nElem << "." << endl;
@@ -488,14 +479,14 @@ void CPhysicalGeometry::Read_SU2_Format_Parallel_FEM(CConfig        *config,
             This is a linear partitioning with the addition of a simple load
             balancing for any remainder elements. ---*/
       unsigned long total_elem_accounted = 0;
-      for(unsigned long i = 0; i < (unsigned long)size; i++) {
-        nPointLinear[i] = Global_nElem/size;
+      for (unsigned long i = 0; i < (unsigned long)size; i++) {
+        nPointLinear[i] = Global_nElem / size;
         total_elem_accounted = total_elem_accounted + nPointLinear[i];
       }
 
       /*--- Get the number of remainder elements after the even division ---*/
       unsigned long rem_elem = Global_nElem - total_elem_accounted;
-      for (unsigned long i = 0; i<rem_elem; i++) {
+      for (unsigned long i = 0; i < rem_elem; i++) {
         ++nPointLinear[i];
       }
 
@@ -504,12 +495,12 @@ void CPhysicalGeometry::Read_SU2_Format_Parallel_FEM(CConfig        *config,
       beg_node[0] = 0;
       end_node[0] = beg_node[0] + nPointLinear[0];
       for (unsigned long i = 1; i < (unsigned long)size; i++) {
-        beg_node[i] = end_node[i-1];
-        end_node[i] = beg_node[i] + nPointLinear[i] ;
+        beg_node[i] = end_node[i - 1];
+        end_node[i] = beg_node[i] + nPointLinear[i];
       }
 
       /*--- Allocate space for elements ---*/
-      elem = new CPrimalGrid*[nElem] ();
+      elem = new CPrimalGrid*[nElem]();
 
       /*--- Loop over all the elements and store the elements to be stored on
             this rank. Furthermore, determine the total amount of DOFs for
@@ -517,40 +508,35 @@ void CPhysicalGeometry::Read_SU2_Format_Parallel_FEM(CConfig        *config,
             grid).                                                          ---*/
       unsigned long nDOFs_tot = 0;
       for (unsigned long i = 0; i < Global_nElem; i++) {
-
         getline(mesh_file, text_line);
         istringstream elem_line(text_line);
 
         /*--- Read the value that defines the element type, the polynomial
               degree of the geometry and the polynomial degree of the
               solution. Extract this info as well.                     ---*/
-        unsigned long typeRead; elem_line >> typeRead;
+        unsigned long typeRead;
+        elem_line >> typeRead;
         unsigned long typeReadErrorMessage = typeRead;
         unsigned short nPolySol, nPolyGrid;
-        if(typeRead > 10000) {
-          nPolySol  = typeRead/10000 -1;
-          typeRead  = typeRead%10000;
-          nPolyGrid = typeRead/100 + 1;
-        }
-        else {
-          nPolyGrid = typeRead/100 + 1;
-          nPolySol  = nPolyGrid;
+        if (typeRead > 10000) {
+          nPolySol = typeRead / 10000 - 1;
+          typeRead = typeRead % 10000;
+          nPolyGrid = typeRead / 100 + 1;
+        } else {
+          nPolyGrid = typeRead / 100 + 1;
+          nPolySol = nPolyGrid;
         }
 
-        unsigned short VTK_Type = typeRead%100;
+        unsigned short VTK_Type = typeRead % 100;
 
-        unsigned short nDOFsGrid = CFEMStandardElementBase::GetNDOFsStatic(VTK_Type, nPolyGrid,
-                                                                           typeReadErrorMessage);
-        unsigned short nDOFsSol  = CFEMStandardElementBase::GetNDOFsStatic(VTK_Type, nPolySol,
-                                                                           typeReadErrorMessage);
+        unsigned short nDOFsGrid = CFEMStandardElementBase::GetNDOFsStatic(VTK_Type, nPolyGrid, typeReadErrorMessage);
+        unsigned short nDOFsSol = CFEMStandardElementBase::GetNDOFsStatic(VTK_Type, nPolySol, typeReadErrorMessage);
 
         /*--- Allocate the memory for a new primary grid FEM element if
               this element must be stored on this rank.                 ---*/
         if ((i >= beg_node[rank]) && (i < end_node[rank])) {
-
-          elem[loc_element_count] = new CPrimalGridFEM(i, VTK_Type, nPolyGrid, nPolySol,
-                                                       nDOFsGrid, nDOFsSol, nDOFs_tot,
-                                                       elem_line);
+          elem[loc_element_count] =
+              new CPrimalGridFEM(i, VTK_Type, nPolyGrid, nPolySol, nDOFsGrid, nDOFsSol, nDOFs_tot, elem_line);
           nDOFsGrid_Local += nDOFsGrid;
           loc_element_count++;
         }
@@ -569,11 +555,9 @@ void CPhysicalGeometry::Read_SU2_Format_Parallel_FEM(CConfig        *config,
   /*--- Create a vector, which contains the global node IDs of the local elements. ---*/
   vector<unsigned long> nodeIDsElemLoc;
   nodeIDsElemLoc.reserve(nDOFsGrid_Local);
-  for(unsigned long i=0; i<loc_element_count; i++)
-  {
+  for (unsigned long i = 0; i < loc_element_count; i++) {
     unsigned short nDOFsElem = elem[i]->GetnNodes();
-    for(unsigned short j=0; j<nDOFsElem; ++j)
-      nodeIDsElemLoc.push_back(elem[i]->GetNode(j));
+    for (unsigned short j = 0; j < nDOFsElem; ++j) nodeIDsElemLoc.push_back(elem[i]->GetNode(j));
   }
 
   sort(nodeIDsElemLoc.begin(), nodeIDsElemLoc.end());
@@ -582,7 +566,7 @@ void CPhysicalGeometry::Read_SU2_Format_Parallel_FEM(CConfig        *config,
   nodeIDsElemLoc.erase(lastNode, nodeIDsElemLoc.end());
 
   /*--- Allocate the memory for the coordinates to be stored on this rank. ---*/
-  nPoint     = nodeIDsElemLoc.size();
+  nPoint = nodeIDsElemLoc.size();
   nodes = new CPoint(nPoint, nDim);
 
   /*--- Open the grid file again and go to the position where
@@ -590,37 +574,36 @@ void CPhysicalGeometry::Read_SU2_Format_Parallel_FEM(CConfig        *config,
   mesh_file.open(val_mesh_filename.c_str(), ios::in);
 
   if (val_nZone > 1 && !time_spectral) {
-    while (getline (mesh_file,text_line)) {
-      position = text_line.find ("IZONE=",0);
+    while (getline(mesh_file, text_line)) {
+      position = text_line.find("IZONE=", 0);
       if (position != string::npos) {
-        text_line.erase (0,6);
+        text_line.erase(0, 6);
         unsigned short jDomain = atoi(text_line.c_str());
-        if (jDomain == val_iZone+1) break;
+        if (jDomain == val_iZone + 1) break;
       }
     }
   }
 
   /*--- While loop to read the point information. ---*/
-  while (getline (mesh_file, text_line)) {
-
-    position = text_line.find ("NPOIN=",0);
+  while (getline(mesh_file, text_line)) {
+    position = text_line.find("NPOIN=", 0);
     if (position != string::npos) {
-      text_line.erase (0,6);
+      text_line.erase(0, 6);
       stringstream stream_line(text_line);
       stream_line >> Global_nPoint;
 
       /*--- Loop over the global number of points and store the
             ones that are needed on this processor.             ---*/
       unsigned long ii = 0;
-      for(unsigned long i=0; i<Global_nPoint; ++i) {
+      for (unsigned long i = 0; i < Global_nPoint; ++i) {
         getline(mesh_file, text_line);
 
-        if( binary_search(nodeIDsElemLoc.begin(), nodeIDsElemLoc.end(), i) ) {
+        if (binary_search(nodeIDsElemLoc.begin(), nodeIDsElemLoc.end(), i)) {
           istringstream point_line(text_line);
           su2double Coord[3] = {0.0};
           point_line >> Coord[0];
           point_line >> Coord[1];
-          if (nDim==3) point_line >> Coord[2];
+          if (nDim == 3) point_line >> Coord[2];
           nodes->SetCoord(ii, Coord);
           nodes->SetGlobalIndex(ii, i);
           ++ii;
@@ -635,21 +618,19 @@ void CPhysicalGeometry::Read_SU2_Format_Parallel_FEM(CConfig        *config,
 
   /*--- Determine the faces of the local elements. --- */
   vector<CFaceOfElement> localFaces;
-  for(unsigned long k=0; k<loc_element_count; k++) {
-
+  for (unsigned long k = 0; k < loc_element_count; k++) {
     /*--- Get the global IDs of the corner points of all the faces of this elements. ---*/
     unsigned short nFaces;
     unsigned short nPointsPerFace[6];
-    unsigned long  faceConn[6][4];
+    unsigned long faceConn[6][4];
 
     elem[k]->GetCornerPointsAllFaces(nFaces, nPointsPerFace, faceConn);
 
     /*--- Loop over the faces and add them to localFaces. ---*/
-    for(unsigned short i=0; i<nFaces; ++i) {
+    for (unsigned short i = 0; i < nFaces; ++i) {
       CFaceOfElement thisFace;
       thisFace.nCornerPoints = nPointsPerFace[i];
-      for(unsigned short j=0; j<nPointsPerFace[i]; ++j)
-        thisFace.cornerPoints[j] = faceConn[i][j];
+      for (unsigned short j = 0; j < nPointsPerFace[i]; ++j) thisFace.cornerPoints[j] = faceConn[i][j];
       thisFace.elemID0 = k + beg_node[rank];
 
       thisFace.CreateUniqueNumbering();
@@ -664,105 +645,106 @@ void CPhysicalGeometry::Read_SU2_Format_Parallel_FEM(CConfig        *config,
   lastFace = unique(localFaces.begin(), localFaces.end());
   localFaces.erase(lastFace, localFaces.end());
 
-
   /*--- Open the grid file again and go to the position where
         the correct zone is stored.                           ---*/
   mesh_file.open(val_mesh_filename.c_str(), ios::in);
 
   if (val_nZone > 1 && !time_spectral) {
-    while (getline (mesh_file,text_line)) {
-      position = text_line.find ("IZONE=",0);
+    while (getline(mesh_file, text_line)) {
+      position = text_line.find("IZONE=", 0);
       if (position != string::npos) {
-        text_line.erase (0,6);
+        text_line.erase(0, 6);
         unsigned short jDomain = atoi(text_line.c_str());
-        if (jDomain == val_iZone+1) break;
+        if (jDomain == val_iZone + 1) break;
       }
     }
   }
 
   /*--- While loop to read the boundary information. ---*/
-  while (getline (mesh_file, text_line)) {
+  while (getline(mesh_file, text_line)) {
     /*--- Read number of markers ---*/
-    position = text_line.find ("NMARK=",0);
+    position = text_line.find("NMARK=", 0);
     if (position != string::npos) {
-      text_line.erase (0,6);
+      text_line.erase(0, 6);
       istringstream stream_line(text_line);
       stream_line >> nMarker;
 
       if (rank == MASTER_NODE) cout << nMarker << " surface markers." << endl;
       config->SetnMarker_All(nMarker);
       bound = new CPrimalGrid**[nMarker];
-      nElem_Bound = new unsigned long [nMarker];
-      Tag_to_Marker = new string [nMarker_Max];
+      nElem_Bound = new unsigned long[nMarker];
+      Tag_to_Marker = new string[nMarker_Max];
 
-      for(unsigned short iMarker = 0 ; iMarker < nMarker; iMarker++) {
-        getline (mesh_file, text_line);
-        text_line.erase (0,11);
-        text_line.erase (remove(text_line.begin(), text_line.end(), ' '),  text_line.end());
-        text_line.erase (remove(text_line.begin(), text_line.end(), '\r'), text_line.end());
-        text_line.erase (remove(text_line.begin(), text_line.end(), '\n'), text_line.end());
+      for (unsigned short iMarker = 0; iMarker < nMarker; iMarker++) {
+        getline(mesh_file, text_line);
+        text_line.erase(0, 11);
+        text_line.erase(remove(text_line.begin(), text_line.end(), ' '), text_line.end());
+        text_line.erase(remove(text_line.begin(), text_line.end(), '\r'), text_line.end());
+        text_line.erase(remove(text_line.begin(), text_line.end(), '\n'), text_line.end());
 
         Marker_Tag = text_line.c_str();
 
         /*--- Read the number of elements for this marker. ---*/
-        getline (mesh_file, text_line);
-        text_line.erase (0,13); istringstream nmark_line(text_line);
+        getline(mesh_file, text_line);
+        text_line.erase(0, 13);
+        istringstream nmark_line(text_line);
         unsigned long nElem_Bound_Global;
         nmark_line >> nElem_Bound_Global;
         if (rank == MASTER_NODE)
-          cout << nElem_Bound_Global  << " boundary elements in index "<< iMarker
-               <<" (Marker = " <<Marker_Tag<< ")." << endl;
+          cout << nElem_Bound_Global << " boundary elements in index " << iMarker << " (Marker = " << Marker_Tag << ")."
+               << endl;
 
         /*--- Define a vector of FEM boundary elements to store the local boundary faces. ---*/
         vector<CBoundaryFace> boundElems;
 
         /*--- Loop over the global boundary faces. ---*/
-        for(unsigned long i=0; i<nElem_Bound_Global; ++i) {
-          getline (mesh_file, text_line);
+        for (unsigned long i = 0; i < nElem_Bound_Global; ++i) {
+          getline(mesh_file, text_line);
           istringstream bound_line(text_line);
 
           /*--- Determine the element type, its number of DOFs and read
                 its node IDs.                                           ---*/
-          unsigned long typeRead; bound_line >> typeRead;
-          unsigned short nPolyGrid    = typeRead/100 + 1;
-          unsigned short VTK_Type     = typeRead%100;
+          unsigned long typeRead;
+          bound_line >> typeRead;
+          unsigned short nPolyGrid = typeRead / 100 + 1;
+          unsigned short VTK_Type = typeRead % 100;
           unsigned short nDOFEdgeGrid = nPolyGrid + 1;
 
           unsigned short nDOFsGrid = 0;
           CFaceOfElement thisFace;
-          thisFace.cornerPoints[0] = 0; thisFace.cornerPoints[1] = nPolyGrid;
-          switch( VTK_Type ) {
+          thisFace.cornerPoints[0] = 0;
+          thisFace.cornerPoints[1] = nPolyGrid;
+          switch (VTK_Type) {
             case LINE:
               nDOFsGrid = nDOFEdgeGrid;
               thisFace.nCornerPoints = 2;
               break;
 
             case TRIANGLE:
-              nDOFsGrid = nDOFEdgeGrid*(nDOFEdgeGrid+1)/2;
+              nDOFsGrid = nDOFEdgeGrid * (nDOFEdgeGrid + 1) / 2;
               thisFace.nCornerPoints = 3;
-              thisFace.cornerPoints[2] = nDOFsGrid -1;
+              thisFace.cornerPoints[2] = nDOFsGrid - 1;
               break;
 
             case QUADRILATERAL:
-              nDOFsGrid = nDOFEdgeGrid*nDOFEdgeGrid;
+              nDOFsGrid = nDOFEdgeGrid * nDOFEdgeGrid;
               thisFace.nCornerPoints = 4;
-              thisFace.cornerPoints[2] = nPolyGrid*nDOFEdgeGrid;
-              thisFace.cornerPoints[3] = nDOFsGrid -1;
+              thisFace.cornerPoints[2] = nPolyGrid * nDOFEdgeGrid;
+              thisFace.cornerPoints[3] = nDOFsGrid - 1;
               break;
 
             default:
               ostringstream message;
-              message << "Unknown FEM boundary element value, " << typeRead
-                      << ", in " << val_mesh_filename;
+              message << "Unknown FEM boundary element value, " << typeRead << ", in " << val_mesh_filename;
               SU2_MPI::Error(message.str(), CURRENT_FUNCTION);
           }
 
           vector<unsigned long> nodeIDs(nDOFsGrid);
-          for(unsigned short j=0; j<nDOFsGrid; ++j) bound_line >> nodeIDs[j];
+          for (unsigned short j = 0; j < nDOFsGrid; ++j) bound_line >> nodeIDs[j];
 
           /*--- Convert the local numbering of thisFace to global numbering
                 and create a unique numbering of these nodes.               ---*/
-          for(unsigned short j=0; j<thisFace.nCornerPoints; ++j)
+          for (unsigned short j = 0; j < thisFace.nCornerPoints; ++j)
             thisFace.cornerPoints[j] = nodeIDs[thisFace.cornerPoints[j]];
           thisFace.CreateUniqueNumbering();
 
@@ -771,16 +753,15 @@ void CPhysicalGeometry::Read_SU2_Format_Parallel_FEM(CConfig        *config,
                 to boundElems.                                          ---*/
           vector<CFaceOfElement>::iterator low;
           low = lower_bound(localFaces.begin(), localFaces.end(), thisFace);
-          if(low != localFaces.end()) {
-            if( !(thisFace < *low) ) {
-
+          if (low != localFaces.end()) {
+            if (!(thisFace < *low)) {
               CBoundaryFace thisBoundFace;
-              thisBoundFace.VTK_Type          = VTK_Type;
-              thisBoundFace.nPolyGrid         = nPolyGrid;
-              thisBoundFace.nDOFsGrid         = nDOFsGrid;
+              thisBoundFace.VTK_Type = VTK_Type;
+              thisBoundFace.nPolyGrid = nPolyGrid;
+              thisBoundFace.nDOFsGrid = nDOFsGrid;
               thisBoundFace.globalBoundElemID = i;
-              thisBoundFace.domainElementID   = low->elemID0;
-              thisBoundFace.Nodes             = nodeIDs;
+              thisBoundFace.domainElementID = low->elemID0;
+              thisBoundFace.Nodes = nodeIDs;
 
               boundElems.push_back(thisBoundFace);
             }
@@ -790,15 +771,12 @@ void CPhysicalGeometry::Read_SU2_Format_Parallel_FEM(CConfig        *config,
         /*--- Allocate space for the boundary elements and store the ones
               whose parent element is stored on this rank. ---*/
         nElem_Bound[iMarker] = boundElems.size();
-        bound[iMarker] = new CPrimalGrid* [nElem_Bound[iMarker]];
+        bound[iMarker] = new CPrimalGrid*[nElem_Bound[iMarker]];
 
-        for(unsigned long i=0; i<nElem_Bound[iMarker]; ++i)
-          bound[iMarker][i] = new CPrimalGridBoundFEM(boundElems[i].globalBoundElemID,
-                                                      boundElems[i].domainElementID,
-                                                      boundElems[i].VTK_Type,
-                                                      boundElems[i].nPolyGrid,
-                                                      boundElems[i].nDOFsGrid,
-                                                      boundElems[i].Nodes);
+        for (unsigned long i = 0; i < nElem_Bound[iMarker]; ++i)
+          bound[iMarker][i] = new CPrimalGridBoundFEM(boundElems[i].globalBoundElemID, boundElems[i].domainElementID,
+                                                      boundElems[i].VTK_Type, boundElems[i].nPolyGrid,
+                                                      boundElems[i].nDOFsGrid, boundElems[i].Nodes);
 
         /*--- Update config information storing the boundary information in the right place ---*/
         Tag_to_Marker[config->GetMarker_CfgFile_TagBound(Marker_Tag)] = Marker_Tag;
@@ -824,10 +802,8 @@ void CPhysicalGeometry::Read_SU2_Format_Parallel_FEM(CConfig        *config,
   mesh_file.close();
 }
 
-void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
-                                                      string         val_mesh_filename,
-                                                      unsigned short val_iZone,
-                                                      unsigned short val_nZone) {
+void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig* config, string val_mesh_filename,
+                                                      unsigned short val_iZone, unsigned short val_nZone) {
 #ifdef HAVE_CGNS
 
   /*--- For proper support of the high order elements, at least version 3.3
@@ -837,18 +813,26 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
   /*--- Check whether the supplied file is truly a CGNS file. ---*/
   int file_type;
   if (cg_is_cgns(val_mesh_filename.c_str(), &file_type) != CG_OK)
-    SU2_MPI::Error(val_mesh_filename + string(" is not a CGNS file that can be read."),
-                   CURRENT_FUNCTION);
+    SU2_MPI::Error(val_mesh_filename + string(" is not a CGNS file that can be read."), CURRENT_FUNCTION);
 
   /*--- Initialize counters for local/global points & elements ---*/
-  Global_nPoint  = 0; Global_nPointDomain   = 0; Global_nElem = 0;
-  nelem_edge     = 0; Global_nelem_edge     = 0;
-  nelem_triangle = 0; Global_nelem_triangle = 0;
-  nelem_quad     = 0; Global_nelem_quad     = 0;
-  nelem_tetra    = 0; Global_nelem_tetra    = 0;
-  nelem_hexa     = 0; Global_nelem_hexa     = 0;
-  nelem_prism    = 0; Global_nelem_prism    = 0;
-  nelem_pyramid  = 0; Global_nelem_pyramid  = 0;
+  Global_nPoint = 0;
+  Global_nPointDomain = 0;
+  Global_nElem = 0;
+  nelem_edge = 0;
+  Global_nelem_edge = 0;
+  nelem_triangle = 0;
+  Global_nelem_triangle = 0;
+  nelem_quad = 0;
+  Global_nelem_quad = 0;
+  nelem_tetra = 0;
+  Global_nelem_tetra = 0;
+  nelem_hexa = 0;
+  Global_nelem_hexa = 0;
+  nelem_prism = 0;
+  Global_nelem_prism = 0;
+  nelem_pyramid = 0;
+  Global_nelem_pyramid = 0;
 
   /*--------------------------------------------------------------------------*/
   /*---       Checking of the file, determine the dimensions, etc.         ---*/
@@ -858,20 +842,20 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
         These arrays are the size of the number of ranks. ---*/
   beg_node = new unsigned long[size];
   end_node = new unsigned long[size];
-  nPointLinear  = new unsigned long[size];
+  nPointLinear = new unsigned long[size];
 
   /* Open the CGNS file for reading and check if it went OK. */
   int fn;
-  if(cg_open(val_mesh_filename.c_str(), CG_MODE_READ, &fn) != CG_OK) cg_error_exit();
-  if(rank == MASTER_NODE) {
+  if (cg_open(val_mesh_filename.c_str(), CG_MODE_READ, &fn) != CG_OK) cg_error_exit();
+  if (rank == MASTER_NODE) {
     cout << "Reading the CGNS file: " << val_mesh_filename << "." << endl;
   }
 
   /* Get the number of databases. This is the highest node in the CGNS heirarchy.
      The current implementation assumes that there is only one database. */
   int nbases;
-  if(cg_nbases(fn, &nbases) != CG_OK) cg_error_exit();
-  if(nbases > 1) {
+  if (cg_nbases(fn, &nbases) != CG_OK) cg_error_exit();
+  if (nbases > 1) {
     ostringstream message;
     message << "CGNS file contains " << nbases << " databases." << endl;
     message << "CGNS reader can handle only 1 at the moment." << endl;
@@ -881,22 +865,22 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
 
   /* Read the information of the base, especially the number of dimensions. */
   char cgnsname[CGNS_STRING_SIZE];
-  int  cellDim, physDim;
+  int cellDim, physDim;
   const int iBase = 1;
-  if(cg_base_read(fn, iBase, cgnsname, &cellDim, &physDim)) cg_error_exit();
+  if (cg_base_read(fn, iBase, cgnsname, &cellDim, &physDim)) cg_error_exit();
   nDim = physDim;
 
-  if(cellDim != physDim) {
+  if (cellDim != physDim) {
     ostringstream message;
-    message << "The element dimension, " << cellDim
-            << ", differs from the physical dimension, " << physDim << "." << endl;
+    message << "The element dimension, " << cellDim << ", differs from the physical dimension, " << physDim << "."
+            << endl;
     message << "These should be the same for the DG-FEM solver." << endl;
 
     SU2_MPI::Error(message.str(), CURRENT_FUNCTION);
   }
 
   /* Write the info about the number of dimensions. */
-  if(rank == MASTER_NODE) {
+  if (rank == MASTER_NODE) {
     if (nDim == 2) cout << "Two dimensional problem." << endl;
     if (nDim == 3) cout << "Three dimensional problem." << endl;
   }
@@ -906,11 +890,11 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
   const int iZone = val_iZone + 1;
 
   int nzones;
-  if(cg_nzones(fn, iBase, &nzones) != CG_OK) cg_error_exit();
-  if(iZone < 1 || iZone > nzones) {
+  if (cg_nzones(fn, iBase, &nzones) != CG_OK) cg_error_exit();
+  if (iZone < 1 || iZone > nzones) {
     ostringstream message;
-    message << "Zone " << iZone << " requested for reading, but there are only "
-            << nzones << " zones present in the CGNS file." << endl;
+    message << "Zone " << iZone << " requested for reading, but there are only " << nzones
+            << " zones present in the CGNS file." << endl;
 
     SU2_MPI::Error(message.str(), CURRENT_FUNCTION);
   }
@@ -918,14 +902,13 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
   /* Determine the zone type for the requested zone and check if it is
      unstructured. */
   ZoneType_t zoneType;
-  if(cg_zone_type(fn, iBase, iZone, &zoneType) != CG_OK) cg_error_exit();
-  if(zoneType != Unstructured)
-    SU2_MPI::Error("Structured CGNS zone found while unstructured expected.",
-                   CURRENT_FUNCTION);
+  if (cg_zone_type(fn, iBase, iZone, &zoneType) != CG_OK) cg_error_exit();
+  if (zoneType != Unstructured)
+    SU2_MPI::Error("Structured CGNS zone found while unstructured expected.", CURRENT_FUNCTION);
 
   /* Determine the number of sections for the connectivities in this zone. */
   int nsections;
-  if(cg_nsections(fn, iBase, iZone, &nsections) != CG_OK) cg_error_exit();
+  if (cg_nsections(fn, iBase, iZone, &nsections) != CG_OK) cg_error_exit();
 
   /*--------------------------------------------------------------------------*/
   /*---            Reading and distributing the volume elements.           ---*/
@@ -936,20 +919,19 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
      Note that the indices start at 1 in CGNS. */
   vector<CCGNSElementType> CGNSElemTypes(nsections);
 
-  for(int iConn=1; iConn<=nsections; ++iConn) {
-    CGNSElemTypes[iConn-1].DetermineMetaData(nDim, fn, iBase, iZone, iConn);
-    if( CGNSElemTypes[iConn-1].volumeConn )
-      Global_nElem += CGNSElemTypes[iConn-1].nElem;
+  for (int iConn = 1; iConn <= nsections; ++iConn) {
+    CGNSElemTypes[iConn - 1].DetermineMetaData(nDim, fn, iBase, iZone, iConn);
+    if (CGNSElemTypes[iConn - 1].volumeConn) Global_nElem += CGNSElemTypes[iConn - 1].nElem;
   }
 
-  if((rank == MASTER_NODE) && (size > SINGLE_NODE))
+  if ((rank == MASTER_NODE) && (size > SINGLE_NODE))
     cout << Global_nElem << " interior elements before parallel partitioning." << endl;
 
   /*--- Check if the number of cores used is larger than the number of
         elements. Terminate if this is the case, because it does not make
         sense to do this. ---*/
-  unsigned long nCores = size;   // Correct for the number of cores per rank.
-  if(nCores > Global_nElem) {
+  unsigned long nCores = size;  // Correct for the number of cores per rank.
+  if (nCores > Global_nElem) {
     ostringstream message;
     message << "The number of cores, " << nCores;
     message << ", is larger than the number of elements, " << Global_nElem << "." << endl;
@@ -963,37 +945,36 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
         This is a linear partitioning with the addition of a simple load
         balancing for any remainder elements. ---*/
   unsigned long total_elem_accounted = 0;
-  for(unsigned long i = 0; i < (unsigned long)size; i++) {
-    nPointLinear[i] = Global_nElem/size;
+  for (unsigned long i = 0; i < (unsigned long)size; i++) {
+    nPointLinear[i] = Global_nElem / size;
     total_elem_accounted = total_elem_accounted + nPointLinear[i];
   }
 
   /*--- Get the number of remainder elements after the even division ---*/
   const unsigned long rem_elem = Global_nElem - total_elem_accounted;
-  for (unsigned long i = 0; i<rem_elem; i++) {
+  for (unsigned long i = 0; i < rem_elem; i++) {
     ++nPointLinear[i];
   }
 
   /*--- Store the local number of elements and the beginning/end index ---*/
   nElem = nPointLinear[rank];
   beg_node[0] = 0;
-  end_node[0]   = beg_node[0] + nPointLinear[0];
-  for(int i=1; i<size; i++) {
-    beg_node[i] = end_node[i-1];
-    end_node[i]   = beg_node[i] + nPointLinear[i] ;
+  end_node[0] = beg_node[0] + nPointLinear[0];
+  for (int i = 1; i < size; i++) {
+    beg_node[i] = end_node[i - 1];
+    end_node[i] = beg_node[i] + nPointLinear[i];
   }
 
   /*--- Allocate space for elements ---*/
-  elem = new CPrimalGrid*[nElem] ();
+  elem = new CPrimalGrid*[nElem]();
 
   /*--- Loop over over the connectivities and read the elements to be stored on
         this rank. Furthermore, determine the local amount of DOFs for the
         solution (which may differ from the number of DOFS for the grid). ---*/
   unsigned long nDOFsLoc = 0, elemCount = 0, locElemCount = 0;
 
-  for(int iConn=0; iConn<nsections; ++iConn) {
-    if( CGNSElemTypes[iConn].volumeConn ) {
-
+  for (int iConn = 0; iConn < nsections; ++iConn) {
+    if (CGNSElemTypes[iConn].volumeConn) {
       /* Determine the global volume element range for this connectivity. */
       const unsigned long elemCountOld = elemCount;
       elemCount += CGNSElemTypes[iConn].nElem;
@@ -1002,18 +983,16 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
       const unsigned long indBegOverlap = max(elemCountOld, beg_node[rank]);
       const unsigned long indEndOverlap = min(elemCount, end_node[rank]);
 
-      if(indEndOverlap > indBegOverlap) {
-
+      if (indEndOverlap > indBegOverlap) {
         /* This rank must read element data from this connectivity section.
            Determine the offset relative to the start of this section and the
            number of elements to be read by this rank. */
         const unsigned long offsetRank = indBegOverlap - elemCountOld;
-        const unsigned long nElemRank  = indEndOverlap - indBegOverlap;
+        const unsigned long nElemRank = indEndOverlap - indBegOverlap;
 
         /* Read the connectivity range determined above. */
-        CGNSElemTypes[iConn].ReadConnectivityRange(fn, iBase, iZone, offsetRank,
-                                                   nElemRank, beg_node[rank],
-                                                   elem, locElemCount, nDOFsLoc);
+        CGNSElemTypes[iConn].ReadConnectivityRange(fn, iBase, iZone, offsetRank, nElemRank, beg_node[rank], elem,
+                                                   locElemCount, nDOFsLoc);
       }
     }
   }
@@ -1022,17 +1001,14 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
   /* The global offset of the DOFs must be corrected when running in
      parallel. Therefore gather the number of DOFs of all the ranks. */
   vector<unsigned long> nDOFsPerRank(size);
-  SU2_MPI::Allgather(&nDOFsLoc, 1, MPI_UNSIGNED_LONG, nDOFsPerRank.data(), 1,
-                     MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
+  SU2_MPI::Allgather(&nDOFsLoc, 1, MPI_UNSIGNED_LONG, nDOFsPerRank.data(), 1, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
 
   /* Determine the offset for the DOFs on this rank. */
   unsigned long offsetRank = 0;
-  for(int i=0; i<rank; ++i)
-    offsetRank += nDOFsPerRank[i];
+  for (int i = 0; i < rank; ++i) offsetRank += nDOFsPerRank[i];
 
   /* Loop over the local elements to correct the global offset of the DOFs. */
-  for(unsigned long i=0; i<nElem; ++i)
-    elem[i]->AddOffsetGlobalDOFs(offsetRank);
+  for (unsigned long i = 0; i < nElem; ++i) elem[i]->AddOffsetGlobalDOFs(offsetRank);
 #endif
 
   /*--------------------------------------------------------------------------*/
@@ -1042,7 +1018,7 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
   /* Determine the global number of vertices in the requested zone.
      The other size information is not used. */
   cgsize_t sizes[3];
-  if(cg_zone_read(fn, iBase, iZone, cgnsname, sizes) != CG_OK) cg_error_exit();
+  if (cg_zone_read(fn, iBase, iZone, cgnsname, sizes) != CG_OK) cg_error_exit();
   Global_nPoint = sizes[0];
 
   /*--- Determine the number of points per rank in cumulative storage format.
@@ -1050,71 +1026,69 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
         The required coordinates for each rank are later obtained via
         communication.  ---*/
   unsigned long totalPointsAccounted = 0;
-  vector<cgsize_t> nPointsPerRank(size+1);
-  for(int i=1; i<=size; ++i) {
-    nPointsPerRank[i]    = Global_nPoint/size;
+  vector<cgsize_t> nPointsPerRank(size + 1);
+  for (int i = 1; i <= size; ++i) {
+    nPointsPerRank[i] = Global_nPoint / size;
     totalPointsAccounted += nPointsPerRank[i];
   }
 
   const unsigned long nPointsRem = Global_nPoint - totalPointsAccounted;
-  for(unsigned long i=1; i<=nPointsRem; ++i) ++nPointsPerRank[i];
+  for (unsigned long i = 1; i <= nPointsRem; ++i) ++nPointsPerRank[i];
 
   nPointsPerRank[0] = 0;
-  for(int i=0; i<size; ++i)
-    nPointsPerRank[i+1] += nPointsPerRank[i];
+  for (int i = 0; i < size; ++i) nPointsPerRank[i + 1] += nPointsPerRank[i];
 
   /* Determine the number of points that must be read by this rank and
      allocate the memory for the coordinate buffers. */
-  const cgsize_t nPointsRead = nPointsPerRank[rank+1] - nPointsPerRank[rank];
+  const cgsize_t nPointsRead = nPointsPerRank[rank + 1] - nPointsPerRank[rank];
   vector<vector<su2double> > coorBuf(nDim, vector<su2double>(nPointsRead));
 
   /* Loop over the number of dimensions to read the coordinates. Note that
      the loop starts at 1 and ends at nDim because CGNS requires this. */
-  for(unsigned short iDim=1; iDim<=nDim; ++iDim) {
-
+  for (unsigned short iDim = 1; iDim <= nDim; ++iDim) {
     /* Determine the data type and name of the coordinate. Copy the name
        of the coordinate in a string for easier comparison. */
     DataType_t datatype;
-    if(cg_coord_info(fn, iBase, iZone, iDim, &datatype, cgnsname) != CG_OK)
-      cg_error_exit();
+    if (cg_coord_info(fn, iBase, iZone, iDim, &datatype, cgnsname) != CG_OK) cg_error_exit();
     string coorname = cgnsname;
 
     /* Check the name of the coordinate and determine the index in coorBuf
        where to store this coordinate. Normally this should be iDim-1. */
     unsigned short indC = 0;
-    if(     coorname == "CoordinateX") indC = 0;
-    else if(coorname == "CoordinateY") indC = 1;
-    else if(coorname == "CoordinateZ") indC = 2;
+    if (coorname == "CoordinateX")
+      indC = 0;
+    else if (coorname == "CoordinateY")
+      indC = 1;
+    else if (coorname == "CoordinateZ")
+      indC = 2;
     else
-      SU2_MPI::Error(string("Unknown coordinate name, ") + coorname +
-                     string(", encountered in the CGNS file."), CURRENT_FUNCTION);
+      SU2_MPI::Error(string("Unknown coordinate name, ") + coorname + string(", encountered in the CGNS file."),
+                     CURRENT_FUNCTION);
 
     /* Easier storage of the range in the CGNS file. */
     cgsize_t range_min = nPointsPerRank[rank] + 1;
-    cgsize_t range_max = nPointsPerRank[rank+1];
+    cgsize_t range_max = nPointsPerRank[rank + 1];
 
     /*--- Read the coordinate with the required precision and copy
           this data to the correct index in coorBuf. ---*/
-    switch( datatype ) {
+    switch (datatype) {
       case RealSingle: {
         /* Single precision used. */
         vector<float> buf(nPointsRead);
-        if(cg_coord_read(fn, iBase, iZone, cgnsname, datatype, &range_min,
-                         &range_max, buf.data()) != CG_OK) cg_error_exit();
+        if (cg_coord_read(fn, iBase, iZone, cgnsname, datatype, &range_min, &range_max, buf.data()) != CG_OK)
+          cg_error_exit();
 
-        for(cgsize_t i=0; i<nPointsRead; ++i)
-          coorBuf[indC][i] = buf[i];
+        for (cgsize_t i = 0; i < nPointsRead; ++i) coorBuf[indC][i] = buf[i];
         break;
       }
 
       case RealDouble: {
         /* Double precision used. */
         vector<double> buf(nPointsRead);
-        if(cg_coord_read(fn, iBase, iZone, cgnsname, datatype, &range_min,
-                         &range_max, buf.data()) != CG_OK) cg_error_exit();
+        if (cg_coord_read(fn, iBase, iZone, cgnsname, datatype, &range_min, &range_max, buf.data()) != CG_OK)
+          cg_error_exit();
 
-        for(cgsize_t i=0; i<nPointsRead; ++i)
-          coorBuf[indC][i] = buf[i];
+        for (cgsize_t i = 0; i < nPointsRead; ++i) coorBuf[indC][i] = buf[i];
         break;
       }
 
@@ -1133,10 +1107,9 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
         node IDs of the local elements. ---*/
   vector<unsigned long> nodeIDsElemLoc;
   nodeIDsElemLoc.reserve(nDOFsLoc);
-  for(unsigned long i=0; i<locElemCount; ++i) {
+  for (unsigned long i = 0; i < locElemCount; ++i) {
     unsigned short nDOFsElem = elem[i]->GetnNodes();
-    for(unsigned short j=0; j<nDOFsElem; ++j)
-      nodeIDsElemLoc.push_back(elem[i]->GetNode(j));
+    for (unsigned short j = 0; j < nDOFsElem; ++j) nodeIDsElemLoc.push_back(elem[i]->GetNode(j));
   }
 
   sort(nodeIDsElemLoc.begin(), nodeIDsElemLoc.end());
@@ -1145,18 +1118,18 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
   nodeIDsElemLoc.erase(lastNode, nodeIDsElemLoc.end());
 
   /*--- Allocate the memory for the coordinates to be stored on this rank. ---*/
-  nPoint     = nodeIDsElemLoc.size();
+  nPoint = nodeIDsElemLoc.size();
   nodes = new CPoint(nPoint, nDim);
 
   /*--- Store the global ID's of the nodes in such a way that they can
         be sent to the rank that actually stores the coordinates.. ---*/
   vector<vector<unsigned long> > nodeBuf(size, vector<unsigned long>(0));
-  for(unsigned long i=0; i<nodeIDsElemLoc.size(); ++i) {
+  for (unsigned long i = 0; i < nodeIDsElemLoc.size(); ++i) {
     const cgsize_t nodeID = nodeIDsElemLoc[i];
     vector<cgsize_t>::iterator low;
     low = lower_bound(nPointsPerRank.begin(), nPointsPerRank.end(), nodeID);
     cgsize_t rankNode = low - nPointsPerRank.begin();
-    if(*low > nodeID) --rankNode;
+    if (*low > nodeID) --rankNode;
 
     nodeBuf[rankNode].push_back(nodeIDsElemLoc[i]);
   }
@@ -1168,13 +1141,13 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
         node. ---*/
   int nRankSend = 0;
   vector<int> sendToRank(size, 0);
-  vector<unsigned long> startingIndRanksInNode(size+1);
+  vector<unsigned long> startingIndRanksInNode(size + 1);
   startingIndRanksInNode[0] = 0;
 
-  for(int i=0; i<size; ++i) {
-    startingIndRanksInNode[i+1] = startingIndRanksInNode[i] + nodeBuf[i].size();
+  for (int i = 0; i < size; ++i) {
+    startingIndRanksInNode[i + 1] = startingIndRanksInNode[i] + nodeBuf[i].size();
 
-    if( nodeBuf[i].size() ) {
+    if (nodeBuf[i].size()) {
       ++nRankSend;
       sendToRank[i] = 1;
     }
@@ -1182,17 +1155,16 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
 
   int nRankRecv;
   vector<int> sizeRecv(size, 1);
-  SU2_MPI::Reduce_scatter(sendToRank.data(), &nRankRecv, sizeRecv.data(),
-                          MPI_INT, MPI_SUM, SU2_MPI::GetComm());
+  SU2_MPI::Reduce_scatter(sendToRank.data(), &nRankRecv, sizeRecv.data(), MPI_INT, MPI_SUM, SU2_MPI::GetComm());
 
   /*--- Send out the messages with the global node numbers. Use nonblocking
         sends to avoid deadlock. ---*/
   vector<SU2_MPI::Request> sendReqs(nRankSend);
   nRankSend = 0;
-  for(int i=0; i<size; ++i) {
-    if( nodeBuf[i].size() ) {
-      SU2_MPI::Isend(nodeBuf[i].data(), nodeBuf[i].size(), MPI_UNSIGNED_LONG,
-                     i, i, SU2_MPI::GetComm(), &sendReqs[nRankSend]);
+  for (int i = 0; i < size; ++i) {
+    if (nodeBuf[i].size()) {
+      SU2_MPI::Isend(nodeBuf[i].data(), nodeBuf[i].size(), MPI_UNSIGNED_LONG, i, i, SU2_MPI::GetComm(),
+                     &sendReqs[nRankSend]);
       ++nRankSend;
     }
   }
@@ -1204,8 +1176,7 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
 
   /*--- Loop over the number of ranks from which this rank receives global
         point numbers that should be stored on this rank. ---*/
-  for(int i=0; i<nRankRecv; ++i) {
-
+  for (int i = 0; i < nRankRecv; ++i) {
     /* Block until a message arrives. Determine the source and size
        of the message. */
     SU2_MPI::Status status;
@@ -1218,51 +1189,47 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
     /* Allocate the memory for a buffer to receive this message and also
        for the buffer to return to coordinates. */
     vector<unsigned long> nodeRecvBuf(sizeMess);
-    coorReturnBuf[i].resize(nDim*sizeMess);
+    coorReturnBuf[i].resize(nDim * sizeMess);
 
     /* Receive the message using a blocking receive. */
-    SU2_MPI::Recv(nodeRecvBuf.data(), sizeMess, MPI_UNSIGNED_LONG,
-                  source, rank, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Recv(nodeRecvBuf.data(), sizeMess, MPI_UNSIGNED_LONG, source, rank, SU2_MPI::GetComm(), &status);
 
     /*--- Loop over the nodes just received and fill the return communication
           buffer with the coordinates of the requested nodes. ---*/
-    for(int j=0; j<sizeMess; ++j) {
-      const int jj = nDim*j;
+    for (int j = 0; j < sizeMess; ++j) {
+      const int jj = nDim * j;
       const long kk = nodeRecvBuf[j] - nPointsPerRank[rank];
-      if(kk < 0 || kk >= nPointsRead)
+      if (kk < 0 || kk >= nPointsRead)
         SU2_MPI::Error("Invalid point requested. This should not happen.", CURRENT_FUNCTION);
 
-      for(unsigned short k=0; k<nDim; ++k)
-        coorReturnBuf[i][jj+k] = coorBuf[k][kk];
+      for (unsigned short k = 0; k < nDim; ++k) coorReturnBuf[i][jj + k] = coorBuf[k][kk];
     }
 
     /* Send the buffer just filled back to the requesting rank.
        Use a non-blocking send to avoid deadlock. */
-    SU2_MPI::Isend(coorReturnBuf[i].data(), coorReturnBuf[i].size(), MPI_DOUBLE,
-                   source, source+1, SU2_MPI::GetComm(), &returnReqs[i]);
+    SU2_MPI::Isend(coorReturnBuf[i].data(), coorReturnBuf[i].size(), MPI_DOUBLE, source, source + 1, SU2_MPI::GetComm(),
+                   &returnReqs[i]);
   }
 
   /* Loop over the ranks from which this rank has requested coordinates. */
-  for(int i=0; i<nRankSend; ++i) {
-
+  for (int i = 0; i < nRankSend; ++i) {
     /* Block until a message arrives. Determine the source of the message. */
     SU2_MPI::Status status;
-    SU2_MPI::Probe(MPI_ANY_SOURCE, rank+1, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Probe(MPI_ANY_SOURCE, rank + 1, SU2_MPI::GetComm(), &status);
     int source = status.MPI_SOURCE;
 
     /* Allocate the memory for the coordinate receive buffer. */
-    vector<su2double> coorRecvBuf(nDim*nodeBuf[source].size());
+    vector<su2double> coorRecvBuf(nDim * nodeBuf[source].size());
 
     /* Receive the message using a blocking receive. */
-    SU2_MPI::Recv(coorRecvBuf.data(), coorRecvBuf.size(), MPI_DOUBLE,
-                  source, rank+1, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Recv(coorRecvBuf.data(), coorRecvBuf.size(), MPI_DOUBLE, source, rank + 1, SU2_MPI::GetComm(), &status);
 
     /*--- Make a distinction between 2D and 3D to store the data of the nodes.
           This data is created by taking the offset of the source rank into
           account. In this way the nodes are numbered with increading
           global node ID. ---*/
-    for(unsigned long j=0; j<nodeBuf[source].size(); ++j) {
-      const unsigned long jj = nDim*j;
+    for (unsigned long j = 0; j < nodeBuf[source].size(); ++j) {
+      const unsigned long jj = nDim * j;
       const unsigned long kk = startingIndRanksInNode[source] + j;
 
       nodes->SetCoord(kk, &coorRecvBuf[jj]);
@@ -1281,12 +1248,11 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
 #else
   /*--- Sequential mode. Create the data for the points. The global
         number of points equals the local number of points. ---*/
-  nPoint     = Global_nPoint;
+  nPoint = Global_nPoint;
   nodes = new CPoint(nPoint, nDim);
 
-  for(unsigned long i=0; i<nPoint; ++i) {
-    for (unsigned short iDim=0; iDim < nDim; ++iDim)
-      nodes->SetCoord(i, iDim, coorBuf[iDim][i]);
+  for (unsigned long i = 0; i < nPoint; ++i) {
+    for (unsigned short iDim = 0; iDim < nDim; ++iDim) nodes->SetCoord(i, iDim, coorBuf[iDim][i]);
     nodes->SetGlobalIndex(i, i);
   }
 
@@ -1301,23 +1267,21 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
 
   /*--- Determine the faces of the local elements. --- */
   vector<CFaceOfElement> localFaces;
-  for(unsigned long k=0; k<nElem; ++k) {
-
+  for (unsigned long k = 0; k < nElem; ++k) {
     /*--- Get the global IDs of the corner points of all the faces of this elements. ---*/
     unsigned short nFaces;
     unsigned short nPointsPerFace[6];
-    unsigned long  faceConn[6][4];
+    unsigned long faceConn[6][4];
 
     elem[k]->GetCornerPointsAllFaces(nFaces, nPointsPerFace, faceConn);
 
     /*--- Loop over the faces and add them to localFaces. For consistency
           between sequential and parallel mode the rank is stored at the
           position for the second element ID. ---*/
-    for(unsigned short i=0; i<nFaces; ++i) {
+    for (unsigned short i = 0; i < nFaces; ++i) {
       CFaceOfElement thisFace;
       thisFace.nCornerPoints = nPointsPerFace[i];
-      for(unsigned short j=0; j<nPointsPerFace[i]; ++j)
-        thisFace.cornerPoints[j] = faceConn[i][j];
+      for (unsigned short j = 0; j < nPointsPerFace[i]; ++j) thisFace.cornerPoints[j] = faceConn[i][j];
       thisFace.elemID0 = k + beg_node[rank];
       thisFace.elemID1 = rank;
 
@@ -1340,15 +1304,15 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
         based on nPointsPerRank. Define the communication buffers and
         determine their contents. ---*/
   vector<vector<unsigned long> > faceBuf(size, vector<unsigned long>(0));
-  for(unsigned long i=0; i<localFaces.size(); ++i) {
+  for (unsigned long i = 0; i < localFaces.size(); ++i) {
     const cgsize_t nodeID = localFaces[i].cornerPoints[0];
     vector<cgsize_t>::iterator low;
     low = lower_bound(nPointsPerRank.begin(), nPointsPerRank.end(), nodeID);
     cgsize_t rankNode = low - nPointsPerRank.begin();
-    if(*low > nodeID) --rankNode;
+    if (*low > nodeID) --rankNode;
 
     faceBuf[rankNode].push_back(localFaces[i].nCornerPoints);
-    for(unsigned short j=0; j<localFaces[i].nCornerPoints; ++j)
+    for (unsigned short j = 0; j < localFaces[i].nCornerPoints; ++j)
       faceBuf[rankNode].push_back(localFaces[i].cornerPoints[j]);
     faceBuf[rankNode].push_back(localFaces[i].elemID0);
   }
@@ -1359,37 +1323,34 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
 
   /*--- Determine the number of messages this rank will send and receive. ---*/
   nRankSend = 0;
-  for(int i=0; i<size; ++i) {
-    if( faceBuf[i].size() ) {
+  for (int i = 0; i < size; ++i) {
+    if (faceBuf[i].size()) {
       ++nRankSend;
       sendToRank[i] = 1;
-    }
-    else {
+    } else {
       sendToRank[i] = 0;
     }
   }
 
-  SU2_MPI::Reduce_scatter(sendToRank.data(), &nRankRecv, sizeRecv.data(),
-                          MPI_INT, MPI_SUM, SU2_MPI::GetComm());
+  SU2_MPI::Reduce_scatter(sendToRank.data(), &nRankRecv, sizeRecv.data(), MPI_INT, MPI_SUM, SU2_MPI::GetComm());
 
   /*--- Send the messages using non-blocking sends to avoid deadlock. ---*/
   sendReqs.resize(nRankSend);
   nRankSend = 0;
-  for(int i=0; i<size; ++i) {
-    if( faceBuf[i].size() ) {
-      SU2_MPI::Isend(faceBuf[i].data(), faceBuf[i].size(), MPI_UNSIGNED_LONG,
-                     i, i+4, SU2_MPI::GetComm(), &sendReqs[nRankSend]);
+  for (int i = 0; i < size; ++i) {
+    if (faceBuf[i].size()) {
+      SU2_MPI::Isend(faceBuf[i].data(), faceBuf[i].size(), MPI_UNSIGNED_LONG, i, i + 4, SU2_MPI::GetComm(),
+                     &sendReqs[nRankSend]);
       ++nRankSend;
     }
   }
 
   /* Loop over the number of ranks from which this rank will receive data. */
-  for(int i=0; i<nRankRecv; ++i) {
-
+  for (int i = 0; i < nRankRecv; ++i) {
     /* Block until a message arrives and determine the source and size
        of the message. */
     SU2_MPI::Status status;
-    SU2_MPI::Probe(MPI_ANY_SOURCE, rank+4, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Probe(MPI_ANY_SOURCE, rank + 4, SU2_MPI::GetComm(), &status);
     int source = status.MPI_SOURCE;
 
     int sizeMess;
@@ -1398,22 +1359,20 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
     /* Allocate the memory for the receive buffer and receive the
        message using a non-blocking receive. */
     vector<unsigned long> faceRecvBuf(sizeMess);
-    SU2_MPI::Recv(faceRecvBuf.data(), faceRecvBuf.size(), MPI_UNSIGNED_LONG,
-                  source, rank+4, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Recv(faceRecvBuf.data(), faceRecvBuf.size(), MPI_UNSIGNED_LONG, source, rank + 4, SU2_MPI::GetComm(),
+                  &status);
 
     /* Loop to extract the data from the receive buffer. */
     int ii = 0;
-    while(ii < sizeMess) {
-
+    while (ii < sizeMess) {
       /* Store the data for this face in localFaces. The rank where the
          corresponding element is physically present is stored in the
          second element ID. Note that it is not necessary to create a unique
          numbering anymore, because this has already been done before the
          communication buffer was created. */
       CFaceOfElement thisFace;
-      thisFace.nCornerPoints = (unsigned short) faceRecvBuf[ii++];
-      for(unsigned short j=0; j<thisFace.nCornerPoints; ++j, ++ii)
-        thisFace.cornerPoints[j] = faceRecvBuf[ii];
+      thisFace.nCornerPoints = (unsigned short)faceRecvBuf[ii++];
+      for (unsigned short j = 0; j < thisFace.nCornerPoints; ++j, ++ii) thisFace.cornerPoints[j] = faceRecvBuf[ii];
       thisFace.elemID0 = faceRecvBuf[ii++];
 
       thisFace.elemID1 = source;
@@ -1442,45 +1401,46 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
      Note that when multiple zones are present, this step is repeated for
      every zone. */
   int nFamilies;
-  if(cg_nfamilies(fn, iBase, &nFamilies) != CG_OK) cg_error_exit();
+  if (cg_nfamilies(fn, iBase, &nFamilies) != CG_OK) cg_error_exit();
 
   vector<string> familyNames(nFamilies);
-  for(int i=1; i<=nFamilies; ++i) {
+  for (int i = 1; i <= nFamilies; ++i) {
     int nFamBC, nGeo;
-    if(cg_family_read(fn, iBase, i, cgnsname, &nFamBC, &nGeo) != CG_OK) cg_error_exit();
-    familyNames[i-1] = cgnsname;
+    if (cg_family_read(fn, iBase, i, cgnsname, &nFamBC, &nGeo) != CG_OK) cg_error_exit();
+    familyNames[i - 1] = cgnsname;
   }
 
   /* Determine the number of boundary conditions for this zone. */
   int nBCs;
-  if(cg_nbocos(fn, iBase, iZone, &nBCs) != CG_OK) cg_error_exit();
+  if (cg_nbocos(fn, iBase, iZone, &nBCs) != CG_OK) cg_error_exit();
 
   /* Read the names of the boundary conditions and determine their family names.
      If not family name is specified for a boundary condition, the family name
      is set to the name of the boundary condition. */
   vector<string> BCNames(nBCs), BCFamilyNames(nBCs);
-  for(int i=1; i<=nBCs; ++i) {
-
+  for (int i = 1; i <= nBCs; ++i) {
     /* Read the info for this boundary condition. */
     BCType_t BCType;
     PointSetType_t ptsetType;
     cgsize_t npnts, NormalListSize;
     int NormalIndex, nDataSet;
     DataType_t NormalDataType;
-    if(cg_boco_info(fn, iBase, iZone, i, cgnsname, &BCType, &ptsetType,
-                    &npnts, &NormalIndex, &NormalListSize, &NormalDataType,
-                    &nDataSet) != CG_OK) cg_error_exit();
-    BCNames[i-1] = cgnsname;
+    if (cg_boco_info(fn, iBase, iZone, i, cgnsname, &BCType, &ptsetType, &npnts, &NormalIndex, &NormalListSize,
+                     &NormalDataType, &nDataSet) != CG_OK)
+      cg_error_exit();
+    BCNames[i - 1] = cgnsname;
 
     /* Read the possibly family name and set it. If not present, it is
        equal to BCName. */
-    if(cg_goto(fn, iBase, "Zone_t", iZone, "ZoneBC_t", 1,
-               "BC_t", i, "end") != CG_OK) cg_error_exit();
+    if (cg_goto(fn, iBase, "Zone_t", iZone, "ZoneBC_t", 1, "BC_t", i, "end") != CG_OK) cg_error_exit();
 
     int ierr = cg_famname_read(cgnsname);
-    if(ierr ==  CG_ERROR)  cg_error_exit();
-    else if(ierr == CG_OK) BCFamilyNames[i-1] = cgnsname;
-    else                   BCFamilyNames[i-1] = BCNames[i-1];
+    if (ierr == CG_ERROR)
+      cg_error_exit();
+    else if (ierr == CG_OK)
+      BCFamilyNames[i - 1] = cgnsname;
+    else
+      BCFamilyNames[i - 1] = BCNames[i - 1];
   }
 
   /*--- Determine the number of different surface connectivities. It is
@@ -1491,9 +1451,8 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
   vector<string> surfaceNames;
   vector<vector<int> > surfaceConnIDs;
 
-  for(int i=0; i<nsections; ++i) {
-    if( CGNSElemTypes[i].surfaceConn ) {
-
+  for (int i = 0; i < nsections; ++i) {
+    if (CGNSElemTypes[i].surfaceConn) {
       /*--- Determine the surface name to use for this connectivity.
             This name is determined as follows (in terms of importance).
             1) Family name specified for this connectivity.
@@ -1504,17 +1463,18 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
       const int connID = CGNSElemTypes[i].connID;
 
       /* First try to read the family name for the connectivity. */
-      if(cg_goto(fn, iBase, "Zone_t", iZone,
-                 "Elements_t", connID, "end") != CG_OK) cg_error_exit();
+      if (cg_goto(fn, iBase, "Zone_t", iZone, "Elements_t", connID, "end") != CG_OK) cg_error_exit();
       int ierr = cg_famname_read(cgnsname);
-      if(ierr ==  CG_ERROR)  cg_error_exit();
-      else if(ierr == CG_OK) thisSurfaceName = cgnsname;
+      if (ierr == CG_ERROR)
+        cg_error_exit();
+      else if (ierr == CG_OK)
+        thisSurfaceName = cgnsname;
       else {
         /* No family name. Check the boundary conditions. It is assumed that
            the boundary conditions have the same name as the connectivities. */
         int j;
-        for(j=0; j<nBCs; ++j) {
-          if(BCNames[j] == CGNSElemTypes[i].connName) {
+        for (j = 0; j < nBCs; ++j) {
+          if (BCNames[j] == CGNSElemTypes[i].connName) {
             thisSurfaceName = BCFamilyNames[j];
             break;
           }
@@ -1522,21 +1482,21 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
 
         /* If the name is not found in the boundary conditions, set the name
            of this surface connectivity to the name of this connectivity. */
-        if(j == nBCs) thisSurfaceName = CGNSElemTypes[i].connName;
+        if (j == nBCs) thisSurfaceName = CGNSElemTypes[i].connName;
       }
 
       /* Loop over the previously stored surface names and check if this
          surface name is already present. */
       unsigned long j;
-      for(j=0; j<surfaceNames.size(); ++j) {
-        if(thisSurfaceName == surfaceNames[j]) {
+      for (j = 0; j < surfaceNames.size(); ++j) {
+        if (thisSurfaceName == surfaceNames[j]) {
           surfaceConnIDs[j].push_back(i);
         }
       }
 
       /* If the surface name is not stored yet, create new entries in
           surfaceNames and surfaceConnIDs. */
-      if(j == surfaceNames.size()) {
+      if (j == surfaceNames.size()) {
         surfaceNames.push_back(thisSurfaceName);
         vector<int> thisSurfaceConn(1, i);
         surfaceConnIDs.push_back(thisSurfaceConn);
@@ -1547,7 +1507,7 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
   /* Write a message about the number of surface markers and allocate the
      memory for the data structures to store the required information. */
   nMarker = surfaceNames.size();
-  if(rank == MASTER_NODE) cout << nMarker << " surface markers." << endl;
+  if (rank == MASTER_NODE) cout << nMarker << " surface markers." << endl;
   config->SetnMarker_All(nMarker);
 
   unsigned short nMarker_Max = config->GetnMarker_Max();
@@ -1557,42 +1517,39 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
   Tag_to_Marker = new string[nMarker_Max];
 
   /* Loop over the number of markers to read and distribute the connectivities. */
-  for(unsigned short iMarker = 0 ; iMarker < nMarker; ++iMarker) {
-
+  for (unsigned short iMarker = 0; iMarker < nMarker; ++iMarker) {
     /* Easier storage of the entries in CGNSElemTypes that contribute
        to this boundary marker. */
     const int nEntries = surfaceConnIDs[iMarker].size();
-    const int *entries = surfaceConnIDs[iMarker].data();
+    const int* entries = surfaceConnIDs[iMarker].data();
 
     /* Determine the global number of elements for this boundary marker. */
     cgsize_t nElem_Bound_Global = 0;
-    for(int iConn=0; iConn<nEntries; ++iConn)
-      nElem_Bound_Global += CGNSElemTypes[entries[iConn]].nElem;
+    for (int iConn = 0; iConn < nEntries; ++iConn) nElem_Bound_Global += CGNSElemTypes[entries[iConn]].nElem;
 
     /* Write a message about the global number of surface elements
        present in this marker. */
     string Marker_Tag = surfaceNames[iMarker];
-    if(rank == MASTER_NODE)
-      cout << nElem_Bound_Global  << " boundary elements in index "<< iMarker
-           <<" (Marker = " << Marker_Tag << ")." << endl;
+    if (rank == MASTER_NODE)
+      cout << nElem_Bound_Global << " boundary elements in index " << iMarker << " (Marker = " << Marker_Tag << ")."
+           << endl;
 
     /* Determine the number of surface elements per rank in cumulative storage
        format. This is done to avoid that every rank reads all the elements.
        This is to avoid that every rank reads all the elements. The correct
        rank for storage is determined later via communication. */
     unsigned long totalBoundElemAccounted = 0;
-    vector<unsigned long> nBoundElemPerRank(size+1);
-    for(int i=1; i<=size; ++i) {
-      nBoundElemPerRank[i]     = nElem_Bound_Global/size;
+    vector<unsigned long> nBoundElemPerRank(size + 1);
+    for (int i = 1; i <= size; ++i) {
+      nBoundElemPerRank[i] = nElem_Bound_Global / size;
       totalBoundElemAccounted += nBoundElemPerRank[i];
     }
 
     const unsigned long nBoundElemRem = nElem_Bound_Global - totalBoundElemAccounted;
-    for(unsigned long i=1; i<=nBoundElemRem; ++i) ++nBoundElemPerRank[i];
+    for (unsigned long i = 1; i <= nBoundElemRem; ++i) ++nBoundElemPerRank[i];
 
     nBoundElemPerRank[0] = 0;
-    for(int i=0; i<size; ++i)
-      nBoundElemPerRank[i+1] += nBoundElemPerRank[i];
+    for (int i = 0; i < size; ++i) nBoundElemPerRank[i + 1] += nBoundElemPerRank[i];
 
     /* Define a vector of FEM boundary elements to store the local
        boundary faces to be read. */
@@ -1600,28 +1557,25 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
 
     /* Loop over the connectivity sections that contribute. */
     elemCount = locElemCount = 0;
-    for(int iConn=0; iConn<nEntries; ++iConn) {
-
+    for (int iConn = 0; iConn < nEntries; ++iConn) {
       /* Determine the global range for this connectivity. */
       const unsigned long elemCountOld = elemCount;
       elemCount += CGNSElemTypes[entries[iConn]].nElem;
 
       /* Check for overlap with the element range this rank is responsible for. */
       const unsigned long indBegOverlap = max(elemCountOld, nBoundElemPerRank[rank]);
-      const unsigned long indEndOverlap = min(elemCount, nBoundElemPerRank[rank+1]);
-
-      if(indEndOverlap > indBegOverlap) {
+      const unsigned long indEndOverlap = min(elemCount, nBoundElemPerRank[rank + 1]);
 
+      if (indEndOverlap > indBegOverlap) {
         /* This rank must read boundary element data from this connectivity
            section. Determine the offset relative to the start of this section
            and the number of elements to be read by this rank. */
         const unsigned long offsetRank = indBegOverlap - elemCountOld;
-        const unsigned long nElemRank  = indEndOverlap - indBegOverlap;
+        const unsigned long nElemRank = indEndOverlap - indBegOverlap;
 
         /* Read the connectivity range determined above. */
-        CGNSElemTypes[entries[iConn]].ReadBoundaryConnectivityRange(fn, iBase, iZone, offsetRank,
-                                                                    nElemRank, nBoundElemPerRank[rank],
-                                                                    locElemCount, boundElems);
+        CGNSElemTypes[entries[iConn]].ReadBoundaryConnectivityRange(fn, iBase, iZone, offsetRank, nElemRank,
+                                                                    nBoundElemPerRank[rank], locElemCount, boundElems);
       }
     }
 
@@ -1631,18 +1585,15 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
           communicated to find out where it must be stored. First clear the
           contents of the faceBuf, such that it can be used again to send
           data to the appropiate rank. ---*/
-    for(int i=0; i<size; ++i) faceBuf[i].clear();
+    for (int i = 0; i < size; ++i) faceBuf[i].clear();
 
     /*-- Loop over the locally read boundary elements and store its contents
          in the appropiate location in faceBuf. ---*/
-    for(unsigned long i=0; i<boundElems.size(); ++i) {
-
+    for (unsigned long i = 0; i < boundElems.size(); ++i) {
       /* Create an object of the class CFaceOfElement to determine the
          node number that determines on which rank the corresponding face
          in localFaces is stored. */
-      CFaceOfElement thisFace(boundElems[i].VTK_Type,
-                              boundElems[i].nPolyGrid,
-                              boundElems[i].Nodes.data());
+      CFaceOfElement thisFace(boundElems[i].VTK_Type, boundElems[i].nPolyGrid, boundElems[i].Nodes.data());
       thisFace.CreateUniqueNumbering();
 
       /* Determine the rank to which this face must be sent to. */
@@ -1650,16 +1601,14 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
       vector<cgsize_t>::iterator low;
       low = lower_bound(nPointsPerRank.begin(), nPointsPerRank.end(), nodeID);
       cgsize_t rankNode = low - nPointsPerRank.begin();
-      if(*low > nodeID) --rankNode;
+      if (*low > nodeID) --rankNode;
 
       /*--- Copy the relevant data of this boundary element into faceBuf. ---*/
       faceBuf[rankNode].push_back(boundElems[i].VTK_Type);
       faceBuf[rankNode].push_back(boundElems[i].nPolyGrid);
       faceBuf[rankNode].push_back(boundElems[i].nDOFsGrid);
       faceBuf[rankNode].push_back(boundElems[i].globalBoundElemID);
-      faceBuf[rankNode].insert(faceBuf[rankNode].end(),
-                               boundElems[i].Nodes.begin(),
-                               boundElems[i].Nodes.end());
+      faceBuf[rankNode].insert(faceBuf[rankNode].end(), boundElems[i].Nodes.begin(), boundElems[i].Nodes.end());
     }
 
     /* The contents of boundElems is copied into faceBuf, so it can
@@ -1668,42 +1617,39 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
 
     /*--- Determine the number of messages this rank will send and receive. ---*/
     nRankSend = 0;
-    for(int i=0; i<size; ++i) {
-      if( faceBuf[i].size() ) {
+    for (int i = 0; i < size; ++i) {
+      if (faceBuf[i].size()) {
         ++nRankSend;
         sendToRank[i] = 1;
-      }
-      else {
+      } else {
         sendToRank[i] = 0;
       }
     }
 
-    SU2_MPI::Reduce_scatter(sendToRank.data(), &nRankRecv, sizeRecv.data(),
-                            MPI_INT, MPI_SUM, SU2_MPI::GetComm());
+    SU2_MPI::Reduce_scatter(sendToRank.data(), &nRankRecv, sizeRecv.data(), MPI_INT, MPI_SUM, SU2_MPI::GetComm());
 
     /*--- Send the messages using non-blocking sends to avoid deadlock. ---*/
     sendReqs.resize(nRankSend);
     nRankSend = 0;
-    for(int i=0; i<size; ++i) {
-      if( faceBuf[i].size() ) {
-        SU2_MPI::Isend(faceBuf[i].data(), faceBuf[i].size(), MPI_UNSIGNED_LONG,
-                       i, i+5, SU2_MPI::GetComm(), &sendReqs[nRankSend]);
+    for (int i = 0; i < size; ++i) {
+      if (faceBuf[i].size()) {
+        SU2_MPI::Isend(faceBuf[i].data(), faceBuf[i].size(), MPI_UNSIGNED_LONG, i, i + 5, SU2_MPI::GetComm(),
+                       &sendReqs[nRankSend]);
         ++nRankSend;
       }
     }
 
     /* Use nodeBuf as storage for the sending of the surface element data
        to the correct rank. First clear its contents. */
-    for(int i=0; i<size; ++i) nodeBuf[i].clear();
+    for (int i = 0; i < size; ++i) nodeBuf[i].clear();
 
     /*--- Loop over the number of ranks from which this rank receives
           surface elements to be processed. ---*/
-    for(int i=0; i<nRankRecv; ++i) {
-
+    for (int i = 0; i < nRankRecv; ++i) {
       /* Block until a message arrives. Determine the source and size
          of the message. */
       SU2_MPI::Status status;
-      SU2_MPI::Probe(MPI_ANY_SOURCE, rank+5, SU2_MPI::GetComm(), &status);
+      SU2_MPI::Probe(MPI_ANY_SOURCE, rank + 5, SU2_MPI::GetComm(), &status);
       int source = status.MPI_SOURCE;
 
       int sizeMess;
@@ -1712,20 +1658,19 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
       /* Allocate the memory for the receive buffer and receive the message
          using a blocking send. */
       vector<unsigned long> boundElemRecvBuf(sizeMess);
-      SU2_MPI::Recv(boundElemRecvBuf.data(), sizeMess, MPI_UNSIGNED_LONG,
-                    source, rank+5, SU2_MPI::GetComm(), &status);
+      SU2_MPI::Recv(boundElemRecvBuf.data(), sizeMess, MPI_UNSIGNED_LONG, source, rank + 5, SU2_MPI::GetComm(),
+                    &status);
 
       /* Loop to extract the data from the receive buffer. */
       int ii = 0;
-      while(ii < sizeMess) {
-
+      while (ii < sizeMess) {
         /* Store the data for this boundary element. */
-        const unsigned short VTK_Type  = (unsigned short) boundElemRecvBuf[ii++];
-        const unsigned short nPolyGrid = (unsigned short) boundElemRecvBuf[ii++];
-        const unsigned short nDOFsGrid = (unsigned short) boundElemRecvBuf[ii++];
+        const unsigned short VTK_Type = (unsigned short)boundElemRecvBuf[ii++];
+        const unsigned short nPolyGrid = (unsigned short)boundElemRecvBuf[ii++];
+        const unsigned short nDOFsGrid = (unsigned short)boundElemRecvBuf[ii++];
 
         const unsigned long globalBoundElemID = boundElemRecvBuf[ii++];
-        const unsigned long *Nodes            = boundElemRecvBuf.data() + ii;
+        const unsigned long* Nodes = boundElemRecvBuf.data() + ii;
         ii += nDOFsGrid;
 
         /* Determine the corner nodes and store them in an object of
@@ -1739,18 +1684,17 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
         low = lower_bound(localFaces.begin(), localFaces.end(), thisFace);
 
         bool thisFaceFound = false;
-        if(low != localFaces.end()) {
-          if( !(thisFace < *low) ) thisFaceFound = true;
+        if (low != localFaces.end()) {
+          if (!(thisFace < *low)) thisFaceFound = true;
         }
 
-        if( !thisFaceFound )
-          SU2_MPI::Error("Boundary element not found in list of faces. This is a bug.",
-                         CURRENT_FUNCTION);
+        if (!thisFaceFound)
+          SU2_MPI::Error("Boundary element not found in list of faces. This is a bug.", CURRENT_FUNCTION);
 
         /* Determine the domain element and the rank where
            this boundary element should be sent to.. */
         const unsigned long domainElementID = low->elemID0;
-        const int rankBoundElem = (int) low->elemID1;
+        const int rankBoundElem = (int)low->elemID1;
 
         /*--- Store the data for this element in the communication buffer
               for rankBoundElem. ---*/
@@ -1760,8 +1704,7 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
         nodeBuf[rankBoundElem].push_back(globalBoundElemID);
         nodeBuf[rankBoundElem].push_back(domainElementID);
 
-        for(unsigned short j=0; j<nDOFsGrid; ++j)
-          nodeBuf[rankBoundElem].push_back(Nodes[j]);
+        for (unsigned short j = 0; j < nDOFsGrid; ++j) nodeBuf[rankBoundElem].push_back(Nodes[j]);
       }
     }
 
@@ -1770,38 +1713,35 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
 
     /*--- Determine the number of messages this rank will send and receive. ---*/
     nRankSend = 0;
-    for(int i=0; i<size; ++i) {
-      if( nodeBuf[i].size() ) {
+    for (int i = 0; i < size; ++i) {
+      if (nodeBuf[i].size()) {
         ++nRankSend;
         sendToRank[i] = 1;
-      }
-      else {
+      } else {
         sendToRank[i] = 0;
       }
     }
 
-    SU2_MPI::Reduce_scatter(sendToRank.data(), &nRankRecv, sizeRecv.data(),
-                            MPI_INT, MPI_SUM, SU2_MPI::GetComm());
+    SU2_MPI::Reduce_scatter(sendToRank.data(), &nRankRecv, sizeRecv.data(), MPI_INT, MPI_SUM, SU2_MPI::GetComm());
 
     /*--- Send the messages using non-blocking sends to avoid deadlock. ---*/
     sendReqs.resize(nRankSend);
     nRankSend = 0;
-    for(int i=0; i<size; ++i) {
-      if( nodeBuf[i].size() ) {
-        SU2_MPI::Isend(nodeBuf[i].data(), nodeBuf[i].size(), MPI_UNSIGNED_LONG,
-                       i, i+6, SU2_MPI::GetComm(), &sendReqs[nRankSend]);
+    for (int i = 0; i < size; ++i) {
+      if (nodeBuf[i].size()) {
+        SU2_MPI::Isend(nodeBuf[i].data(), nodeBuf[i].size(), MPI_UNSIGNED_LONG, i, i + 6, SU2_MPI::GetComm(),
+                       &sendReqs[nRankSend]);
         ++nRankSend;
       }
     }
 
     /*--- Loop over the number of ranks from which this rank receives
           surface elements to be stored on this rank. ---*/
-    for(int i=0; i<nRankRecv; ++i) {
-
+    for (int i = 0; i < nRankRecv; ++i) {
       /* Block until a message arrives. Determine the source and size
          of the message. */
       SU2_MPI::Status status;
-      SU2_MPI::Probe(MPI_ANY_SOURCE, rank+6, SU2_MPI::GetComm(), &status);
+      SU2_MPI::Probe(MPI_ANY_SOURCE, rank + 6, SU2_MPI::GetComm(), &status);
       int source = status.MPI_SOURCE;
 
       int sizeMess;
@@ -1810,34 +1750,32 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
       /* Allocate the memory for the receive buffer and receive the message
          using a blocking send. */
       vector<unsigned long> boundElemRecvBuf(sizeMess);
-      SU2_MPI::Recv(boundElemRecvBuf.data(), sizeMess, MPI_UNSIGNED_LONG,
-                    source, rank+6, SU2_MPI::GetComm(), &status);
+      SU2_MPI::Recv(boundElemRecvBuf.data(), sizeMess, MPI_UNSIGNED_LONG, source, rank + 6, SU2_MPI::GetComm(),
+                    &status);
 
       /* Loop to extract the data from the receive buffer. */
       int ii = 0;
-      while(ii < sizeMess) {
-
+      while (ii < sizeMess) {
         /* Store the data for this boundary element. */
-        const unsigned short VTK_Type  = (unsigned short) boundElemRecvBuf[ii++];
-        const unsigned short nPolyGrid = (unsigned short) boundElemRecvBuf[ii++];
-        const unsigned short nDOFsGrid = (unsigned short) boundElemRecvBuf[ii++];
+        const unsigned short VTK_Type = (unsigned short)boundElemRecvBuf[ii++];
+        const unsigned short nPolyGrid = (unsigned short)boundElemRecvBuf[ii++];
+        const unsigned short nDOFsGrid = (unsigned short)boundElemRecvBuf[ii++];
 
         const unsigned long globalBoundElemID = boundElemRecvBuf[ii++];
-        const unsigned long domainElementID   = boundElemRecvBuf[ii++];
-        const unsigned long *Nodes            = boundElemRecvBuf.data() + ii;
+        const unsigned long domainElementID = boundElemRecvBuf[ii++];
+        const unsigned long* Nodes = boundElemRecvBuf.data() + ii;
         ii += nDOFsGrid;
 
         /* Create an object of CBoundaryFace and store it in boundElems. */
         CBoundaryFace thisBoundFace;
-        thisBoundFace.VTK_Type          = VTK_Type;
-        thisBoundFace.nPolyGrid         = nPolyGrid;
-        thisBoundFace.nDOFsGrid         = nDOFsGrid;
+        thisBoundFace.VTK_Type = VTK_Type;
+        thisBoundFace.nPolyGrid = nPolyGrid;
+        thisBoundFace.nDOFsGrid = nDOFsGrid;
         thisBoundFace.globalBoundElemID = globalBoundElemID;
-        thisBoundFace.domainElementID   = domainElementID;
+        thisBoundFace.domainElementID = domainElementID;
 
         thisBoundFace.Nodes.resize(nDOFsGrid);
-        for(unsigned short j=0; j<nDOFsGrid; ++j)
-          thisBoundFace.Nodes[j] = Nodes[j];
+        for (unsigned short j = 0; j < nDOFsGrid; ++j) thisBoundFace.Nodes[j] = Nodes[j];
 
         boundElems.push_back(thisBoundFace);
       }
@@ -1857,13 +1795,10 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
     /*--- Sequential mode. All boundary elements read must be stored on this
           rank. The only information missing is the global ID of the domain
           element of the boundary elements. This is created below. ---*/
-    for(unsigned long i=0; i<boundElems.size(); ++i) {
-
+    for (unsigned long i = 0; i < boundElems.size(); ++i) {
       /* Determine the corner nodes and store them in an object of
          the class CFaceOfElement to carry out the search in localFaces. */
-      CFaceOfElement thisFace(boundElems[i].VTK_Type,
-                              boundElems[i].nPolyGrid,
-                              boundElems[i].Nodes.data());
+      CFaceOfElement thisFace(boundElems[i].VTK_Type, boundElems[i].nPolyGrid, boundElems[i].Nodes.data());
 
       /* Check if the face is actually present. If not, print an error message
          and exit. */
@@ -1872,13 +1807,12 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
       low = lower_bound(localFaces.begin(), localFaces.end(), thisFace);
 
       bool thisFaceFound = false;
-      if(low != localFaces.end()) {
-        if( !(thisFace < *low) ) thisFaceFound = true;
+      if (low != localFaces.end()) {
+        if (!(thisFace < *low)) thisFaceFound = true;
       }
 
-      if( !thisFaceFound )
-        SU2_MPI::Error("Boundary element not found in list of faces. This is a bug.",
-                       CURRENT_FUNCTION);
+      if (!thisFaceFound)
+        SU2_MPI::Error("Boundary element not found in list of faces. This is a bug.", CURRENT_FUNCTION);
 
       /* Set the domain element. */
       boundElems[i].domainElementID = low->elemID0;
@@ -1888,15 +1822,12 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
     /*--- Allocate space for the local boundary elements and copy the data
           from boundElems into bound. ---*/
     nElem_Bound[iMarker] = boundElems.size();
-    bound[iMarker] = new CPrimalGrid* [nElem_Bound[iMarker]];
+    bound[iMarker] = new CPrimalGrid*[nElem_Bound[iMarker]];
 
-    for(unsigned long i=0; i<nElem_Bound[iMarker]; ++i)
-      bound[iMarker][i] = new CPrimalGridBoundFEM(boundElems[i].globalBoundElemID,
-                                                  boundElems[i].domainElementID,
-                                                  boundElems[i].VTK_Type,
-                                                  boundElems[i].nPolyGrid,
-                                                  boundElems[i].nDOFsGrid,
-                                                  boundElems[i].Nodes);
+    for (unsigned long i = 0; i < nElem_Bound[iMarker]; ++i)
+      bound[iMarker][i] = new CPrimalGridBoundFEM(boundElems[i].globalBoundElemID, boundElems[i].domainElementID,
+                                                  boundElems[i].VTK_Type, boundElems[i].nPolyGrid,
+                                                  boundElems[i].nDOFsGrid, boundElems[i].Nodes);
 
     /*--- Update config information storing the boundary information in the right place ---*/
     Tag_to_Marker[config->GetMarker_CfgFile_TagBound(Marker_Tag)] = Marker_Tag;
@@ -1916,52 +1847,45 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig        *config,
   }
 
   /* Close the CGNS file again. */
-  if(cg_close(fn) != CG_OK) cg_error_exit();
-  if(rank == MASTER_NODE)
-    cout << "Successfully closed the CGNS file." << endl;
+  if (cg_close(fn) != CG_OK) cg_error_exit();
+  if (rank == MASTER_NODE) cout << "Successfully closed the CGNS file." << endl;
 
-#else  /* CGNS_VERSION >= 3300 */
+#else /* CGNS_VERSION >= 3300 */
 
-  SU2_MPI::Error("CGNS version 3.3 or higher is necessary for the DG FEM solver",
-                 CURRENT_FUNCTION);
+  SU2_MPI::Error("CGNS version 3.3 or higher is necessary for the DG FEM solver", CURRENT_FUNCTION);
 
 #endif /* CGNS_VERSION >= 3300 */
 
-#else  /* HAVE_CGNS. */
+#else /* HAVE_CGNS. */
 
-  SU2_MPI::Error("SU2 built without CGNS support!!\nTo use CGNS, build SU2 accordingly.",
-                 CURRENT_FUNCTION);
+  SU2_MPI::Error("SU2 built without CGNS support!!\nTo use CGNS, build SU2 accordingly.", CURRENT_FUNCTION);
 
-#endif  /* HAVE_CGNS. */
+#endif /* HAVE_CGNS. */
 }
 
-void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
-
+void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig* config) {
   /*--- Initialize the color vector of the elements. ---*/
-  for(unsigned long i=0; i<nElem; ++i)
-    elem[i]->SetColor(0);
+  for (unsigned long i = 0; i < nElem; ++i) elem[i]->SetColor(0);
 
   /*--- Determine the faces of the elements. ---*/
   vector<CFaceOfElement> localFaces;
-  for(unsigned long k=0; k<nElem; k++) {
-
+  for (unsigned long k = 0; k < nElem; k++) {
     /*--- Get the global IDs of the corner points of all the faces of this element. ---*/
     unsigned short nFaces;
     unsigned short nPointsPerFace[6];
-    unsigned long  faceConn[6][4];
+    unsigned long faceConn[6][4];
 
     elem[k]->GetCornerPointsAllFaces(nFaces, nPointsPerFace, faceConn);
 
     /*--- Loop over the faces and add them to localFaces. ---*/
-    for(unsigned short i=0; i<nFaces; ++i) {
+    for (unsigned short i = 0; i < nFaces; ++i) {
       CFaceOfElement thisFace;
       thisFace.nCornerPoints = nPointsPerFace[i];
-      for(unsigned short j=0; j<nPointsPerFace[i]; ++j)
-        thisFace.cornerPoints[j] = faceConn[i][j];
-      thisFace.elemID0    = beg_node[rank] + k;
-      thisFace.nPolySol0  = elem[k]->GetNPolySol();
+      for (unsigned short j = 0; j < nPointsPerFace[i]; ++j) thisFace.cornerPoints[j] = faceConn[i][j];
+      thisFace.elemID0 = beg_node[rank] + k;
+      thisFace.nPolySol0 = elem[k]->GetNPolySol();
       thisFace.nDOFsElem0 = elem[k]->GetNDOFsSol();
-      thisFace.elemType0  = elem[k]->GetVTK_Type();
+      thisFace.elemType0 = elem[k]->GetVTK_Type();
 
       thisFace.CreateUniqueNumbering();
       localFaces.push_back(thisFace);
@@ -1976,19 +1900,17 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
         overloaded function GetCornerPointsAllFaces, which explains the
         dimensions of the variables used in the function call. Also note that
         the periodic boundaries are excluded, because they are not physical.  ---*/
-  for(unsigned short iMarker=0; iMarker<nMarker; ++iMarker) {
-    if(config->GetMarker_All_KindBC(iMarker) != PERIODIC_BOUNDARY) {
-      for(unsigned long k=0; k<nElem_Bound[iMarker]; ++k) {
-
+  for (unsigned short iMarker = 0; iMarker < nMarker; ++iMarker) {
+    if (config->GetMarker_All_KindBC(iMarker) != PERIODIC_BOUNDARY) {
+      for (unsigned long k = 0; k < nElem_Bound[iMarker]; ++k) {
         unsigned short nFaces;
         unsigned short nPointsPerFace[6];
-        unsigned long  faceConn[6][4];
+        unsigned long faceConn[6][4];
         bound[iMarker][k]->GetCornerPointsAllFaces(nFaces, nPointsPerFace, faceConn);
 
         CFaceOfElement thisFace;
         thisFace.nCornerPoints = nPointsPerFace[0];
-        for(unsigned short j=0; j<nPointsPerFace[0]; ++j)
-          thisFace.cornerPoints[j] = faceConn[0][j];
+        for (unsigned short j = 0; j < nPointsPerFace[0]; ++j) thisFace.cornerPoints[j] = faceConn[0][j];
         thisFace.CreateUniqueNumbering();
 
         vector<CFaceOfElement>::iterator low;
@@ -2006,13 +1928,13 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
         found, the elemID from the second entry is copied to the first entry,
         the polynomial degree is updated, and the second entry is invalidated. ---*/
   unsigned long nFacesLoc = localFaces.size();
-  for(unsigned long i=1; i<nFacesLoc; ++i) {
-    if(localFaces[i] == localFaces[i-1]) {
-      localFaces[i-1].elemID1    = localFaces[i].elemID0;
-      localFaces[i-1].nPolySol1  = localFaces[i].nPolySol0;
-      localFaces[i-1].nDOFsElem1 = localFaces[i].nDOFsElem0;
-      localFaces[i-1].elemType1  = localFaces[i].elemType0;
-      localFaces[i].elemID0      = Global_nElem + 10;
+  for (unsigned long i = 1; i < nFacesLoc; ++i) {
+    if (localFaces[i] == localFaces[i - 1]) {
+      localFaces[i - 1].elemID1 = localFaces[i].elemID0;
+      localFaces[i - 1].nPolySol1 = localFaces[i].nPolySol0;
+      localFaces[i - 1].nDOFsElem1 = localFaces[i].nDOFsElem0;
+      localFaces[i - 1].elemType1 = localFaces[i].elemType0;
+      localFaces[i].elemID0 = Global_nElem + 10;
     }
   }
 
@@ -2022,8 +1944,8 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
         these faces at the end of the vector, see also the < operator
         of CFaceOfElement.                                         ---*/
   unsigned long nFacesLocOr = nFacesLoc;
-  for(unsigned long i=0; i<nFacesLocOr; ++i) {
-    if(localFaces[i].elemID0 > Global_nElem) {
+  for (unsigned long i = 0; i < nFacesLocOr; ++i) {
+    if (localFaces[i].elemID0 > Global_nElem) {
       localFaces[i].nCornerPoints = 4;
       localFaces[i].cornerPoints[0] = Global_nPoint;
       localFaces[i].cornerPoints[1] = Global_nPoint;
@@ -2045,98 +1967,94 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
         was found. For these faces the other neighbor might be stored on
         a different rank (unless there are non-matching interfaces).     ---*/
   vector<CFaceOfElement> localFacesComm;
-  for(unsigned long i=0; i<nFacesLoc; ++i)
-    if(localFaces[i].elemID1 > Global_nElem) localFacesComm.push_back(localFaces[i]);
+  for (unsigned long i = 0; i < nFacesLoc; ++i)
+    if (localFaces[i].elemID1 > Global_nElem) localFacesComm.push_back(localFaces[i]);
 
   /*--- Determine the maximum global point ID that occurs in localFacesComm
         of all ranks. Note that only the first point is taken into account,
         because this point determines the rank where the face is sent to. ---*/
   unsigned long nFacesLocComm = localFacesComm.size();
   unsigned long maxPointIDLoc = 0;
-  for(unsigned long i=0; i<nFacesLocComm; ++i)
+  for (unsigned long i = 0; i < nFacesLocComm; ++i)
     maxPointIDLoc = max(maxPointIDLoc, localFacesComm[i].cornerPoints[0]);
 
   unsigned long maxPointID;
-  SU2_MPI::Allreduce(&maxPointIDLoc, &maxPointID, 1, MPI_UNSIGNED_LONG,
-                     MPI_MAX, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&maxPointIDLoc, &maxPointID, 1, MPI_UNSIGNED_LONG, MPI_MAX, SU2_MPI::GetComm());
   ++maxPointID;
 
   /*--- Create a vector with a linear distribution over the ranks for
         the points that occur in the faces of localFacesComm.        ---*/
-  vector<unsigned long> facePointsProc(size+1, 0);
+  vector<unsigned long> facePointsProc(size + 1, 0);
   unsigned long total_point_accounted = 0;
-  for(unsigned long i=1; i<=(unsigned long)size; ++i) {
-   facePointsProc[i]      =  maxPointID/size;
-   total_point_accounted += facePointsProc[i];
+  for (unsigned long i = 1; i <= (unsigned long)size; ++i) {
+    facePointsProc[i] = maxPointID / size;
+    total_point_accounted += facePointsProc[i];
   }
 
   unsigned long rem_point = maxPointID - total_point_accounted;
-  for(unsigned long i=1; i<=rem_point; ++i)
-    ++facePointsProc[i];
+  for (unsigned long i = 1; i <= rem_point; ++i) ++facePointsProc[i];
 
-  for(unsigned long i=0; i<(unsigned long)size; ++i)
-    facePointsProc[i+1] += facePointsProc[i];
+  for (unsigned long i = 0; i < (unsigned long)size; ++i) facePointsProc[i + 1] += facePointsProc[i];
 
   /*--- Determine the number of faces that has to be sent to each rank.
         Note that the rank is stored in elemID1, such that the search
         does not have to be repeated below.               ---*/
   vector<unsigned long> nFacesComm(size, 0);
-  for(unsigned long i=0; i<nFacesLocComm; ++i) {
+  for (unsigned long i = 0; i < nFacesLocComm; ++i) {
     vector<unsigned long>::iterator low;
-    low = lower_bound(facePointsProc.begin(), facePointsProc.end(),
-                      localFacesComm[i].cornerPoints[0]);
+    low = lower_bound(facePointsProc.begin(), facePointsProc.end(), localFacesComm[i].cornerPoints[0]);
     unsigned long rankFace = low - facePointsProc.begin();
-    if(*low > localFacesComm[i].cornerPoints[0]) --rankFace;
+    if (*low > localFacesComm[i].cornerPoints[0]) --rankFace;
 
     ++nFacesComm[rankFace];
     localFacesComm[i].elemID1 = rankFace;
   }
 
   /*--- Create the send buffer for the faces to be communicated. ---*/
-  vector<unsigned long> sendBufFace(9*nFacesLocComm);
+  vector<unsigned long> sendBufFace(9 * nFacesLocComm);
   vector<unsigned long> counter(size);
   counter[0] = 0;
-  for(unsigned long i=1; i<(unsigned long)size; ++i)
-    counter[i] = counter[i-1] + 9*nFacesComm[i-1];
+  for (unsigned long i = 1; i < (unsigned long)size; ++i) counter[i] = counter[i - 1] + 9 * nFacesComm[i - 1];
 
-  for(unsigned long i=0; i<nFacesLocComm; ++i) {
+  for (unsigned long i = 0; i < nFacesLocComm; ++i) {
     unsigned long rankFace = localFacesComm[i].elemID1;
     unsigned long ii = counter[rankFace];
     counter[rankFace] += 9;
 
-    sendBufFace[ii]   = localFacesComm[i].nCornerPoints;
-    sendBufFace[ii+1] = localFacesComm[i].cornerPoints[0];
-    sendBufFace[ii+2] = localFacesComm[i].cornerPoints[1];
-    sendBufFace[ii+3] = localFacesComm[i].cornerPoints[2];
-    sendBufFace[ii+4] = localFacesComm[i].cornerPoints[3];
-    sendBufFace[ii+5] = localFacesComm[i].elemID0;
-    sendBufFace[ii+6] = localFacesComm[i].nPolySol0;
-    sendBufFace[ii+7] = localFacesComm[i].nDOFsElem0;
-    sendBufFace[ii+8] = localFacesComm[i].elemType0;
+    sendBufFace[ii] = localFacesComm[i].nCornerPoints;
+    sendBufFace[ii + 1] = localFacesComm[i].cornerPoints[0];
+    sendBufFace[ii + 2] = localFacesComm[i].cornerPoints[1];
+    sendBufFace[ii + 3] = localFacesComm[i].cornerPoints[2];
+    sendBufFace[ii + 4] = localFacesComm[i].cornerPoints[3];
+    sendBufFace[ii + 5] = localFacesComm[i].elemID0;
+    sendBufFace[ii + 6] = localFacesComm[i].nPolySol0;
+    sendBufFace[ii + 7] = localFacesComm[i].nDOFsElem0;
+    sendBufFace[ii + 8] = localFacesComm[i].elemType0;
   }
 
   /*--- Determine the number of ranks from which I receive a message. */
   unsigned long nMessSend = 0;
-  for(unsigned long i=0; i<(unsigned long)size; ++i) {
-    if( nFacesComm[i] ) {counter[i] = 1; ++nMessSend;}
-    else                 counter[i] = 0;
+  for (unsigned long i = 0; i < (unsigned long)size; ++i) {
+    if (nFacesComm[i]) {
+      counter[i] = 1;
+      ++nMessSend;
+    } else
+      counter[i] = 0;
   }
   vector<int> sizeRecv(size, 1);
 
   unsigned long nMessRecv;
-  SU2_MPI::Reduce_scatter(counter.data(), &nMessRecv, sizeRecv.data(),
-                          MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
+  SU2_MPI::Reduce_scatter(counter.data(), &nMessRecv, sizeRecv.data(), MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
 
   /*--- Send the data using nonblocking sends. ---*/
-  vector<SU2_MPI::Request> commReqs(max(nMessSend,nMessRecv));
+  vector<SU2_MPI::Request> commReqs(max(nMessSend, nMessRecv));
 
   nMessSend = 0;
   unsigned long indSend = 0;
-  for(unsigned long i=0; i<(unsigned long)size; ++i) {
-    if( nFacesComm[i] ) {
-      unsigned long count = 9*nFacesComm[i];
-      SU2_MPI::Isend(&sendBufFace[indSend], count, MPI_UNSIGNED_LONG, i, i,
-                     SU2_MPI::GetComm(), &commReqs[nMessSend]);
+  for (unsigned long i = 0; i < (unsigned long)size; ++i) {
+    if (nFacesComm[i]) {
+      unsigned long count = 9 * nFacesComm[i];
+      SU2_MPI::Isend(&sendBufFace[indSend], count, MPI_UNSIGNED_LONG, i, i, SU2_MPI::GetComm(), &commReqs[nMessSend]);
       ++nMessSend;
       indSend += count;
     }
@@ -2145,10 +2063,10 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
   /*--- Loop over the number of ranks from which faces are received.
         Receive the messages and store them in facesRecv.         ---*/
   vector<CFaceOfElement> facesRecv;
-  vector<unsigned long> nFacesRecv(nMessRecv+1);
-  vector<int>           rankRecv(nMessRecv);
+  vector<unsigned long> nFacesRecv(nMessRecv + 1);
+  vector<int> rankRecv(nMessRecv);
   nFacesRecv[0] = 0;
-  for(unsigned long i=0; i<nMessRecv; ++i) {
+  for (unsigned long i = 0; i < nMessRecv; ++i) {
     SU2_MPI::Status status;
     SU2_MPI::Probe(MPI_ANY_SOURCE, rank, SU2_MPI::GetComm(), &status);
     rankRecv[i] = status.MPI_SOURCE;
@@ -2156,22 +2074,21 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
     SU2_MPI::Get_count(&status, MPI_UNSIGNED_LONG, &sizeMess);
 
     vector<unsigned long> recvBuf(sizeMess);
-    SU2_MPI::Recv(recvBuf.data(), sizeMess, MPI_UNSIGNED_LONG,
-                  rankRecv[i], rank, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Recv(recvBuf.data(), sizeMess, MPI_UNSIGNED_LONG, rankRecv[i], rank, SU2_MPI::GetComm(), &status);
 
-    nFacesRecv[i+1] = nFacesRecv[i] + sizeMess/9;
-    facesRecv.resize(nFacesRecv[i+1]);
+    nFacesRecv[i + 1] = nFacesRecv[i] + sizeMess / 9;
+    facesRecv.resize(nFacesRecv[i + 1]);
     unsigned long ii = 0;
-    for(unsigned long j=nFacesRecv[i]; j<nFacesRecv[i+1]; ++j, ii+=9) {
-      facesRecv[j].nCornerPoints   = recvBuf[ii];
-      facesRecv[j].cornerPoints[0] = recvBuf[ii+1];
-      facesRecv[j].cornerPoints[1] = recvBuf[ii+2];
-      facesRecv[j].cornerPoints[2] = recvBuf[ii+3];
-      facesRecv[j].cornerPoints[3] = recvBuf[ii+4];
-      facesRecv[j].elemID0         = recvBuf[ii+5];
-      facesRecv[j].nPolySol0       = recvBuf[ii+6];
-      facesRecv[j].nDOFsElem0      = recvBuf[ii+7];
-      facesRecv[j].elemType0       = recvBuf[ii+8];
+    for (unsigned long j = nFacesRecv[i]; j < nFacesRecv[i + 1]; ++j, ii += 9) {
+      facesRecv[j].nCornerPoints = recvBuf[ii];
+      facesRecv[j].cornerPoints[0] = recvBuf[ii + 1];
+      facesRecv[j].cornerPoints[1] = recvBuf[ii + 2];
+      facesRecv[j].cornerPoints[2] = recvBuf[ii + 3];
+      facesRecv[j].cornerPoints[3] = recvBuf[ii + 4];
+      facesRecv[j].elemID0 = recvBuf[ii + 5];
+      facesRecv[j].nPolySol0 = recvBuf[ii + 6];
+      facesRecv[j].nDOFsElem0 = recvBuf[ii + 7];
+      facesRecv[j].elemType0 = recvBuf[ii + 8];
     }
   }
 
@@ -2183,12 +2100,12 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
   sort(localFacesComm.begin(), localFacesComm.end());
 
   nFacesLocComm = localFacesComm.size();
-  for(unsigned long i=1; i<localFacesComm.size(); ++i) {
-    if(localFacesComm[i] == localFacesComm[i-1]) {
-      localFacesComm[i-1].elemID1    = localFacesComm[i].elemID0;
-      localFacesComm[i-1].nPolySol1  = localFacesComm[i].nPolySol0;
-      localFacesComm[i-1].nDOFsElem1 = localFacesComm[i].nDOFsElem0;
-      localFacesComm[i-1].elemType1  = localFacesComm[i].elemType0;
+  for (unsigned long i = 1; i < localFacesComm.size(); ++i) {
+    if (localFacesComm[i] == localFacesComm[i - 1]) {
+      localFacesComm[i - 1].elemID1 = localFacesComm[i].elemID0;
+      localFacesComm[i - 1].nPolySol1 = localFacesComm[i].nPolySol0;
+      localFacesComm[i - 1].nDOFsElem1 = localFacesComm[i].nDOFsElem0;
+      localFacesComm[i - 1].elemType1 = localFacesComm[i].elemType0;
 
       localFacesComm[i].nCornerPoints = 4;
       localFacesComm[i].cornerPoints[0] = Global_nPoint;
@@ -2206,69 +2123,66 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
   SU2_MPI::Waitall(nMessSend, commReqs.data(), MPI_STATUSES_IGNORE);
 
   /*--- Send the data back to the requesting ranks. ---*/
-  sendBufFace.resize(9*nFacesRecv[nMessRecv]);
+  sendBufFace.resize(9 * nFacesRecv[nMessRecv]);
   indSend = 0;
-  for(unsigned long i=0; i<nMessRecv; ++i) {
+  for (unsigned long i = 0; i < nMessRecv; ++i) {
     unsigned long ii = indSend;
-    for(unsigned long j=nFacesRecv[i]; j<nFacesRecv[i+1]; ++j, ii+=9) {
-      sendBufFace[ii]   = facesRecv[j].nCornerPoints;
-      sendBufFace[ii+1] = facesRecv[j].cornerPoints[0];
-      sendBufFace[ii+2] = facesRecv[j].cornerPoints[1];
-      sendBufFace[ii+3] = facesRecv[j].cornerPoints[2];
-      sendBufFace[ii+4] = facesRecv[j].cornerPoints[3];
+    for (unsigned long j = nFacesRecv[i]; j < nFacesRecv[i + 1]; ++j, ii += 9) {
+      sendBufFace[ii] = facesRecv[j].nCornerPoints;
+      sendBufFace[ii + 1] = facesRecv[j].cornerPoints[0];
+      sendBufFace[ii + 2] = facesRecv[j].cornerPoints[1];
+      sendBufFace[ii + 3] = facesRecv[j].cornerPoints[2];
+      sendBufFace[ii + 4] = facesRecv[j].cornerPoints[3];
 
       vector<CFaceOfElement>::iterator low;
-      low = lower_bound(localFacesComm.begin(), localFacesComm.end(),
-                        facesRecv[j]);
-      if(facesRecv[j].elemID0 == low->elemID0) {
-        sendBufFace[ii+5] = low->elemID1;
-        sendBufFace[ii+6] = low->nPolySol1;
-        sendBufFace[ii+7] = low->nDOFsElem1;
-        sendBufFace[ii+8] = low->elemType1;
-      }
-      else {
-        sendBufFace[ii+5] = low->elemID0;
-        sendBufFace[ii+6] = low->nPolySol0;
-        sendBufFace[ii+7] = low->nDOFsElem0;
-        sendBufFace[ii+8] = low->elemType0;
+      low = lower_bound(localFacesComm.begin(), localFacesComm.end(), facesRecv[j]);
+      if (facesRecv[j].elemID0 == low->elemID0) {
+        sendBufFace[ii + 5] = low->elemID1;
+        sendBufFace[ii + 6] = low->nPolySol1;
+        sendBufFace[ii + 7] = low->nDOFsElem1;
+        sendBufFace[ii + 8] = low->elemType1;
+      } else {
+        sendBufFace[ii + 5] = low->elemID0;
+        sendBufFace[ii + 6] = low->nPolySol0;
+        sendBufFace[ii + 7] = low->nDOFsElem0;
+        sendBufFace[ii + 8] = low->elemType0;
       }
     }
 
     unsigned long count = ii - indSend;
-    SU2_MPI::Isend(&sendBufFace[indSend], count, MPI_UNSIGNED_LONG, rankRecv[i],
-                   rankRecv[i]+1, SU2_MPI::GetComm(), &commReqs[i]);
+    SU2_MPI::Isend(&sendBufFace[indSend], count, MPI_UNSIGNED_LONG, rankRecv[i], rankRecv[i] + 1, SU2_MPI::GetComm(),
+                   &commReqs[i]);
     indSend = ii;
   }
 
-
   /*--- Loop over the ranks to which I originally sent my face data.
         The return data contains information about the neighboring element. ---*/
-  for(unsigned long i=0; i<nMessSend; ++i) {
+  for (unsigned long i = 0; i < nMessSend; ++i) {
     SU2_MPI::Status status;
-    SU2_MPI::Probe(MPI_ANY_SOURCE, rank+1, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Probe(MPI_ANY_SOURCE, rank + 1, SU2_MPI::GetComm(), &status);
     int sizeMess;
     SU2_MPI::Get_count(&status, MPI_UNSIGNED_LONG, &sizeMess);
 
     vector<unsigned long> recvBuf(sizeMess);
-    SU2_MPI::Recv(recvBuf.data(), sizeMess, MPI_UNSIGNED_LONG,
-                  status.MPI_SOURCE, rank+1, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Recv(recvBuf.data(), sizeMess, MPI_UNSIGNED_LONG, status.MPI_SOURCE, rank + 1, SU2_MPI::GetComm(),
+                  &status);
 
     sizeMess /= 9;
     unsigned long jj = 0;
-    for(unsigned long j=0; j<(unsigned long) sizeMess; ++j, jj+=9) {
+    for (unsigned long j = 0; j < (unsigned long)sizeMess; ++j, jj += 9) {
       CFaceOfElement thisFace;
-      thisFace.nCornerPoints   = recvBuf[jj];
-      thisFace.cornerPoints[0] = recvBuf[jj+1];
-      thisFace.cornerPoints[1] = recvBuf[jj+2];
-      thisFace.cornerPoints[2] = recvBuf[jj+3];
-      thisFace.cornerPoints[3] = recvBuf[jj+4];
+      thisFace.nCornerPoints = recvBuf[jj];
+      thisFace.cornerPoints[0] = recvBuf[jj + 1];
+      thisFace.cornerPoints[1] = recvBuf[jj + 2];
+      thisFace.cornerPoints[2] = recvBuf[jj + 3];
+      thisFace.cornerPoints[3] = recvBuf[jj + 4];
 
       vector<CFaceOfElement>::iterator low;
       low = lower_bound(localFaces.begin(), localFaces.end(), thisFace);
-      low->elemID1    = recvBuf[jj+5];
-      low->nPolySol1  = recvBuf[jj+6];
-      low->nDOFsElem1 = recvBuf[jj+7];
-      low->elemType1  = recvBuf[jj+8];
+      low->elemID1 = recvBuf[jj + 5];
+      low->nPolySol1 = recvBuf[jj + 6];
+      low->nDOFsElem1 = recvBuf[jj + 7];
+      low->elemType1 = recvBuf[jj + 8];
     }
   }
 
@@ -2286,10 +2200,10 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
   DeterminePeriodicFacesFEMGrid(config, localFaces);
 
   /*--- Determine the total number of non-matching faces in the grid. ---*/
-  nFacesLoc   = localFaces.size();
+  nFacesLoc = localFaces.size();
   nFacesLocOr = nFacesLoc;
-  for(unsigned long i=0; i<nFacesLocOr; ++i) {
-    if(localFaces[i].elemID1 > Global_nElem) {
+  for (unsigned long i = 0; i < nFacesLocOr; ++i) {
+    if (localFaces[i].elemID1 > Global_nElem) {
       localFaces[i].nCornerPoints = 4;
       localFaces[i].cornerPoints[0] = Global_nPoint;
       localFaces[i].cornerPoints[1] = Global_nPoint;
@@ -2300,7 +2214,7 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
   }
 
   nFacesLocOr -= nFacesLoc;
-  if( nFacesLocOr ) {
+  if (nFacesLocOr) {
     sort(localFaces.begin(), localFaces.end());
     localFaces.resize(nFacesLoc);
   }
@@ -2308,10 +2222,9 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
   unsigned long nNonMatchingFaces = nFacesLocOr;
 
 #ifdef HAVE_MPI
-  SU2_MPI::Reduce(&nFacesLocOr, &nNonMatchingFaces, 1, MPI_UNSIGNED_LONG,
-                  MPI_SUM, MASTER_NODE, SU2_MPI::GetComm());
+  SU2_MPI::Reduce(&nFacesLocOr, &nNonMatchingFaces, 1, MPI_UNSIGNED_LONG, MPI_SUM, MASTER_NODE, SU2_MPI::GetComm());
 #endif
-  if(rank == MASTER_NODE && nNonMatchingFaces) {
+  if (rank == MASTER_NODE && nNonMatchingFaces) {
     cout << "There are " << nNonMatchingFaces << " non-matching faces in the grid. "
          << "These are ignored in the partitioning." << endl;
   }
@@ -2330,65 +2243,51 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
 
   /*--- Determine the ownership of the internal faces, i.e. which adjacent
         element is responsible for computing the fluxes through the face. ---*/
-  for(unsigned long i=0; i<nFacesLoc; ++i) {
-
+  for (unsigned long i = 0; i < nFacesLoc; ++i) {
     /* Check for a matching face. */
-    if(localFaces[i].elemID1 < Global_nElem) {
-
+    if (localFaces[i].elemID1 < Global_nElem) {
       /* Determine the time level for both elements. Elem0 is always owned, while
          elem1 is either owned or external. The data for external elements is
          stored in mapExternalElemIDToTimeLevel. */
-      unsigned long  elemID0    = localFaces[i].elemID0 - beg_node[rank];
+      unsigned long elemID0 = localFaces[i].elemID0 - beg_node[rank];
       unsigned short timeLevel0 = elem[elemID0]->GetTimeLevel();
 
       unsigned short timeLevel1;
-      if(localFaces[i].elemID1 >= beg_node[rank] &&
-         localFaces[i].elemID1 <  beg_node[rank]+nElem) {
-
+      if (localFaces[i].elemID1 >= beg_node[rank] && localFaces[i].elemID1 < beg_node[rank] + nElem) {
         unsigned long elemID1 = localFaces[i].elemID1 - beg_node[rank];
         timeLevel1 = elem[elemID1]->GetTimeLevel();
-      }
-      else {
-
-        map<unsigned long,CUnsignedShort2T>::const_iterator MI;
+      } else {
+        map<unsigned long, CUnsignedShort2T>::const_iterator MI;
         MI = mapExternalElemIDToTimeLevel.find(localFaces[i].elemID1);
-        if(MI == mapExternalElemIDToTimeLevel.end())
+        if (MI == mapExternalElemIDToTimeLevel.end())
           SU2_MPI::Error("Entry not found in mapExternalElemIDToTimeLevel", CURRENT_FUNCTION);
         timeLevel1 = MI->second.short0;
       }
 
       /* Check if both elements have the same time level. */
-      if(timeLevel0 == timeLevel1) {
-
+      if (timeLevel0 == timeLevel1) {
         /* Same time level, hence both elements can own the face. First check whether
            elemID0 == elemID1 (which happens for periodic problems with only one
            element in the periodic direction), because this is a special case. */
-        if(localFaces[i].elemID0 == localFaces[i].elemID1) {
-
+        if (localFaces[i].elemID0 == localFaces[i].elemID1) {
           /* This face occurs twice, but should be owned only once. Base this
              decision on the periodic index. */
           localFaces[i].elem0IsOwner = localFaces[i].periodicIndex < localFaces[i].periodicIndexDonor;
-        }
-        else {
-
+        } else {
           /* Different elements on both sides of the face. The ownership decision
              below makes an attempt to spread the workload evenly. */
           const unsigned long sumElemID = localFaces[i].elemID0 + localFaces[i].elemID1;
-          if( sumElemID%2 )
+          if (sumElemID % 2)
             localFaces[i].elem0IsOwner = localFaces[i].elemID0 < localFaces[i].elemID1;
           else
             localFaces[i].elem0IsOwner = localFaces[i].elemID0 > localFaces[i].elemID1;
         }
-      }
-      else {
-
+      } else {
         /* The time level of both elements differ. The element with the smallest
            time level must be the owner of the element. */
         localFaces[i].elem0IsOwner = timeLevel0 < timeLevel1;
       }
-    }
-    else {
-
+    } else {
       /* Non-matching face. Give the ownership to element 0. */
       localFaces[i].elem0IsOwner = true;
     }
@@ -2397,21 +2296,20 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
   /*--- All the matching face information is known now, including periodic
         faces. Store the information of the neighbors in the data structure
         for the local elements.     ---*/
-  for(unsigned long k=0; k<nElem; ++k) {
+  for (unsigned long k = 0; k < nElem; ++k) {
     unsigned short nFaces;
     unsigned short nPointsPerFace[6];
-    unsigned long  faceConn[6][4];
+    unsigned long faceConn[6][4];
 
     elem[k]->GetCornerPointsAllFaces(nFaces, nPointsPerFace, faceConn);
     elem[k]->InitializeNeighbors(nFaces);
 
-    for(unsigned short i=0; i<nFaces; ++i) {
+    for (unsigned short i = 0; i < nFaces; ++i) {
       CFaceOfElement thisFace;
       thisFace.nCornerPoints = nPointsPerFace[i];
-      for(unsigned short j=0; j<nPointsPerFace[i]; ++j)
-        thisFace.cornerPoints[j] = faceConn[i][j];
-      thisFace.elemID0    = beg_node[rank] + k;
-      thisFace.nPolySol0  = elem[k]->GetNPolySol();
+      for (unsigned short j = 0; j < nPointsPerFace[i]; ++j) thisFace.cornerPoints[j] = faceConn[i][j];
+      thisFace.elemID0 = beg_node[rank] + k;
+      thisFace.nPolySol0 = elem[k]->GetNPolySol();
       thisFace.nDOFsElem0 = elem[k]->GetNDOFsSol();
 
       thisFace.CreateUniqueNumbering();
@@ -2419,19 +2317,17 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
       vector<CFaceOfElement>::iterator low;
       low = lower_bound(localFaces.begin(), localFaces.end(), thisFace);
 
-      if(low != localFaces.end() ) {
-        if( !(thisFace < *low) ) {
-          if(low->elemID0 == thisFace.elemID0) {
+      if (low != localFaces.end()) {
+        if (!(thisFace < *low)) {
+          if (low->elemID0 == thisFace.elemID0) {
             elem[k]->SetNeighbor_Elements(low->elemID1, i);
             elem[k]->SetOwnerFace(low->elem0IsOwner, i);
-          }
-          else {
+          } else {
             elem[k]->SetNeighbor_Elements(low->elemID0, i);
             elem[k]->SetOwnerFace(!(low->elem0IsOwner), i);
           }
 
-          if(low->periodicIndex > 0)
-            elem[k]->SetPeriodicIndex(low->periodicIndex-1, i);
+          if (low->periodicIndex > 0) elem[k]->SetPeriodicIndex(low->periodicIndex - 1, i);
         }
       }
     }
@@ -2440,21 +2336,20 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
   /*--- Create the vector of vectors that describe the connectivity
         of the graph. First the faces. ---*/
   vector<vector<unsigned long> > adjacency(nElem, vector<unsigned long>(0));
-  for(unsigned long i=0; i<nFacesLoc; ++i) {
+  for (unsigned long i = 0; i < nFacesLoc; ++i) {
     long ii = localFaces[i].elemID0 - beg_node[rank];
     adjacency[ii].push_back(localFaces[i].elemID1);
 
-    if(localFaces[i].periodicIndex == 0) {
+    if (localFaces[i].periodicIndex == 0) {
       ii = localFaces[i].elemID1 - beg_node[rank];
-      if(ii >= 0 && ii < (long) nElem)
-        adjacency[ii].push_back(localFaces[i].elemID0);
+      if (ii >= 0 && ii < (long)nElem) adjacency[ii].push_back(localFaces[i].elemID0);
     }
   }
 
   /* It is possible that some neighbors appear multiple times due to e.g.
      periodic boundary conditions. ParMETIS is not able to deal with this
      situation, hence these multiple entries must be removed. */
-  for(unsigned long i=0; i<nElem; ++i) {
+  for (unsigned long i = 0; i < nElem; ++i) {
     sort(adjacency[i].begin(), adjacency[i].end());
     vector<unsigned long>::iterator lastEntry;
     lastEntry = unique(adjacency[i].begin(), adjacency[i].end());
@@ -2464,12 +2359,12 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
   /* Due to periodic boundary conditions it is also possible that self entries
      are present. ParMETIS is not able to deal with self entries, hence
      they must be removed as well. */
-  for(unsigned long i=0; i<nElem; ++i) {
+  for (unsigned long i = 0; i < nElem; ++i) {
     const unsigned long globalElemID = i + beg_node[rank];
     unsigned long nEntriesNew = adjacency[i].size();
 
-    for(unsigned long j=0; j<adjacency[i].size(); ++j) {
-      if(adjacency[i][j] == globalElemID) {
+    for (unsigned long j = 0; j < adjacency[i].size(); ++j) {
+      if (adjacency[i][j] == globalElemID) {
         adjacency[i][j] = ULONG_MAX;
         --nEntriesNew;
       }
@@ -2484,43 +2379,35 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
         and communicated later. ---*/
   vector<unsigned long> additionalExternalEntriesGraph;
 
-  for(unsigned short iMarker=0; iMarker<nMarker; ++iMarker) {
-    for(unsigned long l=0; l<nElem_Bound[iMarker]; ++l) {
-
+  for (unsigned short iMarker = 0; iMarker < nMarker; ++iMarker) {
+    for (unsigned long l = 0; l < nElem_Bound[iMarker]; ++l) {
       /* Get the global and local element ID adjacent to this boundary face. */
       const unsigned long globalElemID = bound[iMarker][l]->GetDomainElement();
-      const unsigned long elemID       = globalElemID - beg_node[rank];
+      const unsigned long elemID = globalElemID - beg_node[rank];
 
       /* Get the number of donor elements for the wall function treatment
          and the pointer to the array which stores this info. */
       const unsigned short nDonors = bound[iMarker][l]->GetNDonorsWallFunctions();
-      const unsigned long  *donors = bound[iMarker][l]->GetDonorsWallFunctions();
+      const unsigned long* donors = bound[iMarker][l]->GetDonorsWallFunctions();
 
       /* Loop over the number of donors and add the entry in the graph,
          if not already present. */
-      for(unsigned short i=0; i<nDonors; ++i) {
-
-        if(donors[i] != globalElemID) {
-          if( !binary_search(adjacency[elemID].begin(), adjacency[elemID].end(),
-                             donors[i]) ) {
-
+      for (unsigned short i = 0; i < nDonors; ++i) {
+        if (donors[i] != globalElemID) {
+          if (!binary_search(adjacency[elemID].begin(), adjacency[elemID].end(), donors[i])) {
             /* Donor not present in the graph for elemID. Add it and sort it
                afterwards, such that a binary search can be applied later. */
             adjacency[elemID].push_back(donors[i]);
             sort(adjacency[elemID].begin(), adjacency[elemID].end());
 
             /* Check if the donor element is stored locally. */
-            if(donors[i] >= beg_node[rank] &&
-               donors[i] <  beg_node[rank]+nElem) {
-
+            if (donors[i] >= beg_node[rank] && donors[i] < beg_node[rank] + nElem) {
               /* Donor is stored locally. Add the entry to the graph
                  and sort it afterwards. */
               const unsigned long localDonorID = donors[i] - beg_node[rank];
               adjacency[localDonorID].push_back(globalElemID);
               sort(adjacency[localDonorID].begin(), adjacency[localDonorID].end());
-            }
-            else {
-
+            } else {
               /* Donor is stored externally. Store the graph entry in
                  additionalExternalEntriesGraph. */
               additionalExternalEntriesGraph.push_back(donors[i]);
@@ -2538,50 +2425,47 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
   vector<vector<unsigned long> > sendBufsGraphData(size, vector<unsigned long>(0));
   vector<int> sendToRank(size, 0);
 
-  for(unsigned long i=0; i<additionalExternalEntriesGraph.size(); i+=2) {
-
+  for (unsigned long i = 0; i < additionalExternalEntriesGraph.size(); i += 2) {
     /* Determine the rank where this external is stored. */
     const unsigned long elemID = additionalExternalEntriesGraph[i];
     int rankElem;
-    if(elemID >= beg_node[size-1]) rankElem = size-1;
+    if (elemID >= beg_node[size - 1])
+      rankElem = size - 1;
     else {
-      const unsigned long *low;
-      low = lower_bound(beg_node, beg_node+size, elemID);
+      const unsigned long* low;
+      low = lower_bound(beg_node, beg_node + size, elemID);
 
       rankElem = low - beg_node;
-      if(*low > elemID) --rankElem;
+      if (*low > elemID) --rankElem;
     }
 
     sendBufsGraphData[rankElem].push_back(additionalExternalEntriesGraph[i]);
-    sendBufsGraphData[rankElem].push_back(additionalExternalEntriesGraph[i+1]);
+    sendBufsGraphData[rankElem].push_back(additionalExternalEntriesGraph[i + 1]);
     sendToRank[rankElem] = 1;
   }
 
   /*-- Determine to how many ranks this rank will send data and from how
        many ranks it will receive data. ---*/
   int nRankSend = 0;
-  for(int i=0; i<size; ++i) {
-    if( sendToRank[i] ) ++nRankSend;
+  for (int i = 0; i < size; ++i) {
+    if (sendToRank[i]) ++nRankSend;
   }
 
   int nRankRecv;
   vector<int> sizeSend(size, 1);
-  SU2_MPI::Reduce_scatter(sendToRank.data(), &nRankRecv, sizeSend.data(),
-                          MPI_INT, MPI_SUM, SU2_MPI::GetComm());
+  SU2_MPI::Reduce_scatter(sendToRank.data(), &nRankRecv, sizeSend.data(), MPI_INT, MPI_SUM, SU2_MPI::GetComm());
 
   /* Send the data using non-blocking sends. */
   vector<SU2_MPI::Request> sendReqs(nRankSend);
   nRankSend = 0;
-  for(int i=0; i<size; ++i) {
-    if( sendToRank[i] )
-      SU2_MPI::Isend(sendBufsGraphData[i].data(), sendBufsGraphData[i].size(),
-                     MPI_UNSIGNED_LONG, i, i, SU2_MPI::GetComm(),
-                     &sendReqs[nRankSend++]);
+  for (int i = 0; i < size; ++i) {
+    if (sendToRank[i])
+      SU2_MPI::Isend(sendBufsGraphData[i].data(), sendBufsGraphData[i].size(), MPI_UNSIGNED_LONG, i, i,
+                     SU2_MPI::GetComm(), &sendReqs[nRankSend++]);
   }
 
   /* Loop over the number of ranks from which this rank receives data. */
-  for(int i=0; i<nRankRecv; ++i) {
-
+  for (int i = 0; i < nRankRecv; ++i) {
     /* Block until a message with unsigned longs arrives from any processor.
        Determine the source and the size of the message.   */
     SU2_MPI::Status status;
@@ -2594,14 +2478,13 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
     /* Allocate the memory for the receive buffer and receive the message
        using a blocking receive. */
     vector<unsigned long> recvBuf(sizeMess);
-    SU2_MPI::Recv(recvBuf.data(), sizeMess, MPI_UNSIGNED_LONG,
-                   source, rank, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Recv(recvBuf.data(), sizeMess, MPI_UNSIGNED_LONG, source, rank, SU2_MPI::GetComm(), &status);
 
     /* Loop over the contents of the receive buffer and update the
        graph accordingly. */
-    for(int j=0; j<sizeMess; j+=2) {
+    for (int j = 0; j < sizeMess; j += 2) {
       const unsigned long elemID = recvBuf[j] - beg_node[rank];
-      adjacency[elemID].push_back(recvBuf[j+1]);
+      adjacency[elemID].push_back(recvBuf[j + 1]);
       sort(adjacency[elemID].begin(), adjacency[elemID].end());
     }
   }
@@ -2614,15 +2497,13 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
 #endif
 
   /* Allocate the memory to store the weights of the graph. */
-  vector<su2double> vwgt(2*nElem);
+  vector<su2double> vwgt(2 * nElem);
   vector<vector<su2double> > adjwgt(nElem, vector<su2double>(0));
 
-  for(unsigned long i=0; i<nElem; ++i)
-    adjwgt[i].resize(adjacency[i].size());
+  for (unsigned long i = 0; i < nElem; ++i) adjwgt[i].resize(adjacency[i].size());
 
   /* Compute the weigts of the graph. */
-  ComputeFEMGraphWeights(config, localFaces, adjacency,
-                         mapExternalElemIDToTimeLevel, vwgt, adjwgt);
+  ComputeFEMGraphWeights(config, localFaces, adjacency, mapExternalElemIDToTimeLevel, vwgt, adjwgt);
 
   /*--- The remainder of this function should only be called if we have parallel
         support with MPI and have the ParMETIS library compiled and linked. ---*/
@@ -2631,55 +2512,49 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
 #ifdef HAVE_PARMETIS
 
   /*--- Only call ParMETIS if we have more than one rank to avoid errors ---*/
-  if(size > SINGLE_NODE)
-  {
+  if (size > SINGLE_NODE) {
     /*--- The scalar variables and the options array for the call to ParMETIS. ---*/
-    idx_t  wgtflag = 3;               // Weights on both the vertices and edges.
-    idx_t  numflag = 0;               // C-numbering.
-    idx_t  ncon    = 2;               // Number of constraints.
-    real_t ubvec[] = {1.05, 1.05};    // Tolerances for the vertex weights, recommended value is 1.05.
-    idx_t  nparts  = (idx_t)size;     // Number of subdomains. Must be number of MPI ranks.
-    idx_t  options[METIS_NOPTIONS];   // Just use the default options.
+    idx_t wgtflag = 3;              // Weights on both the vertices and edges.
+    idx_t numflag = 0;              // C-numbering.
+    idx_t ncon = 2;                 // Number of constraints.
+    real_t ubvec[] = {1.05, 1.05};  // Tolerances for the vertex weights, recommended value is 1.05.
+    idx_t nparts = (idx_t)size;     // Number of subdomains. Must be number of MPI ranks.
+    idx_t options[METIS_NOPTIONS];  // Just use the default options.
     METIS_SetDefaultOptions(options);
     options[1] = 0;
 
     /*--- Determine the array, which stores the distribution of the graph nodes
           over the ranks.     ---*/
-    vector<idx_t> vtxdist(size+1);
+    vector<idx_t> vtxdist(size + 1);
     vtxdist[0] = 0;
-    for(int i=0; i<size; ++i)
-      vtxdist[i+1] = (idx_t)end_node[i];
+    for (int i = 0; i < size; ++i) vtxdist[i + 1] = (idx_t)end_node[i];
 
     /* Create the array xadjPar, which contains the number of edges for each
        vertex of the graph in ParMETIS format. */
-    vector<idx_t> xadjPar(nElem+1);
+    vector<idx_t> xadjPar(nElem + 1);
     xadjPar[0] = 0;
-    for(unsigned long i=0; i<nElem; ++i)
-      xadjPar[i+1] = xadjPar[i] + (idx_t)adjacency[i].size();
+    for (unsigned long i = 0; i < nElem; ++i) xadjPar[i + 1] = xadjPar[i] + (idx_t)adjacency[i].size();
 
     /* Create the adjacency information in ParMETIS format. */
     vector<idx_t> adjacencyPar(xadjPar[nElem]);
     unsigned long ii = 0;
-    for(unsigned long i=0; i<nElem; ++i) {
-      for(unsigned long j=0; j<adjacency[i].size(); ++j, ++ii)
-        adjacencyPar[ii] = adjacency[i][j];
+    for (unsigned long i = 0; i < nElem; ++i) {
+      for (unsigned long j = 0; j < adjacency[i].size(); ++j, ++ii) adjacencyPar[ii] = adjacency[i][j];
     }
 
     /* Create the vertex weights in ParMETIS format. */
-    vector<idx_t> vwgtPar(nElem*ncon);
-    for(unsigned long i=0; i<nElem*ncon; ++i)
-      vwgtPar[i] = (idx_t) ceil(vwgt[i]);
+    vector<idx_t> vwgtPar(nElem * ncon);
+    for (unsigned long i = 0; i < nElem * ncon; ++i) vwgtPar[i] = (idx_t)ceil(vwgt[i]);
 
     /* Create the adjacency weight in ParMETIS format. */
     vector<idx_t> adjwgtPar(xadjPar[nElem]);
     ii = 0;
-    for(unsigned long i=0; i<nElem; ++i) {
-      for(unsigned long j=0; j<adjwgt[i].size(); ++j, ++ii)
-        adjwgtPar[ii] = (idx_t) ceil(adjwgt[i][j]);
+    for (unsigned long i = 0; i < nElem; ++i) {
+      for (unsigned long j = 0; j < adjwgt[i].size(); ++j, ++ii) adjwgtPar[ii] = (idx_t)ceil(adjwgt[i][j]);
     }
 
     /* Make sure that an equal distribution is obtained. */
-    vector<real_t> tpwgts(size*ncon, 1.0/((real_t)size));
+    vector<real_t> tpwgts(size * ncon, 1.0 / ((real_t)size));
 
     /*--- Calling ParMETIS ---*/
     vector<idx_t> part(nElem);
@@ -2687,24 +2562,21 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
 
     idx_t edgecut;
     MPI_Comm comm = SU2_MPI::GetComm();
-    ParMETIS_V3_PartKway(vtxdist.data(), xadjPar.data(), adjacencyPar.data(),
-                         vwgtPar.data(), adjwgtPar.data(), &wgtflag, &numflag,
-                         &ncon, &nparts, tpwgts.data(), ubvec, options,
-                         &edgecut, part.data(), &comm);
+    ParMETIS_V3_PartKway(vtxdist.data(), xadjPar.data(), adjacencyPar.data(), vwgtPar.data(), adjwgtPar.data(),
+                         &wgtflag, &numflag, &ncon, &nparts, tpwgts.data(), ubvec, options, &edgecut, part.data(),
+                         &comm);
     if (rank == MASTER_NODE) {
       cout << " graph partitioning complete (";
       cout << edgecut << " edge cuts)." << endl;
     }
 
     /*--- Set the color of the elements to the outcome of ParMETIS. ---*/
-    for(unsigned long i=0; i<nElem; ++i)
-      elem[i]->SetColor(part[i]);
+    for (unsigned long i = 0; i < nElem; ++i) elem[i]->SetColor(part[i]);
   }
 
-#else   /* HAVE_PARMETIS */
+#else /* HAVE_PARMETIS */
 
-  if(size > SINGLE_NODE)
-  {
+  if (size > SINGLE_NODE) {
     if (rank == MASTER_NODE) {
       cout << endl;
       cout << "--------------------- WARNING -------------------------------" << endl;
@@ -2715,46 +2587,40 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig *config) {
     }
 
     /* Set the color to the current rank. */
-    for(unsigned long i=0; i<nElem; ++i)
-      elem[i]->SetColor(rank);
+    for (unsigned long i = 0; i < nElem; ++i) elem[i]->SetColor(rank);
   }
 
-#endif  /* HAVE_PARMETIS */
+#endif /* HAVE_PARMETIS */
 
-#endif  /* HAVE_MPI */
+#endif /* HAVE_MPI */
 }
 
-void CPhysicalGeometry::DeterminePeriodicFacesFEMGrid(CConfig                *config,
-                                                      vector<CFaceOfElement> &localFaces) {
-
+void CPhysicalGeometry::DeterminePeriodicFacesFEMGrid(CConfig* config, vector<CFaceOfElement>& localFaces) {
   /*--- Determine a mapping from the global point ID to the local index
         of the points.            ---*/
-  map<unsigned long,unsigned long> globalPointIDToLocalInd;
-  for(unsigned i=0; i<nPoint; ++i) {
+  map<unsigned long, unsigned long> globalPointIDToLocalInd;
+  for (unsigned i = 0; i < nPoint; ++i) {
     globalPointIDToLocalInd[nodes->GetGlobalIndex(i)] = i;
   }
 
   /*--- Loop over the number of markers present in the grid and check for a periodic one. ---*/
-  for(unsigned short iMarker=0; iMarker<config->GetnMarker_All(); ++iMarker) {
-    if(config->GetMarker_All_KindBC(iMarker) == PERIODIC_BOUNDARY) {
-
+  for (unsigned short iMarker = 0; iMarker < config->GetnMarker_All(); ++iMarker) {
+    if (config->GetMarker_All_KindBC(iMarker) == PERIODIC_BOUNDARY) {
       /*--- Determine the donor marker and the transformation from the
             current marker to the donor marker.    ---*/
       unsigned short jMarker = config->GetMarker_Periodic_Donor(config->GetMarker_All_TagBound(iMarker));
 
       auto center = config->GetPeriodicRotCenter(config->GetMarker_All_TagBound(iMarker));
       auto angles = config->GetPeriodicRotAngles(config->GetMarker_All_TagBound(iMarker));
-      auto trans  = config->GetPeriodicTranslation(config->GetMarker_All_TagBound(iMarker));
+      auto trans = config->GetPeriodicTranslation(config->GetMarker_All_TagBound(iMarker));
 
       /*--- Store (center+trans) as it is constant and will be added on. ---*/
-      su2double translation[] = {center[0] + trans[0],
-                                 center[1] + trans[1],
-                                 center[2] + trans[2]};
+      su2double translation[] = {center[0] + trans[0], center[1] + trans[1], center[2] + trans[2]};
 
       /*--- Store angles separately for clarity. Compute sines/cosines. ---*/
       su2double theta = angles[0];
-      su2double phi   = angles[1];
-      su2double psi   = angles[2];
+      su2double phi = angles[1];
+      su2double psi = angles[2];
 
       su2double cosTheta = cos(theta), cosPhi = cos(phi), cosPsi = cos(psi);
       su2double sinTheta = sin(theta), sinPhi = sin(phi), sinPsi = sin(psi);
@@ -2762,17 +2628,17 @@ void CPhysicalGeometry::DeterminePeriodicFacesFEMGrid(CConfig                *co
       /*--- Compute the rotation matrix. Note that the implicit
             ordering is rotation about the x-axis, y-axis, then z-axis. ---*/
       su2double rotMatrix[3][3];
-      rotMatrix[0][0] =  cosPhi*cosPsi;
-      rotMatrix[1][0] =  cosPhi*sinPsi;
+      rotMatrix[0][0] = cosPhi * cosPsi;
+      rotMatrix[1][0] = cosPhi * sinPsi;
       rotMatrix[2][0] = -sinPhi;
 
-      rotMatrix[0][1] = sinTheta*sinPhi*cosPsi - cosTheta*sinPsi;
-      rotMatrix[1][1] = sinTheta*sinPhi*sinPsi + cosTheta*cosPsi;
-      rotMatrix[2][1] = sinTheta*cosPhi;
+      rotMatrix[0][1] = sinTheta * sinPhi * cosPsi - cosTheta * sinPsi;
+      rotMatrix[1][1] = sinTheta * sinPhi * sinPsi + cosTheta * cosPsi;
+      rotMatrix[2][1] = sinTheta * cosPhi;
 
-      rotMatrix[0][2] = cosTheta*sinPhi*cosPsi + sinTheta*sinPsi;
-      rotMatrix[1][2] = cosTheta*sinPhi*sinPsi - sinTheta*cosPsi;
-      rotMatrix[2][2] = cosTheta*cosPhi;
+      rotMatrix[0][2] = cosTheta * sinPhi * cosPsi + sinTheta * sinPsi;
+      rotMatrix[1][2] = cosTheta * sinPhi * sinPsi - sinTheta * cosPsi;
+      rotMatrix[2][2] = cosTheta * cosPhi;
 
       /*--- Define the vector to store the faces of the donor. Initialize its
             size to the number of local donor faces.    ---*/
@@ -2784,41 +2650,38 @@ void CPhysicalGeometry::DeterminePeriodicFacesFEMGrid(CConfig                *co
       /*------------------------------------------------------------------*/
 
       /*--- Loop over the local elements of the donor marker. ---*/
-      for(unsigned long k=0; k<nElem_Bound[jMarker]; ++k) {
-
+      for (unsigned long k = 0; k < nElem_Bound[jMarker]; ++k) {
         /*--- Get the connectivity of this face. The reason for the used
               function arguments for GetCornerPointsAllFaces, is that
               GetCornerPointsAllFaces is an overloaded function.   ---*/
         unsigned short nFaces;
         unsigned short nPointsPerFace[6];
-        unsigned long  faceConn[6][4];
+        unsigned long faceConn[6][4];
         bound[jMarker][k]->GetCornerPointsAllFaces(nFaces, nPointsPerFace, faceConn);
 
         /*--- Search for this face in localFaces. It must be present. ---*/
         CFaceOfElement thisFace;
         thisFace.nCornerPoints = nPointsPerFace[0];
-        for(unsigned short j=0; j<nPointsPerFace[0]; ++j)
-          thisFace.cornerPoints[j] = faceConn[0][j];
+        for (unsigned short j = 0; j < nPointsPerFace[0]; ++j) thisFace.cornerPoints[j] = faceConn[0][j];
         thisFace.CreateUniqueNumbering();
 
         vector<CFaceOfElement>::iterator low;
         low = lower_bound(localFaces.begin(), localFaces.end(), thisFace);
 
         /*--- Store the relevant data in facesDonor. ---*/
-        facesDonor[k].nDim          = nDim;
+        facesDonor[k].nDim = nDim;
         facesDonor[k].nCornerPoints = nPointsPerFace[0];
-        facesDonor[k].elemID        = low->elemID0;
-        facesDonor[k].nPoly         = low->nPolySol0;
-        facesDonor[k].nDOFsElem     = low->nDOFsElem0;
-        facesDonor[k].elemType      = low->elemType0;
+        facesDonor[k].elemID = low->elemID0;
+        facesDonor[k].nPoly = low->nPolySol0;
+        facesDonor[k].nDOFsElem = low->nDOFsElem0;
+        facesDonor[k].elemType = low->elemType0;
 
-        for(unsigned short j=0; j<nPointsPerFace[0]; ++j) {
-          map<unsigned long,unsigned long>::const_iterator MI;
+        for (unsigned short j = 0; j < nPointsPerFace[0]; ++j) {
+          map<unsigned long, unsigned long>::const_iterator MI;
           MI = globalPointIDToLocalInd.find(faceConn[0][j]);
           unsigned long ind = MI->second;
 
-          for(unsigned l=0; l<nDim; ++l)
-            facesDonor[k].cornerCoor[j][l] = nodes->GetCoord(ind, l);
+          for (unsigned l = 0; l < nDim; ++l) facesDonor[k].cornerCoor[j][l] = nodes->GetCoord(ind, l);
         }
 
         /*--- Create the tolerance for this face and sort the coordinates. ---*/
@@ -2833,21 +2696,19 @@ void CPhysicalGeometry::DeterminePeriodicFacesFEMGrid(CConfig                *co
 #ifdef HAVE_MPI
 
       /*--- Check if this is indeed a parallel simulation. ---*/
-      if(size > 1) {
-
+      if (size > 1) {
         /*--- Allocate the memory for the size arrays in Allgatherv. ---*/
         vector<int> recvCounts(size), displs(size);
 
         /*--- Create the values of recvCounts for the gather of the facesDonor. ---*/
         int sizeLocal = facesDonor.size();
 
-        SU2_MPI::Allgather(&sizeLocal, 1, MPI_INT, recvCounts.data(), 1,
-                           MPI_INT, SU2_MPI::GetComm());
+        SU2_MPI::Allgather(&sizeLocal, 1, MPI_INT, recvCounts.data(), 1, MPI_INT, SU2_MPI::GetComm());
 
         /*--- Create the data for the vector displs from the known values of
               recvCounts. Also determine the total size of the data.   ---*/
         displs[0] = 0;
-        for(int i=1; i<size; ++i) displs[i] = displs[i-1] + recvCounts[i-1];
+        for (int i = 1; i < size; ++i) displs[i] = displs[i - 1] + recvCounts[i - 1];
 
         int sizeGlobal = displs.back() + recvCounts.back();
 
@@ -2855,13 +2716,12 @@ void CPhysicalGeometry::DeterminePeriodicFacesFEMGrid(CConfig                *co
               at least not at the moment when this was coded. Therefore the data
               from facesDonor is copied into buffers of primitive types, which
               are communicated. ---*/
-        vector<unsigned short> shortLocBuf(5*sizeLocal);
-        vector<unsigned long>  longLocBuf(sizeLocal);
-        vector<su2double>      doubleLocBuf(13*sizeLocal);
+        vector<unsigned short> shortLocBuf(5 * sizeLocal);
+        vector<unsigned long> longLocBuf(sizeLocal);
+        vector<su2double> doubleLocBuf(13 * sizeLocal);
 
-        unsigned long cS=0, cL=0, cD=0;
-        for(vector<CMatchingFace>::const_iterator fIt =facesDonor.begin();
-                                                  fIt!=facesDonor.end(); ++fIt) {
+        unsigned long cS = 0, cL = 0, cD = 0;
+        for (vector<CMatchingFace>::const_iterator fIt = facesDonor.begin(); fIt != facesDonor.end(); ++fIt) {
           shortLocBuf[cS++] = fIt->nCornerPoints;
           shortLocBuf[cS++] = fIt->nDim;
           shortLocBuf[cS++] = fIt->nPoly;
@@ -2891,43 +2751,42 @@ void CPhysicalGeometry::DeterminePeriodicFacesFEMGrid(CConfig                *co
 
         /*--- Gather the faces from all ranks to all ranks. Use Allgatherv
               for this purpose.                  ---*/
-        vector<unsigned short> shortGlobBuf(5*sizeGlobal);
-        vector<unsigned long>  longGlobBuf(sizeGlobal);
-        vector<su2double>      doubleGlobBuf(13*sizeGlobal);
+        vector<unsigned short> shortGlobBuf(5 * sizeGlobal);
+        vector<unsigned long> longGlobBuf(sizeGlobal);
+        vector<su2double> doubleGlobBuf(13 * sizeGlobal);
 
-        SU2_MPI::Allgatherv(longLocBuf.data(), longLocBuf.size(), MPI_UNSIGNED_LONG,
-                            longGlobBuf.data(), recvCounts.data(), displs.data(),
-                            MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
+        SU2_MPI::Allgatherv(longLocBuf.data(), longLocBuf.size(), MPI_UNSIGNED_LONG, longGlobBuf.data(),
+                            recvCounts.data(), displs.data(), MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
 
-        for(int i=0; i<size; ++i) {
-          recvCounts[i] *= 5; displs[i] *= 5;
+        for (int i = 0; i < size; ++i) {
+          recvCounts[i] *= 5;
+          displs[i] *= 5;
         }
 
-        SU2_MPI::Allgatherv(shortLocBuf.data(), shortLocBuf.size(), MPI_UNSIGNED_SHORT,
-                            shortGlobBuf.data(), recvCounts.data(), displs.data(),
-                            MPI_UNSIGNED_SHORT, SU2_MPI::GetComm());
+        SU2_MPI::Allgatherv(shortLocBuf.data(), shortLocBuf.size(), MPI_UNSIGNED_SHORT, shortGlobBuf.data(),
+                            recvCounts.data(), displs.data(), MPI_UNSIGNED_SHORT, SU2_MPI::GetComm());
 
-        for(int i=0; i<size; ++i) {
-          recvCounts[i] /=  5; displs[i] /=  5;
-          recvCounts[i] *= 13; displs[i] *= 13;
+        for (int i = 0; i < size; ++i) {
+          recvCounts[i] /= 5;
+          displs[i] /= 5;
+          recvCounts[i] *= 13;
+          displs[i] *= 13;
         }
 
-        SU2_MPI::Allgatherv(doubleLocBuf.data(), doubleLocBuf.size(), MPI_DOUBLE,
-                            doubleGlobBuf.data(), recvCounts.data(), displs.data(),
-                            MPI_DOUBLE, SU2_MPI::GetComm());
+        SU2_MPI::Allgatherv(doubleLocBuf.data(), doubleLocBuf.size(), MPI_DOUBLE, doubleGlobBuf.data(),
+                            recvCounts.data(), displs.data(), MPI_DOUBLE, SU2_MPI::GetComm());
 
         /*--- Copy the data back into facesDonor, which will contain the
               global information after the copies. ---*/
         facesDonor.resize(sizeGlobal);
         cS = cL = cD = 0;
 
-        for(vector<CMatchingFace>::iterator fIt =facesDonor.begin();
-                                            fIt!=facesDonor.end(); ++fIt) {
+        for (vector<CMatchingFace>::iterator fIt = facesDonor.begin(); fIt != facesDonor.end(); ++fIt) {
           fIt->nCornerPoints = shortGlobBuf[cS++];
-          fIt->nDim          = shortGlobBuf[cS++];
-          fIt->nPoly         = shortGlobBuf[cS++];
-          fIt->nDOFsElem     = shortGlobBuf[cS++];
-          fIt->elemType      = shortGlobBuf[cS++];
+          fIt->nDim = shortGlobBuf[cS++];
+          fIt->nPoly = shortGlobBuf[cS++];
+          fIt->nDOFsElem = shortGlobBuf[cS++];
+          fIt->elemType = shortGlobBuf[cS++];
 
           fIt->elemID = longGlobBuf[cL++];
 
@@ -2961,21 +2820,19 @@ void CPhysicalGeometry::DeterminePeriodicFacesFEMGrid(CConfig                *co
       /*------------------------------------------------------------------*/
 
       /*--- Loop over the local faces of this boundary marker. ---*/
-      for(unsigned long k=0; k<nElem_Bound[iMarker]; ++k) {
-
+      for (unsigned long k = 0; k < nElem_Bound[iMarker]; ++k) {
         /*--- Get the connectivity of this face. The reason for the used
               function arguments for GetCornerPointsAllFaces, is that
               GetCornerPointsAllFaces is an overloaded function.   ---*/
         unsigned short nFaces;
         unsigned short nPointsPerFace[6];
-        unsigned long  faceConn[6][4];
+        unsigned long faceConn[6][4];
         bound[iMarker][k]->GetCornerPointsAllFaces(nFaces, nPointsPerFace, faceConn);
 
         /*--- Search for this face in localFaces. It must be present. ---*/
         CFaceOfElement thisFace;
         thisFace.nCornerPoints = nPointsPerFace[0];
-        for(unsigned short j=0; j<nPointsPerFace[0]; ++j)
-          thisFace.cornerPoints[j] = faceConn[0][j];
+        for (unsigned short j = 0; j < nPointsPerFace[0]; ++j) thisFace.cornerPoints[j] = faceConn[0][j];
         thisFace.CreateUniqueNumbering();
 
         vector<CFaceOfElement>::iterator low;
@@ -2989,29 +2846,29 @@ void CPhysicalGeometry::DeterminePeriodicFacesFEMGrid(CConfig                *co
               such that a search can be carried out in donorFaces. Note that the
               periodic transformation must be applied to the coordinates. ---*/
         CMatchingFace thisMatchingFace;
-        thisMatchingFace.nDim          = nDim;
+        thisMatchingFace.nDim = nDim;
         thisMatchingFace.nCornerPoints = nPointsPerFace[0];
-        thisMatchingFace.elemID        = low->elemID0;
-        thisMatchingFace.nPoly         = low->nPolySol0;
-        thisMatchingFace.nDOFsElem     = low->nDOFsElem0;
-        thisMatchingFace.elemType      = low->elemType0;
+        thisMatchingFace.elemID = low->elemID0;
+        thisMatchingFace.nPoly = low->nPolySol0;
+        thisMatchingFace.nDOFsElem = low->nDOFsElem0;
+        thisMatchingFace.elemType = low->elemType0;
 
-        for(unsigned short j=0; j<nPointsPerFace[0]; ++j) {
-          map<unsigned long,unsigned long>::const_iterator MI;
+        for (unsigned short j = 0; j < nPointsPerFace[0]; ++j) {
+          map<unsigned long, unsigned long>::const_iterator MI;
           MI = globalPointIDToLocalInd.find(faceConn[0][j]);
           unsigned long ind = MI->second;
-          const su2double *coor = nodes->GetCoord(ind);
+          const su2double* coor = nodes->GetCoord(ind);
 
-          const su2double dx =             coor[0] - center[0];
-          const su2double dy =             coor[1] - center[1];
+          const su2double dx = coor[0] - center[0];
+          const su2double dy = coor[1] - center[1];
           const su2double dz = nDim == 3 ? coor[2] - center[2] : su2double(0.0);
 
-          thisMatchingFace.cornerCoor[j][0] = rotMatrix[0][0]*dx + rotMatrix[0][1]*dy
-                                            + rotMatrix[0][2]*dz + translation[0];
-          thisMatchingFace.cornerCoor[j][1] = rotMatrix[1][0]*dx + rotMatrix[1][1]*dy
-                                            + rotMatrix[1][2]*dz + translation[1];
-          thisMatchingFace.cornerCoor[j][2] = rotMatrix[2][0]*dx + rotMatrix[2][1]*dy
-                                            + rotMatrix[2][2]*dz + translation[2];
+          thisMatchingFace.cornerCoor[j][0] =
+              rotMatrix[0][0] * dx + rotMatrix[0][1] * dy + rotMatrix[0][2] * dz + translation[0];
+          thisMatchingFace.cornerCoor[j][1] =
+              rotMatrix[1][0] * dx + rotMatrix[1][1] * dy + rotMatrix[1][2] * dz + translation[1];
+          thisMatchingFace.cornerCoor[j][2] =
+              rotMatrix[2][0] * dx + rotMatrix[2][1] * dy + rotMatrix[2][2] * dz + translation[2];
         }
 
         /*--- Create the tolerance for this face and sort the coordinates. ---*/
@@ -3022,12 +2879,12 @@ void CPhysicalGeometry::DeterminePeriodicFacesFEMGrid(CConfig                *co
         vector<CMatchingFace>::const_iterator donorLow;
         donorLow = lower_bound(facesDonor.begin(), facesDonor.end(), thisMatchingFace);
 
-        if(donorLow != facesDonor.end()) {
-          if( !(thisMatchingFace < *donorLow) ) {
-            low->elemID1            = donorLow->elemID;
-            low->nPolySol1          = donorLow->nPoly;
-            low->nDOFsElem1         = donorLow->nDOFsElem;
-            low->elemType1          = donorLow->elemType;
+        if (donorLow != facesDonor.end()) {
+          if (!(thisMatchingFace < *donorLow)) {
+            low->elemID1 = donorLow->elemID;
+            low->nPolySol1 = donorLow->nPoly;
+            low->nDOFsElem1 = donorLow->nDOFsElem;
+            low->elemType1 = donorLow->elemType;
             low->periodicIndexDonor = jMarker + 1;
           }
         }
@@ -3036,15 +2893,14 @@ void CPhysicalGeometry::DeterminePeriodicFacesFEMGrid(CConfig                *co
   }
 }
 
-void CPhysicalGeometry::DetermineFEMConstantJacobiansAndLenScale(CConfig *config) {
-
+void CPhysicalGeometry::DetermineFEMConstantJacobiansAndLenScale(CConfig* config) {
   /* Definition of the object that is used to carry out the BLAS calls. */
   CBlasStructure blasFunctions;
 
   /*--- Determine a mapping from the global point ID to the local index
         of the points.    ---*/
-  map<unsigned long,unsigned long> globalPointIDToLocalInd;
-  for(unsigned long i=0; i<nPoint; ++i) {
+  map<unsigned long, unsigned long> globalPointIDToLocalInd;
+  for (unsigned long i = 0; i < nPoint; ++i) {
     globalPointIDToLocalInd[nodes->GetGlobalIndex(i)] = i;
   }
 
@@ -3054,8 +2910,7 @@ void CPhysicalGeometry::DetermineFEMConstantJacobiansAndLenScale(CConfig *config
   vector<CFEMStandardElement> standardVolumeElements, standardFaceElements;
 
   /*--- Loop over the local volume elements. ---*/
-  for(unsigned long i=0; i<nElem; ++i) {
-
+  for (unsigned long i = 0; i < nElem; ++i) {
     /*------------------------------------------------------------------------*/
     /*--- Compute the Jacobians of the volume element and determine        ---*/
     /*--- whether the Jacobians can be considered constant.                ---*/
@@ -3065,72 +2920,68 @@ void CPhysicalGeometry::DetermineFEMConstantJacobiansAndLenScale(CConfig *config
           exist yet, it will be created. Note that it suffices to indicate that
           the Jacobians are constant, because the only task here is to determine
           whether or not the Jacobians are constant. ---*/
-    unsigned short VTK_Type  = elem[i]->GetVTK_Type();
+    unsigned short VTK_Type = elem[i]->GetVTK_Type();
     unsigned short nPolyGrid = elem[i]->GetNPolyGrid();
 
     unsigned long ii;
-    for(ii=0; ii<standardVolumeElements.size(); ++ii) {
-      if( standardVolumeElements[ii].SameStandardElement(VTK_Type, nPolyGrid, true) )
-        break;
+    for (ii = 0; ii < standardVolumeElements.size(); ++ii) {
+      if (standardVolumeElements[ii].SameStandardElement(VTK_Type, nPolyGrid, true)) break;
     }
 
-    if(ii == standardVolumeElements.size())
-      standardVolumeElements.push_back(CFEMStandardElement(VTK_Type, nPolyGrid,
-                                                           true, config));
+    if (ii == standardVolumeElements.size())
+      standardVolumeElements.push_back(CFEMStandardElement(VTK_Type, nPolyGrid, true, config));
 
     /*--- Allocate the memory for some help vectors to carry out the matrix
           product to determine the derivatives of the coordinates w.r.t.
           the parametric coordinates. ---*/
-    unsigned short nDOFs        = standardVolumeElements[ii].GetNDOFs();
+    unsigned short nDOFs = standardVolumeElements[ii].GetNDOFs();
     unsigned short nIntegration = standardVolumeElements[ii].GetNIntegration();
 
-    unsigned long sizeResult = nDim*nDim*nIntegration;
-    unsigned long sizeRHS    = nDim*nDOFs;
+    unsigned long sizeResult = nDim * nDim * nIntegration;
+    unsigned long sizeRHS = nDim * nDOFs;
 
     vector<su2double> vecResult(sizeResult), vecRHS(sizeRHS);
 
     /* Store the coordinates in vecRHS. */
     unsigned long jj = 0;
-    for(unsigned short j=0; j<nDOFs; ++j) {
+    for (unsigned short j = 0; j < nDOFs; ++j) {
       unsigned long nodeID = elem[i]->GetNode(j);
 
-      map<unsigned long,unsigned long>::const_iterator MI = globalPointIDToLocalInd.find(nodeID);
+      map<unsigned long, unsigned long>::const_iterator MI = globalPointIDToLocalInd.find(nodeID);
       unsigned long ind = MI->second;
-      for(unsigned short k=0; k<nDim; ++k, ++jj)
-        vecRHS[jj] = nodes->GetCoord(ind, k);
+      for (unsigned short k = 0; k < nDim; ++k, ++jj) vecRHS[jj] = nodes->GetCoord(ind, k);
     }
 
     /*--- Get the pointer to the matrix storage of the basis functions and its
           derivatives. The first nDOFs*nIntegration entries of this matrix
           correspond to the interpolation data to the integration points
           and are not needed. Hence this part is skipped. ---*/
-    const su2double *matBasisInt    = standardVolumeElements[ii].GetMatBasisFunctionsIntegration();
-    const su2double *matDerBasisInt = &matBasisInt[nDOFs*nIntegration];
+    const su2double* matBasisInt = standardVolumeElements[ii].GetMatBasisFunctionsIntegration();
+    const su2double* matDerBasisInt = &matBasisInt[nDOFs * nIntegration];
 
     /* Carry out the matrix matrix product. The last argument is NULL, such
        that this gemm call is ignored in the profiling. Replace by config if
        if should be included. */
-    blasFunctions.gemm(nDim*nIntegration, nDim, nDOFs, matDerBasisInt,
-                       vecRHS.data(), vecResult.data(), nullptr);
+    blasFunctions.gemm(nDim * nIntegration, nDim, nDOFs, matDerBasisInt, vecRHS.data(), vecResult.data(), nullptr);
 
     /*--- Compute the Jacobians in the integration points and determine
           the minimum and maximum values. Make a distinction between
           a 2D and 3D element. ---*/
     su2double jacMin = 1.e+25, jacMax = -1.e+25;
 
-    switch( nDim ) {
+    switch (nDim) {
       case 2: {
-
         /* 2D computation. Store the offset between the r and s derivatives. */
-        const unsigned int off = 2*nIntegration;
+        const unsigned int off = 2 * nIntegration;
 
         /*--- Loop over the integration points to compute the Jacobians. ---*/
-        for(unsigned short j=0; j<nIntegration; ++j) {
-          const unsigned int jx = 2*j; const unsigned int jy = jx+1;
-          const su2double dxdr = vecResult[jx],     dydr = vecResult[jy];
-          const su2double dxds = vecResult[jx+off], dyds = vecResult[jy+off];
+        for (unsigned short j = 0; j < nIntegration; ++j) {
+          const unsigned int jx = 2 * j;
+          const unsigned int jy = jx + 1;
+          const su2double dxdr = vecResult[jx], dydr = vecResult[jy];
+          const su2double dxds = vecResult[jx + off], dyds = vecResult[jy + off];
 
-          const su2double Jac = dxdr*dyds - dxds*dydr;
+          const su2double Jac = dxdr * dyds - dxds * dydr;
 
           jacMin = min(jacMin, Jac);
           jacMax = max(jacMax, Jac);
@@ -3141,17 +2992,18 @@ void CPhysicalGeometry::DetermineFEMConstantJacobiansAndLenScale(CConfig *config
 
       case 3: {
         /* 3D computation. Store the offset between the r and s and r and t derivatives. */
-        const unsigned int offS = 3*nIntegration, offT = 6*nIntegration;
+        const unsigned int offS = 3 * nIntegration, offT = 6 * nIntegration;
 
         /*--- Loop over the integration points to compute the Jacobians. ---*/
-        for(unsigned short j=0; j<nIntegration; ++j) {
-          const unsigned int jx = 3*j; const unsigned int jy = jx+1, jz = jx+2;
-          const su2double dxdr = vecResult[jx],      dydr = vecResult[jy],      dzdr = vecResult[jz];
-          const su2double dxds = vecResult[jx+offS], dyds = vecResult[jy+offS], dzds = vecResult[jz+offS];
-          const su2double dxdt = vecResult[jx+offT], dydt = vecResult[jy+offT], dzdt = vecResult[jz+offT];
+        for (unsigned short j = 0; j < nIntegration; ++j) {
+          const unsigned int jx = 3 * j;
+          const unsigned int jy = jx + 1, jz = jx + 2;
+          const su2double dxdr = vecResult[jx], dydr = vecResult[jy], dzdr = vecResult[jz];
+          const su2double dxds = vecResult[jx + offS], dyds = vecResult[jy + offS], dzds = vecResult[jz + offS];
+          const su2double dxdt = vecResult[jx + offT], dydt = vecResult[jy + offT], dzdt = vecResult[jz + offT];
 
-          const su2double Jac = dxdr*(dyds*dzdt - dzds*dydt) - dxds*(dydr*dzdt - dzdr*dydt)
-                              + dxdt*(dydr*dzds - dzdr*dyds);
+          const su2double Jac = dxdr * (dyds * dzdt - dzds * dydt) - dxds * (dydr * dzdt - dzdr * dydt) +
+                                dxdt * (dydr * dzds - dzdr * dyds);
 
           jacMin = min(jacMin, Jac);
           jacMax = max(jacMax, Jac);
@@ -3162,13 +3014,12 @@ void CPhysicalGeometry::DetermineFEMConstantJacobiansAndLenScale(CConfig *config
     }
 
     /*--- Check for negative Jacobians. ---*/
-    if(jacMin <= 0.0)
-      SU2_MPI::Error("Negative Jacobian found", CURRENT_FUNCTION);
+    if (jacMin <= 0.0) SU2_MPI::Error("Negative Jacobian found", CURRENT_FUNCTION);
 
     /*--- Determine the ratio of the maximum and minimum value of the Jacobian.
           From this ratio, determine whether or not the element is considered to
           have a constant Jacobian. ---*/
-    bool constJacobian = (jacMax/jacMin) <= 1.000001;
+    bool constJacobian = (jacMax / jacMin) <= 1.000001;
     elem[i]->SetJacobianConsideredConstant(constJacobian);
 
     /*------------------------------------------------------------------------*/
@@ -3180,7 +3031,7 @@ void CPhysicalGeometry::DetermineFEMConstantJacobiansAndLenScale(CConfig *config
           of this element. ---*/
     unsigned short nFaces;
     unsigned short nPointsPerFace[6];
-    unsigned long  faceConn[6][4];
+    unsigned long faceConn[6][4];
 
     elem[i]->GetCornerPointsAllFaces(nFaces, nPointsPerFace, faceConn);
 
@@ -3190,99 +3041,112 @@ void CPhysicalGeometry::DetermineFEMConstantJacobiansAndLenScale(CConfig *config
 
     /*--- Loop over the number of faces of this element. ---*/
     su2double jacFaceMax = 0.0;
-    for(unsigned short j=0; j<nFaces; ++j) {
-
+    for (unsigned short j = 0; j < nFaces; ++j) {
       /*--- Determine the index jj in the standard face elements for this face.
             If not present, create the standard element. ---*/
-      switch( nPointsPerFace[j] ) {
-        case 2: VTK_Type = LINE;          break;
-        case 3: VTK_Type = TRIANGLE;      break;
-        case 4: VTK_Type = QUADRILATERAL; break;
+      switch (nPointsPerFace[j]) {
+        case 2:
+          VTK_Type = LINE;
+          break;
+        case 3:
+          VTK_Type = TRIANGLE;
+          break;
+        case 4:
+          VTK_Type = QUADRILATERAL;
+          break;
       }
 
-      for(jj=0; jj<standardFaceElements.size(); ++jj) {
-        if( standardFaceElements[jj].SameStandardElement(VTK_Type, nPolyGrid, true) )
-          break;
+      for (jj = 0; jj < standardFaceElements.size(); ++jj) {
+        if (standardFaceElements[jj].SameStandardElement(VTK_Type, nPolyGrid, true)) break;
       }
 
-      if(jj == standardFaceElements.size())
-        standardFaceElements.push_back(CFEMStandardElement(VTK_Type, nPolyGrid,
-                                                           true, config));
+      if (jj == standardFaceElements.size())
+        standardFaceElements.push_back(CFEMStandardElement(VTK_Type, nPolyGrid, true, config));
 
       /*--- Set the pointer to store the face connectivity of this face. ---*/
-      unsigned short *connFace = nullptr;
-      switch( j) {
-        case 0: connFace = standardVolumeElements[ii].GetConnFace0(); break;
-        case 1: connFace = standardVolumeElements[ii].GetConnFace1(); break;
-        case 2: connFace = standardVolumeElements[ii].GetConnFace2(); break;
-        case 3: connFace = standardVolumeElements[ii].GetConnFace3(); break;
-        case 4: connFace = standardVolumeElements[ii].GetConnFace4(); break;
-        case 5: connFace = standardVolumeElements[ii].GetConnFace5(); break;
+      unsigned short* connFace = nullptr;
+      switch (j) {
+        case 0:
+          connFace = standardVolumeElements[ii].GetConnFace0();
+          break;
+        case 1:
+          connFace = standardVolumeElements[ii].GetConnFace1();
+          break;
+        case 2:
+          connFace = standardVolumeElements[ii].GetConnFace2();
+          break;
+        case 3:
+          connFace = standardVolumeElements[ii].GetConnFace3();
+          break;
+        case 4:
+          connFace = standardVolumeElements[ii].GetConnFace4();
+          break;
+        case 5:
+          connFace = standardVolumeElements[ii].GetConnFace5();
+          break;
       }
 
       /*--- Store the relevant derivative vectors of the standard element of
             the face as well as the number of DOFs and integration points. ---*/
-      nDOFs        = standardFaceElements[jj].GetNDOFs();
+      nDOFs = standardFaceElements[jj].GetNDOFs();
       nIntegration = standardFaceElements[jj].GetNIntegration();
 
-      const su2double *dr = standardFaceElements[jj].GetDrBasisFunctionsIntegration();
-      const su2double *ds = standardFaceElements[jj].GetDsBasisFunctionsIntegration();
+      const su2double* dr = standardFaceElements[jj].GetDrBasisFunctionsIntegration();
+      const su2double* ds = standardFaceElements[jj].GetDsBasisFunctionsIntegration();
 
       /*--- Allocate the memory for the vector to store the normals in the
             integration points of the face. */
-      vector<su2double> normalsFace((nDim+1)*nIntegration);
+      vector<su2double> normalsFace((nDim + 1) * nIntegration);
 
       /*--- Compute the unit normals in the integration points. Make a
             distinction between two and three dimensions.  ---*/
-      switch( nDim ) {
+      switch (nDim) {
         case 2: {
-
           /*--- Two dimensional case, for which the faces are edges.
                 The normal is the vector normal to the tangent vector
                 of the edge. Loop over the integration points. ---*/
-          for(unsigned short k=0; k<nIntegration; ++k) {
-
-            const su2double *drr = &dr[k*nDOFs];
+          for (unsigned short k = 0; k < nIntegration; ++k) {
+            const su2double* drr = &dr[k * nDOFs];
             su2double dxdr = 0.0, dydr = 0.0;
-            for(unsigned short l=0; l<nDOFs; ++l) {
-              dxdr += vecRHS[2*connFace[l]]  *drr[l];
-              dydr += vecRHS[2*connFace[l]+1]*drr[l];
+            for (unsigned short l = 0; l < nDOFs; ++l) {
+              dxdr += vecRHS[2 * connFace[l]] * drr[l];
+              dydr += vecRHS[2 * connFace[l] + 1] * drr[l];
             }
 
-            normalsFace[3*k]   =  dydr;
-            normalsFace[3*k+1] = -dxdr;
-            normalsFace[3*k+2] =  sqrt(dxdr*dxdr + dydr*dydr);
+            normalsFace[3 * k] = dydr;
+            normalsFace[3 * k + 1] = -dxdr;
+            normalsFace[3 * k + 2] = sqrt(dxdr * dxdr + dydr * dydr);
           }
 
           break;
         }
 
         case 3: {
-
           /*--- Three dimensional case, for which the faces are triangles or
                 quadrilaterals. The normal is the vector obtained via the
                 cross product of two tangent vectors.
                 Loop over the integration points.               ---*/
-          for(unsigned short k=0; k<nIntegration; ++k) {
-
-            const su2double *drr = &dr[k*nDOFs], *dss = &ds[k*nDOFs];
-            su2double dxdr = 0.0, dydr = 0.0, dzdr = 0.0,
-                      dxds = 0.0, dyds = 0.0, dzds = 0.0;
-
-            for(unsigned short l=0; l<nDOFs; ++l) {
-              dxdr += vecRHS[3*connFace[l]]  *drr[l]; dxds += vecRHS[3*connFace[l]]  *dss[l];
-              dydr += vecRHS[3*connFace[l]+1]*drr[l]; dyds += vecRHS[3*connFace[l]+1]*dss[l];
-              dzdr += vecRHS[3*connFace[l]+2]*drr[l]; dzds += vecRHS[3*connFace[l]+2]*dss[l];
+          for (unsigned short k = 0; k < nIntegration; ++k) {
+            const su2double *drr = &dr[k * nDOFs], *dss = &ds[k * nDOFs];
+            su2double dxdr = 0.0, dydr = 0.0, dzdr = 0.0, dxds = 0.0, dyds = 0.0, dzds = 0.0;
+
+            for (unsigned short l = 0; l < nDOFs; ++l) {
+              dxdr += vecRHS[3 * connFace[l]] * drr[l];
+              dxds += vecRHS[3 * connFace[l]] * dss[l];
+              dydr += vecRHS[3 * connFace[l] + 1] * drr[l];
+              dyds += vecRHS[3 * connFace[l] + 1] * dss[l];
+              dzdr += vecRHS[3 * connFace[l] + 2] * drr[l];
+              dzds += vecRHS[3 * connFace[l] + 2] * dss[l];
             }
 
-            su2double nx = dydr*dzds - dyds*dzdr;
-            su2double ny = dxds*dzdr - dxdr*dzds;
-            su2double nz = dxdr*dyds - dxds*dydr;
+            su2double nx = dydr * dzds - dyds * dzdr;
+            su2double ny = dxds * dzdr - dxdr * dzds;
+            su2double nz = dxdr * dyds - dxds * dydr;
 
-            normalsFace[4*k]   = nx;
-            normalsFace[4*k+1] = ny;
-            normalsFace[4*k+2] = nz;
-            normalsFace[4*k+3] = sqrt(nx*nx + ny*ny + nz*nz);
+            normalsFace[4 * k] = nx;
+            normalsFace[4 * k + 1] = ny;
+            normalsFace[4 * k + 2] = nz;
+            normalsFace[4 * k + 3] = sqrt(nx * nx + ny * ny + nz * nz);
           }
 
           break;
@@ -3294,20 +3158,19 @@ void CPhysicalGeometry::DetermineFEMConstantJacobiansAndLenScale(CConfig *config
             maximum length of the normal is determined.     ---*/
       su2double normLenMin = 1.0e-15, normLenMax = 0.0;
       su2double minCosAngleFaceNormals = 1.0;
-      unsigned short kk = (nDim+1);
-      for(unsigned short k=0; k<nIntegration; ++k) {
-
-        if(k == 0) normLenMin = normLenMax = normalsFace[nDim];
+      unsigned short kk = (nDim + 1);
+      for (unsigned short k = 0; k < nIntegration; ++k) {
+        if (k == 0)
+          normLenMin = normLenMax = normalsFace[nDim];
         else {
-          normLenMin = min(normLenMin, normalsFace[k*kk+nDim]);
-          normLenMax = max(normLenMax, normalsFace[k*kk+nDim]);
+          normLenMin = min(normLenMin, normalsFace[k * kk + nDim]);
+          normLenMax = max(normLenMax, normalsFace[k * kk + nDim]);
         }
 
-        for(unsigned short l=k+1; l<nIntegration; ++l) {
+        for (unsigned short l = k + 1; l < nIntegration; ++l) {
           su2double dot = 0.0;
-          for(unsigned short m=0; m<nDim; ++m)
-            dot += normalsFace[k*kk+m]*normalsFace[l*kk+m];
-          dot /= normalsFace[k*kk+nDim]*normalsFace[l*kk+nDim];
+          for (unsigned short m = 0; m < nDim; ++m) dot += normalsFace[k * kk + m] * normalsFace[l * kk + m];
+          dot /= normalsFace[k * kk + nDim] * normalsFace[l * kk + nDim];
 
           minCosAngleFaceNormals = min(minCosAngleFaceNormals, dot);
         }
@@ -3315,10 +3178,9 @@ void CPhysicalGeometry::DetermineFEMConstantJacobiansAndLenScale(CConfig *config
 
       /*--- Compute the ratio of normLenMin and normLenMax and determine
             whether the face is considered to have a constant Jacobian. ---*/
-      su2double maxRatioLenFaceNormals = normLenMax/normLenMin;
+      su2double maxRatioLenFaceNormals = normLenMax / normLenMin;
 
-      constJacobian = minCosAngleFaceNormals >= 0.999999 &&
-                      maxRatioLenFaceNormals <= 1.000001;
+      constJacobian = minCosAngleFaceNormals >= 0.999999 && maxRatioLenFaceNormals <= 1.000001;
 
       elem[i]->SetJacobianConstantFace(constJacobian, j);
 
@@ -3336,36 +3198,33 @@ void CPhysicalGeometry::DetermineFEMConstantJacobiansAndLenScale(CConfig *config
     /*--- of all the reference elements used in this code.                 ---*/
     /*------------------------------------------------------------------------*/
 
-    const su2double lenScale = 2.0*jacMin/jacFaceMax;
+    const su2double lenScale = 2.0 * jacMin / jacFaceMax;
     elem[i]->SetLengthScale(lenScale);
   }
 }
 
-void CPhysicalGeometry::DetermineDonorElementsWallFunctions(CConfig *config) {
-
+void CPhysicalGeometry::DetermineDonorElementsWallFunctions(CConfig* config) {
   /*--------------------------------------------------------------------------*/
   /*--- Step 1: Check whether wall functions are used at all.              ---*/
   /*--------------------------------------------------------------------------*/
 
   bool wallFunctions = false;
-  for(unsigned short iMarker=0; iMarker<nMarker; ++iMarker) {
-
+  for (unsigned short iMarker = 0; iMarker < nMarker; ++iMarker) {
     switch (config->GetMarker_All_KindBC(iMarker)) {
       case ISOTHERMAL:
       case HEAT_FLUX: {
         const string Marker_Tag = config->GetMarker_All_TagBound(iMarker);
-        if(config->GetWallFunction_Treatment(Marker_Tag) != WALL_FUNCTIONS::NONE)
-          wallFunctions = true;
+        if (config->GetWallFunction_Treatment(Marker_Tag) != WALL_FUNCTIONS::NONE) wallFunctions = true;
         break;
       }
-      default:  /* Just to avoid a compiler warning. */
+      default: /* Just to avoid a compiler warning. */
         break;
     }
   }
 
   /* If no wall functions are used, nothing needs to be done and a
      return can be made. */
-  if( !wallFunctions ) return;
+  if (!wallFunctions) return;
 
   /*--------------------------------------------------------------------------*/
   /*--- Step 2: Build the ADT of the linear sub-elements of the locally    ---*/
@@ -3374,8 +3233,8 @@ void CPhysicalGeometry::DetermineDonorElementsWallFunctions(CConfig *config) {
 
   /* Determine a mapping from the global point ID to the local index
      of the points. */
-  map<unsigned long,unsigned long> globalPointIDToLocalInd;
-  for(unsigned long i=0; i<nPoint; ++i) {
+  map<unsigned long, unsigned long> globalPointIDToLocalInd;
+  for (unsigned long i = 0; i < nPoint; ++i) {
     globalPointIDToLocalInd[nodes->GetGlobalIndex(i)] = i;
   }
 
@@ -3385,65 +3244,61 @@ void CPhysicalGeometry::DetermineDonorElementsWallFunctions(CConfig *config) {
   /* Define the vectors, which store the mapping from the subelement to the
      parent element, subelement ID within the parent element, the element
      type and the connectivity of the subelements. */
-  vector<unsigned long>  parentElement;
+  vector<unsigned long> parentElement;
   vector<unsigned short> subElementIDInParent;
   vector<unsigned short> VTK_TypeElem;
-  vector<unsigned long>  elemConn;
+  vector<unsigned long> elemConn;
 
   /* Loop over the local volume elements to create the connectivity of
      the linear sub-elements. */
-  for(unsigned long l=0; l<nElem; ++l) {
-
+  for (unsigned long l = 0; l < nElem; ++l) {
     /* Determine the standard element of the volume element. If it does not
        exist yet, it will be created. Note that it suffices to create a
        standard element for a constant Jacobian, because the element is
        split into its linear sub-elements for the ADT. */
     unsigned short VTK_Parent = elem[l]->GetVTK_Type();
-    unsigned short nPolyGrid  = elem[l]->GetNPolyGrid();
+    unsigned short nPolyGrid = elem[l]->GetNPolyGrid();
 
     unsigned long ii;
-    for(ii=0; ii<standardVolumeElements.size(); ++ii) {
-      if( standardVolumeElements[ii].SameStandardElement(VTK_Parent, nPolyGrid, true) )
-        break;
+    for (ii = 0; ii < standardVolumeElements.size(); ++ii) {
+      if (standardVolumeElements[ii].SameStandardElement(VTK_Parent, nPolyGrid, true)) break;
     }
 
-    if(ii == standardVolumeElements.size())
-      standardVolumeElements.push_back(CFEMStandardElement(VTK_Parent, nPolyGrid,
-                                                           true, config));
+    if (ii == standardVolumeElements.size())
+      standardVolumeElements.push_back(CFEMStandardElement(VTK_Parent, nPolyGrid, true, config));
 
     /* Determine the necessary data for splitting the element in its linear
        sub-elements. */
-    unsigned short VTK_Type[]  = {standardVolumeElements[ii].GetVTK_Type1(),
-                                  standardVolumeElements[ii].GetVTK_Type2()};
+    unsigned short VTK_Type[] = {standardVolumeElements[ii].GetVTK_Type1(), standardVolumeElements[ii].GetVTK_Type2()};
     unsigned short nSubElems[] = {0, 0};
     unsigned short nDOFsPerSubElem[] = {0, 0};
-    const unsigned short *connSubElems[] = {nullptr, nullptr};
+    const unsigned short* connSubElems[] = {nullptr, nullptr};
 
-    if(VTK_Type[0] != NONE) {
-      nSubElems[0]       = standardVolumeElements[ii].GetNSubElemsType1();
+    if (VTK_Type[0] != NONE) {
+      nSubElems[0] = standardVolumeElements[ii].GetNSubElemsType1();
       nDOFsPerSubElem[0] = standardVolumeElements[ii].GetNDOFsPerSubElem(VTK_Type[0]);
-      connSubElems[0]    = standardVolumeElements[ii].GetSubConnType1();
+      connSubElems[0] = standardVolumeElements[ii].GetSubConnType1();
     }
 
-    if(VTK_Type[1] != NONE) {
-      nSubElems[1]       = standardVolumeElements[ii].GetNSubElemsType2();
+    if (VTK_Type[1] != NONE) {
+      nSubElems[1] = standardVolumeElements[ii].GetNSubElemsType2();
       nDOFsPerSubElem[1] = standardVolumeElements[ii].GetNDOFsPerSubElem(VTK_Type[1]);
-      connSubElems[1]    = standardVolumeElements[ii].GetSubConnType2();
+      connSubElems[1] = standardVolumeElements[ii].GetSubConnType2();
     }
 
     /* Store the connectivity of the sub-elements. Note that local node
        numbering must be used for these sub-elements. */
     unsigned short jj = 0;
-    for(unsigned short i=0; i<2; ++i) {
+    for (unsigned short i = 0; i < 2; ++i) {
       unsigned short kk = 0;
-      for(unsigned short j=0; j<nSubElems[i]; ++j, ++jj) {
+      for (unsigned short j = 0; j < nSubElems[i]; ++j, ++jj) {
         parentElement.push_back(elem[l]->GetGlobalElemID());
         subElementIDInParent.push_back(jj);
         VTK_TypeElem.push_back(VTK_Type[i]);
 
-        for(unsigned short k=0; k<nDOFsPerSubElem[i]; ++k, ++kk) {
+        for (unsigned short k = 0; k < nDOFsPerSubElem[i]; ++k, ++kk) {
           unsigned long nodeID = elem[l]->GetNode(connSubElems[i][kk]);
-          map<unsigned long,unsigned long>::const_iterator MI;
+          map<unsigned long, unsigned long>::const_iterator MI;
           MI = globalPointIDToLocalInd.find(nodeID);
 
           elemConn.push_back(MI->second);
@@ -3454,17 +3309,15 @@ void CPhysicalGeometry::DetermineDonorElementsWallFunctions(CConfig *config) {
 
   /* Store the coordinates of the locally stored nodes in the format
      expected by the ADT. */
-  vector<su2double> volCoor(nDim*nPoint);
+  vector<su2double> volCoor(nDim * nPoint);
 
   unsigned long jj = 0;
-  for(unsigned long l=0; l<nPoint; ++l) {
-    for(unsigned short k=0; k<nDim; ++k, ++jj)
-      volCoor[jj] = nodes->GetCoord(l, k);
+  for (unsigned long l = 0; l < nPoint; ++l) {
+    for (unsigned short k = 0; k < nDim; ++k, ++jj) volCoor[jj] = nodes->GetCoord(l, k);
   }
 
   /* Build the local ADT. */
-  CADTElemClass localVolumeADT(nDim, volCoor, elemConn, VTK_TypeElem,
-                               subElementIDInParent, parentElement, false);
+  CADTElemClass localVolumeADT(nDim, volCoor, elemConn, VTK_TypeElem, subElementIDInParent, parentElement, false);
 
   /* Release the memory of the vectors used to build the ADT. To make sure
      that all the memory is deleted, the swap function is used. */
@@ -3483,53 +3336,46 @@ void CPhysicalGeometry::DetermineDonorElementsWallFunctions(CConfig *config) {
      and exchange coordinates for the integration points for which no donor
      element was found in the locally stored volume elements. */
   vector<unsigned short> markerIDGlobalSearch;
-  vector<unsigned long>  boundaryElemIDGlobalSearch;
-  vector<su2double>      coorExGlobalSearch;
-
+  vector<unsigned long> boundaryElemIDGlobalSearch;
+  vector<su2double> coorExGlobalSearch;
 
   /* Define the standard boundary faces for the solution and the grid. */
-  vector<CFEMStandardBoundaryFace> standardBoundaryFacesSol,
-                                   standardBoundaryFacesGrid;
+  vector<CFEMStandardBoundaryFace> standardBoundaryFacesSol, standardBoundaryFacesGrid;
 
   /* Loop over the markers and select the ones for which a wall function
      treatment must be carried out. */
-  for(unsigned short iMarker=0; iMarker<nMarker; ++iMarker) {
-
+  for (unsigned short iMarker = 0; iMarker < nMarker; ++iMarker) {
     switch (config->GetMarker_All_KindBC(iMarker)) {
       case ISOTHERMAL:
       case HEAT_FLUX: {
         const string Marker_Tag = config->GetMarker_All_TagBound(iMarker);
-        if(config->GetWallFunction_Treatment(Marker_Tag) != WALL_FUNCTIONS::NONE) {
-
+        if (config->GetWallFunction_Treatment(Marker_Tag) != WALL_FUNCTIONS::NONE) {
           /* Retrieve the floating point information for this boundary marker.
              The exchange location is the first element of this array. */
-          const su2double *doubleInfo = config->GetWallFunction_DoubleInfo(Marker_Tag);
+          const su2double* doubleInfo = config->GetWallFunction_DoubleInfo(Marker_Tag);
 
           /* Loop over the local boundary elements for this marker. */
-          for(unsigned long l=0; l<nElem_Bound[iMarker]; ++l) {
-
+          for (unsigned long l = 0; l < nElem_Bound[iMarker]; ++l) {
             /* Easier storage of the element type, the corresponding volume
                element and the polynomial degree for the solution and grid. */
-            const unsigned short VTK_Type  = bound[iMarker][l]->GetVTK_Type();
-            const unsigned long  elemID    = bound[iMarker][l]->GetDomainElement()
-                                           - beg_node[rank];
+            const unsigned short VTK_Type = bound[iMarker][l]->GetVTK_Type();
+            const unsigned long elemID = bound[iMarker][l]->GetDomainElement() - beg_node[rank];
             const unsigned short nPolyGrid = bound[iMarker][l]->GetNPolyGrid();
-            const unsigned short nPolySol  = elem[elemID]->GetNPolySol();
-            const unsigned short VTK_Elem  = elem[elemID]->GetVTK_Type();
+            const unsigned short nPolySol = elem[elemID]->GetNPolySol();
+            const unsigned short VTK_Elem = elem[elemID]->GetVTK_Type();
 
             /* Get the corner points of the boundary element. Note that this
                is an overloaded function, hence the arguments that allow for
                multiple faces. */
             unsigned short nFaces;
             unsigned short nPointsPerFace[6];
-            unsigned long  faceConn[6][4];
+            unsigned long faceConn[6][4];
             bound[iMarker][l]->GetCornerPointsAllFaces(nFaces, nPointsPerFace, faceConn);
 
             /* Create an object of CFaceOfElement to store the information. */
             CFaceOfElement boundaryFace;
             boundaryFace.nCornerPoints = nPointsPerFace[0];
-            for(unsigned short i=0; i<nPointsPerFace[0]; ++i)
-              boundaryFace.cornerPoints[i] = faceConn[0][i];
+            for (unsigned short i = 0; i < nPointsPerFace[0]; ++i) boundaryFace.cornerPoints[i] = faceConn[0][i];
             boundaryFace.elemID0 = elemID;
 
             /* Renumber the corner points of the face, but keep the orientation. */
@@ -3543,23 +3389,20 @@ void CPhysicalGeometry::DetermineDonorElementsWallFunctions(CConfig *config) {
             /* Loop over the faces of the element to determine which one is
                the boundary face. */
             unsigned long ii;
-            bool outwardPointing = true;   /* Initialized to avoid compiler warning. */
-            for(ii=0; ii<nFaces; ++ii) {
-
+            bool outwardPointing = true; /* Initialized to avoid compiler warning. */
+            for (ii = 0; ii < nFaces; ++ii) {
               /* Create an object of CFaceOfElement to store the information.
                  Renumber the corner points, but keep the orientation. */
               CFaceOfElement thisFace;
               thisFace.nCornerPoints = nPointsPerFace[ii];
-              for(unsigned short i=0; i<nPointsPerFace[ii]; ++i)
-                thisFace.cornerPoints[i] = faceConn[ii][i];
+              for (unsigned short i = 0; i < nPointsPerFace[ii]; ++i) thisFace.cornerPoints[i] = faceConn[ii][i];
               thisFace.elemID0 = elemID;
 
               thisFace.CreateUniqueNumberingWithOrientation();
               const bool thisFaceSwapped = thisFace.elemID1 == elemID;
 
               /* Check if this face is the boundary face. */
-              if(boundaryFace == thisFace) {
-
+              if (boundaryFace == thisFace) {
                 /* Determine whether the orientation of the boundary face is
                    pointing out of the adjacent element. */
                 outwardPointing = boundaryFaceSwapped == thisFaceSwapped;
@@ -3570,9 +3413,7 @@ void CPhysicalGeometry::DetermineDonorElementsWallFunctions(CConfig *config) {
             }
 
             /* Additional check, just to be sure. */
-            if(ii == nFaces)
-              SU2_MPI::Error("Boundary face not found in faces of element",
-                             CURRENT_FUNCTION);
+            if (ii == nFaces) SU2_MPI::Error("Boundary face not found in faces of element", CURRENT_FUNCTION);
 
             /* Determine whether or not the Jacobian of the boundary face
                is constant. */
@@ -3584,43 +3425,38 @@ void CPhysicalGeometry::DetermineDonorElementsWallFunctions(CConfig *config) {
                of both the solution and grid must match. If a new standard
                element must be created, make sure that the integration points
                of the solution element are used for the grid element. */
-            for(ii=0; ii<standardBoundaryFacesSol.size(); ++ii) {
-              if(standardBoundaryFacesSol[ii].SameStandardBoundaryFace(VTK_Type, constJac,
-                                                                       VTK_Elem, nPolySol,
-                                                                       false) &&
-                 standardBoundaryFacesGrid[ii].SameStandardBoundaryFace(VTK_Type, constJac,
-                                                                        VTK_Elem, nPolyGrid,
-                                                                        false) )
+            for (ii = 0; ii < standardBoundaryFacesSol.size(); ++ii) {
+              if (standardBoundaryFacesSol[ii].SameStandardBoundaryFace(VTK_Type, constJac, VTK_Elem, nPolySol,
+                                                                        false) &&
+                  standardBoundaryFacesGrid[ii].SameStandardBoundaryFace(VTK_Type, constJac, VTK_Elem, nPolyGrid,
+                                                                         false))
                 break;
             }
 
-            if(ii == standardBoundaryFacesSol.size()) {
-              standardBoundaryFacesSol.push_back(CFEMStandardBoundaryFace(VTK_Type, VTK_Elem,
-                                                                          nPolySol, constJac,
-                                                                          false, config));
-              standardBoundaryFacesGrid.push_back(CFEMStandardBoundaryFace(VTK_Type, VTK_Elem,
-                                                                           nPolyGrid, constJac,
-                                                                           false, config,
-                                                                           standardBoundaryFacesSol[ii].GetOrderExact()) );
+            if (ii == standardBoundaryFacesSol.size()) {
+              standardBoundaryFacesSol.push_back(
+                  CFEMStandardBoundaryFace(VTK_Type, VTK_Elem, nPolySol, constJac, false, config));
+              standardBoundaryFacesGrid.push_back(
+                  CFEMStandardBoundaryFace(VTK_Type, VTK_Elem, nPolyGrid, constJac, false, config,
+                                           standardBoundaryFacesSol[ii].GetOrderExact()));
             }
 
             /* Get the required information from the standard element. */
             const unsigned short nDOFs = standardBoundaryFacesGrid[ii].GetNDOFsFace();
-            const unsigned short nInt  = standardBoundaryFacesGrid[ii].GetNIntegration();
-            const su2double *lag = standardBoundaryFacesGrid[ii].GetBasisFaceIntegration();
-            const su2double *dr  = standardBoundaryFacesGrid[ii].GetDrBasisFaceIntegration();
-            const su2double *ds  = standardBoundaryFacesGrid[ii].GetDsBasisFaceIntegration();
+            const unsigned short nInt = standardBoundaryFacesGrid[ii].GetNIntegration();
+            const su2double* lag = standardBoundaryFacesGrid[ii].GetBasisFaceIntegration();
+            const su2double* dr = standardBoundaryFacesGrid[ii].GetDrBasisFaceIntegration();
+            const su2double* ds = standardBoundaryFacesGrid[ii].GetDsBasisFaceIntegration();
 
             /* Create the vector of coordinates for this boundary face. */
-            vector<su2double> coorBoundFace(nDim*nDOFs);
+            vector<su2double> coorBoundFace(nDim * nDOFs);
             ii = 0;
-            for(unsigned short j=0; j<nDOFs; ++j) {
+            for (unsigned short j = 0; j < nDOFs; ++j) {
               unsigned long nodeID = bound[iMarker][l]->GetNode(j);
-              map<unsigned long,unsigned long>::const_iterator MI;
+              map<unsigned long, unsigned long>::const_iterator MI;
               MI = globalPointIDToLocalInd.find(nodeID);
               nodeID = MI->second;
-              for(unsigned short k=0; k<nDim; ++k, ++ii)
-              coorBoundFace[ii] = nodes->GetCoord(nodeID, k);
+              for (unsigned short k = 0; k < nDim; ++k, ++ii) coorBoundFace[ii] = nodes->GetCoord(nodeID, k);
             }
 
             /* Set the multiplication factor for the normal, such that
@@ -3630,39 +3466,40 @@ void CPhysicalGeometry::DetermineDonorElementsWallFunctions(CConfig *config) {
 
             /* Allocate the memory for the exchange locations corresponding to
                the integration points of this face. */
-            vector<su2double> coorExchange(nDim*nInt);
+            vector<su2double> coorExchange(nDim * nInt);
 
             /* Make a distinction between 2D and 3D to compute the actual
                coordinates of the exchange locations. */
-            switch(nDim) {
+            switch (nDim) {
               case 2: {
                 /* Two dimensional computation. Loop over the integration
                    points to compute the corresponding exchange coordinates. */
-                for(unsigned short i=0; i<nInt; ++i) {
-
+                for (unsigned short i = 0; i < nInt; ++i) {
                   /* Compute the coordinates and the tangential vector
                      in the integration point. */
                   su2double xInt = 0.0, yInt = 0.0, dxdr = 0.0, dydr = 0.0;
-                  const su2double *lagInt = lag + i*nDOFs;
-                  const su2double *drr    = dr  + i*nDOFs;
-
-                  for(unsigned short k=0; k<nDOFs; ++k) {
-                    const su2double *coorDOF = coorBoundFace.data() + 2*k;
-                    xInt += lagInt[k]*coorDOF[0]; yInt += lagInt[k]*coorDOF[1];
-                    dxdr += drr[k]*coorDOF[0];    dydr += drr[k]*coorDOF[1];
+                  const su2double* lagInt = lag + i * nDOFs;
+                  const su2double* drr = dr + i * nDOFs;
+
+                  for (unsigned short k = 0; k < nDOFs; ++k) {
+                    const su2double* coorDOF = coorBoundFace.data() + 2 * k;
+                    xInt += lagInt[k] * coorDOF[0];
+                    yInt += lagInt[k] * coorDOF[1];
+                    dxdr += drr[k] * coorDOF[0];
+                    dydr += drr[k] * coorDOF[1];
                   }
 
                   /* Compute the vector from the integration point to
                      the coordinates of the exchange location. This is the
                      unit inward normal multiplied by the exchange distance. */
-                  const su2double lenNorm = sqrt(dxdr*dxdr + dydr*dydr);
-                  const su2double invLenNorm = lenNorm < su2double(1.e-35) ? su2double(1.e+35) : 1.0/lenNorm;
+                  const su2double lenNorm = sqrt(dxdr * dxdr + dydr * dydr);
+                  const su2double invLenNorm = lenNorm < su2double(1.e-35) ? su2double(1.e+35) : 1.0 / lenNorm;
 
-                  const su2double dx =  factNorm*dydr*invLenNorm;
-                  const su2double dy = -factNorm*dxdr*invLenNorm;
+                  const su2double dx = factNorm * dydr * invLenNorm;
+                  const su2double dy = -factNorm * dxdr * invLenNorm;
 
                   /* Compute the coordinates of the exchange location. */
-                  su2double *coorEx = coorExchange.data() + nDim*i;
+                  su2double* coorEx = coorExchange.data() + nDim * i;
                   coorEx[0] = xInt + dx;
                   coorEx[1] = yInt + dy;
                 }
@@ -3673,40 +3510,44 @@ void CPhysicalGeometry::DetermineDonorElementsWallFunctions(CConfig *config) {
               case 3: {
                 /* Three dimensional computation. Loop over the integration
                    points to compute the corresponding exchange coordinates. */
-                for(unsigned short i=0; i<nInt; ++i) {
-
+                for (unsigned short i = 0; i < nInt; ++i) {
                   /* Compute the coordinates and the tangential vectors
                      in the integration point. */
-                  const su2double *lagInt = lag + i*nDOFs;
-                  const su2double *drr = dr + i*nDOFs, *dss = ds + i*nDOFs;
-                  su2double xInt = 0.0, yInt = 0.0, zInt = 0.0,
-                            dxdr = 0.0, dydr = 0.0, dzdr = 0.0,
-                            dxds = 0.0, dyds = 0.0, dzds = 0.0;
-
-                  for(unsigned short k=0; k<nDOFs; ++k) {
-                    const su2double *coorDOF = coorBoundFace.data() + 3*k;
-                    xInt += lagInt[k]*coorDOF[0]; yInt += lagInt[k]*coorDOF[1]; zInt += lagInt[k]*coorDOF[2];
-                    dxdr += drr[k]*coorDOF[0];    dydr += drr[k]*coorDOF[1];    dzdr += drr[k]*coorDOF[2];
-                    dxds += dss[k]*coorDOF[0];    dyds += dss[k]*coorDOF[1];    dzds += dss[k]*coorDOF[2];
+                  const su2double* lagInt = lag + i * nDOFs;
+                  const su2double *drr = dr + i * nDOFs, *dss = ds + i * nDOFs;
+                  su2double xInt = 0.0, yInt = 0.0, zInt = 0.0, dxdr = 0.0, dydr = 0.0, dzdr = 0.0, dxds = 0.0,
+                            dyds = 0.0, dzds = 0.0;
+
+                  for (unsigned short k = 0; k < nDOFs; ++k) {
+                    const su2double* coorDOF = coorBoundFace.data() + 3 * k;
+                    xInt += lagInt[k] * coorDOF[0];
+                    yInt += lagInt[k] * coorDOF[1];
+                    zInt += lagInt[k] * coorDOF[2];
+                    dxdr += drr[k] * coorDOF[0];
+                    dydr += drr[k] * coorDOF[1];
+                    dzdr += drr[k] * coorDOF[2];
+                    dxds += dss[k] * coorDOF[0];
+                    dyds += dss[k] * coorDOF[1];
+                    dzds += dss[k] * coorDOF[2];
                   }
 
                   /* Compute the outward pointing normal. */
-                  const su2double nx = -(dydr*dzds - dyds*dzdr);
-                  const su2double ny = -(dxds*dzdr - dxdr*dzds);
-                  const su2double nz = -(dxdr*dyds - dxds*dydr);
+                  const su2double nx = -(dydr * dzds - dyds * dzdr);
+                  const su2double ny = -(dxds * dzdr - dxdr * dzds);
+                  const su2double nz = -(dxdr * dyds - dxds * dydr);
 
                   /* Compute the vector from the integration point to
                      the coordinates of the exchange location. This is the
                      unit inward normal multiplied by the exchange distance. */
-                  const su2double lenNorm = sqrt(nx*nx + ny*ny + nz*nz);
-                  const su2double invLenNorm = lenNorm < su2double(1.e-35) ? su2double(1.e+35) : 1.0/lenNorm;
+                  const su2double lenNorm = sqrt(nx * nx + ny * ny + nz * nz);
+                  const su2double invLenNorm = lenNorm < su2double(1.e-35) ? su2double(1.e+35) : 1.0 / lenNorm;
 
-                  const su2double dx = factNorm*nx*invLenNorm;
-                  const su2double dy = factNorm*ny*invLenNorm;
-                  const su2double dz = factNorm*nz*invLenNorm;
+                  const su2double dx = factNorm * nx * invLenNorm;
+                  const su2double dy = factNorm * ny * invLenNorm;
+                  const su2double dz = factNorm * nz * invLenNorm;
 
                   /* Compute the coordinates of the exchange location. */
-                  su2double *coorEx = coorExchange.data() + nDim*i;
+                  su2double* coorEx = coorExchange.data() + nDim * i;
                   coorEx[0] = xInt + dx;
                   coorEx[1] = yInt + dy;
                   coorEx[2] = zInt + dz;
@@ -3719,30 +3560,24 @@ void CPhysicalGeometry::DetermineDonorElementsWallFunctions(CConfig *config) {
             /* Loop over the integration points and determine the donor elements
                for the corresponding exchange locations. */
             vector<unsigned long> donorElementsFace;
-            for(unsigned short i=0; i<nInt; ++i) {
-
+            for (unsigned short i = 0; i < nInt; ++i) {
               /* Search for the element, which contains the exchange location. */
               unsigned short subElem;
-              unsigned long  parElem;
-              int            mpirank;
-              su2double      parCoor[3], weightsInterpol[8];
-              su2double      *coorEx = coorExchange.data() + nDim*i;
-
-              if( localVolumeADT.DetermineContainingElement(coorEx, subElem,
-                                                            parElem, mpirank, parCoor,
-                                                            weightsInterpol) ) {
+              unsigned long parElem;
+              int mpirank;
+              su2double parCoor[3], weightsInterpol[8];
+              su2double* coorEx = coorExchange.data() + nDim * i;
 
+              if (localVolumeADT.DetermineContainingElement(coorEx, subElem, parElem, mpirank, parCoor,
+                                                            weightsInterpol)) {
                 /* Donor element found. Store it in donorElementsFace. */
                 donorElementsFace.push_back(parElem);
-              }
-              else {
-
+              } else {
                 /* Donor element not found in the local ADT. Store the exchange
                    coordinates, boundary marker and boundary element ID. */
                 markerIDGlobalSearch.push_back(iMarker);
                 boundaryElemIDGlobalSearch.push_back(l);
-                for(unsigned short iDim=0; iDim<nDim; ++iDim)
-                  coorExGlobalSearch.push_back(coorEx[iDim]);
+                for (unsigned short iDim = 0; iDim < nDim; ++iDim) coorExGlobalSearch.push_back(coorEx[iDim]);
               }
             }
 
@@ -3761,7 +3596,7 @@ void CPhysicalGeometry::DetermineDonorElementsWallFunctions(CConfig *config) {
 
         break;
       }
-      default:  /* Just to avoid a compiler warning. */
+      default: /* Just to avoid a compiler warning. */
         break;
     }
   }
@@ -3769,7 +3604,7 @@ void CPhysicalGeometry::DetermineDonorElementsWallFunctions(CConfig *config) {
 #ifndef HAVE_MPI
   /* In sequential mode it should not be possible that there are points for which
      no donor elements are found. Check this. */
-  if( markerIDGlobalSearch.size() ) {
+  if (markerIDGlobalSearch.size()) {
     ostringstream message;
     message << markerIDGlobalSearch.size() << " integration points for which "
             << "no donor elements for the wall functions were found." << endl
@@ -3785,51 +3620,46 @@ void CPhysicalGeometry::DetermineDonorElementsWallFunctions(CConfig *config) {
      carried out for each rank and store them in such a way that the info can
      be used directly in Allgatherv. */
   vector<int> recvCounts(size), displs(size);
-  int nLocalSearchPoints = (int) markerIDGlobalSearch.size();
+  int nLocalSearchPoints = (int)markerIDGlobalSearch.size();
 
-  SU2_MPI::Allgather(&nLocalSearchPoints, 1, MPI_INT, recvCounts.data(), 1,
-                     MPI_INT, SU2_MPI::GetComm());
+  SU2_MPI::Allgather(&nLocalSearchPoints, 1, MPI_INT, recvCounts.data(), 1, MPI_INT, SU2_MPI::GetComm());
   displs[0] = 0;
-  for(int i=1; i<size; ++i) displs[i] = displs[i-1] + recvCounts[i-1];
+  for (int i = 1; i < size; ++i) displs[i] = displs[i - 1] + recvCounts[i - 1];
 
   int nGlobalSearchPoints = displs.back() + recvCounts.back();
 
   /* Check if there actually are global searches to be carried out. */
-  if(nGlobalSearchPoints > 0) {
-
+  if (nGlobalSearchPoints > 0) {
     /* Create a cumulative storage version of recvCounts. */
-    vector<int> nSearchPerRank(size+1);
+    vector<int> nSearchPerRank(size + 1);
     nSearchPerRank[0] = 0;
 
-    for(int i=0; i<size; ++i)
-      nSearchPerRank[i+1] = nSearchPerRank[i] + recvCounts[i];
+    for (int i = 0; i < size; ++i) nSearchPerRank[i + 1] = nSearchPerRank[i] + recvCounts[i];
 
     /* Gather the data of the search points for which a global search must
        be carried out on all ranks. */
     vector<unsigned short> bufMarkerIDGlobalSearch(nGlobalSearchPoints);
-    SU2_MPI::Allgatherv(markerIDGlobalSearch.data(), nLocalSearchPoints,
-                        MPI_UNSIGNED_SHORT, bufMarkerIDGlobalSearch.data(),
-                        recvCounts.data(), displs.data(), MPI_UNSIGNED_SHORT,
+    SU2_MPI::Allgatherv(markerIDGlobalSearch.data(), nLocalSearchPoints, MPI_UNSIGNED_SHORT,
+                        bufMarkerIDGlobalSearch.data(), recvCounts.data(), displs.data(), MPI_UNSIGNED_SHORT,
                         SU2_MPI::GetComm());
 
-
     vector<unsigned long> bufBoundaryElemIDGlobalSearch(nGlobalSearchPoints);
-    SU2_MPI::Allgatherv(boundaryElemIDGlobalSearch.data(), nLocalSearchPoints,
-                        MPI_UNSIGNED_LONG, bufBoundaryElemIDGlobalSearch.data(),
-                        recvCounts.data(), displs.data(), MPI_UNSIGNED_LONG,
+    SU2_MPI::Allgatherv(boundaryElemIDGlobalSearch.data(), nLocalSearchPoints, MPI_UNSIGNED_LONG,
+                        bufBoundaryElemIDGlobalSearch.data(), recvCounts.data(), displs.data(), MPI_UNSIGNED_LONG,
                         SU2_MPI::GetComm());
 
-    for(int i=0; i<size; ++i) {recvCounts[i] *= nDim; displs[i] *= nDim;}
-    vector<su2double> bufCoorExGlobalSearch(nDim*nGlobalSearchPoints);
-    SU2_MPI::Allgatherv(coorExGlobalSearch.data(), nDim*nLocalSearchPoints,
-                        MPI_DOUBLE, bufCoorExGlobalSearch.data(),
-                        recvCounts.data(), displs.data(), MPI_DOUBLE,
-                        SU2_MPI::GetComm());
+    for (int i = 0; i < size; ++i) {
+      recvCounts[i] *= nDim;
+      displs[i] *= nDim;
+    }
+    vector<su2double> bufCoorExGlobalSearch(nDim * nGlobalSearchPoints);
+    SU2_MPI::Allgatherv(coorExGlobalSearch.data(), nDim * nLocalSearchPoints, MPI_DOUBLE, bufCoorExGlobalSearch.data(),
+                        recvCounts.data(), displs.data(), MPI_DOUBLE, SU2_MPI::GetComm());
 
     /* Buffers to store the return information. */
     vector<unsigned short> markerIDReturn;
-    vector<unsigned long>  boundaryElemIDReturn;
-    vector<unsigned long>  volElemIDDonorReturn;
+    vector<unsigned long> boundaryElemIDReturn;
+    vector<unsigned long> volElemIDDonorReturn;
 
     /* Loop over the number of global search points to check if these points
        are contained in the volume elements of this rank. The loop is carried
@@ -3838,21 +3668,18 @@ void CPhysicalGeometry::DetermineDonorElementsWallFunctions(CConfig *config) {
        that were not found earlier on this rank. The vector recvCounts is used
        as storage for the number of search items that must be returned to the
        other ranks. */
-    for(int rankID=0; rankID<size; ++rankID) {
+    for (int rankID = 0; rankID < size; ++rankID) {
       recvCounts[rankID] = 0;
-      if(rankID != rank) {
-        for(int i=nSearchPerRank[rankID]; i<nSearchPerRank[rankID+1]; ++i) {
-
+      if (rankID != rank) {
+        for (int i = nSearchPerRank[rankID]; i < nSearchPerRank[rankID + 1]; ++i) {
           /* Search the local ADT for the coordinate of the exchange point
              and check if it is found. */
           unsigned short subElem;
-          unsigned long  parElem;
-          int            rankDonor;
-          su2double      parCoor[3], weightsInterpol[8];
-          if( localVolumeADT.DetermineContainingElement(bufCoorExGlobalSearch.data() + i*nDim,
-                                                        subElem, parElem, rankDonor, parCoor,
-                                                        weightsInterpol) ) {
-
+          unsigned long parElem;
+          int rankDonor;
+          su2double parCoor[3], weightsInterpol[8];
+          if (localVolumeADT.DetermineContainingElement(bufCoorExGlobalSearch.data() + i * nDim, subElem, parElem,
+                                                        rankDonor, parCoor, weightsInterpol)) {
             /* Store the required data in the return buffers. */
             ++recvCounts[rankID];
             markerIDReturn.push_back(bufMarkerIDGlobalSearch[i]);
@@ -3864,42 +3691,39 @@ void CPhysicalGeometry::DetermineDonorElementsWallFunctions(CConfig *config) {
     }
 
     /* Create a cumulative version of recvCounts. */
-    for(int i=0; i<size; ++i)
-      nSearchPerRank[i+1] = nSearchPerRank[i] + recvCounts[i];
+    for (int i = 0; i < size; ++i) nSearchPerRank[i + 1] = nSearchPerRank[i] + recvCounts[i];
 
     /* Determine the number of return messages this rank has to receive.
        Use displs and recvCounts as temporary storage. */
     int nRankSend = 0;
-    for(int i=0; i<size; ++i) {
-      if( recvCounts[i] ) {recvCounts[i] = 1; ++nRankSend;}
+    for (int i = 0; i < size; ++i) {
+      if (recvCounts[i]) {
+        recvCounts[i] = 1;
+        ++nRankSend;
+      }
       displs[i] = 1;
     }
 
     int nRankRecv;
-    SU2_MPI::Reduce_scatter(recvCounts.data(), &nRankRecv, displs.data(),
-                            MPI_INT, MPI_SUM, SU2_MPI::GetComm());
+    SU2_MPI::Reduce_scatter(recvCounts.data(), &nRankRecv, displs.data(), MPI_INT, MPI_SUM, SU2_MPI::GetComm());
 
     /* Send the data using nonblocking sends to avoid deadlock. */
-    vector<SU2_MPI::Request> commReqs(3*nRankSend);
+    vector<SU2_MPI::Request> commReqs(3 * nRankSend);
     nRankSend = 0;
-    for(int i=0; i<size; ++i) {
-      if( recvCounts[i] ) {
-        const int sizeMessage = nSearchPerRank[i+1] - nSearchPerRank[i];
-        SU2_MPI::Isend(markerIDReturn.data() + nSearchPerRank[i],
-                       sizeMessage, MPI_UNSIGNED_SHORT, i, i, SU2_MPI::GetComm(),
-                       &commReqs[nRankSend++]);
-        SU2_MPI::Isend(boundaryElemIDReturn.data() + nSearchPerRank[i],
-                       sizeMessage, MPI_UNSIGNED_LONG, i, i+1, SU2_MPI::GetComm(),
-                       &commReqs[nRankSend++]);
-        SU2_MPI::Isend(volElemIDDonorReturn.data() + nSearchPerRank[i],
-                       sizeMessage, MPI_UNSIGNED_LONG, i, i+2, SU2_MPI::GetComm(),
-                       &commReqs[nRankSend++]);
+    for (int i = 0; i < size; ++i) {
+      if (recvCounts[i]) {
+        const int sizeMessage = nSearchPerRank[i + 1] - nSearchPerRank[i];
+        SU2_MPI::Isend(markerIDReturn.data() + nSearchPerRank[i], sizeMessage, MPI_UNSIGNED_SHORT, i, i,
+                       SU2_MPI::GetComm(), &commReqs[nRankSend++]);
+        SU2_MPI::Isend(boundaryElemIDReturn.data() + nSearchPerRank[i], sizeMessage, MPI_UNSIGNED_LONG, i, i + 1,
+                       SU2_MPI::GetComm(), &commReqs[nRankSend++]);
+        SU2_MPI::Isend(volElemIDDonorReturn.data() + nSearchPerRank[i], sizeMessage, MPI_UNSIGNED_LONG, i, i + 2,
+                       SU2_MPI::GetComm(), &commReqs[nRankSend++]);
       }
     }
 
     /* Loop over the number of ranks from which I receive return data. */
-    for(int i=0; i<nRankRecv; ++i) {
-
+    for (int i = 0; i < nRankRecv; ++i) {
       /* Block until a message with unsigned shorts arrives from any processor.
          Determine the source and the size of the message.   */
       SU2_MPI::Status status;
@@ -3911,25 +3735,24 @@ void CPhysicalGeometry::DetermineDonorElementsWallFunctions(CConfig *config) {
 
       /* Allocate the memory for the receive buffers. */
       vector<unsigned short> bufMarkerIDReturn(sizeMess);
-      vector<unsigned long>  bufBoundaryElemIDReturn(sizeMess);
-      vector<unsigned long>  bufVolElemIDDonorReturn(sizeMess);
+      vector<unsigned long> bufBoundaryElemIDReturn(sizeMess);
+      vector<unsigned long> bufVolElemIDDonorReturn(sizeMess);
 
       /* Receive the three messages using blocking receives. */
-      SU2_MPI::Recv(bufMarkerIDReturn.data(), sizeMess, MPI_UNSIGNED_SHORT,
-                    source, rank, SU2_MPI::GetComm(), &status);
+      SU2_MPI::Recv(bufMarkerIDReturn.data(), sizeMess, MPI_UNSIGNED_SHORT, source, rank, SU2_MPI::GetComm(), &status);
 
-      SU2_MPI::Recv(bufBoundaryElemIDReturn.data(), sizeMess, MPI_UNSIGNED_LONG,
-                    source, rank+1, SU2_MPI::GetComm(), &status);
+      SU2_MPI::Recv(bufBoundaryElemIDReturn.data(), sizeMess, MPI_UNSIGNED_LONG, source, rank + 1, SU2_MPI::GetComm(),
+                    &status);
 
-      SU2_MPI::Recv(bufVolElemIDDonorReturn.data(), sizeMess, MPI_UNSIGNED_LONG,
-                    source, rank+2, SU2_MPI::GetComm(), &status);
+      SU2_MPI::Recv(bufVolElemIDDonorReturn.data(), sizeMess, MPI_UNSIGNED_LONG, source, rank + 2, SU2_MPI::GetComm(),
+                    &status);
 
       /* Loop over the data just received and add it to the wall function
          donor information of the corresponding boundary element. */
-      for(int j=0; j<sizeMess; ++j) {
+      for (int j = 0; j < sizeMess; ++j) {
         const unsigned short iMarker = bufMarkerIDReturn[j];
-        const unsigned long  l       = bufBoundaryElemIDReturn[j];
-        const unsigned long  volID   = bufVolElemIDDonorReturn[j];
+        const unsigned long l = bufBoundaryElemIDReturn[j];
+        const unsigned long volID = bufVolElemIDDonorReturn[j];
 
         bound[iMarker][l]->AddDonorWallFunctions(volID);
       }
@@ -3945,22 +3768,20 @@ void CPhysicalGeometry::DetermineDonorElementsWallFunctions(CConfig *config) {
     /* Loop again over the boundary elements of the marker for which a wall
        function treatment must be used and make remove the multiple entries
        of the donor information. */
-    for(unsigned short iMarker=0; iMarker<nMarker; ++iMarker) {
-
+    for (unsigned short iMarker = 0; iMarker < nMarker; ++iMarker) {
       switch (config->GetMarker_All_KindBC(iMarker)) {
         case ISOTHERMAL:
         case HEAT_FLUX: {
           const string Marker_Tag = config->GetMarker_All_TagBound(iMarker);
-          if(config->GetWallFunction_Treatment(Marker_Tag) != WALL_FUNCTIONS::NONE) {
-
-            for(unsigned long l=0; l<nElem_Bound[iMarker]; ++l)
+          if (config->GetWallFunction_Treatment(Marker_Tag) != WALL_FUNCTIONS::NONE) {
+            for (unsigned long l = 0; l < nElem_Bound[iMarker]; ++l)
               bound[iMarker][l]->RemoveMultipleDonorsWallFunctions();
           }
 
           break;
         }
 
-        default:  /* Just to avoid a compiler warning. */
+        default: /* Just to avoid a compiler warning. */
           break;
       }
     }
@@ -3969,30 +3790,24 @@ void CPhysicalGeometry::DetermineDonorElementsWallFunctions(CConfig *config) {
 #endif
 }
 
-void CPhysicalGeometry::DetermineTimeLevelElements(
-                          CConfig                              *config,
-                          const vector<CFaceOfElement>         &localFaces,
-                          map<unsigned long, CUnsignedShort2T> &mapExternalElemIDToTimeLevel) {
-
+void CPhysicalGeometry::DetermineTimeLevelElements(CConfig* config, const vector<CFaceOfElement>& localFaces,
+                                                   map<unsigned long, CUnsignedShort2T>& mapExternalElemIDToTimeLevel) {
   /*--------------------------------------------------------------------------*/
   /*--- Step 1: Initialize the map mapExternalElemIDToTimeLevel.           ---*/
   /*--------------------------------------------------------------------------*/
 
   /*--- Initialize the time level of external elements to zero.
         First the externals from the faces. ---*/
-  for(vector<CFaceOfElement>::const_iterator FI =localFaces.begin();
-                                             FI!=localFaces.end(); ++FI) {
-    if(FI->elemID1 < Global_nElem) {     // Safeguard against non-matching faces.
-
-      if(FI->elemID1 <  beg_node[rank] ||
-         FI->elemID1 >= beg_node[rank]+nElem) {
+  for (vector<CFaceOfElement>::const_iterator FI = localFaces.begin(); FI != localFaces.end(); ++FI) {
+    if (FI->elemID1 < Global_nElem) {  // Safeguard against non-matching faces.
 
+      if (FI->elemID1 < beg_node[rank] || FI->elemID1 >= beg_node[rank] + nElem) {
         /* This element is an external element. Store it in the map
            mapExternalElemIDToTimeLevel if not already done so. */
-        map<unsigned long,CUnsignedShort2T>::iterator MI;
+        map<unsigned long, CUnsignedShort2T>::iterator MI;
         MI = mapExternalElemIDToTimeLevel.find(FI->elemID1);
-        if(MI == mapExternalElemIDToTimeLevel.end())
-          mapExternalElemIDToTimeLevel[FI->elemID1] = CUnsignedShort2T(0,0);
+        if (MI == mapExternalElemIDToTimeLevel.end())
+          mapExternalElemIDToTimeLevel[FI->elemID1] = CUnsignedShort2T(0, 0);
       }
     }
   }
@@ -4006,40 +3821,36 @@ void CPhysicalGeometry::DetermineTimeLevelElements(
 
   /*--- Add the externals from the wall function donors. Loop over the
         boundary elements of all markers. ---*/
-  for(unsigned short iMarker=0; iMarker<nMarker; ++iMarker) {
-    for(unsigned long l=0; l<nElem_Bound[iMarker]; ++l) {
-
+  for (unsigned short iMarker = 0; iMarker < nMarker; ++iMarker) {
+    for (unsigned long l = 0; l < nElem_Bound[iMarker]; ++l) {
       /* Get the number of donor elements for the wall function treatment
          and the pointer to the array which stores this info. */
       const unsigned short nDonors = bound[iMarker][l]->GetNDonorsWallFunctions();
-      const unsigned long  *donors = bound[iMarker][l]->GetDonorsWallFunctions();
+      const unsigned long* donors = bound[iMarker][l]->GetDonorsWallFunctions();
 
       /* Loop over the number of donors and add the externals to
          mapExternalElemIDToTimeLevel, if not already present. */
-      for(unsigned short i=0; i<nDonors; ++i) {
-
-        if(donors[i] <  beg_node[rank] ||
-           donors[i] >= beg_node[rank]+nElem) {
-
-          map<unsigned long,CUnsignedShort2T>::iterator MI;
+      for (unsigned short i = 0; i < nDonors; ++i) {
+        if (donors[i] < beg_node[rank] || donors[i] >= beg_node[rank] + nElem) {
+          map<unsigned long, CUnsignedShort2T>::iterator MI;
           MI = mapExternalElemIDToTimeLevel.find(donors[i]);
-          if(MI == mapExternalElemIDToTimeLevel.end()) {
-
+          if (MI == mapExternalElemIDToTimeLevel.end()) {
             /* Element not present in external. Add it. */
-            mapExternalElemIDToTimeLevel[donors[i]] = CUnsignedShort2T(0,0);
+            mapExternalElemIDToTimeLevel[donors[i]] = CUnsignedShort2T(0, 0);
           }
 
           /* The reverse connection may not be present either. Store the global
              ID of this element in the send buffers for the additional
              externals. */
           int rankDonor;
-          if(donors[i] >= beg_node[size-1]) rankDonor = size-1;
+          if (donors[i] >= beg_node[size - 1])
+            rankDonor = size - 1;
           else {
-            const unsigned long *low;
-            low = lower_bound(beg_node, beg_node+size, donors[i]);
+            const unsigned long* low;
+            low = lower_bound(beg_node, beg_node + size, donors[i]);
 
             rankDonor = (int)(low - beg_node);
-            if(*low > donors[i]) --rankDonor;
+            if (*low > donors[i]) --rankDonor;
           }
 
           sendBufAddExternals[rankDonor].push_back(bound[iMarker][l]->GetDomainElement());
@@ -4055,33 +3866,29 @@ void CPhysicalGeometry::DetermineTimeLevelElements(
      externals to be stored. */
   int nRankRecv;
   vector<int> sizeSend(size, 1);
-  SU2_MPI::Reduce_scatter(recvFromRank.data(), &nRankRecv, sizeSend.data(),
-                          MPI_INT, MPI_SUM, SU2_MPI::GetComm());
+  SU2_MPI::Reduce_scatter(recvFromRank.data(), &nRankRecv, sizeSend.data(), MPI_INT, MPI_SUM, SU2_MPI::GetComm());
 
   /* Determine the number of messages this rank will send. */
   int nRankSend = 0;
-  for(int i=0; i<size; ++i)
-    nRankSend += recvFromRank[i];
+  for (int i = 0; i < size; ++i) nRankSend += recvFromRank[i];
 
   /* Send the data using non-blocking sends to avoid deadlock. */
   vector<SU2_MPI::Request> sendReqs(nRankSend);
   nRankSend = 0;
-  for(int i=0; i<size; ++i) {
-    if( recvFromRank[i] ) {
+  for (int i = 0; i < size; ++i) {
+    if (recvFromRank[i]) {
       sort(sendBufAddExternals[i].begin(), sendBufAddExternals[i].end());
-      vector<unsigned long>::iterator lastElem = unique(sendBufAddExternals[i].begin(),
-                                                        sendBufAddExternals[i].end());
+      vector<unsigned long>::iterator lastElem = unique(sendBufAddExternals[i].begin(), sendBufAddExternals[i].end());
       sendBufAddExternals[i].erase(lastElem, sendBufAddExternals[i].end());
 
-      SU2_MPI::Isend(sendBufAddExternals[i].data(), sendBufAddExternals[i].size(),
-                     MPI_UNSIGNED_LONG, i, i, SU2_MPI::GetComm(), &sendReqs[nRankSend++]);
+      SU2_MPI::Isend(sendBufAddExternals[i].data(), sendBufAddExternals[i].size(), MPI_UNSIGNED_LONG, i, i,
+                     SU2_MPI::GetComm(), &sendReqs[nRankSend++]);
     }
   }
 
   /* Loop over the number of ranks from which this rank will receive data
      to be stored in mapExternalElemIDToTimeLevel. */
-  for(int i=0; i<nRankRecv; ++i) {
-
+  for (int i = 0; i < nRankRecv; ++i) {
     /* Block until a message arrives and determine the source and size
        of the message. Allocate the memory for a receive buffer. */
     SU2_MPI::Status status;
@@ -4092,16 +3899,14 @@ void CPhysicalGeometry::DetermineTimeLevelElements(
     SU2_MPI::Get_count(&status, MPI_UNSIGNED_LONG, &sizeMess);
     vector<unsigned long> recvBuf(sizeMess);
 
-    SU2_MPI::Recv(recvBuf.data(), sizeMess, MPI_UNSIGNED_LONG,
-                  source, rank, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Recv(recvBuf.data(), sizeMess, MPI_UNSIGNED_LONG, source, rank, SU2_MPI::GetComm(), &status);
 
     /* Loop over the entries of recvBuf and add them to
        mapExternalElemIDToTimeLevel, if not present already. */
-    for(int j=0; j<sizeMess; ++j) {
-      map<unsigned long,CUnsignedShort2T>::iterator MI;
+    for (int j = 0; j < sizeMess; ++j) {
+      map<unsigned long, CUnsignedShort2T>::iterator MI;
       MI = mapExternalElemIDToTimeLevel.find(recvBuf[j]);
-      if(MI == mapExternalElemIDToTimeLevel.end())
-        mapExternalElemIDToTimeLevel[recvBuf[j]] = CUnsignedShort2T(0,0);
+      if (MI == mapExternalElemIDToTimeLevel.end()) mapExternalElemIDToTimeLevel[recvBuf[j]] = CUnsignedShort2T(0, 0);
     }
   }
 
@@ -4120,64 +3925,57 @@ void CPhysicalGeometry::DetermineTimeLevelElements(
         time accurate local time stepping is used. ---*/
   const unsigned short nTimeLevels = config->GetnLevels_TimeAccurateLTS();
 
-  if(nTimeLevels == 1) {
-
+  if (nTimeLevels == 1) {
     /*--- No time accurate local time stepping. Set the time level of
           all elements to zero. ---*/
-    for(unsigned long i=0; i<nElem; ++i)
-      elem[i]->SetTimeLevel(0);
-  }
-  else {
-
+    for (unsigned long i = 0; i < nElem; ++i) elem[i]->SetTimeLevel(0);
+  } else {
     /*--- Time accurate local time stepping is used. The estimate of the time
           step is based on free stream values at the moment, but this is easy
           to change, if needed. ---*/
-    const su2double Gamma   = config->GetGamma();
+    const su2double Gamma = config->GetGamma();
     const su2double Prandtl = config->GetPrandtl_Lam();
 
-    const su2double Density   = config->GetDensity_FreeStreamND();
-    const su2double *Vel      = config->GetVelocity_FreeStreamND();
+    const su2double Density = config->GetDensity_FreeStreamND();
+    const su2double* Vel = config->GetVelocity_FreeStreamND();
     const su2double Viscosity = config->GetViscosity_FreeStreamND();
 
     su2double VelMag = 0.0;
-    for(unsigned short iDim=0; iDim<nDim; ++iDim)
-      VelMag += Vel[iDim]*Vel[iDim];
+    for (unsigned short iDim = 0; iDim < nDim; ++iDim) VelMag += Vel[iDim] * Vel[iDim];
     VelMag = sqrt(VelMag);
 
-    const su2double SoundSpeed = VelMag/config->GetMach();
+    const su2double SoundSpeed = VelMag / config->GetMach();
 
     /* In the estimate of the time step the spectral radius of the inviscid terms is
        needed. As the current estimate is based on the free stream, the value of this
        spectral radius can be computed beforehand. Note that this is a rather
        conservative estimate. */
     su2double charVel2 = 0.0;
-    for(unsigned short iDim=0; iDim<nDim; ++iDim) {
+    for (unsigned short iDim = 0; iDim < nDim; ++iDim) {
       const su2double rad = fabs(Vel[iDim]) + SoundSpeed;
-      charVel2 += rad*rad;
+      charVel2 += rad * rad;
     }
 
     const su2double charVel = sqrt(charVel2);
 
     /* Also the viscous contribution to the time step is constant. Compute it. */
-    const su2double factHeatFlux  =  Gamma/Prandtl;
-    const su2double lambdaOverMu  = -TWO3;
-    const su2double radVisc       =  max(max(1.0, 2.0+lambdaOverMu),factHeatFlux)
-                                  *  Viscosity/Density;
+    const su2double factHeatFlux = Gamma / Prandtl;
+    const su2double lambdaOverMu = -TWO3;
+    const su2double radVisc = max(max(1.0, 2.0 + lambdaOverMu), factHeatFlux) * Viscosity / Density;
 
     /*--- Allocate the memory for time step estimate of the local elements and
           determine the values. Also keep track of the minimum value. ---*/
     su2double minDeltaT = 1.e25;
     vector<su2double> timeStepElements(nElem);
 
-    for(unsigned long i=0; i<nElem; ++i) {
-
+    for (unsigned long i = 0; i < nElem; ++i) {
       unsigned short nPoly = elem[i]->GetNPolySol();
-      if(nPoly == 0) nPoly = 1;
-      const su2double lenScaleInv = nPoly/elem[i]->GetLengthScale();
-      const su2double lenScale    = 1.0/lenScaleInv;
+      if (nPoly == 0) nPoly = 1;
+      const su2double lenScaleInv = nPoly / elem[i]->GetLengthScale();
+      const su2double lenScale = 1.0 / lenScaleInv;
 
-      timeStepElements[i] = lenScale/(charVel + lenScaleInv*radVisc);
-      minDeltaT           = min(minDeltaT, timeStepElements[i]);
+      timeStepElements[i] = lenScale / (charVel + lenScaleInv * radVisc);
+      minDeltaT = min(minDeltaT, timeStepElements[i]);
     }
 
     /* Determine the minimum value of all elements in the grid.
@@ -4188,12 +3986,12 @@ void CPhysicalGeometry::DetermineTimeLevelElements(
 #endif
 
     /* Initial estimate of the time level of the owned elements. */
-    for(unsigned long i=0; i<nElem; ++i) {
+    for (unsigned long i = 0; i < nElem; ++i) {
       unsigned short timeLevel;
       su2double deltaT = minDeltaT;
-      for(timeLevel=0; timeLevel<(nTimeLevels-1); ++timeLevel) {
+      for (timeLevel = 0; timeLevel < (nTimeLevels - 1); ++timeLevel) {
         deltaT *= 2;
-        if(timeStepElements[i] < deltaT) break;
+        if (timeStepElements[i] < deltaT) break;
       }
 
       elem[i]->SetTimeLevel(timeLevel);
@@ -4205,35 +4003,34 @@ void CPhysicalGeometry::DetermineTimeLevelElements(
   /*---         of the external element data.                              ---*/
   /*--------------------------------------------------------------------------*/
 
-  map<unsigned long,CUnsignedShort2T>::iterator MI;
+  map<unsigned long, CUnsignedShort2T>::iterator MI;
 #ifdef HAVE_MPI
 
   /*--- Determine the ranks from which I receive element data during
         the actual exchange. ---*/
   recvFromRank.assign(size, 0);
 
-  for(MI =mapExternalElemIDToTimeLevel.begin();
-      MI!=mapExternalElemIDToTimeLevel.end(); ++MI) {
-
+  for (MI = mapExternalElemIDToTimeLevel.begin(); MI != mapExternalElemIDToTimeLevel.end(); ++MI) {
     /* Determine the rank where this external is stored. */
     const unsigned long elemID = MI->first;
     int rankElem;
-    if(elemID >= beg_node[size-1]) rankElem = size-1;
+    if (elemID >= beg_node[size - 1])
+      rankElem = size - 1;
     else {
-      const unsigned long *low;
-      low = lower_bound(beg_node, beg_node+size, elemID);
+      const unsigned long* low;
+      low = lower_bound(beg_node, beg_node + size, elemID);
 
       rankElem = low - beg_node;
-      if(*low > elemID) --rankElem;
+      if (*low > elemID) --rankElem;
     }
 
     /* Set the corresponding index of recvFromRank to 1. */
     recvFromRank[rankElem] = 1;
   }
 
-  map<int,int> mapRankToIndRecv;
-  for(int i=0; i<size; ++i) {
-    if( recvFromRank[i] ) {
+  map<int, int> mapRankToIndRecv;
+  for (int i = 0; i < size; ++i) {
+    if (recvFromRank[i]) {
       int ind = mapRankToIndRecv.size();
       mapRankToIndRecv[i] = ind;
     }
@@ -4242,28 +4039,26 @@ void CPhysicalGeometry::DetermineTimeLevelElements(
   /* Determine the number of ranks from which I will receive data and to
      which I will send data. */
   nRankRecv = mapRankToIndRecv.size();
-  SU2_MPI::Reduce_scatter(recvFromRank.data(), &nRankSend, sizeSend.data(),
-                          MPI_INT, MPI_SUM, SU2_MPI::GetComm());
+  SU2_MPI::Reduce_scatter(recvFromRank.data(), &nRankSend, sizeSend.data(), MPI_INT, MPI_SUM, SU2_MPI::GetComm());
 
   /*--- Create the vector of vectors of the global element ID's that
         will be received from other ranks. ---*/
   vector<vector<unsigned long> > recvElem(nRankRecv, vector<unsigned long>(0));
 
-  for(MI =mapExternalElemIDToTimeLevel.begin();
-      MI!=mapExternalElemIDToTimeLevel.end(); ++MI) {
-
+  for (MI = mapExternalElemIDToTimeLevel.begin(); MI != mapExternalElemIDToTimeLevel.end(); ++MI) {
     const unsigned long elemID = MI->first;
     int rankElem;
-    if(elemID >= beg_node[size-1]) rankElem = size-1;
+    if (elemID >= beg_node[size - 1])
+      rankElem = size - 1;
     else {
-      const unsigned long *low;
-      low = lower_bound(beg_node, beg_node+size, elemID);
+      const unsigned long* low;
+      low = lower_bound(beg_node, beg_node + size, elemID);
 
       rankElem = low - beg_node;
-      if(*low > elemID) --rankElem;
+      if (*low > elemID) --rankElem;
     }
 
-    map<int,int>::const_iterator MRI = mapRankToIndRecv.find(rankElem);
+    map<int, int>::const_iterator MRI = mapRankToIndRecv.find(rankElem);
     recvElem[MRI->second].push_back(elemID);
   }
 
@@ -4271,17 +4066,15 @@ void CPhysicalGeometry::DetermineTimeLevelElements(
         exchange and send over the global element ID's. In order to avoid
         unnecessary communication, multiple entries are filtered out. ---*/
   sendReqs.resize(nRankRecv);
-  map<int,int>::const_iterator MRI = mapRankToIndRecv.begin();
-
-  for(int i=0; i<nRankRecv; ++i, ++MRI) {
+  map<int, int>::const_iterator MRI = mapRankToIndRecv.begin();
 
+  for (int i = 0; i < nRankRecv; ++i, ++MRI) {
     sort(recvElem[i].begin(), recvElem[i].end());
-    vector<unsigned long>::iterator lastElem = unique(recvElem[i].begin(),
-                                                      recvElem[i].end());
+    vector<unsigned long>::iterator lastElem = unique(recvElem[i].begin(), recvElem[i].end());
     recvElem[i].erase(lastElem, recvElem[i].end());
 
-    SU2_MPI::Isend(recvElem[i].data(), recvElem[i].size(), MPI_UNSIGNED_LONG,
-                   MRI->first, MRI->first, SU2_MPI::GetComm(), &sendReqs[i]);
+    SU2_MPI::Isend(recvElem[i].data(), recvElem[i].size(), MPI_UNSIGNED_LONG, MRI->first, MRI->first,
+                   SU2_MPI::GetComm(), &sendReqs[i]);
   }
 
   /*--- Receive the messages in arbitrary sequence and store the requested
@@ -4290,8 +4083,7 @@ void CPhysicalGeometry::DetermineTimeLevelElements(
   vector<vector<unsigned long> > sendElem(nRankSend, vector<unsigned long>(0));
   vector<int> sendRank(nRankSend);
 
-  for(int i=0; i<nRankSend; ++i) {
-
+  for (int i = 0; i < nRankSend; ++i) {
     SU2_MPI::Status status;
     SU2_MPI::Probe(MPI_ANY_SOURCE, rank, SU2_MPI::GetComm(), &status);
     sendRank[i] = status.MPI_SOURCE;
@@ -4300,11 +4092,9 @@ void CPhysicalGeometry::DetermineTimeLevelElements(
     SU2_MPI::Get_count(&status, MPI_UNSIGNED_LONG, &sizeMess);
     sendElem[i].resize(sizeMess);
 
-    SU2_MPI::Recv(sendElem[i].data(), sizeMess, MPI_UNSIGNED_LONG,
-                  sendRank[i], rank, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Recv(sendElem[i].data(), sizeMess, MPI_UNSIGNED_LONG, sendRank[i], rank, SU2_MPI::GetComm(), &status);
 
-    for(int j=0; j<sizeMess; ++j)
-      sendElem[i][j] -= beg_node[rank];
+    for (int j = 0; j < sizeMess; ++j) sendElem[i][j] -= beg_node[rank];
   }
 
   /* Complete the non-blocking sends. Synchronize the processors afterwards,
@@ -4331,16 +4121,15 @@ void CPhysicalGeometry::DetermineTimeLevelElements(
 
   /*--- Copy the information of the time level and number of DOFs into the
         send buffers and send the data using non-blocking sends. ---*/
-  for(int i=0; i<nRankSend; ++i) {
-
-    sendBuf[i].resize(2*sendElem[i].size());
-    for(unsigned long j=0; j<sendElem[i].size(); ++j) {
-      sendBuf[i][2*j]   = elem[sendElem[i][j]]->GetTimeLevel();
-      sendBuf[i][2*j+1] = elem[sendElem[i][j]]->GetNDOFsSol();
+  for (int i = 0; i < nRankSend; ++i) {
+    sendBuf[i].resize(2 * sendElem[i].size());
+    for (unsigned long j = 0; j < sendElem[i].size(); ++j) {
+      sendBuf[i][2 * j] = elem[sendElem[i][j]]->GetTimeLevel();
+      sendBuf[i][2 * j + 1] = elem[sendElem[i][j]]->GetNDOFsSol();
     }
 
-    SU2_MPI::Isend(sendBuf[i].data(), sendBuf[i].size(), MPI_UNSIGNED_SHORT,
-                   sendRank[i], sendRank[i], SU2_MPI::GetComm(), &sendReqs[i]);
+    SU2_MPI::Isend(sendBuf[i].data(), sendBuf[i].size(), MPI_UNSIGNED_SHORT, sendRank[i], sendRank[i],
+                   SU2_MPI::GetComm(), &sendReqs[i]);
   }
 
   /*--- Receive the data for the externals. As this data is needed immediately,
@@ -4348,19 +4137,18 @@ void CPhysicalGeometry::DetermineTimeLevelElements(
         of the externals is stored in the second entry of the
         mapExternalElemIDToTimeLevel, which is set accordingly. ---*/
   MRI = mapRankToIndRecv.begin();
-  for(int i=0; i<nRankRecv; ++i, ++MRI) {
-
-    returnBuf[i].resize(2*recvElem[i].size());
+  for (int i = 0; i < nRankRecv; ++i, ++MRI) {
+    returnBuf[i].resize(2 * recvElem[i].size());
     SU2_MPI::Status status;
-    SU2_MPI::Recv(returnBuf[i].data(), returnBuf[i].size(), MPI_UNSIGNED_SHORT,
-                  MRI->first, rank, SU2_MPI::GetComm(), &status);
+    SU2_MPI::Recv(returnBuf[i].data(), returnBuf[i].size(), MPI_UNSIGNED_SHORT, MRI->first, rank, SU2_MPI::GetComm(),
+                  &status);
 
-    for(unsigned long j=0; j<recvElem[i].size(); ++j) {
+    for (unsigned long j = 0; j < recvElem[i].size(); ++j) {
       MI = mapExternalElemIDToTimeLevel.find(recvElem[i][j]);
-      if(MI == mapExternalElemIDToTimeLevel.end())
+      if (MI == mapExternalElemIDToTimeLevel.end())
         SU2_MPI::Error("Entry not found in mapExternalElemIDToTimeLevel", CURRENT_FUNCTION);
-      MI->second.short0 = returnBuf[i][2*j];
-      MI->second.short1 = returnBuf[i][2*j+1];
+      MI->second.short0 = returnBuf[i][2 * j];
+      MI->second.short1 = returnBuf[i][2 * j + 1];
     }
   }
 
@@ -4382,11 +4170,9 @@ void CPhysicalGeometry::DetermineTimeLevelElements(
   /*--------------------------------------------------------------------------*/
 
   /* Test for time accurate local time stepping. */
-  if(nTimeLevels > 1) {
-
+  if (nTimeLevels > 1) {
     /* Infinite loop for the iterative algorithm. */
-    for(;;) {
-
+    for (;;) {
       /* Variable to indicate whether the local situation has changed. */
       unsigned short localSituationChanged = 0;
 
@@ -4396,66 +4182,58 @@ void CPhysicalGeometry::DetermineTimeLevelElements(
             restriction, because in the vast majority of cases, the donor
             element is this adjacent element itself. Requiring it to be the
             same makes the implementation of the wall functions easier. ---*/
-      for(unsigned short iMarker=0; iMarker<nMarker; ++iMarker) {
-        for(unsigned long l=0; l<nElem_Bound[iMarker]; ++l) {
-
+      for (unsigned short iMarker = 0; iMarker < nMarker; ++iMarker) {
+        for (unsigned long l = 0; l < nElem_Bound[iMarker]; ++l) {
           /* Determine the ID of the adjacent element. */
-          const unsigned long elemID = bound[iMarker][l]->GetDomainElement()
-                                     - beg_node[rank];
+          const unsigned long elemID = bound[iMarker][l]->GetDomainElement() - beg_node[rank];
 
           /* Get the number of donor elements for the wall function treatment
              and the pointer to the array which stores this info. */
           const unsigned short nDonors = bound[iMarker][l]->GetNDonorsWallFunctions();
-          const unsigned long  *donors = bound[iMarker][l]->GetDonorsWallFunctions();
+          const unsigned long* donors = bound[iMarker][l]->GetDonorsWallFunctions();
 
           /* Loop over the number of donors and check the time levels. */
-          for(unsigned short i=0; i<nDonors; ++i) {
-
+          for (unsigned short i = 0; i < nDonors; ++i) {
             /* Determine the status of the donor element. */
-            if(donors[i] >= beg_node[rank] &&
-               donors[i] <  beg_node[rank]+nElem) {
-
+            if (donors[i] >= beg_node[rank] && donors[i] < beg_node[rank] + nElem) {
               /* Donor is stored locally. Determine its local ID and
                  get the time levels of both elements. */
-              const unsigned long  donorID    = donors[i] - beg_node[rank];
+              const unsigned long donorID = donors[i] - beg_node[rank];
               const unsigned short timeLevelB = elem[elemID]->GetTimeLevel();
               const unsigned short timeLevelD = elem[donorID]->GetTimeLevel();
-              const unsigned short timeLevel  = min(timeLevelB, timeLevelD);
+              const unsigned short timeLevel = min(timeLevelB, timeLevelD);
 
               /* If the time level of either element is larger than timeLevel,
                  adapt the time levels and indicate that the local situation
                  has changed. */
-              if(timeLevelB > timeLevel) {
+              if (timeLevelB > timeLevel) {
                 elem[elemID]->SetTimeLevel(timeLevel);
                 localSituationChanged = 1;
               }
 
-              if(timeLevelD > timeLevel) {
+              if (timeLevelD > timeLevel) {
                 elem[donorID]->SetTimeLevel(timeLevel);
                 localSituationChanged = 1;
               }
-            }
-            else {
-
+            } else {
               /* The donor element is stored on a different processor.
                  Retrieve its time level from mapExternalElemIDToTimeLevel
                  and determine the minimum time level. */
               const unsigned short timeLevelB = elem[elemID]->GetTimeLevel();
               MI = mapExternalElemIDToTimeLevel.find(donors[i]);
-              if(MI == mapExternalElemIDToTimeLevel.end())
-                SU2_MPI::Error("Entry not found in mapExternalElemIDToTimeLevel",
-                               CURRENT_FUNCTION);
+              if (MI == mapExternalElemIDToTimeLevel.end())
+                SU2_MPI::Error("Entry not found in mapExternalElemIDToTimeLevel", CURRENT_FUNCTION);
               const unsigned short timeLevel = min(timeLevelB, MI->second.short0);
 
               /* If the time level of either element is larger than timeLevel,
                  adapt the time levels and indicate that the local situation
                  has changed. */
-              if(timeLevelB > timeLevel) {
+              if (timeLevelB > timeLevel) {
                 elem[elemID]->SetTimeLevel(timeLevel);
                 localSituationChanged = 1;
               }
 
-              if(MI->second.short0 > timeLevel) {
+              if (MI->second.short0 > timeLevel) {
                 MI->second.short0 = timeLevel;
                 localSituationChanged = 1;
               }
@@ -4466,61 +4244,54 @@ void CPhysicalGeometry::DetermineTimeLevelElements(
 
       /*--- Loop over the matching faces and update the time levels of the
             adjacent elements, if needed. ---*/
-      for(vector<CFaceOfElement>::const_iterator FI =localFaces.begin();
-                                                 FI!=localFaces.end(); ++FI) {
+      for (vector<CFaceOfElement>::const_iterator FI = localFaces.begin(); FI != localFaces.end(); ++FI) {
         /* Safeguard against non-matching faces. */
-        if(FI->elemID1 < Global_nElem) {
-
+        if (FI->elemID1 < Global_nElem) {
           /* Local element ID of the first element. Per definition this is
              always a locally stored element. Also store its time level. */
-          const unsigned long  elemID0    = FI->elemID0 - beg_node[rank];
+          const unsigned long elemID0 = FI->elemID0 - beg_node[rank];
           const unsigned short timeLevel0 = elem[elemID0]->GetTimeLevel();
 
           /* Determine the status of the second element. */
-          if(FI->elemID1 >= beg_node[rank] &&
-             FI->elemID1 <  beg_node[rank]+nElem) {
-
+          if (FI->elemID1 >= beg_node[rank] && FI->elemID1 < beg_node[rank] + nElem) {
             /* Both elements are stored locally. Determine the local
                element of the second element and determine the minimum
                time level. */
-            const unsigned long  elemID1    = FI->elemID1 - beg_node[rank];
+            const unsigned long elemID1 = FI->elemID1 - beg_node[rank];
             const unsigned short timeLevel1 = elem[elemID1]->GetTimeLevel();
-            const unsigned short timeLevel  = min(timeLevel0, timeLevel1);
+            const unsigned short timeLevel = min(timeLevel0, timeLevel1);
 
             /* If the time level of either element is larger than timeLevel+1,
                adapt the time levels and indicate that the local situation
                has changed. */
-            if(timeLevel0 > timeLevel+1) {
-              elem[elemID0]->SetTimeLevel(timeLevel+1);
+            if (timeLevel0 > timeLevel + 1) {
+              elem[elemID0]->SetTimeLevel(timeLevel + 1);
               localSituationChanged = 1;
             }
 
-            if(timeLevel1 > timeLevel+1) {
-              elem[elemID1]->SetTimeLevel(timeLevel+1);
+            if (timeLevel1 > timeLevel + 1) {
+              elem[elemID1]->SetTimeLevel(timeLevel + 1);
               localSituationChanged = 1;
             }
-          }
-          else {
-
+          } else {
             /* The second element is stored on a different processor.
                Retrieve its time level from mapExternalElemIDToTimeLevel
                and determine the minimum time level. */
             MI = mapExternalElemIDToTimeLevel.find(FI->elemID1);
-            if(MI == mapExternalElemIDToTimeLevel.end())
-              SU2_MPI::Error("Entry not found in mapExternalElemIDToTimeLevel",
-                             CURRENT_FUNCTION);
+            if (MI == mapExternalElemIDToTimeLevel.end())
+              SU2_MPI::Error("Entry not found in mapExternalElemIDToTimeLevel", CURRENT_FUNCTION);
             const unsigned short timeLevel = min(timeLevel0, MI->second.short0);
 
             /* If the time level of either element is larger than timeLevel+1,
                adapt the time levels and indicate that the local situation
                has changed. */
-            if(timeLevel0 > timeLevel+1) {
-              elem[elemID0]->SetTimeLevel(timeLevel+1);
+            if (timeLevel0 > timeLevel + 1) {
+              elem[elemID0]->SetTimeLevel(timeLevel + 1);
               localSituationChanged = 1;
             }
 
-            if(MI->second.short0 > timeLevel+1) {
-              MI->second.short0 = timeLevel+1;
+            if (MI->second.short0 > timeLevel + 1) {
+              MI->second.short0 = timeLevel + 1;
               localSituationChanged = 1;
             }
           }
@@ -4532,25 +4303,23 @@ void CPhysicalGeometry::DetermineTimeLevelElements(
       unsigned short globalSituationChanged = localSituationChanged;
 
 #ifdef HAVE_MPI
-      SU2_MPI::Allreduce(&localSituationChanged, &globalSituationChanged,
-                         1, MPI_UNSIGNED_SHORT, MPI_MAX, SU2_MPI::GetComm());
+      SU2_MPI::Allreduce(&localSituationChanged, &globalSituationChanged, 1, MPI_UNSIGNED_SHORT, MPI_MAX,
+                         SU2_MPI::GetComm());
 #endif
-      if( !globalSituationChanged ) break;
+      if (!globalSituationChanged) break;
 
-      /*--- Communicate the information of the externals, if needed. ---*/
+        /*--- Communicate the information of the externals, if needed. ---*/
 #ifdef HAVE_MPI
 
       /*--- Copy the information of the time level into the send buffers
             and send the data using non-blocking sends. Note that the size
             of sendElem is used and not sendBuf, because the size of sendBuf
             is twice the size, see step 4.  ---*/
-      for(int i=0; i<nRankSend; ++i) {
+      for (int i = 0; i < nRankSend; ++i) {
+        for (unsigned long j = 0; j < sendElem[i].size(); ++j) sendBuf[i][j] = elem[sendElem[i][j]]->GetTimeLevel();
 
-        for(unsigned long j=0; j<sendElem[i].size(); ++j)
-          sendBuf[i][j] = elem[sendElem[i][j]]->GetTimeLevel();
-
-        SU2_MPI::Isend(sendBuf[i].data(), sendElem[i].size(), MPI_UNSIGNED_SHORT,
-                       sendRank[i], sendRank[i], SU2_MPI::GetComm(), &sendReqs[i]);
+        SU2_MPI::Isend(sendBuf[i].data(), sendElem[i].size(), MPI_UNSIGNED_SHORT, sendRank[i], sendRank[i],
+                       SU2_MPI::GetComm(), &sendReqs[i]);
       }
 
       /*--- Receive the data for the externals. As this data is needed
@@ -4563,22 +4332,21 @@ void CPhysicalGeometry::DetermineTimeLevelElements(
             of recvElem is used and not returnBuf, because the latter is twice
             as large, see step 4. ---*/
       MRI = mapRankToIndRecv.begin();
-      for(int i=0; i<nRankRecv; ++i, ++MRI) {
-
+      for (int i = 0; i < nRankRecv; ++i, ++MRI) {
         SU2_MPI::Status status;
-        SU2_MPI::Recv(returnBuf[i].data(), recvElem[i].size(), MPI_UNSIGNED_SHORT,
-                      MRI->first, rank, SU2_MPI::GetComm(), &status);
+        SU2_MPI::Recv(returnBuf[i].data(), recvElem[i].size(), MPI_UNSIGNED_SHORT, MRI->first, rank, SU2_MPI::GetComm(),
+                      &status);
 
-        for(unsigned long j=0; j<recvElem[i].size(); ++j) {
+        for (unsigned long j = 0; j < recvElem[i].size(); ++j) {
           MI = mapExternalElemIDToTimeLevel.find(recvElem[i][j]);
-          if(MI == mapExternalElemIDToTimeLevel.end())
+          if (MI == mapExternalElemIDToTimeLevel.end())
             SU2_MPI::Error("Entry not found in mapExternalElemIDToTimeLevel", CURRENT_FUNCTION);
           MI->second.short0 = min(returnBuf[i][j], MI->second.short0);
-          returnBuf[i][j]   = MI->second.short0;
+          returnBuf[i][j] = MI->second.short0;
         }
 
-        SU2_MPI::Isend(returnBuf[i].data(), recvElem[i].size(), MPI_UNSIGNED_SHORT,
-                       MRI->first, MRI->first+1, SU2_MPI::GetComm(), &returnReqs[i]);
+        SU2_MPI::Isend(returnBuf[i].data(), recvElem[i].size(), MPI_UNSIGNED_SHORT, MRI->first, MRI->first + 1,
+                       SU2_MPI::GetComm(), &returnReqs[i]);
       }
 
       /* Complete the first round of nonblocking sends, such that the
@@ -4589,14 +4357,12 @@ void CPhysicalGeometry::DetermineTimeLevelElements(
       /* Loop again over the original sending processors to receive
          the updated time level of elements that may have been updated
          on other ranks. */
-      for(int i=0; i<nRankSend; ++i) {
-
+      for (int i = 0; i < nRankSend; ++i) {
         SU2_MPI::Status status;
-        SU2_MPI::Recv(sendBuf[i].data(), sendElem[i].size(), MPI_UNSIGNED_SHORT,
-                      sendRank[i], rank+1, SU2_MPI::GetComm(), &status);
+        SU2_MPI::Recv(sendBuf[i].data(), sendElem[i].size(), MPI_UNSIGNED_SHORT, sendRank[i], rank + 1,
+                      SU2_MPI::GetComm(), &status);
 
-        for(unsigned long j=0; j<sendElem[i].size(); ++j)
-          elem[sendElem[i][j]]->SetTimeLevel(sendBuf[i][j]);
+        for (unsigned long j = 0; j < sendElem[i].size(); ++j) elem[sendElem[i][j]]->SetTimeLevel(sendBuf[i][j]);
       }
 
       /* Complete the second round of nonblocking sends. */
@@ -4609,52 +4375,43 @@ void CPhysicalGeometry::DetermineTimeLevelElements(
     /*---         time level.                                              ---*/
     /*------------------------------------------------------------------------*/
 
-    if(rank == MASTER_NODE)
-      cout << endl <<"------- Element distribution for time accurate local time stepping ------" << endl;
+    if (rank == MASTER_NODE)
+      cout << endl << "------- Element distribution for time accurate local time stepping ------" << endl;
 
     /* Determine the local number of elements per time level. */
     vector<unsigned long> nLocalElemPerLevel(nTimeLevels, 0);
-    for(unsigned long i=0; i<nElem; ++i)
-      ++nLocalElemPerLevel[elem[i]->GetTimeLevel()];
+    for (unsigned long i = 0; i < nElem; ++i) ++nLocalElemPerLevel[elem[i]->GetTimeLevel()];
 
     /* Determine the global version of nLocalElemPerLevel. This only needs to
        be known on the master node. */
     vector<unsigned long> nGlobalElemPerLevel = nLocalElemPerLevel;
 
 #ifdef HAVE_MPI
-     SU2_MPI::Reduce(nLocalElemPerLevel.data(), nGlobalElemPerLevel.data(),
-                     nTimeLevels, MPI_UNSIGNED_LONG, MPI_SUM,
-                     MASTER_NODE, SU2_MPI::GetComm());
+    SU2_MPI::Reduce(nLocalElemPerLevel.data(), nGlobalElemPerLevel.data(), nTimeLevels, MPI_UNSIGNED_LONG, MPI_SUM,
+                    MASTER_NODE, SU2_MPI::GetComm());
 #endif
 
     /* Write the output. */
-    if(rank == MASTER_NODE) {
-      for(unsigned short i=0; i<nTimeLevels; ++i) {
-        if( nGlobalElemPerLevel[i] )
-          cout << "Number of elements time level " << i << ": "
-               << nGlobalElemPerLevel[i] << endl;
+    if (rank == MASTER_NODE) {
+      for (unsigned short i = 0; i < nTimeLevels; ++i) {
+        if (nGlobalElemPerLevel[i])
+          cout << "Number of elements time level " << i << ": " << nGlobalElemPerLevel[i] << endl;
       }
     }
   }
 }
 
-void CPhysicalGeometry::ComputeFEMGraphWeights(
-              CConfig                                    *config,
-              const vector<CFaceOfElement>               &localFaces,
-              const vector<vector<unsigned long> >       &adjacency,
-              const map<unsigned long, CUnsignedShort2T> &mapExternalElemIDToTimeLevel,
-                    vector<su2double>                    &vwgt,
-                    vector<vector<su2double> >           &adjwgt) {
-
+void CPhysicalGeometry::ComputeFEMGraphWeights(CConfig* config, const vector<CFaceOfElement>& localFaces,
+                                               const vector<vector<unsigned long> >& adjacency,
+                                               const map<unsigned long, CUnsignedShort2T>& mapExternalElemIDToTimeLevel,
+                                               vector<su2double>& vwgt, vector<vector<su2double> >& adjwgt) {
   /*--- Determine the maximum time level that occurs in the grid. ---*/
   unsigned short maxTimeLevel = 0;
-  for(unsigned long i=0; i<nElem; ++i)
-    maxTimeLevel = max(maxTimeLevel, elem[i]->GetTimeLevel());
+  for (unsigned long i = 0; i < nElem; ++i) maxTimeLevel = max(maxTimeLevel, elem[i]->GetTimeLevel());
 
 #ifdef HAVE_MPI
   unsigned short maxTimeLevelLocal = maxTimeLevel;
-  SU2_MPI::Allreduce(&maxTimeLevelLocal, &maxTimeLevel, 1,
-                     MPI_UNSIGNED_SHORT, MPI_MAX, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&maxTimeLevelLocal, &maxTimeLevel, 1, MPI_UNSIGNED_SHORT, MPI_MAX, SU2_MPI::GetComm());
 #endif
 
   /*--------------------------------------------------------------------------*/
@@ -4667,7 +4424,7 @@ void CPhysicalGeometry::ComputeFEMGraphWeights(
 
   /*--- Define the standard elements for the volume elements, the boundary faces
         and the matching internal faces. ---*/
-  vector<CFEMStandardElement>      standardElements;
+  vector<CFEMStandardElement> standardElements;
   vector<CFEMStandardBoundaryFace> standardBoundaryFaces;
   vector<CFEMStandardInternalFace> standardMatchingFaces;
 
@@ -4676,32 +4433,29 @@ void CPhysicalGeometry::ComputeFEMGraphWeights(
         surface integral to allow for Discontinuous and Continuous Galerkin
         schemes. For the latter the contribution of the surface integral will
         be negligible to the total amount of work.         ---*/
-  for(unsigned long i=0; i<nElem; ++i) {
-
+  for (unsigned long i = 0; i < nElem; ++i) {
     /*------------------------------------------------------------------------*/
     /*--- Determine the computational weight of the volume integral in the ---*/
     /*--- (DG-)FEM formulation.                                            ---*/
     /*------------------------------------------------------------------------*/
 
     /* Easier storage of the two indices for the vertex weights of this element. */
-    const unsigned long ind0 = 2*i;
+    const unsigned long ind0 = 2 * i;
     const unsigned long ind1 = ind0 + 1;
 
     /*--- Determine the corresponding standard element for this volume element.
           Create it, if it does not exist. ---*/
     unsigned short VTK_Type = elem[i]->GetVTK_Type();
     unsigned short nPolySol = elem[i]->GetNPolySol();
-    bool JacIsConstant      = elem[i]->GetJacobianConsideredConstant();
+    bool JacIsConstant = elem[i]->GetJacobianConsideredConstant();
 
     unsigned long ii;
-    for(ii=0; ii<standardElements.size(); ++ii) {
-      if( standardElements[ii].SameStandardElement(VTK_Type, nPolySol,
-                                                   JacIsConstant) ) break;
+    for (ii = 0; ii < standardElements.size(); ++ii) {
+      if (standardElements[ii].SameStandardElement(VTK_Type, nPolySol, JacIsConstant)) break;
     }
 
-    if(ii == standardElements.size())
-      standardElements.push_back(CFEMStandardElement(VTK_Type, nPolySol,
-                                                     JacIsConstant, config));
+    if (ii == standardElements.size())
+      standardElements.push_back(CFEMStandardElement(VTK_Type, nPolySol, JacIsConstant, config));
 
     /* Initialize the computational work for this element, which is stored
        in the 1st vertex weight. */
@@ -4718,19 +4472,24 @@ void CPhysicalGeometry::ComputeFEMGraphWeights(
     /*--- Get the global IDs of the corner points of all the faces of this element. ---*/
     unsigned short nFaces;
     unsigned short nPointsPerFace[6];
-    unsigned long  faceConn[6][4];
+    unsigned long faceConn[6][4];
 
     elem[i]->GetCornerPointsAllFaces(nFaces, nPointsPerFace, faceConn);
 
     /*--- Loop over the number of faces of this element. ---*/
-    for(unsigned short j=0; j<nFaces; ++j) {
-
+    for (unsigned short j = 0; j < nFaces; ++j) {
       /* Determine the VTK type of the face. */
       unsigned short VTK_Type_Face = 0;
-      switch( nPointsPerFace[j] ) {
-        case 2: VTK_Type_Face = LINE;          break;
-        case 3: VTK_Type_Face = TRIANGLE;      break;
-        case 4: VTK_Type_Face = QUADRILATERAL; break;
+      switch (nPointsPerFace[j]) {
+        case 2:
+          VTK_Type_Face = LINE;
+          break;
+        case 3:
+          VTK_Type_Face = TRIANGLE;
+          break;
+        case 4:
+          VTK_Type_Face = QUADRILATERAL;
+          break;
       }
 
       /* Easier storage whether or not the Jacobian is constant. */
@@ -4739,65 +4498,57 @@ void CPhysicalGeometry::ComputeFEMGraphWeights(
       /*--- Check if this is a matching internal face. ---*/
       CFaceOfElement thisFace;
       thisFace.nCornerPoints = nPointsPerFace[j];
-      for(unsigned short k=0; k<nPointsPerFace[j]; ++k)
-        thisFace.cornerPoints[k] = faceConn[j][k];
+      for (unsigned short k = 0; k < nPointsPerFace[j]; ++k) thisFace.cornerPoints[k] = faceConn[j][k];
       thisFace.CreateUniqueNumbering();
 
       vector<CFaceOfElement>::const_iterator low;
       low = lower_bound(localFaces.begin(), localFaces.end(), thisFace);
 
       bool thisFaceFound = false;
-      if(low != localFaces.end()) {
-        if( !(thisFace < *low) ) thisFaceFound = true;
+      if (low != localFaces.end()) {
+        if (!(thisFace < *low)) thisFaceFound = true;
       }
 
-      if( thisFaceFound ) {
-
+      if (thisFaceFound) {
         /* Check if this internal matching face is owned by this element. */
         bool faceIsOwned;
-        if(elemID == low->elemID0) faceIsOwned =  low->elem0IsOwner;
-        else                       faceIsOwned = !low->elem0IsOwner;
-
-        if( faceIsOwned ) {
+        if (elemID == low->elemID0)
+          faceIsOwned = low->elem0IsOwner;
+        else
+          faceIsOwned = !low->elem0IsOwner;
 
+        if (faceIsOwned) {
           /*--- Determine the index of the corresponding standard matching
                 face. If it does not exist, create it. ---*/
-          for(ii=0; ii<standardMatchingFaces.size(); ++ii) {
-            if( standardMatchingFaces[ii].SameStandardMatchingFace(VTK_Type_Face, JacIsConstant,
-                                                                   low->elemType0, low->nPolySol0,
-                                                                   low->elemType1, low->nPolySol1,
-                                                                   false, false) )
+          for (ii = 0; ii < standardMatchingFaces.size(); ++ii) {
+            if (standardMatchingFaces[ii].SameStandardMatchingFace(VTK_Type_Face, JacIsConstant, low->elemType0,
+                                                                   low->nPolySol0, low->elemType1, low->nPolySol1,
+                                                                   false, false))
               break;
           }
 
-          if(ii == standardMatchingFaces.size())
-            standardMatchingFaces.push_back(CFEMStandardInternalFace(VTK_Type_Face,
-                                                                     low->elemType0, low->nPolySol0,
-                                                                     low->elemType1, low->nPolySol1,
-                                                                     JacIsConstant, false, false,
-                                                                     config));
+          if (ii == standardMatchingFaces.size())
+            standardMatchingFaces.push_back(CFEMStandardInternalFace(VTK_Type_Face, low->elemType0, low->nPolySol0,
+                                                                     low->elemType1, low->nPolySol1, JacIsConstant,
+                                                                     false, false, config));
 
           /* Update the computational work for this element, i.e. the 1st
              vertex weight. */
           vwgt[ind0] += standardMatchingFaces[ii].WorkEstimateMetis(config);
         }
-      }
-      else {
-
+      } else {
         /*--- This is a boundary face, which is owned by definition. Determine
               the index of the corresponding standard boundary face. If it
               does not exist, create it. ---*/
-        for(ii=0; ii<standardBoundaryFaces.size(); ++ii) {
-          if(standardBoundaryFaces[ii].SameStandardBoundaryFace(VTK_Type_Face, JacIsConstant,
-                                                                VTK_Type, nPolySol, false) )
+        for (ii = 0; ii < standardBoundaryFaces.size(); ++ii) {
+          if (standardBoundaryFaces[ii].SameStandardBoundaryFace(VTK_Type_Face, JacIsConstant, VTK_Type, nPolySol,
+                                                                 false))
             break;
         }
 
-        if(ii == standardBoundaryFaces.size())
-          standardBoundaryFaces.push_back(CFEMStandardBoundaryFace(VTK_Type_Face,
-                                                                   VTK_Type, nPolySol,
-                                                                   JacIsConstant, false,
-                                                                   config));
+        if (ii == standardBoundaryFaces.size())
+          standardBoundaryFaces.push_back(
+              CFEMStandardBoundaryFace(VTK_Type_Face, VTK_Type, nPolySol, JacIsConstant, false, config));
 
         /* Update the computational work for this element, i.e. the 1st
            vertex weight. */
@@ -4818,56 +4569,52 @@ void CPhysicalGeometry::ComputeFEMGraphWeights(
 
   /* Loop over the markers and select the ones for which a wall function
      treatment must be carried out. */
-  for(unsigned short iMarker=0; iMarker<nMarker; ++iMarker) {
-
+  for (unsigned short iMarker = 0; iMarker < nMarker; ++iMarker) {
     switch (config->GetMarker_All_KindBC(iMarker)) {
       case ISOTHERMAL:
       case HEAT_FLUX: {
         const string Marker_Tag = config->GetMarker_All_TagBound(iMarker);
-        if(config->GetWallFunction_Treatment(Marker_Tag) != WALL_FUNCTIONS::NONE) {
-
+        if (config->GetWallFunction_Treatment(Marker_Tag) != WALL_FUNCTIONS::NONE) {
           /* Retrieve the integer information for this boundary marker.
              The number of points in normal direction for the wall function
              treatment is the first element of this array. */
-          const unsigned short *shortInfo = config->GetWallFunction_IntInfo(Marker_Tag);
+          const unsigned short* shortInfo = config->GetWallFunction_IntInfo(Marker_Tag);
 
           /* Loop over the local boundary elements for this marker. */
-          for(unsigned long l=0; l<nElem_Bound[iMarker]; ++l) {
-
+          for (unsigned long l = 0; l < nElem_Bound[iMarker]; ++l) {
             /* Get the required data to define the standard boundary element. */
 
             /* Easier storage of the element type, the corresponding volume
                element, the polynomial degree for the solution and whether or
                not the Jacobian can be considered constant. */
             const unsigned short VTK_Type_Face = bound[iMarker][l]->GetVTK_Type();
-            const unsigned long  elemID        = bound[iMarker][l]->GetDomainElement()
-                                               - beg_node[rank];
-            const unsigned short nPolySol      = elem[elemID]->GetNPolySol();
+            const unsigned long elemID = bound[iMarker][l]->GetDomainElement() - beg_node[rank];
+            const unsigned short nPolySol = elem[elemID]->GetNPolySol();
             const unsigned short VTK_Type_Elem = elem[elemID]->GetVTK_Type();
-            const bool JacIsConstant           = bound[iMarker][l]->GetJacobianConsideredConstant();
+            const bool JacIsConstant = bound[iMarker][l]->GetJacobianConsideredConstant();
 
             /* Determine the corresponding entry in the standard elements for
                boundary faces. This entry must be found. */
             unsigned long ii;
-            for(ii=0; ii<standardBoundaryFaces.size(); ++ii) {
-              if(standardBoundaryFaces[ii].SameStandardBoundaryFace(VTK_Type_Face, JacIsConstant,
-                                                                    VTK_Type_Elem, nPolySol, false) )
+            for (ii = 0; ii < standardBoundaryFaces.size(); ++ii) {
+              if (standardBoundaryFaces[ii].SameStandardBoundaryFace(VTK_Type_Face, JacIsConstant, VTK_Type_Elem,
+                                                                     nPolySol, false))
                 break;
             }
 
-            if(ii == standardBoundaryFaces.size())
+            if (ii == standardBoundaryFaces.size())
               SU2_MPI::Error("No matching standard boundary element found", CURRENT_FUNCTION);
 
             /* Update the computational work for the corresponding volume element,
                i.e. the 1st vertex weight. */
-            vwgt[2*elemID] += standardBoundaryFaces[ii].WorkEstimateMetisWallFunctions(config, shortInfo[0]);
+            vwgt[2 * elemID] += standardBoundaryFaces[ii].WorkEstimateMetisWallFunctions(config, shortInfo[0]);
           }
         }
 
         break;
       }
 
-      default:  /* Just to avoid a compiler warning. */
+      default: /* Just to avoid a compiler warning. */
         break;
     }
   }
@@ -4878,15 +4625,15 @@ void CPhysicalGeometry::ComputeFEMGraphWeights(
   /*--- accurate local time stepping is employed.                          ---*/
   /*--------------------------------------------------------------------------*/
 
-  for(unsigned long i=0; i<nElem; ++i) {
+  for (unsigned long i = 0; i < nElem; ++i) {
     const unsigned short diffLevel = maxTimeLevel - elem[i]->GetTimeLevel();
-    vwgt[2*i] *= pow(2, diffLevel);
+    vwgt[2 * i] *= pow(2, diffLevel);
   }
 
   /*--- Determine the minimum of the workload of the elements, i.e. 1st vertex
         weight, over the entire domain. ---*/
   su2double minvwgt = vwgt[0];
-  for(unsigned long i=0; i<nElem; ++i) minvwgt = min(minvwgt, vwgt[2*i]);
+  for (unsigned long i = 0; i < nElem; ++i) minvwgt = min(minvwgt, vwgt[2 * i]);
 
 #ifdef HAVE_MPI
   su2double locminvwgt = minvwgt;
@@ -4897,8 +4644,8 @@ void CPhysicalGeometry::ComputeFEMGraphWeights(
         minimum value and multiply by 100, such that the conversion to integer
         weights (ParMETIS is using integers for the weights) does not lead to
         a significant increase in the load imbalance. ---*/
-  minvwgt = 100.0/minvwgt;
-  for(unsigned long i=0; i<nElem; ++i) vwgt[2*i] *= minvwgt;
+  minvwgt = 100.0 / minvwgt;
+  for (unsigned long i = 0; i < nElem; ++i) vwgt[2 * i] *= minvwgt;
 
   /*--------------------------------------------------------------------------*/
   /* Step 2: Determine the adjacency weights, which are proportional to the   */
@@ -4909,40 +4656,34 @@ void CPhysicalGeometry::ComputeFEMGraphWeights(
   /*--- Determine the edge weights by a double loop over the local elements
         and its edges. The map mapElemIDsToFaceInd is used to determine
         the corresponding index in localFaces.   ---*/
-  for(unsigned long i=0; i<nElem; ++i) {
-
+  for (unsigned long i = 0; i < nElem; ++i) {
     /* Easier storage of the time level of the current element and the
        number of solution DOFs. */
     const unsigned short timeLevel0 = elem[i]->GetTimeLevel();
-    const unsigned short nDOFs0     = elem[i]->GetNDOFsSol();
+    const unsigned short nDOFs0 = elem[i]->GetNDOFsSol();
 
     /* Loop over the number of entries in the graph for this element. */
-    for(unsigned long j=0; j<adjacency[i].size(); ++j) {
-
+    for (unsigned long j = 0; j < adjacency[i].size(); ++j) {
       /* Define the variables for the time level and number of solution
          DOFs for the neighboring element. */
       unsigned short timeLevel1, nDOFs1;
 
       /* Check if the neighor is stored locally. */
-      if(adjacency[i][j] >= beg_node[rank] &&
-         adjacency[i][j] <  beg_node[rank]+nElem) {
-
+      if (adjacency[i][j] >= beg_node[rank] && adjacency[i][j] < beg_node[rank] + nElem) {
         /* Locally stored element. Determine its local ID and set the
            time level and number of solution DOFs. */
         unsigned long elemID1 = adjacency[i][j] - beg_node[rank];
         timeLevel1 = elem[elemID1]->GetTimeLevel();
-        nDOFs1     = elem[elemID1]->GetNDOFsSol();
-      }
-      else {
-
+        nDOFs1 = elem[elemID1]->GetNDOFsSol();
+      } else {
         /* The neighbor is an external element. Find it in mapExternalElemIDToTimeLevel
            and set the time level and number of solution DOFs accordingly. */
-        map<unsigned long,CUnsignedShort2T>::const_iterator MI;
+        map<unsigned long, CUnsignedShort2T>::const_iterator MI;
         MI = mapExternalElemIDToTimeLevel.find(adjacency[i][j]);
-        if(MI == mapExternalElemIDToTimeLevel.end())
+        if (MI == mapExternalElemIDToTimeLevel.end())
           SU2_MPI::Error("Entry not found in mapExternalElemIDToTimeLevel", CURRENT_FUNCTION);
         timeLevel1 = MI->second.short0;
-        nDOFs1     = MI->second.short1;
+        nDOFs1 = MI->second.short1;
       }
 
       /* Determine the difference of the maximum time level that occurs and
@@ -4954,7 +4695,7 @@ void CPhysicalGeometry::ComputeFEMGraphWeights(
       /* Set the edge weight. As ParMetis expects an undirected graph, set the edge weight
          to the sum of the number of DOFs on both sides, multiplied by the weight factor
          to account for different time levels. */
-      adjwgt[i][j] = pow(2, diffLevel) *(nDOFs0 + nDOFs1);
+      adjwgt[i][j] = pow(2, diffLevel) * (nDOFs0 + nDOFs1);
     }
   }
 }
diff --git a/Common/src/geometry/CDummyGeometry.cpp b/Common/src/geometry/CDummyGeometry.cpp
index 433eefa5b0a..44f820d8877 100644
--- a/Common/src/geometry/CDummyGeometry.cpp
+++ b/Common/src/geometry/CDummyGeometry.cpp
@@ -27,15 +27,13 @@
 
 #include "../../include/geometry/CDummyGeometry.hpp"
 
-
-CDummyGeometry::CDummyGeometry(CConfig *config) : CGeometry() {
-
+CDummyGeometry::CDummyGeometry(CConfig* config) : CGeometry() {
   nZone = config->GetnZone();
 
-  nPoint_P2PSend = new int[size] ();
-  nPoint_P2PRecv = new int[size] ();
+  nPoint_P2PSend = new int[size]();
+  nPoint_P2PRecv = new int[size]();
 
-  nVertex = new unsigned long[config->GetnMarker_All()] ();
+  nVertex = new unsigned long[config->GetnMarker_All()]();
 
   Tag_to_Marker = new string[config->GetnMarker_All()];
 
diff --git a/Common/src/geometry/CGeometry.cpp b/Common/src/geometry/CGeometry.cpp
index ad15762ce5e..8035608ebc9 100644
--- a/Common/src/geometry/CGeometry.cpp
+++ b/Common/src/geometry/CGeometry.cpp
@@ -33,20 +33,14 @@
 #include "../../include/toolboxes/geometry_toolbox.hpp"
 #include "../../include/toolboxes/ndflattener.hpp"
 
-CGeometry::CGeometry(void) :
-  size(SU2_MPI::GetSize()),
-  rank(SU2_MPI::GetRank()) {
-
-}
+CGeometry::CGeometry(void) : size(SU2_MPI::GetSize()), rank(SU2_MPI::GetRank()) {}
 
 CGeometry::~CGeometry(void) {
-
   unsigned long iElem, iElem_Bound, iVertex;
   unsigned short iMarker;
 
   if (elem != nullptr) {
-    for (iElem = 0; iElem < nElem; iElem++)
-      delete elem[iElem];
+    for (iElem = 0; iElem < nElem; iElem++) delete elem[iElem];
     delete[] elem;
   }
 
@@ -55,9 +49,9 @@ CGeometry::~CGeometry(void) {
       for (iElem_Bound = 0; iElem_Bound < nElem_Bound[iMarker]; iElem_Bound++) {
         delete bound[iMarker][iElem_Bound];
       }
-      delete [] bound[iMarker];
+      delete[] bound[iMarker];
     }
-    delete [] bound;
+    delete[] bound;
   }
 
   delete nodes;
@@ -69,83 +63,80 @@ CGeometry::~CGeometry(void) {
       for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
         delete vertex[iMarker][iVertex];
       }
-      delete [] vertex[iMarker];
+      delete[] vertex[iMarker];
     }
-    delete [] vertex;
+    delete[] vertex;
   }
 
-  delete [] nElem_Bound;
-  delete [] nVertex;
-  delete [] Marker_All_SendRecv;
-  delete [] Tag_to_Marker;
+  delete[] nElem_Bound;
+  delete[] nVertex;
+  delete[] Marker_All_SendRecv;
+  delete[] Tag_to_Marker;
 
-  delete [] beg_node;
-  delete [] end_node;
-  delete [] nPointLinear;
-  delete [] nPointCumulative;
+  delete[] beg_node;
+  delete[] end_node;
+  delete[] nPointLinear;
+  delete[] nPointCumulative;
 
-  if(CustomBoundaryHeatFlux != nullptr){
-    for(iMarker=0; iMarker < nMarker; iMarker++){
-      delete [] CustomBoundaryHeatFlux[iMarker];
+  if (CustomBoundaryHeatFlux != nullptr) {
+    for (iMarker = 0; iMarker < nMarker; iMarker++) {
+      delete[] CustomBoundaryHeatFlux[iMarker];
     }
-    delete [] CustomBoundaryHeatFlux;
+    delete[] CustomBoundaryHeatFlux;
   }
 
-  if(CustomBoundaryTemperature != nullptr){
-    for(iMarker=0; iMarker < nMarker; iMarker++){
-      delete [] CustomBoundaryTemperature[iMarker];
+  if (CustomBoundaryTemperature != nullptr) {
+    for (iMarker = 0; iMarker < nMarker; iMarker++) {
+      delete[] CustomBoundaryTemperature[iMarker];
     }
-    delete [] CustomBoundaryTemperature;
+    delete[] CustomBoundaryTemperature;
   }
 
   /*--- Delete structures for MPI point-to-point communication. ---*/
 
-  delete [] bufD_P2PRecv;
-  delete [] bufD_P2PSend;
+  delete[] bufD_P2PRecv;
+  delete[] bufD_P2PSend;
 
-  delete [] bufS_P2PRecv;
-  delete [] bufS_P2PSend;
+  delete[] bufS_P2PRecv;
+  delete[] bufS_P2PSend;
 
-  delete [] req_P2PSend;
-  delete [] req_P2PRecv;
+  delete[] req_P2PSend;
+  delete[] req_P2PRecv;
 
-  delete [] nPoint_P2PRecv;
-  delete [] nPoint_P2PSend;
+  delete[] nPoint_P2PRecv;
+  delete[] nPoint_P2PSend;
 
-  delete [] Neighbors_P2PSend;
-  delete [] Neighbors_P2PRecv;
+  delete[] Neighbors_P2PSend;
+  delete[] Neighbors_P2PRecv;
 
-  delete [] Local_Point_P2PSend;
-  delete [] Local_Point_P2PRecv;
+  delete[] Local_Point_P2PSend;
+  delete[] Local_Point_P2PRecv;
 
   /*--- Delete structures for MPI periodic communication. ---*/
 
-  delete [] bufD_PeriodicRecv;
-  delete [] bufD_PeriodicSend;
-
-  delete [] bufS_PeriodicRecv;
-  delete [] bufS_PeriodicSend;
+  delete[] bufD_PeriodicRecv;
+  delete[] bufD_PeriodicSend;
 
-  delete [] req_PeriodicSend;
-  delete [] req_PeriodicRecv;
+  delete[] bufS_PeriodicRecv;
+  delete[] bufS_PeriodicSend;
 
-  delete [] nPoint_PeriodicRecv;
-  delete [] nPoint_PeriodicSend;
+  delete[] req_PeriodicSend;
+  delete[] req_PeriodicRecv;
 
-  delete [] Neighbors_PeriodicSend;
-  delete [] Neighbors_PeriodicRecv;
+  delete[] nPoint_PeriodicRecv;
+  delete[] nPoint_PeriodicSend;
 
-  delete [] Local_Point_PeriodicSend;
-  delete [] Local_Point_PeriodicRecv;
+  delete[] Neighbors_PeriodicSend;
+  delete[] Neighbors_PeriodicRecv;
 
-  delete [] Local_Marker_PeriodicSend;
-  delete [] Local_Marker_PeriodicRecv;
+  delete[] Local_Point_PeriodicSend;
+  delete[] Local_Point_PeriodicRecv;
 
+  delete[] Local_Marker_PeriodicSend;
+  delete[] Local_Marker_PeriodicRecv;
 }
 
-void CGeometry::PreprocessP2PComms(CGeometry *geometry,
-                                   CConfig *config) {
-
+void CGeometry::PreprocessP2PComms(CGeometry* geometry, CConfig* config) {
   /*--- We start with the send and receive lists already available in
    the form of SEND_RECEIVE boundary markers. We will loop through
    these markers and establish the neighboring ranks and number of
@@ -159,91 +150,94 @@ void CGeometry::PreprocessP2PComms(CGeometry *geometry,
   /*--- Local variables. ---*/
 
   unsigned short iMarker;
-  unsigned long  nVertexS, nVertexR, iVertex, MarkerS, MarkerR;
+  unsigned long nVertexS, nVertexR, iVertex, MarkerS, MarkerR;
 
   int iRank, iSend, iRecv, count;
 
   /*--- Create some temporary structures for tracking sends/recvs. ---*/
 
-  int *nPoint_Send_All = new int[size+1]; nPoint_Send_All[0] = 0;
-  int *nPoint_Recv_All = new int[size+1]; nPoint_Recv_All[0] = 0;
-  int *nPoint_Flag = new int[size];
+  int* nPoint_Send_All = new int[size + 1];
+  nPoint_Send_All[0] = 0;
+  int* nPoint_Recv_All = new int[size + 1];
+  nPoint_Recv_All[0] = 0;
+  int* nPoint_Flag = new int[size];
 
   for (iRank = 0; iRank < size; iRank++) {
-    nPoint_Send_All[iRank] = 0; nPoint_Recv_All[iRank] = 0; nPoint_Flag[iRank]= -1;
+    nPoint_Send_All[iRank] = 0;
+    nPoint_Recv_All[iRank] = 0;
+    nPoint_Flag[iRank] = -1;
   }
-  nPoint_Send_All[size] = 0; nPoint_Recv_All[size] = 0;
+  nPoint_Send_All[size] = 0;
+  nPoint_Recv_All[size] = 0;
 
   /*--- Loop through all of our SEND_RECEIVE markers and track
    our sends with each rank. ---*/
 
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-    if ((config->GetMarker_All_KindBC(iMarker) == SEND_RECEIVE) &&
-        (config->GetMarker_All_SendRecv(iMarker) > 0)) {
-
+    if ((config->GetMarker_All_KindBC(iMarker) == SEND_RECEIVE) && (config->GetMarker_All_SendRecv(iMarker) > 0)) {
       /*--- Get the destination rank and number of points to send. ---*/
 
-      iRank    = config->GetMarker_All_SendRecv(iMarker)-1;
+      iRank = config->GetMarker_All_SendRecv(iMarker) - 1;
       nVertexS = geometry->nVertex[iMarker];
 
       /*--- If we have not visited this element yet, increment our
        number of elements that must be sent to a particular proc. ---*/
 
       if ((nPoint_Flag[iRank] != (int)iMarker)) {
-        nPoint_Flag[iRank]        = (int)iMarker;
-        nPoint_Send_All[iRank+1] += nVertexS;
+        nPoint_Flag[iRank] = (int)iMarker;
+        nPoint_Send_All[iRank + 1] += nVertexS;
       }
-
     }
   }
 
-  delete [] nPoint_Flag;
+  delete[] nPoint_Flag;
 
   /*--- Communicate the number of points to be sent/recv'd amongst
    all processors. After this communication, each proc knows how
    many cells it will receive from each other processor. ---*/
 
-  SU2_MPI::Alltoall(&(nPoint_Send_All[1]), 1, MPI_INT,
-                    &(nPoint_Recv_All[1]), 1, MPI_INT, SU2_MPI::GetComm());
+  SU2_MPI::Alltoall(&(nPoint_Send_All[1]), 1, MPI_INT, &(nPoint_Recv_All[1]), 1, MPI_INT, SU2_MPI::GetComm());
 
   /*--- Prepare to send connectivities. First check how many
    messages we will be sending and receiving. Here we also put
    the counters into cumulative storage format to make the
    communications simpler. ---*/
 
-  nP2PSend = 0; nP2PRecv = 0;
+  nP2PSend = 0;
+  nP2PRecv = 0;
 
   for (iRank = 0; iRank < size; iRank++) {
-    if ((iRank != rank) && (nPoint_Send_All[iRank+1] > 0)) nP2PSend++;
-    if ((iRank != rank) && (nPoint_Recv_All[iRank+1] > 0)) nP2PRecv++;
+    if ((iRank != rank) && (nPoint_Send_All[iRank + 1] > 0)) nP2PSend++;
+    if ((iRank != rank) && (nPoint_Recv_All[iRank + 1] > 0)) nP2PRecv++;
 
-    nPoint_Send_All[iRank+1] += nPoint_Send_All[iRank];
-    nPoint_Recv_All[iRank+1] += nPoint_Recv_All[iRank];
+    nPoint_Send_All[iRank + 1] += nPoint_Send_All[iRank];
+    nPoint_Recv_All[iRank + 1] += nPoint_Recv_All[iRank];
   }
 
   /*--- Allocate only as much memory as we need for the P2P neighbors. ---*/
 
-  nPoint_P2PSend = new int[nP2PSend+1]; nPoint_P2PSend[0] = 0;
-  nPoint_P2PRecv = new int[nP2PRecv+1]; nPoint_P2PRecv[0] = 0;
+  nPoint_P2PSend = new int[nP2PSend + 1];
+  nPoint_P2PSend[0] = 0;
+  nPoint_P2PRecv = new int[nP2PRecv + 1];
+  nPoint_P2PRecv[0] = 0;
 
   Neighbors_P2PSend = new int[nP2PSend];
   Neighbors_P2PRecv = new int[nP2PRecv];
 
-  iSend = 0; iRecv = 0;
+  iSend = 0;
+  iRecv = 0;
   for (iRank = 0; iRank < size; iRank++) {
-
-    if ((nPoint_Send_All[iRank+1] > nPoint_Send_All[iRank]) && (iRank != rank)) {
+    if ((nPoint_Send_All[iRank + 1] > nPoint_Send_All[iRank]) && (iRank != rank)) {
       Neighbors_P2PSend[iSend] = iRank;
-      nPoint_P2PSend[iSend+1] = nPoint_Send_All[iRank+1];
+      nPoint_P2PSend[iSend + 1] = nPoint_Send_All[iRank + 1];
       iSend++;
     }
 
-    if ((nPoint_Recv_All[iRank+1] > nPoint_Recv_All[iRank]) && (iRank != rank)) {
+    if ((nPoint_Recv_All[iRank + 1] > nPoint_Recv_All[iRank]) && (iRank != rank)) {
       Neighbors_P2PRecv[iRecv] = iRank;
-      nPoint_P2PRecv[iRecv+1] = nPoint_Recv_All[iRank+1];
+      nPoint_P2PRecv[iRecv + 1] = nPoint_Recv_All[iRank + 1];
       iRecv++;
     }
-
   }
 
   /*--- Create a reverse mapping of the message to the rank so that we
@@ -251,15 +245,13 @@ void CGeometry::PreprocessP2PComms(CGeometry *geometry,
    messages dynamically. ---*/
 
   P2PSend2Neighbor.clear();
-  for (iSend = 0; iSend < nP2PSend; iSend++)
-    P2PSend2Neighbor[Neighbors_P2PSend[iSend]] = iSend;
+  for (iSend = 0; iSend < nP2PSend; iSend++) P2PSend2Neighbor[Neighbors_P2PSend[iSend]] = iSend;
 
   P2PRecv2Neighbor.clear();
-  for (iRecv = 0; iRecv < nP2PRecv; iRecv++)
-    P2PRecv2Neighbor[Neighbors_P2PRecv[iRecv]] = iRecv;
+  for (iRecv = 0; iRecv < nP2PRecv; iRecv++) P2PRecv2Neighbor[Neighbors_P2PRecv[iRecv]] = iRecv;
 
-  delete [] nPoint_Send_All;
-  delete [] nPoint_Recv_All;
+  delete[] nPoint_Send_All;
+  delete[] nPoint_Recv_All;
 
   /*--- Allocate the memory that we need for receiving the conn
    values and then cue up the non-blocking receives. Note that
@@ -268,13 +260,11 @@ void CGeometry::PreprocessP2PComms(CGeometry *geometry,
 
   Local_Point_P2PSend = nullptr;
   Local_Point_P2PSend = new unsigned long[nPoint_P2PSend[nP2PSend]];
-  for (iSend = 0; iSend < nPoint_P2PSend[nP2PSend]; iSend++)
-    Local_Point_P2PSend[iSend] = 0;
+  for (iSend = 0; iSend < nPoint_P2PSend[nP2PSend]; iSend++) Local_Point_P2PSend[iSend] = 0;
 
   Local_Point_P2PRecv = nullptr;
   Local_Point_P2PRecv = new unsigned long[nPoint_P2PRecv[nP2PRecv]];
-  for (iRecv = 0; iRecv < nPoint_P2PRecv[nP2PRecv]; iRecv++)
-    Local_Point_P2PRecv[iRecv] = 0;
+  for (iRecv = 0; iRecv < nPoint_P2PRecv[nP2PRecv]; iRecv++) Local_Point_P2PRecv[iRecv] = 0;
 
   /*--- We allocate the memory for communicating values in a later step
    once we know the maximum packet size that we need to communicate. This
@@ -290,10 +280,10 @@ void CGeometry::PreprocessP2PComms(CGeometry *geometry,
   /*--- Allocate memory for the MPI requests if we need to communicate. ---*/
 
   if (nP2PSend > 0) {
-    req_P2PSend   = new SU2_MPI::Request[nP2PSend];
+    req_P2PSend = new SU2_MPI::Request[nP2PSend];
   }
   if (nP2PRecv > 0) {
-    req_P2PRecv   = new SU2_MPI::Request[nP2PRecv];
+    req_P2PRecv = new SU2_MPI::Request[nP2PRecv];
   }
 
   /*--- Build lists of local index values for send. ---*/
@@ -301,12 +291,10 @@ void CGeometry::PreprocessP2PComms(CGeometry *geometry,
   count = 0;
   for (iSend = 0; iSend < nP2PSend; iSend++) {
     for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-      if ((config->GetMarker_All_KindBC(iMarker) == SEND_RECEIVE) &&
-          (config->GetMarker_All_SendRecv(iMarker) > 0)) {
-
-        MarkerS  = iMarker;
+      if ((config->GetMarker_All_KindBC(iMarker) == SEND_RECEIVE) && (config->GetMarker_All_SendRecv(iMarker) > 0)) {
+        MarkerS = iMarker;
         nVertexS = geometry->nVertex[MarkerS];
-        iRank    = config->GetMarker_All_SendRecv(MarkerS)-1;
+        iRank = config->GetMarker_All_SendRecv(MarkerS) - 1;
 
         if (iRank == Neighbors_P2PSend[iSend]) {
           for (iVertex = 0; iVertex < nVertexS; iVertex++) {
@@ -314,7 +302,6 @@ void CGeometry::PreprocessP2PComms(CGeometry *geometry,
             count++;
           }
         }
-
       }
     }
   }
@@ -324,12 +311,10 @@ void CGeometry::PreprocessP2PComms(CGeometry *geometry,
   count = 0;
   for (iRecv = 0; iRecv < nP2PRecv; iRecv++) {
     for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-      if ((config->GetMarker_All_KindBC(iMarker) == SEND_RECEIVE) &&
-          (config->GetMarker_All_SendRecv(iMarker) > 0)) {
-
-        MarkerR  = iMarker+1;
+      if ((config->GetMarker_All_KindBC(iMarker) == SEND_RECEIVE) && (config->GetMarker_All_SendRecv(iMarker) > 0)) {
+        MarkerR = iMarker + 1;
         nVertexR = geometry->nVertex[MarkerR];
-        iRank    = abs(config->GetMarker_All_SendRecv(MarkerR))-1;
+        iRank = abs(config->GetMarker_All_SendRecv(MarkerR)) - 1;
 
         if (iRank == Neighbors_P2PRecv[iRecv]) {
           for (iVertex = 0; iVertex < nVertexR; iVertex++) {
@@ -337,7 +322,6 @@ void CGeometry::PreprocessP2PComms(CGeometry *geometry,
             count++;
           }
         }
-
       }
     }
   }
@@ -345,11 +329,9 @@ void CGeometry::PreprocessP2PComms(CGeometry *geometry,
   /*--- In the future, some additional data structures could be created
    here to separate the interior and boundary nodes in order to help
    further overlap computation and communication. ---*/
-
 }
 
 void CGeometry::AllocateP2PComms(unsigned short countPerPoint) {
-
   /*--- This routine is activated whenever we attempt to perform
    a point-to-point MPI communication with our neighbors but the
    memory buffer allocated is not large enough for the packet size.
@@ -360,36 +342,29 @@ void CGeometry::AllocateP2PComms(unsigned short countPerPoint) {
   if (countPerPoint <= maxCountPerPoint) return;
 
   BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
+    /*--- Store the larger packet size to the class data. ---*/
 
-  /*--- Store the larger packet size to the class data. ---*/
-
-  maxCountPerPoint = countPerPoint;
-
-  /*-- Deallocate and reallocate our su2double cummunication memory. ---*/
+    maxCountPerPoint = countPerPoint;
 
-  delete [] bufD_P2PSend;
-  bufD_P2PSend = new su2double[maxCountPerPoint*nPoint_P2PSend[nP2PSend]] ();
+    /*-- Deallocate and reallocate our su2double cummunication memory. ---*/
 
-  delete [] bufD_P2PRecv;
-  bufD_P2PRecv = new su2double[maxCountPerPoint*nPoint_P2PRecv[nP2PRecv]] ();
+    delete[] bufD_P2PSend;
+    bufD_P2PSend = new su2double[maxCountPerPoint * nPoint_P2PSend[nP2PSend]]();
 
-  delete [] bufS_P2PSend;
-  bufS_P2PSend = new unsigned short[maxCountPerPoint*nPoint_P2PSend[nP2PSend]] ();
+    delete[] bufD_P2PRecv;
+    bufD_P2PRecv = new su2double[maxCountPerPoint * nPoint_P2PRecv[nP2PRecv]]();
 
-  delete [] bufS_P2PRecv;
-  bufS_P2PRecv = new unsigned short[maxCountPerPoint*nPoint_P2PRecv[nP2PRecv]] ();
+    delete[] bufS_P2PSend;
+    bufS_P2PSend = new unsigned short[maxCountPerPoint * nPoint_P2PSend[nP2PSend]]();
 
+    delete[] bufS_P2PRecv;
+    bufS_P2PRecv = new unsigned short[maxCountPerPoint * nPoint_P2PRecv[nP2PRecv]]();
   }
   END_SU2_OMP_SAFE_GLOBAL_ACCESS
-
 }
 
-void CGeometry::PostP2PRecvs(CGeometry *geometry,
-                             const CConfig *config,
-                             unsigned short commType,
-                             unsigned short countPerPoint,
-                             bool val_reverse) const {
-
+void CGeometry::PostP2PRecvs(CGeometry* geometry, const CConfig* config, unsigned short commType,
+                             unsigned short countPerPoint, bool val_reverse) const {
   /*--- Launch the non-blocking recv's first. Note that we have stored
    the counts and sources, so we can launch these before we even load
    the data and send from the neighbor ranks. ---*/
@@ -403,21 +378,20 @@ void CGeometry::PostP2PRecvs(CGeometry *geometry,
      send nodes become the recv nodes and vice-versa. ---*/
 
     if (val_reverse) {
-
       /*--- Compute our location in the buffer using the send data
        structure since we are reversing the comms. ---*/
 
-      auto offset = countPerPoint*nPoint_P2PSend[iRecv];
+      auto offset = countPerPoint * nPoint_P2PSend[iRecv];
 
       /*--- Take advantage of cumulative storage format to get the number
        of elems that we need to recv. Note again that we select the send
        points here as the recv points. ---*/
 
-      auto nPointP2P = nPoint_P2PSend[iRecv+1] - nPoint_P2PSend[iRecv];
+      auto nPointP2P = nPoint_P2PSend[iRecv + 1] - nPoint_P2PSend[iRecv];
 
       /*--- Total count can include multiple pieces of data per element. ---*/
 
-      auto count = countPerPoint*nPointP2P;
+      auto count = countPerPoint * nPointP2P;
 
       /*--- Get the rank from which we receive the message. Note again
        that we use the send rank as the source instead of the recv rank. ---*/
@@ -431,33 +405,31 @@ void CGeometry::PostP2PRecvs(CGeometry *geometry,
 
       switch (commType) {
         case COMM_TYPE_DOUBLE:
-          SU2_MPI::Irecv(&(bufD_P2PSend[offset]), count, MPI_DOUBLE,
-                         source, tag, SU2_MPI::GetComm(), &(req_P2PRecv[iRecv]));
+          SU2_MPI::Irecv(&(bufD_P2PSend[offset]), count, MPI_DOUBLE, source, tag, SU2_MPI::GetComm(),
+                         &(req_P2PRecv[iRecv]));
           break;
         case COMM_TYPE_UNSIGNED_SHORT:
-          SU2_MPI::Irecv(&(bufS_P2PSend[offset]), count, MPI_UNSIGNED_SHORT,
-                         source, tag, SU2_MPI::GetComm(), &(req_P2PRecv[iRecv]));
+          SU2_MPI::Irecv(&(bufS_P2PSend[offset]), count, MPI_UNSIGNED_SHORT, source, tag, SU2_MPI::GetComm(),
+                         &(req_P2PRecv[iRecv]));
           break;
         default:
-          SU2_MPI::Error("Unrecognized data type for point-to-point MPI comms.",
-                         CURRENT_FUNCTION);
+          SU2_MPI::Error("Unrecognized data type for point-to-point MPI comms.", CURRENT_FUNCTION);
           break;
       }
 
     } else {
-
       /*--- Compute our location in the recv buffer. ---*/
 
-      auto offset = countPerPoint*nPoint_P2PRecv[iRecv];
+      auto offset = countPerPoint * nPoint_P2PRecv[iRecv];
 
       /*--- Take advantage of cumulative storage format to get the number
        of elems that we need to recv. ---*/
 
-      auto nPointP2P = nPoint_P2PRecv[iRecv+1] - nPoint_P2PRecv[iRecv];
+      auto nPointP2P = nPoint_P2PRecv[iRecv + 1] - nPoint_P2PRecv[iRecv];
 
       /*--- Total count can include multiple pieces of data per element. ---*/
 
-      auto count = countPerPoint*nPointP2P;
+      auto count = countPerPoint * nPointP2P;
 
       /*--- Get the rank from which we receive the message. ---*/
 
@@ -468,33 +440,24 @@ void CGeometry::PostP2PRecvs(CGeometry *geometry,
 
       switch (commType) {
         case COMM_TYPE_DOUBLE:
-          SU2_MPI::Irecv(&(bufD_P2PRecv[offset]), count, MPI_DOUBLE,
-                         source, tag, SU2_MPI::GetComm(), &(req_P2PRecv[iMessage]));
+          SU2_MPI::Irecv(&(bufD_P2PRecv[offset]), count, MPI_DOUBLE, source, tag, SU2_MPI::GetComm(),
+                         &(req_P2PRecv[iMessage]));
           break;
         case COMM_TYPE_UNSIGNED_SHORT:
-          SU2_MPI::Irecv(&(bufS_P2PRecv[offset]), count, MPI_UNSIGNED_SHORT,
-                         source, tag, SU2_MPI::GetComm(), &(req_P2PRecv[iMessage]));
+          SU2_MPI::Irecv(&(bufS_P2PRecv[offset]), count, MPI_UNSIGNED_SHORT, source, tag, SU2_MPI::GetComm(),
+                         &(req_P2PRecv[iMessage]));
           break;
         default:
-          SU2_MPI::Error("Unrecognized data type for point-to-point MPI comms.",
-                         CURRENT_FUNCTION);
+          SU2_MPI::Error("Unrecognized data type for point-to-point MPI comms.", CURRENT_FUNCTION);
           break;
       }
-
     }
-
   }
   END_SU2_OMP_MASTER
-
 }
 
-void CGeometry::PostP2PSends(CGeometry *geometry,
-                             const CConfig *config,
-                             unsigned short commType,
-                             unsigned short countPerPoint,
-                             int val_iSend,
-                             bool val_reverse) const {
-
+void CGeometry::PostP2PSends(CGeometry* geometry, const CConfig* config, unsigned short commType,
+                             unsigned short countPerPoint, int val_iSend, bool val_reverse) const {
   /*--- Post the non-blocking send as soon as the buffer is loaded. ---*/
 
   /*--- In some instances related to the adjoint solver, we need
@@ -503,21 +466,20 @@ void CGeometry::PostP2PSends(CGeometry *geometry,
 
   SU2_OMP_MASTER
   if (val_reverse) {
-
     /*--- Compute our location in the buffer using the recv data
      structure since we are reversing the comms. ---*/
 
-    auto offset = countPerPoint*nPoint_P2PRecv[val_iSend];
+    auto offset = countPerPoint * nPoint_P2PRecv[val_iSend];
 
     /*--- Take advantage of cumulative storage format to get the number
      of points that we need to send. Note again that we select the recv
      points here as the send points. ---*/
 
-    auto nPointP2P = nPoint_P2PRecv[val_iSend+1] - nPoint_P2PRecv[val_iSend];
+    auto nPointP2P = nPoint_P2PRecv[val_iSend + 1] - nPoint_P2PRecv[val_iSend];
 
     /*--- Total count can include multiple pieces of data per element. ---*/
 
-    auto count = countPerPoint*nPointP2P;
+    auto count = countPerPoint * nPointP2P;
 
     /*--- Get the rank to which we send the message. Note again
      that we use the recv rank as the dest instead of the send rank. ---*/
@@ -531,33 +493,31 @@ void CGeometry::PostP2PSends(CGeometry *geometry,
 
     switch (commType) {
       case COMM_TYPE_DOUBLE:
-        SU2_MPI::Isend(&(bufD_P2PRecv[offset]), count, MPI_DOUBLE,
-                       dest, tag, SU2_MPI::GetComm(), &(req_P2PSend[val_iSend]));
+        SU2_MPI::Isend(&(bufD_P2PRecv[offset]), count, MPI_DOUBLE, dest, tag, SU2_MPI::GetComm(),
+                       &(req_P2PSend[val_iSend]));
         break;
       case COMM_TYPE_UNSIGNED_SHORT:
-        SU2_MPI::Isend(&(bufS_P2PRecv[offset]), count, MPI_UNSIGNED_SHORT,
-                       dest, tag, SU2_MPI::GetComm(), &(req_P2PSend[val_iSend]));
+        SU2_MPI::Isend(&(bufS_P2PRecv[offset]), count, MPI_UNSIGNED_SHORT, dest, tag, SU2_MPI::GetComm(),
+                       &(req_P2PSend[val_iSend]));
         break;
       default:
-        SU2_MPI::Error("Unrecognized data type for point-to-point MPI comms.",
-                       CURRENT_FUNCTION);
+        SU2_MPI::Error("Unrecognized data type for point-to-point MPI comms.", CURRENT_FUNCTION);
         break;
     }
 
   } else {
-
     /*--- Compute our location in the send buffer. ---*/
 
-    auto offset = countPerPoint*nPoint_P2PSend[val_iSend];
+    auto offset = countPerPoint * nPoint_P2PSend[val_iSend];
 
     /*--- Take advantage of cumulative storage format to get the number
      of points that we need to send. ---*/
 
-    auto nPointP2P = nPoint_P2PSend[val_iSend+1] - nPoint_P2PSend[val_iSend];
+    auto nPointP2P = nPoint_P2PSend[val_iSend + 1] - nPoint_P2PSend[val_iSend];
 
     /*--- Total count can include multiple pieces of data per element. ---*/
 
-    auto count = countPerPoint*nPointP2P;
+    auto count = countPerPoint * nPointP2P;
 
     /*--- Get the rank to which we send the message. ---*/
 
@@ -568,70 +528,61 @@ void CGeometry::PostP2PSends(CGeometry *geometry,
 
     switch (commType) {
       case COMM_TYPE_DOUBLE:
-        SU2_MPI::Isend(&(bufD_P2PSend[offset]), count, MPI_DOUBLE,
-                       dest, tag, SU2_MPI::GetComm(), &(req_P2PSend[val_iSend]));
+        SU2_MPI::Isend(&(bufD_P2PSend[offset]), count, MPI_DOUBLE, dest, tag, SU2_MPI::GetComm(),
+                       &(req_P2PSend[val_iSend]));
         break;
       case COMM_TYPE_UNSIGNED_SHORT:
-        SU2_MPI::Isend(&(bufS_P2PSend[offset]), count, MPI_UNSIGNED_SHORT,
-                       dest, tag, SU2_MPI::GetComm(), &(req_P2PSend[val_iSend]));
+        SU2_MPI::Isend(&(bufS_P2PSend[offset]), count, MPI_UNSIGNED_SHORT, dest, tag, SU2_MPI::GetComm(),
+                       &(req_P2PSend[val_iSend]));
         break;
       default:
-        SU2_MPI::Error("Unrecognized data type for point-to-point MPI comms.",
-                       CURRENT_FUNCTION);
+        SU2_MPI::Error("Unrecognized data type for point-to-point MPI comms.", CURRENT_FUNCTION);
         break;
     }
-
   }
   END_SU2_OMP_MASTER
-
 }
 
-void CGeometry::GetCommCountAndType(const CConfig* config,
-                                    unsigned short commType,
-                                    unsigned short &COUNT_PER_POINT,
-                                    unsigned short &MPI_TYPE) const {
+void CGeometry::GetCommCountAndType(const CConfig* config, unsigned short commType, unsigned short& COUNT_PER_POINT,
+                                    unsigned short& MPI_TYPE) const {
   switch (commType) {
     case COORDINATES:
-      COUNT_PER_POINT  = nDim;
-      MPI_TYPE         = COMM_TYPE_DOUBLE;
+      COUNT_PER_POINT = nDim;
+      MPI_TYPE = COMM_TYPE_DOUBLE;
       break;
     case GRID_VELOCITY:
-      COUNT_PER_POINT  = nDim;
-      MPI_TYPE         = COMM_TYPE_DOUBLE;
+      COUNT_PER_POINT = nDim;
+      MPI_TYPE = COMM_TYPE_DOUBLE;
       break;
     case COORDINATES_OLD:
       if (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND)
-        COUNT_PER_POINT  = nDim*2;
+        COUNT_PER_POINT = nDim * 2;
       else
-        COUNT_PER_POINT  = nDim;
-      MPI_TYPE         = COMM_TYPE_DOUBLE;
+        COUNT_PER_POINT = nDim;
+      MPI_TYPE = COMM_TYPE_DOUBLE;
       break;
     case MAX_LENGTH:
-      COUNT_PER_POINT  = 1;
-      MPI_TYPE         = COMM_TYPE_DOUBLE;
+      COUNT_PER_POINT = 1;
+      MPI_TYPE = COMM_TYPE_DOUBLE;
       break;
     case NEIGHBORS:
-      COUNT_PER_POINT  = 1;
-      MPI_TYPE         = COMM_TYPE_UNSIGNED_SHORT;
+      COUNT_PER_POINT = 1;
+      MPI_TYPE = COMM_TYPE_UNSIGNED_SHORT;
       break;
     default:
-      SU2_MPI::Error("Unrecognized quantity for point-to-point MPI comms.",
-                     CURRENT_FUNCTION);
+      SU2_MPI::Error("Unrecognized quantity for point-to-point MPI comms.", CURRENT_FUNCTION);
       break;
   }
 }
 
-void CGeometry::InitiateComms(CGeometry *geometry,
-                              const CConfig *config,
-                              unsigned short commType) const {
-
+void CGeometry::InitiateComms(CGeometry* geometry, const CConfig* config, unsigned short commType) const {
   if (nP2PSend == 0) return;
 
   /*--- Local variables ---*/
 
   unsigned short iDim;
   unsigned short COUNT_PER_POINT = 0;
-  unsigned short MPI_TYPE        = 0;
+  unsigned short MPI_TYPE = 0;
 
   unsigned long iPoint, msg_offset, buf_offset;
 
@@ -650,10 +601,10 @@ void CGeometry::InitiateComms(CGeometry *geometry,
 
   /*--- Set some local pointers to make access simpler. ---*/
 
-  su2double *bufDSend      = geometry->bufD_P2PSend;
-  unsigned short *bufSSend = geometry->bufS_P2PSend;
+  su2double* bufDSend = geometry->bufD_P2PSend;
+  unsigned short* bufSSend = geometry->bufS_P2PSend;
 
-  su2double *vector = nullptr;
+  su2double* vector = nullptr;
 
   /*--- Load the specified quantity from the solver into the generic
    communication buffer in the geometry class. ---*/
@@ -663,46 +614,42 @@ void CGeometry::InitiateComms(CGeometry *geometry,
   geometry->PostP2PRecvs(geometry, config, MPI_TYPE, COUNT_PER_POINT, false);
 
   for (iMessage = 0; iMessage < nP2PSend; iMessage++) {
-
     /*--- Get the offset in the buffer for the start of this message. ---*/
 
     msg_offset = nPoint_P2PSend[iMessage];
 
     /*--- Total count can include multiple pieces of data per element. ---*/
 
-    nSend = (nPoint_P2PSend[iMessage+1] - nPoint_P2PSend[iMessage]);
+    nSend = (nPoint_P2PSend[iMessage + 1] - nPoint_P2PSend[iMessage]);
 
     SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
     for (iSend = 0; iSend < nSend; iSend++) {
-
       /*--- Get the local index for this communicated data. ---*/
 
       iPoint = geometry->Local_Point_P2PSend[msg_offset + iSend];
 
       /*--- Compute the offset in the recv buffer for this point. ---*/
 
-      buf_offset = (msg_offset + iSend)*COUNT_PER_POINT;
+      buf_offset = (msg_offset + iSend) * COUNT_PER_POINT;
 
       switch (commType) {
         case COORDINATES:
           vector = nodes->GetCoord(iPoint);
-          for (iDim = 0; iDim < nDim; iDim++)
-            bufDSend[buf_offset+iDim] = vector[iDim];
+          for (iDim = 0; iDim < nDim; iDim++) bufDSend[buf_offset + iDim] = vector[iDim];
           break;
         case GRID_VELOCITY:
           vector = nodes->GetGridVel(iPoint);
-          for (iDim = 0; iDim < nDim; iDim++)
-            bufDSend[buf_offset+iDim] = vector[iDim];
+          for (iDim = 0; iDim < nDim; iDim++) bufDSend[buf_offset + iDim] = vector[iDim];
           break;
         case COORDINATES_OLD:
           vector = nodes->GetCoord_n(iPoint);
           for (iDim = 0; iDim < nDim; iDim++) {
-            bufDSend[buf_offset+iDim] = vector[iDim];
+            bufDSend[buf_offset + iDim] = vector[iDim];
           }
           if (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND) {
             vector = nodes->GetCoord_n1(iPoint);
             for (iDim = 0; iDim < nDim; iDim++) {
-              bufDSend[buf_offset+nDim+iDim] = vector[iDim];
+              bufDSend[buf_offset + nDim + iDim] = vector[iDim];
             }
           }
           break;
@@ -713,8 +660,7 @@ void CGeometry::InitiateComms(CGeometry *geometry,
           bufSSend[buf_offset] = geometry->nodes->GetnNeighbor(iPoint);
           break;
         default:
-          SU2_MPI::Error("Unrecognized quantity for point-to-point MPI comms.",
-                         CURRENT_FUNCTION);
+          SU2_MPI::Error("Unrecognized quantity for point-to-point MPI comms.", CURRENT_FUNCTION);
           break;
       }
     }
@@ -723,15 +669,10 @@ void CGeometry::InitiateComms(CGeometry *geometry,
     /*--- Launch the point-to-point MPI send for this message. ---*/
 
     geometry->PostP2PSends(geometry, config, MPI_TYPE, COUNT_PER_POINT, iMessage, false);
-
   }
-
 }
 
-void CGeometry::CompleteComms(CGeometry *geometry,
-                              const CConfig *config,
-                              unsigned short commType) {
-
+void CGeometry::CompleteComms(CGeometry* geometry, const CConfig* config, unsigned short commType) {
   if (nP2PRecv == 0) return;
 
   /*--- Local variables ---*/
@@ -750,8 +691,8 @@ void CGeometry::CompleteComms(CGeometry *geometry,
 
   /*--- Set some local pointers to make access simpler. ---*/
 
-  const su2double *bufDRecv      = geometry->bufD_P2PRecv;
-  const unsigned short *bufSRecv = geometry->bufS_P2PRecv;
+  const su2double* bufDRecv = geometry->bufD_P2PRecv;
+  const unsigned short* bufSRecv = geometry->bufS_P2PRecv;
 
   /*--- Store the data that was communicated into the appropriate
    location within the local class data structures. Note that we
@@ -759,7 +700,6 @@ void CGeometry::CompleteComms(CGeometry *geometry,
    non-blocking comms. ---*/
 
   for (iMessage = 0; iMessage < nP2PRecv; iMessage++) {
-
     /*--- For efficiency, recv the messages dynamically based on
      the order they arrive. ---*/
 
@@ -779,34 +719,31 @@ void CGeometry::CompleteComms(CGeometry *geometry,
 
     /*--- Get the number of packets to be received in this message. ---*/
 
-    nRecv = nPoint_P2PRecv[jRecv+1] - nPoint_P2PRecv[jRecv];
+    nRecv = nPoint_P2PRecv[jRecv + 1] - nPoint_P2PRecv[jRecv];
 
     SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
     for (iRecv = 0; iRecv < nRecv; iRecv++) {
-
       /*--- Get the local index for this communicated data. ---*/
 
       iPoint = geometry->Local_Point_P2PRecv[msg_offset + iRecv];
 
       /*--- Compute the total offset in the recv buffer for this point. ---*/
 
-      buf_offset = (msg_offset + iRecv)*COUNT_PER_POINT;
+      buf_offset = (msg_offset + iRecv) * COUNT_PER_POINT;
 
       /*--- Store the data correctly depending on the quantity. ---*/
 
       switch (commType) {
         case COORDINATES:
-          for (iDim = 0; iDim < nDim; iDim++)
-            nodes->SetCoord(iPoint, iDim, bufDRecv[buf_offset+iDim]);
+          for (iDim = 0; iDim < nDim; iDim++) nodes->SetCoord(iPoint, iDim, bufDRecv[buf_offset + iDim]);
           break;
         case GRID_VELOCITY:
-          for (iDim = 0; iDim < nDim; iDim++)
-            nodes->SetGridVel(iPoint, iDim, bufDRecv[buf_offset+iDim]);
+          for (iDim = 0; iDim < nDim; iDim++) nodes->SetGridVel(iPoint, iDim, bufDRecv[buf_offset + iDim]);
           break;
         case COORDINATES_OLD:
           nodes->SetCoord_n(iPoint, &bufDRecv[buf_offset]);
           if (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND)
-            nodes->SetCoord_n1(iPoint, &bufDRecv[buf_offset+nDim]);
+            nodes->SetCoord_n1(iPoint, &bufDRecv[buf_offset + nDim]);
           break;
         case MAX_LENGTH:
           nodes->SetMaxLength(iPoint, bufDRecv[buf_offset]);
@@ -815,8 +752,7 @@ void CGeometry::CompleteComms(CGeometry *geometry,
           nodes->SetnNeighbor(iPoint, bufSRecv[buf_offset]);
           break;
         default:
-          SU2_MPI::Error("Unrecognized quantity for point-to-point MPI comms.",
-                         CURRENT_FUNCTION);
+          SU2_MPI::Error("Unrecognized quantity for point-to-point MPI comms.", CURRENT_FUNCTION);
           break;
       }
     }
@@ -832,9 +768,7 @@ void CGeometry::CompleteComms(CGeometry *geometry,
 #endif
 }
 
-void CGeometry::PreprocessPeriodicComms(CGeometry *geometry,
-                                        CConfig *config) {
-
+void CGeometry::PreprocessPeriodicComms(CGeometry* geometry, CConfig* config) {
   /*--- We start with the send and receive lists already available in
    the form of stored periodic point-donor pairs. We will loop through
    these markers and establish the neighboring ranks and number of
@@ -854,16 +788,19 @@ void CGeometry::PreprocessPeriodicComms(CGeometry *geometry,
 
   /*--- Create some temporary structures for tracking sends/recvs. ---*/
 
-  int *nPoint_Send_All = new int[size+1]; nPoint_Send_All[0] = 0;
-  int *nPoint_Recv_All = new int[size+1]; nPoint_Recv_All[0] = 0;
-  int *nPoint_Flag     = new int[size];
+  int* nPoint_Send_All = new int[size + 1];
+  nPoint_Send_All[0] = 0;
+  int* nPoint_Recv_All = new int[size + 1];
+  nPoint_Recv_All[0] = 0;
+  int* nPoint_Flag = new int[size];
 
   for (iRank = 0; iRank < size; iRank++) {
     nPoint_Send_All[iRank] = 0;
     nPoint_Recv_All[iRank] = 0;
-    nPoint_Flag[iRank]= -1;
+    nPoint_Flag[iRank] = -1;
   }
-  nPoint_Send_All[size] = 0; nPoint_Recv_All[size] = 0;
+  nPoint_Send_All[size] = 0;
+  nPoint_Recv_All[size] = 0;
 
   /*--- Loop through all of our periodic markers and track
    our sends with each rank. ---*/
@@ -872,7 +809,6 @@ void CGeometry::PreprocessPeriodicComms(CGeometry *geometry,
     if (config->GetMarker_All_KindBC(iMarker) == PERIODIC_BOUNDARY) {
       iPeriodic = config->GetMarker_All_PerBound(iMarker);
       for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
-
         /*--- Get the current periodic point index. We only communicate
          the owned nodes on a rank, as the MPI comms will take care of
          the halos after completing the periodic comms. ---*/
@@ -880,7 +816,6 @@ void CGeometry::PreprocessPeriodicComms(CGeometry *geometry,
         iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
 
         if (geometry->nodes->GetDomain(iPoint)) {
-
           /*--- Get the rank that holds the matching periodic point
            on the other marker in the periodic pair. ---*/
 
@@ -890,23 +825,21 @@ void CGeometry::PreprocessPeriodicComms(CGeometry *geometry,
            number of points that must be sent to a particular proc. ---*/
 
           if ((nPoint_Flag[iRank] != (int)iPoint)) {
-            nPoint_Flag[iRank]    = (int)iPoint;
-            nPoint_Send_All[iRank+1] += 1;
+            nPoint_Flag[iRank] = (int)iPoint;
+            nPoint_Send_All[iRank + 1] += 1;
           }
-
         }
       }
     }
   }
 
-  delete [] nPoint_Flag;
+  delete[] nPoint_Flag;
 
   /*--- Communicate the number of points to be sent/recv'd amongst
    all processors. After this communication, each proc knows how
    many periodic points it will receive from each other processor. ---*/
 
-  SU2_MPI::Alltoall(&(nPoint_Send_All[1]), 1, MPI_INT,
-                    &(nPoint_Recv_All[1]), 1, MPI_INT, SU2_MPI::GetComm());
+  SU2_MPI::Alltoall(&(nPoint_Send_All[1]), 1, MPI_INT, &(nPoint_Recv_All[1]), 1, MPI_INT, SU2_MPI::GetComm());
 
   /*--- Check how many messages we will be sending and receiving.
    Here we also put the counters into cumulative storage format to
@@ -914,34 +847,38 @@ void CGeometry::PreprocessPeriodicComms(CGeometry *geometry,
    rank to communicate to themselves in these counters, although
    it will not be done through MPI. ---*/
 
-  nPeriodicSend = 0; nPeriodicRecv = 0;
+  nPeriodicSend = 0;
+  nPeriodicRecv = 0;
 
   for (iRank = 0; iRank < size; iRank++) {
-    if ((nPoint_Send_All[iRank+1] > 0)) nPeriodicSend++;
-    if ((nPoint_Recv_All[iRank+1] > 0)) nPeriodicRecv++;
+    if ((nPoint_Send_All[iRank + 1] > 0)) nPeriodicSend++;
+    if ((nPoint_Recv_All[iRank + 1] > 0)) nPeriodicRecv++;
 
-    nPoint_Send_All[iRank+1] += nPoint_Send_All[iRank];
-    nPoint_Recv_All[iRank+1] += nPoint_Recv_All[iRank];
+    nPoint_Send_All[iRank + 1] += nPoint_Send_All[iRank];
+    nPoint_Recv_All[iRank + 1] += nPoint_Recv_All[iRank];
   }
 
   /*--- Allocate only as much memory as needed for the periodic neighbors. ---*/
 
-  nPoint_PeriodicSend = new int[nPeriodicSend+1]; nPoint_PeriodicSend[0] = 0;
-  nPoint_PeriodicRecv = new int[nPeriodicRecv+1]; nPoint_PeriodicRecv[0] = 0;
+  nPoint_PeriodicSend = new int[nPeriodicSend + 1];
+  nPoint_PeriodicSend[0] = 0;
+  nPoint_PeriodicRecv = new int[nPeriodicRecv + 1];
+  nPoint_PeriodicRecv[0] = 0;
 
   Neighbors_PeriodicSend = new int[nPeriodicSend];
   Neighbors_PeriodicRecv = new int[nPeriodicRecv];
 
-  iSend = 0; iRecv = 0;
+  iSend = 0;
+  iRecv = 0;
   for (iRank = 0; iRank < size; iRank++) {
-    if ((nPoint_Send_All[iRank+1] > nPoint_Send_All[iRank])) {
+    if ((nPoint_Send_All[iRank + 1] > nPoint_Send_All[iRank])) {
       Neighbors_PeriodicSend[iSend] = iRank;
-      nPoint_PeriodicSend[iSend+1] = nPoint_Send_All[iRank+1];
+      nPoint_PeriodicSend[iSend + 1] = nPoint_Send_All[iRank + 1];
       iSend++;
     }
-    if ((nPoint_Recv_All[iRank+1] > nPoint_Recv_All[iRank])) {
+    if ((nPoint_Recv_All[iRank + 1] > nPoint_Recv_All[iRank])) {
       Neighbors_PeriodicRecv[iRecv] = iRank;
-      nPoint_PeriodicRecv[iRecv+1] = nPoint_Recv_All[iRank+1];
+      nPoint_PeriodicRecv[iRecv + 1] = nPoint_Recv_All[iRank + 1];
       iRecv++;
     }
   }
@@ -951,38 +888,32 @@ void CGeometry::PreprocessPeriodicComms(CGeometry *geometry,
    messages dynamically later during the iterations. ---*/
 
   PeriodicSend2Neighbor.clear();
-  for (iSend = 0; iSend < nPeriodicSend; iSend++)
-    PeriodicSend2Neighbor[Neighbors_PeriodicSend[iSend]] = iSend;
+  for (iSend = 0; iSend < nPeriodicSend; iSend++) PeriodicSend2Neighbor[Neighbors_PeriodicSend[iSend]] = iSend;
 
   PeriodicRecv2Neighbor.clear();
-  for (iRecv = 0; iRecv < nPeriodicRecv; iRecv++)
-    PeriodicRecv2Neighbor[Neighbors_PeriodicRecv[iRecv]] = iRecv;
+  for (iRecv = 0; iRecv < nPeriodicRecv; iRecv++) PeriodicRecv2Neighbor[Neighbors_PeriodicRecv[iRecv]] = iRecv;
 
-  delete [] nPoint_Send_All;
-  delete [] nPoint_Recv_All;
+  delete[] nPoint_Send_All;
+  delete[] nPoint_Recv_All;
 
   /*--- Allocate the memory to store the local index values for both
    the send and receive periodic points and periodic index. ---*/
 
   Local_Point_PeriodicSend = nullptr;
   Local_Point_PeriodicSend = new unsigned long[nPoint_PeriodicSend[nPeriodicSend]];
-  for (iSend = 0; iSend < nPoint_PeriodicSend[nPeriodicSend]; iSend++)
-    Local_Point_PeriodicSend[iSend] = 0;
+  for (iSend = 0; iSend < nPoint_PeriodicSend[nPeriodicSend]; iSend++) Local_Point_PeriodicSend[iSend] = 0;
 
   Local_Marker_PeriodicSend = nullptr;
   Local_Marker_PeriodicSend = new unsigned long[nPoint_PeriodicSend[nPeriodicSend]];
-  for (iSend = 0; iSend < nPoint_PeriodicSend[nPeriodicSend]; iSend++)
-    Local_Marker_PeriodicSend[iSend] = 0;
+  for (iSend = 0; iSend < nPoint_PeriodicSend[nPeriodicSend]; iSend++) Local_Marker_PeriodicSend[iSend] = 0;
 
   Local_Point_PeriodicRecv = nullptr;
   Local_Point_PeriodicRecv = new unsigned long[nPoint_PeriodicRecv[nPeriodicRecv]];
-  for (iRecv = 0; iRecv < nPoint_PeriodicRecv[nPeriodicRecv]; iRecv++)
-    Local_Point_PeriodicRecv[iRecv] = 0;
+  for (iRecv = 0; iRecv < nPoint_PeriodicRecv[nPeriodicRecv]; iRecv++) Local_Point_PeriodicRecv[iRecv] = 0;
 
   Local_Marker_PeriodicRecv = nullptr;
   Local_Marker_PeriodicRecv = new unsigned long[nPoint_PeriodicRecv[nPeriodicRecv]];
-  for (iRecv = 0; iRecv < nPoint_PeriodicRecv[nPeriodicRecv]; iRecv++)
-    Local_Marker_PeriodicRecv[iRecv] = 0;
+  for (iRecv = 0; iRecv < nPoint_PeriodicRecv[nPeriodicRecv]; iRecv++) Local_Marker_PeriodicRecv[iRecv] = 0;
 
   /*--- We allocate the buffers for communicating values in a later step
    once we know the maximum packet size that we need to communicate. This
@@ -998,10 +929,10 @@ void CGeometry::PreprocessPeriodicComms(CGeometry *geometry,
   /*--- Allocate memory for the MPI requests if we need to communicate. ---*/
 
   if (nPeriodicSend > 0) {
-    req_PeriodicSend   = new SU2_MPI::Request[nPeriodicSend];
+    req_PeriodicSend = new SU2_MPI::Request[nPeriodicSend];
   }
   if (nPeriodicRecv > 0) {
-    req_PeriodicRecv   = new SU2_MPI::Request[nPeriodicRecv];
+    req_PeriodicRecv = new SU2_MPI::Request[nPeriodicRecv];
   }
 
   /*--- Allocate arrays for sending the periodic point index and marker
@@ -1009,19 +940,18 @@ void CGeometry::PreprocessPeriodicComms(CGeometry *geometry,
    the recv rank can quickly loop through the buffers to unpack the data. ---*/
 
   unsigned short nPackets = 2;
-  unsigned long *idSend = new unsigned long[nPoint_PeriodicSend[nPeriodicSend]*nPackets];
-  for (iSend = 0; iSend < nPoint_PeriodicSend[nPeriodicSend]*nPackets; iSend++)
-    idSend[iSend] = 0;
+  unsigned long* idSend = new unsigned long[nPoint_PeriodicSend[nPeriodicSend] * nPackets];
+  for (iSend = 0; iSend < nPoint_PeriodicSend[nPeriodicSend] * nPackets; iSend++) idSend[iSend] = 0;
 
   /*--- Build the lists of local index and periodic marker index values. ---*/
 
-  ii = 0; jj = 0;
+  ii = 0;
+  jj = 0;
   for (iSend = 0; iSend < nPeriodicSend; iSend++) {
     for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
       if (config->GetMarker_All_KindBC(iMarker) == PERIODIC_BOUNDARY) {
         iPeriodic = config->GetMarker_All_PerBound(iMarker);
         for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
-
           /*--- Get the current periodic point index. We only communicate
            the owned nodes on a rank, as the MPI comms will take care of
            the halos after completing the periodic comms. ---*/
@@ -1029,7 +959,6 @@ void CGeometry::PreprocessPeriodicComms(CGeometry *geometry,
           iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
 
           if (geometry->nodes->GetDomain(iPoint)) {
-
             /*--- Get the rank that holds the matching periodic point
              on the other marker in the periodic pair. ---*/
 
@@ -1041,15 +970,14 @@ void CGeometry::PreprocessPeriodicComms(CGeometry *geometry,
              index to be communicated to the recv rank. ---*/
 
             if (iRank == Neighbors_PeriodicSend[iSend]) {
-              Local_Point_PeriodicSend[ii]  = iPoint;
+              Local_Point_PeriodicSend[ii] = iPoint;
               Local_Marker_PeriodicSend[ii] = (unsigned long)iMarker;
-              jj = ii*nPackets;
+              jj = ii * nPackets;
               idSend[jj] = geometry->vertex[iMarker][iVertex]->GetDonorPoint();
               jj++;
               idSend[jj] = (unsigned long)iPeriodic;
               ii++;
             }
-
           }
         }
       }
@@ -1059,9 +987,8 @@ void CGeometry::PreprocessPeriodicComms(CGeometry *geometry,
   /*--- Allocate arrays for receiving the periodic point index and marker
    index to the recv rank so that it can store the local values. ---*/
 
-  unsigned long *idRecv = new unsigned long[nPoint_PeriodicRecv[nPeriodicRecv]*nPackets];
-  for (iRecv = 0; iRecv < nPoint_PeriodicRecv[nPeriodicRecv]*nPackets; iRecv++)
-    idRecv[iRecv] = 0;
+  unsigned long* idRecv = new unsigned long[nPoint_PeriodicRecv[nPeriodicRecv] * nPackets];
+  for (iRecv = 0; iRecv < nPoint_PeriodicRecv[nPeriodicRecv] * nPackets; iRecv++) idRecv[iRecv] = 0;
 
 #ifdef HAVE_MPI
 
@@ -1073,62 +1000,56 @@ void CGeometry::PreprocessPeriodicComms(CGeometry *geometry,
 
   iMessage = 0;
   for (iRecv = 0; iRecv < nPeriodicRecv; iRecv++) {
-
     /*--- Compute our location in the recv buffer. ---*/
 
-    offset = nPackets*nPoint_PeriodicRecv[iRecv];
+    offset = nPackets * nPoint_PeriodicRecv[iRecv];
 
     /*--- Take advantage of cumulative storage format to get the number
      of elems that we need to recv. ---*/
 
-    count = nPackets*(nPoint_PeriodicRecv[iRecv+1] - nPoint_PeriodicRecv[iRecv]);
+    count = nPackets * (nPoint_PeriodicRecv[iRecv + 1] - nPoint_PeriodicRecv[iRecv]);
 
     /*--- Get the rank from which we receive the message. ---*/
 
     source = Neighbors_PeriodicRecv[iRecv];
-    tag    = source + 1;
+    tag = source + 1;
 
     /*--- Post non-blocking recv for this proc. ---*/
 
-    SU2_MPI::Irecv(&(static_cast<unsigned long*>(idRecv)[offset]),
-                   count, MPI_UNSIGNED_LONG, source, tag, SU2_MPI::GetComm(),
-                   &(req_PeriodicRecv[iMessage]));
+    SU2_MPI::Irecv(&(static_cast<unsigned long*>(idRecv)[offset]), count, MPI_UNSIGNED_LONG, source, tag,
+                   SU2_MPI::GetComm(), &(req_PeriodicRecv[iMessage]));
 
     /*--- Increment message counter. ---*/
 
     iMessage++;
-
   }
 
   /*--- Post the non-blocking sends. ---*/
 
   iMessage = 0;
   for (iSend = 0; iSend < nPeriodicSend; iSend++) {
-
     /*--- Compute our location in the send buffer. ---*/
 
-    offset = nPackets*nPoint_PeriodicSend[iSend];
+    offset = nPackets * nPoint_PeriodicSend[iSend];
 
     /*--- Take advantage of cumulative storage format to get the number
      of points that we need to send. ---*/
 
-    count = nPackets*(nPoint_PeriodicSend[iSend+1] - nPoint_PeriodicSend[iSend]);
+    count = nPackets * (nPoint_PeriodicSend[iSend + 1] - nPoint_PeriodicSend[iSend]);
 
     /*--- Get the rank to which we send the message. ---*/
 
     dest = Neighbors_PeriodicSend[iSend];
-    tag  = rank + 1;
+    tag = rank + 1;
 
     /*--- Post non-blocking send for this proc. ---*/
 
-    SU2_MPI::Isend(&(static_cast<unsigned long*>(idSend)[offset]),
-                   count, MPI_UNSIGNED_LONG, dest, tag, SU2_MPI::GetComm(),
-                   &(req_PeriodicSend[iMessage]));
+    SU2_MPI::Isend(&(static_cast<unsigned long*>(idSend)[offset]), count, MPI_UNSIGNED_LONG, dest, tag,
+                   SU2_MPI::GetComm(), &(req_PeriodicSend[iMessage]));
 
     /*--- Increment message counter. ---*/
 
     iMessage++;
-
   }
 
   /*--- Wait for the non-blocking comms to complete. ---*/
@@ -1142,10 +1063,10 @@ void CGeometry::PreprocessPeriodicComms(CGeometry *geometry,
 
   int myStart, myFinal;
   for (int val_iSend = 0; val_iSend < nPeriodicSend; val_iSend++) {
-    iRank   = geometry->PeriodicRecv2Neighbor[rank];
-    iRecv   = geometry->nPoint_PeriodicRecv[iRank]*nPackets;
-    myStart = nPoint_PeriodicSend[val_iSend]*nPackets;
-    myFinal = nPoint_PeriodicSend[val_iSend+1]*nPackets;
+    iRank = geometry->PeriodicRecv2Neighbor[rank];
+    iRecv = geometry->nPoint_PeriodicRecv[iRank] * nPackets;
+    myStart = nPoint_PeriodicSend[val_iSend] * nPackets;
+    myFinal = nPoint_PeriodicSend[val_iSend + 1] * nPackets;
     for (iSend = myStart; iSend < myFinal; iSend++) {
       idRecv[iRecv] = idSend[iSend];
       iRecv++;
@@ -1159,17 +1080,17 @@ void CGeometry::PreprocessPeriodicComms(CGeometry *geometry,
 
   ii = 0;
   for (iRecv = 0; iRecv < nPoint_PeriodicRecv[nPeriodicRecv]; iRecv++) {
-    Local_Point_PeriodicRecv[iRecv]  = idRecv[ii]; ii++;
-    Local_Marker_PeriodicRecv[iRecv] = idRecv[ii]; ii++;
+    Local_Point_PeriodicRecv[iRecv] = idRecv[ii];
+    ii++;
+    Local_Marker_PeriodicRecv[iRecv] = idRecv[ii];
+    ii++;
   }
 
-  delete [] idSend;
-  delete [] idRecv;
-
+  delete[] idSend;
+  delete[] idRecv;
 }
 
 void CGeometry::AllocatePeriodicComms(unsigned short countPerPeriodicPoint) {
-
   /*--- This routine is activated whenever we attempt to perform
    a periodic MPI communication with our neighbors but the
    memory buffer allocated is not large enough for the packet size.
@@ -1180,39 +1101,34 @@ void CGeometry::AllocatePeriodicComms(unsigned short countPerPeriodicPoint) {
   if (countPerPeriodicPoint <= maxCountPerPeriodicPoint) return;
 
   BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
+    /*--- Store the larger packet size to the class data. ---*/
 
-  /*--- Store the larger packet size to the class data. ---*/
-
-  maxCountPerPeriodicPoint = countPerPeriodicPoint;
-
-  /*--- Store the total size of the send/recv arrays for clarity. ---*/
+    maxCountPerPeriodicPoint = countPerPeriodicPoint;
 
-  auto nSend = countPerPeriodicPoint*nPoint_PeriodicSend[nPeriodicSend];
-  auto nRecv = countPerPeriodicPoint*nPoint_PeriodicRecv[nPeriodicRecv];
+    /*--- Store the total size of the send/recv arrays for clarity. ---*/
 
-  /*-- Deallocate and reallocate our cummunication memory. ---*/
+    auto nSend = countPerPeriodicPoint * nPoint_PeriodicSend[nPeriodicSend];
+    auto nRecv = countPerPeriodicPoint * nPoint_PeriodicRecv[nPeriodicRecv];
 
-  delete [] bufD_PeriodicSend;
-  bufD_PeriodicSend = new su2double[nSend] ();
+    /*-- Deallocate and reallocate our cummunication memory. ---*/
 
-  delete [] bufD_PeriodicRecv;
-  bufD_PeriodicRecv = new su2double[nRecv] ();
+    delete[] bufD_PeriodicSend;
+    bufD_PeriodicSend = new su2double[nSend]();
 
-  delete [] bufS_PeriodicSend;
-  bufS_PeriodicSend = new unsigned short[nSend] ();
+    delete[] bufD_PeriodicRecv;
+    bufD_PeriodicRecv = new su2double[nRecv]();
 
-  delete [] bufS_PeriodicRecv;
-  bufS_PeriodicRecv = new unsigned short[nRecv] ();
+    delete[] bufS_PeriodicSend;
+    bufS_PeriodicSend = new unsigned short[nSend]();
 
+    delete[] bufS_PeriodicRecv;
+    bufS_PeriodicRecv = new unsigned short[nRecv]();
   }
   END_SU2_OMP_SAFE_GLOBAL_ACCESS
 }
 
-void CGeometry::PostPeriodicRecvs(CGeometry *geometry,
-                                  const CConfig *config,
-                                  unsigned short commType,
+void CGeometry::PostPeriodicRecvs(CGeometry* geometry, const CConfig* config, unsigned short commType,
                                   unsigned short countPerPeriodicPoint) {
-
   /*--- In parallel, communicate the data with non-blocking send/recv. ---*/
 
 #ifdef HAVE_MPI
@@ -1223,19 +1139,18 @@ void CGeometry::PostPeriodicRecvs(CGeometry *geometry,
 
   SU2_OMP_MASTER
   for (int iRecv = 0; iRecv < nPeriodicRecv; iRecv++) {
-
     /*--- Compute our location in the recv buffer. ---*/
 
-    auto offset = countPerPeriodicPoint*nPoint_PeriodicRecv[iRecv];
+    auto offset = countPerPeriodicPoint * nPoint_PeriodicRecv[iRecv];
 
     /*--- Take advantage of cumulative storage format to get the number
      of elems that we need to recv. ---*/
 
-    auto nPointPeriodic = nPoint_PeriodicRecv[iRecv+1] - nPoint_PeriodicRecv[iRecv];
+    auto nPointPeriodic = nPoint_PeriodicRecv[iRecv + 1] - nPoint_PeriodicRecv[iRecv];
 
     /*--- Total count can include multiple pieces of data per element. ---*/
 
-    auto count = countPerPeriodicPoint*nPointPeriodic;
+    auto count = countPerPeriodicPoint * nPointPeriodic;
 
     /*--- Get the rank from which we receive the message. ---*/
 
@@ -1246,77 +1161,64 @@ void CGeometry::PostPeriodicRecvs(CGeometry *geometry,
 
     switch (commType) {
       case COMM_TYPE_DOUBLE:
-        SU2_MPI::Irecv(&(static_cast<su2double*>(bufD_PeriodicRecv)[offset]),
-                       count, MPI_DOUBLE, source, tag, SU2_MPI::GetComm(),
-                       &(req_PeriodicRecv[iRecv]));
+        SU2_MPI::Irecv(&(static_cast<su2double*>(bufD_PeriodicRecv)[offset]), count, MPI_DOUBLE, source, tag,
+                       SU2_MPI::GetComm(), &(req_PeriodicRecv[iRecv]));
         break;
       case COMM_TYPE_UNSIGNED_SHORT:
-        SU2_MPI::Irecv(&(static_cast<unsigned short*>(bufS_PeriodicRecv)[offset]),
-                       count, MPI_UNSIGNED_SHORT, source, tag, SU2_MPI::GetComm(),
-                       &(req_PeriodicRecv[iRecv]));
+        SU2_MPI::Irecv(&(static_cast<unsigned short*>(bufS_PeriodicRecv)[offset]), count, MPI_UNSIGNED_SHORT, source,
+                       tag, SU2_MPI::GetComm(), &(req_PeriodicRecv[iRecv]));
         break;
       default:
-        SU2_MPI::Error("Unrecognized data type for periodic MPI comms.",
-                       CURRENT_FUNCTION);
+        SU2_MPI::Error("Unrecognized data type for periodic MPI comms.", CURRENT_FUNCTION);
         break;
     }
-
   }
   END_SU2_OMP_MASTER
 
 #endif
-
 }
 
-void CGeometry::PostPeriodicSends(CGeometry *geometry,
-                                  const CConfig *config,
-                                  unsigned short commType,
-                                  unsigned short countPerPeriodicPoint,
-                                  int val_iSend) const {
-
+void CGeometry::PostPeriodicSends(CGeometry* geometry, const CConfig* config, unsigned short commType,
+                                  unsigned short countPerPeriodicPoint, int val_iSend) const {
   /*--- In parallel, communicate the data with non-blocking send/recv. ---*/
 
 #ifdef HAVE_MPI
   SU2_OMP_MASTER {
-  /*--- Post the non-blocking send as soon as the buffer is loaded. ---*/
+    /*--- Post the non-blocking send as soon as the buffer is loaded. ---*/
 
-  /*--- Compute our location in the send buffer. ---*/
+    /*--- Compute our location in the send buffer. ---*/
 
-  auto offset = countPerPeriodicPoint*nPoint_PeriodicSend[val_iSend];
+    auto offset = countPerPeriodicPoint * nPoint_PeriodicSend[val_iSend];
 
-  /*--- Take advantage of cumulative storage format to get the number
-   of points that we need to send. ---*/
+    /*--- Take advantage of cumulative storage format to get the number
+     of points that we need to send. ---*/
 
-  auto nPointPeriodic = (nPoint_PeriodicSend[val_iSend+1] -
-                         nPoint_PeriodicSend[val_iSend]);
+    auto nPointPeriodic = (nPoint_PeriodicSend[val_iSend + 1] - nPoint_PeriodicSend[val_iSend]);
 
-  /*--- Total count can include multiple pieces of data per element. ---*/
+    /*--- Total count can include multiple pieces of data per element. ---*/
 
-  auto count = countPerPeriodicPoint*nPointPeriodic;
+    auto count = countPerPeriodicPoint * nPointPeriodic;
 
-  /*--- Get the rank to which we send the message. ---*/
+    /*--- Get the rank to which we send the message. ---*/
 
-  auto dest = Neighbors_PeriodicSend[val_iSend];
-  auto tag = rank + 1;
+    auto dest = Neighbors_PeriodicSend[val_iSend];
+    auto tag = rank + 1;
 
-  /*--- Post non-blocking send for this proc. ---*/
+    /*--- Post non-blocking send for this proc. ---*/
 
-  switch (commType) {
-    case COMM_TYPE_DOUBLE:
-      SU2_MPI::Isend(&(static_cast<su2double*>(bufD_PeriodicSend)[offset]),
-                     count, MPI_DOUBLE, dest, tag, SU2_MPI::GetComm(),
-                     &(req_PeriodicSend[val_iSend]));
-      break;
-    case COMM_TYPE_UNSIGNED_SHORT:
-      SU2_MPI::Isend(&(static_cast<unsigned short*>(bufS_PeriodicSend)[offset]),
-                     count, MPI_UNSIGNED_SHORT, dest, tag, SU2_MPI::GetComm(),
-                     &(req_PeriodicSend[val_iSend]));
-      break;
-    default:
-      SU2_MPI::Error("Unrecognized data type for periodic MPI comms.",
-                     CURRENT_FUNCTION);
-      break;
-  }
+    switch (commType) {
+      case COMM_TYPE_DOUBLE:
+        SU2_MPI::Isend(&(static_cast<su2double*>(bufD_PeriodicSend)[offset]), count, MPI_DOUBLE, dest, tag,
+                       SU2_MPI::GetComm(), &(req_PeriodicSend[val_iSend]));
+        break;
+      case COMM_TYPE_UNSIGNED_SHORT:
+        SU2_MPI::Isend(&(static_cast<unsigned short*>(bufS_PeriodicSend)[offset]), count, MPI_UNSIGNED_SHORT, dest, tag,
+                       SU2_MPI::GetComm(), &(req_PeriodicSend[val_iSend]));
+        break;
+      default:
+        SU2_MPI::Error("Unrecognized data type for periodic MPI comms.", CURRENT_FUNCTION);
+        break;
+    }
   }
   END_SU2_OMP_MASTER
 #else
@@ -1324,54 +1226,51 @@ void CGeometry::PostPeriodicSends(CGeometry *geometry,
   /*--- Copy my own rank's data into the recv buffer directly in serial. ---*/
 
   int myStart, myFinal, iRecv, iRank;
-  iRank   = geometry->PeriodicRecv2Neighbor[rank];
-  iRecv   = geometry->nPoint_PeriodicRecv[iRank]*countPerPeriodicPoint;
-  myStart = nPoint_PeriodicSend[val_iSend]*countPerPeriodicPoint;
-  myFinal = nPoint_PeriodicSend[val_iSend+1]*countPerPeriodicPoint;
+  iRank = geometry->PeriodicRecv2Neighbor[rank];
+  iRecv = geometry->nPoint_PeriodicRecv[iRank] * countPerPeriodicPoint;
+  myStart = nPoint_PeriodicSend[val_iSend] * countPerPeriodicPoint;
+  myFinal = nPoint_PeriodicSend[val_iSend + 1] * countPerPeriodicPoint;
 
   switch (commType) {
     case COMM_TYPE_DOUBLE:
-      parallelCopy(myFinal-myStart, &bufD_PeriodicSend[myStart], &bufD_PeriodicRecv[iRecv]);
+      parallelCopy(myFinal - myStart, &bufD_PeriodicSend[myStart], &bufD_PeriodicRecv[iRecv]);
       break;
     case COMM_TYPE_UNSIGNED_SHORT:
-      parallelCopy(myFinal-myStart, &bufS_PeriodicSend[myStart], &bufS_PeriodicRecv[iRecv]);
+      parallelCopy(myFinal - myStart, &bufS_PeriodicSend[myStart], &bufS_PeriodicRecv[iRecv]);
       break;
     default:
-      SU2_MPI::Error("Unrecognized data type for periodic MPI comms.",
-                     CURRENT_FUNCTION);
+      SU2_MPI::Error("Unrecognized data type for periodic MPI comms.", CURRENT_FUNCTION);
       break;
   }
 
 #endif
-
 }
 
-su2double CGeometry::Point2Plane_Distance(const su2double *Coord, const su2double *iCoord, const su2double *jCoord, const su2double *kCoord) {
+su2double CGeometry::Point2Plane_Distance(const su2double* Coord, const su2double* iCoord, const su2double* jCoord,
+                                          const su2double* kCoord) {
   su2double CrossProduct[3], iVector[3], jVector[3], distance, modulus;
   unsigned short iDim;
 
-  for (iDim = 0; iDim < 3; iDim ++) {
+  for (iDim = 0; iDim < 3; iDim++) {
     iVector[iDim] = jCoord[iDim] - iCoord[iDim];
     jVector[iDim] = kCoord[iDim] - iCoord[iDim];
   }
 
-  CrossProduct[0] = iVector[1]*jVector[2] - iVector[2]*jVector[1];
-  CrossProduct[1] = iVector[2]*jVector[0] - iVector[0]*jVector[2];
-  CrossProduct[2] = iVector[0]*jVector[1] - iVector[1]*jVector[0];
+  CrossProduct[0] = iVector[1] * jVector[2] - iVector[2] * jVector[1];
+  CrossProduct[1] = iVector[2] * jVector[0] - iVector[0] * jVector[2];
+  CrossProduct[2] = iVector[0] * jVector[1] - iVector[1] * jVector[0];
 
-  modulus = sqrt(CrossProduct[0]*CrossProduct[0]+CrossProduct[1]*CrossProduct[1]+CrossProduct[2]*CrossProduct[2]);
+  modulus =
+      sqrt(CrossProduct[0] * CrossProduct[0] + CrossProduct[1] * CrossProduct[1] + CrossProduct[2] * CrossProduct[2]);
 
   distance = 0.0;
-  for (iDim = 0; iDim < 3; iDim ++)
-    distance += CrossProduct[iDim]*(Coord[iDim]-iCoord[iDim]);
+  for (iDim = 0; iDim < 3; iDim++) distance += CrossProduct[iDim] * (Coord[iDim] - iCoord[iDim]);
   distance /= modulus;
 
   return distance;
-
 }
 
 void CGeometry::SetEdges(void) {
-
   nEdge = 0;
   for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
     for (auto iNode = 0u; iNode < nodes->GetnPoint(iPoint); iNode++) {
@@ -1390,7 +1289,7 @@ void CGeometry::SetEdges(void) {
     }
   }
 
-  edges = new CEdge(nEdge,nDim);
+  edges = new CEdge(nEdge, nDim);
 
   for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
     for (auto jPoint : nodes->GetPoints(iPoint)) {
@@ -1435,20 +1334,18 @@ void CGeometry::SetFaces(void) {
 }
 
 void CGeometry::TestGeometry(void) const {
-
   ofstream para_file;
 
   para_file.open("test_geometry.dat", ios::out);
 
-  su2double *Normal = new su2double[nDim];
+  su2double* Normal = new su2double[nDim];
 
   for (unsigned long iEdge = 0; iEdge < nEdge; iEdge++) {
     para_file << "Edge index: " << iEdge << endl;
-    para_file << "   Point index: " << edges->GetNode(iEdge,0) << "\t" << edges->GetNode(iEdge,1) << endl;
-    edges->GetNormal(iEdge,Normal);
+    para_file << "   Point index: " << edges->GetNode(iEdge, 0) << "\t" << edges->GetNode(iEdge, 1) << endl;
+    edges->GetNormal(iEdge, Normal);
     para_file << "      Face normal : ";
-    for (unsigned short iDim = 0; iDim < nDim; iDim++)
-      para_file << Normal[iDim] << "\t";
+    for (unsigned short iDim = 0; iDim < nDim; iDim++) para_file << Normal[iDim] << "\t";
     para_file << endl;
   }
 
@@ -1457,52 +1354,53 @@ void CGeometry::TestGeometry(void) const {
   para_file << endl;
   para_file << endl;
 
-  for (unsigned short iMarker =0; iMarker < nMarker; iMarker++) {
+  for (unsigned short iMarker = 0; iMarker < nMarker; iMarker++) {
     para_file << "Marker index: " << iMarker << endl;
     for (unsigned long iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
       para_file << "   Vertex index: " << iVertex << endl;
       para_file << "      Point index: " << vertex[iMarker][iVertex]->GetNode() << endl;
       para_file << "      Point coordinates : ";
       for (unsigned short iDim = 0; iDim < nDim; iDim++) {
-        para_file << nodes->GetCoord(vertex[iMarker][iVertex]->GetNode(), iDim) << "\t";}
+        para_file << nodes->GetCoord(vertex[iMarker][iVertex]->GetNode(), iDim) << "\t";
+      }
       para_file << endl;
       vertex[iMarker][iVertex]->GetNormal(Normal);
       para_file << "         Face normal : ";
-      for (unsigned short iDim = 0; iDim < nDim; iDim++)
-        para_file << Normal[iDim] << "\t";
+      for (unsigned short iDim = 0; iDim < nDim; iDim++) para_file << Normal[iDim] << "\t";
       para_file << endl;
     }
   }
 
-  delete [] Normal;
-
+  delete[] Normal;
 }
 
-bool CGeometry::SegmentIntersectsPlane(const su2double *Segment_P0, const su2double *Segment_P1, su2double Variable_P0, su2double Variable_P1,
-                                       const su2double *Plane_P0, const su2double *Plane_Normal, su2double *Intersection, su2double &Variable_Interp) {
+bool CGeometry::SegmentIntersectsPlane(const su2double* Segment_P0, const su2double* Segment_P1, su2double Variable_P0,
+                                       su2double Variable_P1, const su2double* Plane_P0, const su2double* Plane_Normal,
+                                       su2double* Intersection, su2double& Variable_Interp) {
   su2double u[3], v[3], Denominator, Numerator, Aux, ModU;
-  su2double epsilon = 1E-6; // An epsilon is added to eliminate, as much as possible, the posibility of a line that intersects a point
+  su2double epsilon =
+      1E-6;  // An epsilon is added to eliminate, as much as possible, the posibility of a line that intersects a point
   unsigned short iDim;
 
   for (iDim = 0; iDim < 3; iDim++) {
     u[iDim] = Segment_P1[iDim] - Segment_P0[iDim];
-    v[iDim] = (Plane_P0[iDim]+epsilon) - Segment_P0[iDim];
+    v[iDim] = (Plane_P0[iDim] + epsilon) - Segment_P0[iDim];
   }
 
-  ModU = sqrt(u[0]*u[0]+u[1]*u[1]+u[2]*u[2]);
+  ModU = sqrt(u[0] * u[0] + u[1] * u[1] + u[2] * u[2]);
 
-  Numerator = (Plane_Normal[0]+epsilon)*v[0] + (Plane_Normal[1]+epsilon)*v[1] + (Plane_Normal[2]+epsilon)*v[2];
-  Denominator = (Plane_Normal[0]+epsilon)*u[0] + (Plane_Normal[1]+epsilon)*u[1] + (Plane_Normal[2]+epsilon)*u[2];
+  Numerator =
+      (Plane_Normal[0] + epsilon) * v[0] + (Plane_Normal[1] + epsilon) * v[1] + (Plane_Normal[2] + epsilon) * v[2];
+  Denominator =
+      (Plane_Normal[0] + epsilon) * u[0] + (Plane_Normal[1] + epsilon) * u[1] + (Plane_Normal[2] + epsilon) * u[2];
 
-  if (fabs(Denominator) <= 0.0) return (false); // No intersection.
+  if (fabs(Denominator) <= 0.0) return (false);  // No intersection.
 
   Aux = Numerator / Denominator;
 
-  if (Aux < 0.0 || Aux > 1.0) return (false); // No intersection.
-
-  for (iDim = 0; iDim < 3; iDim++)
-    Intersection[iDim] = Segment_P0[iDim] + Aux * u[iDim];
+  if (Aux < 0.0 || Aux > 1.0) return (false);  // No intersection.
 
+  for (iDim = 0; iDim < 3; iDim++) Intersection[iDim] = Segment_P0[iDim] + Aux * u[iDim];
 
   /*--- Check that the intersection is in the segment ---*/
 
@@ -1511,23 +1409,22 @@ bool CGeometry::SegmentIntersectsPlane(const su2double *Segment_P0, const su2dou
     v[iDim] = Segment_P1[iDim] - Intersection[iDim];
   }
 
-  Variable_Interp = Variable_P0 + (Variable_P1 - Variable_P0)*sqrt(u[0]*u[0]+u[1]*u[1]+u[2]*u[2])/ModU;
+  Variable_Interp = Variable_P0 + (Variable_P1 - Variable_P0) * sqrt(u[0] * u[0] + u[1] * u[1] + u[2] * u[2]) / ModU;
 
-  Denominator = (Plane_Normal[0]+epsilon)*u[0] + (Plane_Normal[1]+epsilon)*u[1] + (Plane_Normal[2]+epsilon)*u[2];
-  Numerator = (Plane_Normal[0]+epsilon)*v[0] + (Plane_Normal[1]+epsilon)*v[1] + (Plane_Normal[2]+epsilon)*v[2];
+  Denominator =
+      (Plane_Normal[0] + epsilon) * u[0] + (Plane_Normal[1] + epsilon) * u[1] + (Plane_Normal[2] + epsilon) * u[2];
+  Numerator =
+      (Plane_Normal[0] + epsilon) * v[0] + (Plane_Normal[1] + epsilon) * v[1] + (Plane_Normal[2] + epsilon) * v[2];
 
   Aux = Numerator * Denominator;
 
-  if (Aux > 0.0) return (false); // Intersection outside the segment.
+  if (Aux > 0.0) return (false);  // Intersection outside the segment.
 
   return (true);
-
 }
 
-bool CGeometry::RayIntersectsTriangle(const su2double orig[3], const su2double dir[3],
-                                      const su2double vert0[3], const su2double vert1[3], const su2double vert2[3],
-                                      su2double *intersect) {
-
+bool CGeometry::RayIntersectsTriangle(const su2double orig[3], const su2double dir[3], const su2double vert0[3],
+                                      const su2double vert1[3], const su2double vert2[3], su2double* intersect) {
   const passivedouble epsilon = 0.000001;
   su2double edge1[3], edge2[3], tvec[3], pvec[3], qvec[3];
   su2double det, inv_det, t, u, v;
@@ -1545,8 +1442,7 @@ bool CGeometry::RayIntersectsTriangle(const su2double orig[3], const su2double d
 
   det = GeometryToolbox::DotProduct(3, edge1, pvec);
 
-
-  if (fabs(det) < epsilon) return(false);
+  if (fabs(det) < epsilon) return (false);
 
   inv_det = 1.0 / det;
 
@@ -1558,7 +1454,7 @@ bool CGeometry::RayIntersectsTriangle(const su2double orig[3], const su2double d
 
   u = inv_det * GeometryToolbox::DotProduct(3, tvec, pvec);
 
-  if (u < 0.0 || u > 1.0) return(false);
+  if (u < 0.0 || u > 1.0) return (false);
 
   /*--- prepare to test V parameter ---*/
 
@@ -1568,7 +1464,7 @@ bool CGeometry::RayIntersectsTriangle(const su2double orig[3], const su2double d
 
   v = inv_det * GeometryToolbox::DotProduct(3, dir, qvec);
 
-  if (v < 0.0 || u + v > 1.0) return(false);
+  if (v < 0.0 || u + v > 1.0) return (false);
 
   /*--- Calculate t, ray intersects triangle ---*/
 
@@ -1581,11 +1477,10 @@ bool CGeometry::RayIntersectsTriangle(const su2double orig[3], const su2double d
   intersect[2] = orig[2] + (t * dir[2]);
 
   return (true);
-
 }
 
-bool CGeometry::SegmentIntersectsLine(const su2double point0[2], const su2double point1[2], const su2double vert0[2], const su2double vert1[2]) {
-
+bool CGeometry::SegmentIntersectsLine(const su2double point0[2], const su2double point1[2], const su2double vert0[2],
+                                      const su2double vert1[2]) {
   su2double det, diff0_A, diff0_B, diff1_A, diff1_B, intersect[2];
 
   diff0_A = point0[0] - point1[0];
@@ -1594,48 +1489,46 @@ bool CGeometry::SegmentIntersectsLine(const su2double point0[2], const su2double
   diff0_B = vert0[0] - vert1[0];
   diff1_B = vert0[1] - vert1[1];
 
-  det = (diff0_A)*(diff1_B) - (diff1_A)*(diff0_B);
+  det = (diff0_A) * (diff1_B) - (diff1_A) * (diff0_B);
 
   if (det == 0) return false;
 
   /*--- Compute point of intersection ---*/
 
-  intersect[0] = ((point0[0]*point1[1] - point0[1]*point1[0])*diff0_B
-                -(vert0[0]* vert1[1]  - vert0[1]* vert1[0])*diff0_A)/det;
-
-  intersect[1] =  ((point0[0]*point1[1] - point0[1]*point1[0])*diff1_B
-                  -(vert0[0]* vert1[1]  - vert0[1]* vert1[0])*diff1_A)/det;
+  intersect[0] = ((point0[0] * point1[1] - point0[1] * point1[0]) * diff0_B -
+                  (vert0[0] * vert1[1] - vert0[1] * vert1[0]) * diff0_A) /
+                 det;
 
+  intersect[1] = ((point0[0] * point1[1] - point0[1] * point1[0]) * diff1_B -
+                  (vert0[0] * vert1[1] - vert0[1] * vert1[0]) * diff1_A) /
+                 det;
 
   /*--- Check that the point is between the two surface points ---*/
 
   su2double dist0, dist1, length;
 
-  dist0 = (intersect[0] - point0[0])*(intersect[0] - point0[0])
-         +(intersect[1] - point0[1])*(intersect[1] - point0[1]);
+  dist0 =
+      (intersect[0] - point0[0]) * (intersect[0] - point0[0]) + (intersect[1] - point0[1]) * (intersect[1] - point0[1]);
 
-  dist1 = (intersect[0] - point1[0])*(intersect[0] - point1[0])
-         +(intersect[1] - point1[1])*(intersect[1] - point1[1]);
+  dist1 =
+      (intersect[0] - point1[0]) * (intersect[0] - point1[0]) + (intersect[1] - point1[1]) * (intersect[1] - point1[1]);
 
-  length = diff0_A*diff0_A
-          +diff1_A*diff1_A;
+  length = diff0_A * diff0_A + diff1_A * diff1_A;
 
-  if ( (dist0 > length) || (dist1 > length) ) {
+  if ((dist0 > length) || (dist1 > length)) {
     return false;
   }
 
   return true;
 }
 
-bool CGeometry::SegmentIntersectsTriangle(su2double point0[3], const su2double point1[3],
-                                          su2double vert0[3], su2double vert1[3], su2double vert2[3]) {
-
+bool CGeometry::SegmentIntersectsTriangle(su2double point0[3], const su2double point1[3], su2double vert0[3],
+                                          su2double vert1[3], su2double vert2[3]) {
   su2double dir[3], intersect[3], u[3], v[3], edge1[3], edge2[3], Plane_Normal[3], Denominator, Numerator, Aux;
 
   GeometryToolbox::Distance(3, point1, point0, dir);
 
   if (RayIntersectsTriangle(point0, dir, vert0, vert1, vert2, intersect)) {
-
     /*--- Check that the intersection is in the segment ---*/
 
     GeometryToolbox::Distance(3, point0, intersect, u);
@@ -1654,45 +1547,41 @@ bool CGeometry::SegmentIntersectsTriangle(su2double point0[3], const su2double p
 
     if (Aux > 0.0) return (false);
 
-  }
-  else {
-
+  } else {
     /*--- No intersection with the ray ---*/
 
     return (false);
-
   }
 
   /*--- Intersection inside the segment ---*/
 
   return (true);
-
 }
 
-void CGeometry::ComputeAirfoil_Section(su2double *Plane_P0, su2double *Plane_Normal,
-                                       su2double MinXCoord, su2double MaxXCoord,
-                                       su2double MinYCoord, su2double MaxYCoord,
-                                       su2double MinZCoord, su2double MaxZCoord,
-                                       const su2double *FlowVariable,
-                                       vector<su2double> &Xcoord_Airfoil, vector<su2double> &Ycoord_Airfoil,
-                                       vector<su2double> &Zcoord_Airfoil, vector<su2double> &Variable_Airfoil,
-                                       bool original_surface, CConfig *config) {
-
+void CGeometry::ComputeAirfoil_Section(su2double* Plane_P0, su2double* Plane_Normal, su2double MinXCoord,
+                                       su2double MaxXCoord, su2double MinYCoord, su2double MaxYCoord,
+                                       su2double MinZCoord, su2double MaxZCoord, const su2double* FlowVariable,
+                                       vector<su2double>& Xcoord_Airfoil, vector<su2double>& Ycoord_Airfoil,
+                                       vector<su2double>& Zcoord_Airfoil, vector<su2double>& Variable_Airfoil,
+                                       bool original_surface, CConfig* config) {
   const bool wasActive = AD::BeginPassive();
 
   unsigned short iMarker, iNode, jNode, iDim, Index = 0;
   bool intersect;
   long Next_Edge = 0;
   unsigned long iPoint, jPoint, iElem, Trailing_Point, Airfoil_Point, iVertex, iEdge, PointIndex, jEdge;
-  su2double Segment_P0[3] = {0.0, 0.0, 0.0}, Segment_P1[3] = {0.0, 0.0, 0.0}, Variable_P0 = 0.0, Variable_P1 = 0.0, Intersection[3] = {0.0, 0.0, 0.0}, Trailing_Coord,
-  *VarCoord = nullptr, Variable_Interp, v1[3] = {0.0, 0.0, 0.0}, v3[3] = {0.0, 0.0, 0.0}, CrossProduct = 1.0;
+  su2double Segment_P0[3] = {0.0, 0.0, 0.0}, Segment_P1[3] = {0.0, 0.0, 0.0}, Variable_P0 = 0.0, Variable_P1 = 0.0,
+            Intersection[3] = {0.0, 0.0, 0.0}, Trailing_Coord, *VarCoord = nullptr, Variable_Interp,
+            v1[3] = {0.0, 0.0, 0.0}, v3[3] = {0.0, 0.0, 0.0}, CrossProduct = 1.0;
   bool Found_Edge;
   passivedouble Dist_Value;
-  vector<su2double> Xcoord_Index0, Ycoord_Index0, Zcoord_Index0, Variable_Index0, Xcoord_Index1, Ycoord_Index1, Zcoord_Index1, Variable_Index1;
-  vector<unsigned long> IGlobalID_Index0, JGlobalID_Index0, IGlobalID_Index1, JGlobalID_Index1, IGlobalID_Airfoil, JGlobalID_Airfoil;
+  vector<su2double> Xcoord_Index0, Ycoord_Index0, Zcoord_Index0, Variable_Index0, Xcoord_Index1, Ycoord_Index1,
+      Zcoord_Index1, Variable_Index1;
+  vector<unsigned long> IGlobalID_Index0, JGlobalID_Index0, IGlobalID_Index1, JGlobalID_Index1, IGlobalID_Airfoil,
+      JGlobalID_Airfoil;
   vector<unsigned short> Conection_Index0, Conection_Index1;
   vector<unsigned long> Duplicate;
-  su2double **Coord_Variation = nullptr;
+  su2double** Coord_Variation = nullptr;
   vector<su2double> XcoordExtra, YcoordExtra, ZcoordExtra, VariableExtra;
   vector<unsigned long> IGlobalIDExtra, JGlobalIDExtra;
   vector<bool> AddExtra;
@@ -1700,7 +1589,8 @@ void CGeometry::ComputeAirfoil_Section(su2double *Plane_P0, su2double *Plane_Nor
   bool FoundEdge;
 
 #ifdef HAVE_MPI
-  unsigned long nLocalEdge, MaxLocalEdge, *Buffer_Send_nEdge, *Buffer_Receive_nEdge, nBuffer_Coord, nBuffer_Variable, nBuffer_GlobalID;
+  unsigned long nLocalEdge, MaxLocalEdge, *Buffer_Send_nEdge, *Buffer_Receive_nEdge, nBuffer_Coord, nBuffer_Variable,
+      nBuffer_GlobalID;
   int nProcessor, iProcessor;
   su2double *Buffer_Send_Coord, *Buffer_Receive_Coord;
   su2double *Buffer_Send_Variable, *Buffer_Receive_Variable;
@@ -1717,39 +1607,36 @@ void CGeometry::ComputeAirfoil_Section(su2double *Plane_P0, su2double *Plane_Nor
   /*--- Set the right plane in 2D (note the change in Y-Z plane) ---*/
 
   if (nDim == 2) {
-    Plane_P0[0] = 0.0;      Plane_P0[1] = 0.0;      Plane_P0[2] = 0.0;
-    Plane_Normal[0] = 0.0;  Plane_Normal[1] = 1.0;  Plane_Normal[2] = 0.0;
+    Plane_P0[0] = 0.0;
+    Plane_P0[1] = 0.0;
+    Plane_P0[2] = 0.0;
+    Plane_Normal[0] = 0.0;
+    Plane_Normal[1] = 1.0;
+    Plane_Normal[2] = 0.0;
   }
 
   /*--- Grid movement is stored using a vertices information,
    we should go from vertex to points ---*/
 
   if (original_surface == false) {
-
-    Coord_Variation = new su2double *[nPoint];
-    for (iPoint = 0; iPoint < nPoint; iPoint++)
-      Coord_Variation[iPoint] = new su2double [nDim];
+    Coord_Variation = new su2double*[nPoint];
+    for (iPoint = 0; iPoint < nPoint; iPoint++) Coord_Variation[iPoint] = new su2double[nDim];
 
     for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
       if (config->GetMarker_All_GeoEval(iMarker) == YES) {
         for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
           VarCoord = vertex[iMarker][iVertex]->GetVarCoord();
           iPoint = vertex[iMarker][iVertex]->GetNode();
-          for (iDim = 0; iDim < nDim; iDim++)
-            Coord_Variation[iPoint][iDim] = VarCoord[iDim];
+          for (iDim = 0; iDim < nDim; iDim++) Coord_Variation[iPoint][iDim] = VarCoord[iDim];
         }
       }
     }
-
   }
 
   for (iMarker = 0; iMarker < nMarker; iMarker++) {
-
     if (config->GetMarker_All_GeoEval(iMarker) == YES) {
-
       for (iElem = 0; iElem < nElem_Bound[iMarker]; iElem++) {
-
-        PointIndex=0;
+        PointIndex = 0;
 
         /*--- To decide if an element is going to be used or not should be done element based,
          The first step is to compute and average coordinate for the element ---*/
@@ -1776,9 +1663,8 @@ void CGeometry::ComputeAirfoil_Section(su2double *Plane_P0, su2double *Plane_Nor
         CrossProduct = 1.0;
 
         if (config->GetGeo_Description() == NACELLE) {
-
-          su2double Tilt_Angle = config->GetNacelleLocation(3)*PI_NUMBER/180;
-          su2double Toe_Angle = config->GetNacelleLocation(4)*PI_NUMBER/180;
+          su2double Tilt_Angle = config->GetNacelleLocation(3) * PI_NUMBER / 180;
+          su2double Toe_Angle = config->GetNacelleLocation(4) * PI_NUMBER / 180;
 
           /*--- Translate to the origin ---*/
 
@@ -1788,57 +1674,58 @@ void CGeometry::ComputeAirfoil_Section(su2double *Plane_P0, su2double *Plane_Nor
 
           /*--- Apply tilt angle ---*/
 
-          su2double XCoord_Trans_Tilt = XCoord_Trans*cos(Tilt_Angle) + ZCoord_Trans*sin(Tilt_Angle);
+          su2double XCoord_Trans_Tilt = XCoord_Trans * cos(Tilt_Angle) + ZCoord_Trans * sin(Tilt_Angle);
           su2double YCoord_Trans_Tilt = YCoord_Trans;
-          su2double ZCoord_Trans_Tilt = ZCoord_Trans*cos(Tilt_Angle) - XCoord_Trans*sin(Tilt_Angle);
+          su2double ZCoord_Trans_Tilt = ZCoord_Trans * cos(Tilt_Angle) - XCoord_Trans * sin(Tilt_Angle);
 
           /*--- Apply toe angle ---*/
 
-          su2double YCoord_Trans_Tilt_Toe = XCoord_Trans_Tilt*sin(Toe_Angle) + YCoord_Trans_Tilt*cos(Toe_Angle);
+          su2double YCoord_Trans_Tilt_Toe = XCoord_Trans_Tilt * sin(Toe_Angle) + YCoord_Trans_Tilt * cos(Toe_Angle);
           su2double ZCoord_Trans_Tilt_Toe = ZCoord_Trans_Tilt;
 
           /*--- Undo plane rotation, we have already rotated the nacelle ---*/
 
           /*--- Undo tilt angle ---*/
 
-          su2double XPlane_Normal_Tilt = Plane_Normal[0]*cos(-Tilt_Angle) + Plane_Normal[2]*sin(-Tilt_Angle);
+          su2double XPlane_Normal_Tilt = Plane_Normal[0] * cos(-Tilt_Angle) + Plane_Normal[2] * sin(-Tilt_Angle);
           su2double YPlane_Normal_Tilt = Plane_Normal[1];
-          su2double ZPlane_Normal_Tilt = Plane_Normal[2]*cos(-Tilt_Angle) - Plane_Normal[0]*sin(-Tilt_Angle);
+          su2double ZPlane_Normal_Tilt = Plane_Normal[2] * cos(-Tilt_Angle) - Plane_Normal[0] * sin(-Tilt_Angle);
 
           /*--- Undo toe angle ---*/
 
-          su2double YPlane_Normal_Tilt_Toe = XPlane_Normal_Tilt*sin(-Toe_Angle) + YPlane_Normal_Tilt*cos(-Toe_Angle);
+          su2double YPlane_Normal_Tilt_Toe =
+              XPlane_Normal_Tilt * sin(-Toe_Angle) + YPlane_Normal_Tilt * cos(-Toe_Angle);
           su2double ZPlane_Normal_Tilt_Toe = ZPlane_Normal_Tilt;
 
-
           v1[1] = YCoord_Trans_Tilt_Toe - 0.0;
           v1[2] = ZCoord_Trans_Tilt_Toe - 0.0;
-          v3[0] = v1[1]*ZPlane_Normal_Tilt_Toe-v1[2]*YPlane_Normal_Tilt_Toe;
+          v3[0] = v1[1] * ZPlane_Normal_Tilt_Toe - v1[2] * YPlane_Normal_Tilt_Toe;
           CrossProduct = v3[0] * 1.0;
-
         }
 
-        for (unsigned short iFace = 0; iFace < bound[iMarker][iElem]->GetnFaces(); iFace++){
-          iNode = bound[iMarker][iElem]->GetFaces(iFace,0);
-          jNode = bound[iMarker][iElem]->GetFaces(iFace,1);
+        for (unsigned short iFace = 0; iFace < bound[iMarker][iElem]->GetnFaces(); iFace++) {
+          iNode = bound[iMarker][iElem]->GetFaces(iFace, 0);
+          jNode = bound[iMarker][iElem]->GetFaces(iFace, 1);
           iPoint = bound[iMarker][iElem]->GetNode(iNode);
           jPoint = bound[iMarker][iElem]->GetNode(jNode);
 
-          if ((CrossProduct >= 0.0)
-              && ((AveXCoord > MinXCoord) && (AveXCoord < MaxXCoord))
-              && ((AveYCoord > MinYCoord) && (AveYCoord < MaxYCoord))
-              && ((AveZCoord > MinZCoord) && (AveZCoord < MaxZCoord))) {
-
-            Segment_P0[0] = 0.0;  Segment_P0[1] = 0.0;  Segment_P0[2] = 0.0;  Variable_P0 = 0.0;
-            Segment_P1[0] = 0.0;  Segment_P1[1] = 0.0;  Segment_P1[2] = 0.0;  Variable_P1 = 0.0;
-
+          if ((CrossProduct >= 0.0) && ((AveXCoord > MinXCoord) && (AveXCoord < MaxXCoord)) &&
+              ((AveYCoord > MinYCoord) && (AveYCoord < MaxYCoord)) &&
+              ((AveZCoord > MinZCoord) && (AveZCoord < MaxZCoord))) {
+            Segment_P0[0] = 0.0;
+            Segment_P0[1] = 0.0;
+            Segment_P0[2] = 0.0;
+            Variable_P0 = 0.0;
+            Segment_P1[0] = 0.0;
+            Segment_P1[1] = 0.0;
+            Segment_P1[2] = 0.0;
+            Variable_P1 = 0.0;
 
             for (iDim = 0; iDim < nDim; iDim++) {
               if (original_surface == true) {
                 Segment_P0[iDim] = nodes->GetCoord(iPoint, iDim);
                 Segment_P1[iDim] = nodes->GetCoord(jPoint, iDim);
-              }
-              else {
+              } else {
                 Segment_P0[iDim] = nodes->GetCoord(iPoint, iDim) + Coord_Variation[iPoint][iDim];
                 Segment_P1[iDim] = nodes->GetCoord(jPoint, iDim) + Coord_Variation[jPoint][iDim];
               }
@@ -1852,19 +1739,26 @@ void CGeometry::ComputeAirfoil_Section(su2double *Plane_P0, su2double *Plane_Nor
             /*--- In 2D add the points directly (note the change between Y and Z coordinate) ---*/
 
             if (nDim == 2) {
-              Xcoord_Index0.push_back(Segment_P0[0]);                     Xcoord_Index1.push_back(Segment_P1[0]);
-              Ycoord_Index0.push_back(Segment_P0[2]);                     Ycoord_Index1.push_back(Segment_P1[2]);
-              Zcoord_Index0.push_back(Segment_P0[1]);                     Zcoord_Index1.push_back(Segment_P1[1]);
-              Variable_Index0.push_back(Variable_P0);                     Variable_Index1.push_back(Variable_P1);
-              IGlobalID_Index0.push_back(nodes->GetGlobalIndex(iPoint)); IGlobalID_Index1.push_back(nodes->GetGlobalIndex(jPoint));
-              JGlobalID_Index0.push_back(nodes->GetGlobalIndex(iPoint)); JGlobalID_Index1.push_back(nodes->GetGlobalIndex(jPoint));
+              Xcoord_Index0.push_back(Segment_P0[0]);
+              Xcoord_Index1.push_back(Segment_P1[0]);
+              Ycoord_Index0.push_back(Segment_P0[2]);
+              Ycoord_Index1.push_back(Segment_P1[2]);
+              Zcoord_Index0.push_back(Segment_P0[1]);
+              Zcoord_Index1.push_back(Segment_P1[1]);
+              Variable_Index0.push_back(Variable_P0);
+              Variable_Index1.push_back(Variable_P1);
+              IGlobalID_Index0.push_back(nodes->GetGlobalIndex(iPoint));
+              IGlobalID_Index1.push_back(nodes->GetGlobalIndex(jPoint));
+              JGlobalID_Index0.push_back(nodes->GetGlobalIndex(iPoint));
+              JGlobalID_Index1.push_back(nodes->GetGlobalIndex(jPoint));
               PointIndex++;
             }
 
             /*--- In 3D compute the intersection ---*/
 
             else if (nDim == 3) {
-              intersect = SegmentIntersectsPlane(Segment_P0, Segment_P1, Variable_P0, Variable_P1, Plane_P0, Plane_Normal, Intersection, Variable_Interp);
+              intersect = SegmentIntersectsPlane(Segment_P0, Segment_P1, Variable_P0, Variable_P1, Plane_P0,
+                                                 Plane_Normal, Intersection, Variable_Interp);
               if (intersect == true) {
                 if (PointIndex == 0) {
                   Xcoord_Index0.push_back(Intersection[0]);
@@ -1892,9 +1786,8 @@ void CGeometry::ComputeAirfoil_Section(su2double *Plane_P0, su2double *Plane_Nor
   }
 
   if (original_surface == false) {
-    for (iPoint = 0; iPoint < nPoint; iPoint++)
-      delete [] Coord_Variation[iPoint];
-    delete [] Coord_Variation;
+    for (iPoint = 0; iPoint < nPoint; iPoint++) delete[] Coord_Variation[iPoint];
+    delete[] Coord_Variation;
   }
 
 #ifdef HAVE_MPI
@@ -1904,117 +1797,131 @@ void CGeometry::ComputeAirfoil_Section(su2double *Plane_P0, su2double *Plane_Nor
   nLocalEdge = 0, MaxLocalEdge = 0;
   nProcessor = size;
 
-  Buffer_Send_nEdge = new unsigned long [1];
-  Buffer_Receive_nEdge = new unsigned long [nProcessor];
+  Buffer_Send_nEdge = new unsigned long[1];
+  Buffer_Receive_nEdge = new unsigned long[nProcessor];
 
   nLocalEdge = Xcoord_Index0.size();
 
   Buffer_Send_nEdge[0] = nLocalEdge;
 
   SU2_MPI::Allreduce(&nLocalEdge, &MaxLocalEdge, 1, MPI_UNSIGNED_LONG, MPI_MAX, SU2_MPI::GetComm());
-  SU2_MPI::Allgather(Buffer_Send_nEdge, 1, MPI_UNSIGNED_LONG, Buffer_Receive_nEdge, 1, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
+  SU2_MPI::Allgather(Buffer_Send_nEdge, 1, MPI_UNSIGNED_LONG, Buffer_Receive_nEdge, 1, MPI_UNSIGNED_LONG,
+                     SU2_MPI::GetComm());
 
-  Buffer_Send_Coord    = new su2double [MaxLocalEdge*6];
-  Buffer_Receive_Coord = new su2double [nProcessor*MaxLocalEdge*6];
+  Buffer_Send_Coord = new su2double[MaxLocalEdge * 6];
+  Buffer_Receive_Coord = new su2double[nProcessor * MaxLocalEdge * 6];
 
-  Buffer_Send_Variable    = new su2double [MaxLocalEdge*2];
-  Buffer_Receive_Variable = new su2double [nProcessor*MaxLocalEdge*2];
+  Buffer_Send_Variable = new su2double[MaxLocalEdge * 2];
+  Buffer_Receive_Variable = new su2double[nProcessor * MaxLocalEdge * 2];
 
-  Buffer_Send_GlobalID    = new unsigned long [MaxLocalEdge*4];
-  Buffer_Receive_GlobalID = new unsigned long [nProcessor*MaxLocalEdge*4];
+  Buffer_Send_GlobalID = new unsigned long[MaxLocalEdge * 4];
+  Buffer_Receive_GlobalID = new unsigned long[nProcessor * MaxLocalEdge * 4];
 
-  nBuffer_Coord    = MaxLocalEdge*6;
-  nBuffer_Variable = MaxLocalEdge*2;
-  nBuffer_GlobalID = MaxLocalEdge*4;
+  nBuffer_Coord = MaxLocalEdge * 6;
+  nBuffer_Variable = MaxLocalEdge * 2;
+  nBuffer_GlobalID = MaxLocalEdge * 4;
 
   for (iEdge = 0; iEdge < nLocalEdge; iEdge++) {
-    Buffer_Send_Coord[iEdge*6 + 0] = Xcoord_Index0[iEdge];
-    Buffer_Send_Coord[iEdge*6 + 1] = Ycoord_Index0[iEdge];
-    Buffer_Send_Coord[iEdge*6 + 2] = Zcoord_Index0[iEdge];
-    Buffer_Send_Coord[iEdge*6 + 3] = Xcoord_Index1[iEdge];
-    Buffer_Send_Coord[iEdge*6 + 4] = Ycoord_Index1[iEdge];
-    Buffer_Send_Coord[iEdge*6 + 5] = Zcoord_Index1[iEdge];
-
-    Buffer_Send_Variable[iEdge*2 + 0] = Variable_Index0[iEdge];
-    Buffer_Send_Variable[iEdge*2 + 1] = Variable_Index1[iEdge];
-
-    Buffer_Send_GlobalID[iEdge*4 + 0] = IGlobalID_Index0[iEdge];
-    Buffer_Send_GlobalID[iEdge*4 + 1] = JGlobalID_Index0[iEdge];
-    Buffer_Send_GlobalID[iEdge*4 + 2] = IGlobalID_Index1[iEdge];
-    Buffer_Send_GlobalID[iEdge*4 + 3] = JGlobalID_Index1[iEdge];
+    Buffer_Send_Coord[iEdge * 6 + 0] = Xcoord_Index0[iEdge];
+    Buffer_Send_Coord[iEdge * 6 + 1] = Ycoord_Index0[iEdge];
+    Buffer_Send_Coord[iEdge * 6 + 2] = Zcoord_Index0[iEdge];
+    Buffer_Send_Coord[iEdge * 6 + 3] = Xcoord_Index1[iEdge];
+    Buffer_Send_Coord[iEdge * 6 + 4] = Ycoord_Index1[iEdge];
+    Buffer_Send_Coord[iEdge * 6 + 5] = Zcoord_Index1[iEdge];
+
+    Buffer_Send_Variable[iEdge * 2 + 0] = Variable_Index0[iEdge];
+    Buffer_Send_Variable[iEdge * 2 + 1] = Variable_Index1[iEdge];
+
+    Buffer_Send_GlobalID[iEdge * 4 + 0] = IGlobalID_Index0[iEdge];
+    Buffer_Send_GlobalID[iEdge * 4 + 1] = JGlobalID_Index0[iEdge];
+    Buffer_Send_GlobalID[iEdge * 4 + 2] = IGlobalID_Index1[iEdge];
+    Buffer_Send_GlobalID[iEdge * 4 + 3] = JGlobalID_Index1[iEdge];
   }
 
-  SU2_MPI::Allgather(Buffer_Send_Coord, nBuffer_Coord, MPI_DOUBLE, Buffer_Receive_Coord, nBuffer_Coord, MPI_DOUBLE, SU2_MPI::GetComm());
-  SU2_MPI::Allgather(Buffer_Send_Variable, nBuffer_Variable, MPI_DOUBLE, Buffer_Receive_Variable, nBuffer_Variable, MPI_DOUBLE, SU2_MPI::GetComm());
-  SU2_MPI::Allgather(Buffer_Send_GlobalID, nBuffer_GlobalID, MPI_UNSIGNED_LONG, Buffer_Receive_GlobalID, nBuffer_GlobalID, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
+  SU2_MPI::Allgather(Buffer_Send_Coord, nBuffer_Coord, MPI_DOUBLE, Buffer_Receive_Coord, nBuffer_Coord, MPI_DOUBLE,
+                     SU2_MPI::GetComm());
+  SU2_MPI::Allgather(Buffer_Send_Variable, nBuffer_Variable, MPI_DOUBLE, Buffer_Receive_Variable, nBuffer_Variable,
+                     MPI_DOUBLE, SU2_MPI::GetComm());
+  SU2_MPI::Allgather(Buffer_Send_GlobalID, nBuffer_GlobalID, MPI_UNSIGNED_LONG, Buffer_Receive_GlobalID,
+                     nBuffer_GlobalID, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
 
   /*--- Clean the vectors before adding the new vertices only to the master node ---*/
 
-  Xcoord_Index0.clear();     Xcoord_Index1.clear();
-  Ycoord_Index0.clear();     Ycoord_Index1.clear();
-  Zcoord_Index0.clear();     Zcoord_Index1.clear();
-  Variable_Index0.clear();   Variable_Index1.clear();
-  IGlobalID_Index0.clear();  IGlobalID_Index1.clear();
-  JGlobalID_Index0.clear();  JGlobalID_Index1.clear();
+  Xcoord_Index0.clear();
+  Xcoord_Index1.clear();
+  Ycoord_Index0.clear();
+  Ycoord_Index1.clear();
+  Zcoord_Index0.clear();
+  Zcoord_Index1.clear();
+  Variable_Index0.clear();
+  Variable_Index1.clear();
+  IGlobalID_Index0.clear();
+  IGlobalID_Index1.clear();
+  JGlobalID_Index0.clear();
+  JGlobalID_Index1.clear();
 
   /*--- Copy the boundary to the master node vectors ---*/
 
   if (rank == MASTER_NODE) {
     for (iProcessor = 0; iProcessor < nProcessor; iProcessor++) {
       for (iEdge = 0; iEdge < Buffer_Receive_nEdge[iProcessor]; iEdge++) {
-        Xcoord_Index0.push_back( Buffer_Receive_Coord[ iProcessor*MaxLocalEdge*6 + iEdge*6 + 0] );
-        Ycoord_Index0.push_back( Buffer_Receive_Coord[ iProcessor*MaxLocalEdge*6 + iEdge*6 + 1] );
-        Zcoord_Index0.push_back( Buffer_Receive_Coord[ iProcessor*MaxLocalEdge*6 + iEdge*6 + 2] );
-        Xcoord_Index1.push_back( Buffer_Receive_Coord[ iProcessor*MaxLocalEdge*6 + iEdge*6 + 3] );
-        Ycoord_Index1.push_back( Buffer_Receive_Coord[ iProcessor*MaxLocalEdge*6 + iEdge*6 + 4] );
-        Zcoord_Index1.push_back( Buffer_Receive_Coord[ iProcessor*MaxLocalEdge*6 + iEdge*6 + 5] );
-
-        Variable_Index0.push_back( Buffer_Receive_Variable[ iProcessor*MaxLocalEdge*2 + iEdge*2 + 0] );
-        Variable_Index1.push_back( Buffer_Receive_Variable[ iProcessor*MaxLocalEdge*2 + iEdge*2 + 1] );
-
-        IGlobalID_Index0.push_back( Buffer_Receive_GlobalID[ iProcessor*MaxLocalEdge*4 + iEdge*4 + 0] );
-        JGlobalID_Index0.push_back( Buffer_Receive_GlobalID[ iProcessor*MaxLocalEdge*4 + iEdge*4 + 1] );
-        IGlobalID_Index1.push_back( Buffer_Receive_GlobalID[ iProcessor*MaxLocalEdge*4 + iEdge*4 + 2] );
-        JGlobalID_Index1.push_back( Buffer_Receive_GlobalID[ iProcessor*MaxLocalEdge*4 + iEdge*4 + 3] );
-
+        Xcoord_Index0.push_back(Buffer_Receive_Coord[iProcessor * MaxLocalEdge * 6 + iEdge * 6 + 0]);
+        Ycoord_Index0.push_back(Buffer_Receive_Coord[iProcessor * MaxLocalEdge * 6 + iEdge * 6 + 1]);
+        Zcoord_Index0.push_back(Buffer_Receive_Coord[iProcessor * MaxLocalEdge * 6 + iEdge * 6 + 2]);
+        Xcoord_Index1.push_back(Buffer_Receive_Coord[iProcessor * MaxLocalEdge * 6 + iEdge * 6 + 3]);
+        Ycoord_Index1.push_back(Buffer_Receive_Coord[iProcessor * MaxLocalEdge * 6 + iEdge * 6 + 4]);
+        Zcoord_Index1.push_back(Buffer_Receive_Coord[iProcessor * MaxLocalEdge * 6 + iEdge * 6 + 5]);
+
+        Variable_Index0.push_back(Buffer_Receive_Variable[iProcessor * MaxLocalEdge * 2 + iEdge * 2 + 0]);
+        Variable_Index1.push_back(Buffer_Receive_Variable[iProcessor * MaxLocalEdge * 2 + iEdge * 2 + 1]);
+
+        IGlobalID_Index0.push_back(Buffer_Receive_GlobalID[iProcessor * MaxLocalEdge * 4 + iEdge * 4 + 0]);
+        JGlobalID_Index0.push_back(Buffer_Receive_GlobalID[iProcessor * MaxLocalEdge * 4 + iEdge * 4 + 1]);
+        IGlobalID_Index1.push_back(Buffer_Receive_GlobalID[iProcessor * MaxLocalEdge * 4 + iEdge * 4 + 2]);
+        JGlobalID_Index1.push_back(Buffer_Receive_GlobalID[iProcessor * MaxLocalEdge * 4 + iEdge * 4 + 3]);
       }
     }
   }
 
-  delete[] Buffer_Send_Coord;      delete[] Buffer_Receive_Coord;
-  delete[] Buffer_Send_Variable;   delete[] Buffer_Receive_Variable;
-  delete[] Buffer_Send_GlobalID;   delete[] Buffer_Receive_GlobalID;
-  delete[] Buffer_Send_nEdge;    delete[] Buffer_Receive_nEdge;
+  delete[] Buffer_Send_Coord;
+  delete[] Buffer_Receive_Coord;
+  delete[] Buffer_Send_Variable;
+  delete[] Buffer_Receive_Variable;
+  delete[] Buffer_Send_GlobalID;
+  delete[] Buffer_Receive_GlobalID;
+  delete[] Buffer_Send_nEdge;
+  delete[] Buffer_Receive_nEdge;
 
 #endif
 
   if ((rank == MASTER_NODE) && (Xcoord_Index0.size() != 0)) {
-
     /*--- Remove singular edges ---*/
 
     bool Remove;
 
-    do { Remove = false;
+    do {
+      Remove = false;
       for (iEdge = 0; iEdge < Xcoord_Index0.size(); iEdge++) {
-
-        if (((IGlobalID_Index0[iEdge] == IGlobalID_Index1[iEdge]) && (JGlobalID_Index0[iEdge] == JGlobalID_Index1[iEdge])) ||
-            ((IGlobalID_Index0[iEdge] == JGlobalID_Index1[iEdge]) && (JGlobalID_Index0[iEdge] == IGlobalID_Index1[iEdge]))) {
-
-          Xcoord_Index0.erase (Xcoord_Index0.begin() + iEdge);
-          Ycoord_Index0.erase (Ycoord_Index0.begin() + iEdge);
-          Zcoord_Index0.erase (Zcoord_Index0.begin() + iEdge);
-          Variable_Index0.erase (Variable_Index0.begin() + iEdge);
-          IGlobalID_Index0.erase (IGlobalID_Index0.begin() + iEdge);
-          JGlobalID_Index0.erase (JGlobalID_Index0.begin() + iEdge);
-
-          Xcoord_Index1.erase (Xcoord_Index1.begin() + iEdge);
-          Ycoord_Index1.erase (Ycoord_Index1.begin() + iEdge);
-          Zcoord_Index1.erase (Zcoord_Index1.begin() + iEdge);
-          Variable_Index1.erase (Variable_Index1.begin() + iEdge);
-          IGlobalID_Index1.erase (IGlobalID_Index1.begin() + iEdge);
-          JGlobalID_Index1.erase (JGlobalID_Index1.begin() + iEdge);
-
-          Remove = true; break;
+        if (((IGlobalID_Index0[iEdge] == IGlobalID_Index1[iEdge]) &&
+             (JGlobalID_Index0[iEdge] == JGlobalID_Index1[iEdge])) ||
+            ((IGlobalID_Index0[iEdge] == JGlobalID_Index1[iEdge]) &&
+             (JGlobalID_Index0[iEdge] == IGlobalID_Index1[iEdge]))) {
+          Xcoord_Index0.erase(Xcoord_Index0.begin() + iEdge);
+          Ycoord_Index0.erase(Ycoord_Index0.begin() + iEdge);
+          Zcoord_Index0.erase(Zcoord_Index0.begin() + iEdge);
+          Variable_Index0.erase(Variable_Index0.begin() + iEdge);
+          IGlobalID_Index0.erase(IGlobalID_Index0.begin() + iEdge);
+          JGlobalID_Index0.erase(JGlobalID_Index0.begin() + iEdge);
+
+          Xcoord_Index1.erase(Xcoord_Index1.begin() + iEdge);
+          Ycoord_Index1.erase(Ycoord_Index1.begin() + iEdge);
+          Zcoord_Index1.erase(Zcoord_Index1.begin() + iEdge);
+          Variable_Index1.erase(Variable_Index1.begin() + iEdge);
+          IGlobalID_Index1.erase(IGlobalID_Index1.begin() + iEdge);
+          JGlobalID_Index1.erase(JGlobalID_Index1.begin() + iEdge);
+
+          Remove = true;
+          break;
         }
         if (Remove) break;
       }
@@ -2022,58 +1929,65 @@ void CGeometry::ComputeAirfoil_Section(su2double *Plane_P0, su2double *Plane_Nor
 
     /*--- Remove repeated edges computing distance, this could happend because the MPI ---*/
 
-    do { Remove = false;
-      for (iEdge = 0; iEdge < Xcoord_Index0.size()-1; iEdge++) {
-        for (jEdge = iEdge+1; jEdge < Xcoord_Index0.size(); jEdge++) {
-
+    do {
+      Remove = false;
+      for (iEdge = 0; iEdge < Xcoord_Index0.size() - 1; iEdge++) {
+        for (jEdge = iEdge + 1; jEdge < Xcoord_Index0.size(); jEdge++) {
           /*--- Edges with the same orientation ---*/
 
-          if ((((IGlobalID_Index0[iEdge] == IGlobalID_Index0[jEdge]) && (JGlobalID_Index0[iEdge] == JGlobalID_Index0[jEdge])) ||
-               ((IGlobalID_Index0[iEdge] == JGlobalID_Index0[jEdge]) && (JGlobalID_Index0[iEdge] == IGlobalID_Index0[jEdge]))) &&
-              (((IGlobalID_Index1[iEdge] == IGlobalID_Index1[jEdge]) && (JGlobalID_Index1[iEdge] == JGlobalID_Index1[jEdge])) ||
-               ((IGlobalID_Index1[iEdge] == JGlobalID_Index1[jEdge]) && (JGlobalID_Index1[iEdge] == IGlobalID_Index1[jEdge])))) {
-
-                Xcoord_Index0.erase (Xcoord_Index0.begin() + jEdge);
-                Ycoord_Index0.erase (Ycoord_Index0.begin() + jEdge);
-                Zcoord_Index0.erase (Zcoord_Index0.begin() + jEdge);
-                Variable_Index0.erase (Variable_Index0.begin() + jEdge);
-                IGlobalID_Index0.erase (IGlobalID_Index0.begin() + jEdge);
-                JGlobalID_Index0.erase (JGlobalID_Index0.begin() + jEdge);
-
-                Xcoord_Index1.erase (Xcoord_Index1.begin() + jEdge);
-                Ycoord_Index1.erase (Ycoord_Index1.begin() + jEdge);
-                Zcoord_Index1.erase (Zcoord_Index1.begin() + jEdge);
-                Variable_Index1.erase (Variable_Index1.begin() + jEdge);
-                IGlobalID_Index1.erase (IGlobalID_Index1.begin() + jEdge);
-                JGlobalID_Index1.erase (JGlobalID_Index1.begin() + jEdge);
-
-                Remove = true; break;
-
-              }
+          if ((((IGlobalID_Index0[iEdge] == IGlobalID_Index0[jEdge]) &&
+                (JGlobalID_Index0[iEdge] == JGlobalID_Index0[jEdge])) ||
+               ((IGlobalID_Index0[iEdge] == JGlobalID_Index0[jEdge]) &&
+                (JGlobalID_Index0[iEdge] == IGlobalID_Index0[jEdge]))) &&
+              (((IGlobalID_Index1[iEdge] == IGlobalID_Index1[jEdge]) &&
+                (JGlobalID_Index1[iEdge] == JGlobalID_Index1[jEdge])) ||
+               ((IGlobalID_Index1[iEdge] == JGlobalID_Index1[jEdge]) &&
+                (JGlobalID_Index1[iEdge] == IGlobalID_Index1[jEdge])))) {
+            Xcoord_Index0.erase(Xcoord_Index0.begin() + jEdge);
+            Ycoord_Index0.erase(Ycoord_Index0.begin() + jEdge);
+            Zcoord_Index0.erase(Zcoord_Index0.begin() + jEdge);
+            Variable_Index0.erase(Variable_Index0.begin() + jEdge);
+            IGlobalID_Index0.erase(IGlobalID_Index0.begin() + jEdge);
+            JGlobalID_Index0.erase(JGlobalID_Index0.begin() + jEdge);
+
+            Xcoord_Index1.erase(Xcoord_Index1.begin() + jEdge);
+            Ycoord_Index1.erase(Ycoord_Index1.begin() + jEdge);
+            Zcoord_Index1.erase(Zcoord_Index1.begin() + jEdge);
+            Variable_Index1.erase(Variable_Index1.begin() + jEdge);
+            IGlobalID_Index1.erase(IGlobalID_Index1.begin() + jEdge);
+            JGlobalID_Index1.erase(JGlobalID_Index1.begin() + jEdge);
+
+            Remove = true;
+            break;
+          }
 
           /*--- Edges with oposite orientation ---*/
 
-          if ((((IGlobalID_Index0[iEdge] == IGlobalID_Index1[jEdge]) && (JGlobalID_Index0[iEdge] == JGlobalID_Index1[jEdge])) ||
-               ((IGlobalID_Index0[iEdge] == JGlobalID_Index1[jEdge]) && (JGlobalID_Index0[iEdge] == IGlobalID_Index1[jEdge]))) &&
-              (((IGlobalID_Index1[iEdge] == IGlobalID_Index0[jEdge]) && (JGlobalID_Index1[iEdge] == JGlobalID_Index0[jEdge])) ||
-               ((IGlobalID_Index1[iEdge] == JGlobalID_Index0[jEdge]) && (JGlobalID_Index1[iEdge] == IGlobalID_Index0[jEdge])))) {
-
-                Xcoord_Index0.erase (Xcoord_Index0.begin() + jEdge);
-                Ycoord_Index0.erase (Ycoord_Index0.begin() + jEdge);
-                Zcoord_Index0.erase (Zcoord_Index0.begin() + jEdge);
-                Variable_Index0.erase (Variable_Index0.begin() + jEdge);
-                IGlobalID_Index0.erase (IGlobalID_Index0.begin() + jEdge);
-                JGlobalID_Index0.erase (JGlobalID_Index0.begin() + jEdge);
-
-                Xcoord_Index1.erase (Xcoord_Index1.begin() + jEdge);
-                Ycoord_Index1.erase (Ycoord_Index1.begin() + jEdge);
-                Zcoord_Index1.erase (Zcoord_Index1.begin() + jEdge);
-                Variable_Index1.erase (Variable_Index1.begin() + jEdge);
-                IGlobalID_Index1.erase (IGlobalID_Index1.begin() + jEdge);
-                JGlobalID_Index1.erase (JGlobalID_Index1.begin() + jEdge);
-
-                Remove = true; break;
-              }
+          if ((((IGlobalID_Index0[iEdge] == IGlobalID_Index1[jEdge]) &&
+                (JGlobalID_Index0[iEdge] == JGlobalID_Index1[jEdge])) ||
+               ((IGlobalID_Index0[iEdge] == JGlobalID_Index1[jEdge]) &&
+                (JGlobalID_Index0[iEdge] == IGlobalID_Index1[jEdge]))) &&
+              (((IGlobalID_Index1[iEdge] == IGlobalID_Index0[jEdge]) &&
+                (JGlobalID_Index1[iEdge] == JGlobalID_Index0[jEdge])) ||
+               ((IGlobalID_Index1[iEdge] == JGlobalID_Index0[jEdge]) &&
+                (JGlobalID_Index1[iEdge] == IGlobalID_Index0[jEdge])))) {
+            Xcoord_Index0.erase(Xcoord_Index0.begin() + jEdge);
+            Ycoord_Index0.erase(Ycoord_Index0.begin() + jEdge);
+            Zcoord_Index0.erase(Zcoord_Index0.begin() + jEdge);
+            Variable_Index0.erase(Variable_Index0.begin() + jEdge);
+            IGlobalID_Index0.erase(IGlobalID_Index0.begin() + jEdge);
+            JGlobalID_Index0.erase(JGlobalID_Index0.begin() + jEdge);
+
+            Xcoord_Index1.erase(Xcoord_Index1.begin() + jEdge);
+            Ycoord_Index1.erase(Ycoord_Index1.begin() + jEdge);
+            Zcoord_Index1.erase(Zcoord_Index1.begin() + jEdge);
+            Variable_Index1.erase(Variable_Index1.begin() + jEdge);
+            IGlobalID_Index1.erase(IGlobalID_Index1.begin() + jEdge);
+            JGlobalID_Index1.erase(JGlobalID_Index1.begin() + jEdge);
+
+            Remove = true;
+            break;
+          }
           if (Remove) break;
         }
         if (Remove) break;
@@ -2082,38 +1996,38 @@ void CGeometry::ComputeAirfoil_Section(su2double *Plane_P0, su2double *Plane_Nor
     } while (Remove == true);
 
     if (Xcoord_Index0.size() != 1) {
-
       /*--- Rotate from the Y-Z plane to the X-Z plane to reuse the rest of subroutines  ---*/
 
       if (config->GetGeo_Description() == FUSELAGE) {
-        su2double Angle = -0.5*PI_NUMBER;
+        su2double Angle = -0.5 * PI_NUMBER;
         for (iEdge = 0; iEdge < Xcoord_Index0.size(); iEdge++) {
-          su2double XCoord = Xcoord_Index0[iEdge]*cos(Angle) - Ycoord_Index0[iEdge]*sin(Angle);
-          su2double YCoord = Ycoord_Index0[iEdge]*cos(Angle) + Xcoord_Index0[iEdge]*sin(Angle);
+          su2double XCoord = Xcoord_Index0[iEdge] * cos(Angle) - Ycoord_Index0[iEdge] * sin(Angle);
+          su2double YCoord = Ycoord_Index0[iEdge] * cos(Angle) + Xcoord_Index0[iEdge] * sin(Angle);
           su2double ZCoord = Zcoord_Index0[iEdge];
-          Xcoord_Index0[iEdge] = XCoord; Ycoord_Index0[iEdge] = YCoord; Zcoord_Index0[iEdge] = ZCoord;
-          XCoord = Xcoord_Index1[iEdge]*cos(Angle) - Ycoord_Index1[iEdge]*sin(Angle);
-          YCoord = Ycoord_Index1[iEdge]*cos(Angle) + Xcoord_Index1[iEdge]*sin(Angle);
+          Xcoord_Index0[iEdge] = XCoord;
+          Ycoord_Index0[iEdge] = YCoord;
+          Zcoord_Index0[iEdge] = ZCoord;
+          XCoord = Xcoord_Index1[iEdge] * cos(Angle) - Ycoord_Index1[iEdge] * sin(Angle);
+          YCoord = Ycoord_Index1[iEdge] * cos(Angle) + Xcoord_Index1[iEdge] * sin(Angle);
           ZCoord = Zcoord_Index1[iEdge];
-          Xcoord_Index1[iEdge] = XCoord; Ycoord_Index1[iEdge] = YCoord; Zcoord_Index1[iEdge] = ZCoord;
+          Xcoord_Index1[iEdge] = XCoord;
+          Ycoord_Index1[iEdge] = YCoord;
+          Zcoord_Index1[iEdge] = ZCoord;
         }
       }
 
       /*--- Rotate nacelle secction to a X-Z plane to reuse the rest of subroutines  ---*/
 
-
       if (config->GetGeo_Description() == NACELLE) {
-
-        su2double Tilt_Angle = config->GetNacelleLocation(3)*PI_NUMBER/180;
-        su2double Toe_Angle = config->GetNacelleLocation(4)*PI_NUMBER/180;
-        su2double Theta_deg = atan2(Plane_Normal[1],-Plane_Normal[2])/PI_NUMBER*180 + 180;
-        su2double Roll_Angle = 0.5*PI_NUMBER - Theta_deg*PI_NUMBER/180;
+        su2double Tilt_Angle = config->GetNacelleLocation(3) * PI_NUMBER / 180;
+        su2double Toe_Angle = config->GetNacelleLocation(4) * PI_NUMBER / 180;
+        su2double Theta_deg = atan2(Plane_Normal[1], -Plane_Normal[2]) / PI_NUMBER * 180 + 180;
+        su2double Roll_Angle = 0.5 * PI_NUMBER - Theta_deg * PI_NUMBER / 180;
 
         su2double XCoord_Trans, YCoord_Trans, ZCoord_Trans, XCoord_Trans_Tilt, YCoord_Trans_Tilt, ZCoord_Trans_Tilt,
-        XCoord_Trans_Tilt_Toe, YCoord_Trans_Tilt_Toe, ZCoord_Trans_Tilt_Toe, XCoord, YCoord, ZCoord;
+            XCoord_Trans_Tilt_Toe, YCoord_Trans_Tilt_Toe, ZCoord_Trans_Tilt_Toe, XCoord, YCoord, ZCoord;
 
         for (iEdge = 0; iEdge < Xcoord_Index0.size(); iEdge++) {
-
           /*--- First point of the edge ---*/
 
           /*--- Translate to the origin ---*/
@@ -2124,25 +2038,27 @@ void CGeometry::ComputeAirfoil_Section(su2double *Plane_P0, su2double *Plane_Nor
 
           /*--- Apply tilt angle ---*/
 
-          XCoord_Trans_Tilt = XCoord_Trans*cos(Tilt_Angle) + ZCoord_Trans*sin(Tilt_Angle);
+          XCoord_Trans_Tilt = XCoord_Trans * cos(Tilt_Angle) + ZCoord_Trans * sin(Tilt_Angle);
           YCoord_Trans_Tilt = YCoord_Trans;
-          ZCoord_Trans_Tilt = ZCoord_Trans*cos(Tilt_Angle) - XCoord_Trans*sin(Tilt_Angle);
+          ZCoord_Trans_Tilt = ZCoord_Trans * cos(Tilt_Angle) - XCoord_Trans * sin(Tilt_Angle);
 
           /*--- Apply toe angle ---*/
 
-          XCoord_Trans_Tilt_Toe = XCoord_Trans_Tilt*cos(Toe_Angle) - YCoord_Trans_Tilt*sin(Toe_Angle);
-          YCoord_Trans_Tilt_Toe = XCoord_Trans_Tilt*sin(Toe_Angle) + YCoord_Trans_Tilt*cos(Toe_Angle);
+          XCoord_Trans_Tilt_Toe = XCoord_Trans_Tilt * cos(Toe_Angle) - YCoord_Trans_Tilt * sin(Toe_Angle);
+          YCoord_Trans_Tilt_Toe = XCoord_Trans_Tilt * sin(Toe_Angle) + YCoord_Trans_Tilt * cos(Toe_Angle);
           ZCoord_Trans_Tilt_Toe = ZCoord_Trans_Tilt;
 
           /*--- Rotate to X-Z plane (roll) ---*/
 
           XCoord = XCoord_Trans_Tilt_Toe;
-          YCoord = YCoord_Trans_Tilt_Toe*cos(Roll_Angle) - ZCoord_Trans_Tilt_Toe*sin(Roll_Angle);
-          ZCoord = YCoord_Trans_Tilt_Toe*sin(Roll_Angle) + ZCoord_Trans_Tilt_Toe*cos(Roll_Angle);
+          YCoord = YCoord_Trans_Tilt_Toe * cos(Roll_Angle) - ZCoord_Trans_Tilt_Toe * sin(Roll_Angle);
+          ZCoord = YCoord_Trans_Tilt_Toe * sin(Roll_Angle) + ZCoord_Trans_Tilt_Toe * cos(Roll_Angle);
 
           /*--- Update coordinates ---*/
 
-          Xcoord_Index0[iEdge] = XCoord; Ycoord_Index0[iEdge] = YCoord; Zcoord_Index0[iEdge] = ZCoord;
+          Xcoord_Index0[iEdge] = XCoord;
+          Ycoord_Index0[iEdge] = YCoord;
+          Zcoord_Index0[iEdge] = ZCoord;
 
           /*--- Second point of the edge ---*/
 
@@ -2154,59 +2070,73 @@ void CGeometry::ComputeAirfoil_Section(su2double *Plane_P0, su2double *Plane_Nor
 
           /*--- Apply tilt angle ---*/
 
-          XCoord_Trans_Tilt = XCoord_Trans*cos(Tilt_Angle) + ZCoord_Trans*sin(Tilt_Angle);
+          XCoord_Trans_Tilt = XCoord_Trans * cos(Tilt_Angle) + ZCoord_Trans * sin(Tilt_Angle);
           YCoord_Trans_Tilt = YCoord_Trans;
-          ZCoord_Trans_Tilt = ZCoord_Trans*cos(Tilt_Angle) - XCoord_Trans*sin(Tilt_Angle);
+          ZCoord_Trans_Tilt = ZCoord_Trans * cos(Tilt_Angle) - XCoord_Trans * sin(Tilt_Angle);
 
           /*--- Apply toe angle ---*/
 
-          XCoord_Trans_Tilt_Toe = XCoord_Trans_Tilt*cos(Toe_Angle) - YCoord_Trans_Tilt*sin(Toe_Angle);
-          YCoord_Trans_Tilt_Toe = XCoord_Trans_Tilt*sin(Toe_Angle) + YCoord_Trans_Tilt*cos(Toe_Angle);
+          XCoord_Trans_Tilt_Toe = XCoord_Trans_Tilt * cos(Toe_Angle) - YCoord_Trans_Tilt * sin(Toe_Angle);
+          YCoord_Trans_Tilt_Toe = XCoord_Trans_Tilt * sin(Toe_Angle) + YCoord_Trans_Tilt * cos(Toe_Angle);
           ZCoord_Trans_Tilt_Toe = ZCoord_Trans_Tilt;
 
           /*--- Rotate to X-Z plane (roll) ---*/
 
           XCoord = XCoord_Trans_Tilt_Toe;
-          YCoord = YCoord_Trans_Tilt_Toe*cos(Roll_Angle) - ZCoord_Trans_Tilt_Toe*sin(Roll_Angle);
-          ZCoord = YCoord_Trans_Tilt_Toe*sin(Roll_Angle) + ZCoord_Trans_Tilt_Toe*cos(Roll_Angle);
+          YCoord = YCoord_Trans_Tilt_Toe * cos(Roll_Angle) - ZCoord_Trans_Tilt_Toe * sin(Roll_Angle);
+          ZCoord = YCoord_Trans_Tilt_Toe * sin(Roll_Angle) + ZCoord_Trans_Tilt_Toe * cos(Roll_Angle);
 
           /*--- Update coordinates ---*/
 
-          Xcoord_Index1[iEdge] = XCoord; Ycoord_Index1[iEdge] = YCoord; Zcoord_Index1[iEdge] = ZCoord;
-
+          Xcoord_Index1[iEdge] = XCoord;
+          Ycoord_Index1[iEdge] = YCoord;
+          Zcoord_Index1[iEdge] = ZCoord;
         }
       }
 
-
       /*--- Identify the extreme of the curve and close it ---*/
 
-      Conection_Index0.reserve(Xcoord_Index0.size()+1);
-      Conection_Index1.reserve(Xcoord_Index0.size()+1);
+      Conection_Index0.reserve(Xcoord_Index0.size() + 1);
+      Conection_Index1.reserve(Xcoord_Index0.size() + 1);
 
       for (iEdge = 0; iEdge < Xcoord_Index0.size(); iEdge++) {
         Conection_Index0[iEdge] = 0;
         Conection_Index1[iEdge] = 0;
       }
 
-      for (iEdge = 0; iEdge < Xcoord_Index0.size()-1; iEdge++) {
-        for (jEdge = iEdge+1; jEdge < Xcoord_Index0.size(); jEdge++) {
-
-          if (((IGlobalID_Index0[iEdge] == IGlobalID_Index0[jEdge]) && (JGlobalID_Index0[iEdge] == JGlobalID_Index0[jEdge])) ||
-              ((IGlobalID_Index0[iEdge] == JGlobalID_Index0[jEdge]) && (JGlobalID_Index0[iEdge] == IGlobalID_Index0[jEdge])))
-          { Conection_Index0[iEdge]++; Conection_Index0[jEdge]++; }
-
-          if (((IGlobalID_Index0[iEdge] == IGlobalID_Index1[jEdge]) && (JGlobalID_Index0[iEdge] == JGlobalID_Index1[jEdge])) ||
-              ((IGlobalID_Index0[iEdge] == JGlobalID_Index1[jEdge]) && (JGlobalID_Index0[iEdge] == IGlobalID_Index1[jEdge])))
-          { Conection_Index0[iEdge]++; Conection_Index1[jEdge]++; }
+      for (iEdge = 0; iEdge < Xcoord_Index0.size() - 1; iEdge++) {
+        for (jEdge = iEdge + 1; jEdge < Xcoord_Index0.size(); jEdge++) {
+          if (((IGlobalID_Index0[iEdge] == IGlobalID_Index0[jEdge]) &&
+               (JGlobalID_Index0[iEdge] == JGlobalID_Index0[jEdge])) ||
+              ((IGlobalID_Index0[iEdge] == JGlobalID_Index0[jEdge]) &&
+               (JGlobalID_Index0[iEdge] == IGlobalID_Index0[jEdge]))) {
+            Conection_Index0[iEdge]++;
+            Conection_Index0[jEdge]++;
+          }
 
-          if (((IGlobalID_Index1[iEdge] == IGlobalID_Index0[jEdge]) && (JGlobalID_Index1[iEdge] == JGlobalID_Index0[jEdge])) ||
-              ((IGlobalID_Index1[iEdge] == JGlobalID_Index0[jEdge]) && (JGlobalID_Index1[iEdge] == IGlobalID_Index0[jEdge])))
-          { Conection_Index1[iEdge]++; Conection_Index0[jEdge]++; }
+          if (((IGlobalID_Index0[iEdge] == IGlobalID_Index1[jEdge]) &&
+               (JGlobalID_Index0[iEdge] == JGlobalID_Index1[jEdge])) ||
+              ((IGlobalID_Index0[iEdge] == JGlobalID_Index1[jEdge]) &&
+               (JGlobalID_Index0[iEdge] == IGlobalID_Index1[jEdge]))) {
+            Conection_Index0[iEdge]++;
+            Conection_Index1[jEdge]++;
+          }
 
-          if (((IGlobalID_Index1[iEdge] == IGlobalID_Index1[jEdge]) && (JGlobalID_Index1[iEdge] == JGlobalID_Index1[jEdge])) ||
-              ((IGlobalID_Index1[iEdge] == JGlobalID_Index1[jEdge]) && (JGlobalID_Index1[iEdge] == IGlobalID_Index1[jEdge])))
-          { Conection_Index1[iEdge]++; Conection_Index1[jEdge]++; }
+          if (((IGlobalID_Index1[iEdge] == IGlobalID_Index0[jEdge]) &&
+               (JGlobalID_Index1[iEdge] == JGlobalID_Index0[jEdge])) ||
+              ((IGlobalID_Index1[iEdge] == JGlobalID_Index0[jEdge]) &&
+               (JGlobalID_Index1[iEdge] == IGlobalID_Index0[jEdge]))) {
+            Conection_Index1[iEdge]++;
+            Conection_Index0[jEdge]++;
+          }
 
+          if (((IGlobalID_Index1[iEdge] == IGlobalID_Index1[jEdge]) &&
+               (JGlobalID_Index1[iEdge] == JGlobalID_Index1[jEdge])) ||
+              ((IGlobalID_Index1[iEdge] == JGlobalID_Index1[jEdge]) &&
+               (JGlobalID_Index1[iEdge] == IGlobalID_Index1[jEdge]))) {
+            Conection_Index1[iEdge]++;
+            Conection_Index1[jEdge]++;
+          }
         }
       }
 
@@ -2238,56 +2168,57 @@ void CGeometry::ComputeAirfoil_Section(su2double *Plane_P0, su2double *Plane_Nor
       /*--- Second, if it is an open curve then find the closest point to an extreme to close it  ---*/
 
       if (XcoordExtra.size() > 1) {
-
-        for (iEdge = 0; iEdge < XcoordExtra.size()-1; iEdge++) {
-
-          su2double MinDist = 1E6; FoundEdge = false; EdgeDonor = 0;
-          for (jEdge = iEdge+1; jEdge < XcoordExtra.size(); jEdge++) {
-            Dist_Value = sqrt(pow(SU2_TYPE::GetValue(XcoordExtra[iEdge])-SU2_TYPE::GetValue(XcoordExtra[jEdge]), 2.0));
+        for (iEdge = 0; iEdge < XcoordExtra.size() - 1; iEdge++) {
+          su2double MinDist = 1E6;
+          FoundEdge = false;
+          EdgeDonor = 0;
+          for (jEdge = iEdge + 1; jEdge < XcoordExtra.size(); jEdge++) {
+            Dist_Value =
+                sqrt(pow(SU2_TYPE::GetValue(XcoordExtra[iEdge]) - SU2_TYPE::GetValue(XcoordExtra[jEdge]), 2.0));
             if ((Dist_Value < MinDist) && (AddExtra[iEdge]) && (AddExtra[jEdge])) {
-              EdgeDonor = jEdge; FoundEdge = true;
+              EdgeDonor = jEdge;
+              FoundEdge = true;
             }
           }
 
           if (FoundEdge) {
-
             /*--- Add first point of the new edge ---*/
 
-            Xcoord_Index0.push_back (XcoordExtra[iEdge]);
-            Ycoord_Index0.push_back (YcoordExtra[iEdge]);
-            Zcoord_Index0.push_back (ZcoordExtra[iEdge]);
-            Variable_Index0.push_back (VariableExtra[iEdge]);
-            IGlobalID_Index0.push_back (IGlobalIDExtra[iEdge]);
-            JGlobalID_Index0.push_back (JGlobalIDExtra[iEdge]);
+            Xcoord_Index0.push_back(XcoordExtra[iEdge]);
+            Ycoord_Index0.push_back(YcoordExtra[iEdge]);
+            Zcoord_Index0.push_back(ZcoordExtra[iEdge]);
+            Variable_Index0.push_back(VariableExtra[iEdge]);
+            IGlobalID_Index0.push_back(IGlobalIDExtra[iEdge]);
+            JGlobalID_Index0.push_back(JGlobalIDExtra[iEdge]);
             AddExtra[iEdge] = false;
 
             /*--- Add second (closest)  point of the new edge ---*/
 
-            Xcoord_Index1.push_back (XcoordExtra[EdgeDonor]);
-            Ycoord_Index1.push_back (YcoordExtra[EdgeDonor]);
-            Zcoord_Index1.push_back (ZcoordExtra[EdgeDonor]);
-            Variable_Index1.push_back (VariableExtra[EdgeDonor]);
-            IGlobalID_Index1.push_back (IGlobalIDExtra[EdgeDonor]);
-            JGlobalID_Index1.push_back (JGlobalIDExtra[EdgeDonor]);
+            Xcoord_Index1.push_back(XcoordExtra[EdgeDonor]);
+            Ycoord_Index1.push_back(YcoordExtra[EdgeDonor]);
+            Zcoord_Index1.push_back(ZcoordExtra[EdgeDonor]);
+            Variable_Index1.push_back(VariableExtra[EdgeDonor]);
+            IGlobalID_Index1.push_back(IGlobalIDExtra[EdgeDonor]);
+            JGlobalID_Index1.push_back(JGlobalIDExtra[EdgeDonor]);
             AddExtra[EdgeDonor] = false;
-
           }
-
         }
 
       }
 
       else if (XcoordExtra.size() == 1) {
-        cout <<"There cutting system has failed, there is an incomplete curve (not used)." << endl;
+        cout << "There cutting system has failed, there is an incomplete curve (not used)." << endl;
       }
 
       /*--- Find and add the trailing edge to to the list
        and the contect the first point to the trailing edge ---*/
 
-      Trailing_Point = 0; Trailing_Coord = Xcoord_Index0[0];
+      Trailing_Point = 0;
+      Trailing_Coord = Xcoord_Index0[0];
       for (iEdge = 1; iEdge < Xcoord_Index0.size(); iEdge++) {
         if (Xcoord_Index0[iEdge] > Trailing_Coord) {
-          Trailing_Point = iEdge; Trailing_Coord = Xcoord_Index0[iEdge];
+          Trailing_Point = iEdge;
+          Trailing_Coord = Xcoord_Index0[iEdge];
         }
       }
 
@@ -2305,25 +2236,23 @@ void CGeometry::ComputeAirfoil_Section(su2double *Plane_P0, su2double *Plane_Nor
       IGlobalID_Airfoil.push_back(IGlobalID_Index1[Trailing_Point]);
       JGlobalID_Airfoil.push_back(JGlobalID_Index1[Trailing_Point]);
 
-      Xcoord_Index0.erase (Xcoord_Index0.begin() + Trailing_Point);
-      Ycoord_Index0.erase (Ycoord_Index0.begin() + Trailing_Point);
-      Zcoord_Index0.erase (Zcoord_Index0.begin() + Trailing_Point);
-      Variable_Index0.erase (Variable_Index0.begin() + Trailing_Point);
-      IGlobalID_Index0.erase (IGlobalID_Index0.begin() + Trailing_Point);
-      JGlobalID_Index0.erase (JGlobalID_Index0.begin() + Trailing_Point);
-
-      Xcoord_Index1.erase (Xcoord_Index1.begin() + Trailing_Point);
-      Ycoord_Index1.erase (Ycoord_Index1.begin() + Trailing_Point);
-      Zcoord_Index1.erase (Zcoord_Index1.begin() + Trailing_Point);
-      Variable_Index1.erase (Variable_Index1.begin() + Trailing_Point);
-      IGlobalID_Index1.erase (IGlobalID_Index1.begin() + Trailing_Point);
-      JGlobalID_Index1.erase (JGlobalID_Index1.begin() + Trailing_Point);
+      Xcoord_Index0.erase(Xcoord_Index0.begin() + Trailing_Point);
+      Ycoord_Index0.erase(Ycoord_Index0.begin() + Trailing_Point);
+      Zcoord_Index0.erase(Zcoord_Index0.begin() + Trailing_Point);
+      Variable_Index0.erase(Variable_Index0.begin() + Trailing_Point);
+      IGlobalID_Index0.erase(IGlobalID_Index0.begin() + Trailing_Point);
+      JGlobalID_Index0.erase(JGlobalID_Index0.begin() + Trailing_Point);
 
+      Xcoord_Index1.erase(Xcoord_Index1.begin() + Trailing_Point);
+      Ycoord_Index1.erase(Ycoord_Index1.begin() + Trailing_Point);
+      Zcoord_Index1.erase(Zcoord_Index1.begin() + Trailing_Point);
+      Variable_Index1.erase(Variable_Index1.begin() + Trailing_Point);
+      IGlobalID_Index1.erase(IGlobalID_Index1.begin() + Trailing_Point);
+      JGlobalID_Index1.erase(JGlobalID_Index1.begin() + Trailing_Point);
 
       /*--- Algorithm for adding the rest of the points ---*/
 
       do {
-
         /*--- Last added point in the list ---*/
 
         Airfoil_Point = Xcoord_Airfoil.size() - 1;
@@ -2333,23 +2262,30 @@ void CGeometry::ComputeAirfoil_Section(su2double *Plane_P0, su2double *Plane_Nor
         Found_Edge = false;
 
         for (iEdge = 0; iEdge < Xcoord_Index0.size(); iEdge++) {
-
-          if (((IGlobalID_Index0[iEdge] == IGlobalID_Airfoil[Airfoil_Point]) && (JGlobalID_Index0[iEdge] == JGlobalID_Airfoil[Airfoil_Point])) ||
-              ((IGlobalID_Index0[iEdge] == JGlobalID_Airfoil[Airfoil_Point]) && (JGlobalID_Index0[iEdge] == IGlobalID_Airfoil[Airfoil_Point]))) {
-            Next_Edge = iEdge; Found_Edge = true; Index = 0; break;
+          if (((IGlobalID_Index0[iEdge] == IGlobalID_Airfoil[Airfoil_Point]) &&
+               (JGlobalID_Index0[iEdge] == JGlobalID_Airfoil[Airfoil_Point])) ||
+              ((IGlobalID_Index0[iEdge] == JGlobalID_Airfoil[Airfoil_Point]) &&
+               (JGlobalID_Index0[iEdge] == IGlobalID_Airfoil[Airfoil_Point]))) {
+            Next_Edge = iEdge;
+            Found_Edge = true;
+            Index = 0;
+            break;
           }
 
-          if (((IGlobalID_Index1[iEdge] == IGlobalID_Airfoil[Airfoil_Point]) && (JGlobalID_Index1[iEdge] == JGlobalID_Airfoil[Airfoil_Point])) ||
-              ((IGlobalID_Index1[iEdge] == JGlobalID_Airfoil[Airfoil_Point]) && (JGlobalID_Index1[iEdge] == IGlobalID_Airfoil[Airfoil_Point]))) {
-            Next_Edge = iEdge; Found_Edge = true; Index = 1; break;
+          if (((IGlobalID_Index1[iEdge] == IGlobalID_Airfoil[Airfoil_Point]) &&
+               (JGlobalID_Index1[iEdge] == JGlobalID_Airfoil[Airfoil_Point])) ||
+              ((IGlobalID_Index1[iEdge] == JGlobalID_Airfoil[Airfoil_Point]) &&
+               (JGlobalID_Index1[iEdge] == IGlobalID_Airfoil[Airfoil_Point]))) {
+            Next_Edge = iEdge;
+            Found_Edge = true;
+            Index = 1;
+            break;
           }
-
         }
 
         /*--- Add and remove the next point to the list and the next point in the edge ---*/
 
         if (Found_Edge) {
-
           if (Index == 0) {
             Xcoord_Airfoil.push_back(Xcoord_Index1[Next_Edge]);
             Ycoord_Airfoil.push_back(Ycoord_Index1[Next_Edge]);
@@ -2382,36 +2318,43 @@ void CGeometry::ComputeAirfoil_Section(su2double *Plane_P0, su2double *Plane_Nor
           IGlobalID_Index1.erase(IGlobalID_Index1.begin() + Next_Edge);
           JGlobalID_Index1.erase(JGlobalID_Index1.begin() + Next_Edge);
 
+        } else {
+          break;
         }
-        else { break; }
 
       } while (Xcoord_Index0.size() != 0);
 
       /*--- Clean the vector before using them again for storing the upper or the lower side ---*/
 
-      Xcoord_Index0.clear(); Ycoord_Index0.clear(); Zcoord_Index0.clear(); Variable_Index0.clear();  IGlobalID_Index0.clear();  JGlobalID_Index0.clear();
-      Xcoord_Index1.clear(); Ycoord_Index1.clear(); Zcoord_Index1.clear(); Variable_Index1.clear();  IGlobalID_Index1.clear();  JGlobalID_Index1.clear();
-
+      Xcoord_Index0.clear();
+      Ycoord_Index0.clear();
+      Zcoord_Index0.clear();
+      Variable_Index0.clear();
+      IGlobalID_Index0.clear();
+      JGlobalID_Index0.clear();
+      Xcoord_Index1.clear();
+      Ycoord_Index1.clear();
+      Zcoord_Index1.clear();
+      Variable_Index1.clear();
+      IGlobalID_Index1.clear();
+      JGlobalID_Index1.clear();
     }
-
   }
 
   AD::EndPassive(wasActive);
-
 }
 
 void CGeometry::RegisterCoordinates() const {
   const bool input = true;
 
-  SU2_OMP_FOR_STAT(roundUpDiv(nPoint,omp_get_num_threads()))
+  SU2_OMP_FOR_STAT(roundUpDiv(nPoint, omp_get_num_threads()))
   for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
     nodes->RegisterCoordinates(iPoint, input);
   }
   END_SU2_OMP_FOR
 }
 
-void CGeometry::UpdateGeometry(CGeometry **geometry_container, CConfig *config) {
-
+void CGeometry::UpdateGeometry(CGeometry** geometry_container, CConfig* config) {
   geometry_container[MESH_0]->InitiateComms(geometry_container[MESH_0], config, COORDINATES);
   geometry_container[MESH_0]->CompleteComms(geometry_container[MESH_0], config, COORDINATES);
 
@@ -2422,18 +2365,16 @@ void CGeometry::UpdateGeometry(CGeometry **geometry_container, CConfig *config)
   for (unsigned short iMesh = 1; iMesh <= config->GetnMGLevels(); iMesh++) {
     /*--- Update the control volume structures ---*/
 
-    geometry_container[iMesh]->SetControlVolume(geometry_container[iMesh-1], UPDATE);
-    geometry_container[iMesh]->SetBoundControlVolume(geometry_container[iMesh-1], UPDATE);
-    geometry_container[iMesh]->SetCoord(geometry_container[iMesh-1]);
-
+    geometry_container[iMesh]->SetControlVolume(geometry_container[iMesh - 1], UPDATE);
+    geometry_container[iMesh]->SetBoundControlVolume(geometry_container[iMesh - 1], UPDATE);
+    geometry_container[iMesh]->SetCoord(geometry_container[iMesh - 1]);
   }
 
   /*--- Compute the global surface areas for all markers. ---*/
   geometry_container[MESH_0]->ComputeSurfaceAreaCfgFile(config);
 }
 
-void CGeometry::SetCustomBoundary(CConfig *config) {
-
+void CGeometry::SetCustomBoundary(CConfig* config) {
   unsigned short iMarker;
   unsigned long iVertex;
   string Marker_Tag;
@@ -2443,21 +2384,21 @@ void CGeometry::SetCustomBoundary(CConfig *config) {
   CustomBoundaryTemperature = new su2double*[nMarker];
   CustomBoundaryHeatFlux = new su2double*[nMarker];
 
-  for(iMarker=0; iMarker < nMarker; iMarker++){
+  for (iMarker = 0; iMarker < nMarker; iMarker++) {
     Marker_Tag = config->GetMarker_All_TagBound(iMarker);
     CustomBoundaryHeatFlux[iMarker] = nullptr;
     CustomBoundaryTemperature[iMarker] = nullptr;
-    if(config->GetMarker_All_PyCustom(iMarker)){
-      switch(config->GetMarker_All_KindBC(iMarker)){
+    if (config->GetMarker_All_PyCustom(iMarker)) {
+      switch (config->GetMarker_All_KindBC(iMarker)) {
         case HEAT_FLUX:
           CustomBoundaryHeatFlux[iMarker] = new su2double[nVertex[iMarker]];
-          for(iVertex=0; iVertex < nVertex[iMarker]; iVertex++){
+          for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
             CustomBoundaryHeatFlux[iMarker][iVertex] = config->GetWall_HeatFlux(Marker_Tag);
           }
           break;
         case ISOTHERMAL:
           CustomBoundaryTemperature[iMarker] = new su2double[nVertex[iMarker]];
-          for(iVertex=0; iVertex < nVertex[iMarker]; iVertex++){
+          for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
             CustomBoundaryTemperature[iMarker][iVertex] = config->GetIsothermal_Temperature(Marker_Tag);
           }
           break;
@@ -2470,19 +2411,17 @@ void CGeometry::SetCustomBoundary(CConfig *config) {
       }
     }
   }
-
 }
 
-void CGeometry::UpdateCustomBoundaryConditions(CGeometry **geometry_container, CConfig *config){
-
+void CGeometry::UpdateCustomBoundaryConditions(CGeometry** geometry_container, CConfig* config) {
   unsigned short iMGfine, iMGlevel, nMGlevel, iMarker;
 
   nMGlevel = config->GetnMGLevels();
-  for (iMGlevel=1; iMGlevel <= nMGlevel; iMGlevel++){
-    iMGfine = iMGlevel-1;
-    for(iMarker = 0; iMarker< config->GetnMarker_All(); iMarker++){
-      if(config->GetMarker_All_PyCustom(iMarker)){
-        switch(config->GetMarker_All_KindBC(iMarker)){
+  for (iMGlevel = 1; iMGlevel <= nMGlevel; iMGlevel++) {
+    iMGfine = iMGlevel - 1;
+    for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
+      if (config->GetMarker_All_PyCustom(iMarker)) {
+        switch (config->GetMarker_All_KindBC(iMarker)) {
           case HEAT_FLUX:
             geometry_container[iMGlevel]->SetMultiGridWallHeatFlux(geometry_container[iMGfine], iMarker);
             break;
@@ -2490,85 +2429,71 @@ void CGeometry::UpdateCustomBoundaryConditions(CGeometry **geometry_container, C
             geometry_container[iMGlevel]->SetMultiGridWallTemperature(geometry_container[iMGfine], iMarker);
             break;
           // Inlet flow handled in solver class.
-          default: break;
+          default:
+            break;
         }
       }
     }
   }
 }
 
-void CGeometry::ComputeSurfaceAreaCfgFile(const CConfig *config) {
-  SU2_OMP_MASTER
-  {
-    const auto nMarker_Global = config->GetnMarker_CfgFile();
-    SurfaceAreaCfgFile.resize(nMarker_Global);
-    vector<su2double> LocalSurfaceArea(nMarker_Global, 0.0);
-
-    /*--- Loop over all local markers ---*/
-    for (unsigned short iMarker = 0; iMarker < nMarker; iMarker++) {
-
-      const auto Local_TagBound = config->GetMarker_All_TagBound(iMarker);
-
-      /*--- Loop over all global markers, and find the local-global pair via
-            matching unique string tags. ---*/
-      for (unsigned short iMarker_Global = 0; iMarker_Global < nMarker_Global; iMarker_Global++) {
-
-        const auto Global_TagBound = config->GetMarker_CfgFile_TagBound(iMarker_Global);
-        if (Local_TagBound == Global_TagBound) {
+void CGeometry::ComputeSurfaceAreaCfgFile(const CConfig* config){
+    SU2_OMP_MASTER{const auto nMarker_Global = config->GetnMarker_CfgFile();
+SurfaceAreaCfgFile.resize(nMarker_Global);
+vector<su2double> LocalSurfaceArea(nMarker_Global, 0.0);
 
-          for(auto iVertex = 0ul; iVertex < nVertex[iMarker]; iVertex++ ) {
+/*--- Loop over all local markers ---*/
+for (unsigned short iMarker = 0; iMarker < nMarker; iMarker++) {
+  const auto Local_TagBound = config->GetMarker_All_TagBound(iMarker);
 
-            const auto iPoint = vertex[iMarker][iVertex]->GetNode();
+  /*--- Loop over all global markers, and find the local-global pair via
+        matching unique string tags. ---*/
+  for (unsigned short iMarker_Global = 0; iMarker_Global < nMarker_Global; iMarker_Global++) {
+    const auto Global_TagBound = config->GetMarker_CfgFile_TagBound(iMarker_Global);
+    if (Local_TagBound == Global_TagBound) {
+      for (auto iVertex = 0ul; iVertex < nVertex[iMarker]; iVertex++) {
+        const auto iPoint = vertex[iMarker][iVertex]->GetNode();
 
-            if(!nodes->GetDomain(iPoint)) continue;
+        if (!nodes->GetDomain(iPoint)) continue;
 
-            const auto AreaNormal = vertex[iMarker][iVertex]->GetNormal();
-            const auto Area = GeometryToolbox::Norm(nDim, AreaNormal);
+        const auto AreaNormal = vertex[iMarker][iVertex]->GetNormal();
+        const auto Area = GeometryToolbox::Norm(nDim, AreaNormal);
 
-            LocalSurfaceArea[iMarker_Global] += Area;
-          }// for iVertex
-        }//if Local == Global
-      }//for iMarker_Global
-    }//for iMarker
+        LocalSurfaceArea[iMarker_Global] += Area;
+      }  // for iVertex
+    }    // if Local == Global
+  }      // for iMarker_Global
+}  // for iMarker
 
-    SU2_MPI::Allreduce(LocalSurfaceArea.data(), SurfaceAreaCfgFile.data(), SurfaceAreaCfgFile.size(), MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-  } END_SU2_OMP_MASTER
+SU2_MPI::Allreduce(LocalSurfaceArea.data(), SurfaceAreaCfgFile.data(), SurfaceAreaCfgFile.size(), MPI_DOUBLE, MPI_SUM,
+                   SU2_MPI::GetComm());
+}
+END_SU2_OMP_MASTER
 }
 
-su2double CGeometry::GetSurfaceArea(const CConfig *config, unsigned short val_marker) const {
+su2double CGeometry::GetSurfaceArea(const CConfig* config, unsigned short val_marker) const {
   /*---Find the precomputed marker surface area by local-global string-matching. ---*/
   const auto Marker_Tag = config->GetMarker_All_TagBound(val_marker);
 
   for (unsigned short iMarker_Global = 0; iMarker_Global < config->GetnMarker_CfgFile(); iMarker_Global++) {
-
     const auto Global_TagBound = config->GetMarker_CfgFile_TagBound(iMarker_Global);
 
-    if (Marker_Tag == Global_TagBound)
-      return SurfaceAreaCfgFile[iMarker_Global];
-
+    if (Marker_Tag == Global_TagBound) return SurfaceAreaCfgFile[iMarker_Global];
   }
 
   SU2_MPI::Error("Unable to match local-marker with cfg-marker for Surface Area.", CURRENT_FUNCTION);
   return 0.0;
 }
 
-void CGeometry::ComputeSurf_Straightness(CConfig *config,
-                                         bool    print_on_screen) {
-
+void CGeometry::ComputeSurf_Straightness(CConfig* config, bool print_on_screen) {
   bool RefUnitNormal_defined;
-  unsigned short iDim,
-                 iMarker,
-                 iMarker_Global,
-                 nMarker_Global = config->GetnMarker_CfgFile();
+  unsigned short iDim, iMarker, iMarker_Global, nMarker_Global = config->GetnMarker_CfgFile();
   unsigned long iVertex;
   constexpr passivedouble epsilon = 1.0e-6;
   su2double Area;
-  string Local_TagBound,
-         Global_TagBound;
+  string Local_TagBound, Global_TagBound;
 
-  vector<su2double> Normal(nDim),
-                    UnitNormal(nDim),
-                    RefUnitNormal(nDim);
+  vector<su2double> Normal(nDim), UnitNormal(nDim), RefUnitNormal(nDim);
 
   /*--- Assume now that this boundary marker is straight. As soon as one
         AreaElement is found that is not aligend with a Reference then it is
@@ -2584,7 +2509,6 @@ void CGeometry::ComputeSurf_Straightness(CConfig *config,
 
   /*--- Loop over all local markers ---*/
   for (iMarker = 0; iMarker < nMarker; iMarker++) {
-
     Local_TagBound = config->GetMarker_All_TagBound(iMarker);
 
     /*--- Marker has to be Symmetry or Euler. Additionally marker can't be a
@@ -2592,62 +2516,53 @@ void CGeometry::ComputeSurf_Straightness(CConfig *config,
           other GridMovements are rigid. ---*/
     if ((config->GetMarker_All_KindBC(iMarker) == SYMMETRY_PLANE ||
          config->GetMarker_All_KindBC(iMarker) == EULER_WALL) &&
-         !config->GetMarker_Moving_Bool(Local_TagBound) &&
-         !config->GetMarker_Deform_Mesh_Bool(Local_TagBound)) {
-
+        !config->GetMarker_Moving_Bool(Local_TagBound) && !config->GetMarker_Deform_Mesh_Bool(Local_TagBound)) {
       /*--- Loop over all global markers, and find the local-global pair via
             matching unique string tags. ---*/
       for (iMarker_Global = 0; iMarker_Global < nMarker_Global; iMarker_Global++) {
-
         Global_TagBound = config->GetMarker_CfgFile_TagBound(iMarker_Global);
         if (Local_TagBound == Global_TagBound) {
-
           RefUnitNormal_defined = false;
           iVertex = 0;
 
-          while(bound_is_straight[iMarker] == true &&
-                iVertex < nVertex[iMarker]) {
-
+          while (bound_is_straight[iMarker] == true && iVertex < nVertex[iMarker]) {
             vertex[iMarker][iVertex]->GetNormal(Normal.data());
             UnitNormal = Normal;
 
             /*--- Compute unit normal. ---*/
             Area = 0.0;
-            for (iDim = 0; iDim < nDim; iDim++)
-              Area += Normal[iDim]*Normal[iDim];
+            for (iDim = 0; iDim < nDim; iDim++) Area += Normal[iDim] * Normal[iDim];
             Area = sqrt(Area);
 
             /*--- Negate for outward convention. ---*/
-            for (iDim = 0; iDim < nDim; iDim++)
-              UnitNormal[iDim] /= -Area;
+            for (iDim = 0; iDim < nDim; iDim++) UnitNormal[iDim] /= -Area;
 
             /*--- Check if unit normal is within tolerance of the Reference unit normal.
                   Reference unit normal = first unit normal found. ---*/
-            if(RefUnitNormal_defined) {
+            if (RefUnitNormal_defined) {
               for (iDim = 0; iDim < nDim; iDim++) {
-                if( abs(RefUnitNormal[iDim] - UnitNormal[iDim]) > epsilon ) {
+                if (abs(RefUnitNormal[iDim] - UnitNormal[iDim]) > epsilon) {
                   bound_is_straight[iMarker] = false;
                   break;
                 }
               }
             } else {
-              RefUnitNormal = UnitNormal; //deep copy of values
+              RefUnitNormal = UnitNormal;  // deep copy of values
               RefUnitNormal_defined = true;
             }
 
-          iVertex++;
-          }//while iVertex
-        }//if Local == Global
-      }//for iMarker_Global
+            iVertex++;
+          }  // while iVertex
+        }    // if Local == Global
+      }      // for iMarker_Global
     } else {
       /*--- Enforce default value: false ---*/
       bound_is_straight[iMarker] = false;
-    }//if sym or euler ...
-  }//for iMarker
+    }  // if sym or euler ...
+  }    // for iMarker
 
   /*--- Communicate results and print on screen. ---*/
-  if(print_on_screen) {
-
+  if (print_on_screen) {
     /*--- Additional vector which can later be MPI::Allreduce(d) to pring the results
           on screen as nMarker (local) can vary across ranks. Default 'true' as it can
           happen that a local rank does not contain an element of each surface marker.  ---*/
@@ -2658,65 +2573,60 @@ void CGeometry::ComputeSurf_Straightness(CConfig *config,
       for (iMarker_Global = 0; iMarker_Global < nMarker_Global; iMarker_Global++) {
         Global_TagBound = config->GetMarker_CfgFile_TagBound(iMarker_Global);
 
-        if(Local_TagBound == Global_TagBound)
-          bound_is_straight_Global[iMarker_Global] = bound_is_straight[iMarker];
+        if (Local_TagBound == Global_TagBound) bound_is_straight_Global[iMarker_Global] = bound_is_straight[iMarker];
 
-      }//for iMarker_Global
-    }//for iMarker
+      }  // for iMarker_Global
+    }    // for iMarker
 
-    vector<int> Buff_Send_isStraight(nMarker_Global),
-                Buff_Recv_isStraight(nMarker_Global);
+    vector<int> Buff_Send_isStraight(nMarker_Global), Buff_Recv_isStraight(nMarker_Global);
 
     /*--- Cast to int as std::vector<boolean> can be a special construct. MPI handling using <int>
           is more straight-forward. ---*/
     for (iMarker_Global = 0; iMarker_Global < nMarker_Global; iMarker_Global++)
-      Buff_Send_isStraight[iMarker_Global] = static_cast<int> (bound_is_straight_Global[iMarker_Global]);
+      Buff_Send_isStraight[iMarker_Global] = static_cast<int>(bound_is_straight_Global[iMarker_Global]);
 
     /*--- Product of type <int>(bool) is equivalnt to a 'logical and' ---*/
-    SU2_MPI::Allreduce(Buff_Send_isStraight.data(), Buff_Recv_isStraight.data(),
-                       nMarker_Global, MPI_INT, MPI_PROD, SU2_MPI::GetComm());
+    SU2_MPI::Allreduce(Buff_Send_isStraight.data(), Buff_Recv_isStraight.data(), nMarker_Global, MPI_INT, MPI_PROD,
+                       SU2_MPI::GetComm());
 
     /*--- Print results on screen. ---*/
-    if(rank == MASTER_NODE) {
+    if (rank == MASTER_NODE) {
       for (iMarker_Global = 0; iMarker_Global < nMarker_Global; iMarker_Global++) {
         if (config->GetMarker_CfgFile_KindBC(config->GetMarker_CfgFile_TagBound(iMarker_Global)) == SYMMETRY_PLANE ||
-          config->GetMarker_CfgFile_KindBC(config->GetMarker_CfgFile_TagBound(iMarker_Global)) == EULER_WALL) {
-
+            config->GetMarker_CfgFile_KindBC(config->GetMarker_CfgFile_TagBound(iMarker_Global)) == EULER_WALL) {
           cout << "Boundary marker " << config->GetMarker_CfgFile_TagBound(iMarker_Global) << " is";
-          if(Buff_Recv_isStraight[iMarker_Global] == false) cout << " NOT";
-          if(nDim == 2) cout << " a single straight." << endl;
-          if(nDim == 3) cout << " a single plane." << endl;
-        }//if sym or euler
-      }//for iMarker_Global
-    }//if rank==MASTER
-  }//if print_on_scren
-
+          if (Buff_Recv_isStraight[iMarker_Global] == false) cout << " NOT";
+          if (nDim == 2) cout << " a single straight." << endl;
+          if (nDim == 3) cout << " a single plane." << endl;
+        }  // if sym or euler
+      }    // for iMarker_Global
+    }      // if rank==MASTER
+  }        // if print_on_scren
 }
 
-
-void CGeometry::ComputeSurf_Curvature(CConfig *config) {
-
+void CGeometry::ComputeSurf_Curvature(CConfig* config) {
   unsigned short iMarker, iNeigh_Point, iDim, iNode, iNeighbor_Nodes, Neighbor_Node;
-  unsigned long Neighbor_Point, iVertex, iPoint, jPoint, iElem_Bound, iEdge, nLocalVertex, MaxLocalVertex , *Buffer_Send_nVertex, *Buffer_Receive_nVertex, TotalnPointDomain;
+  unsigned long Neighbor_Point, iVertex, iPoint, jPoint, iElem_Bound, iEdge, nLocalVertex, MaxLocalVertex,
+      *Buffer_Send_nVertex, *Buffer_Receive_nVertex, TotalnPointDomain;
   vector<unsigned long> Point_NeighborList, Elem_NeighborList, Point_Triangle, Point_Edge, Point_Critical;
-  su2double U[3] = {0.0}, V[3] = {0.0}, W[3] = {0.0}, Length_U, Length_V, Length_W, CosValue, Angle_Value, *K, *Angle_Defect, *Area_Vertex, *Angle_Alpha, *Angle_Beta, **NormalMeanK, MeanK, GaussK, MaxPrinK, cot_alpha, cot_beta, delta, X1, X2, X3, Y1, Y2, Y3, radius, *Buffer_Send_Coord, *Buffer_Receive_Coord, *Coord, Dist, MinDist, MaxK, MinK, SigmaK;
-  bool *Check_Edge;
+  su2double U[3] = {0.0}, V[3] = {0.0}, W[3] = {0.0}, Length_U, Length_V, Length_W, CosValue, Angle_Value, *K,
+            *Angle_Defect, *Area_Vertex, *Angle_Alpha, *Angle_Beta, **NormalMeanK, MeanK, GaussK, MaxPrinK, cot_alpha,
+            cot_beta, delta, X1, X2, X3, Y1, Y2, Y3, radius, *Buffer_Send_Coord, *Buffer_Receive_Coord, *Coord, Dist,
+            MinDist, MaxK, MinK, SigmaK;
+  bool* Check_Edge;
 
   /*--- Allocate surface curvature ---*/
-  K = new su2double [nPoint];
+  K = new su2double[nPoint];
   for (iPoint = 0; iPoint < nPoint; iPoint++) K[iPoint] = 0.0;
 
   if (nDim == 2) {
-
     /*--- Loop over all the markers ---*/
     for (iMarker = 0; iMarker < nMarker; iMarker++) {
-
       if (config->GetMarker_All_KindBC(iMarker) != SEND_RECEIVE) {
-
         /*--- Loop through all marker vertices again, this time also
          finding the neighbors of each node.---*/
         for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
-          iPoint  = vertex[iMarker][iVertex]->GetNode();
+          iPoint = vertex[iMarker][iVertex]->GetNode();
 
           if (nodes->GetDomain(iPoint)) {
             /*--- Loop through neighbors. In 2-D, there should be 2 nodes on either
@@ -2731,11 +2641,9 @@ void CGeometry::ComputeSurf_Curvature(CConfig *config) {
               if (nodes->GetPhysicalBoundary(Neighbor_Point)) {
                 Point_Edge.push_back(Neighbor_Point);
               }
-
             }
 
             if (Point_Edge.size() == 2) {
-
               /*--- Compute the curvature using three points ---*/
               X1 = nodes->GetCoord(iPoint, 0);
               X2 = nodes->GetCoord(Point_Edge[0], 0);
@@ -2744,46 +2652,41 @@ void CGeometry::ComputeSurf_Curvature(CConfig *config) {
               Y2 = nodes->GetCoord(Point_Edge[0], 1);
               Y3 = nodes->GetCoord(Point_Edge[1], 1);
 
-              radius = sqrt(((X2-X1)*(X2-X1) + (Y2-Y1)*(Y2-Y1))*
-                            ((X2-X3)*(X2-X3) + (Y2-Y3)*(Y2-Y3))*
-                            ((X3-X1)*(X3-X1) + (Y3-Y1)*(Y3-Y1)))/
-              (2.0*fabs(X1*Y2+X2*Y3+X3*Y1-X1*Y3-X2*Y1-X3*Y2)+EPS);
+              radius = sqrt(((X2 - X1) * (X2 - X1) + (Y2 - Y1) * (Y2 - Y1)) *
+                            ((X2 - X3) * (X2 - X3) + (Y2 - Y3) * (Y2 - Y3)) *
+                            ((X3 - X1) * (X3 - X1) + (Y3 - Y1) * (Y3 - Y1))) /
+                       (2.0 * fabs(X1 * Y2 + X2 * Y3 + X3 * Y1 - X1 * Y3 - X2 * Y1 - X3 * Y2) + EPS);
 
-              K[iPoint] = 1.0/radius;
+              K[iPoint] = 1.0 / radius;
               nodes->SetCurvature(iPoint, K[iPoint]);
             }
-
           }
-
         }
-
       }
-
     }
 
   }
 
   else {
-
-    Angle_Defect = new su2double [nPoint];
-    Area_Vertex = new su2double [nPoint];
+    Angle_Defect = new su2double[nPoint];
+    Area_Vertex = new su2double[nPoint];
     for (iPoint = 0; iPoint < nPoint; iPoint++) {
-      Angle_Defect[iPoint] = 2*PI_NUMBER;
+      Angle_Defect[iPoint] = 2 * PI_NUMBER;
       Area_Vertex[iPoint] = 0.0;
     }
 
-    Angle_Alpha = new su2double [nEdge];
-    Angle_Beta = new su2double [nEdge];
-    Check_Edge = new bool [nEdge];
+    Angle_Alpha = new su2double[nEdge];
+    Angle_Beta = new su2double[nEdge];
+    Check_Edge = new bool[nEdge];
     for (iEdge = 0; iEdge < nEdge; iEdge++) {
       Angle_Alpha[iEdge] = 0.0;
       Angle_Beta[iEdge] = 0.0;
       Check_Edge[iEdge] = true;
     }
 
-    NormalMeanK = new su2double *[nPoint];
+    NormalMeanK = new su2double*[nPoint];
     for (iPoint = 0; iPoint < nPoint; iPoint++) {
-      NormalMeanK[iPoint] = new su2double [nDim];
+      NormalMeanK[iPoint] = new su2double[nDim];
       for (iDim = 0; iDim < nDim; iDim++) {
         NormalMeanK[iPoint][iDim] = 0.0;
       }
@@ -2791,23 +2694,19 @@ void CGeometry::ComputeSurf_Curvature(CConfig *config) {
 
     /*--- Loop over all the markers ---*/
     for (iMarker = 0; iMarker < nMarker; iMarker++) {
-
       if (config->GetMarker_All_KindBC(iMarker) != SEND_RECEIVE) {
-
         /*--- Loop over all the boundary elements ---*/
         for (iElem_Bound = 0; iElem_Bound < nElem_Bound[iMarker]; iElem_Bound++) {
-
           /*--- Only triangles ---*/
           if (bound[iMarker][iElem_Bound]->GetVTK_Type() == TRIANGLE) {
-
             /*--- Loop over all the nodes of the boundary element ---*/
             for (iNode = 0; iNode < bound[iMarker][iElem_Bound]->GetnNodes(); iNode++) {
-
               iPoint = bound[iMarker][iElem_Bound]->GetNode(iNode);
 
               Point_Triangle.clear();
 
-              for (iNeighbor_Nodes = 0; iNeighbor_Nodes < bound[iMarker][iElem_Bound]->GetnNeighbor_Nodes(iNode); iNeighbor_Nodes++) {
+              for (iNeighbor_Nodes = 0; iNeighbor_Nodes < bound[iMarker][iElem_Bound]->GetnNeighbor_Nodes(iNode);
+                   iNeighbor_Nodes++) {
                 Neighbor_Node = bound[iMarker][iElem_Bound]->GetNeighbor_Nodes(iNode, iNeighbor_Nodes);
                 Neighbor_Point = bound[iMarker][iElem_Bound]->GetNode(Neighbor_Node);
                 Point_Triangle.push_back(Neighbor_Point);
@@ -2820,21 +2719,37 @@ void CGeometry::ComputeSurf_Curvature(CConfig *config) {
                 V[iDim] = nodes->GetCoord(Point_Triangle[1], iDim) - nodes->GetCoord(iPoint, iDim);
               }
 
-              W[0] = 0.5*(U[1]*V[2]-U[2]*V[1]); W[1] = -0.5*(U[0]*V[2]-U[2]*V[0]); W[2] = 0.5*(U[0]*V[1]-U[1]*V[0]);
+              W[0] = 0.5 * (U[1] * V[2] - U[2] * V[1]);
+              W[1] = -0.5 * (U[0] * V[2] - U[2] * V[0]);
+              W[2] = 0.5 * (U[0] * V[1] - U[1] * V[0]);
 
-              Length_U = 0.0; Length_V = 0.0; Length_W = 0.0; CosValue = 0.0;
-              for (iDim = 0; iDim < nDim; iDim++) { Length_U += U[iDim]*U[iDim]; Length_V += V[iDim]*V[iDim]; Length_W += W[iDim]*W[iDim]; }
-              Length_U = sqrt(Length_U); Length_V = sqrt(Length_V); Length_W = sqrt(Length_W);
-              for (iDim = 0; iDim < nDim; iDim++) { U[iDim] /= Length_U; V[iDim] /= Length_V; CosValue += U[iDim]*V[iDim]; }
+              Length_U = 0.0;
+              Length_V = 0.0;
+              Length_W = 0.0;
+              CosValue = 0.0;
+              for (iDim = 0; iDim < nDim; iDim++) {
+                Length_U += U[iDim] * U[iDim];
+                Length_V += V[iDim] * V[iDim];
+                Length_W += W[iDim] * W[iDim];
+              }
+              Length_U = sqrt(Length_U);
+              Length_V = sqrt(Length_V);
+              Length_W = sqrt(Length_W);
+              for (iDim = 0; iDim < nDim; iDim++) {
+                U[iDim] /= Length_U;
+                V[iDim] /= Length_V;
+                CosValue += U[iDim] * V[iDim];
+              }
               if (CosValue >= 1.0) CosValue = 1.0;
               if (CosValue <= -1.0) CosValue = -1.0;
 
               Angle_Value = acos(CosValue);
               Area_Vertex[iPoint] += Length_W;
               Angle_Defect[iPoint] -= Angle_Value;
-              if (Angle_Alpha[iEdge] == 0.0) Angle_Alpha[iEdge] = Angle_Value;
-              else Angle_Beta[iEdge] = Angle_Value;
-
+              if (Angle_Alpha[iEdge] == 0.0)
+                Angle_Alpha[iEdge] = Angle_Value;
+              else
+                Angle_Beta[iEdge] = Angle_Value;
             }
           }
         }
@@ -2849,26 +2764,37 @@ void CGeometry::ComputeSurf_Curvature(CConfig *config) {
             for (iNode = 0; iNode < bound[iMarker][iElem_Bound]->GetnNodes(); iNode++) {
               iPoint = bound[iMarker][iElem_Bound]->GetNode(iNode);
 
-              for (iNeighbor_Nodes = 0; iNeighbor_Nodes < bound[iMarker][iElem_Bound]->GetnNeighbor_Nodes(iNode); iNeighbor_Nodes++) {
+              for (iNeighbor_Nodes = 0; iNeighbor_Nodes < bound[iMarker][iElem_Bound]->GetnNeighbor_Nodes(iNode);
+                   iNeighbor_Nodes++) {
                 Neighbor_Node = bound[iMarker][iElem_Bound]->GetNeighbor_Nodes(iNode, iNeighbor_Nodes);
                 jPoint = bound[iMarker][iElem_Bound]->GetNode(Neighbor_Node);
 
                 iEdge = FindEdge(iPoint, jPoint);
 
                 if (Check_Edge[iEdge]) {
-
                   Check_Edge[iEdge] = false;
 
-                  if (tan(Angle_Alpha[iEdge]) != 0.0) cot_alpha = 1.0/tan(Angle_Alpha[iEdge]); else cot_alpha = 0.0;
-                  if (tan(Angle_Beta[iEdge]) != 0.0) cot_beta = 1.0/tan(Angle_Beta[iEdge]); else cot_beta = 0.0;
+                  if (tan(Angle_Alpha[iEdge]) != 0.0)
+                    cot_alpha = 1.0 / tan(Angle_Alpha[iEdge]);
+                  else
+                    cot_alpha = 0.0;
+                  if (tan(Angle_Beta[iEdge]) != 0.0)
+                    cot_beta = 1.0 / tan(Angle_Beta[iEdge]);
+                  else
+                    cot_beta = 0.0;
 
                   /*--- iPoint, and jPoint ---*/
                   for (iDim = 0; iDim < nDim; iDim++) {
-                    if (Area_Vertex[iPoint] != 0.0) NormalMeanK[iPoint][iDim] += 3.0 * (cot_alpha + cot_beta) * (nodes->GetCoord(iPoint, iDim) - nodes->GetCoord(jPoint, iDim)) / Area_Vertex[iPoint];
-                    if (Area_Vertex[jPoint] != 0.0) NormalMeanK[jPoint][iDim] += 3.0 * (cot_alpha + cot_beta) * (nodes->GetCoord(jPoint, iDim) - nodes->GetCoord(iPoint, iDim)) / Area_Vertex[jPoint];
+                    if (Area_Vertex[iPoint] != 0.0)
+                      NormalMeanK[iPoint][iDim] += 3.0 * (cot_alpha + cot_beta) *
+                                                   (nodes->GetCoord(iPoint, iDim) - nodes->GetCoord(jPoint, iDim)) /
+                                                   Area_Vertex[iPoint];
+                    if (Area_Vertex[jPoint] != 0.0)
+                      NormalMeanK[jPoint][iDim] += 3.0 * (cot_alpha + cot_beta) *
+                                                   (nodes->GetCoord(jPoint, iDim) - nodes->GetCoord(iPoint, iDim)) /
+                                                   Area_Vertex[jPoint];
                   }
                 }
-
               }
             }
           }
@@ -2882,19 +2808,19 @@ void CGeometry::ComputeSurf_Curvature(CConfig *config) {
     for (iMarker = 0; iMarker < nMarker; iMarker++) {
       if (config->GetMarker_All_KindBC(iMarker) != SEND_RECEIVE) {
         for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
-          iPoint  = vertex[iMarker][iVertex]->GetNode();
+          iPoint = vertex[iMarker][iVertex]->GetNode();
 
           if (nodes->GetDomain(iPoint)) {
-
-            if (Area_Vertex[iPoint] != 0.0) GaussK = 3.0*Angle_Defect[iPoint]/Area_Vertex[iPoint];
-            else GaussK = 0.0;
+            if (Area_Vertex[iPoint] != 0.0)
+              GaussK = 3.0 * Angle_Defect[iPoint] / Area_Vertex[iPoint];
+            else
+              GaussK = 0.0;
 
             MeanK = 0.0;
-            for (iDim = 0; iDim < nDim; iDim++)
-              MeanK += NormalMeanK[iPoint][iDim]*NormalMeanK[iPoint][iDim];
+            for (iDim = 0; iDim < nDim; iDim++) MeanK += NormalMeanK[iPoint][iDim] * NormalMeanK[iPoint][iDim];
             MeanK = sqrt(MeanK);
 
-            delta = max((MeanK*MeanK - GaussK), 0.0);
+            delta = max((MeanK * MeanK - GaussK), 0.0);
 
             MaxPrinK = MeanK + sqrt(delta);
 
@@ -2902,31 +2828,31 @@ void CGeometry::ComputeSurf_Curvature(CConfig *config) {
             K[iPoint] = MaxPrinK;
             nodes->SetCurvature(iPoint, K[iPoint]);
           }
-
         }
       }
     }
 
-    delete [] Angle_Defect;
-    delete [] Area_Vertex;
-    delete [] Angle_Alpha;
-    delete [] Angle_Beta;
-    delete [] Check_Edge;
-
-    for (iPoint = 0; iPoint < nPoint; iPoint++)
-      delete [] NormalMeanK[iPoint];
-    delete [] NormalMeanK;
+    delete[] Angle_Defect;
+    delete[] Area_Vertex;
+    delete[] Angle_Alpha;
+    delete[] Angle_Beta;
+    delete[] Check_Edge;
 
+    for (iPoint = 0; iPoint < nPoint; iPoint++) delete[] NormalMeanK[iPoint];
+    delete[] NormalMeanK;
   }
 
   /*--- Sharp edge detection is based in the statistical
    distribution of the curvature ---*/
 
-  MaxK = K[0]; MinK = K[0]; MeanK = 0.0; TotalnPointDomain = 0;
+  MaxK = K[0];
+  MinK = K[0];
+  MeanK = 0.0;
+  TotalnPointDomain = 0;
   for (iMarker = 0; iMarker < nMarker; iMarker++) {
     if (config->GetMarker_All_KindBC(iMarker) != SEND_RECEIVE) {
       for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
-        iPoint  = vertex[iMarker][iVertex]->GetNode();
+        iPoint = vertex[iMarker][iVertex]->GetNode();
         if (nodes->GetDomain(iPoint)) {
           MaxK = max(MaxK, fabs(K[iPoint]));
           MinK = min(MinK, fabs(K[iPoint]));
@@ -2937,9 +2863,12 @@ void CGeometry::ComputeSurf_Curvature(CConfig *config) {
     }
   }
 
-  su2double MyMeanK = MeanK; MeanK = 0.0;
-  su2double MyMaxK = MaxK; MaxK = 0.0;
-  unsigned long MynPointDomain = TotalnPointDomain; TotalnPointDomain = 0;
+  su2double MyMeanK = MeanK;
+  MeanK = 0.0;
+  su2double MyMaxK = MaxK;
+  MaxK = 0.0;
+  unsigned long MynPointDomain = TotalnPointDomain;
+  TotalnPointDomain = 0;
   SU2_MPI::Allreduce(&MyMeanK, &MeanK, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
   SU2_MPI::Allreduce(&MyMaxK, &MaxK, 1, MPI_DOUBLE, MPI_MAX, SU2_MPI::GetComm());
   SU2_MPI::Allreduce(&MynPointDomain, &TotalnPointDomain, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
@@ -2952,7 +2881,7 @@ void CGeometry::ComputeSurf_Curvature(CConfig *config) {
   for (iMarker = 0; iMarker < nMarker; iMarker++) {
     if (config->GetMarker_All_KindBC(iMarker) != SEND_RECEIVE) {
       for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
-        iPoint  = vertex[iMarker][iVertex]->GetNode();
+        iPoint = vertex[iMarker][iVertex]->GetNode();
         if (nodes->GetDomain(iPoint)) {
           SigmaK += (fabs(K[iPoint]) - MeanK) * (fabs(K[iPoint]) - MeanK);
         }
@@ -2960,10 +2889,11 @@ void CGeometry::ComputeSurf_Curvature(CConfig *config) {
     }
   }
 
-  su2double MySigmaK = SigmaK; SigmaK = 0.0;
+  su2double MySigmaK = SigmaK;
+  SigmaK = 0.0;
   SU2_MPI::Allreduce(&MySigmaK, &SigmaK, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
 
-  SigmaK = sqrt(SigmaK/su2double(TotalnPointDomain));
+  SigmaK = sqrt(SigmaK / su2double(TotalnPointDomain));
 
   if (rank == MASTER_NODE)
     cout << "Max K: " << MaxK << ". Mean K: " << MeanK << ". Standard deviation K: " << SigmaK << "." << endl;
@@ -2973,9 +2903,9 @@ void CGeometry::ComputeSurf_Curvature(CConfig *config) {
   for (iMarker = 0; iMarker < nMarker; iMarker++) {
     if (config->GetMarker_All_KindBC(iMarker) != SEND_RECEIVE) {
       for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
-        iPoint  = vertex[iMarker][iVertex]->GetNode();
+        iPoint = vertex[iMarker][iVertex]->GetNode();
         if (nodes->GetDomain(iPoint)) {
-          if (fabs(K[iPoint]) > MeanK + config->GetRefSharpEdges()*SigmaK) {
+          if (fabs(K[iPoint]) > MeanK + config->GetRefSharpEdges() * SigmaK) {
             Point_Critical.push_back(iPoint);
           }
         }
@@ -2985,8 +2915,8 @@ void CGeometry::ComputeSurf_Curvature(CConfig *config) {
 
   /*--- Variables and buffers needed for MPI ---*/
 
-  Buffer_Send_nVertex    = new unsigned long [1];
-  Buffer_Receive_nVertex = new unsigned long [size];
+  Buffer_Send_nVertex = new unsigned long[1];
+  Buffer_Receive_nVertex = new unsigned long[size];
 
   /*--- Count the total number of critical edge nodes. ---*/
 
@@ -2997,25 +2927,26 @@ void CGeometry::ComputeSurf_Curvature(CConfig *config) {
 
   MaxLocalVertex = 0;
   SU2_MPI::Allreduce(&nLocalVertex, &MaxLocalVertex, 1, MPI_UNSIGNED_LONG, MPI_MAX, SU2_MPI::GetComm());
-  SU2_MPI::Allgather(Buffer_Send_nVertex, 1, MPI_UNSIGNED_LONG, Buffer_Receive_nVertex, 1, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
+  SU2_MPI::Allgather(Buffer_Send_nVertex, 1, MPI_UNSIGNED_LONG, Buffer_Receive_nVertex, 1, MPI_UNSIGNED_LONG,
+                     SU2_MPI::GetComm());
 
   /*--- Create and initialize to zero some buffers to hold the coordinates
    of the boundary nodes that are communicated from each partition (all-to-all). ---*/
 
-  const unsigned long nBuffer = MaxLocalVertex*nDim;
-  Buffer_Send_Coord     = new su2double [nBuffer] ();
-  Buffer_Receive_Coord  = new su2double [size*nBuffer];
+  const unsigned long nBuffer = MaxLocalVertex * nDim;
+  Buffer_Send_Coord = new su2double[nBuffer]();
+  Buffer_Receive_Coord = new su2double[size * nBuffer];
 
   /*--- Retrieve and store the coordinates of the sharp edges boundary nodes on
    the local partition and broadcast them to all partitions. ---*/
 
   for (iVertex = 0; iVertex < Point_Critical.size(); iVertex++) {
     iPoint = Point_Critical[iVertex];
-    for (iDim = 0; iDim < nDim; iDim++)
-      Buffer_Send_Coord[iVertex*nDim+iDim] = nodes->GetCoord(iPoint, iDim);
+    for (iDim = 0; iDim < nDim; iDim++) Buffer_Send_Coord[iVertex * nDim + iDim] = nodes->GetCoord(iPoint, iDim);
   }
 
-  SU2_MPI::Allgather(Buffer_Send_Coord, nBuffer, MPI_DOUBLE, Buffer_Receive_Coord, nBuffer, MPI_DOUBLE, SU2_MPI::GetComm());
+  SU2_MPI::Allgather(Buffer_Send_Coord, nBuffer, MPI_DOUBLE, Buffer_Receive_Coord, nBuffer, MPI_DOUBLE,
+                     SU2_MPI::GetComm());
 
   /*--- Loop over all interior mesh nodes on the local partition and compute
    the distances to each of the no-slip boundary nodes in the entire mesh.
@@ -3029,11 +2960,13 @@ void CGeometry::ComputeSurf_Curvature(CConfig *config) {
       for (iVertex = 0; iVertex < Buffer_Receive_nVertex[iProcessor]; iVertex++) {
         Dist = 0.0;
         for (iDim = 0; iDim < nDim; iDim++) {
-          Dist += (Coord[iDim]-Buffer_Receive_Coord[(iProcessor*MaxLocalVertex+iVertex)*nDim+iDim])*
-          (Coord[iDim]-Buffer_Receive_Coord[(iProcessor*MaxLocalVertex+iVertex)*nDim+iDim]);
+          Dist += (Coord[iDim] - Buffer_Receive_Coord[(iProcessor * MaxLocalVertex + iVertex) * nDim + iDim]) *
+                  (Coord[iDim] - Buffer_Receive_Coord[(iProcessor * MaxLocalVertex + iVertex) * nDim + iDim]);
         }
-        if (Dist!=0.0) Dist = sqrt(Dist);
-        else Dist = 0.0;
+        if (Dist != 0.0)
+          Dist = sqrt(Dist);
+        else
+          Dist = 0.0;
         if (Dist < MinDist) MinDist = Dist;
       }
     }
@@ -3048,14 +2981,11 @@ void CGeometry::ComputeSurf_Curvature(CConfig *config) {
   delete[] Buffer_Receive_Coord;
   delete[] Buffer_Send_nVertex;
   delete[] Buffer_Receive_nVertex;
-
 }
 
-void CGeometry::FilterValuesAtElementCG(const vector<su2double> &filter_radius,
-                                        const vector<pair<ENUM_FILTER_KERNEL,su2double> > &kernels,
-                                        const unsigned short search_limit,
-                                        su2double *values) const
-{
+void CGeometry::FilterValuesAtElementCG(const vector<su2double>& filter_radius,
+                                        const vector<pair<ENUM_FILTER_KERNEL, su2double>>& kernels,
+                                        const unsigned short search_limit, su2double* values) const {
   /*--- Apply a filter to "input_values". The filter is an averaging process over the neighbourhood
   of each element, which is a circle in 2D and a sphere in 3D of radius "filter_radius".
   The filter is characterized by its kernel, i.e. how the weights are computed. Multiple kernels
@@ -3063,246 +2993,239 @@ void CGeometry::FilterValuesAtElementCG(const vector<su2double> &filter_radius,
   output values of the previous filter. ---*/
 
   /*--- Check if we need to do any work. ---*/
-  if ( kernels.empty() ) return;
-
+  if (kernels.empty()) return;
 
   /*--- FIRST: Gather the adjacency matrix, element centroids, volumes, and values on every
   processor, this is required because the filter reaches far into adjacent partitions. ---*/
 
   /*--- Adjacency matrix ---*/
   vector<unsigned long> neighbour_start;
-  long *neighbour_idx = nullptr;
-  GetGlobalElementAdjacencyMatrix(neighbour_start,neighbour_idx);
+  long* neighbour_idx = nullptr;
+  GetGlobalElementAdjacencyMatrix(neighbour_start, neighbour_idx);
 
   /*--- Element centroids and volumes. ---*/
-  su2double *cg_elem  = new su2double [Global_nElemDomain*nDim],
-            *vol_elem = new su2double [Global_nElemDomain];
+  su2double *cg_elem = new su2double[Global_nElemDomain * nDim], *vol_elem = new su2double[Global_nElemDomain];
 #ifdef HAVE_MPI
   /*--- Number of subdomain each point is part of. ---*/
   vector<char> halo_detect(Global_nElemDomain);
 #endif
 
   /*--- Inputs of a filter stage, like with CG and volumes, each processor needs to see everything. ---*/
-  su2double *work_values = new su2double [Global_nElemDomain];
+  su2double* work_values = new su2double[Global_nElemDomain];
 
   /*--- When gathering the neighborhood of each element we use a vector of booleans to indicate
   whether an element is already added to the list of neighbors (one vector per thread). ---*/
-  vector<vector<bool> > is_neighbor(omp_get_max_threads());
+  vector<vector<bool>> is_neighbor(omp_get_max_threads());
 
   /*--- Begin OpenMP parallel section, count total number of searches for which
   the recursion limit is reached and the full neighborhood is not considered. ---*/
   unsigned long limited_searches = 0;
 
-  SU2_OMP_PARALLEL_(reduction(+:limited_searches))
-  {
-
-  /*--- Initialize ---*/
-  SU2_OMP_FOR_STAT(256)
-  for(auto iElem=0ul; iElem<Global_nElemDomain; ++iElem) {
-    for(unsigned short iDim=0; iDim<nDim; ++iDim)
-      cg_elem[nDim*iElem+iDim] = 0.0;
-    vol_elem[iElem] = 0.0;
-  }
-  END_SU2_OMP_FOR
-
-  /*--- Populate ---*/
-  SU2_OMP_FOR_STAT(256)
-  for(auto iElem=0ul; iElem<nElem; ++iElem) {
-    auto iElem_global = elem[iElem]->GetGlobalIndex();
-    for(unsigned short iDim=0; iDim<nDim; ++iDim)
-      cg_elem[nDim*iElem_global+iDim] = elem[iElem]->GetCG(iDim);
-    vol_elem[iElem_global] = elem[iElem]->GetVolume();
-  }
-  END_SU2_OMP_FOR
-
-#ifdef HAVE_MPI
-  /*--- Account for the duplication introduced by the halo elements and the
-  reduction using MPI_SUM, which is required to maintain differentiabillity. ---*/
-  SU2_OMP_FOR_STAT(256)
-  for(auto iElem=0ul; iElem<Global_nElemDomain; ++iElem)
-    halo_detect[iElem] = 0;
-  END_SU2_OMP_FOR
-
-  SU2_OMP_FOR_STAT(256)
-  for(auto iElem=0ul; iElem<nElem; ++iElem)
-    halo_detect[elem[iElem]->GetGlobalIndex()] = 1;
-  END_SU2_OMP_FOR
-
-  /*--- Share with all processors ---*/
-  BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS
-  {
-    su2double* dbl_buffer = new su2double [Global_nElemDomain*nDim];
-    SU2_MPI::Allreduce(cg_elem,dbl_buffer,Global_nElemDomain*nDim,MPI_DOUBLE,MPI_SUM,SU2_MPI::GetComm());
-    swap(dbl_buffer, cg_elem); delete [] dbl_buffer;
-
-    dbl_buffer = new su2double [Global_nElemDomain];
-    SU2_MPI::Allreduce(vol_elem,dbl_buffer,Global_nElemDomain,MPI_DOUBLE,MPI_SUM,SU2_MPI::GetComm());
-    swap(dbl_buffer, vol_elem); delete [] dbl_buffer;
-
-    vector<char> char_buffer(Global_nElemDomain);
-    MPI_Allreduce(halo_detect.data(),char_buffer.data(),Global_nElemDomain,MPI_CHAR,MPI_SUM,SU2_MPI::GetComm());
-    halo_detect.swap(char_buffer);
-  }
-  END_SU2_OMP_SAFE_GLOBAL_ACCESS
-
-  SU2_OMP_FOR_STAT(256)
-  for(auto iElem=0ul; iElem<Global_nElemDomain; ++iElem) {
-    su2double numRepeat = halo_detect[iElem];
-    for(unsigned short iDim=0; iDim<nDim; ++iDim)
-      cg_elem[nDim*iElem+iDim] /= numRepeat;
-    vol_elem[iElem] /= numRepeat;
-  }
-  END_SU2_OMP_FOR
-#endif
-
-  /*--- SECOND: Each processor performs the average for its elements. For each
-  element we look for neighbours of neighbours of... until the distance to the
-  closest newly found one is greater than the filter radius.  ---*/
-
-  is_neighbor[omp_get_thread_num()].resize(Global_nElemDomain,false);
-
-  for (unsigned long iKernel=0; iKernel<kernels.size(); ++iKernel)
-  {
-    auto kernel_type = kernels[iKernel].first;
-    su2double kernel_param = kernels[iKernel].second;
-    su2double kernel_radius = filter_radius[iKernel];
-
-    /*--- Synchronize work values ---*/
+  SU2_OMP_PARALLEL_(reduction(+ : limited_searches)) {
     /*--- Initialize ---*/
     SU2_OMP_FOR_STAT(256)
-    for(auto iElem=0ul; iElem<Global_nElemDomain; ++iElem)
-      work_values[iElem] = 0.0;
+    for (auto iElem = 0ul; iElem < Global_nElemDomain; ++iElem) {
+      for (unsigned short iDim = 0; iDim < nDim; ++iDim) cg_elem[nDim * iElem + iDim] = 0.0;
+      vol_elem[iElem] = 0.0;
+    }
     END_SU2_OMP_FOR
 
     /*--- Populate ---*/
     SU2_OMP_FOR_STAT(256)
-    for(auto iElem=0ul; iElem<nElem; ++iElem)
-      work_values[elem[iElem]->GetGlobalIndex()] = values[iElem];
+    for (auto iElem = 0ul; iElem < nElem; ++iElem) {
+      auto iElem_global = elem[iElem]->GetGlobalIndex();
+      for (unsigned short iDim = 0; iDim < nDim; ++iDim) cg_elem[nDim * iElem_global + iDim] = elem[iElem]->GetCG(iDim);
+      vol_elem[iElem_global] = elem[iElem]->GetVolume();
+    }
     END_SU2_OMP_FOR
 
 #ifdef HAVE_MPI
+    /*--- Account for the duplication introduced by the halo elements and the
+    reduction using MPI_SUM, which is required to maintain differentiabillity. ---*/
+    SU2_OMP_FOR_STAT(256)
+    for (auto iElem = 0ul; iElem < Global_nElemDomain; ++iElem) halo_detect[iElem] = 0;
+    END_SU2_OMP_FOR
+
+    SU2_OMP_FOR_STAT(256)
+    for (auto iElem = 0ul; iElem < nElem; ++iElem) halo_detect[elem[iElem]->GetGlobalIndex()] = 1;
+    END_SU2_OMP_FOR
+
     /*--- Share with all processors ---*/
-    BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS
-    {
-      su2double *buffer = new su2double [Global_nElemDomain];
-      SU2_MPI::Allreduce(work_values,buffer,Global_nElemDomain,MPI_DOUBLE,MPI_SUM,SU2_MPI::GetComm());
-      swap(buffer, work_values); delete [] buffer;
+    BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
+      su2double* dbl_buffer = new su2double[Global_nElemDomain * nDim];
+      SU2_MPI::Allreduce(cg_elem, dbl_buffer, Global_nElemDomain * nDim, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
+      swap(dbl_buffer, cg_elem);
+      delete[] dbl_buffer;
+
+      dbl_buffer = new su2double[Global_nElemDomain];
+      SU2_MPI::Allreduce(vol_elem, dbl_buffer, Global_nElemDomain, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
+      swap(dbl_buffer, vol_elem);
+      delete[] dbl_buffer;
+
+      vector<char> char_buffer(Global_nElemDomain);
+      MPI_Allreduce(halo_detect.data(), char_buffer.data(), Global_nElemDomain, MPI_CHAR, MPI_SUM, SU2_MPI::GetComm());
+      halo_detect.swap(char_buffer);
     }
     END_SU2_OMP_SAFE_GLOBAL_ACCESS
 
-    /*--- Account for duplication ---*/
     SU2_OMP_FOR_STAT(256)
-    for(auto iElem=0ul; iElem<Global_nElemDomain; ++iElem) {
+    for (auto iElem = 0ul; iElem < Global_nElemDomain; ++iElem) {
       su2double numRepeat = halo_detect[iElem];
-      work_values[iElem] /= numRepeat;
+      for (unsigned short iDim = 0; iDim < nDim; ++iDim) cg_elem[nDim * iElem + iDim] /= numRepeat;
+      vol_elem[iElem] /= numRepeat;
     }
     END_SU2_OMP_FOR
 #endif
 
-    /*--- Filter ---*/
-    SU2_OMP_FOR_DYN(128)
-    for(auto iElem=0ul; iElem<nElem; ++iElem)
-    {
-      int thread = omp_get_thread_num();
+    /*--- SECOND: Each processor performs the average for its elements. For each
+    element we look for neighbours of neighbours of... until the distance to the
+    closest newly found one is greater than the filter radius.  ---*/
 
-      /*--- Center of the search ---*/
-      auto iElem_global = elem[iElem]->GetGlobalIndex();
+    is_neighbor[omp_get_thread_num()].resize(Global_nElemDomain, false);
+
+    for (unsigned long iKernel = 0; iKernel < kernels.size(); ++iKernel) {
+      auto kernel_type = kernels[iKernel].first;
+      su2double kernel_param = kernels[iKernel].second;
+      su2double kernel_radius = filter_radius[iKernel];
+
+      /*--- Synchronize work values ---*/
+      /*--- Initialize ---*/
+      SU2_OMP_FOR_STAT(256)
+      for (auto iElem = 0ul; iElem < Global_nElemDomain; ++iElem) work_values[iElem] = 0.0;
+      END_SU2_OMP_FOR
 
-      /*--- Find the neighbours of iElem ---*/
-      vector<long> neighbours;
-      limited_searches += !GetRadialNeighbourhood(iElem_global, SU2_TYPE::GetValue(kernel_radius),
-                                                  search_limit, neighbour_start, neighbour_idx,
-                                                  cg_elem, neighbours, is_neighbor[thread]);
-      /*--- Apply the kernel ---*/
-      su2double weight = 0.0, numerator = 0.0, denominator = 0.0;
-
-      switch ( kernel_type ) {
-        /*--- distance-based kernels (weighted averages) ---*/
-        case ENUM_FILTER_KERNEL::CONSTANT_WEIGHT:
-        case ENUM_FILTER_KERNEL::CONICAL_WEIGHT:
-        case ENUM_FILTER_KERNEL::GAUSSIAN_WEIGHT:
-
-          for (auto idx : neighbours)
-          {
-            su2double distance = 0.0;
-            for (unsigned short iDim=0; iDim<nDim; ++iDim)
-              distance += pow(cg_elem[nDim*iElem_global+iDim]-cg_elem[nDim*idx+iDim],2);
-            distance = sqrt(distance);
-
-            switch ( kernel_type ) {
-              case ENUM_FILTER_KERNEL::CONSTANT_WEIGHT: weight = 1.0; break;
-              case ENUM_FILTER_KERNEL::CONICAL_WEIGHT: weight = kernel_radius-distance; break;
-              case ENUM_FILTER_KERNEL::GAUSSIAN_WEIGHT: weight = exp(-0.5*pow(distance/kernel_param,2)); break;
-              default: break;
+      /*--- Populate ---*/
+      SU2_OMP_FOR_STAT(256)
+      for (auto iElem = 0ul; iElem < nElem; ++iElem) work_values[elem[iElem]->GetGlobalIndex()] = values[iElem];
+      END_SU2_OMP_FOR
+
+#ifdef HAVE_MPI
+      /*--- Share with all processors ---*/
+      BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
+        su2double* buffer = new su2double[Global_nElemDomain];
+        SU2_MPI::Allreduce(work_values, buffer, Global_nElemDomain, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
+        swap(buffer, work_values);
+        delete[] buffer;
+      }
+      END_SU2_OMP_SAFE_GLOBAL_ACCESS
+
+      /*--- Account for duplication ---*/
+      SU2_OMP_FOR_STAT(256)
+      for (auto iElem = 0ul; iElem < Global_nElemDomain; ++iElem) {
+        su2double numRepeat = halo_detect[iElem];
+        work_values[iElem] /= numRepeat;
+      }
+      END_SU2_OMP_FOR
+#endif
+
+      /*--- Filter ---*/
+      SU2_OMP_FOR_DYN(128)
+      for (auto iElem = 0ul; iElem < nElem; ++iElem) {
+        int thread = omp_get_thread_num();
+
+        /*--- Center of the search ---*/
+        auto iElem_global = elem[iElem]->GetGlobalIndex();
+
+        /*--- Find the neighbours of iElem ---*/
+        vector<long> neighbours;
+        limited_searches +=
+            !GetRadialNeighbourhood(iElem_global, SU2_TYPE::GetValue(kernel_radius), search_limit, neighbour_start,
+                                    neighbour_idx, cg_elem, neighbours, is_neighbor[thread]);
+        /*--- Apply the kernel ---*/
+        su2double weight = 0.0, numerator = 0.0, denominator = 0.0;
+
+        switch (kernel_type) {
+          /*--- distance-based kernels (weighted averages) ---*/
+          case ENUM_FILTER_KERNEL::CONSTANT_WEIGHT:
+          case ENUM_FILTER_KERNEL::CONICAL_WEIGHT:
+          case ENUM_FILTER_KERNEL::GAUSSIAN_WEIGHT:
+
+            for (auto idx : neighbours) {
+              su2double distance = 0.0;
+              for (unsigned short iDim = 0; iDim < nDim; ++iDim)
+                distance += pow(cg_elem[nDim * iElem_global + iDim] - cg_elem[nDim * idx + iDim], 2);
+              distance = sqrt(distance);
+
+              switch (kernel_type) {
+                case ENUM_FILTER_KERNEL::CONSTANT_WEIGHT:
+                  weight = 1.0;
+                  break;
+                case ENUM_FILTER_KERNEL::CONICAL_WEIGHT:
+                  weight = kernel_radius - distance;
+                  break;
+                case ENUM_FILTER_KERNEL::GAUSSIAN_WEIGHT:
+                  weight = exp(-0.5 * pow(distance / kernel_param, 2));
+                  break;
+                default:
+                  break;
+              }
+              weight *= vol_elem[idx];
+              numerator += weight * work_values[idx];
+              denominator += weight;
             }
-            weight *= vol_elem[idx];
-            numerator   += weight*work_values[idx];
-            denominator += weight;
-          }
-          values[iElem] = numerator/denominator;
-          break;
+            values[iElem] = numerator / denominator;
+            break;
 
-        /*--- morphology kernels (image processing) ---*/
-        case ENUM_FILTER_KERNEL::DILATE_MORPH:
-        case ENUM_FILTER_KERNEL::ERODE_MORPH:
+          /*--- morphology kernels (image processing) ---*/
+          case ENUM_FILTER_KERNEL::DILATE_MORPH:
+          case ENUM_FILTER_KERNEL::ERODE_MORPH:
 
-          for (auto idx : neighbours)
-          {
-            switch ( kernel_type ) {
-              case ENUM_FILTER_KERNEL::DILATE_MORPH: numerator += exp(kernel_param*work_values[idx]); break;
-              case ENUM_FILTER_KERNEL::ERODE_MORPH: numerator += exp(kernel_param*(1.0-work_values[idx])); break;
-              default: break;
+            for (auto idx : neighbours) {
+              switch (kernel_type) {
+                case ENUM_FILTER_KERNEL::DILATE_MORPH:
+                  numerator += exp(kernel_param * work_values[idx]);
+                  break;
+                case ENUM_FILTER_KERNEL::ERODE_MORPH:
+                  numerator += exp(kernel_param * (1.0 - work_values[idx]));
+                  break;
+                default:
+                  break;
+              }
+              denominator += 1.0;
             }
-            denominator += 1.0;
-          }
-          values[iElem] = log(numerator/denominator)/kernel_param;
-          if ( kernel_type==ENUM_FILTER_KERNEL::ERODE_MORPH ) values[iElem] = 1.0-values[iElem];
-          break;
+            values[iElem] = log(numerator / denominator) / kernel_param;
+            if (kernel_type == ENUM_FILTER_KERNEL::ERODE_MORPH) values[iElem] = 1.0 - values[iElem];
+            break;
 
-        default:
-          SU2_MPI::Error("Unknown type of filter kernel",CURRENT_FUNCTION);
+          default:
+            SU2_MPI::Error("Unknown type of filter kernel", CURRENT_FUNCTION);
+        }
       }
+      END_SU2_OMP_FOR
     }
-    END_SU2_OMP_FOR
-  }
-
   }
   END_SU2_OMP_PARALLEL
 
   limited_searches /= kernels.size();
 
   unsigned long tmp = limited_searches;
-  SU2_MPI::Reduce(&tmp,&limited_searches,1,MPI_UNSIGNED_LONG,MPI_SUM,MASTER_NODE,SU2_MPI::GetComm());
+  SU2_MPI::Reduce(&tmp, &limited_searches, 1, MPI_UNSIGNED_LONG, MPI_SUM, MASTER_NODE, SU2_MPI::GetComm());
 
-  if (rank==MASTER_NODE && limited_searches>0)
-    cout << "Warning: The filter radius was limited for " << limited_searches
-         << " elements (" << limited_searches/(0.01*Global_nElemDomain) << "%).\n";
+  if (rank == MASTER_NODE && limited_searches > 0)
+    cout << "Warning: The filter radius was limited for " << limited_searches << " elements ("
+         << limited_searches / (0.01 * Global_nElemDomain) << "%).\n";
 
-  delete [] neighbour_idx;
-  delete [] cg_elem;
-  delete [] vol_elem;
-  delete [] work_values;
+  delete[] neighbour_idx;
+  delete[] cg_elem;
+  delete[] vol_elem;
+  delete[] work_values;
 }
 
-void CGeometry::GetGlobalElementAdjacencyMatrix(vector<unsigned long> &neighbour_start,
-                                                long *&neighbour_idx) const
-{
-  if ( neighbour_idx != nullptr )
-    SU2_MPI::Error("neighbour_idx is expected to be NULL, stopping to avoid a potential memory leak",CURRENT_FUNCTION);
+void CGeometry::GetGlobalElementAdjacencyMatrix(vector<unsigned long>& neighbour_start, long*& neighbour_idx) const {
+  if (neighbour_idx != nullptr)
+    SU2_MPI::Error("neighbour_idx is expected to be NULL, stopping to avoid a potential memory leak", CURRENT_FUNCTION);
 
   /*--- Determine how much space we need for the adjacency matrix by counting the
   neighbours of each element, i.e. its number of faces---*/
-  unsigned short *nFaces_elem = new unsigned short [Global_nElemDomain];
+  unsigned short* nFaces_elem = new unsigned short[Global_nElemDomain];
 
-  SU2_OMP_PARALLEL
-  {
+  SU2_OMP_PARALLEL {
     SU2_OMP_FOR_STAT(256)
-    for(auto iElem=0ul; iElem<Global_nElemDomain; ++iElem)
-      nFaces_elem[iElem] = 0;
+    for (auto iElem = 0ul; iElem < Global_nElemDomain; ++iElem) nFaces_elem[iElem] = 0;
     END_SU2_OMP_FOR
 
     SU2_OMP_FOR_STAT(256)
-    for(auto iElem=0ul; iElem<nElem; ++iElem) {
+    for (auto iElem = 0ul; iElem < nElem; ++iElem) {
       auto iElem_global = elem[iElem]->GetGlobalIndex();
       nFaces_elem[iElem_global] = elem[iElem]->GetnFaces();
     }
@@ -3312,47 +3235,45 @@ void CGeometry::GetGlobalElementAdjacencyMatrix(vector<unsigned long> &neighbour
 #ifdef HAVE_MPI
   /*--- Share with all processors ---*/
   {
-    unsigned short *buffer = new unsigned short [Global_nElemDomain];
-    MPI_Allreduce(nFaces_elem,buffer,Global_nElemDomain,MPI_UNSIGNED_SHORT,MPI_MAX,SU2_MPI::GetComm());
+    unsigned short* buffer = new unsigned short[Global_nElemDomain];
+    MPI_Allreduce(nFaces_elem, buffer, Global_nElemDomain, MPI_UNSIGNED_SHORT, MPI_MAX, SU2_MPI::GetComm());
     /*--- swap pointers and delete old data to keep the same variable name after reduction ---*/
-    swap(buffer, nFaces_elem); delete [] buffer;
+    swap(buffer, nFaces_elem);
+    delete[] buffer;
   }
 #endif
 
   /*--- Vector with the addresses of the start of the neighbours of a given element.
   This is generated by a cumulative sum of the neighbour count. ---*/
-  neighbour_start.resize(Global_nElemDomain+1);
+  neighbour_start.resize(Global_nElemDomain + 1);
 
   neighbour_start[0] = 0;
-  for(auto iElem=0ul; iElem<Global_nElemDomain; ++iElem) {
-    neighbour_start[iElem+1] = neighbour_start[iElem]+nFaces_elem[iElem];
+  for (auto iElem = 0ul; iElem < Global_nElemDomain; ++iElem) {
+    neighbour_start[iElem + 1] = neighbour_start[iElem] + nFaces_elem[iElem];
   }
-  delete [] nFaces_elem;
+  delete[] nFaces_elem;
 
   /*--- Allocate ---*/
   unsigned long matrix_size = neighbour_start[Global_nElemDomain];
-  neighbour_idx = new long [matrix_size];
+  neighbour_idx = new long[matrix_size];
 
-  SU2_OMP_PARALLEL
-  {
+  SU2_OMP_PARALLEL {
     /*--- Initialize ---*/
     SU2_OMP_FOR_STAT(256)
-    for(auto iElem=0ul; iElem<matrix_size; ++iElem) neighbour_idx[iElem] = -1;
+    for (auto iElem = 0ul; iElem < matrix_size; ++iElem) neighbour_idx[iElem] = -1;
     END_SU2_OMP_FOR
 
     /*--- Populate ---*/
     SU2_OMP_FOR_STAT(128)
-    for(auto iElem=0ul; iElem<nElem; ++iElem)
-    {
+    for (auto iElem = 0ul; iElem < nElem; ++iElem) {
       auto iElem_global = elem[iElem]->GetGlobalIndex();
       auto start_pos = neighbour_start[iElem_global];
 
-      for(unsigned short iFace=0; iFace<elem[iElem]->GetnFaces(); ++iFace)
-      {
+      for (unsigned short iFace = 0; iFace < elem[iElem]->GetnFaces(); ++iFace) {
         long neighbour = elem[iElem]->GetNeighbor_Elements(iFace);
 
-        if ( neighbour>=0 ) {
-          neighbour_idx[start_pos+iFace] = elem[neighbour]->GetGlobalIndex();
+        if (neighbour >= 0) {
+          neighbour_idx[start_pos + iFace] = elem[neighbour]->GetGlobalIndex();
         }
       }
     }
@@ -3362,25 +3283,20 @@ void CGeometry::GetGlobalElementAdjacencyMatrix(vector<unsigned long> &neighbour
 #ifdef HAVE_MPI
   /*--- Share with all processors ---*/
   {
-    long *buffer = new long [matrix_size];
-    MPI_Allreduce(neighbour_idx,buffer,matrix_size,MPI_LONG,MPI_MAX,SU2_MPI::GetComm());
-    swap(buffer, neighbour_idx); delete [] buffer;
+    long* buffer = new long[matrix_size];
+    MPI_Allreduce(neighbour_idx, buffer, matrix_size, MPI_LONG, MPI_MAX, SU2_MPI::GetComm());
+    swap(buffer, neighbour_idx);
+    delete[] buffer;
   }
 #endif
 }
 
-bool CGeometry::GetRadialNeighbourhood(const unsigned long iElem_global,
-                                       const passivedouble radius,
-                                       size_t search_limit,
-                                       const vector<unsigned long> &neighbour_start,
-                                       const long *neighbour_idx,
-                                       const su2double *cg_elem,
-                                       vector<long> &neighbours,
-                                       vector<bool> &is_neighbor) const
-{
+bool CGeometry::GetRadialNeighbourhood(const unsigned long iElem_global, const passivedouble radius,
+                                       size_t search_limit, const vector<unsigned long>& neighbour_start,
+                                       const long* neighbour_idx, const su2double* cg_elem, vector<long>& neighbours,
+                                       vector<bool>& is_neighbor) const {
   /*--- Validate inputs if we are debugging. ---*/
-  assert(neighbour_start.size() == Global_nElemDomain+1 &&
-         neighbour_idx != nullptr && cg_elem != nullptr &&
+  assert(neighbour_start.size() == Global_nElemDomain + 1 && neighbour_idx != nullptr && cg_elem != nullptr &&
          is_neighbor.size() == Global_nElemDomain && "invalid inputs");
 
   /*--- 0 search_limit means "unlimited" (it will probably
@@ -3393,26 +3309,25 @@ bool CGeometry::GetRadialNeighbourhood(const unsigned long iElem_global,
   is_neighbor[iElem_global] = true;
 
   passivedouble X0[3] = {0.0, 0.0, 0.0};
-  for (unsigned short iDim=0; iDim<nDim; ++iDim)
-    X0[iDim] = SU2_TYPE::GetValue(cg_elem[nDim*iElem_global+iDim]);
+  for (unsigned short iDim = 0; iDim < nDim; ++iDim) X0[iDim] = SU2_TYPE::GetValue(cg_elem[nDim * iElem_global + iDim]);
 
   /*--- Loop stops when "neighbours" stops changing size, or degree reaches limit. ---*/
   bool finished = false;
-  for (size_t degree=0, start=0; degree < search_limit && !finished; ++degree)
-  {
+  for (size_t degree = 0, start = 0; degree < search_limit && !finished; ++degree) {
     /*--- For each element of the last degree added consider its immediate
      neighbours, that are not already neighbours, as candidates. ---*/
     vector<long> candidates;
 
-    for (auto it = neighbours.begin()+start; it!=neighbours.end(); ++it) {
+    for (auto it = neighbours.begin() + start; it != neighbours.end(); ++it) {
       /*--- scan row of the adjacency matrix of element *it ---*/
-      for (auto i = neighbour_start[*it]; i < neighbour_start[(*it)+1]; ++i) {
+      for (auto i = neighbour_start[*it]; i < neighbour_start[(*it) + 1]; ++i) {
         auto idx = neighbour_idx[i];
-        if (idx>=0) if (!is_neighbor[idx]) {
-          candidates.push_back(idx);
-          /*--- mark as neighbour for now to avoid duplicate candidates. ---*/
-          is_neighbor[idx] = true;
-        }
+        if (idx >= 0)
+          if (!is_neighbor[idx]) {
+            candidates.push_back(idx);
+            /*--- mark as neighbour for now to avoid duplicate candidates. ---*/
+            is_neighbor[idx] = true;
+          }
       }
     }
     /*--- update start position to fetch next degree candidates. ---*/
@@ -3420,100 +3335,108 @@ bool CGeometry::GetRadialNeighbourhood(const unsigned long iElem_global,
 
     /*--- Add candidates within "radius" of X0, if none qualifies we are "finished". ---*/
     finished = true;
-    for (auto idx : candidates)
-    {
+    for (auto idx : candidates) {
       /*--- passivedouble as we only need to compare "distance". ---*/
       passivedouble distance = 0.0;
-      for (unsigned short iDim=0; iDim<nDim; ++iDim)
-        distance += pow(X0[iDim]-SU2_TYPE::GetValue(cg_elem[nDim*idx+iDim]),2);
+      for (unsigned short iDim = 0; iDim < nDim; ++iDim)
+        distance += pow(X0[iDim] - SU2_TYPE::GetValue(cg_elem[nDim * idx + iDim]), 2);
 
-      if(distance < pow(radius,2)) {
+      if (distance < pow(radius, 2)) {
         neighbours.push_back(idx);
         finished = false;
       }
       /*--- not a neighbour in the end. ---*/
-      else is_neighbor[idx] = false;
+      else
+        is_neighbor[idx] = false;
     }
   }
   /*--- Restore the state of the working vector for next call. ---*/
-  for(auto idx : neighbours) is_neighbor[idx] = false;
+  for (auto idx : neighbours) is_neighbor[idx] = false;
 
   return finished;
 }
 
-void CGeometry::SetElemVolume()
-{
-  SU2_OMP_PARALLEL
-  {
-  /*--- Create a bank of elements to avoid instantiating inside loop. ---*/
-  CElement *elements[4] = {nullptr, nullptr, nullptr, nullptr};
+void CGeometry::SetElemVolume() {
+  SU2_OMP_PARALLEL {
+    /*--- Create a bank of elements to avoid instantiating inside loop. ---*/
+    CElement* elements[4] = {nullptr, nullptr, nullptr, nullptr};
 
-  if (nDim==2) {
-    elements[0] = new CTRIA1();
-    elements[1] = new CQUAD4();
-  } else {
-    elements[0] = new CTETRA1();
-    elements[1] = new CPYRAM5();
-    elements[2] = new CPRISM6();
-    elements[3] = new CHEXA8();
-  }
-
-  /*--- Compute and store the volume of each "elem". ---*/
-  SU2_OMP_FOR_DYN(128)
-  for (unsigned long iElem=0; iElem<nElem; ++iElem)
-  {
-    /*--- Get the appropriate type of element. ---*/
-    CElement* element = nullptr;
-    switch (elem[iElem]->GetVTK_Type()) {
-      case TRIANGLE:      element = elements[0]; break;
-      case QUADRILATERAL: element = elements[1]; break;
-      case TETRAHEDRON:   element = elements[0]; break;
-      case PYRAMID:       element = elements[1]; break;
-      case PRISM:         element = elements[2]; break;
-      case HEXAHEDRON:    element = elements[3]; break;
-      default:
-        SU2_MPI::Error("Cannot compute the area/volume of a 1D element.",CURRENT_FUNCTION);
+    if (nDim == 2) {
+      elements[0] = new CTRIA1();
+      elements[1] = new CQUAD4();
+    } else {
+      elements[0] = new CTETRA1();
+      elements[1] = new CPYRAM5();
+      elements[2] = new CPRISM6();
+      elements[3] = new CHEXA8();
     }
-    /*--- Set the nodal coordinates of the element. ---*/
-    for (unsigned short iNode=0; iNode<elem[iElem]->GetnNodes(); ++iNode) {
-      unsigned long node_idx = elem[iElem]->GetNode(iNode);
-      for (unsigned short iDim=0; iDim<nDim; ++iDim) {
-        su2double coord = nodes->GetCoord(node_idx, iDim);
-        element->SetRef_Coord(iNode, iDim, coord);
+
+    /*--- Compute and store the volume of each "elem". ---*/
+    SU2_OMP_FOR_DYN(128)
+    for (unsigned long iElem = 0; iElem < nElem; ++iElem) {
+      /*--- Get the appropriate type of element. ---*/
+      CElement* element = nullptr;
+      switch (elem[iElem]->GetVTK_Type()) {
+        case TRIANGLE:
+          element = elements[0];
+          break;
+        case QUADRILATERAL:
+          element = elements[1];
+          break;
+        case TETRAHEDRON:
+          element = elements[0];
+          break;
+        case PYRAMID:
+          element = elements[1];
+          break;
+        case PRISM:
+          element = elements[2];
+          break;
+        case HEXAHEDRON:
+          element = elements[3];
+          break;
+        default:
+          SU2_MPI::Error("Cannot compute the area/volume of a 1D element.", CURRENT_FUNCTION);
+      }
+      /*--- Set the nodal coordinates of the element. ---*/
+      for (unsigned short iNode = 0; iNode < elem[iElem]->GetnNodes(); ++iNode) {
+        unsigned long node_idx = elem[iElem]->GetNode(iNode);
+        for (unsigned short iDim = 0; iDim < nDim; ++iDim) {
+          su2double coord = nodes->GetCoord(node_idx, iDim);
+          element->SetRef_Coord(iNode, iDim, coord);
+        }
       }
+      /*--- Compute ---*/
+      if (nDim == 2)
+        elem[iElem]->SetVolume(element->ComputeArea());
+      else
+        elem[iElem]->SetVolume(element->ComputeVolume());
     }
-    /*--- Compute ---*/
-    if(nDim==2) elem[iElem]->SetVolume(element->ComputeArea());
-    else        elem[iElem]->SetVolume(element->ComputeVolume());
-  }
-  END_SU2_OMP_FOR
-
-  delete elements[0];
-  delete elements[1];
-  if (nDim==3) {
-    delete elements[2];
-    delete elements[3];
-  }
+    END_SU2_OMP_FOR
 
+    delete elements[0];
+    delete elements[1];
+    if (nDim == 3) {
+      delete elements[2];
+      delete elements[3];
+    }
   }
   END_SU2_OMP_PARALLEL
 }
 
-void CGeometry::SetRotationalVelocity(const CConfig *config, bool print) {
-
+void CGeometry::SetRotationalVelocity(const CConfig* config, bool print) {
   unsigned long iPoint;
   unsigned short iDim;
 
-  su2double GridVel[3] = {0.0,0.0,0.0}, Distance[3] = {0.0,0.0,0.0},
-            Center[3] = {0.0,0.0,0.0}, Omega[3] = {0.0,0.0,0.0},
-            xDot[3] = {0.0,0.0,0.0};
+  su2double GridVel[3] = {0.0, 0.0, 0.0}, Distance[3] = {0.0, 0.0, 0.0}, Center[3] = {0.0, 0.0, 0.0},
+            Omega[3] = {0.0, 0.0, 0.0}, xDot[3] = {0.0, 0.0, 0.0};
 
   /*--- Center of rotation & angular velocity vector from config ---*/
 
   for (iDim = 0; iDim < 3; iDim++) {
     Center[iDim] = config->GetMotion_Origin(iDim);
-    Omega[iDim]  = config->GetRotation_Rate(iDim)/config->GetOmega_Ref();
-    xDot[iDim] = config->GetTranslation_Rate(iDim)/config->GetVelocity_Ref();
+    Omega[iDim] = config->GetRotation_Rate(iDim) / config->GetOmega_Ref();
+    xDot[iDim] = config->GetTranslation_Rate(iDim) / config->GetVelocity_Ref();
   }
 
   su2double L_Ref = config->GetLength_Ref();
@@ -3525,48 +3448,43 @@ void CGeometry::SetRotationalVelocity(const CConfig *config, bool print) {
     cout << ", " << Center[2] << " )\n";
     cout << " Angular velocity about x, y, z axes: ( " << Omega[0] << ", ";
     cout << Omega[1] << ", " << Omega[2] << " ) rad/s" << endl;
-    cout << " Translational velocity in x, y, z direction: ("
-         << xDot[0] << ", " << xDot[1] << ", " << xDot[2] << ")." << endl;
+    cout << " Translational velocity in x, y, z direction: (" << xDot[0] << ", " << xDot[1] << ", " << xDot[2] << ")."
+         << endl;
   }
 
   /*--- Loop over all nodes and set the rotational and translational velocity ---*/
 
   for (iPoint = 0; iPoint < nPoint; iPoint++) {
-
     /*--- Get the coordinates of the current node ---*/
 
     const su2double* Coord = nodes->GetCoord(iPoint);
 
     /*--- Calculate the non-dim. distance from the rotation center ---*/
 
-    for (iDim = 0; iDim < nDim; iDim++)
-      Distance[iDim] = (Coord[iDim]-Center[iDim])/L_Ref;
+    for (iDim = 0; iDim < nDim; iDim++) Distance[iDim] = (Coord[iDim] - Center[iDim]) / L_Ref;
 
     /*--- Calculate the angular velocity as omega X r and add translational velocity ---*/
 
-    GridVel[0] = Omega[1]*(Distance[2]) - Omega[2]*(Distance[1]) + xDot[0];
-    GridVel[1] = Omega[2]*(Distance[0]) - Omega[0]*(Distance[2]) + xDot[1];
-    GridVel[2] = Omega[0]*(Distance[1]) - Omega[1]*(Distance[0]) + xDot[2];
+    GridVel[0] = Omega[1] * (Distance[2]) - Omega[2] * (Distance[1]) + xDot[0];
+    GridVel[1] = Omega[2] * (Distance[0]) - Omega[0] * (Distance[2]) + xDot[1];
+    GridVel[2] = Omega[0] * (Distance[1]) - Omega[1] * (Distance[0]) + xDot[2];
 
     /*--- Store the grid velocity at this node ---*/
 
     nodes->SetGridVel(iPoint, GridVel);
-
   }
-
 }
 
-void CGeometry::SetShroudVelocity(const CConfig *config) {
-
+void CGeometry::SetShroudVelocity(const CConfig* config) {
   unsigned long iPoint, iVertex;
   unsigned short iMarker, iMarkerShroud;
-  su2double RotVel[3] = {0.0,0.0,0.0};
+  su2double RotVel[3] = {0.0, 0.0, 0.0};
 
   /*--- Loop over all vertex in the shroud marker and set the rotational velocity to 0.0 ---*/
-  for (iMarker = 0; iMarker < nMarker; iMarker++){
-    for(iMarkerShroud=0; iMarkerShroud < config->GetnMarker_Shroud(); iMarkerShroud++){
-      if(config->GetMarker_Shroud(iMarkerShroud) == config->GetMarker_All_TagBound(iMarker)){
-        for (iVertex = 0; iVertex  < nVertex[iMarker]; iVertex++) {
+  for (iMarker = 0; iMarker < nMarker; iMarker++) {
+    for (iMarkerShroud = 0; iMarkerShroud < config->GetnMarker_Shroud(); iMarkerShroud++) {
+      if (config->GetMarker_Shroud(iMarkerShroud) == config->GetMarker_All_TagBound(iMarker)) {
+        for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
           iPoint = vertex[iMarker][iVertex]->GetNode();
           nodes->SetGridVel(iPoint, RotVel);
         }
@@ -3575,30 +3493,26 @@ void CGeometry::SetShroudVelocity(const CConfig *config) {
   }
 }
 
-void CGeometry::SetTranslationalVelocity(const CConfig *config, bool print) {
-
-  su2double xDot[3] = {0.0,0.0,0.0};
+void CGeometry::SetTranslationalVelocity(const CConfig* config, bool print) {
+  su2double xDot[3] = {0.0, 0.0, 0.0};
 
   /*--- Get the translational velocity vector from config ---*/
 
   for (unsigned short iDim = 0; iDim < nDim; iDim++)
-    xDot[iDim] = config->GetTranslation_Rate(iDim)/config->GetVelocity_Ref();
+    xDot[iDim] = config->GetTranslation_Rate(iDim) / config->GetVelocity_Ref();
 
   /*--- Print some information to the console ---*/
 
   if (rank == MASTER_NODE && print) {
-    cout << " Non-dim. translational velocity: ("
-         << xDot[0] << ", " << xDot[1] << ", " << xDot[2] << ")." << endl;
+    cout << " Non-dim. translational velocity: (" << xDot[0] << ", " << xDot[1] << ", " << xDot[2] << ")." << endl;
   }
 
   /*--- Loop over all nodes and set the translational velocity ---*/
 
-  for (unsigned long iPoint = 0; iPoint < nPoint; iPoint++)
-    nodes->SetGridVel(iPoint, xDot);
+  for (unsigned long iPoint = 0; iPoint < nPoint; iPoint++) nodes->SetGridVel(iPoint, xDot);
 }
 
-void CGeometry::SetWallVelocity(const CConfig *config, bool print) {
-
+void CGeometry::SetWallVelocity(const CConfig* config, bool print) {
   const su2double L_Ref = config->GetLength_Ref();
   const su2double Omega_Ref = config->GetOmega_Ref();
   const su2double Vel_Ref = config->GetVelocity_Ref();
@@ -3617,7 +3531,7 @@ void CGeometry::SetWallVelocity(const CConfig *config, bool print) {
 
     su2double xDot[MAXNDIM], Center[MAXNDIM], Omega[MAXNDIM];
 
-    for (auto iDim = 0u; iDim < MAXNDIM; iDim++){
+    for (auto iDim = 0u; iDim < MAXNDIM; iDim++) {
       Center[iDim] = config->GetMarkerMotion_Origin(jMarker, iDim);
       Omega[iDim] = config->GetMarkerRotationRate(jMarker, iDim) / Omega_Ref;
       xDot[iDim] = config->GetMarkerTranslationRate(jMarker, iDim) / Vel_Ref;
@@ -3626,10 +3540,13 @@ void CGeometry::SetWallVelocity(const CConfig *config, bool print) {
     if (rank == MASTER_NODE && print) {
       cout << " Storing grid velocity for marker: ";
       cout << Marker_Tag << ".\n";
-      cout << " Translational velocity: (" << xDot[0]*config->GetVelocity_Ref() << ", " << xDot[1]*config->GetVelocity_Ref();
-      cout << ", " << xDot[2]*config->GetVelocity_Ref();
-      if (config->GetSystemMeasurements() == SI) cout << ") m/s.\n";
-      else cout << ") ft/s.\n";
+      cout << " Translational velocity: (" << xDot[0] * config->GetVelocity_Ref() << ", "
+           << xDot[1] * config->GetVelocity_Ref();
+      cout << ", " << xDot[2] * config->GetVelocity_Ref();
+      if (config->GetSystemMeasurements() == SI)
+        cout << ") m/s.\n";
+      else
+        cout << ") ft/s.\n";
       cout << " Angular velocity: (" << Omega[0] << ", " << Omega[1];
       cout << ", " << Omega[2] << ") rad/s about origin: (" << Center[0];
       cout << ", " << Center[1] << ", " << Center[2] << ")." << endl;
@@ -3640,8 +3557,7 @@ void CGeometry::SetWallVelocity(const CConfig *config, bool print) {
 
       /*--- Calculate non-dim. position from rotation center ---*/
       su2double r[MAXNDIM] = {0.0};
-      for (auto iDim = 0u; iDim < nDim; iDim++)
-        r[iDim] = (nodes->GetCoord(iPoint,iDim) - Center[iDim]) / L_Ref;
+      for (auto iDim = 0u; iDim < nDim; iDim++) r[iDim] = (nodes->GetCoord(iPoint, iDim) - Center[iDim]) / L_Ref;
 
       /*--- Cross Product of angular velocity and distance from center to
        get the rotational velocity. Note that we are adding on the velocity
@@ -3650,14 +3566,12 @@ void CGeometry::SetWallVelocity(const CConfig *config, bool print) {
       su2double GridVel[MAXNDIM];
       GeometryToolbox::CrossProduct(Omega, r, GridVel);
 
-      for (auto iDim = 0u; iDim < nDim; iDim++)
-        nodes->SetGridVel(iPoint, iDim, xDot[iDim]+GridVel[iDim]);
+      for (auto iDim = 0u; iDim < nDim; iDim++) nodes->SetGridVel(iPoint, iDim, xDot[iDim] + GridVel[iDim]);
     }
   }
 }
 
-void CGeometry::SetGridVelocity(const CConfig *config) {
-
+void CGeometry::SetGridVelocity(const CConfig* config) {
   /*--- Get timestep and whether to use 1st or 2nd order backward finite differences ---*/
 
   bool FirstOrder = (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST);
@@ -3668,41 +3582,35 @@ void CGeometry::SetGridVelocity(const CConfig *config) {
   /*--- Compute the velocity of each node in the volume mesh ---*/
 
   for (unsigned long iPoint = 0; iPoint < nPoint; iPoint++) {
-
     /*--- Coordinates of the current point at n+1, n, & n-1 time levels ---*/
 
-    const su2double *Coord_nM1 = nodes->GetCoord_n1(iPoint);
-    const su2double *Coord_n   = nodes->GetCoord_n(iPoint);
-    const su2double *Coord_nP1 = nodes->GetCoord(iPoint);
+    const su2double* Coord_nM1 = nodes->GetCoord_n1(iPoint);
+    const su2double* Coord_n = nodes->GetCoord_n(iPoint);
+    const su2double* Coord_nP1 = nodes->GetCoord(iPoint);
 
     /*--- Compute and store mesh velocity with 1st or 2nd-order approximation ---*/
 
     for (unsigned short iDim = 0; iDim < nDim; iDim++) {
-
       su2double GridVel = 0.0;
 
-      if (FirstOrder)
-        GridVel = (Coord_nP1[iDim] - Coord_n[iDim]) / TimeStep;
+      if (FirstOrder) GridVel = (Coord_nP1[iDim] - Coord_n[iDim]) / TimeStep;
 
-      if (SecondOrder)
-        GridVel = (1.5*Coord_nP1[iDim] - 2.0*Coord_n[iDim] + 0.5*Coord_nM1[iDim]) / TimeStep;
+      if (SecondOrder) GridVel = (1.5 * Coord_nP1[iDim] - 2.0 * Coord_n[iDim] + 0.5 * Coord_nM1[iDim]) / TimeStep;
 
       nodes->SetGridVel(iPoint, iDim, GridVel);
     }
   }
-
 }
 
-const CCompressedSparsePatternUL& CGeometry::GetSparsePattern(ConnectivityType type, unsigned long fillLvl)
-{
+const CCompressedSparsePatternUL& CGeometry::GetSparsePattern(ConnectivityType type, unsigned long fillLvl) {
   bool fvm = (type == ConnectivityType::FiniteVolume);
 
   CCompressedSparsePatternUL* pattern = nullptr;
 
   if (fillLvl == 0)
-    pattern = fvm? &finiteVolumeCSRFill0 : &finiteElementCSRFill0;
+    pattern = fvm ? &finiteVolumeCSRFill0 : &finiteElementCSRFill0;
   else
-    pattern = fvm? &finiteVolumeCSRFillN : &finiteElementCSRFillN;
+    pattern = fvm ? &finiteVolumeCSRFillN : &finiteElementCSRFillN;
 
   if (pattern->empty()) {
     *pattern = buildCSRPattern(*this, type, fillLvl);
@@ -3712,8 +3620,7 @@ const CCompressedSparsePatternUL& CGeometry::GetSparsePattern(ConnectivityType t
   return *pattern;
 }
 
-const CEdgeToNonZeroMapUL& CGeometry::GetEdgeToSparsePatternMap(void)
-{
+const CEdgeToNonZeroMapUL& CGeometry::GetEdgeToSparsePatternMap(void) {
   if (edgeToCSRMap.empty()) {
     if (finiteVolumeCSRFill0.empty()) {
       finiteVolumeCSRFill0 = buildCSRPattern(*this, ConnectivityType::FiniteVolume, 0ul);
@@ -3723,39 +3630,36 @@ const CEdgeToNonZeroMapUL& CGeometry::GetEdgeToSparsePatternMap(void)
   return edgeToCSRMap;
 }
 
-const su2vector<unsigned long>& CGeometry::GetTransposeSparsePatternMap(ConnectivityType type)
-{
+const su2vector<unsigned long>& CGeometry::GetTransposeSparsePatternMap(ConnectivityType type) {
   /*--- Yes the const cast is weird but it is still better than repeating code. ---*/
   auto& pattern = const_cast<CCompressedSparsePatternUL&>(GetSparsePattern(type));
   pattern.buildTransposePtr();
   return pattern.transposePtr();
 }
 
-const CCompressedSparsePatternUL& CGeometry::GetEdgeColoring(su2double* efficiency)
-{
+const CCompressedSparsePatternUL& CGeometry::GetEdgeColoring(su2double* efficiency) {
   /*--- Check for dry run mode with dummy geometry. ---*/
-  if (nEdge==0) return edgeColoring;
+  if (nEdge == 0) return edgeColoring;
 
   /*--- Build if required. ---*/
   if (edgeColoring.empty()) {
-
     /*--- When not using threading use the natural coloring to reduce overhead. ---*/
     if (omp_get_max_threads() == 1) {
       SetNaturalEdgeColoring();
-      if (efficiency != nullptr) *efficiency = 1.0; // by definition
+      if (efficiency != nullptr) *efficiency = 1.0;  // by definition
       return edgeColoring;
     }
 
     /*--- Create a temporary sparse pattern from the edges. ---*/
-    su2vector<unsigned long> outerPtr(nEdge+1);
-    su2vector<unsigned long> innerIdx(nEdge*2);
+    su2vector<unsigned long> outerPtr(nEdge + 1);
+    su2vector<unsigned long> innerIdx(nEdge * 2);
 
     for (unsigned long iEdge = 0; iEdge < nEdge; ++iEdge) {
-      outerPtr(iEdge) = 2*iEdge;
-      innerIdx(iEdge*2+0) = edges->GetNode(iEdge,0);
-      innerIdx(iEdge*2+1) = edges->GetNode(iEdge,1);
+      outerPtr(iEdge) = 2 * iEdge;
+      innerIdx(iEdge * 2 + 0) = edges->GetNode(iEdge, 0);
+      innerIdx(iEdge * 2 + 1) = edges->GetNode(iEdge, 1);
     }
-    outerPtr(nEdge) = 2*nEdge;
+    outerPtr(nEdge) = 2 * nEdge;
 
     CCompressedSparsePatternUL pattern(move(outerPtr), move(innerIdx));
 
@@ -3775,32 +3679,30 @@ const CCompressedSparsePatternUL& CGeometry::GetEdgeColoring(su2double* efficien
   return edgeColoring;
 }
 
-void CGeometry::SetNaturalEdgeColoring()
-{
+void CGeometry::SetNaturalEdgeColoring() {
   if (nEdge == 0) return;
   edgeColoring = createNaturalColoring(nEdge);
   /*--- In parallel, set the group size to nEdge to protect client code. ---*/
   if (omp_get_max_threads() > 1) edgeColorGroupSize = nEdge;
 }
 
-const CCompressedSparsePatternUL& CGeometry::GetElementColoring(su2double* efficiency)
-{
+const CCompressedSparsePatternUL& CGeometry::GetElementColoring(su2double* efficiency) {
   /*--- Check for dry run mode with dummy geometry. ---*/
-  if (nElem==0) return elemColoring;
+  if (nElem == 0) return elemColoring;
 
   /*--- Build if required. ---*/
   if (elemColoring.empty()) {
-
     /*--- When not using threading use the natural coloring. ---*/
     if (omp_get_max_threads() == 1) {
       SetNaturalElementColoring();
-      if (efficiency != nullptr) *efficiency = 1.0; // by definition
+      if (efficiency != nullptr) *efficiency = 1.0;  // by definition
       return elemColoring;
     }
 
     /*--- Create a temporary sparse pattern from the elements. ---*/
-    vector<unsigned long> outerPtr(nElem+1);
-    vector<unsigned long> innerIdx; innerIdx.reserve(nElem);
+    vector<unsigned long> outerPtr(nElem + 1);
+    vector<unsigned long> innerIdx;
+    innerIdx.reserve(nElem);
 
     for (unsigned long iElem = 0; iElem < nElem; ++iElem) {
       outerPtr[iElem] = innerIdx.size();
@@ -3827,8 +3729,7 @@ const CCompressedSparsePatternUL& CGeometry::GetElementColoring(su2double* effic
   return elemColoring;
 }
 
-void CGeometry::SetNaturalElementColoring()
-{
+void CGeometry::SetNaturalElementColoring() {
   if (nElem == 0) return;
   elemColoring = createNaturalColoring(nElem);
   /*--- In parallel, set the group size to nElem to protect client code. ---*/
@@ -3836,28 +3737,26 @@ void CGeometry::SetNaturalElementColoring()
 }
 
 void CGeometry::ColorMGLevels(unsigned short nMGLevels, const CGeometry* const* geometry) {
-
   using tColor = uint8_t;
   constexpr auto nColor = numeric_limits<tColor>::max();
 
-  if (nMGLevels) CoarseGridColor_.resize(nPoint,nMGLevels) = 0;
+  if (nMGLevels) CoarseGridColor_.resize(nPoint, nMGLevels) = 0;
 
   for (auto iMesh = nMGLevels; iMesh >= 1; --iMesh) {
     /*--- Color the coarse points. ---*/
     vector<tColor> color;
     const auto& adjacency = geometry[iMesh]->nodes->GetPoints();
-    if (colorSparsePattern<tColor, nColor>(adjacency, 1, false, &color).empty())
-      continue;
+    if (colorSparsePattern<tColor, nColor>(adjacency, 1, false, &color).empty()) continue;
 
     /*--- Propagate colors to fine mesh. ---*/
     for (auto step = 0u; step < iMesh; ++step) {
-      auto coarseMesh = geometry[iMesh-1-step];
+      auto coarseMesh = geometry[iMesh - 1 - step];
       if (step)
         for (auto iPoint = 0ul; iPoint < coarseMesh->GetnPoint(); ++iPoint)
-          CoarseGridColor_(iPoint,step) = CoarseGridColor_(coarseMesh->nodes->GetParent_CV(iPoint), step-1);
+          CoarseGridColor_(iPoint, step) = CoarseGridColor_(coarseMesh->nodes->GetParent_CV(iPoint), step - 1);
       else
         for (auto iPoint = 0ul; iPoint < coarseMesh->GetnPoint(); ++iPoint)
-          CoarseGridColor_(iPoint,step) = color[coarseMesh->nodes->GetParent_CV(iPoint)];
+          CoarseGridColor_(iPoint, step) = color[coarseMesh->nodes->GetParent_CV(iPoint)];
     }
   }
 }
@@ -3993,8 +3892,8 @@ const CGeometry::CLineletInfo& CGeometry::GetLineletInfo(const CConfig* config)
     }
   }
 
-  const auto coloring = colorSparsePattern<uint8_t, std::numeric_limits<uint8_t>::max()>(
-      CCompressedSparsePatternUL(adjacency), 1, true);
+  const auto coloring =
+      colorSparsePattern<uint8_t, std::numeric_limits<uint8_t>::max()>(CCompressedSparsePatternUL(adjacency), 1, true);
   const auto nColors = coloring.getOuterSize();
 
   /*--- Sort linelets by color. ---*/
@@ -4034,43 +3933,38 @@ const CGeometry::CLineletInfo& CGeometry::GetLineletInfo(const CConfig* config)
   return li;
 }
 
-void CGeometry::ComputeWallDistance(const CConfig* const* config_container, CGeometry ****geometry_container){
-
+void CGeometry::ComputeWallDistance(const CConfig* const* config_container, CGeometry**** geometry_container) {
   int nZone = config_container[ZONE_0]->GetnZone();
   bool allEmpty = true;
   vector<bool> wallDistanceNeeded(nZone, false);
 
-  for (int iInst = 0; iInst < config_container[ZONE_0]->GetnTimeInstances(); iInst++){
-    for (int iZone = 0; iZone < nZone; iZone++){
-
+  for (int iInst = 0; iInst < config_container[ZONE_0]->GetnTimeInstances(); iInst++) {
+    for (int iZone = 0; iZone < nZone; iZone++) {
       /*--- Check if a zone needs the wall distance and store a boolean ---*/
 
       MAIN_SOLVER kindSolver = config_container[iZone]->GetKind_Solver();
-      if (kindSolver == MAIN_SOLVER::RANS ||
-          kindSolver == MAIN_SOLVER::INC_RANS ||
-          kindSolver == MAIN_SOLVER::DISC_ADJ_RANS ||
-          kindSolver == MAIN_SOLVER::DISC_ADJ_INC_RANS ||
-          kindSolver == MAIN_SOLVER::FEM_LES ||
-          kindSolver == MAIN_SOLVER::FEM_RANS){
+      if (kindSolver == MAIN_SOLVER::RANS || kindSolver == MAIN_SOLVER::INC_RANS ||
+          kindSolver == MAIN_SOLVER::DISC_ADJ_RANS || kindSolver == MAIN_SOLVER::DISC_ADJ_INC_RANS ||
+          kindSolver == MAIN_SOLVER::FEM_LES || kindSolver == MAIN_SOLVER::FEM_RANS) {
         wallDistanceNeeded[iZone] = true;
       }
 
       /*--- Set the wall distances in all zones to the numerical limit.
-     * This is necessary, because before a computed distance is set, it will be checked
-     * whether the new distance is smaller than the currently stored one. ---*/
-      CGeometry *geometry = geometry_container[iZone][iInst][MESH_0];
-      if (wallDistanceNeeded[iZone])
-        geometry->SetWallDistance(numeric_limits<su2double>::max());
+       * This is necessary, because before a computed distance is set, it will be checked
+       * whether the new distance is smaller than the currently stored one. ---*/
+      CGeometry* geometry = geometry_container[iZone][iInst][MESH_0];
+      if (wallDistanceNeeded[iZone]) geometry->SetWallDistance(numeric_limits<su2double>::max());
     }
 
     /*--- Loop over all zones and compute the ADT based on the viscous walls in that zone ---*/
-    for (int iZone = 0; iZone < nZone; iZone++){
-      unique_ptr<CADTElemClass> WallADT = geometry_container[iZone][iInst][MESH_0]->ComputeViscousWallADT(config_container[iZone]);
-      if (WallADT && !WallADT->IsEmpty()){
+    for (int iZone = 0; iZone < nZone; iZone++) {
+      unique_ptr<CADTElemClass> WallADT =
+          geometry_container[iZone][iInst][MESH_0]->ComputeViscousWallADT(config_container[iZone]);
+      if (WallADT && !WallADT->IsEmpty()) {
         allEmpty = false;
         /*--- Inner loop over all zones to update the wall distances.
-       * It might happen that there is a closer viscous wall in zone iZone for points in zone jZone. ---*/
-        for (int jZone = 0; jZone < nZone; jZone++){
+         * It might happen that there is a closer viscous wall in zone iZone for points in zone jZone. ---*/
+        for (int jZone = 0; jZone < nZone; jZone++) {
           if (wallDistanceNeeded[jZone])
             geometry_container[jZone][iInst][MESH_0]->SetWallDistance(WallADT.get(), config_container[jZone], iZone);
         }
@@ -4078,31 +3972,30 @@ void CGeometry::ComputeWallDistance(const CConfig* const* config_container, CGeo
     }
 
     /*--- If there are no viscous walls in the entire domain, set distances to zero ---*/
-    if (allEmpty){
-      for (int iZone = 0; iZone < nZone; iZone++){
-        CGeometry *geometry = geometry_container[iZone][iInst][MESH_0];
+    if (allEmpty) {
+      for (int iZone = 0; iZone < nZone; iZone++) {
+        CGeometry* geometry = geometry_container[iZone][iInst][MESH_0];
         geometry->SetWallDistance(0.0);
       }
     }
     /*--- Otherwise, set wall roughnesses. ---*/
-    if(!allEmpty){
+    if (!allEmpty) {
       /*--- Store all wall roughnesses in a common data structure. ---*/
       // [iZone][iMarker] -> roughness, for this rank
-      auto roughness_f =
-        make_pair( nZone, [config_container,geometry_container,iInst](unsigned long iZone){
-          const CConfig* config = config_container[iZone];
-          const auto nMarker = geometry_container[iZone][iInst][MESH_0]->GetnMarker();
-
-          return make_pair( nMarker, [config](unsigned long iMarker){
-            return config->GetWallRoughnessProperties(config->GetMarker_All_TagBound(iMarker)).second;
-          });
+      auto roughness_f = make_pair(nZone, [config_container, geometry_container, iInst](unsigned long iZone) {
+        const CConfig* config = config_container[iZone];
+        const auto nMarker = geometry_container[iZone][iInst][MESH_0]->GetnMarker();
+
+        return make_pair(nMarker, [config](unsigned long iMarker) {
+          return config->GetWallRoughnessProperties(config->GetMarker_All_TagBound(iMarker)).second;
         });
+      });
       NdFlattener<2> roughness_local(roughness_f);
       // [rank][iZone][iMarker] -> roughness
       NdFlattener<3> roughness_global(Nd_MPI_Environment(), roughness_local);
       // use it to update roughnesses
-      for(int jZone=0; jZone<nZone; jZone++){
-        if (wallDistanceNeeded[jZone] && config_container[jZone]->GetnRoughWall()>0){
+      for (int jZone = 0; jZone < nZone; jZone++) {
+        if (wallDistanceNeeded[jZone] && config_container[jZone]->GetnRoughWall() > 0) {
           geometry_container[jZone][iInst][MESH_0]->nodes->SetWallRoughness(roughness_global);
         }
       }
diff --git a/Common/src/geometry/CMultiGridGeometry.cpp b/Common/src/geometry/CMultiGridGeometry.cpp
index f28716fb795..e131d569df0 100644
--- a/Common/src/geometry/CMultiGridGeometry.cpp
+++ b/Common/src/geometry/CMultiGridGeometry.cpp
@@ -30,9 +30,8 @@
 #include "../../include/toolboxes/printing_toolbox.hpp"
 #include "../../../Common/include/toolboxes/geometry_toolbox.hpp"
 
-CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, unsigned short iMesh) : CGeometry() {
-
-  nDim = fine_grid->GetnDim(); // Write the number of dimensions of the coarse grid.
+CMultiGridGeometry::CMultiGridGeometry(CGeometry* fine_grid, CConfig* config, unsigned short iMesh) : CGeometry() {
+  nDim = fine_grid->GetnDim();  // Write the number of dimensions of the coarse grid.
 
   /*--- Create a queue system to do the agglomeration
    1st) More than two markers ---> Vertices (never agglomerate)
@@ -45,8 +44,7 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
    For other levels this information is propagated down during their construction. ---*/
 
   if (iMesh == MESH_1) {
-
-    for (auto iPoint = 0ul; iPoint < fine_grid->GetnPoint(); iPoint ++)
+    for (auto iPoint = 0ul; iPoint < fine_grid->GetnPoint(); iPoint++)
       fine_grid->nodes->SetAgglomerate_Indirect(iPoint, false);
 
     for (auto iElem = 0ul; iElem < fine_grid->GetnElem(); iElem++) {
@@ -58,7 +56,6 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
         }
       }
     }
-
   }
 
   /*--- Create the coarse grid structure using as baseline the fine grid ---*/
@@ -73,7 +70,6 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
   /*--- The first step is the boundary agglomeration. ---*/
 
   for (auto iMarker = 0u; iMarker < fine_grid->GetnMarker(); iMarker++) {
-
     for (auto iVertex = 0ul; iVertex < fine_grid->GetnVertex(iMarker); iVertex++) {
       const auto iPoint = fine_grid->vertex[iMarker][iVertex]->GetNode();
 
@@ -81,10 +77,8 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
        belongs to this physical domain, and it meets the geometrical
        criteria, the agglomeration is studied. ---*/
 
-      if ((fine_grid->nodes->GetAgglomerate(iPoint) == false) &&
-          (fine_grid->nodes->GetDomain(iPoint)) &&
+      if ((fine_grid->nodes->GetAgglomerate(iPoint) == false) && (fine_grid->nodes->GetDomain(iPoint)) &&
           (GeometricalCheck(iPoint, fine_grid, config))) {
-
         unsigned short nChildren = 1;
 
         /*--- We set an index for the parent control volume, this
@@ -103,7 +97,7 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
         /*--- For a particular point in the fine grid we save all the markers
          that are in that point ---*/
 
-        for (auto jMarker = 0u; jMarker < fine_grid->GetnMarker() && counter < 3; jMarker ++) {
+        for (auto jMarker = 0u; jMarker < fine_grid->GetnMarker() && counter < 3; jMarker++) {
           if (fine_grid->nodes->GetVertex(iPoint, jMarker) != -1) {
             copy_marker[counter] = jMarker;
             counter++;
@@ -123,8 +117,7 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
           if ((config->GetMarker_All_KindBC(copy_marker[0]) == SEND_RECEIVE) ||
               (config->GetMarker_All_KindBC(copy_marker[1]) == SEND_RECEIVE)) {
             agglomerate_seed = true;
-          }
-          else {
+          } else {
             agglomerate_seed = false;
           }
         }
@@ -136,15 +129,12 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
         /*--- If the seed can be agglomerated, we try to agglomerate more points ---*/
 
         if (agglomerate_seed) {
-
           /*--- Now we do a sweep over all the nodes that surround the seed point ---*/
 
           for (auto CVPoint : fine_grid->nodes->GetPoints(iPoint)) {
-
             /*--- The new point can be agglomerated ---*/
 
             if (SetBoundAgglomeration(CVPoint, marker_seed, fine_grid, config)) {
-
               /*--- We set the value of the parent ---*/
 
               fine_grid->nodes->SetParent_CV(CVPoint, Index_CoarseCV);
@@ -154,7 +144,6 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
               nodes->SetChildren_CV(Index_CoarseCV, nChildren, CVPoint);
               nChildren++;
             }
-
           }
 
           Suitable_Indirect_Neighbors.clear();
@@ -165,11 +154,9 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
           /*--- Now we do a sweep over all the indirect nodes that can be added ---*/
 
           for (auto CVPoint : Suitable_Indirect_Neighbors) {
-
             /*--- The new point can be agglomerated ---*/
 
             if (SetBoundAgglomeration(CVPoint, marker_seed, fine_grid, config)) {
-
               /*--- We set the value of the parent ---*/
 
               fine_grid->nodes->SetParent_CV(CVPoint, Index_CoarseCV);
@@ -186,7 +173,6 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
               nChildren++;
             }
           }
-
         }
 
         /*--- Update the number of children of the coarse control volume. ---*/
@@ -204,8 +190,7 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
     for (auto iVertex = 0ul; iVertex < fine_grid->GetnVertex(iMarker); iVertex++) {
       const auto iPoint = fine_grid->vertex[iMarker][iVertex]->GetNode();
 
-      if ((fine_grid->nodes->GetAgglomerate(iPoint) == false) &&
-          (fine_grid->nodes->GetDomain(iPoint))) {
+      if ((fine_grid->nodes->GetAgglomerate(iPoint) == false) && (fine_grid->nodes->GetDomain(iPoint))) {
         fine_grid->nodes->SetParent_CV(iPoint, Index_CoarseCV);
         nodes->SetChildren_CV(Index_CoarseCV, 0, iPoint);
         nodes->SetnChildren_CV(Index_CoarseCV, 1);
@@ -216,14 +201,11 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
 
   /*--- Update the queue with the results from the boundary agglomeration ---*/
 
-  for (auto iPoint = 0ul; iPoint < fine_grid->GetnPoint(); iPoint ++) {
-
+  for (auto iPoint = 0ul; iPoint < fine_grid->GetnPoint(); iPoint++) {
     if (fine_grid->nodes->GetAgglomerate(iPoint)) {
-
       MGQueue_InnerCV.RemoveCV(iPoint);
 
-    }
-    else {
+    } else {
       /*--- Count the number of agglomerated neighbors, and modify the queue,
        Points with more agglomerated neighbors are processed first. ---*/
 
@@ -239,17 +221,14 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
 
   auto iteration = 0ul;
   while (!MGQueue_InnerCV.EmptyQueue() && (iteration < fine_grid->GetnPoint())) {
-
     const auto iPoint = MGQueue_InnerCV.NextCV();
     iteration++;
 
     /*--- If the element has not being previously agglomerated, belongs to the physical domain,
      and satisfies several geometrical criteria then the seed CV is accepted for agglomeration. ---*/
 
-    if ((fine_grid->nodes->GetAgglomerate(iPoint) == false) &&
-        (fine_grid->nodes->GetDomain(iPoint)) &&
+    if ((fine_grid->nodes->GetAgglomerate(iPoint) == false) && (fine_grid->nodes->GetDomain(iPoint)) &&
         (GeometricalCheck(iPoint, fine_grid, config))) {
-
       unsigned short nChildren = 1;
 
       /*--- We set an index for the parent control volume ---*/
@@ -268,13 +247,10 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
       /*--- Now we do a sweep over all the nodes that surround the seed point ---*/
 
       for (auto CVPoint : fine_grid->nodes->GetPoints(iPoint)) {
-
         /*--- Determine if the CVPoint can be agglomerated ---*/
 
-        if ((fine_grid->nodes->GetAgglomerate(CVPoint) == false) &&
-            (fine_grid->nodes->GetDomain(CVPoint)) &&
+        if ((fine_grid->nodes->GetAgglomerate(CVPoint) == false) && (fine_grid->nodes->GetDomain(CVPoint)) &&
             (GeometricalCheck(CVPoint, fine_grid, config))) {
-
           /*--- We set the value of the parent ---*/
 
           fine_grid->nodes->SetParent_CV(CVPoint, Index_CoarseCV);
@@ -288,9 +264,7 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
            increase the priority of its neighbors) ---*/
 
           MGQueue_InnerCV.Update(CVPoint, fine_grid);
-
         }
-
       }
 
       /*--- Identify the indirect neighbors ---*/
@@ -302,20 +276,16 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
       /*--- Now we do a sweep over all the indirect nodes that can be added ---*/
 
       for (auto CVPoint : Suitable_Indirect_Neighbors) {
-
         /*--- The new point can be agglomerated ---*/
 
-        if ((fine_grid->nodes->GetAgglomerate(CVPoint) == false) &&
-            (fine_grid->nodes->GetDomain(CVPoint))) {
-
+        if ((fine_grid->nodes->GetAgglomerate(CVPoint) == false) && (fine_grid->nodes->GetDomain(CVPoint))) {
           /*--- We set the value of the parent ---*/
 
           fine_grid->nodes->SetParent_CV(CVPoint, Index_CoarseCV);
 
           /*--- We set the indirect agglomeration information ---*/
 
-          if (fine_grid->nodes->GetAgglomerate_Indirect(CVPoint))
-            nodes->SetAgglomerate_Indirect(Index_CoarseCV, true);
+          if (fine_grid->nodes->GetAgglomerate_Indirect(CVPoint)) nodes->SetAgglomerate_Indirect(Index_CoarseCV, true);
 
           /*--- We set the value of the child ---*/
 
@@ -326,7 +296,6 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
            increase the priority of the neighbors) ---*/
 
           MGQueue_InnerCV.Update(CVPoint, fine_grid);
-
         }
       }
 
@@ -334,26 +303,20 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
 
       nodes->SetnChildren_CV(Index_CoarseCV, nChildren);
       Index_CoarseCV++;
-    }
-    else {
-
+    } else {
       /*--- The seed point can not be agglomerated because of size, domain, streching, etc.
        move the point to the lowest priority ---*/
 
       MGQueue_InnerCV.MoveCV(iPoint, -1);
     }
-
   }
 
   /*--- Convert any point that was not agglomerated into a coarse point. ---*/
 
   for (auto iPoint = 0ul; iPoint < fine_grid->GetnPoint(); iPoint++) {
-    if ((fine_grid->nodes->GetAgglomerate(iPoint) == false) &&
-        (fine_grid->nodes->GetDomain(iPoint))) {
-
+    if ((fine_grid->nodes->GetAgglomerate(iPoint) == false) && (fine_grid->nodes->GetDomain(iPoint))) {
       fine_grid->nodes->SetParent_CV(iPoint, Index_CoarseCV);
-      if (fine_grid->nodes->GetAgglomerate_Indirect(iPoint))
-        nodes->SetAgglomerate_Indirect(Index_CoarseCV, true);
+      if (fine_grid->nodes->GetAgglomerate_Indirect(iPoint)) nodes->SetAgglomerate_Indirect(Index_CoarseCV, true);
       nodes->SetChildren_CV(Index_CoarseCV, 0, iPoint);
       nodes->SetnChildren_CV(Index_CoarseCV, 1);
       Index_CoarseCV++;
@@ -369,9 +332,7 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
   SetPoint_Connectivity(fine_grid);
 
   for (auto iCoarsePoint = 0ul; iCoarsePoint < nPointDomain; iCoarsePoint++) {
-
     if (nodes->GetnPoint(iCoarsePoint) == 1) {
-
       /*--- Find the neighbor of the isolated point. This neighbor is the right control volume ---*/
 
       const auto iCoarsePoint_Complete = nodes->GetPoint(iCoarsePoint, 0);
@@ -395,7 +356,6 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
       nodes->SetnChildren_CV(iCoarsePoint_Complete, nChildren);
       nodes->SetnChildren_CV(iCoarsePoint, 0);
     }
-
   }
 
   /*--- Reset the neighbor information. ---*/
@@ -409,10 +369,7 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
    they are domain points. ---*/
 
   for (auto iMarker = 0u; iMarker < config->GetnMarker_All(); iMarker++) {
-
-    if ((config->GetMarker_All_KindBC(iMarker) == SEND_RECEIVE) &&
-        (config->GetMarker_All_SendRecv(iMarker) > 0)) {
-
+    if ((config->GetMarker_All_KindBC(iMarker) == SEND_RECEIVE) && (config->GetMarker_All_SendRecv(iMarker) > 0)) {
       const auto MarkerS = iMarker;
       const auto MarkerR = iMarker + 1;
 
@@ -444,8 +401,8 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
                         Buffer_Receive_Children.data(), nVertexR, MPI_UNSIGNED_LONG, receive_from, 0,
                         SU2_MPI::GetComm(), MPI_STATUS_IGNORE);
       SU2_MPI::Sendrecv(Buffer_Send_Parent.data(), nVertexS, MPI_UNSIGNED_LONG, send_to, 1,
-                        Buffer_Receive_Parent.data(), nVertexR, MPI_UNSIGNED_LONG, receive_from, 1,
-                        SU2_MPI::GetComm(), MPI_STATUS_IGNORE);
+                        Buffer_Receive_Parent.data(), nVertexR, MPI_UNSIGNED_LONG, receive_from, 1, SU2_MPI::GetComm(),
+                        MPI_STATUS_IGNORE);
 
       /*--- Create a list of the parent nodes without duplicates. ---*/
 
@@ -462,7 +419,6 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
       vector<unsigned long> Children_Local(nVertexR);
 
       for (auto iVertex = 0ul; iVertex < nVertexR; iVertex++) {
-
         /*--- We use the same sorting as in the donor domain, i.e. the local parents
          are numbered according to their order in the remote rank. ---*/
 
@@ -493,11 +449,9 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
         nodes->SetnChildren_CV(iPoint_Coarse, nChildren_MPI[iPoint_Coarse]);
         nodes->SetDomain(iPoint_Coarse, false);
       }
-
     }
-
   }
-#endif // HAVE_MPI
+#endif  // HAVE_MPI
 
   /*--- Update the number of points after the MPI agglomeration ---*/
 
@@ -516,17 +470,15 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
   if (iMesh != MESH_0) {
     const su2double factor = 1.5;
     const su2double Coeff = pow(su2double(Global_nPointFine) / Global_nPointCoarse, 1.0 / nDim);
-    const su2double CFL = factor * config->GetCFL(iMesh-1) / Coeff;
+    const su2double CFL = factor * config->GetCFL(iMesh - 1) / Coeff;
     config->SetCFL(iMesh, CFL);
   }
 
   const su2double ratio = su2double(Global_nPointFine) / su2double(Global_nPointCoarse);
 
-  if (((nDim == 2) && (ratio < 2.5)) ||
-      ((nDim == 3) && (ratio < 2.5))) {
-    config->SetMGLevels(iMesh-1);
-  }
-  else if (rank == MASTER_NODE) {
+  if (((nDim == 2) && (ratio < 2.5)) || ((nDim == 3) && (ratio < 2.5))) {
+    config->SetMGLevels(iMesh - 1);
+  } else if (rank == MASTER_NODE) {
     PrintingToolbox::CTablePrinter MGTable(&std::cout);
     MGTable.AddColumn("MG Level", 10);
     MGTable.AddColumn("CVs", 10);
@@ -534,37 +486,33 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry *fine_grid, CConfig *config, un
     MGTable.AddColumn("CFL", 10);
     MGTable.SetAlign(PrintingToolbox::CTablePrinter::RIGHT);
 
-    if (iMesh == MESH_1){
+    if (iMesh == MESH_1) {
       MGTable.PrintHeader();
-      MGTable << iMesh - 1 << Global_nPointFine << "1/1.00" << config->GetCFL(iMesh -1);
+      MGTable << iMesh - 1 << Global_nPointFine << "1/1.00" << config->GetCFL(iMesh - 1);
     }
     stringstream ss;
     ss << "1/" << std::setprecision(3) << ratio;
     MGTable << iMesh << Global_nPointCoarse << ss.str() << config->GetCFL(iMesh);
-    if (iMesh == config->GetnMGLevels()){
+    if (iMesh == config->GetnMGLevels()) {
       MGTable.PrintFooter();
     }
   }
 
   edgeColorGroupSize = config->GetEdgeColoringGroupSize();
-
 }
 
-bool CMultiGridGeometry::SetBoundAgglomeration(unsigned long CVPoint, short marker_seed,
-                                               const CGeometry *fine_grid, const CConfig *config) const {
+bool CMultiGridGeometry::SetBoundAgglomeration(unsigned long CVPoint, short marker_seed, const CGeometry* fine_grid,
+                                               const CConfig* config) const {
   bool agglomerate_CV = false;
 
   /*--- Basic condition, the point has not being previously agglomerated, it belongs to the domain,
    and has passed some basic geometrical checks. ---*/
 
-  if ((fine_grid->nodes->GetAgglomerate(CVPoint) == false) &&
-      (fine_grid->nodes->GetDomain(CVPoint)) &&
+  if ((fine_grid->nodes->GetAgglomerate(CVPoint) == false) && (fine_grid->nodes->GetDomain(CVPoint)) &&
       (GeometricalCheck(CVPoint, fine_grid, config))) {
-
     /*--- If the point belongs to a boundary, its type must be compatible with the seed marker. ---*/
 
     if (fine_grid->nodes->GetBoundary(CVPoint)) {
-
       /*--- Identify the markers of the vertex that we want to agglomerate ---*/
 
       int counter = 0;
@@ -582,58 +530,51 @@ bool CMultiGridGeometry::SetBoundAgglomeration(unsigned long CVPoint, short mark
       /*--- Only one marker in the vertex that is going to be aglomerated ---*/
 
       if (counter == 1) {
-
         /*--- We agglomerate if there is only a marker and is the same marker as the seed marker ---*/
 
-        if (copy_marker[0] == marker_seed)
-          agglomerate_CV = true;
+        if (copy_marker[0] == marker_seed) agglomerate_CV = true;
 
         /*--- If there is only one marker, but the marker is the SEND_RECEIVE ---*/
 
-        if (config->GetMarker_All_KindBC(copy_marker[0]) == SEND_RECEIVE)
-          agglomerate_CV = true;
-
+        if (config->GetMarker_All_KindBC(copy_marker[0]) == SEND_RECEIVE) agglomerate_CV = true;
       }
 
       /*--- If there are two markers in the vertex that is going to be aglomerated ---*/
 
       if (counter == 2) {
-
         /*--- First we verify that the seed is a physical boundary ---*/
 
         if (config->GetMarker_All_KindBC(marker_seed) != SEND_RECEIVE) {
-
           /*--- Then we check that one of the marker is equal to the seed marker, and the other is send/receive ---*/
 
           if (((copy_marker[0] == marker_seed) && (config->GetMarker_All_KindBC(copy_marker[1]) == SEND_RECEIVE)) ||
               ((config->GetMarker_All_KindBC(copy_marker[0]) == SEND_RECEIVE) && (copy_marker[1] == marker_seed)))
             agglomerate_CV = true;
         }
-
       }
 
     }
 
     /*--- If the element belongs to the domain, it is allways aglomerated. ---*/
 
-    else { agglomerate_CV = true; }
-
+    else {
+      agglomerate_CV = true;
+    }
   }
 
   return agglomerate_CV;
 }
 
-
-bool CMultiGridGeometry::GeometricalCheck(unsigned long iPoint, const CGeometry *fine_grid, const CConfig *config) const {
-
+bool CMultiGridGeometry::GeometricalCheck(unsigned long iPoint, const CGeometry* fine_grid,
+                                          const CConfig* config) const {
   su2double max_dimension = 1.2;
 
   /*--- Evaluate the total size of the element ---*/
 
   bool Volume = true;
-  su2double ratio = pow(fine_grid->nodes->GetVolume(iPoint), 1.0/su2double(nDim))*max_dimension;
-  su2double limit = pow(config->GetDomainVolume(), 1.0/su2double(nDim));
-  if ( ratio > limit ) Volume = false;
+  su2double ratio = pow(fine_grid->nodes->GetVolume(iPoint), 1.0 / su2double(nDim)) * max_dimension;
+  su2double limit = pow(config->GetDomainVolume(), 1.0 / su2double(nDim));
+  if (ratio > limit) Volume = false;
 
   /*--- Evaluate the stretching of the element ---*/
 
@@ -656,27 +597,22 @@ bool CMultiGridGeometry::GeometricalCheck(unsigned long iPoint, const CGeometry
    if ( max_dist/min_dist > 100.0 ) Stretching = false;*/
 
   return (Stretching && Volume);
-
 }
 
 void CMultiGridGeometry::SetSuitableNeighbors(vector<unsigned long>& Suitable_Indirect_Neighbors, unsigned long iPoint,
-                                              unsigned long Index_CoarseCV, const CGeometry *fine_grid) const {
-
+                                              unsigned long Index_CoarseCV, const CGeometry* fine_grid) const {
   /*--- Create a list with the first neighbors, including the seed. ---*/
 
   vector<unsigned long> First_Neighbor_Points;
   First_Neighbor_Points.push_back(iPoint);
-  for (auto jPoint : fine_grid->nodes->GetPoints(iPoint))
-    First_Neighbor_Points.push_back(jPoint);
+  for (auto jPoint : fine_grid->nodes->GetPoints(iPoint)) First_Neighbor_Points.push_back(jPoint);
 
   /*--- Create a list with the second neighbors, without first, and seed neighbors. ---*/
 
   vector<unsigned long> Second_Neighbor_Points, Second_Origin_Points, Suitable_Second_Neighbors;
 
   for (auto jPoint : fine_grid->nodes->GetPoints(iPoint)) {
-
     for (auto kPoint : fine_grid->nodes->GetPoints(jPoint)) {
-
       /*--- Check that the second neighbor does not belong to the first neighbors or the seed. ---*/
 
       auto end = First_Neighbor_Points.end();
@@ -692,21 +628,17 @@ void CMultiGridGeometry::SetSuitableNeighbors(vector<unsigned long>& Suitable_In
    neighbors, and for hexs it produces a 27-point stencil. ---*/
 
   for (auto iNeighbor = 0ul; iNeighbor < Second_Neighbor_Points.size(); iNeighbor++) {
-
-    for (auto jNeighbor = iNeighbor+1; jNeighbor < Second_Neighbor_Points.size(); jNeighbor++) {
-
+    for (auto jNeighbor = iNeighbor + 1; jNeighbor < Second_Neighbor_Points.size(); jNeighbor++) {
       /*--- Repeated second neighbor with different origin ---*/
 
       if ((Second_Neighbor_Points[iNeighbor] == Second_Neighbor_Points[jNeighbor]) &&
           (Second_Origin_Points[iNeighbor] != Second_Origin_Points[jNeighbor])) {
-
         Suitable_Indirect_Neighbors.push_back(Second_Neighbor_Points[iNeighbor]);
 
         /*--- Create a list of suitable second neighbors, that we will use
          to compute the third neighbors. --*/
 
         Suitable_Second_Neighbors.push_back(Second_Neighbor_Points[iNeighbor]);
-
       }
     }
   }
@@ -725,7 +657,6 @@ void CMultiGridGeometry::SetSuitableNeighbors(vector<unsigned long>& Suitable_In
 
   for (auto kPoint : Suitable_Second_Neighbors) {
     for (auto lPoint : fine_grid->nodes->GetPoints(kPoint)) {
-
       /*--- Check that the third neighbor does not belong to the first neighbors or the seed ---*/
 
       auto end1 = First_Neighbor_Points.end();
@@ -743,14 +674,12 @@ void CMultiGridGeometry::SetSuitableNeighbors(vector<unsigned long>& Suitable_In
 
   /*--- Identify those third neighbors that are repeated (candidate to be added). ---*/
 
-  for (auto iNeighbor = 0ul; iNeighbor < Third_Neighbor_Points.size(); iNeighbor ++) {
-    for (auto jNeighbor = iNeighbor+1; jNeighbor < Third_Neighbor_Points.size(); jNeighbor ++) {
-
+  for (auto iNeighbor = 0ul; iNeighbor < Third_Neighbor_Points.size(); iNeighbor++) {
+    for (auto jNeighbor = iNeighbor + 1; jNeighbor < Third_Neighbor_Points.size(); jNeighbor++) {
       /*--- Repeated third neighbor with different origin ---*/
 
       if ((Third_Neighbor_Points[iNeighbor] == Third_Neighbor_Points[jNeighbor]) &&
           (Third_Origin_Points[iNeighbor] != Third_Origin_Points[jNeighbor])) {
-
         Suitable_Indirect_Neighbors.push_back(Third_Neighbor_Points[iNeighbor]);
       }
     }
@@ -761,11 +690,9 @@ void CMultiGridGeometry::SetSuitableNeighbors(vector<unsigned long>& Suitable_In
   sort(Suitable_Indirect_Neighbors.begin(), Suitable_Indirect_Neighbors.end());
   auto it2 = unique(Suitable_Indirect_Neighbors.begin(), Suitable_Indirect_Neighbors.end());
   Suitable_Indirect_Neighbors.resize(it2 - Suitable_Indirect_Neighbors.begin());
-
 }
 
-void CMultiGridGeometry::SetPoint_Connectivity(const CGeometry *fine_grid) {
-
+void CMultiGridGeometry::SetPoint_Connectivity(const CGeometry* fine_grid) {
   /*--- Temporary, CPoint (nodes) then compresses this structure. ---*/
   vector<vector<unsigned long> > points(nPoint);
 
@@ -780,8 +707,7 @@ void CMultiGridGeometry::SetPoint_Connectivity(const CGeometry *fine_grid) {
         if (iParent != iCoarsePoint) {
           /*--- Avoid duplicates. ---*/
           auto End = points[iCoarsePoint].end();
-          if (find(points[iCoarsePoint].begin(), End, iParent) == End)
-            points[iCoarsePoint].push_back(iParent);
+          if (find(points[iCoarsePoint].begin(), End, iParent) == End) points[iCoarsePoint].push_back(iParent);
         }
       }
     }
@@ -792,11 +718,10 @@ void CMultiGridGeometry::SetPoint_Connectivity(const CGeometry *fine_grid) {
   }
 
   nodes->SetPoints(points);
-
 }
 
-void CMultiGridGeometry::SetVertex(const CGeometry *fine_grid, const CConfig *config) {
-  unsigned long  iVertex, iFinePoint, iCoarsePoint;
+void CMultiGridGeometry::SetVertex(const CGeometry* fine_grid, const CConfig* config) {
+  unsigned long iVertex, iFinePoint, iCoarsePoint;
   unsigned short iMarker, iMarker_Tag, iChildren;
 
   nMarker = fine_grid->GetnMarker();
@@ -804,8 +729,8 @@ void CMultiGridGeometry::SetVertex(const CGeometry *fine_grid, const CConfig *co
 
   /*--- If any children node belong to the boundary then the entire control
    volume will belong to the boundary ---*/
-  for (iCoarsePoint = 0; iCoarsePoint < nPoint; iCoarsePoint ++)
-    for (iChildren = 0; iChildren < nodes->GetnChildren_CV(iCoarsePoint); iChildren ++) {
+  for (iCoarsePoint = 0; iCoarsePoint < nPoint; iCoarsePoint++)
+    for (iChildren = 0; iChildren < nodes->GetnChildren_CV(iCoarsePoint); iChildren++) {
       iFinePoint = nodes->GetChildren_CV(iCoarsePoint, iChildren);
       if (fine_grid->nodes->GetBoundary(iFinePoint)) {
         nodes->SetBoundary(iCoarsePoint, nMarker);
@@ -814,22 +739,22 @@ void CMultiGridGeometry::SetVertex(const CGeometry *fine_grid, const CConfig *co
     }
 
   vertex = new CVertex**[nMarker];
-  nVertex = new unsigned long [nMarker];
+  nVertex = new unsigned long[nMarker];
 
-  Tag_to_Marker = new string [nMarker_Max];
+  Tag_to_Marker = new string[nMarker_Max];
   for (iMarker_Tag = 0; iMarker_Tag < nMarker_Max; iMarker_Tag++)
     Tag_to_Marker[iMarker_Tag] = fine_grid->GetMarker_Tag(iMarker_Tag);
 
   /*--- Compute the number of vertices to do the dimensionalization ---*/
   for (iMarker = 0; iMarker < nMarker; iMarker++) nVertex[iMarker] = 0;
 
-
-  for (iCoarsePoint = 0; iCoarsePoint < nPoint; iCoarsePoint ++) {
+  for (iCoarsePoint = 0; iCoarsePoint < nPoint; iCoarsePoint++) {
     if (nodes->GetBoundary(iCoarsePoint)) {
-      for (iChildren = 0; iChildren < nodes->GetnChildren_CV(iCoarsePoint); iChildren ++) {
+      for (iChildren = 0; iChildren < nodes->GetnChildren_CV(iCoarsePoint); iChildren++) {
         iFinePoint = nodes->GetChildren_CV(iCoarsePoint, iChildren);
-        for (iMarker = 0; iMarker < nMarker; iMarker ++) {
-          if ((fine_grid->nodes->GetVertex(iFinePoint, iMarker) != -1) && (nodes->GetVertex(iCoarsePoint, iMarker) == -1)) {
+        for (iMarker = 0; iMarker < nMarker; iMarker++) {
+          if ((fine_grid->nodes->GetVertex(iFinePoint, iMarker) != -1) &&
+              (nodes->GetVertex(iCoarsePoint, iMarker) == -1)) {
             iVertex = nVertex[iMarker];
             nodes->SetVertex(iCoarsePoint, iVertex, iMarker);
             nVertex[iMarker]++;
@@ -840,23 +765,23 @@ void CMultiGridGeometry::SetVertex(const CGeometry *fine_grid, const CConfig *co
   }
 
   for (iMarker = 0; iMarker < nMarker; iMarker++) {
-    vertex[iMarker] = new CVertex* [fine_grid->GetnVertex(iMarker)+1];
+    vertex[iMarker] = new CVertex*[fine_grid->GetnVertex(iMarker) + 1];
     nVertex[iMarker] = 0;
   }
 
-  for (iCoarsePoint = 0; iCoarsePoint < nPoint; iCoarsePoint ++)
+  for (iCoarsePoint = 0; iCoarsePoint < nPoint; iCoarsePoint++)
     if (nodes->GetBoundary(iCoarsePoint))
-      for (iMarker = 0; iMarker < nMarker; iMarker ++)
-        nodes->SetVertex(iCoarsePoint, -1, iMarker);
+      for (iMarker = 0; iMarker < nMarker; iMarker++) nodes->SetVertex(iCoarsePoint, -1, iMarker);
 
   for (iMarker = 0; iMarker < nMarker; iMarker++) nVertex[iMarker] = 0;
 
-  for (iCoarsePoint = 0; iCoarsePoint < nPoint; iCoarsePoint ++) {
+  for (iCoarsePoint = 0; iCoarsePoint < nPoint; iCoarsePoint++) {
     if (nodes->GetBoundary(iCoarsePoint)) {
-      for (iChildren = 0; iChildren < nodes->GetnChildren_CV(iCoarsePoint); iChildren ++) {
+      for (iChildren = 0; iChildren < nodes->GetnChildren_CV(iCoarsePoint); iChildren++) {
         iFinePoint = nodes->GetChildren_CV(iCoarsePoint, iChildren);
-        for (iMarker = 0; iMarker < fine_grid->GetnMarker(); iMarker ++) {
-          if ((fine_grid->nodes->GetVertex(iFinePoint, iMarker) != -1) && (nodes->GetVertex(iCoarsePoint, iMarker) == -1)) {
+        for (iMarker = 0; iMarker < fine_grid->GetnMarker(); iMarker++) {
+          if ((fine_grid->nodes->GetVertex(iFinePoint, iMarker) != -1) &&
+              (nodes->GetVertex(iCoarsePoint, iMarker) == -1)) {
             iVertex = nVertex[iMarker];
             vertex[iMarker][iVertex] = new CVertex(iCoarsePoint, nDim);
             nodes->SetVertex(iCoarsePoint, iVertex, iMarker);
@@ -873,8 +798,7 @@ void CMultiGridGeometry::SetVertex(const CGeometry *fine_grid, const CConfig *co
   }
 }
 
-void CMultiGridGeometry::MatchActuator_Disk(const CConfig *config) {
-
+void CMultiGridGeometry::MatchActuator_Disk(const CConfig* config) {
   unsigned short iMarker;
   unsigned long iVertex, iPoint;
   int iProcessor = size;
@@ -890,11 +814,9 @@ void CMultiGridGeometry::MatchActuator_Disk(const CConfig *config) {
       }
     }
   }
-
 }
 
-void CMultiGridGeometry::MatchPeriodic(const CConfig *config, unsigned short val_periodic) {
-
+void CMultiGridGeometry::MatchPeriodic(const CConfig* config, unsigned short val_periodic) {
   unsigned short iMarker, iPeriodic, nPeriodic;
   unsigned long iVertex, iPoint;
   int iProcessor = rank;
@@ -906,133 +828,123 @@ void CMultiGridGeometry::MatchPeriodic(const CConfig *config, unsigned short val
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
     if (config->GetMarker_All_KindBC(iMarker) == PERIODIC_BOUNDARY) {
       iPeriodic = config->GetMarker_All_PerBound(iMarker);
-      if ((iPeriodic == val_periodic) ||
-          (iPeriodic == val_periodic + nPeriodic/2)) {
+      if ((iPeriodic == val_periodic) || (iPeriodic == val_periodic + nPeriodic / 2)) {
         for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
           iPoint = vertex[iMarker][iVertex]->GetNode();
           if (nodes->GetDomain(iPoint)) {
-            vertex[iMarker][iVertex]->SetDonorPoint(iPoint, nodes->GetGlobalIndex(iPoint), iVertex, iMarker, iProcessor);
+            vertex[iMarker][iVertex]->SetDonorPoint(iPoint, nodes->GetGlobalIndex(iPoint), iVertex, iMarker,
+                                                    iProcessor);
           }
         }
       }
     }
   }
-
 }
 
-void CMultiGridGeometry::SetControlVolume(const CGeometry *fine_grid, unsigned short action) {
-
+void CMultiGridGeometry::SetControlVolume(const CGeometry* fine_grid, unsigned short action) {
   BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
-
-  unsigned long iFinePoint, iCoarsePoint, iEdge, iParent;
-  long FineEdge, CoarseEdge;
-  unsigned short iChildren;
-  bool change_face_orientation;
-  su2double Coarse_Volume, Area;
-
-  /*--- Compute the area of the coarse volume ---*/
-  for (iCoarsePoint = 0; iCoarsePoint < nPoint; iCoarsePoint ++) {
-    nodes->SetVolume(iCoarsePoint, 0.0);
-    Coarse_Volume = 0.0;
-    for (iChildren = 0; iChildren < nodes->GetnChildren_CV(iCoarsePoint); iChildren ++) {
-      iFinePoint = nodes->GetChildren_CV(iCoarsePoint, iChildren);
-      Coarse_Volume += fine_grid->nodes->GetVolume(iFinePoint);
+    unsigned long iFinePoint, iCoarsePoint, iEdge, iParent;
+    long FineEdge, CoarseEdge;
+    unsigned short iChildren;
+    bool change_face_orientation;
+    su2double Coarse_Volume, Area;
+
+    /*--- Compute the area of the coarse volume ---*/
+    for (iCoarsePoint = 0; iCoarsePoint < nPoint; iCoarsePoint++) {
+      nodes->SetVolume(iCoarsePoint, 0.0);
+      Coarse_Volume = 0.0;
+      for (iChildren = 0; iChildren < nodes->GetnChildren_CV(iCoarsePoint); iChildren++) {
+        iFinePoint = nodes->GetChildren_CV(iCoarsePoint, iChildren);
+        Coarse_Volume += fine_grid->nodes->GetVolume(iFinePoint);
+      }
+      nodes->SetVolume(iCoarsePoint, Coarse_Volume);
     }
-    nodes->SetVolume(iCoarsePoint, Coarse_Volume);
-  }
-
-  /*--- Update or not the values of faces at the edge ---*/
-  if (action != ALLOCATE) {
-    edges->SetZeroValues();
-  }
 
-  for (iCoarsePoint = 0; iCoarsePoint < nPoint; iCoarsePoint ++)
-    for (iChildren = 0; iChildren < nodes->GetnChildren_CV(iCoarsePoint); iChildren ++) {
-      iFinePoint = nodes->GetChildren_CV(iCoarsePoint, iChildren);
+    /*--- Update or not the values of faces at the edge ---*/
+    if (action != ALLOCATE) {
+      edges->SetZeroValues();
+    }
 
-      for (auto iFinePoint_Neighbor : fine_grid->nodes->GetPoints(iFinePoint)) {
-        iParent = fine_grid->nodes->GetParent_CV(iFinePoint_Neighbor);
-        if ((iParent != iCoarsePoint) && (iParent < iCoarsePoint)) {
+    for (iCoarsePoint = 0; iCoarsePoint < nPoint; iCoarsePoint++)
+      for (iChildren = 0; iChildren < nodes->GetnChildren_CV(iCoarsePoint); iChildren++) {
+        iFinePoint = nodes->GetChildren_CV(iCoarsePoint, iChildren);
 
-          FineEdge = fine_grid->FindEdge(iFinePoint, iFinePoint_Neighbor);
+        for (auto iFinePoint_Neighbor : fine_grid->nodes->GetPoints(iFinePoint)) {
+          iParent = fine_grid->nodes->GetParent_CV(iFinePoint_Neighbor);
+          if ((iParent != iCoarsePoint) && (iParent < iCoarsePoint)) {
+            FineEdge = fine_grid->FindEdge(iFinePoint, iFinePoint_Neighbor);
 
-          change_face_orientation = false;
-          if (iFinePoint < iFinePoint_Neighbor) change_face_orientation = true;
+            change_face_orientation = false;
+            if (iFinePoint < iFinePoint_Neighbor) change_face_orientation = true;
 
-          CoarseEdge = FindEdge(iParent, iCoarsePoint);
+            CoarseEdge = FindEdge(iParent, iCoarsePoint);
 
-          const auto Normal = fine_grid->edges->GetNormal(FineEdge);
+            const auto Normal = fine_grid->edges->GetNormal(FineEdge);
 
-          if (change_face_orientation) {
-            edges->SubNormal(CoarseEdge,Normal);
-          }
-          else {
-            edges->AddNormal(CoarseEdge,Normal);
+            if (change_face_orientation) {
+              edges->SubNormal(CoarseEdge, Normal);
+            } else {
+              edges->AddNormal(CoarseEdge, Normal);
+            }
           }
         }
       }
-    }
 
-  /*--- Check if there is a normal with null area ---*/
+    /*--- Check if there is a normal with null area ---*/
 
-  for (iEdge = 0; iEdge < nEdge; iEdge++) {
-    const auto NormalFace = edges->GetNormal(iEdge);
-    Area = GeometryToolbox::Norm(nDim, NormalFace);
-    if (Area == 0.0) {
-      su2double DefaultNormal[3] = {EPS*EPS};
-      edges->SetNormal(iEdge, DefaultNormal);
+    for (iEdge = 0; iEdge < nEdge; iEdge++) {
+      const auto NormalFace = edges->GetNormal(iEdge);
+      Area = GeometryToolbox::Norm(nDim, NormalFace);
+      if (Area == 0.0) {
+        su2double DefaultNormal[3] = {EPS * EPS};
+        edges->SetNormal(iEdge, DefaultNormal);
+      }
     }
   }
-
-  }
   END_SU2_OMP_SAFE_GLOBAL_ACCESS
 }
 
-void CMultiGridGeometry::SetBoundControlVolume(const CGeometry *fine_grid, unsigned short action) {
-
+void CMultiGridGeometry::SetBoundControlVolume(const CGeometry* fine_grid, unsigned short action) {
   BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
+    unsigned long iCoarsePoint, iFinePoint, FineVertex, iVertex;
+    unsigned short iMarker, iChildren, iDim;
+    su2double *Normal, Area, *NormalFace = nullptr;
 
-  unsigned long iCoarsePoint, iFinePoint, FineVertex, iVertex;
-  unsigned short iMarker, iChildren, iDim;
-  su2double *Normal, Area, *NormalFace = nullptr;
+    Normal = new su2double[nDim];
 
-  Normal = new su2double [nDim];
+    if (action != ALLOCATE) {
+      for (iMarker = 0; iMarker < nMarker; iMarker++)
+        for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) vertex[iMarker][iVertex]->SetZeroValues();
+    }
 
-  if (action != ALLOCATE) {
     for (iMarker = 0; iMarker < nMarker; iMarker++)
-      for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++)
-        vertex[iMarker][iVertex]->SetZeroValues();
-  }
-
-  for (iMarker = 0; iMarker < nMarker; iMarker ++)
-    for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
-      iCoarsePoint = vertex[iMarker][iVertex]->GetNode();
-      for (iChildren = 0; iChildren < nodes->GetnChildren_CV(iCoarsePoint); iChildren ++) {
-        iFinePoint = nodes->GetChildren_CV(iCoarsePoint, iChildren);
-        if (fine_grid->nodes->GetVertex(iFinePoint, iMarker)!=-1) {
-          FineVertex = fine_grid->nodes->GetVertex(iFinePoint, iMarker);
-          fine_grid->vertex[iMarker][FineVertex]->GetNormal(Normal);
-          vertex[iMarker][iVertex]->AddNormal(Normal);
+      for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
+        iCoarsePoint = vertex[iMarker][iVertex]->GetNode();
+        for (iChildren = 0; iChildren < nodes->GetnChildren_CV(iCoarsePoint); iChildren++) {
+          iFinePoint = nodes->GetChildren_CV(iCoarsePoint, iChildren);
+          if (fine_grid->nodes->GetVertex(iFinePoint, iMarker) != -1) {
+            FineVertex = fine_grid->nodes->GetVertex(iFinePoint, iMarker);
+            fine_grid->vertex[iMarker][FineVertex]->GetNormal(Normal);
+            vertex[iMarker][iVertex]->AddNormal(Normal);
+          }
         }
       }
-    }
 
-  delete[] Normal;
-
-  /*--- Check if there is a normal with null area ---*/
-  for (iMarker = 0; iMarker < nMarker; iMarker ++)
-    for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
-      NormalFace = vertex[iMarker][iVertex]->GetNormal();
-      Area = GeometryToolbox::Norm(nDim, NormalFace);
-      if (Area == 0.0) for (iDim = 0; iDim < nDim; iDim++) NormalFace[iDim] = EPS*EPS;
-    }
+    delete[] Normal;
 
+    /*--- Check if there is a normal with null area ---*/
+    for (iMarker = 0; iMarker < nMarker; iMarker++)
+      for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
+        NormalFace = vertex[iMarker][iVertex]->GetNormal();
+        Area = GeometryToolbox::Norm(nDim, NormalFace);
+        if (Area == 0.0)
+          for (iDim = 0; iDim < nDim; iDim++) NormalFace[iDim] = EPS * EPS;
+      }
   }
   END_SU2_OMP_SAFE_GLOBAL_ACCESS
 }
 
-void CMultiGridGeometry::SetCoord(const CGeometry *fine_grid) {
-
+void CMultiGridGeometry::SetCoord(const CGeometry* fine_grid) {
   SU2_OMP_FOR_STAT(roundUpDiv(nPoint, omp_get_max_threads()))
   for (auto Point_Coarse = 0ul; Point_Coarse < nPoint; Point_Coarse++) {
     auto Area_Parent = nodes->GetVolume(Point_Coarse);
@@ -1042,15 +954,14 @@ void CMultiGridGeometry::SetCoord(const CGeometry *fine_grid) {
       auto Area_Children = fine_grid->nodes->GetVolume(Point_Fine);
       auto Coordinates_Fine = fine_grid->nodes->GetCoord(Point_Fine);
       for (auto iDim = 0u; iDim < nDim; iDim++)
-        Coordinates[iDim] += Coordinates_Fine[iDim]*Area_Children/Area_Parent;
+        Coordinates[iDim] += Coordinates_Fine[iDim] * Area_Children / Area_Parent;
     }
     nodes->SetCoord(Point_Coarse, Coordinates);
   }
   END_SU2_OMP_FOR
 }
 
-void CMultiGridGeometry::SetMultiGridWallHeatFlux(const CGeometry *fine_grid, unsigned short val_marker) {
-
+void CMultiGridGeometry::SetMultiGridWallHeatFlux(const CGeometry* fine_grid, unsigned short val_marker) {
   struct {
     const CGeometry* fine_grid;
     unsigned short marker;
@@ -1068,8 +979,7 @@ void CMultiGridGeometry::SetMultiGridWallHeatFlux(const CGeometry *fine_grid, un
   SetMultiGridWallQuantity(fine_grid, val_marker, wall_heat_flux);
 }
 
-void CMultiGridGeometry::SetMultiGridWallTemperature(const CGeometry *fine_grid, unsigned short val_marker){
-
+void CMultiGridGeometry::SetMultiGridWallTemperature(const CGeometry* fine_grid, unsigned short val_marker) {
   struct {
     const CGeometry* fine_grid;
     unsigned short marker;
@@ -1087,10 +997,9 @@ void CMultiGridGeometry::SetMultiGridWallTemperature(const CGeometry *fine_grid,
   SetMultiGridWallQuantity(fine_grid, val_marker, wall_temperature);
 }
 
-void CMultiGridGeometry::SetRestricted_GridVelocity(const CGeometry *fine_grid) {
-
+void CMultiGridGeometry::SetRestricted_GridVelocity(const CGeometry* fine_grid) {
   /*--- Loop over all coarse mesh points. ---*/
-  SU2_OMP_FOR_STAT(roundUpDiv(nPoint,omp_get_max_threads()))
+  SU2_OMP_FOR_STAT(roundUpDiv(nPoint, omp_get_max_threads()))
   for (unsigned long Point_Coarse = 0; Point_Coarse < nPoint; Point_Coarse++) {
     su2double Area_Parent = nodes->GetVolume(Point_Coarse);
 
@@ -1100,55 +1009,50 @@ void CMultiGridGeometry::SetRestricted_GridVelocity(const CGeometry *fine_grid)
     /*--- Loop over all of the children for this coarse CV and compute
      a grid velocity based on the values in the child CVs (fine mesh). ---*/
     for (unsigned short iChild = 0; iChild < nodes->GetnChildren_CV(Point_Coarse); iChild++) {
-      unsigned long Point_Fine       = nodes->GetChildren_CV(Point_Coarse, iChild);
-      su2double Area_Child           = fine_grid->nodes->GetVolume(Point_Fine);
+      unsigned long Point_Fine = nodes->GetChildren_CV(Point_Coarse, iChild);
+      su2double Area_Child = fine_grid->nodes->GetVolume(Point_Fine);
       const su2double* Grid_Vel_Fine = fine_grid->nodes->GetGridVel(Point_Fine);
       for (unsigned short iDim = 0; iDim < nDim; iDim++)
-        Grid_Vel[iDim] += Grid_Vel_Fine[iDim]*Area_Child/Area_Parent;
+        Grid_Vel[iDim] += Grid_Vel_Fine[iDim] * Area_Child / Area_Parent;
     }
 
     /*--- Set the grid velocity for this coarse node. ---*/
-    for (unsigned short iDim = 0; iDim < nDim; iDim++)
-      nodes->SetGridVel(Point_Coarse, iDim, Grid_Vel[iDim]);
+    for (unsigned short iDim = 0; iDim < nDim; iDim++) nodes->SetGridVel(Point_Coarse, iDim, Grid_Vel[iDim]);
   }
   END_SU2_OMP_FOR
 }
 
-
-void CMultiGridGeometry::FindNormal_Neighbor(const CConfig *config) {
-
+void CMultiGridGeometry::FindNormal_Neighbor(const CConfig* config) {
   unsigned short iMarker, iDim;
   unsigned long iPoint, iVertex;
 
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-
     if (config->GetMarker_All_KindBC(iMarker) != SEND_RECEIVE &&
         config->GetMarker_All_KindBC(iMarker) != INTERNAL_BOUNDARY &&
-        config->GetMarker_All_KindBC(iMarker) != NEARFIELD_BOUNDARY ) {
-
+        config->GetMarker_All_KindBC(iMarker) != NEARFIELD_BOUNDARY) {
       for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
-
         iPoint = vertex[iMarker][iVertex]->GetNode();
 
         /*--- If the node belong to the domain ---*/
         if (nodes->GetDomain(iPoint)) {
-
           /*--- Compute closest normal neighbor ---*/
           su2double cos_max, scalar_prod, norm_vect, norm_Normal, cos_alpha, diff_coord;
           unsigned long Point_Normal = 0;
-          su2double *Normal = vertex[iMarker][iVertex]->GetNormal();
+          su2double* Normal = vertex[iMarker][iVertex]->GetNormal();
           cos_max = -1.0;
           for (auto jPoint : nodes->GetPoints(iPoint)) {
-            scalar_prod = 0.0; norm_vect = 0.0; norm_Normal = 0.0;
+            scalar_prod = 0.0;
+            norm_vect = 0.0;
+            norm_Normal = 0.0;
             for (iDim = 0; iDim < nDim; iDim++) {
-              diff_coord = nodes->GetCoord(jPoint, iDim)-nodes->GetCoord(iPoint, iDim);
-              scalar_prod += diff_coord*Normal[iDim];
-              norm_vect += diff_coord*diff_coord;
-              norm_Normal += Normal[iDim]*Normal[iDim];
+              diff_coord = nodes->GetCoord(jPoint, iDim) - nodes->GetCoord(iPoint, iDim);
+              scalar_prod += diff_coord * Normal[iDim];
+              norm_vect += diff_coord * diff_coord;
+              norm_Normal += Normal[iDim] * Normal[iDim];
             }
             norm_vect = sqrt(norm_vect);
             norm_Normal = sqrt(norm_Normal);
-            cos_alpha = scalar_prod/(norm_vect*norm_Normal);
+            cos_alpha = scalar_prod / (norm_vect * norm_Normal);
 
             /*--- Get maximum cosine (not minimum because normals are oriented inwards) ---*/
             if (cos_alpha >= cos_max) {
@@ -1162,4 +1066,3 @@ void CMultiGridGeometry::FindNormal_Neighbor(const CConfig *config) {
     }
   }
 }
-
diff --git a/Common/src/geometry/CMultiGridQueue.cpp b/Common/src/geometry/CMultiGridQueue.cpp
index 3d670b05455..cc6a16a8b4d 100644
--- a/Common/src/geometry/CMultiGridQueue.cpp
+++ b/Common/src/geometry/CMultiGridQueue.cpp
@@ -28,14 +28,9 @@
 #include "../../include/geometry/CMultiGridQueue.hpp"
 #include <numeric>
 
-CMultiGridQueue::CMultiGridQueue(unsigned long npoint) :
-  Priority(npoint,0),
-  RightCV(npoint,true),
-  nPoint(npoint) {
-
+CMultiGridQueue::CMultiGridQueue(unsigned long npoint) : Priority(npoint, 0), RightCV(npoint, true), nPoint(npoint) {
   /*--- Queue initialization with all the points in the fine grid. ---*/
   QueueCV.emplace_back(nPoint);
-
 }
 
 void CMultiGridQueue::ThrowPointNotInListError(unsigned long iPoint) const {
@@ -45,8 +40,7 @@ void CMultiGridQueue::ThrowPointNotInListError(unsigned long iPoint) const {
 }
 
 void CMultiGridQueue::AddCV(unsigned long newPoint, short numberNeighbors) {
-
-  const short maxNeighbors = QueueCV.size()-1;
+  const short maxNeighbors = QueueCV.size() - 1;
 
   /*--- Basic check ---*/
   if (newPoint >= nPoint) {
@@ -55,9 +49,8 @@ void CMultiGridQueue::AddCV(unsigned long newPoint, short numberNeighbors) {
 
   /*--- Resize the list ---*/
   if (numberNeighbors > maxNeighbors) {
-    const size_t newSize = numberNeighbors+1;
-    if (QueueCV.capacity() < newSize)
-      QueueCV.reserve(2*newSize);
+    const size_t newSize = numberNeighbors + 1;
+    if (QueueCV.capacity() < newSize) QueueCV.reserve(2 * newSize);
     QueueCV.resize(newSize);
   }
 
@@ -69,11 +62,9 @@ void CMultiGridQueue::AddCV(unsigned long newPoint, short numberNeighbors) {
     QueueCV[numberNeighbors].push_back(newPoint);
     Priority[newPoint] = numberNeighbors;
   }
-
 }
 
 void CMultiGridQueue::RemoveCV(unsigned long removePoint) {
-
   /*--- Basic check ---*/
   if (removePoint >= nPoint) {
     SU2_MPI::Error("The index of the CV is greater than the size of the priority list.", CURRENT_FUNCTION);
@@ -94,25 +85,21 @@ void CMultiGridQueue::RemoveCV(unsigned long removePoint) {
   while (sizeQueueCV > 0) {
     if (!QueueCV[--sizeQueueCV].empty()) break;
   }
-  QueueCV.resize(sizeQueueCV+1);
-
+  QueueCV.resize(sizeQueueCV + 1);
 }
 
 void CMultiGridQueue::MoveCV(unsigned long movePoint, short numberNeighbors) {
-
   RightCV[movePoint] = (numberNeighbors >= 0);
-  numberNeighbors = max<short>(numberNeighbors,0);
+  numberNeighbors = max<short>(numberNeighbors, 0);
 
   /*--- Remove the control volume ---*/
   RemoveCV(movePoint);
 
   /*--- Add a new control volume ---*/
   AddCV(movePoint, numberNeighbors);
-
 }
 
 void CMultiGridQueue::IncrPriorityCV(unsigned long incrPoint) {
-
   /*--- Find the priority list ---*/
   const short numberNeighbors = Priority[incrPoint];
 
@@ -120,12 +107,10 @@ void CMultiGridQueue::IncrPriorityCV(unsigned long incrPoint) {
   RemoveCV(incrPoint);
 
   /*--- Increase the priority ---*/
-  AddCV(incrPoint, numberNeighbors+1);
-
+  AddCV(incrPoint, numberNeighbors + 1);
 }
 
 void CMultiGridQueue::RedPriorityCV(unsigned long redPoint) {
-
   /*--- Find the priority list ---*/
   const short numberNeighbors = Priority[redPoint];
   if (numberNeighbors == 0) return;
@@ -134,42 +119,35 @@ void CMultiGridQueue::RedPriorityCV(unsigned long redPoint) {
   RemoveCV(redPoint);
 
   /*--- Decrease the priority ---*/
-  AddCV(redPoint, numberNeighbors-1);
-
+  AddCV(redPoint, numberNeighbors - 1);
 }
 
 void CMultiGridQueue::VisualizeQueue(void) const {
-
   cout << endl;
   unsigned short iQ = 0;
   for (const auto& Q : QueueCV) {
     cout << "Number of neighbors " << iQ << ": ";
     for (auto iPoint : Q)
-      if (iPoint != QueueType::ErasedValue)
-        cout << iPoint << " ";
+      if (iPoint != QueueType::ErasedValue) cout << iPoint << " ";
     cout << endl;
     iQ++;
   }
 }
 
 void CMultiGridQueue::VisualizePriority(void) const {
-
   for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint) {
     cout << "Control Volume: " << iPoint << " Priority: " << Priority[iPoint] << endl;
   }
 }
 
 bool CMultiGridQueue::EmptyQueue(void) const {
-
   /*--- In case there is only the no agglomerated elements (size 1), check
    *    if they can be agglomerated or if we have already finished. ---*/
 
   if (QueueCV.size() == 1) {
     for (auto iPoint : QueueCV[0])
-      if ((iPoint != QueueType::ErasedValue) && RightCV[iPoint])
-        return false;
-  }
-  else {
+      if ((iPoint != QueueType::ErasedValue) && RightCV[iPoint]) return false;
+  } else {
     for (size_t iQ = 1; iQ < QueueCV.size(); ++iQ)
       if (!QueueCV[iQ].empty()) return false;
   }
@@ -182,11 +160,9 @@ unsigned long CMultiGridQueue::TotalCV(void) const {
   return TotalCV;
 }
 
-void CMultiGridQueue::Update(unsigned long updatePoint, CGeometry *fineGrid) {
-
+void CMultiGridQueue::Update(unsigned long updatePoint, CGeometry* fineGrid) {
   RemoveCV(updatePoint);
 
   for (auto jPoint : fineGrid->nodes->GetPoints(updatePoint))
-    if (!fineGrid->nodes->GetAgglomerate(jPoint))
-      IncrPriorityCV(jPoint);
+    if (!fineGrid->nodes->GetAgglomerate(jPoint)) IncrPriorityCV(jPoint);
 }
diff --git a/Common/src/geometry/CPhysicalGeometry.cpp b/Common/src/geometry/CPhysicalGeometry.cpp
index 5d097a75daa..8496dcb6491 100644
--- a/Common/src/geometry/CPhysicalGeometry.cpp
+++ b/Common/src/geometry/CPhysicalGeometry.cpp
@@ -55,11 +55,10 @@
 #include <direct.h>
 #endif
 
+CPhysicalGeometry::CPhysicalGeometry() : CGeometry() {}
 
-CPhysicalGeometry::CPhysicalGeometry() : CGeometry() { }
-
-CPhysicalGeometry::CPhysicalGeometry(CConfig *config, unsigned short val_iZone, unsigned short val_nZone) : CGeometry() {
-
+CPhysicalGeometry::CPhysicalGeometry(CConfig* config, unsigned short val_iZone, unsigned short val_nZone)
+    : CGeometry() {
   edgeColorGroupSize = config->GetEdgeColoringGroupSize();
 
   string text_line, Marker_Tag;
@@ -70,7 +69,7 @@ CPhysicalGeometry::CPhysicalGeometry(CConfig *config, unsigned short val_iZone,
   ofstream boundary_file;
   string Grid_Marker;
 
-  string val_mesh_filename  = config->GetMesh_FileName();
+  string val_mesh_filename = config->GetMesh_FileName();
   unsigned short val_format = config->GetMesh_FileFormat();
 
   /*--- Determine whether or not a FEM discretization is used ---*/
@@ -79,7 +78,7 @@ CPhysicalGeometry::CPhysicalGeometry(CConfig *config, unsigned short val_iZone,
 
   /*--- Initialize counters for local/global points & elements ---*/
 
-  if( fem_solver ) {
+  if (fem_solver) {
     switch (val_format) {
       case SU2:
         Read_SU2_Format_Parallel_FEM(config, val_mesh_filename, val_iZone, val_nZone);
@@ -93,11 +92,12 @@ CPhysicalGeometry::CPhysicalGeometry(CConfig *config, unsigned short val_iZone,
         SU2_MPI::Error("Unrecognized mesh format specified for the FEM solver!", CURRENT_FUNCTION);
         break;
     }
-  }
-  else {
-
+  } else {
     switch (val_format) {
-      case SU2: case CGNS_GRID: case RECTANGLE: case BOX:
+      case SU2:
+      case CGNS_GRID:
+      case RECTANGLE:
+      case BOX:
         Read_Mesh_FVM(config, val_mesh_filename, val_iZone, val_nZone);
         break;
       default:
@@ -113,23 +113,20 @@ CPhysicalGeometry::CPhysicalGeometry(CConfig *config, unsigned short val_iZone,
   /*--- Loop over the points element to re-scale the mesh, and plot it (only SU2_CFD) ---*/
 
   if (config->GetKind_SU2() == SU2_COMPONENT::SU2_CFD) {
-
     /*--- The US system uses feet, but SU2 assumes that the grid is in inches ---*/
 
     if (config->GetSystemMeasurements() == US) {
       for (iPoint = 0; iPoint < nPoint; iPoint++) {
         for (iDim = 0; iDim < nDim; iDim++) {
-          nodes->SetCoord(iPoint, iDim, nodes->GetCoord(iPoint, iDim)/12.0);
+          nodes->SetCoord(iPoint, iDim, nodes->GetCoord(iPoint, iDim) / 12.0);
         }
       }
     }
-
   }
 
   /*--- If SU2_DEF then write a file with the boundary information ---*/
 
   if ((config->GetKind_SU2() == SU2_COMPONENT::SU2_DEF) && (rank == MASTER_NODE)) {
-
     string str = "boundary.dat";
 
     str = config->GetMultizone_FileName(str, val_iZone, ".dat");
@@ -143,16 +140,15 @@ CPhysicalGeometry::CPhysicalGeometry(CConfig *config, unsigned short val_iZone,
     boundary_file << "NMARK= " << nMarker << endl;
 
     for (iMarker = 0; iMarker < nMarker; iMarker++) {
-
       Grid_Marker = config->GetMarker_All_TagBound(iMarker);
       boundary_file << "MARKER_TAG= " << Grid_Marker << endl;
-      boundary_file << "MARKER_ELEMS= " << nElem_Bound[iMarker]<< endl;
+      boundary_file << "MARKER_ELEMS= " << nElem_Bound[iMarker] << endl;
       boundary_file << "SEND_TO= " << config->GetMarker_All_SendRecv(iMarker) << endl;
       if (nDim == 2) {
         for (iElem_Bound = 0; iElem_Bound < nElem_Bound[iMarker]; iElem_Bound++) {
-          boundary_file << bound[iMarker][iElem_Bound]->GetVTK_Type() << "\t" ;
+          boundary_file << bound[iMarker][iElem_Bound]->GetVTK_Type() << "\t";
           for (iNodes = 0; iNodes < bound[iMarker][iElem_Bound]->GetnNodes(); iNodes++)
-            boundary_file << bound[iMarker][iElem_Bound]->GetNode(iNodes) << "\t" ;
+            boundary_file << bound[iMarker][iElem_Bound]->GetNode(iNodes) << "\t";
 
           if (bound[iMarker][iElem_Bound]->GetVTK_Type() == VERTEX) {
             boundary_file << bound[iMarker][iElem_Bound]->GetRotation_Type() << "\t";
@@ -163,9 +159,9 @@ CPhysicalGeometry::CPhysicalGeometry(CConfig *config, unsigned short val_iZone,
 
       if (nDim == 3) {
         for (iElem_Bound = 0; iElem_Bound < nElem_Bound[iMarker]; iElem_Bound++) {
-          boundary_file << bound[iMarker][iElem_Bound]->GetVTK_Type() << "\t" ;
+          boundary_file << bound[iMarker][iElem_Bound]->GetVTK_Type() << "\t";
           for (iNodes = 0; iNodes < bound[iMarker][iElem_Bound]->GetnNodes(); iNodes++)
-            boundary_file << bound[iMarker][iElem_Bound]->GetNode(iNodes) << "\t" ;
+            boundary_file << bound[iMarker][iElem_Bound]->GetNode(iNodes) << "\t";
 
           if (bound[iMarker][iElem_Bound]->GetVTK_Type() == VERTEX) {
             boundary_file << bound[iMarker][iElem_Bound]->GetRotation_Type() << "\t";
@@ -173,28 +169,23 @@ CPhysicalGeometry::CPhysicalGeometry(CConfig *config, unsigned short val_iZone,
           boundary_file << iElem_Bound << endl;
         }
       }
-
     }
 
     boundary_file.close();
-
   }
 
   /*--- If the gradient smoothing solver is active, allocate space for the sensitivity and initialize. ---*/
   if (config->GetSmoothGradient()) {
-    Sensitivity.resize(nPoint,nDim) = su2double(0.0);
+    Sensitivity.resize(nPoint, nDim) = su2double(0.0);
   }
-
 }
 
-CPhysicalGeometry::CPhysicalGeometry(CGeometry *geometry,
-                                     CConfig *config) : CGeometry() {
-
+CPhysicalGeometry::CPhysicalGeometry(CGeometry* geometry, CConfig* config) : CGeometry() {
   edgeColorGroupSize = config->GetEdgeColoringGroupSize();
 
   /*--- The new geometry class has the same problem dimension/zone. ---*/
 
-  nDim  = geometry->GetnDim();
+  nDim = geometry->GetnDim();
   nZone = geometry->GetnZone();
 
   /*--- Recompute the linear partitioning offsets. ---*/
@@ -204,34 +195,30 @@ CPhysicalGeometry::CPhysicalGeometry(CGeometry *geometry,
   /*--- Communicate the coloring data so that each rank has a complete set
    of colors for all points that reside on it, including repeats. ---*/
 
-  if ((rank == MASTER_NODE) && (size != SINGLE_NODE))
-    cout <<"Distributing ParMETIS coloring." << endl;
+  if ((rank == MASTER_NODE) && (size != SINGLE_NODE)) cout << "Distributing ParMETIS coloring." << endl;
 
   DistributeColoring(config, geometry);
 
   /*--- Redistribute the points to all ranks based on the coloring. ---*/
 
-  if ((rank == MASTER_NODE) && (size != SINGLE_NODE))
-    cout <<"Rebalancing vertices." << endl;
+  if ((rank == MASTER_NODE) && (size != SINGLE_NODE)) cout << "Rebalancing vertices." << endl;
 
   DistributePoints(config, geometry);
 
   /*--- Distribute the element information to all ranks based on coloring. ---*/
 
-  if ((rank == MASTER_NODE) && (size != SINGLE_NODE))
-    cout <<"Rebalancing volume element connectivity." << endl;
+  if ((rank == MASTER_NODE) && (size != SINGLE_NODE)) cout << "Rebalancing volume element connectivity." << endl;
 
-  DistributeVolumeConnectivity(config, geometry, TRIANGLE     );
+  DistributeVolumeConnectivity(config, geometry, TRIANGLE);
   DistributeVolumeConnectivity(config, geometry, QUADRILATERAL);
-  DistributeVolumeConnectivity(config, geometry, TETRAHEDRON  );
-  DistributeVolumeConnectivity(config, geometry, HEXAHEDRON   );
-  DistributeVolumeConnectivity(config, geometry, PRISM        );
-  DistributeVolumeConnectivity(config, geometry, PYRAMID      );
+  DistributeVolumeConnectivity(config, geometry, TETRAHEDRON);
+  DistributeVolumeConnectivity(config, geometry, HEXAHEDRON);
+  DistributeVolumeConnectivity(config, geometry, PRISM);
+  DistributeVolumeConnectivity(config, geometry, PYRAMID);
 
   /*--- Distribute the marker information to all ranks based on coloring. ---*/
 
-  if ((rank == MASTER_NODE) && (size != SINGLE_NODE))
-    cout <<"Rebalancing markers and surface elements." << endl;
+  if ((rank == MASTER_NODE) && (size != SINGLE_NODE)) cout << "Rebalancing markers and surface elements." << endl;
 
   /*--- First, perform a linear partitioning of the marker information, as
    the grid readers currently store all boundary information on the master
@@ -239,32 +226,25 @@ CPhysicalGeometry::CPhysicalGeometry(CGeometry *geometry,
    reader to avoid reading the markers to the master rank alone at first. ---*/
 
   DistributeMarkerTags(config, geometry);
-  PartitionSurfaceConnectivity(config, geometry, LINE         );
-  PartitionSurfaceConnectivity(config, geometry, TRIANGLE     );
+  PartitionSurfaceConnectivity(config, geometry, LINE);
+  PartitionSurfaceConnectivity(config, geometry, TRIANGLE);
   PartitionSurfaceConnectivity(config, geometry, QUADRILATERAL);
 
   /*--- Once the markers are distributed according to the linear partitioning
    of the grid points, we can use similar techniques as above for distributing
    the surface element connectivity. ---*/
 
-  DistributeSurfaceConnectivity(config, geometry, LINE         );
-  DistributeSurfaceConnectivity(config, geometry, TRIANGLE     );
+  DistributeSurfaceConnectivity(config, geometry, LINE);
+  DistributeSurfaceConnectivity(config, geometry, TRIANGLE);
   DistributeSurfaceConnectivity(config, geometry, QUADRILATERAL);
 
   /*--- Reduce the total number of elements that we have on each rank. ---*/
 
-  nLocal_Elem = (nLocal_Tria +
-                 nLocal_Quad +
-                 nLocal_Tetr +
-                 nLocal_Hexa +
-                 nLocal_Pris +
-                 nLocal_Pyra);
+  nLocal_Elem = (nLocal_Tria + nLocal_Quad + nLocal_Tetr + nLocal_Hexa + nLocal_Pris + nLocal_Pyra);
   nLocal_Bound_Elem = nLocal_Line + nLocal_BoundTria + nLocal_BoundQuad;
 
-  SU2_MPI::Allreduce(&nLocal_Elem, &nGlobal_Elem, 1,
-                     MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
-  SU2_MPI::Allreduce(&nLocal_Bound_Elem, &nGlobal_Bound_Elem, 1,
-                     MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&nLocal_Elem, &nGlobal_Elem, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&nLocal_Bound_Elem, &nGlobal_Bound_Elem, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
 
   /*--- With the distribution of all points, elements, and markers based
    on the ParMETIS coloring complete, as a final step, load this data into
@@ -276,7 +256,7 @@ CPhysicalGeometry::CPhysicalGeometry(CGeometry *geometry,
 
   /*--- If the gradient smoothing solver is active, allocate space for the sensitivity and initialize. ---*/
   if (config->GetSmoothGradient()) {
-    Sensitivity.resize(nPoint,nDim) = su2double(0.0);
+    Sensitivity.resize(nPoint, nDim) = su2double(0.0);
   }
 
   /*--- Free memory associated with the partitioning of points and elems. ---*/
@@ -284,83 +264,81 @@ CPhysicalGeometry::CPhysicalGeometry(CGeometry *geometry,
   decltype(Neighbors)().swap(Neighbors);
   decltype(Color_List)().swap(Color_List);
 
-  delete [] Local_Points;
-  delete [] Local_Colors;
-  delete [] Local_Coords;
-
-  delete [] Conn_Line_Linear;
-  delete [] Conn_BoundTria_Linear;
-  delete [] Conn_BoundQuad_Linear;
-
-  delete [] Conn_Line;
-  delete [] Conn_BoundTria;
-  delete [] Conn_BoundQuad;
-  delete [] Conn_Tria;
-  delete [] Conn_Quad;
-  delete [] Conn_Tetr;
-  delete [] Conn_Hexa;
-  delete [] Conn_Pris;
-  delete [] Conn_Pyra;
-
-  delete [] ID_Line;
-  delete [] ID_BoundTria;
-  delete [] ID_BoundQuad;
-  delete [] ID_Line_Linear;
-  delete [] ID_BoundTria_Linear;
-  delete [] ID_BoundQuad_Linear;
-
-  delete [] ID_Tria;
-  delete [] ID_Quad;
-  delete [] ID_Tetr;
-  delete [] ID_Hexa;
-  delete [] ID_Pris;
-  delete [] ID_Pyra;
-
-  delete [] Elem_ID_Line;
-  delete [] Elem_ID_BoundTria;
-  delete [] Elem_ID_BoundQuad;
-  delete [] Elem_ID_Line_Linear;
-  delete [] Elem_ID_BoundTria_Linear;
-  delete [] Elem_ID_BoundQuad_Linear;
-
+  delete[] Local_Points;
+  delete[] Local_Colors;
+  delete[] Local_Coords;
+
+  delete[] Conn_Line_Linear;
+  delete[] Conn_BoundTria_Linear;
+  delete[] Conn_BoundQuad_Linear;
+
+  delete[] Conn_Line;
+  delete[] Conn_BoundTria;
+  delete[] Conn_BoundQuad;
+  delete[] Conn_Tria;
+  delete[] Conn_Quad;
+  delete[] Conn_Tetr;
+  delete[] Conn_Hexa;
+  delete[] Conn_Pris;
+  delete[] Conn_Pyra;
+
+  delete[] ID_Line;
+  delete[] ID_BoundTria;
+  delete[] ID_BoundQuad;
+  delete[] ID_Line_Linear;
+  delete[] ID_BoundTria_Linear;
+  delete[] ID_BoundQuad_Linear;
+
+  delete[] ID_Tria;
+  delete[] ID_Quad;
+  delete[] ID_Tetr;
+  delete[] ID_Hexa;
+  delete[] ID_Pris;
+  delete[] ID_Pyra;
+
+  delete[] Elem_ID_Line;
+  delete[] Elem_ID_BoundTria;
+  delete[] Elem_ID_BoundQuad;
+  delete[] Elem_ID_Line_Linear;
+  delete[] Elem_ID_BoundTria_Linear;
+  delete[] Elem_ID_BoundQuad_Linear;
 }
 
 CPhysicalGeometry::~CPhysicalGeometry(void) {
-
-  delete [] Local_to_Global_Point;
+  delete[] Local_to_Global_Point;
 
   /*--- Free up memory from turbomachinery performance computation  ---*/
 
   unsigned short iMarker;
   if (TangGridVelIn != nullptr) {
     for (iMarker = 0; iMarker < nTurboPerf; iMarker++)
-      if (TangGridVelIn[iMarker] != nullptr) delete [] TangGridVelIn[iMarker];
-    delete [] TangGridVelIn;
+      if (TangGridVelIn[iMarker] != nullptr) delete[] TangGridVelIn[iMarker];
+    delete[] TangGridVelIn;
   }
   if (SpanAreaIn != nullptr) {
     for (iMarker = 0; iMarker < nTurboPerf; iMarker++)
-      if (SpanAreaIn[iMarker] != nullptr) delete [] SpanAreaIn[iMarker];
-    delete [] SpanAreaIn;
+      if (SpanAreaIn[iMarker] != nullptr) delete[] SpanAreaIn[iMarker];
+    delete[] SpanAreaIn;
   }
   if (TurboRadiusIn != nullptr) {
     for (iMarker = 0; iMarker < nTurboPerf; iMarker++)
-      if (TurboRadiusIn[iMarker] != nullptr) delete [] TurboRadiusIn[iMarker];
-    delete [] TurboRadiusIn;
+      if (TurboRadiusIn[iMarker] != nullptr) delete[] TurboRadiusIn[iMarker];
+    delete[] TurboRadiusIn;
   }
   if (TangGridVelOut != nullptr) {
     for (iMarker = 0; iMarker < nTurboPerf; iMarker++)
-      if (TangGridVelOut[iMarker] != nullptr) delete [] TangGridVelOut[iMarker];
-    delete [] TangGridVelOut;
+      if (TangGridVelOut[iMarker] != nullptr) delete[] TangGridVelOut[iMarker];
+    delete[] TangGridVelOut;
   }
   if (SpanAreaOut != nullptr) {
     for (iMarker = 0; iMarker < nTurboPerf; iMarker++)
-      if (SpanAreaOut[iMarker] != nullptr) delete [] SpanAreaOut[iMarker];
-    delete [] SpanAreaOut;
+      if (SpanAreaOut[iMarker] != nullptr) delete[] SpanAreaOut[iMarker];
+    delete[] SpanAreaOut;
   }
   if (TurboRadiusOut != nullptr) {
     for (iMarker = 0; iMarker < nTurboPerf; iMarker++)
-      if (TurboRadiusOut[iMarker] != nullptr) delete [] TurboRadiusOut[iMarker];
-    delete [] TurboRadiusOut;
+      if (TurboRadiusOut[iMarker] != nullptr) delete[] TurboRadiusOut[iMarker];
+    delete[] TurboRadiusOut;
   }
 
   /*--- Free up memory from turbomachinery computations
@@ -372,108 +350,97 @@ CPhysicalGeometry::~CPhysicalGeometry(void) {
   if (turbovertex != nullptr) {
     for (iMarker = 0; iMarker < nMarker; iMarker++) {
       if (Marker_All_SendRecv[iMarker] == 0 && turbovertex[iMarker] != nullptr) {
-        for (iSpan= 0; iSpan < nSpanSectionsByMarker[iMarker]; iSpan++) {
+        for (iSpan = 0; iSpan < nSpanSectionsByMarker[iMarker]; iSpan++) {
           if (turbovertex[iMarker][iSpan] != nullptr) {
             for (iVertex = 0; iVertex < nVertexSpan[iMarker][iSpan]; iVertex++)
-              if (turbovertex[iMarker][iSpan][iVertex] != nullptr)
-                delete turbovertex[iMarker][iSpan][iVertex];
-            delete [] turbovertex[iMarker][iSpan];
+              if (turbovertex[iMarker][iSpan][iVertex] != nullptr) delete turbovertex[iMarker][iSpan][iVertex];
+            delete[] turbovertex[iMarker][iSpan];
           }
         }
-        delete [] turbovertex[iMarker];
+        delete[] turbovertex[iMarker];
       }
     }
-    delete [] turbovertex;
+    delete[] turbovertex;
   }
   if (AverageTurboNormal != nullptr) {
     for (iMarker = 0; iMarker < nMarker; iMarker++) {
       if (Marker_All_SendRecv[iMarker] == 0 && AverageTurboNormal[iMarker] != nullptr) {
-        for (iSpan= 0; iSpan < nSpanSectionsByMarker[iMarker]+1; iSpan++)
-          delete [] AverageTurboNormal[iMarker][iSpan];
-        delete [] AverageTurboNormal[iMarker];
+        for (iSpan = 0; iSpan < nSpanSectionsByMarker[iMarker] + 1; iSpan++)
+          delete[] AverageTurboNormal[iMarker][iSpan];
+        delete[] AverageTurboNormal[iMarker];
       }
     }
-    delete [] AverageTurboNormal;
+    delete[] AverageTurboNormal;
   }
   if (AverageNormal != nullptr) {
     for (iMarker = 0; iMarker < nMarker; iMarker++) {
       if (Marker_All_SendRecv[iMarker] == 0 && AverageNormal[iMarker] != nullptr) {
-        for (iSpan= 0; iSpan < nSpanSectionsByMarker[iMarker]+1; iSpan++)
-          delete [] AverageNormal[iMarker][iSpan];
-        delete [] AverageNormal[iMarker];
+        for (iSpan = 0; iSpan < nSpanSectionsByMarker[iMarker] + 1; iSpan++) delete[] AverageNormal[iMarker][iSpan];
+        delete[] AverageNormal[iMarker];
       }
     }
-    delete [] AverageNormal;
+    delete[] AverageNormal;
   }
   if (AverageGridVel != nullptr) {
     for (iMarker = 0; iMarker < nMarker; iMarker++) {
       if (Marker_All_SendRecv[iMarker] == 0 && AverageGridVel[iMarker] != nullptr) {
-        for (iSpan= 0; iSpan < nSpanSectionsByMarker[iMarker]+1; iSpan++)
-          delete [] AverageGridVel[iMarker][iSpan];
-        delete [] AverageGridVel[iMarker];
+        for (iSpan = 0; iSpan < nSpanSectionsByMarker[iMarker] + 1; iSpan++) delete[] AverageGridVel[iMarker][iSpan];
+        delete[] AverageGridVel[iMarker];
       }
     }
-    delete [] AverageGridVel;
+    delete[] AverageGridVel;
   }
 
   if (AverageTangGridVel != nullptr) {
     for (iMarker = 0; iMarker < nMarker; iMarker++)
       if (Marker_All_SendRecv[iMarker] == 0 && AverageTangGridVel[iMarker] != nullptr)
-        delete [] AverageTangGridVel[iMarker];
-    delete [] AverageTangGridVel;
+        delete[] AverageTangGridVel[iMarker];
+    delete[] AverageTangGridVel;
   }
   if (SpanArea != nullptr) {
     for (iMarker = 0; iMarker < nMarker; iMarker++)
-      if (Marker_All_SendRecv[iMarker] == 0 && SpanArea[iMarker] != nullptr)
-        delete [] SpanArea[iMarker];
-    delete [] SpanArea;
+      if (Marker_All_SendRecv[iMarker] == 0 && SpanArea[iMarker] != nullptr) delete[] SpanArea[iMarker];
+    delete[] SpanArea;
   }
   if (TurboRadius != nullptr) {
     for (iMarker = 0; iMarker < nMarker; iMarker++)
-      if (Marker_All_SendRecv[iMarker] == 0 && TurboRadius[iMarker] != nullptr)
-        delete [] TurboRadius[iMarker];
-    delete [] TurboRadius;
+      if (Marker_All_SendRecv[iMarker] == 0 && TurboRadius[iMarker] != nullptr) delete[] TurboRadius[iMarker];
+    delete[] TurboRadius;
   }
   if (MaxAngularCoord != nullptr) {
     for (iMarker = 0; iMarker < nMarker; iMarker++)
-      if (Marker_All_SendRecv[iMarker] == 0 && MaxAngularCoord[iMarker] != nullptr)
-        delete [] MaxAngularCoord[iMarker];
-    delete [] MaxAngularCoord;
+      if (Marker_All_SendRecv[iMarker] == 0 && MaxAngularCoord[iMarker] != nullptr) delete[] MaxAngularCoord[iMarker];
+    delete[] MaxAngularCoord;
   }
   if (MinAngularCoord != nullptr) {
     for (iMarker = 0; iMarker < nMarker; iMarker++)
-      if (Marker_All_SendRecv[iMarker] == 0 && MinAngularCoord[iMarker] != nullptr)
-        delete [] MinAngularCoord[iMarker];
-    delete [] MinAngularCoord;
+      if (Marker_All_SendRecv[iMarker] == 0 && MinAngularCoord[iMarker] != nullptr) delete[] MinAngularCoord[iMarker];
+    delete[] MinAngularCoord;
   }
   if (MinRelAngularCoord != nullptr) {
     for (iMarker = 0; iMarker < nMarker; iMarker++)
       if (Marker_All_SendRecv[iMarker] == 0 && MinRelAngularCoord[iMarker] != nullptr)
-        delete [] MinRelAngularCoord[iMarker];
-    delete [] MinRelAngularCoord;
+        delete[] MinRelAngularCoord[iMarker];
+    delete[] MinRelAngularCoord;
   }
 
-  delete [] nSpanWiseSections;
-  delete [] nSpanSectionsByMarker;
+  delete[] nSpanWiseSections;
+  delete[] nSpanSectionsByMarker;
   if (SpanWiseValue != nullptr) {
     for (iMarker = 0; iMarker < 2; iMarker++)
-      if (Marker_All_SendRecv[iMarker] == 0 && SpanWiseValue[iMarker] != nullptr)
-        delete [] SpanWiseValue[iMarker];
-    delete [] SpanWiseValue;
+      if (Marker_All_SendRecv[iMarker] == 0 && SpanWiseValue[iMarker] != nullptr) delete[] SpanWiseValue[iMarker];
+    delete[] SpanWiseValue;
   }
   if (nVertexSpan != nullptr) {
     for (iMarker = 0; iMarker < nMarker; iMarker++)
-      if (Marker_All_SendRecv[iMarker] == 0 && nVertexSpan[iMarker] != nullptr)
-        delete [] nVertexSpan[iMarker];
-    delete [] nVertexSpan;
+      if (Marker_All_SendRecv[iMarker] == 0 && nVertexSpan[iMarker] != nullptr) delete[] nVertexSpan[iMarker];
+    delete[] nVertexSpan;
   }
   if (nTotVertexSpan != nullptr) {
     for (iMarker = 0; iMarker < nMarker; iMarker++)
-      if (Marker_All_SendRecv[iMarker] == 0 && nTotVertexSpan[iMarker] != nullptr)
-        delete [] nTotVertexSpan[iMarker];
-    delete [] nTotVertexSpan;
+      if (Marker_All_SendRecv[iMarker] == 0 && nTotVertexSpan[iMarker] != nullptr) delete[] nTotVertexSpan[iMarker];
+    delete[] nTotVertexSpan;
   }
-
 }
 
 void CPhysicalGeometry::SetGlobal_to_Local_Point(void) {
@@ -483,9 +450,7 @@ void CPhysicalGeometry::SetGlobal_to_Local_Point(void) {
   }
 }
 
-void CPhysicalGeometry::DistributeColoring(const CConfig *config,
-                                           CGeometry *geometry) {
-
+void CPhysicalGeometry::DistributeColoring(const CConfig* config, CGeometry* geometry) {
   /*--- To start, each linear partition carries the color only for the
    owned nodes (nPoint), but we have repeated elems on each linear partition.
    We need to complete the coloring information such that the repeated
@@ -502,7 +467,7 @@ void CPhysicalGeometry::DistributeColoring(const CConfig *config,
 
   /*--- Get a linear partitioner to track the partition counts. ---*/
 
-  CLinearPartitioner pointPartitioner(geometry->GetGlobal_nPoint(),0);
+  CLinearPartitioner pointPartitioner(geometry->GetGlobal_nPoint(), 0);
 
   /*--- First, create a complete map of the points on this rank (excluding
    repeats) and their neighbors so that we can efficiently loop through the
@@ -519,9 +484,8 @@ void CPhysicalGeometry::DistributeColoring(const CConfig *config,
    rank matches the number in the mesh file (in serial). ---*/
 
   if ((size == SINGLE_NODE) && (Point_Map.size() < geometry->GetnPoint())) {
-    SU2_MPI::Error( string("Mismatch between NPOIN and number of points")
-                   +string(" listed in mesh file.\n")
-                   +string("Please check the mesh file for correctness.\n"),
+    SU2_MPI::Error(string("Mismatch between NPOIN and number of points") + string(" listed in mesh file.\n") +
+                       string("Please check the mesh file for correctness.\n"),
                    CURRENT_FUNCTION);
   }
 
@@ -536,8 +500,8 @@ void CPhysicalGeometry::DistributeColoring(const CConfig *config,
 
   jPoint = geometry->GetnPoint();
   for (auto iPoint : Point_Map) {
-    if ((iPoint <  pointPartitioner.GetFirstIndexOnRank(rank)) ||
-        (iPoint >= pointPartitioner.GetLastIndexOnRank(rank))){
+    if ((iPoint < pointPartitioner.GetFirstIndexOnRank(rank)) ||
+        (iPoint >= pointPartitioner.GetLastIndexOnRank(rank))) {
       Global2Local[iPoint] = jPoint;
       jPoint++;
     }
@@ -567,14 +531,19 @@ void CPhysicalGeometry::DistributeColoring(const CConfig *config,
 
   /*--- Prepare structures for communication. ---*/
 
-  int *nPoint_Send = new int[size+1]; nPoint_Send[0] = 0;
-  int *nPoint_Recv = new int[size+1]; nPoint_Recv[0] = 0;
-  int *nPoint_Flag = new int[size];
+  int* nPoint_Send = new int[size + 1];
+  nPoint_Send[0] = 0;
+  int* nPoint_Recv = new int[size + 1];
+  nPoint_Recv[0] = 0;
+  int* nPoint_Flag = new int[size];
 
   for (iProc = 0; iProc < size; iProc++) {
-    nPoint_Send[iProc] = 0; nPoint_Recv[iProc] = 0; nPoint_Flag[iProc]= -1;
+    nPoint_Send[iProc] = 0;
+    nPoint_Recv[iProc] = 0;
+    nPoint_Flag[iProc] = -1;
   }
-  nPoint_Send[size] = 0; nPoint_Recv[size] = 0;
+  nPoint_Send[size] = 0;
+  nPoint_Recv[size] = 0;
 
   /*--- Loop over the owned points and check all the neighbors for unowned
    points. The colors of all owned points will be communicated to any ranks
@@ -583,7 +552,6 @@ void CPhysicalGeometry::DistributeColoring(const CConfig *config,
 
   for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++) {
     for (iNeighbor = 0; iNeighbor < Neighbors[iPoint].size(); iNeighbor++) {
-
       /*--- Global ID of the neighbor ---*/
 
       jPoint = Neighbors[iPoint][iNeighbor];
@@ -597,9 +565,8 @@ void CPhysicalGeometry::DistributeColoring(const CConfig *config,
 
       if (nPoint_Flag[iProcessor] != (int)iPoint) {
         nPoint_Flag[iProcessor] = (int)iPoint;
-        nPoint_Send[iProcessor+1]++;
+        nPoint_Send[iProcessor + 1]++;
       }
-
     }
   }
 
@@ -607,8 +574,7 @@ void CPhysicalGeometry::DistributeColoring(const CConfig *config,
    all processors. After this communication, each proc knows how
    many points it will receive from each other processor. ---*/
 
-  SU2_MPI::Alltoall(&(nPoint_Send[1]), 1, MPI_INT,
-                    &(nPoint_Recv[1]), 1, MPI_INT, SU2_MPI::GetComm());
+  SU2_MPI::Alltoall(&(nPoint_Send[1]), 1, MPI_INT, &(nPoint_Recv[1]), 1, MPI_INT, SU2_MPI::GetComm());
 
   /*--- Prepare to send colors. First check how many
    messages we will be sending and receiving. Here we also put
@@ -619,34 +585,33 @@ void CPhysicalGeometry::DistributeColoring(const CConfig *config,
   for (iProc = 0; iProc < size; iProc++) nPoint_Flag[iProc] = -1;
 
   for (iProc = 0; iProc < size; iProc++) {
-    if ((iProc != rank) && (nPoint_Send[iProc+1] > 0)) nSends++;
-    if ((iProc != rank) && (nPoint_Recv[iProc+1] > 0)) nRecvs++;
+    if ((iProc != rank) && (nPoint_Send[iProc + 1] > 0)) nSends++;
+    if ((iProc != rank) && (nPoint_Recv[iProc + 1] > 0)) nRecvs++;
 
-    nPoint_Send[iProc+1] += nPoint_Send[iProc];
-    nPoint_Recv[iProc+1] += nPoint_Recv[iProc];
+    nPoint_Send[iProc + 1] += nPoint_Send[iProc];
+    nPoint_Recv[iProc + 1] += nPoint_Recv[iProc];
   }
 
   /*--- Allocate arrays for sending the global ID. ---*/
 
-  unsigned long *idSend = new unsigned long[nPoint_Send[size]];
+  unsigned long* idSend = new unsigned long[nPoint_Send[size]];
   for (iSend = 0; iSend < nPoint_Send[size]; iSend++) idSend[iSend] = 0;
 
   /*--- Allocate memory to hold the colors that we are sending. ---*/
 
-  unsigned long *colorSend = new unsigned long[nPoint_Send[size]];
+  unsigned long* colorSend = new unsigned long[nPoint_Send[size]];
   for (iSend = 0; iSend < nPoint_Send[size]; iSend++) colorSend[iSend] = 0;
 
   /*--- Create an index variable to keep track of our index
    positions as we load up the send buffer. ---*/
 
-  unsigned long *index = new unsigned long[size];
+  unsigned long* index = new unsigned long[size];
   for (iProc = 0; iProc < size; iProc++) index[iProc] = nPoint_Send[iProc];
 
   /*--- Now load up our buffers with the Global IDs and colors. ---*/
 
   for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++) {
     for (iNeighbor = 0; iNeighbor < Neighbors[iPoint].size(); iNeighbor++) {
-
       /*--- Global ID of the neighbor ---*/
 
       jPoint = Neighbors[iPoint][iNeighbor];
@@ -659,76 +624,69 @@ void CPhysicalGeometry::DistributeColoring(const CConfig *config,
        counters and load up the global ID and color. ---*/
 
       if (nPoint_Flag[iProcessor] != (int)iPoint) {
-
         nPoint_Flag[iProcessor] = (int)iPoint;
         unsigned long nn = index[iProcessor];
 
         /*--- Load the data values. ---*/
 
-        idSend[nn]    = geometry->nodes->GetGlobalIndex(iPoint);
+        idSend[nn] = geometry->nodes->GetGlobalIndex(iPoint);
         colorSend[nn] = geometry->nodes->GetColor(iPoint);
 
         /*--- Increment the index by the message length ---*/
 
         index[iProcessor]++;
-
       }
     }
   }
 
   /*--- Free memory after loading up the send buffer. ---*/
 
-  delete [] index;
+  delete[] index;
 
   /*--- Allocate the memory that we need for receiving the conn
    values and then cue up the non-blocking receives. Note that
    we do not include our own rank in the communications. We will
    directly copy our own data later. ---*/
 
-  unsigned long *colorRecv = new unsigned long[nPoint_Recv[size]];
-  for (iRecv = 0; iRecv < nPoint_Recv[size]; iRecv++)
-    colorRecv[iRecv] = 0;
+  unsigned long* colorRecv = new unsigned long[nPoint_Recv[size]];
+  for (iRecv = 0; iRecv < nPoint_Recv[size]; iRecv++) colorRecv[iRecv] = 0;
 
-  unsigned long *idRecv = new unsigned long[nPoint_Recv[size]];
-  for (iRecv = 0; iRecv < nPoint_Recv[size]; iRecv++)
-    idRecv[iRecv] = 0;
+  unsigned long* idRecv = new unsigned long[nPoint_Recv[size]];
+  for (iRecv = 0; iRecv < nPoint_Recv[size]; iRecv++) idRecv[iRecv] = 0;
 
   /*--- Allocate memory for the MPI requests if we need to communicate. ---*/
 
   if (nSends > 0) {
     colorSendReq = new SU2_MPI::Request[nSends];
-    idSendReq    = new SU2_MPI::Request[nSends];
+    idSendReq = new SU2_MPI::Request[nSends];
   }
   if (nRecvs > 0) {
     colorRecvReq = new SU2_MPI::Request[nRecvs];
-    idRecvReq    = new SU2_MPI::Request[nRecvs];
+    idRecvReq = new SU2_MPI::Request[nRecvs];
   }
 
   /*--- Launch the non-blocking sends and receives. ---*/
 
-  InitiateCommsAll(colorSend, nPoint_Send, colorSendReq,
-                   colorRecv, nPoint_Recv, colorRecvReq,
-                   1, COMM_TYPE_UNSIGNED_LONG);
+  InitiateCommsAll(colorSend, nPoint_Send, colorSendReq, colorRecv, nPoint_Recv, colorRecvReq, 1,
+                   COMM_TYPE_UNSIGNED_LONG);
 
-  InitiateCommsAll(idSend, nPoint_Send, idSendReq,
-                   idRecv, nPoint_Recv, idRecvReq,
-                   1, COMM_TYPE_UNSIGNED_LONG);
+  InitiateCommsAll(idSend, nPoint_Send, idSendReq, idRecv, nPoint_Recv, idRecvReq, 1, COMM_TYPE_UNSIGNED_LONG);
 
   /*--- Copy my own rank's data into the recv buffer directly. ---*/
 
-  iRecv   = nPoint_Recv[rank];
+  iRecv = nPoint_Recv[rank];
   myStart = nPoint_Send[rank];
-  myFinal = nPoint_Send[rank+1];
+  myFinal = nPoint_Send[rank + 1];
   for (iSend = myStart; iSend < myFinal; iSend++) {
     colorRecv[iRecv] = colorSend[iSend];
-    idRecv[iRecv]    = idSend[iSend];
+    idRecv[iRecv] = idSend[iSend];
     iRecv++;
   }
 
   /*--- Complete the non-blocking communications. ---*/
 
   CompleteCommsAll(nSends, colorSendReq, nRecvs, colorRecvReq);
-  CompleteCommsAll(nSends,    idSendReq, nRecvs,    idRecvReq);
+  CompleteCommsAll(nSends, idSendReq, nRecvs, idRecvReq);
 
   /*--- Store the complete color map for this rank in class data. Now,
    each rank has a color value for all owned nodes as well as any repeated
@@ -742,32 +700,29 @@ void CPhysicalGeometry::DistributeColoring(const CConfig *config,
 
   /*--- Free temporary memory from communications ---*/
 
-  delete [] colorSendReq;
-  delete [] idSendReq;
-
-  delete [] colorRecvReq;
-  delete [] idRecvReq;
+  delete[] colorSendReq;
+  delete[] idSendReq;
 
-  delete [] colorSend;
-  delete [] colorRecv;
-  delete [] idSend;
-  delete [] idRecv;
-  delete [] nPoint_Recv;
-  delete [] nPoint_Send;
-  delete [] nPoint_Flag;
+  delete[] colorRecvReq;
+  delete[] idRecvReq;
 
+  delete[] colorSend;
+  delete[] colorRecv;
+  delete[] idSend;
+  delete[] idRecv;
+  delete[] nPoint_Recv;
+  delete[] nPoint_Send;
+  delete[] nPoint_Flag;
 }
 
-void CPhysicalGeometry::DistributeVolumeConnectivity(const CConfig *config,
-                                                     CGeometry *geometry,
+void CPhysicalGeometry::DistributeVolumeConnectivity(const CConfig* config, CGeometry* geometry,
                                                      unsigned short Elem_Type) {
-
   unsigned short NODES_PER_ELEMENT = 0;
 
   unsigned long iProcessor;
   unsigned long iElem, iNode, jNode, nElem_Total = 0, Global_Index;
-  unsigned long *Conn_Elem  = nullptr;
-  unsigned long *ID_Elems   = nullptr;
+  unsigned long* Conn_Elem = nullptr;
+  unsigned long* ID_Elems = nullptr;
 
   SU2_MPI::Request *connSendReq = nullptr, *idSendReq = nullptr;
   SU2_MPI::Request *connRecvReq = nullptr, *idRecvReq = nullptr;
@@ -813,19 +768,23 @@ void CPhysicalGeometry::DistributeVolumeConnectivity(const CConfig *config,
    and decide how many elements we must send to each other rank in order to
    have all elements distributed according to the ParMETIS coloring. ---*/
 
-  int *nElem_Send = new int[size+1]; nElem_Send[0] = 0;
-  int *nElem_Recv = new int[size+1]; nElem_Recv[0] = 0;
-  int *nElem_Flag = new int[size];
+  int* nElem_Send = new int[size + 1];
+  nElem_Send[0] = 0;
+  int* nElem_Recv = new int[size + 1];
+  nElem_Recv[0] = 0;
+  int* nElem_Flag = new int[size];
 
   for (iProc = 0; iProc < size; iProc++) {
-    nElem_Send[iProc] = 0; nElem_Recv[iProc] = 0; nElem_Flag[iProc]= -1;
+    nElem_Send[iProc] = 0;
+    nElem_Recv[iProc] = 0;
+    nElem_Flag[iProc] = -1;
   }
-  nElem_Send[size] = 0; nElem_Recv[size] = 0;
+  nElem_Send[size] = 0;
+  nElem_Recv[size] = 0;
 
-  for (iElem = 0; iElem < geometry->GetnElem(); iElem++ ) {
+  for (iElem = 0; iElem < geometry->GetnElem(); iElem++) {
     if (geometry->elem[iElem]->GetVTK_Type() == Elem_Type) {
-      for (iNode = 0; iNode < NODES_PER_ELEMENT; iNode++ ) {
-
+      for (iNode = 0; iNode < NODES_PER_ELEMENT; iNode++) {
         /*--- Get the index of the current point. ---*/
 
         Global_Index = geometry->elem[iElem]->GetNode(iNode);
@@ -839,9 +798,8 @@ void CPhysicalGeometry::DistributeVolumeConnectivity(const CConfig *config,
 
         if ((nElem_Flag[iProcessor] != (int)iElem)) {
           nElem_Flag[iProcessor] = (int)iElem;
-          nElem_Send[iProcessor+1]++;
+          nElem_Send[iProcessor + 1]++;
         }
-
       }
     }
   }
@@ -850,8 +808,7 @@ void CPhysicalGeometry::DistributeVolumeConnectivity(const CConfig *config,
    all processors. After this communication, each proc knows how
    many cells it will receive from each other processor. ---*/
 
-  SU2_MPI::Alltoall(&(nElem_Send[1]), 1, MPI_INT,
-                    &(nElem_Recv[1]), 1, MPI_INT, SU2_MPI::GetComm());
+  SU2_MPI::Alltoall(&(nElem_Send[1]), 1, MPI_INT, &(nElem_Recv[1]), 1, MPI_INT, SU2_MPI::GetComm());
 
   /*--- Prepare to send connectivities. First check how many
    messages we will be sending and receiving. Here we also put
@@ -862,44 +819,40 @@ void CPhysicalGeometry::DistributeVolumeConnectivity(const CConfig *config,
   for (iProc = 0; iProc < size; iProc++) nElem_Flag[iProc] = -1;
 
   for (iProc = 0; iProc < size; iProc++) {
-    if ((iProc != rank) && (nElem_Send[iProc+1] > 0)) nSends++;
-    if ((iProc != rank) && (nElem_Recv[iProc+1] > 0)) nRecvs++;
+    if ((iProc != rank) && (nElem_Send[iProc + 1] > 0)) nSends++;
+    if ((iProc != rank) && (nElem_Recv[iProc + 1] > 0)) nRecvs++;
 
-    nElem_Send[iProc+1] += nElem_Send[iProc];
-    nElem_Recv[iProc+1] += nElem_Recv[iProc];
+    nElem_Send[iProc + 1] += nElem_Send[iProc];
+    nElem_Recv[iProc + 1] += nElem_Recv[iProc];
   }
 
   /*--- Allocate memory to hold the connectivity and element IDs
    that we are sending. ---*/
 
-  unsigned long *connSend = nullptr;
-  connSend = new unsigned long[NODES_PER_ELEMENT*nElem_Send[size]];
-  for (iSend = 0; iSend < NODES_PER_ELEMENT*nElem_Send[size]; iSend++)
-    connSend[iSend] = 0;
+  unsigned long* connSend = nullptr;
+  connSend = new unsigned long[NODES_PER_ELEMENT * nElem_Send[size]];
+  for (iSend = 0; iSend < NODES_PER_ELEMENT * nElem_Send[size]; iSend++) connSend[iSend] = 0;
 
   /*--- Allocate arrays for storing element global index. ---*/
 
-  unsigned long *idSend = new unsigned long[nElem_Send[size]];
+  unsigned long* idSend = new unsigned long[nElem_Send[size]];
   for (iSend = 0; iSend < nElem_Send[size]; iSend++) idSend[iSend] = 0;
 
   /*--- Create an index variable to keep track of our index
    position as we load up the send buffer. ---*/
 
-  unsigned long *index = new unsigned long[size];
-  for (iProc = 0; iProc < size; iProc++)
-    index[iProc] = NODES_PER_ELEMENT*nElem_Send[iProc];
+  unsigned long* index = new unsigned long[size];
+  for (iProc = 0; iProc < size; iProc++) index[iProc] = NODES_PER_ELEMENT * nElem_Send[iProc];
 
-  unsigned long *idIndex = new unsigned long[size];
-  for (iProc = 0; iProc < size; iProc++)
-    idIndex[iProc] = nElem_Send[iProc];
+  unsigned long* idIndex = new unsigned long[size];
+  for (iProc = 0; iProc < size; iProc++) idIndex[iProc] = nElem_Send[iProc];
 
   /*--- Loop through our elements and load the elems and their
    additional data that we will send to the other procs. ---*/
 
   for (iElem = 0; iElem < geometry->GetnElem(); iElem++) {
     if (geometry->elem[iElem]->GetVTK_Type() == Elem_Type) {
-      for (iNode = 0; iNode < NODES_PER_ELEMENT; iNode++ ) {
-
+      for (iNode = 0; iNode < NODES_PER_ELEMENT; iNode++) {
         /*--- Get the index of the current point. ---*/
 
         Global_Index = geometry->elem[iElem]->GetNode(iNode);
@@ -911,7 +864,6 @@ void CPhysicalGeometry::DistributeVolumeConnectivity(const CConfig *config,
         /*--- Load connectivity and IDs into the buffer for sending ---*/
 
         if (nElem_Flag[iProcessor] != (int)iElem) {
-
           nElem_Flag[iProcessor] = (int)iElem;
           unsigned long nn = index[iProcessor];
           unsigned long mm = idIndex[iProcessor];
@@ -920,7 +872,8 @@ void CPhysicalGeometry::DistributeVolumeConnectivity(const CConfig *config,
           stored directly based on their global index for the nodes.---*/
 
           for (jNode = 0; jNode < NODES_PER_ELEMENT; jNode++) {
-            connSend[nn] = geometry->elem[iElem]->GetNode(jNode); nn++;
+            connSend[nn] = geometry->elem[iElem]->GetNode(jNode);
+            nn++;
           }
 
           /*--- Global ID for this element. ---*/
@@ -931,7 +884,6 @@ void CPhysicalGeometry::DistributeVolumeConnectivity(const CConfig *config,
 
           index[iProcessor] += NODES_PER_ELEMENT;
           idIndex[iProcessor]++;
-
         }
       }
     }
@@ -939,56 +891,52 @@ void CPhysicalGeometry::DistributeVolumeConnectivity(const CConfig *config,
 
   /*--- Free memory after loading up the send buffer. ---*/
 
-  delete [] index;
-  delete [] idIndex;
+  delete[] index;
+  delete[] idIndex;
 
   /*--- Allocate the memory that we need for receiving the
    values and then cue up the non-blocking receives. Note that
    we do not include our own rank in the communications. We will
    directly copy our own data later. ---*/
 
-  unsigned long *connRecv = nullptr;
-  connRecv = new unsigned long[NODES_PER_ELEMENT*nElem_Recv[size]];
-  for (iRecv = 0; iRecv < NODES_PER_ELEMENT*nElem_Recv[size]; iRecv++)
-    connRecv[iRecv] = 0;
+  unsigned long* connRecv = nullptr;
+  connRecv = new unsigned long[NODES_PER_ELEMENT * nElem_Recv[size]];
+  for (iRecv = 0; iRecv < NODES_PER_ELEMENT * nElem_Recv[size]; iRecv++) connRecv[iRecv] = 0;
 
-  unsigned long *idRecv = new unsigned long[nElem_Recv[size]];
+  unsigned long* idRecv = new unsigned long[nElem_Recv[size]];
   for (iRecv = 0; iRecv < nElem_Recv[size]; iRecv++) idRecv[iRecv] = 0;
 
   /*--- Allocate memory for the MPI requests if we need to communicate. ---*/
 
   if (nSends > 0) {
     connSendReq = new SU2_MPI::Request[nSends];
-    idSendReq   = new SU2_MPI::Request[nSends];
+    idSendReq = new SU2_MPI::Request[nSends];
   }
   if (nRecvs > 0) {
     connRecvReq = new SU2_MPI::Request[nRecvs];
-    idRecvReq   = new SU2_MPI::Request[nRecvs];
+    idRecvReq = new SU2_MPI::Request[nRecvs];
   }
 
   /*--- Launch the non-blocking sends and receives. ---*/
 
-  InitiateCommsAll(connSend, nElem_Send, connSendReq,
-                   connRecv, nElem_Recv, connRecvReq,
-                   NODES_PER_ELEMENT, COMM_TYPE_UNSIGNED_LONG);
+  InitiateCommsAll(connSend, nElem_Send, connSendReq, connRecv, nElem_Recv, connRecvReq, NODES_PER_ELEMENT,
+                   COMM_TYPE_UNSIGNED_LONG);
 
-  InitiateCommsAll(idSend, nElem_Send, idSendReq,
-                   idRecv, nElem_Recv, idRecvReq,
-                   1, COMM_TYPE_UNSIGNED_LONG);
+  InitiateCommsAll(idSend, nElem_Send, idSendReq, idRecv, nElem_Recv, idRecvReq, 1, COMM_TYPE_UNSIGNED_LONG);
 
   /*--- Copy my own rank's data into the recv buffer directly. ---*/
 
-  iRecv   = NODES_PER_ELEMENT*nElem_Recv[rank];
-  myStart = NODES_PER_ELEMENT*nElem_Send[rank];
-  myFinal = NODES_PER_ELEMENT*nElem_Send[rank+1];
+  iRecv = NODES_PER_ELEMENT * nElem_Recv[rank];
+  myStart = NODES_PER_ELEMENT * nElem_Send[rank];
+  myFinal = NODES_PER_ELEMENT * nElem_Send[rank + 1];
   for (iSend = myStart; iSend < myFinal; iSend++) {
     connRecv[iRecv] = connSend[iSend];
     iRecv++;
   }
 
-  iRecv   = nElem_Recv[rank];
+  iRecv = nElem_Recv[rank];
   myStart = nElem_Send[rank];
-  myFinal = nElem_Send[rank+1];
+  myFinal = nElem_Send[rank + 1];
   for (iSend = myStart; iSend < myFinal; iSend++) {
     idRecv[iRecv] = idSend[iSend];
     iRecv++;
@@ -997,18 +945,19 @@ void CPhysicalGeometry::DistributeVolumeConnectivity(const CConfig *config,
   /*--- Complete the non-blocking communications. ---*/
 
   CompleteCommsAll(nSends, connSendReq, nRecvs, connRecvReq);
-  CompleteCommsAll(nSends,   idSendReq, nRecvs,   idRecvReq);
+  CompleteCommsAll(nSends, idSendReq, nRecvs, idRecvReq);
 
   /*--- Store the connectivity for this rank in the proper structure
    It will be loaded into the geometry objects in a later step. ---*/
 
   if (nElem_Recv[size] > 0) {
-    Conn_Elem = new unsigned long[NODES_PER_ELEMENT*nElem_Recv[size]];
-    int count = 0; nElem_Total = 0;
+    Conn_Elem = new unsigned long[NODES_PER_ELEMENT * nElem_Recv[size]];
+    int count = 0;
+    nElem_Total = 0;
     for (iRecv = 0; iRecv < nElem_Recv[size]; iRecv++) {
       nElem_Total++;
       for (iNode = 0; iNode < NODES_PER_ELEMENT; iNode++) {
-        Conn_Elem[count] = connRecv[iRecv*NODES_PER_ELEMENT+iNode];
+        Conn_Elem[count] = connRecv[iRecv * NODES_PER_ELEMENT + iNode];
         count++;
       }
     }
@@ -1031,42 +980,42 @@ void CPhysicalGeometry::DistributeVolumeConnectivity(const CConfig *config,
       nLocal_Tria = nElem_Total;
       if (nLocal_Tria > 0) {
         Conn_Tria = Conn_Elem;
-        ID_Tria   = ID_Elems;
+        ID_Tria = ID_Elems;
       }
       break;
     case QUADRILATERAL:
       nLocal_Quad = nElem_Total;
       if (nLocal_Quad > 0) {
         Conn_Quad = Conn_Elem;
-        ID_Quad   = ID_Elems;
+        ID_Quad = ID_Elems;
       }
       break;
     case TETRAHEDRON:
       nLocal_Tetr = nElem_Total;
       if (nLocal_Tetr > 0) {
         Conn_Tetr = Conn_Elem;
-        ID_Tetr   = ID_Elems;
+        ID_Tetr = ID_Elems;
       }
       break;
     case HEXAHEDRON:
       nLocal_Hexa = nElem_Total;
       if (nLocal_Hexa > 0) {
         Conn_Hexa = Conn_Elem;
-        ID_Hexa   = ID_Elems;
+        ID_Hexa = ID_Elems;
       }
       break;
     case PRISM:
       nLocal_Pris = nElem_Total;
       if (nLocal_Pris > 0) {
         Conn_Pris = Conn_Elem;
-        ID_Pris   = ID_Elems;
+        ID_Pris = ID_Elems;
       }
       break;
     case PYRAMID:
       nLocal_Pyra = nElem_Total;
       if (nLocal_Pyra > 0) {
         Conn_Pyra = Conn_Elem;
-        ID_Pyra   = ID_Elems;
+        ID_Pyra = ID_Elems;
       }
       break;
     default:
@@ -1076,24 +1025,22 @@ void CPhysicalGeometry::DistributeVolumeConnectivity(const CConfig *config,
 
   /*--- Free temporary memory from communications ---*/
 
-  delete [] connSendReq;
-  delete [] idSendReq;
-
-  delete [] connRecvReq;
-  delete [] idRecvReq;
+  delete[] connSendReq;
+  delete[] idSendReq;
 
-  delete [] connSend;
-  delete [] connRecv;
-  delete [] idSend;
-  delete [] idRecv;
-  delete [] nElem_Recv;
-  delete [] nElem_Send;
-  delete [] nElem_Flag;
+  delete[] connRecvReq;
+  delete[] idRecvReq;
 
+  delete[] connSend;
+  delete[] connRecv;
+  delete[] idSend;
+  delete[] idRecv;
+  delete[] nElem_Recv;
+  delete[] nElem_Send;
+  delete[] nElem_Flag;
 }
 
-void CPhysicalGeometry::DistributePoints(const CConfig *config, CGeometry *geometry) {
-
+void CPhysicalGeometry::DistributePoints(const CConfig* config, CGeometry* geometry) {
   /*--- We now know all of the coloring for our local points and neighbors.
    From this, we can communicate the owned nodes in our linear partitioning
    to all other ranks, including coordinates and coloring info, so that the
@@ -1108,14 +1055,19 @@ void CPhysicalGeometry::DistributePoints(const CConfig *config, CGeometry *geome
 
   /*--- Prepare structures for communication. ---*/
 
-  int *nPoint_Send = new int[size+1]; nPoint_Send[0] = 0;
-  int *nPoint_Recv = new int[size+1]; nPoint_Recv[0] = 0;
-  int *nPoint_Flag = new int[size];
+  int* nPoint_Send = new int[size + 1];
+  nPoint_Send[0] = 0;
+  int* nPoint_Recv = new int[size + 1];
+  nPoint_Recv[0] = 0;
+  int* nPoint_Flag = new int[size];
 
   for (iProc = 0; iProc < size; iProc++) {
-    nPoint_Send[iProc] = 0; nPoint_Recv[iProc] = 0; nPoint_Flag[iProc]= -1;
+    nPoint_Send[iProc] = 0;
+    nPoint_Recv[iProc] = 0;
+    nPoint_Flag[iProc] = -1;
   }
-  nPoint_Send[size] = 0; nPoint_Recv[size] = 0;
+  nPoint_Send[size] = 0;
+  nPoint_Recv[size] = 0;
 
   /*--- Loop over the owned points and check all the neighbors for unowned
    points. The colors of all owned points will be communicated to any ranks
@@ -1124,7 +1076,6 @@ void CPhysicalGeometry::DistributePoints(const CConfig *config, CGeometry *geome
 
   for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++) {
     for (iNeighbor = 0; iNeighbor < Neighbors[iPoint].size(); iNeighbor++) {
-
       /*--- Global ID of the neighbor ---*/
 
       jPoint = Neighbors[iPoint][iNeighbor];
@@ -1138,7 +1089,7 @@ void CPhysicalGeometry::DistributePoints(const CConfig *config, CGeometry *geome
 
       if (nPoint_Flag[iProcessor] != (int)iPoint) {
         nPoint_Flag[iProcessor] = (int)iPoint;
-        nPoint_Send[iProcessor+1]++;
+        nPoint_Send[iProcessor + 1]++;
       }
     }
   }
@@ -1147,8 +1098,7 @@ void CPhysicalGeometry::DistributePoints(const CConfig *config, CGeometry *geome
    all processors. After this communication, each proc knows how
    many points it will receive from each other processor. ---*/
 
-  SU2_MPI::Alltoall(&(nPoint_Send[1]), 1, MPI_INT,
-                    &(nPoint_Recv[1]), 1, MPI_INT, SU2_MPI::GetComm());
+  SU2_MPI::Alltoall(&(nPoint_Send[1]), 1, MPI_INT, &(nPoint_Recv[1]), 1, MPI_INT, SU2_MPI::GetComm());
 
   /*--- Prepare to send colors, ids, and coords. First check how many
    messages we will be sending and receiving. Here we also put
@@ -1159,46 +1109,42 @@ void CPhysicalGeometry::DistributePoints(const CConfig *config, CGeometry *geome
   for (iProc = 0; iProc < size; iProc++) nPoint_Flag[iProc] = -1;
 
   for (iProc = 0; iProc < size; iProc++) {
-    if ((iProc != rank) && (nPoint_Send[iProc+1] > 0)) nSends++;
-    if ((iProc != rank) && (nPoint_Recv[iProc+1] > 0)) nRecvs++;
+    if ((iProc != rank) && (nPoint_Send[iProc + 1] > 0)) nSends++;
+    if ((iProc != rank) && (nPoint_Recv[iProc + 1] > 0)) nRecvs++;
 
-    nPoint_Send[iProc+1] += nPoint_Send[iProc];
-    nPoint_Recv[iProc+1] += nPoint_Recv[iProc];
+    nPoint_Send[iProc + 1] += nPoint_Send[iProc];
+    nPoint_Recv[iProc + 1] += nPoint_Recv[iProc];
   }
 
   /*--- Allocate arrays for sending the global ID. ---*/
 
-  unsigned long *idSend = new unsigned long[nPoint_Send[size]];
+  unsigned long* idSend = new unsigned long[nPoint_Send[size]];
   for (iSend = 0; iSend < nPoint_Send[size]; iSend++) idSend[iSend] = 0;
 
   /*--- Allocate memory to hold the colors that we are sending. ---*/
 
-  unsigned long *colorSend = new unsigned long[nPoint_Send[size]];
+  unsigned long* colorSend = new unsigned long[nPoint_Send[size]];
   for (iSend = 0; iSend < nPoint_Send[size]; iSend++) colorSend[iSend] = 0;
 
   /*--- Allocate memory to hold the coordinates that we are sending. ---*/
 
-  su2double *coordSend = nullptr;
-  coordSend = new su2double[nDim*nPoint_Send[size]];
-  for (iSend = 0; iSend < nDim*nPoint_Send[size]; iSend++)
-    coordSend[iSend] = 0;
+  su2double* coordSend = nullptr;
+  coordSend = new su2double[nDim * nPoint_Send[size]];
+  for (iSend = 0; iSend < nDim * nPoint_Send[size]; iSend++) coordSend[iSend] = 0;
 
   /*--- Create index variables to keep track of our index
    positions as we load up the send buffer. ---*/
 
-  unsigned long *index = new unsigned long[size];
-  for (iProc = 0; iProc < size; iProc++)
-    index[iProc] = nPoint_Send[iProc];
+  unsigned long* index = new unsigned long[size];
+  for (iProc = 0; iProc < size; iProc++) index[iProc] = nPoint_Send[iProc];
 
-  unsigned long *coordIndex = new unsigned long[size];
-  for (iProc = 0; iProc < size; iProc++)
-    coordIndex[iProc] = nDim*nPoint_Send[iProc];
+  unsigned long* coordIndex = new unsigned long[size];
+  for (iProc = 0; iProc < size; iProc++) coordIndex[iProc] = nDim * nPoint_Send[iProc];
 
   /*--- Now load up our buffers with the colors, ids, and coords. ---*/
 
   for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++) {
     for (iNeighbor = 0; iNeighbor < Neighbors[iPoint].size(); iNeighbor++) {
-
       /*--- Global ID of the neighbor ---*/
 
       jPoint = Neighbors[iPoint][iNeighbor];
@@ -1211,94 +1157,84 @@ void CPhysicalGeometry::DistributePoints(const CConfig *config, CGeometry *geome
        counters and load up the colors, ids, and coords. ---*/
 
       if (nPoint_Flag[iProcessor] != (int)iPoint) {
-
         nPoint_Flag[iProcessor] = (int)iPoint;
         unsigned long nn = index[iProcessor];
 
         /*--- Load the global ID, color, and coordinate values. ---*/
 
-        idSend[nn]    = geometry->nodes->GetGlobalIndex(iPoint);
+        idSend[nn] = geometry->nodes->GetGlobalIndex(iPoint);
         colorSend[nn] = geometry->nodes->GetColor(iPoint);
 
         nn = coordIndex[iProcessor];
-        for (iDim  = 0; iDim < nDim; iDim++) {
-          coordSend[nn] = geometry->nodes->GetCoord(iPoint, iDim); nn++;
+        for (iDim = 0; iDim < nDim; iDim++) {
+          coordSend[nn] = geometry->nodes->GetCoord(iPoint, iDim);
+          nn++;
         }
 
         /*--- Increment the index by the message length ---*/
 
         coordIndex[iProcessor] += nDim;
         index[iProcessor]++;
-
       }
     }
   }
 
   /*--- Free memory after loading up the send buffer. ---*/
 
-  delete [] index;
-  delete [] coordIndex;
+  delete[] index;
+  delete[] coordIndex;
 
   /*--- Allocate the memory that we need for receiving the
    values and then cue up the non-blocking receives. Note that
    we do not include our own rank in the communications. We will
    directly copy our own data later. ---*/
 
-  unsigned long *colorRecv = new unsigned long[nPoint_Recv[size]];
-  for (iRecv = 0; iRecv < nPoint_Recv[size]; iRecv++)
-    colorRecv[iRecv] = 0;
+  unsigned long* colorRecv = new unsigned long[nPoint_Recv[size]];
+  for (iRecv = 0; iRecv < nPoint_Recv[size]; iRecv++) colorRecv[iRecv] = 0;
 
-  unsigned long *idRecv = new unsigned long[nPoint_Recv[size]];
-  for (iRecv = 0; iRecv < nPoint_Recv[size]; iRecv++)
-    idRecv[iRecv] = 0;
+  unsigned long* idRecv = new unsigned long[nPoint_Recv[size]];
+  for (iRecv = 0; iRecv < nPoint_Recv[size]; iRecv++) idRecv[iRecv] = 0;
 
-  su2double *coordRecv = nullptr;
-  coordRecv = new su2double[nDim*nPoint_Recv[size]];
-  for (iRecv = 0; iRecv < nDim*nPoint_Recv[size]; iRecv++)
-    coordRecv[iRecv] = 0;
+  su2double* coordRecv = nullptr;
+  coordRecv = new su2double[nDim * nPoint_Recv[size]];
+  for (iRecv = 0; iRecv < nDim * nPoint_Recv[size]; iRecv++) coordRecv[iRecv] = 0;
 
   /*--- Allocate memory for the MPI requests if we need to communicate. ---*/
 
   if (nSends > 0) {
     colorSendReq = new SU2_MPI::Request[nSends];
-    idSendReq    = new SU2_MPI::Request[nSends];
+    idSendReq = new SU2_MPI::Request[nSends];
     coordSendReq = new SU2_MPI::Request[nSends];
-
   }
   if (nRecvs > 0) {
     colorRecvReq = new SU2_MPI::Request[nRecvs];
-    idRecvReq    = new SU2_MPI::Request[nRecvs];
+    idRecvReq = new SU2_MPI::Request[nRecvs];
     coordRecvReq = new SU2_MPI::Request[nRecvs];
   }
 
   /*--- Launch the non-blocking sends and receives. ---*/
 
-  InitiateCommsAll(colorSend, nPoint_Send, colorSendReq,
-                   colorRecv, nPoint_Recv, colorRecvReq,
-                   1, COMM_TYPE_UNSIGNED_LONG);
+  InitiateCommsAll(colorSend, nPoint_Send, colorSendReq, colorRecv, nPoint_Recv, colorRecvReq, 1,
+                   COMM_TYPE_UNSIGNED_LONG);
 
-  InitiateCommsAll(idSend, nPoint_Send, idSendReq,
-                   idRecv, nPoint_Recv, idRecvReq,
-                   1, COMM_TYPE_UNSIGNED_LONG);
+  InitiateCommsAll(idSend, nPoint_Send, idSendReq, idRecv, nPoint_Recv, idRecvReq, 1, COMM_TYPE_UNSIGNED_LONG);
 
-  InitiateCommsAll(coordSend, nPoint_Send, coordSendReq,
-                   coordRecv, nPoint_Recv, coordRecvReq,
-                   nDim, COMM_TYPE_DOUBLE);
+  InitiateCommsAll(coordSend, nPoint_Send, coordSendReq, coordRecv, nPoint_Recv, coordRecvReq, nDim, COMM_TYPE_DOUBLE);
 
   /*--- Copy my own rank's data into the recv buffer directly. ---*/
 
-  iRecv   = nPoint_Recv[rank];
+  iRecv = nPoint_Recv[rank];
   myStart = nPoint_Send[rank];
-  myFinal = nPoint_Send[rank+1];
+  myFinal = nPoint_Send[rank + 1];
   for (iSend = myStart; iSend < myFinal; iSend++) {
     colorRecv[iRecv] = colorSend[iSend];
-    idRecv[iRecv]    = idSend[iSend];
+    idRecv[iRecv] = idSend[iSend];
     iRecv++;
   }
 
-  iRecv   = nDim*nPoint_Recv[rank];
-  myStart = nDim*nPoint_Send[rank];
-  myFinal = nDim*nPoint_Send[rank+1];
+  iRecv = nDim * nPoint_Recv[rank];
+  myStart = nDim * nPoint_Send[rank];
+  myFinal = nDim * nPoint_Send[rank + 1];
   for (iSend = myStart; iSend < myFinal; iSend++) {
     coordRecv[iRecv] = coordSend[iSend];
     iRecv++;
@@ -1307,7 +1243,7 @@ void CPhysicalGeometry::DistributePoints(const CConfig *config, CGeometry *geome
   /*--- Complete the non-blocking communications. ---*/
 
   CompleteCommsAll(nSends, colorSendReq, nRecvs, colorRecvReq);
-  CompleteCommsAll(nSends,    idSendReq, nRecvs,    idRecvReq);
+  CompleteCommsAll(nSends, idSendReq, nRecvs, idRecvReq);
   CompleteCommsAll(nSends, coordSendReq, nRecvs, coordRecvReq);
 
   /*--- Store the total number of local points my rank has for
@@ -1320,44 +1256,42 @@ void CPhysicalGeometry::DistributePoints(const CConfig *config, CGeometry *geome
 
   Local_Points = new unsigned long[nPoint_Recv[size]];
   Local_Colors = new unsigned long[nPoint_Recv[size]];
-  Local_Coords = new su2double[nDim*nPoint_Recv[size]];
+  Local_Coords = new su2double[nDim * nPoint_Recv[size]];
 
-  nLocal_PointDomain = 0; nLocal_PointGhost = 0;
+  nLocal_PointDomain = 0;
+  nLocal_PointGhost = 0;
   for (iRecv = 0; iRecv < nPoint_Recv[size]; iRecv++) {
     Local_Points[iRecv] = idRecv[iRecv];
     Local_Colors[iRecv] = colorRecv[iRecv];
-    for (iDim = 0; iDim < nDim; iDim++)
-      Local_Coords[iRecv*nDim+iDim] = coordRecv[iRecv*nDim+iDim];
-    if (Local_Colors[iRecv] == (unsigned long)rank) nLocal_PointDomain++;
-    else nLocal_PointGhost++;
+    for (iDim = 0; iDim < nDim; iDim++) Local_Coords[iRecv * nDim + iDim] = coordRecv[iRecv * nDim + iDim];
+    if (Local_Colors[iRecv] == (unsigned long)rank)
+      nLocal_PointDomain++;
+    else
+      nLocal_PointGhost++;
   }
 
   /*--- Free temporary memory from communications ---*/
 
-  delete [] colorSendReq;
-  delete [] idSendReq;
-  delete [] coordSendReq;
-
-  delete [] colorRecvReq;
-  delete [] idRecvReq;
-  delete [] coordRecvReq;
-
-  delete [] colorSend;
-  delete [] colorRecv;
-  delete [] idSend;
-  delete [] idRecv;
-  delete [] coordSend;
-  delete [] coordRecv;
-  delete [] nPoint_Recv;
-  delete [] nPoint_Send;
-  delete [] nPoint_Flag;
-
+  delete[] colorSendReq;
+  delete[] idSendReq;
+  delete[] coordSendReq;
+
+  delete[] colorRecvReq;
+  delete[] idRecvReq;
+  delete[] coordRecvReq;
+
+  delete[] colorSend;
+  delete[] colorRecv;
+  delete[] idSend;
+  delete[] idRecv;
+  delete[] coordSend;
+  delete[] coordRecv;
+  delete[] nPoint_Recv;
+  delete[] nPoint_Send;
+  delete[] nPoint_Flag;
 }
 
-void CPhysicalGeometry::PartitionSurfaceConnectivity(CConfig *config,
-                                                     CGeometry *geometry,
-                                                     unsigned short Elem_Type) {
-
+void CPhysicalGeometry::PartitionSurfaceConnectivity(CConfig* config, CGeometry* geometry, unsigned short Elem_Type) {
   /*--- We begin with all marker information residing on the master rank,
    as the master currently stores all marker info when reading the grid.
    We first check and communicate basic information that each rank will
@@ -1374,9 +1308,9 @@ void CPhysicalGeometry::PartitionSurfaceConnectivity(CConfig *config,
   unsigned long iMarker, iProcessor, iElem, iNode, jNode;
   unsigned long nElem_Total = 0, Global_Index, Global_Elem_Index;
 
-  unsigned long *Conn_Elem      = nullptr;
-  unsigned long *Linear_Markers = nullptr;
-  unsigned long *ID_SurfElem    = nullptr;
+  unsigned long* Conn_Elem = nullptr;
+  unsigned long* Linear_Markers = nullptr;
+  unsigned long* ID_SurfElem = nullptr;
 
   SU2_MPI::Request *connSendReq = nullptr, *markerSendReq = nullptr, *idSendReq = nullptr;
   SU2_MPI::Request *connRecvReq = nullptr, *markerRecvReq = nullptr, *idRecvReq = nullptr;
@@ -1402,33 +1336,34 @@ void CPhysicalGeometry::PartitionSurfaceConnectivity(CConfig *config,
       break;
   }
 
-  int *nElem_Send = new int[size+1]; nElem_Send[0] = 0;
-  int *nElem_Recv = new int[size+1]; nElem_Recv[0] = 0;
-  int *nElem_Flag = new int[size];
+  int* nElem_Send = new int[size + 1];
+  nElem_Send[0] = 0;
+  int* nElem_Recv = new int[size + 1];
+  nElem_Recv[0] = 0;
+  int* nElem_Flag = new int[size];
 
   for (iProc = 0; iProc < size; iProc++) {
-    nElem_Send[iProc] = 0; nElem_Recv[iProc] = 0; nElem_Flag[iProc]= -1;
+    nElem_Send[iProc] = 0;
+    nElem_Recv[iProc] = 0;
+    nElem_Flag[iProc] = -1;
   }
-  nElem_Send[size] = 0; nElem_Recv[size] = 0;
+  nElem_Send[size] = 0;
+  nElem_Recv[size] = 0;
 
   /*--- We know that the master owns all of the info and will be the only
    rank sending anything, although all ranks might receive something. ---*/
 
   if (rank == MASTER_NODE) {
     for (iMarker = 0; iMarker < geometry->GetnMarker(); iMarker++) {
-
       /*--- Reset the flag in between markers, just to ensure that we
        don't miss some elements on different markers with the same local
        index. ---*/
 
-      for (iProc = 0; iProc < size; iProc++) nElem_Flag[iProc]= -1;
+      for (iProc = 0; iProc < size; iProc++) nElem_Flag[iProc] = -1;
 
       for (iElem = 0; iElem < geometry->GetnElem_Bound(iMarker); iElem++) {
-
         if (geometry->bound[iMarker][iElem]->GetVTK_Type() == Elem_Type) {
-
-          for (iNode = 0; iNode < NODES_PER_ELEMENT; iNode++ ) {
-
+          for (iNode = 0; iNode < NODES_PER_ELEMENT; iNode++) {
             /*--- Get the index of the current point (stored as global). ---*/
 
             Global_Index = geometry->bound[iMarker][iElem]->GetNode(iNode);
@@ -1442,7 +1377,7 @@ void CPhysicalGeometry::PartitionSurfaceConnectivity(CConfig *config,
 
             if ((nElem_Flag[iProcessor] != (int)iElem)) {
               nElem_Flag[iProcessor] = (int)iElem;
-              nElem_Send[iProcessor+1]++;
+              nElem_Send[iProcessor + 1]++;
             }
           }
         }
@@ -1454,8 +1389,7 @@ void CPhysicalGeometry::PartitionSurfaceConnectivity(CConfig *config,
    all processors. After this communication, each proc knows how
    many cells it will receive from each other processor. ---*/
 
-  SU2_MPI::Scatter(&(nElem_Send[1]), 1, MPI_INT,
-                   &(nElem_Recv[1]), 1, MPI_INT, MASTER_NODE, SU2_MPI::GetComm());
+  SU2_MPI::Scatter(&(nElem_Send[1]), 1, MPI_INT, &(nElem_Recv[1]), 1, MPI_INT, MASTER_NODE, SU2_MPI::GetComm());
 
   /*--- Prepare to send connectivities. First check how many
    messages we will be sending and receiving. Here we also put
@@ -1466,60 +1400,52 @@ void CPhysicalGeometry::PartitionSurfaceConnectivity(CConfig *config,
   for (iProc = 0; iProc < size; iProc++) nElem_Flag[iProc] = -1;
 
   for (iProc = 0; iProc < size; iProc++) {
-    if ((iProc != rank) && (nElem_Send[iProc+1] > 0)) nSends++;
-    if ((iProc != rank) && (nElem_Recv[iProc+1] > 0)) nRecvs++;
+    if ((iProc != rank) && (nElem_Send[iProc + 1] > 0)) nSends++;
+    if ((iProc != rank) && (nElem_Recv[iProc + 1] > 0)) nRecvs++;
 
-    nElem_Send[iProc+1] += nElem_Send[iProc];
-    nElem_Recv[iProc+1] += nElem_Recv[iProc];
+    nElem_Send[iProc + 1] += nElem_Send[iProc];
+    nElem_Recv[iProc + 1] += nElem_Recv[iProc];
   }
 
   /*--- Allocate memory to hold the connectivity that we are sending. ---*/
 
-  unsigned long *connSend   = nullptr;
-  unsigned long *markerSend = nullptr;
-  unsigned long *idSend     = nullptr;
+  unsigned long* connSend = nullptr;
+  unsigned long* markerSend = nullptr;
+  unsigned long* idSend = nullptr;
 
   if (rank == MASTER_NODE) {
-
-    connSend = new unsigned long[NODES_PER_ELEMENT*nElem_Send[size]];
-    for (iSend = 0; iSend < NODES_PER_ELEMENT*nElem_Send[size]; iSend++)
-      connSend[iSend] = 0;
+    connSend = new unsigned long[NODES_PER_ELEMENT * nElem_Send[size]];
+    for (iSend = 0; iSend < NODES_PER_ELEMENT * nElem_Send[size]; iSend++) connSend[iSend] = 0;
 
     markerSend = new unsigned long[nElem_Send[size]];
-    for (iSend = 0; iSend < nElem_Send[size]; iSend++)
-      markerSend[iSend] = 0;
+    for (iSend = 0; iSend < nElem_Send[size]; iSend++) markerSend[iSend] = 0;
 
     idSend = new unsigned long[nElem_Send[size]];
-    for (iSend = 0; iSend < nElem_Send[size]; iSend++)
-      idSend[iSend] = 0;
+    for (iSend = 0; iSend < nElem_Send[size]; iSend++) idSend[iSend] = 0;
 
     /*--- Create an index variable to keep track of our index
      position as we load up the send buffer. ---*/
 
-    unsigned long *index = new unsigned long[size];
-    for (iProc = 0; iProc < size; iProc++)
-      index[iProc] = NODES_PER_ELEMENT*nElem_Send[iProc];
+    unsigned long* index = new unsigned long[size];
+    for (iProc = 0; iProc < size; iProc++) index[iProc] = NODES_PER_ELEMENT * nElem_Send[iProc];
 
-    unsigned long *markerIndex = new unsigned long[size];
-    for (iProc = 0; iProc < size; iProc++)
-      markerIndex[iProc] = nElem_Send[iProc];
+    unsigned long* markerIndex = new unsigned long[size];
+    for (iProc = 0; iProc < size; iProc++) markerIndex[iProc] = nElem_Send[iProc];
 
     /*--- Loop through our elements and load the elems and their
      additional data that we will send to the other procs. ---*/
 
     Global_Elem_Index = 0;
     for (iMarker = 0; iMarker < geometry->GetnMarker(); iMarker++) {
-
       /*--- Reset the flag in between markers, just to ensure that we
        don't miss some elements on different markers with the same local
        index. ---*/
 
-      for (iProc = 0; iProc < size; iProc++) nElem_Flag[iProc]= -1;
+      for (iProc = 0; iProc < size; iProc++) nElem_Flag[iProc] = -1;
 
       for (iElem = 0; iElem < geometry->GetnElem_Bound(iMarker); iElem++) {
         if (geometry->bound[iMarker][iElem]->GetVTK_Type() == Elem_Type) {
-          for (iNode = 0; iNode < NODES_PER_ELEMENT; iNode++ ) {
-
+          for (iNode = 0; iNode < NODES_PER_ELEMENT; iNode++) {
             /*--- Get the index of the current point. ---*/
 
             Global_Index = geometry->bound[iMarker][iElem]->GetNode(iNode);
@@ -1531,7 +1457,6 @@ void CPhysicalGeometry::PartitionSurfaceConnectivity(CConfig *config,
             /*--- Load connectivity into the buffer for sending ---*/
 
             if ((nElem_Flag[iProcessor] != (int)iElem)) {
-
               nElem_Flag[iProcessor] = (int)iElem;
               unsigned long nn = index[iProcessor];
               unsigned long mm = markerIndex[iProcessor];
@@ -1546,27 +1471,24 @@ void CPhysicalGeometry::PartitionSurfaceConnectivity(CConfig *config,
               /*--- Store the marker index and surface elem global ID ---*/
 
               markerSend[mm] = iMarker;
-              idSend[mm]     = Global_Elem_Index;
+              idSend[mm] = Global_Elem_Index;
 
               /*--- Increment the index by the message length ---*/
 
               index[iProcessor] += NODES_PER_ELEMENT;
               markerIndex[iProcessor]++;
             }
-
           }
         }
 
         Global_Elem_Index++;
-
       }
     }
 
     /*--- Free memory after loading up the send buffer. ---*/
 
-    delete [] index;
-    delete [] markerIndex;
-
+    delete[] index;
+    delete[] markerIndex;
   }
 
   /*--- Allocate the memory that we need for receiving the conn
@@ -1574,86 +1496,78 @@ void CPhysicalGeometry::PartitionSurfaceConnectivity(CConfig *config,
    we do not include our own rank in the communications. We will
    directly copy our own data later. ---*/
 
-  unsigned long *connRecv = nullptr;
-  connRecv = new unsigned long[NODES_PER_ELEMENT*nElem_Recv[size]];
-  for (iRecv = 0; iRecv < NODES_PER_ELEMENT*nElem_Recv[size]; iRecv++)
-    connRecv[iRecv] = 0;
+  unsigned long* connRecv = nullptr;
+  connRecv = new unsigned long[NODES_PER_ELEMENT * nElem_Recv[size]];
+  for (iRecv = 0; iRecv < NODES_PER_ELEMENT * nElem_Recv[size]; iRecv++) connRecv[iRecv] = 0;
 
-  unsigned long *markerRecv = new unsigned long[nElem_Recv[size]];
-  for (iRecv = 0; iRecv < nElem_Recv[size]; iRecv++)
-    markerRecv[iRecv] = 0;
+  unsigned long* markerRecv = new unsigned long[nElem_Recv[size]];
+  for (iRecv = 0; iRecv < nElem_Recv[size]; iRecv++) markerRecv[iRecv] = 0;
 
-  unsigned long *idRecv = new unsigned long[nElem_Recv[size]];
-  for (iRecv = 0; iRecv < nElem_Recv[size]; iRecv++)
-    idRecv[iRecv] = 0;
+  unsigned long* idRecv = new unsigned long[nElem_Recv[size]];
+  for (iRecv = 0; iRecv < nElem_Recv[size]; iRecv++) idRecv[iRecv] = 0;
 
   /*--- Allocate memory for the MPI requests if we need to communicate. ---*/
 
   if (nSends > 0) {
-    connSendReq   = new SU2_MPI::Request[nSends];
+    connSendReq = new SU2_MPI::Request[nSends];
     markerSendReq = new SU2_MPI::Request[nSends];
-    idSendReq     = new SU2_MPI::Request[nSends];
+    idSendReq = new SU2_MPI::Request[nSends];
   }
   if (nRecvs > 0) {
-    connRecvReq   = new SU2_MPI::Request[nRecvs];
+    connRecvReq = new SU2_MPI::Request[nRecvs];
     markerRecvReq = new SU2_MPI::Request[nRecvs];
-    idRecvReq     = new SU2_MPI::Request[nRecvs];
+    idRecvReq = new SU2_MPI::Request[nRecvs];
   }
 
   /*--- Launch the non-blocking sends and receives. ---*/
 
-  InitiateCommsAll(connSend, nElem_Send, connSendReq,
-                   connRecv, nElem_Recv, connRecvReq,
-                   NODES_PER_ELEMENT, COMM_TYPE_UNSIGNED_LONG);
+  InitiateCommsAll(connSend, nElem_Send, connSendReq, connRecv, nElem_Recv, connRecvReq, NODES_PER_ELEMENT,
+                   COMM_TYPE_UNSIGNED_LONG);
 
-  InitiateCommsAll(markerSend, nElem_Send, markerSendReq,
-                   markerRecv, nElem_Recv, markerRecvReq,
-                   1, COMM_TYPE_UNSIGNED_LONG);
+  InitiateCommsAll(markerSend, nElem_Send, markerSendReq, markerRecv, nElem_Recv, markerRecvReq, 1,
+                   COMM_TYPE_UNSIGNED_LONG);
 
-  InitiateCommsAll(idSend, nElem_Send, idSendReq,
-                   idRecv, nElem_Recv, idRecvReq,
-                   1, COMM_TYPE_UNSIGNED_LONG);
+  InitiateCommsAll(idSend, nElem_Send, idSendReq, idRecv, nElem_Recv, idRecvReq, 1, COMM_TYPE_UNSIGNED_LONG);
 
   /*--- Copy my own rank's data into the recv buffer directly. ---*/
 
   if (rank == MASTER_NODE) {
-
-    iRecv   = NODES_PER_ELEMENT*nElem_Recv[rank];
-    myStart = NODES_PER_ELEMENT*nElem_Send[rank];
-    myFinal = NODES_PER_ELEMENT*nElem_Send[rank+1];
+    iRecv = NODES_PER_ELEMENT * nElem_Recv[rank];
+    myStart = NODES_PER_ELEMENT * nElem_Send[rank];
+    myFinal = NODES_PER_ELEMENT * nElem_Send[rank + 1];
     for (iSend = myStart; iSend < myFinal; iSend++) {
       connRecv[iRecv] = connSend[iSend];
       iRecv++;
     }
 
-    iRecv   = nElem_Recv[rank];
+    iRecv = nElem_Recv[rank];
     myStart = nElem_Send[rank];
-    myFinal = nElem_Send[rank+1];
+    myFinal = nElem_Send[rank + 1];
     for (iSend = myStart; iSend < myFinal; iSend++) {
       markerRecv[iRecv] = markerSend[iSend];
-      idRecv[iRecv]     = idSend[iSend];
+      idRecv[iRecv] = idSend[iSend];
       iRecv++;
     }
-
   }
 
   /*--- Complete the non-blocking communications. ---*/
 
-  CompleteCommsAll(nSends,   connSendReq, nRecvs,   connRecvReq);
+  CompleteCommsAll(nSends, connSendReq, nRecvs, connRecvReq);
   CompleteCommsAll(nSends, markerSendReq, nRecvs, markerRecvReq);
-  CompleteCommsAll(nSends,     idSendReq, nRecvs,     idRecvReq);
+  CompleteCommsAll(nSends, idSendReq, nRecvs, idRecvReq);
 
   /*--- Store the connectivity for this rank in the proper data
    structure before post-processing below. First, allocate
    appropriate amount of memory for this section. ---*/
 
   if (nElem_Recv[size] > 0) {
-    Conn_Elem = new unsigned long[NODES_PER_ELEMENT*nElem_Recv[size]];
-    int count = 0; nElem_Total = 0;
+    Conn_Elem = new unsigned long[NODES_PER_ELEMENT * nElem_Recv[size]];
+    int count = 0;
+    nElem_Total = 0;
     for (iRecv = 0; iRecv < nElem_Recv[size]; iRecv++) {
       nElem_Total++;
       for (iNode = 0; iNode < NODES_PER_ELEMENT; iNode++) {
-        Conn_Elem[count] = connRecv[iRecv*NODES_PER_ELEMENT+iNode];
+        Conn_Elem[count] = connRecv[iRecv * NODES_PER_ELEMENT + iNode];
         count++;
       }
     }
@@ -1684,24 +1598,24 @@ void CPhysicalGeometry::PartitionSurfaceConnectivity(CConfig *config,
     case LINE:
       nLinear_Line = nElem_Total;
       if (nLinear_Line > 0) {
-        Conn_Line_Linear    = Conn_Elem;
-        ID_Line_Linear      = Linear_Markers;
+        Conn_Line_Linear = Conn_Elem;
+        ID_Line_Linear = Linear_Markers;
         Elem_ID_Line_Linear = ID_SurfElem;
       }
       break;
     case TRIANGLE:
       nLinear_BoundTria = nElem_Total;
       if (nLinear_BoundTria > 0) {
-        Conn_BoundTria_Linear    = Conn_Elem;
-        ID_BoundTria_Linear      = Linear_Markers;
+        Conn_BoundTria_Linear = Conn_Elem;
+        ID_BoundTria_Linear = Linear_Markers;
         Elem_ID_BoundTria_Linear = ID_SurfElem;
       }
       break;
     case QUADRILATERAL:
       nLinear_BoundQuad = nElem_Total;
       if (nLinear_BoundQuad > 0) {
-        Conn_BoundQuad_Linear    = Conn_Elem;
-        ID_BoundQuad_Linear      = Linear_Markers;
+        Conn_BoundQuad_Linear = Conn_Elem;
+        ID_BoundQuad_Linear = Linear_Markers;
         Elem_ID_BoundQuad_Linear = ID_SurfElem;
       }
       break;
@@ -1712,46 +1626,42 @@ void CPhysicalGeometry::PartitionSurfaceConnectivity(CConfig *config,
 
   /*--- Free temporary memory from communications ---*/
 
-  delete [] connSendReq;
-  delete [] markerSendReq;
-  delete [] idSendReq;
-
-  delete [] connRecvReq;
-  delete [] markerRecvReq;
-  delete [] idRecvReq;
+  delete[] connSendReq;
+  delete[] markerSendReq;
+  delete[] idSendReq;
 
-  delete [] connSend;
-  delete [] markerSend;
-  delete [] idSend;
+  delete[] connRecvReq;
+  delete[] markerRecvReq;
+  delete[] idRecvReq;
 
-  delete [] connRecv;
-  delete [] markerRecv;
-  delete [] idRecv;
+  delete[] connSend;
+  delete[] markerSend;
+  delete[] idSend;
 
-  delete [] nElem_Recv;
-  delete [] nElem_Send;
-  delete [] nElem_Flag;
+  delete[] connRecv;
+  delete[] markerRecv;
+  delete[] idRecv;
 
+  delete[] nElem_Recv;
+  delete[] nElem_Send;
+  delete[] nElem_Flag;
 }
 
-void CPhysicalGeometry::DistributeSurfaceConnectivity(CConfig *config,
-                                                      CGeometry *geometry,
-                                                      unsigned short Elem_Type) {
-
+void CPhysicalGeometry::DistributeSurfaceConnectivity(CConfig* config, CGeometry* geometry, unsigned short Elem_Type) {
   unsigned short NODES_PER_ELEMENT = 0;
 
   unsigned long iProcessor, NELEM = 0;
   unsigned long iElem, iNode, jNode, nElem_Total = 0, Global_Index;
 
-  unsigned long *Conn_Linear        = nullptr;
-  unsigned long *Conn_Elem          = nullptr;
-  unsigned long *Linear_Markers     = nullptr;
-  unsigned long *ID_SurfElem_Linear = nullptr;
-  unsigned long *Local_Markers      = nullptr;
-  unsigned long *ID_SurfElem        = nullptr;
+  unsigned long* Conn_Linear = nullptr;
+  unsigned long* Conn_Elem = nullptr;
+  unsigned long* Linear_Markers = nullptr;
+  unsigned long* ID_SurfElem_Linear = nullptr;
+  unsigned long* Local_Markers = nullptr;
+  unsigned long* ID_SurfElem = nullptr;
 
-  SU2_MPI::Request *connSendReq = nullptr,*markerSendReq = nullptr,*idSendReq = nullptr;
-  SU2_MPI::Request *connRecvReq = nullptr,*markerRecvReq = nullptr,*idRecvReq = nullptr;
+  SU2_MPI::Request *connSendReq = nullptr, *markerSendReq = nullptr, *idSendReq = nullptr;
+  SU2_MPI::Request *connRecvReq = nullptr, *markerRecvReq = nullptr, *idRecvReq = nullptr;
   int iProc, iSend, iRecv, myStart, myFinal;
 
   /*--- Store the local number of this element type and the number of nodes
@@ -1761,24 +1671,24 @@ void CPhysicalGeometry::DistributeSurfaceConnectivity(CConfig *config,
 
   switch (Elem_Type) {
     case LINE:
-      NELEM              = nLinear_Line;
-      NODES_PER_ELEMENT  = N_POINTS_LINE;
-      Conn_Linear        = Conn_Line_Linear;
-      Linear_Markers     = ID_Line_Linear;
+      NELEM = nLinear_Line;
+      NODES_PER_ELEMENT = N_POINTS_LINE;
+      Conn_Linear = Conn_Line_Linear;
+      Linear_Markers = ID_Line_Linear;
       ID_SurfElem_Linear = Elem_ID_Line_Linear;
       break;
     case TRIANGLE:
-      NELEM              = nLinear_BoundTria;
-      NODES_PER_ELEMENT  = N_POINTS_TRIANGLE;
-      Conn_Linear        = Conn_BoundTria_Linear;
-      Linear_Markers     = ID_BoundTria_Linear;
+      NELEM = nLinear_BoundTria;
+      NODES_PER_ELEMENT = N_POINTS_TRIANGLE;
+      Conn_Linear = Conn_BoundTria_Linear;
+      Linear_Markers = ID_BoundTria_Linear;
       ID_SurfElem_Linear = Elem_ID_BoundTria_Linear;
       break;
     case QUADRILATERAL:
-      NELEM              = nLinear_BoundQuad;
-      NODES_PER_ELEMENT  = N_POINTS_QUADRILATERAL;
-      Conn_Linear        = Conn_BoundQuad_Linear;
-      Linear_Markers     = ID_BoundQuad_Linear;
+      NELEM = nLinear_BoundQuad;
+      NODES_PER_ELEMENT = N_POINTS_QUADRILATERAL;
+      Conn_Linear = Conn_BoundQuad_Linear;
+      Linear_Markers = ID_BoundQuad_Linear;
       ID_SurfElem_Linear = Elem_ID_BoundQuad_Linear;
       break;
     default:
@@ -1791,21 +1701,25 @@ void CPhysicalGeometry::DistributeSurfaceConnectivity(CConfig *config,
    and decide how many elements we must send to each other rank in order to
    have all elements distributed according to the ParMETIS coloring. ---*/
 
-  int *nElem_Send = new int[size+1]; nElem_Send[0] = 0;
-  int *nElem_Recv = new int[size+1]; nElem_Recv[0] = 0;
-  int *nElem_Flag = new int[size];
+  int* nElem_Send = new int[size + 1];
+  nElem_Send[0] = 0;
+  int* nElem_Recv = new int[size + 1];
+  nElem_Recv[0] = 0;
+  int* nElem_Flag = new int[size];
 
   for (iProc = 0; iProc < size; iProc++) {
-    nElem_Send[iProc] = 0; nElem_Recv[iProc] = 0; nElem_Flag[iProc]= -1;
+    nElem_Send[iProc] = 0;
+    nElem_Recv[iProc] = 0;
+    nElem_Flag[iProc] = -1;
   }
-  nElem_Send[size] = 0; nElem_Recv[size] = 0;
+  nElem_Send[size] = 0;
+  nElem_Recv[size] = 0;
 
   for (iElem = 0; iElem < NELEM; iElem++) {
     for (iNode = 0; iNode < NODES_PER_ELEMENT; iNode++) {
-
       /*--- Get the index of the current point. ---*/
 
-      Global_Index = Conn_Linear[iElem*NODES_PER_ELEMENT+iNode];
+      Global_Index = Conn_Linear[iElem * NODES_PER_ELEMENT + iNode];
 
       /*--- We have the color stored in a map for all local points. ---*/
 
@@ -1816,9 +1730,8 @@ void CPhysicalGeometry::DistributeSurfaceConnectivity(CConfig *config,
 
       if ((nElem_Flag[iProcessor] != (int)iElem)) {
         nElem_Flag[iProcessor] = (int)iElem;
-        nElem_Send[iProcessor+1]++;
+        nElem_Send[iProcessor + 1]++;
       }
-
     }
   }
 
@@ -1826,8 +1739,7 @@ void CPhysicalGeometry::DistributeSurfaceConnectivity(CConfig *config,
    all processors. After this communication, each proc knows how
    many cells it will receive from each other processor. ---*/
 
-  SU2_MPI::Alltoall(&(nElem_Send[1]), 1, MPI_INT,
-                    &(nElem_Recv[1]), 1, MPI_INT, SU2_MPI::GetComm());
+  SU2_MPI::Alltoall(&(nElem_Send[1]), 1, MPI_INT, &(nElem_Recv[1]), 1, MPI_INT, SU2_MPI::GetComm());
 
   /*--- Prepare to send connectivities. First check how many
    messages we will be sending and receiving. Here we also put
@@ -1838,49 +1750,45 @@ void CPhysicalGeometry::DistributeSurfaceConnectivity(CConfig *config,
   for (iProc = 0; iProc < size; iProc++) nElem_Flag[iProc] = -1;
 
   for (iProc = 0; iProc < size; iProc++) {
-    if ((iProc != rank) && (nElem_Send[iProc+1] > 0)) nSends++;
-    if ((iProc != rank) && (nElem_Recv[iProc+1] > 0)) nRecvs++;
+    if ((iProc != rank) && (nElem_Send[iProc + 1] > 0)) nSends++;
+    if ((iProc != rank) && (nElem_Recv[iProc + 1] > 0)) nRecvs++;
 
-    nElem_Send[iProc+1] += nElem_Send[iProc];
-    nElem_Recv[iProc+1] += nElem_Recv[iProc];
+    nElem_Send[iProc + 1] += nElem_Send[iProc];
+    nElem_Recv[iProc + 1] += nElem_Recv[iProc];
   }
 
   /*--- Allocate memory to hold the connectivity that we are
    sending. ---*/
 
-  unsigned long *connSend = nullptr;
-  connSend = new unsigned long[NODES_PER_ELEMENT*nElem_Send[size]];
-  for (iSend = 0; iSend < NODES_PER_ELEMENT*nElem_Send[size]; iSend++)
-    connSend[iSend] = 0;
+  unsigned long* connSend = nullptr;
+  connSend = new unsigned long[NODES_PER_ELEMENT * nElem_Send[size]];
+  for (iSend = 0; iSend < NODES_PER_ELEMENT * nElem_Send[size]; iSend++) connSend[iSend] = 0;
 
   /*--- Allocate arrays for storing the marker global index. ---*/
 
-  unsigned long *markerSend = new unsigned long[nElem_Send[size]];
+  unsigned long* markerSend = new unsigned long[nElem_Send[size]];
   for (iSend = 0; iSend < nElem_Send[size]; iSend++) markerSend[iSend] = 0;
 
-  unsigned long *idSend = new unsigned long[nElem_Send[size]];
+  unsigned long* idSend = new unsigned long[nElem_Send[size]];
   for (iSend = 0; iSend < nElem_Send[size]; iSend++) idSend[iSend] = 0;
 
   /*--- Create an index variable to keep track of our index
    position as we load up the send buffer. ---*/
 
-  unsigned long *index = new unsigned long[size];
-  for (iProc = 0; iProc < size; iProc++)
-    index[iProc] = NODES_PER_ELEMENT*nElem_Send[iProc];
+  unsigned long* index = new unsigned long[size];
+  for (iProc = 0; iProc < size; iProc++) index[iProc] = NODES_PER_ELEMENT * nElem_Send[iProc];
 
-  unsigned long *markerIndex = new unsigned long[size];
-  for (iProc = 0; iProc < size; iProc++)
-    markerIndex[iProc] = nElem_Send[iProc];
+  unsigned long* markerIndex = new unsigned long[size];
+  for (iProc = 0; iProc < size; iProc++) markerIndex[iProc] = nElem_Send[iProc];
 
   /*--- Loop through our elements and load the elems and their
    additional data that we will send to the other procs. ---*/
 
   for (iElem = 0; iElem < NELEM; iElem++) {
     for (iNode = 0; iNode < NODES_PER_ELEMENT; iNode++) {
-
       /*--- Get the index of the current point. ---*/
 
-      Global_Index = Conn_Linear[iElem*NODES_PER_ELEMENT+iNode];
+      Global_Index = Conn_Linear[iElem * NODES_PER_ELEMENT + iNode];
 
       /*--- We have the color stored in a map for all local points. ---*/
 
@@ -1890,7 +1798,6 @@ void CPhysicalGeometry::DistributeSurfaceConnectivity(CConfig *config,
        for sending. ---*/
 
       if (nElem_Flag[iProcessor] != (int)iElem) {
-
         nElem_Flag[iProcessor] = (int)iElem;
         unsigned long nn = index[iProcessor];
         unsigned long mm = markerIndex[iProcessor];
@@ -1898,111 +1805,105 @@ void CPhysicalGeometry::DistributeSurfaceConnectivity(CConfig *config,
         /*--- Load the connectivity values. ---*/
 
         for (jNode = 0; jNode < NODES_PER_ELEMENT; jNode++) {
-
           /*--- Note that elements are already stored directly based on
            their global index for the nodes. ---*/
 
-          connSend[nn] = Conn_Linear[iElem*NODES_PER_ELEMENT+jNode]; nn++;
-
+          connSend[nn] = Conn_Linear[iElem * NODES_PER_ELEMENT + jNode];
+          nn++;
         }
 
         /*--- Global marker ID for this element. ---*/
 
         markerSend[mm] = Linear_Markers[iElem];
-        idSend[mm]     = ID_SurfElem_Linear[iElem];
+        idSend[mm] = ID_SurfElem_Linear[iElem];
 
         /*--- Increment the index by the message length ---*/
 
         index[iProcessor] += NODES_PER_ELEMENT;
         markerIndex[iProcessor]++;
-
       }
     }
   }
 
   /*--- Free memory after loading up the send buffer. ---*/
 
-  delete [] index;
-  delete [] markerIndex;
+  delete[] index;
+  delete[] markerIndex;
 
   /*--- Allocate the memory that we need for receiving the conn
    values and then cue up the non-blocking receives. Note that
    we do not include our own rank in the communications. We will
    directly copy our own data later. ---*/
 
-  unsigned long *connRecv = nullptr;
-  connRecv = new unsigned long[NODES_PER_ELEMENT*nElem_Recv[size]];
-  for (iRecv = 0; iRecv < NODES_PER_ELEMENT*nElem_Recv[size]; iRecv++)
-    connRecv[iRecv] = 0;
+  unsigned long* connRecv = nullptr;
+  connRecv = new unsigned long[NODES_PER_ELEMENT * nElem_Recv[size]];
+  for (iRecv = 0; iRecv < NODES_PER_ELEMENT * nElem_Recv[size]; iRecv++) connRecv[iRecv] = 0;
 
-  unsigned long *markerRecv = new unsigned long[nElem_Recv[size]];
+  unsigned long* markerRecv = new unsigned long[nElem_Recv[size]];
   for (iRecv = 0; iRecv < nElem_Recv[size]; iRecv++) markerRecv[iRecv] = 0;
 
-  unsigned long *idRecv = new unsigned long[nElem_Recv[size]];
+  unsigned long* idRecv = new unsigned long[nElem_Recv[size]];
   for (iRecv = 0; iRecv < nElem_Recv[size]; iRecv++) idRecv[iRecv] = 0;
 
   /*--- Allocate memory for the MPI requests if we need to communicate. ---*/
 
   if (nSends > 0) {
-    connSendReq   = new SU2_MPI::Request[nSends];
+    connSendReq = new SU2_MPI::Request[nSends];
     markerSendReq = new SU2_MPI::Request[nSends];
-    idSendReq     = new SU2_MPI::Request[nSends];
+    idSendReq = new SU2_MPI::Request[nSends];
   }
   if (nRecvs > 0) {
-    connRecvReq   = new SU2_MPI::Request[nRecvs];
+    connRecvReq = new SU2_MPI::Request[nRecvs];
     markerRecvReq = new SU2_MPI::Request[nRecvs];
-    idRecvReq     = new SU2_MPI::Request[nRecvs];
+    idRecvReq = new SU2_MPI::Request[nRecvs];
   }
 
   /*--- Launch the non-blocking sends and receives. ---*/
 
-  InitiateCommsAll(connSend, nElem_Send, connSendReq,
-                   connRecv, nElem_Recv, connRecvReq,
-                   NODES_PER_ELEMENT, COMM_TYPE_UNSIGNED_LONG);
+  InitiateCommsAll(connSend, nElem_Send, connSendReq, connRecv, nElem_Recv, connRecvReq, NODES_PER_ELEMENT,
+                   COMM_TYPE_UNSIGNED_LONG);
 
-  InitiateCommsAll(markerSend, nElem_Send, markerSendReq,
-                   markerRecv, nElem_Recv, markerRecvReq,
-                   1, COMM_TYPE_UNSIGNED_LONG);
+  InitiateCommsAll(markerSend, nElem_Send, markerSendReq, markerRecv, nElem_Recv, markerRecvReq, 1,
+                   COMM_TYPE_UNSIGNED_LONG);
 
-  InitiateCommsAll(idSend, nElem_Send, idSendReq,
-                   idRecv, nElem_Recv, idRecvReq,
-                   1, COMM_TYPE_UNSIGNED_LONG);
+  InitiateCommsAll(idSend, nElem_Send, idSendReq, idRecv, nElem_Recv, idRecvReq, 1, COMM_TYPE_UNSIGNED_LONG);
 
   /*--- Copy my own rank's data into the recv buffer directly. ---*/
 
-  iRecv   = NODES_PER_ELEMENT*nElem_Recv[rank];
-  myStart = NODES_PER_ELEMENT*nElem_Send[rank];
-  myFinal = NODES_PER_ELEMENT*nElem_Send[rank+1];
+  iRecv = NODES_PER_ELEMENT * nElem_Recv[rank];
+  myStart = NODES_PER_ELEMENT * nElem_Send[rank];
+  myFinal = NODES_PER_ELEMENT * nElem_Send[rank + 1];
   for (iSend = myStart; iSend < myFinal; iSend++) {
     connRecv[iRecv] = connSend[iSend];
     iRecv++;
   }
 
-  iRecv   = nElem_Recv[rank];
+  iRecv = nElem_Recv[rank];
   myStart = nElem_Send[rank];
-  myFinal = nElem_Send[rank+1];
+  myFinal = nElem_Send[rank + 1];
   for (iSend = myStart; iSend < myFinal; iSend++) {
     markerRecv[iRecv] = markerSend[iSend];
-    idRecv[iRecv]     = idSend[iSend];
+    idRecv[iRecv] = idSend[iSend];
     iRecv++;
   }
 
   /*--- Complete the non-blocking communications. ---*/
 
-  CompleteCommsAll(nSends,   connSendReq, nRecvs,   connRecvReq);
+  CompleteCommsAll(nSends, connSendReq, nRecvs, connRecvReq);
   CompleteCommsAll(nSends, markerSendReq, nRecvs, markerRecvReq);
-  CompleteCommsAll(nSends,     idSendReq, nRecvs,     idRecvReq);
+  CompleteCommsAll(nSends, idSendReq, nRecvs, idRecvReq);
 
   /*--- Store the connectivity for this rank in the proper data
    structure. It will be loaded into the geometry objects in a later step. ---*/
 
   if (nElem_Recv[size] > 0) {
-    Conn_Elem = new unsigned long[NODES_PER_ELEMENT*nElem_Recv[size]];
-    int count = 0; nElem_Total = 0;
+    Conn_Elem = new unsigned long[NODES_PER_ELEMENT * nElem_Recv[size]];
+    int count = 0;
+    nElem_Total = 0;
     for (iRecv = 0; iRecv < nElem_Recv[size]; iRecv++) {
       nElem_Total++;
       for (iNode = 0; iNode < NODES_PER_ELEMENT; iNode++) {
-        Conn_Elem[count] = connRecv[iRecv*NODES_PER_ELEMENT+iNode];
+        Conn_Elem[count] = connRecv[iRecv * NODES_PER_ELEMENT + iNode];
         count++;
       }
     }
@@ -2033,24 +1934,24 @@ void CPhysicalGeometry::DistributeSurfaceConnectivity(CConfig *config,
     case LINE:
       nLocal_Line = nElem_Total;
       if (nLocal_Line > 0) {
-        Conn_Line    = Conn_Elem;
-        ID_Line      = Local_Markers;
+        Conn_Line = Conn_Elem;
+        ID_Line = Local_Markers;
         Elem_ID_Line = ID_SurfElem;
       }
       break;
     case TRIANGLE:
       nLocal_BoundTria = nElem_Total;
       if (nLocal_BoundTria > 0) {
-        Conn_BoundTria    = Conn_Elem;
-        ID_BoundTria      = Local_Markers;
+        Conn_BoundTria = Conn_Elem;
+        ID_BoundTria = Local_Markers;
         Elem_ID_BoundTria = ID_SurfElem;
       }
       break;
     case QUADRILATERAL:
       nLocal_BoundQuad = nElem_Total;
       if (nLocal_BoundQuad > 0) {
-        Conn_BoundQuad    = Conn_Elem;
-        ID_BoundQuad      = Local_Markers;
+        Conn_BoundQuad = Conn_Elem;
+        ID_BoundQuad = Local_Markers;
         Elem_ID_BoundQuad = ID_SurfElem;
       }
       break;
@@ -2061,28 +1962,26 @@ void CPhysicalGeometry::DistributeSurfaceConnectivity(CConfig *config,
 
   /*--- Free temporary memory from communications ---*/
 
-  delete [] connSendReq;
-  delete [] markerSendReq;
-  delete [] idSendReq;
-
-  delete [] connRecvReq;
-  delete [] markerRecvReq;
-  delete [] idRecvReq;
-
-  delete [] connSend;
-  delete [] connRecv;
-  delete [] markerSend;
-  delete [] markerRecv;
-  delete [] idSend;
-  delete [] idRecv;
-  delete [] nElem_Recv;
-  delete [] nElem_Send;
-  delete [] nElem_Flag;
-
+  delete[] connSendReq;
+  delete[] markerSendReq;
+  delete[] idSendReq;
+
+  delete[] connRecvReq;
+  delete[] markerRecvReq;
+  delete[] idRecvReq;
+
+  delete[] connSend;
+  delete[] connRecv;
+  delete[] markerSend;
+  delete[] markerRecv;
+  delete[] idSend;
+  delete[] idRecv;
+  delete[] nElem_Recv;
+  delete[] nElem_Send;
+  delete[] nElem_Flag;
 }
 
-void CPhysicalGeometry::DistributeMarkerTags(CConfig *config, CGeometry *geometry) {
-
+void CPhysicalGeometry::DistributeMarkerTags(CConfig* config, CGeometry* geometry) {
   unsigned long iMarker, index, iChar;
 
   char str_buf[MAX_STRING_SIZE];
@@ -2096,48 +1995,43 @@ void CPhysicalGeometry::DistributeMarkerTags(CConfig *config, CGeometry *geometr
 
   /*--- Broadcast the global number of markers in the mesh. ---*/
 
-  SU2_MPI::Bcast(&nMarker_Global, 1, MPI_UNSIGNED_LONG,
-                 MASTER_NODE, SU2_MPI::GetComm());
+  SU2_MPI::Bcast(&nMarker_Global, 1, MPI_UNSIGNED_LONG, MASTER_NODE, SU2_MPI::GetComm());
 
-  char *mpi_str_buf = new char[nMarker_Global*MAX_STRING_SIZE]();
+  char* mpi_str_buf = new char[nMarker_Global * MAX_STRING_SIZE]();
   if (rank == MASTER_NODE) {
     for (iMarker = 0; iMarker < nMarker_Global; iMarker++) {
-      SPRINTF(&mpi_str_buf[iMarker*MAX_STRING_SIZE], "%s",
-              config->GetMarker_All_TagBound(iMarker).c_str());
+      SPRINTF(&mpi_str_buf[iMarker * MAX_STRING_SIZE], "%s", config->GetMarker_All_TagBound(iMarker).c_str());
     }
   }
 
   /*--- Broadcast the string names of the variables. ---*/
 
-  SU2_MPI::Bcast(mpi_str_buf, (int)nMarker_Global*MAX_STRING_SIZE, MPI_CHAR,
-                 MASTER_NODE, SU2_MPI::GetComm());
+  SU2_MPI::Bcast(mpi_str_buf, (int)nMarker_Global * MAX_STRING_SIZE, MPI_CHAR, MASTER_NODE, SU2_MPI::GetComm());
 
   /*--- Now parse the string names and load into our marker tag vector.
    We also need to set the values of all markers into the config. ---*/
 
   for (iMarker = 0; iMarker < nMarker_Global; iMarker++) {
-    index = iMarker*MAX_STRING_SIZE;
+    index = iMarker * MAX_STRING_SIZE;
     for (iChar = 0; iChar < MAX_STRING_SIZE; iChar++) {
       str_buf[iChar] = mpi_str_buf[index + iChar];
     }
     Marker_Tags.push_back(str_buf);
-    config->SetMarker_All_TagBound(iMarker,str_buf);
-    config->SetMarker_All_SendRecv(iMarker,NO);
+    config->SetMarker_All_TagBound(iMarker, str_buf);
+    config->SetMarker_All_SendRecv(iMarker, NO);
   }
 
   /*--- Free string buffer memory. ---*/
 
-  delete [] mpi_str_buf;
-
+  delete[] mpi_str_buf;
 }
 
-void CPhysicalGeometry::LoadPoints(CConfig *config, CGeometry *geometry) {
-
+void CPhysicalGeometry::LoadPoints(CConfig* config, CGeometry* geometry) {
   unsigned long iPoint, jPoint, iOwned, iPeriodic, iGhost;
 
   /*--- Create the basic point structures before storing the points. ---*/
 
-  nPoint       = nLocal_Point;
+  nPoint = nLocal_Point;
   nPointDomain = nLocal_PointDomain;
 
   nodes = new CPoint(nPoint, nDim, MESH_0, config);
@@ -2153,22 +2047,22 @@ void CPhysicalGeometry::LoadPoints(CConfig *config, CGeometry *geometry) {
   /*--- Set our counters correctly based on the number of owned and ghost
    nodes that we counted during the partitioning. ---*/
 
-  jPoint    = 0;
-  iOwned    = 0;
+  jPoint = 0;
+  iOwned = 0;
   iPeriodic = nLocal_PointDomain;
-  iGhost    = nLocal_PointDomain + nLocal_PointPeriodic;
+  iGhost = nLocal_PointDomain + nLocal_PointPeriodic;
 
   /*--- Loop over all of the points that we have recv'd and store the
    coordinates, global index, and colors ---*/
 
   for (iPoint = 0; iPoint < nPoint; iPoint++) {
-
     /*--- Set the starting point to the correct counter for this point. ---*/
 
     if (Local_Colors[iPoint] == (unsigned long)rank) {
       if (Local_Points[iPoint] < geometry->GetGlobal_nPointDomain())
         jPoint = iOwned;
-      else jPoint = iPeriodic;
+      else
+        jPoint = iPeriodic;
     } else {
       jPoint = iGhost;
     }
@@ -2179,7 +2073,7 @@ void CPhysicalGeometry::LoadPoints(CConfig *config, CGeometry *geometry) {
 
     /*--- Allocating the Point object ---*/
 
-    nodes->SetCoord(jPoint, &Local_Coords[iPoint*nDim]);
+    nodes->SetCoord(jPoint, &Local_Coords[iPoint * nDim]);
     nodes->SetGlobalIndex(jPoint, Local_to_Global_Point[jPoint]);
 
     /*--- Set the color ---*/
@@ -2191,7 +2085,8 @@ void CPhysicalGeometry::LoadPoints(CConfig *config, CGeometry *geometry) {
     if (Local_Colors[iPoint] == (unsigned long)rank) {
       if (Local_Points[iPoint] < geometry->GetGlobal_nPointDomain())
         iOwned++;
-      else iPeriodic++;
+      else
+        iPeriodic++;
     } else {
       iGhost++;
     }
@@ -2200,8 +2095,7 @@ void CPhysicalGeometry::LoadPoints(CConfig *config, CGeometry *geometry) {
   /*--- Create the global to local mapping, which will be useful for loading
    the elements and boundaries in subsequent steps. ---*/
 
-  for (iPoint = 0; iPoint < nPoint; iPoint++)
-    Global_to_Local_Point[Local_to_Global_Point[iPoint]] = iPoint;
+  for (iPoint = 0; iPoint < nPoint; iPoint++) Global_to_Local_Point[Local_to_Global_Point[iPoint]] = iPoint;
 
   /*--- Set the value of Global_nPoint and Global_nPointDomain ---*/
 
@@ -2209,10 +2103,8 @@ void CPhysicalGeometry::LoadPoints(CConfig *config, CGeometry *geometry) {
   unsigned long Local_nPointDomain = nPointDomain;
 
 #ifdef HAVE_MPI
-  SU2_MPI::Allreduce(&Local_nPoint, &Global_nPoint, 1,
-                     MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
-  SU2_MPI::Allreduce(&Local_nPointDomain, &Global_nPointDomain, 1,
-                     MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&Local_nPoint, &Global_nPoint, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&Local_nPointDomain, &Global_nPointDomain, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
 #else
   Global_nPoint = Local_nPoint;
   Global_nPointDomain = Local_nPointDomain;
@@ -2220,11 +2112,9 @@ void CPhysicalGeometry::LoadPoints(CConfig *config, CGeometry *geometry) {
 
   if ((rank == MASTER_NODE) && (size > SINGLE_NODE))
     cout << Global_nPoint << " vertices including ghost points. " << endl;
-
 }
 
-void CPhysicalGeometry::LoadVolumeElements(CConfig *config, CGeometry *geometry) {
-
+void CPhysicalGeometry::LoadVolumeElements(CConfig* config, CGeometry* geometry) {
   unsigned short NODES_PER_ELEMENT;
 
   unsigned long iElem, jElem, kElem, iNode, Local_Elem, iGlobal_Index;
@@ -2253,37 +2143,37 @@ void CPhysicalGeometry::LoadVolumeElements(CConfig *config, CGeometry *geometry)
    overwriting the duplicate entries. ---*/
 
   jElem = 0;
-  for (iElem=0; iElem < nLocal_Tria; iElem++) {
+  for (iElem = 0; iElem < nLocal_Tria; iElem++) {
     Tria_List[ID_Tria[iElem]] = iElem;
   }
   nTria = Tria_List.size();
 
   jElem = 0;
-  for (iElem=0; iElem < nLocal_Quad; iElem++) {
+  for (iElem = 0; iElem < nLocal_Quad; iElem++) {
     Quad_List[ID_Quad[iElem]] = iElem;
   }
   nQuad = Quad_List.size();
 
   jElem = 0;
-  for (iElem=0; iElem < nLocal_Tetr; iElem++) {
+  for (iElem = 0; iElem < nLocal_Tetr; iElem++) {
     Tetr_List[ID_Tetr[iElem]] = iElem;
   }
   nTetr = Tetr_List.size();
 
   jElem = 0;
-  for (iElem=0; iElem < nLocal_Hexa; iElem++) {
+  for (iElem = 0; iElem < nLocal_Hexa; iElem++) {
     Hexa_List[ID_Hexa[iElem]] = iElem;
   }
   nHexa = Hexa_List.size();
 
   jElem = 0;
-  for (iElem=0; iElem < nLocal_Pris; iElem++) {
+  for (iElem = 0; iElem < nLocal_Pris; iElem++) {
     Pris_List[ID_Pris[iElem]] = iElem;
   }
   nPris = Pris_List.size();
 
   jElem = 0;
-  for (iElem=0; iElem < nLocal_Pyra; iElem++) {
+  for (iElem = 0; iElem < nLocal_Pyra; iElem++) {
     Pyra_List[ID_Pyra[iElem]] = iElem;
   }
   nPyra = Pyra_List.size();
@@ -2296,12 +2186,11 @@ void CPhysicalGeometry::LoadVolumeElements(CConfig *config, CGeometry *geometry)
 
   jElem = 0;
   nElem = Local_Elem;
-  elem  = new CPrimalGrid*[nElem] ();
+  elem = new CPrimalGrid*[nElem]();
 
   /*--- Store the elements of each type in the proper containers. ---*/
 
   for (it = Tria_List.begin(); it != Tria_List.end(); it++) {
-
     kElem = it->first;
     iElem = it->second;
 
@@ -2310,22 +2199,20 @@ void CPhysicalGeometry::LoadVolumeElements(CConfig *config, CGeometry *geometry)
 
     NODES_PER_ELEMENT = N_POINTS_TRIANGLE;
     for (iNode = 0; iNode < NODES_PER_ELEMENT; iNode++) {
-      iGlobal_Index      = Conn_Tria[iElem*NODES_PER_ELEMENT+iNode];
+      iGlobal_Index = Conn_Tria[iElem * NODES_PER_ELEMENT + iNode];
       Local_Nodes[iNode] = Global_to_Local_Point[iGlobal_Index];
     }
 
     /*--- Create the element object. ---*/
 
-    elem[jElem] = new CTriangle(Local_Nodes[0],
-                                Local_Nodes[1],
-                                Local_Nodes[2]);
+    elem[jElem] = new CTriangle(Local_Nodes[0], Local_Nodes[1], Local_Nodes[2]);
 
     elem[jElem]->SetGlobalIndex(kElem);
 
     /*--- Increment our local counters. ---*/
 
-    jElem++; iElemTria++;
-
+    jElem++;
+    iElemTria++;
   }
 
   /*--- Free memory as we go. ---*/
@@ -2333,7 +2220,6 @@ void CPhysicalGeometry::LoadVolumeElements(CConfig *config, CGeometry *geometry)
   Tria_List.clear();
 
   for (it = Quad_List.begin(); it != Quad_List.end(); it++) {
-
     kElem = it->first;
     iElem = it->second;
 
@@ -2342,23 +2228,20 @@ void CPhysicalGeometry::LoadVolumeElements(CConfig *config, CGeometry *geometry)
 
     NODES_PER_ELEMENT = N_POINTS_QUADRILATERAL;
     for (iNode = 0; iNode < NODES_PER_ELEMENT; iNode++) {
-      iGlobal_Index      = Conn_Quad[iElem*NODES_PER_ELEMENT+iNode];
+      iGlobal_Index = Conn_Quad[iElem * NODES_PER_ELEMENT + iNode];
       Local_Nodes[iNode] = Global_to_Local_Point[iGlobal_Index];
     }
 
     /*--- Create the element object. ---*/
 
-    elem[jElem] = new CQuadrilateral(Local_Nodes[0],
-                                     Local_Nodes[1],
-                                     Local_Nodes[2],
-                                     Local_Nodes[3]);
+    elem[jElem] = new CQuadrilateral(Local_Nodes[0], Local_Nodes[1], Local_Nodes[2], Local_Nodes[3]);
 
     elem[jElem]->SetGlobalIndex(kElem);
 
     /*--- Increment our local counters. ---*/
 
-    jElem++; iElemQuad++;
-
+    jElem++;
+    iElemQuad++;
   }
 
   /*--- Free memory as we go. ---*/
@@ -2366,7 +2249,6 @@ void CPhysicalGeometry::LoadVolumeElements(CConfig *config, CGeometry *geometry)
   Quad_List.clear();
 
   for (it = Tetr_List.begin(); it != Tetr_List.end(); it++) {
-
     kElem = it->first;
     iElem = it->second;
 
@@ -2375,23 +2257,20 @@ void CPhysicalGeometry::LoadVolumeElements(CConfig *config, CGeometry *geometry)
 
     NODES_PER_ELEMENT = N_POINTS_TETRAHEDRON;
     for (iNode = 0; iNode < NODES_PER_ELEMENT; iNode++) {
-      iGlobal_Index      = Conn_Tetr[iElem*NODES_PER_ELEMENT+iNode];
+      iGlobal_Index = Conn_Tetr[iElem * NODES_PER_ELEMENT + iNode];
       Local_Nodes[iNode] = Global_to_Local_Point[iGlobal_Index];
     }
 
     /*--- Create the element object. ---*/
 
-    elem[jElem] = new CTetrahedron(Local_Nodes[0],
-                                   Local_Nodes[1],
-                                   Local_Nodes[2],
-                                   Local_Nodes[3]);
+    elem[jElem] = new CTetrahedron(Local_Nodes[0], Local_Nodes[1], Local_Nodes[2], Local_Nodes[3]);
 
     elem[jElem]->SetGlobalIndex(kElem);
 
     /*--- Increment our local counters. ---*/
 
-    jElem++; iElemTetr++;
-
+    jElem++;
+    iElemTetr++;
   }
 
   /*--- Free memory as we go. ---*/
@@ -2399,7 +2278,6 @@ void CPhysicalGeometry::LoadVolumeElements(CConfig *config, CGeometry *geometry)
   Tetr_List.clear();
 
   for (it = Hexa_List.begin(); it != Hexa_List.end(); it++) {
-
     kElem = it->first;
     iElem = it->second;
 
@@ -2408,27 +2286,21 @@ void CPhysicalGeometry::LoadVolumeElements(CConfig *config, CGeometry *geometry)
 
     NODES_PER_ELEMENT = N_POINTS_HEXAHEDRON;
     for (iNode = 0; iNode < NODES_PER_ELEMENT; iNode++) {
-      iGlobal_Index      = Conn_Hexa[iElem*NODES_PER_ELEMENT+iNode];
+      iGlobal_Index = Conn_Hexa[iElem * NODES_PER_ELEMENT + iNode];
       Local_Nodes[iNode] = Global_to_Local_Point[iGlobal_Index];
     }
 
     /*--- Create the element object. ---*/
 
-    elem[jElem] = new CHexahedron(Local_Nodes[0],
-                                  Local_Nodes[1],
-                                  Local_Nodes[2],
-                                  Local_Nodes[3],
-                                  Local_Nodes[4],
-                                  Local_Nodes[5],
-                                  Local_Nodes[6],
-                                  Local_Nodes[7]);
+    elem[jElem] = new CHexahedron(Local_Nodes[0], Local_Nodes[1], Local_Nodes[2], Local_Nodes[3], Local_Nodes[4],
+                                  Local_Nodes[5], Local_Nodes[6], Local_Nodes[7]);
 
     elem[jElem]->SetGlobalIndex(kElem);
 
     /*--- Increment our local counters. ---*/
 
-    jElem++; iElemHexa++;
-
+    jElem++;
+    iElemHexa++;
   }
 
   /*--- Free memory as we go. ---*/
@@ -2436,7 +2308,6 @@ void CPhysicalGeometry::LoadVolumeElements(CConfig *config, CGeometry *geometry)
   Hexa_List.clear();
 
   for (it = Pris_List.begin(); it != Pris_List.end(); it++) {
-
     kElem = it->first;
     iElem = it->second;
 
@@ -2445,25 +2316,21 @@ void CPhysicalGeometry::LoadVolumeElements(CConfig *config, CGeometry *geometry)
 
     NODES_PER_ELEMENT = N_POINTS_PRISM;
     for (iNode = 0; iNode < NODES_PER_ELEMENT; iNode++) {
-      iGlobal_Index      = Conn_Pris[iElem*NODES_PER_ELEMENT+iNode];
+      iGlobal_Index = Conn_Pris[iElem * NODES_PER_ELEMENT + iNode];
       Local_Nodes[iNode] = Global_to_Local_Point[iGlobal_Index];
     }
 
     /*--- Create the element object. ---*/
 
-    elem[jElem] = new CPrism(Local_Nodes[0],
-                             Local_Nodes[1],
-                             Local_Nodes[2],
-                             Local_Nodes[3],
-                             Local_Nodes[4],
-                             Local_Nodes[5]);
+    elem[jElem] =
+        new CPrism(Local_Nodes[0], Local_Nodes[1], Local_Nodes[2], Local_Nodes[3], Local_Nodes[4], Local_Nodes[5]);
 
     elem[jElem]->SetGlobalIndex(kElem);
 
     /*--- Increment our local counters. ---*/
 
-    jElem++; iElemPris++;
-
+    jElem++;
+    iElemPris++;
   }
 
   /*--- Free memory as we go. ---*/
@@ -2471,7 +2338,6 @@ void CPhysicalGeometry::LoadVolumeElements(CConfig *config, CGeometry *geometry)
   Pris_List.clear();
 
   for (it = Pyra_List.begin(); it != Pyra_List.end(); it++) {
-
     kElem = it->first;
     iElem = it->second;
 
@@ -2480,24 +2346,20 @@ void CPhysicalGeometry::LoadVolumeElements(CConfig *config, CGeometry *geometry)
 
     NODES_PER_ELEMENT = N_POINTS_PYRAMID;
     for (iNode = 0; iNode < NODES_PER_ELEMENT; iNode++) {
-      iGlobal_Index      = Conn_Pyra[iElem*NODES_PER_ELEMENT+iNode];
+      iGlobal_Index = Conn_Pyra[iElem * NODES_PER_ELEMENT + iNode];
       Local_Nodes[iNode] = Global_to_Local_Point[iGlobal_Index];
     }
 
     /*--- Create the element object. ---*/
 
-    elem[jElem] = new CPyramid(Local_Nodes[0],
-                               Local_Nodes[1],
-                               Local_Nodes[2],
-                               Local_Nodes[3],
-                               Local_Nodes[4]);
+    elem[jElem] = new CPyramid(Local_Nodes[0], Local_Nodes[1], Local_Nodes[2], Local_Nodes[3], Local_Nodes[4]);
 
     elem[jElem]->SetGlobalIndex(kElem);
 
     /*--- Increment our local counters. ---*/
 
-    jElem++; iElemPyra++;
-
+    jElem++;
+    iElemPyra++;
   }
 
   /*--- Free memory as we go. ---*/
@@ -2507,8 +2369,7 @@ void CPhysicalGeometry::LoadVolumeElements(CConfig *config, CGeometry *geometry)
   /*--- Communicate the number of each element type to all processors. These
    values are important for merging and writing output later. ---*/
 
-  SU2_MPI::Allreduce(&Local_Elem, &Global_nElem, 1,
-                     MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&Local_Elem, &Global_nElem, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
 
   if ((rank == MASTER_NODE) && (size > SINGLE_NODE))
     cout << Global_nElem << " interior elements including halo cells. " << endl;
@@ -2522,62 +2383,48 @@ void CPhysicalGeometry::LoadVolumeElements(CConfig *config, CGeometry *geometry)
    counters in the recv loop above (to make sure there aren't repeats). ---*/
 
   nelem_triangle = iElemTria;
-  nelem_quad     = iElemQuad;
-  nelem_tetra    = iElemTetr;
-  nelem_hexa     = iElemHexa;
-  nelem_prism    = iElemPris;
-  nelem_pyramid  = iElemPyra;
+  nelem_quad = iElemQuad;
+  nelem_tetra = iElemTetr;
+  nelem_hexa = iElemHexa;
+  nelem_prism = iElemPris;
+  nelem_pyramid = iElemPyra;
 
 #ifdef HAVE_MPI
-  unsigned long Local_nElemTri     = nelem_triangle;
-  unsigned long Local_nElemQuad    = nelem_quad;
-  unsigned long Local_nElemTet     = nelem_tetra;
-  unsigned long Local_nElemHex     = nelem_hexa;
-  unsigned long Local_nElemPrism   = nelem_prism;
+  unsigned long Local_nElemTri = nelem_triangle;
+  unsigned long Local_nElemQuad = nelem_quad;
+  unsigned long Local_nElemTet = nelem_tetra;
+  unsigned long Local_nElemHex = nelem_hexa;
+  unsigned long Local_nElemPrism = nelem_prism;
   unsigned long Local_nElemPyramid = nelem_pyramid;
 
-  SU2_MPI::Allreduce(&Local_nElemTri, &Global_nelem_triangle, 1,
-                     MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
-  SU2_MPI::Allreduce(&Local_nElemQuad, &Global_nelem_quad, 1,
-                     MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
-  SU2_MPI::Allreduce(&Local_nElemTet, &Global_nelem_tetra, 1,
-                     MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
-  SU2_MPI::Allreduce(&Local_nElemHex, &Global_nelem_hexa, 1,
-                     MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
-  SU2_MPI::Allreduce(&Local_nElemPrism, &Global_nelem_prism, 1,
-                     MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
-  SU2_MPI::Allreduce(&Local_nElemPyramid, &Global_nelem_pyramid, 1,
-                     MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&Local_nElemTri, &Global_nelem_triangle, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&Local_nElemQuad, &Global_nelem_quad, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&Local_nElemTet, &Global_nelem_tetra, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&Local_nElemHex, &Global_nelem_hexa, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&Local_nElemPrism, &Global_nelem_prism, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&Local_nElemPyramid, &Global_nelem_pyramid, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
 #else
   Global_nelem_triangle = nelem_triangle;
-  Global_nelem_quad     = nelem_quad;
-  Global_nelem_tetra    = nelem_tetra;
-  Global_nelem_hexa     = nelem_hexa;
-  Global_nelem_prism    = nelem_prism;
-  Global_nelem_pyramid  = nelem_pyramid;
+  Global_nelem_quad = nelem_quad;
+  Global_nelem_tetra = nelem_tetra;
+  Global_nelem_hexa = nelem_hexa;
+  Global_nelem_prism = nelem_prism;
+  Global_nelem_pyramid = nelem_pyramid;
 #endif
 
   /*--- Print information about the elements to the console ---*/
 
   if (rank == MASTER_NODE) {
-    if (Global_nelem_triangle > 0)
-      cout << Global_nelem_triangle << " triangles."      << endl;
-    if (Global_nelem_quad     > 0)
-      cout << Global_nelem_quad     << " quadrilaterals." << endl;
-    if (Global_nelem_tetra    > 0)
-      cout << Global_nelem_tetra    << " tetrahedra."     << endl;
-    if (Global_nelem_hexa     > 0)
-      cout << Global_nelem_hexa     << " hexahedra."      << endl;
-    if (Global_nelem_prism    > 0)
-      cout << Global_nelem_prism    << " prisms."         << endl;
-    if (Global_nelem_pyramid  > 0)
-      cout << Global_nelem_pyramid  << " pyramids."       << endl;
+    if (Global_nelem_triangle > 0) cout << Global_nelem_triangle << " triangles." << endl;
+    if (Global_nelem_quad > 0) cout << Global_nelem_quad << " quadrilaterals." << endl;
+    if (Global_nelem_tetra > 0) cout << Global_nelem_tetra << " tetrahedra." << endl;
+    if (Global_nelem_hexa > 0) cout << Global_nelem_hexa << " hexahedra." << endl;
+    if (Global_nelem_prism > 0) cout << Global_nelem_prism << " prisms." << endl;
+    if (Global_nelem_pyramid > 0) cout << Global_nelem_pyramid << " pyramids." << endl;
   }
-
 }
 
-void CPhysicalGeometry::LoadSurfaceElements(CConfig *config, CGeometry *geometry) {
-
+void CPhysicalGeometry::LoadSurfaceElements(CConfig* config, CGeometry* geometry) {
   unsigned short NODES_PER_ELEMENT;
   unsigned short iNode, nMarker_Max = config->GetnMarker_Max();
 
@@ -2600,22 +2447,19 @@ void CPhysicalGeometry::LoadSurfaceElements(CConfig *config, CGeometry *geometry
    counting the unique set. ---*/
 
   for (iElem = 0; iElem < nLocal_Line; iElem++) {
-    if (find(Marker_Local.begin(), Marker_Local.end(),
-             ID_Line[iElem]) == Marker_Local.end()) {
+    if (find(Marker_Local.begin(), Marker_Local.end(), ID_Line[iElem]) == Marker_Local.end()) {
       Marker_Local.push_back(ID_Line[iElem]);
     }
   }
 
   for (iElem = 0; iElem < nLocal_BoundTria; iElem++) {
-    if (find(Marker_Local.begin(), Marker_Local.end(),
-             ID_BoundTria[iElem]) == Marker_Local.end()) {
+    if (find(Marker_Local.begin(), Marker_Local.end(), ID_BoundTria[iElem]) == Marker_Local.end()) {
       Marker_Local.push_back(ID_BoundTria[iElem]);
     }
   }
 
   for (iElem = 0; iElem < nLocal_BoundQuad; iElem++) {
-    if (find(Marker_Local.begin(), Marker_Local.end(),
-             ID_BoundQuad[iElem]) == Marker_Local.end()) {
+    if (find(Marker_Local.begin(), Marker_Local.end(), ID_BoundQuad[iElem]) == Marker_Local.end()) {
       Marker_Local.push_back(ID_BoundQuad[iElem]);
     }
   }
@@ -2642,13 +2486,11 @@ void CPhysicalGeometry::LoadSurfaceElements(CConfig *config, CGeometry *geometry
 
   vector<unsigned long> nElemBound_Local;
   nElemBound_Local.resize(Marker_Local.size());
-  for (iMarker = 0; iMarker < Marker_Local.size(); iMarker++)
-    nElemBound_Local[iMarker] = 0;
+  for (iMarker = 0; iMarker < Marker_Local.size(); iMarker++) nElemBound_Local[iMarker] = 0;
 
   for (iElem = 0; iElem < nLocal_Line; iElem++) {
     iMarker = Marker_Global_to_Local[ID_Line[iElem]];
-    if (find(Line_List[iMarker].begin(), Line_List[iMarker].end(),
-             Elem_ID_Line[iElem]) == Line_List[iMarker].end()) {
+    if (find(Line_List[iMarker].begin(), Line_List[iMarker].end(), Elem_ID_Line[iElem]) == Line_List[iMarker].end()) {
       nElemBound_Local[iMarker]++;
       Line_List[iMarker].push_back(Elem_ID_Line[iElem]);
     }
@@ -2656,8 +2498,8 @@ void CPhysicalGeometry::LoadSurfaceElements(CConfig *config, CGeometry *geometry
 
   for (iElem = 0; iElem < nLocal_BoundTria; iElem++) {
     iMarker = Marker_Global_to_Local[ID_BoundTria[iElem]];
-    if (find(BoundTria_List[iMarker].begin(), BoundTria_List[iMarker].end(),
-             Elem_ID_BoundTria[iElem]) == BoundTria_List[iMarker].end()) {
+    if (find(BoundTria_List[iMarker].begin(), BoundTria_List[iMarker].end(), Elem_ID_BoundTria[iElem]) ==
+        BoundTria_List[iMarker].end()) {
       nElemBound_Local[iMarker]++;
       BoundTria_List[iMarker].push_back(Elem_ID_BoundTria[iElem]);
     }
@@ -2665,8 +2507,8 @@ void CPhysicalGeometry::LoadSurfaceElements(CConfig *config, CGeometry *geometry
 
   for (iElem = 0; iElem < nLocal_BoundQuad; iElem++) {
     iMarker = Marker_Global_to_Local[ID_BoundQuad[iElem]];
-    if (find(BoundQuad_List[iMarker].begin(), BoundQuad_List[iMarker].end(),
-             Elem_ID_BoundQuad[iElem]) == BoundQuad_List[iMarker].end()) {
+    if (find(BoundQuad_List[iMarker].begin(), BoundQuad_List[iMarker].end(), Elem_ID_BoundQuad[iElem]) ==
+        BoundQuad_List[iMarker].end()) {
       nElemBound_Local[iMarker]++;
       BoundQuad_List[iMarker].push_back(Elem_ID_BoundQuad[iElem]);
     }
@@ -2676,22 +2518,19 @@ void CPhysicalGeometry::LoadSurfaceElements(CConfig *config, CGeometry *geometry
    with nMarkerMax here, but come back and compute size we need. Same for
    OVERHEAD - this can precomputed. ---*/
 
-  nMarker             = Marker_Local.size();
-  nElem_Bound         = new unsigned long[nMarker_Max];
-  Tag_to_Marker       = new string[nMarker_Max];
+  nMarker = Marker_Local.size();
+  nElem_Bound = new unsigned long[nMarker_Max];
+  Tag_to_Marker = new string[nMarker_Max];
   Marker_All_SendRecv = new short[nMarker_Max];
 
   /*--- Allocate space for the elements on each marker ---*/
 
-  for (iMarker = 0; iMarker < nMarker; iMarker++)
-    nElem_Bound[iMarker] = nElemBound_Local[iMarker];
+  for (iMarker = 0; iMarker < nMarker; iMarker++) nElem_Bound[iMarker] = nElemBound_Local[iMarker];
 
-  bound = new CPrimalGrid**[nMarker+(OVERHEAD*size)];
-  for (iMarker = 0; iMarker < nMarker+(OVERHEAD*size); iMarker++)
-    bound[iMarker] = nullptr;
+  bound = new CPrimalGrid**[nMarker + (OVERHEAD * size)];
+  for (iMarker = 0; iMarker < nMarker + (OVERHEAD * size); iMarker++) bound[iMarker] = nullptr;
 
-  for (iMarker = 0; iMarker < nMarker; iMarker++)
-    bound[iMarker] = new CPrimalGrid*[nElem_Bound[iMarker]];
+  for (iMarker = 0; iMarker < nMarker; iMarker++) bound[iMarker] = new CPrimalGrid*[nElem_Bound[iMarker]];
 
   /*--- Initialize boundary element counters ---*/
 
@@ -2699,134 +2538,123 @@ void CPhysicalGeometry::LoadSurfaceElements(CConfig *config, CGeometry *geometry
   iElem_Tria = 0;
   iElem_Quad = 0;
 
-  Line_List.clear();      Line_List.resize(Marker_Local.size());
-  BoundTria_List.clear(); BoundTria_List.resize(Marker_Local.size());
-  BoundQuad_List.clear(); BoundQuad_List.resize(Marker_Local.size());
+  Line_List.clear();
+  Line_List.resize(Marker_Local.size());
+  BoundTria_List.clear();
+  BoundTria_List.resize(Marker_Local.size());
+  BoundQuad_List.clear();
+  BoundQuad_List.resize(Marker_Local.size());
 
   /*--- Reset our element counter on a marker-basis. ---*/
 
-  for (iMarker = 0; iMarker < nMarker; iMarker++)
-    nElemBound_Local[iMarker] = 0;
+  for (iMarker = 0; iMarker < nMarker; iMarker++) nElemBound_Local[iMarker] = 0;
 
   /*--- Store the boundary element connectivity. Note here that we have
    communicated the global index values for the elements, so we need to
    convert this to the local index when instantiating the element. ---*/
 
   for (iElem = 0; iElem < nLocal_Line; iElem++) {
-
     iMarker = Marker_Global_to_Local[ID_Line[iElem]];
 
     /*--- Avoid duplicates on this marker. ---*/
 
-    if (find(Line_List[iMarker].begin(), Line_List[iMarker].end(),
-             Elem_ID_Line[iElem]) == Line_List[iMarker].end()) {
-
+    if (find(Line_List[iMarker].begin(), Line_List[iMarker].end(), Elem_ID_Line[iElem]) == Line_List[iMarker].end()) {
       /*--- Transform the stored connectivity for this element from global
        to local values on this rank. ---*/
 
       NODES_PER_ELEMENT = N_POINTS_LINE;
       for (iNode = 0; iNode < NODES_PER_ELEMENT; iNode++) {
-        iGlobal_Index      = Conn_Line[iElem*NODES_PER_ELEMENT+iNode];
+        iGlobal_Index = Conn_Line[iElem * NODES_PER_ELEMENT + iNode];
         Local_Nodes[iNode] = Global_to_Local_Point[iGlobal_Index];
       }
 
       /*--- Create the geometry object for this element. ---*/
 
-      bound[iMarker][nElemBound_Local[iMarker]] = new CLine(Local_Nodes[0],
-                                                            Local_Nodes[1]);
+      bound[iMarker][nElemBound_Local[iMarker]] = new CLine(Local_Nodes[0], Local_Nodes[1]);
 
       /*--- Increment our counters for this marker and element type. ---*/
 
-      nElemBound_Local[iMarker]++; iElem_Line++;
+      nElemBound_Local[iMarker]++;
+      iElem_Line++;
 
       Line_List[iMarker].push_back(Elem_ID_Line[iElem]);
-
     }
   }
 
   for (iElem = 0; iElem < nLocal_BoundTria; iElem++) {
-
     iMarker = Marker_Global_to_Local[ID_BoundTria[iElem]];
 
     /*--- Avoid duplicates on this marker. ---*/
 
-    if (find(BoundTria_List[iMarker].begin(), BoundTria_List[iMarker].end(),
-             Elem_ID_BoundTria[iElem]) == BoundTria_List[iMarker].end()) {
-
+    if (find(BoundTria_List[iMarker].begin(), BoundTria_List[iMarker].end(), Elem_ID_BoundTria[iElem]) ==
+        BoundTria_List[iMarker].end()) {
       /*--- Transform the stored connectivity for this element from global
        to local values on this rank. ---*/
 
       NODES_PER_ELEMENT = N_POINTS_TRIANGLE;
       for (iNode = 0; iNode < NODES_PER_ELEMENT; iNode++) {
-        iGlobal_Index      = Conn_BoundTria[iElem*NODES_PER_ELEMENT+iNode];
+        iGlobal_Index = Conn_BoundTria[iElem * NODES_PER_ELEMENT + iNode];
         Local_Nodes[iNode] = Global_to_Local_Point[iGlobal_Index];
       }
 
       /*--- Create the geometry object for this element. ---*/
 
-      bound[iMarker][nElemBound_Local[iMarker]] = new CTriangle(Local_Nodes[0],
-                                                                Local_Nodes[1],
-                                                                Local_Nodes[2]);
+      bound[iMarker][nElemBound_Local[iMarker]] = new CTriangle(Local_Nodes[0], Local_Nodes[1], Local_Nodes[2]);
 
       /*--- Increment our counters for this marker and element type. ---*/
 
-      nElemBound_Local[iMarker]++; iElem_Tria++;
+      nElemBound_Local[iMarker]++;
+      iElem_Tria++;
 
       BoundTria_List[iMarker].push_back(Elem_ID_BoundTria[iElem]);
-
     }
   }
 
   for (iElem = 0; iElem < nLocal_BoundQuad; iElem++) {
-
     iMarker = Marker_Global_to_Local[ID_BoundQuad[iElem]];
 
     /*--- Avoid duplicates on this marker. ---*/
 
-    if (find(BoundQuad_List[iMarker].begin(), BoundQuad_List[iMarker].end(),
-             Elem_ID_BoundQuad[iElem]) == BoundQuad_List[iMarker].end()) {
-
+    if (find(BoundQuad_List[iMarker].begin(), BoundQuad_List[iMarker].end(), Elem_ID_BoundQuad[iElem]) ==
+        BoundQuad_List[iMarker].end()) {
       /*--- Transform the stored connectivity for this element from global
        to local values on this rank. ---*/
 
       NODES_PER_ELEMENT = N_POINTS_QUADRILATERAL;
       for (iNode = 0; iNode < NODES_PER_ELEMENT; iNode++) {
-        iGlobal_Index      = Conn_BoundQuad[iElem*NODES_PER_ELEMENT+iNode];
+        iGlobal_Index = Conn_BoundQuad[iElem * NODES_PER_ELEMENT + iNode];
         Local_Nodes[iNode] = Global_to_Local_Point[iGlobal_Index];
       }
 
       /*--- Create the geometry object for this element. ---*/
 
-      bound[iMarker][nElemBound_Local[iMarker]] = new CQuadrilateral(Local_Nodes[0],
-                                                                     Local_Nodes[1],
-                                                                     Local_Nodes[2],
-                                                                     Local_Nodes[3]);
+      bound[iMarker][nElemBound_Local[iMarker]] =
+          new CQuadrilateral(Local_Nodes[0], Local_Nodes[1], Local_Nodes[2], Local_Nodes[3]);
 
       /*--- Increment our counters for this marker and element type. ---*/
 
-      nElemBound_Local[iMarker]++; iElem_Quad++;
+      nElemBound_Local[iMarker]++;
+      iElem_Quad++;
 
       BoundQuad_List[iMarker].push_back(Elem_ID_BoundQuad[iElem]);
-
     }
   }
 
   /*--- Store total number of each boundary element type ---*/
 
-  nelem_edge_bound     = iElem_Line;
+  nelem_edge_bound = iElem_Line;
   nelem_triangle_bound = iElem_Tria;
-  nelem_quad_bound     = iElem_Quad;
+  nelem_quad_bound = iElem_Quad;
 
   /*--- Set some auxiliary information on a per-marker basis. ---*/
 
   for (iMarker = 0; iMarker < nMarker; iMarker++) {
-
     Global_Marker = Marker_Local_to_Global[iMarker];
 
     /*--- Now each domain has the right information ---*/
 
     string Grid_Marker = config->GetMarker_All_TagBound(Global_Marker);
-    short SendRecv     = config->GetMarker_All_SendRecv(Global_Marker);
+    short SendRecv = config->GetMarker_All_SendRecv(Global_Marker);
 
     Tag_to_Marker[iMarker] = Marker_Tags[Global_Marker];
     Marker_All_SendRecv[iMarker] = SendRecv;
@@ -2835,49 +2663,41 @@ void CPhysicalGeometry::LoadSurfaceElements(CConfig *config, CGeometry *geometry
 
     config->SetMarker_All_TagBound(iMarker, Tag_to_Marker[iMarker]);
     config->SetMarker_All_SendRecv(iMarker, Marker_All_SendRecv[iMarker]);
-
   }
 
   /*--- Initialize pointers for turbomachinery computations  ---*/
 
-  nSpanWiseSections       = new unsigned short[2] ();
-  SpanWiseValue           = new su2double*[2] ();
-
-  nSpanSectionsByMarker   = new unsigned short[nMarker] ();
-  nVertexSpan             = new long* [nMarker] ();
-  nTotVertexSpan          = new unsigned long* [nMarker] ();
-  turbovertex             = new CTurboVertex***[nMarker] ();
-  AverageTurboNormal      = new su2double**[nMarker] ();
-  AverageNormal           = new su2double**[nMarker] ();
-  AverageGridVel          = new su2double**[nMarker] ();
-  AverageTangGridVel      = new su2double*[nMarker] ();
-  SpanArea                = new su2double*[nMarker] ();
-  TurboRadius             = new su2double*[nMarker] ();
-  MaxAngularCoord         = new su2double*[nMarker] ();
-  MinAngularCoord         = new su2double*[nMarker] ();
-  MinRelAngularCoord      = new su2double*[nMarker] ();
+  nSpanWiseSections = new unsigned short[2]();
+  SpanWiseValue = new su2double*[2]();
+
+  nSpanSectionsByMarker = new unsigned short[nMarker]();
+  nVertexSpan = new long*[nMarker]();
+  nTotVertexSpan = new unsigned long*[nMarker]();
+  turbovertex = new CTurboVertex***[nMarker]();
+  AverageTurboNormal = new su2double**[nMarker]();
+  AverageNormal = new su2double**[nMarker]();
+  AverageGridVel = new su2double**[nMarker]();
+  AverageTangGridVel = new su2double*[nMarker]();
+  SpanArea = new su2double*[nMarker]();
+  TurboRadius = new su2double*[nMarker]();
+  MaxAngularCoord = new su2double*[nMarker]();
+  MinAngularCoord = new su2double*[nMarker]();
+  MinRelAngularCoord = new su2double*[nMarker]();
 
   /*--- Initialize pointers for turbomachinery performance computation  ---*/
 
-  nTurboPerf     = config->GetnMarker_TurboPerformance();
-  TangGridVelIn  = new su2double*[nTurboPerf] ();
-  SpanAreaIn     = new su2double*[nTurboPerf] ();
-  TurboRadiusIn  = new su2double*[nTurboPerf] ();
-  TangGridVelOut = new su2double*[nTurboPerf] ();
-  SpanAreaOut    = new su2double*[nTurboPerf] ();
-  TurboRadiusOut = new su2double*[nTurboPerf] ();
-
+  nTurboPerf = config->GetnMarker_TurboPerformance();
+  TangGridVelIn = new su2double*[nTurboPerf]();
+  SpanAreaIn = new su2double*[nTurboPerf]();
+  TurboRadiusIn = new su2double*[nTurboPerf]();
+  TangGridVelOut = new su2double*[nTurboPerf]();
+  SpanAreaOut = new su2double*[nTurboPerf]();
+  TurboRadiusOut = new su2double*[nTurboPerf]();
 }
 
-void CPhysicalGeometry::InitiateCommsAll(void *bufSend,
-                                         const int *nElemSend,
-                                         SU2_MPI::Request *sendReq,
-                                         void *bufRecv,
-                                         const int *nElemRecv,
-                                         SU2_MPI::Request *recvReq,
-                                         unsigned short countPerElem,
+void CPhysicalGeometry::InitiateCommsAll(void* bufSend, const int* nElemSend, SU2_MPI::Request* sendReq, void* bufRecv,
+                                         const int* nElemRecv, SU2_MPI::Request* recvReq, unsigned short countPerElem,
                                          unsigned short commType) {
-
   /*--- Local variables ---*/
 
   int iMessage, iProc, offset, nElem, count, source, dest, tag;
@@ -2886,64 +2706,56 @@ void CPhysicalGeometry::InitiateCommsAll(void *bufSend,
 
   iMessage = 0;
   for (iProc = 0; iProc < size; iProc++) {
-
     /*--- Post recv's only if another proc is sending us data. We do
      not communicate with ourselves or post recv's for zero length
      messages to keep overhead down. ---*/
 
-    if ((nElemRecv[iProc+1] > nElemRecv[iProc]) && (iProc != rank)) {
-
+    if ((nElemRecv[iProc + 1] > nElemRecv[iProc]) && (iProc != rank)) {
       /*--- Compute our location in the recv buffer. ---*/
 
-      offset = countPerElem*nElemRecv[iProc];
+      offset = countPerElem * nElemRecv[iProc];
 
       /*--- Take advantage of cumulative storage format to get the number
        of elems that we need to recv. ---*/
 
-      nElem = nElemRecv[iProc+1] - nElemRecv[iProc];
+      nElem = nElemRecv[iProc + 1] - nElemRecv[iProc];
 
       /*--- Total count can include multiple pieces of data per element. ---*/
 
-      count = countPerElem*nElem;
+      count = countPerElem * nElem;
 
       /*--- Post non-blocking recv for this proc. ---*/
 
-      source = iProc; tag = iProc + 1;
+      source = iProc;
+      tag = iProc + 1;
 
       switch (commType) {
         case COMM_TYPE_DOUBLE:
-          SU2_MPI::Irecv(&(static_cast<su2double*>(bufRecv)[offset]),
-                         count, MPI_DOUBLE, source, tag, SU2_MPI::GetComm(),
-                         &(recvReq[iMessage]));
+          SU2_MPI::Irecv(&(static_cast<su2double*>(bufRecv)[offset]), count, MPI_DOUBLE, source, tag,
+                         SU2_MPI::GetComm(), &(recvReq[iMessage]));
           break;
         case COMM_TYPE_UNSIGNED_LONG:
-          SU2_MPI::Irecv(&(static_cast<unsigned long*>(bufRecv)[offset]),
-                         count, MPI_UNSIGNED_LONG, source, tag, SU2_MPI::GetComm(),
-                         &(recvReq[iMessage]));
+          SU2_MPI::Irecv(&(static_cast<unsigned long*>(bufRecv)[offset]), count, MPI_UNSIGNED_LONG, source, tag,
+                         SU2_MPI::GetComm(), &(recvReq[iMessage]));
           break;
         case COMM_TYPE_LONG:
-          SU2_MPI::Irecv(&(static_cast<long*>(bufRecv)[offset]),
-                         count, MPI_LONG, source, tag, SU2_MPI::GetComm(),
+          SU2_MPI::Irecv(&(static_cast<long*>(bufRecv)[offset]), count, MPI_LONG, source, tag, SU2_MPI::GetComm(),
                          &(recvReq[iMessage]));
           break;
         case COMM_TYPE_UNSIGNED_SHORT:
-          SU2_MPI::Irecv(&(static_cast<unsigned short*>(bufRecv)[offset]),
-                         count, MPI_UNSIGNED_SHORT, source, tag, SU2_MPI::GetComm(),
-                         &(recvReq[iMessage]));
+          SU2_MPI::Irecv(&(static_cast<unsigned short*>(bufRecv)[offset]), count, MPI_UNSIGNED_SHORT, source, tag,
+                         SU2_MPI::GetComm(), &(recvReq[iMessage]));
           break;
         case COMM_TYPE_CHAR:
-          SU2_MPI::Irecv(&(static_cast<char*>(bufRecv)[offset]),
-                         count, MPI_CHAR, source, tag, SU2_MPI::GetComm(),
+          SU2_MPI::Irecv(&(static_cast<char*>(bufRecv)[offset]), count, MPI_CHAR, source, tag, SU2_MPI::GetComm(),
                          &(recvReq[iMessage]));
           break;
         case COMM_TYPE_SHORT:
-          SU2_MPI::Irecv(&(static_cast<short*>(bufRecv)[offset]),
-                         count, MPI_SHORT, source, tag, SU2_MPI::GetComm(),
+          SU2_MPI::Irecv(&(static_cast<short*>(bufRecv)[offset]), count, MPI_SHORT, source, tag, SU2_MPI::GetComm(),
                          &(recvReq[iMessage]));
           break;
         case COMM_TYPE_INT:
-          SU2_MPI::Irecv(&(static_cast<int*>(bufRecv)[offset]),
-                         count, MPI_INT, source, tag, SU2_MPI::GetComm(),
+          SU2_MPI::Irecv(&(static_cast<int*>(bufRecv)[offset]), count, MPI_INT, source, tag, SU2_MPI::GetComm(),
                          &(recvReq[iMessage]));
           break;
         default:
@@ -2953,7 +2765,6 @@ void CPhysicalGeometry::InitiateCommsAll(void *bufSend,
       /*--- Increment message counter. ---*/
 
       iMessage++;
-
     }
   }
 
@@ -2961,64 +2772,56 @@ void CPhysicalGeometry::InitiateCommsAll(void *bufSend,
 
   iMessage = 0;
   for (iProc = 0; iProc < size; iProc++) {
-
     /*--- Post sends only if we are sending another proc data. We do
      not communicate with ourselves or post sends for zero length
      messages to keep overhead down. ---*/
 
-    if ((nElemSend[iProc+1] > nElemSend[iProc]) && (iProc != rank)) {
-
+    if ((nElemSend[iProc + 1] > nElemSend[iProc]) && (iProc != rank)) {
       /*--- Compute our location in the send buffer. ---*/
 
-      offset = countPerElem*nElemSend[iProc];
+      offset = countPerElem * nElemSend[iProc];
 
       /*--- Take advantage of cumulative storage format to get the number
        of elems that we need to send. ---*/
 
-      nElem = nElemSend[iProc+1] - nElemSend[iProc];
+      nElem = nElemSend[iProc + 1] - nElemSend[iProc];
 
       /*--- Total count can include multiple pieces of data per element. ---*/
 
-      count = countPerElem*nElem;
+      count = countPerElem * nElem;
 
       /*--- Post non-blocking send for this proc. ---*/
 
-      dest = iProc; tag = rank + 1;
+      dest = iProc;
+      tag = rank + 1;
 
       switch (commType) {
         case COMM_TYPE_DOUBLE:
-          SU2_MPI::Isend(&(static_cast<su2double*>(bufSend)[offset]),
-                         count, MPI_DOUBLE, dest, tag, SU2_MPI::GetComm(),
+          SU2_MPI::Isend(&(static_cast<su2double*>(bufSend)[offset]), count, MPI_DOUBLE, dest, tag, SU2_MPI::GetComm(),
                          &(sendReq[iMessage]));
           break;
         case COMM_TYPE_UNSIGNED_LONG:
-          SU2_MPI::Isend(&(static_cast<unsigned long*>(bufSend)[offset]),
-                         count, MPI_UNSIGNED_LONG, dest, tag, SU2_MPI::GetComm(),
-                         &(sendReq[iMessage]));
+          SU2_MPI::Isend(&(static_cast<unsigned long*>(bufSend)[offset]), count, MPI_UNSIGNED_LONG, dest, tag,
+                         SU2_MPI::GetComm(), &(sendReq[iMessage]));
           break;
         case COMM_TYPE_LONG:
-          SU2_MPI::Isend(&(static_cast<long*>(bufSend)[offset]),
-                         count, MPI_LONG, dest, tag, SU2_MPI::GetComm(),
+          SU2_MPI::Isend(&(static_cast<long*>(bufSend)[offset]), count, MPI_LONG, dest, tag, SU2_MPI::GetComm(),
                          &(sendReq[iMessage]));
           break;
         case COMM_TYPE_UNSIGNED_SHORT:
-          SU2_MPI::Isend(&(static_cast<unsigned short*>(bufSend)[offset]),
-                         count, MPI_UNSIGNED_SHORT, dest, tag, SU2_MPI::GetComm(),
-                         &(sendReq[iMessage]));
+          SU2_MPI::Isend(&(static_cast<unsigned short*>(bufSend)[offset]), count, MPI_UNSIGNED_SHORT, dest, tag,
+                         SU2_MPI::GetComm(), &(sendReq[iMessage]));
           break;
         case COMM_TYPE_CHAR:
-          SU2_MPI::Isend(&(static_cast<char*>(bufSend)[offset]),
-                         count, MPI_CHAR, dest, tag, SU2_MPI::GetComm(),
+          SU2_MPI::Isend(&(static_cast<char*>(bufSend)[offset]), count, MPI_CHAR, dest, tag, SU2_MPI::GetComm(),
                          &(sendReq[iMessage]));
           break;
         case COMM_TYPE_SHORT:
-          SU2_MPI::Isend(&(static_cast<short*>(bufSend)[offset]),
-                         count, MPI_SHORT, dest, tag, SU2_MPI::GetComm(),
+          SU2_MPI::Isend(&(static_cast<short*>(bufSend)[offset]), count, MPI_SHORT, dest, tag, SU2_MPI::GetComm(),
                          &(sendReq[iMessage]));
           break;
         case COMM_TYPE_INT:
-          SU2_MPI::Isend(&(static_cast<int*>(bufSend)[offset]),
-                         count, MPI_INT, dest, tag, SU2_MPI::GetComm(),
+          SU2_MPI::Isend(&(static_cast<int*>(bufSend)[offset]), count, MPI_INT, dest, tag, SU2_MPI::GetComm(),
                          &(sendReq[iMessage]));
           break;
         default:
@@ -3028,17 +2831,11 @@ void CPhysicalGeometry::InitiateCommsAll(void *bufSend,
       /*--- Increment message counter. ---*/
 
       iMessage++;
-
     }
   }
-
 }
 
-void CPhysicalGeometry::CompleteCommsAll(int nSends,
-                                         SU2_MPI::Request *sendReq,
-                                         int nRecvs,
-                                         SU2_MPI::Request *recvReq) {
-
+void CPhysicalGeometry::CompleteCommsAll(int nSends, SU2_MPI::Request* sendReq, int nRecvs, SU2_MPI::Request* recvReq) {
   /*--- Local variables ---*/
 
   int ind, iSend, iRecv;
@@ -3046,18 +2843,14 @@ void CPhysicalGeometry::CompleteCommsAll(int nSends,
 
   /*--- Wait for the non-blocking sends to complete. ---*/
 
-  for (iSend = 0; iSend < nSends; iSend++)
-    SU2_MPI::Waitany(nSends, sendReq, &ind, &status);
+  for (iSend = 0; iSend < nSends; iSend++) SU2_MPI::Waitany(nSends, sendReq, &ind, &status);
 
   /*--- Wait for the non-blocking recvs to complete. ---*/
 
-  for (iRecv = 0; iRecv < nRecvs; iRecv++)
-    SU2_MPI::Waitany(nRecvs, recvReq, &ind, &status);
-
+  for (iRecv = 0; iRecv < nRecvs; iRecv++) SU2_MPI::Waitany(nRecvs, recvReq, &ind, &status);
 }
 
 void CPhysicalGeometry::PrepareOffsets(unsigned long val_npoint_global) {
-
   /*--- Compute the number of points that will be on each processor.
    This is a linear partitioning with the addition of a simple load
    balancing for any remainder points. ---*/
@@ -3065,11 +2858,11 @@ void CPhysicalGeometry::PrepareOffsets(unsigned long val_npoint_global) {
   if (beg_node == nullptr) beg_node = new unsigned long[size];
   if (end_node == nullptr) end_node = new unsigned long[size];
 
-  if (nPointLinear     == nullptr) nPointLinear     = new unsigned long[size];
-  if (nPointCumulative == nullptr) nPointCumulative = new unsigned long[size+1];
+  if (nPointLinear == nullptr) nPointLinear = new unsigned long[size];
+  if (nPointCumulative == nullptr) nPointCumulative = new unsigned long[size + 1];
 
-  unsigned long quotient = val_npoint_global/size;
-  int remainder = int(val_npoint_global%size);
+  unsigned long quotient = val_npoint_global / size;
+  int remainder = int(val_npoint_global % size);
   for (int ii = 0; ii < size; ii++) {
     nPointLinear[ii] = quotient + int(ii < remainder);
   }
@@ -3082,63 +2875,54 @@ void CPhysicalGeometry::PrepareOffsets(unsigned long val_npoint_global) {
   end_node[0] = beg_node[0] + nPointLinear[0];
   nPointCumulative[0] = 0;
   for (int iProc = 1; iProc < size; iProc++) {
-    beg_node[iProc] = end_node[iProc-1];
+    beg_node[iProc] = end_node[iProc - 1];
     end_node[iProc] = beg_node[iProc] + nPointLinear[iProc];
-    nPointCumulative[iProc] = nPointCumulative[iProc-1] + nPointLinear[iProc-1];
+    nPointCumulative[iProc] = nPointCumulative[iProc - 1] + nPointLinear[iProc - 1];
   }
   nPointCumulative[size] = val_npoint_global;
-
 }
 
 unsigned long CPhysicalGeometry::GetLinearPartition(unsigned long val_global_index) {
-
   unsigned long iProcessor = 0;
 
   /*--- Initial guess ---*/
 
-  iProcessor = val_global_index/nPointLinear[0];
+  iProcessor = val_global_index / nPointLinear[0];
 
   /*--- Guard against going over size. ---*/
 
-  if (iProcessor >= (unsigned long)size)
-    iProcessor = (unsigned long)size-1;
+  if (iProcessor >= (unsigned long)size) iProcessor = (unsigned long)size - 1;
 
   /*--- Move up or down until we find the processor. ---*/
 
   if (val_global_index >= nPointCumulative[iProcessor])
-    while(val_global_index >= nPointCumulative[iProcessor+1])
-      iProcessor++;
+    while (val_global_index >= nPointCumulative[iProcessor + 1]) iProcessor++;
   else
-    while(val_global_index < nPointCumulative[iProcessor])
-      iProcessor--;
+    while (val_global_index < nPointCumulative[iProcessor]) iProcessor--;
 
   return iProcessor;
-
 }
 
-void CPhysicalGeometry::SortAdjacency(const CConfig *config) {
-
+void CPhysicalGeometry::SortAdjacency(const CConfig* config) {
 #ifdef HAVE_MPI
 #ifdef HAVE_PARMETIS
 
-  if ((rank == MASTER_NODE) && (size > SINGLE_NODE))
-    cout << "Executing the partitioning functions." << endl;
+  if ((rank == MASTER_NODE) && (size > SINGLE_NODE)) cout << "Executing the partitioning functions." << endl;
 
   /*--- Post process the adjacency information in order to get it into the
    CSR format before sending the data to ParMETIS. We need to remove
    repeats and adjust the size of the array for each local node. ---*/
 
-  if ((rank == MASTER_NODE) && (size > SINGLE_NODE))
-    cout << "Building the graph adjacency structure." << endl;
+  if ((rank == MASTER_NODE) && (size > SINGLE_NODE)) cout << "Building the graph adjacency structure." << endl;
 
   /*--- Create a partitioner object so we can transform the global
    index values stored in the elements to a local index. ---*/
 
-  CLinearPartitioner pointPartitioner(Global_nPointDomain,0);
+  CLinearPartitioner pointPartitioner(Global_nPointDomain, 0);
 
   /*--- We can already create the array that indexes the adjacency. ---*/
 
-  xadj.resize(pointPartitioner.GetSizeOnRank(rank)+1);
+  xadj.resize(pointPartitioner.GetSizeOnRank(rank) + 1);
   xadj[0] = 0;
 
   /*--- Here, we transfer the adjacency information from a multi-dim vector
@@ -3172,7 +2956,7 @@ void CPhysicalGeometry::SortAdjacency(const CConfig *config) {
     for (auto jPoint : neighbors) adjacency.push_back(jPoint);
 
     /*--- Increment the starting index for the next point (CSR). ---*/
-    xadj[iPoint+1] = xadj[iPoint] + neighbors.size();
+    xadj[iPoint + 1] = xadj[iPoint] + neighbors.size();
     ++iPoint;
   }
 
@@ -3182,28 +2966,29 @@ void CPhysicalGeometry::SortAdjacency(const CConfig *config) {
 
 #endif
 #endif
-
 }
 
-void CPhysicalGeometry::SetSendReceive(const CConfig *config) {
-
+void CPhysicalGeometry::SetSendReceive(const CConfig* config) {
   unsigned short Counter_Send, Counter_Receive, iMarkerSend, iMarkerReceive;
   unsigned long iVertex, LocalNode;
   unsigned short nMarker_Max = config->GetnMarker_Max();
-  unsigned long  iPoint, jPoint, iElem, nDomain, iDomain, jDomain;
-  unsigned long *nVertexDomain = new unsigned long[nMarker_Max];
+  unsigned long iPoint, jPoint, iElem, nDomain, iDomain, jDomain;
+  unsigned long* nVertexDomain = new unsigned long[nMarker_Max];
   unsigned short iNode, jNode;
   vector<unsigned long>::iterator it;
 
-  vector<vector<unsigned long> > SendTransfLocal;       /*!< \brief Vector to store the type of transformation for this send point. */
-  vector<vector<unsigned long> > ReceivedTransfLocal;   /*!< \brief Vector to store the type of transformation for this received point. */
-  vector<vector<unsigned long> > SendDomainLocal;       /*!< \brief SendDomain[from domain][to domain] and return the point index of the node that must me sended. */
-  vector<vector<unsigned long> > ReceivedDomainLocal;   /*!< \brief SendDomain[from domain][to domain] and return the point index of the node that must me sended. */
+  vector<vector<unsigned long> >
+      SendTransfLocal; /*!< \brief Vector to store the type of transformation for this send point. */
+  vector<vector<unsigned long> >
+      ReceivedTransfLocal; /*!< \brief Vector to store the type of transformation for this received point. */
+  vector<vector<unsigned long> > SendDomainLocal; /*!< \brief SendDomain[from domain][to domain] and return the point
+                                                     index of the node that must me sended. */
+  vector<vector<unsigned long> > ReceivedDomainLocal; /*!< \brief SendDomain[from domain][to domain] and return the
+                                                         point index of the node that must me sended. */
 
   unordered_map<unsigned long, unsigned long>::const_iterator MI;
 
-  if (rank == MASTER_NODE && size > SINGLE_NODE)
-    cout << "Establishing MPI communication patterns." << endl;
+  if (rank == MASTER_NODE && size > SINGLE_NODE) cout << "Establishing MPI communication patterns." << endl;
 
   nDomain = size;
 
@@ -3218,21 +3003,18 @@ void CPhysicalGeometry::SetSendReceive(const CConfig *config) {
 
   for (iElem = 0; iElem < nElem; iElem++) {
     for (iNode = 0; iNode < elem[iElem]->GetnNodes(); iNode++) {
-
-      iPoint  = elem[iElem]->GetNode(iNode);
+      iPoint = elem[iElem]->GetNode(iNode);
       iDomain = nodes->GetColor(iPoint);
 
-      if (iDomain == (unsigned long) rank) {
+      if (iDomain == (unsigned long)rank) {
         for (jNode = 0; jNode < elem[iElem]->GetnNodes(); jNode++) {
-
-          jPoint  = elem[iElem]->GetNode(jNode);
+          jPoint = elem[iElem]->GetNode(jNode);
           jDomain = nodes->GetColor(jPoint);
 
           /*--- If one of the neighbors is a different color and connected
            by an edge, then we add them to the list. ---*/
 
           if (iDomain != jDomain) {
-
             /*--- We send from iDomain to jDomain the value of iPoint,
              we save the global value becuase we need to sort the lists. ---*/
 
@@ -3242,7 +3024,6 @@ void CPhysicalGeometry::SetSendReceive(const CConfig *config) {
              we save the global value becuase we need to sort the lists. ---*/
 
             ReceivedDomainLocal[jDomain].push_back(Local_to_Global_Point[jPoint]);
-
           }
         }
       }
@@ -3263,7 +3044,7 @@ void CPhysicalGeometry::SetSendReceive(const CConfig *config) {
 
   for (iDomain = 0; iDomain < nDomain; iDomain++) {
     sort(ReceivedDomainLocal[iDomain].begin(), ReceivedDomainLocal[iDomain].end());
-    it = unique( ReceivedDomainLocal[iDomain].begin(), ReceivedDomainLocal[iDomain].end());
+    it = unique(ReceivedDomainLocal[iDomain].begin(), ReceivedDomainLocal[iDomain].end());
     ReceivedDomainLocal[iDomain].resize(it - ReceivedDomainLocal[iDomain].begin());
   }
 
@@ -3271,13 +3052,11 @@ void CPhysicalGeometry::SetSendReceive(const CConfig *config) {
    number of points in the simulation  ---*/
   Max_GlobalPoint = 0;
   for (iPoint = 0; iPoint < nPoint; iPoint++) {
-    if (Local_to_Global_Point[iPoint] > (long)Max_GlobalPoint)
-      Max_GlobalPoint = Local_to_Global_Point[iPoint];
+    if (Local_to_Global_Point[iPoint] > (long)Max_GlobalPoint) Max_GlobalPoint = Local_to_Global_Point[iPoint];
   }
 
   /*--- Set the value of some of the points ---*/
-  for (iPoint = 0; iPoint < nPoint; iPoint++)
-    Global_to_Local_Point[Local_to_Global_Point[iPoint]] = iPoint;
+  for (iPoint = 0; iPoint < nPoint; iPoint++) Global_to_Local_Point[Local_to_Global_Point[iPoint]] = iPoint;
 
   /*--- Add the new MPI send boundaries, reset the transformation,
    and save the local value. ---*/
@@ -3286,11 +3065,11 @@ void CPhysicalGeometry::SetSendReceive(const CConfig *config) {
     if (SendDomainLocal[iDomain].size() != 0) {
       nVertexDomain[nMarker] = SendDomainLocal[iDomain].size();
       for (iVertex = 0; iVertex < nVertexDomain[nMarker]; iVertex++) {
-
         MI = Global_to_Local_Point.find(SendDomainLocal[iDomain][iVertex]);
         if (MI != Global_to_Local_Point.end())
           iPoint = Global_to_Local_Point[SendDomainLocal[iDomain][iVertex]];
-        else iPoint = std::numeric_limits<unsigned long>::max();
+        else
+          iPoint = std::numeric_limits<unsigned long>::max();
 
         SendDomainLocal[iDomain][iVertex] = iPoint;
         SendTransfLocal[iDomain].push_back(0);
@@ -3306,11 +3085,11 @@ void CPhysicalGeometry::SetSendReceive(const CConfig *config) {
     if (ReceivedDomainLocal[iDomain].size() != 0) {
       nVertexDomain[nMarker] = ReceivedDomainLocal[iDomain].size();
       for (iVertex = 0; iVertex < nVertexDomain[nMarker]; iVertex++) {
-
         MI = Global_to_Local_Point.find(ReceivedDomainLocal[iDomain][iVertex]);
         if (MI != Global_to_Local_Point.end())
           iPoint = Global_to_Local_Point[ReceivedDomainLocal[iDomain][iVertex]];
-        else iPoint = std::numeric_limits<unsigned long>::max();
+        else
+          iPoint = std::numeric_limits<unsigned long>::max();
 
         ReceivedDomainLocal[iDomain][iVertex] = iPoint;
         ReceivedTransfLocal[iDomain].push_back(0);
@@ -3322,14 +3101,15 @@ void CPhysicalGeometry::SetSendReceive(const CConfig *config) {
   }
 
   /*--- First compute the Send/Receive boundaries ---*/
-  Counter_Send = 0;   Counter_Receive = 0;
+  Counter_Send = 0;
+  Counter_Receive = 0;
   for (iDomain = 0; iDomain < nDomain; iDomain++)
     if (SendDomainLocal[iDomain].size() != 0) Counter_Send++;
 
   for (iDomain = 0; iDomain < nDomain; iDomain++)
     if (ReceivedDomainLocal[iDomain].size() != 0) Counter_Receive++;
 
-  iMarkerSend    = nMarker - Counter_Send - Counter_Receive;
+  iMarkerSend = nMarker - Counter_Send - Counter_Receive;
   iMarkerReceive = nMarker - Counter_Receive;
 
   /*--- First we do the send ---*/
@@ -3340,7 +3120,7 @@ void CPhysicalGeometry::SetSendReceive(const CConfig *config) {
         bound[iMarkerSend][iVertex] = new CVertexMPI(LocalNode);
         bound[iMarkerSend][iVertex]->SetRotation_Type(SendTransfLocal[iDomain][iVertex]);
       }
-      Marker_All_SendRecv[iMarkerSend] = iDomain+1;
+      Marker_All_SendRecv[iMarkerSend] = iDomain + 1;
       iMarkerSend++;
     }
   }
@@ -3353,28 +3133,27 @@ void CPhysicalGeometry::SetSendReceive(const CConfig *config) {
         bound[iMarkerReceive][iVertex] = new CVertexMPI(LocalNode);
         bound[iMarkerReceive][iVertex]->SetRotation_Type(ReceivedTransfLocal[iDomain][iVertex]);
       }
-      Marker_All_SendRecv[iMarkerReceive] = -(iDomain+1);
+      Marker_All_SendRecv[iMarkerReceive] = -(iDomain + 1);
       iMarkerReceive++;
     }
   }
 
   /*--- Free memory ---*/
 
-  delete [] nVertexDomain;
-
+  delete[] nVertexDomain;
 }
 
-void CPhysicalGeometry::SetBoundaries(CConfig *config) {
-
+void CPhysicalGeometry::SetBoundaries(CConfig* config) {
   unsigned long iElem_Bound, TotalElem, *nElem_Bound_Copy, iVertex_;
   string Grid_Marker;
-  unsigned short iDomain, nDomain, iMarkersDomain, iLoop, *DomainCount, nMarker_Physical, Duplicate_SendReceive, *DomainSendCount,
-                 **DomainSendMarkers, *DomainReceiveCount, **DomainReceiveMarkers, nMarker_SendRecv, iMarker, iMarker_;
+  unsigned short iDomain, nDomain, iMarkersDomain, iLoop, *DomainCount, nMarker_Physical, Duplicate_SendReceive,
+      *DomainSendCount, **DomainSendMarkers, *DomainReceiveCount, **DomainReceiveMarkers, nMarker_SendRecv, iMarker,
+      iMarker_;
   CPrimalGrid*** bound_Copy;
-  short *Marker_All_SendRecv_Copy;
+  short* Marker_All_SendRecv_Copy;
   bool CheckStart;
 
-  nDomain = size+1;
+  nDomain = size + 1;
 
   /*--- Count the number of physical markers
    in the boundaries ---*/
@@ -3391,19 +3170,16 @@ void CPhysicalGeometry::SetBoundaries(CConfig *config) {
 
   Duplicate_SendReceive = 0;
   for (iLoop = 0; iLoop < 2; iLoop++) {
+    DomainCount = new unsigned short[nDomain];
 
-    DomainCount = new unsigned short [nDomain];
-
-    for (iDomain = 0; iDomain < nDomain; iDomain++)
-      DomainCount[iDomain] = 0;
+    for (iDomain = 0; iDomain < nDomain; iDomain++) DomainCount[iDomain] = 0;
 
     if (iLoop == 0) {
       for (iDomain = 0; iDomain < nDomain; iDomain++)
         for (iMarker = 0; iMarker < nMarker; iMarker++)
           if (bound[iMarker][0]->GetVTK_Type() == VERTEX)
             if (Marker_All_SendRecv[iMarker] == iDomain) DomainCount[iDomain]++;
-    }
-    else {
+    } else {
       for (iDomain = 0; iDomain < nDomain; iDomain++)
         for (iMarker = 0; iMarker < nMarker; iMarker++)
           if (bound[iMarker][0]->GetVTK_Type() == VERTEX)
@@ -3413,21 +3189,20 @@ void CPhysicalGeometry::SetBoundaries(CConfig *config) {
     for (iDomain = 0; iDomain < nDomain; iDomain++)
       if (DomainCount[iDomain] > 1) Duplicate_SendReceive++;
 
-    delete [] DomainCount;
-
+    delete[] DomainCount;
   }
 
-  DomainSendCount = new unsigned short [nDomain];
-  DomainSendMarkers = new unsigned short *[nDomain];
-  DomainReceiveCount = new unsigned short [nDomain];
-  DomainReceiveMarkers = new unsigned short *[nDomain];
+  DomainSendCount = new unsigned short[nDomain];
+  DomainSendMarkers = new unsigned short*[nDomain];
+  DomainReceiveCount = new unsigned short[nDomain];
+  DomainReceiveMarkers = new unsigned short*[nDomain];
 
   for (iDomain = 0; iDomain < nDomain; iDomain++) {
     DomainSendCount[iDomain] = 0;
-    DomainSendMarkers[iDomain] = new unsigned short [nMarker];
+    DomainSendMarkers[iDomain] = new unsigned short[nMarker];
 
     DomainReceiveCount[iDomain] = 0;
-    DomainReceiveMarkers[iDomain] = new unsigned short [nMarker];
+    DomainReceiveMarkers[iDomain] = new unsigned short[nMarker];
   }
 
   for (iDomain = 0; iDomain < nDomain; iDomain++) {
@@ -3450,8 +3225,8 @@ void CPhysicalGeometry::SetBoundaries(CConfig *config) {
 
   nMarker_SendRecv = nMarker - nMarker_Physical - Duplicate_SendReceive;
   bound_Copy = new CPrimalGrid**[nMarker_Physical + nMarker_SendRecv];
-  nElem_Bound_Copy = new unsigned long [nMarker_Physical + nMarker_SendRecv];
-  Marker_All_SendRecv_Copy = new short [nMarker_Physical + nMarker_SendRecv];
+  nElem_Bound_Copy = new unsigned long[nMarker_Physical + nMarker_SendRecv];
+  Marker_All_SendRecv_Copy = new short[nMarker_Physical + nMarker_SendRecv];
   iMarker_ = nMarker_Physical;
   iVertex_ = 0;
   CheckStart = false;
@@ -3460,31 +3235,27 @@ void CPhysicalGeometry::SetBoundaries(CConfig *config) {
 
   for (iMarker = 0; iMarker < nMarker; iMarker++) {
     if (bound[iMarker][0]->GetVTK_Type() != VERTEX) {
-
       nElem_Bound_Copy[iMarker] = nElem_Bound[iMarker];
-      bound_Copy[iMarker] = new CPrimalGrid* [nElem_Bound[iMarker]];
+      bound_Copy[iMarker] = new CPrimalGrid*[nElem_Bound[iMarker]];
 
       for (iElem_Bound = 0; iElem_Bound < nElem_Bound[iMarker]; iElem_Bound++) {
         if (bound[iMarker][iElem_Bound]->GetVTK_Type() == LINE)
-          bound_Copy[iMarker][iElem_Bound] = new CLine(bound[iMarker][iElem_Bound]->GetNode(0),
-                                                       bound[iMarker][iElem_Bound]->GetNode(1));
+          bound_Copy[iMarker][iElem_Bound] =
+              new CLine(bound[iMarker][iElem_Bound]->GetNode(0), bound[iMarker][iElem_Bound]->GetNode(1));
         if (bound[iMarker][iElem_Bound]->GetVTK_Type() == TRIANGLE)
 
-          bound_Copy[iMarker][iElem_Bound] = new CTriangle(bound[iMarker][iElem_Bound]->GetNode(0),
-                                                           bound[iMarker][iElem_Bound]->GetNode(1),
-                                                           bound[iMarker][iElem_Bound]->GetNode(2));
+          bound_Copy[iMarker][iElem_Bound] =
+              new CTriangle(bound[iMarker][iElem_Bound]->GetNode(0), bound[iMarker][iElem_Bound]->GetNode(1),
+                            bound[iMarker][iElem_Bound]->GetNode(2));
         if (bound[iMarker][iElem_Bound]->GetVTK_Type() == QUADRILATERAL)
-          bound_Copy[iMarker][iElem_Bound] = new CQuadrilateral(bound[iMarker][iElem_Bound]->GetNode(0),
-                                                            bound[iMarker][iElem_Bound]->GetNode(1),
-                                                            bound[iMarker][iElem_Bound]->GetNode(2),
-                                                            bound[iMarker][iElem_Bound]->GetNode(3));
+          bound_Copy[iMarker][iElem_Bound] =
+              new CQuadrilateral(bound[iMarker][iElem_Bound]->GetNode(0), bound[iMarker][iElem_Bound]->GetNode(1),
+                                 bound[iMarker][iElem_Bound]->GetNode(2), bound[iMarker][iElem_Bound]->GetNode(3));
       }
     }
   }
 
-
   for (iDomain = 0; iDomain < nDomain; iDomain++) {
-
     /*--- Compute the total number of elements (adding all the
      boundaries with the same Send/Receive ---*/
 
@@ -3510,7 +3281,6 @@ void CPhysicalGeometry::SetBoundaries(CConfig *config) {
         bound_Copy[iMarker_][iVertex_]->SetRotation_Type(bound[iMarker][iElem_Bound]->GetRotation_Type());
         iVertex_++;
       }
-
     }
 
     /*--- Compute the total number of elements (adding all the
@@ -3527,7 +3297,6 @@ void CPhysicalGeometry::SetBoundaries(CConfig *config) {
       iVertex_ = 0;
       nElem_Bound_Copy[iMarker_] = TotalElem;
       bound_Copy[iMarker_] = new CPrimalGrid*[TotalElem];
-
     }
 
     for (iMarkersDomain = 0; iMarkersDomain < DomainReceiveCount[iDomain]; iMarkersDomain++) {
@@ -3539,29 +3308,25 @@ void CPhysicalGeometry::SetBoundaries(CConfig *config) {
         bound_Copy[iMarker_][iVertex_]->SetRotation_Type(bound[iMarker][iElem_Bound]->GetRotation_Type());
         iVertex_++;
       }
-
     }
-
   }
 
-  delete [] DomainSendCount;
-  for (iDomain = 0; iDomain < nDomain; iDomain++)
-    delete [] DomainSendMarkers[iDomain];
+  delete[] DomainSendCount;
+  for (iDomain = 0; iDomain < nDomain; iDomain++) delete[] DomainSendMarkers[iDomain];
   delete[] DomainSendMarkers;
 
-  delete [] DomainReceiveCount;
-  for (iDomain = 0; iDomain < nDomain; iDomain++)
-    delete [] DomainReceiveMarkers[iDomain];
+  delete[] DomainReceiveCount;
+  for (iDomain = 0; iDomain < nDomain; iDomain++) delete[] DomainReceiveMarkers[iDomain];
   delete[] DomainReceiveMarkers;
 
-   /*--- Deallocate the bound variables ---*/
+  /*--- Deallocate the bound variables ---*/
 
   for (iMarker = 0; iMarker < nMarker; iMarker++) {
-   for (iElem_Bound = 0; iElem_Bound < nElem_Bound[iMarker]; iElem_Bound++)
-     if (bound[iMarker][iElem_Bound] != nullptr) delete bound[iMarker][iElem_Bound];
-    if (bound[iMarker] != nullptr) delete [] bound[iMarker];
+    for (iElem_Bound = 0; iElem_Bound < nElem_Bound[iMarker]; iElem_Bound++)
+      if (bound[iMarker][iElem_Bound] != nullptr) delete bound[iMarker][iElem_Bound];
+    if (bound[iMarker] != nullptr) delete[] bound[iMarker];
   }
-  delete [] bound;
+  delete[] bound;
 
   /*--- Allocate the new bound variables, and set the number of markers ---*/
 
@@ -3582,12 +3347,10 @@ void CPhysicalGeometry::SetBoundaries(CConfig *config) {
 
   /*--- Update config information storing the boundary information in the right place ---*/
 
-  for (iMarker = 0 ; iMarker < nMarker; iMarker++) {
-
+  for (iMarker = 0; iMarker < nMarker; iMarker++) {
     string Marker_Tag = config->GetMarker_All_TagBound(iMarker);
 
     if (Marker_Tag != "SEND_RECEIVE") {
-
       /*--- Update config information storing the boundary information in the right place ---*/
 
       Tag_to_Marker[config->GetMarker_CfgFile_TagBound(Marker_Tag)] = Marker_Tag;
@@ -3615,7 +3378,6 @@ void CPhysicalGeometry::SetBoundaries(CConfig *config) {
     /*--- Send-Receive boundaries definition ---*/
 
     else {
-
       config->SetMarker_All_KindBC(iMarker, SEND_RECEIVE);
       config->SetMarker_All_Monitoring(iMarker, NO);
       config->SetMarker_All_GeoEval(iMarker, NO);
@@ -3639,7 +3401,6 @@ void CPhysicalGeometry::SetBoundaries(CConfig *config) {
         if (config->GetMarker_All_SendRecv(iMarker) < 0)
           nodes->SetDomain(bound[iMarker][iElem_Bound]->GetNode(0), false);
       }
-
     }
 
     /*--- Loop over the surface element to set the boundaries ---*/
@@ -3657,39 +3418,41 @@ void CPhysicalGeometry::SetBoundaries(CConfig *config) {
             config->GetMarker_All_KindBC(iMarker) != PERIODIC_BOUNDARY)
           nodes->SetPhysicalBoundary(Point_Surface, true);
 
-        if (config->GetSolid_Wall(iMarker))
-          nodes->SetSolidBoundary(Point_Surface, true);
+        if (config->GetSolid_Wall(iMarker)) nodes->SetSolidBoundary(Point_Surface, true);
 
-        if (config->GetViscous_Wall(iMarker))
-          nodes->SetViscousBoundary(Point_Surface, true);
+        if (config->GetViscous_Wall(iMarker)) nodes->SetViscousBoundary(Point_Surface, true);
 
-        if (config->GetMarker_All_KindBC(iMarker) == PERIODIC_BOUNDARY)
-          nodes->SetPeriodicBoundary(Point_Surface, true);
+        if (config->GetMarker_All_KindBC(iMarker) == PERIODIC_BOUNDARY) nodes->SetPeriodicBoundary(Point_Surface, true);
       }
     }
-
   }
 
-  delete [] Marker_All_SendRecv_Copy;
-  delete [] nElem_Bound_Copy;
+  delete[] Marker_All_SendRecv_Copy;
+  delete[] nElem_Bound_Copy;
 }
 
-void CPhysicalGeometry::Read_Mesh_FVM(CConfig        *config,
-                                      string         val_mesh_filename,
-                                      unsigned short val_iZone,
+void CPhysicalGeometry::Read_Mesh_FVM(CConfig* config, string val_mesh_filename, unsigned short val_iZone,
                                       unsigned short val_nZone) {
-
   /*--- Initialize counters for local/global points & elements ---*/
 
-  Global_nPoint  = 0; Global_nPointDomain   = 0;
-  Global_nElem   = 0; Global_nElemDomain    = 0;
-  nelem_edge     = 0; Global_nelem_edge     = 0;
-  nelem_triangle = 0; Global_nelem_triangle = 0;
-  nelem_quad     = 0; Global_nelem_quad     = 0;
-  nelem_tetra    = 0; Global_nelem_tetra    = 0;
-  nelem_hexa     = 0; Global_nelem_hexa     = 0;
-  nelem_prism    = 0; Global_nelem_prism    = 0;
-  nelem_pyramid  = 0; Global_nelem_pyramid  = 0;
+  Global_nPoint = 0;
+  Global_nPointDomain = 0;
+  Global_nElem = 0;
+  Global_nElemDomain = 0;
+  nelem_edge = 0;
+  Global_nelem_edge = 0;
+  nelem_triangle = 0;
+  Global_nelem_triangle = 0;
+  nelem_quad = 0;
+  Global_nelem_quad = 0;
+  nelem_tetra = 0;
+  Global_nelem_tetra = 0;
+  nelem_hexa = 0;
+  Global_nelem_hexa = 0;
+  nelem_prism = 0;
+  Global_nelem_prism = 0;
+  nelem_pyramid = 0;
+  Global_nelem_pyramid = 0;
 
   /*--- Set the zone number from the input value. ---*/
 
@@ -3699,7 +3462,7 @@ void CPhysicalGeometry::Read_Mesh_FVM(CConfig        *config,
 
   unsigned short val_format = config->GetMesh_FileFormat();
 
-  CMeshReaderFVM *MeshFVM = nullptr;
+  CMeshReaderFVM* MeshFVM = nullptr;
   switch (val_format) {
     case SU2:
       MeshFVM = new CSU2ASCIIMeshReaderFVM(config, val_iZone, val_nZone);
@@ -3728,9 +3491,9 @@ void CPhysicalGeometry::Read_Mesh_FVM(CConfig        *config,
 
   /*--- Store the local and global number of nodes for this rank. ---*/
 
-  nPoint              = MeshFVM->GetNumberOfLocalPoints();
-  nPointDomain        = MeshFVM->GetNumberOfLocalPoints();
-  Global_nPoint       = MeshFVM->GetNumberOfGlobalPoints();
+  nPoint = MeshFVM->GetNumberOfLocalPoints();
+  nPointDomain = MeshFVM->GetNumberOfLocalPoints();
+  Global_nPoint = MeshFVM->GetNumberOfGlobalPoints();
   Global_nPointDomain = MeshFVM->GetNumberOfGlobalPoints();
 
   if ((rank == MASTER_NODE) && (size > SINGLE_NODE)) {
@@ -3741,8 +3504,8 @@ void CPhysicalGeometry::Read_Mesh_FVM(CConfig        *config,
 
   /*--- Store the local and global number of interior elements. ---*/
 
-  nElem              = MeshFVM->GetNumberOfLocalElements();
-  Global_nElem       = MeshFVM->GetNumberOfGlobalElements();
+  nElem = MeshFVM->GetNumberOfLocalElements();
+  Global_nElem = MeshFVM->GetNumberOfGlobalElements();
   Global_nElemDomain = MeshFVM->GetNumberOfGlobalElements();
 
   if ((rank == MASTER_NODE) && (size > SINGLE_NODE)) {
@@ -3754,9 +3517,9 @@ void CPhysicalGeometry::Read_Mesh_FVM(CConfig        *config,
   /*--- Load the grid points, volume elements, and surface elements
    from the mesh object into the proper SU2 data structures. ---*/
 
-  LoadLinearlyPartitionedPoints(config,         MeshFVM);
+  LoadLinearlyPartitionedPoints(config, MeshFVM);
   LoadLinearlyPartitionedVolumeElements(config, MeshFVM);
-  LoadUnpartitionedSurfaceElements(config,      MeshFVM);
+  LoadUnpartitionedSurfaceElements(config, MeshFVM);
 
   /*--- Prepare the nodal adjacency structures for ParMETIS. ---*/
 
@@ -3766,12 +3529,9 @@ void CPhysicalGeometry::Read_Mesh_FVM(CConfig        *config,
    delete the mesh reader object. ---*/
 
   delete MeshFVM;
-
 }
 
-void CPhysicalGeometry::LoadLinearlyPartitionedPoints(CConfig        *config,
-                                                      CMeshReaderFVM *mesh) {
-
+void CPhysicalGeometry::LoadLinearlyPartitionedPoints(CConfig* config, CMeshReaderFVM* mesh) {
   /*--- Get the linearly partitioned coordinates from the mesh object. ---*/
 
   const auto& gridCoords = mesh->GetLocalPointCoordinates();
@@ -3785,20 +3545,16 @@ void CPhysicalGeometry::LoadLinearlyPartitionedPoints(CConfig        *config,
    of the grid nodes, we can simply initialize the global index to
    the first node that lies on our rank and increment. ---*/
 
-  CLinearPartitioner pointPartitioner(Global_nPointDomain,0);
+  CLinearPartitioner pointPartitioner(Global_nPointDomain, 0);
   unsigned long GlobalIndex = pointPartitioner.GetFirstIndexOnRank(rank);
   for (unsigned long iPoint = 0; iPoint < nPoint; iPoint++) {
-    for (unsigned short iDim = 0; iDim < nDim; ++iDim)
-      nodes->SetCoord(iPoint, iDim, gridCoords[iDim][iPoint]);
+    for (unsigned short iDim = 0; iDim < nDim; ++iDim) nodes->SetCoord(iPoint, iDim, gridCoords[iDim][iPoint]);
     nodes->SetGlobalIndex(iPoint, GlobalIndex);
     ++GlobalIndex;
   }
-
 }
 
-void CPhysicalGeometry::LoadLinearlyPartitionedVolumeElements(CConfig        *config,
-                                                              CMeshReaderFVM *mesh) {
-
+void CPhysicalGeometry::LoadLinearlyPartitionedVolumeElements(CConfig* config, CMeshReaderFVM* mesh) {
   /*--- Reset the global to local element mapping. ---*/
 
   Global_to_Local_Elem.clear();
@@ -3810,82 +3566,58 @@ void CPhysicalGeometry::LoadLinearlyPartitionedVolumeElements(CConfig        *co
   /*--- Allocate space for the CGNS interior elements in our SU2 data
    structure. Note that we only instantiate our rank's local set. ---*/
 
-  elem = new CPrimalGrid*[nElem] ();
+  elem = new CPrimalGrid*[nElem]();
 
   /*--- Loop over all of the internal, local volumetric elements. ---*/
 
   for (unsigned long iElem = 0; iElem < nElem; iElem++) {
-
     /*--- Get the global ID for this element. This is stored in
      the first entry of our connectivity stucture. ---*/
 
-    const auto Global_Index_Elem = connElems[iElem*SU2_CONN_SIZE + 0];
+    const auto Global_Index_Elem = connElems[iElem * SU2_CONN_SIZE + 0];
     Global_to_Local_Elem[Global_Index_Elem] = iElem;
 
     /*--- Get the VTK type for this element. This is stored in the
      second entry of the connectivity structure. ---*/
 
-    const auto vtk_type = static_cast<int>(connElems[iElem*SU2_CONN_SIZE + 1]);
+    const auto vtk_type = static_cast<int>(connElems[iElem * SU2_CONN_SIZE + 1]);
 
     /*--- Instantiate this element in the proper SU2 data structure.
      During this loop, we also set the global to local element map
      for later use and increment the element counts for all types. ---*/
 
-    auto connectivity = &connElems[iElem*SU2_CONN_SIZE + SU2_CONN_SKIP];
-
-    switch(vtk_type) {
+    auto connectivity = &connElems[iElem * SU2_CONN_SIZE + SU2_CONN_SKIP];
 
+    switch (vtk_type) {
       case TRIANGLE:
-        elem[iElem] = new CTriangle(connectivity[0],
-                                    connectivity[1],
-                                    connectivity[2]);
+        elem[iElem] = new CTriangle(connectivity[0], connectivity[1], connectivity[2]);
         nelem_triangle++;
         break;
 
       case QUADRILATERAL:
-        elem[iElem] = new CQuadrilateral(connectivity[0],
-                                         connectivity[1],
-                                         connectivity[2],
-                                         connectivity[3]);
+        elem[iElem] = new CQuadrilateral(connectivity[0], connectivity[1], connectivity[2], connectivity[3]);
         nelem_quad++;
         break;
 
       case TETRAHEDRON:
-        elem[iElem] = new CTetrahedron(connectivity[0],
-                                       connectivity[1],
-                                       connectivity[2],
-                                       connectivity[3]);
+        elem[iElem] = new CTetrahedron(connectivity[0], connectivity[1], connectivity[2], connectivity[3]);
         nelem_tetra++;
         break;
 
       case HEXAHEDRON:
-        elem[iElem] = new CHexahedron(connectivity[0],
-                                      connectivity[1],
-                                      connectivity[2],
-                                      connectivity[3],
-                                      connectivity[4],
-                                      connectivity[5],
-                                      connectivity[6],
-                                      connectivity[7]);
+        elem[iElem] = new CHexahedron(connectivity[0], connectivity[1], connectivity[2], connectivity[3],
+                                      connectivity[4], connectivity[5], connectivity[6], connectivity[7]);
         nelem_hexa++;
         break;
 
       case PRISM:
-        elem[iElem] = new CPrism(connectivity[0],
-                                 connectivity[1],
-                                 connectivity[2],
-                                 connectivity[3],
-                                 connectivity[4],
+        elem[iElem] = new CPrism(connectivity[0], connectivity[1], connectivity[2], connectivity[3], connectivity[4],
                                  connectivity[5]);
         nelem_prism++;
         break;
 
       case PYRAMID:
-        elem[iElem] = new CPyramid(connectivity[0],
-                                   connectivity[1],
-                                   connectivity[2],
-                                   connectivity[3],
-                                   connectivity[4]);
+        elem[iElem] = new CPyramid(connectivity[0], connectivity[1], connectivity[2], connectivity[3], connectivity[4]);
         nelem_pyramid++;
         break;
 
@@ -3907,20 +3639,16 @@ void CPhysicalGeometry::LoadLinearlyPartitionedVolumeElements(CConfig        *co
   reduce(nelem_tetra, Global_nelem_tetra);
   reduce(nelem_prism, Global_nelem_prism);
   reduce(nelem_pyramid, Global_nelem_pyramid);
-
 }
 
-void CPhysicalGeometry::LoadUnpartitionedSurfaceElements(CConfig        *config,
-                                                         CMeshReaderFVM *mesh) {
-
+void CPhysicalGeometry::LoadUnpartitionedSurfaceElements(CConfig* config, CMeshReaderFVM* mesh) {
   /*--- The master node takes care of loading all markers and
    surface elements from the file. This information is later
    put into linear partitions to make its redistribution easier
    after we call ParMETIS. ---*/
 
   if (rank == MASTER_NODE) {
-
-    const vector<string> &sectionNames = mesh->GetMarkerNames();
+    const vector<string>& sectionNames = mesh->GetMarkerNames();
 
     /*--- Store the number of markers and print to the screen. ---*/
 
@@ -3930,9 +3658,9 @@ void CPhysicalGeometry::LoadUnpartitionedSurfaceElements(CConfig        *config,
 
     /*--- Create the data structure for boundary elements. ---*/
 
-    bound         = new CPrimalGrid**[nMarker];
-    nElem_Bound   = new unsigned long [nMarker];
-    Tag_to_Marker = new string [config->GetnMarker_Max()];
+    bound = new CPrimalGrid**[nMarker];
+    nElem_Bound = new unsigned long[nMarker];
+    Tag_to_Marker = new string[config->GetnMarker_Max()];
 
     /*--- Set some temporaries for the loop below. ---*/
 
@@ -3945,11 +3673,12 @@ void CPhysicalGeometry::LoadUnpartitionedSurfaceElements(CConfig        *config,
      store those elements into our SU2 data structures. ---*/
 
     for (int iMarker = 0; iMarker < nMarker; iMarker++) {
-
       /*--- Initialize some counter variables ---*/
 
-      nelem_edge_bound = 0; nelem_triangle_bound = 0;
-      nelem_quad_bound = 0; iElem = 0;
+      nelem_edge_bound = 0;
+      nelem_triangle_bound = 0;
+      nelem_quad_bound = 0;
+      iElem = 0;
 
       /*--- Get the string name for this marker. ---*/
 
@@ -3957,11 +3686,9 @@ void CPhysicalGeometry::LoadUnpartitionedSurfaceElements(CConfig        *config,
 
       /* Get the marker info and surface connectivity from the mesh object. */
 
-      const unsigned long surfElems =
-      mesh->GetNumberOfSurfaceElementsForMarker(iMarker);
+      const unsigned long surfElems = mesh->GetNumberOfSurfaceElementsForMarker(iMarker);
 
-      const vector<unsigned long> &connElems =
-      mesh->GetSurfaceElementConnectivityForMarker(iMarker);
+      const vector<unsigned long>& connElems = mesh->GetSurfaceElementConnectivityForMarker(iMarker);
 
       /*--- Set the number of boundary elements in this marker. ---*/
 
@@ -3969,51 +3696,50 @@ void CPhysicalGeometry::LoadUnpartitionedSurfaceElements(CConfig        *config,
 
       /*--- Report the number and name of the marker to the console. ---*/
 
-      cout << nElem_Bound[iMarker]  << " boundary elements in index ";
-      cout << iMarker <<" (Marker = " <<Marker_Tag<< ")." << endl;
+      cout << nElem_Bound[iMarker] << " boundary elements in index ";
+      cout << iMarker << " (Marker = " << Marker_Tag << ")." << endl;
 
       /*--- Instantiate the list of elements in the data structure. ---*/
 
       bound[iMarker] = new CPrimalGrid*[nElem_Bound[iMarker]];
 
-      for (unsigned long jElem = 0; jElem < nElem_Bound[iMarker]; jElem++ ) {
-
+      for (unsigned long jElem = 0; jElem < nElem_Bound[iMarker]; jElem++) {
         /*--- Not a mixed section. We already know the element type,
          which is stored ---*/
 
-        vtk_type = (int)connElems[jElem*SU2_CONN_SIZE + 1];
+        vtk_type = (int)connElems[jElem * SU2_CONN_SIZE + 1];
 
         /*--- Store the loop size more easily. ---*/
 
-        npe = (int)(SU2_CONN_SIZE-SU2_CONN_SKIP);
+        npe = (int)(SU2_CONN_SIZE - SU2_CONN_SKIP);
 
         /*--- Store the nodes for this element more clearly. ---*/
 
         for (int j = 0; j < npe; j++) {
-          unsigned long nn = jElem*SU2_CONN_SIZE + SU2_CONN_SKIP + j;
+          unsigned long nn = jElem * SU2_CONN_SIZE + SU2_CONN_SKIP + j;
           connectivity[j] = connElems[nn];
         }
 
         /*--- Instantiate the boundary element object. ---*/
 
-        switch(vtk_type) {
+        switch (vtk_type) {
           case LINE:
-            bound[iMarker][iElem] = new CLine(connectivity[0],
-                                              connectivity[1]);
-            iElem++; nelem_edge_bound++; break;
+            bound[iMarker][iElem] = new CLine(connectivity[0], connectivity[1]);
+            iElem++;
+            nelem_edge_bound++;
+            break;
           case TRIANGLE:
-            bound[iMarker][iElem] = new CTriangle(connectivity[0],
-                                                  connectivity[1],
-                                                  connectivity[2]);
-            iElem++; nelem_triangle_bound++; break;
+            bound[iMarker][iElem] = new CTriangle(connectivity[0], connectivity[1], connectivity[2]);
+            iElem++;
+            nelem_triangle_bound++;
+            break;
           case QUADRILATERAL:
-            bound[iMarker][iElem] = new CQuadrilateral(connectivity[0],
-                                                       connectivity[1],
-                                                       connectivity[2],
-                                                       connectivity[3]);
-            iElem++; nelem_quad_bound++; break;
+            bound[iMarker][iElem] =
+                new CQuadrilateral(connectivity[0], connectivity[1], connectivity[2], connectivity[3]);
+            iElem++;
+            nelem_quad_bound++;
+            break;
         }
-
       }
 
       /*--- Update config file lists in order to store the boundary
@@ -4040,14 +3766,11 @@ void CPhysicalGeometry::LoadUnpartitionedSurfaceElements(CConfig        *config,
       config->SetMarker_All_TurbomachineryFlag(iMarker, config->GetMarker_CfgFile_TurbomachineryFlag(Marker_Tag));
       config->SetMarker_All_MixingPlaneInterface(iMarker, config->GetMarker_CfgFile_MixingPlaneInterface(Marker_Tag));
       config->SetMarker_All_SobolevBC(iMarker, config->GetMarker_CfgFile_SobolevBC(Marker_Tag));
-
     }
   }
-
 }
 
-void CPhysicalGeometry::PrepareAdjacency(const CConfig *config) {
-
+void CPhysicalGeometry::PrepareAdjacency(const CConfig* config) {
 #ifdef HAVE_MPI
 #ifdef HAVE_PARMETIS
 
@@ -4059,13 +3782,12 @@ void CPhysicalGeometry::PrepareAdjacency(const CConfig *config) {
   /*--- Create a partitioner object so we can transform the global
    index values stored in the elements to a local index. ---*/
 
-  CLinearPartitioner pointPartitioner(Global_nPointDomain,0);
+  CLinearPartitioner pointPartitioner(Global_nPointDomain, 0);
   const unsigned long firstIndex = pointPartitioner.GetFirstIndexOnRank(rank);
 
   /*--- Loop over all elements that are now loaded and store adjacency. ---*/
 
   for (unsigned long iElem = 0; iElem < nElem; iElem++) {
-
     /*--- Store the connectivity for this element more easily. ---*/
     unsigned long connectivity[8] = {0};
     for (unsigned long iNode = 0; iNode < elem[iElem]->GetnNodes(); iNode++) {
@@ -4074,8 +3796,7 @@ void CPhysicalGeometry::PrepareAdjacency(const CConfig *config) {
 
     /*--- Instantiate this element and build adjacency structure. ---*/
 
-    switch(elem[iElem]->GetVTK_Type()) {
-
+    switch (elem[iElem]->GetVTK_Type()) {
       case TRIANGLE:
 
         /*--- Decide whether we need to store the adjacency for any nodes
@@ -4083,20 +3804,16 @@ void CPhysicalGeometry::PrepareAdjacency(const CConfig *config) {
          global index value within the range of our linear partitioning. ---*/
 
         for (unsigned long iNode = 0; iNode < N_POINTS_TRIANGLE; iNode++) {
-
-          const long local_index = connectivity[iNode]-firstIndex;
+          const long local_index = connectivity[iNode] - firstIndex;
 
           if ((local_index >= 0) && (local_index < (long)nPoint)) {
-
             /*--- This node is within our linear partition.
              Add the neighboring nodes to this nodes' adjacency list. ---*/
 
             for (unsigned long jNode = 0; jNode < N_POINTS_TRIANGLE; jNode++) {
-
               /*--- Build adjacency assuming the VTK connectivity ---*/
 
-              if (iNode != jNode)
-              adj_nodes[local_index].push_back(connectivity[jNode]);
+              if (iNode != jNode) adj_nodes[local_index].push_back(connectivity[jNode]);
             }
           }
         }
@@ -4110,18 +3827,16 @@ void CPhysicalGeometry::PrepareAdjacency(const CConfig *config) {
          global index value within the range of our linear partitioning. ---*/
 
         for (unsigned long iNode = 0; iNode < N_POINTS_QUADRILATERAL; iNode++) {
-
-          const long local_index = connectivity[iNode]-firstIndex;
+          const long local_index = connectivity[iNode] - firstIndex;
 
           if ((local_index >= 0) && (local_index < (long)nPoint)) {
-
             /*--- This node is within our linear partition.
              Add the neighboring nodes to this nodes' adjacency list. ---*/
 
             /*--- Build adjacency assuming the VTK connectivity ---*/
 
-            adj_nodes[local_index].push_back(connectivity[(iNode+1)%4]);
-            adj_nodes[local_index].push_back(connectivity[(iNode+3)%4]);
+            adj_nodes[local_index].push_back(connectivity[(iNode + 1) % 4]);
+            adj_nodes[local_index].push_back(connectivity[(iNode + 3) % 4]);
           }
         }
 
@@ -4134,20 +3849,16 @@ void CPhysicalGeometry::PrepareAdjacency(const CConfig *config) {
          global index value within the range of our linear partitioning. ---*/
 
         for (unsigned long iNode = 0; iNode < N_POINTS_TETRAHEDRON; iNode++) {
-
-          const long local_index = connectivity[iNode]-firstIndex;
+          const long local_index = connectivity[iNode] - firstIndex;
 
           if ((local_index >= 0) && (local_index < (long)nPoint)) {
-
             /*--- This node is within our linear partition.
              Add the neighboring nodes to this nodes' adjacency list. ---*/
 
             for (unsigned long jNode = 0; jNode < N_POINTS_TETRAHEDRON; jNode++) {
-
               /*--- Build adjacency assuming the VTK connectivity ---*/
 
-              if (iNode != jNode)
-              adj_nodes[local_index].push_back(connectivity[jNode]);
+              if (iNode != jNode) adj_nodes[local_index].push_back(connectivity[jNode]);
             }
           }
         }
@@ -4161,24 +3872,22 @@ void CPhysicalGeometry::PrepareAdjacency(const CConfig *config) {
          global index value within the range of our linear partitioning. ---*/
 
         for (unsigned long iNode = 0; iNode < N_POINTS_HEXAHEDRON; iNode++) {
-
-          const long local_index = connectivity[iNode]-firstIndex;
+          const long local_index = connectivity[iNode] - firstIndex;
 
           if ((local_index >= 0) && (local_index < (long)nPoint)) {
-
             /*--- This node is within our linear partition.
              Add the neighboring nodes to this nodes' adjacency list. ---*/
 
             /*--- Build adjacency assuming the VTK connectivity ---*/
 
             if (iNode < 4) {
-              adj_nodes[local_index].push_back(connectivity[(iNode+1)%4]);
-              adj_nodes[local_index].push_back(connectivity[(iNode+3)%4]);
+              adj_nodes[local_index].push_back(connectivity[(iNode + 1) % 4]);
+              adj_nodes[local_index].push_back(connectivity[(iNode + 3) % 4]);
             } else {
-              adj_nodes[local_index].push_back(connectivity[(iNode-3)%4+4]);
-              adj_nodes[local_index].push_back(connectivity[(iNode-1)%4+4]);
+              adj_nodes[local_index].push_back(connectivity[(iNode - 3) % 4 + 4]);
+              adj_nodes[local_index].push_back(connectivity[(iNode - 1) % 4 + 4]);
             }
-            adj_nodes[local_index].push_back(connectivity[(iNode+4)%8]);
+            adj_nodes[local_index].push_back(connectivity[(iNode + 4) % 8]);
           }
         }
 
@@ -4191,24 +3900,22 @@ void CPhysicalGeometry::PrepareAdjacency(const CConfig *config) {
          global index value within the range of our linear partitioning. ---*/
 
         for (unsigned long iNode = 0; iNode < N_POINTS_PRISM; iNode++) {
-
-          const long local_index = connectivity[iNode]-firstIndex;
+          const long local_index = connectivity[iNode] - firstIndex;
 
           if ((local_index >= 0) && (local_index < (long)nPoint)) {
-
             /*--- This node is within our linear partition.
              Add the neighboring nodes to this nodes' adjacency list. ---*/
 
             /*--- Build adjacency assuming the VTK connectivity ---*/
 
             if (iNode < 3) {
-              adj_nodes[local_index].push_back(connectivity[(iNode+1)%3]);
-              adj_nodes[local_index].push_back(connectivity[(iNode+2)%3]);
+              adj_nodes[local_index].push_back(connectivity[(iNode + 1) % 3]);
+              adj_nodes[local_index].push_back(connectivity[(iNode + 2) % 3]);
             } else {
-              adj_nodes[local_index].push_back(connectivity[(iNode-2)%3+3]);
-              adj_nodes[local_index].push_back(connectivity[(iNode-1)%3+3]);
+              adj_nodes[local_index].push_back(connectivity[(iNode - 2) % 3 + 3]);
+              adj_nodes[local_index].push_back(connectivity[(iNode - 1) % 3 + 3]);
             }
-            adj_nodes[local_index].push_back(connectivity[(iNode+3)%6]);
+            adj_nodes[local_index].push_back(connectivity[(iNode + 3) % 6]);
           }
         }
 
@@ -4221,19 +3928,17 @@ void CPhysicalGeometry::PrepareAdjacency(const CConfig *config) {
          global index value within the range of our linear partitioning. ---*/
 
         for (unsigned long iNode = 0; iNode < N_POINTS_PYRAMID; iNode++) {
-
-          const long local_index = connectivity[iNode]-firstIndex;
+          const long local_index = connectivity[iNode] - firstIndex;
 
           if ((local_index >= 0) && (local_index < (long)nPoint)) {
-
             /*--- This node is within our linear partition.
              Add the neighboring nodes to this nodes' adjacency list. ---*/
 
             /*--- Build adjacency assuming the VTK connectivity ---*/
 
             if (iNode < 4) {
-              adj_nodes[local_index].push_back(connectivity[(iNode+1)%4]);
-              adj_nodes[local_index].push_back(connectivity[(iNode+3)%4]);
+              adj_nodes[local_index].push_back(connectivity[(iNode + 1) % 4]);
+              adj_nodes[local_index].push_back(connectivity[(iNode + 3) % 4]);
               adj_nodes[local_index].push_back(connectivity[4]);
             } else {
               adj_nodes[local_index].push_back(connectivity[0]);
@@ -4259,140 +3964,125 @@ void CPhysicalGeometry::PrepareAdjacency(const CConfig *config) {
 
 #endif
 #endif
-
 }
 
-void CPhysicalGeometry::Check_IntElem_Orientation(const CConfig *config) {
-
-  unsigned long tria_flip=0, quad_flip=0, tet_flip=0, prism_flip=0, hexa_flip=0, pyram_flip=0;
-  unsigned long quad_error=0, prism_error=0, hexa_error=0, pyram_error=0;
-
-  SU2_OMP_PARALLEL_(reduction(+:tria_flip,quad_flip,tet_flip,prism_flip,hexa_flip,pyram_flip)) {
-
-  /*--- Lambda to test triangles. Normal should be positive in the z direction (right hand rule). ---*/
-  auto checkTria = [this](unsigned long iElem, int Node_1, int Node_2, int Node_3) {
-    const auto Coord_1 = nodes->GetCoord(elem[iElem]->GetNode(Node_1));
-    const auto Coord_2 = nodes->GetCoord(elem[iElem]->GetNode(Node_2));
-    const auto Coord_3 = nodes->GetCoord(elem[iElem]->GetNode(Node_3));
-    constexpr int nDim = 2;
-    su2double a[nDim]={0.0}, b[nDim]={0.0};
-    GeometryToolbox::Distance(nDim, Coord_2, Coord_1, a);
-    GeometryToolbox::Distance(nDim, Coord_3, Coord_1, b);
-    return a[0]*b[1]-a[1]*b[0] < 0.0;
-  };
-
-  /*--- Lambda to test tetrahedrons, volume must be positive,
-   * the normal of any face must point towards the other point. ---*/
-  auto checkTetra = [this](unsigned long iElem, int Node_1, int Node_2, int Node_3, int Node_4) {
-    const auto Coord_1 = nodes->GetCoord(elem[iElem]->GetNode(Node_1));
-    const auto Coord_2 = nodes->GetCoord(elem[iElem]->GetNode(Node_2));
-    const auto Coord_3 = nodes->GetCoord(elem[iElem]->GetNode(Node_3));
-    const auto Coord_4 = nodes->GetCoord(elem[iElem]->GetNode(Node_4));
-    constexpr int nDim = 3;
-    su2double a[nDim]={0.0}, b[nDim]={0.0}, c[nDim]={0.0}, n[nDim]={0.0};
-    GeometryToolbox::Distance(nDim, Coord_2, Coord_1, a);
-    GeometryToolbox::Distance(nDim, Coord_3, Coord_1, b);
-    GeometryToolbox::Distance(nDim, Coord_4, Coord_1, c);
-    GeometryToolbox::CrossProduct(a,b,n);
-    return GeometryToolbox::DotProduct(nDim,n,c) < 0.0;
-  };
-
-  /*--- Loop over all the elements. ---*/
-
-  SU2_OMP_FOR_DYN(roundUpDiv(nElem, 2*omp_get_max_threads()))
-  for (auto iElem = 0ul; iElem < nElem; iElem++) {
+void CPhysicalGeometry::Check_IntElem_Orientation(const CConfig* config) {
+  unsigned long tria_flip = 0, quad_flip = 0, tet_flip = 0, prism_flip = 0, hexa_flip = 0, pyram_flip = 0;
+  unsigned long quad_error = 0, prism_error = 0, hexa_error = 0, pyram_error = 0;
+
+  SU2_OMP_PARALLEL_(reduction(+ : tria_flip, quad_flip, tet_flip, prism_flip, hexa_flip, pyram_flip)) {
+    /*--- Lambda to test triangles. Normal should be positive in the z direction (right hand rule). ---*/
+    auto checkTria = [this](unsigned long iElem, int Node_1, int Node_2, int Node_3) {
+      const auto Coord_1 = nodes->GetCoord(elem[iElem]->GetNode(Node_1));
+      const auto Coord_2 = nodes->GetCoord(elem[iElem]->GetNode(Node_2));
+      const auto Coord_3 = nodes->GetCoord(elem[iElem]->GetNode(Node_3));
+      constexpr int nDim = 2;
+      su2double a[nDim] = {0.0}, b[nDim] = {0.0};
+      GeometryToolbox::Distance(nDim, Coord_2, Coord_1, a);
+      GeometryToolbox::Distance(nDim, Coord_3, Coord_1, b);
+      return a[0] * b[1] - a[1] * b[0] < 0.0;
+    };
+
+    /*--- Lambda to test tetrahedrons, volume must be positive,
+     * the normal of any face must point towards the other point. ---*/
+    auto checkTetra = [this](unsigned long iElem, int Node_1, int Node_2, int Node_3, int Node_4) {
+      const auto Coord_1 = nodes->GetCoord(elem[iElem]->GetNode(Node_1));
+      const auto Coord_2 = nodes->GetCoord(elem[iElem]->GetNode(Node_2));
+      const auto Coord_3 = nodes->GetCoord(elem[iElem]->GetNode(Node_3));
+      const auto Coord_4 = nodes->GetCoord(elem[iElem]->GetNode(Node_4));
+      constexpr int nDim = 3;
+      su2double a[nDim] = {0.0}, b[nDim] = {0.0}, c[nDim] = {0.0}, n[nDim] = {0.0};
+      GeometryToolbox::Distance(nDim, Coord_2, Coord_1, a);
+      GeometryToolbox::Distance(nDim, Coord_3, Coord_1, b);
+      GeometryToolbox::Distance(nDim, Coord_4, Coord_1, c);
+      GeometryToolbox::CrossProduct(a, b, n);
+      return GeometryToolbox::DotProduct(nDim, n, c) < 0.0;
+    };
+
+    /*--- Loop over all the elements. ---*/
+
+    SU2_OMP_FOR_DYN(roundUpDiv(nElem, 2 * omp_get_max_threads()))
+    for (auto iElem = 0ul; iElem < nElem; iElem++) {
+      /*--- 2D grid. ---*/
 
-    /*--- 2D grid. ---*/
+      if (elem[iElem]->GetVTK_Type() == TRIANGLE) {
+        if (checkTria(iElem, 0, 1, 2)) {
+          elem[iElem]->Change_Orientation();
+          tria_flip++;
+        }
+      }
 
-    if (elem[iElem]->GetVTK_Type() == TRIANGLE) {
+      if (elem[iElem]->GetVTK_Type() == QUADRILATERAL) {
+        /*--- Two triangles. ---*/
+        bool test_1 = checkTria(iElem, 0, 1, 2);
+        bool test_2 = checkTria(iElem, 0, 2, 3);
 
-      if (checkTria(iElem,0,1,2)) {
-        elem[iElem]->Change_Orientation();
-        tria_flip++;
+        if (test_1 && test_2) {
+          elem[iElem]->Change_Orientation();
+          quad_flip++;
+        } else if (test_1 || test_2) {
+          /*--- If one test fails and the other passes the
+           * element probably has serious problems. ---*/
+          SU2_OMP_ATOMIC
+          quad_error++;
+        }
       }
-    }
 
-    if (elem[iElem]->GetVTK_Type() == QUADRILATERAL) {
-
-      /*--- Two triangles. ---*/
-      bool test_1 = checkTria(iElem,0,1,2);
-      bool test_2 = checkTria(iElem,0,2,3);
+      /*--- 3D grid. ---*/
 
-      if (test_1 && test_2) {
-        elem[iElem]->Change_Orientation();
-        quad_flip++;
-      }
-      else if (test_1 || test_2) {
-        /*--- If one test fails and the other passes the
-         * element probably has serious problems. ---*/
-        SU2_OMP_ATOMIC
-        quad_error++;
+      if (elem[iElem]->GetVTK_Type() == TETRAHEDRON) {
+        if (checkTetra(iElem, 0, 1, 2, 3)) {
+          elem[iElem]->Change_Orientation();
+          tet_flip++;
+        }
       }
-    }
 
-    /*--- 3D grid. ---*/
-
-    if (elem[iElem]->GetVTK_Type() == TETRAHEDRON) {
+      if (elem[iElem]->GetVTK_Type() == PYRAMID) {
+        /*--- Slice across top vertex into 2 tets. ---*/
+        bool test_1 = checkTetra(iElem, 0, 1, 2, 4);
+        bool test_2 = checkTetra(iElem, 2, 3, 0, 4);
 
-      if (checkTetra(iElem,0,1,2,3)) {
-        elem[iElem]->Change_Orientation();
-        tet_flip++;
+        if (test_1 && test_2) {
+          elem[iElem]->Change_Orientation();
+          pyram_flip++;
+        } else if (test_1 || test_2) {
+          SU2_OMP_ATOMIC
+          pyram_error++;
+        }
       }
-    }
-
-    if (elem[iElem]->GetVTK_Type() == PYRAMID) {
 
-      /*--- Slice across top vertex into 2 tets. ---*/
-      bool test_1 = checkTetra(iElem,0,1,2,4);
-      bool test_2 = checkTetra(iElem,2,3,0,4);
+      if (elem[iElem]->GetVTK_Type() == PRISM) {
+        /*--- The triangular faces should point at each other. ---*/
+        bool test_1 = checkTetra(iElem, 0, 2, 1, 3);
+        bool test_2 = checkTetra(iElem, 3, 4, 5, 2);
 
-      if (test_1 && test_2) {
-        elem[iElem]->Change_Orientation();
-        pyram_flip++;
+        if (test_1 && test_2) {
+          elem[iElem]->Change_Orientation();
+          prism_flip++;
+        } else if (test_1 || test_2) {
+          SU2_OMP_ATOMIC
+          prism_error++;
+        }
       }
-      else if (test_1 || test_2) {
-        SU2_OMP_ATOMIC
-        pyram_error++;
+
+      if (elem[iElem]->GetVTK_Type() == HEXAHEDRON) {
+        /*--- The base points at the top. ---*/
+        bool test_1 = checkTetra(iElem, 0, 1, 2, 5);
+        bool test_2 = checkTetra(iElem, 0, 2, 3, 7);
+        /*--- The top points at the base. ---*/
+        bool test_3 = checkTetra(iElem, 4, 6, 5, 1);
+        bool test_4 = checkTetra(iElem, 4, 7, 6, 3);
+
+        if (test_1 && test_2 && test_3 && test_4) {
+          elem[iElem]->Change_Orientation();
+          hexa_flip++;
+        } else if (test_1 || test_2 || test_3 || test_4) {
+          SU2_OMP_ATOMIC
+          hexa_error++;
+        }
       }
     }
-
-    if (elem[iElem]->GetVTK_Type() == PRISM) {
-
-      /*--- The triangular faces should point at each other. ---*/
-      bool test_1 = checkTetra(iElem,0,2,1,3);
-      bool test_2 = checkTetra(iElem,3,4,5,2);
-
-      if (test_1 && test_2) {
-        elem[iElem]->Change_Orientation();
-        prism_flip++;
-      }
-      else if (test_1 || test_2) {
-        SU2_OMP_ATOMIC
-        prism_error++;
-      }
-    }
-
-    if (elem[iElem]->GetVTK_Type() == HEXAHEDRON) {
-
-      /*--- The base points at the top. ---*/
-      bool test_1 = checkTetra(iElem,0,1,2,5);
-      bool test_2 = checkTetra(iElem,0,2,3,7);
-      /*--- The top points at the base. ---*/
-      bool test_3 = checkTetra(iElem,4,6,5,1);
-      bool test_4 = checkTetra(iElem,4,7,6,3);
-
-      if (test_1 && test_2 && test_3 && test_4) {
-        elem[iElem]->Change_Orientation();
-        hexa_flip++;
-      }
-      else if (test_1 || test_2 || test_3 || test_4) {
-        SU2_OMP_ATOMIC
-        hexa_error++;
-      }
-    }
-
-  }
-  END_SU2_OMP_FOR
+    END_SU2_OMP_FOR
   }
   END_SU2_OMP_PARALLEL
 
@@ -4400,11 +4090,16 @@ void CPhysicalGeometry::Check_IntElem_Orientation(const CConfig *config) {
     unsigned long tmp = val;
     SU2_MPI::Allreduce(&tmp, &val, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
   };
-  reduce(tria_flip); reduce(quad_flip);
-  reduce(tet_flip); reduce(pyram_flip);
-  reduce(prism_flip); reduce(hexa_flip);
-  reduce(quad_error); reduce(pyram_error);
-  reduce(prism_error); reduce(hexa_error);
+  reduce(tria_flip);
+  reduce(quad_flip);
+  reduce(tet_flip);
+  reduce(pyram_flip);
+  reduce(prism_flip);
+  reduce(hexa_flip);
+  reduce(quad_error);
+  reduce(pyram_error);
+  reduce(prism_error);
+  reduce(hexa_error);
 
   if (rank == MASTER_NODE) {
     string start("There has been a re-orientation of ");
@@ -4415,134 +4110,130 @@ void CPhysicalGeometry::Check_IntElem_Orientation(const CConfig *config) {
     if (pyram_flip) cout << start << pyram_flip << " PYRAMID volume elements." << endl;
     if (prism_flip) cout << start << prism_flip << " PRISM volume elements." << endl;
 
-    if (quad_error+pyram_error+prism_error+hexa_error) {
+    if (quad_error + pyram_error + prism_error + hexa_error) {
       cout << ">>> WARNING: ";
       if (quad_error) cout << quad_error << " QUADRILATERAL, ";
       if (pyram_error) cout << pyram_error << " PYRAMID, ";
       if (prism_error) cout << prism_error << " PRISM, ";
       if (hexa_error) cout << hexa_error << " HEXAHEDRON, ";
       cout << "volume elements are distorted.\n    It was not possible "
-              "to determine if their orientation is correct." << endl;
+              "to determine if their orientation is correct."
+           << endl;
     }
 
-    if (tria_flip+quad_flip+tet_flip+hexa_flip+pyram_flip+prism_flip+
-        quad_error+pyram_error+prism_error+hexa_error == 0) {
+    if (tria_flip + quad_flip + tet_flip + hexa_flip + pyram_flip + prism_flip + quad_error + pyram_error +
+            prism_error + hexa_error ==
+        0) {
       cout << "All volume elements are correctly orientend." << endl;
     }
   }
-
 }
 
-void CPhysicalGeometry::Check_BoundElem_Orientation(const CConfig *config) {
-
+void CPhysicalGeometry::Check_BoundElem_Orientation(const CConfig* config) {
   unsigned long line_flip = 0, tria_flip = 0, quad_flip = 0, quad_error = 0;
 
-  SU2_OMP_PARALLEL_(reduction(+:line_flip,tria_flip,quad_flip,quad_error)) {
-
-  /*--- Lambda to test tetrahedrons. ---*/
-  auto checkTetra = [this](unsigned long Point_1, unsigned long Point_2,
-                           unsigned long Point_3, unsigned long Point_4) {
-    const auto Coord_1 = nodes->GetCoord(Point_1);
-    const auto Coord_2 = nodes->GetCoord(Point_2);
-    const auto Coord_3 = nodes->GetCoord(Point_3);
-    const auto Coord_4 = nodes->GetCoord(Point_4);
-    constexpr int nDim = 3;
-    su2double a[nDim]={0.0}, b[nDim]={0.0}, c[nDim]={0.0}, n[nDim]={0.0};
-    GeometryToolbox::Distance(nDim, Coord_2, Coord_1, a);
-    GeometryToolbox::Distance(nDim, Coord_3, Coord_1, b);
-    GeometryToolbox::Distance(nDim, Coord_4, Coord_1, c);
-    GeometryToolbox::CrossProduct(a,b,n);
-    return GeometryToolbox::DotProduct(nDim,n,c) < 0.0;
-  };
-
-  for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
-
-    if (config->GetMarker_All_KindBC(iMarker) == INTERNAL_BOUNDARY) continue;
-
-    SU2_OMP_FOR_DYN(OMP_MIN_SIZE)
-    for (auto iElem_Surface = 0ul; iElem_Surface < nElem_Bound[iMarker]; iElem_Surface++) {
-
-      /*--- Pick a reference point inside the domain that is not part of the surface element. ---*/
-      const auto iElem_Domain = bound[iMarker][iElem_Surface]->GetDomainElement();
-      unsigned long Point_Domain = 0;
-
-      for (auto iNode_Domain = 0u; iNode_Domain < elem[iElem_Domain]->GetnNodes(); iNode_Domain++) {
-        Point_Domain = elem[iElem_Domain]->GetNode(iNode_Domain);
-        bool find = false;
-        for (auto iNode_Surface = 0u; iNode_Surface < bound[iMarker][iElem_Surface]->GetnNodes(); iNode_Surface++) {
-          auto Point_Surface = bound[iMarker][iElem_Surface]->GetNode(iNode_Surface);
-          if (Point_Surface == Point_Domain) {find = true; break;}
+  SU2_OMP_PARALLEL_(reduction(+ : line_flip, tria_flip, quad_flip, quad_error)) {
+    /*--- Lambda to test tetrahedrons. ---*/
+    auto checkTetra = [this](unsigned long Point_1, unsigned long Point_2, unsigned long Point_3,
+                             unsigned long Point_4) {
+      const auto Coord_1 = nodes->GetCoord(Point_1);
+      const auto Coord_2 = nodes->GetCoord(Point_2);
+      const auto Coord_3 = nodes->GetCoord(Point_3);
+      const auto Coord_4 = nodes->GetCoord(Point_4);
+      constexpr int nDim = 3;
+      su2double a[nDim] = {0.0}, b[nDim] = {0.0}, c[nDim] = {0.0}, n[nDim] = {0.0};
+      GeometryToolbox::Distance(nDim, Coord_2, Coord_1, a);
+      GeometryToolbox::Distance(nDim, Coord_3, Coord_1, b);
+      GeometryToolbox::Distance(nDim, Coord_4, Coord_1, c);
+      GeometryToolbox::CrossProduct(a, b, n);
+      return GeometryToolbox::DotProduct(nDim, n, c) < 0.0;
+    };
+
+    for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
+      if (config->GetMarker_All_KindBC(iMarker) == INTERNAL_BOUNDARY) continue;
+
+      SU2_OMP_FOR_DYN(OMP_MIN_SIZE)
+      for (auto iElem_Surface = 0ul; iElem_Surface < nElem_Bound[iMarker]; iElem_Surface++) {
+        /*--- Pick a reference point inside the domain that is not part of the surface element. ---*/
+        const auto iElem_Domain = bound[iMarker][iElem_Surface]->GetDomainElement();
+        unsigned long Point_Domain = 0;
+
+        for (auto iNode_Domain = 0u; iNode_Domain < elem[iElem_Domain]->GetnNodes(); iNode_Domain++) {
+          Point_Domain = elem[iElem_Domain]->GetNode(iNode_Domain);
+          bool find = false;
+          for (auto iNode_Surface = 0u; iNode_Surface < bound[iMarker][iElem_Surface]->GetnNodes(); iNode_Surface++) {
+            auto Point_Surface = bound[iMarker][iElem_Surface]->GetNode(iNode_Surface);
+            if (Point_Surface == Point_Domain) {
+              find = true;
+              break;
+            }
+          }
+          if (!find) break;
         }
-        if (!find) break;
-      }
-
-      /*--- 2D grid. ---*/
 
-      if (bound[iMarker][iElem_Surface]->GetVTK_Type() == LINE) {
-
-        auto Point_1_Surface = bound[iMarker][iElem_Surface]->GetNode(0);
-        auto Point_2_Surface = bound[iMarker][iElem_Surface]->GetNode(1);
-        const auto Coord_1 = nodes->GetCoord(Point_1_Surface);
-        const auto Coord_2 = nodes->GetCoord(Point_2_Surface);
-        const auto Coord_3 = nodes->GetCoord(Point_Domain);
-
-        /*--- The normal of the triangle formed by the line and domain
-         * point should point in the positive z direction. ---*/
-        constexpr int nDim = 2;
-        su2double a[nDim]={0.0}, b[nDim]={0.0};
-        GeometryToolbox::Distance(nDim, Coord_2, Coord_1, a);
-        GeometryToolbox::Distance(nDim, Coord_3, Coord_1, b);
-        bool test = a[0]*b[1]-a[1]*b[0] < 0.0;
-
-        if (test) {
-          bound[iMarker][iElem_Surface]->Change_Orientation();
-          line_flip++;
+        /*--- 2D grid. ---*/
+
+        if (bound[iMarker][iElem_Surface]->GetVTK_Type() == LINE) {
+          auto Point_1_Surface = bound[iMarker][iElem_Surface]->GetNode(0);
+          auto Point_2_Surface = bound[iMarker][iElem_Surface]->GetNode(1);
+          const auto Coord_1 = nodes->GetCoord(Point_1_Surface);
+          const auto Coord_2 = nodes->GetCoord(Point_2_Surface);
+          const auto Coord_3 = nodes->GetCoord(Point_Domain);
+
+          /*--- The normal of the triangle formed by the line and domain
+           * point should point in the positive z direction. ---*/
+          constexpr int nDim = 2;
+          su2double a[nDim] = {0.0}, b[nDim] = {0.0};
+          GeometryToolbox::Distance(nDim, Coord_2, Coord_1, a);
+          GeometryToolbox::Distance(nDim, Coord_3, Coord_1, b);
+          bool test = a[0] * b[1] - a[1] * b[0] < 0.0;
+
+          if (test) {
+            bound[iMarker][iElem_Surface]->Change_Orientation();
+            line_flip++;
+          }
         }
-      }
-
-      /*--- 3D grid. ---*/
 
-      if (bound[iMarker][iElem_Surface]->GetVTK_Type() == TRIANGLE) {
+        /*--- 3D grid. ---*/
 
-        auto Point_1_Surface = bound[iMarker][iElem_Surface]->GetNode(0);
-        auto Point_2_Surface = bound[iMarker][iElem_Surface]->GetNode(1);
-        auto Point_3_Surface = bound[iMarker][iElem_Surface]->GetNode(2);
+        if (bound[iMarker][iElem_Surface]->GetVTK_Type() == TRIANGLE) {
+          auto Point_1_Surface = bound[iMarker][iElem_Surface]->GetNode(0);
+          auto Point_2_Surface = bound[iMarker][iElem_Surface]->GetNode(1);
+          auto Point_3_Surface = bound[iMarker][iElem_Surface]->GetNode(2);
 
-        /*--- The normal of the triangle should point into the domain,
-         * resulting in a tetrahedron with positive volume. ---*/
-        if (checkTetra(Point_1_Surface, Point_2_Surface, Point_3_Surface, Point_Domain)) {
-          bound[iMarker][iElem_Surface]->Change_Orientation();
-          tria_flip++;
+          /*--- The normal of the triangle should point into the domain,
+           * resulting in a tetrahedron with positive volume. ---*/
+          if (checkTetra(Point_1_Surface, Point_2_Surface, Point_3_Surface, Point_Domain)) {
+            bound[iMarker][iElem_Surface]->Change_Orientation();
+            tria_flip++;
+          }
         }
-      }
-
-      if (bound[iMarker][iElem_Surface]->GetVTK_Type() == QUADRILATERAL) {
-
-        auto Point_1_Surface = bound[iMarker][iElem_Surface]->GetNode(0);
-        auto Point_2_Surface = bound[iMarker][iElem_Surface]->GetNode(1);
-        auto Point_3_Surface = bound[iMarker][iElem_Surface]->GetNode(2);
-        auto Point_4_Surface = bound[iMarker][iElem_Surface]->GetNode(3);
 
-        /*--- Divide quadrilateral/pyramid into triangles/tetrahedrons. ---*/
-        int test_1 = checkTetra(Point_1_Surface, Point_2_Surface, Point_3_Surface, Point_Domain);
-        int test_2 = checkTetra(Point_2_Surface, Point_3_Surface, Point_4_Surface, Point_Domain);
-        int test_3 = checkTetra(Point_3_Surface, Point_4_Surface, Point_1_Surface, Point_Domain);
-        int test_4 = checkTetra(Point_4_Surface, Point_1_Surface, Point_2_Surface, Point_Domain);
-
-        if (test_1+test_2+test_3+test_4 >= 3) {
-          /*--- If 3 or 4 tests fail there is > 75% chance flipping is the right choice. ---*/
-          bound[iMarker][iElem_Surface]->Change_Orientation();
-          quad_flip++;
-        }
-        else if (test_1+test_2+test_3+test_4 == 2) {
-          /*--- If 50/50 we cannot be sure of what to do -> report to user.
-           * If only one test fails it is probably (75%) due to skewness or warping. ---*/
-          quad_error++;
+        if (bound[iMarker][iElem_Surface]->GetVTK_Type() == QUADRILATERAL) {
+          auto Point_1_Surface = bound[iMarker][iElem_Surface]->GetNode(0);
+          auto Point_2_Surface = bound[iMarker][iElem_Surface]->GetNode(1);
+          auto Point_3_Surface = bound[iMarker][iElem_Surface]->GetNode(2);
+          auto Point_4_Surface = bound[iMarker][iElem_Surface]->GetNode(3);
+
+          /*--- Divide quadrilateral/pyramid into triangles/tetrahedrons. ---*/
+          int test_1 = checkTetra(Point_1_Surface, Point_2_Surface, Point_3_Surface, Point_Domain);
+          int test_2 = checkTetra(Point_2_Surface, Point_3_Surface, Point_4_Surface, Point_Domain);
+          int test_3 = checkTetra(Point_3_Surface, Point_4_Surface, Point_1_Surface, Point_Domain);
+          int test_4 = checkTetra(Point_4_Surface, Point_1_Surface, Point_2_Surface, Point_Domain);
+
+          if (test_1 + test_2 + test_3 + test_4 >= 3) {
+            /*--- If 3 or 4 tests fail there is > 75% chance flipping is the right choice. ---*/
+            bound[iMarker][iElem_Surface]->Change_Orientation();
+            quad_flip++;
+          } else if (test_1 + test_2 + test_3 + test_4 == 2) {
+            /*--- If 50/50 we cannot be sure of what to do -> report to user.
+             * If only one test fails it is probably (75%) due to skewness or warping. ---*/
+            quad_error++;
+          }
         }
       }
+      END_SU2_OMP_FOR
     }
-    END_SU2_OMP_FOR
-  }
   }
   END_SU2_OMP_PARALLEL
 
@@ -4550,8 +4241,10 @@ void CPhysicalGeometry::Check_BoundElem_Orientation(const CConfig *config) {
     unsigned long tmp = val;
     SU2_MPI::Allreduce(&tmp, &val, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
   };
-  reduce(line_flip); reduce(tria_flip);
-  reduce(quad_flip); reduce(quad_error);
+  reduce(line_flip);
+  reduce(tria_flip);
+  reduce(quad_flip);
+  reduce(quad_error);
 
   if (rank == MASTER_NODE) {
     string start("There has been a re-orientation of ");
@@ -4560,24 +4253,27 @@ void CPhysicalGeometry::Check_BoundElem_Orientation(const CConfig *config) {
     if (quad_flip) cout << start << quad_flip << " QUADRILATERAL surface elements." << endl;
 
     if (quad_error) {
-      cout << ">>> WARNING: " << quad_error << " QUADRILATERAL surface elements are distorted.\n"
-              "    It was not possible to determine if their orientation is correct." << endl;
+      cout << ">>> WARNING: " << quad_error
+           << " QUADRILATERAL surface elements are distorted.\n"
+              "    It was not possible to determine if their orientation is correct."
+           << endl;
     }
 
-    if (line_flip+tria_flip+quad_flip+quad_error == 0) {
+    if (line_flip + tria_flip + quad_flip + quad_error == 0) {
       cout << "All surface elements are correctly orientend." << endl;
     }
   }
-
 }
 
-void CPhysicalGeometry::SetPositive_ZArea(CConfig *config) {
+void CPhysicalGeometry::SetPositive_ZArea(CConfig* config) {
   unsigned short iMarker, Boundary, Monitoring;
   unsigned long iVertex, iPoint;
-  su2double *Normal, PositiveXArea, PositiveYArea, PositiveZArea, WettedArea, CoordX = 0.0, CoordY = 0.0, CoordZ = 0.0, MinCoordX = 1E10, MinCoordY = 1E10,
-  MinCoordZ = 1E10, MaxCoordX = -1E10, MaxCoordY = -1E10, MaxCoordZ = -1E10, TotalMinCoordX = 1E10, TotalMinCoordY = 1E10,
-  TotalMinCoordZ = 1E10, TotalMaxCoordX = -1E10, TotalMaxCoordY = -1E10, TotalMaxCoordZ = -1E10;
-  su2double TotalPositiveXArea = 0.0, TotalPositiveYArea = 0.0, TotalPositiveZArea = 0.0, TotalWettedArea = 0.0, AxiFactor;
+  su2double *Normal, PositiveXArea, PositiveYArea, PositiveZArea, WettedArea,
+      CoordX = 0.0, CoordY = 0.0, CoordZ = 0.0, MinCoordX = 1E10, MinCoordY = 1E10, MinCoordZ = 1E10, MaxCoordX = -1E10,
+      MaxCoordY = -1E10, MaxCoordZ = -1E10, TotalMinCoordX = 1E10, TotalMinCoordY = 1E10, TotalMinCoordZ = 1E10,
+      TotalMaxCoordX = -1E10, TotalMaxCoordY = -1E10, TotalMaxCoordZ = -1E10;
+  su2double TotalPositiveXArea = 0.0, TotalPositiveYArea = 0.0, TotalPositiveZArea = 0.0, TotalWettedArea = 0.0,
+            AxiFactor;
 
   const bool axisymmetric = config->GetAxisymmetric();
   const bool fea = config->GetStructuralProblem();
@@ -4591,9 +4287,9 @@ void CPhysicalGeometry::SetPositive_ZArea(CConfig *config) {
     Boundary = config->GetMarker_All_KindBC(iMarker);
     Monitoring = config->GetMarker_All_Monitoring(iMarker);
 
-    if (((config->GetSolid_Wall(iMarker) || Boundary == LOAD_BOUNDARY ||
-          Boundary == DISPLACEMENT_BOUNDARY) && Monitoring == YES) || fea) {
-
+    if (((config->GetSolid_Wall(iMarker) || Boundary == LOAD_BOUNDARY || Boundary == DISPLACEMENT_BOUNDARY) &&
+         Monitoring == YES) ||
+        fea) {
       for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
         iPoint = vertex[iMarker][iVertex]->GetNode();
 
@@ -4603,8 +4299,10 @@ void CPhysicalGeometry::SetPositive_ZArea(CConfig *config) {
           CoordY = nodes->GetCoord(iPoint, 1);
           if (nDim == 3) CoordZ = nodes->GetCoord(iPoint, 2);
 
-          if (axisymmetric) AxiFactor = 2.0*PI_NUMBER*nodes->GetCoord(iPoint, 1);
-          else AxiFactor = 1.0;
+          if (axisymmetric)
+            AxiFactor = 2.0 * PI_NUMBER * nodes->GetCoord(iPoint, 1);
+          else
+            AxiFactor = 1.0;
 
           WettedArea += AxiFactor * GeometryToolbox::Norm(nDim, Normal);
 
@@ -4643,131 +4341,126 @@ void CPhysicalGeometry::SetPositive_ZArea(CConfig *config) {
 
   /*--- Set a reference area if no value is provided ---*/
 
-  const string L = (config->GetSystemMeasurements() == SI)? " m" : " ft";
-  const string A = (config->GetSystemMeasurements() == SI)? " m^2" : " ft^2";
+  const string L = (config->GetSystemMeasurements() == SI) ? " m" : " ft";
+  const string A = (config->GetSystemMeasurements() == SI) ? " m^2" : " ft^2";
   const bool D3 = (nDim == 3);
 
   if (config->GetRefArea() == 0.0) {
-
-    if (D3) config->SetRefArea(TotalPositiveZArea);
-    else config->SetRefArea(TotalPositiveYArea);
+    if (D3)
+      config->SetRefArea(TotalPositiveZArea);
+    else
+      config->SetRefArea(TotalPositiveYArea);
 
     if (rank == MASTER_NODE) {
-      if (D3) cout << "Reference area = "<< TotalPositiveZArea << A << ".\n";
-      else cout << "Reference length = "<< TotalPositiveYArea << L << ".\n";
+      if (D3)
+        cout << "Reference area = " << TotalPositiveZArea << A << ".\n";
+      else
+        cout << "Reference length = " << TotalPositiveYArea << L << ".\n";
     }
   }
 
   /*--- Set a semi-span value if no value is provided ---*/
 
   if (config->GetSemiSpan() == 0.0) {
-
-    if (D3) config->SetSemiSpan(fabs(TotalMaxCoordY));
-    else config->SetSemiSpan(1.0);
+    if (D3)
+      config->SetSemiSpan(fabs(TotalMaxCoordY));
+    else
+      config->SetSemiSpan(1.0);
 
     if (D3 && (rank == MASTER_NODE)) {
-      cout << "Semi-span length = "<< TotalMaxCoordY << L << ".\n";
+      cout << "Semi-span length = " << TotalMaxCoordY << L << ".\n";
     }
   }
 
   if (rank == MASTER_NODE) {
+    if (fea)
+      cout << "Surface area = " << TotalWettedArea;
+    else
+      cout << "Wetted area = " << TotalWettedArea;
+    if (D3 || axisymmetric)
+      cout << A << ".\n";
+    else
+      cout << L << ".\n";
 
-    if (fea) cout << "Surface area = "<< TotalWettedArea;
-    else cout << "Wetted area = "<< TotalWettedArea;
-    if (D3 || axisymmetric) cout << A << ".\n";
-    else cout << L << ".\n";
-
-    cout << "Area projection in the x-plane = "<< TotalPositiveXArea << (D3? A : L);
-    cout << ", y-plane = "<< TotalPositiveYArea << (D3? A : L);
-    if (D3) cout << ", z-plane = "<< TotalPositiveZArea << A;
+    cout << "Area projection in the x-plane = " << TotalPositiveXArea << (D3 ? A : L);
+    cout << ", y-plane = " << TotalPositiveYArea << (D3 ? A : L);
+    if (D3) cout << ", z-plane = " << TotalPositiveZArea << A;
     cout << ".\n";
 
-    cout << "Max. coordinate in the x-direction = "<< TotalMaxCoordX << L;
-    cout << ", y-direction = "<< TotalMaxCoordY << L;
-    if (D3) cout << ", z-direction = "<< TotalMaxCoordZ << L;
+    cout << "Max. coordinate in the x-direction = " << TotalMaxCoordX << L;
+    cout << ", y-direction = " << TotalMaxCoordY << L;
+    if (D3) cout << ", z-direction = " << TotalMaxCoordZ << L;
     cout << ".\n";
 
-    cout << "Min. coordinate in the x-direction = "<< TotalMinCoordX << L;
-    cout << ", y-direction = "<< TotalMinCoordY << L;
-    if (D3) cout << ", z-direction = "<< TotalMinCoordZ << L;
+    cout << "Min. coordinate in the x-direction = " << TotalMinCoordX << L;
+    cout << ", y-direction = " << TotalMinCoordY << L;
+    if (D3) cout << ", z-direction = " << TotalMinCoordZ << L;
     cout << "." << endl;
-
   }
-
 }
 
 void CPhysicalGeometry::SetPoint_Connectivity() {
-
   vector<vector<unsigned long> > points(nPoint);
 
-  SU2_OMP_PARALLEL
-  {
-  unsigned short Node_Neighbor, iNode, iNeighbor;
-  unsigned long jElem, Point_Neighbor, iPoint, iElem;
-
-  /*--- Loop over all the elements ---*/
-  BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS
-  {
-    vector<vector<long> > elems(nPoint);
+  SU2_OMP_PARALLEL {
+    unsigned short Node_Neighbor, iNode, iNeighbor;
+    unsigned long jElem, Point_Neighbor, iPoint, iElem;
 
-    for (iElem = 0; iElem < nElem; iElem++) {
+    /*--- Loop over all the elements ---*/
+    BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
+      vector<vector<long> > elems(nPoint);
 
-      /*--- Loop over all the nodes of an element ---*/
-      for (iNode = 0; iNode < elem[iElem]->GetnNodes(); iNode++) {
-        iPoint = elem[iElem]->GetNode(iNode);
-        elems[iPoint].push_back(iElem);
+      for (iElem = 0; iElem < nElem; iElem++) {
+        /*--- Loop over all the nodes of an element ---*/
+        for (iNode = 0; iNode < elem[iElem]->GetnNodes(); iNode++) {
+          iPoint = elem[iElem]->GetNode(iNode);
+          elems[iPoint].push_back(iElem);
+        }
       }
+      nodes->SetElems(elems);
     }
-    nodes->SetElems(elems);
-  }
-  END_SU2_OMP_SAFE_GLOBAL_ACCESS
-
-  /*--- Loop over all the points ---*/
-
-  SU2_OMP_FOR_DYN(roundUpDiv(nPoint,2*omp_get_max_threads()))
-  for (iPoint = 0; iPoint < nPoint; iPoint++) {
+    END_SU2_OMP_SAFE_GLOBAL_ACCESS
 
-    /*--- Loop over all elements shared by the point ---*/
+    /*--- Loop over all the points ---*/
 
-    for (iElem = 0; iElem < nodes->GetnElem(iPoint); iElem++) {
-
-      jElem = nodes->GetElem(iPoint, iElem);
+    SU2_OMP_FOR_DYN(roundUpDiv(nPoint, 2 * omp_get_max_threads()))
+    for (iPoint = 0; iPoint < nPoint; iPoint++) {
+      /*--- Loop over all elements shared by the point ---*/
 
-      /*--- If we find the point iPoint in the surrounding element ---*/
+      for (iElem = 0; iElem < nodes->GetnElem(iPoint); iElem++) {
+        jElem = nodes->GetElem(iPoint, iElem);
 
-      for (iNode = 0; iNode < elem[jElem]->GetnNodes(); iNode++) {
+        /*--- If we find the point iPoint in the surrounding element ---*/
 
-        if (elem[jElem]->GetNode(iNode) != iPoint) continue;
+        for (iNode = 0; iNode < elem[jElem]->GetnNodes(); iNode++) {
+          if (elem[jElem]->GetNode(iNode) != iPoint) continue;
 
-        /*--- Localize the local index of the neighbor of iPoint in the element ---*/
+          /*--- Localize the local index of the neighbor of iPoint in the element ---*/
 
-        for (iNeighbor = 0; iNeighbor < elem[jElem]->GetnNeighbor_Nodes(iNode); iNeighbor++) {
-          Node_Neighbor = elem[jElem]->GetNeighbor_Nodes(iNode, iNeighbor);
-          Point_Neighbor = elem[jElem]->GetNode(Node_Neighbor);
+          for (iNeighbor = 0; iNeighbor < elem[jElem]->GetnNeighbor_Nodes(iNode); iNeighbor++) {
+            Node_Neighbor = elem[jElem]->GetNeighbor_Nodes(iNode, iNeighbor);
+            Point_Neighbor = elem[jElem]->GetNode(Node_Neighbor);
 
-          /*--- Store the point into the point, if it is new ---*/
-          auto End = points[iPoint].end();
-          if (find(points[iPoint].begin(), End, Point_Neighbor) == End)
-            points[iPoint].push_back(Point_Neighbor);
+            /*--- Store the point into the point, if it is new ---*/
+            auto End = points[iPoint].end();
+            if (find(points[iPoint].begin(), End, Point_Neighbor) == End) points[iPoint].push_back(Point_Neighbor);
+          }
         }
       }
-    }
-
-    /*--- Set the number of neighbors variable, this is important for JST and multigrid in parallel. ---*/
-    nodes->SetnNeighbor(iPoint, points[iPoint].size());
-  }
-  END_SU2_OMP_FOR
 
-  SU2_OMP_MASTER
-  nodes->SetPoints(points);
-  END_SU2_OMP_MASTER
+      /*--- Set the number of neighbors variable, this is important for JST and multigrid in parallel. ---*/
+      nodes->SetnNeighbor(iPoint, points[iPoint].size());
+    }
+    END_SU2_OMP_FOR
 
+    SU2_OMP_MASTER
+    nodes->SetPoints(points);
+    END_SU2_OMP_MASTER
   }
   END_SU2_OMP_PARALLEL
 }
 
-void CPhysicalGeometry::SetRCM_Ordering(CConfig *config) {
-
+void CPhysicalGeometry::SetRCM_Ordering(CConfig* config) {
   /*--- The result is the RCM ordering, during the process it is also used as
    * the queue of new points considered by the algorithm. This is possible
    * because points move from the front of the queue to the back of the result,
@@ -4785,7 +4478,6 @@ void CPhysicalGeometry::SetRCM_Ordering(CConfig *config) {
 
   /*--- Repeat as many times as necessary to handle disconnected graphs. ---*/
   while (Result.size() < nPointDomain) {
-
     /*--- Select the node with the lowest degree in the grid. ---*/
     auto AddPoint = nPoint;
     auto MinDegree = std::numeric_limits<unsigned short>::max();
@@ -4807,7 +4499,6 @@ void CPhysicalGeometry::SetRCM_Ordering(CConfig *config) {
     /*--- Loop until reorganizing all nodes connected to AddPoint. This will
      * also terminate early once the ordering + queue include all points. ---*/
     while (QueueStart < Result.size() && Result.size() < nPointDomain) {
-
       /*--- Move the start of the queue, equivalent to taking from the front of
        * the queue and inserting at the end of the result. ---*/
       AddPoint = Result[QueueStart];
@@ -4826,11 +4517,9 @@ void CPhysicalGeometry::SetRCM_Ordering(CConfig *config) {
       if (AuxQueue.empty()) continue;
 
       /*--- Sort the auxiliar queue based on the number of neighbors (degree). ---*/
-      stable_sort(AuxQueue.begin(), AuxQueue.end(),
-        [&](unsigned long iPoint, unsigned long jPoint) {
-          return nodes->GetnPoint(iPoint) < nodes->GetnPoint(jPoint);
-        }
-      );
+      stable_sort(AuxQueue.begin(), AuxQueue.end(), [&](unsigned long iPoint, unsigned long jPoint) {
+        return nodes->GetnPoint(iPoint) < nodes->GetnPoint(jPoint);
+      });
       Result.insert(Result.end(), AuxQueue.begin(), AuxQueue.end());
     }
   }
@@ -4868,7 +4557,7 @@ void CPhysicalGeometry::SetRCM_Ordering(CConfig *config) {
   for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
     AuxGlobalIndex[iPoint] = nodes->GetGlobalIndex(iPoint);
     for (auto iDim = 0u; iDim < nDim; iDim++) {
-      AuxCoord(iPoint,iDim) = nodes->GetCoord(iPoint, iDim);
+      AuxCoord(iPoint, iDim) = nodes->GetCoord(iPoint, iDim);
     }
   }
 
@@ -4879,7 +4568,7 @@ void CPhysicalGeometry::SetRCM_Ordering(CConfig *config) {
 
   /*--- Set the new conectivities ---*/
 
-  auto& InvResult = AuxGlobalIndex; // alias to re-use storage
+  auto& InvResult = AuxGlobalIndex;  // alias to re-use storage
   for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
     InvResult[Result[iPoint]] = iPoint;
   }
@@ -4893,9 +4582,7 @@ void CPhysicalGeometry::SetRCM_Ordering(CConfig *config) {
 
   for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
     for (auto iElem = 0ul; iElem < nElem_Bound[iMarker]; iElem++) {
-
-      if (config->GetMarker_All_KindBC(iMarker) == SEND_RECEIVE &&
-          config->GetMarker_All_SendRecv(iMarker) < 0) {
+      if (config->GetMarker_All_KindBC(iMarker) == SEND_RECEIVE && config->GetMarker_All_SendRecv(iMarker) < 0) {
         nodes->SetDomain(bound[iMarker][iElem]->GetNode(0), false);
       }
 
@@ -4909,18 +4596,15 @@ void CPhysicalGeometry::SetRCM_Ordering(CConfig *config) {
             config->GetMarker_All_KindBC(iMarker) != PERIODIC_BOUNDARY)
           nodes->SetPhysicalBoundary(InvResult[iPoint], true);
 
-        if (config->GetSolid_Wall(iMarker))
-          nodes->SetSolidBoundary(InvResult[iPoint], true);
+        if (config->GetSolid_Wall(iMarker)) nodes->SetSolidBoundary(InvResult[iPoint], true);
 
-        if (config->GetViscous_Wall(iMarker) )
-          nodes->SetViscousBoundary(InvResult[iPoint], true);
+        if (config->GetViscous_Wall(iMarker)) nodes->SetViscousBoundary(InvResult[iPoint], true);
 
         if (config->GetMarker_All_KindBC(iMarker) == PERIODIC_BOUNDARY)
           nodes->SetPeriodicBoundary(InvResult[iPoint], true);
       }
     }
   }
-
 }
 
 void CPhysicalGeometry::SetElement_Connectivity(void) {
@@ -4943,7 +4627,6 @@ void CPhysicalGeometry::SetElement_Connectivity(void) {
 
           if ((elem[iElem]->GetNeighbor_Elements(iFace) == -1) && (iElem < Test_Elem) &&
               FindFace(iElem, Test_Elem, first_elem_face, second_elem_face)) {
-
             /*--- Localice which faces are sharing both elements ---*/
 
             elem[iElem]->SetNeighbor_Elements(Test_Elem, first_elem_face);
@@ -4951,7 +4634,6 @@ void CPhysicalGeometry::SetElement_Connectivity(void) {
             /*--- Store the element for both elements ---*/
 
             elem[Test_Elem]->SetNeighbor_Elements(iElem, second_elem_face);
-
           }
         }
       }
@@ -4964,14 +4646,14 @@ void CPhysicalGeometry::SetBoundVolume(void) {
 
   for (iMarker = 0; iMarker < nMarker; iMarker++)
     for (iElem_Surface = 0; iElem_Surface < nElem_Bound[iMarker]; iElem_Surface++) {
-
       /*--- Choose and arbitrary point from the surface --*/
       Point = bound[iMarker][iElem_Surface]->GetNode(0);
       CheckVol = false;
 
       for (iElem = 0; iElem < nodes->GetnElem(Point); iElem++) {
         /*--- Look for elements surronding that point --*/
-        cont = 0; iElem_Domain = nodes->GetElem(Point, iElem);
+        cont = 0;
+        iElem_Domain = nodes->GetElem(Point, iElem);
         for (iNode_Domain = 0; iNode_Domain < elem[iElem_Domain]->GetnNodes(); iNode_Domain++) {
           Point_Domain = elem[iElem_Domain]->GetNode(iNode_Domain);
           for (iNode_Surface = 0; iNode_Surface < bound[iMarker][iElem_Surface]->GetnNodes(); iNode_Surface++) {
@@ -4990,27 +4672,25 @@ void CPhysicalGeometry::SetBoundVolume(void) {
       }
       if (!CheckVol) {
         char buf[100];
-        SPRINTF(buf,"The surface element (%u, %lu) doesn't have an associated volume element", iMarker, iElem_Surface );
+        SPRINTF(buf, "The surface element (%u, %lu) doesn't have an associated volume element", iMarker, iElem_Surface);
         SU2_MPI::Error(buf, CURRENT_FUNCTION);
       }
     }
 }
 
-void CPhysicalGeometry::SetVertex(const CConfig *config) {
-  unsigned long  iPoint, iVertex, iElem;
+void CPhysicalGeometry::SetVertex(const CConfig* config) {
+  unsigned long iPoint, iVertex, iElem;
   unsigned short iMarker, iNode;
 
   /*--- Initialize the Vertex vector for each node of the grid ---*/
 
   for (iPoint = 0; iPoint < nPoint; iPoint++)
-    for (iMarker = 0; iMarker < nMarker; iMarker++)
-      nodes->SetVertex(iPoint, -1, iMarker);
+    for (iMarker = 0; iMarker < nMarker; iMarker++) nodes->SetVertex(iPoint, -1, iMarker);
 
   /*--- Create and compute the vector with the number of vertex per marker ---*/
 
-  nVertex = new unsigned long [nMarker];
+  nVertex = new unsigned long[nMarker];
   for (iMarker = 0; iMarker < nMarker; iMarker++) {
-
     /*--- Initialize the number of Bound Vertex for each Marker ---*/
 
     nVertex[iMarker] = 0;
@@ -5030,15 +4710,14 @@ void CPhysicalGeometry::SetVertex(const CConfig *config) {
   /*--- Initialize the Vertex vector for each node, the previous result is deleted ---*/
 
   for (iPoint = 0; iPoint < nPoint; iPoint++)
-    for (iMarker = 0; iMarker < nMarker; iMarker++)
-      nodes->SetVertex(iPoint, -1, iMarker);
+    for (iMarker = 0; iMarker < nMarker; iMarker++) nodes->SetVertex(iPoint, -1, iMarker);
 
   /*--- Create the bound vertex structure, note that the order
    is the same as in the input file, this is important for Send/Receive part ---*/
 
   vertex = new CVertex**[nMarker];
   for (iMarker = 0; iMarker < nMarker; iMarker++) {
-    vertex[iMarker] = new CVertex* [nVertex[iMarker]];
+    vertex[iMarker] = new CVertex*[nVertex[iMarker]];
     nVertex[iMarker] = 0;
 
     /*--- Initialize the number of Bound Vertex for each Marker ---*/
@@ -5063,7 +4742,8 @@ void CPhysicalGeometry::SetVertex(const CConfig *config) {
   }
 }
 
-void CPhysicalGeometry::ComputeNSpan(CConfig *config, unsigned short val_iZone, unsigned short marker_flag, bool allocate) {
+void CPhysicalGeometry::ComputeNSpan(CConfig* config, unsigned short val_iZone, unsigned short marker_flag,
+                                     bool allocate) {
   unsigned short iMarker, jMarker, iMarkerTP, iSpan, jSpan;
   unsigned long iPoint, iVertex;
   long jVertex;
@@ -5078,40 +4758,37 @@ void CPhysicalGeometry::ComputeNSpan(CConfig *config, unsigned short val_iZone,
 
   nSpan = 0;
   nSpan_loc = 0;
-  if (nDim == 2){
-    nSpanWiseSections[marker_flag-1] = 1;
-    //TODO (turbo) make it more genral
-    if(marker_flag == OUTFLOW) config->SetnSpanWiseSections(1);
+  if (nDim == 2) {
+    nSpanWiseSections[marker_flag - 1] = 1;
+    // TODO (turbo) make it more genral
+    if (marker_flag == OUTFLOW) config->SetnSpanWiseSections(1);
 
     /*---Initilize the vector of span-wise values that will be ordered ---*/
-    SpanWiseValue[marker_flag -1] = new su2double[1];
-    for (iSpan = 0; iSpan < 1; iSpan++){
-      SpanWiseValue[marker_flag -1][iSpan] = 0;
+    SpanWiseValue[marker_flag - 1] = new su2double[1];
+    for (iSpan = 0; iSpan < 1; iSpan++) {
+      SpanWiseValue[marker_flag - 1][iSpan] = 0;
     }
-  }
-  else{
-    if(SpanWise_Kind == AUTOMATIC){
+  } else {
+    if (SpanWise_Kind == AUTOMATIC) {
       /*--- loop to find inflow of outflow marker---*/
-      for (iMarker = 0; iMarker < nMarker; iMarker++){
-        for (iMarkerTP=1; iMarkerTP < config->GetnMarker_Turbomachinery()+1; iMarkerTP++){
-
+      for (iMarker = 0; iMarker < nMarker; iMarker++) {
+        for (iMarkerTP = 1; iMarkerTP < config->GetnMarker_Turbomachinery() + 1; iMarkerTP++) {
           if (config->GetMarker_All_Turbomachinery(iMarker) != iMarkerTP) continue;
           if (config->GetMarker_All_TurbomachineryFlag(iMarker) != marker_flag) continue;
 
           /*--- loop to find the vertex that ar both of inflow or outflow marker and on the periodic
            * in order to caount the number of Span ---*/
-          for (jMarker = 0; jMarker < nMarker; jMarker++){
+          for (jMarker = 0; jMarker < nMarker; jMarker++) {
             if (config->GetMarker_All_KindBC(jMarker) != PERIODIC_BOUNDARY) continue;
 
             for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
-
               iPoint = vertex[iMarker][iVertex]->GetNode();
               if (!nodes->GetDomain(iPoint)) continue;
 
               PeriodicBoundary = config->GetMarker_All_PerBound(jMarker);
               jVertex = nodes->GetVertex(iPoint, jMarker);
 
-              if ((jVertex != -1) && (PeriodicBoundary == (val_iZone + 1))){
+              if ((jVertex != -1) && (PeriodicBoundary == (val_iZone + 1))) {
                 nSpan++;
               }
             }
@@ -5125,61 +4802,57 @@ void CPhysicalGeometry::ComputeNSpan(CConfig *config, unsigned short val_iZone,
       SU2_MPI::Allreduce(&nSpan_loc, &nSpan_max, 1, MPI_INT, MPI_MAX, SU2_MPI::GetComm());
 
       /*--- initialize the vector that will contain the disordered values span-wise ---*/
-      nSpanWiseSections[marker_flag -1] = nSpan;
+      nSpanWiseSections[marker_flag - 1] = nSpan;
       valueSpan = new su2double[nSpan];
 
-      for (iSpan = 0; iSpan < nSpan; iSpan ++ ){
+      for (iSpan = 0; iSpan < nSpan; iSpan++) {
         valueSpan[iSpan] = -1001.0;
       }
 
       /*--- store the local span-wise value for each processor ---*/
       nSpan_loc = 0;
-      for (iMarker = 0; iMarker < nMarker; iMarker++){
-        for (iMarkerTP=1; iMarkerTP < config->GetnMarker_Turbomachinery()+1; iMarkerTP++){
-
+      for (iMarker = 0; iMarker < nMarker; iMarker++) {
+        for (iMarkerTP = 1; iMarkerTP < config->GetnMarker_Turbomachinery() + 1; iMarkerTP++) {
           if (config->GetMarker_All_Turbomachinery(iMarker) != iMarkerTP) continue;
           if (config->GetMarker_All_TurbomachineryFlag(iMarker) != marker_flag) continue;
 
-          for (jMarker = 0; jMarker < nMarker; jMarker++){
+          for (jMarker = 0; jMarker < nMarker; jMarker++) {
             if (config->GetMarker_All_KindBC(jMarker) != PERIODIC_BOUNDARY) continue;
 
             for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
-
               iPoint = vertex[iMarker][iVertex]->GetNode();
               if (!nodes->GetDomain(iPoint)) continue;
 
               PeriodicBoundary = config->GetMarker_All_PerBound(jMarker);
               jVertex = nodes->GetVertex(iPoint, jMarker);
 
-              if ((jVertex != -1) && (PeriodicBoundary == (val_iZone + 1))){
+              if ((jVertex != -1) && (PeriodicBoundary == (val_iZone + 1))) {
                 coord = nodes->GetCoord(iPoint);
-                radius = sqrt(coord[0]*coord[0]+coord[1]*coord[1]);
-                switch (config->GetKind_TurboMachinery(val_iZone)){
-                case CENTRIFUGAL:
-                  valueSpan[nSpan_loc] = coord[2];
-                  break;
-                case CENTRIPETAL:
-                  valueSpan[nSpan_loc] = coord[2];
-                  break;
-                case AXIAL:
-                  valueSpan[nSpan_loc] = radius;
-                  break;
-                case CENTRIPETAL_AXIAL:
-                  if (marker_flag == OUTFLOW){
-                    valueSpan[nSpan_loc] = radius;
-                  }
-                  else{
+                radius = sqrt(coord[0] * coord[0] + coord[1] * coord[1]);
+                switch (config->GetKind_TurboMachinery(val_iZone)) {
+                  case CENTRIFUGAL:
                     valueSpan[nSpan_loc] = coord[2];
-                  }
-                  break;
-                case AXIAL_CENTRIFUGAL:
-                  if (marker_flag == INFLOW){
-                    valueSpan[nSpan_loc] = radius;
-                  }
-                  else{
+                    break;
+                  case CENTRIPETAL:
                     valueSpan[nSpan_loc] = coord[2];
-                  }
-                  break;
+                    break;
+                  case AXIAL:
+                    valueSpan[nSpan_loc] = radius;
+                    break;
+                  case CENTRIPETAL_AXIAL:
+                    if (marker_flag == OUTFLOW) {
+                      valueSpan[nSpan_loc] = radius;
+                    } else {
+                      valueSpan[nSpan_loc] = coord[2];
+                    }
+                    break;
+                  case AXIAL_CENTRIFUGAL:
+                    if (marker_flag == INFLOW) {
+                      valueSpan[nSpan_loc] = radius;
+                    } else {
+                      valueSpan[nSpan_loc] = coord[2];
+                    }
+                    break;
                 }
                 nSpan_loc++;
               }
@@ -5190,96 +4863,92 @@ void CPhysicalGeometry::ComputeNSpan(CConfig *config, unsigned short val_iZone,
 
       /*--- Gather the span-wise values on all the processor ---*/
 
-      vector<su2double> MyTotValueSpan(nSpan_max*size, -1001.0);
+      vector<su2double> MyTotValueSpan(nSpan_max * size, -1001.0);
       vector<su2double> MyValueSpan(nSpan_max, -1001.0);
       vector<int> My_nSpan_loc(size);
 
-      for(iSpan = 0; iSpan<nSpan_loc; iSpan++){
+      for (iSpan = 0; iSpan < nSpan_loc; iSpan++) {
         MyValueSpan[iSpan] = valueSpan[iSpan];
       }
 
-      SU2_MPI::Allgather(MyValueSpan.data(), nSpan_max , MPI_DOUBLE, MyTotValueSpan.data(), nSpan_max, MPI_DOUBLE, SU2_MPI::GetComm());
-      SU2_MPI::Allgather(&nSpan_loc, 1 , MPI_INT, My_nSpan_loc.data(), 1, MPI_INT, SU2_MPI::GetComm());
+      SU2_MPI::Allgather(MyValueSpan.data(), nSpan_max, MPI_DOUBLE, MyTotValueSpan.data(), nSpan_max, MPI_DOUBLE,
+                         SU2_MPI::GetComm());
+      SU2_MPI::Allgather(&nSpan_loc, 1, MPI_INT, My_nSpan_loc.data(), 1, MPI_INT, SU2_MPI::GetComm());
 
       jSpan = 0;
-      for (iSize = 0; iSize< size; iSize++){
-        for(iSpan = 0; iSpan < My_nSpan_loc[iSize]; iSpan++){
-          valueSpan[jSpan] = MyTotValueSpan[iSize*nSpan_max + iSpan];
+      for (iSize = 0; iSize < size; iSize++) {
+        for (iSpan = 0; iSpan < My_nSpan_loc[iSize]; iSpan++) {
+          valueSpan[jSpan] = MyTotValueSpan[iSize * nSpan_max + iSpan];
           jSpan++;
         }
       }
-      if (jSpan != nSpan) SU2_MPI::Error("Panic!",CURRENT_FUNCTION);
+      if (jSpan != nSpan) SU2_MPI::Error("Panic!", CURRENT_FUNCTION);
 
       /*--- Terrible stuff to do but so is this entire bloody function goodness me... ---*/
-      SpanWiseValue[marker_flag -1] = valueSpan;
+      SpanWiseValue[marker_flag - 1] = valueSpan;
 
-      sort(SpanWiseValue[marker_flag -1], SpanWiseValue[marker_flag -1]+nSpan);
+      sort(SpanWiseValue[marker_flag - 1], SpanWiseValue[marker_flag - 1] + nSpan);
 
       /*--- Find the minimum value among the span-wise values  ---*/
-      min = SpanWiseValue[marker_flag -1][0];
+      min = SpanWiseValue[marker_flag - 1][0];
     }
     /*--- Compute equispaced Span-wise sections using number of section specified by the User---*/
-    else{
+    else {
       /*--- Initialize number of span---*/
-      nSpanWiseSections[marker_flag-1] = config->Get_nSpanWiseSections_User();
-      SpanWiseValue[marker_flag -1] = new su2double[config->Get_nSpanWiseSections_User()];
-      for (iSpan = 0; iSpan < config->Get_nSpanWiseSections_User(); iSpan++){
-        SpanWiseValue[marker_flag -1][iSpan] = 0;
+      nSpanWiseSections[marker_flag - 1] = config->Get_nSpanWiseSections_User();
+      SpanWiseValue[marker_flag - 1] = new su2double[config->Get_nSpanWiseSections_User()];
+      for (iSpan = 0; iSpan < config->Get_nSpanWiseSections_User(); iSpan++) {
+        SpanWiseValue[marker_flag - 1][iSpan] = 0;
       }
       /*--- Compute maximum and minimum value span-wise---*/
       min = 1E+07;
-      max =-1E+07;
-      for (iMarker = 0; iMarker < nMarker; iMarker++){
-        for (iMarkerTP=1; iMarkerTP < config->GetnMarker_Turbomachinery()+1; iMarkerTP++){
-
+      max = -1E+07;
+      for (iMarker = 0; iMarker < nMarker; iMarker++) {
+        for (iMarkerTP = 1; iMarkerTP < config->GetnMarker_Turbomachinery() + 1; iMarkerTP++) {
           if (config->GetMarker_All_Turbomachinery(iMarker) != iMarkerTP) continue;
           if (config->GetMarker_All_TurbomachineryFlag(iMarker) != marker_flag) continue;
 
-          for (jMarker = 0; jMarker < nMarker; jMarker++){
+          for (jMarker = 0; jMarker < nMarker; jMarker++) {
             if (config->GetMarker_All_KindBC(jMarker) != PERIODIC_BOUNDARY) continue;
 
             for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
-
               iPoint = vertex[iMarker][iVertex]->GetNode();
               if (!nodes->GetDomain(iPoint)) continue;
 
               PeriodicBoundary = config->GetMarker_All_PerBound(jMarker);
               jVertex = nodes->GetVertex(iPoint, jMarker);
 
-              if ((jVertex != -1) && (PeriodicBoundary == (val_iZone + 1))){
-
+              if ((jVertex != -1) && (PeriodicBoundary == (val_iZone + 1))) {
                 coord = nodes->GetCoord(iPoint);
-                radius = sqrt(coord[0]*coord[0]+coord[1]*coord[1]);
-                switch (config->GetKind_TurboMachinery(val_iZone)){
-                case CENTRIFUGAL:
-                case CENTRIPETAL:
-                  if (coord[2] < min) min = coord[2];
-                  if (coord[2] > max) max = coord[2];
-                  break;
-                case AXIAL:
-                  if (radius < min) min = radius;
-                  if (radius > max) max = radius;
-                  break;
-                case CENTRIPETAL_AXIAL:
-                  if (marker_flag == OUTFLOW){
-                    if (radius < min) min = radius;
-                    if (radius > max) max = radius;
-                  }
-                  else{
+                radius = sqrt(coord[0] * coord[0] + coord[1] * coord[1]);
+                switch (config->GetKind_TurboMachinery(val_iZone)) {
+                  case CENTRIFUGAL:
+                  case CENTRIPETAL:
                     if (coord[2] < min) min = coord[2];
                     if (coord[2] > max) max = coord[2];
-                  }
-                  break;
-                case AXIAL_CENTRIFUGAL:
-                  if (marker_flag == INFLOW){
+                    break;
+                  case AXIAL:
                     if (radius < min) min = radius;
                     if (radius > max) max = radius;
-                  }
-                  else{
-                    if (coord[2] < min) min = coord[2];
-                    if (coord[2] > max) max = coord[2];
-                  }
-                  break;
+                    break;
+                  case CENTRIPETAL_AXIAL:
+                    if (marker_flag == OUTFLOW) {
+                      if (radius < min) min = radius;
+                      if (radius > max) max = radius;
+                    } else {
+                      if (coord[2] < min) min = coord[2];
+                      if (coord[2] > max) max = coord[2];
+                    }
+                    break;
+                  case AXIAL_CENTRIFUGAL:
+                    if (marker_flag == INFLOW) {
+                      if (radius < min) min = radius;
+                      if (radius > max) max = radius;
+                    } else {
+                      if (coord[2] < min) min = coord[2];
+                      if (coord[2] > max) max = coord[2];
+                    }
+                    break;
                 }
               }
             }
@@ -5287,115 +4956,120 @@ void CPhysicalGeometry::ComputeNSpan(CConfig *config, unsigned short val_iZone,
         }
       }
       /*--- compute global minimum and maximum value on span-wise ---*/
-      MyMin= min;  min = 0;
-      MyMax= max;  max = 0;
+      MyMin = min;
+      min = 0;
+      MyMax = max;
+      max = 0;
       SU2_MPI::Allreduce(&MyMin, &min, 1, MPI_DOUBLE, MPI_MIN, SU2_MPI::GetComm());
       SU2_MPI::Allreduce(&MyMax, &max, 1, MPI_DOUBLE, MPI_MAX, SU2_MPI::GetComm());
 
       /*--- compute height value for each spanwise section---*/
-      delta = (max - min)/(nSpanWiseSections[marker_flag-1] -1);
-      for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-        SpanWiseValue[marker_flag - 1][iSpan]= min + delta*iSpan;
+      delta = (max - min) / (nSpanWiseSections[marker_flag - 1] - 1);
+      for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+        SpanWiseValue[marker_flag - 1][iSpan] = min + delta * iSpan;
       }
     }
 
-    if(marker_flag == OUTFLOW){
-      if(nSpanWiseSections[INFLOW -1] != nSpanWiseSections[OUTFLOW - 1]){
+    if (marker_flag == OUTFLOW) {
+      if (nSpanWiseSections[INFLOW - 1] != nSpanWiseSections[OUTFLOW - 1]) {
         char buf[100];
-        SPRINTF(buf, "nSpan inflow %u, nSpan outflow %u", nSpanWiseSections[INFLOW-1], nSpanWiseSections[OUTFLOW-1]);
-        SU2_MPI::Error(string(" At the moment only turbomachinery with the same amount of span-wise section can be simulated\n") + buf, CURRENT_FUNCTION);
-      }
-      else{
-        config->SetnSpanWiseSections(nSpanWiseSections[OUTFLOW -1]);
+        SPRINTF(buf, "nSpan inflow %u, nSpan outflow %u", nSpanWiseSections[INFLOW - 1],
+                nSpanWiseSections[OUTFLOW - 1]);
+        SU2_MPI::Error(
+            string(" At the moment only turbomachinery with the same amount of span-wise section can be simulated\n") +
+                buf,
+            CURRENT_FUNCTION);
+      } else {
+        config->SetnSpanWiseSections(nSpanWiseSections[OUTFLOW - 1]);
       }
     }
-
   }
-
 }
 
-void CPhysicalGeometry::SetTurboVertex(CConfig *config, unsigned short val_iZone, unsigned short marker_flag, bool allocate) {
-  unsigned long  iPoint, **ordered, **disordered, **oldVertex3D, iInternalVertex;
+void CPhysicalGeometry::SetTurboVertex(CConfig* config, unsigned short val_iZone, unsigned short marker_flag,
+                                       bool allocate) {
+  unsigned long iPoint, **ordered, **disordered, **oldVertex3D, iInternalVertex;
   unsigned long nVert, nVertMax;
   unsigned short iMarker, iMarkerTP, iSpan, jSpan, iDim;
-  su2double min, minInt, max, *coord, dist, Normal2, *TurboNormal, *NormalArea, target = 0.0, **area, ***unitnormal, Area = 0.0;
-  bool **checkAssign;
-  min    =  10.0E+06;
-  minInt =  10.0E+06;
-  max    = -10.0E+06;
+  su2double min, minInt, max, *coord, dist, Normal2, *TurboNormal, *NormalArea, target = 0.0, **area, ***unitnormal,
+                                                                                Area = 0.0;
+  bool** checkAssign;
+  min = 10.0E+06;
+  minInt = 10.0E+06;
+  max = -10.0E+06;
 
   su2double radius;
   long iVertex, iSpanVertex, jSpanVertex, kSpanVertex = 0;
   int *nTotVertex_gb, *nVertexSpanHalo;
-  su2double **x_loc, **y_loc, **z_loc, **angCoord_loc, **deltaAngCoord_loc, **angPitch, **deltaAngPitch, *minIntAngPitch,
-  *minAngPitch, *maxAngPitch;
-  int       **rank_loc;
+  su2double **x_loc, **y_loc, **z_loc, **angCoord_loc, **deltaAngCoord_loc, **angPitch, **deltaAngPitch,
+      *minIntAngPitch, *minAngPitch, *maxAngPitch;
+  int** rank_loc;
 #ifdef HAVE_MPI
   unsigned short iSize, kSize = 0, jSize;
-  su2double MyMin,MyIntMin, MyMax;
+  su2double MyMin, MyIntMin, MyMax;
   su2double *x_gb = NULL, *y_gb = NULL, *z_gb = NULL, *angCoord_gb = NULL, *deltaAngCoord_gb = NULL;
-  bool *checkAssign_gb =NULL;
+  bool* checkAssign_gb = NULL;
   unsigned long My_nVert;
 
 #endif
   string multizone_filename;
 
-  x_loc              = new su2double*[nSpanWiseSections[marker_flag-1]];
-  y_loc              = new su2double*[nSpanWiseSections[marker_flag-1]];
-  z_loc              = new su2double*[nSpanWiseSections[marker_flag-1]];
-  angCoord_loc       = new su2double*[nSpanWiseSections[marker_flag-1]];
-  deltaAngCoord_loc  = new su2double*[nSpanWiseSections[marker_flag-1]];
-  angPitch           = new su2double*[nSpanWiseSections[marker_flag-1]];
-  deltaAngPitch      = new su2double*[nSpanWiseSections[marker_flag-1]];
-  rank_loc           = new int*[nSpanWiseSections[marker_flag-1]];
-  minAngPitch        = new su2double[nSpanWiseSections[marker_flag-1]];
-  minIntAngPitch     = new su2double[nSpanWiseSections[marker_flag-1]];
-  maxAngPitch        = new su2double[nSpanWiseSections[marker_flag-1]];
-
-  nTotVertex_gb      = new int[nSpanWiseSections[marker_flag-1]];
-  nVertexSpanHalo    = new int[nSpanWiseSections[marker_flag-1]];
-  for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-    nTotVertex_gb[iSpan]   = -1;
+  x_loc = new su2double*[nSpanWiseSections[marker_flag - 1]];
+  y_loc = new su2double*[nSpanWiseSections[marker_flag - 1]];
+  z_loc = new su2double*[nSpanWiseSections[marker_flag - 1]];
+  angCoord_loc = new su2double*[nSpanWiseSections[marker_flag - 1]];
+  deltaAngCoord_loc = new su2double*[nSpanWiseSections[marker_flag - 1]];
+  angPitch = new su2double*[nSpanWiseSections[marker_flag - 1]];
+  deltaAngPitch = new su2double*[nSpanWiseSections[marker_flag - 1]];
+  rank_loc = new int*[nSpanWiseSections[marker_flag - 1]];
+  minAngPitch = new su2double[nSpanWiseSections[marker_flag - 1]];
+  minIntAngPitch = new su2double[nSpanWiseSections[marker_flag - 1]];
+  maxAngPitch = new su2double[nSpanWiseSections[marker_flag - 1]];
+
+  nTotVertex_gb = new int[nSpanWiseSections[marker_flag - 1]];
+  nVertexSpanHalo = new int[nSpanWiseSections[marker_flag - 1]];
+  for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+    nTotVertex_gb[iSpan] = -1;
     nVertexSpanHalo[iSpan] = 0;
-    minAngPitch[iSpan]     = 10.0E+06;
-    minIntAngPitch[iSpan]  = 10.0E+06;
-    maxAngPitch[iSpan]     = -10.0E+06;
+    minAngPitch[iSpan] = 10.0E+06;
+    minIntAngPitch[iSpan] = 10.0E+06;
+    maxAngPitch[iSpan] = -10.0E+06;
   }
 
   /*--- Initialize auxiliary pointers ---*/
-  TurboNormal        = new su2double[3];
-  NormalArea         = new su2double[3];
-  ordered            = new unsigned long* [nSpanWiseSections[marker_flag-1]];
-  disordered         = new unsigned long* [nSpanWiseSections[marker_flag-1]];
-  oldVertex3D        = new unsigned long* [nSpanWiseSections[marker_flag-1]];
-  area               = new su2double* [nSpanWiseSections[marker_flag-1]];
-  unitnormal         = new su2double** [nSpanWiseSections[marker_flag-1]];
-  checkAssign        = new bool* [nSpanWiseSections[marker_flag-1]];
+  TurboNormal = new su2double[3];
+  NormalArea = new su2double[3];
+  ordered = new unsigned long*[nSpanWiseSections[marker_flag - 1]];
+  disordered = new unsigned long*[nSpanWiseSections[marker_flag - 1]];
+  oldVertex3D = new unsigned long*[nSpanWiseSections[marker_flag - 1]];
+  area = new su2double*[nSpanWiseSections[marker_flag - 1]];
+  unitnormal = new su2double**[nSpanWiseSections[marker_flag - 1]];
+  checkAssign = new bool*[nSpanWiseSections[marker_flag - 1]];
 
   /*--- Initialize the new Vertex structure. The if statement ensures that these vectors are initialized
    * only once even if the routine is called more than once.---*/
 
-  if (allocate){
-    for (iMarker = 0; iMarker < nMarker; iMarker++){
-      for (iMarkerTP=1; iMarkerTP < config->GetnMarker_Turbomachinery()+1; iMarkerTP++){
-        if (config->GetMarker_All_Turbomachinery(iMarker) == iMarkerTP){
-          if (config->GetMarker_All_TurbomachineryFlag(iMarker) == marker_flag){
-            nSpanSectionsByMarker[iMarker]       = nSpanWiseSections[marker_flag-1];
-            nVertexSpan[iMarker]                 = new long[nSpanWiseSections[marker_flag-1]];
-            turbovertex[iMarker]                 = new CTurboVertex** [nSpanWiseSections[marker_flag-1]];
-            nTotVertexSpan[iMarker]              = new unsigned long [nSpanWiseSections[marker_flag-1] +1];
-            MaxAngularCoord[iMarker]             = new su2double [nSpanWiseSections[marker_flag-1]];
-            MinAngularCoord[iMarker]             = new su2double [nSpanWiseSections[marker_flag-1]];
-            MinRelAngularCoord[iMarker]          = new su2double [nSpanWiseSections[marker_flag-1]];
-            for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-              nVertexSpan[iMarker][iSpan]        = 0;
-              turbovertex[iMarker][iSpan]        = nullptr;
-              MinAngularCoord[iMarker][iSpan]    = 10.0E+06;
-              MaxAngularCoord[iMarker][iSpan]    = -10.0E+06;
+  if (allocate) {
+    for (iMarker = 0; iMarker < nMarker; iMarker++) {
+      for (iMarkerTP = 1; iMarkerTP < config->GetnMarker_Turbomachinery() + 1; iMarkerTP++) {
+        if (config->GetMarker_All_Turbomachinery(iMarker) == iMarkerTP) {
+          if (config->GetMarker_All_TurbomachineryFlag(iMarker) == marker_flag) {
+            nSpanSectionsByMarker[iMarker] = nSpanWiseSections[marker_flag - 1];
+            nVertexSpan[iMarker] = new long[nSpanWiseSections[marker_flag - 1]];
+            turbovertex[iMarker] = new CTurboVertex**[nSpanWiseSections[marker_flag - 1]];
+            nTotVertexSpan[iMarker] = new unsigned long[nSpanWiseSections[marker_flag - 1] + 1];
+            MaxAngularCoord[iMarker] = new su2double[nSpanWiseSections[marker_flag - 1]];
+            MinAngularCoord[iMarker] = new su2double[nSpanWiseSections[marker_flag - 1]];
+            MinRelAngularCoord[iMarker] = new su2double[nSpanWiseSections[marker_flag - 1]];
+            for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+              nVertexSpan[iMarker][iSpan] = 0;
+              turbovertex[iMarker][iSpan] = nullptr;
+              MinAngularCoord[iMarker][iSpan] = 10.0E+06;
+              MaxAngularCoord[iMarker][iSpan] = -10.0E+06;
               MinRelAngularCoord[iMarker][iSpan] = 10.0E+06;
             }
-            for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1] +1; iSpan++){
-              nTotVertexSpan[iMarker][iSpan]     = 0;
+            for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1] + 1; iSpan++) {
+              nTotVertexSpan[iMarker][iSpan] = 0;
             }
           }
         }
@@ -5403,330 +5077,324 @@ void CPhysicalGeometry::SetTurboVertex(CConfig *config, unsigned short val_iZone
     }
   }
 
-  //this works only for turbomachinery rotating around the Z-Axes.
-  // the reordering algorithm pitch-wise assumes that X-coordinate of each boundary vertex is positive so that reordering can be based on the Y-coordinate.
-    for (iMarker = 0; iMarker < nMarker; iMarker++){
-      for (iMarkerTP=1; iMarkerTP < config->GetnMarker_Turbomachinery()+1; iMarkerTP++){
-        if (config->GetMarker_All_Turbomachinery(iMarker) == iMarkerTP){
-          if (config->GetMarker_All_TurbomachineryFlag(iMarker) == marker_flag){
-
-            /*--- compute the amount of vertexes for each span-wise section to initialize the CTurboVertex pointers and auxiliary pointers  ---*/
-            for (iVertex = 0; (unsigned long)iVertex  < nVertex[iMarker]; iVertex++) {
-              iPoint = vertex[iMarker][iVertex]->GetNode();
-              if (nDim == 3){
-                dist = 10E+06;
-                jSpan = std::numeric_limits<unsigned short>::max();
-                coord = nodes->GetCoord(iPoint);
+  // this works only for turbomachinery rotating around the Z-Axes.
+  //  the reordering algorithm pitch-wise assumes that X-coordinate of each boundary vertex is positive so that
+  //  reordering can be based on the Y-coordinate.
+  for (iMarker = 0; iMarker < nMarker; iMarker++) {
+    for (iMarkerTP = 1; iMarkerTP < config->GetnMarker_Turbomachinery() + 1; iMarkerTP++) {
+      if (config->GetMarker_All_Turbomachinery(iMarker) == iMarkerTP) {
+        if (config->GetMarker_All_TurbomachineryFlag(iMarker) == marker_flag) {
+          /*--- compute the amount of vertexes for each span-wise section to initialize the CTurboVertex pointers and
+           * auxiliary pointers  ---*/
+          for (iVertex = 0; (unsigned long)iVertex < nVertex[iMarker]; iVertex++) {
+            iPoint = vertex[iMarker][iVertex]->GetNode();
+            if (nDim == 3) {
+              dist = 10E+06;
+              jSpan = std::numeric_limits<unsigned short>::max();
+              coord = nodes->GetCoord(iPoint);
 
-                switch (config->GetKind_TurboMachinery(val_iZone)){
-                case CENTRIFUGAL: case CENTRIPETAL:
-                  for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-                    if (dist > (abs(coord[2]-SpanWiseValue[marker_flag-1][iSpan]))){
-                      dist= abs(coord[2]-SpanWiseValue[marker_flag-1][iSpan]);
-                      jSpan=iSpan;
+              switch (config->GetKind_TurboMachinery(val_iZone)) {
+                case CENTRIFUGAL:
+                case CENTRIPETAL:
+                  for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+                    if (dist > (abs(coord[2] - SpanWiseValue[marker_flag - 1][iSpan]))) {
+                      dist = abs(coord[2] - SpanWiseValue[marker_flag - 1][iSpan]);
+                      jSpan = iSpan;
                     }
                   }
                   break;
                 case AXIAL:
-                  radius = sqrt(coord[0]*coord[0]+coord[1]*coord[1]);
-                  for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-                    if (dist > (abs(radius - SpanWiseValue[marker_flag-1][iSpan]))){
-                      dist= abs(radius-SpanWiseValue[marker_flag-1][iSpan]);
-                      jSpan=iSpan;
+                  radius = sqrt(coord[0] * coord[0] + coord[1] * coord[1]);
+                  for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+                    if (dist > (abs(radius - SpanWiseValue[marker_flag - 1][iSpan]))) {
+                      dist = abs(radius - SpanWiseValue[marker_flag - 1][iSpan]);
+                      jSpan = iSpan;
                     }
                   }
                   break;
                 case CENTRIPETAL_AXIAL:
-                  if (marker_flag == OUTFLOW){
-                    radius = sqrt(coord[0]*coord[0]+coord[1]*coord[1]);
-                    for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-                      if (dist > (abs(radius - SpanWiseValue[marker_flag-1][iSpan]))){
-                        dist= abs(radius-SpanWiseValue[marker_flag-1][iSpan]);
-                        jSpan=iSpan;
+                  if (marker_flag == OUTFLOW) {
+                    radius = sqrt(coord[0] * coord[0] + coord[1] * coord[1]);
+                    for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+                      if (dist > (abs(radius - SpanWiseValue[marker_flag - 1][iSpan]))) {
+                        dist = abs(radius - SpanWiseValue[marker_flag - 1][iSpan]);
+                        jSpan = iSpan;
                       }
                     }
-                  }
-                  else{
-                    for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-                      if (dist > (abs(coord[2]-SpanWiseValue[marker_flag-1][iSpan]))){
-                        dist= abs(coord[2]-SpanWiseValue[marker_flag-1][iSpan]);
-                        jSpan=iSpan;
+                  } else {
+                    for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+                      if (dist > (abs(coord[2] - SpanWiseValue[marker_flag - 1][iSpan]))) {
+                        dist = abs(coord[2] - SpanWiseValue[marker_flag - 1][iSpan]);
+                        jSpan = iSpan;
                       }
                     }
                   }
                   break;
 
                 case AXIAL_CENTRIFUGAL:
-                  if (marker_flag == INFLOW){
-                    radius = sqrt(coord[0]*coord[0]+coord[1]*coord[1]);
-                    for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-                      if (dist > (abs(radius - SpanWiseValue[marker_flag-1][iSpan]))){
-                        dist= abs(radius-SpanWiseValue[marker_flag-1][iSpan]);
-                        jSpan=iSpan;
+                  if (marker_flag == INFLOW) {
+                    radius = sqrt(coord[0] * coord[0] + coord[1] * coord[1]);
+                    for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+                      if (dist > (abs(radius - SpanWiseValue[marker_flag - 1][iSpan]))) {
+                        dist = abs(radius - SpanWiseValue[marker_flag - 1][iSpan]);
+                        jSpan = iSpan;
                       }
                     }
-                  }
-                  else{
-                    for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-                      if (dist > (abs(coord[2]-SpanWiseValue[marker_flag-1][iSpan]))){
-                        dist= abs(coord[2]-SpanWiseValue[marker_flag-1][iSpan]);
-                        jSpan=iSpan;
+                  } else {
+                    for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+                      if (dist > (abs(coord[2] - SpanWiseValue[marker_flag - 1][iSpan]))) {
+                        dist = abs(coord[2] - SpanWiseValue[marker_flag - 1][iSpan]);
+                        jSpan = iSpan;
                       }
                     }
                   }
                   break;
-                }
               }
+            }
 
-              /*--- 2D problem do not need span-wise separation---*/
-              else{
-                jSpan = 0;
-              }
+            /*--- 2D problem do not need span-wise separation---*/
+            else {
+              jSpan = 0;
+            }
 
-              if(nodes->GetDomain(iPoint)){
-                nVertexSpan[iMarker][jSpan]++;
-              }
-              nVertexSpanHalo[jSpan]++;
+            if (nodes->GetDomain(iPoint)) {
+              nVertexSpan[iMarker][jSpan]++;
             }
+            nVertexSpanHalo[jSpan]++;
+          }
 
-            /*--- initialize the CTurboVertex pointers and auxiliary pointers  ---*/
-            for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-              if (allocate){
-                turbovertex[iMarker][iSpan] = new CTurboVertex* [nVertexSpan[iMarker][iSpan]];
-                for (iVertex = 0; iVertex < nVertexSpan[iMarker][iSpan]; iVertex++){
-                  turbovertex[iMarker][iSpan][iVertex] = nullptr;
-                }
-              }
-              ordered[iSpan]                           = new unsigned long [nVertexSpanHalo[iSpan]];
-              disordered[iSpan]                        = new unsigned long [nVertexSpanHalo[iSpan]];
-              oldVertex3D[iSpan]                       = new unsigned long [nVertexSpanHalo[iSpan]];
-              checkAssign[iSpan]                       = new bool [nVertexSpanHalo[iSpan]];
-              area[iSpan]                              = new su2double [nVertexSpanHalo[iSpan]];
-              unitnormal[iSpan]                        = new su2double* [nVertexSpanHalo[iSpan]];
-              for (iVertex = 0; iVertex < nVertexSpanHalo[iSpan]; iVertex++){
-                unitnormal[iSpan][iVertex]             = new su2double [nDim];
+          /*--- initialize the CTurboVertex pointers and auxiliary pointers  ---*/
+          for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+            if (allocate) {
+              turbovertex[iMarker][iSpan] = new CTurboVertex*[nVertexSpan[iMarker][iSpan]];
+              for (iVertex = 0; iVertex < nVertexSpan[iMarker][iSpan]; iVertex++) {
+                turbovertex[iMarker][iSpan][iVertex] = nullptr;
               }
-              angPitch[iSpan]                          = new su2double [nVertexSpanHalo[iSpan]];
-              deltaAngPitch[iSpan]                     = new su2double [nVertexSpanHalo[iSpan]];
-              nVertexSpanHalo[iSpan]                   = 0;
             }
+            ordered[iSpan] = new unsigned long[nVertexSpanHalo[iSpan]];
+            disordered[iSpan] = new unsigned long[nVertexSpanHalo[iSpan]];
+            oldVertex3D[iSpan] = new unsigned long[nVertexSpanHalo[iSpan]];
+            checkAssign[iSpan] = new bool[nVertexSpanHalo[iSpan]];
+            area[iSpan] = new su2double[nVertexSpanHalo[iSpan]];
+            unitnormal[iSpan] = new su2double*[nVertexSpanHalo[iSpan]];
+            for (iVertex = 0; iVertex < nVertexSpanHalo[iSpan]; iVertex++) {
+              unitnormal[iSpan][iVertex] = new su2double[nDim];
+            }
+            angPitch[iSpan] = new su2double[nVertexSpanHalo[iSpan]];
+            deltaAngPitch[iSpan] = new su2double[nVertexSpanHalo[iSpan]];
+            nVertexSpanHalo[iSpan] = 0;
+          }
 
-            /*--- store the vertexes in a ordered manner in span-wise directions but not yet ordered pitch-wise ---*/
-            for (iVertex = 0; (unsigned long)iVertex < nVertex[iMarker]; iVertex++) {
-              iPoint = vertex[iMarker][iVertex]->GetNode();
-              if(nDim == 3){
-                dist  = 10E+06;
-                jSpan = std::numeric_limits<unsigned short>::max();
+          /*--- store the vertexes in a ordered manner in span-wise directions but not yet ordered pitch-wise ---*/
+          for (iVertex = 0; (unsigned long)iVertex < nVertex[iMarker]; iVertex++) {
+            iPoint = vertex[iMarker][iVertex]->GetNode();
+            if (nDim == 3) {
+              dist = 10E+06;
+              jSpan = std::numeric_limits<unsigned short>::max();
 
-                coord = nodes->GetCoord(iPoint);
-                switch (config->GetKind_TurboMachinery(val_iZone)){
-                case CENTRIFUGAL: case CENTRIPETAL:
-                  for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-                    if (dist > (abs(coord[2]-SpanWiseValue[marker_flag-1][iSpan]))){
-                      dist= abs(coord[2]-SpanWiseValue[marker_flag-1][iSpan]);
-                      jSpan=iSpan;
+              coord = nodes->GetCoord(iPoint);
+              switch (config->GetKind_TurboMachinery(val_iZone)) {
+                case CENTRIFUGAL:
+                case CENTRIPETAL:
+                  for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+                    if (dist > (abs(coord[2] - SpanWiseValue[marker_flag - 1][iSpan]))) {
+                      dist = abs(coord[2] - SpanWiseValue[marker_flag - 1][iSpan]);
+                      jSpan = iSpan;
                     }
                   }
                   break;
                 case AXIAL:
-                  radius = sqrt(coord[0]*coord[0]+coord[1]*coord[1]);
-                  for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-                    if (dist > (abs(radius - SpanWiseValue[marker_flag-1][iSpan]))){
-                      dist= abs(radius-SpanWiseValue[marker_flag-1][iSpan]);
-                      jSpan=iSpan;
+                  radius = sqrt(coord[0] * coord[0] + coord[1] * coord[1]);
+                  for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+                    if (dist > (abs(radius - SpanWiseValue[marker_flag - 1][iSpan]))) {
+                      dist = abs(radius - SpanWiseValue[marker_flag - 1][iSpan]);
+                      jSpan = iSpan;
                     }
                   }
                   break;
                 case CENTRIPETAL_AXIAL:
-                  if(marker_flag == OUTFLOW){
-                    radius = sqrt(coord[0]*coord[0]+coord[1]*coord[1]);
-                    for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-                      if (dist > (abs(radius - SpanWiseValue[marker_flag-1][iSpan]))){
-                        dist= abs(radius-SpanWiseValue[marker_flag-1][iSpan]);
-                        jSpan=iSpan;
+                  if (marker_flag == OUTFLOW) {
+                    radius = sqrt(coord[0] * coord[0] + coord[1] * coord[1]);
+                    for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+                      if (dist > (abs(radius - SpanWiseValue[marker_flag - 1][iSpan]))) {
+                        dist = abs(radius - SpanWiseValue[marker_flag - 1][iSpan]);
+                        jSpan = iSpan;
                       }
                     }
-                  }else{
-                    for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-                      if (dist > (abs(coord[2]-SpanWiseValue[marker_flag-1][iSpan]))){
-                        dist= abs(coord[2]-SpanWiseValue[marker_flag-1][iSpan]);
-                        jSpan=iSpan;
+                  } else {
+                    for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+                      if (dist > (abs(coord[2] - SpanWiseValue[marker_flag - 1][iSpan]))) {
+                        dist = abs(coord[2] - SpanWiseValue[marker_flag - 1][iSpan]);
+                        jSpan = iSpan;
                       }
                     }
                   }
                   break;
 
                 case AXIAL_CENTRIFUGAL:
-                  if(marker_flag == INFLOW){
-                    radius = sqrt(coord[0]*coord[0]+coord[1]*coord[1]);
-                    for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-                      if (dist > (abs(radius - SpanWiseValue[marker_flag-1][iSpan]))){
-                        dist= abs(radius-SpanWiseValue[marker_flag-1][iSpan]);
-                        jSpan=iSpan;
+                  if (marker_flag == INFLOW) {
+                    radius = sqrt(coord[0] * coord[0] + coord[1] * coord[1]);
+                    for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+                      if (dist > (abs(radius - SpanWiseValue[marker_flag - 1][iSpan]))) {
+                        dist = abs(radius - SpanWiseValue[marker_flag - 1][iSpan]);
+                        jSpan = iSpan;
                       }
                     }
-                  }else{
-                    for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-                      if (dist > (abs(coord[2]-SpanWiseValue[marker_flag-1][iSpan]))){
-                        dist= abs(coord[2]-SpanWiseValue[marker_flag-1][iSpan]);
-                        jSpan=iSpan;
+                  } else {
+                    for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+                      if (dist > (abs(coord[2] - SpanWiseValue[marker_flag - 1][iSpan]))) {
+                        dist = abs(coord[2] - SpanWiseValue[marker_flag - 1][iSpan]);
+                        jSpan = iSpan;
                       }
                     }
                   }
                   break;
-                }
-              }
-              /*--- 2D problem do not need span-wise separation---*/
-              else{
-                jSpan = 0;
               }
-              /*--- compute the face area associated with the vertex ---*/
-              vertex[iMarker][iVertex]->GetNormal(NormalArea);
-              for (iDim = 0; iDim < nDim; iDim++) NormalArea[iDim] = -NormalArea[iDim];
-              Area = GeometryToolbox::Norm(nDim, NormalArea);
-
-              for (iDim = 0; iDim < nDim; iDim++) NormalArea[iDim] /= Area;
-              /*--- store all the all the info into the auxiliary containers ---*/
-              disordered[jSpan][nVertexSpanHalo[jSpan]]  = iPoint;
-              oldVertex3D[jSpan][nVertexSpanHalo[jSpan]] = iVertex;
-              area[jSpan][nVertexSpanHalo[jSpan]]        = Area;
-              for (iDim = 0; iDim < nDim; iDim++){
-                unitnormal[jSpan][nVertexSpanHalo[jSpan]][iDim] = NormalArea[iDim];
-              }
-              checkAssign[jSpan][nVertexSpanHalo[jSpan]] = false;
-              nVertexSpanHalo[jSpan]++;
             }
+            /*--- 2D problem do not need span-wise separation---*/
+            else {
+              jSpan = 0;
+            }
+            /*--- compute the face area associated with the vertex ---*/
+            vertex[iMarker][iVertex]->GetNormal(NormalArea);
+            for (iDim = 0; iDim < nDim; iDim++) NormalArea[iDim] = -NormalArea[iDim];
+            Area = GeometryToolbox::Norm(nDim, NormalArea);
+
+            for (iDim = 0; iDim < nDim; iDim++) NormalArea[iDim] /= Area;
+            /*--- store all the all the info into the auxiliary containers ---*/
+            disordered[jSpan][nVertexSpanHalo[jSpan]] = iPoint;
+            oldVertex3D[jSpan][nVertexSpanHalo[jSpan]] = iVertex;
+            area[jSpan][nVertexSpanHalo[jSpan]] = Area;
+            for (iDim = 0; iDim < nDim; iDim++) {
+              unitnormal[jSpan][nVertexSpanHalo[jSpan]][iDim] = NormalArea[iDim];
+            }
+            checkAssign[jSpan][nVertexSpanHalo[jSpan]] = false;
+            nVertexSpanHalo[jSpan]++;
+          }
 
-            /*--- using the auxiliary container reordered the vertexes pitch-wise direction at each span ---*/
-            // the reordering algorithm can be based on the Y-coordinate.
-            for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-
-              /*--- find the local minimum and maximum pitch-wise for each processor---*/
-              min    = 10E+06;
-              minInt = 10E+06;
-              max    = -10E+06;
-              for(iSpanVertex = 0; iSpanVertex < nVertexSpanHalo[iSpan]; iSpanVertex++){
-                iPoint = disordered[iSpan][iSpanVertex];
-                coord = nodes->GetCoord(iPoint);
-                /*--- find nodes at minimum pitch among all nodes---*/
-                if (coord[1]<min){
-                  min = coord[1];
-                  if (nDim == 2 && config->GetKind_TurboMachinery(val_iZone) == AXIAL){
-                    MinAngularCoord[iMarker][iSpan] = coord[1];
-                  }
-                  else{
-                  MinAngularCoord[iMarker][iSpan] = atan(coord[1]/coord[0]);
-                  }
-                  minAngPitch[iSpan]= MinAngularCoord[iMarker][iSpan];
-                  kSpanVertex =iSpanVertex;
+          /*--- using the auxiliary container reordered the vertexes pitch-wise direction at each span ---*/
+          // the reordering algorithm can be based on the Y-coordinate.
+          for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+            /*--- find the local minimum and maximum pitch-wise for each processor---*/
+            min = 10E+06;
+            minInt = 10E+06;
+            max = -10E+06;
+            for (iSpanVertex = 0; iSpanVertex < nVertexSpanHalo[iSpan]; iSpanVertex++) {
+              iPoint = disordered[iSpan][iSpanVertex];
+              coord = nodes->GetCoord(iPoint);
+              /*--- find nodes at minimum pitch among all nodes---*/
+              if (coord[1] < min) {
+                min = coord[1];
+                if (nDim == 2 && config->GetKind_TurboMachinery(val_iZone) == AXIAL) {
+                  MinAngularCoord[iMarker][iSpan] = coord[1];
+                } else {
+                  MinAngularCoord[iMarker][iSpan] = atan(coord[1] / coord[0]);
                 }
+                minAngPitch[iSpan] = MinAngularCoord[iMarker][iSpan];
+                kSpanVertex = iSpanVertex;
+              }
 
-                /*--- find nodes at minimum pitch among the internal nodes---*/
-                if (coord[1]<minInt){
-                  if(nodes->GetDomain(iPoint)){
-                    minInt = coord[1];
-                    if (nDim == 2 && config->GetKind_TurboMachinery(val_iZone) == AXIAL){
-                      minIntAngPitch[iSpan] = coord[1];
-                    }
-                    else{
-                      minIntAngPitch[iSpan] = atan(coord[1]/coord[0]);
-                    }
+              /*--- find nodes at minimum pitch among the internal nodes---*/
+              if (coord[1] < minInt) {
+                if (nodes->GetDomain(iPoint)) {
+                  minInt = coord[1];
+                  if (nDim == 2 && config->GetKind_TurboMachinery(val_iZone) == AXIAL) {
+                    minIntAngPitch[iSpan] = coord[1];
+                  } else {
+                    minIntAngPitch[iSpan] = atan(coord[1] / coord[0]);
                   }
                 }
+              }
 
-                /*--- find nodes at maximum pitch among the internal nodes---*/
-                if (coord[1]>max){
-                  if(nodes->GetDomain(iPoint)){
-                    max =coord[1];
-                    if (nDim == 2 && config->GetKind_TurboMachinery(val_iZone) == AXIAL){
-                      MaxAngularCoord[iMarker][iSpan] = coord[1];
-                    }
-                    else{
-                      MaxAngularCoord[iMarker][iSpan] = atan(coord[1]/coord[0]);
-                    }
-                    maxAngPitch[iSpan]= MaxAngularCoord[iMarker][iSpan];
+              /*--- find nodes at maximum pitch among the internal nodes---*/
+              if (coord[1] > max) {
+                if (nodes->GetDomain(iPoint)) {
+                  max = coord[1];
+                  if (nDim == 2 && config->GetKind_TurboMachinery(val_iZone) == AXIAL) {
+                    MaxAngularCoord[iMarker][iSpan] = coord[1];
+                  } else {
+                    MaxAngularCoord[iMarker][iSpan] = atan(coord[1] / coord[0]);
                   }
+                  maxAngPitch[iSpan] = MaxAngularCoord[iMarker][iSpan];
                 }
               }
+            }
 
-              iInternalVertex = 0;
-
-              /*--- reordering the vertex pitch-wise, store the ordered vertexes span-wise and pitch-wise---*/
-              for(iSpanVertex = 0; iSpanVertex<nVertexSpanHalo[iSpan]; iSpanVertex++){
-                dist = 10E+06;
-                ordered[iSpan][iSpanVertex] = disordered[iSpan][kSpanVertex];
-                checkAssign[iSpan][kSpanVertex] = true;
-                coord = nodes->GetCoord(ordered[iSpan][iSpanVertex]);
-                target = coord[1];
-                if (nDim == 2 && config->GetKind_TurboMachinery(val_iZone) == AXIAL){
-                   angPitch[iSpan][iSpanVertex]=coord[1];
-                }
-                else{
-                  angPitch[iSpan][iSpanVertex]=atan(coord[1]/coord[0]);
-                }
-                if(iSpanVertex == 0){
-                  deltaAngPitch[iSpan][iSpanVertex]=0.0;
-                }
-                else{
-                  deltaAngPitch[iSpan][iSpanVertex]= angPitch[iSpan][iSpanVertex] - angPitch[iSpan][iSpanVertex - 1];
+            iInternalVertex = 0;
+
+            /*--- reordering the vertex pitch-wise, store the ordered vertexes span-wise and pitch-wise---*/
+            for (iSpanVertex = 0; iSpanVertex < nVertexSpanHalo[iSpan]; iSpanVertex++) {
+              dist = 10E+06;
+              ordered[iSpan][iSpanVertex] = disordered[iSpan][kSpanVertex];
+              checkAssign[iSpan][kSpanVertex] = true;
+              coord = nodes->GetCoord(ordered[iSpan][iSpanVertex]);
+              target = coord[1];
+              if (nDim == 2 && config->GetKind_TurboMachinery(val_iZone) == AXIAL) {
+                angPitch[iSpan][iSpanVertex] = coord[1];
+              } else {
+                angPitch[iSpan][iSpanVertex] = atan(coord[1] / coord[0]);
+              }
+              if (iSpanVertex == 0) {
+                deltaAngPitch[iSpan][iSpanVertex] = 0.0;
+              } else {
+                deltaAngPitch[iSpan][iSpanVertex] = angPitch[iSpan][iSpanVertex] - angPitch[iSpan][iSpanVertex - 1];
+              }
+              /*---create turbovertex structure only for the internal nodes---*/
+              if (nodes->GetDomain(ordered[iSpan][iSpanVertex])) {
+                if (allocate) {
+                  turbovertex[iMarker][iSpan][iInternalVertex] = new CTurboVertex(ordered[iSpan][iSpanVertex], nDim);
                 }
-                /*---create turbovertex structure only for the internal nodes---*/
-                if(nodes->GetDomain(ordered[iSpan][iSpanVertex])){
-                  if (allocate){
-                    turbovertex[iMarker][iSpan][iInternalVertex] = new CTurboVertex(ordered[iSpan][iSpanVertex], nDim);
-                  }
-                  turbovertex[iMarker][iSpan][iInternalVertex]->SetArea(area[iSpan][kSpanVertex]);
-                  turbovertex[iMarker][iSpan][iInternalVertex]->SetNormal(unitnormal[iSpan][kSpanVertex]);
-                  turbovertex[iMarker][iSpan][iInternalVertex]->SetOldVertex(oldVertex3D[iSpan][kSpanVertex]);
-                  turbovertex[iMarker][iSpan][iInternalVertex]->SetAngularCoord(angPitch[iSpan][iSpanVertex]);
-                  turbovertex[iMarker][iSpan][iInternalVertex]->SetDeltaAngularCoord(deltaAngPitch[iSpan][iSpanVertex]);
-                  switch (config->GetKind_TurboMachinery(val_iZone)){
+                turbovertex[iMarker][iSpan][iInternalVertex]->SetArea(area[iSpan][kSpanVertex]);
+                turbovertex[iMarker][iSpan][iInternalVertex]->SetNormal(unitnormal[iSpan][kSpanVertex]);
+                turbovertex[iMarker][iSpan][iInternalVertex]->SetOldVertex(oldVertex3D[iSpan][kSpanVertex]);
+                turbovertex[iMarker][iSpan][iInternalVertex]->SetAngularCoord(angPitch[iSpan][iSpanVertex]);
+                turbovertex[iMarker][iSpan][iInternalVertex]->SetDeltaAngularCoord(deltaAngPitch[iSpan][iSpanVertex]);
+                switch (config->GetKind_TurboMachinery(val_iZone)) {
                   case CENTRIFUGAL:
                     Normal2 = 0.0;
-                    for(iDim = 0; iDim < 2; iDim++) Normal2 +=coord[iDim]*coord[iDim];
-                    if (marker_flag == INFLOW){
-                      TurboNormal[0] = -coord[0]/sqrt(Normal2);
-                      TurboNormal[1] = -coord[1]/sqrt(Normal2);
+                    for (iDim = 0; iDim < 2; iDim++) Normal2 += coord[iDim] * coord[iDim];
+                    if (marker_flag == INFLOW) {
+                      TurboNormal[0] = -coord[0] / sqrt(Normal2);
+                      TurboNormal[1] = -coord[1] / sqrt(Normal2);
                       TurboNormal[2] = 0.0;
-                    }else{
-                      TurboNormal[0] = coord[0]/sqrt(Normal2);
-                      TurboNormal[1] = coord[1]/sqrt(Normal2);
+                    } else {
+                      TurboNormal[0] = coord[0] / sqrt(Normal2);
+                      TurboNormal[1] = coord[1] / sqrt(Normal2);
                       TurboNormal[2] = 0.0;
                     }
                     break;
                   case CENTRIPETAL:
                     Normal2 = 0.0;
-                    for(iDim = 0; iDim < 2; iDim++) Normal2 +=coord[iDim]*coord[iDim];
-                    if (marker_flag == OUTFLOW){
-                      TurboNormal[0] = -coord[0]/sqrt(Normal2);
-                      TurboNormal[1] = -coord[1]/sqrt(Normal2);
+                    for (iDim = 0; iDim < 2; iDim++) Normal2 += coord[iDim] * coord[iDim];
+                    if (marker_flag == OUTFLOW) {
+                      TurboNormal[0] = -coord[0] / sqrt(Normal2);
+                      TurboNormal[1] = -coord[1] / sqrt(Normal2);
                       TurboNormal[2] = 0.0;
-                    }else{
-                      TurboNormal[0] = coord[0]/sqrt(Normal2);
-                      TurboNormal[1] = coord[1]/sqrt(Normal2);
+                    } else {
+                      TurboNormal[0] = coord[0] / sqrt(Normal2);
+                      TurboNormal[1] = coord[1] / sqrt(Normal2);
                       TurboNormal[2] = 0.0;
                     }
                     break;
                   case AXIAL:
                     Normal2 = 0.0;
-                    for(iDim = 0; iDim < 2; iDim++) Normal2 +=coord[iDim]*coord[iDim];
-                    if(nDim == 3){
-                      if (marker_flag == INFLOW){
-                        TurboNormal[0] = coord[0]/sqrt(Normal2);
-                        TurboNormal[1] = coord[1]/sqrt(Normal2);
+                    for (iDim = 0; iDim < 2; iDim++) Normal2 += coord[iDim] * coord[iDim];
+                    if (nDim == 3) {
+                      if (marker_flag == INFLOW) {
+                        TurboNormal[0] = coord[0] / sqrt(Normal2);
+                        TurboNormal[1] = coord[1] / sqrt(Normal2);
                         TurboNormal[2] = 0.0;
-                      }else{
-                        TurboNormal[0] = coord[0]/sqrt(Normal2);
-                        TurboNormal[1] = coord[1]/sqrt(Normal2);
+                      } else {
+                        TurboNormal[0] = coord[0] / sqrt(Normal2);
+                        TurboNormal[1] = coord[1] / sqrt(Normal2);
                         TurboNormal[2] = 0.0;
                       }
-                    }
-                    else{
-                      if (marker_flag == INFLOW){
+                    } else {
+                      if (marker_flag == INFLOW) {
                         TurboNormal[0] = -1.0;
                         TurboNormal[1] = 0.0;
                         TurboNormal[2] = 0.0;
-                      }else{
+                      } else {
                         TurboNormal[0] = 1.0;
                         TurboNormal[1] = 0.0;
                         TurboNormal[2] = 0.0;
@@ -5736,167 +5404,164 @@ void CPhysicalGeometry::SetTurboVertex(CConfig *config, unsigned short val_iZone
                     break;
                   case CENTRIPETAL_AXIAL:
                     Normal2 = 0.0;
-                    for(iDim = 0; iDim < 2; iDim++) Normal2 +=coord[iDim]*coord[iDim];
-                    if (marker_flag == INFLOW){
-                      TurboNormal[0] = coord[0]/sqrt(Normal2);
-                      TurboNormal[1] = coord[1]/sqrt(Normal2);
+                    for (iDim = 0; iDim < 2; iDim++) Normal2 += coord[iDim] * coord[iDim];
+                    if (marker_flag == INFLOW) {
+                      TurboNormal[0] = coord[0] / sqrt(Normal2);
+                      TurboNormal[1] = coord[1] / sqrt(Normal2);
                       TurboNormal[2] = 0.0;
-                    }else{
-                      TurboNormal[0] = coord[0]/sqrt(Normal2);
-                      TurboNormal[1] = coord[1]/sqrt(Normal2);
+                    } else {
+                      TurboNormal[0] = coord[0] / sqrt(Normal2);
+                      TurboNormal[1] = coord[1] / sqrt(Normal2);
                       TurboNormal[2] = 0.0;
                     }
                     break;
 
                   case AXIAL_CENTRIFUGAL:
                     Normal2 = 0.0;
-                    for(iDim = 0; iDim < 2; iDim++) Normal2 +=coord[iDim]*coord[iDim];
-                    if (marker_flag == INFLOW){
-                      TurboNormal[0] = coord[0]/sqrt(Normal2);
-                      TurboNormal[1] = coord[1]/sqrt(Normal2);
+                    for (iDim = 0; iDim < 2; iDim++) Normal2 += coord[iDim] * coord[iDim];
+                    if (marker_flag == INFLOW) {
+                      TurboNormal[0] = coord[0] / sqrt(Normal2);
+                      TurboNormal[1] = coord[1] / sqrt(Normal2);
                       TurboNormal[2] = 0.0;
-                    }else{
-                      TurboNormal[0] = coord[0]/sqrt(Normal2);
-                      TurboNormal[1] = coord[1]/sqrt(Normal2);
+                    } else {
+                      TurboNormal[0] = coord[0] / sqrt(Normal2);
+                      TurboNormal[1] = coord[1] / sqrt(Normal2);
                       TurboNormal[2] = 0.0;
                     }
                     break;
-
-                  }
-                  turbovertex[iMarker][iSpan][iInternalVertex]->SetTurboNormal(TurboNormal);
-                  iInternalVertex++;
                 }
+                turbovertex[iMarker][iSpan][iInternalVertex]->SetTurboNormal(TurboNormal);
+                iInternalVertex++;
+              }
 
-
-                for(jSpanVertex = 0; jSpanVertex<nVertexSpanHalo[iSpan]; jSpanVertex++){
-                  coord = nodes->GetCoord(disordered[iSpan][jSpanVertex]);
-                  if(dist >= (coord[1] - target) && !checkAssign[iSpan][jSpanVertex] && (coord[1] - target) >= 0.0){
-                    dist= coord[1] - target;
-                    kSpanVertex =jSpanVertex;
-                  }
+              for (jSpanVertex = 0; jSpanVertex < nVertexSpanHalo[iSpan]; jSpanVertex++) {
+                coord = nodes->GetCoord(disordered[iSpan][jSpanVertex]);
+                if (dist >= (coord[1] - target) && !checkAssign[iSpan][jSpanVertex] && (coord[1] - target) >= 0.0) {
+                  dist = coord[1] - target;
+                  kSpanVertex = jSpanVertex;
                 }
               }
             }
+          }
 
-            for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-
-              delete [] ordered[iSpan];
-              delete [] disordered[iSpan];
-              delete [] oldVertex3D[iSpan];
-              delete [] checkAssign[iSpan];
-              delete [] area[iSpan];
-              delete [] angPitch[iSpan];
-              delete [] deltaAngPitch[iSpan];
-
-              for(iVertex=0; iVertex < nVertexSpanHalo[iSpan]; iVertex++){
-                delete [] unitnormal[iSpan][iVertex];
-              }
-              delete [] unitnormal[iSpan];
+          for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+            delete[] ordered[iSpan];
+            delete[] disordered[iSpan];
+            delete[] oldVertex3D[iSpan];
+            delete[] checkAssign[iSpan];
+            delete[] area[iSpan];
+            delete[] angPitch[iSpan];
+            delete[] deltaAngPitch[iSpan];
+
+            for (iVertex = 0; iVertex < nVertexSpanHalo[iSpan]; iVertex++) {
+              delete[] unitnormal[iSpan][iVertex];
             }
+            delete[] unitnormal[iSpan];
           }
         }
       }
     }
+  }
 
   /*--- to be set for all the processor to initialize an appropriate number of frequency for the NR BC ---*/
   nVertMax = 0;
 
   /*--- compute global max and min pitch per span ---*/
-  for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-    nVert    = 0;
+  for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+    nVert = 0;
 
 #ifdef HAVE_MPI
-    MyMin     = minAngPitch[iSpan];      minAngPitch[iSpan]    = 10.0E+6;
-    MyIntMin  = minIntAngPitch[iSpan];   minIntAngPitch[iSpan] = 10.0E+6;
-    MyMax     = maxAngPitch[iSpan];      maxAngPitch[iSpan]    = -10.0E+6;
+    MyMin = minAngPitch[iSpan];
+    minAngPitch[iSpan] = 10.0E+6;
+    MyIntMin = minIntAngPitch[iSpan];
+    minIntAngPitch[iSpan] = 10.0E+6;
+    MyMax = maxAngPitch[iSpan];
+    maxAngPitch[iSpan] = -10.0E+6;
 
     SU2_MPI::Allreduce(&MyMin, &minAngPitch[iSpan], 1, MPI_DOUBLE, MPI_MIN, SU2_MPI::GetComm());
     SU2_MPI::Allreduce(&MyIntMin, &minIntAngPitch[iSpan], 1, MPI_DOUBLE, MPI_MIN, SU2_MPI::GetComm());
     SU2_MPI::Allreduce(&MyMax, &maxAngPitch[iSpan], 1, MPI_DOUBLE, MPI_MAX, SU2_MPI::GetComm());
 #endif
 
-
     /*--- compute the relative angular pitch with respect to the minimum value ---*/
 
-    for (iMarker = 0; iMarker < nMarker; iMarker++){
-      for (iMarkerTP=1; iMarkerTP < config->GetnMarker_Turbomachinery()+1; iMarkerTP++){
-        if (config->GetMarker_All_Turbomachinery(iMarker) == iMarkerTP){
-          if (config->GetMarker_All_TurbomachineryFlag(iMarker) == marker_flag){
+    for (iMarker = 0; iMarker < nMarker; iMarker++) {
+      for (iMarkerTP = 1; iMarkerTP < config->GetnMarker_Turbomachinery() + 1; iMarkerTP++) {
+        if (config->GetMarker_All_Turbomachinery(iMarker) == iMarkerTP) {
+          if (config->GetMarker_All_TurbomachineryFlag(iMarker) == marker_flag) {
             nVert = nVertexSpan[iMarker][iSpan];
-            MinAngularCoord[iMarker][iSpan]    = minAngPitch[iSpan];
-            MaxAngularCoord[iMarker][iSpan]    = maxAngPitch[iSpan];
+            MinAngularCoord[iMarker][iSpan] = minAngPitch[iSpan];
+            MaxAngularCoord[iMarker][iSpan] = maxAngPitch[iSpan];
             MinRelAngularCoord[iMarker][iSpan] = minIntAngPitch[iSpan] - minAngPitch[iSpan];
-            for(iSpanVertex = 0; iSpanVertex< nVertexSpan[iMarker][iSpan]; iSpanVertex++){
-             turbovertex[iMarker][iSpan][iSpanVertex]->SetRelAngularCoord(MinAngularCoord[iMarker][iSpan]);
+            for (iSpanVertex = 0; iSpanVertex < nVertexSpan[iMarker][iSpan]; iSpanVertex++) {
+              turbovertex[iMarker][iSpan][iSpanVertex]->SetRelAngularCoord(MinAngularCoord[iMarker][iSpan]);
             }
           }
         }
       }
     }
 
-
 #ifdef HAVE_MPI
-    My_nVert = nVert;nVert = 0;
+    My_nVert = nVert;
+    nVert = 0;
     SU2_MPI::Allreduce(&My_nVert, &nVert, 1, MPI_INT, MPI_SUM, SU2_MPI::GetComm());
 #endif
 
     /*--- to be set for all the processor to initialize an appropriate number of frequency for the NR BC ---*/
-    if(nVert > nVertMax){
-      SetnVertexSpanMax(marker_flag,nVert);
+    if (nVert > nVertMax) {
+      SetnVertexSpanMax(marker_flag, nVert);
     }
     /*--- for all the processor should be known the amount of total turbovertex per span  ---*/
-    nTotVertex_gb[iSpan]= (int)nVert;
-
-    for (iMarker = 0; iMarker < nMarker; iMarker++){
-      for (iMarkerTP=1; iMarkerTP < config->GetnMarker_Turbomachinery()+1; iMarkerTP++){
-        if (config->GetMarker_All_Turbomachinery(iMarker) == iMarkerTP){
-          if (config->GetMarker_All_TurbomachineryFlag(iMarker) == marker_flag){
-            nTotVertexSpan[iMarker][iSpan]= nVert;
-            nTotVertexSpan[iMarker][nSpanWiseSections[marker_flag-1]]+= nVert;
+    nTotVertex_gb[iSpan] = (int)nVert;
+
+    for (iMarker = 0; iMarker < nMarker; iMarker++) {
+      for (iMarkerTP = 1; iMarkerTP < config->GetnMarker_Turbomachinery() + 1; iMarkerTP++) {
+        if (config->GetMarker_All_Turbomachinery(iMarker) == iMarkerTP) {
+          if (config->GetMarker_All_TurbomachineryFlag(iMarker) == marker_flag) {
+            nTotVertexSpan[iMarker][iSpan] = nVert;
+            nTotVertexSpan[iMarker][nSpanWiseSections[marker_flag - 1]] += nVert;
           }
         }
       }
     }
   }
 
-
   /*--- Printing Tec file to check the global ordering of the turbovertex pitch-wise ---*/
   /*--- Send all the info to the MASTERNODE ---*/
 
-  for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-    x_loc[iSpan]             = new su2double[nTotVertex_gb[iSpan]];
-    y_loc[iSpan]             = new su2double[nTotVertex_gb[iSpan]];
-    z_loc[iSpan]             = new su2double[nTotVertex_gb[iSpan]];
-    angCoord_loc[iSpan]      = new su2double[nTotVertex_gb[iSpan]];
+  for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+    x_loc[iSpan] = new su2double[nTotVertex_gb[iSpan]];
+    y_loc[iSpan] = new su2double[nTotVertex_gb[iSpan]];
+    z_loc[iSpan] = new su2double[nTotVertex_gb[iSpan]];
+    angCoord_loc[iSpan] = new su2double[nTotVertex_gb[iSpan]];
     deltaAngCoord_loc[iSpan] = new su2double[nTotVertex_gb[iSpan]];
-    rank_loc[iSpan]          = new int[nTotVertex_gb[iSpan]];
-    for(iSpanVertex = 0; iSpanVertex<nTotVertex_gb[iSpan]; iSpanVertex++){
-      x_loc[iSpan][iSpanVertex]             = -1.0;
-      y_loc[iSpan][iSpanVertex]             = -1.0;
-      z_loc[iSpan][iSpanVertex]             = -1.0;
-      angCoord_loc[iSpan][iSpanVertex]      = -1.0;
+    rank_loc[iSpan] = new int[nTotVertex_gb[iSpan]];
+    for (iSpanVertex = 0; iSpanVertex < nTotVertex_gb[iSpan]; iSpanVertex++) {
+      x_loc[iSpan][iSpanVertex] = -1.0;
+      y_loc[iSpan][iSpanVertex] = -1.0;
+      z_loc[iSpan][iSpanVertex] = -1.0;
+      angCoord_loc[iSpan][iSpanVertex] = -1.0;
       deltaAngCoord_loc[iSpan][iSpanVertex] = -1.0;
-      rank_loc[iSpan][iSpanVertex]          = -1;
+      rank_loc[iSpan][iSpanVertex] = -1;
     }
   }
 
-  for (iMarker = 0; iMarker < nMarker; iMarker++){
-    for (iMarkerTP=1; iMarkerTP < config->GetnMarker_Turbomachinery()+1; iMarkerTP++){
-      if (config->GetMarker_All_Turbomachinery(iMarker) == iMarkerTP){
-        if (config->GetMarker_All_TurbomachineryFlag(iMarker) == marker_flag){
-          for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-            for(iSpanVertex = 0; iSpanVertex<nVertexSpan[iMarker][iSpan]; iSpanVertex++){
+  for (iMarker = 0; iMarker < nMarker; iMarker++) {
+    for (iMarkerTP = 1; iMarkerTP < config->GetnMarker_Turbomachinery() + 1; iMarkerTP++) {
+      if (config->GetMarker_All_Turbomachinery(iMarker) == iMarkerTP) {
+        if (config->GetMarker_All_TurbomachineryFlag(iMarker) == marker_flag) {
+          for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+            for (iSpanVertex = 0; iSpanVertex < nVertexSpan[iMarker][iSpan]; iSpanVertex++) {
               iPoint = turbovertex[iMarker][iSpan][iSpanVertex]->GetNode();
-              coord  = nodes->GetCoord(iPoint);
-              x_loc[iSpan][iSpanVertex]   = coord[0];
-              y_loc[iSpan][iSpanVertex]   = coord[1];
-              if (nDim == 3){
+              coord = nodes->GetCoord(iPoint);
+              x_loc[iSpan][iSpanVertex] = coord[0];
+              y_loc[iSpan][iSpanVertex] = coord[1];
+              if (nDim == 3) {
                 z_loc[iSpan][iSpanVertex] = coord[2];
-              }
-              else{
+              } else {
                 z_loc[iSpan][iSpanVertex] = 0.0;
               }
-              angCoord_loc[iSpan][iSpanVertex]      = turbovertex[iMarker][iSpan][iSpanVertex]->GetRelAngularCoord();
+              angCoord_loc[iSpan][iSpanVertex] = turbovertex[iMarker][iSpan][iSpanVertex]->GetRelAngularCoord();
               deltaAngCoord_loc[iSpan][iSpanVertex] = turbovertex[iMarker][iSpan][iSpanVertex]->GetDeltaAngularCoord();
             }
           }
@@ -5907,283 +5572,301 @@ void CPhysicalGeometry::SetTurboVertex(CConfig *config, unsigned short val_iZone
 
 #ifdef HAVE_MPI
 
-  for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-    if (rank == MASTER_NODE){
-      x_gb                = new su2double[nTotVertex_gb[iSpan]*size];
-      y_gb                = new su2double[nTotVertex_gb[iSpan]*size];
-      z_gb                = new su2double[nTotVertex_gb[iSpan]*size];
-      angCoord_gb         = new su2double[nTotVertex_gb[iSpan]*size];
-      deltaAngCoord_gb    = new su2double[nTotVertex_gb[iSpan]*size];
-      checkAssign_gb      = new bool[nTotVertex_gb[iSpan]*size];
-
-     for(iSize= 0; iSize < size; iSize++){
-       for(iSpanVertex = 0; iSpanVertex < nTotVertex_gb[iSpan]; iSpanVertex++){
-         checkAssign_gb[iSize*nTotVertex_gb[iSpan] + iSpanVertex] = false;
-       }
-     }
-    }
-    SU2_MPI::Gather(y_loc[iSpan], nTotVertex_gb[iSpan] , MPI_DOUBLE, y_gb, nTotVertex_gb[iSpan], MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Gather(x_loc[iSpan], nTotVertex_gb[iSpan] , MPI_DOUBLE, x_gb, nTotVertex_gb[iSpan], MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Gather(z_loc[iSpan], nTotVertex_gb[iSpan] , MPI_DOUBLE, z_gb, nTotVertex_gb[iSpan], MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Gather(angCoord_loc[iSpan], nTotVertex_gb[iSpan] , MPI_DOUBLE, angCoord_gb, nTotVertex_gb[iSpan], MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Gather(deltaAngCoord_loc[iSpan], nTotVertex_gb[iSpan] , MPI_DOUBLE, deltaAngCoord_gb, nTotVertex_gb[iSpan], MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-
-    if (rank == MASTER_NODE){
-      for(iSpanVertex = 0; iSpanVertex<nTotVertex_gb[iSpan]; iSpanVertex++){
-        x_loc[iSpan][iSpanVertex]             = -1.0;
-        y_loc[iSpan][iSpanVertex]             = -1.0;
-        z_loc[iSpan][iSpanVertex]             = -1.0;
-        angCoord_loc[iSpan][iSpanVertex]      = -1.0;
-        deltaAngCoord_loc[iSpan][iSpanVertex] = -1.0;
+  for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+    if (rank == MASTER_NODE) {
+      x_gb = new su2double[nTotVertex_gb[iSpan] * size];
+      y_gb = new su2double[nTotVertex_gb[iSpan] * size];
+      z_gb = new su2double[nTotVertex_gb[iSpan] * size];
+      angCoord_gb = new su2double[nTotVertex_gb[iSpan] * size];
+      deltaAngCoord_gb = new su2double[nTotVertex_gb[iSpan] * size];
+      checkAssign_gb = new bool[nTotVertex_gb[iSpan] * size];
+
+      for (iSize = 0; iSize < size; iSize++) {
+        for (iSpanVertex = 0; iSpanVertex < nTotVertex_gb[iSpan]; iSpanVertex++) {
+          checkAssign_gb[iSize * nTotVertex_gb[iSpan] + iSpanVertex] = false;
+        }
       }
+    }
+    SU2_MPI::Gather(y_loc[iSpan], nTotVertex_gb[iSpan], MPI_DOUBLE, y_gb, nTotVertex_gb[iSpan], MPI_DOUBLE, MASTER_NODE,
+                    SU2_MPI::GetComm());
+    SU2_MPI::Gather(x_loc[iSpan], nTotVertex_gb[iSpan], MPI_DOUBLE, x_gb, nTotVertex_gb[iSpan], MPI_DOUBLE, MASTER_NODE,
+                    SU2_MPI::GetComm());
+    SU2_MPI::Gather(z_loc[iSpan], nTotVertex_gb[iSpan], MPI_DOUBLE, z_gb, nTotVertex_gb[iSpan], MPI_DOUBLE, MASTER_NODE,
+                    SU2_MPI::GetComm());
+    SU2_MPI::Gather(angCoord_loc[iSpan], nTotVertex_gb[iSpan], MPI_DOUBLE, angCoord_gb, nTotVertex_gb[iSpan],
+                    MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
+    SU2_MPI::Gather(deltaAngCoord_loc[iSpan], nTotVertex_gb[iSpan], MPI_DOUBLE, deltaAngCoord_gb, nTotVertex_gb[iSpan],
+                    MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
 
-
+    if (rank == MASTER_NODE) {
+      for (iSpanVertex = 0; iSpanVertex < nTotVertex_gb[iSpan]; iSpanVertex++) {
+        x_loc[iSpan][iSpanVertex] = -1.0;
+        y_loc[iSpan][iSpanVertex] = -1.0;
+        z_loc[iSpan][iSpanVertex] = -1.0;
+        angCoord_loc[iSpan][iSpanVertex] = -1.0;
+        deltaAngCoord_loc[iSpan][iSpanVertex] = -1.0;
+      }
 
       min = 10.0E+06;
-      for(iSize= 0; iSize < size; iSize++){
-        if (angCoord_gb[iSize*nTotVertex_gb[iSpan]] < min && angCoord_gb[iSize*nTotVertex_gb[iSpan]] >= 0.0){
+      for (iSize = 0; iSize < size; iSize++) {
+        if (angCoord_gb[iSize * nTotVertex_gb[iSpan]] < min && angCoord_gb[iSize * nTotVertex_gb[iSpan]] >= 0.0) {
           kSize = iSize;
-          min = angCoord_gb[iSize*nTotVertex_gb[iSpan]];
+          min = angCoord_gb[iSize * nTotVertex_gb[iSpan]];
         }
       }
 
       kSpanVertex = 0;
-      for(iSpanVertex = 0; iSpanVertex < nTotVertex_gb[iSpan]; iSpanVertex++){
-        x_loc[iSpan][iSpanVertex]              = x_gb[kSize*nTotVertex_gb[iSpan] + kSpanVertex];
-        y_loc[iSpan][iSpanVertex]              = y_gb[kSize*nTotVertex_gb[iSpan] + kSpanVertex];
-        z_loc[iSpan][iSpanVertex]              = z_gb[kSize*nTotVertex_gb[iSpan] + kSpanVertex];
-        angCoord_loc[iSpan][iSpanVertex]       = angCoord_gb[kSize*nTotVertex_gb[iSpan] + kSpanVertex];
-        deltaAngCoord_loc[iSpan][iSpanVertex]  = deltaAngCoord_gb[kSize*nTotVertex_gb[iSpan] + kSpanVertex];
-        rank_loc[iSpan][iSpanVertex]           = kSize;
+      for (iSpanVertex = 0; iSpanVertex < nTotVertex_gb[iSpan]; iSpanVertex++) {
+        x_loc[iSpan][iSpanVertex] = x_gb[kSize * nTotVertex_gb[iSpan] + kSpanVertex];
+        y_loc[iSpan][iSpanVertex] = y_gb[kSize * nTotVertex_gb[iSpan] + kSpanVertex];
+        z_loc[iSpan][iSpanVertex] = z_gb[kSize * nTotVertex_gb[iSpan] + kSpanVertex];
+        angCoord_loc[iSpan][iSpanVertex] = angCoord_gb[kSize * nTotVertex_gb[iSpan] + kSpanVertex];
+        deltaAngCoord_loc[iSpan][iSpanVertex] = deltaAngCoord_gb[kSize * nTotVertex_gb[iSpan] + kSpanVertex];
+        rank_loc[iSpan][iSpanVertex] = kSize;
         target = angCoord_loc[iSpan][iSpanVertex];
-        checkAssign_gb[kSize*nTotVertex_gb[iSpan] + kSpanVertex] = true;
+        checkAssign_gb[kSize * nTotVertex_gb[iSpan] + kSpanVertex] = true;
         min = 10.0E+06;
-        for(jSize= 0; jSize < size; jSize++){
-          for(jSpanVertex = 0; jSpanVertex < nTotVertex_gb[iSpan]; jSpanVertex++){
-            if ((angCoord_gb[jSize*nTotVertex_gb[iSpan] + jSpanVertex] < min) &&
-                (angCoord_gb[jSize*nTotVertex_gb[iSpan] + jSpanVertex] >= target) &&
-                !checkAssign_gb[jSize*nTotVertex_gb[iSpan] + jSpanVertex]) {
+        for (jSize = 0; jSize < size; jSize++) {
+          for (jSpanVertex = 0; jSpanVertex < nTotVertex_gb[iSpan]; jSpanVertex++) {
+            if ((angCoord_gb[jSize * nTotVertex_gb[iSpan] + jSpanVertex] < min) &&
+                (angCoord_gb[jSize * nTotVertex_gb[iSpan] + jSpanVertex] >= target) &&
+                !checkAssign_gb[jSize * nTotVertex_gb[iSpan] + jSpanVertex]) {
               kSize = jSize;
               kSpanVertex = jSpanVertex;
-              min = angCoord_gb[jSize*nTotVertex_gb[iSpan] + jSpanVertex];
+              min = angCoord_gb[jSize * nTotVertex_gb[iSpan] + jSpanVertex];
             }
           }
         }
       }
 
-      delete [] x_gb; delete [] y_gb; delete [] z_gb;  delete [] angCoord_gb; delete [] deltaAngCoord_gb; delete[] checkAssign_gb;
-
+      delete[] x_gb;
+      delete[] y_gb;
+      delete[] z_gb;
+      delete[] angCoord_gb;
+      delete[] deltaAngCoord_gb;
+      delete[] checkAssign_gb;
     }
   }
 
 #endif
 
-  if (rank == MASTER_NODE){
-    if (marker_flag == INFLOW && val_iZone ==0){
+  if (rank == MASTER_NODE) {
+    if (marker_flag == INFLOW && val_iZone == 0) {
       std::string sPath = "TURBOMACHINERY";
       int nError = 0;
 #if defined(_WIN32)
 #ifdef __MINGW32__
       nError = mkdir(sPath.c_str());  // MINGW on Windows
 #else
-      nError = _mkdir(sPath.c_str()); // can be used on Windows
+      nError = _mkdir(sPath.c_str());  // can be used on Windows
 #endif
 #else
-      mode_t nMode = 0733; // UNIX style permissions
-      nError = mkdir(sPath.c_str(),nMode); // can be used on non-Windows
+      mode_t nMode = 0733;                   // UNIX style permissions
+      nError = mkdir(sPath.c_str(), nMode);  // can be used on non-Windows
 #endif
       if (nError != 0) {
-        cout << "TURBOMACHINERY folder creation failed." <<endl;
+        cout << "TURBOMACHINERY folder creation failed." << endl;
       }
     }
-    if (marker_flag == INFLOW){
+    if (marker_flag == INFLOW) {
       multizone_filename = "TURBOMACHINERY/spanwise_division_inflow.dat";
-    }
-    else{
+    } else {
       multizone_filename = "TURBOMACHINERY/spanwise_division_outflow.dat";
     }
     char buffer[50];
 
-    if (GetnZone() > 1){
+    if (GetnZone() > 1) {
       unsigned short lastindex = multizone_filename.find_last_of(".");
       multizone_filename = multizone_filename.substr(0, lastindex);
-      SPRINTF (buffer, "_%d.dat", SU2_TYPE::Int(val_iZone));
+      SPRINTF(buffer, "_%d.dat", SU2_TYPE::Int(val_iZone));
       multizone_filename.append(string(buffer));
     }
 
     // File to print the vector x_loc, y_loc, z_loc, globIdx_loc to check vertex ordering
     ofstream myfile;
-    myfile.open (multizone_filename.data(), ios::out | ios::trunc);
+    myfile.open(multizone_filename.data(), ios::out | ios::trunc);
     myfile.setf(ios::uppercase | ios::scientific);
     myfile.precision(8);
 
     myfile << "TITLE = \"Global index visualization file\"" << endl;
     myfile << "VARIABLES =" << endl;
-    myfile.width(10); myfile << "\"iSpan\"";
-    myfile.width(20); myfile << "\"x_coord\"" ;
-    myfile.width(20); myfile << "\"y_coord\"" ;
-    myfile.width(20); myfile << "\"z_coord\"" ;
-    myfile.width(20); myfile << "\"radius\"" ;
-    myfile.width(20); myfile << "\"Relative Angular Coord \"" ;
-    myfile.width(20); myfile << "\"Delta Angular Coord \"" ;
-    myfile.width(20); myfile << "\"processor\"" <<endl;
-    for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-      for(iSpanVertex = 0; iSpanVertex < nTotVertex_gb[iSpan]; iSpanVertex++){
-        radius = sqrt(x_loc[iSpan][iSpanVertex]*x_loc[iSpan][iSpanVertex] + y_loc[iSpan][iSpanVertex]*y_loc[iSpan][iSpanVertex]);
-        myfile.width(10); myfile << iSpan;
-        myfile.width(20); myfile << x_loc[iSpan][iSpanVertex];
-        myfile.width(20); myfile << y_loc[iSpan][iSpanVertex];
-        myfile.width(20); myfile << z_loc[iSpan][iSpanVertex];
-        myfile.width(20); myfile << radius;
-        if (nDim ==2 && config->GetKind_TurboMachinery(val_iZone)){
-          myfile.width(20); myfile << angCoord_loc[iSpan][iSpanVertex];
-          myfile.width(20); myfile << deltaAngCoord_loc[iSpan][iSpanVertex];
+    myfile.width(10);
+    myfile << "\"iSpan\"";
+    myfile.width(20);
+    myfile << "\"x_coord\"";
+    myfile.width(20);
+    myfile << "\"y_coord\"";
+    myfile.width(20);
+    myfile << "\"z_coord\"";
+    myfile.width(20);
+    myfile << "\"radius\"";
+    myfile.width(20);
+    myfile << "\"Relative Angular Coord \"";
+    myfile.width(20);
+    myfile << "\"Delta Angular Coord \"";
+    myfile.width(20);
+    myfile << "\"processor\"" << endl;
+    for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+      for (iSpanVertex = 0; iSpanVertex < nTotVertex_gb[iSpan]; iSpanVertex++) {
+        radius = sqrt(x_loc[iSpan][iSpanVertex] * x_loc[iSpan][iSpanVertex] +
+                      y_loc[iSpan][iSpanVertex] * y_loc[iSpan][iSpanVertex]);
+        myfile.width(10);
+        myfile << iSpan;
+        myfile.width(20);
+        myfile << x_loc[iSpan][iSpanVertex];
+        myfile.width(20);
+        myfile << y_loc[iSpan][iSpanVertex];
+        myfile.width(20);
+        myfile << z_loc[iSpan][iSpanVertex];
+        myfile.width(20);
+        myfile << radius;
+        if (nDim == 2 && config->GetKind_TurboMachinery(val_iZone)) {
+          myfile.width(20);
+          myfile << angCoord_loc[iSpan][iSpanVertex];
+          myfile.width(20);
+          myfile << deltaAngCoord_loc[iSpan][iSpanVertex];
+        } else {
+          myfile.width(20);
+          myfile << angCoord_loc[iSpan][iSpanVertex] * 180.0 / PI_NUMBER;
+          myfile.width(20);
+          myfile << deltaAngCoord_loc[iSpan][iSpanVertex] * 180.0 / PI_NUMBER;
         }
-        else{
-          myfile.width(20); myfile << angCoord_loc[iSpan][iSpanVertex]*180.0/PI_NUMBER;
-          myfile.width(20); myfile << deltaAngCoord_loc[iSpan][iSpanVertex]*180.0/PI_NUMBER;
-        }
-        myfile.width(20); myfile << rank_loc[iSpan][iSpanVertex]<<endl;
+        myfile.width(20);
+        myfile << rank_loc[iSpan][iSpanVertex] << endl;
       }
       myfile << endl;
     }
   }
 
-
-  for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-    delete [] x_loc[iSpan];
-    delete [] y_loc[iSpan];
-    delete [] z_loc[iSpan];
-    delete [] angCoord_loc[iSpan];
-    delete [] deltaAngCoord_loc[iSpan];
-    delete [] rank_loc[iSpan];
-
-  }
-
-
-  delete [] area;
-  delete [] ordered;
-  delete [] disordered;
-  delete [] oldVertex3D;
-  delete [] checkAssign;
-  delete [] TurboNormal;
-  delete [] unitnormal;
-  delete [] NormalArea;
-  delete [] x_loc;
-  delete [] y_loc;
-  delete [] z_loc;
-  delete [] angCoord_loc;
-  delete [] nTotVertex_gb;
-  delete [] nVertexSpanHalo;
-  delete [] angPitch;
-  delete [] deltaAngPitch;
-  delete [] deltaAngCoord_loc;
-  delete [] rank_loc;
-  delete [] minAngPitch;
-  delete [] maxAngPitch;
-  delete [] minIntAngPitch;
-
+  for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+    delete[] x_loc[iSpan];
+    delete[] y_loc[iSpan];
+    delete[] z_loc[iSpan];
+    delete[] angCoord_loc[iSpan];
+    delete[] deltaAngCoord_loc[iSpan];
+    delete[] rank_loc[iSpan];
+  }
+
+  delete[] area;
+  delete[] ordered;
+  delete[] disordered;
+  delete[] oldVertex3D;
+  delete[] checkAssign;
+  delete[] TurboNormal;
+  delete[] unitnormal;
+  delete[] NormalArea;
+  delete[] x_loc;
+  delete[] y_loc;
+  delete[] z_loc;
+  delete[] angCoord_loc;
+  delete[] nTotVertex_gb;
+  delete[] nVertexSpanHalo;
+  delete[] angPitch;
+  delete[] deltaAngPitch;
+  delete[] deltaAngCoord_loc;
+  delete[] rank_loc;
+  delete[] minAngPitch;
+  delete[] maxAngPitch;
+  delete[] minIntAngPitch;
 }
 
-
-void CPhysicalGeometry::UpdateTurboVertex(CConfig *config, unsigned short val_iZone, unsigned short marker_flag) {
+void CPhysicalGeometry::UpdateTurboVertex(CConfig* config, unsigned short val_iZone, unsigned short marker_flag) {
   unsigned short iMarker, iMarkerTP, iSpan, iDim;
   long iSpanVertex, iPoint;
   su2double *coord, *TurboNormal, Normal2;
 
   /*--- Initialize auxiliary pointers ---*/
-  TurboNormal      = new su2double[3];
-
-  for (iMarker = 0; iMarker < nMarker; iMarker++){
-    for (iMarkerTP=1; iMarkerTP < config->GetnMarker_Turbomachinery()+1; iMarkerTP++){
-      if (config->GetMarker_All_Turbomachinery(iMarker) == iMarkerTP){
-        if (config->GetMarker_All_TurbomachineryFlag(iMarker) == marker_flag){
-          for(iSpan = 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-            for(iSpanVertex = 0; iSpanVertex<nVertexSpan[iMarker][iSpan]; iSpanVertex++){
+  TurboNormal = new su2double[3];
+
+  for (iMarker = 0; iMarker < nMarker; iMarker++) {
+    for (iMarkerTP = 1; iMarkerTP < config->GetnMarker_Turbomachinery() + 1; iMarkerTP++) {
+      if (config->GetMarker_All_Turbomachinery(iMarker) == iMarkerTP) {
+        if (config->GetMarker_All_TurbomachineryFlag(iMarker) == marker_flag) {
+          for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
+            for (iSpanVertex = 0; iSpanVertex < nVertexSpan[iMarker][iSpan]; iSpanVertex++) {
               iPoint = turbovertex[iMarker][iSpan][iSpanVertex]->GetNode();
-              coord  = nodes->GetCoord(iPoint);
+              coord = nodes->GetCoord(iPoint);
               /*--- compute appropriate turbo normal ---*/
-              switch (config->GetKind_TurboMachinery(val_iZone)){
-              case CENTRIFUGAL:
-                Normal2 = 0.0;
-                for(iDim = 0; iDim < 2; iDim++) Normal2 +=coord[iDim]*coord[iDim];
-                if (marker_flag == INFLOW){
-                  TurboNormal[0] = -coord[0]/sqrt(Normal2);
-                  TurboNormal[1] = -coord[1]/sqrt(Normal2);
-                  TurboNormal[2] = 0.0;
-                }else{
-                  TurboNormal[0] = coord[0]/sqrt(Normal2);
-                  TurboNormal[1] = coord[1]/sqrt(Normal2);
-                  TurboNormal[2] = 0.0;
-                }
-                break;
-              case CENTRIPETAL:
-                Normal2 = 0.0;
-                for(iDim = 0; iDim < 2; iDim++) Normal2 +=coord[iDim]*coord[iDim];
-                if (marker_flag == OUTFLOW){
-                  TurboNormal[0] = -coord[0]/sqrt(Normal2);
-                  TurboNormal[1] = -coord[1]/sqrt(Normal2);
-                  TurboNormal[2] = 0.0;
-                }else{
-                  TurboNormal[0] = coord[0]/sqrt(Normal2);
-                  TurboNormal[1] = coord[1]/sqrt(Normal2);
-                  TurboNormal[2] = 0.0;
-                }
-                break;
-              case AXIAL:
-                Normal2 = 0.0;
-                for(iDim = 0; iDim < 2; iDim++) Normal2 +=coord[iDim]*coord[iDim];
-                if(nDim == 3){
-                  if (marker_flag == INFLOW){
-                    TurboNormal[0] = coord[0]/sqrt(Normal2);
-                    TurboNormal[1] = coord[1]/sqrt(Normal2);
+              switch (config->GetKind_TurboMachinery(val_iZone)) {
+                case CENTRIFUGAL:
+                  Normal2 = 0.0;
+                  for (iDim = 0; iDim < 2; iDim++) Normal2 += coord[iDim] * coord[iDim];
+                  if (marker_flag == INFLOW) {
+                    TurboNormal[0] = -coord[0] / sqrt(Normal2);
+                    TurboNormal[1] = -coord[1] / sqrt(Normal2);
                     TurboNormal[2] = 0.0;
-                  }else{
-                    TurboNormal[0] = coord[0]/sqrt(Normal2);
-                    TurboNormal[1] = coord[1]/sqrt(Normal2);
+                  } else {
+                    TurboNormal[0] = coord[0] / sqrt(Normal2);
+                    TurboNormal[1] = coord[1] / sqrt(Normal2);
                     TurboNormal[2] = 0.0;
                   }
-                }
-                else{
-                  if (marker_flag == INFLOW){
-                    TurboNormal[0] = -1.0;
-                    TurboNormal[1] = 0.0;
+                  break;
+                case CENTRIPETAL:
+                  Normal2 = 0.0;
+                  for (iDim = 0; iDim < 2; iDim++) Normal2 += coord[iDim] * coord[iDim];
+                  if (marker_flag == OUTFLOW) {
+                    TurboNormal[0] = -coord[0] / sqrt(Normal2);
+                    TurboNormal[1] = -coord[1] / sqrt(Normal2);
                     TurboNormal[2] = 0.0;
-                  }else{
-                    TurboNormal[0] = 1.0;
-                    TurboNormal[1] = 0.0;
+                  } else {
+                    TurboNormal[0] = coord[0] / sqrt(Normal2);
+                    TurboNormal[1] = coord[1] / sqrt(Normal2);
                     TurboNormal[2] = 0.0;
                   }
-                }
+                  break;
+                case AXIAL:
+                  Normal2 = 0.0;
+                  for (iDim = 0; iDim < 2; iDim++) Normal2 += coord[iDim] * coord[iDim];
+                  if (nDim == 3) {
+                    if (marker_flag == INFLOW) {
+                      TurboNormal[0] = coord[0] / sqrt(Normal2);
+                      TurboNormal[1] = coord[1] / sqrt(Normal2);
+                      TurboNormal[2] = 0.0;
+                    } else {
+                      TurboNormal[0] = coord[0] / sqrt(Normal2);
+                      TurboNormal[1] = coord[1] / sqrt(Normal2);
+                      TurboNormal[2] = 0.0;
+                    }
+                  } else {
+                    if (marker_flag == INFLOW) {
+                      TurboNormal[0] = -1.0;
+                      TurboNormal[1] = 0.0;
+                      TurboNormal[2] = 0.0;
+                    } else {
+                      TurboNormal[0] = 1.0;
+                      TurboNormal[1] = 0.0;
+                      TurboNormal[2] = 0.0;
+                    }
+                  }
 
-                break;
-              case CENTRIPETAL_AXIAL:
-                Normal2 = 0.0;
-                for(iDim = 0; iDim < 2; iDim++) Normal2 +=coord[iDim]*coord[iDim];
-                if (marker_flag == INFLOW){
-                  TurboNormal[0] = coord[0]/sqrt(Normal2);
-                  TurboNormal[1] = coord[1]/sqrt(Normal2);
-                  TurboNormal[2] = 0.0;
-                }else{
-                  TurboNormal[0] = coord[0]/sqrt(Normal2);
-                  TurboNormal[1] = coord[1]/sqrt(Normal2);
-                  TurboNormal[2] = 0.0;
-                }
-                break;
-
-              case AXIAL_CENTRIFUGAL:
-                Normal2 = 0.0;
-                for(iDim = 0; iDim < 2; iDim++) Normal2 +=coord[iDim]*coord[iDim];
-                if (marker_flag == INFLOW){
-                  TurboNormal[0] = coord[0]/sqrt(Normal2);
-                  TurboNormal[1] = coord[1]/sqrt(Normal2);
-                  TurboNormal[2] = 0.0;
-                }else{
-                  TurboNormal[0] = coord[0]/sqrt(Normal2);
-                  TurboNormal[1] = coord[1]/sqrt(Normal2);
-                  TurboNormal[2] = 0.0;
-                }
-                break;
+                  break;
+                case CENTRIPETAL_AXIAL:
+                  Normal2 = 0.0;
+                  for (iDim = 0; iDim < 2; iDim++) Normal2 += coord[iDim] * coord[iDim];
+                  if (marker_flag == INFLOW) {
+                    TurboNormal[0] = coord[0] / sqrt(Normal2);
+                    TurboNormal[1] = coord[1] / sqrt(Normal2);
+                    TurboNormal[2] = 0.0;
+                  } else {
+                    TurboNormal[0] = coord[0] / sqrt(Normal2);
+                    TurboNormal[1] = coord[1] / sqrt(Normal2);
+                    TurboNormal[2] = 0.0;
+                  }
+                  break;
+
+                case AXIAL_CENTRIFUGAL:
+                  Normal2 = 0.0;
+                  for (iDim = 0; iDim < 2; iDim++) Normal2 += coord[iDim] * coord[iDim];
+                  if (marker_flag == INFLOW) {
+                    TurboNormal[0] = coord[0] / sqrt(Normal2);
+                    TurboNormal[1] = coord[1] / sqrt(Normal2);
+                    TurboNormal[2] = 0.0;
+                  } else {
+                    TurboNormal[0] = coord[0] / sqrt(Normal2);
+                    TurboNormal[1] = coord[1] / sqrt(Normal2);
+                    TurboNormal[2] = 0.0;
+                  }
+                  break;
               }
 
               /*--- store the new turbo normal ---*/
@@ -6195,54 +5878,54 @@ void CPhysicalGeometry::UpdateTurboVertex(CConfig *config, unsigned short val_iZ
     }
   }
 
-  delete [] TurboNormal;
+  delete[] TurboNormal;
 }
 
-void CPhysicalGeometry::SetAvgTurboValue(CConfig *config, unsigned short val_iZone, unsigned short marker_flag, bool allocate) {
-
+void CPhysicalGeometry::SetAvgTurboValue(CConfig* config, unsigned short val_iZone, unsigned short marker_flag,
+                                         bool allocate) {
   unsigned short iMarker, iMarkerTP, iSpan, iDim;
   unsigned long iPoint;
-  su2double *TurboNormal,*coord, *Normal, turboNormal2, Normal2, *gridVel, TotalArea, TotalRadius, radius;
-  su2double *TotalTurboNormal,*TotalNormal, *TotalGridVel, Area;
+  su2double *TurboNormal, *coord, *Normal, turboNormal2, Normal2, *gridVel, TotalArea, TotalRadius, radius;
+  su2double *TotalTurboNormal, *TotalNormal, *TotalGridVel, Area;
   long iVertex;
   /*-- Variables declaration and allocation ---*/
   TotalTurboNormal = new su2double[nDim];
-  TotalNormal      = new su2double[nDim];
-  TurboNormal      = new su2double[nDim];
-  TotalGridVel     = new su2double[nDim];
-  Normal           = new su2double[nDim];
+  TotalNormal = new su2double[nDim];
+  TurboNormal = new su2double[nDim];
+  TotalGridVel = new su2double[nDim];
+  Normal = new su2double[nDim];
 
-  bool grid_movement        = config->GetGrid_Movement();
+  bool grid_movement = config->GetGrid_Movement();
 #ifdef HAVE_MPI
-  su2double MyTotalArea, MyTotalRadius, *MyTotalTurboNormal= NULL, *MyTotalNormal= NULL, *MyTotalGridVel= NULL;
+  su2double MyTotalArea, MyTotalRadius, *MyTotalTurboNormal = NULL, *MyTotalNormal = NULL, *MyTotalGridVel = NULL;
 #endif
 
   /*--- Intialization of the vector for the interested boundary ---*/
-  for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++){
-    for (iMarkerTP=1; iMarkerTP < config->GetnMarker_Turbomachinery()+1; iMarkerTP++){
-      if (config->GetMarker_All_Turbomachinery(iMarker) == iMarkerTP){
-        if (config->GetMarker_All_TurbomachineryFlag(iMarker) == marker_flag){
-          if(allocate){
-            AverageTurboNormal[iMarker]               = new su2double *[nSpanWiseSections[marker_flag-1] + 1];
-            AverageNormal[iMarker]                    = new su2double *[nSpanWiseSections[marker_flag-1] + 1];
-            AverageGridVel[iMarker]                   = new su2double *[nSpanWiseSections[marker_flag-1] + 1];
-            AverageTangGridVel[iMarker]               = new su2double [nSpanWiseSections[marker_flag-1] + 1];
-            SpanArea[iMarker]                         = new su2double [nSpanWiseSections[marker_flag-1] + 1];
-            TurboRadius[iMarker]                      = new su2double [nSpanWiseSections[marker_flag-1] + 1];
-            for (iSpan= 0; iSpan < nSpanWiseSections[marker_flag-1] + 1; iSpan++){
-              AverageTurboNormal[iMarker][iSpan]      = new su2double [nDim];
-              AverageNormal[iMarker][iSpan]           = new su2double [nDim];
-              AverageGridVel[iMarker][iSpan]          = new su2double [nDim];
+  for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
+    for (iMarkerTP = 1; iMarkerTP < config->GetnMarker_Turbomachinery() + 1; iMarkerTP++) {
+      if (config->GetMarker_All_Turbomachinery(iMarker) == iMarkerTP) {
+        if (config->GetMarker_All_TurbomachineryFlag(iMarker) == marker_flag) {
+          if (allocate) {
+            AverageTurboNormal[iMarker] = new su2double*[nSpanWiseSections[marker_flag - 1] + 1];
+            AverageNormal[iMarker] = new su2double*[nSpanWiseSections[marker_flag - 1] + 1];
+            AverageGridVel[iMarker] = new su2double*[nSpanWiseSections[marker_flag - 1] + 1];
+            AverageTangGridVel[iMarker] = new su2double[nSpanWiseSections[marker_flag - 1] + 1];
+            SpanArea[iMarker] = new su2double[nSpanWiseSections[marker_flag - 1] + 1];
+            TurboRadius[iMarker] = new su2double[nSpanWiseSections[marker_flag - 1] + 1];
+            for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1] + 1; iSpan++) {
+              AverageTurboNormal[iMarker][iSpan] = new su2double[nDim];
+              AverageNormal[iMarker][iSpan] = new su2double[nDim];
+              AverageGridVel[iMarker][iSpan] = new su2double[nDim];
             }
           }
-          for (iSpan= 0; iSpan < nSpanWiseSections[marker_flag-1] + 1; iSpan++){
-            AverageTangGridVel[iMarker][iSpan]          = 0.0;
-            SpanArea[iMarker][iSpan]                    = 0.0;
-            TurboRadius[iMarker][iSpan]                 = 0.0;
-            for(iDim=0; iDim < nDim; iDim++){
-              AverageTurboNormal[iMarker][iSpan][iDim]  = 0.0;
-              AverageNormal[iMarker][iSpan][iDim]       = 0.0;
-              AverageGridVel[iMarker][iSpan][iDim]      = 0.0;
+          for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1] + 1; iSpan++) {
+            AverageTangGridVel[iMarker][iSpan] = 0.0;
+            SpanArea[iMarker][iSpan] = 0.0;
+            TurboRadius[iMarker][iSpan] = 0.0;
+            for (iDim = 0; iDim < nDim; iDim++) {
+              AverageTurboNormal[iMarker][iSpan][iDim] = 0.0;
+              AverageNormal[iMarker][iSpan][iDim] = 0.0;
+              AverageGridVel[iMarker][iSpan][iDim] = 0.0;
             }
           }
         }
@@ -6250,45 +5933,41 @@ void CPhysicalGeometry::SetAvgTurboValue(CConfig *config, unsigned short val_iZo
     }
   }
 
-
-
   /*--- start computing the average quantities span wise --- */
-  for (iSpan= 0; iSpan < nSpanWiseSections[marker_flag-1]; iSpan++){
-
+  for (iSpan = 0; iSpan < nSpanWiseSections[marker_flag - 1]; iSpan++) {
     /*--- Forces initialization for contenitors to zero ---*/
-    for (iDim=0; iDim<nDim; iDim++) {
-      TotalTurboNormal[iDim]  =0.0;
-      TotalNormal[iDim]         =0.0;
-      TotalGridVel[iDim]        =0.0;
+    for (iDim = 0; iDim < nDim; iDim++) {
+      TotalTurboNormal[iDim] = 0.0;
+      TotalNormal[iDim] = 0.0;
+      TotalGridVel[iDim] = 0.0;
     }
     TotalArea = 0.0;
     TotalRadius = 0.0;
-    for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++){
-      for (iMarkerTP=1; iMarkerTP < config->GetnMarker_Turbomachinery()+1; iMarkerTP++){
-        if (config->GetMarker_All_Turbomachinery(iMarker) == iMarkerTP){
-          if (config->GetMarker_All_TurbomachineryFlag(iMarker) == marker_flag){
-            for(iVertex = 0; iVertex < nVertexSpan[iMarker][iSpan]; iVertex++){
+    for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
+      for (iMarkerTP = 1; iMarkerTP < config->GetnMarker_Turbomachinery() + 1; iMarkerTP++) {
+        if (config->GetMarker_All_Turbomachinery(iMarker) == iMarkerTP) {
+          if (config->GetMarker_All_TurbomachineryFlag(iMarker) == marker_flag) {
+            for (iVertex = 0; iVertex < nVertexSpan[iMarker][iSpan]; iVertex++) {
               iPoint = turbovertex[iMarker][iSpan][iVertex]->GetNode();
               turbovertex[iMarker][iSpan][iVertex]->GetTurboNormal(TurboNormal);
               turbovertex[iMarker][iSpan][iVertex]->GetNormal(Normal);
-              coord  = nodes->GetCoord(iPoint);
+              coord = nodes->GetCoord(iPoint);
 
-              if (nDim == 3){
-                radius = sqrt(coord[0]*coord[0] + coord[1]*coord[1]);
-              }
-              else{
+              if (nDim == 3) {
+                radius = sqrt(coord[0] * coord[0] + coord[1] * coord[1]);
+              } else {
                 radius = 0.0;
               }
               Area = turbovertex[iMarker][iSpan][iVertex]->GetArea();
-              TotalArea   += Area;
+              TotalArea += Area;
               TotalRadius += radius;
               for (iDim = 0; iDim < nDim; iDim++) {
-                TotalTurboNormal[iDim]  +=TurboNormal[iDim];
-                TotalNormal[iDim]       +=Normal[iDim];
+                TotalTurboNormal[iDim] += TurboNormal[iDim];
+                TotalNormal[iDim] += Normal[iDim];
               }
-              if (grid_movement){
+              if (grid_movement) {
                 gridVel = nodes->GetGridVel(iPoint);
-                for (iDim = 0; iDim < nDim; iDim++) TotalGridVel[iDim] +=gridVel[iDim];
+                for (iDim = 0; iDim < nDim; iDim++) TotalGridVel[iDim] += gridVel[iDim];
               }
             }
           }
@@ -6298,104 +5977,120 @@ void CPhysicalGeometry::SetAvgTurboValue(CConfig *config, unsigned short val_iZo
 
 #ifdef HAVE_MPI
 
-    MyTotalArea            = TotalArea;                 TotalArea            = 0;
-    MyTotalRadius          = TotalRadius;               TotalRadius          = 0;
+    MyTotalArea = TotalArea;
+    TotalArea = 0;
+    MyTotalRadius = TotalRadius;
+    TotalRadius = 0;
     SU2_MPI::Allreduce(&MyTotalArea, &TotalArea, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
     SU2_MPI::Allreduce(&MyTotalRadius, &TotalRadius, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
 
-    MyTotalTurboNormal     = new su2double[nDim];
-    MyTotalNormal          = new su2double[nDim];
-    MyTotalGridVel         = new su2double[nDim];
+    MyTotalTurboNormal = new su2double[nDim];
+    MyTotalNormal = new su2double[nDim];
+    MyTotalGridVel = new su2double[nDim];
 
     for (iDim = 0; iDim < nDim; iDim++) {
-      MyTotalTurboNormal[iDim]  = TotalTurboNormal[iDim];
-      TotalTurboNormal[iDim]    = 0.0;
-      MyTotalNormal[iDim]       = TotalNormal[iDim];
-      TotalNormal[iDim]         = 0.0;
-      MyTotalGridVel[iDim]      = TotalGridVel[iDim];
-      TotalGridVel[iDim]        = 0.0;
+      MyTotalTurboNormal[iDim] = TotalTurboNormal[iDim];
+      TotalTurboNormal[iDim] = 0.0;
+      MyTotalNormal[iDim] = TotalNormal[iDim];
+      TotalNormal[iDim] = 0.0;
+      MyTotalGridVel[iDim] = TotalGridVel[iDim];
+      TotalGridVel[iDim] = 0.0;
     }
 
     SU2_MPI::Allreduce(MyTotalTurboNormal, TotalTurboNormal, nDim, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
     SU2_MPI::Allreduce(MyTotalNormal, TotalNormal, nDim, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
     SU2_MPI::Allreduce(MyTotalGridVel, TotalGridVel, nDim, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
 
-    delete [] MyTotalTurboNormal;delete [] MyTotalNormal; delete [] MyTotalGridVel;
+    delete[] MyTotalTurboNormal;
+    delete[] MyTotalNormal;
+    delete[] MyTotalGridVel;
 
 #endif
 
-    for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++){
-      for (iMarkerTP=1; iMarkerTP < config->GetnMarker_Turbomachinery()+1; iMarkerTP++){
-        if (config->GetMarker_All_Turbomachinery(iMarker) == iMarkerTP){
-          if (config->GetMarker_All_TurbomachineryFlag(iMarker) == marker_flag){
-
-
-            SpanArea[iMarker][iSpan]           = TotalArea;
-            TurboRadius[iMarker][iSpan]        = TotalRadius/nTotVertexSpan[iMarker][iSpan];
-
-            turboNormal2    = 0.0;
-            Normal2         = 0.0;
-            for (iDim = 0; iDim < nDim; iDim++){
-              turboNormal2 += TotalTurboNormal[iDim]*TotalTurboNormal[iDim];
-              Normal2      += TotalNormal[iDim]*TotalNormal[iDim];
+    for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
+      for (iMarkerTP = 1; iMarkerTP < config->GetnMarker_Turbomachinery() + 1; iMarkerTP++) {
+        if (config->GetMarker_All_Turbomachinery(iMarker) == iMarkerTP) {
+          if (config->GetMarker_All_TurbomachineryFlag(iMarker) == marker_flag) {
+            SpanArea[iMarker][iSpan] = TotalArea;
+            TurboRadius[iMarker][iSpan] = TotalRadius / nTotVertexSpan[iMarker][iSpan];
+
+            turboNormal2 = 0.0;
+            Normal2 = 0.0;
+            for (iDim = 0; iDim < nDim; iDim++) {
+              turboNormal2 += TotalTurboNormal[iDim] * TotalTurboNormal[iDim];
+              Normal2 += TotalNormal[iDim] * TotalNormal[iDim];
             }
-            for (iDim = 0; iDim < nDim; iDim++){
-              AverageTurboNormal[iMarker][iSpan][iDim] = TotalTurboNormal[iDim]/sqrt(turboNormal2);
-              AverageNormal[iMarker][iSpan][iDim]      = TotalNormal[iDim]/sqrt(Normal2);
+            for (iDim = 0; iDim < nDim; iDim++) {
+              AverageTurboNormal[iMarker][iSpan][iDim] = TotalTurboNormal[iDim] / sqrt(turboNormal2);
+              AverageNormal[iMarker][iSpan][iDim] = TotalNormal[iDim] / sqrt(Normal2);
             }
-            if (grid_movement){
-              for (iDim = 0; iDim < nDim; iDim++){
-                AverageGridVel[iMarker][iSpan][iDim]   =TotalGridVel[iDim]/nTotVertexSpan[iMarker][iSpan];
+            if (grid_movement) {
+              for (iDim = 0; iDim < nDim; iDim++) {
+                AverageGridVel[iMarker][iSpan][iDim] = TotalGridVel[iDim] / nTotVertexSpan[iMarker][iSpan];
               }
-              switch (config->GetKind_TurboMachinery(val_iZone)){
-              case CENTRIFUGAL:case CENTRIPETAL:
-                if (marker_flag == INFLOW ){
-                  AverageTangGridVel[iMarker][iSpan]= -(AverageTurboNormal[iMarker][iSpan][0]*AverageGridVel[iMarker][iSpan][1]-AverageTurboNormal[iMarker][iSpan][1]*AverageGridVel[iMarker][iSpan][0]);
-                }
-                else{
-                  AverageTangGridVel[iMarker][iSpan]= AverageTurboNormal[iMarker][iSpan][0]*AverageGridVel[iMarker][iSpan][1]-AverageTurboNormal[iMarker][iSpan][1]*AverageGridVel[iMarker][iSpan][0];
-                }
-                break;
-              case AXIAL:
-                if (marker_flag == INFLOW && nDim == 2){
-                  AverageTangGridVel[iMarker][iSpan]= -AverageTurboNormal[iMarker][iSpan][0]*AverageGridVel[iMarker][iSpan][1] + AverageTurboNormal[iMarker][iSpan][1]*AverageGridVel[iMarker][iSpan][0];
-                }
-                else{
-                  AverageTangGridVel[iMarker][iSpan]= AverageTurboNormal[iMarker][iSpan][0]*AverageGridVel[iMarker][iSpan][1]-AverageTurboNormal[iMarker][iSpan][1]*AverageGridVel[iMarker][iSpan][0];
-                }
+              switch (config->GetKind_TurboMachinery(val_iZone)) {
+                case CENTRIFUGAL:
+                case CENTRIPETAL:
+                  if (marker_flag == INFLOW) {
+                    AverageTangGridVel[iMarker][iSpan] =
+                        -(AverageTurboNormal[iMarker][iSpan][0] * AverageGridVel[iMarker][iSpan][1] -
+                          AverageTurboNormal[iMarker][iSpan][1] * AverageGridVel[iMarker][iSpan][0]);
+                  } else {
+                    AverageTangGridVel[iMarker][iSpan] =
+                        AverageTurboNormal[iMarker][iSpan][0] * AverageGridVel[iMarker][iSpan][1] -
+                        AverageTurboNormal[iMarker][iSpan][1] * AverageGridVel[iMarker][iSpan][0];
+                  }
+                  break;
+                case AXIAL:
+                  if (marker_flag == INFLOW && nDim == 2) {
+                    AverageTangGridVel[iMarker][iSpan] =
+                        -AverageTurboNormal[iMarker][iSpan][0] * AverageGridVel[iMarker][iSpan][1] +
+                        AverageTurboNormal[iMarker][iSpan][1] * AverageGridVel[iMarker][iSpan][0];
+                  } else {
+                    AverageTangGridVel[iMarker][iSpan] =
+                        AverageTurboNormal[iMarker][iSpan][0] * AverageGridVel[iMarker][iSpan][1] -
+                        AverageTurboNormal[iMarker][iSpan][1] * AverageGridVel[iMarker][iSpan][0];
+                  }
+                  break;
+                case CENTRIPETAL_AXIAL:
+                  if (marker_flag == OUTFLOW) {
+                    AverageTangGridVel[iMarker][iSpan] =
+                        (AverageTurboNormal[iMarker][iSpan][0] * AverageGridVel[iMarker][iSpan][1] -
+                         AverageTurboNormal[iMarker][iSpan][1] * AverageGridVel[iMarker][iSpan][0]);
+                  } else {
+                    AverageTangGridVel[iMarker][iSpan] =
+                        -(AverageTurboNormal[iMarker][iSpan][0] * AverageGridVel[iMarker][iSpan][1] -
+                          AverageTurboNormal[iMarker][iSpan][1] * AverageGridVel[iMarker][iSpan][0]);
+                  }
+                  break;
+                case AXIAL_CENTRIFUGAL:
+                  if (marker_flag == INFLOW) {
+                    AverageTangGridVel[iMarker][iSpan] =
+                        AverageTurboNormal[iMarker][iSpan][0] * AverageGridVel[iMarker][iSpan][1] -
+                        AverageTurboNormal[iMarker][iSpan][1] * AverageGridVel[iMarker][iSpan][0];
+                  } else {
+                    AverageTangGridVel[iMarker][iSpan] =
+                        AverageTurboNormal[iMarker][iSpan][0] * AverageGridVel[iMarker][iSpan][1] -
+                        AverageTurboNormal[iMarker][iSpan][1] * AverageGridVel[iMarker][iSpan][0];
+                  }
                   break;
-              case CENTRIPETAL_AXIAL:
-                if (marker_flag == OUTFLOW){
-                  AverageTangGridVel[iMarker][iSpan]= (AverageTurboNormal[iMarker][iSpan][0]*AverageGridVel[iMarker][iSpan][1]-AverageTurboNormal[iMarker][iSpan][1]*AverageGridVel[iMarker][iSpan][0]);
-                }
-                else{
-                  AverageTangGridVel[iMarker][iSpan]= -(AverageTurboNormal[iMarker][iSpan][0]*AverageGridVel[iMarker][iSpan][1]-AverageTurboNormal[iMarker][iSpan][1]*AverageGridVel[iMarker][iSpan][0]);
-                }
-                break;
-              case AXIAL_CENTRIFUGAL:
-                if (marker_flag == INFLOW)
-                {
-                  AverageTangGridVel[iMarker][iSpan]= AverageTurboNormal[iMarker][iSpan][0]*AverageGridVel[iMarker][iSpan][1]-AverageTurboNormal[iMarker][iSpan][1]*AverageGridVel[iMarker][iSpan][0];
-                }else
-                {
-                  AverageTangGridVel[iMarker][iSpan]= AverageTurboNormal[iMarker][iSpan][0]*AverageGridVel[iMarker][iSpan][1]-AverageTurboNormal[iMarker][iSpan][1]*AverageGridVel[iMarker][iSpan][0];
-                }
-                break;
 
-              default:
+                default:
                   SU2_MPI::Error("Tang grid velocity NOT IMPLEMENTED YET for this configuration", CURRENT_FUNCTION);
-                break;
+                  break;
               }
             }
 
             /*--- Compute the 1D average values ---*/
-            AverageTangGridVel[iMarker][nSpanWiseSections[marker_flag-1]]             += AverageTangGridVel[iMarker][iSpan]/nSpanWiseSections[marker_flag-1];
-            SpanArea[iMarker][nSpanWiseSections[marker_flag-1]]                       += SpanArea[iMarker][iSpan];
-            for(iDim=0; iDim < nDim; iDim++){
-              AverageTurboNormal[iMarker][nSpanWiseSections[marker_flag-1]][iDim]     += AverageTurboNormal[iMarker][iSpan][iDim];
-              AverageNormal[iMarker][nSpanWiseSections[marker_flag-1]][iDim]          += AverageNormal[iMarker][iSpan][iDim];
-              AverageGridVel[iMarker][nSpanWiseSections[marker_flag-1]][iDim]         += AverageGridVel[iMarker][iSpan][iDim]/nSpanWiseSections[marker_flag-1];
-
+            AverageTangGridVel[iMarker][nSpanWiseSections[marker_flag - 1]] +=
+                AverageTangGridVel[iMarker][iSpan] / nSpanWiseSections[marker_flag - 1];
+            SpanArea[iMarker][nSpanWiseSections[marker_flag - 1]] += SpanArea[iMarker][iSpan];
+            for (iDim = 0; iDim < nDim; iDim++) {
+              AverageTurboNormal[iMarker][nSpanWiseSections[marker_flag - 1]][iDim] +=
+                  AverageTurboNormal[iMarker][iSpan][iDim];
+              AverageNormal[iMarker][nSpanWiseSections[marker_flag - 1]][iDim] += AverageNormal[iMarker][iSpan][iDim];
+              AverageGridVel[iMarker][nSpanWiseSections[marker_flag - 1]][iDim] +=
+                  AverageGridVel[iMarker][iSpan][iDim] / nSpanWiseSections[marker_flag - 1];
             }
           }
         }
@@ -6404,38 +6099,36 @@ void CPhysicalGeometry::SetAvgTurboValue(CConfig *config, unsigned short val_iZo
   }
 
   /*--- Normalize 1D normals---*/
-  for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++){
-    for (iMarkerTP=1; iMarkerTP < config->GetnMarker_Turbomachinery()+1; iMarkerTP++){
-      if (config->GetMarker_All_Turbomachinery(iMarker) == iMarkerTP){
-        if (config->GetMarker_All_TurbomachineryFlag(iMarker) == marker_flag){
+  for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
+    for (iMarkerTP = 1; iMarkerTP < config->GetnMarker_Turbomachinery() + 1; iMarkerTP++) {
+      if (config->GetMarker_All_Turbomachinery(iMarker) == iMarkerTP) {
+        if (config->GetMarker_All_TurbomachineryFlag(iMarker) == marker_flag) {
           turboNormal2 = 0.0;
-          Normal2     = 0.0;
+          Normal2 = 0.0;
 
-          for (iDim = 0; iDim < nDim; iDim++){
-            turboNormal2 += AverageTurboNormal[iMarker][nSpanWiseSections[marker_flag-1]][iDim]*AverageTurboNormal[iMarker][nSpanWiseSections[marker_flag-1]][iDim];
-            Normal2      += AverageNormal[iMarker][nSpanWiseSections[marker_flag-1]][iDim]*AverageNormal[iMarker][nSpanWiseSections[marker_flag-1]][iDim];
+          for (iDim = 0; iDim < nDim; iDim++) {
+            turboNormal2 += AverageTurboNormal[iMarker][nSpanWiseSections[marker_flag - 1]][iDim] *
+                            AverageTurboNormal[iMarker][nSpanWiseSections[marker_flag - 1]][iDim];
+            Normal2 += AverageNormal[iMarker][nSpanWiseSections[marker_flag - 1]][iDim] *
+                       AverageNormal[iMarker][nSpanWiseSections[marker_flag - 1]][iDim];
           }
-          for (iDim = 0; iDim < nDim; iDim++){
-            AverageTurboNormal[iMarker][nSpanWiseSections[marker_flag-1]][iDim] /=sqrt(turboNormal2);
-            AverageNormal[iMarker][nSpanWiseSections[marker_flag-1]][iDim] /=sqrt(Normal2);
+          for (iDim = 0; iDim < nDim; iDim++) {
+            AverageTurboNormal[iMarker][nSpanWiseSections[marker_flag - 1]][iDim] /= sqrt(turboNormal2);
+            AverageNormal[iMarker][nSpanWiseSections[marker_flag - 1]][iDim] /= sqrt(Normal2);
           }
         }
       }
     }
   }
 
-
-  delete [] TotalTurboNormal;
-  delete [] TotalNormal;
-  delete [] TotalGridVel;
-  delete [] TurboNormal;
-  delete [] Normal;
-
+  delete[] TotalTurboNormal;
+  delete[] TotalNormal;
+  delete[] TotalGridVel;
+  delete[] TurboNormal;
+  delete[] Normal;
 }
 
-
-void CPhysicalGeometry::GatherInOutAverageValues(CConfig *config, bool allocate){
-
+void CPhysicalGeometry::GatherInOutAverageValues(CConfig* config, bool allocate) {
   unsigned short iMarker, iMarkerTP;
   unsigned short iSpan, iDim;
   int markerTP;
@@ -6449,97 +6142,92 @@ void CPhysicalGeometry::GatherInOutAverageValues(CConfig *config, bool allocate)
   turboNormal = new su2double[nDim];
   Pitch = 0.0;
 
-  if(allocate){
-    for (iMarkerTP=0; iMarkerTP < config->GetnMarker_TurboPerformance(); iMarkerTP++){
-      SpanAreaIn[iMarkerTP]       = new su2double[config->GetnSpanMaxAllZones() +1];
-      TangGridVelIn[iMarkerTP]    = new su2double[config->GetnSpanMaxAllZones() +1];
-      TurboRadiusIn[iMarkerTP]    = new su2double[config->GetnSpanMaxAllZones() +1];
-      SpanAreaOut[iMarkerTP]      = new su2double[config->GetnSpanMaxAllZones() +1];
-      TangGridVelOut[iMarkerTP]   = new su2double[config->GetnSpanMaxAllZones() +1];
-      TurboRadiusOut[iMarkerTP]   = new su2double[config->GetnSpanMaxAllZones() +1];
+  if (allocate) {
+    for (iMarkerTP = 0; iMarkerTP < config->GetnMarker_TurboPerformance(); iMarkerTP++) {
+      SpanAreaIn[iMarkerTP] = new su2double[config->GetnSpanMaxAllZones() + 1];
+      TangGridVelIn[iMarkerTP] = new su2double[config->GetnSpanMaxAllZones() + 1];
+      TurboRadiusIn[iMarkerTP] = new su2double[config->GetnSpanMaxAllZones() + 1];
+      SpanAreaOut[iMarkerTP] = new su2double[config->GetnSpanMaxAllZones() + 1];
+      TangGridVelOut[iMarkerTP] = new su2double[config->GetnSpanMaxAllZones() + 1];
+      TurboRadiusOut[iMarkerTP] = new su2double[config->GetnSpanMaxAllZones() + 1];
 
-      for (iSpan= 0; iSpan < config->GetnSpanMaxAllZones() + 1 ; iSpan++){
-        SpanAreaIn[iMarkerTP][iSpan]       = 0.0;
-        TangGridVelIn[iMarkerTP][iSpan]    = 0.0;
-        TurboRadiusIn[iMarkerTP][iSpan]    = 0.0;
-        SpanAreaOut[iMarkerTP][iSpan]      = 0.0;
-        TangGridVelOut[iMarkerTP][iSpan]   = 0.0;
-        TurboRadiusOut[iMarkerTP][iSpan]   = 0.0;
+      for (iSpan = 0; iSpan < config->GetnSpanMaxAllZones() + 1; iSpan++) {
+        SpanAreaIn[iMarkerTP][iSpan] = 0.0;
+        TangGridVelIn[iMarkerTP][iSpan] = 0.0;
+        TurboRadiusIn[iMarkerTP][iSpan] = 0.0;
+        SpanAreaOut[iMarkerTP][iSpan] = 0.0;
+        TangGridVelOut[iMarkerTP][iSpan] = 0.0;
+        TurboRadiusOut[iMarkerTP][iSpan] = 0.0;
       }
     }
   }
 
-
-
-  for (iSpan= 0; iSpan < nSpanWiseSections + 1 ; iSpan++){
+  for (iSpan = 0; iSpan < nSpanWiseSections + 1; iSpan++) {
 #ifdef HAVE_MPI
-    unsigned short i, n1, n2, n1t,n2t;
-    su2double *TurbGeoIn= NULL,*TurbGeoOut= NULL;
-    su2double *TotTurbGeoIn = NULL,*TotTurbGeoOut = NULL;
-    int *TotMarkerTP;
-
-    n1          = 6;
-    n2          = 3;
-    n1t         = n1*size;
-    n2t         = n2*size;
-    TurbGeoIn  = new su2double[n1];
+    unsigned short i, n1, n2, n1t, n2t;
+    su2double *TurbGeoIn = NULL, *TurbGeoOut = NULL;
+    su2double *TotTurbGeoIn = NULL, *TotTurbGeoOut = NULL;
+    int* TotMarkerTP;
+
+    n1 = 6;
+    n2 = 3;
+    n1t = n1 * size;
+    n2t = n2 * size;
+    TurbGeoIn = new su2double[n1];
     TurbGeoOut = new su2double[n2];
 
-    for (i=0;i<n1;i++)
-      TurbGeoIn[i]    = -1.0;
-    for (i=0;i<n2;i++)
-      TurbGeoOut[i]   = -1.0;
+    for (i = 0; i < n1; i++) TurbGeoIn[i] = -1.0;
+    for (i = 0; i < n2; i++) TurbGeoOut[i] = -1.0;
 #endif
-    pitchIn           =  0.0;
-    areaIn            = -1.0;
-    tangGridVelIn     = -1.0;
-    radiusIn          = -1.0;
-    for(iDim = 0; iDim < nDim; iDim++){
+    pitchIn = 0.0;
+    areaIn = -1.0;
+    tangGridVelIn = -1.0;
+    radiusIn = -1.0;
+    for (iDim = 0; iDim < nDim; iDim++) {
       turboNormal[iDim] = -1.0;
     }
 
-    areaOut           = -1.0;
-    tangGridVelOut    = -1.0;
-    radiusOut         = -1.0;
+    areaOut = -1.0;
+    tangGridVelOut = -1.0;
+    radiusOut = -1.0;
 
-    markerTP          = -1;
+    markerTP = -1;
 
-    for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++){
-      for (iMarkerTP = 1; iMarkerTP < config->GetnMarker_Turbomachinery()+1; iMarkerTP++){
-        if (config->GetMarker_All_Turbomachinery(iMarker) == iMarkerTP){
-          if (config->GetMarker_All_TurbomachineryFlag(iMarker) == INFLOW){
-            markerTP          = iMarkerTP;
-            if (iSpan < nSpanWiseSections){
-              pitchIn         = MaxAngularCoord[iMarker][iSpan] - MinAngularCoord[iMarker][iSpan];
+    for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
+      for (iMarkerTP = 1; iMarkerTP < config->GetnMarker_Turbomachinery() + 1; iMarkerTP++) {
+        if (config->GetMarker_All_Turbomachinery(iMarker) == iMarkerTP) {
+          if (config->GetMarker_All_TurbomachineryFlag(iMarker) == INFLOW) {
+            markerTP = iMarkerTP;
+            if (iSpan < nSpanWiseSections) {
+              pitchIn = MaxAngularCoord[iMarker][iSpan] - MinAngularCoord[iMarker][iSpan];
             }
-            areaIn            = SpanArea[iMarker][iSpan];
-            tangGridVelIn     = AverageTangGridVel[iMarker][iSpan];
-            radiusIn          = TurboRadius[iMarker][iSpan];
-            for(iDim = 0; iDim < nDim; iDim++) turboNormal[iDim] = AverageTurboNormal[iMarker][iSpan][iDim];
-
+            areaIn = SpanArea[iMarker][iSpan];
+            tangGridVelIn = AverageTangGridVel[iMarker][iSpan];
+            radiusIn = TurboRadius[iMarker][iSpan];
+            for (iDim = 0; iDim < nDim; iDim++) turboNormal[iDim] = AverageTurboNormal[iMarker][iSpan][iDim];
 
 #ifdef HAVE_MPI
-            TurbGeoIn[0]  = areaIn;
-            TurbGeoIn[1]  = tangGridVelIn;
-            TurbGeoIn[2]  = radiusIn;
-            TurbGeoIn[3]  = turboNormal[0];
-            TurbGeoIn[4]  = turboNormal[1];
-            TurbGeoIn[5]  = pitchIn;
+            TurbGeoIn[0] = areaIn;
+            TurbGeoIn[1] = tangGridVelIn;
+            TurbGeoIn[2] = radiusIn;
+            TurbGeoIn[3] = turboNormal[0];
+            TurbGeoIn[4] = turboNormal[1];
+            TurbGeoIn[5] = pitchIn;
 #endif
           }
 
           /*--- retrieve outlet information ---*/
-          if (config->GetMarker_All_TurbomachineryFlag(iMarker) == OUTFLOW){
-            if (iSpan < nSpanWiseSections){
-              pitchIn       = MaxAngularCoord[iMarker][iSpan] - MinAngularCoord[iMarker][iSpan];
+          if (config->GetMarker_All_TurbomachineryFlag(iMarker) == OUTFLOW) {
+            if (iSpan < nSpanWiseSections) {
+              pitchIn = MaxAngularCoord[iMarker][iSpan] - MinAngularCoord[iMarker][iSpan];
             }
-            areaOut         = SpanArea[iMarker][iSpan];
-            tangGridVelOut  = AverageTangGridVel[iMarker][iSpan];
-            radiusOut       = TurboRadius[iMarker][iSpan];
+            areaOut = SpanArea[iMarker][iSpan];
+            tangGridVelOut = AverageTangGridVel[iMarker][iSpan];
+            radiusOut = TurboRadius[iMarker][iSpan];
 #ifdef HAVE_MPI
-            TurbGeoOut[0]  = areaOut;
-            TurbGeoOut[1]  = tangGridVelOut;
-            TurbGeoOut[2]  = radiusOut;
+            TurbGeoOut[0] = areaOut;
+            TurbGeoOut[1] = tangGridVelOut;
+            TurbGeoOut[2] = radiusOut;
 #endif
           }
         }
@@ -6547,89 +6235,83 @@ void CPhysicalGeometry::GatherInOutAverageValues(CConfig *config, bool allocate)
     }
 
 #ifdef HAVE_MPI
-    TotTurbGeoIn       = new su2double[n1t];
-    TotTurbGeoOut      = new su2double[n2t];
-    for (i=0;i<n1t;i++)
-      TotTurbGeoIn[i]  = -1.0;
-    for (i=0;i<n2t;i++)
-      TotTurbGeoOut[i] = -1.0;
+    TotTurbGeoIn = new su2double[n1t];
+    TotTurbGeoOut = new su2double[n2t];
+    for (i = 0; i < n1t; i++) TotTurbGeoIn[i] = -1.0;
+    for (i = 0; i < n2t; i++) TotTurbGeoOut[i] = -1.0;
     TotMarkerTP = new int[size];
-    for(i=0; i<size; i++){
-      TotMarkerTP[i]    = -1;
+    for (i = 0; i < size; i++) {
+      TotMarkerTP[i] = -1;
     }
 
     SU2_MPI::Allgather(TurbGeoIn, n1, MPI_DOUBLE, TotTurbGeoIn, n1, MPI_DOUBLE, SU2_MPI::GetComm());
-    SU2_MPI::Allgather(TurbGeoOut, n2, MPI_DOUBLE,TotTurbGeoOut, n2, MPI_DOUBLE, SU2_MPI::GetComm());
-    SU2_MPI::Allgather(&markerTP, 1, MPI_INT,TotMarkerTP, 1, MPI_INT, SU2_MPI::GetComm());
-
-    delete [] TurbGeoIn, delete [] TurbGeoOut;
+    SU2_MPI::Allgather(TurbGeoOut, n2, MPI_DOUBLE, TotTurbGeoOut, n2, MPI_DOUBLE, SU2_MPI::GetComm());
+    SU2_MPI::Allgather(&markerTP, 1, MPI_INT, TotMarkerTP, 1, MPI_INT, SU2_MPI::GetComm());
 
+    delete[] TurbGeoIn, delete[] TurbGeoOut;
 
-    for (i=0;i<size;i++){
-      if(TotTurbGeoIn[n1*i] > 0.0){
-        areaIn              = 0.0;
-        areaIn              = TotTurbGeoIn[n1*i];
-        tangGridVelIn       = 0.0;
-        tangGridVelIn       = TotTurbGeoIn[n1*i+1];
-        radiusIn            = 0.0;
-        radiusIn            = TotTurbGeoIn[n1*i+2];
-        turboNormal[0]      = 0.0;
-        turboNormal[0]      = TotTurbGeoIn[n1*i+3];
-        turboNormal[1]      = 0.0;
-        turboNormal[1]      = TotTurbGeoIn[n1*i+4];
-        pitchIn             = 0.0;
-        pitchIn             = TotTurbGeoIn[n1*i+5];
+    for (i = 0; i < size; i++) {
+      if (TotTurbGeoIn[n1 * i] > 0.0) {
+        areaIn = 0.0;
+        areaIn = TotTurbGeoIn[n1 * i];
+        tangGridVelIn = 0.0;
+        tangGridVelIn = TotTurbGeoIn[n1 * i + 1];
+        radiusIn = 0.0;
+        radiusIn = TotTurbGeoIn[n1 * i + 2];
+        turboNormal[0] = 0.0;
+        turboNormal[0] = TotTurbGeoIn[n1 * i + 3];
+        turboNormal[1] = 0.0;
+        turboNormal[1] = TotTurbGeoIn[n1 * i + 4];
+        pitchIn = 0.0;
+        pitchIn = TotTurbGeoIn[n1 * i + 5];
 
-        markerTP            = -1;
-        markerTP            = TotMarkerTP[i];
+        markerTP = -1;
+        markerTP = TotMarkerTP[i];
       }
 
-      if(TotTurbGeoOut[n2*i] > 0.0){
-        areaOut             = 0.0;
-        areaOut             = TotTurbGeoOut[n2*i];
-        tangGridVelOut      = 0.0;
-        tangGridVelOut      = TotTurbGeoOut[n2*i+1];
-        radiusOut           = 0.0;
-        radiusOut           = TotTurbGeoOut[n2*i+2];
+      if (TotTurbGeoOut[n2 * i] > 0.0) {
+        areaOut = 0.0;
+        areaOut = TotTurbGeoOut[n2 * i];
+        tangGridVelOut = 0.0;
+        tangGridVelOut = TotTurbGeoOut[n2 * i + 1];
+        radiusOut = 0.0;
+        radiusOut = TotTurbGeoOut[n2 * i + 2];
       }
     }
 
-    delete [] TotTurbGeoIn, delete [] TotTurbGeoOut; delete [] TotMarkerTP;
-
+    delete[] TotTurbGeoIn, delete[] TotTurbGeoOut;
+    delete[] TotMarkerTP;
 
 #endif
 
-    Pitch +=pitchIn/nSpanWiseSections;
+    Pitch += pitchIn / nSpanWiseSections;
 
     if (iSpan == nSpanWiseSections) {
       config->SetFreeStreamTurboNormal(turboNormal);
-      if (config->GetKind_TurboMachinery(config->GetiZone()) == AXIAL && nDim == 2){
-        nBlades = 1/Pitch;
-      }
-      else{
-        nBlades = 2*PI_NUMBER/Pitch;
+      if (config->GetKind_TurboMachinery(config->GetiZone()) == AXIAL && nDim == 2) {
+        nBlades = 1 / Pitch;
+      } else {
+        nBlades = 2 * PI_NUMBER / Pitch;
       }
       config->SetnBlades(config->GetiZone(), nBlades);
     }
 
-    if (rank == MASTER_NODE){
+    if (rank == MASTER_NODE) {
       /*----Quantities needed for computing the turbomachinery performance -----*/
-      SpanAreaIn[markerTP -1][iSpan]       = areaIn;
-      TangGridVelIn[markerTP -1][iSpan]    = tangGridVelIn;
-      TurboRadiusIn[markerTP -1][iSpan]    = radiusIn;
+      SpanAreaIn[markerTP - 1][iSpan] = areaIn;
+      TangGridVelIn[markerTP - 1][iSpan] = tangGridVelIn;
+      TurboRadiusIn[markerTP - 1][iSpan] = radiusIn;
 
-      SpanAreaOut[markerTP -1][iSpan]      = areaOut;
-      TangGridVelOut[markerTP -1][iSpan]   = tangGridVelOut;
-      TurboRadiusOut[markerTP -1][iSpan]   = radiusOut;
+      SpanAreaOut[markerTP - 1][iSpan] = areaOut;
+      TangGridVelOut[markerTP - 1][iSpan] = tangGridVelOut;
+      TurboRadiusOut[markerTP - 1][iSpan] = radiusOut;
     }
   }
-  delete [] turboNormal;
-
+  delete[] turboNormal;
 }
 
 void CPhysicalGeometry::SetMaxLength(CConfig* config) {
-
-  SU2_OMP_FOR_STAT(roundUpDiv(nPointDomain,omp_get_max_threads()))
+  SU2_OMP_FOR_STAT(roundUpDiv(nPointDomain, omp_get_max_threads()))
   for (unsigned long iPoint = 0; iPoint < nPointDomain; iPoint++) {
     const su2double* Coord_i = nodes->GetCoord(iPoint);
 
@@ -6639,13 +6321,12 @@ void CPhysicalGeometry::SetMaxLength(CConfig* config) {
 
     const bool wasActive = AD::BeginPassive();
 
-    su2double max_delta=0;
+    su2double max_delta = 0;
     auto max_neighbor = iPoint;
     for (unsigned short iNeigh = 0; iNeigh < nodes->GetnPoint(iPoint); iNeigh++) {
-
       /*-- Calculate the cell-center to cell-center length ---*/
 
-      const unsigned long jPoint  = nodes->GetPoint(iPoint, iNeigh);
+      const unsigned long jPoint = nodes->GetPoint(iPoint, iNeigh);
       const su2double* Coord_j = nodes->GetCoord(jPoint);
 
       su2double delta = GeometryToolbox::SquaredDistance(nDim, Coord_i, Coord_j);
@@ -6669,19 +6350,17 @@ void CPhysicalGeometry::SetMaxLength(CConfig* config) {
 
   InitiateComms(this, config, MAX_LENGTH);
   CompleteComms(this, config, MAX_LENGTH);
-
 }
 
-void CPhysicalGeometry::MatchActuator_Disk(const CConfig *config) {
-
+void CPhysicalGeometry::MatchActuator_Disk(const CConfig* config) {
   su2double epsilon = 1e-1;
 
   unsigned short nMarker_ActDiskInlet = config->GetnMarker_ActDiskInlet();
 
   if (nMarker_ActDiskInlet != 0) {
-
     unsigned short iMarker, iDim;
-    unsigned long iVertex, iPoint, iPointGlobal, pPoint = 0, pPointGlobal = 0, pVertex = 0, pMarker = 0, jVertex, jVertex_, jPoint, jPointGlobal, jMarker;
+    unsigned long iVertex, iPoint, iPointGlobal, pPoint = 0, pPointGlobal = 0, pVertex = 0, pMarker = 0, jVertex,
+                                                 jVertex_, jPoint, jPointGlobal, jMarker;
     su2double *Coord_i, Coord_j[3], dist = 0.0, mindist, maxdist_local = 0.0, maxdist_global = 0.0;
     int iProcessor, pProcessor = 0;
     unsigned long nLocalVertex_ActDisk = 0, MaxLocalVertex_ActDisk = 0;
@@ -6690,12 +6369,17 @@ void CPhysicalGeometry::MatchActuator_Disk(const CConfig *config) {
     bool Perimeter;
 
     for (iBC = 0; iBC < 2; iBC++) {
+      if (iBC == 0) {
+        Beneficiary = ACTDISK_INLET;
+        Donor = ACTDISK_OUTLET;
+      }
+      if (iBC == 1) {
+        Beneficiary = ACTDISK_OUTLET;
+        Donor = ACTDISK_INLET;
+      }
 
-      if (iBC == 0) { Beneficiary = ACTDISK_INLET; Donor = ACTDISK_OUTLET; }
-      if (iBC == 1) { Beneficiary = ACTDISK_OUTLET; Donor = ACTDISK_INLET; }
-
-      unsigned long *Buffer_Send_nVertex = new unsigned long [1];
-      unsigned long *Buffer_Receive_nVertex = new unsigned long [nProcessor];
+      unsigned long* Buffer_Send_nVertex = new unsigned long[1];
+      unsigned long* Buffer_Receive_nVertex = new unsigned long[nProcessor];
 
       if ((iBC == 0) && (rank == MASTER_NODE)) cout << "Set Actuator Disk inlet boundary conditions." << endl;
       if ((iBC == 1) && (rank == MASTER_NODE)) cout << "Set Actuator Disk outlet boundary conditions." << endl;
@@ -6708,7 +6392,7 @@ void CPhysicalGeometry::MatchActuator_Disk(const CConfig *config) {
         if (config->GetMarker_All_KindBC(iMarker) == Donor) {
           for (iVertex = 0; iVertex < GetnVertex(iMarker); iVertex++) {
             iPoint = vertex[iMarker][iVertex]->GetNode();
-            if (nodes->GetDomain(iPoint)) nLocalVertex_ActDisk ++;
+            if (nodes->GetDomain(iPoint)) nLocalVertex_ActDisk++;
           }
         }
       }
@@ -6717,24 +6401,26 @@ void CPhysicalGeometry::MatchActuator_Disk(const CConfig *config) {
 
       /*--- Send actuator disk vertex information --*/
 
-      SU2_MPI::Allreduce(&nLocalVertex_ActDisk, &MaxLocalVertex_ActDisk, 1, MPI_UNSIGNED_LONG, MPI_MAX, SU2_MPI::GetComm());
-      SU2_MPI::Allgather(Buffer_Send_nVertex, 1, MPI_UNSIGNED_LONG, Buffer_Receive_nVertex, 1, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
+      SU2_MPI::Allreduce(&nLocalVertex_ActDisk, &MaxLocalVertex_ActDisk, 1, MPI_UNSIGNED_LONG, MPI_MAX,
+                         SU2_MPI::GetComm());
+      SU2_MPI::Allgather(Buffer_Send_nVertex, 1, MPI_UNSIGNED_LONG, Buffer_Receive_nVertex, 1, MPI_UNSIGNED_LONG,
+                         SU2_MPI::GetComm());
 
       /*--- Array dimensionalization --*/
 
-      su2double *Buffer_Send_Coord = new su2double [MaxLocalVertex_ActDisk*nDim];
-      unsigned long *Buffer_Send_Point  = new unsigned long [MaxLocalVertex_ActDisk];
-      unsigned long *Buffer_Send_GlobalIndex  = new unsigned long [MaxLocalVertex_ActDisk];
-      unsigned long *Buffer_Send_Vertex  = new unsigned long [MaxLocalVertex_ActDisk];
-      unsigned long *Buffer_Send_Marker  = new unsigned long [MaxLocalVertex_ActDisk];
+      su2double* Buffer_Send_Coord = new su2double[MaxLocalVertex_ActDisk * nDim];
+      unsigned long* Buffer_Send_Point = new unsigned long[MaxLocalVertex_ActDisk];
+      unsigned long* Buffer_Send_GlobalIndex = new unsigned long[MaxLocalVertex_ActDisk];
+      unsigned long* Buffer_Send_Vertex = new unsigned long[MaxLocalVertex_ActDisk];
+      unsigned long* Buffer_Send_Marker = new unsigned long[MaxLocalVertex_ActDisk];
 
-      su2double *Buffer_Receive_Coord = new su2double [nProcessor*MaxLocalVertex_ActDisk*nDim];
-      unsigned long *Buffer_Receive_Point = new unsigned long [nProcessor*MaxLocalVertex_ActDisk];
-      unsigned long *Buffer_Receive_GlobalIndex = new unsigned long [nProcessor*MaxLocalVertex_ActDisk];
-      unsigned long *Buffer_Receive_Vertex = new unsigned long [nProcessor*MaxLocalVertex_ActDisk];
-      unsigned long *Buffer_Receive_Marker = new unsigned long [nProcessor*MaxLocalVertex_ActDisk];
+      su2double* Buffer_Receive_Coord = new su2double[nProcessor * MaxLocalVertex_ActDisk * nDim];
+      unsigned long* Buffer_Receive_Point = new unsigned long[nProcessor * MaxLocalVertex_ActDisk];
+      unsigned long* Buffer_Receive_GlobalIndex = new unsigned long[nProcessor * MaxLocalVertex_ActDisk];
+      unsigned long* Buffer_Receive_Vertex = new unsigned long[nProcessor * MaxLocalVertex_ActDisk];
+      unsigned long* Buffer_Receive_Marker = new unsigned long[nProcessor * MaxLocalVertex_ActDisk];
 
-      unsigned long nBuffer_Coord = MaxLocalVertex_ActDisk*nDim;
+      unsigned long nBuffer_Coord = MaxLocalVertex_ActDisk * nDim;
       unsigned long nBuffer_Point = MaxLocalVertex_ActDisk;
       unsigned long nBuffer_GlobalIndex = MaxLocalVertex_ActDisk;
       unsigned long nBuffer_Vertex = MaxLocalVertex_ActDisk;
@@ -6745,8 +6431,7 @@ void CPhysicalGeometry::MatchActuator_Disk(const CConfig *config) {
         Buffer_Send_GlobalIndex[iVertex] = 0;
         Buffer_Send_Vertex[iVertex] = 0;
         Buffer_Send_Marker[iVertex] = 0;
-        for (iDim = 0; iDim < nDim; iDim++)
-          Buffer_Send_Coord[iVertex*nDim+iDim] = 0.0;
+        for (iDim = 0; iDim < nDim; iDim++) Buffer_Send_Coord[iVertex * nDim + iDim] = 0.0;
       }
 
       /*--- Copy coordinates and point to the auxiliar vector --*/
@@ -6763,18 +6448,23 @@ void CPhysicalGeometry::MatchActuator_Disk(const CConfig *config) {
               Buffer_Send_Vertex[nLocalVertex_ActDisk] = iVertex;
               Buffer_Send_Marker[nLocalVertex_ActDisk] = iMarker;
               for (iDim = 0; iDim < nDim; iDim++)
-                Buffer_Send_Coord[nLocalVertex_ActDisk*nDim+iDim] = nodes->GetCoord(iPoint, iDim);
+                Buffer_Send_Coord[nLocalVertex_ActDisk * nDim + iDim] = nodes->GetCoord(iPoint, iDim);
               nLocalVertex_ActDisk++;
             }
           }
         }
       }
 
-      SU2_MPI::Allgather(Buffer_Send_Coord, nBuffer_Coord, MPI_DOUBLE, Buffer_Receive_Coord, nBuffer_Coord, MPI_DOUBLE, SU2_MPI::GetComm());
-      SU2_MPI::Allgather(Buffer_Send_Point, nBuffer_Point, MPI_UNSIGNED_LONG, Buffer_Receive_Point, nBuffer_Point, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
-      SU2_MPI::Allgather(Buffer_Send_GlobalIndex, nBuffer_GlobalIndex, MPI_UNSIGNED_LONG, Buffer_Receive_GlobalIndex, nBuffer_GlobalIndex, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
-      SU2_MPI::Allgather(Buffer_Send_Vertex, nBuffer_Vertex, MPI_UNSIGNED_LONG, Buffer_Receive_Vertex, nBuffer_Vertex, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
-      SU2_MPI::Allgather(Buffer_Send_Marker, nBuffer_Marker, MPI_UNSIGNED_LONG, Buffer_Receive_Marker, nBuffer_Marker, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
+      SU2_MPI::Allgather(Buffer_Send_Coord, nBuffer_Coord, MPI_DOUBLE, Buffer_Receive_Coord, nBuffer_Coord, MPI_DOUBLE,
+                         SU2_MPI::GetComm());
+      SU2_MPI::Allgather(Buffer_Send_Point, nBuffer_Point, MPI_UNSIGNED_LONG, Buffer_Receive_Point, nBuffer_Point,
+                         MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
+      SU2_MPI::Allgather(Buffer_Send_GlobalIndex, nBuffer_GlobalIndex, MPI_UNSIGNED_LONG, Buffer_Receive_GlobalIndex,
+                         nBuffer_GlobalIndex, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
+      SU2_MPI::Allgather(Buffer_Send_Vertex, nBuffer_Vertex, MPI_UNSIGNED_LONG, Buffer_Receive_Vertex, nBuffer_Vertex,
+                         MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
+      SU2_MPI::Allgather(Buffer_Send_Marker, nBuffer_Marker, MPI_UNSIGNED_LONG, Buffer_Receive_Marker, nBuffer_Marker,
+                         MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
 
       /*--- Compute the closest point to an actuator disk inlet point ---*/
 
@@ -6782,17 +6472,17 @@ void CPhysicalGeometry::MatchActuator_Disk(const CConfig *config) {
 
       for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
         if (config->GetMarker_All_KindBC(iMarker) == Beneficiary) {
-
           for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
             iPoint = vertex[iMarker][iVertex]->GetNode();
             iPointGlobal = nodes->GetGlobalIndex(iPoint);
 
-
             if (nodes->GetDomain(iPoint)) {
-
               /*--- Coordinates of the boundary point ---*/
 
-              Coord_i = nodes->GetCoord(iPoint); mindist = 1E6; pProcessor = 0; pPoint = 0;
+              Coord_i = nodes->GetCoord(iPoint);
+              mindist = 1E6;
+              pProcessor = 0;
+              pPoint = 0;
 
               /*--- Loop over all the boundaries to find the pair ---*/
 
@@ -6800,32 +6490,36 @@ void CPhysicalGeometry::MatchActuator_Disk(const CConfig *config) {
 
               for (iProcessor = 0; iProcessor < nProcessor; iProcessor++) {
                 for (jVertex = 0; jVertex < Buffer_Receive_nVertex[iProcessor]; jVertex++) {
-                  jPoint = Buffer_Receive_Point[iProcessor*MaxLocalVertex_ActDisk+jVertex];
-                  jPointGlobal = Buffer_Receive_GlobalIndex[iProcessor*MaxLocalVertex_ActDisk+jVertex];
-                  jVertex_ = Buffer_Receive_Vertex[iProcessor*MaxLocalVertex_ActDisk+jVertex];
-                  jMarker = Buffer_Receive_Marker[iProcessor*MaxLocalVertex_ActDisk+jVertex];
+                  jPoint = Buffer_Receive_Point[iProcessor * MaxLocalVertex_ActDisk + jVertex];
+                  jPointGlobal = Buffer_Receive_GlobalIndex[iProcessor * MaxLocalVertex_ActDisk + jVertex];
+                  jVertex_ = Buffer_Receive_Vertex[iProcessor * MaxLocalVertex_ActDisk + jVertex];
+                  jMarker = Buffer_Receive_Marker[iProcessor * MaxLocalVertex_ActDisk + jVertex];
 
- //                 if (jPointGlobal != iPointGlobal) {
- //                 ActDisk_Perimeter
+                  //                 if (jPointGlobal != iPointGlobal) {
+                  //                 ActDisk_Perimeter
 
-                    /*--- Compute the distance ---*/
+                  /*--- Compute the distance ---*/
 
-                    dist = 0.0;
-                    for (iDim = 0; iDim < nDim; iDim++) {
-                      Coord_j[iDim] = Buffer_Receive_Coord[(iProcessor*MaxLocalVertex_ActDisk+jVertex)*nDim+iDim];
-                      dist += pow(Coord_j[iDim]-Coord_i[iDim], 2.0);
-                    }
-                    dist = sqrt(dist);
-
-                    if (dist < mindist) {
-                      mindist = dist; pProcessor = iProcessor; pPoint = jPoint; pPointGlobal = jPointGlobal;
-                      pVertex = jVertex_; pMarker = jMarker;
-                      if (dist == 0.0) break;
-                    }
+                  dist = 0.0;
+                  for (iDim = 0; iDim < nDim; iDim++) {
+                    Coord_j[iDim] = Buffer_Receive_Coord[(iProcessor * MaxLocalVertex_ActDisk + jVertex) * nDim + iDim];
+                    dist += pow(Coord_j[iDim] - Coord_i[iDim], 2.0);
+                  }
+                  dist = sqrt(dist);
+
+                  if (dist < mindist) {
+                    mindist = dist;
+                    pProcessor = iProcessor;
+                    pPoint = jPoint;
+                    pPointGlobal = jPointGlobal;
+                    pVertex = jVertex_;
+                    pMarker = jMarker;
+                    if (dist == 0.0) break;
+                  }
 
-//                  }
-//                  else { Perimeter = true; mindist = 0.0; dist = 0.0; break; }
-               }
+                  //                  }
+                  //                  else { Perimeter = true; mindist = 0.0; dist = 0.0; break; }
+                }
               }
 
               /*--- Store the value of the pair ---*/
@@ -6842,16 +6536,14 @@ void CPhysicalGeometry::MatchActuator_Disk(const CConfig *config) {
                 vertex[iMarker][iVertex]->SetDonorPoint(iPoint, iPointGlobal, pVertex, pMarker, pProcessor);
                 maxdist_local = min(maxdist_local, 0.0);
               }
-
             }
           }
-
         }
       }
 
       SU2_MPI::Reduce(&maxdist_local, &maxdist_global, 1, MPI_DOUBLE, MPI_MAX, MASTER_NODE, SU2_MPI::GetComm());
 
-      if (rank == MASTER_NODE) cout <<"The max distance between points is: " << maxdist_global <<"."<< endl;
+      if (rank == MASTER_NODE) cout << "The max distance between points is: " << maxdist_global << "." << endl;
 
       delete[] Buffer_Send_Coord;
       delete[] Buffer_Send_Point;
@@ -6862,22 +6554,18 @@ void CPhysicalGeometry::MatchActuator_Disk(const CConfig *config) {
       delete[] Buffer_Send_nVertex;
       delete[] Buffer_Receive_nVertex;
 
-      delete [] Buffer_Send_GlobalIndex;
-      delete [] Buffer_Send_Vertex;
-      delete [] Buffer_Send_Marker;
-
-      delete [] Buffer_Receive_GlobalIndex;
-      delete [] Buffer_Receive_Vertex;
-      delete [] Buffer_Receive_Marker;
+      delete[] Buffer_Send_GlobalIndex;
+      delete[] Buffer_Send_Vertex;
+      delete[] Buffer_Send_Marker;
 
+      delete[] Buffer_Receive_GlobalIndex;
+      delete[] Buffer_Receive_Vertex;
+      delete[] Buffer_Receive_Marker;
     }
   }
-
 }
 
-void CPhysicalGeometry::MatchPeriodic(const CConfig *config,
-                                      unsigned short val_periodic) {
-
+void CPhysicalGeometry::MatchPeriodic(const CConfig* config, unsigned short val_periodic) {
   unsigned short iMarker, iDim, jMarker, pMarker = 0;
   unsigned short iPeriodic, nPeriodic;
 
@@ -6895,8 +6583,8 @@ void CPhysicalGeometry::MatchPeriodic(const CConfig *config,
 
   su2double *Coord_i, Coord_j[3], dist, mindist, maxdist_local, maxdist_global;
   const su2double *center, *angles, *trans;
-  su2double translation[3]={0.0,0.0,0.0}, dx, dy, dz;
-  su2double rotMatrix[3][3] = {{1.0,0.0,0.0},{0.0,1.0,0.0},{0.0,0.0,1.0}};
+  su2double translation[3] = {0.0, 0.0, 0.0}, dx, dy, dz;
+  su2double rotMatrix[3][3] = {{1.0, 0.0, 0.0}, {0.0, 1.0, 0.0}, {0.0, 0.0, 1.0}};
   su2double Theta, Phi, Psi, cosTheta, sinTheta, cosPhi, sinPhi, cosPsi, sinPsi;
   su2double rotCoord[3] = {0.0, 0.0, 0.0};
 
@@ -6928,8 +6616,7 @@ void CPhysicalGeometry::MatchPeriodic(const CConfig *config,
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
     if (config->GetMarker_All_KindBC(iMarker) == PERIODIC_BOUNDARY) {
       iPeriodic = config->GetMarker_All_PerBound(iMarker);
-      if ((iPeriodic == val_periodic) ||
-          (iPeriodic == val_periodic + nPeriodic/2)) {
+      if ((iPeriodic == val_periodic) || (iPeriodic == val_periodic + nPeriodic / 2)) {
         for (iVertex = 0; iVertex < GetnVertex(iMarker); iVertex++) {
           iPoint = vertex[iMarker][iVertex]->GetNode();
           if (nodes->GetDomain(iPoint)) nLocalVertex_Periodic++;
@@ -6941,46 +6628,45 @@ void CPhysicalGeometry::MatchPeriodic(const CConfig *config,
   /*--- Communicate our local periodic point count globally
    and receive the counts of periodic points from all other ranks.---*/
 
-  unsigned long *Buffer_Send_nVertex = new unsigned long [1];
-  unsigned long *Buffer_Recv_nVertex = new unsigned long [nProcessor];
+  unsigned long* Buffer_Send_nVertex = new unsigned long[1];
+  unsigned long* Buffer_Recv_nVertex = new unsigned long[nProcessor];
 
   Buffer_Send_nVertex[0] = nLocalVertex_Periodic;
 
   /*--- Copy our own count in serial or use collective comms with MPI. ---*/
 
-  SU2_MPI::Allreduce(&nLocalVertex_Periodic, &MaxLocalVertex_Periodic, 1,
-                     MPI_UNSIGNED_LONG, MPI_MAX, SU2_MPI::GetComm());
-  SU2_MPI::Allgather(Buffer_Send_nVertex, 1, MPI_UNSIGNED_LONG,
-                     Buffer_Recv_nVertex, 1, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&nLocalVertex_Periodic, &MaxLocalVertex_Periodic, 1, MPI_UNSIGNED_LONG, MPI_MAX,
+                     SU2_MPI::GetComm());
+  SU2_MPI::Allgather(Buffer_Send_nVertex, 1, MPI_UNSIGNED_LONG, Buffer_Recv_nVertex, 1, MPI_UNSIGNED_LONG,
+                     SU2_MPI::GetComm());
 
   /*--- Prepare buffers to send the information for each
    periodic point to all ranks so that we can match pairs. ---*/
 
-  su2double *Buffer_Send_Coord           = new su2double [MaxLocalVertex_Periodic*nDim];
-  unsigned long *Buffer_Send_Point       = new unsigned long [MaxLocalVertex_Periodic];
-  unsigned long *Buffer_Send_GlobalIndex = new unsigned long [MaxLocalVertex_Periodic];
-  unsigned long *Buffer_Send_Vertex      = new unsigned long [MaxLocalVertex_Periodic];
-  unsigned long *Buffer_Send_Marker      = new unsigned long [MaxLocalVertex_Periodic];
+  su2double* Buffer_Send_Coord = new su2double[MaxLocalVertex_Periodic * nDim];
+  unsigned long* Buffer_Send_Point = new unsigned long[MaxLocalVertex_Periodic];
+  unsigned long* Buffer_Send_GlobalIndex = new unsigned long[MaxLocalVertex_Periodic];
+  unsigned long* Buffer_Send_Vertex = new unsigned long[MaxLocalVertex_Periodic];
+  unsigned long* Buffer_Send_Marker = new unsigned long[MaxLocalVertex_Periodic];
 
-  su2double *Buffer_Recv_Coord           = new su2double [nProcessor*MaxLocalVertex_Periodic*nDim];
-  unsigned long *Buffer_Recv_Point       = new unsigned long [nProcessor*MaxLocalVertex_Periodic];
-  unsigned long *Buffer_Recv_GlobalIndex = new unsigned long [nProcessor*MaxLocalVertex_Periodic];
-  unsigned long *Buffer_Recv_Vertex      = new unsigned long [nProcessor*MaxLocalVertex_Periodic];
-  unsigned long *Buffer_Recv_Marker      = new unsigned long [nProcessor*MaxLocalVertex_Periodic];
+  su2double* Buffer_Recv_Coord = new su2double[nProcessor * MaxLocalVertex_Periodic * nDim];
+  unsigned long* Buffer_Recv_Point = new unsigned long[nProcessor * MaxLocalVertex_Periodic];
+  unsigned long* Buffer_Recv_GlobalIndex = new unsigned long[nProcessor * MaxLocalVertex_Periodic];
+  unsigned long* Buffer_Recv_Vertex = new unsigned long[nProcessor * MaxLocalVertex_Periodic];
+  unsigned long* Buffer_Recv_Marker = new unsigned long[nProcessor * MaxLocalVertex_Periodic];
 
-  unsigned long nBuffer_Coord       = MaxLocalVertex_Periodic*nDim;
-  unsigned long nBuffer_Point       = MaxLocalVertex_Periodic;
+  unsigned long nBuffer_Coord = MaxLocalVertex_Periodic * nDim;
+  unsigned long nBuffer_Point = MaxLocalVertex_Periodic;
   unsigned long nBuffer_GlobalIndex = MaxLocalVertex_Periodic;
-  unsigned long nBuffer_Vertex      = MaxLocalVertex_Periodic;
-  unsigned long nBuffer_Marker      = MaxLocalVertex_Periodic;
+  unsigned long nBuffer_Vertex = MaxLocalVertex_Periodic;
+  unsigned long nBuffer_Marker = MaxLocalVertex_Periodic;
 
   for (iVertex = 0; iVertex < MaxLocalVertex_Periodic; iVertex++) {
-    Buffer_Send_Point[iVertex]       = 0;
+    Buffer_Send_Point[iVertex] = 0;
     Buffer_Send_GlobalIndex[iVertex] = 0;
-    Buffer_Send_Vertex[iVertex]      = 0;
-    Buffer_Send_Marker[iVertex]      = 0;
-    for (iDim = 0; iDim < nDim; iDim++)
-    Buffer_Send_Coord[iVertex*nDim+iDim] = 0.0;
+    Buffer_Send_Vertex[iVertex] = 0;
+    Buffer_Send_Marker[iVertex] = 0;
+    for (iDim = 0; iDim < nDim; iDim++) Buffer_Send_Coord[iVertex * nDim + iDim] = 0.0;
   }
 
   /*--- Store the local index, global index, local boundary index,
@@ -6992,8 +6678,7 @@ void CPhysicalGeometry::MatchPeriodic(const CConfig *config,
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
     if (config->GetMarker_All_KindBC(iMarker) == PERIODIC_BOUNDARY) {
       iPeriodic = config->GetMarker_All_PerBound(iMarker);
-      if ((iPeriodic == val_periodic) ||
-          (iPeriodic == val_periodic + nPeriodic/2)) {
+      if ((iPeriodic == val_periodic) || (iPeriodic == val_periodic + nPeriodic / 2)) {
         for (iVertex = 0; iVertex < GetnVertex(iMarker); iVertex++) {
           iPoint = vertex[iMarker][iVertex]->GetNode();
           iPointGlobal = nodes->GetGlobalIndex(iPoint);
@@ -7003,7 +6688,7 @@ void CPhysicalGeometry::MatchPeriodic(const CConfig *config,
             Buffer_Send_Vertex[nLocalVertex_Periodic] = iVertex;
             Buffer_Send_Marker[nLocalVertex_Periodic] = iMarker;
             for (iDim = 0; iDim < nDim; iDim++)
-            Buffer_Send_Coord[nLocalVertex_Periodic*nDim+iDim] = nodes->GetCoord(iPoint, iDim);
+              Buffer_Send_Coord[nLocalVertex_Periodic * nDim + iDim] = nodes->GetCoord(iPoint, iDim);
             nLocalVertex_Periodic++;
           }
         }
@@ -7017,16 +6702,16 @@ void CPhysicalGeometry::MatchPeriodic(const CConfig *config,
    and we are only storing one periodic marker pair at a time,
    repeating the data for each pair on all ranks should be manageable. ---*/
 
-  SU2_MPI::Allgather(Buffer_Send_Coord, nBuffer_Coord, MPI_DOUBLE,
-                     Buffer_Recv_Coord, nBuffer_Coord, MPI_DOUBLE, SU2_MPI::GetComm());
-  SU2_MPI::Allgather(Buffer_Send_Point, nBuffer_Point, MPI_UNSIGNED_LONG,
-                     Buffer_Recv_Point, nBuffer_Point, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
-  SU2_MPI::Allgather(Buffer_Send_GlobalIndex, nBuffer_GlobalIndex, MPI_UNSIGNED_LONG,
-                     Buffer_Recv_GlobalIndex, nBuffer_GlobalIndex, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
-  SU2_MPI::Allgather(Buffer_Send_Vertex, nBuffer_Vertex, MPI_UNSIGNED_LONG,
-                     Buffer_Recv_Vertex, nBuffer_Vertex, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
-  SU2_MPI::Allgather(Buffer_Send_Marker, nBuffer_Marker, MPI_UNSIGNED_LONG,
-                     Buffer_Recv_Marker, nBuffer_Marker, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
+  SU2_MPI::Allgather(Buffer_Send_Coord, nBuffer_Coord, MPI_DOUBLE, Buffer_Recv_Coord, nBuffer_Coord, MPI_DOUBLE,
+                     SU2_MPI::GetComm());
+  SU2_MPI::Allgather(Buffer_Send_Point, nBuffer_Point, MPI_UNSIGNED_LONG, Buffer_Recv_Point, nBuffer_Point,
+                     MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
+  SU2_MPI::Allgather(Buffer_Send_GlobalIndex, nBuffer_GlobalIndex, MPI_UNSIGNED_LONG, Buffer_Recv_GlobalIndex,
+                     nBuffer_GlobalIndex, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
+  SU2_MPI::Allgather(Buffer_Send_Vertex, nBuffer_Vertex, MPI_UNSIGNED_LONG, Buffer_Recv_Vertex, nBuffer_Vertex,
+                     MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
+  SU2_MPI::Allgather(Buffer_Send_Marker, nBuffer_Marker, MPI_UNSIGNED_LONG, Buffer_Recv_Marker, nBuffer_Marker,
+                     MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
 
   /*--- Now that all ranks have the data for all periodic points for
    this pair of periodic markers, we match the individual points
@@ -7035,17 +6720,14 @@ void CPhysicalGeometry::MatchPeriodic(const CConfig *config,
   maxdist_local = 0.0;
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
     if (config->GetMarker_All_KindBC(iMarker) == PERIODIC_BOUNDARY) {
-
       iPeriodic = config->GetMarker_All_PerBound(iMarker);
-      if ((iPeriodic == val_periodic) ||
-          (iPeriodic == val_periodic + nPeriodic/2)) {
-
+      if ((iPeriodic == val_periodic) || (iPeriodic == val_periodic + nPeriodic / 2)) {
         /*--- Retrieve the supplied periodic information. ---*/
 
         Marker_Tag = config->GetMarker_All_TagBound(iMarker);
-        center     = config->GetPeriodicRotCenter(Marker_Tag);
-        angles     = config->GetPeriodicRotAngles(Marker_Tag);
-        trans      = config->GetPeriodicTranslation(Marker_Tag);
+        center = config->GetPeriodicRotCenter(Marker_Tag);
+        angles = config->GetPeriodicRotAngles(Marker_Tag);
+        trans = config->GetPeriodicTranslation(Marker_Tag);
 
         /*--- Store (center+trans) as it is constant and will be added. ---*/
 
@@ -7055,39 +6737,43 @@ void CPhysicalGeometry::MatchPeriodic(const CConfig *config,
 
         /*--- Store angles separately for clarity. Compute sines/cosines. ---*/
 
-        Theta    = angles[0];      Phi = angles[1];     Psi = angles[2];
-        cosTheta = cos(Theta);  cosPhi = cos(Phi);   cosPsi = cos(Psi);
-        sinTheta = sin(Theta);  sinPhi = sin(Phi);   sinPsi = sin(Psi);
+        Theta = angles[0];
+        Phi = angles[1];
+        Psi = angles[2];
+        cosTheta = cos(Theta);
+        cosPhi = cos(Phi);
+        cosPsi = cos(Psi);
+        sinTheta = sin(Theta);
+        sinPhi = sin(Phi);
+        sinPsi = sin(Psi);
 
         /*--- Compute the rotation matrix. Note that the implicit
          ordering is rotation about the x-axis, y-axis, then z-axis. ---*/
 
-        rotMatrix[0][0] = cosPhi*cosPsi;
-        rotMatrix[1][0] = cosPhi*sinPsi;
+        rotMatrix[0][0] = cosPhi * cosPsi;
+        rotMatrix[1][0] = cosPhi * sinPsi;
         rotMatrix[2][0] = -sinPhi;
 
-        rotMatrix[0][1] = sinTheta*sinPhi*cosPsi - cosTheta*sinPsi;
-        rotMatrix[1][1] = sinTheta*sinPhi*sinPsi + cosTheta*cosPsi;
-        rotMatrix[2][1] = sinTheta*cosPhi;
+        rotMatrix[0][1] = sinTheta * sinPhi * cosPsi - cosTheta * sinPsi;
+        rotMatrix[1][1] = sinTheta * sinPhi * sinPsi + cosTheta * cosPsi;
+        rotMatrix[2][1] = sinTheta * cosPhi;
 
-        rotMatrix[0][2] = cosTheta*sinPhi*cosPsi + sinTheta*sinPsi;
-        rotMatrix[1][2] = cosTheta*sinPhi*sinPsi - sinTheta*cosPsi;
-        rotMatrix[2][2] = cosTheta*cosPhi;
+        rotMatrix[0][2] = cosTheta * sinPhi * cosPsi + sinTheta * sinPsi;
+        rotMatrix[1][2] = cosTheta * sinPhi * sinPsi - sinTheta * cosPsi;
+        rotMatrix[2][2] = cosTheta * cosPhi;
 
         /*--- Loop over each point on the periodic marker that this rank
          holds locally and find the matching point from the donor marker. ---*/
 
         for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
-
           /*--- Local and global index for the owned periodic point. ---*/
 
-          iPoint       = vertex[iMarker][iVertex]->GetNode();
+          iPoint = vertex[iMarker][iVertex]->GetNode();
           iPointGlobal = nodes->GetGlobalIndex(iPoint);
 
           /*--- If this is not a ghost, find the periodic match. ---*/
 
           if (nodes->GetDomain(iPoint)) {
-
             /*--- Coordinates of the current boundary point ---*/
 
             Coord_i = nodes->GetCoord(iPoint);
@@ -7096,22 +6782,18 @@ void CPhysicalGeometry::MatchPeriodic(const CConfig *config,
 
             dx = Coord_i[0] - center[0];
             dy = Coord_i[1] - center[1];
-            if (nDim == 3) dz = Coord_i[2] - center[2];
-            else           dz = 0.0;
+            if (nDim == 3)
+              dz = Coord_i[2] - center[2];
+            else
+              dz = 0.0;
 
             /*--- Compute transformed point coordinates. ---*/
 
-            rotCoord[0] = (rotMatrix[0][0]*dx +
-                           rotMatrix[0][1]*dy +
-                           rotMatrix[0][2]*dz + translation[0]);
+            rotCoord[0] = (rotMatrix[0][0] * dx + rotMatrix[0][1] * dy + rotMatrix[0][2] * dz + translation[0]);
 
-            rotCoord[1] = (rotMatrix[1][0]*dx +
-                           rotMatrix[1][1]*dy +
-                           rotMatrix[1][2]*dz + translation[1]);
+            rotCoord[1] = (rotMatrix[1][0] * dx + rotMatrix[1][1] * dy + rotMatrix[1][2] * dz + translation[1]);
 
-            rotCoord[2] = (rotMatrix[2][0]*dx +
-                           rotMatrix[2][1]*dy +
-                           rotMatrix[2][2]*dz + translation[2]);
+            rotCoord[2] = (rotMatrix[2][0] * dx + rotMatrix[2][1] * dy + rotMatrix[2][2] * dz + translation[2]);
 
             /*--- Check if the point lies on the axis of rotation. If it does,
              the rotated coordinate and the original coordinate are the same. ---*/
@@ -7119,7 +6801,7 @@ void CPhysicalGeometry::MatchPeriodic(const CConfig *config,
             pointOnAxis = false;
             distToAxis = 0.0;
             for (iDim = 0; iDim < nDim; iDim++)
-               distToAxis = (rotCoord[iDim] - Coord_i[iDim])*(rotCoord[iDim] - Coord_i[iDim]);
+              distToAxis = (rotCoord[iDim] - Coord_i[iDim]) * (rotCoord[iDim] - Coord_i[iDim]);
             distToAxis = sqrt(distToAxis);
 
             if (distToAxis < epsilon) pointOnAxis = true;
@@ -7127,70 +6809,66 @@ void CPhysicalGeometry::MatchPeriodic(const CConfig *config,
             /*--- Our search is based on the minimum distance, so we
              initialize the distance to a large value. ---*/
 
-            mindist = 1E6; pProcessor = 0; pPoint = 0;
+            mindist = 1E6;
+            pProcessor = 0;
+            pPoint = 0;
 
             /*--- Loop over all of the periodic data that was gathered from
              all ranks in order to find the matching periodic point. ---*/
 
             for (iProcessor = 0; iProcessor < nProcessor; iProcessor++)
-            for (jVertex = 0; jVertex < Buffer_Recv_nVertex[iProcessor]; jVertex++) {
+              for (jVertex = 0; jVertex < Buffer_Recv_nVertex[iProcessor]; jVertex++) {
+                /*--- Store the loop index more easily. ---*/
 
-              /*--- Store the loop index more easily. ---*/
+                index = iProcessor * MaxLocalVertex_Periodic + jVertex;
 
-              index = iProcessor*MaxLocalVertex_Periodic + jVertex;
+                /*--- For each candidate, we have the local and global index,
+                 along with the boundary vertex and marker index. ---*/
 
-              /*--- For each candidate, we have the local and global index,
-               along with the boundary vertex and marker index. ---*/
+                jPoint = Buffer_Recv_Point[index];
+                jPointGlobal = Buffer_Recv_GlobalIndex[index];
+                jVertex_ = Buffer_Recv_Vertex[index];
+                jMarker = Buffer_Recv_Marker[index];
 
-              jPoint       = Buffer_Recv_Point[index];
-              jPointGlobal = Buffer_Recv_GlobalIndex[index];
-              jVertex_     = Buffer_Recv_Vertex[index];
-              jMarker      = Buffer_Recv_Marker[index];
+                /*--- The gathered data will also include the current
+                 "owned" periodic point that we are matching, so first make
+                 sure that we avoid the original point by checking that the
+                 global index values are not the same. ---*/
 
-              /*--- The gathered data will also include the current
-               "owned" periodic point that we are matching, so first make
-               sure that we avoid the original point by checking that the
-               global index values are not the same. ---*/
-
-              if ((jPointGlobal != iPointGlobal) || (pointOnAxis)) {
-
-                /*--- Compute the distance between the candidate periodic
-                 point and the transformed coordinates of the owned point. ---*/
-
-                dist = 0.0;
-                for (iDim = 0; iDim < nDim; iDim++) {
-                  Coord_j[iDim] = Buffer_Recv_Coord[index*nDim + iDim];
-                  dist         += pow(Coord_j[iDim]-rotCoord[iDim],2.0);
-                }
-                dist = sqrt(dist);
-
-                /*--- Compare the distance against the existing minimum
-                 and also perform checks just to be sure that this is an
-                 independent periodic point (even if on the same rank),
-                  unless it lies on the axis of rotation. ---*/
-
-                chkSamePoint = false;
-                chkSamePoint = (((dist < mindist) && (iProcessor != rank)) ||
-                                ((dist < mindist) && (iProcessor == rank) &&
-                                (jPoint != iPoint)));
-
-                if (chkSamePoint || ((dist < mindist) && (pointOnAxis))) {
-
-                  /*--- We have found an intermediate match. Store the
-                   data for this point before continuing the search. ---*/
-
-                  mindist      = dist;
-                  pProcessor   = iProcessor;
-                  pPoint       = jPoint;
-                  pPointGlobal = jPointGlobal;
-                  pVertex      = jVertex_;
-                  pMarker      = jMarker;
+                if ((jPointGlobal != iPointGlobal) || (pointOnAxis)) {
+                  /*--- Compute the distance between the candidate periodic
+                   point and the transformed coordinates of the owned point. ---*/
 
+                  dist = 0.0;
+                  for (iDim = 0; iDim < nDim; iDim++) {
+                    Coord_j[iDim] = Buffer_Recv_Coord[index * nDim + iDim];
+                    dist += pow(Coord_j[iDim] - rotCoord[iDim], 2.0);
+                  }
+                  dist = sqrt(dist);
+
+                  /*--- Compare the distance against the existing minimum
+                   and also perform checks just to be sure that this is an
+                   independent periodic point (even if on the same rank),
+                    unless it lies on the axis of rotation. ---*/
+
+                  chkSamePoint = false;
+                  chkSamePoint = (((dist < mindist) && (iProcessor != rank)) ||
+                                  ((dist < mindist) && (iProcessor == rank) && (jPoint != iPoint)));
+
+                  if (chkSamePoint || ((dist < mindist) && (pointOnAxis))) {
+                    /*--- We have found an intermediate match. Store the
+                     data for this point before continuing the search. ---*/
+
+                    mindist = dist;
+                    pProcessor = iProcessor;
+                    pPoint = jPoint;
+                    pPointGlobal = jPointGlobal;
+                    pVertex = jVertex_;
+                    pMarker = jMarker;
+                  }
                 }
               }
 
-            }
-
             /*--- Store the data for the best match found for the
              owned periodic point. ---*/
 
@@ -7209,7 +6887,6 @@ void CPhysicalGeometry::MatchPeriodic(const CConfig *config,
               maxdist_local = min(maxdist_local, 0.0);
               isBadMatch = true;
             }
-
           }
         }
       }
@@ -7221,19 +6898,17 @@ void CPhysicalGeometry::MatchPeriodic(const CConfig *config,
    pairs of points. ---*/
 
   unsigned long nPointMatch_Local = nPointMatch;
-  SU2_MPI::Reduce(&nPointMatch_Local, &nPointMatch, 1, MPI_UNSIGNED_LONG,
-                  MPI_SUM, MASTER_NODE, SU2_MPI::GetComm());
-  SU2_MPI::Reduce(&maxdist_local, &maxdist_global, 1, MPI_DOUBLE,
-                  MPI_MAX, MASTER_NODE, SU2_MPI::GetComm());
+  SU2_MPI::Reduce(&nPointMatch_Local, &nPointMatch, 1, MPI_UNSIGNED_LONG, MPI_SUM, MASTER_NODE, SU2_MPI::GetComm());
+  SU2_MPI::Reduce(&maxdist_local, &maxdist_global, 1, MPI_DOUBLE, MPI_MAX, MASTER_NODE, SU2_MPI::GetComm());
 
   /*--- Output some information about the matching process. ---*/
 
   if (rank == MASTER_NODE) {
     if (nPointMatch > 0) {
-      cout <<" Matched " << nPointMatch << " points with a max distance of: ";
-      cout << maxdist_global <<"."<< endl;
+      cout << " Matched " << nPointMatch << " points with a max distance of: ";
+      cout << maxdist_global << "." << endl;
     } else {
-      cout <<" No matching points for periodic marker pair ";
+      cout << " No matching points for periodic marker pair ";
       cout << val_periodic << " in current zone." << endl;
     }
 
@@ -7257,17 +6932,16 @@ void CPhysicalGeometry::MatchPeriodic(const CConfig *config,
   delete[] Buffer_Send_nVertex;
   delete[] Buffer_Recv_nVertex;
 
-  delete [] Buffer_Send_GlobalIndex;
-  delete [] Buffer_Send_Vertex;
-  delete [] Buffer_Send_Marker;
+  delete[] Buffer_Send_GlobalIndex;
+  delete[] Buffer_Send_Vertex;
+  delete[] Buffer_Send_Marker;
 
-  delete [] Buffer_Recv_GlobalIndex;
-  delete [] Buffer_Recv_Vertex;
-  delete [] Buffer_Recv_Marker;
+  delete[] Buffer_Recv_GlobalIndex;
+  delete[] Buffer_Recv_Vertex;
+  delete[] Buffer_Recv_Marker;
 }
 
-void CPhysicalGeometry::FindUniqueNode_PeriodicBound(const CConfig *config) {
-
+void CPhysicalGeometry::FindUniqueNode_PeriodicBound(const CConfig* config) {
   /*-------------------------------------------------------------------------------------------*/
   /*--- Find reference node on the 'inlet' streamwise periodic marker for the computation   ---*/
   /*--- of recovered pressure/temperature, such that this found node is independent of the  ---*/
@@ -7284,9 +6958,9 @@ void CPhysicalGeometry::FindUniqueNode_PeriodicBound(const CConfig *config) {
   su2double min_norm = numeric_limits<su2double>::max();
 
   /*--- Communicate Coordinates plus the minimum distance, therefor the nDim+1 ---*/
-  vector<su2double> Buffer_Send_RefNode(nDim+1, numeric_limits<su2double>::max());
-  su2activematrix Buffer_Recv_RefNode(size,nDim+1);
-  unsigned long iPointMin = 0; // Initialisaton, otherwise 'may be uninitialized` warning'
+  vector<su2double> Buffer_Send_RefNode(nDim + 1, numeric_limits<su2double>::max());
+  su2activematrix Buffer_Recv_RefNode(size, nDim + 1);
+  unsigned long iPointMin = 0;  // Initialisaton, otherwise 'may be uninitialized` warning'
 
   /*-------------------------------------------------------------------------------------------*/
   /*--- Step 1: Find a unique reference node on each rank and communicate them such that    ---*/
@@ -7297,16 +6971,14 @@ void CPhysicalGeometry::FindUniqueNode_PeriodicBound(const CConfig *config) {
 
   for (unsigned short iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
     if (config->GetMarker_All_KindBC(iMarker) == PERIODIC_BOUNDARY) {
-
       /*--- 1 is the receiver/'inlet', 2 is the donor/'outlet', 0 if no PBC at all. ---*/
       auto iPeriodic = config->GetMarker_All_PerBound(iMarker);
       if (iPeriodic == 1) {
-
         for (auto iVertex = 0ul; iVertex < GetnVertex(iMarker); iVertex++) {
-
           auto iPoint = vertex[iMarker][iVertex]->GetNode();
 
-          /*--- Get the squared norm of the current point. sqrt is a monotonic function in [0,R+) so for comparison we dont need Norm. ---*/
+          /*--- Get the squared norm of the current point. sqrt is a monotonic function in [0,R+) so for comparison we
+           * dont need Norm. ---*/
           auto norm = GeometryToolbox::SquaredNorm(nDim, nodes->GetCoord(iPoint));
 
           /*--- Check if new unique reference node is found and store Point ID. ---*/
@@ -7314,21 +6986,21 @@ void CPhysicalGeometry::FindUniqueNode_PeriodicBound(const CConfig *config) {
             min_norm = norm;
             iPointMin = iPoint;
           }
-          /*--- The theoretical case, that multiple inlet points with the same distance to the origin exists, remains. ---*/
+          /*--- The theoretical case, that multiple inlet points with the same distance to the origin exists, remains.
+           * ---*/
         }
-        break; // Actually no more than one streamwise periodic marker pair is allowed
-      } // receiver conditional
-    } // periodic conditional
-  } // marker loop
+        break;  // Actually no more than one streamwise periodic marker pair is allowed
+      }         // receiver conditional
+    }           // periodic conditional
+  }             // marker loop
 
   /*--- Copy the Coordinates and norm into send buffer. ---*/
-  for (unsigned short iDim = 0; iDim < nDim; iDim++)
-    Buffer_Send_RefNode[iDim] = nodes->GetCoord(iPointMin,iDim);
+  for (unsigned short iDim = 0; iDim < nDim; iDim++) Buffer_Send_RefNode[iDim] = nodes->GetCoord(iPointMin, iDim);
   Buffer_Send_RefNode[nDim] = min_norm;
 
   /*--- Communicate unique nodes to all processes. In case of serial mode nothing happens. ---*/
-  SU2_MPI::Allgather(Buffer_Send_RefNode.data(), nDim+1, MPI_DOUBLE,
-                     Buffer_Recv_RefNode.data(), nDim+1, MPI_DOUBLE, SU2_MPI::GetComm());
+  SU2_MPI::Allgather(Buffer_Send_RefNode.data(), nDim + 1, MPI_DOUBLE, Buffer_Recv_RefNode.data(), nDim + 1, MPI_DOUBLE,
+                     SU2_MPI::GetComm());
 
   /*-------------------------------------------------------------------------------------------*/
   /*--- Step 2: Amongst all local nodes with the smallest distance to the origin, find the  ---*/
@@ -7339,176 +7011,164 @@ void CPhysicalGeometry::FindUniqueNode_PeriodicBound(const CConfig *config) {
   min_norm = numeric_limits<su2double>::max();
 
   for (int iRank = 0; iRank < size; iRank++) {
-
-    auto norm = Buffer_Recv_RefNode(iRank,nDim);
+    auto norm = Buffer_Recv_RefNode(iRank, nDim);
 
     /*--- Check if new unique reference node is found. ---*/
     if (norm < min_norm) {
       min_norm = norm;
       for (unsigned short iDim = 0; iDim < nDim; iDim++)
-        Streamwise_Periodic_RefNode[iDim] = Buffer_Recv_RefNode(iRank,iDim);
+        Streamwise_Periodic_RefNode[iDim] = Buffer_Recv_RefNode(iRank, iDim);
     }
   }
 
   /*--- Print the reference node to screen. ---*/
   if (rank == MASTER_NODE) {
     cout << "Streamwise Periodic Reference Node: [";
-    for (unsigned short iDim = 0; iDim < nDim; iDim++)
-      cout <<  " " << Streamwise_Periodic_RefNode[iDim];
+    for (unsigned short iDim = 0; iDim < nDim; iDim++) cout << " " << Streamwise_Periodic_RefNode[iDim];
     cout << " ]" << endl;
   }
-
 }
 
-void CPhysicalGeometry::SetControlVolume(CConfig *config, unsigned short action) {
-
+void CPhysicalGeometry::SetControlVolume(CConfig* config, unsigned short action) {
   /*--- Update values of faces of the edge ---*/
   if (action != ALLOCATE) {
     su2double ZeroArea[MAXNDIM] = {0.0};
 
     SU2_OMP_FOR_STAT(1024)
-    for (auto iEdge = 0ul; iEdge < nEdge; iEdge++)
-      edges->SetNormal(iEdge, ZeroArea);
+    for (auto iEdge = 0ul; iEdge < nEdge; iEdge++) edges->SetNormal(iEdge, ZeroArea);
     END_SU2_OMP_FOR
 
     SU2_OMP_FOR_STAT(1024)
-    for (auto iPoint = 0ul; iPoint < nPoint; iPoint++)
-      nodes->SetVolume(iPoint, 0.0);
+    for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) nodes->SetVolume(iPoint, 0.0);
     END_SU2_OMP_FOR
   }
 
   BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS { /*--- The following is difficult to parallelize with threads. ---*/
 
-  su2double my_DomainVolume = 0.0;
-  for (auto iElem = 0ul; iElem < nElem; iElem++) {
-
-    const auto nNodes = elem[iElem]->GetnNodes();
+    su2double my_DomainVolume = 0.0;
+    for (auto iElem = 0ul; iElem < nElem; iElem++) {
+      const auto nNodes = elem[iElem]->GetnNodes();
 
-    /*--- To make preaccumulation more effective, use as few inputs
-     as possible, recomputing intermediate quantities as needed. ---*/
-    AD::StartPreacc();
+      /*--- To make preaccumulation more effective, use as few inputs
+       as possible, recomputing intermediate quantities as needed. ---*/
+      AD::StartPreacc();
 
-    /*--- Get pointers to the coordinates of all the element nodes ---*/
-    array<const su2double*, N_POINTS_MAXIMUM> Coord;
+      /*--- Get pointers to the coordinates of all the element nodes ---*/
+      array<const su2double*, N_POINTS_MAXIMUM> Coord;
 
-    for (unsigned short iNode = 0; iNode < nNodes; iNode++) {
-      auto iPoint = elem[iElem]->GetNode(iNode);
-      Coord[iNode] = nodes->GetCoord(iPoint);
+      for (unsigned short iNode = 0; iNode < nNodes; iNode++) {
+        auto iPoint = elem[iElem]->GetNode(iNode);
+        Coord[iNode] = nodes->GetCoord(iPoint);
 #ifdef CODI_REVERSE_TYPE
-      /*--- The same points and edges will be referenced multiple times as they are common
-       to many of the element's faces, therefore they are "registered" here only once. ---*/
-      AD::SetPreaccIn(nodes->Volume(iPoint));
-      for (unsigned short jNode = iNode+1; jNode < nNodes; jNode++) {
-        auto jPoint = elem[iElem]->GetNode(jNode);
-        auto iEdge = FindEdge(iPoint, jPoint, false);
-        if (iEdge >= 0) AD::SetPreaccIn(edges->Normal[iEdge], nDim);
-      }
+        /*--- The same points and edges will be referenced multiple times as they are common
+         to many of the element's faces, therefore they are "registered" here only once. ---*/
+        AD::SetPreaccIn(nodes->Volume(iPoint));
+        for (unsigned short jNode = iNode + 1; jNode < nNodes; jNode++) {
+          auto jPoint = elem[iElem]->GetNode(jNode);
+          auto iEdge = FindEdge(iPoint, jPoint, false);
+          if (iEdge >= 0) AD::SetPreaccIn(edges->Normal[iEdge], nDim);
+        }
 #endif
-    }
-    AD::SetPreaccIn(Coord, nNodes, nDim);
-
-    /*--- Compute the element median CG coordinates ---*/
-    auto Coord_Elem_CG = elem[iElem]->SetCoord_CG(nDim, Coord);
-    AD::SetPreaccOut(Coord_Elem_CG, nDim);
+      }
+      AD::SetPreaccIn(Coord, nNodes, nDim);
 
-    for (unsigned short iFace = 0; iFace < elem[iElem]->GetnFaces(); iFace++) {
+      /*--- Compute the element median CG coordinates ---*/
+      auto Coord_Elem_CG = elem[iElem]->SetCoord_CG(nDim, Coord);
+      AD::SetPreaccOut(Coord_Elem_CG, nDim);
 
-      /*--- In 2D all the faces have only one edge ---*/
-      unsigned short nEdgesFace = 1;
+      for (unsigned short iFace = 0; iFace < elem[iElem]->GetnFaces(); iFace++) {
+        /*--- In 2D all the faces have only one edge ---*/
+        unsigned short nEdgesFace = 1;
 
-      /*--- In 3D the number of edges per face is the same as the number of point
-       per face and the median CG of the face is needed. ---*/
-      su2double Coord_FaceElem_CG[MAXNDIM] = {0.0};
-      if (nDim == 3) {
-        nEdgesFace = elem[iElem]->GetnNodesFace(iFace);
+        /*--- In 3D the number of edges per face is the same as the number of point
+         per face and the median CG of the face is needed. ---*/
+        su2double Coord_FaceElem_CG[MAXNDIM] = {0.0};
+        if (nDim == 3) {
+          nEdgesFace = elem[iElem]->GetnNodesFace(iFace);
 
-        for (unsigned short iNode = 0; iNode < nEdgesFace; iNode++) {
-          auto NodeFace = elem[iElem]->GetFaces(iFace, iNode);
-          for (unsigned short iDim = 0; iDim < nDim; iDim++)
-            Coord_FaceElem_CG[iDim] += Coord[NodeFace][iDim]/nEdgesFace;
+          for (unsigned short iNode = 0; iNode < nEdgesFace; iNode++) {
+            auto NodeFace = elem[iElem]->GetFaces(iFace, iNode);
+            for (unsigned short iDim = 0; iDim < nDim; iDim++)
+              Coord_FaceElem_CG[iDim] += Coord[NodeFace][iDim] / nEdgesFace;
+          }
         }
-      }
 
-      /*-- Loop over the edges of a face ---*/
-      for (unsigned short iEdgesFace = 0; iEdgesFace < nEdgesFace; iEdgesFace++) {
+        /*-- Loop over the edges of a face ---*/
+        for (unsigned short iEdgesFace = 0; iEdgesFace < nEdgesFace; iEdgesFace++) {
+          const auto face_iNode = elem[iElem]->GetFaces(iFace, iEdgesFace);
+          unsigned short face_jNode;
 
-        const auto face_iNode = elem[iElem]->GetFaces(iFace,iEdgesFace);
-        unsigned short face_jNode;
-
-        if (nDim == 2) {
-          /*--- In 2D only one edge (two points) per edge ---*/
-          face_jNode = elem[iElem]->GetFaces(iFace,1);
-        }
-        else {
-          /*--- In 3D we "circle around" the face ---*/
-          face_jNode = elem[iElem]->GetFaces(iFace, (iEdgesFace+1)%nEdgesFace);
-        }
+          if (nDim == 2) {
+            /*--- In 2D only one edge (two points) per edge ---*/
+            face_jNode = elem[iElem]->GetFaces(iFace, 1);
+          } else {
+            /*--- In 3D we "circle around" the face ---*/
+            face_jNode = elem[iElem]->GetFaces(iFace, (iEdgesFace + 1) % nEdgesFace);
+          }
 
-        const auto face_iPoint = elem[iElem]->GetNode(face_iNode);
-        const auto face_jPoint = elem[iElem]->GetNode(face_jNode);
+          const auto face_iPoint = elem[iElem]->GetNode(face_iNode);
+          const auto face_jPoint = elem[iElem]->GetNode(face_jNode);
 
-        /*--- We define a direction (from the smalest index to the greatest) --*/
-        const bool change_face_orientation = (face_iPoint > face_jPoint);
-        const auto iEdge = FindEdge(face_iPoint, face_jPoint);
+          /*--- We define a direction (from the smalest index to the greatest) --*/
+          const bool change_face_orientation = (face_iPoint > face_jPoint);
+          const auto iEdge = FindEdge(face_iPoint, face_jPoint);
 
-        su2double Coord_Edge_CG[MAXNDIM] = {0.0};
-        for (unsigned short iDim = 0; iDim < nDim; iDim++) {
-          Coord_Edge_CG[iDim] = 0.5 * (Coord[face_iNode][iDim] + Coord[face_jNode][iDim]);
-        }
+          su2double Coord_Edge_CG[MAXNDIM] = {0.0};
+          for (unsigned short iDim = 0; iDim < nDim; iDim++) {
+            Coord_Edge_CG[iDim] = 0.5 * (Coord[face_iNode][iDim] + Coord[face_jNode][iDim]);
+          }
 
-        su2double Volume_i, Volume_j;
+          su2double Volume_i, Volume_j;
 
-        if (nDim == 2) {
-          /*--- Two dimensional problem ---*/
-          if (change_face_orientation)
-            edges->SetNodes_Coord(iEdge, Coord_Elem_CG, Coord_Edge_CG);
-          else
-            edges->SetNodes_Coord(iEdge, Coord_Edge_CG, Coord_Elem_CG);
+          if (nDim == 2) {
+            /*--- Two dimensional problem ---*/
+            if (change_face_orientation)
+              edges->SetNodes_Coord(iEdge, Coord_Elem_CG, Coord_Edge_CG);
+            else
+              edges->SetNodes_Coord(iEdge, Coord_Edge_CG, Coord_Elem_CG);
+
+            Volume_i = CEdge::GetVolume(Coord[face_iNode], Coord_Edge_CG, Coord_Elem_CG);
+            Volume_j = CEdge::GetVolume(Coord[face_jNode], Coord_Edge_CG, Coord_Elem_CG);
+          } else {
+            /*--- Three dimensional problem ---*/
+            if (change_face_orientation)
+              edges->SetNodes_Coord(iEdge, Coord_FaceElem_CG, Coord_Edge_CG, Coord_Elem_CG);
+            else
+              edges->SetNodes_Coord(iEdge, Coord_Edge_CG, Coord_FaceElem_CG, Coord_Elem_CG);
+
+            Volume_i = CEdge::GetVolume(Coord[face_iNode], Coord_Edge_CG, Coord_FaceElem_CG, Coord_Elem_CG);
+            Volume_j = CEdge::GetVolume(Coord[face_jNode], Coord_Edge_CG, Coord_FaceElem_CG, Coord_Elem_CG);
+          }
 
-          Volume_i = CEdge::GetVolume(Coord[face_iNode], Coord_Edge_CG, Coord_Elem_CG);
-          Volume_j = CEdge::GetVolume(Coord[face_jNode], Coord_Edge_CG, Coord_Elem_CG);
-        }
-        else {
-          /*--- Three dimensional problem ---*/
-          if (change_face_orientation)
-            edges->SetNodes_Coord(iEdge, Coord_FaceElem_CG, Coord_Edge_CG, Coord_Elem_CG);
-          else
-            edges->SetNodes_Coord(iEdge, Coord_Edge_CG, Coord_FaceElem_CG, Coord_Elem_CG);
+          nodes->AddVolume(face_iPoint, Volume_i);
+          nodes->AddVolume(face_jPoint, Volume_j);
 
-          Volume_i = CEdge::GetVolume(Coord[face_iNode], Coord_Edge_CG, Coord_FaceElem_CG, Coord_Elem_CG);
-          Volume_j = CEdge::GetVolume(Coord[face_jNode], Coord_Edge_CG, Coord_FaceElem_CG, Coord_Elem_CG);
+          my_DomainVolume += Volume_i + Volume_j;
         }
-
-        nodes->AddVolume(face_iPoint, Volume_i);
-        nodes->AddVolume(face_jPoint, Volume_j);
-
-        my_DomainVolume += Volume_i+Volume_j;
       }
-    }
 
 #ifdef CODI_REVERSE_TYPE
-    for (unsigned short iNode = 0; iNode < nNodes; iNode++) {
-      auto iPoint = elem[iElem]->GetNode(iNode);
-      AD::SetPreaccOut(nodes->Volume(iPoint));
-      for (unsigned short jNode = iNode+1; jNode < nNodes; jNode++) {
-        auto jPoint = elem[iElem]->GetNode(jNode);
-        auto iEdge = FindEdge(iPoint, jPoint, false);
-        if (iEdge >= 0) AD::SetPreaccOut(edges->Normal[iEdge], nDim);
+      for (unsigned short iNode = 0; iNode < nNodes; iNode++) {
+        auto iPoint = elem[iElem]->GetNode(iNode);
+        AD::SetPreaccOut(nodes->Volume(iPoint));
+        for (unsigned short jNode = iNode + 1; jNode < nNodes; jNode++) {
+          auto jPoint = elem[iElem]->GetNode(jNode);
+          auto iEdge = FindEdge(iPoint, jPoint, false);
+          if (iEdge >= 0) AD::SetPreaccOut(edges->Normal[iEdge], nDim);
+        }
       }
-    }
 #endif
-    AD::EndPreacc();
-  }
-
-  su2double DomainVolume;
-  SU2_MPI::Allreduce(&my_DomainVolume, &DomainVolume, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-  config->SetDomainVolume(DomainVolume);
+      AD::EndPreacc();
+    }
 
-  if ((rank == MASTER_NODE) && (action == ALLOCATE)) {
-    if (nDim == 2) cout <<"Area of the computational grid: "<< DomainVolume <<"."<< endl;
-    if (nDim == 3) cout <<"Volume of the computational grid: "<< DomainVolume <<"."<< endl;
-  }
+    su2double DomainVolume;
+    SU2_MPI::Allreduce(&my_DomainVolume, &DomainVolume, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
+    config->SetDomainVolume(DomainVolume);
 
+    if ((rank == MASTER_NODE) && (action == ALLOCATE)) {
+      if (nDim == 2) cout << "Area of the computational grid: " << DomainVolume << "." << endl;
+      if (nDim == 3) cout << "Volume of the computational grid: " << DomainVolume << "." << endl;
+    }
   }
   END_SU2_OMP_SAFE_GLOBAL_ACCESS
 
@@ -7516,21 +7176,19 @@ void CPhysicalGeometry::SetControlVolume(CConfig *config, unsigned short action)
   SU2_OMP_FOR_STAT(1024)
   for (auto iEdge = 0ul; iEdge < nEdge; iEdge++) {
     const auto Area2 = GeometryToolbox::SquaredNorm(nDim, edges->GetNormal(iEdge));
-    su2double DefaultArea[MAXNDIM] = {EPS*EPS};
+    su2double DefaultArea[MAXNDIM] = {EPS * EPS};
     if (Area2 == 0.0) edges->SetNormal(iEdge, DefaultArea);
   }
   END_SU2_OMP_FOR
 }
 
-void CPhysicalGeometry::SetBoundControlVolume(const CConfig *config, unsigned short action) {
-
+void CPhysicalGeometry::SetBoundControlVolume(const CConfig* config, unsigned short action) {
   /*--- Clear normals ---*/
 
   if (action != ALLOCATE) {
     SU2_OMP_FOR_DYN(1)
     for (unsigned short iMarker = 0; iMarker < nMarker; iMarker++)
-      for (unsigned long iVertex = 0; iVertex < nVertex[iMarker]; iVertex++)
-        vertex[iMarker][iVertex]->SetZeroValues();
+      for (unsigned long iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) vertex[iMarker][iVertex]->SetZeroValues();
     END_SU2_OMP_FOR
   }
 
@@ -7539,7 +7197,6 @@ void CPhysicalGeometry::SetBoundControlVolume(const CConfig *config, unsigned sh
   SU2_OMP_FOR_DYN(1)
   for (unsigned short iMarker = 0; iMarker < nMarker; iMarker++) {
     for (unsigned long iElem = 0; iElem < nElem_Bound[iMarker]; iElem++) {
-
       const auto nNodes = bound[iMarker][iElem]->GetnNodes();
 
       /*--- Cannot preaccumulate if hybrid parallel due to shared reading. ---*/
@@ -7574,8 +7231,7 @@ void CPhysicalGeometry::SetBoundControlVolume(const CConfig *config, unsigned sh
             /*--- Store the 2D face ---*/
             if (iNode == 0) vertex[iMarker][iVertex]->SetNodes_Coord(Coord_Elem_CG, Coord_Vertex);
             if (iNode == 1) vertex[iMarker][iVertex]->SetNodes_Coord(Coord_Vertex, Coord_Elem_CG);
-          }
-          else {
+          } else {
             const auto Neighbor_Node = bound[iMarker][iElem]->GetNeighbor_Nodes(iNode, iNeighbor);
             auto Neighbor_Coord = Coord[Neighbor_Node];
 
@@ -7603,18 +7259,17 @@ void CPhysicalGeometry::SetBoundControlVolume(const CConfig *config, unsigned sh
   /*--- Check if there is a normal with null area ---*/
 
   SU2_OMP_FOR_DYN(1)
-  for (unsigned short iMarker = 0; iMarker < nMarker; iMarker ++) {
+  for (unsigned short iMarker = 0; iMarker < nMarker; iMarker++) {
     for (unsigned long iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
       auto Area2 = GeometryToolbox::SquaredNorm(nDim, vertex[iMarker][iVertex]->GetNormal());
-      su2double DefaultArea[MAXNDIM] = {EPS*EPS};
+      su2double DefaultArea[MAXNDIM] = {EPS * EPS};
       if (Area2 == 0.0) vertex[iMarker][iVertex]->SetNormal(DefaultArea);
     }
   }
   END_SU2_OMP_FOR
 }
 
-void CPhysicalGeometry::VisualizeControlVolume(const CConfig *config) const {
-
+void CPhysicalGeometry::VisualizeControlVolume(const CConfig* config) const {
   /*--- Access the point number for control volume we want to vizualize ---*/
 
   auto iPoint = GetGlobal_to_Local_Point(config->GetVisualize_CV());
@@ -7627,7 +7282,6 @@ void CPhysicalGeometry::VisualizeControlVolume(const CConfig *config) const {
   /*--- Loop over each face of each element ---*/
 
   for (auto iElem = 0ul; iElem < nElem; iElem++) {
-
     /*--- Get pointers to the coordinates of all the element nodes ---*/
     array<const su2double*, N_POINTS_MAXIMUM> Coord;
 
@@ -7637,7 +7291,6 @@ void CPhysicalGeometry::VisualizeControlVolume(const CConfig *config) const {
     }
 
     for (unsigned short iFace = 0; iFace < elem[iElem]->GetnFaces(); iFace++) {
-
       /*--- In 2D all the faces have only one edge ---*/
       unsigned short nEdgesFace = 1;
 
@@ -7650,30 +7303,27 @@ void CPhysicalGeometry::VisualizeControlVolume(const CConfig *config) const {
         for (unsigned short iNode = 0; iNode < nEdgesFace; iNode++) {
           auto NodeFace = elem[iElem]->GetFaces(iFace, iNode);
           for (unsigned short iDim = 0; iDim < nDim; iDim++)
-            Coord_FaceElem_CG[iDim] += Coord[NodeFace][iDim]/nEdgesFace;
+            Coord_FaceElem_CG[iDim] += Coord[NodeFace][iDim] / nEdgesFace;
         }
       }
 
       /*-- Loop over the edges of a face ---*/
       for (unsigned short iEdgesFace = 0; iEdgesFace < nEdgesFace; iEdgesFace++) {
-
-        const auto face_iPoint = elem[iElem]->GetNode(elem[iElem]->GetFaces(iFace,iEdgesFace));
+        const auto face_iPoint = elem[iElem]->GetNode(elem[iElem]->GetFaces(iFace, iEdgesFace));
         unsigned long face_jPoint;
 
         if (nDim == 2) {
           /*--- In 2D only one edge (two points) per edge ---*/
-          face_jPoint = elem[iElem]->GetNode(elem[iElem]->GetFaces(iFace,1));
-        }
-        else {
+          face_jPoint = elem[iElem]->GetNode(elem[iElem]->GetFaces(iFace, 1));
+        } else {
           /*--- In 3D we "circle around" the face ---*/
-          face_jPoint = elem[iElem]->GetNode(elem[iElem]->GetFaces(iFace, (iEdgesFace+1)%nEdgesFace));
+          face_jPoint = elem[iElem]->GetNode(elem[iElem]->GetFaces(iFace, (iEdgesFace + 1) % nEdgesFace));
         }
 
         /*--- Print out the coordinates for a set of triangles making
          up a single dual control volume for visualization. ---*/
 
         if (face_iPoint == iPoint_Viz || face_jPoint == iPoint_Viz) {
-
           const su2double* Coord_FaceiPoint = nodes->GetCoord(face_iPoint);
           const su2double* Coord_FacejPoint = nodes->GetCoord(face_jPoint);
           const su2double* Coord_Elem_CG = elem[iElem]->GetCG();
@@ -7684,12 +7334,20 @@ void CPhysicalGeometry::VisualizeControlVolume(const CConfig *config) const {
           }
 
           if (nDim == 2) {
-            X.push_back(Coord_Elem_CG[0]); X.push_back(Coord_Edge_CG[0]);
-            Y.push_back(Coord_Elem_CG[1]); Y.push_back(Coord_Edge_CG[1]);
+            X.push_back(Coord_Elem_CG[0]);
+            X.push_back(Coord_Edge_CG[0]);
+            Y.push_back(Coord_Elem_CG[1]);
+            Y.push_back(Coord_Edge_CG[1]);
           } else {
-            X.push_back(Coord_FaceElem_CG[0]); X.push_back(Coord_Edge_CG[0]); X.push_back(Coord_Elem_CG[0]);
-            Y.push_back(Coord_FaceElem_CG[1]); Y.push_back(Coord_Edge_CG[1]); Y.push_back(Coord_Elem_CG[1]);
-            Z.push_back(Coord_FaceElem_CG[2]); Z.push_back(Coord_Edge_CG[2]); Z.push_back(Coord_Elem_CG[2]);
+            X.push_back(Coord_FaceElem_CG[0]);
+            X.push_back(Coord_Edge_CG[0]);
+            X.push_back(Coord_Elem_CG[0]);
+            Y.push_back(Coord_FaceElem_CG[1]);
+            Y.push_back(Coord_Edge_CG[1]);
+            Y.push_back(Coord_Elem_CG[1]);
+            Z.push_back(Coord_FaceElem_CG[2]);
+            Z.push_back(Coord_Edge_CG[2]);
+            Z.push_back(Coord_Elem_CG[2]);
           }
           counter++;
         }
@@ -7707,12 +7365,12 @@ void CPhysicalGeometry::VisualizeControlVolume(const CConfig *config) const {
 
   if (nDim == 2) {
     Tecplot_File << "VARIABLES = \"x\",\"y\" " << endl;
-    Tecplot_File << "ZONE NODES= "<< counter*2 <<", ELEMENTS= ";
-    Tecplot_File << counter <<", DATAPACKING=POINT, ZONETYPE=FEQUADRILATERAL"<< endl;
+    Tecplot_File << "ZONE NODES= " << counter * 2 << ", ELEMENTS= ";
+    Tecplot_File << counter << ", DATAPACKING=POINT, ZONETYPE=FEQUADRILATERAL" << endl;
   } else {
     Tecplot_File << "VARIABLES = \"x\",\"y\",\"z\" " << endl;
-    Tecplot_File << "ZONE NODES= "<< counter*3 <<", ELEMENTS= ";
-    Tecplot_File << counter <<", DATAPACKING=POINT, ZONETYPE=FEBRICK"<< endl;
+    Tecplot_File << "ZONE NODES= " << counter * 3 << ", ELEMENTS= ";
+    Tecplot_File << counter << ", DATAPACKING=POINT, ZONETYPE=FEBRICK" << endl;
   }
 
   /*--- Write coordinates for the nodes in the order that they were found
@@ -7728,44 +7386,42 @@ void CPhysicalGeometry::VisualizeControlVolume(const CConfig *config) const {
 
   for (int i = 0, j; i < counter; i++) {
     if (nDim == 2) {
-      j = i*2;
-      Tecplot_File << j+1 <<"\t"<<j+2 <<"\t"<<j+2 <<"\t"<<j+2 << endl;
+      j = i * 2;
+      Tecplot_File << j + 1 << "\t" << j + 2 << "\t" << j + 2 << "\t" << j + 2 << endl;
     } else {
-      j = i*3;
-      Tecplot_File << j+1 <<"\t"<<j+2 <<"\t"<<j+3 <<"\t"<<j+3 <<"\t";
-      Tecplot_File << j+3<<"\t" <<j+3 <<"\t"<<j+3 <<"\t"<<j+3 << endl;
+      j = i * 3;
+      Tecplot_File << j + 1 << "\t" << j + 2 << "\t" << j + 3 << "\t" << j + 3 << "\t";
+      Tecplot_File << j + 3 << "\t" << j + 3 << "\t" << j + 3 << "\t" << j + 3 << endl;
     }
   }
 }
 
-void CPhysicalGeometry::SetCoord_Smoothing (unsigned short val_nSmooth, su2double val_smooth_coeff, CConfig *config) {
+void CPhysicalGeometry::SetCoord_Smoothing(unsigned short val_nSmooth, su2double val_smooth_coeff, CConfig* config) {
   unsigned short iSmooth, nneigh, iMarker;
   su2double *Coord_Old, *Coord_Sum, *Coord, *Coord_i, *Coord_j, Position_Plane = 0.0;
   unsigned long iEdge, iPoint, jPoint, iVertex;
   su2double eps = 1E-6;
   bool NearField = false;
 
-  Coord = new su2double [nDim];
+  Coord = new su2double[nDim];
 
   nodes->SetCoord_Old();
 
   /*--- Jacobi iterations ---*/
   for (iSmooth = 0; iSmooth < val_nSmooth; iSmooth++) {
-
     nodes->SetCoord_SumZero();
 
     /*--- Loop over Interior edges ---*/
     for (iEdge = 0; iEdge < nEdge; iEdge++) {
-      iPoint = edges->GetNode(iEdge,0);
+      iPoint = edges->GetNode(iEdge, 0);
       Coord_i = nodes->GetCoord(iPoint);
 
-      jPoint = edges->GetNode(iEdge,1);
+      jPoint = edges->GetNode(iEdge, 1);
       Coord_j = nodes->GetCoord(jPoint);
 
       /*--- Accumulate nearest neighbor Coord to Res_sum for each variable ---*/
       nodes->AddCoord_Sum(iPoint, Coord_j);
       nodes->AddCoord_Sum(jPoint, Coord_i);
-
     }
 
     /*--- Loop over all mesh points (Update Coords with averaged sum) ---*/
@@ -7775,17 +7431,17 @@ void CPhysicalGeometry::SetCoord_Smoothing (unsigned short val_nSmooth, su2doubl
       Coord_Old = nodes->GetCoord_Old(iPoint);
 
       if (nDim == 2) {
-        Coord[0] =(Coord_Old[0] + val_smooth_coeff*Coord_Sum[0]) /(1.0 + val_smooth_coeff*su2double(nneigh));
-        Coord[1] =(Coord_Old[1] + val_smooth_coeff*Coord_Sum[1]) /(1.0 + val_smooth_coeff*su2double(nneigh));
-        if ((NearField) && ((Coord_Old[1] > Position_Plane-eps) && (Coord_Old[1] < Position_Plane+eps)))
+        Coord[0] = (Coord_Old[0] + val_smooth_coeff * Coord_Sum[0]) / (1.0 + val_smooth_coeff * su2double(nneigh));
+        Coord[1] = (Coord_Old[1] + val_smooth_coeff * Coord_Sum[1]) / (1.0 + val_smooth_coeff * su2double(nneigh));
+        if ((NearField) && ((Coord_Old[1] > Position_Plane - eps) && (Coord_Old[1] < Position_Plane + eps)))
           Coord[1] = Coord_Old[1];
       }
 
       if (nDim == 3) {
-        Coord[0] =(Coord_Old[0] + val_smooth_coeff*Coord_Sum[0]) /(1.0 + val_smooth_coeff*su2double(nneigh));
-        Coord[1] =(Coord_Old[1] + val_smooth_coeff*Coord_Sum[1]) /(1.0 + val_smooth_coeff*su2double(nneigh));
-        Coord[2] =(Coord_Old[2] + val_smooth_coeff*Coord_Sum[2]) /(1.0 + val_smooth_coeff*su2double(nneigh));
-        if ((NearField) && ((Coord_Old[2] > Position_Plane-eps) && (Coord_Old[2] < Position_Plane+eps)))
+        Coord[0] = (Coord_Old[0] + val_smooth_coeff * Coord_Sum[0]) / (1.0 + val_smooth_coeff * su2double(nneigh));
+        Coord[1] = (Coord_Old[1] + val_smooth_coeff * Coord_Sum[1]) / (1.0 + val_smooth_coeff * su2double(nneigh));
+        Coord[2] = (Coord_Old[2] + val_smooth_coeff * Coord_Sum[2]) / (1.0 + val_smooth_coeff * su2double(nneigh));
+        if ((NearField) && ((Coord_Old[2] > Position_Plane - eps) && (Coord_Old[2] < Position_Plane + eps)))
           Coord[2] = Coord_Old[2];
       }
 
@@ -7804,9 +7460,8 @@ void CPhysicalGeometry::SetCoord_Smoothing (unsigned short val_nSmooth, su2doubl
   delete[] Coord;
 }
 
-bool CPhysicalGeometry::FindFace(unsigned long first_elem, unsigned long second_elem, unsigned short &face_first_elem,
-                                 unsigned short &face_second_elem) {
-
+bool CPhysicalGeometry::FindFace(unsigned long first_elem, unsigned long second_elem, unsigned short& face_first_elem,
+                                 unsigned short& face_second_elem) {
   if (first_elem == second_elem) return false;
 
   /*--- Find repeated nodes between two elements to identify the common face. ---*/
@@ -7827,7 +7482,7 @@ bool CPhysicalGeometry::FindFace(unsigned long first_elem, unsigned long second_
   }
 
   /*--- Sort point in face and check that the list is unique ---*/
-  sort(CommonPoints, CommonPoints+numCommonPoints);
+  sort(CommonPoints, CommonPoints + numCommonPoints);
 
   /*--- In 2D, the two elements must share two points that make up
    an edge, as all "faces" are edges in 2D. In 3D, we need to find
@@ -7838,9 +7493,8 @@ bool CPhysicalGeometry::FindFace(unsigned long first_elem, unsigned long second_
 
   /*--- Find the faces with the CommonPoint sequence in the first and second elements ---*/
   for (auto iElem = 0ul; iElem < 2; ++iElem) {
-
-    const auto idxElem = (iElem==0)? first_elem : second_elem;
-    auto& idxFaceOut = (iElem==0)? face_first_elem : face_second_elem;
+    const auto idxElem = (iElem == 0) ? first_elem : second_elem;
+    auto& idxFaceOut = (iElem == 0) ? face_first_elem : face_second_elem;
     bool faceFound = false;
 
     for (auto iFace = 0u; iFace < elem[idxElem]->GetnFaces(); iFace++) {
@@ -7856,7 +7510,7 @@ bool CPhysicalGeometry::FindFace(unsigned long first_elem, unsigned long second_
       }
 
       /*--- Sort face_poin to perform comparison ---*/
-      const auto PointsFaceEnd = PointsFace+nNodesFace;
+      const auto PointsFaceEnd = PointsFace + nNodesFace;
       sort(PointsFace, PointsFaceEnd);
 
       /*--- List comparison ---*/
@@ -7876,7 +7530,6 @@ bool CPhysicalGeometry::FindFace(unsigned long first_elem, unsigned long second_
 }
 
 void CPhysicalGeometry::SetTecPlot(char mesh_filename[MAX_STRING_SIZE], bool new_file) {
-
   unsigned long iElem, iPoint;
   unsigned short iDim;
   ofstream Tecplot_File;
@@ -7888,21 +7541,22 @@ void CPhysicalGeometry::SetTecPlot(char mesh_filename[MAX_STRING_SIZE], bool new
     Tecplot_File << "TITLE= \"Visualization of the volumetric grid\"" << endl;
     if (nDim == 2) Tecplot_File << "VARIABLES = \"x\",\"y\" " << endl;
     if (nDim == 3) Tecplot_File << "VARIABLES = \"x\",\"y\",\"z\" " << endl;
-  }
-  else Tecplot_File.open(mesh_filename, ios::out | ios::app);
+  } else
+    Tecplot_File.open(mesh_filename, ios::out | ios::app);
 
   Tecplot_File << "ZONE T= ";
-  if (new_file) Tecplot_File << "\"Original grid\", C=BLACK, ";
-  else Tecplot_File << "\"Deformed grid\", C=RED, ";
-  Tecplot_File << "NODES= "<< nPoint <<", ELEMENTS= "<< nElem <<", DATAPACKING= POINT";
-  if (nDim == 2) Tecplot_File << ", ZONETYPE= FEQUADRILATERAL"<< endl;
-  if (nDim == 3) Tecplot_File << ", ZONETYPE= FEBRICK"<< endl;
+  if (new_file)
+    Tecplot_File << "\"Original grid\", C=BLACK, ";
+  else
+    Tecplot_File << "\"Deformed grid\", C=RED, ";
+  Tecplot_File << "NODES= " << nPoint << ", ELEMENTS= " << nElem << ", DATAPACKING= POINT";
+  if (nDim == 2) Tecplot_File << ", ZONETYPE= FEQUADRILATERAL" << endl;
+  if (nDim == 3) Tecplot_File << ", ZONETYPE= FEBRICK" << endl;
 
   /*--- Adding coordinates ---*/
 
   for (iPoint = 0; iPoint < nPoint; iPoint++) {
-    for (iDim = 0; iDim < nDim; iDim++)
-      Tecplot_File << scientific << nodes->GetCoord(iPoint, iDim) << "\t";
+    for (iDim = 0; iDim < nDim; iDim++) Tecplot_File << scientific << nodes->GetCoord(iPoint, iDim) << "\t";
     Tecplot_File << "\n";
   }
 
@@ -7910,50 +7564,43 @@ void CPhysicalGeometry::SetTecPlot(char mesh_filename[MAX_STRING_SIZE], bool new
 
   for (iElem = 0; iElem < nElem; iElem++) {
     if (elem[iElem]->GetVTK_Type() == TRIANGLE) {
-      Tecplot_File <<
-      elem[iElem]->GetNode(0)+1 <<" "<< elem[iElem]->GetNode(1)+1 <<" "<<
-      elem[iElem]->GetNode(2)+1 <<" "<< elem[iElem]->GetNode(2)+1 << endl;
+      Tecplot_File << elem[iElem]->GetNode(0) + 1 << " " << elem[iElem]->GetNode(1) + 1 << " "
+                   << elem[iElem]->GetNode(2) + 1 << " " << elem[iElem]->GetNode(2) + 1 << endl;
     }
     if (elem[iElem]->GetVTK_Type() == QUADRILATERAL) {
-      Tecplot_File <<
-      elem[iElem]->GetNode(0)+1 <<" "<< elem[iElem]->GetNode(1)+1 <<" "<<
-      elem[iElem]->GetNode(2)+1 <<" "<< elem[iElem]->GetNode(3)+1 << endl;
+      Tecplot_File << elem[iElem]->GetNode(0) + 1 << " " << elem[iElem]->GetNode(1) + 1 << " "
+                   << elem[iElem]->GetNode(2) + 1 << " " << elem[iElem]->GetNode(3) + 1 << endl;
     }
     if (elem[iElem]->GetVTK_Type() == TETRAHEDRON) {
-      Tecplot_File <<
-      elem[iElem]->GetNode(0)+1 <<" "<< elem[iElem]->GetNode(1)+1 <<" "<<
-      elem[iElem]->GetNode(2)+1 <<" "<< elem[iElem]->GetNode(2)+1 <<" "<<
-      elem[iElem]->GetNode(3)+1 <<" "<< elem[iElem]->GetNode(3)+1 <<" "<<
-      elem[iElem]->GetNode(3)+1 <<" "<< elem[iElem]->GetNode(3)+1 << endl;
+      Tecplot_File << elem[iElem]->GetNode(0) + 1 << " " << elem[iElem]->GetNode(1) + 1 << " "
+                   << elem[iElem]->GetNode(2) + 1 << " " << elem[iElem]->GetNode(2) + 1 << " "
+                   << elem[iElem]->GetNode(3) + 1 << " " << elem[iElem]->GetNode(3) + 1 << " "
+                   << elem[iElem]->GetNode(3) + 1 << " " << elem[iElem]->GetNode(3) + 1 << endl;
     }
     if (elem[iElem]->GetVTK_Type() == HEXAHEDRON) {
-      Tecplot_File <<
-      elem[iElem]->GetNode(0)+1 <<" "<< elem[iElem]->GetNode(1)+1 <<" "<<
-      elem[iElem]->GetNode(2)+1 <<" "<< elem[iElem]->GetNode(3)+1 <<" "<<
-      elem[iElem]->GetNode(4)+1 <<" "<< elem[iElem]->GetNode(5)+1 <<" "<<
-      elem[iElem]->GetNode(6)+1 <<" "<< elem[iElem]->GetNode(7)+1 << endl;
+      Tecplot_File << elem[iElem]->GetNode(0) + 1 << " " << elem[iElem]->GetNode(1) + 1 << " "
+                   << elem[iElem]->GetNode(2) + 1 << " " << elem[iElem]->GetNode(3) + 1 << " "
+                   << elem[iElem]->GetNode(4) + 1 << " " << elem[iElem]->GetNode(5) + 1 << " "
+                   << elem[iElem]->GetNode(6) + 1 << " " << elem[iElem]->GetNode(7) + 1 << endl;
     }
     if (elem[iElem]->GetVTK_Type() == PYRAMID) {
-      Tecplot_File <<
-      elem[iElem]->GetNode(0)+1 <<" "<< elem[iElem]->GetNode(1)+1 <<" "<<
-      elem[iElem]->GetNode(2)+1 <<" "<< elem[iElem]->GetNode(3)+1 <<" "<<
-      elem[iElem]->GetNode(4)+1 <<" "<< elem[iElem]->GetNode(4)+1 <<" "<<
-      elem[iElem]->GetNode(4)+1 <<" "<< elem[iElem]->GetNode(4)+1 << endl;
+      Tecplot_File << elem[iElem]->GetNode(0) + 1 << " " << elem[iElem]->GetNode(1) + 1 << " "
+                   << elem[iElem]->GetNode(2) + 1 << " " << elem[iElem]->GetNode(3) + 1 << " "
+                   << elem[iElem]->GetNode(4) + 1 << " " << elem[iElem]->GetNode(4) + 1 << " "
+                   << elem[iElem]->GetNode(4) + 1 << " " << elem[iElem]->GetNode(4) + 1 << endl;
     }
     if (elem[iElem]->GetVTK_Type() == PRISM) {
-      Tecplot_File <<
-      elem[iElem]->GetNode(0)+1 <<" "<< elem[iElem]->GetNode(1)+1 <<" "<<
-      elem[iElem]->GetNode(1)+1 <<" "<< elem[iElem]->GetNode(2)+1 <<" "<<
-      elem[iElem]->GetNode(3)+1 <<" "<< elem[iElem]->GetNode(4)+1 <<" "<<
-      elem[iElem]->GetNode(4)+1 <<" "<< elem[iElem]->GetNode(5)+1 << endl;
+      Tecplot_File << elem[iElem]->GetNode(0) + 1 << " " << elem[iElem]->GetNode(1) + 1 << " "
+                   << elem[iElem]->GetNode(1) + 1 << " " << elem[iElem]->GetNode(2) + 1 << " "
+                   << elem[iElem]->GetNode(3) + 1 << " " << elem[iElem]->GetNode(4) + 1 << " "
+                   << elem[iElem]->GetNode(4) + 1 << " " << elem[iElem]->GetNode(5) + 1 << endl;
     }
   }
 
   Tecplot_File.close();
 }
 
-void CPhysicalGeometry::SetBoundTecPlot(char mesh_filename[MAX_STRING_SIZE], bool new_file, CConfig *config) {
-
+void CPhysicalGeometry::SetBoundTecPlot(char mesh_filename[MAX_STRING_SIZE], bool new_file, CConfig* config) {
   ofstream Tecplot_File;
   unsigned long iPoint, Total_nElem_Bound, iElem, *PointSurface = nullptr, nPointSurface = 0;
   unsigned short Coord_i, iMarker;
@@ -7984,35 +7631,33 @@ void CPhysicalGeometry::SetBoundTecPlot(char mesh_filename[MAX_STRING_SIZE], boo
     Tecplot_File << "TITLE= \"Visualization of the surface grid\"" << endl;
     if (nDim == 2) Tecplot_File << "VARIABLES = \"x\",\"y\" " << endl;
     if (nDim == 3) Tecplot_File << "VARIABLES = \"x\",\"y\",\"z\" " << endl;
-  }
-  else Tecplot_File.open(mesh_filename, ios::out | ios::app);
+  } else
+    Tecplot_File.open(mesh_filename, ios::out | ios::app);
 
   if (Total_nElem_Bound != 0) {
-
     /*--- Write the header of the file ---*/
 
     Tecplot_File << "ZONE T= ";
-    if (new_file) Tecplot_File << "\"Original grid\", C=BLACK, ";
-    else Tecplot_File << "\"Deformed grid\", C=RED, ";
-    Tecplot_File << "NODES= "<< nPointSurface <<", ELEMENTS= "<< Total_nElem_Bound <<", DATAPACKING= POINT";
-    if (nDim == 2) Tecplot_File << ", ZONETYPE= FELINESEG"<< endl;
-    if (nDim == 3) Tecplot_File << ", ZONETYPE= FEQUADRILATERAL"<< endl;
+    if (new_file)
+      Tecplot_File << "\"Original grid\", C=BLACK, ";
+    else
+      Tecplot_File << "\"Deformed grid\", C=RED, ";
+    Tecplot_File << "NODES= " << nPointSurface << ", ELEMENTS= " << Total_nElem_Bound << ", DATAPACKING= POINT";
+    if (nDim == 2) Tecplot_File << ", ZONETYPE= FELINESEG" << endl;
+    if (nDim == 3) Tecplot_File << ", ZONETYPE= FEQUADRILATERAL" << endl;
 
     /*--- Only write the coordiantes of the points that are on the surfaces ---*/
 
     if (nDim == 3) {
       for (iPoint = 0; iPoint < nPoint; iPoint++)
         if (nodes->GetBoundary(iPoint)) {
-          for (Coord_i = 0; Coord_i < nDim-1; Coord_i++)
-            Tecplot_File << nodes->GetCoord(iPoint, Coord_i) << " ";
-          Tecplot_File << nodes->GetCoord(iPoint, nDim-1) << "\n";
+          for (Coord_i = 0; Coord_i < nDim - 1; Coord_i++) Tecplot_File << nodes->GetCoord(iPoint, Coord_i) << " ";
+          Tecplot_File << nodes->GetCoord(iPoint, nDim - 1) << "\n";
         }
-    }
-    else {
+    } else {
       for (iPoint = 0; iPoint < nPoint; iPoint++)
         if (nodes->GetBoundary(iPoint)) {
-          for (Coord_i = 0; Coord_i < nDim; Coord_i++)
-            Tecplot_File << nodes->GetCoord(iPoint, Coord_i) << " ";
+          for (Coord_i = 0; Coord_i < nDim; Coord_i++) Tecplot_File << nodes->GetCoord(iPoint, Coord_i) << " ";
           Tecplot_File << "\n";
         }
     }
@@ -8023,38 +7668,36 @@ void CPhysicalGeometry::SetBoundTecPlot(char mesh_filename[MAX_STRING_SIZE], boo
       if (config->GetMarker_All_Plotting(iMarker) == YES)
         for (iElem = 0; iElem < nElem_Bound[iMarker]; iElem++) {
           if (nDim == 2) {
-            Tecplot_File << PointSurface[bound[iMarker][iElem]->GetNode(0)]+1 << " "
-            << PointSurface[bound[iMarker][iElem]->GetNode(1)]+1 << endl;
+            Tecplot_File << PointSurface[bound[iMarker][iElem]->GetNode(0)] + 1 << " "
+                         << PointSurface[bound[iMarker][iElem]->GetNode(1)] + 1 << endl;
           }
           if (nDim == 3) {
             if (bound[iMarker][iElem]->GetnNodes() == 3) {
-              Tecplot_File << PointSurface[bound[iMarker][iElem]->GetNode(0)]+1 << " "
-              << PointSurface[bound[iMarker][iElem]->GetNode(1)]+1 << " "
-              << PointSurface[bound[iMarker][iElem]->GetNode(2)]+1 << " "
-              << PointSurface[bound[iMarker][iElem]->GetNode(2)]+1 << endl;
+              Tecplot_File << PointSurface[bound[iMarker][iElem]->GetNode(0)] + 1 << " "
+                           << PointSurface[bound[iMarker][iElem]->GetNode(1)] + 1 << " "
+                           << PointSurface[bound[iMarker][iElem]->GetNode(2)] + 1 << " "
+                           << PointSurface[bound[iMarker][iElem]->GetNode(2)] + 1 << endl;
             }
             if (bound[iMarker][iElem]->GetnNodes() == 4) {
-              Tecplot_File << PointSurface[bound[iMarker][iElem]->GetNode(0)]+1 << " "
-              << PointSurface[bound[iMarker][iElem]->GetNode(1)]+1 << " "
-              << PointSurface[bound[iMarker][iElem]->GetNode(2)]+1 << " "
-              << PointSurface[bound[iMarker][iElem]->GetNode(3)]+1 << endl;
+              Tecplot_File << PointSurface[bound[iMarker][iElem]->GetNode(0)] + 1 << " "
+                           << PointSurface[bound[iMarker][iElem]->GetNode(1)] + 1 << " "
+                           << PointSurface[bound[iMarker][iElem]->GetNode(2)] + 1 << " "
+                           << PointSurface[bound[iMarker][iElem]->GetNode(3)] + 1 << endl;
             }
           }
         }
-  }
-  else {
-
+  } else {
     /*--- No elements in the surface ---*/
 
     if (nDim == 2) {
-      Tecplot_File << "ZONE NODES= 1, ELEMENTS= 1, DATAPACKING=POINT, ZONETYPE=FELINESEG"<< endl;
-      Tecplot_File << "0.0 0.0"<< endl;
-      Tecplot_File << "1 1"<< endl;
+      Tecplot_File << "ZONE NODES= 1, ELEMENTS= 1, DATAPACKING=POINT, ZONETYPE=FELINESEG" << endl;
+      Tecplot_File << "0.0 0.0" << endl;
+      Tecplot_File << "1 1" << endl;
     }
     if (nDim == 3) {
-      Tecplot_File << "ZONE NODES= 1, ELEMENTS= 1, DATAPACKING=POINT, ZONETYPE=FEQUADRILATERAL"<< endl;
-      Tecplot_File << "0.0 0.0 0.0"<< endl;
-      Tecplot_File << "1 1 1 1"<< endl;
+      Tecplot_File << "ZONE NODES= 1, ELEMENTS= 1, DATAPACKING=POINT, ZONETYPE=FEQUADRILATERAL" << endl;
+      Tecplot_File << "0.0 0.0 0.0" << endl;
+      Tecplot_File << "1 1 1 1" << endl;
     }
   }
 
@@ -8062,11 +7705,9 @@ void CPhysicalGeometry::SetBoundTecPlot(char mesh_filename[MAX_STRING_SIZE], boo
 
   delete[] PointSurface;
   Tecplot_File.close();
-
 }
 
-void CPhysicalGeometry::SetColorGrid_Parallel(const CConfig *config) {
-
+void CPhysicalGeometry::SetColorGrid_Parallel(const CConfig* config) {
   /*--- We need to have parallel support with MPI and have the ParMETIS
    library compiled and linked for parallel graph partitioning. ---*/
 
@@ -8080,27 +7721,27 @@ void CPhysicalGeometry::SetColorGrid_Parallel(const CConfig *config) {
 
   /*--- Linear partitioner object to help prepare parmetis data. ---*/
 
-  CLinearPartitioner pointPartitioner(Global_nPointDomain,0);
+  CLinearPartitioner pointPartitioner(Global_nPointDomain, 0);
 
   /*--- Some recommended defaults for the various ParMETIS options. ---*/
 
   idx_t wgtflag = 2;
   idx_t numflag = 0;
-  idx_t ncon    = 1;
-  real_t ubvec  = 1.0 + config->GetParMETIS_Tolerance();
-  idx_t nparts  = size;
+  idx_t ncon = 1;
+  real_t ubvec = 1.0 + config->GetParMETIS_Tolerance();
+  idx_t nparts = size;
   idx_t options[METIS_NOPTIONS];
   METIS_SetDefaultOptions(options);
   options[1] = 0;
 
   /*--- Fill the necessary ParMETIS input data arrays. ---*/
 
-  vector<real_t> tpwgts(size, 1.0/size);
+  vector<real_t> tpwgts(size, 1.0 / size);
 
-  vector<idx_t> vtxdist(size+1);
+  vector<idx_t> vtxdist(size + 1);
   vtxdist[0] = 0;
   for (int i = 0; i < size; i++) {
-    vtxdist[i+1] = pointPartitioner.GetLastIndexOnRank(i);
+    vtxdist[i + 1] = pointPartitioner.GetLastIndexOnRank(i);
   }
 
   /*--- For most FVM-type operations the amount of work is proportional to the
@@ -8114,7 +7755,7 @@ void CPhysicalGeometry::SetColorGrid_Parallel(const CConfig *config) {
 
   vector<idx_t> vwgt(nPoint);
   for (unsigned long iPoint = 0; iPoint < nPoint; ++iPoint) {
-    vwgt[iPoint] = wp + we * (xadj[iPoint+1] - xadj[iPoint]);
+    vwgt[iPoint] = wp + we * (xadj[iPoint + 1] - xadj[iPoint]);
   }
 
   /*--- Create some structures that ParMETIS needs to output the partitioning. ---*/
@@ -8125,9 +7766,9 @@ void CPhysicalGeometry::SetColorGrid_Parallel(const CConfig *config) {
   /*--- Calling ParMETIS ---*/
 
   if (rank == MASTER_NODE) cout << "Calling ParMETIS...";
-  auto err = ParMETIS_V3_PartKway(vtxdist.data(), xadj.data(), adjacency.data(), vwgt.data(),
-                                  nullptr, &wgtflag, &numflag, &ncon, &nparts, tpwgts.data(),
-                                  &ubvec, options, &edgecut, part.data(), &comm);
+  auto err =
+      ParMETIS_V3_PartKway(vtxdist.data(), xadj.data(), adjacency.data(), vwgt.data(), nullptr, &wgtflag, &numflag,
+                           &ncon, &nparts, tpwgts.data(), &ubvec, options, &edgecut, part.data(), &comm);
   if (err != METIS_OK) SU2_MPI::Error("Partitioning failed.", CURRENT_FUNCTION);
   if (rank == MASTER_NODE) {
     cout << " graph partitioning complete (" << edgecut << " edge cuts)." << endl;
@@ -8149,32 +7790,30 @@ void CPhysicalGeometry::SetColorGrid_Parallel(const CConfig *config) {
 #endif
 }
 
-void CPhysicalGeometry::ComputeMeshQualityStatistics(const CConfig *config) {
-
+void CPhysicalGeometry::ComputeMeshQualityStatistics(const CConfig* config) {
   /*--- Resize our vectors for the 3 metrics: orthogonality, aspect
    ratio, and volume ratio. All are vertex-based for the dual CV. ---*/
 
-  Orthogonality.resize(nPoint,0.0);
-  Aspect_Ratio.resize(nPoint,0.0);
-  Volume_Ratio.resize(nPoint,0.0);
+  Orthogonality.resize(nPoint, 0.0);
+  Aspect_Ratio.resize(nPoint, 0.0);
+  Volume_Ratio.resize(nPoint, 0.0);
 
   /*--- Helper vectors for holding intermediate values. ---*/
 
-  vector<su2double> SurfaceArea(nPoint,0.0);
-  vector<su2double> Area_Max(nPoint,0.0);
-  vector<su2double> Area_Min(nPoint,1.e6);
-  vector<su2double> SubVolume_Max(nPoint,0.0);
-  vector<su2double> SubVolume_Min(nPoint,1.e6);
+  vector<su2double> SurfaceArea(nPoint, 0.0);
+  vector<su2double> Area_Max(nPoint, 0.0);
+  vector<su2double> Area_Min(nPoint, 1.e6);
+  vector<su2double> SubVolume_Max(nPoint, 0.0);
+  vector<su2double> SubVolume_Min(nPoint, 1.e6);
 
   /*--- Orthogonality and aspect ratio (areas) are computed by
    looping over all edges to check the angles and the face areas. ---*/
 
   for (unsigned long iEdge = 0; iEdge < nEdge; iEdge++) {
-
     /*--- Point identification, edge normal vector and area ---*/
 
-    const unsigned long iPoint = edges->GetNode(iEdge,0);
-    const unsigned long jPoint = edges->GetNode(iEdge,1);
+    const unsigned long iPoint = edges->GetNode(iEdge, 0);
+    const unsigned long jPoint = edges->GetNode(iEdge, 1);
 
     const unsigned long GlobalIndex_i = nodes->GetGlobalIndex(iPoint);
     const unsigned long GlobalIndex_j = nodes->GetGlobalIndex(jPoint);
@@ -8183,26 +7822,26 @@ void CPhysicalGeometry::ComputeMeshQualityStatistics(const CConfig *config) {
      is computed by summing the normals of adjacent faces along
      the edge between iPoint & jPoint. ---*/
 
-    const su2double *Normal = edges->GetNormal(iEdge);
+    const su2double* Normal = edges->GetNormal(iEdge);
 
     /*--- Get the coordinates for point i & j. ---*/
 
-    const su2double *Coord_i = nodes->GetCoord(iPoint);
-    const su2double *Coord_j = nodes->GetCoord(jPoint);
+    const su2double* Coord_i = nodes->GetCoord(iPoint);
+    const su2double* Coord_j = nodes->GetCoord(jPoint);
 
     /*--- Compute the vector pointing from iPoint to jPoint and
      its distance. We also compute face area (norm of the normal vector). ---*/
 
     su2double distance = 0.0;
-    su2double area     = 0.0;
+    su2double area = 0.0;
     vector<su2double> edgeVector(nDim);
     for (unsigned short iDim = 0; iDim < nDim; iDim++) {
-      edgeVector[iDim] = Coord_j[iDim]-Coord_i[iDim];
-      distance        += edgeVector[iDim]*edgeVector[iDim];
-      area            += Normal[iDim]*Normal[iDim];
+      edgeVector[iDim] = Coord_j[iDim] - Coord_i[iDim];
+      distance += edgeVector[iDim] * edgeVector[iDim];
+      area += Normal[iDim] * Normal[iDim];
     }
     distance = sqrt(distance);
-    area     = sqrt(area);
+    area = sqrt(area);
 
     /*--- Aspect ratio is the ratio between the largest and smallest
      faces making up the boundary of the dual CV and is a measure
@@ -8221,8 +7860,7 @@ void CPhysicalGeometry::ComputeMeshQualityStatistics(const CConfig *config) {
 
     if (area <= 0.0) {
       char buf[200];
-      SPRINTF(buf, "Zero-area CV face found for edge (%lu,%lu).",
-              GlobalIndex_i, GlobalIndex_j);
+      SPRINTF(buf, "Zero-area CV face found for edge (%lu,%lu).", GlobalIndex_i, GlobalIndex_j);
       SU2_MPI::Error(string(buf), CURRENT_FUNCTION);
     }
 
@@ -8231,7 +7869,7 @@ void CPhysicalGeometry::ComputeMeshQualityStatistics(const CConfig *config) {
 
     su2double dotProduct = 0.0;
     for (unsigned short iDim = 0; iDim < nDim; iDim++) {
-      dotProduct += (Normal[iDim]/area)*(edgeVector[iDim]/distance);
+      dotProduct += (Normal[iDim] / area) * (edgeVector[iDim] / distance);
     }
 
     /*--- The definition of orthogonality is an area-weighted average of
@@ -8242,12 +7880,12 @@ void CPhysicalGeometry::ComputeMeshQualityStatistics(const CConfig *config) {
      are close to 90 degress, poor values are typically below 20 degress. ---*/
 
     if (nodes->GetDomain(iPoint)) {
-      Orthogonality[iPoint] += area*(90.0 - acos(dotProduct)*180.0/PI_NUMBER);
-      SurfaceArea[iPoint]   += area;
+      Orthogonality[iPoint] += area * (90.0 - acos(dotProduct) * 180.0 / PI_NUMBER);
+      SurfaceArea[iPoint] += area;
     }
     if (nodes->GetDomain(jPoint)) {
-      Orthogonality[jPoint] += area*(90.0 - acos(dotProduct)*180.0/PI_NUMBER);
-      SurfaceArea[jPoint]   += area;
+      Orthogonality[jPoint] += area * (90.0 - acos(dotProduct) * 180.0 / PI_NUMBER);
+      SurfaceArea[jPoint] += area;
     }
 
     /*--- Error check for zero volume of the dual CVs. ---*/
@@ -8263,33 +7901,28 @@ void CPhysicalGeometry::ComputeMeshQualityStatistics(const CConfig *config) {
       SPRINTF(buf, "Zero-area CV face found for point %lu.", GlobalIndex_j);
       SU2_MPI::Error(string(buf), CURRENT_FUNCTION);
     }
-
   }
 
   /*--- Loop boundary edges to include the area of the boundary elements.  ---*/
 
   for (unsigned short iMarker = 0; iMarker < nMarker; iMarker++) {
     if ((config->GetMarker_All_KindBC(iMarker) != INTERNAL_BOUNDARY) &&
-        (config->GetMarker_All_KindBC(iMarker) != SEND_RECEIVE)){
-
+        (config->GetMarker_All_KindBC(iMarker) != SEND_RECEIVE)) {
       for (unsigned long iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
         const unsigned long iPoint = vertex[iMarker][iVertex]->GetNode();
-        const su2double *Normal    = vertex[iMarker][iVertex]->GetNormal();
+        const su2double* Normal = vertex[iMarker][iVertex]->GetNormal();
 
         if (nodes->GetDomain(iPoint)) {
-
           /*--- Face area (norm of the normal vector) ---*/
 
           su2double area = 0.0;
-          for (unsigned short iDim = 0; iDim < nDim; iDim++)
-            area += Normal[iDim]*Normal[iDim];
+          for (unsigned short iDim = 0; iDim < nDim; iDim++) area += Normal[iDim] * Normal[iDim];
           area = sqrt(area);
 
           /*--- Check to store the area as the min or max for i or j. ---*/
 
           Area_Min[iPoint] = min(Area_Min[iPoint], area);
           Area_Max[iPoint] = max(Area_Max[iPoint], area);
-
         }
       }
     }
@@ -8302,7 +7935,6 @@ void CPhysicalGeometry::ComputeMeshQualityStatistics(const CConfig *config) {
    is better (closer to isotropic). ----*/
 
   for (unsigned long iElem = 0; iElem < nElem; iElem++) {
-
     /*--- Get pointers to the coordinates of all the element nodes ---*/
     array<const su2double*, N_POINTS_MAXIMUM> Coord;
 
@@ -8314,7 +7946,6 @@ void CPhysicalGeometry::ComputeMeshQualityStatistics(const CConfig *config) {
     const su2double* Coord_Elem_CG = elem[iElem]->GetCG();
 
     for (unsigned short iFace = 0; iFace < elem[iElem]->GetnFaces(); iFace++) {
-
       /*--- In 2D all the faces have only one edge ---*/
       unsigned short nEdgesFace = 1;
 
@@ -8327,23 +7958,21 @@ void CPhysicalGeometry::ComputeMeshQualityStatistics(const CConfig *config) {
         for (unsigned short iNode = 0; iNode < nEdgesFace; iNode++) {
           auto NodeFace = elem[iElem]->GetFaces(iFace, iNode);
           for (unsigned short iDim = 0; iDim < nDim; iDim++)
-            Coord_FaceElem_CG[iDim] += Coord[NodeFace][iDim]/nEdgesFace;
+            Coord_FaceElem_CG[iDim] += Coord[NodeFace][iDim] / nEdgesFace;
         }
       }
 
       /*-- Loop over the edges of a face ---*/
       for (unsigned short iEdgesFace = 0; iEdgesFace < nEdgesFace; iEdgesFace++) {
-
-        const auto face_iNode = elem[iElem]->GetFaces(iFace,iEdgesFace);
+        const auto face_iNode = elem[iElem]->GetFaces(iFace, iEdgesFace);
         unsigned short face_jNode;
 
         if (nDim == 2) {
           /*--- In 2D only one edge (two points) per edge ---*/
-          face_jNode = elem[iElem]->GetFaces(iFace,1);
-        }
-        else {
+          face_jNode = elem[iElem]->GetFaces(iFace, 1);
+        } else {
           /*--- In 3D we "circle around" the face ---*/
-          face_jNode = elem[iElem]->GetFaces(iFace, (iEdgesFace+1)%nEdgesFace);
+          face_jNode = elem[iElem]->GetFaces(iFace, (iEdgesFace + 1) % nEdgesFace);
         }
 
         const auto face_iPoint = elem[iElem]->GetNode(face_iNode);
@@ -8360,12 +7989,9 @@ void CPhysicalGeometry::ComputeMeshQualityStatistics(const CConfig *config) {
         if (nDim == 2) {
           Volume_i = CEdge::GetVolume(Coord[face_iNode], Coord_Edge_CG, Coord_Elem_CG);
           Volume_j = CEdge::GetVolume(Coord[face_jNode], Coord_Edge_CG, Coord_Elem_CG);
-        }
-        else {
-          Volume_i = CEdge::GetVolume(Coord[face_iNode], Coord_Edge_CG,
-                                      Coord_FaceElem_CG, Coord_Elem_CG);
-          Volume_j = CEdge::GetVolume(Coord[face_jNode], Coord_Edge_CG,
-                                      Coord_FaceElem_CG, Coord_Elem_CG);
+        } else {
+          Volume_i = CEdge::GetVolume(Coord[face_iNode], Coord_Edge_CG, Coord_FaceElem_CG, Coord_Elem_CG);
+          Volume_j = CEdge::GetVolume(Coord[face_jNode], Coord_Edge_CG, Coord_FaceElem_CG, Coord_Elem_CG);
         }
 
         /*--- Check if sub-elem volume is the min or max for iPoint. ---*/
@@ -8381,7 +8007,6 @@ void CPhysicalGeometry::ComputeMeshQualityStatistics(const CConfig *config) {
           SubVolume_Min[face_jPoint] = min(SubVolume_Min[face_jPoint], Volume_j);
           SubVolume_Max[face_jPoint] = max(SubVolume_Max[face_jPoint], Volume_j);
         }
-
       }
     }
   }
@@ -8390,17 +8015,17 @@ void CPhysicalGeometry::ComputeMeshQualityStatistics(const CConfig *config) {
    compute the local min and max values here for reporting. ---*/
 
   su2double orthoMin = 1.e6, arMin = 1.e6, vrMin = 1.e6;
-  su2double orthoMax = 0.0,  arMax = 0.0,  vrMax = 0.0;
-  for (unsigned long iPoint= 0; iPoint < nPointDomain; iPoint++) {
-    Orthogonality[iPoint] = Orthogonality[iPoint]/SurfaceArea[iPoint];
+  su2double orthoMax = 0.0, arMax = 0.0, vrMax = 0.0;
+  for (unsigned long iPoint = 0; iPoint < nPointDomain; iPoint++) {
+    Orthogonality[iPoint] = Orthogonality[iPoint] / SurfaceArea[iPoint];
     orthoMin = min(Orthogonality[iPoint], orthoMin);
     orthoMax = max(Orthogonality[iPoint], orthoMax);
 
-    Aspect_Ratio[iPoint] = Area_Max[iPoint]/Area_Min[iPoint];
+    Aspect_Ratio[iPoint] = Area_Max[iPoint] / Area_Min[iPoint];
     arMin = min(Aspect_Ratio[iPoint], arMin);
     arMax = max(Aspect_Ratio[iPoint], arMax);
 
-    Volume_Ratio[iPoint] = SubVolume_Max[iPoint]/SubVolume_Min[iPoint];
+    Volume_Ratio[iPoint] = SubVolume_Max[iPoint] / SubVolume_Min[iPoint];
     vrMin = min(Volume_Ratio[iPoint], vrMin);
     vrMax = max(Volume_Ratio[iPoint], vrMax);
   }
@@ -8408,22 +8033,16 @@ void CPhysicalGeometry::ComputeMeshQualityStatistics(const CConfig *config) {
   /*--- Reduction to find the min and max values globally. ---*/
 
   su2double Global_Ortho_Min, Global_Ortho_Max;
-  SU2_MPI::Allreduce(&orthoMin, &Global_Ortho_Min, 1,
-                     MPI_DOUBLE, MPI_MIN, SU2_MPI::GetComm());
-  SU2_MPI::Allreduce(&orthoMax, &Global_Ortho_Max, 1,
-                     MPI_DOUBLE, MPI_MAX, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&orthoMin, &Global_Ortho_Min, 1, MPI_DOUBLE, MPI_MIN, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&orthoMax, &Global_Ortho_Max, 1, MPI_DOUBLE, MPI_MAX, SU2_MPI::GetComm());
 
   su2double Global_AR_Min, Global_AR_Max;
-  SU2_MPI::Allreduce(&arMin, &Global_AR_Min, 1,
-                     MPI_DOUBLE, MPI_MIN, SU2_MPI::GetComm());
-  SU2_MPI::Allreduce(&arMax, &Global_AR_Max, 1,
-                     MPI_DOUBLE, MPI_MAX, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&arMin, &Global_AR_Min, 1, MPI_DOUBLE, MPI_MIN, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&arMax, &Global_AR_Max, 1, MPI_DOUBLE, MPI_MAX, SU2_MPI::GetComm());
 
   su2double Global_VR_Min, Global_VR_Max;
-  SU2_MPI::Allreduce(&vrMin, &Global_VR_Min, 1,
-                     MPI_DOUBLE, MPI_MIN, SU2_MPI::GetComm());
-  SU2_MPI::Allreduce(&vrMax, &Global_VR_Max, 1,
-                     MPI_DOUBLE, MPI_MAX, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&vrMin, &Global_VR_Min, 1, MPI_DOUBLE, MPI_MIN, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&vrMax, &Global_VR_Max, 1, MPI_DOUBLE, MPI_MAX, SU2_MPI::GetComm());
 
   /*--- Print the summary to the console for the user. ---*/
 
@@ -8431,7 +8050,7 @@ void CPhysicalGeometry::ComputeMeshQualityStatistics(const CConfig *config) {
   MetricsTable.AddColumn("Mesh Quality Metric", 30);
   MetricsTable.AddColumn("Minimum", 15);
   MetricsTable.AddColumn("Maximum", 15);
-  if (rank == MASTER_NODE){
+  if (rank == MASTER_NODE) {
     MetricsTable.PrintHeader();
     MetricsTable << "Orthogonality Angle (deg.)" << Global_Ortho_Min << Global_Ortho_Max;
     MetricsTable << "CV Face Area Aspect Ratio" << Global_AR_Min << Global_AR_Max;
@@ -8447,40 +8066,39 @@ void CPhysicalGeometry::ComputeMeshQualityStatistics(const CConfig *config) {
     vector<su2double>().swap(Aspect_Ratio);
     vector<su2double>().swap(Volume_Ratio);
   }
-
 }
 
-void CPhysicalGeometry::FindNormal_Neighbor(const CConfig *config) {
+void CPhysicalGeometry::FindNormal_Neighbor(const CConfig* config) {
   su2double cos_max, scalar_prod, norm_vect, norm_Normal, cos_alpha, diff_coord, *Normal;
   unsigned long Point_Normal, jPoint;
   unsigned short iNeigh, iMarker, iDim;
   unsigned long iPoint, iVertex;
 
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-
     if (config->GetMarker_All_KindBC(iMarker) != SEND_RECEIVE &&
         config->GetMarker_All_KindBC(iMarker) != INTERNAL_BOUNDARY &&
-        config->GetMarker_All_KindBC(iMarker) != NEARFIELD_BOUNDARY ) {
-
+        config->GetMarker_All_KindBC(iMarker) != NEARFIELD_BOUNDARY) {
       for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
-
         iPoint = vertex[iMarker][iVertex]->GetNode();
         Normal = vertex[iMarker][iVertex]->GetNormal();
 
         /*--- Compute closest normal neighbor, note that the normal are oriented inwards ---*/
-        Point_Normal = 0; cos_max = -1.0;
+        Point_Normal = 0;
+        cos_max = -1.0;
         for (iNeigh = 0; iNeigh < nodes->GetnPoint(iPoint); iNeigh++) {
           jPoint = nodes->GetPoint(iPoint, iNeigh);
-          scalar_prod = 0.0; norm_vect = 0.0; norm_Normal = 0.0;
+          scalar_prod = 0.0;
+          norm_vect = 0.0;
+          norm_Normal = 0.0;
           for (iDim = 0; iDim < nDim; iDim++) {
-            diff_coord = nodes->GetCoord(jPoint, iDim)-nodes->GetCoord(iPoint, iDim);
-            scalar_prod += diff_coord*Normal[iDim];
-            norm_vect += diff_coord*diff_coord;
-            norm_Normal += Normal[iDim]*Normal[iDim];
+            diff_coord = nodes->GetCoord(jPoint, iDim) - nodes->GetCoord(iPoint, iDim);
+            scalar_prod += diff_coord * Normal[iDim];
+            norm_vect += diff_coord * diff_coord;
+            norm_Normal += Normal[iDim] * Normal[iDim];
           }
           norm_vect = sqrt(norm_vect);
           norm_Normal = sqrt(norm_Normal);
-          cos_alpha = scalar_prod/(norm_vect*norm_Normal);
+          cos_alpha = scalar_prod / (norm_vect * norm_Normal);
 
           /*--- Get maximum cosine ---*/
           if (cos_alpha >= cos_max) {
@@ -8494,11 +8112,11 @@ void CPhysicalGeometry::FindNormal_Neighbor(const CConfig *config) {
   }
 }
 
-void CPhysicalGeometry::SetBoundSensitivity(CConfig *config) {
+void CPhysicalGeometry::SetBoundSensitivity(CConfig* config) {
   unsigned short iMarker, icommas;
   unsigned long iVertex, iPoint, (*Point2Vertex)[2], nPointLocal = 0, nPointGlobal = 0;
   su2double Sensitivity;
-  bool *PointInDomain;
+  bool* PointInDomain;
 
   nPointLocal = nPoint;
   SU2_MPI::Allreduce(&nPointLocal, &nPointGlobal, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
@@ -8506,13 +8124,11 @@ void CPhysicalGeometry::SetBoundSensitivity(CConfig *config) {
   Point2Vertex = new unsigned long[nPointGlobal][2];
   PointInDomain = new bool[nPointGlobal];
 
-  for (iPoint = 0; iPoint < nPointGlobal; iPoint ++)
-    PointInDomain[iPoint] = false;
+  for (iPoint = 0; iPoint < nPointGlobal; iPoint++) PointInDomain[iPoint] = false;
 
   for (iMarker = 0; iMarker < nMarker; iMarker++)
     if (config->GetMarker_All_DV(iMarker) == YES)
       for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
-
         /*--- The sensitivity file uses the global numbering ---*/
         iPoint = nodes->GetGlobalIndex(vertex[iMarker][iVertex]->GetNode());
 
@@ -8530,25 +8146,23 @@ void CPhysicalGeometry::SetBoundSensitivity(CConfig *config) {
   su2double delta_T, total_T;
   if ((config->GetTime_Marching() != TIME_MARCHING::STEADY) && config->GetTime_Domain()) {
     nTimeIter = config->GetUnst_AdjointIter();
-    delta_T  = config->GetTime_Step();
-    total_T  = (su2double)nTimeIter*delta_T;
+    delta_T = config->GetTime_Step();
+    total_T = (su2double)nTimeIter * delta_T;
   } else if (config->GetTime_Marching() == TIME_MARCHING::HARMONIC_BALANCE) {
-
     /*--- Compute period of oscillation & compute time interval using nTimeInstances ---*/
 
     su2double period = config->GetHarmonicBalance_Period();
-    nTimeIter  = config->GetnTimeInstances();
-    delta_T   = period/(su2double)nTimeIter;
-    total_T   = period;
+    nTimeIter = config->GetnTimeInstances();
+    delta_T = period / (su2double)nTimeIter;
+    total_T = period;
 
   } else {
     nTimeIter = 1;
-    delta_T  = 1.0;
-    total_T  = 1.0;
+    delta_T = 1.0;
+    total_T = 1.0;
   }
 
   for (iTimeIter = 0; iTimeIter < nTimeIter; iTimeIter++) {
-
     /*--- Prepare to read surface sensitivity files (CSV) ---*/
 
     string text_line;
@@ -8556,24 +8170,27 @@ void CPhysicalGeometry::SetBoundSensitivity(CConfig *config) {
     char buffer[50];
     char cstr[MAX_STRING_SIZE];
     string surfadj_filename = config->GetSurfAdjCoeff_FileName();
-    strcpy (cstr, surfadj_filename.c_str());
+    strcpy(cstr, surfadj_filename.c_str());
 
     /*--- Write file name with extension if unsteady or steady ---*/
     if (config->GetTime_Marching() == TIME_MARCHING::HARMONIC_BALANCE)
-      SPRINTF (buffer, "_%d.csv", SU2_TYPE::Int(iTimeIter));
+      SPRINTF(buffer, "_%d.csv", SU2_TYPE::Int(iTimeIter));
 
     if (((config->GetTime_Marching() != TIME_MARCHING::STEADY) && config->GetTime_Domain()) ||
         (config->GetTime_Marching() == TIME_MARCHING::HARMONIC_BALANCE)) {
-      if ((SU2_TYPE::Int(iTimeIter) >= 0)    && (SU2_TYPE::Int(iTimeIter) < 10))    SPRINTF (buffer, "_0000%d.csv", SU2_TYPE::Int(iTimeIter));
-      if ((SU2_TYPE::Int(iTimeIter) >= 10)   && (SU2_TYPE::Int(iTimeIter) < 100))   SPRINTF (buffer, "_000%d.csv",  SU2_TYPE::Int(iTimeIter));
-      if ((SU2_TYPE::Int(iTimeIter) >= 100)  && (SU2_TYPE::Int(iTimeIter) < 1000))  SPRINTF (buffer, "_00%d.csv",   SU2_TYPE::Int(iTimeIter));
-      if ((SU2_TYPE::Int(iTimeIter) >= 1000) && (SU2_TYPE::Int(iTimeIter) < 10000)) SPRINTF (buffer, "_0%d.csv",    SU2_TYPE::Int(iTimeIter));
-      if (SU2_TYPE::Int(iTimeIter) >= 10000) SPRINTF (buffer, "_%d.csv", SU2_TYPE::Int(iTimeIter));
-    }
-    else
-      SPRINTF (buffer, ".csv");
-
-    strcat (cstr, buffer);
+      if ((SU2_TYPE::Int(iTimeIter) >= 0) && (SU2_TYPE::Int(iTimeIter) < 10))
+        SPRINTF(buffer, "_0000%d.csv", SU2_TYPE::Int(iTimeIter));
+      if ((SU2_TYPE::Int(iTimeIter) >= 10) && (SU2_TYPE::Int(iTimeIter) < 100))
+        SPRINTF(buffer, "_000%d.csv", SU2_TYPE::Int(iTimeIter));
+      if ((SU2_TYPE::Int(iTimeIter) >= 100) && (SU2_TYPE::Int(iTimeIter) < 1000))
+        SPRINTF(buffer, "_00%d.csv", SU2_TYPE::Int(iTimeIter));
+      if ((SU2_TYPE::Int(iTimeIter) >= 1000) && (SU2_TYPE::Int(iTimeIter) < 10000))
+        SPRINTF(buffer, "_0%d.csv", SU2_TYPE::Int(iTimeIter));
+      if (SU2_TYPE::Int(iTimeIter) >= 10000) SPRINTF(buffer, "_%d.csv", SU2_TYPE::Int(iTimeIter));
+    } else
+      SPRINTF(buffer, ".csv");
+
+    strcat(cstr, buffer);
 
     /*--- Read the sensitivity file ---*/
 
@@ -8590,13 +8207,13 @@ void CPhysicalGeometry::SetBoundSensitivity(CConfig *config) {
     char delimiter = ',';
     split_line = PrintingToolbox::split(text_line, delimiter);
 
-    for (unsigned short iField = 0; iField < split_line.size(); iField++){
+    for (unsigned short iField = 0; iField < split_line.size(); iField++) {
       PrintingToolbox::trim(split_line[iField]);
     }
 
     std::vector<string>::iterator it = std::find(split_line.begin(), split_line.end(), "\"Surface_Sensitivity\"");
 
-    if (it == split_line.end()){
+    if (it == split_line.end()) {
       SU2_MPI::Error("Surface sensitivity not found in file.", CURRENT_FUNCTION);
     }
 
@@ -8604,17 +8221,15 @@ void CPhysicalGeometry::SetBoundSensitivity(CConfig *config) {
 
     while (getline(Surface_file, text_line)) {
       for (icommas = 0; icommas < 50; icommas++) {
-        position = text_line.find( ",", 0 );
-        if (position!=string::npos) text_line.erase (position,1);
+        position = text_line.find(",", 0);
+        if (position != string::npos) text_line.erase(position, 1);
       }
-      stringstream  point_line(text_line);
+      stringstream point_line(text_line);
       point_line >> iPoint;
 
-      for (int i = 1; i <= sens_index; i++)
-        point_line >> Sensitivity;
+      for (int i = 1; i <= sens_index; i++) point_line >> Sensitivity;
 
       if (PointInDomain[iPoint]) {
-
         /*--- Find the vertex for the Point and Marker ---*/
 
         iMarker = Point2Vertex[iPoint][0];
@@ -8624,20 +8239,17 @@ void CPhysicalGeometry::SetBoundSensitivity(CConfig *config) {
          this unsteady timestep. For steady problems, this reduces to
          a single sensitivity value multiplied by 1.0. ---*/
 
-        vertex[iMarker][iVertex]->AddAuxVar(Sensitivity*(delta_T/total_T));
+        vertex[iMarker][iVertex]->AddAuxVar(Sensitivity * (delta_T / total_T));
       }
-
     }
     Surface_file.close();
   }
 
   delete[] Point2Vertex;
   delete[] PointInDomain;
-
 }
 
-void CPhysicalGeometry::SetSensitivity(CConfig *config) {
-
+void CPhysicalGeometry::SetSensitivity(CConfig* config) {
   ifstream restart_file;
   string filename = config->GetSolution_AdjFileName();
 
@@ -8647,19 +8259,20 @@ void CPhysicalGeometry::SetSensitivity(CConfig *config) {
   string::size_type position;
   int counter = 0;
 
-  Sensitivity.resize(nPoint,nDim) = su2double(0.0);
+  Sensitivity.resize(nPoint, nDim) = su2double(0.0);
 
   if (config->GetTime_Domain()) {
     nTimeIter = config->GetnTime_Iter();
-  }else {
+  } else {
     nTimeIter = 1;
   }
 
-  if (rank == MASTER_NODE)
-    cout << "Reading in sensitivity at iteration " << nTimeIter-1 << "."<< endl;
+  if (rank == MASTER_NODE) cout << "Reading in sensitivity at iteration " << nTimeIter - 1 << "." << endl;
 
   /*--- Read all lines in the restart file ---*/
-  long iPoint_Local; unsigned long iPoint_Global = 0; string text_line;
+  long iPoint_Local;
+  unsigned long iPoint_Global = 0;
+  string text_line;
 
   iPoint_Global = 0;
 
@@ -8667,27 +8280,25 @@ void CPhysicalGeometry::SetSensitivity(CConfig *config) {
 
   filename = config->GetObjFunc_Extension(filename);
 
-
   if (config->GetRead_Binary_Restart()) {
-
-    filename = config->GetFilename(filename, ".dat", nTimeIter-1);
+    filename = config->GetFilename(filename, ".dat", nTimeIter - 1);
 
     char str_buf[CGNS_STRING_SIZE], fname[100];
     unsigned short iVar;
     strcpy(fname, filename.c_str());
     int nRestart_Vars = 5, nFields;
-    int *Restart_Vars = new int[5];
-    passivedouble *Restart_Data = nullptr;
+    int* Restart_Vars = new int[5];
+    passivedouble* Restart_Data = nullptr;
     int Restart_Iter = 0;
-    passivedouble Restart_Meta_Passive[8] = {0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0};
-    su2double Restart_Meta[8] = {0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0};
+    passivedouble Restart_Meta_Passive[8] = {0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0};
+    su2double Restart_Meta[8] = {0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0};
 
 #ifndef HAVE_MPI
 
     /*--- Serial binary input. ---*/
 
-    FILE *fhw;
-    fhw = fopen(fname,"rb");
+    FILE* fhw;
+    fhw = fopen(fname, "rb");
     size_t ret;
 
     /*--- Error check for opening the file. ---*/
@@ -8708,9 +8319,10 @@ void CPhysicalGeometry::SetSensitivity(CConfig *config) {
 
     if (Restart_Vars[0] != 535532) {
       SU2_MPI::Error(string("File ") + string(fname) + string(" is not a binary SU2 restart file.\n") +
-                     string("SU2 reads/writes binary restart files by default.\n") +
-                     string("Note that backward compatibility for ASCII restart files is\n") +
-                     string("possible with the READ_BINARY_RESTART option."), CURRENT_FUNCTION);
+                         string("SU2 reads/writes binary restart files by default.\n") +
+                         string("Note that backward compatibility for ASCII restart files is\n") +
+                         string("possible with the READ_BINARY_RESTART option."),
+                     CURRENT_FUNCTION);
     }
 
     /*--- Store the number of fields for simplicity. ---*/
@@ -8733,19 +8345,19 @@ void CPhysicalGeometry::SetSensitivity(CConfig *config) {
 
     /*--- For now, create a temp 1D buffer to read the data from file. ---*/
 
-    Restart_Data = new passivedouble[nFields*GetnPointDomain()];
+    Restart_Data = new passivedouble[nFields * GetnPointDomain()];
 
     /*--- Read in the data for the restart at all local points. ---*/
 
-    ret = fread(Restart_Data, sizeof(passivedouble), nFields*GetnPointDomain(), fhw);
-    if (ret != (unsigned long)nFields*GetnPointDomain()) {
+    ret = fread(Restart_Data, sizeof(passivedouble), nFields * GetnPointDomain(), fhw);
+    if (ret != (unsigned long)nFields * GetnPointDomain()) {
       SU2_MPI::Error("Error reading restart file.", CURRENT_FUNCTION);
     }
 
     /*--- Compute (negative) displacements and grab the metadata. ---*/
 
-    ret = sizeof(int) + 8*sizeof(passivedouble);
-    fseek(fhw,-ret, SEEK_END);
+    ret = sizeof(int) + 8 * sizeof(passivedouble);
+    fseek(fhw, -ret, SEEK_END);
 
     /*--- Read the external iteration. ---*/
 
@@ -8792,8 +8404,7 @@ void CPhysicalGeometry::SetSensitivity(CConfig *config) {
      which we will need in order to read the file later. Also, read the
      variable string names here. Only the master rank reads the header. ---*/
 
-    if (rank == MASTER_NODE)
-      MPI_File_read(fhw, Restart_Vars, nRestart_Vars, MPI_INT, MPI_STATUS_IGNORE);
+    if (rank == MASTER_NODE) MPI_File_read(fhw, Restart_Vars, nRestart_Vars, MPI_INT, MPI_STATUS_IGNORE);
 
     /*--- Broadcast the number of variables to all procs and store clearly. ---*/
 
@@ -8803,11 +8414,11 @@ void CPhysicalGeometry::SetSensitivity(CConfig *config) {
      have the hex representation of "SU2" as the first int in the file. ---*/
 
     if (Restart_Vars[0] != 535532) {
-
       SU2_MPI::Error(string("File ") + string(fname) + string(" is not a binary SU2 restart file.\n") +
-                     string("SU2 reads/writes binary restart files by default.\n") +
-                     string("Note that backward compatibility for ASCII restart files is\n") +
-                     string("possible with the READ_BINARY_RESTART option."), CURRENT_FUNCTION);
+                         string("SU2 reads/writes binary restart files by default.\n") +
+                         string("Note that backward compatibility for ASCII restart files is\n") +
+                         string("possible with the READ_BINARY_RESTART option."),
+                     CURRENT_FUNCTION);
     }
 
     /*--- Store the number of fields for simplicity. ---*/
@@ -8818,24 +8429,22 @@ void CPhysicalGeometry::SetSensitivity(CConfig *config) {
      fixed length of 33 for the string length to match with CGNS. This is
      needed for when we read the strings later. ---*/
 
-    char *mpi_str_buf = new char[nFields*CGNS_STRING_SIZE];
+    char* mpi_str_buf = new char[nFields * CGNS_STRING_SIZE];
     if (rank == MASTER_NODE) {
-      disp = nRestart_Vars*sizeof(int);
-      MPI_File_read_at(fhw, disp, mpi_str_buf, nFields*CGNS_STRING_SIZE,
-                       MPI_CHAR, MPI_STATUS_IGNORE);
+      disp = nRestart_Vars * sizeof(int);
+      MPI_File_read_at(fhw, disp, mpi_str_buf, nFields * CGNS_STRING_SIZE, MPI_CHAR, MPI_STATUS_IGNORE);
     }
 
     /*--- Broadcast the string names of the variables. ---*/
 
-    SU2_MPI::Bcast(mpi_str_buf, nFields*CGNS_STRING_SIZE, MPI_CHAR,
-                   MASTER_NODE, SU2_MPI::GetComm());
+    SU2_MPI::Bcast(mpi_str_buf, nFields * CGNS_STRING_SIZE, MPI_CHAR, MASTER_NODE, SU2_MPI::GetComm());
 
     /*--- Now parse the string names and load into the config class in case
      we need them for writing visualization files (SU2_SOL). ---*/
 
     config->fields.push_back("Point_ID");
     for (iVar = 0; iVar < nFields; iVar++) {
-      index = iVar*CGNS_STRING_SIZE;
+      index = iVar * CGNS_STRING_SIZE;
       for (iChar = 0; iChar < (unsigned long)CGNS_STRING_SIZE; iChar++) {
         str_buf[iChar] = mpi_str_buf[index + iChar];
       }
@@ -8846,7 +8455,7 @@ void CPhysicalGeometry::SetSensitivity(CConfig *config) {
 
     /*--- Free string buffer memory. ---*/
 
-    delete [] mpi_str_buf;
+    delete[] mpi_str_buf;
 
     /*--- We're writing only su2doubles in the data portion of the file. ---*/
 
@@ -8855,20 +8464,20 @@ void CPhysicalGeometry::SetSensitivity(CConfig *config) {
     /*--- We need to ignore the 4 ints describing the nVar_Restart and nPoints,
      along with the string names of the variables. ---*/
 
-    disp = nRestart_Vars*sizeof(int) + CGNS_STRING_SIZE*nFields*sizeof(char);
+    disp = nRestart_Vars * sizeof(int) + CGNS_STRING_SIZE * nFields * sizeof(char);
 
     /*--- Define a derived datatype for this rank's set of non-contiguous data
      that will be placed in the restart. Here, we are collecting each one of the
      points which are distributed throughout the file in blocks of nVar_Restart data. ---*/
 
-    int *blocklen = new int[GetnPointDomain()];
-    MPI_Aint *displace = new MPI_Aint[GetnPointDomain()];
+    int* blocklen = new int[GetnPointDomain()];
+    MPI_Aint* displace = new MPI_Aint[GetnPointDomain()];
 
     counter = 0;
-    for (iPoint_Global = 0; iPoint_Global < GetGlobal_nPointDomain(); iPoint_Global++ ) {
+    for (iPoint_Global = 0; iPoint_Global < GetGlobal_nPointDomain(); iPoint_Global++) {
       if (GetGlobal_to_Local_Point(iPoint_Global) > -1) {
         blocklen[counter] = nFields;
-        displace[counter] = iPoint_Global*nFields*sizeof(passivedouble);
+        displace[counter] = iPoint_Global * nFields * sizeof(passivedouble);
         counter++;
       }
     }
@@ -8882,11 +8491,11 @@ void CPhysicalGeometry::SetSensitivity(CConfig *config) {
 
     /*--- For now, create a temp 1D buffer to read the data from file. ---*/
 
-    Restart_Data = new passivedouble[nFields*GetnPointDomain()];
+    Restart_Data = new passivedouble[nFields * GetnPointDomain()];
 
     /*--- Collective call for all ranks to read from their view simultaneously. ---*/
 
-    MPI_File_read_all(fhw, Restart_Data, nFields*GetnPointDomain(), MPI_DOUBLE, &status);
+    MPI_File_read_all(fhw, Restart_Data, nFields * GetnPointDomain(), MPI_DOUBLE, &status);
 
     /*--- Free the derived datatype. ---*/
 
@@ -8899,18 +8508,16 @@ void CPhysicalGeometry::SetSensitivity(CConfig *config) {
     /*--- Access the metadata. ---*/
 
     if (rank == MASTER_NODE) {
-
       /*--- External iteration. ---*/
-      disp = (nRestart_Vars*sizeof(int) + nFields*CGNS_STRING_SIZE*sizeof(char) +
-              nFields*Restart_Vars[2]*sizeof(passivedouble));
+      disp = (nRestart_Vars * sizeof(int) + nFields * CGNS_STRING_SIZE * sizeof(char) +
+              nFields * Restart_Vars[2] * sizeof(passivedouble));
       MPI_File_read_at(fhw, disp, &Restart_Iter, 1, MPI_INT, MPI_STATUS_IGNORE);
 
       /*--- Additional doubles for AoA, AoS, etc. ---*/
 
-      disp = (nRestart_Vars*sizeof(int) + nFields*CGNS_STRING_SIZE*sizeof(char) +
-              nFields*Restart_Vars[2]*sizeof(passivedouble) + 1*sizeof(int));
+      disp = (nRestart_Vars * sizeof(int) + nFields * CGNS_STRING_SIZE * sizeof(char) +
+              nFields * Restart_Vars[2] * sizeof(passivedouble) + 1 * sizeof(int));
       MPI_File_read_at(fhw, disp, Restart_Meta_Passive, 8, MPI_DOUBLE, MPI_STATUS_IGNORE);
-
     }
 
     /*--- Communicate metadata. ---*/
@@ -8920,8 +8527,7 @@ void CPhysicalGeometry::SetSensitivity(CConfig *config) {
     /*--- Copy to a su2double structure (because of the SU2_MPI::Bcast
               doesn't work with passive data)---*/
 
-    for (unsigned short iVar = 0; iVar < 8; iVar++)
-      Restart_Meta[iVar] = Restart_Meta_Passive[iVar];
+    for (unsigned short iVar = 0; iVar < 8; iVar++) Restart_Meta[iVar] = Restart_Meta_Passive[iVar];
 
     SU2_MPI::Bcast(Restart_Meta, 8, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
 
@@ -8929,8 +8535,8 @@ void CPhysicalGeometry::SetSensitivity(CConfig *config) {
 
     MPI_File_close(&fhw);
 
-    delete [] blocklen;
-    delete [] displace;
+    delete[] blocklen;
+    delete[] displace;
 
 #endif
 
@@ -8938,14 +8544,14 @@ void CPhysicalGeometry::SetSensitivity(CConfig *config) {
     std::vector<string>::iterator ity = std::find(config->fields.begin(), config->fields.end(), "Sensitivity_y");
     std::vector<string>::iterator itz = std::find(config->fields.begin(), config->fields.end(), "Sensitivity_z");
 
-    if (itx == config->fields.end()){
+    if (itx == config->fields.end()) {
       SU2_MPI::Error("Sensitivity x not found in file.", CURRENT_FUNCTION);
     }
-    if (ity == config->fields.end()){
+    if (ity == config->fields.end()) {
       SU2_MPI::Error("Sensitivity y not found in file.", CURRENT_FUNCTION);
     }
-    if (nDim == 3){
-      if (itz == config->fields.end()){
+    if (nDim == 3) {
+      if (itz == config->fields.end()) {
         SU2_MPI::Error("Sensitivity z not found in file.", CURRENT_FUNCTION);
       }
     }
@@ -8953,32 +8559,29 @@ void CPhysicalGeometry::SetSensitivity(CConfig *config) {
     unsigned short sens_x_idx = std::distance(config->fields.begin(), itx);
     unsigned short sens_y_idx = std::distance(config->fields.begin(), ity);
     unsigned short sens_z_idx = 0;
-    if (nDim == 3)
-      sens_z_idx = std::distance(config->fields.begin(), itz);
+    if (nDim == 3) sens_z_idx = std::distance(config->fields.begin(), itz);
 
     /*--- Load the data from the binary restart. ---*/
 
     counter = 0;
-    for (iPoint_Global = 0; iPoint_Global < GetGlobal_nPointDomain(); iPoint_Global++ ) {
-
+    for (iPoint_Global = 0; iPoint_Global < GetGlobal_nPointDomain(); iPoint_Global++) {
       /*--- Retrieve local index. If this node from the restart file lives
        on the current processor, we will load and instantiate the vars. ---*/
 
       iPoint_Local = GetGlobal_to_Local_Point(iPoint_Global);
 
       if (iPoint_Local > -1) {
-
         /*--- We need to store this point's data, so jump to the correct
          offset in the buffer of data from the restart file and load it. ---*/
 
-        index = counter*nFields + sens_x_idx - 1;
-        Sensitivity(iPoint_Local,0) = Restart_Data[index];
-        index = counter*nFields + sens_y_idx - 1;
-        Sensitivity(iPoint_Local,1) = Restart_Data[index];
+        index = counter * nFields + sens_x_idx - 1;
+        Sensitivity(iPoint_Local, 0) = Restart_Data[index];
+        index = counter * nFields + sens_y_idx - 1;
+        Sensitivity(iPoint_Local, 1) = Restart_Data[index];
 
-        if (nDim == 3){
-          index = counter*nFields + sens_z_idx - 1;
-          Sensitivity(iPoint_Local,2) = Restart_Data[index];
+        if (nDim == 3) {
+          index = counter * nFields + sens_z_idx - 1;
+          Sensitivity(iPoint_Local, 2) = Restart_Data[index];
         }
         /*--- Increment the overall counter for how many points have been loaded. ---*/
         counter++;
@@ -8990,8 +8593,7 @@ void CPhysicalGeometry::SetSensitivity(CConfig *config) {
     config->SetAoA_Sens(Restart_Meta[4]);
 
   } else {
-
-    filename = config->GetFilename(filename, ".csv", nTimeIter-1);
+    filename = config->GetFilename(filename, ".csv", nTimeIter - 1);
 
     /*--- First, check that this is not a binary restart file. ---*/
 
@@ -9003,8 +8605,8 @@ void CPhysicalGeometry::SetSensitivity(CConfig *config) {
 
     /*--- Serial binary input. ---*/
 
-    FILE *fhw;
-    fhw = fopen(fname,"rb");
+    FILE* fhw;
+    fhw = fopen(fname, "rb");
     size_t ret;
 
     /*--- Error check for opening the file. ---*/
@@ -9025,9 +8627,10 @@ void CPhysicalGeometry::SetSensitivity(CConfig *config) {
 
     if (magic_number == 535532) {
       SU2_MPI::Error(string("File ") + string(fname) + string(" is a binary SU2 restart file, expected ASCII.\n") +
-                     string("SU2 reads/writes binary restart files by default.\n") +
-                     string("Note that backward compatibility for ASCII restart files is\n") +
-                     string("possible with the READ_BINARY_RESTART option."), CURRENT_FUNCTION);
+                         string("SU2 reads/writes binary restart files by default.\n") +
+                         string("Note that backward compatibility for ASCII restart files is\n") +
+                         string("possible with the READ_BINARY_RESTART option."),
+                     CURRENT_FUNCTION);
     }
 
     fclose(fhw);
@@ -9051,8 +8654,7 @@ void CPhysicalGeometry::SetSensitivity(CConfig *config) {
 
     /*--- Have the master attempt to read the magic number. ---*/
 
-    if (rank == MASTER_NODE)
-      MPI_File_read(fhw, &magic_number, 1, MPI_INT, MPI_STATUS_IGNORE);
+    if (rank == MASTER_NODE) MPI_File_read(fhw, &magic_number, 1, MPI_INT, MPI_STATUS_IGNORE);
 
     /*--- Broadcast the number of variables to all procs and store clearly. ---*/
 
@@ -9062,93 +8664,86 @@ void CPhysicalGeometry::SetSensitivity(CConfig *config) {
      have the hex representation of "SU2" as the first int in the file. ---*/
 
     if (magic_number == 535532) {
-
       SU2_MPI::Error(string("File ") + string(fname) + string(" is a binary SU2 restart file, expected ASCII.\n") +
-                     string("SU2 reads/writes binary restart files by default.\n") +
-                     string("Note that backward compatibility for ASCII restart files is\n") +
-                     string("possible with the READ_BINARY_RESTART option."), CURRENT_FUNCTION);
+                         string("SU2 reads/writes binary restart files by default.\n") +
+                         string("Note that backward compatibility for ASCII restart files is\n") +
+                         string("possible with the READ_BINARY_RESTART option."),
+                     CURRENT_FUNCTION);
     }
 
     MPI_File_close(&fhw);
 
 #endif
 
-  restart_file.open(filename.data(), ios::in);
-  if (restart_file.fail()) {
-    SU2_MPI::Error(string("There is no adjoint restart file ") + filename, CURRENT_FUNCTION);
-  }
-
-  /*--- The first line is the header ---*/
-
-  getline (restart_file, text_line);
+    restart_file.open(filename.data(), ios::in);
+    if (restart_file.fail()) {
+      SU2_MPI::Error(string("There is no adjoint restart file ") + filename, CURRENT_FUNCTION);
+    }
 
-  vector<string> fields = PrintingToolbox::split(text_line, ',');
+    /*--- The first line is the header ---*/
 
-  for (unsigned short iField = 0; iField < fields.size(); iField++){
-    PrintingToolbox::trim(fields[iField]);
-  }
+    getline(restart_file, text_line);
 
-  std::vector<string>::iterator itx = std::find(fields.begin(), fields.end(), "\"Sensitivity_x\"");
-  std::vector<string>::iterator ity = std::find(fields.begin(), fields.end(), "\"Sensitivity_y\"");
-  std::vector<string>::iterator itz = std::find(fields.begin(), fields.end(), "\"Sensitivity_z\"");
+    vector<string> fields = PrintingToolbox::split(text_line, ',');
 
-  if (itx == fields.end()){
-    SU2_MPI::Error("Sensitivity x not found in file.", CURRENT_FUNCTION);
-  }
-  if (ity ==fields.end()){
-    SU2_MPI::Error("Sensitivity y not found in file.", CURRENT_FUNCTION);
-  }
-  if (nDim == 3){
-    if (itz == fields.end()){
-      SU2_MPI::Error("Sensitivity z not found in file.", CURRENT_FUNCTION);
+    for (unsigned short iField = 0; iField < fields.size(); iField++) {
+      PrintingToolbox::trim(fields[iField]);
     }
-  }
 
-  unsigned short sens_x_idx = std::distance(fields.begin(), itx);
-  unsigned short sens_y_idx = std::distance(fields.begin(), ity);
-  unsigned short sens_z_idx = 0;
-  if (nDim == 3)
-    sens_z_idx = std::distance(fields.begin(), itz);
+    std::vector<string>::iterator itx = std::find(fields.begin(), fields.end(), "\"Sensitivity_x\"");
+    std::vector<string>::iterator ity = std::find(fields.begin(), fields.end(), "\"Sensitivity_y\"");
+    std::vector<string>::iterator itz = std::find(fields.begin(), fields.end(), "\"Sensitivity_z\"");
 
+    if (itx == fields.end()) {
+      SU2_MPI::Error("Sensitivity x not found in file.", CURRENT_FUNCTION);
+    }
+    if (ity == fields.end()) {
+      SU2_MPI::Error("Sensitivity y not found in file.", CURRENT_FUNCTION);
+    }
+    if (nDim == 3) {
+      if (itz == fields.end()) {
+        SU2_MPI::Error("Sensitivity z not found in file.", CURRENT_FUNCTION);
+      }
+    }
 
-  for (iPoint_Global = 0; iPoint_Global < GetGlobal_nPointDomain(); iPoint_Global++ ) {
+    unsigned short sens_x_idx = std::distance(fields.begin(), itx);
+    unsigned short sens_y_idx = std::distance(fields.begin(), ity);
+    unsigned short sens_z_idx = 0;
+    if (nDim == 3) sens_z_idx = std::distance(fields.begin(), itz);
 
-    getline (restart_file, text_line);
+    for (iPoint_Global = 0; iPoint_Global < GetGlobal_nPointDomain(); iPoint_Global++) {
+      getline(restart_file, text_line);
 
-    vector<string> point_line = PrintingToolbox::split(text_line, ',');
+      vector<string> point_line = PrintingToolbox::split(text_line, ',');
 
-    /*--- Retrieve local index. If this node from the restart file lives
-     on the current processor, we will load and instantiate the vars. ---*/
+      /*--- Retrieve local index. If this node from the restart file lives
+       on the current processor, we will load and instantiate the vars. ---*/
 
-    iPoint_Local = GetGlobal_to_Local_Point(iPoint_Global);
+      iPoint_Local = GetGlobal_to_Local_Point(iPoint_Global);
 
-    if (iPoint_Local > -1) {
-      Sensitivity(iPoint_Local,0) = PrintingToolbox::stod(point_line[sens_x_idx]);
-      Sensitivity(iPoint_Local,1) = PrintingToolbox::stod(point_line[sens_y_idx]);
-      if (nDim == 3)
-        Sensitivity(iPoint_Local,2) = PrintingToolbox::stod(point_line[sens_z_idx]);
+      if (iPoint_Local > -1) {
+        Sensitivity(iPoint_Local, 0) = PrintingToolbox::stod(point_line[sens_x_idx]);
+        Sensitivity(iPoint_Local, 1) = PrintingToolbox::stod(point_line[sens_y_idx]);
+        if (nDim == 3) Sensitivity(iPoint_Local, 2) = PrintingToolbox::stod(point_line[sens_z_idx]);
+      }
     }
 
-  }
-
-  /*--- Read AoA sensitivity ---*/
+    /*--- Read AoA sensitivity ---*/
 
-  while (getline (restart_file, text_line)) {
-    position = text_line.find ("SENS_AOA=",0);
-    if (position != string::npos) {
-      text_line.erase (0,9); AoASens = atof(text_line.c_str());
-      config->SetAoA_Sens(AoASens);
+    while (getline(restart_file, text_line)) {
+      position = text_line.find("SENS_AOA=", 0);
+      if (position != string::npos) {
+        text_line.erase(0, 9);
+        AoASens = atof(text_line.c_str());
+        config->SetAoA_Sens(AoASens);
+      }
     }
-  }
-
-  restart_file.close();
 
+    restart_file.close();
   }
-
 }
 
-void CPhysicalGeometry::ReadUnorderedSensitivity(CConfig *config) {
-
+void CPhysicalGeometry::ReadUnorderedSensitivity(CConfig* config) {
   /*--- This routine makes SU2_DOT more interoperable with other
    packages so that folks can customize their workflows. For example, one
    may want to compute flow and adjoint with package A, deform the mesh
@@ -9168,7 +8763,7 @@ void CPhysicalGeometry::ReadUnorderedSensitivity(CConfig *config) {
   unsigned long iPoint, pointID;
   unsigned long unmatched = 0, iPoint_Found = 0, iPoint_Ext = 0;
 
-  su2double Coor_External[3] = {0.0,0.0,0.0}, Sens_External[3] = {0.0,0.0,0.0};
+  su2double Coor_External[3] = {0.0, 0.0, 0.0}, Sens_External[3] = {0.0, 0.0, 0.0};
   su2double dist;
   int rankID;
 
@@ -9176,26 +8771,24 @@ void CPhysicalGeometry::ReadUnorderedSensitivity(CConfig *config) {
   ifstream external_file;
   ofstream sens_file;
 
-  if (rank == MASTER_NODE)
-    cout << "Parsing unordered ASCII volume sensitivity file."<< endl;
+  if (rank == MASTER_NODE) cout << "Parsing unordered ASCII volume sensitivity file." << endl;
 
   /*--- Allocate space for the sensitivity and initialize. ---*/
 
-  Sensitivity.resize(nPoint,nDim) = su2double(0.0);
+  Sensitivity.resize(nPoint, nDim) = su2double(0.0);
 
   /*--- Get the filename for the unordered ASCII sensitivity file input. ---*/
 
   filename = config->GetDV_Unordered_Sens_Filename();
   external_file.open(filename.data(), ios::in);
   if (external_file.fail()) {
-    SU2_MPI::Error(string("There is no unordered ASCII sensitivity file ") +
-                   filename, CURRENT_FUNCTION);
+    SU2_MPI::Error(string("There is no unordered ASCII sensitivity file ") + filename, CURRENT_FUNCTION);
   }
 
   /*--- Allocate the vectors to hold boundary node coordinates
    and its local ID. ---*/
 
-  vector<su2double>     Coords(nDim*nPointDomain);
+  vector<su2double> Coords(nDim * nPointDomain);
   vector<unsigned long> PointIDs(nPointDomain);
 
   /*--- Retrieve and store the coordinates of owned interior nodes
@@ -9203,39 +8796,33 @@ void CPhysicalGeometry::ReadUnorderedSensitivity(CConfig *config) {
 
   for (iPoint = 0; iPoint < nPointDomain; iPoint++) {
     PointIDs[iPoint] = iPoint;
-    for (iDim = 0; iDim < nDim; iDim++)
-      Coords[iPoint*nDim + iDim] = nodes->GetCoord(iPoint, iDim);
+    for (iDim = 0; iDim < nDim; iDim++) Coords[iPoint * nDim + iDim] = nodes->GetCoord(iPoint, iDim);
   }
 
   /*--- Build the ADT of all interior nodes. ---*/
 
-  CADTPointsOnlyClass VertexADT(nDim, nPointDomain,
-                                Coords.data(), PointIDs.data(), true);
+  CADTPointsOnlyClass VertexADT(nDim, nPointDomain, Coords.data(), PointIDs.data(), true);
 
   /*--- Loop over all interior mesh nodes owned by this rank and find the
    matching point with minimum distance. Once we have the match, store the
    sensitivities from the file for that node. ---*/
 
   if (VertexADT.IsEmpty()) {
-
     SU2_MPI::Error("No external points given to ADT.", CURRENT_FUNCTION);
 
   } else {
-
     /*--- Read the input sensitivity file and locate the point matches
      using the ADT search, on a line-by-line basis. ---*/
 
-    iPoint_Found = 0; iPoint_Ext  = 0;
-    while (getline (external_file, text_line)) {
-
+    iPoint_Found = 0;
+    iPoint_Ext = 0;
+    while (getline(external_file, text_line)) {
       /*--- First, check that the line has 6 entries, otherwise throw out. ---*/
 
       istringstream point_line(text_line);
-      vector<string> tokens((istream_iterator<string>(point_line)),
-                             istream_iterator<string>());
+      vector<string> tokens((istream_iterator<string>(point_line)), istream_iterator<string>());
 
       if (tokens.size() == 6) {
-
         istringstream point_line(text_line);
 
         /*--- Get the coordinates and sensitivity for this line. ---*/
@@ -9246,15 +8833,12 @@ void CPhysicalGeometry::ReadUnorderedSensitivity(CConfig *config) {
         /*--- Locate the nearest node to this external point. If it is on
          our rank, then store the sensitivity value. ---*/
 
-        VertexADT.DetermineNearestNode(&Coor_External[0], dist,
-                                       pointID, rankID);
+        VertexADT.DetermineNearestNode(&Coor_External[0], dist, pointID, rankID);
 
         if (rankID == rank) {
-
           /*--- Store the sensitivities at the matched local node. ---*/
 
-          for (iDim = 0; iDim < nDim; iDim++)
-            Sensitivity(pointID,iDim) = Sens_External[iDim];
+          for (iDim = 0; iDim < nDim; iDim++) Sensitivity(pointID, iDim) = Sens_External[iDim];
 
           /*--- Keep track of how many points we match. ---*/
 
@@ -9263,13 +8847,11 @@ void CPhysicalGeometry::ReadUnorderedSensitivity(CConfig *config) {
           /*--- Keep track of points with poor matches for reporting. ---*/
 
           if (dist > 1e-10) unmatched++;
-
         }
 
         /*--- Increment counter for total points in the external file. ---*/
 
         iPoint_Ext++;
-
       }
     }
 
@@ -9282,56 +8864,60 @@ void CPhysicalGeometry::ReadUnorderedSensitivity(CConfig *config) {
     if ((iPoint_Ext < GetGlobal_nPointDomain()) && (rank == MASTER_NODE)) {
       sens_file.open(config->GetDV_Unordered_Sens_Filename().data(), ios::out);
       sens_file.close();
-      SU2_MPI::Error("Not enough points in the input sensitivity file.",
-                     CURRENT_FUNCTION);
+      SU2_MPI::Error("Not enough points in the input sensitivity file.", CURRENT_FUNCTION);
     }
 
     /*--- Check for points with a poor match and report the count. ---*/
 
-    unsigned long myUnmatched = unmatched; unmatched = 0;
-    SU2_MPI::Allreduce(&myUnmatched, &unmatched, 1,
-                       MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
+    unsigned long myUnmatched = unmatched;
+    unmatched = 0;
+    SU2_MPI::Allreduce(&myUnmatched, &unmatched, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
     if ((unmatched > 0) && (rank == MASTER_NODE)) {
       cout << " Warning: there are " << unmatched;
       cout << " points with a match distance > 1e-10." << endl;
     }
-
   }
-
 }
 
-void CPhysicalGeometry::Check_Periodicity(CConfig *config) {
-
+void CPhysicalGeometry::Check_Periodicity(CConfig* config) {
   /*--- Check for the presence of any periodic BCs and disable multigrid
    for now if found. ---*/
 
   if ((config->GetnMarker_Periodic() != 0) && (config->GetnMGLevels() > 0)) {
-    if (rank == MASTER_NODE)
-      cout << "WARNING: Periodicity has been detected. Disabling multigrid. "<< endl;
+    if (rank == MASTER_NODE) cout << "WARNING: Periodicity has been detected. Disabling multigrid. " << endl;
     config->SetMGLevels(0);
   }
-
 }
 
-su2double CPhysicalGeometry::Compute_MaxThickness(su2double *Plane_P0, su2double *Plane_Normal, CConfig *config, vector<su2double> &Xcoord_Airfoil,
-                                                  vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) {
-
+su2double CPhysicalGeometry::Compute_MaxThickness(su2double* Plane_P0, su2double* Plane_Normal, CConfig* config,
+                                                  vector<su2double>& Xcoord_Airfoil, vector<su2double>& Ycoord_Airfoil,
+                                                  vector<su2double>& Zcoord_Airfoil) {
   unsigned long iVertex, jVertex, Trailing_Point, Leading_Point;
-  su2double Normal[3], Tangent[3], BiNormal[3], auxXCoord, auxYCoord, auxZCoord, zp1, zpn, MaxThickness_Value = 0, Thickness, Length, Xcoord_Trailing, Ycoord_Trailing, Zcoord_Trailing, ValCos, ValSin, XValue, ZValue, MaxDistance, Distance, AoA;
-  vector<su2double> Xcoord, Ycoord, Zcoord, Xcoord_Normal, Ycoord_Normal, Zcoord_Normal, Xcoord_Airfoil_, Ycoord_Airfoil_, Zcoord_Airfoil_;
+  su2double Normal[3], Tangent[3], BiNormal[3], auxXCoord, auxYCoord, auxZCoord, zp1, zpn,
+      MaxThickness_Value = 0, Thickness, Length, Xcoord_Trailing, Ycoord_Trailing, Zcoord_Trailing, ValCos, ValSin,
+      XValue, ZValue, MaxDistance, Distance, AoA;
+  vector<su2double> Xcoord, Ycoord, Zcoord, Xcoord_Normal, Ycoord_Normal, Zcoord_Normal, Xcoord_Airfoil_,
+      Ycoord_Airfoil_, Zcoord_Airfoil_;
 
   /*--- Find the leading and trailing edges and compute the angle of attack ---*/
 
-  MaxDistance = 0.0; Trailing_Point = 0; Leading_Point = 0;
+  MaxDistance = 0.0;
+  Trailing_Point = 0;
+  Leading_Point = 0;
   for (iVertex = 1; iVertex < Xcoord_Airfoil.size(); iVertex++) {
     Distance = sqrt(pow(Xcoord_Airfoil[iVertex] - Xcoord_Airfoil[Trailing_Point], 2.0) +
                     pow(Ycoord_Airfoil[iVertex] - Ycoord_Airfoil[Trailing_Point], 2.0) +
                     pow(Zcoord_Airfoil[iVertex] - Zcoord_Airfoil[Trailing_Point], 2.0));
 
-    if (MaxDistance < Distance) { MaxDistance = Distance; Leading_Point = iVertex; }
+    if (MaxDistance < Distance) {
+      MaxDistance = Distance;
+      Leading_Point = iVertex;
+    }
   }
 
-  AoA = atan((Zcoord_Airfoil[Leading_Point] - Zcoord_Airfoil[Trailing_Point]) / (Xcoord_Airfoil[Trailing_Point] - Xcoord_Airfoil[Leading_Point]))*180/PI_NUMBER;
+  AoA = atan((Zcoord_Airfoil[Leading_Point] - Zcoord_Airfoil[Trailing_Point]) /
+             (Xcoord_Airfoil[Trailing_Point] - Xcoord_Airfoil[Leading_Point])) *
+        180 / PI_NUMBER;
 
   /*--- Translate to the origin ---*/
 
@@ -9347,67 +8933,78 @@ su2double CPhysicalGeometry::Compute_MaxThickness(su2double *Plane_P0, su2double
 
   /*--- Rotate the airfoil ---*/
 
-  ValCos = cos(AoA*PI_NUMBER/180.0);
-  ValSin = sin(AoA*PI_NUMBER/180.0);
+  ValCos = cos(AoA * PI_NUMBER / 180.0);
+  ValSin = sin(AoA * PI_NUMBER / 180.0);
 
   for (iVertex = 0; iVertex < Xcoord_Airfoil.size(); iVertex++) {
     XValue = Xcoord_Airfoil_[iVertex];
     ZValue = Zcoord_Airfoil_[iVertex];
-    Xcoord_Airfoil_[iVertex] = XValue*ValCos - ZValue*ValSin;
-    Zcoord_Airfoil_[iVertex] = ZValue*ValCos + XValue*ValSin;
+    Xcoord_Airfoil_[iVertex] = XValue * ValCos - ZValue * ValSin;
+    Zcoord_Airfoil_[iVertex] = ZValue * ValCos + XValue * ValSin;
   }
 
   /*--- Identify upper and lower side, and store the value of the normal --*/
 
   for (iVertex = 1; iVertex < Xcoord_Airfoil_.size(); iVertex++) {
-    Tangent[0] = Xcoord_Airfoil_[iVertex] - Xcoord_Airfoil_[iVertex-1];
-    Tangent[1] = Ycoord_Airfoil_[iVertex] - Ycoord_Airfoil_[iVertex-1];
-    Tangent[2] = Zcoord_Airfoil_[iVertex] - Zcoord_Airfoil_[iVertex-1];
+    Tangent[0] = Xcoord_Airfoil_[iVertex] - Xcoord_Airfoil_[iVertex - 1];
+    Tangent[1] = Ycoord_Airfoil_[iVertex] - Ycoord_Airfoil_[iVertex - 1];
+    Tangent[2] = Zcoord_Airfoil_[iVertex] - Zcoord_Airfoil_[iVertex - 1];
     Length = sqrt(pow(Tangent[0], 2.0) + pow(Tangent[1], 2.0) + pow(Tangent[2], 2.0));
 
-    Tangent[0] /= Length; Tangent[1] /= Length; Tangent[2] /= Length;
+    Tangent[0] /= Length;
+    Tangent[1] /= Length;
+    Tangent[2] /= Length;
 
     BiNormal[0] = Plane_Normal[0];
     BiNormal[1] = Plane_Normal[1];
     BiNormal[2] = Plane_Normal[2];
     Length = sqrt(pow(BiNormal[0], 2.0) + pow(BiNormal[1], 2.0) + pow(BiNormal[2], 2.0));
-    BiNormal[0] /= Length; BiNormal[1] /= Length; BiNormal[2] /= Length;
+    BiNormal[0] /= Length;
+    BiNormal[1] /= Length;
+    BiNormal[2] /= Length;
 
-    Normal[0] = Tangent[1]*BiNormal[2] - Tangent[2]*BiNormal[1];
-    Normal[1] = Tangent[2]*BiNormal[0] - Tangent[0]*BiNormal[2];
-    Normal[2] = Tangent[0]*BiNormal[1] - Tangent[1]*BiNormal[0];
+    Normal[0] = Tangent[1] * BiNormal[2] - Tangent[2] * BiNormal[1];
+    Normal[1] = Tangent[2] * BiNormal[0] - Tangent[0] * BiNormal[2];
+    Normal[2] = Tangent[0] * BiNormal[1] - Tangent[1] * BiNormal[0];
 
-    Xcoord_Normal.push_back(Normal[0]); Ycoord_Normal.push_back(Normal[1]); Zcoord_Normal.push_back(Normal[2]);
+    Xcoord_Normal.push_back(Normal[0]);
+    Ycoord_Normal.push_back(Normal[1]);
+    Zcoord_Normal.push_back(Normal[2]);
 
     unsigned short index = 2;
 
     /*--- Removing the trailing edge from list of points that we are going to use in the interpolation,
       to be sure that a blunt trailing edge do not affect the interpolation ---*/
 
-    if ((Normal[index] >= 0.0) && (fabs(Xcoord_Airfoil_[iVertex]) > MaxDistance*0.01)) {
+    if ((Normal[index] >= 0.0) && (fabs(Xcoord_Airfoil_[iVertex]) > MaxDistance * 0.01)) {
       Xcoord.push_back(Xcoord_Airfoil_[iVertex]);
       Ycoord.push_back(Ycoord_Airfoil_[iVertex]);
       Zcoord.push_back(Zcoord_Airfoil_[iVertex]);
     }
-
   }
 
   /*--- Order the arrays using the X component ---*/
 
   for (iVertex = 0; iVertex < Xcoord.size(); iVertex++) {
     for (jVertex = 0; jVertex < Xcoord.size() - 1 - iVertex; jVertex++) {
-      if (Xcoord[jVertex] > Xcoord[jVertex+1]) {
-        auxXCoord = Xcoord[jVertex]; Xcoord[jVertex] = Xcoord[jVertex+1]; Xcoord[jVertex+1] = auxXCoord;
-        auxYCoord = Ycoord[jVertex]; Ycoord[jVertex] = Ycoord[jVertex+1]; Ycoord[jVertex+1] = auxYCoord;
-        auxZCoord = Zcoord[jVertex]; Zcoord[jVertex] = Zcoord[jVertex+1]; Zcoord[jVertex+1] = auxZCoord;
+      if (Xcoord[jVertex] > Xcoord[jVertex + 1]) {
+        auxXCoord = Xcoord[jVertex];
+        Xcoord[jVertex] = Xcoord[jVertex + 1];
+        Xcoord[jVertex + 1] = auxXCoord;
+        auxYCoord = Ycoord[jVertex];
+        Ycoord[jVertex] = Ycoord[jVertex + 1];
+        Ycoord[jVertex + 1] = auxYCoord;
+        auxZCoord = Zcoord[jVertex];
+        Zcoord[jVertex] = Zcoord[jVertex + 1];
+        Zcoord[jVertex + 1] = auxZCoord;
       }
     }
   }
 
   const auto n = Xcoord.size();
   if (n > 1) {
-    zp1 = (Zcoord[1]-Zcoord[0])/(Xcoord[1]-Xcoord[0]);
-    zpn = (Zcoord[n-1]-Zcoord[n-2])/(Xcoord[n-1]-Xcoord[n-2]);
+    zp1 = (Zcoord[1] - Zcoord[0]) / (Xcoord[1] - Xcoord[0]);
+    zpn = (Zcoord[n - 1] - Zcoord[n - 2]) / (Xcoord[n - 1] - Xcoord[n - 2]);
 
     CCubicSpline spline(Xcoord, Zcoord, CCubicSpline::FIRST, zp1, CCubicSpline::FIRST, zpn);
 
@@ -9418,33 +9015,34 @@ su2double CPhysicalGeometry::Compute_MaxThickness(su2double *Plane_P0, su2double
     for (iVertex = 0; iVertex < Xcoord_Airfoil_.size(); iVertex++) {
       if (Zcoord_Normal[iVertex] < 0.0) {
         Thickness = fabs(Zcoord_Airfoil_[iVertex] - spline(Xcoord_Airfoil_[iVertex]));
-        if (Thickness > MaxThickness_Value) { MaxThickness_Value = Thickness; }
+        if (Thickness > MaxThickness_Value) {
+          MaxThickness_Value = Thickness;
+        }
       }
     }
+  } else {
+    MaxThickness_Value = 0.0;
   }
-  else { MaxThickness_Value = 0.0; }
 
   return MaxThickness_Value;
-
 }
 
-su2double CPhysicalGeometry::Compute_Dihedral(su2double *LeadingEdge_im1, su2double *TrailingEdge_im1,
-                                              su2double *LeadingEdge_i, su2double *TrailingEdge_i) {
-
-  // su2double Dihedral_Leading = atan((LeadingEdge_i[2] - LeadingEdge_im1[2]) / (LeadingEdge_i[1] - LeadingEdge_im1[1]))*180/PI_NUMBER;
-  su2double Dihedral_Trailing = atan((TrailingEdge_i[2] - TrailingEdge_im1[2]) / (TrailingEdge_i[1] - TrailingEdge_im1[1]))*180/PI_NUMBER;
+su2double CPhysicalGeometry::Compute_Dihedral(su2double* LeadingEdge_im1, su2double* TrailingEdge_im1,
+                                              su2double* LeadingEdge_i, su2double* TrailingEdge_i) {
+  // su2double Dihedral_Leading = atan((LeadingEdge_i[2] - LeadingEdge_im1[2]) / (LeadingEdge_i[1] -
+  // LeadingEdge_im1[1]))*180/PI_NUMBER;
+  su2double Dihedral_Trailing =
+      atan((TrailingEdge_i[2] - TrailingEdge_im1[2]) / (TrailingEdge_i[1] - TrailingEdge_im1[1])) * 180 / PI_NUMBER;
 
   // su2double Dihedral = 0.5*(Dihedral_Leading + Dihedral_Trailing);
 
   return Dihedral_Trailing;
-
 }
 
-su2double CPhysicalGeometry::Compute_Curvature(su2double *LeadingEdge_im1, su2double *TrailingEdge_im1,
-                                               su2double *LeadingEdge_i, su2double *TrailingEdge_i,
-                                               su2double *LeadingEdge_ip1, su2double *TrailingEdge_ip1) {
-
-  su2double A[2], B[2], C[2], BC[2], AB[2], AC[2], BC_MOD, AB_MOD,  AC_MOD, AB_CROSS_AC;
+su2double CPhysicalGeometry::Compute_Curvature(su2double* LeadingEdge_im1, su2double* TrailingEdge_im1,
+                                               su2double* LeadingEdge_i, su2double* TrailingEdge_i,
+                                               su2double* LeadingEdge_ip1, su2double* TrailingEdge_ip1) {
+  su2double A[2], B[2], C[2], BC[2], AB[2], AC[2], BC_MOD, AB_MOD, AC_MOD, AB_CROSS_AC;
 
   // A[0] = LeadingEdge_im1[1];     A[1] = LeadingEdge_im1[2];
   // B[0] = LeadingEdge_i[1];           B[1] = LeadingEdge_i[2];
@@ -9460,64 +9058,82 @@ su2double CPhysicalGeometry::Compute_Curvature(su2double *LeadingEdge_im1, su2do
 
   // su2double Curvature_Leading = fabs(1.0/(0.5*BC_MOD*AB_MOD*AC_MOD/AB_CROSS_AC));
 
-  A[0] = TrailingEdge_im1[1];      A[1] = TrailingEdge_im1[2];
-  B[0] = TrailingEdge_i[1];                B[1] = TrailingEdge_i[2];
-  C[0] = TrailingEdge_ip1[1];      C[1] = TrailingEdge_ip1[2];
-
-  BC[0] = C[0] - B[0]; BC[1] = C[1] - B[1];
-  AB[0] = B[0] - A[0]; AB[1] = B[1] - A[1];
-  AC[0] = C[0] - A[0]; AC[1] = C[1] - A[1];
-  BC_MOD = sqrt(BC[0]*BC[0] + BC[1]*BC[1] );
-  AB_MOD = sqrt(AB[0]*AB[0] + AB[1]*AB[1] );
-  AC_MOD = sqrt(AC[0]*AC[0] + AC[1]*AC[1] );
-  AB_CROSS_AC = AB[0]* AC[1] - AB[1]* AC[0];
-
-  su2double Curvature_Trailing = fabs(1.0/(0.5*BC_MOD*AB_MOD*AC_MOD/AB_CROSS_AC));
+  A[0] = TrailingEdge_im1[1];
+  A[1] = TrailingEdge_im1[2];
+  B[0] = TrailingEdge_i[1];
+  B[1] = TrailingEdge_i[2];
+  C[0] = TrailingEdge_ip1[1];
+  C[1] = TrailingEdge_ip1[2];
+
+  BC[0] = C[0] - B[0];
+  BC[1] = C[1] - B[1];
+  AB[0] = B[0] - A[0];
+  AB[1] = B[1] - A[1];
+  AC[0] = C[0] - A[0];
+  AC[1] = C[1] - A[1];
+  BC_MOD = sqrt(BC[0] * BC[0] + BC[1] * BC[1]);
+  AB_MOD = sqrt(AB[0] * AB[0] + AB[1] * AB[1]);
+  AC_MOD = sqrt(AC[0] * AC[0] + AC[1] * AC[1]);
+  AB_CROSS_AC = AB[0] * AC[1] - AB[1] * AC[0];
+
+  su2double Curvature_Trailing = fabs(1.0 / (0.5 * BC_MOD * AB_MOD * AC_MOD / AB_CROSS_AC));
 
   // su2double Curvature = 0.5*(Curvature_Leading + Curvature_Trailing);
 
   return Curvature_Trailing;
-
 }
 
-su2double CPhysicalGeometry::Compute_Twist(su2double *Plane_P0, su2double *Plane_Normal, vector<su2double> &Xcoord_Airfoil,
-                                           vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) {
+su2double CPhysicalGeometry::Compute_Twist(su2double* Plane_P0, su2double* Plane_Normal,
+                                           vector<su2double>& Xcoord_Airfoil, vector<su2double>& Ycoord_Airfoil,
+                                           vector<su2double>& Zcoord_Airfoil) {
   unsigned long iVertex, Trailing_Point, Leading_Point;
   su2double MaxDistance, Distance, Twist = 0.0;
 
   /*--- Find the leading and trailing edges and compute the angle of attack ---*/
 
-  MaxDistance = 0.0; Trailing_Point = 0; Leading_Point = 0;
+  MaxDistance = 0.0;
+  Trailing_Point = 0;
+  Leading_Point = 0;
   for (iVertex = 1; iVertex < Xcoord_Airfoil.size(); iVertex++) {
     Distance = sqrt(pow(Xcoord_Airfoil[iVertex] - Xcoord_Airfoil[Trailing_Point], 2.0) +
                     pow(Ycoord_Airfoil[iVertex] - Ycoord_Airfoil[Trailing_Point], 2.0) +
                     pow(Zcoord_Airfoil[iVertex] - Zcoord_Airfoil[Trailing_Point], 2.0));
 
-    if (MaxDistance < Distance) { MaxDistance = Distance; Leading_Point = iVertex; }
+    if (MaxDistance < Distance) {
+      MaxDistance = Distance;
+      Leading_Point = iVertex;
+    }
   }
 
-  Twist = atan((Zcoord_Airfoil[Leading_Point] - Zcoord_Airfoil[Trailing_Point]) / (Xcoord_Airfoil[Trailing_Point] - Xcoord_Airfoil[Leading_Point]))*180/PI_NUMBER;
+  Twist = atan((Zcoord_Airfoil[Leading_Point] - Zcoord_Airfoil[Trailing_Point]) /
+               (Xcoord_Airfoil[Trailing_Point] - Xcoord_Airfoil[Leading_Point])) *
+          180 / PI_NUMBER;
 
   return Twist;
-
 }
 
-void CPhysicalGeometry::Compute_Wing_LeadingTrailing(su2double *LeadingEdge, su2double *TrailingEdge, su2double *Plane_P0, su2double *Plane_Normal,
-                                                vector<su2double> &Xcoord_Airfoil, vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) {
-
+void CPhysicalGeometry::Compute_Wing_LeadingTrailing(su2double* LeadingEdge, su2double* TrailingEdge,
+                                                     su2double* Plane_P0, su2double* Plane_Normal,
+                                                     vector<su2double>& Xcoord_Airfoil,
+                                                     vector<su2double>& Ycoord_Airfoil,
+                                                     vector<su2double>& Zcoord_Airfoil) {
   unsigned long iVertex, Trailing_Point, Leading_Point;
   su2double MaxDistance, Distance;
 
   /*--- Find the leading and trailing edges and compute the angle of attack ---*/
 
-  MaxDistance = 0.0; Trailing_Point = 0; Leading_Point = 0;
+  MaxDistance = 0.0;
+  Trailing_Point = 0;
+  Leading_Point = 0;
   for (iVertex = 1; iVertex < Xcoord_Airfoil.size(); iVertex++) {
-
     Distance = sqrt(pow(Xcoord_Airfoil[iVertex] - Xcoord_Airfoil[Trailing_Point], 2.0) +
                     pow(Ycoord_Airfoil[iVertex] - Ycoord_Airfoil[Trailing_Point], 2.0) +
                     pow(Zcoord_Airfoil[iVertex] - Zcoord_Airfoil[Trailing_Point], 2.0));
 
-    if (MaxDistance < Distance) { MaxDistance = Distance; Leading_Point = iVertex; }
+    if (MaxDistance < Distance) {
+      MaxDistance = Distance;
+      Leading_Point = iVertex;
+    }
   }
 
   LeadingEdge[0] = Xcoord_Airfoil[Leading_Point];
@@ -9527,84 +9143,101 @@ void CPhysicalGeometry::Compute_Wing_LeadingTrailing(su2double *LeadingEdge, su2
   TrailingEdge[0] = Xcoord_Airfoil[Trailing_Point];
   TrailingEdge[1] = Ycoord_Airfoil[Trailing_Point];
   TrailingEdge[2] = Zcoord_Airfoil[Trailing_Point];
-
 }
 
-void CPhysicalGeometry::Compute_Fuselage_LeadingTrailing(su2double *LeadingEdge, su2double *TrailingEdge, su2double *Plane_P0, su2double *Plane_Normal,
-                                                vector<su2double> &Xcoord_Airfoil, vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) {
-
+void CPhysicalGeometry::Compute_Fuselage_LeadingTrailing(su2double* LeadingEdge, su2double* TrailingEdge,
+                                                         su2double* Plane_P0, su2double* Plane_Normal,
+                                                         vector<su2double>& Xcoord_Airfoil,
+                                                         vector<su2double>& Ycoord_Airfoil,
+                                                         vector<su2double>& Zcoord_Airfoil) {
   unsigned long iVertex, Trailing_Point, Leading_Point;
   su2double MaxDistance, Distance;
 
-  MaxDistance = 0.0; Trailing_Point = 0; Leading_Point = 0;
+  MaxDistance = 0.0;
+  Trailing_Point = 0;
+  Leading_Point = 0;
   for (iVertex = 1; iVertex < Xcoord_Airfoil.size(); iVertex++) {
     Distance = sqrt(pow(Xcoord_Airfoil[iVertex] - Xcoord_Airfoil[Trailing_Point], 2.0));
-    if (MaxDistance < Distance) { MaxDistance = Distance; Leading_Point = iVertex; }
+    if (MaxDistance < Distance) {
+      MaxDistance = Distance;
+      Leading_Point = iVertex;
+    }
   }
 
   LeadingEdge[0] = Xcoord_Airfoil[Leading_Point];
   LeadingEdge[1] = Ycoord_Airfoil[Leading_Point];
   LeadingEdge[2] = Zcoord_Airfoil[Leading_Point];
 
-  MaxDistance = 0.0; Trailing_Point = 0; Leading_Point = 0;
+  MaxDistance = 0.0;
+  Trailing_Point = 0;
+  Leading_Point = 0;
   for (iVertex = 1; iVertex < Zcoord_Airfoil.size(); iVertex++) {
     Distance = sqrt(pow(Zcoord_Airfoil[iVertex] - Zcoord_Airfoil[Trailing_Point], 2.0));
-    if (MaxDistance < Distance) { MaxDistance = Distance; Leading_Point = iVertex; }
+    if (MaxDistance < Distance) {
+      MaxDistance = Distance;
+      Leading_Point = iVertex;
+    }
   }
 
-  TrailingEdge[0] = 0.5*(Xcoord_Airfoil[Trailing_Point]+Xcoord_Airfoil[Leading_Point]);
-  TrailingEdge[1] = 0.5*(Ycoord_Airfoil[Trailing_Point]+Ycoord_Airfoil[Leading_Point]);
-  TrailingEdge[2] = 0.5*(Zcoord_Airfoil[Trailing_Point]+Zcoord_Airfoil[Leading_Point]);
-
+  TrailingEdge[0] = 0.5 * (Xcoord_Airfoil[Trailing_Point] + Xcoord_Airfoil[Leading_Point]);
+  TrailingEdge[1] = 0.5 * (Ycoord_Airfoil[Trailing_Point] + Ycoord_Airfoil[Leading_Point]);
+  TrailingEdge[2] = 0.5 * (Zcoord_Airfoil[Trailing_Point] + Zcoord_Airfoil[Leading_Point]);
 }
 
-su2double CPhysicalGeometry::Compute_Chord(su2double *Plane_P0, su2double *Plane_Normal, vector<su2double> &Xcoord_Airfoil,
-                                           vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) {
+su2double CPhysicalGeometry::Compute_Chord(su2double* Plane_P0, su2double* Plane_Normal,
+                                           vector<su2double>& Xcoord_Airfoil, vector<su2double>& Ycoord_Airfoil,
+                                           vector<su2double>& Zcoord_Airfoil) {
   unsigned long iVertex, Trailing_Point;
   su2double MaxDistance, Distance, Chord = 0.0;
 
   /*--- Find the leading and trailing edges and compute the angle of attack ---*/
-  MaxDistance = 0.0; Trailing_Point = 0;
+  MaxDistance = 0.0;
+  Trailing_Point = 0;
   for (iVertex = 1; iVertex < Xcoord_Airfoil.size(); iVertex++) {
-
     Distance = sqrt(pow(Xcoord_Airfoil[iVertex] - Xcoord_Airfoil[Trailing_Point], 2.0) +
                     pow(Ycoord_Airfoil[iVertex] - Ycoord_Airfoil[Trailing_Point], 2.0) +
                     pow(Zcoord_Airfoil[iVertex] - Zcoord_Airfoil[Trailing_Point], 2.0));
 
-    if (MaxDistance < Distance) { MaxDistance = Distance; }
+    if (MaxDistance < Distance) {
+      MaxDistance = Distance;
+    }
   }
 
   Chord = MaxDistance;
 
   return Chord;
-
 }
 
-su2double CPhysicalGeometry::Compute_Width(su2double *Plane_P0, su2double *Plane_Normal, vector<su2double> &Xcoord_Airfoil,
-                                           vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) {
-
+su2double CPhysicalGeometry::Compute_Width(su2double* Plane_P0, su2double* Plane_Normal,
+                                           vector<su2double>& Xcoord_Airfoil, vector<su2double>& Ycoord_Airfoil,
+                                           vector<su2double>& Zcoord_Airfoil) {
   unsigned long iVertex, Trailing_Point;
   su2double MaxDistance, Distance, Width = 0.0;
 
-  MaxDistance = 0.0; Trailing_Point = 0;
+  MaxDistance = 0.0;
+  Trailing_Point = 0;
   for (iVertex = 1; iVertex < Xcoord_Airfoil.size(); iVertex++) {
     Distance = fabs(Xcoord_Airfoil[iVertex] - Xcoord_Airfoil[Trailing_Point]);
-    if (MaxDistance < Distance) { MaxDistance = Distance; }
+    if (MaxDistance < Distance) {
+      MaxDistance = Distance;
+    }
   }
 
   Width = MaxDistance;
   return Width;
-
 }
 
-su2double CPhysicalGeometry::Compute_WaterLineWidth(su2double *Plane_P0, su2double *Plane_Normal, CConfig *config,
-                                                    vector<su2double> &Xcoord_Airfoil, vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) {
-
+su2double CPhysicalGeometry::Compute_WaterLineWidth(su2double* Plane_P0, su2double* Plane_Normal, CConfig* config,
+                                                    vector<su2double>& Xcoord_Airfoil,
+                                                    vector<su2double>& Ycoord_Airfoil,
+                                                    vector<su2double>& Zcoord_Airfoil) {
   unsigned long iVertex, Trailing_Point;
   su2double MinDistance, Distance, WaterLineWidth = 0.0;
   su2double WaterLine = config->GetGeo_Waterline_Location();
 
-  MinDistance = 1E10; WaterLineWidth = 0; Trailing_Point = 0;
+  MinDistance = 1E10;
+  WaterLineWidth = 0;
+  Trailing_Point = 0;
   for (iVertex = 0; iVertex < Xcoord_Airfoil.size(); iVertex++) {
     Distance = fabs(Zcoord_Airfoil[iVertex] - WaterLine);
     if (Distance < MinDistance) {
@@ -9614,91 +9247,119 @@ su2double CPhysicalGeometry::Compute_WaterLineWidth(su2double *Plane_P0, su2doub
   }
 
   return WaterLineWidth;
-
 }
 
-su2double CPhysicalGeometry::Compute_Height(su2double *Plane_P0, su2double *Plane_Normal, vector<su2double> &Xcoord_Airfoil,
-                                            vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) {
-
+su2double CPhysicalGeometry::Compute_Height(su2double* Plane_P0, su2double* Plane_Normal,
+                                            vector<su2double>& Xcoord_Airfoil, vector<su2double>& Ycoord_Airfoil,
+                                            vector<su2double>& Zcoord_Airfoil) {
   unsigned long iVertex, Trailing_Point;
   su2double MaxDistance, Distance, Height = 0.0;
 
-  MaxDistance = 0.0; Trailing_Point = 0;
+  MaxDistance = 0.0;
+  Trailing_Point = 0;
   for (iVertex = 1; iVertex < Zcoord_Airfoil.size(); iVertex++) {
     Distance = sqrt(pow(Zcoord_Airfoil[iVertex] - Zcoord_Airfoil[Trailing_Point], 2.0));
-    if (MaxDistance < Distance) { MaxDistance = Distance; }
+    if (MaxDistance < Distance) {
+      MaxDistance = Distance;
+    }
   }
 
   Height = MaxDistance;
 
   return Height;
-
 }
 
-su2double CPhysicalGeometry::Compute_LERadius(su2double *Plane_P0, su2double *Plane_Normal, vector<su2double> &Xcoord_Airfoil,
-                                              vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) {
-
+su2double CPhysicalGeometry::Compute_LERadius(su2double* Plane_P0, su2double* Plane_Normal,
+                                              vector<su2double>& Xcoord_Airfoil, vector<su2double>& Ycoord_Airfoil,
+                                              vector<su2double>& Zcoord_Airfoil) {
   unsigned long iVertex, Trailing_Point, Leading_Point;
   su2double MaxDistance, Distance, LERadius = 0.0, X1, X2, X3, Y1, Y2, Y3, Ma, Mb, Xc, Yc, Radius;
 
   /*--- Find the leading and trailing edges and compute the radius of curvature ---*/
 
-  MaxDistance = 0.0; Trailing_Point = 0;  Leading_Point = 0;
+  MaxDistance = 0.0;
+  Trailing_Point = 0;
+  Leading_Point = 0;
   for (iVertex = 1; iVertex < Xcoord_Airfoil.size(); iVertex++) {
-
     Distance = sqrt(pow(Xcoord_Airfoil[iVertex] - Xcoord_Airfoil[Trailing_Point], 2.0) +
                     pow(Ycoord_Airfoil[iVertex] - Ycoord_Airfoil[Trailing_Point], 2.0) +
                     pow(Zcoord_Airfoil[iVertex] - Zcoord_Airfoil[Trailing_Point], 2.0));
 
-    if (MaxDistance < Distance) { MaxDistance = Distance; Leading_Point = iVertex; }
+    if (MaxDistance < Distance) {
+      MaxDistance = Distance;
+      Leading_Point = iVertex;
+    }
   }
 
-  X1 = Xcoord_Airfoil[Leading_Point-3];
-  Y1 = Zcoord_Airfoil[Leading_Point-3];
+  X1 = Xcoord_Airfoil[Leading_Point - 3];
+  Y1 = Zcoord_Airfoil[Leading_Point - 3];
 
   X2 = Xcoord_Airfoil[Leading_Point];
   Y2 = Zcoord_Airfoil[Leading_Point];
 
-  X3 = Xcoord_Airfoil[Leading_Point+3];
-  Y3 = Zcoord_Airfoil[Leading_Point+3];
+  X3 = Xcoord_Airfoil[Leading_Point + 3];
+  Y3 = Zcoord_Airfoil[Leading_Point + 3];
 
-  if (X2 != X1) Ma = (Y2-Y1) / (X2-X1); else Ma = 0.0;
-  if (X3 != X2) Mb = (Y3-Y2) / (X3-X2); else Mb = 0.0;
+  if (X2 != X1)
+    Ma = (Y2 - Y1) / (X2 - X1);
+  else
+    Ma = 0.0;
+  if (X3 != X2)
+    Mb = (Y3 - Y2) / (X3 - X2);
+  else
+    Mb = 0.0;
 
-  if (Mb != Ma) Xc = (Ma*Mb*(Y1-Y3)+Mb*(X1+X2)-Ma*(X2+X3))/(2.0*(Mb-Ma)); else Xc = 0.0;
-  if (Ma != 0.0) Yc = -(1.0/Ma)*(Xc-0.5*(X1+X2))+0.5*(Y1+Y2); else Yc = 0.0;
+  if (Mb != Ma)
+    Xc = (Ma * Mb * (Y1 - Y3) + Mb * (X1 + X2) - Ma * (X2 + X3)) / (2.0 * (Mb - Ma));
+  else
+    Xc = 0.0;
+  if (Ma != 0.0)
+    Yc = -(1.0 / Ma) * (Xc - 0.5 * (X1 + X2)) + 0.5 * (Y1 + Y2);
+  else
+    Yc = 0.0;
 
-  Radius = sqrt((Xc-X1)*(Xc-X1)+(Yc-Y1)*(Yc-Y1));
-  if (Radius != 0.0) LERadius = 1.0/Radius; else LERadius = 0.0;
+  Radius = sqrt((Xc - X1) * (Xc - X1) + (Yc - Y1) * (Yc - Y1));
+  if (Radius != 0.0)
+    LERadius = 1.0 / Radius;
+  else
+    LERadius = 0.0;
 
   return LERadius;
-
 }
 
-su2double CPhysicalGeometry::Compute_Thickness(su2double *Plane_P0, su2double *Plane_Normal, su2double Location, CConfig *config,
-                                               vector<su2double> &Xcoord_Airfoil, vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil, su2double &ZLoc) {
-
+su2double CPhysicalGeometry::Compute_Thickness(su2double* Plane_P0, su2double* Plane_Normal, su2double Location,
+                                               CConfig* config, vector<su2double>& Xcoord_Airfoil,
+                                               vector<su2double>& Ycoord_Airfoil, vector<su2double>& Zcoord_Airfoil,
+                                               su2double& ZLoc) {
   unsigned long iVertex, jVertex, n_Upper, n_Lower, Trailing_Point, Leading_Point;
-  su2double Thickness_Location, Normal[3], Tangent[3], BiNormal[3], auxXCoord, auxYCoord, auxZCoord, Thickness_Value = 0.0, Length,
-            Xcoord_Trailing, Ycoord_Trailing, Zcoord_Trailing, ValCos, ValSin, XValue, ZValue, zp1, zpn, Chord, MaxDistance, Distance, AoA;
+  su2double Thickness_Location, Normal[3], Tangent[3], BiNormal[3], auxXCoord, auxYCoord, auxZCoord,
+      Thickness_Value = 0.0, Length, Xcoord_Trailing, Ycoord_Trailing, Zcoord_Trailing, ValCos, ValSin, XValue, ZValue,
+      zp1, zpn, Chord, MaxDistance, Distance, AoA;
 
-  vector<su2double> Xcoord_Upper, Ycoord_Upper, Zcoord_Upper, Xcoord_Lower, Ycoord_Lower, Zcoord_Lower,
-                    Xcoord_Normal, Ycoord_Normal, Zcoord_Normal, Xcoord_Airfoil_, Ycoord_Airfoil_, Zcoord_Airfoil_;
+  vector<su2double> Xcoord_Upper, Ycoord_Upper, Zcoord_Upper, Xcoord_Lower, Ycoord_Lower, Zcoord_Lower, Xcoord_Normal,
+      Ycoord_Normal, Zcoord_Normal, Xcoord_Airfoil_, Ycoord_Airfoil_, Zcoord_Airfoil_;
 
   su2double Zcoord_Up, Zcoord_Down, ZLoc_, YLoc_;
 
   /*--- Find the leading and trailing edges and compute the angle of attack ---*/
 
-  MaxDistance = 0.0; Trailing_Point = 0; Leading_Point = 0;
+  MaxDistance = 0.0;
+  Trailing_Point = 0;
+  Leading_Point = 0;
   for (iVertex = 1; iVertex < Xcoord_Airfoil.size(); iVertex++) {
     Distance = sqrt(pow(Xcoord_Airfoil[iVertex] - Xcoord_Airfoil[Trailing_Point], 2.0) +
                     pow(Ycoord_Airfoil[iVertex] - Ycoord_Airfoil[Trailing_Point], 2.0) +
                     pow(Zcoord_Airfoil[iVertex] - Zcoord_Airfoil[Trailing_Point], 2.0));
 
-    if (MaxDistance < Distance) { MaxDistance = Distance; Leading_Point = iVertex; }
+    if (MaxDistance < Distance) {
+      MaxDistance = Distance;
+      Leading_Point = iVertex;
+    }
   }
 
-  AoA = atan((Zcoord_Airfoil[Leading_Point] - Zcoord_Airfoil[Trailing_Point]) / (Xcoord_Airfoil[Trailing_Point] - Xcoord_Airfoil[Leading_Point]))*180/PI_NUMBER;
+  AoA = atan((Zcoord_Airfoil[Leading_Point] - Zcoord_Airfoil[Trailing_Point]) /
+             (Xcoord_Airfoil[Trailing_Point] - Xcoord_Airfoil[Leading_Point])) *
+        180 / PI_NUMBER;
   Chord = MaxDistance;
 
   /*--- Translate to the origin ---*/
@@ -9715,37 +9376,43 @@ su2double CPhysicalGeometry::Compute_Thickness(su2double *Plane_P0, su2double *P
 
   /*--- Rotate the airfoil ---*/
 
-  ValCos = cos(AoA*PI_NUMBER/180.0);
-  ValSin = sin(AoA*PI_NUMBER/180.0);
+  ValCos = cos(AoA * PI_NUMBER / 180.0);
+  ValSin = sin(AoA * PI_NUMBER / 180.0);
 
   for (iVertex = 0; iVertex < Xcoord_Airfoil.size(); iVertex++) {
     XValue = Xcoord_Airfoil_[iVertex];
     ZValue = Zcoord_Airfoil_[iVertex];
 
-    Xcoord_Airfoil_[iVertex] = XValue*ValCos - ZValue*ValSin;
-    Zcoord_Airfoil_[iVertex] = ZValue*ValCos + XValue*ValSin;
+    Xcoord_Airfoil_[iVertex] = XValue * ValCos - ZValue * ValSin;
+    Zcoord_Airfoil_[iVertex] = ZValue * ValCos + XValue * ValSin;
   }
 
   /*--- Identify upper and lower side, and store the value of the normal --*/
 
   for (iVertex = 1; iVertex < Xcoord_Airfoil_.size(); iVertex++) {
-    Tangent[0] = Xcoord_Airfoil_[iVertex] - Xcoord_Airfoil_[iVertex-1];
-    Tangent[1] = Ycoord_Airfoil_[iVertex] - Ycoord_Airfoil_[iVertex-1];
-    Tangent[2] = Zcoord_Airfoil_[iVertex] - Zcoord_Airfoil_[iVertex-1];
+    Tangent[0] = Xcoord_Airfoil_[iVertex] - Xcoord_Airfoil_[iVertex - 1];
+    Tangent[1] = Ycoord_Airfoil_[iVertex] - Ycoord_Airfoil_[iVertex - 1];
+    Tangent[2] = Zcoord_Airfoil_[iVertex] - Zcoord_Airfoil_[iVertex - 1];
     Length = sqrt(pow(Tangent[0], 2.0) + pow(Tangent[1], 2.0) + pow(Tangent[2], 2.0));
-    Tangent[0] /= Length; Tangent[1] /= Length; Tangent[2] /= Length;
+    Tangent[0] /= Length;
+    Tangent[1] /= Length;
+    Tangent[2] /= Length;
 
     BiNormal[0] = Plane_Normal[0];
     BiNormal[1] = Plane_Normal[1];
     BiNormal[2] = Plane_Normal[2];
     Length = sqrt(pow(BiNormal[0], 2.0) + pow(BiNormal[1], 2.0) + pow(BiNormal[2], 2.0));
-    BiNormal[0] /= Length; BiNormal[1] /= Length; BiNormal[2] /= Length;
+    BiNormal[0] /= Length;
+    BiNormal[1] /= Length;
+    BiNormal[2] /= Length;
 
-    Normal[0] = Tangent[1]*BiNormal[2] - Tangent[2]*BiNormal[1];
-    Normal[1] = Tangent[2]*BiNormal[0] - Tangent[0]*BiNormal[2];
-    Normal[2] = Tangent[0]*BiNormal[1] - Tangent[1]*BiNormal[0];
+    Normal[0] = Tangent[1] * BiNormal[2] - Tangent[2] * BiNormal[1];
+    Normal[1] = Tangent[2] * BiNormal[0] - Tangent[0] * BiNormal[2];
+    Normal[2] = Tangent[0] * BiNormal[1] - Tangent[1] * BiNormal[0];
 
-    Xcoord_Normal.push_back(Normal[0]); Ycoord_Normal.push_back(Normal[1]); Zcoord_Normal.push_back(Normal[2]);
+    Xcoord_Normal.push_back(Normal[0]);
+    Ycoord_Normal.push_back(Normal[1]);
+    Zcoord_Normal.push_back(Normal[2]);
 
     unsigned short index = 2;
 
@@ -9753,23 +9420,27 @@ su2double CPhysicalGeometry::Compute_Thickness(su2double *Plane_P0, su2double *P
       Xcoord_Upper.push_back(Xcoord_Airfoil_[iVertex]);
       Ycoord_Upper.push_back(Ycoord_Airfoil_[iVertex]);
       Zcoord_Upper.push_back(Zcoord_Airfoil_[iVertex]);
-    }
-    else {
+    } else {
       Xcoord_Lower.push_back(Xcoord_Airfoil_[iVertex]);
       Ycoord_Lower.push_back(Ycoord_Airfoil_[iVertex]);
       Zcoord_Lower.push_back(Zcoord_Airfoil_[iVertex]);
     }
-
   }
 
   /*--- Order the arrays using the X component ---*/
 
   for (iVertex = 0; iVertex < Xcoord_Upper.size(); iVertex++) {
     for (jVertex = 0; jVertex < Xcoord_Upper.size() - 1 - iVertex; jVertex++) {
-      if (Xcoord_Upper[jVertex] > Xcoord_Upper[jVertex+1]) {
-        auxXCoord = Xcoord_Upper[jVertex]; Xcoord_Upper[jVertex] = Xcoord_Upper[jVertex+1]; Xcoord_Upper[jVertex+1] = auxXCoord;
-        auxYCoord = Ycoord_Upper[jVertex]; Ycoord_Upper[jVertex] = Ycoord_Upper[jVertex+1]; Ycoord_Upper[jVertex+1] = auxYCoord;
-        auxZCoord = Zcoord_Upper[jVertex]; Zcoord_Upper[jVertex] = Zcoord_Upper[jVertex+1]; Zcoord_Upper[jVertex+1] = auxZCoord;
+      if (Xcoord_Upper[jVertex] > Xcoord_Upper[jVertex + 1]) {
+        auxXCoord = Xcoord_Upper[jVertex];
+        Xcoord_Upper[jVertex] = Xcoord_Upper[jVertex + 1];
+        Xcoord_Upper[jVertex + 1] = auxXCoord;
+        auxYCoord = Ycoord_Upper[jVertex];
+        Ycoord_Upper[jVertex] = Ycoord_Upper[jVertex + 1];
+        Ycoord_Upper[jVertex + 1] = auxYCoord;
+        auxZCoord = Zcoord_Upper[jVertex];
+        Zcoord_Upper[jVertex] = Zcoord_Upper[jVertex + 1];
+        Zcoord_Upper[jVertex + 1] = auxZCoord;
       }
     }
   }
@@ -9778,10 +9449,16 @@ su2double CPhysicalGeometry::Compute_Thickness(su2double *Plane_P0, su2double *P
 
   for (iVertex = 0; iVertex < Xcoord_Lower.size(); iVertex++) {
     for (jVertex = 0; jVertex < Xcoord_Lower.size() - 1 - iVertex; jVertex++) {
-      if (Xcoord_Lower[jVertex] > Xcoord_Lower[jVertex+1]) {
-        auxXCoord = Xcoord_Lower[jVertex]; Xcoord_Lower[jVertex] = Xcoord_Lower[jVertex+1]; Xcoord_Lower[jVertex+1] = auxXCoord;
-        auxYCoord = Ycoord_Lower[jVertex]; Ycoord_Lower[jVertex] = Ycoord_Lower[jVertex+1]; Ycoord_Lower[jVertex+1] = auxYCoord;
-        auxZCoord = Zcoord_Lower[jVertex]; Zcoord_Lower[jVertex] = Zcoord_Lower[jVertex+1]; Zcoord_Lower[jVertex+1] = auxZCoord;
+      if (Xcoord_Lower[jVertex] > Xcoord_Lower[jVertex + 1]) {
+        auxXCoord = Xcoord_Lower[jVertex];
+        Xcoord_Lower[jVertex] = Xcoord_Lower[jVertex + 1];
+        Xcoord_Lower[jVertex + 1] = auxXCoord;
+        auxYCoord = Ycoord_Lower[jVertex];
+        Ycoord_Lower[jVertex] = Ycoord_Lower[jVertex + 1];
+        Ycoord_Lower[jVertex + 1] = auxYCoord;
+        auxZCoord = Zcoord_Lower[jVertex];
+        Zcoord_Lower[jVertex] = Zcoord_Lower[jVertex + 1];
+        Zcoord_Lower[jVertex + 1] = auxZCoord;
       }
     }
   }
@@ -9790,45 +9467,47 @@ su2double CPhysicalGeometry::Compute_Thickness(su2double *Plane_P0, su2double *P
   n_Lower = Xcoord_Lower.size();
 
   if ((n_Upper > 1) && (n_Lower > 1)) {
-
-    zp1 = (Zcoord_Upper[1]-Zcoord_Upper[0])/(Xcoord_Upper[1]-Xcoord_Upper[0]);
-    zpn = (Zcoord_Upper[n_Upper-1]-Zcoord_Upper[n_Upper-2])/(Xcoord_Upper[n_Upper-1]-Xcoord_Upper[n_Upper-2]);
+    zp1 = (Zcoord_Upper[1] - Zcoord_Upper[0]) / (Xcoord_Upper[1] - Xcoord_Upper[0]);
+    zpn = (Zcoord_Upper[n_Upper - 1] - Zcoord_Upper[n_Upper - 2]) /
+          (Xcoord_Upper[n_Upper - 1] - Xcoord_Upper[n_Upper - 2]);
 
     CCubicSpline splineUpper(Xcoord_Upper, Zcoord_Upper, CCubicSpline::FIRST, zp1, CCubicSpline::FIRST, zpn);
 
-    zp1 = (Zcoord_Lower[1]-Zcoord_Lower[0])/(Xcoord_Lower[1]-Xcoord_Lower[0]);
-    zpn = (Zcoord_Lower[n_Lower-1]-Zcoord_Lower[n_Lower-2])/(Xcoord_Lower[n_Lower-1]-Xcoord_Lower[n_Lower-2]);
+    zp1 = (Zcoord_Lower[1] - Zcoord_Lower[0]) / (Xcoord_Lower[1] - Xcoord_Lower[0]);
+    zpn = (Zcoord_Lower[n_Lower - 1] - Zcoord_Lower[n_Lower - 2]) /
+          (Xcoord_Lower[n_Lower - 1] - Xcoord_Lower[n_Lower - 2]);
 
     CCubicSpline splineLower(Xcoord_Lower, Zcoord_Lower, CCubicSpline::FIRST, zp1, CCubicSpline::FIRST, zpn);
 
-    Thickness_Location = - Chord*(1.0-Location);
+    Thickness_Location = -Chord * (1.0 - Location);
 
     Zcoord_Up = splineUpper(Thickness_Location);
     Zcoord_Down = splineLower(Thickness_Location);
 
     YLoc_ = Thickness_Location;
-    ZLoc_ = 0.5*(Zcoord_Up + Zcoord_Down);
+    ZLoc_ = 0.5 * (Zcoord_Up + Zcoord_Down);
 
-    ZLoc = sin(-AoA*PI_NUMBER/180.0)*YLoc_ + cos(-AoA*PI_NUMBER/180.0)*ZLoc_ + Zcoord_Trailing;
+    ZLoc = sin(-AoA * PI_NUMBER / 180.0) * YLoc_ + cos(-AoA * PI_NUMBER / 180.0) * ZLoc_ + Zcoord_Trailing;
 
     /*--- Compute the thickness (we add a fabs because we can not guarantee the
      right sorting of the points and the upper and/or lower part of the airfoil is not well defined) ---*/
 
     Thickness_Value = fabs(Zcoord_Up - Zcoord_Down);
 
+  } else {
+    Thickness_Value = 0.0;
   }
-  else { Thickness_Value = 0.0; }
 
   return Thickness_Value;
-
 }
 
-su2double CPhysicalGeometry::Compute_Area(su2double *Plane_P0, su2double *Plane_Normal, CConfig *config,
-                                          vector<su2double> &Xcoord_Airfoil, vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) {
+su2double CPhysicalGeometry::Compute_Area(su2double* Plane_P0, su2double* Plane_Normal, CConfig* config,
+                                          vector<su2double>& Xcoord_Airfoil, vector<su2double>& Ycoord_Airfoil,
+                                          vector<su2double>& Zcoord_Airfoil) {
   unsigned long iVertex;
   su2double Area_Value = 0.0;
-  vector<su2double> Xcoord_Upper, Ycoord_Upper, Zcoord_Upper, Xcoord_Lower, Ycoord_Lower, Zcoord_Lower, Z2coord, Xcoord_Normal,
-                    Ycoord_Normal, Zcoord_Normal, Xcoord_Airfoil_, Ycoord_Airfoil_, Zcoord_Airfoil_;
+  vector<su2double> Xcoord_Upper, Ycoord_Upper, Zcoord_Upper, Xcoord_Lower, Ycoord_Lower, Zcoord_Lower, Z2coord,
+      Xcoord_Normal, Ycoord_Normal, Zcoord_Normal, Xcoord_Airfoil_, Ycoord_Airfoil_, Zcoord_Airfoil_;
   su2double DeltaZ, DeltaX, X, Z;
 
   /*--- Use the Green theorem to evaluate the area (the points have been sortered),
@@ -9836,28 +9515,28 @@ su2double CPhysicalGeometry::Compute_Area(su2double *Plane_P0, su2double *Plane_
 
   Area_Value = 0.0;
 
-  for (iVertex = 0; iVertex < Xcoord_Airfoil.size()-1; iVertex++) {
-    X = 0.5*(Xcoord_Airfoil[iVertex]+Xcoord_Airfoil[iVertex+1]);
-    Z = 0.5*(Zcoord_Airfoil[iVertex]+Zcoord_Airfoil[iVertex+1]);
-    DeltaX = Xcoord_Airfoil[iVertex+1] - Xcoord_Airfoil[iVertex];
-    DeltaZ = Zcoord_Airfoil[iVertex+1] - Zcoord_Airfoil[iVertex];
-    Area_Value += 0.5*( X*DeltaZ-Z*DeltaX);
+  for (iVertex = 0; iVertex < Xcoord_Airfoil.size() - 1; iVertex++) {
+    X = 0.5 * (Xcoord_Airfoil[iVertex] + Xcoord_Airfoil[iVertex + 1]);
+    Z = 0.5 * (Zcoord_Airfoil[iVertex] + Zcoord_Airfoil[iVertex + 1]);
+    DeltaX = Xcoord_Airfoil[iVertex + 1] - Xcoord_Airfoil[iVertex];
+    DeltaZ = Zcoord_Airfoil[iVertex + 1] - Zcoord_Airfoil[iVertex];
+    Area_Value += 0.5 * (X * DeltaZ - Z * DeltaX);
   }
 
-  X = 0.5*(Xcoord_Airfoil[Xcoord_Airfoil.size()-1]+Xcoord_Airfoil[0]);
-  Z = 0.5*(Zcoord_Airfoil[Xcoord_Airfoil.size()-1]+Zcoord_Airfoil[0]);
-  DeltaX = Xcoord_Airfoil[0] - Xcoord_Airfoil[Xcoord_Airfoil.size()-1];
-  DeltaZ = Zcoord_Airfoil[0] - Zcoord_Airfoil[Xcoord_Airfoil.size()-1];
-  Area_Value += 0.5 * (X*DeltaZ-Z*DeltaX);
+  X = 0.5 * (Xcoord_Airfoil[Xcoord_Airfoil.size() - 1] + Xcoord_Airfoil[0]);
+  Z = 0.5 * (Zcoord_Airfoil[Xcoord_Airfoil.size() - 1] + Zcoord_Airfoil[0]);
+  DeltaX = Xcoord_Airfoil[0] - Xcoord_Airfoil[Xcoord_Airfoil.size() - 1];
+  DeltaZ = Zcoord_Airfoil[0] - Zcoord_Airfoil[Xcoord_Airfoil.size() - 1];
+  Area_Value += 0.5 * (X * DeltaZ - Z * DeltaX);
 
   Area_Value = fabs(Area_Value);
 
   return Area_Value;
-
 }
 
-su2double CPhysicalGeometry::Compute_Length(su2double *Plane_P0, su2double *Plane_Normal, CConfig *config,
-                                          vector<su2double> &Xcoord_Airfoil, vector<su2double> &Ycoord_Airfoil, vector<su2double> &Zcoord_Airfoil) {
+su2double CPhysicalGeometry::Compute_Length(su2double* Plane_P0, su2double* Plane_Normal, CConfig* config,
+                                            vector<su2double>& Xcoord_Airfoil, vector<su2double>& Ycoord_Airfoil,
+                                            vector<su2double>& Zcoord_Airfoil) {
   unsigned long iVertex;
   su2double Length_Value = 0.0, Length_Value_ = 0.0;
   su2double DeltaZ, DeltaX;
@@ -9867,35 +9546,35 @@ su2double CPhysicalGeometry::Compute_Length(su2double *Plane_P0, su2double *Plan
    both distance and picked the smallest one ---*/
 
   Length_Value = 0.0;
-  for (iVertex = 0; iVertex < Xcoord_Airfoil.size()-2; iVertex++) {
-    DeltaX = Xcoord_Airfoil[iVertex+1] - Xcoord_Airfoil[iVertex];
-    DeltaZ = Zcoord_Airfoil[iVertex+1] - Zcoord_Airfoil[iVertex];
-    Length_Value += sqrt(DeltaX*DeltaX + DeltaZ*DeltaZ);
+  for (iVertex = 0; iVertex < Xcoord_Airfoil.size() - 2; iVertex++) {
+    DeltaX = Xcoord_Airfoil[iVertex + 1] - Xcoord_Airfoil[iVertex];
+    DeltaZ = Zcoord_Airfoil[iVertex + 1] - Zcoord_Airfoil[iVertex];
+    Length_Value += sqrt(DeltaX * DeltaX + DeltaZ * DeltaZ);
   }
 
   Length_Value_ = 0.0;
-  for (iVertex = 1; iVertex < Xcoord_Airfoil.size()-1; iVertex++) {
-    DeltaX = Xcoord_Airfoil[iVertex+1] - Xcoord_Airfoil[iVertex];
-    DeltaZ = Zcoord_Airfoil[iVertex+1] - Zcoord_Airfoil[iVertex];
-    Length_Value_ += sqrt(DeltaX*DeltaX + DeltaZ*DeltaZ);
+  for (iVertex = 1; iVertex < Xcoord_Airfoil.size() - 1; iVertex++) {
+    DeltaX = Xcoord_Airfoil[iVertex + 1] - Xcoord_Airfoil[iVertex];
+    DeltaZ = Zcoord_Airfoil[iVertex + 1] - Zcoord_Airfoil[iVertex];
+    Length_Value_ += sqrt(DeltaX * DeltaX + DeltaZ * DeltaZ);
   }
 
   Length_Value = min(Length_Value, Length_Value_);
 
   return Length_Value;
-
 }
 
-void CPhysicalGeometry::Compute_Wing(CConfig *config, bool original_surface,
-                                     su2double &Wing_Volume, su2double &Wing_MinMaxThickness, su2double &Wing_MaxMaxThickness, su2double &Wing_MinChord, su2double &Wing_MaxChord,
-                                     su2double &Wing_MinLERadius, su2double &Wing_MaxLERadius,
-                                     su2double &Wing_MinToC, su2double &Wing_MaxToC, su2double &Wing_ObjFun_MinToC, su2double &Wing_MaxTwist, su2double &Wing_MaxCurvature,
-                                     su2double &Wing_MaxDihedral) {
-
+void CPhysicalGeometry::Compute_Wing(CConfig* config, bool original_surface, su2double& Wing_Volume,
+                                     su2double& Wing_MinMaxThickness, su2double& Wing_MaxMaxThickness,
+                                     su2double& Wing_MinChord, su2double& Wing_MaxChord, su2double& Wing_MinLERadius,
+                                     su2double& Wing_MaxLERadius, su2double& Wing_MinToC, su2double& Wing_MaxToC,
+                                     su2double& Wing_ObjFun_MinToC, su2double& Wing_MaxTwist,
+                                     su2double& Wing_MaxCurvature, su2double& Wing_MaxDihedral) {
   unsigned short iPlane, iDim, nPlane = 0;
   unsigned long iVertex;
-  su2double MinPlane, MaxPlane, dPlane, *Area, *MaxThickness, *ToC, *Chord, *LERadius, *Twist, *Curvature, *Dihedral, SemiSpan;
-  vector<su2double> *Xcoord_Airfoil, *Ycoord_Airfoil, *Zcoord_Airfoil, *Variable_Airfoil;
+  su2double MinPlane, MaxPlane, dPlane, *Area, *MaxThickness, *ToC, *Chord, *LERadius, *Twist, *Curvature, *Dihedral,
+      SemiSpan;
+  vector<su2double>*Xcoord_Airfoil, *Ycoord_Airfoil, *Zcoord_Airfoil, *Variable_Airfoil;
   ofstream Wing_File, Section_File;
 
   /*--- Make a large number of section cuts for approximating volume ---*/
@@ -9905,160 +9584,173 @@ void CPhysicalGeometry::Compute_Wing(CConfig *config, bool original_surface,
 
   /*--- Allocate memory for the section cutting ---*/
 
-  Area = new su2double [nPlane];
-  MaxThickness = new su2double [nPlane];
-  Chord = new su2double [nPlane];
-  LERadius = new su2double [nPlane];
-  ToC = new su2double [nPlane];
-  Twist = new su2double [nPlane];
-  Curvature = new su2double [nPlane];
-  Dihedral = new su2double [nPlane];
+  Area = new su2double[nPlane];
+  MaxThickness = new su2double[nPlane];
+  Chord = new su2double[nPlane];
+  LERadius = new su2double[nPlane];
+  ToC = new su2double[nPlane];
+  Twist = new su2double[nPlane];
+  Curvature = new su2double[nPlane];
+  Dihedral = new su2double[nPlane];
 
-  su2double **LeadingEdge = new su2double*[nPlane];
-  for (iPlane = 0; iPlane < nPlane; iPlane++ )
-    LeadingEdge[iPlane] = new su2double[nDim];
+  su2double** LeadingEdge = new su2double*[nPlane];
+  for (iPlane = 0; iPlane < nPlane; iPlane++) LeadingEdge[iPlane] = new su2double[nDim];
 
-  su2double **TrailingEdge = new su2double*[nPlane];
-  for (iPlane = 0; iPlane < nPlane; iPlane++ )
-    TrailingEdge[iPlane] = new su2double[nDim];
+  su2double** TrailingEdge = new su2double*[nPlane];
+  for (iPlane = 0; iPlane < nPlane; iPlane++) TrailingEdge[iPlane] = new su2double[nDim];
 
-  su2double **Plane_P0 = new su2double*[nPlane];
-  for (iPlane = 0; iPlane < nPlane; iPlane++ )
-    Plane_P0[iPlane] = new su2double[nDim];
+  su2double** Plane_P0 = new su2double*[nPlane];
+  for (iPlane = 0; iPlane < nPlane; iPlane++) Plane_P0[iPlane] = new su2double[nDim];
 
-  su2double **Plane_Normal = new su2double*[nPlane];
-  for (iPlane = 0; iPlane < nPlane; iPlane++ )
-    Plane_Normal[iPlane] = new su2double[nDim];
+  su2double** Plane_Normal = new su2double*[nPlane];
+  for (iPlane = 0; iPlane < nPlane; iPlane++) Plane_Normal[iPlane] = new su2double[nDim];
 
-  MinPlane = config->GetStations_Bounds(0); MaxPlane = config->GetStations_Bounds(1);
-  dPlane = fabs((MaxPlane - MinPlane)/su2double(nPlane-1));
+  MinPlane = config->GetStations_Bounds(0);
+  MaxPlane = config->GetStations_Bounds(1);
+  dPlane = fabs((MaxPlane - MinPlane) / su2double(nPlane - 1));
 
   for (iPlane = 0; iPlane < nPlane; iPlane++) {
-    Plane_Normal[iPlane][0] = 0.0;    Plane_P0[iPlane][0] = 0.0;
-    Plane_Normal[iPlane][1] = 0.0;    Plane_P0[iPlane][1] = 0.0;
-    Plane_Normal[iPlane][2] = 0.0;    Plane_P0[iPlane][2] = 0.0;
+    Plane_Normal[iPlane][0] = 0.0;
+    Plane_P0[iPlane][0] = 0.0;
+    Plane_Normal[iPlane][1] = 0.0;
+    Plane_P0[iPlane][1] = 0.0;
+    Plane_Normal[iPlane][2] = 0.0;
+    Plane_P0[iPlane][2] = 0.0;
 
     if (config->GetGeo_Description() == WING) {
       Plane_Normal[iPlane][1] = 1.0;
-      Plane_P0[iPlane][1] = MinPlane + iPlane*dPlane;
+      Plane_P0[iPlane][1] = MinPlane + iPlane * dPlane;
     }
 
     if (config->GetGeo_Description() == TWOD_AIRFOIL) {
       Plane_Normal[iPlane][2] = 1.0;
-      Plane_P0[iPlane][2] = MinPlane + iPlane*dPlane;
+      Plane_P0[iPlane][2] = MinPlane + iPlane * dPlane;
     }
-
   }
 
   /*--- Allocate some vectors for storing airfoil coordinates ---*/
 
-  Xcoord_Airfoil   = new vector<su2double>[nPlane];
-  Ycoord_Airfoil   = new vector<su2double>[nPlane];
-  Zcoord_Airfoil   = new vector<su2double>[nPlane];
+  Xcoord_Airfoil = new vector<su2double>[nPlane];
+  Ycoord_Airfoil = new vector<su2double>[nPlane];
+  Zcoord_Airfoil = new vector<su2double>[nPlane];
   Variable_Airfoil = new vector<su2double>[nPlane];
 
   /*--- Create the section slices through the geometry ---*/
 
   for (iPlane = 0; iPlane < nPlane; iPlane++) {
-
-    ComputeAirfoil_Section(Plane_P0[iPlane], Plane_Normal[iPlane],
-                           -1E6, 1E6, -1E6, 1E6, -1E6, 1E6, nullptr, Xcoord_Airfoil[iPlane],
-                           Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane],
+    ComputeAirfoil_Section(Plane_P0[iPlane], Plane_Normal[iPlane], -1E6, 1E6, -1E6, 1E6, -1E6, 1E6, nullptr,
+                           Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane],
                            Variable_Airfoil[iPlane], original_surface, config);
-
-   }
+  }
 
   /*--- Compute airfoil characteristic only in the master node ---*/
 
   if (rank == MASTER_NODE) {
-
     /*--- Write an output file---*/
 
     if (config->GetTabular_FileFormat() == TAB_OUTPUT::TAB_CSV) {
       Wing_File.open("wing_description.csv", ios::out);
       if (config->GetSystemMeasurements() == US)
-        Wing_File << "\"yCoord/SemiSpan\",\"Area (in^2)\",\"Max. Thickness (in)\",\"Chord (in)\",\"Leading Edge Radius (1/in)\",\"Max. Thickness/Chord\",\"Twist (deg)\",\"Curvature (1/in)\",\"Dihedral (deg)\",\"Leading Edge XLoc/SemiSpan\",\"Leading Edge ZLoc/SemiSpan\",\"Trailing Edge XLoc/SemiSpan\",\"Trailing Edge ZLoc/SemiSpan\"" << endl;
+        Wing_File << "\"yCoord/SemiSpan\",\"Area (in^2)\",\"Max. Thickness (in)\",\"Chord (in)\",\"Leading Edge Radius "
+                     "(1/in)\",\"Max. Thickness/Chord\",\"Twist (deg)\",\"Curvature (1/in)\",\"Dihedral "
+                     "(deg)\",\"Leading Edge XLoc/SemiSpan\",\"Leading Edge ZLoc/SemiSpan\",\"Trailing Edge "
+                     "XLoc/SemiSpan\",\"Trailing Edge ZLoc/SemiSpan\""
+                  << endl;
       else
-        Wing_File << "\"yCoord/SemiSpan\",\"Area (m^2)\",\"Max. Thickness (m)\",\"Chord (m)\",\"Leading Edge Radius (1/m)\",\"Max. Thickness/Chord\",\"Twist (deg)\",\"Curvature (1/in)\",\"Dihedral (deg)\",\"Leading Edge XLoc/SemiSpan\",\"Leading Edge ZLoc/SemiSpan\",\"Trailing Edge XLoc/SemiSpan\",\"Trailing Edge ZLoc/SemiSpan\"" << endl;
-    }
-    else {
+        Wing_File << "\"yCoord/SemiSpan\",\"Area (m^2)\",\"Max. Thickness (m)\",\"Chord (m)\",\"Leading Edge Radius "
+                     "(1/m)\",\"Max. Thickness/Chord\",\"Twist (deg)\",\"Curvature (1/in)\",\"Dihedral "
+                     "(deg)\",\"Leading Edge XLoc/SemiSpan\",\"Leading Edge ZLoc/SemiSpan\",\"Trailing Edge "
+                     "XLoc/SemiSpan\",\"Trailing Edge ZLoc/SemiSpan\""
+                  << endl;
+    } else {
       Wing_File.open("wing_description.dat", ios::out);
       Wing_File << "TITLE = \"Wing description\"" << endl;
       if (config->GetSystemMeasurements() == US)
-        Wing_File << "VARIABLES = \"<greek>h</greek>\",\"Area (in<sup>2</sup>)\",\"Max. Thickness (in)\",\"Chord (in)\",\"Leading Edge Radius (1/in)\",\"Max. Thickness/Chord\",\"Twist (deg)\",\"Curvature (1/in)\",\"Dihedral (deg)\",\"Leading Edge XLoc/SemiSpan\",\"Leading Edge ZLoc/SemiSpan\",\"Trailing Edge XLoc/SemiSpan\",\"Trailing Edge ZLoc/SemiSpan\"" << endl;
+        Wing_File << "VARIABLES = \"<greek>h</greek>\",\"Area (in<sup>2</sup>)\",\"Max. Thickness (in)\",\"Chord "
+                     "(in)\",\"Leading Edge Radius (1/in)\",\"Max. Thickness/Chord\",\"Twist (deg)\",\"Curvature "
+                     "(1/in)\",\"Dihedral (deg)\",\"Leading Edge XLoc/SemiSpan\",\"Leading Edge "
+                     "ZLoc/SemiSpan\",\"Trailing Edge XLoc/SemiSpan\",\"Trailing Edge ZLoc/SemiSpan\""
+                  << endl;
       else
-        Wing_File << "VARIABLES = \"<greek>h</greek>\",\"Area (m<sup>2</sup>)\",\"Max. Thickness (m)\",\"Chord (m)\",\"Leading Edge Radius (1/m)\",\"Max. Thickness/Chord\",\"Twist (deg)\",\"Curvature (1/m)\",\"Dihedral (deg)\",\"Leading Edge XLoc/SemiSpan\",\"Leading Edge ZLoc/SemiSpan\",\"Trailing Edge XLoc/SemiSpan\",\"Trailing Edge ZLoc/SemiSpan\"" << endl;
+        Wing_File << "VARIABLES = \"<greek>h</greek>\",\"Area (m<sup>2</sup>)\",\"Max. Thickness (m)\",\"Chord "
+                     "(m)\",\"Leading Edge Radius (1/m)\",\"Max. Thickness/Chord\",\"Twist (deg)\",\"Curvature "
+                     "(1/m)\",\"Dihedral (deg)\",\"Leading Edge XLoc/SemiSpan\",\"Leading Edge "
+                     "ZLoc/SemiSpan\",\"Trailing Edge XLoc/SemiSpan\",\"Trailing Edge ZLoc/SemiSpan\""
+                  << endl;
       Wing_File << "ZONE T= \"Baseline wing\"" << endl;
     }
 
-
     /*--- Evaluate  geometrical quatities that do not require any kind of filter, local to each point ---*/
 
     for (iPlane = 0; iPlane < nPlane; iPlane++) {
-
       for (iDim = 0; iDim < nDim; iDim++) {
-        LeadingEdge[iPlane][iDim]  = 0.0;
+        LeadingEdge[iPlane][iDim] = 0.0;
         TrailingEdge[iPlane][iDim] = 0.0;
       }
 
-      Area[iPlane]                = 0.0;
-      MaxThickness[iPlane]        = 0.0;
-      Chord[iPlane]               = 0.0;
-      LERadius[iPlane]            = 0.0;
-      ToC[iPlane]                 = 0.0;
-      Twist[iPlane]               = 0.0;
+      Area[iPlane] = 0.0;
+      MaxThickness[iPlane] = 0.0;
+      Chord[iPlane] = 0.0;
+      LERadius[iPlane] = 0.0;
+      ToC[iPlane] = 0.0;
+      Twist[iPlane] = 0.0;
 
       if (Xcoord_Airfoil[iPlane].size() > 1) {
+        Compute_Wing_LeadingTrailing(LeadingEdge[iPlane], TrailingEdge[iPlane], Plane_P0[iPlane], Plane_Normal[iPlane],
+                                     Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
 
-        Compute_Wing_LeadingTrailing(LeadingEdge[iPlane], TrailingEdge[iPlane], Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+        Area[iPlane] = Compute_Area(Plane_P0[iPlane], Plane_Normal[iPlane], config, Xcoord_Airfoil[iPlane],
+                                    Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
 
-        Area[iPlane] = Compute_Area(Plane_P0[iPlane], Plane_Normal[iPlane], config, Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+        MaxThickness[iPlane] =
+            Compute_MaxThickness(Plane_P0[iPlane], Plane_Normal[iPlane], config, Xcoord_Airfoil[iPlane],
+                                 Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
 
-        MaxThickness[iPlane] = Compute_MaxThickness(Plane_P0[iPlane], Plane_Normal[iPlane], config, Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+        Chord[iPlane] = Compute_Chord(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane],
+                                      Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
 
-        Chord[iPlane] = Compute_Chord(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+        Twist[iPlane] = Compute_Twist(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane],
+                                      Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
 
-        Twist[iPlane] = Compute_Twist(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-
-        LERadius[iPlane] = Compute_LERadius(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+        LERadius[iPlane] = Compute_LERadius(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane],
+                                            Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
 
         ToC[iPlane] = MaxThickness[iPlane] / Chord[iPlane];
-
-
       }
-
     }
 
-    /*--- Evaluate  geometrical quatities that have been computed using a filtered value (they depend on more than one point) ---*/
+    /*--- Evaluate  geometrical quatities that have been computed using a filtered value (they depend on more than one
+     * point) ---*/
 
     for (iPlane = 0; iPlane < nPlane; iPlane++) {
-
-      Curvature[iPlane]      = 0.0;
-      Dihedral[iPlane]       = 0.0;
+      Curvature[iPlane] = 0.0;
+      Dihedral[iPlane] = 0.0;
 
       if (Xcoord_Airfoil[iPlane].size() > 1) {
+        if ((iPlane == 0) || (iPlane == nPlane - 1))
+          Curvature[iPlane] = 0.0;
+        else
+          Curvature[iPlane] =
+              Compute_Curvature(LeadingEdge[iPlane - 1], TrailingEdge[iPlane - 1], LeadingEdge[iPlane],
+                                TrailingEdge[iPlane], LeadingEdge[iPlane + 1], TrailingEdge[iPlane + 1]);
 
-        if ((iPlane == 0) || (iPlane == nPlane-1)) Curvature[iPlane] = 0.0;
-        else Curvature[iPlane] = Compute_Curvature(LeadingEdge[iPlane-1], TrailingEdge[iPlane-1],
-                                                   LeadingEdge[iPlane], TrailingEdge[iPlane],
-                                                   LeadingEdge[iPlane+1], TrailingEdge[iPlane+1]);
-
-        if (iPlane == 0) Dihedral[iPlane] = 0.0;
-        else Dihedral[iPlane] = Compute_Dihedral(LeadingEdge[iPlane-1], TrailingEdge[iPlane-1],
-                                                 LeadingEdge[iPlane], TrailingEdge[iPlane]);
-
+        if (iPlane == 0)
+          Dihedral[iPlane] = 0.0;
+        else
+          Dihedral[iPlane] = Compute_Dihedral(LeadingEdge[iPlane - 1], TrailingEdge[iPlane - 1], LeadingEdge[iPlane],
+                                              TrailingEdge[iPlane]);
       }
-
     }
 
     /*--- Set the curvature and dihedral angles at the extremes ---*/
 
     if (nPlane > 1) {
       if ((Xcoord_Airfoil[0].size() != 0) && (Xcoord_Airfoil[1].size() != 0)) {
-        Curvature[0] = Curvature[1]; Dihedral[0] = Dihedral[1];
+        Curvature[0] = Curvature[1];
+        Dihedral[0] = Dihedral[1];
       }
-      if ((Xcoord_Airfoil[nPlane-1].size() != 0) && (Xcoord_Airfoil[nPlane-2].size() != 0)) {
-        Curvature[nPlane-1] = Curvature[nPlane-2];
+      if ((Xcoord_Airfoil[nPlane - 1].size() != 0) && (Xcoord_Airfoil[nPlane - 2].size() != 0)) {
+        Curvature[nPlane - 1] = Curvature[nPlane - 2];
       }
     }
 
@@ -10067,17 +9759,17 @@ void CPhysicalGeometry::Compute_Wing(CConfig *config, bool original_surface,
     for (iPlane = 0; iPlane < nPlane; iPlane++) {
       if (Xcoord_Airfoil[iPlane].size() > 1) {
         if (config->GetTabular_FileFormat() == TAB_OUTPUT::TAB_CSV) {
-          Wing_File  << Ycoord_Airfoil[iPlane][0]/SemiSpan <<", "<< Area[iPlane] <<", "<< MaxThickness[iPlane] <<", "<< Chord[iPlane] <<", "<< LERadius[iPlane] <<", "<< ToC[iPlane]
-                     <<", "<< Twist[iPlane] <<", "<< Curvature[iPlane] <<", "<< Dihedral[iPlane]
-                     <<", "<< LeadingEdge[iPlane][0]/SemiSpan <<", "<< LeadingEdge[iPlane][2]/SemiSpan
-                     <<", "<< TrailingEdge[iPlane][0]/SemiSpan <<", "<< TrailingEdge[iPlane][2]/SemiSpan << endl;
-        }
-        else  {
-          Wing_File  << Ycoord_Airfoil[iPlane][0]/SemiSpan <<" "<< Area[iPlane] <<" "<< MaxThickness[iPlane] <<" "<< Chord[iPlane] <<" "<< LERadius[iPlane] <<" "<< ToC[iPlane]
-                     <<" "<< Twist[iPlane] <<" "<< Curvature[iPlane]  <<" "<< Dihedral[iPlane]
-                     <<" "<< LeadingEdge[iPlane][0]/SemiSpan <<" "<< LeadingEdge[iPlane][2]/SemiSpan
-                     <<" "<< TrailingEdge[iPlane][0]/SemiSpan <<" "<< TrailingEdge[iPlane][2]/SemiSpan << endl;
-
+          Wing_File << Ycoord_Airfoil[iPlane][0] / SemiSpan << ", " << Area[iPlane] << ", " << MaxThickness[iPlane]
+                    << ", " << Chord[iPlane] << ", " << LERadius[iPlane] << ", " << ToC[iPlane] << ", " << Twist[iPlane]
+                    << ", " << Curvature[iPlane] << ", " << Dihedral[iPlane] << ", "
+                    << LeadingEdge[iPlane][0] / SemiSpan << ", " << LeadingEdge[iPlane][2] / SemiSpan << ", "
+                    << TrailingEdge[iPlane][0] / SemiSpan << ", " << TrailingEdge[iPlane][2] / SemiSpan << endl;
+        } else {
+          Wing_File << Ycoord_Airfoil[iPlane][0] / SemiSpan << " " << Area[iPlane] << " " << MaxThickness[iPlane] << " "
+                    << Chord[iPlane] << " " << LERadius[iPlane] << " " << ToC[iPlane] << " " << Twist[iPlane] << " "
+                    << Curvature[iPlane] << " " << Dihedral[iPlane] << " " << LeadingEdge[iPlane][0] / SemiSpan << " "
+                    << LeadingEdge[iPlane][2] / SemiSpan << " " << TrailingEdge[iPlane][0] / SemiSpan << " "
+                    << TrailingEdge[iPlane][2] / SemiSpan << endl;
         }
       }
     }
@@ -10087,20 +9779,21 @@ void CPhysicalGeometry::Compute_Wing(CConfig *config, bool original_surface,
     Section_File.open("wing_slices.dat", ios::out);
 
     for (iPlane = 0; iPlane < nPlane; iPlane++) {
-
       if (iPlane == 0) {
         Section_File << "TITLE = \"Aircraft Slices\"" << endl;
         if (config->GetSystemMeasurements() == US)
-          Section_File << "VARIABLES = \"x (in)\", \"y (in)\", \"z (in)\", \"x<sub>2D</sub>/c\", \"y<sub>2D</sub>/c\"" << endl;
-        else Section_File << "VARIABLES = \"x (m)\", \"y (m)\", \"z (m)\", \"x<sub>2D</sub>/c\", \"y<sub>2D</sub>/c\"" << endl;
+          Section_File << "VARIABLES = \"x (in)\", \"y (in)\", \"z (in)\", \"x<sub>2D</sub>/c\", \"y<sub>2D</sub>/c\""
+                       << endl;
+        else
+          Section_File << "VARIABLES = \"x (m)\", \"y (m)\", \"z (m)\", \"x<sub>2D</sub>/c\", \"y<sub>2D</sub>/c\""
+                       << endl;
       }
 
       if (Xcoord_Airfoil[iPlane].size() > 1) {
-
-        Section_File << "ZONE T=\"<greek>h</greek> = " << Ycoord_Airfoil[iPlane][0]/SemiSpan << " \", I= " << Xcoord_Airfoil[iPlane].size() << ", F=POINT" << endl;
+        Section_File << "ZONE T=\"<greek>h</greek> = " << Ycoord_Airfoil[iPlane][0] / SemiSpan
+                     << " \", I= " << Xcoord_Airfoil[iPlane].size() << ", F=POINT" << endl;
 
         for (iVertex = 0; iVertex < Xcoord_Airfoil[iPlane].size(); iVertex++) {
-
           /*--- Move to the origin  ---*/
 
           su2double XValue_ = Xcoord_Airfoil[iPlane][iVertex] - LeadingEdge[iPlane][0];
@@ -10108,37 +9801,44 @@ void CPhysicalGeometry::Compute_Wing(CConfig *config, bool original_surface,
 
           /*--- Rotate the airfoil and divide by the chord ---*/
 
-          su2double ValCos = cos(Twist[iPlane]*PI_NUMBER/180.0);
-          su2double ValSin = sin(Twist[iPlane]*PI_NUMBER/180.0);
+          su2double ValCos = cos(Twist[iPlane] * PI_NUMBER / 180.0);
+          su2double ValSin = sin(Twist[iPlane] * PI_NUMBER / 180.0);
 
-          su2double XValue = (XValue_*ValCos - ZValue_*ValSin) / Chord[iPlane];
-          su2double ZValue = (ZValue_*ValCos + XValue_*ValSin) / Chord[iPlane];
+          su2double XValue = (XValue_ * ValCos - ZValue_ * ValSin) / Chord[iPlane];
+          su2double ZValue = (ZValue_ * ValCos + XValue_ * ValSin) / Chord[iPlane];
 
           /*--- Write the file ---*/
 
-          Section_File  << Xcoord_Airfoil[iPlane][iVertex] << " " << Ycoord_Airfoil[iPlane][iVertex] << " " << Zcoord_Airfoil[iPlane][iVertex] << " " << XValue  << " " << ZValue << endl;
+          Section_File << Xcoord_Airfoil[iPlane][iVertex] << " " << Ycoord_Airfoil[iPlane][iVertex] << " "
+                       << Zcoord_Airfoil[iPlane][iVertex] << " " << XValue << " " << ZValue << endl;
         }
       }
-
     }
 
     Section_File.close();
 
-
     /*--- Compute the wing volume using a composite Simpson's rule ---*/
 
     Wing_Volume = 0.0;
-    for (iPlane = 0; iPlane < nPlane-2; iPlane+=2) {
+    for (iPlane = 0; iPlane < nPlane - 2; iPlane += 2) {
       if (Xcoord_Airfoil[iPlane].size() > 1) {
-        Wing_Volume += (1.0/3.0)*dPlane*(Area[iPlane] + 4.0*Area[iPlane+1] + Area[iPlane+2]);
+        Wing_Volume += (1.0 / 3.0) * dPlane * (Area[iPlane] + 4.0 * Area[iPlane + 1] + Area[iPlane + 2]);
       }
     }
 
     /*--- Evaluate Max and Min quantities ---*/
 
-    Wing_MaxMaxThickness = -1E6; Wing_MinMaxThickness = 1E6; Wing_MinChord = 1E6; Wing_MaxChord = -1E6;
-    Wing_MinLERadius = 1E6; Wing_MaxLERadius = -1E6; Wing_MinToC = 1E6; Wing_MaxToC = -1E6;
-    Wing_MaxTwist = -1E6; Wing_MaxCurvature = -1E6; Wing_MaxDihedral = -1E6;
+    Wing_MaxMaxThickness = -1E6;
+    Wing_MinMaxThickness = 1E6;
+    Wing_MinChord = 1E6;
+    Wing_MaxChord = -1E6;
+    Wing_MinLERadius = 1E6;
+    Wing_MaxLERadius = -1E6;
+    Wing_MinToC = 1E6;
+    Wing_MaxToC = -1E6;
+    Wing_MaxTwist = -1E6;
+    Wing_MaxCurvature = -1E6;
+    Wing_MaxDihedral = -1E6;
 
     for (iPlane = 0; iPlane < nPlane; iPlane++) {
       if (MaxThickness[iPlane] != 0.0) Wing_MinMaxThickness = min(Wing_MinMaxThickness, MaxThickness[iPlane]);
@@ -10149,59 +9849,51 @@ void CPhysicalGeometry::Compute_Wing(CConfig *config, bool original_surface,
       Wing_MaxLERadius = max(Wing_MaxLERadius, LERadius[iPlane]);
       if (ToC[iPlane] != 0.0) Wing_MinToC = min(Wing_MinToC, ToC[iPlane]);
       Wing_MaxToC = max(Wing_MaxToC, ToC[iPlane]);
-      Wing_ObjFun_MinToC = sqrt((Wing_MinToC - 0.07)*(Wing_MinToC - 0.07));
+      Wing_ObjFun_MinToC = sqrt((Wing_MinToC - 0.07) * (Wing_MinToC - 0.07));
       Wing_MaxTwist = max(Wing_MaxTwist, fabs(Twist[iPlane]));
       Wing_MaxCurvature = max(Wing_MaxCurvature, Curvature[iPlane]);
       Wing_MaxDihedral = max(Wing_MaxDihedral, fabs(Dihedral[iPlane]));
     }
-
   }
 
   /*--- Free memory for the section cuts ---*/
 
-  delete [] Xcoord_Airfoil;
-  delete [] Ycoord_Airfoil;
-  delete [] Zcoord_Airfoil;
-  delete [] Variable_Airfoil;
+  delete[] Xcoord_Airfoil;
+  delete[] Ycoord_Airfoil;
+  delete[] Zcoord_Airfoil;
+  delete[] Variable_Airfoil;
 
-  for (iPlane = 0; iPlane < nPlane; iPlane++)
-    delete [] LeadingEdge[iPlane];
-  delete [] LeadingEdge;
+  for (iPlane = 0; iPlane < nPlane; iPlane++) delete[] LeadingEdge[iPlane];
+  delete[] LeadingEdge;
 
-  for (iPlane = 0; iPlane < nPlane; iPlane++)
-    delete [] TrailingEdge[iPlane];
-  delete [] TrailingEdge;
+  for (iPlane = 0; iPlane < nPlane; iPlane++) delete[] TrailingEdge[iPlane];
+  delete[] TrailingEdge;
 
-  for (iPlane = 0; iPlane < nPlane; iPlane++)
-    delete [] Plane_P0[iPlane];
-  delete [] Plane_P0;
+  for (iPlane = 0; iPlane < nPlane; iPlane++) delete[] Plane_P0[iPlane];
+  delete[] Plane_P0;
 
-  for (iPlane = 0; iPlane < nPlane; iPlane++)
-    delete [] Plane_Normal[iPlane];
-  delete [] Plane_Normal;
-
-  delete [] Area;
-  delete [] MaxThickness;
-  delete [] Chord;
-  delete [] LERadius;
-  delete [] ToC;
-  delete [] Twist;
-  delete [] Curvature;
-  delete [] Dihedral;
+  for (iPlane = 0; iPlane < nPlane; iPlane++) delete[] Plane_Normal[iPlane];
+  delete[] Plane_Normal;
 
+  delete[] Area;
+  delete[] MaxThickness;
+  delete[] Chord;
+  delete[] LERadius;
+  delete[] ToC;
+  delete[] Twist;
+  delete[] Curvature;
+  delete[] Dihedral;
 }
 
-void CPhysicalGeometry::Compute_Fuselage(CConfig *config, bool original_surface,
-                                         su2double &Fuselage_Volume, su2double &Fuselage_WettedArea,
-                                         su2double &Fuselage_MinWidth, su2double &Fuselage_MaxWidth,
-                                         su2double &Fuselage_MinWaterLineWidth, su2double &Fuselage_MaxWaterLineWidth,
-                                         su2double &Fuselage_MinHeight, su2double &Fuselage_MaxHeight,
-                                         su2double &Fuselage_MaxCurvature) {
-
+void CPhysicalGeometry::Compute_Fuselage(CConfig* config, bool original_surface, su2double& Fuselage_Volume,
+                                         su2double& Fuselage_WettedArea, su2double& Fuselage_MinWidth,
+                                         su2double& Fuselage_MaxWidth, su2double& Fuselage_MinWaterLineWidth,
+                                         su2double& Fuselage_MaxWaterLineWidth, su2double& Fuselage_MinHeight,
+                                         su2double& Fuselage_MaxHeight, su2double& Fuselage_MaxCurvature) {
   unsigned short iPlane, iDim, nPlane = 0;
   unsigned long iVertex;
   su2double MinPlane, MaxPlane, dPlane, *Area, *Length, *Width, *WaterLineWidth, *Height, *Curvature;
-  vector<su2double> *Xcoord_Airfoil, *Ycoord_Airfoil, *Zcoord_Airfoil, *Variable_Airfoil;
+  vector<su2double>*Xcoord_Airfoil, *Ycoord_Airfoil, *Zcoord_Airfoil, *Variable_Airfoil;
   ofstream Fuselage_File, Section_File;
 
   /*--- Make a large number of section cuts for approximating volume ---*/
@@ -10210,131 +9902,144 @@ void CPhysicalGeometry::Compute_Fuselage(CConfig *config, bool original_surface,
 
   /*--- Allocate memory for the section cutting ---*/
 
-  Area = new su2double [nPlane];
-  Length = new su2double [nPlane];
-  Width = new su2double [nPlane];
-  WaterLineWidth = new su2double [nPlane];
-  Height = new su2double [nPlane];
-  Curvature = new su2double [nPlane];
+  Area = new su2double[nPlane];
+  Length = new su2double[nPlane];
+  Width = new su2double[nPlane];
+  WaterLineWidth = new su2double[nPlane];
+  Height = new su2double[nPlane];
+  Curvature = new su2double[nPlane];
 
-  su2double **LeadingEdge = new su2double*[nPlane];
-  for (iPlane = 0; iPlane < nPlane; iPlane++ )
-    LeadingEdge[iPlane] = new su2double[nDim];
+  su2double** LeadingEdge = new su2double*[nPlane];
+  for (iPlane = 0; iPlane < nPlane; iPlane++) LeadingEdge[iPlane] = new su2double[nDim];
 
-  su2double **TrailingEdge = new su2double*[nPlane];
-  for (iPlane = 0; iPlane < nPlane; iPlane++ )
-    TrailingEdge[iPlane] = new su2double[nDim];
+  su2double** TrailingEdge = new su2double*[nPlane];
+  for (iPlane = 0; iPlane < nPlane; iPlane++) TrailingEdge[iPlane] = new su2double[nDim];
 
-  su2double **Plane_P0 = new su2double*[nPlane];
-  for (iPlane = 0; iPlane < nPlane; iPlane++ )
-    Plane_P0[iPlane] = new su2double[nDim];
+  su2double** Plane_P0 = new su2double*[nPlane];
+  for (iPlane = 0; iPlane < nPlane; iPlane++) Plane_P0[iPlane] = new su2double[nDim];
 
-  su2double **Plane_Normal = new su2double*[nPlane];
-  for (iPlane = 0; iPlane < nPlane; iPlane++ )
-    Plane_Normal[iPlane] = new su2double[nDim];
+  su2double** Plane_Normal = new su2double*[nPlane];
+  for (iPlane = 0; iPlane < nPlane; iPlane++) Plane_Normal[iPlane] = new su2double[nDim];
 
-  MinPlane = config->GetStations_Bounds(0); MaxPlane = config->GetStations_Bounds(1);
-  dPlane = fabs((MaxPlane - MinPlane)/su2double(nPlane-1));
+  MinPlane = config->GetStations_Bounds(0);
+  MaxPlane = config->GetStations_Bounds(1);
+  dPlane = fabs((MaxPlane - MinPlane) / su2double(nPlane - 1));
 
   for (iPlane = 0; iPlane < nPlane; iPlane++) {
-    Plane_Normal[iPlane][0] = 0.0;    Plane_P0[iPlane][0] = 0.0;
-    Plane_Normal[iPlane][1] = 0.0;    Plane_P0[iPlane][1] = 0.0;
-    Plane_Normal[iPlane][2] = 0.0;    Plane_P0[iPlane][2] = 0.0;
+    Plane_Normal[iPlane][0] = 0.0;
+    Plane_P0[iPlane][0] = 0.0;
+    Plane_Normal[iPlane][1] = 0.0;
+    Plane_P0[iPlane][1] = 0.0;
+    Plane_Normal[iPlane][2] = 0.0;
+    Plane_P0[iPlane][2] = 0.0;
 
     Plane_Normal[iPlane][0] = 1.0;
-    Plane_P0[iPlane][0] = MinPlane + iPlane*dPlane;
-
+    Plane_P0[iPlane][0] = MinPlane + iPlane * dPlane;
   }
 
   /*--- Allocate some vectors for storing airfoil coordinates ---*/
 
-  Xcoord_Airfoil   = new vector<su2double>[nPlane];
-  Ycoord_Airfoil   = new vector<su2double>[nPlane];
-  Zcoord_Airfoil   = new vector<su2double>[nPlane];
+  Xcoord_Airfoil = new vector<su2double>[nPlane];
+  Ycoord_Airfoil = new vector<su2double>[nPlane];
+  Zcoord_Airfoil = new vector<su2double>[nPlane];
   Variable_Airfoil = new vector<su2double>[nPlane];
 
   /*--- Create the section slices through the geometry ---*/
 
   for (iPlane = 0; iPlane < nPlane; iPlane++) {
-
-    ComputeAirfoil_Section(Plane_P0[iPlane], Plane_Normal[iPlane],
-                           -1E6, 1E6, -1E6, 1E6, -1E6, 1E6, nullptr, Xcoord_Airfoil[iPlane],
-                           Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane],
+    ComputeAirfoil_Section(Plane_P0[iPlane], Plane_Normal[iPlane], -1E6, 1E6, -1E6, 1E6, -1E6, 1E6, nullptr,
+                           Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane],
                            Variable_Airfoil[iPlane], original_surface, config);
   }
 
   /*--- Compute the area at each section ---*/
 
   if (rank == MASTER_NODE) {
-
     /*--- Write an output file---*/
 
     if (config->GetTabular_FileFormat() == TAB_OUTPUT::TAB_CSV) {
       Fuselage_File.open("fuselage_description.csv", ios::out);
       if (config->GetSystemMeasurements() == US)
-        Fuselage_File << "\"x (in)\",\"Area (in^2)\",\"Length (in)\",\"Width (in)\",\"Waterline width (in)\",\"Height (in)\",\"Curvature (1/in)\",\"Generatrix Curve X (in)\",\"Generatrix Curve Y (in)\",\"Generatrix Curve Z (in)\",\"Axis Curve X (in)\",\"Axis Curve Y (in)\",\"Axis Curve Z (in)\"" << endl;
+        Fuselage_File
+            << "\"x (in)\",\"Area (in^2)\",\"Length (in)\",\"Width (in)\",\"Waterline width (in)\",\"Height "
+               "(in)\",\"Curvature (1/in)\",\"Generatrix Curve X (in)\",\"Generatrix Curve Y (in)\",\"Generatrix Curve "
+               "Z (in)\",\"Axis Curve X (in)\",\"Axis Curve Y (in)\",\"Axis Curve Z (in)\""
+            << endl;
       else
-        Fuselage_File << "\"x (m)\",\"Area (m^2)\",\"Length (m)\",\"Width (m)\",\"Waterline width (m)\",\"Height (m)\",\"Curvature (1/in)\",\"Generatrix Curve X (m)\",\"Generatrix Curve Y (m)\",\"Generatrix Curve Z (m)\",\"Axis Curve X (m)\",\"Axis Curve Y (m)\",\"Axis Curve Z (m)\"" << endl;
-    }
-    else {
+        Fuselage_File
+            << "\"x (m)\",\"Area (m^2)\",\"Length (m)\",\"Width (m)\",\"Waterline width (m)\",\"Height "
+               "(m)\",\"Curvature (1/in)\",\"Generatrix Curve X (m)\",\"Generatrix Curve Y (m)\",\"Generatrix Curve Z "
+               "(m)\",\"Axis Curve X (m)\",\"Axis Curve Y (m)\",\"Axis Curve Z (m)\""
+            << endl;
+    } else {
       Fuselage_File.open("fuselage_description.dat", ios::out);
       Fuselage_File << "TITLE = \"Fuselage description\"" << endl;
       if (config->GetSystemMeasurements() == US)
-        Fuselage_File << "VARIABLES = \"x (in)\",\"Area (in<sup>2</sup>)\",\"Length (in)\",\"Width (in)\",\"Waterline width (in)\",\"Height (in)\",\"Curvature (1/in)\",\"Generatrix Curve X (in)\",\"Generatrix Curve Y (in)\",\"Generatrix Curve Z (in)\",\"Axis Curve X (in)\",\"Axis Curve Y (in)\",\"Axis Curve Z (in)\"" << endl;
+        Fuselage_File
+            << "VARIABLES = \"x (in)\",\"Area (in<sup>2</sup>)\",\"Length (in)\",\"Width (in)\",\"Waterline width "
+               "(in)\",\"Height (in)\",\"Curvature (1/in)\",\"Generatrix Curve X (in)\",\"Generatrix Curve Y "
+               "(in)\",\"Generatrix Curve Z (in)\",\"Axis Curve X (in)\",\"Axis Curve Y (in)\",\"Axis Curve Z (in)\""
+            << endl;
       else
-        Fuselage_File << "VARIABLES = \"x (m)\",\"Area (m<sup>2</sup>)\",\"Length (m)\",\"Width (m)\",\"Waterline width (m)\",\"Height (m)\",\"Curvature (1/m)\",\"Generatrix Curve X (m)\",\"Generatrix Curve Y (m)\",\"Generatrix Curve Z (m)\",\"Axis Curve X (m)\",\"Axis Curve Y (m)\",\"Axis Curve Z (m)\"" << endl;
+        Fuselage_File
+            << "VARIABLES = \"x (m)\",\"Area (m<sup>2</sup>)\",\"Length (m)\",\"Width (m)\",\"Waterline width "
+               "(m)\",\"Height (m)\",\"Curvature (1/m)\",\"Generatrix Curve X (m)\",\"Generatrix Curve Y "
+               "(m)\",\"Generatrix Curve Z (m)\",\"Axis Curve X (m)\",\"Axis Curve Y (m)\",\"Axis Curve Z (m)\""
+            << endl;
       Fuselage_File << "ZONE T= \"Baseline fuselage\"" << endl;
     }
 
-
     /*--- Evaluate  geometrical quatities that do not require any kind of filter, local to each point ---*/
 
     for (iPlane = 0; iPlane < nPlane; iPlane++) {
-
       for (iDim = 0; iDim < nDim; iDim++) {
-        LeadingEdge[iPlane][iDim]  = 0.0;
+        LeadingEdge[iPlane][iDim] = 0.0;
         TrailingEdge[iPlane][iDim] = 0.0;
       }
 
-      Area[iPlane]   = 0.0;
-      Length[iPlane]   = 0.0;
-      Width[iPlane]  = 0.0;
-      WaterLineWidth[iPlane]  = 0.0;
+      Area[iPlane] = 0.0;
+      Length[iPlane] = 0.0;
+      Width[iPlane] = 0.0;
+      WaterLineWidth[iPlane] = 0.0;
       Height[iPlane] = 0.0;
 
       if (Xcoord_Airfoil[iPlane].size() > 1) {
+        Compute_Fuselage_LeadingTrailing(LeadingEdge[iPlane], TrailingEdge[iPlane], Plane_P0[iPlane],
+                                         Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane],
+                                         Zcoord_Airfoil[iPlane]);
 
-        Compute_Fuselage_LeadingTrailing(LeadingEdge[iPlane], TrailingEdge[iPlane], Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-
-        Area[iPlane] = Compute_Area(Plane_P0[iPlane], Plane_Normal[iPlane], config, Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+        Area[iPlane] = Compute_Area(Plane_P0[iPlane], Plane_Normal[iPlane], config, Xcoord_Airfoil[iPlane],
+                                    Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
 
-        Length[iPlane] = Compute_Length(Plane_P0[iPlane], Plane_Normal[iPlane], config, Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+        Length[iPlane] = Compute_Length(Plane_P0[iPlane], Plane_Normal[iPlane], config, Xcoord_Airfoil[iPlane],
+                                        Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
 
-        Width[iPlane] = Compute_Width(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+        Width[iPlane] = Compute_Width(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane],
+                                      Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
 
-        WaterLineWidth[iPlane] = Compute_WaterLineWidth(Plane_P0[iPlane], Plane_Normal[iPlane], config, Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-
-        Height[iPlane] = Compute_Height(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+        WaterLineWidth[iPlane] =
+            Compute_WaterLineWidth(Plane_P0[iPlane], Plane_Normal[iPlane], config, Xcoord_Airfoil[iPlane],
+                                   Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
 
+        Height[iPlane] = Compute_Height(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane],
+                                        Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
       }
-
     }
 
-    /*--- Evaluate  geometrical quatities that have been computed using a filtered value (they depend on more than one point) ---*/
+    /*--- Evaluate  geometrical quatities that have been computed using a filtered value (they depend on more than one
+     * point) ---*/
 
     for (iPlane = 0; iPlane < nPlane; iPlane++) {
-
       Curvature[iPlane] = 0.0;
 
       if (Xcoord_Airfoil[iPlane].size() > 1) {
-
-        if ((iPlane == 0) || (iPlane == nPlane-1)) Curvature[iPlane] = 0.0;
-        else Curvature[iPlane] = Compute_Curvature(LeadingEdge[iPlane-1], TrailingEdge[iPlane-1],
-                                                   LeadingEdge[iPlane], TrailingEdge[iPlane],
-                                                   LeadingEdge[iPlane+1], TrailingEdge[iPlane+1]);
-
+        if ((iPlane == 0) || (iPlane == nPlane - 1))
+          Curvature[iPlane] = 0.0;
+        else
+          Curvature[iPlane] =
+              Compute_Curvature(LeadingEdge[iPlane - 1], TrailingEdge[iPlane - 1], LeadingEdge[iPlane],
+                                TrailingEdge[iPlane], LeadingEdge[iPlane + 1], TrailingEdge[iPlane + 1]);
       }
-
     }
 
     /*--- Set the curvature and dihedral angles at the extremes ---*/
@@ -10343,8 +10048,8 @@ void CPhysicalGeometry::Compute_Fuselage(CConfig *config, bool original_surface,
       if ((Xcoord_Airfoil[0].size() != 0) && (Xcoord_Airfoil[1].size() != 0)) {
         Curvature[0] = Curvature[1];
       }
-      if ((Xcoord_Airfoil[nPlane-1].size() != 0) && (Xcoord_Airfoil[nPlane-2].size() != 0)) {
-        Curvature[nPlane-1] = Curvature[nPlane-2];
+      if ((Xcoord_Airfoil[nPlane - 1].size() != 0) && (Xcoord_Airfoil[nPlane - 2].size() != 0)) {
+        Curvature[nPlane - 1] = Curvature[nPlane - 2];
       }
     }
 
@@ -10353,14 +10058,17 @@ void CPhysicalGeometry::Compute_Fuselage(CConfig *config, bool original_surface,
     for (iPlane = 0; iPlane < nPlane; iPlane++) {
       if (Xcoord_Airfoil[iPlane].size() > 1) {
         if (config->GetTabular_FileFormat() == TAB_OUTPUT::TAB_CSV) {
-          Fuselage_File  << -Ycoord_Airfoil[iPlane][0] <<", "<< Area[iPlane] <<", "<< Length[iPlane] <<", "<< Width[iPlane] <<", "<< WaterLineWidth[iPlane] <<", "<< Height[iPlane] <<", "<< Curvature[iPlane]
-                     <<", "<< -LeadingEdge[iPlane][1] <<", "<< LeadingEdge[iPlane][0]  <<", "<< LeadingEdge[iPlane][2]
-                     <<", "<< -TrailingEdge[iPlane][1] <<", "<< TrailingEdge[iPlane][0]  <<", "<< TrailingEdge[iPlane][2]  << endl;
-        }
-        else  {
-          Fuselage_File  << -Ycoord_Airfoil[iPlane][0] <<" "<< Area[iPlane] <<" "<< Length[iPlane] <<" "<< Width[iPlane] <<" "<< WaterLineWidth[iPlane] <<" "<< Height[iPlane] <<" "<< Curvature[iPlane]
-                     <<" "<< -LeadingEdge[iPlane][1] <<" "<< LeadingEdge[iPlane][0]  <<" "<< LeadingEdge[iPlane][2]
-                     <<" "<< -TrailingEdge[iPlane][1] <<" "<< TrailingEdge[iPlane][0]  <<" "<< TrailingEdge[iPlane][2] << endl;
+          Fuselage_File << -Ycoord_Airfoil[iPlane][0] << ", " << Area[iPlane] << ", " << Length[iPlane] << ", "
+                        << Width[iPlane] << ", " << WaterLineWidth[iPlane] << ", " << Height[iPlane] << ", "
+                        << Curvature[iPlane] << ", " << -LeadingEdge[iPlane][1] << ", " << LeadingEdge[iPlane][0]
+                        << ", " << LeadingEdge[iPlane][2] << ", " << -TrailingEdge[iPlane][1] << ", "
+                        << TrailingEdge[iPlane][0] << ", " << TrailingEdge[iPlane][2] << endl;
+        } else {
+          Fuselage_File << -Ycoord_Airfoil[iPlane][0] << " " << Area[iPlane] << " " << Length[iPlane] << " "
+                        << Width[iPlane] << " " << WaterLineWidth[iPlane] << " " << Height[iPlane] << " "
+                        << Curvature[iPlane] << " " << -LeadingEdge[iPlane][1] << " " << LeadingEdge[iPlane][0] << " "
+                        << LeadingEdge[iPlane][2] << " " << -TrailingEdge[iPlane][1] << " " << TrailingEdge[iPlane][0]
+                        << " " << TrailingEdge[iPlane][2] << endl;
         }
       }
     }
@@ -10370,156 +10078,150 @@ void CPhysicalGeometry::Compute_Fuselage(CConfig *config, bool original_surface,
     Section_File.open("fuselage_slices.dat", ios::out);
 
     for (iPlane = 0; iPlane < nPlane; iPlane++) {
-
       if (iPlane == 0) {
         Section_File << "TITLE = \"Aircraft Slices\"" << endl;
         if (config->GetSystemMeasurements() == US)
           Section_File << "VARIABLES = \"x (in)\", \"y (in)\", \"z (in)\"" << endl;
-        else Section_File << "VARIABLES = \"x (m)\", \"y (m)\", \"z (m)\"" << endl;
+        else
+          Section_File << "VARIABLES = \"x (m)\", \"y (m)\", \"z (m)\"" << endl;
       }
 
       if (Xcoord_Airfoil[iPlane].size() > 1) {
-
-        Section_File << "ZONE T=\"X = " << -Ycoord_Airfoil[iPlane][0] << " \", I= " << Ycoord_Airfoil[iPlane].size() << ", F=POINT" << endl;
+        Section_File << "ZONE T=\"X = " << -Ycoord_Airfoil[iPlane][0] << " \", I= " << Ycoord_Airfoil[iPlane].size()
+                     << ", F=POINT" << endl;
 
         for (iVertex = 0; iVertex < Xcoord_Airfoil[iPlane].size(); iVertex++) {
-
           /*--- Write the file ---*/
 
-          Section_File  << -Ycoord_Airfoil[iPlane][iVertex] << " " << Xcoord_Airfoil[iPlane][iVertex] << " " << Zcoord_Airfoil[iPlane][iVertex] << endl;
+          Section_File << -Ycoord_Airfoil[iPlane][iVertex] << " " << Xcoord_Airfoil[iPlane][iVertex] << " "
+                       << Zcoord_Airfoil[iPlane][iVertex] << endl;
         }
       }
-
     }
 
     Section_File.close();
 
-
     /*--- Compute the fuselage volume using a composite Simpson's rule ---*/
 
     Fuselage_Volume = 0.0;
-    for (iPlane = 0; iPlane < nPlane-2; iPlane+=2) {
+    for (iPlane = 0; iPlane < nPlane - 2; iPlane += 2) {
       if (Xcoord_Airfoil[iPlane].size() > 1) {
-        Fuselage_Volume += (1.0/3.0)*dPlane*(Area[iPlane] + 4.0*Area[iPlane+1] + Area[iPlane+2]);
+        Fuselage_Volume += (1.0 / 3.0) * dPlane * (Area[iPlane] + 4.0 * Area[iPlane + 1] + Area[iPlane + 2]);
       }
     }
 
     /*--- Compute the fuselage wetted area ---*/
 
     Fuselage_WettedArea = 0.0;
-    if (Xcoord_Airfoil[0].size() > 1) Fuselage_WettedArea += (1.0/2.0)*dPlane*Length[0];
-    for (iPlane = 1; iPlane < nPlane-1; iPlane++) {
+    if (Xcoord_Airfoil[0].size() > 1) Fuselage_WettedArea += (1.0 / 2.0) * dPlane * Length[0];
+    for (iPlane = 1; iPlane < nPlane - 1; iPlane++) {
       if (Xcoord_Airfoil[iPlane].size() > 1) {
-        Fuselage_WettedArea += dPlane*Length[iPlane];
+        Fuselage_WettedArea += dPlane * Length[iPlane];
       }
     }
-    if (Xcoord_Airfoil[nPlane-1].size() > 1) Fuselage_WettedArea += (1.0/2.0)*dPlane*Length[nPlane-1];
+    if (Xcoord_Airfoil[nPlane - 1].size() > 1) Fuselage_WettedArea += (1.0 / 2.0) * dPlane * Length[nPlane - 1];
 
     /*--- Evaluate Max and Min quantities ---*/
 
-    Fuselage_MaxWidth = -1E6; Fuselage_MinWidth = 1E6;
-    Fuselage_MaxWaterLineWidth = -1E6; Fuselage_MinWaterLineWidth = 1E6;
-    Fuselage_MaxHeight = -1E6; Fuselage_MinHeight = 1E6;
+    Fuselage_MaxWidth = -1E6;
+    Fuselage_MinWidth = 1E6;
+    Fuselage_MaxWaterLineWidth = -1E6;
+    Fuselage_MinWaterLineWidth = 1E6;
+    Fuselage_MaxHeight = -1E6;
+    Fuselage_MinHeight = 1E6;
     Fuselage_MaxCurvature = -1E6;
 
     for (iPlane = 0; iPlane < nPlane; iPlane++) {
       if (Width[iPlane] != 0.0) Fuselage_MinWidth = min(Fuselage_MinWidth, Width[iPlane]);
       Fuselage_MaxWidth = max(Fuselage_MaxWidth, Width[iPlane]);
-      if (WaterLineWidth[iPlane] != 0.0) Fuselage_MinWaterLineWidth = min(Fuselage_MinWaterLineWidth, WaterLineWidth[iPlane]);
+      if (WaterLineWidth[iPlane] != 0.0)
+        Fuselage_MinWaterLineWidth = min(Fuselage_MinWaterLineWidth, WaterLineWidth[iPlane]);
       Fuselage_MaxWaterLineWidth = max(Fuselage_MaxWaterLineWidth, WaterLineWidth[iPlane]);
       if (Height[iPlane] != 0.0) Fuselage_MinHeight = min(Fuselage_MinHeight, Height[iPlane]);
       Fuselage_MaxHeight = max(Fuselage_MaxHeight, Height[iPlane]);
       Fuselage_MaxCurvature = max(Fuselage_MaxCurvature, Curvature[iPlane]);
     }
-
   }
 
   /*--- Free memory for the section cuts ---*/
 
-  delete [] Xcoord_Airfoil;
-  delete [] Ycoord_Airfoil;
-  delete [] Zcoord_Airfoil;
-  delete [] Variable_Airfoil;
-
-  for (iPlane = 0; iPlane < nPlane; iPlane++)
-    delete [] LeadingEdge[iPlane];
-  delete [] LeadingEdge;
+  delete[] Xcoord_Airfoil;
+  delete[] Ycoord_Airfoil;
+  delete[] Zcoord_Airfoil;
+  delete[] Variable_Airfoil;
 
-  for (iPlane = 0; iPlane < nPlane; iPlane++)
-    delete [] TrailingEdge[iPlane];
-  delete [] TrailingEdge;
+  for (iPlane = 0; iPlane < nPlane; iPlane++) delete[] LeadingEdge[iPlane];
+  delete[] LeadingEdge;
 
-  for (iPlane = 0; iPlane < nPlane; iPlane++)
-    delete [] Plane_P0[iPlane];
-  delete [] Plane_P0;
+  for (iPlane = 0; iPlane < nPlane; iPlane++) delete[] TrailingEdge[iPlane];
+  delete[] TrailingEdge;
 
-  for (iPlane = 0; iPlane < nPlane; iPlane++)
-    delete [] Plane_Normal[iPlane];
-  delete [] Plane_Normal;
+  for (iPlane = 0; iPlane < nPlane; iPlane++) delete[] Plane_P0[iPlane];
+  delete[] Plane_P0;
 
-  delete [] Area;
-  delete [] Length;
-  delete [] Width;
-  delete [] WaterLineWidth;
-  delete [] Height;
-  delete [] Curvature;
+  for (iPlane = 0; iPlane < nPlane; iPlane++) delete[] Plane_Normal[iPlane];
+  delete[] Plane_Normal;
 
+  delete[] Area;
+  delete[] Length;
+  delete[] Width;
+  delete[] WaterLineWidth;
+  delete[] Height;
+  delete[] Curvature;
 }
 
-void CPhysicalGeometry::Compute_Nacelle(CConfig *config, bool original_surface,
-                                        su2double &Nacelle_Volume, su2double &Nacelle_MinMaxThickness,
-                                        su2double &Nacelle_MinChord, su2double &Nacelle_MaxChord,
-                                        su2double &Nacelle_MaxMaxThickness, su2double &Nacelle_MinLERadius,
-                                        su2double &Nacelle_MaxLERadius, su2double &Nacelle_MinToC, su2double &Nacelle_MaxToC,
-                                        su2double &Nacelle_ObjFun_MinToC, su2double &Nacelle_MaxTwist) {
-
+void CPhysicalGeometry::Compute_Nacelle(CConfig* config, bool original_surface, su2double& Nacelle_Volume,
+                                        su2double& Nacelle_MinMaxThickness, su2double& Nacelle_MinChord,
+                                        su2double& Nacelle_MaxChord, su2double& Nacelle_MaxMaxThickness,
+                                        su2double& Nacelle_MinLERadius, su2double& Nacelle_MaxLERadius,
+                                        su2double& Nacelle_MinToC, su2double& Nacelle_MaxToC,
+                                        su2double& Nacelle_ObjFun_MinToC, su2double& Nacelle_MaxTwist) {
   unsigned short iPlane, iDim, nPlane = 0;
   unsigned long iVertex;
   su2double Angle, MinAngle, MaxAngle, dAngle, *Area, *MaxThickness, *ToC, *Chord, *LERadius, *Twist;
-  vector<su2double> *Xcoord_Airfoil, *Ycoord_Airfoil, *Zcoord_Airfoil, *Variable_Airfoil;
+  vector<su2double>*Xcoord_Airfoil, *Ycoord_Airfoil, *Zcoord_Airfoil, *Variable_Airfoil;
   ofstream Nacelle_File, Section_File;
 
-
   /*--- Make a large number of section cuts for approximating volume ---*/
 
   nPlane = config->GetnWingStations();
 
   /*--- Allocate memory for the section cutting ---*/
 
-  Area = new su2double [nPlane];
-  MaxThickness = new su2double [nPlane];
-  Chord = new su2double [nPlane];
-  LERadius = new su2double [nPlane];
-  ToC = new su2double [nPlane];
-  Twist = new su2double [nPlane];
+  Area = new su2double[nPlane];
+  MaxThickness = new su2double[nPlane];
+  Chord = new su2double[nPlane];
+  LERadius = new su2double[nPlane];
+  ToC = new su2double[nPlane];
+  Twist = new su2double[nPlane];
 
-  su2double **LeadingEdge = new su2double*[nPlane];
-  for (iPlane = 0; iPlane < nPlane; iPlane++ )
-    LeadingEdge[iPlane] = new su2double[nDim];
+  su2double** LeadingEdge = new su2double*[nPlane];
+  for (iPlane = 0; iPlane < nPlane; iPlane++) LeadingEdge[iPlane] = new su2double[nDim];
 
-  su2double **TrailingEdge = new su2double*[nPlane];
-  for (iPlane = 0; iPlane < nPlane; iPlane++ )
-    TrailingEdge[iPlane] = new su2double[nDim];
+  su2double** TrailingEdge = new su2double*[nPlane];
+  for (iPlane = 0; iPlane < nPlane; iPlane++) TrailingEdge[iPlane] = new su2double[nDim];
 
-  su2double **Plane_P0 = new su2double*[nPlane];
-  for (iPlane = 0; iPlane < nPlane; iPlane++ )
-    Plane_P0[iPlane] = new su2double[nDim];
+  su2double** Plane_P0 = new su2double*[nPlane];
+  for (iPlane = 0; iPlane < nPlane; iPlane++) Plane_P0[iPlane] = new su2double[nDim];
 
-  su2double **Plane_Normal = new su2double*[nPlane];
-  for (iPlane = 0; iPlane < nPlane; iPlane++ )
-    Plane_Normal[iPlane] = new su2double[nDim];
+  su2double** Plane_Normal = new su2double*[nPlane];
+  for (iPlane = 0; iPlane < nPlane; iPlane++) Plane_Normal[iPlane] = new su2double[nDim];
 
-  MinAngle = config->GetStations_Bounds(0); MaxAngle = config->GetStations_Bounds(1);
-  dAngle = fabs((MaxAngle - MinAngle)/su2double(nPlane-1));
+  MinAngle = config->GetStations_Bounds(0);
+  MaxAngle = config->GetStations_Bounds(1);
+  dAngle = fabs((MaxAngle - MinAngle) / su2double(nPlane - 1));
 
   for (iPlane = 0; iPlane < nPlane; iPlane++) {
-    Plane_Normal[iPlane][0] = 0.0;    Plane_P0[iPlane][0] = 0.0;
-    Plane_Normal[iPlane][1] = 0.0;    Plane_P0[iPlane][1] = 0.0;
-    Plane_Normal[iPlane][2] = 0.0;    Plane_P0[iPlane][2] = 0.0;
+    Plane_Normal[iPlane][0] = 0.0;
+    Plane_P0[iPlane][0] = 0.0;
+    Plane_Normal[iPlane][1] = 0.0;
+    Plane_P0[iPlane][1] = 0.0;
+    Plane_Normal[iPlane][2] = 0.0;
+    Plane_P0[iPlane][2] = 0.0;
 
     /*--- Apply roll to cut the nacelle ---*/
 
-    Angle = MinAngle + iPlane*dAngle*PI_NUMBER/180.0;
+    Angle = MinAngle + iPlane * dAngle * PI_NUMBER / 180.0;
 
     if (Angle <= 0) Angle = 1E-6;
     if (Angle >= 360) Angle = 359.999999;
@@ -10530,16 +10232,18 @@ void CPhysicalGeometry::Compute_Nacelle(CConfig *config, bool original_surface,
 
     /*--- Apply tilt angle to the plane ---*/
 
-    su2double Tilt_Angle = config->GetNacelleLocation(3)*PI_NUMBER/180;
-    su2double Plane_NormalX_Tilt = Plane_Normal[iPlane][0]*cos(Tilt_Angle) + Plane_Normal[iPlane][2]*sin(Tilt_Angle);
+    su2double Tilt_Angle = config->GetNacelleLocation(3) * PI_NUMBER / 180;
+    su2double Plane_NormalX_Tilt =
+        Plane_Normal[iPlane][0] * cos(Tilt_Angle) + Plane_Normal[iPlane][2] * sin(Tilt_Angle);
     su2double Plane_NormalY_Tilt = Plane_Normal[iPlane][1];
-    su2double Plane_NormalZ_Tilt = Plane_Normal[iPlane][2]*cos(Tilt_Angle) - Plane_Normal[iPlane][0]*sin(Tilt_Angle);
+    su2double Plane_NormalZ_Tilt =
+        Plane_Normal[iPlane][2] * cos(Tilt_Angle) - Plane_Normal[iPlane][0] * sin(Tilt_Angle);
 
     /*--- Apply toe angle to the plane ---*/
 
-    su2double Toe_Angle = config->GetNacelleLocation(4)*PI_NUMBER/180;
-    su2double Plane_NormalX_Tilt_Toe = Plane_NormalX_Tilt*cos(Toe_Angle) - Plane_NormalY_Tilt*sin(Toe_Angle);
-    su2double Plane_NormalY_Tilt_Toe = Plane_NormalX_Tilt*sin(Toe_Angle) + Plane_NormalY_Tilt*cos(Toe_Angle);
+    su2double Toe_Angle = config->GetNacelleLocation(4) * PI_NUMBER / 180;
+    su2double Plane_NormalX_Tilt_Toe = Plane_NormalX_Tilt * cos(Toe_Angle) - Plane_NormalY_Tilt * sin(Toe_Angle);
+    su2double Plane_NormalY_Tilt_Toe = Plane_NormalX_Tilt * sin(Toe_Angle) + Plane_NormalY_Tilt * cos(Toe_Angle);
     su2double Plane_NormalZ_Tilt_Toe = Plane_NormalZ_Tilt;
 
     /*--- Update normal vector ---*/
@@ -10553,108 +10257,116 @@ void CPhysicalGeometry::Compute_Nacelle(CConfig *config, bool original_surface,
     Plane_P0[iPlane][0] = config->GetNacelleLocation(0);
     Plane_P0[iPlane][1] = config->GetNacelleLocation(1);
     Plane_P0[iPlane][2] = config->GetNacelleLocation(2);
-
   }
 
   /*--- Allocate some vectors for storing airfoil coordinates ---*/
 
-  Xcoord_Airfoil   = new vector<su2double>[nPlane];
-  Ycoord_Airfoil   = new vector<su2double>[nPlane];
-  Zcoord_Airfoil   = new vector<su2double>[nPlane];
+  Xcoord_Airfoil = new vector<su2double>[nPlane];
+  Ycoord_Airfoil = new vector<su2double>[nPlane];
+  Zcoord_Airfoil = new vector<su2double>[nPlane];
   Variable_Airfoil = new vector<su2double>[nPlane];
 
   /*--- Create the section slices through the geometry ---*/
 
   for (iPlane = 0; iPlane < nPlane; iPlane++) {
-
-    ComputeAirfoil_Section(Plane_P0[iPlane], Plane_Normal[iPlane],
-                           -1E6, 1E6, -1E6, 1E6, -1E6, 1E6, nullptr, Xcoord_Airfoil[iPlane],
-                           Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane],
+    ComputeAirfoil_Section(Plane_P0[iPlane], Plane_Normal[iPlane], -1E6, 1E6, -1E6, 1E6, -1E6, 1E6, nullptr,
+                           Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane],
                            Variable_Airfoil[iPlane], original_surface, config);
-
   }
 
   /*--- Compute airfoil characteristic only in the master node ---*/
 
   if (rank == MASTER_NODE) {
-
     /*--- Write an output file---*/
 
     if (config->GetTabular_FileFormat() == TAB_OUTPUT::TAB_CSV) {
       Nacelle_File.open("nacelle_description.csv", ios::out);
       if (config->GetSystemMeasurements() == US)
-        Nacelle_File << "\"Theta (deg)\",\"Area (in^2)\",\"Max. Thickness (in)\",\"Chord (in)\",\"Leading Edge Radius (1/in)\",\"Max. Thickness/Chord\",\"Twist (deg)\",\"Leading Edge XLoc\",\"Leading Edge ZLoc\",\"Trailing Edge XLoc\",\"Trailing Edge ZLoc\"" << endl;
+        Nacelle_File << "\"Theta (deg)\",\"Area (in^2)\",\"Max. Thickness (in)\",\"Chord (in)\",\"Leading Edge Radius "
+                        "(1/in)\",\"Max. Thickness/Chord\",\"Twist (deg)\",\"Leading Edge XLoc\",\"Leading Edge "
+                        "ZLoc\",\"Trailing Edge XLoc\",\"Trailing Edge ZLoc\""
+                     << endl;
       else
-        Nacelle_File << "\"Theta (deg)\",\"Area (m^2)\",\"Max. Thickness (m)\",\"Chord (m)\",\"Leading Edge Radius (1/m)\",\"Max. Thickness/Chord\",\"Twist (deg)\",\"Curvature (1/in)\",\"Dihedral (deg)\",\"Leading Edge XLoc\",\"Leading Edge ZLoc\",\"Trailing Edge XLoc\",\"Trailing Edge ZLoc\"" << endl;
-    }
-    else {
+        Nacelle_File
+            << "\"Theta (deg)\",\"Area (m^2)\",\"Max. Thickness (m)\",\"Chord (m)\",\"Leading Edge Radius "
+               "(1/m)\",\"Max. Thickness/Chord\",\"Twist (deg)\",\"Curvature (1/in)\",\"Dihedral (deg)\",\"Leading "
+               "Edge XLoc\",\"Leading Edge ZLoc\",\"Trailing Edge XLoc\",\"Trailing Edge ZLoc\""
+            << endl;
+    } else {
       Nacelle_File.open("nacelle_description.dat", ios::out);
       Nacelle_File << "TITLE = \"Nacelle description\"" << endl;
       if (config->GetSystemMeasurements() == US)
-        Nacelle_File << "VARIABLES = \"<greek>q</greek> (deg)\",\"Area (in<sup>2</sup>)\",\"Max. Thickness (in)\",\"Chord (in)\",\"Leading Edge Radius (1/in)\",\"Max. Thickness/Chord\",\"Twist (deg)\",\"Leading Edge XLoc\",\"Leading Edge ZLoc\",\"Trailing Edge XLoc\",\"Trailing Edge ZLoc\"" << endl;
+        Nacelle_File
+            << "VARIABLES = \"<greek>q</greek> (deg)\",\"Area (in<sup>2</sup>)\",\"Max. Thickness (in)\",\"Chord "
+               "(in)\",\"Leading Edge Radius (1/in)\",\"Max. Thickness/Chord\",\"Twist (deg)\",\"Leading Edge "
+               "XLoc\",\"Leading Edge ZLoc\",\"Trailing Edge XLoc\",\"Trailing Edge ZLoc\""
+            << endl;
       else
-        Nacelle_File << "VARIABLES = \"<greek>q</greek> (deg)\",\"Area (m<sup>2</sup>)\",\"Max. Thickness (m)\",\"Chord (m)\",\"Leading Edge Radius (1/m)\",\"Max. Thickness/Chord\",\"Twist (deg)\",\"Leading Edge XLoc\",\"Leading Edge ZLoc\",\"Trailing Edge XLoc\",\"Trailing Edge ZLoc\"" << endl;
+        Nacelle_File
+            << "VARIABLES = \"<greek>q</greek> (deg)\",\"Area (m<sup>2</sup>)\",\"Max. Thickness (m)\",\"Chord "
+               "(m)\",\"Leading Edge Radius (1/m)\",\"Max. Thickness/Chord\",\"Twist (deg)\",\"Leading Edge "
+               "XLoc\",\"Leading Edge ZLoc\",\"Trailing Edge XLoc\",\"Trailing Edge ZLoc\""
+            << endl;
       Nacelle_File << "ZONE T= \"Baseline nacelle\"" << endl;
     }
 
-
     /*--- Evaluate  geometrical quatities that do not require any kind of filter, local to each point ---*/
 
     for (iPlane = 0; iPlane < nPlane; iPlane++) {
-
       for (iDim = 0; iDim < nDim; iDim++) {
-        LeadingEdge[iPlane][iDim]  = 0.0;
+        LeadingEdge[iPlane][iDim] = 0.0;
         TrailingEdge[iPlane][iDim] = 0.0;
       }
 
-      Area[iPlane]                = 0.0;
-      MaxThickness[iPlane]        = 0.0;
-      Chord[iPlane]               = 0.0;
-      LERadius[iPlane]            = 0.0;
-      ToC[iPlane]                 = 0.0;
-      Twist[iPlane]               = 0.0;
+      Area[iPlane] = 0.0;
+      MaxThickness[iPlane] = 0.0;
+      Chord[iPlane] = 0.0;
+      LERadius[iPlane] = 0.0;
+      ToC[iPlane] = 0.0;
+      Twist[iPlane] = 0.0;
 
       if (Xcoord_Airfoil[iPlane].size() > 1) {
+        Compute_Wing_LeadingTrailing(LeadingEdge[iPlane], TrailingEdge[iPlane], Plane_P0[iPlane], Plane_Normal[iPlane],
+                                     Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
 
-        Compute_Wing_LeadingTrailing(LeadingEdge[iPlane], TrailingEdge[iPlane], Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+        Area[iPlane] = Compute_Area(Plane_P0[iPlane], Plane_Normal[iPlane], config, Xcoord_Airfoil[iPlane],
+                                    Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
 
-        Area[iPlane] = Compute_Area(Plane_P0[iPlane], Plane_Normal[iPlane], config, Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+        MaxThickness[iPlane] =
+            Compute_MaxThickness(Plane_P0[iPlane], Plane_Normal[iPlane], config, Xcoord_Airfoil[iPlane],
+                                 Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
 
-        MaxThickness[iPlane] = Compute_MaxThickness(Plane_P0[iPlane], Plane_Normal[iPlane], config, Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+        Chord[iPlane] = Compute_Chord(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane],
+                                      Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
 
-        Chord[iPlane] = Compute_Chord(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+        Twist[iPlane] = Compute_Twist(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane],
+                                      Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
 
-        Twist[iPlane] = Compute_Twist(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-
-        LERadius[iPlane] = Compute_LERadius(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+        LERadius[iPlane] = Compute_LERadius(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane],
+                                            Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
 
         ToC[iPlane] = MaxThickness[iPlane] / Chord[iPlane];
-
-
       }
-
     }
 
     /*--- Plot the geometrical quatities ---*/
 
     for (iPlane = 0; iPlane < nPlane; iPlane++) {
-
-      su2double theta_deg = atan2(Plane_Normal[iPlane][1], -Plane_Normal[iPlane][2])/PI_NUMBER*180 + 180;
+      su2double theta_deg = atan2(Plane_Normal[iPlane][1], -Plane_Normal[iPlane][2]) / PI_NUMBER * 180 + 180;
 
       if (Xcoord_Airfoil[iPlane].size() > 1) {
         if (config->GetTabular_FileFormat() == TAB_OUTPUT::TAB_CSV) {
-          Nacelle_File  << theta_deg <<", "<< Area[iPlane] <<", "<< MaxThickness[iPlane] <<", "<< Chord[iPlane] <<", "<< LERadius[iPlane] <<", "<< ToC[iPlane]
-          <<", "<< Twist[iPlane] <<", "<< LeadingEdge[iPlane][0] <<", "<< LeadingEdge[iPlane][2]
-          <<", "<< TrailingEdge[iPlane][0] <<", "<< TrailingEdge[iPlane][2] << endl;
-        }
-        else  {
-          Nacelle_File  << theta_deg <<" "<< Area[iPlane] <<" "<< MaxThickness[iPlane] <<" "<< Chord[iPlane] <<" "<< LERadius[iPlane] <<" "<< ToC[iPlane]
-          <<" "<< Twist[iPlane] <<" "<< LeadingEdge[iPlane][0] <<" "<< LeadingEdge[iPlane][2]
-          <<" "<< TrailingEdge[iPlane][0] <<" "<< TrailingEdge[iPlane][2] << endl;
-
+          Nacelle_File << theta_deg << ", " << Area[iPlane] << ", " << MaxThickness[iPlane] << ", " << Chord[iPlane]
+                       << ", " << LERadius[iPlane] << ", " << ToC[iPlane] << ", " << Twist[iPlane] << ", "
+                       << LeadingEdge[iPlane][0] << ", " << LeadingEdge[iPlane][2] << ", " << TrailingEdge[iPlane][0]
+                       << ", " << TrailingEdge[iPlane][2] << endl;
+        } else {
+          Nacelle_File << theta_deg << " " << Area[iPlane] << " " << MaxThickness[iPlane] << " " << Chord[iPlane] << " "
+                       << LERadius[iPlane] << " " << ToC[iPlane] << " " << Twist[iPlane] << " "
+                       << LeadingEdge[iPlane][0] << " " << LeadingEdge[iPlane][2] << " " << TrailingEdge[iPlane][0]
+                       << " " << TrailingEdge[iPlane][2] << endl;
         }
       }
-
     }
 
     Nacelle_File.close();
@@ -10662,23 +10374,24 @@ void CPhysicalGeometry::Compute_Nacelle(CConfig *config, bool original_surface,
     Section_File.open("nacelle_slices.dat", ios::out);
 
     for (iPlane = 0; iPlane < nPlane; iPlane++) {
-
       if (iPlane == 0) {
         Section_File << "TITLE = \"Nacelle Slices\"" << endl;
         if (config->GetSystemMeasurements() == US)
-          Section_File << "VARIABLES = \"x (in)\", \"y (in)\", \"z (in)\", \"x<sub>2D</sub>/c\", \"y<sub>2D</sub>/c\"" << endl;
-        else Section_File << "VARIABLES = \"x (m)\", \"y (m)\", \"z (m)\", \"x<sub>2D</sub>/c\", \"y<sub>2D</sub>/c\"" << endl;
+          Section_File << "VARIABLES = \"x (in)\", \"y (in)\", \"z (in)\", \"x<sub>2D</sub>/c\", \"y<sub>2D</sub>/c\""
+                       << endl;
+        else
+          Section_File << "VARIABLES = \"x (m)\", \"y (m)\", \"z (m)\", \"x<sub>2D</sub>/c\", \"y<sub>2D</sub>/c\""
+                       << endl;
       }
 
       if (Xcoord_Airfoil[iPlane].size() > 1) {
+        su2double theta_deg = atan2(Plane_Normal[iPlane][1], -Plane_Normal[iPlane][2]) / PI_NUMBER * 180 + 180;
+        su2double Angle = theta_deg * PI_NUMBER / 180 - 0.5 * PI_NUMBER;
 
-        su2double theta_deg = atan2(Plane_Normal[iPlane][1], -Plane_Normal[iPlane][2])/PI_NUMBER*180 + 180;
-        su2double Angle = theta_deg*PI_NUMBER/180 - 0.5*PI_NUMBER;
-
-        Section_File << "ZONE T=\"<greek>q</greek> = " << theta_deg << " deg\", I= " << Xcoord_Airfoil[iPlane].size() << ", F=POINT" << endl;
+        Section_File << "ZONE T=\"<greek>q</greek> = " << theta_deg << " deg\", I= " << Xcoord_Airfoil[iPlane].size()
+                     << ", F=POINT" << endl;
 
         for (iVertex = 0; iVertex < Xcoord_Airfoil[iPlane].size(); iVertex++) {
-
           /*--- Move to the origin  ---*/
 
           su2double XValue_ = Xcoord_Airfoil[iPlane][iVertex] - LeadingEdge[iPlane][0];
@@ -10686,40 +10399,48 @@ void CPhysicalGeometry::Compute_Nacelle(CConfig *config, bool original_surface,
 
           /*--- Rotate the airfoil and divide by the chord ---*/
 
-          su2double ValCos = cos(Twist[iPlane]*PI_NUMBER/180.0);
-          su2double ValSin = sin(Twist[iPlane]*PI_NUMBER/180.0);
+          su2double ValCos = cos(Twist[iPlane] * PI_NUMBER / 180.0);
+          su2double ValSin = sin(Twist[iPlane] * PI_NUMBER / 180.0);
 
-          su2double XValue = (XValue_*ValCos - ZValue_*ValSin) / Chord[iPlane];
-          su2double ZValue = (ZValue_*ValCos + XValue_*ValSin) / Chord[iPlane];
+          su2double XValue = (XValue_ * ValCos - ZValue_ * ValSin) / Chord[iPlane];
+          su2double ZValue = (ZValue_ * ValCos + XValue_ * ValSin) / Chord[iPlane];
 
           su2double XCoord = Xcoord_Airfoil[iPlane][iVertex] + config->GetNacelleLocation(0);
-          su2double YCoord = (Ycoord_Airfoil[iPlane][iVertex]*cos(Angle) - Zcoord_Airfoil[iPlane][iVertex]*sin(Angle)) + config->GetNacelleLocation(1);
-          su2double ZCoord = (Zcoord_Airfoil[iPlane][iVertex]*cos(Angle) + Ycoord_Airfoil[iPlane][iVertex]*sin(Angle)) + config->GetNacelleLocation(2);
+          su2double YCoord =
+              (Ycoord_Airfoil[iPlane][iVertex] * cos(Angle) - Zcoord_Airfoil[iPlane][iVertex] * sin(Angle)) +
+              config->GetNacelleLocation(1);
+          su2double ZCoord =
+              (Zcoord_Airfoil[iPlane][iVertex] * cos(Angle) + Ycoord_Airfoil[iPlane][iVertex] * sin(Angle)) +
+              config->GetNacelleLocation(2);
 
           /*--- Write the file ---*/
 
-          Section_File  << XCoord << " " << YCoord << " " << ZCoord << " " << XValue  << " " << ZValue << endl;
+          Section_File << XCoord << " " << YCoord << " " << ZCoord << " " << XValue << " " << ZValue << endl;
         }
       }
-
     }
 
     Section_File.close();
 
-
     /*--- Compute the wing volume using a composite Simpson's rule ---*/
 
     Nacelle_Volume = 0.0;
-    for (iPlane = 0; iPlane < nPlane-2; iPlane+=2) {
+    for (iPlane = 0; iPlane < nPlane - 2; iPlane += 2) {
       if (Xcoord_Airfoil[iPlane].size() > 1) {
-        Nacelle_Volume += (1.0/3.0)*dAngle*(Area[iPlane] + 4.0*Area[iPlane+1] + Area[iPlane+2]);
+        Nacelle_Volume += (1.0 / 3.0) * dAngle * (Area[iPlane] + 4.0 * Area[iPlane + 1] + Area[iPlane + 2]);
       }
     }
 
     /*--- Evaluate Max and Min quantities ---*/
 
-    Nacelle_MaxMaxThickness = -1E6; Nacelle_MinMaxThickness = 1E6; Nacelle_MinChord = 1E6; Nacelle_MaxChord = -1E6;
-    Nacelle_MinLERadius = 1E6; Nacelle_MaxLERadius = -1E6; Nacelle_MinToC = 1E6; Nacelle_MaxToC = -1E6;
+    Nacelle_MaxMaxThickness = -1E6;
+    Nacelle_MinMaxThickness = 1E6;
+    Nacelle_MinChord = 1E6;
+    Nacelle_MaxChord = -1E6;
+    Nacelle_MinLERadius = 1E6;
+    Nacelle_MaxLERadius = -1E6;
+    Nacelle_MinToC = 1E6;
+    Nacelle_MaxToC = -1E6;
     Nacelle_MaxTwist = -1E6;
 
     for (iPlane = 0; iPlane < nPlane; iPlane++) {
@@ -10731,46 +10452,39 @@ void CPhysicalGeometry::Compute_Nacelle(CConfig *config, bool original_surface,
       Nacelle_MaxLERadius = max(Nacelle_MaxLERadius, LERadius[iPlane]);
       if (ToC[iPlane] != 0.0) Nacelle_MinToC = min(Nacelle_MinToC, ToC[iPlane]);
       Nacelle_MaxToC = max(Nacelle_MaxToC, ToC[iPlane]);
-      Nacelle_ObjFun_MinToC = sqrt((Nacelle_MinToC - 0.07)*(Nacelle_MinToC - 0.07));
+      Nacelle_ObjFun_MinToC = sqrt((Nacelle_MinToC - 0.07) * (Nacelle_MinToC - 0.07));
       Nacelle_MaxTwist = max(Nacelle_MaxTwist, fabs(Twist[iPlane]));
     }
-
   }
 
   /*--- Free memory for the section cuts ---*/
 
-  delete [] Xcoord_Airfoil;
-  delete [] Ycoord_Airfoil;
-  delete [] Zcoord_Airfoil;
-  delete [] Variable_Airfoil;
+  delete[] Xcoord_Airfoil;
+  delete[] Ycoord_Airfoil;
+  delete[] Zcoord_Airfoil;
+  delete[] Variable_Airfoil;
 
-  for (iPlane = 0; iPlane < nPlane; iPlane++)
-    delete [] LeadingEdge[iPlane];
-  delete [] LeadingEdge;
+  for (iPlane = 0; iPlane < nPlane; iPlane++) delete[] LeadingEdge[iPlane];
+  delete[] LeadingEdge;
 
-  for (iPlane = 0; iPlane < nPlane; iPlane++)
-    delete [] TrailingEdge[iPlane];
-  delete [] TrailingEdge;
+  for (iPlane = 0; iPlane < nPlane; iPlane++) delete[] TrailingEdge[iPlane];
+  delete[] TrailingEdge;
 
-  for (iPlane = 0; iPlane < nPlane; iPlane++)
-    delete [] Plane_P0[iPlane];
-  delete [] Plane_P0;
+  for (iPlane = 0; iPlane < nPlane; iPlane++) delete[] Plane_P0[iPlane];
+  delete[] Plane_P0;
 
-  for (iPlane = 0; iPlane < nPlane; iPlane++)
-    delete [] Plane_Normal[iPlane];
-  delete [] Plane_Normal;
-
-  delete [] Area;
-  delete [] MaxThickness;
-  delete [] Chord;
-  delete [] LERadius;
-  delete [] ToC;
-  delete [] Twist;
+  for (iPlane = 0; iPlane < nPlane; iPlane++) delete[] Plane_Normal[iPlane];
+  delete[] Plane_Normal;
 
+  delete[] Area;
+  delete[] MaxThickness;
+  delete[] Chord;
+  delete[] LERadius;
+  delete[] ToC;
+  delete[] Twist;
 }
 
-std::unique_ptr<CADTElemClass> CPhysicalGeometry::ComputeViscousWallADT(const CConfig *config) const{
-
+std::unique_ptr<CADTElemClass> CPhysicalGeometry::ComputeViscousWallADT(const CConfig* config) const {
   /*--------------------------------------------------------------------------*/
   /*--- Step 1: Create the coordinates and connectivity of the linear      ---*/
   /*---         subelements of the local boundaries that must be taken     ---*/
@@ -10792,15 +10506,11 @@ std::unique_ptr<CADTElemClass> CPhysicalGeometry::ComputeViscousWallADT(const CC
 
   /* Loop over the boundary markers. */
 
-  for(unsigned short iMarker=0; iMarker<config->GetnMarker_All(); ++iMarker) {
-
-
+  for (unsigned short iMarker = 0; iMarker < config->GetnMarker_All(); ++iMarker) {
     /* Check for a viscous wall. */
-    if( config->GetViscous_Wall(iMarker)) {
-
+    if (config->GetViscous_Wall(iMarker)) {
       /* Loop over the surface elements of this marker. */
-      for(unsigned long iElem=0; iElem < nElem_Bound[iMarker]; iElem++) {
-
+      for (unsigned long iElem = 0; iElem < nElem_Bound[iMarker]; iElem++) {
         /* Set the flag of the mesh points on this surface to true. */
         for (unsigned short iNode = 0; iNode < bound[iMarker][iElem]->GetnNodes(); iNode++) {
           unsigned long iPoint = bound[iMarker][iElem]->GetNode(iNode);
@@ -10809,10 +10519,10 @@ std::unique_ptr<CADTElemClass> CPhysicalGeometry::ComputeViscousWallADT(const CC
         /* Determine the necessary data from the corresponding standard face,
           such as the number of linear subfaces, the number of DOFs per
           linear subface and the corresponding local connectivity. */
-        const unsigned short VTK_Type      = bound[iMarker][iElem]->GetVTK_Type();
-        const unsigned short nDOFsPerElem  = bound[iMarker][iElem]->GetnNodes();
+        const unsigned short VTK_Type = bound[iMarker][iElem]->GetVTK_Type();
+        const unsigned short nDOFsPerElem = bound[iMarker][iElem]->GetnNodes();
 
-          /* Loop over the nodes of element and store the required data. */
+        /* Loop over the nodes of element and store the required data. */
 
         markerIDs.push_back(iMarker);
         VTK_TypeElem.push_back(VTK_Type);
@@ -10829,19 +10539,17 @@ std::unique_ptr<CADTElemClass> CPhysicalGeometry::ComputeViscousWallADT(const CC
   vector<su2double> surfaceCoor;
   unsigned long nVertex_SolidWall = 0;
 
-  for(unsigned long i=0; i<nPoint; ++i) {
-    if( meshToSurface[i] ) {
+  for (unsigned long i = 0; i < nPoint; ++i) {
+    if (meshToSurface[i]) {
       meshToSurface[i] = nVertex_SolidWall++;
 
-      for(unsigned short k=0; k<nDim; ++k)
-        surfaceCoor.push_back(nodes->GetCoord(i, k));
+      for (unsigned short k = 0; k < nDim; ++k) surfaceCoor.push_back(nodes->GetCoord(i, k));
     }
   }
 
   /*--- Change the surface connectivity, such that it corresponds to
         the entries in surfaceCoor rather than in meshPoints. ---*/
-  for(unsigned long i=0; i<surfaceConn.size(); ++i)
-    surfaceConn[i] = meshToSurface[surfaceConn[i]];
+  for (unsigned long i = 0; i < surfaceConn.size(); ++i) surfaceConn[i] = meshToSurface[surfaceConn[i]];
 
   /*--------------------------------------------------------------------------*/
   /*--- Step 2: Build the ADT, which is an ADT of bounding boxes of the    ---*/
@@ -10850,15 +10558,13 @@ std::unique_ptr<CADTElemClass> CPhysicalGeometry::ComputeViscousWallADT(const CC
   /*---         points of the elements close to a wall boundary.           ---*/
   /*--------------------------------------------------------------------------*/
 
-  std::unique_ptr<CADTElemClass> WallADT(new CADTElemClass(nDim, surfaceCoor, surfaceConn, VTK_TypeElem,
-                                                           markerIDs, elemIDs, true));
+  std::unique_ptr<CADTElemClass> WallADT(
+      new CADTElemClass(nDim, surfaceCoor, surfaceConn, VTK_TypeElem, markerIDs, elemIDs, true));
 
   return WallADT;
-
 }
 
 void CPhysicalGeometry::SetWallDistance(CADTElemClass* WallADT, const CConfig* config, unsigned short iZone) {
-
   /*--------------------------------------------------------------------------*/
   /*--- Step 3: Loop over all interior mesh nodes and compute minimum      ---*/
   /*---        distance to a solid wall element                           ---*/
@@ -10869,16 +10575,16 @@ void CPhysicalGeometry::SetWallDistance(CADTElemClass* WallADT, const CConfig* c
     /*--- Solid wall boundary nodes are present. Compute the wall
      distance for all nodes. ---*/
 
-    SU2_OMP_FOR_DYN(roundUpDiv(nPoint,2*omp_get_max_threads()))
-    for (unsigned long iPoint=0; iPoint<GetnPoint(); ++iPoint) {
+    SU2_OMP_FOR_DYN(roundUpDiv(nPoint, 2 * omp_get_max_threads()))
+    for (unsigned long iPoint = 0; iPoint < GetnPoint(); ++iPoint) {
       unsigned short markerID;
-      unsigned long  elemID;
-      int            rankID;
-      su2double      dist;
+      unsigned long elemID;
+      int rankID;
+      su2double dist;
 
       WallADT->DetermineNearestElement(nodes->GetCoord(iPoint), dist, markerID, elemID, rankID);
 
-      if(dist < nodes->GetWall_Distance(iPoint)){
+      if (dist < nodes->GetWall_Distance(iPoint)) {
         nodes->SetWall_Distance(iPoint, dist, rankID, iZone, markerID, elemID);
       }
     }
diff --git a/Common/src/geometry/dual_grid/CDualGrid.cpp b/Common/src/geometry/dual_grid/CDualGrid.cpp
index a3969b4088e..2a277094bc6 100644
--- a/Common/src/geometry/dual_grid/CDualGrid.cpp
+++ b/Common/src/geometry/dual_grid/CDualGrid.cpp
@@ -29,6 +29,6 @@
 
 unsigned short CDualGrid::nDim = 0;
 
-CDualGrid::CDualGrid(unsigned short val_nDim) { nDim = val_nDim;}
+CDualGrid::CDualGrid(unsigned short val_nDim) { nDim = val_nDim; }
 
 CDualGrid::~CDualGrid() {}
diff --git a/Common/src/geometry/dual_grid/CEdge.cpp b/Common/src/geometry/dual_grid/CEdge.cpp
index a5f30f90473..d3a45abeee1 100644
--- a/Common/src/geometry/dual_grid/CEdge.cpp
+++ b/Common/src/geometry/dual_grid/CEdge.cpp
@@ -32,39 +32,31 @@
 using namespace GeometryToolbox;
 
 CEdge::CEdge(unsigned long nEdge_, unsigned long nDim)
-  : nEdge(nEdge_),
-    nEdgeSIMD(nextMultiple(nEdge_, simd::preferredLen<su2double>())) {
+    : nEdge(nEdge_), nEdgeSIMD(nextMultiple(nEdge_, simd::preferredLen<su2double>())) {
   /*--- Allocate with padding. ---*/
-  Nodes.resize(nEdgeSIMD,2) = 0;
-  Normal.resize(nEdgeSIMD,nDim) = su2double(0.0);
+  Nodes.resize(nEdgeSIMD, 2) = 0;
+  Normal.resize(nEdgeSIMD, nDim) = su2double(0.0);
 }
 
-void CEdge::SetZeroValues(void) {
-  Normal = su2double(0.0);
-}
-
-su2double CEdge::GetVolume(const su2double *coord_Edge_CG,
-                           const su2double *coord_FaceElem_CG,
-                           const su2double *coord_Elem_CG,
-                           const su2double *coord_Point) {
+void CEdge::SetZeroValues(void) { Normal = su2double(0.0); }
 
+su2double CEdge::GetVolume(const su2double* coord_Edge_CG, const su2double* coord_FaceElem_CG,
+                           const su2double* coord_Elem_CG, const su2double* coord_Point) {
   constexpr unsigned long nDim = 3;
 
   su2double vec_a[nDim] = {0.0}, vec_b[nDim] = {0.0}, vec_c[nDim] = {0.0}, vec_d[nDim] = {0.0};
 
-  Distance(nDim, coord_Edge_CG,     coord_Point, vec_a);
+  Distance(nDim, coord_Edge_CG, coord_Point, vec_a);
   Distance(nDim, coord_FaceElem_CG, coord_Point, vec_b);
-  Distance(nDim, coord_Elem_CG,     coord_Point, vec_c);
+  Distance(nDim, coord_Elem_CG, coord_Point, vec_c);
 
   CrossProduct(vec_a, vec_b, vec_d);
 
   return fabs(DotProduct(nDim, vec_c, vec_d)) / 6.0;
 }
 
-su2double CEdge::GetVolume(const su2double *coord_Edge_CG,
-                           const su2double *coord_Elem_CG,
-                           const su2double *coord_Point) {
-
+su2double CEdge::GetVolume(const su2double* coord_Edge_CG, const su2double* coord_Elem_CG,
+                           const su2double* coord_Point) {
   constexpr unsigned long nDim = 2;
 
   su2double vec_a[nDim] = {0.0}, vec_b[nDim] = {0.0};
@@ -72,14 +64,11 @@ su2double CEdge::GetVolume(const su2double *coord_Edge_CG,
   Distance(nDim, coord_Elem_CG, coord_Point, vec_a);
   Distance(nDim, coord_Edge_CG, coord_Point, vec_b);
 
-  return 0.5 * fabs(vec_a[0]*vec_b[1] - vec_a[1]*vec_b[0]);
+  return 0.5 * fabs(vec_a[0] * vec_b[1] - vec_a[1] * vec_b[0]);
 }
 
-void CEdge::SetNodes_Coord(unsigned long iEdge,
-                           const su2double *coord_Edge_CG,
-                           const su2double *coord_FaceElem_CG,
-                           const su2double *coord_Elem_CG) {
-
+void CEdge::SetNodes_Coord(unsigned long iEdge, const su2double* coord_Edge_CG, const su2double* coord_FaceElem_CG,
+                           const su2double* coord_Elem_CG) {
   constexpr unsigned long nDim = 3;
 
   su2double vec_a[nDim] = {0.0}, vec_b[nDim] = {0.0}, Dim_Normal[nDim];
@@ -89,14 +78,10 @@ void CEdge::SetNodes_Coord(unsigned long iEdge,
 
   CrossProduct(vec_a, vec_b, Dim_Normal);
 
-  for (auto iDim = 0ul; iDim < nDim; ++iDim)
-    Normal(iEdge,iDim) += 0.5 * Dim_Normal[iDim];
+  for (auto iDim = 0ul; iDim < nDim; ++iDim) Normal(iEdge, iDim) += 0.5 * Dim_Normal[iDim];
 }
 
-void CEdge::SetNodes_Coord(unsigned long iEdge,
-                           const su2double *coord_Edge_CG,
-                           const su2double *coord_Elem_CG) {
-
-  Normal(iEdge,0) += coord_Elem_CG[1] - coord_Edge_CG[1];
-  Normal(iEdge,1) -= coord_Elem_CG[0] - coord_Edge_CG[0];
+void CEdge::SetNodes_Coord(unsigned long iEdge, const su2double* coord_Edge_CG, const su2double* coord_Elem_CG) {
+  Normal(iEdge, 0) += coord_Elem_CG[1] - coord_Edge_CG[1];
+  Normal(iEdge, 1) -= coord_Elem_CG[0] - coord_Edge_CG[0];
 }
diff --git a/Common/src/geometry/dual_grid/CPoint.cpp b/Common/src/geometry/dual_grid/CPoint.cpp
index 8f3eaefff01..190bf7ad69a 100644
--- a/Common/src/geometry/dual_grid/CPoint.cpp
+++ b/Common/src/geometry/dual_grid/CPoint.cpp
@@ -29,13 +29,9 @@
 #include "../../../include/CConfig.hpp"
 #include "../../../include/parallelization/omp_structure.hpp"
 
-CPoint::CPoint(unsigned long npoint, unsigned long ndim) : nDim(ndim) {
-
-  MinimalAllocation(npoint);
-}
+CPoint::CPoint(unsigned long npoint, unsigned long ndim) : nDim(ndim) { MinimalAllocation(npoint); }
 
 void CPoint::MinimalAllocation(unsigned long npoint) {
-
   /*--- Global index a parallel simulation. ---*/
   GlobalIndex.resize(npoint) = 0;
 
@@ -43,19 +39,16 @@ void CPoint::MinimalAllocation(unsigned long npoint) {
   Color.resize(npoint) = 0;
 
   /*--- Coordinates. ---*/
-  Coord.resize(npoint,nDim) = su2double(0.0);
-
+  Coord.resize(npoint, nDim) = su2double(0.0);
 }
 
-CPoint::CPoint(unsigned long npoint, unsigned long ndim, unsigned short imesh, const CConfig *config) : nDim(ndim) {
-
+CPoint::CPoint(unsigned long npoint, unsigned long ndim, unsigned short imesh, const CConfig* config) : nDim(ndim) {
   MinimalAllocation(npoint);
 
   FullAllocation(imesh, config);
 }
 
-void CPoint::FullAllocation(unsigned short imesh, const CConfig *config) {
-
+void CPoint::FullAllocation(unsigned short imesh, const CConfig* config) {
   const auto npoint = GlobalIndex.size();
 
   /*--- Volumes ---*/
@@ -74,8 +67,8 @@ void CPoint::FullAllocation(unsigned short imesh, const CConfig *config) {
   }
 
   if (config->GetDiscrete_Adjoint()) {
-    AD_InputIndex.resize(npoint,nDim) = 0;
-    AD_OutputIndex.resize(npoint,nDim) = 0;
+    AD_InputIndex.resize(npoint, nDim) = 0;
+    AD_OutputIndex.resize(npoint, nDim) = 0;
   }
 
   /*--- Multigrid structures. ---*/
@@ -103,27 +96,26 @@ void CPoint::FullAllocation(unsigned short imesh, const CConfig *config) {
 
   /*--- For smoothing the numerical grid coordinates ---*/
   if (config->GetSmoothNumGrid()) {
-    Coord_Old.resize(npoint,nDim) = su2double(0.0);
-    Coord_Sum.resize(npoint,nDim) = su2double(0.0);
+    Coord_Old.resize(npoint, nDim) = su2double(0.0);
+    Coord_Sum.resize(npoint, nDim) = su2double(0.0);
   }
 
   /*--- Storage of grid velocities for dynamic meshes. ---*/
 
   if (config->GetDynamic_Grid()) {
-    GridVel.resize(npoint,nDim) = su2double(0.0);
+    GridVel.resize(npoint, nDim) = su2double(0.0);
 
     /*--- Grid velocity gradients are needed for the continuous adjoint. ---*/
-    if (config->GetContinuous_Adjoint())
-      GridVel_Grad.resize(npoint,nDim,nDim,0.0);
+    if (config->GetContinuous_Adjoint()) GridVel_Grad.resize(npoint, nDim, nDim, 0.0);
 
     /*--- Structures for storing old node coordinates for computing grid
      *    velocities via finite differencing with dynamically deforming meshes. ---*/
     /*--- In the case of CMeshSolver, these coordinates are stored as solutions to the mesh problem. ---*/
     if (config->GetGrid_Movement() && (config->GetTime_Marching() != TIME_MARCHING::STEADY)) {
-      Coord_n.resize(npoint,nDim) = su2double(0.0);
-      Coord_p1.resize(npoint,nDim) = su2double(0.0);
-      Coord_n1.resize(npoint,nDim) = su2double(0.0);
-      if (Coord_Old.empty()) Coord_Old.resize(npoint,nDim) = su2double(0.0);
+      Coord_n.resize(npoint, nDim) = su2double(0.0);
+      Coord_p1.resize(npoint, nDim) = su2double(0.0);
+      Coord_n1.resize(npoint, nDim) = su2double(0.0);
+      if (Coord_Old.empty()) Coord_Old.resize(npoint, nDim) = su2double(0.0);
     }
   }
 
@@ -140,18 +132,13 @@ void CPoint::FullAllocation(unsigned short imesh, const CConfig *config) {
 
   RoughnessHeight.resize(npoint) = su2double(0.0);
   SharpEdge_Distance.resize(npoint) = su2double(0.0);
-
 }
 
-void CPoint::SetElems(const vector<vector<long> >& elemsMatrix) {
-
-  Elem = CCompressedSparsePatternL(elemsMatrix);
-}
+void CPoint::SetElems(const vector<vector<long> >& elemsMatrix) { Elem = CCompressedSparsePatternL(elemsMatrix); }
 
 void CPoint::SetPoints(const vector<vector<unsigned long> >& pointsMatrix) {
-
   Point = CCompressedSparsePatternUL(pointsMatrix);
-  Edge = CCompressedSparsePatternL(Point.outerPtr(), Point.outerPtr()+Point.getOuterSize()+1, long(-1));
+  Edge = CCompressedSparsePatternL(Point.outerPtr(), Point.outerPtr() + Point.getOuterSize() + 1, long(-1));
 }
 
 void CPoint::SetVolume_n() {
@@ -205,4 +192,3 @@ void CPoint::SetCoord_Old() {
 }
 
 void CPoint::SetCoord_SumZero() { parallelSet(Coord_Sum.size(), 0.0, Coord_Sum.data()); }
-
diff --git a/Common/src/geometry/dual_grid/CTurboVertex.cpp b/Common/src/geometry/dual_grid/CTurboVertex.cpp
index 592bbc1cb6c..4c19dd2bf21 100644
--- a/Common/src/geometry/dual_grid/CTurboVertex.cpp
+++ b/Common/src/geometry/dual_grid/CTurboVertex.cpp
@@ -27,20 +27,15 @@
 
 #include "../../../include/geometry/dual_grid/CTurboVertex.hpp"
 
-CTurboVertex::CTurboVertex(unsigned long val_point, unsigned short val_nDim) : CVertex(val_point, val_nDim){
+CTurboVertex::CTurboVertex(unsigned long val_point, unsigned short val_nDim) : CVertex(val_point, val_nDim) {
   unsigned short iDim;
- /*--- Pointers initialization ---*/
+  /*--- Pointers initialization ---*/
   TurboNormal = nullptr;
   /*--- Allocate node, and face normal ---*/
-  TurboNormal = new su2double [nDim];
+  TurboNormal = new su2double[nDim];
 
   /*--- Initializate the structure ---*/
-  for (iDim = 0; iDim < nDim; iDim ++) TurboNormal[iDim] = 0.0;
-
+  for (iDim = 0; iDim < nDim; iDim++) TurboNormal[iDim] = 0.0;
 }
 
-CTurboVertex::~CTurboVertex() {
-
-  delete [] TurboNormal;
-
-}
+CTurboVertex::~CTurboVertex() { delete[] TurboNormal; }
diff --git a/Common/src/geometry/dual_grid/CVertex.cpp b/Common/src/geometry/dual_grid/CVertex.cpp
index 4b3e9d657d8..844245759ab 100644
--- a/Common/src/geometry/dual_grid/CVertex.cpp
+++ b/Common/src/geometry/dual_grid/CVertex.cpp
@@ -30,15 +30,10 @@
 
 using namespace GeometryToolbox;
 
-CVertex::CVertex(unsigned long val_point, unsigned short val_nDim) :
-  CDualGrid(val_nDim) {
-  Nodes[0] = val_point;
-}
-
-void CVertex::SetNodes_Coord(const su2double *coord_Edge_CG,
-                             const su2double *coord_FaceElem_CG,
-                             const su2double *coord_Elem_CG) {
+CVertex::CVertex(unsigned long val_point, unsigned short val_nDim) : CDualGrid(val_nDim) { Nodes[0] = val_point; }
 
+void CVertex::SetNodes_Coord(const su2double* coord_Edge_CG, const su2double* coord_FaceElem_CG,
+                             const su2double* coord_Elem_CG) {
   constexpr unsigned long nDim = 3;
   su2double vec_a[nDim] = {0.0}, vec_b[nDim] = {0.0}, Dim_Normal[nDim];
 
@@ -47,13 +42,10 @@ void CVertex::SetNodes_Coord(const su2double *coord_Edge_CG,
 
   CrossProduct(vec_a, vec_b, Dim_Normal);
 
-  for (auto iDim = 0ul; iDim < nDim; ++iDim)
-    Normal[iDim] += 0.5 * Dim_Normal[iDim];
+  for (auto iDim = 0ul; iDim < nDim; ++iDim) Normal[iDim] += 0.5 * Dim_Normal[iDim];
 }
 
-void CVertex::SetNodes_Coord(const su2double *val_coord_Edge_CG,
-                             const su2double *val_coord_Elem_CG) {
-
-  Normal[0] += val_coord_Elem_CG[1]-val_coord_Edge_CG[1];
-  Normal[1] -= val_coord_Elem_CG[0]-val_coord_Edge_CG[0];
+void CVertex::SetNodes_Coord(const su2double* val_coord_Edge_CG, const su2double* val_coord_Elem_CG) {
+  Normal[0] += val_coord_Elem_CG[1] - val_coord_Edge_CG[1];
+  Normal[1] -= val_coord_Elem_CG[0] - val_coord_Edge_CG[0];
 }
diff --git a/Common/src/geometry/elements/CElement.cpp b/Common/src/geometry/elements/CElement.cpp
index 2e35eeecf98..91c41d7ff9a 100644
--- a/Common/src/geometry/elements/CElement.cpp
+++ b/Common/src/geometry/elements/CElement.cpp
@@ -27,9 +27,7 @@
 
 #include "../../../include/geometry/elements/CElement.hpp"
 
-
 CElement::CElement(unsigned short ngauss, unsigned short nnodes, unsigned short ndim) {
-
   nGaussPoints = ngauss;
   nNodes = nnodes;
   nDim = ndim;
@@ -42,8 +40,7 @@ CElement::CElement(unsigned short ngauss, unsigned short nnodes, unsigned short
   RefCoord.resize(nNodes, MAXNDIM) = su2double(0.0);
 
   GaussPoint.reserve(nGaussPoints);
-  for(unsigned short iGauss = 0; iGauss < nGaussPoints; ++iGauss)
-    GaussPoint.emplace_back(iGauss, nDim, nNodes);
+  for (unsigned short iGauss = 0; iGauss < nGaussPoints; ++iGauss) GaussPoint.emplace_back(iGauss, nDim, nNodes);
 
   GaussWeight.resize(nGaussPoints) = su2double(0.0);
   NodalExtrap.resize(nNodes, nGaussPoints) = su2double(0.0);
@@ -53,33 +50,30 @@ CElement::CElement(unsigned short ngauss, unsigned short nnodes, unsigned short
   Mab.resize(nNodes, nNodes);
   Ks_ab.resize(nNodes, nNodes);
   Kab.resize(nNodes);
-  for(auto& kab_i : Kab) kab_i.resize(nNodes, nDim*nDim);
+  for (auto& kab_i : Kab) kab_i.resize(nNodes, nDim * nDim);
 
   Kt_a.resize(nNodes, nDim);
   FDL_a.resize(nNodes, nDim);
 
-  HiHj.resize(nNodes,nNodes);
+  HiHj.resize(nNodes, nNodes);
   DHiDHj.resize(nNodes);
-  for(auto& DHiDHj_a : DHiDHj) {
+  for (auto& DHiDHj_a : DHiDHj) {
     DHiDHj_a.resize(nNodes);
-    for(auto& DHiDHj_ab : DHiDHj_a) DHiDHj_ab.resize(nDim,nDim);
+    for (auto& DHiDHj_ab : DHiDHj_a) DHiDHj_ab.resize(nDim, nDim);
   }
 
   ClearElement();
 }
 
 void CElement::ClearElement(void) {
-
   Mab.setConstant(0.0);
   Kt_a.setConstant(0.0);
   FDL_a.setConstant(0.0);
   Ks_ab.setConstant(0.0);
 
   HiHj.setConstant(0.0);
-  for(auto& DHiDHj_a : DHiDHj) {
-    for(auto& DHiDHj_ab : DHiDHj_a) DHiDHj_ab.setConstant(0.0);
+  for (auto& DHiDHj_a : DHiDHj) {
+    for (auto& DHiDHj_ab : DHiDHj_a) DHiDHj_ab.setConstant(0.0);
   }
-  for(auto& kab_i : Kab)
-    kab_i.setConstant(0.0);
+  for (auto& kab_i : Kab) kab_i.setConstant(0.0);
 }
-
diff --git a/Common/src/geometry/elements/CHEXA8.cpp b/Common/src/geometry/elements/CHEXA8.cpp
index 79d033c0e59..fee133c71fe 100644
--- a/Common/src/geometry/elements/CHEXA8.cpp
+++ b/Common/src/geometry/elements/CHEXA8.cpp
@@ -27,21 +27,43 @@
 
 #include "../../../include/geometry/elements/CElement.hpp"
 
-
-CHEXA8::CHEXA8() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
-
+CHEXA8::CHEXA8() : CElementWithKnownSizes<NGAUSS, NNODE, NDIM>() {
   /*--- Gauss coordinates and weights ---*/
 
   su2double oneOnSqrt3 = 0.577350269189626;
 
-  GaussCoord[0][0] = -oneOnSqrt3;  GaussCoord[0][1] = -oneOnSqrt3;  GaussCoord[0][2] = -oneOnSqrt3;  GaussWeight(0) = 1.0;
-  GaussCoord[1][0] =  oneOnSqrt3;  GaussCoord[1][1] = -oneOnSqrt3;  GaussCoord[1][2] = -oneOnSqrt3;  GaussWeight(1) = 1.0;
-  GaussCoord[2][0] =  oneOnSqrt3;  GaussCoord[2][1] =  oneOnSqrt3;  GaussCoord[2][2] = -oneOnSqrt3;  GaussWeight(2) = 1.0;
-  GaussCoord[3][0] = -oneOnSqrt3;  GaussCoord[3][1] =  oneOnSqrt3;  GaussCoord[3][2] = -oneOnSqrt3;  GaussWeight(3) = 1.0;
-  GaussCoord[4][0] = -oneOnSqrt3;  GaussCoord[4][1] = -oneOnSqrt3;  GaussCoord[4][2] =  oneOnSqrt3;  GaussWeight(4) = 1.0;
-  GaussCoord[5][0] =  oneOnSqrt3;  GaussCoord[5][1] = -oneOnSqrt3;  GaussCoord[5][2] =  oneOnSqrt3;  GaussWeight(5) = 1.0;
-  GaussCoord[6][0] =  oneOnSqrt3;  GaussCoord[6][1] =  oneOnSqrt3;  GaussCoord[6][2] =  oneOnSqrt3;  GaussWeight(6) = 1.0;
-  GaussCoord[7][0] = -oneOnSqrt3;  GaussCoord[7][1] =  oneOnSqrt3;  GaussCoord[7][2] =  oneOnSqrt3;  GaussWeight(7) = 1.0;
+  GaussCoord[0][0] = -oneOnSqrt3;
+  GaussCoord[0][1] = -oneOnSqrt3;
+  GaussCoord[0][2] = -oneOnSqrt3;
+  GaussWeight(0) = 1.0;
+  GaussCoord[1][0] = oneOnSqrt3;
+  GaussCoord[1][1] = -oneOnSqrt3;
+  GaussCoord[1][2] = -oneOnSqrt3;
+  GaussWeight(1) = 1.0;
+  GaussCoord[2][0] = oneOnSqrt3;
+  GaussCoord[2][1] = oneOnSqrt3;
+  GaussCoord[2][2] = -oneOnSqrt3;
+  GaussWeight(2) = 1.0;
+  GaussCoord[3][0] = -oneOnSqrt3;
+  GaussCoord[3][1] = oneOnSqrt3;
+  GaussCoord[3][2] = -oneOnSqrt3;
+  GaussWeight(3) = 1.0;
+  GaussCoord[4][0] = -oneOnSqrt3;
+  GaussCoord[4][1] = -oneOnSqrt3;
+  GaussCoord[4][2] = oneOnSqrt3;
+  GaussWeight(4) = 1.0;
+  GaussCoord[5][0] = oneOnSqrt3;
+  GaussCoord[5][1] = -oneOnSqrt3;
+  GaussCoord[5][2] = oneOnSqrt3;
+  GaussWeight(5) = 1.0;
+  GaussCoord[6][0] = oneOnSqrt3;
+  GaussCoord[6][1] = oneOnSqrt3;
+  GaussCoord[6][2] = oneOnSqrt3;
+  GaussWeight(6) = 1.0;
+  GaussCoord[7][0] = -oneOnSqrt3;
+  GaussCoord[7][1] = oneOnSqrt3;
+  GaussCoord[7][2] = oneOnSqrt3;
+  GaussWeight(7) = 1.0;
 
   /*--- Store the values of the shape functions and their derivatives ---*/
 
@@ -49,96 +71,115 @@ CHEXA8::CHEXA8() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
   su2double Xi, Eta, Zeta, val_Ni;
 
   for (iGauss = 0; iGauss < NGAUSS; iGauss++) {
-
     Xi = GaussCoord[iGauss][0];
     Eta = GaussCoord[iGauss][1];
     Zeta = GaussCoord[iGauss][2];
 
-    val_Ni = 0.125*(1.0-Xi)*(1.0-Eta)*(1.0-Zeta);   GaussPoint[iGauss].SetNi(val_Ni,0);
-    val_Ni = 0.125*(1.0+Xi)*(1.0-Eta)*(1.0-Zeta);   GaussPoint[iGauss].SetNi(val_Ni,1);
-    val_Ni = 0.125*(1.0+Xi)*(1.0+Eta)*(1.0-Zeta);   GaussPoint[iGauss].SetNi(val_Ni,2);
-    val_Ni = 0.125*(1.0-Xi)*(1.0+Eta)*(1.0-Zeta);   GaussPoint[iGauss].SetNi(val_Ni,3);
-    val_Ni = 0.125*(1.0-Xi)*(1.0-Eta)*(1.0+Zeta);   GaussPoint[iGauss].SetNi(val_Ni,4);
-    val_Ni = 0.125*(1.0+Xi)*(1.0-Eta)*(1.0+Zeta);   GaussPoint[iGauss].SetNi(val_Ni,5);
-    val_Ni = 0.125*(1.0+Xi)*(1.0+Eta)*(1.0+Zeta);   GaussPoint[iGauss].SetNi(val_Ni,6);
-    val_Ni = 0.125*(1.0-Xi)*(1.0+Eta)*(1.0+Zeta);   GaussPoint[iGauss].SetNi(val_Ni,7);
+    val_Ni = 0.125 * (1.0 - Xi) * (1.0 - Eta) * (1.0 - Zeta);
+    GaussPoint[iGauss].SetNi(val_Ni, 0);
+    val_Ni = 0.125 * (1.0 + Xi) * (1.0 - Eta) * (1.0 - Zeta);
+    GaussPoint[iGauss].SetNi(val_Ni, 1);
+    val_Ni = 0.125 * (1.0 + Xi) * (1.0 + Eta) * (1.0 - Zeta);
+    GaussPoint[iGauss].SetNi(val_Ni, 2);
+    val_Ni = 0.125 * (1.0 - Xi) * (1.0 + Eta) * (1.0 - Zeta);
+    GaussPoint[iGauss].SetNi(val_Ni, 3);
+    val_Ni = 0.125 * (1.0 - Xi) * (1.0 - Eta) * (1.0 + Zeta);
+    GaussPoint[iGauss].SetNi(val_Ni, 4);
+    val_Ni = 0.125 * (1.0 + Xi) * (1.0 - Eta) * (1.0 + Zeta);
+    GaussPoint[iGauss].SetNi(val_Ni, 5);
+    val_Ni = 0.125 * (1.0 + Xi) * (1.0 + Eta) * (1.0 + Zeta);
+    GaussPoint[iGauss].SetNi(val_Ni, 6);
+    val_Ni = 0.125 * (1.0 - Xi) * (1.0 + Eta) * (1.0 + Zeta);
+    GaussPoint[iGauss].SetNi(val_Ni, 7);
 
     /*--- dN/d xi ---*/
 
-    dNiXj[iGauss][0][0] = -0.125*(1.0-Eta)*(1.0-Zeta);
-    dNiXj[iGauss][1][0] =  0.125*(1.0-Eta)*(1.0-Zeta);
-    dNiXj[iGauss][2][0] =  0.125*(1.0+Eta)*(1.0-Zeta);
-    dNiXj[iGauss][3][0] = -0.125*(1.0+Eta)*(1.0-Zeta);
-    dNiXj[iGauss][4][0] = -0.125*(1.0-Eta)*(1.0+Zeta);
-    dNiXj[iGauss][5][0] =  0.125*(1.0-Eta)*(1.0+Zeta);
-    dNiXj[iGauss][6][0] =  0.125*(1.0+Eta)*(1.0+Zeta);
-    dNiXj[iGauss][7][0] = -0.125*(1.0+Eta)*(1.0+Zeta);
+    dNiXj[iGauss][0][0] = -0.125 * (1.0 - Eta) * (1.0 - Zeta);
+    dNiXj[iGauss][1][0] = 0.125 * (1.0 - Eta) * (1.0 - Zeta);
+    dNiXj[iGauss][2][0] = 0.125 * (1.0 + Eta) * (1.0 - Zeta);
+    dNiXj[iGauss][3][0] = -0.125 * (1.0 + Eta) * (1.0 - Zeta);
+    dNiXj[iGauss][4][0] = -0.125 * (1.0 - Eta) * (1.0 + Zeta);
+    dNiXj[iGauss][5][0] = 0.125 * (1.0 - Eta) * (1.0 + Zeta);
+    dNiXj[iGauss][6][0] = 0.125 * (1.0 + Eta) * (1.0 + Zeta);
+    dNiXj[iGauss][7][0] = -0.125 * (1.0 + Eta) * (1.0 + Zeta);
 
     /*--- dN/d eta ---*/
 
-    dNiXj[iGauss][0][1] = -0.125*(1.0-Xi)*(1.0-Zeta);
-    dNiXj[iGauss][1][1] = -0.125*(1.0+Xi)*(1.0-Zeta);
-    dNiXj[iGauss][2][1] =  0.125*(1.0+Xi)*(1.0-Zeta);
-    dNiXj[iGauss][3][1] =  0.125*(1.0-Xi)*(1.0-Zeta);
-    dNiXj[iGauss][4][1] = -0.125*(1.0-Xi)*(1.0+Zeta);
-    dNiXj[iGauss][5][1] = -0.125*(1.0+Xi)*(1.0+Zeta);
-    dNiXj[iGauss][6][1] =  0.125*(1.0+Xi)*(1.0+Zeta);
-    dNiXj[iGauss][7][1] =  0.125*(1.0-Xi)*(1.0+Zeta);
+    dNiXj[iGauss][0][1] = -0.125 * (1.0 - Xi) * (1.0 - Zeta);
+    dNiXj[iGauss][1][1] = -0.125 * (1.0 + Xi) * (1.0 - Zeta);
+    dNiXj[iGauss][2][1] = 0.125 * (1.0 + Xi) * (1.0 - Zeta);
+    dNiXj[iGauss][3][1] = 0.125 * (1.0 - Xi) * (1.0 - Zeta);
+    dNiXj[iGauss][4][1] = -0.125 * (1.0 - Xi) * (1.0 + Zeta);
+    dNiXj[iGauss][5][1] = -0.125 * (1.0 + Xi) * (1.0 + Zeta);
+    dNiXj[iGauss][6][1] = 0.125 * (1.0 + Xi) * (1.0 + Zeta);
+    dNiXj[iGauss][7][1] = 0.125 * (1.0 - Xi) * (1.0 + Zeta);
 
     /*--- dN/d zeta ---*/
 
-    dNiXj[iGauss][0][2] = -0.125*(1.0-Xi)*(1.0-Eta);
-    dNiXj[iGauss][1][2] = -0.125*(1.0+Xi)*(1.0-Eta);
-    dNiXj[iGauss][2][2] = -0.125*(1.0+Xi)*(1.0+Eta);
-    dNiXj[iGauss][3][2] = -0.125*(1.0-Xi)*(1.0+Eta);
-    dNiXj[iGauss][4][2] =  0.125*(1.0-Xi)*(1.0-Eta);
-    dNiXj[iGauss][5][2] =  0.125*(1.0+Xi)*(1.0-Eta);
-    dNiXj[iGauss][6][2] =  0.125*(1.0+Xi)*(1.0+Eta);
-    dNiXj[iGauss][7][2] =  0.125*(1.0-Xi)*(1.0+Eta);
-
+    dNiXj[iGauss][0][2] = -0.125 * (1.0 - Xi) * (1.0 - Eta);
+    dNiXj[iGauss][1][2] = -0.125 * (1.0 + Xi) * (1.0 - Eta);
+    dNiXj[iGauss][2][2] = -0.125 * (1.0 + Xi) * (1.0 + Eta);
+    dNiXj[iGauss][3][2] = -0.125 * (1.0 - Xi) * (1.0 + Eta);
+    dNiXj[iGauss][4][2] = 0.125 * (1.0 - Xi) * (1.0 - Eta);
+    dNiXj[iGauss][5][2] = 0.125 * (1.0 + Xi) * (1.0 - Eta);
+    dNiXj[iGauss][6][2] = 0.125 * (1.0 + Xi) * (1.0 + Eta);
+    dNiXj[iGauss][7][2] = 0.125 * (1.0 - Xi) * (1.0 + Eta);
   }
 
   /*--- Store the extrapolation functions ---*/
 
   su2double ExtrapCoord[8][3], sqrt3 = 1.732050807568877;
 
-  ExtrapCoord[0][0] = -sqrt3;  ExtrapCoord[0][1] = -sqrt3;  ExtrapCoord[0][2] = -sqrt3;
-  ExtrapCoord[1][0] =  sqrt3;  ExtrapCoord[1][1] = -sqrt3;  ExtrapCoord[1][2] = -sqrt3;
-  ExtrapCoord[2][0] =  sqrt3;  ExtrapCoord[2][1] =  sqrt3;  ExtrapCoord[2][2] = -sqrt3;
-  ExtrapCoord[3][0] = -sqrt3;  ExtrapCoord[3][1] =  sqrt3;  ExtrapCoord[3][2] = -sqrt3;
-  ExtrapCoord[4][0] = -sqrt3;  ExtrapCoord[4][1] = -sqrt3;  ExtrapCoord[4][2] =  sqrt3;
-  ExtrapCoord[5][0] =  sqrt3;  ExtrapCoord[5][1] = -sqrt3;  ExtrapCoord[5][2] =  sqrt3;
-  ExtrapCoord[6][0] =  sqrt3;  ExtrapCoord[6][1] =  sqrt3;  ExtrapCoord[6][2] =  sqrt3;
-  ExtrapCoord[7][0] = -sqrt3;  ExtrapCoord[7][1] =  sqrt3;  ExtrapCoord[7][2] =  sqrt3;
+  ExtrapCoord[0][0] = -sqrt3;
+  ExtrapCoord[0][1] = -sqrt3;
+  ExtrapCoord[0][2] = -sqrt3;
+  ExtrapCoord[1][0] = sqrt3;
+  ExtrapCoord[1][1] = -sqrt3;
+  ExtrapCoord[1][2] = -sqrt3;
+  ExtrapCoord[2][0] = sqrt3;
+  ExtrapCoord[2][1] = sqrt3;
+  ExtrapCoord[2][2] = -sqrt3;
+  ExtrapCoord[3][0] = -sqrt3;
+  ExtrapCoord[3][1] = sqrt3;
+  ExtrapCoord[3][2] = -sqrt3;
+  ExtrapCoord[4][0] = -sqrt3;
+  ExtrapCoord[4][1] = -sqrt3;
+  ExtrapCoord[4][2] = sqrt3;
+  ExtrapCoord[5][0] = sqrt3;
+  ExtrapCoord[5][1] = -sqrt3;
+  ExtrapCoord[5][2] = sqrt3;
+  ExtrapCoord[6][0] = sqrt3;
+  ExtrapCoord[6][1] = sqrt3;
+  ExtrapCoord[6][2] = sqrt3;
+  ExtrapCoord[7][0] = -sqrt3;
+  ExtrapCoord[7][1] = sqrt3;
+  ExtrapCoord[7][2] = sqrt3;
 
   for (iNode = 0; iNode < NNODE; iNode++) {
-
     Xi = ExtrapCoord[iNode][0];
     Eta = ExtrapCoord[iNode][1];
     Zeta = ExtrapCoord[iNode][2];
 
-    NodalExtrap[iNode][0] = 0.125*(1.0-Xi)*(1.0-Eta)*(1.0-Zeta);
-    NodalExtrap[iNode][1] = 0.125*(1.0+Xi)*(1.0-Eta)*(1.0-Zeta);
-    NodalExtrap[iNode][2] = 0.125*(1.0+Xi)*(1.0+Eta)*(1.0-Zeta);
-    NodalExtrap[iNode][3] = 0.125*(1.0-Xi)*(1.0+Eta)*(1.0-Zeta);
-    NodalExtrap[iNode][4] = 0.125*(1.0-Xi)*(1.0-Eta)*(1.0+Zeta);
-    NodalExtrap[iNode][5] = 0.125*(1.0+Xi)*(1.0-Eta)*(1.0+Zeta);
-    NodalExtrap[iNode][6] = 0.125*(1.0+Xi)*(1.0+Eta)*(1.0+Zeta);
-    NodalExtrap[iNode][7] = 0.125*(1.0-Xi)*(1.0+Eta)*(1.0+Zeta);
-
+    NodalExtrap[iNode][0] = 0.125 * (1.0 - Xi) * (1.0 - Eta) * (1.0 - Zeta);
+    NodalExtrap[iNode][1] = 0.125 * (1.0 + Xi) * (1.0 - Eta) * (1.0 - Zeta);
+    NodalExtrap[iNode][2] = 0.125 * (1.0 + Xi) * (1.0 + Eta) * (1.0 - Zeta);
+    NodalExtrap[iNode][3] = 0.125 * (1.0 - Xi) * (1.0 + Eta) * (1.0 - Zeta);
+    NodalExtrap[iNode][4] = 0.125 * (1.0 - Xi) * (1.0 - Eta) * (1.0 + Zeta);
+    NodalExtrap[iNode][5] = 0.125 * (1.0 + Xi) * (1.0 - Eta) * (1.0 + Zeta);
+    NodalExtrap[iNode][6] = 0.125 * (1.0 + Xi) * (1.0 + Eta) * (1.0 + Zeta);
+    NodalExtrap[iNode][7] = 0.125 * (1.0 - Xi) * (1.0 + Eta) * (1.0 + Zeta);
   }
-
 }
 
 su2double CHEXA8::ComputeVolume(const FrameType mode) const {
-
   unsigned short iDim;
-  su2double r1[3] = {0.0,0.0,0.0}, r2[3] = {0.0,0.0,0.0}, r3[3] = {0.0,0.0,0.0}, CrossProduct[3] = {0.0,0.0,0.0};
+  su2double r1[3] = {0.0, 0.0, 0.0}, r2[3] = {0.0, 0.0, 0.0}, r3[3] = {0.0, 0.0, 0.0},
+            CrossProduct[3] = {0.0, 0.0, 0.0};
   su2double Volume = 0.0;
 
   /*--- Select the appropriate source for the nodal coordinates depending on the frame requested
         for the gradient computation, REFERENCE (undeformed) or CURRENT (deformed)---*/
-  const su2activematrix& Coord = (mode==REFERENCE) ? RefCoord : CurrentCoord;
+  const su2activematrix& Coord = (mode == REFERENCE) ? RefCoord : CurrentCoord;
 
   for (iDim = 0; iDim < NDIM; iDim++) {
     r1[iDim] = Coord[1][iDim] - Coord[0][iDim];
@@ -146,11 +187,11 @@ su2double CHEXA8::ComputeVolume(const FrameType mode) const {
     r3[iDim] = Coord[5][iDim] - Coord[0][iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume = fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume = fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   for (iDim = 0; iDim < NDIM; iDim++) {
     r1[iDim] = Coord[2][iDim] - Coord[0][iDim];
@@ -158,11 +199,11 @@ su2double CHEXA8::ComputeVolume(const FrameType mode) const {
     r3[iDim] = Coord[5][iDim] - Coord[0][iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   for (iDim = 0; iDim < NDIM; iDim++) {
     r1[iDim] = Coord[2][iDim] - Coord[0][iDim];
@@ -170,11 +211,11 @@ su2double CHEXA8::ComputeVolume(const FrameType mode) const {
     r3[iDim] = Coord[7][iDim] - Coord[0][iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   for (iDim = 0; iDim < NDIM; iDim++) {
     r1[iDim] = Coord[5][iDim] - Coord[0][iDim];
@@ -182,11 +223,11 @@ su2double CHEXA8::ComputeVolume(const FrameType mode) const {
     r3[iDim] = Coord[4][iDim] - Coord[0][iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   for (iDim = 0; iDim < NDIM; iDim++) {
     r1[iDim] = Coord[7][iDim] - Coord[2][iDim];
@@ -194,13 +235,11 @@ su2double CHEXA8::ComputeVolume(const FrameType mode) const {
     r3[iDim] = Coord[6][iDim] - Coord[2][iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   return Volume;
-
 }
-
diff --git a/Common/src/geometry/elements/CLINE.cpp b/Common/src/geometry/elements/CLINE.cpp
index f9b62361137..d2dd6dd66fd 100644
--- a/Common/src/geometry/elements/CLINE.cpp
+++ b/Common/src/geometry/elements/CLINE.cpp
@@ -27,40 +27,38 @@
 
 #include "../../../include/geometry/elements/CElement.hpp"
 
-CLINE::CLINE() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
-
+CLINE::CLINE() : CElementWithKnownSizes<NGAUSS, NNODE, NDIM>() {
   su2double Xi, val_Ni;
 
   /*--- Gauss coordinates and weights ---*/
 
   su2double oneOnTwoSqrt3 = 0.288675134594813;
-  GaussCoord[0][0] = 0.5-oneOnTwoSqrt3;  GaussWeight(0) = 0.5;
-  GaussCoord[1][0] = 0.5+oneOnTwoSqrt3;  GaussWeight(1) = 0.5;
+  GaussCoord[0][0] = 0.5 - oneOnTwoSqrt3;
+  GaussWeight(0) = 0.5;
+  GaussCoord[1][0] = 0.5 + oneOnTwoSqrt3;
+  GaussWeight(1) = 0.5;
 
   /*--- Store the values of the shape functions and their derivatives ---*/
 
   unsigned short iGauss;
   for (iGauss = 0; iGauss < nGaussPoints; iGauss++) {
-
     Xi = GaussCoord[iGauss][0];
 
-    val_Ni = 1.0-Xi;  GaussPoint[iGauss].SetNi(val_Ni, 0);
-    val_Ni = Xi;  GaussPoint[iGauss].SetNi(val_Ni, 1);
+    val_Ni = 1.0 - Xi;
+    GaussPoint[iGauss].SetNi(val_Ni, 0);
+    val_Ni = Xi;
+    GaussPoint[iGauss].SetNi(val_Ni, 1);
 
     /*--- dN/d xi ---*/
 
     dNiXj[iGauss][0][0] = -1.0;
     dNiXj[iGauss][1][0] = 1.0;
-
   }
-
 }
 
 su2double CLINE::ComputeLength(const FrameType mode) const {
-
   /*--- Select the appropriate source for the nodal coordinates depending on the frame requested
         for the gradient computation, REFERENCE (undeformed) or CURRENT (deformed)---*/
-  const su2activematrix& Coord = (mode==REFERENCE) ? RefCoord : CurrentCoord;
+  const su2activematrix& Coord = (mode == REFERENCE) ? RefCoord : CurrentCoord;
   return fabs(Coord[1][0] - Coord[0][0]);
-
 }
diff --git a/Common/src/geometry/elements/CPRISM6.cpp b/Common/src/geometry/elements/CPRISM6.cpp
index 4e7fb019a3d..111c771c8b7 100644
--- a/Common/src/geometry/elements/CPRISM6.cpp
+++ b/Common/src/geometry/elements/CPRISM6.cpp
@@ -27,21 +27,37 @@
 
 #include "../../../include/geometry/elements/CElement.hpp"
 
-
-CPRISM6::CPRISM6() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
-
+CPRISM6::CPRISM6() : CElementWithKnownSizes<NGAUSS, NNODE, NDIM>() {
   /*--- Gauss coordinates and weights ---*/
 
   /*--- There is some inconsistency between the shape functions and the order of the nodes
         that causes "negative" stiffness, the remedy is to use negative weights. ---*/
 
   su2double oneOnSqrt3 = 0.577350269189626;
-  GaussCoord[0][0] = -oneOnSqrt3;  GaussCoord[0][1] = 1.0/6.0;  GaussCoord[0][2] = 1.0/6.0;  GaussWeight(0) = -1.0/6.0;
-  GaussCoord[1][0] = -oneOnSqrt3;  GaussCoord[1][1] = 2.0/3.0;  GaussCoord[1][2] = 1.0/6.0;  GaussWeight(1) = -1.0/6.0;
-  GaussCoord[2][0] = -oneOnSqrt3;  GaussCoord[2][1] = 1.0/6.0;  GaussCoord[2][2] = 2.0/3.0;  GaussWeight(2) = -1.0/6.0;
-  GaussCoord[3][0] =  oneOnSqrt3;  GaussCoord[3][1] = 1.0/6.0;  GaussCoord[3][2] = 1.0/6.0;  GaussWeight(3) = -1.0/6.0;
-  GaussCoord[4][0] =  oneOnSqrt3;  GaussCoord[4][1] = 2.0/3.0;  GaussCoord[4][2] = 1.0/6.0;  GaussWeight(4) = -1.0/6.0;
-  GaussCoord[5][0] =  oneOnSqrt3;  GaussCoord[5][1] = 1.0/6.0;  GaussCoord[5][2] = 2.0/3.0;  GaussWeight(5) = -1.0/6.0;
+  GaussCoord[0][0] = -oneOnSqrt3;
+  GaussCoord[0][1] = 1.0 / 6.0;
+  GaussCoord[0][2] = 1.0 / 6.0;
+  GaussWeight(0) = -1.0 / 6.0;
+  GaussCoord[1][0] = -oneOnSqrt3;
+  GaussCoord[1][1] = 2.0 / 3.0;
+  GaussCoord[1][2] = 1.0 / 6.0;
+  GaussWeight(1) = -1.0 / 6.0;
+  GaussCoord[2][0] = -oneOnSqrt3;
+  GaussCoord[2][1] = 1.0 / 6.0;
+  GaussCoord[2][2] = 2.0 / 3.0;
+  GaussWeight(2) = -1.0 / 6.0;
+  GaussCoord[3][0] = oneOnSqrt3;
+  GaussCoord[3][1] = 1.0 / 6.0;
+  GaussCoord[3][2] = 1.0 / 6.0;
+  GaussWeight(3) = -1.0 / 6.0;
+  GaussCoord[4][0] = oneOnSqrt3;
+  GaussCoord[4][1] = 2.0 / 3.0;
+  GaussCoord[4][2] = 1.0 / 6.0;
+  GaussWeight(4) = -1.0 / 6.0;
+  GaussCoord[5][0] = oneOnSqrt3;
+  GaussCoord[5][1] = 1.0 / 6.0;
+  GaussCoord[5][2] = 2.0 / 3.0;
+  GaussWeight(5) = -1.0 / 6.0;
 
   /*--- Store the values of the shape functions and their derivatives ---*/
 
@@ -49,84 +65,97 @@ CPRISM6::CPRISM6() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
   su2double Xi, Eta, Zeta, val_Ni;
 
   for (iGauss = 0; iGauss < NGAUSS; iGauss++) {
-
     Xi = GaussCoord[iGauss][0];
     Eta = GaussCoord[iGauss][1];
     Zeta = GaussCoord[iGauss][2];
 
-    val_Ni = 0.5*Eta*(1.0-Xi);              GaussPoint[iGauss].SetNi(val_Ni,0);
-    val_Ni = 0.5*Zeta*(1.0-Xi);             GaussPoint[iGauss].SetNi(val_Ni,1);
-    val_Ni = 0.5*(1.0-Eta-Zeta)*(1.0-Xi);   GaussPoint[iGauss].SetNi(val_Ni,2);
-    val_Ni = 0.5*Eta*(Xi+1.0);              GaussPoint[iGauss].SetNi(val_Ni,3);
-    val_Ni = 0.5*Zeta*(Xi+1.0);             GaussPoint[iGauss].SetNi(val_Ni,4);
-    val_Ni = 0.5*(1.0-Eta-Zeta)*(Xi+1.0);   GaussPoint[iGauss].SetNi(val_Ni,5);
+    val_Ni = 0.5 * Eta * (1.0 - Xi);
+    GaussPoint[iGauss].SetNi(val_Ni, 0);
+    val_Ni = 0.5 * Zeta * (1.0 - Xi);
+    GaussPoint[iGauss].SetNi(val_Ni, 1);
+    val_Ni = 0.5 * (1.0 - Eta - Zeta) * (1.0 - Xi);
+    GaussPoint[iGauss].SetNi(val_Ni, 2);
+    val_Ni = 0.5 * Eta * (Xi + 1.0);
+    GaussPoint[iGauss].SetNi(val_Ni, 3);
+    val_Ni = 0.5 * Zeta * (Xi + 1.0);
+    GaussPoint[iGauss].SetNi(val_Ni, 4);
+    val_Ni = 0.5 * (1.0 - Eta - Zeta) * (Xi + 1.0);
+    GaussPoint[iGauss].SetNi(val_Ni, 5);
 
     /*--- dN/d xi ---*/
 
-    dNiXj[iGauss][0][0] = -0.5*Eta;
-    dNiXj[iGauss][1][0] = -0.5*Zeta;
-    dNiXj[iGauss][2][0] = -0.5*(1.0-Eta-Zeta);
-    dNiXj[iGauss][3][0] =  0.5*Eta;
-    dNiXj[iGauss][4][0] =  0.5*Zeta;
-    dNiXj[iGauss][5][0] =  0.5*(1.0-Eta-Zeta);
+    dNiXj[iGauss][0][0] = -0.5 * Eta;
+    dNiXj[iGauss][1][0] = -0.5 * Zeta;
+    dNiXj[iGauss][2][0] = -0.5 * (1.0 - Eta - Zeta);
+    dNiXj[iGauss][3][0] = 0.5 * Eta;
+    dNiXj[iGauss][4][0] = 0.5 * Zeta;
+    dNiXj[iGauss][5][0] = 0.5 * (1.0 - Eta - Zeta);
 
     /*--- dN/d eta ---*/
 
-    dNiXj[iGauss][0][1] =  0.5*(1.0-Xi);
-    dNiXj[iGauss][1][1] =  0.0;
-    dNiXj[iGauss][2][1] = -0.5*(1.0-Xi);
-    dNiXj[iGauss][3][1] =  0.5*(Xi+1.0);
-    dNiXj[iGauss][4][1] =  0.0;
-    dNiXj[iGauss][5][1] = -0.5*(Xi+1.0);
+    dNiXj[iGauss][0][1] = 0.5 * (1.0 - Xi);
+    dNiXj[iGauss][1][1] = 0.0;
+    dNiXj[iGauss][2][1] = -0.5 * (1.0 - Xi);
+    dNiXj[iGauss][3][1] = 0.5 * (Xi + 1.0);
+    dNiXj[iGauss][4][1] = 0.0;
+    dNiXj[iGauss][5][1] = -0.5 * (Xi + 1.0);
 
     /*--- dN/d mu ---*/
 
-    dNiXj[iGauss][0][2] =  0.0;
-    dNiXj[iGauss][1][2] =  0.5*(1.0-Xi);
-    dNiXj[iGauss][2][2] = -0.5*(1.0-Xi);
-    dNiXj[iGauss][3][2] =  0.0;
-    dNiXj[iGauss][4][2] =  0.5*(Xi+1.0);
-    dNiXj[iGauss][5][2] = -0.5*(Xi+1.0);
-
+    dNiXj[iGauss][0][2] = 0.0;
+    dNiXj[iGauss][1][2] = 0.5 * (1.0 - Xi);
+    dNiXj[iGauss][2][2] = -0.5 * (1.0 - Xi);
+    dNiXj[iGauss][3][2] = 0.0;
+    dNiXj[iGauss][4][2] = 0.5 * (Xi + 1.0);
+    dNiXj[iGauss][5][2] = -0.5 * (Xi + 1.0);
   }
 
   /*--- Store the extrapolation functions ---*/
 
   su2double ExtrapCoord[6][3], sqrt3 = 1.732050807568877;
 
-  ExtrapCoord[0][0] = -sqrt3;  ExtrapCoord[0][1] = -1.0/3.0;  ExtrapCoord[0][2] = -1.0/3.0;
-  ExtrapCoord[1][0] = -sqrt3;  ExtrapCoord[1][1] =  5.0/3.0;  ExtrapCoord[1][2] = -1.0/3.0;
-  ExtrapCoord[2][0] = -sqrt3;  ExtrapCoord[2][1] = -1.0/3.0;  ExtrapCoord[2][2] =  5.0/3.0;
-  ExtrapCoord[3][0] =  sqrt3;  ExtrapCoord[3][1] = -1.0/3.0;  ExtrapCoord[3][2] = -1.0/3.0;
-  ExtrapCoord[4][0] =  sqrt3;  ExtrapCoord[4][1] =  5.0/3.0;  ExtrapCoord[4][2] = -1.0/3.0;
-  ExtrapCoord[5][0] =  sqrt3;  ExtrapCoord[5][1] = -1.0/3.0;  ExtrapCoord[5][2] =  5.0/3.0;
+  ExtrapCoord[0][0] = -sqrt3;
+  ExtrapCoord[0][1] = -1.0 / 3.0;
+  ExtrapCoord[0][2] = -1.0 / 3.0;
+  ExtrapCoord[1][0] = -sqrt3;
+  ExtrapCoord[1][1] = 5.0 / 3.0;
+  ExtrapCoord[1][2] = -1.0 / 3.0;
+  ExtrapCoord[2][0] = -sqrt3;
+  ExtrapCoord[2][1] = -1.0 / 3.0;
+  ExtrapCoord[2][2] = 5.0 / 3.0;
+  ExtrapCoord[3][0] = sqrt3;
+  ExtrapCoord[3][1] = -1.0 / 3.0;
+  ExtrapCoord[3][2] = -1.0 / 3.0;
+  ExtrapCoord[4][0] = sqrt3;
+  ExtrapCoord[4][1] = 5.0 / 3.0;
+  ExtrapCoord[4][2] = -1.0 / 3.0;
+  ExtrapCoord[5][0] = sqrt3;
+  ExtrapCoord[5][1] = -1.0 / 3.0;
+  ExtrapCoord[5][2] = 5.0 / 3.0;
 
   for (iNode = 0; iNode < NNODE; iNode++) {
-
     Xi = ExtrapCoord[iNode][0];
     Eta = ExtrapCoord[iNode][1];
     Zeta = ExtrapCoord[iNode][2];
 
-    NodalExtrap[iNode][0] = 0.5*Eta*(1.0-Xi);
-    NodalExtrap[iNode][1] = 0.5*Zeta*(1.0-Xi);
-    NodalExtrap[iNode][2] = 0.5*(1.0-Eta-Zeta)*(1.0-Xi);
-    NodalExtrap[iNode][3] = 0.5*Eta*(Xi+1.0);
-    NodalExtrap[iNode][4] = 0.5*Zeta*(Xi+1.0);
-    NodalExtrap[iNode][5] = 0.5*(1.0-Eta-Zeta)*(Xi+1.0);
-
+    NodalExtrap[iNode][0] = 0.5 * Eta * (1.0 - Xi);
+    NodalExtrap[iNode][1] = 0.5 * Zeta * (1.0 - Xi);
+    NodalExtrap[iNode][2] = 0.5 * (1.0 - Eta - Zeta) * (1.0 - Xi);
+    NodalExtrap[iNode][3] = 0.5 * Eta * (Xi + 1.0);
+    NodalExtrap[iNode][4] = 0.5 * Zeta * (Xi + 1.0);
+    NodalExtrap[iNode][5] = 0.5 * (1.0 - Eta - Zeta) * (Xi + 1.0);
   }
-
 }
 
 su2double CPRISM6::ComputeVolume(const FrameType mode) const {
-
   unsigned short iDim;
-  su2double r1[3] = {0.0,0.0,0.0}, r2[3] = {0.0,0.0,0.0}, r3[3] = {0.0,0.0,0.0}, CrossProduct[3] = {0.0,0.0,0.0};
+  su2double r1[3] = {0.0, 0.0, 0.0}, r2[3] = {0.0, 0.0, 0.0}, r3[3] = {0.0, 0.0, 0.0},
+            CrossProduct[3] = {0.0, 0.0, 0.0};
   su2double Volume = 0.0;
 
   /*--- Select the appropriate source for the nodal coordinates depending on the frame requested
         for the gradient computation, REFERENCE (undeformed) or CURRENT (deformed)---*/
-  const su2activematrix& Coord = (mode==REFERENCE) ? RefCoord : CurrentCoord;
+  const su2activematrix& Coord = (mode == REFERENCE) ? RefCoord : CurrentCoord;
 
   for (iDim = 0; iDim < NDIM; iDim++) {
     r1[iDim] = Coord[2][iDim] - Coord[0][iDim];
@@ -134,11 +163,11 @@ su2double CPRISM6::ComputeVolume(const FrameType mode) const {
     r3[iDim] = Coord[5][iDim] - Coord[0][iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume = fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume = fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   for (iDim = 0; iDim < NDIM; iDim++) {
     r1[iDim] = Coord[5][iDim] - Coord[0][iDim];
@@ -146,11 +175,11 @@ su2double CPRISM6::ComputeVolume(const FrameType mode) const {
     r3[iDim] = Coord[4][iDim] - Coord[0][iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   for (iDim = 0; iDim < NDIM; iDim++) {
     r1[iDim] = Coord[5][iDim] - Coord[0][iDim];
@@ -158,13 +187,11 @@ su2double CPRISM6::ComputeVolume(const FrameType mode) const {
     r3[iDim] = Coord[3][iDim] - Coord[0][iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   return Volume;
-
 }
-
diff --git a/Common/src/geometry/elements/CPYRAM5.cpp b/Common/src/geometry/elements/CPYRAM5.cpp
index 9003a7d378e..c82d1dbbfeb 100644
--- a/Common/src/geometry/elements/CPYRAM5.cpp
+++ b/Common/src/geometry/elements/CPYRAM5.cpp
@@ -27,16 +27,29 @@
 
 #include "../../../include/geometry/elements/CElement.hpp"
 
-
-CPYRAM5::CPYRAM5() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
-
+CPYRAM5::CPYRAM5() : CElementWithKnownSizes<NGAUSS, NNODE, NDIM>() {
   /*--- Gauss coordinates and weights ---*/
 
-  GaussCoord[0][0] = 0.5;  GaussCoord[0][1] = 0.0;  GaussCoord[0][2] = 0.1531754163448146;  GaussWeight(0) = 2.0/15.0;
-  GaussCoord[1][0] = 0.0;  GaussCoord[1][1] = 0.5;  GaussCoord[1][2] = 0.1531754163448146;  GaussWeight(1) = 2.0/15.0;
-  GaussCoord[2][0] =-0.5;  GaussCoord[2][1] = 0.0;  GaussCoord[2][2] = 0.1531754163448146;  GaussWeight(2) = 2.0/15.0;
-  GaussCoord[3][0] = 0.0;  GaussCoord[3][1] =-0.5;  GaussCoord[3][2] = 0.1531754163448146;  GaussWeight(3) = 2.0/15.0;
-  GaussCoord[4][0] = 0.0;  GaussCoord[4][1] = 0.0;  GaussCoord[4][2] = 0.6372983346207416;  GaussWeight(4) = 2.0/15.0;
+  GaussCoord[0][0] = 0.5;
+  GaussCoord[0][1] = 0.0;
+  GaussCoord[0][2] = 0.1531754163448146;
+  GaussWeight(0) = 2.0 / 15.0;
+  GaussCoord[1][0] = 0.0;
+  GaussCoord[1][1] = 0.5;
+  GaussCoord[1][2] = 0.1531754163448146;
+  GaussWeight(1) = 2.0 / 15.0;
+  GaussCoord[2][0] = -0.5;
+  GaussCoord[2][1] = 0.0;
+  GaussCoord[2][2] = 0.1531754163448146;
+  GaussWeight(2) = 2.0 / 15.0;
+  GaussCoord[3][0] = 0.0;
+  GaussCoord[3][1] = -0.5;
+  GaussCoord[3][2] = 0.1531754163448146;
+  GaussWeight(3) = 2.0 / 15.0;
+  GaussCoord[4][0] = 0.0;
+  GaussCoord[4][1] = 0.0;
+  GaussCoord[4][2] = 0.6372983346207416;
+  GaussWeight(4) = 2.0 / 15.0;
 
   /*--- Store the values of the shape functions and their derivatives ---*/
 
@@ -44,78 +57,90 @@ CPYRAM5::CPYRAM5() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
   su2double Xi, Eta, Zeta, val_Ni;
 
   for (iGauss = 0; iGauss < NGAUSS; iGauss++) {
-
     Xi = GaussCoord[iGauss][0];
     Eta = GaussCoord[iGauss][1];
     Zeta = GaussCoord[iGauss][2];
 
-    val_Ni = 0.25*(-Xi+Eta+Zeta-1.0)*(-Xi-Eta+Zeta-1.0)/(1.0-Zeta);  GaussPoint[iGauss].SetNi(val_Ni,0);
-    val_Ni = 0.25*(-Xi-Eta+Zeta-1.0)*( Xi-Eta+Zeta-1.0)/(1.0-Zeta);  GaussPoint[iGauss].SetNi(val_Ni,1);
-    val_Ni = 0.25*( Xi+Eta+Zeta-1.0)*( Xi-Eta+Zeta-1.0)/(1.0-Zeta);  GaussPoint[iGauss].SetNi(val_Ni,2);
-    val_Ni = 0.25*( Xi+Eta+Zeta-1.0)*(-Xi+Eta+Zeta-1.0)/(1.0-Zeta);  GaussPoint[iGauss].SetNi(val_Ni,3);
-    val_Ni = Zeta;                                                   GaussPoint[iGauss].SetNi(val_Ni,4);
+    val_Ni = 0.25 * (-Xi + Eta + Zeta - 1.0) * (-Xi - Eta + Zeta - 1.0) / (1.0 - Zeta);
+    GaussPoint[iGauss].SetNi(val_Ni, 0);
+    val_Ni = 0.25 * (-Xi - Eta + Zeta - 1.0) * (Xi - Eta + Zeta - 1.0) / (1.0 - Zeta);
+    GaussPoint[iGauss].SetNi(val_Ni, 1);
+    val_Ni = 0.25 * (Xi + Eta + Zeta - 1.0) * (Xi - Eta + Zeta - 1.0) / (1.0 - Zeta);
+    GaussPoint[iGauss].SetNi(val_Ni, 2);
+    val_Ni = 0.25 * (Xi + Eta + Zeta - 1.0) * (-Xi + Eta + Zeta - 1.0) / (1.0 - Zeta);
+    GaussPoint[iGauss].SetNi(val_Ni, 3);
+    val_Ni = Zeta;
+    GaussPoint[iGauss].SetNi(val_Ni, 4);
 
     /*--- dN/d xi ---*/
 
-    dNiXj[iGauss][0][0] = 0.5*(Zeta-Xi-1.0)/(Zeta-1.0);
-    dNiXj[iGauss][1][0] = 0.5*Xi/(Zeta-1.0);
-    dNiXj[iGauss][2][0] = 0.5*(1.0-Zeta-Xi)/(Zeta-1.0);
+    dNiXj[iGauss][0][0] = 0.5 * (Zeta - Xi - 1.0) / (Zeta - 1.0);
+    dNiXj[iGauss][1][0] = 0.5 * Xi / (Zeta - 1.0);
+    dNiXj[iGauss][2][0] = 0.5 * (1.0 - Zeta - Xi) / (Zeta - 1.0);
     dNiXj[iGauss][3][0] = dNiXj[iGauss][1][0];
     dNiXj[iGauss][4][0] = 0.0;
 
     /*--- dN/d eta ---*/
 
-    dNiXj[iGauss][0][1] = 0.5*Eta/(Zeta-1.0);
-    dNiXj[iGauss][1][1] = 0.5*(Zeta-Eta-1.0)/(Zeta-1.0);
+    dNiXj[iGauss][0][1] = 0.5 * Eta / (Zeta - 1.0);
+    dNiXj[iGauss][1][1] = 0.5 * (Zeta - Eta - 1.0) / (Zeta - 1.0);
     dNiXj[iGauss][2][1] = dNiXj[iGauss][0][1];
-    dNiXj[iGauss][3][1] = 0.5*(1.0-Zeta-Eta)/(Zeta-1.0);
+    dNiXj[iGauss][3][1] = 0.5 * (1.0 - Zeta - Eta) / (Zeta - 1.0);
     dNiXj[iGauss][4][1] = 0.0;
 
     /*--- dN/d zeta ---*/
 
-    dNiXj[iGauss][0][2] = 0.25*(-1.0 + 2.0*Zeta - Zeta*Zeta - Eta*Eta + Xi*Xi)/((1.0-Zeta)*(1.0-Zeta));
-    dNiXj[iGauss][1][2] = 0.25*(-1.0 + 2.0*Zeta - Zeta*Zeta + Eta*Eta - Xi*Xi)/((1.0-Zeta)*(1.0-Zeta));
+    dNiXj[iGauss][0][2] =
+        0.25 * (-1.0 + 2.0 * Zeta - Zeta * Zeta - Eta * Eta + Xi * Xi) / ((1.0 - Zeta) * (1.0 - Zeta));
+    dNiXj[iGauss][1][2] =
+        0.25 * (-1.0 + 2.0 * Zeta - Zeta * Zeta + Eta * Eta - Xi * Xi) / ((1.0 - Zeta) * (1.0 - Zeta));
     dNiXj[iGauss][2][2] = dNiXj[iGauss][0][2];
     dNiXj[iGauss][3][2] = dNiXj[iGauss][1][2];
     dNiXj[iGauss][4][2] = 1.0;
-
   }
 
   /*--- Store the extrapolation functions ---*/
 
   su2double ExtrapCoord[5][3];
 
-  ExtrapCoord[0][0] =  2.0;  ExtrapCoord[0][1] =  0.0;  ExtrapCoord[0][2] = -0.316397779494322;
-  ExtrapCoord[1][0] =  0.0;  ExtrapCoord[1][1] =  2.0;  ExtrapCoord[1][2] = -0.316397779494322;
-  ExtrapCoord[2][0] = -2.0;  ExtrapCoord[2][1] =  0.0;  ExtrapCoord[2][2] = -0.316397779494322;
-  ExtrapCoord[3][0] =  0.0;  ExtrapCoord[3][1] = -2.0;  ExtrapCoord[3][2] = -0.316397779494322;
-  ExtrapCoord[4][0] =  0.0;  ExtrapCoord[4][1] =  0.0;  ExtrapCoord[4][2] =  1.749193338482970;
+  ExtrapCoord[0][0] = 2.0;
+  ExtrapCoord[0][1] = 0.0;
+  ExtrapCoord[0][2] = -0.316397779494322;
+  ExtrapCoord[1][0] = 0.0;
+  ExtrapCoord[1][1] = 2.0;
+  ExtrapCoord[1][2] = -0.316397779494322;
+  ExtrapCoord[2][0] = -2.0;
+  ExtrapCoord[2][1] = 0.0;
+  ExtrapCoord[2][2] = -0.316397779494322;
+  ExtrapCoord[3][0] = 0.0;
+  ExtrapCoord[3][1] = -2.0;
+  ExtrapCoord[3][2] = -0.316397779494322;
+  ExtrapCoord[4][0] = 0.0;
+  ExtrapCoord[4][1] = 0.0;
+  ExtrapCoord[4][2] = 1.749193338482970;
 
   for (iNode = 0; iNode < NNODE; iNode++) {
-
     Xi = ExtrapCoord[iNode][0];
     Eta = ExtrapCoord[iNode][1];
     Zeta = ExtrapCoord[iNode][2];
 
-    NodalExtrap[iNode][0] = 0.25*(-Xi+Eta+Zeta-1.0)*(-Xi-Eta+Zeta-1.0)/(1.0-Zeta);
-    NodalExtrap[iNode][1] = 0.25*(-Xi-Eta+Zeta-1.0)*( Xi-Eta+Zeta-1.0)/(1.0-Zeta);
-    NodalExtrap[iNode][2] = 0.25*( Xi+Eta+Zeta-1.0)*( Xi-Eta+Zeta-1.0)/(1.0-Zeta);
-    NodalExtrap[iNode][3] = 0.25*( Xi+Eta+Zeta-1.0)*(-Xi+Eta+Zeta-1.0)/(1.0-Zeta);
+    NodalExtrap[iNode][0] = 0.25 * (-Xi + Eta + Zeta - 1.0) * (-Xi - Eta + Zeta - 1.0) / (1.0 - Zeta);
+    NodalExtrap[iNode][1] = 0.25 * (-Xi - Eta + Zeta - 1.0) * (Xi - Eta + Zeta - 1.0) / (1.0 - Zeta);
+    NodalExtrap[iNode][2] = 0.25 * (Xi + Eta + Zeta - 1.0) * (Xi - Eta + Zeta - 1.0) / (1.0 - Zeta);
+    NodalExtrap[iNode][3] = 0.25 * (Xi + Eta + Zeta - 1.0) * (-Xi + Eta + Zeta - 1.0) / (1.0 - Zeta);
     NodalExtrap[iNode][4] = Zeta;
-
   }
-
 }
 
 su2double CPYRAM5::ComputeVolume(const FrameType mode) const {
-
   unsigned short iDim;
-  su2double r1[3] = {0.0,0.0,0.0}, r2[3] = {0.0,0.0,0.0}, r3[3] = {0.0,0.0,0.0}, CrossProduct[3] = {0.0,0.0,0.0};
+  su2double r1[3] = {0.0, 0.0, 0.0}, r2[3] = {0.0, 0.0, 0.0}, r3[3] = {0.0, 0.0, 0.0},
+            CrossProduct[3] = {0.0, 0.0, 0.0};
   su2double Volume = 0.0;
 
   /*--- Select the appropriate source for the nodal coordinates depending on the frame requested
         for the gradient computation, REFERENCE (undeformed) or CURRENT (deformed)---*/
-  const su2activematrix& Coord = (mode==REFERENCE) ? RefCoord : CurrentCoord;
+  const su2activematrix& Coord = (mode == REFERENCE) ? RefCoord : CurrentCoord;
 
   for (iDim = 0; iDim < NDIM; iDim++) {
     r1[iDim] = Coord[1][iDim] - Coord[0][iDim];
@@ -123,11 +148,11 @@ su2double CPYRAM5::ComputeVolume(const FrameType mode) const {
     r3[iDim] = Coord[4][iDim] - Coord[0][iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume = fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume = fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   for (iDim = 0; iDim < NDIM; iDim++) {
     r1[iDim] = Coord[2][iDim] - Coord[0][iDim];
@@ -135,13 +160,11 @@ su2double CPYRAM5::ComputeVolume(const FrameType mode) const {
     r3[iDim] = Coord[4][iDim] - Coord[0][iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   return Volume;
-
 }
-
diff --git a/Common/src/geometry/elements/CPYRAM6.cpp b/Common/src/geometry/elements/CPYRAM6.cpp
index 8ea03251f51..d152598b594 100644
--- a/Common/src/geometry/elements/CPYRAM6.cpp
+++ b/Common/src/geometry/elements/CPYRAM6.cpp
@@ -27,95 +27,124 @@
 
 #include "../../../include/geometry/elements/CElement.hpp"
 
-
-CPYRAM6::CPYRAM6() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
-
+CPYRAM6::CPYRAM6() : CElementWithKnownSizes<NGAUSS, NNODE, NDIM>() {
   /*--- Gauss coordinates and weights ---*/
 
-   GaussCoord[0][0] = sqrt(4.0/27.0);  GaussCoord[0][1] = sqrt(4.0/27.0);  GaussCoord[0][2] = 1.0/6.0;  GaussWeight(0) = 9.0/20.0;
-   GaussCoord[0][0] = sqrt(4.0/27.0);  GaussCoord[0][1] = sqrt(4.0/27.0);  GaussCoord[0][2] = 1.0/6.0;  GaussWeight(1) = 9.0/20.0;
-   GaussCoord[0][0] = sqrt(4.0/27.0);  GaussCoord[0][1] = sqrt(4.0/27.0);  GaussCoord[0][2] = 1.0/6.0;  GaussWeight(2) = 9.0/20.0;
-   GaussCoord[0][0] = sqrt(4.0/27.0);  GaussCoord[0][1] = sqrt(4.0/27.0);  GaussCoord[0][2] = 1.0/6.0;  GaussWeight(3) = 9.0/20.0;
-   GaussCoord[4][0] = 0.0;             GaussCoord[4][1] = 0.0;             GaussCoord[4][2] = 0.5;      GaussWeight(4) = 3.0/5.0;
-   GaussCoord[5][0] = 0.0;             GaussCoord[5][1] = 0.0;             GaussCoord[5][2] = 0.25;     GaussWeight(5) = -16.0/15.0;
-
-   /*--- Store the values of the shape functions and their derivatives ---*/
-
-   unsigned short iNode, iGauss;
-   su2double Xi, Eta, Zeta, val_Ni;
-
-   for (iGauss = 0; iGauss < nGaussPoints; iGauss++) {
-
-     Xi = GaussCoord[iGauss][0];
-     Eta = GaussCoord[iGauss][1];
-     Zeta = GaussCoord[iGauss][2];
-
-     val_Ni = 0.25*(-Xi+Eta+Zeta-1.0)*(-Xi-Eta+Zeta-1.0)/(1.0-Zeta);  GaussPoint[iGauss].SetNi(val_Ni,0);
-     val_Ni = 0.25*(-Xi-Eta+Zeta-1.0)*( Xi-Eta+Zeta-1.0)/(1.0-Zeta);  GaussPoint[iGauss].SetNi(val_Ni,1);
-     val_Ni = 0.25*( Xi+Eta+Zeta-1.0)*( Xi-Eta+Zeta-1.0)/(1.0-Zeta);  GaussPoint[iGauss].SetNi(val_Ni,2);
-     val_Ni = 0.25*( Xi+Eta+Zeta-1.0)*(-Xi+Eta+Zeta-1.0)/(1.0-Zeta);  GaussPoint[iGauss].SetNi(val_Ni,3);
-     val_Ni = Zeta;                                                   GaussPoint[iGauss].SetNi(val_Ni,4);
-
-     /*--- dN/d xi ---*/
-
-     dNiXj[iGauss][0][0] = 0.5*(Zeta-Xi-1.0)/(Zeta-1.0);
-     dNiXj[iGauss][1][0] = 0.5*Xi/(Zeta-1.0);
-     dNiXj[iGauss][2][0] = 0.5*(1.0-Zeta-Xi)/(Zeta-1.0);
-     dNiXj[iGauss][3][0] = dNiXj[iGauss][1][0];
-     dNiXj[iGauss][4][0] = 0.0;
-
-     /*--- dN/d eta ---*/
-
-     dNiXj[iGauss][0][1] = 0.5*Eta/(Zeta-1.0);
-     dNiXj[iGauss][1][1] = 0.5*(Zeta-Eta-1.0)/(Zeta-1.0);
-     dNiXj[iGauss][2][1] = dNiXj[iGauss][0][1];
-     dNiXj[iGauss][3][1] = 0.5*(1.0-Zeta-Eta)/(Zeta-1.0);
-     dNiXj[iGauss][4][1] = 0.0;
-
-     /*--- dN/d zeta ---*/
-
-     dNiXj[iGauss][0][2] = 0.25*(-1.0 + 2.0*Zeta - Zeta*Zeta - Eta*Eta + Xi*Xi)/((1.0-Zeta)*(1.0-Zeta));
-     dNiXj[iGauss][1][2] = 0.25*(-1.0 + 2.0*Zeta - Zeta*Zeta + Eta*Eta - Xi*Xi)/((1.0-Zeta)*(1.0-Zeta));
-     dNiXj[iGauss][2][2] = dNiXj[iGauss][0][2];
-     dNiXj[iGauss][3][2] = dNiXj[iGauss][1][2];
-     dNiXj[iGauss][4][2] = 1.0;
-
-   }
-
-   /*--- Store the extrapolation functions ---*/
-
-   su2double ExtrapCoord[5][3];
-
-   ExtrapCoord[0][0] =  2.0;  ExtrapCoord[0][1] =  0.0;  ExtrapCoord[0][2] = -0.316397779494322;
-   ExtrapCoord[1][0] =  0.0;  ExtrapCoord[1][1] =  2.0;  ExtrapCoord[1][2] = -0.316397779494322;
-   ExtrapCoord[2][0] = -2.0;  ExtrapCoord[2][1] =  0.0;  ExtrapCoord[2][2] = -0.316397779494322;
-   ExtrapCoord[3][0] =  0.0;  ExtrapCoord[3][1] = -2.0;  ExtrapCoord[3][2] = -0.316397779494322;
-   ExtrapCoord[4][0] =  0.0;  ExtrapCoord[4][1] =  0.0;  ExtrapCoord[4][2] =  1.749193338482970;
-
-   for (iNode = 0; iNode < nNodes; iNode++) {
-
-     Xi = ExtrapCoord[iNode][0];
-     Eta = ExtrapCoord[iNode][1];
-     Zeta = ExtrapCoord[iNode][2];
-
-     NodalExtrap[iNode][0] = 0.25*(-Xi+Eta+Zeta-1.0)*(-Xi-Eta+Zeta-1.0)/(1.0-Zeta);
-     NodalExtrap[iNode][1] = 0.25*(-Xi-Eta+Zeta-1.0)*( Xi-Eta+Zeta-1.0)/(1.0-Zeta);
-     NodalExtrap[iNode][2] = 0.25*( Xi+Eta+Zeta-1.0)*( Xi-Eta+Zeta-1.0)/(1.0-Zeta);
-     NodalExtrap[iNode][3] = 0.25*( Xi+Eta+Zeta-1.0)*(-Xi+Eta+Zeta-1.0)/(1.0-Zeta);
-     NodalExtrap[iNode][4] = Zeta;
+  GaussCoord[0][0] = sqrt(4.0 / 27.0);
+  GaussCoord[0][1] = sqrt(4.0 / 27.0);
+  GaussCoord[0][2] = 1.0 / 6.0;
+  GaussWeight(0) = 9.0 / 20.0;
+  GaussCoord[0][0] = sqrt(4.0 / 27.0);
+  GaussCoord[0][1] = sqrt(4.0 / 27.0);
+  GaussCoord[0][2] = 1.0 / 6.0;
+  GaussWeight(1) = 9.0 / 20.0;
+  GaussCoord[0][0] = sqrt(4.0 / 27.0);
+  GaussCoord[0][1] = sqrt(4.0 / 27.0);
+  GaussCoord[0][2] = 1.0 / 6.0;
+  GaussWeight(2) = 9.0 / 20.0;
+  GaussCoord[0][0] = sqrt(4.0 / 27.0);
+  GaussCoord[0][1] = sqrt(4.0 / 27.0);
+  GaussCoord[0][2] = 1.0 / 6.0;
+  GaussWeight(3) = 9.0 / 20.0;
+  GaussCoord[4][0] = 0.0;
+  GaussCoord[4][1] = 0.0;
+  GaussCoord[4][2] = 0.5;
+  GaussWeight(4) = 3.0 / 5.0;
+  GaussCoord[5][0] = 0.0;
+  GaussCoord[5][1] = 0.0;
+  GaussCoord[5][2] = 0.25;
+  GaussWeight(5) = -16.0 / 15.0;
+
+  /*--- Store the values of the shape functions and their derivatives ---*/
+
+  unsigned short iNode, iGauss;
+  su2double Xi, Eta, Zeta, val_Ni;
+
+  for (iGauss = 0; iGauss < nGaussPoints; iGauss++) {
+    Xi = GaussCoord[iGauss][0];
+    Eta = GaussCoord[iGauss][1];
+    Zeta = GaussCoord[iGauss][2];
+
+    val_Ni = 0.25 * (-Xi + Eta + Zeta - 1.0) * (-Xi - Eta + Zeta - 1.0) / (1.0 - Zeta);
+    GaussPoint[iGauss].SetNi(val_Ni, 0);
+    val_Ni = 0.25 * (-Xi - Eta + Zeta - 1.0) * (Xi - Eta + Zeta - 1.0) / (1.0 - Zeta);
+    GaussPoint[iGauss].SetNi(val_Ni, 1);
+    val_Ni = 0.25 * (Xi + Eta + Zeta - 1.0) * (Xi - Eta + Zeta - 1.0) / (1.0 - Zeta);
+    GaussPoint[iGauss].SetNi(val_Ni, 2);
+    val_Ni = 0.25 * (Xi + Eta + Zeta - 1.0) * (-Xi + Eta + Zeta - 1.0) / (1.0 - Zeta);
+    GaussPoint[iGauss].SetNi(val_Ni, 3);
+    val_Ni = Zeta;
+    GaussPoint[iGauss].SetNi(val_Ni, 4);
+
+    /*--- dN/d xi ---*/
+
+    dNiXj[iGauss][0][0] = 0.5 * (Zeta - Xi - 1.0) / (Zeta - 1.0);
+    dNiXj[iGauss][1][0] = 0.5 * Xi / (Zeta - 1.0);
+    dNiXj[iGauss][2][0] = 0.5 * (1.0 - Zeta - Xi) / (Zeta - 1.0);
+    dNiXj[iGauss][3][0] = dNiXj[iGauss][1][0];
+    dNiXj[iGauss][4][0] = 0.0;
+
+    /*--- dN/d eta ---*/
+
+    dNiXj[iGauss][0][1] = 0.5 * Eta / (Zeta - 1.0);
+    dNiXj[iGauss][1][1] = 0.5 * (Zeta - Eta - 1.0) / (Zeta - 1.0);
+    dNiXj[iGauss][2][1] = dNiXj[iGauss][0][1];
+    dNiXj[iGauss][3][1] = 0.5 * (1.0 - Zeta - Eta) / (Zeta - 1.0);
+    dNiXj[iGauss][4][1] = 0.0;
+
+    /*--- dN/d zeta ---*/
+
+    dNiXj[iGauss][0][2] =
+        0.25 * (-1.0 + 2.0 * Zeta - Zeta * Zeta - Eta * Eta + Xi * Xi) / ((1.0 - Zeta) * (1.0 - Zeta));
+    dNiXj[iGauss][1][2] =
+        0.25 * (-1.0 + 2.0 * Zeta - Zeta * Zeta + Eta * Eta - Xi * Xi) / ((1.0 - Zeta) * (1.0 - Zeta));
+    dNiXj[iGauss][2][2] = dNiXj[iGauss][0][2];
+    dNiXj[iGauss][3][2] = dNiXj[iGauss][1][2];
+    dNiXj[iGauss][4][2] = 1.0;
+  }
 
-   }
+  /*--- Store the extrapolation functions ---*/
+
+  su2double ExtrapCoord[5][3];
+
+  ExtrapCoord[0][0] = 2.0;
+  ExtrapCoord[0][1] = 0.0;
+  ExtrapCoord[0][2] = -0.316397779494322;
+  ExtrapCoord[1][0] = 0.0;
+  ExtrapCoord[1][1] = 2.0;
+  ExtrapCoord[1][2] = -0.316397779494322;
+  ExtrapCoord[2][0] = -2.0;
+  ExtrapCoord[2][1] = 0.0;
+  ExtrapCoord[2][2] = -0.316397779494322;
+  ExtrapCoord[3][0] = 0.0;
+  ExtrapCoord[3][1] = -2.0;
+  ExtrapCoord[3][2] = -0.316397779494322;
+  ExtrapCoord[4][0] = 0.0;
+  ExtrapCoord[4][1] = 0.0;
+  ExtrapCoord[4][2] = 1.749193338482970;
+
+  for (iNode = 0; iNode < nNodes; iNode++) {
+    Xi = ExtrapCoord[iNode][0];
+    Eta = ExtrapCoord[iNode][1];
+    Zeta = ExtrapCoord[iNode][2];
+
+    NodalExtrap[iNode][0] = 0.25 * (-Xi + Eta + Zeta - 1.0) * (-Xi - Eta + Zeta - 1.0) / (1.0 - Zeta);
+    NodalExtrap[iNode][1] = 0.25 * (-Xi - Eta + Zeta - 1.0) * (Xi - Eta + Zeta - 1.0) / (1.0 - Zeta);
+    NodalExtrap[iNode][2] = 0.25 * (Xi + Eta + Zeta - 1.0) * (Xi - Eta + Zeta - 1.0) / (1.0 - Zeta);
+    NodalExtrap[iNode][3] = 0.25 * (Xi + Eta + Zeta - 1.0) * (-Xi + Eta + Zeta - 1.0) / (1.0 - Zeta);
+    NodalExtrap[iNode][4] = Zeta;
+  }
 }
 
 su2double CPYRAM6::ComputeVolume(const FrameType mode) const {
-
   unsigned short iDim;
-  su2double r1[3] = {0.0,0.0,0.0}, r2[3] = {0.0,0.0,0.0}, r3[3] = {0.0,0.0,0.0}, CrossProduct[3] = {0.0,0.0,0.0};
+  su2double r1[3] = {0.0, 0.0, 0.0}, r2[3] = {0.0, 0.0, 0.0}, r3[3] = {0.0, 0.0, 0.0},
+            CrossProduct[3] = {0.0, 0.0, 0.0};
   su2double Volume = 0.0;
 
   /*--- Select the appropriate source for the nodal coordinates depending on the frame requested
         for the gradient computation, REFERENCE (undeformed) or CURRENT (deformed)---*/
-  const su2activematrix& Coord = (mode==REFERENCE) ? RefCoord : CurrentCoord;
+  const su2activematrix& Coord = (mode == REFERENCE) ? RefCoord : CurrentCoord;
 
   for (iDim = 0; iDim < NDIM; iDim++) {
     r1[iDim] = Coord[1][iDim] - Coord[0][iDim];
@@ -123,11 +152,11 @@ su2double CPYRAM6::ComputeVolume(const FrameType mode) const {
     r3[iDim] = Coord[4][iDim] - Coord[0][iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume = fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume = fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   for (iDim = 0; iDim < NDIM; iDim++) {
     r1[iDim] = Coord[2][iDim] - Coord[0][iDim];
@@ -135,13 +164,11 @@ su2double CPYRAM6::ComputeVolume(const FrameType mode) const {
     r3[iDim] = Coord[4][iDim] - Coord[0][iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   return Volume;
-
 }
-
diff --git a/Common/src/geometry/elements/CQUAD4.cpp b/Common/src/geometry/elements/CQUAD4.cpp
index 5a495abcb07..628700ed0b7 100644
--- a/Common/src/geometry/elements/CQUAD4.cpp
+++ b/Common/src/geometry/elements/CQUAD4.cpp
@@ -27,17 +27,23 @@
 
 #include "../../../include/geometry/elements/CElement.hpp"
 
-
-CQUAD4::CQUAD4() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
-
+CQUAD4::CQUAD4() : CElementWithKnownSizes<NGAUSS, NNODE, NDIM>() {
   /*--- Gauss coordinates and weights ---*/
 
   su2double oneOnSqrt3 = 0.577350269189626;
 
-  GaussCoord[0][0] = -oneOnSqrt3;  GaussCoord[0][1] = -oneOnSqrt3;  GaussWeight(0) = 1.0;
-  GaussCoord[1][0] =  oneOnSqrt3;  GaussCoord[1][1] = -oneOnSqrt3;  GaussWeight(1) = 1.0;
-  GaussCoord[2][0] =  oneOnSqrt3;  GaussCoord[2][1] =  oneOnSqrt3;  GaussWeight(2) = 1.0;
-  GaussCoord[3][0] = -oneOnSqrt3;  GaussCoord[3][1] =  oneOnSqrt3;  GaussWeight(3) = 1.0;
+  GaussCoord[0][0] = -oneOnSqrt3;
+  GaussCoord[0][1] = -oneOnSqrt3;
+  GaussWeight(0) = 1.0;
+  GaussCoord[1][0] = oneOnSqrt3;
+  GaussCoord[1][1] = -oneOnSqrt3;
+  GaussWeight(1) = 1.0;
+  GaussCoord[2][0] = oneOnSqrt3;
+  GaussCoord[2][1] = oneOnSqrt3;
+  GaussWeight(2) = 1.0;
+  GaussCoord[3][0] = -oneOnSqrt3;
+  GaussCoord[3][1] = oneOnSqrt3;
+  GaussWeight(3) = 1.0;
 
   /*--- Store the values of the shape functions and their derivatives ---*/
 
@@ -45,70 +51,66 @@ CQUAD4::CQUAD4() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
   su2double Xi, Eta;
 
   for (iGauss = 0; iGauss < NGAUSS; iGauss++) {
-
     Xi = GaussCoord[iGauss][0];
     Eta = GaussCoord[iGauss][1];
 
     su2double Ni[4] = {0.0};
     ShapeFunctions(Xi, Eta, Ni);
 
-    for (jGauss = 0; jGauss < NGAUSS; jGauss++)
-      GaussPoint[iGauss].SetNi(Ni[jGauss], jGauss);
+    for (jGauss = 0; jGauss < NGAUSS; jGauss++) GaussPoint[iGauss].SetNi(Ni[jGauss], jGauss);
 
     /*--- dN/d xi, dN/d eta ---*/
 
     ShapeFunctionJacobian(Xi, Eta, dNiXj[iGauss]);
-
   }
 
   /*--- Store the extrapolation functions (used to compute nodal stresses) ---*/
 
-  su2double ExtrapCoord[4][2], sqrt3 = 1.732050807568877;;
+  su2double ExtrapCoord[4][2], sqrt3 = 1.732050807568877;
+  ;
 
-  ExtrapCoord[0][0] = -sqrt3;  ExtrapCoord[0][1] = -sqrt3;
-  ExtrapCoord[1][0] =  sqrt3;  ExtrapCoord[1][1] = -sqrt3;
-  ExtrapCoord[2][0] =  sqrt3;  ExtrapCoord[2][1] =  sqrt3;
-  ExtrapCoord[3][0] = -sqrt3;  ExtrapCoord[3][1] =  sqrt3;
+  ExtrapCoord[0][0] = -sqrt3;
+  ExtrapCoord[0][1] = -sqrt3;
+  ExtrapCoord[1][0] = sqrt3;
+  ExtrapCoord[1][1] = -sqrt3;
+  ExtrapCoord[2][0] = sqrt3;
+  ExtrapCoord[2][1] = sqrt3;
+  ExtrapCoord[3][0] = -sqrt3;
+  ExtrapCoord[3][1] = sqrt3;
 
   for (iNode = 0; iNode < NNODE; iNode++) {
-
     Xi = ExtrapCoord[iNode][0];
     Eta = ExtrapCoord[iNode][1];
 
-    NodalExtrap[iNode][0] = 0.25*(1.0-Xi)*(1.0-Eta);
-    NodalExtrap[iNode][1] = 0.25*(1.0+Xi)*(1.0-Eta);
-    NodalExtrap[iNode][2] = 0.25*(1.0+Xi)*(1.0+Eta);
-    NodalExtrap[iNode][3] = 0.25*(1.0-Xi)*(1.0+Eta);
-
+    NodalExtrap[iNode][0] = 0.25 * (1.0 - Xi) * (1.0 - Eta);
+    NodalExtrap[iNode][1] = 0.25 * (1.0 + Xi) * (1.0 - Eta);
+    NodalExtrap[iNode][2] = 0.25 * (1.0 + Xi) * (1.0 + Eta);
+    NodalExtrap[iNode][3] = 0.25 * (1.0 - Xi) * (1.0 + Eta);
   }
-
 }
 
 su2double CQUAD4::ComputeArea(const FrameType mode) const {
-
   unsigned short iDim;
-  su2double a[2] = {0.0,0.0}, b[2] = {0.0,0.0};
+  su2double a[2] = {0.0, 0.0}, b[2] = {0.0, 0.0};
   su2double Area = 0.0;
 
   /*--- Select the appropriate source for the nodal coordinates depending on the frame requested
         for the gradient computation, REFERENCE (undeformed) or CURRENT (deformed)---*/
-  const su2activematrix& Coord = (mode==REFERENCE) ? RefCoord : CurrentCoord;
+  const su2activematrix& Coord = (mode == REFERENCE) ? RefCoord : CurrentCoord;
 
   for (iDim = 0; iDim < NDIM; iDim++) {
-    a[iDim] = Coord[0][iDim]-Coord[2][iDim];
-    b[iDim] = Coord[1][iDim]-Coord[2][iDim];
+    a[iDim] = Coord[0][iDim] - Coord[2][iDim];
+    b[iDim] = Coord[1][iDim] - Coord[2][iDim];
   }
 
-  Area = 0.5*fabs(a[0]*b[1]-a[1]*b[0]);
+  Area = 0.5 * fabs(a[0] * b[1] - a[1] * b[0]);
 
   for (iDim = 0; iDim < NDIM; iDim++) {
-    a[iDim] = Coord[0][iDim]-Coord[3][iDim];
-    b[iDim] = Coord[2][iDim]-Coord[3][iDim];
+    a[iDim] = Coord[0][iDim] - Coord[3][iDim];
+    b[iDim] = Coord[2][iDim] - Coord[3][iDim];
   }
 
-  Area += 0.5*fabs(a[0]*b[1]-a[1]*b[0]);
+  Area += 0.5 * fabs(a[0] * b[1] - a[1] * b[0]);
 
   return Area;
-
 }
-
diff --git a/Common/src/geometry/elements/CTETRA1.cpp b/Common/src/geometry/elements/CTETRA1.cpp
index 41242eec185..1d937ef56ce 100644
--- a/Common/src/geometry/elements/CTETRA1.cpp
+++ b/Common/src/geometry/elements/CTETRA1.cpp
@@ -28,11 +28,13 @@
 #include "../../../include/geometry/elements/CElement.hpp"
 #include "../../../include/toolboxes/geometry_toolbox.hpp"
 
-CTETRA1::CTETRA1() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
-
+CTETRA1::CTETRA1() : CElementWithKnownSizes<NGAUSS, NNODE, NDIM>() {
   /*--- Gauss coordinates and weights ---*/
 
-  GaussCoord[0][0] = 0.25;  GaussCoord[0][1] = 0.25; GaussCoord[0][2] = 0.25;  GaussWeight(0) = 1.0/6.0;
+  GaussCoord[0][0] = 0.25;
+  GaussCoord[0][1] = 0.25;
+  GaussCoord[0][2] = 0.25;
+  GaussWeight(0) = 1.0 / 6.0;
 
   /*--- Store the values of the shape functions and their derivatives ---*/
 
@@ -40,23 +42,33 @@ CTETRA1::CTETRA1() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
   su2double Xi, Eta, Zeta, val_Ni;
 
   for (iGauss = 0; iGauss < NGAUSS; iGauss++) {
-
     Xi = GaussCoord[iGauss][0];
     Eta = GaussCoord[iGauss][1];
     Zeta = GaussCoord[iGauss][2];
 
-    val_Ni = Xi;              GaussPoint[iGauss].SetNi(val_Ni,0);
-    val_Ni = Eta;             GaussPoint[iGauss].SetNi(val_Ni,1);
-    val_Ni = 1.0-Xi-Eta-Zeta; GaussPoint[iGauss].SetNi(val_Ni,2);
-    val_Ni = Zeta;            GaussPoint[iGauss].SetNi(val_Ni,3);
+    val_Ni = Xi;
+    GaussPoint[iGauss].SetNi(val_Ni, 0);
+    val_Ni = Eta;
+    GaussPoint[iGauss].SetNi(val_Ni, 1);
+    val_Ni = 1.0 - Xi - Eta - Zeta;
+    GaussPoint[iGauss].SetNi(val_Ni, 2);
+    val_Ni = Zeta;
+    GaussPoint[iGauss].SetNi(val_Ni, 3);
 
     /*--- dN/d xi, dN/d eta, dN/d zeta ---*/
 
-    dNiXj[iGauss][0][0] =  1.0;  dNiXj[iGauss][0][1] =  0.0;  dNiXj[iGauss][0][2] =  0.0;
-    dNiXj[iGauss][1][0] =  0.0;  dNiXj[iGauss][1][1] =  1.0;  dNiXj[iGauss][1][2] =  0.0;
-    dNiXj[iGauss][2][0] = -1.0;  dNiXj[iGauss][2][1] = -1.0;  dNiXj[iGauss][2][2] = -1.0;
-    dNiXj[iGauss][3][0] =  0.0;  dNiXj[iGauss][3][1] =  0.0;  dNiXj[iGauss][3][2] =  1.0;
-
+    dNiXj[iGauss][0][0] = 1.0;
+    dNiXj[iGauss][0][1] = 0.0;
+    dNiXj[iGauss][0][2] = 0.0;
+    dNiXj[iGauss][1][0] = 0.0;
+    dNiXj[iGauss][1][1] = 1.0;
+    dNiXj[iGauss][1][2] = 0.0;
+    dNiXj[iGauss][2][0] = -1.0;
+    dNiXj[iGauss][2][1] = -1.0;
+    dNiXj[iGauss][2][2] = -1.0;
+    dNiXj[iGauss][3][0] = 0.0;
+    dNiXj[iGauss][3][1] = 0.0;
+    dNiXj[iGauss][3][2] = 1.0;
   }
 
   /*--- Shape functions evaluated at the nodes for extrapolation of the stresses at the Gaussian Points ---*/
@@ -66,18 +78,17 @@ CTETRA1::CTETRA1() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
   NodalExtrap[1][0] = 1.0;
   NodalExtrap[2][0] = 1.0;
   NodalExtrap[3][0] = 1.0;
-
 }
 
 su2double CTETRA1::ComputeVolume(const FrameType mode) const {
-
   unsigned short iDim;
-  su2double r1[3] = {0.0,0.0,0.0}, r2[3] = {0.0,0.0,0.0}, r3[3] = {0.0,0.0,0.0}, CrossProduct[3] = {0.0,0.0,0.0};
+  su2double r1[3] = {0.0, 0.0, 0.0}, r2[3] = {0.0, 0.0, 0.0}, r3[3] = {0.0, 0.0, 0.0},
+            CrossProduct[3] = {0.0, 0.0, 0.0};
   su2double Volume = 0.0;
 
   /*--- Select the appropriate source for the nodal coordinates depending on the frame requested
         for the gradient computation, REFERENCE (undeformed) or CURRENT (deformed)---*/
-  const su2activematrix& Coord = (mode==REFERENCE) ? RefCoord : CurrentCoord;
+  const su2activematrix& Coord = (mode == REFERENCE) ? RefCoord : CurrentCoord;
 
   for (iDim = 0; iDim < NDIM; iDim++) {
     r1[iDim] = Coord[1][iDim] - Coord[0][iDim];
@@ -86,9 +97,7 @@ su2double CTETRA1::ComputeVolume(const FrameType mode) const {
   }
 
   GeometryToolbox::CrossProduct(r1, r2, CrossProduct);
-  Volume = fabs(GeometryToolbox::DotProduct(3, CrossProduct, r3))/6.0;
+  Volume = fabs(GeometryToolbox::DotProduct(3, CrossProduct, r3)) / 6.0;
 
   return Volume;
-
 }
-
diff --git a/Common/src/geometry/elements/CTETRA4.cpp b/Common/src/geometry/elements/CTETRA4.cpp
index 74740cb227e..614d0352c29 100644
--- a/Common/src/geometry/elements/CTETRA4.cpp
+++ b/Common/src/geometry/elements/CTETRA4.cpp
@@ -28,16 +28,27 @@
 #include "../../../include/geometry/elements/CElement.hpp"
 #include "../../../include/toolboxes/geometry_toolbox.hpp"
 
-CTETRA4::CTETRA4() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
-
+CTETRA4::CTETRA4() : CElementWithKnownSizes<NGAUSS, NNODE, NDIM>() {
   /*--- Gauss coordinates and weights ---*/
 
-  su2double r = ((5.0-sqrt(5.0))/20);
-  su2double s = ((5.0+3*sqrt(5.0))/20);
-  GaussCoord[0][0] = r;  GaussCoord[0][1] = r; GaussCoord[0][2] = r;  GaussWeight(0) = 1.0/24.0;
-  GaussCoord[0][0] = s;  GaussCoord[0][1] = r; GaussCoord[0][2] = r;  GaussWeight(1) = 1.0/24.0;
-  GaussCoord[0][0] = r;  GaussCoord[0][1] = s; GaussCoord[0][2] = r;  GaussWeight(2) = 1.0/24.0;
-  GaussCoord[0][0] = r;  GaussCoord[0][1] = r; GaussCoord[0][2] = s;  GaussWeight(3) = 1.0/24.0;
+  su2double r = ((5.0 - sqrt(5.0)) / 20);
+  su2double s = ((5.0 + 3 * sqrt(5.0)) / 20);
+  GaussCoord[0][0] = r;
+  GaussCoord[0][1] = r;
+  GaussCoord[0][2] = r;
+  GaussWeight(0) = 1.0 / 24.0;
+  GaussCoord[0][0] = s;
+  GaussCoord[0][1] = r;
+  GaussCoord[0][2] = r;
+  GaussWeight(1) = 1.0 / 24.0;
+  GaussCoord[0][0] = r;
+  GaussCoord[0][1] = s;
+  GaussCoord[0][2] = r;
+  GaussWeight(2) = 1.0 / 24.0;
+  GaussCoord[0][0] = r;
+  GaussCoord[0][1] = r;
+  GaussCoord[0][2] = s;
+  GaussWeight(3) = 1.0 / 24.0;
 
   /*--- Store the values of the shape functions and their derivatives ---*/
 
@@ -45,23 +56,33 @@ CTETRA4::CTETRA4() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
   su2double Xi, Eta, Zeta, val_Ni;
 
   for (iGauss = 0; iGauss < nGaussPoints; iGauss++) {
-
     Xi = GaussCoord[iGauss][0];
     Eta = GaussCoord[iGauss][1];
     Zeta = GaussCoord[iGauss][2];
 
-    val_Ni = Xi;              GaussPoint[iGauss].SetNi(val_Ni,0);
-    val_Ni = Eta;             GaussPoint[iGauss].SetNi(val_Ni,1);
-    val_Ni = 1.0-Xi-Eta-Zeta; GaussPoint[iGauss].SetNi(val_Ni,2);
-    val_Ni = Zeta;            GaussPoint[iGauss].SetNi(val_Ni,3);
+    val_Ni = Xi;
+    GaussPoint[iGauss].SetNi(val_Ni, 0);
+    val_Ni = Eta;
+    GaussPoint[iGauss].SetNi(val_Ni, 1);
+    val_Ni = 1.0 - Xi - Eta - Zeta;
+    GaussPoint[iGauss].SetNi(val_Ni, 2);
+    val_Ni = Zeta;
+    GaussPoint[iGauss].SetNi(val_Ni, 3);
 
     /*--- dN/d xi, dN/d eta, dN/d zeta ---*/
 
-    dNiXj[iGauss][0][0] =  1.0;  dNiXj[iGauss][0][1] =  0.0;  dNiXj[iGauss][0][2] =  0.0;
-    dNiXj[iGauss][1][0] =  0.0;  dNiXj[iGauss][1][1] =  1.0;  dNiXj[iGauss][1][2] =  0.0;
-    dNiXj[iGauss][2][0] = -1.0;  dNiXj[iGauss][2][1] = -1.0;  dNiXj[iGauss][2][2] = -1.0;
-    dNiXj[iGauss][3][0] =  0.0;  dNiXj[iGauss][3][1] =  0.0;  dNiXj[iGauss][3][2] =  1.0;
-
+    dNiXj[iGauss][0][0] = 1.0;
+    dNiXj[iGauss][0][1] = 0.0;
+    dNiXj[iGauss][0][2] = 0.0;
+    dNiXj[iGauss][1][0] = 0.0;
+    dNiXj[iGauss][1][1] = 1.0;
+    dNiXj[iGauss][1][2] = 0.0;
+    dNiXj[iGauss][2][0] = -1.0;
+    dNiXj[iGauss][2][1] = -1.0;
+    dNiXj[iGauss][2][2] = -1.0;
+    dNiXj[iGauss][3][0] = 0.0;
+    dNiXj[iGauss][3][1] = 0.0;
+    dNiXj[iGauss][3][2] = 1.0;
   }
 
   /*--- Shape functions evaluated at the nodes for extrapolation of the stresses at the Gaussian Points ---*/
@@ -71,18 +92,17 @@ CTETRA4::CTETRA4() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
   NodalExtrap[1][0] = 1.0;
   NodalExtrap[2][0] = 1.0;
   NodalExtrap[3][0] = 1.0;
-
 }
 
 su2double CTETRA4::ComputeVolume(const FrameType mode) const {
-
   unsigned short iDim;
-  su2double r1[3] = {0.0,0.0,0.0}, r2[3] = {0.0,0.0,0.0}, r3[3] = {0.0,0.0,0.0}, CrossProduct[3] = {0.0,0.0,0.0};
+  su2double r1[3] = {0.0, 0.0, 0.0}, r2[3] = {0.0, 0.0, 0.0}, r3[3] = {0.0, 0.0, 0.0},
+            CrossProduct[3] = {0.0, 0.0, 0.0};
   su2double Volume = 0.0;
 
   /*--- Select the appropriate source for the nodal coordinates depending on the frame requested
         for the gradient computation, REFERENCE (undeformed) or CURRENT (deformed)---*/
-  const su2activematrix& Coord = (mode==REFERENCE) ? RefCoord : CurrentCoord;
+  const su2activematrix& Coord = (mode == REFERENCE) ? RefCoord : CurrentCoord;
 
   for (iDim = 0; iDim < NDIM; iDim++) {
     r1[iDim] = Coord[1][iDim] - Coord[0][iDim];
@@ -91,9 +111,7 @@ su2double CTETRA4::ComputeVolume(const FrameType mode) const {
   }
 
   GeometryToolbox::CrossProduct(r1, r2, CrossProduct);
-  Volume = fabs(GeometryToolbox::DotProduct(3, CrossProduct, r3))/6.0;
+  Volume = fabs(GeometryToolbox::DotProduct(3, CrossProduct, r3)) / 6.0;
 
   return Volume;
-
 }
-
diff --git a/Common/src/geometry/elements/CTRIA1.cpp b/Common/src/geometry/elements/CTRIA1.cpp
index e74c707f627..f845f2634fb 100644
--- a/Common/src/geometry/elements/CTRIA1.cpp
+++ b/Common/src/geometry/elements/CTRIA1.cpp
@@ -27,12 +27,12 @@
 
 #include "../../../include/geometry/elements/CElement.hpp"
 
-
-CTRIA1::CTRIA1() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
-
+CTRIA1::CTRIA1() : CElementWithKnownSizes<NGAUSS, NNODE, NDIM>() {
   /*--- Gauss coordinates and weights ---*/
 
-  GaussCoord[0][0] = 1.0/3.0;  GaussCoord[0][1] = 1.0/3.0;  GaussWeight(0) = 0.5;
+  GaussCoord[0][0] = 1.0 / 3.0;
+  GaussCoord[0][1] = 1.0 / 3.0;
+  GaussWeight(0) = 0.5;
 
   /*--- Store the values of the shape functions and their derivatives ---*/
 
@@ -40,20 +40,24 @@ CTRIA1::CTRIA1() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
   su2double Xi, Eta, val_Ni;
 
   for (iGauss = 0; iGauss < NGAUSS; iGauss++) {
-
     Xi = GaussCoord[iGauss][0];
     Eta = GaussCoord[iGauss][1];
 
-    val_Ni = Xi;        GaussPoint[iGauss].SetNi(val_Ni,0);
-    val_Ni = Eta;       GaussPoint[iGauss].SetNi(val_Ni,1);
-    val_Ni = 1-Xi-Eta;  GaussPoint[iGauss].SetNi(val_Ni,2);
+    val_Ni = Xi;
+    GaussPoint[iGauss].SetNi(val_Ni, 0);
+    val_Ni = Eta;
+    GaussPoint[iGauss].SetNi(val_Ni, 1);
+    val_Ni = 1 - Xi - Eta;
+    GaussPoint[iGauss].SetNi(val_Ni, 2);
 
     /*--- dN/d xi, dN/d eta ---*/
 
-    dNiXj[iGauss][0][0] =  1.0;  dNiXj[iGauss][0][1] =  0.0;
-    dNiXj[iGauss][1][0] =  0.0;  dNiXj[iGauss][1][1] =  1.0;
-    dNiXj[iGauss][2][0] = -1.0;  dNiXj[iGauss][2][1] = -1.0;
-
+    dNiXj[iGauss][0][0] = 1.0;
+    dNiXj[iGauss][0][1] = 0.0;
+    dNiXj[iGauss][1][0] = 0.0;
+    dNiXj[iGauss][1][1] = 1.0;
+    dNiXj[iGauss][2][0] = -1.0;
+    dNiXj[iGauss][2][1] = -1.0;
   }
 
   /*--- Shape functions evaluated at the nodes for extrapolation of the stresses at the Gaussian Points ---*/
@@ -62,27 +66,23 @@ CTRIA1::CTRIA1() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
   NodalExtrap[0][0] = 1.0;
   NodalExtrap[1][0] = 1.0;
   NodalExtrap[2][0] = 1.0;
-
 }
 
 su2double CTRIA1::ComputeArea(const FrameType mode) const {
-
   unsigned short iDim;
-  su2double a[2] = {0.0,0.0}, b[2] = {0.0,0.0};
+  su2double a[2] = {0.0, 0.0}, b[2] = {0.0, 0.0};
   su2double Area = 0.0;
 
   /*--- Select the appropriate source for the nodal coordinates depending on the frame requested
         for the gradient computation, REFERENCE (undeformed) or CURRENT (deformed) ---*/
-  const su2activematrix& Coord = (mode==REFERENCE) ? RefCoord : CurrentCoord;
+  const su2activematrix& Coord = (mode == REFERENCE) ? RefCoord : CurrentCoord;
 
   for (iDim = 0; iDim < NDIM; iDim++) {
-    a[iDim] = Coord[0][iDim]-Coord[2][iDim];
-    b[iDim] = Coord[1][iDim]-Coord[2][iDim];
+    a[iDim] = Coord[0][iDim] - Coord[2][iDim];
+    b[iDim] = Coord[1][iDim] - Coord[2][iDim];
   }
 
-  Area = 0.5*fabs(a[0]*b[1]-a[1]*b[0]);
+  Area = 0.5 * fabs(a[0] * b[1] - a[1] * b[0]);
 
   return Area;
-
 }
-
diff --git a/Common/src/geometry/elements/CTRIA3.cpp b/Common/src/geometry/elements/CTRIA3.cpp
index afc3996a811..f9856113e4a 100644
--- a/Common/src/geometry/elements/CTRIA3.cpp
+++ b/Common/src/geometry/elements/CTRIA3.cpp
@@ -27,13 +27,18 @@
 
 #include "../../../include/geometry/elements/CElement.hpp"
 
-CTRIA3::CTRIA3() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
-
+CTRIA3::CTRIA3() : CElementWithKnownSizes<NGAUSS, NNODE, NDIM>() {
   /*--- Gauss coordinates and weights ---*/
 
-  GaussCoord[0][0] = 0.66666666666666666667; GaussCoord[0][1] = 0.16666666666666666667; GaussWeight(0) = 0.33333333333333333333;
-  GaussCoord[1][0] = 0.16666666666666666667; GaussCoord[1][1] = 0.66666666666666666667; GaussWeight(1) = 0.33333333333333333333;
-  GaussCoord[2][0] = 0.16666666666666666667; GaussCoord[2][1] = 0.16666666666666666667; GaussWeight(2) = 0.33333333333333333333;
+  GaussCoord[0][0] = 0.66666666666666666667;
+  GaussCoord[0][1] = 0.16666666666666666667;
+  GaussWeight(0) = 0.33333333333333333333;
+  GaussCoord[1][0] = 0.16666666666666666667;
+  GaussCoord[1][1] = 0.66666666666666666667;
+  GaussWeight(1) = 0.33333333333333333333;
+  GaussCoord[2][0] = 0.16666666666666666667;
+  GaussCoord[2][1] = 0.16666666666666666667;
+  GaussWeight(2) = 0.33333333333333333333;
 
   /*--- Store the values of the shape functions and their derivatives ---*/
 
@@ -41,20 +46,24 @@ CTRIA3::CTRIA3() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
   su2double Xi, Eta, val_Ni;
 
   for (iGauss = 0; iGauss < nGaussPoints; iGauss++) {
-
     Xi = GaussCoord[iGauss][0];
     Eta = GaussCoord[iGauss][1];
 
-    val_Ni = 1-Xi-Eta;        GaussPoint[iGauss].SetNi(val_Ni,0);
-    val_Ni = Xi;              GaussPoint[iGauss].SetNi(val_Ni,1);
-    val_Ni = Eta;             GaussPoint[iGauss].SetNi(val_Ni,2);
+    val_Ni = 1 - Xi - Eta;
+    GaussPoint[iGauss].SetNi(val_Ni, 0);
+    val_Ni = Xi;
+    GaussPoint[iGauss].SetNi(val_Ni, 1);
+    val_Ni = Eta;
+    GaussPoint[iGauss].SetNi(val_Ni, 2);
 
     /*--- dN/d xi, dN/d eta ---*/
 
-    dNiXj[iGauss][0][0] =  -1.0;  dNiXj[iGauss][0][1] =  -1.0;
-    dNiXj[iGauss][1][0] =   1.0;  dNiXj[iGauss][1][1] =   0.0;
-    dNiXj[iGauss][2][0] =   0.0;  dNiXj[iGauss][2][1] =   1.0;
-
+    dNiXj[iGauss][0][0] = -1.0;
+    dNiXj[iGauss][0][1] = -1.0;
+    dNiXj[iGauss][1][0] = 1.0;
+    dNiXj[iGauss][1][1] = 0.0;
+    dNiXj[iGauss][2][0] = 0.0;
+    dNiXj[iGauss][2][1] = 1.0;
   }
 
   /*--- Shape functions evaluated at the nodes for extrapolation of the stresses at the Gaussian Points ---*/
@@ -63,26 +72,23 @@ CTRIA3::CTRIA3() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
   NodalExtrap[0][0] = 1.0;
   NodalExtrap[1][0] = 1.0;
   NodalExtrap[2][0] = 1.0;
-
 }
 
 su2double CTRIA3::ComputeArea(const FrameType mode) const {
-
   unsigned short iDim;
-  su2double a[3] = {0.0,0.0,0.0}, b[3] = {0.0,0.0,0.0};
+  su2double a[3] = {0.0, 0.0, 0.0}, b[3] = {0.0, 0.0, 0.0};
   su2double Area = 0.0;
 
   /*--- Select the appropriate source for the nodal coordinates depending on the frame requested
         for the gradient computation, REFERENCE (undeformed) or CURRENT (deformed) ---*/
-  const su2activematrix& Coord = (mode==REFERENCE) ? RefCoord : CurrentCoord;
+  const su2activematrix& Coord = (mode == REFERENCE) ? RefCoord : CurrentCoord;
 
   for (iDim = 0; iDim < NDIM; iDim++) {
-    a[iDim] = Coord[0][iDim]-Coord[2][iDim];
-    b[iDim] = Coord[1][iDim]-Coord[2][iDim];
+    a[iDim] = Coord[0][iDim] - Coord[2][iDim];
+    b[iDim] = Coord[1][iDim] - Coord[2][iDim];
   }
 
-  Area = 0.5*fabs(a[0]*b[1]-a[1]*b[0]);
+  Area = 0.5 * fabs(a[0] * b[1] - a[1] * b[0]);
 
   return Area;
-
 }
diff --git a/Common/src/geometry/meshreader/CBoxMeshReaderFVM.cpp b/Common/src/geometry/meshreader/CBoxMeshReaderFVM.cpp
index 09c0427c920..7d63be15052 100644
--- a/Common/src/geometry/meshreader/CBoxMeshReaderFVM.cpp
+++ b/Common/src/geometry/meshreader/CBoxMeshReaderFVM.cpp
@@ -29,16 +29,13 @@
 #include "../../../include/toolboxes/CLinearPartitioner.hpp"
 #include "../../../include/geometry/meshreader/CBoxMeshReaderFVM.hpp"
 
-CBoxMeshReaderFVM::CBoxMeshReaderFVM(CConfig        *val_config,
-                                     unsigned short val_iZone,
-                                     unsigned short val_nZone)
-: CMeshReaderFVM(val_config, val_iZone, val_nZone) {
-
+CBoxMeshReaderFVM::CBoxMeshReaderFVM(CConfig* val_config, unsigned short val_iZone, unsigned short val_nZone)
+    : CMeshReaderFVM(val_config, val_iZone, val_nZone) {
   /* The box mesh is always 3D. */
   dimension = 3;
 
   /* Set the VTK type for the interior elements and the boundary elements. */
-  KindElem  = HEXAHEDRON;
+  KindElem = HEXAHEDRON;
   KindBound = QUADRILATERAL;
 
   /* The number of nodes in the i and j directions. */
@@ -64,21 +61,19 @@ CBoxMeshReaderFVM::CBoxMeshReaderFVM(CConfig        *val_config,
   ComputeBoxPointCoordinates();
   ComputeBoxVolumeConnectivity();
   ComputeBoxSurfaceConnectivity();
-
 }
 
-CBoxMeshReaderFVM::~CBoxMeshReaderFVM(void) { }
+CBoxMeshReaderFVM::~CBoxMeshReaderFVM(void) {}
 
 void CBoxMeshReaderFVM::ComputeBoxPointCoordinates() {
-
   /* Set the global count of points based on the grid dimensions. */
-  numberOfGlobalPoints = (nNode)*(mNode)*(pNode);
+  numberOfGlobalPoints = (nNode) * (mNode) * (pNode);
 
   /* Get a partitioner to help with linear partitioning. */
-  CLinearPartitioner pointPartitioner(numberOfGlobalPoints,0);
+  CLinearPartitioner pointPartitioner(numberOfGlobalPoints, 0);
 
   /* Determine number of local points */
-  for(unsigned long globalIndex=0; globalIndex < numberOfGlobalPoints; globalIndex++) {
+  for (unsigned long globalIndex = 0; globalIndex < numberOfGlobalPoints; globalIndex++) {
     if ((int)pointPartitioner.GetRankContainingIndex(globalIndex) == rank) {
       numberOfLocalPoints++;
     }
@@ -87,19 +82,17 @@ void CBoxMeshReaderFVM::ComputeBoxPointCoordinates() {
   /* Loop over our analytically defined of coordinates and store only
    those that contain a node within our linear partition of points. */
   localPointCoordinates.resize(dimension);
-  for (int k = 0; k < dimension; k++)
-    localPointCoordinates[k].reserve(numberOfLocalPoints);
+  for (int k = 0; k < dimension; k++) localPointCoordinates[k].reserve(numberOfLocalPoints);
 
   unsigned long globalIndex = 0;
   for (unsigned long kNode = 0; kNode < pNode; kNode++) {
     for (unsigned long jNode = 0; jNode < mNode; jNode++) {
       for (unsigned long iNode = 0; iNode < nNode; iNode++) {
         if ((int)pointPartitioner.GetRankContainingIndex(globalIndex) == rank) {
-
           /* Store the coordinates more clearly. */
-          const passivedouble x = SU2_TYPE::GetValue(Lx*((su2double)iNode)/((su2double)(nNode-1))+Ox);
-          const passivedouble y = SU2_TYPE::GetValue(Ly*((su2double)jNode)/((su2double)(mNode-1))+Oy);
-          const passivedouble z = SU2_TYPE::GetValue(Lz*((su2double)kNode)/((su2double)(pNode-1))+Oz);
+          const passivedouble x = SU2_TYPE::GetValue(Lx * ((su2double)iNode) / ((su2double)(nNode - 1)) + Ox);
+          const passivedouble y = SU2_TYPE::GetValue(Ly * ((su2double)jNode) / ((su2double)(mNode - 1)) + Oy);
+          const passivedouble z = SU2_TYPE::GetValue(Lz * ((su2double)kNode) / ((su2double)(pNode - 1)) + Oz);
 
           /* Load into the coordinate class data structure. */
           localPointCoordinates[0].push_back(x);
@@ -110,35 +103,32 @@ void CBoxMeshReaderFVM::ComputeBoxPointCoordinates() {
       }
     }
   }
-
 }
 
 void CBoxMeshReaderFVM::ComputeBoxVolumeConnectivity() {
-
   /* Set the global count of elements based on the grid dimensions. */
-  numberOfGlobalElements = (nNode-1)*(mNode-1)*(pNode-1);
+  numberOfGlobalElements = (nNode - 1) * (mNode - 1) * (pNode - 1);
 
   /* Get a partitioner to help with linear partitioning. */
-  CLinearPartitioner pointPartitioner(numberOfGlobalPoints,0);
+  CLinearPartitioner pointPartitioner(numberOfGlobalPoints, 0);
 
   /* Loop over our analytically defined of elements and store only those
    that contain a node within our linear partition of points. */
-  numberOfLocalElements  = 0;
-  vector<unsigned long> connectivity(N_POINTS_HEXAHEDRON,0);
+  numberOfLocalElements = 0;
+  vector<unsigned long> connectivity(N_POINTS_HEXAHEDRON, 0);
   unsigned long globalIndex = 0;
-  for (unsigned long kNode = 0; kNode < pNode-1; kNode++) {
-    for (unsigned long jNode = 0; jNode < mNode-1; jNode++) {
-      for (unsigned long iNode = 0; iNode < nNode-1; iNode++) {
-
+  for (unsigned long kNode = 0; kNode < pNode - 1; kNode++) {
+    for (unsigned long jNode = 0; jNode < mNode - 1; jNode++) {
+      for (unsigned long iNode = 0; iNode < nNode - 1; iNode++) {
         /* Compute connectivity based on the i,j,k index. */
-        connectivity[0] = kNode*mNode*nNode + jNode*nNode + iNode;
-        connectivity[1] = kNode*mNode*nNode + jNode*nNode + iNode + 1;
-        connectivity[2] = kNode*mNode*nNode + (jNode + 1)*nNode + (iNode + 1);
-        connectivity[3] = kNode*mNode*nNode + (jNode + 1)*nNode + iNode;
-        connectivity[4] = (kNode + 1)*mNode*nNode + jNode*nNode + iNode;
-        connectivity[5] = (kNode + 1)*mNode*nNode + jNode*nNode + iNode + 1;
-        connectivity[6] = (kNode + 1)*mNode*nNode + (jNode + 1)*nNode + (iNode + 1);
-        connectivity[7] = (kNode + 1)*mNode*nNode + (jNode + 1)*nNode + iNode;
+        connectivity[0] = kNode * mNode * nNode + jNode * nNode + iNode;
+        connectivity[1] = kNode * mNode * nNode + jNode * nNode + iNode + 1;
+        connectivity[2] = kNode * mNode * nNode + (jNode + 1) * nNode + (iNode + 1);
+        connectivity[3] = kNode * mNode * nNode + (jNode + 1) * nNode + iNode;
+        connectivity[4] = (kNode + 1) * mNode * nNode + jNode * nNode + iNode;
+        connectivity[5] = (kNode + 1) * mNode * nNode + jNode * nNode + iNode + 1;
+        connectivity[6] = (kNode + 1) * mNode * nNode + (jNode + 1) * nNode + (iNode + 1);
+        connectivity[7] = (kNode + 1) * mNode * nNode + (jNode + 1) * nNode + iNode;
 
         /* Check whether any of the points is in our linear partition. */
         bool isOwned = false;
@@ -161,126 +151,117 @@ void CBoxMeshReaderFVM::ComputeBoxVolumeConnectivity() {
       }
     }
   }
-
 }
 
 void CBoxMeshReaderFVM::ComputeBoxSurfaceConnectivity() {
-
   /* The rectangle alays has 4 markers. */
   numberOfMarkers = 6;
   surfaceElementConnectivity.resize(numberOfMarkers);
   markerNames.resize(numberOfMarkers);
 
-  vector<unsigned long> connectivity(N_POINTS_HEXAHEDRON,0);
+  vector<unsigned long> connectivity(N_POINTS_HEXAHEDRON, 0);
 
   /* Compute and store the 6 sets of connectivity. */
 
   markerNames[0] = "x_minus";
   if (rank == MASTER_NODE) {
-    for (unsigned long kNode = 0; kNode < pNode-1; kNode++) {
-      for (unsigned long jNode = 0; jNode < mNode-1; jNode++) {
-
-        connectivity[0] = kNode*mNode*nNode + jNode*nNode;
-        connectivity[1] = (kNode + 1)*mNode*nNode + jNode*nNode;
-        connectivity[2] = (kNode + 1)*mNode*nNode + (jNode + 1)*nNode;
-        connectivity[3] = kNode*mNode*nNode + (jNode + 1)*nNode;
+    for (unsigned long kNode = 0; kNode < pNode - 1; kNode++) {
+      for (unsigned long jNode = 0; jNode < mNode - 1; jNode++) {
+        connectivity[0] = kNode * mNode * nNode + jNode * nNode;
+        connectivity[1] = (kNode + 1) * mNode * nNode + jNode * nNode;
+        connectivity[2] = (kNode + 1) * mNode * nNode + (jNode + 1) * nNode;
+        connectivity[3] = kNode * mNode * nNode + (jNode + 1) * nNode;
 
         surfaceElementConnectivity[0].push_back(0);
         surfaceElementConnectivity[0].push_back(KindBound);
         for (unsigned short i = 0; i < N_POINTS_HEXAHEDRON; i++)
-        surfaceElementConnectivity[0].push_back(connectivity[i]);
+          surfaceElementConnectivity[0].push_back(connectivity[i]);
       }
     }
   }
 
   markerNames[1] = "x_plus";
   if (rank == MASTER_NODE) {
-    for (unsigned long kNode = 0; kNode < pNode-1; kNode++) {
-      for (unsigned long jNode = 0; jNode < mNode-1; jNode++) {
-
-        connectivity[0] = kNode*mNode*nNode + jNode*nNode + (nNode - 1);
-        connectivity[1] = kNode*mNode*nNode + (jNode + 1)*nNode + (nNode - 1);
-        connectivity[2] = (kNode + 1)*mNode*nNode + (jNode + 1)*nNode + (nNode - 1);
-        connectivity[3] = (kNode + 1)*mNode*nNode + jNode*nNode + (nNode - 1);
+    for (unsigned long kNode = 0; kNode < pNode - 1; kNode++) {
+      for (unsigned long jNode = 0; jNode < mNode - 1; jNode++) {
+        connectivity[0] = kNode * mNode * nNode + jNode * nNode + (nNode - 1);
+        connectivity[1] = kNode * mNode * nNode + (jNode + 1) * nNode + (nNode - 1);
+        connectivity[2] = (kNode + 1) * mNode * nNode + (jNode + 1) * nNode + (nNode - 1);
+        connectivity[3] = (kNode + 1) * mNode * nNode + jNode * nNode + (nNode - 1);
 
         surfaceElementConnectivity[1].push_back(0);
         surfaceElementConnectivity[1].push_back(KindBound);
         for (unsigned short i = 0; i < N_POINTS_HEXAHEDRON; i++)
-        surfaceElementConnectivity[1].push_back(connectivity[i]);
+          surfaceElementConnectivity[1].push_back(connectivity[i]);
       }
     }
   }
 
   markerNames[2] = "y_minus";
   if (rank == MASTER_NODE) {
-    for (unsigned long kNode = 0; kNode < pNode-1; kNode++) {
-      for (unsigned long iNode = 0; iNode < nNode-1; iNode++) {
-
-        connectivity[0] = kNode*mNode*nNode + iNode;
-        connectivity[1] = kNode*mNode*nNode + iNode + 1;
-        connectivity[2] = (kNode + 1)*mNode*nNode + iNode + 1;
-        connectivity[3] = (kNode + 1)*mNode*nNode + iNode;
+    for (unsigned long kNode = 0; kNode < pNode - 1; kNode++) {
+      for (unsigned long iNode = 0; iNode < nNode - 1; iNode++) {
+        connectivity[0] = kNode * mNode * nNode + iNode;
+        connectivity[1] = kNode * mNode * nNode + iNode + 1;
+        connectivity[2] = (kNode + 1) * mNode * nNode + iNode + 1;
+        connectivity[3] = (kNode + 1) * mNode * nNode + iNode;
 
         surfaceElementConnectivity[2].push_back(0);
         surfaceElementConnectivity[2].push_back(KindBound);
         for (unsigned short i = 0; i < N_POINTS_HEXAHEDRON; i++)
-        surfaceElementConnectivity[2].push_back(connectivity[i]);
+          surfaceElementConnectivity[2].push_back(connectivity[i]);
       }
     }
   }
 
   markerNames[3] = "y_plus";
   if (rank == MASTER_NODE) {
-    for (unsigned long kNode = 0; kNode < pNode-1; kNode++) {
-      for (unsigned long iNode = 0; iNode < nNode-1; iNode++) {
-
-        connectivity[0] = kNode*mNode*nNode + (mNode - 1)*nNode + iNode;
-        connectivity[1] = kNode*mNode*nNode + (mNode - 1)*nNode + iNode + 1;
-        connectivity[2] = (kNode + 1)*mNode*nNode + (mNode - 1)*nNode + iNode + 1;
-        connectivity[3] = (kNode + 1)*mNode*nNode + (mNode - 1)*nNode + iNode;
+    for (unsigned long kNode = 0; kNode < pNode - 1; kNode++) {
+      for (unsigned long iNode = 0; iNode < nNode - 1; iNode++) {
+        connectivity[0] = kNode * mNode * nNode + (mNode - 1) * nNode + iNode;
+        connectivity[1] = kNode * mNode * nNode + (mNode - 1) * nNode + iNode + 1;
+        connectivity[2] = (kNode + 1) * mNode * nNode + (mNode - 1) * nNode + iNode + 1;
+        connectivity[3] = (kNode + 1) * mNode * nNode + (mNode - 1) * nNode + iNode;
 
         surfaceElementConnectivity[3].push_back(0);
         surfaceElementConnectivity[3].push_back(KindBound);
         for (unsigned short i = 0; i < N_POINTS_HEXAHEDRON; i++)
-        surfaceElementConnectivity[3].push_back(connectivity[i]);
+          surfaceElementConnectivity[3].push_back(connectivity[i]);
       }
     }
   }
 
   markerNames[4] = "z_minus";
   if (rank == MASTER_NODE) {
-    for (unsigned long jNode = 0; jNode < mNode-1; jNode++) {
-      for (unsigned long iNode = 0; iNode < nNode-1; iNode++) {
-
-        connectivity[0] = jNode*nNode + iNode;
-        connectivity[1] = jNode*nNode + iNode + 1;
-        connectivity[2] = (jNode + 1)*nNode + (iNode + 1);
-        connectivity[3] = (jNode + 1)*nNode + iNode;
+    for (unsigned long jNode = 0; jNode < mNode - 1; jNode++) {
+      for (unsigned long iNode = 0; iNode < nNode - 1; iNode++) {
+        connectivity[0] = jNode * nNode + iNode;
+        connectivity[1] = jNode * nNode + iNode + 1;
+        connectivity[2] = (jNode + 1) * nNode + (iNode + 1);
+        connectivity[3] = (jNode + 1) * nNode + iNode;
 
         surfaceElementConnectivity[4].push_back(0);
         surfaceElementConnectivity[4].push_back(KindBound);
         for (unsigned short i = 0; i < N_POINTS_HEXAHEDRON; i++)
-        surfaceElementConnectivity[4].push_back(connectivity[i]);
+          surfaceElementConnectivity[4].push_back(connectivity[i]);
       }
     }
   }
 
   markerNames[5] = "z_plus";
   if (rank == MASTER_NODE) {
-    for (unsigned long jNode = 0; jNode < mNode-1; jNode++) {
-      for (unsigned long iNode = 0; iNode < nNode-1; iNode++) {
-
-        connectivity[0] = (pNode-1)*mNode*nNode + jNode*nNode + iNode;
-        connectivity[1] = (pNode-1)*mNode*nNode + jNode*nNode + iNode + 1;
-        connectivity[2] = (pNode-1)*mNode*nNode + (jNode + 1)*nNode + (iNode + 1);
-        connectivity[3] = (pNode-1)*mNode*nNode + (jNode + 1)*nNode + iNode;
+    for (unsigned long jNode = 0; jNode < mNode - 1; jNode++) {
+      for (unsigned long iNode = 0; iNode < nNode - 1; iNode++) {
+        connectivity[0] = (pNode - 1) * mNode * nNode + jNode * nNode + iNode;
+        connectivity[1] = (pNode - 1) * mNode * nNode + jNode * nNode + iNode + 1;
+        connectivity[2] = (pNode - 1) * mNode * nNode + (jNode + 1) * nNode + (iNode + 1);
+        connectivity[3] = (pNode - 1) * mNode * nNode + (jNode + 1) * nNode + iNode;
 
         surfaceElementConnectivity[5].push_back(0);
         surfaceElementConnectivity[5].push_back(KindBound);
         for (unsigned short i = 0; i < N_POINTS_HEXAHEDRON; i++)
-        surfaceElementConnectivity[5].push_back(connectivity[i]);
+          surfaceElementConnectivity[5].push_back(connectivity[i]);
       }
     }
   }
-
 }
diff --git a/Common/src/geometry/meshreader/CCGNSMeshReaderFVM.cpp b/Common/src/geometry/meshreader/CCGNSMeshReaderFVM.cpp
index 53e3b3dd0c7..8c5019c9c53 100644
--- a/Common/src/geometry/meshreader/CCGNSMeshReaderFVM.cpp
+++ b/Common/src/geometry/meshreader/CCGNSMeshReaderFVM.cpp
@@ -29,11 +29,8 @@
 #include "../../../include/toolboxes/CLinearPartitioner.hpp"
 #include "../../../include/geometry/meshreader/CCGNSMeshReaderFVM.hpp"
 
-CCGNSMeshReaderFVM::CCGNSMeshReaderFVM(CConfig        *val_config,
-                                       unsigned short val_iZone,
-                                       unsigned short val_nZone)
-: CMeshReaderFVM(val_config, val_iZone, val_nZone) {
-
+CCGNSMeshReaderFVM::CCGNSMeshReaderFVM(CConfig* val_config, unsigned short val_iZone, unsigned short val_nZone)
+    : CMeshReaderFVM(val_config, val_iZone, val_nZone) {
 #ifdef HAVE_CGNS
   OpenCGNSFile(config->GetMesh_FileName());
 
@@ -69,26 +66,23 @@ CCGNSMeshReaderFVM::CCGNSMeshReaderFVM(CConfig        *val_config,
   ReformatCGNSSurfaceConnectivity();
 
 #else
-  SU2_MPI::Error(string(" SU2 built without CGNS support. \n") +
-                 string(" To use CGNS, build SU2 accordingly."),
+  SU2_MPI::Error(string(" SU2 built without CGNS support. \n") + string(" To use CGNS, build SU2 accordingly."),
                  CURRENT_FUNCTION);
 #endif
 }
 
-CCGNSMeshReaderFVM::~CCGNSMeshReaderFVM(void) { }
+CCGNSMeshReaderFVM::~CCGNSMeshReaderFVM(void) {}
 
 #ifdef HAVE_CGNS
 void CCGNSMeshReaderFVM::OpenCGNSFile(string val_filename) {
-
   /*--- Check whether the supplied file is truly a CGNS file. ---*/
 
   int file_type;
   float file_version;
   if (cg_is_cgns(val_filename.c_str(), &file_type) != CG_OK) {
-    SU2_MPI::Error(val_filename +
-                   string(" was not found or is not a properly formatted") +
-                   string(" CGNS file.\nNote that SU2 expects unstructured") +
-                   string(" CGNS files in ADF data format."),
+    SU2_MPI::Error(val_filename + string(" was not found or is not a properly formatted") +
+                       string(" CGNS file.\nNote that SU2 expects unstructured") +
+                       string(" CGNS files in ADF data format."),
                    CURRENT_FUNCTION);
   }
 
@@ -96,46 +90,42 @@ void CCGNSMeshReaderFVM::OpenCGNSFile(string val_filename) {
    is the specific index number for this file and will be
    repeatedly used in the function calls. ---*/
 
-  if (cg_open(val_filename.c_str(), CG_MODE_READ, &cgnsFileID))
-    cg_error_exit();
+  if (cg_open(val_filename.c_str(), CG_MODE_READ, &cgnsFileID)) cg_error_exit();
   if (rank == MASTER_NODE) {
     cout << "Reading the CGNS file: ";
     cout << val_filename.c_str() << "." << endl;
   }
-  if (cg_version(cgnsFileID, &file_version))
-    cg_error_exit();
+  if (cg_version(cgnsFileID, &file_version)) cg_error_exit();
   if (rank == MASTER_NODE) {
     if (file_version < 4.0) {
-      cout << "WARNING: The CGNS file version (" << file_version << ")  is old and may cause high memory usage issues, consider updating the file with the cgnsupdate tool.\n";
+      cout
+          << "WARNING: The CGNS file version (" << file_version
+          << ")  is old and may cause high memory usage issues, consider updating the file with the cgnsupdate tool.\n";
     }
   }
 }
 
 void CCGNSMeshReaderFVM::ReadCGNSDatabaseMetadata() {
-
   /*--- Get the number of databases. This is the highest node
    in the CGNS heirarchy. ---*/
 
   int nbases;
   if (cg_nbases(cgnsFileID, &nbases)) cg_error_exit();
-  if (rank == MASTER_NODE)
-    cout << "CGNS file contains " << nbases << " database(s)." << endl;
+  if (rank == MASTER_NODE) cout << "CGNS file contains " << nbases << " database(s)." << endl;
 
   /*--- Check if there is more than one database. Throw an
    error if there is because this reader can currently
    only handle one database. ---*/
 
-  if ( nbases > 1 ) {
-    SU2_MPI::Error("CGNS reader currently can only handle 1 database.",
-                   CURRENT_FUNCTION);
+  if (nbases > 1) {
+    SU2_MPI::Error("CGNS reader currently can only handle 1 database.", CURRENT_FUNCTION);
   }
 
   /*--- Read the database. Note that the CGNS indexing starts at 1. ---*/
 
   int cell_dim, phys_dim;
   char basename[CGNS_STRING_SIZE];
-  if (cg_base_read(cgnsFileID, cgnsBase, basename, &cell_dim, &phys_dim))
-    cg_error_exit();
+  if (cg_base_read(cgnsFileID, cgnsBase, basename, &cell_dim, &phys_dim)) cg_error_exit();
   if (rank == MASTER_NODE) {
     cout << "Database " << cgnsBase << ", " << basename << ": ";
     cout << " cell dimension of " << cell_dim << ", physical ";
@@ -145,11 +135,9 @@ void CCGNSMeshReaderFVM::ReadCGNSDatabaseMetadata() {
   /*--- Set the number of dimensions baed on cell_dim. ---*/
 
   dimension = (unsigned short)cell_dim;
-
 }
 
 void CCGNSMeshReaderFVM::ReadCGNSZoneMetadata() {
-
   /*--- First, check all sections to find the element types and to
    classify them as either surface or volume elements. We will also
    perform some error checks here to avoid partitioning issues. ---*/
@@ -159,16 +147,17 @@ void CCGNSMeshReaderFVM::ReadCGNSZoneMetadata() {
   int nzones;
   if (cg_nzones(cgnsFileID, cgnsBase, &nzones)) cg_error_exit();
   if (rank == MASTER_NODE) {
-    cout <<  nzones << " total zone(s)." << endl;
+    cout << nzones << " total zone(s)." << endl;
   }
 
   /*--- Check if there is more than one zone. Until we enable it, we
    will require a single zone CGNS file. Multizone problems can still
    be run with CGNS by using separate CGNS files for each zone. ---*/
 
-  if ( nzones > 1 ) {
+  if (nzones > 1) {
     SU2_MPI::Error(string("CGNS reader currently expects only 1 zone per CGNS file.") +
-                   string("Multizone problems can be run with separate CGNS files for each zone."), CURRENT_FUNCTION);
+                       string("Multizone problems can be run with separate CGNS files for each zone."),
+                   CURRENT_FUNCTION);
   }
 
   /*--- Read the basic information for this zone, including
@@ -178,8 +167,7 @@ void CCGNSMeshReaderFVM::ReadCGNSZoneMetadata() {
   vector<cgsize_t> cgsize(3);
   ZoneType_t zonetype;
   char zonename[CGNS_STRING_SIZE];
-  if (cg_zone_read(cgnsFileID, cgnsBase, cgnsZone, zonename, cgsize.data()))
-    cg_error_exit();
+  if (cg_zone_read(cgnsFileID, cgnsBase, cgnsZone, zonename, cgsize.data())) cg_error_exit();
 
   /*--- Rename the zone size information for clarity.
    NOTE: The number of cells here may be only the number of
@@ -187,7 +175,7 @@ void CCGNSMeshReaderFVM::ReadCGNSZoneMetadata() {
    be counted explicitly later. ---*/
 
   numberOfGlobalPoints = cgsize[0];
-  int nElemCGNS        = cgsize[1];
+  int nElemCGNS = cgsize[1];
 
   /*--- Get some additional information about the current zone. ---*/
 
@@ -196,8 +184,7 @@ void CCGNSMeshReaderFVM::ReadCGNSZoneMetadata() {
   /*--- Check for an unstructured mesh. Throw an error if not found. ---*/
 
   if (zonetype != Unstructured)
-    SU2_MPI::Error("Structured CGNS zone found while unstructured expected.",
-                   CURRENT_FUNCTION);
+    SU2_MPI::Error("Structured CGNS zone found while unstructured expected.", CURRENT_FUNCTION);
 
   /*--- Print current zone info to the console. ---*/
 
@@ -214,19 +201,16 @@ void CCGNSMeshReaderFVM::ReadCGNSZoneMetadata() {
   int ngrids;
   if (cg_ngrids(cgnsFileID, cgnsBase, cgnsZone, &ngrids)) cg_error_exit();
   if (ngrids > 1) {
-    SU2_MPI::Error("CGNS reader currently handles only 1 grid per zone.",
-                   CURRENT_FUNCTION);
+    SU2_MPI::Error("CGNS reader currently handles only 1 grid per zone.", CURRENT_FUNCTION);
   }
-
 }
 
 void CCGNSMeshReaderFVM::ReadCGNSPointCoordinates() {
-
   /*--- Compute the number of points that will be on each processor.
    This is a linear partitioning with the addition of a simple load
    balancing for any remainder points. ---*/
 
-  CLinearPartitioner pointPartitioner(numberOfGlobalPoints,0);
+  CLinearPartitioner pointPartitioner(numberOfGlobalPoints, 0);
 
   /*--- Store the local number of nodes for this rank. ---*/
 
@@ -235,21 +219,19 @@ void CCGNSMeshReaderFVM::ReadCGNSPointCoordinates() {
   /*--- Create buffer to hold the grid coordinates for our rank. ---*/
 
   localPointCoordinates.resize(dimension);
-  for (int k = 0; k < dimension; k++)
-    localPointCoordinates[k].resize(numberOfLocalPoints, 0.0);
+  for (int k = 0; k < dimension; k++) localPointCoordinates[k].resize(numberOfLocalPoints, 0.0);
 
   /*--- Set the value of range_max to the total number of nodes in
    the unstructured mesh. Also allocate memory for the temporary array
    that will hold the grid coordinates as they are extracted. Note the
    +1 for CGNS convention. ---*/
 
-  cgsize_t range_min = (cgsize_t)pointPartitioner.GetFirstIndexOnRank(rank)+1;
+  cgsize_t range_min = (cgsize_t)pointPartitioner.GetFirstIndexOnRank(rank) + 1;
   cgsize_t range_max = (cgsize_t)pointPartitioner.GetLastIndexOnRank(rank);
 
   /*--- Loop over each set of coordinates. ---*/
 
   for (int k = 0; k < dimension; k++) {
-
     /*--- Read the coordinate info. This will retrieve the
      data type (either RealSingle or RealDouble) as
      well as the coordname which will specify the
@@ -258,8 +240,7 @@ void CCGNSMeshReaderFVM::ReadCGNSPointCoordinates() {
 
     char coordname[CGNS_STRING_SIZE];
     DataType_t datatype;
-    if (cg_coord_info(cgnsFileID, cgnsBase, cgnsZone, k+1,
-                      &datatype, coordname)) cg_error_exit();
+    if (cg_coord_info(cgnsFileID, cgnsBase, cgnsZone, k + 1, &datatype, coordname)) cg_error_exit();
     if (rank == MASTER_NODE) {
       cout << "Loading " << coordname;
       if (size > SINGLE_NODE) {
@@ -272,30 +253,29 @@ void CCGNSMeshReaderFVM::ReadCGNSPointCoordinates() {
     /*--- Check the coordinate name to decide the index for storage. ---*/
 
     unsigned short indC = 0;
-    if      (string(coordname) == "CoordinateX") indC = 0;
-    else if (string(coordname) == "CoordinateY") indC = 1;
-    else if (string(coordname) == "CoordinateZ") indC = 2;
+    if (string(coordname) == "CoordinateX")
+      indC = 0;
+    else if (string(coordname) == "CoordinateY")
+      indC = 1;
+    else if (string(coordname) == "CoordinateZ")
+      indC = 2;
     else
-      SU2_MPI::Error(string("Unknown coordinate name, ") + coordname +
-                     string(", in the CGNS file."), CURRENT_FUNCTION);
+      SU2_MPI::Error(string("Unknown coordinate name, ") + coordname + string(", in the CGNS file."), CURRENT_FUNCTION);
 
     /*--- Now read our rank's chunk of coordinates from the file.
      Ask for datatype RealDouble and let CGNS library do the translation
      when RealSingle is found. ---*/
 
-    if (cg_coord_read(cgnsFileID, cgnsBase, cgnsZone, coordname, RealDouble,
-                      &range_min, &range_max, localPointCoordinates[indC].data()))
+    if (cg_coord_read(cgnsFileID, cgnsBase, cgnsZone, coordname, RealDouble, &range_min, &range_max,
+                      localPointCoordinates[indC].data()))
       cg_error_exit();
   }
-
 }
 
 void CCGNSMeshReaderFVM::ReadCGNSSectionMetadata() {
-
   /*--- Begin section for retrieving the connectivity info. ---*/
 
-  if ((rank == MASTER_NODE) && (size > SINGLE_NODE))
-    cout << "Distributing connectivity across all ranks." << endl;
+  if ((rank == MASTER_NODE) && (size > SINGLE_NODE)) cout << "Distributing connectivity across all ranks." << endl;
 
   /*--- First check the number of sections. ---*/
 
@@ -309,26 +289,26 @@ void CCGNSMeshReaderFVM::ReadCGNSSectionMetadata() {
    pieces of information describing each section. ---*/
 
   isInterior.resize(nSections);
-  nElems.resize(nSections,0);
-  elemOffset.resize(nSections+1, 0); elemOffset[0] = 0;
+  nElems.resize(nSections, 0);
+  elemOffset.resize(nSections + 1, 0);
+  elemOffset[0] = 0;
   connElems.resize(nSections);
   sectionNames.resize(nSections, vector<char>(CGNS_STRING_SIZE));
   numberOfGlobalElements = 0;
 
   for (int s = 0; s < nSections; s++) {
-
     /*--- Read the connectivity details for this section. ---*/
 
     int nbndry, parent_flag, vtk_type;
     cgsize_t startE, endE, sizeNeeded;
     ElementType_t elemType;
-    if (cg_section_read(cgnsFileID, cgnsBase, cgnsZone, s+1,
-                        sectionNames[s].data(), &elemType, &startE, &endE,
-                        &nbndry, &parent_flag)) cg_error_exit();
+    if (cg_section_read(cgnsFileID, cgnsBase, cgnsZone, s + 1, sectionNames[s].data(), &elemType, &startE, &endE,
+                        &nbndry, &parent_flag))
+      cg_error_exit();
 
     /*--- Compute the total element count in this section (global). ---*/
 
-    unsigned long element_count = (endE-startE+1);
+    unsigned long element_count = (endE - startE + 1);
 
     /* Get the details for the CGNS element type in this section. */
 
@@ -343,26 +323,23 @@ void CCGNSMeshReaderFVM::ReadCGNSSectionMetadata() {
     isInterior[s] = true;
 
     if (elemType == MIXED) {
-
       /* For a mixed section, we check the type of the first element
        so that we can correctly label this section as an interior or
        boundary element section. Here, we also assume that a section
        can not hold both interior and boundary elements. First, get
        the size required to read a single element from the section. */
 
-      if (cg_ElementPartialSize(cgnsFileID, cgnsBase, cgnsZone, s+1, startE,
-                                startE, &sizeNeeded) != CG_OK)
+      if (cg_ElementPartialSize(cgnsFileID, cgnsBase, cgnsZone, s + 1, startE, startE, &sizeNeeded) != CG_OK)
         cg_error_exit();
 
       /* A couple of auxiliary vectors for mixed element sections. */
 
       vector<cgsize_t> connElemCGNS(sizeNeeded);
-      vector<cgsize_t> connOffsetCGNS(2,0);
+      vector<cgsize_t> connOffsetCGNS(2, 0);
 
       /* Retrieve the connectivity information for the first element. */
 
-      if (cg_poly_elements_partial_read(cgnsFileID, cgnsBase, cgnsZone, s+1,
-                                        startE, startE, connElemCGNS.data(),
+      if (cg_poly_elements_partial_read(cgnsFileID, cgnsBase, cgnsZone, s + 1, startE, startE, connElemCGNS.data(),
                                         connOffsetCGNS.data(), NULL) != CG_OK)
         cg_error_exit();
 
@@ -370,39 +347,35 @@ void CCGNSMeshReaderFVM::ReadCGNSSectionMetadata() {
        information that we retrieved from the CGNS file. */
 
       elemType = ElementType_t(connElemCGNS[0]);
-
     }
 
     /* Check for 1D elements in 2D problems, or for 2D elements in
      3D problems. If found, mark the section as a boundary section. */
 
-    if ((dimension == 2) &&
-        (elemType == BAR_2 || elemType == BAR_3))  isInterior[s] = false;
-    if ((dimension == 3) &&
-        (elemType == TRI_3 || elemType == QUAD_4)) isInterior[s] = false;
+    if ((dimension == 2) && (elemType == BAR_2 || elemType == BAR_3)) isInterior[s] = false;
+    if ((dimension == 3) && (elemType == TRI_3 || elemType == QUAD_4)) isInterior[s] = false;
 
     /*--- Increment the global element offset for each section
      based on whether or not this is a surface or volume section.
      We also keep a running count of the total elements globally. ---*/
 
-    elemOffset[s+1] = elemOffset[s];
-    if (!isInterior[s]) elemOffset[s+1] += element_count;
-    else numberOfGlobalElements += element_count;
+    elemOffset[s + 1] = elemOffset[s];
+    if (!isInterior[s])
+      elemOffset[s + 1] += element_count;
+    else
+      numberOfGlobalElements += element_count;
 
     /*--- Print some information to the console. ---*/
 
     if (rank == MASTER_NODE) {
       cout << "Section " << string(sectionNames[s].data());
       cout << " contains " << element_count << " elements";
-      cout << " of type " << elem_name << "." <<endl;
+      cout << " of type " << elem_name << "." << endl;
     }
-
   }
-
 }
 
 void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
-
   /*--- In this routine, each rank will read a chunk of the element
    connectivity for a single specified section of the CGNS mesh file.
    All operations are executed in parallel here and the reading of the
@@ -423,14 +396,14 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
    Store the total number of elements in this section
    to be used later for memory allocation. ---*/
 
-  if (cg_section_read(cgnsFileID, cgnsBase, cgnsZone, val_section+1, sectionName,
-                      &elemType, &startE, &endE, &nbndry, &parent_flag))
+  if (cg_section_read(cgnsFileID, cgnsBase, cgnsZone, val_section + 1, sectionName, &elemType, &startE, &endE, &nbndry,
+                      &parent_flag))
     cg_error_exit();
 
   /*--- Compute element linear partitioning ---*/
 
-  unsigned long element_count = (endE-startE+1);
-  CLinearPartitioner elementPartitioner(element_count,startE,true);
+  unsigned long element_count = (endE - startE + 1);
+  CLinearPartitioner elementPartitioner(element_count, startE, true);
 
   /*--- Store the number of elements that this rank is responsible for
    in the current section. ---*/
@@ -440,9 +413,9 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
   /*--- Allocate some memory for the handling the connectivity
    and auxiliary data that we need to communicate. ---*/
 
-  vector<cgsize_t> elemTypes(nElems[val_section],   0);
-  vector<cgsize_t> nPoinPerElem(nElems[val_section],0);
-  vector<cgsize_t> elemGlobalID(nElems[val_section],0);
+  vector<cgsize_t> elemTypes(nElems[val_section], 0);
+  vector<cgsize_t> nPoinPerElem(nElems[val_section], 0);
+  vector<cgsize_t> elemGlobalID(nElems[val_section], 0);
 
   /*--- Determine the size of the vector needed to read the connectivity
    data from the CGNS file. Only call the CGNS API if we have a non-zero
@@ -450,21 +423,20 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
 
   cgsize_t sizeNeeded = 0, sizeOffset = 0;
   if (nElems[val_section] > 0) {
-    if (cg_ElementPartialSize(cgnsFileID, cgnsBase, cgnsZone, val_section+1,
+    if (cg_ElementPartialSize(cgnsFileID, cgnsBase, cgnsZone, val_section + 1,
                               (cgsize_t)elementPartitioner.GetFirstIndexOnRank(rank),
-                              (cgsize_t)elementPartitioner.GetLastIndexOnRank(rank),
-                              &sizeNeeded) != CG_OK)
-    cg_error_exit();
+                              (cgsize_t)elementPartitioner.GetLastIndexOnRank(rank), &sizeNeeded) != CG_OK)
+      cg_error_exit();
   }
 
   /*--- Allocate the memory for the connectivity, the offset if needed
    and read the data. ---*/
 
-  vector<cgsize_t> connElemCGNS(sizeNeeded,0);
+  vector<cgsize_t> connElemCGNS(sizeNeeded, 0);
   if (elemType == MIXED || elemType == NFACE_n || elemType == NGON_n) {
-    sizeOffset = nElems[val_section]+1;
+    sizeOffset = nElems[val_section] + 1;
   }
-  vector<cgsize_t> connOffsetCGNS(sizeOffset,0);
+  vector<cgsize_t> connOffsetCGNS(sizeOffset, 0);
 
   /*--- Retrieve the connectivity information and store. Note that
    we are only accessing our rank's piece of the data here in the
@@ -473,18 +445,16 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
 
   if (nElems[val_section] > 0) {
     if (elemType == MIXED || elemType == NFACE_n || elemType == NGON_n) {
-      if (cg_poly_elements_partial_read(cgnsFileID, cgnsBase, cgnsZone, val_section+1,
+      if (cg_poly_elements_partial_read(cgnsFileID, cgnsBase, cgnsZone, val_section + 1,
                                         (cgsize_t)elementPartitioner.GetFirstIndexOnRank(rank),
-                                        (cgsize_t)elementPartitioner.GetLastIndexOnRank(rank),
-                                        connElemCGNS.data(),
+                                        (cgsize_t)elementPartitioner.GetLastIndexOnRank(rank), connElemCGNS.data(),
                                         connOffsetCGNS.data(), NULL) != CG_OK)
-      cg_error_exit();
+        cg_error_exit();
     } else {
-      if (cg_elements_partial_read(cgnsFileID, cgnsBase, cgnsZone, val_section+1,
-                                   (cgsize_t)elementPartitioner.GetFirstIndexOnRank(rank),
-                                   (cgsize_t)elementPartitioner.GetLastIndexOnRank(rank),
-                                   connElemCGNS.data(), NULL) != CG_OK)
-      cg_error_exit();
+      if (cg_elements_partial_read(
+              cgnsFileID, cgnsBase, cgnsZone, val_section + 1, (cgsize_t)elementPartitioner.GetFirstIndexOnRank(rank),
+              (cgsize_t)elementPartitioner.GetLastIndexOnRank(rank), connElemCGNS.data(), NULL) != CG_OK)
+        cg_error_exit();
     }
   }
 
@@ -492,7 +462,7 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
 
   if (rank == MASTER_NODE) {
     cout << "Loading volume section " << string(sectionName);
-    cout <<  " from file." << endl;
+    cout << " from file." << endl;
   }
 
   /*--- Find the number of nodes required to represent
@@ -514,7 +484,6 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
 
   unsigned long counterCGNS = 0;
   for (iElem = 0; iElem < nElems[val_section]; iElem++) {
-
     ElementType_t iElemType = elemType;
 
     /*--- If we have a mixed element section, we need to check the elem
@@ -523,7 +492,7 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
 
     if (isMixed) {
       iElemType = ElementType_t(connElemCGNS[counterCGNS]);
-      npe       = connOffsetCGNS[iElem+1]-connOffsetCGNS[iElem]-1;
+      npe = connOffsetCGNS[iElem + 1] - connOffsetCGNS[iElem] - 1;
       counterCGNS++;
       for (int jj = 0; jj < npe; jj++) counterCGNS++;
     }
@@ -538,15 +507,13 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
      prior to this one, in order to keep the internal element global
      IDs indexed starting from zero. ---*/
 
-    elemGlobalID[iElem] = (elementPartitioner.GetFirstIndexOnRank(rank) +
-                           iElem - elemOffset[val_section]);
+    elemGlobalID[iElem] = (elementPartitioner.GetFirstIndexOnRank(rank) + iElem - elemOffset[val_section]);
 
     /* Get the VTK type for this element. */
 
     int vtk_type;
     string elem_name = GetCGNSElementType(iElemType, vtk_type);
     elemTypes[iElem] = vtk_type;
-
   }
 
   /*--- Force free the memory for the conn offset from the CGNS file. ---*/
@@ -555,22 +522,23 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
 
   /*--- These are internal elems. Allocate memory on each proc. ---*/
 
-  vector<cgsize_t> connElemTemp(nElems[val_section]*SU2_CONN_SIZE,0);
+  vector<cgsize_t> connElemTemp(nElems[val_section] * SU2_CONN_SIZE, 0);
 
   /*--- Copy the connectivity into the larger array with a standard
    format per element: [globalID vtkType n0 n1 n2 n3 n4 n5 n6 n7 n8]. ---*/
 
   counterCGNS = 0;
   for (iElem = 0; iElem < nElems[val_section]; iElem++) {
-
     /*--- Store the conn in chunks of SU2_CONN_SIZE for simplicity. ---*/
 
-    unsigned long nn = iElem*SU2_CONN_SIZE;
+    unsigned long nn = iElem * SU2_CONN_SIZE;
 
     /*--- First, store the global element ID and the VTK type. ---*/
 
-    connElemTemp[nn] = elemGlobalID[iElem]; nn++;
-    connElemTemp[nn] = elemTypes[iElem];    nn++;
+    connElemTemp[nn] = elemGlobalID[iElem];
+    nn++;
+    connElemTemp[nn] = elemTypes[iElem];
+    nn++;
 
     /*--- Store the connectivity values. Note we subtract one from
      the CGNS 1-based convention. We may also need to remove the first
@@ -578,10 +546,10 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
 
     if (isMixed) counterCGNS++;
     for (iNode = 0; iNode < (unsigned long)nPoinPerElem[iElem]; iNode++) {
-      connElemTemp[nn] = connElemCGNS[counterCGNS + iNode] - 1; nn++;
+      connElemTemp[nn] = connElemCGNS[counterCGNS + iNode] - 1;
+      nn++;
     }
     counterCGNS += nPoinPerElem[iElem];
-
   }
 
   /*--- Force free the memory for the conn from the CGNS file. ---*/
@@ -595,28 +563,29 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
    will appear on multiple ranks). First, initialize a counter
    and flag. ---*/
 
-  int *nElem_Send = new int[size+1]; nElem_Send[0] = 0;
-  int *nElem_Recv = new int[size+1]; nElem_Recv[0] = 0;
-  int *nElem_Flag = new int[size];
+  int* nElem_Send = new int[size + 1];
+  nElem_Send[0] = 0;
+  int* nElem_Recv = new int[size + 1];
+  nElem_Recv[0] = 0;
+  int* nElem_Flag = new int[size];
 
   for (iProcessor = 0; iProcessor < size; iProcessor++) {
     nElem_Send[iProcessor] = 0;
     nElem_Recv[iProcessor] = 0;
-    nElem_Flag[iProcessor]= -1;
+    nElem_Flag[iProcessor] = -1;
   }
   nElem_Send[size] = 0;
   nElem_Recv[size] = 0;
 
   /*--- Create a partitioner object to find the owning rank of points. ---*/
 
-  CLinearPartitioner pointPartitioner(numberOfGlobalPoints,0);
+  CLinearPartitioner pointPartitioner(numberOfGlobalPoints, 0);
 
   for (iElem = 0; iElem < nElems[val_section]; iElem++) {
     for (iNode = 0; iNode < (unsigned long)nPoinPerElem[iElem]; iNode++) {
-
       /*--- Get the index of the current point. ---*/
 
-      iPoint = connElemTemp[iElem*SU2_CONN_SIZE + SU2_CONN_SKIP + iNode];
+      iPoint = connElemTemp[iElem * SU2_CONN_SIZE + SU2_CONN_SKIP + iNode];
 
       /*--- Search for the processor that owns this point. ---*/
 
@@ -627,9 +596,8 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
 
       if ((nElem_Flag[iProcessor] != (int)iElem)) {
         nElem_Flag[iProcessor] = iElem;
-        nElem_Send[iProcessor+1]++;
+        nElem_Send[iProcessor + 1]++;
       }
-
     }
   }
 
@@ -637,8 +605,7 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
    all processors. After this communication, each proc knows how
    many cells it will receive from each other processor. ---*/
 
-  SU2_MPI::Alltoall(&(nElem_Send[1]), 1, MPI_INT,
-                    &(nElem_Recv[1]), 1, MPI_INT, SU2_MPI::GetComm());
+  SU2_MPI::Alltoall(&(nElem_Send[1]), 1, MPI_INT, &(nElem_Recv[1]), 1, MPI_INT, SU2_MPI::GetComm());
 
   /*--- Prepare to send connectivities. First check how many
    messages we will be sending and receiving. Here we also put
@@ -646,15 +613,14 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
    communications simpler. ---*/
 
   unsigned long nSends = 0, nRecvs = 0;
-  for (iProcessor = 0; iProcessor < size; iProcessor++)
-    nElem_Flag[iProcessor] = -1;
+  for (iProcessor = 0; iProcessor < size; iProcessor++) nElem_Flag[iProcessor] = -1;
 
   for (iProcessor = 0; iProcessor < size; iProcessor++) {
-    if ((iProcessor != rank) && (nElem_Send[iProcessor+1] > 0)) nSends++;
-    if ((iProcessor != rank) && (nElem_Recv[iProcessor+1] > 0)) nRecvs++;
+    if ((iProcessor != rank) && (nElem_Send[iProcessor + 1] > 0)) nSends++;
+    if ((iProcessor != rank) && (nElem_Recv[iProcessor + 1] > 0)) nRecvs++;
 
-    nElem_Send[iProcessor+1] += nElem_Send[iProcessor];
-    nElem_Recv[iProcessor+1] += nElem_Recv[iProcessor];
+    nElem_Send[iProcessor + 1] += nElem_Send[iProcessor];
+    nElem_Recv[iProcessor + 1] += nElem_Recv[iProcessor];
   }
 
   /*--- Allocate memory to hold the connectivity that we are
@@ -664,27 +630,24 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
    + 2 extra values for the ID and VTK. ---*/
 
   unsigned long *connSend = NULL, iSend = 0;
-  unsigned long sendSize = (unsigned long)SU2_CONN_SIZE*nElem_Send[size];
+  unsigned long sendSize = (unsigned long)SU2_CONN_SIZE * nElem_Send[size];
   connSend = new unsigned long[sendSize];
-  for (iSend = 0; iSend < sendSize; iSend++)
-    connSend[iSend] = 0;
+  for (iSend = 0; iSend < sendSize; iSend++) connSend[iSend] = 0;
 
   /*--- Create an index variable to keep track of our index
    position as we load up the send buffer. ---*/
 
   vector<unsigned long> index(size);
-  for (iProcessor = 0; iProcessor < size; iProcessor++)
-    index[iProcessor] = SU2_CONN_SIZE*nElem_Send[iProcessor];
+  for (iProcessor = 0; iProcessor < size; iProcessor++) index[iProcessor] = SU2_CONN_SIZE * nElem_Send[iProcessor];
 
   /*--- Loop through our elements and load the elems and their
    additional data that we will send to the other procs. ---*/
 
   for (iElem = 0; iElem < (unsigned long)nElems[val_section]; iElem++) {
     for (iNode = 0; iNode < (unsigned long)nPoinPerElem[iElem]; iNode++) {
-
       /*--- Get the index of the current point. ---*/
 
-      iPoint = connElemTemp[iElem*SU2_CONN_SIZE + SU2_CONN_SKIP + iNode];
+      iPoint = connElemTemp[iElem * SU2_CONN_SIZE + SU2_CONN_SKIP + iNode];
 
       /*--- Search for the processor that owns this point ---*/
 
@@ -693,7 +656,6 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
       /*--- Load connectivity into the buffer for sending ---*/
 
       if (nElem_Flag[iProcessor] != (int)iElem) {
-
         nElem_Flag[iProcessor] = iElem;
         unsigned long nn = index[iProcessor];
 
@@ -701,15 +663,14 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
          then the connectivity vals, and last, the global ID. ---*/
 
         for (jNode = 0; jNode < SU2_CONN_SIZE; jNode++) {
-          connSend[nn] = connElemTemp[iElem*SU2_CONN_SIZE + jNode]; nn++;
+          connSend[nn] = connElemTemp[iElem * SU2_CONN_SIZE + jNode];
+          nn++;
         }
 
         /*--- Increment the index by the message length ---*/
 
         index[iProcessor] += SU2_CONN_SIZE;
-
       }
-
     }
   }
 
@@ -728,15 +689,14 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
    directly copy our own data later. ---*/
 
   unsigned long *connRecv = NULL, iRecv = 0;
-  unsigned long recvSize = (unsigned long)SU2_CONN_SIZE*nElem_Recv[size];
+  unsigned long recvSize = (unsigned long)SU2_CONN_SIZE * nElem_Recv[size];
   connRecv = new unsigned long[recvSize];
-  for (iRecv = 0; iRecv < recvSize; iRecv++)
-    connRecv[iRecv] = 0;
+  for (iRecv = 0; iRecv < recvSize; iRecv++) connRecv[iRecv] = 0;
 
   /*--- Allocate memory for the MPI requests if we will communicate. ---*/
 
-  SU2_MPI::Request *connSendReq = NULL;
-  SU2_MPI::Request *connRecvReq = NULL;
+  SU2_MPI::Request* connSendReq = NULL;
+  SU2_MPI::Request* connRecvReq = NULL;
 
   if (nSends > 0) {
     connSendReq = new SU2_MPI::Request[nSends];
@@ -747,15 +707,14 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
 
   /*--- Launch the non-blocking sends and receives. ---*/
 
-  InitiateCommsAll(connSend, nElem_Send, connSendReq,
-                   connRecv, nElem_Recv, connRecvReq,
-                   SU2_CONN_SIZE, COMM_TYPE_UNSIGNED_LONG);
+  InitiateCommsAll(connSend, nElem_Send, connSendReq, connRecv, nElem_Recv, connRecvReq, SU2_CONN_SIZE,
+                   COMM_TYPE_UNSIGNED_LONG);
 
   /*--- Copy the current rank's data into the recv buffer directly. ---*/
 
-  iRecv = SU2_CONN_SIZE*nElem_Recv[rank];
-  unsigned long myStart = SU2_CONN_SIZE*nElem_Send[rank];
-  unsigned long myFinal = SU2_CONN_SIZE*nElem_Send[rank+1];
+  iRecv = SU2_CONN_SIZE * nElem_Recv[rank];
+  unsigned long myStart = SU2_CONN_SIZE * nElem_Send[rank];
+  unsigned long myFinal = SU2_CONN_SIZE * nElem_Send[rank + 1];
   for (iSend = myStart; iSend < myFinal; iSend++) {
     connRecv[iRecv] = connSend[iSend];
     iRecv++;
@@ -770,11 +729,11 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
    for this section, then write the recv'd values. ---*/
 
   if (nElem_Recv[size] > 0) {
-    connElems[val_section].resize(nElem_Recv[size]*SU2_CONN_SIZE,0);
+    connElems[val_section].resize(nElem_Recv[size] * SU2_CONN_SIZE, 0);
     unsigned long count = 0;
     for (iElem = 0; iElem < (unsigned long)nElem_Recv[size]; iElem++) {
       for (iNode = 0; iNode < SU2_CONN_SIZE; iNode++) {
-        unsigned long nn = iElem*SU2_CONN_SIZE+iNode;
+        unsigned long nn = iElem * SU2_CONN_SIZE + iNode;
         connElems[val_section][count] = (cgsize_t)connRecv[nn];
         count++;
       }
@@ -786,30 +745,26 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
     nElems[val_section] = nElem_Recv[size];
 
   } else {
-
     /*--- The current rank did not recv any elements from this
      section. Set the count to zero and nullify the data structure. ---*/
 
-    nElems[val_section]    = 0;
+    nElems[val_section] = 0;
     connElems[val_section].resize(0);
-
   }
 
   /*--- Free temporary memory from communications ---*/
 
-  if (connSendReq != NULL) delete [] connSendReq;
-  if (connRecvReq != NULL) delete [] connRecvReq;
-
-  delete [] connSend;
-  delete [] connRecv;
-  delete [] nElem_Recv;
-  delete [] nElem_Send;
-  delete [] nElem_Flag;
+  if (connSendReq != NULL) delete[] connSendReq;
+  if (connRecvReq != NULL) delete[] connRecvReq;
 
+  delete[] connSend;
+  delete[] connRecv;
+  delete[] nElem_Recv;
+  delete[] nElem_Send;
+  delete[] nElem_Flag;
 }
 
 void CCGNSMeshReaderFVM::ReadCGNSSurfaceSection(int val_section) {
-
   /*--- In this routine, we access a CGNS surface section and have the
    master rank load all of the surface conn. This can help avoid issues
    where there are fewer elements than ranks on a surface. This is later
@@ -825,37 +780,33 @@ void CCGNSMeshReaderFVM::ReadCGNSSurfaceSection(int val_section) {
   char sectionName[CGNS_STRING_SIZE];
 
   if (rank == MASTER_NODE) {
-
     /*--- Allocate some memory for the handling the connectivity
      and auxiliary data that we are need to communicate. ---*/
 
-    vector<cgsize_t> connElemCGNS(nElems[val_section]*SU2_CONN_SIZE,0);
-    vector<unsigned short> elemTypes(nElems[val_section],0);
-    vector<unsigned short> nPoinPerElem(nElems[val_section],0);
-    vector<unsigned long>  elemGlobalID(nElems[val_section],0);
+    vector<cgsize_t> connElemCGNS(nElems[val_section] * SU2_CONN_SIZE, 0);
+    vector<unsigned short> elemTypes(nElems[val_section], 0);
+    vector<unsigned short> nPoinPerElem(nElems[val_section], 0);
+    vector<unsigned long> elemGlobalID(nElems[val_section], 0);
 
     /*--- Read the section info again ---*/
 
-    if (cg_section_read(cgnsFileID, cgnsBase, cgnsZone, val_section+1,
-                        sectionName, &elemType, &startE, &endE, &nbndry,
-                        &parent_flag))
+    if (cg_section_read(cgnsFileID, cgnsBase, cgnsZone, val_section + 1, sectionName, &elemType, &startE, &endE,
+                        &nbndry, &parent_flag))
       cg_error_exit();
 
     /*--- Print some information to the console. ---*/
 
     cout << "Loading surface section " << string(sectionName);
-    cout <<  " from file." << endl;
+    cout << " from file." << endl;
 
     /*--- Store the number of elems (all on the master). ---*/
 
-    nElems[val_section] = (endE-startE+1);
+    nElems[val_section] = (endE - startE + 1);
 
     /*--- Read and store the total amount of data that will be
      listed when reading this section. ---*/
 
-    if (cg_ElementDataSize(cgnsFileID, cgnsBase, cgnsZone, val_section+1,
-                           &ElementDataSize))
-      cg_error_exit();
+    if (cg_ElementDataSize(cgnsFileID, cgnsBase, cgnsZone, val_section + 1, &ElementDataSize)) cg_error_exit();
 
     /*--- Find the number of nodes required to represent
      this type of element. ---*/
@@ -874,31 +825,26 @@ void CCGNSMeshReaderFVM::ReadCGNSSurfaceSection(int val_section) {
     /*--- Allocate memory for accessing the connectivity and to
      store it in the proper data structure for post-processing. ---*/
 
-    vector<cgsize_t> connElemTemp(ElementDataSize,0);
+    vector<cgsize_t> connElemTemp(ElementDataSize, 0);
 
     /*--- Retrieve the connectivity information and store. ---*/
 
     if (elemType == MIXED || elemType == NGON_n || elemType == NFACE_n) {
-      vector<cgsize_t> connOffsetTemp(nElems[val_section]+1, 0);
-      if (cg_poly_elements_partial_read(cgnsFileID, cgnsBase, cgnsZone,
-                                        val_section+1, startE, endE,
-                                        connElemTemp.data(),
-                                        connOffsetTemp.data(), NULL) != CG_OK)
+      vector<cgsize_t> connOffsetTemp(nElems[val_section] + 1, 0);
+      if (cg_poly_elements_partial_read(cgnsFileID, cgnsBase, cgnsZone, val_section + 1, startE, endE,
+                                        connElemTemp.data(), connOffsetTemp.data(), NULL) != CG_OK)
         cg_error_exit();
     } else {
-      if (cg_elements_read(cgnsFileID, cgnsBase, cgnsZone, val_section+1,
-                           connElemTemp.data(), NULL))
-        cg_error_exit();
+      if (cg_elements_read(cgnsFileID, cgnsBase, cgnsZone, val_section + 1, connElemTemp.data(), NULL)) cg_error_exit();
     }
 
     /*--- Allocate the memory for the data structure used to carry
      the connectivity for this section. ---*/
 
-    connElems[val_section].resize(nElems[val_section]*SU2_CONN_SIZE,0);
+    connElems[val_section].resize(nElems[val_section] * SU2_CONN_SIZE, 0);
 
     unsigned long counterCGNS = 0;
     for (iElem = 0; iElem < nElems[val_section]; iElem++) {
-
       ElementType_t iElemType = elemType;
 
       /*--- If we have a mixed element section, we need to check the elem
@@ -925,29 +871,24 @@ void CCGNSMeshReaderFVM::ReadCGNSSurfaceSection(int val_section) {
        format as the interior elements. Note that we subtract 1 to
        move from the CGNS 1-based indexing to SU2's zero-based. ---*/
 
-      connElems[val_section][iElem*SU2_CONN_SIZE+0] = 0;
-      connElems[val_section][iElem*SU2_CONN_SIZE+1] = vtk_type;
+      connElems[val_section][iElem * SU2_CONN_SIZE + 0] = 0;
+      connElems[val_section][iElem * SU2_CONN_SIZE + 1] = vtk_type;
       for (iNode = 0; iNode < (unsigned long)npe; iNode++) {
-        unsigned long nn = iElem*SU2_CONN_SIZE+SU2_CONN_SKIP+iNode;
+        unsigned long nn = iElem * SU2_CONN_SIZE + SU2_CONN_SKIP + iNode;
         connElems[val_section][nn] = connElemTemp[counterCGNS] - 1;
         counterCGNS++;
       }
-
     }
 
   } else {
-
     /*--- We are not the master, so we resize to zero for safety. ---*/
 
     nElems[val_section] = 0;
     connElems[val_section].resize(0);
-
   }
-
 }
 
 void CCGNSMeshReaderFVM::ReformatCGNSVolumeConnectivity() {
-
   /*--- Loop to store total number of elements we have locally.
    This number includes repeats across ranks due to redistribution
    according to the linear partitioning of the grid nodes. ---*/
@@ -958,13 +899,13 @@ void CCGNSMeshReaderFVM::ReformatCGNSVolumeConnectivity() {
 
   /* Put our CGNS data into the class data structures for the mesh reader */
 
-  localVolumeElementConnectivity.resize(numberOfLocalElements*SU2_CONN_SIZE);
+  localVolumeElementConnectivity.resize(numberOfLocalElements * SU2_CONN_SIZE);
   unsigned long count = 0;
   for (int s = 0; s < nSections; s++) {
     if (isInterior[s]) {
       for (unsigned long iElem = 0; iElem < nElems[s]; iElem++) {
         for (unsigned long iNode = 0; iNode < SU2_CONN_SIZE; iNode++) {
-          unsigned long nn = iElem*SU2_CONN_SIZE+iNode;
+          unsigned long nn = iElem * SU2_CONN_SIZE + iNode;
           localVolumeElementConnectivity[count] = (unsigned long)connElems[s][nn];
           count++;
         }
@@ -972,37 +913,33 @@ void CCGNSMeshReaderFVM::ReformatCGNSVolumeConnectivity() {
       vector<cgsize_t>().swap(connElems[s]);
     }
   }
-
 }
 
 void CCGNSMeshReaderFVM::ReformatCGNSSurfaceConnectivity() {
-
   /*--- Prepare the class data for the marker names and connectivity. ---*/
 
   markerNames.resize(numberOfMarkers);
   surfaceElementConnectivity.resize(numberOfMarkers);
 
-  int markerCount  = 0;
+  int markerCount = 0;
   int elementCount = 0;
   for (int s = 0; s < nSections; s++) {
     if (!isInterior[s]) {
-
       /*--- Store the tag for this marker. Remove any whitespaces from
        the marker names found in the CGNS file to avoid any issues. ---*/
 
       string Marker_Tag = string(sectionNames[s].data());
-      Marker_Tag.erase(remove(Marker_Tag.begin(), Marker_Tag.end(),' '),
-                       Marker_Tag.end());
+      Marker_Tag.erase(remove(Marker_Tag.begin(), Marker_Tag.end(), ' '), Marker_Tag.end());
       markerNames[markerCount] = Marker_Tag;
 
       /*--- The master node alone stores the connectivity. ---*/
 
       if (rank == MASTER_NODE) {
-        surfaceElementConnectivity[markerCount].resize(nElems[s]*SU2_CONN_SIZE);
+        surfaceElementConnectivity[markerCount].resize(nElems[s] * SU2_CONN_SIZE);
         elementCount = 0;
         for (unsigned long iElem = 0; iElem < nElems[s]; iElem++) {
           for (unsigned long iNode = 0; iNode < SU2_CONN_SIZE; iNode++) {
-            unsigned long nn = iElem*SU2_CONN_SIZE+iNode;
+            unsigned long nn = iElem * SU2_CONN_SIZE + iNode;
             surfaceElementConnectivity[markerCount][elementCount] = (unsigned long)connElems[s][nn];
             elementCount++;
           }
@@ -1012,87 +949,71 @@ void CCGNSMeshReaderFVM::ReformatCGNSSurfaceConnectivity() {
       markerCount++;
     }
   }
-
 }
 
-string CCGNSMeshReaderFVM::GetCGNSElementType(ElementType_t val_elem_type,
-                                              int           &val_vtk_type) {
-
+string CCGNSMeshReaderFVM::GetCGNSElementType(ElementType_t val_elem_type, int& val_vtk_type) {
   /* Check the CGNS element type and return the string name
    for the element and the associated VTK type index. */
 
   string elem_name;
   switch (val_elem_type) {
     case NODE:
-      elem_name      = "Vertex";
-      val_vtk_type   = 1;
-      SU2_MPI::Error("Vertex elements detected. Please remove.",
-                     CURRENT_FUNCTION);
+      elem_name = "Vertex";
+      val_vtk_type = 1;
+      SU2_MPI::Error("Vertex elements detected. Please remove.", CURRENT_FUNCTION);
       break;
     case BAR_2:
-      elem_name     = "Line";
-      val_vtk_type  = 3;
-      if (dimension == 3)
-        SU2_MPI::Error("Line elements detected in a 3D mesh. Please remove.",
-                       CURRENT_FUNCTION);
+      elem_name = "Line";
+      val_vtk_type = 3;
+      if (dimension == 3) SU2_MPI::Error("Line elements detected in a 3D mesh. Please remove.", CURRENT_FUNCTION);
       break;
     case BAR_3:
-      elem_name     = "Line";
-      val_vtk_type  = 3;
-      if (dimension == 3)
-        SU2_MPI::Error("Line elements detected in a 3D mesh. Please remove.",
-                       CURRENT_FUNCTION);
+      elem_name = "Line";
+      val_vtk_type = 3;
+      if (dimension == 3) SU2_MPI::Error("Line elements detected in a 3D mesh. Please remove.", CURRENT_FUNCTION);
       break;
     case TRI_3:
-      elem_name     = "Triangle";
-      val_vtk_type  = 5;
+      elem_name = "Triangle";
+      val_vtk_type = 5;
       break;
     case QUAD_4:
-      elem_name     = "Quadrilateral";
-      val_vtk_type  = 9;
+      elem_name = "Quadrilateral";
+      val_vtk_type = 9;
       break;
     case TETRA_4:
-      elem_name     = "Tetrahedron";
-      val_vtk_type  = 10;
+      elem_name = "Tetrahedron";
+      val_vtk_type = 10;
       break;
     case HEXA_8:
-      elem_name     = "Hexahedron";
-      val_vtk_type  = 12;
+      elem_name = "Hexahedron";
+      val_vtk_type = 12;
       break;
     case PENTA_6:
-      elem_name     = "Prism";
-      val_vtk_type  = 13;
+      elem_name = "Prism";
+      val_vtk_type = 13;
       break;
     case PYRA_5:
-      elem_name     = "Pyramid";
-      val_vtk_type  = 14;
+      elem_name = "Pyramid";
+      val_vtk_type = 14;
       break;
     case MIXED:
-      elem_name     = "Mixed";
-      val_vtk_type  = -1;
+      elem_name = "Mixed";
+      val_vtk_type = -1;
       break;
     default:
       char buf[100];
-      SPRINTF(buf, "Unsupported or unknown CGNS element type: (type %d)\n",
-              val_elem_type);
+      SPRINTF(buf, "Unsupported or unknown CGNS element type: (type %d)\n", val_elem_type);
       SU2_MPI::Error(string(buf), CURRENT_FUNCTION);
       break;
   }
 
   return elem_name;
-
 }
 #endif
 
-void CCGNSMeshReaderFVM::InitiateCommsAll(void *bufSend,
-                                          const int *nElemSend,
-                                          SU2_MPI::Request *sendReq,
-                                          void *bufRecv,
-                                          const int *nElemRecv,
-                                          SU2_MPI::Request *recvReq,
-                                          unsigned short countPerElem,
+void CCGNSMeshReaderFVM::InitiateCommsAll(void* bufSend, const int* nElemSend, SU2_MPI::Request* sendReq, void* bufRecv,
+                                          const int* nElemRecv, SU2_MPI::Request* recvReq, unsigned short countPerElem,
                                           unsigned short commType) {
-
   /*--- Local variables ---*/
 
   int iMessage, iProc, offset, nElem, count, source, dest, tag;
@@ -1101,64 +1022,56 @@ void CCGNSMeshReaderFVM::InitiateCommsAll(void *bufSend,
 
   iMessage = 0;
   for (iProc = 0; iProc < size; iProc++) {
-
     /*--- Post recv's only if another proc is sending us data. We do
      not communicate with ourselves or post recv's for zero length
      messages to keep overhead down. ---*/
 
-    if ((nElemRecv[iProc+1] > nElemRecv[iProc]) && (iProc != rank)) {
-
+    if ((nElemRecv[iProc + 1] > nElemRecv[iProc]) && (iProc != rank)) {
       /*--- Compute our location in the recv buffer. ---*/
 
-      offset = countPerElem*nElemRecv[iProc];
+      offset = countPerElem * nElemRecv[iProc];
 
       /*--- Take advantage of cumulative storage format to get the number
        of elems that we need to recv. ---*/
 
-      nElem = nElemRecv[iProc+1] - nElemRecv[iProc];
+      nElem = nElemRecv[iProc + 1] - nElemRecv[iProc];
 
       /*--- Total count can include multiple pieces of data per element. ---*/
 
-      count = countPerElem*nElem;
+      count = countPerElem * nElem;
 
       /*--- Post non-blocking recv for this proc. ---*/
 
-      source = iProc; tag = iProc + 1;
+      source = iProc;
+      tag = iProc + 1;
 
       switch (commType) {
         case COMM_TYPE_DOUBLE:
-          SU2_MPI::Irecv(&(static_cast<su2double*>(bufRecv)[offset]),
-                         count, MPI_DOUBLE, source, tag, SU2_MPI::GetComm(),
-                         &(recvReq[iMessage]));
+          SU2_MPI::Irecv(&(static_cast<su2double*>(bufRecv)[offset]), count, MPI_DOUBLE, source, tag,
+                         SU2_MPI::GetComm(), &(recvReq[iMessage]));
           break;
         case COMM_TYPE_UNSIGNED_LONG:
-          SU2_MPI::Irecv(&(static_cast<unsigned long*>(bufRecv)[offset]),
-                         count, MPI_UNSIGNED_LONG, source, tag, SU2_MPI::GetComm(),
-                         &(recvReq[iMessage]));
+          SU2_MPI::Irecv(&(static_cast<unsigned long*>(bufRecv)[offset]), count, MPI_UNSIGNED_LONG, source, tag,
+                         SU2_MPI::GetComm(), &(recvReq[iMessage]));
           break;
         case COMM_TYPE_LONG:
-          SU2_MPI::Irecv(&(static_cast<long*>(bufRecv)[offset]),
-                         count, MPI_LONG, source, tag, SU2_MPI::GetComm(),
+          SU2_MPI::Irecv(&(static_cast<long*>(bufRecv)[offset]), count, MPI_LONG, source, tag, SU2_MPI::GetComm(),
                          &(recvReq[iMessage]));
           break;
         case COMM_TYPE_UNSIGNED_SHORT:
-          SU2_MPI::Irecv(&(static_cast<unsigned short*>(bufRecv)[offset]),
-                         count, MPI_UNSIGNED_SHORT, source, tag, SU2_MPI::GetComm(),
-                         &(recvReq[iMessage]));
+          SU2_MPI::Irecv(&(static_cast<unsigned short*>(bufRecv)[offset]), count, MPI_UNSIGNED_SHORT, source, tag,
+                         SU2_MPI::GetComm(), &(recvReq[iMessage]));
           break;
         case COMM_TYPE_CHAR:
-          SU2_MPI::Irecv(&(static_cast<char*>(bufRecv)[offset]),
-                         count, MPI_CHAR, source, tag, SU2_MPI::GetComm(),
+          SU2_MPI::Irecv(&(static_cast<char*>(bufRecv)[offset]), count, MPI_CHAR, source, tag, SU2_MPI::GetComm(),
                          &(recvReq[iMessage]));
           break;
         case COMM_TYPE_SHORT:
-          SU2_MPI::Irecv(&(static_cast<short*>(bufRecv)[offset]),
-                         count, MPI_SHORT, source, tag, SU2_MPI::GetComm(),
+          SU2_MPI::Irecv(&(static_cast<short*>(bufRecv)[offset]), count, MPI_SHORT, source, tag, SU2_MPI::GetComm(),
                          &(recvReq[iMessage]));
           break;
         case COMM_TYPE_INT:
-          SU2_MPI::Irecv(&(static_cast<int*>(bufRecv)[offset]),
-                         count, MPI_INT, source, tag, SU2_MPI::GetComm(),
+          SU2_MPI::Irecv(&(static_cast<int*>(bufRecv)[offset]), count, MPI_INT, source, tag, SU2_MPI::GetComm(),
                          &(recvReq[iMessage]));
           break;
         default:
@@ -1168,7 +1081,6 @@ void CCGNSMeshReaderFVM::InitiateCommsAll(void *bufSend,
       /*--- Increment message counter. ---*/
 
       iMessage++;
-
     }
   }
 
@@ -1176,64 +1088,56 @@ void CCGNSMeshReaderFVM::InitiateCommsAll(void *bufSend,
 
   iMessage = 0;
   for (iProc = 0; iProc < size; iProc++) {
-
     /*--- Post sends only if we are sending another proc data. We do
      not communicate with ourselves or post sends for zero length
      messages to keep overhead down. ---*/
 
-    if ((nElemSend[iProc+1] > nElemSend[iProc]) && (iProc != rank)) {
-
+    if ((nElemSend[iProc + 1] > nElemSend[iProc]) && (iProc != rank)) {
       /*--- Compute our location in the send buffer. ---*/
 
-      offset = countPerElem*nElemSend[iProc];
+      offset = countPerElem * nElemSend[iProc];
 
       /*--- Take advantage of cumulative storage format to get the number
        of elems that we need to send. ---*/
 
-      nElem = nElemSend[iProc+1] - nElemSend[iProc];
+      nElem = nElemSend[iProc + 1] - nElemSend[iProc];
 
       /*--- Total count can include multiple pieces of data per element. ---*/
 
-      count = countPerElem*nElem;
+      count = countPerElem * nElem;
 
       /*--- Post non-blocking send for this proc. ---*/
 
-      dest = iProc; tag = rank + 1;
+      dest = iProc;
+      tag = rank + 1;
 
       switch (commType) {
         case COMM_TYPE_DOUBLE:
-          SU2_MPI::Isend(&(static_cast<su2double*>(bufSend)[offset]),
-                         count, MPI_DOUBLE, dest, tag, SU2_MPI::GetComm(),
+          SU2_MPI::Isend(&(static_cast<su2double*>(bufSend)[offset]), count, MPI_DOUBLE, dest, tag, SU2_MPI::GetComm(),
                          &(sendReq[iMessage]));
           break;
         case COMM_TYPE_UNSIGNED_LONG:
-          SU2_MPI::Isend(&(static_cast<unsigned long*>(bufSend)[offset]),
-                         count, MPI_UNSIGNED_LONG, dest, tag, SU2_MPI::GetComm(),
-                         &(sendReq[iMessage]));
+          SU2_MPI::Isend(&(static_cast<unsigned long*>(bufSend)[offset]), count, MPI_UNSIGNED_LONG, dest, tag,
+                         SU2_MPI::GetComm(), &(sendReq[iMessage]));
           break;
         case COMM_TYPE_LONG:
-          SU2_MPI::Isend(&(static_cast<long*>(bufSend)[offset]),
-                         count, MPI_LONG, dest, tag, SU2_MPI::GetComm(),
+          SU2_MPI::Isend(&(static_cast<long*>(bufSend)[offset]), count, MPI_LONG, dest, tag, SU2_MPI::GetComm(),
                          &(sendReq[iMessage]));
           break;
         case COMM_TYPE_UNSIGNED_SHORT:
-          SU2_MPI::Isend(&(static_cast<unsigned short*>(bufSend)[offset]),
-                         count, MPI_UNSIGNED_SHORT, dest, tag, SU2_MPI::GetComm(),
-                         &(sendReq[iMessage]));
+          SU2_MPI::Isend(&(static_cast<unsigned short*>(bufSend)[offset]), count, MPI_UNSIGNED_SHORT, dest, tag,
+                         SU2_MPI::GetComm(), &(sendReq[iMessage]));
           break;
         case COMM_TYPE_CHAR:
-          SU2_MPI::Isend(&(static_cast<char*>(bufSend)[offset]),
-                         count, MPI_CHAR, dest, tag, SU2_MPI::GetComm(),
+          SU2_MPI::Isend(&(static_cast<char*>(bufSend)[offset]), count, MPI_CHAR, dest, tag, SU2_MPI::GetComm(),
                          &(sendReq[iMessage]));
           break;
         case COMM_TYPE_SHORT:
-          SU2_MPI::Isend(&(static_cast<short*>(bufSend)[offset]),
-                         count, MPI_SHORT, dest, tag, SU2_MPI::GetComm(),
+          SU2_MPI::Isend(&(static_cast<short*>(bufSend)[offset]), count, MPI_SHORT, dest, tag, SU2_MPI::GetComm(),
                          &(sendReq[iMessage]));
           break;
         case COMM_TYPE_INT:
-          SU2_MPI::Isend(&(static_cast<int*>(bufSend)[offset]),
-                         count, MPI_INT, dest, tag, SU2_MPI::GetComm(),
+          SU2_MPI::Isend(&(static_cast<int*>(bufSend)[offset]), count, MPI_INT, dest, tag, SU2_MPI::GetComm(),
                          &(sendReq[iMessage]));
           break;
         default:
@@ -1243,17 +1147,12 @@ void CCGNSMeshReaderFVM::InitiateCommsAll(void *bufSend,
       /*--- Increment message counter. ---*/
 
       iMessage++;
-
     }
   }
-
 }
 
-void CCGNSMeshReaderFVM::CompleteCommsAll(int nSends,
-                                          SU2_MPI::Request *sendReq,
-                                          int nRecvs,
-                                          SU2_MPI::Request *recvReq) {
-
+void CCGNSMeshReaderFVM::CompleteCommsAll(int nSends, SU2_MPI::Request* sendReq, int nRecvs,
+                                          SU2_MPI::Request* recvReq) {
   /*--- Local variables ---*/
 
   int ind, iSend, iRecv;
@@ -1261,12 +1160,9 @@ void CCGNSMeshReaderFVM::CompleteCommsAll(int nSends,
 
   /*--- Wait for the non-blocking sends to complete. ---*/
 
-  for (iSend = 0; iSend < nSends; iSend++)
-    SU2_MPI::Waitany(nSends, sendReq, &ind, &status);
+  for (iSend = 0; iSend < nSends; iSend++) SU2_MPI::Waitany(nSends, sendReq, &ind, &status);
 
   /*--- Wait for the non-blocking recvs to complete. ---*/
 
-  for (iRecv = 0; iRecv < nRecvs; iRecv++)
-    SU2_MPI::Waitany(nRecvs, recvReq, &ind, &status);
-
+  for (iRecv = 0; iRecv < nRecvs; iRecv++) SU2_MPI::Waitany(nRecvs, recvReq, &ind, &status);
 }
diff --git a/Common/src/geometry/meshreader/CMeshReaderFVM.cpp b/Common/src/geometry/meshreader/CMeshReaderFVM.cpp
index dde520aa244..23a23db1d87 100644
--- a/Common/src/geometry/meshreader/CMeshReaderFVM.cpp
+++ b/Common/src/geometry/meshreader/CMeshReaderFVM.cpp
@@ -28,10 +28,5 @@
 
 #include "../../../include/geometry/meshreader/CMeshReaderFVM.hpp"
 
-CMeshReaderFVM::CMeshReaderFVM(const CConfig *val_config,
-                               unsigned short val_iZone,
-                               unsigned short val_nZone) :
-  rank(SU2_MPI::GetRank()),
-  size(SU2_MPI::GetSize()),
-  config(val_config) {
-}
+CMeshReaderFVM::CMeshReaderFVM(const CConfig* val_config, unsigned short val_iZone, unsigned short val_nZone)
+    : rank(SU2_MPI::GetRank()), size(SU2_MPI::GetSize()), config(val_config) {}
diff --git a/Common/src/geometry/meshreader/CRectangularMeshReaderFVM.cpp b/Common/src/geometry/meshreader/CRectangularMeshReaderFVM.cpp
index e4dd6c48a26..5b312489b74 100644
--- a/Common/src/geometry/meshreader/CRectangularMeshReaderFVM.cpp
+++ b/Common/src/geometry/meshreader/CRectangularMeshReaderFVM.cpp
@@ -29,16 +29,14 @@
 #include "../../../include/toolboxes/CLinearPartitioner.hpp"
 #include "../../../include/geometry/meshreader/CRectangularMeshReaderFVM.hpp"
 
-CRectangularMeshReaderFVM::CRectangularMeshReaderFVM(const CConfig *val_config,
-                                                     unsigned short val_iZone,
+CRectangularMeshReaderFVM::CRectangularMeshReaderFVM(const CConfig* val_config, unsigned short val_iZone,
                                                      unsigned short val_nZone)
-: CMeshReaderFVM(val_config, val_iZone, val_nZone) {
-
+    : CMeshReaderFVM(val_config, val_iZone, val_nZone) {
   /* The rectangular mesh is always 2D. */
   dimension = 2;
 
   /* Set the VTK type for the interior elements and the boundary elements. */
-  KindElem  = QUADRILATERAL;
+  KindElem = QUADRILATERAL;
   KindBound = LINE;
 
   /* The number of nodes in the i and j directions. */
@@ -61,19 +59,17 @@ CRectangularMeshReaderFVM::CRectangularMeshReaderFVM(const CConfig *val_config,
   ComputeRectangularPointCoordinates();
   ComputeRectangularVolumeConnectivity();
   ComputeRectangularSurfaceConnectivity();
-
 }
 
 void CRectangularMeshReaderFVM::ComputeRectangularPointCoordinates() {
-
   /* Set the global count of points based on the grid dimensions. */
-  numberOfGlobalPoints = (nNode)*(mNode);
+  numberOfGlobalPoints = (nNode) * (mNode);
 
   /* Get a partitioner to help with linear partitioning. */
-  CLinearPartitioner pointPartitioner(numberOfGlobalPoints,0);
+  CLinearPartitioner pointPartitioner(numberOfGlobalPoints, 0);
 
   /* Determine number of local points */
-  for(unsigned long globalIndex=0; globalIndex < numberOfGlobalPoints; globalIndex++) {
+  for (unsigned long globalIndex = 0; globalIndex < numberOfGlobalPoints; globalIndex++) {
     if ((int)pointPartitioner.GetRankContainingIndex(globalIndex) == rank) {
       numberOfLocalPoints++;
     }
@@ -82,16 +78,14 @@ void CRectangularMeshReaderFVM::ComputeRectangularPointCoordinates() {
   /* Loop over our analytically defined of coordinates and store only
    those that contain a node within our linear partition of points. */
   localPointCoordinates.resize(dimension);
-  for (int k = 0; k < dimension; k++)
-    localPointCoordinates[k].reserve(numberOfLocalPoints);
+  for (int k = 0; k < dimension; k++) localPointCoordinates[k].reserve(numberOfLocalPoints);
   unsigned long globalIndex = 0;
   for (unsigned long jNode = 0; jNode < mNode; jNode++) {
     for (unsigned long iNode = 0; iNode < nNode; iNode++) {
       if ((int)pointPartitioner.GetRankContainingIndex(globalIndex) == rank) {
-
         /* Store the coordinates more clearly. */
-        const passivedouble x = SU2_TYPE::GetValue(Lx*((su2double)iNode)/((su2double)(nNode-1))+Ox);
-        const passivedouble y = SU2_TYPE::GetValue(Ly*((su2double)jNode)/((su2double)(mNode-1))+Oy);
+        const passivedouble x = SU2_TYPE::GetValue(Lx * ((su2double)iNode) / ((su2double)(nNode - 1)) + Ox);
+        const passivedouble y = SU2_TYPE::GetValue(Ly * ((su2double)jNode) / ((su2double)(mNode - 1)) + Oy);
 
         /* Load into the coordinate class data structure. */
         localPointCoordinates[0].push_back(x);
@@ -100,30 +94,27 @@ void CRectangularMeshReaderFVM::ComputeRectangularPointCoordinates() {
       globalIndex++;
     }
   }
-
 }
 
 void CRectangularMeshReaderFVM::ComputeRectangularVolumeConnectivity() {
-
   /* Set the global count of elements based on the grid dimensions. */
-  numberOfGlobalElements = (nNode-1)*(mNode-1);
+  numberOfGlobalElements = (nNode - 1) * (mNode - 1);
 
   /* Get a partitioner to help with linear partitioning. */
-  CLinearPartitioner pointPartitioner(numberOfGlobalPoints,0);
+  CLinearPartitioner pointPartitioner(numberOfGlobalPoints, 0);
 
   /* Loop over our analytically defined of elements and store only those
    that contain a node within our linear partition of points. */
-  numberOfLocalElements  = 0;
-  vector<unsigned long> connectivity(N_POINTS_HEXAHEDRON,0);
+  numberOfLocalElements = 0;
+  vector<unsigned long> connectivity(N_POINTS_HEXAHEDRON, 0);
   unsigned long globalIndex = 0;
-  for (unsigned long jNode = 0; jNode < mNode-1; jNode++) {
-    for (unsigned long iNode = 0; iNode < nNode-1; iNode++) {
-
+  for (unsigned long jNode = 0; jNode < mNode - 1; jNode++) {
+    for (unsigned long iNode = 0; iNode < nNode - 1; iNode++) {
       /* Compute connectivity based on the i,j index. */
-      connectivity[0] = jNode*nNode + iNode;
-      connectivity[1] = jNode*nNode + iNode + 1;
-      connectivity[2] = (jNode + 1)*nNode + (iNode + 1);
-      connectivity[3] = (jNode + 1)*nNode + iNode;
+      connectivity[0] = jNode * nNode + iNode;
+      connectivity[1] = jNode * nNode + iNode + 1;
+      connectivity[2] = (jNode + 1) * nNode + (iNode + 1);
+      connectivity[3] = (jNode + 1) * nNode + iNode;
 
       /* Check whether any of the points is in our linear partition. */
       bool isOwned = false;
@@ -145,11 +136,9 @@ void CRectangularMeshReaderFVM::ComputeRectangularVolumeConnectivity() {
       globalIndex++;
     }
   }
-
 }
 
 void CRectangularMeshReaderFVM::ComputeRectangularSurfaceConnectivity() {
-
   /* The rectangle alays has 4 markers. */
   numberOfMarkers = 4;
   surfaceElementConnectivity.resize(numberOfMarkers);
@@ -158,49 +147,45 @@ void CRectangularMeshReaderFVM::ComputeRectangularSurfaceConnectivity() {
   /* Compute and store the 4 sets of connectivity. */
   markerNames[0] = "y_minus";
   if (rank == MASTER_NODE) {
-    for (unsigned long iNode = 0; iNode < nNode-1; iNode++) {
+    for (unsigned long iNode = 0; iNode < nNode - 1; iNode++) {
       surfaceElementConnectivity[0].push_back(0);
       surfaceElementConnectivity[0].push_back(KindBound);
       surfaceElementConnectivity[0].push_back(iNode);
       surfaceElementConnectivity[0].push_back(iNode + 1);
-      for (unsigned short i = 0; i < 6; i++)
-      surfaceElementConnectivity[0].push_back(0);
+      for (unsigned short i = 0; i < 6; i++) surfaceElementConnectivity[0].push_back(0);
     }
   }
 
   markerNames[1] = "x_plus";
   if (rank == MASTER_NODE) {
-    for (unsigned long jNode = 0; jNode < mNode-1; jNode++) {
+    for (unsigned long jNode = 0; jNode < mNode - 1; jNode++) {
       surfaceElementConnectivity[1].push_back(0);
       surfaceElementConnectivity[1].push_back(KindBound);
-      surfaceElementConnectivity[1].push_back(jNode*nNode + (nNode - 1));
-      surfaceElementConnectivity[1].push_back((jNode + 1)*nNode + (nNode - 1));
-      for (unsigned short i = 0; i < 6; i++)
-      surfaceElementConnectivity[1].push_back(0);
+      surfaceElementConnectivity[1].push_back(jNode * nNode + (nNode - 1));
+      surfaceElementConnectivity[1].push_back((jNode + 1) * nNode + (nNode - 1));
+      for (unsigned short i = 0; i < 6; i++) surfaceElementConnectivity[1].push_back(0);
     }
   }
 
   markerNames[2] = "y_plus";
   if (rank == MASTER_NODE) {
-    for (unsigned long iNode = 0; iNode < nNode-1; iNode++) {
+    for (unsigned long iNode = 0; iNode < nNode - 1; iNode++) {
       surfaceElementConnectivity[2].push_back(0);
       surfaceElementConnectivity[2].push_back(KindBound);
-      surfaceElementConnectivity[2].push_back((nNode*mNode - 1) - iNode);
-      surfaceElementConnectivity[2].push_back((nNode*mNode - 1) - (iNode + 1));
-      for (unsigned short i = 0; i < 6; i++)
-      surfaceElementConnectivity[2].push_back(0);
+      surfaceElementConnectivity[2].push_back((nNode * mNode - 1) - iNode);
+      surfaceElementConnectivity[2].push_back((nNode * mNode - 1) - (iNode + 1));
+      for (unsigned short i = 0; i < 6; i++) surfaceElementConnectivity[2].push_back(0);
     }
   }
 
   markerNames[3] = "x_minus";
   if (rank == MASTER_NODE) {
-    for (unsigned long jNode = 0; jNode < mNode-1; jNode++) {
+    for (unsigned long jNode = 0; jNode < mNode - 1; jNode++) {
       surfaceElementConnectivity[3].push_back(0);
       surfaceElementConnectivity[3].push_back(KindBound);
-      surfaceElementConnectivity[3].push_back((jNode + 1)*nNode);
-      surfaceElementConnectivity[3].push_back(jNode*nNode);
-      for (unsigned short i = 0; i < 6; i++)
-      surfaceElementConnectivity[3].push_back(0);
+      surfaceElementConnectivity[3].push_back((jNode + 1) * nNode);
+      surfaceElementConnectivity[3].push_back(jNode * nNode);
+      for (unsigned short i = 0; i < 6; i++) surfaceElementConnectivity[3].push_back(0);
     }
   }
 }
diff --git a/Common/src/geometry/meshreader/CSU2ASCIIMeshReaderFVM.cpp b/Common/src/geometry/meshreader/CSU2ASCIIMeshReaderFVM.cpp
index 92e63d0623d..272dafd79ed 100644
--- a/Common/src/geometry/meshreader/CSU2ASCIIMeshReaderFVM.cpp
+++ b/Common/src/geometry/meshreader/CSU2ASCIIMeshReaderFVM.cpp
@@ -29,19 +29,14 @@
 #include "../../../include/toolboxes/CLinearPartitioner.hpp"
 #include "../../../include/geometry/meshreader/CSU2ASCIIMeshReaderFVM.hpp"
 
-CSU2ASCIIMeshReaderFVM::CSU2ASCIIMeshReaderFVM(CConfig *val_config,
-                                               unsigned short val_iZone,
-                                               unsigned short val_nZone)
-: CMeshReaderFVM(val_config, val_iZone, val_nZone),
-  myZone(val_iZone),
-  nZones(val_nZone),
-  meshFilename(config->GetMesh_FileName()) {
-
-  actuator_disk  = (((config->GetnMarker_ActDiskInlet() != 0) ||
-                     (config->GetnMarker_ActDiskOutlet() != 0)) &&
-                    ((config->GetKind_SU2() == SU2_COMPONENT::SU2_CFD) ||
-                     ((config->GetKind_SU2() == SU2_COMPONENT::SU2_DEF) &&
-                      (config->GetActDisk_SU2_DEF()))));
+CSU2ASCIIMeshReaderFVM::CSU2ASCIIMeshReaderFVM(CConfig* val_config, unsigned short val_iZone, unsigned short val_nZone)
+    : CMeshReaderFVM(val_config, val_iZone, val_nZone),
+      myZone(val_iZone),
+      nZones(val_nZone),
+      meshFilename(config->GetMesh_FileName()) {
+  actuator_disk = (((config->GetnMarker_ActDiskInlet() != 0) || (config->GetnMarker_ActDiskOutlet() != 0)) &&
+                   ((config->GetKind_SU2() == SU2_COMPONENT::SU2_CFD) ||
+                    ((config->GetKind_SU2() == SU2_COMPONENT::SU2_DEF) && (config->GetActDisk_SU2_DEF()))));
   if (config->GetActDisk_DoubleSurface()) actuator_disk = false;
 
   /* Read the basic metadata and perform some basic error checks. */
@@ -55,8 +50,7 @@ CSU2ASCIIMeshReaderFVM::CSU2ASCIIMeshReaderFVM(CConfig *val_config,
   /* If the mesh contains an actuator disk as a single surface,
    we need to first split the surface into repeated points and update
    the connectivity for each element touching the surface. */
-  if (actuator_disk)
-    SplitActuatorDiskSurface();
+  if (actuator_disk) SplitActuatorDiskSurface();
 
   /* Read and store the points, interior elements, and surface elements.
    We store only the points and interior elements on our rank's linear
@@ -67,22 +61,21 @@ CSU2ASCIIMeshReaderFVM::CSU2ASCIIMeshReaderFVM(CConfig *val_config,
 
   for (auto section : SectionOrder) {
     switch (section) {
-    case FileSection::ELEMENTS:
-      ReadVolumeElementConnectivity();
-      break;
-    case FileSection::POINTS:
-      ReadPointCoordinates();
-      break;
-    case FileSection::MARKERS:
-      ReadSurfaceElementConnectivity();
-      break;
+      case FileSection::ELEMENTS:
+        ReadVolumeElementConnectivity();
+        break;
+      case FileSection::POINTS:
+        ReadPointCoordinates();
+        break;
+      case FileSection::MARKERS:
+        ReadSurfaceElementConnectivity();
+        break;
     }
   }
   mesh_file.close();
 }
 
-bool CSU2ASCIIMeshReaderFVM::ReadMetadata(const bool single_pass, CConfig *config) {
-
+bool CSU2ASCIIMeshReaderFVM::ReadMetadata(const bool single_pass, CConfig* config) {
   const bool harmonic_balance = config->GetTime_Marching() == TIME_MARCHING::HARMONIC_BALANCE;
   const bool multizone_file = config->GetMultizone_Mesh();
 
@@ -90,8 +83,10 @@ bool CSU2ASCIIMeshReaderFVM::ReadMetadata(const bool single_pass, CConfig *confi
 
   mesh_file.open(meshFilename);
   if (mesh_file.fail()) {
-    SU2_MPI::Error("Error opening SU2 ASCII grid.\n"
-                   "Check that the file exists.", CURRENT_FUNCTION);
+    SU2_MPI::Error(
+        "Error opening SU2 ASCII grid.\n"
+        "Check that the file exists.",
+        CURRENT_FUNCTION);
   }
 
   /*--- If more than one, find the curent zone in the mesh file. ---*/
@@ -99,16 +94,15 @@ bool CSU2ASCIIMeshReaderFVM::ReadMetadata(const bool single_pass, CConfig *confi
   string text_line;
   if ((nZones > 1 && multizone_file) || harmonic_balance) {
     if (harmonic_balance) {
-      if (rank == MASTER_NODE) cout << "Reading time instance " << config->GetiInst()+1 << "." << endl;
-    }
-    else {
+      if (rank == MASTER_NODE) cout << "Reading time instance " << config->GetiInst() + 1 << "." << endl;
+    } else {
       bool foundZone = false;
-      while (getline (mesh_file,text_line)) {
+      while (getline(mesh_file, text_line)) {
         /*--- Search for the current domain ---*/
-        if (text_line.find ("IZONE=",0) != string::npos) {
-          text_line.erase (0,6);
+        if (text_line.find("IZONE=", 0) != string::npos) {
+          text_line.erase(0, 6);
           unsigned short jZone = atoi(text_line.c_str());
-          if (jZone == myZone+1) {
+          if (jZone == myZone + 1) {
             if (rank == MASTER_NODE) cout << "Reading zone " << myZone << " from native SU2 ASCII mesh." << endl;
             foundZone = true;
             break;
@@ -116,8 +110,10 @@ bool CSU2ASCIIMeshReaderFVM::ReadMetadata(const bool single_pass, CConfig *confi
         }
       }
       if (!foundZone) {
-        SU2_MPI::Error("Could not find the IZONE= keyword or the zone contents.\n"
-                       "Check the SU2 ASCII file format.", CURRENT_FUNCTION);
+        SU2_MPI::Error(
+            "Could not find the IZONE= keyword or the zone contents.\n"
+            "Check the SU2 ASCII file format.",
+            CURRENT_FUNCTION);
       }
     }
   }
@@ -132,12 +128,11 @@ bool CSU2ASCIIMeshReaderFVM::ReadMetadata(const bool single_pass, CConfig *confi
   int current_section_idx = 0;
   bool single_pass_active = false;
 
-  while (getline (mesh_file, text_line)) {
-
+  while (getline(mesh_file, text_line)) {
     /*--- Read the dimension of the problem ---*/
 
-    if (!foundNDIME && text_line.find ("NDIME=",0) != string::npos) {
-      text_line.erase (0,6);
+    if (!foundNDIME && text_line.find("NDIME=", 0) != string::npos) {
+      text_line.erase(0, 6);
       dimension = atoi(text_line.c_str());
       foundNDIME = true;
       continue;
@@ -145,8 +140,8 @@ bool CSU2ASCIIMeshReaderFVM::ReadMetadata(const bool single_pass, CConfig *confi
 
     /*--- The AoA and AoS offset values are optional. ---*/
 
-    if (text_line.find ("AOA_OFFSET=",0) != string::npos) {
-      text_line.erase (0,11);
+    if (text_line.find("AOA_OFFSET=", 0) != string::npos) {
+      text_line.erase(0, 11);
       su2double AoA_Offset = atof(text_line.c_str());
 
       /*--- The offset is in deg ---*/
@@ -158,16 +153,15 @@ bool CSU2ASCIIMeshReaderFVM::ReadMetadata(const bool single_pass, CConfig *confi
         if (!config->GetDiscard_InFiles()) {
           cout << "WARNING: AoA in the config file (" << config->GetAoA() << " deg.) +\n";
           cout << "         AoA offset in mesh file (" << AoA_Offset << " deg.) = " << AoA_Current << " deg." << endl;
-        }
-        else {
+        } else {
           cout << "WARNING: Discarding the AoA offset in the mesh file." << endl;
         }
       }
       continue;
     }
 
-    if (text_line.find ("AOS_OFFSET=",0) != string::npos) {
-      text_line.erase (0,11);
+    if (text_line.find("AOS_OFFSET=", 0) != string::npos) {
+      text_line.erase(0, 11);
       su2double AoS_Offset = atof(text_line.c_str());
 
       /*--- The offset is in deg ---*/
@@ -179,50 +173,45 @@ bool CSU2ASCIIMeshReaderFVM::ReadMetadata(const bool single_pass, CConfig *confi
         if (!config->GetDiscard_InFiles()) {
           cout << "WARNING: AoS in the config file (" << config->GetAoS() << " deg.) +\n";
           cout << "         AoS offset in mesh file (" << AoS_Offset << " deg.) = " << AoS_Current << " deg." << endl;
-        }
-        else {
+        } else {
           cout << "WARNING: Discarding the AoS offset in the mesh file." << endl;
         }
       }
       continue;
     }
 
-    if (!foundNPOIN && text_line.find ("NPOIN=",0) != string::npos) {
-      text_line.erase (0,6);
+    if (!foundNPOIN && text_line.find("NPOIN=", 0) != string::npos) {
+      text_line.erase(0, 6);
       numberOfGlobalPoints = atoi(text_line.c_str());
 
       /* If the points were found first, read them, otherwise just consume the lines. */
       if (single_pass && foundNDIME && current_section_idx == 0) {
         single_pass_active = true;
         ReadPointCoordinates(true);
-      }
-      else {
-        for (auto iPoint = 0ul; iPoint < numberOfGlobalPoints; iPoint++)
-          getline (mesh_file, text_line);
+      } else {
+        for (auto iPoint = 0ul; iPoint < numberOfGlobalPoints; iPoint++) getline(mesh_file, text_line);
       }
       SectionOrder[current_section_idx++] = FileSection::POINTS;
       foundNPOIN = true;
       continue;
     }
 
-    if (!foundNELEM && text_line.find ("NELEM=",0) != string::npos) {
-      text_line.erase (0,6);
+    if (!foundNELEM && text_line.find("NELEM=", 0) != string::npos) {
+      text_line.erase(0, 6);
       numberOfGlobalElements = atoi(text_line.c_str());
 
       if (single_pass_active) {
         ReadVolumeElementConnectivity(true);
-      }
-      else {
-        for (auto iElem = 0ul; iElem < numberOfGlobalElements; iElem++)
-          getline (mesh_file, text_line);
+      } else {
+        for (auto iElem = 0ul; iElem < numberOfGlobalElements; iElem++) getline(mesh_file, text_line);
       }
       SectionOrder[current_section_idx++] = FileSection::ELEMENTS;
       foundNELEM = true;
       continue;
     }
 
-    if (!foundNMARK && text_line.find ("NMARK=",0) != string::npos) {
-      text_line.erase (0,6);
+    if (!foundNMARK && text_line.find("NMARK=", 0) != string::npos) {
+      text_line.erase(0, 6);
       numberOfMarkers = atoi(text_line.c_str());
 
       if (current_section_idx != 2) {
@@ -237,7 +226,7 @@ bool CSU2ASCIIMeshReaderFVM::ReadMetadata(const bool single_pass, CConfig *confi
     }
 
     /* Stop before we reach the next zone then check for errors below. */
-    if (text_line.find ("IZONE=",0) != string::npos) {
+    if (text_line.find("IZONE=", 0) != string::npos) {
       break;
     }
   }
@@ -246,32 +235,41 @@ bool CSU2ASCIIMeshReaderFVM::ReadMetadata(const bool single_pass, CConfig *confi
 
   /* Throw an error if any of the keywords was not found. */
   if (!foundNDIME) {
-    SU2_MPI::Error("Could not find the keyword \"NDIME=\".\n"
-                   "Check the SU2 ASCII file format.", CURRENT_FUNCTION);
+    SU2_MPI::Error(
+        "Could not find the keyword \"NDIME=\".\n"
+        "Check the SU2 ASCII file format.",
+        CURRENT_FUNCTION);
   }
   if (!foundNPOIN) {
-    SU2_MPI::Error("Could not find the keyword \"NPOIN=\".\n"
-                   "Check the SU2 ASCII file format.", CURRENT_FUNCTION);
+    SU2_MPI::Error(
+        "Could not find the keyword \"NPOIN=\".\n"
+        "Check the SU2 ASCII file format.",
+        CURRENT_FUNCTION);
   }
   if (!foundNELEM) {
-    SU2_MPI::Error("Could not find the keyword \"NELEM=\".\n"
-                   "Check the SU2 ASCII file format.", CURRENT_FUNCTION);
+    SU2_MPI::Error(
+        "Could not find the keyword \"NELEM=\".\n"
+        "Check the SU2 ASCII file format.",
+        CURRENT_FUNCTION);
   }
   if (!foundNMARK) {
-    SU2_MPI::Error("Could not find the keyword \"NMARK=\".\n"
-                   "Check the SU2 ASCII file format.", CURRENT_FUNCTION);
+    SU2_MPI::Error(
+        "Could not find the keyword \"NMARK=\".\n"
+        "Check the SU2 ASCII file format.",
+        CURRENT_FUNCTION);
   }
 
   return single_pass_active;
 }
 
 void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
-
   /*--- Actuator disk preprocesing ---*/
 
   bool InElem, Perimeter;
   unsigned long Counter = 0;
-  Xloc = 0.0; Yloc = 0.0; Zloc = 0.0;
+  Xloc = 0.0;
+  Yloc = 0.0;
+  Zloc = 0.0;
   unsigned long nElem_Bound_;
 
   vector<unsigned long long> EdgeBegin, EdgeEnd;
@@ -279,7 +277,7 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
   unsigned long AuxEdge, iEdge, jEdge, nEdges, nPointVolume;
   unsigned long long FirstEdgeIndex, SecondEdgeIndex;
 
-  vector<unsigned long> connectivity(N_POINTS_HEXAHEDRON,0);
+  vector<unsigned long> connectivity(N_POINTS_HEXAHEDRON, 0);
   vector<unsigned long> ActDiskPoint_Front_Inv(numberOfGlobalPoints);
   vector<unsigned long> ActDiskPoint_Front;
   vector<unsigned long> VolumePoint;
@@ -291,7 +289,7 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
    boundary. Throw an error otherwise. */
   if (config->GetnMarker_ActDiskInlet() > 1) {
     SU2_MPI::Error(string("Current implementation can only split a single actuator disk.") +
-                   string(" \n Remove disks or re-export your mesh with double surfaces (repeated points)."),
+                       string(" \n Remove disks or re-export your mesh with double surfaces (repeated points)."),
                    CURRENT_FUNCTION);
   }
 
@@ -304,74 +302,78 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
 
   string text_line;
   string::size_type position;
-  while (getline (mesh_file, text_line)) {
-
-    position = text_line.find ("NMARK=",0);
+  while (getline(mesh_file, text_line)) {
+    position = text_line.find("NMARK=", 0);
     if (position != string::npos) {
-
-      for (unsigned short iMarker = 0 ; iMarker < numberOfMarkers; iMarker++) {
-
-        getline (mesh_file, text_line);
-        text_line.erase (0,11); string::size_type position;
+      for (unsigned short iMarker = 0; iMarker < numberOfMarkers; iMarker++) {
+        getline(mesh_file, text_line);
+        text_line.erase(0, 11);
+        string::size_type position;
         for (unsigned short iChar = 0; iChar < 20; iChar++) {
-          position = text_line.find( " ", 0 );
-          if (position != string::npos) text_line.erase (position,1);
-          position = text_line.find( "\r", 0 );
-          if (position != string::npos) text_line.erase (position,1);
-          position = text_line.find( "\n", 0 );
-          if (position != string::npos) text_line.erase (position,1);
+          position = text_line.find(" ", 0);
+          if (position != string::npos) text_line.erase(position, 1);
+          position = text_line.find("\r", 0);
+          if (position != string::npos) text_line.erase(position, 1);
+          position = text_line.find("\n", 0);
+          if (position != string::npos) text_line.erase(position, 1);
         }
         string Marker_Tag = text_line.c_str();
 
-        getline (mesh_file, text_line);
-        text_line.erase (0,13);
+        getline(mesh_file, text_line);
+        text_line.erase(0, 13);
         nElem_Bound_ = atoi(text_line.c_str());
 
         if (Marker_Tag != config->GetMarker_ActDiskInlet_TagBound(0)) {
-          for (unsigned long iElem_Bound = 0; iElem_Bound < nElem_Bound_; iElem_Bound++) { getline (mesh_file, text_line); }
-        }
-        else {
-
+          for (unsigned long iElem_Bound = 0; iElem_Bound < nElem_Bound_; iElem_Bound++) {
+            getline(mesh_file, text_line);
+          }
+        } else {
           if (rank == MASTER_NODE)
-            cout << "Splitting the surface " << Marker_Tag << "( " << nElem_Bound_  << " boundary elements )." << endl;
+            cout << "Splitting the surface " << Marker_Tag << "( " << nElem_Bound_ << " boundary elements )." << endl;
 
           /*--- Create a list of edges ---*/
 
           for (unsigned long iElem_Bound = 0; iElem_Bound < nElem_Bound_; iElem_Bound++) {
-
             getline(mesh_file, text_line);
 
             unsigned short VTK_Type;
             istringstream bound_line(text_line);
             bound_line >> VTK_Type;
 
-            switch(VTK_Type) {
+            switch (VTK_Type) {
               case LINE:
                 bound_line >> connectivity[0];
                 bound_line >> connectivity[1];
 
-                EdgeBegin.push_back(connectivity[0]); EdgeEnd.push_back(connectivity[1]);
+                EdgeBegin.push_back(connectivity[0]);
+                EdgeEnd.push_back(connectivity[1]);
                 break;
               case TRIANGLE:
                 bound_line >> connectivity[0];
                 bound_line >> connectivity[1];
                 bound_line >> connectivity[2];
-                EdgeBegin.push_back(connectivity[0]); EdgeEnd.push_back(connectivity[1]);
-                EdgeBegin.push_back(connectivity[1]); EdgeEnd.push_back(connectivity[2]);
-                EdgeBegin.push_back(connectivity[2]); EdgeEnd.push_back(connectivity[0]);
+                EdgeBegin.push_back(connectivity[0]);
+                EdgeEnd.push_back(connectivity[1]);
+                EdgeBegin.push_back(connectivity[1]);
+                EdgeEnd.push_back(connectivity[2]);
+                EdgeBegin.push_back(connectivity[2]);
+                EdgeEnd.push_back(connectivity[0]);
                 break;
               case QUADRILATERAL:
                 bound_line >> connectivity[0];
                 bound_line >> connectivity[1];
                 bound_line >> connectivity[2];
                 bound_line >> connectivity[3];
-                EdgeBegin.push_back(connectivity[0]); EdgeEnd.push_back(connectivity[1]);
-                EdgeBegin.push_back(connectivity[1]); EdgeEnd.push_back(connectivity[2]);
-                EdgeBegin.push_back(connectivity[2]); EdgeEnd.push_back(connectivity[3]);
-                EdgeBegin.push_back(connectivity[3]); EdgeEnd.push_back(connectivity[0]);
+                EdgeBegin.push_back(connectivity[0]);
+                EdgeEnd.push_back(connectivity[1]);
+                EdgeBegin.push_back(connectivity[1]);
+                EdgeEnd.push_back(connectivity[2]);
+                EdgeBegin.push_back(connectivity[2]);
+                EdgeEnd.push_back(connectivity[3]);
+                EdgeBegin.push_back(connectivity[3]);
+                EdgeEnd.push_back(connectivity[0]);
                 break;
             }
-
           }
 
           /*--- Set the total number of edges ---*/
@@ -380,17 +382,18 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
 
           /*--- Sort edges based on local point index, first index is always the largest ---*/
 
-          for (iEdge = 0; iEdge <  nEdges; iEdge++) {
+          for (iEdge = 0; iEdge < nEdges; iEdge++) {
             if (EdgeEnd[iEdge] < EdgeBegin[iEdge]) {
-              AuxEdge = EdgeEnd[iEdge]; EdgeEnd[iEdge] = EdgeBegin[iEdge]; EdgeBegin[iEdge] = AuxEdge;
+              AuxEdge = EdgeEnd[iEdge];
+              EdgeEnd[iEdge] = EdgeBegin[iEdge];
+              EdgeBegin[iEdge] = AuxEdge;
             }
           }
 
           /*--- Bubble sort of the points based on the first index   ---*/
 
           for (iEdge = 0; iEdge < nEdges; iEdge++) {
-            for (jEdge = iEdge+1; jEdge < nEdges; jEdge++) {
-
+            for (jEdge = iEdge + 1; jEdge < nEdges; jEdge++) {
               FirstEdgeIndex = EdgeBegin[jEdge] << 31;
               FirstEdgeIndex += EdgeEnd[jEdge];
 
@@ -398,14 +401,17 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
               SecondEdgeIndex += EdgeEnd[iEdge];
 
               if (FirstEdgeIndex <= SecondEdgeIndex) {
-                AuxEdge = EdgeBegin[iEdge]; EdgeBegin[iEdge] = EdgeBegin[jEdge]; EdgeBegin[jEdge] = AuxEdge;
-                AuxEdge = EdgeEnd[iEdge];  EdgeEnd[iEdge] = EdgeEnd[jEdge]; EdgeEnd[jEdge] = AuxEdge;
+                AuxEdge = EdgeBegin[iEdge];
+                EdgeBegin[iEdge] = EdgeBegin[jEdge];
+                EdgeBegin[jEdge] = AuxEdge;
+                AuxEdge = EdgeEnd[iEdge];
+                EdgeEnd[iEdge] = EdgeEnd[jEdge];
+                EdgeEnd[jEdge] = AuxEdge;
               }
             }
           }
 
           if (dimension == 3) {
-
             /*--- Check the begning of the list ---*/
 
             if (!((EdgeBegin[0] == EdgeBegin[1]) && (EdgeEnd[0] == EdgeEnd[1]))) {
@@ -413,9 +419,9 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
               PerimeterPoint.push_back(EdgeEnd[0]);
             }
 
-            for (iEdge = 1; iEdge < nEdges-1; iEdge++) {
-              bool Check_1 = !((EdgeBegin[iEdge] == EdgeBegin[iEdge-1]) && (EdgeEnd[iEdge] == EdgeEnd[iEdge-1]));
-              bool Check_2 = !((EdgeBegin[iEdge] == EdgeBegin[iEdge+1]) && (EdgeEnd[iEdge] == EdgeEnd[iEdge+1]));
+            for (iEdge = 1; iEdge < nEdges - 1; iEdge++) {
+              bool Check_1 = !((EdgeBegin[iEdge] == EdgeBegin[iEdge - 1]) && (EdgeEnd[iEdge] == EdgeEnd[iEdge - 1]));
+              bool Check_2 = !((EdgeBegin[iEdge] == EdgeBegin[iEdge + 1]) && (EdgeEnd[iEdge] == EdgeEnd[iEdge + 1]));
               if ((Check_1 && Check_2)) {
                 PerimeterPoint.push_back(EdgeBegin[iEdge]);
                 PerimeterPoint.push_back(EdgeEnd[iEdge]);
@@ -424,14 +430,12 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
 
             /*--- Check the  end of the list ---*/
 
-            if (!((EdgeBegin[nEdges-1] == EdgeBegin[nEdges-2]) && (EdgeEnd[nEdges-1] == EdgeEnd[nEdges-2]))) {
-              PerimeterPoint.push_back(EdgeBegin[nEdges-1]);
-              PerimeterPoint.push_back(EdgeEnd[nEdges-1]);
+            if (!((EdgeBegin[nEdges - 1] == EdgeBegin[nEdges - 2]) && (EdgeEnd[nEdges - 1] == EdgeEnd[nEdges - 2]))) {
+              PerimeterPoint.push_back(EdgeBegin[nEdges - 1]);
+              PerimeterPoint.push_back(EdgeEnd[nEdges - 1]);
             }
 
           } else {
-
-
             /*--- Create a list with all the points ---*/
 
             for (iEdge = 0; iEdge < nEdges; iEdge++) {
@@ -445,22 +449,25 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
 
             /*--- Check the begning of the list ---*/
 
-            if (!(ActDiskPoint_Front[0] == ActDiskPoint_Front[1]) ) { PerimeterPoint.push_back(ActDiskPoint_Front[0]); }
+            if (!(ActDiskPoint_Front[0] == ActDiskPoint_Front[1])) {
+              PerimeterPoint.push_back(ActDiskPoint_Front[0]);
+            }
 
-            for (unsigned long iPoint = 1; iPoint < ActDiskPoint_Front.size()-1; iPoint++) {
-              bool Check_1 = !((ActDiskPoint_Front[iPoint] == ActDiskPoint_Front[iPoint-1]) );
-              bool Check_2 = !((ActDiskPoint_Front[iPoint] == ActDiskPoint_Front[iPoint+1]) );
-              if ((Check_1 && Check_2)) { PerimeterPoint.push_back(ActDiskPoint_Front[iEdge]); }
+            for (unsigned long iPoint = 1; iPoint < ActDiskPoint_Front.size() - 1; iPoint++) {
+              bool Check_1 = !((ActDiskPoint_Front[iPoint] == ActDiskPoint_Front[iPoint - 1]));
+              bool Check_2 = !((ActDiskPoint_Front[iPoint] == ActDiskPoint_Front[iPoint + 1]));
+              if ((Check_1 && Check_2)) {
+                PerimeterPoint.push_back(ActDiskPoint_Front[iEdge]);
+              }
             }
 
             /*--- Check the  end of the list ---*/
 
-            if (!((EdgeBegin[ActDiskPoint_Front.size()-1] == EdgeBegin[ActDiskPoint_Front.size()-2]) )) {
-              PerimeterPoint.push_back(ActDiskPoint_Front[ActDiskPoint_Front.size()-1]);
+            if (!((EdgeBegin[ActDiskPoint_Front.size() - 1] == EdgeBegin[ActDiskPoint_Front.size() - 2]))) {
+              PerimeterPoint.push_back(ActDiskPoint_Front[ActDiskPoint_Front.size() - 1]);
             }
 
             ActDiskPoint_Front.clear();
-
           }
 
           vector<unsigned long>::iterator it;
@@ -469,11 +476,11 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
           PerimeterPoint.resize(it - PerimeterPoint.begin());
 
           for (iEdge = 0; iEdge < nEdges; iEdge++) {
-
             Perimeter = false;
             for (unsigned long iPoint = 0; iPoint < PerimeterPoint.size(); iPoint++) {
               if (EdgeBegin[iEdge] == PerimeterPoint[iPoint]) {
-                Perimeter = true; break;
+                Perimeter = true;
+                break;
               }
             }
 
@@ -482,12 +489,12 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
             Perimeter = false;
             for (unsigned long iPoint = 0; iPoint < PerimeterPoint.size(); iPoint++) {
               if (EdgeEnd[iEdge] == PerimeterPoint[iPoint]) {
-                Perimeter = true; break;
+                Perimeter = true;
+                break;
               }
             }
 
             if (!Perimeter) ActDiskPoint_Front.push_back(EdgeEnd[iEdge]);
-
           }
 
           /*--- Sort, and remove repeated points from the disk list of points ---*/
@@ -498,7 +505,8 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
           ActDiskNewPoints = ActDiskPoint_Front.size();
 
           if (rank == MASTER_NODE)
-            cout << "Splitting the surface " << Marker_Tag << "( " << ActDiskPoint_Front.size()  << " internal points )." << endl;
+            cout << "Splitting the surface " << Marker_Tag << "( " << ActDiskPoint_Front.size() << " internal points )."
+                 << endl;
 
           /*--- Create a map from original point to the new ones (back plane) ---*/
 
@@ -517,7 +525,6 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
             ActDiskPoint_Back[ActDiskPoint_Front[iPoint]] = kPoint;
             kPoint++;
           }
-
         }
       }
       break;
@@ -537,15 +544,14 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
   mesh_file.open(meshFilename);
   FastForwardToMyZone();
 
-  while (getline (mesh_file, text_line)) {
-
-    position = text_line.find ("NPOIN=",0);
+  while (getline(mesh_file, text_line)) {
+    position = text_line.find("NPOIN=", 0);
     if (position != string::npos) {
       for (unsigned long iPoint = 0; iPoint < numberOfGlobalPoints; iPoint++) {
-        getline (mesh_file, text_line);
+        getline(mesh_file, text_line);
         istringstream point_line(text_line);
 
-        su2double Coords[3] = {0.0,0.0,0.0};
+        su2double Coords[3] = {0.0, 0.0, 0.0};
         if (dimension == 2) {
           point_line >> Coords[0];
           point_line >> Coords[1];
@@ -560,40 +566,45 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
         if (ActDisk_Bool[iPoint]) {
           CoordXActDisk[ActDiskPoint_Front_Inv[iPoint]] = Coords[0];
           CoordYActDisk[ActDiskPoint_Front_Inv[iPoint]] = Coords[1];
-          Xloc += Coords[0]; Yloc += Coords[1];
+          Xloc += Coords[0];
+          Yloc += Coords[1];
           if (dimension == 3) {
             CoordZActDisk[ActDiskPoint_Front_Inv[iPoint]] = Coords[2];
             Zloc += Coords[2];
           }
           Counter++;
         }
-
       }
     }
 
     /*--- Locate and tag points that touch the actuator disk surface. ---*/
 
-    position = text_line.find ("NELEM=",0);
+    position = text_line.find("NELEM=", 0);
     if (position != string::npos) {
       for (unsigned long iElem = 0; iElem < numberOfGlobalElements; iElem++) {
-
         getline(mesh_file, text_line);
         istringstream elem_line(text_line);
 
         unsigned short VTK_Type;
         elem_line >> VTK_Type;
 
-        switch(VTK_Type) {
+        switch (VTK_Type) {
           case TRIANGLE:
             elem_line >> connectivity[0];
             elem_line >> connectivity[1];
             elem_line >> connectivity[2];
             InElem = false;
             for (unsigned long i = 0; i < (unsigned long)N_POINTS_TRIANGLE; i++) {
-              if (ActDisk_Bool[connectivity[i]]) { InElem = true; break; } }
+              if (ActDisk_Bool[connectivity[i]]) {
+                InElem = true;
+                break;
+              }
+            }
             if (InElem) {
               for (unsigned long i = 0; i < (unsigned long)N_POINTS_TRIANGLE; i++) {
-                VolumePoint.push_back(connectivity[i]); } }
+                VolumePoint.push_back(connectivity[i]);
+              }
+            }
             break;
           case QUADRILATERAL:
             elem_line >> connectivity[0];
@@ -602,10 +613,16 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
             elem_line >> connectivity[3];
             InElem = false;
             for (unsigned long i = 0; i < (unsigned long)N_POINTS_QUADRILATERAL; i++) {
-              if (ActDisk_Bool[connectivity[i]]) { InElem = true; break; } }
+              if (ActDisk_Bool[connectivity[i]]) {
+                InElem = true;
+                break;
+              }
+            }
             if (InElem) {
               for (unsigned long i = 0; i < (unsigned long)N_POINTS_QUADRILATERAL; i++) {
-                VolumePoint.push_back(connectivity[i]); } }
+                VolumePoint.push_back(connectivity[i]);
+              }
+            }
             break;
           case TETRAHEDRON:
             elem_line >> connectivity[0];
@@ -614,10 +631,16 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
             elem_line >> connectivity[3];
             InElem = false;
             for (unsigned long i = 0; i < (unsigned long)N_POINTS_TETRAHEDRON; i++) {
-              if (ActDisk_Bool[connectivity[i]]) { InElem = true; break; }              }
+              if (ActDisk_Bool[connectivity[i]]) {
+                InElem = true;
+                break;
+              }
+            }
             if (InElem) {
               for (unsigned long i = 0; i < (unsigned long)N_POINTS_TETRAHEDRON; i++) {
-                VolumePoint.push_back(connectivity[i]); } }
+                VolumePoint.push_back(connectivity[i]);
+              }
+            }
             break;
           case HEXAHEDRON:
             elem_line >> connectivity[0];
@@ -630,10 +653,16 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
             elem_line >> connectivity[7];
             InElem = false;
             for (unsigned long i = 0; i < (unsigned long)N_POINTS_HEXAHEDRON; i++) {
-              if (ActDisk_Bool[connectivity[i]]) { InElem = true; break; } }
+              if (ActDisk_Bool[connectivity[i]]) {
+                InElem = true;
+                break;
+              }
+            }
             if (InElem) {
               for (unsigned long i = 0; i < (unsigned long)N_POINTS_HEXAHEDRON; i++) {
-                VolumePoint.push_back(connectivity[i]); } }
+                VolumePoint.push_back(connectivity[i]);
+              }
+            }
             break;
           case PRISM:
             elem_line >> connectivity[0];
@@ -644,10 +673,16 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
             elem_line >> connectivity[5];
             InElem = false;
             for (unsigned long i = 0; i < (unsigned long)N_POINTS_PRISM; i++) {
-              if (ActDisk_Bool[connectivity[i]]) { InElem = true; break; } }
+              if (ActDisk_Bool[connectivity[i]]) {
+                InElem = true;
+                break;
+              }
+            }
             if (InElem) {
               for (unsigned long i = 0; i < (unsigned long)N_POINTS_PRISM; i++) {
-                VolumePoint.push_back(connectivity[i]); } }
+                VolumePoint.push_back(connectivity[i]);
+              }
+            }
             break;
           case PYRAMID:
             elem_line >> connectivity[0];
@@ -657,10 +692,16 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
             elem_line >> connectivity[4];
             InElem = false;
             for (unsigned long i = 0; i < (unsigned long)N_POINTS_PYRAMID; i++) {
-              if (ActDisk_Bool[connectivity[i]]) { InElem = true; break; } }
+              if (ActDisk_Bool[connectivity[i]]) {
+                InElem = true;
+                break;
+              }
+            }
             if (InElem) {
               for (unsigned long i = 0; i < (unsigned long)N_POINTS_PYRAMID; i++) {
-                VolumePoint.push_back(connectivity[i]); } }
+                VolumePoint.push_back(connectivity[i]);
+              }
+            }
             break;
         }
       }
@@ -697,7 +738,7 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
 
   for (unsigned long iPoint = 0; iPoint < nPointVolume; iPoint++) {
     MapVolumePointBool[VolumePoint[iPoint]] = true;
-    VolumePoint_Inv[VolumePoint[iPoint]]    = iPoint;
+    VolumePoint_Inv[VolumePoint[iPoint]] = iPoint;
   }
 
   /*--- Store the coordinates of all the surface and volume
@@ -706,13 +747,13 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
   mesh_file.open(meshFilename);
   FastForwardToMyZone();
 
-  while (getline (mesh_file, text_line)) {
-    position = text_line.find ("NPOIN=",0);
+  while (getline(mesh_file, text_line)) {
+    position = text_line.find("NPOIN=", 0);
     if (position != string::npos) {
       for (unsigned long iPoint = 0; iPoint < numberOfGlobalPoints; iPoint++) {
-        getline (mesh_file, text_line);
+        getline(mesh_file, text_line);
         istringstream point_line(text_line);
-        su2double Coords[3] = {0.0,0.0,0.0};
+        su2double Coords[3] = {0.0, 0.0, 0.0};
         if (dimension == 2) {
           point_line >> Coords[0];
           point_line >> Coords[1];
@@ -741,21 +782,18 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
   numberOfMarkers++;
 
   mesh_file.close();
-
 }
 
 void CSU2ASCIIMeshReaderFVM::ReadPointCoordinates(const bool single_pass) {
-
   /* Get a partitioner to help with linear partitioning. */
-  CLinearPartitioner pointPartitioner(numberOfGlobalPoints,0);
+  CLinearPartitioner pointPartitioner(numberOfGlobalPoints, 0);
 
   /* Determine number of local points */
   numberOfLocalPoints = pointPartitioner.GetSizeOnRank(rank);
 
   /* Prepare our data structure for the point coordinates. */
   localPointCoordinates.resize(dimension);
-  for (int k = 0; k < dimension; k++)
-    localPointCoordinates[k].reserve(numberOfLocalPoints);
+  for (int k = 0; k < dimension; k++) localPointCoordinates[k].reserve(numberOfLocalPoints);
 
   /*--- Read the point coordinates into our data structure. ---*/
 
@@ -763,28 +801,30 @@ void CSU2ASCIIMeshReaderFVM::ReadPointCoordinates(const bool single_pass) {
     string text_line;
     if (!single_pass) {
       getline(mesh_file, text_line);
-      if (text_line.find("NPOIN=",0) == string::npos) continue;
+      if (text_line.find("NPOIN=", 0) == string::npos) continue;
     }
 
     for (unsigned long GlobalIndex = 0; GlobalIndex < numberOfGlobalPoints; ++GlobalIndex) {
-
       if (!actuator_disk) {
         getline(mesh_file, text_line);
-      }
-      else {
-        if (GlobalIndex < numberOfGlobalPoints-ActDiskNewPoints) {
+      } else {
+        if (GlobalIndex < numberOfGlobalPoints - ActDiskNewPoints) {
           getline(mesh_file, text_line);
-        }
-        else {
+        } else {
           /* This is a new actuator disk point, so we must construct a
            string with the new point's coordinates. */
           ostringstream strsX, strsY, strsZ;
           unsigned long BackActDisk_Index = GlobalIndex;
-          unsigned long LocalIndex = BackActDisk_Index - (numberOfGlobalPoints-ActDiskNewPoints);
-          strsX.precision(20); strsY.precision(20); strsZ.precision(20);
-          su2double CoordX = CoordXActDisk[LocalIndex]; strsX << scientific << CoordX;
-          su2double CoordY = CoordYActDisk[LocalIndex]; strsY << scientific << CoordY;
-          su2double CoordZ = CoordZActDisk[LocalIndex]; strsZ << scientific << CoordZ;
+          unsigned long LocalIndex = BackActDisk_Index - (numberOfGlobalPoints - ActDiskNewPoints);
+          strsX.precision(20);
+          strsY.precision(20);
+          strsZ.precision(20);
+          su2double CoordX = CoordXActDisk[LocalIndex];
+          strsX << scientific << CoordX;
+          su2double CoordY = CoordYActDisk[LocalIndex];
+          strsY << scientific << CoordY;
+          su2double CoordZ = CoordZActDisk[LocalIndex];
+          strsZ << scientific << CoordZ;
           text_line = strsX.str() + "\t" + strsY.str() + "\t" + strsZ.str();
         }
       }
@@ -792,9 +832,8 @@ void CSU2ASCIIMeshReaderFVM::ReadPointCoordinates(const bool single_pass) {
       /*--- We only read information for this node if it is owned by this
        rank based upon our initial linear partitioning. ---*/
 
-      passivedouble Coords[3] = {0.0,0.0,0.0};
+      passivedouble Coords[3] = {0.0, 0.0, 0.0};
       if (pointPartitioner.IndexBelongsToRank(GlobalIndex, rank)) {
-
         istringstream point_line(text_line);
 
         /* Store the coordinates more clearly. */
@@ -815,20 +854,19 @@ void CSU2ASCIIMeshReaderFVM::ReadPointCoordinates(const bool single_pass) {
 }
 
 void CSU2ASCIIMeshReaderFVM::ReadVolumeElementConnectivity(const bool single_pass) {
-
   /* Get a partitioner to help with linear partitioning. */
-  CLinearPartitioner pointPartitioner(numberOfGlobalPoints,0);
+  CLinearPartitioner pointPartitioner(numberOfGlobalPoints, 0);
 
   /* Loop over our analytically defined of elements and store only those
    that contain a node within our linear partition of points. */
-  numberOfLocalElements  = 0;
+  numberOfLocalElements = 0;
   array<unsigned long, N_POINTS_HEXAHEDRON> connectivity{};
 
   while (true) {
     string text_line;
     if (!single_pass) {
       if (!getline(mesh_file, text_line)) break;
-      if (text_line.find("NELEM=",0) == string::npos) continue;
+      if (text_line.find("NELEM=", 0) == string::npos) continue;
     }
 
     /*--- Loop over all the volumetric elements and store any element that
@@ -849,24 +887,24 @@ void CSU2ASCIIMeshReaderFVM::ReadVolumeElementConnectivity(const bool single_pas
 
       const auto nPointsElem = nPointsOfElementType(VTK_Type);
 
-      for (unsigned short  i = 0; i < nPointsElem; i++) {
+      for (unsigned short i = 0; i < nPointsElem; i++) {
         elem_line >> connectivity[i];
       }
 
       if (actuator_disk) {
-        for (unsigned short  i = 0; i<nPointsElem; i++) {
+        for (unsigned short i = 0; i < nPointsElem; i++) {
           if (ActDisk_Bool[connectivity[i]]) {
-
-            su2double Xcg = 0.0; unsigned long Counter = 0;
-            for (unsigned short j = 0; j<nPointsElem; j++) {
-              if (connectivity[j] < numberOfGlobalPoints-ActDiskNewPoints) {
+            su2double Xcg = 0.0;
+            unsigned long Counter = 0;
+            for (unsigned short j = 0; j < nPointsElem; j++) {
+              if (connectivity[j] < numberOfGlobalPoints - ActDiskNewPoints) {
                 Xcg += CoordXVolumePoint[VolumePoint_Inv[connectivity[j]]];
                 Counter++;
               }
             }
             Xcg = Xcg / su2double(Counter);
 
-            if (Counter != 0 && Xcg > Xloc)  {
+            if (Counter != 0 && Xcg > Xloc) {
               connectivity[i] = ActDiskPoint_Back[connectivity[i]];
             }
           }
@@ -898,7 +936,6 @@ void CSU2ASCIIMeshReaderFVM::ReadVolumeElementConnectivity(const bool single_pas
 }
 
 void CSU2ASCIIMeshReaderFVM::ReadSurfaceElementConnectivity(const bool single_pass) {
-
   /* We already read in the number of markers with the metadata. */
   surfaceElementConnectivity.resize(numberOfMarkers);
   markerNames.resize(numberOfMarkers);
@@ -913,29 +950,28 @@ void CSU2ASCIIMeshReaderFVM::ReadSurfaceElementConnectivity(const bool single_pa
     string text_line;
     if (!single_pass) {
       if (!getline(mesh_file, text_line)) break;
-      if (text_line.find("NMARK=",0) == string::npos) continue;
+      if (text_line.find("NMARK=", 0) == string::npos) continue;
     }
 
     for (unsigned short iMarker = 0; iMarker < numberOfMarkers; ++iMarker) {
-      getline (mesh_file, text_line);
-      text_line.erase (0,11);
+      getline(mesh_file, text_line);
+      text_line.erase(0, 11);
       string::size_type position;
 
       for (unsigned short iChar = 0; iChar < 20; iChar++) {
-        position = text_line.find( " ", 0 );
-        if (position != string::npos) text_line.erase (position,1);
-        position = text_line.find( "\r", 0 );
-        if (position != string::npos) text_line.erase (position,1);
-        position = text_line.find( "\n", 0 );
-        if (position != string::npos) text_line.erase (position,1);
+        position = text_line.find(" ", 0);
+        if (position != string::npos) text_line.erase(position, 1);
+        position = text_line.find("\r", 0);
+        if (position != string::npos) text_line.erase(position, 1);
+        position = text_line.find("\n", 0);
+        if (position != string::npos) text_line.erase(position, 1);
       }
       markerNames[iMarker] = text_line;
 
       bool duplicate = false;
-      if ((actuator_disk) &&
-          (markerNames[iMarker] == config->GetMarker_ActDiskInlet_TagBound(0))) {
+      if ((actuator_disk) && (markerNames[iMarker] == config->GetMarker_ActDiskInlet_TagBound(0))) {
         duplicate = true;
-        markerNames[iMarker+1] = config->GetMarker_ActDiskOutlet_TagBound(0);
+        markerNames[iMarker + 1] = config->GetMarker_ActDiskOutlet_TagBound(0);
       }
 
       /*--- Physical boundaries definition ---*/
@@ -943,13 +979,14 @@ void CSU2ASCIIMeshReaderFVM::ReadSurfaceElementConnectivity(const bool single_pa
       if (markerNames[iMarker] == "SEND_RECEIVE") {
         /*--- Throw an error if we find deprecated references to SEND_RECEIVE
          boundaries in the mesh. ---*/
-        SU2_MPI::Error("Mesh file contains deprecated SEND_RECEIVE marker!\n"
-                       "Please remove any SEND_RECEIVE markers from the SU2 ASCII mesh.",
-                       CURRENT_FUNCTION);
+        SU2_MPI::Error(
+            "Mesh file contains deprecated SEND_RECEIVE marker!\n"
+            "Please remove any SEND_RECEIVE markers from the SU2 ASCII mesh.",
+            CURRENT_FUNCTION);
       }
 
-      getline (mesh_file, text_line);
-      text_line.erase (0,13);
+      getline(mesh_file, text_line);
+      text_line.erase(0, 13);
       unsigned long nElem_Bound = atoi(text_line.c_str());
 
       /*--- Allocate space for elements ---*/
@@ -964,8 +1001,10 @@ void CSU2ASCIIMeshReaderFVM::ReadSurfaceElementConnectivity(const bool single_pa
         const auto nPointsElem = nPointsOfElementType(VTK_Type);
 
         if (dimension == 3 && VTK_Type == LINE) {
-          SU2_MPI::Error("Line boundary conditions are not possible for 3D calculations.\n"
-                         "Please check the SU2 ASCII mesh file.", CURRENT_FUNCTION);
+          SU2_MPI::Error(
+              "Line boundary conditions are not possible for 3D calculations.\n"
+              "Please check the SU2 ASCII mesh file.",
+              CURRENT_FUNCTION);
         }
 
         for (unsigned short i = 0; i < nPointsElem; i++) {
@@ -1002,42 +1041,39 @@ void CSU2ASCIIMeshReaderFVM::ReadSurfaceElementConnectivity(const bool single_pa
   /*--- Final error check for deprecated periodic BC format. ---*/
 
   string text_line;
-  while (getline (mesh_file, text_line)) {
-
+  while (getline(mesh_file, text_line)) {
     /*--- Find any periodic transformation information. ---*/
 
-    if (text_line.find ("NPERIODIC=",0) != string::npos) {
-
+    if (text_line.find("NPERIODIC=", 0) != string::npos) {
       /*--- Read and store the number of transformations. ---*/
-      text_line.erase(0,10);
+      text_line.erase(0, 10);
       unsigned short nPeriodic = atoi(text_line.c_str());
       if (nPeriodic - 1 != 0) {
-        SU2_MPI::Error("Mesh file contains deprecated periodic format!\n\n"
-                       "For SU2 v7.0.0 and later, preprocessing of periodic grids by SU2_MSH\n"
-                       "is no longer necessary. Please use the original mesh file (prior to SU2_MSH)\n"
-                       "with the same MARKER_PERIODIC definition in the configuration file.", CURRENT_FUNCTION);
+        SU2_MPI::Error(
+            "Mesh file contains deprecated periodic format!\n\n"
+            "For SU2 v7.0.0 and later, preprocessing of periodic grids by SU2_MSH\n"
+            "is no longer necessary. Please use the original mesh file (prior to SU2_MSH)\n"
+            "with the same MARKER_PERIODIC definition in the configuration file.",
+            CURRENT_FUNCTION);
       }
     }
 
     /*--- Stop before we reach the next zone. ---*/
-    if (text_line.find ("IZONE=",0) != string::npos) break;
+    if (text_line.find("IZONE=", 0) != string::npos) break;
   }
-
 }
 
 void CSU2ASCIIMeshReaderFVM::FastForwardToMyZone() {
-
   /*--- If more than one, fast-forward to my zone in the mesh file.  ---*/
 
   if (nZones == 1 || !config->GetMultizone_Mesh()) return;
 
   string text_line;
-  while (getline (mesh_file,text_line)) {
+  while (getline(mesh_file, text_line)) {
     /*--- Search for the current domain ---*/
-    if (text_line.find ("IZONE=",0) == string::npos) continue;
-    text_line.erase (0,6);
+    if (text_line.find("IZONE=", 0) == string::npos) continue;
+    text_line.erase(0, 6);
     unsigned short jZone = atoi(text_line.c_str());
-    if (jZone == myZone+1) break;
+    if (jZone == myZone + 1) break;
   }
-
 }
diff --git a/Common/src/geometry/meson.build b/Common/src/geometry/meson.build
index 0da48dee7b0..b67e2b98658 100644
--- a/Common/src/geometry/meson.build
+++ b/Common/src/geometry/meson.build
@@ -3,4 +3,3 @@ common_src += files(['CGeometry.cpp',
                      'CMultiGridGeometry.cpp',
                      'CDummyGeometry.cpp',
                      'CMultiGridQueue.cpp'])
-
diff --git a/Common/src/geometry/primal_grid/CHexahedron.cpp b/Common/src/geometry/primal_grid/CHexahedron.cpp
index 1ee5c813f46..a4f7f7cf918 100644
--- a/Common/src/geometry/primal_grid/CHexahedron.cpp
+++ b/Common/src/geometry/primal_grid/CHexahedron.cpp
@@ -33,17 +33,19 @@ constexpr unsigned short CHexahedronConnectivity::Faces[6][4];
 constexpr unsigned short CHexahedronConnectivity::nNeighbor_Nodes[8];
 constexpr unsigned short CHexahedronConnectivity::Neighbor_Nodes[8][3];
 
-CHexahedron::CHexahedron(unsigned long val_point_0, unsigned long val_point_1,
-             unsigned long val_point_2, unsigned long val_point_3,
-             unsigned long val_point_4, unsigned long val_point_5,
-             unsigned long val_point_6, unsigned long val_point_7):
-  CPrimalGridWithConnectivity<CHexahedronConnectivity>(false)
-{
+CHexahedron::CHexahedron(unsigned long val_point_0, unsigned long val_point_1, unsigned long val_point_2,
+                         unsigned long val_point_3, unsigned long val_point_4, unsigned long val_point_5,
+                         unsigned long val_point_6, unsigned long val_point_7)
+    : CPrimalGridWithConnectivity<CHexahedronConnectivity>(false) {
   /*--- Define face structure of the element ---*/
-  Nodes[0] = val_point_0; Nodes[1] = val_point_1;
-  Nodes[2] = val_point_2; Nodes[3] = val_point_3;
-  Nodes[4] = val_point_4; Nodes[5] = val_point_5;
-  Nodes[6] = val_point_6; Nodes[7] = val_point_7;
+  Nodes[0] = val_point_0;
+  Nodes[1] = val_point_1;
+  Nodes[2] = val_point_2;
+  Nodes[3] = val_point_3;
+  Nodes[4] = val_point_4;
+  Nodes[5] = val_point_5;
+  Nodes[6] = val_point_6;
+  Nodes[7] = val_point_7;
 }
 
 void CHexahedron::Change_Orientation() {
diff --git a/Common/src/geometry/primal_grid/CLine.cpp b/Common/src/geometry/primal_grid/CLine.cpp
index 66bd2a3cc5c..c3d0d7c26c3 100644
--- a/Common/src/geometry/primal_grid/CLine.cpp
+++ b/Common/src/geometry/primal_grid/CLine.cpp
@@ -33,10 +33,8 @@ constexpr unsigned short CLineConnectivity::Faces[1][2];
 constexpr unsigned short CLineConnectivity::nNeighbor_Nodes[2];
 constexpr unsigned short CLineConnectivity::Neighbor_Nodes[2][1];
 
-
-CLine::CLine(unsigned long val_point_0, unsigned long val_point_1):
-  CPrimalGridWithConnectivity<CLineConnectivity>(false)
-{
+CLine::CLine(unsigned long val_point_0, unsigned long val_point_1)
+    : CPrimalGridWithConnectivity<CLineConnectivity>(false) {
   /*--- Define face structure of the element ---*/
   Nodes[0] = val_point_0;
   Nodes[1] = val_point_1;
diff --git a/Common/src/geometry/primal_grid/CPrimalGrid.cpp b/Common/src/geometry/primal_grid/CPrimalGrid.cpp
index 2ed6d9a550c..94269844044 100644
--- a/Common/src/geometry/primal_grid/CPrimalGrid.cpp
+++ b/Common/src/geometry/primal_grid/CPrimalGrid.cpp
@@ -27,18 +27,13 @@
 
 #include "../../../include/geometry/primal_grid/CPrimalGrid.hpp"
 
-CPrimalGrid::CPrimalGrid(bool FEM, unsigned short nNodes, unsigned short nNeighbor_Elements) :
-  Nodes(new unsigned long[nNodes]),
-  Neighbor_Elements(new long[nNeighbor_Elements]),
-  FEM(FEM) {
-
+CPrimalGrid::CPrimalGrid(bool FEM, unsigned short nNodes, unsigned short nNeighbor_Elements)
+    : Nodes(new unsigned long[nNodes]), Neighbor_Elements(new long[nNeighbor_Elements]), FEM(FEM) {
   GlobalIndex_DomainElement = 0;
-  for(unsigned short i = 0; i < nNeighbor_Elements; i++)
-    Neighbor_Elements[i] = -1;
+  for (unsigned short i = 0; i < nNeighbor_Elements; i++) Neighbor_Elements[i] = -1;
 }
 
 void CPrimalGrid::InitializeNeighbors(unsigned short val_nFaces) {
-
   /*--- Initialize arrays to -1/false to indicate that no neighbor is present and
         that no periodic transformation is needed to the neighbor. ---*/
   for (size_t i = 0; i < val_nFaces; i++) {
@@ -46,6 +41,5 @@ void CPrimalGrid::InitializeNeighbors(unsigned short val_nFaces) {
     PeriodIndexNeighbors[i] = -1;
   }
 
-  for (auto i = 0; i < N_FACES_MAXIMUM; ++i)
-    ElementOwnsFace[i] = false;
+  for (auto i = 0; i < N_FACES_MAXIMUM; ++i) ElementOwnsFace[i] = false;
 }
diff --git a/Common/src/geometry/primal_grid/CPrimalGridBoundFEM.cpp b/Common/src/geometry/primal_grid/CPrimalGridBoundFEM.cpp
index b8dc1c1191b..bd33fb325e5 100644
--- a/Common/src/geometry/primal_grid/CPrimalGridBoundFEM.cpp
+++ b/Common/src/geometry/primal_grid/CPrimalGridBoundFEM.cpp
@@ -27,13 +27,10 @@
 
 #include "../../../include/geometry/primal_grid/CPrimalGridBoundFEM.hpp"
 
-CPrimalGridBoundFEM::CPrimalGridBoundFEM(unsigned long         val_elemGlobalID,
-                                         unsigned long         val_domainElementID,
-                                         unsigned short        val_VTK_Type,
-                                         unsigned short        val_nPolyGrid,
-                                         unsigned short        val_nDOFsGrid,
-                                         std::vector<unsigned long> &val_nodes): CPrimalGrid(true, val_nDOFsGrid, 1)
-{
+CPrimalGridBoundFEM::CPrimalGridBoundFEM(unsigned long val_elemGlobalID, unsigned long val_domainElementID,
+                                         unsigned short val_VTK_Type, unsigned short val_nPolyGrid,
+                                         unsigned short val_nDOFsGrid, std::vector<unsigned long>& val_nodes)
+    : CPrimalGrid(true, val_nDOFsGrid, 1) {
   /*--- Store the integer data in the member variables of this object. ---*/
   VTK_Type = val_VTK_Type;
 
@@ -41,51 +38,51 @@ CPrimalGridBoundFEM::CPrimalGridBoundFEM(unsigned long         val_elemGlobalID,
   nDOFsGrid = val_nDOFsGrid;
 
   boundElemIDGlobal = val_elemGlobalID;
-  GlobalIndex_DomainElement     = val_domainElementID;
+  GlobalIndex_DomainElement = val_domainElementID;
 
   /*--- Copy face structure of the element from val_nodes. ---*/
 
-  for(unsigned short i=0; i<nDOFsGrid; i++)
-    Nodes[i] = val_nodes[i];
+  for (unsigned short i = 0; i < nDOFsGrid; i++) Nodes[i] = val_nodes[i];
 
   /*--- For a linear quadrilateral the two last node numbers must be swapped,
         such that the element numbering is consistent with the FEM solver.    ---*/
 
-  if(nPolyGrid == 1 && VTK_Type == QUADRILATERAL) std::swap(Nodes[2], Nodes[3]);
+  if (nPolyGrid == 1 && VTK_Type == QUADRILATERAL) std::swap(Nodes[2], Nodes[3]);
 }
 
-void CPrimalGridBoundFEM::GetLocalCornerPointsFace(unsigned short elementType,
-                                                   unsigned short nPoly,
-                                                   unsigned short nDOFs,
-                                                   unsigned short &nPointsPerFace,
-                                                   unsigned long  faceConn[]) {
-
+void CPrimalGridBoundFEM::GetLocalCornerPointsFace(unsigned short elementType, unsigned short nPoly,
+                                                   unsigned short nDOFs, unsigned short& nPointsPerFace,
+                                                   unsigned long faceConn[]) {
   /*--- Determine the element type and set the face data accordingly.
         The faceConn values are local to the element.                 ---*/
 
-  switch( elementType ) {
+  switch (elementType) {
     case LINE:
       nPointsPerFace = 2;
-      faceConn[0] = 0; faceConn[1] = nPoly;
+      faceConn[0] = 0;
+      faceConn[1] = nPoly;
       break;
 
     case TRIANGLE:
       nPointsPerFace = 3;
-      faceConn[0] = 0; faceConn[1] = nPoly; faceConn[2] = nDOFs -1;
+      faceConn[0] = 0;
+      faceConn[1] = nPoly;
+      faceConn[2] = nDOFs - 1;
       break;
 
     case QUADRILATERAL:
-      unsigned short nn2 = nPoly*(nPoly+1);
+      unsigned short nn2 = nPoly * (nPoly + 1);
       nPointsPerFace = 4;
-      faceConn[0] = 0; faceConn[1] = nPoly; faceConn[2] = nDOFs -1; faceConn[3] = nn2;
+      faceConn[0] = 0;
+      faceConn[1] = nPoly;
+      faceConn[2] = nDOFs - 1;
+      faceConn[3] = nn2;
       break;
   }
 }
 
-void CPrimalGridBoundFEM::GetCornerPointsAllFaces(unsigned short &nFaces,
-                                                  unsigned short nPointsPerFace[],
-                                                  unsigned long  faceConn[6][4]) const {
-
+void CPrimalGridBoundFEM::GetCornerPointsAllFaces(unsigned short& nFaces, unsigned short nPointsPerFace[],
+                                                  unsigned long faceConn[6][4]) const {
   /*--- For compatibility reasons with the base class, nFaces is also an
         argument to this function. However, it is always 1, because the
         boundary element is the face.                                   ---*/
@@ -94,22 +91,17 @@ void CPrimalGridBoundFEM::GetCornerPointsAllFaces(unsigned short &nFaces,
   /*--- Get the corner points of the face local to the element. ---*/
 
   unsigned long thisFaceConn[4] = {0, 0, 0, 0};
-  GetLocalCornerPointsFace(VTK_Type, nPolyGrid, nDOFsGrid,
-                           nPointsPerFace[0], thisFaceConn);
-
+  GetLocalCornerPointsFace(VTK_Type, nPolyGrid, nDOFsGrid, nPointsPerFace[0], thisFaceConn);
 
   /*--- Convert the local values of thisFaceConn to global values. ---*/
 
-  for(unsigned short j=0; j<nPointsPerFace[0]; ++j)
-    faceConn[0][j] = Nodes[thisFaceConn[j]];
+  for (unsigned short j = 0; j < nPointsPerFace[0]; ++j) faceConn[0][j] = Nodes[thisFaceConn[j]];
 }
 
 void CPrimalGridBoundFEM::RemoveMultipleDonorsWallFunctions(void) {
-
   /* Sort donorElementsWallFunctions in increasing order and remove the
      the double entities. */
   std::sort(donorElementsWallFunctions.begin(), donorElementsWallFunctions.end());
-  auto lastEntry = std::unique(donorElementsWallFunctions.begin(),
-                               donorElementsWallFunctions.end());
+  auto lastEntry = std::unique(donorElementsWallFunctions.begin(), donorElementsWallFunctions.end());
   donorElementsWallFunctions.erase(lastEntry, donorElementsWallFunctions.end());
 }
diff --git a/Common/src/geometry/primal_grid/CPrimalGridFEM.cpp b/Common/src/geometry/primal_grid/CPrimalGridFEM.cpp
index 3740f1f3b4a..75d12b9067f 100644
--- a/Common/src/geometry/primal_grid/CPrimalGridFEM.cpp
+++ b/Common/src/geometry/primal_grid/CPrimalGridFEM.cpp
@@ -27,36 +27,32 @@
 
 #include "../../../include/geometry/primal_grid/CPrimalGridFEM.hpp"
 
-CPrimalGridFEM::CPrimalGridFEM(unsigned long  val_elemGlobalID, unsigned short val_VTK_Type,
-                               unsigned short val_nPolyGrid,    unsigned short val_nPolySol,
-                               unsigned short val_nDOFsGrid,    unsigned short val_nDOFsSol,
-                               unsigned long  val_offDOfsSol,   std::istringstream  &elem_line)
-  : CPrimalGrid(true, val_nDOFsGrid, nFacesOfElementType(val_VTK_Type))
-{
+CPrimalGridFEM::CPrimalGridFEM(unsigned long val_elemGlobalID, unsigned short val_VTK_Type,
+                               unsigned short val_nPolyGrid, unsigned short val_nPolySol, unsigned short val_nDOFsGrid,
+                               unsigned short val_nDOFsSol, unsigned long val_offDOfsSol, std::istringstream& elem_line)
+    : CPrimalGrid(true, val_nDOFsGrid, nFacesOfElementType(val_VTK_Type)) {
   /*--- Store the integer data in the member variables of this object. ---*/
   VTK_Type = val_VTK_Type;
   nFaces = nFacesOfElementType(VTK_Type);
 
   nPolyGrid = val_nPolyGrid;
-  nPolySol  = val_nPolySol;
+  nPolySol = val_nPolySol;
   nDOFsGrid = val_nDOFsGrid;
-  nDOFsSol  = val_nDOFsSol;
+  nDOFsSol = val_nDOFsSol;
 
-  elemIDGlobal        = val_elemGlobalID;
+  elemIDGlobal = val_elemGlobalID;
   offsetDOFsSolGlobal = val_offDOfsSol;
 
   /*--- Read face structure of the element from elem_line. ---*/
 
-  for(unsigned short i=0; i<nDOFsGrid; i++)
-    elem_line >> Nodes[i];
+  for (unsigned short i = 0; i < nDOFsGrid; i++) elem_line >> Nodes[i];
 
   /*--- If a linear element is used, the node numbering for non-simplices
         must be adapted. The reason is that compatability with the original
         SU2 format is maintained for linear elements, but for the FEM solver
         the nodes of the elements are stored row-wise.                       ---*/
-  if(nPolyGrid == 1){
-    switch( VTK_Type ) {
-
+  if (nPolyGrid == 1) {
+    switch (VTK_Type) {
       case QUADRILATERAL:
         std::swap(Nodes[2], Nodes[3]);
         break;
@@ -73,110 +69,190 @@ CPrimalGridFEM::CPrimalGridFEM(unsigned long  val_elemGlobalID, unsigned short v
   }
 }
 
-CPrimalGridFEM::CPrimalGridFEM(unsigned long  val_elemGlobalID, unsigned short val_VTK_Type,
-                               unsigned short val_nPolyGrid,    unsigned short val_nPolySol,
-                               unsigned short val_nDOFsGrid,    unsigned short val_nDOFsSol,
-                               unsigned long  val_offDOfsSol,   const unsigned long *connGrid)
-  : CPrimalGrid(true, val_nDOFsGrid, nFacesOfElementType(val_VTK_Type))
-{
+CPrimalGridFEM::CPrimalGridFEM(unsigned long val_elemGlobalID, unsigned short val_VTK_Type,
+                               unsigned short val_nPolyGrid, unsigned short val_nPolySol, unsigned short val_nDOFsGrid,
+                               unsigned short val_nDOFsSol, unsigned long val_offDOfsSol, const unsigned long* connGrid)
+    : CPrimalGrid(true, val_nDOFsGrid, nFacesOfElementType(val_VTK_Type)) {
   /*--- Store the integer data in the member variables of this object. ---*/
   VTK_Type = val_VTK_Type;
   nFaces = nFacesOfElementType(VTK_Type);
 
   nPolyGrid = val_nPolyGrid;
-  nPolySol  = val_nPolySol;
+  nPolySol = val_nPolySol;
   nDOFsGrid = val_nDOFsGrid;
-  nDOFsSol  = val_nDOFsSol;
+  nDOFsSol = val_nDOFsSol;
 
-  elemIDGlobal        = val_elemGlobalID;
+  elemIDGlobal = val_elemGlobalID;
   offsetDOFsSolGlobal = val_offDOfsSol;
 
   /*--- Copy face structure of the element from connGrid. ---*/
-  for(unsigned short i=0; i<nDOFsGrid; i++)
-    Nodes[i] = connGrid[i];
+  for (unsigned short i = 0; i < nDOFsGrid; i++) Nodes[i] = connGrid[i];
 }
 
-void CPrimalGridFEM::GetLocalCornerPointsAllFaces(unsigned short elementType,
-                                                  unsigned short nPoly,
-                                                  unsigned short nDOFs,
-                                                  unsigned short &numFaces,
-                                                  unsigned short nPointsPerFace[],
-                                                  unsigned long  faceConn[6][4]) {
-
+void CPrimalGridFEM::GetLocalCornerPointsAllFaces(unsigned short elementType, unsigned short nPoly,
+                                                  unsigned short nDOFs, unsigned short& numFaces,
+                                                  unsigned short nPointsPerFace[], unsigned long faceConn[6][4]) {
   /*--- Determine the element type and set the face data accordingly.
         The faceConn values are local to the element.                 ---*/
 
   numFaces = nFacesOfElementType(elementType);
   unsigned short nn2, nn3, nn4;
-  switch( elementType ) {
+  switch (elementType) {
     case TRIANGLE:
-      nPointsPerFace[0] = 2; faceConn[0][0] = 0;        faceConn[0][1] = nPoly;
-      nPointsPerFace[1] = 2; faceConn[1][0] = nPoly;    faceConn[1][1] = nDOFs -1;
-      nPointsPerFace[2] = 2; faceConn[2][0] = nDOFs -1; faceConn[2][1] = 0;
+      nPointsPerFace[0] = 2;
+      faceConn[0][0] = 0;
+      faceConn[0][1] = nPoly;
+      nPointsPerFace[1] = 2;
+      faceConn[1][0] = nPoly;
+      faceConn[1][1] = nDOFs - 1;
+      nPointsPerFace[2] = 2;
+      faceConn[2][0] = nDOFs - 1;
+      faceConn[2][1] = 0;
       break;
 
     case QUADRILATERAL:
-      nn2 = nPoly*(nPoly+1);
-      nPointsPerFace[0] = 2; faceConn[0][0] = 0;        faceConn[0][1] = nPoly;
-      nPointsPerFace[1] = 2; faceConn[1][0] = nPoly;    faceConn[1][1] = nDOFs -1;
-      nPointsPerFace[2] = 2; faceConn[2][0] = nDOFs -1; faceConn[2][1] = nn2;
-      nPointsPerFace[3] = 2; faceConn[3][0] = nn2;      faceConn[3][1] = 0;
+      nn2 = nPoly * (nPoly + 1);
+      nPointsPerFace[0] = 2;
+      faceConn[0][0] = 0;
+      faceConn[0][1] = nPoly;
+      nPointsPerFace[1] = 2;
+      faceConn[1][0] = nPoly;
+      faceConn[1][1] = nDOFs - 1;
+      nPointsPerFace[2] = 2;
+      faceConn[2][0] = nDOFs - 1;
+      faceConn[2][1] = nn2;
+      nPointsPerFace[3] = 2;
+      faceConn[3][0] = nn2;
+      faceConn[3][1] = 0;
       break;
 
     case TETRAHEDRON:
-      nn2 = (nPoly+1)*(nPoly+2)/2 -1; nn3 = nDOFs -1;
-      nPointsPerFace[0] = 3; faceConn[0][0] = 0;     faceConn[0][1] = nPoly; faceConn[0][2] = nn2;
-      nPointsPerFace[1] = 3; faceConn[1][0] = 0;     faceConn[1][1] = nn3;   faceConn[1][2] = nPoly;
-      nPointsPerFace[2] = 3; faceConn[2][0] = 0;     faceConn[2][1] = nn2;   faceConn[2][2] = nn3;
-      nPointsPerFace[3] = 3; faceConn[3][0] = nPoly; faceConn[3][1] = nn3;   faceConn[3][2] = nn2;
+      nn2 = (nPoly + 1) * (nPoly + 2) / 2 - 1;
+      nn3 = nDOFs - 1;
+      nPointsPerFace[0] = 3;
+      faceConn[0][0] = 0;
+      faceConn[0][1] = nPoly;
+      faceConn[0][2] = nn2;
+      nPointsPerFace[1] = 3;
+      faceConn[1][0] = 0;
+      faceConn[1][1] = nn3;
+      faceConn[1][2] = nPoly;
+      nPointsPerFace[2] = 3;
+      faceConn[2][0] = 0;
+      faceConn[2][1] = nn2;
+      faceConn[2][2] = nn3;
+      nPointsPerFace[3] = 3;
+      faceConn[3][0] = nPoly;
+      faceConn[3][1] = nn3;
+      faceConn[3][2] = nn2;
       break;
 
     case PYRAMID:
-      nn2 = (nPoly+1)*(nPoly+1) -1; nn3 = nn2 - nPoly;
-      nPointsPerFace[0] = 4; faceConn[0][0] = 0;     faceConn[0][1] = nPoly;    faceConn[0][2] = nn2; faceConn[0][3] = nn3;
-      nPointsPerFace[1] = 3; faceConn[1][0] = 0;     faceConn[1][1] = nDOFs -1; faceConn[1][2] = nPoly;
-      nPointsPerFace[2] = 3; faceConn[2][0] = nn3;   faceConn[2][1] = nn2;      faceConn[2][2] = nDOFs -1;
-      nPointsPerFace[3] = 3; faceConn[3][0] = 0;     faceConn[3][1] = nn3;      faceConn[3][2] = nDOFs -1;
-      nPointsPerFace[4] = 3; faceConn[4][0] = nPoly; faceConn[4][1] = nDOFs -1; faceConn[4][2] = nn2;
+      nn2 = (nPoly + 1) * (nPoly + 1) - 1;
+      nn3 = nn2 - nPoly;
+      nPointsPerFace[0] = 4;
+      faceConn[0][0] = 0;
+      faceConn[0][1] = nPoly;
+      faceConn[0][2] = nn2;
+      faceConn[0][3] = nn3;
+      nPointsPerFace[1] = 3;
+      faceConn[1][0] = 0;
+      faceConn[1][1] = nDOFs - 1;
+      faceConn[1][2] = nPoly;
+      nPointsPerFace[2] = 3;
+      faceConn[2][0] = nn3;
+      faceConn[2][1] = nn2;
+      faceConn[2][2] = nDOFs - 1;
+      nPointsPerFace[3] = 3;
+      faceConn[3][0] = 0;
+      faceConn[3][1] = nn3;
+      faceConn[3][2] = nDOFs - 1;
+      nPointsPerFace[4] = 3;
+      faceConn[4][0] = nPoly;
+      faceConn[4][1] = nDOFs - 1;
+      faceConn[4][2] = nn2;
       break;
 
     case PRISM:
-      nn2 = (nPoly+1)*(nPoly+2)/2; nn3 = nPoly*nn2; --nn2;
-      nPointsPerFace[0] = 3; faceConn[0][0] = 0;     faceConn[0][1] = nPoly;     faceConn[0][2] = nn2;
-      nPointsPerFace[1] = 3; faceConn[1][0] = nn3;   faceConn[1][1] = nn2+nn3;   faceConn[1][2] = nPoly+nn3;
-      nPointsPerFace[2] = 4; faceConn[2][0] = 0;     faceConn[2][1] = nn3;       faceConn[2][2] = nPoly+nn3; faceConn[2][3] = nPoly;
-      nPointsPerFace[3] = 4; faceConn[3][0] = 0;     faceConn[3][1] = nn2;       faceConn[3][2] = nn2+nn3;   faceConn[3][3] = nn3;
-      nPointsPerFace[4] = 4; faceConn[4][0] = nPoly; faceConn[4][1] = nPoly+nn3; faceConn[4][2] = nn2+nn3;   faceConn[4][3] = nn2;
+      nn2 = (nPoly + 1) * (nPoly + 2) / 2;
+      nn3 = nPoly * nn2;
+      --nn2;
+      nPointsPerFace[0] = 3;
+      faceConn[0][0] = 0;
+      faceConn[0][1] = nPoly;
+      faceConn[0][2] = nn2;
+      nPointsPerFace[1] = 3;
+      faceConn[1][0] = nn3;
+      faceConn[1][1] = nn2 + nn3;
+      faceConn[1][2] = nPoly + nn3;
+      nPointsPerFace[2] = 4;
+      faceConn[2][0] = 0;
+      faceConn[2][1] = nn3;
+      faceConn[2][2] = nPoly + nn3;
+      faceConn[2][3] = nPoly;
+      nPointsPerFace[3] = 4;
+      faceConn[3][0] = 0;
+      faceConn[3][1] = nn2;
+      faceConn[3][2] = nn2 + nn3;
+      faceConn[3][3] = nn3;
+      nPointsPerFace[4] = 4;
+      faceConn[4][0] = nPoly;
+      faceConn[4][1] = nPoly + nn3;
+      faceConn[4][2] = nn2 + nn3;
+      faceConn[4][3] = nn2;
       break;
 
     case HEXAHEDRON:
-      nn2 = (nPoly+1)*(nPoly+1); nn4 = nPoly*nn2; --nn2; nn3 = nn2 - nPoly;
-      nPointsPerFace[0] = 4; faceConn[0][0] = 0;     faceConn[0][1] = nPoly;     faceConn[0][2] = nn2;       faceConn[0][3] = nn3;
-      nPointsPerFace[1] = 4; faceConn[1][0] = nn4;   faceConn[1][1] = nn3+nn4;   faceConn[1][2] = nn2+nn4;   faceConn[1][3] = nPoly+nn4;
-      nPointsPerFace[2] = 4; faceConn[2][0] = 0;     faceConn[2][1] = nn4;       faceConn[2][2] = nPoly+nn4; faceConn[2][3] = nPoly;
-      nPointsPerFace[3] = 4; faceConn[3][0] = nn3;   faceConn[3][1] = nn2;       faceConn[3][2] = nn2+nn4;   faceConn[3][3] = nn3+nn4;
-      nPointsPerFace[4] = 4; faceConn[4][0] = 0;     faceConn[4][1] = nn3;       faceConn[4][2] = nn3+nn4;   faceConn[4][3] = nn4;
-      nPointsPerFace[5] = 4; faceConn[5][0] = nPoly; faceConn[5][1] = nPoly+nn4; faceConn[5][2] = nn2+nn4;   faceConn[5][3] = nn2;
+      nn2 = (nPoly + 1) * (nPoly + 1);
+      nn4 = nPoly * nn2;
+      --nn2;
+      nn3 = nn2 - nPoly;
+      nPointsPerFace[0] = 4;
+      faceConn[0][0] = 0;
+      faceConn[0][1] = nPoly;
+      faceConn[0][2] = nn2;
+      faceConn[0][3] = nn3;
+      nPointsPerFace[1] = 4;
+      faceConn[1][0] = nn4;
+      faceConn[1][1] = nn3 + nn4;
+      faceConn[1][2] = nn2 + nn4;
+      faceConn[1][3] = nPoly + nn4;
+      nPointsPerFace[2] = 4;
+      faceConn[2][0] = 0;
+      faceConn[2][1] = nn4;
+      faceConn[2][2] = nPoly + nn4;
+      faceConn[2][3] = nPoly;
+      nPointsPerFace[3] = 4;
+      faceConn[3][0] = nn3;
+      faceConn[3][1] = nn2;
+      faceConn[3][2] = nn2 + nn4;
+      faceConn[3][3] = nn3 + nn4;
+      nPointsPerFace[4] = 4;
+      faceConn[4][0] = 0;
+      faceConn[4][1] = nn3;
+      faceConn[4][2] = nn3 + nn4;
+      faceConn[4][3] = nn4;
+      nPointsPerFace[5] = 4;
+      faceConn[5][0] = nPoly;
+      faceConn[5][1] = nPoly + nn4;
+      faceConn[5][2] = nn2 + nn4;
+      faceConn[5][3] = nn2;
       break;
   }
 }
 
-void CPrimalGridFEM::GetCornerPointsAllFaces(unsigned short &numFaces,
-                                             unsigned short nPointsPerFace[],
-                                             unsigned long  faceConn[6][4]) const {
-
+void CPrimalGridFEM::GetCornerPointsAllFaces(unsigned short& numFaces, unsigned short nPointsPerFace[],
+                                             unsigned long faceConn[6][4]) const {
   /*--- Get the corner points of the faces local to the element. ---*/
 
-  GetLocalCornerPointsAllFaces(VTK_Type, nPolyGrid, nDOFsGrid,
-                               numFaces, nPointsPerFace, faceConn);
+  GetLocalCornerPointsAllFaces(VTK_Type, nPolyGrid, nDOFsGrid, numFaces, nPointsPerFace, faceConn);
 
   /*--- Convert the local values of faceConn to global values. ---*/
 
-  for(unsigned short i=0; i<numFaces; ++i) {
-    for(unsigned short j=0; j<nPointsPerFace[i]; ++j) {
+  for (unsigned short i = 0; i < numFaces; ++i) {
+    for (unsigned short j = 0; j < nPointsPerFace[i]; ++j) {
       unsigned long nn = faceConn[i][j];
       faceConn[i][j] = Nodes[nn];
     }
   }
-
 }
diff --git a/Common/src/geometry/primal_grid/CPrism.cpp b/Common/src/geometry/primal_grid/CPrism.cpp
index 0442d0b5664..c3998a0ba0b 100644
--- a/Common/src/geometry/primal_grid/CPrism.cpp
+++ b/Common/src/geometry/primal_grid/CPrism.cpp
@@ -33,11 +33,9 @@ constexpr unsigned short CPrismConnectivity::Faces[5][4];
 constexpr unsigned short CPrismConnectivity::nNeighbor_Nodes[6];
 constexpr unsigned short CPrismConnectivity::Neighbor_Nodes[6][3];
 
-CPrism::CPrism(unsigned long val_point_0, unsigned long val_point_1,
-         unsigned long val_point_2, unsigned long val_point_3,
-         unsigned long val_point_4, unsigned long val_point_5):
-  CPrimalGridWithConnectivity<CPrismConnectivity>(false)
-{
+CPrism::CPrism(unsigned long val_point_0, unsigned long val_point_1, unsigned long val_point_2,
+               unsigned long val_point_3, unsigned long val_point_4, unsigned long val_point_5)
+    : CPrimalGridWithConnectivity<CPrismConnectivity>(false) {
   /*--- Define face structure of the element ---*/
   Nodes[0] = val_point_0;
   Nodes[1] = val_point_1;
diff --git a/Common/src/geometry/primal_grid/CPyramid.cpp b/Common/src/geometry/primal_grid/CPyramid.cpp
index f75aac437f0..38baeaae45e 100644
--- a/Common/src/geometry/primal_grid/CPyramid.cpp
+++ b/Common/src/geometry/primal_grid/CPyramid.cpp
@@ -33,11 +33,9 @@ constexpr unsigned short CPyramidConnectivity::Faces[5][4];
 constexpr unsigned short CPyramidConnectivity::nNeighbor_Nodes[5];
 constexpr unsigned short CPyramidConnectivity::Neighbor_Nodes[5][4];
 
-CPyramid::CPyramid(unsigned long val_point_0, unsigned long val_point_1,
-           unsigned long val_point_2, unsigned long val_point_3,
-           unsigned long val_point_4):
-  CPrimalGridWithConnectivity<CPyramidConnectivity>(false)
-{
+CPyramid::CPyramid(unsigned long val_point_0, unsigned long val_point_1, unsigned long val_point_2,
+                   unsigned long val_point_3, unsigned long val_point_4)
+    : CPrimalGridWithConnectivity<CPyramidConnectivity>(false) {
   /*--- Define face structure of the element ---*/
   Nodes[0] = val_point_0;
   Nodes[1] = val_point_1;
@@ -46,6 +44,4 @@ CPyramid::CPyramid(unsigned long val_point_0, unsigned long val_point_1,
   Nodes[4] = val_point_4;
 }
 
-void CPyramid::Change_Orientation() {
-  std::swap(Nodes[1],Nodes[3]);
-}
+void CPyramid::Change_Orientation() { std::swap(Nodes[1], Nodes[3]); }
diff --git a/Common/src/geometry/primal_grid/CQuadrilateral.cpp b/Common/src/geometry/primal_grid/CQuadrilateral.cpp
index 643e10209b8..fab0b7a280a 100644
--- a/Common/src/geometry/primal_grid/CQuadrilateral.cpp
+++ b/Common/src/geometry/primal_grid/CQuadrilateral.cpp
@@ -33,10 +33,9 @@ constexpr unsigned short CQuadrilateralConnectivity::Faces[4][2];
 constexpr unsigned short CQuadrilateralConnectivity::nNeighbor_Nodes[4];
 constexpr unsigned short CQuadrilateralConnectivity::Neighbor_Nodes[4][2];
 
-CQuadrilateral::CQuadrilateral(unsigned long val_point_0, unsigned long val_point_1,
-             unsigned long val_point_2, unsigned long val_point_3):
-  CPrimalGridWithConnectivity<CQuadrilateralConnectivity>(false)
-{
+CQuadrilateral::CQuadrilateral(unsigned long val_point_0, unsigned long val_point_1, unsigned long val_point_2,
+                               unsigned long val_point_3)
+    : CPrimalGridWithConnectivity<CQuadrilateralConnectivity>(false) {
   /*--- Define face structure of the element ---*/
   Nodes[0] = val_point_0;
   Nodes[1] = val_point_1;
@@ -44,6 +43,4 @@ CQuadrilateral::CQuadrilateral(unsigned long val_point_0, unsigned long val_poin
   Nodes[3] = val_point_3;
 }
 
-void CQuadrilateral::Change_Orientation() {
-  std::swap(Nodes[1], Nodes[3]);
-}
+void CQuadrilateral::Change_Orientation() { std::swap(Nodes[1], Nodes[3]); }
diff --git a/Common/src/geometry/primal_grid/CTetrahedron.cpp b/Common/src/geometry/primal_grid/CTetrahedron.cpp
index 0c82ac1ef45..78a9ae6de17 100644
--- a/Common/src/geometry/primal_grid/CTetrahedron.cpp
+++ b/Common/src/geometry/primal_grid/CTetrahedron.cpp
@@ -33,10 +33,9 @@ constexpr unsigned short CTetrahedronConnectivity::Faces[4][3];
 constexpr unsigned short CTetrahedronConnectivity::nNeighbor_Nodes[4];
 constexpr unsigned short CTetrahedronConnectivity::Neighbor_Nodes[4][3];
 
-CTetrahedron::CTetrahedron(unsigned long val_point_0, unsigned long val_point_1,
-               unsigned long val_point_2, unsigned long val_point_3):
-  CPrimalGridWithConnectivity<CTetrahedronConnectivity>(false)
-{
+CTetrahedron::CTetrahedron(unsigned long val_point_0, unsigned long val_point_1, unsigned long val_point_2,
+                           unsigned long val_point_3)
+    : CPrimalGridWithConnectivity<CTetrahedronConnectivity>(false) {
   /*--- Define face structure of the element ---*/
   Nodes[0] = val_point_0;
   Nodes[1] = val_point_1;
@@ -44,6 +43,4 @@ CTetrahedron::CTetrahedron(unsigned long val_point_0, unsigned long val_point_1,
   Nodes[3] = val_point_3;
 }
 
-void CTetrahedron::Change_Orientation() {
-  std::swap(Nodes[0],Nodes[1]);
-}
+void CTetrahedron::Change_Orientation() { std::swap(Nodes[0], Nodes[1]); }
diff --git a/Common/src/geometry/primal_grid/CTriangle.cpp b/Common/src/geometry/primal_grid/CTriangle.cpp
index 8f5dbdfa1c8..36370731c4d 100644
--- a/Common/src/geometry/primal_grid/CTriangle.cpp
+++ b/Common/src/geometry/primal_grid/CTriangle.cpp
@@ -33,10 +33,8 @@ constexpr unsigned short CTriangleConnectivity::Faces[3][2];
 constexpr unsigned short CTriangleConnectivity::nNeighbor_Nodes[3];
 constexpr unsigned short CTriangleConnectivity::Neighbor_Nodes[3][2];
 
-CTriangle::CTriangle(unsigned long val_point_0, unsigned long val_point_1,
-           unsigned long val_point_2):
-  CPrimalGridWithConnectivity<CTriangleConnectivity>(false)
-{
+CTriangle::CTriangle(unsigned long val_point_0, unsigned long val_point_1, unsigned long val_point_2)
+    : CPrimalGridWithConnectivity<CTriangleConnectivity>(false) {
   /*--- Define face structure of the element ---*/
   Nodes[0] = val_point_0;
   Nodes[1] = val_point_1;
diff --git a/Common/src/geometry/primal_grid/CVertexMPI.cpp b/Common/src/geometry/primal_grid/CVertexMPI.cpp
index 7fe7451cce5..0de612a88bf 100644
--- a/Common/src/geometry/primal_grid/CVertexMPI.cpp
+++ b/Common/src/geometry/primal_grid/CVertexMPI.cpp
@@ -32,9 +32,7 @@ constexpr unsigned short CVertexMPIConnectivity::Faces[1][1];
 constexpr unsigned short CVertexMPIConnectivity::nNeighbor_Nodes[1];
 constexpr unsigned short CVertexMPIConnectivity::Neighbor_Nodes[1][1];
 
-CVertexMPI::CVertexMPI(unsigned long val_point):
-  CPrimalGridWithConnectivity<CVertexMPIConnectivity>(false)
-{
+CVertexMPI::CVertexMPI(unsigned long val_point) : CPrimalGridWithConnectivity<CVertexMPIConnectivity>(false) {
   /*--- Define face structure of the element ---*/
   Nodes[0] = val_point;
 
diff --git a/Common/src/graph_coloring_structure.cpp b/Common/src/graph_coloring_structure.cpp
index 1b661765d9b..16755851014 100644
--- a/Common/src/graph_coloring_structure.cpp
+++ b/Common/src/graph_coloring_structure.cpp
@@ -28,15 +28,11 @@
 #include "../include/graph_coloring_structure.hpp"
 
 /* Function, which determines the colors for the vertices of the given graph. */
-void CGraphColoringStructure::GraphVertexColoring(
-                         CConfig                              *config,
-                         const vector<unsigned long>          &nVerticesPerRank,
-                         const vector<vector<unsigned long> > &entriesVertices,
-                         int                                  &nGlobalColors,
-                         vector<int>                          &colorLocalVertices) {
-
+void CGraphColoringStructure::GraphVertexColoring(CConfig* config, const vector<unsigned long>& nVerticesPerRank,
+                                                  const vector<vector<unsigned long> >& entriesVertices,
+                                                  int& nGlobalColors, vector<int>& colorLocalVertices) {
   /* Determine the number of ranks and the current rank. */
-  int nRank  = 1;
+  int nRank = 1;
   int myRank = 0;
 
 #ifdef HAVE_MPI
@@ -45,14 +41,11 @@ void CGraphColoringStructure::GraphVertexColoring(
 #endif
 
   /*--- Determine the algorithm to use for the graph coloring. ---*/
-  switch( config->GetKind_Matrix_Coloring() ) {
-
+  switch (config->GetKind_Matrix_Coloring()) {
     case GREEDY_COLORING: {
-
       /* Greedy algorithm, which is implemented sequentially.
          Make a distinction between the master rank and the other ranks. */
-      if(myRank == 0) {
-
+      if (myRank == 0) {
         /*--------------------------------------------------------------------*/
         /*             Master node, which does all the work.                  */
         /* Step 1: Create the global vector for the graph by gathering all the*/
@@ -63,16 +56,13 @@ void CGraphColoringStructure::GraphVertexColoring(
         /**************************************************************************/
 
         /* Define the global vector and copy my data in it. */
-        vector<vector<unsigned long> > entriesVert(nVerticesPerRank[nRank],
-                                                   vector<unsigned long>(0));
+        vector<vector<unsigned long> > entriesVert(nVerticesPerRank[nRank], vector<unsigned long>(0));
 
-        for(unsigned long i=nVerticesPerRank[0]; i<nVerticesPerRank[1]; ++i)
-          entriesVert[i] = entriesVertices[i];
+        for (unsigned long i = nVerticesPerRank[0]; i < nVerticesPerRank[1]; ++i) entriesVert[i] = entriesVertices[i];
 
-        /* Receive the data from the other ranks. Only needed in parallel mode. */
+          /* Receive the data from the other ranks. Only needed in parallel mode. */
 #ifdef HAVE_MPI
-        for(int rank=1; rank<nRank; ++rank) {
-
+        for (int rank = 1; rank < nRank; ++rank) {
           /* Determine the size of the message to be received. */
           SU2_MPI::Status status;
           SU2_MPI::Probe(rank, rank, SU2_MPI::GetComm(), &status);
@@ -82,17 +72,15 @@ void CGraphColoringStructure::GraphVertexColoring(
 
           /* Allocate the memory for the receive buffer and receive the message. */
           vector<unsigned long> recvBuf(sizeMess);
-          SU2_MPI::Recv(recvBuf.data(), sizeMess, MPI_UNSIGNED_LONG, rank, rank,
-                        SU2_MPI::GetComm(), &status);
+          SU2_MPI::Recv(recvBuf.data(), sizeMess, MPI_UNSIGNED_LONG, rank, rank, SU2_MPI::GetComm(), &status);
 
           /* Store the data just received in the global vector for the graph. */
           unsigned long ii = 0;
-          for(unsigned long i=nVerticesPerRank[rank]; i<nVerticesPerRank[rank+1]; ++i) {
+          for (unsigned long i = nVerticesPerRank[rank]; i < nVerticesPerRank[rank + 1]; ++i) {
             const unsigned long nEntries = recvBuf[ii++];
 
             entriesVert[i].resize(nEntries);
-            for(unsigned long j=0; j<nEntries; ++j, ++ii)
-              entriesVert[i][j] = recvBuf[ii];
+            for (unsigned long j = 0; j < nEntries; ++j, ++ii) entriesVert[i][j] = recvBuf[ii];
           }
         }
 #endif
@@ -106,40 +94,38 @@ void CGraphColoringStructure::GraphVertexColoring(
 
         /* Allocate and reserve the memory for vectors that are used
            in the greedy algorithm. */
-        vector<unsigned long> flagColorStored(nVerticesPerRank[nRank],
-                                              nVerticesPerRank[nRank]);
+        vector<unsigned long> flagColorStored(nVerticesPerRank[nRank], nVerticesPerRank[nRank]);
         vector<int> colorNeighbors;
         colorNeighbors.reserve(1000);
 
         /* Loop over the vertices of the graph. */
-        for(unsigned long i=0; i<nVerticesPerRank[nRank]; ++i) {
-
+        for (unsigned long i = 0; i < nVerticesPerRank[nRank]; ++i) {
           /* Make sure that colorNeighbors is empty. */
           colorNeighbors.resize(0);
 
           /* Loop over the entries of this vertex. */
-          for(unsigned long j=0; j<entriesVert[i].size(); ++j) {
+          for (unsigned long j = 0; j < entriesVert[i].size(); ++j) {
             const unsigned long jj = entriesVert[i][j];
 
             /* Add the color of jj if jj is less than i and if its color
                is not stored yet. */
-            if(jj < i) {
+            if (jj < i) {
               const int cJJ = colorVertices[jj];
-              if(flagColorStored[cJJ] != i) {
+              if (flagColorStored[cJJ] != i) {
                 flagColorStored[cJJ] = i;
                 colorNeighbors.push_back(cJJ);
               }
             }
 
             /* Loop over the entries of vertex jj. */
-            for(unsigned long k=0; k<entriesVert[jj].size(); ++k) {
+            for (unsigned long k = 0; k < entriesVert[jj].size(); ++k) {
               const unsigned long kk = entriesVert[jj][k];
 
               /* Add the color of kk if kk is less than i and if its color
                  is not stored yet. */
-              if(kk < i) {
+              if (kk < i) {
                 const int cKK = colorVertices[kk];
-                if(flagColorStored[cKK] != i) {
+                if (flagColorStored[cKK] != i) {
                   flagColorStored[cKK] = i;
                   colorNeighbors.push_back(cKK);
                 }
@@ -152,8 +138,8 @@ void CGraphColoringStructure::GraphVertexColoring(
 
           /* Determine the color of this vertex. */
           int cVert;
-          for(cVert=0; cVert<(int) colorNeighbors.size(); ++cVert) {
-            if(cVert != colorNeighbors[cVert]) break;
+          for (cVert = 0; cVert < (int)colorNeighbors.size(); ++cVert) {
+            if (cVert != colorNeighbors[cVert]) break;
           }
 
           colorVertices[i] = cVert;
@@ -161,13 +147,12 @@ void CGraphColoringStructure::GraphVertexColoring(
 
         /* Check if the coloring is done correctly. */
         flagColorStored.assign(nVerticesPerRank[nRank], nVerticesPerRank[nRank]);
-        for(unsigned long i=0; i<entriesVert.size(); ++i) {
-          for(unsigned long j=0; j<entriesVert[i].size(); ++j) {
+        for (unsigned long i = 0; i < entriesVert.size(); ++i) {
+          for (unsigned long j = 0; j < entriesVert[i].size(); ++j) {
             const int cJJ = colorVertices[entriesVert[i][j]];
-            if(flagColorStored[cJJ] == i) {
+            if (flagColorStored[cJJ] == i) {
               cout << "In function GraphVertexColoring: Color " << cJJ
-                   << " appears more than once in the stencil of vertex "
-                   << i << "." << endl;
+                   << " appears more than once in the stencil of vertex " << i << "." << endl;
               exit(1);
             }
             flagColorStored[cJJ] = i;
@@ -180,16 +165,15 @@ void CGraphColoringStructure::GraphVertexColoring(
 
         /* Store the data of the root rank. */
         colorLocalVertices.resize(nVerticesPerRank[1]);
-        memcpy(colorLocalVertices.data(), colorVertices.data(),
-               nVerticesPerRank[1]*sizeof(int));
+        memcpy(colorLocalVertices.data(), colorVertices.data(), nVerticesPerRank[1] * sizeof(int));
 
         /* Send the color of the vertices to the other ranks. Only in parallel
            mode. Use blocking sends, because deadlock cannot occur. */
 #ifdef HAVE_MPI
-        for(int rank=1; rank<nRank; ++rank) {
-          int *sendBuf = colorVertices.data() + nVerticesPerRank[rank];
-          unsigned long sizeMess = nVerticesPerRank[rank+1] - nVerticesPerRank[rank];
-          SU2_MPI::Send(sendBuf, sizeMess, MPI_INT, rank, rank+1, SU2_MPI::GetComm());
+        for (int rank = 1; rank < nRank; ++rank) {
+          int* sendBuf = colorVertices.data() + nVerticesPerRank[rank];
+          unsigned long sizeMess = nVerticesPerRank[rank + 1] - nVerticesPerRank[rank];
+          SU2_MPI::Send(sendBuf, sizeMess, MPI_INT, rank, rank + 1, SU2_MPI::GetComm());
         }
 #endif
       }
@@ -198,40 +182,35 @@ void CGraphColoringStructure::GraphVertexColoring(
         /* Not the master node. Communicate the data of my graph to the master
            node. First copy the data in a buffer.  */
         vector<unsigned long> sendBuf;
-        for(unsigned long i=0; i<entriesVertices.size(); ++i) {
+        for (unsigned long i = 0; i < entriesVertices.size(); ++i) {
           sendBuf.push_back(entriesVertices[i].size());
-          sendBuf.insert(sendBuf.end(), entriesVertices[i].begin(),
-                         entriesVertices[i].end());
+          sendBuf.insert(sendBuf.end(), entriesVertices[i].begin(), entriesVertices[i].end());
         }
 
         /* Send the data to the master node. A blocking send can be used,
            because there is no danger of deadlock here. */
-        SU2_MPI::Send(sendBuf.data(), sendBuf.size(), MPI_UNSIGNED_LONG, 0,
-                      myRank, SU2_MPI::GetComm());
+        SU2_MPI::Send(sendBuf.data(), sendBuf.size(), MPI_UNSIGNED_LONG, 0, myRank, SU2_MPI::GetComm());
 
         /* Receive the data for the colors of my locally owned DOFs. */
         unsigned long nLocalVert = entriesVertices.size();
         colorLocalVertices.resize(nLocalVert);
 
         SU2_MPI::Status status;
-        SU2_MPI::Recv(colorLocalVertices.data(), nLocalVert, MPI_INT, 0, myRank+1,
-                      SU2_MPI::GetComm(), &status);
+        SU2_MPI::Recv(colorLocalVertices.data(), nLocalVert, MPI_INT, 0, myRank + 1, SU2_MPI::GetComm(), &status);
       }
 #endif
       break;
     }
 
-    /*-----------------------------------------------------------------------*/
+      /*-----------------------------------------------------------------------*/
 
     case NATURAL_COLORING: {
-
       /* Natural coloring, i.e. every DOF gets its own color. This is very
         inefficient and should only be used for debugging. */
       unsigned long nLocalVert = entriesVertices.size();
       colorLocalVertices.resize(nLocalVert);
 
-      for(unsigned long i=0; i<nLocalVert; ++i)
-        colorLocalVertices[i] = (int)(i + nVerticesPerRank[myRank]);
+      for (unsigned long i = 0; i < nLocalVert; ++i) colorLocalVertices[i] = (int)(i + nVerticesPerRank[myRank]);
 
       break;
     }
@@ -239,13 +218,11 @@ void CGraphColoringStructure::GraphVertexColoring(
 
   /* Determine the total (global) number of colors. */
   int nLocalColors = 0;
-  for(unsigned long i=0; i<colorLocalVertices.size(); ++i)
-    nLocalColors = max(nLocalColors, colorLocalVertices[i]);
+  for (unsigned long i = 0; i < colorLocalVertices.size(); ++i) nLocalColors = max(nLocalColors, colorLocalVertices[i]);
   ++nLocalColors;
 
 #ifdef HAVE_MPI
-  SU2_MPI::Allreduce(&nLocalColors, &nGlobalColors, 1, MPI_INT,
-                     MPI_MAX, SU2_MPI::GetComm());
+  SU2_MPI::Allreduce(&nLocalColors, &nGlobalColors, 1, MPI_INT, MPI_MAX, SU2_MPI::GetComm());
 #else
   nGlobalColors = nLocalColors;
 #endif
diff --git a/Common/src/grid_movement/CBSplineBlending.cpp b/Common/src/grid_movement/CBSplineBlending.cpp
index b7568c7942a..8dad4572be6 100644
--- a/Common/src/grid_movement/CBSplineBlending.cpp
+++ b/Common/src/grid_movement/CBSplineBlending.cpp
@@ -28,18 +28,17 @@
 #include "../../include/grid_movement/CBSplineBlending.hpp"
 #include "../../include/parallelization/mpi_structure.hpp"
 
-CBSplineBlending::CBSplineBlending(short val_order, short n_controlpoints): CFreeFormBlending(){
+CBSplineBlending::CBSplineBlending(short val_order, short n_controlpoints) : CFreeFormBlending() {
   SetOrder(val_order, n_controlpoints);
 }
 
-CBSplineBlending::~CBSplineBlending(){}
-
-void CBSplineBlending::SetOrder(short val_order, short n_controlpoints){
+CBSplineBlending::~CBSplineBlending() {}
 
+void CBSplineBlending::SetOrder(short val_order, short n_controlpoints) {
   unsigned short iKnot;
 
-  Order    = val_order;
-  Degree   = Order - 1;
+  Order = val_order;
+  Degree = Order - 1;
   nControl = n_controlpoints;
 
   KnotSize = Order + nControl;
@@ -52,11 +51,11 @@ void CBSplineBlending::SetOrder(short val_order, short n_controlpoints){
 
   /*--- The next knots are equidistantly distributed in [0,1] ---*/
 
-  for (iKnot = 0; iKnot < nControl - Order; iKnot++){
-    U[Order + iKnot] = su2double(iKnot+1)/su2double(nControl - Order + 1);
+  for (iKnot = 0; iKnot < nControl - Order; iKnot++) {
+    U[Order + iKnot] = su2double(iKnot + 1) / su2double(nControl - Order + 1);
   }
-  for (iKnot = nControl - Order; iKnot < nControl; iKnot++){
-    U[Order + iKnot]  = 1.0;
+  for (iKnot = nControl - Order; iKnot < nControl; iKnot++) {
+    U[Order + iKnot] = 1.0;
   }
 
   /*--- Allocate the temporary vectors for the basis evaluation ---*/
@@ -64,45 +63,54 @@ void CBSplineBlending::SetOrder(short val_order, short n_controlpoints){
   N.resize(Order, vector<su2double>(Order, 0.0));
 }
 
-su2double CBSplineBlending::GetBasis(short val_i, su2double val_t){
-
+su2double CBSplineBlending::GetBasis(short val_i, su2double val_t) {
   /*--- Evaluation is based on the algorithm from "The NURBS Book (Les Piegl and Wayne Tiller)" ---*/
 
   /*--- Special cases ---*/
 
-  if ((val_i == 0 && val_t == U[0]) || (val_i == (short)U.size()-1 && val_t == U.back())) {return 1.0;}
+  if ((val_i == 0 && val_t == U[0]) || (val_i == (short)U.size() - 1 && val_t == U.back())) {
+    return 1.0;
+  }
 
   /*--- Local property of BSplines ---*/
 
-  if ((val_t < U[val_i]) || (val_t >= U[val_i+Order])){ return 0.0;}
+  if ((val_t < U[val_i]) || (val_t >= U[val_i + Order])) {
+    return 0.0;
+  }
 
-  unsigned short j,k;
+  unsigned short j, k;
   su2double saved, temp;
 
-  for (j = 0; j < Order; j++){
-    if ((val_t >= U[val_i+j]) && (val_t < U[val_i+j+1])) N[j][0] = 1.0;
-    else N[j][0] = 0;
+  for (j = 0; j < Order; j++) {
+    if ((val_t >= U[val_i + j]) && (val_t < U[val_i + j + 1]))
+      N[j][0] = 1.0;
+    else
+      N[j][0] = 0;
   }
 
-  for (k = 1; k < Order; k++){
-    if (N[0][k-1] == 0.0) saved = 0.0;
-    else saved = ((val_t - U[val_i])*N[0][k-1])/(U[val_i+k] - U[val_i]);
-    for (j = 0; j < Order-k; j++){
-      if (N[j+1][k-1] == 0.0){
-        N[j][k] = saved; saved = 0.0;
+  for (k = 1; k < Order; k++) {
+    if (N[0][k - 1] == 0.0)
+      saved = 0.0;
+    else
+      saved = ((val_t - U[val_i]) * N[0][k - 1]) / (U[val_i + k] - U[val_i]);
+    for (j = 0; j < Order - k; j++) {
+      if (N[j + 1][k - 1] == 0.0) {
+        N[j][k] = saved;
+        saved = 0.0;
       } else {
-        temp     = N[j+1][k-1]/(U[val_i+j+k+1] - U[val_i+j+1]);
-        N[j][k]  = saved+(U[val_i+j+k+1] - val_t)*temp;
-        saved    = (val_t - U[val_i+j+1])*temp;
+        temp = N[j + 1][k - 1] / (U[val_i + j + k + 1] - U[val_i + j + 1]);
+        N[j][k] = saved + (U[val_i + j + k + 1] - val_t) * temp;
+        saved = (val_t - U[val_i + j + 1]) * temp;
       }
     }
   }
-  return N[0][Order-1];
+  return N[0][Order - 1];
 }
 
-su2double CBSplineBlending::GetDerivative(short val_i, su2double val_t, short val_order_der){
-
-  if ((val_t < U[val_i]) || (val_t >= U[val_i+Order])){ return 0.0;}
+su2double CBSplineBlending::GetDerivative(short val_i, su2double val_t, short val_order_der) {
+  if ((val_t < U[val_i]) || (val_t >= U[val_i + Order])) {
+    return 0.0;
+  }
 
   /*--- Evaluate the i+p basis functions up to the order p (stored in the matrix N). ---*/
 
@@ -110,27 +118,29 @@ su2double CBSplineBlending::GetDerivative(short val_i, su2double val_t, short va
 
   /*--- Use the recursive definition for the derivative (hardcoded for 1st and 2nd derivative). ---*/
 
-  if (val_order_der == 0){ return N[0][Order-1];}
+  if (val_order_der == 0) {
+    return N[0][Order - 1];
+  }
 
-  if (val_order_der == 1){
-    return (Order-1.0)/(1e-10 + U[val_i+Order-1] - U[val_i]  )*N[0][Order-2]
-         - (Order-1.0)/(1e-10 + U[val_i+Order]   - U[val_i+1])*N[1][Order-2];
+  if (val_order_der == 1) {
+    return (Order - 1.0) / (1e-10 + U[val_i + Order - 1] - U[val_i]) * N[0][Order - 2] -
+           (Order - 1.0) / (1e-10 + U[val_i + Order] - U[val_i + 1]) * N[1][Order - 2];
   }
 
-  if (val_order_der == 2 && Order > 2){
-    const su2double left = (Order-2.0)/(1e-10 + U[val_i+Order-2] - U[val_i])  *N[0][Order-3]
-                         - (Order-2.0)/(1e-10 + U[val_i+Order-1] - U[val_i+1])*N[1][Order-3];
+  if (val_order_der == 2 && Order > 2) {
+    const su2double left = (Order - 2.0) / (1e-10 + U[val_i + Order - 2] - U[val_i]) * N[0][Order - 3] -
+                           (Order - 2.0) / (1e-10 + U[val_i + Order - 1] - U[val_i + 1]) * N[1][Order - 3];
 
-    const su2double right = (Order-2.0)/(1e-10 + U[val_i+Order-1] - U[val_i+1])*N[1][Order-3]
-                          - (Order-2.0)/(1e-10 + U[val_i+Order]   - U[val_i+2])*N[2][Order-3];
+    const su2double right = (Order - 2.0) / (1e-10 + U[val_i + Order - 1] - U[val_i + 1]) * N[1][Order - 3] -
+                            (Order - 2.0) / (1e-10 + U[val_i + Order] - U[val_i + 2]) * N[2][Order - 3];
 
-    return (Order-1.0)/(1e-10 + U[val_i+Order-1] - U[val_i]  )*left
-         - (Order-1.0)/(1e-10 + U[val_i+Order]   - U[val_i+1])*right;
+    return (Order - 1.0) / (1e-10 + U[val_i + Order - 1] - U[val_i]) * left -
+           (Order - 1.0) / (1e-10 + U[val_i + Order] - U[val_i + 1]) * right;
   }
 
   /*--- Higher order derivatives are not implemented, so we exit if they are requested. ---*/
 
-  if (val_order_der > 2){
+  if (val_order_der > 2) {
     SU2_MPI::Error("Higher order derivatives for BSplines are not implemented.", CURRENT_FUNCTION);
   }
   return 0.0;
diff --git a/Common/src/grid_movement/CBezierBlending.cpp b/Common/src/grid_movement/CBezierBlending.cpp
index 03c41efd037..d24ebdbb974 100644
--- a/Common/src/grid_movement/CBezierBlending.cpp
+++ b/Common/src/grid_movement/CBezierBlending.cpp
@@ -28,71 +28,73 @@
 #include "../../include/grid_movement/CBezierBlending.hpp"
 #include "../../include/option_structure.hpp"
 
+CBezierBlending::CBezierBlending(short val_order, short n_controlpoints) { SetOrder(val_order, n_controlpoints); }
 
-CBezierBlending::CBezierBlending(short val_order, short n_controlpoints){
-  SetOrder(val_order, n_controlpoints);
-}
-
-CBezierBlending::~CBezierBlending(){}
+CBezierBlending::~CBezierBlending() {}
 
-void CBezierBlending::SetOrder(short val_order, short n_controlpoints){
-  Order  = val_order;
+void CBezierBlending::SetOrder(short val_order, short n_controlpoints) {
+  Order = val_order;
   Degree = Order - 1;
-  binomial.resize(Order+1, 0.0);
-}
-
-su2double CBezierBlending::GetBasis(short val_i, su2double val_t){
-  return GetBernstein(Degree, val_i, val_t);
+  binomial.resize(Order + 1, 0.0);
 }
 
-su2double CBezierBlending::GetBernstein(short val_n, short val_i, su2double val_t){
+su2double CBezierBlending::GetBasis(short val_i, su2double val_t) { return GetBernstein(Degree, val_i, val_t); }
 
+su2double CBezierBlending::GetBernstein(short val_n, short val_i, su2double val_t) {
   su2double value = 0.0;
 
-  if (val_i > val_n) { value = 0.0; return value; }
+  if (val_i > val_n) {
+    value = 0.0;
+    return value;
+  }
 
   if (val_i == 0) {
-    if (val_t == 0) value = 1.0;
-    else if (val_t == 1) value = 0.0;
-    else value = Binomial(val_n, val_i) * pow(val_t, val_i) * pow(1.0 - val_t, val_n - val_i);
-  }
-  else if (val_i == val_n) {
-    if (val_t == 0) value = 0.0;
-    else if (val_t == 1) value = 1.0;
-    else value = pow(val_t, val_n);
-  }
-  else {
+    if (val_t == 0)
+      value = 1.0;
+    else if (val_t == 1)
+      value = 0.0;
+    else
+      value = Binomial(val_n, val_i) * pow(val_t, val_i) * pow(1.0 - val_t, val_n - val_i);
+  } else if (val_i == val_n) {
+    if (val_t == 0)
+      value = 0.0;
+    else if (val_t == 1)
+      value = 1.0;
+    else
+      value = pow(val_t, val_n);
+  } else {
     if ((val_t == 0) || (val_t == 1)) value = 0.0;
-    value = Binomial(val_n, val_i) * pow(val_t, val_i) * pow(1.0-val_t, val_n - val_i);
+    value = Binomial(val_n, val_i) * pow(val_t, val_i) * pow(1.0 - val_t, val_n - val_i);
   }
 
   return value;
 }
 
-su2double CBezierBlending::GetDerivative(short val_i, su2double val_t, short val_order_der){
+su2double CBezierBlending::GetDerivative(short val_i, su2double val_t, short val_order_der) {
   return GetBernsteinDerivative(Degree, val_i, val_t, val_order_der);
 }
 
-su2double CBezierBlending::GetBernsteinDerivative(short val_n, short val_i, su2double val_t, short val_order_der){
-
+su2double CBezierBlending::GetBernsteinDerivative(short val_n, short val_i, su2double val_t, short val_order_der) {
   su2double value = 0.0;
 
   /*--- Verify this subroutine, it provides negative val_n,
    which is a wrong value for GetBernstein ---*/
 
   if (val_order_der == 0) {
-    value = GetBernstein(val_n, val_i, val_t); return value;
+    value = GetBernstein(val_n, val_i, val_t);
+    return value;
   }
 
   if (val_i == 0) {
-    value = val_n*(-GetBernsteinDerivative(val_n-1, val_i, val_t, val_order_der-1)); return value;
-  }
-  else {
+    value = val_n * (-GetBernsteinDerivative(val_n - 1, val_i, val_t, val_order_der - 1));
+    return value;
+  } else {
     if (val_n == 0) {
-      value = val_t; return value;
-    }
-    else {
-      value = val_n*(GetBernsteinDerivative(val_n-1, val_i-1, val_t, val_order_der-1) - GetBernsteinDerivative(val_n-1, val_i, val_t, val_order_der-1));
+      value = val_t;
+      return value;
+    } else {
+      value = val_n * (GetBernsteinDerivative(val_n - 1, val_i - 1, val_t, val_order_der - 1) -
+                       GetBernsteinDerivative(val_n - 1, val_i, val_t, val_order_der - 1));
       return value;
     }
   }
@@ -100,22 +102,22 @@ su2double CBezierBlending::GetBernsteinDerivative(short val_n, short val_i, su2d
   return value;
 }
 
-su2double CBezierBlending::Binomial(unsigned short n, unsigned short m){
-
+su2double CBezierBlending::Binomial(unsigned short n, unsigned short m) {
   unsigned short i, j;
   su2double result;
 
   binomial[0] = 1.0;
   for (i = 1; i <= n; ++i) {
     binomial[i] = 1.0;
-    for (j = i-1U; j > 0; --j) {
-      binomial[j] += binomial[j-1U];
+    for (j = i - 1U; j > 0; --j) {
+      binomial[j] += binomial[j - 1U];
     }
   }
 
   result = binomial[m];
-  if (fabs(result) < EPS*EPS) { result = 0.0; }
+  if (fabs(result) < EPS * EPS) {
+    result = 0.0;
+  }
 
   return result;
-
 }
diff --git a/Common/src/grid_movement/CFreeFormBlending.cpp b/Common/src/grid_movement/CFreeFormBlending.cpp
index 9a1871c2f31..50aa23a131f 100644
--- a/Common/src/grid_movement/CFreeFormBlending.cpp
+++ b/Common/src/grid_movement/CFreeFormBlending.cpp
@@ -27,6 +27,6 @@
 
 #include "../../include/grid_movement/CFreeFormBlending.hpp"
 
-CFreeFormBlending::CFreeFormBlending(){}
+CFreeFormBlending::CFreeFormBlending() {}
 
-CFreeFormBlending::~CFreeFormBlending(){}
+CFreeFormBlending::~CFreeFormBlending() {}
diff --git a/Common/src/grid_movement/CFreeFormDefBox.cpp b/Common/src/grid_movement/CFreeFormDefBox.cpp
index c16ef15b716..0d0ca8351c3 100644
--- a/Common/src/grid_movement/CFreeFormDefBox.cpp
+++ b/Common/src/grid_movement/CFreeFormDefBox.cpp
@@ -29,10 +29,11 @@
 #include "../../include/grid_movement/CBezierBlending.hpp"
 #include "../../include/grid_movement/CBSplineBlending.hpp"
 
-CFreeFormDefBox::CFreeFormDefBox(void) : CGridMovement() { }
-
-CFreeFormDefBox::CFreeFormDefBox(const unsigned short Degree[], unsigned short BSplineOrder[], unsigned short kind_blending) : CGridMovement() {
+CFreeFormDefBox::CFreeFormDefBox(void) : CGridMovement() {}
 
+CFreeFormDefBox::CFreeFormDefBox(const unsigned short Degree[], unsigned short BSplineOrder[],
+                                 unsigned short kind_blending)
+    : CGridMovement() {
   unsigned short iCornerPoints, iOrder, jOrder, kOrder, iDim;
 
   /*--- FFD is always 3D (even in 2D problems) ---*/
@@ -42,39 +43,47 @@ CFreeFormDefBox::CFreeFormDefBox(const unsigned short Degree[], unsigned short B
 
   /*--- Allocate Corners points ---*/
 
-  Coord_Corner_Points = new su2double* [nCornerPoints];
+  Coord_Corner_Points = new su2double*[nCornerPoints];
   for (iCornerPoints = 0; iCornerPoints < nCornerPoints; iCornerPoints++)
-    Coord_Corner_Points[iCornerPoints] = new su2double [nDim];
+    Coord_Corner_Points[iCornerPoints] = new su2double[nDim];
 
-  ParamCoord = new su2double[nDim]; ParamCoord_ = new su2double[nDim];
-  cart_coord = new su2double[nDim]; cart_coord_ = new su2double[nDim];
+  ParamCoord = new su2double[nDim];
+  ParamCoord_ = new su2double[nDim];
+  cart_coord = new su2double[nDim];
+  cart_coord_ = new su2double[nDim];
   Gradient = new su2double[nDim];
 
-  lDegree = Degree[0]; lOrder = lDegree+1;
-  mDegree = Degree[1]; mOrder = mDegree+1;
-  nDegree = Degree[2]; nOrder = nDegree+1;
-  nControlPoints = lOrder*mOrder*nOrder;
-
-  lDegree_Copy = Degree[0]; lOrder_Copy = lDegree+1;
-  mDegree_Copy = Degree[1]; mOrder_Copy = mDegree+1;
-  nDegree_Copy = Degree[2]; nOrder_Copy = nDegree+1;
-  nControlPoints_Copy = lOrder_Copy*mOrder_Copy*nOrder_Copy;
-
-  Coord_Control_Points = new su2double*** [lOrder];
-  ParCoord_Control_Points = new su2double*** [lOrder];
-  Coord_Control_Points_Copy = new su2double*** [lOrder];
+  lDegree = Degree[0];
+  lOrder = lDegree + 1;
+  mDegree = Degree[1];
+  mOrder = mDegree + 1;
+  nDegree = Degree[2];
+  nOrder = nDegree + 1;
+  nControlPoints = lOrder * mOrder * nOrder;
+
+  lDegree_Copy = Degree[0];
+  lOrder_Copy = lDegree + 1;
+  mDegree_Copy = Degree[1];
+  mOrder_Copy = mDegree + 1;
+  nDegree_Copy = Degree[2];
+  nOrder_Copy = nDegree + 1;
+  nControlPoints_Copy = lOrder_Copy * mOrder_Copy * nOrder_Copy;
+
+  Coord_Control_Points = new su2double***[lOrder];
+  ParCoord_Control_Points = new su2double***[lOrder];
+  Coord_Control_Points_Copy = new su2double***[lOrder];
   for (iOrder = 0; iOrder < lOrder; iOrder++) {
-    Coord_Control_Points[iOrder] = new su2double** [mOrder];
-    ParCoord_Control_Points[iOrder] = new su2double** [mOrder];
-    Coord_Control_Points_Copy[iOrder] = new su2double** [mOrder];
+    Coord_Control_Points[iOrder] = new su2double**[mOrder];
+    ParCoord_Control_Points[iOrder] = new su2double**[mOrder];
+    Coord_Control_Points_Copy[iOrder] = new su2double**[mOrder];
     for (jOrder = 0; jOrder < mOrder; jOrder++) {
-      Coord_Control_Points[iOrder][jOrder] = new su2double* [nOrder];
-      ParCoord_Control_Points[iOrder][jOrder] = new su2double* [nOrder];
-      Coord_Control_Points_Copy[iOrder][jOrder] = new su2double* [nOrder];
+      Coord_Control_Points[iOrder][jOrder] = new su2double*[nOrder];
+      ParCoord_Control_Points[iOrder][jOrder] = new su2double*[nOrder];
+      Coord_Control_Points_Copy[iOrder][jOrder] = new su2double*[nOrder];
       for (kOrder = 0; kOrder < nOrder; kOrder++) {
-        Coord_Control_Points[iOrder][jOrder][kOrder] = new su2double [nDim];
-        ParCoord_Control_Points[iOrder][jOrder][kOrder] = new su2double [nDim];
-        Coord_Control_Points_Copy[iOrder][jOrder][kOrder] = new su2double [nDim];
+        Coord_Control_Points[iOrder][jOrder][kOrder] = new su2double[nDim];
+        ParCoord_Control_Points[iOrder][jOrder][kOrder] = new su2double[nDim];
+        Coord_Control_Points_Copy[iOrder][jOrder][kOrder] = new su2double[nDim];
         for (iDim = 0; iDim < nDim; iDim++) {
           Coord_Control_Points[iOrder][jOrder][kOrder][iDim] = 0.0;
           ParCoord_Control_Points[iOrder][jOrder][kOrder][iDim] = 0.0;
@@ -86,17 +95,16 @@ CFreeFormDefBox::CFreeFormDefBox(const unsigned short Degree[], unsigned short B
 
   BlendingFunction = new CFreeFormBlending*[nDim];
 
-  if (kind_blending == BEZIER){
+  if (kind_blending == BEZIER) {
     BlendingFunction[0] = new CBezierBlending(lOrder, lOrder);
     BlendingFunction[1] = new CBezierBlending(mOrder, mOrder);
     BlendingFunction[2] = new CBezierBlending(nOrder, nOrder);
   }
-  if (kind_blending == BSPLINE_UNIFORM){
+  if (kind_blending == BSPLINE_UNIFORM) {
     BlendingFunction[0] = new CBSplineBlending(BSplineOrder[0], lOrder);
     BlendingFunction[1] = new CBSplineBlending(BSplineOrder[1], mOrder);
     BlendingFunction[2] = new CBSplineBlending(BSplineOrder[2], nOrder);
   }
-
 }
 
 CFreeFormDefBox::~CFreeFormDefBox(void) {
@@ -105,146 +113,171 @@ CFreeFormDefBox::~CFreeFormDefBox(void) {
   for (iOrder = 0; iOrder < lOrder; iOrder++) {
     for (jOrder = 0; jOrder < mOrder; jOrder++) {
       for (kOrder = 0; kOrder < nOrder; kOrder++) {
-        delete [] Coord_Control_Points[iOrder][jOrder][kOrder];
-        delete [] ParCoord_Control_Points[iOrder][jOrder][kOrder];
-        delete [] Coord_Control_Points_Copy[iOrder][jOrder][kOrder];
-        if (Coord_SupportCP != nullptr) delete [] Coord_SupportCP[iOrder][jOrder][kOrder];
+        delete[] Coord_Control_Points[iOrder][jOrder][kOrder];
+        delete[] ParCoord_Control_Points[iOrder][jOrder][kOrder];
+        delete[] Coord_Control_Points_Copy[iOrder][jOrder][kOrder];
+        if (Coord_SupportCP != nullptr) delete[] Coord_SupportCP[iOrder][jOrder][kOrder];
       }
-      delete [] Coord_Control_Points[iOrder][jOrder];
-      delete [] ParCoord_Control_Points[iOrder][jOrder];
-      delete [] Coord_Control_Points_Copy[iOrder][jOrder];
-      if (Coord_SupportCP != nullptr) delete [] Coord_SupportCP[iOrder][jOrder];
-    }
-    delete [] Coord_Control_Points[iOrder];
-    delete [] ParCoord_Control_Points[iOrder];
-    delete [] Coord_Control_Points_Copy[iOrder];
-    if (Coord_SupportCP != nullptr) delete [] Coord_SupportCP[iOrder];
+      delete[] Coord_Control_Points[iOrder][jOrder];
+      delete[] ParCoord_Control_Points[iOrder][jOrder];
+      delete[] Coord_Control_Points_Copy[iOrder][jOrder];
+      if (Coord_SupportCP != nullptr) delete[] Coord_SupportCP[iOrder][jOrder];
     }
+    delete[] Coord_Control_Points[iOrder];
+    delete[] ParCoord_Control_Points[iOrder];
+    delete[] Coord_Control_Points_Copy[iOrder];
+    if (Coord_SupportCP != nullptr) delete[] Coord_SupportCP[iOrder];
+  }
 
-  delete [] Coord_Control_Points;
-  delete [] ParCoord_Control_Points;
-  delete [] Coord_Control_Points_Copy;
-  delete [] Coord_SupportCP;
+  delete[] Coord_Control_Points;
+  delete[] ParCoord_Control_Points;
+  delete[] Coord_Control_Points_Copy;
+  delete[] Coord_SupportCP;
 
-  delete [] ParamCoord;
-  delete [] ParamCoord_;
-  delete [] cart_coord;
-  delete [] cart_coord_;
-  delete [] Gradient;
+  delete[] ParamCoord;
+  delete[] ParamCoord_;
+  delete[] cart_coord;
+  delete[] cart_coord_;
+  delete[] Gradient;
 
-  for (iCornerPoints = 0; iCornerPoints < nCornerPoints; iCornerPoints++)
-    delete [] Coord_Corner_Points[iCornerPoints];
-  delete [] Coord_Corner_Points;
+  for (iCornerPoints = 0; iCornerPoints < nCornerPoints; iCornerPoints++) delete[] Coord_Corner_Points[iCornerPoints];
+  delete[] Coord_Corner_Points;
 
-  for (iDim = 0; iDim < nDim; iDim++){
+  for (iDim = 0; iDim < nDim; iDim++) {
     delete BlendingFunction[iDim];
   }
-  delete [] BlendingFunction;
+  delete[] BlendingFunction;
 }
 
-void  CFreeFormDefBox::SetUnitCornerPoints(void) {
-
+void CFreeFormDefBox::SetUnitCornerPoints(void) {
   unsigned short iDim;
-  su2double *coord = new su2double [nDim];
+  su2double* coord = new su2double[nDim];
 
   for (iDim = 0; iDim < nDim; iDim++) coord[iDim] = 0.0;
 
-  coord [0] = 0.0; coord [1] = 0.0; coord [2] = 0.0; this->SetCoordCornerPoints(coord, 0);
-  coord [0] = 1.0; coord [1] = 0.0; coord [2] = 0.0; this->SetCoordCornerPoints(coord, 1);
-  coord [0] = 1.0; coord [1] = 1.0; coord [2] = 0.0; this->SetCoordCornerPoints(coord, 2);
-  coord [0] = 0.0; coord [1] = 1.0; coord [2] = 0.0; this->SetCoordCornerPoints(coord, 3);
-  coord [0] = 0.0; coord [1] = 0.0; coord [2] = 1.0; this->SetCoordCornerPoints(coord, 4);
-  coord [0] = 1.0; coord [1] = 0.0; coord [2] = 1.0; this->SetCoordCornerPoints(coord, 5);
-  coord [0] = 1.0; coord [1] = 1.0; coord [2] = 1.0; this->SetCoordCornerPoints(coord, 6);
-  coord [0] = 0.0; coord [1] = 1.0; coord [2] = 1.0; this->SetCoordCornerPoints(coord, 7);
-
-  delete [] coord;
-
+  coord[0] = 0.0;
+  coord[1] = 0.0;
+  coord[2] = 0.0;
+  this->SetCoordCornerPoints(coord, 0);
+  coord[0] = 1.0;
+  coord[1] = 0.0;
+  coord[2] = 0.0;
+  this->SetCoordCornerPoints(coord, 1);
+  coord[0] = 1.0;
+  coord[1] = 1.0;
+  coord[2] = 0.0;
+  this->SetCoordCornerPoints(coord, 2);
+  coord[0] = 0.0;
+  coord[1] = 1.0;
+  coord[2] = 0.0;
+  this->SetCoordCornerPoints(coord, 3);
+  coord[0] = 0.0;
+  coord[1] = 0.0;
+  coord[2] = 1.0;
+  this->SetCoordCornerPoints(coord, 4);
+  coord[0] = 1.0;
+  coord[1] = 0.0;
+  coord[2] = 1.0;
+  this->SetCoordCornerPoints(coord, 5);
+  coord[0] = 1.0;
+  coord[1] = 1.0;
+  coord[2] = 1.0;
+  this->SetCoordCornerPoints(coord, 6);
+  coord[0] = 0.0;
+  coord[1] = 1.0;
+  coord[2] = 1.0;
+  this->SetCoordCornerPoints(coord, 7);
+
+  delete[] coord;
 }
 
-void CFreeFormDefBox::SetControlPoints_Parallelepiped (void) {
+void CFreeFormDefBox::SetControlPoints_Parallelepiped(void) {
   unsigned short iDim, iDegree, jDegree, kDegree;
 
   /*--- Set base control points according to the notation of Vtk for hexahedrons ---*/
   for (iDim = 0; iDim < nDim; iDim++) {
-    Coord_Control_Points  [0]      [0]      [0]      [iDim]  = Coord_Corner_Points[0][iDim];
-    Coord_Control_Points  [lOrder-1]  [0]      [0]      [iDim]  = Coord_Corner_Points[1][iDim];
-    Coord_Control_Points  [lOrder-1]  [mOrder-1]  [0]      [iDim]  = Coord_Corner_Points[2][iDim];
-    Coord_Control_Points  [0]      [mOrder-1]  [0]      [iDim]  = Coord_Corner_Points[3][iDim];
-    Coord_Control_Points  [0]      [0]      [nOrder-1]  [iDim]  = Coord_Corner_Points[4][iDim];
-    Coord_Control_Points  [lOrder-1]  [0]      [nOrder-1]  [iDim]  = Coord_Corner_Points[5][iDim];
-    Coord_Control_Points  [lOrder-1]  [mOrder-1]  [nOrder-1]  [iDim]  = Coord_Corner_Points[6][iDim];
-    Coord_Control_Points  [0]      [mOrder-1]  [nOrder-1]  [iDim]  = Coord_Corner_Points[7][iDim];
+    Coord_Control_Points[0][0][0][iDim] = Coord_Corner_Points[0][iDim];
+    Coord_Control_Points[lOrder - 1][0][0][iDim] = Coord_Corner_Points[1][iDim];
+    Coord_Control_Points[lOrder - 1][mOrder - 1][0][iDim] = Coord_Corner_Points[2][iDim];
+    Coord_Control_Points[0][mOrder - 1][0][iDim] = Coord_Corner_Points[3][iDim];
+    Coord_Control_Points[0][0][nOrder - 1][iDim] = Coord_Corner_Points[4][iDim];
+    Coord_Control_Points[lOrder - 1][0][nOrder - 1][iDim] = Coord_Corner_Points[5][iDim];
+    Coord_Control_Points[lOrder - 1][mOrder - 1][nOrder - 1][iDim] = Coord_Corner_Points[6][iDim];
+    Coord_Control_Points[0][mOrder - 1][nOrder - 1][iDim] = Coord_Corner_Points[7][iDim];
   }
 
   /*--- Fill the rest of the cubic matrix of control points with uniform spacing (parallelepiped) ---*/
   for (iDegree = 0; iDegree <= lDegree; iDegree++)
     for (jDegree = 0; jDegree <= mDegree; jDegree++)
       for (kDegree = 0; kDegree <= nDegree; kDegree++) {
-        Coord_Control_Points[iDegree][jDegree][kDegree][0] = Coord_Corner_Points[0][0]
-        + su2double(iDegree)/su2double(lDegree)*(Coord_Corner_Points[1][0]-Coord_Corner_Points[0][0]);
-        Coord_Control_Points[iDegree][jDegree][kDegree][1] = Coord_Corner_Points[0][1]
-        + su2double(jDegree)/su2double(mDegree)*(Coord_Corner_Points[3][1]-Coord_Corner_Points[0][1]);
-        Coord_Control_Points[iDegree][jDegree][kDegree][2] = Coord_Corner_Points[0][2]
-        + su2double(kDegree)/su2double(nDegree)*(Coord_Corner_Points[4][2]-Coord_Corner_Points[0][2]);
+        Coord_Control_Points[iDegree][jDegree][kDegree][0] =
+            Coord_Corner_Points[0][0] +
+            su2double(iDegree) / su2double(lDegree) * (Coord_Corner_Points[1][0] - Coord_Corner_Points[0][0]);
+        Coord_Control_Points[iDegree][jDegree][kDegree][1] =
+            Coord_Corner_Points[0][1] +
+            su2double(jDegree) / su2double(mDegree) * (Coord_Corner_Points[3][1] - Coord_Corner_Points[0][1]);
+        Coord_Control_Points[iDegree][jDegree][kDegree][2] =
+            Coord_Corner_Points[0][2] +
+            su2double(kDegree) / su2double(nDegree) * (Coord_Corner_Points[4][2] - Coord_Corner_Points[0][2]);
       }
 }
 
-void CFreeFormDefBox::SetSupportCP(CFreeFormDefBox *FFDBox) {
+void CFreeFormDefBox::SetSupportCP(CFreeFormDefBox* FFDBox) {
   unsigned short iDim, iOrder, jOrder, kOrder;
   unsigned short lOrder = FFDBox->GetlOrder();
   unsigned short mOrder = FFDBox->GetmOrder();
   unsigned short nOrder = FFDBox->GetnOrder();
 
-  Coord_SupportCP = new su2double*** [lOrder];
+  Coord_SupportCP = new su2double***[lOrder];
   for (iOrder = 0; iOrder < lOrder; iOrder++) {
-    Coord_SupportCP[iOrder] = new su2double** [mOrder];
+    Coord_SupportCP[iOrder] = new su2double**[mOrder];
     for (jOrder = 0; jOrder < mOrder; jOrder++) {
-      Coord_SupportCP[iOrder][jOrder] = new su2double* [nOrder];
-      for (kOrder = 0; kOrder < nOrder; kOrder++)
-        Coord_SupportCP[iOrder][jOrder][kOrder] = new su2double [nDim];
+      Coord_SupportCP[iOrder][jOrder] = new su2double*[nOrder];
+      for (kOrder = 0; kOrder < nOrder; kOrder++) Coord_SupportCP[iOrder][jOrder][kOrder] = new su2double[nDim];
     }
   }
 
   /*--- Set base support control points according to the notation of Vtk for hexahedrons ---*/
   for (iDim = 0; iDim < nDim; iDim++) {
-    Coord_SupportCP  [0]      [0]      [0]      [iDim]  = Coord_Corner_Points[0][iDim];
-    Coord_SupportCP  [lOrder-1]  [0]      [0]      [iDim]  = Coord_Corner_Points[1][iDim];
-    Coord_SupportCP  [lOrder-1]  [mOrder-1]  [0]      [iDim]  = Coord_Corner_Points[2][iDim];
-    Coord_SupportCP  [0]      [mOrder-1]  [0]      [iDim]  = Coord_Corner_Points[3][iDim];
-    Coord_SupportCP  [0]      [0]      [nOrder-1]  [iDim]  = Coord_Corner_Points[4][iDim];
-    Coord_SupportCP  [lOrder-1]  [0]      [nOrder-1]  [iDim]  = Coord_Corner_Points[5][iDim];
-    Coord_SupportCP  [lOrder-1]  [mOrder-1]  [nOrder-1]  [iDim]  = Coord_Corner_Points[6][iDim];
-    Coord_SupportCP  [0]      [mOrder-1]  [nOrder-1]  [iDim]  = Coord_Corner_Points[7][iDim];
+    Coord_SupportCP[0][0][0][iDim] = Coord_Corner_Points[0][iDim];
+    Coord_SupportCP[lOrder - 1][0][0][iDim] = Coord_Corner_Points[1][iDim];
+    Coord_SupportCP[lOrder - 1][mOrder - 1][0][iDim] = Coord_Corner_Points[2][iDim];
+    Coord_SupportCP[0][mOrder - 1][0][iDim] = Coord_Corner_Points[3][iDim];
+    Coord_SupportCP[0][0][nOrder - 1][iDim] = Coord_Corner_Points[4][iDim];
+    Coord_SupportCP[lOrder - 1][0][nOrder - 1][iDim] = Coord_Corner_Points[5][iDim];
+    Coord_SupportCP[lOrder - 1][mOrder - 1][nOrder - 1][iDim] = Coord_Corner_Points[6][iDim];
+    Coord_SupportCP[0][mOrder - 1][nOrder - 1][iDim] = Coord_Corner_Points[7][iDim];
   }
 
   /*--- Fill the rest of the cubic matrix of support control points with uniform spacing  ---*/
   for (iOrder = 0; iOrder < lOrder; iOrder++)
     for (jOrder = 0; jOrder < mOrder; jOrder++)
       for (kOrder = 0; kOrder < nOrder; kOrder++) {
-        Coord_SupportCP[iOrder][jOrder][kOrder][0] = Coord_Corner_Points[0][0]
-        + su2double(iOrder)/su2double(lOrder-1)*(Coord_Corner_Points[1][0]-Coord_Corner_Points[0][0]);
-        Coord_SupportCP[iOrder][jOrder][kOrder][1] = Coord_Corner_Points[0][1]
-        + su2double(jOrder)/su2double(mOrder-1)*(Coord_Corner_Points[3][1]-Coord_Corner_Points[0][1]);
-        Coord_SupportCP[iOrder][jOrder][kOrder][2] = Coord_Corner_Points[0][2]
-        + su2double(kOrder)/su2double(nOrder-1)*(Coord_Corner_Points[4][2]-Coord_Corner_Points[0][2]);
+        Coord_SupportCP[iOrder][jOrder][kOrder][0] =
+            Coord_Corner_Points[0][0] +
+            su2double(iOrder) / su2double(lOrder - 1) * (Coord_Corner_Points[1][0] - Coord_Corner_Points[0][0]);
+        Coord_SupportCP[iOrder][jOrder][kOrder][1] =
+            Coord_Corner_Points[0][1] +
+            su2double(jOrder) / su2double(mOrder - 1) * (Coord_Corner_Points[3][1] - Coord_Corner_Points[0][1]);
+        Coord_SupportCP[iOrder][jOrder][kOrder][2] =
+            Coord_Corner_Points[0][2] +
+            su2double(kOrder) / su2double(nOrder - 1) * (Coord_Corner_Points[4][2] - Coord_Corner_Points[0][2]);
       }
 }
 
-void CFreeFormDefBox::SetSupportCPChange(CFreeFormDefBox *FFDBox) {
+void CFreeFormDefBox::SetSupportCPChange(CFreeFormDefBox* FFDBox) {
   unsigned short iDim, iOrder, jOrder, kOrder;
   su2double *CartCoordNew, *ParamCoord;
   unsigned short lOrder = FFDBox->GetlOrder();
   unsigned short mOrder = FFDBox->GetmOrder();
   unsigned short nOrder = FFDBox->GetnOrder();
 
-  su2double ****ParamCoord_SupportCP = new su2double*** [lOrder];
+  su2double**** ParamCoord_SupportCP = new su2double***[lOrder];
   for (iOrder = 0; iOrder < lOrder; iOrder++) {
-    ParamCoord_SupportCP[iOrder] = new su2double** [mOrder];
+    ParamCoord_SupportCP[iOrder] = new su2double**[mOrder];
     for (jOrder = 0; jOrder < mOrder; jOrder++) {
-      ParamCoord_SupportCP[iOrder][jOrder] = new su2double* [nOrder];
-      for (kOrder = 0; kOrder < nOrder; kOrder++)
-        ParamCoord_SupportCP[iOrder][jOrder][kOrder] = new su2double [nDim];
+      ParamCoord_SupportCP[iOrder][jOrder] = new su2double*[nOrder];
+      for (kOrder = 0; kOrder < nOrder; kOrder++) ParamCoord_SupportCP[iOrder][jOrder][kOrder] = new su2double[nDim];
     }
   }
 
@@ -252,18 +285,17 @@ void CFreeFormDefBox::SetSupportCPChange(CFreeFormDefBox *FFDBox) {
     for (jOrder = 0; jOrder < mOrder; jOrder++)
       for (kOrder = 0; kOrder < nOrder; kOrder++)
         for (iDim = 0; iDim < nDim; iDim++)
-          ParamCoord_SupportCP[iOrder][jOrder][kOrder][iDim] =
-          Coord_SupportCP[iOrder][jOrder][kOrder][iDim];
+          ParamCoord_SupportCP[iOrder][jOrder][kOrder][iDim] = Coord_SupportCP[iOrder][jOrder][kOrder][iDim];
 
   for (iDim = 0; iDim < nDim; iDim++) {
-    Coord_Control_Points[0][0][0][iDim]  = FFDBox->GetCoordCornerPoints(iDim, 0);
-    Coord_Control_Points[1][0][0][iDim]  = FFDBox->GetCoordCornerPoints(iDim, 1);
-    Coord_Control_Points[1][1][0][iDim]  = FFDBox->GetCoordCornerPoints(iDim, 2);
-    Coord_Control_Points[0][1][0][iDim]  = FFDBox->GetCoordCornerPoints(iDim, 3);
-    Coord_Control_Points[0][0][1][iDim]  = FFDBox->GetCoordCornerPoints(iDim, 4);
-    Coord_Control_Points[1][0][1][iDim]  = FFDBox->GetCoordCornerPoints(iDim, 5);
-    Coord_Control_Points[1][1][1][iDim]  = FFDBox->GetCoordCornerPoints(iDim, 6);
-    Coord_Control_Points[0][1][1][iDim]  = FFDBox->GetCoordCornerPoints(iDim, 7);
+    Coord_Control_Points[0][0][0][iDim] = FFDBox->GetCoordCornerPoints(iDim, 0);
+    Coord_Control_Points[1][0][0][iDim] = FFDBox->GetCoordCornerPoints(iDim, 1);
+    Coord_Control_Points[1][1][0][iDim] = FFDBox->GetCoordCornerPoints(iDim, 2);
+    Coord_Control_Points[0][1][0][iDim] = FFDBox->GetCoordCornerPoints(iDim, 3);
+    Coord_Control_Points[0][0][1][iDim] = FFDBox->GetCoordCornerPoints(iDim, 4);
+    Coord_Control_Points[1][0][1][iDim] = FFDBox->GetCoordCornerPoints(iDim, 5);
+    Coord_Control_Points[1][1][1][iDim] = FFDBox->GetCoordCornerPoints(iDim, 6);
+    Coord_Control_Points[0][1][1][iDim] = FFDBox->GetCoordCornerPoints(iDim, 7);
   }
 
   for (iOrder = 0; iOrder < FFDBox->GetlOrder(); iOrder++) {
@@ -276,180 +308,186 @@ void CFreeFormDefBox::SetSupportCPChange(CFreeFormDefBox *FFDBox) {
       }
     }
   }
-
 }
 
-void CFreeFormDefBox::SetCart2Cyl_ControlPoints(CConfig *config) {
-
+void CFreeFormDefBox::SetCart2Cyl_ControlPoints(CConfig* config) {
   unsigned short iDegree, jDegree, kDegree;
   su2double CartCoord[3];
   su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
 
-  X_0 = config->GetFFD_Axis(0); Y_0 = config->GetFFD_Axis(1);  Z_0 = config->GetFFD_Axis(2);
+  X_0 = config->GetFFD_Axis(0);
+  Y_0 = config->GetFFD_Axis(1);
+  Z_0 = config->GetFFD_Axis(2);
 
   for (kDegree = 0; kDegree <= nDegree; kDegree++) {
     for (jDegree = 0; jDegree <= mDegree; jDegree++) {
       for (iDegree = 0; iDegree <= lDegree; iDegree++) {
-
         CartCoord[0] = Coord_Control_Points[iDegree][jDegree][kDegree][0];
         CartCoord[1] = Coord_Control_Points[iDegree][jDegree][kDegree][1];
         CartCoord[2] = Coord_Control_Points[iDegree][jDegree][kDegree][2];
 
-        Xbar =  CartCoord[0] - X_0; Ybar =  CartCoord[1] - Y_0; Zbar =  CartCoord[2] - Z_0;
+        Xbar = CartCoord[0] - X_0;
+        Ybar = CartCoord[1] - Y_0;
+        Zbar = CartCoord[2] - Z_0;
 
-        Coord_Control_Points[iDegree][jDegree][kDegree][0] = sqrt(Ybar*Ybar + Zbar*Zbar);
-        Coord_Control_Points[iDegree][jDegree][kDegree][1] = atan2 ( Zbar, Ybar);
-        if (Coord_Control_Points[iDegree][jDegree][kDegree][1] > PI_NUMBER/2.0) Coord_Control_Points[iDegree][jDegree][kDegree][1] -= 2.0*PI_NUMBER;
+        Coord_Control_Points[iDegree][jDegree][kDegree][0] = sqrt(Ybar * Ybar + Zbar * Zbar);
+        Coord_Control_Points[iDegree][jDegree][kDegree][1] = atan2(Zbar, Ybar);
+        if (Coord_Control_Points[iDegree][jDegree][kDegree][1] > PI_NUMBER / 2.0)
+          Coord_Control_Points[iDegree][jDegree][kDegree][1] -= 2.0 * PI_NUMBER;
         Coord_Control_Points[iDegree][jDegree][kDegree][2] = Xbar;
 
         CartCoord[0] = Coord_Control_Points_Copy[iDegree][jDegree][kDegree][0];
         CartCoord[1] = Coord_Control_Points_Copy[iDegree][jDegree][kDegree][1];
         CartCoord[2] = Coord_Control_Points_Copy[iDegree][jDegree][kDegree][2];
 
-        Xbar =  CartCoord[0] - X_0; Ybar =  CartCoord[1] - Y_0; Zbar =  CartCoord[2] - Z_0;
+        Xbar = CartCoord[0] - X_0;
+        Ybar = CartCoord[1] - Y_0;
+        Zbar = CartCoord[2] - Z_0;
 
-        Coord_Control_Points_Copy[iDegree][jDegree][kDegree][0] = sqrt(Ybar*Ybar + Zbar*Zbar);
-        Coord_Control_Points_Copy[iDegree][jDegree][kDegree][1] = atan2 (Zbar, Ybar);
-        if (Coord_Control_Points_Copy[iDegree][jDegree][kDegree][1] > PI_NUMBER/2.0) Coord_Control_Points_Copy[iDegree][jDegree][kDegree][1] -= 2.0*PI_NUMBER;
+        Coord_Control_Points_Copy[iDegree][jDegree][kDegree][0] = sqrt(Ybar * Ybar + Zbar * Zbar);
+        Coord_Control_Points_Copy[iDegree][jDegree][kDegree][1] = atan2(Zbar, Ybar);
+        if (Coord_Control_Points_Copy[iDegree][jDegree][kDegree][1] > PI_NUMBER / 2.0)
+          Coord_Control_Points_Copy[iDegree][jDegree][kDegree][1] -= 2.0 * PI_NUMBER;
         Coord_Control_Points_Copy[iDegree][jDegree][kDegree][2] = Xbar;
-
       }
     }
   }
-
 }
 
-void CFreeFormDefBox::SetCyl2Cart_ControlPoints(CConfig *config) {
-
+void CFreeFormDefBox::SetCyl2Cart_ControlPoints(CConfig* config) {
   unsigned short iDegree, jDegree, kDegree;
   su2double PolarCoord[3];
 
-   su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
-  X_0 = config->GetFFD_Axis(0); Y_0 = config->GetFFD_Axis(1);  Z_0 = config->GetFFD_Axis(2);
+  su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
+  X_0 = config->GetFFD_Axis(0);
+  Y_0 = config->GetFFD_Axis(1);
+  Z_0 = config->GetFFD_Axis(2);
 
   for (kDegree = 0; kDegree <= nDegree; kDegree++) {
     for (jDegree = 0; jDegree <= mDegree; jDegree++) {
       for (iDegree = 0; iDegree <= lDegree; iDegree++) {
-
-
-         PolarCoord[0] = Coord_Control_Points[iDegree][jDegree][kDegree][0];
-         PolarCoord[1] = Coord_Control_Points[iDegree][jDegree][kDegree][1];
-         PolarCoord[2] = Coord_Control_Points[iDegree][jDegree][kDegree][2];
-
+        PolarCoord[0] = Coord_Control_Points[iDegree][jDegree][kDegree][0];
+        PolarCoord[1] = Coord_Control_Points[iDegree][jDegree][kDegree][1];
+        PolarCoord[2] = Coord_Control_Points[iDegree][jDegree][kDegree][2];
 
         Xbar = PolarCoord[2];
         Ybar = PolarCoord[0] * cos(PolarCoord[1]);
         Zbar = PolarCoord[0] * sin(PolarCoord[1]);
 
-        PolarCoord[0] =  Xbar +X_0;  PolarCoord[1] = Ybar +Y_0; PolarCoord[2] = Zbar +Z_0;
+        PolarCoord[0] = Xbar + X_0;
+        PolarCoord[1] = Ybar + Y_0;
+        PolarCoord[2] = Zbar + Z_0;
 
         Coord_Control_Points[iDegree][jDegree][kDegree][0] = PolarCoord[0];
         Coord_Control_Points[iDegree][jDegree][kDegree][1] = PolarCoord[1];
         Coord_Control_Points[iDegree][jDegree][kDegree][2] = PolarCoord[2];
-
       }
     }
   }
-
 }
 
-void CFreeFormDefBox::SetCart2Cyl_CornerPoints(CConfig *config) {
-
+void CFreeFormDefBox::SetCart2Cyl_CornerPoints(CConfig* config) {
   unsigned short iCornerPoint;
-  su2double *CartCoord;
+  su2double* CartCoord;
   su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
 
-  X_0 = config->GetFFD_Axis(0); Y_0 = config->GetFFD_Axis(1);  Z_0 = config->GetFFD_Axis(2);
+  X_0 = config->GetFFD_Axis(0);
+  Y_0 = config->GetFFD_Axis(1);
+  Z_0 = config->GetFFD_Axis(2);
 
   for (iCornerPoint = 0; iCornerPoint < 8; iCornerPoint++) {
-
     CartCoord = GetCoordCornerPoints(iCornerPoint);
-    Xbar =  CartCoord[0] - X_0; Ybar =  CartCoord[1] - Y_0; Zbar =  CartCoord[2] - Z_0;
-
-    CartCoord[0] = sqrt(Ybar*Ybar + Zbar*Zbar);
-    CartCoord[1] = atan2 ( Zbar, Ybar); if (CartCoord[1] > PI_NUMBER/2.0) CartCoord[1] -= 2.0*PI_NUMBER;
-    CartCoord[2] =  Xbar;
-
+    Xbar = CartCoord[0] - X_0;
+    Ybar = CartCoord[1] - Y_0;
+    Zbar = CartCoord[2] - Z_0;
+
+    CartCoord[0] = sqrt(Ybar * Ybar + Zbar * Zbar);
+    CartCoord[1] = atan2(Zbar, Ybar);
+    if (CartCoord[1] > PI_NUMBER / 2.0) CartCoord[1] -= 2.0 * PI_NUMBER;
+    CartCoord[2] = Xbar;
   }
-
 }
 
-
-void CFreeFormDefBox::SetCyl2Cart_CornerPoints(CConfig *config) {
-
+void CFreeFormDefBox::SetCyl2Cart_CornerPoints(CConfig* config) {
   unsigned short iCornerPoint;
-  su2double *PolarCoord;
+  su2double* PolarCoord;
   su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
 
-  X_0 = config->GetFFD_Axis(0); Y_0 = config->GetFFD_Axis(1);  Z_0 = config->GetFFD_Axis(2);
+  X_0 = config->GetFFD_Axis(0);
+  Y_0 = config->GetFFD_Axis(1);
+  Z_0 = config->GetFFD_Axis(2);
 
   for (iCornerPoint = 0; iCornerPoint < 8; iCornerPoint++) {
-
     PolarCoord = GetCoordCornerPoints(iCornerPoint);
 
     Xbar = PolarCoord[2];
     Ybar = PolarCoord[0] * cos(PolarCoord[1]);
     Zbar = PolarCoord[0] * sin(PolarCoord[1]);
 
-    PolarCoord[0] =  Xbar + X_0;  PolarCoord[1] = Ybar + Y_0; PolarCoord[2] = Zbar + Z_0;
-
+    PolarCoord[0] = Xbar + X_0;
+    PolarCoord[1] = Ybar + Y_0;
+    PolarCoord[2] = Zbar + Z_0;
   }
-
 }
 
-void CFreeFormDefBox::SetCart2Sphe_ControlPoints(CConfig *config) {
-
+void CFreeFormDefBox::SetCart2Sphe_ControlPoints(CConfig* config) {
   unsigned short iDegree, jDegree, kDegree;
   su2double CartCoord[3];
   su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
 
-  X_0 = config->GetFFD_Axis(0); Y_0 = config->GetFFD_Axis(1);  Z_0 = config->GetFFD_Axis(2);
+  X_0 = config->GetFFD_Axis(0);
+  Y_0 = config->GetFFD_Axis(1);
+  Z_0 = config->GetFFD_Axis(2);
 
   for (kDegree = 0; kDegree <= nDegree; kDegree++) {
     for (jDegree = 0; jDegree <= mDegree; jDegree++) {
       for (iDegree = 0; iDegree <= lDegree; iDegree++) {
-
         CartCoord[0] = Coord_Control_Points[iDegree][jDegree][kDegree][0];
         CartCoord[1] = Coord_Control_Points[iDegree][jDegree][kDegree][1];
         CartCoord[2] = Coord_Control_Points[iDegree][jDegree][kDegree][2];
 
-        Xbar =  CartCoord[0] - X_0; Ybar =  CartCoord[1] - Y_0; Zbar =  CartCoord[2] - Z_0;
+        Xbar = CartCoord[0] - X_0;
+        Ybar = CartCoord[1] - Y_0;
+        Zbar = CartCoord[2] - Z_0;
 
-        Coord_Control_Points[iDegree][jDegree][kDegree][0] = sqrt(Xbar*Xbar + Ybar*Ybar + Zbar*Zbar);
-        Coord_Control_Points[iDegree][jDegree][kDegree][1] = atan2 ( Zbar, Ybar);
-        if (Coord_Control_Points[iDegree][jDegree][kDegree][1] > PI_NUMBER/2.0) Coord_Control_Points[iDegree][jDegree][kDegree][1] -= 2.0*PI_NUMBER;
-        Coord_Control_Points[iDegree][jDegree][kDegree][2] = acos(Xbar/Coord_Control_Points[iDegree][jDegree][kDegree][0] );
+        Coord_Control_Points[iDegree][jDegree][kDegree][0] = sqrt(Xbar * Xbar + Ybar * Ybar + Zbar * Zbar);
+        Coord_Control_Points[iDegree][jDegree][kDegree][1] = atan2(Zbar, Ybar);
+        if (Coord_Control_Points[iDegree][jDegree][kDegree][1] > PI_NUMBER / 2.0)
+          Coord_Control_Points[iDegree][jDegree][kDegree][1] -= 2.0 * PI_NUMBER;
+        Coord_Control_Points[iDegree][jDegree][kDegree][2] =
+            acos(Xbar / Coord_Control_Points[iDegree][jDegree][kDegree][0]);
 
         CartCoord[0] = Coord_Control_Points_Copy[iDegree][jDegree][kDegree][0];
         CartCoord[1] = Coord_Control_Points_Copy[iDegree][jDegree][kDegree][1];
         CartCoord[2] = Coord_Control_Points_Copy[iDegree][jDegree][kDegree][2];
 
-        Xbar =  CartCoord[0] - X_0; Ybar =  CartCoord[1] - Y_0; Zbar =  CartCoord[2] - Z_0;
-
-        Coord_Control_Points_Copy[iDegree][jDegree][kDegree][0] = sqrt(Xbar*Xbar + Ybar*Ybar + Zbar*Zbar);
-        Coord_Control_Points_Copy[iDegree][jDegree][kDegree][1] = atan2 ( Zbar, Ybar);
-        if (Coord_Control_Points_Copy[iDegree][jDegree][kDegree][1] > PI_NUMBER/2.0)
-          Coord_Control_Points_Copy[iDegree][jDegree][kDegree][1]  -= 2.0*PI_NUMBER;
-        Coord_Control_Points_Copy[iDegree][jDegree][kDegree][2] = acos(Xbar/Coord_Control_Points_Copy[iDegree][jDegree][kDegree][0]);
+        Xbar = CartCoord[0] - X_0;
+        Ybar = CartCoord[1] - Y_0;
+        Zbar = CartCoord[2] - Z_0;
 
+        Coord_Control_Points_Copy[iDegree][jDegree][kDegree][0] = sqrt(Xbar * Xbar + Ybar * Ybar + Zbar * Zbar);
+        Coord_Control_Points_Copy[iDegree][jDegree][kDegree][1] = atan2(Zbar, Ybar);
+        if (Coord_Control_Points_Copy[iDegree][jDegree][kDegree][1] > PI_NUMBER / 2.0)
+          Coord_Control_Points_Copy[iDegree][jDegree][kDegree][1] -= 2.0 * PI_NUMBER;
+        Coord_Control_Points_Copy[iDegree][jDegree][kDegree][2] =
+            acos(Xbar / Coord_Control_Points_Copy[iDegree][jDegree][kDegree][0]);
       }
     }
   }
-
 }
 
-void CFreeFormDefBox::SetSphe2Cart_ControlPoints(CConfig *config) {
-
+void CFreeFormDefBox::SetSphe2Cart_ControlPoints(CConfig* config) {
   unsigned short iDegree, jDegree, kDegree;
   su2double PolarCoord[3];
 
-   su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
-  X_0 = config->GetFFD_Axis(0); Y_0 = config->GetFFD_Axis(1);  Z_0 = config->GetFFD_Axis(2);
+  su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
+  X_0 = config->GetFFD_Axis(0);
+  Y_0 = config->GetFFD_Axis(1);
+  Z_0 = config->GetFFD_Axis(2);
 
   for (kDegree = 0; kDegree <= nDegree; kDegree++) {
     for (jDegree = 0; jDegree <= mDegree; jDegree++) {
       for (iDegree = 0; iDegree <= lDegree; iDegree++) {
-
         PolarCoord[0] = Coord_Control_Points[iDegree][jDegree][kDegree][0];
         PolarCoord[1] = Coord_Control_Points[iDegree][jDegree][kDegree][1];
         PolarCoord[2] = Coord_Control_Points[iDegree][jDegree][kDegree][2];
@@ -458,64 +496,63 @@ void CFreeFormDefBox::SetSphe2Cart_ControlPoints(CConfig *config) {
         Ybar = PolarCoord[0] * cos(PolarCoord[1]) * sin(PolarCoord[2]);
         Zbar = PolarCoord[0] * sin(PolarCoord[1]) * sin(PolarCoord[2]);
 
-        PolarCoord[0] = Xbar + X_0;  PolarCoord[1] = Ybar + Y_0; PolarCoord[2] = Zbar + Z_0;
+        PolarCoord[0] = Xbar + X_0;
+        PolarCoord[1] = Ybar + Y_0;
+        PolarCoord[2] = Zbar + Z_0;
 
         Coord_Control_Points[iDegree][jDegree][kDegree][0] = PolarCoord[0];
         Coord_Control_Points[iDegree][jDegree][kDegree][1] = PolarCoord[1];
         Coord_Control_Points[iDegree][jDegree][kDegree][2] = PolarCoord[2];
-
       }
     }
   }
-
 }
 
-void CFreeFormDefBox::SetCart2Sphe_CornerPoints(CConfig *config) {
-
+void CFreeFormDefBox::SetCart2Sphe_CornerPoints(CConfig* config) {
   unsigned short iCornerPoint;
-  su2double *CartCoord;
+  su2double* CartCoord;
   su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
 
-  X_0 = config->GetFFD_Axis(0); Y_0 = config->GetFFD_Axis(1);  Z_0 = config->GetFFD_Axis(2);
+  X_0 = config->GetFFD_Axis(0);
+  Y_0 = config->GetFFD_Axis(1);
+  Z_0 = config->GetFFD_Axis(2);
 
   for (iCornerPoint = 0; iCornerPoint < 8; iCornerPoint++) {
-
     CartCoord = GetCoordCornerPoints(iCornerPoint);
-    Xbar =  CartCoord[0] - X_0; Ybar =  CartCoord[1] - Y_0; Zbar =  CartCoord[2] - Z_0;
-
-    CartCoord[0] = sqrt(Xbar*Xbar + Ybar*Ybar + Zbar*Zbar);
-    CartCoord[1] = atan2(Zbar, Ybar);  if (CartCoord[1] > PI_NUMBER/2.0) CartCoord[1] -= 2.0*PI_NUMBER;
-    CartCoord[2] = acos(Xbar/CartCoord[0]);
-
+    Xbar = CartCoord[0] - X_0;
+    Ybar = CartCoord[1] - Y_0;
+    Zbar = CartCoord[2] - Z_0;
+
+    CartCoord[0] = sqrt(Xbar * Xbar + Ybar * Ybar + Zbar * Zbar);
+    CartCoord[1] = atan2(Zbar, Ybar);
+    if (CartCoord[1] > PI_NUMBER / 2.0) CartCoord[1] -= 2.0 * PI_NUMBER;
+    CartCoord[2] = acos(Xbar / CartCoord[0]);
   }
-
 }
 
-
-void CFreeFormDefBox::SetSphe2Cart_CornerPoints(CConfig *config) {
-
+void CFreeFormDefBox::SetSphe2Cart_CornerPoints(CConfig* config) {
   unsigned short iCornerPoint;
-  su2double *PolarCoord;
+  su2double* PolarCoord;
   su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
 
-  X_0 = config->GetFFD_Axis(0); Y_0 = config->GetFFD_Axis(1);  Z_0 = config->GetFFD_Axis(2);
+  X_0 = config->GetFFD_Axis(0);
+  Y_0 = config->GetFFD_Axis(1);
+  Z_0 = config->GetFFD_Axis(2);
 
   for (iCornerPoint = 0; iCornerPoint < 8; iCornerPoint++) {
-
     PolarCoord = GetCoordCornerPoints(iCornerPoint);
 
     Xbar = PolarCoord[0] * cos(PolarCoord[2]);
     Ybar = PolarCoord[0] * cos(PolarCoord[1]) * sin(PolarCoord[2]);
     Zbar = PolarCoord[0] * sin(PolarCoord[1]) * sin(PolarCoord[2]);
 
-    PolarCoord[0] =  Xbar + X_0;  PolarCoord[1] = Ybar + Y_0; PolarCoord[2] = Zbar + Z_0;
-
+    PolarCoord[0] = Xbar + X_0;
+    PolarCoord[1] = Ybar + Y_0;
+    PolarCoord[2] = Zbar + Z_0;
   }
-
 }
 
-
-void CFreeFormDefBox::SetCGNS(CGeometry *geometry, unsigned short iFFDBox, bool original) {
+void CFreeFormDefBox::SetCGNS(CGeometry* geometry, unsigned short iFFDBox, bool original) {
 #ifdef HAVE_CGNS
 
   char FFDBox_filename[MAX_STRING_SIZE];
@@ -526,39 +563,38 @@ void CFreeFormDefBox::SetCGNS(CGeometry *geometry, unsigned short iFFDBox, bool
   char zonename[33];
   int FFDBox_cgns_file;
   int cell_dim, phys_dim;
-  int cgns_base=0, cgns_family, cgns_zone, cgns_err, dummy;
-  const char * basename;
+  int cgns_base = 0, cgns_family, cgns_zone, cgns_err, dummy;
+  const char* basename;
 
   /*--- FFD output is always 3D (even in 2D problems),
    this is important for debuging ---*/
   nDim = geometry->GetnDim();
-  cell_dim = nDim,
-  phys_dim = 3;
+  cell_dim = nDim, phys_dim = 3;
 
-  SPRINTF (FFDBox_filename, "ffd_boxes.cgns");
+  SPRINTF(FFDBox_filename, "ffd_boxes.cgns");
 
-  if ((original) && (iFFDBox == 0)) new_file = true;
-  else new_file = false;
+  if ((original) && (iFFDBox == 0))
+    new_file = true;
+  else
+    new_file = false;
 
   if (new_file) {
     cgns_err = cg_open(FFDBox_filename, CG_MODE_WRITE, &FFDBox_cgns_file);
     if (cgns_err) cg_error_print();
-    cgns_err = cg_descriptor_write("Title", "Visualization of the FFD boxes generated by SU2_DEF." );
+    cgns_err = cg_descriptor_write("Title", "Visualization of the FFD boxes generated by SU2_DEF.");
     if (cgns_err) cg_error_print();
-  }
-  else {
+  } else {
     cgns_err = cg_open(FFDBox_filename, CG_MODE_MODIFY, &FFDBox_cgns_file);
     if (cgns_err) cg_error_print();
   }
 
   if (original) {
     basename = "Original_FFD";
-  }
-  else {
+  } else {
     basename = "Deformed_FFD";
   }
 
-  if (iFFDBox == 0){
+  if (iFFDBox == 0) {
     cgns_err = cg_base_write(FFDBox_cgns_file, basename, cell_dim, phys_dim, &cgns_base);
     if (cgns_err) cg_error_print();
   }
@@ -566,20 +602,20 @@ void CFreeFormDefBox::SetCGNS(CGeometry *geometry, unsigned short iFFDBox, bool
   if (cgns_err) cg_error_print();
 
   cgsize_t dims[9];
-  dims[0] = lDegree+1;
-  dims[1] = mDegree+1;
-  if (cell_dim == 3){
-     dims[2] = nDegree+1;
+  dims[0] = lDegree + 1;
+  dims[1] = mDegree + 1;
+  if (cell_dim == 3) {
+    dims[2] = nDegree + 1;
   }
   cgsize_t pointlen = 1;
-  for(int ii=0; ii<cell_dim; ii++){
-    dims[ii+cell_dim] = dims[ii] -1;
-    dims[ii+2*cell_dim] = 0;
+  for (int ii = 0; ii < cell_dim; ii++) {
+    dims[ii + cell_dim] = dims[ii] - 1;
+    dims[ii + 2 * cell_dim] = 0;
     pointlen *= dims[ii];
   }
 
-  passivedouble *buffer = new passivedouble[pointlen];
-  SPRINTF (zonename, "SU2_Zone_%d", SU2_TYPE::Int(iFFDBox));
+  passivedouble* buffer = new passivedouble[pointlen];
+  SPRINTF(zonename, "SU2_Zone_%d", SU2_TYPE::Int(iFFDBox));
 
   cgns_err = cg_zone_write(FFDBox_cgns_file, cgns_base, zonename, dims, CGNS_ENUMV(Structured), &cgns_zone);
   if (cgns_err) cg_error_print();
@@ -588,69 +624,75 @@ void CFreeFormDefBox::SetCGNS(CGeometry *geometry, unsigned short iFFDBox, bool
   cgns_err = cg_famname_write(Tag.c_str());
   if (cgns_err) cg_error_print();
 
-
-  const char* coord_names[3] = { "CoordinateX", "CoordinateY", "CoordinateZ" };
-  for (iDim=0; iDim<nDim; iDim++)
-  {
-    outDim = nDim == 2 ? 0: nDegree;
+  const char* coord_names[3] = {"CoordinateX", "CoordinateY", "CoordinateZ"};
+  for (iDim = 0; iDim < nDim; iDim++) {
+    outDim = nDim == 2 ? 0 : nDegree;
     for (kDegree = 0; kDegree <= outDim; kDegree++) {
       for (jDegree = 0; jDegree <= mDegree; jDegree++) {
         for (iDegree = 0; iDegree <= lDegree; iDegree++) {
-          pos = iDegree + jDegree*(lDegree+1)+ kDegree*(lDegree+1)*(mDegree+1);
+          pos = iDegree + jDegree * (lDegree + 1) + kDegree * (lDegree + 1) * (mDegree + 1);
           buffer[pos] = SU2_TYPE::GetValue(Coord_Control_Points[iDegree][jDegree][kDegree][iDim]);
         }
       }
     }
-    cgns_err = cg_coord_write(FFDBox_cgns_file, cgns_base, cgns_zone, CGNS_ENUMV(RealDouble), coord_names[iDim], buffer, &dummy);
+    cgns_err = cg_coord_write(FFDBox_cgns_file, cgns_base, cgns_zone, CGNS_ENUMV(RealDouble), coord_names[iDim], buffer,
+                              &dummy);
     if (cgns_err) cg_error_print();
-
   }
-  if (nDim==2){
+  if (nDim == 2) {
     std::fill_n(buffer, pointlen, 0.0);
-    cgns_err = cg_coord_write(FFDBox_cgns_file, cgns_base, cgns_zone, CGNS_ENUMV(RealDouble), coord_names[2], buffer, &dummy);
+    cgns_err =
+        cg_coord_write(FFDBox_cgns_file, cgns_base, cgns_zone, CGNS_ENUMV(RealDouble), coord_names[2], buffer, &dummy);
     if (cgns_err) cg_error_print();
   }
 
-  delete [] buffer;
+  delete[] buffer;
   cgns_err = cg_close(FFDBox_cgns_file);
   if (cgns_err) cg_error_print();
-#else // Not built with CGNS support
-  cout << "CGNS file requested for FFD but SU2 was built without CGNS support. No file written" << "\n";
+#else  // Not built with CGNS support
+  cout << "CGNS file requested for FFD but SU2 was built without CGNS support. No file written"
+       << "\n";
 #endif
 }
 
-
-void CFreeFormDefBox::SetTecplot(CGeometry *geometry, unsigned short iFFDBox, bool original) {
-
+void CFreeFormDefBox::SetTecplot(CGeometry* geometry, unsigned short iFFDBox, bool original) {
   ofstream FFDBox_file;
   char FFDBox_filename[MAX_STRING_SIZE];
   bool new_file;
   unsigned short iDim, iDegree, jDegree, kDegree;
 
-
   /*--- FFD output is always 3D (even in 2D problems),
    this is important for debuging ---*/
 
   nDim = 3;
 
-  SPRINTF (FFDBox_filename, "ffd_boxes.dat");
+  SPRINTF(FFDBox_filename, "ffd_boxes.dat");
 
-  if ((original) && (iFFDBox == 0)) new_file = true;
-  else new_file = false;
+  if ((original) && (iFFDBox == 0))
+    new_file = true;
+  else
+    new_file = false;
 
   if (new_file) {
     FFDBox_file.open(FFDBox_filename, ios::out);
     FFDBox_file << "TITLE = \"Visualization of the FFD boxes generated by SU2_DEF.\"" << endl;
-    if (nDim == 2) FFDBox_file << "VARIABLES = \"x\", \"y\"" << endl;
-    else FFDBox_file << "VARIABLES = \"x\", \"y\", \"z\"" << endl;
-  }
-  else FFDBox_file.open(FFDBox_filename, ios::out | ios::app);
+    if (nDim == 2)
+      FFDBox_file << "VARIABLES = \"x\", \"y\"" << endl;
+    else
+      FFDBox_file << "VARIABLES = \"x\", \"y\", \"z\"" << endl;
+  } else
+    FFDBox_file.open(FFDBox_filename, ios::out | ios::app);
 
   FFDBox_file << "ZONE T= \"" << Tag;
-  if (original) FFDBox_file << " (Original FFD)\"";
-  else FFDBox_file << " (Deformed FFD)\"";
-  if (nDim == 2) FFDBox_file << ", I="<<lDegree+1<<", J="<<mDegree+1<<", DATAPACKING=POINT" << endl;
-  else FFDBox_file << ", I="<<lDegree+1<<", J="<<mDegree+1<<", K="<<nDegree+1<<", DATAPACKING=POINT" << endl;
+  if (original)
+    FFDBox_file << " (Original FFD)\"";
+  else
+    FFDBox_file << " (Deformed FFD)\"";
+  if (nDim == 2)
+    FFDBox_file << ", I=" << lDegree + 1 << ", J=" << mDegree + 1 << ", DATAPACKING=POINT" << endl;
+  else
+    FFDBox_file << ", I=" << lDegree + 1 << ", J=" << mDegree + 1 << ", K=" << nDegree + 1 << ", DATAPACKING=POINT"
+                << endl;
 
   FFDBox_file.precision(15);
 
@@ -662,8 +704,7 @@ void CFreeFormDefBox::SetTecplot(CGeometry *geometry, unsigned short iFFDBox, bo
         FFDBox_file << "\n";
       }
     }
-  }
-  else {
+  } else {
     for (kDegree = 0; kDegree <= nDegree; kDegree++) {
       for (jDegree = 0; jDegree <= mDegree; jDegree++) {
         for (iDegree = 0; iDegree <= lDegree; iDegree++) {
@@ -678,8 +719,7 @@ void CFreeFormDefBox::SetTecplot(CGeometry *geometry, unsigned short iFFDBox, bo
   FFDBox_file.close();
 }
 
-void CFreeFormDefBox::SetParaview(CGeometry *geometry, unsigned short iFFDBox, bool original) {
-
+void CFreeFormDefBox::SetParaview(CGeometry* geometry, unsigned short iFFDBox, bool original) {
   ofstream FFDBox_file;
   char FFDBox_filename[MAX_STRING_SIZE];
   bool new_file;
@@ -687,11 +727,15 @@ void CFreeFormDefBox::SetParaview(CGeometry *geometry, unsigned short iFFDBox, b
 
   nDim = geometry->GetnDim();
 
-  if (original) new_file = true;
-  else new_file = false;
+  if (original)
+    new_file = true;
+  else
+    new_file = false;
 
-  if (new_file) SPRINTF (FFDBox_filename, "ffd_boxes_%d.vtk", SU2_TYPE::Int(iFFDBox));
-  else SPRINTF (FFDBox_filename, "ffd_boxes_def_%d.vtk", SU2_TYPE::Int(iFFDBox));
+  if (new_file)
+    SPRINTF(FFDBox_filename, "ffd_boxes_%d.vtk", SU2_TYPE::Int(iFFDBox));
+  else
+    SPRINTF(FFDBox_filename, "ffd_boxes_def_%d.vtk", SU2_TYPE::Int(iFFDBox));
 
   FFDBox_file.open(FFDBox_filename, ios::out);
   FFDBox_file << "# vtk DataFile Version 3.0" << endl;
@@ -699,10 +743,14 @@ void CFreeFormDefBox::SetParaview(CGeometry *geometry, unsigned short iFFDBox, b
   FFDBox_file << "ASCII" << endl;
   FFDBox_file << "DATASET STRUCTURED_GRID" << endl;
 
-  if (nDim == 2) FFDBox_file << "DIMENSIONS "<<lDegree+1<<" "<<mDegree+1<<" "<<1<< endl;
-  else FFDBox_file << "DIMENSIONS "<<lDegree+1<<" "<<mDegree+1<<" "<<nDegree+1<< endl;
-  if (nDim == 2) FFDBox_file << "POINTS "<<(lDegree+1)*(mDegree+1)<<" float"<< endl;
-  else FFDBox_file << "POINTS "<<(lDegree+1)*(mDegree+1)*(nDegree+1)<<" float"<< endl;
+  if (nDim == 2)
+    FFDBox_file << "DIMENSIONS " << lDegree + 1 << " " << mDegree + 1 << " " << 1 << endl;
+  else
+    FFDBox_file << "DIMENSIONS " << lDegree + 1 << " " << mDegree + 1 << " " << nDegree + 1 << endl;
+  if (nDim == 2)
+    FFDBox_file << "POINTS " << (lDegree + 1) * (mDegree + 1) << " float" << endl;
+  else
+    FFDBox_file << "POINTS " << (lDegree + 1) * (mDegree + 1) * (nDegree + 1) << " float" << endl;
 
   FFDBox_file.precision(15);
 
@@ -710,17 +758,16 @@ void CFreeFormDefBox::SetParaview(CGeometry *geometry, unsigned short iFFDBox, b
     for (jDegree = 0; jDegree <= mDegree; jDegree++) {
       for (iDegree = 0; iDegree <= lDegree; iDegree++) {
         for (iDim = 0; iDim < nDim; iDim++)
-        FFDBox_file << scientific << Coord_Control_Points[iDegree][jDegree][0][iDim] << "\t";
+          FFDBox_file << scientific << Coord_Control_Points[iDegree][jDegree][0][iDim] << "\t";
         FFDBox_file << " 0.0 \n";
       }
     }
-  }
-  else {
+  } else {
     for (kDegree = 0; kDegree <= nDegree; kDegree++) {
       for (jDegree = 0; jDegree <= mDegree; jDegree++) {
         for (iDegree = 0; iDegree <= lDegree; iDegree++) {
           for (iDim = 0; iDim < nDim; iDim++)
-          FFDBox_file << scientific << Coord_Control_Points[iDegree][jDegree][kDegree][iDim] << "\t";
+            FFDBox_file << scientific << Coord_Control_Points[iDegree][jDegree][kDegree][iDim] << "\t";
           FFDBox_file << "\n";
         }
       }
@@ -728,158 +775,157 @@ void CFreeFormDefBox::SetParaview(CGeometry *geometry, unsigned short iFFDBox, b
   }
 
   FFDBox_file.close();
-
 }
 
-su2double *CFreeFormDefBox::GetParametricCoord_Analytical(const su2double *cart_coord) {
+su2double* CFreeFormDefBox::GetParametricCoord_Analytical(const su2double* cart_coord) {
   unsigned short iDim;
   su2double *e1, *e2, *e3, *e12, *e23, *e13, *p;
 
   /*--- Auxiliary Basis Vectors of the deformed FFDBox ---*/
-  e1 = new su2double[3]; e2 = new su2double[3]; e3 = new su2double[3];
+  e1 = new su2double[3];
+  e2 = new su2double[3];
+  e3 = new su2double[3];
   for (iDim = 0; iDim < nDim; iDim++) {
-    e1[iDim] = Coord_Corner_Points[1][iDim]-Coord_Corner_Points[0][iDim];
-    e2[iDim] = Coord_Corner_Points[3][iDim]-Coord_Corner_Points[0][iDim];
-    e3[iDim] = Coord_Corner_Points[4][iDim]-Coord_Corner_Points[0][iDim];
+    e1[iDim] = Coord_Corner_Points[1][iDim] - Coord_Corner_Points[0][iDim];
+    e2[iDim] = Coord_Corner_Points[3][iDim] - Coord_Corner_Points[0][iDim];
+    e3[iDim] = Coord_Corner_Points[4][iDim] - Coord_Corner_Points[0][iDim];
   }
 
   /*--- Respective Cross-Products ---*/
-  e12 = new su2double[3]; e23 = new su2double[3]; e13 = new su2double[3];
+  e12 = new su2double[3];
+  e23 = new su2double[3];
+  e13 = new su2double[3];
   CrossProduct(e1, e2, e12);
   CrossProduct(e1, e3, e13);
   CrossProduct(e2, e3, e23);
 
   /*--- p is Tranlated vector from the origin ---*/
   p = new su2double[3];
-  for (iDim = 0; iDim < nDim; iDim++)
-    p[iDim] = cart_coord[iDim] - Coord_Corner_Points[0][iDim];
+  for (iDim = 0; iDim < nDim; iDim++) p[iDim] = cart_coord[iDim] - Coord_Corner_Points[0][iDim];
 
-  ParamCoord[0] = DotProduct(e23, p)/DotProduct(e23, e1);
-  ParamCoord[1] = DotProduct(e13, p)/DotProduct(e13, e2);
-  ParamCoord[2] = DotProduct(e12, p)/DotProduct(e12, e3);
+  ParamCoord[0] = DotProduct(e23, p) / DotProduct(e23, e1);
+  ParamCoord[1] = DotProduct(e13, p) / DotProduct(e13, e2);
+  ParamCoord[2] = DotProduct(e12, p) / DotProduct(e12, e3);
 
-  delete [] e1;
-  delete [] e2;
-  delete [] e3;
-  delete [] e12;
-  delete [] e23;
-  delete [] e13;
-  delete [] p;
+  delete[] e1;
+  delete[] e2;
+  delete[] e3;
+  delete[] e12;
+  delete[] e23;
+  delete[] e13;
+  delete[] p;
 
   return ParamCoord;
 }
 
-su2double *CFreeFormDefBox::EvalCartesianCoord(su2double *ParamCoord) const {
+su2double* CFreeFormDefBox::EvalCartesianCoord(su2double* ParamCoord) const {
   unsigned short iDim, iDegree, jDegree, kDegree;
 
-  for (iDim = 0; iDim < nDim; iDim++)
-    cart_coord[iDim] = 0.0;
+  for (iDim = 0; iDim < nDim; iDim++) cart_coord[iDim] = 0.0;
 
   for (iDegree = 0; iDegree <= lDegree; iDegree++)
     for (jDegree = 0; jDegree <= mDegree; jDegree++)
       for (kDegree = 0; kDegree <= nDegree; kDegree++)
         for (iDim = 0; iDim < nDim; iDim++) {
-          cart_coord[iDim] += Coord_Control_Points[iDegree][jDegree][kDegree][iDim]
-          * BlendingFunction[0]->GetBasis(iDegree, ParamCoord[0])
-          * BlendingFunction[1]->GetBasis(jDegree, ParamCoord[1])
-          * BlendingFunction[2]->GetBasis(kDegree, ParamCoord[2]);
+          cart_coord[iDim] += Coord_Control_Points[iDegree][jDegree][kDegree][iDim] *
+                              BlendingFunction[0]->GetBasis(iDegree, ParamCoord[0]) *
+                              BlendingFunction[1]->GetBasis(jDegree, ParamCoord[1]) *
+                              BlendingFunction[2]->GetBasis(kDegree, ParamCoord[2]);
         }
 
   return cart_coord;
 }
 
-
-su2double *CFreeFormDefBox::GetFFDGradient(su2double *val_coord, su2double *xyz) {
-
+su2double* CFreeFormDefBox::GetFFDGradient(su2double* val_coord, su2double* xyz) {
   unsigned short iDim, jDim, lmn[3];
 
   /*--- Set the Degree of the spline ---*/
 
-  lmn[0] = lDegree; lmn[1] = mDegree; lmn[2] = nDegree;
+  lmn[0] = lDegree;
+  lmn[1] = mDegree;
+  lmn[2] = nDegree;
 
   for (iDim = 0; iDim < nDim; iDim++) Gradient[iDim] = 0.0;
 
   for (iDim = 0; iDim < nDim; iDim++)
     for (jDim = 0; jDim < nDim; jDim++)
-      Gradient[jDim] += GetDerivative2(val_coord, iDim, xyz,  lmn) *
-      GetDerivative3(val_coord, iDim, jDim, lmn);
+      Gradient[jDim] += GetDerivative2(val_coord, iDim, xyz, lmn) * GetDerivative3(val_coord, iDim, jDim, lmn);
 
   return Gradient;
-
 }
 
-void CFreeFormDefBox::GetFFDHessian(su2double *uvw, su2double *xyz, su2double **val_Hessian) {
-
+void CFreeFormDefBox::GetFFDHessian(su2double* uvw, su2double* xyz, su2double** val_Hessian) {
   unsigned short iDim, jDim, lmn[3];
 
   /*--- Set the Degree of the spline ---*/
 
-  lmn[0] = lDegree; lmn[1] = mDegree; lmn[2] = nDegree;
+  lmn[0] = lDegree;
+  lmn[1] = mDegree;
+  lmn[2] = nDegree;
 
   for (iDim = 0; iDim < nDim; iDim++)
-    for (jDim = 0; jDim < nDim; jDim++)
-      val_Hessian[iDim][jDim] = 0.0;
+    for (jDim = 0; jDim < nDim; jDim++) val_Hessian[iDim][jDim] = 0.0;
 
   /*--- Note that being all the functions linear combinations of polynomials, they are C^\infty,
    and the Hessian will be symmetric; no need to compute the under-diagonal part, for example ---*/
 
   for (iDim = 0; iDim < nDim; iDim++) {
-    val_Hessian[0][0] += 2.0 * GetDerivative3(uvw, iDim,0, lmn) * GetDerivative3(uvw, iDim,0, lmn) +
-    GetDerivative2(uvw, iDim,xyz, lmn) * GetDerivative5(uvw, iDim,0,0, lmn);
+    val_Hessian[0][0] += 2.0 * GetDerivative3(uvw, iDim, 0, lmn) * GetDerivative3(uvw, iDim, 0, lmn) +
+                         GetDerivative2(uvw, iDim, xyz, lmn) * GetDerivative5(uvw, iDim, 0, 0, lmn);
 
-    val_Hessian[1][1] += 2.0 * GetDerivative3(uvw, iDim,1, lmn) * GetDerivative3(uvw, iDim,1, lmn) +
-    GetDerivative2(uvw, iDim,xyz, lmn) * GetDerivative5(uvw, iDim,1,1, lmn);
+    val_Hessian[1][1] += 2.0 * GetDerivative3(uvw, iDim, 1, lmn) * GetDerivative3(uvw, iDim, 1, lmn) +
+                         GetDerivative2(uvw, iDim, xyz, lmn) * GetDerivative5(uvw, iDim, 1, 1, lmn);
 
-    val_Hessian[2][2] += 2.0 * GetDerivative3(uvw, iDim,2, lmn) * GetDerivative3(uvw, iDim,2, lmn) +
-    GetDerivative2(uvw, iDim,xyz, lmn) * GetDerivative5(uvw, iDim,2,2, lmn);
+    val_Hessian[2][2] += 2.0 * GetDerivative3(uvw, iDim, 2, lmn) * GetDerivative3(uvw, iDim, 2, lmn) +
+                         GetDerivative2(uvw, iDim, xyz, lmn) * GetDerivative5(uvw, iDim, 2, 2, lmn);
 
-    val_Hessian[0][1] += 2.0 * GetDerivative3(uvw, iDim,0, lmn) * GetDerivative3(uvw, iDim,1, lmn) +
-    GetDerivative2(uvw, iDim,xyz, lmn) * GetDerivative5(uvw, iDim,0,1, lmn);
+    val_Hessian[0][1] += 2.0 * GetDerivative3(uvw, iDim, 0, lmn) * GetDerivative3(uvw, iDim, 1, lmn) +
+                         GetDerivative2(uvw, iDim, xyz, lmn) * GetDerivative5(uvw, iDim, 0, 1, lmn);
 
-    val_Hessian[0][2] += 2.0 * GetDerivative3(uvw, iDim,0, lmn) * GetDerivative3(uvw, iDim,2, lmn) +
-    GetDerivative2(uvw, iDim,xyz, lmn) * GetDerivative5(uvw, iDim,0,2, lmn);
+    val_Hessian[0][2] += 2.0 * GetDerivative3(uvw, iDim, 0, lmn) * GetDerivative3(uvw, iDim, 2, lmn) +
+                         GetDerivative2(uvw, iDim, xyz, lmn) * GetDerivative5(uvw, iDim, 0, 2, lmn);
 
-    val_Hessian[1][2] += 2.0 * GetDerivative3(uvw, iDim,1, lmn) * GetDerivative3(uvw, iDim,2, lmn) +
-    GetDerivative2(uvw, iDim,xyz, lmn) * GetDerivative5(uvw, iDim,1,2, lmn);
+    val_Hessian[1][2] += 2.0 * GetDerivative3(uvw, iDim, 1, lmn) * GetDerivative3(uvw, iDim, 2, lmn) +
+                         GetDerivative2(uvw, iDim, xyz, lmn) * GetDerivative5(uvw, iDim, 1, 2, lmn);
   }
 
   val_Hessian[1][0] = val_Hessian[0][1];
   val_Hessian[2][0] = val_Hessian[0][2];
   val_Hessian[2][1] = val_Hessian[1][2];
-
 }
 
-su2double *CFreeFormDefBox::GetParametricCoord_Iterative(unsigned long iPoint, su2double *xyz, const su2double *ParamCoordGuess, CConfig *config) {
-
-  su2double *IndepTerm, SOR_Factor = 1.0, MinNormError, NormError, Determinant, AdjHessian[3][3], Temp[3] = {0.0,0.0,0.0};
+su2double* CFreeFormDefBox::GetParametricCoord_Iterative(unsigned long iPoint, su2double* xyz,
+                                                         const su2double* ParamCoordGuess, CConfig* config) {
+  su2double *IndepTerm, SOR_Factor = 1.0, MinNormError, NormError, Determinant, AdjHessian[3][3],
+                        Temp[3] = {0.0, 0.0, 0.0};
   unsigned short iDim, jDim, RandonCounter;
   unsigned long iter;
 
-  su2double tol = config->GetFFD_Tol()*1E-3;
+  su2double tol = config->GetFFD_Tol() * 1E-3;
   unsigned short it_max = config->GetnFFD_Iter();
   unsigned short Random_Trials = 500;
 
   /*--- Allocate the Hessian ---*/
 
-  Hessian = new su2double* [nDim];
-  IndepTerm = new su2double [nDim];
+  Hessian = new su2double*[nDim];
+  IndepTerm = new su2double[nDim];
   for (iDim = 0; iDim < nDim; iDim++) {
     Hessian[iDim] = new su2double[nDim];
     ParamCoord[iDim] = ParamCoordGuess[iDim];
-    IndepTerm [iDim] = 0.0;
+    IndepTerm[iDim] = 0.0;
   }
 
-  RandonCounter = 0; MinNormError = 1E6;
+  RandonCounter = 0;
+  MinNormError = 1E6;
 
   /*--- External iteration ---*/
 
-  for (iter = 0; iter < (unsigned long)it_max*Random_Trials; iter++) {
-
+  for (iter = 0; iter < (unsigned long)it_max * Random_Trials; iter++) {
     /*--- The independent term of the solution of our system is -Gradient(sol_old) ---*/
 
     Gradient = GetFFDGradient(ParamCoord, xyz);
 
-    for (iDim = 0; iDim < nDim; iDim++) IndepTerm[iDim] = - Gradient[iDim];
+    for (iDim = 0; iDim < nDim; iDim++) IndepTerm[iDim] = -Gradient[iDim];
 
     /*--- Hessian = The Matrix of our system, getHessian(sol_old,xyz,...) ---*/
 
@@ -887,19 +933,20 @@ su2double *CFreeFormDefBox::GetParametricCoord_Iterative(unsigned long iPoint, s
 
     /*--- Adjoint to Hessian ---*/
 
-    AdjHessian[0][0] = Hessian[1][1]*Hessian[2][2]-Hessian[1][2]*Hessian[2][1];
-    AdjHessian[0][1] = Hessian[0][2]*Hessian[2][1]-Hessian[0][1]*Hessian[2][2];
-    AdjHessian[0][2] = Hessian[0][1]*Hessian[1][2]-Hessian[0][2]*Hessian[1][1];
-    AdjHessian[1][0] = Hessian[1][2]*Hessian[2][0]-Hessian[1][0]*Hessian[2][2];
-    AdjHessian[1][1] = Hessian[0][0]*Hessian[2][2]-Hessian[0][2]*Hessian[2][0];
-    AdjHessian[1][2] = Hessian[0][2]*Hessian[1][0]-Hessian[0][0]*Hessian[1][2];
-    AdjHessian[2][0] = Hessian[1][0]*Hessian[2][1]-Hessian[1][1]*Hessian[2][0];
-    AdjHessian[2][1] = Hessian[0][1]*Hessian[2][0]-Hessian[0][0]*Hessian[2][1];
-    AdjHessian[2][2] = Hessian[0][0]*Hessian[1][1]-Hessian[0][1]*Hessian[1][0];
+    AdjHessian[0][0] = Hessian[1][1] * Hessian[2][2] - Hessian[1][2] * Hessian[2][1];
+    AdjHessian[0][1] = Hessian[0][2] * Hessian[2][1] - Hessian[0][1] * Hessian[2][2];
+    AdjHessian[0][2] = Hessian[0][1] * Hessian[1][2] - Hessian[0][2] * Hessian[1][1];
+    AdjHessian[1][0] = Hessian[1][2] * Hessian[2][0] - Hessian[1][0] * Hessian[2][2];
+    AdjHessian[1][1] = Hessian[0][0] * Hessian[2][2] - Hessian[0][2] * Hessian[2][0];
+    AdjHessian[1][2] = Hessian[0][2] * Hessian[1][0] - Hessian[0][0] * Hessian[1][2];
+    AdjHessian[2][0] = Hessian[1][0] * Hessian[2][1] - Hessian[1][1] * Hessian[2][0];
+    AdjHessian[2][1] = Hessian[0][1] * Hessian[2][0] - Hessian[0][0] * Hessian[2][1];
+    AdjHessian[2][2] = Hessian[0][0] * Hessian[1][1] - Hessian[0][1] * Hessian[1][0];
 
     /*--- Determinant of Hessian ---*/
 
-    Determinant = Hessian[0][0]*AdjHessian[0][0]+Hessian[0][1]*AdjHessian[1][0]+Hessian[0][2]*AdjHessian[2][0];
+    Determinant =
+        Hessian[0][0] * AdjHessian[0][0] + Hessian[0][1] * AdjHessian[1][0] + Hessian[0][2] * AdjHessian[2][0];
 
     /*--- Hessian inverse ---*/
 
@@ -907,7 +954,7 @@ su2double *CFreeFormDefBox::GetParametricCoord_Iterative(unsigned long iPoint, s
       for (iDim = 0; iDim < nDim; iDim++) {
         Temp[iDim] = 0.0;
         for (jDim = 0; jDim < nDim; jDim++) {
-          Temp[iDim] += AdjHessian[iDim][jDim]*IndepTerm[jDim]/Determinant;
+          Temp[iDim] += AdjHessian[iDim][jDim] * IndepTerm[jDim] / Determinant;
         }
       }
       for (iDim = 0; iDim < nDim; iDim++) {
@@ -918,18 +965,17 @@ su2double *CFreeFormDefBox::GetParametricCoord_Iterative(unsigned long iPoint, s
     /*--- Update with Successive over-relaxation ---*/
 
     for (iDim = 0; iDim < nDim; iDim++) {
-      ParamCoord[iDim] = (1.0-SOR_Factor)*ParamCoord[iDim] + SOR_Factor*(ParamCoord[iDim] + IndepTerm[iDim]);
+      ParamCoord[iDim] = (1.0 - SOR_Factor) * ParamCoord[iDim] + SOR_Factor * (ParamCoord[iDim] + IndepTerm[iDim]);
     }
 
     /*--- If the gradient is small, we have converged ---*/
 
-    if ((fabs(IndepTerm[0]) < tol) && (fabs(IndepTerm[1]) < tol) && (fabs(IndepTerm[2]) < tol))  break;
+    if ((fabs(IndepTerm[0]) < tol) && (fabs(IndepTerm[1]) < tol) && (fabs(IndepTerm[2]) < tol)) break;
 
     /*--- Compute the norm of the error ---*/
 
     NormError = 0.0;
-    for (iDim = 0; iDim < nDim; iDim++)
-      NormError += IndepTerm[iDim]*IndepTerm[iDim];
+    for (iDim = 0; iDim < nDim; iDim++) NormError += IndepTerm[iDim] * IndepTerm[iDim];
     NormError = sqrt(NormError);
 
     MinNormError = min(NormError, MinNormError);
@@ -937,54 +983,47 @@ su2double *CFreeFormDefBox::GetParametricCoord_Iterative(unsigned long iPoint, s
     /*--- If we have no convergence with Random_Trials iterations probably we are in a local minima. ---*/
 
     if (((iter % it_max) == 0) && (iter != 0)) {
-
       RandonCounter++;
       if (RandonCounter == Random_Trials) {
-        cout << endl << "Unknown point: "<< iPoint <<" (" << xyz[0] <<", "<< xyz[1] <<", "<< xyz[2] <<"). Min Error: "<< MinNormError <<". Iter: "<< iter <<"."<< endl;
-      }
-      else {
+        cout << endl
+             << "Unknown point: " << iPoint << " (" << xyz[0] << ", " << xyz[1] << ", " << xyz[2]
+             << "). Min Error: " << MinNormError << ". Iter: " << iter << "." << endl;
+      } else {
         SOR_Factor = 0.1;
-        for (iDim = 0; iDim < nDim; iDim++)
-          ParamCoord[iDim] = su2double(rand())/su2double(RAND_MAX);
+        for (iDim = 0; iDim < nDim; iDim++) ParamCoord[iDim] = su2double(rand()) / su2double(RAND_MAX);
       }
-
     }
 
     /* --- Splines are not defined outside of [0,1]. So if the parametric coords are outside of
      *  [0,1] the step was too big and we have to use a smaller relaxation factor. ---*/
 
-    if ((config->GetFFD_Blending() == BSPLINE_UNIFORM)     &&
-        (((ParamCoord[0] < 0.0) || (ParamCoord[0] > 1.0))  ||
-         ((ParamCoord[1] < 0.0) || (ParamCoord[1] > 1.0))  ||
+    if ((config->GetFFD_Blending() == BSPLINE_UNIFORM) &&
+        (((ParamCoord[0] < 0.0) || (ParamCoord[0] > 1.0)) || ((ParamCoord[1] < 0.0) || (ParamCoord[1] > 1.0)) ||
          ((ParamCoord[2] < 0.0) || (ParamCoord[2] > 1.0)))) {
-
-      for (iDim = 0; iDim < nDim; iDim++){
+      for (iDim = 0; iDim < nDim; iDim++) {
         ParamCoord[iDim] = ParamCoordGuess[iDim];
       }
-      SOR_Factor = 0.9*SOR_Factor;
+      SOR_Factor = 0.9 * SOR_Factor;
     }
-
   }
 
-  for (iDim = 0; iDim < nDim; iDim++)
-    delete [] Hessian[iDim];
-  delete [] Hessian;
-  delete [] IndepTerm;
+  for (iDim = 0; iDim < nDim; iDim++) delete[] Hessian[iDim];
+  delete[] Hessian;
+  delete[] IndepTerm;
 
   /*--- The code has hit the max number of iterations ---*/
 
-  if (iter == (unsigned long)it_max*Random_Trials) {
-    cout << "Unknown point: (" << xyz[0] <<", "<< xyz[1] <<", "<< xyz[2] <<"). Increase the value of FFD_ITERATIONS." << endl;
+  if (iter == (unsigned long)it_max * Random_Trials) {
+    cout << "Unknown point: (" << xyz[0] << ", " << xyz[1] << ", " << xyz[2]
+         << "). Increase the value of FFD_ITERATIONS." << endl;
   }
 
   /*--- Real Solution is now ParamCoord; Return it ---*/
 
   return ParamCoord;
-
 }
 
-bool CFreeFormDefBox::GetPointFFD(CGeometry *geometry, CConfig *config, unsigned long iPoint) const {
-
+bool CFreeFormDefBox::GetPointFFD(CGeometry* geometry, CConfig* config, unsigned long iPoint) const {
   bool Inside = true;
   bool cylindrical = (config->GetFFD_CoordSystem() == CYLINDRICAL);
   bool spherical = (config->GetFFD_CoordSystem() == SPHERICAL);
@@ -992,74 +1031,75 @@ bool CFreeFormDefBox::GetPointFFD(CGeometry *geometry, CConfig *config, unsigned
 
   /*--- indices of the FFD box. Note that the front face is labelled 0,1,2,3 and the back face is 4,5,6,7 ---*/
 
-  unsigned short Index[6][5] = {
-  {0,1,2,3,0},  // front side
-  {1,5,6,2,1},  // right side
-  {2,6,7,3,2},  // top side
-  {3,7,4,0,3},  // left side
-  {4,5,1,0,4},  // bottom side
-  {4,7,6,5,4}}; // back side
+  unsigned short Index[6][5] = {{0, 1, 2, 3, 0},   // front side
+                                {1, 5, 6, 2, 1},   // right side
+                                {2, 6, 7, 3, 2},   // top side
+                                {3, 7, 4, 0, 3},   // left side
+                                {4, 5, 1, 0, 4},   // bottom side
+                                {4, 7, 6, 5, 4}};  // back side
 
   /*--- The current approach is to subdivide each of the 6 faces of the hexahedral FFD box into 4 triangles
       by defining a supporting middle point. This allows nonplanar FFD boxes.
-      Note that the definition of the FFD box is as follows: the FFD box is a 6-sided die and we are looking at the side "1".
-      The opposite side is side "6".
-      If we are looking at side "1", we define the nodes counterclockwise.
-      If we are looking at side "6", we define the face clockwise  ---*/
+      Note that the definition of the FFD box is as follows: the FFD box is a 6-sided die and we are looking at the side
+     "1". The opposite side is side "6". If we are looking at side "1", we define the nodes counterclockwise. If we are
+     looking at side "6", we define the face clockwise  ---*/
 
   unsigned short nDim = geometry->GetnDim();
 
   su2double Coord[3] = {0.0, 0.0, 0.0};
-  for (unsigned short iDim = 0; iDim < nDim; iDim++)
-    Coord[iDim] = geometry->nodes->GetCoord(iPoint, iDim);
+  for (unsigned short iDim = 0; iDim < nDim; iDim++) Coord[iDim] = geometry->nodes->GetCoord(iPoint, iDim);
 
   su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
 
   if (cylindrical) {
+    X_0 = config->GetFFD_Axis(0);
+    Y_0 = config->GetFFD_Axis(1);
+    Z_0 = config->GetFFD_Axis(2);
 
-    X_0 = config->GetFFD_Axis(0); Y_0 = config->GetFFD_Axis(1);  Z_0 = config->GetFFD_Axis(2);
-
-    Xbar =  Coord[0] - X_0; Ybar =  Coord[1] - Y_0; Zbar =  Coord[2] - Z_0;
+    Xbar = Coord[0] - X_0;
+    Ybar = Coord[1] - Y_0;
+    Zbar = Coord[2] - Z_0;
 
-    Coord[0] = sqrt(Ybar*Ybar + Zbar*Zbar);
-    Coord[1] = atan2(Zbar, Ybar); if (Coord[1] > PI_NUMBER/2.0) Coord[1] -= 2.0*PI_NUMBER;
+    Coord[0] = sqrt(Ybar * Ybar + Zbar * Zbar);
+    Coord[1] = atan2(Zbar, Ybar);
+    if (Coord[1] > PI_NUMBER / 2.0) Coord[1] -= 2.0 * PI_NUMBER;
     Coord[2] = Xbar;
 
   }
 
   else if (spherical || polar) {
-
-    X_0 = config->GetFFD_Axis(0); Y_0 = config->GetFFD_Axis(1);  Z_0 = config->GetFFD_Axis(2);
-
-    Xbar =  Coord[0] - X_0; Ybar =  Coord[1] - Y_0; Zbar =  Coord[2] - Z_0;
-
-    Coord[0] = sqrt(Xbar*Xbar + Ybar*Ybar + Zbar*Zbar);
-    Coord[1] = atan2(Zbar, Ybar);  if (Coord[1] > PI_NUMBER/2.0) Coord[1] -= 2.0*PI_NUMBER;
-    Coord[2] = acos(Xbar/Coord[0]);
-
+    X_0 = config->GetFFD_Axis(0);
+    Y_0 = config->GetFFD_Axis(1);
+    Z_0 = config->GetFFD_Axis(2);
+
+    Xbar = Coord[0] - X_0;
+    Ybar = Coord[1] - Y_0;
+    Zbar = Coord[2] - Z_0;
+
+    Coord[0] = sqrt(Xbar * Xbar + Ybar * Ybar + Zbar * Zbar);
+    Coord[1] = atan2(Zbar, Ybar);
+    if (Coord[1] > PI_NUMBER / 2.0) Coord[1] -= 2.0 * PI_NUMBER;
+    Coord[2] = acos(Xbar / Coord[0]);
   }
 
   /*--- loop over the faces of the FFD box  ---*/
 
   for (unsigned short iVar = 0; iVar < 6; iVar++) {
-
     su2double P[3] = {0.0, 0.0, 0.0};
 
     /*--- every face needs an interpolated middle point for the triangles ---*/
 
-    for (int p = 0; p < 4; p++){
-      P[0] += 0.25*Coord_Corner_Points[Index[iVar][p]][0];
-      P[1] += 0.25*Coord_Corner_Points[Index[iVar][p]][1];
-      P[2] += 0.25*Coord_Corner_Points[Index[iVar][p]][2];
+    for (int p = 0; p < 4; p++) {
+      P[0] += 0.25 * Coord_Corner_Points[Index[iVar][p]][0];
+      P[1] += 0.25 * Coord_Corner_Points[Index[iVar][p]][1];
+      P[2] += 0.25 * Coord_Corner_Points[Index[iVar][p]][2];
     }
 
     /*--- loop over the 4 triangles making up the FFD box. The sign is equal for all distances ---*/
 
     for (unsigned short jVar = 0; jVar < 4; jVar++) {
-      su2double Distance_Point = geometry->Point2Plane_Distance(Coord,
-                                                                Coord_Corner_Points[Index[iVar][jVar]],
-                                                                Coord_Corner_Points[Index[iVar][jVar+1]],
-                                                                P);
+      su2double Distance_Point = geometry->Point2Plane_Distance(Coord, Coord_Corner_Points[Index[iVar][jVar]],
+                                                                Coord_Corner_Points[Index[iVar][jVar + 1]], P);
       if (Distance_Point < 0) {
         Inside = false;
         return Inside;
@@ -1068,104 +1108,97 @@ bool CFreeFormDefBox::GetPointFFD(CGeometry *geometry, CConfig *config, unsigned
   }
 
   return Inside;
-
 }
 
-
-su2double CFreeFormDefBox::GetDerivative1(su2double *uvw, unsigned short val_diff, unsigned short *ijk, unsigned short *lmn) const {
-
+su2double CFreeFormDefBox::GetDerivative1(su2double* uvw, unsigned short val_diff, unsigned short* ijk,
+                                          unsigned short* lmn) const {
   unsigned short iDim;
   su2double value = 0.0;
 
   value = BlendingFunction[val_diff]->GetDerivative(ijk[val_diff], uvw[val_diff], 1);
   for (iDim = 0; iDim < nDim; iDim++)
-    if (iDim != val_diff)
-      value *= BlendingFunction[iDim]->GetBasis(ijk[iDim], uvw[iDim]);
+    if (iDim != val_diff) value *= BlendingFunction[iDim]->GetBasis(ijk[iDim], uvw[iDim]);
 
   return value;
-
 }
 
-su2double CFreeFormDefBox::GetDerivative2 (su2double *uvw, unsigned short dim, const su2double *xyz, const unsigned short *lmn) const {
-
+su2double CFreeFormDefBox::GetDerivative2(su2double* uvw, unsigned short dim, const su2double* xyz,
+                                          const unsigned short* lmn) const {
   unsigned short iDegree, jDegree, kDegree;
   su2double value = 0.0;
 
   for (iDegree = 0; iDegree <= lmn[0]; iDegree++)
     for (jDegree = 0; jDegree <= lmn[1]; jDegree++)
       for (kDegree = 0; kDegree <= lmn[2]; kDegree++) {
-        value += Coord_Control_Points[iDegree][jDegree][kDegree][dim]
-        * BlendingFunction[0]->GetBasis(iDegree, uvw[0])
-        * BlendingFunction[1]->GetBasis(jDegree, uvw[1])
-        * BlendingFunction[2]->GetBasis(kDegree, uvw[2]);
+        value += Coord_Control_Points[iDegree][jDegree][kDegree][dim] * BlendingFunction[0]->GetBasis(iDegree, uvw[0]) *
+                 BlendingFunction[1]->GetBasis(jDegree, uvw[1]) * BlendingFunction[2]->GetBasis(kDegree, uvw[2]);
       }
 
-  return 2.0*(value - xyz[dim]);
+  return 2.0 * (value - xyz[dim]);
 }
 
-su2double CFreeFormDefBox::GetDerivative3(su2double *uvw, unsigned short dim, unsigned short diff_this, unsigned short *lmn) {
-
+su2double CFreeFormDefBox::GetDerivative3(su2double* uvw, unsigned short dim, unsigned short diff_this,
+                                          unsigned short* lmn) {
   unsigned short iDegree, jDegree, kDegree, iDim;
   su2double value = 0;
 
-  unsigned short *ijk = new unsigned short[nDim];
+  unsigned short* ijk = new unsigned short[nDim];
 
   for (iDim = 0; iDim < nDim; iDim++) ijk[iDim] = 0;
 
   for (iDegree = 0; iDegree <= lmn[0]; iDegree++)
     for (jDegree = 0; jDegree <= lmn[1]; jDegree++)
       for (kDegree = 0; kDegree <= lmn[2]; kDegree++) {
-        ijk[0] = iDegree; ijk[1] = jDegree; ijk[2] = kDegree;
-        value += Coord_Control_Points[iDegree][jDegree][kDegree][dim] *
-        GetDerivative1(uvw, diff_this, ijk, lmn);
+        ijk[0] = iDegree;
+        ijk[1] = jDegree;
+        ijk[2] = kDegree;
+        value += Coord_Control_Points[iDegree][jDegree][kDegree][dim] * GetDerivative1(uvw, diff_this, ijk, lmn);
       }
 
-  delete [] ijk;
+  delete[] ijk;
 
   return value;
 }
 
-su2double CFreeFormDefBox::GetDerivative4(su2double *uvw, unsigned short val_diff, unsigned short val_diff2,
-                                       unsigned short *ijk, unsigned short *lmn) const {
+su2double CFreeFormDefBox::GetDerivative4(su2double* uvw, unsigned short val_diff, unsigned short val_diff2,
+                                          unsigned short* ijk, unsigned short* lmn) const {
   unsigned short iDim;
   su2double value = 0.0;
 
   if (val_diff == val_diff2) {
     value = BlendingFunction[val_diff]->GetDerivative(ijk[val_diff], uvw[val_diff], 2);
     for (iDim = 0; iDim < nDim; iDim++)
-      if (iDim != val_diff)
-        value *= BlendingFunction[iDim]->GetBasis(ijk[iDim], uvw[iDim]);
-  }
-  else {
-    value = BlendingFunction[val_diff]->GetDerivative(ijk[val_diff],  uvw[val_diff],1) *
-    BlendingFunction[val_diff2]->GetDerivative(ijk[val_diff2], uvw[val_diff2], 1);
+      if (iDim != val_diff) value *= BlendingFunction[iDim]->GetBasis(ijk[iDim], uvw[iDim]);
+  } else {
+    value = BlendingFunction[val_diff]->GetDerivative(ijk[val_diff], uvw[val_diff], 1) *
+            BlendingFunction[val_diff2]->GetDerivative(ijk[val_diff2], uvw[val_diff2], 1);
     for (iDim = 0; iDim < nDim; iDim++)
-      if ((iDim != val_diff) && (iDim != val_diff2))
-        value *= BlendingFunction[iDim]->GetBasis(ijk[iDim], uvw[iDim]);
+      if ((iDim != val_diff) && (iDim != val_diff2)) value *= BlendingFunction[iDim]->GetBasis(ijk[iDim], uvw[iDim]);
   }
 
   return value;
 }
 
-su2double CFreeFormDefBox::GetDerivative5(su2double *uvw, unsigned short dim, unsigned short diff_this, unsigned short diff_this_also,
-                                      unsigned short *lmn) {
-
+su2double CFreeFormDefBox::GetDerivative5(su2double* uvw, unsigned short dim, unsigned short diff_this,
+                                          unsigned short diff_this_also, unsigned short* lmn) {
   unsigned short iDegree, jDegree, kDegree, iDim;
   su2double value = 0.0;
 
-  unsigned short *ijk = new unsigned short[nDim];
+  unsigned short* ijk = new unsigned short[nDim];
 
   for (iDim = 0; iDim < nDim; iDim++) ijk[iDim] = 0;
 
   for (iDegree = 0; iDegree <= lmn[0]; iDegree++)
     for (jDegree = 0; jDegree <= lmn[1]; jDegree++)
       for (kDegree = 0; kDegree <= lmn[2]; kDegree++) {
-        ijk[0] = iDegree; ijk[1] = jDegree; ijk[2] = kDegree;
+        ijk[0] = iDegree;
+        ijk[1] = jDegree;
+        ijk[2] = kDegree;
         value += Coord_Control_Points[iDegree][jDegree][kDegree][dim] *
-        GetDerivative4(uvw, diff_this, diff_this_also, ijk, lmn);
+                 GetDerivative4(uvw, diff_this, diff_this_also, ijk, lmn);
       }
 
-  delete [] ijk;
+  delete[] ijk;
 
   return value;
 }
diff --git a/Common/src/grid_movement/CGridMovement.cpp b/Common/src/grid_movement/CGridMovement.cpp
index 3ead32ae339..656583439b4 100644
--- a/Common/src/grid_movement/CGridMovement.cpp
+++ b/Common/src/grid_movement/CGridMovement.cpp
@@ -27,6 +27,6 @@
 
 #include "../../include/grid_movement/CGridMovement.hpp"
 
-CGridMovement::CGridMovement(void) { }
+CGridMovement::CGridMovement(void) {}
 
-CGridMovement::~CGridMovement(void) { }
+CGridMovement::~CGridMovement(void) {}
diff --git a/Common/src/grid_movement/CSurfaceMovement.cpp b/Common/src/grid_movement/CSurfaceMovement.cpp
index f4e7844ce32..0834e05c426 100644
--- a/Common/src/grid_movement/CSurfaceMovement.cpp
+++ b/Common/src/grid_movement/CSurfaceMovement.cpp
@@ -29,7 +29,6 @@
 #include "../../include/toolboxes/C1DInterpolation.hpp"
 
 CSurfaceMovement::CSurfaceMovement(void) : CGridMovement() {
-
   size = SU2_MPI::GetSize();
   rank = SU2_MPI::GetRank();
 
@@ -40,18 +39,17 @@ CSurfaceMovement::CSurfaceMovement(void) : CGridMovement() {
 
 CSurfaceMovement::~CSurfaceMovement(void) {}
 
-vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *geometry, CConfig *config) {
-
+vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry* geometry, CConfig* config) {
   unsigned short iFFDBox, iDV, iLevel, iChild, iParent, jFFDBox, iMarker;
-  unsigned short Degree_Unitary [] = {1,1,1}, BSpline_Unitary [] = {2,2,2};
+  unsigned short Degree_Unitary[] = {1, 1, 1}, BSpline_Unitary[] = {2, 2, 2};
   su2double MaxDiff, Current_Scale, Ratio, New_Scale;
   string FFDBoxTag;
   bool allmoving;
 
   const bool cylindrical = (config->GetFFD_CoordSystem() == CYLINDRICAL);
-  const bool spherical   = (config->GetFFD_CoordSystem() == SPHERICAL);
-  const bool polar       = (config->GetFFD_CoordSystem() == POLAR);
-  const bool cartesian   = (config->GetFFD_CoordSystem() == CARTESIAN);
+  const bool spherical = (config->GetFFD_CoordSystem() == SPHERICAL);
+  const bool polar = (config->GetFFD_CoordSystem() == POLAR);
+  const bool cartesian = (config->GetFFD_CoordSystem() == CARTESIAN);
   const su2double BoundLimit = config->GetOpt_LineSearch_Bound();
 
   vector<vector<su2double> > totaldeformation;
@@ -59,7 +57,6 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
   /*--- Setting the Free Form Deformation ---*/
 
   if (config->GetDesign_Variable(0) == FFD_SETTING) {
-
     /*--- Definition of the FFD deformation class ---*/
 
     FFDBox = new CFreeFormDefBox*[MAX_NUMBER_FFD];
@@ -71,15 +68,13 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
     /*--- If there is a FFDBox in the input file ---*/
 
     if (nFFDBox != 0) {
-
       /*--- if polar coordinates, trnasform the corner to polar ---*/
 
       if (cylindrical) {
         for (iFFDBox = 0; iFFDBox < GetnFFDBox(); iFFDBox++) {
           FFDBox[iFFDBox]->SetCart2Cyl_CornerPoints(config);
         }
-      }
-      else if (spherical || polar) {
+      } else if (spherical || polar) {
         for (iFFDBox = 0; iFFDBox < GetnFFDBox(); iFFDBox++) {
           FFDBox[iFFDBox]->SetCart2Sphe_CornerPoints(config);
         }
@@ -88,10 +83,14 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
       /*--- If the FFDBox was not defined in the input file ---*/
 
       if ((rank == MASTER_NODE) && (GetnFFDBox() != 0)) {
-        if (cartesian) cout << endl <<"----------------- FFD technique (cartesian -> parametric) ---------------" << endl;
-        else if (cylindrical) cout << endl <<"----------------- FFD technique (cylinder -> parametric) ---------------" << endl;
-        else if (spherical) cout << endl <<"----------------- FFD technique (spherical -> parametric) ---------------" << endl;
-        else if (polar) cout << endl <<"----------------- FFD technique (polar -> parametric) ---------------" << endl;
+        if (cartesian)
+          cout << endl << "----------------- FFD technique (cartesian -> parametric) ---------------" << endl;
+        else if (cylindrical)
+          cout << endl << "----------------- FFD technique (cylinder -> parametric) ---------------" << endl;
+        else if (spherical)
+          cout << endl << "----------------- FFD technique (spherical -> parametric) ---------------" << endl;
+        else if (polar)
+          cout << endl << "----------------- FFD technique (polar -> parametric) ---------------" << endl;
       }
 
       /*--- Create a unitary FFDBox as baseline for other FFDBoxes shapes ---*/
@@ -104,7 +103,6 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
       FFDBox_unitary.SetControlPoints_Parallelepiped();
 
       for (iFFDBox = 0; iFFDBox < GetnFFDBox(); iFFDBox++) {
-
         /*--- Compute the support control points for the final FFD using the unitary box ---*/
 
         FFDBox_unitary.SetSupportCP(FFDBox[iFFDBox]);
@@ -118,14 +116,12 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
 
         SetParametricCoord(geometry, config, FFDBox[iFFDBox], iFFDBox);
 
-
         /*--- If polar coordinates, transform the corners and control points to cartesians ---*/
 
         if (cylindrical) {
           FFDBox[iFFDBox]->SetCyl2Cart_CornerPoints(config);
           FFDBox[iFFDBox]->SetCyl2Cart_ControlPoints(config);
-        }
-        else if (spherical || polar) {
+        } else if (spherical || polar) {
           FFDBox[iFFDBox]->SetSphe2Cart_CornerPoints(config);
           FFDBox[iFFDBox]->SetSphe2Cart_ControlPoints(config);
         }
@@ -133,7 +129,7 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
       /*--- Output original FFD FFDBox ---*/
 
       if (rank == MASTER_NODE) {
-        for (unsigned short iFile = 0; iFile < config->GetnVolumeOutputFiles(); iFile++){
+        for (unsigned short iFile = 0; iFile < config->GetnVolumeOutputFiles(); iFile++) {
           auto FileFormat = config->GetVolumeOutputFiles();
           if (isParaview(FileFormat[iFile])) {
             cout << "Writing a Paraview file of the FFD boxes." << endl;
@@ -145,8 +141,7 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
             for (iFFDBox = 0; iFFDBox < GetnFFDBox(); iFFDBox++) {
               FFDBox[iFFDBox]->SetTecplot(geometry, iFFDBox, true);
             }
-          }
-          else if (FileFormat[iFile] == OUTPUT_TYPE::CGNS)  {
+          } else if (FileFormat[iFile] == OUTPUT_TYPE::CGNS) {
             cout << "Writing a CGNS file of the FFD boxes." << endl;
             for (iFFDBox = 0; iFFDBox < GetnFFDBox(); iFFDBox++) {
               FFDBox[iFFDBox]->SetCGNS(geometry, iFFDBox, true);
@@ -159,25 +154,17 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
     else {
       SU2_MPI::Error("There are no FFD boxes in the mesh file!!", CURRENT_FUNCTION);
     }
-
   }
 
   /*--- Free Form deformation based ---*/
 
-  if ((config->GetDesign_Variable(0) == FFD_CONTROL_POINT_2D) ||
-      (config->GetDesign_Variable(0) == FFD_CAMBER_2D) ||
-      (config->GetDesign_Variable(0) == FFD_THICKNESS_2D) ||
-      (config->GetDesign_Variable(0) == FFD_TWIST_2D) ||
-      (config->GetDesign_Variable(0) == FFD_CONTROL_POINT) ||
-      (config->GetDesign_Variable(0) == FFD_NACELLE) ||
-      (config->GetDesign_Variable(0) == FFD_GULL) ||
-      (config->GetDesign_Variable(0) == FFD_TWIST) ||
-      (config->GetDesign_Variable(0) == FFD_ROTATION) ||
-      (config->GetDesign_Variable(0) == FFD_CONTROL_SURFACE) ||
-      (config->GetDesign_Variable(0) == FFD_CAMBER) ||
-      (config->GetDesign_Variable(0) == FFD_THICKNESS) ||
+  if ((config->GetDesign_Variable(0) == FFD_CONTROL_POINT_2D) || (config->GetDesign_Variable(0) == FFD_CAMBER_2D) ||
+      (config->GetDesign_Variable(0) == FFD_THICKNESS_2D) || (config->GetDesign_Variable(0) == FFD_TWIST_2D) ||
+      (config->GetDesign_Variable(0) == FFD_CONTROL_POINT) || (config->GetDesign_Variable(0) == FFD_NACELLE) ||
+      (config->GetDesign_Variable(0) == FFD_GULL) || (config->GetDesign_Variable(0) == FFD_TWIST) ||
+      (config->GetDesign_Variable(0) == FFD_ROTATION) || (config->GetDesign_Variable(0) == FFD_CONTROL_SURFACE) ||
+      (config->GetDesign_Variable(0) == FFD_CAMBER) || (config->GetDesign_Variable(0) == FFD_THICKNESS) ||
       (config->GetDesign_Variable(0) == FFD_ANGLE_OF_ATTACK)) {
-
     /*--- Definition of the FFD deformation class ---*/
 
     FFDBox = new CFreeFormDefBox*[MAX_NUMBER_FFD];
@@ -189,20 +176,22 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
     /*--- If there is a FFDBox in the input file ---*/
 
     if (nFFDBox != 0) {
-
       /*--- If the FFDBox was not defined in the input file ---*/
 
       if (!GetFFDBoxDefinition()) {
-        SU2_MPI::Error(string("There is not FFD box definition in the mesh file,\n") +
-                       string("run DV_KIND=FFD_SETTING first !!"), CURRENT_FUNCTION);
+        SU2_MPI::Error(
+            string("There is not FFD box definition in the mesh file,\n") + string("run DV_KIND=FFD_SETTING first !!"),
+            CURRENT_FUNCTION);
       }
 
       /* --- Check if the FFD boxes referenced in the design variable definition can be found --- */
 
       for (iDV = 0; iDV < config->GetnDV(); iDV++) {
         if (!CheckFFDBoxDefinition(config, iDV)) {
-          SU2_MPI::Error(string("There is no FFD box with tag \"") + config->GetFFDTag(iDV) + string("\" defined in the mesh file.\n") +
-                         string("Check the definition of the design variables and/or the FFD settings !!"), CURRENT_FUNCTION);
+          SU2_MPI::Error(string("There is no FFD box with tag \"") + config->GetFFDTag(iDV) +
+                             string("\" defined in the mesh file.\n") +
+                             string("Check the definition of the design variables and/or the FFD settings !!"),
+                         CURRENT_FUNCTION);
         }
       }
 
@@ -210,14 +199,14 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
 
       if (config->GetnMarker_DV() == 0) {
         SU2_MPI::Error(string("No markers are specified in DV_MARKER, so no deformation will occur.\n") +
-                       string("List markers to be deformed in DV_MARKER."), CURRENT_FUNCTION);
+                           string("List markers to be deformed in DV_MARKER."),
+                       CURRENT_FUNCTION);
       }
 
       /*--- Output original FFD FFDBox ---*/
 
       if ((rank == MASTER_NODE) && (config->GetKind_SU2() != SU2_COMPONENT::SU2_DOT)) {
-
-        for (unsigned short iFile = 0; iFile < config->GetnVolumeOutputFiles(); iFile++){
+        for (unsigned short iFile = 0; iFile < config->GetnVolumeOutputFiles(); iFile++) {
           auto FileFormat = config->GetVolumeOutputFiles();
 
           if (isParaview(FileFormat[iFile])) {
@@ -230,8 +219,7 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
             for (iFFDBox = 0; iFFDBox < GetnFFDBox(); iFFDBox++) {
               FFDBox[iFFDBox]->SetTecplot(geometry, iFFDBox, true);
             }
-          }
-          else if (FileFormat[iFile] == OUTPUT_TYPE::CGNS)  {
+          } else if (FileFormat[iFile] == OUTPUT_TYPE::CGNS) {
             cout << "Writing a CGNS file of the FFD boxes." << endl;
             for (iFFDBox = 0; iFFDBox < GetnFFDBox(); iFFDBox++) {
               FFDBox[iFFDBox]->SetCGNS(geometry, iFFDBox, true);
@@ -247,8 +235,7 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
           FFDBox[iFFDBox]->SetCart2Cyl_CornerPoints(config);
           FFDBox[iFFDBox]->SetCart2Cyl_ControlPoints(config);
         }
-      }
-      else if (spherical || polar) {
+      } else if (spherical || polar) {
         for (iFFDBox = 0; iFFDBox < GetnFFDBox(); iFFDBox++) {
           FFDBox[iFFDBox]->SetCart2Sphe_CornerPoints(config);
           FFDBox[iFFDBox]->SetCart2Sphe_ControlPoints(config);
@@ -258,20 +245,17 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
       /*--- Apply the deformation to the orifinal FFD box ---*/
 
       if ((rank == MASTER_NODE) && (GetnFFDBox() != 0))
-        cout << endl <<"----------------- FFD technique (parametric -> cartesian) ---------------" << endl;
+        cout << endl << "----------------- FFD technique (parametric -> cartesian) ---------------" << endl;
 
       /*--- Loop over all the FFD boxes levels ---*/
 
       for (iLevel = 0; iLevel < GetnLevel(); iLevel++) {
-
         /*--- Loop over all FFD FFDBoxes ---*/
 
         for (iFFDBox = 0; iFFDBox < GetnFFDBox(); iFFDBox++) {
-
           /*--- Check the level of the FFD box ---*/
 
           if (FFDBox[iFFDBox]->GetLevel() == iLevel) {
-
             /*--- Check the dimension of the FFD compared with the design variables ---*/
 
             if (rank == MASTER_NODE) cout << "Checking FFD box dimension." << endl;
@@ -305,12 +289,12 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
             MaxDiff = SetCartesianCoord(geometry, config, FFDBox[iFFDBox], iFFDBox, false);
 
             if ((MaxDiff > BoundLimit) && (config->GetKind_SU2() == SU2_COMPONENT::SU2_DEF)) {
-
-              if (rank == MASTER_NODE) cout << "Out-of-bounds, re-adjusting scale factor to safisfy line search limit." << endl;
+              if (rank == MASTER_NODE)
+                cout << "Out-of-bounds, re-adjusting scale factor to safisfy line search limit." << endl;
 
               Current_Scale = config->GetOpt_RelaxFactor();
-              Ratio = (BoundLimit/MaxDiff);
-              New_Scale = Current_Scale *(Ratio-1.0);
+              Ratio = (BoundLimit / MaxDiff);
+              New_Scale = Current_Scale * (Ratio - 1.0);
               config->SetOpt_RelaxFactor(New_Scale);
 
               /*--- Apply the design variables to the control point position ---*/
@@ -319,12 +303,10 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
               /*--- Recompute cartesian coordinates using the new control point location ---*/
 
               MaxDiff = SetCartesianCoord(geometry, config, FFDBox[iFFDBox], iFFDBox, false);
-
             }
 
             /*--- Set total deformation values in config ---*/
             if (config->GetKind_SU2() == SU2_COMPONENT::SU2_DEF) {
-
               totaldeformation.resize(config->GetnDV());
               for (iDV = 0; iDV < config->GetnDV(); iDV++) {
                 totaldeformation[iDV].resize(config->GetnDV_Value(iDV));
@@ -352,7 +334,6 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
               /*--- If enabled: start recursive procedure to decrease deformation magnitude
               to remove self-intersections in FFD box ---*/
               if (nNegativeDeterminants > 0) {
-
                 if (rank == MASTER_NODE) {
                   cout << "Self-intersections within FFD box present. ";
                   cout << "Performing iterative deformation reduction procedure." << endl;
@@ -362,8 +343,8 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
                 for (iDV = 0; iDV < config->GetnDV(); iDV++) {
                   for (auto iDV_Value = 0u; iDV_Value < config->GetnDV_Value(iDV); iDV_Value++) {
                     auto dv_value = config->GetDV_Value(iDV, iDV_Value);
-                    config->SetDV_Value(iDV, iDV_Value, -dv_value/2);
-                    totaldeformation[iDV][iDV_Value] -= dv_value/2;
+                    config->SetDV_Value(iDV, iDV_Value, -dv_value / 2);
+                    totaldeformation[iDV][iDV_Value] -= dv_value / 2;
                   }
                 }
 
@@ -374,18 +355,16 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
                 /*--- Recursively check for self-intersections. ---*/
                 unsigned short FFD_IntPrev_Iter, FFD_IntPrev_Depth = 0;
 
-                for (FFD_IntPrev_Iter = 1; FFD_IntPrev_Iter <= FFD_IntPrev_MaxIter; FFD_IntPrev_Iter++){
-
+                for (FFD_IntPrev_Iter = 1; FFD_IntPrev_Iter <= FFD_IntPrev_MaxIter; FFD_IntPrev_Iter++) {
                   if (rank == MASTER_NODE) cout << "Checking FFD box intersections with the solid surfaces." << endl;
-                    CheckFFDIntersections(geometry, config, FFDBox[iFFDBox], iFFDBox);
+                  CheckFFDIntersections(geometry, config, FFDBox[iFFDBox], iFFDBox);
 
                   /*--- Compute the parametric coordinates of the child box
                   control points (using the parent FFDBox)  ---*/
                   for (iChild = 0; iChild < FFDBox[iFFDBox]->GetnChildFFDBox(); iChild++) {
                     FFDBoxTag = FFDBox[iFFDBox]->GetChildFFDBoxTag(iChild);
                     for (jFFDBox = 0; jFFDBox < GetnFFDBox(); jFFDBox++)
-                      if (FFDBoxTag == FFDBox[jFFDBox]->GetTag())
-                        break;
+                      if (FFDBoxTag == FFDBox[jFFDBox]->GetTag()) break;
                     SetParametricCoordCP(geometry, config, FFDBox[iFFDBox], FFDBox[jFFDBox]);
                   }
 
@@ -405,13 +384,14 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
                   if (rank == MASTER_NODE) {
                     cout << "Amount of points with negative Jacobian determinant for iteration ";
                     cout << FFD_IntPrev_Iter << ": " << nNegativeDeterminants << endl;
-                    cout << "Remaining amount of original deformation: " << DeformationFactor*100.0 << " percent." << endl;
+                    cout << "Remaining amount of original deformation: " << DeformationFactor * 100.0 << " percent."
+                         << endl;
                   }
 
                   /*--- Recursively change deformation magnitude.
                   Increase if there are no points with negative determinants, decrease otherwise. ---*/
-                  if (nNegativeDeterminants == 0){
-                    DeformationDifference = abs(DeformationDifference/2.0);
+                  if (nNegativeDeterminants == 0) {
+                    DeformationDifference = abs(DeformationDifference / 2.0);
 
                     /*--- Update recursion depth if there are no points with negative determinant.
                     Quit if maximum depth is reached. ---*/
@@ -421,12 +401,12 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
                       if (rank == MASTER_NODE) {
                         cout << "Maximum recursion depth reached." << endl;
                         cout << "Remaining amount of original deformation: " << endl;
-                        cout << DeformationFactor*100.0 << " percent." << endl;
+                        cout << DeformationFactor * 100.0 << " percent." << endl;
                       }
                       break;
                     }
                   } else {
-                    DeformationDifference = -abs(DeformationDifference/2.0);
+                    DeformationDifference = -abs(DeformationDifference / 2.0);
                   }
 
                   if (FFD_IntPrev_Iter < FFD_IntPrev_MaxIter) {
@@ -438,23 +418,22 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
                   if (FFD_IntPrev_Iter < FFD_IntPrev_MaxIter) {
                     su2double sign = -1.0;
                     if ((nNegativeDeterminants_previous > 0 && nNegativeDeterminants > 0) ||
-                        (nNegativeDeterminants_previous == 0 && nNegativeDeterminants == 0)){
+                        (nNegativeDeterminants_previous == 0 && nNegativeDeterminants == 0)) {
                       sign = 1.0;
                     }
                     for (iDV = 0; iDV < config->GetnDV(); iDV++) {
                       for (auto iDV_Value = 0u; iDV_Value < config->GetnDV_Value(iDV); iDV_Value++) {
                         auto dv_value = sign * config->GetDV_Value(iDV, iDV_Value);
-                        config->SetDV_Value(iDV, iDV_Value, dv_value/2.0);
-                        totaldeformation[iDV][iDV_Value] += dv_value/2.0;
+                        config->SetDV_Value(iDV, iDV_Value, dv_value / 2.0);
+                        totaldeformation[iDV][iDV_Value] += dv_value / 2.0;
                       }
                     }
                   }
                   nNegativeDeterminants_previous = nNegativeDeterminants;
                 }
-
               }
 
-            } // end SU2_DEF
+            }  // end SU2_DEF
 
             /*--- Reparametrization of the parent FFD box ---*/
 
@@ -484,8 +463,7 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
             FFDBox[iFFDBox]->SetCyl2Cart_CornerPoints(config);
             FFDBox[iFFDBox]->SetCyl2Cart_ControlPoints(config);
           }
-        }
-        else if (spherical || polar) {
+        } else if (spherical || polar) {
           for (iFFDBox = 0; iFFDBox < GetnFFDBox(); iFFDBox++) {
             FFDBox[iFFDBox]->SetSphe2Cart_CornerPoints(config);
             FFDBox[iFFDBox]->SetSphe2Cart_ControlPoints(config);
@@ -495,8 +473,7 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
         /*--- Output the deformed FFD Boxes ---*/
 
         if ((rank == MASTER_NODE) && (config->GetKind_SU2() != SU2_COMPONENT::SU2_DOT)) {
-
-          for (unsigned short iFile = 0; iFile < config->GetnVolumeOutputFiles(); iFile++){
+          for (unsigned short iFile = 0; iFile < config->GetnVolumeOutputFiles(); iFile++) {
             auto FileFormat = config->GetVolumeOutputFiles();
 
             if (isParaview(FileFormat[iFile])) {
@@ -509,8 +486,7 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
               for (iFFDBox = 0; iFFDBox < GetnFFDBox(); iFFDBox++) {
                 FFDBox[iFFDBox]->SetTecplot(geometry, iFFDBox, false);
               }
-            }
-            else if (FileFormat[iFile] == OUTPUT_TYPE::CGNS)  {
+            } else if (FileFormat[iFile] == OUTPUT_TYPE::CGNS) {
               cout << "Writing a CGNS file of the FFD boxes." << endl;
               for (iFFDBox = 0; iFFDBox < GetnFFDBox(); iFFDBox++) {
                 FFDBox[iFFDBox]->SetCGNS(geometry, iFFDBox, false);
@@ -530,7 +506,6 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
   /*--- External surface file based ---*/
 
   else if (config->GetDesign_Variable(0) == SURFACE_FILE) {
-
     /*--- Check whether a surface file exists for input ---*/
     ofstream Surface_File;
     string filename = config->GetDV_Filename();
@@ -539,13 +514,13 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
     /*--- A surface file does not exist, so write a new one for the
      markers that are specified as part of the motion. ---*/
     if (Surface_File.fail()) {
-
       if (rank == MASTER_NODE && size == SINGLE_NODE) {
         cout << "No surface positions file found. Writing a template file: " << filename << "." << endl;
 
         Surface_File.open(filename.c_str(), ios::out);
         Surface_File.precision(15);
-        unsigned long iMarker, jPoint, GlobalIndex, iVertex; su2double *Coords;
+        unsigned long iMarker, jPoint, GlobalIndex, iVertex;
+        su2double* Coords;
         for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
           if (config->GetMarker_All_DV(iMarker) == YES) {
             for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
@@ -553,15 +528,20 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
               GlobalIndex = geometry->nodes->GetGlobalIndex(jPoint);
               Coords = geometry->nodes->GetCoord(jPoint);
               Surface_File << GlobalIndex << "\t" << Coords[0] << "\t" << Coords[1];
-              if (geometry->GetnDim() == 2) Surface_File << endl;
-              else Surface_File << "\t" << Coords[2] << endl;
+              if (geometry->GetnDim() == 2)
+                Surface_File << endl;
+              else
+                Surface_File << "\t" << Coords[2] << endl;
             }
           }
         }
         Surface_File.close();
 
       } else {
-        SU2_MPI::Error("No surface positions file found and template writing not yet supported in parallel.\n To generate a template surface positions file, run SU2_DEF again in serial.", CURRENT_FUNCTION);
+        SU2_MPI::Error(
+            "No surface positions file found and template writing not yet supported in parallel.\n To generate a "
+            "template surface positions file, run SU2_DEF again in serial.",
+            CURRENT_FUNCTION);
       }
     }
 
@@ -574,45 +554,53 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
 
   }
 
-  else if ((config->GetDesign_Variable(0) == ROTATION) ||
-           (config->GetDesign_Variable(0) == TRANSLATION) ||
-           (config->GetDesign_Variable(0) == SCALE) ||
-           (config->GetDesign_Variable(0) == HICKS_HENNE) ||
-           (config->GetDesign_Variable(0) == SURFACE_BUMP) ||
-           (config->GetDesign_Variable(0) == ANGLE_OF_ATTACK)) {
-
+  else if ((config->GetDesign_Variable(0) == ROTATION) || (config->GetDesign_Variable(0) == TRANSLATION) ||
+           (config->GetDesign_Variable(0) == SCALE) || (config->GetDesign_Variable(0) == HICKS_HENNE) ||
+           (config->GetDesign_Variable(0) == SURFACE_BUMP) || (config->GetDesign_Variable(0) == ANGLE_OF_ATTACK)) {
     /*--- Apply rotation, displacement and stretching design variables (this
      should be done before the bump function design variables) ---*/
 
     for (iDV = 0; iDV < config->GetnDV(); iDV++) {
-      switch ( config->GetDesign_Variable(iDV) ) {
-        case SCALE :  SetScale(geometry, config, iDV, false); break;
-        case TRANSLATION :  SetTranslation(geometry, config, iDV, false); break;
-        case ROTATION :     SetRotation(geometry, config, iDV, false); break;
+      switch (config->GetDesign_Variable(iDV)) {
+        case SCALE:
+          SetScale(geometry, config, iDV, false);
+          break;
+        case TRANSLATION:
+          SetTranslation(geometry, config, iDV, false);
+          break;
+        case ROTATION:
+          SetRotation(geometry, config, iDV, false);
+          break;
       }
     }
 
     /*--- Apply the design variables to the control point position ---*/
 
     for (iDV = 0; iDV < config->GetnDV(); iDV++) {
-      switch ( config->GetDesign_Variable(iDV) ) {
-        case HICKS_HENNE :  SetHicksHenne(geometry, config, iDV, false); break;
+      switch (config->GetDesign_Variable(iDV)) {
+        case HICKS_HENNE:
+          SetHicksHenne(geometry, config, iDV, false);
+          break;
       }
     }
 
     /*--- Apply the design variables to the control point position ---*/
 
     for (iDV = 0; iDV < config->GetnDV(); iDV++) {
-      switch ( config->GetDesign_Variable(iDV) ) {
-        case SURFACE_BUMP :  SetSurface_Bump(geometry, config, iDV, false); break;
+      switch (config->GetDesign_Variable(iDV)) {
+        case SURFACE_BUMP:
+          SetSurface_Bump(geometry, config, iDV, false);
+          break;
       }
     }
 
     /*--- Apply the angle of attack design variable ---*/
 
     for (iDV = 0; iDV < config->GetnDV(); iDV++) {
-      switch ( config->GetDesign_Variable(iDV) ) {
-        case ANGLE_OF_ATTACK :  SetAngleOfAttack(geometry, config, iDV, false); break;
+      switch (config->GetDesign_Variable(iDV)) {
+        case ANGLE_OF_ATTACK:
+          SetAngleOfAttack(geometry, config, iDV, false);
+          break;
       }
     }
 
@@ -620,29 +608,32 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
 
   /*--- NACA_4Digits design variable ---*/
 
-  else if (config->GetDesign_Variable(0) == NACA_4DIGITS) { SetNACA_4Digits(geometry, config); }
+  else if (config->GetDesign_Variable(0) == NACA_4DIGITS) {
+    SetNACA_4Digits(geometry, config);
+  }
 
   /*--- Parabolic airfoil design variable ---*/
 
-  else if (config->GetDesign_Variable(0) == PARABOLIC) { SetParabolic(geometry, config); }
+  else if (config->GetDesign_Variable(0) == PARABOLIC) {
+    SetParabolic(geometry, config);
+  }
 
   /*--- Airfoil from file design variable ---*/
 
-  else if (config->GetDesign_Variable(0) == AIRFOIL) { SetAirfoil(geometry, config); }
+  else if (config->GetDesign_Variable(0) == AIRFOIL) {
+    SetAirfoil(geometry, config);
+  }
 
   /*--- FFD setting ---*/
 
   else if (config->GetDesign_Variable(0) == FFD_SETTING) {
-    if (rank == MASTER_NODE)
-      cout << "No surface deformation (setting FFD)." << endl;
+    if (rank == MASTER_NODE) cout << "No surface deformation (setting FFD)." << endl;
   }
 
   /*--- Scale, Translate, and Rotate will be done with rigid mesh transforms. ---*/
 
-  else if ((config->GetDesign_Variable(0) == ROTATION) ||
-           (config->GetDesign_Variable(0) == TRANSLATION) ||
+  else if ((config->GetDesign_Variable(0) == ROTATION) || (config->GetDesign_Variable(0) == TRANSLATION) ||
            (config->GetDesign_Variable(0) == SCALE)) {
-
     /*--- If all markers are deforming, use volume method.
      If only some are deforming, use surface method ---*/
 
@@ -653,52 +644,41 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry *g
 
     /*--- Loop over markers ---*/
     for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-      if (config->GetMarker_All_DV(iMarker) == NO)
-        allmoving = false;
+      if (config->GetMarker_All_DV(iMarker) == NO) allmoving = false;
     }
 
     if (!allmoving) {
       /*---Only some markers are moving, use the surface method ---*/
-      if (config->GetDesign_Variable(0) == ROTATION)
-        SetRotation(geometry, config, iDV, false);
-      if (config->GetDesign_Variable(0) == SCALE)
-        SetScale(geometry, config, iDV, false);
-      if (config->GetDesign_Variable(0) == TRANSLATION)
-        SetTranslation(geometry, config, iDV, false);
-    }
-    else {
-      if (rank == MASTER_NODE)
-        cout << "No surface deformation (scaling, rotation, or translation)." << endl;
+      if (config->GetDesign_Variable(0) == ROTATION) SetRotation(geometry, config, iDV, false);
+      if (config->GetDesign_Variable(0) == SCALE) SetScale(geometry, config, iDV, false);
+      if (config->GetDesign_Variable(0) == TRANSLATION) SetTranslation(geometry, config, iDV, false);
+    } else {
+      if (rank == MASTER_NODE) cout << "No surface deformation (scaling, rotation, or translation)." << endl;
     }
   }
 
   /*--- Design variable not implement ---*/
 
   else {
-    if (rank == MASTER_NODE)
-      cout << "Design Variable not implemented yet" << endl;
+    if (rank == MASTER_NODE) cout << "Design Variable not implemented yet" << endl;
   }
 
   return totaldeformation;
 }
 
-
-void CSurfaceMovement::SetSurface_Derivative(CGeometry *geometry, CConfig *config) {
-
+void CSurfaceMovement::SetSurface_Derivative(CGeometry* geometry, CConfig* config) {
   su2double DV_Value = 0.0;
 
   unsigned short iDV = 0, iDV_Value = 0;
 
   for (iDV = 0; iDV < config->GetnDV(); iDV++) {
     for (iDV_Value = 0; iDV_Value < config->GetnDV_Value(iDV); iDV_Value++) {
-
       DV_Value = config->GetDV_Value(iDV, iDV_Value);
 
       /*--- If value of the design variable is not 0.0 we apply the differentation.
-      *     Note if multiple variables are non-zero, we end up with the sum of all the derivatives. ---*/
+       *     Note if multiple variables are non-zero, we end up with the sum of all the derivatives. ---*/
 
       if (DV_Value != 0.0) {
-
         DV_Value = 0.0;
 
         SU2_TYPE::SetDerivative(DV_Value, 1.0);
@@ -713,11 +693,10 @@ void CSurfaceMovement::SetSurface_Derivative(CGeometry *geometry, CConfig *confi
   SetSurface_Deformation(geometry, config);
 }
 
-void CSurfaceMovement::CopyBoundary(CGeometry *geometry, CConfig *config) {
-
+void CSurfaceMovement::CopyBoundary(CGeometry* geometry, CConfig* config) {
   unsigned short iMarker;
   unsigned long iVertex, iPoint;
-  su2double *Coord;
+  su2double* Coord;
 
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
     for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
@@ -726,11 +705,10 @@ void CSurfaceMovement::CopyBoundary(CGeometry *geometry, CConfig *config) {
       geometry->vertex[iMarker][iVertex]->SetCoord(Coord);
     }
   }
-
 }
 
-void CSurfaceMovement::SetParametricCoord(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, unsigned short iFFDBox) {
-
+void CSurfaceMovement::SetParametricCoord(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox,
+                                          unsigned short iFFDBox) {
   unsigned short iMarker, iDim, iOrder, jOrder, kOrder, lOrder, mOrder, nOrder;
   unsigned long iVertex, iPoint, TotalVertex = 0;
   su2double *CartCoordNew, *ParamCoord, CartCoord[3], ParamCoordGuess[3], MaxDiff, my_MaxDiff = 0.0, Diff, *Coord;
@@ -747,25 +725,32 @@ void CSurfaceMovement::SetParametricCoord(CGeometry *geometry, CConfig *config,
  in case of Bezier curves, and we maintain an internal copy)---*/
 
   if (BoxFFD && (config->GetFFD_Blending() == BEZIER)) {
-
     for (iOrder = 0; iOrder < 2; iOrder++) {
       for (jOrder = 0; jOrder < 2; jOrder++) {
         for (kOrder = 0; kOrder < 2; kOrder++) {
-
-          lOrder = 0; mOrder = 0; nOrder = 0;
-          if (iOrder == 1) {lOrder = FFDBox->GetlOrder()-1;}
-          if (jOrder == 1) {mOrder = FFDBox->GetmOrder()-1;}
-          if (kOrder == 1) {nOrder = FFDBox->GetnOrder()-1;}
+          lOrder = 0;
+          mOrder = 0;
+          nOrder = 0;
+          if (iOrder == 1) {
+            lOrder = FFDBox->GetlOrder() - 1;
+          }
+          if (jOrder == 1) {
+            mOrder = FFDBox->GetmOrder() - 1;
+          }
+          if (kOrder == 1) {
+            nOrder = FFDBox->GetnOrder() - 1;
+          }
 
           Coord = FFDBox->GetCoordControlPoints(lOrder, mOrder, nOrder);
 
           FFDBox->SetCoordControlPoints(Coord, iOrder, jOrder, kOrder);
-
         }
       }
     }
 
-    FFDBox->SetlOrder(2); FFDBox->SetmOrder(2); FFDBox->SetnOrder(2);
+    FFDBox->SetlOrder(2);
+    FFDBox->SetmOrder(2);
+    FFDBox->SetnOrder(2);
     FFDBox->SetnControlPoints();
     FFDBox->BlendingFunction[0]->SetOrder(2, 2);
     FFDBox->BlendingFunction[1]->SetOrder(2, 2);
@@ -773,44 +758,54 @@ void CSurfaceMovement::SetParametricCoord(CGeometry *geometry, CConfig *config,
   }
   /*--- Point inversion algorithm with a basic box ---*/
 
-  ParamCoordGuess[0]  = 0.5; ParamCoordGuess[1] = 0.5; ParamCoordGuess[2] = 0.5;
-  CartCoord[0]        = 0.0; CartCoord[1]       = 0.0; CartCoord[2]       = 0.0;
+  ParamCoordGuess[0] = 0.5;
+  ParamCoordGuess[1] = 0.5;
+  ParamCoordGuess[2] = 0.5;
+  CartCoord[0] = 0.0;
+  CartCoord[1] = 0.0;
+  CartCoord[2] = 0.0;
 
   /*--- Count the number of vertices ---*/
 
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++)
     if (config->GetMarker_All_DV(iMarker) == YES)
-      for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++)
-        TotalVertex++;
+      for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) TotalVertex++;
 
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
     if (config->GetMarker_All_DV(iMarker) == YES) {
       for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
-
         /*--- Get the cartesian coordinates ---*/
 
-        for (iDim = 0; iDim < nDim; iDim++)
-          CartCoord[iDim] = geometry->vertex[iMarker][iVertex]->GetCoord(iDim);
+        for (iDim = 0; iDim < nDim; iDim++) CartCoord[iDim] = geometry->vertex[iMarker][iVertex]->GetCoord(iDim);
 
         /*--- Transform the cartesian into polar ---*/
 
         if (cylindrical) {
-          X_0 = config->GetFFD_Axis(0); Y_0 = config->GetFFD_Axis(1);  Z_0 = config->GetFFD_Axis(2);
+          X_0 = config->GetFFD_Axis(0);
+          Y_0 = config->GetFFD_Axis(1);
+          Z_0 = config->GetFFD_Axis(2);
 
-          Xbar =  CartCoord[0] - X_0; Ybar =  CartCoord[1] - Y_0; Zbar =  CartCoord[2] - Z_0;
+          Xbar = CartCoord[0] - X_0;
+          Ybar = CartCoord[1] - Y_0;
+          Zbar = CartCoord[2] - Z_0;
 
-          CartCoord[0] = sqrt(Ybar*Ybar + Zbar*Zbar);
-          CartCoord[1] = atan2(Zbar, Ybar); if (CartCoord[1] > PI_NUMBER/2.0) CartCoord[1] -= 2.0*PI_NUMBER;
+          CartCoord[0] = sqrt(Ybar * Ybar + Zbar * Zbar);
+          CartCoord[1] = atan2(Zbar, Ybar);
+          if (CartCoord[1] > PI_NUMBER / 2.0) CartCoord[1] -= 2.0 * PI_NUMBER;
           CartCoord[2] = Xbar;
-        }
-        else if (spherical || polar) {
-          X_0 = config->GetFFD_Axis(0); Y_0 = config->GetFFD_Axis(1);  Z_0 = config->GetFFD_Axis(2);
-
-          Xbar =  CartCoord[0] - X_0; Ybar =  CartCoord[1] - Y_0; Zbar =  CartCoord[2] - Z_0;
-
-          CartCoord[0] = sqrt(Xbar*Xbar + Ybar*Ybar + Zbar*Zbar);
-          CartCoord[1] = atan2(Zbar, Ybar);  if (CartCoord[1] > PI_NUMBER/2.0) CartCoord[1] -= 2.0*PI_NUMBER;
-          CartCoord[2] = acos(Xbar/CartCoord[0]);
+        } else if (spherical || polar) {
+          X_0 = config->GetFFD_Axis(0);
+          Y_0 = config->GetFFD_Axis(1);
+          Z_0 = config->GetFFD_Axis(2);
+
+          Xbar = CartCoord[0] - X_0;
+          Ybar = CartCoord[1] - Y_0;
+          Zbar = CartCoord[2] - Z_0;
+
+          CartCoord[0] = sqrt(Xbar * Xbar + Ybar * Ybar + Zbar * Zbar);
+          CartCoord[1] = atan2(Zbar, Ybar);
+          if (CartCoord[1] > PI_NUMBER / 2.0) CartCoord[1] -= 2.0 * PI_NUMBER;
+          CartCoord[2] = acos(Xbar / CartCoord[0]);
         }
 
         iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
@@ -818,7 +813,6 @@ void CSurfaceMovement::SetParametricCoord(CGeometry *geometry, CConfig *config,
         /*--- If the point is inside the FFD, compute the value of the parametric coordinate ---*/
 
         if (FFDBox->GetPointFFD(geometry, config, iPoint)) {
-
           /*--- Find the parametric coordinate ---*/
 
           ParamCoord = FFDBox->GetParametricCoord_Iterative(iPoint, CartCoord, ParamCoordGuess, config);
@@ -832,22 +826,21 @@ void CSurfaceMovement::SetParametricCoord(CGeometry *geometry, CConfig *config,
 
           Diff = 0.0;
           for (iDim = 0; iDim < nDim; iDim++)
-            Diff += (CartCoordNew[iDim]-CartCoord[iDim])*(CartCoordNew[iDim]-CartCoord[iDim]);
+            Diff += (CartCoordNew[iDim] - CartCoord[iDim]) * (CartCoordNew[iDim] - CartCoord[iDim]);
           Diff = sqrt(Diff);
           my_MaxDiff = max(my_MaxDiff, Diff);
 
-          /*--- If the parametric coordinates are in (0,1) the point belongs to the FFDBox, using the input tolerance  ---*/
-
-          if (((ParamCoord[0] >= - config->GetFFD_Tol()) && (ParamCoord[0] <= 1.0 + config->GetFFD_Tol())) &&
-              ((ParamCoord[1] >= - config->GetFFD_Tol()) && (ParamCoord[1] <= 1.0 + config->GetFFD_Tol())) &&
-              ((ParamCoord[2] >= - config->GetFFD_Tol()) && (ParamCoord[2] <= 1.0 + config->GetFFD_Tol()))) {
-
+          /*--- If the parametric coordinates are in (0,1) the point belongs to the FFDBox, using the input tolerance
+           * ---*/
 
+          if (((ParamCoord[0] >= -config->GetFFD_Tol()) && (ParamCoord[0] <= 1.0 + config->GetFFD_Tol())) &&
+              ((ParamCoord[1] >= -config->GetFFD_Tol()) && (ParamCoord[1] <= 1.0 + config->GetFFD_Tol())) &&
+              ((ParamCoord[2] >= -config->GetFFD_Tol()) && (ParamCoord[2] <= 1.0 + config->GetFFD_Tol()))) {
             /*--- Rectification of the initial tolerance (we have detected situations
              where 0.0 and 1.0 doesn't work properly ---*/
 
             su2double lower_limit = config->GetFFD_Tol();
-            su2double upper_limit = 1.0-config->GetFFD_Tol();
+            su2double upper_limit = 1.0 - config->GetFFD_Tol();
 
             if (ParamCoord[0] < lower_limit) ParamCoord[0] = lower_limit;
             if (ParamCoord[1] < lower_limit) ParamCoord[1] = lower_limit;
@@ -864,23 +857,23 @@ void CSurfaceMovement::SetParametricCoord(CGeometry *geometry, CConfig *config,
             FFDBox->Set_ParametricCoord(ParamCoord);
             FFDBox->Set_CartesianCoord(CartCoord);
 
-            ParamCoordGuess[0] = ParamCoord[0]; ParamCoordGuess[1] = ParamCoord[1]; ParamCoordGuess[2] = ParamCoord[2];
+            ParamCoordGuess[0] = ParamCoord[0];
+            ParamCoordGuess[1] = ParamCoord[1];
+            ParamCoordGuess[2] = ParamCoord[2];
 
             if (Diff >= config->GetFFD_Tol()) {
-              cout << "Please check this point: Local (" << ParamCoord[0] <<" "<< ParamCoord[1] <<" "<< ParamCoord[2] <<") <-> Global ("
-              << CartCoord[0] <<" "<< CartCoord[1] <<" "<< CartCoord[2] <<") <-> Error "<< Diff <<" vs "<< config->GetFFD_Tol() <<"." << endl;
+              cout << "Please check this point: Local (" << ParamCoord[0] << " " << ParamCoord[1] << " "
+                   << ParamCoord[2] << ") <-> Global (" << CartCoord[0] << " " << CartCoord[1] << " " << CartCoord[2]
+                   << ") <-> Error " << Diff << " vs " << config->GetFFD_Tol() << "." << endl;
             }
 
-          }
-          else {
-
+          } else {
             if (Diff >= config->GetFFD_Tol()) {
-              cout << "Please check this point: Local (" << ParamCoord[0] <<" "<< ParamCoord[1] <<" "<< ParamCoord[2] <<") <-> Global ("
-              << CartCoord[0] <<" "<< CartCoord[1] <<" "<< CartCoord[2] <<") <-> Error "<< Diff <<" vs "<< config->GetFFD_Tol() <<"." << endl;
+              cout << "Please check this point: Local (" << ParamCoord[0] << " " << ParamCoord[1] << " "
+                   << ParamCoord[2] << ") <-> Global (" << CartCoord[0] << " " << CartCoord[1] << " " << CartCoord[2]
+                   << ") <-> Error " << Diff << " vs " << config->GetFFD_Tol() << "." << endl;
             }
-
           }
-
         }
       }
     }
@@ -893,8 +886,7 @@ void CSurfaceMovement::SetParametricCoord(CGeometry *geometry, CConfig *config,
 #endif
 
   if (rank == MASTER_NODE)
-    cout << "Compute parametric coord      | FFD box: " << FFDBox->GetTag() << ". Max Diff: " << MaxDiff <<"."<< endl;
-
+    cout << "Compute parametric coord      | FFD box: " << FFDBox->GetTag() << ". Max Diff: " << MaxDiff << "." << endl;
 
   /*--- After the point inversion, copy the original
    information back (this only works with boxes,
@@ -902,7 +894,7 @@ void CSurfaceMovement::SetParametricCoord(CGeometry *geometry, CConfig *config,
 
   if (BoxFFD) {
     FFDBox->SetOriginalControlPoints();
-    if (config->GetFFD_Blending() == BEZIER){
+    if (config->GetFFD_Blending() == BEZIER) {
       FFDBox->BlendingFunction[0]->SetOrder(FFDBox->GetlOrder(), FFDBox->GetlOrder());
       FFDBox->BlendingFunction[1]->SetOrder(FFDBox->GetmOrder(), FFDBox->GetmOrder());
       FFDBox->BlendingFunction[2]->SetOrder(FFDBox->GetnOrder(), FFDBox->GetnOrder());
@@ -910,7 +902,8 @@ void CSurfaceMovement::SetParametricCoord(CGeometry *geometry, CConfig *config,
   }
 }
 
-void CSurfaceMovement::SetParametricCoordCP(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBoxParent, CFreeFormDefBox *FFDBoxChild) {
+void CSurfaceMovement::SetParametricCoordCP(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBoxParent,
+                                            CFreeFormDefBox* FFDBoxChild) {
   unsigned short iOrder, jOrder, kOrder;
   su2double *CartCoord, *ParamCoord, ParamCoordGuess[3];
 
@@ -923,12 +916,12 @@ void CSurfaceMovement::SetParametricCoordCP(CGeometry *geometry, CConfig *config
       }
 
   if (rank == MASTER_NODE)
-    cout << "Compute parametric coord (CP) | FFD parent box: " << FFDBoxParent->GetTag() << ". FFD child box: " << FFDBoxChild->GetTag() <<"."<< endl;
-
-
+    cout << "Compute parametric coord (CP) | FFD parent box: " << FFDBoxParent->GetTag()
+         << ". FFD child box: " << FFDBoxChild->GetTag() << "." << endl;
 }
 
-void CSurfaceMovement::GetCartesianCoordCP(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBoxParent, CFreeFormDefBox *FFDBoxChild) {
+void CSurfaceMovement::GetCartesianCoordCP(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBoxParent,
+                                           CFreeFormDefBox* FFDBoxChild) {
   unsigned short iOrder, jOrder, kOrder, iDim;
   su2double *CartCoord, *ParamCoord;
 
@@ -946,57 +939,59 @@ void CSurfaceMovement::GetCartesianCoordCP(CGeometry *geometry, CConfig *config,
         CartCoord = FFDBoxParent->EvalCartesianCoord(ParamCoord);
         FFDBoxChild->SetCoordControlPoints(CartCoord, iOrder, jOrder, kOrder);
         FFDBoxChild->SetCoordControlPoints_Copy(CartCoord, iOrder, jOrder, kOrder);
-
       }
 
   if (rank == MASTER_NODE)
-    cout << "Update cartesian coord (CP)   | FFD parent box: " << FFDBoxParent->GetTag() << ". FFD child box: " << FFDBoxChild->GetTag() <<"."<< endl;
-
+    cout << "Update cartesian coord (CP)   | FFD parent box: " << FFDBoxParent->GetTag()
+         << ". FFD child box: " << FFDBoxChild->GetTag() << "." << endl;
 }
 
-void CSurfaceMovement::CheckFFDDimension(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, unsigned short iFFDBox) {
-
+void CSurfaceMovement::CheckFFDDimension(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox,
+                                         unsigned short iFFDBox) {
   unsigned short iIndex, jIndex, kIndex, lDegree, mDegree, nDegree, iDV;
   bool OutOffLimits;
   bool polar = (config->GetFFD_CoordSystem() == POLAR);
 
-  lDegree = FFDBox->GetlOrder()-1;
-  mDegree = FFDBox->GetmOrder()-1;
-  nDegree = FFDBox->GetnOrder()-1;
+  lDegree = FFDBox->GetlOrder() - 1;
+  mDegree = FFDBox->GetmOrder() - 1;
+  nDegree = FFDBox->GetnOrder() - 1;
 
   OutOffLimits = false;
   for (iDV = 0; iDV < config->GetnDV(); iDV++) {
-    if (config->GetFFDTag(iDV)== FFDBox->GetTag()){
-      switch ( config->GetDesign_Variable(iDV) ) {
-        case FFD_CONTROL_POINT_2D :
+    if (config->GetFFDTag(iDV) == FFDBox->GetTag()) {
+      switch (config->GetDesign_Variable(iDV)) {
+        case FFD_CONTROL_POINT_2D:
           if (polar) {
             iIndex = SU2_TYPE::Int(fabs(config->GetParamDV(iDV, 1)));
             kIndex = SU2_TYPE::Int(fabs(config->GetParamDV(iDV, 2)));
             if ((iIndex > lDegree) || (kIndex > nDegree)) OutOffLimits = true;
-          }
-          else {
+          } else {
             iIndex = SU2_TYPE::Int(fabs(config->GetParamDV(iDV, 1)));
             jIndex = SU2_TYPE::Int(fabs(config->GetParamDV(iDV, 2)));
             if ((iIndex > lDegree) || (jIndex > mDegree)) OutOffLimits = true;
           }
           break;
-        case FFD_CAMBER :  case FFD_THICKNESS :
-            iIndex = SU2_TYPE::Int(fabs(config->GetParamDV(iDV, 1)));
-            jIndex = SU2_TYPE::Int(fabs(config->GetParamDV(iDV, 2)));
-            if ((iIndex > lDegree) || (jIndex > mDegree)) OutOffLimits = true;
+        case FFD_CAMBER:
+        case FFD_THICKNESS:
+          iIndex = SU2_TYPE::Int(fabs(config->GetParamDV(iDV, 1)));
+          jIndex = SU2_TYPE::Int(fabs(config->GetParamDV(iDV, 2)));
+          if ((iIndex > lDegree) || (jIndex > mDegree)) OutOffLimits = true;
           break;
-        case FFD_CAMBER_2D :  case FFD_THICKNESS_2D :
+        case FFD_CAMBER_2D:
+        case FFD_THICKNESS_2D:
           iIndex = SU2_TYPE::Int(fabs(config->GetParamDV(iDV, 1)));
           if (iIndex > lDegree) OutOffLimits = true;
           break;
-        case FFD_CONTROL_POINT :  case FFD_NACELLE :
+        case FFD_CONTROL_POINT:
+        case FFD_NACELLE:
           iIndex = SU2_TYPE::Int(fabs(config->GetParamDV(iDV, 1)));
-          jIndex= SU2_TYPE::Int(fabs(config->GetParamDV(iDV, 2)));
+          jIndex = SU2_TYPE::Int(fabs(config->GetParamDV(iDV, 2)));
           kIndex = SU2_TYPE::Int(fabs(config->GetParamDV(iDV, 3)));
           if ((iIndex > lDegree) || (jIndex > mDegree) || (kIndex > nDegree)) OutOffLimits = true;
           break;
-        case FFD_GULL :  case FFD_TWIST :
-          jIndex= SU2_TYPE::Int(fabs(config->GetParamDV(iDV, 1)));
+        case FFD_GULL:
+        case FFD_TWIST:
+          jIndex = SU2_TYPE::Int(fabs(config->GetParamDV(iDV, 1)));
           if (jIndex > mDegree) OutOffLimits = true;
           break;
       }
@@ -1017,12 +1012,11 @@ void CSurfaceMovement::CheckFFDDimension(CGeometry *geometry, CConfig *config, C
 #ifdef HAVE_MPI
   SU2_MPI::Barrier(SU2_MPI::GetComm());
 #endif
-
 }
 
-void CSurfaceMovement::CheckFFDIntersections(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, unsigned short iFFDBox) {
-
-  su2double Coord_0[] = {0,0,0}, Coord_1[] = {0,0,0};
+void CSurfaceMovement::CheckFFDIntersections(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox,
+                                             unsigned short iFFDBox) {
+  su2double Coord_0[] = {0, 0, 0}, Coord_1[] = {0, 0, 0};
   unsigned short index, iMarker, iNode, jNode, lDegree, mDegree, nDegree, iDim;
   unsigned long iElem, iPoint, jPoint;
   bool IPlane_Intersect_A = false, IPlane_Intersect_B = false;
@@ -1037,90 +1031,89 @@ void CSurfaceMovement::CheckFFDIntersections(CGeometry *geometry, CConfig *confi
   bool polar = (config->GetFFD_CoordSystem() == POLAR);
   bool cartesian = (config->GetFFD_CoordSystem() == CARTESIAN);
 
-  lDegree = FFDBox->GetlOrder()-1;
-  mDegree = FFDBox->GetmOrder()-1;
-  nDegree = FFDBox->GetnOrder()-1;
+  lDegree = FFDBox->GetlOrder() - 1;
+  mDegree = FFDBox->GetmOrder() - 1;
+  nDegree = FFDBox->GetnOrder() - 1;
 
   if (config->GetFFD_Continuity() != USER_INPUT) {
-
     /*--- Check intersection with plane i=0 ---*/
 
-    su2double *IPlane_Coord_0_A = FFDBox->GetCoordControlPoints(0, 0, 0);
-    su2double *IPlane_Coord_1_A = FFDBox->GetCoordControlPoints(0, 0, nDegree);
-    su2double *IPlane_Coord_2_A = FFDBox->GetCoordControlPoints(0, mDegree, 0);
+    su2double* IPlane_Coord_0_A = FFDBox->GetCoordControlPoints(0, 0, 0);
+    su2double* IPlane_Coord_1_A = FFDBox->GetCoordControlPoints(0, 0, nDegree);
+    su2double* IPlane_Coord_2_A = FFDBox->GetCoordControlPoints(0, mDegree, 0);
 
-    su2double *IPlane_Coord_0_A_ = FFDBox->GetCoordControlPoints(0, mDegree, nDegree);
-    su2double *IPlane_Coord_1_A_ = FFDBox->GetCoordControlPoints(0, mDegree, 0);
-    su2double *IPlane_Coord_2_A_ = FFDBox->GetCoordControlPoints(0, 0, nDegree);
+    su2double* IPlane_Coord_0_A_ = FFDBox->GetCoordControlPoints(0, mDegree, nDegree);
+    su2double* IPlane_Coord_1_A_ = FFDBox->GetCoordControlPoints(0, mDegree, 0);
+    su2double* IPlane_Coord_2_A_ = FFDBox->GetCoordControlPoints(0, 0, nDegree);
 
     /*--- Check intersection with plane i=lDegree ---*/
 
-    su2double *IPlane_Coord_0_B = FFDBox->GetCoordControlPoints(lDegree, 0, 0);
-    su2double *IPlane_Coord_1_B = FFDBox->GetCoordControlPoints(lDegree, 0, nDegree);
-    su2double *IPlane_Coord_2_B = FFDBox->GetCoordControlPoints(lDegree, mDegree, 0);
+    su2double* IPlane_Coord_0_B = FFDBox->GetCoordControlPoints(lDegree, 0, 0);
+    su2double* IPlane_Coord_1_B = FFDBox->GetCoordControlPoints(lDegree, 0, nDegree);
+    su2double* IPlane_Coord_2_B = FFDBox->GetCoordControlPoints(lDegree, mDegree, 0);
 
-    su2double *IPlane_Coord_0_B_ = FFDBox->GetCoordControlPoints(lDegree, mDegree, nDegree);
-    su2double *IPlane_Coord_1_B_ = FFDBox->GetCoordControlPoints(lDegree, mDegree, 0);
-    su2double *IPlane_Coord_2_B_ = FFDBox->GetCoordControlPoints(lDegree, 0, nDegree);
+    su2double* IPlane_Coord_0_B_ = FFDBox->GetCoordControlPoints(lDegree, mDegree, nDegree);
+    su2double* IPlane_Coord_1_B_ = FFDBox->GetCoordControlPoints(lDegree, mDegree, 0);
+    su2double* IPlane_Coord_2_B_ = FFDBox->GetCoordControlPoints(lDegree, 0, nDegree);
 
     /*--- Check intersection with plane j=0 ---*/
 
-    su2double *JPlane_Coord_0_A = FFDBox->GetCoordControlPoints(0,      0, 0);
-    su2double *JPlane_Coord_1_A = FFDBox->GetCoordControlPoints(0,      0, nDegree);
-    su2double *JPlane_Coord_2_A = FFDBox->GetCoordControlPoints(lDegree, 0, 0);
+    su2double* JPlane_Coord_0_A = FFDBox->GetCoordControlPoints(0, 0, 0);
+    su2double* JPlane_Coord_1_A = FFDBox->GetCoordControlPoints(0, 0, nDegree);
+    su2double* JPlane_Coord_2_A = FFDBox->GetCoordControlPoints(lDegree, 0, 0);
 
-    su2double *JPlane_Coord_0_A_ = FFDBox->GetCoordControlPoints(lDegree, 0, nDegree);
-    su2double *JPlane_Coord_1_A_ = FFDBox->GetCoordControlPoints(lDegree, 0, 0);
-    su2double *JPlane_Coord_2_A_ = FFDBox->GetCoordControlPoints(0,      0, nDegree);
+    su2double* JPlane_Coord_0_A_ = FFDBox->GetCoordControlPoints(lDegree, 0, nDegree);
+    su2double* JPlane_Coord_1_A_ = FFDBox->GetCoordControlPoints(lDegree, 0, 0);
+    su2double* JPlane_Coord_2_A_ = FFDBox->GetCoordControlPoints(0, 0, nDegree);
 
     /*--- Check intersection with plane j=mDegree ---*/
 
-    su2double *JPlane_Coord_0_B = FFDBox->GetCoordControlPoints(0,      mDegree, 0);
-    su2double *JPlane_Coord_1_B = FFDBox->GetCoordControlPoints(0,      mDegree, nDegree);
-    su2double *JPlane_Coord_2_B = FFDBox->GetCoordControlPoints(lDegree, mDegree, 0);
+    su2double* JPlane_Coord_0_B = FFDBox->GetCoordControlPoints(0, mDegree, 0);
+    su2double* JPlane_Coord_1_B = FFDBox->GetCoordControlPoints(0, mDegree, nDegree);
+    su2double* JPlane_Coord_2_B = FFDBox->GetCoordControlPoints(lDegree, mDegree, 0);
 
-    su2double *JPlane_Coord_0_B_ = FFDBox->GetCoordControlPoints(lDegree, mDegree, nDegree);
-    su2double *JPlane_Coord_1_B_ = FFDBox->GetCoordControlPoints(lDegree, mDegree, 0);
-    su2double *JPlane_Coord_2_B_ = FFDBox->GetCoordControlPoints(0,      mDegree, nDegree);
+    su2double* JPlane_Coord_0_B_ = FFDBox->GetCoordControlPoints(lDegree, mDegree, nDegree);
+    su2double* JPlane_Coord_1_B_ = FFDBox->GetCoordControlPoints(lDegree, mDegree, 0);
+    su2double* JPlane_Coord_2_B_ = FFDBox->GetCoordControlPoints(0, mDegree, nDegree);
 
     /*--- Check intersection with plane k=0 ---*/
 
-    su2double *KPlane_Coord_0_A = FFDBox->GetCoordControlPoints(0,      0,      0);
-    su2double *KPlane_Coord_1_A = FFDBox->GetCoordControlPoints(0,      mDegree, 0);
-    su2double *KPlane_Coord_2_A = FFDBox->GetCoordControlPoints(lDegree, 0,      0);
+    su2double* KPlane_Coord_0_A = FFDBox->GetCoordControlPoints(0, 0, 0);
+    su2double* KPlane_Coord_1_A = FFDBox->GetCoordControlPoints(0, mDegree, 0);
+    su2double* KPlane_Coord_2_A = FFDBox->GetCoordControlPoints(lDegree, 0, 0);
 
-    su2double *KPlane_Coord_0_A_ = FFDBox->GetCoordControlPoints(lDegree, mDegree, 0);
-    su2double *KPlane_Coord_1_A_ = FFDBox->GetCoordControlPoints(lDegree, 0,      0);
-    su2double *KPlane_Coord_2_A_ = FFDBox->GetCoordControlPoints(0,      mDegree, 0);
+    su2double* KPlane_Coord_0_A_ = FFDBox->GetCoordControlPoints(lDegree, mDegree, 0);
+    su2double* KPlane_Coord_1_A_ = FFDBox->GetCoordControlPoints(lDegree, 0, 0);
+    su2double* KPlane_Coord_2_A_ = FFDBox->GetCoordControlPoints(0, mDegree, 0);
 
     /*--- Check intersection with plane k=nDegree ---*/
 
-    su2double *KPlane_Coord_0_B = FFDBox->GetCoordControlPoints(0,      0,      nDegree);
-    su2double *KPlane_Coord_1_B = FFDBox->GetCoordControlPoints(0,      mDegree, nDegree);
-    su2double *KPlane_Coord_2_B = FFDBox->GetCoordControlPoints(lDegree, 0,      nDegree);
+    su2double* KPlane_Coord_0_B = FFDBox->GetCoordControlPoints(0, 0, nDegree);
+    su2double* KPlane_Coord_1_B = FFDBox->GetCoordControlPoints(0, mDegree, nDegree);
+    su2double* KPlane_Coord_2_B = FFDBox->GetCoordControlPoints(lDegree, 0, nDegree);
 
-    su2double *KPlane_Coord_0_B_ = FFDBox->GetCoordControlPoints(lDegree, mDegree, nDegree);
-    su2double *KPlane_Coord_1_B_ = FFDBox->GetCoordControlPoints(lDegree, 0,      nDegree);
-    su2double *KPlane_Coord_2_B_ = FFDBox->GetCoordControlPoints(0,      mDegree, nDegree);
+    su2double* KPlane_Coord_0_B_ = FFDBox->GetCoordControlPoints(lDegree, mDegree, nDegree);
+    su2double* KPlane_Coord_1_B_ = FFDBox->GetCoordControlPoints(lDegree, 0, nDegree);
+    su2double* KPlane_Coord_2_B_ = FFDBox->GetCoordControlPoints(0, mDegree, nDegree);
 
     /*--- Loop over all the grid triangles ---*/
 
-    IPlane_Intersect_A = false; IPlane_Intersect_B = false;
-    JPlane_Intersect_A = false; JPlane_Intersect_B = false;
-    KPlane_Intersect_A = false; KPlane_Intersect_B = false;
+    IPlane_Intersect_A = false;
+    IPlane_Intersect_B = false;
+    JPlane_Intersect_A = false;
+    JPlane_Intersect_B = false;
+    KPlane_Intersect_A = false;
+    KPlane_Intersect_B = false;
 
     /*--- Only the markers in the moving list ---*/
 
     for (iMarker = 0; iMarker < geometry->GetnMarker(); iMarker++) {
-
       if (((config->GetMarker_All_Moving(iMarker) == YES) && (Kind_SU2 == SU2_COMPONENT::SU2_CFD)) ||
           ((config->GetMarker_All_DV(iMarker) == YES) && (Kind_SU2 == SU2_COMPONENT::SU2_DEF)) ||
           ((config->GetMarker_All_DV(iMarker) == YES) && (Kind_SU2 == SU2_COMPONENT::SU2_GEO)) ||
           ((config->GetMarker_All_DV(iMarker) == YES) && (Kind_SU2 == SU2_COMPONENT::SU2_DOT)) ||
           ((config->GetMarker_All_DV(iMarker) == YES) && (config->GetDirectDiff() == D_DESIGN))) {
-
         for (iElem = 0; iElem < geometry->GetnElem_Bound(iMarker); iElem++) {
-
           for (iNode = 0; iNode < geometry->bound[iMarker][iElem]->GetnNodes(); iNode++) {
             iPoint = geometry->bound[iMarker][iElem]->GetNode(iNode);
 
@@ -1128,103 +1121,162 @@ void CSurfaceMovement::CheckFFDIntersections(CGeometry *geometry, CConfig *confi
               jPoint = geometry->bound[iMarker][iElem]->GetNode(jNode);
 
               if (jPoint > iPoint) {
-
                 for (iDim = 0; iDim < geometry->GetnDim(); iDim++) {
-                  Coord_0[iDim] = geometry->nodes->GetCoord(iPoint,iDim);
-                  Coord_1[iDim] = geometry->nodes->GetCoord(jPoint,iDim);
+                  Coord_0[iDim] = geometry->nodes->GetCoord(iPoint, iDim);
+                  Coord_1[iDim] = geometry->nodes->GetCoord(jPoint, iDim);
                 }
 
                 /*--- Write the coordinates in the right parametric system ---*/
 
                 if (cylindrical) {
+                  X_0 = config->GetFFD_Axis(0);
+                  Y_0 = config->GetFFD_Axis(1);
+                  Z_0 = config->GetFFD_Axis(2);
 
-                  X_0 = config->GetFFD_Axis(0); Y_0 = config->GetFFD_Axis(1);  Z_0 = config->GetFFD_Axis(2);
+                  Xbar = Coord_0[0] - X_0;
+                  Ybar = Coord_0[1] - Y_0;
+                  Zbar = Coord_0[2] - Z_0;
 
-                  Xbar =  Coord_0[0] - X_0; Ybar =  Coord_0[1] - Y_0; Zbar =  Coord_0[2] - Z_0;
-
-                  Coord_0[0] = sqrt(Ybar*Ybar + Zbar*Zbar);
-                  Coord_0[1] = atan2(Zbar, Ybar); if (Coord_0[1] > PI_NUMBER/2.0) Coord_0[1] -= 2.0*PI_NUMBER;
+                  Coord_0[0] = sqrt(Ybar * Ybar + Zbar * Zbar);
+                  Coord_0[1] = atan2(Zbar, Ybar);
+                  if (Coord_0[1] > PI_NUMBER / 2.0) Coord_0[1] -= 2.0 * PI_NUMBER;
                   Coord_0[2] = Xbar;
 
-                  Xbar =  Coord_1[0] - X_0; Ybar =  Coord_1[1] - Y_0; Zbar =  Coord_1[2] - Z_0;
+                  Xbar = Coord_1[0] - X_0;
+                  Ybar = Coord_1[1] - Y_0;
+                  Zbar = Coord_1[2] - Z_0;
 
-                  Coord_1[0] = sqrt(Ybar*Ybar + Zbar*Zbar);
-                  Coord_1[1] = atan2(Zbar, Ybar); if (Coord_1[1] > PI_NUMBER/2.0) Coord_1[1] -= 2.0*PI_NUMBER;
+                  Coord_1[0] = sqrt(Ybar * Ybar + Zbar * Zbar);
+                  Coord_1[1] = atan2(Zbar, Ybar);
+                  if (Coord_1[1] > PI_NUMBER / 2.0) Coord_1[1] -= 2.0 * PI_NUMBER;
                   Coord_1[2] = Xbar;
 
                 }
 
                 else if (spherical || polar) {
-
-                  X_0 = config->GetFFD_Axis(0); Y_0 = config->GetFFD_Axis(1);  Z_0 = config->GetFFD_Axis(2);
-
-                  Xbar =  Coord_0[0] - X_0; Ybar =  Coord_0[1] - Y_0; Zbar =  Coord_0[2] - Z_0;
-
-                  Coord_0[0] = sqrt(Xbar*Xbar + Ybar*Ybar + Zbar*Zbar);
-                  Coord_0[1] = atan2(Zbar, Ybar);  if (Coord_0[1] > PI_NUMBER/2.0) Coord_0[1] -= 2.0*PI_NUMBER;
-                  Coord_0[2] = acos (Xbar/Coord_0[0]);
-
-                  Xbar =  Coord_1[0] - X_0; Ybar =  Coord_1[1] - Y_0; Zbar =  Coord_1[2] - Z_0;
-
-                  Coord_1[0] = sqrt(Xbar*Xbar + Ybar*Ybar + Zbar*Zbar);
-                  Coord_1[1] = atan2(Zbar, Ybar);  if (Coord_1[1] > PI_NUMBER/2.0) Coord_1[1] -= 2.0*PI_NUMBER;
-                  Coord_1[2] = acos(Xbar/Coord_1[0]);
-
+                  X_0 = config->GetFFD_Axis(0);
+                  Y_0 = config->GetFFD_Axis(1);
+                  Z_0 = config->GetFFD_Axis(2);
+
+                  Xbar = Coord_0[0] - X_0;
+                  Ybar = Coord_0[1] - Y_0;
+                  Zbar = Coord_0[2] - Z_0;
+
+                  Coord_0[0] = sqrt(Xbar * Xbar + Ybar * Ybar + Zbar * Zbar);
+                  Coord_0[1] = atan2(Zbar, Ybar);
+                  if (Coord_0[1] > PI_NUMBER / 2.0) Coord_0[1] -= 2.0 * PI_NUMBER;
+                  Coord_0[2] = acos(Xbar / Coord_0[0]);
+
+                  Xbar = Coord_1[0] - X_0;
+                  Ybar = Coord_1[1] - Y_0;
+                  Zbar = Coord_1[2] - Z_0;
+
+                  Coord_1[0] = sqrt(Xbar * Xbar + Ybar * Ybar + Zbar * Zbar);
+                  Coord_1[1] = atan2(Zbar, Ybar);
+                  if (Coord_1[1] > PI_NUMBER / 2.0) Coord_1[1] -= 2.0 * PI_NUMBER;
+                  Coord_1[2] = acos(Xbar / Coord_1[0]);
                 }
 
                 if (geometry->GetnDim() == 3) {
-
                   if (!IPlane_Intersect_A) {
-                    if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, IPlane_Coord_0_A, IPlane_Coord_1_A, IPlane_Coord_2_A)) { IPlane_Intersect_A = true; }
-                    if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, IPlane_Coord_0_A_, IPlane_Coord_1_A_, IPlane_Coord_2_A_)) { IPlane_Intersect_A = true; }
+                    if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, IPlane_Coord_0_A, IPlane_Coord_1_A,
+                                                            IPlane_Coord_2_A)) {
+                      IPlane_Intersect_A = true;
+                    }
+                    if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, IPlane_Coord_0_A_, IPlane_Coord_1_A_,
+                                                            IPlane_Coord_2_A_)) {
+                      IPlane_Intersect_A = true;
+                    }
                   }
 
                   if (!IPlane_Intersect_B) {
-                    if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, IPlane_Coord_0_B, IPlane_Coord_1_B, IPlane_Coord_2_B)) { IPlane_Intersect_B = true; }
-                    if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, IPlane_Coord_0_B_, IPlane_Coord_1_B_, IPlane_Coord_2_B_)) { IPlane_Intersect_B = true; }
+                    if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, IPlane_Coord_0_B, IPlane_Coord_1_B,
+                                                            IPlane_Coord_2_B)) {
+                      IPlane_Intersect_B = true;
+                    }
+                    if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, IPlane_Coord_0_B_, IPlane_Coord_1_B_,
+                                                            IPlane_Coord_2_B_)) {
+                      IPlane_Intersect_B = true;
+                    }
                   }
 
                   if ((!JPlane_Intersect_A) && (!FFD_Symmetry_Plane)) {
-                    if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, JPlane_Coord_0_A, JPlane_Coord_1_A, JPlane_Coord_2_A)) { JPlane_Intersect_A = true; }
-                    if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, JPlane_Coord_0_A_, JPlane_Coord_1_A_, JPlane_Coord_2_A_)) { JPlane_Intersect_A = true; }
+                    if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, JPlane_Coord_0_A, JPlane_Coord_1_A,
+                                                            JPlane_Coord_2_A)) {
+                      JPlane_Intersect_A = true;
+                    }
+                    if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, JPlane_Coord_0_A_, JPlane_Coord_1_A_,
+                                                            JPlane_Coord_2_A_)) {
+                      JPlane_Intersect_A = true;
+                    }
                   }
 
                   if (cartesian) {
                     if ((!JPlane_Intersect_B) && (!FFD_Symmetry_Plane)) {
-                      if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, JPlane_Coord_0_B, JPlane_Coord_1_B, JPlane_Coord_2_B)) { JPlane_Intersect_B = true; }
-                      if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, JPlane_Coord_0_B_, JPlane_Coord_1_B_, JPlane_Coord_2_B_)) { JPlane_Intersect_B = true; }
+                      if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, JPlane_Coord_0_B, JPlane_Coord_1_B,
+                                                              JPlane_Coord_2_B)) {
+                        JPlane_Intersect_B = true;
+                      }
+                      if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, JPlane_Coord_0_B_, JPlane_Coord_1_B_,
+                                                              JPlane_Coord_2_B_)) {
+                        JPlane_Intersect_B = true;
+                      }
                     }
-                  }
-                  else {
+                  } else {
                     if (!JPlane_Intersect_B) {
-                      if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, JPlane_Coord_0_B, JPlane_Coord_1_B, JPlane_Coord_2_B)) { JPlane_Intersect_B = true; }
-                      if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, JPlane_Coord_0_B_, JPlane_Coord_1_B_, JPlane_Coord_2_B_)) { JPlane_Intersect_B = true; }
+                      if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, JPlane_Coord_0_B, JPlane_Coord_1_B,
+                                                              JPlane_Coord_2_B)) {
+                        JPlane_Intersect_B = true;
+                      }
+                      if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, JPlane_Coord_0_B_, JPlane_Coord_1_B_,
+                                                              JPlane_Coord_2_B_)) {
+                        JPlane_Intersect_B = true;
+                      }
                     }
                   }
 
                   if (!KPlane_Intersect_A) {
-                    if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, KPlane_Coord_0_A, KPlane_Coord_1_A, KPlane_Coord_2_A)) { KPlane_Intersect_A = true; }
-                    if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, KPlane_Coord_0_A_, KPlane_Coord_1_A_, KPlane_Coord_2_A_)) { KPlane_Intersect_A = true; }
+                    if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, KPlane_Coord_0_A, KPlane_Coord_1_A,
+                                                            KPlane_Coord_2_A)) {
+                      KPlane_Intersect_A = true;
+                    }
+                    if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, KPlane_Coord_0_A_, KPlane_Coord_1_A_,
+                                                            KPlane_Coord_2_A_)) {
+                      KPlane_Intersect_A = true;
+                    }
                   }
 
                   if (!KPlane_Intersect_B) {
-                    if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, KPlane_Coord_0_B, KPlane_Coord_1_B, KPlane_Coord_2_B)) { KPlane_Intersect_B = true; }
-                    if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, KPlane_Coord_0_B_, KPlane_Coord_1_B_, KPlane_Coord_2_B_)) { KPlane_Intersect_B = true; }
+                    if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, KPlane_Coord_0_B, KPlane_Coord_1_B,
+                                                            KPlane_Coord_2_B)) {
+                      KPlane_Intersect_B = true;
+                    }
+                    if (geometry->SegmentIntersectsTriangle(Coord_0, Coord_1, KPlane_Coord_0_B_, KPlane_Coord_1_B_,
+                                                            KPlane_Coord_2_B_)) {
+                      KPlane_Intersect_B = true;
+                    }
                   }
 
                 } else {
-
                   if (!IPlane_Intersect_A) {
-                    if (geometry->SegmentIntersectsLine(Coord_0, Coord_1, IPlane_Coord_0_A, IPlane_Coord_2_A)) { IPlane_Intersect_A = true;}
+                    if (geometry->SegmentIntersectsLine(Coord_0, Coord_1, IPlane_Coord_0_A, IPlane_Coord_2_A)) {
+                      IPlane_Intersect_A = true;
+                    }
                   }
                   if (!IPlane_Intersect_B) {
-                    if (geometry->SegmentIntersectsLine(Coord_0, Coord_1, IPlane_Coord_0_B, IPlane_Coord_2_B)) { IPlane_Intersect_B = true;}
+                    if (geometry->SegmentIntersectsLine(Coord_0, Coord_1, IPlane_Coord_0_B, IPlane_Coord_2_B)) {
+                      IPlane_Intersect_B = true;
+                    }
                   }
                   if (!JPlane_Intersect_A) {
-                    if (geometry->SegmentIntersectsLine(Coord_0, Coord_1, JPlane_Coord_0_A, JPlane_Coord_2_A)) { JPlane_Intersect_A = true;}
+                    if (geometry->SegmentIntersectsLine(Coord_0, Coord_1, JPlane_Coord_0_A, JPlane_Coord_2_A)) {
+                      JPlane_Intersect_A = true;
+                    }
                   }
                   if (!JPlane_Intersect_B) {
-                    if (geometry->SegmentIntersectsLine(Coord_0, Coord_1, JPlane_Coord_0_B, JPlane_Coord_2_B)) { JPlane_Intersect_B = true;}
+                    if (geometry->SegmentIntersectsLine(Coord_0, Coord_1, JPlane_Coord_0_B, JPlane_Coord_2_B)) {
+                      JPlane_Intersect_B = true;
+                    }
                   }
                 }
               }
@@ -1236,7 +1288,7 @@ void CSurfaceMovement::CheckFFDIntersections(CGeometry *geometry, CConfig *confi
 
     /*--- Comunicate the planes that interesect the surface ---*/
 
-    unsigned short MyCode[6] = {0,0,0,0,0,0}, Code[6] = {0,0,0,0,0,0};
+    unsigned short MyCode[6] = {0, 0, 0, 0, 0, 0}, Code[6] = {0, 0, 0, 0, 0, 0};
 
     if (IPlane_Intersect_A) MyCode[0] = 1;
     if (IPlane_Intersect_B) MyCode[1] = 1;
@@ -1253,64 +1305,78 @@ void CSurfaceMovement::CheckFFDIntersections(CGeometry *geometry, CConfig *confi
 
 #else
 
-    Code[0] = MyCode[0]; Code[1] = MyCode[1]; Code[2] = MyCode[2];
-    Code[3] = MyCode[3]; Code[4] = MyCode[4]; Code[5] = MyCode[5];
+    Code[0] = MyCode[0];
+    Code[1] = MyCode[1];
+    Code[2] = MyCode[2];
+    Code[3] = MyCode[3];
+    Code[4] = MyCode[4];
+    Code[5] = MyCode[5];
 
 #endif
 
-    if (Code[0] != 0) IPlane_Intersect_A = true; else IPlane_Intersect_A = false;
-    if (Code[1] != 0) IPlane_Intersect_B = true; else IPlane_Intersect_B = false;
-    if (Code[2] != 0) JPlane_Intersect_A = true; else JPlane_Intersect_A = false;
-    if (Code[3] != 0) JPlane_Intersect_B = true; else JPlane_Intersect_B = false;
-    if (Code[4] != 0) KPlane_Intersect_A = true; else KPlane_Intersect_A = false;
-    if (Code[5] != 0) KPlane_Intersect_B = true; else KPlane_Intersect_B = false;
+    if (Code[0] != 0)
+      IPlane_Intersect_A = true;
+    else
+      IPlane_Intersect_A = false;
+    if (Code[1] != 0)
+      IPlane_Intersect_B = true;
+    else
+      IPlane_Intersect_B = false;
+    if (Code[2] != 0)
+      JPlane_Intersect_A = true;
+    else
+      JPlane_Intersect_A = false;
+    if (Code[3] != 0)
+      JPlane_Intersect_B = true;
+    else
+      JPlane_Intersect_B = false;
+    if (Code[4] != 0)
+      KPlane_Intersect_A = true;
+    else
+      KPlane_Intersect_A = false;
+    if (Code[5] != 0)
+      KPlane_Intersect_B = true;
+    else
+      KPlane_Intersect_B = false;
 
     /*--- Screen output ---*/
 
     if (rank == MASTER_NODE) {
-
-      if (IPlane_Intersect_A || IPlane_Intersect_B ||
-          JPlane_Intersect_A || JPlane_Intersect_B ||
-          KPlane_Intersect_A || KPlane_Intersect_B ) {
-
+      if (IPlane_Intersect_A || IPlane_Intersect_B || JPlane_Intersect_A || JPlane_Intersect_B || KPlane_Intersect_A ||
+          KPlane_Intersect_B) {
         cout << "The FFD planes ";
 
         if (cartesian) {
           if (IPlane_Intersect_A) cout << "i=0, ";
-          if (IPlane_Intersect_B) cout << "i="<< lDegree << ", ";
+          if (IPlane_Intersect_B) cout << "i=" << lDegree << ", ";
           if (JPlane_Intersect_A) cout << "j=0, ";
-          if (JPlane_Intersect_B) cout << "j="<< mDegree << ", ";
+          if (JPlane_Intersect_B) cout << "j=" << mDegree << ", ";
           if (KPlane_Intersect_A) cout << "k=0, ";
-          if (KPlane_Intersect_B) cout << "k="<< nDegree << ", ";
-        }
-        else if (cylindrical) {
+          if (KPlane_Intersect_B) cout << "k=" << nDegree << ", ";
+        } else if (cylindrical) {
           if (IPlane_Intersect_A) cout << "r=0, ";
-          if (IPlane_Intersect_B) cout << "r="<< lDegree << ", ";
+          if (IPlane_Intersect_B) cout << "r=" << lDegree << ", ";
           if (JPlane_Intersect_A) cout << "theta=0, ";
-          if (JPlane_Intersect_B) cout << "theta="<< mDegree << ", ";
+          if (JPlane_Intersect_B) cout << "theta=" << mDegree << ", ";
           if (KPlane_Intersect_A) cout << "z=0, ";
-          if (KPlane_Intersect_B) cout << "z="<< nDegree << ", ";
-        }
-        else if (spherical) {
+          if (KPlane_Intersect_B) cout << "z=" << nDegree << ", ";
+        } else if (spherical) {
           if (IPlane_Intersect_A) cout << "r=0, ";
-          if (IPlane_Intersect_B) cout << "r="<< lDegree << ", ";
+          if (IPlane_Intersect_B) cout << "r=" << lDegree << ", ";
           if (JPlane_Intersect_A) cout << "theta=0, ";
-          if (JPlane_Intersect_B) cout << "theta="<< mDegree << ", ";
+          if (JPlane_Intersect_B) cout << "theta=" << mDegree << ", ";
           if (KPlane_Intersect_A) cout << "phi=0, ";
-          if (KPlane_Intersect_B) cout << "phi="<< nDegree << ", ";
-        }
-        else if (polar) {
+          if (KPlane_Intersect_B) cout << "phi=" << nDegree << ", ";
+        } else if (polar) {
           if (IPlane_Intersect_A) cout << "r=0, ";
-          if (IPlane_Intersect_B) cout << "r="<< lDegree << ", ";
+          if (IPlane_Intersect_B) cout << "r=" << lDegree << ", ";
           if (KPlane_Intersect_A) cout << "theta=0, ";
-          if (KPlane_Intersect_B) cout << "theta="<< nDegree << ", ";
+          if (KPlane_Intersect_B) cout << "theta=" << nDegree << ", ";
         }
 
         cout << "intersect solid surfaces." << endl;
       }
-
     }
-
   }
 
   /*--- Fix the FFD planes based on the intersections with solid surfaces,
@@ -1318,8 +1384,7 @@ void CSurfaceMovement::CheckFFDIntersections(CGeometry *geometry, CConfig *confi
    that we are looking for ---*/
 
   if (config->GetFFD_Continuity() == USER_INPUT) {
-    if (rank == MASTER_NODE)
-      cout << "SU2 is fixing user's input planes." << endl;
+    if (rank == MASTER_NODE) cout << "SU2 is fixing user's input planes." << endl;
 
     for (index = 0; index < config->GetnFFD_Fix_IDir(); index++)
       if ((config->GetFFD_Fix_IDir(index) <= lDegree) && (config->GetFFD_Fix_IDir(index) >= 0))
@@ -1330,67 +1395,112 @@ void CSurfaceMovement::CheckFFDIntersections(CGeometry *geometry, CConfig *confi
     for (index = 0; index < config->GetnFFD_Fix_KDir(); index++)
       if ((config->GetFFD_Fix_KDir(index) <= nDegree) && (config->GetFFD_Fix_KDir(index) >= 0))
         FFDBox->Set_Fix_KPlane(config->GetFFD_Fix_KDir(index));
-
   }
 
   if (config->GetFFD_Continuity() == DERIVATIVE_NONE) {
-    if (rank == MASTER_NODE)
-      cout << "SU2 is fixing the planes to maintain a continuous surface." << endl;
-
-    if (IPlane_Intersect_A) { FFDBox->Set_Fix_IPlane(0); }
-    if (IPlane_Intersect_B) { FFDBox->Set_Fix_IPlane(lDegree); }
-    if (JPlane_Intersect_A) { FFDBox->Set_Fix_JPlane(0); }
-    if (JPlane_Intersect_B) { FFDBox->Set_Fix_JPlane(mDegree); }
-    if (KPlane_Intersect_A) { FFDBox->Set_Fix_KPlane(0); }
-    if (KPlane_Intersect_B) { FFDBox->Set_Fix_KPlane(nDegree); }
+    if (rank == MASTER_NODE) cout << "SU2 is fixing the planes to maintain a continuous surface." << endl;
 
+    if (IPlane_Intersect_A) {
+      FFDBox->Set_Fix_IPlane(0);
+    }
+    if (IPlane_Intersect_B) {
+      FFDBox->Set_Fix_IPlane(lDegree);
+    }
+    if (JPlane_Intersect_A) {
+      FFDBox->Set_Fix_JPlane(0);
+    }
+    if (JPlane_Intersect_B) {
+      FFDBox->Set_Fix_JPlane(mDegree);
+    }
+    if (KPlane_Intersect_A) {
+      FFDBox->Set_Fix_KPlane(0);
+    }
+    if (KPlane_Intersect_B) {
+      FFDBox->Set_Fix_KPlane(nDegree);
+    }
   }
 
   if (config->GetFFD_Continuity() == DERIVATIVE_1ST) {
-    if (rank == MASTER_NODE)
-      cout << "SU2 is fixing the planes to maintain a continuous 1st order derivative." << endl;
-
-    if (IPlane_Intersect_A) { FFDBox->Set_Fix_IPlane(0); FFDBox->Set_Fix_IPlane(1); }
-    if (IPlane_Intersect_B) { FFDBox->Set_Fix_IPlane(lDegree); FFDBox->Set_Fix_IPlane(lDegree-1); }
-    if (JPlane_Intersect_A) { FFDBox->Set_Fix_JPlane(0); FFDBox->Set_Fix_JPlane(1); }
-    if (JPlane_Intersect_B) { FFDBox->Set_Fix_JPlane(mDegree); FFDBox->Set_Fix_JPlane(mDegree-1); }
-    if (KPlane_Intersect_A) { FFDBox->Set_Fix_KPlane(0); FFDBox->Set_Fix_KPlane(1); }
-    if (KPlane_Intersect_B) { FFDBox->Set_Fix_KPlane(nDegree); FFDBox->Set_Fix_KPlane(nDegree-1); }
+    if (rank == MASTER_NODE) cout << "SU2 is fixing the planes to maintain a continuous 1st order derivative." << endl;
 
+    if (IPlane_Intersect_A) {
+      FFDBox->Set_Fix_IPlane(0);
+      FFDBox->Set_Fix_IPlane(1);
+    }
+    if (IPlane_Intersect_B) {
+      FFDBox->Set_Fix_IPlane(lDegree);
+      FFDBox->Set_Fix_IPlane(lDegree - 1);
+    }
+    if (JPlane_Intersect_A) {
+      FFDBox->Set_Fix_JPlane(0);
+      FFDBox->Set_Fix_JPlane(1);
+    }
+    if (JPlane_Intersect_B) {
+      FFDBox->Set_Fix_JPlane(mDegree);
+      FFDBox->Set_Fix_JPlane(mDegree - 1);
+    }
+    if (KPlane_Intersect_A) {
+      FFDBox->Set_Fix_KPlane(0);
+      FFDBox->Set_Fix_KPlane(1);
+    }
+    if (KPlane_Intersect_B) {
+      FFDBox->Set_Fix_KPlane(nDegree);
+      FFDBox->Set_Fix_KPlane(nDegree - 1);
+    }
   }
 
   if (config->GetFFD_Continuity() == DERIVATIVE_2ND) {
-    if (rank == MASTER_NODE)
-      cout << "SU2 is fixing the planes to maintain a continuous 2nd order derivative." << endl;
-
-    if ((IPlane_Intersect_A) && (lDegree > 1)) { FFDBox->Set_Fix_IPlane(0); FFDBox->Set_Fix_IPlane(1); FFDBox->Set_Fix_IPlane(2); }
-    if ((IPlane_Intersect_B) && (lDegree > 1)) { FFDBox->Set_Fix_IPlane(lDegree); FFDBox->Set_Fix_IPlane(lDegree-1); FFDBox->Set_Fix_IPlane(lDegree-2); }
-    if ((JPlane_Intersect_A) && (mDegree > 1)) { FFDBox->Set_Fix_JPlane(0); FFDBox->Set_Fix_JPlane(1); FFDBox->Set_Fix_JPlane(2); }
-    if ((JPlane_Intersect_B) && (mDegree > 1)) { FFDBox->Set_Fix_JPlane(mDegree); FFDBox->Set_Fix_JPlane(mDegree-1); FFDBox->Set_Fix_JPlane(mDegree-2); }
-    if ((KPlane_Intersect_A) && (nDegree > 1)) { FFDBox->Set_Fix_KPlane(0); FFDBox->Set_Fix_KPlane(1);FFDBox->Set_Fix_KPlane(2); }
-    if ((KPlane_Intersect_B) && (nDegree > 1)) { FFDBox->Set_Fix_KPlane(nDegree); FFDBox->Set_Fix_KPlane(nDegree-1); FFDBox->Set_Fix_KPlane(nDegree-2); }
+    if (rank == MASTER_NODE) cout << "SU2 is fixing the planes to maintain a continuous 2nd order derivative." << endl;
 
+    if ((IPlane_Intersect_A) && (lDegree > 1)) {
+      FFDBox->Set_Fix_IPlane(0);
+      FFDBox->Set_Fix_IPlane(1);
+      FFDBox->Set_Fix_IPlane(2);
+    }
+    if ((IPlane_Intersect_B) && (lDegree > 1)) {
+      FFDBox->Set_Fix_IPlane(lDegree);
+      FFDBox->Set_Fix_IPlane(lDegree - 1);
+      FFDBox->Set_Fix_IPlane(lDegree - 2);
+    }
+    if ((JPlane_Intersect_A) && (mDegree > 1)) {
+      FFDBox->Set_Fix_JPlane(0);
+      FFDBox->Set_Fix_JPlane(1);
+      FFDBox->Set_Fix_JPlane(2);
+    }
+    if ((JPlane_Intersect_B) && (mDegree > 1)) {
+      FFDBox->Set_Fix_JPlane(mDegree);
+      FFDBox->Set_Fix_JPlane(mDegree - 1);
+      FFDBox->Set_Fix_JPlane(mDegree - 2);
+    }
+    if ((KPlane_Intersect_A) && (nDegree > 1)) {
+      FFDBox->Set_Fix_KPlane(0);
+      FFDBox->Set_Fix_KPlane(1);
+      FFDBox->Set_Fix_KPlane(2);
+    }
+    if ((KPlane_Intersect_B) && (nDegree > 1)) {
+      FFDBox->Set_Fix_KPlane(nDegree);
+      FFDBox->Set_Fix_KPlane(nDegree - 1);
+      FFDBox->Set_Fix_KPlane(nDegree - 2);
+    }
   }
-
 }
 
-void CSurfaceMovement::UpdateParametricCoord(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, unsigned short iFFDBox) {
+void CSurfaceMovement::UpdateParametricCoord(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox,
+                                             unsigned short iFFDBox) {
   unsigned short iMarker, iDim;
   unsigned long iVertex, iPoint, iSurfacePoints;
-  su2double CartCoord[3] = {0.0,0.0,0.0}, *CartCoordNew, *CartCoordOld;
-  su2double *ParamCoord, *var_coord, ParamCoordGuess[3] = {0.0,0.0,0.0};
+  su2double CartCoord[3] = {0.0, 0.0, 0.0}, *CartCoordNew, *CartCoordOld;
+  su2double *ParamCoord, *var_coord, ParamCoordGuess[3] = {0.0, 0.0, 0.0};
   su2double MaxDiff, my_MaxDiff = 0.0, Diff;
 
   /*--- Recompute the parametric coordinates ---*/
 
   for (iSurfacePoints = 0; iSurfacePoints < FFDBox->GetnSurfacePoint(); iSurfacePoints++) {
-
     /*--- Get the marker of the surface point ---*/
 
     iMarker = FFDBox->Get_MarkerIndex(iSurfacePoints);
 
     if (config->GetMarker_All_DV(iMarker) == YES) {
-
       /*--- Get the vertex of the surface point ---*/
 
       iVertex = FFDBox->Get_VertexIndex(iSurfacePoints);
@@ -1406,13 +1516,14 @@ void CSurfaceMovement::UpdateParametricCoord(CGeometry *geometry, CConfig *confi
 
       var_coord = geometry->vertex[iMarker][iVertex]->GetVarCoord();
       CartCoordOld = geometry->nodes->GetCoord(iPoint);
-      for (iDim = 0; iDim < 3; iDim++)
-        CartCoord[iDim] = CartCoordOld[iDim] + var_coord[iDim];
+      for (iDim = 0; iDim < 3; iDim++) CartCoord[iDim] = CartCoordOld[iDim] + var_coord[iDim];
       FFDBox->Set_CartesianCoord(CartCoord, iSurfacePoints);
 
       /*--- Find the parametric coordinate using as ParamCoordGuess the previous value ---*/
 
-      ParamCoordGuess[0] = ParamCoord[0]; ParamCoordGuess[1] = ParamCoord[1]; ParamCoordGuess[2] = ParamCoord[2];
+      ParamCoordGuess[0] = ParamCoord[0];
+      ParamCoordGuess[1] = ParamCoord[1];
+      ParamCoordGuess[2] = ParamCoord[2];
       ParamCoord = FFDBox->GetParametricCoord_Iterative(iPoint, CartCoord, ParamCoordGuess, config);
 
       /*--- Set the new value of the parametric coordinates ---*/
@@ -1428,10 +1539,9 @@ void CSurfaceMovement::UpdateParametricCoord(CGeometry *geometry, CConfig *confi
 
       Diff = 0.0;
       for (iDim = 0; iDim < geometry->GetnDim(); iDim++)
-        Diff += (CartCoordNew[iDim]-CartCoord[iDim])*(CartCoordNew[iDim]-CartCoord[iDim]);
+        Diff += (CartCoordNew[iDim] - CartCoord[iDim]) * (CartCoordNew[iDim] - CartCoord[iDim]);
       Diff = sqrt(Diff);
       my_MaxDiff = max(my_MaxDiff, Diff);
-
     }
   }
 
@@ -1442,37 +1552,62 @@ void CSurfaceMovement::UpdateParametricCoord(CGeometry *geometry, CConfig *confi
 #endif
 
   if (rank == MASTER_NODE)
-    cout << "Update parametric coord       | FFD box: " << FFDBox->GetTag() << ". Max Diff: " << MaxDiff <<"."<< endl;
-
+    cout << "Update parametric coord       | FFD box: " << FFDBox->GetTag() << ". Max Diff: " << MaxDiff << "." << endl;
 }
 
-void CSurfaceMovement::ApplyDesignVariables(CGeometry *geometry, CConfig *config, CFreeFormDefBox **FFDBox, unsigned short iFFDBox) {
-
+void CSurfaceMovement::ApplyDesignVariables(CGeometry* geometry, CConfig* config, CFreeFormDefBox** FFDBox,
+                                            unsigned short iFFDBox) {
   unsigned short iDV;
 
   for (iDV = 0; iDV < config->GetnDV(); iDV++) {
-    switch ( config->GetDesign_Variable(iDV) ) {
-      case FFD_CONTROL_POINT_2D : SetFFDCPChange_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false); break;
-      case FFD_CAMBER_2D :        SetFFDCamber_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false); break;
-      case FFD_THICKNESS_2D :     SetFFDThickness_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false); break;
-      case FFD_TWIST_2D :         SetFFDTwist_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false); break;
-      case FFD_CONTROL_POINT :    SetFFDCPChange(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false); break;
-      case FFD_NACELLE :          SetFFDNacelle(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false); break;
-      case FFD_GULL :             SetFFDGull(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false); break;
-      case FFD_TWIST :            SetFFDTwist(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false); break;
-      case FFD_ROTATION :         SetFFDRotation(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false); break;
-      case FFD_CONTROL_SURFACE :  SetFFDControl_Surface(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false); break;
-      case FFD_CAMBER :           SetFFDCamber(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false); break;
-      case FFD_THICKNESS :        SetFFDThickness(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false); break;
-      case FFD_ANGLE_OF_ATTACK :  SetFFDAngleOfAttack(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false); break;
+    switch (config->GetDesign_Variable(iDV)) {
+      case FFD_CONTROL_POINT_2D:
+        SetFFDCPChange_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false);
+        break;
+      case FFD_CAMBER_2D:
+        SetFFDCamber_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false);
+        break;
+      case FFD_THICKNESS_2D:
+        SetFFDThickness_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false);
+        break;
+      case FFD_TWIST_2D:
+        SetFFDTwist_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false);
+        break;
+      case FFD_CONTROL_POINT:
+        SetFFDCPChange(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false);
+        break;
+      case FFD_NACELLE:
+        SetFFDNacelle(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false);
+        break;
+      case FFD_GULL:
+        SetFFDGull(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false);
+        break;
+      case FFD_TWIST:
+        SetFFDTwist(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false);
+        break;
+      case FFD_ROTATION:
+        SetFFDRotation(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false);
+        break;
+      case FFD_CONTROL_SURFACE:
+        SetFFDControl_Surface(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false);
+        break;
+      case FFD_CAMBER:
+        SetFFDCamber(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false);
+        break;
+      case FFD_THICKNESS:
+        SetFFDThickness(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false);
+        break;
+      case FFD_ANGLE_OF_ATTACK:
+        SetFFDAngleOfAttack(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false);
+        break;
     }
   }
 }
 
-su2double CSurfaceMovement::SetCartesianCoord(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, unsigned short iFFDBox, bool ResetDef) {
-
-  su2double *CartCoordNew, Diff, my_MaxDiff = 0.0, MaxDiff,
-  *ParamCoord, VarCoord[3] = {0.0, 0.0, 0.0}, CartCoordOld[3] = {0.0, 0.0, 0.0};
+su2double CSurfaceMovement::SetCartesianCoord(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox,
+                                              unsigned short iFFDBox, bool ResetDef) {
+  su2double *CartCoordNew, Diff, my_MaxDiff = 0.0, MaxDiff, *ParamCoord, VarCoord[3] = {0.0, 0.0, 0.0},
+                                 CartCoordOld[3] = {0.0, 0.0, 0.0};
   unsigned short iMarker, iDim;
   unsigned long iVertex, iPoint, iSurfacePoints;
 
@@ -1495,13 +1630,11 @@ su2double CSurfaceMovement::SetCartesianCoord(CGeometry *geometry, CConfig *conf
   /*--- Recompute the cartesians coordinates ---*/
 
   for (iSurfacePoints = 0; iSurfacePoints < FFDBox->GetnSurfacePoint(); iSurfacePoints++) {
-
     /*--- Get the marker of the surface point ---*/
 
     iMarker = FFDBox->Get_MarkerIndex(iSurfacePoints);
 
     if (config->GetMarker_All_DV(iMarker) == YES) {
-
       /*--- Get the vertex of the surface point ---*/
 
       iVertex = FFDBox->Get_VertexIndex(iSurfacePoints);
@@ -1523,28 +1656,32 @@ su2double CSurfaceMovement::SetCartesianCoord(CGeometry *geometry, CConfig *conf
       /*--- If polar coordinates, compute the cartesians from the polar value ---*/
 
       if (cylindrical) {
-
         su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
-        X_0 = config->GetFFD_Axis(0); Y_0 = config->GetFFD_Axis(1);  Z_0 = config->GetFFD_Axis(2);
+        X_0 = config->GetFFD_Axis(0);
+        Y_0 = config->GetFFD_Axis(1);
+        Z_0 = config->GetFFD_Axis(2);
 
         Xbar = CartCoordNew[2];
         Ybar = CartCoordNew[0] * cos(CartCoordNew[1]);
         Zbar = CartCoordNew[0] * sin(CartCoordNew[1]);
 
-        CartCoordNew[0] =  Xbar + X_0;  CartCoordNew[1] = Ybar + Y_0; CartCoordNew[2] = Zbar + Z_0;
-
-      }
-      else if (spherical || polar) {
+        CartCoordNew[0] = Xbar + X_0;
+        CartCoordNew[1] = Ybar + Y_0;
+        CartCoordNew[2] = Zbar + Z_0;
 
+      } else if (spherical || polar) {
         su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
-        X_0 = config->GetFFD_Axis(0); Y_0 = config->GetFFD_Axis(1);  Z_0 = config->GetFFD_Axis(2);
+        X_0 = config->GetFFD_Axis(0);
+        Y_0 = config->GetFFD_Axis(1);
+        Z_0 = config->GetFFD_Axis(2);
 
         Xbar = CartCoordNew[0] * cos(CartCoordNew[2]);
         Ybar = CartCoordNew[0] * cos(CartCoordNew[1]) * sin(CartCoordNew[2]);
         Zbar = CartCoordNew[0] * sin(CartCoordNew[1]) * sin(CartCoordNew[2]);
 
-        CartCoordNew[0] =  Xbar + X_0;  CartCoordNew[1] = Ybar + Y_0; CartCoordNew[2] = Zbar + Z_0;
-
+        CartCoordNew[0] = Xbar + X_0;
+        CartCoordNew[1] = Ybar + Y_0;
+        CartCoordNew[2] = Zbar + Z_0;
       }
 
       FFDBox->Set_CartesianCoord(CartCoordNew, iSurfacePoints);
@@ -1562,7 +1699,7 @@ su2double CSurfaceMovement::SetCartesianCoord(CGeometry *geometry, CConfig *conf
         VarCoord[iDim] = CartCoordNew[iDim] - CartCoordOld[iDim];
         if ((fabs(VarCoord[iDim]) <= EPS) && (config->GetDirectDiff() != D_DESIGN) && (!config->GetAD_Mode()))
           VarCoord[iDim] = 0.0;
-        Diff += (VarCoord[iDim]*VarCoord[iDim]);
+        Diff += (VarCoord[iDim] * VarCoord[iDim]);
       }
       Diff = sqrt(Diff);
 
@@ -1571,24 +1708,20 @@ su2double CSurfaceMovement::SetCartesianCoord(CGeometry *geometry, CConfig *conf
       /*--- Set the variation of the coordinates ---*/
 
       geometry->vertex[iMarker][iVertex]->SetVarCoord(VarCoord);
-
     }
   }
 
   SU2_MPI::Allreduce(&my_MaxDiff, &MaxDiff, 1, MPI_DOUBLE, MPI_MAX, SU2_MPI::GetComm());
 
   if (rank == MASTER_NODE)
-    cout << "Update cartesian coord        | FFD box: " << FFDBox->GetTag() << ". Max Diff: " << MaxDiff <<"."<< endl;
+    cout << "Update cartesian coord        | FFD box: " << FFDBox->GetTag() << ". Max Diff: " << MaxDiff << "." << endl;
 
   return MaxDiff;
-
 }
 
-
-bool CSurfaceMovement::SetFFDCPChange_2D(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox,
-    unsigned short iDV, bool ResetDef) const {
-
-  su2double movement[3] = {0.0,0.0,0.0}, Ampl;
+bool CSurfaceMovement::SetFFDCPChange_2D(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox,
+                                         CFreeFormDefBox** ResetFFDBox, unsigned short iDV, bool ResetDef) const {
+  su2double movement[3] = {0.0, 0.0, 0.0}, Ampl;
   unsigned short index[3], i, j, iFFDBox, iPlane;
   string design_FFDBox;
   su2double Scale = config->GetOpt_RelaxFactor();
@@ -1598,91 +1731,81 @@ bool CSurfaceMovement::SetFFDCPChange_2D(CGeometry *geometry, CConfig *config, C
    design variable is not in this box) ---*/
 
   if (ResetDef == true) {
-    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++)
-      ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
+    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
   }
 
   design_FFDBox = config->GetFFDTag(iDV);
 
   if (design_FFDBox.compare(FFDBox->GetTag()) == 0) {
-
     /*--- Compute deformation ---*/
 
     /*--- If we have only design value, than this value is the amplitude,
      * otherwise we have a general movement. ---*/
 
     if (config->GetnDV_Value(iDV) == 1) {
+      Ampl = config->GetDV_Value(iDV) * Scale;
 
-      Ampl = config->GetDV_Value(iDV)*Scale;
-
-      if (polar){
-        movement[0] = config->GetParamDV(iDV, 3)*Ampl;
+      if (polar) {
+        movement[0] = config->GetParamDV(iDV, 3) * Ampl;
         movement[1] = 0.0;
-        movement[2] = config->GetParamDV(iDV, 4)*Ampl;
-      }
-      else {
-        movement[0] = config->GetParamDV(iDV, 3)*Ampl;
-        movement[1] = config->GetParamDV(iDV, 4)*Ampl;
+        movement[2] = config->GetParamDV(iDV, 4) * Ampl;
+      } else {
+        movement[0] = config->GetParamDV(iDV, 3) * Ampl;
+        movement[1] = config->GetParamDV(iDV, 4) * Ampl;
         movement[2] = 0.0;
       }
 
     } else {
-      if (polar){
+      if (polar) {
         movement[0] = config->GetDV_Value(iDV, 0);
         movement[1] = 0.0;
         movement[2] = config->GetDV_Value(iDV, 1);
+      } else {
+        movement[0] = config->GetDV_Value(iDV, 0);
+        movement[1] = config->GetDV_Value(iDV, 1);
+        movement[2] = 0.0;
       }
-      else {
-      movement[0] = config->GetDV_Value(iDV, 0);
-      movement[1] = config->GetDV_Value(iDV, 1);
-      movement[2] = 0.0;
-      }
-
     }
 
-    if (polar){
-       index[0] = SU2_TYPE::Int(config->GetParamDV(iDV, 1));
-       index[1] = 0;
+    if (polar) {
+      index[0] = SU2_TYPE::Int(config->GetParamDV(iDV, 1));
+      index[1] = 0;
       index[2] = SU2_TYPE::Int(config->GetParamDV(iDV, 2));
-    }
-    else {
-       index[0] = SU2_TYPE::Int(config->GetParamDV(iDV, 1));
-       index[1] = SU2_TYPE::Int(config->GetParamDV(iDV, 2));
+    } else {
+      index[0] = SU2_TYPE::Int(config->GetParamDV(iDV, 1));
+      index[1] = SU2_TYPE::Int(config->GetParamDV(iDV, 2));
       index[2] = 0;
     }
 
     /*--- Check that it is possible to move the control point ---*/
 
-    for (iPlane = 0 ; iPlane < FFDBox->Get_nFix_IPlane(); iPlane++) {
+    for (iPlane = 0; iPlane < FFDBox->Get_nFix_IPlane(); iPlane++) {
       if (index[0] == FFDBox->Get_Fix_IPlane(iPlane)) return false;
     }
 
-    for (iPlane = 0 ; iPlane < FFDBox->Get_nFix_JPlane(); iPlane++) {
+    for (iPlane = 0; iPlane < FFDBox->Get_nFix_JPlane(); iPlane++) {
       if (index[1] == FFDBox->Get_Fix_JPlane(iPlane)) return false;
     }
 
-    for (iPlane = 0 ; iPlane < FFDBox->Get_nFix_KPlane(); iPlane++) {
+    for (iPlane = 0; iPlane < FFDBox->Get_nFix_KPlane(); iPlane++) {
       if (index[2] == FFDBox->Get_Fix_KPlane(iPlane)) return false;
     }
 
-    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) == -1) &&
-        (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1)) {
+    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) == -1) && (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1)) {
       for (i = 0; i < FFDBox->GetlOrder(); i++) {
         index[0] = i;
         FFDBox->SetControlPoints(index, movement);
       }
     }
 
-    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) &&
-        (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) == -1)) {
+    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) && (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) == -1)) {
       for (j = 0; j < FFDBox->GetmOrder(); j++) {
         index[1] = j;
         FFDBox->SetControlPoints(index, movement);
       }
     }
 
-    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) == -1) &&
-        (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) == -1)) {
+    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) == -1) && (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) == -1)) {
       for (i = 0; i < FFDBox->GetlOrder(); i++) {
         index[0] = i;
         for (j = 0; j < FFDBox->GetmOrder(); j++) {
@@ -1691,35 +1814,32 @@ bool CSurfaceMovement::SetFFDCPChange_2D(CGeometry *geometry, CConfig *config, C
         }
       }
     }
-    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) &&
-        (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1)) {
-
+    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) && (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1)) {
       FFDBox->SetControlPoints(index, movement);
     }
 
     /*--- Upper surface ---*/
 
-    if (polar) index[1] = 1;
-    else index[2] = 1;
+    if (polar)
+      index[1] = 1;
+    else
+      index[2] = 1;
 
-    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) == -1) &&
-        (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1)) {
+    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) == -1) && (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1)) {
       for (i = 0; i < FFDBox->GetlOrder(); i++) {
         index[0] = i;
         FFDBox->SetControlPoints(index, movement);
       }
     }
 
-    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) &&
-        (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) == -1)) {
+    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) && (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) == -1)) {
       for (j = 0; j < FFDBox->GetmOrder(); j++) {
         index[1] = j;
         FFDBox->SetControlPoints(index, movement);
       }
     }
 
-    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) == -1) &&
-        (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) == -1)) {
+    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) == -1) && (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) == -1)) {
       for (i = 0; i < FFDBox->GetlOrder(); i++) {
         index[0] = i;
         for (j = 0; j < FFDBox->GetmOrder(); j++) {
@@ -1728,24 +1848,19 @@ bool CSurfaceMovement::SetFFDCPChange_2D(CGeometry *geometry, CConfig *config, C
         }
       }
     }
-    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) &&
-        (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1)) {
-
+    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) && (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1)) {
       FFDBox->SetControlPoints(index, movement);
     }
-  }
-  else {
+  } else {
     return false;
   }
 
   return true;
-
 }
 
-bool CSurfaceMovement::SetFFDCPChange(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox,
-                                      unsigned short iDV, bool ResetDef) const {
-
-  su2double movement[3] = {0.0,0.0,0.0}, Ampl;
+bool CSurfaceMovement::SetFFDCPChange(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox,
+                                      CFreeFormDefBox** ResetFFDBox, unsigned short iDV, bool ResetDef) const {
+  su2double movement[3] = {0.0, 0.0, 0.0}, Ampl;
   unsigned short index[3], i, j, k, iPlane, iFFDBox;
   bool CheckIndex;
   string design_FFDBox;
@@ -1756,33 +1871,28 @@ bool CSurfaceMovement::SetFFDCPChange(CGeometry *geometry, CConfig *config, CFre
 
   if (ResetDef == true) {
     FFDBox->SetOriginalControlPoints();
-    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++)
-      ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
+    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
   }
 
   design_FFDBox = config->GetFFDTag(iDV);
 
   if (design_FFDBox.compare(FFDBox->GetTag()) == 0) {
-
     /*--- Compute deformation ---*/
 
     /*--- If we have only design value, than this value is the amplitude,
      * otherwise we have a general movement. ---*/
 
     if (config->GetnDV_Value(iDV) == 1) {
+      Ampl = config->GetDV_Value(iDV) * Scale;
 
-      Ampl = config->GetDV_Value(iDV)*Scale;
-
-      movement[0] = config->GetParamDV(iDV, 4)*Ampl;
-      movement[1] = config->GetParamDV(iDV, 5)*Ampl;
-      movement[2] = config->GetParamDV(iDV, 6)*Ampl;
+      movement[0] = config->GetParamDV(iDV, 4) * Ampl;
+      movement[1] = config->GetParamDV(iDV, 5) * Ampl;
+      movement[2] = config->GetParamDV(iDV, 6) * Ampl;
 
     } else {
-
       movement[0] = config->GetDV_Value(iDV, 0);
       movement[1] = config->GetDV_Value(iDV, 1);
       movement[2] = config->GetDV_Value(iDV, 2);
-
     }
 
     index[0] = SU2_TYPE::Int(config->GetParamDV(iDV, 1));
@@ -1791,68 +1901,61 @@ bool CSurfaceMovement::SetFFDCPChange(CGeometry *geometry, CConfig *config, CFre
 
     /*--- Check that it is possible to move the control point ---*/
 
-    for (iPlane = 0 ; iPlane < FFDBox->Get_nFix_IPlane(); iPlane++) {
+    for (iPlane = 0; iPlane < FFDBox->Get_nFix_IPlane(); iPlane++) {
       if (index[0] == FFDBox->Get_Fix_IPlane(iPlane)) return false;
     }
 
-    for (iPlane = 0 ; iPlane < FFDBox->Get_nFix_JPlane(); iPlane++) {
+    for (iPlane = 0; iPlane < FFDBox->Get_nFix_JPlane(); iPlane++) {
       if (index[1] == FFDBox->Get_Fix_JPlane(iPlane)) return false;
     }
 
-    for (iPlane = 0 ; iPlane < FFDBox->Get_nFix_KPlane(); iPlane++) {
+    for (iPlane = 0; iPlane < FFDBox->Get_nFix_KPlane(); iPlane++) {
       if (index[2] == FFDBox->Get_Fix_KPlane(iPlane)) return false;
     }
 
-    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) == -1) &&
-        (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1) &&
+    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) == -1) && (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1) &&
         (SU2_TYPE::Int(config->GetParamDV(iDV, 3)) != -1)) {
       for (i = 0; i < FFDBox->GetlOrder(); i++) {
         index[0] = i;
 
         CheckIndex = true;
-        for (iPlane = 0 ; iPlane < FFDBox->Get_nFix_IPlane(); iPlane++) {
+        for (iPlane = 0; iPlane < FFDBox->Get_nFix_IPlane(); iPlane++) {
           if (index[0] == FFDBox->Get_Fix_IPlane(iPlane)) CheckIndex = false;
         }
 
         if (CheckIndex) FFDBox->SetControlPoints(index, movement);
-
       }
     }
 
-    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) &&
-        (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) == -1) &&
+    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) && (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) == -1) &&
         (SU2_TYPE::Int(config->GetParamDV(iDV, 3)) != -1)) {
       for (j = 0; j < FFDBox->GetmOrder(); j++) {
         index[1] = j;
 
         CheckIndex = true;
-        for (iPlane = 0 ; iPlane < FFDBox->Get_nFix_JPlane(); iPlane++) {
+        for (iPlane = 0; iPlane < FFDBox->Get_nFix_JPlane(); iPlane++) {
           if (index[1] == FFDBox->Get_Fix_JPlane(iPlane)) CheckIndex = false;
         }
 
         if (CheckIndex) FFDBox->SetControlPoints(index, movement);
-
       }
     }
 
-    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) &&
-        (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1) &&
+    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) && (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1) &&
         (SU2_TYPE::Int(config->GetParamDV(iDV, 3)) == -1)) {
       for (k = 0; k < FFDBox->GetnOrder(); k++) {
         index[2] = k;
 
         CheckIndex = true;
-        for (iPlane = 0 ; iPlane < FFDBox->Get_nFix_KPlane(); iPlane++) {
+        for (iPlane = 0; iPlane < FFDBox->Get_nFix_KPlane(); iPlane++) {
           if (index[2] == FFDBox->Get_Fix_KPlane(iPlane)) CheckIndex = false;
         }
 
         if (CheckIndex) FFDBox->SetControlPoints(index, movement);
-
       }
     }
 
-    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) == -1) &&
-        (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) == -1) &&
+    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) == -1) && (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) == -1) &&
         (SU2_TYPE::Int(config->GetParamDV(iDV, 3)) != -1)) {
       for (i = 0; i < FFDBox->GetlOrder(); i++) {
         index[0] = i;
@@ -1863,8 +1966,7 @@ bool CSurfaceMovement::SetFFDCPChange(CGeometry *geometry, CConfig *config, CFre
       }
     }
 
-    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) &&
-        (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) == -1) &&
+    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) && (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) == -1) &&
         (SU2_TYPE::Int(config->GetParamDV(iDV, 3)) == -1)) {
       for (j = 0; j < FFDBox->GetmOrder(); j++) {
         index[1] = j;
@@ -1875,8 +1977,7 @@ bool CSurfaceMovement::SetFFDCPChange(CGeometry *geometry, CConfig *config, CFre
       }
     }
 
-    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) == -1) &&
-        (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1) &&
+    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) == -1) && (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1) &&
         (SU2_TYPE::Int(config->GetParamDV(iDV, 3)) == -1)) {
       for (i = 0; i < FFDBox->GetlOrder(); i++) {
         index[0] = i;
@@ -1887,25 +1988,21 @@ bool CSurfaceMovement::SetFFDCPChange(CGeometry *geometry, CConfig *config, CFre
       }
     }
 
-    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) &&
-        (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1) &&
+    if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) && (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1) &&
         (SU2_TYPE::Int(config->GetParamDV(iDV, 3)) != -1)) {
       FFDBox->SetControlPoints(index, movement);
     }
 
-  }
-  else {
+  } else {
     return false;
   }
 
   return true;
-
 }
 
-bool CSurfaceMovement::SetFFDGull(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox,
-                                  unsigned short iDV, bool ResetDef) const {
-
-  su2double movement[3] = {0.0,0.0,0.0}, Ampl;
+bool CSurfaceMovement::SetFFDGull(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox,
+                                  CFreeFormDefBox** ResetFFDBox, unsigned short iDV, bool ResetDef) const {
+  su2double movement[3] = {0.0, 0.0, 0.0}, Ampl;
   unsigned short index[3], i, k, iPlane, iFFDBox;
   string design_FFDBox;
   su2double Scale = config->GetOpt_RelaxFactor();
@@ -1915,17 +2012,15 @@ bool CSurfaceMovement::SetFFDGull(CGeometry *geometry, CConfig *config, CFreeFor
 
   if (ResetDef == true) {
     FFDBox->SetOriginalControlPoints();
-    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++)
-      ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
+    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
   }
 
   design_FFDBox = config->GetFFDTag(iDV);
 
   if (design_FFDBox.compare(FFDBox->GetTag()) == 0) {
-
     /*--- Compute deformation ---*/
 
-    Ampl = config->GetDV_Value(iDV)*Scale;
+    Ampl = config->GetDV_Value(iDV) * Scale;
 
     movement[0] = 0.0;
     movement[1] = 0.0;
@@ -1937,7 +2032,7 @@ bool CSurfaceMovement::SetFFDGull(CGeometry *geometry, CConfig *config, CFreeFor
 
     /*--- Check that it is possible to move the control point ---*/
 
-    for (iPlane = 0 ; iPlane < FFDBox->Get_nFix_JPlane(); iPlane++) {
+    for (iPlane = 0; iPlane < FFDBox->Get_nFix_JPlane(); iPlane++) {
       if (index[1] == FFDBox->Get_Fix_JPlane(iPlane)) return false;
     }
 
@@ -1949,19 +2044,16 @@ bool CSurfaceMovement::SetFFDGull(CGeometry *geometry, CConfig *config, CFreeFor
       }
     }
 
-  }
-  else {
+  } else {
     return false;
   }
 
   return true;
-
 }
 
-bool CSurfaceMovement::SetFFDNacelle(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox,
-                                     unsigned short iDV, bool ResetDef) const {
-
-  su2double movement[3] = {0.0,0.0,0.0}, Ampl;
+bool CSurfaceMovement::SetFFDNacelle(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox,
+                                     CFreeFormDefBox** ResetFFDBox, unsigned short iDV, bool ResetDef) const {
+  su2double movement[3] = {0.0, 0.0, 0.0}, Ampl;
   unsigned short index[3], i, j, k, iPlane, iFFDBox, Theta, ThetaMax;
   string design_FFDBox;
   bool SameCP = false;
@@ -1972,50 +2064,46 @@ bool CSurfaceMovement::SetFFDNacelle(CGeometry *geometry, CConfig *config, CFree
 
   if (ResetDef == true) {
     FFDBox->SetOriginalControlPoints();
-    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++)
-      ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
+    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
   }
 
   design_FFDBox = config->GetFFDTag(iDV);
 
   if (design_FFDBox.compare(FFDBox->GetTag()) == 0) {
-
     /*--- Compute deformation ---*/
 
-    Ampl = config->GetDV_Value(iDV)*Scale;
+    Ampl = config->GetDV_Value(iDV) * Scale;
 
-    movement[0] = config->GetParamDV(iDV, 4)*Ampl;
+    movement[0] = config->GetParamDV(iDV, 4) * Ampl;
     movement[1] = 0.0;
-    movement[2] = config->GetParamDV(iDV, 5)*Ampl;
+    movement[2] = config->GetParamDV(iDV, 5) * Ampl;
 
     index[0] = SU2_TYPE::Int(config->GetParamDV(iDV, 1));
     index[1] = SU2_TYPE::Int(config->GetParamDV(iDV, 2));
     index[2] = SU2_TYPE::Int(config->GetParamDV(iDV, 3));
-    if (index[1] == SU2_TYPE::Int(FFDBox->GetmOrder()) - index[1] -1) SameCP = true;
+    if (index[1] == SU2_TYPE::Int(FFDBox->GetmOrder()) - index[1] - 1) SameCP = true;
 
     ThetaMax = 2;
     if (SameCP) ThetaMax = 1;
 
     for (Theta = 0; Theta < ThetaMax; Theta++) {
-
-      if (Theta == 1) index[1] = SU2_TYPE::Int(FFDBox->GetmOrder()) - index[1] -1;
+      if (Theta == 1) index[1] = SU2_TYPE::Int(FFDBox->GetmOrder()) - index[1] - 1;
 
       /*--- Check that it is possible to move the control point ---*/
 
-      for (iPlane = 0 ; iPlane < FFDBox->Get_nFix_IPlane(); iPlane++) {
+      for (iPlane = 0; iPlane < FFDBox->Get_nFix_IPlane(); iPlane++) {
         if (index[0] == FFDBox->Get_Fix_IPlane(iPlane)) return false;
       }
 
-      for (iPlane = 0 ; iPlane < FFDBox->Get_nFix_JPlane(); iPlane++) {
+      for (iPlane = 0; iPlane < FFDBox->Get_nFix_JPlane(); iPlane++) {
         if (index[1] == FFDBox->Get_Fix_JPlane(iPlane)) return false;
       }
 
-      for (iPlane = 0 ; iPlane < FFDBox->Get_nFix_KPlane(); iPlane++) {
+      for (iPlane = 0; iPlane < FFDBox->Get_nFix_KPlane(); iPlane++) {
         if (index[2] == FFDBox->Get_Fix_KPlane(iPlane)) return false;
       }
 
-      if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) == -1) &&
-          (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1) &&
+      if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) == -1) && (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1) &&
           (SU2_TYPE::Int(config->GetParamDV(iDV, 3)) != -1)) {
         for (i = 0; i < FFDBox->GetlOrder(); i++) {
           index[0] = i;
@@ -2023,8 +2111,7 @@ bool CSurfaceMovement::SetFFDNacelle(CGeometry *geometry, CConfig *config, CFree
         }
       }
 
-      if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) &&
-          (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) == -1) &&
+      if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) && (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) == -1) &&
           (SU2_TYPE::Int(config->GetParamDV(iDV, 3)) != -1)) {
         for (j = 0; j < FFDBox->GetmOrder(); j++) {
           index[1] = j;
@@ -2032,8 +2119,7 @@ bool CSurfaceMovement::SetFFDNacelle(CGeometry *geometry, CConfig *config, CFree
         }
       }
 
-      if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) &&
-          (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1) &&
+      if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) && (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1) &&
           (SU2_TYPE::Int(config->GetParamDV(iDV, 3)) == -1)) {
         for (k = 0; k < FFDBox->GetnOrder(); k++) {
           index[2] = k;
@@ -2041,8 +2127,7 @@ bool CSurfaceMovement::SetFFDNacelle(CGeometry *geometry, CConfig *config, CFree
         }
       }
 
-      if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) == -1) &&
-          (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) == -1) &&
+      if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) == -1) && (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) == -1) &&
           (SU2_TYPE::Int(config->GetParamDV(iDV, 3)) != -1)) {
         for (i = 0; i < FFDBox->GetlOrder(); i++) {
           index[0] = i;
@@ -2053,8 +2138,7 @@ bool CSurfaceMovement::SetFFDNacelle(CGeometry *geometry, CConfig *config, CFree
         }
       }
 
-      if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) &&
-          (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) == -1) &&
+      if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) && (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) == -1) &&
           (SU2_TYPE::Int(config->GetParamDV(iDV, 3)) == -1)) {
         for (j = 0; j < FFDBox->GetmOrder(); j++) {
           index[1] = j;
@@ -2065,8 +2149,7 @@ bool CSurfaceMovement::SetFFDNacelle(CGeometry *geometry, CConfig *config, CFree
         }
       }
 
-      if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) == -1) &&
-          (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1) &&
+      if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) == -1) && (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1) &&
           (SU2_TYPE::Int(config->GetParamDV(iDV, 3)) == -1)) {
         for (i = 0; i < FFDBox->GetlOrder(); i++) {
           index[0] = i;
@@ -2077,26 +2160,22 @@ bool CSurfaceMovement::SetFFDNacelle(CGeometry *geometry, CConfig *config, CFree
         }
       }
 
-      if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) &&
-          (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1) &&
+      if ((SU2_TYPE::Int(config->GetParamDV(iDV, 1)) != -1) && (SU2_TYPE::Int(config->GetParamDV(iDV, 2)) != -1) &&
           (SU2_TYPE::Int(config->GetParamDV(iDV, 3)) != -1)) {
         FFDBox->SetControlPoints(index, movement);
       }
     }
 
-  }
-  else {
+  } else {
     return false;
   }
 
   return true;
-
 }
 
-bool CSurfaceMovement::SetFFDCamber_2D(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox,
-                                       unsigned short iDV, bool ResetDef) const {
-
-  su2double Ampl, movement[3] = {0.0,0.0,0.0};
+bool CSurfaceMovement::SetFFDCamber_2D(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox,
+                                       CFreeFormDefBox** ResetFFDBox, unsigned short iDV, bool ResetDef) const {
+  su2double Ampl, movement[3] = {0.0, 0.0, 0.0};
   unsigned short index[3], kIndex, iFFDBox;
   string design_FFDBox;
   su2double Scale = config->GetOpt_RelaxFactor();
@@ -2105,44 +2184,41 @@ bool CSurfaceMovement::SetFFDCamber_2D(CGeometry *geometry, CConfig *config, CFr
    design variable is not in this box) ---*/
 
   if (ResetDef == true) {
-    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++)
-      ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
+    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
   }
 
   design_FFDBox = config->GetFFDTag(iDV);
 
   if (design_FFDBox.compare(FFDBox->GetTag()) == 0) {
-
     for (kIndex = 0; kIndex < 2; kIndex++) {
-
-      Ampl = config->GetDV_Value(iDV)*Scale;
+      Ampl = config->GetDV_Value(iDV) * Scale;
 
       movement[0] = 0.0;
-      if (kIndex == 0) movement[1] = Ampl;
-      else movement[1] = Ampl;
+      if (kIndex == 0)
+        movement[1] = Ampl;
+      else
+        movement[1] = Ampl;
       movement[2] = 0.0;
 
-      index[0] = SU2_TYPE::Int(config->GetParamDV(iDV, 1)); index[1] = kIndex; index[2] = 0;
+      index[0] = SU2_TYPE::Int(config->GetParamDV(iDV, 1));
+      index[1] = kIndex;
+      index[2] = 0;
       FFDBox->SetControlPoints(index, movement);
 
       index[2] = 1;
       FFDBox->SetControlPoints(index, movement);
-
     }
 
-  }
-  else {
+  } else {
     return false;
   }
 
   return true;
-
 }
 
-bool CSurfaceMovement::SetFFDThickness_2D(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox,
-                                          unsigned short iDV, bool ResetDef) const {
-
-  su2double Ampl, movement[3]= {0.0,0.0,0.0};
+bool CSurfaceMovement::SetFFDThickness_2D(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox,
+                                          CFreeFormDefBox** ResetFFDBox, unsigned short iDV, bool ResetDef) const {
+  su2double Ampl, movement[3] = {0.0, 0.0, 0.0};
   unsigned short index[3], kIndex, iFFDBox;
   string design_FFDBox;
   su2double Scale = config->GetOpt_RelaxFactor();
@@ -2151,51 +2227,46 @@ bool CSurfaceMovement::SetFFDThickness_2D(CGeometry *geometry, CConfig *config,
    design variable is not in this box) ---*/
 
   if (ResetDef == true) {
-    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++)
-      ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
+    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
   }
 
   design_FFDBox = config->GetFFDTag(iDV);
 
   if (design_FFDBox.compare(FFDBox->GetTag()) == 0) {
-
     for (kIndex = 0; kIndex < 2; kIndex++) {
-
-      Ampl = config->GetDV_Value(iDV)*Scale;
+      Ampl = config->GetDV_Value(iDV) * Scale;
 
       movement[0] = 0.0;
-      if (kIndex == 0) movement[1] = -Ampl;
-      else movement[1] = Ampl;
+      if (kIndex == 0)
+        movement[1] = -Ampl;
+      else
+        movement[1] = Ampl;
       movement[2] = 0.0;
 
-      index[0] = SU2_TYPE::Int(config->GetParamDV(iDV, 1)); index[1] = kIndex; index[2] = 0;
+      index[0] = SU2_TYPE::Int(config->GetParamDV(iDV, 1));
+      index[1] = kIndex;
+      index[2] = 0;
       FFDBox->SetControlPoints(index, movement);
 
       index[2] = 1;
       FFDBox->SetControlPoints(index, movement);
-
     }
 
-  }
-  else {
+  } else {
     return false;
   }
 
   return true;
-
 }
 
-bool CSurfaceMovement::SetFFDTwist_2D(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox,
-                                      unsigned short iDV, bool ResetDef) {
-
+bool CSurfaceMovement::SetFFDTwist_2D(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox,
+                                      CFreeFormDefBox** ResetFFDBox, unsigned short iDV, bool ResetDef) {
   return true;
-
 }
 
-bool CSurfaceMovement::SetFFDCamber(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox,
-                                    unsigned short iDV, bool ResetDef) const {
-
-  su2double Ampl, movement[3] = {0.0,0.0,0.0};
+bool CSurfaceMovement::SetFFDCamber(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox,
+                                    CFreeFormDefBox** ResetFFDBox, unsigned short iDV, bool ResetDef) const {
+  su2double Ampl, movement[3] = {0.0, 0.0, 0.0};
   unsigned short index[3], kIndex, iPlane, iFFDBox;
   string design_FFDBox;
   su2double Scale = config->GetOpt_RelaxFactor();
@@ -2204,76 +2275,68 @@ bool CSurfaceMovement::SetFFDCamber(CGeometry *geometry, CConfig *config, CFreeF
    design variable is not in this box) ---*/
 
   if (ResetDef == true) {
-    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++)
-      ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
+    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
   }
 
   design_FFDBox = config->GetFFDTag(iDV);
 
   if (design_FFDBox.compare(FFDBox->GetTag()) == 0) {
-
     /*--- Check that it is possible to move the control point ---*/
 
     for (kIndex = 0; kIndex < 2; kIndex++) {
-
       index[0] = SU2_TYPE::Int(config->GetParamDV(iDV, 1));
       index[1] = SU2_TYPE::Int(config->GetParamDV(iDV, 2));
       index[2] = kIndex;
 
-      for (iPlane = 0 ; iPlane < FFDBox->Get_nFix_IPlane(); iPlane++) {
+      for (iPlane = 0; iPlane < FFDBox->Get_nFix_IPlane(); iPlane++) {
         if (index[0] == FFDBox->Get_Fix_IPlane(iPlane)) return false;
       }
 
-      for (iPlane = 0 ; iPlane < FFDBox->Get_nFix_JPlane(); iPlane++) {
+      for (iPlane = 0; iPlane < FFDBox->Get_nFix_JPlane(); iPlane++) {
         if (index[1] == FFDBox->Get_Fix_JPlane(iPlane)) return false;
       }
 
-      for (iPlane = 0 ; iPlane < FFDBox->Get_nFix_KPlane(); iPlane++) {
+      for (iPlane = 0; iPlane < FFDBox->Get_nFix_KPlane(); iPlane++) {
         if (index[2] == FFDBox->Get_Fix_KPlane(iPlane)) return false;
       }
-
     }
 
     for (kIndex = 0; kIndex < 2; kIndex++) {
-
-      Ampl = config->GetDV_Value(iDV)*Scale;
+      Ampl = config->GetDV_Value(iDV) * Scale;
 
       index[0] = SU2_TYPE::Int(config->GetParamDV(iDV, 1));
       index[1] = SU2_TYPE::Int(config->GetParamDV(iDV, 2));
       index[2] = kIndex;
 
-      movement[0] = 0.0; movement[1] = 0.0;
-      if (kIndex == 0) movement[2] = Ampl;
-      else movement[2] = Ampl;
+      movement[0] = 0.0;
+      movement[1] = 0.0;
+      if (kIndex == 0)
+        movement[2] = Ampl;
+      else
+        movement[2] = Ampl;
 
       FFDBox->SetControlPoints(index, movement);
-
     }
 
-  }
-  else {
+  } else {
     return false;
   }
 
   return true;
-
 }
 
-void CSurfaceMovement::SetFFDAngleOfAttack(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox,
-                                           unsigned short iDV, bool ResetDef) {
-
+void CSurfaceMovement::SetFFDAngleOfAttack(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox,
+                                           CFreeFormDefBox** ResetFFDBox, unsigned short iDV, bool ResetDef) {
   su2double Scale = config->GetOpt_RelaxFactor();
 
-  su2double Ampl = config->GetDV_Value(iDV)*Scale;
+  su2double Ampl = config->GetDV_Value(iDV) * Scale;
 
   config->SetAoA_Offset(Ampl);
-
 }
 
-bool CSurfaceMovement::SetFFDThickness(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox,
-                                       unsigned short iDV, bool ResetDef) const {
-
-  su2double Ampl, movement[3] = {0.0,0.0,0.0};
+bool CSurfaceMovement::SetFFDThickness(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox,
+                                       CFreeFormDefBox** ResetFFDBox, unsigned short iDV, bool ResetDef) const {
+  su2double Ampl, movement[3] = {0.0, 0.0, 0.0};
   unsigned short index[3], kIndex, iPlane, iFFDBox;
   string design_FFDBox;
   su2double Scale = config->GetOpt_RelaxFactor();
@@ -2282,68 +2345,61 @@ bool CSurfaceMovement::SetFFDThickness(CGeometry *geometry, CConfig *config, CFr
    design variable is not in this box) ---*/
 
   if (ResetDef == true) {
-    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++)
-      ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
+    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
   }
 
   design_FFDBox = config->GetFFDTag(iDV);
 
   if (design_FFDBox.compare(FFDBox->GetTag()) == 0) {
-
     /*--- Check that it is possible to move the control point ---*/
 
     for (kIndex = 0; kIndex < 2; kIndex++) {
-
       index[0] = SU2_TYPE::Int(config->GetParamDV(iDV, 1));
       index[1] = SU2_TYPE::Int(config->GetParamDV(iDV, 2));
       index[2] = kIndex;
 
-      for (iPlane = 0 ; iPlane < FFDBox->Get_nFix_IPlane(); iPlane++) {
+      for (iPlane = 0; iPlane < FFDBox->Get_nFix_IPlane(); iPlane++) {
         if (index[0] == FFDBox->Get_Fix_IPlane(iPlane)) return false;
       }
 
-      for (iPlane = 0 ; iPlane < FFDBox->Get_nFix_JPlane(); iPlane++) {
+      for (iPlane = 0; iPlane < FFDBox->Get_nFix_JPlane(); iPlane++) {
         if (index[1] == FFDBox->Get_Fix_JPlane(iPlane)) return false;
       }
 
-      for (iPlane = 0 ; iPlane < FFDBox->Get_nFix_KPlane(); iPlane++) {
+      for (iPlane = 0; iPlane < FFDBox->Get_nFix_KPlane(); iPlane++) {
         if (index[2] == FFDBox->Get_Fix_KPlane(iPlane)) return false;
       }
-
     }
 
-
     for (kIndex = 0; kIndex < 2; kIndex++) {
-
-      Ampl = config->GetDV_Value(iDV)*Scale;
+      Ampl = config->GetDV_Value(iDV) * Scale;
 
       index[0] = SU2_TYPE::Int(config->GetParamDV(iDV, 1));
       index[1] = SU2_TYPE::Int(config->GetParamDV(iDV, 2));
       index[2] = kIndex;
 
-      movement[0] = 0.0; movement[1] = 0.0;
-      if (kIndex == 0) movement[2] = -Ampl;
-      else movement[2] = Ampl;
+      movement[0] = 0.0;
+      movement[1] = 0.0;
+      if (kIndex == 0)
+        movement[2] = -Ampl;
+      else
+        movement[2] = Ampl;
 
       FFDBox->SetControlPoints(index, movement);
-
     }
 
-  }
-  else {
+  } else {
     return false;
   }
 
   return true;
-
 }
 
-bool CSurfaceMovement::SetFFDTwist(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox,
-                                   unsigned short iDV, bool ResetDef) const {
-
+bool CSurfaceMovement::SetFFDTwist(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox,
+                                   CFreeFormDefBox** ResetFFDBox, unsigned short iDV, bool ResetDef) const {
   unsigned short iOrder, jOrder, kOrder;
-  su2double  x, y, z, movement[3], Segment_P0[3], Segment_P1[3], Plane_P0[3], Plane_Normal[3],
-  Variable_P0, Variable_P1, Intersection[3], Variable_Interp;
+  su2double x, y, z, movement[3], Segment_P0[3], Segment_P1[3], Plane_P0[3], Plane_Normal[3], Variable_P0, Variable_P1,
+      Intersection[3], Variable_Interp;
   unsigned short index[3], iPlane, iFFDBox;
   string design_FFDBox;
   su2double Scale = config->GetOpt_RelaxFactor();
@@ -2352,18 +2408,16 @@ bool CSurfaceMovement::SetFFDTwist(CGeometry *geometry, CConfig *config, CFreeFo
    design variable is not in this box) ---*/
 
   if (ResetDef == true) {
-    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++)
-      ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
+    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
   }
 
   design_FFDBox = config->GetFFDTag(iDV);
 
   if (design_FFDBox.compare(FFDBox->GetTag()) == 0) {
-
     /*--- Check that it is possible to move the control point ---*/
 
     jOrder = SU2_TYPE::Int(config->GetParamDV(iDV, 1));
-    for (iPlane = 0 ; iPlane < FFDBox->Get_nFix_JPlane(); iPlane++) {
+    for (iPlane = 0; iPlane < FFDBox->Get_nFix_JPlane(); iPlane++) {
       if (jOrder == FFDBox->Get_Fix_JPlane(iPlane)) return false;
     }
 
@@ -2380,19 +2434,25 @@ bool CSurfaceMovement::SetFFDTwist(CGeometry *geometry, CConfig *config, CFreeFo
     iOrder = 0;
     jOrder = SU2_TYPE::Int(config->GetParamDV(iDV, 1));
     kOrder = 0;
-    su2double *coord = FFDBox->GetCoordControlPoints(iOrder, jOrder, kOrder);
-    Plane_P0[0] = coord[0]; Plane_P0[1] = coord[1]; Plane_P0[2] = coord[2];
-    Plane_Normal[0] = 0.0; Plane_Normal[1] = 1.0; Plane_Normal[2] = 0.0;
+    su2double* coord = FFDBox->GetCoordControlPoints(iOrder, jOrder, kOrder);
+    Plane_P0[0] = coord[0];
+    Plane_P0[1] = coord[1];
+    Plane_P0[2] = coord[2];
+    Plane_Normal[0] = 0.0;
+    Plane_Normal[1] = 1.0;
+    Plane_Normal[2] = 0.0;
 
-    Variable_P0 = 0.0; Variable_P1 = 0.0;
+    Variable_P0 = 0.0;
+    Variable_P1 = 0.0;
 
-    Intersection[0] = 0.0; Intersection[1] = 0.0;  Intersection[2] = 0.0;
+    Intersection[0] = 0.0;
+    Intersection[1] = 0.0;
+    Intersection[2] = 0.0;
 
-    bool result = geometry->SegmentIntersectsPlane(Segment_P0, Segment_P1, Variable_P0, Variable_P1,
-                                                   Plane_P0, Plane_Normal, Intersection, Variable_Interp);
+    bool result = geometry->SegmentIntersectsPlane(Segment_P0, Segment_P1, Variable_P0, Variable_P1, Plane_P0,
+                                                   Plane_Normal, Intersection, Variable_Interp);
 
     if (result) {
-
       /*--- xyz-coordinates of a point on the line of rotation. ---*/
 
       su2double a = Intersection[0];
@@ -2409,75 +2469,82 @@ bool CSurfaceMovement::SetFFDTwist(CGeometry *geometry, CConfig *config, CFreeFo
        otherwise it is difficult to compare with other length based design variables. ---*/
 
       su2double RefLength = config->GetRefLength();
-      su2double theta = atan(config->GetDV_Value(iDV)*Scale/RefLength);
+      su2double theta = atan(config->GetDV_Value(iDV) * Scale / RefLength);
 
       /*--- An intermediate value used in computations. ---*/
 
-      su2double u2=u*u; su2double v2=v*v; su2double w2=w*w;
-      su2double l2 = u2 + v2 + w2; su2double l = sqrt(l2);
-      su2double cosT; su2double sinT;
+      su2double u2 = u * u;
+      su2double v2 = v * v;
+      su2double w2 = w * w;
+      su2double l2 = u2 + v2 + w2;
+      su2double l = sqrt(l2);
+      su2double cosT;
+      su2double sinT;
 
       /*--- Change the value of the control point if move is true ---*/
 
       jOrder = SU2_TYPE::Int(config->GetParamDV(iDV, 1));
       for (iOrder = 0; iOrder < FFDBox->GetlOrder(); iOrder++)
         for (kOrder = 0; kOrder < FFDBox->GetnOrder(); kOrder++) {
-          index[0] = iOrder; index[1] = jOrder; index[2] = kOrder;
-          su2double *coord = FFDBox->GetCoordControlPoints(iOrder, jOrder, kOrder);
-          x = coord[0]; y = coord[1]; z = coord[2];
+          index[0] = iOrder;
+          index[1] = jOrder;
+          index[2] = kOrder;
+          su2double* coord = FFDBox->GetCoordControlPoints(iOrder, jOrder, kOrder);
+          x = coord[0];
+          y = coord[1];
+          z = coord[2];
 
           cosT = cos(theta);
           sinT = sin(theta);
 
-          movement[0] = a*(v2 + w2) + u*(-b*v - c*w + u*x + v*y + w*z)
-          + (-a*(v2 + w2) + u*(b*v + c*w - v*y - w*z) + (v2 + w2)*x)*cosT
-          + l*(-c*v + b*w - w*y + v*z)*sinT;
-          movement[0] = movement[0]/l2 - x;
+          movement[0] = a * (v2 + w2) + u * (-b * v - c * w + u * x + v * y + w * z) +
+                        (-a * (v2 + w2) + u * (b * v + c * w - v * y - w * z) + (v2 + w2) * x) * cosT +
+                        l * (-c * v + b * w - w * y + v * z) * sinT;
+          movement[0] = movement[0] / l2 - x;
 
-          movement[1] = b*(u2 + w2) + v*(-a*u - c*w + u*x + v*y + w*z)
-          + (-b*(u2 + w2) + v*(a*u + c*w - u*x - w*z) + (u2 + w2)*y)*cosT
-          + l*(c*u - a*w + w*x - u*z)*sinT;
-          movement[1] = movement[1]/l2 - y;
+          movement[1] = b * (u2 + w2) + v * (-a * u - c * w + u * x + v * y + w * z) +
+                        (-b * (u2 + w2) + v * (a * u + c * w - u * x - w * z) + (u2 + w2) * y) * cosT +
+                        l * (c * u - a * w + w * x - u * z) * sinT;
+          movement[1] = movement[1] / l2 - y;
 
-          movement[2] = c*(u2 + v2) + w*(-a*u - b*v + u*x + v*y + w*z)
-          + (-c*(u2 + v2) + w*(a*u + b*v - u*x - v*y) + (u2 + v2)*z)*cosT
-          + l*(-b*u + a*v - v*x + u*y)*sinT;
-          movement[2] = movement[2]/l2 - z;
+          movement[2] = c * (u2 + v2) + w * (-a * u - b * v + u * x + v * y + w * z) +
+                        (-c * (u2 + v2) + w * (a * u + b * v - u * x - v * y) + (u2 + v2) * z) * cosT +
+                        l * (-b * u + a * v - v * x + u * y) * sinT;
+          movement[2] = movement[2] / l2 - z;
 
           /*--- Check that it is possible to move the control point ---*/
 
-          for (iPlane = 0 ; iPlane < FFDBox->Get_nFix_IPlane(); iPlane++) {
+          for (iPlane = 0; iPlane < FFDBox->Get_nFix_IPlane(); iPlane++) {
             if (iOrder == FFDBox->Get_Fix_IPlane(iPlane)) {
-              movement[0] = 0.0; movement[1] = 0.0; movement[2] = 0.0;
+              movement[0] = 0.0;
+              movement[1] = 0.0;
+              movement[2] = 0.0;
             }
           }
 
-          for (iPlane = 0 ; iPlane < FFDBox->Get_nFix_KPlane(); iPlane++) {
+          for (iPlane = 0; iPlane < FFDBox->Get_nFix_KPlane(); iPlane++) {
             if (kOrder == FFDBox->Get_Fix_KPlane(iPlane)) {
-              movement[0] = 0.0; movement[1] = 0.0; movement[2] = 0.0;
+              movement[0] = 0.0;
+              movement[1] = 0.0;
+              movement[2] = 0.0;
             }
           }
 
           FFDBox->SetControlPoints(index, movement);
-
         }
-
     }
 
-  }
-  else {
+  } else {
     return false;
   }
 
   return true;
-
 }
 
-bool CSurfaceMovement::SetFFDRotation(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox,
-                                      unsigned short iDV, bool ResetDef) const {
-
+bool CSurfaceMovement::SetFFDRotation(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox,
+                                      CFreeFormDefBox** ResetFFDBox, unsigned short iDV, bool ResetDef) const {
   unsigned short iOrder, jOrder, kOrder;
-  su2double movement[3] = {0.0,0.0,0.0}, x, y, z;
+  su2double movement[3] = {0.0, 0.0, 0.0}, x, y, z;
   unsigned short index[3], iFFDBox;
   string design_FFDBox;
   su2double Scale = config->GetOpt_RelaxFactor();
@@ -2486,14 +2553,12 @@ bool CSurfaceMovement::SetFFDRotation(CGeometry *geometry, CConfig *config, CFre
    design variable is not in this box) ---*/
 
   if (ResetDef == true) {
-    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++)
-      ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
+    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
   }
 
   design_FFDBox = config->GetFFDTag(iDV);
 
   if (design_FFDBox.compare(FFDBox->GetTag()) == 0) {
-
     /*--- xyz-coordinates of a point on the line of rotation. ---*/
 
     su2double a = config->GetParamDV(iDV, 1);
@@ -2502,60 +2567,64 @@ bool CSurfaceMovement::SetFFDRotation(CGeometry *geometry, CConfig *config, CFre
 
     /*--- xyz-coordinate of the line's direction vector. ---*/
 
-    su2double u = config->GetParamDV(iDV, 4)-config->GetParamDV(iDV, 1);
-    su2double v = config->GetParamDV(iDV, 5)-config->GetParamDV(iDV, 2);
-    su2double w = config->GetParamDV(iDV, 6)-config->GetParamDV(iDV, 3);
+    su2double u = config->GetParamDV(iDV, 4) - config->GetParamDV(iDV, 1);
+    su2double v = config->GetParamDV(iDV, 5) - config->GetParamDV(iDV, 2);
+    su2double w = config->GetParamDV(iDV, 6) - config->GetParamDV(iDV, 3);
 
     /*--- The angle of rotation. ---*/
 
-    su2double theta = config->GetDV_Value(iDV)*Scale*PI_NUMBER/180.0;
+    su2double theta = config->GetDV_Value(iDV) * Scale * PI_NUMBER / 180.0;
 
     /*--- An intermediate value used in computations. ---*/
 
-    su2double u2=u*u; su2double v2=v*v; su2double w2=w*w;
-    su2double cosT = cos(theta); su2double sinT = sin(theta);
-    su2double l2 = u2 + v2 + w2; su2double l = sqrt(l2);
+    su2double u2 = u * u;
+    su2double v2 = v * v;
+    su2double w2 = w * w;
+    su2double cosT = cos(theta);
+    su2double sinT = sin(theta);
+    su2double l2 = u2 + v2 + w2;
+    su2double l = sqrt(l2);
 
     /*--- Change the value of the control point if move is true ---*/
 
     for (iOrder = 0; iOrder < FFDBox->GetlOrder(); iOrder++)
       for (jOrder = 0; jOrder < FFDBox->GetmOrder(); jOrder++)
         for (kOrder = 0; kOrder < FFDBox->GetnOrder(); kOrder++) {
-          index[0] = iOrder; index[1] = jOrder; index[2] = kOrder;
-          su2double *coord = FFDBox->GetCoordControlPoints(iOrder, jOrder, kOrder);
-          x = coord[0]; y = coord[1]; z = coord[2];
-          movement[0] = a*(v2 + w2) + u*(-b*v - c*w + u*x + v*y + w*z)
-          + (-a*(v2 + w2) + u*(b*v + c*w - v*y - w*z) + (v2 + w2)*x)*cosT
-          + l*(-c*v + b*w - w*y + v*z)*sinT;
-          movement[0] = movement[0]/l2 - x;
-
-          movement[1] = b*(u2 + w2) + v*(-a*u - c*w + u*x + v*y + w*z)
-          + (-b*(u2 + w2) + v*(a*u + c*w - u*x - w*z) + (u2 + w2)*y)*cosT
-          + l*(c*u - a*w + w*x - u*z)*sinT;
-          movement[1] = movement[1]/l2 - y;
-
-          movement[2] = c*(u2 + v2) + w*(-a*u - b*v + u*x + v*y + w*z)
-          + (-c*(u2 + v2) + w*(a*u + b*v - u*x - v*y) + (u2 + v2)*z)*cosT
-          + l*(-b*u + a*v - v*x + u*y)*sinT;
-          movement[2] = movement[2]/l2 - z;
+          index[0] = iOrder;
+          index[1] = jOrder;
+          index[2] = kOrder;
+          su2double* coord = FFDBox->GetCoordControlPoints(iOrder, jOrder, kOrder);
+          x = coord[0];
+          y = coord[1];
+          z = coord[2];
+          movement[0] = a * (v2 + w2) + u * (-b * v - c * w + u * x + v * y + w * z) +
+                        (-a * (v2 + w2) + u * (b * v + c * w - v * y - w * z) + (v2 + w2) * x) * cosT +
+                        l * (-c * v + b * w - w * y + v * z) * sinT;
+          movement[0] = movement[0] / l2 - x;
+
+          movement[1] = b * (u2 + w2) + v * (-a * u - c * w + u * x + v * y + w * z) +
+                        (-b * (u2 + w2) + v * (a * u + c * w - u * x - w * z) + (u2 + w2) * y) * cosT +
+                        l * (c * u - a * w + w * x - u * z) * sinT;
+          movement[1] = movement[1] / l2 - y;
+
+          movement[2] = c * (u2 + v2) + w * (-a * u - b * v + u * x + v * y + w * z) +
+                        (-c * (u2 + v2) + w * (a * u + b * v - u * x - v * y) + (u2 + v2) * z) * cosT +
+                        l * (-b * u + a * v - v * x + u * y) * sinT;
+          movement[2] = movement[2] / l2 - z;
 
           FFDBox->SetControlPoints(index, movement);
-
         }
-  }
-  else {
+  } else {
     return false;
   }
 
   return true;
-
 }
 
-bool CSurfaceMovement::SetFFDControl_Surface(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox, CFreeFormDefBox **ResetFFDBox,
-                                             unsigned short iDV, bool ResetDef) const {
-
+bool CSurfaceMovement::SetFFDControl_Surface(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox,
+                                             CFreeFormDefBox** ResetFFDBox, unsigned short iDV, bool ResetDef) const {
   unsigned short iOrder, jOrder, kOrder;
-  su2double movement[3] = {0.0,0.0,0.0}, x, y, z;
+  su2double movement[3] = {0.0, 0.0, 0.0}, x, y, z;
   unsigned short index[3], iFFDBox;
   string design_FFDBox;
   su2double Scale = config->GetOpt_RelaxFactor();
@@ -2564,14 +2633,12 @@ bool CSurfaceMovement::SetFFDControl_Surface(CGeometry *geometry, CConfig *confi
    design variable is not in this box) ---*/
 
   if (ResetDef == true) {
-    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++)
-      ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
+    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
   }
 
   design_FFDBox = config->GetFFDTag(iDV);
 
   if (design_FFDBox.compare(FFDBox->GetTag()) == 0) {
-
     /*--- xyz-coordinates of a point on the line of rotation. ---*/
 
     su2double a = config->GetParamDV(iDV, 1);
@@ -2580,69 +2647,72 @@ bool CSurfaceMovement::SetFFDControl_Surface(CGeometry *geometry, CConfig *confi
 
     /*--- xyz-coordinate of the line's direction vector. ---*/
 
-    su2double u = config->GetParamDV(iDV, 4)-config->GetParamDV(iDV, 1);
-    su2double v = config->GetParamDV(iDV, 5)-config->GetParamDV(iDV, 2);
-    su2double w = config->GetParamDV(iDV, 6)-config->GetParamDV(iDV, 3);
+    su2double u = config->GetParamDV(iDV, 4) - config->GetParamDV(iDV, 1);
+    su2double v = config->GetParamDV(iDV, 5) - config->GetParamDV(iDV, 2);
+    su2double w = config->GetParamDV(iDV, 6) - config->GetParamDV(iDV, 3);
 
     /*--- The angle of rotation. ---*/
 
-    su2double theta = -config->GetDV_Value(iDV)*Scale*PI_NUMBER/180.0;
+    su2double theta = -config->GetDV_Value(iDV) * Scale * PI_NUMBER / 180.0;
 
     /*--- An intermediate value used in computations. ---*/
 
-    su2double u2=u*u; su2double v2=v*v; su2double w2=w*w;
-    su2double cosT = cos(theta); su2double sinT = sin(theta);
-    su2double l2 = u2 + v2 + w2; su2double l = sqrt(l2);
+    su2double u2 = u * u;
+    su2double v2 = v * v;
+    su2double w2 = w * w;
+    su2double cosT = cos(theta);
+    su2double sinT = sin(theta);
+    su2double l2 = u2 + v2 + w2;
+    su2double l = sqrt(l2);
 
     /*--- Change the value of the control point if move is true ---*/
 
-    for (iOrder = 0; iOrder < FFDBox->GetlOrder()-2; iOrder++)
-      for (jOrder = 2; jOrder < FFDBox->GetmOrder()-2; jOrder++)
+    for (iOrder = 0; iOrder < FFDBox->GetlOrder() - 2; iOrder++)
+      for (jOrder = 2; jOrder < FFDBox->GetmOrder() - 2; jOrder++)
         for (kOrder = 0; kOrder < FFDBox->GetnOrder(); kOrder++) {
-          index[0] = iOrder; index[1] = jOrder; index[2] = kOrder;
-          su2double *coord = FFDBox->GetCoordControlPoints(iOrder, jOrder, kOrder);
-          x = coord[0]; y = coord[1]; z = coord[2];
-          movement[0] = a*(v2 + w2) + u*(-b*v - c*w + u*x + v*y + w*z)
-          + (-a*(v2 + w2) + u*(b*v + c*w - v*y - w*z) + (v2 + w2)*x)*cosT
-          + l*(-c*v + b*w - w*y + v*z)*sinT;
-          movement[0] = movement[0]/l2 - x;
-
-          movement[1] = b*(u2 + w2) + v*(-a*u - c*w + u*x + v*y + w*z)
-          + (-b*(u2 + w2) + v*(a*u + c*w - u*x - w*z) + (u2 + w2)*y)*cosT
-          + l*(c*u - a*w + w*x - u*z)*sinT;
-          movement[1] = movement[1]/l2 - y;
-
-          movement[2] = c*(u2 + v2) + w*(-a*u - b*v + u*x + v*y + w*z)
-          + (-c*(u2 + v2) + w*(a*u + b*v - u*x - v*y) + (u2 + v2)*z)*cosT
-          + l*(-b*u + a*v - v*x + u*y)*sinT;
-          movement[2] = movement[2]/l2 - z;
+          index[0] = iOrder;
+          index[1] = jOrder;
+          index[2] = kOrder;
+          su2double* coord = FFDBox->GetCoordControlPoints(iOrder, jOrder, kOrder);
+          x = coord[0];
+          y = coord[1];
+          z = coord[2];
+          movement[0] = a * (v2 + w2) + u * (-b * v - c * w + u * x + v * y + w * z) +
+                        (-a * (v2 + w2) + u * (b * v + c * w - v * y - w * z) + (v2 + w2) * x) * cosT +
+                        l * (-c * v + b * w - w * y + v * z) * sinT;
+          movement[0] = movement[0] / l2 - x;
+
+          movement[1] = b * (u2 + w2) + v * (-a * u - c * w + u * x + v * y + w * z) +
+                        (-b * (u2 + w2) + v * (a * u + c * w - u * x - w * z) + (u2 + w2) * y) * cosT +
+                        l * (c * u - a * w + w * x - u * z) * sinT;
+          movement[1] = movement[1] / l2 - y;
+
+          movement[2] = c * (u2 + v2) + w * (-a * u - b * v + u * x + v * y + w * z) +
+                        (-c * (u2 + v2) + w * (a * u + b * v - u * x - v * y) + (u2 + v2) * z) * cosT +
+                        l * (-b * u + a * v - v * x + u * y) * sinT;
+          movement[2] = movement[2] / l2 - z;
 
           FFDBox->SetControlPoints(index, movement);
-
         }
-  }
-  else {
+  } else {
     return false;
   }
 
   return true;
-
 }
 
-void CSurfaceMovement::SetAngleOfAttack(CGeometry *boundary, CConfig *config, unsigned short iDV, bool ResetDef) {
-
+void CSurfaceMovement::SetAngleOfAttack(CGeometry* boundary, CConfig* config, unsigned short iDV, bool ResetDef) {
   su2double Scale = config->GetOpt_RelaxFactor();
-  su2double Ampl = config->GetDV_Value(iDV)*Scale;
+  su2double Ampl = config->GetDV_Value(iDV) * Scale;
   config->SetAoA_Offset(Ampl);
-
 }
 
-void CSurfaceMovement::SetHicksHenne(CGeometry *boundary, CConfig *config, unsigned short iDV, bool ResetDef) {
+void CSurfaceMovement::SetHicksHenne(CGeometry* boundary, CConfig* config, unsigned short iDV, bool ResetDef) {
   unsigned long iVertex;
   unsigned short iMarker;
-  su2double VarCoord[3] = {0.0,0.0,0.0}, VarCoord_[3] = {0.0,0.0,0.0}, *Coord_, *Normal_, ek, fk,
-      Coord[3] = {0.0,0.0,0.0}, Normal[3] = {0.0,0.0,0.0},
-  TPCoord[2] = {0.0, 0.0}, LPCoord[2] = {0.0, 0.0}, Distance, Chord, AoA, ValCos, ValSin;
+  su2double VarCoord[3] = {0.0, 0.0, 0.0}, VarCoord_[3] = {0.0, 0.0, 0.0}, *Coord_, *Normal_, ek, fk,
+            Coord[3] = {0.0, 0.0, 0.0}, Normal[3] = {0.0, 0.0, 0.0}, TPCoord[2] = {0.0, 0.0}, LPCoord[2] = {0.0, 0.0},
+            Distance, Chord, AoA, ValCos, ValSin;
 
   bool upper = true;
   su2double Scale = config->GetOpt_RelaxFactor();
@@ -2652,7 +2722,9 @@ void CSurfaceMovement::SetHicksHenne(CGeometry *boundary, CConfig *config, unsig
   if ((iDV == 0) || (ResetDef == true)) {
     for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++)
       for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
-        VarCoord[0] = 0.0; VarCoord[1] = 0.0; VarCoord[2] = 0.0;
+        VarCoord[0] = 0.0;
+        VarCoord[1] = 0.0;
+        VarCoord[2] = 0.0;
         boundary->vertex[iMarker][iVertex]->SetVarCoord(VarCoord);
       }
   }
@@ -2662,10 +2734,14 @@ void CSurfaceMovement::SetHicksHenne(CGeometry *boundary, CConfig *config, unsig
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
     if (config->GetMarker_All_DV(iMarker) == YES) {
       Coord_ = boundary->vertex[iMarker][0]->GetCoord();
-      TPCoord[0] = Coord_[0]; TPCoord[1] = Coord_[1];
+      TPCoord[0] = Coord_[0];
+      TPCoord[1] = Coord_[1];
       for (iVertex = 1; iVertex < boundary->nVertex[iMarker]; iVertex++) {
         Coord_ = boundary->vertex[iMarker][iVertex]->GetCoord();
-        if (Coord_[0] > TPCoord[0]) { TPCoord[0] = Coord_[0]; TPCoord[1] = Coord_[1]; }
+        if (Coord_[0] > TPCoord[0]) {
+          TPCoord[0] = Coord_[0];
+          TPCoord[1] = Coord_[1];
+        }
       }
     }
   }
@@ -2675,126 +2751,148 @@ void CSurfaceMovement::SetHicksHenne(CGeometry *boundary, CConfig *config, unsig
   int iProcessor, nProcessor = size;
   su2double *Buffer_Send_Coord, *Buffer_Receive_Coord;
 
-  Buffer_Receive_Coord = new su2double [nProcessor*2];
-  Buffer_Send_Coord = new su2double [2];
+  Buffer_Receive_Coord = new su2double[nProcessor * 2];
+  Buffer_Send_Coord = new su2double[2];
 
-  Buffer_Send_Coord[0] = TPCoord[0]; Buffer_Send_Coord[1] = TPCoord[1];
+  Buffer_Send_Coord[0] = TPCoord[0];
+  Buffer_Send_Coord[1] = TPCoord[1];
 
   SU2_MPI::Allgather(Buffer_Send_Coord, 2, MPI_DOUBLE, Buffer_Receive_Coord, 2, MPI_DOUBLE, SU2_MPI::GetComm());
 
-  TPCoord[0] = Buffer_Receive_Coord[0]; TPCoord[1] = Buffer_Receive_Coord[1];
+  TPCoord[0] = Buffer_Receive_Coord[0];
+  TPCoord[1] = Buffer_Receive_Coord[1];
   for (iProcessor = 1; iProcessor < nProcessor; iProcessor++) {
-    Coord[0] = Buffer_Receive_Coord[iProcessor*2 + 0];
-    Coord[1] = Buffer_Receive_Coord[iProcessor*2 + 1];
-    if (Coord[0] > TPCoord[0]) { TPCoord[0] = Coord[0]; TPCoord[1] = Coord[1]; }
+    Coord[0] = Buffer_Receive_Coord[iProcessor * 2 + 0];
+    Coord[1] = Buffer_Receive_Coord[iProcessor * 2 + 1];
+    if (Coord[0] > TPCoord[0]) {
+      TPCoord[0] = Coord[0];
+      TPCoord[1] = Coord[1];
+    }
   }
 
-  delete[] Buffer_Send_Coord;   delete[] Buffer_Receive_Coord;
+  delete[] Buffer_Send_Coord;
+  delete[] Buffer_Receive_Coord;
 
 #endif
 
-
   Chord = 0.0;
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
     if (config->GetMarker_All_DV(iMarker) == YES) {
       for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
         Coord_ = boundary->vertex[iMarker][iVertex]->GetCoord();
         Distance = sqrt(pow(Coord_[0] - TPCoord[0], 2.0) + pow(Coord_[1] - TPCoord[1], 2.0));
-        if (Chord < Distance) { Chord = Distance; LPCoord[0] = Coord_[0]; LPCoord[1] = Coord_[1]; }
+        if (Chord < Distance) {
+          Chord = Distance;
+          LPCoord[0] = Coord_[0];
+          LPCoord[1] = Coord_[1];
+        }
       }
     }
   }
 
 #ifdef HAVE_MPI
 
-  Buffer_Receive_Coord = new su2double [nProcessor*2];
-  Buffer_Send_Coord = new su2double [2];
+  Buffer_Receive_Coord = new su2double[nProcessor * 2];
+  Buffer_Send_Coord = new su2double[2];
 
-  Buffer_Send_Coord[0] = LPCoord[0]; Buffer_Send_Coord[1] = LPCoord[1];
+  Buffer_Send_Coord[0] = LPCoord[0];
+  Buffer_Send_Coord[1] = LPCoord[1];
 
   SU2_MPI::Allgather(Buffer_Send_Coord, 2, MPI_DOUBLE, Buffer_Receive_Coord, 2, MPI_DOUBLE, SU2_MPI::GetComm());
 
   Chord = 0.0;
   for (iProcessor = 0; iProcessor < nProcessor; iProcessor++) {
-    Coord[0] = Buffer_Receive_Coord[iProcessor*2 + 0];
-    Coord[1] = Buffer_Receive_Coord[iProcessor*2 + 1];
+    Coord[0] = Buffer_Receive_Coord[iProcessor * 2 + 0];
+    Coord[1] = Buffer_Receive_Coord[iProcessor * 2 + 1];
     Distance = sqrt(pow(Coord[0] - TPCoord[0], 2.0) + pow(Coord[1] - TPCoord[1], 2.0));
-    if (Chord < Distance) { Chord = Distance; LPCoord[0] = Coord[0]; LPCoord[1] = Coord[1]; }
+    if (Chord < Distance) {
+      Chord = Distance;
+      LPCoord[0] = Coord[0];
+      LPCoord[1] = Coord[1];
+    }
   }
 
-  delete[] Buffer_Send_Coord;   delete[] Buffer_Receive_Coord;
+  delete[] Buffer_Send_Coord;
+  delete[] Buffer_Receive_Coord;
 
 #endif
 
-  AoA = atan((LPCoord[1] - TPCoord[1]) / (TPCoord[0] - LPCoord[0]))*180/PI_NUMBER;
+  AoA = atan((LPCoord[1] - TPCoord[1]) / (TPCoord[0] - LPCoord[0])) * 180 / PI_NUMBER;
 
   /*--- WARNING: AoA currently overwritten to zero. ---*/
   AoA = 0.0;
 
   /*--- Perform multiple airfoil deformation ---*/
 
-  su2double Ampl = config->GetDV_Value(iDV)*Scale;
+  su2double Ampl = config->GetDV_Value(iDV) * Scale;
   su2double xk = config->GetParamDV(iDV, 1);
   const su2double t2 = 3.0;
 
-  if (config->GetParamDV(iDV, 0) == NO) { upper = false; }
-  if (config->GetParamDV(iDV, 0) == YES) { upper = true; }
+  if (config->GetParamDV(iDV, 0) == NO) {
+    upper = false;
+  }
+  if (config->GetParamDV(iDV, 0) == YES) {
+    upper = true;
+  }
 
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-
     for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
-      VarCoord[0] = 0.0; VarCoord[1] = 0.0; VarCoord[2] = 0.0;
+      VarCoord[0] = 0.0;
+      VarCoord[1] = 0.0;
+      VarCoord[2] = 0.0;
 
       if (config->GetMarker_All_DV(iMarker) == YES) {
-
         Coord_ = boundary->vertex[iMarker][iVertex]->GetCoord();
         Normal_ = boundary->vertex[iMarker][iVertex]->GetNormal();
 
         /*--- The Hicks Henne bump functions should be applied to a basic airfoil without AoA,
          and unitary chord, a tranformation is required ---*/
 
-        ValCos = cos(AoA*PI_NUMBER/180.0);
-        ValSin = sin(AoA*PI_NUMBER/180.0);
+        ValCos = cos(AoA * PI_NUMBER / 180.0);
+        ValSin = sin(AoA * PI_NUMBER / 180.0);
 
-        Coord[0] = Coord_[0]*ValCos - Coord_[1]*ValSin;
-        Coord[0] = max(0.0, Coord[0]); // Coord x should be always positive
-        Coord[1] = Coord_[1]*ValCos + Coord_[0]*ValSin;
+        Coord[0] = Coord_[0] * ValCos - Coord_[1] * ValSin;
+        Coord[0] = max(0.0, Coord[0]);  // Coord x should be always positive
+        Coord[1] = Coord_[1] * ValCos + Coord_[0] * ValSin;
 
-        Normal[0] = Normal_[0]*ValCos - Normal_[1]*ValSin;
-        Normal[1] = Normal_[1]*ValCos + Normal_[0]*ValSin;
+        Normal[0] = Normal_[0] * ValCos - Normal_[1] * ValSin;
+        Normal[1] = Normal_[1] * ValCos + Normal_[0] * ValSin;
 
         /*--- Bump computation ---*/
 
-        ek = log10(0.5)/log10(xk);
-        if (Coord[0] > 10*EPS) fk = pow( sin( PI_NUMBER * pow(Coord[0], ek) ), t2);
-        else fk = 0.0;
+        ek = log10(0.5) / log10(xk);
+        if (Coord[0] > 10 * EPS)
+          fk = pow(sin(PI_NUMBER * pow(Coord[0], ek)), t2);
+        else
+          fk = 0.0;
 
         /*--- Upper and lower surface ---*/
 
-        if (( upper) && (Normal[1] > 0)) { VarCoord[1] =  Ampl*fk; }
-        if ((!upper) && (Normal[1] < 0)) { VarCoord[1] = -Ampl*fk; }
-
+        if ((upper) && (Normal[1] > 0)) {
+          VarCoord[1] = Ampl * fk;
+        }
+        if ((!upper) && (Normal[1] < 0)) {
+          VarCoord[1] = -Ampl * fk;
+        }
       }
 
       /*--- Apply the transformation to the coordinate variation ---*/
 
-      ValCos = cos(-AoA*PI_NUMBER/180.0);
-      ValSin = sin(-AoA*PI_NUMBER/180.0);
+      ValCos = cos(-AoA * PI_NUMBER / 180.0);
+      ValSin = sin(-AoA * PI_NUMBER / 180.0);
 
-      VarCoord_[0] = VarCoord[0]*ValCos - VarCoord[1]*ValSin;
-      VarCoord_[1] = VarCoord[1]*ValCos + VarCoord[0]*ValSin;
+      VarCoord_[0] = VarCoord[0] * ValCos - VarCoord[1] * ValSin;
+      VarCoord_[1] = VarCoord[1] * ValCos + VarCoord[0] * ValSin;
 
       boundary->vertex[iMarker][iVertex]->AddVarCoord(VarCoord_);
-
     }
   }
-
 }
 
-void CSurfaceMovement::SetSurface_Bump(CGeometry *boundary, CConfig *config, unsigned short iDV, bool ResetDef) {
+void CSurfaceMovement::SetSurface_Bump(CGeometry* boundary, CConfig* config, unsigned short iDV, bool ResetDef) {
   unsigned long iVertex;
   unsigned short iMarker;
-  su2double VarCoord[3] = {0.0,0.0,0.0}, ek, fk, *Coord, xCoord;
+  su2double VarCoord[3] = {0.0, 0.0, 0.0}, ek, fk, *Coord, xCoord;
   su2double Scale = config->GetOpt_RelaxFactor();
 
   /*--- Reset airfoil deformation if first deformation or if it required by the solver ---*/
@@ -2802,14 +2900,16 @@ void CSurfaceMovement::SetSurface_Bump(CGeometry *boundary, CConfig *config, uns
   if ((iDV == 0) || (ResetDef == true)) {
     for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++)
       for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
-        VarCoord[0] = 0.0; VarCoord[1] = 0.0; VarCoord[2] = 0.0;
+        VarCoord[0] = 0.0;
+        VarCoord[1] = 0.0;
+        VarCoord[2] = 0.0;
         boundary->vertex[iMarker][iVertex]->SetVarCoord(VarCoord);
       }
   }
 
   /*--- Perform multiple airfoil deformation ---*/
 
-  su2double Ampl = config->GetDV_Value(iDV)*Scale;
+  su2double Ampl = config->GetDV_Value(iDV) * Scale;
   su2double x_start = config->GetParamDV(iDV, 0);
   su2double x_end = config->GetParamDV(iDV, 1);
   su2double BumpSize = x_end - x_start;
@@ -2818,37 +2918,39 @@ void CSurfaceMovement::SetSurface_Bump(CGeometry *boundary, CConfig *config, uns
   const su2double t2 = 3.0;
 
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-
     for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
-      VarCoord[0] = 0.0; VarCoord[1] = 0.0; VarCoord[2] = 0.0;
+      VarCoord[0] = 0.0;
+      VarCoord[1] = 0.0;
+      VarCoord[2] = 0.0;
 
       if (config->GetMarker_All_DV(iMarker) == YES) {
-
         Coord = boundary->vertex[iMarker][iVertex]->GetCoord();
 
         xCoord = (Coord[0] - BumpLoc);
-        ek = log10(0.5)/log10((xk-BumpLoc+EPS)/BumpSize);
-        if (xCoord > 0.0) fk = pow( sin( PI_NUMBER * pow((xCoord+EPS)/BumpSize, ek)), t2);
-        else fk = 0.0;
-
-        if ((xCoord <= 0.0) || (xCoord >= BumpSize)) VarCoord[1] =  0.0;
-        else { VarCoord[1] =  Ampl*fk; }
-
+        ek = log10(0.5) / log10((xk - BumpLoc + EPS) / BumpSize);
+        if (xCoord > 0.0)
+          fk = pow(sin(PI_NUMBER * pow((xCoord + EPS) / BumpSize, ek)), t2);
+        else
+          fk = 0.0;
+
+        if ((xCoord <= 0.0) || (xCoord >= BumpSize))
+          VarCoord[1] = 0.0;
+        else {
+          VarCoord[1] = Ampl * fk;
+        }
       }
 
       boundary->vertex[iMarker][iVertex]->AddVarCoord(VarCoord);
-
     }
   }
-
 }
 
-void CSurfaceMovement::SetCST(CGeometry *boundary, CConfig *config, unsigned short iDV, bool ResetDef) {
+void CSurfaceMovement::SetCST(CGeometry* boundary, CConfig* config, unsigned short iDV, bool ResetDef) {
   unsigned long iVertex;
   unsigned short iMarker;
-  su2double VarCoord[3] = {0.0,0.0,0.0}, VarCoord_[3] = {0.0,0.0,0.0}, *Coord_, *Normal_, fk,
-    Coord[3] = {0.0,0.0,0.0}, Normal[3] = {0.0,0.0,0.0},
-    TPCoord[2] = {0.0, 0.0}, LPCoord[2] = {0.0, 0.0}, Distance, Chord, AoA, ValCos, ValSin;
+  su2double VarCoord[3] = {0.0, 0.0, 0.0}, VarCoord_[3] = {0.0, 0.0, 0.0}, *Coord_, *Normal_, fk,
+            Coord[3] = {0.0, 0.0, 0.0}, Normal[3] = {0.0, 0.0, 0.0}, TPCoord[2] = {0.0, 0.0}, LPCoord[2] = {0.0, 0.0},
+            Distance, Chord, AoA, ValCos, ValSin;
 
   bool upper = true;
   su2double Scale = config->GetOpt_RelaxFactor();
@@ -2858,20 +2960,26 @@ void CSurfaceMovement::SetCST(CGeometry *boundary, CConfig *config, unsigned sho
   if ((iDV == 0) || (ResetDef == true)) {
     for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++)
       for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
-        VarCoord[0] = 0.0; VarCoord[1] = 0.0; VarCoord[2] = 0.0;
+        VarCoord[0] = 0.0;
+        VarCoord[1] = 0.0;
+        VarCoord[2] = 0.0;
         boundary->vertex[iMarker][iVertex]->SetVarCoord(VarCoord);
       }
   }
 
-    /*--- Compute the angle of attack to apply the deformation ---*/
+  /*--- Compute the angle of attack to apply the deformation ---*/
 
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
     if (config->GetMarker_All_DV(iMarker) == YES) {
       Coord_ = boundary->vertex[iMarker][0]->GetCoord();
-      TPCoord[0] = Coord_[0]; TPCoord[1] = Coord_[1];
+      TPCoord[0] = Coord_[0];
+      TPCoord[1] = Coord_[1];
       for (iVertex = 1; iVertex < boundary->nVertex[iMarker]; iVertex++) {
         Coord_ = boundary->vertex[iMarker][iVertex]->GetCoord();
-        if (Coord_[0] > TPCoord[0]) { TPCoord[0] = Coord_[0]; TPCoord[1] = Coord_[1]; }
+        if (Coord_[0] > TPCoord[0]) {
+          TPCoord[0] = Coord_[0];
+          TPCoord[1] = Coord_[1];
+        }
       }
     }
   }
@@ -2881,65 +2989,80 @@ void CSurfaceMovement::SetCST(CGeometry *boundary, CConfig *config, unsigned sho
   int iProcessor, nProcessor = size;
   su2double *Buffer_Send_Coord, *Buffer_Receive_Coord;
 
-  Buffer_Receive_Coord = new su2double [nProcessor*2];
-  Buffer_Send_Coord = new su2double [2];
+  Buffer_Receive_Coord = new su2double[nProcessor * 2];
+  Buffer_Send_Coord = new su2double[2];
 
-  Buffer_Send_Coord[0] = TPCoord[0]; Buffer_Send_Coord[1] = TPCoord[1];
+  Buffer_Send_Coord[0] = TPCoord[0];
+  Buffer_Send_Coord[1] = TPCoord[1];
 
   SU2_MPI::Allgather(Buffer_Send_Coord, 2, MPI_DOUBLE, Buffer_Receive_Coord, 2, MPI_DOUBLE, SU2_MPI::GetComm());
 
-  TPCoord[0] = Buffer_Receive_Coord[0]; TPCoord[1] = Buffer_Receive_Coord[1];
+  TPCoord[0] = Buffer_Receive_Coord[0];
+  TPCoord[1] = Buffer_Receive_Coord[1];
   for (iProcessor = 1; iProcessor < nProcessor; iProcessor++) {
-    Coord[0] = Buffer_Receive_Coord[iProcessor*2 + 0];
-    Coord[1] = Buffer_Receive_Coord[iProcessor*2 + 1];
-    if (Coord[0] > TPCoord[0]) { TPCoord[0] = Coord[0]; TPCoord[1] = Coord[1]; }
+    Coord[0] = Buffer_Receive_Coord[iProcessor * 2 + 0];
+    Coord[1] = Buffer_Receive_Coord[iProcessor * 2 + 1];
+    if (Coord[0] > TPCoord[0]) {
+      TPCoord[0] = Coord[0];
+      TPCoord[1] = Coord[1];
+    }
   }
 
-  delete[] Buffer_Send_Coord;   delete[] Buffer_Receive_Coord;
+  delete[] Buffer_Send_Coord;
+  delete[] Buffer_Receive_Coord;
 
 #endif
 
-
   Chord = 0.0;
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
     if (config->GetMarker_All_DV(iMarker) == YES) {
       for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
         Coord_ = boundary->vertex[iMarker][iVertex]->GetCoord();
         Distance = sqrt(pow(Coord_[0] - TPCoord[0], 2.0) + pow(Coord_[1] - TPCoord[1], 2.0));
-        if (Chord < Distance) { Chord = Distance; LPCoord[0] = Coord_[0]; LPCoord[1] = Coord_[1]; }
+        if (Chord < Distance) {
+          Chord = Distance;
+          LPCoord[0] = Coord_[0];
+          LPCoord[1] = Coord_[1];
+        }
       }
     }
   }
 
 #ifdef HAVE_MPI
 
-  Buffer_Receive_Coord = new su2double [nProcessor*2];
-  Buffer_Send_Coord = new su2double [2];
+  Buffer_Receive_Coord = new su2double[nProcessor * 2];
+  Buffer_Send_Coord = new su2double[2];
 
-  Buffer_Send_Coord[0] = LPCoord[0]; Buffer_Send_Coord[1] = LPCoord[1];
+  Buffer_Send_Coord[0] = LPCoord[0];
+  Buffer_Send_Coord[1] = LPCoord[1];
 
   SU2_MPI::Allgather(Buffer_Send_Coord, 2, MPI_DOUBLE, Buffer_Receive_Coord, 2, MPI_DOUBLE, SU2_MPI::GetComm());
 
   Chord = 0.0;
   for (iProcessor = 0; iProcessor < nProcessor; iProcessor++) {
-    Coord[0] = Buffer_Receive_Coord[iProcessor*2 + 0];
-    Coord[1] = Buffer_Receive_Coord[iProcessor*2 + 1];
+    Coord[0] = Buffer_Receive_Coord[iProcessor * 2 + 0];
+    Coord[1] = Buffer_Receive_Coord[iProcessor * 2 + 1];
     Distance = sqrt(pow(Coord[0] - TPCoord[0], 2.0) + pow(Coord[1] - TPCoord[1], 2.0));
-    if (Chord < Distance) { Chord = Distance; LPCoord[0] = Coord[0]; LPCoord[1] = Coord[1]; }
+    if (Chord < Distance) {
+      Chord = Distance;
+      LPCoord[0] = Coord[0];
+      LPCoord[1] = Coord[1];
+    }
   }
 
-  delete[] Buffer_Send_Coord;   delete[] Buffer_Receive_Coord;
+  delete[] Buffer_Send_Coord;
+  delete[] Buffer_Receive_Coord;
 
 #endif
 
-  AoA = atan((LPCoord[1] - TPCoord[1]) / (TPCoord[0] - LPCoord[0]))*180/PI_NUMBER;
+  AoA = atan((LPCoord[1] - TPCoord[1]) / (TPCoord[0] - LPCoord[0])) * 180 / PI_NUMBER;
 
   /*--- WARNING: AoA currently overwritten to zero. ---*/
   AoA = 0.0;
 
   /*--- Perform multiple airfoil deformation ---*/
 
-  su2double Ampl = config->GetDV_Value(iDV)*Scale;
+  su2double Ampl = config->GetDV_Value(iDV) * Scale;
   su2double KulfanNum = config->GetParamDV(iDV, 1) - 1.0;
   su2double maxKulfanNum = config->GetParamDV(iDV, 2) - 1.0;
   if (KulfanNum < 0) {
@@ -2949,80 +3072,88 @@ void CSurfaceMovement::SetCST(CGeometry *boundary, CConfig *config, unsigned sho
     std::cout << "Warning: Kulfan number should be less than provided maximum." << std::endl;
   }
 
-  if (config->GetParamDV(iDV, 0) == NO) { upper = false;}
-  if (config->GetParamDV(iDV, 0) == YES) { upper = true;}
+  if (config->GetParamDV(iDV, 0) == NO) {
+    upper = false;
+  }
+  if (config->GetParamDV(iDV, 0) == YES) {
+    upper = true;
+  }
 
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-
     for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
-      VarCoord[0] = 0.0; VarCoord[1] = 0.0; VarCoord[2] = 0.0;
+      VarCoord[0] = 0.0;
+      VarCoord[1] = 0.0;
+      VarCoord[2] = 0.0;
 
       if (config->GetMarker_All_DV(iMarker) == YES) {
-
         Coord_ = boundary->vertex[iMarker][iVertex]->GetCoord();
         Normal_ = boundary->vertex[iMarker][iVertex]->GetNormal();
 
         /*--- The CST functions should be applied to a basic airfoil without AoA,
          and unitary chord, a tranformation is required ---*/
 
-        ValCos = cos(AoA*PI_NUMBER/180.0);
-        ValSin = sin(AoA*PI_NUMBER/180.0);
+        ValCos = cos(AoA * PI_NUMBER / 180.0);
+        ValSin = sin(AoA * PI_NUMBER / 180.0);
 
-        Coord[0] = Coord_[0]*ValCos - Coord_[1]*ValSin;
-        Coord[0] = max(0.0, Coord[0]); // Coord x should be always positive
-        Coord[1] = Coord_[1]*ValCos + Coord_[0]*ValSin;
+        Coord[0] = Coord_[0] * ValCos - Coord_[1] * ValSin;
+        Coord[0] = max(0.0, Coord[0]);  // Coord x should be always positive
+        Coord[1] = Coord_[1] * ValCos + Coord_[0] * ValSin;
 
-        Normal[0] = Normal_[0]*ValCos - Normal_[1]*ValSin;
-        Normal[1] = Normal_[1]*ValCos + Normal_[0]*ValSin;
+        Normal[0] = Normal_[0] * ValCos - Normal_[1] * ValSin;
+        Normal[1] = Normal_[1] * ValCos + Normal_[0] * ValSin;
 
         /*--- CST computation ---*/
         su2double fact_n = 1;
         su2double fact_cst = 1;
         su2double fact_cst_n = 1;
 
-  for (int i = 1; i <= maxKulfanNum; i++) {
-    fact_n = fact_n * i;
-  }
-  for (int i = 1; i <= KulfanNum; i++) {
-    fact_cst = fact_cst * i;
-  }
-  for (int i = 1; i <= maxKulfanNum - KulfanNum; i++) {
-    fact_cst_n = fact_cst_n * i;
-  }
-
-  // CST method only for 2D NACA type airfoils
-  su2double N1, N2;
-  N1 = 0.5;
-  N2 = 1.0;
-
-  /*--- Upper and lower surface change in coordinates based on CST equations by Kulfan et. al (www.brendakulfan.com/docs/CST3.pdf)  ---*/
-        fk = pow(Coord[0],N1)*pow((1-Coord[0]), N2) * fact_n/(fact_cst*(fact_cst_n)) * pow(Coord[0], KulfanNum) * pow((1-Coord[0]), (maxKulfanNum-(KulfanNum)));
+        for (int i = 1; i <= maxKulfanNum; i++) {
+          fact_n = fact_n * i;
+        }
+        for (int i = 1; i <= KulfanNum; i++) {
+          fact_cst = fact_cst * i;
+        }
+        for (int i = 1; i <= maxKulfanNum - KulfanNum; i++) {
+          fact_cst_n = fact_cst_n * i;
+        }
 
-  if (( upper) && (Normal[1] > 0)) { VarCoord[1] =  Ampl*fk; }
+        // CST method only for 2D NACA type airfoils
+        su2double N1, N2;
+        N1 = 0.5;
+        N2 = 1.0;
 
-        if ((!upper) && (Normal[1] < 0)) { VarCoord[1] =  Ampl*fk; }
+        /*--- Upper and lower surface change in coordinates based on CST equations by Kulfan et. al
+         * (www.brendakulfan.com/docs/CST3.pdf)  ---*/
+        fk = pow(Coord[0], N1) * pow((1 - Coord[0]), N2) * fact_n / (fact_cst * (fact_cst_n)) *
+             pow(Coord[0], KulfanNum) * pow((1 - Coord[0]), (maxKulfanNum - (KulfanNum)));
 
+        if ((upper) && (Normal[1] > 0)) {
+          VarCoord[1] = Ampl * fk;
+        }
 
-  }
+        if ((!upper) && (Normal[1] < 0)) {
+          VarCoord[1] = Ampl * fk;
+        }
+      }
 
       /*--- Apply the transformation to the coordinate variation ---*/
 
-      ValCos = cos(-AoA*PI_NUMBER/180.0);
-      ValSin = sin(-AoA*PI_NUMBER/180.0);
+      ValCos = cos(-AoA * PI_NUMBER / 180.0);
+      ValSin = sin(-AoA * PI_NUMBER / 180.0);
 
-      VarCoord_[0] = VarCoord[0]*ValCos - VarCoord[1]*ValSin;
-      VarCoord_[1] = VarCoord[1]*ValCos + VarCoord[0]*ValSin;
+      VarCoord_[0] = VarCoord[0] * ValCos - VarCoord[1] * ValSin;
+      VarCoord_[1] = VarCoord[1] * ValCos + VarCoord[0] * ValSin;
 
-            boundary->vertex[iMarker][iVertex]->AddVarCoord(VarCoord_);
+      boundary->vertex[iMarker][iVertex]->AddVarCoord(VarCoord_);
     }
   }
 }
 
-void CSurfaceMovement::SetRotation(CGeometry *boundary, CConfig *config, unsigned short iDV, bool ResetDef) {
+void CSurfaceMovement::SetRotation(CGeometry* boundary, CConfig* config, unsigned short iDV, bool ResetDef) {
   unsigned long iVertex;
   unsigned short iMarker;
-  su2double VarCoord[3] = {0.0,0.0,0.0}, *Coord;
-  su2double movement[3] = {0.0,0.0,0.0}, x, y, z;
+  su2double VarCoord[3] = {0.0, 0.0, 0.0}, *Coord;
+  su2double movement[3] = {0.0, 0.0, 0.0}, x, y, z;
   su2double Scale = config->GetOpt_RelaxFactor();
 
   /*--- Reset airfoil deformation if first deformation or if it required by the solver ---*/
@@ -3030,7 +3161,9 @@ void CSurfaceMovement::SetRotation(CGeometry *boundary, CConfig *config, unsigne
   if ((iDV == 0) || (ResetDef == true)) {
     for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++)
       for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
-        VarCoord[0] = 0.0; VarCoord[1] = 0.0; VarCoord[2] = 0.0;
+        VarCoord[0] = 0.0;
+        VarCoord[1] = 0.0;
+        VarCoord[2] = 0.0;
         boundary->vertex[iMarker][iVertex]->SetVarCoord(VarCoord);
       }
   }
@@ -3040,70 +3173,81 @@ void CSurfaceMovement::SetRotation(CGeometry *boundary, CConfig *config, unsigne
   su2double a = config->GetParamDV(iDV, 0);
   su2double b = config->GetParamDV(iDV, 1);
   su2double c = 0.0;
-  if (boundary->GetnDim() == 3) c = config->GetParamDV(0,2);
+  if (boundary->GetnDim() == 3) c = config->GetParamDV(0, 2);
 
   /*--- xyz-coordinate of the line's direction vector. ---*/
 
-  su2double u = config->GetParamDV(iDV, 3)-config->GetParamDV(iDV, 0);
-  su2double v = config->GetParamDV(iDV, 4)-config->GetParamDV(iDV, 1);
+  su2double u = config->GetParamDV(iDV, 3) - config->GetParamDV(iDV, 0);
+  su2double v = config->GetParamDV(iDV, 4) - config->GetParamDV(iDV, 1);
   su2double w = 1.0;
-  if (boundary->GetnDim() == 3) w = config->GetParamDV(iDV, 5)-config->GetParamDV(iDV, 2);
+  if (boundary->GetnDim() == 3) w = config->GetParamDV(iDV, 5) - config->GetParamDV(iDV, 2);
 
   /*--- The angle of rotation. ---*/
 
-  su2double theta = config->GetDV_Value(iDV)*Scale*PI_NUMBER/180.0;
+  su2double theta = config->GetDV_Value(iDV) * Scale * PI_NUMBER / 180.0;
 
   /*--- An intermediate value used in computations. ---*/
 
-  su2double u2=u*u; su2double v2=v*v; su2double w2=w*w;
-  su2double cosT = cos(theta); su2double sinT = sin(theta);
-  su2double l2 = u2 + v2 + w2; su2double l = sqrt(l2);
+  su2double u2 = u * u;
+  su2double v2 = v * v;
+  su2double w2 = w * w;
+  su2double cosT = cos(theta);
+  su2double sinT = sin(theta);
+  su2double l2 = u2 + v2 + w2;
+  su2double l = sqrt(l2);
 
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++)
     for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
-      VarCoord[0] = 0.0; VarCoord[1] = 0.0; VarCoord[2] = 0.0;
+      VarCoord[0] = 0.0;
+      VarCoord[1] = 0.0;
+      VarCoord[2] = 0.0;
       if (config->GetMarker_All_DV(iMarker) == YES) {
         Coord = boundary->vertex[iMarker][iVertex]->GetCoord();
-        x = Coord[0]; y = Coord[1]; z = Coord[2];
-
-        movement[0] = a*(v2 + w2) + u*(-b*v - c*w + u*x + v*y + w*z)
-        + (-a*(v2 + w2) + u*(b*v + c*w - v*y - w*z) + (v2 + w2)*x)*cosT
-        + l*(-c*v + b*w - w*y + v*z)*sinT;
-        movement[0] = movement[0]/l2 - x;
-
-        movement[1] = b*(u2 + w2) + v*(-a*u - c*w + u*x + v*y + w*z)
-        + (-b*(u2 + w2) + v*(a*u + c*w - u*x - w*z) + (u2 + w2)*y)*cosT
-        + l*(c*u - a*w + w*x - u*z)*sinT;
-        movement[1] = movement[1]/l2 - y;
-
-        movement[2] = c*(u2 + v2) + w*(-a*u - b*v + u*x + v*y + w*z)
-        + (-c*(u2 + v2) + w*(a*u + b*v - u*x - v*y) + (u2 + v2)*z)*cosT
-        + l*(-b*u + a*v - v*x + u*y)*sinT;
-        if (boundary->GetnDim() == 3) movement[2] = movement[2]/l2 - z;
-        else movement[2] = 0.0;
+        x = Coord[0];
+        y = Coord[1];
+        z = Coord[2];
+
+        movement[0] = a * (v2 + w2) + u * (-b * v - c * w + u * x + v * y + w * z) +
+                      (-a * (v2 + w2) + u * (b * v + c * w - v * y - w * z) + (v2 + w2) * x) * cosT +
+                      l * (-c * v + b * w - w * y + v * z) * sinT;
+        movement[0] = movement[0] / l2 - x;
+
+        movement[1] = b * (u2 + w2) + v * (-a * u - c * w + u * x + v * y + w * z) +
+                      (-b * (u2 + w2) + v * (a * u + c * w - u * x - w * z) + (u2 + w2) * y) * cosT +
+                      l * (c * u - a * w + w * x - u * z) * sinT;
+        movement[1] = movement[1] / l2 - y;
+
+        movement[2] = c * (u2 + v2) + w * (-a * u - b * v + u * x + v * y + w * z) +
+                      (-c * (u2 + v2) + w * (a * u + b * v - u * x - v * y) + (u2 + v2) * z) * cosT +
+                      l * (-b * u + a * v - v * x + u * y) * sinT;
+        if (boundary->GetnDim() == 3)
+          movement[2] = movement[2] / l2 - z;
+        else
+          movement[2] = 0.0;
 
         VarCoord[0] = movement[0];
         VarCoord[1] = movement[1];
         if (boundary->GetnDim() == 3) VarCoord[2] = movement[2];
-
       }
       boundary->vertex[iMarker][iVertex]->AddVarCoord(VarCoord);
     }
 }
 
-void CSurfaceMovement::SetTranslation(CGeometry *boundary, CConfig *config, unsigned short iDV, bool ResetDef) {
+void CSurfaceMovement::SetTranslation(CGeometry* boundary, CConfig* config, unsigned short iDV, bool ResetDef) {
   unsigned long iVertex;
   unsigned short iMarker;
-  su2double VarCoord[3] = {0.0,0.0,0.0};
+  su2double VarCoord[3] = {0.0, 0.0, 0.0};
   su2double Scale = config->GetOpt_RelaxFactor();
-  su2double Ampl = config->GetDV_Value(iDV)*Scale;
+  su2double Ampl = config->GetDV_Value(iDV) * Scale;
 
   /*--- Reset airfoil deformation if first deformation or if it required by the solver ---*/
 
   if ((iDV == 0) || (ResetDef == true)) {
     for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++)
       for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
-        VarCoord[0] = 0.0; VarCoord[1] = 0.0; VarCoord[2] = 0.0;
+        VarCoord[0] = 0.0;
+        VarCoord[1] = 0.0;
+        VarCoord[2] = 0.0;
         boundary->vertex[iMarker][iVertex]->SetVarCoord(VarCoord);
       }
   }
@@ -3115,59 +3259,66 @@ void CSurfaceMovement::SetTranslation(CGeometry *boundary, CConfig *config, unsi
 
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++)
     for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
-      VarCoord[0] = 0.0; VarCoord[1] = 0.0; VarCoord[2] = 0.0;
+      VarCoord[0] = 0.0;
+      VarCoord[1] = 0.0;
+      VarCoord[2] = 0.0;
       if (config->GetMarker_All_DV(iMarker) == YES) {
-        VarCoord[0] = Ampl*xDispl;
-        VarCoord[1] = Ampl*yDispl;
-        if (boundary->GetnDim() == 3) VarCoord[2] = Ampl*zDispl;
+        VarCoord[0] = Ampl * xDispl;
+        VarCoord[1] = Ampl * yDispl;
+        if (boundary->GetnDim() == 3) VarCoord[2] = Ampl * zDispl;
       }
       boundary->vertex[iMarker][iVertex]->AddVarCoord(VarCoord);
     }
-
 }
 
-void CSurfaceMovement::SetScale(CGeometry *boundary, CConfig *config, unsigned short iDV, bool ResetDef) {
+void CSurfaceMovement::SetScale(CGeometry* boundary, CConfig* config, unsigned short iDV, bool ResetDef) {
   unsigned long iVertex;
   unsigned short iMarker;
-  su2double VarCoord[3] = {0.0,0.0,0.0}, x, y, z, *Coord;
+  su2double VarCoord[3] = {0.0, 0.0, 0.0}, x, y, z, *Coord;
   su2double Scale = config->GetOpt_RelaxFactor();
-  su2double Ampl = config->GetDV_Value(iDV)*Scale;
+  su2double Ampl = config->GetDV_Value(iDV) * Scale;
 
   /*--- Reset airfoil deformation if first deformation or if it required by the solver ---*/
 
   if ((iDV == 0) || (ResetDef == true)) {
     for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++)
       for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
-        VarCoord[0] = 0.0; VarCoord[1] = 0.0; VarCoord[2] = 0.0;
+        VarCoord[0] = 0.0;
+        VarCoord[1] = 0.0;
+        VarCoord[2] = 0.0;
         boundary->vertex[iMarker][iVertex]->SetVarCoord(VarCoord);
       }
   }
 
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++)
     for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
-      VarCoord[0] = 0.0; VarCoord[1] = 0.0; VarCoord[2] = 0.0;
+      VarCoord[0] = 0.0;
+      VarCoord[1] = 0.0;
+      VarCoord[2] = 0.0;
       if (config->GetMarker_All_DV(iMarker) == YES) {
         Coord = boundary->vertex[iMarker][iVertex]->GetCoord();
-        x = Coord[0]; y = Coord[1]; z = Coord[2];
-        VarCoord[0] = (Ampl-1.0)*x;
-        VarCoord[1] = (Ampl-1.0)*y;
-        if (boundary->GetnDim() == 3) VarCoord[2] = (Ampl-1.0)*z;
+        x = Coord[0];
+        y = Coord[1];
+        z = Coord[2];
+        VarCoord[0] = (Ampl - 1.0) * x;
+        VarCoord[1] = (Ampl - 1.0) * y;
+        if (boundary->GetnDim() == 3) VarCoord[2] = (Ampl - 1.0) * z;
       }
       boundary->vertex[iMarker][iVertex]->AddVarCoord(VarCoord);
     }
-
 }
 
-void CSurfaceMovement::AeroelasticDeform(CGeometry *geometry, CConfig *config, unsigned long TimeIter, unsigned short iMarker, unsigned short iMarker_Monitoring, vector<su2double>& displacements) {
-
+void CSurfaceMovement::AeroelasticDeform(CGeometry* geometry, CConfig* config, unsigned long TimeIter,
+                                         unsigned short iMarker, unsigned short iMarker_Monitoring,
+                                         vector<su2double>& displacements) {
   /* The sign conventions of these are those of the Typical Section Wing Model, below the signs are corrected */
-  su2double dh = -displacements[0];           // relative plunge
-  su2double dalpha = -displacements[1];       // relative pitch
+  su2double dh = -displacements[0];      // relative plunge
+  su2double dalpha = -displacements[1];  // relative pitch
   su2double dh_x, dh_y;
   su2double Center[2];
   unsigned short iDim;
   su2double Lref = config->GetLength_Ref();
-  su2double *Coord;
+  su2double* Coord;
   unsigned long iPoint, iVertex;
   su2double x_new, y_new;
   su2double VarCoord[3];
@@ -3177,24 +3328,22 @@ void CSurfaceMovement::AeroelasticDeform(CGeometry *geometry, CConfig *config, u
   if (config->GetKind_GridMovement() == AEROELASTIC_RIGID_MOTION) {
     su2double Omega, dt, psi;
     dt = config->GetDelta_UnstTimeND();
-    Omega = config->GetRotation_Rate(2)/config->GetOmega_Ref();
-    psi = Omega*(dt*TimeIter);
+    Omega = config->GetRotation_Rate(2) / config->GetOmega_Ref();
+    psi = Omega * (dt * TimeIter);
 
     /*--- Correct for the airfoil starting position (This is hardcoded in here) ---*/
     if (Monitoring_Tag == "Airfoil1") {
       psi = psi + 0.0;
-    }
-    else if (Monitoring_Tag == "Airfoil2") {
-      psi = psi + 2.0/3.0*PI_NUMBER;
-    }
-    else if (Monitoring_Tag == "Airfoil3") {
-      psi = psi + 4.0/3.0*PI_NUMBER;
-    }
-    else
-      cout << "WARNING: There is a marker that we are monitoring that doesn't match the values hardcoded above!" << endl;
+    } else if (Monitoring_Tag == "Airfoil2") {
+      psi = psi + 2.0 / 3.0 * PI_NUMBER;
+    } else if (Monitoring_Tag == "Airfoil3") {
+      psi = psi + 4.0 / 3.0 * PI_NUMBER;
+    } else
+      cout << "WARNING: There is a marker that we are monitoring that doesn't match the values hardcoded above!"
+           << endl;
 
-    dh_x = -dh*sin(psi);
-    dh_y = dh*cos(psi);
+    dh_x = -dh * sin(psi);
+    dh_y = dh * cos(psi);
 
   } else {
     dh_x = 0;
@@ -3212,15 +3361,14 @@ void CSurfaceMovement::AeroelasticDeform(CGeometry *geometry, CConfig *config, u
     Coord = geometry->nodes->GetCoord(iPoint);
 
     /*--- Calculate non-dim. position from rotation center ---*/
-    su2double r[2] = {0,0};
-    for (iDim = 0; iDim < geometry->GetnDim(); iDim++)
-        r[iDim] = (Coord[iDim]-Center[iDim])/Lref;
+    su2double r[2] = {0, 0};
+    for (iDim = 0; iDim < geometry->GetnDim(); iDim++) r[iDim] = (Coord[iDim] - Center[iDim]) / Lref;
 
     /*--- Compute delta of transformed point coordinates ---*/
     // The deltas are needed for the FEA grid deformation Method.
     // rotation contribution - previous position + plunging contribution
-    x_new = cos(dalpha)*r[0] - sin(dalpha)*r[1] -r[0] + dh_x;
-    y_new = sin(dalpha)*r[0] + cos(dalpha)*r[1] -r[1] + dh_y;
+    x_new = cos(dalpha) * r[0] - sin(dalpha) * r[1] - r[0] + dh_x;
+    y_new = sin(dalpha) * r[0] + cos(dalpha) * r[1] - r[1] + dh_y;
 
     VarCoord[0] = x_new;
     VarCoord[1] = y_new;
@@ -3230,20 +3378,17 @@ void CSurfaceMovement::AeroelasticDeform(CGeometry *geometry, CConfig *config, u
     geometry->vertex[iMarker][iVertex]->SetVarCoord(VarCoord);
   }
   /*--- Set the elastic axis to the new location after incrementing the position with the plunge ---*/
-  config->SetRefOriginMoment_X(iMarker_Monitoring, Center[0]+dh_x);
-  config->SetRefOriginMoment_Y(iMarker_Monitoring, Center[1]+dh_y);
-
-
+  config->SetRefOriginMoment_X(iMarker_Monitoring, Center[0] + dh_x);
+  config->SetRefOriginMoment_Y(iMarker_Monitoring, Center[1] + dh_y);
 }
 
-void CSurfaceMovement::SetBoundary_Flutter3D(CGeometry *geometry, CConfig *config,
-                                             CFreeFormDefBox **FFDBox, unsigned long iter, unsigned short iZone) {
-
+void CSurfaceMovement::SetBoundary_Flutter3D(CGeometry* geometry, CConfig* config, CFreeFormDefBox** FFDBox,
+                                             unsigned long iter, unsigned short iZone) {
   su2double omega, deltaT;
   su2double alpha, alpha_new, alpha_old;
   su2double time_new, time_old;
   su2double Omega[3], Ampl[3];
-  su2double DEG2RAD = PI_NUMBER/180.0;
+  su2double DEG2RAD = PI_NUMBER / 180.0;
   bool adjoint = (config->GetContinuous_Adjoint() || config->GetDiscrete_Adjoint());
   unsigned short iDim = 0;
 
@@ -3253,50 +3398,49 @@ void CSurfaceMovement::SetBoundary_Flutter3D(CGeometry *geometry, CConfig *confi
 
   /*--- Pitching origin, frequency, and amplitude from config. ---*/
 
-  for (iDim = 0; iDim < 3; iDim++){
-    Omega[iDim] = config->GetPitching_Omega(iDim)/config->GetOmega_Ref();
-    Ampl[iDim] = config->GetPitching_Ampl(iDim)*DEG2RAD;
+  for (iDim = 0; iDim < 3; iDim++) {
+    Omega[iDim] = config->GetPitching_Omega(iDim) / config->GetOmega_Ref();
+    Ampl[iDim] = config->GetPitching_Ampl(iDim) * DEG2RAD;
   }
 
   /*--- Compute delta time based on physical time step ---*/
 
   if (adjoint) {
-
     /*--- For the unsteady adjoint, we integrate backwards through
      physical time, so perform mesh motion in reverse. ---*/
 
-    unsigned long nFlowIter  = config->GetnTime_Iter();
+    unsigned long nFlowIter = config->GetnTime_Iter();
     unsigned long directIter = nFlowIter - iter - 1;
-    time_new = static_cast<su2double>(directIter)*deltaT;
+    time_new = static_cast<su2double>(directIter) * deltaT;
     time_old = time_new;
-    if (iter != 0) time_old = (static_cast<su2double>(directIter)+1.0)*deltaT;
+    if (iter != 0) time_old = (static_cast<su2double>(directIter) + 1.0) * deltaT;
   } else {
-
     /*--- Forward time for the direct problem ---*/
 
-    time_new = static_cast<su2double>(iter)*deltaT;
+    time_new = static_cast<su2double>(iter) * deltaT;
     time_old = time_new;
-    if (iter != 0) time_old = (static_cast<su2double>(iter)-1.0)*deltaT;
+    if (iter != 0) time_old = (static_cast<su2double>(iter) - 1.0) * deltaT;
   }
 
   /*--- Update the pitching angle at this time step. Flip sign for
    nose-up positive convention. ---*/
 
-  omega     = Omega[2];
-  alpha_new = Ampl[2]*sin(omega*time_new);
-  alpha_old = Ampl[2]*sin(omega*time_old);
-  alpha     = (1E-10 + (alpha_new - alpha_old))*(-PI_NUMBER/180.0);
+  omega = Omega[2];
+  alpha_new = Ampl[2] * sin(omega * time_new);
+  alpha_old = Ampl[2] * sin(omega * time_old);
+  alpha = (1E-10 + (alpha_new - alpha_old)) * (-PI_NUMBER / 180.0);
 
-  if (rank == MASTER_NODE)
-    cout << "New dihedral angle (alpha): " << alpha_new/DEG2RAD << " degrees." << endl;
+  if (rank == MASTER_NODE) cout << "New dihedral angle (alpha): " << alpha_new / DEG2RAD << " degrees." << endl;
 
   unsigned short iOrder, jOrder, kOrder;
   short iFFDBox;
-  su2double movement[3] = {0.0,0.0,0.0};
-  bool *move = new bool [nFFDBox];
-  unsigned short *index = new unsigned short[3];
+  su2double movement[3] = {0.0, 0.0, 0.0};
+  bool* move = new bool[nFFDBox];
+  unsigned short* index = new unsigned short[3];
 
-  move[0] = true; move[1] = true; move[2] = true;
+  move[0] = true;
+  move[1] = true;
+  move[2] = true;
 
   /*--- Change the value of the control point if move is true ---*/
 
@@ -3305,33 +3449,35 @@ void CSurfaceMovement::SetBoundary_Flutter3D(CGeometry *geometry, CConfig *confi
       for (iOrder = 0; iOrder < FFDBox[iFFDBox]->GetlOrder(); iOrder++)
         for (jOrder = 0; jOrder < FFDBox[iFFDBox]->GetmOrder(); jOrder++)
           for (kOrder = 0; kOrder < FFDBox[iFFDBox]->GetnOrder(); kOrder++) {
-            index[0] = iOrder; index[1] = jOrder; index[2] = kOrder;
-            su2double *coord = FFDBox[iFFDBox]->GetCoordControlPoints(iOrder, jOrder, kOrder);
-            movement[0] = 0.0; movement[1] = 0.0; movement[2] = coord[1]*tan(alpha);
+            index[0] = iOrder;
+            index[1] = jOrder;
+            index[2] = kOrder;
+            su2double* coord = FFDBox[iFFDBox]->GetCoordControlPoints(iOrder, jOrder, kOrder);
+            movement[0] = 0.0;
+            movement[1] = 0.0;
+            movement[2] = coord[1] * tan(alpha);
             FFDBox[iFFDBox]->SetControlPoints(index, movement);
           }
 
   /*--- Recompute cartesian coordinates using the new control points position ---*/
 
-  for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++)
-    SetCartesianCoord(geometry, config, FFDBox[iFFDBox], iFFDBox, false);
-
-  delete [] index;
-  delete [] move;
+  for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) SetCartesianCoord(geometry, config, FFDBox[iFFDBox], iFFDBox, false);
 
+  delete[] index;
+  delete[] move;
 }
 
-void CSurfaceMovement::SetExternal_Deformation(CGeometry *geometry, CConfig *config, unsigned short iZone, unsigned long iter) {
-
+void CSurfaceMovement::SetExternal_Deformation(CGeometry* geometry, CConfig* config, unsigned short iZone,
+                                               unsigned long iter) {
   /*--- Local variables ---*/
 
   unsigned short iDim, nDim;
   unsigned long iPoint = 0, flowIter = 0;
   unsigned long jPoint, GlobalIndex;
-  su2double VarCoord[3], *Coord_Old = nullptr, *Coord_New = nullptr, Center[3] = {0.0,0.0,0.0};
-  su2double Lref   = config->GetLength_Ref();
-  su2double NewCoord[3] = {0.0,0.0,0.0}, rotMatrix[3][3] = {{0.0,0.0,0.0}, {0.0,0.0,0.0}, {0.0,0.0,0.0}};
-  su2double r[3] = {0.0,0.0,0.0}, rotCoord[3] = {0.0,0.0,0.0};
+  su2double VarCoord[3], *Coord_Old = nullptr, *Coord_New = nullptr, Center[3] = {0.0, 0.0, 0.0};
+  su2double Lref = config->GetLength_Ref();
+  su2double NewCoord[3] = {0.0, 0.0, 0.0}, rotMatrix[3][3] = {{0.0, 0.0, 0.0}, {0.0, 0.0, 0.0}, {0.0, 0.0, 0.0}};
+  su2double r[3] = {0.0, 0.0, 0.0}, rotCoord[3] = {0.0, 0.0, 0.0};
   unsigned long iVertex;
   unsigned short iMarker;
   char buffer[50];
@@ -3352,14 +3498,18 @@ void CSurfaceMovement::SetExternal_Deformation(CGeometry *geometry, CConfig *con
       /*--- For the unsteady adjoint, we integrate backwards through
        physical time, so perform mesh motion in reverse. ---*/
       unsigned long nFlowIter = config->GetnTime_Iter() - 1;
-      flowIter  = nFlowIter - iter;
+      flowIter = nFlowIter - iter;
       unsigned short lastindex = DV_Filename.find_last_of(".");
       DV_Filename = DV_Filename.substr(0, lastindex);
-      if ((SU2_TYPE::Int(flowIter) >= 0) && (SU2_TYPE::Int(flowIter) < 10)) SPRINTF (buffer, "_0000%d.dat", SU2_TYPE::Int(flowIter));
-      if ((SU2_TYPE::Int(flowIter) >= 10) && (SU2_TYPE::Int(flowIter) < 100)) SPRINTF (buffer, "_000%d.dat", SU2_TYPE::Int(flowIter));
-      if ((SU2_TYPE::Int(flowIter) >= 100) && (SU2_TYPE::Int(flowIter) < 1000)) SPRINTF (buffer, "_00%d.dat", SU2_TYPE::Int(flowIter));
-      if ((SU2_TYPE::Int(flowIter) >= 1000) && (SU2_TYPE::Int(flowIter) < 10000)) SPRINTF (buffer, "_0%d.dat", SU2_TYPE::Int(flowIter));
-      if (SU2_TYPE::Int(flowIter) >= 10000) SPRINTF (buffer, "_%d.dat", SU2_TYPE::Int(flowIter));
+      if ((SU2_TYPE::Int(flowIter) >= 0) && (SU2_TYPE::Int(flowIter) < 10))
+        SPRINTF(buffer, "_0000%d.dat", SU2_TYPE::Int(flowIter));
+      if ((SU2_TYPE::Int(flowIter) >= 10) && (SU2_TYPE::Int(flowIter) < 100))
+        SPRINTF(buffer, "_000%d.dat", SU2_TYPE::Int(flowIter));
+      if ((SU2_TYPE::Int(flowIter) >= 100) && (SU2_TYPE::Int(flowIter) < 1000))
+        SPRINTF(buffer, "_00%d.dat", SU2_TYPE::Int(flowIter));
+      if ((SU2_TYPE::Int(flowIter) >= 1000) && (SU2_TYPE::Int(flowIter) < 10000))
+        SPRINTF(buffer, "_0%d.dat", SU2_TYPE::Int(flowIter));
+      if (SU2_TYPE::Int(flowIter) >= 10000) SPRINTF(buffer, "_%d.dat", SU2_TYPE::Int(flowIter));
       UnstExt = string(buffer);
       DV_Filename.append(UnstExt);
     } else {
@@ -3367,11 +3517,15 @@ void CSurfaceMovement::SetExternal_Deformation(CGeometry *geometry, CConfig *con
       flowIter = iter;
       unsigned short lastindex = DV_Filename.find_last_of(".");
       DV_Filename = DV_Filename.substr(0, lastindex);
-      if ((SU2_TYPE::Int(flowIter) >= 0) && (SU2_TYPE::Int(flowIter) < 10)) SPRINTF (buffer, "_0000%d.dat", SU2_TYPE::Int(flowIter));
-      if ((SU2_TYPE::Int(flowIter) >= 10) && (SU2_TYPE::Int(flowIter) < 100)) SPRINTF (buffer, "_000%d.dat", SU2_TYPE::Int(flowIter));
-      if ((SU2_TYPE::Int(flowIter) >= 100) && (SU2_TYPE::Int(flowIter) < 1000)) SPRINTF (buffer, "_00%d.dat", SU2_TYPE::Int(flowIter));
-      if ((SU2_TYPE::Int(flowIter) >= 1000) && (SU2_TYPE::Int(flowIter) < 10000)) SPRINTF (buffer, "_0%d.dat", SU2_TYPE::Int(flowIter));
-      if (SU2_TYPE::Int(flowIter) >= 10000) SPRINTF (buffer, "_%d.dat", SU2_TYPE::Int(flowIter));
+      if ((SU2_TYPE::Int(flowIter) >= 0) && (SU2_TYPE::Int(flowIter) < 10))
+        SPRINTF(buffer, "_0000%d.dat", SU2_TYPE::Int(flowIter));
+      if ((SU2_TYPE::Int(flowIter) >= 10) && (SU2_TYPE::Int(flowIter) < 100))
+        SPRINTF(buffer, "_000%d.dat", SU2_TYPE::Int(flowIter));
+      if ((SU2_TYPE::Int(flowIter) >= 100) && (SU2_TYPE::Int(flowIter) < 1000))
+        SPRINTF(buffer, "_00%d.dat", SU2_TYPE::Int(flowIter));
+      if ((SU2_TYPE::Int(flowIter) >= 1000) && (SU2_TYPE::Int(flowIter) < 10000))
+        SPRINTF(buffer, "_0%d.dat", SU2_TYPE::Int(flowIter));
+      if (SU2_TYPE::Int(flowIter) >= 10000) SPRINTF(buffer, "_%d.dat", SU2_TYPE::Int(flowIter));
       UnstExt = string(buffer);
       DV_Filename.append(UnstExt);
     }
@@ -3418,7 +3572,6 @@ void CSurfaceMovement::SetExternal_Deformation(CGeometry *geometry, CConfig *con
   /*--- If rotating as well, prepare the rotation matrix ---*/
 
   if (config->GetKind_GridMovement() == EXTERNAL_ROTATION) {
-
     /*--- Variables needed only for rotation ---*/
 
     su2double Omega[3], dt;
@@ -3432,17 +3585,18 @@ void CSurfaceMovement::SetExternal_Deformation(CGeometry *geometry, CConfig *con
 
     /*--- Angular velocity vector from config ---*/
 
-    dt = static_cast<su2double>(iter)*config->GetDelta_UnstTimeND();
-    Omega[0]  = config->GetRotation_Rate(0);
-    Omega[1]  = config->GetRotation_Rate(1);
-    Omega[2]  = config->GetRotation_Rate(2);
+    dt = static_cast<su2double>(iter) * config->GetDelta_UnstTimeND();
+    Omega[0] = config->GetRotation_Rate(0);
+    Omega[1] = config->GetRotation_Rate(1);
+    Omega[2] = config->GetRotation_Rate(2);
 
     /*--- For the unsteady adjoint, use reverse time ---*/
     if (adjoint) {
       /*--- Set the first adjoint mesh position to the final direct one ---*/
-      if (iter == 0) dt = ((su2double)config->GetnTime_Iter()-1) * dt;
+      if (iter == 0) dt = ((su2double)config->GetnTime_Iter() - 1) * dt;
       /*--- Reverse the rotation direction for the adjoint ---*/
-      else dt = -1.0*dt;
+      else
+        dt = -1.0 * dt;
     } else {
       /*--- No rotation at all for the first direct solution ---*/
       if (iter == 0) dt = 0;
@@ -3450,30 +3604,33 @@ void CSurfaceMovement::SetExternal_Deformation(CGeometry *geometry, CConfig *con
 
     /*--- Compute delta change in the angle about the x, y, & z axes. ---*/
 
-    dtheta = Omega[0]*dt;
-    dphi   = Omega[1]*dt;
-    dpsi   = Omega[2]*dt;
+    dtheta = Omega[0] * dt;
+    dphi = Omega[1] * dt;
+    dpsi = Omega[2] * dt;
 
     /*--- Store angles separately for clarity. Compute sines/cosines. ---*/
 
-    cosTheta = cos(dtheta);  cosPhi = cos(dphi);  cosPsi = cos(dpsi);
-    sinTheta = sin(dtheta);  sinPhi = sin(dphi);  sinPsi = sin(dpsi);
+    cosTheta = cos(dtheta);
+    cosPhi = cos(dphi);
+    cosPsi = cos(dpsi);
+    sinTheta = sin(dtheta);
+    sinPhi = sin(dphi);
+    sinPsi = sin(dpsi);
 
     /*--- Compute the rotation matrix. Note that the implicit
      ordering is rotation about the x-axis, y-axis, then z-axis. ---*/
 
-    rotMatrix[0][0] = cosPhi*cosPsi;
-    rotMatrix[1][0] = cosPhi*sinPsi;
+    rotMatrix[0][0] = cosPhi * cosPsi;
+    rotMatrix[1][0] = cosPhi * sinPsi;
     rotMatrix[2][0] = -sinPhi;
 
-    rotMatrix[0][1] = sinTheta*sinPhi*cosPsi - cosTheta*sinPsi;
-    rotMatrix[1][1] = sinTheta*sinPhi*sinPsi + cosTheta*cosPsi;
-    rotMatrix[2][1] = sinTheta*cosPhi;
-
-    rotMatrix[0][2] = cosTheta*sinPhi*cosPsi + sinTheta*sinPsi;
-    rotMatrix[1][2] = cosTheta*sinPhi*sinPsi - sinTheta*cosPsi;
-    rotMatrix[2][2] = cosTheta*cosPhi;
+    rotMatrix[0][1] = sinTheta * sinPhi * cosPsi - cosTheta * sinPsi;
+    rotMatrix[1][1] = sinTheta * sinPhi * sinPsi + cosTheta * cosPsi;
+    rotMatrix[2][1] = sinTheta * cosPhi;
 
+    rotMatrix[0][2] = cosTheta * sinPhi * cosPsi + sinTheta * sinPsi;
+    rotMatrix[1][2] = cosTheta * sinPhi * sinPsi - sinTheta * cosPsi;
+    rotMatrix[2][2] = cosTheta * cosPhi;
   }
 
   /*--- Loop through to find only moving surface markers ---*/
@@ -3481,7 +3638,6 @@ void CSurfaceMovement::SetExternal_Deformation(CGeometry *geometry, CConfig *con
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
     if ((config->GetMarker_All_DV(iMarker) == YES && config->GetKind_SU2() == SU2_COMPONENT::SU2_DEF) ||
         (config->GetMarker_All_Moving(iMarker) == YES && config->GetKind_SU2() == SU2_COMPONENT::SU2_CFD)) {
-
       /*--- Loop over all surface points for this marker ---*/
 
       for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
@@ -3497,115 +3653,115 @@ void CSurfaceMovement::SetExternal_Deformation(CGeometry *geometry, CConfig *con
          Coord_Old have already been rotated using SetRigid_Rotation(). ---*/
 
         if (config->GetKind_GridMovement() == EXTERNAL_ROTATION) {
-
           /*--- Calculate non-dim. position from rotation center ---*/
 
-          for (iDim = 0; iDim < nDim; iDim++)
-            r[iDim] = (Coord_New[iDim]-Center[iDim])/Lref;
+          for (iDim = 0; iDim < nDim; iDim++) r[iDim] = (Coord_New[iDim] - Center[iDim]) / Lref;
           if (nDim == 2) r[nDim] = 0.0;
 
           /*--- Compute transformed point coordinates ---*/
 
-          rotCoord[0] = rotMatrix[0][0]*r[0]
-                      + rotMatrix[0][1]*r[1]
-                      + rotMatrix[0][2]*r[2] + Center[0];
+          rotCoord[0] = rotMatrix[0][0] * r[0] + rotMatrix[0][1] * r[1] + rotMatrix[0][2] * r[2] + Center[0];
 
-          rotCoord[1] = rotMatrix[1][0]*r[0]
-                      + rotMatrix[1][1]*r[1]
-                      + rotMatrix[1][2]*r[2] + Center[1];
+          rotCoord[1] = rotMatrix[1][0] * r[0] + rotMatrix[1][1] * r[1] + rotMatrix[1][2] * r[2] + Center[1];
 
-          rotCoord[2] = rotMatrix[2][0]*r[0]
-                      + rotMatrix[2][1]*r[1]
-                      + rotMatrix[2][2]*r[2] + Center[2];
+          rotCoord[2] = rotMatrix[2][0] * r[0] + rotMatrix[2][1] * r[1] + rotMatrix[2][2] * r[2] + Center[2];
 
           /*--- Copy rotated coords back to original array for consistency ---*/
-          for (iDim = 0; iDim < nDim; iDim++)
-            Coord_New[iDim] = rotCoord[iDim];
+          for (iDim = 0; iDim < nDim; iDim++) Coord_New[iDim] = rotCoord[iDim];
         }
 
         /*--- Calculate delta change in the x, y, & z directions ---*/
-        for (iDim = 0; iDim < nDim; iDim++)
-          VarCoord[iDim] = (Coord_New[iDim]-Coord_Old[iDim])/Lref;
+        for (iDim = 0; iDim < nDim; iDim++) VarCoord[iDim] = (Coord_New[iDim] - Coord_Old[iDim]) / Lref;
         if (nDim == 2) VarCoord[nDim] = 0.0;
 
         /*--- Set position changes to be applied by the spring analogy ---*/
         geometry->vertex[iMarker][iVertex]->SetVarCoord(VarCoord);
-
       }
     }
   }
 }
 
-void CSurfaceMovement::SetNACA_4Digits(CGeometry *boundary, CConfig *config) {
+void CSurfaceMovement::SetNACA_4Digits(CGeometry* boundary, CConfig* config) {
   unsigned long iVertex;
   unsigned short iMarker;
   su2double VarCoord[3], *Coord, *Normal, Ycurv, Yesp;
 
-  if (config->GetnDV() != 1) { cout << "This kind of design variable is not prepared for multiple deformations."; cin.get();  }
+  if (config->GetnDV() != 1) {
+    cout << "This kind of design variable is not prepared for multiple deformations.";
+    cin.get();
+  }
 
-  su2double Ya = config->GetParamDV(0,0) / 100.0; /*--- Maximum camber as a fraction of the chord
-          (100 m is the first of the four digits) ---*/
-  su2double Xa = config->GetParamDV(0,1) / 10.0; /*--- Location of maximum camber as a fraction of
-          the chord (10 p is the second digit in the NACA xxxx description) ---*/
-  su2double t = config->GetParamDV(0,2) / 100.0; /*--- Maximum thickness as a fraction of the
-            chord (so 100 t gives the last two digits in
-            the NACA 4-digit denomination) ---*/
+  su2double Ya = config->GetParamDV(0, 0) / 100.0; /*--- Maximum camber as a fraction of the chord
+           (100 m is the first of the four digits) ---*/
+  su2double Xa = config->GetParamDV(0, 1) / 10.0;  /*--- Location of maximum camber as a fraction of
+            the chord (10 p is the second digit in the NACA xxxx description) ---*/
+  su2double t = config->GetParamDV(0, 2) / 100.0;  /*--- Maximum thickness as a fraction of the
+              chord (so 100 t gives the last two digits in
+              the NACA 4-digit denomination) ---*/
 
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++)
     for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
-      VarCoord[0] = 0.0; VarCoord[1] = 0.0; VarCoord[2] = 0.0;
+      VarCoord[0] = 0.0;
+      VarCoord[1] = 0.0;
+      VarCoord[2] = 0.0;
       if (config->GetMarker_All_DV(iMarker) == YES) {
         Coord = boundary->vertex[iMarker][iVertex]->GetCoord();
         Normal = boundary->vertex[iMarker][iVertex]->GetNormal();
 
-        if (Coord[0] < Xa) Ycurv = (2.0*Xa*Coord[0]-pow(Coord[0],2.0))*(Ya/pow(Xa,2.0));
-        else Ycurv = ((1.0-2.0*Xa)+2.0*Xa*Coord[0]-pow(Coord[0],2.0))*(Ya/pow((1.0-Xa), 2.0));
-
-        Yesp = t*(1.4845*sqrt(Coord[0])-0.6300*Coord[0]-1.7580*pow(Coord[0],2.0)+
-              1.4215*pow(Coord[0],3.0)-0.518*pow(Coord[0],4.0));
+        if (Coord[0] < Xa)
+          Ycurv = (2.0 * Xa * Coord[0] - pow(Coord[0], 2.0)) * (Ya / pow(Xa, 2.0));
+        else
+          Ycurv = ((1.0 - 2.0 * Xa) + 2.0 * Xa * Coord[0] - pow(Coord[0], 2.0)) * (Ya / pow((1.0 - Xa), 2.0));
 
-        if (Normal[1] > 0) VarCoord[1] =  (Ycurv + Yesp) - Coord[1];
-        if (Normal[1] < 0) VarCoord[1] =  (Ycurv - Yesp) - Coord[1];
+        Yesp = t * (1.4845 * sqrt(Coord[0]) - 0.6300 * Coord[0] - 1.7580 * pow(Coord[0], 2.0) +
+                    1.4215 * pow(Coord[0], 3.0) - 0.518 * pow(Coord[0], 4.0));
 
+        if (Normal[1] > 0) VarCoord[1] = (Ycurv + Yesp) - Coord[1];
+        if (Normal[1] < 0) VarCoord[1] = (Ycurv - Yesp) - Coord[1];
       }
       boundary->vertex[iMarker][iVertex]->SetVarCoord(VarCoord);
     }
 }
 
-void CSurfaceMovement::SetParabolic(CGeometry *boundary, CConfig *config) {
+void CSurfaceMovement::SetParabolic(CGeometry* boundary, CConfig* config) {
   unsigned long iVertex;
   unsigned short iMarker;
   su2double VarCoord[3], *Coord, *Normal;
 
-  if (config->GetnDV() != 1) { cout << "This kind of design variable is not prepared for multiple deformations."; cin.get();  }
+  if (config->GetnDV() != 1) {
+    cout << "This kind of design variable is not prepared for multiple deformations.";
+    cin.get();
+  }
 
-  su2double c = config->GetParamDV(0,0); /*--- Center of the parabola ---*/
-  su2double t = config->GetParamDV(0,1) / 100.0; /*--- Thickness of the parabola ---*/
+  su2double c = config->GetParamDV(0, 0);         /*--- Center of the parabola ---*/
+  su2double t = config->GetParamDV(0, 1) / 100.0; /*--- Thickness of the parabola ---*/
 
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++)
     for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
-      VarCoord[0] = 0.0; VarCoord[1] = 0.0; VarCoord[2] = 0.0;
+      VarCoord[0] = 0.0;
+      VarCoord[1] = 0.0;
+      VarCoord[2] = 0.0;
       if (config->GetMarker_All_DV(iMarker) == YES) {
         Coord = boundary->vertex[iMarker][iVertex]->GetCoord();
         Normal = boundary->vertex[iMarker][iVertex]->GetNormal();
 
         if (Normal[1] > 0) {
-          VarCoord[1] =  t*(Coord[0]*Coord[0]-Coord[0])/(2.0*(c*c-c)) - Coord[1];
+          VarCoord[1] = t * (Coord[0] * Coord[0] - Coord[0]) / (2.0 * (c * c - c)) - Coord[1];
         }
         if (Normal[1] < 0) {
-          VarCoord[1] =  t*(Coord[0]-Coord[0]*Coord[0])/(2.0*(c*c-c)) - Coord[1];
+          VarCoord[1] = t * (Coord[0] - Coord[0] * Coord[0]) / (2.0 * (c * c - c)) - Coord[1];
         }
       }
       boundary->vertex[iMarker][iVertex]->SetVarCoord(VarCoord);
     }
 }
 
-void CSurfaceMovement::SetAirfoil(CGeometry *boundary, CConfig *config) {
+void CSurfaceMovement::SetAirfoil(CGeometry* boundary, CConfig* config) {
   unsigned long iVertex, n_Airfoil = 0;
   unsigned short iMarker, nUpper, nLower, iUpper, iLower, iVar, iDim;
   su2double *VarCoord, *Coord, NewYCoord, NewXCoord, *Coord_i, *Coord_ip1, yp1, ypn,
-  Airfoil_Coord[2]= {0.0,0.0}, factor, coeff = 10000, Upper, Lower, Arch = 0.0, TotalArch = 0.0,
-  x_i, x_ip1, y_i, y_ip1;
+      Airfoil_Coord[2] = {0.0, 0.0}, factor, coeff = 10000, Upper, Lower, Arch = 0.0, TotalArch = 0.0, x_i, x_ip1, y_i,
+      y_ip1;
   passivedouble AirfoilScale;
   vector<su2double> Svalue, Xcoord, Ycoord, Xcoord2, Ycoord2, Xcoord_Aux, Ycoord_Aux;
   bool AddBegin = true, AddEnd = true;
@@ -3617,8 +3773,7 @@ void CSurfaceMovement::SetAirfoil(CGeometry *boundary, CConfig *config) {
   unsigned short nDim = boundary->GetnDim();
 
   VarCoord = new su2double[nDim];
-  for (iDim = 0; iDim < nDim; iDim++)
-    VarCoord[iDim] = 0.0;
+  for (iDim = 0; iDim < nDim; iDim++) VarCoord[iDim] = 0.0;
 
   /*--- Get the SU2 module. SU2_CFD will use this routine for dynamically
    deforming meshes (MARKER_MOVING), while SU2_DEF will use it for deforming
@@ -3637,35 +3792,44 @@ void CSurfaceMovement::SetAirfoil(CGeometry *boundary, CConfig *config) {
 
   cout << "Enter the name of file with the airfoil information: ";
   ierr = scanf("%255s", AirfoilFile);
-  if (ierr == 0) { SU2_MPI::Error("No input read!!", CURRENT_FUNCTION); }
+  if (ierr == 0) {
+    SU2_MPI::Error("No input read!!", CURRENT_FUNCTION);
+  }
   airfoil_file.open(AirfoilFile, ios::in);
   if (airfoil_file.fail()) {
     SU2_MPI::Error(string("There is no airfoil file ") + string(AirfoilFile), CURRENT_FUNCTION);
   }
   cout << "Enter the format of the airfoil (Selig or Lednicer): ";
   ierr = scanf("%14s", AirfoilFormat);
-  if (ierr == 0) { SU2_MPI::Error("No input read!!", CURRENT_FUNCTION); }
+  if (ierr == 0) {
+    SU2_MPI::Error("No input read!!", CURRENT_FUNCTION);
+  }
 
   cout << "Thickness scaling (1.0 means no scaling)?: ";
   ierr = scanf("%lf", &AirfoilScale);
-  if (ierr == 0) { SU2_MPI::Error("No input read!!", CURRENT_FUNCTION); }
+  if (ierr == 0) {
+    SU2_MPI::Error("No input read!!", CURRENT_FUNCTION);
+  }
 
   cout << "Close the airfoil (Yes or No)?: ";
   ierr = scanf("%14s", AirfoilClose);
-  if (ierr == 0) { SU2_MPI::Error("No input read!!", CURRENT_FUNCTION); }
+  if (ierr == 0) {
+    SU2_MPI::Error("No input read!!", CURRENT_FUNCTION);
+  }
 
   cout << "Surface mesh orientation (clockwise, or anticlockwise): ";
   ierr = scanf("%14s", MeshOrientation);
-  if (ierr == 0) { SU2_MPI::Error("No input read!!", CURRENT_FUNCTION); }
+  if (ierr == 0) {
+    SU2_MPI::Error("No input read!!", CURRENT_FUNCTION);
+  }
 
   /*--- The first line is the header ---*/
 
-  getline (airfoil_file, text_line);
+  getline(airfoil_file, text_line);
   cout << "File info: " << text_line << endl;
 
-  if (strcmp (AirfoilFormat,"Selig") == 0) {
-
-    while (getline (airfoil_file, text_line)) {
+  if (strcmp(AirfoilFormat, "Selig") == 0) {
+    while (getline(airfoil_file, text_line)) {
       istringstream point_line(text_line);
 
       /*--- Read the x & y coordinates from this line of the file (anticlockwise) ---*/
@@ -3674,19 +3838,18 @@ void CSurfaceMovement::SetAirfoil(CGeometry *boundary, CConfig *config) {
 
       /*--- Close the arifoil ---*/
 
-      if (strcmp (AirfoilClose,"Yes") == 0)
-        factor = -atan(coeff*(Airfoil_Coord[0]-1.0))*2.0/PI_NUMBER;
-      else factor = 1.0;
+      if (strcmp(AirfoilClose, "Yes") == 0)
+        factor = -atan(coeff * (Airfoil_Coord[0] - 1.0)) * 2.0 / PI_NUMBER;
+      else
+        factor = 1.0;
 
       /*--- Store the coordinates in vectors ---*/
 
       Xcoord.push_back(Airfoil_Coord[0]);
-      Ycoord.push_back(Airfoil_Coord[1]*factor*AirfoilScale);
+      Ycoord.push_back(Airfoil_Coord[1] * factor * AirfoilScale);
     }
-
   }
-  if (strcmp (AirfoilFormat,"Lednicer") == 0) {
-
+  if (strcmp(AirfoilFormat, "Lednicer") == 0) {
     /*--- The second line is the number of points ---*/
 
     getline(airfoil_file, text_line);
@@ -3696,82 +3859,96 @@ void CSurfaceMovement::SetAirfoil(CGeometry *boundary, CConfig *config) {
     nUpper = SU2_TYPE::Int(Upper);
     nLower = SU2_TYPE::Int(Lower);
 
-    Xcoord.resize(nUpper+nLower-1);
-    Ycoord.resize(nUpper+nLower-1);
+    Xcoord.resize(nUpper + nLower - 1);
+    Ycoord.resize(nUpper + nLower - 1);
 
     /*--- White line ---*/
 
-    getline (airfoil_file, text_line);
+    getline(airfoil_file, text_line);
 
     for (iUpper = 0; iUpper < nUpper; iUpper++) {
-      getline (airfoil_file, text_line);
+      getline(airfoil_file, text_line);
       istringstream point_line(text_line);
       point_line >> Airfoil_Coord[0] >> Airfoil_Coord[1];
-      Xcoord[nUpper-iUpper-1] = Airfoil_Coord[0];
+      Xcoord[nUpper - iUpper - 1] = Airfoil_Coord[0];
 
-      if (strcmp (AirfoilClose,"Yes") == 0)
-        factor = -atan(coeff*(Airfoil_Coord[0]-1.0))*2.0/PI_NUMBER;
-      else factor = 1.0;
+      if (strcmp(AirfoilClose, "Yes") == 0)
+        factor = -atan(coeff * (Airfoil_Coord[0] - 1.0)) * 2.0 / PI_NUMBER;
+      else
+        factor = 1.0;
 
-      Ycoord[nUpper-iUpper-1] = Airfoil_Coord[1]*AirfoilScale*factor;
+      Ycoord[nUpper - iUpper - 1] = Airfoil_Coord[1] * AirfoilScale * factor;
     }
 
-    getline (airfoil_file, text_line);
+    getline(airfoil_file, text_line);
 
     for (iLower = 0; iLower < nLower; iLower++) {
-      getline (airfoil_file, text_line);
+      getline(airfoil_file, text_line);
       istringstream point_line(text_line);
       point_line >> Airfoil_Coord[0] >> Airfoil_Coord[1];
 
-      if (strcmp (AirfoilClose,"Yes") == 0)
-        factor = -atan(coeff*(Airfoil_Coord[0]-1.0))*2.0/PI_NUMBER;
-      else factor = 1.0;
+      if (strcmp(AirfoilClose, "Yes") == 0)
+        factor = -atan(coeff * (Airfoil_Coord[0] - 1.0)) * 2.0 / PI_NUMBER;
+      else
+        factor = 1.0;
 
-      Xcoord[nUpper+iLower-1] = Airfoil_Coord[0];
-      Ycoord[nUpper+iLower-1] = Airfoil_Coord[1]*AirfoilScale*factor;
+      Xcoord[nUpper + iLower - 1] = Airfoil_Coord[0];
+      Ycoord[nUpper + iLower - 1] = Airfoil_Coord[1] * AirfoilScale * factor;
     }
-
   }
 
   /*--- Check the coordinate (1,0) at the beginning and end of the file ---*/
 
   if (Xcoord[0] == 1.0) AddBegin = false;
-  if (Xcoord[Xcoord.size()-1] == 1.0) AddEnd = false;
+  if (Xcoord[Xcoord.size() - 1] == 1.0) AddEnd = false;
 
-  if (AddBegin) { Xcoord.insert(Xcoord.begin(), 1.0);   Ycoord.insert(Ycoord.begin(), 0.0);}
-  if (AddEnd) { Xcoord.push_back(1.0);                Ycoord.push_back(0.0);}
+  if (AddBegin) {
+    Xcoord.insert(Xcoord.begin(), 1.0);
+    Ycoord.insert(Ycoord.begin(), 0.0);
+  }
+  if (AddEnd) {
+    Xcoord.push_back(1.0);
+    Ycoord.push_back(0.0);
+  }
 
   /*--- Change the orientation (depend on the input file, and the mesh file) ---*/
 
-  if (strcmp (MeshOrientation,"clockwise") == 0) {
+  if (strcmp(MeshOrientation, "clockwise") == 0) {
     for (iVar = 0; iVar < Xcoord.size(); iVar++) {
       Xcoord_Aux.push_back(Xcoord[iVar]);
       Ycoord_Aux.push_back(Ycoord[iVar]);
     }
 
     for (iVar = 0; iVar < Xcoord.size(); iVar++) {
-      Xcoord[iVar] = Xcoord_Aux[Xcoord.size()-iVar-1];
-      Ycoord[iVar] = Ycoord_Aux[Xcoord.size()-iVar-1];
+      Xcoord[iVar] = Xcoord_Aux[Xcoord.size() - iVar - 1];
+      Ycoord[iVar] = Ycoord_Aux[Xcoord.size() - iVar - 1];
     }
   }
 
   /*--- Compute the total arch length ---*/
 
-  Arch = 0.0; Svalue.push_back(Arch);
+  Arch = 0.0;
+  Svalue.push_back(Arch);
 
-  for (iVar = 0; iVar < Xcoord.size()-1; iVar++) {
-    x_i = Xcoord[iVar];  x_ip1 = Xcoord[iVar+1];
-    y_i = Ycoord[iVar];  y_ip1 = Ycoord[iVar+1];
-    Arch += sqrt((x_ip1-x_i)*(x_ip1-x_i)+(y_ip1-y_i)*(y_ip1-y_i));
+  for (iVar = 0; iVar < Xcoord.size() - 1; iVar++) {
+    x_i = Xcoord[iVar];
+    x_ip1 = Xcoord[iVar + 1];
+    y_i = Ycoord[iVar];
+    y_ip1 = Ycoord[iVar + 1];
+    Arch += sqrt((x_ip1 - x_i) * (x_ip1 - x_i) + (y_ip1 - y_i) * (y_ip1 - y_i));
     Svalue.push_back(Arch);
   }
-  x_i = Xcoord[Xcoord.size()-1];  x_ip1 = Xcoord[0];
-  y_i = Ycoord[Xcoord.size()-1];  y_ip1 = Ycoord[0];
-  Arch += sqrt((x_ip1-x_i)*(x_ip1-x_i)+(y_ip1-y_i)*(y_ip1-y_i));
+  x_i = Xcoord[Xcoord.size() - 1];
+  x_ip1 = Xcoord[0];
+  y_i = Ycoord[Xcoord.size() - 1];
+  y_ip1 = Ycoord[0];
+  Arch += sqrt((x_ip1 - x_i) * (x_ip1 - x_i) + (y_ip1 - y_i) * (y_ip1 - y_i));
 
   /*--- Non dimensionalization ---*/
 
-  for (iVar = 0; iVar < Svalue.size(); iVar++) { Svalue[iVar] /= Arch; }
+  for (iVar = 0; iVar < Svalue.size(); iVar++) {
+    Svalue[iVar] /= Arch;
+  }
 
   /*--- Close the restart file ---*/
 
@@ -3780,14 +3957,14 @@ void CSurfaceMovement::SetAirfoil(CGeometry *boundary, CConfig *config) {
   /*--- Create a spline for X and Y coordiantes using the arch length ---*/
 
   n_Airfoil = Svalue.size();
-  yp1 = (Xcoord[1]-Xcoord[0])/(Svalue[1]-Svalue[0]);
-  ypn = (Xcoord[n_Airfoil-1]-Xcoord[n_Airfoil-2])/(Svalue[n_Airfoil-1]-Svalue[n_Airfoil-2]);
+  yp1 = (Xcoord[1] - Xcoord[0]) / (Svalue[1] - Svalue[0]);
+  ypn = (Xcoord[n_Airfoil - 1] - Xcoord[n_Airfoil - 2]) / (Svalue[n_Airfoil - 1] - Svalue[n_Airfoil - 2]);
 
   CCubicSpline splineX(Svalue, Xcoord, CCubicSpline::FIRST, yp1, CCubicSpline::FIRST, ypn);
 
   n_Airfoil = Svalue.size();
-  yp1 = (Ycoord[1]-Ycoord[0])/(Svalue[1]-Svalue[0]);
-  ypn = (Ycoord[n_Airfoil-1]-Ycoord[n_Airfoil-2])/(Svalue[n_Airfoil-1]-Svalue[n_Airfoil-2]);
+  yp1 = (Ycoord[1] - Ycoord[0]) / (Svalue[1] - Svalue[0]);
+  ypn = (Ycoord[n_Airfoil - 1] - Ycoord[n_Airfoil - 2]) / (Svalue[n_Airfoil - 1] - Svalue[n_Airfoil - 2]);
 
   CCubicSpline splineY(Svalue, Ycoord, CCubicSpline::FIRST, yp1, CCubicSpline::FIRST, ypn);
 
@@ -3795,39 +3972,47 @@ void CSurfaceMovement::SetAirfoil(CGeometry *boundary, CConfig *config) {
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
     if (((config->GetMarker_All_Moving(iMarker) == YES) && (Kind_SU2 == SU2_COMPONENT::SU2_CFD)) ||
         ((config->GetMarker_All_DV(iMarker) == YES) && (Kind_SU2 == SU2_COMPONENT::SU2_DEF))) {
-      for (iVertex = 0; iVertex < boundary->nVertex[iMarker]-1; iVertex++) {
+      for (iVertex = 0; iVertex < boundary->nVertex[iMarker] - 1; iVertex++) {
         Coord_i = boundary->vertex[iMarker][iVertex]->GetCoord();
-        Coord_ip1 = boundary->vertex[iMarker][iVertex+1]->GetCoord();
+        Coord_ip1 = boundary->vertex[iMarker][iVertex + 1]->GetCoord();
 
-        x_i = Coord_i[0]; x_ip1 = Coord_ip1[0];
-        y_i = Coord_i[1]; y_ip1 = Coord_ip1[1];
+        x_i = Coord_i[0];
+        x_ip1 = Coord_ip1[0];
+        y_i = Coord_i[1];
+        y_ip1 = Coord_ip1[1];
 
-        TotalArch += sqrt((x_ip1-x_i)*(x_ip1-x_i)+(y_ip1-y_i)*(y_ip1-y_i));
+        TotalArch += sqrt((x_ip1 - x_i) * (x_ip1 - x_i) + (y_ip1 - y_i) * (y_ip1 - y_i));
       }
-      Coord_i = boundary->vertex[iMarker][boundary->nVertex[iMarker]-1]->GetCoord();
+      Coord_i = boundary->vertex[iMarker][boundary->nVertex[iMarker] - 1]->GetCoord();
       Coord_ip1 = boundary->vertex[iMarker][0]->GetCoord();
-      x_i = Coord_i[0]; x_ip1 = Coord_ip1[0];
-      y_i = Coord_i[1]; y_ip1 = Coord_ip1[1];
-      TotalArch += sqrt((x_ip1-x_i)*(x_ip1-x_i)+(y_ip1-y_i)*(y_ip1-y_i));
+      x_i = Coord_i[0];
+      x_ip1 = Coord_ip1[0];
+      y_i = Coord_i[1];
+      y_ip1 = Coord_ip1[1];
+      TotalArch += sqrt((x_ip1 - x_i) * (x_ip1 - x_i) + (y_ip1 - y_i) * (y_ip1 - y_i));
     }
   }
 
-
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
     Arch = 0.0;
     for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
-      VarCoord[0] = 0.0; VarCoord[1] = 0.0; VarCoord[2] = 0.0;
+      VarCoord[0] = 0.0;
+      VarCoord[1] = 0.0;
+      VarCoord[2] = 0.0;
       if (((config->GetMarker_All_Moving(iMarker) == YES) && (Kind_SU2 == SU2_COMPONENT::SU2_CFD)) ||
           ((config->GetMarker_All_DV(iMarker) == YES) && (Kind_SU2 == SU2_COMPONENT::SU2_DEF))) {
         Coord = boundary->vertex[iMarker][iVertex]->GetCoord();
 
-        if (iVertex == 0) Arch = 0.0;
+        if (iVertex == 0)
+          Arch = 0.0;
         else {
-          Coord_i = boundary->vertex[iMarker][iVertex-1]->GetCoord();
+          Coord_i = boundary->vertex[iMarker][iVertex - 1]->GetCoord();
           Coord_ip1 = boundary->vertex[iMarker][iVertex]->GetCoord();
-          x_i = Coord_i[0]; x_ip1 = Coord_ip1[0];
-          y_i = Coord_i[1]; y_ip1 = Coord_ip1[1];
-          Arch += sqrt((x_ip1-x_i)*(x_ip1-x_i)+(y_ip1-y_i)*(y_ip1-y_i))/TotalArch;
+          x_i = Coord_i[0];
+          x_ip1 = Coord_ip1[0];
+          y_i = Coord_i[1];
+          y_ip1 = Coord_ip1[1];
+          Arch += sqrt((x_ip1 - x_i) * (x_ip1 - x_i) + (y_ip1 - y_i) * (y_ip1 - y_i)) / TotalArch;
         }
 
         NewXCoord = splineX(Arch);
@@ -3840,24 +4025,21 @@ void CSurfaceMovement::SetAirfoil(CGeometry *boundary, CConfig *config) {
       }
 
       boundary->vertex[iMarker][iVertex]->SetVarCoord(VarCoord);
-
     }
   }
 
-  delete [] VarCoord;
-
+  delete[] VarCoord;
 }
 
-void CSurfaceMovement::ReadFFDInfo(CGeometry *geometry, CConfig *config, CFreeFormDefBox **FFDBox, string val_mesh_filename) {
-
+void CSurfaceMovement::ReadFFDInfo(CGeometry* geometry, CConfig* config, CFreeFormDefBox** FFDBox,
+                                   string val_mesh_filename) {
   string text_line, iTag;
   ifstream mesh_file;
-  su2double CPcoord[3], coord[] = {0,0,0};
-  unsigned short degree[3], iFFDBox, iCornerPoints, iControlPoints, iMarker, iDegree, jDegree, kDegree,
-  iChar, LevelFFDBox, nParentFFDBox, iParentFFDBox, nChildFFDBox, iChildFFDBox, nMarker, *nCornerPoints,
-  *nControlPoints;
-  unsigned long iSurfacePoints, iPoint, jPoint, iVertex, nVertex, nPoint, iElem = 0,
-  nElem, my_nSurfPoints, nSurfPoints, *nSurfacePoints;
+  su2double CPcoord[3], coord[] = {0, 0, 0};
+  unsigned short degree[3], iFFDBox, iCornerPoints, iControlPoints, iMarker, iDegree, jDegree, kDegree, iChar,
+      LevelFFDBox, nParentFFDBox, iParentFFDBox, nChildFFDBox, iChildFFDBox, nMarker, *nCornerPoints, *nControlPoints;
+  unsigned long iSurfacePoints, iPoint, jPoint, iVertex, nVertex, nPoint, iElem = 0, nElem, my_nSurfPoints, nSurfPoints,
+                                                                          *nSurfacePoints;
   su2double XCoord, YCoord;
 
   bool polar = (config->GetFFD_CoordSystem() == POLAR);
@@ -3870,13 +4052,13 @@ void CSurfaceMovement::ReadFFDInfo(CGeometry *geometry, CConfig *config, CFreeFo
     SU2_MPI::Error("There is no geometry file (ReadFFDInfo)!!", CURRENT_FUNCTION);
   }
 
-  while (getline (mesh_file, text_line)) {
-
+  while (getline(mesh_file, text_line)) {
     /*--- Read the inner elements ---*/
 
-    string::size_type position = text_line.find ("NELEM=",0);
+    string::size_type position = text_line.find("NELEM=", 0);
     if (position != string::npos) {
-      text_line.erase (0,6); nElem = atoi(text_line.c_str());
+      text_line.erase(0, 6);
+      nElem = atoi(text_line.c_str());
       for (iElem = 0; iElem < nElem; iElem++) {
         getline(mesh_file, text_line);
       }
@@ -3884,9 +4066,10 @@ void CSurfaceMovement::ReadFFDInfo(CGeometry *geometry, CConfig *config, CFreeFo
 
     /*--- Read the inner points ---*/
 
-    position = text_line.find ("NPOIN=",0);
+    position = text_line.find("NPOIN=", 0);
     if (position != string::npos) {
-      text_line.erase (0,6); nPoint = atoi(text_line.c_str());
+      text_line.erase(0, 6);
+      nPoint = atoi(text_line.c_str());
       for (iPoint = 0; iPoint < nPoint; iPoint++) {
         getline(mesh_file, text_line);
       }
@@ -3894,13 +4077,15 @@ void CSurfaceMovement::ReadFFDInfo(CGeometry *geometry, CConfig *config, CFreeFo
 
     /*--- Read the boundaries  ---*/
 
-    position = text_line.find ("NMARK=",0);
+    position = text_line.find("NMARK=", 0);
     if (position != string::npos) {
-      text_line.erase (0,6); nMarker = atoi(text_line.c_str());
+      text_line.erase(0, 6);
+      nMarker = atoi(text_line.c_str());
       for (iMarker = 0; iMarker < nMarker; iMarker++) {
         getline(mesh_file, text_line);
         getline(mesh_file, text_line);
-        text_line.erase (0,13); nVertex = atoi(text_line.c_str());
+        text_line.erase(0, 13);
+        nVertex = atoi(text_line.c_str());
         for (iVertex = 0; iVertex < nVertex; iVertex++) {
           getline(mesh_file, text_line);
         }
@@ -3909,9 +4094,9 @@ void CSurfaceMovement::ReadFFDInfo(CGeometry *geometry, CConfig *config, CFreeFo
 
     /*--- Read the FFDBox information  ---*/
 
-    position = text_line.find ("FFD_NBOX=",0);
+    position = text_line.find("FFD_NBOX=", 0);
     if (position != string::npos) {
-      text_line.erase (0,9);
+      text_line.erase(0, 9);
       nFFDBox = atoi(text_line.c_str());
 
       if (rank == MASTER_NODE) cout << nFFDBox << " Free Form Deformation boxes." << endl;
@@ -3920,126 +4105,138 @@ void CSurfaceMovement::ReadFFDInfo(CGeometry *geometry, CConfig *config, CFreeFo
       nControlPoints = new unsigned short[nFFDBox];
       nSurfacePoints = new unsigned long[nFFDBox];
 
-      getline (mesh_file, text_line);
-      text_line.erase (0,11);
+      getline(mesh_file, text_line);
+      text_line.erase(0, 11);
       nLevel = atoi(text_line.c_str());
 
       if (rank == MASTER_NODE) cout << nLevel << " Free Form Deformation nested levels." << endl;
 
-      for (iFFDBox = 0 ; iFFDBox < nFFDBox; iFFDBox++) {
-
+      for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) {
         /*--- Read the name of the FFD box ---*/
 
-        getline (mesh_file, text_line);
-        text_line.erase (0,8);
+        getline(mesh_file, text_line);
+        text_line.erase(0, 8);
 
         /*--- Remove extra data from the FFDBox name ---*/
 
         string::size_type position;
         for (iChar = 0; iChar < 20; iChar++) {
-          position = text_line.find( " ", 0 );
-          if (position != string::npos) text_line.erase (position,1);
-          position = text_line.find( "\r", 0 );
-          if (position != string::npos) text_line.erase (position,1);
-          position = text_line.find( "\n", 0 );
-          if (position != string::npos) text_line.erase (position,1);
+          position = text_line.find(" ", 0);
+          if (position != string::npos) text_line.erase(position, 1);
+          position = text_line.find("\r", 0);
+          if (position != string::npos) text_line.erase(position, 1);
+          position = text_line.find("\n", 0);
+          if (position != string::npos) text_line.erase(position, 1);
         }
 
         string TagFFDBox = text_line.c_str();
 
-        if (rank == MASTER_NODE) cout << "FFD box tag: " << TagFFDBox <<". ";
+        if (rank == MASTER_NODE) cout << "FFD box tag: " << TagFFDBox << ". ";
 
         /*--- Read the level of the FFD box ---*/
 
-        getline (mesh_file, text_line);
-        text_line.erase (0,10);
+        getline(mesh_file, text_line);
+        text_line.erase(0, 10);
         LevelFFDBox = atoi(text_line.c_str());
 
-        if (rank == MASTER_NODE) cout << "FFD box level: " << LevelFFDBox <<". ";
+        if (rank == MASTER_NODE) cout << "FFD box level: " << LevelFFDBox << ". ";
 
         /*--- Read the degree of the FFD box ---*/
 
-
         if (nDim == 2) {
           if (polar) {
-            getline (mesh_file, text_line);
-            text_line.erase (0,13); degree[0] = atoi(text_line.c_str());
+            getline(mesh_file, text_line);
+            text_line.erase(0, 13);
+            degree[0] = atoi(text_line.c_str());
             degree[1] = 1;
-            getline (mesh_file, text_line);
-            text_line.erase (0,13); degree[2] = atoi(text_line.c_str());
-          }
-          else {
-            getline (mesh_file, text_line);
-            text_line.erase (0,13); degree[0] = atoi(text_line.c_str());
-            getline (mesh_file, text_line);
-            text_line.erase (0,13); degree[1] = atoi(text_line.c_str());
+            getline(mesh_file, text_line);
+            text_line.erase(0, 13);
+            degree[2] = atoi(text_line.c_str());
+          } else {
+            getline(mesh_file, text_line);
+            text_line.erase(0, 13);
+            degree[0] = atoi(text_line.c_str());
+            getline(mesh_file, text_line);
+            text_line.erase(0, 13);
+            degree[1] = atoi(text_line.c_str());
             degree[2] = 1;
           }
-        }
-        else {
-          getline (mesh_file, text_line);
-          text_line.erase (0,13); degree[0] = atoi(text_line.c_str());
-          getline (mesh_file, text_line);
-          text_line.erase (0,13); degree[1] = atoi(text_line.c_str());
-          getline (mesh_file, text_line);
-          text_line.erase (0,13); degree[2] = atoi(text_line.c_str());
+        } else {
+          getline(mesh_file, text_line);
+          text_line.erase(0, 13);
+          degree[0] = atoi(text_line.c_str());
+          getline(mesh_file, text_line);
+          text_line.erase(0, 13);
+          degree[1] = atoi(text_line.c_str());
+          getline(mesh_file, text_line);
+          text_line.erase(0, 13);
+          degree[2] = atoi(text_line.c_str());
         }
 
         if (rank == MASTER_NODE) {
           if (nDim == 2) {
-            if (polar) cout << "Degrees: " << degree[0] << ", " << degree[2] << "." << endl;
-            else cout << "Degrees: " << degree[0] << ", " << degree[1] << "." << endl;
-          }
-          else cout << "Degrees: " << degree[0] << ", " << degree[1] << ", " << degree[2] << "." << endl;
+            if (polar)
+              cout << "Degrees: " << degree[0] << ", " << degree[2] << "." << endl;
+            else
+              cout << "Degrees: " << degree[0] << ", " << degree[1] << "." << endl;
+          } else
+            cout << "Degrees: " << degree[0] << ", " << degree[1] << ", " << degree[2] << "." << endl;
         }
 
-        getline (mesh_file, text_line);
-        if (text_line.substr(0,12) != "FFD_BLENDING"){
-          SU2_MPI::Error(string("Deprecated FFD information found in mesh file.\n") +
-                         string("FFD information generated with SU2 version <= 4.3 is incompatible with the current version.") +
-                         string("Run SU2_DEF again with DV_KIND= FFD_SETTING."), CURRENT_FUNCTION);
+        getline(mesh_file, text_line);
+        if (text_line.substr(0, 12) != "FFD_BLENDING") {
+          SU2_MPI::Error(
+              string("Deprecated FFD information found in mesh file.\n") +
+                  string(
+                      "FFD information generated with SU2 version <= 4.3 is incompatible with the current version.") +
+                  string("Run SU2_DEF again with DV_KIND= FFD_SETTING."),
+              CURRENT_FUNCTION);
         }
-        text_line.erase(0,14);
-        if (text_line == "BEZIER"){
+        text_line.erase(0, 14);
+        if (text_line == "BEZIER") {
           Blending = BEZIER;
         }
-        if (text_line == "BSPLINE_UNIFORM"){
+        if (text_line == "BSPLINE_UNIFORM") {
           Blending = BSPLINE_UNIFORM;
         }
 
         if (Blending == BSPLINE_UNIFORM) {
-          getline (mesh_file, text_line);
-          text_line.erase (0,17); SplineOrder[0] = atoi(text_line.c_str());
-          getline (mesh_file, text_line);
-          text_line.erase (0,17); SplineOrder[1] = atoi(text_line.c_str());
-          if (nDim == 3){
-            getline (mesh_file, text_line);
-            text_line.erase (0,17); SplineOrder[2] = atoi(text_line.c_str());
+          getline(mesh_file, text_line);
+          text_line.erase(0, 17);
+          SplineOrder[0] = atoi(text_line.c_str());
+          getline(mesh_file, text_line);
+          text_line.erase(0, 17);
+          SplineOrder[1] = atoi(text_line.c_str());
+          if (nDim == 3) {
+            getline(mesh_file, text_line);
+            text_line.erase(0, 17);
+            SplineOrder[2] = atoi(text_line.c_str());
           } else {
             SplineOrder[2] = 2;
           }
         }
-        if (rank == MASTER_NODE){
-          if (Blending == BSPLINE_UNIFORM){
+        if (rank == MASTER_NODE) {
+          if (Blending == BSPLINE_UNIFORM) {
             cout << "FFD Blending using B-Splines. ";
             cout << "Order: " << SplineOrder[0] << ", " << SplineOrder[1];
             if (nDim == 3) cout << ", " << SplineOrder[2];
             cout << ". " << endl;
           }
-          if (Blending == BEZIER){
+          if (Blending == BEZIER) {
             cout << "FFD Blending using Bezier Curves." << endl;
           }
         }
 
         FFDBox[iFFDBox] = new CFreeFormDefBox(degree, SplineOrder, Blending);
-        FFDBox[iFFDBox]->SetTag(TagFFDBox); FFDBox[iFFDBox]->SetLevel(LevelFFDBox);
+        FFDBox[iFFDBox]->SetTag(TagFFDBox);
+        FFDBox[iFFDBox]->SetLevel(LevelFFDBox);
 
         /*--- Read the number of parents boxes ---*/
 
-        getline (mesh_file, text_line);
-        text_line.erase (0,12);
+        getline(mesh_file, text_line);
+        text_line.erase(0, 12);
         nParentFFDBox = atoi(text_line.c_str());
-        if (rank == MASTER_NODE) cout << "Number of parent boxes: " << nParentFFDBox <<". ";
+        if (rank == MASTER_NODE) cout << "Number of parent boxes: " << nParentFFDBox << ". ";
         for (iParentFFDBox = 0; iParentFFDBox < nParentFFDBox; iParentFFDBox++) {
           getline(mesh_file, text_line);
 
@@ -4047,12 +4244,12 @@ void CSurfaceMovement::ReadFFDInfo(CGeometry *geometry, CConfig *config, CFreeFo
 
           string::size_type position;
           for (iChar = 0; iChar < 20; iChar++) {
-            position = text_line.find( " ", 0 );
-            if (position != string::npos) text_line.erase (position,1);
-            position = text_line.find( "\r", 0 );
-            if (position != string::npos) text_line.erase (position,1);
-            position = text_line.find( "\n", 0 );
-            if (position != string::npos) text_line.erase (position,1);
+            position = text_line.find(" ", 0);
+            if (position != string::npos) text_line.erase(position, 1);
+            position = text_line.find("\r", 0);
+            if (position != string::npos) text_line.erase(position, 1);
+            position = text_line.find("\n", 0);
+            if (position != string::npos) text_line.erase(position, 1);
           }
 
           string ParentFFDBox = text_line.c_str();
@@ -4061,10 +4258,10 @@ void CSurfaceMovement::ReadFFDInfo(CGeometry *geometry, CConfig *config, CFreeFo
 
         /*--- Read the number of children boxes ---*/
 
-        getline (mesh_file, text_line);
-        text_line.erase (0,13);
+        getline(mesh_file, text_line);
+        text_line.erase(0, 13);
         nChildFFDBox = atoi(text_line.c_str());
-        if (rank == MASTER_NODE) cout << "Number of child boxes: " << nChildFFDBox <<"." << endl;
+        if (rank == MASTER_NODE) cout << "Number of child boxes: " << nChildFFDBox << "." << endl;
 
         for (iChildFFDBox = 0; iChildFFDBox < nChildFFDBox; iChildFFDBox++) {
           getline(mesh_file, text_line);
@@ -4073,12 +4270,12 @@ void CSurfaceMovement::ReadFFDInfo(CGeometry *geometry, CConfig *config, CFreeFo
 
           string::size_type position;
           for (iChar = 0; iChar < 20; iChar++) {
-            position = text_line.find( " ", 0 );
-            if (position != string::npos) text_line.erase (position,1);
-            position = text_line.find( "\r", 0 );
-            if (position != string::npos) text_line.erase (position,1);
-            position = text_line.find( "\n", 0 );
-            if (position != string::npos) text_line.erase (position,1);
+            position = text_line.find(" ", 0);
+            if (position != string::npos) text_line.erase(position, 1);
+            position = text_line.find("\r", 0);
+            if (position != string::npos) text_line.erase(position, 1);
+            position = text_line.find("\n", 0);
+            if (position != string::npos) text_line.erase(position, 1);
           }
 
           string ChildFFDBox = text_line.c_str();
@@ -4087,103 +4284,113 @@ void CSurfaceMovement::ReadFFDInfo(CGeometry *geometry, CConfig *config, CFreeFo
 
         /*--- Read the number of the corner points ---*/
 
-        getline (mesh_file, text_line);
-        text_line.erase (0,18); nCornerPoints[iFFDBox] = atoi(text_line.c_str());
-        if (rank == MASTER_NODE) cout << "Corner points: " << nCornerPoints[iFFDBox] <<". ";
-        if (nDim == 2) nCornerPoints[iFFDBox] = nCornerPoints[iFFDBox]*SU2_TYPE::Int(2);
-
-
+        getline(mesh_file, text_line);
+        text_line.erase(0, 18);
+        nCornerPoints[iFFDBox] = atoi(text_line.c_str());
+        if (rank == MASTER_NODE) cout << "Corner points: " << nCornerPoints[iFFDBox] << ". ";
+        if (nDim == 2) nCornerPoints[iFFDBox] = nCornerPoints[iFFDBox] * SU2_TYPE::Int(2);
 
         /*--- Read the coordinates of the corner points ---*/
 
-
         if (nDim == 2) {
-
           if (polar) {
-
-            getline(mesh_file, text_line); istringstream FFDBox_line_1(text_line);
-            FFDBox_line_1 >> XCoord; FFDBox_line_1 >> YCoord;
+            getline(mesh_file, text_line);
+            istringstream FFDBox_line_1(text_line);
+            FFDBox_line_1 >> XCoord;
+            FFDBox_line_1 >> YCoord;
 
             CPcoord[0] = XCoord;
-            CPcoord[1] = cos(0.1)*YCoord;
-            CPcoord[2] = -sin(0.1)*YCoord;
+            CPcoord[1] = cos(0.1) * YCoord;
+            CPcoord[2] = -sin(0.1) * YCoord;
             FFDBox[iFFDBox]->SetCoordCornerPoints(coord, 4);
 
             CPcoord[0] = XCoord;
-            CPcoord[1] = cos(0.1)*YCoord;
-            CPcoord[2] = sin(0.1)*YCoord;
+            CPcoord[1] = cos(0.1) * YCoord;
+            CPcoord[2] = sin(0.1) * YCoord;
             FFDBox[iFFDBox]->SetCoordCornerPoints(coord, 7);
 
-            getline(mesh_file, text_line); istringstream FFDBox_line_2(text_line);
-            FFDBox_line_2 >> XCoord; FFDBox_line_2 >> YCoord;
+            getline(mesh_file, text_line);
+            istringstream FFDBox_line_2(text_line);
+            FFDBox_line_2 >> XCoord;
+            FFDBox_line_2 >> YCoord;
 
             CPcoord[0] = XCoord;
-            CPcoord[1] = cos(0.1)*YCoord;
-            CPcoord[2] = -sin(0.1)*YCoord;
+            CPcoord[1] = cos(0.1) * YCoord;
+            CPcoord[2] = -sin(0.1) * YCoord;
             FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, 0);
 
             CPcoord[0] = XCoord;
-            CPcoord[1] = cos(0.1)*YCoord;
-            CPcoord[2] = sin(0.1)*YCoord;
+            CPcoord[1] = cos(0.1) * YCoord;
+            CPcoord[2] = sin(0.1) * YCoord;
             FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, 3);
 
-            getline(mesh_file, text_line); istringstream FFDBox_line_3(text_line);
-            FFDBox_line_3 >> XCoord; FFDBox_line_3 >> YCoord;
+            getline(mesh_file, text_line);
+            istringstream FFDBox_line_3(text_line);
+            FFDBox_line_3 >> XCoord;
+            FFDBox_line_3 >> YCoord;
 
             CPcoord[0] = XCoord;
-            CPcoord[1] = cos(0.1)*YCoord;
-            CPcoord[2] = -sin(0.1)*YCoord;
+            CPcoord[1] = cos(0.1) * YCoord;
+            CPcoord[2] = -sin(0.1) * YCoord;
             FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, 1);
 
             CPcoord[0] = XCoord;
-            CPcoord[1] = cos(0.1)*YCoord;
-            CPcoord[2] = sin(0.1)*YCoord;
+            CPcoord[1] = cos(0.1) * YCoord;
+            CPcoord[2] = sin(0.1) * YCoord;
             FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, 2);
 
-            getline(mesh_file, text_line); istringstream FFDBox_line_4(text_line);
-            FFDBox_line_4 >> XCoord; FFDBox_line_4 >> YCoord;
+            getline(mesh_file, text_line);
+            istringstream FFDBox_line_4(text_line);
+            FFDBox_line_4 >> XCoord;
+            FFDBox_line_4 >> YCoord;
 
             CPcoord[0] = XCoord;
-            CPcoord[1] = cos(0.1)*YCoord;
-            CPcoord[2] = -sin(0.1)*YCoord;
+            CPcoord[1] = cos(0.1) * YCoord;
+            CPcoord[2] = -sin(0.1) * YCoord;
             FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, 5);
 
             CPcoord[0] = XCoord;
-            CPcoord[1] = cos(0.1)*YCoord;
-            CPcoord[2] = sin(0.1)*YCoord;
+            CPcoord[1] = cos(0.1) * YCoord;
+            CPcoord[2] = sin(0.1) * YCoord;
             FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, 6);
 
-          }
-          else {
+          } else {
             for (iCornerPoints = 0; iCornerPoints < nCornerPoints[iFFDBox]; iCornerPoints++) {
-              if (iCornerPoints < nCornerPoints[iFFDBox]/SU2_TYPE::Int(2)) {
-                getline(mesh_file, text_line); istringstream FFDBox_line(text_line);
-                FFDBox_line >> CPcoord[0]; FFDBox_line >> CPcoord[1]; CPcoord[2] = -0.5;
-              }
-              else {
-                CPcoord[0] = FFDBox[iFFDBox]->GetCoordCornerPoints(0, iCornerPoints-nCornerPoints[iFFDBox]/SU2_TYPE::Int(2));
-                CPcoord[1] = FFDBox[iFFDBox]->GetCoordCornerPoints(1, iCornerPoints-nCornerPoints[iFFDBox]/SU2_TYPE::Int(2));
+              if (iCornerPoints < nCornerPoints[iFFDBox] / SU2_TYPE::Int(2)) {
+                getline(mesh_file, text_line);
+                istringstream FFDBox_line(text_line);
+                FFDBox_line >> CPcoord[0];
+                FFDBox_line >> CPcoord[1];
+                CPcoord[2] = -0.5;
+              } else {
+                CPcoord[0] =
+                    FFDBox[iFFDBox]->GetCoordCornerPoints(0, iCornerPoints - nCornerPoints[iFFDBox] / SU2_TYPE::Int(2));
+                CPcoord[1] =
+                    FFDBox[iFFDBox]->GetCoordCornerPoints(1, iCornerPoints - nCornerPoints[iFFDBox] / SU2_TYPE::Int(2));
                 CPcoord[2] = 0.5;
               }
               FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, iCornerPoints);
             }
           }
 
-        }
-        else {
+        } else {
           for (iCornerPoints = 0; iCornerPoints < nCornerPoints[iFFDBox]; iCornerPoints++) {
-            getline(mesh_file, text_line); istringstream FFDBox_line(text_line);
-            FFDBox_line >> CPcoord[0]; FFDBox_line >> CPcoord[1]; FFDBox_line >> CPcoord[2];
+            getline(mesh_file, text_line);
+            istringstream FFDBox_line(text_line);
+            FFDBox_line >> CPcoord[0];
+            FFDBox_line >> CPcoord[1];
+            FFDBox_line >> CPcoord[2];
             FFDBox[iFFDBox]->SetCoordCornerPoints(CPcoord, iCornerPoints);
           }
         }
 
         /*--- Read the number of the control points ---*/
 
-        getline (mesh_file, text_line);
-        text_line.erase (0,19); nControlPoints[iFFDBox] = atoi(text_line.c_str());
+        getline(mesh_file, text_line);
+        text_line.erase(0, 19);
+        nControlPoints[iFFDBox] = atoi(text_line.c_str());
 
-        if (rank == MASTER_NODE) cout << "Control points: " << nControlPoints[iFFDBox] <<". ";
+        if (rank == MASTER_NODE) cout << "Control points: " << nControlPoints[iFFDBox] << ". ";
 
         /*--- Method to identify if there is a FFDBox definition ---*/
 
@@ -4192,34 +4399,43 @@ void CSurfaceMovement::ReadFFDInfo(CGeometry *geometry, CConfig *config, CFreeFo
         /*--- Read the coordinates of the control points ---*/
 
         for (iControlPoints = 0; iControlPoints < nControlPoints[iFFDBox]; iControlPoints++) {
-          getline(mesh_file, text_line); istringstream FFDBox_line(text_line);
-          FFDBox_line >> iDegree; FFDBox_line >> jDegree; FFDBox_line >> kDegree;
-          FFDBox_line >> CPcoord[0]; FFDBox_line >> CPcoord[1]; FFDBox_line >> CPcoord[2];
+          getline(mesh_file, text_line);
+          istringstream FFDBox_line(text_line);
+          FFDBox_line >> iDegree;
+          FFDBox_line >> jDegree;
+          FFDBox_line >> kDegree;
+          FFDBox_line >> CPcoord[0];
+          FFDBox_line >> CPcoord[1];
+          FFDBox_line >> CPcoord[2];
           FFDBox[iFFDBox]->SetCoordControlPoints(CPcoord, iDegree, jDegree, kDegree);
           FFDBox[iFFDBox]->SetCoordControlPoints_Copy(CPcoord, iDegree, jDegree, kDegree);
         }
 
-        getline (mesh_file, text_line);
-        text_line.erase (0,19); nSurfacePoints[iFFDBox] = atoi(text_line.c_str());
+        getline(mesh_file, text_line);
+        text_line.erase(0, 19);
+        nSurfacePoints[iFFDBox] = atoi(text_line.c_str());
 
         /*--- The surface points parametric coordinates, all the nodes read the FFD
          information but they only store their part ---*/
 
         my_nSurfPoints = 0;
         for (iSurfacePoints = 0; iSurfacePoints < nSurfacePoints[iFFDBox]; iSurfacePoints++) {
-          getline(mesh_file, text_line); istringstream FFDBox_line(text_line);
-          FFDBox_line >> iTag; FFDBox_line >> iPoint;
+          getline(mesh_file, text_line);
+          istringstream FFDBox_line(text_line);
+          FFDBox_line >> iTag;
+          FFDBox_line >> iPoint;
 
           if (config->GetMarker_All_TagBound(iTag) != -1) {
-
             iMarker = config->GetMarker_All_TagBound(iTag);
-            FFDBox_line >> CPcoord[0]; FFDBox_line >> CPcoord[1]; FFDBox_line >> CPcoord[2];
+            FFDBox_line >> CPcoord[0];
+            FFDBox_line >> CPcoord[1];
+            FFDBox_line >> CPcoord[2];
 
             for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
-              jPoint =  geometry->vertex[iMarker][iVertex]->GetNode();
+              jPoint = geometry->vertex[iMarker][iVertex]->GetNode();
               if (iPoint == geometry->nodes->GetGlobalIndex(jPoint)) {
                 for (iDim = 0; iDim < nDim; iDim++) {
-                  coord[iDim] = geometry->nodes->GetCoord(jPoint,iDim);
+                  coord[iDim] = geometry->nodes->GetCoord(jPoint, iDim);
                 }
                 FFDBox[iFFDBox]->Set_MarkerIndex(iMarker);
                 FFDBox[iFFDBox]->Set_VertexIndex(iVertex);
@@ -4229,9 +4445,7 @@ void CSurfaceMovement::ReadFFDInfo(CGeometry *geometry, CConfig *config, CFreeFo
                 my_nSurfPoints++;
               }
             }
-
           }
-
         }
 
         nSurfacePoints[iFFDBox] = my_nSurfPoints;
@@ -4239,44 +4453,40 @@ void CSurfaceMovement::ReadFFDInfo(CGeometry *geometry, CConfig *config, CFreeFo
 #ifdef HAVE_MPI
         nSurfPoints = 0;
         SU2_MPI::Allreduce(&my_nSurfPoints, &nSurfPoints, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
-        if (rank == MASTER_NODE) cout << "Surface points: " << nSurfPoints <<"."<< endl;
+        if (rank == MASTER_NODE) cout << "Surface points: " << nSurfPoints << "." << endl;
 #else
         nSurfPoints = my_nSurfPoints;
-        if (rank == MASTER_NODE) cout << "Surface points: " << nSurfPoints <<"."<< endl;
+        if (rank == MASTER_NODE) cout << "Surface points: " << nSurfPoints << "." << endl;
 #endif
-
       }
 
-      delete [] nCornerPoints;
-      delete [] nControlPoints;
-      delete [] nSurfacePoints;
+      delete[] nCornerPoints;
+      delete[] nControlPoints;
+      delete[] nSurfacePoints;
     }
   }
   mesh_file.close();
 
   if (nFFDBox == 0) {
-    if (rank == MASTER_NODE) cout <<"There is no FFD box definition. Just in case, check the .su2 file" << endl;
+    if (rank == MASTER_NODE) cout << "There is no FFD box definition. Just in case, check the .su2 file" << endl;
   }
-
 }
 
-void CSurfaceMovement::ReadFFDInfo(CGeometry *geometry, CConfig *config, CFreeFormDefBox **FFDBox) {
-
+void CSurfaceMovement::ReadFFDInfo(CGeometry* geometry, CConfig* config, CFreeFormDefBox** FFDBox) {
   string text_line, iTag;
   ifstream mesh_file;
   su2double coord[3];
-  unsigned short degree[3], iFFDBox, iCornerPoints, LevelFFDBox, nParentFFDBox,
-  iParentFFDBox, nChildFFDBox, iChildFFDBox, *nCornerPoints;
+  unsigned short degree[3], iFFDBox, iCornerPoints, LevelFFDBox, nParentFFDBox, iParentFFDBox, nChildFFDBox,
+      iChildFFDBox, *nCornerPoints;
 
   bool polar = (config->GetFFD_CoordSystem() == POLAR);
   unsigned short nDim = geometry->GetnDim(), iDim;
-  unsigned short SplineOrder[3]={2,2,2};
+  unsigned short SplineOrder[3] = {2, 2, 2};
 
-  for (iDim = 0; iDim < 3; iDim++){
+  for (iDim = 0; iDim < 3; iDim++) {
     SplineOrder[iDim] = SU2_TYPE::Short(config->GetFFD_BSplineOrder()[iDim]);
   }
 
-
   /*--- Read the FFDBox information from the config file ---*/
 
   nFFDBox = config->GetnFFDBox();
@@ -4285,23 +4495,22 @@ void CSurfaceMovement::ReadFFDInfo(CGeometry *geometry, CConfig *config, CFreeFo
 
   nCornerPoints = new unsigned short[nFFDBox];
 
-  nLevel = 1; // Nested FFD is not active
+  nLevel = 1;  // Nested FFD is not active
 
   if (rank == MASTER_NODE) cout << nLevel << " Free Form Deformation nested levels." << endl;
 
-  for (iFFDBox = 0 ; iFFDBox < nFFDBox; iFFDBox++) {
-
+  for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) {
     /*--- Read the name of the FFD box ---*/
 
     string TagFFDBox = config->GetTagFFDBox(iFFDBox);
 
-    if (rank == MASTER_NODE) cout << "FFD box tag: " << TagFFDBox <<". ";
+    if (rank == MASTER_NODE) cout << "FFD box tag: " << TagFFDBox << ". ";
 
     /*--- Read the level of the FFD box ---*/
 
-    LevelFFDBox = 0; // Nested FFD is not active
+    LevelFFDBox = 0;  // Nested FFD is not active
 
-    if (rank == MASTER_NODE) cout << "FFD box level: " << LevelFFDBox <<". ";
+    if (rank == MASTER_NODE) cout << "FFD box level: " << LevelFFDBox << ". ";
 
     /*--- Read the degree of the FFD box ---*/
 
@@ -4310,14 +4519,12 @@ void CSurfaceMovement::ReadFFDInfo(CGeometry *geometry, CConfig *config, CFreeFo
         degree[0] = config->GetDegreeFFDBox(iFFDBox, 0);
         degree[1] = 1;
         degree[2] = config->GetDegreeFFDBox(iFFDBox, 1);
-      }
-      else {
+      } else {
         degree[0] = config->GetDegreeFFDBox(iFFDBox, 0);
         degree[1] = config->GetDegreeFFDBox(iFFDBox, 1);
         degree[2] = 1;
       }
-    }
-    else {
+    } else {
       degree[0] = config->GetDegreeFFDBox(iFFDBox, 0);
       degree[1] = config->GetDegreeFFDBox(iFFDBox, 1);
       degree[2] = config->GetDegreeFFDBox(iFFDBox, 2);
@@ -4325,44 +4532,47 @@ void CSurfaceMovement::ReadFFDInfo(CGeometry *geometry, CConfig *config, CFreeFo
 
     if (rank == MASTER_NODE) {
       if (nDim == 2) {
-        if (polar) cout << "Degrees: " << degree[0] << ", " << degree[2] << "." << endl;
-        else cout << "Degrees: " << degree[0] << ", " << degree[1] << "." << endl;
-      }
-      else cout << "Degrees: " << degree[0] << ", " << degree[1] << ", " << degree[2] << "." << endl;
+        if (polar)
+          cout << "Degrees: " << degree[0] << ", " << degree[2] << "." << endl;
+        else
+          cout << "Degrees: " << degree[0] << ", " << degree[1] << "." << endl;
+      } else
+        cout << "Degrees: " << degree[0] << ", " << degree[1] << ", " << degree[2] << "." << endl;
     }
 
-    if (rank == MASTER_NODE){
-      if (config->GetFFD_Blending() == BSPLINE_UNIFORM){
+    if (rank == MASTER_NODE) {
+      if (config->GetFFD_Blending() == BSPLINE_UNIFORM) {
         cout << "FFD Blending using B-Splines. ";
         cout << "Order: " << SplineOrder[0] << ", " << SplineOrder[1];
         if (nDim == 3) cout << ", " << SplineOrder[2];
         cout << ". " << endl;
       }
-      if (config->GetFFD_Blending() == BEZIER){
+      if (config->GetFFD_Blending() == BEZIER) {
         cout << "FFD Blending using Bezier Curves." << endl;
       }
     }
 
     FFDBox[iFFDBox] = new CFreeFormDefBox(degree, SplineOrder, config->GetFFD_Blending());
-    FFDBox[iFFDBox]->SetTag(TagFFDBox); FFDBox[iFFDBox]->SetLevel(LevelFFDBox);
+    FFDBox[iFFDBox]->SetTag(TagFFDBox);
+    FFDBox[iFFDBox]->SetLevel(LevelFFDBox);
 
     /*--- Read the number of parents boxes ---*/
 
-    nParentFFDBox = 0; // Nested FFD is not active
-    if (rank == MASTER_NODE) cout << "Number of parent boxes: " << nParentFFDBox <<". ";
+    nParentFFDBox = 0;  // Nested FFD is not active
+    if (rank == MASTER_NODE) cout << "Number of parent boxes: " << nParentFFDBox << ". ";
 
     for (iParentFFDBox = 0; iParentFFDBox < nParentFFDBox; iParentFFDBox++) {
-      string ParentFFDBox = "NONE"; // Nested FFD is not active
+      string ParentFFDBox = "NONE";  // Nested FFD is not active
       FFDBox[iFFDBox]->SetParentFFDBox(ParentFFDBox);
     }
 
     /*--- Read the number of children boxes ---*/
 
-    nChildFFDBox = 0; // Nested FFD is not active
-    if (rank == MASTER_NODE) cout << "Number of child boxes: " << nChildFFDBox <<"." << endl;
+    nChildFFDBox = 0;  // Nested FFD is not active
+    if (rank == MASTER_NODE) cout << "Number of child boxes: " << nChildFFDBox << "." << endl;
 
     for (iChildFFDBox = 0; iChildFFDBox < nChildFFDBox; iChildFFDBox++) {
-      string ChildFFDBox = "NONE"; // Nested FFD is not active
+      string ChildFFDBox = "NONE";  // Nested FFD is not active
       FFDBox[iFFDBox]->SetChildFFDBox(ChildFFDBox);
     }
 
@@ -4373,93 +4583,86 @@ void CSurfaceMovement::ReadFFDInfo(CGeometry *geometry, CConfig *config, CFreeFo
     /*--- Read the coordinates of the corner points ---*/
 
     for (iCornerPoints = 0; iCornerPoints < nCornerPoints[iFFDBox]; iCornerPoints++) {
-
       if (nDim == 2) {
-
         if (polar) {
-
-          coord[0] = config->GetCoordFFDBox(iFFDBox, 1*3);
-          coord[1] = cos(0.1)*config->GetCoordFFDBox(iFFDBox, 1*3+1);
-          coord[2] = -sin(0.1)*config->GetCoordFFDBox(iFFDBox, 1*3+1);
+          coord[0] = config->GetCoordFFDBox(iFFDBox, 1 * 3);
+          coord[1] = cos(0.1) * config->GetCoordFFDBox(iFFDBox, 1 * 3 + 1);
+          coord[2] = -sin(0.1) * config->GetCoordFFDBox(iFFDBox, 1 * 3 + 1);
           FFDBox[iFFDBox]->SetCoordCornerPoints(coord, 0);
 
-          coord[0] = config->GetCoordFFDBox(iFFDBox, 2*3);
-          coord[1] = cos(0.1)*config->GetCoordFFDBox(iFFDBox, 2*3+1);
-          coord[2] = -sin(0.1)*config->GetCoordFFDBox(iFFDBox, 2*3+1);
+          coord[0] = config->GetCoordFFDBox(iFFDBox, 2 * 3);
+          coord[1] = cos(0.1) * config->GetCoordFFDBox(iFFDBox, 2 * 3 + 1);
+          coord[2] = -sin(0.1) * config->GetCoordFFDBox(iFFDBox, 2 * 3 + 1);
           FFDBox[iFFDBox]->SetCoordCornerPoints(coord, 1);
 
-          coord[0] = config->GetCoordFFDBox(iFFDBox, 2*3);
-          coord[1] = cos(0.1)*config->GetCoordFFDBox(iFFDBox, 2*3+1);
-          coord[2] = sin(0.1)*config->GetCoordFFDBox(iFFDBox, 2*3+1);
+          coord[0] = config->GetCoordFFDBox(iFFDBox, 2 * 3);
+          coord[1] = cos(0.1) * config->GetCoordFFDBox(iFFDBox, 2 * 3 + 1);
+          coord[2] = sin(0.1) * config->GetCoordFFDBox(iFFDBox, 2 * 3 + 1);
           FFDBox[iFFDBox]->SetCoordCornerPoints(coord, 2);
 
-          coord[0] = config->GetCoordFFDBox(iFFDBox, 1*3);
-          coord[1] = cos(0.1)*config->GetCoordFFDBox(iFFDBox, 1*3+1);
-          coord[2] = sin(0.1)*config->GetCoordFFDBox(iFFDBox, 1*3+1);
+          coord[0] = config->GetCoordFFDBox(iFFDBox, 1 * 3);
+          coord[1] = cos(0.1) * config->GetCoordFFDBox(iFFDBox, 1 * 3 + 1);
+          coord[2] = sin(0.1) * config->GetCoordFFDBox(iFFDBox, 1 * 3 + 1);
           FFDBox[iFFDBox]->SetCoordCornerPoints(coord, 3);
 
-          coord[0] = config->GetCoordFFDBox(iFFDBox, 0*3);
-          coord[1] = cos(0.1)*config->GetCoordFFDBox(iFFDBox, 0*3+1);
-          coord[2] = -sin(0.1)*config->GetCoordFFDBox(iFFDBox, 0*3+1);
+          coord[0] = config->GetCoordFFDBox(iFFDBox, 0 * 3);
+          coord[1] = cos(0.1) * config->GetCoordFFDBox(iFFDBox, 0 * 3 + 1);
+          coord[2] = -sin(0.1) * config->GetCoordFFDBox(iFFDBox, 0 * 3 + 1);
           FFDBox[iFFDBox]->SetCoordCornerPoints(coord, 4);
 
-          coord[0] = config->GetCoordFFDBox(iFFDBox, 3*3);
-          coord[1] = cos(0.1)*config->GetCoordFFDBox(iFFDBox, 3*3+1);
-          coord[2] = -sin(0.1)*config->GetCoordFFDBox(iFFDBox, 3*3+1);
+          coord[0] = config->GetCoordFFDBox(iFFDBox, 3 * 3);
+          coord[1] = cos(0.1) * config->GetCoordFFDBox(iFFDBox, 3 * 3 + 1);
+          coord[2] = -sin(0.1) * config->GetCoordFFDBox(iFFDBox, 3 * 3 + 1);
           FFDBox[iFFDBox]->SetCoordCornerPoints(coord, 5);
 
-          coord[0] = config->GetCoordFFDBox(iFFDBox, 3*3);
-          coord[1] = cos(0.1)*config->GetCoordFFDBox(iFFDBox, 3*3+1);
-          coord[2] = sin(0.1)*config->GetCoordFFDBox(iFFDBox, 3*3+1);
+          coord[0] = config->GetCoordFFDBox(iFFDBox, 3 * 3);
+          coord[1] = cos(0.1) * config->GetCoordFFDBox(iFFDBox, 3 * 3 + 1);
+          coord[2] = sin(0.1) * config->GetCoordFFDBox(iFFDBox, 3 * 3 + 1);
           FFDBox[iFFDBox]->SetCoordCornerPoints(coord, 6);
 
-          coord[0] = config->GetCoordFFDBox(iFFDBox, 0*3);
-          coord[1] = cos(0.1)*config->GetCoordFFDBox(iFFDBox, 0*3+1);
-          coord[2] = sin(0.1)*config->GetCoordFFDBox(iFFDBox, 0*3+1);
+          coord[0] = config->GetCoordFFDBox(iFFDBox, 0 * 3);
+          coord[1] = cos(0.1) * config->GetCoordFFDBox(iFFDBox, 0 * 3 + 1);
+          coord[2] = sin(0.1) * config->GetCoordFFDBox(iFFDBox, 0 * 3 + 1);
           FFDBox[iFFDBox]->SetCoordCornerPoints(coord, 7);
 
         }
 
         else {
-          if (iCornerPoints < nCornerPoints[iFFDBox]/SU2_TYPE::Int(2)) {
-            coord[0] = config->GetCoordFFDBox(iFFDBox, iCornerPoints*3);
-            coord[1] = config->GetCoordFFDBox(iFFDBox, iCornerPoints*3+1);
+          if (iCornerPoints < nCornerPoints[iFFDBox] / SU2_TYPE::Int(2)) {
+            coord[0] = config->GetCoordFFDBox(iFFDBox, iCornerPoints * 3);
+            coord[1] = config->GetCoordFFDBox(iFFDBox, iCornerPoints * 3 + 1);
             coord[2] = -0.5;
-          }
-          else {
-            coord[0] = FFDBox[iFFDBox]->GetCoordCornerPoints(0, iCornerPoints-nCornerPoints[iFFDBox]/SU2_TYPE::Int(2));
-            coord[1] = FFDBox[iFFDBox]->GetCoordCornerPoints(1, iCornerPoints-nCornerPoints[iFFDBox]/SU2_TYPE::Int(2));
+          } else {
+            coord[0] =
+                FFDBox[iFFDBox]->GetCoordCornerPoints(0, iCornerPoints - nCornerPoints[iFFDBox] / SU2_TYPE::Int(2));
+            coord[1] =
+                FFDBox[iFFDBox]->GetCoordCornerPoints(1, iCornerPoints - nCornerPoints[iFFDBox] / SU2_TYPE::Int(2));
             coord[2] = 0.5;
           }
         }
 
-      }
-      else {
-        coord[0] = config->GetCoordFFDBox(iFFDBox, iCornerPoints*3);
-        coord[1] = config->GetCoordFFDBox(iFFDBox, iCornerPoints*3+1);
-        coord[2] = config->GetCoordFFDBox(iFFDBox, iCornerPoints*3+2);
+      } else {
+        coord[0] = config->GetCoordFFDBox(iFFDBox, iCornerPoints * 3);
+        coord[1] = config->GetCoordFFDBox(iFFDBox, iCornerPoints * 3 + 1);
+        coord[2] = config->GetCoordFFDBox(iFFDBox, iCornerPoints * 3 + 2);
       }
 
       FFDBox[iFFDBox]->SetCoordCornerPoints(coord, iCornerPoints);
-
     }
 
     /*--- Method to identify if there is a FFDBox definition ---*/
 
     FFDBoxDefinition = false;
-
   }
 
-  delete [] nCornerPoints;
+  delete[] nCornerPoints;
 
   if (nFFDBox == 0) {
     SU2_MPI::Error("There is no FFD box definition. Check the config file.", CURRENT_FUNCTION);
   }
-
 }
 
-void CSurfaceMovement::MergeFFDInfo(CGeometry *geometry, CConfig *config) {
-
+void CSurfaceMovement::MergeFFDInfo(CGeometry* geometry, CConfig* config) {
   /*--- Local variables needed on all processors ---*/
 
   unsigned long iPoint;
@@ -4472,12 +4675,10 @@ void CSurfaceMovement::MergeFFDInfo(CGeometry *geometry, CConfig *config) {
 
   /*--- Total number of points in each FFD box. ---*/
 
-  for (iFFDBox = 0 ; iFFDBox < nFFDBox; iFFDBox++) {
-
+  for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) {
     /*--- Loop over the mesh to collect the coords of the local points. ---*/
 
     for (iPoint = 0; iPoint < FFDBox[iFFDBox]->GetnSurfacePoint(); iPoint++) {
-
       /*--- Retrieve the current parametric coordinates at this node. ---*/
 
       GlobalCoordX[iFFDBox].push_back(FFDBox[iFFDBox]->Get_ParametricCoord(iPoint)[0]);
@@ -4498,9 +4699,7 @@ void CSurfaceMovement::MergeFFDInfo(CGeometry *geometry, CConfig *config) {
       /*--- Set the value of the tag at this node. ---*/
 
       GlobalTag[iFFDBox].push_back(TagBound_CfgFile);
-
     }
-
   }
 
 #else
@@ -4518,55 +4717,50 @@ void CSurfaceMovement::MergeFFDInfo(CGeometry *geometry, CConfig *config) {
 
   if (rank == MASTER_NODE) Buffer_Recv_nPoint = new unsigned long[nProcessor];
 
-  for (iFFDBox = 0 ; iFFDBox < nFFDBox; iFFDBox++) {
-
+  for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) {
     nLocalPoint = 0;
     for (iPoint = 0; iPoint < FFDBox[iFFDBox]->GetnSurfacePoint(); iPoint++) {
-
       iPointLocal = FFDBox[iFFDBox]->Get_PointIndex(iPoint);
 
       if (iPointLocal < geometry->GetnPointDomain()) {
         nLocalPoint++;
       }
-
     }
     Buffer_Send_nPoint[0] = nLocalPoint;
 
     /*--- Communicate the total number of nodes on this domain. ---*/
 
-    SU2_MPI::Gather(&Buffer_Send_nPoint, 1, MPI_UNSIGNED_LONG,
-               Buffer_Recv_nPoint, 1, MPI_UNSIGNED_LONG, MASTER_NODE, SU2_MPI::GetComm());
+    SU2_MPI::Gather(&Buffer_Send_nPoint, 1, MPI_UNSIGNED_LONG, Buffer_Recv_nPoint, 1, MPI_UNSIGNED_LONG, MASTER_NODE,
+                    SU2_MPI::GetComm());
     SU2_MPI::Allreduce(&nLocalPoint, &MaxLocalPoint, 1, MPI_UNSIGNED_LONG, MPI_MAX, SU2_MPI::GetComm());
 
     nBuffer_Scalar = MaxLocalPoint;
 
     /*--- Send and Recv buffers. ---*/
 
-    su2double *Buffer_Send_X = new su2double[MaxLocalPoint];
-    su2double *Buffer_Recv_X = nullptr;
+    su2double* Buffer_Send_X = new su2double[MaxLocalPoint];
+    su2double* Buffer_Recv_X = nullptr;
 
-    su2double *Buffer_Send_Y = new su2double[MaxLocalPoint];
-    su2double *Buffer_Recv_Y = nullptr;
+    su2double* Buffer_Send_Y = new su2double[MaxLocalPoint];
+    su2double* Buffer_Recv_Y = nullptr;
 
-    su2double *Buffer_Send_Z = new su2double[MaxLocalPoint];
-    su2double *Buffer_Recv_Z = nullptr;
+    su2double* Buffer_Send_Z = new su2double[MaxLocalPoint];
+    su2double* Buffer_Recv_Z = nullptr;
 
-    unsigned long *Buffer_Send_Point = new unsigned long[MaxLocalPoint];
-    unsigned long *Buffer_Recv_Point = nullptr;
+    unsigned long* Buffer_Send_Point = new unsigned long[MaxLocalPoint];
+    unsigned long* Buffer_Recv_Point = nullptr;
 
-    unsigned short *Buffer_Send_MarkerIndex_CfgFile = new unsigned short[MaxLocalPoint];
-    unsigned short *Buffer_Recv_MarkerIndex_CfgFile = nullptr;
+    unsigned short* Buffer_Send_MarkerIndex_CfgFile = new unsigned short[MaxLocalPoint];
+    unsigned short* Buffer_Recv_MarkerIndex_CfgFile = nullptr;
 
     /*--- Prepare the receive buffers in the master node only. ---*/
 
     if (rank == MASTER_NODE) {
-
-      Buffer_Recv_X = new su2double[nProcessor*MaxLocalPoint];
-      Buffer_Recv_Y = new su2double[nProcessor*MaxLocalPoint];
-      Buffer_Recv_Z = new su2double[nProcessor*MaxLocalPoint];
-      Buffer_Recv_Point = new unsigned long[nProcessor*MaxLocalPoint];
-      Buffer_Recv_MarkerIndex_CfgFile = new unsigned short[nProcessor*MaxLocalPoint];
-
+      Buffer_Recv_X = new su2double[nProcessor * MaxLocalPoint];
+      Buffer_Recv_Y = new su2double[nProcessor * MaxLocalPoint];
+      Buffer_Recv_Z = new su2double[nProcessor * MaxLocalPoint];
+      Buffer_Recv_Point = new unsigned long[nProcessor * MaxLocalPoint];
+      Buffer_Recv_MarkerIndex_CfgFile = new unsigned short[nProcessor * MaxLocalPoint];
     }
 
     /*--- Main communication routine. Loop over each coordinate and perform
@@ -4578,11 +4772,9 @@ void CSurfaceMovement::MergeFFDInfo(CGeometry *geometry, CConfig *config) {
 
     jPoint = 0;
     for (iPoint = 0; iPoint < FFDBox[iFFDBox]->GetnSurfacePoint(); iPoint++) {
-
       iPointLocal = FFDBox[iFFDBox]->Get_PointIndex(iPoint);
 
       if (iPointLocal < geometry->GetnPointDomain()) {
-
         /*--- Load local coords into the temporary send buffer. ---*/
 
         Buffer_Send_X[jPoint] = FFDBox[iFFDBox]->Get_ParametricCoord(iPoint)[0];
@@ -4604,28 +4796,30 @@ void CSurfaceMovement::MergeFFDInfo(CGeometry *geometry, CConfig *config) {
         Buffer_Send_MarkerIndex_CfgFile[jPoint] = MarkerIndex_CfgFile;
 
         jPoint++;
-
       }
-
     }
 
     /*--- Gather the coordinate data on the master node using MPI. ---*/
 
-    SU2_MPI::Gather(Buffer_Send_X, nBuffer_Scalar, MPI_DOUBLE, Buffer_Recv_X, nBuffer_Scalar, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Gather(Buffer_Send_Y, nBuffer_Scalar, MPI_DOUBLE, Buffer_Recv_Y, nBuffer_Scalar, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Gather(Buffer_Send_Z, nBuffer_Scalar, MPI_DOUBLE, Buffer_Recv_Z, nBuffer_Scalar, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Gather(Buffer_Send_Point, nBuffer_Scalar, MPI_UNSIGNED_LONG, Buffer_Recv_Point, nBuffer_Scalar, MPI_UNSIGNED_LONG, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Gather(Buffer_Send_MarkerIndex_CfgFile, nBuffer_Scalar, MPI_UNSIGNED_SHORT, Buffer_Recv_MarkerIndex_CfgFile, nBuffer_Scalar, MPI_UNSIGNED_SHORT, MASTER_NODE, SU2_MPI::GetComm());
+    SU2_MPI::Gather(Buffer_Send_X, nBuffer_Scalar, MPI_DOUBLE, Buffer_Recv_X, nBuffer_Scalar, MPI_DOUBLE, MASTER_NODE,
+                    SU2_MPI::GetComm());
+    SU2_MPI::Gather(Buffer_Send_Y, nBuffer_Scalar, MPI_DOUBLE, Buffer_Recv_Y, nBuffer_Scalar, MPI_DOUBLE, MASTER_NODE,
+                    SU2_MPI::GetComm());
+    SU2_MPI::Gather(Buffer_Send_Z, nBuffer_Scalar, MPI_DOUBLE, Buffer_Recv_Z, nBuffer_Scalar, MPI_DOUBLE, MASTER_NODE,
+                    SU2_MPI::GetComm());
+    SU2_MPI::Gather(Buffer_Send_Point, nBuffer_Scalar, MPI_UNSIGNED_LONG, Buffer_Recv_Point, nBuffer_Scalar,
+                    MPI_UNSIGNED_LONG, MASTER_NODE, SU2_MPI::GetComm());
+    SU2_MPI::Gather(Buffer_Send_MarkerIndex_CfgFile, nBuffer_Scalar, MPI_UNSIGNED_SHORT,
+                    Buffer_Recv_MarkerIndex_CfgFile, nBuffer_Scalar, MPI_UNSIGNED_SHORT, MASTER_NODE,
+                    SU2_MPI::GetComm());
 
     /*--- The master node unpacks and sorts this variable by global index ---*/
 
     if (rank == MASTER_NODE) {
-
       jPoint = 0;
 
       for (iProcessor = 0; iProcessor < nProcessor; iProcessor++) {
         for (iPoint = 0; iPoint < Buffer_Recv_nPoint[iProcessor]; iPoint++) {
-
           /*--- Get global index, then loop over each variable and store ---*/
 
           GlobalCoordX[iFFDBox].push_back(Buffer_Recv_X[jPoint]);
@@ -4636,67 +4830,58 @@ void CSurfaceMovement::MergeFFDInfo(CGeometry *geometry, CConfig *config) {
           string TagBound_CfgFile = config->GetMarker_CfgFile_TagBound(Buffer_Recv_MarkerIndex_CfgFile[jPoint]);
           GlobalTag[iFFDBox].push_back(TagBound_CfgFile);
           jPoint++;
-
         }
 
         /*--- Adjust jPoint to index of next proc's data in the buffers. ---*/
 
-        jPoint = (iProcessor+1)*nBuffer_Scalar;
-
+        jPoint = (iProcessor + 1) * nBuffer_Scalar;
       }
     }
 
     /*--- Immediately release the temporary data buffers. ---*/
 
-    delete [] Buffer_Send_X;
-    delete [] Buffer_Send_Y;
-    delete [] Buffer_Send_Z;
-    delete [] Buffer_Send_Point;
-    delete [] Buffer_Send_MarkerIndex_CfgFile;
+    delete[] Buffer_Send_X;
+    delete[] Buffer_Send_Y;
+    delete[] Buffer_Send_Z;
+    delete[] Buffer_Send_Point;
+    delete[] Buffer_Send_MarkerIndex_CfgFile;
 
     if (rank == MASTER_NODE) {
-      delete [] Buffer_Recv_X;
-      delete [] Buffer_Recv_Y;
-      delete [] Buffer_Recv_Z;
-      delete [] Buffer_Recv_Point;
-      delete [] Buffer_Recv_MarkerIndex_CfgFile;
+      delete[] Buffer_Recv_X;
+      delete[] Buffer_Recv_Y;
+      delete[] Buffer_Recv_Z;
+      delete[] Buffer_Recv_Point;
+      delete[] Buffer_Recv_MarkerIndex_CfgFile;
     }
-
   }
 
   if (rank == MASTER_NODE) {
-    delete [] Buffer_Recv_nPoint;
+    delete[] Buffer_Recv_nPoint;
   }
 
 #endif
-
 }
 
-void CSurfaceMovement::WriteFFDInfo(CSurfaceMovement** surface_movement, CGeometry ****geometry, CConfig **config) {
-
-
+void CSurfaceMovement::WriteFFDInfo(CSurfaceMovement** surface_movement, CGeometry**** geometry, CConfig** config) {
   unsigned short iOrder, jOrder, kOrder, iFFDBox, iCornerPoints, iParentFFDBox, iChildFFDBox, iZone;
   unsigned long iSurfacePoints;
   ofstream output_file;
-  su2double *coord;
+  su2double* coord;
   string text_line;
 
   bool polar = (config[ZONE_0]->GetFFD_CoordSystem() == POLAR);
 
   unsigned short nDim = geometry[ZONE_0][INST_0][MESH_0]->GetnDim();
 
-  for (iZone = 0; iZone < config[ZONE_0]->GetnZone(); iZone++){
-
+  for (iZone = 0; iZone < config[ZONE_0]->GetnZone(); iZone++) {
     /*--- Merge the parallel FFD info ---*/
 
     surface_movement[iZone]->MergeFFDInfo(geometry[iZone][INST_0][MESH_0], config[iZone]);
 
-    if (iZone > 0){
-
+    if (iZone > 0) {
       /* --- Merge the per-zone FFD info from the other zones into ZONE_0 ---*/
 
-      for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++){
-
+      for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) {
         surface_movement[ZONE_0]->GlobalCoordX[iFFDBox].insert(surface_movement[ZONE_0]->GlobalCoordX[iFFDBox].end(),
                                                                surface_movement[iZone]->GlobalCoordX[iFFDBox].begin(),
                                                                surface_movement[iZone]->GlobalCoordX[iFFDBox].end());
@@ -4707,22 +4892,18 @@ void CSurfaceMovement::WriteFFDInfo(CSurfaceMovement** surface_movement, CGeomet
                                                                surface_movement[iZone]->GlobalCoordZ[iFFDBox].begin(),
                                                                surface_movement[iZone]->GlobalCoordZ[iFFDBox].end());
         surface_movement[ZONE_0]->GlobalTag[iFFDBox].insert(surface_movement[ZONE_0]->GlobalTag[iFFDBox].end(),
-                                                               surface_movement[iZone]->GlobalTag[iFFDBox].begin(),
-                                                               surface_movement[iZone]->GlobalTag[iFFDBox].end());
+                                                            surface_movement[iZone]->GlobalTag[iFFDBox].begin(),
+                                                            surface_movement[iZone]->GlobalTag[iFFDBox].end());
         surface_movement[ZONE_0]->GlobalPoint[iFFDBox].insert(surface_movement[ZONE_0]->GlobalPoint[iFFDBox].end(),
-                                                               surface_movement[iZone]->GlobalPoint[iFFDBox].begin(),
-                                                               surface_movement[iZone]->GlobalPoint[iFFDBox].end());
+                                                              surface_movement[iZone]->GlobalPoint[iFFDBox].begin(),
+                                                              surface_movement[iZone]->GlobalPoint[iFFDBox].end());
       }
     }
   }
 
-
-
-
   /*--- Attach to the mesh file the FFD information (all information is in ZONE_0) ---*/
 
   if (rank == MASTER_NODE) {
-
     /*--- Read the name of the output file ---*/
 
     auto str = config[ZONE_0]->GetMesh_Out_FileName();
@@ -4737,20 +4918,23 @@ void CSurfaceMovement::WriteFFDInfo(CSurfaceMovement** surface_movement, CGeomet
       output_file << "FFD_NLEVEL= " << nLevel << endl;
     }
 
-    for (iFFDBox = 0 ; iFFDBox < nFFDBox; iFFDBox++) {
-
+    for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) {
       output_file << "FFD_TAG= " << FFDBox[iFFDBox]->GetTag() << endl;
       output_file << "FFD_LEVEL= " << FFDBox[iFFDBox]->GetLevel() << endl;
 
-      output_file << "FFD_DEGREE_I= " << FFDBox[iFFDBox]->GetlOrder()-1 << endl;
-      if (polar) output_file << "FFD_DEGREE_J= " << FFDBox[iFFDBox]->GetnOrder()-1 << endl;
-      else output_file << "FFD_DEGREE_J= " << FFDBox[iFFDBox]->GetmOrder()-1 << endl;
-      if (nDim == 3) output_file << "FFD_DEGREE_K= " << FFDBox[iFFDBox]->GetnOrder()-1 << endl;
+      output_file << "FFD_DEGREE_I= " << FFDBox[iFFDBox]->GetlOrder() - 1 << endl;
+      if (polar)
+        output_file << "FFD_DEGREE_J= " << FFDBox[iFFDBox]->GetnOrder() - 1 << endl;
+      else
+        output_file << "FFD_DEGREE_J= " << FFDBox[iFFDBox]->GetmOrder() - 1 << endl;
+      if (nDim == 3) output_file << "FFD_DEGREE_K= " << FFDBox[iFFDBox]->GetnOrder() - 1 << endl;
       if (config[ZONE_0]->GetFFD_Blending() == BSPLINE_UNIFORM) {
         output_file << "FFD_BLENDING= BSPLINE_UNIFORM" << endl;
         output_file << "BSPLINE_ORDER_I= " << FFDBox[iFFDBox]->BlendingFunction[0]->GetOrder() << endl;
-        if (polar) output_file << "BSPLINE_ORDER_J= " << FFDBox[iFFDBox]->BlendingFunction[2]->GetOrder() << endl;
-        else output_file << "BSPLINE_ORDER_J= " << FFDBox[iFFDBox]->BlendingFunction[1]->GetOrder() << endl;
+        if (polar)
+          output_file << "BSPLINE_ORDER_J= " << FFDBox[iFFDBox]->BlendingFunction[2]->GetOrder() << endl;
+        else
+          output_file << "BSPLINE_ORDER_J= " << FFDBox[iFFDBox]->BlendingFunction[1]->GetOrder() << endl;
         if (nDim == 3) output_file << "BSPLINE_ORDER_K= " << FFDBox[iFFDBox]->BlendingFunction[2]->GetOrder() << endl;
       }
       if (config[ZONE_0]->GetFFD_Blending() == BEZIER) {
@@ -4765,28 +4949,27 @@ void CSurfaceMovement::WriteFFDInfo(CSurfaceMovement** surface_movement, CGeomet
         output_file << FFDBox[iFFDBox]->GetChildFFDBoxTag(iChildFFDBox) << endl;
 
       if (nDim == 2) {
-        output_file << "FFD_CORNER_POINTS= " << FFDBox[iFFDBox]->GetnCornerPoints()/SU2_TYPE::Int(2) << endl;
+        output_file << "FFD_CORNER_POINTS= " << FFDBox[iFFDBox]->GetnCornerPoints() / SU2_TYPE::Int(2) << endl;
         if (polar) {
           coord = FFDBox[iFFDBox]->GetCoordCornerPoints(4);
-          output_file << coord[0] << "\t" << sqrt(coord[1]*coord[1]+coord[2]*coord[2]) << endl;
+          output_file << coord[0] << "\t" << sqrt(coord[1] * coord[1] + coord[2] * coord[2]) << endl;
 
           coord = FFDBox[iFFDBox]->GetCoordCornerPoints(0);
-          output_file << coord[0] << "\t" << sqrt(coord[1]*coord[1]+coord[2]*coord[2]) << endl;
+          output_file << coord[0] << "\t" << sqrt(coord[1] * coord[1] + coord[2] * coord[2]) << endl;
 
           coord = FFDBox[iFFDBox]->GetCoordCornerPoints(1);
-          output_file << coord[0] << "\t" << sqrt(coord[1]*coord[1]+coord[2]*coord[2]) << endl;
+          output_file << coord[0] << "\t" << sqrt(coord[1] * coord[1] + coord[2] * coord[2]) << endl;
 
           coord = FFDBox[iFFDBox]->GetCoordCornerPoints(5);
-          output_file << coord[0] << "\t" << sqrt(coord[1]*coord[1]+coord[2]*coord[2]) << endl;
-        }
-        else {
-          for (iCornerPoints = 0; iCornerPoints < FFDBox[iFFDBox]->GetnCornerPoints()/SU2_TYPE::Int(2); iCornerPoints++) {
+          output_file << coord[0] << "\t" << sqrt(coord[1] * coord[1] + coord[2] * coord[2]) << endl;
+        } else {
+          for (iCornerPoints = 0; iCornerPoints < FFDBox[iFFDBox]->GetnCornerPoints() / SU2_TYPE::Int(2);
+               iCornerPoints++) {
             coord = FFDBox[iFFDBox]->GetCoordCornerPoints(iCornerPoints);
             output_file << coord[0] << "\t" << coord[1] << endl;
           }
         }
-      }
-      else {
+      } else {
         output_file << "FFD_CORNER_POINTS= " << FFDBox[iFFDBox]->GetnCornerPoints() << endl;
         for (iCornerPoints = 0; iCornerPoints < FFDBox[iFFDBox]->GetnCornerPoints(); iCornerPoints++) {
           coord = FFDBox[iFFDBox]->GetCoordCornerPoints(iCornerPoints);
@@ -4798,14 +4981,14 @@ void CSurfaceMovement::WriteFFDInfo(CSurfaceMovement** surface_movement, CGeomet
 
       if (FFDBox[iFFDBox]->GetnControlPoints() == 0) {
         output_file << "FFD_CONTROL_POINTS= 0" << endl;
-      }
-      else {
+      } else {
         output_file << "FFD_CONTROL_POINTS= " << FFDBox[iFFDBox]->GetnControlPoints() << endl;
         for (iOrder = 0; iOrder < FFDBox[iFFDBox]->GetlOrder(); iOrder++)
           for (jOrder = 0; jOrder < FFDBox[iFFDBox]->GetmOrder(); jOrder++)
             for (kOrder = 0; kOrder < FFDBox[iFFDBox]->GetnOrder(); kOrder++) {
               coord = FFDBox[iFFDBox]->GetCoordControlPoints(iOrder, jOrder, kOrder);
-              output_file << iOrder << "\t" << jOrder << "\t" << kOrder << "\t" << coord[0] << "\t" << coord[1] << "\t" << coord[2] << endl;
+              output_file << iOrder << "\t" << jOrder << "\t" << kOrder << "\t" << coord[0] << "\t" << coord[1] << "\t"
+                          << coord[2] << endl;
             }
       }
 
@@ -4813,39 +4996,33 @@ void CSurfaceMovement::WriteFFDInfo(CSurfaceMovement** surface_movement, CGeomet
 
       if (FFDBox[iFFDBox]->GetnControlPoints() == 0) {
         output_file << "FFD_SURFACE_POINTS= 0" << endl;
-      }
-      else {
+      } else {
         output_file << "FFD_SURFACE_POINTS= " << GlobalTag[iFFDBox].size() << endl;
 
         for (iSurfacePoints = 0; iSurfacePoints < GlobalTag[iFFDBox].size(); iSurfacePoints++) {
-          output_file << scientific << GlobalTag[iFFDBox][iSurfacePoints] << "\t" << GlobalPoint[iFFDBox][iSurfacePoints]
-          << "\t" << GlobalCoordX[iFFDBox][iSurfacePoints] << "\t" << GlobalCoordY[iFFDBox][iSurfacePoints]
-          << "\t" << GlobalCoordZ[iFFDBox][iSurfacePoints] << endl;
+          output_file << scientific << GlobalTag[iFFDBox][iSurfacePoints] << "\t"
+                      << GlobalPoint[iFFDBox][iSurfacePoints] << "\t" << GlobalCoordX[iFFDBox][iSurfacePoints] << "\t"
+                      << GlobalCoordY[iFFDBox][iSurfacePoints] << "\t" << GlobalCoordZ[iFFDBox][iSurfacePoints] << endl;
         }
-
       }
-
     }
 
     output_file.close();
-
   }
 }
 
-unsigned long CSurfaceMovement::calculateJacobianDeterminant(CGeometry *geometry, CConfig *config, CFreeFormDefBox *FFDBox) const {
-
+unsigned long CSurfaceMovement::calculateJacobianDeterminant(CGeometry* geometry, CConfig* config,
+                                                             CFreeFormDefBox* FFDBox) const {
   unsigned long iSurfacePoints;
   unsigned short iMarker;
   unsigned long negative_determinants = 0;
 
   /*--- Loop over the surface points ---*/
   for (iSurfacePoints = 0; iSurfacePoints < FFDBox->GetnSurfacePoint(); iSurfacePoints++) {
-
     /*--- Get the marker of the surface point ---*/
     iMarker = FFDBox->Get_MarkerIndex(iSurfacePoints);
 
     if (config->GetMarker_All_DV(iMarker) == YES) {
-
       const auto ParamCoord = FFDBox->Get_ParametricCoord(iSurfacePoints);
 
       /*--- Calculate partial derivatives ---*/
@@ -4853,32 +5030,33 @@ unsigned long CSurfaceMovement::calculateJacobianDeterminant(CGeometry *geometry
       su2double Ba, Bb, Bc, Ba_der, Bb_der, Bc_der;
       su2double determinant, d_du[3] = {0.0}, d_dv[3] = {0.0}, d_dw[3] = {0.0};
 
-      for (iDegree = 0; iDegree <= FFDBox->lDegree; iDegree++){
+      for (iDegree = 0; iDegree <= FFDBox->lDegree; iDegree++) {
         Ba = FFDBox->BlendingFunction[0]->GetBasis(iDegree, ParamCoord[0]);
         Ba_der = FFDBox->BlendingFunction[0]->GetDerivative(iDegree, ParamCoord[0], 1);
 
-        for (jDegree = 0; jDegree <= FFDBox->mDegree; jDegree++){
+        for (jDegree = 0; jDegree <= FFDBox->mDegree; jDegree++) {
           Bb = FFDBox->BlendingFunction[1]->GetBasis(jDegree, ParamCoord[1]);
           Bb_der = FFDBox->BlendingFunction[1]->GetDerivative(jDegree, ParamCoord[1], 1);
 
-          for (kDegree = 0; kDegree <= FFDBox->nDegree; kDegree++){
-
+          for (kDegree = 0; kDegree <= FFDBox->nDegree; kDegree++) {
             Bc = FFDBox->BlendingFunction[2]->GetBasis(kDegree, ParamCoord[2]);
             Bc_der = FFDBox->BlendingFunction[2]->GetDerivative(kDegree, ParamCoord[2], 1);
 
-            for (int i=0; i<3; ++i) {
-              d_du[i] += Ba_der*Bb*Bc*FFDBox->Coord_Control_Points[iDegree][jDegree][kDegree][i];
-              d_dv[i] += Ba*Bb_der*Bc*FFDBox->Coord_Control_Points[iDegree][jDegree][kDegree][i];
-              d_dw[i] += Ba*Bb*Bc_der*FFDBox->Coord_Control_Points[iDegree][jDegree][kDegree][i];
+            for (int i = 0; i < 3; ++i) {
+              d_du[i] += Ba_der * Bb * Bc * FFDBox->Coord_Control_Points[iDegree][jDegree][kDegree][i];
+              d_dv[i] += Ba * Bb_der * Bc * FFDBox->Coord_Control_Points[iDegree][jDegree][kDegree][i];
+              d_dw[i] += Ba * Bb * Bc_der * FFDBox->Coord_Control_Points[iDegree][jDegree][kDegree][i];
             }
           }
         }
       }
 
       /*--- Calculate determinant ---*/
-      determinant = d_du[0]*(d_dv[1]*d_dw[2] - d_dv[2]*d_dw[1]) - d_dv[0]*(d_du[1]*d_dw[2] - d_du[2]*d_dw[1]) + d_dw[0]*(d_du[1]*d_dv[2] - d_du[2]*d_dv[1]);
+      determinant = d_du[0] * (d_dv[1] * d_dw[2] - d_dv[2] * d_dw[1]) -
+                    d_dv[0] * (d_du[1] * d_dw[2] - d_du[2] * d_dw[1]) +
+                    d_dw[0] * (d_du[1] * d_dv[2] - d_du[2] * d_dv[1]);
 
-      if (determinant < 0){
+      if (determinant < 0) {
         negative_determinants++;
       }
     }
diff --git a/Common/src/grid_movement/CVolumetricMovement.cpp b/Common/src/grid_movement/CVolumetricMovement.cpp
index ef7e3d423af..b1c9ff10f7d 100644
--- a/Common/src/grid_movement/CVolumetricMovement.cpp
+++ b/Common/src/grid_movement/CVolumetricMovement.cpp
@@ -25,42 +25,38 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #include "../../include/grid_movement/CVolumetricMovement.hpp"
 #include "../../include/adt/CADTPointsOnlyClass.hpp"
 #include "../../include/toolboxes/geometry_toolbox.hpp"
 
-CVolumetricMovement::CVolumetricMovement(void) : CGridMovement(), System(LINEAR_SOLVER_MODE::MESH_DEFORM) {
-
-}
-
-CVolumetricMovement::CVolumetricMovement(CGeometry *geometry, CConfig *config) : CGridMovement(), System(LINEAR_SOLVER_MODE::MESH_DEFORM) {
+CVolumetricMovement::CVolumetricMovement(void) : CGridMovement(), System(LINEAR_SOLVER_MODE::MESH_DEFORM) {}
 
+CVolumetricMovement::CVolumetricMovement(CGeometry* geometry, CConfig* config)
+    : CGridMovement(), System(LINEAR_SOLVER_MODE::MESH_DEFORM) {
   size = SU2_MPI::GetSize();
   rank = SU2_MPI::GetRank();
 
   /*--- Initialize the number of spatial dimensions, length of the state
    vector (same as spatial dimensions for grid deformation), and grid nodes. ---*/
 
-  nDim   = geometry->GetnDim();
-  nVar   = geometry->GetnDim();
+  nDim = geometry->GetnDim();
+  nVar = geometry->GetnDim();
   nPoint = geometry->GetnPoint();
   nPointDomain = geometry->GetnPointDomain();
 
   nIterMesh = 0;
 
   /*--- Initialize matrix, solution, and r.h.s. structures for the linear solver. ---*/
-  if (config->GetVolumetric_Movement() || config->GetSmoothGradient()){
+  if (config->GetVolumetric_Movement() || config->GetSmoothGradient()) {
     LinSysSol.Initialize(nPoint, nPointDomain, nVar, 0.0);
     LinSysRes.Initialize(nPoint, nPointDomain, nVar, 0.0);
     StiffMatrix.Initialize(nPoint, nPointDomain, nVar, nVar, false, geometry, config);
   }
 }
 
-CVolumetricMovement::~CVolumetricMovement(void) { }
-
-void CVolumetricMovement::UpdateGridCoord(CGeometry *geometry, CConfig *config) {
+CVolumetricMovement::~CVolumetricMovement(void) {}
 
+void CVolumetricMovement::UpdateGridCoord(CGeometry* geometry, CConfig* config) {
   unsigned short iDim;
   unsigned long iPoint, total_index;
   su2double new_coord;
@@ -70,9 +66,9 @@ void CVolumetricMovement::UpdateGridCoord(CGeometry *geometry, CConfig *config)
 
   for (iPoint = 0; iPoint < nPoint; iPoint++)
     for (iDim = 0; iDim < nDim; iDim++) {
-      total_index = iPoint*nDim + iDim;
-      new_coord = geometry->nodes->GetCoord(iPoint, iDim)+LinSysSol[total_index];
-      if (fabs(new_coord) < EPS*EPS) new_coord = 0.0;
+      total_index = iPoint * nDim + iDim;
+      new_coord = geometry->nodes->GetCoord(iPoint, iDim) + LinSysSol[total_index];
+      if (fabs(new_coord) < EPS * EPS) new_coord = 0.0;
       geometry->nodes->SetCoord(iPoint, iDim, new_coord);
     }
 
@@ -82,52 +78,46 @@ void CVolumetricMovement::UpdateGridCoord(CGeometry *geometry, CConfig *config)
 
   geometry->InitiateComms(geometry, config, COORDINATES);
   geometry->CompleteComms(geometry, config, COORDINATES);
-
 }
 
-void CVolumetricMovement::UpdateDualGrid(CGeometry *geometry, CConfig *config) {
-
+void CVolumetricMovement::UpdateDualGrid(CGeometry* geometry, CConfig* config) {
   /*--- After moving all nodes, update the dual mesh. Recompute the edges and
    dual mesh control volumes in the domain and on the boundaries. ---*/
 
   geometry->SetControlVolume(config, UPDATE);
   geometry->SetBoundControlVolume(config, UPDATE);
   geometry->SetMaxLength(config);
-
 }
 
-void CVolumetricMovement::UpdateMultiGrid(CGeometry **geometry, CConfig *config) {
-
+void CVolumetricMovement::UpdateMultiGrid(CGeometry** geometry, CConfig* config) {
   unsigned short iMGfine, iMGlevel, nMGlevel = config->GetnMGLevels();
 
   /*--- Update the multigrid structure after moving the finest grid,
    including computing the grid velocities on the coarser levels. ---*/
 
   for (iMGlevel = 1; iMGlevel <= nMGlevel; iMGlevel++) {
-    iMGfine = iMGlevel-1;
+    iMGfine = iMGlevel - 1;
     geometry[iMGlevel]->SetControlVolume(geometry[iMGfine], UPDATE);
-    geometry[iMGlevel]->SetBoundControlVolume(geometry[iMGfine],UPDATE);
+    geometry[iMGlevel]->SetBoundControlVolume(geometry[iMGfine], UPDATE);
     geometry[iMGlevel]->SetCoord(geometry[iMGfine]);
-    if (config->GetGrid_Movement())
-      geometry[iMGlevel]->SetRestricted_GridVelocity(geometry[iMGfine]);
+    if (config->GetGrid_Movement()) geometry[iMGlevel]->SetRestricted_GridVelocity(geometry[iMGfine]);
   }
-
 }
 
-void CVolumetricMovement::SetVolume_Deformation(CGeometry *geometry, CConfig *config, bool UpdateGeo, bool Derivative, bool ForwardProjectionDerivative) {
-
+void CVolumetricMovement::SetVolume_Deformation(CGeometry* geometry, CConfig* config, bool UpdateGeo, bool Derivative,
+                                                bool ForwardProjectionDerivative) {
   unsigned long Tot_Iter = 0;
   su2double MinVolume, MaxVolume;
 
   /*--- Retrieve number or iterations, tol, output, etc. from config ---*/
 
-  auto Screen_Output  = config->GetDeform_Output();
+  auto Screen_Output = config->GetDeform_Output();
   auto Nonlinear_Iter = config->GetGridDef_Nonlinear_Iter();
 
   /*--- Disable the screen output if we're running SU2_CFD ---*/
 
   if (config->GetKind_SU2() == SU2_COMPONENT::SU2_CFD && !Derivative) Screen_Output = false;
-  if (config->GetSmoothGradient()) Screen_Output=true;
+  if (config->GetSmoothGradient()) Screen_Output = true;
 
   /*--- Set the number of nonlinear iterations to 1 if Derivative computation is enabled ---*/
 
@@ -138,7 +128,6 @@ void CVolumetricMovement::SetVolume_Deformation(CGeometry *geometry, CConfig *co
    particular, the linear elasticity equations hold only for small deformations. ---*/
 
   for (auto iNonlinear_Iter = 0ul; iNonlinear_Iter < Nonlinear_Iter; iNonlinear_Iter++) {
-
     /*--- Initialize vector and sparse matrix ---*/
 
     LinSysSol.SetValZero();
@@ -163,7 +152,9 @@ void CVolumetricMovement::SetVolume_Deformation(CGeometry *geometry, CConfig *co
 
     /*--- Set the boundary derivatives (overrides the actual displacements) ---*/
 
-    if (Derivative) { SetBoundaryDerivatives(geometry, config, ForwardProjectionDerivative); }
+    if (Derivative) {
+      SetBoundaryDerivatives(geometry, config, ForwardProjectionDerivative);
+    }
 
     /*--- Communicate any prescribed boundary displacements via MPI,
      so that all nodes have the same solution and r.h.s. entries
@@ -183,12 +174,11 @@ void CVolumetricMovement::SetVolume_Deformation(CGeometry *geometry, CConfig *co
     /*--- If we want no derivatives or the direct derivatives, we solve the system using the
      * normal matrix vector product and preconditioner. For the mesh sensitivities using
      * the discrete adjoint method we solve the system using the transposed matrix. ---*/
-    if (!Derivative || ((config->GetKind_SU2() == SU2_COMPONENT::SU2_CFD) && Derivative) || (config->GetSmoothGradient() && ForwardProjectionDerivative)) {
-
+    if (!Derivative || ((config->GetKind_SU2() == SU2_COMPONENT::SU2_CFD) && Derivative) ||
+        (config->GetSmoothGradient() && ForwardProjectionDerivative)) {
       Tot_Iter = System.Solve(StiffMatrix, LinSysRes, LinSysSol, geometry, config);
 
     } else if (Derivative && (config->GetKind_SU2() == SU2_COMPONENT::SU2_DOT)) {
-
       Tot_Iter = System.Solve_b(StiffMatrix, LinSysRes, LinSysSol, geometry, config);
     }
     su2double Residual = System.GetResidual();
@@ -196,9 +186,14 @@ void CVolumetricMovement::SetVolume_Deformation(CGeometry *geometry, CConfig *co
     /*--- Update the grid coordinates and cell volumes using the solution
      of the linear system (usol contains the x, y, z displacements). ---*/
 
-    if (!Derivative) { UpdateGridCoord(geometry, config); }
-    else { UpdateGridCoord_Derivatives(geometry, config, ForwardProjectionDerivative); }
-    if (UpdateGeo) { UpdateDualGrid(geometry, config); }
+    if (!Derivative) {
+      UpdateGridCoord(geometry, config);
+    } else {
+      UpdateGridCoord_Derivatives(geometry, config, ForwardProjectionDerivative);
+    }
+    if (UpdateGeo) {
+      UpdateDualGrid(geometry, config);
+    }
 
     if (!Derivative) {
       /*--- Check for failed deformation (negative volumes). ---*/
@@ -215,37 +210,37 @@ void CVolumetricMovement::SetVolume_Deformation(CGeometry *geometry, CConfig *co
     Set_nIterMesh(Tot_Iter);
 
     if (rank == MASTER_NODE && Screen_Output) {
-      cout << "Non-linear iter.: " << iNonlinear_Iter+1 << "/" << Nonlinear_Iter  << ". Linear iter.: " << Tot_Iter << ". ";
-      if (nDim == 2) cout << "Min. area: " << MinVolume << ". Error: " << Residual << "." << endl;
-      else cout << "Min. volume: " << MinVolume << ". Error: " << Residual << "." << endl;
+      cout << "Non-linear iter.: " << iNonlinear_Iter + 1 << "/" << Nonlinear_Iter << ". Linear iter.: " << Tot_Iter
+           << ". ";
+      if (nDim == 2)
+        cout << "Min. area: " << MinVolume << ". Error: " << Residual << "." << endl;
+      else
+        cout << "Min. volume: " << MinVolume << ". Error: " << Residual << "." << endl;
     }
-
   }
-
 }
 
-void CVolumetricMovement::ComputeDeforming_Element_Volume(CGeometry *geometry, su2double &MinVolume, su2double &MaxVolume, bool Screen_Output) {
-
+void CVolumetricMovement::ComputeDeforming_Element_Volume(CGeometry* geometry, su2double& MinVolume,
+                                                          su2double& MaxVolume, bool Screen_Output) {
   unsigned long iElem, ElemCounter = 0, PointCorners[8];
   su2double Volume = 0.0, CoordCorners[8][3];
   unsigned short nNodes = 0, iNodes, iDim;
   bool RightVol = true;
 
-  if (rank == MASTER_NODE && Screen_Output)
-    cout << "Computing volumes of the grid elements." << endl;
+  if (rank == MASTER_NODE && Screen_Output) cout << "Computing volumes of the grid elements." << endl;
 
-  MaxVolume = -1E22; MinVolume = 1E22;
+  MaxVolume = -1E22;
+  MinVolume = 1E22;
 
   /*--- Load up each triangle and tetrahedron to check for negative volumes. ---*/
 
   for (iElem = 0; iElem < geometry->GetnElem(); iElem++) {
-
-    if (geometry->elem[iElem]->GetVTK_Type() == TRIANGLE)     nNodes = 3;
-    if (geometry->elem[iElem]->GetVTK_Type() == QUADRILATERAL)    nNodes = 4;
-    if (geometry->elem[iElem]->GetVTK_Type() == TETRAHEDRON)  nNodes = 4;
-    if (geometry->elem[iElem]->GetVTK_Type() == PYRAMID)      nNodes = 5;
-    if (geometry->elem[iElem]->GetVTK_Type() == PRISM)        nNodes = 6;
-    if (geometry->elem[iElem]->GetVTK_Type() == HEXAHEDRON)   nNodes = 8;
+    if (geometry->elem[iElem]->GetVTK_Type() == TRIANGLE) nNodes = 3;
+    if (geometry->elem[iElem]->GetVTK_Type() == QUADRILATERAL) nNodes = 4;
+    if (geometry->elem[iElem]->GetVTK_Type() == TETRAHEDRON) nNodes = 4;
+    if (geometry->elem[iElem]->GetVTK_Type() == PYRAMID) nNodes = 5;
+    if (geometry->elem[iElem]->GetVTK_Type() == PRISM) nNodes = 6;
+    if (geometry->elem[iElem]->GetVTK_Type() == HEXAHEDRON) nNodes = 8;
 
     for (iNodes = 0; iNodes < nNodes; iNodes++) {
       PointCorners[iNodes] = geometry->elem[iElem]->GetNode(iNodes);
@@ -278,13 +273,15 @@ void CVolumetricMovement::ComputeDeforming_Element_Volume(CGeometry *geometry, s
     geometry->elem[iElem]->SetVolume(Volume);
 
     if (!RightVol) ElemCounter++;
-
   }
 
 #ifdef HAVE_MPI
-  unsigned long ElemCounter_Local = ElemCounter; ElemCounter = 0;
-  su2double MaxVolume_Local = MaxVolume; MaxVolume = 0.0;
-  su2double MinVolume_Local = MinVolume; MinVolume = 0.0;
+  unsigned long ElemCounter_Local = ElemCounter;
+  ElemCounter = 0;
+  su2double MaxVolume_Local = MaxVolume;
+  MaxVolume = 0.0;
+  su2double MinVolume_Local = MinVolume;
+  MinVolume = 0.0;
   SU2_MPI::Allreduce(&ElemCounter_Local, &ElemCounter, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
   SU2_MPI::Allreduce(&MaxVolume_Local, &MaxVolume, 1, MPI_DOUBLE, MPI_MAX, SU2_MPI::GetComm());
   SU2_MPI::Allreduce(&MinVolume_Local, &MinVolume, 1, MPI_DOUBLE, MPI_MIN, SU2_MPI::GetComm());
@@ -293,22 +290,21 @@ void CVolumetricMovement::ComputeDeforming_Element_Volume(CGeometry *geometry, s
   /*--- Volume from  0 to 1 ---*/
 
   for (iElem = 0; iElem < geometry->GetnElem(); iElem++) {
-    Volume = geometry->elem[iElem]->GetVolume()/MaxVolume;
+    Volume = geometry->elem[iElem]->GetVolume() / MaxVolume;
     geometry->elem[iElem]->SetVolume(Volume);
   }
 
   if ((ElemCounter != 0) && (rank == MASTER_NODE) && (Screen_Output))
-    cout <<"There are " << ElemCounter << " elements with negative volume.\n" << endl;
-
+    cout << "There are " << ElemCounter << " elements with negative volume.\n" << endl;
 }
 
-void CVolumetricMovement::ComputenNonconvexElements(CGeometry *geometry, bool Screen_Output) {
+void CVolumetricMovement::ComputenNonconvexElements(CGeometry* geometry, bool Screen_Output) {
   unsigned long iElem;
   unsigned short iDim;
   unsigned long nNonconvexElements = 0;
 
   /*--- Load up each tetrahedron to check for convex properties. ---*/
-  if (nDim == 2){
+  if (nDim == 2) {
     for (iElem = 0; iElem < geometry->GetnElem(); iElem++) {
       su2double minCrossProduct = 1.e6, maxCrossProduct = -1.e6;
 
@@ -325,35 +321,34 @@ void CVolumetricMovement::ComputenNonconvexElements(CGeometry *geometry, bool Sc
       }
 
       /*--- Determine whether element is convex ---*/
-      for (iNodes = 0; iNodes < nNodes; iNodes ++) {
-
+      for (iNodes = 0; iNodes < nNodes; iNodes++) {
         /*--- Calculate minimum and maximum angle between edge vectors adjacent to each node ---*/
         su2double edgeVector_i[3], edgeVector_j[3];
 
-        for (iDim = 0; iDim < nDim; iDim ++) {
+        for (iDim = 0; iDim < nDim; iDim++) {
           if (iNodes == 0) {
-            edgeVector_i[iDim] = CoordCorners[nNodes-1][iDim] - CoordCorners[iNodes][iDim];
+            edgeVector_i[iDim] = CoordCorners[nNodes - 1][iDim] - CoordCorners[iNodes][iDim];
           } else {
-            edgeVector_i[iDim] = CoordCorners[iNodes-1][iDim] - CoordCorners[iNodes][iDim];
+            edgeVector_i[iDim] = CoordCorners[iNodes - 1][iDim] - CoordCorners[iNodes][iDim];
           }
 
-          if (iNodes == nNodes-1) {
+          if (iNodes == nNodes - 1) {
             edgeVector_j[iDim] = CoordCorners[0][iDim] - CoordCorners[iNodes][iDim];
           } else {
-            edgeVector_j[iDim] = CoordCorners[iNodes+1][iDim] - CoordCorners[iNodes][iDim];
+            edgeVector_j[iDim] = CoordCorners[iNodes + 1][iDim] - CoordCorners[iNodes][iDim];
           }
         }
 
         /*--- Calculate cross product of edge vectors ---*/
         su2double crossProduct;
-        crossProduct = edgeVector_i[1]*edgeVector_j[0] - edgeVector_i[0]*edgeVector_j[1];
+        crossProduct = edgeVector_i[1] * edgeVector_j[0] - edgeVector_i[0] * edgeVector_j[1];
 
         if (crossProduct < minCrossProduct) minCrossProduct = crossProduct;
         if (crossProduct > maxCrossProduct) maxCrossProduct = crossProduct;
       }
 
       /*--- Element is nonconvex if cross product of at least one set of adjacent edges is negative ---*/
-      if (minCrossProduct < 0 && maxCrossProduct > 0){
+      if (minCrossProduct < 0 && maxCrossProduct > 0) {
         nNonconvexElements++;
       }
     }
@@ -361,17 +356,16 @@ void CVolumetricMovement::ComputenNonconvexElements(CGeometry *geometry, bool Sc
     cout << "\nWARNING: Convexity is not checked for 3D elements (issue #1171).\n" << endl;
   }
 
-  unsigned long nNonconvexElements_Local = nNonconvexElements; nNonconvexElements = 0;
+  unsigned long nNonconvexElements_Local = nNonconvexElements;
+  nNonconvexElements = 0;
   SU2_MPI::Allreduce(&nNonconvexElements_Local, &nNonconvexElements, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
 
   /*--- Set number of nonconvex elements in geometry ---*/
   geometry->SetnNonconvexElements(nNonconvexElements);
 }
 
-
-
-void CVolumetricMovement::ComputeSolid_Wall_Distance(CGeometry *geometry, CConfig *config, su2double &MinDistance, su2double &MaxDistance) const {
-
+void CVolumetricMovement::ComputeSolid_Wall_Distance(CGeometry* geometry, CConfig* config, su2double& MinDistance,
+                                                     su2double& MaxDistance) const {
   unsigned long nVertex_SolidWall, ii, jj, iVertex, iPoint, pointID;
   unsigned short iMarker, iDim;
   su2double dist, MaxDistance_Local, MinDistance_Local;
@@ -379,75 +373,69 @@ void CVolumetricMovement::ComputeSolid_Wall_Distance(CGeometry *geometry, CConfi
 
   /*--- Initialize min and max distance ---*/
 
-  MaxDistance = -1E22; MinDistance = 1E22;
+  MaxDistance = -1E22;
+  MinDistance = 1E22;
 
   /*--- Compute the total number of nodes on no-slip boundaries ---*/
 
   nVertex_SolidWall = 0;
-  for(iMarker=0; iMarker<config->GetnMarker_All(); ++iMarker) {
-    if(config->GetSolid_Wall(iMarker))
-      nVertex_SolidWall += geometry->GetnVertex(iMarker);
+  for (iMarker = 0; iMarker < config->GetnMarker_All(); ++iMarker) {
+    if (config->GetSolid_Wall(iMarker)) nVertex_SolidWall += geometry->GetnVertex(iMarker);
   }
 
   /*--- Allocate the vectors to hold boundary node coordinates
    and its local ID. ---*/
 
-  vector<su2double>     Coord_bound(nDim*nVertex_SolidWall);
+  vector<su2double> Coord_bound(nDim * nVertex_SolidWall);
   vector<unsigned long> PointIDs(nVertex_SolidWall);
 
   /*--- Retrieve and store the coordinates of the no-slip boundary nodes
    and their local point IDs. ---*/
 
-  ii = 0; jj = 0;
-  for (iMarker=0; iMarker<config->GetnMarker_All(); ++iMarker) {
+  ii = 0;
+  jj = 0;
+  for (iMarker = 0; iMarker < config->GetnMarker_All(); ++iMarker) {
     if (config->GetSolid_Wall(iMarker)) {
-      for (iVertex=0; iVertex<geometry->GetnVertex(iMarker); ++iVertex) {
+      for (iVertex = 0; iVertex < geometry->GetnVertex(iMarker); ++iVertex) {
         iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
         PointIDs[jj++] = iPoint;
-        for (iDim=0; iDim<nDim; ++iDim)
-          Coord_bound[ii++] = geometry->nodes->GetCoord(iPoint, iDim);
+        for (iDim = 0; iDim < nDim; ++iDim) Coord_bound[ii++] = geometry->nodes->GetCoord(iPoint, iDim);
       }
     }
   }
 
   /*--- Build the ADT of the boundary nodes. ---*/
 
-  CADTPointsOnlyClass WallADT(nDim, nVertex_SolidWall, Coord_bound.data(),
-                              PointIDs.data(), true);
+  CADTPointsOnlyClass WallADT(nDim, nVertex_SolidWall, Coord_bound.data(), PointIDs.data(), true);
 
   /*--- Loop over all interior mesh nodes and compute the distances to each
    of the no-slip boundary nodes. Store the minimum distance to the wall
    for each interior mesh node. ---*/
 
-  if( WallADT.IsEmpty() ) {
-
+  if (WallADT.IsEmpty()) {
     /*--- No solid wall boundary nodes in the entire mesh.
      Set the wall distance to zero for all nodes. ---*/
 
-    for (iPoint=0; iPoint<geometry->GetnPoint(); ++iPoint)
-      geometry->nodes->SetWall_Distance(iPoint, 0.0);
-  }
-  else {
-
+    for (iPoint = 0; iPoint < geometry->GetnPoint(); ++iPoint) geometry->nodes->SetWall_Distance(iPoint, 0.0);
+  } else {
     /*--- Solid wall boundary nodes are present. Compute the wall
      distance for all nodes. ---*/
 
-    for(iPoint=0; iPoint<geometry->GetnPoint(); ++iPoint) {
-
-      WallADT.DetermineNearestNode(geometry->nodes->GetCoord(iPoint), dist,
-                                   pointID, rankID);
+    for (iPoint = 0; iPoint < geometry->GetnPoint(); ++iPoint) {
+      WallADT.DetermineNearestNode(geometry->nodes->GetCoord(iPoint), dist, pointID, rankID);
       geometry->nodes->SetWall_Distance(iPoint, dist);
 
       MaxDistance = max(MaxDistance, dist);
 
       /*--- To discard points on the surface we use > EPS ---*/
 
-      if (sqrt(dist) > EPS)  MinDistance = min(MinDistance, dist);
-
+      if (sqrt(dist) > EPS) MinDistance = min(MinDistance, dist);
     }
 
-    MaxDistance_Local = MaxDistance; MaxDistance = 0.0;
-    MinDistance_Local = MinDistance; MinDistance = 0.0;
+    MaxDistance_Local = MaxDistance;
+    MaxDistance = 0.0;
+    MinDistance_Local = MinDistance;
+    MinDistance = 0.0;
 
 #ifdef HAVE_MPI
     SU2_MPI::Allreduce(&MaxDistance_Local, &MaxDistance, 1, MPI_DOUBLE, MPI_MAX, SU2_MPI::GetComm());
@@ -456,53 +444,52 @@ void CVolumetricMovement::ComputeSolid_Wall_Distance(CGeometry *geometry, CConfi
     MaxDistance = MaxDistance_Local;
     MinDistance = MinDistance_Local;
 #endif
-
   }
-
 }
 
-su2double CVolumetricMovement::SetFEAMethodContributions_Elem(CGeometry *geometry, CConfig *config) {
-
+su2double CVolumetricMovement::SetFEAMethodContributions_Elem(CGeometry* geometry, CConfig* config) {
   unsigned short iVar, iDim, nNodes = 0, iNodes, StiffMatrix_nElem = 0;
   unsigned long iElem, PointCorners[8];
   su2double **StiffMatrix_Elem = nullptr, CoordCorners[8][3];
-  su2double MinVolume = 0.0, MaxVolume = 0.0, MinDistance = 0.0, MaxDistance = 0.0, ElemVolume = 0.0, ElemDistance = 0.0;
+  su2double MinVolume = 0.0, MaxVolume = 0.0, MinDistance = 0.0, MaxDistance = 0.0, ElemVolume = 0.0,
+            ElemDistance = 0.0;
 
-  bool Screen_Output  = config->GetDeform_Output();
+  bool Screen_Output = config->GetDeform_Output();
 
   /*--- Allocate maximum size (quadrilateral and hexahedron) ---*/
 
-  if (nDim == 2) StiffMatrix_nElem = 8;
-  else StiffMatrix_nElem = 24;
+  if (nDim == 2)
+    StiffMatrix_nElem = 8;
+  else
+    StiffMatrix_nElem = 24;
 
-  StiffMatrix_Elem = new su2double* [StiffMatrix_nElem];
-  for (iVar = 0; iVar < StiffMatrix_nElem; iVar++)
-    StiffMatrix_Elem[iVar] = new su2double [StiffMatrix_nElem];
+  StiffMatrix_Elem = new su2double*[StiffMatrix_nElem];
+  for (iVar = 0; iVar < StiffMatrix_nElem; iVar++) StiffMatrix_Elem[iVar] = new su2double[StiffMatrix_nElem];
 
   /*--- Compute min volume in the entire mesh. ---*/
 
   ComputeDeforming_Element_Volume(geometry, MinVolume, MaxVolume, Screen_Output);
-  if (rank == MASTER_NODE && Screen_Output) cout <<"Min. volume: "<< MinVolume <<", max. volume: "<< MaxVolume <<"." << endl;
+  if (rank == MASTER_NODE && Screen_Output)
+    cout << "Min. volume: " << MinVolume << ", max. volume: " << MaxVolume << "." << endl;
 
   /*--- Compute the distance to the nearest surface if needed
    as part of the stiffness calculation.. ---*/
 
-  if ((config->GetDeform_Stiffness_Type() == SOLID_WALL_DISTANCE) ||
-      (config->GetDeform_Limit() < 1E6)) {
+  if ((config->GetDeform_Stiffness_Type() == SOLID_WALL_DISTANCE) || (config->GetDeform_Limit() < 1E6)) {
     ComputeSolid_Wall_Distance(geometry, config, MinDistance, MaxDistance);
-    if (rank == MASTER_NODE && Screen_Output) cout <<"Min. distance: "<< MinDistance <<", max. distance: "<< MaxDistance <<"." << endl;
+    if (rank == MASTER_NODE && Screen_Output)
+      cout << "Min. distance: " << MinDistance << ", max. distance: " << MaxDistance << "." << endl;
   }
 
   /*--- Compute contributions from each element by forming the stiffness matrix (FEA) ---*/
 
   for (iElem = 0; iElem < geometry->GetnElem(); iElem++) {
-
-    if (geometry->elem[iElem]->GetVTK_Type() == TRIANGLE)      nNodes = 3;
+    if (geometry->elem[iElem]->GetVTK_Type() == TRIANGLE) nNodes = 3;
     if (geometry->elem[iElem]->GetVTK_Type() == QUADRILATERAL) nNodes = 4;
-    if (geometry->elem[iElem]->GetVTK_Type() == TETRAHEDRON)   nNodes = 4;
-    if (geometry->elem[iElem]->GetVTK_Type() == PYRAMID)       nNodes = 5;
-    if (geometry->elem[iElem]->GetVTK_Type() == PRISM)         nNodes = 6;
-    if (geometry->elem[iElem]->GetVTK_Type() == HEXAHEDRON)    nNodes = 8;
+    if (geometry->elem[iElem]->GetVTK_Type() == TETRAHEDRON) nNodes = 4;
+    if (geometry->elem[iElem]->GetVTK_Type() == PYRAMID) nNodes = 5;
+    if (geometry->elem[iElem]->GetVTK_Type() == PRISM) nNodes = 6;
+    if (geometry->elem[iElem]->GetVTK_Type() == HEXAHEDRON) nNodes = 8;
 
     for (iNodes = 0; iNodes < nNodes; iNodes++) {
       PointCorners[iNodes] = geometry->elem[iElem]->GetNode(iNodes);
@@ -519,28 +506,29 @@ su2double CVolumetricMovement::SetFEAMethodContributions_Elem(CGeometry *geometr
       ElemDistance = 0.0;
       for (iNodes = 0; iNodes < nNodes; iNodes++)
         ElemDistance += geometry->nodes->GetWall_Distance(PointCorners[iNodes]);
-      ElemDistance = ElemDistance/(su2double)nNodes;
+      ElemDistance = ElemDistance / (su2double)nNodes;
     }
 
-    if (nDim == 2) SetFEA_StiffMatrix2D(geometry, config, StiffMatrix_Elem, PointCorners, CoordCorners, nNodes, ElemVolume, ElemDistance);
-    if (nDim == 3) SetFEA_StiffMatrix3D(geometry, config, StiffMatrix_Elem, PointCorners, CoordCorners, nNodes, ElemVolume, ElemDistance);
+    if (nDim == 2)
+      SetFEA_StiffMatrix2D(geometry, config, StiffMatrix_Elem, PointCorners, CoordCorners, nNodes, ElemVolume,
+                           ElemDistance);
+    if (nDim == 3)
+      SetFEA_StiffMatrix3D(geometry, config, StiffMatrix_Elem, PointCorners, CoordCorners, nNodes, ElemVolume,
+                           ElemDistance);
 
     AddFEA_StiffMatrix(geometry, StiffMatrix_Elem, PointCorners, nNodes);
-
   }
 
   /*--- Deallocate memory and exit ---*/
 
-  for (iVar = 0; iVar < StiffMatrix_nElem; iVar++)
-    delete [] StiffMatrix_Elem[iVar];
-  delete [] StiffMatrix_Elem;
+  for (iVar = 0; iVar < StiffMatrix_nElem; iVar++) delete[] StiffMatrix_Elem[iVar];
+  delete[] StiffMatrix_Elem;
 
   return MinVolume;
-
 }
 
-su2double CVolumetricMovement::ShapeFunc_Triangle(su2double Xi, su2double Eta, su2double CoordCorners[8][3], su2double DShapeFunction[8][4]) {
-
+su2double CVolumetricMovement::ShapeFunc_Triangle(su2double Xi, su2double Eta, su2double CoordCorners[8][3],
+                                                  su2double DShapeFunction[8][4]) {
   int i, j, k;
   su2double c0, c1, xsj;
   su2double xs[3][3], ad[3][3];
@@ -549,13 +537,16 @@ su2double CVolumetricMovement::ShapeFunc_Triangle(su2double Xi, su2double Eta, s
 
   DShapeFunction[0][3] = Xi;
   DShapeFunction[1][3] = Eta;
-  DShapeFunction[2][3] = 1-Xi-Eta;
+  DShapeFunction[2][3] = 1 - Xi - Eta;
 
   /*--- dN/d xi, dN/d eta ---*/
 
-  DShapeFunction[0][0] = 1.0;  DShapeFunction[0][1] = 0.0;
-  DShapeFunction[1][0] = 0.0;  DShapeFunction[1][1] = 1.0;
-  DShapeFunction[2][0] = -1.0; DShapeFunction[2][1] = -1.0;
+  DShapeFunction[0][0] = 1.0;
+  DShapeFunction[0][1] = 0.0;
+  DShapeFunction[1][0] = 0.0;
+  DShapeFunction[1][1] = 1.0;
+  DShapeFunction[2][0] = -1.0;
+  DShapeFunction[2][1] = -1.0;
 
   /*--- Jacobian transformation ---*/
 
@@ -563,7 +554,7 @@ su2double CVolumetricMovement::ShapeFunc_Triangle(su2double Xi, su2double Eta, s
     for (j = 0; j < 2; j++) {
       xs[i][j] = 0.0;
       for (k = 0; k < 3; k++) {
-        xs[i][j] = xs[i][j]+CoordCorners[k][j]*DShapeFunction[k][i];
+        xs[i][j] = xs[i][j] + CoordCorners[k][j] * DShapeFunction[k][i];
       }
     }
   }
@@ -577,48 +568,51 @@ su2double CVolumetricMovement::ShapeFunc_Triangle(su2double Xi, su2double Eta, s
 
   /*--- Determinant of Jacobian ---*/
 
-  xsj = ad[0][0]*ad[1][1]-ad[0][1]*ad[1][0];
+  xsj = ad[0][0] * ad[1][1] - ad[0][1] * ad[1][0];
 
   /*--- Jacobian inverse ---*/
 
   for (i = 0; i < 2; i++) {
     for (j = 0; j < 2; j++) {
-      xs[i][j] = ad[i][j]/xsj;
+      xs[i][j] = ad[i][j] / xsj;
     }
   }
 
   /*--- Derivatives with repect to global coordinates ---*/
 
   for (k = 0; k < 3; k++) {
-    c0 = xs[0][0]*DShapeFunction[k][0]+xs[0][1]*DShapeFunction[k][1]; // dN/dx
-    c1 = xs[1][0]*DShapeFunction[k][0]+xs[1][1]*DShapeFunction[k][1]; // dN/dy
-    DShapeFunction[k][0] = c0; // store dN/dx instead of dN/d xi
-    DShapeFunction[k][1] = c1; // store dN/dy instead of dN/d eta
+    c0 = xs[0][0] * DShapeFunction[k][0] + xs[0][1] * DShapeFunction[k][1];  // dN/dx
+    c1 = xs[1][0] * DShapeFunction[k][0] + xs[1][1] * DShapeFunction[k][1];  // dN/dy
+    DShapeFunction[k][0] = c0;                                               // store dN/dx instead of dN/d xi
+    DShapeFunction[k][1] = c1;                                               // store dN/dy instead of dN/d eta
   }
 
   return xsj;
-
 }
 
-su2double CVolumetricMovement::ShapeFunc_Quadrilateral(su2double Xi, su2double Eta, su2double CoordCorners[8][3], su2double DShapeFunction[8][4]) {
-
+su2double CVolumetricMovement::ShapeFunc_Quadrilateral(su2double Xi, su2double Eta, su2double CoordCorners[8][3],
+                                                       su2double DShapeFunction[8][4]) {
   int i, j, k;
   su2double c0, c1, xsj;
   su2double xs[3][3], ad[3][3];
 
   /*--- Shape functions ---*/
 
-  DShapeFunction[0][3] = 0.25*(1.0-Xi)*(1.0-Eta);
-  DShapeFunction[1][3] = 0.25*(1.0+Xi)*(1.0-Eta);
-  DShapeFunction[2][3] = 0.25*(1.0+Xi)*(1.0+Eta);
-  DShapeFunction[3][3] = 0.25*(1.0-Xi)*(1.0+Eta);
+  DShapeFunction[0][3] = 0.25 * (1.0 - Xi) * (1.0 - Eta);
+  DShapeFunction[1][3] = 0.25 * (1.0 + Xi) * (1.0 - Eta);
+  DShapeFunction[2][3] = 0.25 * (1.0 + Xi) * (1.0 + Eta);
+  DShapeFunction[3][3] = 0.25 * (1.0 - Xi) * (1.0 + Eta);
 
   /*--- dN/d xi, dN/d eta ---*/
 
-  DShapeFunction[0][0] = -0.25*(1.0-Eta); DShapeFunction[0][1] = -0.25*(1.0-Xi);
-  DShapeFunction[1][0] =  0.25*(1.0-Eta); DShapeFunction[1][1] = -0.25*(1.0+Xi);
-  DShapeFunction[2][0] =  0.25*(1.0+Eta); DShapeFunction[2][1] =  0.25*(1.0+Xi);
-  DShapeFunction[3][0] = -0.25*(1.0+Eta); DShapeFunction[3][1] =  0.25*(1.0-Xi);
+  DShapeFunction[0][0] = -0.25 * (1.0 - Eta);
+  DShapeFunction[0][1] = -0.25 * (1.0 - Xi);
+  DShapeFunction[1][0] = 0.25 * (1.0 - Eta);
+  DShapeFunction[1][1] = -0.25 * (1.0 + Xi);
+  DShapeFunction[2][0] = 0.25 * (1.0 + Eta);
+  DShapeFunction[2][1] = 0.25 * (1.0 + Xi);
+  DShapeFunction[3][0] = -0.25 * (1.0 + Eta);
+  DShapeFunction[3][1] = 0.25 * (1.0 - Xi);
 
   /*--- Jacobian transformation ---*/
 
@@ -626,7 +620,7 @@ su2double CVolumetricMovement::ShapeFunc_Quadrilateral(su2double Xi, su2double E
     for (j = 0; j < 2; j++) {
       xs[i][j] = 0.0;
       for (k = 0; k < 4; k++) {
-        xs[i][j] = xs[i][j]+CoordCorners[k][j]*DShapeFunction[k][i];
+        xs[i][j] = xs[i][j] + CoordCorners[k][j] * DShapeFunction[k][i];
       }
     }
   }
@@ -640,31 +634,30 @@ su2double CVolumetricMovement::ShapeFunc_Quadrilateral(su2double Xi, su2double E
 
   /*--- Determinant of Jacobian ---*/
 
-  xsj = ad[0][0]*ad[1][1]-ad[0][1]*ad[1][0];
+  xsj = ad[0][0] * ad[1][1] - ad[0][1] * ad[1][0];
 
   /*--- Jacobian inverse ---*/
 
   for (i = 0; i < 2; i++) {
     for (j = 0; j < 2; j++) {
-      xs[i][j] = ad[i][j]/xsj;
+      xs[i][j] = ad[i][j] / xsj;
     }
   }
 
   /*--- Derivatives with repect to global coordinates ---*/
 
   for (k = 0; k < 4; k++) {
-    c0 = xs[0][0]*DShapeFunction[k][0]+xs[0][1]*DShapeFunction[k][1]; // dN/dx
-    c1 = xs[1][0]*DShapeFunction[k][0]+xs[1][1]*DShapeFunction[k][1]; // dN/dy
-    DShapeFunction[k][0] = c0; // store dN/dx instead of dN/d xi
-    DShapeFunction[k][1] = c1; // store dN/dy instead of dN/d eta
+    c0 = xs[0][0] * DShapeFunction[k][0] + xs[0][1] * DShapeFunction[k][1];  // dN/dx
+    c1 = xs[1][0] * DShapeFunction[k][0] + xs[1][1] * DShapeFunction[k][1];  // dN/dy
+    DShapeFunction[k][0] = c0;                                               // store dN/dx instead of dN/d xi
+    DShapeFunction[k][1] = c1;                                               // store dN/dy instead of dN/d eta
   }
 
   return xsj;
-
 }
 
-su2double CVolumetricMovement::ShapeFunc_Tetra(su2double Xi, su2double Eta, su2double Zeta, su2double CoordCorners[8][3], su2double DShapeFunction[8][4]) {
-
+su2double CVolumetricMovement::ShapeFunc_Tetra(su2double Xi, su2double Eta, su2double Zeta,
+                                               su2double CoordCorners[8][3], su2double DShapeFunction[8][4]) {
   int i, j, k;
   su2double c0, c1, c2, xsj;
   su2double xs[3][3], ad[3][3];
@@ -678,10 +671,18 @@ su2double CVolumetricMovement::ShapeFunc_Tetra(su2double Xi, su2double Eta, su2d
 
   /*--- dN/d xi, dN/d eta, dN/d zeta ---*/
 
-  DShapeFunction[0][0] = 1.0;  DShapeFunction[0][1] = 0.0;  DShapeFunction[0][2] = 0.0;
-  DShapeFunction[1][0] = 0.0;  DShapeFunction[1][1] = 0.0;  DShapeFunction[1][2] = 1.0;
-  DShapeFunction[2][0] = -1.0; DShapeFunction[2][1] = -1.0; DShapeFunction[2][2] = -1.0;
-  DShapeFunction[3][0] = 0.0;  DShapeFunction[3][1] = 1.0;  DShapeFunction[3][2] = 0.0;
+  DShapeFunction[0][0] = 1.0;
+  DShapeFunction[0][1] = 0.0;
+  DShapeFunction[0][2] = 0.0;
+  DShapeFunction[1][0] = 0.0;
+  DShapeFunction[1][1] = 0.0;
+  DShapeFunction[1][2] = 1.0;
+  DShapeFunction[2][0] = -1.0;
+  DShapeFunction[2][1] = -1.0;
+  DShapeFunction[2][2] = -1.0;
+  DShapeFunction[3][0] = 0.0;
+  DShapeFunction[3][1] = 1.0;
+  DShapeFunction[3][2] = 0.0;
 
   /*--- Jacobian transformation ---*/
 
@@ -689,84 +690,83 @@ su2double CVolumetricMovement::ShapeFunc_Tetra(su2double Xi, su2double Eta, su2d
     for (j = 0; j < 3; j++) {
       xs[i][j] = 0.0;
       for (k = 0; k < 4; k++) {
-        xs[i][j] = xs[i][j]+CoordCorners[k][j]*DShapeFunction[k][i];
+        xs[i][j] = xs[i][j] + CoordCorners[k][j] * DShapeFunction[k][i];
       }
     }
   }
 
   /*--- Adjoint to Jacobian ---*/
 
-  ad[0][0] = xs[1][1]*xs[2][2]-xs[1][2]*xs[2][1];
-  ad[0][1] = xs[0][2]*xs[2][1]-xs[0][1]*xs[2][2];
-  ad[0][2] = xs[0][1]*xs[1][2]-xs[0][2]*xs[1][1];
-  ad[1][0] = xs[1][2]*xs[2][0]-xs[1][0]*xs[2][2];
-  ad[1][1] = xs[0][0]*xs[2][2]-xs[0][2]*xs[2][0];
-  ad[1][2] = xs[0][2]*xs[1][0]-xs[0][0]*xs[1][2];
-  ad[2][0] = xs[1][0]*xs[2][1]-xs[1][1]*xs[2][0];
-  ad[2][1] = xs[0][1]*xs[2][0]-xs[0][0]*xs[2][1];
-  ad[2][2] = xs[0][0]*xs[1][1]-xs[0][1]*xs[1][0];
+  ad[0][0] = xs[1][1] * xs[2][2] - xs[1][2] * xs[2][1];
+  ad[0][1] = xs[0][2] * xs[2][1] - xs[0][1] * xs[2][2];
+  ad[0][2] = xs[0][1] * xs[1][2] - xs[0][2] * xs[1][1];
+  ad[1][0] = xs[1][2] * xs[2][0] - xs[1][0] * xs[2][2];
+  ad[1][1] = xs[0][0] * xs[2][2] - xs[0][2] * xs[2][0];
+  ad[1][2] = xs[0][2] * xs[1][0] - xs[0][0] * xs[1][2];
+  ad[2][0] = xs[1][0] * xs[2][1] - xs[1][1] * xs[2][0];
+  ad[2][1] = xs[0][1] * xs[2][0] - xs[0][0] * xs[2][1];
+  ad[2][2] = xs[0][0] * xs[1][1] - xs[0][1] * xs[1][0];
 
   /*--- Determinant of Jacobian ---*/
 
-  xsj = xs[0][0]*ad[0][0]+xs[0][1]*ad[1][0]+xs[0][2]*ad[2][0];
+  xsj = xs[0][0] * ad[0][0] + xs[0][1] * ad[1][0] + xs[0][2] * ad[2][0];
 
   /*--- Jacobian inverse ---*/
 
   for (i = 0; i < 3; i++) {
     for (j = 0; j < 3; j++) {
-      xs[i][j] = ad[i][j]/xsj;
+      xs[i][j] = ad[i][j] / xsj;
     }
   }
 
   /*--- Derivatives with repect to global coordinates ---*/
 
   for (k = 0; k < 4; k++) {
-    c0 = xs[0][0]*DShapeFunction[k][0]+xs[0][1]*DShapeFunction[k][1]+xs[0][2]*DShapeFunction[k][2]; // dN/dx
-    c1 = xs[1][0]*DShapeFunction[k][0]+xs[1][1]*DShapeFunction[k][1]+xs[1][2]*DShapeFunction[k][2]; // dN/dy
-    c2 = xs[2][0]*DShapeFunction[k][0]+xs[2][1]*DShapeFunction[k][1]+xs[2][2]*DShapeFunction[k][2]; // dN/dz
-    DShapeFunction[k][0] = c0; // store dN/dx instead of dN/d xi
-    DShapeFunction[k][1] = c1; // store dN/dy instead of dN/d eta
-    DShapeFunction[k][2] = c2; // store dN/dz instead of dN/d zeta
+    c0 = xs[0][0] * DShapeFunction[k][0] + xs[0][1] * DShapeFunction[k][1] + xs[0][2] * DShapeFunction[k][2];  // dN/dx
+    c1 = xs[1][0] * DShapeFunction[k][0] + xs[1][1] * DShapeFunction[k][1] + xs[1][2] * DShapeFunction[k][2];  // dN/dy
+    c2 = xs[2][0] * DShapeFunction[k][0] + xs[2][1] * DShapeFunction[k][1] + xs[2][2] * DShapeFunction[k][2];  // dN/dz
+    DShapeFunction[k][0] = c0;  // store dN/dx instead of dN/d xi
+    DShapeFunction[k][1] = c1;  // store dN/dy instead of dN/d eta
+    DShapeFunction[k][2] = c2;  // store dN/dz instead of dN/d zeta
   }
 
   return xsj;
-
 }
 
-su2double CVolumetricMovement::ShapeFunc_Pyram(su2double Xi, su2double Eta, su2double Zeta, su2double CoordCorners[8][3], su2double DShapeFunction[8][4]) {
-
+su2double CVolumetricMovement::ShapeFunc_Pyram(su2double Xi, su2double Eta, su2double Zeta,
+                                               su2double CoordCorners[8][3], su2double DShapeFunction[8][4]) {
   int i, j, k;
   su2double c0, c1, c2, xsj;
   su2double xs[3][3], ad[3][3];
 
   /*--- Shape functions ---*/
 
-  DShapeFunction[0][3] = 0.25*(-Xi+Eta+Zeta-1.0)*(-Xi-Eta+Zeta-1.0)/(1.0-Zeta);
-  DShapeFunction[1][3] = 0.25*(-Xi-Eta+Zeta-1.0)*( Xi-Eta+Zeta-1.0)/(1.0-Zeta);
-  DShapeFunction[2][3] = 0.25*( Xi+Eta+Zeta-1.0)*( Xi-Eta+Zeta-1.0)/(1.0-Zeta);
-  DShapeFunction[3][3] = 0.25*( Xi+Eta+Zeta-1.0)*(-Xi+Eta+Zeta-1.0)/(1.0-Zeta);
+  DShapeFunction[0][3] = 0.25 * (-Xi + Eta + Zeta - 1.0) * (-Xi - Eta + Zeta - 1.0) / (1.0 - Zeta);
+  DShapeFunction[1][3] = 0.25 * (-Xi - Eta + Zeta - 1.0) * (Xi - Eta + Zeta - 1.0) / (1.0 - Zeta);
+  DShapeFunction[2][3] = 0.25 * (Xi + Eta + Zeta - 1.0) * (Xi - Eta + Zeta - 1.0) / (1.0 - Zeta);
+  DShapeFunction[3][3] = 0.25 * (Xi + Eta + Zeta - 1.0) * (-Xi + Eta + Zeta - 1.0) / (1.0 - Zeta);
   DShapeFunction[4][3] = Zeta;
 
   /*--- dN/d xi ---*/
 
-  DShapeFunction[0][0] = 0.5*(Zeta-Xi-1.0)/(Zeta-1.0);
-  DShapeFunction[1][0] = 0.5*Xi/(Zeta-1.0);
-  DShapeFunction[2][0] = 0.5*(1.0-Zeta-Xi)/(Zeta-1.0);
+  DShapeFunction[0][0] = 0.5 * (Zeta - Xi - 1.0) / (Zeta - 1.0);
+  DShapeFunction[1][0] = 0.5 * Xi / (Zeta - 1.0);
+  DShapeFunction[2][0] = 0.5 * (1.0 - Zeta - Xi) / (Zeta - 1.0);
   DShapeFunction[3][0] = DShapeFunction[1][0];
   DShapeFunction[4][0] = 0.0;
 
   /*--- dN/d eta ---*/
 
-  DShapeFunction[0][1] = 0.5*Eta/(Zeta-1.0);
-  DShapeFunction[1][1] = 0.5*(Zeta-Eta-1.0)/(Zeta-1.0);
+  DShapeFunction[0][1] = 0.5 * Eta / (Zeta - 1.0);
+  DShapeFunction[1][1] = 0.5 * (Zeta - Eta - 1.0) / (Zeta - 1.0);
   DShapeFunction[2][1] = DShapeFunction[0][1];
-  DShapeFunction[3][1] = 0.5*(1.0-Zeta-Eta)/(Zeta-1.0);
+  DShapeFunction[3][1] = 0.5 * (1.0 - Zeta - Eta) / (Zeta - 1.0);
   DShapeFunction[4][1] = 0.0;
 
   /*--- dN/d zeta ---*/
 
-  DShapeFunction[0][2] = 0.25*(-1.0 + 2.0*Zeta - Zeta*Zeta - Eta*Eta + Xi*Xi)/((1.0-Zeta)*(1.0-Zeta));
-  DShapeFunction[1][2] = 0.25*(-1.0 + 2.0*Zeta - Zeta*Zeta + Eta*Eta - Xi*Xi)/((1.0-Zeta)*(1.0-Zeta));
+  DShapeFunction[0][2] = 0.25 * (-1.0 + 2.0 * Zeta - Zeta * Zeta - Eta * Eta + Xi * Xi) / ((1.0 - Zeta) * (1.0 - Zeta));
+  DShapeFunction[1][2] = 0.25 * (-1.0 + 2.0 * Zeta - Zeta * Zeta + Eta * Eta - Xi * Xi) / ((1.0 - Zeta) * (1.0 - Zeta));
   DShapeFunction[2][2] = DShapeFunction[0][2];
   DShapeFunction[3][2] = DShapeFunction[1][2];
   DShapeFunction[4][2] = 1.0;
@@ -777,73 +777,84 @@ su2double CVolumetricMovement::ShapeFunc_Pyram(su2double Xi, su2double Eta, su2d
     for (j = 0; j < 3; j++) {
       xs[i][j] = 0.0;
       for (k = 0; k < 5; k++) {
-        xs[i][j] = xs[i][j]+CoordCorners[k][j]*DShapeFunction[k][i];
+        xs[i][j] = xs[i][j] + CoordCorners[k][j] * DShapeFunction[k][i];
       }
     }
   }
 
   /*--- Adjoint to Jacobian ---*/
 
-  ad[0][0] = xs[1][1]*xs[2][2]-xs[1][2]*xs[2][1];
-  ad[0][1] = xs[0][2]*xs[2][1]-xs[0][1]*xs[2][2];
-  ad[0][2] = xs[0][1]*xs[1][2]-xs[0][2]*xs[1][1];
-  ad[1][0] = xs[1][2]*xs[2][0]-xs[1][0]*xs[2][2];
-  ad[1][1] = xs[0][0]*xs[2][2]-xs[0][2]*xs[2][0];
-  ad[1][2] = xs[0][2]*xs[1][0]-xs[0][0]*xs[1][2];
-  ad[2][0] = xs[1][0]*xs[2][1]-xs[1][1]*xs[2][0];
-  ad[2][1] = xs[0][1]*xs[2][0]-xs[0][0]*xs[2][1];
-  ad[2][2] = xs[0][0]*xs[1][1]-xs[0][1]*xs[1][0];
+  ad[0][0] = xs[1][1] * xs[2][2] - xs[1][2] * xs[2][1];
+  ad[0][1] = xs[0][2] * xs[2][1] - xs[0][1] * xs[2][2];
+  ad[0][2] = xs[0][1] * xs[1][2] - xs[0][2] * xs[1][1];
+  ad[1][0] = xs[1][2] * xs[2][0] - xs[1][0] * xs[2][2];
+  ad[1][1] = xs[0][0] * xs[2][2] - xs[0][2] * xs[2][0];
+  ad[1][2] = xs[0][2] * xs[1][0] - xs[0][0] * xs[1][2];
+  ad[2][0] = xs[1][0] * xs[2][1] - xs[1][1] * xs[2][0];
+  ad[2][1] = xs[0][1] * xs[2][0] - xs[0][0] * xs[2][1];
+  ad[2][2] = xs[0][0] * xs[1][1] - xs[0][1] * xs[1][0];
 
   /*--- Determinant of Jacobian ---*/
 
-  xsj = xs[0][0]*ad[0][0]+xs[0][1]*ad[1][0]+xs[0][2]*ad[2][0];
+  xsj = xs[0][0] * ad[0][0] + xs[0][1] * ad[1][0] + xs[0][2] * ad[2][0];
 
   /*--- Jacobian inverse ---*/
 
   for (i = 0; i < 3; i++) {
     for (j = 0; j < 3; j++) {
-      xs[i][j] = ad[i][j]/xsj;
+      xs[i][j] = ad[i][j] / xsj;
     }
   }
 
   /*--- Derivatives with repect to global coordinates ---*/
 
   for (k = 0; k < 5; k++) {
-    c0 = xs[0][0]*DShapeFunction[k][0]+xs[0][1]*DShapeFunction[k][1]+xs[0][2]*DShapeFunction[k][2]; // dN/dx
-    c1 = xs[1][0]*DShapeFunction[k][0]+xs[1][1]*DShapeFunction[k][1]+xs[1][2]*DShapeFunction[k][2]; // dN/dy
-    c2 = xs[2][0]*DShapeFunction[k][0]+xs[2][1]*DShapeFunction[k][1]+xs[2][2]*DShapeFunction[k][2]; // dN/dz
-    DShapeFunction[k][0] = c0; // store dN/dx instead of dN/d xi
-    DShapeFunction[k][1] = c1; // store dN/dy instead of dN/d eta
-    DShapeFunction[k][2] = c2; // store dN/dz instead of dN/d zeta
+    c0 = xs[0][0] * DShapeFunction[k][0] + xs[0][1] * DShapeFunction[k][1] + xs[0][2] * DShapeFunction[k][2];  // dN/dx
+    c1 = xs[1][0] * DShapeFunction[k][0] + xs[1][1] * DShapeFunction[k][1] + xs[1][2] * DShapeFunction[k][2];  // dN/dy
+    c2 = xs[2][0] * DShapeFunction[k][0] + xs[2][1] * DShapeFunction[k][1] + xs[2][2] * DShapeFunction[k][2];  // dN/dz
+    DShapeFunction[k][0] = c0;  // store dN/dx instead of dN/d xi
+    DShapeFunction[k][1] = c1;  // store dN/dy instead of dN/d eta
+    DShapeFunction[k][2] = c2;  // store dN/dz instead of dN/d zeta
   }
 
   return xsj;
-
 }
 
-su2double CVolumetricMovement::ShapeFunc_Prism(su2double Xi, su2double Eta, su2double Zeta, su2double CoordCorners[8][3], su2double DShapeFunction[8][4]) {
-
+su2double CVolumetricMovement::ShapeFunc_Prism(su2double Xi, su2double Eta, su2double Zeta,
+                                               su2double CoordCorners[8][3], su2double DShapeFunction[8][4]) {
   int i, j, k;
   su2double c0, c1, c2, xsj;
   su2double xs[3][3], ad[3][3];
 
   /*--- Shape functions ---*/
 
-  DShapeFunction[0][3] = 0.5*Eta*(1.0-Xi);
-  DShapeFunction[1][3] = 0.5*Zeta*(1.0-Xi);
-  DShapeFunction[2][3] = 0.5*(1.0-Eta-Zeta)*(1.0-Xi);
-  DShapeFunction[3][3] = 0.5*Eta*(Xi+1.0);
-  DShapeFunction[4][3] = 0.5*Zeta*(Xi+1.0);
-  DShapeFunction[5][3] = 0.5*(1.0-Eta-Zeta)*(Xi+1.0);
+  DShapeFunction[0][3] = 0.5 * Eta * (1.0 - Xi);
+  DShapeFunction[1][3] = 0.5 * Zeta * (1.0 - Xi);
+  DShapeFunction[2][3] = 0.5 * (1.0 - Eta - Zeta) * (1.0 - Xi);
+  DShapeFunction[3][3] = 0.5 * Eta * (Xi + 1.0);
+  DShapeFunction[4][3] = 0.5 * Zeta * (Xi + 1.0);
+  DShapeFunction[5][3] = 0.5 * (1.0 - Eta - Zeta) * (Xi + 1.0);
 
   /*--- dN/d Xi, dN/d Eta, dN/d Zeta ---*/
 
-  DShapeFunction[0][0] = -0.5*Eta;            DShapeFunction[0][1] = 0.5*(1.0-Xi);      DShapeFunction[0][2] = 0.0;
-  DShapeFunction[1][0] = -0.5*Zeta;           DShapeFunction[1][1] = 0.0;               DShapeFunction[1][2] = 0.5*(1.0-Xi);
-  DShapeFunction[2][0] = -0.5*(1.0-Eta-Zeta); DShapeFunction[2][1] = -0.5*(1.0-Xi);     DShapeFunction[2][2] = -0.5*(1.0-Xi);
-  DShapeFunction[3][0] = 0.5*Eta;             DShapeFunction[3][1] = 0.5*(Xi+1.0);      DShapeFunction[3][2] = 0.0;
-  DShapeFunction[4][0] = 0.5*Zeta;            DShapeFunction[4][1] = 0.0;               DShapeFunction[4][2] = 0.5*(Xi+1.0);
-  DShapeFunction[5][0] = 0.5*(1.0-Eta-Zeta);  DShapeFunction[5][1] = -0.5*(Xi+1.0);     DShapeFunction[5][2] = -0.5*(Xi+1.0);
+  DShapeFunction[0][0] = -0.5 * Eta;
+  DShapeFunction[0][1] = 0.5 * (1.0 - Xi);
+  DShapeFunction[0][2] = 0.0;
+  DShapeFunction[1][0] = -0.5 * Zeta;
+  DShapeFunction[1][1] = 0.0;
+  DShapeFunction[1][2] = 0.5 * (1.0 - Xi);
+  DShapeFunction[2][0] = -0.5 * (1.0 - Eta - Zeta);
+  DShapeFunction[2][1] = -0.5 * (1.0 - Xi);
+  DShapeFunction[2][2] = -0.5 * (1.0 - Xi);
+  DShapeFunction[3][0] = 0.5 * Eta;
+  DShapeFunction[3][1] = 0.5 * (Xi + 1.0);
+  DShapeFunction[3][2] = 0.0;
+  DShapeFunction[4][0] = 0.5 * Zeta;
+  DShapeFunction[4][1] = 0.0;
+  DShapeFunction[4][2] = 0.5 * (Xi + 1.0);
+  DShapeFunction[5][0] = 0.5 * (1.0 - Eta - Zeta);
+  DShapeFunction[5][1] = -0.5 * (Xi + 1.0);
+  DShapeFunction[5][2] = -0.5 * (Xi + 1.0);
 
   /*--- Jacobian transformation ---*/
 
@@ -851,100 +862,98 @@ su2double CVolumetricMovement::ShapeFunc_Prism(su2double Xi, su2double Eta, su2d
     for (j = 0; j < 3; j++) {
       xs[i][j] = 0.0;
       for (k = 0; k < 6; k++) {
-        xs[i][j] = xs[i][j]+CoordCorners[k][j]*DShapeFunction[k][i];
+        xs[i][j] = xs[i][j] + CoordCorners[k][j] * DShapeFunction[k][i];
       }
     }
   }
 
   /*--- Adjoint to Jacobian ---*/
 
-  ad[0][0] = xs[1][1]*xs[2][2]-xs[1][2]*xs[2][1];
-  ad[0][1] = xs[0][2]*xs[2][1]-xs[0][1]*xs[2][2];
-  ad[0][2] = xs[0][1]*xs[1][2]-xs[0][2]*xs[1][1];
-  ad[1][0] = xs[1][2]*xs[2][0]-xs[1][0]*xs[2][2];
-  ad[1][1] = xs[0][0]*xs[2][2]-xs[0][2]*xs[2][0];
-  ad[1][2] = xs[0][2]*xs[1][0]-xs[0][0]*xs[1][2];
-  ad[2][0] = xs[1][0]*xs[2][1]-xs[1][1]*xs[2][0];
-  ad[2][1] = xs[0][1]*xs[2][0]-xs[0][0]*xs[2][1];
-  ad[2][2] = xs[0][0]*xs[1][1]-xs[0][1]*xs[1][0];
+  ad[0][0] = xs[1][1] * xs[2][2] - xs[1][2] * xs[2][1];
+  ad[0][1] = xs[0][2] * xs[2][1] - xs[0][1] * xs[2][2];
+  ad[0][2] = xs[0][1] * xs[1][2] - xs[0][2] * xs[1][1];
+  ad[1][0] = xs[1][2] * xs[2][0] - xs[1][0] * xs[2][2];
+  ad[1][1] = xs[0][0] * xs[2][2] - xs[0][2] * xs[2][0];
+  ad[1][2] = xs[0][2] * xs[1][0] - xs[0][0] * xs[1][2];
+  ad[2][0] = xs[1][0] * xs[2][1] - xs[1][1] * xs[2][0];
+  ad[2][1] = xs[0][1] * xs[2][0] - xs[0][0] * xs[2][1];
+  ad[2][2] = xs[0][0] * xs[1][1] - xs[0][1] * xs[1][0];
 
   /*--- Determinant of Jacobian ---*/
 
-  xsj = xs[0][0]*ad[0][0]+xs[0][1]*ad[1][0]+xs[0][2]*ad[2][0];
+  xsj = xs[0][0] * ad[0][0] + xs[0][1] * ad[1][0] + xs[0][2] * ad[2][0];
 
   /*--- Jacobian inverse ---*/
 
   for (i = 0; i < 3; i++) {
     for (j = 0; j < 3; j++) {
-      xs[i][j] = ad[i][j]/xsj;
+      xs[i][j] = ad[i][j] / xsj;
     }
   }
 
   /*--- Derivatives with repect to global coordinates ---*/
 
   for (k = 0; k < 6; k++) {
-    c0 = xs[0][0]*DShapeFunction[k][0]+xs[0][1]*DShapeFunction[k][1]+xs[0][2]*DShapeFunction[k][2]; // dN/dx
-    c1 = xs[1][0]*DShapeFunction[k][0]+xs[1][1]*DShapeFunction[k][1]+xs[1][2]*DShapeFunction[k][2]; // dN/dy
-    c2 = xs[2][0]*DShapeFunction[k][0]+xs[2][1]*DShapeFunction[k][1]+xs[2][2]*DShapeFunction[k][2]; // dN/dz
-    DShapeFunction[k][0] = c0; // store dN/dx instead of dN/d xi
-    DShapeFunction[k][1] = c1; // store dN/dy instead of dN/d eta
-    DShapeFunction[k][2] = c2; // store dN/dz instead of dN/d zeta
+    c0 = xs[0][0] * DShapeFunction[k][0] + xs[0][1] * DShapeFunction[k][1] + xs[0][2] * DShapeFunction[k][2];  // dN/dx
+    c1 = xs[1][0] * DShapeFunction[k][0] + xs[1][1] * DShapeFunction[k][1] + xs[1][2] * DShapeFunction[k][2];  // dN/dy
+    c2 = xs[2][0] * DShapeFunction[k][0] + xs[2][1] * DShapeFunction[k][1] + xs[2][2] * DShapeFunction[k][2];  // dN/dz
+    DShapeFunction[k][0] = c0;  // store dN/dx instead of dN/d xi
+    DShapeFunction[k][1] = c1;  // store dN/dy instead of dN/d eta
+    DShapeFunction[k][2] = c2;  // store dN/dz instead of dN/d zeta
   }
 
   return xsj;
-
 }
 
-su2double CVolumetricMovement::ShapeFunc_Hexa(su2double Xi, su2double Eta, su2double Zeta, su2double CoordCorners[8][3], su2double DShapeFunction[8][4]) {
-
+su2double CVolumetricMovement::ShapeFunc_Hexa(su2double Xi, su2double Eta, su2double Zeta, su2double CoordCorners[8][3],
+                                              su2double DShapeFunction[8][4]) {
   int i, j, k;
   su2double c0, c1, c2, xsj;
   su2double xs[3][3], ad[3][3];
 
-
   /*--- Shape functions ---*/
 
-  DShapeFunction[0][3] = 0.125*(1.0-Xi)*(1.0-Eta)*(1.0-Zeta);
-  DShapeFunction[1][3] = 0.125*(1.0+Xi)*(1.0-Eta)*(1.0-Zeta);
-  DShapeFunction[2][3] = 0.125*(1.0+Xi)*(1.0+Eta)*(1.0-Zeta);
-  DShapeFunction[3][3] = 0.125*(1.0-Xi)*(1.0+Eta)*(1.0-Zeta);
-  DShapeFunction[4][3] = 0.125*(1.0-Xi)*(1.0-Eta)*(1.0+Zeta);
-  DShapeFunction[5][3] = 0.125*(1.0+Xi)*(1.0-Eta)*(1.0+Zeta);
-  DShapeFunction[6][3] = 0.125*(1.0+Xi)*(1.0+Eta)*(1.0+Zeta);
-  DShapeFunction[7][3] = 0.125*(1.0-Xi)*(1.0+Eta)*(1.0+Zeta);
+  DShapeFunction[0][3] = 0.125 * (1.0 - Xi) * (1.0 - Eta) * (1.0 - Zeta);
+  DShapeFunction[1][3] = 0.125 * (1.0 + Xi) * (1.0 - Eta) * (1.0 - Zeta);
+  DShapeFunction[2][3] = 0.125 * (1.0 + Xi) * (1.0 + Eta) * (1.0 - Zeta);
+  DShapeFunction[3][3] = 0.125 * (1.0 - Xi) * (1.0 + Eta) * (1.0 - Zeta);
+  DShapeFunction[4][3] = 0.125 * (1.0 - Xi) * (1.0 - Eta) * (1.0 + Zeta);
+  DShapeFunction[5][3] = 0.125 * (1.0 + Xi) * (1.0 - Eta) * (1.0 + Zeta);
+  DShapeFunction[6][3] = 0.125 * (1.0 + Xi) * (1.0 + Eta) * (1.0 + Zeta);
+  DShapeFunction[7][3] = 0.125 * (1.0 - Xi) * (1.0 + Eta) * (1.0 + Zeta);
 
   /*--- dN/d xi ---*/
 
-  DShapeFunction[0][0] = -0.125*(1.0-Eta)*(1.0-Zeta);
-  DShapeFunction[1][0] = 0.125*(1.0-Eta)*(1.0-Zeta);
-  DShapeFunction[2][0] = 0.125*(1.0+Eta)*(1.0-Zeta);
-  DShapeFunction[3][0] = -0.125*(1.0+Eta)*(1.0-Zeta);
-  DShapeFunction[4][0] = -0.125*(1.0-Eta)*(1.0+Zeta);
-  DShapeFunction[5][0] = 0.125*(1.0-Eta)*(1.0+Zeta);
-  DShapeFunction[6][0] = 0.125*(1.0+Eta)*(1.0+Zeta);
-  DShapeFunction[7][0] = -0.125*(1.0+Eta)*(1.0+Zeta);
+  DShapeFunction[0][0] = -0.125 * (1.0 - Eta) * (1.0 - Zeta);
+  DShapeFunction[1][0] = 0.125 * (1.0 - Eta) * (1.0 - Zeta);
+  DShapeFunction[2][0] = 0.125 * (1.0 + Eta) * (1.0 - Zeta);
+  DShapeFunction[3][0] = -0.125 * (1.0 + Eta) * (1.0 - Zeta);
+  DShapeFunction[4][0] = -0.125 * (1.0 - Eta) * (1.0 + Zeta);
+  DShapeFunction[5][0] = 0.125 * (1.0 - Eta) * (1.0 + Zeta);
+  DShapeFunction[6][0] = 0.125 * (1.0 + Eta) * (1.0 + Zeta);
+  DShapeFunction[7][0] = -0.125 * (1.0 + Eta) * (1.0 + Zeta);
 
   /*--- dN/d eta ---*/
 
-  DShapeFunction[0][1] = -0.125*(1.0-Xi)*(1.0-Zeta);
-  DShapeFunction[1][1] = -0.125*(1.0+Xi)*(1.0-Zeta);
-  DShapeFunction[2][1] = 0.125*(1.0+Xi)*(1.0-Zeta);
-  DShapeFunction[3][1] = 0.125*(1.0-Xi)*(1.0-Zeta);
-  DShapeFunction[4][1] = -0.125*(1.0-Xi)*(1.0+Zeta);
-  DShapeFunction[5][1] = -0.125*(1.0+Xi)*(1.0+Zeta);
-  DShapeFunction[6][1] = 0.125*(1.0+Xi)*(1.0+Zeta);
-  DShapeFunction[7][1] = 0.125*(1.0-Xi)*(1.0+Zeta);
+  DShapeFunction[0][1] = -0.125 * (1.0 - Xi) * (1.0 - Zeta);
+  DShapeFunction[1][1] = -0.125 * (1.0 + Xi) * (1.0 - Zeta);
+  DShapeFunction[2][1] = 0.125 * (1.0 + Xi) * (1.0 - Zeta);
+  DShapeFunction[3][1] = 0.125 * (1.0 - Xi) * (1.0 - Zeta);
+  DShapeFunction[4][1] = -0.125 * (1.0 - Xi) * (1.0 + Zeta);
+  DShapeFunction[5][1] = -0.125 * (1.0 + Xi) * (1.0 + Zeta);
+  DShapeFunction[6][1] = 0.125 * (1.0 + Xi) * (1.0 + Zeta);
+  DShapeFunction[7][1] = 0.125 * (1.0 - Xi) * (1.0 + Zeta);
 
   /*--- dN/d zeta ---*/
 
-  DShapeFunction[0][2] = -0.125*(1.0-Xi)*(1.0-Eta);
-  DShapeFunction[1][2] = -0.125*(1.0+Xi)*(1.0-Eta);
-  DShapeFunction[2][2] = -0.125*(1.0+Xi)*(1.0+Eta);
-  DShapeFunction[3][2] = -0.125*(1.0-Xi)*(1.0+Eta);
-  DShapeFunction[4][2] = 0.125*(1.0-Xi)*(1.0-Eta);
-  DShapeFunction[5][2] = 0.125*(1.0+Xi)*(1.0-Eta);
-  DShapeFunction[6][2] = 0.125*(1.0+Xi)*(1.0+Eta);
-  DShapeFunction[7][2] = 0.125*(1.0-Xi)*(1.0+Eta);
+  DShapeFunction[0][2] = -0.125 * (1.0 - Xi) * (1.0 - Eta);
+  DShapeFunction[1][2] = -0.125 * (1.0 + Xi) * (1.0 - Eta);
+  DShapeFunction[2][2] = -0.125 * (1.0 + Xi) * (1.0 + Eta);
+  DShapeFunction[3][2] = -0.125 * (1.0 - Xi) * (1.0 + Eta);
+  DShapeFunction[4][2] = 0.125 * (1.0 - Xi) * (1.0 - Eta);
+  DShapeFunction[5][2] = 0.125 * (1.0 + Xi) * (1.0 - Eta);
+  DShapeFunction[6][2] = 0.125 * (1.0 + Xi) * (1.0 + Eta);
+  DShapeFunction[7][2] = 0.125 * (1.0 - Xi) * (1.0 + Eta);
 
   /*--- Jacobian transformation ---*/
 
@@ -952,53 +961,51 @@ su2double CVolumetricMovement::ShapeFunc_Hexa(su2double Xi, su2double Eta, su2do
     for (j = 0; j < 3; j++) {
       xs[i][j] = 0.0;
       for (k = 0; k < 8; k++) {
-        xs[i][j] = xs[i][j]+CoordCorners[k][j]*DShapeFunction[k][i];
+        xs[i][j] = xs[i][j] + CoordCorners[k][j] * DShapeFunction[k][i];
       }
     }
   }
 
   /*--- Adjoint to Jacobian ---*/
 
-  ad[0][0] = xs[1][1]*xs[2][2]-xs[1][2]*xs[2][1];
-  ad[0][1] = xs[0][2]*xs[2][1]-xs[0][1]*xs[2][2];
-  ad[0][2] = xs[0][1]*xs[1][2]-xs[0][2]*xs[1][1];
-  ad[1][0] = xs[1][2]*xs[2][0]-xs[1][0]*xs[2][2];
-  ad[1][1] = xs[0][0]*xs[2][2]-xs[0][2]*xs[2][0];
-  ad[1][2] = xs[0][2]*xs[1][0]-xs[0][0]*xs[1][2];
-  ad[2][0] = xs[1][0]*xs[2][1]-xs[1][1]*xs[2][0];
-  ad[2][1] = xs[0][1]*xs[2][0]-xs[0][0]*xs[2][1];
-  ad[2][2] = xs[0][0]*xs[1][1]-xs[0][1]*xs[1][0];
+  ad[0][0] = xs[1][1] * xs[2][2] - xs[1][2] * xs[2][1];
+  ad[0][1] = xs[0][2] * xs[2][1] - xs[0][1] * xs[2][2];
+  ad[0][2] = xs[0][1] * xs[1][2] - xs[0][2] * xs[1][1];
+  ad[1][0] = xs[1][2] * xs[2][0] - xs[1][0] * xs[2][2];
+  ad[1][1] = xs[0][0] * xs[2][2] - xs[0][2] * xs[2][0];
+  ad[1][2] = xs[0][2] * xs[1][0] - xs[0][0] * xs[1][2];
+  ad[2][0] = xs[1][0] * xs[2][1] - xs[1][1] * xs[2][0];
+  ad[2][1] = xs[0][1] * xs[2][0] - xs[0][0] * xs[2][1];
+  ad[2][2] = xs[0][0] * xs[1][1] - xs[0][1] * xs[1][0];
 
   /*--- Determinant of Jacobian ---*/
 
-  xsj = xs[0][0]*ad[0][0]+xs[0][1]*ad[1][0]+xs[0][2]*ad[2][0];
+  xsj = xs[0][0] * ad[0][0] + xs[0][1] * ad[1][0] + xs[0][2] * ad[2][0];
 
   /*--- Jacobian inverse ---*/
   for (i = 0; i < 3; i++) {
     for (j = 0; j < 3; j++) {
-      xs[i][j] = ad[i][j]/xsj;
+      xs[i][j] = ad[i][j] / xsj;
     }
   }
 
   /*--- Derivatives with repect to global coordinates ---*/
 
   for (k = 0; k < 8; k++) {
-    c0 = xs[0][0]*DShapeFunction[k][0]+xs[0][1]*DShapeFunction[k][1]+xs[0][2]*DShapeFunction[k][2]; // dN/dx
-    c1 = xs[1][0]*DShapeFunction[k][0]+xs[1][1]*DShapeFunction[k][1]+xs[1][2]*DShapeFunction[k][2]; // dN/dy
-    c2 = xs[2][0]*DShapeFunction[k][0]+xs[2][1]*DShapeFunction[k][1]+xs[2][2]*DShapeFunction[k][2]; // dN/dz
-    DShapeFunction[k][0] = c0; // store dN/dx instead of dN/d xi
-    DShapeFunction[k][1] = c1; // store dN/dy instead of dN/d eta
-    DShapeFunction[k][2] = c2; // store dN/dz instead of dN/d zeta
+    c0 = xs[0][0] * DShapeFunction[k][0] + xs[0][1] * DShapeFunction[k][1] + xs[0][2] * DShapeFunction[k][2];  // dN/dx
+    c1 = xs[1][0] * DShapeFunction[k][0] + xs[1][1] * DShapeFunction[k][1] + xs[1][2] * DShapeFunction[k][2];  // dN/dy
+    c2 = xs[2][0] * DShapeFunction[k][0] + xs[2][1] * DShapeFunction[k][1] + xs[2][2] * DShapeFunction[k][2];  // dN/dz
+    DShapeFunction[k][0] = c0;  // store dN/dx instead of dN/d xi
+    DShapeFunction[k][1] = c1;  // store dN/dy instead of dN/d eta
+    DShapeFunction[k][2] = c2;  // store dN/dz instead of dN/d zeta
   }
 
   return xsj;
-
 }
 
 su2double CVolumetricMovement::GetTriangle_Area(su2double CoordCorners[8][3]) const {
-
   unsigned short iDim;
-  su2double a[3] = {0.0,0.0,0.0}, b[3] = {0.0,0.0,0.0};
+  su2double a[3] = {0.0, 0.0, 0.0}, b[3] = {0.0, 0.0, 0.0};
   su2double *Coord_0, *Coord_1, *Coord_2, Area;
 
   Coord_0 = CoordCorners[0];
@@ -1006,20 +1013,18 @@ su2double CVolumetricMovement::GetTriangle_Area(su2double CoordCorners[8][3]) co
   Coord_2 = CoordCorners[2];
 
   for (iDim = 0; iDim < nDim; iDim++) {
-    a[iDim] = Coord_0[iDim]-Coord_2[iDim];
-    b[iDim] = Coord_1[iDim]-Coord_2[iDim];
+    a[iDim] = Coord_0[iDim] - Coord_2[iDim];
+    b[iDim] = Coord_1[iDim] - Coord_2[iDim];
   }
 
-  Area = 0.5*fabs(a[0]*b[1]-a[1]*b[0]);
+  Area = 0.5 * fabs(a[0] * b[1] - a[1] * b[0]);
 
   return Area;
-
 }
 
 su2double CVolumetricMovement::GetQuadrilateral_Area(su2double CoordCorners[8][3]) const {
-
   unsigned short iDim;
-  su2double a[3] = {0.0,0.0,0.0}, b[3] = {0.0,0.0,0.0};
+  su2double a[3] = {0.0, 0.0, 0.0}, b[3] = {0.0, 0.0, 0.0};
   su2double *Coord_0, *Coord_1, *Coord_2, Area;
 
   Coord_0 = CoordCorners[0];
@@ -1027,32 +1032,31 @@ su2double CVolumetricMovement::GetQuadrilateral_Area(su2double CoordCorners[8][3
   Coord_2 = CoordCorners[2];
 
   for (iDim = 0; iDim < nDim; iDim++) {
-    a[iDim] = Coord_0[iDim]-Coord_2[iDim];
-    b[iDim] = Coord_1[iDim]-Coord_2[iDim];
+    a[iDim] = Coord_0[iDim] - Coord_2[iDim];
+    b[iDim] = Coord_1[iDim] - Coord_2[iDim];
   }
 
-  Area = 0.5*fabs(a[0]*b[1]-a[1]*b[0]);
+  Area = 0.5 * fabs(a[0] * b[1] - a[1] * b[0]);
 
   Coord_0 = CoordCorners[0];
   Coord_1 = CoordCorners[2];
   Coord_2 = CoordCorners[3];
 
   for (iDim = 0; iDim < nDim; iDim++) {
-    a[iDim] = Coord_0[iDim]-Coord_2[iDim];
-    b[iDim] = Coord_1[iDim]-Coord_2[iDim];
+    a[iDim] = Coord_0[iDim] - Coord_2[iDim];
+    b[iDim] = Coord_1[iDim] - Coord_2[iDim];
   }
 
-  Area += 0.5*fabs(a[0]*b[1]-a[1]*b[0]);
+  Area += 0.5 * fabs(a[0] * b[1] - a[1] * b[0]);
 
   return Area;
-
 }
 
 su2double CVolumetricMovement::GetTetra_Volume(su2double CoordCorners[8][3]) const {
-
   unsigned short iDim;
   su2double *Coord_0, *Coord_1, *Coord_2, *Coord_3;
-  su2double r1[3] = {0.0,0.0,0.0}, r2[3] = {0.0,0.0,0.0}, r3[3] = {0.0,0.0,0.0}, CrossProduct[3] = {0.0,0.0,0.0}, Volume;
+  su2double r1[3] = {0.0, 0.0, 0.0}, r2[3] = {0.0, 0.0, 0.0}, r3[3] = {0.0, 0.0, 0.0},
+            CrossProduct[3] = {0.0, 0.0, 0.0}, Volume;
 
   Coord_0 = CoordCorners[0];
   Coord_1 = CoordCorners[1];
@@ -1065,21 +1069,20 @@ su2double CVolumetricMovement::GetTetra_Volume(su2double CoordCorners[8][3]) con
     r3[iDim] = Coord_3[iDim] - Coord_0[iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume = fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume = fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   return Volume;
-
 }
 
 su2double CVolumetricMovement::GetPyram_Volume(su2double CoordCorners[8][3]) const {
-
   unsigned short iDim;
   su2double *Coord_0, *Coord_1, *Coord_2, *Coord_3;
-  su2double r1[3] = {0.0,0.0,0.0}, r2[3] = {0.0,0.0,0.0}, r3[3] = {0.0,0.0,0.0}, CrossProduct[3] = {0.0,0.0,0.0}, Volume;
+  su2double r1[3] = {0.0, 0.0, 0.0}, r2[3] = {0.0, 0.0, 0.0}, r3[3] = {0.0, 0.0, 0.0},
+            CrossProduct[3] = {0.0, 0.0, 0.0}, Volume;
 
   Coord_0 = CoordCorners[0];
   Coord_1 = CoordCorners[1];
@@ -1092,11 +1095,11 @@ su2double CVolumetricMovement::GetPyram_Volume(su2double CoordCorners[8][3]) con
     r3[iDim] = Coord_3[iDim] - Coord_0[iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume = fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume = fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   Coord_0 = CoordCorners[0];
   Coord_1 = CoordCorners[2];
@@ -1109,21 +1112,20 @@ su2double CVolumetricMovement::GetPyram_Volume(su2double CoordCorners[8][3]) con
     r3[iDim] = Coord_3[iDim] - Coord_0[iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   return Volume;
-
 }
 
 su2double CVolumetricMovement::GetPrism_Volume(su2double CoordCorners[8][3]) const {
-
   unsigned short iDim;
   su2double *Coord_0, *Coord_1, *Coord_2, *Coord_3;
-  su2double r1[3] = {0.0,0.0,0.0}, r2[3] = {0.0,0.0,0.0}, r3[3] = {0.0,0.0,0.0}, CrossProduct[3] = {0.0,0.0,0.0}, Volume;
+  su2double r1[3] = {0.0, 0.0, 0.0}, r2[3] = {0.0, 0.0, 0.0}, r3[3] = {0.0, 0.0, 0.0},
+            CrossProduct[3] = {0.0, 0.0, 0.0}, Volume;
 
   Coord_0 = CoordCorners[0];
   Coord_1 = CoordCorners[2];
@@ -1136,11 +1138,11 @@ su2double CVolumetricMovement::GetPrism_Volume(su2double CoordCorners[8][3]) con
     r3[iDim] = Coord_3[iDim] - Coord_0[iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume = fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume = fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   Coord_0 = CoordCorners[0];
   Coord_1 = CoordCorners[5];
@@ -1153,11 +1155,11 @@ su2double CVolumetricMovement::GetPrism_Volume(su2double CoordCorners[8][3]) con
     r3[iDim] = Coord_3[iDim] - Coord_0[iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   Coord_0 = CoordCorners[0];
   Coord_1 = CoordCorners[5];
@@ -1170,21 +1172,20 @@ su2double CVolumetricMovement::GetPrism_Volume(su2double CoordCorners[8][3]) con
     r3[iDim] = Coord_3[iDim] - Coord_0[iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   return Volume;
-
 }
 
 su2double CVolumetricMovement::GetHexa_Volume(su2double CoordCorners[8][3]) const {
-
   unsigned short iDim;
   su2double *Coord_0, *Coord_1, *Coord_2, *Coord_3;
-  su2double r1[3] = {0.0,0.0,0.0}, r2[3] = {0.0,0.0,0.0}, r3[3] = {0.0,0.0,0.0}, CrossProduct[3] = {0.0,0.0,0.0}, Volume;
+  su2double r1[3] = {0.0, 0.0, 0.0}, r2[3] = {0.0, 0.0, 0.0}, r3[3] = {0.0, 0.0, 0.0},
+            CrossProduct[3] = {0.0, 0.0, 0.0}, Volume;
 
   Coord_0 = CoordCorners[0];
   Coord_1 = CoordCorners[1];
@@ -1197,11 +1198,11 @@ su2double CVolumetricMovement::GetHexa_Volume(su2double CoordCorners[8][3]) cons
     r3[iDim] = Coord_3[iDim] - Coord_0[iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume = fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume = fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   Coord_0 = CoordCorners[0];
   Coord_1 = CoordCorners[2];
@@ -1214,11 +1215,11 @@ su2double CVolumetricMovement::GetHexa_Volume(su2double CoordCorners[8][3]) cons
     r3[iDim] = Coord_3[iDim] - Coord_0[iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   Coord_0 = CoordCorners[0];
   Coord_1 = CoordCorners[2];
@@ -1231,11 +1232,11 @@ su2double CVolumetricMovement::GetHexa_Volume(su2double CoordCorners[8][3]) cons
     r3[iDim] = Coord_3[iDim] - Coord_0[iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   Coord_0 = CoordCorners[0];
   Coord_1 = CoordCorners[5];
@@ -1248,11 +1249,11 @@ su2double CVolumetricMovement::GetHexa_Volume(su2double CoordCorners[8][3]) cons
     r3[iDim] = Coord_3[iDim] - Coord_0[iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   Coord_0 = CoordCorners[2];
   Coord_1 = CoordCorners[7];
@@ -1265,29 +1266,29 @@ su2double CVolumetricMovement::GetHexa_Volume(su2double CoordCorners[8][3]) cons
     r3[iDim] = Coord_3[iDim] - Coord_0[iDim];
   }
 
-  CrossProduct[0] = (r1[1]*r2[2] - r1[2]*r2[1])*r3[0];
-  CrossProduct[1] = (r1[2]*r2[0] - r1[0]*r2[2])*r3[1];
-  CrossProduct[2] = (r1[0]*r2[1] - r1[1]*r2[0])*r3[2];
+  CrossProduct[0] = (r1[1] * r2[2] - r1[2] * r2[1]) * r3[0];
+  CrossProduct[1] = (r1[2] * r2[0] - r1[0] * r2[2]) * r3[1];
+  CrossProduct[2] = (r1[0] * r2[1] - r1[1] * r2[0]) * r3[2];
 
-  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2])/6.0;
+  Volume += fabs(CrossProduct[0] + CrossProduct[1] + CrossProduct[2]) / 6.0;
 
   return Volume;
-
 }
 
-void CVolumetricMovement::SetFEA_StiffMatrix2D(CGeometry *geometry, CConfig *config, su2double **StiffMatrix_Elem, unsigned long PointCorners[8], su2double CoordCorners[8][3],
+void CVolumetricMovement::SetFEA_StiffMatrix2D(CGeometry* geometry, CConfig* config, su2double** StiffMatrix_Elem,
+                                               unsigned long PointCorners[8], su2double CoordCorners[8][3],
                                                unsigned short nNodes, su2double ElemVolume, su2double ElemDistance) {
-
   su2double B_Matrix[3][8], D_Matrix[3][3], Aux_Matrix[8][3];
-  su2double Xi = 0.0, Eta = 0.0, Det = 0.0, E = 1/EPS, Lambda = 0.0, Mu = 0.0, Nu = 0.0;
+  su2double Xi = 0.0, Eta = 0.0, Det = 0.0, E = 1 / EPS, Lambda = 0.0, Mu = 0.0, Nu = 0.0;
   unsigned short iNode, iVar, jVar, kVar, iGauss, nGauss = 0;
-  su2double DShapeFunction[8][4] = {{0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0},
-    {0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0}};
+  su2double DShapeFunction[8][4] = {{0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0},
+                                    {0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0},
+                                    {0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0}};
   su2double Location[4][3], Weight[4];
   unsigned short nVar = geometry->GetnDim();
 
-  for (iVar = 0; iVar < nNodes*nVar; iVar++) {
-    for (jVar = 0; jVar < nNodes*nVar; jVar++) {
+  for (iVar = 0; iVar < nNodes * nVar; iVar++) {
+    for (jVar = 0; jVar < nNodes * nVar; jVar++) {
       StiffMatrix_Elem[iVar][jVar] = 0.0;
     }
   }
@@ -1299,22 +1300,32 @@ void CVolumetricMovement::SetFEA_StiffMatrix2D(CGeometry *geometry, CConfig *con
 
   if (nNodes == 3) {
     nGauss = 1;
-    Location[0][0] = 0.333333333333333;  Location[0][1] = 0.333333333333333;  Weight[0] = 0.5;
+    Location[0][0] = 0.333333333333333;
+    Location[0][1] = 0.333333333333333;
+    Weight[0] = 0.5;
   }
 
   /*--- Quadrilateral. Nodes of numerical integration at 4 points (order 2). ---*/
 
   if (nNodes == 4) {
     nGauss = 4;
-    Location[0][0] = -0.577350269189626;  Location[0][1] = -0.577350269189626;  Weight[0] = 1.0;
-    Location[1][0] = 0.577350269189626;   Location[1][1] = -0.577350269189626;  Weight[1] = 1.0;
-    Location[2][0] = 0.577350269189626;   Location[2][1] = 0.577350269189626;   Weight[2] = 1.0;
-    Location[3][0] = -0.577350269189626;  Location[3][1] = 0.577350269189626;   Weight[3] = 1.0;
+    Location[0][0] = -0.577350269189626;
+    Location[0][1] = -0.577350269189626;
+    Weight[0] = 1.0;
+    Location[1][0] = 0.577350269189626;
+    Location[1][1] = -0.577350269189626;
+    Weight[1] = 1.0;
+    Location[2][0] = 0.577350269189626;
+    Location[2][1] = 0.577350269189626;
+    Weight[2] = 1.0;
+    Location[3][0] = -0.577350269189626;
+    Location[3][1] = 0.577350269189626;
+    Weight[3] = 1.0;
   }
 
   for (iGauss = 0; iGauss < nGauss; iGauss++) {
-
-    Xi = Location[iGauss][0]; Eta = Location[iGauss][1];
+    Xi = Location[iGauss][0];
+    Eta = Location[iGauss][1];
 
     if (nNodes == 3) Det = ShapeFunc_Triangle(Xi, Eta, CoordCorners, DShapeFunction);
     if (nNodes == 4) Det = ShapeFunc_Quadrilateral(Xi, Eta, CoordCorners, DShapeFunction);
@@ -1322,75 +1333,85 @@ void CVolumetricMovement::SetFEA_StiffMatrix2D(CGeometry *geometry, CConfig *con
     /*--- Compute the B Matrix ---*/
 
     for (iVar = 0; iVar < 3; iVar++)
-      for (jVar = 0; jVar < nNodes*nVar; jVar++)
-        B_Matrix[iVar][jVar] = 0.0;
+      for (jVar = 0; jVar < nNodes * nVar; jVar++) B_Matrix[iVar][jVar] = 0.0;
 
     for (iNode = 0; iNode < nNodes; iNode++) {
-      B_Matrix[0][0+iNode*nVar] = DShapeFunction[iNode][0];
-      B_Matrix[1][1+iNode*nVar] = DShapeFunction[iNode][1];
+      B_Matrix[0][0 + iNode * nVar] = DShapeFunction[iNode][0];
+      B_Matrix[1][1 + iNode * nVar] = DShapeFunction[iNode][1];
 
-      B_Matrix[2][0+iNode*nVar] = DShapeFunction[iNode][1];
-      B_Matrix[2][1+iNode*nVar] = DShapeFunction[iNode][0];
+      B_Matrix[2][0 + iNode * nVar] = DShapeFunction[iNode][1];
+      B_Matrix[2][1 + iNode * nVar] = DShapeFunction[iNode][0];
     }
 
     /*--- Impose a type of stiffness for each element ---*/
 
     switch (config->GetDeform_Stiffness_Type()) {
-      case INVERSE_VOLUME: E = 1.0 / ElemVolume; break;
-      case SOLID_WALL_DISTANCE: E = 1.0 / ElemDistance; break;
-      case CONSTANT_STIFFNESS: E = 1.0 / EPS; break;
+      case INVERSE_VOLUME:
+        E = 1.0 / ElemVolume;
+        break;
+      case SOLID_WALL_DISTANCE:
+        E = 1.0 / ElemDistance;
+        break;
+      case CONSTANT_STIFFNESS:
+        E = 1.0 / EPS;
+        break;
     }
 
     Nu = config->GetDeform_Coeff();
-    Mu = E / (2.0*(1.0 + Nu));
-    Lambda = Nu*E/((1.0+Nu)*(1.0-2.0*Nu));
+    Mu = E / (2.0 * (1.0 + Nu));
+    Lambda = Nu * E / ((1.0 + Nu) * (1.0 - 2.0 * Nu));
 
     /*--- Compute the D Matrix (for plane strain and 3-D)---*/
 
-    D_Matrix[0][0] = Lambda + 2.0*Mu;    D_Matrix[0][1] = Lambda;            D_Matrix[0][2] = 0.0;
-    D_Matrix[1][0] = Lambda;            D_Matrix[1][1] = Lambda + 2.0*Mu;   D_Matrix[1][2] = 0.0;
-    D_Matrix[2][0] = 0.0;               D_Matrix[2][1] = 0.0;               D_Matrix[2][2] = Mu;
-
+    D_Matrix[0][0] = Lambda + 2.0 * Mu;
+    D_Matrix[0][1] = Lambda;
+    D_Matrix[0][2] = 0.0;
+    D_Matrix[1][0] = Lambda;
+    D_Matrix[1][1] = Lambda + 2.0 * Mu;
+    D_Matrix[1][2] = 0.0;
+    D_Matrix[2][0] = 0.0;
+    D_Matrix[2][1] = 0.0;
+    D_Matrix[2][2] = Mu;
 
     /*--- Compute the BT.D Matrix ---*/
 
-    for (iVar = 0; iVar < nNodes*nVar; iVar++) {
+    for (iVar = 0; iVar < nNodes * nVar; iVar++) {
       for (jVar = 0; jVar < 3; jVar++) {
         Aux_Matrix[iVar][jVar] = 0.0;
-        for (kVar = 0; kVar < 3; kVar++)
-          Aux_Matrix[iVar][jVar] += B_Matrix[kVar][iVar]*D_Matrix[kVar][jVar];
+        for (kVar = 0; kVar < 3; kVar++) Aux_Matrix[iVar][jVar] += B_Matrix[kVar][iVar] * D_Matrix[kVar][jVar];
       }
     }
 
     /*--- Compute the BT.D.B Matrix (stiffness matrix), and add to the original
      matrix using Gauss integration ---*/
 
-    for (iVar = 0; iVar < nNodes*nVar; iVar++) {
-      for (jVar = 0; jVar < nNodes*nVar; jVar++) {
+    for (iVar = 0; iVar < nNodes * nVar; iVar++) {
+      for (jVar = 0; jVar < nNodes * nVar; jVar++) {
         for (kVar = 0; kVar < 3; kVar++) {
-          StiffMatrix_Elem[iVar][jVar] += Weight[iGauss] * Aux_Matrix[iVar][kVar]*B_Matrix[kVar][jVar] * fabs(Det);
+          StiffMatrix_Elem[iVar][jVar] += Weight[iGauss] * Aux_Matrix[iVar][kVar] * B_Matrix[kVar][jVar] * fabs(Det);
         }
       }
     }
-
   }
-
 }
 
-void CVolumetricMovement::SetFEA_StiffMatrix3D(CGeometry *geometry, CConfig *config, su2double **StiffMatrix_Elem, unsigned long PointCorners[8], su2double CoordCorners[8][3],
+void CVolumetricMovement::SetFEA_StiffMatrix3D(CGeometry* geometry, CConfig* config, su2double** StiffMatrix_Elem,
+                                               unsigned long PointCorners[8], su2double CoordCorners[8][3],
                                                unsigned short nNodes, su2double ElemVolume, su2double ElemDistance) {
-
-  su2double B_Matrix[6][24], D_Matrix[6][6] = {{0.0, 0.0, 0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0, 0.0, 0.0},
-    {0.0, 0.0, 0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0, 0.0, 0.0}}, Aux_Matrix[24][6];
+  su2double B_Matrix[6][24],
+      D_Matrix[6][6] = {{0.0, 0.0, 0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0, 0.0, 0.0},
+                        {0.0, 0.0, 0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0, 0.0, 0.0}},
+      Aux_Matrix[24][6];
   su2double Xi = 0.0, Eta = 0.0, Zeta = 0.0, Det = 0.0, Mu = 0.0, E = 0.0, Lambda = 0.0, Nu = 0.0;
   unsigned short iNode, iVar, jVar, kVar, iGauss, nGauss = 0;
-  su2double DShapeFunction[8][4] = {{0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0},
-    {0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0}};
+  su2double DShapeFunction[8][4] = {{0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0},
+                                    {0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0},
+                                    {0.0, 0.0, 0.0, 0.0}, {0.0, 0.0, 0.0, 0.0}};
   su2double Location[8][3], Weight[8];
   unsigned short nVar = geometry->GetnDim();
 
-  for (iVar = 0; iVar < nNodes*nVar; iVar++) {
-    for (jVar = 0; jVar < nNodes*nVar; jVar++) {
+  for (iVar = 0; iVar < nNodes * nVar; iVar++) {
+    for (jVar = 0; jVar < nNodes * nVar; jVar++) {
       StiffMatrix_Elem[iVar][jVar] = 0.0;
     }
   }
@@ -1402,49 +1423,110 @@ void CVolumetricMovement::SetFEA_StiffMatrix3D(CGeometry *geometry, CConfig *con
 
   if (nNodes == 4) {
     nGauss = 1;
-    Location[0][0] = 0.25;  Location[0][1] = 0.25;  Location[0][2] = 0.25;  Weight[0] = 0.166666666666666;
+    Location[0][0] = 0.25;
+    Location[0][1] = 0.25;
+    Location[0][2] = 0.25;
+    Weight[0] = 0.166666666666666;
   }
 
   /*--- Pyramids. Nodes numerical integration at 5 points. ---*/
 
   if (nNodes == 5) {
     nGauss = 5;
-    Location[0][0] = 0.5;   Location[0][1] = 0.0;   Location[0][2] = 0.1531754163448146;  Weight[0] = 0.133333333333333;
-    Location[1][0] = 0.0;   Location[1][1] = 0.5;   Location[1][2] = 0.1531754163448146;  Weight[1] = 0.133333333333333;
-    Location[2][0] = -0.5;  Location[2][1] = 0.0;   Location[2][2] = 0.1531754163448146;  Weight[2] = 0.133333333333333;
-    Location[3][0] = 0.0;   Location[3][1] = -0.5;  Location[3][2] = 0.1531754163448146;  Weight[3] = 0.133333333333333;
-    Location[4][0] = 0.0;   Location[4][1] = 0.0;   Location[4][2] = 0.6372983346207416;  Weight[4] = 0.133333333333333;
+    Location[0][0] = 0.5;
+    Location[0][1] = 0.0;
+    Location[0][2] = 0.1531754163448146;
+    Weight[0] = 0.133333333333333;
+    Location[1][0] = 0.0;
+    Location[1][1] = 0.5;
+    Location[1][2] = 0.1531754163448146;
+    Weight[1] = 0.133333333333333;
+    Location[2][0] = -0.5;
+    Location[2][1] = 0.0;
+    Location[2][2] = 0.1531754163448146;
+    Weight[2] = 0.133333333333333;
+    Location[3][0] = 0.0;
+    Location[3][1] = -0.5;
+    Location[3][2] = 0.1531754163448146;
+    Weight[3] = 0.133333333333333;
+    Location[4][0] = 0.0;
+    Location[4][1] = 0.0;
+    Location[4][2] = 0.6372983346207416;
+    Weight[4] = 0.133333333333333;
   }
 
   /*--- Prism. Nodes of numerical integration at 6 points (order 3 in Xi, order 2 in Eta and Mu ). ---*/
 
   if (nNodes == 6) {
     nGauss = 6;
-    Location[0][0] = -0.577350269189626;  Location[0][1] = 0.166666666666667;  Location[0][2] = 0.166666666666667;  Weight[0] = 0.166666666666667;
-    Location[1][0] = -0.577350269189626;  Location[1][1] = 0.666666666666667;  Location[1][2] = 0.166666666666667;  Weight[1] = 0.166666666666667;
-    Location[2][0] = -0.577350269189626;  Location[2][1] = 0.166666666666667;  Location[2][2] = 0.666666666666667;  Weight[2] = 0.166666666666667;
-    Location[3][0] =  0.577350269189626;  Location[3][1] = 0.166666666666667;  Location[3][2] = 0.166666666666667;  Weight[3] = 0.166666666666667;
-    Location[4][0] =  0.577350269189626;  Location[4][1] = 0.666666666666667;  Location[4][2] = 0.166666666666667;  Weight[4] = 0.166666666666667;
-    Location[5][0] =  0.577350269189626;  Location[5][1] = 0.166666666666667;  Location[5][2] = 0.666666666666667;  Weight[5] = 0.166666666666667;
+    Location[0][0] = -0.577350269189626;
+    Location[0][1] = 0.166666666666667;
+    Location[0][2] = 0.166666666666667;
+    Weight[0] = 0.166666666666667;
+    Location[1][0] = -0.577350269189626;
+    Location[1][1] = 0.666666666666667;
+    Location[1][2] = 0.166666666666667;
+    Weight[1] = 0.166666666666667;
+    Location[2][0] = -0.577350269189626;
+    Location[2][1] = 0.166666666666667;
+    Location[2][2] = 0.666666666666667;
+    Weight[2] = 0.166666666666667;
+    Location[3][0] = 0.577350269189626;
+    Location[3][1] = 0.166666666666667;
+    Location[3][2] = 0.166666666666667;
+    Weight[3] = 0.166666666666667;
+    Location[4][0] = 0.577350269189626;
+    Location[4][1] = 0.666666666666667;
+    Location[4][2] = 0.166666666666667;
+    Weight[4] = 0.166666666666667;
+    Location[5][0] = 0.577350269189626;
+    Location[5][1] = 0.166666666666667;
+    Location[5][2] = 0.666666666666667;
+    Weight[5] = 0.166666666666667;
   }
 
   /*--- Hexahedrons. Nodes of numerical integration at 6 points (order 3). ---*/
 
   if (nNodes == 8) {
     nGauss = 8;
-    Location[0][0] = -0.577350269189626;  Location[0][1] = -0.577350269189626;  Location[0][2] = -0.577350269189626;  Weight[0] = 1.0;
-    Location[1][0] = -0.577350269189626;  Location[1][1] = -0.577350269189626;  Location[1][2] = 0.577350269189626;   Weight[1] = 1.0;
-    Location[2][0] = -0.577350269189626;  Location[2][1] = 0.577350269189626;   Location[2][2] = -0.577350269189626;  Weight[2] = 1.0;
-    Location[3][0] = -0.577350269189626;  Location[3][1] = 0.577350269189626;   Location[3][2] = 0.577350269189626;   Weight[3] = 1.0;
-    Location[4][0] = 0.577350269189626;   Location[4][1] = -0.577350269189626;  Location[4][2] = -0.577350269189626;  Weight[4] = 1.0;
-    Location[5][0] = 0.577350269189626;   Location[5][1] = -0.577350269189626;  Location[5][2] = 0.577350269189626;   Weight[5] = 1.0;
-    Location[6][0] = 0.577350269189626;   Location[6][1] = 0.577350269189626;   Location[6][2] = -0.577350269189626;  Weight[6] = 1.0;
-    Location[7][0] = 0.577350269189626;   Location[7][1] = 0.577350269189626;   Location[7][2] = 0.577350269189626;   Weight[7] = 1.0;
+    Location[0][0] = -0.577350269189626;
+    Location[0][1] = -0.577350269189626;
+    Location[0][2] = -0.577350269189626;
+    Weight[0] = 1.0;
+    Location[1][0] = -0.577350269189626;
+    Location[1][1] = -0.577350269189626;
+    Location[1][2] = 0.577350269189626;
+    Weight[1] = 1.0;
+    Location[2][0] = -0.577350269189626;
+    Location[2][1] = 0.577350269189626;
+    Location[2][2] = -0.577350269189626;
+    Weight[2] = 1.0;
+    Location[3][0] = -0.577350269189626;
+    Location[3][1] = 0.577350269189626;
+    Location[3][2] = 0.577350269189626;
+    Weight[3] = 1.0;
+    Location[4][0] = 0.577350269189626;
+    Location[4][1] = -0.577350269189626;
+    Location[4][2] = -0.577350269189626;
+    Weight[4] = 1.0;
+    Location[5][0] = 0.577350269189626;
+    Location[5][1] = -0.577350269189626;
+    Location[5][2] = 0.577350269189626;
+    Weight[5] = 1.0;
+    Location[6][0] = 0.577350269189626;
+    Location[6][1] = 0.577350269189626;
+    Location[6][2] = -0.577350269189626;
+    Weight[6] = 1.0;
+    Location[7][0] = 0.577350269189626;
+    Location[7][1] = 0.577350269189626;
+    Location[7][2] = 0.577350269189626;
+    Weight[7] = 1.0;
   }
 
   for (iGauss = 0; iGauss < nGauss; iGauss++) {
-
-    Xi = Location[iGauss][0]; Eta = Location[iGauss][1];  Zeta = Location[iGauss][2];
+    Xi = Location[iGauss][0];
+    Eta = Location[iGauss][1];
+    Zeta = Location[iGauss][2];
 
     if (nNodes == 4) Det = ShapeFunc_Tetra(Xi, Eta, Zeta, CoordCorners, DShapeFunction);
     if (nNodes == 5) Det = ShapeFunc_Pyram(Xi, Eta, Zeta, CoordCorners, DShapeFunction);
@@ -1454,116 +1536,116 @@ void CVolumetricMovement::SetFEA_StiffMatrix3D(CGeometry *geometry, CConfig *con
     /*--- Compute the B Matrix ---*/
 
     for (iVar = 0; iVar < 6; iVar++)
-      for (jVar = 0; jVar < nNodes*nVar; jVar++)
-        B_Matrix[iVar][jVar] = 0.0;
+      for (jVar = 0; jVar < nNodes * nVar; jVar++) B_Matrix[iVar][jVar] = 0.0;
 
     for (iNode = 0; iNode < nNodes; iNode++) {
-      B_Matrix[0][0+iNode*nVar] = DShapeFunction[iNode][0];
-      B_Matrix[1][1+iNode*nVar] = DShapeFunction[iNode][1];
-      B_Matrix[2][2+iNode*nVar] = DShapeFunction[iNode][2];
+      B_Matrix[0][0 + iNode * nVar] = DShapeFunction[iNode][0];
+      B_Matrix[1][1 + iNode * nVar] = DShapeFunction[iNode][1];
+      B_Matrix[2][2 + iNode * nVar] = DShapeFunction[iNode][2];
 
-      B_Matrix[3][0+iNode*nVar] = DShapeFunction[iNode][1];
-      B_Matrix[3][1+iNode*nVar] = DShapeFunction[iNode][0];
+      B_Matrix[3][0 + iNode * nVar] = DShapeFunction[iNode][1];
+      B_Matrix[3][1 + iNode * nVar] = DShapeFunction[iNode][0];
 
-      B_Matrix[4][1+iNode*nVar] = DShapeFunction[iNode][2];
-      B_Matrix[4][2+iNode*nVar] = DShapeFunction[iNode][1];
+      B_Matrix[4][1 + iNode * nVar] = DShapeFunction[iNode][2];
+      B_Matrix[4][2 + iNode * nVar] = DShapeFunction[iNode][1];
 
-      B_Matrix[5][0+iNode*nVar] = DShapeFunction[iNode][2];
-      B_Matrix[5][2+iNode*nVar] = DShapeFunction[iNode][0];
+      B_Matrix[5][0 + iNode * nVar] = DShapeFunction[iNode][2];
+      B_Matrix[5][2 + iNode * nVar] = DShapeFunction[iNode][0];
     }
 
     /*--- Impose a type of stiffness for each element ---*/
 
     switch (config->GetDeform_Stiffness_Type()) {
-      case INVERSE_VOLUME: E = 1.0 / ElemVolume; break;
-      case SOLID_WALL_DISTANCE: E = 1.0 / ElemDistance; break;
-      case CONSTANT_STIFFNESS: E = 1.0 / EPS; break;
+      case INVERSE_VOLUME:
+        E = 1.0 / ElemVolume;
+        break;
+      case SOLID_WALL_DISTANCE:
+        E = 1.0 / ElemDistance;
+        break;
+      case CONSTANT_STIFFNESS:
+        E = 1.0 / EPS;
+        break;
     }
 
     Nu = config->GetDeform_Coeff();
-    Mu = E / (2.0*(1.0 + Nu));
-    Lambda = Nu*E/((1.0+Nu)*(1.0-2.0*Nu));
+    Mu = E / (2.0 * (1.0 + Nu));
+    Lambda = Nu * E / ((1.0 + Nu) * (1.0 - 2.0 * Nu));
 
     /*--- Compute the D Matrix (for plane strain and 3-D)---*/
 
-    D_Matrix[0][0] = Lambda + 2.0*Mu;  D_Matrix[0][1] = Lambda;          D_Matrix[0][2] = Lambda;
-    D_Matrix[1][0] = Lambda;          D_Matrix[1][1] = Lambda + 2.0*Mu;  D_Matrix[1][2] = Lambda;
-    D_Matrix[2][0] = Lambda;          D_Matrix[2][1] = Lambda;          D_Matrix[2][2] = Lambda + 2.0*Mu;
+    D_Matrix[0][0] = Lambda + 2.0 * Mu;
+    D_Matrix[0][1] = Lambda;
+    D_Matrix[0][2] = Lambda;
+    D_Matrix[1][0] = Lambda;
+    D_Matrix[1][1] = Lambda + 2.0 * Mu;
+    D_Matrix[1][2] = Lambda;
+    D_Matrix[2][0] = Lambda;
+    D_Matrix[2][1] = Lambda;
+    D_Matrix[2][2] = Lambda + 2.0 * Mu;
     D_Matrix[3][3] = Mu;
     D_Matrix[4][4] = Mu;
     D_Matrix[5][5] = Mu;
 
-
     /*--- Compute the BT.D Matrix ---*/
 
-    for (iVar = 0; iVar < nNodes*nVar; iVar++) {
+    for (iVar = 0; iVar < nNodes * nVar; iVar++) {
       for (jVar = 0; jVar < 6; jVar++) {
         Aux_Matrix[iVar][jVar] = 0.0;
-        for (kVar = 0; kVar < 6; kVar++)
-          Aux_Matrix[iVar][jVar] += B_Matrix[kVar][iVar]*D_Matrix[kVar][jVar];
+        for (kVar = 0; kVar < 6; kVar++) Aux_Matrix[iVar][jVar] += B_Matrix[kVar][iVar] * D_Matrix[kVar][jVar];
       }
     }
 
     /*--- Compute the BT.D.B Matrix (stiffness matrix), and add to the original
      matrix using Gauss integration ---*/
 
-    for (iVar = 0; iVar < nNodes*nVar; iVar++) {
-      for (jVar = 0; jVar < nNodes*nVar; jVar++) {
+    for (iVar = 0; iVar < nNodes * nVar; iVar++) {
+      for (jVar = 0; jVar < nNodes * nVar; jVar++) {
         for (kVar = 0; kVar < 6; kVar++) {
-          StiffMatrix_Elem[iVar][jVar] += Weight[iGauss] * Aux_Matrix[iVar][kVar]*B_Matrix[kVar][jVar] * fabs(Det);
+          StiffMatrix_Elem[iVar][jVar] += Weight[iGauss] * Aux_Matrix[iVar][kVar] * B_Matrix[kVar][jVar] * fabs(Det);
         }
       }
     }
-
   }
-
 }
 
-void CVolumetricMovement::AddFEA_StiffMatrix(CGeometry *geometry, su2double **StiffMatrix_Elem, unsigned long PointCorners[8], unsigned short nNodes) {
-
+void CVolumetricMovement::AddFEA_StiffMatrix(CGeometry* geometry, su2double** StiffMatrix_Elem,
+                                             unsigned long PointCorners[8], unsigned short nNodes) {
   unsigned short iVar, jVar, iDim, jDim;
 
   unsigned short nVar = geometry->GetnDim();
 
-  su2double **StiffMatrix_Node;
-  StiffMatrix_Node = new su2double* [nVar];
-  for (iVar = 0; iVar < nVar; iVar++)
-    StiffMatrix_Node[iVar] = new su2double [nVar];
+  su2double** StiffMatrix_Node;
+  StiffMatrix_Node = new su2double*[nVar];
+  for (iVar = 0; iVar < nVar; iVar++) StiffMatrix_Node[iVar] = new su2double[nVar];
 
   for (iVar = 0; iVar < nVar; iVar++)
-    for (jVar = 0; jVar < nVar; jVar++)
-      StiffMatrix_Node[iVar][jVar] = 0.0;
+    for (jVar = 0; jVar < nVar; jVar++) StiffMatrix_Node[iVar][jVar] = 0.0;
 
   /*--- Transform the stiffness matrix for the hexahedral element into the
    contributions for the individual nodes relative to each other. ---*/
 
   for (iVar = 0; iVar < nNodes; iVar++) {
     for (jVar = 0; jVar < nNodes; jVar++) {
-
       for (iDim = 0; iDim < nVar; iDim++) {
         for (jDim = 0; jDim < nVar; jDim++) {
-          StiffMatrix_Node[iDim][jDim] = StiffMatrix_Elem[(iVar*nVar)+iDim][(jVar*nVar)+jDim];
+          StiffMatrix_Node[iDim][jDim] = StiffMatrix_Elem[(iVar * nVar) + iDim][(jVar * nVar) + jDim];
         }
       }
 
       StiffMatrix.AddBlock(PointCorners[iVar], PointCorners[jVar], StiffMatrix_Node);
-
     }
   }
 
   /*--- Deallocate memory and exit ---*/
 
-  for (iVar = 0; iVar < nVar; iVar++)
-    delete [] StiffMatrix_Node[iVar];
-  delete [] StiffMatrix_Node;
-
+  for (iVar = 0; iVar < nVar; iVar++) delete[] StiffMatrix_Node[iVar];
+  delete[] StiffMatrix_Node;
 }
 
-void CVolumetricMovement::SetBoundaryDisplacements(CGeometry *geometry, CConfig *config) {
-
+void CVolumetricMovement::SetBoundaryDisplacements(CGeometry* geometry, CConfig* config) {
   unsigned short iDim, nDim = geometry->GetnDim(), iMarker, axis = 0;
   unsigned long iPoint, total_index, iVertex;
-  su2double *VarCoord, MeanCoord[3] = {0.0,0.0,0.0}, VarIncrement = 1.0;
+  su2double *VarCoord, MeanCoord[3] = {0.0, 0.0, 0.0}, VarIncrement = 1.0;
 
   /*--- Get the SU2 module. SU2_CFD will use this routine for dynamically
    deforming meshes (MARKER_MOVING), while SU2_DEF will use it for deforming
@@ -1575,7 +1657,7 @@ void CVolumetricMovement::SetBoundaryDisplacements(CGeometry *geometry, CConfig
    increments and solve the grid deformation equations iteratively with
    successive small deformations. ---*/
 
-  VarIncrement = 1.0/((su2double)config->GetGridDef_Nonlinear_Iter());
+  VarIncrement = 1.0 / ((su2double)config->GetGridDef_Nonlinear_Iter());
 
   /*--- As initialization, set to zero displacements of all the surfaces except the symmetry
    plane (which is treated specially, see below), internal and the send-receive boundaries ---*/
@@ -1587,7 +1669,7 @@ void CVolumetricMovement::SetBoundaryDisplacements(CGeometry *geometry, CConfig
       for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
         iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
         for (iDim = 0; iDim < nDim; iDim++) {
-          total_index = iPoint*nDim + iDim;
+          total_index = iPoint * nDim + iDim;
           LinSysRes[total_index] = 0.0;
           LinSysSol[total_index] = 0.0;
           StiffMatrix.DeleteValsRowi(total_index);
@@ -1602,13 +1684,14 @@ void CVolumetricMovement::SetBoundaryDisplacements(CGeometry *geometry, CConfig
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
     if (((config->GetMarker_All_Moving(iMarker) == YES) && (Kind_SU2 == SU2_COMPONENT::SU2_CFD)) ||
         ((config->GetMarker_All_DV(iMarker) == YES) && (Kind_SU2 == SU2_COMPONENT::SU2_DEF)) ||
-        ((config->GetDirectDiff() == D_DESIGN) && (Kind_SU2 == SU2_COMPONENT::SU2_CFD) && (config->GetMarker_All_DV(iMarker) == YES)) ||
+        ((config->GetDirectDiff() == D_DESIGN) && (Kind_SU2 == SU2_COMPONENT::SU2_CFD) &&
+         (config->GetMarker_All_DV(iMarker) == YES)) ||
         ((config->GetMarker_All_DV(iMarker) == YES) && (Kind_SU2 == SU2_COMPONENT::SU2_DOT))) {
       for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
         iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
         VarCoord = geometry->vertex[iMarker][iVertex]->GetVarCoord();
         for (iDim = 0; iDim < nDim; iDim++) {
-          total_index = iPoint*nDim + iDim;
+          total_index = iPoint * nDim + iDim;
           LinSysRes[total_index] = SU2_TYPE::GetValue(VarCoord[iDim] * VarIncrement);
           LinSysSol[total_index] = SU2_TYPE::GetValue(VarCoord[iDim] * VarIncrement);
           StiffMatrix.DeleteValsRowi(total_index);
@@ -1620,37 +1703,35 @@ void CVolumetricMovement::SetBoundaryDisplacements(CGeometry *geometry, CConfig
   /*--- Set to zero displacements of the normal component for the symmetry plane condition ---*/
 
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-    if ((config->GetMarker_All_KindBC(iMarker) == SYMMETRY_PLANE) ) {
-
-      su2double *Coord_0 = nullptr;
+    if ((config->GetMarker_All_KindBC(iMarker) == SYMMETRY_PLANE)) {
+      su2double* Coord_0 = nullptr;
 
       for (iDim = 0; iDim < nDim; iDim++) MeanCoord[iDim] = 0.0;
 
       /*--- Store the coord of the first point to help identify the axis. ---*/
 
-      iPoint  = geometry->vertex[iMarker][0]->GetNode();
+      iPoint = geometry->vertex[iMarker][0]->GetNode();
       Coord_0 = geometry->nodes->GetCoord(iPoint);
 
       for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
         iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
         VarCoord = geometry->nodes->GetCoord(iPoint);
         for (iDim = 0; iDim < nDim; iDim++)
-          MeanCoord[iDim] += (VarCoord[iDim]-Coord_0[iDim])*(VarCoord[iDim]-Coord_0[iDim]);
+          MeanCoord[iDim] += (VarCoord[iDim] - Coord_0[iDim]) * (VarCoord[iDim] - Coord_0[iDim]);
       }
       for (iDim = 0; iDim < nDim; iDim++) MeanCoord[iDim] = sqrt(MeanCoord[iDim]);
-      if (nDim==3) {
+      if (nDim == 3) {
         if ((MeanCoord[0] <= MeanCoord[1]) && (MeanCoord[0] <= MeanCoord[2])) axis = 0;
         if ((MeanCoord[1] <= MeanCoord[0]) && (MeanCoord[1] <= MeanCoord[2])) axis = 1;
         if ((MeanCoord[2] <= MeanCoord[0]) && (MeanCoord[2] <= MeanCoord[1])) axis = 2;
-      }
-      else {
-        if ((MeanCoord[0] <= MeanCoord[1]) ) axis = 0;
-        if ((MeanCoord[1] <= MeanCoord[0]) ) axis = 1;
+      } else {
+        if ((MeanCoord[0] <= MeanCoord[1])) axis = 0;
+        if ((MeanCoord[1] <= MeanCoord[0])) axis = 1;
       }
 
       for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
         iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
-        total_index = iPoint*nDim + axis;
+        total_index = iPoint * nDim + axis;
         LinSysRes[total_index] = 0.0;
         LinSysSol[total_index] = 0.0;
         StiffMatrix.DeleteValsRowi(total_index);
@@ -1665,7 +1746,7 @@ void CVolumetricMovement::SetBoundaryDisplacements(CGeometry *geometry, CConfig
       for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
         iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
         for (iDim = 0; iDim < nDim; iDim++) {
-          total_index = iPoint*nDim + iDim;
+          total_index = iPoint * nDim + iDim;
           LinSysRes[total_index] = 0.0;
           LinSysSol[total_index] = 0.0;
           StiffMatrix.DeleteValsRowi(total_index);
@@ -1682,7 +1763,7 @@ void CVolumetricMovement::SetBoundaryDisplacements(CGeometry *geometry, CConfig
         iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
         VarCoord = geometry->vertex[iMarker][iVertex]->GetVarCoord();
         for (iDim = 0; iDim < nDim; iDim++) {
-          total_index = iPoint*nDim + iDim;
+          total_index = iPoint * nDim + iDim;
           LinSysRes[total_index] = SU2_TYPE::GetValue(VarCoord[iDim] * VarIncrement);
           LinSysSol[total_index] = SU2_TYPE::GetValue(VarCoord[iDim] * VarIncrement);
           StiffMatrix.DeleteValsRowi(total_index);
@@ -1690,14 +1771,14 @@ void CVolumetricMovement::SetBoundaryDisplacements(CGeometry *geometry, CConfig
       }
     }
   }
-
 }
 
-void CVolumetricMovement::SetBoundaryDerivatives(CGeometry *geometry, CConfig *config, bool ForwardProjectionDerivative) {
+void CVolumetricMovement::SetBoundaryDerivatives(CGeometry* geometry, CConfig* config,
+                                                 bool ForwardProjectionDerivative) {
   unsigned short iDim, iMarker;
   unsigned long iPoint, total_index, iVertex;
 
-  su2double * VarCoord;
+  su2double* VarCoord;
   SU2_COMPONENT Kind_SU2 = config->GetKind_SU2();
   if ((config->GetDirectDiff() == D_DESIGN) && (Kind_SU2 == SU2_COMPONENT::SU2_CFD)) {
     for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
@@ -1706,7 +1787,7 @@ void CVolumetricMovement::SetBoundaryDerivatives(CGeometry *geometry, CConfig *c
           iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
           VarCoord = geometry->vertex[iMarker][iVertex]->GetVarCoord();
           for (iDim = 0; iDim < nDim; iDim++) {
-            total_index = iPoint*nDim + iDim;
+            total_index = iPoint * nDim + iDim;
             LinSysRes[total_index] = SU2_TYPE::GetDerivative(VarCoord[iDim]);
             LinSysSol[total_index] = SU2_TYPE::GetDerivative(VarCoord[iDim]);
           }
@@ -1714,11 +1795,10 @@ void CVolumetricMovement::SetBoundaryDerivatives(CGeometry *geometry, CConfig *c
       }
     }
     if (LinSysRes.norm() == 0.0) cout << "Warning: Derivatives are zero!" << endl;
-  } else if ((Kind_SU2 == SU2_COMPONENT::SU2_DOT) && !ForwardProjectionDerivative ) {
-
+  } else if ((Kind_SU2 == SU2_COMPONENT::SU2_DOT) && !ForwardProjectionDerivative) {
     for (iPoint = 0; iPoint < nPoint; iPoint++) {
       for (iDim = 0; iDim < nDim; iDim++) {
-        total_index = iPoint*nDim + iDim;
+        total_index = iPoint * nDim + iDim;
         LinSysRes[total_index] = SU2_TYPE::GetValue(geometry->GetSensitivity(iPoint, iDim));
         LinSysSol[total_index] = SU2_TYPE::GetValue(geometry->GetSensitivity(iPoint, iDim));
       }
@@ -1729,7 +1809,7 @@ void CVolumetricMovement::SetBoundaryDerivatives(CGeometry *geometry, CConfig *c
         for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
           iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
           for (iDim = 0; iDim < nDim; iDim++) {
-            total_index = iPoint*nDim + iDim;
+            total_index = iPoint * nDim + iDim;
             LinSysRes[total_index] = SU2_TYPE::GetValue(geometry->GetSensitivity(iPoint, iDim));
             LinSysSol[total_index] = SU2_TYPE::GetValue(geometry->GetSensitivity(iPoint, iDim));
           }
@@ -1740,10 +1820,11 @@ void CVolumetricMovement::SetBoundaryDerivatives(CGeometry *geometry, CConfig *c
   }
 }
 
-void CVolumetricMovement::UpdateGridCoord_Derivatives(CGeometry *geometry, CConfig *config, bool ForwardProjectionDerivative) {
+void CVolumetricMovement::UpdateGridCoord_Derivatives(CGeometry* geometry, CConfig* config,
+                                                      bool ForwardProjectionDerivative) {
   unsigned short iDim, iMarker;
   unsigned long iPoint, total_index, iVertex;
-  su2double *new_coord = new su2double[3];
+  su2double* new_coord = new su2double[3];
 
   SU2_COMPONENT Kind_SU2 = config->GetKind_SU2();
 
@@ -1751,9 +1832,11 @@ void CVolumetricMovement::UpdateGridCoord_Derivatives(CGeometry *geometry, CConf
      after grid deformation (LinSysSol contains the derivatives of the x, y, z displacements). ---*/
   if ((config->GetDirectDiff() == D_DESIGN) && (Kind_SU2 == SU2_COMPONENT::SU2_CFD)) {
     for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++) {
-      new_coord[0] = 0.0; new_coord[1] = 0.0; new_coord[2] = 0.0;
+      new_coord[0] = 0.0;
+      new_coord[1] = 0.0;
+      new_coord[2] = 0.0;
       for (iDim = 0; iDim < nDim; iDim++) {
-        total_index = iPoint*nDim + iDim;
+        total_index = iPoint * nDim + iDim;
         new_coord[iDim] = geometry->nodes->GetCoord(iPoint, iDim);
         SU2_TYPE::SetDerivative(new_coord[iDim], SU2_TYPE::GetValue(LinSysSol[total_index]));
       }
@@ -1764,19 +1847,19 @@ void CVolumetricMovement::UpdateGridCoord_Derivatives(CGeometry *geometry, CConf
     if (config->GetSmoothGradient()) {
       for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++) {
         for (iDim = 0; iDim < nDim; iDim++) {
-          total_index = iPoint*nDim + iDim;
-          geometry->SetSensitivity(iPoint,iDim, 0.0);
+          total_index = iPoint * nDim + iDim;
+          geometry->SetSensitivity(iPoint, iDim, 0.0);
         }
       }
     }
     for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-      if(config->GetSolid_Wall(iMarker) || (config->GetMarker_All_DV(iMarker) == YES)) {
+      if (config->GetSolid_Wall(iMarker) || (config->GetMarker_All_DV(iMarker) == YES)) {
         for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
           iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
           if (geometry->nodes->GetDomain(iPoint)) {
             for (iDim = 0; iDim < nDim; iDim++) {
-              total_index = iPoint*nDim + iDim;
-              geometry->SetSensitivity(iPoint,iDim, LinSysSol[total_index]);
+              total_index = iPoint * nDim + iDim;
+              geometry->SetSensitivity(iPoint, iDim, LinSysSol[total_index]);
             }
           }
         }
@@ -1785,22 +1868,20 @@ void CVolumetricMovement::UpdateGridCoord_Derivatives(CGeometry *geometry, CConf
   } else if (config->GetSmoothGradient() && ForwardProjectionDerivative) {
     for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++) {
       for (iDim = 0; iDim < nDim; iDim++) {
-        total_index = iPoint*nDim + iDim;
-        geometry->SetSensitivity(iPoint,iDim, LinSysSol[total_index]);
+        total_index = iPoint * nDim + iDim;
+        geometry->SetSensitivity(iPoint, iDim, LinSysSol[total_index]);
       }
     }
   }
 
-  delete [] new_coord;
+  delete[] new_coord;
 }
 
-void CVolumetricMovement::SetDomainDisplacements(CGeometry *geometry, CConfig *config) {
-
+void CVolumetricMovement::SetDomainDisplacements(CGeometry* geometry, CConfig* config) {
   unsigned short iDim, nDim = geometry->GetnDim();
   unsigned long iPoint, total_index;
 
   if (config->GetHold_GridFixed()) {
-
     auto MinCoordValues = config->GetHold_GridFixed_Coord();
     auto MaxCoordValues = &config->GetHold_GridFixed_Coord()[3];
 
@@ -1811,7 +1892,7 @@ void CVolumetricMovement::SetDomainDisplacements(CGeometry *geometry, CConfig *c
       auto Coord = geometry->nodes->GetCoord(iPoint);
       for (iDim = 0; iDim < nDim; iDim++) {
         if ((Coord[iDim] < MinCoordValues[iDim]) || (Coord[iDim] > MaxCoordValues[iDim])) {
-          total_index = iPoint*nDim + iDim;
+          total_index = iPoint * nDim + iDim;
           LinSysRes[total_index] = 0.0;
           LinSysSol[total_index] = 0.0;
           StiffMatrix.DeleteValsRowi(total_index);
@@ -1827,7 +1908,7 @@ void CVolumetricMovement::SetDomainDisplacements(CGeometry *geometry, CConfig *c
     for (iPoint = 0; iPoint < nPoint; iPoint++) {
       if (geometry->nodes->GetWall_Distance(iPoint) >= config->GetDeform_Limit()) {
         for (iDim = 0; iDim < nDim; iDim++) {
-          total_index = iPoint*nDim + iDim;
+          total_index = iPoint * nDim + iDim;
           LinSysRes[total_index] = 0.0;
           LinSysSol[total_index] = 0.0;
           StiffMatrix.DeleteValsRowi(total_index);
@@ -1835,20 +1916,18 @@ void CVolumetricMovement::SetDomainDisplacements(CGeometry *geometry, CConfig *c
       }
     }
   }
-
 }
 
-void CVolumetricMovement::Rigid_Rotation(CGeometry *geometry, CConfig *config,
-                                         unsigned short iZone, unsigned long iter) {
-
+void CVolumetricMovement::Rigid_Rotation(CGeometry* geometry, CConfig* config, unsigned short iZone,
+                                         unsigned long iter) {
   /*--- Local variables ---*/
   unsigned short iDim, nDim;
   unsigned long iPoint;
-  su2double r[3] = {0.0,0.0,0.0}, rotCoord[3] = {0.0,0.0,0.0}, *Coord;
-  su2double Center[3] = {0.0,0.0,0.0}, Omega[3] = {0.0,0.0,0.0}, Lref;
-  su2double dt, Center_Moment[3] = {0.0,0.0,0.0};
-  su2double *GridVel, newGridVel[3] = {0.0,0.0,0.0};
-  su2double rotMatrix[3][3] = {{0.0,0.0,0.0}, {0.0,0.0,0.0}, {0.0,0.0,0.0}};
+  su2double r[3] = {0.0, 0.0, 0.0}, rotCoord[3] = {0.0, 0.0, 0.0}, *Coord;
+  su2double Center[3] = {0.0, 0.0, 0.0}, Omega[3] = {0.0, 0.0, 0.0}, Lref;
+  su2double dt, Center_Moment[3] = {0.0, 0.0, 0.0};
+  su2double *GridVel, newGridVel[3] = {0.0, 0.0, 0.0};
+  su2double rotMatrix[3][3] = {{0.0, 0.0, 0.0}, {0.0, 0.0, 0.0}, {0.0, 0.0, 0.0}};
   su2double dtheta, dphi, dpsi, cosTheta, sinTheta;
   su2double cosPhi, sinPhi, cosPsi, sinPsi;
   bool harmonic_balance = (config->GetTime_Marching() == TIME_MARCHING::HARMONIC_BALANCE);
@@ -1856,15 +1935,16 @@ void CVolumetricMovement::Rigid_Rotation(CGeometry *geometry, CConfig *config,
 
   /*--- Problem dimension and physical time step ---*/
   nDim = geometry->GetnDim();
-  dt   = config->GetDelta_UnstTimeND();
+  dt = config->GetDelta_UnstTimeND();
   Lref = config->GetLength_Ref();
 
   /*--- For the unsteady adjoint, use reverse time ---*/
   if (adjoint) {
     /*--- Set the first adjoint mesh position to the final direct one ---*/
-    if (iter == 0) dt = ((su2double)config->GetnTime_Iter()-1)*dt;
+    if (iter == 0) dt = ((su2double)config->GetnTime_Iter() - 1) * dt;
     /*--- Reverse the rotation direction for the adjoint ---*/
-    else dt = -1.0*dt;
+    else
+      dt = -1.0 * dt;
   } else {
     /*--- No rotation at all for the first direct solution ---*/
     if (iter == 0) dt = 0;
@@ -1872,9 +1952,9 @@ void CVolumetricMovement::Rigid_Rotation(CGeometry *geometry, CConfig *config,
 
   /*--- Center of rotation & angular velocity vector from config ---*/
 
-  for (iDim = 0; iDim < 3; iDim++){
+  for (iDim = 0; iDim < 3; iDim++) {
     Center[iDim] = config->GetMotion_Origin(iDim);
-    Omega[iDim]  = config->GetRotation_Rate(iDim)/config->GetOmega_Ref();
+    Omega[iDim] = config->GetRotation_Rate(iDim) / config->GetOmega_Ref();
   }
 
   /*-- Set dt for harmonic balance cases ---*/
@@ -1882,14 +1962,14 @@ void CVolumetricMovement::Rigid_Rotation(CGeometry *geometry, CConfig *config,
     /*--- period of oscillation & compute time interval using nTimeInstances ---*/
     su2double period = config->GetHarmonicBalance_Period();
     period /= config->GetTime_Ref();
-    dt = period * (su2double)iter/(su2double)(config->GetnTimeInstances());
+    dt = period * (su2double)iter / (su2double)(config->GetnTimeInstances());
   }
 
   /*--- Compute delta change in the angle about the x, y, & z axes. ---*/
 
-  dtheta = Omega[0]*dt;
-  dphi   = Omega[1]*dt;
-  dpsi   = Omega[2]*dt;
+  dtheta = Omega[0] * dt;
+  dphi = Omega[1] * dt;
+  dpsi = Omega[2] * dt;
 
   if (rank == MASTER_NODE && iter == 0) {
     cout << " Angular velocity: (" << Omega[0] << ", " << Omega[1];
@@ -1898,56 +1978,53 @@ void CVolumetricMovement::Rigid_Rotation(CGeometry *geometry, CConfig *config,
 
   /*--- Store angles separately for clarity. Compute sines/cosines. ---*/
 
-  cosTheta = cos(dtheta);  cosPhi = cos(dphi);  cosPsi = cos(dpsi);
-  sinTheta = sin(dtheta);  sinPhi = sin(dphi);  sinPsi = sin(dpsi);
+  cosTheta = cos(dtheta);
+  cosPhi = cos(dphi);
+  cosPsi = cos(dpsi);
+  sinTheta = sin(dtheta);
+  sinPhi = sin(dphi);
+  sinPsi = sin(dpsi);
 
   /*--- Compute the rotation matrix. Note that the implicit
    ordering is rotation about the x-axis, y-axis, then z-axis. ---*/
 
-  rotMatrix[0][0] = cosPhi*cosPsi;
-  rotMatrix[1][0] = cosPhi*sinPsi;
+  rotMatrix[0][0] = cosPhi * cosPsi;
+  rotMatrix[1][0] = cosPhi * sinPsi;
   rotMatrix[2][0] = -sinPhi;
 
-  rotMatrix[0][1] = sinTheta*sinPhi*cosPsi - cosTheta*sinPsi;
-  rotMatrix[1][1] = sinTheta*sinPhi*sinPsi + cosTheta*cosPsi;
-  rotMatrix[2][1] = sinTheta*cosPhi;
+  rotMatrix[0][1] = sinTheta * sinPhi * cosPsi - cosTheta * sinPsi;
+  rotMatrix[1][1] = sinTheta * sinPhi * sinPsi + cosTheta * cosPsi;
+  rotMatrix[2][1] = sinTheta * cosPhi;
 
-  rotMatrix[0][2] = cosTheta*sinPhi*cosPsi + sinTheta*sinPsi;
-  rotMatrix[1][2] = cosTheta*sinPhi*sinPsi - sinTheta*cosPsi;
-  rotMatrix[2][2] = cosTheta*cosPhi;
+  rotMatrix[0][2] = cosTheta * sinPhi * cosPsi + sinTheta * sinPsi;
+  rotMatrix[1][2] = cosTheta * sinPhi * sinPsi - sinTheta * cosPsi;
+  rotMatrix[2][2] = cosTheta * cosPhi;
 
   /*--- Loop over and rotate each node in the volume mesh ---*/
   for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++) {
-
     /*--- Coordinates of the current point ---*/
-    Coord   = geometry->nodes->GetCoord(iPoint);
+    Coord = geometry->nodes->GetCoord(iPoint);
     GridVel = geometry->nodes->GetGridVel(iPoint);
 
     /*--- Calculate non-dim. position from rotation center ---*/
-    r[0] = (Coord[0]-Center[0])/Lref;
-    r[1] = (Coord[1]-Center[1])/Lref;
-    if (nDim == 3) r[2] = (Coord[2]-Center[2])/Lref;
+    r[0] = (Coord[0] - Center[0]) / Lref;
+    r[1] = (Coord[1] - Center[1]) / Lref;
+    if (nDim == 3) r[2] = (Coord[2] - Center[2]) / Lref;
 
     /*--- Compute transformed point coordinates ---*/
-    rotCoord[0] = rotMatrix[0][0]*r[0]
-                + rotMatrix[0][1]*r[1]
-                + rotMatrix[0][2]*r[2];
+    rotCoord[0] = rotMatrix[0][0] * r[0] + rotMatrix[0][1] * r[1] + rotMatrix[0][2] * r[2];
 
-    rotCoord[1] = rotMatrix[1][0]*r[0]
-                + rotMatrix[1][1]*r[1]
-                + rotMatrix[1][2]*r[2];
+    rotCoord[1] = rotMatrix[1][0] * r[0] + rotMatrix[1][1] * r[1] + rotMatrix[1][2] * r[2];
 
-    rotCoord[2] = rotMatrix[2][0]*r[0]
-                + rotMatrix[2][1]*r[1]
-                + rotMatrix[2][2]*r[2];
+    rotCoord[2] = rotMatrix[2][0] * r[0] + rotMatrix[2][1] * r[1] + rotMatrix[2][2] * r[2];
 
     /*--- Cross Product of angular velocity and distance from center.
      Note that we have assumed the grid velocities have been set to
      an initial value in the plunging routine. ---*/
 
-    newGridVel[0] = GridVel[0] + Omega[1]*rotCoord[2] - Omega[2]*rotCoord[1];
-    newGridVel[1] = GridVel[1] + Omega[2]*rotCoord[0] - Omega[0]*rotCoord[2];
-    if (nDim == 3) newGridVel[2] = GridVel[2] + Omega[0]*rotCoord[1] - Omega[1]*rotCoord[0];
+    newGridVel[0] = GridVel[0] + Omega[1] * rotCoord[2] - Omega[2] * rotCoord[1];
+    newGridVel[1] = GridVel[1] + Omega[2] * rotCoord[0] - Omega[0] * rotCoord[2];
+    if (nDim == 3) newGridVel[2] = GridVel[2] + Omega[0] * rotCoord[1] - Omega[1] * rotCoord[0];
 
     /*--- Store new node location & grid velocity. Add center.
      Do not store the grid velocity if this is an adjoint calculation.---*/
@@ -1955,61 +2032,51 @@ void CVolumetricMovement::Rigid_Rotation(CGeometry *geometry, CConfig *config,
     for (iDim = 0; iDim < nDim; iDim++) {
       geometry->nodes->SetCoord(iPoint, iDim, rotCoord[iDim] + Center[iDim]);
       if (!adjoint) geometry->nodes->SetGridVel(iPoint, iDim, newGridVel[iDim]);
-
     }
   }
 
   /*--- Set the moment computation center to the new location after
    incrementing the position with the rotation. ---*/
 
-  for (unsigned short jMarker=0; jMarker<config->GetnMarker_Monitoring(); jMarker++) {
-
+  for (unsigned short jMarker = 0; jMarker < config->GetnMarker_Monitoring(); jMarker++) {
     Center_Moment[0] = config->GetRefOriginMoment_X(jMarker);
     Center_Moment[1] = config->GetRefOriginMoment_Y(jMarker);
     Center_Moment[2] = config->GetRefOriginMoment_Z(jMarker);
 
     /*--- Calculate non-dim. position from rotation center ---*/
 
-    for (iDim = 0; iDim < nDim; iDim++)
-      r[iDim] = (Center_Moment[iDim]-Center[iDim])/Lref;
+    for (iDim = 0; iDim < nDim; iDim++) r[iDim] = (Center_Moment[iDim] - Center[iDim]) / Lref;
     if (nDim == 2) r[nDim] = 0.0;
 
     /*--- Compute transformed point coordinates ---*/
 
-    rotCoord[0] = rotMatrix[0][0]*r[0]
-    + rotMatrix[0][1]*r[1]
-    + rotMatrix[0][2]*r[2];
+    rotCoord[0] = rotMatrix[0][0] * r[0] + rotMatrix[0][1] * r[1] + rotMatrix[0][2] * r[2];
 
-    rotCoord[1] = rotMatrix[1][0]*r[0]
-    + rotMatrix[1][1]*r[1]
-    + rotMatrix[1][2]*r[2];
+    rotCoord[1] = rotMatrix[1][0] * r[0] + rotMatrix[1][1] * r[1] + rotMatrix[1][2] * r[2];
 
-    rotCoord[2] = rotMatrix[2][0]*r[0]
-    + rotMatrix[2][1]*r[1]
-    + rotMatrix[2][2]*r[2];
+    rotCoord[2] = rotMatrix[2][0] * r[0] + rotMatrix[2][1] * r[1] + rotMatrix[2][2] * r[2];
 
-    config->SetRefOriginMoment_X(jMarker, Center[0]+rotCoord[0]);
-    config->SetRefOriginMoment_Y(jMarker, Center[1]+rotCoord[1]);
-    config->SetRefOriginMoment_Z(jMarker, Center[2]+rotCoord[2]);
+    config->SetRefOriginMoment_X(jMarker, Center[0] + rotCoord[0]);
+    config->SetRefOriginMoment_Y(jMarker, Center[1] + rotCoord[1]);
+    config->SetRefOriginMoment_Z(jMarker, Center[2] + rotCoord[2]);
   }
 
   /*--- After moving all nodes, update geometry class ---*/
 
   UpdateDualGrid(geometry, config);
-
 }
 
-void CVolumetricMovement::Rigid_Pitching(CGeometry *geometry, CConfig *config, unsigned short iZone, unsigned long iter) {
-
+void CVolumetricMovement::Rigid_Pitching(CGeometry* geometry, CConfig* config, unsigned short iZone,
+                                         unsigned long iter) {
   /*--- Local variables ---*/
-  su2double r[3] = {0.0,0.0,0.0}, rotCoord[3] = {0.0,0.0,0.0}, *Coord, Center[3] = {0.0,0.0,0.0},
-  Omega[3] = {0.0,0.0,0.0}, Ampl[3] = {0.0,0.0,0.0}, Phase[3] = {0.0,0.0,0.0};
-  su2double Lref, deltaT, alphaDot[3], *GridVel, newGridVel[3] = {0.0,0.0,0.0};
-  su2double rotMatrix[3][3] = {{0.0,0.0,0.0}, {0.0,0.0,0.0}, {0.0,0.0,0.0}};
+  su2double r[3] = {0.0, 0.0, 0.0}, rotCoord[3] = {0.0, 0.0, 0.0}, *Coord, Center[3] = {0.0, 0.0, 0.0},
+            Omega[3] = {0.0, 0.0, 0.0}, Ampl[3] = {0.0, 0.0, 0.0}, Phase[3] = {0.0, 0.0, 0.0};
+  su2double Lref, deltaT, alphaDot[3], *GridVel, newGridVel[3] = {0.0, 0.0, 0.0};
+  su2double rotMatrix[3][3] = {{0.0, 0.0, 0.0}, {0.0, 0.0, 0.0}, {0.0, 0.0, 0.0}};
   su2double dtheta, dphi, dpsi, cosTheta, sinTheta;
   su2double cosPhi, sinPhi, cosPsi, sinPsi;
   su2double time_new, time_old;
-  su2double DEG2RAD = PI_NUMBER/180.0;
+  su2double DEG2RAD = PI_NUMBER / 180.0;
   unsigned short iDim;
   unsigned short nDim = geometry->GetnDim();
   unsigned long iPoint;
@@ -2018,127 +2085,122 @@ void CVolumetricMovement::Rigid_Pitching(CGeometry *geometry, CConfig *config, u
 
   /*--- Retrieve values from the config file ---*/
   deltaT = config->GetDelta_UnstTimeND();
-  Lref   = config->GetLength_Ref();
+  Lref = config->GetLength_Ref();
 
   /*--- Pitching origin, frequency, and amplitude from config. ---*/
 
-  for (iDim = 0; iDim < 3; iDim++){
+  for (iDim = 0; iDim < 3; iDim++) {
     Center[iDim] = config->GetMotion_Origin(iDim);
-    Omega[iDim]  = config->GetPitching_Omega(iDim)/config->GetOmega_Ref();
-    Ampl[iDim]   = config->GetPitching_Ampl(iDim)*DEG2RAD;
-    Phase[iDim]  = config->GetPitching_Phase(iDim)*DEG2RAD;
+    Omega[iDim] = config->GetPitching_Omega(iDim) / config->GetOmega_Ref();
+    Ampl[iDim] = config->GetPitching_Ampl(iDim) * DEG2RAD;
+    Phase[iDim] = config->GetPitching_Phase(iDim) * DEG2RAD;
   }
 
-
   if (harmonic_balance) {
     /*--- period of oscillation & compute time interval using nTimeInstances ---*/
     su2double period = config->GetHarmonicBalance_Period();
     period /= config->GetTime_Ref();
-    deltaT = period/(su2double)(config->GetnTimeInstances());
+    deltaT = period / (su2double)(config->GetnTimeInstances());
   }
 
   /*--- Compute delta time based on physical time step ---*/
   if (adjoint) {
     /*--- For the unsteady adjoint, we integrate backwards through
      physical time, so perform mesh motion in reverse. ---*/
-    unsigned long nFlowIter  = config->GetnTime_Iter();
+    unsigned long nFlowIter = config->GetnTime_Iter();
     unsigned long directIter = nFlowIter - iter - 1;
-    time_new = static_cast<su2double>(directIter)*deltaT;
+    time_new = static_cast<su2double>(directIter) * deltaT;
     time_old = time_new;
-    if (iter != 0) time_old = (static_cast<su2double>(directIter)+1.0)*deltaT;
+    if (iter != 0) time_old = (static_cast<su2double>(directIter) + 1.0) * deltaT;
   } else {
     /*--- Forward time for the direct problem ---*/
-    time_new = static_cast<su2double>(iter)*deltaT;
+    time_new = static_cast<su2double>(iter) * deltaT;
     if (harmonic_balance) {
       /*--- For harmonic balance, begin movement from the zero position ---*/
       time_old = 0.0;
     } else {
       time_old = time_new;
-      if (iter != 0) time_old = (static_cast<su2double>(iter)-1.0)*deltaT;
+      if (iter != 0) time_old = (static_cast<su2double>(iter) - 1.0) * deltaT;
     }
   }
 
   /*--- Compute delta change in the angle about the x, y, & z axes. ---*/
 
-  dtheta = -Ampl[0]*(sin(Omega[0]*time_new + Phase[0]) - sin(Omega[0]*time_old + Phase[0]));
-  dphi   = -Ampl[1]*(sin(Omega[1]*time_new + Phase[1]) - sin(Omega[1]*time_old + Phase[1]));
-  dpsi   = -Ampl[2]*(sin(Omega[2]*time_new + Phase[2]) - sin(Omega[2]*time_old + Phase[2]));
+  dtheta = -Ampl[0] * (sin(Omega[0] * time_new + Phase[0]) - sin(Omega[0] * time_old + Phase[0]));
+  dphi = -Ampl[1] * (sin(Omega[1] * time_new + Phase[1]) - sin(Omega[1] * time_old + Phase[1]));
+  dpsi = -Ampl[2] * (sin(Omega[2] * time_new + Phase[2]) - sin(Omega[2] * time_old + Phase[2]));
 
   /*--- Angular velocity at the new time ---*/
 
-  alphaDot[0] = -Omega[0]*Ampl[0]*cos(Omega[0]*time_new + Phase[0]);
-  alphaDot[1] = -Omega[1]*Ampl[1]*cos(Omega[1]*time_new + Phase[1]);
-  alphaDot[2] = -Omega[2]*Ampl[2]*cos(Omega[2]*time_new + Phase[2]);
+  alphaDot[0] = -Omega[0] * Ampl[0] * cos(Omega[0] * time_new + Phase[0]);
+  alphaDot[1] = -Omega[1] * Ampl[1] * cos(Omega[1] * time_new + Phase[1]);
+  alphaDot[2] = -Omega[2] * Ampl[2] * cos(Omega[2] * time_new + Phase[2]);
 
   if (rank == MASTER_NODE && iter == 0) {
-      cout << " Pitching frequency: (" << Omega[0] << ", " << Omega[1];
-      cout << ", " << Omega[2] << ") rad/s." << endl;
-      cout << " Pitching amplitude: (" << Ampl[0]/DEG2RAD << ", ";
-      cout << Ampl[1]/DEG2RAD << ", " << Ampl[2]/DEG2RAD;
-      cout << ") degrees."<< endl;
-      cout << " Pitching phase lag: (" << Phase[0]/DEG2RAD << ", ";
-      cout << Phase[1]/DEG2RAD <<", "<< Phase[2]/DEG2RAD;
-      cout << ") degrees."<< endl;
+    cout << " Pitching frequency: (" << Omega[0] << ", " << Omega[1];
+    cout << ", " << Omega[2] << ") rad/s." << endl;
+    cout << " Pitching amplitude: (" << Ampl[0] / DEG2RAD << ", ";
+    cout << Ampl[1] / DEG2RAD << ", " << Ampl[2] / DEG2RAD;
+    cout << ") degrees." << endl;
+    cout << " Pitching phase lag: (" << Phase[0] / DEG2RAD << ", ";
+    cout << Phase[1] / DEG2RAD << ", " << Phase[2] / DEG2RAD;
+    cout << ") degrees." << endl;
   }
 
   /*--- Store angles separately for clarity. Compute sines/cosines. ---*/
 
-  cosTheta = cos(dtheta);  cosPhi = cos(dphi);  cosPsi = cos(dpsi);
-  sinTheta = sin(dtheta);  sinPhi = sin(dphi);  sinPsi = sin(dpsi);
+  cosTheta = cos(dtheta);
+  cosPhi = cos(dphi);
+  cosPsi = cos(dpsi);
+  sinTheta = sin(dtheta);
+  sinPhi = sin(dphi);
+  sinPsi = sin(dpsi);
 
   /*--- Compute the rotation matrix. Note that the implicit
    ordering is rotation about the x-axis, y-axis, then z-axis. ---*/
 
-  rotMatrix[0][0] = cosPhi*cosPsi;
-  rotMatrix[1][0] = cosPhi*sinPsi;
+  rotMatrix[0][0] = cosPhi * cosPsi;
+  rotMatrix[1][0] = cosPhi * sinPsi;
   rotMatrix[2][0] = -sinPhi;
 
-  rotMatrix[0][1] = sinTheta*sinPhi*cosPsi - cosTheta*sinPsi;
-  rotMatrix[1][1] = sinTheta*sinPhi*sinPsi + cosTheta*cosPsi;
-  rotMatrix[2][1] = sinTheta*cosPhi;
+  rotMatrix[0][1] = sinTheta * sinPhi * cosPsi - cosTheta * sinPsi;
+  rotMatrix[1][1] = sinTheta * sinPhi * sinPsi + cosTheta * cosPsi;
+  rotMatrix[2][1] = sinTheta * cosPhi;
 
-  rotMatrix[0][2] = cosTheta*sinPhi*cosPsi + sinTheta*sinPsi;
-  rotMatrix[1][2] = cosTheta*sinPhi*sinPsi - sinTheta*cosPsi;
-  rotMatrix[2][2] = cosTheta*cosPhi;
+  rotMatrix[0][2] = cosTheta * sinPhi * cosPsi + sinTheta * sinPsi;
+  rotMatrix[1][2] = cosTheta * sinPhi * sinPsi - sinTheta * cosPsi;
+  rotMatrix[2][2] = cosTheta * cosPhi;
 
   /*--- Loop over and rotate each node in the volume mesh ---*/
   for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++) {
-
     /*--- Coordinates of the current point ---*/
-    Coord   = geometry->nodes->GetCoord(iPoint);
+    Coord = geometry->nodes->GetCoord(iPoint);
     GridVel = geometry->nodes->GetGridVel(iPoint);
 
     /*--- Calculate non-dim. position from rotation center ---*/
-    for (iDim = 0; iDim < nDim; iDim++)
-      r[iDim] = (Coord[iDim]-Center[iDim])/Lref;
+    for (iDim = 0; iDim < nDim; iDim++) r[iDim] = (Coord[iDim] - Center[iDim]) / Lref;
     if (nDim == 2) r[nDim] = 0.0;
 
     /*--- Compute transformed point coordinates ---*/
-    rotCoord[0] = rotMatrix[0][0]*r[0]
-                + rotMatrix[0][1]*r[1]
-                + rotMatrix[0][2]*r[2];
+    rotCoord[0] = rotMatrix[0][0] * r[0] + rotMatrix[0][1] * r[1] + rotMatrix[0][2] * r[2];
 
-    rotCoord[1] = rotMatrix[1][0]*r[0]
-                + rotMatrix[1][1]*r[1]
-                + rotMatrix[1][2]*r[2];
+    rotCoord[1] = rotMatrix[1][0] * r[0] + rotMatrix[1][1] * r[1] + rotMatrix[1][2] * r[2];
 
-    rotCoord[2] = rotMatrix[2][0]*r[0]
-                + rotMatrix[2][1]*r[1]
-                + rotMatrix[2][2]*r[2];
+    rotCoord[2] = rotMatrix[2][0] * r[0] + rotMatrix[2][1] * r[1] + rotMatrix[2][2] * r[2];
 
     /*--- Cross Product of angular velocity and distance from center.
      Note that we have assumed the grid velocities have been set to
      an initial value in the plunging routine. ---*/
 
-    newGridVel[0] = GridVel[0] + alphaDot[1]*rotCoord[2] - alphaDot[2]*rotCoord[1];
-    newGridVel[1] = GridVel[1] + alphaDot[2]*rotCoord[0] - alphaDot[0]*rotCoord[2];
-    if (nDim == 3) newGridVel[2] = GridVel[2] + alphaDot[0]*rotCoord[1] - alphaDot[1]*rotCoord[0];
+    newGridVel[0] = GridVel[0] + alphaDot[1] * rotCoord[2] - alphaDot[2] * rotCoord[1];
+    newGridVel[1] = GridVel[1] + alphaDot[2] * rotCoord[0] - alphaDot[0] * rotCoord[2];
+    if (nDim == 3) newGridVel[2] = GridVel[2] + alphaDot[0] * rotCoord[1] - alphaDot[1] * rotCoord[0];
 
     /*--- Store new node location & grid velocity. Add center location.
      Do not store the grid velocity if this is an adjoint calculation.---*/
 
     for (iDim = 0; iDim < nDim; iDim++) {
-      geometry->nodes->SetCoord(iPoint, iDim, rotCoord[iDim]+Center[iDim]);
+      geometry->nodes->SetCoord(iPoint, iDim, rotCoord[iDim] + Center[iDim]);
       if (!adjoint) geometry->nodes->SetGridVel(iPoint, iDim, newGridVel[iDim]);
     }
   }
@@ -2148,11 +2210,10 @@ void CVolumetricMovement::Rigid_Pitching(CGeometry *geometry, CConfig *config, u
   /*--- After moving all nodes, update geometry class ---*/
 
   UpdateDualGrid(geometry, config);
-
 }
 
-void CVolumetricMovement::Rigid_Plunging(CGeometry *geometry, CConfig *config, unsigned short iZone, unsigned long iter) {
-
+void CVolumetricMovement::Rigid_Plunging(CGeometry* geometry, CConfig* config, unsigned short iZone,
+                                         unsigned long iter) {
   /*--- Local variables ---*/
   su2double deltaX[3], newCoord[3] = {0.0, 0.0, 0.0}, Center[3], *Coord, Omega[3], Ampl[3], Lref;
   su2double *GridVel, newGridVel[3] = {0.0, 0.0, 0.0}, xDot[3];
@@ -2164,12 +2225,12 @@ void CVolumetricMovement::Rigid_Plunging(CGeometry *geometry, CConfig *config, u
 
   /*--- Retrieve values from the config file ---*/
   deltaT = config->GetDelta_UnstTimeND();
-  Lref   = config->GetLength_Ref();
+  Lref = config->GetLength_Ref();
 
-  for (iDim = 0; iDim < 3; iDim++){
+  for (iDim = 0; iDim < 3; iDim++) {
     Center[iDim] = config->GetMotion_Origin(iDim);
-    Omega[iDim]  = config->GetPlunging_Omega(iDim)/config->GetOmega_Ref();
-    Ampl[iDim]   = config->GetPlunging_Ampl(iDim)/Lref;
+    Omega[iDim] = config->GetPlunging_Omega(iDim) / config->GetOmega_Ref();
+    Ampl[iDim] = config->GetPlunging_Ampl(iDim) / Lref;
   }
 
   /*--- Plunging frequency and amplitude from config. ---*/
@@ -2178,57 +2239,55 @@ void CVolumetricMovement::Rigid_Plunging(CGeometry *geometry, CConfig *config, u
     /*--- period of oscillation & time interval using nTimeInstances ---*/
     su2double period = config->GetHarmonicBalance_Period();
     period /= config->GetTime_Ref();
-    deltaT = period/(su2double)(config->GetnTimeInstances());
+    deltaT = period / (su2double)(config->GetnTimeInstances());
   }
 
   /*--- Compute delta time based on physical time step ---*/
   if (adjoint) {
     /*--- For the unsteady adjoint, we integrate backwards through
      physical time, so perform mesh motion in reverse. ---*/
-    unsigned long nFlowIter  = config->GetnTime_Iter();
+    unsigned long nFlowIter = config->GetnTime_Iter();
     unsigned long directIter = nFlowIter - iter - 1;
-    time_new = static_cast<su2double>(directIter)*deltaT;
+    time_new = static_cast<su2double>(directIter) * deltaT;
     time_old = time_new;
-    if (iter != 0) time_old = (static_cast<su2double>(directIter)+1.0)*deltaT;
+    if (iter != 0) time_old = (static_cast<su2double>(directIter) + 1.0) * deltaT;
   } else {
     /*--- Forward time for the direct problem ---*/
-    time_new = static_cast<su2double>(iter)*deltaT;
+    time_new = static_cast<su2double>(iter) * deltaT;
     if (harmonic_balance) {
       /*--- For harmonic balance, begin movement from the zero position ---*/
       time_old = 0.0;
     } else {
       time_old = time_new;
-      if (iter != 0) time_old = (static_cast<su2double>(iter)-1.0)*deltaT;
+      if (iter != 0) time_old = (static_cast<su2double>(iter) - 1.0) * deltaT;
     }
   }
 
   /*--- Compute delta change in the position in the x, y, & z directions. ---*/
-  deltaX[0] = -Ampl[0]*(sin(Omega[0]*time_new) - sin(Omega[0]*time_old));
-  deltaX[1] = -Ampl[1]*(sin(Omega[1]*time_new) - sin(Omega[1]*time_old));
-  deltaX[2] = -Ampl[2]*(sin(Omega[2]*time_new) - sin(Omega[2]*time_old));
+  deltaX[0] = -Ampl[0] * (sin(Omega[0] * time_new) - sin(Omega[0] * time_old));
+  deltaX[1] = -Ampl[1] * (sin(Omega[1] * time_new) - sin(Omega[1] * time_old));
+  deltaX[2] = -Ampl[2] * (sin(Omega[2] * time_new) - sin(Omega[2] * time_old));
 
   /*--- Compute grid velocity due to plunge in the x, y, & z directions. ---*/
-  xDot[0] = -Ampl[0]*Omega[0]*(cos(Omega[0]*time_new));
-  xDot[1] = -Ampl[1]*Omega[1]*(cos(Omega[1]*time_new));
-  xDot[2] = -Ampl[2]*Omega[2]*(cos(Omega[2]*time_new));
+  xDot[0] = -Ampl[0] * Omega[0] * (cos(Omega[0] * time_new));
+  xDot[1] = -Ampl[1] * Omega[1] * (cos(Omega[1] * time_new));
+  xDot[2] = -Ampl[2] * Omega[2] * (cos(Omega[2] * time_new));
 
   if (rank == MASTER_NODE && iter == 0) {
     cout << " Plunging frequency: (" << Omega[0] << ", " << Omega[1];
     cout << ", " << Omega[2] << ") rad/s." << endl;
     cout << " Plunging amplitude: (" << Ampl[0] << ", ";
-    cout << Ampl[1] << ", " << Ampl[2] <<  ") m."<< endl;
+    cout << Ampl[1] << ", " << Ampl[2] << ") m." << endl;
   }
 
   /*--- Loop over and move each node in the volume mesh ---*/
   for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++) {
-
     /*--- Coordinates of the current point ---*/
-    Coord   = geometry->nodes->GetCoord(iPoint);
+    Coord = geometry->nodes->GetCoord(iPoint);
     GridVel = geometry->nodes->GetGridVel(iPoint);
 
     /*--- Increment the node position using the delta values. ---*/
-    for (iDim = 0; iDim < nDim; iDim++)
-      newCoord[iDim] = Coord[iDim] + deltaX[iDim];
+    for (iDim = 0; iDim < nDim; iDim++) newCoord[iDim] = Coord[iDim] + deltaX[iDim];
 
     /*--- Cross Product of angular velocity and distance from center.
      Note that we have assumed the grid velocities have been set to
@@ -2236,7 +2295,7 @@ void CVolumetricMovement::Rigid_Plunging(CGeometry *geometry, CConfig *config, u
 
     newGridVel[0] = GridVel[0] + xDot[0];
     newGridVel[1] = GridVel[1] + xDot[1];
-   if (nDim == 3) newGridVel[2] = GridVel[2] + xDot[2];
+    if (nDim == 3) newGridVel[2] = GridVel[2] + xDot[2];
 
     /*--- Store new node location & grid velocity. Do not store the grid
      velocity if this is an adjoint calculation. ---*/
@@ -2251,23 +2310,23 @@ void CVolumetricMovement::Rigid_Plunging(CGeometry *geometry, CConfig *config, u
    incrementing the position with the rigid translation. This
    new location will be used for subsequent pitching/rotation.---*/
 
-  for (iDim = 0; iDim < 3; iDim++){
+  for (iDim = 0; iDim < 3; iDim++) {
     Center[iDim] = config->GetMotion_Origin(iDim) + deltaX[iDim];
   }
   config->SetMotion_Origin(Center);
 
   /*--- As the body origin may have moved, print it to the console ---*/
 
-//  if (rank == MASTER_NODE) {
-//    cout << " Body origin: (" << Center[0]+deltaX[0];
-//    cout << ", " << Center[1]+deltaX[1] << ", " << Center[2]+deltaX[2];
-//    cout << ")." << endl;
-//  }
+  //  if (rank == MASTER_NODE) {
+  //    cout << " Body origin: (" << Center[0]+deltaX[0];
+  //    cout << ", " << Center[1]+deltaX[1] << ", " << Center[2]+deltaX[2];
+  //    cout << ")." << endl;
+  //  }
 
   /*--- Set the moment computation center to the new location after
    incrementing the position with the plunging. ---*/
 
-  for (unsigned short jMarker=0; jMarker<config->GetnMarker_Monitoring(); jMarker++) {
+  for (unsigned short jMarker = 0; jMarker < config->GetnMarker_Monitoring(); jMarker++) {
     Center[0] = config->GetRefOriginMoment_X(jMarker) + deltaX[0];
     Center[1] = config->GetRefOriginMoment_Y(jMarker) + deltaX[1];
     Center[2] = config->GetRefOriginMoment_Z(jMarker) + deltaX[2];
@@ -2279,11 +2338,10 @@ void CVolumetricMovement::Rigid_Plunging(CGeometry *geometry, CConfig *config, u
   /*--- After moving all nodes, update geometry class ---*/
 
   UpdateDualGrid(geometry, config);
-
 }
 
-void CVolumetricMovement::Rigid_Translation(CGeometry *geometry, CConfig *config, unsigned short iZone, unsigned long iter) {
-
+void CVolumetricMovement::Rigid_Translation(CGeometry* geometry, CConfig* config, unsigned short iZone,
+                                            unsigned long iter) {
   /*--- Local variables ---*/
   su2double deltaX[3], newCoord[3] = {0.0, 0.0, 0.0}, Center[3], *Coord;
   su2double xDot[3];
@@ -2298,70 +2356,71 @@ void CVolumetricMovement::Rigid_Translation(CGeometry *geometry, CConfig *config
 
   /*--- Get motion center and translation rates from config ---*/
 
-  for (iDim = 0; iDim < 3; iDim++){
+  for (iDim = 0; iDim < 3; iDim++) {
     Center[iDim] = config->GetMotion_Origin(iDim);
-    xDot[iDim]   = config->GetTranslation_Rate(iDim);
+    xDot[iDim] = config->GetTranslation_Rate(iDim);
   }
 
   if (harmonic_balance) {
     /*--- period of oscillation & time interval using nTimeInstances ---*/
     su2double period = config->GetHarmonicBalance_Period();
     period /= config->GetTime_Ref();
-    deltaT = period/(su2double)(config->GetnTimeInstances());
+    deltaT = period / (su2double)(config->GetnTimeInstances());
   }
 
   /*--- Compute delta time based on physical time step ---*/
   if (adjoint) {
     /*--- For the unsteady adjoint, we integrate backwards through
      physical time, so perform mesh motion in reverse. ---*/
-    unsigned long nFlowIter  = config->GetnTime_Iter();
+    unsigned long nFlowIter = config->GetnTime_Iter();
     unsigned long directIter = nFlowIter - iter - 1;
-    time_new = static_cast<su2double>(directIter)*deltaT;
+    time_new = static_cast<su2double>(directIter) * deltaT;
     time_old = time_new;
-    if (iter != 0) time_old = (static_cast<su2double>(directIter)+1.0)*deltaT;
+    if (iter != 0) time_old = (static_cast<su2double>(directIter) + 1.0) * deltaT;
   } else {
     /*--- Forward time for the direct problem ---*/
-    time_new = static_cast<su2double>(iter)*deltaT;
+    time_new = static_cast<su2double>(iter) * deltaT;
     if (harmonic_balance) {
       /*--- For harmonic balance, begin movement from the zero position ---*/
       time_old = 0.0;
     } else {
       time_old = time_new;
-      if (iter != 0) time_old = (static_cast<su2double>(iter)-1.0)*deltaT;
+      if (iter != 0) time_old = (static_cast<su2double>(iter) - 1.0) * deltaT;
     }
   }
 
   /*--- Compute delta change in the position in the x, y, & z directions. ---*/
-  deltaX[0] = xDot[0]*(time_new-time_old);
-  deltaX[1] = xDot[1]*(time_new-time_old);
-  deltaX[2] = xDot[2]*(time_new-time_old);
+  deltaX[0] = xDot[0] * (time_new - time_old);
+  deltaX[1] = xDot[1] * (time_new - time_old);
+  deltaX[2] = xDot[2] * (time_new - time_old);
 
   if (rank == MASTER_NODE) {
     cout << " New physical time: " << time_new << " seconds." << endl;
     if (iter == 0) {
-    cout << " Translational velocity: (" << xDot[0]*config->GetVelocity_Ref() << ", " << xDot[1]*config->GetVelocity_Ref();
-      cout << ", " << xDot[2]*config->GetVelocity_Ref();
-      if (config->GetSystemMeasurements() == SI) cout << ") m/s." << endl;
-      else cout << ") ft/s." << endl;
+      cout << " Translational velocity: (" << xDot[0] * config->GetVelocity_Ref() << ", "
+           << xDot[1] * config->GetVelocity_Ref();
+      cout << ", " << xDot[2] * config->GetVelocity_Ref();
+      if (config->GetSystemMeasurements() == SI)
+        cout << ") m/s." << endl;
+      else
+        cout << ") ft/s." << endl;
     }
   }
 
   /*--- Loop over and move each node in the volume mesh ---*/
   for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++) {
-
     /*--- Coordinates of the current point ---*/
     Coord = geometry->nodes->GetCoord(iPoint);
 
     /*--- Increment the node position using the delta values. ---*/
-    for (iDim = 0; iDim < nDim; iDim++)
-      newCoord[iDim] = Coord[iDim] + deltaX[iDim];
+    for (iDim = 0; iDim < nDim; iDim++) newCoord[iDim] = Coord[iDim] + deltaX[iDim];
 
     /*--- Store new node location & grid velocity. Do not store the grid
      velocity if this is an adjoint calculation. ---*/
 
     for (iDim = 0; iDim < nDim; iDim++) {
       geometry->nodes->SetCoord(iPoint, iDim, newCoord[iDim]);
-      if (!adjoint) geometry->nodes->SetGridVel(iPoint, iDim,xDot[iDim]);
+      if (!adjoint) geometry->nodes->SetGridVel(iPoint, iDim, xDot[iDim]);
     }
   }
 
@@ -2369,16 +2428,15 @@ void CVolumetricMovement::Rigid_Translation(CGeometry *geometry, CConfig *config
    incrementing the position with the rigid translation. This
    new location will be used for subsequent pitching/rotation.---*/
 
-  for (iDim = 0; iDim < 3; iDim++){
+  for (iDim = 0; iDim < 3; iDim++) {
     Center[iDim] = config->GetMotion_Origin(iDim) + deltaX[iDim];
   }
   config->SetMotion_Origin(Center);
 
-
   /*--- Set the moment computation center to the new location after
    incrementing the position with the translation. ---*/
 
-  for (unsigned short jMarker=0; jMarker<config->GetnMarker_Monitoring(); jMarker++) {
+  for (unsigned short jMarker = 0; jMarker < config->GetnMarker_Monitoring(); jMarker++) {
     Center[0] = config->GetRefOriginMoment_X(jMarker) + deltaX[0];
     Center[1] = config->GetRefOriginMoment_Y(jMarker) + deltaX[1];
     Center[2] = config->GetRefOriginMoment_Z(jMarker) + deltaX[2];
@@ -2390,19 +2448,17 @@ void CVolumetricMovement::Rigid_Translation(CGeometry *geometry, CConfig *config
   /*--- After moving all nodes, update geometry class ---*/
 
   UpdateDualGrid(geometry, config);
-
 }
 
-void CVolumetricMovement::SetVolume_Scaling(CGeometry *geometry, CConfig *config, bool UpdateGeo) {
-
+void CVolumetricMovement::SetVolume_Scaling(CGeometry* geometry, CConfig* config, bool UpdateGeo) {
   unsigned short iDim;
   unsigned long iPoint;
-  su2double newCoord[3] = {0.0,0.0,0.0}, *Coord;
+  su2double newCoord[3] = {0.0, 0.0, 0.0}, *Coord;
 
   /*--- The scaling factor is the only input to this option. Currently,
    the mesh must be scaled the same amount in all three directions. ---*/
 
-  su2double Scale = config->GetDV_Value(0)*config->GetOpt_RelaxFactor();
+  su2double Scale = config->GetDV_Value(0) * config->GetOpt_RelaxFactor();
 
   if (rank == MASTER_NODE) {
     cout << "Scaling the mesh by a constant factor of " << Scale << "." << endl;
@@ -2410,13 +2466,11 @@ void CVolumetricMovement::SetVolume_Scaling(CGeometry *geometry, CConfig *config
 
   /*--- Loop over and move each node in the volume mesh ---*/
   for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++) {
-
     /*--- Coordinates of the current point ---*/
     Coord = geometry->nodes->GetCoord(iPoint);
 
     /*--- Scale the node position by the specified factor. ---*/
-    for (iDim = 0; iDim < nDim; iDim++)
-      newCoord[iDim] = Scale*Coord[iDim];
+    for (iDim = 0; iDim < nDim; iDim++) newCoord[iDim] = Scale * Coord[iDim];
 
     /*--- Store the new node location. ---*/
     for (iDim = 0; iDim < nDim; iDim++) {
@@ -2426,43 +2480,38 @@ void CVolumetricMovement::SetVolume_Scaling(CGeometry *geometry, CConfig *config
 
   /*--- After moving all nodes, update geometry class ---*/
   if (UpdateGeo) UpdateDualGrid(geometry, config);
-
 }
 
-void CVolumetricMovement::SetVolume_Translation(CGeometry *geometry, CConfig *config, bool UpdateGeo)  {
-
+void CVolumetricMovement::SetVolume_Translation(CGeometry* geometry, CConfig* config, bool UpdateGeo) {
   unsigned short iDim;
   unsigned long iPoint;
-  su2double *Coord, deltaX[3] = {0.0,0.0,0.0}, newCoord[3] = {0.0,0.0,0.0};
+  su2double *Coord, deltaX[3] = {0.0, 0.0, 0.0}, newCoord[3] = {0.0, 0.0, 0.0};
   su2double Scale = config->GetOpt_RelaxFactor();
 
   /*--- Get the unit vector and magnitude of displacement. Note that we
    assume this is the first DV entry since it is for mesh translation.
    Create the displacement vector from the magnitude and direction. ---*/
 
-  su2double Ampl = config->GetDV_Value(0)*Scale;
+  su2double Ampl = config->GetDV_Value(0) * Scale;
   su2double length = 0.0;
   for (iDim = 0; iDim < nDim; iDim++) {
     deltaX[iDim] = config->GetParamDV(0, iDim);
-    length += deltaX[iDim]*deltaX[iDim];
+    length += deltaX[iDim] * deltaX[iDim];
   }
   length = sqrt(length);
-  for (iDim = 0; iDim < nDim; iDim++)
-    deltaX[iDim] = Ampl*deltaX[iDim]/length;
+  for (iDim = 0; iDim < nDim; iDim++) deltaX[iDim] = Ampl * deltaX[iDim] / length;
   if (rank == MASTER_NODE) {
     cout << "Translational displacement: (" << deltaX[0] << ", ";
-    cout  << deltaX[1] << ", " << deltaX[2] << ")." << endl;
+    cout << deltaX[1] << ", " << deltaX[2] << ")." << endl;
   }
 
   /*--- Loop over and move each node in the volume mesh ---*/
   for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++) {
-
     /*--- Coordinates of the current point ---*/
     Coord = geometry->nodes->GetCoord(iPoint);
 
     /*--- Increment the node position using the delta values. ---*/
-    for (iDim = 0; iDim < nDim; iDim++)
-      newCoord[iDim] = Coord[iDim] + deltaX[iDim];
+    for (iDim = 0; iDim < nDim; iDim++) newCoord[iDim] = Coord[iDim] + deltaX[iDim];
 
     /*--- Store new node location. ---*/
     for (iDim = 0; iDim < nDim; iDim++) {
@@ -2472,75 +2521,78 @@ void CVolumetricMovement::SetVolume_Translation(CGeometry *geometry, CConfig *co
 
   /*--- After moving all nodes, update geometry class ---*/
   if (UpdateGeo) UpdateDualGrid(geometry, config);
-
 }
 
-void CVolumetricMovement::SetVolume_Rotation(CGeometry *geometry, CConfig *config, bool UpdateGeo) {
-
+void CVolumetricMovement::SetVolume_Rotation(CGeometry* geometry, CConfig* config, bool UpdateGeo) {
   unsigned short iDim;
   unsigned long iPoint;
   su2double x, y, z;
-  su2double *Coord, deltaX[3] = {0.0,0.0,0.0}, newCoord[3] = {0.0,0.0,0.0};
+  su2double *Coord, deltaX[3] = {0.0, 0.0, 0.0}, newCoord[3] = {0.0, 0.0, 0.0};
   su2double Scale = config->GetOpt_RelaxFactor();
 
   /*--- xyz-coordinates of a point on the line of rotation. */
   su2double a = config->GetParamDV(0, 0);
   su2double b = config->GetParamDV(0, 1);
   su2double c = 0.0;
-  if (geometry->GetnDim() == 3) c = config->GetParamDV(0,2);
+  if (geometry->GetnDim() == 3) c = config->GetParamDV(0, 2);
 
   /*--- xyz-coordinate of the line's direction vector. ---*/
-  su2double u = config->GetParamDV(0, 3)-config->GetParamDV(0, 0);
-  su2double v = config->GetParamDV(0, 4)-config->GetParamDV(0, 1);
+  su2double u = config->GetParamDV(0, 3) - config->GetParamDV(0, 0);
+  su2double v = config->GetParamDV(0, 4) - config->GetParamDV(0, 1);
   su2double w = 1.0;
-  if (geometry->GetnDim() == 3)
-    w = config->GetParamDV(0, 5)-config->GetParamDV(0, 2);
+  if (geometry->GetnDim() == 3) w = config->GetParamDV(0, 5) - config->GetParamDV(0, 2);
 
   /*--- The angle of rotation. ---*/
-  su2double theta = config->GetDV_Value(0)*Scale*PI_NUMBER/180.0;
+  su2double theta = config->GetDV_Value(0) * Scale * PI_NUMBER / 180.0;
 
   /*--- Print to the console. ---*/
   if (rank == MASTER_NODE) {
     cout << "Rotation axis vector: (" << u << ", ";
     cout << v << ", " << w << ")." << endl;
-    cout << "Angle of rotation: " << config->GetDV_Value(0)*Scale;
+    cout << "Angle of rotation: " << config->GetDV_Value(0) * Scale;
     cout << " degrees." << endl;
   }
 
   /*--- Intermediate values used in computations. ---*/
-  su2double u2=u*u; su2double v2=v*v; su2double w2=w*w;
-  su2double cosT = cos(theta); su2double sinT = sin(theta);
-  su2double l2 = u2 + v2 + w2; su2double l = sqrt(l2);
+  su2double u2 = u * u;
+  su2double v2 = v * v;
+  su2double w2 = w * w;
+  su2double cosT = cos(theta);
+  su2double sinT = sin(theta);
+  su2double l2 = u2 + v2 + w2;
+  su2double l = sqrt(l2);
 
   /*--- Loop over and move each node in the volume mesh ---*/
   for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++) {
-
     /*--- Coordinates of the current point ---*/
     Coord = geometry->nodes->GetCoord(iPoint);
 
     /*--- Displacement for this point due to the rotation. ---*/
-    x = Coord[0]; y = Coord[1]; z = 0.0;
+    x = Coord[0];
+    y = Coord[1];
+    z = 0.0;
     if (geometry->GetnDim() == 3) z = Coord[2];
 
-    deltaX[0] = a*(v2 + w2) + u*(-b*v - c*w + u*x + v*y + w*z)
-    + (-a*(v2 + w2) + u*(b*v + c*w - v*y - w*z) + (v2 + w2)*x)*cosT
-    + l*(-c*v + b*w - w*y + v*z)*sinT;
-    deltaX[0] = deltaX[0]/l2 - x;
+    deltaX[0] = a * (v2 + w2) + u * (-b * v - c * w + u * x + v * y + w * z) +
+                (-a * (v2 + w2) + u * (b * v + c * w - v * y - w * z) + (v2 + w2) * x) * cosT +
+                l * (-c * v + b * w - w * y + v * z) * sinT;
+    deltaX[0] = deltaX[0] / l2 - x;
 
-    deltaX[1] = b*(u2 + w2) + v*(-a*u - c*w + u*x + v*y + w*z)
-    + (-b*(u2 + w2) + v*(a*u + c*w - u*x - w*z) + (u2 + w2)*y)*cosT
-    + l*(c*u - a*w + w*x - u*z)*sinT;
-    deltaX[1] = deltaX[1]/l2 - y;
+    deltaX[1] = b * (u2 + w2) + v * (-a * u - c * w + u * x + v * y + w * z) +
+                (-b * (u2 + w2) + v * (a * u + c * w - u * x - w * z) + (u2 + w2) * y) * cosT +
+                l * (c * u - a * w + w * x - u * z) * sinT;
+    deltaX[1] = deltaX[1] / l2 - y;
 
-    deltaX[2] = c*(u2 + v2) + w*(-a*u - b*v + u*x + v*y + w*z)
-    + (-c*(u2 + v2) + w*(a*u + b*v - u*x - v*y) + (u2 + v2)*z)*cosT
-    + l*(-b*u + a*v - v*x + u*y)*sinT;
-    if (geometry->GetnDim() == 3) deltaX[2] = deltaX[2]/l2 - z;
-    else deltaX[2] = 0.0;
+    deltaX[2] = c * (u2 + v2) + w * (-a * u - b * v + u * x + v * y + w * z) +
+                (-c * (u2 + v2) + w * (a * u + b * v - u * x - v * y) + (u2 + v2) * z) * cosT +
+                l * (-b * u + a * v - v * x + u * y) * sinT;
+    if (geometry->GetnDim() == 3)
+      deltaX[2] = deltaX[2] / l2 - z;
+    else
+      deltaX[2] = 0.0;
 
     /*--- Increment the node position using the delta values. ---*/
-    for (iDim = 0; iDim < nDim; iDim++)
-      newCoord[iDim] = Coord[iDim] + deltaX[iDim];
+    for (iDim = 0; iDim < nDim; iDim++) newCoord[iDim] = Coord[iDim] + deltaX[iDim];
 
     /*--- Store new node location. ---*/
     for (iDim = 0; iDim < nDim; iDim++) {
@@ -2550,5 +2602,4 @@ void CVolumetricMovement::SetVolume_Rotation(CGeometry *geometry, CConfig *confi
 
   /*--- After moving all nodes, update geometry class ---*/
   if (UpdateGeo) UpdateDualGrid(geometry, config);
-
 }
diff --git a/Common/src/interface_interpolation/CInterpolator.cpp b/Common/src/interface_interpolation/CInterpolator.cpp
index 250bf916d98..8879287a440 100644
--- a/Common/src/interface_interpolation/CInterpolator.cpp
+++ b/Common/src/interface_interpolation/CInterpolator.cpp
@@ -153,7 +153,6 @@ unsigned long CInterpolator::Collect_ElementInfo(int markDonor, unsigned short n
 }
 
 void CInterpolator::ReconstructBoundary(unsigned long val_zone, int val_marker) {
-
   const CGeometry* geom = Geometry[val_zone][INST_0][MESH_0];
   const auto nDim = geom->GetnDim();
 
@@ -197,7 +196,8 @@ void CInterpolator::ReconstructBoundary(unsigned long val_zone, int val_marker)
     if (geom->nodes->GetDomain(iPoint)) {
       const auto iLocalVertex = iVertex_to_iLocalVertex[iVertex];
       Buffer_Send_GlobalPoint[iLocalVertex] = geom->nodes->GetGlobalIndex(iPoint);
-      for (unsigned long iDim = 0; iDim < nDim; iDim++) Buffer_Send_Coord(iLocalVertex,iDim) = geom->nodes->GetCoord(iPoint, iDim);
+      for (unsigned long iDim = 0; iDim < nDim; iDim++)
+        Buffer_Send_Coord(iLocalVertex, iDim) = geom->nodes->GetCoord(iPoint, iDim);
       neighbors.insert(pair<unsigned long, set<unsigned long> >(iPoint, set<unsigned long>()));
     }
   }
@@ -344,7 +344,7 @@ void CInterpolator::ReconstructBoundary(unsigned long val_zone, int val_marker)
    * Buffer_Receive_GlobalPoint, Buffer_Receive_nLinkedNodes etc. ---*/
   if (rank == MASTER_NODE) {
     for (unsigned long iVertex = 0; iVertex < nGlobalVertex; iVertex++) {
-      unsigned long *uptr = &Buffer_Receive_LinkedNodes[Buffer_Receive_StartLinkedNodes[iVertex]];
+      unsigned long* uptr = &Buffer_Receive_LinkedNodes[Buffer_Receive_StartLinkedNodes[iVertex]];
 
       for (unsigned long jLinkedNode = 0; jLinkedNode < Buffer_Receive_nLinkedNodes[iVertex]; jLinkedNode++) {
         const auto jPoint = uptr[jLinkedNode];
diff --git a/Common/src/interface_interpolation/CInterpolatorFactory.cpp b/Common/src/interface_interpolation/CInterpolatorFactory.cpp
index 64b989981e5..be50f5075ce 100644
--- a/Common/src/interface_interpolation/CInterpolatorFactory.cpp
+++ b/Common/src/interface_interpolation/CInterpolatorFactory.cpp
@@ -34,11 +34,9 @@
 #include "../../include/interface_interpolation/CSlidingMesh.hpp"
 
 namespace CInterpolatorFactory {
-CInterpolator* CreateInterpolator(CGeometry ****geometry_container,
-                                  const CConfig* const* config,
-                                  const CInterpolator* transpInterpolator,
-                                  unsigned iZone, unsigned jZone, bool verbose) {
-
+CInterpolator* CreateInterpolator(CGeometry**** geometry_container, const CConfig* const* config,
+                                  const CInterpolator* transpInterpolator, unsigned iZone, unsigned jZone,
+                                  bool verbose) {
   CInterpolator* interpolator = nullptr;
 
   /*--- Only print information on master node. ---*/
@@ -57,30 +55,28 @@ CInterpolator* CreateInterpolator(CGeometry ****geometry_container,
   if (type == INTERFACE_INTERPOLATOR::WEIGHTED_AVERAGE) {
     if (verbose) cout << "using a sliding mesh approach." << endl;
     interpolator = new CSlidingMesh(geometry_container, config, iZone, jZone);
-  }
-  else if (config[jZone]->GetConservativeInterpolation()) {
+  } else if (config[jZone]->GetConservativeInterpolation()) {
     if (verbose) cout << "using the mirror approach, \"transposing\" coefficients from opposite mesh." << endl;
     interpolator = new CMirror(geometry_container, config, transpInterpolator, iZone, jZone);
-  }
-  else {
-    switch(type) {
-    case INTERFACE_INTERPOLATOR::ISOPARAMETRIC:
-      if (verbose) cout << "using the isoparametric approach." << endl;
-      interpolator = new CIsoparametric(geometry_container, config, iZone, jZone);
-      break;
+  } else {
+    switch (type) {
+      case INTERFACE_INTERPOLATOR::ISOPARAMETRIC:
+        if (verbose) cout << "using the isoparametric approach." << endl;
+        interpolator = new CIsoparametric(geometry_container, config, iZone, jZone);
+        break;
 
-    case INTERFACE_INTERPOLATOR::NEAREST_NEIGHBOR:
-      if (verbose) cout << "using a nearest neighbor approach." << endl;
-      interpolator = new CNearestNeighbor(geometry_container, config, iZone, jZone);
-      break;
+      case INTERFACE_INTERPOLATOR::NEAREST_NEIGHBOR:
+        if (verbose) cout << "using a nearest neighbor approach." << endl;
+        interpolator = new CNearestNeighbor(geometry_container, config, iZone, jZone);
+        break;
 
-    case INTERFACE_INTERPOLATOR::RADIAL_BASIS_FUNCTION:
-      if (verbose) cout << "using a radial basis function approach." << endl;
-      interpolator = new CRadialBasisFunction(geometry_container, config, iZone, jZone);
-      break;
+      case INTERFACE_INTERPOLATOR::RADIAL_BASIS_FUNCTION:
+        if (verbose) cout << "using a radial basis function approach." << endl;
+        interpolator = new CRadialBasisFunction(geometry_container, config, iZone, jZone);
+        break;
 
-    default:
-      SU2_MPI::Error("Unknown type of interpolation.", CURRENT_FUNCTION);
+      default:
+        SU2_MPI::Error("Unknown type of interpolation.", CURRENT_FUNCTION);
     }
   }
 
@@ -88,4 +84,4 @@ CInterpolator* CreateInterpolator(CGeometry ****geometry_container,
 
   return interpolator;
 }
-} // end namespace
+}  // namespace CInterpolatorFactory
diff --git a/Common/src/interface_interpolation/CIsoparametric.cpp b/Common/src/interface_interpolation/CIsoparametric.cpp
index e660664a891..f8ed1c6b588 100644
--- a/Common/src/interface_interpolation/CIsoparametric.cpp
+++ b/Common/src/interface_interpolation/CIsoparametric.cpp
@@ -34,9 +34,9 @@
 
 using namespace GeometryToolbox;
 
-CIsoparametric::CIsoparametric(CGeometry ****geometry_container, const CConfig* const* config,
-                               unsigned int iZone, unsigned int jZone) :
-  CInterpolator(geometry_container, config, iZone, jZone) {
+CIsoparametric::CIsoparametric(CGeometry**** geometry_container, const CConfig* const* config, unsigned int iZone,
+                               unsigned int jZone)
+    : CInterpolator(geometry_container, config, iZone, jZone) {
   SetTransferCoeff(config);
 }
 
@@ -47,27 +47,26 @@ void CIsoparametric::PrintStatistics(void) const {
 }
 
 void CIsoparametric::SetTransferCoeff(const CConfig* const* config) {
-
-  const su2double matchingVertexTol = 1e-12; // 1um^2
+  const su2double matchingVertexTol = 1e-12;  // 1um^2
 
   const int nProcessor = size;
-  const auto nMarkerInt = config[donorZone]->GetMarker_n_ZoneInterface()/2;
+  const auto nMarkerInt = config[donorZone]->GetMarker_n_ZoneInterface() / 2;
   const auto nDim = donor_geometry->GetnDim();
 
-  Buffer_Receive_nVertex_Donor = new unsigned long [nProcessor];
+  Buffer_Receive_nVertex_Donor = new unsigned long[nProcessor];
 
   /*--- Make space for donor info. ---*/
 
   targetVertices.resize(config[targetZone]->GetnMarker_All());
 
   /*--- Init stats. ---*/
-  MaxDistance = 0.0; ErrorCounter = 0;
+  MaxDistance = 0.0;
+  ErrorCounter = 0;
   unsigned long nGlobalVertexTarget = 0;
 
   /*--- Cycle over nMarkersInt interface to determine communication pattern. ---*/
 
   for (unsigned short iMarkerInt = 0; iMarkerInt < nMarkerInt; iMarkerInt++) {
-
     /* High level procedure:
      * - Loop through vertices of the target grid;
      * - Find nearest element;
@@ -90,12 +89,12 @@ void CIsoparametric::SetTransferCoeff(const CConfig* const* config) {
     /*--- Sets MaxLocalVertex_Donor, Buffer_Receive_nVertex_Donor. ---*/
     Determine_ArraySize(markDonor, markTarget, nVertexDonor, nDim);
 
-    const auto nGlobalVertexDonor = accumulate(Buffer_Receive_nVertex_Donor,
-                                    Buffer_Receive_nVertex_Donor+nProcessor, 0ul);
+    const auto nGlobalVertexDonor =
+        accumulate(Buffer_Receive_nVertex_Donor, Buffer_Receive_nVertex_Donor + nProcessor, 0ul);
 
     Buffer_Send_Coord.resize(MaxLocalVertex_Donor, nDim);
-    Buffer_Send_GlobalPoint .resize(MaxLocalVertex_Donor);
-    Buffer_Receive_Coord.resize(nProcessor*MaxLocalVertex_Donor,nDim);
+    Buffer_Send_GlobalPoint.resize(MaxLocalVertex_Donor);
+    Buffer_Receive_Coord.resize(nProcessor * MaxLocalVertex_Donor, nDim);
     Buffer_Receive_GlobalPoint.resize(nProcessor * MaxLocalVertex_Donor);
 
     /*--- Collect coordinates and global point indices. ---*/
@@ -114,9 +113,8 @@ void CIsoparametric::SetTransferCoeff(const CConfig* const* config) {
     for (int iProcessor = 0; iProcessor < nProcessor; ++iProcessor) {
       auto offset = iProcessor * MaxLocalVertex_Donor;
       for (auto iVertex = 0ul; iVertex < Buffer_Receive_nVertex_Donor[iProcessor]; ++iVertex) {
-        for (int iDim = 0; iDim < nDim; ++iDim)
-          donorCoord(iCount,iDim) = Buffer_Receive_Coord(offset+iVertex, iDim);
-        donorPoint[iCount] = Buffer_Receive_GlobalPoint[offset+iVertex];
+        for (int iDim = 0; iDim < nDim; ++iDim) donorCoord(iCount, iDim) = Buffer_Receive_Coord(offset + iVertex, iDim);
+        donorPoint[iCount] = Buffer_Receive_GlobalPoint[offset + iVertex];
         donorProc[iCount] = iProcessor;
         assert((globalToLocalMap.count(donorPoint[iCount]) == 0) && "Duplicate donor point found.");
         globalToLocalMap[donorPoint[iCount]] = iCount;
@@ -131,135 +129,132 @@ void CIsoparametric::SetTransferCoeff(const CConfig* const* config) {
     vector<unsigned short> elemNumNodes;
     su2matrix<long> elemIdxNodes;
 
-    const auto nGlobalElemDonor = Collect_ElementInfo(markDonor, nDim, true,
-                                    allNumElem, elemNumNodes, elemIdxNodes);
+    const auto nGlobalElemDonor = Collect_ElementInfo(markDonor, nDim, true, allNumElem, elemNumNodes, elemIdxNodes);
 
     /*--- Map the node to "local" indices and create a list of connected elements for each vertex. ---*/
 
     vector<vector<unsigned> > vertexElements(nGlobalVertexDonor);
 
     for (auto iElem = 0u; iElem < nGlobalElemDonor; ++iElem) {
-
       const auto nNode = elemNumNodes[iElem];
 
       for (auto iNode = 0u; iNode < nNode; ++iNode) {
-
-        assert(globalToLocalMap.count(elemIdxNodes(iElem,iNode)) &&
+        assert(globalToLocalMap.count(elemIdxNodes(iElem, iNode)) &&
                "Unknown donor point referenced by donor element.");
-        const auto iVertex = globalToLocalMap.at(elemIdxNodes(iElem,iNode));
-        elemIdxNodes(iElem,iNode) = iVertex;
+        const auto iVertex = globalToLocalMap.at(elemIdxNodes(iElem, iNode));
+        elemIdxNodes(iElem, iNode) = iVertex;
 
         vertexElements[iVertex].push_back(iElem);
       }
     }
 
     /*--- Compute transfer coefficients for each target point. ---*/
-    SU2_OMP_PARALLEL
-    {
-    su2double maxDist = 0.0;
-    unsigned long errorCount = 0, totalCount = 0;
-
-    SU2_OMP_FOR_DYN(roundUpDiv(nVertexTarget,2*omp_get_max_threads()))
-    for (auto iVertexTarget = 0u; iVertexTarget < nVertexTarget; ++iVertexTarget) {
-
-      auto& target_vertex = targetVertices[markTarget][iVertexTarget];
-      const auto iPoint = target_geometry->vertex[markTarget][iVertexTarget]->GetNode();
-
-      if (!target_geometry->nodes->GetDomain(iPoint)) continue;
-      totalCount += 1;
-
-      /*--- Coordinates of the target point. ---*/
-      const su2double* coord_i = target_geometry->nodes->GetCoord(iPoint);
-
-      /*--- Find the closest donor vertex. ---*/
-      su2double minDist = 1e9;
-      unsigned iClosestVertex = 0;
-      for (auto iVertexDonor = 0u; iVertexDonor < nGlobalVertexDonor; ++iVertexDonor) {
-        su2double d = SquaredDistance(nDim, coord_i, donorCoord[iVertexDonor]);
-        if (d < minDist) {
-          minDist = d;
-          iClosestVertex = iVertexDonor;
+    SU2_OMP_PARALLEL {
+      su2double maxDist = 0.0;
+      unsigned long errorCount = 0, totalCount = 0;
+
+      SU2_OMP_FOR_DYN(roundUpDiv(nVertexTarget, 2 * omp_get_max_threads()))
+      for (auto iVertexTarget = 0u; iVertexTarget < nVertexTarget; ++iVertexTarget) {
+        auto& target_vertex = targetVertices[markTarget][iVertexTarget];
+        const auto iPoint = target_geometry->vertex[markTarget][iVertexTarget]->GetNode();
+
+        if (!target_geometry->nodes->GetDomain(iPoint)) continue;
+        totalCount += 1;
+
+        /*--- Coordinates of the target point. ---*/
+        const su2double* coord_i = target_geometry->nodes->GetCoord(iPoint);
+
+        /*--- Find the closest donor vertex. ---*/
+        su2double minDist = 1e9;
+        unsigned iClosestVertex = 0;
+        for (auto iVertexDonor = 0u; iVertexDonor < nGlobalVertexDonor; ++iVertexDonor) {
+          su2double d = SquaredDistance(nDim, coord_i, donorCoord[iVertexDonor]);
+          if (d < minDist) {
+            minDist = d;
+            iClosestVertex = iVertexDonor;
+          }
         }
-      }
-
-      if (minDist < matchingVertexTol) {
-        /*--- Perfect match. ---*/
-        target_vertex.resize(1);
-        target_vertex.coefficient[0] = 1.0;
-        target_vertex.globalPoint[0] = donorPoint[iClosestVertex];
-        target_vertex.processor[0] = donorProc[iClosestVertex];
-        continue;
-      }
-
-      /*--- Evaluate interpolation for the elements connected to the closest vertex. ---*/
-      DonorInfo donor;
-      donor.error = 2;
-      donor.distance = 1e9;
-      for (auto iElem : vertexElements[iClosestVertex]) {
-        /*--- Fetch element info. ---*/
-        DonorInfo candidate;
-        candidate.iElem = iElem;
-        const auto nNode = elemNumNodes[iElem];
-        su2double coords[4][3] = {{0.0}};
 
-        for (auto iNode = 0u; iNode < nNode; ++iNode) {
-          const auto iVertex = elemIdxNodes(iElem, iNode);
-          for (auto iDim = 0u; iDim < nDim; ++iDim)
-            coords[iNode][iDim] = donorCoord(iVertex,iDim);
-        }
-
-        /*--- Compute the interpolation coefficients. ---*/
-        switch (nNode) {
-          case 2: candidate.error = LineIsoparameters(coords, coord_i, candidate.isoparams); break;
-          case 3: candidate.error = TriangleIsoparameters(coords, coord_i, candidate.isoparams); break;
-          case 4: candidate.error = QuadrilateralIsoparameters(coords, coord_i, candidate.isoparams); break;
+        if (minDist < matchingVertexTol) {
+          /*--- Perfect match. ---*/
+          target_vertex.resize(1);
+          target_vertex.coefficient[0] = 1.0;
+          target_vertex.globalPoint[0] = donorPoint[iClosestVertex];
+          target_vertex.processor[0] = donorProc[iClosestVertex];
+          continue;
         }
 
-        /*--- Evaluate distance from target to final mapped point. ---*/
-        su2double finalCoord[3] = {0.0};
-        for (auto iDim = 0u; iDim < nDim; ++iDim)
-          for (auto iNode = 0u; iNode < nNode; ++iNode)
-            finalCoord[iDim] += coords[iNode][iDim] * candidate.isoparams[iNode];
+        /*--- Evaluate interpolation for the elements connected to the closest vertex. ---*/
+        DonorInfo donor;
+        donor.error = 2;
+        donor.distance = 1e9;
+        for (auto iElem : vertexElements[iClosestVertex]) {
+          /*--- Fetch element info. ---*/
+          DonorInfo candidate;
+          candidate.iElem = iElem;
+          const auto nNode = elemNumNodes[iElem];
+          su2double coords[4][3] = {{0.0}};
+
+          for (auto iNode = 0u; iNode < nNode; ++iNode) {
+            const auto iVertex = elemIdxNodes(iElem, iNode);
+            for (auto iDim = 0u; iDim < nDim; ++iDim) coords[iNode][iDim] = donorCoord(iVertex, iDim);
+          }
+
+          /*--- Compute the interpolation coefficients. ---*/
+          switch (nNode) {
+            case 2:
+              candidate.error = LineIsoparameters(coords, coord_i, candidate.isoparams);
+              break;
+            case 3:
+              candidate.error = TriangleIsoparameters(coords, coord_i, candidate.isoparams);
+              break;
+            case 4:
+              candidate.error = QuadrilateralIsoparameters(coords, coord_i, candidate.isoparams);
+              break;
+          }
+
+          /*--- Evaluate distance from target to final mapped point. ---*/
+          su2double finalCoord[3] = {0.0};
+          for (auto iDim = 0u; iDim < nDim; ++iDim)
+            for (auto iNode = 0u; iNode < nNode; ++iNode)
+              finalCoord[iDim] += coords[iNode][iDim] * candidate.isoparams[iNode];
 
-        candidate.distance = Distance(nDim, coord_i, finalCoord);
+          candidate.distance = Distance(nDim, coord_i, finalCoord);
 
-        /*--- Detect a very bad candidate (NaN). ---*/
-        if (candidate.distance != candidate.distance) continue;
+          /*--- Detect a very bad candidate (NaN). ---*/
+          if (candidate.distance != candidate.distance) continue;
 
-        /*--- Check if the candidate is an improvement, update donor if so. ---*/
-        if (candidate < donor) donor = candidate;
-      }
+          /*--- Check if the candidate is an improvement, update donor if so. ---*/
+          if (candidate < donor) donor = candidate;
+        }
 
-      if (donor.error > 1)
-        SU2_MPI::Error("Isoparametric interpolation failed, NaN detected.", CURRENT_FUNCTION);
+        if (donor.error > 1) SU2_MPI::Error("Isoparametric interpolation failed, NaN detected.", CURRENT_FUNCTION);
 
-      errorCount += donor.error;
-      maxDist = max(maxDist, donor.distance);
+        errorCount += donor.error;
+        maxDist = max(maxDist, donor.distance);
 
-      const auto nNode = elemNumNodes[donor.iElem];
+        const auto nNode = elemNumNodes[donor.iElem];
 
-      target_vertex.resize(nNode);
+        target_vertex.resize(nNode);
 
-      for (auto iNode = 0u; iNode < nNode; ++iNode) {
-        const auto iVertex = elemIdxNodes(donor.iElem, iNode);
-        target_vertex.coefficient[iNode] = donor.isoparams[iNode];
-        target_vertex.globalPoint[iNode] = donorPoint[iVertex];
-        target_vertex.processor[iNode] = donorProc[iVertex];
+        for (auto iNode = 0u; iNode < nNode; ++iNode) {
+          const auto iVertex = elemIdxNodes(donor.iElem, iNode);
+          target_vertex.coefficient[iNode] = donor.isoparams[iNode];
+          target_vertex.globalPoint[iNode] = donorPoint[iVertex];
+          target_vertex.processor[iNode] = donorProc[iVertex];
+        }
       }
-
-    }
-    END_SU2_OMP_FOR
-    SU2_OMP_CRITICAL
-    {
-      MaxDistance = max(MaxDistance, maxDist);
-      ErrorCounter += errorCount;
-      nGlobalVertexTarget += totalCount;
-    }
-    END_SU2_OMP_CRITICAL
+      END_SU2_OMP_FOR
+      SU2_OMP_CRITICAL {
+        MaxDistance = max(MaxDistance, maxDist);
+        ErrorCounter += errorCount;
+        nGlobalVertexTarget += totalCount;
+      }
+      END_SU2_OMP_CRITICAL
     }
     END_SU2_OMP_PARALLEL
 
-  } // end nMarkerInt loop
+  }  // end nMarkerInt loop
 
   /*--- Final reduction of statistics. ---*/
   su2double tmp = MaxDistance;
@@ -268,18 +263,16 @@ void CIsoparametric::SetTransferCoeff(const CConfig* const* config) {
   SU2_MPI::Allreduce(&tmp1, &ErrorCounter, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
   SU2_MPI::Allreduce(&tmp2, &nGlobalVertexTarget, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
 
-  ErrorRate = 100*su2double(ErrorCounter) / nGlobalVertexTarget;
-
+  ErrorRate = 100 * su2double(ErrorCounter) / nGlobalVertexTarget;
 }
 
-int CIsoparametric::LineIsoparameters(const su2double X[][3], const su2double *xj, su2double *isoparams) {
-
+int CIsoparametric::LineIsoparameters(const su2double X[][3], const su2double* xj, su2double* isoparams) {
   /*--- Project the target point onto the line. ---*/
 
   su2double normal[2] = {0.0};
   LineNormal(X, normal);
   su2double xprj[2] = {0.0};
-  PointPlaneProjection<su2double,2>(xj, X[0], normal, xprj);
+  PointPlaneProjection<su2double, 2>(xj, X[0], normal, xprj);
 
   su2double l01 = Distance(2, X[0], X[1]);
   su2double l0j = Distance(2, X[0], xprj);
@@ -287,16 +280,15 @@ int CIsoparametric::LineIsoparameters(const su2double X[][3], const su2double *x
 
   /*--- Detect out of bounds point. ---*/
 
-  const int outOfBounds = (l0j+lj1) > (2*l01);
+  const int outOfBounds = (l0j + lj1) > (2 * l01);
 
-  isoparams[0] = max(-0.5, min(lj1/l01, 1.5));
+  isoparams[0] = max(-0.5, min(lj1 / l01, 1.5));
   isoparams[1] = 1.0 - isoparams[0];
 
   return outOfBounds;
 }
 
-int CIsoparametric::TriangleIsoparameters(const su2double X[][3], const su2double *xj, su2double *isoparams) {
-
+int CIsoparametric::TriangleIsoparameters(const su2double X[][3], const su2double* xj, su2double* isoparams) {
   /*--- The isoparameters are the solution to the determined system X^T * isoparams = xj.
    *    For which we solve the normal equations to avoid divisions by zero.
    *    This is consistent with the shape functions of the linear triangular element. ---*/
@@ -307,18 +299,15 @@ int CIsoparametric::TriangleIsoparameters(const su2double X[][3], const su2doubl
 
   su2double normal[3] = {0.0}, xproj[3] = {0.0};
   TriangleNormal(X, normal);
-  PointPlaneProjection<su2double,3>(xj, X[0], normal, xproj);
+  PointPlaneProjection<su2double, 3>(xj, X[0], normal, xproj);
 
-  su2double A[3][3] = {{0.0}}; // = X*X^T
+  su2double A[3][3] = {{0.0}};  // = X*X^T
   for (int i = 0; i < 3; ++i) {
-
     for (int j = 0; j < 3; ++j)
-      for (int k = 0; k < 3; ++k)
-        A[i][j] += X[i][k] * X[j][k];
+      for (int k = 0; k < 3; ++k) A[i][j] += X[i][k] * X[j][k];
 
-    isoparams[i] = 0.0; // use isoparams as rhs
-    for (int k = 0; k < 3; ++k)
-      isoparams[i] += X[i][k] * xproj[k];
+    isoparams[i] = 0.0;  // use isoparams as rhs
+    for (int k = 0; k < 3; ++k) isoparams[i] += X[i][k] * xproj[k];
   }
 
   /*--- Solve system by in-place Gaussian elimination without pivoting. ---*/
@@ -327,22 +316,18 @@ int CIsoparametric::TriangleIsoparameters(const su2double X[][3], const su2doubl
   for (int i = 1; i < 3; ++i) {
     for (int j = 0; j < i; ++j) {
       su2double w = A[i][j] / A[j][j];
-      for (int k = j; k < 3; ++k)
-        A[i][k] -= w * A[j][k];
+      for (int k = j; k < 3; ++k) A[i][k] -= w * A[j][k];
       isoparams[i] -= w * isoparams[j];
     }
   }
   /*--- Backwards substitution. ---*/
   for (int i = 2; i >= 0; --i) {
-    for (int j = i+1; j < 3; ++j)
-      isoparams[i] -= A[i][j] * isoparams[j];
+    for (int j = i + 1; j < 3; ++j) isoparams[i] -= A[i][j] * isoparams[j];
     isoparams[i] /= A[i][i];
   }
 
   /*--- Detect out of bounds point. ---*/
-  const int outOfBounds = (isoparams[0] < extrapTol) ||
-                          (isoparams[1] < extrapTol) ||
-                          (isoparams[2] < extrapTol);
+  const int outOfBounds = (isoparams[0] < extrapTol) || (isoparams[1] < extrapTol) || (isoparams[2] < extrapTol);
 
   /*--- Mitigation. ---*/
   if (outOfBounds) {
@@ -353,15 +338,13 @@ int CIsoparametric::TriangleIsoparameters(const su2double X[][3], const su2doubl
       sum += isoparams[i];
     }
     /*--- Enforce unit sum. ---*/
-    for (int i = 0; i < 3; ++i)
-      isoparams[i] /= sum;
+    for (int i = 0; i < 3; ++i) isoparams[i] /= sum;
   }
 
   return outOfBounds;
 }
 
-int CIsoparametric::QuadrilateralIsoparameters(const su2double X[][3], const su2double *xj, su2double *isoparams) {
-
+int CIsoparametric::QuadrilateralIsoparameters(const su2double X[][3], const su2double* xj, su2double* isoparams) {
   /*--- The isoparameters are the shape functions (Ni) evaluated at xj, for that we need
    *    the corresponding Xi and Eta, which are obtained by solving the overdetermined
    *    nonlinear system r = xj - X^T * Ni(Xi,Eta) = 0 via the modified Marquardt method.
@@ -380,14 +363,12 @@ int CIsoparametric::QuadrilateralIsoparameters(const su2double X[][3], const su2
   const bool wasActive = AD::BeginPassive();
 
   for (int iter = 0; iter < NITER; ++iter) {
-
     /*--- Evaluate the residual. ---*/
     su2double r[3] = {xj[0], xj[1], xj[2]};
     su2double Ni[4] = {0.0};
     CQUAD4::ShapeFunctions(Xi, Eta, Ni);
     for (int i = 0; i < 3; ++i)
-      for (int j = 0; j < 4; ++j)
-        r[i] -= X[j][i] * Ni[j];
+      for (int j = 0; j < 4; ++j) r[i] -= X[j][i] * Ni[j];
 
     /*--- Evaluate the residual Jacobian. ---*/
     su2double dNi[4][2] = {{0.0}};
@@ -396,30 +377,27 @@ int CIsoparametric::QuadrilateralIsoparameters(const su2double X[][3], const su2
     su2double jac[3][2] = {{0.0}};
     for (int i = 0; i < 3; ++i)
       for (int j = 0; j < 2; ++j)
-        for (int k = 0; k < 4; ++k)
-          jac[i][j] -= X[k][i] * dNi[k][j];
+        for (int k = 0; k < 4; ++k) jac[i][j] -= X[k][i] * dNi[k][j];
 
     /*--- Compute the correction (normal equations and Cramer's rule). ---*/
     su2double A[2][2] = {{0.0}}, b[2] = {0.0};
     for (int i = 0; i < 2; ++i) {
       for (int j = i; j < 2; ++j)
-        for (int k = 0; k < 3; ++k)
-          A[i][j] += jac[k][i] * jac[k][j];
+        for (int k = 0; k < 3; ++k) A[i][j] += jac[k][i] * jac[k][j];
 
-      A[i][i] *= (1.0+lambda);
+      A[i][i] *= (1.0 + lambda);
 
-      for (int k = 0; k < 3; ++k)
-        b[i] += jac[k][i] * r[k];
+      for (int k = 0; k < 3; ++k) b[i] += jac[k][i] * r[k];
     }
     A[1][0] = A[0][1];
 
-    su2double detA = 1.0 / (A[0][0]*A[1][1] - A[0][1]*A[1][0]);
-    su2double dXi = (b[0]*A[1][1] - b[1]*A[0][1]) * detA;
-    su2double dEta = (A[0][0]*b[1] - A[1][0]*b[0]) * detA;
+    su2double detA = 1.0 / (A[0][0] * A[1][1] - A[0][1] * A[1][0]);
+    su2double dXi = (b[0] * A[1][1] - b[1] * A[0][1]) * detA;
+    su2double dEta = (A[0][0] * b[1] - A[1][0] * b[0]) * detA;
     Xi -= dXi;
     Eta -= dEta;
 
-    eps = fabs(dXi)+fabs(dEta);
+    eps = fabs(dXi) + fabs(dEta);
     if (eps < tol) break;
   }
 
@@ -431,8 +409,7 @@ int CIsoparametric::QuadrilateralIsoparameters(const su2double X[][3], const su2
     /*--- Iteration diverged, hard fallback. ---*/
     Xi = Eta = 0.0;
     outOfBounds = 1;
-  }
-  else {
+  } else {
     /*--- Check bounds. ---*/
     outOfBounds = (fabs(Xi) > extrapTol) || (fabs(Eta) > extrapTol);
 
diff --git a/Common/src/interface_interpolation/CMirror.cpp b/Common/src/interface_interpolation/CMirror.cpp
index 9e1695635dc..c663af40763 100644
--- a/Common/src/interface_interpolation/CMirror.cpp
+++ b/Common/src/interface_interpolation/CMirror.cpp
@@ -30,21 +30,20 @@
 #include "../../include/geometry/CGeometry.hpp"
 #include "../../include/toolboxes/printing_toolbox.hpp"
 
-
-CMirror::CMirror(CGeometry ****geometry_container, const CConfig* const* config,
-                 const CInterpolator* interpolator, unsigned int iZone, unsigned int jZone) :
-  CInterpolator(geometry_container, config, iZone, jZone),
-  transpInterpolator(interpolator) {
+CMirror::CMirror(CGeometry**** geometry_container, const CConfig* const* config, const CInterpolator* interpolator,
+                 unsigned int iZone, unsigned int jZone)
+    : CInterpolator(geometry_container, config, iZone, jZone), transpInterpolator(interpolator) {
   using PrintingToolbox::to_string;
   if (jZone < iZone) {
     SU2_MPI::Error(string("The order of the zones does not allow conservative interpolation to be setup.\n"
-      "Swap zones ") + to_string(iZone) + string(" and ") + to_string(jZone) + string("."),CURRENT_FUNCTION);
+                          "Swap zones ") +
+                       to_string(iZone) + string(" and ") + to_string(jZone) + string("."),
+                   CURRENT_FUNCTION);
   }
   SetTransferCoeff(config);
 }
 
 void CMirror::SetTransferCoeff(const CConfig* const* config) {
-
   const int nProcessor = size;
 
   vector<unsigned long> allNumVertexTarget(nProcessor);
@@ -57,15 +56,14 @@ void CMirror::SetTransferCoeff(const CConfig* const* config) {
   targetVertices.resize(config[targetZone]->GetnMarker_All());
 
   /*--- Number of markers on the interface ---*/
-  const auto nMarkerInt = (config[targetZone]->GetMarker_n_ZoneInterface())/2;
+  const auto nMarkerInt = (config[targetZone]->GetMarker_n_ZoneInterface()) / 2;
 
   /*--- For the number of markers on the interface... ---*/
   for (unsigned short iMarkerInt = 0; iMarkerInt < nMarkerInt; iMarkerInt++) {
-
-   /* High level procedure:
-    * - Gather the interpolation matrix of the donor geometry;
-    * - Set the interpolation matrix of the target as the transpose.
-    */
+    /* High level procedure:
+     * - Gather the interpolation matrix of the donor geometry;
+     * - Set the interpolation matrix of the target as the transpose.
+     */
 
     /*--- On the donor side: find the tag of the boundary sharing the interface ---*/
     const auto markDonor = config[donorZone]->FindInterfaceMarker(iMarkerInt);
@@ -77,8 +75,8 @@ void CMirror::SetTransferCoeff(const CConfig* const* config) {
     if (!CheckInterfaceBoundary(markDonor, markTarget)) continue;
 
     unsigned long nVertexDonor = 0, nVertexTarget = 0;
-    if (markDonor != -1) nVertexDonor = donor_geometry->GetnVertex( markDonor );
-    if (markTarget != -1) nVertexTarget = target_geometry->GetnVertex( markTarget );
+    if (markDonor != -1) nVertexDonor = donor_geometry->GetnVertex(markDonor);
+    if (markTarget != -1) nVertexTarget = target_geometry->GetnVertex(markTarget);
 
     /*--- Count the number of donor nodes on the donor geometry. ---*/
     unsigned long nVertexDonorLocal = 0;
@@ -92,12 +90,12 @@ void CMirror::SetTransferCoeff(const CConfig* const* config) {
     }
 
     /*--- Communicate vertex and donor node counts. ---*/
-    SU2_MPI::Allgather(&nVertexTarget, 1, MPI_UNSIGNED_LONG,
-                       allNumVertexTarget.data(), 1, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
-    SU2_MPI::Allgather(&nVertexDonorLocal, 1, MPI_UNSIGNED_LONG,
-                       allNumVertexDonor.data(), 1, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
-    SU2_MPI::Allgather(&nNodeDonorLocal, 1, MPI_UNSIGNED_LONG,
-                       allNumNodeDonor.data(), 1, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
+    SU2_MPI::Allgather(&nVertexTarget, 1, MPI_UNSIGNED_LONG, allNumVertexTarget.data(), 1, MPI_UNSIGNED_LONG,
+                       SU2_MPI::GetComm());
+    SU2_MPI::Allgather(&nVertexDonorLocal, 1, MPI_UNSIGNED_LONG, allNumVertexDonor.data(), 1, MPI_UNSIGNED_LONG,
+                       SU2_MPI::GetComm());
+    SU2_MPI::Allgather(&nNodeDonorLocal, 1, MPI_UNSIGNED_LONG, allNumNodeDonor.data(), 1, MPI_UNSIGNED_LONG,
+                       SU2_MPI::GetComm());
 
     /*--- Copy donor interpolation matrix (triplet format). ---*/
     vector<long> sendGlobalIndex(nNodeDonorLocal);
@@ -105,7 +103,6 @@ void CMirror::SetTransferCoeff(const CConfig* const* config) {
     vector<su2double> sendDonorCoeff(nNodeDonorLocal);
 
     for (auto iVertex = 0ul, iDonor = 0ul; iVertex < nVertexDonor; ++iVertex) {
-
       auto& donor_vertex = donorVertices[markDonor][iVertex];
       const auto iPoint = donor_geometry->vertex[markDonor][iVertex]->GetNode();
 
@@ -125,11 +122,7 @@ void CMirror::SetTransferCoeff(const CConfig* const* config) {
     /*--- Sort the matrix by donor index, effectively transposing the triplets. ---*/
     vector<int> order(nNodeDonorLocal);
     iota(order.begin(), order.end(), 0);
-    sort(order.begin(), order.end(),
-      [&sendDonorIndex](int i, int j) {
-         return sendDonorIndex[i] < sendDonorIndex[j];
-      }
-    );
+    sort(order.begin(), order.end(), [&sendDonorIndex](int i, int j) { return sendDonorIndex[i] < sendDonorIndex[j]; });
     for (int i = 0; i < int(nNodeDonorLocal); ++i) {
       int j = order[i];
       while (j < i) j = order[j];
@@ -138,7 +131,7 @@ void CMirror::SetTransferCoeff(const CConfig* const* config) {
       swap(sendDonorIndex[i], sendDonorIndex[j]);
       swap(sendDonorCoeff[i], sendDonorCoeff[j]);
     }
-    vector<int>().swap(order); // no longer needed
+    vector<int>().swap(order);  // no longer needed
 
     /*--- Communicate donor interpolation matrix and info. We only gather the
      *    matrix in ranks that need it, i.e. have target vertices, to avoid
@@ -147,13 +140,12 @@ void CMirror::SetTransferCoeff(const CConfig* const* config) {
 
     vector<int> iSendProcessor;
     for (int iProcessor = 0; iProcessor < nProcessor; ++iProcessor)
-      if (allNumVertexDonor[iProcessor] != 0)
-        iSendProcessor.push_back(iProcessor);
+      if (allNumVertexDonor[iProcessor] != 0) iSendProcessor.push_back(iProcessor);
 
     const int nSend = iSendProcessor.size();
 
-    vector<long*> GlobalIndex(nSend,nullptr), DonorIndex(nSend,nullptr);
-    vector<su2double*> DonorCoeff(nSend,nullptr);
+    vector<long*> GlobalIndex(nSend, nullptr), DonorIndex(nSend, nullptr);
+    vector<su2double*> DonorCoeff(nSend, nullptr);
 
     /*--- For each "target processor" that needs the interpolation matrix. ---*/
     for (int iProcessor = 0; iProcessor < nProcessor; ++iProcessor) {
@@ -169,20 +161,18 @@ void CMirror::SetTransferCoeff(const CConfig* const* config) {
           GlobalIndex[iSend] = sendGlobalIndex.data();
           DonorIndex[iSend] = sendDonorIndex.data();
           DonorCoeff[iSend] = sendDonorCoeff.data();
-        }
-        else if (rank == iProcessor) {
+        } else if (rank == iProcessor) {
           /*--- "I'm" the target, allocate and receive. ---*/
-          GlobalIndex[iSend] = new long [numCoeff];
-          DonorIndex[iSend] = new long [numCoeff];
-          DonorCoeff[iSend] = new su2double [numCoeff];
+          GlobalIndex[iSend] = new long[numCoeff];
+          DonorIndex[iSend] = new long[numCoeff];
+          DonorCoeff[iSend] = new su2double[numCoeff];
           SU2_MPI::Recv(GlobalIndex[iSend], numCoeff, MPI_LONG, jProcessor, 0, SU2_MPI::GetComm(), MPI_STATUS_IGNORE);
-          SU2_MPI::Recv(DonorIndex[iSend],  numCoeff, MPI_LONG, jProcessor, 0, SU2_MPI::GetComm(), MPI_STATUS_IGNORE);
+          SU2_MPI::Recv(DonorIndex[iSend], numCoeff, MPI_LONG, jProcessor, 0, SU2_MPI::GetComm(), MPI_STATUS_IGNORE);
           SU2_MPI::Recv(DonorCoeff[iSend], numCoeff, MPI_DOUBLE, jProcessor, 0, SU2_MPI::GetComm(), MPI_STATUS_IGNORE);
-        }
-        else if (rank == jProcessor) {
+        } else if (rank == jProcessor) {
           /*--- "I'm" the donor, send. ---*/
           SU2_MPI::Send(sendGlobalIndex.data(), numCoeff, MPI_LONG, iProcessor, 0, SU2_MPI::GetComm());
-          SU2_MPI::Send(sendDonorIndex.data(),  numCoeff, MPI_LONG, iProcessor, 0, SU2_MPI::GetComm());
+          SU2_MPI::Send(sendDonorIndex.data(), numCoeff, MPI_LONG, iProcessor, 0, SU2_MPI::GetComm());
           SU2_MPI::Send(sendDonorCoeff.data(), numCoeff, MPI_DOUBLE, iProcessor, 0, SU2_MPI::GetComm());
         }
       }
@@ -192,11 +182,9 @@ void CMirror::SetTransferCoeff(const CConfig* const* config) {
 
     /*--- Loop over the vertices on the target marker, define one row of the transpose matrix. ---*/
 
-    SU2_OMP_PARALLEL
-    {
-      SU2_OMP_FOR_DYN(roundUpDiv(nVertexTarget, 2*omp_get_max_threads()))
+    SU2_OMP_PARALLEL {
+      SU2_OMP_FOR_DYN(roundUpDiv(nVertexTarget, 2 * omp_get_max_threads()))
       for (auto iVertex = 0ul; iVertex < nVertexTarget; ++iVertex) {
-
         auto& target_vertex = targetVertices[markTarget][iVertex];
         const auto iPoint = target_geometry->vertex[markTarget][iVertex]->GetNode();
 
@@ -207,11 +195,11 @@ void CMirror::SetTransferCoeff(const CConfig* const* config) {
 
         /*--- Count donors and safe the binary search results (this is why we sorted the matrix). ---*/
         auto nDonor = 0ul;
-        vector<pair<long*,long*> > ranges(nSend);
+        vector<pair<long*, long*> > ranges(nSend);
         for (int iSend = 0; iSend < nSend; ++iSend) {
           const auto iProcessor = iSendProcessor[iSend];
           const auto numCoeff = allNumNodeDonor[iProcessor];
-          auto p = equal_range(DonorIndex[iSend], DonorIndex[iSend]+numCoeff, targetGlobalIndex);
+          auto p = equal_range(DonorIndex[iSend], DonorIndex[iSend] + numCoeff, targetGlobalIndex);
           nDonor += (p.second - p.first);
           ranges[iSend] = p;
         }
@@ -238,10 +226,12 @@ void CMirror::SetTransferCoeff(const CConfig* const* config) {
     END_SU2_OMP_PARALLEL
 
     /*--- Free the heap allocations. ---*/
-    for (auto ptr : GlobalIndex) if (ptr != sendGlobalIndex.data()) delete [] ptr;
-    for (auto ptr : DonorIndex) if (ptr != sendDonorIndex.data()) delete [] ptr;
-    for (auto ptr : DonorCoeff) if (ptr != sendDonorCoeff.data()) delete [] ptr;
-
-  } // end marker loop
-
+    for (auto ptr : GlobalIndex)
+      if (ptr != sendGlobalIndex.data()) delete[] ptr;
+    for (auto ptr : DonorIndex)
+      if (ptr != sendDonorIndex.data()) delete[] ptr;
+    for (auto ptr : DonorCoeff)
+      if (ptr != sendDonorCoeff.data()) delete[] ptr;
+
+  }  // end marker loop
 }
diff --git a/Common/src/interface_interpolation/CNearestNeighbor.cpp b/Common/src/interface_interpolation/CNearestNeighbor.cpp
index 8518b4a19dc..1fba622ef70 100644
--- a/Common/src/interface_interpolation/CNearestNeighbor.cpp
+++ b/Common/src/interface_interpolation/CNearestNeighbor.cpp
@@ -30,9 +30,9 @@
 #include "../../include/geometry/CGeometry.hpp"
 #include "../../include/toolboxes/geometry_toolbox.hpp"
 
-CNearestNeighbor::CNearestNeighbor(CGeometry ****geometry_container, const CConfig* const* config,
-                                   unsigned int iZone, unsigned int jZone) :
-  CInterpolator(geometry_container, config, iZone, jZone) {
+CNearestNeighbor::CNearestNeighbor(CGeometry**** geometry_container, const CConfig* const* config, unsigned int iZone,
+                                   unsigned int jZone)
+    : CInterpolator(geometry_container, config, iZone, jZone) {
   SetTransferCoeff(config);
 }
 
@@ -42,7 +42,6 @@ void CNearestNeighbor::PrintStatistics() const {
 }
 
 void CNearestNeighbor::SetTransferCoeff(const CConfig* const* config) {
-
   /*--- Desired number of donor points. ---*/
   const auto nDonor = max<unsigned long>(config[donorZone]->GetNumNearestNeighbors(), 1);
 
@@ -50,10 +49,10 @@ void CNearestNeighbor::SetTransferCoeff(const CConfig* const* config) {
   const su2double eps = numeric_limits<passivedouble>::epsilon();
 
   const int nProcessor = size;
-  const auto nMarkerInt = config[donorZone]->GetMarker_n_ZoneInterface()/2;
+  const auto nMarkerInt = config[donorZone]->GetMarker_n_ZoneInterface() / 2;
   const auto nDim = donor_geometry->GetnDim();
 
-  Buffer_Receive_nVertex_Donor = new unsigned long [nProcessor];
+  Buffer_Receive_nVertex_Donor = new unsigned long[nProcessor];
 
   targetVertices.resize(config[targetZone]->GetnMarker_All());
 
@@ -65,7 +64,6 @@ void CNearestNeighbor::SetTransferCoeff(const CConfig* const* config) {
   unsigned long totalTargetPoints = 0;
 
   for (unsigned short iMarkerInt = 0; iMarkerInt < nMarkerInt; iMarkerInt++) {
-
     /*--- On the donor side: find the tag of the boundary sharing the interface. ---*/
     const auto markDonor = config[donorZone]->FindInterfaceMarker(iMarkerInt);
 
@@ -83,8 +81,8 @@ void CNearestNeighbor::SetTransferCoeff(const CConfig* const* config) {
     Determine_ArraySize(markDonor, markTarget, nVertexDonor, nDim);
     if (nVertexTarget) targetVertices[markTarget].resize(nVertexTarget);
 
-    const auto nPossibleDonor = accumulate(Buffer_Receive_nVertex_Donor,
-                                Buffer_Receive_nVertex_Donor+nProcessor, 0ul);
+    const auto nPossibleDonor =
+        accumulate(Buffer_Receive_nVertex_Donor, Buffer_Receive_nVertex_Donor + nProcessor, 0ul);
 
     Buffer_Send_Coord.resize(MaxLocalVertex_Donor, nDim);
     Buffer_Send_GlobalPoint.resize(MaxLocalVertex_Donor);
@@ -95,80 +93,74 @@ void CNearestNeighbor::SetTransferCoeff(const CConfig* const* config) {
     Collect_VertexInfo(markDonor, markTarget, nVertexDonor, nDim);
 
     /*--- Find the closest donor points to each target. ---*/
-    SU2_OMP_PARALLEL
-    {
-    /*--- Working array for this thread. ---*/
-    auto& donorInfo = DonorInfoVec[omp_get_thread_num()];
-    donorInfo.resize(nPossibleDonor);
-
-    su2double avgDist = 0.0, maxDist = 0.0;
-    unsigned long numTarget = 0;
-
-    SU2_OMP_FOR_DYN(roundUpDiv(nVertexTarget,2*omp_get_max_threads()))
-    for (auto iVertexTarget = 0ul; iVertexTarget < nVertexTarget; iVertexTarget++) {
-
-      auto& target_vertex = targetVertices[markTarget][iVertexTarget];
-      const auto Point_Target = target_geometry->vertex[markTarget][iVertexTarget]->GetNode();
-
-      if (!target_geometry->nodes->GetDomain(Point_Target)) continue;
-
-      /*--- Coordinates of the target point. ---*/
-      const su2double* Coord_i = target_geometry->nodes->GetCoord(Point_Target);
-
-      /*--- Compute all distances. ---*/
-      for (int iProcessor = 0, iDonor = 0; iProcessor < nProcessor; ++iProcessor) {
-        for (auto jVertex = 0ul; jVertex < Buffer_Receive_nVertex_Donor[iProcessor]; ++jVertex) {
-
-          const auto idx = iProcessor*MaxLocalVertex_Donor + jVertex;
-          const auto pGlobalPoint = Buffer_Receive_GlobalPoint[idx];
-          const su2double* Coord_j = Buffer_Receive_Coord[idx];
-          const auto dist2 = GeometryToolbox::SquaredDistance(nDim, Coord_i, Coord_j);
-
-          donorInfo[iDonor++] = DonorInfo(dist2, pGlobalPoint, iProcessor);
+    SU2_OMP_PARALLEL {
+      /*--- Working array for this thread. ---*/
+      auto& donorInfo = DonorInfoVec[omp_get_thread_num()];
+      donorInfo.resize(nPossibleDonor);
+
+      su2double avgDist = 0.0, maxDist = 0.0;
+      unsigned long numTarget = 0;
+
+      SU2_OMP_FOR_DYN(roundUpDiv(nVertexTarget, 2 * omp_get_max_threads()))
+      for (auto iVertexTarget = 0ul; iVertexTarget < nVertexTarget; iVertexTarget++) {
+        auto& target_vertex = targetVertices[markTarget][iVertexTarget];
+        const auto Point_Target = target_geometry->vertex[markTarget][iVertexTarget]->GetNode();
+
+        if (!target_geometry->nodes->GetDomain(Point_Target)) continue;
+
+        /*--- Coordinates of the target point. ---*/
+        const su2double* Coord_i = target_geometry->nodes->GetCoord(Point_Target);
+
+        /*--- Compute all distances. ---*/
+        for (int iProcessor = 0, iDonor = 0; iProcessor < nProcessor; ++iProcessor) {
+          for (auto jVertex = 0ul; jVertex < Buffer_Receive_nVertex_Donor[iProcessor]; ++jVertex) {
+            const auto idx = iProcessor * MaxLocalVertex_Donor + jVertex;
+            const auto pGlobalPoint = Buffer_Receive_GlobalPoint[idx];
+            const su2double* Coord_j = Buffer_Receive_Coord[idx];
+            const auto dist2 = GeometryToolbox::SquaredDistance(nDim, Coord_i, Coord_j);
+
+            donorInfo[iDonor++] = DonorInfo(dist2, pGlobalPoint, iProcessor);
+          }
         }
-      }
 
-      /*--- Find k closest points. ---*/
-      partial_sort(donorInfo.begin(), donorInfo.begin()+nDonor, donorInfo.end(),
-        [](const DonorInfo& a, const DonorInfo& b) {
-          /*--- Global index is used as tie-breaker to make sorted order independent of initial. ---*/
-          return (a.dist != b.dist)? (a.dist < b.dist) : (a.pidx < b.pidx);
+        /*--- Find k closest points. ---*/
+        partial_sort(donorInfo.begin(), donorInfo.begin() + nDonor, donorInfo.end(),
+                     [](const DonorInfo& a, const DonorInfo& b) {
+                       /*--- Global index is used as tie-breaker to make sorted order independent of initial. ---*/
+                       return (a.dist != b.dist) ? (a.dist < b.dist) : (a.pidx < b.pidx);
+                     });
+
+        /*--- Update stats. ---*/
+        numTarget += 1;
+        su2double d = sqrt(donorInfo[0].dist);
+        avgDist += d;
+        maxDist = max(maxDist, d);
+
+        /*--- Compute interpolation numerators and denominator. ---*/
+        su2double denom = 0.0;
+        for (auto iDonor = 0ul; iDonor < nDonor; ++iDonor) {
+          donorInfo[iDonor].dist = 1.0 / (donorInfo[iDonor].dist + eps);
+          denom += donorInfo[iDonor].dist;
         }
-      );
-
-      /*--- Update stats. ---*/
-      numTarget += 1;
-      su2double d = sqrt(donorInfo[0].dist);
-      avgDist += d;
-      maxDist = max(maxDist, d);
-
-      /*--- Compute interpolation numerators and denominator. ---*/
-      su2double denom = 0.0;
-      for (auto iDonor = 0ul; iDonor < nDonor; ++iDonor) {
-        donorInfo[iDonor].dist = 1.0 / (donorInfo[iDonor].dist + eps);
-        denom += donorInfo[iDonor].dist;
-      }
 
-      /*--- Set interpolation coefficients. ---*/
-      target_vertex.resize(nDonor);
+        /*--- Set interpolation coefficients. ---*/
+        target_vertex.resize(nDonor);
 
-      for (auto iDonor = 0ul; iDonor < nDonor; ++iDonor) {
-        target_vertex.globalPoint[iDonor] = donorInfo[iDonor].pidx;
-        target_vertex.processor[iDonor] = donorInfo[iDonor].proc;
-        target_vertex.coefficient[iDonor] = donorInfo[iDonor].dist/denom;
+        for (auto iDonor = 0ul; iDonor < nDonor; ++iDonor) {
+          target_vertex.globalPoint[iDonor] = donorInfo[iDonor].pidx;
+          target_vertex.processor[iDonor] = donorInfo[iDonor].proc;
+          target_vertex.coefficient[iDonor] = donorInfo[iDonor].dist / denom;
+        }
       }
-    }
-    END_SU2_OMP_FOR
-    SU2_OMP_CRITICAL
-    {
-      totalTargetPoints += numTarget;
-      AvgDistance += avgDist;
-      MaxDistance = max(MaxDistance, maxDist);
-    }
-    END_SU2_OMP_CRITICAL
+      END_SU2_OMP_FOR
+      SU2_OMP_CRITICAL {
+        totalTargetPoints += numTarget;
+        AvgDistance += avgDist;
+        MaxDistance = max(MaxDistance, maxDist);
+      }
+      END_SU2_OMP_CRITICAL
     }
     END_SU2_OMP_PARALLEL
-
   }
 
   delete[] Buffer_Receive_nVertex_Donor;
@@ -179,5 +171,4 @@ void CNearestNeighbor::SetTransferCoeff(const CConfig* const* config) {
   SU2_MPI::Allreduce(&tmp1, &AvgDistance, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
   SU2_MPI::Allreduce(&tmp2, &MaxDistance, 1, MPI_DOUBLE, MPI_MAX, SU2_MPI::GetComm());
   AvgDistance /= totalTargetPoints;
-
 }
diff --git a/Common/src/interface_interpolation/CRadialBasisFunction.cpp b/Common/src/interface_interpolation/CRadialBasisFunction.cpp
index 7433a401299..424c227b745 100644
--- a/Common/src/interface_interpolation/CRadialBasisFunction.cpp
+++ b/Common/src/interface_interpolation/CRadialBasisFunction.cpp
@@ -38,56 +38,60 @@
 #endif
 #elif defined(HAVE_LAPACK)
 // dgemm(opA, opB, m, n, k, alpha, A, lda, B, ldb, beta, C, ldc)
-extern "C" void dgemm_(const char*, const char*, const int*, const int*, const int*,
-  const passivedouble*, const passivedouble*, const int*, const passivedouble*,
-  const int*, const passivedouble*, passivedouble*, const int*);
+extern "C" void dgemm_(const char*, const char*, const int*, const int*, const int*, const passivedouble*,
+                       const passivedouble*, const int*, const passivedouble*, const int*, const passivedouble*,
+                       passivedouble*, const int*);
 #define DGEMM dgemm_
 #endif
 
-
-CRadialBasisFunction::CRadialBasisFunction(CGeometry ****geometry_container, const CConfig* const* config,
-                                           unsigned int iZone, unsigned int jZone) :
-  CInterpolator(geometry_container, config, iZone, jZone) {
+CRadialBasisFunction::CRadialBasisFunction(CGeometry**** geometry_container, const CConfig* const* config,
+                                           unsigned int iZone, unsigned int jZone)
+    : CInterpolator(geometry_container, config, iZone, jZone) {
   SetTransferCoeff(config);
 }
 
 void CRadialBasisFunction::PrintStatistics() const {
   if (rank != MASTER_NODE) return;
   cout.precision(3);
-  cout << "  Min/avg/max number of RBF donors per target point: "
-       << MinDonors << "/" << AvgDonors << "/" << MaxDonors << "\n"
+  cout << "  Min/avg/max number of RBF donors per target point: " << MinDonors << "/" << AvgDonors << "/" << MaxDonors
+       << "\n"
        << "  Avg/max correction factor after pruning: " << AvgCorrection << "/" << MaxCorrection;
-  if (MaxCorrection < 1.1 || AvgCorrection < 1.02) cout << " (ok)\n";
-  else if (MaxCorrection < 2.0 && AvgCorrection < 1.05) cout << " (warning)\n";
-  else cout << " <<< WARNING >>>\n";
+  if (MaxCorrection < 1.1 || AvgCorrection < 1.02)
+    cout << " (ok)\n";
+  else if (MaxCorrection < 2.0 && AvgCorrection < 1.05)
+    cout << " (warning)\n";
+  else
+    cout << " <<< WARNING >>>\n";
   cout << "  Interpolation matrix is " << Density << "% dense." << endl;
   cout.unsetf(ios::floatfield);
 }
 
-su2double CRadialBasisFunction::Get_RadialBasisValue(RADIAL_BASIS type, const su2double radius, const su2double dist)
-{
-  su2double rbf = dist/radius;
+su2double CRadialBasisFunction::Get_RadialBasisValue(RADIAL_BASIS type, const su2double radius, const su2double dist) {
+  su2double rbf = dist / radius;
 
   switch (type) {
-
     case RADIAL_BASIS::WENDLAND_C2:
-      if(rbf < 1) rbf = pow(pow((1-rbf),2),2)*(4*rbf+1); // double use of pow(x,2) for optimization
-      else        rbf = 0.0;
+      if (rbf < 1)
+        rbf = pow(pow((1 - rbf), 2), 2) * (4 * rbf + 1);  // double use of pow(x,2) for optimization
+      else
+        rbf = 0.0;
       break;
 
     case RADIAL_BASIS::GAUSSIAN:
-      rbf = exp(-rbf*rbf);
+      rbf = exp(-rbf * rbf);
       break;
 
     case RADIAL_BASIS::THIN_PLATE_SPLINE:
-      if(rbf < numeric_limits<float>::min()) rbf = 0.0;
-      else rbf *= rbf*log(rbf);
+      if (rbf < numeric_limits<float>::min())
+        rbf = 0.0;
+      else
+        rbf *= rbf * log(rbf);
       break;
 
     case RADIAL_BASIS::MULTI_QUADRIC:
     case RADIAL_BASIS::INV_MULTI_QUADRIC:
-      rbf = sqrt(1.0+rbf*rbf);
-      if(type == RADIAL_BASIS::INV_MULTI_QUADRIC) rbf = 1.0/rbf;
+      rbf = sqrt(1.0 + rbf * rbf);
+      if (type == RADIAL_BASIS::INV_MULTI_QUADRIC) rbf = 1.0 / rbf;
       break;
   }
 
@@ -95,18 +99,17 @@ su2double CRadialBasisFunction::Get_RadialBasisValue(RADIAL_BASIS type, const su
 }
 
 void CRadialBasisFunction::SetTransferCoeff(const CConfig* const* config) {
-
   /*--- RBF options. ---*/
   const auto kindRBF = config[donorZone]->GetKindRadialBasisFunction();
   const bool usePolynomial = config[donorZone]->GetRadialBasisFunctionPolynomialOption();
   const su2double paramRBF = config[donorZone]->GetRadialBasisFunctionParameter();
   const su2double pruneTol = config[donorZone]->GetRadialBasisFunctionPruneTol();
 
-  const auto nMarkerInt = config[donorZone]->GetMarker_n_ZoneInterface()/2;
+  const auto nMarkerInt = config[donorZone]->GetMarker_n_ZoneInterface() / 2;
   const int nDim = donor_geometry->GetnDim();
 
   const int nProcessor = size;
-  Buffer_Receive_nVertex_Donor = new unsigned long [nProcessor];
+  Buffer_Receive_nVertex_Donor = new unsigned long[nProcessor];
 
   targetVertices.resize(config[targetZone]->GetnMarker_All());
 
@@ -118,11 +121,10 @@ void CRadialBasisFunction::SetTransferCoeff(const CConfig* const* config) {
   vector<su2activematrix> donorCoordinates(nMarkerInt);
   vector<vector<long> > donorGlobalPoint(nMarkerInt);
   vector<vector<int> > donorProcessor(nMarkerInt);
-  vector<int> assignedProcessor(nMarkerInt,-1);
-  vector<unsigned long> totalWork(nProcessor,0);
+  vector<int> assignedProcessor(nMarkerInt, -1);
+  vector<unsigned long> totalWork(nProcessor, 0);
 
   for (unsigned short iMarkerInt = 0; iMarkerInt < nMarkerInt; ++iMarkerInt) {
-
     /*--- On the donor side: find the tag of the boundary sharing the interface. ---*/
     const auto markDonor = config[donorZone]->FindInterfaceMarker(iMarkerInt);
 
@@ -130,7 +132,7 @@ void CRadialBasisFunction::SetTransferCoeff(const CConfig* const* config) {
     const auto markTarget = config[targetZone]->FindInterfaceMarker(iMarkerInt);
 
     /*--- If the zone does not contain the interface continue to the next pair of markers. ---*/
-    if (!CheckInterfaceBoundary(markDonor,markTarget)) continue;
+    if (!CheckInterfaceBoundary(markDonor, markTarget)) continue;
 
     unsigned long nVertexDonor = 0;
     if (markDonor != -1) nVertexDonor = donor_geometry->GetnVertex(markDonor);
@@ -139,8 +141,8 @@ void CRadialBasisFunction::SetTransferCoeff(const CConfig* const* config) {
     Determine_ArraySize(markDonor, markTarget, nVertexDonor, nDim);
 
     /*--- Compute total number of donor vertices. ---*/
-    const auto nGlobalVertexDonor = accumulate(Buffer_Receive_nVertex_Donor,
-                                    Buffer_Receive_nVertex_Donor+nProcessor, 0ul);
+    const auto nGlobalVertexDonor =
+        accumulate(Buffer_Receive_nVertex_Donor, Buffer_Receive_nVertex_Donor + nProcessor, 0ul);
 
     /*--- Gather coordinates and global point indices. ---*/
     Buffer_Send_Coord.resize(MaxLocalVertex_Donor, nDim);
@@ -162,9 +164,8 @@ void CRadialBasisFunction::SetTransferCoeff(const CConfig* const* config) {
     for (int iProcessor = 0; iProcessor < nProcessor; ++iProcessor) {
       auto offset = iProcessor * MaxLocalVertex_Donor;
       for (auto iVertex = 0ul; iVertex < Buffer_Receive_nVertex_Donor[iProcessor]; ++iVertex) {
-        for (int iDim = 0; iDim < nDim; ++iDim)
-          donorCoord(iCount,iDim) = Buffer_Receive_Coord(offset+iVertex, iDim);
-        donorPoint[iCount] = Buffer_Receive_GlobalPoint[offset+iVertex];
+        for (int iDim = 0; iDim < nDim; ++iDim) donorCoord(iCount, iDim) = Buffer_Receive_Coord(offset + iVertex, iDim);
+        donorPoint[iCount] = Buffer_Receive_GlobalPoint[offset + iVertex];
         donorProc[iCount] = iProcessor;
         ++iCount;
       }
@@ -175,7 +176,7 @@ void CRadialBasisFunction::SetTransferCoeff(const CConfig* const* config) {
      *    number of the RBF matrix, avoids diff results with diff number of ranks. ---*/
     vector<int> order(nGlobalVertexDonor);
     iota(order.begin(), order.end(), 0);
-    sort(order.begin(), order.end(), [&donorPoint](int i, int j){return donorPoint[i] < donorPoint[j];});
+    sort(order.begin(), order.end(), [&donorPoint](int i, int j) { return donorPoint[i] < donorPoint[j]; });
 
     for (int i = 0; i < int(nGlobalVertexDonor); ++i) {
       int j = order[i];
@@ -183,8 +184,7 @@ void CRadialBasisFunction::SetTransferCoeff(const CConfig* const* config) {
       if (i == j) continue;
       swap(donorProc[i], donorProc[j]);
       swap(donorPoint[i], donorPoint[j]);
-      for (int iDim = 0; iDim < nDim; ++iDim)
-        swap(donorCoord(i,iDim), donorCoord(j,iDim));
+      for (int iDim = 0; iDim < nDim; ++iDim) swap(donorCoord(i, iDim), donorCoord(j, iDim));
     }
 
     /*--- Static work scheduling over ranks based on which one has less work currently. ---*/
@@ -192,24 +192,22 @@ void CRadialBasisFunction::SetTransferCoeff(const CConfig* const* config) {
     for (int i = 1; i < nProcessor; ++i)
       if (totalWork[i] < totalWork[iProcessor]) iProcessor = i;
 
-    totalWork[iProcessor] += pow(nGlobalVertexDonor,3); // based on matrix inversion.
+    totalWork[iProcessor] += pow(nGlobalVertexDonor, 3);  // based on matrix inversion.
 
     assignedProcessor[iMarkerInt] = iProcessor;
-
   }
   delete[] Buffer_Receive_nVertex_Donor;
 
   /*--- Compute the interpolation matrices for each patch of coordinates
    *    assigned to the rank. Subdivide work further by threads. ---*/
-  vector<int> nPolynomialVec(nMarkerInt,-1);
-  vector<vector<int> > keepPolynomialRowVec(nMarkerInt, vector<int>(nDim,1));
+  vector<int> nPolynomialVec(nMarkerInt, -1);
+  vector<vector<int> > keepPolynomialRowVec(nMarkerInt, vector<int>(nDim, 1));
   vector<su2passivematrix> CinvTrucVec(nMarkerInt);
 
   SU2_OMP_PARALLEL_(for schedule(dynamic,1))
   for (unsigned short iMarkerInt = 0; iMarkerInt < nMarkerInt; ++iMarkerInt) {
     if (rank == assignedProcessor[iMarkerInt]) {
-      ComputeGeneratorMatrix(kindRBF, usePolynomial, paramRBF,
-                             donorCoordinates[iMarkerInt], nPolynomialVec[iMarkerInt],
+      ComputeGeneratorMatrix(kindRBF, usePolynomial, paramRBF, donorCoordinates[iMarkerInt], nPolynomialVec[iMarkerInt],
                              keepPolynomialRowVec[iMarkerInt], CinvTrucVec[iMarkerInt]);
     }
   }
@@ -219,10 +217,12 @@ void CRadialBasisFunction::SetTransferCoeff(const CConfig* const* config) {
 
   /*--- Initialize variables for interpolation statistics. ---*/
   unsigned long totalTargetPoints = 0, totalDonorPoints = 0, denseSize = 0;
-  MinDonors = 1<<30; MaxDonors = 0; MaxCorrection = 0.0; AvgCorrection = 0.0;
+  MinDonors = 1 << 30;
+  MaxDonors = 0;
+  MaxCorrection = 0.0;
+  AvgCorrection = 0.0;
 
   for (unsigned short iMarkerInt = 0; iMarkerInt < nMarkerInt; iMarkerInt++) {
-
     /*--- Identify the rank that computed the interpolation matrix for this marker. ---*/
     const int iProcessor = assignedProcessor[iMarkerInt];
     /*--- If no processor was assigned to work, the zone does not contain the interface. ---*/
@@ -252,19 +252,17 @@ void CRadialBasisFunction::SetTransferCoeff(const CConfig* const* config) {
     /*--- Send C_inv_trunc only to the ranks that need it (those with target points),
      *    partial broadcast. MPI wrapper not used due to passive double. ---*/
     vector<unsigned long> allNumVertex(nProcessor);
-    SU2_MPI::Allgather(&nVertexTarget, 1, MPI_UNSIGNED_LONG,
-      allNumVertex.data(), 1, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
+    SU2_MPI::Allgather(&nVertexTarget, 1, MPI_UNSIGNED_LONG, allNumVertex.data(), 1, MPI_UNSIGNED_LONG,
+                       SU2_MPI::GetComm());
 
     if (rank == iProcessor) {
       for (int jProcessor = 0; jProcessor < nProcessor; ++jProcessor)
         if ((jProcessor != iProcessor) && (allNumVertex[jProcessor] != 0))
-          MPI_Send(C_inv_trunc.data(), C_inv_trunc.size(),
-                   MPI_DOUBLE, jProcessor, 0, SU2_MPI::GetComm());
-    }
-    else if (nVertexTarget != 0) {
-      C_inv_trunc.resize(1+nPolynomial+nGlobalVertexDonor, nGlobalVertexDonor);
-      MPI_Recv(C_inv_trunc.data(), C_inv_trunc.size(), MPI_DOUBLE,
-               iProcessor, 0, SU2_MPI::GetComm(), MPI_STATUS_IGNORE);
+          MPI_Send(C_inv_trunc.data(), C_inv_trunc.size(), MPI_DOUBLE, jProcessor, 0, SU2_MPI::GetComm());
+    } else if (nVertexTarget != 0) {
+      C_inv_trunc.resize(1 + nPolynomial + nGlobalVertexDonor, nGlobalVertexDonor);
+      MPI_Recv(C_inv_trunc.data(), C_inv_trunc.size(), MPI_DOUBLE, iProcessor, 0, SU2_MPI::GetComm(),
+               MPI_STATUS_IGNORE);
     }
 #endif
 
@@ -283,123 +281,119 @@ void CRadialBasisFunction::SetTransferCoeff(const CConfig* const* config) {
       targetCoord[iVertexTarget] = target_geometry->nodes->GetCoord(pointTarget);
     }
     totalTargetPoints += nVertexTarget;
-    denseSize += nVertexTarget*nGlobalVertexDonor;
+    denseSize += nVertexTarget * nGlobalVertexDonor;
 
     /*--- Distribute target slabs over the threads in the rank for processing. ---*/
 
     SU2_OMP_PARALLEL
     if (nVertexTarget > 0) {
-
-    constexpr unsigned long targetSlabSize = 32;
-
-    su2passivematrix funcMat(targetSlabSize, 1+nPolynomial+nGlobalVertexDonor);
-    su2passivematrix interpMat(targetSlabSize, nGlobalVertexDonor);
-
-    /*--- Thread-local variables for statistics. ---*/
-    unsigned long minDonors = 1<<30, maxDonors = 0, totalDonors = 0;
-    passivedouble sumCorr = 0.0, maxCorr = 0.0;
-
-    SU2_OMP_FOR_DYN(1)
-    for (auto iVertexTarget = 0ul; iVertexTarget < nVertexTarget; iVertexTarget += targetSlabSize) {
-
-      const auto iLastVertex = min(nVertexTarget, iVertexTarget+targetSlabSize);
-      const auto slabSize = iLastVertex - iVertexTarget;
-
-      /*--- Prepare matrix of functions A (the targets to donors matrix). ---*/
-
-      /*--- Polynominal part: ---*/
-      if (usePolynomial) {
-        /*--- Constant term. ---*/
-        for (auto k = 0ul; k < slabSize; ++k) funcMat(k,0) = 1.0;
-
-        /*--- Linear terms. ---*/
-        for (int iDim = 0, idx = 1; iDim < nDim; ++iDim) {
-          /*--- Of which one may have been excluded. ---*/
-          if (!keepPolynomialRow[iDim]) continue;
-          for (auto k = 0ul; k < slabSize; ++k)
-            funcMat(k, idx) = SU2_TYPE::GetValue(targetCoord[iVertexTarget+k][iDim]);
-          idx += 1;
+      constexpr unsigned long targetSlabSize = 32;
+
+      su2passivematrix funcMat(targetSlabSize, 1 + nPolynomial + nGlobalVertexDonor);
+      su2passivematrix interpMat(targetSlabSize, nGlobalVertexDonor);
+
+      /*--- Thread-local variables for statistics. ---*/
+      unsigned long minDonors = 1 << 30, maxDonors = 0, totalDonors = 0;
+      passivedouble sumCorr = 0.0, maxCorr = 0.0;
+
+      SU2_OMP_FOR_DYN(1)
+      for (auto iVertexTarget = 0ul; iVertexTarget < nVertexTarget; iVertexTarget += targetSlabSize) {
+        const auto iLastVertex = min(nVertexTarget, iVertexTarget + targetSlabSize);
+        const auto slabSize = iLastVertex - iVertexTarget;
+
+        /*--- Prepare matrix of functions A (the targets to donors matrix). ---*/
+
+        /*--- Polynominal part: ---*/
+        if (usePolynomial) {
+          /*--- Constant term. ---*/
+          for (auto k = 0ul; k < slabSize; ++k) funcMat(k, 0) = 1.0;
+
+          /*--- Linear terms. ---*/
+          for (int iDim = 0, idx = 1; iDim < nDim; ++iDim) {
+            /*--- Of which one may have been excluded. ---*/
+            if (!keepPolynomialRow[iDim]) continue;
+            for (auto k = 0ul; k < slabSize; ++k)
+              funcMat(k, idx) = SU2_TYPE::GetValue(targetCoord[iVertexTarget + k][iDim]);
+            idx += 1;
+          }
         }
-      }
-      /*--- RBF terms: ---*/
-      for (auto iVertexDonor = 0ul; iVertexDonor < nGlobalVertexDonor; ++iVertexDonor) {
-        for (auto k = 0ul; k < slabSize; ++k) {
-          auto dist = GeometryToolbox::Distance(nDim, targetCoord[iVertexTarget+k], donorCoord[iVertexDonor]);
-          auto rbf = Get_RadialBasisValue(kindRBF, paramRBF, dist);
-          funcMat(k, 1+nPolynomial+iVertexDonor) = SU2_TYPE::GetValue(rbf);
+        /*--- RBF terms: ---*/
+        for (auto iVertexDonor = 0ul; iVertexDonor < nGlobalVertexDonor; ++iVertexDonor) {
+          for (auto k = 0ul; k < slabSize; ++k) {
+            auto dist = GeometryToolbox::Distance(nDim, targetCoord[iVertexTarget + k], donorCoord[iVertexDonor]);
+            auto rbf = Get_RadialBasisValue(kindRBF, paramRBF, dist);
+            funcMat(k, 1 + nPolynomial + iVertexDonor) = SU2_TYPE::GetValue(rbf);
+          }
         }
-      }
 
-      /*--- Compute slab of the interpolation matrix. ---*/
+        /*--- Compute slab of the interpolation matrix. ---*/
 #ifdef HAVE_LAPACK
-      /*--- interpMat = funcMat * C_inv_trunc, but order of gemm arguments
-       *    is swapped due to row-major storage of su2passivematrix. ---*/
-      const char op = 'N';
-      const int M = interpMat.cols(), N = slabSize, K = funcMat.cols();
-      // lda = C_inv_trunc.cols() = M; ldb = funcMat.cols() = K; ldc = interpMat.cols() = M;
-      const passivedouble alpha = 1.0, beta = 0.0;
-      DGEMM(&op, &op, &M, &N, &K, &alpha, C_inv_trunc[0], &M, funcMat[0], &K, &beta, interpMat[0], &M);
+        /*--- interpMat = funcMat * C_inv_trunc, but order of gemm arguments
+         *    is swapped due to row-major storage of su2passivematrix. ---*/
+        const char op = 'N';
+        const int M = interpMat.cols(), N = slabSize, K = funcMat.cols();
+        // lda = C_inv_trunc.cols() = M; ldb = funcMat.cols() = K; ldc = interpMat.cols() = M;
+        const passivedouble alpha = 1.0, beta = 0.0;
+        DGEMM(&op, &op, &M, &N, &K, &alpha, C_inv_trunc[0], &M, funcMat[0], &K, &beta, interpMat[0], &M);
 #else
-      /*--- Naive product, loop order considers short-wide
-       *    nature of funcMat and interpMat. ---*/
-      interpMat = 0.0;
-      for (auto k = 0ul; k < funcMat.cols(); ++k)
-        for (auto i = 0ul; i < slabSize; ++i)
-          for (auto j = 0ul; j < interpMat.cols(); ++j)
-            interpMat(i,j) += funcMat(i,k) * C_inv_trunc(k,j);
+        /*--- Naive product, loop order considers short-wide
+         *    nature of funcMat and interpMat. ---*/
+        interpMat = 0.0;
+        for (auto k = 0ul; k < funcMat.cols(); ++k)
+          for (auto i = 0ul; i < slabSize; ++i)
+            for (auto j = 0ul; j < interpMat.cols(); ++j) interpMat(i, j) += funcMat(i, k) * C_inv_trunc(k, j);
 #endif
-      /*--- Set interpolation coefficients. ---*/
-
-      for (auto k = 0ul; k < slabSize; ++k) {
-        auto& targetVertex = targetVertices[markTarget][iVertexTarget+k];
-
-        /*--- Prune small coefficients. ---*/
-        auto info = PruneSmallCoefficients(SU2_TYPE::GetValue(pruneTol), interpMat.cols(), interpMat[k]);
-        auto nnz = info.first;
-        totalDonors += nnz;
-        minDonors = min(minDonors, nnz);
-        maxDonors = max(maxDonors, nnz);
-        auto corr = fabs(info.second-1.0); // far from 1 either way is bad;
-        sumCorr += corr;
-        maxCorr = max(maxCorr, corr);
-
-        /*--- Allocate and set donor information for this target point. ---*/
-        targetVertex.resize(nnz);
-
-        for (unsigned long iVertex = 0, iSet = 0; iVertex < nGlobalVertexDonor; ++iVertex) {
-          auto coeff = interpMat(k,iVertex);
-          if (fabs(coeff) > 0.0) {
-            targetVertex.processor[iSet] = donorProc[iVertex];
-            targetVertex.globalPoint[iSet] = donorPoint[iVertex];
-            targetVertex.coefficient[iSet] = coeff;
-            ++iSet;
+        /*--- Set interpolation coefficients. ---*/
+
+        for (auto k = 0ul; k < slabSize; ++k) {
+          auto& targetVertex = targetVertices[markTarget][iVertexTarget + k];
+
+          /*--- Prune small coefficients. ---*/
+          auto info = PruneSmallCoefficients(SU2_TYPE::GetValue(pruneTol), interpMat.cols(), interpMat[k]);
+          auto nnz = info.first;
+          totalDonors += nnz;
+          minDonors = min(minDonors, nnz);
+          maxDonors = max(maxDonors, nnz);
+          auto corr = fabs(info.second - 1.0);  // far from 1 either way is bad;
+          sumCorr += corr;
+          maxCorr = max(maxCorr, corr);
+
+          /*--- Allocate and set donor information for this target point. ---*/
+          targetVertex.resize(nnz);
+
+          for (unsigned long iVertex = 0, iSet = 0; iVertex < nGlobalVertexDonor; ++iVertex) {
+            auto coeff = interpMat(k, iVertex);
+            if (fabs(coeff) > 0.0) {
+              targetVertex.processor[iSet] = donorProc[iVertex];
+              targetVertex.globalPoint[iSet] = donorPoint[iVertex];
+              targetVertex.coefficient[iSet] = coeff;
+              ++iSet;
+            }
           }
         }
+      }  // end target vertex loop
+      END_SU2_OMP_FOR
+      SU2_OMP_CRITICAL {
+        totalDonorPoints += totalDonors;
+        MinDonors = min(MinDonors, minDonors);
+        MaxDonors = max(MaxDonors, maxDonors);
+        AvgCorrection += sumCorr;
+        MaxCorrection = max(MaxCorrection, maxCorr);
       }
-    } // end target vertex loop
-    END_SU2_OMP_FOR
-    SU2_OMP_CRITICAL
-    {
-      totalDonorPoints += totalDonors;
-      MinDonors = min(MinDonors, minDonors);
-      MaxDonors = max(MaxDonors, maxDonors);
-      AvgCorrection += sumCorr;
-      MaxCorrection = max(MaxCorrection, maxCorr);
-    }
-    END_SU2_OMP_CRITICAL
+      END_SU2_OMP_CRITICAL
     }
     END_SU2_OMP_PARALLEL
 
     /*--- Free global data that will no longer be used. ---*/
-    donorCoord.resize(0,0);
+    donorCoord.resize(0, 0);
     vector<long>().swap(donorPoint);
     vector<int>().swap(donorProc);
-    C_inv_trunc.resize(0,0);
+    C_inv_trunc.resize(0, 0);
 
-  } // end loop over interface markers
+  }  // end loop over interface markers
 
   /*--- Final reduction of interpolation statistics and basic sanity checks. ---*/
-  auto Reduce = [](SU2_MPI::Op op, unsigned long &val) {
+  auto Reduce = [](SU2_MPI::Op op, unsigned long& val) {
     auto tmp = val;
     SU2_MPI::Allreduce(&tmp, &val, 1, MPI_UNSIGNED_LONG, op, SU2_MPI::GetComm());
   };
@@ -413,26 +407,25 @@ void CRadialBasisFunction::SetTransferCoeff(const CConfig* const* config) {
   MPI_Allreduce(&tmp1, &AvgCorrection, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
   MPI_Allreduce(&tmp2, &MaxCorrection, 1, MPI_DOUBLE, MPI_MAX, SU2_MPI::GetComm());
 #endif
-  if (totalTargetPoints == 0)
-    SU2_MPI::Error("Somehow there are no target interpolation points.", CURRENT_FUNCTION);
+  if (totalTargetPoints == 0) SU2_MPI::Error("Somehow there are no target interpolation points.", CURRENT_FUNCTION);
 
   if (MinDonors == 0)
-    SU2_MPI::Error("One or more target points have no donors, either:\n"
-                   " - The interface surfaces are not in contact.\n"
-                   " - The RBF radius is too small.\n"
-                   " - The pruning tolerance is too aggressive.", CURRENT_FUNCTION);
-
-  MaxCorrection += 1.0; // put back the reference "1"
+    SU2_MPI::Error(
+        "One or more target points have no donors, either:\n"
+        " - The interface surfaces are not in contact.\n"
+        " - The RBF radius is too small.\n"
+        " - The pruning tolerance is too aggressive.",
+        CURRENT_FUNCTION);
+
+  MaxCorrection += 1.0;  // put back the reference "1"
   AvgCorrection = AvgCorrection / totalTargetPoints + 1.0;
   AvgDonors = totalDonorPoints / totalTargetPoints;
-  Density = totalDonorPoints / (0.01*denseSize);
-
+  Density = totalDonorPoints / (0.01 * denseSize);
 }
 
-void CRadialBasisFunction::ComputeGeneratorMatrix(RADIAL_BASIS type, bool usePolynomial,
-                           su2double radius, const su2activematrix& coords, int& nPolynomial,
-                           vector<int>& keepPolynomialRow, su2passivematrix& C_inv_trunc) {
-
+void CRadialBasisFunction::ComputeGeneratorMatrix(RADIAL_BASIS type, bool usePolynomial, su2double radius,
+                                                  const su2activematrix& coords, int& nPolynomial,
+                                                  vector<int>& keepPolynomialRow, su2passivematrix& C_inv_trunc) {
   const su2double interfaceCoordTol = 1e6 * numeric_limits<passivedouble>::epsilon();
 
   const int nVertexDonor = coords.rows();
@@ -443,24 +436,22 @@ void CRadialBasisFunction::ComputeGeneratorMatrix(RADIAL_BASIS type, bool usePol
 
   for (int iVertex = 0; iVertex < nVertexDonor; ++iVertex)
     for (int jVertex = iVertex; jVertex < nVertexDonor; ++jVertex)
-      global_M(iVertex, jVertex) = SU2_TYPE::GetValue(Get_RadialBasisValue(type, radius,
-                                   GeometryToolbox::Distance(nDim, coords[iVertex], coords[jVertex])));
+      global_M(iVertex, jVertex) = SU2_TYPE::GetValue(
+          Get_RadialBasisValue(type, radius, GeometryToolbox::Distance(nDim, coords[iVertex], coords[jVertex])));
 
   /*--- Invert M matrix (operation is in-place). ---*/
-  const bool kernelIsSPD = (type==RADIAL_BASIS::WENDLAND_C2) || (type==RADIAL_BASIS::GAUSSIAN) ||
-                           (type==RADIAL_BASIS::INV_MULTI_QUADRIC);
+  const bool kernelIsSPD = (type == RADIAL_BASIS::WENDLAND_C2) || (type == RADIAL_BASIS::GAUSSIAN) ||
+                           (type == RADIAL_BASIS::INV_MULTI_QUADRIC);
   global_M.Invert(kernelIsSPD);
 
   /*--- Compute C_inv_trunc. ---*/
   if (usePolynomial) {
-
     /*--- Fill P matrix (P for points, with an extra top row of ones). ---*/
-    su2passivematrix P(1+nDim, nVertexDonor);
+    su2passivematrix P(1 + nDim, nVertexDonor);
 
     for (int iVertex = 0; iVertex < nVertexDonor; iVertex++) {
       P(0, iVertex) = 1.0;
-      for (int iDim = 0; iDim < nDim; ++iDim)
-        P(1+iDim, iVertex) = SU2_TYPE::GetValue(coords(iVertex, iDim));
+      for (int iDim = 0; iDim < nDim; ++iDim) P(1 + iDim, iVertex) = SU2_TYPE::GetValue(coords(iVertex, iDim));
     }
 
     /*--- Check if points lie on a plane and remove one coordinate from P if so. ---*/
@@ -471,13 +462,12 @@ void CRadialBasisFunction::ComputeGeneratorMatrix(RADIAL_BASIS type, bool usePol
     global_M.MatMatMult('R', P, Q);
 
     /*--- Compute Mp = (Q * P^T)^-1 ---*/
-    CSymmetricMatrix Mp(nPolynomial+1);
+    CSymmetricMatrix Mp(nPolynomial + 1);
 
     for (int i = 0; i <= nPolynomial; ++i)
       for (int j = i; j <= nPolynomial; ++j) {
-        Mp(i,j) = 0.0;
-        for (int k = 0; k < nVertexDonor; ++k)
-          Mp(i,j) += Q(i,k) * P(j,k);
+        Mp(i, j) = 0.0;
+        for (int k = 0; k < nVertexDonor; ++k) Mp(i, j) += Q(i, k) * P(j, k);
       }
     Mp.Invert(false);
 
@@ -490,40 +480,36 @@ void CRadialBasisFunction::ComputeGeneratorMatrix(RADIAL_BASIS type, bool usePol
 #ifdef HAVE_LAPACK
     /*--- Order of gemm arguments swapped due to row-major storage. ---*/
     const char opa = 'N', opb = 'T';
-    const int M = nVertexDonor, N = nVertexDonor, K = nPolynomial+1;
+    const int M = nVertexDonor, N = nVertexDonor, K = nPolynomial + 1;
     // lda = C_inv_top.cols() = M; ldb = Q.cols() = M; ldc = C_inv_bot.cols() = M;
     const passivedouble alpha = -1.0, beta = 1.0;
     DGEMM(&opa, &opb, &M, &N, &K, &alpha, C_inv_top[0], &M, Q[0], &M, &beta, C_inv_bot[0], &M);
-#else // naive product
+#else  // naive product
     for (int i = 0; i < nVertexDonor; ++i)
       for (int j = 0; j < nVertexDonor; ++j)
-        for (int k = 0; k <= nPolynomial; ++k)
-          C_inv_bot(i,j) -= Q(k,i) * C_inv_top(k,j);
+        for (int k = 0; k <= nPolynomial; ++k) C_inv_bot(i, j) -= Q(k, i) * C_inv_top(k, j);
 #endif
 
     /*--- Merge top and bottom of C_inv_trunc. More intrusive memory
      *    management, or separate handling of top and bottom, would
      *    avoid these copies (and associated temporary vars). ---*/
-    C_inv_trunc.resize(1+nPolynomial+nVertexDonor, nVertexDonor);
-    memcpy(C_inv_trunc[0], C_inv_top.data(), C_inv_top.size()*sizeof(passivedouble));
-    memcpy(C_inv_trunc[1+nPolynomial], C_inv_bot.data(), C_inv_bot.size()*sizeof(passivedouble));
-  }
-  else {
+    C_inv_trunc.resize(1 + nPolynomial + nVertexDonor, nVertexDonor);
+    memcpy(C_inv_trunc[0], C_inv_top.data(), C_inv_top.size() * sizeof(passivedouble));
+    memcpy(C_inv_trunc[1 + nPolynomial], C_inv_bot.data(), C_inv_bot.size() * sizeof(passivedouble));
+  } else {
     /*--- No polynomial term used in the interpolation, C_inv_trunc = M^-1. ---*/
 
     C_inv_trunc = global_M.StealData();
 
-  } // end usePolynomial
-
+  }  // end usePolynomial
 }
 
-int CRadialBasisFunction::CheckPolynomialTerms(su2double max_diff_tol, vector<int>& keep_row,
-                                               su2passivematrix &P) {
+int CRadialBasisFunction::CheckPolynomialTerms(su2double max_diff_tol, vector<int>& keep_row, su2passivematrix& P) {
   const int m = P.rows();
   const int n = P.cols();
 
   /*--- The first row of P is all ones and we do not care about it for this analysis. ---*/
-  const int n_rows = m-1;
+  const int n_rows = m - 1;
   keep_row.resize(n_rows);
 
   /*--- By default assume points are not on a plane (all rows kept). ---*/
@@ -538,17 +524,16 @@ int CRadialBasisFunction::CheckPolynomialTerms(su2double max_diff_tol, vector<in
 
   for (int i = 0; i < n_rows; ++i)
     for (int j = i; j < n_rows; ++j) {
-      PPT(i,j) = 0.0;
-      for (int k = 0; k < n; ++k) PPT(i,j) += P(i+1,k) * P(j+1,k);
+      PPT(i, j) = 0.0;
+      for (int k = 0; k < n; ++k) PPT(i, j) += P(i + 1, k) * P(j + 1, k);
     }
   PPT.Invert(true);
 
   /*--- RHS for the least squares fit (vector of ones times P). ---*/
-  vector<passivedouble> rhs(n_rows,0.0), coeff(n_rows);
+  vector<passivedouble> rhs(n_rows, 0.0), coeff(n_rows);
 
   for (int i = 0; i < n_rows; ++i)
-    for (int j = 0; j < n; ++j)
-      rhs[i] += P(i+1,j);
+    for (int j = 0; j < n; ++j) rhs[i] += P(i + 1, j);
 
   /*--- Multiply the RHS by the inverse thus obtaining the coefficients. ---*/
   PPT.MatVecMult(rhs.begin(), coeff.begin());
@@ -556,33 +541,29 @@ int CRadialBasisFunction::CheckPolynomialTerms(su2double max_diff_tol, vector<in
   /*--- Determine the maximum deviation of the points from the fitted plane. ---*/
   passivedouble max_diff = 0.0;
 
-  for (int j = 0; j < n; ++j)
-  {
+  for (int j = 0; j < n; ++j) {
     passivedouble sum = 0.0;
-    for (int i = 0; i < n_rows; ++i) sum += coeff[i] * P(i+1,j);
+    for (int i = 0; i < n_rows; ++i) sum += coeff[i] * P(i + 1, j);
 
     /*--- 1.0 is the arbitrary constant we are assuming when fitting
      the plane, i.e. the vector of ones used to generate the RHS. ---*/
-    max_diff = max(abs(1.0-sum), max_diff);
+    max_diff = max(abs(1.0 - sum), max_diff);
   }
 
   /*--- If points lie on plane remove row associated with the maximum coefficient. ---*/
-  if (max_diff < max_diff_tol)
-  {
+  if (max_diff < max_diff_tol) {
     /*--- Find the max coeff and mark the corresponding row for removal. ---*/
     int remove_row = 0;
     for (int i = 1; i < n_rows; ++i)
-      if (abs(coeff[i]) > abs(coeff[remove_row]))
-        remove_row = i;
+      if (abs(coeff[i]) > abs(coeff[remove_row])) remove_row = i;
 
     /*--- Mark row as removed and adjust number of polynomial terms. ---*/
-    n_polynomial = n_rows-1;
+    n_polynomial = n_rows - 1;
     keep_row[remove_row] = 0;
 
     /*--- Truncated P by shifting rows "up". ---*/
-    for (auto i = remove_row+1; i < m-1; ++i)
-      for (int j = 0; j < n; ++j)
-        P(i,j) = P(i+1,j);
+    for (auto i = remove_row + 1; i < m - 1; ++i)
+      for (int j = 0; j < n; ++j) P(i, j) = P(i + 1, j);
   }
 
   return n_polynomial;
diff --git a/Common/src/interface_interpolation/CSlidingMesh.cpp b/Common/src/interface_interpolation/CSlidingMesh.cpp
index 81c46bf88b6..ca01a7d43df 100644
--- a/Common/src/interface_interpolation/CSlidingMesh.cpp
+++ b/Common/src/interface_interpolation/CSlidingMesh.cpp
@@ -30,15 +30,13 @@
 #include "../../include/geometry/CGeometry.hpp"
 #include "../../include/toolboxes/geometry_toolbox.hpp"
 
-
-CSlidingMesh::CSlidingMesh(CGeometry ****geometry_container, const CConfig* const* config,
-                           unsigned int iZone, unsigned int jZone) :
-  CInterpolator(geometry_container, config, iZone, jZone) {
+CSlidingMesh::CSlidingMesh(CGeometry**** geometry_container, const CConfig* const* config, unsigned int iZone,
+                           unsigned int jZone)
+    : CInterpolator(geometry_container, config, iZone, jZone) {
   SetTransferCoeff(config);
 }
 
 void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
-
   /* 0 - Variable declaration */
 
   /* --- General variables --- */
@@ -64,7 +62,6 @@ void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
   su2double Area, Area_old, tmp_Area;
   su2double LineIntersectionLength, *Direction, length;
 
-
   /* --- Markers Variables --- */
 
   unsigned short iMarkerInt, nMarkerInt;
@@ -80,7 +77,7 @@ void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
 
   su2vector<unsigned long> Target_nLinkedNodes;
   su2vector<unsigned long> Target_StartLinkedNodes;
-  unsigned long *target_segment;
+  unsigned long* target_segment;
   su2vector<unsigned long> Target_LinkedNodes;
   su2vector<unsigned long> Target_GlobalPoint, Donor_GlobalPoint;
 
@@ -100,7 +97,7 @@ void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
   su2vector<unsigned long> Donor_Proc;
 
   su2double *donor_iMidEdge_point, *donor_jMidEdge_point;
-  su2double **donor_element;
+  su2double** donor_element;
   su2activematrix DonorPoint_Coord;
 
   targetVertices.resize(config[targetZone]->GetnMarker_All());
@@ -113,24 +110,22 @@ void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
 
   Donor_Vect = nullptr;
   Coeff_Vect = nullptr;
-  storeProc  = nullptr;
+  storeProc = nullptr;
 
   tmp_Donor_Vect = nullptr;
   tmp_Coeff_Vect = nullptr;
-  tmp_storeProc  = nullptr;
+  tmp_storeProc = nullptr;
 
-  Normal    = new su2double[nDim];
+  Normal = new su2double[nDim];
   Direction = new su2double[nDim];
 
-
   /* 2 - Find boundary tag between touching grids */
 
   /*--- Number of markers on the FSI interface ---*/
-  nMarkerInt = (int)( config[ donorZone ]->GetMarker_n_ZoneInterface() ) / 2;
+  nMarkerInt = (int)(config[donorZone]->GetMarker_n_ZoneInterface()) / 2;
 
   /*--- For the number of markers on the interface... ---*/
-  for ( iMarkerInt = 0; iMarkerInt < nMarkerInt; iMarkerInt++ ){
-
+  for (iMarkerInt = 0; iMarkerInt < nMarkerInt; iMarkerInt++) {
     /*--- On the donor side: find the tag of the boundary sharing the interface ---*/
     markDonor = config[donorZone]->FindInterfaceMarker(iMarkerInt);
 
@@ -138,10 +133,10 @@ void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
     markTarget = config[targetZone]->FindInterfaceMarker(iMarkerInt);
 
     /*--- Checks if the zone contains the interface, if not continue to the next step ---*/
-    if(!CheckInterfaceBoundary(markDonor, markTarget)) continue;
+    if (!CheckInterfaceBoundary(markDonor, markTarget)) continue;
 
     nVertexTarget = 0;
-    if(markTarget != -1) nVertexTarget = target_geometry->GetnVertex( markTarget );
+    if (markTarget != -1) nVertexTarget = target_geometry->GetnVertex(markTarget);
 
     /*
     3 -Reconstruct the boundaries from parallel partitioning
@@ -152,23 +147,23 @@ void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
 
     nGlobalVertex_Target = nGlobalVertex;
 
-    TargetPoint_Coord       = Buffer_Receive_Coord;
-    Target_GlobalPoint      = Buffer_Receive_GlobalPoint;
-    Target_nLinkedNodes     = Buffer_Receive_nLinkedNodes;
+    TargetPoint_Coord = Buffer_Receive_Coord;
+    Target_GlobalPoint = Buffer_Receive_GlobalPoint;
+    Target_nLinkedNodes = Buffer_Receive_nLinkedNodes;
     Target_StartLinkedNodes = Buffer_Receive_StartLinkedNodes;
-    Target_LinkedNodes      = Buffer_Receive_LinkedNodes;
+    Target_LinkedNodes = Buffer_Receive_LinkedNodes;
 
     /*--- Donor boundary ---*/
     ReconstructBoundary(donorZone, markDonor);
 
     nGlobalVertex_Donor = nGlobalVertex;
 
-    DonorPoint_Coord       = Buffer_Receive_Coord;
-    Donor_GlobalPoint      = Buffer_Receive_GlobalPoint;
-    Donor_nLinkedNodes     = Buffer_Receive_nLinkedNodes;
+    DonorPoint_Coord = Buffer_Receive_Coord;
+    Donor_GlobalPoint = Buffer_Receive_GlobalPoint;
+    Donor_nLinkedNodes = Buffer_Receive_nLinkedNodes;
     Donor_StartLinkedNodes = Buffer_Receive_StartLinkedNodes;
-    Donor_LinkedNodes      = Buffer_Receive_LinkedNodes;
-    Donor_Proc             = Buffer_Receive_Proc;
+    Donor_LinkedNodes = Buffer_Receive_LinkedNodes;
+    Donor_Proc = Buffer_Receive_Proc;
 
     /*--- Starts building the supermesh layer (2D or 3D) ---*/
     /* - For each target node, it first finds the closest donor point
@@ -178,8 +173,7 @@ void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
      */
     if (nVertexTarget) targetVertices[markTarget].resize(nVertexTarget);
 
-    if(nDim == 2){
-
+    if (nDim == 2) {
       target_iMidEdge_point = new su2double[nDim];
       target_jMidEdge_point = new su2double[nDim];
 
@@ -191,15 +185,13 @@ void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
       target_segment = new unsigned long[2];
 
       for (iVertex = 0; iVertex < nVertexTarget; iVertex++) {
-
         nDonorPoints = 0;
 
         /*--- Stores coordinates of the target node ---*/
 
         target_iPoint = target_geometry->vertex[markTarget][iVertex]->GetNode();
 
-        if (target_geometry->nodes->GetDomain(target_iPoint)){
-
+        if (target_geometry->nodes->GetDomain(target_iPoint)) {
           Coord_i = target_geometry->nodes->GetCoord(target_iPoint);
 
           /*--- Brute force to find the closest donor_node ---*/
@@ -208,8 +200,7 @@ void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
           donor_StartIndex = 0;
 
           for (donor_iPoint = 0; donor_iPoint < nGlobalVertex_Donor; donor_iPoint++) {
-
-            Coord_j = DonorPoint_Coord[ donor_iPoint ];
+            Coord_j = DonorPoint_Coord[donor_iPoint];
 
             dist = GeometryToolbox::Distance(nDim, Coord_i, Coord_j);
 
@@ -218,45 +209,44 @@ void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
               donor_StartIndex = donor_iPoint;
             }
 
-            if (dist == 0.0){
+            if (dist == 0.0) {
               donor_StartIndex = donor_iPoint;
               break;
             }
           }
 
-          donor_iPoint    = donor_StartIndex;
+          donor_iPoint = donor_StartIndex;
           donor_OldiPoint = donor_iPoint;
 
           /*--- Contruct information regarding the target cell ---*/
 
           auto dPoint = target_geometry->nodes->GetGlobalIndex(target_iPoint);
           for (jVertexTarget = 0; jVertexTarget < nGlobalVertex_Target; jVertexTarget++)
-            if( dPoint == Target_GlobalPoint[jVertexTarget] )
-              break;
+            if (dPoint == Target_GlobalPoint[jVertexTarget]) break;
 
-          if ( Target_nLinkedNodes[jVertexTarget] == 1 ){
-            target_segment[0] = Target_LinkedNodes[ Target_StartLinkedNodes[jVertexTarget] ];
+          if (Target_nLinkedNodes[jVertexTarget] == 1) {
+            target_segment[0] = Target_LinkedNodes[Target_StartLinkedNodes[jVertexTarget]];
             target_segment[1] = jVertexTarget;
-          }
-          else{
-            target_segment[0] = Target_LinkedNodes[ Target_StartLinkedNodes[jVertexTarget] ];
-            target_segment[1] = Target_LinkedNodes[ Target_StartLinkedNodes[jVertexTarget] + 1];
+          } else {
+            target_segment[0] = Target_LinkedNodes[Target_StartLinkedNodes[jVertexTarget]];
+            target_segment[1] = Target_LinkedNodes[Target_StartLinkedNodes[jVertexTarget] + 1];
           }
 
           dTMP = 0;
-          for(iDim = 0; iDim < nDim; iDim++){
-            target_iMidEdge_point[iDim] = ( TargetPoint_Coord(target_segment[0], iDim ) +
-                                            target_geometry->nodes->GetCoord( target_iPoint , iDim) ) / 2.;
-            target_jMidEdge_point[iDim] = ( TargetPoint_Coord(target_segment[1], iDim ) +
-                                            target_geometry->nodes->GetCoord( target_iPoint , iDim) ) / 2.;
+          for (iDim = 0; iDim < nDim; iDim++) {
+            target_iMidEdge_point[iDim] =
+                (TargetPoint_Coord(target_segment[0], iDim) + target_geometry->nodes->GetCoord(target_iPoint, iDim)) /
+                2.;
+            target_jMidEdge_point[iDim] =
+                (TargetPoint_Coord(target_segment[1], iDim) + target_geometry->nodes->GetCoord(target_iPoint, iDim)) /
+                2.;
 
             Direction[iDim] = target_jMidEdge_point[iDim] - target_iMidEdge_point[iDim];
             dTMP += Direction[iDim] * Direction[iDim];
           }
 
           dTMP = sqrt(dTMP);
-          for(iDim = 0; iDim < nDim; iDim++)
-            Direction[iDim] /= dTMP;
+          for (iDim = 0; iDim < nDim; iDim++) Direction[iDim] /= dTMP;
 
           length = GeometryToolbox::Distance(nDim, target_iMidEdge_point, target_jMidEdge_point);
 
@@ -264,156 +254,153 @@ void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
 
           /*--- Proceeds along the forward direction (depending on which connected boundary node is found first) ---*/
 
-          while( !check ){
-
+          while (!check) {
             /*--- Proceeds until the value of the intersection area is null ---*/
 
-            if ( Donor_nLinkedNodes[donor_iPoint] == 1 ){
-              donor_forward_point  = Donor_LinkedNodes[ Donor_StartLinkedNodes[donor_iPoint] ];
+            if (Donor_nLinkedNodes[donor_iPoint] == 1) {
+              donor_forward_point = Donor_LinkedNodes[Donor_StartLinkedNodes[donor_iPoint]];
               donor_backward_point = donor_iPoint;
-            }
-            else{
-              uptr = &Donor_LinkedNodes[ Donor_StartLinkedNodes[donor_iPoint] ];
+            } else {
+              uptr = &Donor_LinkedNodes[Donor_StartLinkedNodes[donor_iPoint]];
 
-              if( donor_OldiPoint != uptr[0] ){
-                donor_forward_point  = uptr[0];
+              if (donor_OldiPoint != uptr[0]) {
+                donor_forward_point = uptr[0];
                 donor_backward_point = uptr[1];
-              }
-              else{
-                donor_forward_point  = uptr[1];
+              } else {
+                donor_forward_point = uptr[1];
                 donor_backward_point = uptr[0];
               }
             }
 
-            if(donor_iPoint >= nGlobalVertex_Donor){
+            if (donor_iPoint >= nGlobalVertex_Donor) {
               check = true;
               continue;
             }
 
-            for(iDim = 0; iDim < nDim; iDim++){
-              donor_iMidEdge_point[iDim] = ( DonorPoint_Coord(donor_forward_point, iDim) +
-                                             DonorPoint_Coord(donor_iPoint, iDim) ) / 2.;
-              donor_jMidEdge_point[iDim] = ( DonorPoint_Coord(donor_backward_point, iDim) +
-                                             DonorPoint_Coord(donor_iPoint, iDim) ) / 2.;
+            for (iDim = 0; iDim < nDim; iDim++) {
+              donor_iMidEdge_point[iDim] =
+                  (DonorPoint_Coord(donor_forward_point, iDim) + DonorPoint_Coord(donor_iPoint, iDim)) / 2.;
+              donor_jMidEdge_point[iDim] =
+                  (DonorPoint_Coord(donor_backward_point, iDim) + DonorPoint_Coord(donor_iPoint, iDim)) / 2.;
             }
 
-            LineIntersectionLength = ComputeLineIntersectionLength(nDim, target_iMidEdge_point, target_jMidEdge_point,
-                                                                   donor_iMidEdge_point, donor_jMidEdge_point, Direction);
+            LineIntersectionLength =
+                ComputeLineIntersectionLength(nDim, target_iMidEdge_point, target_jMidEdge_point, donor_iMidEdge_point,
+                                              donor_jMidEdge_point, Direction);
 
-            if ( LineIntersectionLength == 0.0 ){
+            if (LineIntersectionLength == 0.0) {
               check = true;
               continue;
             }
 
-            /*--- In case the element intersects the target cell, update the auxiliary communication data structure ---*/
+            /*--- In case the element intersects the target cell, update the auxiliary communication data structure
+             * ---*/
 
-            tmp_Coeff_Vect = new     su2double[ nDonorPoints + 1 ];
-            tmp_Donor_Vect = new unsigned long[ nDonorPoints + 1 ];
-            tmp_storeProc  = new unsigned long[ nDonorPoints + 1 ];
+            tmp_Coeff_Vect = new su2double[nDonorPoints + 1];
+            tmp_Donor_Vect = new unsigned long[nDonorPoints + 1];
+            tmp_storeProc = new unsigned long[nDonorPoints + 1];
 
-            for( iDonor = 0; iDonor < nDonorPoints; iDonor++){
+            for (iDonor = 0; iDonor < nDonorPoints; iDonor++) {
               tmp_Donor_Vect[iDonor] = Donor_Vect[iDonor];
               tmp_Coeff_Vect[iDonor] = Coeff_Vect[iDonor];
-              tmp_storeProc[iDonor]  = storeProc[iDonor];
+              tmp_storeProc[iDonor] = storeProc[iDonor];
             }
 
-            tmp_Donor_Vect[ nDonorPoints ] = donor_iPoint;
-            tmp_Coeff_Vect[ nDonorPoints ] = LineIntersectionLength / length;
-            tmp_storeProc[  nDonorPoints ] = Donor_Proc[donor_iPoint];
+            tmp_Donor_Vect[nDonorPoints] = donor_iPoint;
+            tmp_Coeff_Vect[nDonorPoints] = LineIntersectionLength / length;
+            tmp_storeProc[nDonorPoints] = Donor_Proc[donor_iPoint];
 
-            delete [] Donor_Vect;
-            delete [] Coeff_Vect;
-            delete [] storeProc;
+            delete[] Donor_Vect;
+            delete[] Coeff_Vect;
+            delete[] storeProc;
 
             Donor_Vect = tmp_Donor_Vect;
             Coeff_Vect = tmp_Coeff_Vect;
-            storeProc  = tmp_storeProc;
+            storeProc = tmp_storeProc;
 
             donor_OldiPoint = donor_iPoint;
-            donor_iPoint    = donor_forward_point;
+            donor_iPoint = donor_forward_point;
 
             nDonorPoints++;
           }
 
-          if ( Donor_nLinkedNodes[donor_StartIndex] == 2 ){
+          if (Donor_nLinkedNodes[donor_StartIndex] == 2) {
             check = false;
 
-            uptr = &Donor_LinkedNodes[ Donor_StartLinkedNodes[donor_StartIndex] ];
+            uptr = &Donor_LinkedNodes[Donor_StartLinkedNodes[donor_StartIndex]];
 
             donor_iPoint = uptr[1];
             donor_OldiPoint = donor_StartIndex;
-          }
-          else
+          } else
             check = true;
 
           /*--- Proceeds along the backward direction (depending on which connected boundary node is found first) ---*/
 
-          while( !check ){
-
+          while (!check) {
             /*--- Proceeds until the value of the intersection length is null ---*/
-            if ( Donor_nLinkedNodes[donor_iPoint] == 1 ){
-              donor_forward_point  = donor_OldiPoint;
+            if (Donor_nLinkedNodes[donor_iPoint] == 1) {
+              donor_forward_point = donor_OldiPoint;
               donor_backward_point = donor_iPoint;
-            }
-            else{
-              uptr = &Donor_LinkedNodes[ Donor_StartLinkedNodes[donor_iPoint] ];
+            } else {
+              uptr = &Donor_LinkedNodes[Donor_StartLinkedNodes[donor_iPoint]];
 
-              if( donor_OldiPoint != uptr[0] ){
-                donor_forward_point  = uptr[0];
+              if (donor_OldiPoint != uptr[0]) {
+                donor_forward_point = uptr[0];
                 donor_backward_point = uptr[1];
-              }
-              else{
-                donor_forward_point  = uptr[1];
+              } else {
+                donor_forward_point = uptr[1];
                 donor_backward_point = uptr[0];
               }
             }
 
-            if(donor_iPoint >= nGlobalVertex_Donor){
+            if (donor_iPoint >= nGlobalVertex_Donor) {
               check = true;
               continue;
             }
 
-            for(iDim = 0; iDim < nDim; iDim++){
-              donor_iMidEdge_point[iDim] = ( DonorPoint_Coord(donor_forward_point , iDim) +
-                                             DonorPoint_Coord(donor_iPoint, iDim) ) / 2.;
-              donor_jMidEdge_point[iDim] = ( DonorPoint_Coord(donor_backward_point, iDim) +
-                                             DonorPoint_Coord(donor_iPoint, iDim) ) / 2.;
+            for (iDim = 0; iDim < nDim; iDim++) {
+              donor_iMidEdge_point[iDim] =
+                  (DonorPoint_Coord(donor_forward_point, iDim) + DonorPoint_Coord(donor_iPoint, iDim)) / 2.;
+              donor_jMidEdge_point[iDim] =
+                  (DonorPoint_Coord(donor_backward_point, iDim) + DonorPoint_Coord(donor_iPoint, iDim)) / 2.;
             }
 
-            LineIntersectionLength = ComputeLineIntersectionLength(nDim, target_iMidEdge_point, target_jMidEdge_point,
-                                                                   donor_iMidEdge_point, donor_jMidEdge_point, Direction);
+            LineIntersectionLength =
+                ComputeLineIntersectionLength(nDim, target_iMidEdge_point, target_jMidEdge_point, donor_iMidEdge_point,
+                                              donor_jMidEdge_point, Direction);
 
-            if ( LineIntersectionLength == 0.0 ){
+            if (LineIntersectionLength == 0.0) {
               check = true;
               continue;
             }
 
-            /*--- In case the element intersects the target cell, update the auxiliary communication data structure ---*/
+            /*--- In case the element intersects the target cell, update the auxiliary communication data structure
+             * ---*/
 
-            tmp_Coeff_Vect = new     su2double[ nDonorPoints + 1 ];
-            tmp_Donor_Vect = new unsigned long[ nDonorPoints + 1 ];
-            tmp_storeProc  = new unsigned long[ nDonorPoints + 1 ];
+            tmp_Coeff_Vect = new su2double[nDonorPoints + 1];
+            tmp_Donor_Vect = new unsigned long[nDonorPoints + 1];
+            tmp_storeProc = new unsigned long[nDonorPoints + 1];
 
-            for( iDonor = 0; iDonor < nDonorPoints; iDonor++){
+            for (iDonor = 0; iDonor < nDonorPoints; iDonor++) {
               tmp_Donor_Vect[iDonor] = Donor_Vect[iDonor];
               tmp_Coeff_Vect[iDonor] = Coeff_Vect[iDonor];
-              tmp_storeProc[iDonor]  = storeProc[iDonor];
+              tmp_storeProc[iDonor] = storeProc[iDonor];
             }
 
-            tmp_Coeff_Vect[ nDonorPoints ] = LineIntersectionLength / length;
-            tmp_Donor_Vect[ nDonorPoints ] = donor_iPoint;
-            tmp_storeProc[  nDonorPoints ] = Donor_Proc[donor_iPoint];
+            tmp_Coeff_Vect[nDonorPoints] = LineIntersectionLength / length;
+            tmp_Donor_Vect[nDonorPoints] = donor_iPoint;
+            tmp_storeProc[nDonorPoints] = Donor_Proc[donor_iPoint];
 
-            delete [] Donor_Vect;
-            delete [] Coeff_Vect;
-            delete [] storeProc;
+            delete[] Donor_Vect;
+            delete[] Coeff_Vect;
+            delete[] storeProc;
 
             Donor_Vect = tmp_Donor_Vect;
             Coeff_Vect = tmp_Coeff_Vect;
-            storeProc  = tmp_storeProc;
+            storeProc = tmp_storeProc;
 
             donor_OldiPoint = donor_iPoint;
-            donor_iPoint    = donor_forward_point;
+            donor_iPoint = donor_forward_point;
 
             nDonorPoints++;
           }
@@ -422,7 +409,7 @@ void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
 
           targetVertices[markTarget][iVertex].resize(nDonorPoints);
 
-          for ( iDonor = 0; iDonor < nDonorPoints; iDonor++ ){
+          for (iDonor = 0; iDonor < nDonorPoints; iDonor++) {
             targetVertices[markTarget][iVertex].coefficient[iDonor] = Coeff_Vect[iDonor];
             targetVertices[markTarget][iVertex].globalPoint[iDonor] = Donor_GlobalPoint[Donor_Vect[iDonor]];
             targetVertices[markTarget][iVertex].processor[iDonor] = storeProc[iDonor];
@@ -430,19 +417,17 @@ void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
         }
       }
 
-      delete [] target_segment;
+      delete[] target_segment;
 
-      delete [] target_iMidEdge_point;
-      delete [] target_jMidEdge_point;
+      delete[] target_iMidEdge_point;
+      delete[] target_jMidEdge_point;
 
-      delete [] donor_iMidEdge_point;
-      delete [] donor_jMidEdge_point;
-    }
-    else{
+      delete[] donor_iMidEdge_point;
+      delete[] donor_jMidEdge_point;
+    } else {
       /* --- 3D geometry, creates a superficial super-mesh --- */
 
       for (iVertex = 0; iVertex < nVertexTarget; iVertex++) {
-
         nDonorPoints = 0;
 
         /*--- Stores coordinates of the target node ---*/
@@ -458,27 +443,23 @@ void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
         /*--- The value of Area computed here includes also portion of boundary belonging to different marker ---*/
         Area = GeometryToolbox::Norm(nDim, Normal);
 
-        for (iDim = 0; iDim < nDim; iDim++)
-          Normal[iDim] /= Area;
+        for (iDim = 0; iDim < nDim; iDim++) Normal[iDim] /= Area;
 
-        for (iDim = 0; iDim < nDim; iDim++)
-          Coord_i[iDim] = target_geometry->nodes->GetCoord(target_iPoint, iDim);
+        for (iDim = 0; iDim < nDim; iDim++) Coord_i[iDim] = target_geometry->nodes->GetCoord(target_iPoint, iDim);
 
         auto dPoint = target_geometry->nodes->GetGlobalIndex(target_iPoint);
-        for (target_iPoint = 0; target_iPoint < nGlobalVertex_Target; target_iPoint++){
-          if( dPoint == Target_GlobalPoint[target_iPoint] )
-            break;
+        for (target_iPoint = 0; target_iPoint < nGlobalVertex_Target; target_iPoint++) {
+          if (dPoint == Target_GlobalPoint[target_iPoint]) break;
         }
 
         /*--- Build local surface dual mesh for target element ---*/
 
         nEdges_target = Target_nLinkedNodes[target_iPoint];
 
-        nNode_target = 2*(nEdges_target + 1);
+        nNode_target = 2 * (nEdges_target + 1);
 
         target_element = new su2double*[nNode_target];
-        for (ii = 0; ii < nNode_target; ii++)
-          target_element[ii] = new su2double[nDim];
+        for (ii = 0; ii < nNode_target; ii++) target_element[ii] = new su2double[nDim];
 
         nNode_target = Build_3D_surface_element(Target_LinkedNodes, Target_StartLinkedNodes, Target_nLinkedNodes,
                                                 TargetPoint_Coord, target_iPoint, target_element);
@@ -489,8 +470,7 @@ void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
         donor_StartIndex = 0;
 
         for (donor_iPoint = 0; donor_iPoint < nGlobalVertex_Donor; donor_iPoint++) {
-
-          Coord_j = DonorPoint_Coord[ donor_iPoint ];
+          Coord_j = DonorPoint_Coord[donor_iPoint];
 
           dist = GeometryToolbox::Distance(nDim, Coord_i, Coord_j);
 
@@ -499,7 +479,7 @@ void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
             donor_StartIndex = donor_iPoint;
           }
 
-          if (dist == 0.0){
+          if (dist == 0.0) {
             donor_StartIndex = donor_iPoint;
             break;
           }
@@ -509,36 +489,34 @@ void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
 
         nEdges_donor = Donor_nLinkedNodes[donor_iPoint];
 
-        donor_element = new su2double*[ 2*nEdges_donor + 2 ];
-        for (ii = 0; ii < 2*nEdges_donor + 2; ii++)
-          donor_element[ii] = new su2double[nDim];
+        donor_element = new su2double*[2 * nEdges_donor + 2];
+        for (ii = 0; ii < 2 * nEdges_donor + 2; ii++) donor_element[ii] = new su2double[nDim];
 
         nNode_donor = Build_3D_surface_element(Donor_LinkedNodes, Donor_StartLinkedNodes, Donor_nLinkedNodes,
                                                DonorPoint_Coord, donor_iPoint, donor_element);
 
         Area = 0;
-        for (ii = 1; ii < nNode_target-1; ii++){
-          for (jj = 1; jj < nNode_donor-1; jj++){
-            Area += Compute_Triangle_Intersection(target_element[0], target_element[ii], target_element[ii+1],
-                                                  donor_element[0], donor_element[jj], donor_element[jj+1], Normal);
+        for (ii = 1; ii < nNode_target - 1; ii++) {
+          for (jj = 1; jj < nNode_donor - 1; jj++) {
+            Area += Compute_Triangle_Intersection(target_element[0], target_element[ii], target_element[ii + 1],
+                                                  donor_element[0], donor_element[jj], donor_element[jj + 1], Normal);
           }
         }
 
-        for (ii = 0; ii < 2*nEdges_donor + 2; ii++)
-          delete [] donor_element[ii];
-        delete [] donor_element;
+        for (ii = 0; ii < 2 * nEdges_donor + 2; ii++) delete[] donor_element[ii];
+        delete[] donor_element;
 
         nDonorPoints = 1;
 
         /*--- In case the element intersect the target cell update the auxiliary communication data structure ---*/
 
-        Coeff_Vect = new     su2double[ nDonorPoints ];
-        Donor_Vect = new unsigned long[ nDonorPoints ];
-        storeProc  = new unsigned long[ nDonorPoints ];
+        Coeff_Vect = new su2double[nDonorPoints];
+        Donor_Vect = new unsigned long[nDonorPoints];
+        storeProc = new unsigned long[nDonorPoints];
 
         Coeff_Vect[0] = Area;
         Donor_Vect[0] = donor_iPoint;
-        storeProc[0]  = Donor_Proc[donor_iPoint];
+        storeProc[0] = Donor_Proc[donor_iPoint];
 
         alreadyVisitedDonor = new unsigned long[1];
 
@@ -548,11 +526,11 @@ void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
 
         Area_old = -1;
 
-        while( Area > Area_old ){
-
+        while (Area > Area_old) {
           /*
            * - Starting from the closest donor_point, it expands the supermesh by a countour search pattern.
-           * - The closest donor element becomes the core, at each iteration a new layer of elements around the core is taken into account
+           * - The closest donor element becomes the core, at each iteration a new layer of elements around the core is
+           * taken into account
            */
 
           Area_old = Area;
@@ -560,100 +538,97 @@ void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
           ToVisit = nullptr;
           nToVisit = 0;
 
-          for( iNodeVisited = StartVisited; iNodeVisited < nAlreadyVisited; iNodeVisited++ ){
-
-            vPoint = alreadyVisitedDonor[ iNodeVisited ];
+          for (iNodeVisited = StartVisited; iNodeVisited < nAlreadyVisited; iNodeVisited++) {
+            vPoint = alreadyVisitedDonor[iNodeVisited];
 
             nEdgeVisited = Donor_nLinkedNodes[vPoint];
 
-            for (iEdgeVisited = 0; iEdgeVisited < nEdgeVisited; iEdgeVisited++){
-
-              donor_iPoint = Donor_LinkedNodes[ Donor_StartLinkedNodes[vPoint] + iEdgeVisited];
+            for (iEdgeVisited = 0; iEdgeVisited < nEdgeVisited; iEdgeVisited++) {
+              donor_iPoint = Donor_LinkedNodes[Donor_StartLinkedNodes[vPoint] + iEdgeVisited];
 
               /*--- Check if the node to visit is already listed in the data structure to avoid double visits ---*/
 
               check = 0;
 
-              for( jj = 0; jj < nAlreadyVisited; jj++ ){
-                if( donor_iPoint == alreadyVisitedDonor[jj] ){
+              for (jj = 0; jj < nAlreadyVisited; jj++) {
+                if (donor_iPoint == alreadyVisitedDonor[jj]) {
                   check = 1;
                   break;
                 }
               }
 
-              if( check == 0 && ToVisit != nullptr){
-                for( jj = 0; jj < nToVisit; jj++ )
-                  if( donor_iPoint == ToVisit[jj] ){
+              if (check == 0 && ToVisit != nullptr) {
+                for (jj = 0; jj < nToVisit; jj++)
+                  if (donor_iPoint == ToVisit[jj]) {
                     check = 1;
                     break;
                   }
               }
 
-              if( check == 0 ){
+              if (check == 0) {
                 /*--- If the node was not already visited, visit it and list it into data structure ---*/
 
-                tmpVect = new unsigned long[ nToVisit + 1 ];
+                tmpVect = new unsigned long[nToVisit + 1];
 
-                for( jj = 0; jj < nToVisit; jj++ )
-                  tmpVect[jj] = ToVisit[jj];
+                for (jj = 0; jj < nToVisit; jj++) tmpVect[jj] = ToVisit[jj];
                 tmpVect[nToVisit] = donor_iPoint;
 
-
-                  delete [] ToVisit;
+                delete[] ToVisit;
 
                 ToVisit = tmpVect;
                 tmpVect = nullptr;
 
                 nToVisit++;
 
-                /*--- Find the value of the intersection area between the current donor element and the target element --- */
+                /*--- Find the value of the intersection area between the current donor element and the target element
+                 * --- */
 
                 nEdges_donor = Donor_nLinkedNodes[donor_iPoint];
 
-                donor_element = new su2double*[ 2*nEdges_donor + 2 ];
-                for (ii = 0; ii < 2*nEdges_donor + 2; ii++)
-                  donor_element[ii] = new su2double[nDim];
+                donor_element = new su2double*[2 * nEdges_donor + 2];
+                for (ii = 0; ii < 2 * nEdges_donor + 2; ii++) donor_element[ii] = new su2double[nDim];
 
                 nNode_donor = Build_3D_surface_element(Donor_LinkedNodes, Donor_StartLinkedNodes, Donor_nLinkedNodes,
                                                        DonorPoint_Coord, donor_iPoint, donor_element);
 
                 tmp_Area = 0;
-                for (ii = 1; ii < nNode_target-1; ii++)
-                  for (jj = 1; jj < nNode_donor-1; jj++)
-                    tmp_Area += Compute_Triangle_Intersection(target_element[0], target_element[ii], target_element[ii+1],
-                                                              donor_element[0], donor_element[jj], donor_element[jj+1], Normal);
+                for (ii = 1; ii < nNode_target - 1; ii++)
+                  for (jj = 1; jj < nNode_donor - 1; jj++)
+                    tmp_Area += Compute_Triangle_Intersection(target_element[0], target_element[ii],
+                                                              target_element[ii + 1], donor_element[0],
+                                                              donor_element[jj], donor_element[jj + 1], Normal);
 
-                for (ii = 0; ii < 2*nEdges_donor + 2; ii++)
-                  delete [] donor_element[ii];
-                delete [] donor_element;
+                for (ii = 0; ii < 2 * nEdges_donor + 2; ii++) delete[] donor_element[ii];
+                delete[] donor_element;
 
-                /*--- In case the element intersect the target cell update the auxiliary communication data structure ---*/
+                /*--- In case the element intersect the target cell update the auxiliary communication data structure
+                 * ---*/
 
-                tmp_Coeff_Vect = new     su2double[ nDonorPoints + 1 ];
-                tmp_Donor_Vect = new unsigned long[ nDonorPoints + 1 ];
-                tmp_storeProc  = new unsigned long[ nDonorPoints + 1 ];
+                tmp_Coeff_Vect = new su2double[nDonorPoints + 1];
+                tmp_Donor_Vect = new unsigned long[nDonorPoints + 1];
+                tmp_storeProc = new unsigned long[nDonorPoints + 1];
 
-                for( iDonor = 0; iDonor < nDonorPoints; iDonor++){
+                for (iDonor = 0; iDonor < nDonorPoints; iDonor++) {
                   tmp_Donor_Vect[iDonor] = Donor_Vect[iDonor];
                   tmp_Coeff_Vect[iDonor] = Coeff_Vect[iDonor];
-                  tmp_storeProc[iDonor]  = storeProc[iDonor];
+                  tmp_storeProc[iDonor] = storeProc[iDonor];
                 }
 
-                tmp_Coeff_Vect[ nDonorPoints ] = tmp_Area;
-                tmp_Donor_Vect[ nDonorPoints ] = donor_iPoint;
-                tmp_storeProc[  nDonorPoints ] = Donor_Proc[donor_iPoint];
+                tmp_Coeff_Vect[nDonorPoints] = tmp_Area;
+                tmp_Donor_Vect[nDonorPoints] = donor_iPoint;
+                tmp_storeProc[nDonorPoints] = Donor_Proc[donor_iPoint];
 
-                delete [] Donor_Vect;
-                delete [] Coeff_Vect;
-                delete [] storeProc;
+                delete[] Donor_Vect;
+                delete[] Coeff_Vect;
+                delete[] storeProc;
 
                 Donor_Vect = tmp_Donor_Vect;
                 Coeff_Vect = tmp_Coeff_Vect;
-                storeProc  = tmp_storeProc;
+                storeProc = tmp_storeProc;
 
                 tmp_Coeff_Vect = nullptr;
                 tmp_Donor_Vect = nullptr;
-                tmp_storeProc  = nullptr;
+                tmp_storeProc = nullptr;
 
                 nDonorPoints++;
 
@@ -666,78 +641,75 @@ void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
 
           StartVisited = nAlreadyVisited;
 
-          tmpVect = new unsigned long[ nAlreadyVisited + nToVisit ];
-
-          for( jj = 0; jj < nAlreadyVisited; jj++ )
-            tmpVect[jj] = alreadyVisitedDonor[jj];
+          tmpVect = new unsigned long[nAlreadyVisited + nToVisit];
 
-          for( jj = 0; jj < nToVisit; jj++ )
-            tmpVect[ nAlreadyVisited + jj ] = ToVisit[jj];
+          for (jj = 0; jj < nAlreadyVisited; jj++) tmpVect[jj] = alreadyVisitedDonor[jj];
 
+          for (jj = 0; jj < nToVisit; jj++) tmpVect[nAlreadyVisited + jj] = ToVisit[jj];
 
-          delete [] alreadyVisitedDonor;
+          delete[] alreadyVisitedDonor;
 
           alreadyVisitedDonor = tmpVect;
 
           nAlreadyVisited += nToVisit;
 
-          delete [] ToVisit;
+          delete[] ToVisit;
         }
 
-        delete [] alreadyVisitedDonor;
+        delete[] alreadyVisitedDonor;
 
         /*--- Set the communication data structure and copy data from the auxiliary vectors ---*/
 
         targetVertices[markTarget][iVertex].resize(nDonorPoints);
 
-        for ( iDonor = 0; iDonor < nDonorPoints; iDonor++ ){
+        for (iDonor = 0; iDonor < nDonorPoints; iDonor++) {
           targetVertices[markTarget][iVertex].coefficient[iDonor] = Coeff_Vect[iDonor] / Area;
           targetVertices[markTarget][iVertex].globalPoint[iDonor] = Donor_GlobalPoint[Donor_Vect[iDonor]];
           targetVertices[markTarget][iVertex].processor[iDonor] = storeProc[iDonor];
         }
 
-        for (ii = 0; ii < 2*nEdges_target + 2; ii++)
-          delete [] target_element[ii];
-        delete [] target_element;
+        for (ii = 0; ii < 2 * nEdges_target + 2; ii++) delete[] target_element[ii];
+        delete[] target_element;
 
-        delete [] Donor_Vect; Donor_Vect = nullptr;
-        delete [] Coeff_Vect; Coeff_Vect = nullptr;
-        delete [] storeProc;  storeProc  = nullptr;
+        delete[] Donor_Vect;
+        Donor_Vect = nullptr;
+        delete[] Coeff_Vect;
+        Coeff_Vect = nullptr;
+        delete[] storeProc;
+        storeProc = nullptr;
       }
     }
-
   }
 
-  delete [] Normal;
-  delete [] Direction;
+  delete[] Normal;
+  delete[] Direction;
 
-  delete [] Donor_Vect;
-  delete [] Coeff_Vect;
-  delete [] storeProc;
+  delete[] Donor_Vect;
+  delete[] Coeff_Vect;
+  delete[] storeProc;
 }
 
-int CSlidingMesh::Build_3D_surface_element(const su2vector<unsigned long>& map, const su2vector<unsigned long>& startIndex,
+int CSlidingMesh::Build_3D_surface_element(const su2vector<unsigned long>& map,
+                                           const su2vector<unsigned long>& startIndex,
                                            const su2vector<unsigned long>& nNeighbor, su2activematrix const& coord,
                                            unsigned long centralNode, su2double** element) {
-
   /*--- Given a node "centralNode", this routines reconstruct the vertex centered
    *    surface element around the node and store it into "element" ---*/
 
   constexpr unsigned short nDim = 3;
 
-  const unsigned long *OuterNodes;
+  const unsigned long* OuterNodes;
 
   /* --- Store central node as element first point --- */
 
-  for (unsigned short iDim = 0; iDim < nDim; iDim++)
-    element[0][iDim] = coord(centralNode,iDim);
+  for (unsigned short iDim = 0; iDim < nDim; iDim++) element[0][iDim] = coord(centralNode, iDim);
 
   unsigned long nOuterNodes = nNeighbor[centralNode];
 
-  OuterNodes = &map[ startIndex[centralNode] ];
+  OuterNodes = &map[startIndex[centralNode]];
 
   // For each neighbor n of centralNode, store <=2 neighbors of centralNode that are neighbors of n.
-  su2matrix<int> OuterNodesNeighbour(nOuterNodes,2);
+  su2matrix<int> OuterNodesNeighbour(nOuterNodes, 2);
   OuterNodesNeighbour = -1;
   // Typically there are exactly 2 such neighbors, and all the neighbors of centralNode can be
   // arranged into a closed chain. However at 1D boundaries of 2D markers, the neighbors might
@@ -745,75 +717,73 @@ int CSlidingMesh::Build_3D_surface_element(const su2vector<unsigned long>& map,
   // StartNode is a node where we can start to iterate through the chain. I.e. it's any node in
   // case of a closed chain, or one of the two ends in case of an open chain.
   int StartNode = 0;
-  for( unsigned long iNode = 0; iNode < nOuterNodes; iNode++ ){
-
-    int count = 0; // number of neighboring outer nodes already found
-    const unsigned long iPoint = OuterNodes[ iNode ];
-    const unsigned long *ptr = &map[ startIndex[iPoint] ];
+  for (unsigned long iNode = 0; iNode < nOuterNodes; iNode++) {
+    int count = 0;  // number of neighboring outer nodes already found
+    const unsigned long iPoint = OuterNodes[iNode];
+    const unsigned long* ptr = &map[startIndex[iPoint]];
 
-    for ( unsigned long jNode = 0; jNode < nNeighbor[iPoint]; jNode++ ){
+    for (unsigned long jNode = 0; jNode < nNeighbor[iPoint]; jNode++) {
       const unsigned long jPoint = ptr[jNode];
-      for( unsigned long kNode = 0; kNode < nOuterNodes; kNode++ ){
-        if ( jPoint == OuterNodes[ kNode ] && jPoint != centralNode){
-          OuterNodesNeighbour(iNode,count) = static_cast<int>(kNode);
+      for (unsigned long kNode = 0; kNode < nOuterNodes; kNode++) {
+        if (jPoint == OuterNodes[kNode] && jPoint != centralNode) {
+          OuterNodesNeighbour(iNode, count) = static_cast<int>(kNode);
           count++;
           break;
         }
       }
     }
-    if( count == 1 )
-      StartNode = static_cast<int>(iNode);
+    if (count == 1) StartNode = static_cast<int>(iNode);
   }
 
-  /* --- Build element, starts from one outer node and loops along the external edges until the element is reconstructed --- */
+  /* --- Build element, starts from one outer node and loops along the external edges until the element is reconstructed
+   * --- */
 
   int CurrentNode = StartNode;
-  int NextNode    = OuterNodesNeighbour(CurrentNode,0);
+  int NextNode = OuterNodesNeighbour(CurrentNode, 0);
   unsigned long iElementNode = 1;
 
-  while( NextNode != -1 ){ // We finished iterating through the chain if it is an open chain and we reached the other end.
+  while (NextNode !=
+         -1) {  // We finished iterating through the chain if it is an open chain and we reached the other end.
 
     for (unsigned short iDim = 0; iDim < nDim; iDim++)
-      element[ iElementNode ][iDim] = ( element[0][iDim] + coord(OuterNodes[ CurrentNode ], iDim) )/2.;
+      element[iElementNode][iDim] = (element[0][iDim] + coord(OuterNodes[CurrentNode], iDim)) / 2.;
 
     iElementNode++;
 
     for (unsigned short iDim = 0; iDim < nDim; iDim++)
-      element[ iElementNode ][iDim] = ( element[0][iDim] + coord[ OuterNodes[ CurrentNode ] ][ iDim] +
-                                        coord(OuterNodes[ NextNode ], iDim) )/3.;
+      element[iElementNode][iDim] =
+          (element[0][iDim] + coord[OuterNodes[CurrentNode]][iDim] + coord(OuterNodes[NextNode], iDim)) / 3.;
     iElementNode++;
 
     // "Place the next domino piece in the correct orientation."
-    if( OuterNodesNeighbour(NextNode, 0) == CurrentNode){
+    if (OuterNodesNeighbour(NextNode, 0) == CurrentNode) {
       CurrentNode = NextNode;
       NextNode = OuterNodesNeighbour(NextNode, 1);
-    } else{
+    } else {
       CurrentNode = NextNode;
       NextNode = OuterNodesNeighbour(NextNode, 0);
     }
 
     // We finished iterating through the chain if it is closed and we reached the beginning again.
-    if (CurrentNode == StartNode)
-      break;
+    if (CurrentNode == StartNode) break;
   }
 
-  if( CurrentNode == StartNode ){ // This is a closed element, so add again element 1 to the end of the structure, useful later
-    for (unsigned short iDim = 0; iDim < nDim; iDim++)
-      element[ iElementNode ][iDim] = element[1][iDim];
+  if (CurrentNode ==
+      StartNode) {  // This is a closed element, so add again element 1 to the end of the structure, useful later
+    for (unsigned short iDim = 0; iDim < nDim; iDim++) element[iElementNode][iDim] = element[1][iDim];
     iElementNode++;
-  } else{
+  } else {
     for (unsigned short iDim = 0; iDim < nDim; iDim++)
-      element[ iElementNode ][iDim] = ( element[0][iDim] + coord(OuterNodes[ CurrentNode ], iDim) )/2.;
+      element[iElementNode][iDim] = (element[0][iDim] + coord(OuterNodes[CurrentNode], iDim)) / 2.;
     iElementNode++;
   }
 
   return static_cast<int>(iElementNode);
-
 }
 
 su2double CSlidingMesh::ComputeLineIntersectionLength(unsigned short nDim, const su2double* A1, const su2double* A2,
-                                                      const su2double* B1, const su2double* B2, const su2double* Direction) {
-
+                                                      const su2double* B1, const su2double* B2,
+                                                      const su2double* Direction) {
   /*--- Given 2 segments, each defined by 2 points, it projects them along a given direction
    *    and it computes the length of the segment resulting from their intersection ---*/
   /*--- The algorithm works for both 2D and 3D problems ---*/
@@ -823,46 +793,39 @@ su2double CSlidingMesh::ComputeLineIntersectionLength(unsigned short nDim, const
   su2double dotA2, dotB1, dotB2;
 
   dotA2 = 0;
-  for(iDim = 0; iDim < nDim; iDim++)
-    dotA2 += ( A2[iDim] - A1[iDim] ) * Direction[iDim];
+  for (iDim = 0; iDim < nDim; iDim++) dotA2 += (A2[iDim] - A1[iDim]) * Direction[iDim];
 
-  if( dotA2 >= 0 ){
+  if (dotA2 >= 0) {
     dotB1 = 0;
     dotB2 = 0;
-    for(iDim = 0; iDim < nDim; iDim++){
-      dotB1 += ( B1[iDim] - A1[iDim] ) * Direction[iDim];
-      dotB2 += ( B2[iDim] - A1[iDim] ) * Direction[iDim];
+    for (iDim = 0; iDim < nDim; iDim++) {
+      dotB1 += (B1[iDim] - A1[iDim]) * Direction[iDim];
+      dotB2 += (B2[iDim] - A1[iDim]) * Direction[iDim];
     }
-  }
-  else{
+  } else {
     dotA2 *= -1;
 
     dotB1 = 0;
     dotB2 = 0;
-    for(iDim = 0; iDim < nDim; iDim++){
-      dotB1 -= ( B1[iDim] - A1[iDim] ) * Direction[iDim];
-      dotB2 -= ( B2[iDim] - A1[iDim] ) * Direction[iDim];
+    for (iDim = 0; iDim < nDim; iDim++) {
+      dotB1 -= (B1[iDim] - A1[iDim]) * Direction[iDim];
+      dotB2 -= (B2[iDim] - A1[iDim]) * Direction[iDim];
     }
   }
 
-  if( dotB1 >= 0 && dotB1 <= dotA2 ){
-    if ( dotB2 < 0 )
-      return fabs( dotB1 );
-    if ( dotB2 > dotA2 )
-      return fabs( dotA2 - dotB1 );
+  if (dotB1 >= 0 && dotB1 <= dotA2) {
+    if (dotB2 < 0) return fabs(dotB1);
+    if (dotB2 > dotA2) return fabs(dotA2 - dotB1);
 
-    return fabs( dotB1 - dotB2 );
+    return fabs(dotB1 - dotB2);
   }
 
-  if( dotB2 >= 0 && dotB2 <= dotA2 ){
-    if ( dotB1 < 0 )
-      return fabs(dotB2);
-    if ( dotB1 > dotA2 )
-      return fabs( dotA2 - dotB2 );
+  if (dotB2 >= 0 && dotB2 <= dotA2) {
+    if (dotB1 < 0) return fabs(dotB2);
+    if (dotB1 > dotA2) return fabs(dotA2 - dotB2);
   }
 
-  if( ( dotB1 <= 0 && dotA2 <= dotB2 ) || ( dotB2 <= 0 && dotA2 <= dotB1 ) )
-    return fabs( dotA2 );
+  if ((dotB1 <= 0 && dotA2 <= dotB2) || (dotB2 <= 0 && dotA2 <= dotB1)) return fabs(dotA2);
 
   return 0.0;
 }
@@ -870,9 +833,9 @@ su2double CSlidingMesh::ComputeLineIntersectionLength(unsigned short nDim, const
 su2double CSlidingMesh::Compute_Triangle_Intersection(const su2double* A1, const su2double* A2, const su2double* A3,
                                                       const su2double* B1, const su2double* B2, const su2double* B3,
                                                       const su2double* Direction) {
-
   /* --- This routine is ONLY for 3D grids --- */
-  /* --- Projects triangle points onto a plane, specified by its normal "Direction", and calls the ComputeIntersectionArea routine --- */
+  /* --- Projects triangle points onto a plane, specified by its normal "Direction", and calls the
+   * ComputeIntersectionArea routine --- */
 
   unsigned short iDim;
   constexpr unsigned short nDim = 3;
@@ -884,7 +847,7 @@ su2double CSlidingMesh::Compute_Triangle_Intersection(const su2double* A1, const
 
   /* --- Reference frame is determined by: x = A1A2 y = x ^ ( -Direction ) --- */
 
-  for(iDim = 0; iDim < 3; iDim++){
+  for (iDim = 0; iDim < 3; iDim++) {
     a1[iDim] = 0;
     a2[iDim] = 0;
     a3[iDim] = 0;
@@ -895,36 +858,34 @@ su2double CSlidingMesh::Compute_Triangle_Intersection(const su2double* A1, const
   }
 
   m1 = 0;
-  for(iDim = 0; iDim < nDim; iDim++){
+  for (iDim = 0; iDim < nDim; iDim++) {
     K[iDim] = Direction[iDim];
 
     m1 += K[iDim] * K[iDim];
   }
 
-  for(iDim = 0; iDim < nDim; iDim++)
-    K[iDim] /= sqrt(m1);
+  for (iDim = 0; iDim < nDim; iDim++) K[iDim] /= sqrt(m1);
 
   m2 = 0;
-  for(iDim = 0; iDim < nDim; iDim++)
-    m2 += (A2[iDim] - A1[iDim]) * K[iDim];
+  for (iDim = 0; iDim < nDim; iDim++) m2 += (A2[iDim] - A1[iDim]) * K[iDim];
 
   m1 = 0;
-  for(iDim = 0; iDim < nDim; iDim++){
+  for (iDim = 0; iDim < nDim; iDim++) {
     I[iDim] = (A2[iDim] - A1[iDim]) - m2 * K[iDim];
     m1 += I[iDim] * I[iDim];
   }
 
-  for(iDim = 0; iDim < nDim; iDim++)
-    I[iDim] /= sqrt(m1);
+  for (iDim = 0; iDim < nDim; iDim++) I[iDim] /= sqrt(m1);
 
   // Cross product to find Y
-  J[0] =   K[1]*I[2] - K[2]*I[1];
-  J[1] = -(K[0]*I[2] - K[2]*I[0]);
-  J[2] =   K[0]*I[1] - K[1]*I[0];
+  J[0] = K[1] * I[2] - K[2] * I[1];
+  J[1] = -(K[0] * I[2] - K[2] * I[0]);
+  J[2] = K[0] * I[1] - K[1] * I[0];
 
-  /* --- Project all points on the plane specified by Direction and change their reference frame taking A1 as origin --- */
+  /* --- Project all points on the plane specified by Direction and change their reference frame taking A1 as origin ---
+   */
 
-  for(iDim = 0; iDim < nDim; iDim++){
+  for (iDim = 0; iDim < nDim; iDim++) {
     a2[0] += (A2[iDim] - A1[iDim]) * I[iDim];
     a2[1] += (A2[iDim] - A1[iDim]) * J[iDim];
     a2[2] += (A2[iDim] - A1[iDim]) * K[iDim];
@@ -948,13 +909,13 @@ su2double CSlidingMesh::Compute_Triangle_Intersection(const su2double* A1, const
 
   /*--- Compute intersection area ---*/
 
-  return ComputeIntersectionArea( a1, a2, a3, b1, b2, b3 );
+  return ComputeIntersectionArea(a1, a2, a3, b1, b2, b3);
 }
 
 su2double CSlidingMesh::ComputeIntersectionArea(const su2double* P1, const su2double* P2, const su2double* P3,
                                                 const su2double* Q1, const su2double* Q2, const su2double* Q3) {
-
-  /* --- This routines computes the area of the polygonal element generated by the superimposition of 2 planar triangle --- */
+  /* --- This routines computes the area of the polygonal element generated by the superimposition of 2 planar triangle
+   * --- */
   /* --- The 2 triangle must lie on the same plane --- */
 
   unsigned short iDim, nPoints = 0, i, j, k;
@@ -966,7 +927,7 @@ su2double CSlidingMesh::ComputeIntersectionArea(const su2double* P1, const su2do
 
   constexpr unsigned short nDim = 2;
 
-  for(iDim = 0; iDim < nDim; iDim++){
+  for (iDim = 0; iDim < nDim; iDim++) {
     TriangleP[0][iDim] = 0;
     TriangleP[1][iDim] = P2[iDim] - P1[iDim];
     TriangleP[2][iDim] = P3[iDim] - P1[iDim];
@@ -978,69 +939,61 @@ su2double CSlidingMesh::ComputeIntersectionArea(const su2double* P1, const su2do
     TriangleQ[3][iDim] = Q1[iDim] - P1[iDim];
   }
 
-
-  for( j = 0; j < 3; j++){
-    if( CheckPointInsideTriangle(TriangleP[j], TriangleQ[0], TriangleQ[1], TriangleQ[2]) ){
-
+  for (j = 0; j < 3; j++) {
+    if (CheckPointInsideTriangle(TriangleP[j], TriangleQ[0], TriangleQ[1], TriangleQ[2])) {
       // Then P1 is also inside triangle Q, so store it
-      for(iDim = 0; iDim < nDim; iDim++)
-        points[nPoints][iDim] = TriangleP[j][iDim];
+      for (iDim = 0; iDim < nDim; iDim++) points[nPoints][iDim] = TriangleP[j][iDim];
 
       nPoints++;
     }
   }
 
-  for( j = 0; j < 3; j++){
-    if( CheckPointInsideTriangle(TriangleQ[j], TriangleP[0], TriangleP[1], TriangleP[2]) ){
-
+  for (j = 0; j < 3; j++) {
+    if (CheckPointInsideTriangle(TriangleQ[j], TriangleP[0], TriangleP[1], TriangleP[2])) {
       // Then Q1 is also inside triangle P, so store it
-      for(iDim = 0; iDim < nDim; iDim++)
-        points[nPoints][iDim] = TriangleQ[j][iDim];
+      for (iDim = 0; iDim < nDim; iDim++) points[nPoints][iDim] = TriangleQ[j][iDim];
 
       nPoints++;
     }
   }
 
-
   // Compute all edge intersections
 
-  for( j = 0; j < 3; j++){
-    for( i = 0; i < 3; i++){
+  for (j = 0; j < 3; j++) {
+    for (i = 0; i < 3; i++) {
+      det = (TriangleP[j][0] - TriangleP[j + 1][0]) * (TriangleQ[i][1] - TriangleQ[i + 1][1]) -
+            (TriangleP[j][1] - TriangleP[j + 1][1]) * (TriangleQ[i][0] - TriangleQ[i + 1][0]);
 
-      det = (TriangleP[j][0] - TriangleP[j+1][0]) * (TriangleQ[i][1] - TriangleQ[i+1][1]) -
-            (TriangleP[j][1] - TriangleP[j+1][1]) * (TriangleQ[i][0] - TriangleQ[i+1][0]);
-
-      if ( det != 0.0 ){
-        ComputeLineIntersectionPoint( TriangleP[j], TriangleP[j+1], TriangleQ[i], TriangleQ[i+1], IntersectionPoint );
+      if (det != 0.0) {
+        ComputeLineIntersectionPoint(TriangleP[j], TriangleP[j + 1], TriangleQ[i], TriangleQ[i + 1], IntersectionPoint);
 
         dot1 = 0;
         dot2 = 0;
-        for(iDim = 0; iDim < nDim; iDim++){
-          dot1 += ( TriangleP[j][iDim] - IntersectionPoint[iDim] ) * ( TriangleP[j+1][iDim] - IntersectionPoint[iDim] );
-          dot2 += ( TriangleQ[i][iDim] - IntersectionPoint[iDim] ) * ( TriangleQ[i+1][iDim] - IntersectionPoint[iDim] );
+        for (iDim = 0; iDim < nDim; iDim++) {
+          dot1 += (TriangleP[j][iDim] - IntersectionPoint[iDim]) * (TriangleP[j + 1][iDim] - IntersectionPoint[iDim]);
+          dot2 += (TriangleQ[i][iDim] - IntersectionPoint[iDim]) * (TriangleQ[i + 1][iDim] - IntersectionPoint[iDim]);
         }
 
-       if( dot1 <= 0 && dot2 <= 0 ){ // It found one intersection
+        if (dot1 <= 0 && dot2 <= 0) {  // It found one intersection
 
-         // Store temporarily the intersection point
+          // Store temporarily the intersection point
 
-         for(iDim = 0; iDim < nDim; iDim++)
-           points[nPoints][iDim] = IntersectionPoint[iDim];
+          for (iDim = 0; iDim < nDim; iDim++) points[nPoints][iDim] = IntersectionPoint[iDim];
 
-         nPoints++;
-       }
-     }
-   }
- }
+          nPoints++;
+        }
+      }
+    }
+  }
 
   // Remove double points, if any
 
-  for( i = 0; i < nPoints; i++){
-    for( j = i+1; j < nPoints; j++){
-      if(points[j][0] == points[i][0] && points[j][1] == points[i][1]){
-        for( k = j; k < nPoints-1; k++){
-          points[k][0] = points[k+1][0];
-          points[k][1] = points[k+1][1];
+  for (i = 0; i < nPoints; i++) {
+    for (j = i + 1; j < nPoints; j++) {
+      if (points[j][0] == points[i][0] && points[j][1] == points[i][1]) {
+        for (k = j; k < nPoints - 1; k++) {
+          points[k][0] = points[k + 1][0];
+          points[k][1] = points[k + 1][1];
         }
         nPoints--;
         j--;
@@ -1050,31 +1003,27 @@ su2double CSlidingMesh::ComputeIntersectionArea(const su2double* P1, const su2do
 
   // Re-order nodes
 
-  for( i = 1; i < nPoints; i++){ // Change again reference frame
-    for(iDim = 0; iDim < nDim; iDim++)
-      points[i][iDim] -= points[0][iDim];
+  for (i = 1; i < nPoints; i++) {  // Change again reference frame
+    for (iDim = 0; iDim < nDim; iDim++) points[i][iDim] -= points[0][iDim];
 
     // Compute polar azimuth for each node but the first
     theta[i] = atan2(points[i][1], points[i][0]);
   }
 
-  for(iDim = 0; iDim < nDim; iDim++)
-    points[0][iDim] = 0;
-
-  for( i = 1; i < nPoints; i++){
+  for (iDim = 0; iDim < nDim; iDim++) points[0][iDim] = 0;
 
+  for (i = 1; i < nPoints; i++) {
     min_theta = theta[i];
     min_theta_index = 0;
 
-    for( j = i + 1; j < nPoints; j++){
-
-      if( theta[j] < min_theta ){
+    for (j = i + 1; j < nPoints; j++) {
+      if (theta[j] < min_theta) {
         min_theta = theta[j];
         min_theta_index = j;
       }
     }
 
-    if( min_theta_index != 0 ){
+    if (min_theta_index != 0) {
       dtmp = theta[i];
       theta[i] = theta[min_theta_index];
       theta[min_theta_index] = dtmp;
@@ -1094,39 +1043,39 @@ su2double CSlidingMesh::ComputeIntersectionArea(const su2double* P1, const su2do
 
   Area = 0;
 
-  if (nPoints > 2){
-    for( i = 1; i < nPoints-1; i++ ){
-
+  if (nPoints > 2) {
+    for (i = 1; i < nPoints - 1; i++) {
       // Ax*By
-      Area += ( points[i][0] - points[0][0] ) * ( points[i+1][1] - points[0][1] );
+      Area += (points[i][0] - points[0][0]) * (points[i + 1][1] - points[0][1]);
 
       // Ay*Bx
-      Area -= ( points[i][1] - points[0][1] ) * ( points[i+1][0] - points[0][0] );
+      Area -= (points[i][1] - points[0][1]) * (points[i + 1][0] - points[0][0]);
     }
   }
 
-  return fabs(Area)/2;
+  return fabs(Area) / 2;
 }
 
 void CSlidingMesh::ComputeLineIntersectionPoint(const su2double* A1, const su2double* A2, const su2double* B1,
-                                                const su2double* B2, su2double* IntersectionPoint ){
-
+                                                const su2double* B2, su2double* IntersectionPoint) {
   /* --- Uses determinant rule to compute the intersection point between 2 straight segments --- */
-  /* This works only for lines on a 2D plane, A1, A2 and B1, B2 are respectively the head and the tail points of each segment,
-   * since they're on a 2D plane they are defined by a 2-elements array containing their coordinates */
+  /* This works only for lines on a 2D plane, A1, A2 and B1, B2 are respectively the head and the tail points of each
+   * segment, since they're on a 2D plane they are defined by a 2-elements array containing their coordinates */
 
   su2double det;
 
   det = (A1[0] - A2[0]) * (B1[1] - B2[1]) - (A1[1] - A2[1]) * (B1[0] - B2[0]);
 
-  if ( det != 0.0 ){ // else there is no intersection point
-    IntersectionPoint[0] = ( ( A1[0]*A2[1] - A1[1]*A2[0] ) * ( B1[0] - B2[0] ) - ( B1[0]*B2[1] - B1[1]*B2[0] ) * ( A1[0] - A2[0] ) ) / det;
-    IntersectionPoint[1] = ( ( A1[0]*A2[1] - A1[1]*A2[0] ) * ( B1[1] - B2[1] ) - ( B1[0]*B2[1] - B1[1]*B2[0] ) * ( A1[1] - A2[1] ) ) / det;
+  if (det != 0.0) {  // else there is no intersection point
+    IntersectionPoint[0] =
+        ((A1[0] * A2[1] - A1[1] * A2[0]) * (B1[0] - B2[0]) - (B1[0] * B2[1] - B1[1] * B2[0]) * (A1[0] - A2[0])) / det;
+    IntersectionPoint[1] =
+        ((A1[0] * A2[1] - A1[1] * A2[0]) * (B1[1] - B2[1]) - (B1[0] * B2[1] - B1[1] * B2[0]) * (A1[1] - A2[1])) / det;
   }
 }
 
-bool CSlidingMesh::CheckPointInsideTriangle(const su2double* Point, const su2double* T1, const su2double* T2, const su2double* T3) {
-
+bool CSlidingMesh::CheckPointInsideTriangle(const su2double* Point, const su2double* T1, const su2double* T2,
+                                            const su2double* T3) {
   /* --- Check whether a point "Point" lies inside or outside a triangle defined by 3 points "T1", "T2", "T3" --- */
   /* For each edge it checks on which side the point lies:
    * - Computes the unit vector pointing at the internal side of the edge
@@ -1140,14 +1089,14 @@ bool CSlidingMesh::CheckPointInsideTriangle(const su2double* Point, const su2dou
   su2double vect1[2], vect2[2], r[2];
   su2double dot;
 
-  constexpr unsigned short nDim  = 2;
+  constexpr unsigned short nDim = 2;
 
   /* --- Check first edge --- */
 
   dot = 0;
-  for(iDim = 0; iDim < nDim; iDim++){
-    vect1[iDim] = T3[iDim] - T1[iDim]; // vec 1 is aligned to the edge
-    vect2[iDim] = T2[iDim] - T1[iDim]; // vect 2 is the vector connecting one edge point to the third triangle vertex
+  for (iDim = 0; iDim < nDim; iDim++) {
+    vect1[iDim] = T3[iDim] - T1[iDim];  // vec 1 is aligned to the edge
+    vect2[iDim] = T2[iDim] - T1[iDim];  // vect 2 is the vector connecting one edge point to the third triangle vertex
 
     r[iDim] = Point[iDim] - T1[iDim];  // Connects point to vertex T1
 
@@ -1155,27 +1104,24 @@ bool CSlidingMesh::CheckPointInsideTriangle(const su2double* Point, const su2dou
   }
   dot = sqrt(dot);
 
-  for(iDim = 0; iDim < nDim; iDim++)
-    vect2[iDim] /= dot;
+  for (iDim = 0; iDim < nDim; iDim++) vect2[iDim] /= dot;
 
   dot = 0;
-  for(iDim = 0; iDim < nDim; iDim++)
-    dot += vect1[iDim] * vect2[iDim];
+  for (iDim = 0; iDim < nDim; iDim++) dot += vect1[iDim] * vect2[iDim];
 
-  for(iDim = 0; iDim < nDim; iDim++)
-    vect1[iDim] = T3[iDim] - (T1[iDim] + dot * vect2[iDim]); // Computes the inward unit vector
+  for (iDim = 0; iDim < nDim; iDim++)
+    vect1[iDim] = T3[iDim] - (T1[iDim] + dot * vect2[iDim]);  // Computes the inward unit vector
 
   dot = 0;
-  for(iDim = 0; iDim < nDim; iDim++)  // Checs that the point lies on the internal plane
+  for (iDim = 0; iDim < nDim; iDim++)  // Checs that the point lies on the internal plane
     dot += vect1[iDim] * r[iDim];
 
-  if (dot >= 0)
-    check++;
+  if (dot >= 0) check++;
 
   /* --- Check second edge --- */
 
   dot = 0;
-  for(iDim = 0; iDim < nDim; iDim++){
+  for (iDim = 0; iDim < nDim; iDim++) {
     vect1[iDim] = T1[iDim] - T2[iDim];
     vect2[iDim] = T3[iDim] - T2[iDim];
 
@@ -1185,27 +1131,22 @@ bool CSlidingMesh::CheckPointInsideTriangle(const su2double* Point, const su2dou
   }
   dot = sqrt(dot);
 
-  for(iDim = 0; iDim < nDim; iDim++)
-    vect2[iDim] /= dot;
+  for (iDim = 0; iDim < nDim; iDim++) vect2[iDim] /= dot;
 
   dot = 0;
-  for(iDim = 0; iDim < nDim; iDim++)
-    dot += vect1[iDim] * vect2[iDim];
+  for (iDim = 0; iDim < nDim; iDim++) dot += vect1[iDim] * vect2[iDim];
 
-  for(iDim = 0; iDim < nDim; iDim++)
-    vect1[iDim] = T1[iDim] - (T2[iDim] + dot * vect2[iDim]);
+  for (iDim = 0; iDim < nDim; iDim++) vect1[iDim] = T1[iDim] - (T2[iDim] + dot * vect2[iDim]);
 
   dot = 0;
-  for(iDim = 0; iDim < nDim; iDim++)
-    dot += vect1[iDim] * r[iDim];
+  for (iDim = 0; iDim < nDim; iDim++) dot += vect1[iDim] * r[iDim];
 
-  if (dot >= 0)
-    check++;
+  if (dot >= 0) check++;
 
   /* --- Check third edge --- */
 
   dot = 0;
-  for(iDim = 0; iDim < nDim; iDim++){
+  for (iDim = 0; iDim < nDim; iDim++) {
     vect1[iDim] = T2[iDim] - T3[iDim];
     vect2[iDim] = T1[iDim] - T3[iDim];
 
@@ -1215,22 +1156,17 @@ bool CSlidingMesh::CheckPointInsideTriangle(const su2double* Point, const su2dou
   }
   dot = sqrt(dot);
 
-  for(iDim = 0; iDim < nDim; iDim++)
-    vect2[iDim] /= dot;
+  for (iDim = 0; iDim < nDim; iDim++) vect2[iDim] /= dot;
 
   dot = 0;
-  for(iDim = 0; iDim < nDim; iDim++)
-    dot += vect1[iDim] * vect2[iDim];
+  for (iDim = 0; iDim < nDim; iDim++) dot += vect1[iDim] * vect2[iDim];
 
-  for(iDim = 0; iDim < nDim; iDim++)
-    vect1[iDim] = T2[iDim] - (T3[iDim] + dot * vect2[iDim]);
+  for (iDim = 0; iDim < nDim; iDim++) vect1[iDim] = T2[iDim] - (T3[iDim] + dot * vect2[iDim]);
 
   dot = 0;
-  for(iDim = 0; iDim < nDim; iDim++)
-    dot += vect1[iDim] * r[iDim];
+  for (iDim = 0; iDim < nDim; iDim++) dot += vect1[iDim] * r[iDim];
 
-  if (dot >= 0)
-    check++;
+  if (dot >= 0) check++;
 
   return (check == 3);
 }
diff --git a/Common/src/linear_algebra/CPastixWrapper.cpp b/Common/src/linear_algebra/CPastixWrapper.cpp
index 9cf791cbdd9..8500c44445a 100644
--- a/Common/src/linear_algebra/CPastixWrapper.cpp
+++ b/Common/src/linear_algebra/CPastixWrapper.cpp
@@ -34,33 +34,29 @@
 #include "../../include/geometry/CGeometry.hpp"
 #include "../../include/linear_algebra/CPastixWrapper.hpp"
 
-#include<numeric>
-
-template<class ScalarType>
-void CPastixWrapper<ScalarType>::Initialize(CGeometry *geometry, const CConfig *config) {
+#include <numeric>
 
+template <class ScalarType>
+void CPastixWrapper<ScalarType>::Initialize(CGeometry* geometry, const CConfig* config) {
   using namespace PaStiX;
 
-  if (isinitialized) return; // only need to do this once
+  if (isinitialized) return;  // only need to do this once
 
-  unsigned long nVar = matrix.nVar,
-                nPoint = matrix.nPoint,
-                nPointDomain = matrix.nPointDomain;
-  const unsigned long *row_ptr = matrix.rowptr,
-                      *col_ind = matrix.colidx;
+  unsigned long nVar = matrix.nVar, nPoint = matrix.nPoint, nPointDomain = matrix.nPointDomain;
+  const unsigned long *row_ptr = matrix.rowptr, *col_ind = matrix.colidx;
 
   unsigned long iPoint, offset = 0, nNonZero = row_ptr[nPointDomain];
 
   /*--- Allocate ---*/
 
   nCols = pastix_int_t(nPointDomain);
-  colptr.resize(nPointDomain+1);
+  colptr.resize(nPointDomain + 1);
   rowidx.clear();
   rowidx.reserve(nNonZero);
-  values.resize(nNonZero*nVar*nVar);
+  values.resize(nNonZero * nVar * nVar);
   loc2glb.resize(nPointDomain);
   perm.resize(nPointDomain);
-  workvec.resize(nPointDomain*nVar);
+  workvec.resize(nPointDomain * nVar);
 
   /*--- Set default parameter values ---*/
 
@@ -72,25 +68,25 @@ void CPastixWrapper<ScalarType>::Initialize(CGeometry *geometry, const CConfig *
   /*--- Customize important parameters ---*/
 
   switch (verb) {
-  case 1:
-    iparm[IPARM_VERBOSE] = API_VERBOSE_NO;
-    break;
-  case 2:
-    iparm[IPARM_VERBOSE] = API_VERBOSE_YES;
-    break;
-  default:
-    iparm[IPARM_VERBOSE] = API_VERBOSE_NOT;
-    break;
+    case 1:
+      iparm[IPARM_VERBOSE] = API_VERBOSE_NO;
+      break;
+    case 2:
+      iparm[IPARM_VERBOSE] = API_VERBOSE_YES;
+      break;
+    default:
+      iparm[IPARM_VERBOSE] = API_VERBOSE_NOT;
+      break;
   }
-  iparm[IPARM_DOF_NBR]             = pastix_int_t(nVar);
+  iparm[IPARM_DOF_NBR] = pastix_int_t(nVar);
   iparm[IPARM_MATRIX_VERIFICATION] = API_NO;
-  iparm[IPARM_FREE_CSCPASTIX]      = API_CSC_FREE;
-  iparm[IPARM_CSCD_CORRECT]        = API_NO;
-  iparm[IPARM_RHSD_CHECK]          = API_NO;
-  iparm[IPARM_ORDERING]            = API_ORDER_PTSCOTCH;
-  iparm[IPARM_INCOMPLETE]          = incomplete;
-  iparm[IPARM_LEVEL_OF_FILL]       = pastix_int_t(config->GetPastixFillLvl());
-  iparm[IPARM_THREAD_NBR]          = omp_get_max_threads();
+  iparm[IPARM_FREE_CSCPASTIX] = API_CSC_FREE;
+  iparm[IPARM_CSCD_CORRECT] = API_NO;
+  iparm[IPARM_RHSD_CHECK] = API_NO;
+  iparm[IPARM_ORDERING] = API_ORDER_PTSCOTCH;
+  iparm[IPARM_INCOMPLETE] = incomplete;
+  iparm[IPARM_LEVEL_OF_FILL] = pastix_int_t(config->GetPastixFillLvl());
+  iparm[IPARM_THREAD_NBR] = omp_get_max_threads();
 #if defined(HAVE_MPI) && defined(HAVE_OMP)
   int comm_mode = MPI_THREAD_SINGLE;
   MPI_Query_thread(&comm_mode);
@@ -100,40 +96,37 @@ void CPastixWrapper<ScalarType>::Initialize(CGeometry *geometry, const CConfig *
     iparm[IPARM_THREAD_COMM_MODE] = API_THREAD_FUNNELED;
 #endif
 
-  /*--- Prepare sparsity structure ---*/
+    /*--- Prepare sparsity structure ---*/
 
-  /*--- We need it in global coordinates, i.e. shifted according to the position
-   of the current rank in the linear partitioning space, and "unpacked" halo part.
-   The latter forces us to re-sort the column indices of rows with halo points, which
-   in turn requires blocks to be swapped accordingly. Moreover we need "pointer" and
-   indices in Fortran-style numbering (start at 1), effectively the matrix is copied.
-   Here we prepare the pointer and index part, and map the required swaps. ---*/
+    /*--- We need it in global coordinates, i.e. shifted according to the position
+     of the current rank in the linear partitioning space, and "unpacked" halo part.
+     The latter forces us to re-sort the column indices of rows with halo points, which
+     in turn requires blocks to be swapped accordingly. Moreover we need "pointer" and
+     indices in Fortran-style numbering (start at 1), effectively the matrix is copied.
+     Here we prepare the pointer and index part, and map the required swaps. ---*/
 
-   /*--- 1 - Determine position in the linear partitioning ---*/
+    /*--- 1 - Determine position in the linear partitioning ---*/
 
 #ifdef HAVE_MPI
   vector<unsigned long> domain_sizes(mpi_size);
   MPI_Allgather(&nPointDomain, 1, MPI_UNSIGNED_LONG, domain_sizes.data(), 1, MPI_UNSIGNED_LONG, SU2_MPI::GetComm());
-  for (int i=0; i<mpi_rank; ++i) offset += domain_sizes[i];
+  for (int i = 0; i < mpi_rank; ++i) offset += domain_sizes[i];
 #endif
 
-  iota(loc2glb.begin(), loc2glb.end(), offset+1);
+  iota(loc2glb.begin(), loc2glb.end(), offset + 1);
 
   /*--- 2 - Communicate global indices of halo points to then renumber
    column indices from local to global when unpacking halos. ---*/
 
-  vector<pastix_int_t> map(nPoint-nPointDomain,0);
+  vector<pastix_int_t> map(nPoint - nPointDomain, 0);
 
 #ifdef HAVE_MPI
-  for (unsigned short iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++)
-  {
-    if ((config->GetMarker_All_KindBC(iMarker) == SEND_RECEIVE) &&
-        (config->GetMarker_All_SendRecv(iMarker) > 0))
-    {
-      unsigned short MarkerS = iMarker, MarkerR = iMarker+1;
+  for (unsigned short iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
+    if ((config->GetMarker_All_KindBC(iMarker) == SEND_RECEIVE) && (config->GetMarker_All_SendRecv(iMarker) > 0)) {
+      unsigned short MarkerS = iMarker, MarkerR = iMarker + 1;
 
-      int sender = config->GetMarker_All_SendRecv(MarkerS)-1;
-      int recver = abs(config->GetMarker_All_SendRecv(MarkerR))-1;
+      int sender = config->GetMarker_All_SendRecv(MarkerS) - 1;
+      int recver = abs(config->GetMarker_All_SendRecv(MarkerR)) - 1;
 
       unsigned long nVertexS = geometry->nVertex[MarkerS];
       unsigned long nVertexR = geometry->nVertex[MarkerR];
@@ -143,34 +136,31 @@ void CPastixWrapper<ScalarType>::Initialize(CGeometry *geometry, const CConfig *
 
       /*--- Prepare data to send ---*/
       for (unsigned long iVertex = 0; iVertex < nVertexS; iVertex++)
-        Buffer_Send[iVertex] = geometry->vertex[MarkerS][iVertex]->GetNode()+offset;
+        Buffer_Send[iVertex] = geometry->vertex[MarkerS][iVertex]->GetNode() + offset;
 
       /*--- Send and Receive data ---*/
-      MPI_Sendrecv(Buffer_Send.data(), nVertexS, MPI_UNSIGNED_LONG, sender, 0,
-                   Buffer_Recv.data(), nVertexR, MPI_UNSIGNED_LONG, recver, 0,
-                   SU2_MPI::GetComm(), MPI_STATUS_IGNORE);
+      MPI_Sendrecv(Buffer_Send.data(), nVertexS, MPI_UNSIGNED_LONG, sender, 0, Buffer_Recv.data(), nVertexR,
+                   MPI_UNSIGNED_LONG, recver, 0, SU2_MPI::GetComm(), MPI_STATUS_IGNORE);
 
       /*--- Store received data---*/
       for (unsigned long iVertex = 0; iVertex < nVertexR; iVertex++)
-        map[ geometry->vertex[MarkerR][iVertex]->GetNode()-nPointDomain ] = Buffer_Recv[iVertex];
+        map[geometry->vertex[MarkerR][iVertex]->GetNode() - nPointDomain] = Buffer_Recv[iVertex];
     }
   }
 #endif
 
   /*--- 3 - Copy, map the sparsity, and put it in Fortran numbering ---*/
 
-  for (iPoint = 0; iPoint < nPointDomain; ++iPoint)
-  {
-    colptr[iPoint] = pastix_int_t(row_ptr[iPoint]+1);
+  for (iPoint = 0; iPoint < nPointDomain; ++iPoint) {
+    colptr[iPoint] = pastix_int_t(row_ptr[iPoint] + 1);
 
-    unsigned long begin = row_ptr[iPoint], end = row_ptr[iPoint+1], j;
+    unsigned long begin = row_ptr[iPoint], end = row_ptr[iPoint + 1], j;
 
     /*--- If last point of row is halo ---*/
-    bool sort_required = (col_ind[end-1] >= nPointDomain);
+    bool sort_required = (col_ind[end - 1] >= nPointDomain);
 
-    if (sort_required)
-    {
-      unsigned long nnz_row = end-begin;
+    if (sort_required) {
+      unsigned long nnz_row = end - begin;
 
       sort_rows.push_back(iPoint);
       sort_order.push_back(vector<unsigned long>(nnz_row));
@@ -178,42 +168,36 @@ void CPastixWrapper<ScalarType>::Initialize(CGeometry *geometry, const CConfig *
       /*--- Sort mapped indices ("first") and keep track of source ("second")
             for when we later need to swap blocks for these rows. ---*/
 
-      vector<pair<pastix_int_t,unsigned long> > aux(nnz_row);
+      vector<pair<pastix_int_t, unsigned long> > aux(nnz_row);
 
-      for (j = begin; j < end; ++j)
-      {
+      for (j = begin; j < end; ++j) {
         if (col_ind[j] < nPointDomain)
-          aux[j-begin].first = pastix_int_t(offset+col_ind[j]+1);
+          aux[j - begin].first = pastix_int_t(offset + col_ind[j] + 1);
         else
-          aux[j-begin].first = pastix_int_t(map[col_ind[j]-nPointDomain]+1);
-        aux[j-begin].second = j;
+          aux[j - begin].first = pastix_int_t(map[col_ind[j] - nPointDomain] + 1);
+        aux[j - begin].second = j;
       }
       sort(aux.begin(), aux.end());
 
-      for (j = 0; j < nnz_row; ++j)
-      {
+      for (j = 0; j < nnz_row; ++j) {
         rowidx.push_back(aux[j].first);
         sort_order.back()[j] = aux[j].second;
       }
-    }
-    else
-    {
+    } else {
       /*--- These are all internal, no need to go through map. ---*/
-      for (j = begin; j < end; ++j)
-        rowidx.push_back(pastix_int_t(offset+col_ind[j]+1));
+      for (j = begin; j < end; ++j) rowidx.push_back(pastix_int_t(offset + col_ind[j] + 1));
     }
   }
-  colptr[nPointDomain] = pastix_int_t(nNonZero+1);
+  colptr[nPointDomain] = pastix_int_t(nNonZero + 1);
 
-  if (rowidx.size() != nNonZero)
-    SU2_MPI::Error("Error during preparation of PaStiX data", CURRENT_FUNCTION);
+  if (rowidx.size() != nNonZero) SU2_MPI::Error("Error during preparation of PaStiX data", CURRENT_FUNCTION);
 
   /*--- 4 - Perform ordering, symbolic factorization, and analysis steps ---*/
 
   if (mpi_rank == MASTER_NODE && verb > 0) cout << endl;
 
   iparm[IPARM_START_TASK] = API_TASK_ORDERING;
-  iparm[IPARM_END_TASK]   = API_TASK_ANALYSE;
+  iparm[IPARM_END_TASK] = API_TASK_ANALYSE;
   Run();
 
   if (mpi_rank == MASTER_NODE && verb > 0)
@@ -222,18 +206,17 @@ void CPastixWrapper<ScalarType>::Initialize(CGeometry *geometry, const CConfig *
   isinitialized = true;
 }
 
-template<class ScalarType>
-void CPastixWrapper<ScalarType>::Factorize(CGeometry *geometry, const CConfig *config,
-                                           unsigned short kind_fact) {
+template <class ScalarType>
+void CPastixWrapper<ScalarType>::Factorize(CGeometry* geometry, const CConfig* config, unsigned short kind_fact) {
   using namespace PaStiX;
 
   /*--- Detect a possible change of settings between direct and adjoint that requires a reset ---*/
   if (isinitialized)
-  if ((kind_fact == PASTIX_ILU) != (iparm[IPARM_INCOMPLETE] == API_YES)) {
-    Clean();
-    isinitialized = false;
-    iter = 0;
-  }
+    if ((kind_fact == PASTIX_ILU) != (iparm[IPARM_INCOMPLETE] == API_YES)) {
+      Clean();
+      isinitialized = false;
+      iter = 0;
+    }
 
   verb = config->GetPastixVerbLvl();
   iparm[IPARM_INCOMPLETE] = (kind_fact == PASTIX_ILU);
@@ -243,31 +226,30 @@ void CPastixWrapper<ScalarType>::Factorize(CGeometry *geometry, const CConfig *c
   /*--- Set some options that affect "compute" and could (one day) change during run ---*/
 
   switch (verb) {
-  case 1:
-    iparm[IPARM_VERBOSE] = API_VERBOSE_NO;
-    break;
-  case 2:
-    iparm[IPARM_VERBOSE] = API_VERBOSE_YES;
-    break;
-  default:
-    iparm[IPARM_VERBOSE] = API_VERBOSE_NOT;
-    break;
+    case 1:
+      iparm[IPARM_VERBOSE] = API_VERBOSE_NO;
+      break;
+    case 2:
+      iparm[IPARM_VERBOSE] = API_VERBOSE_YES;
+      break;
+    default:
+      iparm[IPARM_VERBOSE] = API_VERBOSE_NOT;
+      break;
   }
 
   if (kind_fact == PASTIX_LDLT || kind_fact == PASTIX_LDLT_P)
-    iparm[IPARM_TRANSPOSE_SOLVE] = API_NO; // symmetric so no need for slower transp. solve
+    iparm[IPARM_TRANSPOSE_SOLVE] = API_NO;  // symmetric so no need for slower transp. solve
   else
-    iparm[IPARM_TRANSPOSE_SOLVE] = API_YES; // negated due to CSR to CSC copy
+    iparm[IPARM_TRANSPOSE_SOLVE] = API_YES;  // negated due to CSR to CSC copy
 
   /*--- Is factorizing needed on this iteration? ---*/
 
   bool factorize = false;
-  if (config->GetPastixFactFreq() != 0)
-    factorize = (iter % config->GetPastixFactFreq() == 0);
+  if (config->GetPastixFactFreq() != 0) factorize = (iter % config->GetPastixFactFreq() == 0);
 
   iter++;
 
-  if (isfactorized && !factorize) return; // No
+  if (isfactorized && !factorize) return;  // No
 
   /*--- Yes ---*/
 
@@ -278,49 +260,47 @@ void CPastixWrapper<ScalarType>::Factorize(CGeometry *geometry, const CConfig *c
     cout << " +--------------------------------------------------------------------+" << endl;
   }
 
-  unsigned long i, j, k, iRow, begin, target, source,
-                szBlk = matrix.nVar*matrix.nVar, nNonZero = values.size();
+  unsigned long i, j, k, iRow, begin, target, source, szBlk = matrix.nVar * matrix.nVar, nNonZero = values.size();
 
   /*--- Copy matrix values and swap blocks as required ---*/
 
-  for (i = 0; i < nNonZero; ++i)
-    values[i] = SU2_TYPE::GetValue(matrix.values[i]);
+  for (i = 0; i < nNonZero; ++i) values[i] = SU2_TYPE::GetValue(matrix.values[i]);
 
-  for (i = 0; i < sort_rows.size(); ++i)
-  {
+  for (i = 0; i < sort_rows.size(); ++i) {
     iRow = sort_rows[i];
     begin = matrix.rowptr[iRow];
 
-    for (j = 0; j < sort_order[i].size(); ++j)
-    {
-      target = (begin+j)*szBlk;
-      source = sort_order[i][j]*szBlk;
+    for (j = 0; j < sort_order[i].size(); ++j) {
+      target = (begin + j) * szBlk;
+      source = sort_order[i][j] * szBlk;
 
-      for (k = 0; k < szBlk; ++k)
-        values[target+k] = SU2_TYPE::GetValue(matrix.values[source+k]);
+      for (k = 0; k < szBlk; ++k) values[target + k] = SU2_TYPE::GetValue(matrix.values[source + k]);
     }
   }
 
   /*--- Set factorization options ---*/
 
   switch (kind_fact) {
-  case PASTIX_LDLT: case PASTIX_LDLT_P:
-    iparm[IPARM_SYM]           = API_SYM_YES;
-    iparm[IPARM_FACTORIZATION] = API_FACT_LDLT;
-    break;
-  case PASTIX_LU: case PASTIX_LU_P: case PASTIX_ILU:
-    iparm[IPARM_SYM]           = API_SYM_NO;
-    iparm[IPARM_FACTORIZATION] = API_FACT_LU;
-    break;
-  default:
-    SU2_MPI::Error("Unknown type of PaStiX factorization.", CURRENT_FUNCTION);
-    break;
+    case PASTIX_LDLT:
+    case PASTIX_LDLT_P:
+      iparm[IPARM_SYM] = API_SYM_YES;
+      iparm[IPARM_FACTORIZATION] = API_FACT_LDLT;
+      break;
+    case PASTIX_LU:
+    case PASTIX_LU_P:
+    case PASTIX_ILU:
+      iparm[IPARM_SYM] = API_SYM_NO;
+      iparm[IPARM_FACTORIZATION] = API_FACT_LU;
+      break;
+    default:
+      SU2_MPI::Error("Unknown type of PaStiX factorization.", CURRENT_FUNCTION);
+      break;
   }
 
   /*--- Compute factorization ---*/
 
   iparm[IPARM_START_TASK] = API_TASK_NUMFACT;
-  iparm[IPARM_END_TASK]   = API_TASK_NUMFACT;
+  iparm[IPARM_END_TASK] = API_TASK_NUMFACT;
   Run();
 
   if (mpi_rank == MASTER_NODE && verb > 0)
diff --git a/Common/src/linear_algebra/CSysMatrix.cpp b/Common/src/linear_algebra/CSysMatrix.cpp
index a03797b64c7..fa84ecfa131 100644
--- a/Common/src/linear_algebra/CSysMatrix.cpp
+++ b/Common/src/linear_algebra/CSysMatrix.cpp
@@ -32,86 +32,77 @@
 
 #include <cmath>
 
-template<class ScalarType>
-CSysMatrix<ScalarType>::CSysMatrix() :
-  rank(SU2_MPI::GetRank()),
-  size(SU2_MPI::GetSize()) {
-
+template <class ScalarType>
+CSysMatrix<ScalarType>::CSysMatrix() : rank(SU2_MPI::GetRank()), size(SU2_MPI::GetSize()) {
   nPoint = nPointDomain = nVar = nEqn = 0;
   nnz = nnz_ilu = 0;
   ilu_fill_in = 0;
 
-  omp_partitions    = nullptr;
+  omp_partitions = nullptr;
 
-  matrix            = nullptr;
-  row_ptr           = nullptr;
-  dia_ptr           = nullptr;
-  col_ind           = nullptr;
-  col_ptr           = nullptr;
+  matrix = nullptr;
+  row_ptr = nullptr;
+  dia_ptr = nullptr;
+  col_ind = nullptr;
+  col_ptr = nullptr;
 
-  ILU_matrix        = nullptr;
-  row_ptr_ilu       = nullptr;
-  dia_ptr_ilu       = nullptr;
-  col_ind_ilu       = nullptr;
+  ILU_matrix = nullptr;
+  row_ptr_ilu = nullptr;
+  dia_ptr_ilu = nullptr;
+  col_ind_ilu = nullptr;
 
-  invM              = nullptr;
+  invM = nullptr;
 
 #ifdef USE_MKL
-  MatrixMatrixProductJitter              = nullptr;
-  MatrixVectorProductJitterBetaOne       = nullptr;
-  MatrixVectorProductJitterBetaZero      = nullptr;
+  MatrixMatrixProductJitter = nullptr;
+  MatrixVectorProductJitterBetaOne = nullptr;
+  MatrixVectorProductJitterBetaZero = nullptr;
   MatrixVectorProductJitterAlphaMinusOne = nullptr;
 #endif
-
 }
 
-template<class ScalarType>
+template <class ScalarType>
 CSysMatrix<ScalarType>::~CSysMatrix(void) {
-
-  delete [] omp_partitions;
+  delete[] omp_partitions;
   MemoryAllocation::aligned_free(ILU_matrix);
   MemoryAllocation::aligned_free(matrix);
   MemoryAllocation::aligned_free(invM);
 
 #ifdef USE_MKL
-  mkl_jit_destroy( MatrixMatrixProductJitter );
-  mkl_jit_destroy( MatrixVectorProductJitterBetaZero );
-  mkl_jit_destroy( MatrixVectorProductJitterBetaOne );
-  mkl_jit_destroy( MatrixVectorProductJitterAlphaMinusOne );
+  mkl_jit_destroy(MatrixMatrixProductJitter);
+  mkl_jit_destroy(MatrixVectorProductJitterBetaZero);
+  mkl_jit_destroy(MatrixVectorProductJitterBetaOne);
+  mkl_jit_destroy(MatrixVectorProductJitterAlphaMinusOne);
 #endif
-
 }
 
-template<class ScalarType>
-void CSysMatrix<ScalarType>::Initialize(unsigned long npoint, unsigned long npointdomain,
-                                        unsigned short nvar, unsigned short neqn,
-                                        bool EdgeConnect, CGeometry *geometry,
-                                        const CConfig *config, bool needTranspPtr, bool grad_mode) {
-
-  assert(omp_get_thread_num()==0 && "Only the master thread is allowed to initialize the matrix.");
+template <class ScalarType>
+void CSysMatrix<ScalarType>::Initialize(unsigned long npoint, unsigned long npointdomain, unsigned short nvar,
+                                        unsigned short neqn, bool EdgeConnect, CGeometry* geometry,
+                                        const CConfig* config, bool needTranspPtr, bool grad_mode) {
+  assert(omp_get_thread_num() == 0 && "Only the master thread is allowed to initialize the matrix.");
 
-  if(npoint == 0) return;
+  if (npoint == 0) return;
 
-  if(matrix != nullptr) {
+  if (matrix != nullptr) {
     SU2_MPI::Error("CSysMatrix can only be initialized once.", CURRENT_FUNCTION);
   }
 
-  if(nvar > MAXNVAR) {
+  if (nvar > MAXNVAR) {
     SU2_MPI::Error("nVar larger than expected, increase MAXNVAR.", CURRENT_FUNCTION);
   }
 
   /*--- Application of this matrix, FVM or FEM. ---*/
-  const auto type = EdgeConnect? ConnectivityType::FiniteVolume : ConnectivityType::FiniteElement;
+  const auto type = EdgeConnect ? ConnectivityType::FiniteVolume : ConnectivityType::FiniteElement;
 
   /*--- Type of preconditioner the matrix will be asked to build. ---*/
   auto prec = config->GetKind_Linear_Solver_Prec();
 
-  if ((!EdgeConnect && !config->GetStructuralProblem()) ||
-      (config->GetKind_SU2() == SU2_COMPONENT::SU2_DEF) || (config->GetKind_SU2() == SU2_COMPONENT::SU2_DOT)) {
+  if ((!EdgeConnect && !config->GetStructuralProblem()) || (config->GetKind_SU2() == SU2_COMPONENT::SU2_DEF) ||
+      (config->GetKind_SU2() == SU2_COMPONENT::SU2_DOT)) {
     /*--- FEM-type connectivity in non-structural context implies mesh deformation. ---*/
     prec = config->GetKind_Deform_Linear_Solver_Prec();
-  }
-  else if (config->GetDiscrete_Adjoint() && (prec!=ILU)) {
+  } else if (config->GetDiscrete_Adjoint() && (prec != ILU)) {
     /*--- Else "upgrade" primal solver settings. ---*/
     prec = config->GetKind_DiscAdj_Linear_Prec();
   }
@@ -121,8 +112,8 @@ void CSysMatrix<ScalarType>::Initialize(unsigned long npoint, unsigned long npoi
     prec = config->GetKind_Grad_Linear_Solver_Prec();
   }
 
-  const bool ilu_needed = (prec==ILU);
-  const bool diag_needed = ilu_needed || (prec==JACOBI) || (prec==LINELET);
+  const bool ilu_needed = (prec == ILU);
+  const bool diag_needed = ilu_needed || (prec == JACOBI) || (prec == LINELET);
 
   /*--- Basic dimensions. ---*/
   nVar = nvar;
@@ -133,15 +124,14 @@ void CSysMatrix<ScalarType>::Initialize(unsigned long npoint, unsigned long npoi
   /*--- Get sparse structure pointers from geometry,
    *    the data is managed by CGeometry to allow re-use. ---*/
 
-  const auto& csr = geometry->GetSparsePattern(type,0);
+  const auto& csr = geometry->GetSparsePattern(type, 0);
 
   nnz = csr.getNumNonZeros();
   row_ptr = csr.outerPtr();
   col_ind = csr.innerIdx();
   dia_ptr = csr.diagPtr();
 
-  if (needTranspPtr)
-    col_ptr = geometry->GetTransposeSparsePatternMap(type).data();
+  if (needTranspPtr) col_ptr = geometry->GetTransposeSparsePatternMap(type).data();
 
   if (type == ConnectivityType::FiniteVolume) {
     edge_ptr.ptr = geometry->GetEdgeToSparsePatternMap().data();
@@ -150,8 +140,7 @@ void CSysMatrix<ScalarType>::Initialize(unsigned long npoint, unsigned long npoi
 
   /*--- Get ILU sparse pattern, if fill is 0 no new data is allocated. --*/
 
-  if(ilu_needed)
-  {
+  if (ilu_needed) {
     ilu_fill_in = config->GetLinear_Solver_ILU_n();
 
     const auto& csr_ilu = geometry->GetSparsePattern(type, ilu_fill_in);
@@ -164,16 +153,16 @@ void CSysMatrix<ScalarType>::Initialize(unsigned long npoint, unsigned long npoi
 
   /*--- Allocate data. ---*/
   auto allocAndInit = [](ScalarType*& ptr, unsigned long num) {
-    ptr = MemoryAllocation::aligned_alloc<ScalarType,true>(64, num*sizeof(ScalarType));
+    ptr = MemoryAllocation::aligned_alloc<ScalarType, true>(64, num * sizeof(ScalarType));
   };
 
-  allocAndInit(matrix, nnz*nVar*nEqn);
+  allocAndInit(matrix, nnz * nVar * nEqn);
 
   /*--- Preconditioners. ---*/
 
-  if (ilu_needed) allocAndInit(ILU_matrix, nnz_ilu*nVar*nEqn);
+  if (ilu_needed) allocAndInit(ILU_matrix, nnz_ilu * nVar * nEqn);
 
-  if (diag_needed) allocAndInit(invM, nPointDomain*nVar*nEqn);
+  if (diag_needed) allocAndInit(invM, nPointDomain * nVar * nEqn);
 
   /*--- Thread parallel initialization. ---*/
 
@@ -181,33 +170,34 @@ void CSysMatrix<ScalarType>::Initialize(unsigned long npoint, unsigned long npoi
 
   /*--- Set suitable chunk sizes for light static for loops, and heavy
    dynamic ones, such that threads are approximately evenly loaded. ---*/
-  omp_light_size = computeStaticChunkSize(nnz*nVar*nEqn, num_threads, OMP_MAX_SIZE_L);
+  omp_light_size = computeStaticChunkSize(nnz * nVar * nEqn, num_threads, OMP_MAX_SIZE_L);
   omp_heavy_size = computeStaticChunkSize(nPointDomain, num_threads, OMP_MAX_SIZE_H);
 
   omp_num_parts = config->GetLinear_Solver_Prec_Threads();
   if (omp_num_parts == 0) omp_num_parts = num_threads;
 
   /*--- This is akin to the row_ptr. ---*/
-  omp_partitions = new unsigned long [omp_num_parts+1];
+  omp_partitions = new unsigned long[omp_num_parts + 1];
   for (unsigned long i = 0; i <= omp_num_parts; ++i) omp_partitions[i] = nPointDomain;
 
   /*--- Work estimate based on non-zeros to produce balanced partitions. ---*/
 
-  const auto row_ptr_prec = ilu_needed? row_ptr_ilu : row_ptr;
+  const auto row_ptr_prec = ilu_needed ? row_ptr_ilu : row_ptr;
   const auto nnz_prec = row_ptr_prec[nPointDomain];
 
   const auto nnz_per_part = roundUpDiv(nnz_prec, omp_num_parts);
 
   for (auto iPoint = 0ul, part = 0ul; iPoint < nPointDomain; ++iPoint) {
-    if (row_ptr_prec[iPoint] >= part*nnz_per_part)
-      omp_partitions[part++] = iPoint;
+    if (row_ptr_prec[iPoint] >= part * nnz_per_part) omp_partitions[part++] = iPoint;
   }
 
   for (unsigned long thread = 0; thread < omp_num_parts; ++thread) {
     const auto begin = omp_partitions[thread];
     const auto end = omp_partitions[thread + 1];
     if (begin == end) {
-      cout << "WARNING: Redundant thread has been detected. Performance could be impacted due to low number of nodes per thread." << endl;
+      cout << "WARNING: Redundant thread has been detected. Performance could be impacted due to low number of nodes "
+              "per thread."
+           << endl;
       break;
     }
   }
@@ -216,29 +206,27 @@ void CSysMatrix<ScalarType>::Initialize(unsigned long npoint, unsigned long npoi
 
 #ifdef USE_MKL
   using mkl = mkl_jit_wrapper<ScalarType>;
-  mkl::create_gemm(&MatrixMatrixProductJitter, MKL_ROW_MAJOR, MKL_NOTRANS,
-                   MKL_NOTRANS, nVar, nVar, nVar, 1.0, nVar, nVar, 0.0, nVar);
+  mkl::create_gemm(&MatrixMatrixProductJitter, MKL_ROW_MAJOR, MKL_NOTRANS, MKL_NOTRANS, nVar, nVar, nVar, 1.0, nVar,
+                   nVar, 0.0, nVar);
   MatrixMatrixProductKernel = mkl::get_gemm(MatrixMatrixProductJitter);
 
-  mkl::create_gemm(&MatrixVectorProductJitterBetaZero, MKL_COL_MAJOR,
-                   MKL_NOTRANS, MKL_NOTRANS, 1, nVar, nEqn, 1.0, 1, nEqn, 0.0, 1);
+  mkl::create_gemm(&MatrixVectorProductJitterBetaZero, MKL_COL_MAJOR, MKL_NOTRANS, MKL_NOTRANS, 1, nVar, nEqn, 1.0, 1,
+                   nEqn, 0.0, 1);
   MatrixVectorProductKernelBetaZero = mkl::get_gemm(MatrixVectorProductJitterBetaZero);
 
-  mkl::create_gemm(&MatrixVectorProductJitterBetaOne, MKL_COL_MAJOR,
-                   MKL_NOTRANS, MKL_NOTRANS, 1, nVar, nEqn, 1.0, 1, nEqn, 1.0, 1);
+  mkl::create_gemm(&MatrixVectorProductJitterBetaOne, MKL_COL_MAJOR, MKL_NOTRANS, MKL_NOTRANS, 1, nVar, nEqn, 1.0, 1,
+                   nEqn, 1.0, 1);
   MatrixVectorProductKernelBetaOne = mkl::get_gemm(MatrixVectorProductJitterBetaOne);
 
-  mkl::create_gemm(&MatrixVectorProductJitterAlphaMinusOne, MKL_COL_MAJOR,
-                   MKL_NOTRANS, MKL_NOTRANS, 1, nVar, nEqn, -1.0, 1, nEqn, 1.0, 1);
+  mkl::create_gemm(&MatrixVectorProductJitterAlphaMinusOne, MKL_COL_MAJOR, MKL_NOTRANS, MKL_NOTRANS, 1, nVar, nEqn,
+                   -1.0, 1, nEqn, 1.0, 1);
   MatrixVectorProductKernelAlphaMinusOne = mkl::get_gemm(MatrixVectorProductJitterAlphaMinusOne);
 #endif
-
 }
 
-template<class T>
-void CSysMatrixComms::Initiate(const CSysVector<T>& x, CGeometry *geometry,
-                               const CConfig *config, unsigned short commType) {
-
+template <class T>
+void CSysMatrixComms::Initiate(const CSysVector<T>& x, CGeometry* geometry, const CConfig* config,
+                               unsigned short commType) {
   if (geometry->nP2PSend == 0) return;
 
   /*--- Local variables ---*/
@@ -276,11 +264,8 @@ void CSysMatrixComms::Initiate(const CSysVector<T>& x, CGeometry *geometry,
   geometry->PostP2PRecvs(geometry, config, MPI_TYPE, COUNT_PER_POINT, reverse);
 
   for (auto iMessage = 0; iMessage < geometry->nP2PSend; iMessage++) {
-
     switch (commType) {
-
       case SOLUTION_MATRIX: {
-
         su2double* bufDSend = geometry->bufD_P2PSend;
 
         /*--- Get the offset for the start of this message. ---*/
@@ -289,30 +274,27 @@ void CSysMatrixComms::Initiate(const CSysVector<T>& x, CGeometry *geometry,
 
         /*--- Total count can include multiple pieces of data per point. ---*/
 
-        const auto nSend = (geometry->nPoint_P2PSend[iMessage+1] - geometry->nPoint_P2PSend[iMessage]);
+        const auto nSend = (geometry->nPoint_P2PSend[iMessage + 1] - geometry->nPoint_P2PSend[iMessage]);
 
         SU2_OMP_FOR_STAT(CSysMatrix<T>::OMP_MIN_SIZE)
         for (auto iSend = 0; iSend < nSend; iSend++) {
-
           /*--- Get the local index for this communicated data. ---*/
 
           const auto iPoint = geometry->Local_Point_P2PSend[msg_offset + iSend];
 
           /*--- Compute the offset in the recv buffer for this point. ---*/
 
-          const auto buf_offset = (msg_offset + iSend)*COUNT_PER_POINT;
+          const auto buf_offset = (msg_offset + iSend) * COUNT_PER_POINT;
 
           /*--- Load the buffer with the data to be sent. ---*/
 
-          for (auto iVar = 0ul; iVar < x.GetNVar(); iVar++)
-            bufDSend[buf_offset+iVar] = x(iPoint,iVar);
+          for (auto iVar = 0ul; iVar < x.GetNVar(); iVar++) bufDSend[buf_offset + iVar] = x(iPoint, iVar);
         }
         END_SU2_OMP_FOR
         break;
       }
 
       case SOLUTION_MATRIXTRANS: {
-
         /*--- We are going to communicate in reverse, so we use the
          recv buffer for the send instead. Also, all of the offsets
          and counts are derived from the recv data structures. ---*/
@@ -325,11 +307,10 @@ void CSysMatrixComms::Initiate(const CSysVector<T>& x, CGeometry *geometry,
 
         /*--- Total count can include multiple pieces of data per point. ---*/
 
-        const auto nSend = (geometry->nPoint_P2PRecv[iMessage+1] - geometry->nPoint_P2PRecv[iMessage]);
+        const auto nSend = (geometry->nPoint_P2PRecv[iMessage + 1] - geometry->nPoint_P2PRecv[iMessage]);
 
         SU2_OMP_FOR_STAT(CSysMatrix<T>::OMP_MIN_SIZE)
         for (auto iSend = 0; iSend < nSend; iSend++) {
-
           /*--- Get the local index for this communicated data. Here we
            again use the recv structure to find the send point, since
            the usual recv points are now the senders in reverse mode. ---*/
@@ -338,36 +319,29 @@ void CSysMatrixComms::Initiate(const CSysVector<T>& x, CGeometry *geometry,
 
           /*--- Compute the offset in the recv buffer for this point. ---*/
 
-          const auto buf_offset = (msg_offset + iSend)*COUNT_PER_POINT;
+          const auto buf_offset = (msg_offset + iSend) * COUNT_PER_POINT;
 
           /*--- Load the buffer with the data to be sent. ---*/
 
-          for (auto iVar = 0ul; iVar < x.GetNVar(); iVar++)
-            bufDSend[buf_offset+iVar] = x(iPoint,iVar);
+          for (auto iVar = 0ul; iVar < x.GetNVar(); iVar++) bufDSend[buf_offset + iVar] = x(iPoint, iVar);
         }
         END_SU2_OMP_FOR
         break;
       }
 
       default:
-        SU2_MPI::Error("Unrecognized quantity for point-to-point MPI comms.",
-                       CURRENT_FUNCTION);
+        SU2_MPI::Error("Unrecognized quantity for point-to-point MPI comms.", CURRENT_FUNCTION);
         break;
-
     }
 
     /*--- Launch the point-to-point MPI send for this message. ---*/
 
     geometry->PostP2PSends(geometry, config, MPI_TYPE, COUNT_PER_POINT, iMessage, reverse);
-
   }
-
 }
 
-template<class T>
-void CSysMatrixComms::Complete(CSysVector<T>& x, CGeometry *geometry,
-                               const CConfig *config, unsigned short commType) {
-
+template <class T>
+void CSysMatrixComms::Complete(CSysVector<T>& x, CGeometry* geometry, const CConfig* config, unsigned short commType) {
   if (geometry->nP2PRecv == 0) return;
 
   /*--- Local variables ---*/
@@ -382,7 +356,6 @@ void CSysMatrixComms::Complete(CSysVector<T>& x, CGeometry *geometry,
    location within the local class data structures. ---*/
 
   for (auto iMessage = 0; iMessage < geometry->nP2PRecv; iMessage++) {
-
     /*--- For efficiency, recv the messages dynamically based on
      the order they arrive. ---*/
 
@@ -394,8 +367,7 @@ void CSysMatrixComms::Complete(CSysVector<T>& x, CGeometry *geometry,
 
     switch (commType) {
       case SOLUTION_MATRIX: {
-
-        const su2double *bufDRecv = geometry->bufD_P2PRecv;
+        const su2double* bufDRecv = geometry->bufD_P2PRecv;
 
         /*--- We know the offsets based on the source rank. ---*/
 
@@ -407,30 +379,28 @@ void CSysMatrixComms::Complete(CSysVector<T>& x, CGeometry *geometry,
 
         /*--- Get the number of packets to be received in this message. ---*/
 
-        const auto nRecv = (geometry->nPoint_P2PRecv[jRecv+1] - geometry->nPoint_P2PRecv[jRecv]);
+        const auto nRecv = (geometry->nPoint_P2PRecv[jRecv + 1] - geometry->nPoint_P2PRecv[jRecv]);
 
         SU2_OMP_FOR_STAT(CSysMatrix<T>::OMP_MIN_SIZE)
         for (auto iRecv = 0; iRecv < nRecv; iRecv++) {
-
           /*--- Get the local index for this communicated data. ---*/
 
           const auto iPoint = geometry->Local_Point_P2PRecv[msg_offset + iRecv];
 
           /*--- Compute the offset in the recv buffer for this point. ---*/
 
-          const auto buf_offset = (msg_offset + iRecv)*COUNT_PER_POINT;
+          const auto buf_offset = (msg_offset + iRecv) * COUNT_PER_POINT;
 
           /*--- Store the data correctly depending on the quantity. ---*/
 
           for (auto iVar = 0ul; iVar < x.GetNVar(); iVar++)
-            x(iPoint,iVar) = CSysMatrix<T>::template ActiveAssign<T>(bufDRecv[buf_offset+iVar]);
+            x(iPoint, iVar) = CSysMatrix<T>::template ActiveAssign<T>(bufDRecv[buf_offset + iVar]);
         }
         END_SU2_OMP_FOR
         break;
       }
 
       case SOLUTION_MATRIXTRANS: {
-
         /*--- We are going to communicate in reverse, so we use the
          send buffer for the recv instead. Also, all of the offsets
          and counts are derived from the send data structures. ---*/
@@ -447,23 +417,22 @@ void CSysMatrixComms::Complete(CSysVector<T>& x, CGeometry *geometry,
 
         /*--- Get the number of packets to be received in this message. ---*/
 
-        const auto nRecv = (geometry->nPoint_P2PSend[jRecv+1] - geometry->nPoint_P2PSend[jRecv]);
+        const auto nRecv = (geometry->nPoint_P2PSend[jRecv + 1] - geometry->nPoint_P2PSend[jRecv]);
 
         SU2_OMP_FOR_STAT(CSysMatrix<T>::OMP_MIN_SIZE)
         for (auto iRecv = 0; iRecv < nRecv; iRecv++) {
-
           /*--- Get the local index for this communicated data. ---*/
 
           const auto iPoint = geometry->Local_Point_P2PSend[msg_offset + iRecv];
 
           /*--- Compute the offset in the recv buffer for this point. ---*/
 
-          const auto buf_offset = (msg_offset + iRecv)*COUNT_PER_POINT;
+          const auto buf_offset = (msg_offset + iRecv) * COUNT_PER_POINT;
 
           /*--- Update receiving point. ---*/
 
           for (auto iVar = 0ul; iVar < x.GetNVar(); iVar++)
-            x(iPoint,iVar) += CSysMatrix<T>::template ActiveAssign<T>(bufDRecv[buf_offset+iVar]);
+            x(iPoint, iVar) += CSysMatrix<T>::template ActiveAssign<T>(bufDRecv[buf_offset + iVar]);
         }
         END_SU2_OMP_FOR
         break;
@@ -484,60 +453,55 @@ void CSysMatrixComms::Complete(CSysVector<T>& x, CGeometry *geometry,
 #endif
 }
 
-template<class ScalarType>
+template <class ScalarType>
 void CSysMatrix<ScalarType>::SetValZero() {
-  const auto size = nnz*nVar*nEqn;
-  const auto chunk = roundUpDiv(size,omp_get_num_threads());
+  const auto size = nnz * nVar * nEqn;
+  const auto chunk = roundUpDiv(size, omp_get_num_threads());
   const auto begin = chunk * omp_get_thread_num();
-  const auto mySize = min(chunk, size-begin) * sizeof(ScalarType);
+  const auto mySize = min(chunk, size - begin) * sizeof(ScalarType);
   memset(&matrix[begin], 0, mySize);
   SU2_OMP_BARRIER
 }
 
-template<class ScalarType>
+template <class ScalarType>
 void CSysMatrix<ScalarType>::SetValDiagonalZero() {
   SU2_OMP_FOR_STAT(omp_heavy_size)
   for (auto iPoint = 0ul; iPoint < nPointDomain; ++iPoint)
-    for (auto index = 0ul; index < nVar*nEqn; ++index)
-      matrix[dia_ptr[iPoint]*nVar*nEqn + index] = 0.0;
+    for (auto index = 0ul; index < nVar * nEqn; ++index) matrix[dia_ptr[iPoint] * nVar * nEqn + index] = 0.0;
   END_SU2_OMP_FOR
 }
 
-template<class ScalarType>
+template <class ScalarType>
 void CSysMatrix<ScalarType>::Gauss_Elimination(ScalarType* matrix, ScalarType* vec) const {
-
 #ifdef USE_MKL_LAPACK
   // With MKL_DIRECT_CALL enabled, this is significantly faster than native code on Intel Architectures.
   lapack_int ipiv[MAXNVAR];
-  LAPACKE_dgetrf( LAPACK_ROW_MAJOR, nVar, nVar, matrix, nVar, ipiv);
-  LAPACKE_dgetrs( LAPACK_ROW_MAJOR, 'N', nVar, 1, matrix, nVar, ipiv, vec, 1 );
+  LAPACKE_dgetrf(LAPACK_ROW_MAJOR, nVar, nVar, matrix, nVar, ipiv);
+  LAPACKE_dgetrs(LAPACK_ROW_MAJOR, 'N', nVar, 1, matrix, nVar, ipiv, vec, 1);
 #else
-#define A(I,J) matrix[(I)*nVar+(J)]
+#define A(I, J) matrix[(I)*nVar + (J)]
 
   /*--- Transform system in Upper Matrix ---*/
   for (auto iVar = 1ul; iVar < nVar; iVar++) {
     for (auto jVar = 0ul; jVar < iVar; jVar++) {
-      ScalarType weight = A(iVar,jVar) / A(jVar,jVar);
-      for (auto kVar = jVar; kVar < nVar; kVar++)
-        A(iVar,kVar) -= weight * A(jVar,kVar);
+      ScalarType weight = A(iVar, jVar) / A(jVar, jVar);
+      for (auto kVar = jVar; kVar < nVar; kVar++) A(iVar, kVar) -= weight * A(jVar, kVar);
       vec[iVar] -= weight * vec[jVar];
     }
   }
 
   /*--- Backwards substitution ---*/
   for (auto iVar = nVar; iVar > 0ul;) {
-    iVar--; // unsigned type
-    for (auto jVar = iVar+1; jVar < nVar; jVar++)
-      vec[iVar] -= A(iVar,jVar) * vec[jVar];
-    vec[iVar] /= A(iVar,iVar);
+    iVar--;  // unsigned type
+    for (auto jVar = iVar + 1; jVar < nVar; jVar++) vec[iVar] -= A(iVar, jVar) * vec[jVar];
+    vec[iVar] /= A(iVar, iVar);
   }
 #undef A
 #endif
 }
 
-template<class ScalarType>
-void CSysMatrix<ScalarType>::MatrixInverse(ScalarType *matrix, ScalarType *inverse) const {
-
+template <class ScalarType>
+void CSysMatrix<ScalarType>::MatrixInverse(ScalarType* matrix, ScalarType* inverse) const {
   /*--- This is a generalization of Gaussian elimination for multiple rhs' (the basis vectors).
    We could call "Gauss_Elimination" multiple times or fully generalize it for multiple rhs,
    the performance of both routines would suffer in both cases without the use of exotic templating.
@@ -545,70 +509,62 @@ void CSysMatrix<ScalarType>::MatrixInverse(ScalarType *matrix, ScalarType *inver
 
   assert((matrix != inverse) && "Output cannot be the same as the input.");
 
-#define M(I,J) inverse[(I)*nVar+(J)]
+#define M(I, J) inverse[(I)*nVar + (J)]
 
   /*--- Initialize the inverse with the identity. ---*/
   for (auto iVar = 0ul; iVar < nVar; iVar++)
-    for (auto jVar = 0ul; jVar < nVar; jVar++)
-      M(iVar,jVar) = ScalarType(iVar==jVar);
+    for (auto jVar = 0ul; jVar < nVar; jVar++) M(iVar, jVar) = ScalarType(iVar == jVar);
 
-  /*--- Inversion ---*/
+      /*--- Inversion ---*/
 #ifdef USE_MKL_LAPACK
   // With MKL_DIRECT_CALL enabled, this is significantly faster than native code on Intel Architectures.
   lapack_int ipiv[MAXNVAR];
-  LAPACKE_dgetrf( LAPACK_ROW_MAJOR, nVar, nVar, matrix, nVar, ipiv );
-  LAPACKE_dgetrs( LAPACK_ROW_MAJOR, 'N', nVar, nVar, matrix, nVar, ipiv, inverse, nVar );
+  LAPACKE_dgetrf(LAPACK_ROW_MAJOR, nVar, nVar, matrix, nVar, ipiv);
+  LAPACKE_dgetrs(LAPACK_ROW_MAJOR, 'N', nVar, nVar, matrix, nVar, ipiv, inverse, nVar);
 #else
-#define A(I,J) matrix[(I)*nVar+(J)]
+#define A(I, J) matrix[(I)*nVar + (J)]
 
   /*--- Transform system in Upper Matrix ---*/
   for (auto iVar = 1ul; iVar < nVar; iVar++) {
-    for (auto jVar = 0ul; jVar < iVar; jVar++)
-    {
-      ScalarType weight = A(iVar,jVar) / A(jVar,jVar);
+    for (auto jVar = 0ul; jVar < iVar; jVar++) {
+      ScalarType weight = A(iVar, jVar) / A(jVar, jVar);
 
-      for (auto kVar = jVar; kVar < nVar; kVar++)
-        A(iVar,kVar) -= weight * A(jVar,kVar);
+      for (auto kVar = jVar; kVar < nVar; kVar++) A(iVar, kVar) -= weight * A(jVar, kVar);
 
       /*--- at this stage M is lower triangular so not all cols need updating ---*/
-      for (auto kVar = 0ul; kVar <= jVar; kVar++)
-        M(iVar,kVar) -= weight * M(jVar,kVar);
+      for (auto kVar = 0ul; kVar <= jVar; kVar++) M(iVar, kVar) -= weight * M(jVar, kVar);
     }
   }
 
   /*--- Backwards substitution ---*/
   for (auto iVar = nVar; iVar > 0ul;) {
-    iVar--; // unsigned type
-    for (auto jVar = iVar+1; jVar < nVar; jVar++)
-      for (auto kVar = 0ul; kVar < nVar; kVar++)
-        M(iVar,kVar) -= A(iVar,jVar) * M(jVar,kVar);
+    iVar--;  // unsigned type
+    for (auto jVar = iVar + 1; jVar < nVar; jVar++)
+      for (auto kVar = 0ul; kVar < nVar; kVar++) M(iVar, kVar) -= A(iVar, jVar) * M(jVar, kVar);
 
-    for (auto kVar = 0ul; kVar < nVar; kVar++)
-      M(iVar,kVar) /= A(iVar,iVar);
+    for (auto kVar = 0ul; kVar < nVar; kVar++) M(iVar, kVar) /= A(iVar, iVar);
   }
 #undef A
 #endif
 #undef M
 }
 
-template<class ScalarType>
+template <class ScalarType>
 void CSysMatrix<ScalarType>::DeleteValsRowi(unsigned long i) {
+  const auto block_i = i / nVar;
+  const auto row = i % nVar;
 
-  const auto block_i = i/nVar;
-  const auto row = i%nVar;
-
-  for (auto index = row_ptr[block_i]; index < row_ptr[block_i+1]; index++) {
+  for (auto index = row_ptr[block_i]; index < row_ptr[block_i + 1]; index++) {
     for (auto iVar = 0u; iVar < nVar; iVar++)
-      matrix[index*nVar*nVar+row*nVar+iVar] = 0.0; // Delete row values in the block
+      matrix[index * nVar * nVar + row * nVar + iVar] = 0.0;  // Delete row values in the block
     if (col_ind[index] == block_i)
-      matrix[index*nVar*nVar+row*nVar+row] = 1.0; // Set 1 to the diagonal element
+      matrix[index * nVar * nVar + row * nVar + row] = 1.0;  // Set 1 to the diagonal element
   }
 }
 
-template<class ScalarType>
-void CSysMatrix<ScalarType>::MatrixVectorProduct(const CSysVector<ScalarType> & vec, CSysVector<ScalarType> & prod,
-                                                 CGeometry *geometry, const CConfig *config) const {
-
+template <class ScalarType>
+void CSysMatrix<ScalarType>::MatrixVectorProduct(const CSysVector<ScalarType>& vec, CSysVector<ScalarType>& prod,
+                                                 CGeometry* geometry, const CConfig* config) const {
   /*--- Some checks for consistency between CSysMatrix and the CSysVector<ScalarType>s ---*/
 #ifndef NDEBUG
   if ((nEqn != vec.GetNVar()) || (nVar != prod.GetNVar())) {
@@ -627,7 +583,7 @@ void CSysMatrix<ScalarType>::MatrixVectorProduct(const CSysVector<ScalarType> &
 
   SU2_OMP_FOR_DYN(omp_heavy_size)
   for (auto row_i = 0ul; row_i < nPointDomain; row_i++) {
-    RowProduct(vec, row_i, &prod[row_i*nVar]);
+    RowProduct(vec, row_i, &prod[row_i * nVar]);
   }
   END_SU2_OMP_FOR
 
@@ -635,63 +591,55 @@ void CSysMatrix<ScalarType>::MatrixVectorProduct(const CSysVector<ScalarType> &
 
   CSysMatrixComms::Initiate(prod, geometry, config);
   CSysMatrixComms::Complete(prod, geometry, config);
-
 }
 
-template<class ScalarType>
+template <class ScalarType>
 void CSysMatrix<ScalarType>::BuildJacobiPreconditioner() {
-
   /*--- Build Jacobi preconditioner (M = D), compute and store the inverses of the diagonal blocks. ---*/
   SU2_OMP_FOR_DYN(omp_heavy_size)
   for (unsigned long iPoint = 0; iPoint < nPointDomain; iPoint++)
-    InverseDiagonalBlock(iPoint, &(invM[iPoint*nVar*nVar]));
+    InverseDiagonalBlock(iPoint, &(invM[iPoint * nVar * nVar]));
   END_SU2_OMP_FOR
-
 }
 
-template<class ScalarType>
-void CSysMatrix<ScalarType>::ComputeJacobiPreconditioner(const CSysVector<ScalarType> & vec, CSysVector<ScalarType> & prod,
-                                                         CGeometry *geometry, const CConfig *config) const {
-
+template <class ScalarType>
+void CSysMatrix<ScalarType>::ComputeJacobiPreconditioner(const CSysVector<ScalarType>& vec,
+                                                         CSysVector<ScalarType>& prod, CGeometry* geometry,
+                                                         const CConfig* config) const {
   /*--- Apply Jacobi preconditioner, y = D^{-1} * x, the inverse of the diagonal is already known. ---*/
   SU2_OMP_BARRIER
   SU2_OMP_FOR_DYN(omp_heavy_size)
   for (unsigned long iPoint = 0; iPoint < nPointDomain; iPoint++)
-    MatrixVectorProduct(&(invM[iPoint*nVar*nVar]), &vec[iPoint*nVar], &prod[iPoint*nVar]);
+    MatrixVectorProduct(&(invM[iPoint * nVar * nVar]), &vec[iPoint * nVar], &prod[iPoint * nVar]);
   END_SU2_OMP_FOR
 
   /*--- MPI Parallelization ---*/
   CSysMatrixComms::Initiate(prod, geometry, config);
   CSysMatrixComms::Complete(prod, geometry, config);
-
 }
 
-template<class ScalarType>
+template <class ScalarType>
 void CSysMatrix<ScalarType>::BuildILUPreconditioner() {
-
   /*--- Copy block matrix to compute factorization in-place. ---*/
 
   if (ilu_fill_in == 0) {
     /*--- ILU0, direct copy. ---*/
     SU2_OMP_FOR_STAT(omp_light_size)
-    for (auto iVar = 0ul; iVar < nnz*nVar*nVar; ++iVar)
-      ILU_matrix[iVar] = matrix[iVar];
+    for (auto iVar = 0ul; iVar < nnz * nVar * nVar; ++iVar) ILU_matrix[iVar] = matrix[iVar];
     END_SU2_OMP_FOR
-  }
-  else {
+  } else {
     /*--- ILUn clear the ILU matrix first. ---*/
     SU2_OMP_FOR_STAT(omp_light_size)
-    for (auto iVar = 0ul; iVar < nnz_ilu*nVar*nVar; iVar++)
-      ILU_matrix[iVar] = 0.0;
+    for (auto iVar = 0ul; iVar < nnz_ilu * nVar * nVar; iVar++) ILU_matrix[iVar] = 0.0;
     END_SU2_OMP_FOR
 
     /*--- ILUn, traverse matrix to access its blocks
      *    sequentially and set them in the ILU matrix. ---*/
     SU2_OMP_FOR_DYN(omp_heavy_size)
     for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++) {
-      for (auto index = row_ptr[iPoint]; index < row_ptr[iPoint+1]; index++) {
+      for (auto index = row_ptr[iPoint]; index < row_ptr[iPoint + 1]; index++) {
         auto jPoint = col_ind[index];
-        SetBlock_ILUMatrix(iPoint, jPoint, &matrix[index*nVar*nVar]);
+        SetBlock_ILUMatrix(iPoint, jPoint, &matrix[index * nVar * nVar]);
       }
     }
     END_SU2_OMP_FOR
@@ -704,28 +652,25 @@ void CSysMatrix<ScalarType>::BuildILUPreconditioner() {
    *    outside of a parallel section. ---*/
 
   SU2_OMP_FOR_STAT(1)
-  for(unsigned long thread = 0; thread < omp_num_parts; ++thread)
-  {
+  for (unsigned long thread = 0; thread < omp_num_parts; ++thread) {
     const auto begin = omp_partitions[thread];
-    const auto end = omp_partitions[thread+1];
+    const auto end = omp_partitions[thread + 1];
     if (begin == end) continue;
 
     /*--- Each thread will work on the submatrix defined from row/col "begin"
      *    to row/col "end-1" (i.e. the range [begin,end[). Which is exactly
      *    what the MPI-only implementation does. ---*/
 
-    ScalarType weight[MAXNVAR*MAXNVAR], aux_block[MAXNVAR*MAXNVAR];
-
-    for (auto iPoint = begin+1; iPoint < end; iPoint++) {
+    ScalarType weight[MAXNVAR * MAXNVAR], aux_block[MAXNVAR * MAXNVAR];
 
+    for (auto iPoint = begin + 1; iPoint < end; iPoint++) {
       /*--- Invert and store the previous diagonal block to later compute the weight. ---*/
 
-      InverseDiagonalBlock_ILUMatrix(iPoint-1, &invM[(iPoint-1)*nVar*nVar]);
+      InverseDiagonalBlock_ILUMatrix(iPoint - 1, &invM[(iPoint - 1) * nVar * nVar]);
 
       /*--- For this row (unknown), loop over its lower diagonal entries. ---*/
 
       for (auto index = row_ptr_ilu[iPoint]; index < dia_ptr_ilu[iPoint]; index++) {
-
         /*--- jPoint is the column index (jPoint < iPoint). ---*/
 
         auto jPoint = col_ind_ilu[index];
@@ -736,13 +681,12 @@ void CSysMatrix<ScalarType>::BuildILUPreconditioner() {
 
         /*--- Multiply the block by the inverse of the corresponding diagonal block. ---*/
 
-        auto Block_ij = &ILU_matrix[index*nVar*nVar];
-        MatrixMatrixProduct(Block_ij, &invM[jPoint*nVar*nVar], weight);
+        auto Block_ij = &ILU_matrix[index * nVar * nVar];
+        MatrixMatrixProduct(Block_ij, &invM[jPoint * nVar * nVar], weight);
 
         /*--- "weight" holds Aij*inv(Ajj). Jump to the upper part of the jPoint row. ---*/
 
-        for (auto index_ = dia_ptr_ilu[jPoint]+1; index_ < row_ptr_ilu[jPoint+1]; index_++) {
-
+        for (auto index_ = dia_ptr_ilu[jPoint] + 1; index_ < row_ptr_ilu[jPoint + 1]; index_++) {
           /*--- Get the column index (kPoint > jPoint). ---*/
 
           auto kPoint = col_ind_ilu[index_];
@@ -754,7 +698,7 @@ void CSysMatrix<ScalarType>::BuildILUPreconditioner() {
           auto Block_ik = GetBlock_ILUMatrix(iPoint, kPoint);
 
           if (Block_ik != nullptr) {
-            auto Block_jk = &ILU_matrix[index_*nVar*nVar];
+            auto Block_jk = &ILU_matrix[index_ * nVar * nVar];
             MatrixMatrixProduct(weight, Block_jk, aux_block);
             MatrixSubtraction(Block_ik, aux_block, Block_ik);
           }
@@ -763,66 +707,60 @@ void CSysMatrix<ScalarType>::BuildILUPreconditioner() {
         /*--- Lastly, store "weight" in the lower triangular part, which
          will be reused during the forward solve in the precon/smoother. ---*/
 
-        for (auto iVar = 0ul; iVar < nVar*nVar; ++iVar)
-          Block_ij[iVar] = weight[iVar];
+        for (auto iVar = 0ul; iVar < nVar * nVar; ++iVar) Block_ij[iVar] = weight[iVar];
       }
     }
-    InverseDiagonalBlock_ILUMatrix(end-1, &invM[(end-1)*nVar*nVar]);
-
+    InverseDiagonalBlock_ILUMatrix(end - 1, &invM[(end - 1) * nVar * nVar]);
   }
   END_SU2_OMP_FOR
-
 }
 
-template<class ScalarType>
-void CSysMatrix<ScalarType>::ComputeILUPreconditioner(const CSysVector<ScalarType> & vec, CSysVector<ScalarType> & prod,
-                                                      CGeometry *geometry, const CConfig *config) const {
+template <class ScalarType>
+void CSysMatrix<ScalarType>::ComputeILUPreconditioner(const CSysVector<ScalarType>& vec, CSysVector<ScalarType>& prod,
+                                                      CGeometry* geometry, const CConfig* config) const {
   /*--- Coherent view of vectors. ---*/
   SU2_OMP_BARRIER
 
   /*--- OpenMP Parallelization ---*/
   SU2_OMP_FOR_STAT(1)
-  for(unsigned long thread = 0; thread < omp_num_parts; ++thread)
-  {
+  for (unsigned long thread = 0; thread < omp_num_parts; ++thread) {
     const auto begin = omp_partitions[thread];
-    const auto end = omp_partitions[thread+1];
+    const auto end = omp_partitions[thread + 1];
     if (begin == end) continue;
 
     ScalarType aux_vec[MAXNVAR];
 
     /*--- Copy vector to then work on prod in place ---*/
 
-    for (auto iVar = begin*nVar; iVar < end*nVar; iVar++)
-      prod[iVar] = vec[iVar];
+    for (auto iVar = begin * nVar; iVar < end * nVar; iVar++) prod[iVar] = vec[iVar];
 
     /*--- Forward solve the system using the lower matrix entries that
      were computed and stored during the ILU preprocessing. Note
      that we are overwriting the residual vector as we go. ---*/
 
-    for (auto iPoint = begin+1; iPoint < end; iPoint++) {
+    for (auto iPoint = begin + 1; iPoint < end; iPoint++) {
       for (auto index = row_ptr_ilu[iPoint]; index < dia_ptr_ilu[iPoint]; index++) {
         auto jPoint = col_ind_ilu[index];
         if (jPoint < begin) continue;
-        auto Block_ij = &ILU_matrix[index*nVar*nVar];
-        MatrixVectorProductSub(Block_ij, &prod[jPoint*nVar], &prod[iPoint*nVar]);
+        auto Block_ij = &ILU_matrix[index * nVar * nVar];
+        MatrixVectorProductSub(Block_ij, &prod[jPoint * nVar], &prod[iPoint * nVar]);
       }
     }
 
     /*--- Backwards substitution (starts at the last row) ---*/
 
     for (auto iPoint = end; iPoint > begin;) {
-      iPoint--; // unsigned type
-      for (auto iVar = 0ul; iVar < nVar; iVar++)
-        aux_vec[iVar] = prod[iPoint*nVar+iVar];
+      iPoint--;  // unsigned type
+      for (auto iVar = 0ul; iVar < nVar; iVar++) aux_vec[iVar] = prod[iPoint * nVar + iVar];
 
-      for (auto index = dia_ptr_ilu[iPoint]+1; index < row_ptr_ilu[iPoint+1]; index++) {
+      for (auto index = dia_ptr_ilu[iPoint] + 1; index < row_ptr_ilu[iPoint + 1]; index++) {
         auto jPoint = col_ind_ilu[index];
         if (jPoint >= end) break;
-        auto Block_ij = &ILU_matrix[index*nVar*nVar];
-        MatrixVectorProductSub(Block_ij, &prod[jPoint*nVar], aux_vec);
+        auto Block_ij = &ILU_matrix[index * nVar * nVar];
+        MatrixVectorProductSub(Block_ij, &prod[jPoint * nVar], aux_vec);
       }
 
-      MatrixVectorProduct(&invM[iPoint*nVar*nVar], aux_vec, &prod[iPoint*nVar]);
+      MatrixVectorProduct(&invM[iPoint * nVar * nVar], aux_vec, &prod[iPoint * nVar]);
     }
   }
   END_SU2_OMP_FOR
@@ -831,13 +769,12 @@ void CSysMatrix<ScalarType>::ComputeILUPreconditioner(const CSysVector<ScalarTyp
 
   CSysMatrixComms::Initiate(prod, geometry, config);
   CSysMatrixComms::Complete(prod, geometry, config);
-
 }
 
-template<class ScalarType>
-void CSysMatrix<ScalarType>::ComputeLU_SGSPreconditioner(const CSysVector<ScalarType> & vec, CSysVector<ScalarType> & prod,
-                                                         CGeometry *geometry, const CConfig *config) const {
-
+template <class ScalarType>
+void CSysMatrix<ScalarType>::ComputeLU_SGSPreconditioner(const CSysVector<ScalarType>& vec,
+                                                         CSysVector<ScalarType>& prod, CGeometry* geometry,
+                                                         const CConfig* config) const {
   /*--- First part of the symmetric iteration: (D+L).x* = b ---*/
 
   /*--- Coherent view of vectors. ---*/
@@ -845,10 +782,9 @@ void CSysMatrix<ScalarType>::ComputeLU_SGSPreconditioner(const CSysVector<Scalar
 
   /*--- OpenMP Parallelization ---*/
   SU2_OMP_FOR_STAT(1)
-  for(unsigned long thread = 0; thread < omp_num_parts; ++thread)
-  {
+  for (unsigned long thread = 0; thread < omp_num_parts; ++thread) {
     const auto begin = omp_partitions[thread];
-    const auto end = omp_partitions[thread+1];
+    const auto end = omp_partitions[thread + 1];
     if (begin == end) continue;
 
     /*--- Each thread will work on the submatrix defined from row/col "begin"
@@ -859,10 +795,10 @@ void CSysMatrix<ScalarType>::ComputeLU_SGSPreconditioner(const CSysVector<Scalar
     ScalarType low_prod[MAXNVAR];
 
     for (auto iPoint = begin; iPoint < end; ++iPoint) {
-      auto idx = iPoint*nVar;
-      LowerProduct(prod, iPoint, begin, low_prod);        // Compute L.x*
-      VectorSubtraction(&vec[idx], low_prod, &prod[idx]); // Compute y = b - L.x*
-      Gauss_Elimination(iPoint, &prod[idx]);              // Solve D.x* = y
+      auto idx = iPoint * nVar;
+      LowerProduct(prod, iPoint, begin, low_prod);         // Compute L.x*
+      VectorSubtraction(&vec[idx], low_prod, &prod[idx]);  // Compute y = b - L.x*
+      Gauss_Elimination(iPoint, &prod[idx]);               // Solve D.x* = y
     }
   }
   END_SU2_OMP_FOR
@@ -876,21 +812,20 @@ void CSysMatrix<ScalarType>::ComputeLU_SGSPreconditioner(const CSysVector<Scalar
 
   /*--- OpenMP Parallelization ---*/
   SU2_OMP_FOR_STAT(1)
-  for(unsigned long thread = 0; thread < omp_num_parts; ++thread)
-  {
+  for (unsigned long thread = 0; thread < omp_num_parts; ++thread) {
     const auto begin = omp_partitions[thread];
-    const auto row_end = omp_partitions[thread+1];
+    const auto row_end = omp_partitions[thread + 1];
     if (begin == row_end) continue;
 
     ScalarType up_prod[MAXNVAR], dia_prod[MAXNVAR];
 
     for (auto iPoint = row_end; iPoint > begin;) {
-      iPoint--; // because of unsigned type
-      auto idx = iPoint*nVar;
-      DiagonalProduct(prod, iPoint, dia_prod);          // Compute D.x*
-      UpperProduct(prod, iPoint, row_end, up_prod);     // Compute U.x_(n+1)
-      VectorSubtraction(dia_prod, up_prod, &prod[idx]); // Compute y = D.x*-U.x_(n+1)
-      Gauss_Elimination(iPoint, &prod[idx]);            // Solve D.x* = y
+      iPoint--;  // because of unsigned type
+      auto idx = iPoint * nVar;
+      DiagonalProduct(prod, iPoint, dia_prod);           // Compute D.x*
+      UpperProduct(prod, iPoint, row_end, up_prod);      // Compute U.x_(n+1)
+      VectorSubtraction(dia_prod, up_prod, &prod[idx]);  // Compute y = D.x*-U.x_(n+1)
+      Gauss_Elimination(iPoint, &prod[idx]);             // Solve D.x* = y
     }
   }
   END_SU2_OMP_FOR
@@ -899,12 +834,10 @@ void CSysMatrix<ScalarType>::ComputeLU_SGSPreconditioner(const CSysVector<Scalar
 
   CSysMatrixComms::Initiate(prod, geometry, config);
   CSysMatrixComms::Complete(prod, geometry, config);
-
 }
 
-template<class ScalarType>
-void CSysMatrix<ScalarType>::BuildLineletPreconditioner(const CGeometry *geometry, const CConfig *config) {
-
+template <class ScalarType>
+void CSysMatrix<ScalarType>::BuildLineletPreconditioner(const CGeometry* geometry, const CConfig* config) {
   BuildJacobiPreconditioner();
 
   /*--- Allocate working vectors if not done yet. ---*/
@@ -932,9 +865,10 @@ void CSysMatrix<ScalarType>::BuildLineletPreconditioner(const CGeometry *geometr
   END_SU2_OMP_FOR
 }
 
-template<class ScalarType>
-void CSysMatrix<ScalarType>::ComputeLineletPreconditioner(const CSysVector<ScalarType> & vec, CSysVector<ScalarType> & prod,
-                                                          CGeometry *geometry, const CConfig *config) const {
+template <class ScalarType>
+void CSysMatrix<ScalarType>::ComputeLineletPreconditioner(const CSysVector<ScalarType>& vec,
+                                                          CSysVector<ScalarType>& prod, CGeometry* geometry,
+                                                          const CConfig* config) const {
   /*--- Coherent view of vectors. ---*/
   SU2_OMP_BARRIER
 
@@ -942,17 +876,16 @@ void CSysMatrix<ScalarType>::ComputeLineletPreconditioner(const CSysVector<Scala
 
   /*--- Jacobi preconditioning where there are no linelets. ---*/
 
-  SU2_OMP_FOR_(schedule(dynamic,omp_heavy_size) SU2_NOWAIT)
+  SU2_OMP_FOR_(schedule(dynamic, omp_heavy_size) SU2_NOWAIT)
   for (auto iPoint = 0ul; iPoint < nPointDomain; iPoint++)
     if (li.lineletIdx[iPoint] == CGeometry::CLineletInfo::NO_LINELET)
-      MatrixVectorProduct(&(invM[iPoint*nVar*nVar]), &vec[iPoint*nVar], &prod[iPoint*nVar]);
+      MatrixVectorProduct(&(invM[iPoint * nVar * nVar]), &vec[iPoint * nVar], &prod[iPoint * nVar]);
   END_SU2_OMP_FOR
 
   /*--- Solve the tridiagonal systems for the linelets. ---*/
 
   SU2_OMP_FOR_DYN(1)
   for (auto iLinelet = 0ul; iLinelet < li.linelets.size(); iLinelet++) {
-
     /*--- Get references to the working vectors allocated for this thread. ---*/
 
     const int thread = omp_get_thread_num();
@@ -966,32 +899,29 @@ void CSysMatrix<ScalarType>::ComputeLineletPreconditioner(const CSysVector<Scala
 
     for (auto iElem = 0ul; iElem < nElem; iElem++) {
       const auto iPoint = li.linelets[iLinelet][iElem];
-      for (auto iVar = 0ul; iVar < nVar; iVar++)
-        lineletVector[iElem*nVar+iVar] = vec[iPoint*nVar+iVar];
+      for (auto iVar = 0ul; iVar < nVar; iVar++) lineletVector[iElem * nVar + iVar] = vec[iPoint * nVar + iVar];
     }
 
     /*--- Forward pass, eliminate lower entries, modify diagonal and rhs. ---*/
 
     /*--- Small temporaries. ---*/
-    ScalarType aux_block[MAXNVAR*MAXNVAR], aux_vector[MAXNVAR];
+    ScalarType aux_block[MAXNVAR * MAXNVAR], aux_vector[MAXNVAR];
 
     /*--- Copy diagonal block for first point in this linelet. ---*/
-    MatrixCopy(&matrix[dia_ptr[li.linelets[iLinelet][0]]*nVar*nVar],
-               lineletInvDiag.data());
+    MatrixCopy(&matrix[dia_ptr[li.linelets[iLinelet][0]] * nVar * nVar], lineletInvDiag.data());
 
     for (auto iElem = 1ul; iElem < nElem; iElem++) {
-
       /*--- Setup pointers to required matrices and vectors ---*/
-      const auto im1Point = li.linelets[iLinelet][iElem-1];
+      const auto im1Point = li.linelets[iLinelet][iElem - 1];
       const auto iPoint = li.linelets[iLinelet][iElem];
 
-      const auto* d = &matrix[dia_ptr[iPoint]*nVar*nVar];
+      const auto* d = &matrix[dia_ptr[iPoint] * nVar * nVar];
       const auto* l = GetBlock(iPoint, im1Point);
       const auto* u = GetBlock(im1Point, iPoint);
 
-      auto* inv_dm1 = &lineletInvDiag[(iElem-1)*nVar*nVar];
-      auto* d_prime = &lineletInvDiag[iElem*nVar*nVar];
-      auto* b_prime = &lineletVector[iElem*nVar];
+      auto* inv_dm1 = &lineletInvDiag[(iElem - 1) * nVar * nVar];
+      auto* d_prime = &lineletInvDiag[iElem * nVar * nVar];
+      auto* b_prime = &lineletVector[iElem * nVar];
 
       /*--- Invert previous modified diagonal ---*/
       MatrixCopy(inv_dm1, aux_block);
@@ -1005,34 +935,32 @@ void CSysMatrix<ScalarType>::ComputeLineletPreconditioner(const CSysVector<Scala
       MatrixSubtraction(d, d_prime, d_prime);
 
       /*--- Update the rhs ---*/
-      MatrixVectorProduct(aux_block, &lineletVector[(iElem-1)*nVar], aux_vector);
+      MatrixVectorProduct(aux_block, &lineletVector[(iElem - 1) * nVar], aux_vector);
       VectorSubtraction(b_prime, aux_vector, b_prime);
 
       /*--- Cache upper block pointer for the backward substitution phase ---*/
-      lineletUpper[iElem-1] = u;
+      lineletUpper[iElem - 1] = u;
     }
 
     /*--- Backwards substitution, LineletVector becomes the solution ---*/
 
     /*--- x_n = d_n^{-1} * b_n ---*/
-    Gauss_Elimination(&lineletInvDiag[(nElem-1)*nVar*nVar], &lineletVector[(nElem-1)*nVar]);
+    Gauss_Elimination(&lineletInvDiag[(nElem - 1) * nVar * nVar], &lineletVector[(nElem - 1) * nVar]);
 
     /*--- x_i = d_i^{-1}*(b_i - u_i*x_{i+1}) ---*/
-    for (auto iElem = nElem-1; iElem > 0; --iElem) {
-      const auto* inv_dm1 = &lineletInvDiag[(iElem-1)*nVar*nVar];
-      MatrixVectorProduct(lineletUpper[iElem-1], &lineletVector[iElem*nVar], aux_vector);
-      VectorSubtraction(&lineletVector[(iElem-1)*nVar], aux_vector, aux_vector);
-      MatrixVectorProduct(inv_dm1, aux_vector, &lineletVector[(iElem-1)*nVar]);
+    for (auto iElem = nElem - 1; iElem > 0; --iElem) {
+      const auto* inv_dm1 = &lineletInvDiag[(iElem - 1) * nVar * nVar];
+      MatrixVectorProduct(lineletUpper[iElem - 1], &lineletVector[iElem * nVar], aux_vector);
+      VectorSubtraction(&lineletVector[(iElem - 1) * nVar], aux_vector, aux_vector);
+      MatrixVectorProduct(inv_dm1, aux_vector, &lineletVector[(iElem - 1) * nVar]);
     }
 
     /*--- Copy results to product vector ---*/
 
     for (auto iElem = 0ul; iElem < nElem; iElem++) {
       const auto iPoint = li.linelets[iLinelet][iElem];
-      for (auto iVar = 0ul; iVar < nVar; iVar++)
-        prod[iPoint*nVar+iVar] = lineletVector[iElem*nVar+iVar];
+      for (auto iVar = 0ul; iVar < nVar; iVar++) prod[iPoint * nVar + iVar] = lineletVector[iElem * nVar + iVar];
     }
-
   }
   END_SU2_OMP_FOR
 
@@ -1040,40 +968,38 @@ void CSysMatrix<ScalarType>::ComputeLineletPreconditioner(const CSysVector<Scala
 
   CSysMatrixComms::Initiate(prod, geometry, config);
   CSysMatrixComms::Complete(prod, geometry, config);
-
 }
 
-template<class ScalarType>
-void CSysMatrix<ScalarType>::ComputeResidual(const CSysVector<ScalarType> & sol, const CSysVector<ScalarType> & f,
-                                             CSysVector<ScalarType> & res) const {
+template <class ScalarType>
+void CSysMatrix<ScalarType>::ComputeResidual(const CSysVector<ScalarType>& sol, const CSysVector<ScalarType>& f,
+                                             CSysVector<ScalarType>& res) const {
   SU2_OMP_BARRIER
   SU2_OMP_FOR_DYN(omp_heavy_size)
   for (unsigned long iPoint = 0; iPoint < nPointDomain; iPoint++) {
     ScalarType aux_vec[MAXNVAR];
     RowProduct(sol, iPoint, aux_vec);
-    VectorSubtraction(aux_vec, &f[iPoint*nVar], &res[iPoint*nVar]);
+    VectorSubtraction(aux_vec, &f[iPoint * nVar], &res[iPoint * nVar]);
   }
   END_SU2_OMP_FOR
 }
 
-template<class ScalarType>
-template<class OtherType>
-void CSysMatrix<ScalarType>::EnforceSolutionAtNode(const unsigned long node_i, const OtherType *x_i, CSysVector<OtherType> & b) {
-
+template <class ScalarType>
+template <class OtherType>
+void CSysMatrix<ScalarType>::EnforceSolutionAtNode(const unsigned long node_i, const OtherType* x_i,
+                                                   CSysVector<OtherType>& b) {
   /*--- Eliminate the row associated with node i (Block_ii = I and all other Block_ij = 0).
    *    To preserve eventual symmetry, also attempt to eliminate the column, if the sparse pattern is not
    *    symmetric the entire column may not be eliminated, the result (matrix and vector) is still correct.
    *    The vector is updated with the product of column i by the known (enforced) solution at node i. ---*/
 
-  for (auto index = row_ptr[node_i]; index < row_ptr[node_i+1]; ++index) {
-
+  for (auto index = row_ptr[node_i]; index < row_ptr[node_i + 1]; ++index) {
     auto node_j = col_ind[index];
 
     /*--- The diagonal block is handled outside the loop. ---*/
     if (node_j == node_i) continue;
 
     /*--- Delete block j on row i (bij) and ATTEMPT to delete block i on row j (bji). ---*/
-    auto bij = &matrix[index*nVar*nVar];
+    auto bij = &matrix[index * nVar * nVar];
     auto bji = GetBlock(node_j, node_i);
 
     /*--- The "attempt" part. ---*/
@@ -1082,15 +1008,14 @@ void CSysMatrix<ScalarType>::EnforceSolutionAtNode(const unsigned long node_i, c
       bji = bij;
     }
 
-    for(auto iVar = 0ul; iVar < nVar; ++iVar) {
-      for(auto jVar = 0ul; jVar < nVar; ++jVar) {
+    for (auto iVar = 0ul; iVar < nVar; ++iVar) {
+      for (auto jVar = 0ul; jVar < nVar; ++jVar) {
         /*--- Column product. ---*/
-        b[node_j*nVar+iVar] -= bji[iVar*nVar+jVar] * x_i[jVar];
+        b[node_j * nVar + iVar] -= bji[iVar * nVar + jVar] * x_i[jVar];
         /*--- Delete blocks. ---*/
-        bij[iVar*nVar+jVar] = bji[iVar*nVar+jVar] = 0.0;
+        bij[iVar * nVar + jVar] = bji[iVar * nVar + jVar] = 0.0;
       }
     }
-
   }
 
   /*--- Set the diagonal block to the identity. ---*/
@@ -1098,82 +1023,73 @@ void CSysMatrix<ScalarType>::EnforceSolutionAtNode(const unsigned long node_i, c
 
   /*--- Set known solution in rhs vector. ---*/
   b.SetBlock(node_i, x_i);
-
 }
 
-template<class ScalarType>
-template<class OtherType>
-void CSysMatrix<ScalarType>::EnforceSolutionAtDOF(unsigned long node_i, unsigned long iVar,
-                                                  OtherType x_i, CSysVector<OtherType> & b) {
-
-  for (auto index = row_ptr[node_i]; index < row_ptr[node_i+1]; ++index) {
-
+template <class ScalarType>
+template <class OtherType>
+void CSysMatrix<ScalarType>::EnforceSolutionAtDOF(unsigned long node_i, unsigned long iVar, OtherType x_i,
+                                                  CSysVector<OtherType>& b) {
+  for (auto index = row_ptr[node_i]; index < row_ptr[node_i + 1]; ++index) {
     const auto node_j = col_ind[index];
 
     /*--- Delete row iVar of block j on row i (bij) and ATTEMPT
      *    to delete column iVar block i on row j (bji). ---*/
 
-    auto bij = &matrix[index*nVar*nVar];
+    auto bij = &matrix[index * nVar * nVar];
     auto bji = GetBlock(node_j, node_i);
 
     /*--- The "attempt" part. ---*/
     if (bji != nullptr) {
-      for(auto jVar = 0ul; jVar < nVar; ++jVar) {
+      for (auto jVar = 0ul; jVar < nVar; ++jVar) {
         /*--- Column product. ---*/
-        b[node_j*nVar+jVar] -= bji[jVar*nVar+iVar] * x_i;
+        b[node_j * nVar + jVar] -= bji[jVar * nVar + iVar] * x_i;
         /*--- Delete entries. ---*/
-        bji[jVar*nVar+iVar] = 0.0;
+        bji[jVar * nVar + iVar] = 0.0;
       }
     }
 
     /*--- Delete row. ---*/
-    for(auto jVar = 0ul; jVar < nVar; ++jVar)
-      bij[iVar*nVar+jVar] = 0.0;
+    for (auto jVar = 0ul; jVar < nVar; ++jVar) bij[iVar * nVar + jVar] = 0.0;
 
     /*--- Set the diagonal entry of the block to 1. ---*/
-    if (node_j == node_i)
-      bij[iVar*(nVar+1)] = 1.0;
+    if (node_j == node_i) bij[iVar * (nVar + 1)] = 1.0;
   }
 
   /*--- Set known solution in rhs vector. ---*/
   b(node_i, iVar) = x_i;
-
 }
 
-template<class ScalarType>
+template <class ScalarType>
 void CSysMatrix<ScalarType>::SetDiagonalAsColumnSum() {
-
   SU2_OMP_FOR_DYN(omp_heavy_size)
   for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint) {
+    auto block_ii = &matrix[dia_ptr[iPoint] * nVar * nEqn];
 
-    auto block_ii = &matrix[dia_ptr[iPoint]*nVar*nEqn];
-
-    for (auto k = 0ul; k < nVar*nEqn; ++k) block_ii[k] = 0.0;
+    for (auto k = 0ul; k < nVar * nEqn; ++k) block_ii[k] = 0.0;
 
-    for (auto k = row_ptr[iPoint]; k < row_ptr[iPoint+1]; ++k) {
-      auto block_ji = &matrix[col_ptr[k]*nVar*nEqn];
+    for (auto k = row_ptr[iPoint]; k < row_ptr[iPoint + 1]; ++k) {
+      auto block_ji = &matrix[col_ptr[k] * nVar * nEqn];
       if (block_ji != block_ii) MatrixSubtraction(block_ii, block_ji, block_ii);
     }
   }
   END_SU2_OMP_FOR
 }
 
-template<class ScalarType>
+template <class ScalarType>
 void CSysMatrix<ScalarType>::TransposeInPlace() {
-
-  assert(nVar==nEqn && "Cannot transpose with nVar != nEqn.");
+  assert(nVar == nEqn && "Cannot transpose with nVar != nEqn.");
 
   auto swapAndTransp = [](unsigned long n, ScalarType* a, ScalarType* b) {
-    assert(a!=b);
+    assert(a != b);
     /*--- a=b', b=a' ---*/
-    for (auto i=0ul; i<n; ++i) {
-      for (auto j=0ul; j<i; ++j) {
-        const auto lo = i*n+j;
-        const auto up = j*n+i;
+    for (auto i = 0ul; i < n; ++i) {
+      for (auto j = 0ul; j < i; ++j) {
+        const auto lo = i * n + j;
+        const auto up = j * n + i;
         std::swap(a[lo], b[up]);
         std::swap(a[up], b[lo]);
       }
-      std::swap(a[i*n+i], b[i*n+i]);
+      std::swap(a[i * n + i], b[i * n + i]);
     }
   };
 
@@ -1181,36 +1097,34 @@ void CSysMatrix<ScalarType>::TransposeInPlace() {
 
   if (edge_ptr) {
     /*--- The FV way. ---*/
-    SU2_OMP_FOR_DYN(omp_heavy_size*2)
+    SU2_OMP_FOR_DYN(omp_heavy_size * 2)
     for (auto iEdge = 0ul; iEdge < edge_ptr.nEdge; ++iEdge) {
-      auto bij = &matrix[edge_ptr(iEdge,0)*nVar*nVar];
-      auto bji = &matrix[edge_ptr(iEdge,1)*nVar*nVar];
+      auto bij = &matrix[edge_ptr(iEdge, 0) * nVar * nVar];
+      auto bji = &matrix[edge_ptr(iEdge, 1) * nVar * nVar];
 
       swapAndTransp(nVar, bij, bji);
     }
     END_SU2_OMP_FOR
-  }
-  else if (col_ptr) {
+  } else if (col_ptr) {
     /*--- If the column pointer was built. ---*/
     SU2_OMP_FOR_DYN(omp_heavy_size)
     for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint) {
       for (auto k = row_ptr[iPoint]; k < dia_ptr[iPoint]; ++k) {
-        auto bij = &matrix[k*nVar*nVar];
-        auto bji = &matrix[col_ptr[k]*nVar*nVar];
+        auto bij = &matrix[k * nVar * nVar];
+        auto bji = &matrix[col_ptr[k] * nVar * nVar];
 
         swapAndTransp(nVar, bij, bji);
       }
     }
     END_SU2_OMP_FOR
-  }
-  else {
+  } else {
     /*--- Slow fallback, needs to search for ji. ---*/
     SU2_OMP_FOR_DYN(omp_heavy_size)
     for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint) {
-      for (auto k = dia_ptr[iPoint]+1ul; k < row_ptr[iPoint+1]; ++k) {
+      for (auto k = dia_ptr[iPoint] + 1ul; k < row_ptr[iPoint + 1]; ++k) {
         const auto jPoint = col_ind[k];
-        auto bij = &matrix[k*nVar*nVar];
-        auto bji = GetBlock(jPoint,iPoint);
+        auto bij = &matrix[k * nVar * nVar];
+        auto bji = GetBlock(jPoint, iPoint);
         assert(bji && "Pattern is not symmetric.");
 
         swapAndTransp(nVar, bij, bji);
@@ -1223,10 +1137,9 @@ void CSysMatrix<ScalarType>::TransposeInPlace() {
 
   SU2_OMP_FOR_STAT(omp_heavy_size)
   for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint) {
-    auto bii = &matrix[dia_ptr[iPoint]*nVar*nVar];
-    for (auto i=0ul; i<nVar; ++i)
-      for (auto j=0ul; j<i; ++j)
-        std::swap(bii[i*nVar+j], bii[j*nVar+i]);
+    auto bii = &matrix[dia_ptr[iPoint] * nVar * nVar];
+    for (auto i = 0ul; i < nVar; ++i)
+      for (auto j = 0ul; j < i; ++j) std::swap(bii[i * nVar + j], bii[j * nVar + i]);
   }
   END_SU2_OMP_FOR
 
@@ -1237,33 +1150,28 @@ void CSysMatrix<ScalarType>::TransposeInPlace() {
 #endif
 }
 
-template<class ScalarType>
+template <class ScalarType>
 void CSysMatrix<ScalarType>::MatrixMatrixAddition(ScalarType alpha, const CSysMatrix<ScalarType>& B) {
-
   /*--- Check that the sparse structure is shared between the two matrices,
    *    comparing pointers is ok as they are obtained from CGeometry. ---*/
-  bool ok = (row_ptr == B.row_ptr) && (col_ind == B.col_ind) &&
-            (nVar == B.nVar) && (nEqn == B.nEqn) && (nnz == B.nnz);
+  bool ok = (row_ptr == B.row_ptr) && (col_ind == B.col_ind) && (nVar == B.nVar) && (nEqn == B.nEqn) && (nnz == B.nnz);
 
   if (!ok) {
     SU2_MPI::Error("Matrices do not have compatible sparsity.", CURRENT_FUNCTION);
   }
 
   SU2_OMP_FOR_STAT(omp_light_size)
-  for (auto i = 0ul; i < nnz*nVar*nEqn; ++i)
-    matrix[i] += alpha*B.matrix[i];
+  for (auto i = 0ul; i < nnz * nVar * nEqn; ++i) matrix[i] += alpha * B.matrix[i];
   END_SU2_OMP_FOR
-
 }
 
-template<class ScalarType>
-void CSysMatrix<ScalarType>::BuildPastixPreconditioner(CGeometry *geometry, const CConfig *config,
+template <class ScalarType>
+void CSysMatrix<ScalarType>::BuildPastixPreconditioner(CGeometry* geometry, const CConfig* config,
                                                        unsigned short kind_fact) {
 #ifdef HAVE_PASTIX
   /*--- Pastix will launch nested threads. ---*/
-  BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS
-  {
-    pastix_wrapper.SetMatrix(nVar,nPoint,nPointDomain,row_ptr,col_ind,matrix);
+  BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
+    pastix_wrapper.SetMatrix(nVar, nPoint, nPointDomain, row_ptr, col_ind, matrix);
     pastix_wrapper.Factorize(geometry, config, kind_fact);
   }
   END_SU2_OMP_SAFE_GLOBAL_ACCESS
@@ -1272,11 +1180,12 @@ void CSysMatrix<ScalarType>::BuildPastixPreconditioner(CGeometry *geometry, cons
 #endif
 }
 
-template<class ScalarType>
-void CSysMatrix<ScalarType>::ComputePastixPreconditioner(const CSysVector<ScalarType> & vec, CSysVector<ScalarType> & prod,
-                                                         CGeometry *geometry, const CConfig *config) const {
+template <class ScalarType>
+void CSysMatrix<ScalarType>::ComputePastixPreconditioner(const CSysVector<ScalarType>& vec,
+                                                         CSysVector<ScalarType>& prod, CGeometry* geometry,
+                                                         const CConfig* config) const {
 #ifdef HAVE_PASTIX
-  SU2_OMP_SAFE_GLOBAL_ACCESS(pastix_wrapper.Solve(vec,prod);)
+  SU2_OMP_SAFE_GLOBAL_ACCESS(pastix_wrapper.Solve(vec, prod);)
 
   CSysMatrixComms::Initiate(prod, geometry, config);
   CSysMatrixComms::Complete(prod, geometry, config);
@@ -1287,15 +1196,16 @@ void CSysMatrix<ScalarType>::ComputePastixPreconditioner(const CSysVector<Scalar
 
 /*--- Explicit instantiations ---*/
 
-#define INSTANTIATE_COMMS(TYPE)\
-template void CSysMatrixComms::Initiate<TYPE>(const CSysVector<TYPE>&, CGeometry*, const CConfig*, unsigned short);\
-template void CSysMatrixComms::Complete<TYPE>(CSysVector<TYPE>&, CGeometry*, const CConfig*, unsigned short);
+#define INSTANTIATE_COMMS(TYPE)                                                                                       \
+  template void CSysMatrixComms::Initiate<TYPE>(const CSysVector<TYPE>&, CGeometry*, const CConfig*, unsigned short); \
+  template void CSysMatrixComms::Complete<TYPE>(CSysVector<TYPE>&, CGeometry*, const CConfig*, unsigned short);
 
-#define INSTANTIATE_MATRIX(TYPE)\
-template class CSysMatrix<TYPE>;\
-template void CSysMatrix<TYPE>::EnforceSolutionAtNode(unsigned long, const su2double*, CSysVector<su2double>&);\
-template void CSysMatrix<TYPE>::EnforceSolutionAtDOF(unsigned long, unsigned long, su2double, CSysVector<su2double>&);\
-INSTANTIATE_COMMS(TYPE)
+#define INSTANTIATE_MATRIX(TYPE)                                                                                  \
+  template class CSysMatrix<TYPE>;                                                                                \
+  template void CSysMatrix<TYPE>::EnforceSolutionAtNode(unsigned long, const su2double*, CSysVector<su2double>&); \
+  template void CSysMatrix<TYPE>::EnforceSolutionAtDOF(unsigned long, unsigned long, su2double,                   \
+                                                       CSysVector<su2double>&);                                   \
+  INSTANTIATE_COMMS(TYPE)
 
 #ifdef CODI_FORWARD_TYPE
 /*--- In forward AD only the active type is used. ---*/
@@ -1310,4 +1220,4 @@ INSTANTIATE_MATRIX(passivedouble)
 #ifdef CODI_REVERSE_TYPE
 INSTANTIATE_COMMS(su2double)
 #endif
-#endif // CODI_FORWARD_TYPE
+#endif  // CODI_FORWARD_TYPE
diff --git a/Common/src/linear_algebra/CSysSolve.cpp b/Common/src/linear_algebra/CSysSolve.cpp
index 691ae822918..fdebc018574 100644
--- a/Common/src/linear_algebra/CSysSolve.cpp
+++ b/Common/src/linear_algebra/CSysSolve.cpp
@@ -41,80 +41,76 @@
  * decide if the linear system is already solved.
  */
 namespace {
-  template<class T>
-  constexpr T linSolEpsilon() { return numeric_limits<passivedouble>::epsilon(); }
-  template<>
-  constexpr float linSolEpsilon<float>() { return 1e-12; }
+template <class T>
+constexpr T linSolEpsilon() {
+  return numeric_limits<passivedouble>::epsilon();
 }
-
-template<class ScalarType>
-CSysSolve<ScalarType>::CSysSolve(LINEAR_SOLVER_MODE linear_solver_mode) :
-  eps(linSolEpsilon<ScalarType>()),
-  lin_sol_mode(linear_solver_mode),
-  cg_ready(false),
-  bcg_ready(false),
-  smooth_ready(false),
-  LinSysSol_ptr(nullptr),
-  LinSysRes_ptr(nullptr) {
+template <>
+constexpr float linSolEpsilon<float>() {
+  return 1e-12;
 }
-
-template<class ScalarType>
-void CSysSolve<ScalarType>::ApplyGivens(ScalarType s, ScalarType c, ScalarType & h1, ScalarType & h2) const {
-
-  ScalarType temp = c*h1 + s*h2;
-  h2 = c*h2 - s*h1;
+}  // namespace
+
+template <class ScalarType>
+CSysSolve<ScalarType>::CSysSolve(LINEAR_SOLVER_MODE linear_solver_mode)
+    : eps(linSolEpsilon<ScalarType>()),
+      lin_sol_mode(linear_solver_mode),
+      cg_ready(false),
+      bcg_ready(false),
+      smooth_ready(false),
+      LinSysSol_ptr(nullptr),
+      LinSysRes_ptr(nullptr) {}
+
+template <class ScalarType>
+void CSysSolve<ScalarType>::ApplyGivens(ScalarType s, ScalarType c, ScalarType& h1, ScalarType& h2) const {
+  ScalarType temp = c * h1 + s * h2;
+  h2 = c * h2 - s * h1;
   h1 = temp;
 }
 
-template<class ScalarType>
-void CSysSolve<ScalarType>::GenerateGivens(ScalarType & dx, ScalarType & dy, ScalarType & s, ScalarType & c) const {
-
-  if ( (dx == 0.0) && (dy == 0.0) ) {
+template <class ScalarType>
+void CSysSolve<ScalarType>::GenerateGivens(ScalarType& dx, ScalarType& dy, ScalarType& s, ScalarType& c) const {
+  if ((dx == 0.0) && (dy == 0.0)) {
     c = 1.0;
     s = 0.0;
-  }
-  else if ( fabs(dy) > fabs(dx) ) {
-    ScalarType tmp = dx/dy;
-    dx = sqrt(1.0 + tmp*tmp);
-    s = Sign(1.0/dx, dy);
-    c = tmp*s;
-  }
-  else if ( fabs(dy) <= fabs(dx) ) {
-    ScalarType tmp = dy/dx;
-    dy = sqrt(1.0 + tmp*tmp);
-    c = Sign(1.0/dy, dx);
-    s = tmp*c;
-  }
-  else {
+  } else if (fabs(dy) > fabs(dx)) {
+    ScalarType tmp = dx / dy;
+    dx = sqrt(1.0 + tmp * tmp);
+    s = Sign(1.0 / dx, dy);
+    c = tmp * s;
+  } else if (fabs(dy) <= fabs(dx)) {
+    ScalarType tmp = dy / dx;
+    dy = sqrt(1.0 + tmp * tmp);
+    c = Sign(1.0 / dy, dx);
+    s = tmp * c;
+  } else {
     // dx and/or dy must be invalid
     dx = 0.0;
     dy = 0.0;
     c = 1.0;
     s = 0.0;
   }
-  dx = fabs(dx*dy);
+  dx = fabs(dx * dy);
   dy = 0.0;
 }
 
-template<class ScalarType>
-void CSysSolve<ScalarType>::SolveReduced(int n, const su2matrix<ScalarType>& Hsbg,
-                                         const su2vector<ScalarType>& rhs, su2vector<ScalarType>& x) const {
+template <class ScalarType>
+void CSysSolve<ScalarType>::SolveReduced(int n, const su2matrix<ScalarType>& Hsbg, const su2vector<ScalarType>& rhs,
+                                         su2vector<ScalarType>& x) const {
   // initialize...
-  for (int i = 0; i < n; i++)
-    x[i] = rhs[i];
+  for (int i = 0; i < n; i++) x[i] = rhs[i];
   // ... and backsolve
-  for (int i = n-1; i >= 0; i--) {
-    x[i] /= Hsbg(i,i);
-    for (int j = i-1; j >= 0; j--) {
-      x[j] -= Hsbg(j,i)*x[i];
+  for (int i = n - 1; i >= 0; i--) {
+    x[i] /= Hsbg(i, i);
+    for (int j = i - 1; j >= 0; j--) {
+      x[j] -= Hsbg(j, i) * x[i];
     }
   }
 }
 
-template<class ScalarType>
+template <class ScalarType>
 void CSysSolve<ScalarType>::ModGramSchmidt(int i, su2matrix<ScalarType>& Hsbg,
                                            vector<CSysVector<ScalarType> >& w) const {
-
   /*--- Parameter for reorthonormalization ---*/
 
   const ScalarType reorth = 0.98;
@@ -122,8 +118,8 @@ void CSysSolve<ScalarType>::ModGramSchmidt(int i, su2matrix<ScalarType>& Hsbg,
   /*--- Get the norm of the vector being orthogonalized, and find the
   threshold for re-orthogonalization ---*/
 
-  ScalarType nrm = w[i+1].squaredNorm();
-  ScalarType thr = nrm*reorth;
+  ScalarType nrm = w[i + 1].squaredNorm();
+  ScalarType thr = nrm * reorth;
 
   /*--- The norm of w[i+1] < 0.0 or w[i+1] = NaN ---*/
 
@@ -134,72 +130,68 @@ void CSysSolve<ScalarType>::ModGramSchmidt(int i, su2matrix<ScalarType>& Hsbg,
 
   /*--- Begin main Gram-Schmidt loop ---*/
 
-  for (int k = 0; k < i+1; k++) {
-    ScalarType prod = w[i+1].dot(w[k]);
-    Hsbg(k,i) = prod;
-    w[i+1] -= prod * w[k];
+  for (int k = 0; k < i + 1; k++) {
+    ScalarType prod = w[i + 1].dot(w[k]);
+    Hsbg(k, i) = prod;
+    w[i + 1] -= prod * w[k];
 
     /*--- Check if reorthogonalization is necessary ---*/
 
-    if (prod*prod > thr) {
-      prod = w[i+1].dot(w[k]);
-      Hsbg(k,i) += prod;
-      w[i+1] -= prod * w[k];
+    if (prod * prod > thr) {
+      prod = w[i + 1].dot(w[k]);
+      Hsbg(k, i) += prod;
+      w[i + 1] -= prod * w[k];
     }
 
     /*--- Update the norm and check its size ---*/
 
-    nrm -= pow(Hsbg(k,i),2);
+    nrm -= pow(Hsbg(k, i), 2);
     nrm = max<ScalarType>(nrm, 0.0);
-    thr = nrm*reorth;
+    thr = nrm * reorth;
   }
 
   /*--- Test the resulting vector ---*/
 
-  nrm = w[i+1].norm();
-  Hsbg(i+1,i) = nrm;
+  nrm = w[i + 1].norm();
+  Hsbg(i + 1, i) = nrm;
 
   /*--- Scale the resulting vector ---*/
 
-  w[i+1] /= nrm;
-
+  w[i + 1] /= nrm;
 }
 
-template<class ScalarType>
+template <class ScalarType>
 void CSysSolve<ScalarType>::WriteHeader(string solver, ScalarType restol, ScalarType resinit) const {
-
   cout << "\n# " << solver << " residual history\n";
   cout << "# Residual tolerance target = " << restol << "\n";
   cout << "# Initial residual norm     = " << resinit << endl;
 }
 
-template<class ScalarType>
+template <class ScalarType>
 void CSysSolve<ScalarType>::WriteHistory(unsigned long iter, ScalarType res) const {
-
   cout << "     " << iter << "     " << res << endl;
 }
 
-template<class ScalarType>
+template <class ScalarType>
 void CSysSolve<ScalarType>::WriteFinalResidual(string solver, unsigned long iter, ScalarType res) const {
-
   cout << "# " << solver << " final (true) residual:\n";
   cout << "# Iteration = " << iter << ": |res|/|res0| = " << res << ".\n" << endl;
 }
 
-template<class ScalarType>
+template <class ScalarType>
 void CSysSolve<ScalarType>::WriteWarning(ScalarType res_calc, ScalarType res_true, ScalarType tol) const {
-
   cout << "# WARNING:\n";
   cout << "# true residual norm and calculated residual norm do not agree.\n";
-  cout << "# true_res = " << res_true << ", calc_res = " << res_calc << ", tol = " << tol*10 << ".\n";
+  cout << "# true_res = " << res_true << ", calc_res = " << res_calc << ", tol = " << tol * 10 << ".\n";
   cout << "# true_res - calc_res = " << res_true - res_calc << endl;
 }
 
-template<class ScalarType>
-unsigned long CSysSolve<ScalarType>::CG_LinSolver(const CSysVector<ScalarType> & b, CSysVector<ScalarType> & x,
-                                                  const CMatrixVectorProduct<ScalarType> & mat_vec, const CPreconditioner<ScalarType> & precond,
-                                                  ScalarType tol, unsigned long m, ScalarType & residual, bool monitoring, const CConfig *config) const {
-
+template <class ScalarType>
+unsigned long CSysSolve<ScalarType>::CG_LinSolver(const CSysVector<ScalarType>& b, CSysVector<ScalarType>& x,
+                                                  const CMatrixVectorProduct<ScalarType>& mat_vec,
+                                                  const CPreconditioner<ScalarType>& precond, ScalarType tol,
+                                                  unsigned long m, ScalarType& residual, bool monitoring,
+                                                  const CConfig* config) const {
   const bool master = (SU2_MPI::GetRank() == MASTER_NODE) && (omp_get_thread_num() == 0);
   ScalarType norm_r = 0.0, norm0 = 0.0;
   unsigned long i = 0;
@@ -214,8 +206,7 @@ unsigned long CSysSolve<ScalarType>::CG_LinSolver(const CSysVector<ScalarType> &
    *    do this since the working vectors are shared. ---*/
 
   if (!cg_ready) {
-    BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS
-    {
+    BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
       auto nVar = b.GetNVar();
       auto nBlk = b.GetNBlk();
       auto nBlkDomain = b.GetNBlkDomain();
@@ -242,16 +233,16 @@ unsigned long CSysSolve<ScalarType>::CG_LinSolver(const CSysVector<ScalarType> &
   /*--- Only compute the residuals in full communication mode. ---*/
 
   if (config->GetComm_Level() == COMM_FULL) {
-
     norm_r = r.norm();
-    norm0  = b.norm();
+    norm0 = b.norm();
 
     /*--- Set the norm to the initial initial residual value ---*/
 
     if (tol_type == LinearToleranceType::RELATIVE) norm0 = norm_r;
 
-    if ((norm_r < tol*norm0) || (norm_r < eps)) {
-      if (master && (lin_sol_mode!=LINEAR_SOLVER_MODE::MESH_DEFORM)) cout << "CSysSolve::ConjugateGradient(): system solved by initial guess." << endl;
+    if ((norm_r < tol * norm0) || (norm_r < eps)) {
+      if (master && (lin_sol_mode != LINEAR_SOLVER_MODE::MESH_DEFORM))
+        cout << "CSysSolve::ConjugateGradient(): system solved by initial guess." << endl;
       return 0;
     }
 
@@ -259,9 +250,8 @@ unsigned long CSysSolve<ScalarType>::CG_LinSolver(const CSysVector<ScalarType> &
 
     if (monitoring && master) {
       WriteHeader("CG", tol, norm_r);
-      WriteHistory(i, norm_r/norm0);
+      WriteHistory(i, norm_r / norm0);
     }
-
   }
 
   precond(r, z);
@@ -271,7 +261,6 @@ unsigned long CSysSolve<ScalarType>::CG_LinSolver(const CSysVector<ScalarType> &
   /*---  Loop over all search directions ---*/
 
   for (i = 0; i < m; i++) {
-
     /*--- Apply matrix to p to build Krylov subspace ---*/
 
     mat_vec(p, A_x);
@@ -288,14 +277,11 @@ unsigned long CSysSolve<ScalarType>::CG_LinSolver(const CSysVector<ScalarType> &
     /*--- Only compute the residuals in full communication mode. ---*/
 
     if (config->GetComm_Level() == COMM_FULL) {
-
       /*--- Check if solution has converged, else output the relative residual if necessary ---*/
 
       norm_r = r.norm();
-      if (norm_r < tol*norm0) break;
-      if (((monitoring) && (master)) && ((i+1) % monitorFreq == 0))
-        WriteHistory(i+1, norm_r/norm0);
-
+      if (norm_r < tol * norm0) break;
+      if (((monitoring) && (master)) && ((i + 1) % monitorFreq == 0)) WriteHistory(i + 1, norm_r / norm0);
     }
 
     precond(r, z);
@@ -308,22 +294,20 @@ unsigned long CSysSolve<ScalarType>::CG_LinSolver(const CSysVector<ScalarType> &
 
     /*--- Gram-Schmidt orthogonalization. ---*/
 
-    p = beta*p + z;
-
+    p = beta * p + z;
   }
 
   /*--- Recalculate final residual (this should be optional) ---*/
 
   if ((monitoring) && (config->GetComm_Level() == COMM_FULL)) {
-
-    if (master) WriteFinalResidual("CG", i, norm_r/norm0);
+    if (master) WriteFinalResidual("CG", i, norm_r / norm0);
 
     if (recomputeRes) {
       mat_vec(x, A_x);
       r = b - A_x;
       ScalarType true_res = r.norm();
 
-      if (fabs(true_res - norm_r) > tol*10.0) {
+      if (fabs(true_res - norm_r) > tol * 10.0) {
         if (master) {
           WriteWarning(norm_r, true_res, tol);
         }
@@ -331,16 +315,16 @@ unsigned long CSysSolve<ScalarType>::CG_LinSolver(const CSysVector<ScalarType> &
     }
   }
 
-  residual = norm_r/norm0;
+  residual = norm_r / norm0;
   return i;
-
 }
 
-template<class ScalarType>
-unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarType> & b, CSysVector<ScalarType> & x,
-                                                      const CMatrixVectorProduct<ScalarType> & mat_vec, const CPreconditioner<ScalarType> & precond,
-                                                      ScalarType tol, unsigned long m, ScalarType & residual, bool monitoring, const CConfig *config) const {
-
+template <class ScalarType>
+unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarType>& b, CSysVector<ScalarType>& x,
+                                                      const CMatrixVectorProduct<ScalarType>& mat_vec,
+                                                      const CPreconditioner<ScalarType>& precond, ScalarType tol,
+                                                      unsigned long m, ScalarType& residual, bool monitoring,
+                                                      const CConfig* config) const {
   const bool master = (SU2_MPI::GetRank() == MASTER_NODE) && (omp_get_thread_num() == 0);
   const bool flexible = !precond.IsIdentity();
 
@@ -357,12 +341,11 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
   /*--- Allocate if not allocated yet ---*/
 
   if (W.size() <= m || (flexible && Z.size() <= m)) {
-    BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS
-    {
-      W.resize(m+1);
+    BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
+      W.resize(m + 1);
       for (auto& w : W) w.Initialize(x.GetNBlk(), x.GetNBlkDomain(), x.GetNVar(), nullptr);
       if (flexible) {
-        Z.resize(m+1);
+        Z.resize(m + 1);
         for (auto& z : Z) z.Initialize(x.GetNBlk(), x.GetNBlkDomain(), x.GetNVar(), nullptr);
       }
     }
@@ -373,12 +356,12 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
    on its own thread, since calculations on these arrays are based on dot products
    (reduced across all threads and ranks) all threads do the same computations. ---*/
 
-  su2vector<ScalarType> g(m+1), sn(m+1), cs(m+1), y(m);
+  su2vector<ScalarType> g(m + 1), sn(m + 1), cs(m + 1), y(m);
   g = ScalarType(0);
   sn = ScalarType(0);
   cs = ScalarType(0);
   y = ScalarType(0);
-  su2matrix<ScalarType> H(m+1, m);
+  su2matrix<ScalarType> H(m + 1, m);
   H = ScalarType(0);
 
   /*--- Calculate the norm of the rhs vector. ---*/
@@ -390,8 +373,7 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
   if (!xIsZero) {
     mat_vec(x, W[0]);
     W[0] -= b;
-  }
-  else {
+  } else {
     W[0] = -b;
   }
 
@@ -401,8 +383,7 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
 
   if (tol_type == LinearToleranceType::RELATIVE) norm0 = beta;
 
-  if ((beta < tol*norm0) || (beta < eps)) {
-
+  if ((beta < tol * norm0) || (beta < eps)) {
     /*--- System is already solved ---*/
 
     if (master) cout << "CSysSolve::FGMRES(): system solved by initial guess." << endl;
@@ -424,16 +405,15 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
   unsigned long i = 0;
   if ((monitoring) && (master)) {
     WriteHeader("FGMRES", tol, beta);
-    WriteHistory(i, beta/norm0);
+    WriteHistory(i, beta / norm0);
   }
 
   /*---  Loop over all search directions ---*/
 
   for (i = 0; i < m; i++) {
-
     /*---  Check if solution has converged ---*/
 
-    if (beta < tol*norm0) break;
+    if (beta < tol * norm0) break;
 
     if (flexible) {
       /*---  Precondition the CSysVector w[i] and store result in z[i] ---*/
@@ -442,10 +422,9 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
 
       /*---  Add to Krylov subspace ---*/
 
-      mat_vec(Z[i], W[i+1]);
-    }
-    else {
-      mat_vec(W[i], W[i+1]);
+      mat_vec(Z[i], W[i + 1]);
+    } else {
+      mat_vec(W[i], W[i + 1]);
     }
 
     /*---  Modified Gram-Schmidt orthogonalization ---*/
@@ -455,26 +434,24 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
     /*---  Apply old Givens rotations to new column of the Hessenberg matrix then generate the
      new Givens rotation matrix and apply it to the last two elements of H[:][i] and g ---*/
 
-    for (unsigned long k = 0; k < i; k++)
-      ApplyGivens(sn[k], cs[k], H[k][i], H[k+1][i]);
-    GenerateGivens(H[i][i], H[i+1][i], sn[i], cs[i]);
-    ApplyGivens(sn[i], cs[i], g[i], g[i+1]);
+    for (unsigned long k = 0; k < i; k++) ApplyGivens(sn[k], cs[k], H[k][i], H[k + 1][i]);
+    GenerateGivens(H[i][i], H[i + 1][i], sn[i], cs[i]);
+    ApplyGivens(sn[i], cs[i], g[i], g[i + 1]);
 
     /*---  Set L2 norm of residual and check if solution has converged ---*/
 
-    beta = fabs(g[i+1]);
+    beta = fabs(g[i + 1]);
 
     /*---  Output the relative residual if necessary ---*/
 
-    if ((((monitoring) && (master)) && ((i+1) % monitorFreq == 0)) && (master))
-      WriteHistory(i+1, beta/norm0);
+    if ((((monitoring) && (master)) && ((i + 1) % monitorFreq == 0)) && (master)) WriteHistory(i + 1, beta / norm0);
   }
 
   /*---  Solve the least-squares system and update solution ---*/
 
   SolveReduced(i, H, g, y);
 
-  const auto& basis = flexible? Z : W;
+  const auto& basis = flexible ? Z : W;
 
   for (unsigned long k = 0; k < i; k++) {
     x += y[k] * basis[k];
@@ -483,15 +460,14 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
   /*---  Recalculate final (neg.) residual (this should be optional) ---*/
 
   if ((monitoring) && (config->GetComm_Level() == COMM_FULL)) {
-
-    if (master) WriteFinalResidual("FGMRES", i, beta/norm0);
+    if (master) WriteFinalResidual("FGMRES", i, beta / norm0);
 
     if (recomputeRes) {
       mat_vec(x, W[0]);
       W[0] -= b;
       ScalarType res = W[0].norm();
 
-      if (fabs(res - beta) > tol*10) {
+      if (fabs(res - beta) > tol * 10) {
         if (master) {
           WriteWarning(beta, res, tol);
         }
@@ -499,16 +475,16 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
     }
   }
 
-  residual = beta/norm0;
+  residual = beta / norm0;
   return i;
-
 }
 
-template<class ScalarType>
-unsigned long CSysSolve<ScalarType>::RFGMRES_LinSolver(const CSysVector<ScalarType> & b, CSysVector<ScalarType> & x,
-                                                       const CMatrixVectorProduct<ScalarType> & mat_vec, const CPreconditioner<ScalarType> & precond,
-                                                       ScalarType tol, unsigned long MaxIter, ScalarType & residual, bool monitoring, const CConfig *config) {
-
+template <class ScalarType>
+unsigned long CSysSolve<ScalarType>::RFGMRES_LinSolver(const CSysVector<ScalarType>& b, CSysVector<ScalarType>& x,
+                                                       const CMatrixVectorProduct<ScalarType>& mat_vec,
+                                                       const CPreconditioner<ScalarType>& precond, ScalarType tol,
+                                                       unsigned long MaxIter, ScalarType& residual, bool monitoring,
+                                                       const CConfig* config) {
   const auto restartIter = config->GetLinear_Solver_Restart_Frequency();
 
   SU2_OMP_MASTER {
@@ -517,23 +493,24 @@ unsigned long CSysSolve<ScalarType>::RFGMRES_LinSolver(const CSysVector<ScalarTy
   }
   END_SU2_OMP_MASTER
 
-  const ScalarType norm0 = b.norm(); // <- Has a barrier
+  const ScalarType norm0 = b.norm();  // <- Has a barrier
 
   for (auto totalIter = 0ul; totalIter < MaxIter;) {
     /*--- Enforce a hard limit on total number of iterations ---*/
-    auto iterLimit = min(restartIter, MaxIter-totalIter);
+    auto iterLimit = min(restartIter, MaxIter - totalIter);
     auto iter = FGMRES_LinSolver(b, x, mat_vec, precond, tol, iterLimit, residual, monitoring, config);
     totalIter += iter;
-    if (residual <= tol*norm0 || iter < iterLimit) return totalIter;
+    if (residual <= tol * norm0 || iter < iterLimit) return totalIter;
   }
   return 0;
 }
 
-template<class ScalarType>
-unsigned long CSysSolve<ScalarType>::BCGSTAB_LinSolver(const CSysVector<ScalarType> & b, CSysVector<ScalarType> & x,
-                                                       const CMatrixVectorProduct<ScalarType> & mat_vec, const CPreconditioner<ScalarType> & precond,
-                                                       ScalarType tol, unsigned long m, ScalarType & residual, bool monitoring, const CConfig *config) const {
-
+template <class ScalarType>
+unsigned long CSysSolve<ScalarType>::BCGSTAB_LinSolver(const CSysVector<ScalarType>& b, CSysVector<ScalarType>& x,
+                                                       const CMatrixVectorProduct<ScalarType>& mat_vec,
+                                                       const CPreconditioner<ScalarType>& precond, ScalarType tol,
+                                                       unsigned long m, ScalarType& residual, bool monitoring,
+                                                       const CConfig* config) const {
   const bool master = (SU2_MPI::GetRank() == MASTER_NODE) && (omp_get_thread_num() == 0);
   ScalarType norm_r = 0.0, norm0 = 0.0;
   unsigned long i = 0;
@@ -547,8 +524,7 @@ unsigned long CSysSolve<ScalarType>::BCGSTAB_LinSolver(const CSysVector<ScalarTy
   /*--- Allocate if not allocated yet ---*/
 
   if (!bcg_ready) {
-    BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS
-    {
+    BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
       auto nVar = b.GetNVar();
       auto nBlk = b.GetNBlk();
       auto nBlkDomain = b.GetNBlkDomain();
@@ -577,15 +553,14 @@ unsigned long CSysSolve<ScalarType>::BCGSTAB_LinSolver(const CSysVector<ScalarTy
   /*--- Only compute the residuals in full communication mode. ---*/
 
   if (config->GetComm_Level() == COMM_FULL) {
-
     norm_r = r.norm();
-    norm0  = b.norm();
+    norm0 = b.norm();
 
     /*--- Set the norm to the initial initial residual value ---*/
 
     if (tol_type == LinearToleranceType::RELATIVE) norm0 = norm_r;
 
-    if ((norm_r < tol*norm0) || (norm_r < eps)) {
+    if ((norm_r < tol * norm0) || (norm_r < eps)) {
       if (master) cout << "CSysSolve::BCGSTAB(): system solved by initial guess." << endl;
       return 0;
     }
@@ -594,20 +569,20 @@ unsigned long CSysSolve<ScalarType>::BCGSTAB_LinSolver(const CSysVector<ScalarTy
 
     if ((monitoring) && (master)) {
       WriteHeader("BCGSTAB", tol, norm_r);
-      WriteHistory(i, norm_r/norm0);
+      WriteHistory(i, norm_r / norm0);
     }
-
   }
 
   /*--- Initialization ---*/
 
   ScalarType alpha = 1.0, omega = 1.0, rho = 1.0, rho_prime = 1.0;
-  p = ScalarType(0.0); v = ScalarType(0.0); r_0 = r;
+  p = ScalarType(0.0);
+  v = ScalarType(0.0);
+  r_0 = r;
 
   /*--- Loop over all search directions ---*/
 
   for (i = 0; i < m; i++) {
-
     /*--- Compute rho_prime ---*/
 
     rho_prime = rho;
@@ -618,11 +593,11 @@ unsigned long CSysSolve<ScalarType>::BCGSTAB_LinSolver(const CSysVector<ScalarTy
 
     /*--- Compute beta ---*/
 
-    ScalarType beta = (rho / rho_prime) * (alpha /omega);
+    ScalarType beta = (rho / rho_prime) * (alpha / omega);
 
     /*--- Update p ---*/
 
-    p = beta * (p - omega*v) + r;
+    p = beta * (p - omega * v) + r;
 
     /*--- Preconditioning step ---*/
 
@@ -658,44 +633,40 @@ unsigned long CSysSolve<ScalarType>::BCGSTAB_LinSolver(const CSysVector<ScalarTy
     /*--- Only compute the residuals in full communication mode. ---*/
 
     if (config->GetComm_Level() == COMM_FULL) {
-
       /*--- Check if solution has converged, else output the relative residual if necessary ---*/
 
       norm_r = r.norm();
-      if (norm_r < tol*norm0) break;
-      if (((monitoring) && (master)) && ((i+1) % monitorFreq == 0) && (master))
-        WriteHistory(i+1, norm_r/norm0);
-
+      if (norm_r < tol * norm0) break;
+      if (((monitoring) && (master)) && ((i + 1) % monitorFreq == 0) && (master)) WriteHistory(i + 1, norm_r / norm0);
     }
-
   }
 
   /*--- Recalculate final residual (this should be optional) ---*/
 
   if ((monitoring) && (config->GetComm_Level() == COMM_FULL)) {
-
-    if (master) WriteFinalResidual("BCGSTAB", i, norm_r/norm0);
+    if (master) WriteFinalResidual("BCGSTAB", i, norm_r / norm0);
 
     if (recomputeRes) {
       mat_vec(x, A_x);
       r = b - A_x;
       ScalarType true_res = r.norm();
 
-      if ((fabs(true_res - norm_r) > tol*10.0) && (master)) {
+      if ((fabs(true_res - norm_r) > tol * 10.0) && (master)) {
         WriteWarning(norm_r, true_res, tol);
       }
     }
   }
 
-  residual = norm_r/norm0;
+  residual = norm_r / norm0;
   return i;
 }
 
-template<class ScalarType>
-unsigned long CSysSolve<ScalarType>::Smoother_LinSolver(const CSysVector<ScalarType> & b, CSysVector<ScalarType> & x,
-                                                        const CMatrixVectorProduct<ScalarType> & mat_vec, const CPreconditioner<ScalarType> & precond,
-                                                        ScalarType tol, unsigned long m, ScalarType & residual, bool monitoring, const CConfig *config) const {
-
+template <class ScalarType>
+unsigned long CSysSolve<ScalarType>::Smoother_LinSolver(const CSysVector<ScalarType>& b, CSysVector<ScalarType>& x,
+                                                        const CMatrixVectorProduct<ScalarType>& mat_vec,
+                                                        const CPreconditioner<ScalarType>& precond, ScalarType tol,
+                                                        unsigned long m, ScalarType& residual, bool monitoring,
+                                                        const CConfig* config) const {
   const bool master = (SU2_MPI::GetRank() == MASTER_NODE) && (omp_get_thread_num() == 0);
   const bool fix_iter_mode = tol < eps;
   ScalarType norm_r = 0.0, norm0 = 0.0;
@@ -712,8 +683,7 @@ unsigned long CSysSolve<ScalarType>::Smoother_LinSolver(const CSysVector<ScalarT
    product (A_x), for the latter two this is done only on the first call to the method. ---*/
 
   if (!smooth_ready) {
-    BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS
-    {
+    BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
       auto nVar = b.GetNVar();
       auto nBlk = b.GetNBlk();
       auto nBlkDomain = b.GetNBlkDomain();
@@ -739,15 +709,14 @@ unsigned long CSysSolve<ScalarType>::Smoother_LinSolver(const CSysVector<ScalarT
   /*--- Only compute the residuals in full communication mode. ---*/
 
   if (config->GetComm_Level() == COMM_FULL) {
-
     norm_r = r.norm();
-    norm0  = b.norm();
+    norm0 = b.norm();
 
     /*--- Set the norm to the initial initial residual value ---*/
 
     if (tol_type == LinearToleranceType::RELATIVE) norm0 = norm_r;
 
-    if ( (norm_r < tol*norm0) || (norm_r < eps) ) {
+    if ((norm_r < tol * norm0) || (norm_r < eps)) {
       if (master) cout << "CSysSolve::Smoother_LinSolver(): system solved by initial guess." << endl;
       return 0;
     }
@@ -756,15 +725,13 @@ unsigned long CSysSolve<ScalarType>::Smoother_LinSolver(const CSysVector<ScalarT
 
     if ((monitoring) && (master)) {
       WriteHeader("Smoother", tol, norm_r);
-      WriteHistory(i, norm_r/norm0);
+      WriteHistory(i, norm_r / norm0);
     }
-
   }
 
   /*--- Smoothing Iterations ---*/
 
-  for (i=0; i<m; i++) {
-
+  for (i = 0; i < m; i++) {
     /*--- Compute the solution increment (z), or "search" direction, by applying
      the preconditioner to the residual, i.e. z = M^{-1} * r. ---*/
 
@@ -791,25 +758,25 @@ unsigned long CSysSolve<ScalarType>::Smoother_LinSolver(const CSysVector<ScalarT
 
     if (!fix_iter_mode && config->GetComm_Level() == COMM_FULL) {
       norm_r = r.norm();
-      if (norm_r < tol*norm0) break;
-      if (((monitoring) && (master)) && ((i+1) % monitorFreq == 0))
-        WriteHistory(i+1, norm_r/norm0);
+      if (norm_r < tol * norm0) break;
+      if (((monitoring) && (master)) && ((i + 1) % monitorFreq == 0)) WriteHistory(i + 1, norm_r / norm0);
     }
   }
 
   if (fix_iter_mode) norm_r = r.norm();
 
   if ((monitoring) && (master) && (config->GetComm_Level() == COMM_FULL)) {
-    WriteFinalResidual("Smoother", i, norm_r/norm0);
+    WriteFinalResidual("Smoother", i, norm_r / norm0);
   }
 
-  residual = norm_r/norm0;
+  residual = norm_r / norm0;
   return i;
 }
 
-template<class ScalarType>
-unsigned long CSysSolve<ScalarType>::Solve(CSysMatrix<ScalarType> & Jacobian, const CSysVector<su2double> & LinSysRes,
-                                           CSysVector<su2double> & LinSysSol, CGeometry *geometry, const CConfig *config) {
+template <class ScalarType>
+unsigned long CSysSolve<ScalarType>::Solve(CSysMatrix<ScalarType>& Jacobian, const CSysVector<su2double>& LinSysRes,
+                                           CSysVector<su2double>& LinSysSol, CGeometry* geometry,
+                                           const CConfig* config) {
   /*---
    A word about the templated types. It is assumed that the residual and solution vectors are always of su2doubles,
    meaning that they are active in the discrete adjoint. The same assumption is made in SetExternalSolve.
@@ -828,31 +795,32 @@ unsigned long CSysSolve<ScalarType>::Solve(CSysMatrix<ScalarType> & Jacobian, co
   switch (lin_sol_mode) {
     /*--- Mesh Deformation mode ---*/
     case LINEAR_SOLVER_MODE::MESH_DEFORM: {
-      KindSolver   = config->GetKind_Deform_Linear_Solver();
-      KindPrecond  = config->GetKind_Deform_Linear_Solver_Prec();
-      MaxIter      = config->GetDeform_Linear_Solver_Iter();
-      SolverTol    = SU2_TYPE::GetValue(config->GetDeform_Linear_Solver_Error());
+      KindSolver = config->GetKind_Deform_Linear_Solver();
+      KindPrecond = config->GetKind_Deform_Linear_Solver_Prec();
+      MaxIter = config->GetDeform_Linear_Solver_Iter();
+      SolverTol = SU2_TYPE::GetValue(config->GetDeform_Linear_Solver_Error());
       ScreenOutput = config->GetDeform_Output();
       break;
     }
 
     /*--- Gradient Smoothing mode ---*/
     case LINEAR_SOLVER_MODE::GRADIENT_MODE: {
-      KindSolver   = config->GetKind_Grad_Linear_Solver();
-      KindPrecond  = config->GetKind_Grad_Linear_Solver_Prec();
-      MaxIter      = config->GetGrad_Linear_Solver_Iter();
-      SolverTol    = SU2_TYPE::GetValue(config->GetGrad_Linear_Solver_Error());
+      KindSolver = config->GetKind_Grad_Linear_Solver();
+      KindPrecond = config->GetKind_Grad_Linear_Solver_Prec();
+      MaxIter = config->GetGrad_Linear_Solver_Iter();
+      SolverTol = SU2_TYPE::GetValue(config->GetGrad_Linear_Solver_Error());
       ScreenOutput = true;
       break;
     }
 
     /*--- Normal mode
-     * assumes that 'lin_sol_mode==LINEAR_SOLVER_MODE::STANDARD', but does not enforce it to avoid compiler warning. ---*/
+     * assumes that 'lin_sol_mode==LINEAR_SOLVER_MODE::STANDARD', but does not enforce it to avoid compiler warning.
+     * ---*/
     default: {
-      KindSolver   = config->GetKind_Linear_Solver();
-      KindPrecond  = config->GetKind_Linear_Solver_Prec();
-      MaxIter      = config->GetLinear_Solver_Iter();
-      SolverTol    = SU2_TYPE::GetValue(config->GetLinear_Solver_Error());
+      KindSolver = config->GetKind_Linear_Solver();
+      KindPrecond = config->GetKind_Linear_Solver_Prec();
+      MaxIter = config->GetLinear_Solver_Iter();
+      SolverTol = SU2_TYPE::GetValue(config->GetLinear_Solver_Error());
       ScreenOutput = false;
       break;
     }
@@ -905,32 +873,37 @@ unsigned long CSysSolve<ScalarType>::Solve(CSysMatrix<ScalarType> & Jacobian, co
 
     switch (KindSolver) {
       case BCGSTAB:
-        IterLinSol = BCGSTAB_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual, ScreenOutput, config);
+        IterLinSol = BCGSTAB_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual,
+                                       ScreenOutput, config);
         break;
       case FGMRES:
-        IterLinSol = FGMRES_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual, ScreenOutput, config);
+        IterLinSol = FGMRES_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual,
+                                      ScreenOutput, config);
         break;
       case RESTARTED_FGMRES:
-        IterLinSol = RFGMRES_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual, ScreenOutput, config);
+        IterLinSol = RFGMRES_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual,
+                                       ScreenOutput, config);
         break;
       case CONJUGATE_GRADIENT:
-        IterLinSol = CG_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual, ScreenOutput, config);
+        IterLinSol = CG_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual,
+                                  ScreenOutput, config);
         break;
       case SMOOTHER:
-        IterLinSol = Smoother_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual, ScreenOutput, config);
+        IterLinSol = Smoother_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual,
+                                        ScreenOutput, config);
         break;
-      case PASTIX_LDLT : case PASTIX_LU:
+      case PASTIX_LDLT:
+      case PASTIX_LU:
         Jacobian.BuildPastixPreconditioner(geometry, config, KindSolver);
         Jacobian.ComputePastixPreconditioner(*LinSysRes_ptr, *LinSysSol_ptr, geometry, config);
         IterLinSol = 1;
         residual = 1e-20;
         break;
       default:
-        SU2_MPI::Error("Unknown type of linear solver.",CURRENT_FUNCTION);
+        SU2_MPI::Error("Unknown type of linear solver.", CURRENT_FUNCTION);
     }
 
-    SU2_OMP_MASTER
-    {
+    SU2_OMP_MASTER {
       Residual = residual;
       Iterations = IterLinSol;
     }
@@ -940,20 +913,23 @@ unsigned long CSysSolve<ScalarType>::Solve(CSysMatrix<ScalarType> & Jacobian, co
 
     delete precond;
 
-    if(TapeActive) {
-
+    if (TapeActive) {
       /*--- To keep the behavior of SU2_DOT, but not strictly required since jacobian is symmetric(?). ---*/
-      const bool RequiresTranspose = ((lin_sol_mode!=LINEAR_SOLVER_MODE::MESH_DEFORM) || (config->GetKind_SU2() == SU2_COMPONENT::SU2_DOT));
+      const bool RequiresTranspose =
+          ((lin_sol_mode != LINEAR_SOLVER_MODE::MESH_DEFORM) || (config->GetKind_SU2() == SU2_COMPONENT::SU2_DOT));
 
-      if      (lin_sol_mode==LINEAR_SOLVER_MODE::MESH_DEFORM)   KindPrecond = config->GetKind_Deform_Linear_Solver_Prec();
-      else if (lin_sol_mode==LINEAR_SOLVER_MODE::GRADIENT_MODE) KindPrecond  = config->GetKind_Grad_Linear_Solver_Prec();
-      else    KindPrecond = config->GetKind_DiscAdj_Linear_Prec();
+      if (lin_sol_mode == LINEAR_SOLVER_MODE::MESH_DEFORM)
+        KindPrecond = config->GetKind_Deform_Linear_Solver_Prec();
+      else if (lin_sol_mode == LINEAR_SOLVER_MODE::GRADIENT_MODE)
+        KindPrecond = config->GetKind_Grad_Linear_Solver_Prec();
+      else
+        KindPrecond = config->GetKind_DiscAdj_Linear_Prec();
 
       /*--- Build preconditioner for the transposed Jacobian ---*/
 
       if (RequiresTranspose) Jacobian.TransposeInPlace();
 
-      switch(KindPrecond) {
+      switch (KindPrecond) {
         case ILU:
           if (RequiresTranspose) Jacobian.BuildILUPreconditioner();
           break;
@@ -964,11 +940,14 @@ unsigned long CSysSolve<ScalarType>::Solve(CSysMatrix<ScalarType> & Jacobian, co
         case LU_SGS:
           /*--- Nothing to build. ---*/
           break;
-        case PASTIX_ILU: case PASTIX_LU_P: case PASTIX_LDLT_P:
+        case PASTIX_ILU:
+        case PASTIX_LU_P:
+        case PASTIX_LDLT_P:
           /*--- It was already built. ---*/
           break;
         default:
-          SU2_MPI::Error("The specified preconditioner is not yet implemented for the discrete adjoint method.", CURRENT_FUNCTION);
+          SU2_MPI::Error("The specified preconditioner is not yet implemented for the discrete adjoint method.",
+                         CURRENT_FUNCTION);
           break;
       }
     }
@@ -987,11 +966,10 @@ unsigned long CSysSolve<ScalarType>::Solve(CSysMatrix<ScalarType> & Jacobian, co
   return IterLinSol;
 }
 
-template<class ScalarType>
-unsigned long CSysSolve<ScalarType>::Solve_b(CSysMatrix<ScalarType> & Jacobian, const CSysVector<su2double> & LinSysRes,
-                                             CSysVector<su2double> & LinSysSol, CGeometry *geometry, const CConfig *config,
-                                             const bool directCall) {
-
+template <class ScalarType>
+unsigned long CSysSolve<ScalarType>::Solve_b(CSysMatrix<ScalarType>& Jacobian, const CSysVector<su2double>& LinSysRes,
+                                             CSysVector<su2double>& LinSysSol, CGeometry* geometry,
+                                             const CConfig* config, const bool directCall) {
   unsigned short KindSolver, KindPrecond;
   unsigned long MaxIter, IterLinSol = 0;
   ScalarType SolverTol;
@@ -1000,31 +978,32 @@ unsigned long CSysSolve<ScalarType>::Solve_b(CSysMatrix<ScalarType> & Jacobian,
   switch (lin_sol_mode) {
     /*--- Mesh Deformation mode ---*/
     case LINEAR_SOLVER_MODE::MESH_DEFORM: {
-      KindSolver   = config->GetKind_Deform_Linear_Solver();
-      KindPrecond  = config->GetKind_Deform_Linear_Solver_Prec();
-      MaxIter      = config->GetDeform_Linear_Solver_Iter();
-      SolverTol    = SU2_TYPE::GetValue(config->GetDeform_Linear_Solver_Error());
+      KindSolver = config->GetKind_Deform_Linear_Solver();
+      KindPrecond = config->GetKind_Deform_Linear_Solver_Prec();
+      MaxIter = config->GetDeform_Linear_Solver_Iter();
+      SolverTol = SU2_TYPE::GetValue(config->GetDeform_Linear_Solver_Error());
       ScreenOutput = config->GetDeform_Output();
       break;
     }
 
     /*--- Gradient Smoothing mode ---*/
     case LINEAR_SOLVER_MODE::GRADIENT_MODE: {
-      KindSolver   = config->GetKind_Grad_Linear_Solver();
-      KindPrecond  = config->GetKind_Grad_Linear_Solver_Prec();
-      MaxIter      = config->GetGrad_Linear_Solver_Iter();
-      SolverTol    = SU2_TYPE::GetValue(config->GetGrad_Linear_Solver_Error());
+      KindSolver = config->GetKind_Grad_Linear_Solver();
+      KindPrecond = config->GetKind_Grad_Linear_Solver_Prec();
+      MaxIter = config->GetGrad_Linear_Solver_Iter();
+      SolverTol = SU2_TYPE::GetValue(config->GetGrad_Linear_Solver_Error());
       ScreenOutput = true;
       break;
     }
 
     /*--- Normal mode
-     * assumes that 'lin_sol_mode==LINEAR_SOLVER_MODE::STANDARD', but does not enforce it to avoid compiler warning. ---*/
+     * assumes that 'lin_sol_mode==LINEAR_SOLVER_MODE::STANDARD', but does not enforce it to avoid compiler warning.
+     * ---*/
     default: {
-      KindSolver   = config->GetKind_Linear_Solver();
-      KindPrecond  = config->GetKind_Linear_Solver_Prec();
-      MaxIter      = config->GetLinear_Solver_Iter();
-      SolverTol    = SU2_TYPE::GetValue(config->GetLinear_Solver_Error());
+      KindSolver = config->GetKind_Linear_Solver();
+      KindPrecond = config->GetKind_Linear_Solver_Prec();
+      MaxIter = config->GetLinear_Solver_Iter();
+      SolverTol = SU2_TYPE::GetValue(config->GetLinear_Solver_Error());
       ScreenOutput = false;
       break;
     }
@@ -1051,30 +1030,36 @@ unsigned long CSysSolve<ScalarType>::Solve_b(CSysMatrix<ScalarType> & Jacobian,
 
   HandleTemporariesIn(LinSysRes, LinSysSol);
 
-  switch(KindSolver) {
+  switch (KindSolver) {
     case FGMRES:
-      IterLinSol = FGMRES_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol , MaxIter, residual, ScreenOutput, config);
+      IterLinSol = FGMRES_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual,
+                                    ScreenOutput, config);
       break;
     case RESTARTED_FGMRES:
-      IterLinSol = RFGMRES_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol , MaxIter, residual, ScreenOutput, config);
+      IterLinSol = RFGMRES_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual,
+                                     ScreenOutput, config);
       break;
     case BCGSTAB:
-      IterLinSol = BCGSTAB_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol , MaxIter, residual, ScreenOutput, config);
+      IterLinSol = BCGSTAB_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual,
+                                     ScreenOutput, config);
       break;
     case CONJUGATE_GRADIENT:
-      IterLinSol = CG_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual, ScreenOutput, config);
+      IterLinSol = CG_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual,
+                                ScreenOutput, config);
       break;
     case SMOOTHER:
-      IterLinSol = Smoother_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual, ScreenOutput, config);
+      IterLinSol = Smoother_LinSolver(*LinSysRes_ptr, *LinSysSol_ptr, mat_vec, *precond, SolverTol, MaxIter, residual,
+                                      ScreenOutput, config);
       break;
-    case PASTIX_LDLT : case PASTIX_LU:
+    case PASTIX_LDLT:
+    case PASTIX_LU:
       if (directCall) Jacobian.BuildPastixPreconditioner(geometry, config, KindSolver);
       Jacobian.ComputePastixPreconditioner(*LinSysRes_ptr, *LinSysSol_ptr, geometry, config);
       IterLinSol = 1;
       residual = 1e-20;
       break;
     default:
-      SU2_MPI::Error("Unknown type of linear solver.",CURRENT_FUNCTION);
+      SU2_MPI::Error("Unknown type of linear solver.", CURRENT_FUNCTION);
       break;
   }
 
@@ -1082,14 +1067,13 @@ unsigned long CSysSolve<ScalarType>::Solve_b(CSysMatrix<ScalarType> & Jacobian,
 
   delete precond;
 
-  SU2_OMP_MASTER
-  {
+  SU2_OMP_MASTER {
     Residual = residual;
     Iterations = IterLinSol;
-  } END_SU2_OMP_MASTER
+  }
+  END_SU2_OMP_MASTER
 
   return IterLinSol;
-
 }
 
 /*--- Explicit instantiations ---*/
diff --git a/Common/src/linear_algebra/CSysSolve_b.cpp b/Common/src/linear_algebra/CSysSolve_b.cpp
index 238542a8f5e..000b389b8a5 100644
--- a/Common/src/linear_algebra/CSysSolve_b.cpp
+++ b/Common/src/linear_algebra/CSysSolve_b.cpp
@@ -31,11 +31,10 @@
 #include "../../include/linear_algebra/CSysVector.hpp"
 
 #ifdef CODI_REVERSE_TYPE
-template<class ScalarType>
+template <class ScalarType>
 void CSysSolve_b<ScalarType>::Solve_b(const su2double::Real* x, su2double::Real* x_b, size_t m,
                                       const su2double::Real* y, const su2double::Real* y_b, size_t n,
                                       codi::ExternalFunctionUserData* d) {
-
   CSysVector<su2double>* LinSysRes_b = nullptr;
   d->getDataByIndex(LinSysRes_b, 0);
 
@@ -57,7 +56,7 @@ void CSysSolve_b<ScalarType>::Solve_b(const su2double::Real* x, su2double::Real*
   /*--- Initialize the right-hand side with the gradient of the solution of the primal linear system ---*/
 
   SU2_OMP_BARRIER
-  SU2_OMP_FOR_STAT(roundUpDiv(n,omp_get_num_threads()))
+  SU2_OMP_FOR_STAT(roundUpDiv(n, omp_get_num_threads()))
   for (unsigned long i = 0; i < n; i++) {
     (*LinSysRes_b)[i] = y_b[i];
     (*LinSysSol_b)[i] = 0.0;
@@ -66,8 +65,8 @@ void CSysSolve_b<ScalarType>::Solve_b(const su2double::Real* x, su2double::Real*
 
   solver->Solve_b(*Jacobian, *LinSysRes_b, *LinSysSol_b, geometry, config, false);
 
-  SU2_OMP_FOR_STAT(roundUpDiv(n,omp_get_num_threads()))
-  for (unsigned long i = 0; i < n; i ++) {
+  SU2_OMP_FOR_STAT(roundUpDiv(n, omp_get_num_threads()))
+  for (unsigned long i = 0; i < n; i++) {
     x_b[i] = SU2_TYPE::GetValue((*LinSysSol_b)[i]);
   }
   END_SU2_OMP_FOR
diff --git a/Common/src/linear_algebra/CSysVector.cpp b/Common/src/linear_algebra/CSysVector.cpp
index af335ac99f5..9a43baf070a 100644
--- a/Common/src/linear_algebra/CSysVector.cpp
+++ b/Common/src/linear_algebra/CSysVector.cpp
@@ -50,7 +50,7 @@ void CSysVector<ScalarType>::Initialize(unsigned long numBlk, unsigned long numB
 
   omp_chunk_size = computeStaticChunkSize(nElm, omp_get_max_threads(), OMP_MAX_SIZE);
 
-  if (vec_val == nullptr) vec_val = MemoryAllocation::aligned_alloc<ScalarType,true>(64, nElm*sizeof(ScalarType));
+  if (vec_val == nullptr) vec_val = MemoryAllocation::aligned_alloc<ScalarType, true>(64, nElm * sizeof(ScalarType));
 
   if (val != nullptr) {
     if (!valIsArray) {
diff --git a/Common/src/linear_algebra/blas_structure.cpp b/Common/src/linear_algebra/blas_structure.cpp
index c23a77ecec7..5a1ec172b11 100644
--- a/Common/src/linear_algebra/blas_structure.cpp
+++ b/Common/src/linear_algebra/blas_structure.cpp
@@ -31,38 +31,38 @@
 #include <cstring>
 
 /* MKL or BLAS, if supported. */
-#if (defined (HAVE_MKL) || defined(HAVE_BLAS)) && !(defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE))
+#if (defined(HAVE_MKL) || defined(HAVE_BLAS)) && !(defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE))
 
 /* Function prototypes for the BLAS routines used. */
-extern "C" void dgemm_(char*, char*, const int*, const int*, const int*,
-                       const passivedouble*, const passivedouble*, const int*,
-                       const passivedouble*, const int*,
-                       const passivedouble*, passivedouble*, const int*);
-
-extern "C" void dgemv_(char*, const int*, const int*, const passivedouble*,
-                       const passivedouble*, const int*, const passivedouble*,
-                       const int*, const passivedouble*, passivedouble*, const int*);
+extern "C" void dgemm_(char*, char*, const int*, const int*, const int*, const passivedouble*, const passivedouble*,
+                       const int*, const passivedouble*, const int*, const passivedouble*, passivedouble*, const int*);
+
+extern "C" void dgemv_(char*, const int*, const int*, const passivedouble*, const passivedouble*, const int*,
+                       const passivedouble*, const int*, const passivedouble*, passivedouble*, const int*);
 #endif
 
 /* Constructor. Initialize the const member variables, if needed. */
 CBlasStructure::CBlasStructure(void)
-#if !(defined(HAVE_LIBXSMM) || defined(HAVE_BLAS) || defined(HAVE_MKL)) || (defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE))
-  : mc (256), kc (128), nc (128)
+#if !(defined(HAVE_LIBXSMM) || defined(HAVE_BLAS) || defined(HAVE_MKL)) || \
+    (defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE))
+    : mc(256),
+      kc(128),
+      nc(128)
 #endif
-{}
+{
+}
 
 /* Dense matrix multiplication, gemm functionality. */
-void CBlasStructure::gemm(const int M,        const int N,        const int K,
-                          const su2double *A, const su2double *B, su2double *C,
-                          const CConfig *config) {
-
+void CBlasStructure::gemm(const int M, const int N, const int K, const su2double* A, const su2double* B, su2double* C,
+                          const CConfig* config) {
   /* Initialize the variable for the timing, if profiling is active. */
 #ifdef PROFILE
   double timeGemm;
-  if( config ) config->GEMM_Tick(&timeGemm);
+  if (config) config->GEMM_Tick(&timeGemm);
 #endif
 
-#if (defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)) || !(defined(HAVE_LIBXSMM) || defined(HAVE_MKL) || defined(HAVE_BLAS))
+#if (defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)) || \
+    !(defined(HAVE_LIBXSMM) || defined(HAVE_MKL) || defined(HAVE_BLAS))
   /* Native implementation of the matrix product. This optimized implementation
      assumes that the matrices are in column major order. This can be
      accomplished by swapping N and M and A and B. This implementation is based
@@ -76,18 +76,18 @@ void CBlasStructure::gemm(const int M,        const int N,        const int K,
      Note that libxsmm_gemm expects the matrices in column major order. That's
      why the in the calling sequence A and B and M and N are reversed. */
   su2double alpha = 1.0;
-  su2double beta  = 0.0;
+  su2double beta = 0.0;
   char trans = 'N';
 
   libxsmm_dgemm(&trans, &trans, &N, &M, &K, &alpha, B, &N, A, &K, &beta, C, &N);
 
-#else // MKL and BLAS
+#else  // MKL and BLAS
 
   /* The standard blas routine dgemm is used for the multiplication.
      Call dgemm without transposing the matrices. In that case dgemm expects
      the matrices in column major order, see the comments for libxsmm. */
   su2double alpha = 1.0;
-  su2double beta  = 0.0;
+  su2double beta = 0.0;
   char trans = 'N';
 
   dgemm_(&trans, &trans, &N, &M, &K, &alpha, B, &N, A, &K, &beta, C, &N);
@@ -97,44 +97,42 @@ void CBlasStructure::gemm(const int M,        const int N,        const int K,
 
   /* Store the profiling information, if needed. */
 #ifdef PROFILE
-  if( config ) config->GEMM_Tock(timeGemm, M, N, K);
+  if (config) config->GEMM_Tock(timeGemm, M, N, K);
 #endif
 }
 
 /* Dense matrix vector multiplication, gemv functionality. */
-void CBlasStructure::gemv(const int M,        const int N,   const su2double *A,
-                          const su2double *x, su2double *y) {
-
-#if (defined (HAVE_BLAS) || defined(HAVE_MKL)) && !(defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE))
+void CBlasStructure::gemv(const int M, const int N, const su2double* A, const su2double* x, su2double* y) {
+#if (defined(HAVE_BLAS) || defined(HAVE_MKL)) && !(defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE))
 
   /* The standard blas routine dgemv is used for the multiplication.
      Note that dgemv expects the matrices in column major order, while
      A is in row major order. This can be solved by using the transpose
      and switching M and N. */
-     su2double alpha = 1.0;
-     su2double beta  = 0.0;
-     int       inc   = 1;
-     char trans = 'T';
+  su2double alpha = 1.0;
+  su2double beta = 0.0;
+  int inc = 1;
+  char trans = 'T';
 
-     dgemv_(&trans, &N, &M, &alpha, A, &N, x, &inc, &beta, y, &inc);
+  dgemv_(&trans, &N, &M, &alpha, A, &N, x, &inc, &beta, y, &inc);
 
 #else
 
   /* Native implementation of the matix vector product.
      Initialize the elements of y to zero. */
-  for(int i=0; i<M; ++i) y[i] = 0.0;
+  for (int i = 0; i < M; ++i) y[i] = 0.0;
 
   /* Carry out the matrix vector product. */
-  for(int k=0; k<M; ++k) {
-    const su2double *AA = A + k*N;
-    for(int l=0; l<N; ++l)
-      y[k] += AA[l]*x[l];
+  for (int k = 0; k < M; ++k) {
+    const su2double* AA = A + k * N;
+    for (int l = 0; l < N; ++l) y[k] += AA[l] * x[l];
   }
 
 #endif
 }
 
-#if !(defined(HAVE_LIBXSMM) || defined(HAVE_BLAS) || defined(HAVE_MKL)) || (defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE))
+#if !(defined(HAVE_LIBXSMM) || defined(HAVE_BLAS) || defined(HAVE_MKL)) || \
+    (defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE))
 
 /* Macros for accessing submatrices of a matmul using the leading dimension. */
 #define A(i, j) a[(j)*lda + (i)]
@@ -142,11 +140,10 @@ void CBlasStructure::gemv(const int M,        const int N,   const su2double *A,
 #define C(i, j) c[(j)*ldc + (i)]
 
 /* Function, which perform the implementation of the gemm functionality.  */
-void CBlasStructure::gemm_imp(const int m,        const int n,        const int k,
-                              const su2double *a, const su2double *b, su2double *c) {
-
+void CBlasStructure::gemm_imp(const int m, const int n, const int k, const su2double* a, const su2double* b,
+                              su2double* c) {
   /* Initialize the elements of c to zero. */
-  for(int i=0; i<(m*n); ++i) c[i] = 0.0;
+  for (int i = 0; i < (m * n); ++i) c[i] = 0.0;
 
   /* Set the leading dimensions of the three matrices. */
   const int lda = m;
@@ -155,12 +152,12 @@ void CBlasStructure::gemm_imp(const int m,        const int n,        const int
 
   /* The full matrix multiplication is split in several blocks.
      Loop over these blocks. */
-  for(int p=0; p<k; p+=kc) {
-    int pb = min(k-p, kc);
-    for(int j=0; j<n; j+=nc) {
-      int jb = min(n-j, nc);
-      for(int i=0; i<m; i+=mc) {
-        int ib = min(m-i, mc);
+  for (int p = 0; p < k; p += kc) {
+    int pb = min(k - p, kc);
+    for (int j = 0; j < n; j += nc) {
+      int jb = min(n - j, nc);
+      for (int i = 0; i < m; i += mc) {
+        int ib = min(m - i, mc);
 
         /* Carry out the multiplication for this block. */
         gemm_inner(ib, jb, pb, &A(i, p), lda, &B(p, j), ldb, &C(i, j), ldc);
@@ -171,18 +168,16 @@ void CBlasStructure::gemm_imp(const int m,        const int n,        const int
 
 /* Compute a portion of the c matrix one block at a time.
    Handle ragged edges with calls to a slow but general function. */
-void CBlasStructure::gemm_inner(int m, int n, int k, const su2double *a, int lda,
-                                const su2double *b, int ldb, su2double *c, int ldc) {
-
+void CBlasStructure::gemm_inner(int m, int n, int k, const su2double* a, int lda, const su2double* b, int ldb,
+                                su2double* c, int ldc) {
   /* Carry out the multiplication for this block. At the
      moment simply a call to gemm_arbitrary. */
   gemm_arbitrary(m, n, k, a, lda, b, ldb, c, ldc);
 }
 
 /* Naive gemm implementation to handle arbitrary sized matrices. */
-void CBlasStructure::gemm_arbitrary(int m, int n, int k, const su2double *a, int lda,
-                                    const su2double *b, int ldb, su2double *c, int ldc) {
-
+void CBlasStructure::gemm_arbitrary(int m, int n, int k, const su2double* a, int lda, const su2double* b, int ldb,
+                                    su2double* c, int ldc) {
   /* The order of these loops is tuned for column-major matrices. */
   for (int p = 0; p < k; p++) {
     for (int j = 0; j < n; j++) {
diff --git a/Common/src/meson.build b/Common/src/meson.build
index 3d84e6ea17a..f385c4a32ed 100644
--- a/Common/src/meson.build
+++ b/Common/src/meson.build
@@ -20,10 +20,10 @@ subdir('grid_movement')
 subdir('adt')
 
 if get_option('enable-normal')
-  common = static_library('SU2Common', 
+  common = static_library('SU2Common',
                           common_src,
-                          install : false, 
-                          dependencies : su2_deps, 
+                          install : false,
+                          dependencies : su2_deps,
                           cpp_args: [default_warning_flags, su2_cpp_args])
 
   common_dep = declare_dependency(link_with: common,
@@ -31,27 +31,27 @@ if get_option('enable-normal')
 endif
 
 if get_option('enable-autodiff')
-  
+
   commonAD = static_library('SU2CommonAD',
                             common_src,
-                            install : false, 
-                            dependencies : [su2_deps, codi_dep], 
+                            install : false,
+                            dependencies : [su2_deps, codi_dep],
                             cpp_args: [default_warning_flags, su2_cpp_args, codi_rev_args])
 
-  commonAD_dep = declare_dependency(link_with: commonAD, 
+  commonAD_dep = declare_dependency(link_with: commonAD,
                                     include_directories : common_include)
 
 endif
 
 if get_option('enable-directdiff')
-  
+
   commonDD = static_library('SU2CommonDD',
                             common_src,
-                            install : false, 
-                            dependencies : [su2_deps, codi_dep], 
+                            install : false,
+                            dependencies : [su2_deps, codi_dep],
                             cpp_args: [default_warning_flags, su2_cpp_args, codi_for_args])
 
-  commonDD_dep = declare_dependency(link_with: commonDD, 
+  commonDD_dep = declare_dependency(link_with: commonDD,
                                     include_directories : common_include)
 
 endif
diff --git a/Common/src/toolboxes/C1DInterpolation.cpp b/Common/src/toolboxes/C1DInterpolation.cpp
index 31861d67cab..abae1672389 100644
--- a/Common/src/toolboxes/C1DInterpolation.cpp
+++ b/Common/src/toolboxes/C1DInterpolation.cpp
@@ -35,45 +35,45 @@
 using namespace std;
 
 su2double CAkimaInterpolation::EvaluateSpline(su2double Point_Interp) const {
-
   const auto i = lower_bound(Point_Interp);
 
-  if (i >= x.size()-1) return (Point_Interp <= x[0])? y.front() : y.back();
+  if (i >= x.size() - 1) return (Point_Interp <= x[0]) ? y.front() : y.back();
 
-  const su2double h = Point_Interp-x[i];
+  const su2double h = Point_Interp - x[i];
 
-  return y[i]+h*(b[i]+h*(c[i]+h*d[i]));
+  return y[i] + h * (b[i] + h * (c[i] + h * d[i]));
 }
 
 su2double CLinearInterpolation::EvaluateSpline(su2double Point_Interp) const {
-
   const auto i = lower_bound(Point_Interp);
 
-  if (i >= x.size()-1) return (Point_Interp <= x[0])? y.front() : y.back();
+  if (i >= x.size() - 1) return (Point_Interp <= x[0]) ? y.front() : y.back();
 
-  return y[i] + (Point_Interp-x[i]) * (y[i+1]-y[i]) / (x[i+1]-x[i]);
+  return y[i] + (Point_Interp - x[i]) * (y[i + 1] - y[i]) / (x[i + 1] - x[i]);
 }
 
-void CCubicSpline::SetSpline(const vector<su2double> &X, const vector<su2double> &Data) {
-
-  C1DInterpolation::SetSpline(X,Data);
+void CCubicSpline::SetSpline(const vector<su2double>& X, const vector<su2double>& Data) {
+  C1DInterpolation::SetSpline(X, Data);
 
   const int N = x.size();
 
   /*--- Alias the vectors of coefficients to build the tridiagonal system. ---*/
 
-  auto& lower = b; b.resize(N);
-  auto& main = c; c.resize(N);
-  auto& upper = d; d.resize(N);
+  auto& lower = b;
+  b.resize(N);
+  auto& main = c;
+  c.resize(N);
+  auto& upper = d;
+  d.resize(N);
   vector<su2double> rhs(N);
 
   /*--- Main part of the tridiagonal system. ---*/
 
-  for (int i=1; i<N-1; i++) {
-    lower[i] = x[i]-x[i-1];
-    main[i] = (x[i+1]-x[i-1])*2;
-    upper[i] = x[i+1]-x[i];
-    rhs[i] = 6*((y[i+1]-y[i])/upper[i] - (y[i]-y[i-1])/lower[i]);
+  for (int i = 1; i < N - 1; i++) {
+    lower[i] = x[i] - x[i - 1];
+    main[i] = (x[i + 1] - x[i - 1]) * 2;
+    upper[i] = x[i + 1] - x[i];
+    rhs[i] = 6 * ((y[i + 1] - y[i]) / upper[i] - (y[i] - y[i - 1]) / lower[i]);
   }
 
   /*--- Start condition. ---*/
@@ -82,24 +82,22 @@ void CCubicSpline::SetSpline(const vector<su2double> &X, const vector<su2double>
     main[0] = 1.0;
     upper[0] = 0;
     rhs[0] = startVal;
-  }
-  else { // FIRST
-    main[0] = 2*lower[1];
+  } else {  // FIRST
+    main[0] = 2 * lower[1];
     upper[0] = lower[1];
-    rhs[0] = 6*((y[1]-y[0])/lower[1] - startVal);
+    rhs[0] = 6 * ((y[1] - y[0]) / lower[1] - startVal);
   }
 
   /*--- End condition. ---*/
 
   if (endDer == SECOND) {
-    main[N-1] = 1.0;
-    lower[N-1] = 0;
-    rhs[N-1] = endVal;
-  }
-  else { // FIRST
-    main[N-1] = 2*upper[N-2];
-    lower[N-1] = upper[N-2];
-    rhs[N-1] = 6*(endVal - (y[N-1]-y[N-2])/upper[N-2]);
+    main[N - 1] = 1.0;
+    lower[N - 1] = 0;
+    rhs[N - 1] = endVal;
+  } else {  // FIRST
+    main[N - 1] = 2 * upper[N - 2];
+    lower[N - 1] = upper[N - 2];
+    rhs[N - 1] = 6 * (endVal - (y[N - 1] - y[N - 2]) / upper[N - 2]);
   }
 
   /*--- Solve system for 2nd derivative at the knots. ---*/
@@ -109,26 +107,25 @@ void CCubicSpline::SetSpline(const vector<su2double> &X, const vector<su2double>
 
   /*--- Compute the polynomial coefficients. ---*/
 
-  for (int i=0; i<N-1; i++) {
-    su2double dx = x[i+1]-x[i];
-    c[i] = 0.5*d2y[i];
-    d[i] = (d2y[i+1]-d2y[i]) / (6*dx);
-    b[i] = (y[i+1]-y[i])/dx - (c[i]+d[i]*dx)*dx;
+  for (int i = 0; i < N - 1; i++) {
+    su2double dx = x[i + 1] - x[i];
+    c[i] = 0.5 * d2y[i];
+    d[i] = (d2y[i + 1] - d2y[i]) / (6 * dx);
+    b[i] = (y[i + 1] - y[i]) / dx - (c[i] + d[i] * dx) * dx;
   }
 }
 
-void CAkimaInterpolation::SetSpline(const vector<su2double> &X, const vector<su2double> &Data){
-
-  C1DInterpolation::SetSpline(X,Data);
+void CAkimaInterpolation::SetSpline(const vector<su2double>& X, const vector<su2double>& Data) {
+  C1DInterpolation::SetSpline(X, Data);
 
   const int n = X.size();
-  vector<su2double> h (n-1);
-  vector<su2double> p (n-1);
+  vector<su2double> h(n - 1);
+  vector<su2double> p(n - 1);
 
   /*---calculating finite differences (h) and gradients (p) ---*/
-  for (int i=0; i<n-1; i++){
-    h[i]=X[i+1]-X[i];
-    p[i]=(Data[i+1]-Data[i])/h[i];
+  for (int i = 0; i < n - 1; i++) {
+    h[i] = X[i + 1] - X[i];
+    p[i] = (Data[i + 1] - Data[i]) / h[i];
   }
 
   /*--- b,c,d are the akima spline's cofficient for the cubic equation ---*/
@@ -137,67 +134,59 @@ void CAkimaInterpolation::SetSpline(const vector<su2double> &X, const vector<su2
   d.resize(n);
 
   b[0] = p[0];
-  b[1] = (p[0] + p[1])/2;
-  b[n-1] = p[n-2];
-  b[n-2] = (p[n-2]+p[n-3])/2;
-
-  for (int i = 2; i < n-2; i++){
-    su2double w1=fabs(p[i+1]-p[i]) , w2=fabs(p[i-1]-p[i-2]);
-    if (w1+w2<0.0001) {
-      b[i] = (p[i-1]+p[i])/2 ;
-    }
-    else{
-      b[i] = (w1*p[i-1]+w2*p[i])/(w1+w2);
+  b[1] = (p[0] + p[1]) / 2;
+  b[n - 1] = p[n - 2];
+  b[n - 2] = (p[n - 2] + p[n - 3]) / 2;
+
+  for (int i = 2; i < n - 2; i++) {
+    su2double w1 = fabs(p[i + 1] - p[i]), w2 = fabs(p[i - 1] - p[i - 2]);
+    if (w1 + w2 < 0.0001) {
+      b[i] = (p[i - 1] + p[i]) / 2;
+    } else {
+      b[i] = (w1 * p[i - 1] + w2 * p[i]) / (w1 + w2);
     }
   }
 
-  for (int i = 0; i < n-1; i++){
-    c[i] = (3*p[i]-2*b[i]-b[i+1])/h[i] ;
-    d[i] = (b[i+1]+b[i]-2*p[i])/h[i]/h[i];
+  for (int i = 0; i < n - 1; i++) {
+    c[i] = (3 * p[i] - 2 * b[i] - b[i + 1]) / h[i];
+    d[i] = (b[i + 1] + b[i] - 2 * p[i]) / h[i] / h[i];
   }
   b.back() = c.back() = 0;
-
 }
 
-vector<su2double> CorrectedInletValues(const vector<su2double> &Inlet_Interpolated ,
-                                       su2double Theta ,
-                                       unsigned short nDim,
-                                       const su2double *Coord,
-                                       unsigned short nVar_Turb,
-                                       INLET_INTERP_TYPE Interpolation_Type){
-
-  unsigned short size_columns=Inlet_Interpolated.size()+nDim;
+vector<su2double> CorrectedInletValues(const vector<su2double>& Inlet_Interpolated, su2double Theta,
+                                       unsigned short nDim, const su2double* Coord, unsigned short nVar_Turb,
+                                       INLET_INTERP_TYPE Interpolation_Type) {
+  unsigned short size_columns = Inlet_Interpolated.size() + nDim;
   vector<su2double> Inlet_Values(size_columns);
   su2double unit_r, unit_Theta, unit_m, Alpha, Phi;
 
   /*---For x,y,z,T,P columns---*/
-  for (int i=0;i<nDim;i++)
-    Inlet_Values[i] = Coord[i];
+  for (int i = 0; i < nDim; i++) Inlet_Values[i] = Coord[i];
 
-  for (int i=nDim;i<nDim+2;i++)
-    Inlet_Values[i] = Inlet_Interpolated[i-2];
+  for (int i = nDim; i < nDim + 2; i++) Inlet_Values[i] = Inlet_Interpolated[i - 2];
 
   /*---For turbulence variables columns---*/
   if (nVar_Turb == 1)
-    Inlet_Values[nDim+5] = Inlet_Interpolated[5];
-  else if (nVar_Turb == 2){
-    Inlet_Values[nDim+5] = Inlet_Interpolated[5];
-    Inlet_Values[nDim+6] = Inlet_Interpolated[6];
+    Inlet_Values[nDim + 5] = Inlet_Interpolated[5];
+  else if (nVar_Turb == 2) {
+    Inlet_Values[nDim + 5] = Inlet_Interpolated[5];
+    Inlet_Values[nDim + 6] = Inlet_Interpolated[6];
   }
 
   /*--- Correct for Interpolation Type now ---*/
-  switch(Interpolation_Type){
-    case(INLET_INTERP_TYPE::VR_VTHETA):
+  switch (Interpolation_Type) {
+    case (INLET_INTERP_TYPE::VR_VTHETA):
       unit_r = Inlet_Interpolated[nDim];
-      unit_Theta = Inlet_Interpolated[nDim+1];
+      unit_Theta = Inlet_Interpolated[nDim + 1];
       break;
 
-    case(INLET_INTERP_TYPE::ALPHA_PHI):
-      Alpha = Inlet_Interpolated[nDim]*PI_NUMBER/180;
-      Phi = Inlet_Interpolated[nDim+1]*PI_NUMBER/180;
-      unit_m = sqrt(1/(1+pow(tan(Alpha),2)));
-      unit_Theta = tan(Alpha)*unit_m;
-      unit_r=unit_m*sin(Phi);
+    case (INLET_INTERP_TYPE::ALPHA_PHI):
+      Alpha = Inlet_Interpolated[nDim] * PI_NUMBER / 180;
+      Phi = Inlet_Interpolated[nDim + 1] * PI_NUMBER / 180;
+      unit_m = sqrt(1 / (1 + pow(tan(Alpha), 2)));
+      unit_Theta = tan(Alpha) * unit_m;
+      unit_r = unit_m * sin(Phi);
       break;
 
     default:
@@ -206,29 +195,27 @@ vector<su2double> CorrectedInletValues(const vector<su2double> &Inlet_Interpolat
   }
 
   /*--- Converting from cylindrical to cartesian unit vectors ---*/
-  Inlet_Values[nDim+2] = unit_r*cos(Theta) - unit_Theta*sin(Theta);
-  Inlet_Values[nDim+3] = unit_r*sin(Theta) + unit_Theta*cos(Theta);
-  Inlet_Values[nDim+4] = sqrt(1-pow(unit_r,2)- pow(unit_Theta,2));
+  Inlet_Values[nDim + 2] = unit_r * cos(Theta) - unit_Theta * sin(Theta);
+  Inlet_Values[nDim + 3] = unit_r * sin(Theta) + unit_Theta * cos(Theta);
+  Inlet_Values[nDim + 4] = sqrt(1 - pow(unit_r, 2) - pow(unit_Theta, 2));
 
   return Inlet_Values;
 }
 
-void PrintInletInterpolatedData(const vector<su2double>& Inlet_Data_Interpolated, string Marker,
-                                unsigned long nVertex, unsigned short nDim, unsigned short nColumns){
-
+void PrintInletInterpolatedData(const vector<su2double>& Inlet_Data_Interpolated, string Marker, unsigned long nVertex,
+                                unsigned short nDim, unsigned short nColumns) {
   ofstream myfile;
   myfile.precision(16);
-  myfile.open("Interpolated_Data_"+Marker+".dat",ios_base::out);
+  myfile.open("Interpolated_Data_" + Marker + ".dat", ios_base::out);
 
-  if (myfile.is_open()){
+  if (myfile.is_open()) {
     for (unsigned long iVertex = 0; iVertex < nVertex; iVertex++) {
-      for (unsigned short iVar=0; iVar < nColumns; iVar++){
-        myfile<<Inlet_Data_Interpolated[iVertex*nColumns+iVar]<<"\t";
+      for (unsigned short iVar = 0; iVar < nColumns; iVar++) {
+        myfile << Inlet_Data_Interpolated[iVertex * nColumns + iVar] << "\t";
       }
-      myfile<<endl;
+      myfile << endl;
     }
     myfile.close();
-  }
-  else
-    cout<<"file cannot be opened"<<endl;
+  } else
+    cout << "file cannot be opened" << endl;
 }
diff --git a/Common/src/toolboxes/CLinearPartitioner.cpp b/Common/src/toolboxes/CLinearPartitioner.cpp
index 6960344d8a0..b148411738c 100644
--- a/Common/src/toolboxes/CLinearPartitioner.cpp
+++ b/Common/src/toolboxes/CLinearPartitioner.cpp
@@ -28,10 +28,7 @@
 
 #include "../../include/toolboxes/CLinearPartitioner.hpp"
 
-void CLinearPartitioner::Initialize(unsigned long global_count,
-                                    unsigned long offset,
-                                    bool isDisjoint) {
-
+void CLinearPartitioner::Initialize(unsigned long global_count, unsigned long offset, bool isDisjoint) {
   /*--- Store MPI size ---*/
 
   size = SU2_MPI::GetSize();
@@ -41,17 +38,16 @@ void CLinearPartitioner::Initialize(unsigned long global_count,
   firstIndex.resize(size);
   lastIndex.resize(size);
   sizeOnRank.resize(size);
-  cumulativeSizeBeforeRank.resize(size+1);
+  cumulativeSizeBeforeRank.resize(size + 1);
 
   /*--- Compute the number of points that will be on each processor.
    This is a linear partitioning with the addition of a simple load
    balancing for any remainder points. ---*/
 
   unsigned long quotient = 0;
-  if (global_count >= (unsigned long)size)
-    quotient = global_count/size;
+  if (global_count >= (unsigned long)size) quotient = global_count / size;
 
-  int remainder = int(global_count%size);
+  int remainder = int(global_count % size);
   for (int ii = 0; ii < size; ii++) {
     sizeOnRank[ii] = quotient + int(ii < remainder);
   }
@@ -64,32 +60,27 @@ void CLinearPartitioner::Initialize(unsigned long global_count,
   if (isDisjoint) adjust = 1;
 
   firstIndex[0] = offset;
-  lastIndex[0]  = firstIndex[0] + sizeOnRank[0] - adjust;
+  lastIndex[0] = firstIndex[0] + sizeOnRank[0] - adjust;
   cumulativeSizeBeforeRank[0] = 0;
   for (int iProc = 1; iProc < size; iProc++) {
-    firstIndex[iProc] = lastIndex[iProc-1] + adjust;
-    lastIndex[iProc]  = firstIndex[iProc]  + sizeOnRank[iProc] - adjust;
-    cumulativeSizeBeforeRank[iProc] = (cumulativeSizeBeforeRank[iProc-1] +
-                                       sizeOnRank[iProc-1]);
+    firstIndex[iProc] = lastIndex[iProc - 1] + adjust;
+    lastIndex[iProc] = firstIndex[iProc] + sizeOnRank[iProc] - adjust;
+    cumulativeSizeBeforeRank[iProc] = (cumulativeSizeBeforeRank[iProc - 1] + sizeOnRank[iProc - 1]);
   }
   cumulativeSizeBeforeRank[size] = global_count;
-
 }
 
 unsigned long CLinearPartitioner::GetRankContainingIndex(unsigned long index) const {
-
   /*--- Initial guess ---*/
 
-  unsigned long iProcessor = min<unsigned long>(index/sizeOnRank[0], size-1);
+  unsigned long iProcessor = min<unsigned long>(index / sizeOnRank[0], size - 1);
 
   /*--- Move up or down until we find the processor. ---*/
 
   if (index >= cumulativeSizeBeforeRank[iProcessor])
-    while(index >= cumulativeSizeBeforeRank[iProcessor+1])
-      iProcessor++;
+    while (index >= cumulativeSizeBeforeRank[iProcessor + 1]) iProcessor++;
   else
-    while(index < cumulativeSizeBeforeRank[iProcessor])
-      iProcessor--;
+    while (index < cumulativeSizeBeforeRank[iProcessor]) iProcessor--;
 
   return iProcessor;
 }
diff --git a/Common/src/toolboxes/CSquareMatrixCM.cpp b/Common/src/toolboxes/CSquareMatrixCM.cpp
index 09b990dc448..b4a33c8b2db 100644
--- a/Common/src/toolboxes/CSquareMatrixCM.cpp
+++ b/Common/src/toolboxes/CSquareMatrixCM.cpp
@@ -38,26 +38,19 @@ using namespace std;
 #endif
 #elif defined(HAVE_LAPACK)
 /*--- Lapack / Blas routines used in CSquareMatrixCM. ---*/
-extern "C" void dgetrf_(const int*, const int*, passivedouble*, const int*,
-                        int*, int*);
-extern "C" void dgetri_(const int*, passivedouble*, const int*, int*,
-                        passivedouble*, const int*, int*);
-extern "C" void dgemm_(char*, char*, const int*, const int*, const int*,
-                       const passivedouble*, const passivedouble*,
-                       const int *, const passivedouble*, const int*,
-                       const passivedouble*, passivedouble*, const int*);
+extern "C" void dgetrf_(const int*, const int*, passivedouble*, const int*, int*, int*);
+extern "C" void dgetri_(const int*, passivedouble*, const int*, int*, passivedouble*, const int*, int*);
+extern "C" void dgemm_(char*, char*, const int*, const int*, const int*, const passivedouble*, const passivedouble*,
+                       const int*, const passivedouble*, const int*, const passivedouble*, passivedouble*, const int*);
 #define DGEMM dgemm_
 #endif
 
 void CSquareMatrixCM::Transpose() {
-
-  for(int j=1; j<Size(); ++j)
-    for(int i=0; i<j; ++i)
-      swap(mat(i,j), mat(j,i));
+  for (int j = 1; j < Size(); ++j)
+    for (int i = 0; i < j; ++i) swap(mat(i, j), mat(j, i));
 }
 
 void CSquareMatrixCM::Invert() {
-
 #ifdef HAVE_LAPACK
 
   /*--- Computation of the inverse using the Lapack routines. ---*/
@@ -67,29 +60,26 @@ void CSquareMatrixCM::Invert() {
   vector<passivedouble> work(sz);
 
   dgetrf_(&sz, &sz, mat.data(), &sz, ipiv.data(), &info);
-  if(info != 0) SU2_MPI::Error(string("Matrix is singular"), CURRENT_FUNCTION);
+  if (info != 0) SU2_MPI::Error(string("Matrix is singular"), CURRENT_FUNCTION);
 
   dgetri_(&sz, mat.data(), &sz, ipiv.data(), work.data(), &sz, &info);
-  if(info != 0) SU2_MPI::Error(string("Matrix inversion failed"), CURRENT_FUNCTION);
+  if (info != 0) SU2_MPI::Error(string("Matrix inversion failed"), CURRENT_FUNCTION);
 
 #else
   CBlasStructure::inverse(Size(), mat);
 #endif
 }
 
-void CSquareMatrixCM::MatMatMult(const char                          side,
-                                        const ColMajorMatrix<passivedouble> &mat_in,
-                                        ColMajorMatrix<passivedouble>       &mat_out) const {
-
+void CSquareMatrixCM::MatMatMult(const char side, const ColMajorMatrix<passivedouble>& mat_in,
+                                 ColMajorMatrix<passivedouble>& mat_out) const {
   /*--- Check the type of multiplication to be carried out. ---*/
   if (side == 'L' || side == 'l') {
-
     /*--- Left side: mat_out = this * mat_in. Set some sizes
           and allocate the memory for mat_out. ---*/
     const int M = Size(), N = mat_in.cols();
     assert(M == static_cast<int>(mat_in.rows()));
 
-    mat_out.resize(M,N);
+    mat_out.resize(M, N);
 
 #ifdef HAVE_LAPACK
 
@@ -98,28 +88,24 @@ void CSquareMatrixCM::MatMatMult(const char                          side,
     passivedouble alpha = 1.0, beta = 0.0;
     char trans = 'N';
 
-    DGEMM(&trans, &trans, &M, &N, &M, &alpha, mat.data(), &M,
-          mat_in.data(), &M, &beta, mat_out.data(), &M);
+    DGEMM(&trans, &trans, &M, &N, &M, &alpha, mat.data(), &M, mat_in.data(), &M, &beta, mat_out.data(), &M);
 #else
     /*--- Naive product. ---*/
     for (int i = 0; i < M; ++i) {
       for (int j = 0; j < N; ++j) {
-        mat_out(i,j) = 0.0;
-        for (int k = 0; k < M; ++k)
-          mat_out(i,j) += mat(i,k) * mat_in(k,j);
+        mat_out(i, j) = 0.0;
+        for (int k = 0; k < M; ++k) mat_out(i, j) += mat(i, k) * mat_in(k, j);
       }
     }
 #endif
 
-  }
-  else {
-
+  } else {
     /*--- Right_side: mat_out = mat_in * this. Set some sizes
           and allocate the memory for mat_out. ---*/
     const int M = mat_in.rows(), N = Size();
     assert(N == static_cast<int>(mat_in.cols()));
 
-    mat_out.resize(M,N);
+    mat_out.resize(M, N);
 
 #ifdef HAVE_LAPACK
 
@@ -128,15 +114,13 @@ void CSquareMatrixCM::MatMatMult(const char                          side,
     passivedouble alpha = 1.0, beta = 0.0;
     char trans = 'N';
 
-    DGEMM(&trans, &trans, &M, &N, &N, &alpha, mat_in.data(), &M,
-          mat.data(), &N, &beta, mat_out.data(), &M);
+    DGEMM(&trans, &trans, &M, &N, &N, &alpha, mat_in.data(), &M, mat.data(), &N, &beta, mat_out.data(), &M);
 #else
     /*--- Naive product. ---*/
     for (int i = 0; i < M; ++i) {
       for (int j = 0; j < N; ++j) {
-        mat_out(i,j) = 0.0;
-        for (int k = 0; k < N; ++k)
-          mat_out(i,j) += mat_in(i,k) * mat(k,j);
+        mat_out(i, j) = 0.0;
+        for (int k = 0; k < N; ++k) mat_out(i, j) += mat_in(i, k) * mat(k, j);
       }
     }
 #endif
diff --git a/Common/src/toolboxes/CSymmetricMatrix.cpp b/Common/src/toolboxes/CSymmetricMatrix.cpp
index a2adb505562..e5f6daa723f 100644
--- a/Common/src/toolboxes/CSymmetricMatrix.cpp
+++ b/Common/src/toolboxes/CSymmetricMatrix.cpp
@@ -47,38 +47,35 @@ extern "C" void dsymm_(const char*, const char*, const int*, const int*, const p
 #define DSYMM dsymm_
 #endif
 
-void CSymmetricMatrix::Initialize(int N) { mat.resize(N,N); }
+void CSymmetricMatrix::Initialize(int N) { mat.resize(N, N); }
 
-void CSymmetricMatrix::CholeskyDecompose()
-{
+void CSymmetricMatrix::CholeskyDecompose() {
 #ifndef HAVE_LAPACK
   int j;
   for (j = 0; j < Size(); ++j) {
     passivedouble sum = 0.0;
-    for (int k = 0; k < j; ++k) sum -= pow(Get(j,k), 2);
-    sum += Get(j,j);
-    if (sum < 0.0) break; // not SPD
+    for (int k = 0; k < j; ++k) sum -= pow(Get(j, k), 2);
+    sum += Get(j, j);
+    if (sum < 0.0) break;  // not SPD
     Set(j, j, sqrt(sum));
 
-    for (int i = j+1; i < Size(); ++i) {
+    for (int i = j + 1; i < Size(); ++i) {
       passivedouble sum = 0.0;
-      for (int k = 0; k < j; ++k) sum -= Get(i,k) * Get(j,k);
-      sum += Get(i,j);
-      Set(i, j, sum / Get(j,j));
+      for (int k = 0; k < j; ++k) sum -= Get(i, k) * Get(j, k);
+      sum += Get(i, j);
+      Set(i, j, sum / Get(j, j));
     }
   }
-  if (j!=Size()) SU2_MPI::Error("LLT factorization failed.", CURRENT_FUNCTION);
+  if (j != Size()) SU2_MPI::Error("LLT factorization failed.", CURRENT_FUNCTION);
 #endif
 }
 
-void CSymmetricMatrix::CalcInv(bool is_spd)
-{
+void CSymmetricMatrix::CalcInv(bool is_spd) {
 #ifndef HAVE_LAPACK
   const int sz = Size();
 
   /*--- Compute inverse from decomposed matrices. ---*/
-  if (is_spd)
-  {
+  if (is_spd) {
     CholeskyDecompose();
 
     /*--- Initialize inverse matrix. ---*/
@@ -88,24 +85,23 @@ void CSymmetricMatrix::CalcInv(bool is_spd)
     /*--- Solve smaller and smaller systems. ---*/
     for (int j = 0; j < sz; ++j) {
       /*--- Forward substitution. ---*/
-      inv(j,j) = 1.0 / Get(j,j);
+      inv(j, j) = 1.0 / Get(j, j);
 
-      for (int i = j+1; i < sz; ++i) {
+      for (int i = j + 1; i < sz; ++i) {
         passivedouble sum = 0.0;
-        for (int k = j; k < i; ++k) sum -= Get(i,k) * inv(k,j);
-        inv(i,j) = sum / Get(i,i);
+        for (int k = j; k < i; ++k) sum -= Get(i, k) * inv(k, j);
+        inv(i, j) = sum / Get(i, i);
       }
-    } // L inverse in inv
+    }  // L inverse in inv
 
     /*--- Multiply inversed matrices overwrite mat. ---*/
     for (int j = 0; j < sz; ++j)
       for (int i = j; i < sz; ++i) {
         passivedouble sum = 0.0;
-        for (int k = i; k < sz; ++k) sum += inv(k,i) * inv(k,j);
+        for (int k = i; k < sz; ++k) sum += inv(k, i) * inv(k, j);
         Set(i, j, sum);
       }
-  }
-  else {
+  } else {
     auto inv = StealData();
     CBlasStructure::inverse(sz, inv);
     mat = move(inv);
@@ -113,8 +109,7 @@ void CSymmetricMatrix::CalcInv(bool is_spd)
 #endif
 }
 
-void CSymmetricMatrix::CalcInv_sytri()
-{
+void CSymmetricMatrix::CalcInv_sytri() {
 #ifdef HAVE_LAPACK
   const char uplo = 'L';
   const int sz = Size();
@@ -122,66 +117,62 @@ void CSymmetricMatrix::CalcInv_sytri()
   vector<int> ipiv(sz);
 
   /*--- Query the optimum work size. ---*/
-  int query = -1; passivedouble tmp;
+  int query = -1;
+  passivedouble tmp;
   dsytrf_(&uplo, &sz, mat.data(), &sz, ipiv.data(), &tmp, &query, &info);
   query = static_cast<int>(tmp);
   vector<passivedouble> work(query);
 
   /*--- Factorize and invert. ---*/
   dsytrf_(&uplo, &sz, mat.data(), &sz, ipiv.data(), work.data(), &query, &info);
-  if (info!=0) SU2_MPI::Error("LDLT factorization failed.", CURRENT_FUNCTION);
+  if (info != 0) SU2_MPI::Error("LDLT factorization failed.", CURRENT_FUNCTION);
   dsytri_(&uplo, &sz, mat.data(), &sz, ipiv.data(), work.data(), &info);
-  if (info!=0) SU2_MPI::Error("Inversion with LDLT factorization failed.", CURRENT_FUNCTION);
+  if (info != 0) SU2_MPI::Error("Inversion with LDLT factorization failed.", CURRENT_FUNCTION);
 #endif
 }
 
-void CSymmetricMatrix::CalcInv_potri()
-{
+void CSymmetricMatrix::CalcInv_potri() {
 #ifdef HAVE_LAPACK
   const char uplo = 'L';
   const int sz = Size();
   int info;
 
   dpotrf_(&uplo, &sz, mat.data(), &sz, &info);
-  if (info!=0) SU2_MPI::Error("LLT factorization failed.", CURRENT_FUNCTION);
+  if (info != 0) SU2_MPI::Error("LLT factorization failed.", CURRENT_FUNCTION);
   dpotri_(&uplo, &sz, mat.data(), &sz, &info);
-  if (info!=0) SU2_MPI::Error("Inversion with LLT factorization failed.", CURRENT_FUNCTION);
+  if (info != 0) SU2_MPI::Error("Inversion with LLT factorization failed.", CURRENT_FUNCTION);
 #endif
 }
 
-void CSymmetricMatrix::Invert(const bool is_spd)
-{
+void CSymmetricMatrix::Invert(const bool is_spd) {
 #ifdef HAVE_LAPACK
-  if(is_spd) CalcInv_potri();
-  else CalcInv_sytri();
+  if (is_spd)
+    CalcInv_potri();
+  else
+    CalcInv_sytri();
 #else
   CalcInv(is_spd);
 #endif
 }
 
-void CSymmetricMatrix::MatMatMult(const char side,
-                                  const su2passivematrix& mat_in,
-                                  su2passivematrix& mat_out) const
-{
+void CSymmetricMatrix::MatMatMult(const char side, const su2passivematrix& mat_in, su2passivematrix& mat_out) const {
   /*--- Left side: mat_out = this * mat_in. ---*/
   if (side == 'L' || side == 'l') {
     const int M = Size(), N = mat_in.cols();
     assert(M == static_cast<int>(mat_in.rows()));
 
-    mat_out.resize(M,N);
+    mat_out.resize(M, N);
 
 #ifdef HAVE_LAPACK
     /*--- Right and lower because matrices are in row major order. ---*/
     const char side = 'R', uplo = 'L';
     const passivedouble alpha = 1.0, beta = 0.0;
-    DSYMM(&side, &uplo, &N, &M, &alpha, mat.data(), &M,
-          mat_in.data(), &N, &beta, mat_out.data(), &N);
-#else // Naive product
+    DSYMM(&side, &uplo, &N, &M, &alpha, mat.data(), &M, mat_in.data(), &N, &beta, mat_out.data(), &N);
+#else  // Naive product
     for (int i = 0; i < M; ++i)
       for (int j = 0; j < N; ++j) {
-        mat_out(i,j) = 0.0;
-        for (int k = 0; k < M; ++k)
-          mat_out(i,j) += Get(i,k) * mat_in(k,j);
+        mat_out(i, j) = 0.0;
+        for (int k = 0; k < M; ++k) mat_out(i, j) += Get(i, k) * mat_in(k, j);
       }
 #endif
   }
@@ -190,31 +181,27 @@ void CSymmetricMatrix::MatMatMult(const char side,
     const int M = mat_in.rows(), N = Size();
     assert(N == static_cast<int>(mat_in.cols()));
 
-    mat_out.resize(M,N);
+    mat_out.resize(M, N);
 
 #ifdef HAVE_LAPACK
     /*--- Left and lower because matrices are in row major order. ---*/
     const char side = 'L', uplo = 'L';
     const passivedouble alpha = 1.0, beta = 0.0;
-    DSYMM(&side, &uplo, &N, &M, &alpha, mat.data(), &N,
-          mat_in.data(), &N, &beta, mat_out.data(), &N);
-#else // Naive product
+    DSYMM(&side, &uplo, &N, &M, &alpha, mat.data(), &N, mat_in.data(), &N, &beta, mat_out.data(), &N);
+#else  // Naive product
     for (int i = 0; i < M; ++i)
       for (int j = 0; j < N; ++j) {
-        mat_out(i,j) = 0.0;
-        for (int k = 0; k < N; ++k)
-          mat_out(i,j) += mat_in(i,k) * Get(k,j);
+        mat_out(i, j) = 0.0;
+        for (int k = 0; k < N; ++k) mat_out(i, j) += mat_in(i, k) * Get(k, j);
       }
 #endif
   }
 }
 
-su2passivematrix CSymmetricMatrix::StealData()
-{
+su2passivematrix CSymmetricMatrix::StealData() {
   /*--- Fill lower triangular part. ---*/
   for (int i = 1; i < Size(); ++i)
-    for (int j = 0; j < i; ++j)
-      mat(i,j) = mat(j,i);
+    for (int j = 0; j < i; ++j) mat(i, j) = mat(j, i);
 
   return move(mat);
 }
diff --git a/Common/src/toolboxes/MMS/CIncTGVSolution.cpp b/Common/src/toolboxes/MMS/CIncTGVSolution.cpp
index 51b0499dae0..9baa1999c18 100644
--- a/Common/src/toolboxes/MMS/CIncTGVSolution.cpp
+++ b/Common/src/toolboxes/MMS/CIncTGVSolution.cpp
@@ -27,18 +27,14 @@
 
 #include "../../../include/toolboxes/MMS/CIncTGVSolution.hpp"
 
-CIncTGVSolution::CIncTGVSolution(void) : CVerificationSolution() { }
-
-CIncTGVSolution::CIncTGVSolution(unsigned short val_nDim,
-                                 unsigned short val_nVar,
-                                 unsigned short val_iMesh,
-                                 CConfig*       config)
-: CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
+CIncTGVSolution::CIncTGVSolution(void) : CVerificationSolution() {}
 
+CIncTGVSolution::CIncTGVSolution(unsigned short val_nDim, unsigned short val_nVar, unsigned short val_iMesh,
+                                 CConfig* config)
+    : CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
   /*--- Disable this solution for now, as it has not been tested. ---*/
 
-  SU2_MPI::Error("CIncTGVSolution not yet fully implemented/tested.",
-                 CURRENT_FUNCTION);
+  SU2_MPI::Error("CIncTGVSolution not yet fully implemented/tested.", CURRENT_FUNCTION);
 
   /*--- Write a message that the solution is initialized for the
    Taylor-Green vortex test case. ---*/
@@ -52,9 +48,9 @@ CIncTGVSolution::CIncTGVSolution(unsigned short val_nDim,
 
   /*--- Store TGV specific parameters here. ---*/
 
-  tgvLength    = 1.0;
-  tgvVelocity  = 1.0;
-  tgvDensity   = config->GetDensity_FreeStreamND();
+  tgvLength = 1.0;
+  tgvVelocity = 1.0;
+  tgvDensity = config->GetDensity_FreeStreamND();
   tgvViscosity = config->GetViscosity_FreeStreamND();
 
   /*--- We keep a copy of the freestream temperature just to be safe
@@ -64,73 +60,61 @@ CIncTGVSolution::CIncTGVSolution(unsigned short val_nDim,
 
   /*--- Perform some sanity and error checks for this solution here. ---*/
 
-  if((config->GetTime_Marching() != TIME_MARCHING::TIME_STEPPING) &&
-     (config->GetTime_Marching() != TIME_MARCHING::DT_STEPPING_1ST) &&
-     (config->GetTime_Marching() != TIME_MARCHING::DT_STEPPING_2ND))
-    SU2_MPI::Error("Unsteady mode must be selected for the incompressible Taylor Green Vortex",
-                   CURRENT_FUNCTION);
+  if ((config->GetTime_Marching() != TIME_MARCHING::TIME_STEPPING) &&
+      (config->GetTime_Marching() != TIME_MARCHING::DT_STEPPING_1ST) &&
+      (config->GetTime_Marching() != TIME_MARCHING::DT_STEPPING_2ND))
+    SU2_MPI::Error("Unsteady mode must be selected for the incompressible Taylor Green Vortex", CURRENT_FUNCTION);
 
-  if(Kind_Solver != MAIN_SOLVER::INC_EULER && Kind_Solver != MAIN_SOLVER::INC_NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::INC_RANS )
+  if (Kind_Solver != MAIN_SOLVER::INC_EULER && Kind_Solver != MAIN_SOLVER::INC_NAVIER_STOKES &&
+      Kind_Solver != MAIN_SOLVER::INC_RANS)
     SU2_MPI::Error("Incompressible flow equations must be selected for the incompressible Taylor Green Vortex",
                    CURRENT_FUNCTION);
 
-  if(Kind_Solver != MAIN_SOLVER::INC_NAVIER_STOKES)
+  if (Kind_Solver != MAIN_SOLVER::INC_NAVIER_STOKES)
     SU2_MPI::Error("Navier Stokes equations must be selected for the incompressible Taylor Green Vortex",
                    CURRENT_FUNCTION);
 
-  if(config->GetKind_FluidModel() != CONSTANT_DENSITY)
+  if (config->GetKind_FluidModel() != CONSTANT_DENSITY)
     SU2_MPI::Error("Constant density fluid model must be selected for the incompressible Taylor Green Vortex",
                    CURRENT_FUNCTION);
 
-  if(config->GetKind_ViscosityModel() != VISCOSITYMODEL::CONSTANT)
-    SU2_MPI::Error("Constant viscosity must be selected for the incompressible Taylor Green Vortex",
-                   CURRENT_FUNCTION);
+  if (config->GetKind_ViscosityModel() != VISCOSITYMODEL::CONSTANT)
+    SU2_MPI::Error("Constant viscosity must be selected for the incompressible Taylor Green Vortex", CURRENT_FUNCTION);
 
-  if(config->GetEnergy_Equation())
+  if (config->GetEnergy_Equation())
     SU2_MPI::Error("Energy equation must be disabled (isothermal) for the incompressible Taylor Green Vortex",
                    CURRENT_FUNCTION);
 
-  if(nDim != 2)
-    SU2_MPI::Error("2D calculation required for the incompressible Taylor Green Vortex",
-                   CURRENT_FUNCTION);
+  if (nDim != 2) SU2_MPI::Error("2D calculation required for the incompressible Taylor Green Vortex", CURRENT_FUNCTION);
 }
 
-CIncTGVSolution::~CIncTGVSolution(void) { }
-
-void CIncTGVSolution::GetBCState(const su2double *val_coords,
-                                 const su2double val_t,
-                                 su2double       *val_solution) const {
+CIncTGVSolution::~CIncTGVSolution(void) {}
 
+void CIncTGVSolution::GetBCState(const su2double* val_coords, const su2double val_t, su2double* val_solution) const {
   /*--- The exact solution is prescribed on the boundaries. ---*/
   GetSolution(val_coords, val_t, val_solution);
 }
 
-void CIncTGVSolution::GetSolution(const su2double *val_coords,
-                                  const su2double val_t,
-                                  su2double       *val_solution) const {
-
+void CIncTGVSolution::GetSolution(const su2double* val_coords, const su2double val_t, su2double* val_solution) const {
   /* The exact solution is set for the incompressible Taylor-Green
    vortex case. This is the classic solution from the original work
    of Taylor and Green for the specific 2D situation where the
    exact solution can be derived for an incompressible flow. */
 
   /* Store the termporal term more easily (Taylor expansion). */
-  su2double F = 1.0 - 2.0*(tgvViscosity/tgvDensity)*val_t;
+  su2double F = 1.0 - 2.0 * (tgvViscosity / tgvDensity) * val_t;
 
   /* Compute the primitive variables. */
-  su2double u =  tgvVelocity * F * (sin(val_coords[0]/tgvLength)*
-                                    cos(val_coords[1]/tgvLength));
-  su2double v = -tgvVelocity * F * (cos(val_coords[0]/tgvLength)*
-                                    sin(val_coords[1]/tgvLength));
+  su2double u = tgvVelocity * F * (sin(val_coords[0] / tgvLength) * cos(val_coords[1] / tgvLength));
+  su2double v = -tgvVelocity * F * (cos(val_coords[0] / tgvLength) * sin(val_coords[1] / tgvLength));
 
-  su2double B = (cos(2.0*val_coords[0]/tgvLength) +
-                 cos(2.0*val_coords[1]/tgvLength));
-  su2double p = -(tgvDensity/4.0)*B*F*F;
+  su2double B = (cos(2.0 * val_coords[0] / tgvLength) + cos(2.0 * val_coords[1] / tgvLength));
+  su2double p = -(tgvDensity / 4.0) * B * F * F;
 
   /* Compute the conservative variables. Note that both 2D and 3D
    cases are treated correctly. */
-  val_solution[0]      = p;
-  val_solution[1]      = u;
-  val_solution[2]      = v;
-  val_solution[nVar-1] = Temperature;
+  val_solution[0] = p;
+  val_solution[1] = u;
+  val_solution[2] = v;
+  val_solution[nVar - 1] = Temperature;
 }
diff --git a/Common/src/toolboxes/MMS/CInviscidVortexSolution.cpp b/Common/src/toolboxes/MMS/CInviscidVortexSolution.cpp
index f699d9f6ccb..2dc8e090197 100644
--- a/Common/src/toolboxes/MMS/CInviscidVortexSolution.cpp
+++ b/Common/src/toolboxes/MMS/CInviscidVortexSolution.cpp
@@ -27,14 +27,11 @@
 
 #include "../../../include/toolboxes/MMS/CInviscidVortexSolution.hpp"
 
-CInviscidVortexSolution::CInviscidVortexSolution(void) : CVerificationSolution() { }
-
-CInviscidVortexSolution::CInviscidVortexSolution(unsigned short val_nDim,
-                                                 unsigned short val_nVar,
-                                                 unsigned short val_iMesh,
-                                                 CConfig*       config)
-  : CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
+CInviscidVortexSolution::CInviscidVortexSolution(void) : CVerificationSolution() {}
 
+CInviscidVortexSolution::CInviscidVortexSolution(unsigned short val_nDim, unsigned short val_nVar,
+                                                 unsigned short val_iMesh, CConfig* config)
+    : CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
   /*--- Write a message that the solution is initialized for the
    inviscid vortex test case. ---*/
   if ((rank == MASTER_NODE) && (val_iMesh == MESH_0)) {
@@ -45,98 +42,86 @@ CInviscidVortexSolution::CInviscidVortexSolution(unsigned short val_nDim,
   }
 
   /*--- Store the inviscid vortex specific parameters here. ---*/
-  x0Vortex    = -0.5;     // Initial x-coordinate of the vortex center.
-  y0Vortex    =  0.0;     // Initial y-coordinate of the vortex center.
-  RVortex     =  0.1;     // Radius of the vortex.
-  epsVortex   =  1.0;     // Strength of the vortex.
+  x0Vortex = -0.5;  // Initial x-coordinate of the vortex center.
+  y0Vortex = 0.0;   // Initial y-coordinate of the vortex center.
+  RVortex = 0.1;    // Radius of the vortex.
+  epsVortex = 1.0;  // Strength of the vortex.
 
   /* Get the Mach number and advection angle (in degrees). */
-  MachVortex  = config->GetMach();
+  MachVortex = config->GetMach();
   thetaVortex = config->GetAoA();
 
   /*--- Useful coefficients in which Gamma is present. ---*/
-  Gamma    = config->GetGamma();
-  Gm1      = Gamma - 1.0;
-  ovGm1    = 1.0/Gm1;
-  gamOvGm1 = ovGm1*Gamma;
+  Gamma = config->GetGamma();
+  Gm1 = Gamma - 1.0;
+  ovGm1 = 1.0 / Gm1;
+  gamOvGm1 = ovGm1 * Gamma;
 
   /*--- Perform some sanity and error checks for this solution here. ---*/
-  if((config->GetTime_Marching() != TIME_MARCHING::TIME_STEPPING) &&
-     (config->GetTime_Marching() != TIME_MARCHING::DT_STEPPING_1ST) &&
-     (config->GetTime_Marching() != TIME_MARCHING::DT_STEPPING_2ND))
-    SU2_MPI::Error("Unsteady mode must be selected for the inviscid vortex",
-                   CURRENT_FUNCTION);
-
-  if(Kind_Solver != MAIN_SOLVER::EULER && Kind_Solver != MAIN_SOLVER::NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::RANS &&
-     Kind_Solver != MAIN_SOLVER::FEM_EULER && Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::FEM_RANS &&
-     Kind_Solver != MAIN_SOLVER::FEM_LES)
-    SU2_MPI::Error("Compressible flow equations must be selected for the inviscid vortex",
-                   CURRENT_FUNCTION);
-
-  if((Kind_Solver != MAIN_SOLVER::EULER) &&
-     (Kind_Solver != MAIN_SOLVER::FEM_EULER))
-    SU2_MPI::Error("Euler equations must be selected for the inviscid vortex",
-                   CURRENT_FUNCTION);
-
-  if((config->GetKind_FluidModel() != STANDARD_AIR) &&
-     (config->GetKind_FluidModel() != IDEAL_GAS))
-    SU2_MPI::Error("Standard air or ideal gas must be selected for the inviscid vortex",
-                   CURRENT_FUNCTION);
-
-  if(fabs(config->GetPressure_FreeStreamND() - 1.0) > 1.e-8)
-    SU2_MPI::Error("Free-stream pressure must be 1.0 for the inviscid vortex",
-                   CURRENT_FUNCTION);
-
-  if(fabs(config->GetDensity_FreeStreamND() - 1.0) > 1.e-8)
-    SU2_MPI::Error("Free-stream density must be 1.0 for the inviscid vortex",
-                   CURRENT_FUNCTION);
-}
+  if ((config->GetTime_Marching() != TIME_MARCHING::TIME_STEPPING) &&
+      (config->GetTime_Marching() != TIME_MARCHING::DT_STEPPING_1ST) &&
+      (config->GetTime_Marching() != TIME_MARCHING::DT_STEPPING_2ND))
+    SU2_MPI::Error("Unsteady mode must be selected for the inviscid vortex", CURRENT_FUNCTION);
+
+  if (Kind_Solver != MAIN_SOLVER::EULER && Kind_Solver != MAIN_SOLVER::NAVIER_STOKES &&
+      Kind_Solver != MAIN_SOLVER::RANS && Kind_Solver != MAIN_SOLVER::FEM_EULER &&
+      Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::FEM_RANS &&
+      Kind_Solver != MAIN_SOLVER::FEM_LES)
+    SU2_MPI::Error("Compressible flow equations must be selected for the inviscid vortex", CURRENT_FUNCTION);
+
+  if ((Kind_Solver != MAIN_SOLVER::EULER) && (Kind_Solver != MAIN_SOLVER::FEM_EULER))
+    SU2_MPI::Error("Euler equations must be selected for the inviscid vortex", CURRENT_FUNCTION);
 
-CInviscidVortexSolution::~CInviscidVortexSolution(void) { }
+  if ((config->GetKind_FluidModel() != STANDARD_AIR) && (config->GetKind_FluidModel() != IDEAL_GAS))
+    SU2_MPI::Error("Standard air or ideal gas must be selected for the inviscid vortex", CURRENT_FUNCTION);
 
-void CInviscidVortexSolution::GetBCState(const su2double *val_coords,
-                                         const su2double val_t,
-                                         su2double       *val_solution) const {
+  if (fabs(config->GetPressure_FreeStreamND() - 1.0) > 1.e-8)
+    SU2_MPI::Error("Free-stream pressure must be 1.0 for the inviscid vortex", CURRENT_FUNCTION);
 
+  if (fabs(config->GetDensity_FreeStreamND() - 1.0) > 1.e-8)
+    SU2_MPI::Error("Free-stream density must be 1.0 for the inviscid vortex", CURRENT_FUNCTION);
+}
+
+CInviscidVortexSolution::~CInviscidVortexSolution(void) {}
+
+void CInviscidVortexSolution::GetBCState(const su2double* val_coords, const su2double val_t,
+                                         su2double* val_solution) const {
   /*--- For the case that the inviscid vortex is run with boundary
         conditions (other possibility is with periodic conditions),
         the exact solution is prescribed on the boundaries. ---*/
   GetSolution(val_coords, val_t, val_solution);
 }
 
-void CInviscidVortexSolution::GetSolution(const su2double *val_coords,
-                                          const su2double val_t,
-                                          su2double       *val_solution) const {
-
+void CInviscidVortexSolution::GetSolution(const su2double* val_coords, const su2double val_t,
+                                          su2double* val_solution) const {
   /* Compute the free stream velocities in x- and y-direction. */
-  const su2double VelInf = MachVortex*sqrt(Gamma);
-  const su2double uInf   = VelInf*cos(thetaVortex*PI_NUMBER/180.0);
-  const su2double vInf   = VelInf*sin(thetaVortex*PI_NUMBER/180.0);
+  const su2double VelInf = MachVortex * sqrt(Gamma);
+  const su2double uInf = VelInf * cos(thetaVortex * PI_NUMBER / 180.0);
+  const su2double vInf = VelInf * sin(thetaVortex * PI_NUMBER / 180.0);
 
   /* Compute the coordinates relative to the center of the vortex. */
-  const su2double dx = val_coords[0] - (x0Vortex + val_t*uInf);
-  const su2double dy = val_coords[1] - (y0Vortex + val_t*vInf);
+  const su2double dx = val_coords[0] - (x0Vortex + val_t * uInf);
+  const su2double dy = val_coords[1] - (y0Vortex + val_t * vInf);
 
   /* Compute the components of the velocity. */
-  su2double f  = 1.0 - (dx*dx + dy*dy)/(RVortex*RVortex);
-  su2double t1 = epsVortex*dy*exp(0.5*f)/(2.0*PI_NUMBER*RVortex);
-  su2double u  = uInf - VelInf*t1;
+  su2double f = 1.0 - (dx * dx + dy * dy) / (RVortex * RVortex);
+  su2double t1 = epsVortex * dy * exp(0.5 * f) / (2.0 * PI_NUMBER * RVortex);
+  su2double u = uInf - VelInf * t1;
 
-  t1          = epsVortex*dx*exp(0.5*f)/(2.0*PI_NUMBER*RVortex);
-  su2double v = vInf + VelInf*t1;
+  t1 = epsVortex * dx * exp(0.5 * f) / (2.0 * PI_NUMBER * RVortex);
+  su2double v = vInf + VelInf * t1;
 
   /* Compute the density and the pressure. */
-  t1 = 1.0 - epsVortex*epsVortex*Gm1
-     *       MachVortex*MachVortex*exp(f)/(8.0*PI_NUMBER*PI_NUMBER);
+  t1 = 1.0 - epsVortex * epsVortex * Gm1 * MachVortex * MachVortex * exp(f) / (8.0 * PI_NUMBER * PI_NUMBER);
 
-  su2double rho = pow(t1,ovGm1);
-  su2double p   = pow(t1,gamOvGm1);
+  su2double rho = pow(t1, ovGm1);
+  su2double p = pow(t1, gamOvGm1);
 
   /* Compute the conservative variables. Note that both 2D and 3D
      cases are treated correctly. */
-  val_solution[0]      = rho;
-  val_solution[1]      = rho*u;
-  val_solution[2]      = rho*v;
-  val_solution[3]      = 0.0;
-  val_solution[nVar-1] = p*ovGm1 + 0.5*rho*(u*u + v*v);
+  val_solution[0] = rho;
+  val_solution[1] = rho * u;
+  val_solution[2] = rho * v;
+  val_solution[3] = 0.0;
+  val_solution[nVar - 1] = p * ovGm1 + 0.5 * rho * (u * u + v * v);
 }
diff --git a/Common/src/toolboxes/MMS/CMMSIncEulerSolution.cpp b/Common/src/toolboxes/MMS/CMMSIncEulerSolution.cpp
index 2352988dcdc..9c6e28ee18e 100644
--- a/Common/src/toolboxes/MMS/CMMSIncEulerSolution.cpp
+++ b/Common/src/toolboxes/MMS/CMMSIncEulerSolution.cpp
@@ -27,14 +27,11 @@
 
 #include "../../../include/toolboxes/MMS/CMMSIncEulerSolution.hpp"
 
-CMMSIncEulerSolution::CMMSIncEulerSolution(void) : CVerificationSolution() { }
-
-CMMSIncEulerSolution::CMMSIncEulerSolution(unsigned short val_nDim,
-                                           unsigned short val_nVar,
-                                           unsigned short val_iMesh,
-                                           CConfig*       config)
-: CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
+CMMSIncEulerSolution::CMMSIncEulerSolution(void) : CVerificationSolution() {}
 
+CMMSIncEulerSolution::CMMSIncEulerSolution(unsigned short val_nDim, unsigned short val_nVar, unsigned short val_iMesh,
+                                           CConfig* config)
+    : CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
   /*--- Write a message that the solution is initialized for the manufactured
    solution for the incompressible Navier-Stokes equations. ---*/
   if ((rank == MASTER_NODE) && (val_iMesh == MESH_0)) {
@@ -46,7 +43,7 @@ CMMSIncEulerSolution::CMMSIncEulerSolution(unsigned short val_nDim,
   }
 
   /*--- Coefficients, needed to determine the solution. ---*/
-  Density     = config->GetDensity_FreeStreamND();
+  Density = config->GetDensity_FreeStreamND();
   Temperature = config->GetTemperature_FreeStreamND();
 
   /*--- Constants, which describe this manufactured solution. This is a
@@ -55,85 +52,80 @@ CMMSIncEulerSolution::CMMSIncEulerSolution(unsigned short val_nDim,
    Knupp P, "Code verification by the method of manufactured solutions,"
    SAND 2000-1444, Sandia National Laboratories, Albuquerque, NM, 2000. ---*/
 
-  P_0     =   1.0;
-  u_0     =   1.0;
-  v_0     =   1.0;
+  P_0 = 1.0;
+  u_0 = 1.0;
+  v_0 = 1.0;
   epsilon = 0.001;
 
   /*--- Perform some sanity and error checks for this solution here. ---*/
-  if(config->GetTime_Marching() != TIME_MARCHING::STEADY)
-    SU2_MPI::Error("Steady mode must be selected for the MMS incompressible Euler case",
-                   CURRENT_FUNCTION);
+  if (config->GetTime_Marching() != TIME_MARCHING::STEADY)
+    SU2_MPI::Error("Steady mode must be selected for the MMS incompressible Euler case", CURRENT_FUNCTION);
 
-  if(Kind_Solver != MAIN_SOLVER::INC_EULER && Kind_Solver != MAIN_SOLVER::INC_NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::INC_RANS )
+  if (Kind_Solver != MAIN_SOLVER::INC_EULER && Kind_Solver != MAIN_SOLVER::INC_NAVIER_STOKES &&
+      Kind_Solver != MAIN_SOLVER::INC_RANS)
     SU2_MPI::Error("Incompressible flow equations must be selected for the MMS incompressible Euler case",
                    CURRENT_FUNCTION);
 
-  if(Kind_Solver != MAIN_SOLVER::INC_EULER)
-    SU2_MPI::Error("Euler equations must be selected for the MMS incompressible Euler case",
-                   CURRENT_FUNCTION);
+  if (Kind_Solver != MAIN_SOLVER::INC_EULER)
+    SU2_MPI::Error("Euler equations must be selected for the MMS incompressible Euler case", CURRENT_FUNCTION);
 
-  if(config->GetKind_FluidModel() != CONSTANT_DENSITY)
+  if (config->GetKind_FluidModel() != CONSTANT_DENSITY)
     SU2_MPI::Error("Constant density fluid model must be selected for the MMS incompressible Euler case",
                    CURRENT_FUNCTION);
 
-  if(config->GetEnergy_Equation())
+  if (config->GetEnergy_Equation())
     SU2_MPI::Error("Energy equation must be disabled (isothermal) for the MMS incompressible Euler case",
                    CURRENT_FUNCTION);
 }
 
-CMMSIncEulerSolution::~CMMSIncEulerSolution(void) { }
-
-void CMMSIncEulerSolution::GetBCState(const su2double *val_coords,
-                                      const su2double val_t,
-                                      su2double       *val_solution) const {
+CMMSIncEulerSolution::~CMMSIncEulerSolution(void) {}
 
+void CMMSIncEulerSolution::GetBCState(const su2double* val_coords, const su2double val_t,
+                                      su2double* val_solution) const {
   /*--- The exact solution is prescribed on the boundaries. ---*/
   GetSolution(val_coords, val_t, val_solution);
 }
 
-void CMMSIncEulerSolution::GetSolution(const su2double *val_coords,
-                                       const su2double val_t,
-                                       su2double       *val_solution) const {
-
+void CMMSIncEulerSolution::GetSolution(const su2double* val_coords, const su2double val_t,
+                                       su2double* val_solution) const {
   /* Easier storage of the x- and y-coordinates. */
   const su2double x = val_coords[0];
   const su2double y = val_coords[1];
 
   /* Compute the primitives from the defined solution. */
-  const su2double u = u_0*(sin(x*x + y*y) + epsilon);
-  const su2double v = v_0*(cos(x*x + y*y) + epsilon);
-  const su2double p = P_0*(sin(x*x + y*y) +     2.0);
+  const su2double u = u_0 * (sin(x * x + y * y) + epsilon);
+  const su2double v = v_0 * (cos(x * x + y * y) + epsilon);
+  const su2double p = P_0 * (sin(x * x + y * y) + 2.0);
 
   /* For the incompressible solver, we return the primitive variables
    directly, as they are used for the working variables in the solver.
    Note that the implementation below is valid for both 2D and 3D. */
-  val_solution[0]      = p;
-  val_solution[1]      = u;
-  val_solution[2]      = v;
-  val_solution[3]      = 0.0;
-  val_solution[nVar-1] = Temperature;
-
+  val_solution[0] = p;
+  val_solution[1] = u;
+  val_solution[2] = v;
+  val_solution[3] = 0.0;
+  val_solution[nVar - 1] = Temperature;
 }
 
-void CMMSIncEulerSolution::GetMMSSourceTerm(const su2double *val_coords,
-                                            const su2double val_t,
-                                            su2double       *val_source) const {
-
+void CMMSIncEulerSolution::GetMMSSourceTerm(const su2double* val_coords, const su2double val_t,
+                                            su2double* val_source) const {
   /*--- Easier storage of the x- and y-coordinates. ---*/
   const su2double x = val_coords[0];
   const su2double y = val_coords[1];
 
   /*--- The expressions for the source terms are generated
    automatically by the sympy package in python.---*/
-  val_source[0] = 2*Density*(u_0*x*cos(pow(x, 2) + pow(y, 2)) - v_0*y*sin(pow(x, 2) + pow(y, 2)));
-  val_source[1] = 4*Density*pow(u_0, 2)*x*(epsilon + sin(pow(x, 2) + pow(y, 2)))*cos(pow(x, 2) + pow(y, 2)) - 2*Density*u_0*v_0*y*(epsilon + sin(pow(x, 2) + pow(y, 2)))*sin(pow(x, 2) + pow(y, 2)) + 2*Density*u_0*v_0*y*(epsilon + cos(pow(x, 2) + pow(y, 2)))*cos(pow(x, 2) + pow(y, 2)) + 2*P_0*x*cos(pow(x, 2) + pow(y, 2));
-  val_source[2] = -2*Density*u_0*v_0*x*(epsilon + sin(pow(x, 2) + pow(y, 2)))*sin(pow(x, 2) + pow(y, 2)) + 2*Density*u_0*v_0*x*(epsilon + cos(pow(x, 2) + pow(y, 2)))*cos(pow(x, 2) + pow(y, 2)) - 4*Density*pow(v_0, 2)*y*(epsilon + cos(pow(x, 2) + pow(y, 2)))*sin(pow(x, 2) + pow(y, 2)) + 2*P_0*y*cos(pow(x, 2) + pow(y, 2));
-  val_source[3]      = 0.0;
-  val_source[nVar-1] = 0.0;
-
+  val_source[0] = 2 * Density * (u_0 * x * cos(pow(x, 2) + pow(y, 2)) - v_0 * y * sin(pow(x, 2) + pow(y, 2)));
+  val_source[1] = 4 * Density * pow(u_0, 2) * x * (epsilon + sin(pow(x, 2) + pow(y, 2))) * cos(pow(x, 2) + pow(y, 2)) -
+                  2 * Density * u_0 * v_0 * y * (epsilon + sin(pow(x, 2) + pow(y, 2))) * sin(pow(x, 2) + pow(y, 2)) +
+                  2 * Density * u_0 * v_0 * y * (epsilon + cos(pow(x, 2) + pow(y, 2))) * cos(pow(x, 2) + pow(y, 2)) +
+                  2 * P_0 * x * cos(pow(x, 2) + pow(y, 2));
+  val_source[2] = -2 * Density * u_0 * v_0 * x * (epsilon + sin(pow(x, 2) + pow(y, 2))) * sin(pow(x, 2) + pow(y, 2)) +
+                  2 * Density * u_0 * v_0 * x * (epsilon + cos(pow(x, 2) + pow(y, 2))) * cos(pow(x, 2) + pow(y, 2)) -
+                  4 * Density * pow(v_0, 2) * y * (epsilon + cos(pow(x, 2) + pow(y, 2))) * sin(pow(x, 2) + pow(y, 2)) +
+                  2 * P_0 * y * cos(pow(x, 2) + pow(y, 2));
+  val_source[3] = 0.0;
+  val_source[nVar - 1] = 0.0;
 }
 
-bool CMMSIncEulerSolution::IsManufacturedSolution(void) const {
-  return true;
-}
+bool CMMSIncEulerSolution::IsManufacturedSolution(void) const { return true; }
diff --git a/Common/src/toolboxes/MMS/CMMSIncNSSolution.cpp b/Common/src/toolboxes/MMS/CMMSIncNSSolution.cpp
index 8cd7ed00b89..8cf32d65407 100644
--- a/Common/src/toolboxes/MMS/CMMSIncNSSolution.cpp
+++ b/Common/src/toolboxes/MMS/CMMSIncNSSolution.cpp
@@ -27,14 +27,11 @@
 
 #include "../../../include/toolboxes/MMS/CMMSIncNSSolution.hpp"
 
-CMMSIncNSSolution::CMMSIncNSSolution(void) : CVerificationSolution() { }
-
-CMMSIncNSSolution::CMMSIncNSSolution(unsigned short val_nDim,
-                                     unsigned short val_nVar,
-                                     unsigned short val_iMesh,
-                                     CConfig*       config)
-: CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
+CMMSIncNSSolution::CMMSIncNSSolution(void) : CVerificationSolution() {}
 
+CMMSIncNSSolution::CMMSIncNSSolution(unsigned short val_nDim, unsigned short val_nVar, unsigned short val_iMesh,
+                                     CConfig* config)
+    : CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
   /*--- Write a message that the solution is initialized for the manufactured
    solution for the incompressible Navier-Stokes equations. ---*/
   if ((rank == MASTER_NODE) && (val_iMesh == MESH_0)) {
@@ -46,8 +43,8 @@ CMMSIncNSSolution::CMMSIncNSSolution(unsigned short val_nDim,
   }
 
   /*--- Coefficients, needed to determine the solution. ---*/
-  Viscosity   = config->GetViscosity_FreeStreamND();
-  Density     = config->GetDensity_FreeStreamND();
+  Viscosity = config->GetViscosity_FreeStreamND();
+  Density = config->GetDensity_FreeStreamND();
   Temperature = config->GetTemperature_FreeStreamND();
 
   /*--- Constants, which describe this manufactured solution. This is a
@@ -56,89 +53,93 @@ CMMSIncNSSolution::CMMSIncNSSolution(unsigned short val_nDim,
    Knupp P, "Code verification by the method of manufactured solutions,"
    SAND 2000-1444, Sandia National Laboratories, Albuquerque, NM, 2000. ---*/
 
-  P_0     =   1.0;
-  u_0     =   1.0;
-  v_0     =   1.0;
+  P_0 = 1.0;
+  u_0 = 1.0;
+  v_0 = 1.0;
   epsilon = 0.001;
 
   /*--- Perform some sanity and error checks for this solution here. ---*/
-  if(config->GetTime_Marching() != TIME_MARCHING::STEADY)
-    SU2_MPI::Error("Steady mode must be selected for the MMS incompressible NS case",
-                   CURRENT_FUNCTION);
+  if (config->GetTime_Marching() != TIME_MARCHING::STEADY)
+    SU2_MPI::Error("Steady mode must be selected for the MMS incompressible NS case", CURRENT_FUNCTION);
 
-  if(Kind_Solver != MAIN_SOLVER::INC_EULER && Kind_Solver != MAIN_SOLVER::INC_NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::INC_RANS )
+  if (Kind_Solver != MAIN_SOLVER::INC_EULER && Kind_Solver != MAIN_SOLVER::INC_NAVIER_STOKES &&
+      Kind_Solver != MAIN_SOLVER::INC_RANS)
     SU2_MPI::Error("Incompressible flow equations must be selected for the MMS incompressible NS case",
                    CURRENT_FUNCTION);
 
-  if(Kind_Solver != MAIN_SOLVER::INC_NAVIER_STOKES)
-    SU2_MPI::Error("Navier Stokes equations must be selected for the MMS incompressible NS case",
-                   CURRENT_FUNCTION);
+  if (Kind_Solver != MAIN_SOLVER::INC_NAVIER_STOKES)
+    SU2_MPI::Error("Navier Stokes equations must be selected for the MMS incompressible NS case", CURRENT_FUNCTION);
 
-  if(config->GetKind_FluidModel() != CONSTANT_DENSITY)
+  if (config->GetKind_FluidModel() != CONSTANT_DENSITY)
     SU2_MPI::Error("Constant density fluid model must be selected for the MMS incompressible NS case",
                    CURRENT_FUNCTION);
 
-  if(config->GetKind_ViscosityModel() != VISCOSITYMODEL::CONSTANT)
-    SU2_MPI::Error("Constant viscosity must be selected for the MMS incompressible NS case",
-                   CURRENT_FUNCTION);
+  if (config->GetKind_ViscosityModel() != VISCOSITYMODEL::CONSTANT)
+    SU2_MPI::Error("Constant viscosity must be selected for the MMS incompressible NS case", CURRENT_FUNCTION);
 
-  if(config->GetEnergy_Equation())
+  if (config->GetEnergy_Equation())
     SU2_MPI::Error("Energy equation must be disabled (isothermal) for the MMS incompressible NS case",
                    CURRENT_FUNCTION);
 }
 
-CMMSIncNSSolution::~CMMSIncNSSolution(void) { }
-
-void CMMSIncNSSolution::GetBCState(const su2double *val_coords,
-                                   const su2double val_t,
-                                   su2double       *val_solution) const {
+CMMSIncNSSolution::~CMMSIncNSSolution(void) {}
 
+void CMMSIncNSSolution::GetBCState(const su2double* val_coords, const su2double val_t, su2double* val_solution) const {
   /*--- The exact solution is prescribed on the boundaries. ---*/
   GetSolution(val_coords, val_t, val_solution);
 }
 
-void CMMSIncNSSolution::GetSolution(const su2double *val_coords,
-                                    const su2double val_t,
-                                    su2double       *val_solution) const {
-
+void CMMSIncNSSolution::GetSolution(const su2double* val_coords, const su2double val_t, su2double* val_solution) const {
   /* Easier storage of the x- and y-coordinates. */
   const su2double x = val_coords[0];
   const su2double y = val_coords[1];
 
   /* Compute the primitives from the defined solution. */
-  const su2double u = u_0*(sin(x*x + y*y) + epsilon);
-  const su2double v = v_0*(cos(x*x + y*y) + epsilon);
-  const su2double p = P_0*(sin(x*x + y*y) +     2.0);
+  const su2double u = u_0 * (sin(x * x + y * y) + epsilon);
+  const su2double v = v_0 * (cos(x * x + y * y) + epsilon);
+  const su2double p = P_0 * (sin(x * x + y * y) + 2.0);
 
   /* For the incompressible solver, we return the primitive variables
    directly, as they are used for the working variables in the solver.
    Note that the implementation below is valid for both 2D and 3D. */
-  val_solution[0]      = p;
-  val_solution[1]      = u;
-  val_solution[2]      = v;
-  val_solution[3]      = 0.0;
-  val_solution[nVar-1] = Temperature;
-
+  val_solution[0] = p;
+  val_solution[1] = u;
+  val_solution[2] = v;
+  val_solution[3] = 0.0;
+  val_solution[nVar - 1] = Temperature;
 }
 
-void CMMSIncNSSolution::GetMMSSourceTerm(const su2double *val_coords,
-                                         const su2double val_t,
-                                         su2double       *val_source) const {
-
+void CMMSIncNSSolution::GetMMSSourceTerm(const su2double* val_coords, const su2double val_t,
+                                         su2double* val_source) const {
   /*--- Easier storage of the x- and y-coordinates. ---*/
   const su2double x = val_coords[0];
   const su2double y = val_coords[1];
 
   /*--- The expressions for the source terms are generated
    automatically by the sympy package in python.---*/
-  val_source[0] = 2*Density*(u_0*x*cos(pow(x, 2) + pow(y, 2)) - v_0*y*sin(pow(x, 2) + pow(y, 2)));
-  val_source[1] = 4*Density*pow(u_0, 2)*x*(epsilon + sin(pow(x, 2) + pow(y, 2)))*cos(pow(x, 2) + pow(y, 2)) - 2*Density*u_0*v_0*y*(epsilon + sin(pow(x, 2) + pow(y, 2)))*sin(pow(x, 2) + pow(y, 2)) + 2*Density*u_0*v_0*y*(epsilon + cos(pow(x, 2) + pow(y, 2)))*cos(pow(x, 2) + pow(y, 2)) + 2*P_0*x*cos(pow(x, 2) + pow(y, 2)) - 0.666666666666667*Viscosity*(-8.0*u_0*pow(x, 2)*sin(pow(x, 2) + pow(y, 2)) + 4.0*u_0*cos(pow(x, 2) + pow(y, 2)) + 4*v_0*x*y*cos(pow(x, 2) + pow(y, 2))) + 2*Viscosity*(2*u_0*pow(y, 2)*sin(pow(x, 2) + pow(y, 2)) - u_0*cos(pow(x, 2) + pow(y, 2)) + 2*v_0*x*y*cos(pow(x, 2) + pow(y, 2)));
-  val_source[2] = -2*Density*u_0*v_0*x*(epsilon + sin(pow(x, 2) + pow(y, 2)))*sin(pow(x, 2) + pow(y, 2)) + 2*Density*u_0*v_0*x*(epsilon + cos(pow(x, 2) + pow(y, 2)))*cos(pow(x, 2) + pow(y, 2)) - 4*Density*pow(v_0, 2)*y*(epsilon + cos(pow(x, 2) + pow(y, 2)))*sin(pow(x, 2) + pow(y, 2)) + 2*P_0*y*cos(pow(x, 2) + pow(y, 2)) + 0.666666666666667*Viscosity*(-4*u_0*x*y*sin(pow(x, 2) + pow(y, 2)) + 8.0*v_0*pow(y, 2)*cos(pow(x, 2) + pow(y, 2)) + 4.0*v_0*sin(pow(x, 2) + pow(y, 2))) + 2*Viscosity*(2*u_0*x*y*sin(pow(x, 2) + pow(y, 2)) + 2*v_0*pow(x, 2)*cos(pow(x, 2) + pow(y, 2)) + v_0*sin(pow(x, 2) + pow(y, 2)));
-  val_source[3]      = 0.0;
-  val_source[nVar-1] = 0.0;
-
+  val_source[0] = 2 * Density * (u_0 * x * cos(pow(x, 2) + pow(y, 2)) - v_0 * y * sin(pow(x, 2) + pow(y, 2)));
+  val_source[1] = 4 * Density * pow(u_0, 2) * x * (epsilon + sin(pow(x, 2) + pow(y, 2))) * cos(pow(x, 2) + pow(y, 2)) -
+                  2 * Density * u_0 * v_0 * y * (epsilon + sin(pow(x, 2) + pow(y, 2))) * sin(pow(x, 2) + pow(y, 2)) +
+                  2 * Density * u_0 * v_0 * y * (epsilon + cos(pow(x, 2) + pow(y, 2))) * cos(pow(x, 2) + pow(y, 2)) +
+                  2 * P_0 * x * cos(pow(x, 2) + pow(y, 2)) -
+                  0.666666666666667 * Viscosity *
+                      (-8.0 * u_0 * pow(x, 2) * sin(pow(x, 2) + pow(y, 2)) + 4.0 * u_0 * cos(pow(x, 2) + pow(y, 2)) +
+                       4 * v_0 * x * y * cos(pow(x, 2) + pow(y, 2))) +
+                  2 * Viscosity *
+                      (2 * u_0 * pow(y, 2) * sin(pow(x, 2) + pow(y, 2)) - u_0 * cos(pow(x, 2) + pow(y, 2)) +
+                       2 * v_0 * x * y * cos(pow(x, 2) + pow(y, 2)));
+  val_source[2] = -2 * Density * u_0 * v_0 * x * (epsilon + sin(pow(x, 2) + pow(y, 2))) * sin(pow(x, 2) + pow(y, 2)) +
+                  2 * Density * u_0 * v_0 * x * (epsilon + cos(pow(x, 2) + pow(y, 2))) * cos(pow(x, 2) + pow(y, 2)) -
+                  4 * Density * pow(v_0, 2) * y * (epsilon + cos(pow(x, 2) + pow(y, 2))) * sin(pow(x, 2) + pow(y, 2)) +
+                  2 * P_0 * y * cos(pow(x, 2) + pow(y, 2)) +
+                  0.666666666666667 * Viscosity *
+                      (-4 * u_0 * x * y * sin(pow(x, 2) + pow(y, 2)) +
+                       8.0 * v_0 * pow(y, 2) * cos(pow(x, 2) + pow(y, 2)) + 4.0 * v_0 * sin(pow(x, 2) + pow(y, 2))) +
+                  2 * Viscosity *
+                      (2 * u_0 * x * y * sin(pow(x, 2) + pow(y, 2)) + 2 * v_0 * pow(x, 2) * cos(pow(x, 2) + pow(y, 2)) +
+                       v_0 * sin(pow(x, 2) + pow(y, 2)));
+  val_source[3] = 0.0;
+  val_source[nVar - 1] = 0.0;
 }
 
-bool CMMSIncNSSolution::IsManufacturedSolution(void) const {
-  return true;
-}
+bool CMMSIncNSSolution::IsManufacturedSolution(void) const { return true; }
diff --git a/Common/src/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.cpp b/Common/src/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.cpp
index c21f7d927a3..70f6cee1164 100644
--- a/Common/src/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.cpp
+++ b/Common/src/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.cpp
@@ -27,14 +27,11 @@
 
 #include "../../../include/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.hpp"
 
-CMMSNSTwoHalfCirclesSolution::CMMSNSTwoHalfCirclesSolution(void) : CVerificationSolution() { }
-
-CMMSNSTwoHalfCirclesSolution::CMMSNSTwoHalfCirclesSolution(unsigned short val_nDim,
-                                                           unsigned short val_nVar,
-                                                           unsigned short val_iMesh,
-                                                           CConfig*       config)
-  : CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
+CMMSNSTwoHalfCirclesSolution::CMMSNSTwoHalfCirclesSolution(void) : CVerificationSolution() {}
 
+CMMSNSTwoHalfCirclesSolution::CMMSNSTwoHalfCirclesSolution(unsigned short val_nDim, unsigned short val_nVar,
+                                                           unsigned short val_iMesh, CConfig* config)
+    : CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
   /*--- Write a message that the solution is initialized for the manufactured
    solution for the Navier-Stokes equations between two half circles. ---*/
   if ((rank == MASTER_NODE) && (val_iMesh == MESH_0)) {
@@ -48,17 +45,17 @@ CMMSNSTwoHalfCirclesSolution::CMMSNSTwoHalfCirclesSolution(unsigned short val_nD
   /*--- Coefficients, needed to determine the solution. ---*/
   const su2double Prandtl = config->GetPrandtl_Lam();
 
-  RGas         = config->GetGas_Constant();
-  Gamma        = config->GetGamma();
-  Viscosity    = config->GetMu_Constant();
-  Conductivity = Viscosity*Gamma*RGas/(Prandtl*(Gamma-1.0));
+  RGas = config->GetGas_Constant();
+  Gamma = config->GetGamma();
+  Viscosity = config->GetMu_Constant();
+  Conductivity = Viscosity * Gamma * RGas / (Prandtl * (Gamma - 1.0));
 
   /*--- Initialize TWall to the default value of 300 K (in case the outer wall
         is not modelled as an isothermal wall) and try to retrieve the wall
         temperature from the boundary conditions. ---*/
   TWall = 300.0;
-  for(unsigned short iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-    if(config->GetMarker_All_KindBC(iMarker) == ISOTHERMAL) {
+  for (unsigned short iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
+    if (config->GetMarker_All_KindBC(iMarker) == ISOTHERMAL) {
       const string Marker_Tag = config->GetMarker_All_TagBound(iMarker);
       TWall = config->GetIsothermal_Temperature(Marker_Tag);
     }
@@ -66,100 +63,88 @@ CMMSNSTwoHalfCirclesSolution::CMMSNSTwoHalfCirclesSolution(unsigned short val_nD
 
   /*--- Get the reference values for pressure, density and velocity. ---*/
   Pressure_Ref = config->GetPressure_Ref();
-  Density_Ref  = config->GetDensity_Ref();
+  Density_Ref = config->GetDensity_Ref();
   Velocity_Ref = config->GetVelocity_Ref();
 
   /*--- The constants for the density and velocities. ---*/
-  rho_0 =   1.25;
-  u_0   = 135.78;
-  v_0   = -67.61;
+  rho_0 = 1.25;
+  u_0 = 135.78;
+  v_0 = -67.61;
 
   /*--- The constants for the temperature solution. ---*/
-  a_T1 =  1.05;
+  a_T1 = 1.05;
   a_T2 = -0.85;
 
   /*--- Perform some sanity and error checks for this solution here. ---*/
-  if(config->GetTime_Marching() != TIME_MARCHING::STEADY)
-    SU2_MPI::Error("Steady mode must be selected for the MMS NS Two Half Circles case",
+  if (config->GetTime_Marching() != TIME_MARCHING::STEADY)
+    SU2_MPI::Error("Steady mode must be selected for the MMS NS Two Half Circles case", CURRENT_FUNCTION);
+
+  if (Kind_Solver != MAIN_SOLVER::EULER && Kind_Solver != MAIN_SOLVER::NAVIER_STOKES &&
+      Kind_Solver != MAIN_SOLVER::RANS && Kind_Solver != MAIN_SOLVER::FEM_EULER &&
+      Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::FEM_RANS &&
+      Kind_Solver != MAIN_SOLVER::FEM_LES)
+    SU2_MPI::Error("Compressible flow equations must be selected for the MMS NS Two Half Circles case",
                    CURRENT_FUNCTION);
 
-  if(Kind_Solver != MAIN_SOLVER::EULER && Kind_Solver != MAIN_SOLVER::NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::RANS &&
-     Kind_Solver != MAIN_SOLVER::FEM_EULER && Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::FEM_RANS &&
-     Kind_Solver != MAIN_SOLVER::FEM_LES)    SU2_MPI::Error("Compressible flow equations must be selected for the MMS NS Two Half Circles case",
-                   CURRENT_FUNCTION);
+  if ((Kind_Solver != MAIN_SOLVER::NAVIER_STOKES) && (Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES))
+    SU2_MPI::Error("Navier Stokes equations must be selected for the MMS NS Two Half Circles case", CURRENT_FUNCTION);
 
-  if((Kind_Solver != MAIN_SOLVER::NAVIER_STOKES) &&
-     (Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES))
-    SU2_MPI::Error("Navier Stokes equations must be selected for the MMS NS Two Half Circles case",
-                   CURRENT_FUNCTION);
+  if ((config->GetKind_FluidModel() != STANDARD_AIR) && (config->GetKind_FluidModel() != IDEAL_GAS))
+    SU2_MPI::Error("Standard air or ideal gas must be selected for the MMS NS Two Half Circles case", CURRENT_FUNCTION);
 
-  if((config->GetKind_FluidModel() != STANDARD_AIR) &&
-     (config->GetKind_FluidModel() != IDEAL_GAS))
-    SU2_MPI::Error("Standard air or ideal gas must be selected for the MMS NS Two Half Circles case",
-                   CURRENT_FUNCTION);
+  if (config->GetKind_ViscosityModel() != VISCOSITYMODEL::CONSTANT)
+    SU2_MPI::Error("Sutherland must be selected for viscosity for the MMS NS Two Half Circles case", CURRENT_FUNCTION);
 
-  if(config->GetKind_ViscosityModel() != VISCOSITYMODEL::CONSTANT)
-    SU2_MPI::Error("Sutherland must be selected for viscosity for the MMS NS Two Half Circles case",
-                   CURRENT_FUNCTION);
-
-  if(config->GetKind_ConductivityModel() != CONDUCTIVITYMODEL::CONSTANT_PRANDTL)
-    SU2_MPI::Error("Constant Prandtl number must be selected for the MMS NS Two Half Circles case",
-                   CURRENT_FUNCTION);
+  if (config->GetKind_ConductivityModel() != CONDUCTIVITYMODEL::CONSTANT_PRANDTL)
+    SU2_MPI::Error("Constant Prandtl number must be selected for the MMS NS Two Half Circles case", CURRENT_FUNCTION);
 }
 
-CMMSNSTwoHalfCirclesSolution::~CMMSNSTwoHalfCirclesSolution(void) { }
-
-void CMMSNSTwoHalfCirclesSolution::GetBCState(const su2double *val_coords,
-                                              const su2double val_t,
-                                              su2double       *val_solution) const {
+CMMSNSTwoHalfCirclesSolution::~CMMSNSTwoHalfCirclesSolution(void) {}
 
+void CMMSNSTwoHalfCirclesSolution::GetBCState(const su2double* val_coords, const su2double val_t,
+                                              su2double* val_solution) const {
   /*--- The exact solution is prescribed on the boundaries. ---*/
   GetSolution(val_coords, val_t, val_solution);
 }
 
-void CMMSNSTwoHalfCirclesSolution::GetSolution(const su2double *val_coords,
-                                               const su2double val_t,
-                                               su2double       *val_solution) const {
-
+void CMMSNSTwoHalfCirclesSolution::GetSolution(const su2double* val_coords, const su2double val_t,
+                                               su2double* val_solution) const {
   /* Easier storage of the x- and y-coordinates. */
   const su2double x = val_coords[0];
   const su2double y = val_coords[1];
 
   /* Determine the dimensional solution for the temperature. */
-  const su2double Pi   = PI_NUMBER;
-  const su2double r    = sqrt(x*x + y*y);
-  const su2double fact = (r-1.0)*(r-1.0)/(a_T1 + a_T2);
+  const su2double Pi = PI_NUMBER;
+  const su2double r = sqrt(x * x + y * y);
+  const su2double fact = (r - 1.0) * (r - 1.0) / (a_T1 + a_T2);
 
-  su2double T = 0.25*TWall*(3.0 + fact*(a_T1*cos(Pi*(r-2.0))
-              +                         a_T2*cos(Pi*(r-2.0)*2.0)));
+  su2double T = 0.25 * TWall * (3.0 + fact * (a_T1 * cos(Pi * (r - 2.0)) + a_T2 * cos(Pi * (r - 2.0) * 2.0)));
 
   /* Determine the dimensional solution for the velocities. */
-  su2double u = u_0*(r-1.0)*(2.0-r)*4.0;
-  su2double v = v_0*(r-1.0)*(2.0-r)*4.0;
+  su2double u = u_0 * (r - 1.0) * (2.0 - r) * 4.0;
+  su2double v = v_0 * (r - 1.0) * (2.0 - r) * 4.0;
 
   /* Compute the pressure from the density and temperature. */
   su2double rho = rho_0;
-  su2double p   = rho*RGas*T;
+  su2double p = rho * RGas * T;
 
   /* Determine the non-dimensional solution. */
   rho /= Density_Ref;
-  p   /= Pressure_Ref;
-  u   /= Velocity_Ref;
-  v   /= Velocity_Ref;
+  p /= Pressure_Ref;
+  u /= Velocity_Ref;
+  v /= Velocity_Ref;
 
   /* Determine the non-dimensional conserved variables.
      Note that the implementation below is valid for both 2D and 3D. */
-  val_solution[0]      = rho;
-  val_solution[1]      = rho*u;
-  val_solution[2]      = rho*v;
-  val_solution[3]      = 0.0;
-  val_solution[nDim+1] = p/(Gamma-1.0) + 0.5*rho*(u*u + v*v);
+  val_solution[0] = rho;
+  val_solution[1] = rho * u;
+  val_solution[2] = rho * v;
+  val_solution[3] = 0.0;
+  val_solution[nDim + 1] = p / (Gamma - 1.0) + 0.5 * rho * (u * u + v * v);
 }
 
-void CMMSNSTwoHalfCirclesSolution::GetMMSSourceTerm(const su2double *val_coords,
-                                                    const su2double val_t,
-                                                    su2double       *val_source) const {
-
+void CMMSNSTwoHalfCirclesSolution::GetMMSSourceTerm(const su2double* val_coords, const su2double val_t,
+                                                    su2double* val_source) const {
   /*--- Abbreviate Pi and the coordinates. ---*/
   const su2double Pi = PI_NUMBER;
   const su2double x = val_coords[0];
@@ -167,7 +152,7 @@ void CMMSNSTwoHalfCirclesSolution::GetMMSSourceTerm(const su2double *val_coords,
 
   /*--- The source code for the source terms is generated in Maple.
         See the file CMMSNSTwoHalfCirclesSolution.mw in the directory
-       	CreateMMSSourceTerms for the details how to do this. ---*/
+        CreateMMSSourceTerms for the details how to do this. ---*/
   const su2double t1 = rho_0 * u_0;
   const su2double t2 = x * x;
   const su2double t3 = y * y;
@@ -225,12 +210,14 @@ void CMMSNSTwoHalfCirclesSolution::GetMMSSourceTerm(const su2double *val_coords,
   const su2double t99 = t3 * u_0;
   const su2double t102 = t81 * t75;
   const su2double t105 = v_0 * x;
-  const su2double t113 = (0.4e1 * y * t102 * t105 - 0.8e1 * y * t65 * t105 - 0.4e1 * t6 * t75 * u_0
-                       +  0.4e1 * t102 * t99 - 0.8e1 * t65 * t99) * Viscosity;
+  const su2double t113 = (0.4e1 * y * t102 * t105 - 0.8e1 * y * t65 * t105 - 0.4e1 * t6 * t75 * u_0 +
+                          0.4e1 * t102 * t99 - 0.8e1 * t65 * t99) *
+                         Viscosity;
   const su2double t121 = u_0 * y;
   const su2double t131 = t2 * v_0;
-  const su2double t137 = (0.4e1 * x * t102 * t121 - 0.8e1 * x * t65 * t121 - 0.4e1 * t6 * t75 * v_0
-                       +  0.4e1 * t102 * t131 - 0.8e1 * t65 * t131) * Viscosity;
+  const su2double t137 = (0.4e1 * x * t102 * t121 - 0.8e1 * x * t65 * t121 - 0.4e1 * t6 * t75 * v_0 +
+                          0.4e1 * t102 * t131 - 0.8e1 * t65 * t131) *
+                         Viscosity;
   const su2double t138 = v_0 * v_0;
   const su2double t139 = t138 * rho_0;
   const su2double t141 = y * t26;
@@ -263,11 +250,12 @@ void CMMSNSTwoHalfCirclesSolution::GetMMSSourceTerm(const su2double *val_coords,
   const su2double t254 = t30 * t138;
   const su2double t261 = t248 * t246 * t34 / 0.4e1 + 0.8e1 * (t25 * t252 + t25 * t254) * rho_0 + t246 * t34 / 0.4e1;
   const su2double t262 = v_0 * t261;
-  const su2double t267 = -0.4e1 * t193 * t2 * TWall * t65 - 0.4e1 * t193 * TWall * t65 * t3 - 0.8e1 * t193 * t201
-                       + 0.64e2 / 0.3e1 * t8 * t12 * t22 * t76 - 0.4e1 * t9 * t213 + 0.4e1 * t13 * t213
-                       - 0.4e1 * t17 * t218 + 0.4e1 * t19 * t218 + 0.128e3 / 0.3e1 * t8 * t11 * Viscosity * t6 * t161 * t138
-                       + 0.64e2 / 0.3e1 * t231 * t230 * t173 * t172 - 0.32e2 / 0.3e1 * t237 * t236 * t82 * t76
-                       - 0.4e1 * t8 * t236 * t113 - 0.4e1 * t19 * t262 + 0.4e1 * t17 * t262;
+  const su2double t267 = -0.4e1 * t193 * t2 * TWall * t65 - 0.4e1 * t193 * TWall * t65 * t3 - 0.8e1 * t193 * t201 +
+                         0.64e2 / 0.3e1 * t8 * t12 * t22 * t76 - 0.4e1 * t9 * t213 + 0.4e1 * t13 * t213 -
+                         0.4e1 * t17 * t218 + 0.4e1 * t19 * t218 +
+                         0.128e3 / 0.3e1 * t8 * t11 * Viscosity * t6 * t161 * t138 +
+                         0.64e2 / 0.3e1 * t231 * t230 * t173 * t172 - 0.32e2 / 0.3e1 * t237 * t236 * t82 * t76 -
+                         0.4e1 * t8 * t236 * t113 - 0.4e1 * t19 * t262 + 0.4e1 * t17 * t262;
   const su2double t271 = u_0 * t261;
   const su2double t277 = Pi * Pi;
   const su2double t278 = t6 * t277;
@@ -283,37 +271,40 @@ void CMMSNSTwoHalfCirclesSolution::GetMMSSourceTerm(const su2double *val_coords,
   const su2double t321 = t65 * t172;
   const su2double t364 = t11 * t22;
   const su2double t367 = t11 * t138;
-  const su2double t391 = -0.4e1 * t8 * t230 * t137 + 0.4e1 * t9 * t271 - 0.4e1 * t13 * t271
-                        - 0.4e1 * t300 * (-t281 * y * t278 + t11 * a_T2 * y * t285 - Pi * t16 * t183
-                        - 0.2e1 * a_T2 * t51 * y * t292 - t151 / 0.2e1) * t11 * TWall * t16
-                        + 0.4e1 * t300 * t190 * t11 * TWall * t81 * t3 + 0.32e2 / 0.3e1 * t237 * t311 * t310
-                        - 0.64e2 / 0.3e1 * t317 * t316 * y * t168 - 0.64e2 / 0.3e1 * t231 * t316 * t321
-                        + 0.64e2 / 0.3e1 * y * t11 * t316 * t321 - 0.4e1 * t300 * x * (-t281 * x * t278
-                        + t11 * a_T2 * x * t285 - Pi * t7 * t183 - 0.2e1 * a_T2 * t51 * x * t292 - t53 / 0.2e1) * t201
-                        + 0.4e1 * t300 * t2 * t190 * t11 * TWall * t81 + 0.64e2 / 0.3e1 * t317 * u_0 * t70 * x * t66
-                        - 0.32e2 / 0.3e1 * x * t11 * t311 * t310 + 0.4e1 * t317 * u_0 * (t248 * t62 * t34 / 0.4e1
-                        + 0.16e2 * (-t9 * t252 - t9 * t254 + t27 * t364 + t27 * t367) * rho_0 + t64)
-                        + 0.4e1 * t317 * v_0 * (t248 * t158 * t34 / 0.4e1
-                        + 0.16e2 * (t141 * t364 + t141 * t367 - t17 * t252 - t17 * t254) * rho_0 + t160);
+  const su2double t391 =
+      -0.4e1 * t8 * t230 * t137 + 0.4e1 * t9 * t271 - 0.4e1 * t13 * t271 -
+      0.4e1 * t300 *
+          (-t281 * y * t278 + t11 * a_T2 * y * t285 - Pi * t16 * t183 - 0.2e1 * a_T2 * t51 * y * t292 - t151 / 0.2e1) *
+          t11 * TWall * t16 +
+      0.4e1 * t300 * t190 * t11 * TWall * t81 * t3 + 0.32e2 / 0.3e1 * t237 * t311 * t310 -
+      0.64e2 / 0.3e1 * t317 * t316 * y * t168 - 0.64e2 / 0.3e1 * t231 * t316 * t321 +
+      0.64e2 / 0.3e1 * y * t11 * t316 * t321 -
+      0.4e1 * t300 * x *
+          (-t281 * x * t278 + t11 * a_T2 * x * t285 - Pi * t7 * t183 - 0.2e1 * a_T2 * t51 * x * t292 - t53 / 0.2e1) *
+          t201 +
+      0.4e1 * t300 * t2 * t190 * t11 * TWall * t81 + 0.64e2 / 0.3e1 * t317 * u_0 * t70 * x * t66 -
+      0.32e2 / 0.3e1 * x * t11 * t311 * t310 +
+      0.4e1 * t317 * u_0 *
+          (t248 * t62 * t34 / 0.4e1 + 0.16e2 * (-t9 * t252 - t9 * t254 + t27 * t364 + t27 * t367) * rho_0 + t64) +
+      0.4e1 * t317 * v_0 *
+          (t248 * t158 * t34 / 0.4e1 + 0.16e2 * (t141 * t364 + t141 * t367 - t17 * t252 - t17 * t254) * rho_0 + t160);
 
   /*--- Set the source term, which is valid for both 2D and 3D cases.
         Note the scaling for the correct non-dimensionalization. ---*/
-  val_source[0]      = -0.4e1 * t13 * t1 + 0.4e1 * t9 * t1 + 0.4e1 * t17 * t15 - 0.4e1 * t19 * t15;
-  val_source[1]      = 0.32e2 * t27 * t11 * t23 - 0.32e2 * t9 * t30 * t23 + t64 + 0.16e2 / 0.3e1 * t70 * x * t66
-                     + 0.16e2 / 0.3e1 * t6 * u_0 * t76 - 0.8e1 / 0.3e1 * x * t82 * t76 + 0.32e2 * t16 * t87 * t86
-                     - 0.32e2 * t16 * t92 * t91 - t113;
-  val_source[2]      = 0.32e2 * t7 * t87 * t86 - 0.32e2 * t7 * t92 * t91 - t137 + 0.32e2 * t141 * t11 * t139
-                     - 0.32e2 * t17 * t30 * t139 + t160 + 0.32e2 / 0.3e1 * Viscosity * t6 * t161 * v_0
-                     - 0.16e2 / 0.3e1 * y * Viscosity * t168 + 0.16e2 / 0.3e1 * y * t173 * t172;
-  val_source[3]      = 0.0;
-  val_source[nDim+1] = t267 + t391;
-
-  val_source[0]      /= Density_Ref*Velocity_Ref;
-  val_source[1]      /= Pressure_Ref;
-  val_source[2]      /= Pressure_Ref;
-  val_source[nDim+1] /= Velocity_Ref*Pressure_Ref;
+  val_source[0] = -0.4e1 * t13 * t1 + 0.4e1 * t9 * t1 + 0.4e1 * t17 * t15 - 0.4e1 * t19 * t15;
+  val_source[1] = 0.32e2 * t27 * t11 * t23 - 0.32e2 * t9 * t30 * t23 + t64 + 0.16e2 / 0.3e1 * t70 * x * t66 +
+                  0.16e2 / 0.3e1 * t6 * u_0 * t76 - 0.8e1 / 0.3e1 * x * t82 * t76 + 0.32e2 * t16 * t87 * t86 -
+                  0.32e2 * t16 * t92 * t91 - t113;
+  val_source[2] = 0.32e2 * t7 * t87 * t86 - 0.32e2 * t7 * t92 * t91 - t137 + 0.32e2 * t141 * t11 * t139 -
+                  0.32e2 * t17 * t30 * t139 + t160 + 0.32e2 / 0.3e1 * Viscosity * t6 * t161 * v_0 -
+                  0.16e2 / 0.3e1 * y * Viscosity * t168 + 0.16e2 / 0.3e1 * y * t173 * t172;
+  val_source[3] = 0.0;
+  val_source[nDim + 1] = t267 + t391;
+
+  val_source[0] /= Density_Ref * Velocity_Ref;
+  val_source[1] /= Pressure_Ref;
+  val_source[2] /= Pressure_Ref;
+  val_source[nDim + 1] /= Velocity_Ref * Pressure_Ref;
 }
 
-bool CMMSNSTwoHalfCirclesSolution::IsManufacturedSolution(void) const {
-  return true;
-}
+bool CMMSNSTwoHalfCirclesSolution::IsManufacturedSolution(void) const { return true; }
diff --git a/Common/src/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.cpp b/Common/src/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.cpp
index c6e7a5f005a..b86cc10b24a 100644
--- a/Common/src/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.cpp
+++ b/Common/src/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.cpp
@@ -27,14 +27,11 @@
 
 #include "../../../include/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.hpp"
 
-CMMSNSTwoHalfSpheresSolution::CMMSNSTwoHalfSpheresSolution(void) : CVerificationSolution() { }
-
-CMMSNSTwoHalfSpheresSolution::CMMSNSTwoHalfSpheresSolution(unsigned short val_nDim,
-                                                           unsigned short val_nVar,
-                                                           unsigned short val_iMesh,
-                                                           CConfig*       config)
-  : CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
+CMMSNSTwoHalfSpheresSolution::CMMSNSTwoHalfSpheresSolution(void) : CVerificationSolution() {}
 
+CMMSNSTwoHalfSpheresSolution::CMMSNSTwoHalfSpheresSolution(unsigned short val_nDim, unsigned short val_nVar,
+                                                           unsigned short val_iMesh, CConfig* config)
+    : CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
   /*--- Write a message that the solution is initialized for the manufactured
    solution for the Navier-Stokes equations between two half spheres. ---*/
   if ((rank == MASTER_NODE) && (val_iMesh == MESH_0)) {
@@ -48,17 +45,17 @@ CMMSNSTwoHalfSpheresSolution::CMMSNSTwoHalfSpheresSolution(unsigned short val_nD
   /*--- Coefficients, needed to determine the solution. ---*/
   const su2double Prandtl = config->GetPrandtl_Lam();
 
-  RGas         = config->GetGas_Constant();
-  Gamma        = config->GetGamma();
-  Viscosity    = config->GetMu_Constant();
-  Conductivity = Viscosity*Gamma*RGas/(Prandtl*(Gamma-1.0));
+  RGas = config->GetGas_Constant();
+  Gamma = config->GetGamma();
+  Viscosity = config->GetMu_Constant();
+  Conductivity = Viscosity * Gamma * RGas / (Prandtl * (Gamma - 1.0));
 
   /*--- Initialize TWall to the default value of 300 K (in case the outer wall
         is not modelled as an isothermal wall) and try to retrieve the wall
         temperature from the boundary conditions. ---*/
   TWall = 300.0;
-  for(unsigned short iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-    if(config->GetMarker_All_KindBC(iMarker) == ISOTHERMAL) {
+  for (unsigned short iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
+    if (config->GetMarker_All_KindBC(iMarker) == ISOTHERMAL) {
       const string Marker_Tag = config->GetMarker_All_TagBound(iMarker);
       TWall = config->GetIsothermal_Temperature(Marker_Tag);
     }
@@ -66,108 +63,93 @@ CMMSNSTwoHalfSpheresSolution::CMMSNSTwoHalfSpheresSolution(unsigned short val_nD
 
   /*--- Get the reference values for pressure, density and velocity. ---*/
   Pressure_Ref = config->GetPressure_Ref();
-  Density_Ref  = config->GetDensity_Ref();
+  Density_Ref = config->GetDensity_Ref();
   Velocity_Ref = config->GetVelocity_Ref();
 
   /*--- The constants for the density and velocities. ---*/
-  rho_0 =   1.25;
-  u_0   = 135.78;
-  v_0   = -67.61;
-  w_0   =  82.75;
+  rho_0 = 1.25;
+  u_0 = 135.78;
+  v_0 = -67.61;
+  w_0 = 82.75;
 
   /*--- The constants for the temperature solution. ---*/
-  a_T1 =  1.05;
+  a_T1 = 1.05;
   a_T2 = -0.85;
 
   /*--- Perform some sanity and error checks for this solution here. ---*/
-  if(nDim != 3)
-    SU2_MPI::Error("Grid must be 3D for the MMS NS Two Half Spheres case",
-                   CURRENT_FUNCTION);
+  if (nDim != 3) SU2_MPI::Error("Grid must be 3D for the MMS NS Two Half Spheres case", CURRENT_FUNCTION);
 
-  if(config->GetTime_Marching() != TIME_MARCHING::STEADY)
-    SU2_MPI::Error("Steady mode must be selected for the MMS NS Two Half Spheres case",
-                   CURRENT_FUNCTION);
+  if (config->GetTime_Marching() != TIME_MARCHING::STEADY)
+    SU2_MPI::Error("Steady mode must be selected for the MMS NS Two Half Spheres case", CURRENT_FUNCTION);
 
-  if(Kind_Solver != MAIN_SOLVER::EULER && Kind_Solver != MAIN_SOLVER::NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::RANS &&
-     Kind_Solver != MAIN_SOLVER::FEM_EULER && Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::FEM_RANS &&
-     Kind_Solver != MAIN_SOLVER::FEM_LES)
+  if (Kind_Solver != MAIN_SOLVER::EULER && Kind_Solver != MAIN_SOLVER::NAVIER_STOKES &&
+      Kind_Solver != MAIN_SOLVER::RANS && Kind_Solver != MAIN_SOLVER::FEM_EULER &&
+      Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::FEM_RANS &&
+      Kind_Solver != MAIN_SOLVER::FEM_LES)
     SU2_MPI::Error("Compressible flow equations must be selected for the MMS NS Two Half Spheres case",
                    CURRENT_FUNCTION);
 
-  if((Kind_Solver != MAIN_SOLVER::NAVIER_STOKES) &&
-     (Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES))
-    SU2_MPI::Error("Navier Stokes equations must be selected for the MMS NS Two Half Spheres case",
-                   CURRENT_FUNCTION);
+  if ((Kind_Solver != MAIN_SOLVER::NAVIER_STOKES) && (Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES))
+    SU2_MPI::Error("Navier Stokes equations must be selected for the MMS NS Two Half Spheres case", CURRENT_FUNCTION);
 
-  if((config->GetKind_FluidModel() != STANDARD_AIR) &&
-     (config->GetKind_FluidModel() != IDEAL_GAS))
-    SU2_MPI::Error("Standard air or ideal gas must be selected for the MMS NS Two Half Spheres case",
-                   CURRENT_FUNCTION);
+  if ((config->GetKind_FluidModel() != STANDARD_AIR) && (config->GetKind_FluidModel() != IDEAL_GAS))
+    SU2_MPI::Error("Standard air or ideal gas must be selected for the MMS NS Two Half Spheres case", CURRENT_FUNCTION);
 
-  if(config->GetKind_ViscosityModel() != VISCOSITYMODEL::CONSTANT)
-    SU2_MPI::Error("Sutherland must be selected for viscosity for the MMS NS Two Half Spheres case",
-                   CURRENT_FUNCTION);
+  if (config->GetKind_ViscosityModel() != VISCOSITYMODEL::CONSTANT)
+    SU2_MPI::Error("Sutherland must be selected for viscosity for the MMS NS Two Half Spheres case", CURRENT_FUNCTION);
 
-  if(config->GetKind_ConductivityModel() != CONDUCTIVITYMODEL::CONSTANT_PRANDTL)
-    SU2_MPI::Error("Constant Prandtl number must be selected for the MMS NS Two Half Spheres case",
-                   CURRENT_FUNCTION);
+  if (config->GetKind_ConductivityModel() != CONDUCTIVITYMODEL::CONSTANT_PRANDTL)
+    SU2_MPI::Error("Constant Prandtl number must be selected for the MMS NS Two Half Spheres case", CURRENT_FUNCTION);
 }
 
-CMMSNSTwoHalfSpheresSolution::~CMMSNSTwoHalfSpheresSolution(void) { }
-
-void CMMSNSTwoHalfSpheresSolution::GetBCState(const su2double *val_coords,
-                                              const su2double val_t,
-                                              su2double       *val_solution) const {
+CMMSNSTwoHalfSpheresSolution::~CMMSNSTwoHalfSpheresSolution(void) {}
 
+void CMMSNSTwoHalfSpheresSolution::GetBCState(const su2double* val_coords, const su2double val_t,
+                                              su2double* val_solution) const {
   /*--- The exact solution is prescribed on the boundaries. ---*/
   GetSolution(val_coords, val_t, val_solution);
 }
 
-void CMMSNSTwoHalfSpheresSolution::GetSolution(const su2double *val_coords,
-                                               const su2double val_t,
-                                               su2double       *val_solution) const {
-
+void CMMSNSTwoHalfSpheresSolution::GetSolution(const su2double* val_coords, const su2double val_t,
+                                               su2double* val_solution) const {
   /* Easier storage of the x-, y- and z-coordinates. */
   const su2double x = val_coords[0];
   const su2double y = val_coords[1];
   const su2double z = val_coords[2];
 
   /* Determine the dimensional solution for the temperature. */
-  const su2double Pi   = PI_NUMBER;
-  const su2double r    = sqrt(x*x + y*y + z*z);
-  const su2double fact = (r-1.0)*(r-1.0)/(a_T1 + a_T2);
+  const su2double Pi = PI_NUMBER;
+  const su2double r = sqrt(x * x + y * y + z * z);
+  const su2double fact = (r - 1.0) * (r - 1.0) / (a_T1 + a_T2);
 
-  su2double T = 0.25*TWall*(3.0 + fact*(a_T1*cos(Pi*(r-2.0))
-              +                         a_T2*cos(Pi*(r-2.0)*2.0)));
+  su2double T = 0.25 * TWall * (3.0 + fact * (a_T1 * cos(Pi * (r - 2.0)) + a_T2 * cos(Pi * (r - 2.0) * 2.0)));
 
   /* Determine the dimensional solution for the velocities. */
-  su2double u = u_0*(r-1.0)*(2.0-r)*4.0;
-  su2double v = v_0*(r-1.0)*(2.0-r)*4.0;
-  su2double w = w_0*(r-1.0)*(2.0-r)*4.0;
+  su2double u = u_0 * (r - 1.0) * (2.0 - r) * 4.0;
+  su2double v = v_0 * (r - 1.0) * (2.0 - r) * 4.0;
+  su2double w = w_0 * (r - 1.0) * (2.0 - r) * 4.0;
 
   /* Compute the pressure from the density and temperature. */
   su2double rho = rho_0;
-  su2double p   = rho*RGas*T;
+  su2double p = rho * RGas * T;
 
   /* Determine the non-dimensional solution. */
   rho /= Density_Ref;
-  p   /= Pressure_Ref;
-  u   /= Velocity_Ref;
-  v   /= Velocity_Ref;
-  w   /= Velocity_Ref;
+  p /= Pressure_Ref;
+  u /= Velocity_Ref;
+  v /= Velocity_Ref;
+  w /= Velocity_Ref;
 
   /* Determine the non-dimensional conserved variables. */
   val_solution[0] = rho;
-  val_solution[1] = rho*u;
-  val_solution[2] = rho*v;
-  val_solution[3] = rho*w;
-  val_solution[4] = p/(Gamma-1.0) + 0.5*rho*(u*u + v*v + w*w);
+  val_solution[1] = rho * u;
+  val_solution[2] = rho * v;
+  val_solution[3] = rho * w;
+  val_solution[4] = p / (Gamma - 1.0) + 0.5 * rho * (u * u + v * v + w * w);
 }
 
-void CMMSNSTwoHalfSpheresSolution::GetMMSSourceTerm(const su2double *val_coords,
-                                                    const su2double val_t,
-                                                    su2double       *val_source) const {
-
+void CMMSNSTwoHalfSpheresSolution::GetMMSSourceTerm(const su2double* val_coords, const su2double val_t,
+                                                    su2double* val_source) const {
   /*--- Abbreviate Pi and the coordinates. ---*/
   const su2double Pi = PI_NUMBER;
   const su2double x = val_coords[0];
@@ -176,7 +158,7 @@ void CMMSNSTwoHalfSpheresSolution::GetMMSSourceTerm(const su2double *val_coords,
 
   /*--- The source code for the source terms is generated in Maple.
         See the file CMMSNSTwoHalfSpheresSolution.mw in the directory
-       	CreateMMSSourceTerms for the details how to do this. ---*/
+        CreateMMSSourceTerms for the details how to do this. ---*/
   const su2double t1 = rho_0 * u_0;
   const su2double t2 = x * x;
   const su2double t3 = y * y;
@@ -253,10 +235,11 @@ void CMMSNSTwoHalfSpheresSolution::GetMMSSourceTerm(const su2double *val_coords,
   const su2double t134 = t111 * t129;
   const su2double t135 = t89 * Viscosity;
   const su2double t136 = z * t135;
-  const su2double t139 = 0.32e2 * t34 * t12 * t30 - 0.32e2 * t10 * t37 * t30 + t71 + 0.16e2 / 0.3e1 * t78 * x * t73
-                       + 0.16e2 / 0.3e1 * t85 * t84 - 0.8e1 / 0.3e1 * x * t90 * t84 + 0.32e2 * t17 * t95 * t94
-                       - 0.32e2 * t17 * t100 * t99 + 0.8e1 * t108 * t104 + 0.16e2 * t85 * t112 - 0.8e1 * y * t115 * t112
-                       + 0.32e2 * t120 * t94 - 0.32e2 * t124 * t99 + 0.8e1 * t131 * t130 - 0.8e1 * t136 * t134;
+  const su2double t139 = 0.32e2 * t34 * t12 * t30 - 0.32e2 * t10 * t37 * t30 + t71 + 0.16e2 / 0.3e1 * t78 * x * t73 +
+                         0.16e2 / 0.3e1 * t85 * t84 - 0.8e1 / 0.3e1 * x * t90 * t84 + 0.32e2 * t17 * t95 * t94 -
+                         0.32e2 * t17 * t100 * t99 + 0.8e1 * t108 * t104 + 0.16e2 * t85 * t112 -
+                         0.8e1 * y * t115 * t112 + 0.32e2 * t120 * t94 - 0.32e2 * t124 * t99 + 0.8e1 * t131 * t130 -
+                         0.8e1 * t136 * t134;
   const su2double t146 = x * t72;
   const su2double t155 = v_0 * v_0;
   const su2double t156 = t155 * rho_0;
@@ -271,11 +254,11 @@ void CMMSNSTwoHalfSpheresSolution::GetMMSSourceTerm(const su2double *val_coords,
   const su2double t195 = v_0 * z + w_0 * y;
   const su2double t196 = t72 * t195;
   const su2double t199 = t111 * t195;
-  const su2double t202 = 0.32e2 * t8 * t95 * t94 - 0.32e2 * t8 * t100 * t99 + 0.8e1 * t108 * t146
-                       + 0.80e2 / 0.3e1 * t7 * v_0 * t112 - 0.8e1 * x * t115 * t112 + 0.32e2 * t158 * t12 * t156
-                       - 0.32e2 * t18 * t37 * t156 + t177 + 0.16e2 / 0.3e1 * y * t180 * t135
-                       - 0.16e2 / 0.3e1 * y * t179 * t73 + 0.32e2 * t120 * t187 - 0.32e2 * t124 * t190
-                       + 0.8e1 * t131 * t196 - 0.8e1 * t136 * t199;
+  const su2double t202 = 0.32e2 * t8 * t95 * t94 - 0.32e2 * t8 * t100 * t99 + 0.8e1 * t108 * t146 +
+                         0.80e2 / 0.3e1 * t7 * v_0 * t112 - 0.8e1 * x * t115 * t112 + 0.32e2 * t158 * t12 * t156 -
+                         0.32e2 * t18 * t37 * t156 + t177 + 0.16e2 / 0.3e1 * y * t180 * t135 -
+                         0.16e2 / 0.3e1 * y * t179 * t73 + 0.32e2 * t120 * t187 - 0.32e2 * t124 * t190 +
+                         0.8e1 * t131 * t196 - 0.8e1 * t136 * t199;
   const su2double t209 = t111 * w_0;
   const su2double t231 = w_0 * w_0;
   const su2double t232 = t231 * rho_0;
@@ -285,11 +268,11 @@ void CMMSNSTwoHalfSpheresSolution::GetMMSSourceTerm(const su2double *val_coords,
   const su2double t253 = t252 * t41;
   const su2double t255 = t74 + t76 - 0.2e1 * t77;
   const su2double t256 = t111 * t255;
-  const su2double t263 = 0.32e2 * t8 * t119 * t94 - 0.32e2 * t8 * t123 * t99 + 0.80e2 / 0.3e1 * t7 * Viscosity * t209
-                       + 0.8e1 * x * Viscosity * t130 - 0.8e1 * x * t135 * t134 + 0.32e2 * t17 * t119 * t187
-                       - 0.32e2 * t17 * t123 * t190 + 0.8e1 * y * Viscosity * t196 - 0.8e1 * y * t135 * t199
-                       + 0.32e2 * t234 * t12 * t232 - 0.32e2 * t24 * t37 * t232 + t253
-                       + 0.16e2 / 0.3e1 * z * t256 * t135 - 0.16e2 / 0.3e1 * z * t255 * t73;
+  const su2double t263 = 0.32e2 * t8 * t119 * t94 - 0.32e2 * t8 * t123 * t99 + 0.80e2 / 0.3e1 * t7 * Viscosity * t209 +
+                         0.8e1 * x * Viscosity * t130 - 0.8e1 * x * t135 * t134 + 0.32e2 * t17 * t119 * t187 -
+                         0.32e2 * t17 * t123 * t190 + 0.8e1 * y * Viscosity * t196 - 0.8e1 * y * t135 * t199 +
+                         0.32e2 * t234 * t12 * t232 - 0.32e2 * t24 * t37 * t232 + t253 +
+                         0.16e2 / 0.3e1 * z * t256 * t135 - 0.16e2 / 0.3e1 * z * t255 * t73;
   const su2double t265 = t12 * u_0;
   const su2double t266 = x * t9;
   const su2double t270 = t115 * t112;
@@ -308,11 +291,12 @@ void CMMSNSTwoHalfSpheresSolution::GetMMSSourceTerm(const su2double *val_coords,
   const su2double t316 = t305 * Viscosity * w_0;
   const su2double t319 = Viscosity * t134;
   const su2double t320 = w_0 * t72;
-  const su2double t329 = -0.32e2 / 0.3e1 * t266 * t265 * t90 * t84 - 0.32e2 * t266 * t271 * t270
-                       - 0.32e2 * t266 * t276 * t275 - 0.32e2 * t280 * t265 * t270 + 0.64e2 / 0.3e1 * t285 * t180 * t135
-                       - 0.32e2 * t280 * t276 * t288 - 0.32e2 * t292 * t265 * t275 - 0.32e2 * t292 * t271 * t288
-                       + 0.64e2 / 0.3e1 * t300 * t256 * t135 + 0.32e2 * t305 * v_0 * t107 * t303 + 0.32e2 * t266 * t310 * t309
-                       + 0.32e2 * t316 * x * t130 + 0.32e2 * t266 * t320 * t319 + 0.32e2 * t305 * u_0 * t107 * Viscosity * t104;
+  const su2double t329 =
+      -0.32e2 / 0.3e1 * t266 * t265 * t90 * t84 - 0.32e2 * t266 * t271 * t270 - 0.32e2 * t266 * t276 * t275 -
+      0.32e2 * t280 * t265 * t270 + 0.64e2 / 0.3e1 * t285 * t180 * t135 - 0.32e2 * t280 * t276 * t288 -
+      0.32e2 * t292 * t265 * t275 - 0.32e2 * t292 * t271 * t288 + 0.64e2 / 0.3e1 * t300 * t256 * t135 +
+      0.32e2 * t305 * v_0 * t107 * t303 + 0.32e2 * t266 * t310 * t309 + 0.32e2 * t316 * x * t130 +
+      0.32e2 * t266 * t320 * t319 + 0.32e2 * t305 * u_0 * t107 * Viscosity * t104;
   const su2double t330 = u_0 * t72;
   const su2double t334 = t179 * t73;
   const su2double t337 = v_0 * t111;
@@ -333,13 +317,14 @@ void CMMSNSTwoHalfSpheresSolution::GetMMSSourceTerm(const su2double *val_coords,
   const su2double t412 = t12 * t89 * t410;
   const su2double t421 = t78 * t84;
   const su2double t422 = x * t12;
-  const su2double t426 = 0.32e2 * t280 * t330 * t309 - 0.64e2 / 0.3e1 * t285 * t334 - 0.64e2 / 0.3e1 * t280 * t337 * t334
-                       + 0.32e2 * t316 * y * t196 + 0.32e2 * t280 * t320 * t344 + 0.32e2 * t305 * Viscosity * u_0 * z * t130
-                       + 0.32e2 * t292 * t330 * t319 + 0.32e2 * t305 * Viscosity * v_0 * z * t196 + 0.32e2 * t292 * t310 * t344
-                       - 0.64e2 / 0.3e1 * t300 * t364 - 0.64e2 / 0.3e1 * t292 * t209 * t364
-                       + 0.4e1 * t400 * TWall * x * t12 * t7 * (t377 * x * t371 - t12 * a_T2 * x * t381 + Pi * t8 * t385
-                       + 0.2e1 * a_T2 * t58 * x * t389 + t60 / 0.2e1) - 0.4e1 * t400 * t2 * TWall
-                       * t412 + 0.64e2 / 0.3e1 * t305 * u_0 * t78 * t303 - 0.32e2 / 0.3e1 * t422 * t330 * t421;
+  const su2double t426 =
+      0.32e2 * t280 * t330 * t309 - 0.64e2 / 0.3e1 * t285 * t334 - 0.64e2 / 0.3e1 * t280 * t337 * t334 +
+      0.32e2 * t316 * y * t196 + 0.32e2 * t280 * t320 * t344 + 0.32e2 * t305 * Viscosity * u_0 * z * t130 +
+      0.32e2 * t292 * t330 * t319 + 0.32e2 * t305 * Viscosity * v_0 * z * t196 + 0.32e2 * t292 * t310 * t344 -
+      0.64e2 / 0.3e1 * t300 * t364 - 0.64e2 / 0.3e1 * t292 * t209 * t364 +
+      0.4e1 * t400 * TWall * x * t12 * t7 *
+          (t377 * x * t371 - t12 * a_T2 * x * t381 + Pi * t8 * t385 + 0.2e1 * a_T2 * t58 * x * t389 + t60 / 0.2e1) -
+      0.4e1 * t400 * t2 * TWall * t412 + 0.64e2 / 0.3e1 * t305 * u_0 * t78 * t303 - 0.32e2 / 0.3e1 * t422 * t330 * t421;
   const su2double t457 = y * t12;
   const su2double t483 = t400 * TWall * t12;
   const su2double t486 = t410 * t4;
@@ -351,14 +336,18 @@ void CMMSNSTwoHalfSpheresSolution::GetMMSSourceTerm(const su2double *val_coords,
   const su2double t515 = t37 * t231;
   const su2double t521 = t508 * t506 * t41 + 0.8e1 * (t32 * t511 + t32 * t513 + t32 * t515) * rho_0 + t506 * t41;
   const su2double t522 = u_0 * t521;
-  const su2double t527 = -0.32e2 * t422 * t310 * t309 - 0.32e2 * t422 * t320 * t319
-                       + 0.4e1 * t400 * y * TWall * t12 * t7 * (t377 * y * t371 - t12 * a_T2 * y * t381 + Pi * t17 * t385
-                       + 0.2e1 * a_T2 * t58 * y * t389 + t168 / 0.2e1) - 0.4e1 * t400 * TWall * t3 * t412
-                       - 0.32e2 * t457 * t330 * t309 + 0.64e2 / 0.3e1 * t457 * t337 * t334 - 0.32e2 * t457 * t320 * t344
-                       + 0.4e1 * t483 * t7 * (t377 * z * t371 - t12 * a_T2 * z * t381 + Pi * t23 * t385
-                       + 0.2e1 * a_T2 * t58 * z * t389 + t244 / 0.2e1) * z - 0.4e1 * t483 * t89 * t486
-                       - 0.32e2 * t490 * t330 * t319 - 0.32e2 * t490 * t310 * t344 + 0.64e2 / 0.3e1 * t490 * t209 * t364
-                       + 0.32e2 / 0.3e1 * t266 * t330 * t421 + 0.4e1 * t10 * t522 - 0.4e1 * t14 * t522;
+  const su2double t527 =
+      -0.32e2 * t422 * t310 * t309 - 0.32e2 * t422 * t320 * t319 +
+      0.4e1 * t400 * y * TWall * t12 * t7 *
+          (t377 * y * t371 - t12 * a_T2 * y * t381 + Pi * t17 * t385 + 0.2e1 * a_T2 * t58 * y * t389 + t168 / 0.2e1) -
+      0.4e1 * t400 * TWall * t3 * t412 - 0.32e2 * t457 * t330 * t309 + 0.64e2 / 0.3e1 * t457 * t337 * t334 -
+      0.32e2 * t457 * t320 * t344 +
+      0.4e1 * t483 * t7 *
+          (t377 * z * t371 - t12 * a_T2 * z * t381 + Pi * t23 * t385 + 0.2e1 * a_T2 * t58 * z * t389 + t244 / 0.2e1) *
+          z -
+      0.4e1 * t483 * t89 * t486 - 0.32e2 * t490 * t330 * t319 - 0.32e2 * t490 * t310 * t344 +
+      0.64e2 / 0.3e1 * t490 * t209 * t364 + 0.32e2 / 0.3e1 * t266 * t330 * t421 + 0.4e1 * t10 * t522 -
+      0.4e1 * t14 * t522;
   const su2double t528 = v_0 * t521;
   const su2double t533 = w_0 * t521;
   const su2double t541 = Conductivity * t399 * TWall;
@@ -367,30 +356,35 @@ void CMMSNSTwoHalfSpheresSolution::GetMMSSourceTerm(const su2double *val_coords,
   const su2double t570 = t12 * t29;
   const su2double t573 = t12 * t155;
   const su2double t576 = t12 * t231;
-  const su2double t616 = 0.4e1 * t18 * t528 - 0.4e1 * t20 * t528 + 0.4e1 * t24 * t533 - 0.4e1 * t26 * t533
-                       + 0.12e2 * t541 * t12 * t7 * t410 + 0.320e3 / 0.3e1 * t545 * t155 * t112
-                       + 0.320e3 / 0.3e1 * t545 * Viscosity * t111 * t231 + 0.64e2 * t545 * t29 * t112
-                       + 0.64e2 / 0.3e1 * t545 * t29 * t84 + 0.4e1 * t541 * t2 * t558 + 0.4e1 * t541 * t3 * t558
-                       + 0.4e1 * t541 * t72 * t486 + 0.4e1 * t305 * u_0 * (t508 * t70 * t41
-                       + 0.16e2 * (-t10 * t511 - t10 * t513 - t10 * t515 + t34 * t570 + t34 * t573 + t34 * t576) * rho_0 + t71)
-                       + 0.4e1 * t305 * v_0 * (t508 * t176 * t41 + 0.16e2 * (t158 * t570 + t158 * t573 + t158 * t576
-                       - t18 * t511 - t18 * t513 - t18 * t515) * rho_0 + t177) + 0.4e1 * t305 * w_0 * (t508 * t252 * t41
-                       + 0.16e2 * (t234 * t570 + t234 * t573 + t234 * t576 - t24 * t511 - t24 * t513 - t24 * t515) * rho_0 + t253);
+  const su2double t616 =
+      0.4e1 * t18 * t528 - 0.4e1 * t20 * t528 + 0.4e1 * t24 * t533 - 0.4e1 * t26 * t533 +
+      0.12e2 * t541 * t12 * t7 * t410 + 0.320e3 / 0.3e1 * t545 * t155 * t112 +
+      0.320e3 / 0.3e1 * t545 * Viscosity * t111 * t231 + 0.64e2 * t545 * t29 * t112 +
+      0.64e2 / 0.3e1 * t545 * t29 * t84 + 0.4e1 * t541 * t2 * t558 + 0.4e1 * t541 * t3 * t558 +
+      0.4e1 * t541 * t72 * t486 +
+      0.4e1 * t305 * u_0 *
+          (t508 * t70 * t41 +
+           0.16e2 * (-t10 * t511 - t10 * t513 - t10 * t515 + t34 * t570 + t34 * t573 + t34 * t576) * rho_0 + t71) +
+      0.4e1 * t305 * v_0 *
+          (t508 * t176 * t41 +
+           0.16e2 * (t158 * t570 + t158 * t573 + t158 * t576 - t18 * t511 - t18 * t513 - t18 * t515) * rho_0 + t177) +
+      0.4e1 * t305 * w_0 *
+          (t508 * t252 * t41 +
+           0.16e2 * (t234 * t570 + t234 * t573 + t234 * t576 - t24 * t511 - t24 * t513 - t24 * t515) * rho_0 + t253);
 
   /*--- Set the source term. Note the scaling for the correct non-dimensionalization. ---*/
-  val_source[0] = 0.4e1 * t10 * t1 - 0.4e1 * t14 * t1 + 0.4e1 * t18 * t16 - 0.4e1 * t20 * t16 + 0.4e1 * t24 * t22 - 0.4e1 * t26 * t22;
+  val_source[0] = 0.4e1 * t10 * t1 - 0.4e1 * t14 * t1 + 0.4e1 * t18 * t16 - 0.4e1 * t20 * t16 + 0.4e1 * t24 * t22 -
+                  0.4e1 * t26 * t22;
   val_source[1] = t139;
   val_source[2] = t202;
   val_source[3] = t263;
   val_source[4] = t329 + t426 + t527 + t616;
 
-  val_source[0] /= Density_Ref*Velocity_Ref;
+  val_source[0] /= Density_Ref * Velocity_Ref;
   val_source[1] /= Pressure_Ref;
   val_source[2] /= Pressure_Ref;
   val_source[3] /= Pressure_Ref;
-  val_source[4] /= Velocity_Ref*Pressure_Ref;
+  val_source[4] /= Velocity_Ref * Pressure_Ref;
 }
 
-bool CMMSNSTwoHalfSpheresSolution::IsManufacturedSolution(void) const {
-  return true;
-}
+bool CMMSNSTwoHalfSpheresSolution::IsManufacturedSolution(void) const { return true; }
diff --git a/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolution.cpp b/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolution.cpp
index 8a8f537f546..39721dca2d1 100644
--- a/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolution.cpp
+++ b/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolution.cpp
@@ -27,14 +27,11 @@
 
 #include "../../../include/toolboxes/MMS/CMMSNSUnitQuadSolution.hpp"
 
-CMMSNSUnitQuadSolution::CMMSNSUnitQuadSolution(void) : CVerificationSolution() { }
-
-CMMSNSUnitQuadSolution::CMMSNSUnitQuadSolution(unsigned short val_nDim,
-                                               unsigned short val_nVar,
-                                               unsigned short val_iMesh,
-                                               CConfig*       config)
-  : CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
+CMMSNSUnitQuadSolution::CMMSNSUnitQuadSolution(void) : CVerificationSolution() {}
 
+CMMSNSUnitQuadSolution::CMMSNSUnitQuadSolution(unsigned short val_nDim, unsigned short val_nVar,
+                                               unsigned short val_iMesh, CConfig* config)
+    : CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
   /*--- Write a message that the solution is initialized for the manufactured
    solution for the Navier-Stokes equations on a unit quad. ---*/
   if ((rank == MASTER_NODE) && (val_iMesh == MESH_0)) {
@@ -48,132 +45,116 @@ CMMSNSUnitQuadSolution::CMMSNSUnitQuadSolution(unsigned short val_nDim,
   /*--- Coefficients, needed to determine the solution. ---*/
   const su2double Prandtl = config->GetPrandtl_Lam();
 
-  RGas         = config->GetGas_ConstantND();
-  Gamma        = config->GetGamma();
-  Viscosity    = config->GetMu_ConstantND();
-  Conductivity = Viscosity*Gamma*RGas/(Prandtl*(Gamma-1.0));
+  RGas = config->GetGas_ConstantND();
+  Gamma = config->GetGamma();
+  Viscosity = config->GetMu_ConstantND();
+  Conductivity = Viscosity * Gamma * RGas / (Prandtl * (Gamma - 1.0));
 
   /*--- Constants, which describe this manufactured solution. This is a viscous
         solution on the unit quad, where the primitive variables vary as a
         combination of sine and cosine functions. The unit quad is probably not
         necessary, and an arbitrary domain should work as well. ---*/
-  L       =      1.0;
-  a_Px    =      1.0;
-  a_Pxy   =      0.75;
-  a_Py    =      1.25;
-  a_rhox  =      0.75;
-  a_rhoxy =      1.25;
-  a_rhoy  =      1.0;
-  a_ux    =      1.6666666667;
-  a_uxy   =      0.6;
-  a_uy    =      1.5;
-  a_vx    =      1.5;
-  a_vxy   =      0.9;
-  a_vy    =      1.0;
-  P_0     = 100000.0;
-  P_x     = -30000.0;
-  P_xy    = -25000.0;
-  P_y     =  20000.0;
-  rho_0   =      1.0;
-  rho_x   =      0.1;
-  rho_xy  =      0.08;
-  rho_y   =      0.15;
-  u_0     =     70.0;
-  u_x     =      4.0;
-  u_xy    =      7.0;
-  u_y     =    -12.0;
-  v_0     =     90.0;
-  v_x     =    -20.0;
-  v_xy    =    -11.0;
-  v_y     =      4.0;
+  L = 1.0;
+  a_Px = 1.0;
+  a_Pxy = 0.75;
+  a_Py = 1.25;
+  a_rhox = 0.75;
+  a_rhoxy = 1.25;
+  a_rhoy = 1.0;
+  a_ux = 1.6666666667;
+  a_uxy = 0.6;
+  a_uy = 1.5;
+  a_vx = 1.5;
+  a_vxy = 0.9;
+  a_vy = 1.0;
+  P_0 = 100000.0;
+  P_x = -30000.0;
+  P_xy = -25000.0;
+  P_y = 20000.0;
+  rho_0 = 1.0;
+  rho_x = 0.1;
+  rho_xy = 0.08;
+  rho_y = 0.15;
+  u_0 = 70.0;
+  u_x = 4.0;
+  u_xy = 7.0;
+  u_y = -12.0;
+  v_0 = 90.0;
+  v_x = -20.0;
+  v_xy = -11.0;
+  v_y = 4.0;
 
   /*--- Perform some sanity and error checks for this solution here. ---*/
-  if(config->GetTime_Marching() != TIME_MARCHING::STEADY)
-    SU2_MPI::Error("Steady mode must be selected for the MMS NS Unit Quad case",
-                   CURRENT_FUNCTION);
+  if (config->GetTime_Marching() != TIME_MARCHING::STEADY)
+    SU2_MPI::Error("Steady mode must be selected for the MMS NS Unit Quad case", CURRENT_FUNCTION);
 
-  if(Kind_Solver != MAIN_SOLVER::EULER && Kind_Solver != MAIN_SOLVER::NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::RANS &&
-     Kind_Solver != MAIN_SOLVER::FEM_EULER && Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::FEM_RANS &&
-     Kind_Solver != MAIN_SOLVER::FEM_LES)    SU2_MPI::Error("Compressible flow equations must be selected for the MMS NS Unit Quad case",
-                   CURRENT_FUNCTION);
+  if (Kind_Solver != MAIN_SOLVER::EULER && Kind_Solver != MAIN_SOLVER::NAVIER_STOKES &&
+      Kind_Solver != MAIN_SOLVER::RANS && Kind_Solver != MAIN_SOLVER::FEM_EULER &&
+      Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::FEM_RANS &&
+      Kind_Solver != MAIN_SOLVER::FEM_LES)
+    SU2_MPI::Error("Compressible flow equations must be selected for the MMS NS Unit Quad case", CURRENT_FUNCTION);
 
-  if((Kind_Solver != MAIN_SOLVER::NAVIER_STOKES) &&
-     (Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES))
-    SU2_MPI::Error("Navier Stokes equations must be selected for the MMS NS Unit Quad case",
-                   CURRENT_FUNCTION);
+  if ((Kind_Solver != MAIN_SOLVER::NAVIER_STOKES) && (Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES))
+    SU2_MPI::Error("Navier Stokes equations must be selected for the MMS NS Unit Quad case", CURRENT_FUNCTION);
 
-  if((config->GetKind_FluidModel() != STANDARD_AIR) &&
-     (config->GetKind_FluidModel() != IDEAL_GAS))
-    SU2_MPI::Error("Standard air or ideal gas must be selected for the MMS NS Unit Quad case",
-                   CURRENT_FUNCTION);
+  if ((config->GetKind_FluidModel() != STANDARD_AIR) && (config->GetKind_FluidModel() != IDEAL_GAS))
+    SU2_MPI::Error("Standard air or ideal gas must be selected for the MMS NS Unit Quad case", CURRENT_FUNCTION);
 
-  if(config->GetKind_ViscosityModel() != VISCOSITYMODEL::CONSTANT)
-    SU2_MPI::Error("Constant viscosity must be selected for the MMS NS Unit Quad case",
-                   CURRENT_FUNCTION);
+  if (config->GetKind_ViscosityModel() != VISCOSITYMODEL::CONSTANT)
+    SU2_MPI::Error("Constant viscosity must be selected for the MMS NS Unit Quad case", CURRENT_FUNCTION);
 
-  if(config->GetKind_ConductivityModel() != CONDUCTIVITYMODEL::CONSTANT_PRANDTL)
-    SU2_MPI::Error("Constant Prandtl number must be selected for the MMS NS Unit Quad case",
-                   CURRENT_FUNCTION);
+  if (config->GetKind_ConductivityModel() != CONDUCTIVITYMODEL::CONSTANT_PRANDTL)
+    SU2_MPI::Error("Constant Prandtl number must be selected for the MMS NS Unit Quad case", CURRENT_FUNCTION);
 }
 
-CMMSNSUnitQuadSolution::~CMMSNSUnitQuadSolution(void) { }
-
-void CMMSNSUnitQuadSolution::GetBCState(const su2double *val_coords,
-                                        const su2double val_t,
-                                        su2double       *val_solution) const {
+CMMSNSUnitQuadSolution::~CMMSNSUnitQuadSolution(void) {}
 
+void CMMSNSUnitQuadSolution::GetBCState(const su2double* val_coords, const su2double val_t,
+                                        su2double* val_solution) const {
   /*--- The exact solution is prescribed on the boundaries. ---*/
   GetSolution(val_coords, val_t, val_solution);
 }
 
-void CMMSNSUnitQuadSolution::GetSolution(const su2double *val_coords,
-                                         const su2double val_t,
-                                         su2double       *val_solution) const {
-
+void CMMSNSUnitQuadSolution::GetSolution(const su2double* val_coords, const su2double val_t,
+                                         su2double* val_solution) const {
   /* Easier storage of the x- and y-coordinates. */
   const su2double x = val_coords[0];
   const su2double y = val_coords[1];
 
   /* Determine the solution for the density, velocity
      components and pressure. */
-  const su2double LInv    = 1.0/L;
-  const su2double PiLInv  = PI_NUMBER*LInv;
-  const su2double PiL2Inv = PiLInv*LInv;
+  const su2double LInv = 1.0 / L;
+  const su2double PiLInv = PI_NUMBER * LInv;
+  const su2double PiL2Inv = PiLInv * LInv;
 
-  const su2double rho = rho_0 + rho_x *sin(a_rhox *PiLInv*x)
-                      +         rho_y *cos(a_rhoy *PiLInv*y)
-                      +         rho_xy*cos(a_rhoxy*PiL2Inv*x*y);
+  const su2double rho = rho_0 + rho_x * sin(a_rhox * PiLInv * x) + rho_y * cos(a_rhoy * PiLInv * y) +
+                        rho_xy * cos(a_rhoxy * PiL2Inv * x * y);
 
-  const su2double u = u_0 + u_x *sin(a_ux *PiLInv*x)
-                    +       u_y *cos(a_uy *PiLInv*y)
-                    +       u_xy*cos(a_uxy*PiL2Inv*x*y);
+  const su2double u =
+      u_0 + u_x * sin(a_ux * PiLInv * x) + u_y * cos(a_uy * PiLInv * y) + u_xy * cos(a_uxy * PiL2Inv * x * y);
 
-  const su2double v = v_0 + v_x *cos(a_vx *PiLInv*x)
-                    +       v_y *sin(a_vy *PiLInv*y)
-                    +       v_xy*cos(a_vxy*PiL2Inv*x*y);
+  const su2double v =
+      v_0 + v_x * cos(a_vx * PiLInv * x) + v_y * sin(a_vy * PiLInv * y) + v_xy * cos(a_vxy * PiL2Inv * x * y);
 
-  const su2double p = P_0 + P_x *cos(a_Px *PiLInv*x)
-                    +       P_y *sin(a_Py *PiLInv*y)
-                    +       P_xy*sin(a_Pxy*PiL2Inv*x*y);
+  const su2double p =
+      P_0 + P_x * cos(a_Px * PiLInv * x) + P_y * sin(a_Py * PiLInv * y) + P_xy * sin(a_Pxy * PiL2Inv * x * y);
 
   /* Compute the conservative variables from the primitive ones.
      Note that the implementation below is valid for both 2D and 3D. */
-  val_solution[0]      = rho;
-  val_solution[1]      = rho*u;
-  val_solution[2]      = rho*v;
-  val_solution[3]      = 0.0;
-  val_solution[nDim+1] = p/(Gamma-1.0) + 0.5*rho*(u*u + v*v);
+  val_solution[0] = rho;
+  val_solution[1] = rho * u;
+  val_solution[2] = rho * v;
+  val_solution[3] = 0.0;
+  val_solution[nDim + 1] = p / (Gamma - 1.0) + 0.5 * rho * (u * u + v * v);
 }
 
-void CMMSNSUnitQuadSolution::GetMMSSourceTerm(const su2double *val_coords,
-                                              const su2double val_t,
-                                              su2double       *val_source) const {
-
+void CMMSNSUnitQuadSolution::GetMMSSourceTerm(const su2double* val_coords, const su2double val_t,
+                                              su2double* val_source) const {
   /*--- The source code for the source terms is generated in Maple.
         See the file CMMSNSUnitQuadSolution.mw in the directory
-       	CreateMMSSourceTerms for the details how to do this. ---*/
+        CreateMMSSourceTerms for the details how to do this. ---*/
   const su2double Pi = PI_NUMBER;
-  const su2double fourThird = 4.0/3.0;
+  const su2double fourThird = 4.0 / 3.0;
   const su2double x = val_coords[0];
   const su2double y = val_coords[1];
 
@@ -263,7 +244,8 @@ void CMMSNSUnitQuadSolution::GetMMSSourceTerm(const su2double *val_coords,
   const su2double t143 = -t138 * t3 * t137 - t53 * t16 * t52;
   const su2double t147 = a_uy * a_uy;
   const su2double t150 = x * x;
-  const su2double t161 = (-t13 * (u_xy * t34 * t150 * t111 + t31 * Pi * t147) * Pi - t13 * (t122 + t125) * Pi) * Viscosity;
+  const su2double t161 =
+      (-t13 * (u_xy * t34 * t150 * t111 + t31 * Pi * t147) * Pi - t13 * (t122 + t125) * Pi) * Viscosity;
   const su2double t165 = v_x * a_vx;
   const su2double t166 = sin(t66);
   const su2double t171 = -t85 * t14 * t84 - t166 * t3 * t165;
@@ -272,7 +254,8 @@ void CMMSNSUnitQuadSolution::GetMMSSourceTerm(const su2double *val_coords,
   const su2double t177 = a_uxy * t53;
   const su2double t178 = u_xy * t177;
   const su2double t182 = a_vx * a_vx;
-  const su2double t192 = (-t13 * (t176 + t178) * Pi - t13 * (v_xy * t75 * t112 * t118 + t68 * Pi * t182) * Pi) * Viscosity;
+  const su2double t192 =
+      (-t13 * (t176 + t178) * Pi - t13 * (v_xy * t75 * t112 * t118 + t68 * Pi * t182) * Pi) * Viscosity;
   const su2double t193 = t77 * t77;
   const su2double t200 = t28 * a_Py * Pi;
   const su2double t201 = cos(t200);
@@ -291,7 +274,7 @@ void CMMSNSUnitQuadSolution::GetMMSSourceTerm(const su2double *val_coords,
   const su2double t237 = sin(t105);
   const su2double t238 = t237 * P_xy;
   const su2double t239 = P_0 + t234 + t236 + t238;
-  const su2double t243 =  t221 * t239 + t223 * t46 / 0.2e1 + P_0 + t234 + t236 + t238;
+  const su2double t243 = t221 * t239 + t223 * t46 / 0.2e1 + P_0 + t234 + t236 + t238;
   const su2double t245 = a_Px * a_Px;
   const su2double t246 = Pi * t245;
   const su2double t248 = a_Pxy * a_Pxy;
@@ -323,7 +306,8 @@ void CMMSNSUnitQuadSolution::GetMMSSourceTerm(const su2double *val_coords,
   const su2double t330 = t7 * t7;
   const su2double t331 = rho_x * rho_x;
   const su2double t336 = rho_0 * rho_0;
-  const su2double t337 = 0.2e1 * rho_x * rho_0 * t38 + t319 * t318 + 0.2e1 * t44 * t321 + t325 * t324 + 0.2e1 * t42 * t327 - t331 * t330 + t331 + t336;
+  const su2double t337 = 0.2e1 * rho_x * rho_0 * t38 + t319 * t318 + 0.2e1 * t44 * t321 + t325 * t324 +
+                         0.2e1 * t42 * t327 - t331 * t330 + t331 + t336;
   const su2double t338 = 0.1e1 / t337;
   const su2double t340 = 0.1e1 / RGas;
   const su2double t341 = t340 * t13;
@@ -336,7 +320,8 @@ void CMMSNSUnitQuadSolution::GetMMSSourceTerm(const su2double *val_coords,
   const su2double t399 = t120 * t124;
   const su2double t402 = a_ux * u_x * t48;
   const su2double t404 = a_vy * v_y * t80;
-  const su2double t428 = (-t13 * (t137 * t138 * L + t174 * t177) * Pi - t13 * (t165 * t166 * L + v_xy * y * t124) * Pi) * Viscosity;
+  const su2double t428 =
+      (-t13 * (t137 * t138 * L + t174 * t177) * Pi - t13 * (t165 * t166 * L + v_xy * y * t124) * Pi) * Viscosity;
   const su2double t430 = t203 + t205;
   const su2double t442 = a_Py * a_Py;
   const su2double t446 = P_xy * t150 * t248;
@@ -348,36 +333,54 @@ void CMMSNSUnitQuadSolution::GetMMSSourceTerm(const su2double *val_coords,
   const su2double t475 = t474 * rho_y;
   const su2double t480 = P_xy * t59;
   const su2double t486 = t235 * t2;
-  const su2double t564 = t36 * ( t221 * t219 + t223 * t22 / 0.2e1 + (t171 * t77 + t56 * t36) * t46 - t101 + t108) + t56 * t243
-                       + Conductivity * t341 * t338 * (t44 * (t234 * t246 + t252 * t250) * rho_xy - t267 * a_rhoxy * t264
-                       - t19 * t219 * y * t10 - t277 * t112 * t273 - t106 * t7 * t2 * t4 * P_xy * rho_x * t260 + t288 * t250
-                       + (t42 * P_x * t233 * t2 * Pi * rho_y * t245 - t238 * t38 * t2 * Pi * t291
-                       + t107 * t104 * t296 * t1 + t311 * t234 * t2 * t246 - t308 * t306 * t291) * L) * Pi;
-  const su2double t565 = -0.2e1 * (t44 * t7 * t3 * rho_xy * rho_x * a_rhox + t42 * t7 * t3 * rho_y * rho_x * a_rhox
-                       + rho_x * rho_0 * t7 * t2 * t4 + t308 * a_rhox * t331 * t7 - t267 * t369 - t267 * t376) * Conductivity * t341 * t366
-                       * (t44 * t264 - t19 * t239 * y * t10 - t349 * t260 + (t311 * P_x * t99 * a_Px + t42 * t258 * a_Px * rho_y
-                       + t237 * t296 * t1 + t7 * t306 * t1) * L) * Pi - fourThird * t36 * t132 * t131
-                       - fourThird * t56 * t132 * (-t398 + t399 / 0.2e1 + (t402 - t404 / 0.2e1) * L) * Pi;
-  const su2double t566 = -t77 * t192 - t171 * t428 + t77 * ( t221 * t430 + t223 * t64 / 0.2e1 + (t143 * t36 + t88 * t77) * t46 + t203 + t205)
-                       + t88 * t243 - Conductivity * t340 * t338 * t13 * (t44 * (-t236 * Pi * t442 - t252 * t446) * rho_xy
-                       - t460 * a_rhoxy * t457 + t19 * t430 * x * t10 + t277 * t150 * t273 - t106 * t59 * t2 * t40 * P_xy * rho_y * t454
-                       - t288 * t446 + (-P_y * t38 * t486 * Pi * rho_x * t442 - t42 * P_y * t486 * Pi * rho_y * t442
-                       - P_y * t486 * Pi * rho_0 * t442 + t238 * t42 * t2 * Pi * t475 + t204 * t104 * t480 * t58
-                       + t42 * t3 * t306 * t475) * L) * Pi;
-  const su2double t567 = 0.2e1 * (-t44 * t59 * t3 * rho_xy * rho_y * a_rhoy
-                       - t60 * a_rhoy * t325 * t42 - t60 * a_rhoy * t327 - t460 * t369 - t460 * t376) * Conductivity * t340 * t366 * t13
-                       * (t44 * t457 + t19 * t239 * x * t10 + t349 * t454 + (P_y * t38 * t201 * a_Py * rho_x + t42 * t452 * a_Py * rho_y
-                       + t452 * a_Py * rho_0 + t237 * t480 * t58 + t59 * t306 * t58) * L) * Pi - t36 * t161
-                       - t143 * t428 + 0.2e1 / 0.3e1 * t77 * t132 * t215 + 0.2e1 / 0.3e1 * t88 * t132 * (-t398 + 0.2e1 * t399
-                       + (t402 - 0.2e1 * t404) * L) * Pi;
+  const su2double t564 =
+      t36 * (t221 * t219 + t223 * t22 / 0.2e1 + (t171 * t77 + t56 * t36) * t46 - t101 + t108) + t56 * t243 +
+      Conductivity * t341 * t338 *
+          (t44 * (t234 * t246 + t252 * t250) * rho_xy - t267 * a_rhoxy * t264 - t19 * t219 * y * t10 -
+           t277 * t112 * t273 - t106 * t7 * t2 * t4 * P_xy * rho_x * t260 + t288 * t250 +
+           (t42 * P_x * t233 * t2 * Pi * rho_y * t245 - t238 * t38 * t2 * Pi * t291 + t107 * t104 * t296 * t1 +
+            t311 * t234 * t2 * t246 - t308 * t306 * t291) *
+               L) *
+          Pi;
+  const su2double t565 =
+      -0.2e1 *
+          (t44 * t7 * t3 * rho_xy * rho_x * a_rhox + t42 * t7 * t3 * rho_y * rho_x * a_rhox +
+           rho_x * rho_0 * t7 * t2 * t4 + t308 * a_rhox * t331 * t7 - t267 * t369 - t267 * t376) *
+          Conductivity * t341 * t366 *
+          (t44 * t264 - t19 * t239 * y * t10 - t349 * t260 +
+           (t311 * P_x * t99 * a_Px + t42 * t258 * a_Px * rho_y + t237 * t296 * t1 + t7 * t306 * t1) * L) *
+          Pi -
+      fourThird * t36 * t132 * t131 - fourThird * t56 * t132 * (-t398 + t399 / 0.2e1 + (t402 - t404 / 0.2e1) * L) * Pi;
+  const su2double t566 =
+      -t77 * t192 - t171 * t428 +
+      t77 * (t221 * t430 + t223 * t64 / 0.2e1 + (t143 * t36 + t88 * t77) * t46 + t203 + t205) + t88 * t243 -
+      Conductivity * t340 * t338 * t13 *
+          (t44 * (-t236 * Pi * t442 - t252 * t446) * rho_xy - t460 * a_rhoxy * t457 + t19 * t430 * x * t10 +
+           t277 * t150 * t273 - t106 * t59 * t2 * t40 * P_xy * rho_y * t454 - t288 * t446 +
+           (-P_y * t38 * t486 * Pi * rho_x * t442 - t42 * P_y * t486 * Pi * rho_y * t442 -
+            P_y * t486 * Pi * rho_0 * t442 + t238 * t42 * t2 * Pi * t475 + t204 * t104 * t480 * t58 +
+            t42 * t3 * t306 * t475) *
+               L) *
+          Pi;
+  const su2double t567 = 0.2e1 *
+                             (-t44 * t59 * t3 * rho_xy * rho_y * a_rhoy - t60 * a_rhoy * t325 * t42 -
+                              t60 * a_rhoy * t327 - t460 * t369 - t460 * t376) *
+                             Conductivity * t340 * t366 * t13 *
+                             (t44 * t457 + t19 * t239 * x * t10 + t349 * t454 +
+                              (P_y * t38 * t201 * a_Py * rho_x + t42 * t452 * a_Py * rho_y + t452 * a_Py * rho_0 +
+                               t237 * t480 * t58 + t59 * t306 * t58) *
+                                  L) *
+                             Pi -
+                         t36 * t161 - t143 * t428 + 0.2e1 / 0.3e1 * t77 * t132 * t215 +
+                         0.2e1 / 0.3e1 * t88 * t132 * (-t398 + 0.2e1 * t399 + (t402 - 0.2e1 * t404) * L) * Pi;
 
-  val_source[0]      = t88 * t46 + t77 * t64 + t37 + t57;
-  val_source[1]      = t91 * t22 + 0.2e1 * t56 * t93 - t101 + t108 - fourThird * t132 * t131 + t77 * t36 * t64 + t77 * t143 * t46 + t88 * t93 - t161;
-  val_source[2]      = t77 * t37 + t77 * t57 + t171 * t93 - t192 + t193 * t64 + 0.2e1 * t88 * t77 * t46 + t203 + t205 + 0.2e1 / 0.3e1 * t132 * t215;
-  val_source[3]      = 0.0;
-  val_source[nDim+1] = t564 + t565 + t566 + t567;
+  val_source[0] = t88 * t46 + t77 * t64 + t37 + t57;
+  val_source[1] = t91 * t22 + 0.2e1 * t56 * t93 - t101 + t108 - fourThird * t132 * t131 + t77 * t36 * t64 +
+                  t77 * t143 * t46 + t88 * t93 - t161;
+  val_source[2] = t77 * t37 + t77 * t57 + t171 * t93 - t192 + t193 * t64 + 0.2e1 * t88 * t77 * t46 + t203 + t205 +
+                  0.2e1 / 0.3e1 * t132 * t215;
+  val_source[3] = 0.0;
+  val_source[nDim + 1] = t564 + t565 + t566 + t567;
 }
 
-bool CMMSNSUnitQuadSolution::IsManufacturedSolution(void) const {
-  return true;
-}
+bool CMMSNSUnitQuadSolution::IsManufacturedSolution(void) const { return true; }
diff --git a/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.cpp b/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.cpp
index 32fc77ebe74..8fb480d4e4c 100644
--- a/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.cpp
+++ b/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.cpp
@@ -27,14 +27,11 @@
 
 #include "../../../include/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.hpp"
 
-CMMSNSUnitQuadSolutionWallBC::CMMSNSUnitQuadSolutionWallBC(void) : CVerificationSolution() { }
-
-CMMSNSUnitQuadSolutionWallBC::CMMSNSUnitQuadSolutionWallBC(unsigned short val_nDim,
-                                                           unsigned short val_nVar,
-                                                           unsigned short val_iMesh,
-                                                           CConfig*       config)
-  : CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
+CMMSNSUnitQuadSolutionWallBC::CMMSNSUnitQuadSolutionWallBC(void) : CVerificationSolution() {}
 
+CMMSNSUnitQuadSolutionWallBC::CMMSNSUnitQuadSolutionWallBC(unsigned short val_nDim, unsigned short val_nVar,
+                                                           unsigned short val_iMesh, CConfig* config)
+    : CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
   /*--- Write a message that the solution is initialized for the manufactured
    solution for the Navier-Stokes equations on a unit quad with no-slip
    wall boundary conditions. ---*/
@@ -50,17 +47,17 @@ CMMSNSUnitQuadSolutionWallBC::CMMSNSUnitQuadSolutionWallBC(unsigned short val_nD
   /*--- Coefficients, needed to determine the solution. ---*/
   const su2double Prandtl = config->GetPrandtl_Lam();
 
-  RGas         = config->GetGas_Constant();
-  Gamma        = config->GetGamma();
-  Viscosity    = config->GetMu_Constant();
-  Conductivity = Viscosity*Gamma*RGas/(Prandtl*(Gamma-1.0));
+  RGas = config->GetGas_Constant();
+  Gamma = config->GetGamma();
+  Viscosity = config->GetMu_Constant();
+  Conductivity = Viscosity * Gamma * RGas / (Prandtl * (Gamma - 1.0));
 
   /*--- Initialize TWall to the default value of 300 K (in case the outer wall
         is not modelled as an isothermal wall) and try to retrieve the wall
         temperature from the boundary conditions. ---*/
   TWall = 300.0;
-  for(unsigned short iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-    if(config->GetMarker_All_KindBC(iMarker) == ISOTHERMAL) {
+  for (unsigned short iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
+    if (config->GetMarker_All_KindBC(iMarker) == ISOTHERMAL) {
       const string Marker_Tag = config->GetMarker_All_TagBound(iMarker);
       TWall = config->GetIsothermal_Temperature(Marker_Tag);
     }
@@ -68,105 +65,97 @@ CMMSNSUnitQuadSolutionWallBC::CMMSNSUnitQuadSolutionWallBC(unsigned short val_nD
 
   /*--- Get the reference values for pressure, density and velocity. ---*/
   Pressure_Ref = config->GetPressure_Ref();
-  Density_Ref  = config->GetDensity_Ref();
+  Density_Ref = config->GetDensity_Ref();
   Velocity_Ref = config->GetVelocity_Ref();
 
   /*--- The constants for the density and velocities. ---*/
-  rho_0 =   1.25;
-  u_0   = 135.78;
-  v_0   = -67.61;
+  rho_0 = 1.25;
+  u_0 = 135.78;
+  v_0 = -67.61;
 
   /*--- The constants for the temperature solution. ---*/
-  a_T1 =  1.05;
+  a_T1 = 1.05;
   a_T2 = -0.85;
 
   /*--- Perform some sanity and error checks for this solution here. ---*/
-  if(config->GetTime_Marching() != TIME_MARCHING::STEADY)
-    SU2_MPI::Error("Steady mode must be selected for the MMS NS Unit Quad case with wall BCs.",
-                   CURRENT_FUNCTION);
+  if (config->GetTime_Marching() != TIME_MARCHING::STEADY)
+    SU2_MPI::Error("Steady mode must be selected for the MMS NS Unit Quad case with wall BCs.", CURRENT_FUNCTION);
 
-  if(Kind_Solver != MAIN_SOLVER::EULER && Kind_Solver != MAIN_SOLVER::NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::RANS &&
-     Kind_Solver != MAIN_SOLVER::FEM_EULER && Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::FEM_RANS &&
-     Kind_Solver != MAIN_SOLVER::FEM_LES)
+  if (Kind_Solver != MAIN_SOLVER::EULER && Kind_Solver != MAIN_SOLVER::NAVIER_STOKES &&
+      Kind_Solver != MAIN_SOLVER::RANS && Kind_Solver != MAIN_SOLVER::FEM_EULER &&
+      Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::FEM_RANS &&
+      Kind_Solver != MAIN_SOLVER::FEM_LES)
     SU2_MPI::Error("Compressible flow equations must be selected for the MMS NS Unit Quad case with wall BCs.",
                    CURRENT_FUNCTION);
 
-  if((Kind_Solver != MAIN_SOLVER::NAVIER_STOKES) &&
-     (Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES))
+  if ((Kind_Solver != MAIN_SOLVER::NAVIER_STOKES) && (Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES))
     SU2_MPI::Error("Navier Stokes equations must be selected for the MMS NS Unit Quad case with wall BCs.",
                    CURRENT_FUNCTION);
 
-  if((config->GetKind_FluidModel() != STANDARD_AIR) &&
-     (config->GetKind_FluidModel() != IDEAL_GAS))
+  if ((config->GetKind_FluidModel() != STANDARD_AIR) && (config->GetKind_FluidModel() != IDEAL_GAS))
     SU2_MPI::Error("Standard air or ideal gas must be selected for the MMS NS Unit Quad case with wall BCs.",
                    CURRENT_FUNCTION);
 
-  if(config->GetKind_ViscosityModel() != VISCOSITYMODEL::CONSTANT)
+  if (config->GetKind_ViscosityModel() != VISCOSITYMODEL::CONSTANT)
     SU2_MPI::Error("Sutherland must be selected for viscosity for the MMS NS Unit Quad case with wall BCs.",
                    CURRENT_FUNCTION);
 
-  if(config->GetKind_ConductivityModel() != CONDUCTIVITYMODEL::CONSTANT_PRANDTL)
+  if (config->GetKind_ConductivityModel() != CONDUCTIVITYMODEL::CONSTANT_PRANDTL)
     SU2_MPI::Error("Constant Prandtl number must be selected for the MMS NS Unit Quad case with wall BCs.",
                    CURRENT_FUNCTION);
 }
 
-CMMSNSUnitQuadSolutionWallBC::~CMMSNSUnitQuadSolutionWallBC(void) { }
-
-void CMMSNSUnitQuadSolutionWallBC::GetBCState(const su2double *val_coords,
-                                              const su2double val_t,
-                                              su2double       *val_solution) const {
+CMMSNSUnitQuadSolutionWallBC::~CMMSNSUnitQuadSolutionWallBC(void) {}
 
+void CMMSNSUnitQuadSolutionWallBC::GetBCState(const su2double* val_coords, const su2double val_t,
+                                              su2double* val_solution) const {
   /*--- The exact solution is prescribed on the boundaries. ---*/
   GetSolution(val_coords, val_t, val_solution);
 }
 
-void CMMSNSUnitQuadSolutionWallBC::GetSolution(const su2double *val_coords,
-                                               const su2double val_t,
-                                               su2double       *val_solution) const {
+void CMMSNSUnitQuadSolutionWallBC::GetSolution(const su2double* val_coords, const su2double val_t,
+                                               su2double* val_solution) const {
   /* Easier storage of the y-coordinate. */
   const su2double y = val_coords[1];
 
   /* Determine the dimensional solution for the temperature. */
-  const su2double Pi   = PI_NUMBER;
-  const su2double fact = y*y/(a_T1 + a_T2);
+  const su2double Pi = PI_NUMBER;
+  const su2double fact = y * y / (a_T1 + a_T2);
 
-  su2double T = 0.25*TWall*(3.0 + fact*(a_T1*cos(Pi*(y-1.0))
-              +                         a_T2*cos(Pi*(y-1.0)*2.0)));
+  su2double T = 0.25 * TWall * (3.0 + fact * (a_T1 * cos(Pi * (y - 1.0)) + a_T2 * cos(Pi * (y - 1.0) * 2.0)));
 
   /* Determine the dimensional solution for the velocities. */
-  su2double u = u_0*y*(1.0-y)*4.0;
-  su2double v = v_0*y*(1.0-y)*4.0;
+  su2double u = u_0 * y * (1.0 - y) * 4.0;
+  su2double v = v_0 * y * (1.0 - y) * 4.0;
 
   /* Compute the pressure from the density and temperature. */
   su2double rho = rho_0;
-  su2double p   = rho*RGas*T;
+  su2double p = rho * RGas * T;
 
   /* Determine the non-dimensional solution. */
   rho /= Density_Ref;
-  p   /= Pressure_Ref;
-  u   /= Velocity_Ref;
-  v   /= Velocity_Ref;
+  p /= Pressure_Ref;
+  u /= Velocity_Ref;
+  v /= Velocity_Ref;
 
   /* Compute the conservative variables from the primitive ones.
      Note that the implementation below is valid for both 2D and 3D. */
-  val_solution[0]      = rho;
-  val_solution[1]      = rho*u;
-  val_solution[2]      = rho*v;
-  val_solution[3]      = 0.0;
-  val_solution[nDim+1] = p/(Gamma-1.0) + 0.5*rho*(u*u + v*v);
+  val_solution[0] = rho;
+  val_solution[1] = rho * u;
+  val_solution[2] = rho * v;
+  val_solution[3] = 0.0;
+  val_solution[nDim + 1] = p / (Gamma - 1.0) + 0.5 * rho * (u * u + v * v);
 }
 
-void CMMSNSUnitQuadSolutionWallBC::GetMMSSourceTerm(const su2double *val_coords,
-                                                    const su2double val_t,
-                                                    su2double       *val_source) const {
-
+void CMMSNSUnitQuadSolutionWallBC::GetMMSSourceTerm(const su2double* val_coords, const su2double val_t,
+                                                    su2double* val_source) const {
   /*--- Abbreviate Pi and the y-coordinate. ---*/
   const su2double Pi = PI_NUMBER;
   const su2double y = val_coords[1];
 
   /*--- The source code for the source terms is generated in Maple.
         See the file CMMSNSUnitQuadSolutionWallBC.mw in the directory
-       	CreateMMSSourceTerms for the details how to do this. ---*/
+        CreateMMSSourceTerms for the details how to do this. ---*/
   const su2double t1 = (v_0 * rho_0);
   const su2double t2 = 1.0 - y;
   const su2double t6 = rho_0 * u_0;
@@ -210,27 +199,31 @@ void CMMSNSUnitQuadSolutionWallBC::GetMMSSourceTerm(const su2double *val_coords,
   const su2double t118 = a_T2 * y;
   const su2double t138 = Viscosity * (-8.0 * y + 4.0);
   const su2double t149 = Viscosity * (2.0 * y - 1.0);
-  const su2double t155 = 0.4e1 * t75 * v_0 * (t57 * t50 * t26 / 0.4e1 + (16.0 * (-t2 * t64 - t2 * t68 + t7 * t62 + t7 * t66) * rho_0) + t52)
-                       + 0.4e1 * t2 * t92 - 0.4e1 * y * t92 - Conductivity * t111 * (-t102 * Pi * t41 - 0.4e1 * y * t43 * t97 + 0.4e1 * t104 * a_T2
-                       - 0.2e1 * a_T2 + 0.2e1 * t32) * TWall - Conductivity * t111 * (-t102 * t31 * t115 - 0.4e1 * t118 * t115 * t104
-                       + 0.4e1 * t118 * t116 * t115 - 0.12e2 * t43 * t97 - 0.3e1 * t42) * TWall * y + (32.0 * t75 * t61 * Viscosity)
-                       - (4.0 * t2 * t61 * t138) + (4.0 * t62 * t138) + 0.128e3 / 0.3e1 * t75 * t20 * Viscosity + 0.64e2 / 0.3e1 * t2 * t20 * t149
-                       - 0.64e2 / 0.3e1 * t66 * t149;
+  const su2double t155 =
+      0.4e1 * t75 * v_0 *
+          (t57 * t50 * t26 / 0.4e1 + (16.0 * (-t2 * t64 - t2 * t68 + t7 * t62 + t7 * t66) * rho_0) + t52) +
+      0.4e1 * t2 * t92 - 0.4e1 * y * t92 -
+      Conductivity * t111 *
+          (-t102 * Pi * t41 - 0.4e1 * y * t43 * t97 + 0.4e1 * t104 * a_T2 - 0.2e1 * a_T2 + 0.2e1 * t32) * TWall -
+      Conductivity * t111 *
+          (-t102 * t31 * t115 - 0.4e1 * t118 * t115 * t104 + 0.4e1 * t118 * t116 * t115 - 0.12e2 * t43 * t97 -
+           0.3e1 * t42) *
+          TWall * y +
+      (32.0 * t75 * t61 * Viscosity) - (4.0 * t2 * t61 * t138) + (4.0 * t62 * t138) +
+      0.128e3 / 0.3e1 * t75 * t20 * Viscosity + 0.64e2 / 0.3e1 * t2 * t20 * t149 - 0.64e2 / 0.3e1 * t66 * t149;
 
   /*--- Set the source term, which is valid for both 2D and 3D cases.
         Note the scaling for the correct non-dimensionalization. ---*/
-  val_source[0]      = 4.0 * t2 * t1 - 4.0 * y * t1;
-  val_source[1]      = (-0.32e2 * v_0 * t13 * t6 + 0.32e2 * v_0 * t8 * t6 + (8.0 * Viscosity * u_0));
-  val_source[2]      = ((32.0 * t8 * t21) - (32.0 * t13 * t21) + t52 + 0.32e2 / 0.3e1 * Viscosity * v_0);
-  val_source[3]      = 0.0;
-  val_source[nDim+1] = t155;
-
-  val_source[0]      /= Density_Ref*Velocity_Ref;
-  val_source[1]      /= Pressure_Ref;
-  val_source[2]      /= Pressure_Ref;
-  val_source[nDim+1] /= Velocity_Ref*Pressure_Ref;
+  val_source[0] = 4.0 * t2 * t1 - 4.0 * y * t1;
+  val_source[1] = (-0.32e2 * v_0 * t13 * t6 + 0.32e2 * v_0 * t8 * t6 + (8.0 * Viscosity * u_0));
+  val_source[2] = ((32.0 * t8 * t21) - (32.0 * t13 * t21) + t52 + 0.32e2 / 0.3e1 * Viscosity * v_0);
+  val_source[3] = 0.0;
+  val_source[nDim + 1] = t155;
+
+  val_source[0] /= Density_Ref * Velocity_Ref;
+  val_source[1] /= Pressure_Ref;
+  val_source[2] /= Pressure_Ref;
+  val_source[nDim + 1] /= Velocity_Ref * Pressure_Ref;
 }
 
-bool CMMSNSUnitQuadSolutionWallBC::IsManufacturedSolution(void) const {
-  return true;
-}
+bool CMMSNSUnitQuadSolutionWallBC::IsManufacturedSolution(void) const { return true; }
diff --git a/Common/src/toolboxes/MMS/CNSUnitQuadSolution.cpp b/Common/src/toolboxes/MMS/CNSUnitQuadSolution.cpp
index f3b9519e379..b98995b1d50 100644
--- a/Common/src/toolboxes/MMS/CNSUnitQuadSolution.cpp
+++ b/Common/src/toolboxes/MMS/CNSUnitQuadSolution.cpp
@@ -27,14 +27,11 @@
 
 #include "../../../include/toolboxes/MMS/CNSUnitQuadSolution.hpp"
 
-CNSUnitQuadSolution::CNSUnitQuadSolution(void) : CVerificationSolution() { }
-
-CNSUnitQuadSolution::CNSUnitQuadSolution(unsigned short val_nDim,
-                                         unsigned short val_nVar,
-                                         unsigned short val_iMesh,
-                                         CConfig*       config)
-  : CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
+CNSUnitQuadSolution::CNSUnitQuadSolution(void) : CVerificationSolution() {}
 
+CNSUnitQuadSolution::CNSUnitQuadSolution(unsigned short val_nDim, unsigned short val_nVar, unsigned short val_iMesh,
+                                         CConfig* config)
+    : CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
   /*--- Write a message that the solution is initialized for the
    Navier-Stokes case on a unit quad. Note that heat conduction
    is neglected for this case. ---*/
@@ -49,75 +46,61 @@ CNSUnitQuadSolution::CNSUnitQuadSolution(unsigned short val_nDim,
   }
 
   /*--- Coefficients, needed to determine the solution. ---*/
-  Gm1       = config->GetGamma() - 1.0;
-  flowAngle = config->GetAoA()*PI_NUMBER/180.0;
+  Gm1 = config->GetGamma() - 1.0;
+  flowAngle = config->GetAoA() * PI_NUMBER / 180.0;
   Viscosity = config->GetMu_ConstantND();
 
   /*--- Perform some sanity and error checks for this solution here. ---*/
-  if(config->GetTime_Marching() != TIME_MARCHING::STEADY)
-    SU2_MPI::Error("Steady mode must be selected for the NS Unit Quad case",
-                   CURRENT_FUNCTION);
-
-  if(Kind_Solver != MAIN_SOLVER::EULER && Kind_Solver != MAIN_SOLVER::NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::RANS &&
-     Kind_Solver != MAIN_SOLVER::FEM_EULER && Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::FEM_RANS &&
-     Kind_Solver != MAIN_SOLVER::FEM_LES)
-    SU2_MPI::Error("Compressible flow equations must be selected for the NS Unit Quad case",
-                   CURRENT_FUNCTION);
-
-  if((Kind_Solver != MAIN_SOLVER::NAVIER_STOKES) &&
-     (Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES))
-    SU2_MPI::Error("Navier Stokes equations must be selected for the NS Unit Quad case",
-                   CURRENT_FUNCTION);
-
-  if(config->GetKind_FluidModel() != IDEAL_GAS)
-    SU2_MPI::Error("Ideal gas must be selected for the NS Unit Quad case",
-                   CURRENT_FUNCTION);
-
-  if(fabs(Gm1-0.5) > 1.e-8)
-    SU2_MPI::Error("Gamma must be 1.5 for the NS Unit Quad case",
-                   CURRENT_FUNCTION);
-
-  if(config->GetKind_ViscosityModel() != VISCOSITYMODEL::CONSTANT)
-    SU2_MPI::Error("Constant viscosity must be selected for the NS Unit Quad case",
-                   CURRENT_FUNCTION);
-
-  if(config->GetKind_ConductivityModel() != CONDUCTIVITYMODEL::CONSTANT_PRANDTL)
-    SU2_MPI::Error("Constant Prandtl number must be selected for the NS Unit Quad case",
-                   CURRENT_FUNCTION);
-
-  if(config->GetPrandtl_Lam() < 1.e+20)
-     SU2_MPI::Error("Laminar Prandtl number must be larger than 1.e+20 for the NS Unit Quad case",
-                   CURRENT_FUNCTION);
-}
+  if (config->GetTime_Marching() != TIME_MARCHING::STEADY)
+    SU2_MPI::Error("Steady mode must be selected for the NS Unit Quad case", CURRENT_FUNCTION);
+
+  if (Kind_Solver != MAIN_SOLVER::EULER && Kind_Solver != MAIN_SOLVER::NAVIER_STOKES &&
+      Kind_Solver != MAIN_SOLVER::RANS && Kind_Solver != MAIN_SOLVER::FEM_EULER &&
+      Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::FEM_RANS &&
+      Kind_Solver != MAIN_SOLVER::FEM_LES)
+    SU2_MPI::Error("Compressible flow equations must be selected for the NS Unit Quad case", CURRENT_FUNCTION);
+
+  if ((Kind_Solver != MAIN_SOLVER::NAVIER_STOKES) && (Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES))
+    SU2_MPI::Error("Navier Stokes equations must be selected for the NS Unit Quad case", CURRENT_FUNCTION);
+
+  if (config->GetKind_FluidModel() != IDEAL_GAS)
+    SU2_MPI::Error("Ideal gas must be selected for the NS Unit Quad case", CURRENT_FUNCTION);
 
-CNSUnitQuadSolution::~CNSUnitQuadSolution(void) { }
+  if (fabs(Gm1 - 0.5) > 1.e-8) SU2_MPI::Error("Gamma must be 1.5 for the NS Unit Quad case", CURRENT_FUNCTION);
 
-void CNSUnitQuadSolution::GetBCState(const su2double *val_coords,
-                                     const su2double val_t,
-                                     su2double       *val_solution) const {
+  if (config->GetKind_ViscosityModel() != VISCOSITYMODEL::CONSTANT)
+    SU2_MPI::Error("Constant viscosity must be selected for the NS Unit Quad case", CURRENT_FUNCTION);
 
+  if (config->GetKind_ConductivityModel() != CONDUCTIVITYMODEL::CONSTANT_PRANDTL)
+    SU2_MPI::Error("Constant Prandtl number must be selected for the NS Unit Quad case", CURRENT_FUNCTION);
+
+  if (config->GetPrandtl_Lam() < 1.e+20)
+    SU2_MPI::Error("Laminar Prandtl number must be larger than 1.e+20 for the NS Unit Quad case", CURRENT_FUNCTION);
+}
+
+CNSUnitQuadSolution::~CNSUnitQuadSolution(void) {}
+
+void CNSUnitQuadSolution::GetBCState(const su2double* val_coords, const su2double val_t,
+                                     su2double* val_solution) const {
   /*--- The exact solution is prescribed on the boundaries. ---*/
   GetSolution(val_coords, val_t, val_solution);
 }
 
-void CNSUnitQuadSolution::GetSolution(const su2double *val_coords,
-                                      const su2double val_t,
-                                      su2double       *val_solution) const {
-
+void CNSUnitQuadSolution::GetSolution(const su2double* val_coords, const su2double val_t,
+                                      su2double* val_solution) const {
   /*--- Compute the flow direction and the coordinates in
         the rotated frame. ---*/
   const su2double cosFlowAngle = cos(flowAngle);
   const su2double sinFlowAngle = sin(flowAngle);
 
-  const su2double xTilde = val_coords[0]*cosFlowAngle - val_coords[1]*sinFlowAngle;
-  const su2double yTilde = val_coords[0]*sinFlowAngle + val_coords[1]*cosFlowAngle;
+  const su2double xTilde = val_coords[0] * cosFlowAngle - val_coords[1] * sinFlowAngle;
+  const su2double yTilde = val_coords[0] * sinFlowAngle + val_coords[1] * cosFlowAngle;
 
   /*--- Compute the exact solution for this case. Note that it works
         both in 2D and 3D. ---*/
-  val_solution[0]      =  1.0;
-  val_solution[1]      =  cosFlowAngle*yTilde*yTilde;
-  val_solution[2]      = -sinFlowAngle*yTilde*yTilde;
-  val_solution[3]      =  0.0;
-  val_solution[nVar-1] =  (2.0*Viscosity*xTilde + 10.0)/Gm1
-                       +  0.5*yTilde*yTilde*yTilde*yTilde;
+  val_solution[0] = 1.0;
+  val_solution[1] = cosFlowAngle * yTilde * yTilde;
+  val_solution[2] = -sinFlowAngle * yTilde * yTilde;
+  val_solution[3] = 0.0;
+  val_solution[nVar - 1] = (2.0 * Viscosity * xTilde + 10.0) / Gm1 + 0.5 * yTilde * yTilde * yTilde * yTilde;
 }
diff --git a/Common/src/toolboxes/MMS/CRinglebSolution.cpp b/Common/src/toolboxes/MMS/CRinglebSolution.cpp
index 09012fbc4cb..ed2870662fd 100644
--- a/Common/src/toolboxes/MMS/CRinglebSolution.cpp
+++ b/Common/src/toolboxes/MMS/CRinglebSolution.cpp
@@ -27,14 +27,11 @@
 
 #include "../../../include/toolboxes/MMS/CRinglebSolution.hpp"
 
-CRinglebSolution::CRinglebSolution(void) : CVerificationSolution() { }
-
-CRinglebSolution::CRinglebSolution(unsigned short val_nDim,
-                                   unsigned short val_nVar,
-                                   unsigned short val_iMesh,
-                                   CConfig*       config)
-  : CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
+CRinglebSolution::CRinglebSolution(void) : CVerificationSolution() {}
 
+CRinglebSolution::CRinglebSolution(unsigned short val_nDim, unsigned short val_nVar, unsigned short val_iMesh,
+                                   CConfig* config)
+    : CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
   /*--- Write a message that the solution is initialized for the
    Ringleb test case. ---*/
   if ((rank == MASTER_NODE) && (val_iMesh == MESH_0)) {
@@ -45,39 +42,31 @@ CRinglebSolution::CRinglebSolution(unsigned short val_nDim,
   }
 
   /*--- Useful coefficients in which Gamma is present. ---*/
-  Gamma     = config->GetGamma();
-  Gm1       = Gamma - 1.0;
-  tovGm1    = 2.0/Gm1;
-  tGamOvGm1 = Gamma*tovGm1;
+  Gamma = config->GetGamma();
+  Gm1 = Gamma - 1.0;
+  tovGm1 = 2.0 / Gm1;
+  tGamOvGm1 = Gamma * tovGm1;
 
   /*--- Perform some sanity and error checks for this solution here. ---*/
-  if(config->GetTime_Marching() != TIME_MARCHING::STEADY)
-    SU2_MPI::Error("Steady mode must be selected for the Ringleb case",
-                   CURRENT_FUNCTION);
-
-  if(Kind_Solver != MAIN_SOLVER::EULER && Kind_Solver != MAIN_SOLVER::NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::RANS &&
-     Kind_Solver != MAIN_SOLVER::FEM_EULER && Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::FEM_RANS &&
-     Kind_Solver != MAIN_SOLVER::FEM_LES)
-    SU2_MPI::Error("Compressible flow equations must be selected for the Ringleb case",
-                   CURRENT_FUNCTION);
-
-  if((Kind_Solver != MAIN_SOLVER::EULER) &&
-     (Kind_Solver != MAIN_SOLVER::FEM_EULER))
-    SU2_MPI::Error("Euler equations must be selected for the Ringleb case",
-                   CURRENT_FUNCTION);
-
-  if((config->GetKind_FluidModel() != STANDARD_AIR) &&
-     (config->GetKind_FluidModel() != IDEAL_GAS))
-    SU2_MPI::Error("Standard air or ideal gas must be selected for the Ringleb case",
-                   CURRENT_FUNCTION);
-}
+  if (config->GetTime_Marching() != TIME_MARCHING::STEADY)
+    SU2_MPI::Error("Steady mode must be selected for the Ringleb case", CURRENT_FUNCTION);
+
+  if (Kind_Solver != MAIN_SOLVER::EULER && Kind_Solver != MAIN_SOLVER::NAVIER_STOKES &&
+      Kind_Solver != MAIN_SOLVER::RANS && Kind_Solver != MAIN_SOLVER::FEM_EULER &&
+      Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::FEM_RANS &&
+      Kind_Solver != MAIN_SOLVER::FEM_LES)
+    SU2_MPI::Error("Compressible flow equations must be selected for the Ringleb case", CURRENT_FUNCTION);
+
+  if ((Kind_Solver != MAIN_SOLVER::EULER) && (Kind_Solver != MAIN_SOLVER::FEM_EULER))
+    SU2_MPI::Error("Euler equations must be selected for the Ringleb case", CURRENT_FUNCTION);
 
-CRinglebSolution::~CRinglebSolution(void) { }
+  if ((config->GetKind_FluidModel() != STANDARD_AIR) && (config->GetKind_FluidModel() != IDEAL_GAS))
+    SU2_MPI::Error("Standard air or ideal gas must be selected for the Ringleb case", CURRENT_FUNCTION);
+}
 
-void CRinglebSolution::GetBCState(const su2double *val_coords,
-                                  const su2double val_t,
-                                  su2double       *val_solution) const {
+CRinglebSolution::~CRinglebSolution(void) {}
 
+void CRinglebSolution::GetBCState(const su2double* val_coords, const su2double val_t, su2double* val_solution) const {
   /*--- The exact solution is prescribed on the boundaries for the
         Ringleb flow. Note that a (much) more difficult test case is to
         use inviscid wall boundary conditions for the inner and outer
@@ -85,13 +74,10 @@ void CRinglebSolution::GetBCState(const su2double *val_coords,
   GetSolution(val_coords, val_t, val_solution);
 }
 
-void CRinglebSolution::GetSolution(const su2double *val_coords,
-                                   const su2double val_t,
-                                   su2double       *val_solution) const {
-
+void CRinglebSolution::GetSolution(const su2double* val_coords, const su2double val_t, su2double* val_solution) const {
   /* Easier storage of the coordinates and abbreviate y*y. */
-  const su2double x  = val_coords[0], y = val_coords[1];
-  const su2double y2 = y*y;
+  const su2double x = val_coords[0], y = val_coords[1];
+  const su2double y2 = y * y;
 
   /* Initial guess for q (velocity magnitude) and k (streamline parameter). */
   su2double k = 1.2;
@@ -102,85 +88,85 @@ void CRinglebSolution::GetSolution(const su2double *val_coords,
   su2double duMaxPrev = 10.0;
 
   int iter;
-  for(iter=0; iter<iterMax; ++iter) {
-
+  for (iter = 0; iter < iterMax; ++iter) {
     /* Compute the speed of sound, the density, the parameter JJ
        and its derivatives w.r.t. q. */
-    const su2double a   = sqrt(1.0 - 0.5*Gm1*q*q);
-    const su2double rho = pow(a,tovGm1);
-    const su2double JJ  = 1.0/a + 1.0/(3.0*a*a*a) + 1.0/(5.0*a*a*a*a*a)
-                        - 0.5*log((1.0+a)/(1.0-a));
+    const su2double a = sqrt(1.0 - 0.5 * Gm1 * q * q);
+    const su2double rho = pow(a, tovGm1);
+    const su2double JJ =
+        1.0 / a + 1.0 / (3.0 * a * a * a) + 1.0 / (5.0 * a * a * a * a * a) - 0.5 * log((1.0 + a) / (1.0 - a));
 
-    const su2double dadq   = -0.5*Gm1*q/a;
-    const su2double drhodq =  2.0*rho*dadq/(Gm1*a);
-    const su2double dJJdq  =  dadq/(pow(a,6)*(a*a-1.0));
+    const su2double dadq = -0.5 * Gm1 * q / a;
+    const su2double drhodq = 2.0 * rho * dadq / (Gm1 * a);
+    const su2double dJJdq = dadq / (pow(a, 6) * (a * a - 1.0));
 
     /* Determine the values of the nonlinear equations to solve
        and its corresponding Jacobian matrix. */
-    const su2double y2c = (k*k - q*q)/(k*k*k*k*rho*rho*q*q);
-    const su2double f[] = {(2.0/(k*k) - 1.0/(q*q))/(2.0*rho) - 0.5*JJ - x,
-                           y2c - y2};
+    const su2double y2c = (k * k - q * q) / (k * k * k * k * rho * rho * q * q);
+    const su2double f[] = {(2.0 / (k * k) - 1.0 / (q * q)) / (2.0 * rho) - 0.5 * JJ - x, y2c - y2};
     su2double Jac[2][2];
-    Jac[0][0] = -(1.0/(k*k) - 0.50/(q*q))*drhodq/(rho*rho)
-              + 1.0/(rho*q*q*q) - 0.5*dJJdq;
-    Jac[0][1] = -2.0/(rho*k*k*k);
-    Jac[1][0] = -2.0/(k*k*rho*rho*q*q*q) - 2.0*y2c*drhodq/rho;
-    Jac[1][1] = (4.0*q*q - 2.0*k*k)/(k*k*k*k*k*rho*rho*q*q);
+    Jac[0][0] = -(1.0 / (k * k) - 0.50 / (q * q)) * drhodq / (rho * rho) + 1.0 / (rho * q * q * q) - 0.5 * dJJdq;
+    Jac[0][1] = -2.0 / (rho * k * k * k);
+    Jac[1][0] = -2.0 / (k * k * rho * rho * q * q * q) - 2.0 * y2c * drhodq / rho;
+    Jac[1][1] = (4.0 * q * q - 2.0 * k * k) / (k * k * k * k * k * rho * rho * q * q);
 
     /* Determine the update dU. */
-    const su2double det  = Jac[0][0]*Jac[1][1] - Jac[0][1]*Jac[1][0];
-    const su2double dU[] = {(f[0]*Jac[1][1] - f[1]*Jac[0][1])/det,
-                            (f[1]*Jac[0][0] - f[0]*Jac[1][0])/det};
+    const su2double det = Jac[0][0] * Jac[1][1] - Jac[0][1] * Jac[1][0];
+    const su2double dU[] = {(f[0] * Jac[1][1] - f[1] * Jac[0][1]) / det, (f[1] * Jac[0][0] - f[0] * Jac[1][0]) / det};
 
     /* Determine the underrelaxation coefficient alp. */
     const su2double dUMax = max(fabs(dU[0]), fabs(dU[1]));
     su2double alp = 1.0;
-    if(     dUMax > 1.0) alp = 0.04;
-    else if(dUMax > 0.1) alp = 0.2;
+    if (dUMax > 1.0)
+      alp = 0.04;
+    else if (dUMax > 0.1)
+      alp = 0.2;
 
     /* Update q and k. */
-    q -= alp*dU[0];
-    k -= alp*dU[1];
+    q -= alp * dU[0];
+    k -= alp * dU[1];
 
     /* Convergence check, which is independent of the precision used. */
-    if((dUMax < 1.e-3) && (dUMax >= duMaxPrev)) break;
+    if ((dUMax < 1.e-3) && (dUMax >= duMaxPrev)) break;
     duMaxPrev = dUMax;
   }
 
   /* Check if the Newton algorithm actually converged. */
-  if(iter == iterMax)
-    SU2_MPI::Error("Newton algorithm did not converge", CURRENT_FUNCTION);
+  if (iter == iterMax) SU2_MPI::Error("Newton algorithm did not converge", CURRENT_FUNCTION);
 
   /* Compute the speed of sound, density and pressure. */
-  const su2double a   = sqrt(1.0 - 0.5*Gm1*q*q);
-  const su2double rho = pow(a,tovGm1);
-  const su2double p   = pow(a,tGamOvGm1)/Gamma;
+  const su2double a = sqrt(1.0 - 0.5 * Gm1 * q * q);
+  const su2double rho = pow(a, tovGm1);
+  const su2double p = pow(a, tGamOvGm1) / Gamma;
 
   /* Determine the derivative of x w.r.t. q and ydxdq. */
-  const su2double dadq   = -0.5*Gm1*q/a;
-  const su2double drhodq =  2.0*rho*dadq/(Gm1*a);
-  const su2double dJJdq  =  dadq/(pow(a,6)*(a*a-1.0));
+  const su2double dadq = -0.5 * Gm1 * q / a;
+  const su2double drhodq = 2.0 * rho * dadq / (Gm1 * a);
+  const su2double dJJdq = dadq / (pow(a, 6) * (a * a - 1.0));
 
-  const su2double dxdq  = -(1.0/(k*k) - 0.5/(q*q))*drhodq/(rho*rho)
-                        +   1.0/(rho*q*q*q) - 0.5*dJJdq;
-  const su2double ydxdq = y*dxdq;
+  const su2double dxdq =
+      -(1.0 / (k * k) - 0.5 / (q * q)) * drhodq / (rho * rho) + 1.0 / (rho * q * q * q) - 0.5 * dJJdq;
+  const su2double ydxdq = y * dxdq;
 
   /* Determine the derivative of 1/2 y2 w.r.t. q, which is ydydq. The reason is
      that ydydq is always well defined, while dydq is singular for y = 0. */
-  const su2double ydydq = drhodq*(q*q-k*k)/(k*k*k*k*rho*rho*rho*q*q)
-                        - 1.0/(k*k*rho*rho*q*q*q);
+  const su2double ydydq =
+      drhodq * (q * q - k * k) / (k * k * k * k * rho * rho * rho * q * q) - 1.0 / (k * k * rho * rho * q * q * q);
 
   /* Determine the direction of the streamline. */
-  const su2double vecLen = sqrt(ydxdq*ydxdq + ydydq*ydydq);
+  const su2double vecLen = sqrt(ydxdq * ydxdq + ydydq * ydydq);
 
-  su2double velDir[] = {ydxdq/vecLen, ydydq/vecLen};
-  if(velDir[1] > 0.0){velDir[0] = -velDir[0]; velDir[1] = -velDir[1];}
+  su2double velDir[] = {ydxdq / vecLen, ydydq / vecLen};
+  if (velDir[1] > 0.0) {
+    velDir[0] = -velDir[0];
+    velDir[1] = -velDir[1];
+  }
 
   /* Compute the conservative variables. Note that both 2D and 3D
      cases are treated correctly. */
-  val_solution[0]      = rho;
-  val_solution[1]      = rho*q*velDir[0];
-  val_solution[2]      = rho*q*velDir[1];
-  val_solution[3]      = 0.0;
-  val_solution[nVar-1] = p/Gm1 + 0.5*rho*q*q;
+  val_solution[0] = rho;
+  val_solution[1] = rho * q * velDir[0];
+  val_solution[2] = rho * q * velDir[1];
+  val_solution[3] = 0.0;
+  val_solution[nVar - 1] = p / Gm1 + 0.5 * rho * q * q;
 }
diff --git a/Common/src/toolboxes/MMS/CTGVSolution.cpp b/Common/src/toolboxes/MMS/CTGVSolution.cpp
index 77eaf387213..f561b9b54a6 100644
--- a/Common/src/toolboxes/MMS/CTGVSolution.cpp
+++ b/Common/src/toolboxes/MMS/CTGVSolution.cpp
@@ -27,14 +27,10 @@
 
 #include "../../../include/toolboxes/MMS/CTGVSolution.hpp"
 
-CTGVSolution::CTGVSolution(void) : CVerificationSolution() { }
-
-CTGVSolution::CTGVSolution(unsigned short val_nDim,
-                           unsigned short val_nVar,
-                           unsigned short val_iMesh,
-                           CConfig*       config)
-  : CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
+CTGVSolution::CTGVSolution(void) : CVerificationSolution() {}
 
+CTGVSolution::CTGVSolution(unsigned short val_nDim, unsigned short val_nVar, unsigned short val_iMesh, CConfig* config)
+    : CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
   /*--- Write a message that the solution is initialized for the
    Taylor-Green vortex test case. ---*/
 
@@ -47,88 +43,74 @@ CTGVSolution::CTGVSolution(unsigned short val_nDim,
 
   /*--- Store TGV specific parameters here. ---*/
 
-  tgvLength   = 1.0;     // Taylor-Green length scale.
-  tgvVelocity = 1.0;     // Taylor-Green velocity.
-  tgvDensity  = 1.0;     // Taylor-Green density.
-  tgvPressure = 100.0;   // Taylor-Green pressure.
+  tgvLength = 1.0;      // Taylor-Green length scale.
+  tgvVelocity = 1.0;    // Taylor-Green velocity.
+  tgvDensity = 1.0;     // Taylor-Green density.
+  tgvPressure = 100.0;  // Taylor-Green pressure.
 
   /*--- Useful coefficient in which Gamma is present. ---*/
 
-  ovGm1 = 1.0/(config->GetGamma() - 1.0);
+  ovGm1 = 1.0 / (config->GetGamma() - 1.0);
 
   /*--- Perform some sanity and error checks for this solution here. ---*/
 
-  if((config->GetTime_Marching() != TIME_MARCHING::TIME_STEPPING) &&
-     (config->GetTime_Marching() != TIME_MARCHING::DT_STEPPING_1ST) &&
-     (config->GetTime_Marching() != TIME_MARCHING::DT_STEPPING_2ND))
-    SU2_MPI::Error("Unsteady mode must be selected for the Taylor Green Vortex",
-                   CURRENT_FUNCTION);
-
-  if(Kind_Solver != MAIN_SOLVER::EULER && Kind_Solver != MAIN_SOLVER::NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::RANS &&
-     Kind_Solver != MAIN_SOLVER::FEM_EULER && Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::FEM_RANS &&
-     Kind_Solver != MAIN_SOLVER::FEM_LES)
-    SU2_MPI::Error("Compressible flow equations must be selected for the Taylor Green Vortex",
-                   CURRENT_FUNCTION);
-
-  if((Kind_Solver != MAIN_SOLVER::NAVIER_STOKES) &&
-     (Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES))
-    SU2_MPI::Error("Navier Stokes equations must be selected for the Taylor Green Vortex",
-                   CURRENT_FUNCTION);
-
-  if((config->GetKind_FluidModel() != STANDARD_AIR) &&
-     (config->GetKind_FluidModel() != IDEAL_GAS))
-    SU2_MPI::Error("Standard air or ideal gas must be selected for the Taylor Green Vortex",
-                   CURRENT_FUNCTION);
-
-  if(config->GetKind_ViscosityModel() != VISCOSITYMODEL::CONSTANT)
-    SU2_MPI::Error("Constant viscosity must be selected for the Taylor Green Vortex",
-                   CURRENT_FUNCTION);
-
-  if(config->GetKind_ConductivityModel() != CONDUCTIVITYMODEL::CONSTANT_PRANDTL)
-    SU2_MPI::Error("Constant Prandtl number must be selected for the Taylor Green Vortex",
-                   CURRENT_FUNCTION);
-}
+  if ((config->GetTime_Marching() != TIME_MARCHING::TIME_STEPPING) &&
+      (config->GetTime_Marching() != TIME_MARCHING::DT_STEPPING_1ST) &&
+      (config->GetTime_Marching() != TIME_MARCHING::DT_STEPPING_2ND))
+    SU2_MPI::Error("Unsteady mode must be selected for the Taylor Green Vortex", CURRENT_FUNCTION);
+
+  if (Kind_Solver != MAIN_SOLVER::EULER && Kind_Solver != MAIN_SOLVER::NAVIER_STOKES &&
+      Kind_Solver != MAIN_SOLVER::RANS && Kind_Solver != MAIN_SOLVER::FEM_EULER &&
+      Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES && Kind_Solver != MAIN_SOLVER::FEM_RANS &&
+      Kind_Solver != MAIN_SOLVER::FEM_LES)
+    SU2_MPI::Error("Compressible flow equations must be selected for the Taylor Green Vortex", CURRENT_FUNCTION);
+
+  if ((Kind_Solver != MAIN_SOLVER::NAVIER_STOKES) && (Kind_Solver != MAIN_SOLVER::FEM_NAVIER_STOKES))
+    SU2_MPI::Error("Navier Stokes equations must be selected for the Taylor Green Vortex", CURRENT_FUNCTION);
 
-CTGVSolution::~CTGVSolution(void) { }
+  if ((config->GetKind_FluidModel() != STANDARD_AIR) && (config->GetKind_FluidModel() != IDEAL_GAS))
+    SU2_MPI::Error("Standard air or ideal gas must be selected for the Taylor Green Vortex", CURRENT_FUNCTION);
+
+  if (config->GetKind_ViscosityModel() != VISCOSITYMODEL::CONSTANT)
+    SU2_MPI::Error("Constant viscosity must be selected for the Taylor Green Vortex", CURRENT_FUNCTION);
+
+  if (config->GetKind_ConductivityModel() != CONDUCTIVITYMODEL::CONSTANT_PRANDTL)
+    SU2_MPI::Error("Constant Prandtl number must be selected for the Taylor Green Vortex", CURRENT_FUNCTION);
+}
 
-void CTGVSolution::GetSolution(const su2double *val_coords,
-                               const su2double val_t,
-                               su2double       *val_solution) const {
+CTGVSolution::~CTGVSolution(void) {}
 
+void CTGVSolution::GetSolution(const su2double* val_coords, const su2double val_t, su2double* val_solution) const {
   /* The initial conditions are set for the Taylor-Green vortex case, which
    is a DNS case that features vortex breakdown into turbulence. These
    particular settings are for the typical Re = 1600 case (M = 0.08) with
    an initial temperature of 300 K. Note that this condition works in both
    2D and 3D. */
 
-  su2double val_coordsZ      = 0.0;
+  su2double val_coordsZ = 0.0;
   if (nDim == 3) val_coordsZ = val_coords[2];
 
   /* Compute the primitive variables. */
 
-  su2double rho =  tgvDensity;
-  su2double u   =  tgvVelocity * (sin(val_coords[0]/tgvLength)*
-                                  cos(val_coords[1]/tgvLength)*
-                                  cos(val_coordsZ  /tgvLength));
-  su2double v   = -tgvVelocity * (cos(val_coords[0]/tgvLength)*
-                                  sin(val_coords[1]/tgvLength)*
-                                  cos(val_coordsZ  /tgvLength));
+  su2double rho = tgvDensity;
+  su2double u =
+      tgvVelocity * (sin(val_coords[0] / tgvLength) * cos(val_coords[1] / tgvLength) * cos(val_coordsZ / tgvLength));
+  su2double v =
+      -tgvVelocity * (cos(val_coords[0] / tgvLength) * sin(val_coords[1] / tgvLength) * cos(val_coordsZ / tgvLength));
 
-  su2double factorA = cos(2.0*val_coordsZ/tgvLength) + 2.0;
-  su2double factorB = (cos(2.0*val_coords[0]/tgvLength) +
-                       cos(2.0*val_coords[1]/tgvLength));
+  su2double factorA = cos(2.0 * val_coordsZ / tgvLength) + 2.0;
+  su2double factorB = (cos(2.0 * val_coords[0] / tgvLength) + cos(2.0 * val_coords[1] / tgvLength));
 
-  su2double p = (tgvPressure +
-                 tgvDensity*(pow(tgvVelocity,2.0)/16.0)*factorA*factorB);
+  su2double p = (tgvPressure + tgvDensity * (pow(tgvVelocity, 2.0) / 16.0) * factorA * factorB);
 
   /* Compute the conservative variables. Note that both 2D and 3D
    cases are treated correctly. */
 
-  val_solution[0]      = rho;
-  val_solution[1]      = rho*u;
-  val_solution[2]      = rho*v;
-  val_solution[3]      = 0.0;
-  val_solution[nVar-1] = p*ovGm1 + 0.5*rho*(u*u + v*v);
+  val_solution[0] = rho;
+  val_solution[1] = rho * u;
+  val_solution[2] = rho * v;
+  val_solution[3] = 0.0;
+  val_solution[nVar - 1] = p * ovGm1 + 0.5 * rho * (u * u + v * v);
 }
 
-bool CTGVSolution::ExactSolutionKnown(void) const {return false;}
+bool CTGVSolution::ExactSolutionKnown(void) const { return false; }
diff --git a/Common/src/toolboxes/MMS/CUserDefinedSolution.cpp b/Common/src/toolboxes/MMS/CUserDefinedSolution.cpp
index 2332a27d5da..da2806cfcd2 100644
--- a/Common/src/toolboxes/MMS/CUserDefinedSolution.cpp
+++ b/Common/src/toolboxes/MMS/CUserDefinedSolution.cpp
@@ -27,14 +27,11 @@
 
 #include "../../../include/toolboxes/MMS/CUserDefinedSolution.hpp"
 
-CUserDefinedSolution::CUserDefinedSolution(void) : CVerificationSolution() { }
-
-CUserDefinedSolution::CUserDefinedSolution(unsigned short val_nDim,
-                                           unsigned short val_nVar,
-                                           unsigned short val_iMesh,
-                                           CConfig*       config)
-  : CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
+CUserDefinedSolution::CUserDefinedSolution(void) : CVerificationSolution() {}
 
+CUserDefinedSolution::CUserDefinedSolution(unsigned short val_nDim, unsigned short val_nVar, unsigned short val_iMesh,
+                                           CConfig* config)
+    : CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
   /*--- Write a message that the solution is initialized for a
    user-defined verification case. ---*/
 
@@ -48,30 +45,24 @@ CUserDefinedSolution::CUserDefinedSolution(unsigned short val_nDim,
   SU2_MPI::Error("User must implement this function", CURRENT_FUNCTION);
 }
 
-CUserDefinedSolution::~CUserDefinedSolution(void) { }
-
-void CUserDefinedSolution::GetBCState(const su2double *val_coords,
-                                      const su2double val_t,
-                                      su2double       *val_solution) const {
+CUserDefinedSolution::~CUserDefinedSolution(void) {}
 
+void CUserDefinedSolution::GetBCState(const su2double* val_coords, const su2double val_t,
+                                      su2double* val_solution) const {
   SU2_MPI::Error("User must implement this function", CURRENT_FUNCTION);
 }
 
-void CUserDefinedSolution::GetSolution(const su2double *val_coords,
-                                       const su2double val_t,
-                                       su2double       *val_solution) const {
-
+void CUserDefinedSolution::GetSolution(const su2double* val_coords, const su2double val_t,
+                                       su2double* val_solution) const {
   SU2_MPI::Error("User must implement this function", CURRENT_FUNCTION);
 }
 
-void CUserDefinedSolution::GetMMSSourceTerm(const su2double *val_coords,
-                                            const su2double val_t,
-                                            su2double       *val_source) const {
-
+void CUserDefinedSolution::GetMMSSourceTerm(const su2double* val_coords, const su2double val_t,
+                                            su2double* val_source) const {
   SU2_MPI::Error("User must implement this function", CURRENT_FUNCTION);
 }
 
 bool CUserDefinedSolution::IsManufacturedSolution(void) const {
   SU2_MPI::Error("User must implement this function", CURRENT_FUNCTION);
-  return false;  /* True if manufactured. */
+  return false; /* True if manufactured. */
 }
diff --git a/Common/src/toolboxes/MMS/CVerificationSolution.cpp b/Common/src/toolboxes/MMS/CVerificationSolution.cpp
index e5f707a015c..ff8687aad87 100644
--- a/Common/src/toolboxes/MMS/CVerificationSolution.cpp
+++ b/Common/src/toolboxes/MMS/CVerificationSolution.cpp
@@ -28,18 +28,15 @@
 #include "../../../include/toolboxes/MMS/CVerificationSolution.hpp"
 
 CVerificationSolution::CVerificationSolution(void) {
-
   /*--- Initialize the pointers to NULL. ---*/
-  Error_RMS             = nullptr;
-  Error_Max             = nullptr;
-  Error_Point_Max       = nullptr;
+  Error_RMS = nullptr;
+  Error_Max = nullptr;
+  Error_Point_Max = nullptr;
   Error_Point_Max_Coord = nullptr;
 }
 
-CVerificationSolution::CVerificationSolution(unsigned short val_nDim,
-                                             unsigned short val_nVar,
-                                             unsigned short val_iMesh,
-                                             CConfig*       config) {
+CVerificationSolution::CVerificationSolution(unsigned short val_nDim, unsigned short val_nVar, unsigned short val_iMesh,
+                                             CConfig* config) {
   /*--- Store the kind of solver ---*/
 
   Kind_Solver = config->GetKind_Solver();
@@ -59,73 +56,58 @@ CVerificationSolution::CVerificationSolution(unsigned short val_nDim,
   Error_Max = new su2double[nVar];
 
   Error_Point_Max = new unsigned long[nVar];
-  for (unsigned short iVar = 0; iVar < nVar; iVar++)
-    Error_Point_Max[iVar] = 0;
+  for (unsigned short iVar = 0; iVar < nVar; iVar++) Error_Point_Max[iVar] = 0;
 
   Error_Point_Max_Coord = new su2double*[nVar];
   for (unsigned short iVar = 0; iVar < nVar; iVar++) {
     Error_Point_Max_Coord[iVar] = new su2double[nDim];
-    for (unsigned short  iDim = 0; iDim < nDim; iDim++)
-      Error_Point_Max_Coord[iVar][iDim] = 0.0;
+    for (unsigned short iDim = 0; iDim < nDim; iDim++) Error_Point_Max_Coord[iVar][iDim] = 0.0;
   }
 }
 
 CVerificationSolution::~CVerificationSolution(void) {
-
   /*--- Release the memory of the pointers, if allocated. ---*/
-  delete [] Error_RMS;
-  delete [] Error_Max;
+  delete[] Error_RMS;
+  delete[] Error_Max;
 
-  delete [] Error_Point_Max;
+  delete[] Error_Point_Max;
 
   if (Error_Point_Max_Coord != nullptr) {
     for (unsigned short iVar = 0; iVar < nVar; iVar++) {
-      delete [] Error_Point_Max_Coord[iVar];
+      delete[] Error_Point_Max_Coord[iVar];
     }
-    delete [] Error_Point_Max_Coord;
+    delete[] Error_Point_Max_Coord;
   }
 }
 
-void CVerificationSolution::GetSolution(const su2double *val_coords,
-                                        const su2double val_t,
-                                        su2double       *val_solution) const {
-
+void CVerificationSolution::GetSolution(const su2double* val_coords, const su2double val_t,
+                                        su2double* val_solution) const {
   SU2_MPI::Error("Function must be overwritten by the derived class", CURRENT_FUNCTION);
 }
 
-void CVerificationSolution::GetInitialCondition(const su2double *val_coords,
-                                                su2double       *val_solution) const {
-
+void CVerificationSolution::GetInitialCondition(const su2double* val_coords, su2double* val_solution) const {
   /*--- Initial conditions call the GetSolution() method at t = 0. ---*/
   GetSolution(val_coords, 0.0, val_solution);
 }
 
-void CVerificationSolution::GetBCState(const su2double *val_coords,
-                                       const su2double val_t,
-                                       su2double       *val_solution) const {
-
+void CVerificationSolution::GetBCState(const su2double* val_coords, const su2double val_t,
+                                       su2double* val_solution) const {
   SU2_MPI::Error("Function must be overwritten by the derived class", CURRENT_FUNCTION);
 }
 
-void CVerificationSolution::GetMMSSourceTerm(const su2double *val_coords,
-                                             const su2double val_t,
-                                             su2double       *val_source) const {
-
+void CVerificationSolution::GetMMSSourceTerm(const su2double* val_coords, const su2double val_t,
+                                             su2double* val_source) const {
   /* Default implementation of the source terms for the method of manufactured
      solutions. Simply set them to zero. */
-  for(unsigned short iVar=0; iVar<nVar; ++iVar)
-    val_source[iVar] = 0.0;
+  for (unsigned short iVar = 0; iVar < nVar; ++iVar) val_source[iVar] = 0.0;
 }
 
-bool CVerificationSolution::IsManufacturedSolution(void) const {return false;}
+bool CVerificationSolution::IsManufacturedSolution(void) const { return false; }
 
-bool CVerificationSolution::ExactSolutionKnown(void) const {return true;}
-
-void CVerificationSolution::GetLocalError(const su2double *val_coords,
-                                          const su2double val_t,
-                                          const su2double *val_solution,
-                                          su2double       *val_error) const {
+bool CVerificationSolution::ExactSolutionKnown(void) const { return true; }
 
+void CVerificationSolution::GetLocalError(const su2double* val_coords, const su2double val_t,
+                                          const su2double* val_solution, su2double* val_error) const {
   /*--- Get the value of the verification solution first.
         Use val_error to store this solution. ---*/
 
@@ -134,53 +116,44 @@ void CVerificationSolution::GetLocalError(const su2double *val_coords,
   /*--- Compute the local error as the difference between the current
    numerical solution and the verification solution. ---*/
 
-  for (unsigned short iVar=0; iVar<nVar; ++iVar)
-    val_error[iVar] = val_solution[iVar] - val_error[iVar];
-
+  for (unsigned short iVar = 0; iVar < nVar; ++iVar) val_error[iVar] = val_solution[iVar] - val_error[iVar];
 }
 
-void CVerificationSolution::SetVerificationError(unsigned long nDOFsGlobal,
-                                                 CConfig       *config) {
-
+void CVerificationSolution::SetVerificationError(unsigned long nDOFsGlobal, CConfig* config) {
   /* Disable the reduce for the error to avoid overhead if requested. */
   if (config->GetComm_Level() == COMM_FULL) {
-
     /*--- Get the number of ranks and the MPI communicator. ---*/
     int size = SU2_MPI::GetSize();
     SU2_MPI::Comm comm = SU2_MPI::GetComm();
 
     /*--- The local L2 norms must be added to obtain the global value. ---*/
-    vector<su2double> rbufError(nVar,0.0);
-    SU2_MPI::Allreduce(Error_RMS, rbufError.data(), nVar,
-                       MPI_DOUBLE, MPI_SUM, comm);
+    vector<su2double> rbufError(nVar, 0.0);
+    SU2_MPI::Allreduce(Error_RMS, rbufError.data(), nVar, MPI_DOUBLE, MPI_SUM, comm);
 
-    for(unsigned short iVar=0; iVar<nVar; ++iVar) {
-      SetError_RMS(iVar, max(EPS*EPS, sqrt(rbufError[iVar]/nDOFsGlobal)));
+    for (unsigned short iVar = 0; iVar < nVar; ++iVar) {
+      SetError_RMS(iVar, max(EPS * EPS, sqrt(rbufError[iVar] / nDOFsGlobal)));
     }
 
     /*--- The global maximum norms must be obtained. ---*/
-    rbufError.resize(nVar*size,0.0);
-    SU2_MPI::Allgather(Error_Max, nVar, MPI_DOUBLE, rbufError.data(),
-                       nVar, MPI_DOUBLE, comm);
-
-    vector<unsigned long> rbufPoint(nVar*size);
-    SU2_MPI::Allgather(Error_Point_Max, nVar, MPI_UNSIGNED_LONG, rbufPoint.data(),
-                       nVar, MPI_UNSIGNED_LONG, comm);
-
-    vector<su2double> sbufCoor(nDim*nVar,0.0);
-    for(unsigned short iVar=0; iVar<nVar; ++iVar) {
-      for(unsigned short iDim=0; iDim<nDim; ++iDim)
-        sbufCoor[iVar*nDim+iDim] = Error_Point_Max_Coord[iVar][iDim];
+    rbufError.resize(nVar * size, 0.0);
+    SU2_MPI::Allgather(Error_Max, nVar, MPI_DOUBLE, rbufError.data(), nVar, MPI_DOUBLE, comm);
+
+    vector<unsigned long> rbufPoint(nVar * size);
+    SU2_MPI::Allgather(Error_Point_Max, nVar, MPI_UNSIGNED_LONG, rbufPoint.data(), nVar, MPI_UNSIGNED_LONG, comm);
+
+    vector<su2double> sbufCoor(nDim * nVar, 0.0);
+    for (unsigned short iVar = 0; iVar < nVar; ++iVar) {
+      for (unsigned short iDim = 0; iDim < nDim; ++iDim)
+        sbufCoor[iVar * nDim + iDim] = Error_Point_Max_Coord[iVar][iDim];
     }
 
-    vector<su2double> rbufCoor(nDim*nVar*size,0.0);
-    SU2_MPI::Allgather(sbufCoor.data(), nVar*nDim, MPI_DOUBLE, rbufCoor.data(),
-                       nVar*nDim, MPI_DOUBLE, comm);
+    vector<su2double> rbufCoor(nDim * nVar * size, 0.0);
+    SU2_MPI::Allgather(sbufCoor.data(), nVar * nDim, MPI_DOUBLE, rbufCoor.data(), nVar * nDim, MPI_DOUBLE, comm);
 
-    for(unsigned short iVar=0; iVar<nVar; ++iVar) {
-      for(int proc=0; proc<size; ++proc)
-        AddError_Max(iVar, rbufError[proc*nVar+iVar], rbufPoint[proc*nVar+iVar],
-                     &rbufCoor[proc*nVar*nDim+iVar*nDim]);
+    for (unsigned short iVar = 0; iVar < nVar; ++iVar) {
+      for (int proc = 0; proc < size; ++proc)
+        AddError_Max(iVar, rbufError[proc * nVar + iVar], rbufPoint[proc * nVar + iVar],
+                     &rbufCoor[proc * nVar * nDim + iVar * nDim]);
     }
   }
 }
diff --git a/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncEulerSolution.py b/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncEulerSolution.py
index 54aa4707254..4ced7a4efed 100755
--- a/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncEulerSolution.py
+++ b/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncEulerSolution.py
@@ -32,16 +32,16 @@
 
 init_printing()
 
-x = Symbol('x', real=True)
-y = Symbol('y', real=True)
+x = Symbol("x", real=True)
+y = Symbol("y", real=True)
 
-u_0 = Symbol('u_0', real=True)
-v_0 = Symbol('v_0', real=True)
-P_0 = Symbol('P_0', real=True)
+u_0 = Symbol("u_0", real=True)
+v_0 = Symbol("v_0", real=True)
+P_0 = Symbol("P_0", real=True)
 
-Density   = Symbol('Density',   real=True)
-Viscosity = Symbol('Viscosity', real=True)
-epsilon   = Symbol('epsilon',   real=True)
+Density = Symbol("Density", real=True)
+Viscosity = Symbol("Viscosity", real=True)
+epsilon = Symbol("epsilon", real=True)
 
 # Set the manufactured solution. The solution
 # is from Salari K, and Knupp P, "Code verification
@@ -49,22 +49,21 @@
 # SAND 2000-1444, Sandia National Laboratories,
 # Albuquerque, NM, 2000.
 
-u = u_0*(sin(x*x + y*y) + epsilon)
-v = v_0*(cos(x*x + y*y) + epsilon)
-P = P_0*(sin(x*x + y*y) + 2.0)
+u = u_0 * (sin(x * x + y * y) + epsilon)
+v = v_0 * (cos(x * x + y * y) + epsilon)
+P = P_0 * (sin(x * x + y * y) + 2.0)
 
 # Put the manufactured solution through the Euler
 # equations to get the source term for each eqn.
 
 print("\nSource-Rho: ")
-Sp = diff(Density*u, x) + diff(Density*v,y)
+Sp = diff(Density * u, x) + diff(Density * v, y)
 print_ccode(Sp.simplify())
 
 print("\nSource-U: ")
-Su = diff(Density*u*u + P, x) + diff(Density*u*v, y)
+Su = diff(Density * u * u + P, x) + diff(Density * u * v, y)
 print_ccode(Su.simplify())
 
 print("\nSource-V: ")
-Sv = diff(Density*u*v, x) + diff(Density*v*v + P, y)
+Sv = diff(Density * u * v, x) + diff(Density * v * v + P, y)
 print_ccode(Sv.simplify())
-
diff --git a/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncNSSolution.py b/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncNSSolution.py
index d93f92c1c48..457825c8f84 100755
--- a/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncNSSolution.py
+++ b/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncNSSolution.py
@@ -32,16 +32,16 @@
 
 init_printing()
 
-x = Symbol('x', real=True)
-y = Symbol('y', real=True)
+x = Symbol("x", real=True)
+y = Symbol("y", real=True)
 
-u_0 = Symbol('u_0', real=True)
-v_0 = Symbol('v_0', real=True)
-P_0 = Symbol('P_0', real=True)
+u_0 = Symbol("u_0", real=True)
+v_0 = Symbol("v_0", real=True)
+P_0 = Symbol("P_0", real=True)
 
-Density   = Symbol('Density',   real=True)
-Viscosity = Symbol('Viscosity', real=True)
-epsilon   = Symbol('epsilon',   real=True)
+Density = Symbol("Density", real=True)
+Viscosity = Symbol("Viscosity", real=True)
+epsilon = Symbol("epsilon", real=True)
 
 # Set the manufactured solution. The solution
 # is from Salari K, and Knupp P, "Code verification
@@ -49,21 +49,31 @@
 # SAND 2000-1444, Sandia National Laboratories,
 # Albuquerque, NM, 2000.
 
-u = u_0*(sin(x*x + y*y) + epsilon)
-v = v_0*(cos(x*x + y*y) + epsilon)
-P = P_0*(sin(x*x + y*y) + 2.0)
+u = u_0 * (sin(x * x + y * y) + epsilon)
+v = v_0 * (cos(x * x + y * y) + epsilon)
+P = P_0 * (sin(x * x + y * y) + 2.0)
 
 # Put the manufactured solution through the Navier-Stokes
 # equations to get the source term for each eqn.
 
 print("\nSource-Rho: ")
-Sp = diff(Density*u, x) + diff(Density*v,y)
+Sp = diff(Density * u, x) + diff(Density * v, y)
 print_ccode(Sp.simplify())
 
 print("\nSource-U: ")
-Su = diff(Density*u*u + P, x) + diff(Density*u*v, y) - diff(Viscosity*(2.0/3.0)*(2.0*diff(u,x) - diff(v,y)),x) - diff(Viscosity*(diff(v,x)+diff(u,y)),y)
+Su = (
+    diff(Density * u * u + P, x)
+    + diff(Density * u * v, y)
+    - diff(Viscosity * (2.0 / 3.0) * (2.0 * diff(u, x) - diff(v, y)), x)
+    - diff(Viscosity * (diff(v, x) + diff(u, y)), y)
+)
 print_ccode(Su.simplify())
 
 print("\nSource-V: ")
-Sv = diff(Density*u*v, x) + diff(Density*v*v + P, y) - diff(Viscosity*(diff(v,x)+diff(u,y)),x) - diff(Viscosity*(2.0/3.0)*(2.0*diff(v,y) - diff(u,x)),y)
+Sv = (
+    diff(Density * u * v, x)
+    + diff(Density * v * v + P, y)
+    - diff(Viscosity * (diff(v, x) + diff(u, y)), x)
+    - diff(Viscosity * (2.0 / 3.0) * (2.0 * diff(v, y) - diff(u, x)), y)
+)
 print_ccode(Sv.simplify())
diff --git a/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSNSTwoHalfCirclesSolution.mw b/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSNSTwoHalfCirclesSolution.mw
index c726fd40a8e..b24a604474a 100644
--- a/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSNSTwoHalfCirclesSolution.mw
+++ b/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSNSTwoHalfCirclesSolution.mw
@@ -412,4 +412,4 @@
 <Input><Text-field style="Text" layout="Normal"><Equation executable="true" style="2D Math" input-equation="" display="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">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</Equation></Text-field>
 </Input>
 </Group></Presentation-Block>
-</Worksheet>
\ No newline at end of file
+</Worksheet>
diff --git a/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSNSTwoHalfSpheresSolution.mw b/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSNSTwoHalfSpheresSolution.mw
index 931ee55b4ab..9b560a8e61f 100644
--- a/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSNSTwoHalfSpheresSolution.mw
+++ b/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSNSTwoHalfSpheresSolution.mw
@@ -516,4 +516,4 @@
 <Input><Text-field style="Text" layout="Normal"><Equation executable="true" style="2D Math" input-equation="" display="LUklbXJvd0c2Iy9JK21vZHVsZW5hbWVHNiJJLFR5cGVzZXR0aW5nR0koX3N5c2xpYkdGJzYlLUkjbWlHRiQ2I1EhRicvJStleGVjdXRhYmxlR1EmZmFsc2VGJy8lLG1hdGh2YXJpYW50R1Enbm9ybWFsRic=">LUklbXJvd0c2Iy9JK21vZHVsZW5hbWVHNiJJLFR5cGVzZXR0aW5nR0koX3N5c2xpYkdGJzYjLUkjbWlHRiQ2I1EhRic=</Equation></Text-field>
 </Input>
 </Group></Presentation-Block>
-</Worksheet>
\ No newline at end of file
+</Worksheet>
diff --git a/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSNSUnitQuadSolution.mw b/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSNSUnitQuadSolution.mw
index 1cd09221b48..b6d131b2c89 100644
--- a/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSNSUnitQuadSolution.mw
+++ b/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSNSUnitQuadSolution.mw
@@ -404,4 +404,4 @@
 <Input><Text-field style="Text" layout="Normal"><Equation executable="true" style="2D Math" input-equation="" display="LUklbXJvd0c2Iy9JK21vZHVsZW5hbWVHNiJJLFR5cGVzZXR0aW5nR0koX3N5c2xpYkdGJzYlLUkjbWlHRiQ2I1EhRicvJStleGVjdXRhYmxlR1EmZmFsc2VGJy8lLG1hdGh2YXJpYW50R1Enbm9ybWFsRic=">LUklbXJvd0c2Iy9JK21vZHVsZW5hbWVHNiJJLFR5cGVzZXR0aW5nR0koX3N5c2xpYkdGJzYjLUkjbWlHRiQ2I1EhRic=</Equation></Text-field>
 </Input>
 </Group></Presentation-Block>
-</Worksheet>
\ No newline at end of file
+</Worksheet>
diff --git a/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSNSUnitQuadSolutionWallBC.mw b/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSNSUnitQuadSolutionWallBC.mw
index 9793789b2de..08fe53f8771 100644
--- a/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSNSUnitQuadSolutionWallBC.mw
+++ b/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSNSUnitQuadSolutionWallBC.mw
@@ -384,4 +384,4 @@
 <Input><Text-field style="Text" layout="Normal"><Equation executable="true" style="2D Math" input-equation="" display="LUklbXJvd0c2Iy9JK21vZHVsZW5hbWVHNiJJLFR5cGVzZXR0aW5nR0koX3N5c2xpYkdGJzYlLUkjbWlHRiQ2I1EhRicvJStleGVjdXRhYmxlR1EmZmFsc2VGJy8lLG1hdGh2YXJpYW50R1Enbm9ybWFsRic=">JSFH</Equation></Text-field>
 </Input>
 </Group></Presentation-Block>
-</Worksheet>
\ No newline at end of file
+</Worksheet>
diff --git a/Common/src/toolboxes/printing_toolbox.cpp b/Common/src/toolboxes/printing_toolbox.cpp
index f2b21f1da51..7153bcf1b98 100644
--- a/Common/src/toolboxes/printing_toolbox.cpp
+++ b/Common/src/toolboxes/printing_toolbox.cpp
@@ -30,86 +30,71 @@
 #include <stdexcept>
 #include "../../include/toolboxes/printing_toolbox.hpp"
 
-PrintingToolbox::CTablePrinter::CTablePrinter(std::ostream * output, const std::string & separator){
+PrintingToolbox::CTablePrinter::CTablePrinter(std::ostream* output, const std::string& separator) {
   out_stream_ = output;
   i_ = 0;
   j_ = 0;
   separator_ = separator;
   table_width_ = 0;
   print_header_bottom_line_ = true;
-  print_header_top_line_    = true;
+  print_header_top_line_ = true;
   align_ = RIGHT;
   inner_separator_ = separator;
   precision_ = 6;
 }
 
-int PrintingToolbox::CTablePrinter::GetNumColumns() const {
-  return (int)column_headers_.size();
-}
+int PrintingToolbox::CTablePrinter::GetNumColumns() const { return (int)column_headers_.size(); }
 
-int PrintingToolbox::CTablePrinter::GetTableWidth() const {
-  return table_width_;
-}
+int PrintingToolbox::CTablePrinter::GetTableWidth() const { return table_width_; }
 
-void PrintingToolbox::CTablePrinter::SetSeparator(const std::string &separator){
-  separator_ = separator;
-}
+void PrintingToolbox::CTablePrinter::SetSeparator(const std::string& separator) { separator_ = separator; }
 
-void PrintingToolbox::CTablePrinter::SetInnerSeparator(const std::string &inner_separator){
+void PrintingToolbox::CTablePrinter::SetInnerSeparator(const std::string& inner_separator) {
   inner_separator_ = inner_separator;
 }
 
-void PrintingToolbox::CTablePrinter::SetPrintHeaderBottomLine(bool print){
-  print_header_bottom_line_ = print;
-}
+void PrintingToolbox::CTablePrinter::SetPrintHeaderBottomLine(bool print) { print_header_bottom_line_ = print; }
 
-void PrintingToolbox::CTablePrinter::SetPrintHeaderTopLine(bool print){
-  print_header_top_line_ = print;
-}
+void PrintingToolbox::CTablePrinter::SetPrintHeaderTopLine(bool print) { print_header_top_line_ = print; }
 
-void PrintingToolbox::CTablePrinter::SetAlign(int align){
-  align_ = align;
-}
+void PrintingToolbox::CTablePrinter::SetAlign(int align) { align_ = align; }
 
-void PrintingToolbox::CTablePrinter::SetPrecision(int precision){
+void PrintingToolbox::CTablePrinter::SetPrecision(int precision) {
   precision_ = precision;
   out_stream_->precision(precision_);
 }
 
-void PrintingToolbox::CTablePrinter::AddColumn(const std::string & header_name, int column_width){
-  if (column_width < 4){
+void PrintingToolbox::CTablePrinter::AddColumn(const std::string& header_name, int column_width) {
+  if (column_width < 4) {
     throw std::invalid_argument("Column size has to be >= 4");
   }
 
   column_headers_.push_back(header_name);
   column_widths_.push_back(column_width);
-  table_width_ += column_width + separator_.size(); // for the separator
+  table_width_ += column_width + separator_.size();  // for the separator
 }
 
 void PrintingToolbox::CTablePrinter::PrintHorizontalLine() {
-  *out_stream_ << "+"; // the left bar
+  *out_stream_ << "+";  // the left bar
 
-  for (int i=0; i<table_width_-1; ++i)
-    *out_stream_ << "-";
+  for (int i = 0; i < table_width_ - 1; ++i) *out_stream_ << "-";
 
-  *out_stream_ << "+"; // the right bar
+  *out_stream_ << "+";  // the right bar
   *out_stream_ << "\n";
 }
 
-void PrintingToolbox::CTablePrinter::PrintHeader(){
-
+void PrintingToolbox::CTablePrinter::PrintHeader() {
   if (print_header_top_line_) PrintHorizontalLine();
   *out_stream_ << separator_;
   int indent = 0;
-  for (int i=0; i<GetNumColumns(); ++i){
-
+  for (int i = 0; i < GetNumColumns(); ++i) {
     std::stringstream ss;
 
     ss << column_headers_.at(i).substr(0, column_widths_.at(i));
 
     indent = 0;
 
-    if(align_ == LEFT)
+    if (align_ == LEFT)
       *out_stream_ << std::left;
     else if (align_ == RIGHT)
       *out_stream_ << std::right;
@@ -119,18 +104,16 @@ void PrintingToolbox::CTablePrinter::PrintHeader(){
     }
 
     *out_stream_ << std::setw(column_widths_.at(i) - indent) << column_headers_.at(i).substr(0, column_widths_.at(i));
-    if (i != GetNumColumns()-1){
-      *out_stream_ << std::setw(indent+(int)inner_separator_.size()) << inner_separator_;
+    if (i != GetNumColumns() - 1) {
+      *out_stream_ << std::setw(indent + (int)inner_separator_.size()) << inner_separator_;
     }
   }
 
-  *out_stream_ << std::setw((int)separator_.size()+indent) << separator_;
+  *out_stream_ << std::setw((int)separator_.size() + indent) << separator_;
   *out_stream_ << "\n";
-  if (print_header_bottom_line_){
+  if (print_header_bottom_line_) {
     PrintHorizontalLine();
   }
 }
 
-void PrintingToolbox::CTablePrinter::PrintFooter(){
-  PrintHorizontalLine();
-}
+void PrintingToolbox::CTablePrinter::PrintFooter() { PrintHorizontalLine(); }
diff --git a/Common/src/wall_model.cpp b/Common/src/wall_model.cpp
index 21b0c99aedf..639466be7a8 100644
--- a/Common/src/wall_model.cpp
+++ b/Common/src/wall_model.cpp
@@ -30,46 +30,34 @@
 #include "../../SU2_CFD/include/fluid/CFluidModel.hpp"
 
 /* Prototypes for Lapack functions, if MKL or LAPACK is used. */
-#if defined (HAVE_MKL) || defined(HAVE_LAPACK)
-extern "C" void dgtsv_(int*, int*, passivedouble*, passivedouble*,
-                       passivedouble*, passivedouble*, int*, int*);
+#if defined(HAVE_MKL) || defined(HAVE_LAPACK)
+extern "C" void dgtsv_(int*, int*, passivedouble*, passivedouble*, passivedouble*, passivedouble*, int*, int*);
 #endif
 
-CWallModel::CWallModel(CConfig *config) {
-
+CWallModel::CWallModel(CConfig* config) {
   /* Get the laminar and turbulent Prandtl number from config. */
-  Pr_lam  = config->GetPrandtl_Lam();
+  Pr_lam = config->GetPrandtl_Lam();
   Pr_turb = config->GetPrandtl_Turb();
 
-  karman = config->GetwallModel_Kappa(); // von Karman constant -> k = 0.41; or 0.38;
+  karman = config->GetwallModel_Kappa();  // von Karman constant -> k = 0.41; or 0.38;
 }
 
-void CWallModel::WallShearStressAndHeatFlux(const su2double rhoExchange,
-                                            const su2double velExchange,
-                                            const su2double muExchange,
-                                            const su2double pExchange,
-                                            const su2double Wall_HeatFlux,
-                                            const bool      HeatFlux_Prescribed,
-                                            const su2double Wall_Temperature,
-                                            const bool      Temperature_Prescribed,
-                                            CFluidModel     *FluidModel,
-                                            su2double       &tauWall,
-                                            su2double       &qWall,
-                                            su2double       &ViscosityWall,
-                                            su2double       &kOverCvWall) {}
-
-CWallModel1DEQ::CWallModel1DEQ(CConfig      *config,
-                               const string &Marker_Tag)
-  :  CWallModel(config) {
+void CWallModel::WallShearStressAndHeatFlux(const su2double rhoExchange, const su2double velExchange,
+                                            const su2double muExchange, const su2double pExchange,
+                                            const su2double Wall_HeatFlux, const bool HeatFlux_Prescribed,
+                                            const su2double Wall_Temperature, const bool Temperature_Prescribed,
+                                            CFluidModel* FluidModel, su2double& tauWall, su2double& qWall,
+                                            su2double& ViscosityWall, su2double& kOverCvWall) {}
 
+CWallModel1DEQ::CWallModel1DEQ(CConfig* config, const string& Marker_Tag) : CWallModel(config) {
   /* Retrieve the integer and floating point information for this
      boundary marker. */
-  const unsigned short *intInfo    = config->GetWallFunction_IntInfo(Marker_Tag);
-  const su2double      *doubleInfo = config->GetWallFunction_DoubleInfo(Marker_Tag);
+  const unsigned short* intInfo = config->GetWallFunction_IntInfo(Marker_Tag);
+  const su2double* doubleInfo = config->GetWallFunction_DoubleInfo(Marker_Tag);
 
   /* Copy the data into the member variables. */
-  numPoints      = intInfo[0];
-  h_wm           = doubleInfo[0];
+  numPoints = intInfo[0];
+  h_wm = doubleInfo[0];
   expansionRatio = doubleInfo[1];
 
   unsigned short nfa = numPoints + 1;
@@ -78,42 +66,33 @@ CWallModel1DEQ::CWallModel1DEQ(CConfig      *config,
   /* Allocate the memory for the coordinates of the grid points used
      in the 1D equilibrium wall model. */
   y_cv.resize(numPoints);
-  y_fa.resize(numPoints+1);
+  y_fa.resize(numPoints + 1);
 
   /* Determine the scaled version of the normal coordinates, where the
    first normal coordinate is simply 1.0. */
 
   y_fa[0] = 0.0;
-  for(unsigned short i=1; i<nfa; ++i) {
-    y_fa[i] = y_fa[i-1] + currentHeight;
-    y_cv[i-1] = 0.5 * (y_fa[i] + y_fa[i-1]);
-    currentHeight = currentHeight*expansionRatio;
+  for (unsigned short i = 1; i < nfa; ++i) {
+    y_fa[i] = y_fa[i - 1] + currentHeight;
+    y_cv[i - 1] = 0.5 * (y_fa[i] + y_fa[i - 1]);
+    currentHeight = currentHeight * expansionRatio;
   }
 
-  su2double y_max = y_cv[numPoints-1];
-  for(unsigned short i=0; i<nfa; ++i) {
-    y_fa[i] = y_fa[i]/y_max * h_wm;
+  su2double y_max = y_cv[numPoints - 1];
+  for (unsigned short i = 0; i < nfa; ++i) {
+    y_fa[i] = y_fa[i] / y_max * h_wm;
   }
-  for(unsigned short i=0; i<numPoints; ++i) {
-    y_cv[i] = y_cv[i]/y_max * h_wm;
+  for (unsigned short i = 0; i < numPoints; ++i) {
+    y_cv[i] = y_cv[i] / y_max * h_wm;
   }
 }
 
-void CWallModel1DEQ::WallShearStressAndHeatFlux(const su2double tExchange,
-                                                const su2double velExchange,
-                                                const su2double muExchange,
-                                                const su2double pExchange,
-                                                const su2double Wall_HeatFlux,
-                                                const bool      HeatFlux_Prescribed,
-                                                const su2double TWall,
-                                                const bool      Temperature_Prescribed,
-                                                CFluidModel    *FluidModel,
-                                                su2double &tauWall,
-                                                su2double &qWall,
-                                                su2double &ViscosityWall,
-                                                su2double &kOverCvWall) {
-
-
+void CWallModel1DEQ::WallShearStressAndHeatFlux(const su2double tExchange, const su2double velExchange,
+                                                const su2double muExchange, const su2double pExchange,
+                                                const su2double Wall_HeatFlux, const bool HeatFlux_Prescribed,
+                                                const su2double TWall, const bool Temperature_Prescribed,
+                                                CFluidModel* FluidModel, su2double& tauWall, su2double& qWall,
+                                                su2double& ViscosityWall, su2double& kOverCvWall) {
   /* Set tau wall to initial guess
    */
   tauWall = 0.5;
@@ -124,17 +103,17 @@ void CWallModel1DEQ::WallShearStressAndHeatFlux(const su2double tExchange,
   /* Set some constants, assuming air at standard conditions
   Todo: Read values below from the config file or from solver.
    */
-  //su2double C_1 = 2.03929e-04;
+  // su2double C_1 = 2.03929e-04;
   su2double C_1 = 1.716e-5;
   su2double S = 110.4;
   su2double T_ref = 273.15;
   su2double R = 287.058;
   su2double A = 17;
   su2double gamma = 1.4;
-  su2double c_p = (gamma*R)/(gamma-1);
-  su2double c_v = R/(gamma-1);
+  su2double c_p = (gamma * R) / (gamma - 1);
+  su2double c_v = R / (gamma - 1);
   su2double h_wall = c_p * TWall;
-  su2double h_bc   = c_p * tExchange;
+  su2double h_bc = c_p * tExchange;
   unsigned short nfa = numPoints + 1;
 
   /* Set up vectors
@@ -143,21 +122,20 @@ void CWallModel1DEQ::WallShearStressAndHeatFlux(const su2double tExchange,
   vector<su2double> mu_fa(nfa, muExchange);
   vector<su2double> tmp(nfa, 0.0);
   vector<su2double> u(numPoints, 0.0);
-  vector<su2double> lower(numPoints-1,0.0);
-  vector<su2double> upper(numPoints-1,0.0);
-  vector<su2double> diagonal(numPoints,0.0);
-  vector<su2double> rhs(numPoints,0.0);
+  vector<su2double> lower(numPoints - 1, 0.0);
+  vector<su2double> upper(numPoints - 1, 0.0);
+  vector<su2double> diagonal(numPoints, 0.0);
+  vector<su2double> rhs(numPoints, 0.0);
 
   /* Set parameters for control
    */
   bool converged = false;
   unsigned short iter = 0, max_iter = 25;
-  su2double tauWall_prev = 0.0, tol = 1e-3,  aux_rhs=0.0;
-  su2double qWall_prev=0.0;
+  su2double tauWall_prev = 0.0, tol = 1e-3, aux_rhs = 0.0;
+  su2double qWall_prev = 0.0;
   su2double mut, nu, mu_lam, rho, utau, y_plus, D;
 
-  while (converged == false){
-
+  while (converged == false) {
     iter += 1;
     if (iter == max_iter) converged = true;
 
@@ -167,17 +145,17 @@ void CWallModel1DEQ::WallShearStressAndHeatFlux(const su2double tExchange,
     /* Calculate total viscosity
     note: rho and mu_lam will be a function of temperature when solving an energy equation
      */
-    for(unsigned short i=0; i < nfa; ++i){
-      mu_lam = C_1 * pow(T[i]/T_ref, 1.5) * ((T_ref + S)/ (T[i] + S));
+    for (unsigned short i = 0; i < nfa; ++i) {
+      mu_lam = C_1 * pow(T[i] / T_ref, 1.5) * ((T_ref + S) / (T[i] + S));
       mu_fa[i] = mu_lam;
     }
 
-    for(unsigned short i=1; i < nfa; ++i){
-      rho = pExchange / (R*T[i]);
+    for (unsigned short i = 1; i < nfa; ++i) {
+      rho = pExchange / (R * T[i]);
       nu = mu_fa[i] / rho;
       utau = sqrt(tauWall / rho);
       y_plus = y_fa[i] * utau / nu;
-      D = pow(1.0 - exp((-y_plus)/A),2.0);
+      D = pow(1.0 - exp((-y_plus) / A), 2.0);
       mut = rho * karman * y_fa[i] * utau * D;
       mu_fa[i] += mut;
     }
@@ -185,10 +163,10 @@ void CWallModel1DEQ::WallShearStressAndHeatFlux(const su2double tExchange,
     /* Momentum matrix
      The solution vector is u at y_cv
      */
-    lower.assign(numPoints-1,0.0);
-    upper.assign(numPoints-1,0.0);
-    diagonal.assign(numPoints,0.0);
-    rhs.assign(numPoints,0.0);
+    lower.assign(numPoints - 1, 0.0);
+    upper.assign(numPoints - 1, 0.0);
+    diagonal.assign(numPoints, 0.0);
+    rhs.assign(numPoints, 0.0);
 
     /* Top bc
      */
@@ -197,16 +175,16 @@ void CWallModel1DEQ::WallShearStressAndHeatFlux(const su2double tExchange,
 
     /* Internal cvs
      */
-    for (unsigned short i=1; i < (numPoints - 1); ++i){
-      upper[i]  =  mu_fa[i + 1] / (y_cv[i + 1] -  y_cv[i] );
-      lower[i-1]  = mu_fa[i] / (y_cv[i] -  y_cv[i - 1] );
+    for (unsigned short i = 1; i < (numPoints - 1); ++i) {
+      upper[i] = mu_fa[i + 1] / (y_cv[i + 1] - y_cv[i]);
+      lower[i - 1] = mu_fa[i] / (y_cv[i] - y_cv[i - 1]);
       diagonal[i] = -1.0 * (upper[i] + lower[i - 1]);
     }
 
     /* Wall BC
      */
-    upper[0] = mu_fa[1]/(y_cv[1] - y_cv[0]);
-    diagonal[0] = -1.0 * (upper[0] + mu_fa[0]/(y_cv[0]-y_fa[0]) );
+    upper[0] = mu_fa[1] / (y_cv[1] - y_cv[0]);
+    diagonal[0] = -1.0 * (upper[0] + mu_fa[0] / (y_cv[0] - y_fa[0]));
     rhs[0] = 0.0;
 
     /* Solve the matrix problem to get the velocity field
@@ -215,9 +193,8 @@ void CWallModel1DEQ::WallShearStressAndHeatFlux(const su2double tExchange,
 #if (defined(HAVE_MKL) || defined(HAVE_LAPACK)) && !(defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE))
     int info, nrhs = 1;
 
-    dgtsv_(&numPoints,&nrhs,lower.data(),diagonal.data(),upper.data(),rhs.data(),&numPoints, &info);
-    if (info != 0)
-      SU2_MPI::Error("Unsuccessful call to dgtsv_", CURRENT_FUNCTION);
+    dgtsv_(&numPoints, &nrhs, lower.data(), diagonal.data(), upper.data(), rhs.data(), &numPoints, &info);
+    if (info != 0) SU2_MPI::Error("Unsuccessful call to dgtsv_", CURRENT_FUNCTION);
 #else
     SU2_MPI::Error("Not compiled with MKL or LAPACK support", CURRENT_FUNCTION);
 #endif
@@ -226,38 +203,38 @@ void CWallModel1DEQ::WallShearStressAndHeatFlux(const su2double tExchange,
 
     /* Update total viscosity
      */
-    for(unsigned short i=0; i < nfa; ++i){
-      mu_lam = C_1 * pow(T[i]/T_ref, 1.5) * ((T_ref + S)/ (T[i] + S));
+    for (unsigned short i = 0; i < nfa; ++i) {
+      mu_lam = C_1 * pow(T[i] / T_ref, 1.5) * ((T_ref + S) / (T[i] + S));
       mu_fa[i] = mu_lam;
-      tmp[i] = mu_lam/Pr_lam;
+      tmp[i] = mu_lam / Pr_lam;
     }
     /* Update tauWall
      */
-    tauWall = mu_fa[0] * (u[0] - 0.0)/(y_cv[0]-y_fa[0]);
-    for(unsigned short i=1; i < nfa; ++i){
-      rho = pExchange / (R*T[i]);
+    tauWall = mu_fa[0] * (u[0] - 0.0) / (y_cv[0] - y_fa[0]);
+    for (unsigned short i = 1; i < nfa; ++i) {
+      rho = pExchange / (R * T[i]);
       nu = mu_fa[i] / rho;
       utau = sqrt(tauWall / rho);
       y_plus = y_fa[i] * utau / nu;
-      D = pow(1.0 - exp((-y_plus)/A),2.0);
+      D = pow(1.0 - exp((-y_plus) / A), 2.0);
       mut = rho * karman * y_fa[i] * utau * D;
       mu_fa[i] += mut;
-      tmp[i] += mut/Pr_turb;
+      tmp[i] += mut / Pr_turb;
     }
 
     /* Energy matrix
      The Solution vector is Enthalpy at y_cv
      */
-    lower.assign(numPoints-1,0.0);
-    upper.assign(numPoints-1,0.0);
-    diagonal.assign(numPoints,0.0);
-    rhs.assign(numPoints,0.0);
+    lower.assign(numPoints - 1, 0.0);
+    upper.assign(numPoints - 1, 0.0);
+    diagonal.assign(numPoints, 0.0);
+    rhs.assign(numPoints, 0.0);
 
     /* Internal cvs
      */
-    for (unsigned short i=1; i < (numPoints - 1); ++i){
-      upper[i]  =  tmp[i + 1] / (y_cv[i + 1] -  y_cv[i] );
-      lower[i-1]  = tmp[i] / (y_cv[i] -  y_cv[i - 1] );
+    for (unsigned short i = 1; i < (numPoints - 1); ++i) {
+      upper[i] = tmp[i + 1] / (y_cv[i + 1] - y_cv[i]);
+      lower[i - 1] = tmp[i] / (y_cv[i] - y_cv[i - 1]);
       diagonal[i] = -1.0 * (upper[i] + lower[i - 1]);
     }
 
@@ -267,9 +244,9 @@ void CWallModel1DEQ::WallShearStressAndHeatFlux(const su2double tExchange,
 
     /* Wall BC
      */
-    upper[0] = tmp[1]/(y_cv[1] - y_cv[0]);
-    diagonal[0] = -1.0 * (upper[0] + tmp[0]/(y_cv[0]-y_fa[0]) );
-    aux_rhs = tmp[0]/(y_cv[0]-y_fa[0]);
+    upper[0] = tmp[1] / (y_cv[1] - y_cv[0]);
+    diagonal[0] = -1.0 * (upper[0] + tmp[0] / (y_cv[0] - y_fa[0]));
+    aux_rhs = tmp[0] / (y_cv[0] - y_fa[0]);
 
     /* RHS of the Energy equation
        - Compute flux -- (mu + mu_t) * u * du/dy --
@@ -277,28 +254,27 @@ void CWallModel1DEQ::WallShearStressAndHeatFlux(const su2double tExchange,
 
     /* Zero flux at the wall
      */
-    tmp[0] = 0. ;
-    for (unsigned short i=1; i < numPoints; ++i){
-      tmp[i] = 0.5* (mu_fa[i]) * (u[i] + u[i-1]) * (u[i] -u[i-1])/(y_cv[i] -  y_cv[i - 1] )  ;
+    tmp[0] = 0.;
+    for (unsigned short i = 1; i < numPoints; ++i) {
+      tmp[i] = 0.5 * (mu_fa[i]) * (u[i] + u[i - 1]) * (u[i] - u[i - 1]) / (y_cv[i] - y_cv[i - 1]);
     }
-    for (unsigned short i=0; i < (numPoints - 1); ++i){
-      rhs[i] = -tmp[i+1] + tmp[i];
+    for (unsigned short i = 0; i < (numPoints - 1); ++i) {
+      rhs[i] = -tmp[i + 1] + tmp[i];
     }
 
-    if (HeatFlux_Prescribed == true){
+    if (HeatFlux_Prescribed == true) {
       /* dT/dy = 0 -> Twall = T[1] */
       h_wall = c_p * T[1];
     }
 
     rhs[0] -= aux_rhs * h_wall;
-    rhs[numPoints-1] = h_bc;
+    rhs[numPoints - 1] = h_bc;
 
     /* Solve the matrix problem to get the Enthalpy field
      */
 #if (defined(HAVE_MKL) || defined(HAVE_LAPACK)) && !(defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE))
-    dgtsv_(&numPoints,&nrhs,lower.data(),diagonal.data(),upper.data(),rhs.data(),&numPoints, &info);
-    if (info != 0)
-      SU2_MPI::Error("Unsuccessful call to dgtsv_", CURRENT_FUNCTION);
+    dgtsv_(&numPoints, &nrhs, lower.data(), diagonal.data(), upper.data(), rhs.data(), &numPoints, &info);
+    if (info != 0) SU2_MPI::Error("Unsuccessful call to dgtsv_", CURRENT_FUNCTION);
 #else
     SU2_MPI::Error("Not compiled with MKL or LAPACK support", CURRENT_FUNCTION);
 #endif
@@ -306,64 +282,53 @@ void CWallModel1DEQ::WallShearStressAndHeatFlux(const su2double tExchange,
     /* Get Temperature from enthalpy
       - Temperature will be at face
      */
-    T[0] = h_wall/c_p;
-    T[numPoints] = h_bc/c_p;
-    for (unsigned short i=0; i < numPoints-1; i++){
-      T[i+1] = 0.5 * (rhs[i] + rhs[i+1])/c_p;
+    T[0] = h_wall / c_p;
+    T[numPoints] = h_bc / c_p;
+    for (unsigned short i = 0; i < numPoints - 1; i++) {
+      T[i + 1] = 0.5 * (rhs[i] + rhs[i + 1]) / c_p;
     }
 
     /* Final update tauWall
      */
-    mu_lam = C_1 * pow(T[0]/T_ref, 1.5) * ((T_ref + S)/ (T[0] + S));
+    mu_lam = C_1 * pow(T[0] / T_ref, 1.5) * ((T_ref + S) / (T[0] + S));
 
     /* These quantities will be returned.
      */
-    tauWall = mu_lam * (u[0] - 0.0)/(y_cv[0]-y_fa[0]);
-    qWall = mu_lam * (c_p / Pr_lam) * -(T[1] - T[0]) / (y_fa[1]-y_fa[0]);
+    tauWall = mu_lam * (u[0] - 0.0) / (y_cv[0] - y_fa[0]);
+    qWall = mu_lam * (c_p / Pr_lam) * -(T[1] - T[0]) / (y_fa[1] - y_fa[0]);
     ViscosityWall = mu_lam;
-    //kOverCvWall = c_p / c_v * (mu[0]/Pr_lam + muTurb[0]/Pr_turb);
-    kOverCvWall = c_p / c_v * (mu_lam/Pr_lam);
+    // kOverCvWall = c_p / c_v * (mu[0]/Pr_lam + muTurb[0]/Pr_turb);
+    kOverCvWall = c_p / c_v * (mu_lam / Pr_lam);
 
     /* Final check of the Y+
      */
     rho = pExchange / (R * T[0]);
-    if (y_cv[0] * sqrt(tauWall/rho) / (mu_lam/rho) > 1.0)
+    if (y_cv[0] * sqrt(tauWall / rho) / (mu_lam / rho) > 1.0)
       SU2_MPI::Error("Y+ greater than one: Increase the number of points or growth ratio.", CURRENT_FUNCTION);
 
     /* Define a norm
      */
-    if (abs(1.0 - tauWall/tauWall_prev) < tol && abs(1.0 - qWall/qWall_prev) < tol){
+    if (abs(1.0 - tauWall / tauWall_prev) < tol && abs(1.0 - qWall / qWall_prev) < tol) {
       converged = true;
     }
   }
 }
 
-CWallModelLogLaw::CWallModelLogLaw(CConfig      *config,
-                                   const string &Marker_Tag)
-  :  CWallModel(config) {
-
+CWallModelLogLaw::CWallModelLogLaw(CConfig* config, const string& Marker_Tag) : CWallModel(config) {
   C = 5.25; /* Constant to match the Reichardt BL profile ->  C = 4.1;  or 5.25. */
 
   /* Retrieve the floating point information for this boundary marker
      and set the exchange height. */
-  const su2double *doubleInfo = config->GetWallFunction_DoubleInfo(Marker_Tag);
+  const su2double* doubleInfo = config->GetWallFunction_DoubleInfo(Marker_Tag);
   h_wm = doubleInfo[0];
 }
 
-void CWallModelLogLaw::WallShearStressAndHeatFlux(const su2double tExchange,
-                                                  const su2double velExchange,
-                                                  const su2double muExchange,
-                                                  const su2double pExchange,
-                                                  const su2double Wall_HeatFlux,
-                                                  const bool      HeatFlux_Prescribed,
-                                                  const su2double Wall_Temperature,
-                                                  const bool      Temperature_Prescribed,
-                                                  CFluidModel     *FluidModel,
-                                                  su2double       &tauWall,
-                                                  su2double       &qWall,
-                                                  su2double       &ViscosityWall,
-                                                  su2double       &kOverCvWall) {
-
+void CWallModelLogLaw::WallShearStressAndHeatFlux(const su2double tExchange, const su2double velExchange,
+                                                  const su2double muExchange, const su2double pExchange,
+                                                  const su2double Wall_HeatFlux, const bool HeatFlux_Prescribed,
+                                                  const su2double Wall_Temperature, const bool Temperature_Prescribed,
+                                                  CFluidModel* FluidModel, su2double& tauWall, su2double& qWall,
+                                                  su2double& ViscosityWall, su2double& kOverCvWall) {
   /* Set the wall temperature, depending whether or not the temperature
      was prescribed and initialize the fluid model. */
   const su2double TWall = Temperature_Prescribed ? Wall_Temperature : tExchange;
@@ -372,64 +337,67 @@ void CWallModelLogLaw::WallShearStressAndHeatFlux(const su2double tExchange,
 
   /* Get the required data from the fluid model. */
   const su2double rho_wall = FluidModel->GetDensity();
-  const su2double mu_wall  = FluidModel->GetLaminarViscosity();
-  const su2double c_p      = FluidModel->GetCp();
-  const su2double c_v      = FluidModel->GetCv();
-  const su2double nu_wall  = mu_wall / rho_wall;
+  const su2double mu_wall = FluidModel->GetLaminarViscosity();
+  const su2double c_p = FluidModel->GetCp();
+  const su2double c_v = FluidModel->GetCv();
+  const su2double nu_wall = mu_wall / rho_wall;
 
   /* Initial guess of the friction velocity. */
-  su2double u_tau = max(0.01*velExchange, 1.e-5);
+  su2double u_tau = max(0.01 * velExchange, 1.e-5);
 
   /* Set parameters for control of the Newton iteration. */
   bool converged = false;
   unsigned short iter = 0, max_iter = 50;
-  const su2double tol=1e-3;
-
-  while (converged == false){
+  const su2double tol = 1e-3;
 
+  while (converged == false) {
     iter += 1;
     if (iter == max_iter) converged = true;
 
     const su2double u_tau0 = u_tau;
-    const su2double y_plus = u_tau0*h_wm/nu_wall;
+    const su2double y_plus = u_tau0 * h_wm / nu_wall;
 
     /* Reichardt boundary layer analytical law
        fprime is the differentiation of the Reichardt law with repect to u_tau.
      */
-    const su2double fval = velExchange/u_tau0 - ((C - log(karman)/karman)*(1.0 - exp(-y_plus/11.0)
-                         - (y_plus/11.0)*exp(-0.33*y_plus))) - log(karman*y_plus + 1.0)/karman;
-    const su2double fprime = -velExchange/pow(u_tau0,2.0)
-                           + (- C + log(karman)/karman)*(-(1.0/11.0)*h_wm*exp(-0.33*y_plus)/nu_wall
-                           +                              (1.0/11.0)*h_wm*exp(-(1.0/11.0)*y_plus)/nu_wall
-                           +                              (1.0/33.0)*u_tau0*pow(h_wm,2.0)*exp(-0.33*y_plus)/pow(nu_wall, 2.0))
-                           - 1.0*h_wm/(nu_wall*(karman*y_plus + 1.0));
+    const su2double fval =
+        velExchange / u_tau0 -
+        ((C - log(karman) / karman) * (1.0 - exp(-y_plus / 11.0) - (y_plus / 11.0) * exp(-0.33 * y_plus))) -
+        log(karman * y_plus + 1.0) / karman;
+    const su2double fprime = -velExchange / pow(u_tau0, 2.0) +
+                             (-C + log(karman) / karman) *
+                                 (-(1.0 / 11.0) * h_wm * exp(-0.33 * y_plus) / nu_wall +
+                                  (1.0 / 11.0) * h_wm * exp(-(1.0 / 11.0) * y_plus) / nu_wall +
+                                  (1.0 / 33.0) * u_tau0 * pow(h_wm, 2.0) * exp(-0.33 * y_plus) / pow(nu_wall, 2.0)) -
+                             1.0 * h_wm / (nu_wall * (karman * y_plus + 1.0));
 
     /* Newton method
      */
-    const su2double newton_step = fval/fprime;
+    const su2double newton_step = fval / fprime;
     u_tau = u_tau0 - newton_step;
 
     /* Define a norm
      */
-    if (abs(1.0 - u_tau/u_tau0) < tol) converged = true;
+    if (abs(1.0 - u_tau / u_tau0) < tol) converged = true;
   }
 
-  tauWall = rho_wall * pow(u_tau,2.0);
+  tauWall = rho_wall * pow(u_tau, 2.0);
 
-  if (Temperature_Prescribed){
+  if (Temperature_Prescribed) {
     /* The Kader's law will be used to approximate the variations of the temperature inside the boundary layer.
      */
-    const su2double y_plus = u_tau*h_wm/nu_wall;
-    const su2double lhs = - ((tExchange - TWall) * rho_wall * c_p * u_tau);
-    const su2double Gamma = - (0.01 * (Pr_lam * pow(y_plus,4.0))/(1.0 + 5.0*y_plus*pow(Pr_lam,3.0)));
+    const su2double y_plus = u_tau * h_wm / nu_wall;
+    const su2double lhs = -((tExchange - TWall) * rho_wall * c_p * u_tau);
+    const su2double Gamma = -(0.01 * (Pr_lam * pow(y_plus, 4.0)) / (1.0 + 5.0 * y_plus * pow(Pr_lam, 3.0)));
     const su2double rhs_1 = Pr_lam * y_plus * exp(Gamma);
-    const su2double rhs_2 = (2.12*log(1.0+y_plus) + pow((3.85*pow(Pr_lam,(1.0/3.0)) - 1.3),2.0) + 2.12*log(Pr_lam)) * exp(1./Gamma);
-    qWall = lhs/(rhs_1 + rhs_2);
-  }
-  else{
+    const su2double rhs_2 =
+        (2.12 * log(1.0 + y_plus) + pow((3.85 * pow(Pr_lam, (1.0 / 3.0)) - 1.3), 2.0) + 2.12 * log(Pr_lam)) *
+        exp(1. / Gamma);
+    qWall = lhs / (rhs_1 + rhs_2);
+  } else {
     qWall = Wall_HeatFlux;
   }
 
   ViscosityWall = mu_wall;
-  kOverCvWall   = FluidModel->GetThermalConductivity()/c_v;
+  kOverCvWall = FluidModel->GetThermalConductivity() / c_v;
 }
diff --git a/Docs/docmain.hpp b/Docs/docmain.hpp
index 704f85acdcb..ab8b45fa8ec 100644
--- a/Docs/docmain.hpp
+++ b/Docs/docmain.hpp
@@ -224,4 +224,4 @@
  * \defgroup SIMD Vectorization (SIMD)
  * \brief Classes for explicit (done by the programmer) vectorization (SIMD) of computations.
  * \ingroup Toolboxes
- */
\ No newline at end of file
+ */
diff --git a/QuickStart/inv_NACA0012.cfg b/QuickStart/inv_NACA0012.cfg
index 6f6dbc9424a..a4668268b9c 100644
--- a/QuickStart/inv_NACA0012.cfg
+++ b/QuickStart/inv_NACA0012.cfg
@@ -30,7 +30,7 @@ MACH_NUMBER= 0.8
 % Angle of attack (degrees)
 AOA= 1.25
 %
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)  
+% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)
 FREESTREAM_PRESSURE= 101325.0
 %
 % Free-stream temperature (273.15 K by default)
@@ -234,7 +234,7 @@ DEFORM_LINEAR_SOLVER_ERROR= 1E-14
 % Print the residuals during mesh deformation to the console (YES, NO)
 DEFORM_CONSOLE_OUTPUT= YES
 %
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, 
+% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
 %                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
@@ -275,7 +275,7 @@ SOLUTION_ADJ_FILENAME= solution_adj.dat
 % Output file format (TECPLOT, CSV)
 TABULAR_FORMAT= CSV
 %
-% Output file convergence history (w/o extension) 
+% Output file convergence history (w/o extension)
 CONV_FILENAME= history
 %
 % Output file restart flow
@@ -308,7 +308,7 @@ OUTPUT_WRT_FREQ= 250
 %    FORCE_X, FORCE_Y, FORCE_Z,
 %    MOMENT_X, MOMENT_Y, MOMENT_Z,
 %    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE, 
+%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
 %    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
 %    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
 %
diff --git a/SU2_DEF/src/SU2_DEF.cpp b/SU2_DEF/src/SU2_DEF.cpp
index 379a1a356c9..63c8bff70e6 100644
--- a/SU2_DEF/src/SU2_DEF.cpp
+++ b/SU2_DEF/src/SU2_DEF.cpp
@@ -28,7 +28,6 @@
 #include "../include/drivers/CDeformationDriver.hpp"
 
 int main(int argc, char* argv[]) {
-
   char config_file_name[MAX_STRING_SIZE];
 
   /*--- MPI initialization ---*/
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index d88d0048ec3..9ec2b31120a 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -36,7 +36,6 @@ using namespace std;
 
 CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
     : CDriverBase(confFile, 1, MPICommunicator) {
-
 /*--- Initialize MeDiPack (must also be here to initialize it from Python) ---*/
 #ifdef HAVE_MPI
 #if defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)
@@ -73,7 +72,6 @@ CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
     /*--- Preprocessing of the mesh solver for all zones. ---*/
 
     Numerics_Preprocessing();
-
   }
 
   /*--- Preprocessing time is reported now, but not included in the next compute portion. ---*/
@@ -115,7 +113,8 @@ void CDeformationDriver::Input_Preprocessing() {
       strcpy(zone_file_name, driver_config->GetConfigFilename(iZone).c_str());
       config_container[iZone] = new CConfig(driver_config, zone_file_name, SU2_COMPONENT::SU2_DEF, iZone, nZone, true);
     } else {
-      config_container[iZone] = new CConfig(driver_config, config_file_name, SU2_COMPONENT::SU2_DEF, iZone, nZone, true);
+      config_container[iZone] =
+          new CConfig(driver_config, config_file_name, SU2_COMPONENT::SU2_DEF, iZone, nZone, true);
     }
 
     config_container[iZone]->SetMPICommunicator(SU2_MPI::GetComm());
@@ -173,7 +172,8 @@ void CDeformationDriver::Geometrical_Preprocessing() {
 
     /*--- Computational grid preprocessing. ---*/
 
-    if (rank == MASTER_NODE) cout << endl << "----------------------- Preprocessing computations ----------------------" << endl;
+    if (rank == MASTER_NODE)
+      cout << endl << "----------------------- Preprocessing computations ----------------------" << endl;
 
     /*--- Compute elements surrounding points, points surrounding points. ---*/
 
@@ -205,7 +205,8 @@ void CDeformationDriver::Geometrical_Preprocessing() {
 
     /*--- Create the point-to-point MPI communication structures. ---*/
 
-    geometry_container[iZone][INST_0][MESH_0]->PreprocessP2PComms(geometry_container[iZone][INST_0][MESH_0],config_container[iZone]);
+    geometry_container[iZone][INST_0][MESH_0]->PreprocessP2PComms(geometry_container[iZone][INST_0][MESH_0],
+                                                                  config_container[iZone]);
   }
 
   /*--- Get the number of dimensions. ---*/
@@ -221,7 +222,8 @@ void CDeformationDriver::Output_Preprocessing() {
   for (iZone = 0; iZone < nZone; iZone++) {
     /*--- Allocate the mesh output. ---*/
 
-    output_container[iZone] = new CMeshOutput(config_container[iZone], geometry_container[iZone][INST_0][MESH_0]->GetnDim());
+    output_container[iZone] =
+        new CMeshOutput(config_container[iZone], geometry_container[iZone][INST_0][MESH_0]->GetnDim());
 
     /*--- Preprocess the volume output. ---*/
 
@@ -292,7 +294,10 @@ void CDeformationDriver::Run() {
   if (rank == MASTER_NODE) {
     cout << "\nCompleted in " << fixed << UsedTimeCompute << " seconds on " << size;
 
-    if (size == 1) cout << " core." << endl; else cout << " cores." << endl;
+    if (size == 1)
+      cout << " core." << endl;
+    else
+      cout << " cores." << endl;
   }
 
   /*--- Output the deformed mesh. ---*/
@@ -304,7 +309,8 @@ void CDeformationDriver::Update() {
   for (iZone = 0; iZone < nZone; iZone++) {
     /*--- Set the stiffness of each element mesh into the mesh numerics. ---*/
 
-    solver_container[iZone][INST_0][MESH_0][MESH_SOL]->SetMesh_Stiffness(numerics_container[iZone][INST_0][MESH_0][MESH_SOL], config_container[iZone]);
+    solver_container[iZone][INST_0][MESH_0][MESH_SOL]->SetMesh_Stiffness(
+        numerics_container[iZone][INST_0][MESH_0][MESH_SOL], config_container[iZone]);
 
     /*--- Deform the volume grid around the new boundary locations. ---*/
     /*--- Force the number of levels to be 0 because in this driver we do not build MG levels. ---*/
@@ -325,7 +331,8 @@ void CDeformationDriver::Update_Legacy() {
       /*--- Definition of the Class for grid movement. ---*/
 
       grid_movement[iZone] = new CVolumetricMovement*[nInst_Zone]();
-      grid_movement[iZone][INST_0] = new CVolumetricMovement(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
+      grid_movement[iZone][INST_0] =
+          new CVolumetricMovement(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
 
       /*--- Save original coordinates to be reused in convexity checking procedure. ---*/
 
@@ -335,25 +342,32 @@ void CDeformationDriver::Update_Legacy() {
 
       if (config_container[iZone]->GetDesign_Variable(0) == SCALE_GRID) {
         if (rank == MASTER_NODE)
-          cout << endl << "--------------------- Volumetric grid scaling (ZONE " << iZone << ") ------------------" << endl;
-        grid_movement[iZone][INST_0]->SetVolume_Scaling(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], false);
+          cout << endl
+               << "--------------------- Volumetric grid scaling (ZONE " << iZone << ") ------------------" << endl;
+        grid_movement[iZone][INST_0]->SetVolume_Scaling(geometry_container[iZone][INST_0][MESH_0],
+                                                        config_container[iZone], false);
 
       } else if (config_container[iZone]->GetDesign_Variable(0) == TRANSLATE_GRID) {
         if (rank == MASTER_NODE)
-          cout << endl << "------------------- Volumetric grid translation (ZONE " << iZone << ") ----------------" << endl;
-        grid_movement[iZone][INST_0]->SetVolume_Translation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], false);
+          cout << endl
+               << "------------------- Volumetric grid translation (ZONE " << iZone << ") ----------------" << endl;
+        grid_movement[iZone][INST_0]->SetVolume_Translation(geometry_container[iZone][INST_0][MESH_0],
+                                                            config_container[iZone], false);
 
       } else if (config_container[iZone]->GetDesign_Variable(0) == ROTATE_GRID) {
         if (rank == MASTER_NODE)
-          cout << endl << "--------------------- Volumetric grid rotation (ZONE " << iZone << ") -----------------" << endl;
-        grid_movement[iZone][INST_0]->SetVolume_Rotation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], false);
+          cout << endl
+               << "--------------------- Volumetric grid rotation (ZONE " << iZone << ") -----------------" << endl;
+        grid_movement[iZone][INST_0]->SetVolume_Rotation(geometry_container[iZone][INST_0][MESH_0],
+                                                         config_container[iZone], false);
 
       } else {
         /*--- If no volume-type deformations are requested, then this is a
          * surface-based deformation or FFD set up. ---*/
 
         if (rank == MASTER_NODE)
-          cout << endl << "--------------------- Surface grid deformation (ZONE " << iZone << ") -----------------" << endl;
+          cout << endl
+               << "--------------------- Surface grid deformation (ZONE " << iZone << ") -----------------" << endl;
 
         /*--- Definition and initialization of the surface deformation class. ---*/
 
@@ -367,20 +381,24 @@ void CDeformationDriver::Update_Legacy() {
         /*--- Surface grid deformation. ---*/
 
         if (rank == MASTER_NODE) cout << "Performing the deformation of the surface grid." << endl;
-        auto TotalDeformation = surface_movement[iZone]->SetSurface_Deformation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
+        auto TotalDeformation = surface_movement[iZone]->SetSurface_Deformation(
+            geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
 
         if (config_container[iZone]->GetDesign_Variable(0) != FFD_SETTING) {
           if (rank == MASTER_NODE)
-            cout << endl << "------------------- Volumetric grid deformation (ZONE " << iZone << ") ----------------" << endl;
+            cout << endl
+                 << "------------------- Volumetric grid deformation (ZONE " << iZone << ") ----------------" << endl;
 
           if (rank == MASTER_NODE) cout << "Performing the deformation of the volumetric grid." << endl;
-          grid_movement[iZone][INST_0]->SetVolume_Deformation(geometry_container[iZone][INST_0][MESH_0],config_container[iZone], false);
+          grid_movement[iZone][INST_0]->SetVolume_Deformation(geometry_container[iZone][INST_0][MESH_0],
+                                                              config_container[iZone], false);
 
           /*--- Get parameters for convexity check. ---*/
           bool ConvexityCheck;
           unsigned short ConvexityCheck_MaxIter, ConvexityCheck_MaxDepth;
 
-          tie(ConvexityCheck, ConvexityCheck_MaxIter, ConvexityCheck_MaxDepth) = config_container[iZone]->GetConvexityCheck();
+          tie(ConvexityCheck, ConvexityCheck_MaxIter, ConvexityCheck_MaxDepth) =
+              config_container[iZone]->GetConvexityCheck();
 
           /*--- Recursively change deformations if there are non-convex elements. ---*/
 
@@ -397,7 +415,8 @@ void CDeformationDriver::Update_Legacy() {
             unsigned short ConvexityCheckIter, RecursionDepth = 0;
             su2double DeformationFactor = 1.0, DeformationDifference = 1.0;
             for (ConvexityCheckIter = 1; ConvexityCheckIter <= ConvexityCheck_MaxIter; ConvexityCheckIter++) {
-              /*--- Recursively change deformation magnitude (decrease for non-convex elements, increase otherwise). ---*/
+              /*--- Recursively change deformation magnitude (decrease for non-convex elements, increase otherwise).
+               * ---*/
 
               DeformationDifference /= 2.0;
 
@@ -422,7 +441,8 @@ void CDeformationDriver::Update_Legacy() {
 
               for (auto iPoint = 0ul; iPoint < OriginalCoordinates.rows(); iPoint++) {
                 for (auto iDim = 0ul; iDim < OriginalCoordinates.cols(); iDim++) {
-                  geometry_container[iZone][INST_0][MESH_0]->nodes->SetCoord(iPoint, iDim, OriginalCoordinates(iPoint, iDim));
+                  geometry_container[iZone][INST_0][MESH_0]->nodes->SetCoord(iPoint, iDim,
+                                                                             OriginalCoordinates(iPoint, iDim));
                 }
               }
 
@@ -430,7 +450,8 @@ void CDeformationDriver::Update_Legacy() {
 
               for (auto iDV = 0u; iDV < driver_config->GetnDV(); iDV++) {
                 for (auto iDV_Value = 0u; iDV_Value < driver_config->GetnDV_Value(iDV); iDV_Value++) {
-                  config_container[iZone]->SetDV_Value(iDV, iDV_Value,InitialDeformation[iDV][iDV_Value] * DeformationFactor);
+                  config_container[iZone]->SetDV_Value(iDV, iDV_Value,
+                                                       InitialDeformation[iDV][iDV_Value] * DeformationFactor);
                 }
               }
 
@@ -438,13 +459,17 @@ void CDeformationDriver::Update_Legacy() {
 
               if (rank == MASTER_NODE) cout << "Performing the deformation of the surface grid." << endl;
 
-              TotalDeformation = surface_movement[iZone]->SetSurface_Deformation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
+              TotalDeformation = surface_movement[iZone]->SetSurface_Deformation(
+                  geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
 
               if (rank == MASTER_NODE)
-                cout << endl << "------------------- Volumetric grid deformation (ZONE " << iZone << ") ----------------" << endl;
+                cout << endl
+                     << "------------------- Volumetric grid deformation (ZONE " << iZone << ") ----------------"
+                     << endl;
 
               if (rank == MASTER_NODE) cout << "Performing the deformation of the volumetric grid." << endl;
-              grid_movement[iZone][INST_0]->SetVolume_Deformation(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], false);
+              grid_movement[iZone][INST_0]->SetVolume_Deformation(geometry_container[iZone][INST_0][MESH_0],
+                                                                  config_container[iZone], false);
 
               if (rank == MASTER_NODE) {
                 cout << "Number of non-convex elements for iteration " << ConvexityCheckIter << ": ";
@@ -488,7 +513,8 @@ void CDeformationDriver::Output() {
 
     output_container[iZone]->Load_Data(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], nullptr);
 
-    output_container[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone][INST_0][MESH_0],OUTPUT_TYPE::MESH, driver_config->GetMesh_Out_FileName());
+    output_container[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone][INST_0][MESH_0],
+                                         OUTPUT_TYPE::MESH, driver_config->GetMesh_Out_FileName());
 
     /*--- Set the file names for the visualization files. ---*/
 
@@ -499,7 +525,8 @@ void CDeformationDriver::Output() {
       auto FileFormat = config_container[iZone]->GetVolumeOutputFiles();
       if (FileFormat[iFile] != OUTPUT_TYPE::RESTART_ASCII && FileFormat[iFile] != OUTPUT_TYPE::RESTART_BINARY &&
           FileFormat[iFile] != OUTPUT_TYPE::CSV)
-        output_container[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone][INST_0][MESH_0],FileFormat[iFile]);
+        output_container[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone][INST_0][MESH_0],
+                                             FileFormat[iFile]);
     }
   }
 
@@ -508,7 +535,6 @@ void CDeformationDriver::Output() {
         (config_container[ZONE_0]->GetDesign_Variable(0) != SCALE_GRID) &&
         (config_container[ZONE_0]->GetDesign_Variable(0) != TRANSLATE_GRID) &&
         (config_container[ZONE_0]->GetDesign_Variable(0) != ROTATE_GRID)) {
-
       /*--- Write the free form deformation boxes after deformation if defined. ---*/
       if (!haveSurfaceDeformation) {
         if (rank == MASTER_NODE) cout << "No FFD information available." << endl;
@@ -558,6 +584,8 @@ void CDeformationDriver::Postprocessing() {
 }
 
 void CDeformationDriver::CommunicateMeshDisplacements(void) {
-  solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->InitiateComms(geometry_container[ZONE_0][INST_0][MESH_0],config_container[ZONE_0], MESH_DISPLACEMENTS);
-  solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->CompleteComms(geometry_container[ZONE_0][INST_0][MESH_0],config_container[ZONE_0], MESH_DISPLACEMENTS);
+  solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->InitiateComms(geometry_container[ZONE_0][INST_0][MESH_0],
+                                                                    config_container[ZONE_0], MESH_DISPLACEMENTS);
+  solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->CompleteComms(geometry_container[ZONE_0][INST_0][MESH_0],
+                                                                    config_container[ZONE_0], MESH_DISPLACEMENTS);
 }
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index ddab47fc4f9..db2a64f4961 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -42,7 +42,6 @@ using namespace std;
 
 CDiscAdjDeformationDriver::CDiscAdjDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
     : CDriverBase(confFile, 1, MPICommunicator) {
-
 /*--- Initialize MeDiPack (must also be here to initialize it from Python). ---*/
 #ifdef HAVE_MPI
 #if defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)
@@ -122,13 +121,15 @@ void CDiscAdjDeformationDriver::Input_Preprocessing() {
       strcpy(zone_file_name, driver_config->GetConfigFilename(iZone).c_str());
       config_container[iZone] = new CConfig(driver_config, zone_file_name, SU2_COMPONENT::SU2_DOT, iZone, nZone, true);
     } else {
-      config_container[iZone] = new CConfig(driver_config, config_file_name, SU2_COMPONENT::SU2_DOT, iZone, nZone, true);
+      config_container[iZone] =
+          new CConfig(driver_config, config_file_name, SU2_COMPONENT::SU2_DOT, iZone, nZone, true);
     }
 
     config_container[iZone]->SetMPICommunicator(SU2_MPI::GetComm());
 
     if (!config_container[iZone]->GetDiscrete_Adjoint() && !config_container[iZone]->GetContinuous_Adjoint()) {
-      SU2_MPI::Error("An adjoint solver (discrete or continuous) was not specified in the configuration file.", CURRENT_FUNCTION);
+      SU2_MPI::Error("An adjoint solver (discrete or continuous) was not specified in the configuration file.",
+                     CURRENT_FUNCTION);
     }
   }
 
@@ -296,7 +297,8 @@ void CDiscAdjDeformationDriver::Preprocess() {
       unsigned short nInst_Zone = nInst[iZone];
 
       grid_movement[iZone] = new CVolumetricMovement*[nInst_Zone]();
-      grid_movement[iZone][INST_0] = new CVolumetricMovement(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
+      grid_movement[iZone][INST_0] =
+          new CVolumetricMovement(geometry_container[iZone][INST_0][MESH_0], config_container[iZone]);
 
       /*--- Read in sensitivities from file. ---*/
 
@@ -358,10 +360,12 @@ void CDiscAdjDeformationDriver::Run() {
           DerivativeTreatment_Gradient(geometry_container[iZone][INST_0][MESH_0], config_container[iZone],
                                        grid_movement[iZone][INST_0], surface_movement[iZone], Gradient);
         } else {
-          SetProjection_AD(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], surface_movement[iZone], Gradient);
+          SetProjection_AD(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], surface_movement[iZone],
+                           Gradient);
         }
       } else {
-        SetProjection_FD(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], surface_movement[iZone], Gradient);
+        SetProjection_FD(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], surface_movement[iZone],
+                         Gradient);
       }
     }
   }
@@ -417,7 +421,10 @@ void CDiscAdjDeformationDriver::SetProjection_FD(CGeometry* geometry, CConfig* c
   for (iDV = 0; iDV < nDV; iDV++) {
     nDV_Value = config->GetnDV_Value(iDV);
     if (nDV_Value != 1) {
-      SU2_MPI::Error("The projection using finite differences currently only supports a fixed direction of movement for FFD points.", CURRENT_FUNCTION);
+      SU2_MPI::Error(
+          "The projection using finite differences currently only supports a fixed direction of movement for FFD "
+          "points.",
+          CURRENT_FUNCTION);
     }
   }
 
@@ -759,7 +766,6 @@ void CDiscAdjDeformationDriver::SetProjection_AD(CGeometry* geometry, CConfig* c
 }
 
 void CDiscAdjDeformationDriver::OutputGradient(su2double** Gradient, CConfig* config, ofstream& Gradient_file) {
-
   unsigned short nDV, iDV, iDV_Value, nDV_Value;
 
   int rank = SU2_MPI::GetRank();
@@ -782,7 +788,8 @@ void CDiscAdjDeformationDriver::OutputGradient(su2double** Gradient, CConfig* co
 
       /*--- Print the kind of objective function to screen. ---*/
 
-      for (std::map<string, ENUM_OBJECTIVE>::const_iterator it = Objective_Map.begin(); it != Objective_Map.end(); ++it) {
+      for (std::map<string, ENUM_OBJECTIVE>::const_iterator it = Objective_Map.begin(); it != Objective_Map.end();
+           ++it) {
         if (it->second == config->GetKind_ObjFunc()) {
           cout << it->first << " gradient : ";
           if (iDV == 0) Gradient_file << it->first << " gradient " << endl;
@@ -842,7 +849,8 @@ void CDiscAdjDeformationDriver::SetSensitivity_Files(CGeometry**** geometry, CCo
     for (iPoint = 0; iPoint < nPoint; iPoint++) {
       for (iDim = 0; iDim < nDim; iDim++) {
         solver->GetNodes()->SetSolution(iPoint, iDim, geometry[iZone][INST_0][MESH_0]->nodes->GetCoord(iPoint, iDim));
-        solver->GetNodes()->SetSolution(iPoint, iDim + nDim, geometry[iZone][INST_0][MESH_0]->GetSensitivity(iPoint, iDim));
+        solver->GetNodes()->SetSolution(iPoint, iDim + nDim,
+                                        geometry[iZone][INST_0][MESH_0]->GetSensitivity(iPoint, iDim));
       }
     }
 
@@ -954,7 +962,7 @@ void CDiscAdjDeformationDriver::DerivativeTreatment_MeshSensitivity(CGeometry* g
 
       solver->WriteSensToGeometry(geometry);
 
-    /*--- Work with the volume derivatives. ---*/
+      /*--- Work with the volume derivatives. ---*/
     } else {
       /*--- Get the sensitivities from the geometry class to work with. ---*/
 
@@ -1001,7 +1009,7 @@ void CDiscAdjDeformationDriver::DerivativeTreatment_Gradient(CGeometry* geometry
   if (config->GetSobMode() == ENUM_SOBOLEV_MODUS::PARAM_LEVEL_COMPLETE) {
     solver->ApplyGradientSmoothingDV(geometry, numerics.get(), surface_movement, grid_movement, config, Gradient);
 
-  /*--- If smoothing already took place on the mesh level, or none is requested, just do standard projection. ---*/
+    /*--- If smoothing already took place on the mesh level, or none is requested, just do standard projection. ---*/
   } else if (config->GetSobMode() == ENUM_SOBOLEV_MODUS::ONLY_GRAD ||
              config->GetSobMode() == ENUM_SOBOLEV_MODUS::MESH_LEVEL) {
     solver->RecordTapeAndCalculateOriginalGradient(geometry, surface_movement, grid_movement, config, Gradient);
diff --git a/SU2_DOT/src/SU2_DOT.cpp b/SU2_DOT/src/SU2_DOT.cpp
index b8b606ca75c..f66dd007b35 100644
--- a/SU2_DOT/src/SU2_DOT.cpp
+++ b/SU2_DOT/src/SU2_DOT.cpp
@@ -28,7 +28,6 @@
 #include "../../SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp"
 
 int main(int argc, char* argv[]) {
-
   char config_file_name[MAX_STRING_SIZE];
 
   /*--- MPI initialization. ---*/
diff --git a/SU2_GEO/include/SU2_GEO.hpp b/SU2_GEO/include/SU2_GEO.hpp
index 9752149364e..2b2a31f9c4a 100644
--- a/SU2_GEO/include/SU2_GEO.hpp
+++ b/SU2_GEO/include/SU2_GEO.hpp
@@ -26,7 +26,6 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #pragma once
 
 #include "../../Common/include/parallelization/mpi_structure.hpp"
diff --git a/SU2_GEO/src/SU2_GEO.cpp b/SU2_GEO/src/SU2_GEO.cpp
index ffe89dd510a..59ec6cf2107 100644
--- a/SU2_GEO/src/SU2_GEO.cpp
+++ b/SU2_GEO/src/SU2_GEO.cpp
@@ -25,31 +25,48 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #include "../include/SU2_GEO.hpp"
 using namespace std;
 
-int main(int argc, char *argv[]) {
-
+int main(int argc, char* argv[]) {
   unsigned short iZone, nZone = SINGLE_ZONE;
   su2double StartTime = 0.0, StopTime = 0.0, UsedTime = 0.0;
   unsigned short iDV, iFFDBox, iPlane, nPlane, iVar;
-  su2double *ObjectiveFunc, *ObjectiveFunc_New, *Gradient, delta_eps,
-  **Plane_P0, **Plane_Normal,
-
-  Fuselage_Volume = 0.0, Fuselage_WettedArea = 0.0, Fuselage_MinWidth = 0.0, Fuselage_MaxWidth = 0.0, Fuselage_MinWaterLineWidth = 0.0, Fuselage_MaxWaterLineWidth = 0.0, Fuselage_MinHeight = 0.0, Fuselage_MaxHeight = 0.0, Fuselage_MaxCurvature = 0.0,
-  Fuselage_Volume_New = 0.0, Fuselage_WettedArea_New = 0.0, Fuselage_MinWidth_New = 0.0, Fuselage_MaxWidth_New = 0.0, Fuselage_MinWaterLineWidth_New = 0.0, Fuselage_MaxWaterLineWidth_New = 0.0, Fuselage_MinHeight_New = 0.0, Fuselage_MaxHeight_New = 0.0, Fuselage_MaxCurvature_New = 0.0,
-  Fuselage_Volume_Grad = 0.0, Fuselage_WettedArea_Grad = 0.0, Fuselage_MinWidth_Grad = 0.0, Fuselage_MaxWidth_Grad = 0.0, Fuselage_MinWaterLineWidth_Grad = 0.0, Fuselage_MaxWaterLineWidth_Grad = 0.0, Fuselage_MinHeight_Grad = 0.0, Fuselage_MaxHeight_Grad = 0.0, Fuselage_MaxCurvature_Grad = 0.0,
-
-  Wing_Volume = 0.0, Wing_MinThickness = 0.0, Wing_MaxThickness = 0.0, Wing_MinChord = 0.0, Wing_MaxChord = 0.0, Wing_MinLERadius = 0.0, Wing_MaxLERadius = 0.0, Wing_MinToC = 0.0, Wing_MaxToC = 0.0, Wing_ObjFun_MinToC = 0.0, Wing_MaxTwist = 0.0, Wing_MaxCurvature = 0.0, Wing_MaxDihedral = 0.0,
-  Wing_Volume_New = 0.0, Wing_MinThickness_New = 0.0, Wing_MaxThickness_New = 0.0, Wing_MinChord_New = 0.0, Wing_MaxChord_New = 0.0, Wing_MinLERadius_New = 0.0, Wing_MaxLERadius_New = 0.0, Wing_MinToC_New = 0.0, Wing_MaxToC_New = 0.0, Wing_ObjFun_MinToC_New = 0.0, Wing_MaxTwist_New = 0.0, Wing_MaxCurvature_New = 0.0, Wing_MaxDihedral_New = 0.0,
-  Wing_Volume_Grad = 0.0, Wing_MinThickness_Grad = 0.0, Wing_MaxThickness_Grad = 0.0, Wing_MinChord_Grad = 0.0, Wing_MaxChord_Grad = 0.0, Wing_MinLERadius_Grad = 0.0, Wing_MaxLERadius_Grad = 0.0, Wing_MinToC_Grad = 0.0, Wing_MaxToC_Grad = 0.0, Wing_ObjFun_MinToC_Grad = 0.0, Wing_MaxTwist_Grad = 0.0, Wing_MaxCurvature_Grad = 0.0, Wing_MaxDihedral_Grad = 0.0,
-
-  Nacelle_Volume = 0.0, Nacelle_MinThickness = 0.0, Nacelle_MaxThickness = 0.0, Nacelle_MinChord = 0.0, Nacelle_MaxChord = 0.0, Nacelle_MinLERadius = 0.0, Nacelle_MaxLERadius = 0.0, Nacelle_MinToC = 0.0, Nacelle_MaxToC = 0.0, Nacelle_ObjFun_MinToC = 0.0, Nacelle_MaxTwist = 0.0,
-  Nacelle_Volume_New = 0.0, Nacelle_MinThickness_New = 0.0, Nacelle_MaxThickness_New = 0.0, Nacelle_MinChord_New = 0.0, Nacelle_MaxChord_New = 0.0, Nacelle_MinLERadius_New = 0.0, Nacelle_MaxLERadius_New = 0.0, Nacelle_MinToC_New = 0.0, Nacelle_MaxToC_New = 0.0, Nacelle_ObjFun_MinToC_New = 0.0, Nacelle_MaxTwist_New = 0.0,
-  Nacelle_Volume_Grad = 0.0, Nacelle_MinThickness_Grad = 0.0, Nacelle_MaxThickness_Grad = 0.0, Nacelle_MinChord_Grad = 0.0, Nacelle_MaxChord_Grad = 0.0, Nacelle_MinLERadius_Grad = 0.0, Nacelle_MaxLERadius_Grad = 0.0, Nacelle_MinToC_Grad = 0.0, Nacelle_MaxToC_Grad = 0.0, Nacelle_ObjFun_MinToC_Grad = 0.0, Nacelle_MaxTwist_Grad = 0.0;
-
-  vector<su2double> *Xcoord_Airfoil, *Ycoord_Airfoil, *Zcoord_Airfoil, *Variable_Airfoil;
+  su2double *ObjectiveFunc, *ObjectiveFunc_New, *Gradient, delta_eps, **Plane_P0, **Plane_Normal,
+
+      Fuselage_Volume = 0.0, Fuselage_WettedArea = 0.0, Fuselage_MinWidth = 0.0, Fuselage_MaxWidth = 0.0,
+      Fuselage_MinWaterLineWidth = 0.0, Fuselage_MaxWaterLineWidth = 0.0, Fuselage_MinHeight = 0.0,
+      Fuselage_MaxHeight = 0.0, Fuselage_MaxCurvature = 0.0, Fuselage_Volume_New = 0.0, Fuselage_WettedArea_New = 0.0,
+      Fuselage_MinWidth_New = 0.0, Fuselage_MaxWidth_New = 0.0, Fuselage_MinWaterLineWidth_New = 0.0,
+      Fuselage_MaxWaterLineWidth_New = 0.0, Fuselage_MinHeight_New = 0.0, Fuselage_MaxHeight_New = 0.0,
+      Fuselage_MaxCurvature_New = 0.0, Fuselage_Volume_Grad = 0.0, Fuselage_WettedArea_Grad = 0.0,
+      Fuselage_MinWidth_Grad = 0.0, Fuselage_MaxWidth_Grad = 0.0, Fuselage_MinWaterLineWidth_Grad = 0.0,
+      Fuselage_MaxWaterLineWidth_Grad = 0.0, Fuselage_MinHeight_Grad = 0.0, Fuselage_MaxHeight_Grad = 0.0,
+      Fuselage_MaxCurvature_Grad = 0.0,
+
+      Wing_Volume = 0.0, Wing_MinThickness = 0.0, Wing_MaxThickness = 0.0, Wing_MinChord = 0.0, Wing_MaxChord = 0.0,
+      Wing_MinLERadius = 0.0, Wing_MaxLERadius = 0.0, Wing_MinToC = 0.0, Wing_MaxToC = 0.0, Wing_ObjFun_MinToC = 0.0,
+      Wing_MaxTwist = 0.0, Wing_MaxCurvature = 0.0, Wing_MaxDihedral = 0.0, Wing_Volume_New = 0.0,
+      Wing_MinThickness_New = 0.0, Wing_MaxThickness_New = 0.0, Wing_MinChord_New = 0.0, Wing_MaxChord_New = 0.0,
+      Wing_MinLERadius_New = 0.0, Wing_MaxLERadius_New = 0.0, Wing_MinToC_New = 0.0, Wing_MaxToC_New = 0.0,
+      Wing_ObjFun_MinToC_New = 0.0, Wing_MaxTwist_New = 0.0, Wing_MaxCurvature_New = 0.0, Wing_MaxDihedral_New = 0.0,
+      Wing_Volume_Grad = 0.0, Wing_MinThickness_Grad = 0.0, Wing_MaxThickness_Grad = 0.0, Wing_MinChord_Grad = 0.0,
+      Wing_MaxChord_Grad = 0.0, Wing_MinLERadius_Grad = 0.0, Wing_MaxLERadius_Grad = 0.0, Wing_MinToC_Grad = 0.0,
+      Wing_MaxToC_Grad = 0.0, Wing_ObjFun_MinToC_Grad = 0.0, Wing_MaxTwist_Grad = 0.0, Wing_MaxCurvature_Grad = 0.0,
+      Wing_MaxDihedral_Grad = 0.0,
+
+      Nacelle_Volume = 0.0, Nacelle_MinThickness = 0.0, Nacelle_MaxThickness = 0.0, Nacelle_MinChord = 0.0,
+      Nacelle_MaxChord = 0.0, Nacelle_MinLERadius = 0.0, Nacelle_MaxLERadius = 0.0, Nacelle_MinToC = 0.0,
+      Nacelle_MaxToC = 0.0, Nacelle_ObjFun_MinToC = 0.0, Nacelle_MaxTwist = 0.0, Nacelle_Volume_New = 0.0,
+      Nacelle_MinThickness_New = 0.0, Nacelle_MaxThickness_New = 0.0, Nacelle_MinChord_New = 0.0,
+      Nacelle_MaxChord_New = 0.0, Nacelle_MinLERadius_New = 0.0, Nacelle_MaxLERadius_New = 0.0,
+      Nacelle_MinToC_New = 0.0, Nacelle_MaxToC_New = 0.0, Nacelle_ObjFun_MinToC_New = 0.0, Nacelle_MaxTwist_New = 0.0,
+      Nacelle_Volume_Grad = 0.0, Nacelle_MinThickness_Grad = 0.0, Nacelle_MaxThickness_Grad = 0.0,
+      Nacelle_MinChord_Grad = 0.0, Nacelle_MaxChord_Grad = 0.0, Nacelle_MinLERadius_Grad = 0.0,
+      Nacelle_MaxLERadius_Grad = 0.0, Nacelle_MinToC_Grad = 0.0, Nacelle_MaxToC_Grad = 0.0,
+      Nacelle_ObjFun_MinToC_Grad = 0.0, Nacelle_MaxTwist_Grad = 0.0;
+
+  vector<su2double>*Xcoord_Airfoil, *Ycoord_Airfoil, *Zcoord_Airfoil, *Variable_Airfoil;
   vector<su2double> Xcoord_Fan, Ycoord_Fan, Zcoord_Fan;
   char config_file_name[MAX_STRING_SIZE];
   bool Local_MoveSurface, MoveSurface = false;
@@ -58,7 +75,7 @@ int main(int argc, char *argv[]) {
 
   /*--- MPI initialization ---*/
 
-  SU2_MPI::Init(&argc,&argv);
+  SU2_MPI::Init(&argc, &argv);
   SU2_MPI::Comm MPICommunicator = SU2_MPI::GetComm();
 
   rank = SU2_MPI::GetRank();
@@ -66,25 +83,28 @@ int main(int argc, char *argv[]) {
 
   /*--- Pointer to different structures that will be used throughout the entire code ---*/
 
-  CConfig **config_container          = nullptr;
-  CGeometry **geometry_container      = nullptr;
-  CSurfaceMovement *surface_movement  = nullptr;
-  CFreeFormDefBox** FFDBox            = nullptr;
+  CConfig** config_container = nullptr;
+  CGeometry** geometry_container = nullptr;
+  CSurfaceMovement* surface_movement = nullptr;
+  CFreeFormDefBox** FFDBox = nullptr;
 
   /*--- Load in the number of zones and spatial dimensions in the mesh file (if no config
    file is specified, default.cfg is used) ---*/
 
-  if (argc == 2) { strcpy(config_file_name,argv[1]); }
-  else { strcpy(config_file_name, "default.cfg"); }
+  if (argc == 2) {
+    strcpy(config_file_name, argv[1]);
+  } else {
+    strcpy(config_file_name, "default.cfg");
+  }
 
   /*--- Read the name and format of the input mesh file to get from the mesh
    file the number of zones and dimensions from the numerical grid (required
    for variables allocation)  ---*/
 
-  CConfig *config = nullptr;
+  CConfig* config = nullptr;
   config = new CConfig(config_file_name, SU2_COMPONENT::SU2_GEO);
 
-  nZone    = config->GetnZone();
+  nZone = config->GetnZone();
 
   /*--- Definition of the containers per zones ---*/
 
@@ -92,8 +112,8 @@ int main(int argc, char *argv[]) {
   geometry_container = new CGeometry*[nZone];
 
   for (iZone = 0; iZone < nZone; iZone++) {
-    config_container[iZone]       = nullptr;
-    geometry_container[iZone]     = nullptr;
+    config_container[iZone] = nullptr;
+    geometry_container[iZone] = nullptr;
   }
 
   /*--- Loop over all zones to initialize the various classes. In most
@@ -101,7 +121,6 @@ int main(int argc, char *argv[]) {
    differential equation on a single block, unstructured mesh. ---*/
 
   for (iZone = 0; iZone < nZone; iZone++) {
-
     /*--- Definition of the configuration option class for all zones. In this
      constructor, the input configuration file is parsed and all options are
      read and stored. ---*/
@@ -111,7 +130,7 @@ int main(int argc, char *argv[]) {
 
     /*--- Definition of the geometry class to store the primal grid in the partitioning process. ---*/
 
-    CGeometry *geometry_aux = nullptr;
+    CGeometry* geometry_aux = nullptr;
 
     /*--- All ranks process the grid and call ParMETIS for partitioning ---*/
 
@@ -136,7 +155,6 @@ int main(int argc, char *argv[]) {
     /*--- Add the Send/Receive boundaries ---*/
 
     geometry_container[iZone]->SetBoundaries(config_container[iZone]);
-
   }
 
   bool tabTecplot = config_container[ZONE_0]->GetTabular_FileFormat() == TAB_OUTPUT::TAB_TECPLOT;
@@ -148,12 +166,14 @@ int main(int argc, char *argv[]) {
   /*--- Evaluation of the objective function ---*/
 
   if (rank == MASTER_NODE)
-    cout << endl <<"----------------------- Preprocessing computations ----------------------" << endl;
+    cout << endl << "----------------------- Preprocessing computations ----------------------" << endl;
 
   /*--- Set the number of sections, and allocate the memory ---*/
 
-  if (geometry_container[ZONE_0]->GetnDim() == 2) nPlane = 1;
-  else nPlane = config_container[ZONE_0]->GetnLocationStations();
+  if (geometry_container[ZONE_0]->GetnDim() == 2)
+    nPlane = 1;
+  else
+    nPlane = config_container[ZONE_0]->GetnLocationStations();
 
   Xcoord_Airfoil = new vector<su2double>[nPlane];
   Ycoord_Airfoil = new vector<su2double>[nPlane];
@@ -162,38 +182,38 @@ int main(int argc, char *argv[]) {
 
   Plane_P0 = new su2double*[nPlane];
   Plane_Normal = new su2double*[nPlane];
-  for(iPlane = 0; iPlane < nPlane; iPlane++ ) {
+  for (iPlane = 0; iPlane < nPlane; iPlane++) {
     Plane_P0[iPlane] = new su2double[3];
     Plane_Normal[iPlane] = new su2double[3];
   }
 
-  ObjectiveFunc = new su2double[nPlane*20];
-  ObjectiveFunc_New = new su2double[nPlane*20];
-  Gradient = new su2double[nPlane*20];
+  ObjectiveFunc = new su2double[nPlane * 20];
+  ObjectiveFunc_New = new su2double[nPlane * 20];
+  Gradient = new su2double[nPlane * 20];
 
-  for (iVar = 0; iVar < nPlane*20; iVar++) {
+  for (iVar = 0; iVar < nPlane * 20; iVar++) {
     ObjectiveFunc[iVar] = 0.0;
     ObjectiveFunc_New[iVar] = 0.0;
     Gradient[iVar] = 0.0;
   }
 
-
   /*--- Compute elements surrounding points, points surrounding points ---*/
 
-  if (rank == MASTER_NODE) cout << "Setting local point connectivity." <<endl;
+  if (rank == MASTER_NODE) cout << "Setting local point connectivity." << endl;
   geometry_container[ZONE_0]->SetPoint_Connectivity();
 
   /*--- Check the orientation before computing geometrical quantities ---*/
 
   if (config_container[ZONE_0]->GetReorientElements()) {
-    if (rank == MASTER_NODE) cout << "Checking the numerical grid orientation of the interior elements." <<endl;
+    if (rank == MASTER_NODE) cout << "Checking the numerical grid orientation of the interior elements." << endl;
     geometry_container[ZONE_0]->Check_IntElem_Orientation(config_container[ZONE_0]);
   }
 
   /*--- Create the edge structure ---*/
 
-  if (rank == MASTER_NODE) cout << "Identify edges and vertices." <<endl;
-  geometry_container[ZONE_0]->SetEdges(); geometry_container[ZONE_0]->SetVertex(config_container[ZONE_0]);
+  if (rank == MASTER_NODE) cout << "Identify edges and vertices." << endl;
+  geometry_container[ZONE_0]->SetEdges();
+  geometry_container[ZONE_0]->SetVertex(config_container[ZONE_0]);
 
   /*--- Create the dual control volume structures ---*/
 
@@ -218,37 +238,43 @@ int main(int argc, char *argv[]) {
   if (rank == MASTER_NODE) cout << "Set plane structure." << endl;
 
   if (geometry_container[ZONE_0]->GetnDim() == 2) {
-    Plane_Normal[0][0] = 0.0;   Plane_P0[0][0] = 0.0;
-    Plane_Normal[0][1] = 1.0;   Plane_P0[0][1] = 0.0;
-    Plane_Normal[0][2] = 0.0;   Plane_P0[0][2] = 0.0;
-  }
-  else if (geometry_container[ZONE_0]->GetnDim() == 3) {
+    Plane_Normal[0][0] = 0.0;
+    Plane_P0[0][0] = 0.0;
+    Plane_Normal[0][1] = 1.0;
+    Plane_P0[0][1] = 0.0;
+    Plane_Normal[0][2] = 0.0;
+    Plane_P0[0][2] = 0.0;
+  } else if (geometry_container[ZONE_0]->GetnDim() == 3) {
     for (iPlane = 0; iPlane < nPlane; iPlane++) {
-      Plane_Normal[iPlane][0] = 0.0;    Plane_P0[iPlane][0] = 0.0;
-      Plane_Normal[iPlane][1] = 0.0;    Plane_P0[iPlane][1] = 0.0;
-      Plane_Normal[iPlane][2] = 0.0;    Plane_P0[iPlane][2] = 0.0;
+      Plane_Normal[iPlane][0] = 0.0;
+      Plane_P0[iPlane][0] = 0.0;
+      Plane_Normal[iPlane][1] = 0.0;
+      Plane_P0[iPlane][1] = 0.0;
+      Plane_Normal[iPlane][2] = 0.0;
+      Plane_P0[iPlane][2] = 0.0;
 
       if (config_container[ZONE_0]->GetGeo_Description() == FUSELAGE) {
         Plane_Normal[iPlane][0] = 1.0;
         Plane_P0[iPlane][0] = config_container[ZONE_0]->GetLocationStations(iPlane);
-      }
-      else if (config_container[ZONE_0]->GetGeo_Description() == NACELLE) {
+      } else if (config_container[ZONE_0]->GetGeo_Description() == NACELLE) {
         Plane_Normal[iPlane][0] = 0.0;
-        Plane_Normal[iPlane][1] = -sin(config_container[ZONE_0]->GetLocationStations(iPlane)*PI_NUMBER/180.0);
-        Plane_Normal[iPlane][2] = cos(config_container[ZONE_0]->GetLocationStations(iPlane)*PI_NUMBER/180.0);
+        Plane_Normal[iPlane][1] = -sin(config_container[ZONE_0]->GetLocationStations(iPlane) * PI_NUMBER / 180.0);
+        Plane_Normal[iPlane][2] = cos(config_container[ZONE_0]->GetLocationStations(iPlane) * PI_NUMBER / 180.0);
 
         /*--- Apply tilt angle to the plane ---*/
 
-        su2double Tilt_Angle = config_container[ZONE_0]->GetNacelleLocation(3)*PI_NUMBER/180;
-        su2double Plane_NormalX_Tilt = Plane_Normal[iPlane][0]*cos(Tilt_Angle) + Plane_Normal[iPlane][2]*sin(Tilt_Angle);
+        su2double Tilt_Angle = config_container[ZONE_0]->GetNacelleLocation(3) * PI_NUMBER / 180;
+        su2double Plane_NormalX_Tilt =
+            Plane_Normal[iPlane][0] * cos(Tilt_Angle) + Plane_Normal[iPlane][2] * sin(Tilt_Angle);
         su2double Plane_NormalY_Tilt = Plane_Normal[iPlane][1];
-        su2double Plane_NormalZ_Tilt = Plane_Normal[iPlane][2]*cos(Tilt_Angle) - Plane_Normal[iPlane][0]*sin(Tilt_Angle);
+        su2double Plane_NormalZ_Tilt =
+            Plane_Normal[iPlane][2] * cos(Tilt_Angle) - Plane_Normal[iPlane][0] * sin(Tilt_Angle);
 
         /*--- Apply toe angle to the plane ---*/
 
-        su2double Toe_Angle = config_container[ZONE_0]->GetNacelleLocation(4)*PI_NUMBER/180;
-        su2double Plane_NormalX_Tilt_Toe = Plane_NormalX_Tilt*cos(Toe_Angle) - Plane_NormalY_Tilt*sin(Toe_Angle);
-        su2double Plane_NormalY_Tilt_Toe = Plane_NormalX_Tilt*sin(Toe_Angle) + Plane_NormalY_Tilt*cos(Toe_Angle);
+        su2double Toe_Angle = config_container[ZONE_0]->GetNacelleLocation(4) * PI_NUMBER / 180;
+        su2double Plane_NormalX_Tilt_Toe = Plane_NormalX_Tilt * cos(Toe_Angle) - Plane_NormalY_Tilt * sin(Toe_Angle);
+        su2double Plane_NormalY_Tilt_Toe = Plane_NormalX_Tilt * sin(Toe_Angle) + Plane_NormalY_Tilt * cos(Toe_Angle);
         su2double Plane_NormalZ_Tilt_Toe = Plane_NormalZ_Tilt;
 
         /*--- Update normal vector ---*/
@@ -262,321 +288,432 @@ int main(int argc, char *argv[]) {
         Plane_P0[iPlane][0] = config_container[ZONE_0]->GetNacelleLocation(0);
         Plane_P0[iPlane][1] = config_container[ZONE_0]->GetNacelleLocation(1);
         Plane_P0[iPlane][2] = config_container[ZONE_0]->GetNacelleLocation(2);
-      }
-      else {
+      } else {
         Plane_Normal[iPlane][1] = 1.0;
         Plane_P0[iPlane][1] = config_container[ZONE_0]->GetLocationStations(iPlane);
       }
-
     }
   }
 
   /*--- Compute the wing and fan description (only 3D). ---*/
 
   if (geometry_container[ZONE_0]->GetnDim() == 3) {
-
     if (config_container[ZONE_0]->GetGeo_Description() == FUSELAGE) {
-
       if (rank == MASTER_NODE) {
         cout << "Computing the fuselage continuous description." << endl << endl;
       }
 
-      geometry_container[ZONE_0]->Compute_Fuselage(config_container[ZONE_0], true,
-                                                   Fuselage_Volume, Fuselage_WettedArea, Fuselage_MinWidth, Fuselage_MaxWidth,
-                                                   Fuselage_MinWaterLineWidth, Fuselage_MaxWaterLineWidth,
-                                                   Fuselage_MinHeight, Fuselage_MaxHeight,
+      geometry_container[ZONE_0]->Compute_Fuselage(config_container[ZONE_0], true, Fuselage_Volume, Fuselage_WettedArea,
+                                                   Fuselage_MinWidth, Fuselage_MaxWidth, Fuselage_MinWaterLineWidth,
+                                                   Fuselage_MaxWaterLineWidth, Fuselage_MinHeight, Fuselage_MaxHeight,
                                                    Fuselage_MaxCurvature);
 
       /*--- Screen output for the wing definition ---*/
 
       if (rank == MASTER_NODE) {
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Fuselage volume: "    << Fuselage_Volume << " in^3. ";
-        else cout << "Fuselage volume: "    << Fuselage_Volume << " m^3. ";
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Fuselage wetted area: "    << Fuselage_WettedArea << " in^2. " << endl;
-        else cout << "Fuselage wetted area: "    << Fuselage_WettedArea << " m^2. " << endl;
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Fuselage min. width: "  << Fuselage_MinWidth << " in. ";
-        else cout << "Fuselage min. width: "  << Fuselage_MinWidth << " m. ";
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Fuselage max. width: "  << Fuselage_MaxWidth << " in. " << endl;
-        else cout << "Fuselage max. width: "  << Fuselage_MaxWidth << " m. " << endl;
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Fuselage min. waterline width: "  << Fuselage_MinWaterLineWidth << " in. ";
-        else cout << "Fuselage min. waterline width: "  << Fuselage_MinWaterLineWidth << " m. ";
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Fuselage max. waterline width: "  << Fuselage_MaxWaterLineWidth << " in. " << endl;
-        else cout << "Fuselage max. waterline width: "  << Fuselage_MaxWaterLineWidth << " m. " << endl;
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Fuselage min. height: "  << Fuselage_MinHeight << " in. ";
-        else cout << "Fuselage min. height: "  << Fuselage_MinHeight << " m. ";
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Fuselage max. height: "  << Fuselage_MaxHeight << " in. " << endl;
-        else cout << "Fuselage max. height: "  << Fuselage_MaxHeight << " m. " << endl;
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Fuselage max. curvature: "  << Fuselage_MaxCurvature << " 1/in. " << endl;
-        else cout << "Fuselage max. curvature: "  << Fuselage_MaxCurvature << " 1/m. " << endl;
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Fuselage volume: " << Fuselage_Volume << " in^3. ";
+        else
+          cout << "Fuselage volume: " << Fuselage_Volume << " m^3. ";
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Fuselage wetted area: " << Fuselage_WettedArea << " in^2. " << endl;
+        else
+          cout << "Fuselage wetted area: " << Fuselage_WettedArea << " m^2. " << endl;
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Fuselage min. width: " << Fuselage_MinWidth << " in. ";
+        else
+          cout << "Fuselage min. width: " << Fuselage_MinWidth << " m. ";
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Fuselage max. width: " << Fuselage_MaxWidth << " in. " << endl;
+        else
+          cout << "Fuselage max. width: " << Fuselage_MaxWidth << " m. " << endl;
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Fuselage min. waterline width: " << Fuselage_MinWaterLineWidth << " in. ";
+        else
+          cout << "Fuselage min. waterline width: " << Fuselage_MinWaterLineWidth << " m. ";
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Fuselage max. waterline width: " << Fuselage_MaxWaterLineWidth << " in. " << endl;
+        else
+          cout << "Fuselage max. waterline width: " << Fuselage_MaxWaterLineWidth << " m. " << endl;
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Fuselage min. height: " << Fuselage_MinHeight << " in. ";
+        else
+          cout << "Fuselage min. height: " << Fuselage_MinHeight << " m. ";
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Fuselage max. height: " << Fuselage_MaxHeight << " in. " << endl;
+        else
+          cout << "Fuselage max. height: " << Fuselage_MaxHeight << " m. " << endl;
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Fuselage max. curvature: " << Fuselage_MaxCurvature << " 1/in. " << endl;
+        else
+          cout << "Fuselage max. curvature: " << Fuselage_MaxCurvature << " 1/m. " << endl;
       }
 
     }
 
     else if (config_container[ZONE_0]->GetGeo_Description() == NACELLE) {
-
       if (rank == MASTER_NODE) {
         cout << "Computing the nacelle continuous description." << endl << endl;
       }
 
-      geometry_container[ZONE_0]->Compute_Nacelle(config_container[ZONE_0], true,
-                                               Nacelle_Volume, Nacelle_MinThickness, Nacelle_MaxThickness, Nacelle_MinChord, Nacelle_MaxChord,
-                                               Nacelle_MinLERadius, Nacelle_MaxLERadius, Nacelle_MinToC, Nacelle_MaxToC, Nacelle_ObjFun_MinToC,
-                                               Nacelle_MaxTwist);
+      geometry_container[ZONE_0]->Compute_Nacelle(config_container[ZONE_0], true, Nacelle_Volume, Nacelle_MinThickness,
+                                                  Nacelle_MaxThickness, Nacelle_MinChord, Nacelle_MaxChord,
+                                                  Nacelle_MinLERadius, Nacelle_MaxLERadius, Nacelle_MinToC,
+                                                  Nacelle_MaxToC, Nacelle_ObjFun_MinToC, Nacelle_MaxTwist);
 
       /*--- Screen output for the wing definition ---*/
 
       if (rank == MASTER_NODE) {
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Nacelle volume: "    << Nacelle_Volume << " in^3. ";
-        else cout << "Nacelle volume: "    << Nacelle_Volume << " m^3. ";
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Nacelle min. thickness: "  << Nacelle_MinThickness << " in. ";
-        else cout << "Nacelle min. thickness: "  << Nacelle_MinThickness << " m. ";
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Nacelle max. thickness: "  << Nacelle_MaxThickness << " in. " << endl;
-        else cout << "Nacelle max. thickness: "  << Nacelle_MaxThickness << " m. " << endl;
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Nacelle min. chord: "  << Nacelle_MinChord << " in. ";
-        else cout << "Nacelle min. chord: "  << Nacelle_MinChord << " m. ";
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Nacelle max. chord: "  << Nacelle_MaxChord << " in. ";
-        else cout << "Nacelle max. chord: "  << Nacelle_MaxChord << " m. ";
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Nacelle min. LE radius: "  << Nacelle_MinLERadius << " 1/in. ";
-        else cout << "Nacelle min. LE radius: "  << Nacelle_MinLERadius << " 1/m. ";
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Nacelle max. LE radius: "  << Nacelle_MaxLERadius << " 1/in. " << endl;
-        else cout << "Nacelle max. LE radius: "  << Nacelle_MaxLERadius << " 1/m. " << endl;
-        cout << "Nacelle min. ToC: "  << Nacelle_MinToC << ". ";
-        cout << "Nacelle max. ToC: "  << Nacelle_MaxToC << ". ";
-        cout << "Nacelle delta ToC: "  << Nacelle_ObjFun_MinToC << ". ";
-        cout << "Nacelle max. twist: "  << Nacelle_MaxTwist << " deg. "<< endl;
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Nacelle volume: " << Nacelle_Volume << " in^3. ";
+        else
+          cout << "Nacelle volume: " << Nacelle_Volume << " m^3. ";
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Nacelle min. thickness: " << Nacelle_MinThickness << " in. ";
+        else
+          cout << "Nacelle min. thickness: " << Nacelle_MinThickness << " m. ";
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Nacelle max. thickness: " << Nacelle_MaxThickness << " in. " << endl;
+        else
+          cout << "Nacelle max. thickness: " << Nacelle_MaxThickness << " m. " << endl;
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Nacelle min. chord: " << Nacelle_MinChord << " in. ";
+        else
+          cout << "Nacelle min. chord: " << Nacelle_MinChord << " m. ";
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Nacelle max. chord: " << Nacelle_MaxChord << " in. ";
+        else
+          cout << "Nacelle max. chord: " << Nacelle_MaxChord << " m. ";
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Nacelle min. LE radius: " << Nacelle_MinLERadius << " 1/in. ";
+        else
+          cout << "Nacelle min. LE radius: " << Nacelle_MinLERadius << " 1/m. ";
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Nacelle max. LE radius: " << Nacelle_MaxLERadius << " 1/in. " << endl;
+        else
+          cout << "Nacelle max. LE radius: " << Nacelle_MaxLERadius << " 1/m. " << endl;
+        cout << "Nacelle min. ToC: " << Nacelle_MinToC << ". ";
+        cout << "Nacelle max. ToC: " << Nacelle_MaxToC << ". ";
+        cout << "Nacelle delta ToC: " << Nacelle_ObjFun_MinToC << ". ";
+        cout << "Nacelle max. twist: " << Nacelle_MaxTwist << " deg. " << endl;
       }
 
     }
 
     else {
-
       if (rank == MASTER_NODE) {
         cout << "Computing the wing continuous description." << endl << endl;
       }
 
-      geometry_container[ZONE_0]->Compute_Wing(config_container[ZONE_0], true,
-                                               Wing_Volume, Wing_MinThickness, Wing_MaxThickness, Wing_MinChord, Wing_MaxChord,
-                                               Wing_MinLERadius, Wing_MaxLERadius, Wing_MinToC, Wing_MaxToC, Wing_ObjFun_MinToC,
+      geometry_container[ZONE_0]->Compute_Wing(config_container[ZONE_0], true, Wing_Volume, Wing_MinThickness,
+                                               Wing_MaxThickness, Wing_MinChord, Wing_MaxChord, Wing_MinLERadius,
+                                               Wing_MaxLERadius, Wing_MinToC, Wing_MaxToC, Wing_ObjFun_MinToC,
                                                Wing_MaxTwist, Wing_MaxCurvature, Wing_MaxDihedral);
 
       /*--- Screen output for the wing definition ---*/
 
       if (rank == MASTER_NODE) {
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Wing volume: "    << Wing_Volume << " in^3. ";
-        else cout << "Wing volume: "    << Wing_Volume << " m^3. ";
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Wing min. thickness: "  << Wing_MinThickness << " in. ";
-        else cout << "Wing min. thickness: "  << Wing_MinThickness << " m. ";
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Wing max. thickness: "  << Wing_MaxThickness << " in. " << endl;
-        else cout << "Wing max. thickness: "  << Wing_MaxThickness << " m. " << endl;
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Wing min. chord: "  << Wing_MinChord << " in. ";
-        else cout << "Wing min. chord: "  << Wing_MinChord << " m. ";
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Wing max. chord: "  << Wing_MaxChord << " in. ";
-        else cout << "Wing max. chord: "  << Wing_MaxChord << " m. ";
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Wing min. LE radius: "  << Wing_MinLERadius << " 1/in. ";
-        else cout << "Wing min. LE radius: "  << Wing_MinLERadius << " 1/m. ";
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Wing max. LE radius: "  << Wing_MaxLERadius << " 1/in. " << endl;
-        else cout << "Wing max. LE radius: "  << Wing_MaxLERadius << " 1/m. " << endl;
-        cout << "Wing min. ToC: "  << Wing_MinToC << ". ";
-        cout << "Wing max. ToC: "  << Wing_MaxToC << ". ";
-        cout << "Wing delta ToC: "  << Wing_ObjFun_MinToC << ". ";
-        cout << "Wing max. twist: "  << Wing_MaxTwist << " deg. "<< endl;
-        if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << "Wing max. curvature: "  << Wing_MaxCurvature << " 1/in. ";
-        else cout << "Wing max. curvature: "  << Wing_MaxCurvature << " 1/m. ";
-        cout << "Wing max. dihedral: "  << Wing_MaxDihedral << " deg." << endl;
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Wing volume: " << Wing_Volume << " in^3. ";
+        else
+          cout << "Wing volume: " << Wing_Volume << " m^3. ";
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Wing min. thickness: " << Wing_MinThickness << " in. ";
+        else
+          cout << "Wing min. thickness: " << Wing_MinThickness << " m. ";
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Wing max. thickness: " << Wing_MaxThickness << " in. " << endl;
+        else
+          cout << "Wing max. thickness: " << Wing_MaxThickness << " m. " << endl;
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Wing min. chord: " << Wing_MinChord << " in. ";
+        else
+          cout << "Wing min. chord: " << Wing_MinChord << " m. ";
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Wing max. chord: " << Wing_MaxChord << " in. ";
+        else
+          cout << "Wing max. chord: " << Wing_MaxChord << " m. ";
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Wing min. LE radius: " << Wing_MinLERadius << " 1/in. ";
+        else
+          cout << "Wing min. LE radius: " << Wing_MinLERadius << " 1/m. ";
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Wing max. LE radius: " << Wing_MaxLERadius << " 1/in. " << endl;
+        else
+          cout << "Wing max. LE radius: " << Wing_MaxLERadius << " 1/m. " << endl;
+        cout << "Wing min. ToC: " << Wing_MinToC << ". ";
+        cout << "Wing max. ToC: " << Wing_MaxToC << ". ";
+        cout << "Wing delta ToC: " << Wing_ObjFun_MinToC << ". ";
+        cout << "Wing max. twist: " << Wing_MaxTwist << " deg. " << endl;
+        if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+          cout << "Wing max. curvature: " << Wing_MaxCurvature << " 1/in. ";
+        else
+          cout << "Wing max. curvature: " << Wing_MaxCurvature << " 1/m. ";
+        cout << "Wing max. dihedral: " << Wing_MaxDihedral << " deg." << endl;
       }
-
     }
-
   }
 
   for (iPlane = 0; iPlane < nPlane; iPlane++) {
-
-    geometry_container[ZONE_0]->ComputeAirfoil_Section(Plane_P0[iPlane], Plane_Normal[iPlane], -1E6, 1E6, -1E6, 1E6, -1E6, 1E6, nullptr,
-                                                       Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane],
-                                                       Variable_Airfoil[iPlane], true, config_container[ZONE_0]);
+    geometry_container[ZONE_0]->ComputeAirfoil_Section(
+        Plane_P0[iPlane], Plane_Normal[iPlane], -1E6, 1E6, -1E6, 1E6, -1E6, 1E6, nullptr, Xcoord_Airfoil[iPlane],
+        Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane], Variable_Airfoil[iPlane], true, config_container[ZONE_0]);
   }
 
   if (rank == MASTER_NODE)
-    cout << endl <<"-------------------- Objective function evaluation ----------------------" << endl;
+    cout << endl << "-------------------- Objective function evaluation ----------------------" << endl;
 
   if (rank == MASTER_NODE) {
-
     /*--- Evaluate objective function ---*/
 
     for (iPlane = 0; iPlane < nPlane; iPlane++) {
-
       if (Xcoord_Airfoil[iPlane].size() > 1) {
-
-        cout << "\nStation " << (iPlane+1);
+        cout << "\nStation " << (iPlane + 1);
         if (config_container[ZONE_0]->GetGeo_Description() == FUSELAGE) {
-          if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << ". XCoord: " << Plane_P0[iPlane][0] << " in, ";
-          else cout << ". XCoord: " << Plane_P0[iPlane][0] << " m, ";
+          if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+            cout << ". XCoord: " << Plane_P0[iPlane][0] << " in, ";
+          else
+            cout << ". XCoord: " << Plane_P0[iPlane][0] << " m, ";
         }
         if (config_container[ZONE_0]->GetGeo_Description() == WING) {
-          if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << ". YCoord: " << Plane_P0[iPlane][1] << " in, ";
-          else cout << ". YCoord: " << Plane_P0[iPlane][1] << " m, ";
+          if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+            cout << ". YCoord: " << Plane_P0[iPlane][1] << " in, ";
+          else
+            cout << ". YCoord: " << Plane_P0[iPlane][1] << " m, ";
         }
         if (config_container[ZONE_0]->GetGeo_Description() == TWOD_AIRFOIL) {
-          if (config_container[ZONE_0]->GetSystemMeasurements() == US) cout << ". ZCoord: " << Plane_P0[iPlane][2] << " in, ";
-          else cout << ". ZCoord: " << Plane_P0[iPlane][2] << " m, ";
+          if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+            cout << ". ZCoord: " << Plane_P0[iPlane][2] << " in, ";
+          else
+            cout << ". ZCoord: " << Plane_P0[iPlane][2] << " m, ";
         }
-        if (config_container[ZONE_0]->GetGeo_Description() == NACELLE) cout << ". Theta: " << atan2(Plane_Normal[iPlane][1], -Plane_Normal[iPlane][2])/PI_NUMBER*180 + 180 << " deg, ";
+        if (config_container[ZONE_0]->GetGeo_Description() == NACELLE)
+          cout << ". Theta: " << atan2(Plane_Normal[iPlane][1], -Plane_Normal[iPlane][2]) / PI_NUMBER * 180 + 180
+               << " deg, ";
 
         if (config_container[ZONE_0]->GetGeo_Description() == FUSELAGE) {
-          ObjectiveFunc[0*nPlane+iPlane]  = geometry_container[ZONE_0]->Compute_Area(Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-          ObjectiveFunc[1*nPlane+iPlane]  = geometry_container[ZONE_0]->Compute_Length(Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-          ObjectiveFunc[2*nPlane+iPlane]  = geometry_container[ZONE_0]->Compute_Width(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-          ObjectiveFunc[3*nPlane+iPlane]  = geometry_container[ZONE_0]->Compute_WaterLineWidth(Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-          ObjectiveFunc[4*nPlane+iPlane]  = geometry_container[ZONE_0]->Compute_Height(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-
-          if (config_container[ZONE_0]->GetSystemMeasurements() == US)  cout << "Area: "             << ObjectiveFunc[0*nPlane+iPlane] << " in^2, ";
-          else  cout << "Area: "             << ObjectiveFunc[0*nPlane+iPlane] << " m^2, ";
-          if (config_container[ZONE_0]->GetSystemMeasurements() == US)  cout << "Length: "           << ObjectiveFunc[1*nPlane+iPlane] << " in, ";
-          else  cout << "Length: "           << ObjectiveFunc[1*nPlane+iPlane] << " m, ";
-          if (config_container[ZONE_0]->GetSystemMeasurements() == US)  cout << "Width: "            << ObjectiveFunc[2*nPlane+iPlane] << " in, ";
-          else cout << "Width: "             << ObjectiveFunc[2*nPlane+iPlane] << " m, ";
-          if (config_container[ZONE_0]->GetSystemMeasurements() == US)  cout << "Waterline width: "  << ObjectiveFunc[3*nPlane+iPlane] << " in, ";
-          else cout << "Waterline width: "   << ObjectiveFunc[3*nPlane+iPlane] << " m, ";
-          if (config_container[ZONE_0]->GetSystemMeasurements() == US)  cout << "Height: "           << ObjectiveFunc[4*nPlane+iPlane] << " in.";
-          else cout << "Height: "            << ObjectiveFunc[4*nPlane+iPlane] << " m.";
-        }
-        else if (config_container[ZONE_0]->GetGeo_Description() == NACELLE) {
-          ObjectiveFunc[0*nPlane+iPlane]  = geometry_container[ZONE_0]->Compute_Area(Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-          ObjectiveFunc[1*nPlane+iPlane]  = geometry_container[ZONE_0]->Compute_MaxThickness(Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-          ObjectiveFunc[2*nPlane+iPlane]  = geometry_container[ZONE_0]->Compute_Chord(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-          ObjectiveFunc[3*nPlane+iPlane]  = geometry_container[ZONE_0]->Compute_LERadius(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-          ObjectiveFunc[4*nPlane+iPlane]  = ObjectiveFunc[1*nPlane+iPlane]/ObjectiveFunc[2*nPlane+iPlane];
-          ObjectiveFunc[5*nPlane+iPlane]  = geometry_container[ZONE_0]->Compute_Twist(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-
-          if (config_container[ZONE_0]->GetSystemMeasurements() == US)  cout << "Area: "             << ObjectiveFunc[0*nPlane+iPlane] << " in^2, ";
-          else  cout << "Area: "                 << ObjectiveFunc[0*nPlane+iPlane] << " m^2, ";
-          if (config_container[ZONE_0]->GetSystemMeasurements() == US)  cout << "Thickness: "   << ObjectiveFunc[1*nPlane+iPlane] << " in, " << endl;
-          else cout << "Thickness: "             << ObjectiveFunc[1*nPlane+iPlane] << " m, " << endl;
-          if (config_container[ZONE_0]->GetSystemMeasurements() == US)  cout << "Chord: "            << ObjectiveFunc[2*nPlane+iPlane] << " in, ";
-          else cout << "Chord: "                 << ObjectiveFunc[2*nPlane+iPlane] << " m, ";
-          if (config_container[ZONE_0]->GetSystemMeasurements() == US)  cout << "LE radius: "            << ObjectiveFunc[3*nPlane+iPlane] << " 1/in, ";
-          else cout << "LE radius: "             << ObjectiveFunc[3*nPlane+iPlane] << " 1/m, ";
-          cout << "ToC: "                        << ObjectiveFunc[4*nPlane+iPlane] << ", ";
-          if (geometry_container[ZONE_0]->GetnDim() == 2) cout << "Alpha: "      << ObjectiveFunc[5*nPlane+iPlane] <<" deg.";
-          else if (geometry_container[ZONE_0]->GetnDim() == 3) cout << "Twist angle: "      << ObjectiveFunc[5*nPlane+iPlane] <<" deg.";
+          ObjectiveFunc[0 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Area(
+              Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane],
+              Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+          ObjectiveFunc[1 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Length(
+              Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane],
+              Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+          ObjectiveFunc[2 * nPlane + iPlane] =
+              geometry_container[ZONE_0]->Compute_Width(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane],
+                                                        Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+          ObjectiveFunc[3 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_WaterLineWidth(
+              Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane],
+              Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+          ObjectiveFunc[4 * nPlane + iPlane] =
+              geometry_container[ZONE_0]->Compute_Height(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane],
+                                                         Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+
+          if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+            cout << "Area: " << ObjectiveFunc[0 * nPlane + iPlane] << " in^2, ";
+          else
+            cout << "Area: " << ObjectiveFunc[0 * nPlane + iPlane] << " m^2, ";
+          if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+            cout << "Length: " << ObjectiveFunc[1 * nPlane + iPlane] << " in, ";
+          else
+            cout << "Length: " << ObjectiveFunc[1 * nPlane + iPlane] << " m, ";
+          if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+            cout << "Width: " << ObjectiveFunc[2 * nPlane + iPlane] << " in, ";
+          else
+            cout << "Width: " << ObjectiveFunc[2 * nPlane + iPlane] << " m, ";
+          if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+            cout << "Waterline width: " << ObjectiveFunc[3 * nPlane + iPlane] << " in, ";
+          else
+            cout << "Waterline width: " << ObjectiveFunc[3 * nPlane + iPlane] << " m, ";
+          if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+            cout << "Height: " << ObjectiveFunc[4 * nPlane + iPlane] << " in.";
+          else
+            cout << "Height: " << ObjectiveFunc[4 * nPlane + iPlane] << " m.";
+        } else if (config_container[ZONE_0]->GetGeo_Description() == NACELLE) {
+          ObjectiveFunc[0 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Area(
+              Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane],
+              Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+          ObjectiveFunc[1 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_MaxThickness(
+              Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane],
+              Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+          ObjectiveFunc[2 * nPlane + iPlane] =
+              geometry_container[ZONE_0]->Compute_Chord(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane],
+                                                        Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+          ObjectiveFunc[3 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_LERadius(
+              Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane],
+              Zcoord_Airfoil[iPlane]);
+          ObjectiveFunc[4 * nPlane + iPlane] = ObjectiveFunc[1 * nPlane + iPlane] / ObjectiveFunc[2 * nPlane + iPlane];
+          ObjectiveFunc[5 * nPlane + iPlane] =
+              geometry_container[ZONE_0]->Compute_Twist(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane],
+                                                        Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+
+          if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+            cout << "Area: " << ObjectiveFunc[0 * nPlane + iPlane] << " in^2, ";
+          else
+            cout << "Area: " << ObjectiveFunc[0 * nPlane + iPlane] << " m^2, ";
+          if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+            cout << "Thickness: " << ObjectiveFunc[1 * nPlane + iPlane] << " in, " << endl;
+          else
+            cout << "Thickness: " << ObjectiveFunc[1 * nPlane + iPlane] << " m, " << endl;
+          if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+            cout << "Chord: " << ObjectiveFunc[2 * nPlane + iPlane] << " in, ";
+          else
+            cout << "Chord: " << ObjectiveFunc[2 * nPlane + iPlane] << " m, ";
+          if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+            cout << "LE radius: " << ObjectiveFunc[3 * nPlane + iPlane] << " 1/in, ";
+          else
+            cout << "LE radius: " << ObjectiveFunc[3 * nPlane + iPlane] << " 1/m, ";
+          cout << "ToC: " << ObjectiveFunc[4 * nPlane + iPlane] << ", ";
+          if (geometry_container[ZONE_0]->GetnDim() == 2)
+            cout << "Alpha: " << ObjectiveFunc[5 * nPlane + iPlane] << " deg.";
+          else if (geometry_container[ZONE_0]->GetnDim() == 3)
+            cout << "Twist angle: " << ObjectiveFunc[5 * nPlane + iPlane] << " deg.";
+        } else {
+          ObjectiveFunc[0 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Area(
+              Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane],
+              Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+          ObjectiveFunc[1 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_MaxThickness(
+              Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane],
+              Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+          ObjectiveFunc[2 * nPlane + iPlane] =
+              geometry_container[ZONE_0]->Compute_Chord(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane],
+                                                        Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+          ObjectiveFunc[3 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_LERadius(
+              Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane],
+              Zcoord_Airfoil[iPlane]);
+          ObjectiveFunc[4 * nPlane + iPlane] = ObjectiveFunc[1 * nPlane + iPlane] / ObjectiveFunc[2 * nPlane + iPlane];
+          ObjectiveFunc[5 * nPlane + iPlane] =
+              geometry_container[ZONE_0]->Compute_Twist(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane],
+                                                        Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+
+          if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+            cout << "Area: " << ObjectiveFunc[0 * nPlane + iPlane] << " in^2, ";
+          else
+            cout << "Area: " << ObjectiveFunc[0 * nPlane + iPlane] << " m^2, ";
+          if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+            cout << "Thickness: " << ObjectiveFunc[1 * nPlane + iPlane] << " in, " << endl;
+          else
+            cout << "Thickness: " << ObjectiveFunc[1 * nPlane + iPlane] << " m, " << endl;
+          if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+            cout << "Chord: " << ObjectiveFunc[2 * nPlane + iPlane] << " in, ";
+          else
+            cout << "Chord: " << ObjectiveFunc[2 * nPlane + iPlane] << " m, ";
+          if (config_container[ZONE_0]->GetSystemMeasurements() == US)
+            cout << "LE radius: " << ObjectiveFunc[3 * nPlane + iPlane] << " 1/in, ";
+          else
+            cout << "LE radius: " << ObjectiveFunc[3 * nPlane + iPlane] << " 1/m, ";
+          cout << "ToC: " << ObjectiveFunc[4 * nPlane + iPlane] << ", ";
+          if (geometry_container[ZONE_0]->GetnDim() == 2)
+            cout << "Alpha: " << ObjectiveFunc[5 * nPlane + iPlane] << " deg.";
+          else if (geometry_container[ZONE_0]->GetnDim() == 3)
+            cout << "Twist angle: " << ObjectiveFunc[5 * nPlane + iPlane] << " deg.";
         }
-        else {
-          ObjectiveFunc[0*nPlane+iPlane]  = geometry_container[ZONE_0]->Compute_Area(Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-          ObjectiveFunc[1*nPlane+iPlane]  = geometry_container[ZONE_0]->Compute_MaxThickness(Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-          ObjectiveFunc[2*nPlane+iPlane]  = geometry_container[ZONE_0]->Compute_Chord(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-          ObjectiveFunc[3*nPlane+iPlane]  = geometry_container[ZONE_0]->Compute_LERadius(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-          ObjectiveFunc[4*nPlane+iPlane]  = ObjectiveFunc[1*nPlane+iPlane]/ObjectiveFunc[2*nPlane+iPlane];
-          ObjectiveFunc[5*nPlane+iPlane]  = geometry_container[ZONE_0]->Compute_Twist(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-
-          if (config_container[ZONE_0]->GetSystemMeasurements() == US)  cout << "Area: "             << ObjectiveFunc[0*nPlane+iPlane] << " in^2, ";
-          else  cout << "Area: "                 << ObjectiveFunc[0*nPlane+iPlane] << " m^2, ";
-          if (config_container[ZONE_0]->GetSystemMeasurements() == US)  cout << "Thickness: "   << ObjectiveFunc[1*nPlane+iPlane] << " in, " << endl;
-          else cout << "Thickness: "             << ObjectiveFunc[1*nPlane+iPlane] << " m, " << endl;
-          if (config_container[ZONE_0]->GetSystemMeasurements() == US)  cout << "Chord: "            << ObjectiveFunc[2*nPlane+iPlane] << " in, ";
-          else cout << "Chord: "                 << ObjectiveFunc[2*nPlane+iPlane] << " m, ";
-          if (config_container[ZONE_0]->GetSystemMeasurements() == US)  cout << "LE radius: "            << ObjectiveFunc[3*nPlane+iPlane] << " 1/in, ";
-          else cout << "LE radius: "             << ObjectiveFunc[3*nPlane+iPlane] << " 1/m, ";
-          cout << "ToC: "                        << ObjectiveFunc[4*nPlane+iPlane] << ", ";
-          if (geometry_container[ZONE_0]->GetnDim() == 2) cout << "Alpha: "      << ObjectiveFunc[5*nPlane+iPlane] <<" deg.";
-          else if (geometry_container[ZONE_0]->GetnDim() == 3) cout << "Twist angle: "      << ObjectiveFunc[5*nPlane+iPlane] <<" deg.";
-        }
-
       }
-
     }
 
     /*--- Write the objective function in a external file ---*/
     string filename = config_container[ZONE_0]->GetObjFunc_Value_FileName();
     unsigned short lastindex = filename.find_last_of(".");
     filename = filename.substr(0, lastindex);
-    if (tabTecplot) filename += ".dat";
-    else filename += ".csv";
+    if (tabTecplot)
+      filename += ".dat";
+    else
+      filename += ".csv";
     ObjFunc_file.open(filename.c_str(), ios::out);
     if (tabTecplot) ObjFunc_file << "TITLE = \"SU2_GEO Evaluation\"" << endl;
 
     if (geometry_container[ZONE_0]->GetnDim() == 2) {
       if (tabTecplot) ObjFunc_file << "VARIABLES =//" << endl;
-      ObjFunc_file << "\"AIRFOIL_AREA\",\"AIRFOIL_THICKNESS\",\"AIRFOIL_CHORD\",\"AIRFOIL_LE_RADIUS\",\"AIRFOIL_TOC\",\"AIRFOIL_ALPHA\"";
-    }
-    else if (geometry_container[ZONE_0]->GetnDim() == 3) {
-
+      ObjFunc_file << "\"AIRFOIL_AREA\",\"AIRFOIL_THICKNESS\",\"AIRFOIL_CHORD\",\"AIRFOIL_LE_RADIUS\",\"AIRFOIL_TOC\","
+                      "\"AIRFOIL_ALPHA\"";
+    } else if (geometry_container[ZONE_0]->GetnDim() == 3) {
       if (tabTecplot) ObjFunc_file << "VARIABLES = //" << endl;
 
       if (config_container[ZONE_0]->GetGeo_Description() == FUSELAGE) {
-        ObjFunc_file << "\"FUSELAGE_VOLUME\",\"FUSELAGE_WETTED_AREA\",\"FUSELAGE_MIN_WIDTH\",\"FUSELAGE_MAX_WIDTH\",\"FUSELAGE_MIN_WATERLINE_WIDTH\",\"FUSELAGE_MAX_WATERLINE_WIDTH\",\"FUSELAGE_MIN_HEIGHT\",\"FUSELAGE_MAX_HEIGHT\",\"FUSELAGE_MAX_CURVATURE\",";
-        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION"<< (iPlane+1) << "_AREA\",";
-        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION"<< (iPlane+1) << "_LENGTH\",";
-        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION"<< (iPlane+1) << "_WIDTH\",";
-        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION"<< (iPlane+1) << "_WATERLINE_WIDTH\",";
+        ObjFunc_file << "\"FUSELAGE_VOLUME\",\"FUSELAGE_WETTED_AREA\",\"FUSELAGE_MIN_WIDTH\",\"FUSELAGE_MAX_WIDTH\","
+                        "\"FUSELAGE_MIN_WATERLINE_WIDTH\",\"FUSELAGE_MAX_WATERLINE_WIDTH\",\"FUSELAGE_MIN_HEIGHT\","
+                        "\"FUSELAGE_MAX_HEIGHT\",\"FUSELAGE_MAX_CURVATURE\",";
+        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION" << (iPlane + 1) << "_AREA\",";
+        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION" << (iPlane + 1) << "_LENGTH\",";
+        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION" << (iPlane + 1) << "_WIDTH\",";
+        for (iPlane = 0; iPlane < nPlane; iPlane++)
+          ObjFunc_file << "\"STATION" << (iPlane + 1) << "_WATERLINE_WIDTH\",";
         for (iPlane = 0; iPlane < nPlane; iPlane++) {
-          ObjFunc_file << "\"STATION" << (iPlane+1) << "_HEIGHT\"";
-          if (iPlane != nPlane-1) ObjFunc_file << ",";
+          ObjFunc_file << "\"STATION" << (iPlane + 1) << "_HEIGHT\"";
+          if (iPlane != nPlane - 1) ObjFunc_file << ",";
         }
-      }
-      else if (config_container[ZONE_0]->GetGeo_Description() == NACELLE) {
-        ObjFunc_file << "\"NACELLE_VOLUME\",\"NACELLE_MIN_THICKNESS\",\"NACELLE_MAX_THICKNESS\",\"NACELLE_MIN_CHORD\",\"NACELLE_MAX_CHORD\",\"NACELLE_MIN_LE_RADIUS\",\"NACELLE_MAX_LE_RADIUS\",\"NACELLE_MIN_TOC\",\"NACELLE_MAX_TOC\",\"NACELLE_OBJFUN_MIN_TOC\",\"NACELLE_MAX_TWIST\",";
-        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION"<< (iPlane+1) << "_AREA\",";
-        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION"<< (iPlane+1) << "_THICKNESS\",";
-        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION"<< (iPlane+1) << "_CHORD\",";
-        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION"<< (iPlane+1) << "_LE_RADIUS\",";
-        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION"<< (iPlane+1) << "_TOC\",";
+      } else if (config_container[ZONE_0]->GetGeo_Description() == NACELLE) {
+        ObjFunc_file << "\"NACELLE_VOLUME\",\"NACELLE_MIN_THICKNESS\",\"NACELLE_MAX_THICKNESS\",\"NACELLE_MIN_CHORD\","
+                        "\"NACELLE_MAX_CHORD\",\"NACELLE_MIN_LE_RADIUS\",\"NACELLE_MAX_LE_RADIUS\",\"NACELLE_MIN_TOC\","
+                        "\"NACELLE_MAX_TOC\",\"NACELLE_OBJFUN_MIN_TOC\",\"NACELLE_MAX_TWIST\",";
+        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION" << (iPlane + 1) << "_AREA\",";
+        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION" << (iPlane + 1) << "_THICKNESS\",";
+        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION" << (iPlane + 1) << "_CHORD\",";
+        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION" << (iPlane + 1) << "_LE_RADIUS\",";
+        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION" << (iPlane + 1) << "_TOC\",";
         for (iPlane = 0; iPlane < nPlane; iPlane++) {
-          ObjFunc_file << "\"STATION" << (iPlane+1) << "_TWIST\"";
-          if (iPlane != nPlane-1) ObjFunc_file << ",";
+          ObjFunc_file << "\"STATION" << (iPlane + 1) << "_TWIST\"";
+          if (iPlane != nPlane - 1) ObjFunc_file << ",";
         }
-      }
-      else {
-        ObjFunc_file << "\"WING_VOLUME\",\"WING_MIN_THICKNESS\",\"WING_MAX_THICKNESS\",\"WING_MIN_CHORD\",\"WING_MAX_CHORD\",\"WING_MIN_LE_RADIUS\",\"WING_MAX_LE_RADIUS\",\"WING_MIN_TOC\",\"WING_MAX_TOC\",\"WING_OBJFUN_MIN_TOC\",\"WING_MAX_TWIST\",\"WING_MAX_CURVATURE\",\"WING_MAX_DIHEDRAL\",";
-        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION"<< (iPlane+1) << "_AREA\",";
-        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION"<< (iPlane+1) << "_THICKNESS\",";
-        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION"<< (iPlane+1) << "_CHORD\",";
-        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION"<< (iPlane+1) << "_LE_RADIUS\",";
-        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION"<< (iPlane+1) << "_TOC\",";
+      } else {
+        ObjFunc_file << "\"WING_VOLUME\",\"WING_MIN_THICKNESS\",\"WING_MAX_THICKNESS\",\"WING_MIN_CHORD\",\"WING_MAX_"
+                        "CHORD\",\"WING_MIN_LE_RADIUS\",\"WING_MAX_LE_RADIUS\",\"WING_MIN_TOC\",\"WING_MAX_TOC\","
+                        "\"WING_OBJFUN_MIN_TOC\",\"WING_MAX_TWIST\",\"WING_MAX_CURVATURE\",\"WING_MAX_DIHEDRAL\",";
+        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION" << (iPlane + 1) << "_AREA\",";
+        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION" << (iPlane + 1) << "_THICKNESS\",";
+        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION" << (iPlane + 1) << "_CHORD\",";
+        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION" << (iPlane + 1) << "_LE_RADIUS\",";
+        for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"STATION" << (iPlane + 1) << "_TOC\",";
         for (iPlane = 0; iPlane < nPlane; iPlane++) {
-          ObjFunc_file << "\"STATION" << (iPlane+1) << "_TWIST\"";
-          if (iPlane != nPlane-1) ObjFunc_file << ",";
+          ObjFunc_file << "\"STATION" << (iPlane + 1) << "_TWIST\"";
+          if (iPlane != nPlane - 1) ObjFunc_file << ",";
         }
       }
-
     }
 
-    if (tabTecplot) ObjFunc_file << "\nZONE T= \"Geometrical variables (value)\"" << endl;
-    else ObjFunc_file << endl;
+    if (tabTecplot)
+      ObjFunc_file << "\nZONE T= \"Geometrical variables (value)\"" << endl;
+    else
+      ObjFunc_file << endl;
 
     if (config_container[ZONE_0]->GetGeo_Description() == FUSELAGE) {
       if (geometry_container[ZONE_0]->GetnDim() == 3) {
-        ObjFunc_file << Fuselage_Volume <<", "<< Fuselage_WettedArea <<", "<< Fuselage_MinWidth <<", "<< Fuselage_MaxWidth <<", "<< Fuselage_MinWaterLineWidth <<", "<< Fuselage_MaxWaterLineWidth<<", "<< Fuselage_MinHeight <<", "<< Fuselage_MaxHeight <<", "<< Fuselage_MaxCurvature <<", ";
+        ObjFunc_file << Fuselage_Volume << ", " << Fuselage_WettedArea << ", " << Fuselage_MinWidth << ", "
+                     << Fuselage_MaxWidth << ", " << Fuselage_MinWaterLineWidth << ", " << Fuselage_MaxWaterLineWidth
+                     << ", " << Fuselage_MinHeight << ", " << Fuselage_MaxHeight << ", " << Fuselage_MaxCurvature
+                     << ", ";
       }
-      for (iPlane = 0; iPlane < nPlane*5; iPlane++) {
+      for (iPlane = 0; iPlane < nPlane * 5; iPlane++) {
         ObjFunc_file << ObjectiveFunc[iPlane];
-        if (iPlane != (nPlane*5)-1) ObjFunc_file <<", ";
+        if (iPlane != (nPlane * 5) - 1) ObjFunc_file << ", ";
       }
-    }
-    else if (config_container[ZONE_0]->GetGeo_Description() == NACELLE) {
+    } else if (config_container[ZONE_0]->GetGeo_Description() == NACELLE) {
       if (geometry_container[ZONE_0]->GetnDim() == 3) {
-        ObjFunc_file << Nacelle_Volume <<", "<< Nacelle_MinThickness <<", "<< Nacelle_MaxThickness <<", "<< Nacelle_MinChord <<", "<< Nacelle_MaxChord <<", "<< Nacelle_MinLERadius <<", "<< Nacelle_MaxLERadius<<", "<< Nacelle_MinToC <<", "<< Nacelle_MaxToC <<", "<< Nacelle_ObjFun_MinToC <<", "<< Nacelle_MaxTwist <<", ";
+        ObjFunc_file << Nacelle_Volume << ", " << Nacelle_MinThickness << ", " << Nacelle_MaxThickness << ", "
+                     << Nacelle_MinChord << ", " << Nacelle_MaxChord << ", " << Nacelle_MinLERadius << ", "
+                     << Nacelle_MaxLERadius << ", " << Nacelle_MinToC << ", " << Nacelle_MaxToC << ", "
+                     << Nacelle_ObjFun_MinToC << ", " << Nacelle_MaxTwist << ", ";
       }
-      for (iPlane = 0; iPlane < nPlane*6; iPlane++) {
+      for (iPlane = 0; iPlane < nPlane * 6; iPlane++) {
         ObjFunc_file << ObjectiveFunc[iPlane];
-        if (iPlane != (nPlane*6)-1) ObjFunc_file <<", ";
+        if (iPlane != (nPlane * 6) - 1) ObjFunc_file << ", ";
       }
-    }
-    else {
+    } else {
       if (geometry_container[ZONE_0]->GetnDim() == 3) {
-        ObjFunc_file << Wing_Volume <<", "<< Wing_MinThickness <<", "<< Wing_MaxThickness <<", "<< Wing_MinChord <<", "<< Wing_MaxChord <<", "<< Wing_MinLERadius <<", "<< Wing_MaxLERadius<<", "<< Wing_MinToC <<", "<< Wing_MaxToC <<", "<< Wing_ObjFun_MinToC <<", "<< Wing_MaxTwist <<", "<< Wing_MaxCurvature <<", "<< Wing_MaxDihedral <<", ";
+        ObjFunc_file << Wing_Volume << ", " << Wing_MinThickness << ", " << Wing_MaxThickness << ", " << Wing_MinChord
+                     << ", " << Wing_MaxChord << ", " << Wing_MinLERadius << ", " << Wing_MaxLERadius << ", "
+                     << Wing_MinToC << ", " << Wing_MaxToC << ", " << Wing_ObjFun_MinToC << ", " << Wing_MaxTwist
+                     << ", " << Wing_MaxCurvature << ", " << Wing_MaxDihedral << ", ";
       }
-      for (iPlane = 0; iPlane < nPlane*6; iPlane++) {
+      for (iPlane = 0; iPlane < nPlane * 6; iPlane++) {
         ObjFunc_file << ObjectiveFunc[iPlane];
-        if (iPlane != (nPlane*6)-1) ObjFunc_file <<", ";
+        if (iPlane != (nPlane * 6) - 1) ObjFunc_file << ", ";
       }
     }
 
     ObjFunc_file.close();
-
   }
 
   if (config_container[ZONE_0]->GetGeometryMode() == GRADIENT) {
-
     /*--- Definition of the Class for surface deformation ---*/
     surface_movement = new CSurfaceMovement();
 
@@ -595,13 +732,14 @@ int main(int argc, char *argv[]) {
       string filename = config_container[ZONE_0]->GetObjFunc_Grad_FileName();
       unsigned short lastindex = filename.find_last_of(".");
       filename = filename.substr(0, lastindex);
-      if (tabTecplot) filename += ".dat";
-      else filename += ".csv";
+      if (tabTecplot)
+        filename += ".dat";
+      else
+        filename += ".csv";
       Gradient_file.open(filename.c_str(), ios::out);
     }
 
     for (iDV = 0; iDV < config_container[ZONE_0]->GetnDV(); iDV++) {
-
       /*--- Free Form deformation based ---*/
 
       if ((config_container[ZONE_0]->GetDesign_Variable(iDV) == FFD_CONTROL_POINT_2D) ||
@@ -614,17 +752,16 @@ int main(int argc, char *argv[]) {
           (config_container[ZONE_0]->GetDesign_Variable(iDV) == FFD_TWIST) ||
           (config_container[ZONE_0]->GetDesign_Variable(iDV) == FFD_ROTATION) ||
           (config_container[ZONE_0]->GetDesign_Variable(iDV) == FFD_CAMBER) ||
-          (config_container[ZONE_0]->GetDesign_Variable(iDV) == FFD_THICKNESS) ) {
-
+          (config_container[ZONE_0]->GetDesign_Variable(iDV) == FFD_THICKNESS)) {
         /*--- Read the FFD information in the first iteration ---*/
 
         if (iDV == 0) {
-
           if (rank == MASTER_NODE) cout << "Read the FFD information from mesh file." << endl;
 
           /*--- Read the FFD information from the grid file ---*/
 
-          surface_movement->ReadFFDInfo(geometry_container[ZONE_0], config_container[ZONE_0], FFDBox, config_container[ZONE_0]->GetMesh_FileName());
+          surface_movement->ReadFFDInfo(geometry_container[ZONE_0], config_container[ZONE_0], FFDBox,
+                                        config_container[ZONE_0]->GetMesh_FileName());
 
           /*--- Modify the control points for polar based computations ---*/
 
@@ -632,13 +769,11 @@ int main(int argc, char *argv[]) {
             for (iFFDBox = 0; iFFDBox < surface_movement->GetnFFDBox(); iFFDBox++) {
               FFDBox[iFFDBox]->SetCart2Cyl_ControlPoints(config_container[ZONE_0]);
             }
-          }
-          else if (config_container[ZONE_0]->GetFFD_CoordSystem() == SPHERICAL) {
+          } else if (config_container[ZONE_0]->GetFFD_CoordSystem() == SPHERICAL) {
             for (iFFDBox = 0; iFFDBox < surface_movement->GetnFFDBox(); iFFDBox++) {
               FFDBox[iFFDBox]->SetCart2Sphe_ControlPoints(config_container[ZONE_0]);
             }
-          }
-          else if (config_container[ZONE_0]->GetFFD_CoordSystem() == POLAR) {
+          } else if (config_container[ZONE_0]->GetFFD_CoordSystem() == POLAR) {
             for (iFFDBox = 0; iFFDBox < surface_movement->GetnFFDBox(); iFFDBox++) {
               FFDBox[iFFDBox]->SetCart2Sphe_ControlPoints(config_container[ZONE_0]);
             }
@@ -651,23 +786,21 @@ int main(int argc, char *argv[]) {
           }
 
           for (iFFDBox = 0; iFFDBox < surface_movement->GetnFFDBox(); iFFDBox++) {
-
             if (rank == MASTER_NODE) cout << "Checking FFD box dimension." << endl;
-            surface_movement->CheckFFDDimension(geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox], iFFDBox);
-
+            surface_movement->CheckFFDDimension(geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox],
+                                                iFFDBox);
 
             if (rank == MASTER_NODE) cout << "Check the FFD box intersections with the solid surfaces." << endl;
-            surface_movement->CheckFFDIntersections(geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox], iFFDBox);
-
+            surface_movement->CheckFFDIntersections(geometry_container[ZONE_0], config_container[ZONE_0],
+                                                    FFDBox[iFFDBox], iFFDBox);
           }
 
           if (rank == MASTER_NODE)
-            cout <<"-------------------------------------------------------------------------" << endl;
-
+            cout << "-------------------------------------------------------------------------" << endl;
         }
 
         if (rank == MASTER_NODE) {
-          cout << endl << "Design variable number "<< iDV <<"." << endl;
+          cout << endl << "Design variable number " << iDV << "." << endl;
           cout << "Perform 3D deformation of the surface." << endl;
         }
 
@@ -676,31 +809,66 @@ int main(int argc, char *argv[]) {
         MoveSurface = false;
 
         for (iFFDBox = 0; iFFDBox < surface_movement->GetnFFDBox(); iFFDBox++) {
-
           Local_MoveSurface = false;
 
-          switch ( config_container[ZONE_0]->GetDesign_Variable(iDV) ) {
-            case FFD_CONTROL_POINT_2D : Local_MoveSurface = surface_movement->SetFFDCPChange_2D(geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox], FFDBox, iDV, true); break;
-            case FFD_CAMBER_2D :        Local_MoveSurface = surface_movement->SetFFDCamber_2D(geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox], FFDBox, iDV, true); break;
-            case FFD_THICKNESS_2D :     Local_MoveSurface = surface_movement->SetFFDThickness_2D(geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox], FFDBox, iDV, true); break;
-            case FFD_TWIST_2D :         Local_MoveSurface = surface_movement->SetFFDTwist_2D(geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox], FFDBox, iDV, true); break;
-            case FFD_CONTROL_POINT :    Local_MoveSurface = surface_movement->SetFFDCPChange(geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox], FFDBox, iDV, true); break;
-            case FFD_NACELLE :          Local_MoveSurface = surface_movement->SetFFDNacelle(geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox], FFDBox, iDV, true); break;
-            case FFD_GULL :             Local_MoveSurface = surface_movement->SetFFDGull(geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox], FFDBox, iDV, true); break;
-            case FFD_TWIST :            Local_MoveSurface = surface_movement->SetFFDTwist(geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox], FFDBox, iDV, true); break;
-            case FFD_ROTATION :         Local_MoveSurface = surface_movement->SetFFDRotation(geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox], FFDBox, iDV, true); break;
-            case FFD_CAMBER :           Local_MoveSurface = surface_movement->SetFFDCamber(geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox], FFDBox, iDV, true); break;
-            case FFD_THICKNESS :        Local_MoveSurface = surface_movement->SetFFDThickness(geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox], FFDBox, iDV, true); break;
-            case FFD_CONTROL_SURFACE :  Local_MoveSurface = surface_movement->SetFFDControl_Surface(geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox], FFDBox, iDV, true); break;
+          switch (config_container[ZONE_0]->GetDesign_Variable(iDV)) {
+            case FFD_CONTROL_POINT_2D:
+              Local_MoveSurface = surface_movement->SetFFDCPChange_2D(
+                  geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox], FFDBox, iDV, true);
+              break;
+            case FFD_CAMBER_2D:
+              Local_MoveSurface = surface_movement->SetFFDCamber_2D(
+                  geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox], FFDBox, iDV, true);
+              break;
+            case FFD_THICKNESS_2D:
+              Local_MoveSurface = surface_movement->SetFFDThickness_2D(
+                  geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox], FFDBox, iDV, true);
+              break;
+            case FFD_TWIST_2D:
+              Local_MoveSurface = surface_movement->SetFFDTwist_2D(geometry_container[ZONE_0], config_container[ZONE_0],
+                                                                   FFDBox[iFFDBox], FFDBox, iDV, true);
+              break;
+            case FFD_CONTROL_POINT:
+              Local_MoveSurface = surface_movement->SetFFDCPChange(geometry_container[ZONE_0], config_container[ZONE_0],
+                                                                   FFDBox[iFFDBox], FFDBox, iDV, true);
+              break;
+            case FFD_NACELLE:
+              Local_MoveSurface = surface_movement->SetFFDNacelle(geometry_container[ZONE_0], config_container[ZONE_0],
+                                                                  FFDBox[iFFDBox], FFDBox, iDV, true);
+              break;
+            case FFD_GULL:
+              Local_MoveSurface = surface_movement->SetFFDGull(geometry_container[ZONE_0], config_container[ZONE_0],
+                                                               FFDBox[iFFDBox], FFDBox, iDV, true);
+              break;
+            case FFD_TWIST:
+              Local_MoveSurface = surface_movement->SetFFDTwist(geometry_container[ZONE_0], config_container[ZONE_0],
+                                                                FFDBox[iFFDBox], FFDBox, iDV, true);
+              break;
+            case FFD_ROTATION:
+              Local_MoveSurface = surface_movement->SetFFDRotation(geometry_container[ZONE_0], config_container[ZONE_0],
+                                                                   FFDBox[iFFDBox], FFDBox, iDV, true);
+              break;
+            case FFD_CAMBER:
+              Local_MoveSurface = surface_movement->SetFFDCamber(geometry_container[ZONE_0], config_container[ZONE_0],
+                                                                 FFDBox[iFFDBox], FFDBox, iDV, true);
+              break;
+            case FFD_THICKNESS:
+              Local_MoveSurface = surface_movement->SetFFDThickness(
+                  geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox], FFDBox, iDV, true);
+              break;
+            case FFD_CONTROL_SURFACE:
+              Local_MoveSurface = surface_movement->SetFFDControl_Surface(
+                  geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox], FFDBox, iDV, true);
+              break;
           }
 
           /*--- Recompute cartesian coordinates using the new control points position ---*/
 
           if (Local_MoveSurface) {
             MoveSurface = true;
-            surface_movement->SetCartesianCoord(geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox], iFFDBox, true);
+            surface_movement->SetCartesianCoord(geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox],
+                                                iFFDBox, true);
           }
-
         }
 
       }
@@ -709,7 +877,7 @@ int main(int argc, char *argv[]) {
 
       else if (config_container[ZONE_0]->GetDesign_Variable(iDV) == HICKS_HENNE) {
         if (rank == MASTER_NODE) {
-          cout << endl << "Design variable number "<< iDV <<"." << endl;
+          cout << endl << "Design variable number " << iDV << "." << endl;
           cout << "Perform 2D deformation of the surface." << endl;
         }
         MoveSurface = true;
@@ -720,7 +888,7 @@ int main(int argc, char *argv[]) {
 
       else if (config_container[ZONE_0]->GetDesign_Variable(iDV) == SURFACE_BUMP) {
         if (rank == MASTER_NODE) {
-          cout << endl << "Design variable number "<< iDV <<"." << endl;
+          cout << endl << "Design variable number " << iDV << "." << endl;
           cout << "Perform 2D deformation of the surface." << endl;
         }
         MoveSurface = true;
@@ -731,7 +899,7 @@ int main(int argc, char *argv[]) {
 
       else if (config_container[ZONE_0]->GetDesign_Variable(iDV) == CST) {
         if (rank == MASTER_NODE) {
-          cout << endl << "Design variable number "<< iDV <<"." << endl;
+          cout << endl << "Design variable number " << iDV << "." << endl;
           cout << "Perform 2D deformation of the surface." << endl;
         }
         MoveSurface = true;
@@ -742,7 +910,7 @@ int main(int argc, char *argv[]) {
 
       else if (config_container[ZONE_0]->GetDesign_Variable(iDV) == TRANSLATION) {
         if (rank == MASTER_NODE) {
-          cout << endl << "Design variable number "<< iDV <<"." << endl;
+          cout << endl << "Design variable number " << iDV << "." << endl;
           cout << "Perform 2D deformation of the surface." << endl;
         }
         MoveSurface = true;
@@ -753,7 +921,7 @@ int main(int argc, char *argv[]) {
 
       else if (config_container[ZONE_0]->GetDesign_Variable(iDV) == SCALE) {
         if (rank == MASTER_NODE) {
-          cout << endl << "Design variable number "<< iDV <<"." << endl;
+          cout << endl << "Design variable number " << iDV << "." << endl;
           cout << "Perform 2D deformation of the surface." << endl;
         }
         MoveSurface = true;
@@ -764,7 +932,7 @@ int main(int argc, char *argv[]) {
 
       else if (config_container[ZONE_0]->GetDesign_Variable(iDV) == ROTATION) {
         if (rank == MASTER_NODE) {
-          cout << endl << "Design variable number "<< iDV <<"." << endl;
+          cout << endl << "Design variable number " << iDV << "." << endl;
           cout << "Perform 2D deformation of the surface." << endl;
         }
         MoveSurface = true;
@@ -775,7 +943,7 @@ int main(int argc, char *argv[]) {
 
       else if (config_container[ZONE_0]->GetDesign_Variable(iDV) == NACA_4DIGITS) {
         if (rank == MASTER_NODE) {
-          cout << endl << "Design variable number "<< iDV <<"." << endl;
+          cout << endl << "Design variable number " << iDV << "." << endl;
           cout << "Perform 2D deformation of the surface." << endl;
         }
         MoveSurface = true;
@@ -786,7 +954,7 @@ int main(int argc, char *argv[]) {
 
       else if (config_container[ZONE_0]->GetDesign_Variable(iDV) == PARABOLIC) {
         if (rank == MASTER_NODE) {
-          cout << endl << "Design variable number "<< iDV <<"." << endl;
+          cout << endl << "Design variable number " << iDV << "." << endl;
           cout << "Perform 2D deformation of the surface." << endl;
         }
         MoveSurface = true;
@@ -796,53 +964,46 @@ int main(int argc, char *argv[]) {
       /*--- Design variable not implement ---*/
 
       else {
-        if (rank == MASTER_NODE)
-          cout << "Design Variable not implemented yet" << endl;
+        if (rank == MASTER_NODE) cout << "Design Variable not implemented yet" << endl;
       }
 
       if (MoveSurface) {
-
         /*--- Compute the gradient for the volume. In 2D this is just
          the gradient of the area. ---*/
 
         if (geometry_container[ZONE_0]->GetnDim() == 3) {
-
           if (config_container[ZONE_0]->GetGeo_Description() == FUSELAGE) {
-            geometry_container[ZONE_0]->Compute_Fuselage(config_container[ZONE_0], false,
-                                                         Fuselage_Volume_New, Fuselage_WettedArea_New, Fuselage_MinWidth_New, Fuselage_MaxWidth_New,
-                                                         Fuselage_MinWaterLineWidth_New, Fuselage_MaxWaterLineWidth_New,
-                                                         Fuselage_MinHeight_New, Fuselage_MaxHeight_New,
-                                                         Fuselage_MaxCurvature_New);
-          }
-          else if (config_container[ZONE_0]->GetGeo_Description() == NACELLE) {
-            geometry_container[ZONE_0]->Compute_Nacelle(config_container[ZONE_0], false,
-                                                        Nacelle_Volume_New, Nacelle_MinThickness_New, Nacelle_MaxThickness_New, Nacelle_MinChord_New,
-                                                        Nacelle_MaxChord_New, Nacelle_MinLERadius_New, Nacelle_MaxLERadius_New, Nacelle_MinToC_New,
-                                                        Nacelle_MaxToC_New, Nacelle_ObjFun_MinToC_New, Nacelle_MaxTwist_New);
-          }
-          else {
-            geometry_container[ZONE_0]->Compute_Wing(config_container[ZONE_0], false,
-                                                     Wing_Volume_New, Wing_MinThickness_New, Wing_MaxThickness_New, Wing_MinChord_New,
-                                                     Wing_MaxChord_New, Wing_MinLERadius_New, Wing_MaxLERadius_New, Wing_MinToC_New, Wing_MaxToC_New,
-                                                     Wing_ObjFun_MinToC_New, Wing_MaxTwist_New, Wing_MaxCurvature_New, Wing_MaxDihedral_New);
+            geometry_container[ZONE_0]->Compute_Fuselage(
+                config_container[ZONE_0], false, Fuselage_Volume_New, Fuselage_WettedArea_New, Fuselage_MinWidth_New,
+                Fuselage_MaxWidth_New, Fuselage_MinWaterLineWidth_New, Fuselage_MaxWaterLineWidth_New,
+                Fuselage_MinHeight_New, Fuselage_MaxHeight_New, Fuselage_MaxCurvature_New);
+          } else if (config_container[ZONE_0]->GetGeo_Description() == NACELLE) {
+            geometry_container[ZONE_0]->Compute_Nacelle(
+                config_container[ZONE_0], false, Nacelle_Volume_New, Nacelle_MinThickness_New, Nacelle_MaxThickness_New,
+                Nacelle_MinChord_New, Nacelle_MaxChord_New, Nacelle_MinLERadius_New, Nacelle_MaxLERadius_New,
+                Nacelle_MinToC_New, Nacelle_MaxToC_New, Nacelle_ObjFun_MinToC_New, Nacelle_MaxTwist_New);
+          } else {
+            geometry_container[ZONE_0]->Compute_Wing(config_container[ZONE_0], false, Wing_Volume_New,
+                                                     Wing_MinThickness_New, Wing_MaxThickness_New, Wing_MinChord_New,
+                                                     Wing_MaxChord_New, Wing_MinLERadius_New, Wing_MaxLERadius_New,
+                                                     Wing_MinToC_New, Wing_MaxToC_New, Wing_ObjFun_MinToC_New,
+                                                     Wing_MaxTwist_New, Wing_MaxCurvature_New, Wing_MaxDihedral_New);
           }
-
         }
 
         /*--- Create airfoil structure ---*/
 
         for (iPlane = 0; iPlane < nPlane; iPlane++) {
-          geometry_container[ZONE_0]->ComputeAirfoil_Section(Plane_P0[iPlane], Plane_Normal[iPlane], -1E6, 1E6, -1E6, 1E6, -1E6, 1E6, nullptr,
-                                                             Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane],
+          geometry_container[ZONE_0]->ComputeAirfoil_Section(Plane_P0[iPlane], Plane_Normal[iPlane], -1E6, 1E6, -1E6,
+                                                             1E6, -1E6, 1E6, nullptr, Xcoord_Airfoil[iPlane],
+                                                             Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane],
                                                              Variable_Airfoil[iPlane], false, config_container[ZONE_0]);
         }
-
       }
 
       /*--- Compute gradient ---*/
 
       if (rank == MASTER_NODE) {
-
         delta_eps = config_container[ZONE_0]->GetDV_Value(iDV);
 
         if (delta_eps == 0) {
@@ -850,7 +1011,6 @@ int main(int argc, char *argv[]) {
         }
 
         if (MoveSurface) {
-
           if (config_container[ZONE_0]->GetGeo_Description() == FUSELAGE) {
             Fuselage_Volume_Grad = (Fuselage_Volume_New - Fuselage_Volume) / delta_eps;
             Fuselage_WettedArea_Grad = (Fuselage_WettedArea_New - Fuselage_WettedArea) / delta_eps;
@@ -862,8 +1022,7 @@ int main(int argc, char *argv[]) {
             Fuselage_MaxHeight_Grad = (Fuselage_MaxHeight_New - Fuselage_MaxHeight) / delta_eps;
             Fuselage_MaxCurvature_Grad = (Fuselage_MaxCurvature_New - Fuselage_MaxCurvature) / delta_eps;
 
-          }
-          else if (config_container[ZONE_0]->GetGeo_Description() == NACELLE) {
+          } else if (config_container[ZONE_0]->GetGeo_Description() == NACELLE) {
             Nacelle_Volume_Grad = (Nacelle_Volume_New - Nacelle_Volume) / delta_eps;
             Nacelle_MinThickness_Grad = (Nacelle_MinThickness_New - Nacelle_MinThickness) / delta_eps;
             Nacelle_MaxThickness_Grad = (Nacelle_MaxThickness_New - Nacelle_MaxThickness) / delta_eps;
@@ -875,8 +1034,7 @@ int main(int argc, char *argv[]) {
             Nacelle_MaxToC_Grad = (Nacelle_MaxToC_New - Nacelle_MaxToC) / delta_eps;
             Nacelle_ObjFun_MinToC_Grad = (Nacelle_ObjFun_MinToC_New - Nacelle_ObjFun_MinToC) / delta_eps;
             Nacelle_MaxTwist_Grad = (Nacelle_MaxTwist_New - Nacelle_MaxTwist) / delta_eps;
-          }
-          else {
+          } else {
             Wing_Volume_Grad = (Wing_Volume_New - Wing_Volume) / delta_eps;
             Wing_MinThickness_Grad = (Wing_MinThickness_New - Wing_MinThickness) / delta_eps;
             Wing_MaxThickness_Grad = (Wing_MaxThickness_New - Wing_MaxThickness) / delta_eps;
@@ -894,356 +1052,412 @@ int main(int argc, char *argv[]) {
 
           for (iPlane = 0; iPlane < nPlane; iPlane++) {
             if (Xcoord_Airfoil[iPlane].size() > 1) {
-
               if (config_container[ZONE_0]->GetGeo_Description() == FUSELAGE) {
-
-                ObjectiveFunc_New[0*nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Area(Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-                Gradient[0*nPlane + iPlane] = (ObjectiveFunc_New[0*nPlane + iPlane] - ObjectiveFunc[0*nPlane + iPlane]) / delta_eps;
-
-                ObjectiveFunc_New[1*nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Length(Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-                Gradient[1*nPlane + iPlane] = (ObjectiveFunc_New[1*nPlane + iPlane] - ObjectiveFunc[1*nPlane + iPlane]) / delta_eps;
-
-                ObjectiveFunc_New[2*nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Width(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-                Gradient[2*nPlane + iPlane] = (ObjectiveFunc_New[2*nPlane + iPlane] - ObjectiveFunc[2*nPlane + iPlane]) / delta_eps;
-
-                ObjectiveFunc_New[3*nPlane + iPlane] = geometry_container[ZONE_0]->Compute_WaterLineWidth(Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-                Gradient[3*nPlane + iPlane] = (ObjectiveFunc_New[3*nPlane + iPlane] - ObjectiveFunc[3*nPlane + iPlane]) / delta_eps;
-
-                ObjectiveFunc_New[4*nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Height(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-                Gradient[4*nPlane + iPlane] = (ObjectiveFunc_New[4*nPlane + iPlane] - ObjectiveFunc[4*nPlane + iPlane]) / delta_eps;
+                ObjectiveFunc_New[0 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Area(
+                    Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane],
+                    Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+                Gradient[0 * nPlane + iPlane] =
+                    (ObjectiveFunc_New[0 * nPlane + iPlane] - ObjectiveFunc[0 * nPlane + iPlane]) / delta_eps;
+
+                ObjectiveFunc_New[1 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Length(
+                    Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane],
+                    Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+                Gradient[1 * nPlane + iPlane] =
+                    (ObjectiveFunc_New[1 * nPlane + iPlane] - ObjectiveFunc[1 * nPlane + iPlane]) / delta_eps;
+
+                ObjectiveFunc_New[2 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Width(
+                    Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane],
+                    Zcoord_Airfoil[iPlane]);
+                Gradient[2 * nPlane + iPlane] =
+                    (ObjectiveFunc_New[2 * nPlane + iPlane] - ObjectiveFunc[2 * nPlane + iPlane]) / delta_eps;
+
+                ObjectiveFunc_New[3 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_WaterLineWidth(
+                    Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane],
+                    Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+                Gradient[3 * nPlane + iPlane] =
+                    (ObjectiveFunc_New[3 * nPlane + iPlane] - ObjectiveFunc[3 * nPlane + iPlane]) / delta_eps;
+
+                ObjectiveFunc_New[4 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Height(
+                    Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane],
+                    Zcoord_Airfoil[iPlane]);
+                Gradient[4 * nPlane + iPlane] =
+                    (ObjectiveFunc_New[4 * nPlane + iPlane] - ObjectiveFunc[4 * nPlane + iPlane]) / delta_eps;
 
               }
 
               else if (config_container[ZONE_0]->GetGeo_Description() == FUSELAGE) {
-
-                ObjectiveFunc_New[0*nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Area(Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-                Gradient[0*nPlane + iPlane] = (ObjectiveFunc_New[0*nPlane + iPlane] - ObjectiveFunc[0*nPlane + iPlane]) / delta_eps;
-
-                ObjectiveFunc_New[1*nPlane + iPlane] = geometry_container[ZONE_0]->Compute_MaxThickness(Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-                Gradient[1*nPlane + iPlane] = (ObjectiveFunc_New[1*nPlane + iPlane] - ObjectiveFunc[1*nPlane + iPlane]) / delta_eps;
-
-                ObjectiveFunc_New[2*nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Chord(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-                Gradient[2*nPlane + iPlane] = (ObjectiveFunc_New[2*nPlane + iPlane] - ObjectiveFunc[2*nPlane + iPlane]) / delta_eps;
-
-                ObjectiveFunc_New[3*nPlane + iPlane] = geometry_container[ZONE_0]->Compute_LERadius(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-                Gradient[3*nPlane + iPlane] = (ObjectiveFunc_New[3*nPlane + iPlane] - ObjectiveFunc[3*nPlane + iPlane]) / delta_eps;
-
-                ObjectiveFunc_New[4*nPlane + iPlane] = ObjectiveFunc_New[1*nPlane + iPlane] / ObjectiveFunc_New[2*nPlane + iPlane];
-                Gradient[4*nPlane + iPlane] = (ObjectiveFunc_New[4*nPlane + iPlane] - ObjectiveFunc[4*nPlane + iPlane]) / delta_eps;
-
-                ObjectiveFunc_New[5*nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Twist(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-                Gradient[5*nPlane + iPlane] = (ObjectiveFunc_New[5*nPlane + iPlane] - ObjectiveFunc[5*nPlane + iPlane]) / delta_eps;
+                ObjectiveFunc_New[0 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Area(
+                    Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane],
+                    Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+                Gradient[0 * nPlane + iPlane] =
+                    (ObjectiveFunc_New[0 * nPlane + iPlane] - ObjectiveFunc[0 * nPlane + iPlane]) / delta_eps;
+
+                ObjectiveFunc_New[1 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_MaxThickness(
+                    Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane],
+                    Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+                Gradient[1 * nPlane + iPlane] =
+                    (ObjectiveFunc_New[1 * nPlane + iPlane] - ObjectiveFunc[1 * nPlane + iPlane]) / delta_eps;
+
+                ObjectiveFunc_New[2 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Chord(
+                    Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane],
+                    Zcoord_Airfoil[iPlane]);
+                Gradient[2 * nPlane + iPlane] =
+                    (ObjectiveFunc_New[2 * nPlane + iPlane] - ObjectiveFunc[2 * nPlane + iPlane]) / delta_eps;
+
+                ObjectiveFunc_New[3 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_LERadius(
+                    Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane],
+                    Zcoord_Airfoil[iPlane]);
+                Gradient[3 * nPlane + iPlane] =
+                    (ObjectiveFunc_New[3 * nPlane + iPlane] - ObjectiveFunc[3 * nPlane + iPlane]) / delta_eps;
+
+                ObjectiveFunc_New[4 * nPlane + iPlane] =
+                    ObjectiveFunc_New[1 * nPlane + iPlane] / ObjectiveFunc_New[2 * nPlane + iPlane];
+                Gradient[4 * nPlane + iPlane] =
+                    (ObjectiveFunc_New[4 * nPlane + iPlane] - ObjectiveFunc[4 * nPlane + iPlane]) / delta_eps;
+
+                ObjectiveFunc_New[5 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Twist(
+                    Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane],
+                    Zcoord_Airfoil[iPlane]);
+                Gradient[5 * nPlane + iPlane] =
+                    (ObjectiveFunc_New[5 * nPlane + iPlane] - ObjectiveFunc[5 * nPlane + iPlane]) / delta_eps;
 
               }
 
               else {
-
-                ObjectiveFunc_New[0*nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Area(Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-                Gradient[0*nPlane + iPlane] = (ObjectiveFunc_New[0*nPlane + iPlane] - ObjectiveFunc[0*nPlane + iPlane]) / delta_eps;
-
-                ObjectiveFunc_New[1*nPlane + iPlane] = geometry_container[ZONE_0]->Compute_MaxThickness(Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-                Gradient[1*nPlane + iPlane] = (ObjectiveFunc_New[1*nPlane + iPlane] - ObjectiveFunc[1*nPlane + iPlane]) / delta_eps;
-
-                ObjectiveFunc_New[2*nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Chord(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-                Gradient[2*nPlane + iPlane] = (ObjectiveFunc_New[2*nPlane + iPlane] - ObjectiveFunc[2*nPlane + iPlane]) / delta_eps;
-
-                ObjectiveFunc_New[3*nPlane + iPlane] = geometry_container[ZONE_0]->Compute_LERadius(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-                Gradient[3*nPlane + iPlane] = (ObjectiveFunc_New[3*nPlane + iPlane] - ObjectiveFunc[3*nPlane + iPlane]) / delta_eps;
-
-                ObjectiveFunc_New[4*nPlane + iPlane] = ObjectiveFunc_New[1*nPlane + iPlane] / ObjectiveFunc_New[2*nPlane + iPlane];
-                Gradient[4*nPlane + iPlane] = (ObjectiveFunc_New[4*nPlane + iPlane] - ObjectiveFunc[4*nPlane + iPlane]) / delta_eps;
-
-                ObjectiveFunc_New[5*nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Twist(Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
-                Gradient[5*nPlane + iPlane] = (ObjectiveFunc_New[5*nPlane + iPlane] - ObjectiveFunc[5*nPlane + iPlane]) / delta_eps;
-
+                ObjectiveFunc_New[0 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Area(
+                    Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane],
+                    Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+                Gradient[0 * nPlane + iPlane] =
+                    (ObjectiveFunc_New[0 * nPlane + iPlane] - ObjectiveFunc[0 * nPlane + iPlane]) / delta_eps;
+
+                ObjectiveFunc_New[1 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_MaxThickness(
+                    Plane_P0[iPlane], Plane_Normal[iPlane], config_container[ZONE_0], Xcoord_Airfoil[iPlane],
+                    Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane]);
+                Gradient[1 * nPlane + iPlane] =
+                    (ObjectiveFunc_New[1 * nPlane + iPlane] - ObjectiveFunc[1 * nPlane + iPlane]) / delta_eps;
+
+                ObjectiveFunc_New[2 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Chord(
+                    Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane],
+                    Zcoord_Airfoil[iPlane]);
+                Gradient[2 * nPlane + iPlane] =
+                    (ObjectiveFunc_New[2 * nPlane + iPlane] - ObjectiveFunc[2 * nPlane + iPlane]) / delta_eps;
+
+                ObjectiveFunc_New[3 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_LERadius(
+                    Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane],
+                    Zcoord_Airfoil[iPlane]);
+                Gradient[3 * nPlane + iPlane] =
+                    (ObjectiveFunc_New[3 * nPlane + iPlane] - ObjectiveFunc[3 * nPlane + iPlane]) / delta_eps;
+
+                ObjectiveFunc_New[4 * nPlane + iPlane] =
+                    ObjectiveFunc_New[1 * nPlane + iPlane] / ObjectiveFunc_New[2 * nPlane + iPlane];
+                Gradient[4 * nPlane + iPlane] =
+                    (ObjectiveFunc_New[4 * nPlane + iPlane] - ObjectiveFunc[4 * nPlane + iPlane]) / delta_eps;
+
+                ObjectiveFunc_New[5 * nPlane + iPlane] = geometry_container[ZONE_0]->Compute_Twist(
+                    Plane_P0[iPlane], Plane_Normal[iPlane], Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane],
+                    Zcoord_Airfoil[iPlane]);
+                Gradient[5 * nPlane + iPlane] =
+                    (ObjectiveFunc_New[5 * nPlane + iPlane] - ObjectiveFunc[5 * nPlane + iPlane]) / delta_eps;
               }
-
             }
           }
 
         }
 
         else {
-
           if (config_container[ZONE_0]->GetGeo_Description() == FUSELAGE) {
-            Fuselage_Volume_Grad            = 0.0;
-            Fuselage_WettedArea_Grad        = 0.0;
-            Fuselage_MinWidth_Grad          = 0.0;
-            Fuselage_MaxWidth_Grad          = 0.0;
+            Fuselage_Volume_Grad = 0.0;
+            Fuselage_WettedArea_Grad = 0.0;
+            Fuselage_MinWidth_Grad = 0.0;
+            Fuselage_MaxWidth_Grad = 0.0;
             Fuselage_MinWaterLineWidth_Grad = 0.0;
             Fuselage_MaxWaterLineWidth_Grad = 0.0;
-            Fuselage_MinHeight_Grad         = 0.0;
-            Fuselage_MaxHeight_Grad         = 0.0;
-            Fuselage_MaxCurvature_Grad      = 0.0;
+            Fuselage_MinHeight_Grad = 0.0;
+            Fuselage_MaxHeight_Grad = 0.0;
+            Fuselage_MaxCurvature_Grad = 0.0;
 
             for (iPlane = 0; iPlane < nPlane; iPlane++) {
-              Gradient[0*nPlane + iPlane] = 0.0;
-              Gradient[1*nPlane + iPlane] = 0.0;
-              Gradient[2*nPlane + iPlane] = 0.0;
-              Gradient[3*nPlane + iPlane] = 0.0;
-              Gradient[4*nPlane + iPlane] = 0.0;
+              Gradient[0 * nPlane + iPlane] = 0.0;
+              Gradient[1 * nPlane + iPlane] = 0.0;
+              Gradient[2 * nPlane + iPlane] = 0.0;
+              Gradient[3 * nPlane + iPlane] = 0.0;
+              Gradient[4 * nPlane + iPlane] = 0.0;
             }
 
-          }
-          else if (config_container[ZONE_0]->GetGeo_Description() == NACELLE) {
-            Nacelle_Volume_Grad          = 0.0;
-            Nacelle_MinThickness_Grad    = 0.0;
-            Nacelle_MaxThickness_Grad    = 0.0;
-            Nacelle_MinChord_Grad        = 0.0;
-            Nacelle_MaxChord_Grad        = 0.0;
-            Nacelle_MinLERadius_Grad     = 0.0;
-            Nacelle_MaxLERadius_Grad     = 0.0;
-            Nacelle_MinToC_Grad          = 0.0;
-            Nacelle_MaxToC_Grad          = 0.0;
-            Nacelle_ObjFun_MinToC_Grad   = 0.0;
-            Nacelle_MaxTwist_Grad        = 0.0;
+          } else if (config_container[ZONE_0]->GetGeo_Description() == NACELLE) {
+            Nacelle_Volume_Grad = 0.0;
+            Nacelle_MinThickness_Grad = 0.0;
+            Nacelle_MaxThickness_Grad = 0.0;
+            Nacelle_MinChord_Grad = 0.0;
+            Nacelle_MaxChord_Grad = 0.0;
+            Nacelle_MinLERadius_Grad = 0.0;
+            Nacelle_MaxLERadius_Grad = 0.0;
+            Nacelle_MinToC_Grad = 0.0;
+            Nacelle_MaxToC_Grad = 0.0;
+            Nacelle_ObjFun_MinToC_Grad = 0.0;
+            Nacelle_MaxTwist_Grad = 0.0;
 
             for (iPlane = 0; iPlane < nPlane; iPlane++) {
-              Gradient[0*nPlane + iPlane] = 0.0;
-              Gradient[1*nPlane + iPlane] = 0.0;
-              Gradient[2*nPlane + iPlane] = 0.0;
-              Gradient[3*nPlane + iPlane] = 0.0;
-              Gradient[4*nPlane + iPlane] = 0.0;
-              Gradient[5*nPlane + iPlane] = 0.0;
+              Gradient[0 * nPlane + iPlane] = 0.0;
+              Gradient[1 * nPlane + iPlane] = 0.0;
+              Gradient[2 * nPlane + iPlane] = 0.0;
+              Gradient[3 * nPlane + iPlane] = 0.0;
+              Gradient[4 * nPlane + iPlane] = 0.0;
+              Gradient[5 * nPlane + iPlane] = 0.0;
             }
-          }
-          else  {
-            Wing_Volume_Grad          = 0.0;
-            Wing_MinThickness_Grad    = 0.0;
-            Wing_MaxThickness_Grad    = 0.0;
-            Wing_MinChord_Grad        = 0.0;
-            Wing_MaxChord_Grad        = 0.0;
-            Wing_MinLERadius_Grad     = 0.0;
-            Wing_MaxLERadius_Grad     = 0.0;
-            Wing_MinToC_Grad          = 0.0;
-            Wing_MaxToC_Grad          = 0.0;
-            Wing_ObjFun_MinToC_Grad   = 0.0;
-            Wing_MaxTwist_Grad        = 0.0;
-            Wing_MaxCurvature_Grad    = 0.0;
-            Wing_MaxDihedral_Grad     = 0.0;
+          } else {
+            Wing_Volume_Grad = 0.0;
+            Wing_MinThickness_Grad = 0.0;
+            Wing_MaxThickness_Grad = 0.0;
+            Wing_MinChord_Grad = 0.0;
+            Wing_MaxChord_Grad = 0.0;
+            Wing_MinLERadius_Grad = 0.0;
+            Wing_MaxLERadius_Grad = 0.0;
+            Wing_MinToC_Grad = 0.0;
+            Wing_MaxToC_Grad = 0.0;
+            Wing_ObjFun_MinToC_Grad = 0.0;
+            Wing_MaxTwist_Grad = 0.0;
+            Wing_MaxCurvature_Grad = 0.0;
+            Wing_MaxDihedral_Grad = 0.0;
 
             for (iPlane = 0; iPlane < nPlane; iPlane++) {
-              Gradient[0*nPlane + iPlane] = 0.0;
-              Gradient[1*nPlane + iPlane] = 0.0;
-              Gradient[2*nPlane + iPlane] = 0.0;
-              Gradient[3*nPlane + iPlane] = 0.0;
-              Gradient[4*nPlane + iPlane] = 0.0;
-              Gradient[5*nPlane + iPlane] = 0.0;
+              Gradient[0 * nPlane + iPlane] = 0.0;
+              Gradient[1 * nPlane + iPlane] = 0.0;
+              Gradient[2 * nPlane + iPlane] = 0.0;
+              Gradient[3 * nPlane + iPlane] = 0.0;
+              Gradient[4 * nPlane + iPlane] = 0.0;
+              Gradient[5 * nPlane + iPlane] = 0.0;
             }
           }
-
         }
 
         /*--- Screen output ---*/
 
         if (config_container[ZONE_0]->GetGeo_Description() == FUSELAGE) {
           if (geometry_container[ZONE_0]->GetnDim() == 3) {
-            cout << "\nFuselage volume grad.: "    << Fuselage_Volume_Grad << ". ";
-            cout << "Fuselage wetted area grad.: "    << Fuselage_WettedArea_Grad << ". ";
-            cout << "Fuselage min. width grad.: "  << Fuselage_MinWidth_Grad << ". ";
-            cout << "Fuselage max. width grad.: "  << Fuselage_MaxWidth_Grad << "."  << endl;
-            cout << "Fuselage min. waterline width grad.: "  << Fuselage_MinWaterLineWidth_Grad << ". ";
-            cout << "Fuselage max. waterline width grad.: "  << Fuselage_MaxWaterLineWidth_Grad << "."  << endl;
+            cout << "\nFuselage volume grad.: " << Fuselage_Volume_Grad << ". ";
+            cout << "Fuselage wetted area grad.: " << Fuselage_WettedArea_Grad << ". ";
+            cout << "Fuselage min. width grad.: " << Fuselage_MinWidth_Grad << ". ";
+            cout << "Fuselage max. width grad.: " << Fuselage_MaxWidth_Grad << "." << endl;
+            cout << "Fuselage min. waterline width grad.: " << Fuselage_MinWaterLineWidth_Grad << ". ";
+            cout << "Fuselage max. waterline width grad.: " << Fuselage_MaxWaterLineWidth_Grad << "." << endl;
             cout << "Fuselage min. height grad.: " << Fuselage_MinHeight_Grad << ". ";
             cout << "Fuselage max. height grad.: " << Fuselage_MaxHeight_Grad << ". ";
-            cout << "Fuselage max. curv. grad.: "  << Fuselage_MaxCurvature_Grad << ".";
+            cout << "Fuselage max. curv. grad.: " << Fuselage_MaxCurvature_Grad << ".";
           }
 
           for (iPlane = 0; iPlane < nPlane; iPlane++) {
             if (Xcoord_Airfoil[iPlane].size() > 1) {
-              cout << "\nStation " << (iPlane+1) << ". XCoord: " << Plane_P0[iPlane][0] << ". ";
-              cout << "Area grad.: "                 << Gradient[0*nPlane + iPlane] << ". ";
-              cout << "Length grad.: "               << Gradient[1*nPlane + iPlane] << ". ";
-              cout << "Width grad.: "                << Gradient[2*nPlane + iPlane] << ". ";
-              cout << "Waterline width grad.: "      << Gradient[3*nPlane + iPlane] << ". ";
-              cout << "Height grad.: "               << Gradient[4*nPlane + iPlane] << ". ";
+              cout << "\nStation " << (iPlane + 1) << ". XCoord: " << Plane_P0[iPlane][0] << ". ";
+              cout << "Area grad.: " << Gradient[0 * nPlane + iPlane] << ". ";
+              cout << "Length grad.: " << Gradient[1 * nPlane + iPlane] << ". ";
+              cout << "Width grad.: " << Gradient[2 * nPlane + iPlane] << ". ";
+              cout << "Waterline width grad.: " << Gradient[3 * nPlane + iPlane] << ". ";
+              cout << "Height grad.: " << Gradient[4 * nPlane + iPlane] << ". ";
             }
           }
-        }
-        else if (config_container[ZONE_0]->GetGeo_Description() == NACELLE) {
+        } else if (config_container[ZONE_0]->GetGeo_Description() == NACELLE) {
           if (geometry_container[ZONE_0]->GetnDim() == 3) {
-            cout << "\nNacelle volume grad.: "             << Nacelle_Volume_Grad << ". ";
-            cout << "Nacelle min. thickness grad.: "  << Nacelle_MinThickness_Grad << ". ";
-            cout << "Nacelle max. thickness grad.: "  << Nacelle_MaxThickness_Grad << ". ";
-            cout << "Nacelle min. chord grad.: "           << Nacelle_MinChord_Grad << ". ";
-            cout << "Nacelle max. chord grad.: "           << Nacelle_MaxChord_Grad << "." << endl;
-            cout << "Nacelle min. LE radius grad.: "       << Nacelle_MinChord_Grad << ". ";
-            cout << "Nacelle max. LE radius grad.: "       << Nacelle_MaxChord_Grad << ". ";
-            cout << "Nacelle min. ToC grad.: "             << Nacelle_MinToC_Grad << ". ";
-            cout << "Nacelle max. ToC grad.: "             << Nacelle_MaxToC_Grad << ". ";
-            cout << "Nacelle delta ToC grad.: "            << Nacelle_ObjFun_MinToC_Grad << "." << endl;
-            cout << "Nacelle max. twist grad.: "           << Nacelle_MaxTwist_Grad << ". ";
+            cout << "\nNacelle volume grad.: " << Nacelle_Volume_Grad << ". ";
+            cout << "Nacelle min. thickness grad.: " << Nacelle_MinThickness_Grad << ". ";
+            cout << "Nacelle max. thickness grad.: " << Nacelle_MaxThickness_Grad << ". ";
+            cout << "Nacelle min. chord grad.: " << Nacelle_MinChord_Grad << ". ";
+            cout << "Nacelle max. chord grad.: " << Nacelle_MaxChord_Grad << "." << endl;
+            cout << "Nacelle min. LE radius grad.: " << Nacelle_MinChord_Grad << ". ";
+            cout << "Nacelle max. LE radius grad.: " << Nacelle_MaxChord_Grad << ". ";
+            cout << "Nacelle min. ToC grad.: " << Nacelle_MinToC_Grad << ". ";
+            cout << "Nacelle max. ToC grad.: " << Nacelle_MaxToC_Grad << ". ";
+            cout << "Nacelle delta ToC grad.: " << Nacelle_ObjFun_MinToC_Grad << "." << endl;
+            cout << "Nacelle max. twist grad.: " << Nacelle_MaxTwist_Grad << ". ";
           }
 
           for (iPlane = 0; iPlane < nPlane; iPlane++) {
             if (Xcoord_Airfoil[iPlane].size() > 1) {
-              cout << "\nStation " << (iPlane+1) << ". YCoord: " << Plane_P0[iPlane][1] << ". ";
-              cout << "Area grad.: "                 << Gradient[0*nPlane + iPlane] << ". ";
-              cout << "Thickness grad.: "            << Gradient[1*nPlane + iPlane] << ". ";
-              cout << "Chord grad.: "                << Gradient[2*nPlane + iPlane] << ". ";
-              cout << "LE radius grad.: "            << Gradient[3*nPlane + iPlane] << ". ";
-              cout << "ToC grad.: "                  << Gradient[4*nPlane + iPlane] << ". ";
-              cout << "Twist angle grad.: "          << Gradient[5*nPlane + iPlane] << ". ";
+              cout << "\nStation " << (iPlane + 1) << ". YCoord: " << Plane_P0[iPlane][1] << ". ";
+              cout << "Area grad.: " << Gradient[0 * nPlane + iPlane] << ". ";
+              cout << "Thickness grad.: " << Gradient[1 * nPlane + iPlane] << ". ";
+              cout << "Chord grad.: " << Gradient[2 * nPlane + iPlane] << ". ";
+              cout << "LE radius grad.: " << Gradient[3 * nPlane + iPlane] << ". ";
+              cout << "ToC grad.: " << Gradient[4 * nPlane + iPlane] << ". ";
+              cout << "Twist angle grad.: " << Gradient[5 * nPlane + iPlane] << ". ";
             }
           }
-        }
-        else {
+        } else {
           if (geometry_container[ZONE_0]->GetnDim() == 3) {
-            cout << "\nWing volume grad.: "             << Wing_Volume_Grad << ". ";
-            cout << "Wing min. thickness grad.: "  << Wing_MinThickness_Grad << ". ";
-            cout << "Wing max. thickness grad.: "  << Wing_MaxThickness_Grad << ". ";
-            cout << "Wing min. chord grad.: "           << Wing_MinChord_Grad << ". ";
-            cout << "Wing max. chord grad.: "           << Wing_MaxChord_Grad << "." << endl;
-            cout << "Wing min. LE radius grad.: "       << Wing_MinChord_Grad << ". ";
-            cout << "Wing max. LE radius grad.: "       << Wing_MaxChord_Grad << ". ";
-            cout << "Wing min. ToC grad.: "             << Wing_MinToC_Grad << ". ";
-            cout << "Wing max. ToC grad.: "             << Wing_MaxToC_Grad << ". ";
-            cout << "Wing delta ToC grad.: "            << Wing_ObjFun_MinToC_Grad << "." << endl;
-            cout << "Wing max. twist grad.: "           << Wing_MaxTwist_Grad << ". ";
-            cout << "Wing max. curv. grad.: "           << Wing_MaxCurvature_Grad << ". ";
-            cout << "Wing max. dihedral grad.: "        << Wing_MaxDihedral_Grad << "." << endl;
+            cout << "\nWing volume grad.: " << Wing_Volume_Grad << ". ";
+            cout << "Wing min. thickness grad.: " << Wing_MinThickness_Grad << ". ";
+            cout << "Wing max. thickness grad.: " << Wing_MaxThickness_Grad << ". ";
+            cout << "Wing min. chord grad.: " << Wing_MinChord_Grad << ". ";
+            cout << "Wing max. chord grad.: " << Wing_MaxChord_Grad << "." << endl;
+            cout << "Wing min. LE radius grad.: " << Wing_MinChord_Grad << ". ";
+            cout << "Wing max. LE radius grad.: " << Wing_MaxChord_Grad << ". ";
+            cout << "Wing min. ToC grad.: " << Wing_MinToC_Grad << ". ";
+            cout << "Wing max. ToC grad.: " << Wing_MaxToC_Grad << ". ";
+            cout << "Wing delta ToC grad.: " << Wing_ObjFun_MinToC_Grad << "." << endl;
+            cout << "Wing max. twist grad.: " << Wing_MaxTwist_Grad << ". ";
+            cout << "Wing max. curv. grad.: " << Wing_MaxCurvature_Grad << ". ";
+            cout << "Wing max. dihedral grad.: " << Wing_MaxDihedral_Grad << "." << endl;
           }
 
           for (iPlane = 0; iPlane < nPlane; iPlane++) {
             if (Xcoord_Airfoil[iPlane].size() > 1) {
-              cout << "\nStation " << (iPlane+1) << ". YCoord: " << Plane_P0[iPlane][1] << ". ";
-              cout << "Area grad.: "                 << Gradient[0*nPlane + iPlane] << ". ";
-              cout << "Thickness grad.: "            << Gradient[1*nPlane + iPlane] << ". ";
-              cout << "Chord grad.: "                << Gradient[2*nPlane + iPlane] << ". ";
-              cout << "LE radius grad.: "            << Gradient[3*nPlane + iPlane] << ". ";
-              cout << "ToC grad.: "                  << Gradient[4*nPlane + iPlane] << ". ";
-              cout << "Twist angle grad.: "          << Gradient[5*nPlane + iPlane] << ". ";
+              cout << "\nStation " << (iPlane + 1) << ". YCoord: " << Plane_P0[iPlane][1] << ". ";
+              cout << "Area grad.: " << Gradient[0 * nPlane + iPlane] << ". ";
+              cout << "Thickness grad.: " << Gradient[1 * nPlane + iPlane] << ". ";
+              cout << "Chord grad.: " << Gradient[2 * nPlane + iPlane] << ". ";
+              cout << "LE radius grad.: " << Gradient[3 * nPlane + iPlane] << ". ";
+              cout << "ToC grad.: " << Gradient[4 * nPlane + iPlane] << ". ";
+              cout << "Twist angle grad.: " << Gradient[5 * nPlane + iPlane] << ". ";
             }
           }
         }
 
         cout << endl;
 
-
         if (iDV == 0) {
           if (tabTecplot) Gradient_file << "TITLE = \"SU2_GEO Gradient\"" << endl;
           if (tabTecplot) Gradient_file << "VARIABLES = //" << endl;
 
           if (geometry_container[ZONE_0]->GetnDim() == 2) {
-            Gradient_file << "\"DESIGN_VARIABLE\",\"AIRFOIL_AREA\",\"AIRFOIL_THICKNESS\",\"AIRFOIL_CHORD\",\"AIRFOIL_LE_RADIUS\",\"AIRFOIL_TOC\",\"AIRFOIL_ALPHA\"";
-          }
-          else if (geometry_container[ZONE_0]->GetnDim() == 3) {
-
+            Gradient_file << "\"DESIGN_VARIABLE\",\"AIRFOIL_AREA\",\"AIRFOIL_THICKNESS\",\"AIRFOIL_CHORD\",\"AIRFOIL_"
+                             "LE_RADIUS\",\"AIRFOIL_TOC\",\"AIRFOIL_ALPHA\"";
+          } else if (geometry_container[ZONE_0]->GetnDim() == 3) {
             if (config_container[ZONE_0]->GetGeo_Description() == FUSELAGE) {
               Gradient_file << "\"DESIGN_VARIABLE\",";
-              Gradient_file << "\"FUSELAGE_VOLUME\",\"FUSELAGE_WETTED_AREA\",\"FUSELAGE_MIN_WIDTH\",\"FUSELAGE_MAX_WIDTH\",\"FUSELAGE_MIN_WATERLINE_WIDTH\",\"FUSELAGE_MAX_WATERLINE_WIDTH\",\"FUSELAGE_MIN_HEIGHT\",\"FUSELAGE_MAX_HEIGHT\",\"FUSELAGE_MAX_CURVATURE\",";
-              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION"<< (iPlane+1) << "_AREA\",";
-              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION"<< (iPlane+1) << "_LENGTH\",";
-              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION"<< (iPlane+1) << "_WIDTH\",";
-              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION"<< (iPlane+1) << "_WATERLINE_WIDTH\",";
+              Gradient_file << "\"FUSELAGE_VOLUME\",\"FUSELAGE_WETTED_AREA\",\"FUSELAGE_MIN_WIDTH\",\"FUSELAGE_MAX_"
+                               "WIDTH\",\"FUSELAGE_MIN_WATERLINE_WIDTH\",\"FUSELAGE_MAX_WATERLINE_WIDTH\",\"FUSELAGE_"
+                               "MIN_HEIGHT\",\"FUSELAGE_MAX_HEIGHT\",\"FUSELAGE_MAX_CURVATURE\",";
+              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION" << (iPlane + 1) << "_AREA\",";
+              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION" << (iPlane + 1) << "_LENGTH\",";
+              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION" << (iPlane + 1) << "_WIDTH\",";
+              for (iPlane = 0; iPlane < nPlane; iPlane++)
+                Gradient_file << "\"STATION" << (iPlane + 1) << "_WATERLINE_WIDTH\",";
               for (iPlane = 0; iPlane < nPlane; iPlane++) {
-                Gradient_file << "\"STATION"<< (iPlane+1) << "_HEIGHT\"";
-                if (iPlane != nPlane-1) Gradient_file << ",";
+                Gradient_file << "\"STATION" << (iPlane + 1) << "_HEIGHT\"";
+                if (iPlane != nPlane - 1) Gradient_file << ",";
               }
-            }
-            else if (config_container[ZONE_0]->GetGeo_Description() == NACELLE) {
+            } else if (config_container[ZONE_0]->GetGeo_Description() == NACELLE) {
               Gradient_file << "\"DESIGN_VARIABLE\",";
-              Gradient_file << "\"NACELLE_VOLUME\",\"NACELLE_MIN_THICKNESS\",\"NACELLE_MAX_THICKNESS\",\"NACELLE_MIN_CHORD\",\"NACELLE_MAX_CHORD\",\"NACELLE_MIN_LE_RADIUS\",\"NACELLE_MAX_LE_RADIUS\",\"NACELLE_MIN_TOC\",\"NACELLE_MAX_TOC\",\"NACELLE_OBJFUN_MIN_TOC\",\"NACELLE_MAX_TWIST\",";
-              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION"<< (iPlane+1) << "_AREA\",";
-              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION"<< (iPlane+1) << "_THICKNESS\",";
-              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION"<< (iPlane+1) << "_CHORD\",";
-              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION"<< (iPlane+1) << "_LE_RADIUS\",";
-              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION"<< (iPlane+1) << "_TOC\",";
+              Gradient_file
+                  << "\"NACELLE_VOLUME\",\"NACELLE_MIN_THICKNESS\",\"NACELLE_MAX_THICKNESS\",\"NACELLE_MIN_CHORD\","
+                     "\"NACELLE_MAX_CHORD\",\"NACELLE_MIN_LE_RADIUS\",\"NACELLE_MAX_LE_RADIUS\",\"NACELLE_MIN_TOC\","
+                     "\"NACELLE_MAX_TOC\",\"NACELLE_OBJFUN_MIN_TOC\",\"NACELLE_MAX_TWIST\",";
+              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION" << (iPlane + 1) << "_AREA\",";
+              for (iPlane = 0; iPlane < nPlane; iPlane++)
+                Gradient_file << "\"STATION" << (iPlane + 1) << "_THICKNESS\",";
+              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION" << (iPlane + 1) << "_CHORD\",";
+              for (iPlane = 0; iPlane < nPlane; iPlane++)
+                Gradient_file << "\"STATION" << (iPlane + 1) << "_LE_RADIUS\",";
+              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION" << (iPlane + 1) << "_TOC\",";
               for (iPlane = 0; iPlane < nPlane; iPlane++) {
-                Gradient_file << "\"STATION"<< (iPlane+1) << "_TWIST\"";
-                if (iPlane != nPlane-1) Gradient_file << ",";
+                Gradient_file << "\"STATION" << (iPlane + 1) << "_TWIST\"";
+                if (iPlane != nPlane - 1) Gradient_file << ",";
               }
-            }
-            else {
+            } else {
               Gradient_file << "\"DESIGN_VARIABLE\",";
-              Gradient_file << "\"WING_VOLUME\",\"WING_MIN_THICKNESS\",\"WING_MAX_THICKNESS\",\"WING_MIN_CHORD\",\"WING_MAX_CHORD\",\"WING_MIN_LE_RADIUS\",\"WING_MAX_LE_RADIUS\",\"WING_MIN_TOC\",\"WING_MAX_TOC\",\"WING_OBJFUN_MIN_TOC\",\"WING_MAX_TWIST\",\"WING_MAX_CURVATURE\",\"WING_MAX_DIHEDRAL\",";
-              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION"<< (iPlane+1) << "_AREA\",";
-              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION"<< (iPlane+1) << "_THICKNESS\",";
-              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION"<< (iPlane+1) << "_CHORD\",";
-              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION"<< (iPlane+1) << "_LE_RADIUS\",";
-              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION"<< (iPlane+1) << "_TOC\",";
+              Gradient_file
+                  << "\"WING_VOLUME\",\"WING_MIN_THICKNESS\",\"WING_MAX_THICKNESS\",\"WING_MIN_CHORD\",\"WING_MAX_"
+                     "CHORD\",\"WING_MIN_LE_RADIUS\",\"WING_MAX_LE_RADIUS\",\"WING_MIN_TOC\",\"WING_MAX_TOC\",\"WING_"
+                     "OBJFUN_MIN_TOC\",\"WING_MAX_TWIST\",\"WING_MAX_CURVATURE\",\"WING_MAX_DIHEDRAL\",";
+              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION" << (iPlane + 1) << "_AREA\",";
+              for (iPlane = 0; iPlane < nPlane; iPlane++)
+                Gradient_file << "\"STATION" << (iPlane + 1) << "_THICKNESS\",";
+              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION" << (iPlane + 1) << "_CHORD\",";
+              for (iPlane = 0; iPlane < nPlane; iPlane++)
+                Gradient_file << "\"STATION" << (iPlane + 1) << "_LE_RADIUS\",";
+              for (iPlane = 0; iPlane < nPlane; iPlane++) Gradient_file << "\"STATION" << (iPlane + 1) << "_TOC\",";
               for (iPlane = 0; iPlane < nPlane; iPlane++) {
-                Gradient_file << "\"STATION"<< (iPlane+1) << "_TWIST\"";
-                if (iPlane != nPlane-1) Gradient_file << ",";
+                Gradient_file << "\"STATION" << (iPlane + 1) << "_TWIST\"";
+                if (iPlane != nPlane - 1) Gradient_file << ",";
               }
             }
-
           }
 
-          if (tabTecplot) Gradient_file << "\nZONE T= \"Geometrical variables (gradient)\"" << endl;
-          else Gradient_file << endl;
+          if (tabTecplot)
+            Gradient_file << "\nZONE T= \"Geometrical variables (gradient)\"" << endl;
+          else
+            Gradient_file << endl;
         }
 
-        Gradient_file << (iDV) <<",";
+        Gradient_file << (iDV) << ",";
 
         if (config_container[ZONE_0]->GetGeo_Description() == FUSELAGE) {
           if (geometry_container[ZONE_0]->GetnDim() == 3) {
-            Gradient_file << Fuselage_Volume_Grad <<","<< Fuselage_WettedArea_Grad <<","<< Fuselage_MinWidth_Grad <<","<< Fuselage_MaxWidth_Grad <<","<< Fuselage_MinWaterLineWidth_Grad <<","<< Fuselage_MaxWaterLineWidth_Grad <<","<< Fuselage_MinHeight_Grad <<","<< Fuselage_MaxHeight_Grad <<","<< Fuselage_MaxCurvature_Grad <<",";
+            Gradient_file << Fuselage_Volume_Grad << "," << Fuselage_WettedArea_Grad << "," << Fuselage_MinWidth_Grad
+                          << "," << Fuselage_MaxWidth_Grad << "," << Fuselage_MinWaterLineWidth_Grad << ","
+                          << Fuselage_MaxWaterLineWidth_Grad << "," << Fuselage_MinHeight_Grad << ","
+                          << Fuselage_MaxHeight_Grad << "," << Fuselage_MaxCurvature_Grad << ",";
           }
-          for (iPlane = 0; iPlane < nPlane*5; iPlane++) {
+          for (iPlane = 0; iPlane < nPlane * 5; iPlane++) {
             Gradient_file << Gradient[iPlane];
-            if (iPlane != (nPlane*5)-1) Gradient_file <<",";
+            if (iPlane != (nPlane * 5) - 1) Gradient_file << ",";
           }
-        }
-        else if (config_container[ZONE_0]->GetGeo_Description() == NACELLE) {
+        } else if (config_container[ZONE_0]->GetGeo_Description() == NACELLE) {
           if (geometry_container[ZONE_0]->GetnDim() == 3) {
-            Gradient_file << Nacelle_Volume_Grad <<","<< Nacelle_MinThickness_Grad <<","<< Nacelle_MaxThickness_Grad <<","<< Nacelle_MinChord_Grad <<","<< Nacelle_MaxChord_Grad <<","<< Nacelle_MinLERadius_Grad <<","<< Nacelle_MaxLERadius_Grad<<","<< Nacelle_MinToC_Grad <<","<< Nacelle_MaxToC_Grad <<","<< Nacelle_ObjFun_MinToC_Grad <<","<< Nacelle_MaxTwist_Grad <<",";
+            Gradient_file << Nacelle_Volume_Grad << "," << Nacelle_MinThickness_Grad << "," << Nacelle_MaxThickness_Grad
+                          << "," << Nacelle_MinChord_Grad << "," << Nacelle_MaxChord_Grad << ","
+                          << Nacelle_MinLERadius_Grad << "," << Nacelle_MaxLERadius_Grad << "," << Nacelle_MinToC_Grad
+                          << "," << Nacelle_MaxToC_Grad << "," << Nacelle_ObjFun_MinToC_Grad << ","
+                          << Nacelle_MaxTwist_Grad << ",";
           }
-          for (iPlane = 0; iPlane < nPlane*6; iPlane++) {
+          for (iPlane = 0; iPlane < nPlane * 6; iPlane++) {
             Gradient_file << Gradient[iPlane];
-            if (iPlane != (nPlane*6)-1) Gradient_file <<",";
+            if (iPlane != (nPlane * 6) - 1) Gradient_file << ",";
           }
-        }
-        else {
+        } else {
           if (geometry_container[ZONE_0]->GetnDim() == 3) {
-            Gradient_file << Wing_Volume_Grad <<","<< Wing_MinThickness_Grad <<","<< Wing_MaxThickness_Grad <<","<< Wing_MinChord_Grad <<","<< Wing_MaxChord_Grad <<","<< Wing_MinLERadius_Grad <<","<< Wing_MaxLERadius_Grad<<","<< Wing_MinToC_Grad <<","<< Wing_MaxToC_Grad <<","<< Wing_ObjFun_MinToC_Grad <<","<< Wing_MaxTwist_Grad <<","<< Wing_MaxCurvature_Grad <<","<< Wing_MaxDihedral_Grad <<",";
+            Gradient_file << Wing_Volume_Grad << "," << Wing_MinThickness_Grad << "," << Wing_MaxThickness_Grad << ","
+                          << Wing_MinChord_Grad << "," << Wing_MaxChord_Grad << "," << Wing_MinLERadius_Grad << ","
+                          << Wing_MaxLERadius_Grad << "," << Wing_MinToC_Grad << "," << Wing_MaxToC_Grad << ","
+                          << Wing_ObjFun_MinToC_Grad << "," << Wing_MaxTwist_Grad << "," << Wing_MaxCurvature_Grad
+                          << "," << Wing_MaxDihedral_Grad << ",";
           }
-          for (iPlane = 0; iPlane < nPlane*6; iPlane++) {
+          for (iPlane = 0; iPlane < nPlane * 6; iPlane++) {
             Gradient_file << Gradient[iPlane];
-            if (iPlane != (nPlane*6)-1) Gradient_file <<",";
+            if (iPlane != (nPlane * 6) - 1) Gradient_file << ",";
           }
         }
 
         Gradient_file << endl;
 
-        if (iDV != (config_container[ZONE_0]->GetnDV()-1)) cout <<"-------------------------------------------------------------------------" << endl;
-
+        if (iDV != (config_container[ZONE_0]->GetnDV() - 1))
+          cout << "-------------------------------------------------------------------------" << endl;
       }
-
     }
 
-    if (rank == MASTER_NODE)
-      Gradient_file.close();
-
+    if (rank == MASTER_NODE) Gradient_file.close();
   }
 
   if (rank == MASTER_NODE)
-    cout << endl <<"------------------------- Solver Postprocessing -------------------------" << endl;
+    cout << endl << "------------------------- Solver Postprocessing -------------------------" << endl;
 
-  delete [] Xcoord_Airfoil; delete [] Ycoord_Airfoil; delete [] Zcoord_Airfoil;
+  delete[] Xcoord_Airfoil;
+  delete[] Ycoord_Airfoil;
+  delete[] Zcoord_Airfoil;
 
-  delete [] ObjectiveFunc; delete [] ObjectiveFunc_New; delete [] Gradient;
+  delete[] ObjectiveFunc;
+  delete[] ObjectiveFunc_New;
+  delete[] Gradient;
 
-  for(iPlane = 0; iPlane < nPlane; iPlane++ ) {
+  for (iPlane = 0; iPlane < nPlane; iPlane++) {
     delete Plane_P0[iPlane];
     delete Plane_Normal[iPlane];
   }
-  delete [] Plane_P0;
-  delete [] Plane_Normal;
+  delete[] Plane_P0;
+  delete[] Plane_Normal;
 
   delete config;
   config = nullptr;
 
   if (rank == MASTER_NODE) cout << "Deleted main variables." << endl;
 
-
   if (geometry_container != nullptr) {
     for (iZone = 0; iZone < nZone; iZone++) {
       if (geometry_container[iZone] != nullptr) {
         delete geometry_container[iZone];
       }
     }
-    delete [] geometry_container;
+    delete[] geometry_container;
   }
   if (rank == MASTER_NODE) cout << "Deleted CGeometry container." << endl;
 
@@ -1256,7 +1470,7 @@ int main(int argc, char *argv[]) {
         delete FFDBox[iFFDBox];
       }
     }
-    delete [] FFDBox;
+    delete[] FFDBox;
   }
   if (rank == MASTER_NODE) cout << "Deleted CFreeFormDefBox class." << endl;
 
@@ -1266,7 +1480,7 @@ int main(int argc, char *argv[]) {
         delete config_container[iZone];
       }
     }
-    delete [] config_container;
+    delete[] config_container;
   }
   if (rank == MASTER_NODE) cout << "Deleted CConfig container." << endl;
 
@@ -1277,21 +1491,22 @@ int main(int argc, char *argv[]) {
 
   /*--- Compute/print the total time for performance benchmarking. ---*/
 
-  UsedTime = StopTime-StartTime;
+  UsedTime = StopTime - StartTime;
   if (rank == MASTER_NODE) {
-    cout << "\n\nCompleted in " << fixed << UsedTime << " seconds on "<< size;
-    if (size == 1) cout << " core." << endl; else cout << " cores." << endl;
+    cout << "\n\nCompleted in " << fixed << UsedTime << " seconds on " << size;
+    if (size == 1)
+      cout << " core." << endl;
+    else
+      cout << " cores." << endl;
   }
 
   /*--- Exit the solver cleanly ---*/
 
   if (rank == MASTER_NODE)
-    cout << endl <<"------------------------- Exit Success (SU2_GEO) ------------------------" << endl << endl;
-
+    cout << endl << "------------------------- Exit Success (SU2_GEO) ------------------------" << endl << endl;
 
   /*--- Finalize MPI parallelization ---*/
   SU2_MPI::Finalize();
 
   return EXIT_SUCCESS;
-
 }
diff --git a/SU2_GEO/src/meson.build b/SU2_GEO/src/meson.build
index 13e7e6f8875..dbbbbd25333 100644
--- a/SU2_GEO/src/meson.build
+++ b/SU2_GEO/src/meson.build
@@ -4,6 +4,6 @@ if get_option('enable-normal')
   su2_geo = executable('SU2_GEO',
                        su2_geo_src,
                        install: true,
-		       dependencies: [su2_deps, common_dep], 
+		       dependencies: [su2_deps, common_dep],
 		       cpp_args : [default_warning_flags, su2_cpp_args])
 endif
diff --git a/SU2_IDE/Eclipse/README b/SU2_IDE/Eclipse/README
index 454e31b4ebc..07c6b1c46f5 100644
--- a/SU2_IDE/Eclipse/README
+++ b/SU2_IDE/Eclipse/README
@@ -2,10 +2,10 @@ This README file includes instructions on how to use Eclipse with the SU2
 github repository. It is assumed that Eclipse has already been installed.
 -------------------------------------------------------------------------------
 1. Initial Eclipse Set-up
-In order to view files with helpful text highlighting and code navigation 
+In order to view files with helpful text highlighting and code navigation
 tools, install the packages for C++, Python, and Git:
 	Help -> Install New Software
-	Install packages for Git, C++ and Python, for example: 
+	Install packages for Git, C++ and Python, for example:
 		C/C++ Development Tools SDK
 		Eclipse EGit
 		PyDev for Eclipse
@@ -13,8 +13,8 @@ tools, install the packages for C++, Python, and Git:
 -------------------------------------------------------------------------------
 2. Get the code
 
-2a.If you have already cloned the SU2 source code, or prefer to clone via the 
-command line, you will need to import this project into the Eclipse Workspace: 
+2a.If you have already cloned the SU2 source code, or prefer to clone via the
+command line, you will need to import this project into the Eclipse Workspace:
 	File -> New -> Makefile project with existing code
 	Name the project and navigate to the appropriate directory.
 	Make sure "C++" is checked and select "finish"
@@ -37,13 +37,13 @@ command line, you will need to import this project into the Eclipse Workspace:
 If you did not clone the repository using Egit:
 	Window -> open perspective -> Git Repository Exploring
 	Window -> Show View -> Git Repositories
-	Add the repository: 
+	Add the repository:
 	In the Git repositories window, select "add an existing local git
-	repository to this view". 
+	repository to this view".
 	Browse to the location where you cloned the repository, select "finish"
 
-	When in the Git perspective, you will be able to see your local github 
-	repositories and graphically explore the branch structure. 
+	When in the Git perspective, you will be able to see your local github
+	repositories and graphically explore the branch structure.
 
 
 -------------------------------------------------------------------------------
@@ -54,7 +54,3 @@ If you did not clone the repository using Egit:
 	Select Project-> Properties to edit Eclipse behavior
 
 -------------------------------------------------------------------------------
-
-
-
-
diff --git a/SU2_PY/FSI_tools/FSIInterface.py b/SU2_PY/FSI_tools/FSIInterface.py
index 88c030ff6a0..bcd8526c5ee 100644
--- a/SU2_PY/FSI_tools/FSIInterface.py
+++ b/SU2_PY/FSI_tools/FSIInterface.py
@@ -41,6 +41,7 @@
 #  FSI Interface Class
 # ----------------------------------------------------------------------
 
+
 class Interface:
     """
     FSI interface class that handles fluid/solid solvers synchronisation and communication
@@ -52,161 +53,239 @@ def __init__(self, FSI_config, FluidSolver, SolidSolver, have_MPI):
         """
 
         if have_MPI:
-          from mpi4py import MPI
-          self.MPI = MPI
-          self.comm = MPI.COMM_WORLD			#MPI World communicator
-          self.have_MPI = True
-          myid = self.comm.Get_rank()
-        else:
-          self.comm = 0
-          self.have_MPI = False
-          myid = 0
-
-        self.rootProcess = 0				#the root process is chosen to be MPI rank = 0
-
-        self.nDim = FSI_config['NDIM']			#problem dimension
-
-        self.haveFluidSolver = False			#True if the fluid solver is initialized on the current rank
-        self.haveSolidSolver = False			#True if the solid solver is initialized on the current rank
-        self.haveFluidInterface = False			#True if the current rank owns at least one fluid interface node
-        self.haveSolidInterface = False			#True if the current rank owns at least one solid interface node
-
-        self.fluidSolverProcessors = list()		#list of partitions where the fluid solver is initialized
-        self.solidSolverProcessors = list()		#list of partitions where the solid solver is initialized
-        self.fluidInterfaceProcessors = list()          #list of partitions where there are fluid interface nodes
-        self.solidInterfaceProcessors = list() 	        #list of partitions where there are solid interface nodes
-
-        self.fluidInterfaceIdentifier = None		#object that can identify the f/s interface within the fluid solver
-        self.solidInterfaceIdentifier = None		#object that can identify the f/s interface within the solid solver
-
-        self.fluidGlobalIndexRange = {}			#contains the global FSI indexing of each fluid interface node for all partitions
-        self.solidGlobalIndexRange = {}			#contains the global FSI indexing of each solid interface node for all partitions
-
-        self.FluidHaloNodeList = {}			#contains the the indices (fluid solver indexing) of the halo nodes for each partition
-        self.fluidIndexing = {}				#links between the fluid solver indexing and the FSI indexing for the interface nodes
-        self.SolidHaloNodeList = {}			#contains the the indices (solid solver indexing) of the halo nodes for each partition
-        self.solidIndexing = {}				#links between the solid solver indexing and the FSI indexing for the interface nodes
-
-        self.nLocalFluidInterfaceNodes = 0		#number of nodes (halo nodes included) on the fluid interface, on each partition
-        self.nLocalFluidInterfaceHaloNode = 0		#number of halo nodes on the fluid intrface, on each partition
-        self.nLocalFluidInterfacePhysicalNodes = 0	#number of physical (= non halo) nodes on the fluid interface, on each partition
-        self.nFluidInterfaceNodes = np.array(int(0)) #number of nodes on the fluid interface, sum over all the partitions
-        self.nFluidInterfacePhysicalNodes = np.array(int(0)) #number of physical nodes on the fluid interface, sum over all partitions
-
-        self.nLocalSolidInterfaceNodes = 0     		#number of physical nodes on the solid interface, on each partition
-        self.nLocalSolidInterfaceHaloNode = 0		#number of halo nodes on the solid intrface, on each partition
-        self.nLocalSolidInterfacePhysicalNodes = 0	#number of physical (= non halo) nodes on the solid interface, on each partition
-        self.nSolidInterfaceNodes = np.array(int(0)) #number of nodes on the solid interface, sum over all partitions
-        self.nSolidInterfacePhysicalNodes = np.array(int(0)) #number of physical nodes on the solid interface, sum over all partitions
-
-        if FSI_config['MATCHING_MESH'] == 'NO' and (FSI_config['MESH_INTERP_METHOD'] == 'RBF' or FSI_config['MESH_INTERP_METHOD'] == 'TPS'):
-          self.MappingMatrixA = None
-          self.MappingMatrixA_T = None
-          self.MappingMatrixB = None
-          self.MappingMatrixB_T = None
-          self.d_RBF = self.nDim+1
-        else:
-          self.MappingMatrix = None			#interpolation/mapping matrix for meshes interpolation/mapping
-          self.MappingMatrix_T = None			#transposed interpolation/mapping matrix for meshes interpolation/mapping
-          self.d_RBF = 0
-
-        self.localFluidInterface_array_X_init = None	#initial fluid interface position on each partition (used for the meshes mapping)
+            from mpi4py import MPI
+
+            self.MPI = MPI
+            self.comm = MPI.COMM_WORLD  # MPI World communicator
+            self.have_MPI = True
+            myid = self.comm.Get_rank()
+        else:
+            self.comm = 0
+            self.have_MPI = False
+            myid = 0
+
+        self.rootProcess = 0  # the root process is chosen to be MPI rank = 0
+
+        self.nDim = FSI_config["NDIM"]  # problem dimension
+
+        self.haveFluidSolver = (
+            False  # True if the fluid solver is initialized on the current rank
+        )
+        self.haveSolidSolver = (
+            False  # True if the solid solver is initialized on the current rank
+        )
+        self.haveFluidInterface = (
+            False  # True if the current rank owns at least one fluid interface node
+        )
+        self.haveSolidInterface = (
+            False  # True if the current rank owns at least one solid interface node
+        )
+
+        self.fluidSolverProcessors = (
+            list()
+        )  # list of partitions where the fluid solver is initialized
+        self.solidSolverProcessors = (
+            list()
+        )  # list of partitions where the solid solver is initialized
+        self.fluidInterfaceProcessors = (
+            list()
+        )  # list of partitions where there are fluid interface nodes
+        self.solidInterfaceProcessors = (
+            list()
+        )  # list of partitions where there are solid interface nodes
+
+        self.fluidInterfaceIdentifier = (
+            None  # object that can identify the f/s interface within the fluid solver
+        )
+        self.solidInterfaceIdentifier = (
+            None  # object that can identify the f/s interface within the solid solver
+        )
+
+        self.fluidGlobalIndexRange = (
+            {}
+        )  # contains the global FSI indexing of each fluid interface node for all partitions
+        self.solidGlobalIndexRange = (
+            {}
+        )  # contains the global FSI indexing of each solid interface node for all partitions
+
+        self.FluidHaloNodeList = (
+            {}
+        )  # contains the the indices (fluid solver indexing) of the halo nodes for each partition
+        self.fluidIndexing = (
+            {}
+        )  # links between the fluid solver indexing and the FSI indexing for the interface nodes
+        self.SolidHaloNodeList = (
+            {}
+        )  # contains the the indices (solid solver indexing) of the halo nodes for each partition
+        self.solidIndexing = (
+            {}
+        )  # links between the solid solver indexing and the FSI indexing for the interface nodes
+
+        self.nLocalFluidInterfaceNodes = 0  # number of nodes (halo nodes included) on the fluid interface, on each partition
+        self.nLocalFluidInterfaceHaloNode = (
+            0  # number of halo nodes on the fluid intrface, on each partition
+        )
+        self.nLocalFluidInterfacePhysicalNodes = 0  # number of physical (= non halo) nodes on the fluid interface, on each partition
+        self.nFluidInterfaceNodes = np.array(
+            int(0)
+        )  # number of nodes on the fluid interface, sum over all the partitions
+        self.nFluidInterfacePhysicalNodes = np.array(
+            int(0)
+        )  # number of physical nodes on the fluid interface, sum over all partitions
+
+        self.nLocalSolidInterfaceNodes = (
+            0  # number of physical nodes on the solid interface, on each partition
+        )
+        self.nLocalSolidInterfaceHaloNode = (
+            0  # number of halo nodes on the solid intrface, on each partition
+        )
+        self.nLocalSolidInterfacePhysicalNodes = 0  # number of physical (= non halo) nodes on the solid interface, on each partition
+        self.nSolidInterfaceNodes = np.array(
+            int(0)
+        )  # number of nodes on the solid interface, sum over all partitions
+        self.nSolidInterfacePhysicalNodes = np.array(
+            int(0)
+        )  # number of physical nodes on the solid interface, sum over all partitions
+
+        if FSI_config["MATCHING_MESH"] == "NO" and (
+            FSI_config["MESH_INTERP_METHOD"] == "RBF"
+            or FSI_config["MESH_INTERP_METHOD"] == "TPS"
+        ):
+            self.MappingMatrixA = None
+            self.MappingMatrixA_T = None
+            self.MappingMatrixB = None
+            self.MappingMatrixB_T = None
+            self.d_RBF = self.nDim + 1
+        else:
+            self.MappingMatrix = (
+                None  # interpolation/mapping matrix for meshes interpolation/mapping
+            )
+            self.MappingMatrix_T = None  # transposed interpolation/mapping matrix for meshes interpolation/mapping
+            self.d_RBF = 0
+
+        self.localFluidInterface_array_X_init = None  # initial fluid interface position on each partition (used for the meshes mapping)
         self.localFluidInterface_array_Y_init = None
         self.localFluidInterface_array_Z_init = None
 
-        self.localSolidInterface_array_X_init = None    #initial solid interface position on each partition (used for mesh mapping)
+        self.localSolidInterface_array_X_init = None  # initial solid interface position on each partition (used for mesh mapping)
         self.localSolidInterface_array_Y_init = None
         self.localSolidInterface_array_Z_init = None
 
-        self.solidInterface_array_DispX = None		#solid interface displacement
+        self.solidInterface_array_DispX = None  # solid interface displacement
         self.solidInterface_array_DispY = None
         self.solidInterface_array_DispZ = None
 
-        self.solidInterfaceResidual_array_X = None	#solid interface position residual
+        self.solidInterfaceResidual_array_X = None  # solid interface position residual
         self.solidInterfaceResidual_array_Y = None
         self.solidInterfaceResidual_array_Z = None
 
-        self.solidInterfaceResidualnM1_array_X = None	#solid interface position residual at the previous BGS iteration
+        self.solidInterfaceResidualnM1_array_X = (
+            None  # solid interface position residual at the previous BGS iteration
+        )
         self.solidInterfaceResidualnM1_array_Y = None
         self.solidInterfaceResidualnM1_array_Z = None
 
-        self.fluidInterface_array_DispX = None		#fluid interface displacement
+        self.fluidInterface_array_DispX = None  # fluid interface displacement
         self.fluidInterface_array_DispY = None
         self.fluidInterface_array_DispZ = None
 
-        self.fluidLoads_array_X = None			#loads on the fluid side of the f/s interface
+        self.fluidLoads_array_X = None  # loads on the fluid side of the f/s interface
         self.fluidLoads_array_Y = None
         self.fluidLoads_array_Z = None
 
-        self.solidLoads_array_X = None			#loads on the solid side of the f/s interface
+        self.solidLoads_array_X = None  # loads on the solid side of the f/s interface
         self.solidLoads_array_Y = None
         self.solidLoads_array_Z = None
 
-        self.aitkenParam = FSI_config['AITKEN_PARAM']			#relaxation parameter for the BGS method
-        self.FSIIter = 0				#current FSI iteration
-        self.unsteady = False				#flag for steady or unsteady simulation (default is steady)
-        if FSI_config['IMPOSED_MOTION']=='YES':
-          self.ImposedMotion = True
+        self.aitkenParam = FSI_config[
+            "AITKEN_PARAM"
+        ]  # relaxation parameter for the BGS method
+        self.FSIIter = 0  # current FSI iteration
+        self.unsteady = (
+            False  # flag for steady or unsteady simulation (default is steady)
+        )
+        if FSI_config["IMPOSED_MOTION"] == "YES":
+            self.ImposedMotion = True
         else:
-          self.ImposedMotion = False
+            self.ImposedMotion = False
 
         # ---Some screen output ---
-        self.MPIPrint('Fluid solver : SU2_CFD')
-        self.MPIPrint('Solid solver : {}'.format(FSI_config['CSD_SOLVER']))
-
-        if FSI_config['TIME_MARCHING'] == 'YES':
-          self.MPIPrint('Unsteady coupled simulation with physical time step : {} s'.format(FSI_config['UNST_TIMESTEP']))
-          self.unsteady = True
+        self.MPIPrint("Fluid solver : SU2_CFD")
+        self.MPIPrint("Solid solver : {}".format(FSI_config["CSD_SOLVER"]))
+
+        if FSI_config["TIME_MARCHING"] == "YES":
+            self.MPIPrint(
+                "Unsteady coupled simulation with physical time step : {} s".format(
+                    FSI_config["UNST_TIMESTEP"]
+                )
+            )
+            self.unsteady = True
         else:
-          self.MPIPrint('Steady coupled simulation')
+            self.MPIPrint("Steady coupled simulation")
 
-        if FSI_config['MATCHING_MESH'] == 'YES':
-          self.MPIPrint('Matching fluid-solid interface')
+        if FSI_config["MATCHING_MESH"] == "YES":
+            self.MPIPrint("Matching fluid-solid interface")
         else:
-          if FSI_config['MESH_INTERP_METHOD'] == 'TPS':
-            self.MPIPrint('Non matching fluid-solid interface with Thin Plate Spline interpolation')
-          elif FSI_config['MESH_INTERP_METHOD'] == 'RBF':
-            self.MPIPrint('Non matching fluid-solid interface with Radial Basis Function interpolation')
-            self.RBF_rad = FSI_config['RBF_RADIUS']
-            self.MPIPrint('Radius value : {}'.format(self.RBF_rad))
-          else:
-            self.MPIPrint('Non matching fluid-solid interface with Nearest Neighboor interpolation')
-
-        self.MPIPrint('Solid predictor : {}'.format(FSI_config['DISP_PRED']))
-
-        self.MPIPrint('Maximum number of FSI iterations : {}'.format(FSI_config['NB_FSI_ITER']))
-
-        self.MPIPrint('FSI tolerance : {}'.format(FSI_config['FSI_TOLERANCE']))
-
-        if FSI_config['AITKEN_RELAX'] == 'STATIC':
-          self.MPIPrint('Static Aitken under-relaxation with constant parameter {}'.format(FSI_config['AITKEN_PARAM']))
-        elif FSI_config['AITKEN_RELAX'] == 'DYNAMIC':
-          self.MPIPrint('Dynamic Aitken under-relaxation with initial parameter {}'.format(FSI_config['AITKEN_PARAM']))
+            if FSI_config["MESH_INTERP_METHOD"] == "TPS":
+                self.MPIPrint(
+                    "Non matching fluid-solid interface with Thin Plate Spline interpolation"
+                )
+            elif FSI_config["MESH_INTERP_METHOD"] == "RBF":
+                self.MPIPrint(
+                    "Non matching fluid-solid interface with Radial Basis Function interpolation"
+                )
+                self.RBF_rad = FSI_config["RBF_RADIUS"]
+                self.MPIPrint("Radius value : {}".format(self.RBF_rad))
+            else:
+                self.MPIPrint(
+                    "Non matching fluid-solid interface with Nearest Neighboor interpolation"
+                )
+
+        self.MPIPrint("Solid predictor : {}".format(FSI_config["DISP_PRED"]))
+
+        self.MPIPrint(
+            "Maximum number of FSI iterations : {}".format(FSI_config["NB_FSI_ITER"])
+        )
+
+        self.MPIPrint("FSI tolerance : {}".format(FSI_config["FSI_TOLERANCE"]))
+
+        if FSI_config["AITKEN_RELAX"] == "STATIC":
+            self.MPIPrint(
+                "Static Aitken under-relaxation with constant parameter {}".format(
+                    FSI_config["AITKEN_PARAM"]
+                )
+            )
+        elif FSI_config["AITKEN_RELAX"] == "DYNAMIC":
+            self.MPIPrint(
+                "Dynamic Aitken under-relaxation with initial parameter {}".format(
+                    FSI_config["AITKEN_PARAM"]
+                )
+            )
         else:
-          self.MPIPrint('No Aitken under-relaxation')
+            self.MPIPrint("No Aitken under-relaxation")
 
-        self.MPIPrint('FSI interface is set')
+        self.MPIPrint("FSI interface is set")
 
     def MPIPrint(self, message):
-      """
-      Print a message on screen only from the master process.
-      """
+        """
+        Print a message on screen only from the master process.
+        """
 
-      if self.have_MPI:
-        myid = self.comm.Get_rank()
-      else:
-        myid = 0
+        if self.have_MPI:
+            myid = self.comm.Get_rank()
+        else:
+            myid = 0
 
-      if myid == self.rootProcess:
-        print(message)
+        if myid == self.rootProcess:
+            print(message)
 
     def MPIBarrier(self):
-      """
-      Perform a synchronization barrier in case of parallel run with MPI.
-      """
+        """
+        Perform a synchronization barrier in case of parallel run with MPI.
+        """
 
-      if self.have_MPI:
-        self.comm.barrier()
+        if self.have_MPI:
+            self.comm.barrier()
 
     def connect(self, FSI_config, FluidSolver, SolidSolver):
         """
@@ -215,85 +294,108 @@ def connect(self, FSI_config, FluidSolver, SolidSolver):
         Gets information about f/s interfaces from the two solvers.
         """
         if self.have_MPI:
-          myid = self.comm.Get_rank()
-          MPIsize = self.comm.Get_size()
+            myid = self.comm.Get_rank()
+            MPIsize = self.comm.Get_size()
         else:
-          myid = 0
-          MPIsize = 1
+            myid = 0
+            MPIsize = 1
 
         # --- Identify the fluid and solid interfaces and store the number of nodes on both sides (and for each partition) ---
         self.fluidInterfaceIdentifier = None
         self.nLocalFluidInterfaceNodes = 0
         if FluidSolver is not None:
-            print('Fluid solver is initialized on process {}'.format(myid))
+            print("Fluid solver is initialized on process {}".format(myid))
             self.haveFluidSolver = True
             allMovingMarkersTags = FluidSolver.GetDeformableMarkerTags()
             allMarkersID = FluidSolver.GetMarkerTags()
             if not allMovingMarkersTags:
-                raise Exception('No interface for FSI was defined.')
+                raise Exception("No interface for FSI was defined.")
             else:
                 if allMovingMarkersTags[0] in allMarkersID.keys():
-                    self.fluidInterfaceIdentifier = allMarkersID[allMovingMarkersTags[0]]
+                    self.fluidInterfaceIdentifier = allMarkersID[
+                        allMovingMarkersTags[0]
+                    ]
             if self.fluidInterfaceIdentifier is not None:
-                self.nLocalFluidInterfaceNodes = FluidSolver.GetNumberMarkerNodes(self.fluidInterfaceIdentifier)
+                self.nLocalFluidInterfaceNodes = FluidSolver.GetNumberMarkerNodes(
+                    self.fluidInterfaceIdentifier
+                )
             if self.nLocalFluidInterfaceNodes != 0:
-              self.haveFluidInterface = True
-              print('Number of interface fluid nodes (halo nodes included) on proccess {} : {}'.format(myid,self.nLocalFluidInterfaceNodes))
+                self.haveFluidInterface = True
+                print(
+                    "Number of interface fluid nodes (halo nodes included) on proccess {} : {}".format(
+                        myid, self.nLocalFluidInterfaceNodes
+                    )
+                )
         else:
             pass
 
         if SolidSolver is not None:
-            print('Solid solver is initialized on process {}'.format(myid))
+            print("Solid solver is initialized on process {}".format(myid))
             self.haveSolidSolver = True
             self.solidInterfaceIdentifier = SolidSolver.getFSIMarkerID()
-            self.nLocalSolidInterfaceNodes = SolidSolver.getNumberOfSolidInterfaceNodes(self.solidInterfaceIdentifier)
+            self.nLocalSolidInterfaceNodes = SolidSolver.getNumberOfSolidInterfaceNodes(
+                self.solidInterfaceIdentifier
+            )
             if self.nLocalSolidInterfaceNodes != 0:
-              self.haveSolidInterface = True
-              print('Number of interface solid nodes (halo nodes included) on proccess {} : {}'.format(myid,self.nLocalSolidInterfaceNodes))
+                self.haveSolidInterface = True
+                print(
+                    "Number of interface solid nodes (halo nodes included) on proccess {} : {}".format(
+                        myid, self.nLocalSolidInterfaceNodes
+                    )
+                )
         else:
             pass
 
         # --- Exchange information about processors on which the solvers are defined and where the interface nodes are lying ---
         if self.have_MPI:
-          if self.haveFluidSolver:
-            sendBufFluid = np.array(int(1))
-          else:
-            sendBufFluid = np.array(int(0))
-          if self.haveSolidSolver:
-            sendBufSolid = np.array(int(1))
-          else:
-            sendBufSolid = np.array(int(0))
-          if self.haveFluidInterface:
-            sendBufFluidInterface = np.array(int(1))
-          else:
-            sendBufFluidInterface = np.array(int(0))
-          if self.haveSolidInterface:
-            sendBufSolidInterface = np.array(int(1))
-          else:
-            sendBufSolidInterface = np.array(int(0))
-          rcvBufFluid = np.zeros(MPIsize, dtype = int)
-          rcvBufSolid = np.zeros(MPIsize, dtype = int)
-          rcvBufFluidInterface = np.zeros(MPIsize, dtype = int)
-          rcvBufSolidInterface = np.zeros(MPIsize, dtype = int)
-          self.comm.Allgather(sendBufFluid, rcvBufFluid)
-          self.comm.Allgather(sendBufSolid, rcvBufSolid)
-          self.comm.Allgather(sendBufFluidInterface, rcvBufFluidInterface)
-          self.comm.Allgather(sendBufSolidInterface, rcvBufSolidInterface)
-          for iProc in range(MPIsize):
-            if rcvBufFluid[iProc] == 1:
-              self.fluidSolverProcessors.append(iProc)
-            if rcvBufSolid[iProc] == 1:
-              self.solidSolverProcessors.append(iProc)
-            if rcvBufFluidInterface[iProc] == 1:
-              self.fluidInterfaceProcessors.append(iProc)
-            if rcvBufSolidInterface[iProc] == 1:
-              self.solidInterfaceProcessors.append(iProc)
-          del sendBufFluid, sendBufSolid, rcvBufFluid, rcvBufSolid, sendBufFluidInterface, sendBufSolidInterface, rcvBufFluidInterface, rcvBufSolidInterface
-        else:
-          self.fluidSolverProcessors.append(0)
-          self.solidSolverProcessors.append(0)
-          self.fluidInterfaceProcessors.append(0)
-          self.solidInterfaceProcessors.append(0)
+            if self.haveFluidSolver:
+                sendBufFluid = np.array(int(1))
+            else:
+                sendBufFluid = np.array(int(0))
+            if self.haveSolidSolver:
+                sendBufSolid = np.array(int(1))
+            else:
+                sendBufSolid = np.array(int(0))
+            if self.haveFluidInterface:
+                sendBufFluidInterface = np.array(int(1))
+            else:
+                sendBufFluidInterface = np.array(int(0))
+            if self.haveSolidInterface:
+                sendBufSolidInterface = np.array(int(1))
+            else:
+                sendBufSolidInterface = np.array(int(0))
+            rcvBufFluid = np.zeros(MPIsize, dtype=int)
+            rcvBufSolid = np.zeros(MPIsize, dtype=int)
+            rcvBufFluidInterface = np.zeros(MPIsize, dtype=int)
+            rcvBufSolidInterface = np.zeros(MPIsize, dtype=int)
+            self.comm.Allgather(sendBufFluid, rcvBufFluid)
+            self.comm.Allgather(sendBufSolid, rcvBufSolid)
+            self.comm.Allgather(sendBufFluidInterface, rcvBufFluidInterface)
+            self.comm.Allgather(sendBufSolidInterface, rcvBufSolidInterface)
+            for iProc in range(MPIsize):
+                if rcvBufFluid[iProc] == 1:
+                    self.fluidSolverProcessors.append(iProc)
+                if rcvBufSolid[iProc] == 1:
+                    self.solidSolverProcessors.append(iProc)
+                if rcvBufFluidInterface[iProc] == 1:
+                    self.fluidInterfaceProcessors.append(iProc)
+                if rcvBufSolidInterface[iProc] == 1:
+                    self.solidInterfaceProcessors.append(iProc)
+            del (
+                sendBufFluid,
+                sendBufSolid,
+                rcvBufFluid,
+                rcvBufSolid,
+                sendBufFluidInterface,
+                sendBufSolidInterface,
+                rcvBufFluidInterface,
+                rcvBufSolidInterface,
+            )
+        else:
+            self.fluidSolverProcessors.append(0)
+            self.solidSolverProcessors.append(0)
+            self.fluidInterfaceProcessors.append(0)
+            self.solidInterfaceProcessors.append(0)
 
         self.MPIBarrier()
         # --- Calculate the total number of nodes at the fluid interface (sum over all the partitions) ---
@@ -302,29 +404,34 @@ def connect(self, FSI_config, FluidSolver, SolidSolver):
         for iVertex in range(self.nLocalFluidInterfaceNodes):
             iPoint = FluidSolver.GetMarkerNode(self.fluidInterfaceIdentifier, iVertex)
             if not FluidSolver.GetNodeDomain(iPoint):
-              GlobalIndex = FluidSolver.GetNodeGlobalIndex(iPoint)
-              self.FluidHaloNodeList[GlobalIndex] = iVertex
-              self.nLocalFluidInterfaceHaloNode += 1
+                GlobalIndex = FluidSolver.GetNodeGlobalIndex(iPoint)
+                self.FluidHaloNodeList[GlobalIndex] = iVertex
+                self.nLocalFluidInterfaceHaloNode += 1
         # Calculate the number of physical (= not halo) nodes on each partition
-        self.nLocalFluidInterfacePhysicalNodes = self.nLocalFluidInterfaceNodes - self.nLocalFluidInterfaceHaloNode
+        self.nLocalFluidInterfacePhysicalNodes = (
+            self.nLocalFluidInterfaceNodes - self.nLocalFluidInterfaceHaloNode
+        )
         if self.have_MPI:
-          self.FluidHaloNodeList = self.comm.allgather(self.FluidHaloNodeList)
+            self.FluidHaloNodeList = self.comm.allgather(self.FluidHaloNodeList)
         else:
-          self.FluidHaloNodeList = [{}]
+            self.FluidHaloNodeList = [{}]
 
         # Same thing for the solid part
         self.nLocalSolidInterfaceHaloNode = 0
         for iVertex in range(self.nLocalSolidInterfaceNodes):
             if SolidSolver.IsAHaloNode(self.solidInterfaceIdentifier, iVertex):
-              GlobalIndex = SolidSolver.getVertexGlobalIndex(self.solidInterfaceIdentifier, iVertex)
-              self.SolidHaloNodeList[GlobalIndex] = iVertex
-              self.nLocalSolidInterfaceHaloNode += 1
-        self.nLocalSolidInterfacePhysicalNodes = self.nLocalSolidInterfaceNodes - self.nLocalSolidInterfaceHaloNode
+                GlobalIndex = SolidSolver.getVertexGlobalIndex(
+                    self.solidInterfaceIdentifier, iVertex
+                )
+                self.SolidHaloNodeList[GlobalIndex] = iVertex
+                self.nLocalSolidInterfaceHaloNode += 1
+        self.nLocalSolidInterfacePhysicalNodes = (
+            self.nLocalSolidInterfaceNodes - self.nLocalSolidInterfaceHaloNode
+        )
         if self.have_MPI:
-          self.SolidHaloNodeList = self.comm.allgather(self.SolidHaloNodeList)
+            self.SolidHaloNodeList = self.comm.allgather(self.SolidHaloNodeList)
         else:
-          self.SolidHaloNodeList = [{}]
-
+            self.SolidHaloNodeList = [{}]
 
         # --- Calculate the total number of nodes (with and without halo) at the fluid interface (sum over all the partitions) and broadcast the number accross all processors ---
         sendBuffTotal = np.array(int(self.nLocalFluidInterfaceNodes))
@@ -332,12 +439,16 @@ def connect(self, FSI_config, FluidSolver, SolidSolver):
         rcvBuffTotal = np.zeros(1, dtype=int)
         rcvBuffPhysical = np.zeros(1, dtype=int)
         if self.have_MPI:
-          self.comm.barrier()
-          self.comm.Allreduce(sendBuffTotal, self.nFluidInterfaceNodes, op=self.MPI.SUM)
-          self.comm.Allreduce(sendBuffPhysical, self.nFluidInterfacePhysicalNodes, op=self.MPI.SUM)
+            self.comm.barrier()
+            self.comm.Allreduce(
+                sendBuffTotal, self.nFluidInterfaceNodes, op=self.MPI.SUM
+            )
+            self.comm.Allreduce(
+                sendBuffPhysical, self.nFluidInterfacePhysicalNodes, op=self.MPI.SUM
+            )
         else:
-          self.nFluidInterfaceNodes = np.copy(sendBuffTotal)
-          self.nFluidInterfacePhysicalNodes = np.copy(sendBuffPhysical)
+            self.nFluidInterfaceNodes = np.copy(sendBuffTotal)
+            self.nFluidInterfacePhysicalNodes = np.copy(sendBuffPhysical)
         del sendBuffTotal, rcvBuffTotal, sendBuffPhysical, rcvBuffPhysical
 
         # Same thing for the solid part
@@ -346,111 +457,153 @@ def connect(self, FSI_config, FluidSolver, SolidSolver):
         rcvBuffTotal = np.zeros(1, dtype=int)
         rcvBuffPhysical = np.zeros(1, dtype=int)
         if self.have_MPI:
-          self.comm.barrier()
-          self.comm.Allreduce(sendBuffTotal, self.nSolidInterfaceNodes, op=self.MPI.SUM)
-          self.comm.Allreduce(sendBuffPhysical, self.nSolidInterfacePhysicalNodes, op=self.MPI.SUM)
+            self.comm.barrier()
+            self.comm.Allreduce(
+                sendBuffTotal, self.nSolidInterfaceNodes, op=self.MPI.SUM
+            )
+            self.comm.Allreduce(
+                sendBuffPhysical, self.nSolidInterfacePhysicalNodes, op=self.MPI.SUM
+            )
         else:
-          self.nSolidInterfaceNodes = np.copy(sendBuffTotal)
-          self.nSolidInterfacePhysicalNodes = np.copy(sendBuffPhysical)
+            self.nSolidInterfaceNodes = np.copy(sendBuffTotal)
+            self.nSolidInterfacePhysicalNodes = np.copy(sendBuffPhysical)
         del sendBuffTotal, rcvBuffTotal, sendBuffPhysical, rcvBuffPhysical
 
         # --- Store the number of physical interface nodes on each processor and allgather the information ---
         self.fluidPhysicalInterfaceNodesDistribution = np.zeros(MPIsize, dtype=int)
         if self.have_MPI:
-          sendBuffPhysical = np.array(int(self.nLocalFluidInterfacePhysicalNodes))
-          self.comm.Allgather(sendBuffPhysical,self.fluidPhysicalInterfaceNodesDistribution)
-          del sendBuffPhysical
+            sendBuffPhysical = np.array(int(self.nLocalFluidInterfacePhysicalNodes))
+            self.comm.Allgather(
+                sendBuffPhysical, self.fluidPhysicalInterfaceNodesDistribution
+            )
+            del sendBuffPhysical
         else:
-          self.fluidPhysicalInterfaceNodesDistribution[0] = self.nFluidInterfacePhysicalNodes
+            self.fluidPhysicalInterfaceNodesDistribution[
+                0
+            ] = self.nFluidInterfacePhysicalNodes
 
         # Same thing for the solid part
         self.solidPhysicalInterfaceNodesDistribution = np.zeros(MPIsize, dtype=int)
         if self.have_MPI:
-          sendBuffPhysical = np.array(int(self.nLocalSolidInterfacePhysicalNodes))
-          self.comm.Allgather(sendBuffPhysical,self.solidPhysicalInterfaceNodesDistribution)
-          del sendBuffPhysical
+            sendBuffPhysical = np.array(int(self.nLocalSolidInterfacePhysicalNodes))
+            self.comm.Allgather(
+                sendBuffPhysical, self.solidPhysicalInterfaceNodesDistribution
+            )
+            del sendBuffPhysical
         else:
-          self.solidPhysicalInterfaceNodesDistribution[0] = self.nSolidInterfacePhysicalNodes
+            self.solidPhysicalInterfaceNodesDistribution[
+                0
+            ] = self.nSolidInterfacePhysicalNodes
 
         # --- Calculate and store the global indexing of interface physical nodes on each processor and allgather the information ---
         if self.have_MPI:
-          if myid in self.fluidInterfaceProcessors:
-            globalIndexStart = 0
-            for iProc in range(myid):
-                globalIndexStart += self.fluidPhysicalInterfaceNodesDistribution[iProc]
-            globalIndexStop = globalIndexStart + self.nLocalFluidInterfacePhysicalNodes-1
-          else:
-            globalIndexStart = 0
-            globalIndexStop = 0
-          self.fluidGlobalIndexRange[myid] = [globalIndexStart,globalIndexStop]
-          self.fluidGlobalIndexRange = self.comm.allgather(self.fluidGlobalIndexRange)
-        else:
-          temp = {}
-          temp[0] = [0,self.nLocalFluidInterfacePhysicalNodes-1]
-          self.fluidGlobalIndexRange = list()
-          self.fluidGlobalIndexRange.append(temp)
+            if myid in self.fluidInterfaceProcessors:
+                globalIndexStart = 0
+                for iProc in range(myid):
+                    globalIndexStart += self.fluidPhysicalInterfaceNodesDistribution[
+                        iProc
+                    ]
+                globalIndexStop = (
+                    globalIndexStart + self.nLocalFluidInterfacePhysicalNodes - 1
+                )
+            else:
+                globalIndexStart = 0
+                globalIndexStop = 0
+            self.fluidGlobalIndexRange[myid] = [globalIndexStart, globalIndexStop]
+            self.fluidGlobalIndexRange = self.comm.allgather(self.fluidGlobalIndexRange)
+        else:
+            temp = {}
+            temp[0] = [0, self.nLocalFluidInterfacePhysicalNodes - 1]
+            self.fluidGlobalIndexRange = list()
+            self.fluidGlobalIndexRange.append(temp)
 
         # Same thing for the solid part
         if self.have_MPI:
-          if myid in self.solidInterfaceProcessors:
-            globalIndexStart = 0
-            for iProc in range(myid):
-              globalIndexStart += self.solidPhysicalInterfaceNodesDistribution[iProc]
-            globalIndexStop = globalIndexStart + self.nLocalSolidInterfacePhysicalNodes-1
-          else:
-            globalIndexStart = 0
-            globalIndexStop = 0
-          self.solidGlobalIndexRange[myid] = [globalIndexStart,globalIndexStop]
-          self.solidGlobalIndexRange = self.comm.allgather(self.solidGlobalIndexRange)
-        else:
-          temp = {}
-          temp[0] = [0,self.nSolidInterfacePhysicalNodes-1]
-          self.solidGlobalIndexRange = list()
-          self.solidGlobalIndexRange.append(temp)
-
-        self.MPIPrint('Total number of fluid interface nodes (halo nodes included) : {}'.format(self.nFluidInterfaceNodes))
-        self.MPIPrint('Total number of solid interface nodes (halo nodes included) : {}'.format(self.nSolidInterfaceNodes))
-        self.MPIPrint('Total number of fluid interface nodes : {}'.format(self.nFluidInterfacePhysicalNodes))
-        self.MPIPrint('Total number of solid interface nodes : {}'.format(self.nSolidInterfacePhysicalNodes))
+            if myid in self.solidInterfaceProcessors:
+                globalIndexStart = 0
+                for iProc in range(myid):
+                    globalIndexStart += self.solidPhysicalInterfaceNodesDistribution[
+                        iProc
+                    ]
+                globalIndexStop = (
+                    globalIndexStart + self.nLocalSolidInterfacePhysicalNodes - 1
+                )
+            else:
+                globalIndexStart = 0
+                globalIndexStop = 0
+            self.solidGlobalIndexRange[myid] = [globalIndexStart, globalIndexStop]
+            self.solidGlobalIndexRange = self.comm.allgather(self.solidGlobalIndexRange)
+        else:
+            temp = {}
+            temp[0] = [0, self.nSolidInterfacePhysicalNodes - 1]
+            self.solidGlobalIndexRange = list()
+            self.solidGlobalIndexRange.append(temp)
+
+        self.MPIPrint(
+            "Total number of fluid interface nodes (halo nodes included) : {}".format(
+                self.nFluidInterfaceNodes
+            )
+        )
+        self.MPIPrint(
+            "Total number of solid interface nodes (halo nodes included) : {}".format(
+                self.nSolidInterfaceNodes
+            )
+        )
+        self.MPIPrint(
+            "Total number of fluid interface nodes : {}".format(
+                self.nFluidInterfacePhysicalNodes
+            )
+        )
+        self.MPIPrint(
+            "Total number of solid interface nodes : {}".format(
+                self.nSolidInterfacePhysicalNodes
+            )
+        )
 
         self.MPIBarrier()
 
         # --- Create all the PETSc vectors required for parallel communication and parallel mesh mapping/interpolation (working for serial too) ---
         if self.have_MPI:
-          self.solidInterface_array_DispX = PETSc.Vec().create(self.comm)
-          self.solidInterface_array_DispY = PETSc.Vec().create(self.comm)
-          self.solidInterface_array_DispZ = PETSc.Vec().create(self.comm)
-          self.solidInterface_array_DispX.setType('mpi')
-          self.solidInterface_array_DispY.setType('mpi')
-          self.solidInterface_array_DispZ.setType('mpi')
-        else:
-          self.solidInterface_array_DispX = PETSc.Vec().create()
-          self.solidInterface_array_DispY = PETSc.Vec().create()
-          self.solidInterface_array_DispZ = PETSc.Vec().create()
-          self.solidInterface_array_DispX.setType('seq')
-          self.solidInterface_array_DispY.setType('seq')
-          self.solidInterface_array_DispZ.setType('seq')
-        self.solidInterface_array_DispX.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-        self.solidInterface_array_DispY.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-        self.solidInterface_array_DispZ.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
+            self.solidInterface_array_DispX = PETSc.Vec().create(self.comm)
+            self.solidInterface_array_DispY = PETSc.Vec().create(self.comm)
+            self.solidInterface_array_DispZ = PETSc.Vec().create(self.comm)
+            self.solidInterface_array_DispX.setType("mpi")
+            self.solidInterface_array_DispY.setType("mpi")
+            self.solidInterface_array_DispZ.setType("mpi")
+        else:
+            self.solidInterface_array_DispX = PETSc.Vec().create()
+            self.solidInterface_array_DispY = PETSc.Vec().create()
+            self.solidInterface_array_DispZ = PETSc.Vec().create()
+            self.solidInterface_array_DispX.setType("seq")
+            self.solidInterface_array_DispY.setType("seq")
+            self.solidInterface_array_DispZ.setType("seq")
+        self.solidInterface_array_DispX.setSizes(
+            self.nSolidInterfacePhysicalNodes + self.d_RBF
+        )
+        self.solidInterface_array_DispY.setSizes(
+            self.nSolidInterfacePhysicalNodes + self.d_RBF
+        )
+        self.solidInterface_array_DispZ.setSizes(
+            self.nSolidInterfacePhysicalNodes + self.d_RBF
+        )
         self.solidInterface_array_DispX.set(0.0)
         self.solidInterface_array_DispY.set(0.0)
         self.solidInterface_array_DispZ.set(0.0)
 
         if self.have_MPI:
-          self.fluidInterface_array_DispX = PETSc.Vec().create(self.comm)
-          self.fluidInterface_array_DispY = PETSc.Vec().create(self.comm)
-          self.fluidInterface_array_DispZ = PETSc.Vec().create(self.comm)
-          self.fluidInterface_array_DispX.setType('mpi')
-          self.fluidInterface_array_DispY.setType('mpi')
-          self.fluidInterface_array_DispZ.setType('mpi')
-        else:
-          self.fluidInterface_array_DispX = PETSc.Vec().create()
-          self.fluidInterface_array_DispY = PETSc.Vec().create()
-          self.fluidInterface_array_DispZ = PETSc.Vec().create()
-          self.fluidInterface_array_DispX.setType('seq')
-          self.fluidInterface_array_DispY.setType('seq')
-          self.fluidInterface_array_DispZ.setType('seq')
+            self.fluidInterface_array_DispX = PETSc.Vec().create(self.comm)
+            self.fluidInterface_array_DispY = PETSc.Vec().create(self.comm)
+            self.fluidInterface_array_DispZ = PETSc.Vec().create(self.comm)
+            self.fluidInterface_array_DispX.setType("mpi")
+            self.fluidInterface_array_DispY.setType("mpi")
+            self.fluidInterface_array_DispZ.setType("mpi")
+        else:
+            self.fluidInterface_array_DispX = PETSc.Vec().create()
+            self.fluidInterface_array_DispY = PETSc.Vec().create()
+            self.fluidInterface_array_DispZ = PETSc.Vec().create()
+            self.fluidInterface_array_DispX.setType("seq")
+            self.fluidInterface_array_DispY.setType("seq")
+            self.fluidInterface_array_DispZ.setType("seq")
         self.fluidInterface_array_DispX.setSizes(self.nFluidInterfacePhysicalNodes)
         self.fluidInterface_array_DispY.setSizes(self.nFluidInterfacePhysicalNodes)
         self.fluidInterface_array_DispZ.setSizes(self.nFluidInterfacePhysicalNodes)
@@ -459,19 +612,19 @@ def connect(self, FSI_config, FluidSolver, SolidSolver):
         self.fluidInterface_array_DispZ.set(0.0)
 
         if self.have_MPI:
-          self.fluidLoads_array_X = PETSc.Vec().create(self.comm)
-          self.fluidLoads_array_Y = PETSc.Vec().create(self.comm)
-          self.fluidLoads_array_Z = PETSc.Vec().create(self.comm)
-          self.fluidLoads_array_X.setType('mpi')
-          self.fluidLoads_array_Y.setType('mpi')
-          self.fluidLoads_array_Z.setType('mpi')
-        else:
-          self.fluidLoads_array_X = PETSc.Vec().create()
-          self.fluidLoads_array_Y = PETSc.Vec().create()
-          self.fluidLoads_array_Z = PETSc.Vec().create()
-          self.fluidLoads_array_X.setType('seq')
-          self.fluidLoads_array_Y.setType('seq')
-          self.fluidLoads_array_Z.setType('seq')
+            self.fluidLoads_array_X = PETSc.Vec().create(self.comm)
+            self.fluidLoads_array_Y = PETSc.Vec().create(self.comm)
+            self.fluidLoads_array_Z = PETSc.Vec().create(self.comm)
+            self.fluidLoads_array_X.setType("mpi")
+            self.fluidLoads_array_Y.setType("mpi")
+            self.fluidLoads_array_Z.setType("mpi")
+        else:
+            self.fluidLoads_array_X = PETSc.Vec().create()
+            self.fluidLoads_array_Y = PETSc.Vec().create()
+            self.fluidLoads_array_Z = PETSc.Vec().create()
+            self.fluidLoads_array_X.setType("seq")
+            self.fluidLoads_array_Y.setType("seq")
+            self.fluidLoads_array_Z.setType("seq")
         self.fluidLoads_array_X.setSizes(self.nFluidInterfacePhysicalNodes)
         self.fluidLoads_array_Y.setSizes(self.nFluidInterfacePhysicalNodes)
         self.fluidLoads_array_Z.setSizes(self.nFluidInterfacePhysicalNodes)
@@ -480,88 +633,106 @@ def connect(self, FSI_config, FluidSolver, SolidSolver):
         self.fluidLoads_array_Z.set(0.0)
 
         if self.have_MPI:
-          self.solidLoads_array_X = PETSc.Vec().create(self.comm)
-          self.solidLoads_array_Y = PETSc.Vec().create(self.comm)
-          self.solidLoads_array_Z = PETSc.Vec().create(self.comm)
-          self.solidLoads_array_X.setType('mpi')
-          self.solidLoads_array_Y.setType('mpi')
-          self.solidLoads_array_Z.setType('mpi')
-        else:
-          self.solidLoads_array_X = PETSc.Vec().create()
-          self.solidLoads_array_Y = PETSc.Vec().create()
-          self.solidLoads_array_Z = PETSc.Vec().create()
-          self.solidLoads_array_X.setType('seq')
-          self.solidLoads_array_Y.setType('seq')
-          self.solidLoads_array_Z.setType('seq')
-        self.solidLoads_array_X.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-        self.solidLoads_array_Y.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-        self.solidLoads_array_Z.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
+            self.solidLoads_array_X = PETSc.Vec().create(self.comm)
+            self.solidLoads_array_Y = PETSc.Vec().create(self.comm)
+            self.solidLoads_array_Z = PETSc.Vec().create(self.comm)
+            self.solidLoads_array_X.setType("mpi")
+            self.solidLoads_array_Y.setType("mpi")
+            self.solidLoads_array_Z.setType("mpi")
+        else:
+            self.solidLoads_array_X = PETSc.Vec().create()
+            self.solidLoads_array_Y = PETSc.Vec().create()
+            self.solidLoads_array_Z = PETSc.Vec().create()
+            self.solidLoads_array_X.setType("seq")
+            self.solidLoads_array_Y.setType("seq")
+            self.solidLoads_array_Z.setType("seq")
+        self.solidLoads_array_X.setSizes(self.nSolidInterfacePhysicalNodes + self.d_RBF)
+        self.solidLoads_array_Y.setSizes(self.nSolidInterfacePhysicalNodes + self.d_RBF)
+        self.solidLoads_array_Z.setSizes(self.nSolidInterfacePhysicalNodes + self.d_RBF)
         self.solidLoads_array_X.set(0.0)
         self.solidLoads_array_Y.set(0.0)
         self.solidLoads_array_Z.set(0.0)
 
         # --- Create the PETSc vectors required for parallel relaxed BGS algo (working for serial too) ---
         if self.have_MPI:
-          self.solidInterfaceResidual_array_X = PETSc.Vec().create(self.comm)
-          self.solidInterfaceResidual_array_Y = PETSc.Vec().create(self.comm)
-          self.solidInterfaceResidual_array_Z = PETSc.Vec().create(self.comm)
-          self.solidInterfaceResidual_array_X.setType('mpi')
-          self.solidInterfaceResidual_array_Y.setType('mpi')
-          self.solidInterfaceResidual_array_Z.setType('mpi')
-        else:
-          self.solidInterfaceResidual_array_X = PETSc.Vec().create()
-          self.solidInterfaceResidual_array_Y = PETSc.Vec().create()
-          self.solidInterfaceResidual_array_Z = PETSc.Vec().create()
-          self.solidInterfaceResidual_array_X.setType('seq')
-          self.solidInterfaceResidual_array_Y.setType('seq')
-          self.solidInterfaceResidual_array_Z.setType('seq')
-        self.solidInterfaceResidual_array_X.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-        self.solidInterfaceResidual_array_Y.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-        self.solidInterfaceResidual_array_Z.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
+            self.solidInterfaceResidual_array_X = PETSc.Vec().create(self.comm)
+            self.solidInterfaceResidual_array_Y = PETSc.Vec().create(self.comm)
+            self.solidInterfaceResidual_array_Z = PETSc.Vec().create(self.comm)
+            self.solidInterfaceResidual_array_X.setType("mpi")
+            self.solidInterfaceResidual_array_Y.setType("mpi")
+            self.solidInterfaceResidual_array_Z.setType("mpi")
+        else:
+            self.solidInterfaceResidual_array_X = PETSc.Vec().create()
+            self.solidInterfaceResidual_array_Y = PETSc.Vec().create()
+            self.solidInterfaceResidual_array_Z = PETSc.Vec().create()
+            self.solidInterfaceResidual_array_X.setType("seq")
+            self.solidInterfaceResidual_array_Y.setType("seq")
+            self.solidInterfaceResidual_array_Z.setType("seq")
+        self.solidInterfaceResidual_array_X.setSizes(
+            self.nSolidInterfacePhysicalNodes + self.d_RBF
+        )
+        self.solidInterfaceResidual_array_Y.setSizes(
+            self.nSolidInterfacePhysicalNodes + self.d_RBF
+        )
+        self.solidInterfaceResidual_array_Z.setSizes(
+            self.nSolidInterfacePhysicalNodes + self.d_RBF
+        )
         self.solidInterfaceResidual_array_X.set(0.0)
         self.solidInterfaceResidual_array_Y.set(0.0)
         self.solidInterfaceResidual_array_Z.set(0.0)
 
         if self.have_MPI:
-          self.solidInterfaceResidualnM1_array_X = PETSc.Vec().create(self.comm)
-          self.solidInterfaceResidualnM1_array_Y = PETSc.Vec().create(self.comm)
-          self.solidInterfaceResidualnM1_array_Z = PETSc.Vec().create(self.comm)
-          self.solidInterfaceResidualnM1_array_X.setType('mpi')
-          self.solidInterfaceResidualnM1_array_Y.setType('mpi')
-          self.solidInterfaceResidualnM1_array_Z.setType('mpi')
-        else:
-          self.solidInterfaceResidualnM1_array_X = PETSc.Vec().create()
-          self.solidInterfaceResidualnM1_array_Y = PETSc.Vec().create()
-          self.solidInterfaceResidualnM1_array_Z = PETSc.Vec().create()
-          self.solidInterfaceResidualnM1_array_X.setType('seq')
-          self.solidInterfaceResidualnM1_array_Y.setType('seq')
-          self.solidInterfaceResidualnM1_array_Z.setType('seq')
-        self.solidInterfaceResidualnM1_array_X.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-        self.solidInterfaceResidualnM1_array_Y.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-        self.solidInterfaceResidualnM1_array_Z.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
+            self.solidInterfaceResidualnM1_array_X = PETSc.Vec().create(self.comm)
+            self.solidInterfaceResidualnM1_array_Y = PETSc.Vec().create(self.comm)
+            self.solidInterfaceResidualnM1_array_Z = PETSc.Vec().create(self.comm)
+            self.solidInterfaceResidualnM1_array_X.setType("mpi")
+            self.solidInterfaceResidualnM1_array_Y.setType("mpi")
+            self.solidInterfaceResidualnM1_array_Z.setType("mpi")
+        else:
+            self.solidInterfaceResidualnM1_array_X = PETSc.Vec().create()
+            self.solidInterfaceResidualnM1_array_Y = PETSc.Vec().create()
+            self.solidInterfaceResidualnM1_array_Z = PETSc.Vec().create()
+            self.solidInterfaceResidualnM1_array_X.setType("seq")
+            self.solidInterfaceResidualnM1_array_Y.setType("seq")
+            self.solidInterfaceResidualnM1_array_Z.setType("seq")
+        self.solidInterfaceResidualnM1_array_X.setSizes(
+            self.nSolidInterfacePhysicalNodes + self.d_RBF
+        )
+        self.solidInterfaceResidualnM1_array_Y.setSizes(
+            self.nSolidInterfacePhysicalNodes + self.d_RBF
+        )
+        self.solidInterfaceResidualnM1_array_Z.setSizes(
+            self.nSolidInterfacePhysicalNodes + self.d_RBF
+        )
         self.solidInterfaceResidualnM1_array_X.set(0.0)
         self.solidInterfaceResidualnM1_array_Y.set(0.0)
         self.solidInterfaceResidualnM1_array_Z.set(0.0)
 
-    def interfaceMapping(self,FluidSolver, SolidSolver, FSI_config):
+    def interfaceMapping(self, FluidSolver, SolidSolver, FSI_config):
         """
         Creates the one-to-one mapping between interfaces in case of matching meshes.
         Creates the interpolation rules between interfaces in case of non-matching meshes.
         """
         if self.have_MPI:
-          myid = self.comm.Get_rank()
-          MPIsize = self.comm.Get_size()
+            myid = self.comm.Get_rank()
+            MPIsize = self.comm.Get_size()
         else:
-          myid = 0
-          MPIsize = 1
+            myid = 0
+            MPIsize = 1
 
         # --- Get the fluid interface from fluid solver on each partition ---
         GlobalIndex = int()
         localIndex = 0
         fluidIndexing_temp = {}
-        self.localFluidInterface_array_X_init = np.zeros((self.nLocalFluidInterfacePhysicalNodes))
-        self.localFluidInterface_array_Y_init = np.zeros((self.nLocalFluidInterfacePhysicalNodes))
-        self.localFluidInterface_array_Z_init = np.zeros((self.nLocalFluidInterfacePhysicalNodes))
+        self.localFluidInterface_array_X_init = np.zeros(
+            (self.nLocalFluidInterfacePhysicalNodes)
+        )
+        self.localFluidInterface_array_Y_init = np.zeros(
+            (self.nLocalFluidInterfacePhysicalNodes)
+        )
+        self.localFluidInterface_array_Z_init = np.zeros(
+            (self.nLocalFluidInterfacePhysicalNodes)
+        )
         for iVertex in range(self.nLocalFluidInterfaceNodes):
             # Note that the fluid solver is separated in more processors outside the python script
             # thus when, from a core, we request for the vertices on the interface, we only obtain
@@ -574,19 +745,21 @@ def interfaceMapping(self,FluidSolver, SolidSolver, FSI_config):
             else:
                 posx, posy, posz = FluidSolver.InitialCoordinates().Get(iPoint)
             if GlobalIndex not in self.FluidHaloNodeList[myid].keys():
-              fluidIndexing_temp[GlobalIndex] = self.__getGlobalIndex('fluid', myid, localIndex)
-              self.localFluidInterface_array_X_init[localIndex] = posx
-              self.localFluidInterface_array_Y_init[localIndex] = posy
-              self.localFluidInterface_array_Z_init[localIndex] = posz
-              localIndex += 1
+                fluidIndexing_temp[GlobalIndex] = self.__getGlobalIndex(
+                    "fluid", myid, localIndex
+                )
+                self.localFluidInterface_array_X_init[localIndex] = posx
+                self.localFluidInterface_array_Y_init[localIndex] = posy
+                self.localFluidInterface_array_Z_init[localIndex] = posz
+                localIndex += 1
         if self.have_MPI:
-          fluidIndexing_temp = self.comm.allgather(fluidIndexing_temp)
-          for ii in range(len(fluidIndexing_temp)):
-            for key, value in fluidIndexing_temp[ii].items():
-              # This contains the link between the global index in python and that in SU2
-              self.fluidIndexing[key] = value
+            fluidIndexing_temp = self.comm.allgather(fluidIndexing_temp)
+            for ii in range(len(fluidIndexing_temp)):
+                for key, value in fluidIndexing_temp[ii].items():
+                    # This contains the link between the global index in python and that in SU2
+                    self.fluidIndexing[key] = value
         else:
-          self.fluidIndexing = fluidIndexing_temp.copy()
+            self.fluidIndexing = fluidIndexing_temp.copy()
         del fluidIndexing_temp
 
         # --- Get the solid interface from solid solver on each partition ---
@@ -596,181 +769,332 @@ def interfaceMapping(self,FluidSolver, SolidSolver, FSI_config):
         self.localSolidInterface_array_Y_init = np.zeros(self.nLocalSolidInterfaceNodes)
         self.localSolidInterface_array_Z_init = np.zeros(self.nLocalSolidInterfaceNodes)
         for iVertex in range(self.nLocalSolidInterfaceNodes):
-          GlobalIndex = SolidSolver.getVertexGlobalIndex(self.solidInterfaceIdentifier, iVertex)
-          posx, posy, posz = SolidSolver.getInterfaceNodePosInit(self.solidInterfaceIdentifier, iVertex)
-          if GlobalIndex not in self.SolidHaloNodeList[myid].keys():
-            solidIndexing_temp[GlobalIndex] = self.__getGlobalIndex('solid', myid, localIndex)
-            self.localSolidInterface_array_X_init[localIndex] = posx
-            self.localSolidInterface_array_Y_init[localIndex] = posy
-            self.localSolidInterface_array_Z_init[localIndex] = posz
-            localIndex += 1
+            GlobalIndex = SolidSolver.getVertexGlobalIndex(
+                self.solidInterfaceIdentifier, iVertex
+            )
+            posx, posy, posz = SolidSolver.getInterfaceNodePosInit(
+                self.solidInterfaceIdentifier, iVertex
+            )
+            if GlobalIndex not in self.SolidHaloNodeList[myid].keys():
+                solidIndexing_temp[GlobalIndex] = self.__getGlobalIndex(
+                    "solid", myid, localIndex
+                )
+                self.localSolidInterface_array_X_init[localIndex] = posx
+                self.localSolidInterface_array_Y_init[localIndex] = posy
+                self.localSolidInterface_array_Z_init[localIndex] = posz
+                localIndex += 1
         if self.have_MPI:
-          solidIndexing_temp = self.comm.allgather(solidIndexing_temp)
-          for ii in range(len(solidIndexing_temp)):
-            for key, value in solidIndexing_temp[ii].items():
-              self.solidIndexing[key] = value
+            solidIndexing_temp = self.comm.allgather(solidIndexing_temp)
+            for ii in range(len(solidIndexing_temp)):
+                for key, value in solidIndexing_temp[ii].items():
+                    self.solidIndexing[key] = value
         else:
-          self.solidIndexing = solidIndexing_temp.copy()
+            self.solidIndexing = solidIndexing_temp.copy()
         del solidIndexing_temp
 
-
         # --- Create the PETSc parallel interpolation matrix ---
-        if FSI_config['MATCHING_MESH'] == 'NO' and (FSI_config['MESH_INTERP_METHOD'] == 'RBF' or FSI_config['MESH_INTERP_METHOD'] == 'TPS'):
-          if self.have_MPI:
-            self.MappingMatrixA = PETSc.Mat().create(self.comm)
-            self.MappingMatrixB = PETSc.Mat().create(self.comm)
-            self.MappingMatrixA_T = PETSc.Mat().create(self.comm)
-            self.MappingMatrixB_T = PETSc.Mat().create(self.comm)
-            if FSI_config['MESH_INTERP_METHOD'] == 'RBF' :
-              self.MappingMatrixA.setType('mpiaij')
-              self.MappingMatrixB.setType('mpiaij')
-              self.MappingMatrixA_T.setType('mpiaij')
-              self.MappingMatrixB_T.setType('mpiaij')
+        if FSI_config["MATCHING_MESH"] == "NO" and (
+            FSI_config["MESH_INTERP_METHOD"] == "RBF"
+            or FSI_config["MESH_INTERP_METHOD"] == "TPS"
+        ):
+            if self.have_MPI:
+                self.MappingMatrixA = PETSc.Mat().create(self.comm)
+                self.MappingMatrixB = PETSc.Mat().create(self.comm)
+                self.MappingMatrixA_T = PETSc.Mat().create(self.comm)
+                self.MappingMatrixB_T = PETSc.Mat().create(self.comm)
+                if FSI_config["MESH_INTERP_METHOD"] == "RBF":
+                    self.MappingMatrixA.setType("mpiaij")
+                    self.MappingMatrixB.setType("mpiaij")
+                    self.MappingMatrixA_T.setType("mpiaij")
+                    self.MappingMatrixB_T.setType("mpiaij")
+                else:
+                    self.MappingMatrixA.setType("mpiaij")
+                    self.MappingMatrixB.setType("mpiaij")
+                    self.MappingMatrixA_T.setType("mpiaij")
+                    self.MappingMatrixB_T.setType("mpiaij")
             else:
-              self.MappingMatrixA.setType('mpiaij')
-              self.MappingMatrixB.setType('mpiaij')
-              self.MappingMatrixA_T.setType('mpiaij')
-              self.MappingMatrixB_T.setType('mpiaij')
-          else:
-            self.MappingMatrixA = PETSc.Mat().create()
-            self.MappingMatrixB = PETSc.Mat().create()
-            self.MappingMatrixA_T = PETSc.Mat().create()
-            self.MappingMatrixB_T = PETSc.Mat().create()
-            if FSI_config['MESH_INTERP_METHOD'] == 'RBF' :
-              self.MappingMatrixA.setType('aij')
-              self.MappingMatrixB.setType('aij')
-              self.MappingMatrixA_T.setType('aij')
-              self.MappingMatrixB_T.setType('aij')
+                self.MappingMatrixA = PETSc.Mat().create()
+                self.MappingMatrixB = PETSc.Mat().create()
+                self.MappingMatrixA_T = PETSc.Mat().create()
+                self.MappingMatrixB_T = PETSc.Mat().create()
+                if FSI_config["MESH_INTERP_METHOD"] == "RBF":
+                    self.MappingMatrixA.setType("aij")
+                    self.MappingMatrixB.setType("aij")
+                    self.MappingMatrixA_T.setType("aij")
+                    self.MappingMatrixB_T.setType("aij")
+                else:
+                    self.MappingMatrixA.setType("aij")
+                    self.MappingMatrixB.setType("aij")
+                    self.MappingMatrixA_T.setType("aij")
+                    self.MappingMatrixB_T.setType("aij")
+            self.MappingMatrixA.setSizes(
+                (
+                    self.nSolidInterfacePhysicalNodes + self.d_RBF,
+                    self.nSolidInterfacePhysicalNodes + self.d_RBF,
+                )
+            )
+            self.MappingMatrixA.setUp()
+            self.MappingMatrixA.setOption(
+                PETSc.Mat().Option.NEW_NONZERO_ALLOCATION_ERR, False
+            )
+            self.MappingMatrixB.setSizes(
+                (
+                    self.nFluidInterfacePhysicalNodes,
+                    self.nSolidInterfacePhysicalNodes + self.d_RBF,
+                )
+            )
+            self.MappingMatrixB.setUp()
+            self.MappingMatrixB.setOption(
+                PETSc.Mat().Option.NEW_NONZERO_ALLOCATION_ERR, False
+            )
+            self.MappingMatrixA_T.setSizes(
+                (
+                    self.nSolidInterfacePhysicalNodes + self.d_RBF,
+                    self.nSolidInterfacePhysicalNodes + self.d_RBF,
+                )
+            )
+            self.MappingMatrixA_T.setUp()
+            self.MappingMatrixA_T.setOption(
+                PETSc.Mat().Option.NEW_NONZERO_ALLOCATION_ERR, False
+            )
+            self.MappingMatrixB_T.setSizes(
+                (
+                    self.nSolidInterfacePhysicalNodes + self.d_RBF,
+                    self.nFluidInterfacePhysicalNodes,
+                )
+            )
+            self.MappingMatrixB_T.setUp()
+            self.MappingMatrixB_T.setOption(
+                PETSc.Mat().Option.NEW_NONZERO_ALLOCATION_ERR, False
+            )
+        else:
+            if self.have_MPI:
+                self.MappingMatrix = PETSc.Mat().create(self.comm)
+                self.MappingMatrix_T = PETSc.Mat().create(self.comm)
+                self.MappingMatrix.setType("mpiaij")
+                self.MappingMatrix_T.setType("mpiaij")
             else:
-              self.MappingMatrixA.setType('aij')
-              self.MappingMatrixB.setType('aij')
-              self.MappingMatrixA_T.setType('aij')
-              self.MappingMatrixB_T.setType('aij')
-          self.MappingMatrixA.setSizes((self.nSolidInterfacePhysicalNodes+self.d_RBF, self.nSolidInterfacePhysicalNodes+self.d_RBF))
-          self.MappingMatrixA.setUp()
-          self.MappingMatrixA.setOption(PETSc.Mat().Option.NEW_NONZERO_ALLOCATION_ERR, False)
-          self.MappingMatrixB.setSizes((self.nFluidInterfacePhysicalNodes, self.nSolidInterfacePhysicalNodes+self.d_RBF))
-          self.MappingMatrixB.setUp()
-          self.MappingMatrixB.setOption(PETSc.Mat().Option.NEW_NONZERO_ALLOCATION_ERR, False)
-          self.MappingMatrixA_T.setSizes((self.nSolidInterfacePhysicalNodes+self.d_RBF, self.nSolidInterfacePhysicalNodes+self.d_RBF))
-          self.MappingMatrixA_T.setUp()
-          self.MappingMatrixA_T.setOption(PETSc.Mat().Option.NEW_NONZERO_ALLOCATION_ERR, False)
-          self.MappingMatrixB_T.setSizes((self.nSolidInterfacePhysicalNodes+self.d_RBF, self.nFluidInterfacePhysicalNodes))
-          self.MappingMatrixB_T.setUp()
-          self.MappingMatrixB_T.setOption(PETSc.Mat().Option.NEW_NONZERO_ALLOCATION_ERR, False)
-        else:
-          if self.have_MPI:
-            self.MappingMatrix = PETSc.Mat().create(self.comm)
-            self.MappingMatrix_T = PETSc.Mat().create(self.comm)
-            self.MappingMatrix.setType('mpiaij')
-            self.MappingMatrix_T.setType('mpiaij')
-          else:
-            self.MappingMatrix = PETSc.Mat().create()
-            self.MappingMatrix_T = PETSc.Mat().create()
-            self.MappingMatrix.setType('aij')
-            self.MappingMatrix_T.setType('aij')
-          self.MappingMatrix.setSizes((self.nFluidInterfacePhysicalNodes, self.nSolidInterfacePhysicalNodes))
-          self.MappingMatrix.setUp()
-          self.MappingMatrix.setOption(PETSc.Mat().Option.NEW_NONZERO_ALLOCATION_ERR, False)
-          self.MappingMatrix_T.setSizes((self.nSolidInterfacePhysicalNodes, self.nFluidInterfacePhysicalNodes))
-          self.MappingMatrix_T.setUp()
-          self.MappingMatrix_T.setOption(PETSc.Mat().Option.NEW_NONZERO_ALLOCATION_ERR, False)
-
+                self.MappingMatrix = PETSc.Mat().create()
+                self.MappingMatrix_T = PETSc.Mat().create()
+                self.MappingMatrix.setType("aij")
+                self.MappingMatrix_T.setType("aij")
+            self.MappingMatrix.setSizes(
+                (self.nFluidInterfacePhysicalNodes, self.nSolidInterfacePhysicalNodes)
+            )
+            self.MappingMatrix.setUp()
+            self.MappingMatrix.setOption(
+                PETSc.Mat().Option.NEW_NONZERO_ALLOCATION_ERR, False
+            )
+            self.MappingMatrix_T.setSizes(
+                (self.nSolidInterfacePhysicalNodes, self.nFluidInterfacePhysicalNodes)
+            )
+            self.MappingMatrix_T.setUp()
+            self.MappingMatrix_T.setOption(
+                PETSc.Mat().Option.NEW_NONZERO_ALLOCATION_ERR, False
+            )
 
         # --- Fill the interpolation matrix in parallel (working in serial too) ---
-        if FSI_config['MATCHING_MESH'] == 'NO' and (FSI_config['MESH_INTERP_METHOD'] == 'RBF' or FSI_config['MESH_INTERP_METHOD'] == 'TPS'):
-          self.MPIPrint('Building interpolation matrices...')
-          if self.have_MPI:
-            for iProc in self.solidInterfaceProcessors:
-              if myid == iProc:
-                for jProc in self.solidInterfaceProcessors:
-                  if jProc != iProc:
-                    self.comm.Send(self.localSolidInterface_array_X_init, dest=jProc, tag=1)
-                    self.comm.Send(self.localSolidInterface_array_Y_init, dest=jProc, tag=2)
-                    self.comm.Send(self.localSolidInterface_array_Z_init, dest=jProc, tag=3)
-                  else:
-                    solidInterfaceBuffRcv_X = np.copy(self.localSolidInterface_array_X_init)
-                    solidInterfaceBuffRcv_Y = np.copy(self.localSolidInterface_array_Y_init)
-                    solidInterfaceBuffRcv_Z = np.copy(self.localSolidInterface_array_Z_init)
-              if myid in self.solidInterfaceProcessors:
-                if myid != iProc:
-                  sizeOfBuff = self.solidPhysicalInterfaceNodesDistribution[iProc]
-                  solidInterfaceBuffRcv_X = np.empty(sizeOfBuff, dtype=np.float64)
-                  solidInterfaceBuffRcv_Y = np.empty(sizeOfBuff, dtype=np.float64)
-                  solidInterfaceBuffRcv_Z = np.empty(sizeOfBuff, dtype=np.float64)
-                  self.comm.Recv(solidInterfaceBuffRcv_X, source=iProc, tag=1)
-                  self.comm.Recv(solidInterfaceBuffRcv_Y, source=iProc, tag=2)
-                  self.comm.Recv(solidInterfaceBuffRcv_Z, source=iProc, tag=3)
-                if FSI_config['MESH_INTERP_METHOD'] == 'RBF':
-                  self.RBFMeshMapping_A(solidInterfaceBuffRcv_X, solidInterfaceBuffRcv_Y, solidInterfaceBuffRcv_Z, iProc, self.RBF_rad)
-                else:
-                  self.TPSMeshMapping_A(solidInterfaceBuffRcv_X, solidInterfaceBuffRcv_Y, solidInterfaceBuffRcv_Z, iProc)
-          else:
-            if FSI_config['MESH_INTERP_METHOD'] == 'RBF':
-              self.RBFMeshMapping_A(self.localSolidInterface_array_X_init, self.localSolidInterface_array_Y_init, self.localSolidInterface_array_Z_init, 0, self.RBF_rad)
+        if FSI_config["MATCHING_MESH"] == "NO" and (
+            FSI_config["MESH_INTERP_METHOD"] == "RBF"
+            or FSI_config["MESH_INTERP_METHOD"] == "TPS"
+        ):
+            self.MPIPrint("Building interpolation matrices...")
+            if self.have_MPI:
+                for iProc in self.solidInterfaceProcessors:
+                    if myid == iProc:
+                        for jProc in self.solidInterfaceProcessors:
+                            if jProc != iProc:
+                                self.comm.Send(
+                                    self.localSolidInterface_array_X_init,
+                                    dest=jProc,
+                                    tag=1,
+                                )
+                                self.comm.Send(
+                                    self.localSolidInterface_array_Y_init,
+                                    dest=jProc,
+                                    tag=2,
+                                )
+                                self.comm.Send(
+                                    self.localSolidInterface_array_Z_init,
+                                    dest=jProc,
+                                    tag=3,
+                                )
+                            else:
+                                solidInterfaceBuffRcv_X = np.copy(
+                                    self.localSolidInterface_array_X_init
+                                )
+                                solidInterfaceBuffRcv_Y = np.copy(
+                                    self.localSolidInterface_array_Y_init
+                                )
+                                solidInterfaceBuffRcv_Z = np.copy(
+                                    self.localSolidInterface_array_Z_init
+                                )
+                    if myid in self.solidInterfaceProcessors:
+                        if myid != iProc:
+                            sizeOfBuff = self.solidPhysicalInterfaceNodesDistribution[
+                                iProc
+                            ]
+                            solidInterfaceBuffRcv_X = np.empty(
+                                sizeOfBuff, dtype=np.float64
+                            )
+                            solidInterfaceBuffRcv_Y = np.empty(
+                                sizeOfBuff, dtype=np.float64
+                            )
+                            solidInterfaceBuffRcv_Z = np.empty(
+                                sizeOfBuff, dtype=np.float64
+                            )
+                            self.comm.Recv(solidInterfaceBuffRcv_X, source=iProc, tag=1)
+                            self.comm.Recv(solidInterfaceBuffRcv_Y, source=iProc, tag=2)
+                            self.comm.Recv(solidInterfaceBuffRcv_Z, source=iProc, tag=3)
+                        if FSI_config["MESH_INTERP_METHOD"] == "RBF":
+                            self.RBFMeshMapping_A(
+                                solidInterfaceBuffRcv_X,
+                                solidInterfaceBuffRcv_Y,
+                                solidInterfaceBuffRcv_Z,
+                                iProc,
+                                self.RBF_rad,
+                            )
+                        else:
+                            self.TPSMeshMapping_A(
+                                solidInterfaceBuffRcv_X,
+                                solidInterfaceBuffRcv_Y,
+                                solidInterfaceBuffRcv_Z,
+                                iProc,
+                            )
             else:
-              self.TPSMeshMapping_A(self.localSolidInterface_array_X_init, self.localSolidInterface_array_Y_init, self.localSolidInterface_array_Z_init, 0)
-          self.MappingMatrixA.assemblyBegin()
-          self.MappingMatrixA.assemblyEnd()
-          self.MappingMatrixA_T.assemblyBegin()
-          self.MappingMatrixA_T.assemblyEnd()
-          self.MPIPrint('Matrix A is built.')
-        else:
-          self.MPIPrint("Building interpolation matrix...")
+                if FSI_config["MESH_INTERP_METHOD"] == "RBF":
+                    self.RBFMeshMapping_A(
+                        self.localSolidInterface_array_X_init,
+                        self.localSolidInterface_array_Y_init,
+                        self.localSolidInterface_array_Z_init,
+                        0,
+                        self.RBF_rad,
+                    )
+                else:
+                    self.TPSMeshMapping_A(
+                        self.localSolidInterface_array_X_init,
+                        self.localSolidInterface_array_Y_init,
+                        self.localSolidInterface_array_Z_init,
+                        0,
+                    )
+            self.MappingMatrixA.assemblyBegin()
+            self.MappingMatrixA.assemblyEnd()
+            self.MappingMatrixA_T.assemblyBegin()
+            self.MappingMatrixA_T.assemblyEnd()
+            self.MPIPrint("Matrix A is built.")
+        else:
+            self.MPIPrint("Building interpolation matrix...")
         self.MPIBarrier()
         if self.have_MPI:
-          for iProc in self.solidInterfaceProcessors:
-            if myid == iProc:
-              for jProc in self.fluidInterfaceProcessors:
-                if jProc != iProc:
-                  self.comm.Send(self.localSolidInterface_array_X_init, dest=jProc, tag=1)
-                  self.comm.Send(self.localSolidInterface_array_Y_init, dest=jProc, tag=2)
-                  self.comm.Send(self.localSolidInterface_array_Z_init, dest=jProc, tag=3)
-                else:
-                  solidInterfaceBuffRcv_X = np.copy(self.localSolidInterface_array_X_init)
-                  solidInterfaceBuffRcv_Y = np.copy(self.localSolidInterface_array_Y_init)
-                  solidInterfaceBuffRcv_Z = np.copy(self.localSolidInterface_array_Z_init)
-            if myid in self.fluidInterfaceProcessors:
-              if myid != iProc:
-                sizeOfBuff = self.solidPhysicalInterfaceNodesDistribution[iProc]
-                solidInterfaceBuffRcv_X = np.empty(sizeOfBuff, dtype=np.float64)
-                solidInterfaceBuffRcv_Y = np.empty(sizeOfBuff, dtype=np.float64)
-                solidInterfaceBuffRcv_Z = np.empty(sizeOfBuff, dtype=np.float64)
-                self.comm.Recv(solidInterfaceBuffRcv_X, source=iProc, tag=1)
-                self.comm.Recv(solidInterfaceBuffRcv_Y, source=iProc, tag=2)
-                self.comm.Recv(solidInterfaceBuffRcv_Z, source=iProc, tag=3)
-              if FSI_config['MATCHING_MESH'] == 'NO':
-                if FSI_config['MESH_INTERP_METHOD'] == 'RBF':
-                  self.RBFMeshMapping_B(solidInterfaceBuffRcv_X, solidInterfaceBuffRcv_Y, solidInterfaceBuffRcv_Z, iProc, self.RBF_rad)
-                elif FSI_config['MESH_INTERP_METHOD'] == 'TPS':
-                  self.TPSMeshMapping_B(solidInterfaceBuffRcv_X, solidInterfaceBuffRcv_Y, solidInterfaceBuffRcv_Z, iProc)
+            for iProc in self.solidInterfaceProcessors:
+                if myid == iProc:
+                    for jProc in self.fluidInterfaceProcessors:
+                        if jProc != iProc:
+                            self.comm.Send(
+                                self.localSolidInterface_array_X_init, dest=jProc, tag=1
+                            )
+                            self.comm.Send(
+                                self.localSolidInterface_array_Y_init, dest=jProc, tag=2
+                            )
+                            self.comm.Send(
+                                self.localSolidInterface_array_Z_init, dest=jProc, tag=3
+                            )
+                        else:
+                            solidInterfaceBuffRcv_X = np.copy(
+                                self.localSolidInterface_array_X_init
+                            )
+                            solidInterfaceBuffRcv_Y = np.copy(
+                                self.localSolidInterface_array_Y_init
+                            )
+                            solidInterfaceBuffRcv_Z = np.copy(
+                                self.localSolidInterface_array_Z_init
+                            )
+                if myid in self.fluidInterfaceProcessors:
+                    if myid != iProc:
+                        sizeOfBuff = self.solidPhysicalInterfaceNodesDistribution[iProc]
+                        solidInterfaceBuffRcv_X = np.empty(sizeOfBuff, dtype=np.float64)
+                        solidInterfaceBuffRcv_Y = np.empty(sizeOfBuff, dtype=np.float64)
+                        solidInterfaceBuffRcv_Z = np.empty(sizeOfBuff, dtype=np.float64)
+                        self.comm.Recv(solidInterfaceBuffRcv_X, source=iProc, tag=1)
+                        self.comm.Recv(solidInterfaceBuffRcv_Y, source=iProc, tag=2)
+                        self.comm.Recv(solidInterfaceBuffRcv_Z, source=iProc, tag=3)
+                    if FSI_config["MATCHING_MESH"] == "NO":
+                        if FSI_config["MESH_INTERP_METHOD"] == "RBF":
+                            self.RBFMeshMapping_B(
+                                solidInterfaceBuffRcv_X,
+                                solidInterfaceBuffRcv_Y,
+                                solidInterfaceBuffRcv_Z,
+                                iProc,
+                                self.RBF_rad,
+                            )
+                        elif FSI_config["MESH_INTERP_METHOD"] == "TPS":
+                            self.TPSMeshMapping_B(
+                                solidInterfaceBuffRcv_X,
+                                solidInterfaceBuffRcv_Y,
+                                solidInterfaceBuffRcv_Z,
+                                iProc,
+                            )
+                        else:
+                            self.NearestNeighboorMeshMapping(
+                                solidInterfaceBuffRcv_X,
+                                solidInterfaceBuffRcv_Y,
+                                solidInterfaceBuffRcv_Z,
+                                iProc,
+                            )
+                    else:
+                        self.matchingMeshMapping(
+                            solidInterfaceBuffRcv_X,
+                            solidInterfaceBuffRcv_Y,
+                            solidInterfaceBuffRcv_Z,
+                            iProc,
+                        )
+        else:
+            if FSI_config["MATCHING_MESH"] == "NO":
+                if FSI_config["MESH_INTERP_METHOD"] == "RBF":
+                    self.RBFMeshMapping_B(
+                        self.localSolidInterface_array_X_init,
+                        self.localSolidInterface_array_Y_init,
+                        self.localSolidInterface_array_Z_init,
+                        0,
+                        self.RBF_rad,
+                    )
+                elif FSI_config["MESH_INTERP_METHOD"] == "TPS":
+                    self.TPSMeshMapping_B(
+                        self.localSolidInterface_array_X_init,
+                        self.localSolidInterface_array_Y_init,
+                        self.localSolidInterface_array_Z_init,
+                        0,
+                    )
                 else:
-                  self.NearestNeighboorMeshMapping(solidInterfaceBuffRcv_X, solidInterfaceBuffRcv_Y, solidInterfaceBuffRcv_Z, iProc)
-              else:
-                self.matchingMeshMapping(solidInterfaceBuffRcv_X, solidInterfaceBuffRcv_Y, solidInterfaceBuffRcv_Z, iProc)
-        else:
-          if FSI_config['MATCHING_MESH'] == 'NO':
-            if FSI_config['MESH_INTERP_METHOD'] == 'RBF':
-              self.RBFMeshMapping_B(self.localSolidInterface_array_X_init, self.localSolidInterface_array_Y_init, self.localSolidInterface_array_Z_init, 0, self.RBF_rad)
-            elif FSI_config['MESH_INTERP_METHOD'] == 'TPS' :
-              self.TPSMeshMapping_B(self.localSolidInterface_array_X_init, self.localSolidInterface_array_Y_init, self.localSolidInterface_array_Z_init, 0)
+                    self.NearestNeighboorMeshMapping(
+                        self.localSolidInterface_array_X_init,
+                        self.localSolidInterface_array_Y_init,
+                        self.localSolidInterface_array_Z_init,
+                        0,
+                    )
             else:
-              self.NearestNeighboorMeshMapping(self.localSolidInterface_array_X_init, self.localSolidInterface_array_Y_init, self.localSolidInterface_array_Z_init, 0)
-          else:
-            self.matchingMeshMapping(self.localSolidInterface_array_X_init, self.localSolidInterface_array_Y_init, self.localSolidInterface_array_Z_init, 0)
-
-        if FSI_config['MATCHING_MESH'] == 'NO' and (FSI_config['MESH_INTERP_METHOD'] == 'RBF' or FSI_config['MESH_INTERP_METHOD'] == 'TPS'):
-          self.MappingMatrixB.assemblyBegin()
-          self.MappingMatrixB.assemblyEnd()
-          self.MappingMatrixB_T.assemblyBegin()
-          self.MappingMatrixB_T.assemblyEnd()
-          self.MPIPrint('Matrix B is built.')
-        else:
-          self.MappingMatrix.assemblyBegin()
-          self.MappingMatrix.assemblyEnd()
-          self.MappingMatrix_T.assemblyBegin()
-          self.MappingMatrix_T.assemblyEnd()
-          self.MPIPrint("Interpolation matrix is built.")
+                self.matchingMeshMapping(
+                    self.localSolidInterface_array_X_init,
+                    self.localSolidInterface_array_Y_init,
+                    self.localSolidInterface_array_Z_init,
+                    0,
+                )
+
+        if FSI_config["MATCHING_MESH"] == "NO" and (
+            FSI_config["MESH_INTERP_METHOD"] == "RBF"
+            or FSI_config["MESH_INTERP_METHOD"] == "TPS"
+        ):
+            self.MappingMatrixB.assemblyBegin()
+            self.MappingMatrixB.assemblyEnd()
+            self.MappingMatrixB_T.assemblyBegin()
+            self.MappingMatrixB_T.assemblyEnd()
+            self.MPIPrint("Matrix B is built.")
+        else:
+            self.MappingMatrix.assemblyBegin()
+            self.MappingMatrix.assemblyEnd()
+            self.MappingMatrix_T.assemblyBegin()
+            self.MappingMatrix_T.assemblyEnd()
+            self.MPIPrint("Interpolation matrix is built.")
 
         self.MPIBarrier()
 
@@ -781,14 +1105,20 @@ def interfaceMapping(self,FluidSolver, SolidSolver, FSI_config):
         del self.localFluidInterface_array_Y_init
         del self.localFluidInterface_array_Z_init
 
-    def matchingMeshMapping(self,solidInterfaceBuffRcv_X, solidInterfaceBuffRcv_Y, solidInterfaceBuffRcv_Z, iProc):
+    def matchingMeshMapping(
+        self,
+        solidInterfaceBuffRcv_X,
+        solidInterfaceBuffRcv_Y,
+        solidInterfaceBuffRcv_Z,
+        iProc,
+    ):
         """
         Fill the mapping matrix in case of matching meshes at the f/s interface.
         """
         if self.have_MPI:
-          myid = self.comm.Get_rank()
+            myid = self.comm.Get_rank()
         else:
-          myid = 0
+            myid = 0
 
         # --- Instantiate the spatial indexing ---
         prop_index = index.Property()
@@ -798,39 +1128,65 @@ def matchingMeshMapping(self,solidInterfaceBuffRcv_X, solidInterfaceBuffRcv_Y, s
         nSolidNodes = solidInterfaceBuffRcv_X.shape[0]
 
         for jVertex in range(nSolidNodes):
-          posX = solidInterfaceBuffRcv_X[jVertex]
-          posY = solidInterfaceBuffRcv_Y[jVertex]
-          posZ = solidInterfaceBuffRcv_Z[jVertex]
-          if self.nDim == 2 :
-            SolidSpatialTree.add(jVertex, (posX, posY))
-          else :
-            SolidSpatialTree.add(jVertex, (posX, posY, posZ))
+            posX = solidInterfaceBuffRcv_X[jVertex]
+            posY = solidInterfaceBuffRcv_Y[jVertex]
+            posZ = solidInterfaceBuffRcv_Z[jVertex]
+            if self.nDim == 2:
+                SolidSpatialTree.add(jVertex, (posX, posY))
+            else:
+                SolidSpatialTree.add(jVertex, (posX, posY, posZ))
 
         if self.nFluidInterfacePhysicalNodes != self.nSolidInterfacePhysicalNodes:
-          raise Exception("Fluid and solid interface must have the same number of nodes for matching meshes ! ")
+            raise Exception(
+                "Fluid and solid interface must have the same number of nodes for matching meshes ! "
+            )
 
         # --- For each fluid interface node, find the nearest solid interface node and fill the boolean mapping matrix ---
         for iVertexFluid in range(self.nLocalFluidInterfacePhysicalNodes):
-          posX = self.localFluidInterface_array_X_init[iVertexFluid]
-          posY = self.localFluidInterface_array_Y_init[iVertexFluid]
-          posZ = self.localFluidInterface_array_Z_init[iVertexFluid]
-          if self.nDim == 2:
-            neighboors = list(SolidSpatialTree.nearest((posX, posY),1))
-          elif self.nDim == 3:
-            neighboors = list(SolidSpatialTree.nearest((posX, posY, posZ),1))
-          jVertexSolid = neighboors[0]
-          # Check if the distance is small enough to ensure coincidence
-          NodeA = np.array([posX, posY, posZ])
-          NodeB = np.array([solidInterfaceBuffRcv_X[jVertexSolid], solidInterfaceBuffRcv_Y[jVertexSolid], solidInterfaceBuffRcv_Z[jVertexSolid]])
-          distance = spdist.euclidean(NodeA, NodeB)
-          iGlobalVertexFluid = self.__getGlobalIndex('fluid', myid, iVertexFluid)
-          jGlobalVertexSolid = self.__getGlobalIndex('solid', iProc, jVertexSolid)
-          if distance > 1e-6:
-            print("WARNING : Tolerance for matching meshes is not matched between node F{} and S{} : ({}, {}, {})<-->({}, {}, {}) , DISTANCE : {} !".format(iGlobalVertexFluid,jGlobalVertexSolid,posX, posY, posZ,solidInterfaceBuffRcv_X[jVertexSolid], solidInterfaceBuffRcv_Y[jVertexSolid], solidInterfaceBuffRcv_Z[jVertexSolid], distance))
-          self.MappingMatrix.setValue(iGlobalVertexFluid,jGlobalVertexSolid,1.0)
-          self.MappingMatrix_T.setValue(jGlobalVertexSolid, iGlobalVertexFluid,1.0)
-
-    def NearestNeighboorMeshMapping(self, solidInterfaceBuffRcv_X, solidInterfaceBuffRcv_Y, solidInterfaceBuffRcv_Z, iProc):
+            posX = self.localFluidInterface_array_X_init[iVertexFluid]
+            posY = self.localFluidInterface_array_Y_init[iVertexFluid]
+            posZ = self.localFluidInterface_array_Z_init[iVertexFluid]
+            if self.nDim == 2:
+                neighboors = list(SolidSpatialTree.nearest((posX, posY), 1))
+            elif self.nDim == 3:
+                neighboors = list(SolidSpatialTree.nearest((posX, posY, posZ), 1))
+            jVertexSolid = neighboors[0]
+            # Check if the distance is small enough to ensure coincidence
+            NodeA = np.array([posX, posY, posZ])
+            NodeB = np.array(
+                [
+                    solidInterfaceBuffRcv_X[jVertexSolid],
+                    solidInterfaceBuffRcv_Y[jVertexSolid],
+                    solidInterfaceBuffRcv_Z[jVertexSolid],
+                ]
+            )
+            distance = spdist.euclidean(NodeA, NodeB)
+            iGlobalVertexFluid = self.__getGlobalIndex("fluid", myid, iVertexFluid)
+            jGlobalVertexSolid = self.__getGlobalIndex("solid", iProc, jVertexSolid)
+            if distance > 1e-6:
+                print(
+                    "WARNING : Tolerance for matching meshes is not matched between node F{} and S{} : ({}, {}, {})<-->({}, {}, {}) , DISTANCE : {} !".format(
+                        iGlobalVertexFluid,
+                        jGlobalVertexSolid,
+                        posX,
+                        posY,
+                        posZ,
+                        solidInterfaceBuffRcv_X[jVertexSolid],
+                        solidInterfaceBuffRcv_Y[jVertexSolid],
+                        solidInterfaceBuffRcv_Z[jVertexSolid],
+                        distance,
+                    )
+                )
+            self.MappingMatrix.setValue(iGlobalVertexFluid, jGlobalVertexSolid, 1.0)
+            self.MappingMatrix_T.setValue(jGlobalVertexSolid, iGlobalVertexFluid, 1.0)
+
+    def NearestNeighboorMeshMapping(
+        self,
+        solidInterfaceBuffRcv_X,
+        solidInterfaceBuffRcv_Y,
+        solidInterfaceBuffRcv_Z,
+        iProc,
+    ):
         """
         Interpolation based on the nearest neighboor.
         For each node, the mesh is scanned to find the closed node to the first
@@ -838,9 +1194,9 @@ def NearestNeighboorMeshMapping(self, solidInterfaceBuffRcv_X, solidInterfaceBuf
         """
 
         if self.have_MPI:
-          myid = self.comm.Get_rank()
+            myid = self.comm.Get_rank()
         else:
-          myid = 0
+            myid = 0
 
         # --- Instantiate the spatial indexing ---
         prop_index = index.Property()
@@ -850,30 +1206,37 @@ def NearestNeighboorMeshMapping(self, solidInterfaceBuffRcv_X, solidInterfaceBuf
         nSolidNodes = solidInterfaceBuffRcv_X.shape[0]
 
         for jVertex in range(nSolidNodes):
-          posX = solidInterfaceBuffRcv_X[jVertex]
-          posY = solidInterfaceBuffRcv_Y[jVertex]
-          posZ = solidInterfaceBuffRcv_Z[jVertex]
-          if self.nDim == 2 :
-            SolidSpatialTree.add(jVertex, (posX, posY))
-          else :
-            SolidSpatialTree.add(jVertex, (posX, posY, posZ))
+            posX = solidInterfaceBuffRcv_X[jVertex]
+            posY = solidInterfaceBuffRcv_Y[jVertex]
+            posZ = solidInterfaceBuffRcv_Z[jVertex]
+            if self.nDim == 2:
+                SolidSpatialTree.add(jVertex, (posX, posY))
+            else:
+                SolidSpatialTree.add(jVertex, (posX, posY, posZ))
 
         # --- For each fluid interface node, find the nearest solid interface node and fill the boolean mapping matrix ---
         for iVertexFluid in range(self.nLocalFluidInterfacePhysicalNodes):
-          posX = self.localFluidInterface_array_X_init[iVertexFluid]
-          posY = self.localFluidInterface_array_Y_init[iVertexFluid]
-          posZ = self.localFluidInterface_array_Z_init[iVertexFluid]
-          if self.nDim == 2:
-            neighboors = list(SolidSpatialTree.nearest((posX, posY),1))
-          elif self.nDim == 3:
-            neighboors = list(SolidSpatialTree.nearest((posX, posY, posZ),1))
-          jVertexSolid = neighboors[0]
-          iGlobalVertexFluid = self.__getGlobalIndex('fluid', myid, iVertexFluid)
-          jGlobalVertexSolid = self.__getGlobalIndex('solid', iProc, jVertexSolid)
-          self.MappingMatrix.setValue(iGlobalVertexFluid,jGlobalVertexSolid,1.0)
-          self.MappingMatrix_T.setValue(jGlobalVertexSolid, iGlobalVertexFluid,1.0)
-
-    def RBFMeshMapping_A(self, solidInterfaceBuffRcv_X, solidInterfaceBuffRcv_Y, solidInterfaceBuffRcv_Z, iProc, rad):
+            posX = self.localFluidInterface_array_X_init[iVertexFluid]
+            posY = self.localFluidInterface_array_Y_init[iVertexFluid]
+            posZ = self.localFluidInterface_array_Z_init[iVertexFluid]
+            if self.nDim == 2:
+                neighboors = list(SolidSpatialTree.nearest((posX, posY), 1))
+            elif self.nDim == 3:
+                neighboors = list(SolidSpatialTree.nearest((posX, posY, posZ), 1))
+            jVertexSolid = neighboors[0]
+            iGlobalVertexFluid = self.__getGlobalIndex("fluid", myid, iVertexFluid)
+            jGlobalVertexSolid = self.__getGlobalIndex("solid", iProc, jVertexSolid)
+            self.MappingMatrix.setValue(iGlobalVertexFluid, jGlobalVertexSolid, 1.0)
+            self.MappingMatrix_T.setValue(jGlobalVertexSolid, iGlobalVertexFluid, 1.0)
+
+    def RBFMeshMapping_A(
+        self,
+        solidInterfaceBuffRcv_X,
+        solidInterfaceBuffRcv_Y,
+        solidInterfaceBuffRcv_Z,
+        iProc,
+        rad,
+    ):
         """
         First part of the RBF mapping. This method provides the matrix required to
         obtain, from the structural displacements, the loadings of the kernel
@@ -881,9 +1244,9 @@ def RBFMeshMapping_A(self, solidInterfaceBuffRcv_X, solidInterfaceBuffRcv_Y, sol
         """
 
         if self.have_MPI:
-          myid = self.comm.Get_rank()
+            myid = self.comm.Get_rank()
         else:
-          myid = 0
+            myid = 0
 
         # --- Instantiate the spatial indexing ---
         prop_index = index.Property()
@@ -893,52 +1256,86 @@ def RBFMeshMapping_A(self, solidInterfaceBuffRcv_X, solidInterfaceBuffRcv_Y, sol
         nSolidNodes = solidInterfaceBuffRcv_X.shape[0]
 
         for jVertex in range(nSolidNodes):
-          posX = solidInterfaceBuffRcv_X[jVertex]
-          posY = solidInterfaceBuffRcv_Y[jVertex]
-          posZ = solidInterfaceBuffRcv_Z[jVertex]
-          if self.nDim == 2 :
-            SolidSpatialTree.add(jVertex, (posX, posY))
-          else :
-            SolidSpatialTree.add(jVertex, (posX, posY, posZ))
+            posX = solidInterfaceBuffRcv_X[jVertex]
+            posY = solidInterfaceBuffRcv_Y[jVertex]
+            posZ = solidInterfaceBuffRcv_Z[jVertex]
+            if self.nDim == 2:
+                SolidSpatialTree.add(jVertex, (posX, posY))
+            else:
+                SolidSpatialTree.add(jVertex, (posX, posY, posZ))
 
         for iVertexSolid in range(self.nLocalSolidInterfacePhysicalNodes):
-          posX = self.localSolidInterface_array_X_init[iVertexSolid]
-          posY = self.localSolidInterface_array_Y_init[iVertexSolid]
-          posZ = self.localSolidInterface_array_Z_init[iVertexSolid]
-          NodeA = np.array([posX, posY, posZ])
-          iGlobalVertexSolid = self.__getGlobalIndex('solid', myid, iVertexSolid)
-          if self.nDim == 2:
-            neighboors = list(SolidSpatialTree.intersection((posX-rad, posY-rad, posX+rad, posY+rad)))
-          elif self.nDim == 3:
-            neighboors = list(SolidSpatialTree.intersection((posX-rad, posY-rad, posZ-rad, posX+rad, posY+rad, posZ+rad)))
-          for jVertexSolid in neighboors:
-            NodeB = np.array([solidInterfaceBuffRcv_X[jVertexSolid], solidInterfaceBuffRcv_Y[jVertexSolid], solidInterfaceBuffRcv_Z[jVertexSolid]])
-            distance = spdist.euclidean(NodeA, NodeB)
-            phi = self.__CPC2(distance, rad)
-            jGlobalVertexSolid = self.__getGlobalIndex('solid', iProc, jVertexSolid)
-            self.MappingMatrixA.setValue(iGlobalVertexSolid, jGlobalVertexSolid, phi)
-            self.MappingMatrixA_T.setValue(jGlobalVertexSolid, iGlobalVertexSolid, phi)
-          self.MappingMatrixA.setValue(iGlobalVertexSolid, nSolidNodes, 1.0)
-          self.MappingMatrixA.setValue(iGlobalVertexSolid, nSolidNodes+1, posX)
-          self.MappingMatrixA.setValue(iGlobalVertexSolid, nSolidNodes+2, posY)
-          if self.nDim == 3:
-            self.MappingMatrixA.setValue(iGlobalVertexSolid, nSolidNodes+3, posZ)
-          self.MappingMatrixA_T.setValue(nSolidNodes, iGlobalVertexSolid, 1.0)
-          self.MappingMatrixA_T.setValue(nSolidNodes+1, iGlobalVertexSolid, posX)
-          self.MappingMatrixA_T.setValue(nSolidNodes+2, iGlobalVertexSolid, posY)
-          if self.nDim == 3:
-            self.MappingMatrixA_T.setValue(nSolidNodes+3, iGlobalVertexSolid, posZ)
-
-    def RBFMeshMapping_B(self, solidInterfaceBuffRcv_X, solidInterfaceBuffRcv_Y, solidInterfaceBuffRcv_Z, iProc, rad):
+            posX = self.localSolidInterface_array_X_init[iVertexSolid]
+            posY = self.localSolidInterface_array_Y_init[iVertexSolid]
+            posZ = self.localSolidInterface_array_Z_init[iVertexSolid]
+            NodeA = np.array([posX, posY, posZ])
+            iGlobalVertexSolid = self.__getGlobalIndex("solid", myid, iVertexSolid)
+            if self.nDim == 2:
+                neighboors = list(
+                    SolidSpatialTree.intersection(
+                        (posX - rad, posY - rad, posX + rad, posY + rad)
+                    )
+                )
+            elif self.nDim == 3:
+                neighboors = list(
+                    SolidSpatialTree.intersection(
+                        (
+                            posX - rad,
+                            posY - rad,
+                            posZ - rad,
+                            posX + rad,
+                            posY + rad,
+                            posZ + rad,
+                        )
+                    )
+                )
+            for jVertexSolid in neighboors:
+                NodeB = np.array(
+                    [
+                        solidInterfaceBuffRcv_X[jVertexSolid],
+                        solidInterfaceBuffRcv_Y[jVertexSolid],
+                        solidInterfaceBuffRcv_Z[jVertexSolid],
+                    ]
+                )
+                distance = spdist.euclidean(NodeA, NodeB)
+                phi = self.__CPC2(distance, rad)
+                jGlobalVertexSolid = self.__getGlobalIndex("solid", iProc, jVertexSolid)
+                self.MappingMatrixA.setValue(
+                    iGlobalVertexSolid, jGlobalVertexSolid, phi
+                )
+                self.MappingMatrixA_T.setValue(
+                    jGlobalVertexSolid, iGlobalVertexSolid, phi
+                )
+            self.MappingMatrixA.setValue(iGlobalVertexSolid, nSolidNodes, 1.0)
+            self.MappingMatrixA.setValue(iGlobalVertexSolid, nSolidNodes + 1, posX)
+            self.MappingMatrixA.setValue(iGlobalVertexSolid, nSolidNodes + 2, posY)
+            if self.nDim == 3:
+                self.MappingMatrixA.setValue(iGlobalVertexSolid, nSolidNodes + 3, posZ)
+            self.MappingMatrixA_T.setValue(nSolidNodes, iGlobalVertexSolid, 1.0)
+            self.MappingMatrixA_T.setValue(nSolidNodes + 1, iGlobalVertexSolid, posX)
+            self.MappingMatrixA_T.setValue(nSolidNodes + 2, iGlobalVertexSolid, posY)
+            if self.nDim == 3:
+                self.MappingMatrixA_T.setValue(
+                    nSolidNodes + 3, iGlobalVertexSolid, posZ
+                )
+
+    def RBFMeshMapping_B(
+        self,
+        solidInterfaceBuffRcv_X,
+        solidInterfaceBuffRcv_Y,
+        solidInterfaceBuffRcv_Z,
+        iProc,
+        rad,
+    ):
         """
         Second part of the RBF mapping. This method provides the matrix required to
         obtain, from the kernel function loadings, the fluid nodes displacements.
         """
 
         if self.have_MPI:
-          myid = self.comm.Get_rank()
+            myid = self.comm.Get_rank()
         else:
-          myid = 0
+            myid = 0
 
         # --- Instantiate the spatial indexing ---
         prop_index = index.Property()
@@ -948,43 +1345,76 @@ def RBFMeshMapping_B(self, solidInterfaceBuffRcv_X, solidInterfaceBuffRcv_Y, sol
         nSolidNodes = solidInterfaceBuffRcv_X.shape[0]
 
         for jVertex in range(nSolidNodes):
-          posX = solidInterfaceBuffRcv_X[jVertex]
-          posY = solidInterfaceBuffRcv_Y[jVertex]
-          posZ = solidInterfaceBuffRcv_Z[jVertex]
-          if self.nDim == 2 :
-            SolidSpatialTree.add(jVertex, (posX, posY))
-          else :
-            SolidSpatialTree.add(jVertex, (posX, posY, posZ))
+            posX = solidInterfaceBuffRcv_X[jVertex]
+            posY = solidInterfaceBuffRcv_Y[jVertex]
+            posZ = solidInterfaceBuffRcv_Z[jVertex]
+            if self.nDim == 2:
+                SolidSpatialTree.add(jVertex, (posX, posY))
+            else:
+                SolidSpatialTree.add(jVertex, (posX, posY, posZ))
 
         for iVertexFluid in range(self.nLocalFluidInterfacePhysicalNodes):
-          posX = self.localFluidInterface_array_X_init[iVertexFluid]
-          posY = self.localFluidInterface_array_Y_init[iVertexFluid]
-          posZ = self.localFluidInterface_array_Z_init[iVertexFluid]
-          NodeA = np.array([posX, posY, posZ])
-          iGlobalVertexFluid = self.__getGlobalIndex('fluid', myid, iVertexFluid)
-          if self.nDim == 2:
-            neighboors = list(SolidSpatialTree.intersection((posX-rad, posY-rad, posX+rad, posY+rad)))
-          elif self.nDim == 3:
-            neighboors = list(SolidSpatialTree.intersection((posX-rad, posY-rad, posZ-rad, posX+rad, posY+rad, posZ+rad)))
-          for jVertexSolid in neighboors:
-            NodeB = np.array([solidInterfaceBuffRcv_X[jVertexSolid], solidInterfaceBuffRcv_Y[jVertexSolid], solidInterfaceBuffRcv_Z[jVertexSolid]])
-            distance = spdist.euclidean(NodeA, NodeB)
-            phi = self.__CPC2(distance, rad)
-            jGlobalVertexSolid = self.__getGlobalIndex('solid', iProc, jVertexSolid)
-            self.MappingMatrixB.setValue(iGlobalVertexFluid, jGlobalVertexSolid, phi)
-            self.MappingMatrixB_T.setValue(jGlobalVertexSolid, iGlobalVertexFluid, phi)
-          self.MappingMatrixB.setValue(iGlobalVertexFluid, nSolidNodes, 1.0)
-          self.MappingMatrixB.setValue(iGlobalVertexFluid, nSolidNodes+1, posX)
-          self.MappingMatrixB.setValue(iGlobalVertexFluid, nSolidNodes+2, posY)
-          if self.nDim == 3:
-            self.MappingMatrixB.setValue(iGlobalVertexFluid, nSolidNodes+3, posZ)
-          self.MappingMatrixB_T.setValue(nSolidNodes, iGlobalVertexFluid, 1.0)
-          self.MappingMatrixB_T.setValue(nSolidNodes+1, iGlobalVertexFluid, posX)
-          self.MappingMatrixB_T.setValue(nSolidNodes+2, iGlobalVertexFluid, posY)
-          if self.nDim == 3:
-            self.MappingMatrixB_T.setValue(nSolidNodes+3, iGlobalVertexFluid, posZ)
-
-    def TPSMeshMapping_A(self, solidInterfaceBuffRcv_X, solidInterfaceBuffRcv_Y, solidInterfaceBuffRcv_Z, iProc):
+            posX = self.localFluidInterface_array_X_init[iVertexFluid]
+            posY = self.localFluidInterface_array_Y_init[iVertexFluid]
+            posZ = self.localFluidInterface_array_Z_init[iVertexFluid]
+            NodeA = np.array([posX, posY, posZ])
+            iGlobalVertexFluid = self.__getGlobalIndex("fluid", myid, iVertexFluid)
+            if self.nDim == 2:
+                neighboors = list(
+                    SolidSpatialTree.intersection(
+                        (posX - rad, posY - rad, posX + rad, posY + rad)
+                    )
+                )
+            elif self.nDim == 3:
+                neighboors = list(
+                    SolidSpatialTree.intersection(
+                        (
+                            posX - rad,
+                            posY - rad,
+                            posZ - rad,
+                            posX + rad,
+                            posY + rad,
+                            posZ + rad,
+                        )
+                    )
+                )
+            for jVertexSolid in neighboors:
+                NodeB = np.array(
+                    [
+                        solidInterfaceBuffRcv_X[jVertexSolid],
+                        solidInterfaceBuffRcv_Y[jVertexSolid],
+                        solidInterfaceBuffRcv_Z[jVertexSolid],
+                    ]
+                )
+                distance = spdist.euclidean(NodeA, NodeB)
+                phi = self.__CPC2(distance, rad)
+                jGlobalVertexSolid = self.__getGlobalIndex("solid", iProc, jVertexSolid)
+                self.MappingMatrixB.setValue(
+                    iGlobalVertexFluid, jGlobalVertexSolid, phi
+                )
+                self.MappingMatrixB_T.setValue(
+                    jGlobalVertexSolid, iGlobalVertexFluid, phi
+                )
+            self.MappingMatrixB.setValue(iGlobalVertexFluid, nSolidNodes, 1.0)
+            self.MappingMatrixB.setValue(iGlobalVertexFluid, nSolidNodes + 1, posX)
+            self.MappingMatrixB.setValue(iGlobalVertexFluid, nSolidNodes + 2, posY)
+            if self.nDim == 3:
+                self.MappingMatrixB.setValue(iGlobalVertexFluid, nSolidNodes + 3, posZ)
+            self.MappingMatrixB_T.setValue(nSolidNodes, iGlobalVertexFluid, 1.0)
+            self.MappingMatrixB_T.setValue(nSolidNodes + 1, iGlobalVertexFluid, posX)
+            self.MappingMatrixB_T.setValue(nSolidNodes + 2, iGlobalVertexFluid, posY)
+            if self.nDim == 3:
+                self.MappingMatrixB_T.setValue(
+                    nSolidNodes + 3, iGlobalVertexFluid, posZ
+                )
+
+    def TPSMeshMapping_A(
+        self,
+        solidInterfaceBuffRcv_X,
+        solidInterfaceBuffRcv_Y,
+        solidInterfaceBuffRcv_Z,
+        iProc,
+    ):
         """
         First part of the RBF mapping. This method provides the matrix required to
         obtain, from the structural displacements, the loadings of the kernel
@@ -992,73 +1422,102 @@ def TPSMeshMapping_A(self, solidInterfaceBuffRcv_X, solidInterfaceBuffRcv_Y, sol
         """
 
         if self.have_MPI:
-          myid = self.comm.Get_rank()
+            myid = self.comm.Get_rank()
         else:
-          myid = 0
+            myid = 0
 
         nSolidNodes = solidInterfaceBuffRcv_X.shape[0]
 
         for iVertexSolid in range(self.nLocalSolidInterfacePhysicalNodes):
-          posX = self.localSolidInterface_array_X_init[iVertexSolid]
-          posY = self.localSolidInterface_array_Y_init[iVertexSolid]
-          posZ = self.localSolidInterface_array_Z_init[iVertexSolid]
-          NodeA = np.array([posX, posY, posZ])
-          iGlobalVertexSolid = self.__getGlobalIndex('solid', myid, iVertexSolid)
-          for jVertexSolid in range(nSolidNodes):
-            NodeB = np.array([solidInterfaceBuffRcv_X[jVertexSolid], solidInterfaceBuffRcv_Y[jVertexSolid], solidInterfaceBuffRcv_Z[jVertexSolid]])
-            distance = spdist.euclidean(NodeA, NodeB)
-            phi = self.__TPS(distance)
-            jGlobalVertexSolid = self.__getGlobalIndex('solid', iProc, jVertexSolid)
-            self.MappingMatrixA.setValue(iGlobalVertexSolid, jGlobalVertexSolid, phi)
-            self.MappingMatrixA_T.setValue(jGlobalVertexSolid, iGlobalVertexSolid, phi)
-          self.MappingMatrixA.setValue(iGlobalVertexSolid, nSolidNodes, 1.0)
-          self.MappingMatrixA.setValue(iGlobalVertexSolid, nSolidNodes+1, posX)
-          self.MappingMatrixA.setValue(iGlobalVertexSolid, nSolidNodes+2, posY)
-          if self.nDim == 3:
-            self.MappingMatrixA.setValue(iGlobalVertexSolid, nSolidNodes+3, posZ)
-          self.MappingMatrixA_T.setValue(nSolidNodes, iGlobalVertexSolid, 1.0)
-          self.MappingMatrixA_T.setValue(nSolidNodes+1, iGlobalVertexSolid, posX)
-          self.MappingMatrixA_T.setValue(nSolidNodes+2, iGlobalVertexSolid, posY)
-          if self.nDim == 3:
-            self.MappingMatrixA_T.setValue(nSolidNodes+3, iGlobalVertexSolid, posZ)
-
-    def TPSMeshMapping_B(self, solidInterfaceBuffRcv_X, solidInterfaceBuffRcv_Y, solidInterfaceBuffRcv_Z, iProc):
+            posX = self.localSolidInterface_array_X_init[iVertexSolid]
+            posY = self.localSolidInterface_array_Y_init[iVertexSolid]
+            posZ = self.localSolidInterface_array_Z_init[iVertexSolid]
+            NodeA = np.array([posX, posY, posZ])
+            iGlobalVertexSolid = self.__getGlobalIndex("solid", myid, iVertexSolid)
+            for jVertexSolid in range(nSolidNodes):
+                NodeB = np.array(
+                    [
+                        solidInterfaceBuffRcv_X[jVertexSolid],
+                        solidInterfaceBuffRcv_Y[jVertexSolid],
+                        solidInterfaceBuffRcv_Z[jVertexSolid],
+                    ]
+                )
+                distance = spdist.euclidean(NodeA, NodeB)
+                phi = self.__TPS(distance)
+                jGlobalVertexSolid = self.__getGlobalIndex("solid", iProc, jVertexSolid)
+                self.MappingMatrixA.setValue(
+                    iGlobalVertexSolid, jGlobalVertexSolid, phi
+                )
+                self.MappingMatrixA_T.setValue(
+                    jGlobalVertexSolid, iGlobalVertexSolid, phi
+                )
+            self.MappingMatrixA.setValue(iGlobalVertexSolid, nSolidNodes, 1.0)
+            self.MappingMatrixA.setValue(iGlobalVertexSolid, nSolidNodes + 1, posX)
+            self.MappingMatrixA.setValue(iGlobalVertexSolid, nSolidNodes + 2, posY)
+            if self.nDim == 3:
+                self.MappingMatrixA.setValue(iGlobalVertexSolid, nSolidNodes + 3, posZ)
+            self.MappingMatrixA_T.setValue(nSolidNodes, iGlobalVertexSolid, 1.0)
+            self.MappingMatrixA_T.setValue(nSolidNodes + 1, iGlobalVertexSolid, posX)
+            self.MappingMatrixA_T.setValue(nSolidNodes + 2, iGlobalVertexSolid, posY)
+            if self.nDim == 3:
+                self.MappingMatrixA_T.setValue(
+                    nSolidNodes + 3, iGlobalVertexSolid, posZ
+                )
+
+    def TPSMeshMapping_B(
+        self,
+        solidInterfaceBuffRcv_X,
+        solidInterfaceBuffRcv_Y,
+        solidInterfaceBuffRcv_Z,
+        iProc,
+    ):
         """
         Second part of the TPS mapping. This method provides the matrix required to
         obtain, from the kernel function loadings, the fluid nodes displacements.
         """
 
         if self.have_MPI:
-          myid = self.comm.Get_rank()
+            myid = self.comm.Get_rank()
         else:
-          myid = 0
+            myid = 0
 
         nSolidNodes = solidInterfaceBuffRcv_X.shape[0]
 
         for iVertexFluid in range(self.nLocalFluidInterfacePhysicalNodes):
-          posX = self.localFluidInterface_array_X_init[iVertexFluid]
-          posY = self.localFluidInterface_array_Y_init[iVertexFluid]
-          posZ = self.localFluidInterface_array_Z_init[iVertexFluid]
-          NodeA = np.array([posX, posY, posZ])
-          iGlobalVertexFluid = self.__getGlobalIndex('fluid', myid, iVertexFluid)
-          for jVertexSolid in range(nSolidNodes):
-            NodeB = np.array([solidInterfaceBuffRcv_X[jVertexSolid], solidInterfaceBuffRcv_Y[jVertexSolid], solidInterfaceBuffRcv_Z[jVertexSolid]])
-            distance = spdist.euclidean(NodeA, NodeB)
-            phi = self.__TPS(distance)
-            jGlobalVertexSolid = self.__getGlobalIndex('solid', iProc, jVertexSolid)
-            self.MappingMatrixB.setValue(iGlobalVertexFluid, jGlobalVertexSolid, phi)
-            self.MappingMatrixB_T.setValue(jGlobalVertexSolid, iGlobalVertexFluid, phi)
-          self.MappingMatrixB.setValue(iGlobalVertexFluid, nSolidNodes, 1.0)
-          self.MappingMatrixB.setValue(iGlobalVertexFluid, nSolidNodes+1, posX)
-          self.MappingMatrixB.setValue(iGlobalVertexFluid, nSolidNodes+2, posY)
-          if self.nDim == 3:
-            self.MappingMatrixB.setValue(iGlobalVertexFluid, nSolidNodes+3, posZ)
-          self.MappingMatrixB_T.setValue(nSolidNodes, iGlobalVertexFluid, 1.0)
-          self.MappingMatrixB_T.setValue(nSolidNodes+1, iGlobalVertexFluid, posX)
-          self.MappingMatrixB_T.setValue(nSolidNodes+2, iGlobalVertexFluid, posY)
-          if self.nDim == 3:
-            self.MappingMatrixB_T.setValue(nSolidNodes+3, iGlobalVertexFluid, posZ)
-
+            posX = self.localFluidInterface_array_X_init[iVertexFluid]
+            posY = self.localFluidInterface_array_Y_init[iVertexFluid]
+            posZ = self.localFluidInterface_array_Z_init[iVertexFluid]
+            NodeA = np.array([posX, posY, posZ])
+            iGlobalVertexFluid = self.__getGlobalIndex("fluid", myid, iVertexFluid)
+            for jVertexSolid in range(nSolidNodes):
+                NodeB = np.array(
+                    [
+                        solidInterfaceBuffRcv_X[jVertexSolid],
+                        solidInterfaceBuffRcv_Y[jVertexSolid],
+                        solidInterfaceBuffRcv_Z[jVertexSolid],
+                    ]
+                )
+                distance = spdist.euclidean(NodeA, NodeB)
+                phi = self.__TPS(distance)
+                jGlobalVertexSolid = self.__getGlobalIndex("solid", iProc, jVertexSolid)
+                self.MappingMatrixB.setValue(
+                    iGlobalVertexFluid, jGlobalVertexSolid, phi
+                )
+                self.MappingMatrixB_T.setValue(
+                    jGlobalVertexSolid, iGlobalVertexFluid, phi
+                )
+            self.MappingMatrixB.setValue(iGlobalVertexFluid, nSolidNodes, 1.0)
+            self.MappingMatrixB.setValue(iGlobalVertexFluid, nSolidNodes + 1, posX)
+            self.MappingMatrixB.setValue(iGlobalVertexFluid, nSolidNodes + 2, posY)
+            if self.nDim == 3:
+                self.MappingMatrixB.setValue(iGlobalVertexFluid, nSolidNodes + 3, posZ)
+            self.MappingMatrixB_T.setValue(nSolidNodes, iGlobalVertexFluid, 1.0)
+            self.MappingMatrixB_T.setValue(nSolidNodes + 1, iGlobalVertexFluid, posX)
+            self.MappingMatrixB_T.setValue(nSolidNodes + 2, iGlobalVertexFluid, posY)
+            if self.nDim == 3:
+                self.MappingMatrixB_T.setValue(
+                    nSolidNodes + 3, iGlobalVertexFluid, posZ
+                )
 
     def __CPC2(self, distance, rad):
         """
@@ -1066,12 +1525,12 @@ def __CPC2(self, distance, rad):
         distance. The kernel function is the one used for RBF.
         """
         phi = 0.0
-        eps = distance/rad
+        eps = distance / rad
 
         if eps < 1:
-          phi = ((1.0-eps)**4)*(4.0*eps+1.0)
+            phi = ((1.0 - eps) ** 4) * (4.0 * eps + 1.0)
         else:
-          phi = 0.0
+            phi = 0.0
 
         return phi
 
@@ -1083,75 +1542,84 @@ def __TPS(self, distance):
         phi = 0.0
 
         if distance > 0.0:
-          phi = (distance**2)*np.log10(distance)
+            phi = (distance**2) * np.log10(distance)
         else:
-          phi = 0.0
+            phi = 0.0
 
         return phi
 
-
     def interpolateSolidPositionOnFluidMesh(self, FSI_config):
         """
         Applies the one-to-one mapping or the interpolaiton rules from solid to fluid mesh.
         """
         if self.have_MPI:
-          myid = self.comm.Get_rank()
-          MPIsize = self.comm.Get_size()
+            myid = self.comm.Get_rank()
+            MPIsize = self.comm.Get_size()
         else:
-          myid = 0
-          MPIsize = 1
-
+            myid = 0
+            MPIsize = 1
 
         # --- Interpolate (or map) in parallel the solid interface displacement on the fluid interface ---
-        if FSI_config['MATCHING_MESH'] == 'NO' and (FSI_config['MESH_INTERP_METHOD'] == 'RBF' or FSI_config['MESH_INTERP_METHOD'] == 'TPS'):
-          if self.have_MPI:
-            gamma_array_DispX = PETSc.Vec().create(self.comm)
-            gamma_array_DispY = PETSc.Vec().create(self.comm)
-            gamma_array_DispZ = PETSc.Vec().create(self.comm)
-            gamma_array_DispX.setType('mpi')
-            gamma_array_DispY.setType('mpi')
-            gamma_array_DispZ.setType('mpi')
-            KSP_solver = PETSc.KSP().create(self.comm)
-          else:
-            gamma_array_DispX = PETSc.Vec().create()
-            gamma_array_DispY = PETSc.Vec().create()
-            gamma_array_DispZ = PETSc.Vec().create()
-            gamma_array_DispX.setType('seq')
-            gamma_array_DispY.setType('seq')
-            gamma_array_DispZ.setType('seq')
-            KSP_solver = PETSc.KSP().create()
-          gamma_array_DispX.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-          gamma_array_DispY.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-          gamma_array_DispZ.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-          gamma_array_DispX.set(0.0)
-          gamma_array_DispY.set(0.0)
-          gamma_array_DispZ.set(0.0)
-          KSP_solver.setType('fgmres')
-          KSP_solver.getPC().setType('jacobi')
-          KSP_solver.setOperators(self.MappingMatrixA)
-          KSP_solver.setFromOptions()
-          KSP_solver.setInitialGuessNonzero(True)
-          KSP_solver.solve(self.solidInterface_array_DispX, gamma_array_DispX)
-          KSP_solver.solve(self.solidInterface_array_DispY, gamma_array_DispY)
-          if self.nDim==3:
-            KSP_solver.solve(self.solidInterface_array_DispZ, gamma_array_DispZ)
-          self.MappingMatrixB.mult(gamma_array_DispX, self.fluidInterface_array_DispX)
-          self.MappingMatrixB.mult(gamma_array_DispY, self.fluidInterface_array_DispY)
-          if self.nDim==3:
-            self.MappingMatrixB.mult(gamma_array_DispZ, self.fluidInterface_array_DispZ)
-          gamma_array_DispX.destroy()
-          gamma_array_DispY.destroy()
-          gamma_array_DispZ.destroy()
-          KSP_solver.destroy()
-          del gamma_array_DispX
-          del gamma_array_DispY
-          del gamma_array_DispZ
-          del KSP_solver
-        else:
-          self.MappingMatrix.mult(self.solidInterface_array_DispX, self.fluidInterface_array_DispX)
-          self.MappingMatrix.mult(self.solidInterface_array_DispY, self.fluidInterface_array_DispY)
-          if self.nDim==3:
-            self.MappingMatrix.mult(self.solidInterface_array_DispZ, self.fluidInterface_array_DispZ)
+        if FSI_config["MATCHING_MESH"] == "NO" and (
+            FSI_config["MESH_INTERP_METHOD"] == "RBF"
+            or FSI_config["MESH_INTERP_METHOD"] == "TPS"
+        ):
+            if self.have_MPI:
+                gamma_array_DispX = PETSc.Vec().create(self.comm)
+                gamma_array_DispY = PETSc.Vec().create(self.comm)
+                gamma_array_DispZ = PETSc.Vec().create(self.comm)
+                gamma_array_DispX.setType("mpi")
+                gamma_array_DispY.setType("mpi")
+                gamma_array_DispZ.setType("mpi")
+                KSP_solver = PETSc.KSP().create(self.comm)
+            else:
+                gamma_array_DispX = PETSc.Vec().create()
+                gamma_array_DispY = PETSc.Vec().create()
+                gamma_array_DispZ = PETSc.Vec().create()
+                gamma_array_DispX.setType("seq")
+                gamma_array_DispY.setType("seq")
+                gamma_array_DispZ.setType("seq")
+                KSP_solver = PETSc.KSP().create()
+            gamma_array_DispX.setSizes(self.nSolidInterfacePhysicalNodes + self.d_RBF)
+            gamma_array_DispY.setSizes(self.nSolidInterfacePhysicalNodes + self.d_RBF)
+            gamma_array_DispZ.setSizes(self.nSolidInterfacePhysicalNodes + self.d_RBF)
+            gamma_array_DispX.set(0.0)
+            gamma_array_DispY.set(0.0)
+            gamma_array_DispZ.set(0.0)
+            KSP_solver.setType("fgmres")
+            KSP_solver.getPC().setType("jacobi")
+            KSP_solver.setOperators(self.MappingMatrixA)
+            KSP_solver.setFromOptions()
+            KSP_solver.setInitialGuessNonzero(True)
+            KSP_solver.solve(self.solidInterface_array_DispX, gamma_array_DispX)
+            KSP_solver.solve(self.solidInterface_array_DispY, gamma_array_DispY)
+            if self.nDim == 3:
+                KSP_solver.solve(self.solidInterface_array_DispZ, gamma_array_DispZ)
+            self.MappingMatrixB.mult(gamma_array_DispX, self.fluidInterface_array_DispX)
+            self.MappingMatrixB.mult(gamma_array_DispY, self.fluidInterface_array_DispY)
+            if self.nDim == 3:
+                self.MappingMatrixB.mult(
+                    gamma_array_DispZ, self.fluidInterface_array_DispZ
+                )
+            gamma_array_DispX.destroy()
+            gamma_array_DispY.destroy()
+            gamma_array_DispZ.destroy()
+            KSP_solver.destroy()
+            del gamma_array_DispX
+            del gamma_array_DispY
+            del gamma_array_DispZ
+            del KSP_solver
+        else:
+            self.MappingMatrix.mult(
+                self.solidInterface_array_DispX, self.fluidInterface_array_DispX
+            )
+            self.MappingMatrix.mult(
+                self.solidInterface_array_DispY, self.fluidInterface_array_DispY
+            )
+            if self.nDim == 3:
+                self.MappingMatrix.mult(
+                    self.solidInterface_array_DispZ, self.fluidInterface_array_DispZ
+                )
 
         # --- Checking conservation ---
         WSX = self.solidLoads_array_X.dot(self.solidInterface_array_DispX)
@@ -1163,105 +1631,169 @@ def interpolateSolidPositionOnFluidMesh(self, FSI_config):
         WFZ = self.fluidLoads_array_Z.dot(self.fluidInterface_array_DispZ)
 
         self.MPIPrint("Checking f/s interface conservation...")
-        self.MPIPrint('Solid side (Wx, Wy, Wz) = ({}, {}, {})'.format(WSX, WSY, WSZ))
-        self.MPIPrint('Fluid side (Wx, Wy, Wz) = ({}, {}, {})'.format(WFX, WFY, WFZ))
-
+        self.MPIPrint("Solid side (Wx, Wy, Wz) = ({}, {}, {})".format(WSX, WSY, WSZ))
+        self.MPIPrint("Fluid side (Wx, Wy, Wz) = ({}, {}, {})".format(WFX, WFY, WFZ))
 
         # --- Redistribute the interpolated fluid interface according to the partitions that own the fluid interface ---
         # Gather the fluid interface on the master process
         # This is required because PETSc redistributes evenly in the cores, and does not use the same division
         # of SU2, thus we need to redistribute
         if self.have_MPI:
-          sendBuff_X = None
-          sendBuff_Y = None
-          sendBuff_Z = None
-          self.fluidInterface_array_DispX_recon = None
-          self.fluidInterface_array_DispY_recon = None
-          self.fluidInterface_array_DispZ_recon = None
-
-          if myid == self.rootProcess:
-            self.fluidInterface_array_DispX_recon = np.zeros(self.nFluidInterfacePhysicalNodes)
-            self.fluidInterface_array_DispY_recon = np.zeros(self.nFluidInterfacePhysicalNodes)
-            self.fluidInterface_array_DispZ_recon = np.zeros(self.nFluidInterfacePhysicalNodes)
-
-          myNumberOfNodes = self.fluidInterface_array_DispX.getArray().shape[0]
-          sendBuffNumber = np.array([myNumberOfNodes], dtype=int)
-          rcvBuffNumber = np.zeros(MPIsize, dtype=int)
-          self.comm.Allgather(sendBuffNumber, rcvBuffNumber)
-
-          counts = tuple(rcvBuffNumber)
-          displ = np.zeros(MPIsize, dtype=int)
-          for ii in range(rcvBuffNumber.shape[0]):
-            displ[ii] = rcvBuffNumber[0:ii].sum()
-          displ = tuple(displ)
-
-          del sendBuffNumber, rcvBuffNumber
-
-          self.comm.Gatherv(self.fluidInterface_array_DispX.getArray(), [self.fluidInterface_array_DispX_recon, counts, displ, self.MPI.DOUBLE], root=self.rootProcess)
-          self.comm.Gatherv(self.fluidInterface_array_DispY.getArray(), [self.fluidInterface_array_DispY_recon, counts, displ, self.MPI.DOUBLE], root=self.rootProcess)
-          self.comm.Gatherv(self.fluidInterface_array_DispZ.getArray(), [self.fluidInterface_array_DispZ_recon, counts, displ, self.MPI.DOUBLE], root=self.rootProcess)
-
-          # Send the partitioned interface to the right fluid partitions
-          if myid == self.rootProcess:
-            for iProc in self.fluidInterfaceProcessors:
-              sendBuff_X = np.empty(self.fluidPhysicalInterfaceNodesDistribution[iProc], dtype=np.float64)
-              sendBuff_Y = np.empty(self.fluidPhysicalInterfaceNodesDistribution[iProc], dtype=np.float64)
-              sendBuff_Z = np.empty(self.fluidPhysicalInterfaceNodesDistribution[iProc], dtype=np.float64)
-              globalIndex = self.__getGlobalIndex('fluid', iProc, 0)
-              for iVertex in range(self.fluidPhysicalInterfaceNodesDistribution[iProc]):
-                sendBuff_X[iVertex] = self.fluidInterface_array_DispX_recon[globalIndex]
-                sendBuff_Y[iVertex] = self.fluidInterface_array_DispY_recon[globalIndex]
-                sendBuff_Z[iVertex] = self.fluidInterface_array_DispZ_recon[globalIndex]
-                globalIndex += 1
-              if iProc == self.rootProcess:
-                self.localFluidInterface_array_DispX = np.copy(sendBuff_X)
-                self.localFluidInterface_array_DispY = np.copy(sendBuff_Y)
-                self.localFluidInterface_array_DispZ = np.copy(sendBuff_Z)
-              else:
-                self.comm.Send(sendBuff_X, dest=iProc, tag = 1)
-                self.comm.Send(sendBuff_Y, dest=iProc, tag = 2)
-                self.comm.Send(sendBuff_Z, dest=iProc, tag = 3)
-          if myid in self.fluidInterfaceProcessors:
-              if myid != self.rootProcess:
-                self.localFluidInterface_array_DispX = np.empty(self.nLocalFluidInterfacePhysicalNodes, dtype=np.float64)
-                self.localFluidInterface_array_DispY = np.empty(self.nLocalFluidInterfacePhysicalNodes, dtype=np.float64)
-                self.localFluidInterface_array_DispZ = np.empty(self.nLocalFluidInterfacePhysicalNodes, dtype=np.float64)
-                self.comm.Recv(self.localFluidInterface_array_DispX, source=self.rootProcess, tag = 1)
-                self.comm.Recv(self.localFluidInterface_array_DispY, source=self.rootProcess, tag = 2)
-                self.comm.Recv(self.localFluidInterface_array_DispZ, source=self.rootProcess, tag = 3)
-          del sendBuff_X
-          del sendBuff_Y
-          del sendBuff_Z
-          self.comm.barrier()
-        else:
-          self.localFluidInterface_array_DispX = self.fluidInterface_array_DispX.getArray().copy()
-          self.localFluidInterface_array_DispY = self.fluidInterface_array_DispY.getArray().copy()
-          self.localFluidInterface_array_DispZ = self.fluidInterface_array_DispZ.getArray().copy()
+            sendBuff_X = None
+            sendBuff_Y = None
+            sendBuff_Z = None
+            self.fluidInterface_array_DispX_recon = None
+            self.fluidInterface_array_DispY_recon = None
+            self.fluidInterface_array_DispZ_recon = None
+
+            if myid == self.rootProcess:
+                self.fluidInterface_array_DispX_recon = np.zeros(
+                    self.nFluidInterfacePhysicalNodes
+                )
+                self.fluidInterface_array_DispY_recon = np.zeros(
+                    self.nFluidInterfacePhysicalNodes
+                )
+                self.fluidInterface_array_DispZ_recon = np.zeros(
+                    self.nFluidInterfacePhysicalNodes
+                )
+
+            myNumberOfNodes = self.fluidInterface_array_DispX.getArray().shape[0]
+            sendBuffNumber = np.array([myNumberOfNodes], dtype=int)
+            rcvBuffNumber = np.zeros(MPIsize, dtype=int)
+            self.comm.Allgather(sendBuffNumber, rcvBuffNumber)
+
+            counts = tuple(rcvBuffNumber)
+            displ = np.zeros(MPIsize, dtype=int)
+            for ii in range(rcvBuffNumber.shape[0]):
+                displ[ii] = rcvBuffNumber[0:ii].sum()
+            displ = tuple(displ)
+
+            del sendBuffNumber, rcvBuffNumber
+
+            self.comm.Gatherv(
+                self.fluidInterface_array_DispX.getArray(),
+                [self.fluidInterface_array_DispX_recon, counts, displ, self.MPI.DOUBLE],
+                root=self.rootProcess,
+            )
+            self.comm.Gatherv(
+                self.fluidInterface_array_DispY.getArray(),
+                [self.fluidInterface_array_DispY_recon, counts, displ, self.MPI.DOUBLE],
+                root=self.rootProcess,
+            )
+            self.comm.Gatherv(
+                self.fluidInterface_array_DispZ.getArray(),
+                [self.fluidInterface_array_DispZ_recon, counts, displ, self.MPI.DOUBLE],
+                root=self.rootProcess,
+            )
+
+            # Send the partitioned interface to the right fluid partitions
+            if myid == self.rootProcess:
+                for iProc in self.fluidInterfaceProcessors:
+                    sendBuff_X = np.empty(
+                        self.fluidPhysicalInterfaceNodesDistribution[iProc],
+                        dtype=np.float64,
+                    )
+                    sendBuff_Y = np.empty(
+                        self.fluidPhysicalInterfaceNodesDistribution[iProc],
+                        dtype=np.float64,
+                    )
+                    sendBuff_Z = np.empty(
+                        self.fluidPhysicalInterfaceNodesDistribution[iProc],
+                        dtype=np.float64,
+                    )
+                    globalIndex = self.__getGlobalIndex("fluid", iProc, 0)
+                    for iVertex in range(
+                        self.fluidPhysicalInterfaceNodesDistribution[iProc]
+                    ):
+                        sendBuff_X[iVertex] = self.fluidInterface_array_DispX_recon[
+                            globalIndex
+                        ]
+                        sendBuff_Y[iVertex] = self.fluidInterface_array_DispY_recon[
+                            globalIndex
+                        ]
+                        sendBuff_Z[iVertex] = self.fluidInterface_array_DispZ_recon[
+                            globalIndex
+                        ]
+                        globalIndex += 1
+                    if iProc == self.rootProcess:
+                        self.localFluidInterface_array_DispX = np.copy(sendBuff_X)
+                        self.localFluidInterface_array_DispY = np.copy(sendBuff_Y)
+                        self.localFluidInterface_array_DispZ = np.copy(sendBuff_Z)
+                    else:
+                        self.comm.Send(sendBuff_X, dest=iProc, tag=1)
+                        self.comm.Send(sendBuff_Y, dest=iProc, tag=2)
+                        self.comm.Send(sendBuff_Z, dest=iProc, tag=3)
+            if myid in self.fluidInterfaceProcessors:
+                if myid != self.rootProcess:
+                    self.localFluidInterface_array_DispX = np.empty(
+                        self.nLocalFluidInterfacePhysicalNodes, dtype=np.float64
+                    )
+                    self.localFluidInterface_array_DispY = np.empty(
+                        self.nLocalFluidInterfacePhysicalNodes, dtype=np.float64
+                    )
+                    self.localFluidInterface_array_DispZ = np.empty(
+                        self.nLocalFluidInterfacePhysicalNodes, dtype=np.float64
+                    )
+                    self.comm.Recv(
+                        self.localFluidInterface_array_DispX,
+                        source=self.rootProcess,
+                        tag=1,
+                    )
+                    self.comm.Recv(
+                        self.localFluidInterface_array_DispY,
+                        source=self.rootProcess,
+                        tag=2,
+                    )
+                    self.comm.Recv(
+                        self.localFluidInterface_array_DispZ,
+                        source=self.rootProcess,
+                        tag=3,
+                    )
+            del sendBuff_X
+            del sendBuff_Y
+            del sendBuff_Z
+            self.comm.barrier()
+        else:
+            self.localFluidInterface_array_DispX = (
+                self.fluidInterface_array_DispX.getArray().copy()
+            )
+            self.localFluidInterface_array_DispY = (
+                self.fluidInterface_array_DispY.getArray().copy()
+            )
+            self.localFluidInterface_array_DispZ = (
+                self.fluidInterface_array_DispZ.getArray().copy()
+            )
 
         # Special treatment for the halo nodes on the fluid interface
         self.haloNodesDisplacements = {}
         sendBuff = {}
         if self.have_MPI:
-          if myid == self.rootProcess:
-            for iProc in self.fluidInterfaceProcessors:
-              sendBuff = {}
-              for key in self.FluidHaloNodeList[iProc].keys():                  # The keys are the SU2 global IDs of the interface nodes
-                globalIndex = self.fluidIndexing[key]                           # These are the interface global IDs, not the SU2 global IDs
-                DispX = self.fluidInterface_array_DispX_recon[globalIndex]
-                DispY = self.fluidInterface_array_DispY_recon[globalIndex]
-                DispZ = self.fluidInterface_array_DispZ_recon[globalIndex]
-                sendBuff[key] = (DispX, DispY, DispZ)
-              if iProc == self.rootProcess:
-                self.haloNodesDisplacements = sendBuff
-              else:
-                self.comm.send(sendBuff, dest = iProc, tag=4)
-          if myid in self.fluidInterfaceProcessors:
-            if myid != self.rootProcess:
-              self.haloNodesDisplacements = self.comm.recv(source = self.rootProcess, tag = 4)
-          self.comm.barrier()
-          del self.fluidInterface_array_DispX_recon
-          del self.fluidInterface_array_DispY_recon
-          del self.fluidInterface_array_DispZ_recon
+            if myid == self.rootProcess:
+                for iProc in self.fluidInterfaceProcessors:
+                    sendBuff = {}
+                    for key in self.FluidHaloNodeList[
+                        iProc
+                    ].keys():  # The keys are the SU2 global IDs of the interface nodes
+                        globalIndex = self.fluidIndexing[
+                            key
+                        ]  # These are the interface global IDs, not the SU2 global IDs
+                        DispX = self.fluidInterface_array_DispX_recon[globalIndex]
+                        DispY = self.fluidInterface_array_DispY_recon[globalIndex]
+                        DispZ = self.fluidInterface_array_DispZ_recon[globalIndex]
+                        sendBuff[key] = (DispX, DispY, DispZ)
+                    if iProc == self.rootProcess:
+                        self.haloNodesDisplacements = sendBuff
+                    else:
+                        self.comm.send(sendBuff, dest=iProc, tag=4)
+            if myid in self.fluidInterfaceProcessors:
+                if myid != self.rootProcess:
+                    self.haloNodesDisplacements = self.comm.recv(
+                        source=self.rootProcess, tag=4
+                    )
+            self.comm.barrier()
+            del self.fluidInterface_array_DispX_recon
+            del self.fluidInterface_array_DispY_recon
+            del self.fluidInterface_array_DispZ_recon
         del sendBuff
 
     def interpolateFluidLoadsOnSolidMesh(self, FSI_config):
@@ -1269,154 +1801,200 @@ def interpolateFluidLoadsOnSolidMesh(self, FSI_config):
         Applies the one-to-one mapping or the interpolaiton rules from fluid to solid mesh.
         """
         if self.have_MPI:
-          myid = self.comm.Get_rank()
-          MPIsize = self.comm.Get_size()
+            myid = self.comm.Get_rank()
+            MPIsize = self.comm.Get_size()
         else:
-          myid = 0
-          MPIsize = 1
+            myid = 0
+            MPIsize = 1
 
         # --- Interpolate (or map) in parallel the fluid interface loads on the solid interface ---
-        #self.MappingMatrix.transpose()
-        if FSI_config['MATCHING_MESH'] == 'NO' and (FSI_config['MESH_INTERP_METHOD'] == 'RBF' or FSI_config['MESH_INTERP_METHOD'] == 'TPS'):
-          if self.have_MPI:
-            gamma_array_LoadX = PETSc.Vec().create(self.comm)
-            gamma_array_LoadY = PETSc.Vec().create(self.comm)
-            gamma_array_LoadZ = PETSc.Vec().create(self.comm)
-            gamma_array_LoadX.setType('mpi')
-            gamma_array_LoadY.setType('mpi')
-            gamma_array_LoadZ.setType('mpi')
-            KSP_solver = PETSc.KSP().create(self.comm)
-          else:
-            gamma_array_LoadX = PETSc.Vec().create()
-            gamma_array_LoadY = PETSc.Vec().create()
-            gamma_array_LoadZ = PETSc.Vec().create()
-            gamma_array_LoadX.setType('seq')
-            gamma_array_LoadY.setType('seq')
-            gamma_array_LoadZ.setType('seq')
-            KSP_solver = PETSc.KSP().create()
-          gamma_array_LoadX.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-          gamma_array_LoadY.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-          gamma_array_LoadZ.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-          gamma_array_LoadX.set(0.0)
-          gamma_array_LoadY.set(0.0)
-          gamma_array_LoadZ.set(0.0)
-          KSP_solver.setType('fgmres')
-          KSP_solver.getPC().setType('jacobi')
-          KSP_solver.setOperators(self.MappingMatrixA_T)
-          KSP_solver.setFromOptions()
-          self.MappingMatrixB_T.mult(self.fluidLoads_array_X, gamma_array_LoadX)
-          self.MappingMatrixB_T.mult(self.fluidLoads_array_Y, gamma_array_LoadY)
-          if self.nDim==3:
-            self.MappingMatrixB_T.mult(self.fluidLoads_array_Z, gamma_array_LoadZ)
-          KSP_solver.solve(gamma_array_LoadX, self.solidLoads_array_X)
-          KSP_solver.solve(gamma_array_LoadY, self.solidLoads_array_Y)
-          if self.nDim==3:
-            KSP_solver.solve(gamma_array_LoadZ, self.solidLoads_array_Z)
-          gamma_array_LoadX.destroy()
-          gamma_array_LoadY.destroy()
-          gamma_array_LoadZ.destroy()
-          KSP_solver.destroy()
-          del gamma_array_LoadX
-          del gamma_array_LoadY
-          del gamma_array_LoadZ
-          del KSP_solver
-        else:
-          self.MappingMatrix_T.mult(self.fluidLoads_array_X, self.solidLoads_array_X)
-          self.MappingMatrix_T.mult(self.fluidLoads_array_Y, self.solidLoads_array_Y)
-          if self.nDim==3:
-            self.MappingMatrix_T.mult(self.fluidLoads_array_Z, self.solidLoads_array_Z)
+        # self.MappingMatrix.transpose()
+        if FSI_config["MATCHING_MESH"] == "NO" and (
+            FSI_config["MESH_INTERP_METHOD"] == "RBF"
+            or FSI_config["MESH_INTERP_METHOD"] == "TPS"
+        ):
+            if self.have_MPI:
+                gamma_array_LoadX = PETSc.Vec().create(self.comm)
+                gamma_array_LoadY = PETSc.Vec().create(self.comm)
+                gamma_array_LoadZ = PETSc.Vec().create(self.comm)
+                gamma_array_LoadX.setType("mpi")
+                gamma_array_LoadY.setType("mpi")
+                gamma_array_LoadZ.setType("mpi")
+                KSP_solver = PETSc.KSP().create(self.comm)
+            else:
+                gamma_array_LoadX = PETSc.Vec().create()
+                gamma_array_LoadY = PETSc.Vec().create()
+                gamma_array_LoadZ = PETSc.Vec().create()
+                gamma_array_LoadX.setType("seq")
+                gamma_array_LoadY.setType("seq")
+                gamma_array_LoadZ.setType("seq")
+                KSP_solver = PETSc.KSP().create()
+            gamma_array_LoadX.setSizes(self.nSolidInterfacePhysicalNodes + self.d_RBF)
+            gamma_array_LoadY.setSizes(self.nSolidInterfacePhysicalNodes + self.d_RBF)
+            gamma_array_LoadZ.setSizes(self.nSolidInterfacePhysicalNodes + self.d_RBF)
+            gamma_array_LoadX.set(0.0)
+            gamma_array_LoadY.set(0.0)
+            gamma_array_LoadZ.set(0.0)
+            KSP_solver.setType("fgmres")
+            KSP_solver.getPC().setType("jacobi")
+            KSP_solver.setOperators(self.MappingMatrixA_T)
+            KSP_solver.setFromOptions()
+            self.MappingMatrixB_T.mult(self.fluidLoads_array_X, gamma_array_LoadX)
+            self.MappingMatrixB_T.mult(self.fluidLoads_array_Y, gamma_array_LoadY)
+            if self.nDim == 3:
+                self.MappingMatrixB_T.mult(self.fluidLoads_array_Z, gamma_array_LoadZ)
+            KSP_solver.solve(gamma_array_LoadX, self.solidLoads_array_X)
+            KSP_solver.solve(gamma_array_LoadY, self.solidLoads_array_Y)
+            if self.nDim == 3:
+                KSP_solver.solve(gamma_array_LoadZ, self.solidLoads_array_Z)
+            gamma_array_LoadX.destroy()
+            gamma_array_LoadY.destroy()
+            gamma_array_LoadZ.destroy()
+            KSP_solver.destroy()
+            del gamma_array_LoadX
+            del gamma_array_LoadY
+            del gamma_array_LoadZ
+            del KSP_solver
+        else:
+            self.MappingMatrix_T.mult(self.fluidLoads_array_X, self.solidLoads_array_X)
+            self.MappingMatrix_T.mult(self.fluidLoads_array_Y, self.solidLoads_array_Y)
+            if self.nDim == 3:
+                self.MappingMatrix_T.mult(
+                    self.fluidLoads_array_Z, self.solidLoads_array_Z
+                )
 
         # --- Redistribute the interpolated solid loads according to the partitions that own the solid interface ---
         # Gather the solid loads on the master process
         if self.have_MPI:
-          sendBuff_X = None
-          sendBuff_Y = None
-          sendBuff_Z = None
-          self.solidLoads_array_X_recon = None
-          self.solidLoads_array_Y_recon = None
-          self.solidLoads_array_Z_recon = None
-          if myid == self.rootProcess:
-            self.solidLoads_array_X_recon = np.zeros(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-            self.solidLoads_array_Y_recon = np.zeros(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-            self.solidLoads_array_Z_recon = np.zeros(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-          myNumberOfNodes =  self.solidLoads_array_X.getArray().shape[0]
-          sendBuffNumber = np.array([myNumberOfNodes], dtype=int)
-          rcvBuffNumber = np.zeros(MPIsize, dtype=int)
-          self.comm.Allgather(sendBuffNumber, rcvBuffNumber)
-
-          counts = tuple(rcvBuffNumber)
-          displ = np.zeros(MPIsize, dtype=int)
-          for ii in range(rcvBuffNumber.shape[0]):
-            displ[ii] = rcvBuffNumber[0:ii].sum()
-          displ = tuple(displ)
-
-          del sendBuffNumber, rcvBuffNumber
-
-          self.comm.Gatherv(self.solidLoads_array_X.getArray(), [self.solidLoads_array_X_recon, counts, displ, self.MPI.DOUBLE], root=self.rootProcess)
-          self.comm.Gatherv(self.solidLoads_array_Y.getArray(), [self.solidLoads_array_Y_recon, counts, displ, self.MPI.DOUBLE], root=self.rootProcess)
-          self.comm.Gatherv(self.solidLoads_array_Z.getArray(), [self.solidLoads_array_Z_recon, counts, displ, self.MPI.DOUBLE], root=self.rootProcess)
-
-          # Send the partitioned loads to the right solid partitions
-          if myid == self.rootProcess:
-            for iProc in self.solidInterfaceProcessors:
-              sendBuff_X = np.empty(self.solidPhysicalInterfaceNodesDistribution[iProc], dtype=np.float64)
-              sendBuff_Y = np.empty(self.solidPhysicalInterfaceNodesDistribution[iProc], dtype=np.float64)
-              sendBuff_Z = np.empty(self.solidPhysicalInterfaceNodesDistribution[iProc], dtype=np.float64)
-              globalIndex = self.__getGlobalIndex('solid', iProc, 0)
-              for iVertex in range(self.solidPhysicalInterfaceNodesDistribution[iProc]):
-                sendBuff_X[iVertex] = self.solidLoads_array_X_recon[globalIndex]
-                sendBuff_Y[iVertex] = self.solidLoads_array_Y_recon[globalIndex]
-                sendBuff_Z[iVertex] = self.solidLoads_array_Z_recon[globalIndex]
-                globalIndex += 1
-              if iProc != myid:
-                self.comm.Send(sendBuff_X, dest=iProc, tag = 1)
-                self.comm.Send(sendBuff_Y, dest=iProc, tag = 2)
-                self.comm.Send(sendBuff_Z, dest=iProc, tag = 3)
-              else:
-                self.localSolidLoads_array_X = np.copy(sendBuff_X)
-                self.localSolidLoads_array_Y = np.copy(sendBuff_Y)
-                self.localSolidLoads_array_Z = np.copy(sendBuff_Z)
-          if myid in self.solidInterfaceProcessors:
-            if myid != self.rootProcess:
-              self.localSolidLoads_array_X = np.empty(self.nLocalSolidInterfacePhysicalNodes, dtype=np.float64)
-              self.localSolidLoads_array_Y = np.empty(self.nLocalSolidInterfacePhysicalNodes, dtype=np.float64)
-              self.localSolidLoads_array_Z = np.empty(self.nLocalSolidInterfacePhysicalNodes, dtype=np.float64)
-              self.comm.Recv(self.localSolidLoads_array_X, source=self.rootProcess, tag = 1)
-              self.comm.Recv(self.localSolidLoads_array_Y, source=self.rootProcess, tag = 2)
-              self.comm.Recv(self.localSolidLoads_array_Z, source=self.rootProcess, tag = 3)
-          del sendBuff_X
-          del sendBuff_Y
-          del sendBuff_Z
-          self.comm.barrier()
-        else:
-          self.localSolidLoads_array_X = self.solidLoads_array_X.getArray().copy()
-          self.localSolidLoads_array_Y = self.solidLoads_array_Y.getArray().copy()
-          self.localSolidLoads_array_Z = self.solidLoads_array_Z.getArray().copy()
+            sendBuff_X = None
+            sendBuff_Y = None
+            sendBuff_Z = None
+            self.solidLoads_array_X_recon = None
+            self.solidLoads_array_Y_recon = None
+            self.solidLoads_array_Z_recon = None
+            if myid == self.rootProcess:
+                self.solidLoads_array_X_recon = np.zeros(
+                    self.nSolidInterfacePhysicalNodes + self.d_RBF
+                )
+                self.solidLoads_array_Y_recon = np.zeros(
+                    self.nSolidInterfacePhysicalNodes + self.d_RBF
+                )
+                self.solidLoads_array_Z_recon = np.zeros(
+                    self.nSolidInterfacePhysicalNodes + self.d_RBF
+                )
+            myNumberOfNodes = self.solidLoads_array_X.getArray().shape[0]
+            sendBuffNumber = np.array([myNumberOfNodes], dtype=int)
+            rcvBuffNumber = np.zeros(MPIsize, dtype=int)
+            self.comm.Allgather(sendBuffNumber, rcvBuffNumber)
+
+            counts = tuple(rcvBuffNumber)
+            displ = np.zeros(MPIsize, dtype=int)
+            for ii in range(rcvBuffNumber.shape[0]):
+                displ[ii] = rcvBuffNumber[0:ii].sum()
+            displ = tuple(displ)
+
+            del sendBuffNumber, rcvBuffNumber
+
+            self.comm.Gatherv(
+                self.solidLoads_array_X.getArray(),
+                [self.solidLoads_array_X_recon, counts, displ, self.MPI.DOUBLE],
+                root=self.rootProcess,
+            )
+            self.comm.Gatherv(
+                self.solidLoads_array_Y.getArray(),
+                [self.solidLoads_array_Y_recon, counts, displ, self.MPI.DOUBLE],
+                root=self.rootProcess,
+            )
+            self.comm.Gatherv(
+                self.solidLoads_array_Z.getArray(),
+                [self.solidLoads_array_Z_recon, counts, displ, self.MPI.DOUBLE],
+                root=self.rootProcess,
+            )
+
+            # Send the partitioned loads to the right solid partitions
+            if myid == self.rootProcess:
+                for iProc in self.solidInterfaceProcessors:
+                    sendBuff_X = np.empty(
+                        self.solidPhysicalInterfaceNodesDistribution[iProc],
+                        dtype=np.float64,
+                    )
+                    sendBuff_Y = np.empty(
+                        self.solidPhysicalInterfaceNodesDistribution[iProc],
+                        dtype=np.float64,
+                    )
+                    sendBuff_Z = np.empty(
+                        self.solidPhysicalInterfaceNodesDistribution[iProc],
+                        dtype=np.float64,
+                    )
+                    globalIndex = self.__getGlobalIndex("solid", iProc, 0)
+                    for iVertex in range(
+                        self.solidPhysicalInterfaceNodesDistribution[iProc]
+                    ):
+                        sendBuff_X[iVertex] = self.solidLoads_array_X_recon[globalIndex]
+                        sendBuff_Y[iVertex] = self.solidLoads_array_Y_recon[globalIndex]
+                        sendBuff_Z[iVertex] = self.solidLoads_array_Z_recon[globalIndex]
+                        globalIndex += 1
+                    if iProc != myid:
+                        self.comm.Send(sendBuff_X, dest=iProc, tag=1)
+                        self.comm.Send(sendBuff_Y, dest=iProc, tag=2)
+                        self.comm.Send(sendBuff_Z, dest=iProc, tag=3)
+                    else:
+                        self.localSolidLoads_array_X = np.copy(sendBuff_X)
+                        self.localSolidLoads_array_Y = np.copy(sendBuff_Y)
+                        self.localSolidLoads_array_Z = np.copy(sendBuff_Z)
+            if myid in self.solidInterfaceProcessors:
+                if myid != self.rootProcess:
+                    self.localSolidLoads_array_X = np.empty(
+                        self.nLocalSolidInterfacePhysicalNodes, dtype=np.float64
+                    )
+                    self.localSolidLoads_array_Y = np.empty(
+                        self.nLocalSolidInterfacePhysicalNodes, dtype=np.float64
+                    )
+                    self.localSolidLoads_array_Z = np.empty(
+                        self.nLocalSolidInterfacePhysicalNodes, dtype=np.float64
+                    )
+                    self.comm.Recv(
+                        self.localSolidLoads_array_X, source=self.rootProcess, tag=1
+                    )
+                    self.comm.Recv(
+                        self.localSolidLoads_array_Y, source=self.rootProcess, tag=2
+                    )
+                    self.comm.Recv(
+                        self.localSolidLoads_array_Z, source=self.rootProcess, tag=3
+                    )
+            del sendBuff_X
+            del sendBuff_Y
+            del sendBuff_Z
+            self.comm.barrier()
+        else:
+            self.localSolidLoads_array_X = self.solidLoads_array_X.getArray().copy()
+            self.localSolidLoads_array_Y = self.solidLoads_array_Y.getArray().copy()
+            self.localSolidLoads_array_Z = self.solidLoads_array_Z.getArray().copy()
 
         # Special treatment for the halo nodes on the solid interface
         self.haloNodesLoads = {}
         sendBuff = {}
         if self.have_MPI:
-          if myid == self.rootProcess:
-            for iProc in self.solidInterfaceProcessors:
-              sendBuff = {}
-              for key in self.SolidHaloNodeList[iProc].keys():
-                globalIndex = self.solidIndexing[key]
-                DispX = self.solidLoads_array_X_recon[globalIndex]
-                DispY = self.solidLoads_array_Y_recon[globalIndex]
-                DispZ = self.solidLoads_array_Z_recon[globalIndex]
-                sendBuff[key] = (DispX, DispY, DispZ)
-              if iProc == self.rootProcess:
-                self.haloNodesLoads = sendBuff
-              else:
-                self.comm.send(sendBuff, dest = iProc, tag=4)
-          if myid in self.solidInterfaceProcessors:
-            if myid != self.rootProcess:
-              self.haloNodesLoads = self.comm.recv(source = self.rootProcess, tag = 4)
-          self.comm.barrier()
-          del self.solidLoads_array_X_recon
-          del self.solidLoads_array_Y_recon
-          del self.solidLoads_array_Z_recon
+            if myid == self.rootProcess:
+                for iProc in self.solidInterfaceProcessors:
+                    sendBuff = {}
+                    for key in self.SolidHaloNodeList[iProc].keys():
+                        globalIndex = self.solidIndexing[key]
+                        DispX = self.solidLoads_array_X_recon[globalIndex]
+                        DispY = self.solidLoads_array_Y_recon[globalIndex]
+                        DispZ = self.solidLoads_array_Z_recon[globalIndex]
+                        sendBuff[key] = (DispX, DispY, DispZ)
+                    if iProc == self.rootProcess:
+                        self.haloNodesLoads = sendBuff
+                    else:
+                        self.comm.send(sendBuff, dest=iProc, tag=4)
+            if myid in self.solidInterfaceProcessors:
+                if myid != self.rootProcess:
+                    self.haloNodesLoads = self.comm.recv(source=self.rootProcess, tag=4)
+            self.comm.barrier()
+            del self.solidLoads_array_X_recon
+            del self.solidLoads_array_Y_recon
+            del self.solidLoads_array_Z_recon
         del sendBuff
 
     def getSolidInterfaceDisplacement(self, SolidSolver):
@@ -1424,22 +2002,26 @@ def getSolidInterfaceDisplacement(self, SolidSolver):
         Gets the current solid interface position from the solid solver.
         """
         if self.have_MPI:
-          myid = self.comm.Get_rank()
+            myid = self.comm.Get_rank()
         else:
-          myid = 0
+            myid = 0
 
         # --- Get the solid interface position from the solid solver and directly fill the corresponding PETSc vector ---
         GlobalIndex = int()
         localIndex = 0
         for iVertex in range(self.nLocalSolidInterfaceNodes):
-          GlobalIndex = SolidSolver.getVertexGlobalIndex(self.solidInterfaceIdentifier, iVertex)
-          if GlobalIndex not in self.SolidHaloNodeList[myid].keys():
-            newDispx, newDispy, newDispz = SolidSolver.getInterfaceNodeDisp(self.solidInterfaceIdentifier, iVertex)
-            iGlobalVertex = self.__getGlobalIndex('solid', myid, localIndex)
-            self.solidInterface_array_DispX.setValues([iGlobalVertex],newDispx)
-            self.solidInterface_array_DispY.setValues([iGlobalVertex],newDispy)
-            self.solidInterface_array_DispZ.setValues([iGlobalVertex],newDispz)
-            localIndex += 1
+            GlobalIndex = SolidSolver.getVertexGlobalIndex(
+                self.solidInterfaceIdentifier, iVertex
+            )
+            if GlobalIndex not in self.SolidHaloNodeList[myid].keys():
+                newDispx, newDispy, newDispz = SolidSolver.getInterfaceNodeDisp(
+                    self.solidInterfaceIdentifier, iVertex
+                )
+                iGlobalVertex = self.__getGlobalIndex("solid", myid, localIndex)
+                self.solidInterface_array_DispX.setValues([iGlobalVertex], newDispx)
+                self.solidInterface_array_DispY.setValues([iGlobalVertex], newDispy)
+                self.solidInterface_array_DispZ.setValues([iGlobalVertex], newDispz)
+                localIndex += 1
 
         self.solidInterface_array_DispX.assemblyBegin()
         self.solidInterface_array_DispX.assemblyEnd()
@@ -1453,23 +2035,27 @@ def getFluidInterfaceNodalForce(self, FSI_config, FluidSolver):
         Gets the fluid interface loads from the fluid solver.
         """
         if self.have_MPI:
-          myid = self.comm.Get_rank()
+            myid = self.comm.Get_rank()
         else:
-          myid = 0
+            myid = 0
 
         GlobalIndex = int()
         localIndex = 0
 
         # --- Get the fluid interface loads from the fluid solver and directly fill the corresponding PETSc vector ---
         for iVertex in range(self.nLocalFluidInterfaceNodes):
-            GlobalIndex = FluidSolver.GetNodeGlobalIndex(FluidSolver.GetMarkerNode(self.fluidInterfaceIdentifier, iVertex))
+            GlobalIndex = FluidSolver.GetNodeGlobalIndex(
+                FluidSolver.GetMarkerNode(self.fluidInterfaceIdentifier, iVertex)
+            )
             if GlobalIndex not in self.FluidHaloNodeList[myid].keys():
-              loadX, loadY, loadZ = FluidSolver.GetFlowLoad(self.fluidInterfaceIdentifier, iVertex)
-              iGlobalVertex = self.__getGlobalIndex('fluid', myid, localIndex)
-              self.fluidLoads_array_X.setValues([iGlobalVertex], loadX)
-              self.fluidLoads_array_Y.setValues([iGlobalVertex], loadY)
-              self.fluidLoads_array_Z.setValues([iGlobalVertex], loadZ)
-              localIndex += 1
+                loadX, loadY, loadZ = FluidSolver.GetFlowLoad(
+                    self.fluidInterfaceIdentifier, iVertex
+                )
+                iGlobalVertex = self.__getGlobalIndex("fluid", myid, localIndex)
+                self.fluidLoads_array_X.setValues([iGlobalVertex], loadX)
+                self.fluidLoads_array_Y.setValues([iGlobalVertex], loadY)
+                self.fluidLoads_array_Z.setValues([iGlobalVertex], loadZ)
+                localIndex += 1
 
         self.fluidLoads_array_X.assemblyBegin()
         self.fluidLoads_array_X.assemblyEnd()
@@ -1478,31 +2064,39 @@ def getFluidInterfaceNodalForce(self, FSI_config, FluidSolver):
         self.fluidLoads_array_Z.assemblyBegin()
         self.fluidLoads_array_Z.assemblyEnd()
 
-
     def setFluidInterfaceVarCoord(self, FluidSolver):
         """
         Communicate the change of coordinates of the fluid interface to the fluid solver.
         Prepare the fluid solver for mesh deformation.
         """
         if self.have_MPI:
-          myid = self.comm.Get_rank()
+            myid = self.comm.Get_rank()
         else:
-          myid = 0
+            myid = 0
 
         # --- Send the new fluid interface position to the fluid solver (on each partition, halo nodes included) ---
         localIndex = 0
         for iVertex in range(self.nLocalFluidInterfaceNodes):
-            GlobalIndex = FluidSolver.GetNodeGlobalIndex(FluidSolver.GetMarkerNode(self.fluidInterfaceIdentifier, iVertex))
+            GlobalIndex = FluidSolver.GetNodeGlobalIndex(
+                FluidSolver.GetMarkerNode(self.fluidInterfaceIdentifier, iVertex)
+            )
             if GlobalIndex in self.FluidHaloNodeList[myid].keys():
-              DispX, DispY, DispZ = self.haloNodesDisplacements[GlobalIndex]
-              FluidSolver.SetMarkerDisplacements(self.fluidInterfaceIdentifier, int(iVertex), np.array([DispX, DispY, DispZ]))
+                DispX, DispY, DispZ = self.haloNodesDisplacements[GlobalIndex]
+                FluidSolver.SetMarkerDisplacements(
+                    self.fluidInterfaceIdentifier,
+                    int(iVertex),
+                    np.array([DispX, DispY, DispZ]),
+                )
             else:
-              DispX = self.localFluidInterface_array_DispX[localIndex]
-              DispY = self.localFluidInterface_array_DispY[localIndex]
-              DispZ = self.localFluidInterface_array_DispZ[localIndex]
-              FluidSolver.SetMarkerDisplacements(self.fluidInterfaceIdentifier, int(iVertex), np.array([DispX, DispY, DispZ]))
-              localIndex += 1
-
+                DispX = self.localFluidInterface_array_DispX[localIndex]
+                DispY = self.localFluidInterface_array_DispY[localIndex]
+                DispZ = self.localFluidInterface_array_DispZ[localIndex]
+                FluidSolver.SetMarkerDisplacements(
+                    self.fluidInterfaceIdentifier,
+                    int(iVertex),
+                    np.array([DispX, DispY, DispZ]),
+                )
+                localIndex += 1
 
     def setSolidInterfaceLoads(self, SolidSolver, FSI_config):
         """
@@ -1510,17 +2104,17 @@ def setSolidInterfaceLoads(self, SolidSolver, FSI_config):
         Calculates the new resultant forces (lift, drag, ...).
         """
         if self.have_MPI:
-          myid = self.comm.Get_rank()
+            myid = self.comm.Get_rank()
         else:
-          myid = 0
+            myid = 0
 
         FX = np.array(0.0, dtype=np.float64)
-        FY = np.array(0.0, dtype=np.float64) # solid-side resultant forces
+        FY = np.array(0.0, dtype=np.float64)  # solid-side resultant forces
         FZ = np.array(0.0, dtype=np.float64)
         FXSendBuff = np.array(0.0, dtype=np.float64)
         FYSendBuff = np.array(0.0, dtype=np.float64)
         FZSendBuff = np.array(0.0, dtype=np.float64)
-        FFX = 0.0 # fluid-side resultant forces
+        FFX = 0.0  # fluid-side resultant forces
         FFY = 0.0
         FFZ = 0.0
 
@@ -1530,40 +2124,42 @@ def setSolidInterfaceLoads(self, SolidSolver, FSI_config):
         FFZ = self.fluidLoads_array_Z.sum()
 
         for iVertex in range(self.nLocalSolidInterfacePhysicalNodes):
-          FXSendBuff += self.localSolidLoads_array_X[iVertex]
-          FYSendBuff += self.localSolidLoads_array_Y[iVertex]
-          FZSendBuff += self.localSolidLoads_array_Z[iVertex]
+            FXSendBuff += self.localSolidLoads_array_X[iVertex]
+            FYSendBuff += self.localSolidLoads_array_Y[iVertex]
+            FZSendBuff += self.localSolidLoads_array_Z[iVertex]
 
         if self.have_MPI:
-          self.comm.Allreduce(FXSendBuff, FX, op=self.MPI.SUM)
-          self.comm.Allreduce(FYSendBuff, FY, op=self.MPI.SUM)
-          self.comm.Allreduce(FZSendBuff, FZ, op=self.MPI.SUM)
+            self.comm.Allreduce(FXSendBuff, FX, op=self.MPI.SUM)
+            self.comm.Allreduce(FYSendBuff, FY, op=self.MPI.SUM)
+            self.comm.Allreduce(FZSendBuff, FZ, op=self.MPI.SUM)
         else:
-          FX = np.copy(FXSendBuff)
-          FY = np.copy(FYSendBuff)
-          FZ = np.copy(FZSendBuff)
+            FX = np.copy(FXSendBuff)
+            FY = np.copy(FYSendBuff)
+            FZ = np.copy(FZSendBuff)
 
         del FXSendBuff
         del FYSendBuff
         del FZSendBuff
 
         self.MPIPrint("Checking f/s interface total force...")
-        self.MPIPrint('Solid side (Fx, Fy, Fz) = ({}, {}, {})'.format(FX, FY, FZ))
-        self.MPIPrint('Fluid side (Fx, Fy, Fz) = ({}, {}, {})'.format(FFX, FFY, FFZ))
+        self.MPIPrint("Solid side (Fx, Fy, Fz) = ({}, {}, {})".format(FX, FY, FZ))
+        self.MPIPrint("Fluid side (Fx, Fy, Fz) = ({}, {}, {})".format(FFX, FFY, FFZ))
 
         # --- Send the new solid interface loads to the solid solver (on each partition, halo nodes included) ---
         GlobalIndex = int()
         localIndex = 0
         for iVertex in range(self.nLocalSolidInterfaceNodes):
-          GlobalIndex = SolidSolver.getVertexGlobalIndex(self.solidInterfaceIdentifier, iVertex)
-          if GlobalIndex in self.SolidHaloNodeList[myid].keys():
-            pass  #TODO here, when the solid solver will run in parallel, we will need to pass the halo loads
-          else:
-            Fx = self.localSolidLoads_array_X[localIndex]
-            Fy = self.localSolidLoads_array_Y[localIndex]
-            Fz = self.localSolidLoads_array_Z[localIndex]
-            SolidSolver.applyload(iVertex, Fx, Fy, Fz)
-            localIndex += 1
+            GlobalIndex = SolidSolver.getVertexGlobalIndex(
+                self.solidInterfaceIdentifier, iVertex
+            )
+            if GlobalIndex in self.SolidHaloNodeList[myid].keys():
+                pass  # TODO here, when the solid solver will run in parallel, we will need to pass the halo loads
+            else:
+                Fx = self.localSolidLoads_array_X[localIndex]
+                Fy = self.localSolidLoads_array_Y[localIndex]
+                Fz = self.localSolidLoads_array_Z[localIndex]
+                SolidSolver.applyload(iVertex, Fx, Fy, Fz)
+                localIndex += 1
 
     def computeSolidInterfaceResidual(self, SolidSolver):
         """
@@ -1571,40 +2167,42 @@ def computeSolidInterfaceResidual(self, SolidSolver):
         """
 
         if self.have_MPI:
-          myid = self.comm.Get_rank()
+            myid = self.comm.Get_rank()
         else:
-          myid = 0
+            myid = 0
 
         normInterfaceResidualSquare = 0.0
 
         # --- Create and fill the PETSc vector for the predicted solid interface position (predicted by the solid computation) ---
         if self.have_MPI:
-          predDisp_array_X = PETSc.Vec().create(self.comm)
-          predDisp_array_X.setType('mpi')
-          predDisp_array_Y = PETSc.Vec().create(self.comm)
-          predDisp_array_Y.setType('mpi')
-          predDisp_array_Z = PETSc.Vec().create(self.comm)
-          predDisp_array_Z.setType('mpi')
-        else:
-          predDisp_array_X = PETSc.Vec().create()
-          predDisp_array_X.setType('seq')
-          predDisp_array_Y = PETSc.Vec().create()
-          predDisp_array_Y.setType('seq')
-          predDisp_array_Z = PETSc.Vec().create()
-          predDisp_array_Z.setType('seq')
-        predDisp_array_X.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-        predDisp_array_Y.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-        predDisp_array_Z.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
+            predDisp_array_X = PETSc.Vec().create(self.comm)
+            predDisp_array_X.setType("mpi")
+            predDisp_array_Y = PETSc.Vec().create(self.comm)
+            predDisp_array_Y.setType("mpi")
+            predDisp_array_Z = PETSc.Vec().create(self.comm)
+            predDisp_array_Z.setType("mpi")
+        else:
+            predDisp_array_X = PETSc.Vec().create()
+            predDisp_array_X.setType("seq")
+            predDisp_array_Y = PETSc.Vec().create()
+            predDisp_array_Y.setType("seq")
+            predDisp_array_Z = PETSc.Vec().create()
+            predDisp_array_Z.setType("seq")
+        predDisp_array_X.setSizes(self.nSolidInterfacePhysicalNodes + self.d_RBF)
+        predDisp_array_Y.setSizes(self.nSolidInterfacePhysicalNodes + self.d_RBF)
+        predDisp_array_Z.setSizes(self.nSolidInterfacePhysicalNodes + self.d_RBF)
         predDisp_array_X.set(0.0)
         predDisp_array_Y.set(0.0)
         predDisp_array_Z.set(0.0)
 
         for iVertex in range(self.nLocalSolidInterfaceNodes):
-          predDispx, predDispy, predDispz = SolidSolver.getInterfaceNodeDisp(self.solidInterfaceIdentifier, iVertex)
-          iGlobalVertex = self.__getGlobalIndex('solid', myid, iVertex)
-          predDisp_array_X.setValues([iGlobalVertex], predDispx)
-          predDisp_array_Y.setValues([iGlobalVertex], predDispy)
-          predDisp_array_Z.setValues([iGlobalVertex], predDispz)
+            predDispx, predDispy, predDispz = SolidSolver.getInterfaceNodeDisp(
+                self.solidInterfaceIdentifier, iVertex
+            )
+            iGlobalVertex = self.__getGlobalIndex("solid", myid, iVertex)
+            predDisp_array_X.setValues([iGlobalVertex], predDispx)
+            predDisp_array_Y.setValues([iGlobalVertex], predDispy)
+            predDisp_array_Z.setValues([iGlobalVertex], predDispz)
 
         predDisp_array_X.assemblyBegin()
         predDisp_array_X.assemblyEnd()
@@ -1614,15 +2212,25 @@ def computeSolidInterfaceResidual(self, SolidSolver):
         predDisp_array_Z.assemblyEnd()
 
         # --- Calculate the residual (vector and norm) ---
-        self.solidInterfaceResidual_array_X = predDisp_array_X - self.solidInterface_array_DispX
-        self.solidInterfaceResidual_array_Y = predDisp_array_Y - self.solidInterface_array_DispY
-        self.solidInterfaceResidual_array_Z = predDisp_array_Z - self.solidInterface_array_DispZ
+        self.solidInterfaceResidual_array_X = (
+            predDisp_array_X - self.solidInterface_array_DispX
+        )
+        self.solidInterfaceResidual_array_Y = (
+            predDisp_array_Y - self.solidInterface_array_DispY
+        )
+        self.solidInterfaceResidual_array_Z = (
+            predDisp_array_Z - self.solidInterface_array_DispZ
+        )
 
         normInterfaceResidual_X = self.solidInterfaceResidual_array_X.norm()
         normInterfaceResidual_Y = self.solidInterfaceResidual_array_Y.norm()
         normInterfaceResidual_Z = self.solidInterfaceResidual_array_Z.norm()
 
-        normInterfaceResidualSquare = normInterfaceResidual_X**2 + normInterfaceResidual_Y**2 + normInterfaceResidual_Z**2
+        normInterfaceResidualSquare = (
+            normInterfaceResidual_X**2
+            + normInterfaceResidual_Y**2
+            + normInterfaceResidual_Z**2
+        )
 
         predDisp_array_X.destroy()
         predDisp_array_Y.destroy()
@@ -1633,30 +2241,37 @@ def computeSolidInterfaceResidual(self, SolidSolver):
 
         return sqrt(normInterfaceResidualSquare)
 
-    def relaxSolidPosition(self,FSI_config):
+    def relaxSolidPosition(self, FSI_config):
         """
         Apply solid displacement under-relaxation.
         """
         if self.have_MPI:
-          myid = self.comm.Get_rank()
+            myid = self.comm.Get_rank()
         else:
-          myid = 0
+            myid = 0
 
         # --- Set the Aitken coefficient for the relaxation ---
-        if FSI_config['AITKEN_RELAX'] == 'STATIC':
-            self.aitkenParam = FSI_config['AITKEN_PARAM']
-        elif FSI_config['AITKEN_RELAX'] == 'DYNAMIC':
+        if FSI_config["AITKEN_RELAX"] == "STATIC":
+            self.aitkenParam = FSI_config["AITKEN_PARAM"]
+        elif FSI_config["AITKEN_RELAX"] == "DYNAMIC":
             self.setAitkenCoefficient(FSI_config)
         else:
             self.aitkenParam = 1.0
 
-        self.MPIPrint('Aitken under-relaxation step with parameter {}'.format(self.aitkenParam))
+        self.MPIPrint(
+            "Aitken under-relaxation step with parameter {}".format(self.aitkenParam)
+        )
 
         # --- Relax the solid interface position ---
-        self.solidInterface_array_DispX += self.aitkenParam*self.solidInterfaceResidual_array_X
-        self.solidInterface_array_DispY += self.aitkenParam*self.solidInterfaceResidual_array_Y
-        self.solidInterface_array_DispZ += self.aitkenParam*self.solidInterfaceResidual_array_Z
-
+        self.solidInterface_array_DispX += (
+            self.aitkenParam * self.solidInterfaceResidual_array_X
+        )
+        self.solidInterface_array_DispY += (
+            self.aitkenParam * self.solidInterfaceResidual_array_Y
+        )
+        self.solidInterface_array_DispZ += (
+            self.aitkenParam * self.solidInterfaceResidual_array_Z
+        )
 
     def setAitkenCoefficient(self, FSI_config):
         """
@@ -1668,22 +2283,22 @@ def setAitkenCoefficient(self, FSI_config):
 
         # --- Create the PETSc vector for the difference between the residuals (current and previous FSI iter) ---
         if self.FSIIter == 0:
-            self.aitkenParam = max(FSI_config['AITKEN_PARAM'], self.aitkenParam)
+            self.aitkenParam = max(FSI_config["AITKEN_PARAM"], self.aitkenParam)
         else:
             if self.have_MPI:
-              deltaResx_array_X = PETSc.Vec().create(self.comm)
-              deltaResx_array_X.setType('mpi')
-              deltaResx_array_Y = PETSc.Vec().create(self.comm)
-              deltaResx_array_Y.setType('mpi')
-              deltaResx_array_Z = PETSc.Vec().create(self.comm)
-              deltaResx_array_Z.setType('mpi')
+                deltaResx_array_X = PETSc.Vec().create(self.comm)
+                deltaResx_array_X.setType("mpi")
+                deltaResx_array_Y = PETSc.Vec().create(self.comm)
+                deltaResx_array_Y.setType("mpi")
+                deltaResx_array_Z = PETSc.Vec().create(self.comm)
+                deltaResx_array_Z.setType("mpi")
             else:
-              deltaResx_array_X = PETSc.Vec().create()
-              deltaResx_array_X.setType('seq')
-              deltaResx_array_Y = PETSc.Vec().create()
-              deltaResx_array_Y.setType('seq')
-              deltaResx_array_Z = PETSc.Vec().create()
-              deltaResx_array_Z.setType('seq')
+                deltaResx_array_X = PETSc.Vec().create()
+                deltaResx_array_X.setType("seq")
+                deltaResx_array_Y = PETSc.Vec().create()
+                deltaResx_array_Y.setType("seq")
+                deltaResx_array_Z = PETSc.Vec().create()
+                deltaResx_array_Z.setType("seq")
             deltaResx_array_X.setSizes(self.nSolidInterfacePhysicalNodes + self.d_RBF)
             deltaResx_array_X.set(0.0)
             deltaResx_array_Y.setSizes(self.nSolidInterfacePhysicalNodes + self.d_RBF)
@@ -1692,21 +2307,38 @@ def setAitkenCoefficient(self, FSI_config):
             deltaResx_array_Z.set(0.0)
 
             # --- Compute the dynamic Aitken coefficient ---
-            deltaResx_array_X = self.solidInterfaceResidual_array_X - self.solidInterfaceResidualnM1_array_X
-            deltaResx_array_Y = self.solidInterfaceResidual_array_Y - self.solidInterfaceResidualnM1_array_Y
-            deltaResx_array_Z = self.solidInterfaceResidual_array_Z - self.solidInterfaceResidualnM1_array_Z
-
-            prodScalRes_X = deltaResx_array_X.dot(self.solidInterfaceResidualnM1_array_X)
-            prodScalRes_Y = deltaResx_array_Y.dot(self.solidInterfaceResidualnM1_array_Y)
-            prodScalRes_Z = deltaResx_array_Z.dot(self.solidInterfaceResidualnM1_array_Z)
+            deltaResx_array_X = (
+                self.solidInterfaceResidual_array_X
+                - self.solidInterfaceResidualnM1_array_X
+            )
+            deltaResx_array_Y = (
+                self.solidInterfaceResidual_array_Y
+                - self.solidInterfaceResidualnM1_array_Y
+            )
+            deltaResx_array_Z = (
+                self.solidInterfaceResidual_array_Z
+                - self.solidInterfaceResidualnM1_array_Z
+            )
+
+            prodScalRes_X = deltaResx_array_X.dot(
+                self.solidInterfaceResidualnM1_array_X
+            )
+            prodScalRes_Y = deltaResx_array_Y.dot(
+                self.solidInterfaceResidualnM1_array_Y
+            )
+            prodScalRes_Z = deltaResx_array_Z.dot(
+                self.solidInterfaceResidualnM1_array_Z
+            )
             prodScalRes = prodScalRes_X + prodScalRes_Y + prodScalRes_Z
 
-            deltaResNormSquare_X = (deltaResx_array_X.norm())**2
-            deltaResNormSquare_Y = (deltaResx_array_Y.norm())**2
-            deltaResNormSquare_Z = (deltaResx_array_Z.norm())**2
-            deltaResNormSquare = deltaResNormSquare_X + deltaResNormSquare_Y + deltaResNormSquare_Z
+            deltaResNormSquare_X = (deltaResx_array_X.norm()) ** 2
+            deltaResNormSquare_Y = (deltaResx_array_Y.norm()) ** 2
+            deltaResNormSquare_Z = (deltaResx_array_Z.norm()) ** 2
+            deltaResNormSquare = (
+                deltaResNormSquare_X + deltaResNormSquare_Y + deltaResNormSquare_Z
+            )
 
-            self.aitkenParam *= -prodScalRes/deltaResNormSquare
+            self.aitkenParam *= -prodScalRes / deltaResNormSquare
 
             deltaResx_array_X.destroy()
             deltaResx_array_Y.destroy()
@@ -1723,21 +2355,21 @@ def setAitkenCoefficient(self, FSI_config):
         self.solidInterfaceResidual_array_Y.copy(self.solidInterfaceResidualnM1_array_Y)
         self.solidInterfaceResidual_array_Z.copy(self.solidInterfaceResidualnM1_array_Z)
 
-    def displacementPredictor(self, FSI_config , SolidSolver, deltaT):
+    def displacementPredictor(self, FSI_config, SolidSolver, deltaT):
         """
         Calculates a prediciton for the solid interface position for the next time step.
         """
 
         if self.have_MPI:
-          myid = self.comm.Get_rank()
+            myid = self.comm.Get_rank()
         else:
-          myid = 0
+            myid = 0
 
-        if FSI_config['DISP_PRED'] == 'FIRST_ORDER':
+        if FSI_config["DISP_PRED"] == "FIRST_ORDER":
             self.MPIPrint("First order predictor")
             alpha_0 = 1.0
             alpha_1 = 0.0
-        elif FSI_config['DISP_PRED'] == 'SECOND_ORDER':
+        elif FSI_config["DISP_PRED"] == "SECOND_ORDER":
             self.MPIPrint("Second order predictor")
             alpha_0 = 1.0
             alpha_1 = 0.5
@@ -1748,61 +2380,66 @@ def displacementPredictor(self, FSI_config , SolidSolver, deltaT):
 
         # --- Create the PETSc vectors to store the solid interface velocity ---
         if self.have_MPI:
-          Vel_array_X = PETSc.Vec().create(self.comm)
-          Vel_array_X.setType('mpi')
-          Vel_array_Y = PETSc.Vec().create(self.comm)
-          Vel_array_Y.setType('mpi')
-          Vel_array_Z = PETSc.Vec().create(self.comm)
-          Vel_array_Z.setType('mpi')
-          VelnM1_array_X = PETSc.Vec().create(self.comm)
-          VelnM1_array_X.setType('mpi')
-          VelnM1_array_Y = PETSc.Vec().create(self.comm)
-          VelnM1_array_Y.setType('mpi')
-          VelnM1_array_Z = PETSc.Vec().create(self.comm)
-          VelnM1_array_Z.setType('mpi')
-        else:
-          Vel_array_X = PETSc.Vec().create()
-          Vel_array_X.setType('seq')
-          Vel_array_Y = PETSc.Vec().create()
-          Vel_array_Y.setType('seq')
-          Vel_array_Z = PETSc.Vec().create()
-          Vel_array_Z.setType('seq')
-          VelnM1_array_X = PETSc.Vec().create()
-          VelnM1_array_X.setType('seq')
-          VelnM1_array_Y = PETSc.Vec().create()
-          VelnM1_array_Y.setType('seq')
-          VelnM1_array_Z = PETSc.Vec().create()
-          VelnM1_array_Z.setType('seq')
-        Vel_array_X.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-        Vel_array_Y.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-        Vel_array_Z.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
+            Vel_array_X = PETSc.Vec().create(self.comm)
+            Vel_array_X.setType("mpi")
+            Vel_array_Y = PETSc.Vec().create(self.comm)
+            Vel_array_Y.setType("mpi")
+            Vel_array_Z = PETSc.Vec().create(self.comm)
+            Vel_array_Z.setType("mpi")
+            VelnM1_array_X = PETSc.Vec().create(self.comm)
+            VelnM1_array_X.setType("mpi")
+            VelnM1_array_Y = PETSc.Vec().create(self.comm)
+            VelnM1_array_Y.setType("mpi")
+            VelnM1_array_Z = PETSc.Vec().create(self.comm)
+            VelnM1_array_Z.setType("mpi")
+        else:
+            Vel_array_X = PETSc.Vec().create()
+            Vel_array_X.setType("seq")
+            Vel_array_Y = PETSc.Vec().create()
+            Vel_array_Y.setType("seq")
+            Vel_array_Z = PETSc.Vec().create()
+            Vel_array_Z.setType("seq")
+            VelnM1_array_X = PETSc.Vec().create()
+            VelnM1_array_X.setType("seq")
+            VelnM1_array_Y = PETSc.Vec().create()
+            VelnM1_array_Y.setType("seq")
+            VelnM1_array_Z = PETSc.Vec().create()
+            VelnM1_array_Z.setType("seq")
+        Vel_array_X.setSizes(self.nSolidInterfacePhysicalNodes + self.d_RBF)
+        Vel_array_Y.setSizes(self.nSolidInterfacePhysicalNodes + self.d_RBF)
+        Vel_array_Z.setSizes(self.nSolidInterfacePhysicalNodes + self.d_RBF)
         Vel_array_X.set(0.0)
         Vel_array_Y.set(0.0)
         Vel_array_Z.set(0.0)
-        VelnM1_array_X.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-        VelnM1_array_Y.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
-        VelnM1_array_Z.setSizes(self.nSolidInterfacePhysicalNodes+self.d_RBF)
+        VelnM1_array_X.setSizes(self.nSolidInterfacePhysicalNodes + self.d_RBF)
+        VelnM1_array_Y.setSizes(self.nSolidInterfacePhysicalNodes + self.d_RBF)
+        VelnM1_array_Z.setSizes(self.nSolidInterfacePhysicalNodes + self.d_RBF)
         VelnM1_array_X.set(0.0)
         VelnM1_array_Y.set(0.0)
         VelnM1_array_Z.set(0.0)
 
-
         # --- Fill the PETSc vectors ---
         GlobalIndex = int()
         localIndex = 0
         for iVertex in range(self.nLocalSolidInterfaceNodes):
-            GlobalIndex = SolidSolver.getVertexGlobalIndex(self.solidInterfaceIdentifier, iVertex)
+            GlobalIndex = SolidSolver.getVertexGlobalIndex(
+                self.solidInterfaceIdentifier, iVertex
+            )
             if GlobalIndex not in self.SolidHaloNodeList[myid].keys():
-              iGlobalVertex = self.__getGlobalIndex('solid', myid, localIndex)
-              velx, vely, velz = SolidSolver.getInterfaceNodeVel(self.solidInterfaceIdentifier, iVertex)
-              velxNm1, velyNm1, velzNm1 = SolidSolver.getInterfaceNodeVelNm1(self.solidInterfaceIdentifier, iVertex)
-              Vel_array_X.setValues([iGlobalVertex],velx)
-              Vel_array_Y.setValues([iGlobalVertex],vely)
-              Vel_array_Z.setValues([iGlobalVertex],velz)
-              VelnM1_array_X.setValues([iGlobalVertex],velxNm1)
-              VelnM1_array_Y.setValues([iGlobalVertex],velyNm1)
-              VelnM1_array_Z.setValues([iGlobalVertex],velzNm1)
-              localIndex += 1
+                iGlobalVertex = self.__getGlobalIndex("solid", myid, localIndex)
+                velx, vely, velz = SolidSolver.getInterfaceNodeVel(
+                    self.solidInterfaceIdentifier, iVertex
+                )
+                velxNm1, velyNm1, velzNm1 = SolidSolver.getInterfaceNodeVelNm1(
+                    self.solidInterfaceIdentifier, iVertex
+                )
+                Vel_array_X.setValues([iGlobalVertex], velx)
+                Vel_array_Y.setValues([iGlobalVertex], vely)
+                Vel_array_Z.setValues([iGlobalVertex], velz)
+                VelnM1_array_X.setValues([iGlobalVertex], velxNm1)
+                VelnM1_array_Y.setValues([iGlobalVertex], velyNm1)
+                VelnM1_array_Z.setValues([iGlobalVertex], velzNm1)
+                localIndex += 1
 
         Vel_array_X.assemblyBegin()
         Vel_array_X.assemblyEnd()
@@ -1818,9 +2455,18 @@ def displacementPredictor(self, FSI_config , SolidSolver, deltaT):
         VelnM1_array_Z.assemblyEnd()
 
         # --- Predict the solid position for the next time step ---
-        self.solidInterface_array_DispX += alpha_0*deltaT*Vel_array_X + alpha_1*deltaT*(Vel_array_X - VelnM1_array_X)
-        self.solidInterface_array_DispY += alpha_0*deltaT*Vel_array_Y + alpha_1*deltaT*(Vel_array_Y - VelnM1_array_Y)
-        self.solidInterface_array_DispZ += alpha_0*deltaT*Vel_array_Z + alpha_1*deltaT*(Vel_array_Z - VelnM1_array_Z)
+        self.solidInterface_array_DispX += (
+            alpha_0 * deltaT * Vel_array_X
+            + alpha_1 * deltaT * (Vel_array_X - VelnM1_array_X)
+        )
+        self.solidInterface_array_DispY += (
+            alpha_0 * deltaT * Vel_array_Y
+            + alpha_1 * deltaT * (Vel_array_Y - VelnM1_array_Y)
+        )
+        self.solidInterface_array_DispZ += (
+            alpha_0 * deltaT * Vel_array_Z
+            + alpha_1 * deltaT * (Vel_array_Z - VelnM1_array_Z)
+        )
 
         Vel_array_X.destroy()
         Vel_array_Y.destroy()
@@ -1837,31 +2483,48 @@ def writeFSIHistory(self, TimeIter, time, varCoordNorm, FSIConv):
         """
 
         if self.have_MPI:
-          myid = self.comm.Get_rank()
+            myid = self.comm.Get_rank()
         else:
-          myid = 0
+            myid = 0
 
         if myid == self.rootProcess:
-          if self.unsteady:
-            if TimeIter == 0:
-              histFile = open('FSIhistory.dat', "w")
-              histFile.write("TimeIter\tTime\tFSIRes\tFSINbIter\n")
-            else:
-              histFile = open('FSIhistory.dat', "a")
-            if FSIConv:
-              histFile.write(str(TimeIter) + '\t' + str(time) + '\t' + str(varCoordNorm) + '\t' + str(self.FSIIter+1) + '\n')
+            if self.unsteady:
+                if TimeIter == 0:
+                    histFile = open("FSIhistory.dat", "w")
+                    histFile.write("TimeIter\tTime\tFSIRes\tFSINbIter\n")
+                else:
+                    histFile = open("FSIhistory.dat", "a")
+                if FSIConv:
+                    histFile.write(
+                        str(TimeIter)
+                        + "\t"
+                        + str(time)
+                        + "\t"
+                        + str(varCoordNorm)
+                        + "\t"
+                        + str(self.FSIIter + 1)
+                        + "\n"
+                    )
+                else:
+                    histFile.write(
+                        str(TimeIter)
+                        + "\t"
+                        + str(time)
+                        + "\t"
+                        + str(varCoordNorm)
+                        + "\t"
+                        + str(self.FSIIter)
+                        + "\n"
+                    )
+                histFile.close()
             else:
-              histFile.write(str(TimeIter) + '\t' + str(time) + '\t' + str(varCoordNorm) + '\t' + str(self.FSIIter) + '\n')
-            histFile.close()
-          else:
-            if self.FSIIter == 0:
-              histFile = open('FSIhistory.dat', "w")
-              histFile.write("FSI Iter\tFSIRes\n")
-            else :
-              histFile = open('FSIhistory.dat', "a")
-            histFile.write(str(self.FSIIter) + '\t' + str(varCoordNorm) + '\n')
-            histFile.close()
-
+                if self.FSIIter == 0:
+                    histFile = open("FSIhistory.dat", "w")
+                    histFile.write("FSI Iter\tFSIRes\n")
+                else:
+                    histFile = open("FSIhistory.dat", "a")
+                histFile.write(str(self.FSIIter) + "\t" + str(varCoordNorm) + "\n")
+                histFile.close()
 
         self.MPIBarrier()
 
@@ -1873,338 +2536,380 @@ def __getGlobalIndex(self, physics, iProc, iLocalVertex):
         interface.
         """
 
-        if physics == 'fluid':
-          globalStartIndex = self.fluidGlobalIndexRange[iProc][iProc][0]
-        elif physics == 'solid':
-          globalStartIndex = self.solidGlobalIndexRange[iProc][iProc][0]
+        if physics == "fluid":
+            globalStartIndex = self.fluidGlobalIndexRange[iProc][iProc][0]
+        elif physics == "solid":
+            globalStartIndex = self.solidGlobalIndexRange[iProc][iProc][0]
 
         globalIndex = globalStartIndex + iLocalVertex
 
         return globalIndex
 
+    def UnsteadyFSI(self, FSI_config, FluidSolver, SolidSolver):
+        """
+        Run the unsteady FSI computation by synchronizing the fluid and solid solvers.
+        F/s interface data are exchanged through interface mapping and interpolation (if non mathcing meshes).
+        """
 
-    def UnsteadyFSI(self,FSI_config, FluidSolver, SolidSolver):
-          """
-          Run the unsteady FSI computation by synchronizing the fluid and solid solvers.
-          F/s interface data are exchanged through interface mapping and interpolation (if non mathcing meshes).
-          """
-
-          if self.have_MPI:
+        if self.have_MPI:
             myid = self.comm.Get_rank()
             numberPart = self.comm.Get_size()
-          else:
+        else:
             myid = 0
             numberPart = 1
 
-          # --- Set some general variables for the unsteady computation --- #
-          deltaT = FSI_config['UNST_TIMESTEP']                # physical time step
-          totTime = FSI_config['UNST_TIME']                # physical simulation time
-          NbFSIIterMax = FSI_config['NB_FSI_ITER']        # maximum number of FSI iteration (for each time step)
-          FSITolerance = FSI_config['FSI_TOLERANCE']        # f/s interface tolerance
-          TimeIterTreshold = FSI_config['TIME_TRESHOLD']				# time iteration from which we allow the solid to deform
-          self.MPIPrint('The FSI coupling will start after {} iterations'.format(TimeIterTreshold))
-
-          if FSI_config['RESTART_SOL'] == 'YES':
-            NbTimeIter = ((totTime)/deltaT)-1
-            time = (FSI_config['RESTART_ITER'])*deltaT
-            TimeIter = FSI_config['RESTART_ITER']
-          else:
-            NbTimeIter = (totTime/deltaT)-1		# number of time iterations
-            time = 0.0					# initial time
-            TimeIter = 0				# initial time iteration
-
-          NbTimeIter = int(NbTimeIter)			# be sure that NbTimeIter is an integer
-
-          varCoordNorm = 0.0				# FSI residual
-          FSIConv = False				# FSI convergence flag
-
-          self.MPIPrint('\n**********************************')
-          self.MPIPrint('* Begin unsteady FSI computation *')
-          self.MPIPrint('**********************************\n')
-
-          # --- Initialize the coupled solution --- #
-          #If restart
-          if FSI_config['RESTART_SOL'] == 'YES':
+        # --- Set some general variables for the unsteady computation --- #
+        deltaT = FSI_config["UNST_TIMESTEP"]  # physical time step
+        totTime = FSI_config["UNST_TIME"]  # physical simulation time
+        NbFSIIterMax = FSI_config[
+            "NB_FSI_ITER"
+        ]  # maximum number of FSI iteration (for each time step)
+        FSITolerance = FSI_config["FSI_TOLERANCE"]  # f/s interface tolerance
+        TimeIterTreshold = FSI_config[
+            "TIME_TRESHOLD"
+        ]  # time iteration from which we allow the solid to deform
+        self.MPIPrint(
+            "The FSI coupling will start after {} iterations".format(TimeIterTreshold)
+        )
+
+        if FSI_config["RESTART_SOL"] == "YES":
+            NbTimeIter = ((totTime) / deltaT) - 1
+            time = (FSI_config["RESTART_ITER"]) * deltaT
+            TimeIter = FSI_config["RESTART_ITER"]
+        else:
+            NbTimeIter = (totTime / deltaT) - 1  # number of time iterations
+            time = 0.0  # initial time
+            TimeIter = 0  # initial time iteration
+
+        NbTimeIter = int(NbTimeIter)  # be sure that NbTimeIter is an integer
+
+        varCoordNorm = 0.0  # FSI residual
+        FSIConv = False  # FSI convergence flag
+
+        self.MPIPrint("\n**********************************")
+        self.MPIPrint("* Begin unsteady FSI computation *")
+        self.MPIPrint("**********************************\n")
+
+        # --- Initialize the coupled solution --- #
+        # If restart
+        if FSI_config["RESTART_SOL"] == "YES":
             self.getSolidInterfaceDisplacement(SolidSolver)
             self.displacementPredictor(FSI_config, SolidSolver, deltaT)
             if myid in self.solidSolverProcessors:
-              SolidSolver.updateSolution()
-          #If no restart
-          else:
-            self.MPIPrint('Setting FSI initial conditions')
+                SolidSolver.updateSolution()
+        # If no restart
+        else:
+            self.MPIPrint("Setting FSI initial conditions")
             if myid in self.solidSolverProcessors:
-              SolidSolver.setInitialDisplacements()
+                SolidSolver.setInitialDisplacements()
             self.getSolidInterfaceDisplacement(SolidSolver)
             self.interpolateSolidPositionOnFluidMesh(FSI_config)
             self.setFluidInterfaceVarCoord(FluidSolver)
-            self.MPIPrint('\nPerforming static mesh deformation (ALE) of initial mesh...\n')
+            self.MPIPrint(
+                "\nPerforming static mesh deformation (ALE) of initial mesh...\n"
+            )
             if myid in self.fluidSolverProcessors:
-              FluidSolver.SetInitialMesh()	# if there is an initial deformation in the solid, it has to be communicated to the fluid solver
-            self.MPIPrint('\nFSI initial conditions are set')
-            self.MPIPrint('Beginning time integration\n')
+                FluidSolver.SetInitialMesh()  # if there is an initial deformation in the solid, it has to be communicated to the fluid solver
+            self.MPIPrint("\nFSI initial conditions are set")
+            self.MPIPrint("Beginning time integration\n")
+
+        # --- External temporal loop --- #
+        while TimeIter <= NbTimeIter:
+
+            if TimeIter > TimeIterTreshold:
+                NbFSIIter = NbFSIIterMax
+                self.MPIPrint("\n")
+                self.MPIPrint(
+                    " Enter Block Gauss Seidel (BGS) method for strong coupling FSI on time iteration {} ".format(
+                        TimeIter
+                    ).center(
+                        80, "*"
+                    )
+                )
+            else:
+                NbFSIIter = 1
 
-          # --- External temporal loop --- #
-          while TimeIter <= NbTimeIter:
+            self.FSIIter = 0
+            FSIConv = False
 
-                if TimeIter > TimeIterTreshold:
-                  NbFSIIter = NbFSIIterMax
-                  self.MPIPrint("\n")
-                  self.MPIPrint(" Enter Block Gauss Seidel (BGS) method for strong coupling FSI on time iteration {} ".format(TimeIter).center(80,"*"))
-                else:
-                  NbFSIIter = 1
-
-                self.FSIIter = 0
-                FSIConv = False
-
-                # --- Internal FSI loop --- #
-                while self.FSIIter <= (NbFSIIter-1):
-
-                        self.MPIPrint("\n>>>> Time iteration {} / FSI iteration {} <<<<".format(TimeIter,self.FSIIter))
-
-                        # --- Mesh morphing step (displacements interpolation, displacements communication, and mesh morpher call) --- #
-                        self.interpolateSolidPositionOnFluidMesh(FSI_config)
-                        self.MPIPrint('\nPerforming dynamic mesh deformation (ALE)...\n')
-                        self.setFluidInterfaceVarCoord(FluidSolver)
-                        if myid in self.fluidSolverProcessors:
-                          if self.FSIIter == 0:
-                            FluidSolver.Preprocess(TimeIter)	# set some parameters before temporal fluid iteration and dynamic mesh update
-                          else:
-                            FluidSolver.DynamicMeshUpdate(TimeIter)
-                        # --- Fluid solver call for FSI subiteration --- #
-                        self.MPIPrint('\nLaunching fluid solver for one single dual-time iteration...')
-                        self.MPIBarrier()
-                        if myid in self.fluidSolverProcessors:
-                          FluidSolver.ResetConvergence()
-                          FluidSolver.Run()
-                          self.MPIBarrier()
-                          FluidSolver.Postprocess()
-                          self.MPIBarrier()
-
-                        # --- Surface fluid loads interpolation and communication --- #
-                        if TimeIter > TimeIterTreshold:
-                          if not self.ImposedMotion:
-                            self.MPIPrint('\nProcessing interface fluid loads...\n')
-                            self.MPIBarrier()
-                            self.getFluidInterfaceNodalForce(FSI_config, FluidSolver)
-                            self.MPIBarrier()
-                            self.interpolateFluidLoadsOnSolidMesh(FSI_config)
-                            self.setSolidInterfaceLoads(SolidSolver, FSI_config)
-
-                          # --- Solid solver call for FSI subiteration --- #
-                          self.MPIPrint('\nLaunching solid solver for a single time iteration...\n')
-                          if myid in self.solidSolverProcessors:
-                              SolidSolver.run(time)
-
-                          # --- Compute and monitor the FSI residual --- #
-                          varCoordNorm = self.computeSolidInterfaceResidual(SolidSolver)
-                          self.MPIPrint('\nFSI displacement norm : {}\n'.format(varCoordNorm))
-                          if varCoordNorm < FSITolerance:
-                            FSIConv = True
-                            break
-
-                          # --- Relaxe the solid position --- #
-                          self.MPIPrint('\nProcessing interface displacements...\n')
-                          self.relaxSolidPosition(FSI_config)
-
-                        self.FSIIter += 1
-                # --- End OF FSI loop --- #
+            # --- Internal FSI loop --- #
+            while self.FSIIter <= (NbFSIIter - 1):
 
+                self.MPIPrint(
+                    "\n>>>> Time iteration {} / FSI iteration {} <<<<".format(
+                        TimeIter, self.FSIIter
+                    )
+                )
+
+                # --- Mesh morphing step (displacements interpolation, displacements communication, and mesh morpher call) --- #
+                self.interpolateSolidPositionOnFluidMesh(FSI_config)
+                self.MPIPrint("\nPerforming dynamic mesh deformation (ALE)...\n")
+                self.setFluidInterfaceVarCoord(FluidSolver)
+                if myid in self.fluidSolverProcessors:
+                    if self.FSIIter == 0:
+                        FluidSolver.Preprocess(
+                            TimeIter
+                        )  # set some parameters before temporal fluid iteration and dynamic mesh update
+                    else:
+                        FluidSolver.DynamicMeshUpdate(TimeIter)
+                # --- Fluid solver call for FSI subiteration --- #
+                self.MPIPrint(
+                    "\nLaunching fluid solver for one single dual-time iteration..."
+                )
                 self.MPIBarrier()
+                if myid in self.fluidSolverProcessors:
+                    FluidSolver.ResetConvergence()
+                    FluidSolver.Run()
+                    self.MPIBarrier()
+                    FluidSolver.Postprocess()
+                    self.MPIBarrier()
 
-                # --- Update the FSI history file --- #
+                # --- Surface fluid loads interpolation and communication --- #
                 if TimeIter > TimeIterTreshold:
-                  self.MPIPrint('\nBGS is converged (strong coupling)')
-                self.writeFSIHistory(TimeIter, time, varCoordNorm, FSIConv)
-
-                # --- Update, monitor and output the fluid solution before the next time step  ---#
-                if myid in self.fluidSolverProcessors:
-                  FluidSolver.Update()
-                  FluidSolver.Monitor(TimeIter)
-                  FluidSolver.Output(TimeIter)
+                    if not self.ImposedMotion:
+                        self.MPIPrint("\nProcessing interface fluid loads...\n")
+                        self.MPIBarrier()
+                        self.getFluidInterfaceNodalForce(FSI_config, FluidSolver)
+                        self.MPIBarrier()
+                        self.interpolateFluidLoadsOnSolidMesh(FSI_config)
+                        self.setSolidInterfaceLoads(SolidSolver, FSI_config)
+
+                    # --- Solid solver call for FSI subiteration --- #
+                    self.MPIPrint(
+                        "\nLaunching solid solver for a single time iteration...\n"
+                    )
+                    if myid in self.solidSolverProcessors:
+                        SolidSolver.run(time)
+
+                    # --- Compute and monitor the FSI residual --- #
+                    varCoordNorm = self.computeSolidInterfaceResidual(SolidSolver)
+                    self.MPIPrint("\nFSI displacement norm : {}\n".format(varCoordNorm))
+                    if varCoordNorm < FSITolerance:
+                        FSIConv = True
+                        break
+
+                    # --- Relaxe the solid position --- #
+                    self.MPIPrint("\nProcessing interface displacements...\n")
+                    self.relaxSolidPosition(FSI_config)
+
+                self.FSIIter += 1
+            # --- End OF FSI loop --- #
+
+            self.MPIBarrier()
+
+            # --- Update the FSI history file --- #
+            if TimeIter > TimeIterTreshold:
+                self.MPIPrint("\nBGS is converged (strong coupling)")
+            self.writeFSIHistory(TimeIter, time, varCoordNorm, FSIConv)
+
+            # --- Update, monitor and output the fluid solution before the next time step  ---#
+            if myid in self.fluidSolverProcessors:
+                FluidSolver.Update()
+                FluidSolver.Monitor(TimeIter)
+                FluidSolver.Output(TimeIter)
 
-                if TimeIter >= TimeIterTreshold:
-                  if myid in self.solidSolverProcessors:
+            if TimeIter >= TimeIterTreshold:
+                if myid in self.solidSolverProcessors:
                     # --- Output the solid solution before thr next time step --- #
                     SolidSolver.writeSolution(time, TimeIter, self.FSIIter)
 
-                if TimeIter > TimeIterTreshold:
-                  # --- Displacement predictor for the next time step and update of the solid solution --- #
-                  self.MPIPrint('\nSolid displacement prediction for next time step')
-                  self.displacementPredictor(FSI_config, SolidSolver, deltaT)
-                  if myid in self.solidSolverProcessors:
+            if TimeIter > TimeIterTreshold:
+                # --- Displacement predictor for the next time step and update of the solid solution --- #
+                self.MPIPrint("\nSolid displacement prediction for next time step")
+                self.displacementPredictor(FSI_config, SolidSolver, deltaT)
+                if myid in self.solidSolverProcessors:
                     SolidSolver.updateSolution()
 
-                TimeIter += 1
-                time += deltaT
-          #--- End of the temporal loop --- #
+            TimeIter += 1
+            time += deltaT
+        # --- End of the temporal loop --- #
 
-          self.MPIBarrier()
+        self.MPIBarrier()
 
-          self.MPIPrint('\n*************************')
-          self.MPIPrint('*  End FSI computation  *')
-          self.MPIPrint('*************************\n')
+        self.MPIPrint("\n*************************")
+        self.MPIPrint("*  End FSI computation  *")
+        self.MPIPrint("*************************\n")
 
-    def SteadyFSI(self, FSI_config,FluidSolver, SolidSolver):
-          """
-          Runs the steady FSI computation by synchronizing the fluid and solid solver with data exchange at the f/s interface.
-          """
+    def SteadyFSI(self, FSI_config, FluidSolver, SolidSolver):
+        """
+        Runs the steady FSI computation by synchronizing the fluid and solid solver with data exchange at the f/s interface.
+        """
 
-          if self.have_MPI:
+        if self.have_MPI:
             myid = self.comm.Get_rank()
             numberPart = self.comm.Get_size()
-          else:
+        else:
             myid = 0
             numberPart = 1
 
-          # --- Set some general variables for the steady computation --- #
-          NbFSIIterMax = FSI_config['NB_FSI_ITER']	# maximum number of FSI iteration (for each time step)
-          FSITolerance = FSI_config['FSI_TOLERANCE']	# f/s interface tolerance
-          varCoordNorm = 0.0
-
-          self.MPIPrint('\n********************************')
-          self.MPIPrint('* Begin steady FSI computation *')
-          self.MPIPrint('********************************\n')
-          self.MPIPrint("\n")
-          self.MPIPrint(" Enter Block Gauss Seidel (BGS) method for strong coupling FSI ".center(80,"*"))
-
-          self.MPIPrint('Setting initial deformed mesh')
-          if myid in self.solidSolverProcessors:
-              SolidSolver.setInitialDisplacements()
-          self.getSolidInterfaceDisplacement(SolidSolver)
-          self.interpolateSolidPositionOnFluidMesh(FSI_config)
-          self.setFluidInterfaceVarCoord(FluidSolver)
-          self.MPIPrint('\nFSI initial conditions are set')
-
-          # --- External FSI loop --- #
-          self.FSIIter = 0
-          while self.FSIIter < NbFSIIterMax:
+        # --- Set some general variables for the steady computation --- #
+        NbFSIIterMax = FSI_config[
+            "NB_FSI_ITER"
+        ]  # maximum number of FSI iteration (for each time step)
+        FSITolerance = FSI_config["FSI_TOLERANCE"]  # f/s interface tolerance
+        varCoordNorm = 0.0
+
+        self.MPIPrint("\n********************************")
+        self.MPIPrint("* Begin steady FSI computation *")
+        self.MPIPrint("********************************\n")
+        self.MPIPrint("\n")
+        self.MPIPrint(
+            " Enter Block Gauss Seidel (BGS) method for strong coupling FSI ".center(
+                80, "*"
+            )
+        )
+
+        self.MPIPrint("Setting initial deformed mesh")
+        if myid in self.solidSolverProcessors:
+            SolidSolver.setInitialDisplacements()
+        self.getSolidInterfaceDisplacement(SolidSolver)
+        self.interpolateSolidPositionOnFluidMesh(FSI_config)
+        self.setFluidInterfaceVarCoord(FluidSolver)
+        self.MPIPrint("\nFSI initial conditions are set")
+
+        # --- External FSI loop --- #
+        self.FSIIter = 0
+        while self.FSIIter < NbFSIIterMax:
             self.MPIPrint("\n>>>> FSI iteration {} <<<<".format(self.FSIIter))
-            self.MPIPrint('\nLaunching fluid solver for a steady computation...')
+            self.MPIPrint("\nLaunching fluid solver for a steady computation...")
             # --- Fluid solver call for FSI subiteration ---#
 
             if myid in self.fluidSolverProcessors:
-              FluidSolver.ResetConvergence() #This is setting to zero the convergence in the integrator, important to reset it.
-              # The mesh will be deformed in the context of the preprocessor, there is no need to set the initial
-              # mesh pushing back the solution to avoid spurious velocities, as the velocity is not computed at all
-              self.MPIPrint('\nPerforming static mesh deformation...\n')
-              FluidSolver.Preprocess(0)# This will attempt to always set the initial condition, but there is a flag on the unsteady computation that will avoid it
-              FluidSolver.Run()
-              FluidSolver.Postprocess()
-              FluidSolver.Monitor(0) #This is actually not needed, it only saves the fact that the fluid solver converged innerly or reached max iterations
-              FluidSolver.Output(0)
+                FluidSolver.ResetConvergence()  # This is setting to zero the convergence in the integrator, important to reset it.
+                # The mesh will be deformed in the context of the preprocessor, there is no need to set the initial
+                # mesh pushing back the solution to avoid spurious velocities, as the velocity is not computed at all
+                self.MPIPrint("\nPerforming static mesh deformation...\n")
+                FluidSolver.Preprocess(
+                    0
+                )  # This will attempt to always set the initial condition, but there is a flag on the unsteady computation that will avoid it
+                FluidSolver.Run()
+                FluidSolver.Postprocess()
+                FluidSolver.Monitor(
+                    0
+                )  # This is actually not needed, it only saves the fact that the fluid solver converged innerly or reached max iterations
+                FluidSolver.Output(0)
 
             # --- Surface fluid loads interpolation and communication ---#
             if not self.ImposedMotion:
-              self.MPIPrint('\nProcessing interface fluid loads...\n')
-              self.MPIBarrier()
-              self.getFluidInterfaceNodalForce(FSI_config, FluidSolver)
-              self.MPIBarrier()
-              self.interpolateFluidLoadsOnSolidMesh(FSI_config)
-              self.setSolidInterfaceLoads(SolidSolver, FSI_config)
-              # --- Solid solver call for FSI subiteration --- #
-              self.MPIPrint('\nLaunching solid solver for a static computation...\n')
-              if myid in self.solidSolverProcessors:
-                SolidSolver.run(0.0)
-                SolidSolver.writeSolution(0.0, 0, self.FSIIter)
+                self.MPIPrint("\nProcessing interface fluid loads...\n")
+                self.MPIBarrier()
+                self.getFluidInterfaceNodalForce(FSI_config, FluidSolver)
+                self.MPIBarrier()
+                self.interpolateFluidLoadsOnSolidMesh(FSI_config)
+                self.setSolidInterfaceLoads(SolidSolver, FSI_config)
+                # --- Solid solver call for FSI subiteration --- #
+                self.MPIPrint("\nLaunching solid solver for a static computation...\n")
+                if myid in self.solidSolverProcessors:
+                    SolidSolver.run(0.0)
+                    SolidSolver.writeSolution(0.0, 0, self.FSIIter)
 
             # --- Compute and monitor the FSI residual --- #
             varCoordNorm = self.computeSolidInterfaceResidual(SolidSolver)
-            self.MPIPrint('\nFSI displacement norm : {}\n'.format(varCoordNorm))
+            self.MPIPrint("\nFSI displacement norm : {}\n".format(varCoordNorm))
             self.writeFSIHistory(0, 0.0, varCoordNorm, False)
             if varCoordNorm < FSITolerance:
-              break
+                break
 
             # --- Relaxe the solid displacement and update the solid solution --- #
-            self.MPIPrint('\nProcessing interface displacements...\n')
+            self.MPIPrint("\nProcessing interface displacements...\n")
             self.relaxSolidPosition(FSI_config)
             if myid in self.solidSolverProcessors:
-              SolidSolver.updateSolution()
+                SolidSolver.updateSolution()
 
             # --- Mesh morphing step (displacement interpolation, displacements communication, and mesh morpher call) --- #
             self.interpolateSolidPositionOnFluidMesh(FSI_config)
             self.setFluidInterfaceVarCoord(FluidSolver)
             self.FSIIter += 1
 
-          self.MPIBarrier()
+        self.MPIBarrier()
 
-          self.MPIPrint('\nBGS is converged (strong coupling)')
-          self.MPIPrint(' ')
-          self.MPIPrint('*************************')
-          self.MPIPrint('*  End FSI computation  *')
-          self.MPIPrint('*************************')
-          self.MPIPrint(' ')
+        self.MPIPrint("\nBGS is converged (strong coupling)")
+        self.MPIPrint(" ")
+        self.MPIPrint("*************************")
+        self.MPIPrint("*  End FSI computation  *")
+        self.MPIPrint("*************************")
+        self.MPIPrint(" ")
 
     def MapModes(self, FSI_config, FluidSolver, SolidSolver):
-      """
-      Runs nothing, just extract the structural modes mapped on the fluid mesh
-      """
-
-      if self.have_MPI:
-        myid = self.comm.Get_rank()
-        numberPart = self.comm.Get_size()
-      else:
-        myid = 0
-        numberPart = 1
-
-      nodeNormals = {}
-      for iVertex in range(self.nLocalFluidInterfaceNodes):
-        if self.nDim == 2:
-            nx, ny = FluidSolver.GetMarkerVertexNormals(self.fluidInterfaceIdentifier, iVertex, False)
-            nz = 0
-        else:
-            nx, ny, nz = FluidSolver.GetMarkerVertexNormals(self.fluidInterfaceIdentifier, iVertex, False)
-        GlobalIndex = FluidSolver.GetNodeGlobalIndex(FluidSolver.GetMarkerNode(self.fluidInterfaceIdentifier, iVertex))
-        nodeNormals[GlobalIndex] = [nx, ny, nz]
-
-      nodeNormals = self.comm.gather(nodeNormals, root=self.rootProcess)
-      if myid == self.rootProcess:
-        normalsToPrint = {}
-        for iDictionary in range(numberPart):
-          for key, value in nodeNormals[iDictionary].items():
-            normalsToPrint[key] = value
-        normalsToPrint = dict(sorted(normalsToPrint.items()))
-        with open('Normals.csv', 'w') as f:
-          writer = csv.writer(f)
-          for key, value in normalsToPrint.items():
-            writer.writerow([key, value])
-
-
-      SurfaceFileName = FluidSolver.GetSurfaceFileName()
-
-      self.MPIPrint('\n********************************')
-      self.MPIPrint('* Begin mapping the modes *')
-      self.MPIPrint('********************************\n')
-      self.MPIPrint("\n")
-
-      if myid == self.rootProcess:  # The root process contains the solid solver for sure
-        modesNumber = np.array(int(SolidSolver.getNumberOfModes()))
-      else:
-        modesNumber = np.empty(1, dtype=np.int)
-
-      self.comm.Bcast(modesNumber, root=self.rootProcess)
-
-      for mode in range(np.asscalar(modesNumber)):
-        self.MPIPrint("Setting mode {} active".format(mode))
-        if myid in self.solidSolverProcessors:
-          SolidSolver.activateMode(mode)
-        self.MPIBarrier()
-        self.getSolidInterfaceDisplacement(SolidSolver)
-        self.interpolateSolidPositionOnFluidMesh(FSI_config)
-        self.setFluidInterfaceVarCoord(FluidSolver)
+        """
+        Runs nothing, just extract the structural modes mapped on the fluid mesh
+        """
 
-        self.MPIPrint('\nPerforming mesh deformation...\n')
-        FluidSolver.DynamicMeshUpdate(0)
-        FluidSolver.Output(0)
-        self.MPIBarrier()
+        if self.have_MPI:
+            myid = self.comm.Get_rank()
+            numberPart = self.comm.Get_size()
+        else:
+            myid = 0
+            numberPart = 1
 
+        nodeNormals = {}
+        for iVertex in range(self.nLocalFluidInterfaceNodes):
+            if self.nDim == 2:
+                nx, ny = FluidSolver.GetMarkerVertexNormals(
+                    self.fluidInterfaceIdentifier, iVertex, False
+                )
+                nz = 0
+            else:
+                nx, ny, nz = FluidSolver.GetMarkerVertexNormals(
+                    self.fluidInterfaceIdentifier, iVertex, False
+                )
+            GlobalIndex = FluidSolver.GetNodeGlobalIndex(
+                FluidSolver.GetMarkerNode(self.fluidInterfaceIdentifier, iVertex)
+            )
+            nodeNormals[GlobalIndex] = [nx, ny, nz]
+
+        nodeNormals = self.comm.gather(nodeNormals, root=self.rootProcess)
         if myid == self.rootProcess:
-          AllFiles = os.listdir()
-          for FileNumber,FileName in enumerate(AllFiles):
-            if SurfaceFileName in FileName:
-              file = FileName.split(".")[0]
-              extension = FileName.split(".")[1]
-              os.rename(file+"."+extension,"Mode{}.".format(mode)+extension)
-
-      self.MPIPrint('\n*************************')
-      self.MPIPrint('*  Mapping completed  *')
-      self.MPIPrint('*************************\n')
+            normalsToPrint = {}
+            for iDictionary in range(numberPart):
+                for key, value in nodeNormals[iDictionary].items():
+                    normalsToPrint[key] = value
+            normalsToPrint = dict(sorted(normalsToPrint.items()))
+            with open("Normals.csv", "w") as f:
+                writer = csv.writer(f)
+                for key, value in normalsToPrint.items():
+                    writer.writerow([key, value])
+
+        SurfaceFileName = FluidSolver.GetSurfaceFileName()
+
+        self.MPIPrint("\n********************************")
+        self.MPIPrint("* Begin mapping the modes *")
+        self.MPIPrint("********************************\n")
+        self.MPIPrint("\n")
+
+        if (
+            myid == self.rootProcess
+        ):  # The root process contains the solid solver for sure
+            modesNumber = np.array(int(SolidSolver.getNumberOfModes()))
+        else:
+            modesNumber = np.empty(1, dtype=np.int)
+
+        self.comm.Bcast(modesNumber, root=self.rootProcess)
+
+        for mode in range(np.asscalar(modesNumber)):
+            self.MPIPrint("Setting mode {} active".format(mode))
+            if myid in self.solidSolverProcessors:
+                SolidSolver.activateMode(mode)
+            self.MPIBarrier()
+            self.getSolidInterfaceDisplacement(SolidSolver)
+            self.interpolateSolidPositionOnFluidMesh(FSI_config)
+            self.setFluidInterfaceVarCoord(FluidSolver)
+
+            self.MPIPrint("\nPerforming mesh deformation...\n")
+            FluidSolver.DynamicMeshUpdate(0)
+            FluidSolver.Output(0)
+            self.MPIBarrier()
+
+            if myid == self.rootProcess:
+                AllFiles = os.listdir()
+                for FileNumber, FileName in enumerate(AllFiles):
+                    if SurfaceFileName in FileName:
+                        file = FileName.split(".")[0]
+                        extension = FileName.split(".")[1]
+                        os.rename(
+                            file + "." + extension, "Mode{}.".format(mode) + extension
+                        )
+
+        self.MPIPrint("\n*************************")
+        self.MPIPrint("*  Mapping completed  *")
+        self.MPIPrint("*************************\n")
diff --git a/SU2_PY/FSI_tools/FSI_config.py b/SU2_PY/FSI_tools/FSI_config.py
index 2def017c750..a0fca32d019 100644
--- a/SU2_PY/FSI_tools/FSI_config.py
+++ b/SU2_PY/FSI_tools/FSI_config.py
@@ -38,13 +38,14 @@
 #  FSI Configuration Class
 # ----------------------------------------------------------------------
 
+
 class FSIConfig:
     """
     Class that contains all the parameters coming from the FSI configuration file.
     Read the file and store all the options into a dictionary.
     """
 
-    def __init__(self,FileName,comm):
+    def __init__(self, FileName, comm):
         self.ConfigFileName = FileName
         self.comm = comm
         self._ConfigContent = {}
@@ -54,10 +55,10 @@ def __init__(self,FileName,comm):
     def __str__(self):
         tempString = str()
         for key, value in self._ConfigContent.items():
-            tempString += "{} = {}\n".format(key,value)
+            tempString += "{} = {}\n".format(key, value)
         return tempString
 
-    def __getitem__(self,key):
+    def __getitem__(self, key):
         return self._ConfigContent[key]
 
     def __setitem__(self, key, value):
@@ -70,67 +71,91 @@ def readConfig(self):
             if not line:
                 break
             # remove line returns
-            line = line.strip('\r\n')
+            line = line.strip("\r\n")
             # make sure it has useful data
-            if (not "=" in line) or (line[0] == '%'):
+            if (not "=" in line) or (line[0] == "%"):
                 continue
             # split across equal sign
-            line = line.split("=",1)
+            line = line.split("=", 1)
             this_param = line[0].strip()
             this_value = line[1].strip()
 
-	        #integer values
-            if (this_param == "NDIM")	or \
-               (this_param == "RESTART_ITER")	or \
-               (this_param == "TIME_TRESHOLD") or \
-               (this_param == "NB_FSI_ITER") :
+            # integer values
+            if (
+                (this_param == "NDIM")
+                or (this_param == "RESTART_ITER")
+                or (this_param == "TIME_TRESHOLD")
+                or (this_param == "NB_FSI_ITER")
+            ):
                 self._ConfigContent[this_param] = int(this_value)
 
-            #float values
-            elif (this_param == "RBF_RADIUS") or \
-                 (this_param == "AITKEN_PARAM") or \
-                 (this_param == "UNST_TIMESTEP") or \
-                 (this_param == "UNST_TIME") or \
-                 (this_param == "FSI_TOLERANCE") :
+            # float values
+            elif (
+                (this_param == "RBF_RADIUS")
+                or (this_param == "AITKEN_PARAM")
+                or (this_param == "UNST_TIMESTEP")
+                or (this_param == "UNST_TIME")
+                or (this_param == "FSI_TOLERANCE")
+            ):
                 self._ConfigContent[this_param] = float(this_value)
 
-            #string values
-            elif (this_param == "CFD_CONFIG_FILE_NAME") or \
-                 (this_param == "CSD_SOLVER") or \
-                 (this_param == "CSD_CONFIG_FILE_NAME") or \
-                 (this_param == "RESTART_SOL") or \
-                 (this_param == "MATCHING_MESH") or \
-                 (this_param == "MESH_INTERP_METHOD") or \
-                 (this_param == "DISP_PRED") or \
-                 (this_param == "AITKEN_RELAX") or \
-                 (this_param == "TIME_MARCHING") or \
-                 (this_param == "IMPOSED_MOTION") or \
-                 (this_param == "MAPPING_MODES"):
+            # string values
+            elif (
+                (this_param == "CFD_CONFIG_FILE_NAME")
+                or (this_param == "CSD_SOLVER")
+                or (this_param == "CSD_CONFIG_FILE_NAME")
+                or (this_param == "RESTART_SOL")
+                or (this_param == "MATCHING_MESH")
+                or (this_param == "MESH_INTERP_METHOD")
+                or (this_param == "DISP_PRED")
+                or (this_param == "AITKEN_RELAX")
+                or (this_param == "TIME_MARCHING")
+                or (this_param == "IMPOSED_MOTION")
+                or (this_param == "MAPPING_MODES")
+            ):
                 self._ConfigContent[this_param] = this_value
 
-            else :
-                self.MPIPrint(this_param + " is an invalid option !",False)
+            else:
+                self.MPIPrint(this_param + " is an invalid option !", False)
 
     def applyDefaults(self):
 
         if "MAPPING_MODES" not in self._ConfigContent:
             self._ConfigContent["MAPPING_MODES"] = "NO"
-            self.MPIPrint("MAPPING_MODES keyword was not found in the configuration file of the interface, setting to NO",False)
+            self.MPIPrint(
+                "MAPPING_MODES keyword was not found in the configuration file of the interface, setting to NO",
+                False,
+            )
 
         if "IMPOSED_MOTION" not in self._ConfigContent:
             self._ConfigContent["IMPOSED_MOTION"] = "NO"
-            self.MPIPrint("IMPOSED_MOTION keyword was not found in the configuration file of the interface, setting to NO",False)
+            self.MPIPrint(
+                "IMPOSED_MOTION keyword was not found in the configuration file of the interface, setting to NO",
+                False,
+            )
 
         if self._ConfigContent["IMPOSED_MOTION"] == "YES":
-            if self._ConfigContent["AITKEN_RELAX"] != "STATIC" or self._ConfigContent["AITKEN_PARAM"] != 1.0:
-                self.MPIPrint("When imposing motion, the Aitken parameter must be static and equal to 1",True)
+            if (
+                self._ConfigContent["AITKEN_RELAX"] != "STATIC"
+                or self._ConfigContent["AITKEN_PARAM"] != 1.0
+            ):
+                self.MPIPrint(
+                    "When imposing motion, the Aitken parameter must be static and equal to 1",
+                    True,
+                )
 
         if self._ConfigContent["RESTART_SOL"] == "YES":
             if self._ConfigContent["TIME_TRESHOLD"] != -1:
-                self.MPIPrint("When restarting a simulation, the time threshold must be -1 for immediate coupling",True)
-
-        if self._ConfigContent["MAPPING_MODES"] == "YES" and self._ConfigContent["CSD_SOLVER"]!="NATIVE":
-            self.MPIPrint("Mapping modes only works with the native solver",True)
+                self.MPIPrint(
+                    "When restarting a simulation, the time threshold must be -1 for immediate coupling",
+                    True,
+                )
+
+        if (
+            self._ConfigContent["MAPPING_MODES"] == "YES"
+            and self._ConfigContent["CSD_SOLVER"] != "NATIVE"
+        ):
+            self.MPIPrint("Mapping modes only works with the native solver", True)
 
     def MPIPrint(self, message, error):
         """
diff --git a/SU2_PY/OptimalPropeller.py b/SU2_PY/OptimalPropeller.py
index ef22e7db419..388689fb637 100644
--- a/SU2_PY/OptimalPropeller.py
+++ b/SU2_PY/OptimalPropeller.py
@@ -48,83 +48,90 @@
 ###     Functions      ###
 ##########################
 
-def a_distribution (w0, Chi):
+
+def a_distribution(w0, Chi):
     """Function used to compute the value of the axial interference factor using the inviscid theory of the optimal propeller."""
 
-    return (w0*pow(Chi,2))/(pow(Chi,2)+pow((1+(w0)),2))
+    return (w0 * pow(Chi, 2)) / (pow(Chi, 2) + pow((1 + (w0)), 2))
 
 
 def write_su2_config_file():
     """Write the actuator disk configuration file"""
 
-    with open('ActuatorDisk.cfg', 'w') as f:
-        f.write('% Automatic generated actuator disk configuration file.\n')
-        f.write('%\n')
-        f.write('% The first two elements of MARKER_ACTDISK must be filled.\n')
-        f.write('% An example of this file can be found in the TestCases directory.\n')
-        f.write('%\n')
-        f.write('% Author: Ettore Saetta, Lorenzo Russo, Renato Tognaccini.\n')
-        f.write('% Theoretical and Applied Aerodynamic Research Group (TAARG),\n')
-        f.write('% University of Naples Federico II\n')
-        f.write('\n')
-        f.write('ACTDISK_TYPE = VARIABLE_LOAD\n')
-        f.write('ACTDISK_FILENAME = ActuatorDisk.dat\n')
-        f.write('MARKER_ACTDISK = ( , , 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)\n')
+    with open("ActuatorDisk.cfg", "w") as f:
+        f.write("% Automatic generated actuator disk configuration file.\n")
+        f.write("%\n")
+        f.write("% The first two elements of MARKER_ACTDISK must be filled.\n")
+        f.write("% An example of this file can be found in the TestCases directory.\n")
+        f.write("%\n")
+        f.write("% Author: Ettore Saetta, Lorenzo Russo, Renato Tognaccini.\n")
+        f.write("% Theoretical and Applied Aerodynamic Research Group (TAARG),\n")
+        f.write("% University of Naples Federico II\n")
+        f.write("\n")
+        f.write("ACTDISK_TYPE = VARIABLE_LOAD\n")
+        f.write("ACTDISK_FILENAME = ActuatorDisk.dat\n")
+        f.write("MARKER_ACTDISK = ( , , 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)\n")
 
-    print('SU2 file generated!')
+    print("SU2 file generated!")
 
 
 def write_external_file(CTrs, CPrs):
     """Function to write the actuator disk input data file"""
 
-    with open('ActuatorDisk.dat', 'w') as f:
-        f.write('# Automatic generated actuator disk input data file using the Optimal Propeller code.\n')
-        f.write('# Data file needed for the actuator disk VARIABLE_LOAD type.\n')
-        f.write('# The load distribution is obtained using the inviscid theory of the optimal propeller\n')
-        f.write('# using global data.\n')
-        f.write('#\n')
-        f.write('# The first three lines must be filled.\n')
-        f.write('# An example of this file can be found in the TestCases directory.\n')
-        f.write('#\n')
-        f.write('# Author: Ettore Saetta, Lorenzo Russo, Renato Tognaccini.\n')
-        f.write('# Theoretical and Applied Aerodynamic Research Group (TAARG),\n')
-        f.write('# University of Naples Federico II\n')
-        f.write('# -------------------------------------------------------------------------------------\n')
-        f.write('#\n')
-        f.write('MARKER_ACTDISK= \n')
-        f.write('CENTER= \n')
-        f.write('AXIS= \n')
-        f.write('RADIUS= '+str(R)+'\n')
-        f.write('ADV_RATIO= '+str(J)+'\n')
-        f.write('NROW= '+str(stations)+'\n')
-        f.write('# rs=r/R        dCT/drs       dCP/drs       dCR/drs\n')
+    with open("ActuatorDisk.dat", "w") as f:
+        f.write(
+            "# Automatic generated actuator disk input data file using the Optimal Propeller code.\n"
+        )
+        f.write("# Data file needed for the actuator disk VARIABLE_LOAD type.\n")
+        f.write(
+            "# The load distribution is obtained using the inviscid theory of the optimal propeller\n"
+        )
+        f.write("# using global data.\n")
+        f.write("#\n")
+        f.write("# The first three lines must be filled.\n")
+        f.write("# An example of this file can be found in the TestCases directory.\n")
+        f.write("#\n")
+        f.write("# Author: Ettore Saetta, Lorenzo Russo, Renato Tognaccini.\n")
+        f.write("# Theoretical and Applied Aerodynamic Research Group (TAARG),\n")
+        f.write("# University of Naples Federico II\n")
+        f.write(
+            "# -------------------------------------------------------------------------------------\n"
+        )
+        f.write("#\n")
+        f.write("MARKER_ACTDISK= \n")
+        f.write("CENTER= \n")
+        f.write("AXIS= \n")
+        f.write("RADIUS= " + str(R) + "\n")
+        f.write("ADV_RATIO= " + str(J) + "\n")
+        f.write("NROW= " + str(stations) + "\n")
+        f.write("# rs=r/R        dCT/drs       dCP/drs       dCR/drs\n")
 
         for i in range(0, stations):
-            f.write(f'  {r[i]:.7f}     {CTrs[i]:.7f}     {CPrs[i]:.7f}     0.0\n')
+            f.write(f"  {r[i]:.7f}     {CTrs[i]:.7f}     {CPrs[i]:.7f}     0.0\n")
 
 
 ##########################
 ###        Main        ###
 ##########################
 
-print('------------------ Optimal Propeller vsn 7.0.6 ------------------')
-print('| Computation of the optimal dCT/dr and dCP/dr distributions.   |')
-print('| Based on the inviscid theory of the optimal propeller.        |')
-print('|                                                               |')
-print('| This code is used to generate the actuator disk input data    |')
-print('| file needed for the VARIABLE_LOAD actuator disk type          |')
-print('| implemented in SU2 7.0.6.                                     |')
-print('|                                                               |')
-print('| Author: Ettore Saetta, Lorenzo Russo, Renato Tognaccini.      |')
-print('| Theoretical and Applied Aerodynamic Research Group (TAARG),   |')
-print('| University of Naples Federico II.                             |')
-print('-----------------------------------------------------------------')
-print('')
-print('Warning: present version requires input in SI units.')
-print('')
+print("------------------ Optimal Propeller vsn 7.0.6 ------------------")
+print("| Computation of the optimal dCT/dr and dCP/dr distributions.   |")
+print("| Based on the inviscid theory of the optimal propeller.        |")
+print("|                                                               |")
+print("| This code is used to generate the actuator disk input data    |")
+print("| file needed for the VARIABLE_LOAD actuator disk type          |")
+print("| implemented in SU2 7.0.6.                                     |")
+print("|                                                               |")
+print("| Author: Ettore Saetta, Lorenzo Russo, Renato Tognaccini.      |")
+print("| Theoretical and Applied Aerodynamic Research Group (TAARG),   |")
+print("| University of Naples Federico II.                             |")
+print("-----------------------------------------------------------------")
+print("")
+print("Warning: present version requires input in SI units.")
+print("")
 
 # Number of radial stations in input.
-stations = int(input('Number of radial stations: '))
+stations = int(input("Number of radial stations: "))
 
 # Resize the vectors using the number of radial stations.
 r = np.empty(stations)
@@ -136,26 +143,26 @@ def write_external_file(CTrs, CPrs):
 ap_optimal = np.empty(stations)
 
 # Thrust coefficient in input.
-Ct = float(input('\nCT (Renard definition): '))
+Ct = float(input("\nCT (Renard definition): "))
 
 # Propeller radius in input.
-R = float(input('\nR (propeller radius [m]): '))
+R = float(input("\nR (propeller radius [m]): "))
 
 # Hub radius in input.
-rhub = float(input('\nr_hub (hub radius [m]): '))
+rhub = float(input("\nr_hub (hub radius [m]): "))
 
 # Advance ratio in input.
-J = float(input('\nJ (advance ratio): '))
+J = float(input("\nJ (advance ratio): "))
 
 # Freestream velocity in input.
-Vinf = float(input('\nVinf (m/s): '))
+Vinf = float(input("\nVinf (m/s): "))
 
 # Asking if the tip loss Prandtl correction function needs to be used.
-prandtl_input = input('\nUsing tip loss Prandtl correction? (<y>/n): ')
+prandtl_input = input("\nUsing tip loss Prandtl correction? (<y>/n): ")
 
-if prandtl_input.lower() in ['yes', 'y', '']:
+if prandtl_input.lower() in ["yes", "y", ""]:
     # Number of propeller blades in input.
-    N = int(input('\nN (number of propeller blades): '))
+    N = int(input("\nN (number of propeller blades): "))
     prandtl_correction = True
 else:
     prandtl_correction = False
@@ -164,47 +171,54 @@ def write_external_file(CTrs, CPrs):
 rs_hub = rhub / R
 
 # Computation of the non-dimensional radial stations.
-for i in range(1, stations+1):
-    r[i-1] = i / float(stations)
-    if r[i-1] <= rs_hub:
+for i in range(1, stations + 1):
+    r[i - 1] = i / float(stations)
+    if r[i - 1] <= rs_hub:
         i_hub = i - 1
 
 # Computation of the propeller diameter.
 D = 2 * R
 # Computation of the propeller angular velocity (Rounds/s).
-n = Vinf / (D*J)
+n = Vinf / (D * J)
 # Computation of the propeller angular velocity (Rad/s).
 Omega = n * 2 * math.pi
 
 # Computation of the tip loss Prandtl correction function F.
 if prandtl_correction:
-    F = (2/math.pi)*np.arccos(np.exp(-0.5*N*(1-r)*np.sqrt(1+pow(Omega*R/Vinf,2))))
+    F = (2 / math.pi) * np.arccos(
+        np.exp(-0.5 * N * (1 - r) * np.sqrt(1 + pow(Omega * R / Vinf, 2)))
+    )
 else:
     F = np.ones((stations))
 
 # Computation of the non-dimensional radius chi=Omega*r/Vinf.
-chi = Omega*r*R/Vinf
+chi = Omega * r * R / Vinf
 
 
-eps = 5E-20
+eps = 5e-20
 # Computation of the propeller radial stations spacing.
-h = (1.0/stations)
+h = 1.0 / stations
 
 # Computation of the first try induced velocity distribution.
-w = (2/np.power(Vinf,2))*((-1/Vinf)+np.sqrt(1+((np.power(D,4)*(Ct)*np.power(n,2))/(np.power(Vinf,2)*np.pi*r))))
+w = (2 / np.power(Vinf, 2)) * (
+    (-1 / Vinf)
+    + np.sqrt(
+        1 + ((np.power(D, 4) * (Ct) * np.power(n, 2)) / (np.power(Vinf, 2) * np.pi * r))
+    )
+)
 
 # Computation of the first try Lagrange moltiplicator.
-w_0 = sum(w)/(Vinf*stations)
+w_0 = sum(w) / (Vinf * stations)
 
 # Computation of the first try axial interference factor distribution.
 for i in range(0, stations):
-    a_0[i] = a_distribution(w_0*F[i],chi[i])
+    a_0[i] = a_distribution(w_0 * F[i], chi[i])
 
 # Computation of the thrust coefficient distribution
-dCt_0 = math.pi*J**2*r*(1+a_0)*a_0
+dCt_0 = math.pi * J**2 * r * (1 + a_0) * a_0
 
 # Computation of the total thrust coefficient.
-Ct_0 = sum(h*dCt_0[i_hub:])
+Ct_0 = sum(h * dCt_0[i_hub:])
 
 # Compute the error with respect to the thrust coefficient given in input.
 err_0 = Ct_0 - Ct
@@ -216,13 +230,13 @@ def write_external_file(CTrs, CPrs):
 
 # Computation of the second try axial interference factor distribution.
 for i in range(0, stations):
-    a_old[i] = a_distribution(w_old*F[i],chi[i])
+    a_old[i] = a_distribution(w_old * F[i], chi[i])
 
 # Computation of the thrust coefficient distribution
-dCt_old = math.pi*J**2*r*(1+a_old)*a_old
+dCt_old = math.pi * J**2 * r * (1 + a_old) * a_old
 
 # Computation of the total thrust coefficient.
-Ct_old = sum(h*dCt_old[i_hub:])
+Ct_old = sum(h * dCt_old[i_hub:])
 
 # Compute the error with respect to the thrust coefficient given in input.
 err_old = Ct_old - Ct
@@ -239,17 +253,17 @@ def write_external_file(CTrs, CPrs):
     iteration += 1
 
     # Computation of the new Lagrange moltiplicator value based on the false position method.
-    w_new = (w_old*err_0 - w_0*err_old)/(err_0 - err_old)
+    w_new = (w_old * err_0 - w_0 * err_old) / (err_0 - err_old)
 
     # Computation of the new axial interference factor distribution.
     for i in range(0, stations):
-        a_new[i] = a_distribution(w_new*F[i],chi[i])
+        a_new[i] = a_distribution(w_new * F[i], chi[i])
 
     # Computation of the new thrust coefficient distribution.
-    dCt_new = math.pi*J**2*r*(1+a_new)*a_new
+    dCt_new = math.pi * J**2 * r * (1 + a_new) * a_new
 
     # Computation of the new total thrust coefficient.
-    Ct_new = sum(h*dCt_new[i_hub:])
+    Ct_new = sum(h * dCt_new[i_hub:])
 
     # Computation of the total thrust coefficient error with respect to the input value.
     err_new = Ct_new - Ct
@@ -264,46 +278,55 @@ def write_external_file(CTrs, CPrs):
 
 # Computation of the correct axial and rotational interference factors (a and ap).
 for i in range(0, stations):
-    a_optimal[i] = a_distribution(w_new*F[i],chi[i])
-    ap_optimal[i] = (w_new*F[i])*((1+w_new*F[i])/(chi[i]*chi[i]+math.pow(1+w_new*F[i],2)))
+    a_optimal[i] = a_distribution(w_new * F[i], chi[i])
+    ap_optimal[i] = (w_new * F[i]) * (
+        (1 + w_new * F[i]) / (chi[i] * chi[i] + math.pow(1 + w_new * F[i], 2))
+    )
 
 # Computation of the correct thrust coefficient distribution.
-dCt_optimal = math.pi*J**2*r*(1+a_optimal)*a_optimal
+dCt_optimal = math.pi * J**2 * r * (1 + a_optimal) * a_optimal
 
 # Computation of the correct power coefficient distribution.
 for i in range(0, stations):
-    dCp[i] = (R*4*math.pi/(math.pow(n,3)*math.pow(D,5)))*(math.pow(Vinf,3)*math.pow(1+a_optimal[i],2)*a_optimal[i]*r[i]*R+math.pow(Omega,2)*Vinf*(1+a_optimal[i])*math.pow(ap_optimal[i],2)*math.pow(r[i]*R,3))
+    dCp[i] = (R * 4 * math.pi / (math.pow(n, 3) * math.pow(D, 5))) * (
+        math.pow(Vinf, 3) * math.pow(1 + a_optimal[i], 2) * a_optimal[i] * r[i] * R
+        + math.pow(Omega, 2)
+        * Vinf
+        * (1 + a_optimal[i])
+        * math.pow(ap_optimal[i], 2)
+        * math.pow(r[i] * R, 3)
+    )
 
 ##########################
 ###   Check Results    ###
 ##########################
 # Computation of the total power coefficient.
-Cp = sum(h*dCp[i_hub:])
+Cp = sum(h * dCp[i_hub:])
 
 # Computation of the total thrust coefficient.
-Ct_optimal = sum(h*dCt_optimal[i_hub:])
+Ct_optimal = sum(h * dCt_optimal[i_hub:])
 
 # Computation of the static pressure jump distribution.
-DeltaP = dCt_optimal*(2*Vinf**2)/(J**2*math.pi*r)
+DeltaP = dCt_optimal * (2 * Vinf**2) / (J**2 * math.pi * r)
 
 # Computation of the thrust over density (T) using the static pressure jump distribution.
-T = sum(2*math.pi*r[i_hub:]*math.pow(R,2)*h*DeltaP[i_hub:])
+T = sum(2 * math.pi * r[i_hub:] * math.pow(R, 2) * h * DeltaP[i_hub:])
 
 # Computation of the thrust coefficient using T.
-Ct_Renard = T / (math.pow(n,2)*math.pow(D,4))
+Ct_Renard = T / (math.pow(n, 2) * math.pow(D, 4))
 
 # Computation of the efficiency.
-eta = J * (Ct_optimal/Cp)
+eta = J * (Ct_optimal / Cp)
 
 # Screen output used to check that everything worked correcty.
-print('%%%%%%%%%%%%%%%%%%%%%%%%% CHECK OUTPUT VALUES %%%%%%%%%%%%%%%%%%%%%%%%%')
-print(f'       dCT distribution integral: {Ct_optimal:.4f}')
-print(f'       dCT computed using the static pressure jump: {Ct_Renard:.4f}')
-print(f'       dCP distribution integral: {Cp:.4f}')
-print(f'       Thrust over Density (T/rho): {T:.4f} [N*m^3/kg]')
-print(f'       Efficiency eta: {eta:.4f}')
-print(f'       w0/Vinf: {w_new:.4f}')
-print('%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%')
+print("%%%%%%%%%%%%%%%%%%%%%%%%% CHECK OUTPUT VALUES %%%%%%%%%%%%%%%%%%%%%%%%%")
+print(f"       dCT distribution integral: {Ct_optimal:.4f}")
+print(f"       dCT computed using the static pressure jump: {Ct_Renard:.4f}")
+print(f"       dCP distribution integral: {Cp:.4f}")
+print(f"       Thrust over Density (T/rho): {T:.4f} [N*m^3/kg]")
+print(f"       Efficiency eta: {eta:.4f}")
+print(f"       w0/Vinf: {w_new:.4f}")
+print("%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%")
 
 ##########################
 ###    File Writing    ###
@@ -321,29 +344,29 @@ def write_external_file(CTrs, CPrs):
 # Automatically plot the computed propeller performance.
 
 pl.figure(1)
-pl.plot(r, dCt_optimal, 'r', markersize=4, label='$\\frac{dCT}{d\overline{r}}$')
-pl.plot(r, dCp, 'k', markersize=4, label='$\\frac{dCP}{d\overline{r}}$')
+pl.plot(r, dCt_optimal, "r", markersize=4, label="$\\frac{dCT}{d\overline{r}}$")
+pl.plot(r, dCp, "k", markersize=4, label="$\\frac{dCP}{d\overline{r}}$")
 pl.grid(True)
 pl.legend(numpoints=3)
-pl.xlabel('$\overline{r}$')
-pl.ylabel('')
+pl.xlabel("$\overline{r}$")
+pl.ylabel("")
 pl.title("Load Distribution")
 
 pl.figure(2)
-pl.plot(chi, a_optimal, 'r', markersize=4, label='$a$')
-pl.plot(chi, ap_optimal, 'k', markersize=4, label='$a^1$')
+pl.plot(chi, a_optimal, "r", markersize=4, label="$a$")
+pl.plot(chi, ap_optimal, "k", markersize=4, label="$a^1$")
 pl.grid(True)
 pl.legend(numpoints=3)
-pl.xlabel('$\chi$')
-pl.ylabel('')
+pl.xlabel("$\chi$")
+pl.ylabel("")
 pl.title("Interference Factors")
 
 if prandtl_correction:
     pl.figure(3)
-    pl.plot(r, F, 'k', markersize=4)
+    pl.plot(r, F, "k", markersize=4)
     pl.grid(True)
-    pl.xlabel('$\overline{r}$')
-    pl.ylabel('$F(\overline{r})$')
+    pl.xlabel("$\overline{r}$")
+    pl.ylabel("$F(\overline{r})$")
     pl.title("Tip Loss Prandtl Correction Function")
 
 pl.show()
diff --git a/SU2_PY/SU2/__init__.py b/SU2_PY/SU2/__init__.py
index 5bff3570f40..bfb81241707 100644
--- a/SU2_PY/SU2/__init__.py
+++ b/SU2_PY/SU2/__init__.py
@@ -1,7 +1,10 @@
 # SU2/__init__.py
 
+
 class EvaluationFailure(RuntimeError):
     pass
+
+
 class DivergenceFailure(EvaluationFailure):
     pass
 
@@ -20,13 +23,10 @@ class DivergenceFailure(EvaluationFailure):
 try:
     import readline
     import rlcompleter
-    if readline.__doc__ and 'libedit' in readline.__doc__:
+
+    if readline.__doc__ and "libedit" in readline.__doc__:
         readline.parse_and_bind("bind ^I rl_complete")
     else:
         readline.parse_and_bind("tab: complete")
 except:
     pass
-
-
-
-
diff --git a/SU2_PY/SU2/eval/__init__.py b/SU2_PY/SU2/eval/__init__.py
index 58cba7dfb55..5e718795af8 100644
--- a/SU2_PY/SU2/eval/__init__.py
+++ b/SU2_PY/SU2/eval/__init__.py
@@ -1,10 +1,15 @@
-
 from SU2.eval.functions import function as func
 from SU2.eval.functions import aerodynamics, geometry
 from SU2.eval.gradients import gradient as grad
 from SU2.eval.gradients import adjoint, findiff
-from SU2.eval.design import (Design,
-     obj_f, obj_df,
-     con_ceq, con_dceq,
-     con_cieq, con_dcieq,
-     touch, skip)
\ No newline at end of file
+from SU2.eval.design import (
+    Design,
+    obj_f,
+    obj_df,
+    con_ceq,
+    con_dceq,
+    con_cieq,
+    con_dcieq,
+    touch,
+    skip,
+)
diff --git a/SU2_PY/SU2/eval/design.py b/SU2_PY/SU2/eval/design.py
index 82768dcd42f..adc8fb1ab45 100644
--- a/SU2_PY/SU2/eval/design.py
+++ b/SU2_PY/SU2/eval/design.py
@@ -30,9 +30,9 @@
 # ----------------------------------------------------------------------
 
 import os, copy
-from .. import io   as su2io
-from .  import func as su2func
-from .  import grad as su2grad
+from .. import io as su2io
+from . import func as su2func
+from . import grad as su2grad
 from ..io import redirect_folder, save_data
 
 # todo:
@@ -43,166 +43,171 @@
 #  Design Class
 # ----------------------------------------------------------------------
 
+
 class Design(object):
-    """ SU2.eval.Design(config,state=None,folder='DESIGNS/DSN_*')
-
-        Starts a design class, which manages a config and state.
-        Will run design in folder, and with self indexing name if '*' is
-        included in the folder name.
-        Methods are wrappers for SU2.eval.func() and SU2.eval.grad()
-
-        Attributes:
-            state  - design state
-            config - design config
-            files  - design files
-            folder - design folder
-            funcs  - design function value bunch
-            grads  - design gradient values bunch
-
-        Methods:
-            Optimizer Interface
-            The following methods take a design vector for input
-            as a list (shape n) or numpy array (shape n or nx1 or 1xn).
-            Values are returned as floats or lists or lists of lists.
-            See SU2.eval.obj_f, etc for more detail.
-
-            obj_f(dvs)     - objective function              : float
-            obj_df(dvs)    - objective function derivatives  : list
-            con_ceq(dvs)   - equality constraints            : list
-            con_dceq(dvs)  - equality constraint derivatives : list[list]
-            con_cieq(dvs)  - inequality constraints          : list
-            con_dcieq(dvs) - inequality constraint gradients : list[list]
-
-            Functional Interface
-            The following methods take an objective function name for input.
-            func(func_name)                  - function of specified name
-            grad(func_name,method='CONTINUOUS_ADJOINT') - gradient of specified name
+    """SU2.eval.Design(config,state=None,folder='DESIGNS/DSN_*')
+
+    Starts a design class, which manages a config and state.
+    Will run design in folder, and with self indexing name if '*' is
+    included in the folder name.
+    Methods are wrappers for SU2.eval.func() and SU2.eval.grad()
+
+    Attributes:
+        state  - design state
+        config - design config
+        files  - design files
+        folder - design folder
+        funcs  - design function value bunch
+        grads  - design gradient values bunch
+
+    Methods:
+        Optimizer Interface
+        The following methods take a design vector for input
+        as a list (shape n) or numpy array (shape n or nx1 or 1xn).
+        Values are returned as floats or lists or lists of lists.
+        See SU2.eval.obj_f, etc for more detail.
+
+        obj_f(dvs)     - objective function              : float
+        obj_df(dvs)    - objective function derivatives  : list
+        con_ceq(dvs)   - equality constraints            : list
+        con_dceq(dvs)  - equality constraint derivatives : list[list]
+        con_cieq(dvs)  - inequality constraints          : list
+        con_dcieq(dvs) - inequality constraint gradients : list[list]
+
+        Functional Interface
+        The following methods take an objective function name for input.
+        func(func_name)                  - function of specified name
+        grad(func_name,method='CONTINUOUS_ADJOINT') - gradient of specified name
     """
 
-    def __init__(self, config, state=None, folder='DESIGNS/DSN_*'):
-        """ Initializes an SU2 Design """
+    def __init__(self, config, state=None, folder="DESIGNS/DSN_*"):
+        """Initializes an SU2 Design"""
 
         ## ???: Move to Project, no next folder here
 
-        if '*' in folder: folder = su2io.next_folder(folder)
+        if "*" in folder:
+            folder = su2io.next_folder(folder)
 
         config = copy.deepcopy(config)
-        state  = copy.deepcopy(state)
-        state  = su2io.State(state)
+        state = copy.deepcopy(state)
+        state = su2io.State(state)
         state.find_files(config)
 
         self.config = config
-        self.state  = state
-        self.files  = state.FILES
-        self.funcs  = state.FUNCTIONS
-        self.grads  = state.GRADIENTS
+        self.state = state
+        self.files = state.FILES
+        self.funcs = state.FUNCTIONS
+        self.grads = state.GRADIENTS
         self.folder = folder
 
-        self.filename = 'design.pkl'
+        self.filename = "design.pkl"
 
         # initialize folder with files
-        pull,link = state.pullnlink(config)
-        with redirect_folder(folder,pull,link,force=True):
+        pull, link = state.pullnlink(config)
+        with redirect_folder(folder, pull, link, force=True):
             # save design, config
-            save_data(self.filename,self)
-            config.dump('config_DSN.cfg')
+            save_data(self.filename, self)
+            config.dump("config_DSN.cfg")
 
-    def _eval(self,eval_func,*args):
-        """ Evaluates an SU2 Design
-            always adds config and state to the inputs list
+    def _eval(self, eval_func, *args):
+        """Evaluates an SU2 Design
+        always adds config and state to the inputs list
         """
 
         config = self.config
-        state  = self.state
-        files  = self.files
+        state = self.state
+        files = self.files
         folder = self.folder
 
         filename = self.filename
 
         # check folder
-        assert os.path.exists(folder) , 'cannot find design folder %s' % folder
+        assert os.path.exists(folder), "cannot find design folder %s" % folder
 
         konfig = copy.deepcopy(config)
 
-        '''
+        """
         If the time convergence criterion was activated, we have less time iterations.
         Store the changed values of TIME_ITER, ITER_AVERAGE_OBJ and UNST_ADJOINT_ITER in
-        state.WND_CAUCHY_DATA'''
-        if 'TIME_ITER' in state.WND_CAUCHY_DATA:         # Use Convergence data, if we have already a direct run
-            konfig['TIME_ITER'] = state.WND_CAUCHY_DATA['TIME_ITER']
-            konfig['ITER_AVERAGE_OBJ'] = state.WND_CAUCHY_DATA['ITER_AVERAGE_OBJ']
-            konfig['UNST_ADJOINT_ITER'] = state.WND_CAUCHY_DATA['UNST_ADJOINT_ITER']
+        state.WND_CAUCHY_DATA"""
+        if (
+            "TIME_ITER" in state.WND_CAUCHY_DATA
+        ):  # Use Convergence data, if we have already a direct run
+            konfig["TIME_ITER"] = state.WND_CAUCHY_DATA["TIME_ITER"]
+            konfig["ITER_AVERAGE_OBJ"] = state.WND_CAUCHY_DATA["ITER_AVERAGE_OBJ"]
+            konfig["UNST_ADJOINT_ITER"] = state.WND_CAUCHY_DATA["UNST_ADJOINT_ITER"]
 
         # list files to pull and link
-        pull,link = state.pullnlink(konfig)
+        pull, link = state.pullnlink(konfig)
 
         # output redirection, don't re-pull files
-        with redirect_folder(folder,pull,link,force=False) as push:
+        with redirect_folder(folder, pull, link, force=False) as push:
 
             # get timestamp
             timestamp = state.tic()
 
             # run
-            inputs = args + (config,state)
+            inputs = args + (config, state)
             vals = eval_func(*inputs)
 
             # save design
             if state.toc(timestamp):
-                save_data(filename,self)
+                save_data(filename, self)
 
         #: with redirect folder
 
         # update files
-        files.update(state['FILES'])
+        files.update(state["FILES"])
 
         return vals
 
-    def obj_f(self,dvs):
-        """ Evaluates SU2 Design Objectives """
-        return self._eval(obj_f,dvs)
+    def obj_f(self, dvs):
+        """Evaluates SU2 Design Objectives"""
+        return self._eval(obj_f, dvs)
 
-    def obj_df(self,dvs):
-        """ Evaluates SU2 Design Objective Gradients """
-        return self._eval(obj_df,dvs)
+    def obj_df(self, dvs):
+        """Evaluates SU2 Design Objective Gradients"""
+        return self._eval(obj_df, dvs)
 
-    def con_ceq(self,dvs):
-        """ Evaluates SU2 Design Equality Constraints """
-        return self._eval(con_ceq,dvs)
+    def con_ceq(self, dvs):
+        """Evaluates SU2 Design Equality Constraints"""
+        return self._eval(con_ceq, dvs)
 
-    def con_dceq(self,dvs):
-        """ Evaluates SU2 Design Equality Constraint Gradients """
-        return self._eval(con_dceq,dvs)
+    def con_dceq(self, dvs):
+        """Evaluates SU2 Design Equality Constraint Gradients"""
+        return self._eval(con_dceq, dvs)
 
-    def con_cieq(self,dvs):
-        """ Evaluates SU2 Design Inequality Constraints """
-        return self._eval(con_cieq,dvs)
+    def con_cieq(self, dvs):
+        """Evaluates SU2 Design Inequality Constraints"""
+        return self._eval(con_cieq, dvs)
 
-    def con_dcieq(self,dvs):
-        """ Evaluates SU2 Design Inequality Constraint Gradients """
-        return self._eval(con_dcieq,dvs)
+    def con_dcieq(self, dvs):
+        """Evaluates SU2 Design Inequality Constraint Gradients"""
+        return self._eval(con_dcieq, dvs)
 
-    def func(self,func_name):
-        """ Evaluates SU2 Design Functions by Name """
-        return self._eval(su2func,func_name)
+    def func(self, func_name):
+        """Evaluates SU2 Design Functions by Name"""
+        return self._eval(su2func, func_name)
 
-    def grad(self,func_name,method='CONTINUOUS_ADJOINT'):
-        """ Evaluates SU2 Design Gradients by Name """
-        return self._eval(su2grad,func_name,method)
+    def grad(self, func_name, method="CONTINUOUS_ADJOINT"):
+        """Evaluates SU2 Design Gradients by Name"""
+        return self._eval(su2grad, func_name, method)
 
     def touch(self):
         return self._eval(touch)
 
-    def skip(self,*args,**kwarg):
+    def skip(self, *args, **kwarg):
         return self._eval(skip)
 
-
     def __repr__(self):
-        return '<Design> %s' % self.folder
+        return "<Design> %s" % self.folder
+
     def __str__(self):
         output = self.__repr__()
-        output += '\n%s' % self.state
+        output += "\n%s" % self.state
         return output
 
+
 #: class Design()
 
 
@@ -210,178 +215,188 @@ def __str__(self):
 #  Optimization Interface Functions
 # ----------------------------------------------------------------------
 
-def obj_f(dvs,config,state=None):
-    """ val = SU2.eval.obj_f(dvs,config,state=None)
 
-        Evaluates SU2 Objectives
-        Wraps SU2.eval.func()
+def obj_f(dvs, config, state=None):
+    """val = SU2.eval.obj_f(dvs,config,state=None)
+
+    Evaluates SU2 Objectives
+    Wraps SU2.eval.func()
 
-        Takes a design vector for input as a list (shape n)
-        or numpy array (shape n or nx1 or 1xn), a config
-        and optionally a state.
+    Takes a design vector for input as a list (shape n)
+    or numpy array (shape n or nx1 or 1xn), a config
+    and optionally a state.
 
-        Outputs a float.
+    Outputs a float.
     """
 
     # unpack config and state
     config.unpack_dvs(dvs)
     state = su2io.State(state)
 
-    def_objs = config['OPT_OBJECTIVE']
+    def_objs = config["OPT_OBJECTIVE"]
     objectives = def_objs.keys()
 
     # evaluate each objective
     vals_out = []
     func = 0.0
-    for i_obj,this_obj in enumerate(objectives):
-        scale = def_objs[this_obj]['SCALE']
-        global_factor = float(config['OPT_GRADIENT_FACTOR'])
-        sign  = su2io.get_objectiveSign(this_obj)
+    for i_obj, this_obj in enumerate(objectives):
+        scale = def_objs[this_obj]["SCALE"]
+        global_factor = float(config["OPT_GRADIENT_FACTOR"])
+        sign = su2io.get_objectiveSign(this_obj)
 
         # Evaluate Objective Function scaling and sign
         # If default evaluate as normal,
-        if def_objs[this_obj]['OBJTYPE']=='DEFAULT':
-            func += su2func(this_obj,config,state) * sign * scale * global_factor
+        if def_objs[this_obj]["OBJTYPE"] == "DEFAULT":
+            func += su2func(this_obj, config, state) * sign * scale * global_factor
         # otherwise evaluate the penalty function (OBJTYPE = '>','<', or '=')
         else:
-            func += obj_p(config,state,this_obj,def_objs) * scale
+            func += obj_p(config, state, this_obj, def_objs) * scale
     vals_out.append(func)
 
     #: for each objective
     # If evaluating the combined function is desired, update it here.
     # This is only used when OPT_COMBINE_OBJECTIVE = YES
-    if 'COMBO' in state.FUNCTIONS:
-        state['FUNCTIONS']['COMBO'] = func
+    if "COMBO" in state.FUNCTIONS:
+        state["FUNCTIONS"]["COMBO"] = func
 
     return vals_out
 
+
 #: def obj_f()
 
-def obj_p(config,state,this_obj,def_objs):
+
+def obj_p(config, state, this_obj, def_objs):
     # Penalty function: square of the difference between value and limit
     # This function is used when a constraint-type term is added to OPT_OBJECTIVE
     # This code, and obj_dp, must be changed to use a non-quadratic penalty function
-    funcval = su2func(this_obj,config,state)
-    constraint = float(def_objs[this_obj]['VALUE'])
+    funcval = su2func(this_obj, config, state)
+    constraint = float(def_objs[this_obj]["VALUE"])
     penalty = 0.0
-    if (def_objs[this_obj]['OBJTYPE']=='=' or \
-        (def_objs[this_obj]['OBJTYPE']=='>' and funcval < constraint) or \
-        (def_objs[this_obj]['OBJTYPE']=='<' and funcval > constraint )):
-        penalty = (constraint - funcval)**2.0
+    if (
+        def_objs[this_obj]["OBJTYPE"] == "="
+        or (def_objs[this_obj]["OBJTYPE"] == ">" and funcval < constraint)
+        or (def_objs[this_obj]["OBJTYPE"] == "<" and funcval > constraint)
+    ):
+        penalty = (constraint - funcval) ** 2.0
     # If 'DEFAULT' objtype this returns the function value.
     else:
         penalty = funcval
     return penalty
 
+
 #: def obj_p()
 
-def obj_dp(config,state,this_obj,def_objs):
+
+def obj_dp(config, state, this_obj, def_objs):
     # Partial Derivative of Penalty function: square of the difference between value and limit
     # This function is used when a constraint-type term is added to OPT_OBJECTIVE
     # This code, and obj_p, must be changed to use a non-quadratic penalty function
-    funcval = su2func(this_obj,config,state)
-    constraint = float(def_objs[this_obj]['VALUE'])
-    dpenalty=0.0
+    funcval = su2func(this_obj, config, state)
+    constraint = float(def_objs[this_obj]["VALUE"])
+    dpenalty = 0.0
 
     # Inequalities will be 0 or a positive value
-    if ((def_objs[this_obj]['OBJTYPE']=='>' and funcval < constraint)  or\
-         (def_objs[this_obj]['OBJTYPE']=='<' and funcval > constraint )):
-        dpenalty=2.0*abs(constraint - funcval)
+    if (def_objs[this_obj]["OBJTYPE"] == ">" and funcval < constraint) or (
+        def_objs[this_obj]["OBJTYPE"] == "<" and funcval > constraint
+    ):
+        dpenalty = 2.0 * abs(constraint - funcval)
     # Equalities dp will be positive if value>constraint, negative if value<constraint
-    elif (def_objs[this_obj]['OBJTYPE']=='='):
-        dpenalty=2.0*(funcval -constraint)
+    elif def_objs[this_obj]["OBJTYPE"] == "=":
+        dpenalty = 2.0 * (funcval - constraint)
     # If 'DEFAULT' objtype, this will return 1.0
-    elif (def_objs[this_obj]['OBJTYPE']=='DEFAULT'):
+    elif def_objs[this_obj]["OBJTYPE"] == "DEFAULT":
         dpenalty = 1.0
 
-
     return dpenalty
 
+
 #: def obj_dp()
 
-def obj_df(dvs,config,state=None):
-    """ vals = SU2.eval.obj_df(dvs,config,state=None)
 
-        Evaluates SU2 Objective Gradients
-        Wraps SU2.eval.grad()
+def obj_df(dvs, config, state=None):
+    """vals = SU2.eval.obj_df(dvs,config,state=None)
+
+    Evaluates SU2 Objective Gradients
+    Wraps SU2.eval.grad()
 
-        Takes a design vector for input as a list (shape n)
-        or numpy array (shape n or nx1 or 1xn), a config
-        and optionally a state.
+    Takes a design vector for input as a list (shape n)
+    or numpy array (shape n or nx1 or 1xn), a config
+    and optionally a state.
 
-        Outputs a list of gradients.
+    Outputs a list of gradients.
     """
 
     # unpack config and state
     config.unpack_dvs(dvs)
     state = su2io.State(state)
-    grad_method = config.get('GRADIENT_METHOD','CONTINUOUS_ADJOINT')
+    grad_method = config.get("GRADIENT_METHOD", "CONTINUOUS_ADJOINT")
 
-    def_objs    = config['OPT_OBJECTIVE']
-    objectives  = def_objs.keys()
+    def_objs = config["OPT_OBJECTIVE"]
+    objectives = def_objs.keys()
 
     # Number of objective functionals
-    n_obj       = len( objectives )
+    n_obj = len(objectives)
     # Whether to calculate gradients one-by-one or all-at-once
-    combine_obj = (config['OPT_COMBINE_OBJECTIVE']=="YES")
+    combine_obj = config["OPT_COMBINE_OBJECTIVE"] == "YES"
 
-    dv_scales = config['DEFINITION_DV']['SCALE']
-    dv_size   = config['DEFINITION_DV']['SIZE']
+    dv_scales = config["DEFINITION_DV"]["SCALE"]
+    dv_size = config["DEFINITION_DV"]["SIZE"]
 
     # evaluate each objective
     vals_out = []
-    if (combine_obj and n_obj>1):
+    if combine_obj and n_obj > 1:
         # Evaluate objectives all-at-once; for adjoint methods this results in a
         # single, combined objective.
-        scale = [1.0]*n_obj
-        obj_list=['DRAG']*n_obj
-        for i_obj,this_obj in enumerate(objectives):
-            obj_list[i_obj]=this_obj
-            scale[i_obj] = def_objs[this_obj]['SCALE']
-            if def_objs[this_obj]['OBJTYPE']== 'DEFAULT':
+        scale = [1.0] * n_obj
+        obj_list = ["DRAG"] * n_obj
+        for i_obj, this_obj in enumerate(objectives):
+            obj_list[i_obj] = this_obj
+            scale[i_obj] = def_objs[this_obj]["SCALE"]
+            if def_objs[this_obj]["OBJTYPE"] == "DEFAULT":
                 # Standard case
                 sign = su2io.get_objectiveSign(this_obj)
                 scale[i_obj] *= sign
             else:
                 # For a penalty function, the term is scaled by the partial derivative
                 # d p(j) / dx = (dj / dx) * ( dp / dj)
-                scale[i_obj]*=obj_dp(config, state, this_obj, def_objs)
+                scale[i_obj] *= obj_dp(config, state, this_obj, def_objs)
 
-        config['OBJECTIVE_WEIGHT']=','.join(map(str,scale))
-        grad= su2grad(obj_list,grad_method,config,state)
+        config["OBJECTIVE_WEIGHT"] = ",".join(map(str, scale))
+        grad = su2grad(obj_list, grad_method, config, state)
         # scaling : obj scale  and sign are accounted for in combo gradient, dv scale now applied
-        global_factor = float(config['OPT_GRADIENT_FACTOR'])
+        global_factor = float(config["OPT_GRADIENT_FACTOR"])
         k = 0
-        for i_dv,dv_scl in enumerate(dv_scales):
+        for i_dv, dv_scl in enumerate(dv_scales):
             for i_grd in range(dv_size[i_dv]):
-                grad[k] = grad[k]*global_factor / dv_scl
+                grad[k] = grad[k] * global_factor / dv_scl
                 k = k + 1
 
         vals_out.append(grad)
     else:
         # Evaluate objectives one-by-one
-        marker_monitored = config['MARKER_MONITORING']
-        for i_obj,this_obj in enumerate(objectives):
+        marker_monitored = config["MARKER_MONITORING"]
+        for i_obj, this_obj in enumerate(objectives):
             # For multiple objectives are evaluated one-by-one rather than combined
             # MARKER_MONITORING should be updated to only include the marker for i_obj
             # For single objectives, multiple markers can be used
-            if (n_obj>1): config['MARKER_MONITORING'] = marker_monitored[i_obj]
-            scale = def_objs[this_obj]['SCALE']
-            global_factor = float(config['OPT_GRADIENT_FACTOR'])
-            sign  = su2io.get_objectiveSign(this_obj)
-            if def_objs[this_obj]['OBJTYPE']!= 'DEFAULT':
+            if n_obj > 1:
+                config["MARKER_MONITORING"] = marker_monitored[i_obj]
+            scale = def_objs[this_obj]["SCALE"]
+            global_factor = float(config["OPT_GRADIENT_FACTOR"])
+            sign = su2io.get_objectiveSign(this_obj)
+            if def_objs[this_obj]["OBJTYPE"] != "DEFAULT":
                 # For a penalty function, the term is scaled by the partial derivative
                 # and the sign is always positive
                 # d p(j) / dx = (dj / dx) * ( dp / dj)
-                scale*=obj_dp(config, state, this_obj, def_objs)
+                scale *= obj_dp(config, state, this_obj, def_objs)
                 sign = 1.0
 
             # Evaluate Objective Gradient
-            grad = su2grad(this_obj,grad_method,config,state)
+            grad = su2grad(this_obj, grad_method, config, state)
 
             # scaling and sign
             k = 0
-            for i_dv,dv_scl in enumerate(dv_scales):
+            for i_dv, dv_scl in enumerate(dv_scales):
                 for i_grd in range(dv_size[i_dv]):
                     grad[k] = grad[k] * sign * scale * global_factor / dv_scl
                     k = k + 1
@@ -392,38 +407,40 @@ def obj_df(dvs,config,state=None):
 
     return vals_out
 
+
 #: def obj_df()
 
-def con_ceq(dvs,config,state=None):
-    """ vals = SU2.eval.con_ceq(dvs,config,state=None)
 
-        Evaluates SU2 Equality Constraints
-        Wraps SU2.eval.func()
+def con_ceq(dvs, config, state=None):
+    """vals = SU2.eval.con_ceq(dvs,config,state=None)
+
+    Evaluates SU2 Equality Constraints
+    Wraps SU2.eval.func()
 
-        Takes a design vector for input as a list (shape n)
-        or numpy array (shape n or nx1 or 1xn), a config
-        and optionally a state.
+    Takes a design vector for input as a list (shape n)
+    or numpy array (shape n or nx1 or 1xn), a config
+    and optionally a state.
 
-        Returns: a list of constraint values, ordered
-        by the OPT_CONSTRAINT config parameter.
+    Returns: a list of constraint values, ordered
+    by the OPT_CONSTRAINT config parameter.
     """
 
     # unpack state and config
     config.unpack_dvs(dvs)
     state = su2io.State(state)
 
-    def_cons = config['OPT_CONSTRAINT']['EQUALITY']
+    def_cons = config["OPT_CONSTRAINT"]["EQUALITY"]
     constraints = def_cons.keys()
 
     # evaluate each constraint
     vals_out = []
-    for i_obj,this_con in enumerate(constraints):
-        global_factor = float(config['OPT_GRADIENT_FACTOR'])
-        push  = def_cons[this_con]['SCALE']
-        value = def_cons[this_con]['VALUE']
+    for i_obj, this_con in enumerate(constraints):
+        global_factor = float(config["OPT_GRADIENT_FACTOR"])
+        push = def_cons[this_con]["SCALE"]
+        value = def_cons[this_con]["VALUE"]
 
         # Evaluate Constraint Function
-        func = su2func(this_con,config,state)
+        func = su2func(this_con, config, state)
 
         # scaling and centering
         func = (func - value) * global_factor * push
@@ -434,45 +451,47 @@ def con_ceq(dvs,config,state=None):
 
     return vals_out
 
+
 #: def obj_ceq()
 
-def con_dceq(dvs,config,state=None):
-    """ vals = SU2.eval.con_dceq(dvs,config,state=None)
 
-        Evaluates SU2 Equality Constraint Gradients
-        Wraps SU2.eval.grad()
+def con_dceq(dvs, config, state=None):
+    """vals = SU2.eval.con_dceq(dvs,config,state=None)
+
+    Evaluates SU2 Equality Constraint Gradients
+    Wraps SU2.eval.grad()
 
-        Takes a design vector for input as a list (shape n)
-        or numpy array (shape n or nx1 or 1xn), a config
-        and optionally a state.
+    Takes a design vector for input as a list (shape n)
+    or numpy array (shape n or nx1 or 1xn), a config
+    and optionally a state.
 
-        Returns a list of lists of constraint gradients,
-        ordered by the OPT_CONSTRAINT config parameter.
+    Returns a list of lists of constraint gradients,
+    ordered by the OPT_CONSTRAINT config parameter.
     """
 
     # unpack state and config
     config.unpack_dvs(dvs)
     state = su2io.State(state)
-    grad_method = config.get('GRADIENT_METHOD','CONTINUOUS_ADJOINT')
+    grad_method = config.get("GRADIENT_METHOD", "CONTINUOUS_ADJOINT")
 
-    def_cons = config['OPT_CONSTRAINT']['EQUALITY']
+    def_cons = config["OPT_CONSTRAINT"]["EQUALITY"]
     constraints = def_cons.keys()
 
-    dv_scales = config['DEFINITION_DV']['SCALE']
-    dv_size   = config['DEFINITION_DV']['SIZE']
+    dv_scales = config["DEFINITION_DV"]["SCALE"]
+    dv_size = config["DEFINITION_DV"]["SIZE"]
 
     # evaluate each constraint
     vals_out = []
-    for i_obj,this_con in enumerate(constraints):
-        global_factor = float(config['OPT_GRADIENT_FACTOR'])
-        value = def_cons[this_con]['VALUE']
+    for i_obj, this_con in enumerate(constraints):
+        global_factor = float(config["OPT_GRADIENT_FACTOR"])
+        value = def_cons[this_con]["VALUE"]
 
         # Evaluate Constraint Gradient
-        grad = su2grad(this_con,grad_method,config,state)
+        grad = su2grad(this_con, grad_method, config, state)
 
         # scaling
         k = 0
-        for i_dv,dv_scl in enumerate(dv_scales):
+        for i_dv, dv_scl in enumerate(dv_scales):
             for i_grd in range(dv_size[i_dv]):
                 grad[k] = grad[k] * global_factor / dv_scl
                 k = k + 1
@@ -483,41 +502,43 @@ def con_dceq(dvs,config,state=None):
 
     return vals_out
 
+
 #: def obj_dceq()
 
-def con_cieq(dvs,config,state=None):
-    """ vals = SU2.eval.con_cieq(dvs,config,state=None)
 
-        Evaluates SU2 Inequality Constraints
-        Wraps SU2.eval.func()
-        Convention is con(x)<=0
+def con_cieq(dvs, config, state=None):
+    """vals = SU2.eval.con_cieq(dvs,config,state=None)
 
-        Takes a design vector for input as a list (shape n)
-        or numpy array (shape n or nx1 or 1xn), a config
-        and optionally a state.
+    Evaluates SU2 Inequality Constraints
+    Wraps SU2.eval.func()
+    Convention is con(x)<=0
 
-        Returns a list of constraint gradients, ordered
-        by the OPT_CONSTRAINT config parameter.
+    Takes a design vector for input as a list (shape n)
+    or numpy array (shape n or nx1 or 1xn), a config
+    and optionally a state.
+
+    Returns a list of constraint gradients, ordered
+    by the OPT_CONSTRAINT config parameter.
     """
 
     # unpack state and config
     config.unpack_dvs(dvs)
     state = su2io.State(state)
 
-    def_cons = config['OPT_CONSTRAINT']['INEQUALITY']
+    def_cons = config["OPT_CONSTRAINT"]["INEQUALITY"]
     constraints = def_cons.keys()
 
     # evaluate each constraint
     vals_out = []
-    for i_obj,this_con in enumerate(constraints):
-        global_factor = float(config['OPT_GRADIENT_FACTOR'])
-        push  = def_cons[this_con]['SCALE']
-        value = def_cons[this_con]['VALUE']
-        sign  = def_cons[this_con]['SIGN']
-        sign  = su2io.get_constraintSign(sign)
+    for i_obj, this_con in enumerate(constraints):
+        global_factor = float(config["OPT_GRADIENT_FACTOR"])
+        push = def_cons[this_con]["SCALE"]
+        value = def_cons[this_con]["VALUE"]
+        sign = def_cons[this_con]["SIGN"]
+        sign = su2io.get_constraintSign(sign)
 
         # Evaluate Constraint Function
-        func = su2func(this_con,config,state)
+        func = su2func(this_con, config, state)
 
         # scaling and centering
         func = (func - value) * sign * global_factor * push
@@ -528,48 +549,50 @@ def con_cieq(dvs,config,state=None):
 
     return vals_out
 
+
 #: def obj_cieq()
 
-def con_dcieq(dvs,config,state=None):
-    """ vals = SU2.eval.con_dceq(dvs,config,state=None)
 
-        Evaluates SU2 Inequality Constraint Gradients
-        Wraps SU2.eval.grad()
-        Convention is con(x)<=0
+def con_dcieq(dvs, config, state=None):
+    """vals = SU2.eval.con_dceq(dvs,config,state=None)
+
+    Evaluates SU2 Inequality Constraint Gradients
+    Wraps SU2.eval.grad()
+    Convention is con(x)<=0
 
-        Takes a design vector for input as a list (shape n)
-        or numpy array (shape n or nx1 or 1xn), a config
-        and optionally a state.
+    Takes a design vector for input as a list (shape n)
+    or numpy array (shape n or nx1 or 1xn), a config
+    and optionally a state.
 
-        Returns a list of lists of constraint gradients,
-        ordered by the OPT_CONSTRAINT config parameter.
+    Returns a list of lists of constraint gradients,
+    ordered by the OPT_CONSTRAINT config parameter.
     """
 
     # unpack state and config
     config.unpack_dvs(dvs)
     state = su2io.State(state)
-    grad_method = config.get('GRADIENT_METHOD','CONTINUOUS_ADJOINT')
+    grad_method = config.get("GRADIENT_METHOD", "CONTINUOUS_ADJOINT")
 
-    def_cons = config['OPT_CONSTRAINT']['INEQUALITY']
+    def_cons = config["OPT_CONSTRAINT"]["INEQUALITY"]
     constraints = def_cons.keys()
 
-    dv_scales = config['DEFINITION_DV']['SCALE']
-    dv_size   = config['DEFINITION_DV']['SIZE']
+    dv_scales = config["DEFINITION_DV"]["SCALE"]
+    dv_size = config["DEFINITION_DV"]["SIZE"]
 
     # evaluate each constraint
     vals_out = []
-    for i_obj,this_con in enumerate(constraints):
-        global_factor = float(config['OPT_GRADIENT_FACTOR'])
-        value = def_cons[this_con]['VALUE']
-        sign  = def_cons[this_con]['SIGN']
-        sign  = su2io.get_constraintSign(sign)
+    for i_obj, this_con in enumerate(constraints):
+        global_factor = float(config["OPT_GRADIENT_FACTOR"])
+        value = def_cons[this_con]["VALUE"]
+        sign = def_cons[this_con]["SIGN"]
+        sign = su2io.get_constraintSign(sign)
 
         # Evaluate Constraint Gradient
-        grad = su2grad(this_con,grad_method,config,state)
+        grad = su2grad(this_con, grad_method, config, state)
 
         # scaling and sign
         k = 0
-        for i_dv,dv_scl in enumerate(dv_scales):
+        for i_dv, dv_scl in enumerate(dv_scales):
             for i_grd in range(dv_size[i_dv]):
                 grad[k] = grad[k] * sign * global_factor / dv_scl
                 k = k + 1
@@ -580,16 +603,19 @@ def con_dcieq(dvs,config,state=None):
 
     return vals_out
 
+
 #: def obj_dcieq()
 
-def touch(config,state):
-    """ SU2.eval.touch(config,state)
-        resets state timestamp
+
+def touch(config, state):
+    """SU2.eval.touch(config,state)
+    resets state timestamp
     """
     state.set_timestamp()
 
-def skip(config,state):
-    """ SU2.eval.skip(config,state)
-        does nothing
+
+def skip(config, state):
+    """SU2.eval.skip(config,state)
+    does nothing
     """
     pass
diff --git a/SU2_PY/SU2/eval/functions.py b/SU2_PY/SU2/eval/functions.py
index 78bb2f190a2..08dc2f19692 100644
--- a/SU2_PY/SU2/eval/functions.py
+++ b/SU2_PY/SU2/eval/functions.py
@@ -30,8 +30,8 @@
 # ----------------------------------------------------------------------
 
 import os, sys, shutil, copy, time, subprocess
-from .. import run  as su2run
-from .. import io   as su2io
+from .. import run as su2run
+from .. import io as su2io
 from .. import util as su2util
 from ..io import redirect_folder, redirect_output
 
@@ -40,93 +40,101 @@
 #  Main Function Interface
 # ----------------------------------------------------------------------
 
-def function( func_name, config, state=None ):
-    """ val = SU2.eval.func(func_name,config,state=None)
 
-        Evaluates the aerodynamics and geometry functions.
+def function(func_name, config, state=None):
+    """val = SU2.eval.func(func_name,config,state=None)
 
-        Wraps:
-            SU2.eval.aerodynamics()
-            SU2.eval.geometry()
+    Evaluates the aerodynamics and geometry functions.
 
-        Assumptions:
-            Config is already setup for deformation.
-            Mesh need not be deformed.
-            Updates config and state by reference.
-            Redundancy if state.FUNCTIONS is not empty.
+    Wraps:
+        SU2.eval.aerodynamics()
+        SU2.eval.geometry()
 
-        Executes in:
-            ./DIRECT or ./GEOMETRY
+    Assumptions:
+        Config is already setup for deformation.
+        Mesh need not be deformed.
+        Updates config and state by reference.
+        Redundancy if state.FUNCTIONS is not empty.
 
-        Inputs:
-            func_name - SU2 objective function name or 'ALL'
-            config    - an SU2 config
-            state     - optional, an SU2 state
+    Executes in:
+        ./DIRECT or ./GEOMETRY
 
-        Outputs:
-            If func_name is 'ALL', returns a Bunch() of
-            functions with keys of objective function names
-            and values of objective function floats.
-            Otherwise returns a float.
+    Inputs:
+        func_name - SU2 objective function name or 'ALL'
+        config    - an SU2 config
+        state     - optional, an SU2 state
+
+    Outputs:
+        If func_name is 'ALL', returns a Bunch() of
+        functions with keys of objective function names
+        and values of objective function floats.
+        Otherwise returns a float.
     """
 
     # initialize
     state = su2io.State(state)
 
     # check for multiple objectives
-    multi_objective = (type(func_name)==list)
+    multi_objective = type(func_name) == list
 
     # func_name_string is only used to check whether the function has already been evaluated.
     func_name_string = func_name
-    if multi_objective:   func_name_string = func_name[0]
+    if multi_objective:
+        func_name_string = func_name[0]
 
     # redundancy check
-    if not func_name_string in state['FUNCTIONS']:
+    if not func_name_string in state["FUNCTIONS"]:
 
         # Aerodynamics
-        if multi_objective or func_name == 'ALL':
-            aerodynamics( config, state )
+        if multi_objective or func_name == "ALL":
+            aerodynamics(config, state)
 
         elif func_name in su2io.historyOutFields:
-            if su2io.historyOutFields[func_name]['TYPE'] == 'COEFFICIENT' or su2io.historyOutFields[func_name]['TYPE'] == 'D_COEFFICIENT':
-                aerodynamics( config, state )
+            if (
+                su2io.historyOutFields[func_name]["TYPE"] == "COEFFICIENT"
+                or su2io.historyOutFields[func_name]["TYPE"] == "D_COEFFICIENT"
+            ):
+                aerodynamics(config, state)
 
         # Stability
         elif func_name in su2io.optnames_stab:
-            stability( config, state )
+            stability(config, state)
 
         # Multipoint
         elif func_name in su2io.optnames_multi:
-            multipoint( config, state )
+            multipoint(config, state)
 
         # Geometry
         elif func_name in su2io.optnames_geo:
-            geometry( func_name, config, state )
+            geometry(func_name, config, state)
 
         else:
-            raise Exception('unknown function name, %s. Please check config_template.cfg for updated list of function names' % func_name)
+            raise Exception(
+                "unknown function name, %s. Please check config_template.cfg for updated list of function names"
+                % func_name
+            )
 
     #: if not redundant
 
     # prepare output
-    if func_name == 'ALL':
-        func_out = state['FUNCTIONS']
-    elif (multi_objective):
+    if func_name == "ALL":
+        func_out = state["FUNCTIONS"]
+    elif multi_objective:
         # If combine_objective is true, use the 'combo' output.
-        func_out = state['FUNCTIONS']['COMBO']
+        func_out = state["FUNCTIONS"]["COMBO"]
     else:
-        func_out = state['FUNCTIONS'][func_name]
+        func_out = state["FUNCTIONS"][func_name]
 
-    if func_name_string in config['OPT_OBJECTIVE']:
-        marker = config['OPT_OBJECTIVE'][func_name_string]['MARKER']
+    if func_name_string in config["OPT_OBJECTIVE"]:
+        marker = config["OPT_OBJECTIVE"][func_name_string]["MARKER"]
         if func_name_string in su2io.per_surface_map:
-            name = su2io.per_surface_map[func_name_string]+'_'+marker
-            if name in state['FUNCTIONS']:
-                func_out = state['FUNCTIONS'][name]
-
+            name = su2io.per_surface_map[func_name_string] + "_" + marker
+            if name in state["FUNCTIONS"]:
+                func_out = state["FUNCTIONS"][name]
 
     return copy.deepcopy(func_out)
 
+
 #: def function()
 
 
@@ -134,29 +142,30 @@ def function( func_name, config, state=None ):
 #  Aerodynamic Functions
 # ----------------------------------------------------------------------
 
-def aerodynamics( config, state=None ):
-    """ vals = SU2.eval.aerodynamics(config,state=None)
 
-        Evaluates aerodynamics with the following:
-	          SU2.run.deform()
-            SU2.run.direct()
+def aerodynamics(config, state=None):
+    """vals = SU2.eval.aerodynamics(config,state=None)
+
+    Evaluates aerodynamics with the following:
+              SU2.run.deform()
+        SU2.run.direct()
 
-        Assumptions:
-            Config is already setup for deformation.
-            Mesh may or may not be deformed.
-            Updates config and state by reference.
-            Redundancy if state.FUNCTIONS is not empty.
+    Assumptions:
+        Config is already setup for deformation.
+        Mesh may or may not be deformed.
+        Updates config and state by reference.
+        Redundancy if state.FUNCTIONS is not empty.
 
-        Executes in:
-            ./DIRECT
+    Executes in:
+        ./DIRECT
 
-        Inputs:
-            config    - an SU2 config
-            state     - optional, an SU2 state
+    Inputs:
+        config    - an SU2 config
+        state     - optional, an SU2 state
 
-        Outputs:
-            Bunch() of functions with keys of objective function names
-            and values of objective function floats.
+    Outputs:
+        Bunch() of functions with keys of objective function names
+        and values of objective function floats.
     """
 
     # ----------------------------------------------------
@@ -167,16 +176,16 @@ def aerodynamics( config, state=None ):
     state = su2io.State(state)
 
     # Make sure to output aerodynamic coeff.
-    if not 'AERO_COEFF' in config['HISTORY_OUTPUT']:
-        config['HISTORY_OUTPUT'].append('AERO_COEFF')
+    if not "AERO_COEFF" in config["HISTORY_OUTPUT"]:
+        config["HISTORY_OUTPUT"].append("AERO_COEFF")
 
-    if not 'MESH' in state.FILES:
-        state.FILES.MESH = config['MESH_FILENAME']
+    if not "MESH" in state.FILES:
+        state.FILES.MESH = config["MESH_FILENAME"]
     special_cases = su2io.get_specialCases(config)
 
     # console output
-    if config.get('CONSOLE','VERBOSE') in ['QUIET','CONCISE']:
-        log_direct = 'log_Direct.out'
+    if config.get("CONSOLE", "VERBOSE") in ["QUIET", "CONCISE"]:
+        log_direct = "log_Direct.out"
     else:
         log_direct = None
 
@@ -185,13 +194,13 @@ def aerodynamics( config, state=None ):
     # ----------------------------------------------------
 
     # does decomposition and deformation
-    info = update_mesh(config,state)
+    info = update_mesh(config, state)
 
     # ----------------------------------------------------
     #  Adaptation (not implemented)
     # ----------------------------------------------------
 
-    #if not state.['ADAPTED_FUNC']:
+    # if not state.['ADAPTED_FUNC']:
     #    config = su2run.adaptation(config)
     #    state['ADAPTED_FUNC'] = True
 
@@ -200,7 +209,7 @@ def aerodynamics( config, state=None ):
     # ----------------------------------------------------
     opt_names = []
     for key in su2io.historyOutFields:
-        if su2io.historyOutFields[key]['TYPE'] == 'COEFFICIENT':
+        if su2io.historyOutFields[key]["TYPE"] == "COEFFICIENT":
             opt_names.append(key)
 
     # redundancy check
@@ -216,104 +225,108 @@ def aerodynamics( config, state=None ):
 
     # files to pull
     files = state.FILES
-    pull = []; link = []
+    pull = []
+    link = []
 
     # files: mesh
-    name = files['MESH']
-    name = su2io.expand_part(name,config)
+    name = files["MESH"]
+    name = su2io.expand_part(name, config)
     link.extend(name)
 
-    pull.extend(config.get('CONFIG_LIST',[]))
+    pull.extend(config.get("CONFIG_LIST", []))
 
     # files: restarts
-    if config.get('TIME_DOMAIN', 'NO') == 'YES' and config.get('RESTART_SOL','NO') =='YES':
-        if  'RESTART_FILE_1' in files: # not the case for directdiff restart
-            name = files['RESTART_FILE_1']
+    if (
+        config.get("TIME_DOMAIN", "NO") == "YES"
+        and config.get("RESTART_SOL", "NO") == "YES"
+    ):
+        if "RESTART_FILE_1" in files:  # not the case for directdiff restart
+            name = files["RESTART_FILE_1"]
             name = su2io.expand_part(name, config)
             link.extend(name)
-        if 'RESTART_FILE_2' in files:  # not the case for 1st order time stepping
-            name = files['RESTART_FILE_2']
+        if "RESTART_FILE_2" in files:  # not the case for 1st order time stepping
+            name = files["RESTART_FILE_2"]
             name = su2io.expand_part(name, config)
             link.extend(name)
 
-    if 'FLOW_META' in files:
-        pull.append(files['FLOW_META'])
+    if "FLOW_META" in files:
+        pull.append(files["FLOW_META"])
 
     # files: direct solution
-    if 'DIRECT' in files:
-        name = files['DIRECT']
+    if "DIRECT" in files:
+        name = files["DIRECT"]
         name = su2io.expand_zones(name, config)
-        name = su2io.expand_time(name,config)
-        link.extend( name )
+        name = su2io.expand_time(name, config)
+        link.extend(name)
         ##config['RESTART_SOL'] = 'YES' # don't override config file
     else:
-        if config.get('TIME_DOMAIN', 'NO') != 'YES': #rules out steady state optimization special cases.
-            config['RESTART_SOL'] = 'NO' #for shape optimization with restart files.
+        if (
+            config.get("TIME_DOMAIN", "NO") != "YES"
+        ):  # rules out steady state optimization special cases.
+            config["RESTART_SOL"] = "NO"  # for shape optimization with restart files.
 
     # files: target equivarea distribution
-    if ( 'EQUIV_AREA' in special_cases and
-         'TARGET_EA' in files ) :
-        pull.append( files['TARGET_EA'] )
+    if "EQUIV_AREA" in special_cases and "TARGET_EA" in files:
+        pull.append(files["TARGET_EA"])
 
     # files: target pressure distribution
-    if ( 'INV_DESIGN_CP' in special_cases and
-         'TARGET_CP' in files ) :
-        pull.append( files['TARGET_CP'] )
+    if "INV_DESIGN_CP" in special_cases and "TARGET_CP" in files:
+        pull.append(files["TARGET_CP"])
 
     # files: target heat flux distribution
-    if ( 'INV_DESIGN_HEATFLUX' in special_cases and
-         'TARGET_HEATFLUX' in files ) :
-        pull.append( files['TARGET_HEATFLUX'] )
-
+    if "INV_DESIGN_HEATFLUX" in special_cases and "TARGET_HEATFLUX" in files:
+        pull.append(files["TARGET_HEATFLUX"])
 
     # output redirection
-    with redirect_folder( 'DIRECT', pull, link ) as push:
+    with redirect_folder("DIRECT", pull, link) as push:
         with redirect_output(log_direct):
 
             # # RUN DIRECT SOLUTION # #
             info = su2run.direct(config)
 
-
-
             konfig = copy.deepcopy(config)
-            '''
+            """
             If the time convergence criterion was activated, we have less time iterations.
             Store the changed values of TIME_ITER, ITER_AVERAGE_OBJ and UNST_ADJOINT_ITER in
-            info.WND_CAUCHY_DATA'''
-            if konfig.get('WINDOW_CAUCHY_CRIT', 'NO') == 'YES' and konfig.TIME_MARCHING != 'NO':  # Tranfer Convergence Data, if necessary
-                konfig['TIME_ITER']         = info.WND_CAUCHY_DATA['TIME_ITER']
-                konfig['ITER_AVERAGE_OBJ']  = info.WND_CAUCHY_DATA['ITER_AVERAGE_OBJ']
-                konfig['UNST_ADJOINT_ITER'] = info.WND_CAUCHY_DATA['UNST_ADJOINT_ITER']
-
-            su2io.restart2solution(konfig,info)
+            info.WND_CAUCHY_DATA"""
+            if (
+                konfig.get("WINDOW_CAUCHY_CRIT", "NO") == "YES"
+                and konfig.TIME_MARCHING != "NO"
+            ):  # Tranfer Convergence Data, if necessary
+                konfig["TIME_ITER"] = info.WND_CAUCHY_DATA["TIME_ITER"]
+                konfig["ITER_AVERAGE_OBJ"] = info.WND_CAUCHY_DATA["ITER_AVERAGE_OBJ"]
+                konfig["UNST_ADJOINT_ITER"] = info.WND_CAUCHY_DATA["UNST_ADJOINT_ITER"]
+
+            su2io.restart2solution(konfig, info)
             state.update(info)
 
             # direct files to push
-            name = info.FILES['DIRECT']
-            name = su2io.expand_zones(name,konfig)
-            name = su2io.expand_time(name,konfig)
+            name = info.FILES["DIRECT"]
+            name = su2io.expand_zones(name, konfig)
+            name = su2io.expand_time(name, konfig)
             push.extend(name)
 
             # pressure files to push
-            if 'TARGET_CP' in info.FILES:
-                push.append(info.FILES['TARGET_CP'])
+            if "TARGET_CP" in info.FILES:
+                push.append(info.FILES["TARGET_CP"])
 
             # heat flux files to push
-            if 'TARGET_HEATFLUX' in info.FILES:
-                push.append(info.FILES['TARGET_HEATFLUX'])
+            if "TARGET_HEATFLUX" in info.FILES:
+                push.append(info.FILES["TARGET_HEATFLUX"])
 
-            if 'FLOW_META' in info.FILES:
-                push.append(info.FILES['FLOW_META'])
+            if "FLOW_META" in info.FILES:
+                push.append(info.FILES["FLOW_META"])
 
     #: with output redirection
-    su2io.update_persurface(konfig,state)
+    su2io.update_persurface(konfig, state)
     # return output
     funcs = su2util.ordered_bunch()
-    for key in state['FUNCTIONS']:
-            funcs[key] = state['FUNCTIONS'][key]
+    for key in state["FUNCTIONS"]:
+        funcs[key] = state["FUNCTIONS"][key]
 
     return funcs
 
+
 #: def aerodynamics()
 
 
@@ -321,10 +334,10 @@ def aerodynamics( config, state=None ):
 #  Stability Functions
 # ----------------------------------------------------------------------
 
-def stability( config, state=None, step=1e-2 ):
 
+def stability(config, state=None, step=1e-2):
 
-    folder = 'STABILITY' # os.path.join('STABILITY',func_name) #STABILITY/D_MOMENT_Y_D_ALPHA/
+    folder = "STABILITY"  # os.path.join('STABILITY',func_name) #STABILITY/D_MOMENT_Y_D_ALPHA/
 
     # ----------------------------------------------------
     #  Initialize
@@ -332,13 +345,13 @@ def stability( config, state=None, step=1e-2 ):
 
     # initialize
     state = su2io.State(state)
-    if not 'MESH' in state.FILES:
-        state.FILES.MESH = config['MESH_FILENAME']
+    if not "MESH" in state.FILES:
+        state.FILES.MESH = config["MESH_FILENAME"]
     special_cases = su2io.get_specialCases(config)
 
     # console output
-    if config.get('CONSOLE','VERBOSE') in ['QUIET','CONCISE']:
-        log_direct = 'log_Direct.out'
+    if config.get("CONSOLE", "VERBOSE") in ["QUIET", "CONCISE"]:
+        log_direct = "log_Direct.out"
     else:
         log_direct = None
 
@@ -346,17 +359,15 @@ def stability( config, state=None, step=1e-2 ):
     #  Update Mesh
     # ----------------------------------------------------
 
-
     # does decomposition and deformation
-    info = update_mesh(config,state)
+    info = update_mesh(config, state)
 
     # ----------------------------------------------------
     #  CENTRAL POINT
     # ----------------------------------------------------
 
     # will run in DIRECT/
-    func_0 = aerodynamics(config,state)
-
+    func_0 = aerodynamics(config, state)
 
     # ----------------------------------------------------
     #  Run Forward Point
@@ -364,59 +375,57 @@ def stability( config, state=None, step=1e-2 ):
 
     # files to pull
     files = state.FILES
-    pull = []; link = []
+    pull = []
+    link = []
 
     # files: mesh
-    name = files['MESH']
-    name = su2io.expand_part(name,config)
+    name = files["MESH"]
+    name = su2io.expand_part(name, config)
     link.extend(name)
 
     # files: direct solution
-    if 'DIRECT' in files:
-        name = files['DIRECT']
-        name = su2io.expand_time(name,config)
-        link.extend( name )
+    if "DIRECT" in files:
+        name = files["DIRECT"]
+        name = su2io.expand_time(name, config)
+        link.extend(name)
         ##config['RESTART_SOL'] = 'YES' # don't override config file
     else:
-        config['RESTART_SOL'] = 'NO'
+        config["RESTART_SOL"] = "NO"
 
     # files: target equivarea distribution
-    if ( 'EQUIV_AREA' in special_cases and
-         'TARGET_EA' in files ) :
-        pull.append( files['TARGET_EA'] )
+    if "EQUIV_AREA" in special_cases and "TARGET_EA" in files:
+        pull.append(files["TARGET_EA"])
 
     # files: target pressure distribution
-    if ( 'INV_DESIGN_CP' in special_cases and
-         'TARGET_CP' in files ) :
-        pull.append( files['TARGET_CP'] )
+    if "INV_DESIGN_CP" in special_cases and "TARGET_CP" in files:
+        pull.append(files["TARGET_CP"])
 
     # files: target heat flux distribution
-    if ( 'INV_DESIGN_HEATFLUX' in special_cases and
-         'TARGET_HEATFLUX' in files ) :
-        pull.append( files['TARGET_HEATFLUX'] )
+    if "INV_DESIGN_HEATFLUX" in special_cases and "TARGET_HEATFLUX" in files:
+        pull.append(files["TARGET_HEATFLUX"])
 
     # pull needed files, start folder
-    with redirect_folder( folder, pull, link ) as push:
+    with redirect_folder(folder, pull, link) as push:
         with redirect_output(log_direct):
 
             konfig = copy.deepcopy(config)
-            ztate  = copy.deepcopy(state)
+            ztate = copy.deepcopy(state)
 
             # TODO: GENERALIZE
             konfig.AOA = konfig.AOA + step
             ztate.FUNCTIONS.clear()
 
-            func_1 = aerodynamics(konfig,ztate)
+            func_1 = aerodynamics(konfig, ztate)
 
             ## direct files to store
-            #name = ztate.FILES['DIRECT']
-            #if not 'STABILITY' in state.FILES:
-                #state.FILES.STABILITY = su2io.ordered_bunch()
-            #state.FILES.STABILITY['DIRECT'] = name
+            # name = ztate.FILES['DIRECT']
+            # if not 'STABILITY' in state.FILES:
+            # state.FILES.STABILITY = su2io.ordered_bunch()
+            # state.FILES.STABILITY['DIRECT'] = name
 
             ## equivarea files to store
-            #if 'WEIGHT_NF' in ztate.FILES:
-                #state.FILES.STABILITY['WEIGHT_NF'] = ztate.FILES['WEIGHT_NF']
+            # if 'WEIGHT_NF' in ztate.FILES:
+            # state.FILES.STABILITY['WEIGHT_NF'] = ztate.FILES['WEIGHT_NF']
 
     # ----------------------------------------------------
     #  DIFFERENCING
@@ -424,20 +433,20 @@ def stability( config, state=None, step=1e-2 ):
 
     for derv_name in su2io.optnames_stab:
 
-        matches = [ k for k in su2io.optnames_aero if k in derv_name ]
-        if not len(matches) == 1: continue
+        matches = [k for k in su2io.optnames_aero if k in derv_name]
+        if not len(matches) == 1:
+            continue
         func_name = matches[0]
 
-        obj_func = ( func_1[func_name] - func_0[func_name] ) / step
+        obj_func = (func_1[func_name] - func_0[func_name]) / step
 
         state.FUNCTIONS[derv_name] = obj_func
 
-
     # return output
     funcs = su2util.ordered_bunch()
     for key in su2io.optnames_stab:
-        if key in state['FUNCTIONS']:
-            funcs[key] = state['FUNCTIONS'][key]
+        if key in state["FUNCTIONS"]:
+            funcs[key] = state["FUNCTIONS"][key]
 
     return funcs
 
@@ -446,21 +455,47 @@ def stability( config, state=None, step=1e-2 ):
 #  Multipoint Functions
 # ----------------------------------------------------------------------
 
-def multipoint( config, state=None, step=1e-2 ):
-
-    mach_list = config['MULTIPOINT_MACH_NUMBER'].replace("(", "").replace(")", "").split(',')
-    reynolds_list = config['MULTIPOINT_REYNOLDS_NUMBER'].replace("(", "").replace(")", "").split(',')
-    freestream_temp_list = config['MULTIPOINT_FREESTREAM_TEMPERATURE'].replace("(", "").replace(")", "").split(',')
-    freestream_press_list = config['MULTIPOINT_FREESTREAM_PRESSURE'].replace("(", "").replace(")", "").split(',')
-    aoa_list = config['MULTIPOINT_AOA'].replace("(", "").replace(")", "").split(',')
-    sideslip_list = config['MULTIPOINT_SIDESLIP_ANGLE'].replace("(", "").replace(")", "").split(',')
-    target_cl_list = config['MULTIPOINT_TARGET_CL'].replace("(", "").replace(")", "").split(',')
-    weight_list = config['MULTIPOINT_WEIGHT'].replace("(", "").replace(")", "").split(',')
-    outlet_value_list = config['MULTIPOINT_OUTLET_VALUE'].replace("(", "").replace(")", "").split(',')
+
+def multipoint(config, state=None, step=1e-2):
+
+    mach_list = (
+        config["MULTIPOINT_MACH_NUMBER"].replace("(", "").replace(")", "").split(",")
+    )
+    reynolds_list = (
+        config["MULTIPOINT_REYNOLDS_NUMBER"]
+        .replace("(", "")
+        .replace(")", "")
+        .split(",")
+    )
+    freestream_temp_list = (
+        config["MULTIPOINT_FREESTREAM_TEMPERATURE"]
+        .replace("(", "")
+        .replace(")", "")
+        .split(",")
+    )
+    freestream_press_list = (
+        config["MULTIPOINT_FREESTREAM_PRESSURE"]
+        .replace("(", "")
+        .replace(")", "")
+        .split(",")
+    )
+    aoa_list = config["MULTIPOINT_AOA"].replace("(", "").replace(")", "").split(",")
+    sideslip_list = (
+        config["MULTIPOINT_SIDESLIP_ANGLE"].replace("(", "").replace(")", "").split(",")
+    )
+    target_cl_list = (
+        config["MULTIPOINT_TARGET_CL"].replace("(", "").replace(")", "").split(",")
+    )
+    weight_list = (
+        config["MULTIPOINT_WEIGHT"].replace("(", "").replace(")", "").split(",")
+    )
+    outlet_value_list = (
+        config["MULTIPOINT_OUTLET_VALUE"].replace("(", "").replace(")", "").split(",")
+    )
     solution_flow_list = su2io.expand_multipoint(config.SOLUTION_FILENAME, config)
-    flow_meta_list = su2io.expand_multipoint('flow.meta', config)
-    restart_sol = config['RESTART_SOL']
-    dv_value_old = config['DV_VALUE_OLD'];
+    flow_meta_list = su2io.expand_multipoint("flow.meta", config)
+    restart_sol = config["RESTART_SOL"]
+    dv_value_old = config["DV_VALUE_OLD"]
 
     func = []
     folder = []
@@ -469,11 +504,11 @@ def multipoint( config, state=None, step=1e-2 ):
         folder.append(0)
 
     for i in range(len(weight_list)):
-        folder[i] = 'MULTIPOINT_' + str(i)
+        folder[i] = "MULTIPOINT_" + str(i)
 
     opt_names = []
     for key in su2io.historyOutFields:
-        if su2io.historyOutFields[key]['TYPE'] == 'COEFFICIENT':
+        if su2io.historyOutFields[key]["TYPE"] == "COEFFICIENT":
             opt_names.append(key)
 
     # ----------------------------------------------------
@@ -482,13 +517,13 @@ def multipoint( config, state=None, step=1e-2 ):
 
     # initialize
     state = su2io.State(state)
-    if not 'MESH' in state.FILES:
-        state.FILES.MESH = config['MESH_FILENAME']
+    if not "MESH" in state.FILES:
+        state.FILES.MESH = config["MESH_FILENAME"]
     special_cases = su2io.get_specialCases(config)
 
     # console output
-    if config.get('CONSOLE','VERBOSE') in ['QUIET','CONCISE']:
-        log_direct = 'log_Direct.out'
+    if config.get("CONSOLE", "VERBOSE") in ["QUIET", "CONCISE"]:
+        log_direct = "log_Direct.out"
     else:
         log_direct = None
 
@@ -497,12 +532,12 @@ def multipoint( config, state=None, step=1e-2 ):
     # ----------------------------------------------------
 
     # If multiple meshes specified, use relevant mesh
-    if 'MULTIPOINT_MESH_FILENAME' in state.FILES:
+    if "MULTIPOINT_MESH_FILENAME" in state.FILES:
         state.FILES.MESH = state.FILES.MULTIPOINT_MESH_FILENAME[0]
         config.MESH_FILENAME = state.FILES.MULTIPOINT_MESH_FILENAME[0]
 
     # does decomposition and deformation
-    info = update_mesh(config,state)
+    info = update_mesh(config, state)
 
     # ----------------------------------------------------
     #  FIRST POINT
@@ -517,209 +552,223 @@ def multipoint( config, state=None, step=1e-2 ):
     config.FREESTREAM_TEMPERATURE = freestream_temp_list[0]
     config.FREESTREAM_PRESSURE = freestream_press_list[0]
     config.TARGET_CL = target_cl_list[0]
-    orig_marker_outlet = config['MARKER_OUTLET']
-    orig_marker_outlet = orig_marker_outlet.replace("(", "").replace(")", "").split(',')
+    orig_marker_outlet = config["MARKER_OUTLET"]
+    orig_marker_outlet = orig_marker_outlet.replace("(", "").replace(")", "").split(",")
     new_marker_outlet = "(" + orig_marker_outlet[0] + "," + outlet_value_list[0] + ")"
     config.MARKER_OUTLET = new_marker_outlet
     config.SOLUTION_FILENAME = solution_flow_list[0]
 
     # If solution file for the first point is available, use it
-    if 'MULTIPOINT_DIRECT' in state.FILES and state.FILES.MULTIPOINT_DIRECT[0]:
-        state.FILES['DIRECT'] = state.FILES.MULTIPOINT_DIRECT[0]
+    if "MULTIPOINT_DIRECT" in state.FILES and state.FILES.MULTIPOINT_DIRECT[0]:
+        state.FILES["DIRECT"] = state.FILES.MULTIPOINT_DIRECT[0]
 
     # If flow.meta file for the first point is available, rename it before using it
-    if 'MULTIPOINT_FLOW_META' in state.FILES and state.FILES.MULTIPOINT_FLOW_META[0]:
-        os.rename(state.FILES.MULTIPOINT_FLOW_META[0], 'flow.meta')
-        state.FILES['FLOW_META'] = 'flow.meta'
+    if "MULTIPOINT_FLOW_META" in state.FILES and state.FILES.MULTIPOINT_FLOW_META[0]:
+        os.rename(state.FILES.MULTIPOINT_FLOW_META[0], "flow.meta")
+        state.FILES["FLOW_META"] = "flow.meta"
 
-    func[0] = aerodynamics(config,state)
+    func[0] = aerodynamics(config, state)
 
     # change name of flow.meta back to multipoint name
-    if os.path.exists('flow.meta'):
-        os.rename('flow.meta', flow_meta_list[0])
-        state.FILES['FLOW_META'] = flow_meta_list[0]
+    if os.path.exists("flow.meta"):
+        os.rename("flow.meta", flow_meta_list[0])
+        state.FILES["FLOW_META"] = flow_meta_list[0]
 
     src = os.getcwd()
-    src = os.path.abspath(src).rstrip('/')+'/DIRECT/'
+    src = os.path.abspath(src).rstrip("/") + "/DIRECT/"
 
     # files to pull
     files = state.FILES
-    pull = []; link = []
+    pull = []
+    link = []
 
     # files: mesh
-    name = files['MESH']
-    name = su2io.expand_part(name,config)
+    name = files["MESH"]
+    name = su2io.expand_part(name, config)
     link.extend(name)
 
     # files: direct solution
-    if 'DIRECT' in files:
-        name = files['DIRECT']
-        name = su2io.expand_time(name,config)
-        link.extend( name )
+    if "DIRECT" in files:
+        name = files["DIRECT"]
+        name = su2io.expand_time(name, config)
+        link.extend(name)
     else:
-        config['RESTART_SOL'] = 'NO'
+        config["RESTART_SOL"] = "NO"
 
     # files: meta data for the flow
-    if 'FLOW_META' in files:
-        pull.append(files['FLOW_META'])
+    if "FLOW_META" in files:
+        pull.append(files["FLOW_META"])
 
     # files: target equivarea distribution
-    if ( 'EQUIV_AREA' in special_cases and
-        'TARGET_EA' in files ) :
-        pull.append( files['TARGET_EA'] )
+    if "EQUIV_AREA" in special_cases and "TARGET_EA" in files:
+        pull.append(files["TARGET_EA"])
 
     # files: target pressure distribution
-    if ( 'INV_DESIGN_CP' in special_cases and
-        'TARGET_CP' in files ) :
-        pull.append( files['TARGET_CP'] )
+    if "INV_DESIGN_CP" in special_cases and "TARGET_CP" in files:
+        pull.append(files["TARGET_CP"])
 
     # files: target heat flux distribution
-    if ( 'INV_DESIGN_HEATFLUX' in special_cases and
-        'TARGET_HEATFLUX' in files ) :
-        pull.append( files['TARGET_HEATFLUX'] )
+    if "INV_DESIGN_HEATFLUX" in special_cases and "TARGET_HEATFLUX" in files:
+        pull.append(files["TARGET_HEATFLUX"])
 
     # pull needed files, start folder_0
-    with redirect_folder( folder[0], pull, link ) as push:
+    with redirect_folder(folder[0], pull, link) as push:
         with redirect_output(log_direct):
 
             konfig = copy.deepcopy(config)
-            ztate  = copy.deepcopy(state)
+            ztate = copy.deepcopy(state)
             # Reset restart to original value
-            konfig['RESTART_SOL'] = restart_sol
+            konfig["RESTART_SOL"] = restart_sol
 
             dst = os.getcwd()
-            dst = os.path.abspath(dst).rstrip('/')+'/'+'DIRECT'
+            dst = os.path.abspath(dst).rstrip("/") + "/" + "DIRECT"
 
             # make unix link
             string = "ln -s " + src + " " + dst
             stringlist = string.split()
             subprocess.Popen(stringlist)
 
-    for i in range(len(weight_list)-1):
+    for i in range(len(weight_list) - 1):
 
         konfig = copy.deepcopy(config)
-        ztate  = copy.deepcopy(state)
+        ztate = copy.deepcopy(state)
 
-        konfig.SOLUTION_FILENAME = solution_flow_list[i+1]
+        konfig.SOLUTION_FILENAME = solution_flow_list[i + 1]
 
         # delete direct solution file from previous point
-        if 'DIRECT' in ztate.FILES:
+        if "DIRECT" in ztate.FILES:
             del ztate.FILES.DIRECT
 
-        if 'FLOW_META' in ztate.FILES:
+        if "FLOW_META" in ztate.FILES:
             del ztate.FILES.FLOW_META
 
         # use direct solution file from relevant point
-        if 'MULTIPOINT_DIRECT' in state.FILES and state.FILES.MULTIPOINT_DIRECT[i+1]:
-            ztate.FILES['DIRECT'] = state.FILES.MULTIPOINT_DIRECT[i+1]
+        if "MULTIPOINT_DIRECT" in state.FILES and state.FILES.MULTIPOINT_DIRECT[i + 1]:
+            ztate.FILES["DIRECT"] = state.FILES.MULTIPOINT_DIRECT[i + 1]
 
         # use flow.meta file from relevant point
-        if 'MULTIPOINT_FLOW_META' in state.FILES and state.FILES.MULTIPOINT_FLOW_META[i+1]:
-            ztate.FILES['FLOW_META'] = state.FILES.MULTIPOINT_FLOW_META[i+1]
+        if (
+            "MULTIPOINT_FLOW_META" in state.FILES
+            and state.FILES.MULTIPOINT_FLOW_META[i + 1]
+        ):
+            ztate.FILES["FLOW_META"] = state.FILES.MULTIPOINT_FLOW_META[i + 1]
 
         # use mesh file from relevant point
-        if 'MULTIPOINT_MESH_FILENAME' in ztate.FILES:
-            ztate.FILES.MESH = ztate.FILES.MULTIPOINT_MESH_FILENAME[i+1]
-            konfig.MESH_FILENAME= ztate.FILES.MULTIPOINT_MESH_FILENAME[i+1]
-            konfig['DV_VALUE_OLD'] = dv_value_old
+        if "MULTIPOINT_MESH_FILENAME" in ztate.FILES:
+            ztate.FILES.MESH = ztate.FILES.MULTIPOINT_MESH_FILENAME[i + 1]
+            konfig.MESH_FILENAME = ztate.FILES.MULTIPOINT_MESH_FILENAME[i + 1]
+            konfig["DV_VALUE_OLD"] = dv_value_old
 
         files = ztate.FILES
         link = []
         pull = []
 
         # files: mesh
-        name = files['MESH']
-        name = su2io.expand_part(name,konfig)
+        name = files["MESH"]
+        name = su2io.expand_part(name, konfig)
         link.extend(name)
 
         # files: direction solution
-        if 'DIRECT' in files:
-            name = files['DIRECT']
-            name = su2io.expand_time(name,konfig)
-            link.extend( name )
+        if "DIRECT" in files:
+            name = files["DIRECT"]
+            name = su2io.expand_time(name, konfig)
+            link.extend(name)
         else:
-            konfig['RESTART_SOL'] = 'NO'
+            konfig["RESTART_SOL"] = "NO"
 
         # files: meta data for the flow
-        if 'FLOW_META' in files:
-            pull.append(files['FLOW_META'])
+        if "FLOW_META" in files:
+            pull.append(files["FLOW_META"])
 
         # pull needed files, start folder_1
-        with redirect_folder( folder[i+1], pull, link ) as push:
+        with redirect_folder(folder[i + 1], pull, link) as push:
             with redirect_output(log_direct):
 
                 # Perform deformation on multipoint mesh
-                if 'MULTIPOINT_MESH_FILENAME' in state.FILES:
-                    info = update_mesh(konfig,ztate)
+                if "MULTIPOINT_MESH_FILENAME" in state.FILES:
+                    info = update_mesh(konfig, ztate)
 
                 # Update config values
-                konfig.AOA = aoa_list[i+1]
-                konfig.SIDESLIP_ANGLE = sideslip_list[i+1]
-                konfig.MACH_NUMBER = mach_list[i+1]
-                konfig.REYNOLDS_NUMBER = reynolds_list[i+1]
-                konfig.FREESTREAM_TEMPERATURE = freestream_temp_list[i+1]
-                konfig.FREESTREAM_PRESSURE = freestream_press_list[i+1]
-                konfig.TARGET_CL = target_cl_list[i+1]
-                orig_marker_outlet = config['MARKER_OUTLET']
-                orig_marker_outlet = orig_marker_outlet.replace("(", "").replace(")", "").split(',')
-                new_marker_outlet = "(" + orig_marker_outlet[0] + "," + outlet_value_list[i+1] + ")"
+                konfig.AOA = aoa_list[i + 1]
+                konfig.SIDESLIP_ANGLE = sideslip_list[i + 1]
+                konfig.MACH_NUMBER = mach_list[i + 1]
+                konfig.REYNOLDS_NUMBER = reynolds_list[i + 1]
+                konfig.FREESTREAM_TEMPERATURE = freestream_temp_list[i + 1]
+                konfig.FREESTREAM_PRESSURE = freestream_press_list[i + 1]
+                konfig.TARGET_CL = target_cl_list[i + 1]
+                orig_marker_outlet = config["MARKER_OUTLET"]
+                orig_marker_outlet = (
+                    orig_marker_outlet.replace("(", "").replace(")", "").split(",")
+                )
+                new_marker_outlet = (
+                    "(" + orig_marker_outlet[0] + "," + outlet_value_list[i + 1] + ")"
+                )
                 konfig.MARKER_OUTLET = new_marker_outlet
 
                 ztate.FUNCTIONS.clear()
 
                 # rename meta data to flow.meta
-                if 'FLOW_META' in ztate.FILES:
-                    ztate.FILES['FLOW_META'] = 'flow.meta'
-                    os.rename(ztate.FILES.MULTIPOINT_FLOW_META[i+1], 'flow.meta')
+                if "FLOW_META" in ztate.FILES:
+                    ztate.FILES["FLOW_META"] = "flow.meta"
+                    os.rename(ztate.FILES.MULTIPOINT_FLOW_META[i + 1], "flow.meta")
 
-                func[i+1] = aerodynamics(konfig,ztate)
+                func[i + 1] = aerodynamics(konfig, ztate)
 
                 dst = os.getcwd()
 
                 # revert name of flow.meta file to multipoint name
-                if os.path.exists('flow.meta'):
-                    os.rename('flow.meta', flow_meta_list[i+1])
-                    ztate.FILES['FLOW_META'] = flow_meta_list[i+1]
-                    dst_flow_meta = os.path.abspath(dst).rstrip('/')+'/'+ztate.FILES['FLOW_META']
-                    push.append(ztate.FILES['FLOW_META'])
+                if os.path.exists("flow.meta"):
+                    os.rename("flow.meta", flow_meta_list[i + 1])
+                    ztate.FILES["FLOW_META"] = flow_meta_list[i + 1]
+                    dst_flow_meta = (
+                        os.path.abspath(dst).rstrip("/")
+                        + "/"
+                        + ztate.FILES["FLOW_META"]
+                    )
+                    push.append(ztate.FILES["FLOW_META"])
 
                 # direct files to push
-                dst_direct = os.path.abspath(dst).rstrip('/')+'/'+ztate.FILES['DIRECT']
-                name = ztate.FILES['DIRECT']
-                name = su2io.expand_zones(name,konfig)
-                name = su2io.expand_time(name,konfig)
+                dst_direct = (
+                    os.path.abspath(dst).rstrip("/") + "/" + ztate.FILES["DIRECT"]
+                )
+                name = ztate.FILES["DIRECT"]
+                name = su2io.expand_zones(name, konfig)
+                name = su2io.expand_time(name, konfig)
                 push.extend(name)
 
-                if 'MULTIPOINT_MESH_FILENAME' in state.FILES:
+                if "MULTIPOINT_MESH_FILENAME" in state.FILES:
                     # Mesh files to push
-                    dst_mesh = os.path.abspath(dst).rstrip('/')+'/'+ztate.FILES['MESH']
-                    name = ztate.FILES['MESH']
-                    name = su2io.expand_part(name,konfig)
+                    dst_mesh = (
+                        os.path.abspath(dst).rstrip("/") + "/" + ztate.FILES["MESH"]
+                    )
+                    name = ztate.FILES["MESH"]
+                    name = su2io.expand_part(name, konfig)
                     push.extend(name)
 
-
         # Link direct solution to MULTIPOINT_# folder
         src = os.getcwd()
-        src_direct = os.path.abspath(src).rstrip('/')+'/'+ztate.FILES['DIRECT']
+        src_direct = os.path.abspath(src).rstrip("/") + "/" + ztate.FILES["DIRECT"]
 
         # make unix link
         os.symlink(src_direct, dst_direct)
 
         # If the mesh doesn't already exist, link it
-        if 'MULTIPOINT_MESH_FILENAME' in state.FILES:
-            src_mesh = os.path.abspath(src).rstrip('/')+'/'+ztate.FILES['MESH']
+        if "MULTIPOINT_MESH_FILENAME" in state.FILES:
+            src_mesh = os.path.abspath(src).rstrip("/") + "/" + ztate.FILES["MESH"]
             if not os.path.exists(src_mesh):
                 os.symlink(src_mesh, dst_mesh)
 
         # link flow.meta
-        if 'MULTIPOINT_FLOW_META' in state.FILES:
-            src_flow_meta = os.path.abspath(src).rstrip('/')+'/'+ztate.FILES['FLOW_META']
+        if "MULTIPOINT_FLOW_META" in state.FILES:
+            src_flow_meta = (
+                os.path.abspath(src).rstrip("/") + "/" + ztate.FILES["FLOW_META"]
+            )
             if not os.path.exists(src_flow_meta):
                 os.symlink(src_flow_meta, dst_flow_meta)
 
     # Update MULTIPOINT_DIRECT in state.FILES
     state.FILES.MULTIPOINT_DIRECT = solution_flow_list
-    if 'FLOW_META' in state.FILES:
+    if "FLOW_META" in state.FILES:
         state.FILES.MULTIPOINT_FLOW_META = flow_meta_list
 
     # ----------------------------------------------------
@@ -727,20 +776,21 @@ def multipoint( config, state=None, step=1e-2 ):
     # ----------------------------------------------------
 
     for derv_name in su2io.optnames_multi:
-        matches = [ k for k in opt_names if k in derv_name ]
-        if not len(matches) == 1: continue
+        matches = [k for k in opt_names if k in derv_name]
+        if not len(matches) == 1:
+            continue
         func_name = matches[0]
         obj_func = 0.0
         for i in range(len(weight_list)):
-            obj_func = obj_func + float(weight_list[i])*func[i][func_name]
+            obj_func = obj_func + float(weight_list[i]) * func[i][func_name]
 
         state.FUNCTIONS[derv_name] = obj_func
 
     # return output
     funcs = su2util.ordered_bunch()
     for key in su2io.optnames_multi:
-        if key in state['FUNCTIONS']:
-            funcs[key] = state['FUNCTIONS'][key]
+        if key in state["FUNCTIONS"]:
+            funcs[key] = state["FUNCTIONS"][key]
 
     return funcs
 
@@ -749,29 +799,30 @@ def multipoint( config, state=None, step=1e-2 ):
 #  Geometric Functions
 # ----------------------------------------------------------------------
 
-def geometry( func_name, config, state=None ):
-    """ val = SU2.eval.geometry(config,state=None)
 
-        Evaluates geometry with the following:
-            SU2.run.deform()
-            SU2.run.geometry()
+def geometry(func_name, config, state=None):
+    """val = SU2.eval.geometry(config,state=None)
+
+    Evaluates geometry with the following:
+        SU2.run.deform()
+        SU2.run.geometry()
 
-        Assumptions:
-            Config is already setup for deformation.
-            Mesh may or may not be deformed.
-            Updates config and state by reference.
-            Redundancy if state.FUNCTIONS does not have func_name.
+    Assumptions:
+        Config is already setup for deformation.
+        Mesh may or may not be deformed.
+        Updates config and state by reference.
+        Redundancy if state.FUNCTIONS does not have func_name.
 
-        Executes in:
-            ./GEOMETRY
+    Executes in:
+        ./GEOMETRY
 
-        Inputs:
-            config    - an SU2 config
-            state     - optional, an SU2 state
+    Inputs:
+        config    - an SU2 config
+        state     - optional, an SU2 state
 
-        Outputs:
-            Bunch() of functions with keys of objective function names
-            and values of objective function floats.
+    Outputs:
+        Bunch() of functions with keys of objective function names
+        and values of objective function floats.
     """
 
     # ----------------------------------------------------
@@ -780,13 +831,13 @@ def geometry( func_name, config, state=None ):
 
     # initialize
     state = su2io.State(state)
-    if not 'MESH' in state.FILES:
-        state.FILES.MESH = config['MESH_FILENAME']
+    if not "MESH" in state.FILES:
+        state.FILES.MESH = config["MESH_FILENAME"]
     special_cases = su2io.get_specialCases(config)
 
     # console output
-    if config.get('CONSOLE','VERBOSE') in ['QUIET','CONCISE']:
-        log_geom = 'log_Geometry.out'
+    if config.get("CONSOLE", "VERBOSE") in ["QUIET", "CONCISE"]:
+        log_geom = "log_Geometry.out"
     else:
         log_geom = None
 
@@ -795,8 +846,7 @@ def geometry( func_name, config, state=None ):
     # ----------------------------------------------------
 
     # does decomposition and deformation
-    #info = update_mesh(config,state)
-
+    # info = update_mesh(config,state)
 
     # ----------------------------------------------------
     #  Geometry Solution
@@ -804,28 +854,29 @@ def geometry( func_name, config, state=None ):
 
     # redundancy check
     geometry_done = func_name in state.FUNCTIONS
-    #geometry_done = all([key in state.FUNCTIONS for key in su2io.optnames_geo])
+    # geometry_done = all([key in state.FUNCTIONS for key in su2io.optnames_geo])
     if not geometry_done:
 
         # files to pull
         files = state.FILES
-        pull = []; link = []
+        pull = []
+        link = []
 
         # files: mesh
-        name = files['MESH']
-        name = su2io.expand_part(name,config)
+        name = files["MESH"]
+        name = su2io.expand_part(name, config)
         link.extend(name)
 
         # update function name
         ## TODO
 
         # output redirection
-        with redirect_folder( 'GEOMETRY', pull, link ) as push:
+        with redirect_folder("GEOMETRY", pull, link) as push:
             with redirect_output(log_geom):
 
                 # setup config
                 config.GEO_PARAM = func_name
-                config.GEO_MODE  = 'FUNCTION'
+                config.GEO_MODE = "FUNCTION"
 
                 # # RUN GEOMETRY SOLUTION # #
                 info = su2run.geometry(config)
@@ -840,38 +891,37 @@ def geometry( func_name, config, state=None ):
     # return output
     funcs = su2util.ordered_bunch()
     for key in su2io.optnames_geo:
-        if key in state['FUNCTIONS']:
-            funcs[key] = state['FUNCTIONS'][key]
+        if key in state["FUNCTIONS"]:
+            funcs[key] = state["FUNCTIONS"][key]
     return funcs
 
 
 #: def geometry()
 
 
+def update_mesh(config, state=None):
+    """SU2.eval.update_mesh(config,state=None)
 
-def update_mesh(config,state=None):
-    """ SU2.eval.update_mesh(config,state=None)
+    updates mesh with the following:
+              SU2.run.deform()
 
-        updates mesh with the following:
-	          SU2.run.deform()
+    Assumptions:
+        Config is already setup for deformation.
+        Mesh may or may not be deformed.
+        Updates config and state by reference.
 
-        Assumptions:
-            Config is already setup for deformation.
-            Mesh may or may not be deformed.
-            Updates config and state by reference.
+    Executes in:
+        ./DECOMP and ./DEFORM
 
-        Executes in:
-            ./DECOMP and ./DEFORM
+    Inputs:
+        config    - an SU2 config
+        state     - optional, an SU2 state
 
-        Inputs:
-            config    - an SU2 config
-            state     - optional, an SU2 state
+    Outputs:
+        nothing
 
-        Outputs:
-            nothing
-
-        Modifies:
-            config and state by reference
+    Modifies:
+        config and state by reference
     """
 
     # ----------------------------------------------------
@@ -880,37 +930,36 @@ def update_mesh(config,state=None):
 
     # initialize
     state = su2io.State(state)
-    if not 'MESH' in state.FILES:
-        state.FILES.MESH = config['MESH_FILENAME']
+    if not "MESH" in state.FILES:
+        state.FILES.MESH = config["MESH_FILENAME"]
     special_cases = su2io.get_specialCases(config)
 
     # console output
-    if config.get('CONSOLE','VERBOSE') in ['QUIET','CONCISE']:
-        log_decomp = 'log_Decomp.out'
-        log_deform = 'log_Deform.out'
+    if config.get("CONSOLE", "VERBOSE") in ["QUIET", "CONCISE"]:
+        log_decomp = "log_Decomp.out"
+        log_deform = "log_Deform.out"
     else:
         log_decomp = None
         log_deform = None
 
-
     # ----------------------------------------------------
     #  Deformation
     # ----------------------------------------------------
 
     # redundancy check
-    deform_set  = config['DV_KIND'] == config['DEFINITION_DV']['KIND']
-    deform_todo = not config['DV_VALUE_NEW'] == config['DV_VALUE_OLD']
+    deform_set = config["DV_KIND"] == config["DEFINITION_DV"]["KIND"]
+    deform_todo = not config["DV_VALUE_NEW"] == config["DV_VALUE_OLD"]
     if deform_set and deform_todo:
 
         # files to pull
         pull = []
-        link = config['MESH_FILENAME']
-        link = su2io.expand_part(link,config)
+        link = config["MESH_FILENAME"]
+        link = su2io.expand_part(link, config)
 
-        pull.extend(config.get('CONFIG_LIST',[]))
+        pull.extend(config.get("CONFIG_LIST", []))
 
         # output redirection
-        with redirect_folder('DEFORM',pull,link) as push:
+        with redirect_folder("DEFORM", pull, link) as push:
             with redirect_output(log_deform):
 
                 # # RUN DEFORMATION # #
@@ -919,8 +968,8 @@ def update_mesh(config,state=None):
 
                 # data to push
                 meshname = info.FILES.MESH
-                names = su2io.expand_part( meshname , config )
-                push.extend( names )
+                names = su2io.expand_part(meshname, config)
+                push.extend(names)
 
         #: with redirect output
 
@@ -930,4 +979,3 @@ def update_mesh(config,state=None):
     #: if not redundant
 
     return
-
diff --git a/SU2_PY/SU2/eval/gradients.py b/SU2_PY/SU2/eval/gradients.py
index 739001f24e4..da8b76d94c7 100644
--- a/SU2_PY/SU2/eval/gradients.py
+++ b/SU2_PY/SU2/eval/gradients.py
@@ -30,8 +30,8 @@
 # ----------------------------------------------------------------------
 
 import os, sys, shutil, copy, subprocess
-from .. import run  as su2run
-from .. import io   as su2io
+from .. import run as su2run
+from .. import io as su2io
 from .. import util as su2util
 from .functions import function, update_mesh
 from ..io import redirect_folder, redirect_output
@@ -41,99 +41,101 @@
 #  Main Gradient Interface
 # ----------------------------------------------------------------------
 
-def gradient( func_name, method, config, state=None ):
-    """ val = SU2.eval.grad(func_name,method,config,state=None)
 
-        Evaluates the aerodynamic gradients.
+def gradient(func_name, method, config, state=None):
+    """val = SU2.eval.grad(func_name,method,config,state=None)
 
-        Wraps:
-            SU2.eval.adjoint()
-            SU2.eval.findiff()
+    Evaluates the aerodynamic gradients.
 
-        Assumptions:
-            Config is already setup for deformation.
-            Mesh need not be deformed.
-            Updates config and state by reference.
-            Redundancy if state.GRADIENTS has the key func_name.
+    Wraps:
+        SU2.eval.adjoint()
+        SU2.eval.findiff()
 
-        Executes in:
-            ./ADJOINT_* or ./FINDIFF
+    Assumptions:
+        Config is already setup for deformation.
+        Mesh need not be deformed.
+        Updates config and state by reference.
+        Redundancy if state.GRADIENTS has the key func_name.
 
-        Inputs:
-            func_name - SU2 objective function name
-            method    - 'CONTINUOUS_ADJOINT' or 'FINDIFF' or 'DISCRETE_ADJOINT'
-            config    - an SU2 config
-            state     - optional, an SU2 state
+    Executes in:
+        ./ADJOINT_* or ./FINDIFF
 
-        Outputs:
-            A list of floats of gradient values
+    Inputs:
+        func_name - SU2 objective function name
+        method    - 'CONTINUOUS_ADJOINT' or 'FINDIFF' or 'DISCRETE_ADJOINT'
+        config    - an SU2 config
+        state     - optional, an SU2 state
+
+    Outputs:
+        A list of floats of gradient values
     """
 
     # Initialize
     grads = {}
     state = su2io.State(state)
-    if func_name == 'ALL':
+    if func_name == "ALL":
         raise Exception("func_name = 'ALL' not yet supported")
     func_output = func_name
-    if (type(func_name)==list):
-        if (config.OPT_COMBINE_OBJECTIVE=="YES"):
-            func_output = 'COMBO'
+    if type(func_name) == list:
+        if config.OPT_COMBINE_OBJECTIVE == "YES":
+            func_output = "COMBO"
         else:
             func_name = func_name[0]
     else:
-        config.OPT_COMBINE_OBJECTIVE="NO"
+        config.OPT_COMBINE_OBJECTIVE = "NO"
         config.OBJECTIVE_WEIGHT = "1.0"
 
     # redundancy check
-    if not func_output in state['GRADIENTS']:
+    if not func_output in state["GRADIENTS"]:
 
         # Adjoint Gradients
-        if any([method == 'CONTINUOUS_ADJOINT', method == 'DISCRETE_ADJOINT']):
+        if any([method == "CONTINUOUS_ADJOINT", method == "DISCRETE_ADJOINT"]):
 
             # Aerodynamics
             if func_output in su2io.historyOutFields:
-                if su2io.historyOutFields[func_output]['TYPE'] == 'COEFFICIENT':
-                    grads = adjoint( func_name, config, state )
+                if su2io.historyOutFields[func_output]["TYPE"] == "COEFFICIENT":
+                    grads = adjoint(func_name, config, state)
 
             elif func_name in su2io.historyOutFields:
-                if su2io.historyOutFields[func_name]['TYPE'] == 'COEFFICIENT':
-                    grads = adjoint( func_name, config, state )
+                if su2io.historyOutFields[func_name]["TYPE"] == "COEFFICIENT":
+                    grads = adjoint(func_name, config, state)
 
             # Stability
             elif func_output in su2io.optnames_stab:
-                grads = stability( func_name, config, state )
+                grads = stability(func_name, config, state)
 
             # Multipoint
             elif func_output in su2io.optnames_multi:
-              grads = multipoint( func_name, config, state )
+                grads = multipoint(func_name, config, state)
 
             # Geometry (actually a finite difference)
             elif func_output in su2io.optnames_geo:
-                grads = geometry( func_name, config, state )
+                grads = geometry(func_name, config, state)
 
             else:
-                raise Exception('unknown function name: %s' % func_name)
+                raise Exception("unknown function name: %s" % func_name)
 
         # Finite Difference Gradients
-        elif method == 'FINDIFF':
-            grads = findiff( config, state )
+        elif method == "FINDIFF":
+            grads = findiff(config, state)
 
-        elif method == 'DIRECTDIFF':
-            grad = directdiff (config , state )
+        elif method == "DIRECTDIFF":
+            grad = directdiff(config, state)
 
         else:
-            raise Exception('unrecognized gradient method')
+            raise Exception("unrecognized gradient method")
 
         # store
-        state['GRADIENTS'].update(grads)
+        state["GRADIENTS"].update(grads)
 
     # if not redundant
 
     # prepare output
-    grads_out = state['GRADIENTS'][func_output]
+    grads_out = state["GRADIENTS"][func_output]
 
     return copy.deepcopy(grads_out)
 
+
 #: def gradient()
 
 
@@ -141,34 +143,35 @@ def gradient( func_name, method, config, state=None ):
 #  Adjoint Gradients
 # ----------------------------------------------------------------------
 
-def adjoint( func_name, config, state=None ):
-    """ vals = SU2.eval.adjoint(func_name,config,state=None)
-
-        Evaluates the aerodynamics gradients using the
-        adjoint methodology with:
-            SU2.eval.func()
-            SU2.run.deform()
-            SU2.run.direct()
-            SU2.run.adjoint()
-
-        Assumptions:
-            Config is already setup for deformation.
-            Mesh may or may not be deformed.
-            Updates config and state by reference.
-            Adjoint Redundancy if state.GRADIENTS has key func_name.
-            Direct Redundancy if state.FUNCTIONS has key func_name.
-
-        Executes in:
-            ./ADJOINT_<func_name>
-
-        Inputs:
-            func_name - SU2 objective function name
-            config    - an SU2 config
-            state     - optional, an SU2 state
-
-        Outputs:
-            A Bunch() with keys of objective function names
-            and values of list of floats of gradient values
+
+def adjoint(func_name, config, state=None):
+    """vals = SU2.eval.adjoint(func_name,config,state=None)
+
+    Evaluates the aerodynamics gradients using the
+    adjoint methodology with:
+        SU2.eval.func()
+        SU2.run.deform()
+        SU2.run.direct()
+        SU2.run.adjoint()
+
+    Assumptions:
+        Config is already setup for deformation.
+        Mesh may or may not be deformed.
+        Updates config and state by reference.
+        Adjoint Redundancy if state.GRADIENTS has key func_name.
+        Direct Redundancy if state.FUNCTIONS has key func_name.
+
+    Executes in:
+        ./ADJOINT_<func_name>
+
+    Inputs:
+        func_name - SU2 objective function name
+        config    - an SU2 config
+        state     - optional, an SU2 state
+
+    Outputs:
+        A Bunch() with keys of objective function names
+        and values of list of floats of gradient values
     """
 
     # ----------------------------------------------------
@@ -181,15 +184,16 @@ def adjoint( func_name, config, state=None ):
 
     # When a list of objectives is used, they are combined
     # and the output name is 'COMBO'
-    multi_objective = (type(func_name)==list)
+    multi_objective = type(func_name) == list
     func_output = func_name
-    if multi_objective:   func_output = 'COMBO'
+    if multi_objective:
+        func_output = "COMBO"
 
-    ADJ_NAME = 'ADJOINT_'+func_output
+    ADJ_NAME = "ADJOINT_" + func_output
 
     # console output
-    if config.get('CONSOLE','VERBOSE') in ['QUIET','CONCISE']:
-        log_adjoint = 'log_Adjoint.out'
+    if config.get("CONSOLE", "VERBOSE") in ["QUIET", "CONCISE"]:
+        log_adjoint = "log_Adjoint.out"
     else:
         log_adjoint = None
 
@@ -198,8 +202,8 @@ def adjoint( func_name, config, state=None ):
     # ----------------------------------------------------
 
     # master redundancy check
-    if func_output in state['GRADIENTS']:
-        grads = state['GRADIENTS']
+    if func_output in state["GRADIENTS"]:
+        grads = state["GRADIENTS"]
         return copy.deepcopy(grads)
 
     # ----------------------------------------------------
@@ -207,13 +211,13 @@ def adjoint( func_name, config, state=None ):
     # ----------------------------------------------------
 
     # run (includes redundancy checks)
-    function( func_name, config, state )
+    function(func_name, config, state)
 
     # ----------------------------------------------------
     #  Adaptation (not implemented)
     # ----------------------------------------------------
 
-    #if not state.['ADAPTED_ADJOINT']:
+    # if not state.['ADAPTED_ADJOINT']:
     #    config = su2run.adaptation(config)
     #    state['ADAPTED_FUNC'] = True
 
@@ -224,118 +228,132 @@ def adjoint( func_name, config, state=None ):
     konfig = copy.deepcopy(config)
 
     # Set correct starting time for reverse sweep
-    if 'TIME_ITER' in state.WND_CAUCHY_DATA:  # Use Convergence data, if we have already a direct run
-        konfig['TIME_ITER'] = state.WND_CAUCHY_DATA['TIME_ITER']
-        konfig['ITER_AVERAGE_OBJ'] = state.WND_CAUCHY_DATA['ITER_AVERAGE_OBJ']
-        konfig['UNST_ADJOINT_ITER'] = state.WND_CAUCHY_DATA['UNST_ADJOINT_ITER']
-
+    if (
+        "TIME_ITER" in state.WND_CAUCHY_DATA
+    ):  # Use Convergence data, if we have already a direct run
+        konfig["TIME_ITER"] = state.WND_CAUCHY_DATA["TIME_ITER"]
+        konfig["ITER_AVERAGE_OBJ"] = state.WND_CAUCHY_DATA["ITER_AVERAGE_OBJ"]
+        konfig["UNST_ADJOINT_ITER"] = state.WND_CAUCHY_DATA["UNST_ADJOINT_ITER"]
 
     # files to pull
-    files = state['FILES']
-    pull = []; link = []
+    files = state["FILES"]
+    pull = []
+    link = []
 
     # files: mesh
-    name = files['MESH']
-    name = su2io.expand_part(name,konfig)
+    name = files["MESH"]
+    name = su2io.expand_part(name, konfig)
     link.extend(name)
 
     # files: direct solution
-    name = files['DIRECT']
-    name = su2io.expand_zones(name,konfig)
-    name = su2io.expand_time(name,konfig)
+    name = files["DIRECT"]
+    name = su2io.expand_zones(name, konfig)
+    name = su2io.expand_time(name, konfig)
     link.extend(name)
     # files restart
-    if config.get('TIME_DOMAIN', 'NO') == 'YES' and config.get('RESTART_SOL', 'NO') == 'YES':
-       if 'RESTART_FILE_1' in files:
-           name = files['RESTART_FILE_1']
-           name = su2io.expand_part(name, config)
-           link.extend(name)
-       if 'RESTART_FILE_1' in files:  # not the case for 1st order time stepping
-           name = files['RESTART_FILE_2']
-           name = su2io.expand_part(name, config)
-           link.extend(name)
-
-    if 'FLOW_META' in files:
-        pull.append(files['FLOW_META'])
+    if (
+        config.get("TIME_DOMAIN", "NO") == "YES"
+        and config.get("RESTART_SOL", "NO") == "YES"
+    ):
+        if "RESTART_FILE_1" in files:
+            name = files["RESTART_FILE_1"]
+            name = su2io.expand_part(name, config)
+            link.extend(name)
+        if "RESTART_FILE_1" in files:  # not the case for 1st order time stepping
+            name = files["RESTART_FILE_2"]
+            name = su2io.expand_part(name, config)
+            link.extend(name)
+
+    if "FLOW_META" in files:
+        pull.append(files["FLOW_META"])
 
     # files: adjoint solution
     if ADJ_NAME in files:
         name = files[ADJ_NAME]
-        name = su2io.expand_zones(name,konfig)
-        name = su2io.expand_time(name,konfig)
+        name = su2io.expand_zones(name, konfig)
+        name = su2io.expand_time(name, konfig)
         link.extend(name)
     else:
-        config['RESTART_SOL'] = 'NO' #Can this be deleted?
-        if config.get('TIME_DOMAIN', 'NO') != 'YES':  # rules out steady state optimization special cases.
-            konfig['RESTART_SOL'] = 'NO'  # for shape optimization with restart files.
+        config["RESTART_SOL"] = "NO"  # Can this be deleted?
+        if (
+            config.get("TIME_DOMAIN", "NO") != "YES"
+        ):  # rules out steady state optimization special cases.
+            konfig["RESTART_SOL"] = "NO"  # for shape optimization with restart files.
         # Restart solution gets handled just before solver starts for unsteady optimization
 
     # files: target equivarea adjoint weights
-    if 'EQUIV_AREA' in special_cases:
-        pull.append(files['TARGET_EA'])
+    if "EQUIV_AREA" in special_cases:
+        pull.append(files["TARGET_EA"])
 
     # files: target pressure coefficient
-    if 'INV_DESIGN_CP' in special_cases:
-        pull.append(files['TARGET_CP'])
+    if "INV_DESIGN_CP" in special_cases:
+        pull.append(files["TARGET_CP"])
 
     # files: target heat flux coefficient
-    if 'INV_DESIGN_HEATFLUX' in special_cases:
-        pull.append(files['TARGET_HEATFLUX'])
-
-    if not 'OUTPUT_FILES' in config:
-        config['OUTPUT_FILES'] = ['RESTART']
+    if "INV_DESIGN_HEATFLUX" in special_cases:
+        pull.append(files["TARGET_HEATFLUX"])
 
-    if not 'SURFACE_CSV' in config['OUTPUT_FILES']:
-      config['OUTPUT_FILES'].append('SURFACE_CSV')
+    if not "OUTPUT_FILES" in config:
+        config["OUTPUT_FILES"] = ["RESTART"]
 
+    if not "SURFACE_CSV" in config["OUTPUT_FILES"]:
+        config["OUTPUT_FILES"].append("SURFACE_CSV")
 
     # output redirection
-    with redirect_folder( ADJ_NAME, pull, link ) as push:
+    with redirect_folder(ADJ_NAME, pull, link) as push:
         with redirect_output(log_adjoint):
 
             # Format objective list in config
             if multi_objective:
-                config['OBJECTIVE_FUNCTION'] = ", ".join(func_name) #Can this be deleted?
-                konfig['OBJECTIVE_FUNCTION'] = ", ".join(func_name)
+                config["OBJECTIVE_FUNCTION"] = ", ".join(
+                    func_name
+                )  # Can this be deleted?
+                konfig["OBJECTIVE_FUNCTION"] = ", ".join(func_name)
             else:
-                config['OBJECTIVE_FUNCTION'] = func_name            #Can this be deleted?
-                konfig['OBJECTIVE_FUNCTION'] = func_name
+                config["OBJECTIVE_FUNCTION"] = func_name  # Can this be deleted?
+                konfig["OBJECTIVE_FUNCTION"] = func_name
 
             # # RUN ADJOINT SOLUTION # #
 
             # We do not want a restart in adjoint run, we want that the adjoint run computes only up to the restart iteration of the primal run.
             restart_sol_activated = False
-            if konfig.get('TIME_DOMAIN', 'NO') == 'YES' and konfig.get('RESTART_SOL', 'NO') == 'YES':
+            if (
+                konfig.get("TIME_DOMAIN", "NO") == "YES"
+                and konfig.get("RESTART_SOL", "NO") == "YES"
+            ):
                 restart_sol_activated = True
-                original_time_iter = konfig['TIME_ITER']
-                konfig['TIME_ITER'] = konfig['TIME_ITER'] - int(konfig['RESTART_ITER'])
-                konfig.RESTART_SOL = 'NO'
+                original_time_iter = konfig["TIME_ITER"]
+                konfig["TIME_ITER"] = konfig["TIME_ITER"] - int(konfig["RESTART_ITER"])
+                konfig.RESTART_SOL = "NO"
 
             info = su2run.adjoint(konfig)
             # Workaround, since expandTime relies on UNST_ADJOINT_ITER to determine number of solution files.
             if restart_sol_activated:
-                konfig['UNST_ADJOINT_ITER'] = original_time_iter - int(konfig['RESTART_ITER'])
-            su2io.restart2solution(konfig,info)
+                konfig["UNST_ADJOINT_ITER"] = original_time_iter - int(
+                    konfig["RESTART_ITER"]
+                )
+            su2io.restart2solution(konfig, info)
 
             state.update(info)
 
             # Gradient Projection
-            info = su2run.projection(konfig,state)
+            info = su2run.projection(konfig, state)
             state.update(info)
 
             # solution files to push
             name = state.FILES[ADJ_NAME]
-            name = su2io.expand_zones(name,konfig)
-            name = su2io.expand_time(name,konfig)
+            name = su2io.expand_zones(name, konfig)
+            name = su2io.expand_time(name, konfig)
             push.extend(name)
 
     #: with output redirection
 
     # return output
     grads = su2util.ordered_bunch()
-    grads[func_output] = state['GRADIENTS'][func_output]
+    grads[func_output] = state["GRADIENTS"][func_output]
     return grads
 
+
 #: def adjoint()
 
 
@@ -343,10 +361,10 @@ def adjoint( func_name, config, state=None ):
 #  Stability Functions
 # ----------------------------------------------------------------------
 
-def stability( func_name, config, state=None, step=1e-2 ):
 
+def stability(func_name, config, state=None, step=1e-2):
 
-    folder = 'STABILITY' # os.path.join('STABILITY',func_name) #STABILITY/D_MOMENT_Y_D_ALPHA/
+    folder = "STABILITY"  # os.path.join('STABILITY',func_name) #STABILITY/D_MOMENT_Y_D_ALPHA/
 
     # ----------------------------------------------------
     #  Initialize
@@ -354,21 +372,21 @@ def stability( func_name, config, state=None, step=1e-2 ):
 
     # initialize
     state = su2io.State(state)
-    if not 'MESH' in state.FILES:
-        state.FILES.MESH = config['MESH_FILENAME']
+    if not "MESH" in state.FILES:
+        state.FILES.MESH = config["MESH_FILENAME"]
     special_cases = su2io.get_specialCases(config)
 
     # find base func name
-    matches = [ k for k in su2io.optnames_aero if k in func_name ]
+    matches = [k for k in su2io.optnames_aero if k in func_name]
     if not len(matches) == 1:
-        raise Exception('could not find stability function name')
+        raise Exception("could not find stability function name")
     base_name = matches[0]
 
-    ADJ_NAME = 'ADJOINT_'+base_name
+    ADJ_NAME = "ADJOINT_" + base_name
 
     # console output
-    if config.get('CONSOLE','VERBOSE') in ['QUIET','CONCISE']:
-        log_direct = 'log_Direct.out'
+    if config.get("CONSOLE", "VERBOSE") in ["QUIET", "CONCISE"]:
+        log_direct = "log_Direct.out"
     else:
         log_direct = None
 
@@ -377,15 +395,14 @@ def stability( func_name, config, state=None, step=1e-2 ):
     # ----------------------------------------------------
 
     # does decomposition and deformation
-    info = update_mesh(config,state)
+    info = update_mesh(config, state)
 
     # ----------------------------------------------------
     #  CENTRAL POINT
     # ----------------------------------------------------
 
     # will run in ADJOINT/
-    grads_0 = gradient(base_name,'CONTINUOUS_ADJOINT',config,state)
-
+    grads_0 = gradient(base_name, "CONTINUOUS_ADJOINT", config, state)
 
     # ----------------------------------------------------
     #  Run Forward Point
@@ -393,11 +410,12 @@ def stability( func_name, config, state=None, step=1e-2 ):
 
     # files to pull
     files = state.FILES
-    pull = []; link = []
+    pull = []
+    link = []
 
     # files: mesh
-    name = files['MESH']
-    name = su2io.expand_part(name,config)
+    name = files["MESH"]
+    name = su2io.expand_part(name, config)
     link.extend(name)
 
     # files: direct solution
@@ -406,39 +424,36 @@ def stability( func_name, config, state=None, step=1e-2 ):
     # files: adjoint solution
     if ADJ_NAME in files:
         name = files[ADJ_NAME]
-        name = su2io.expand_time(name,config)
+        name = su2io.expand_time(name, config)
         link.extend(name)
     else:
-        config['RESTART_SOL'] = 'NO'
+        config["RESTART_SOL"] = "NO"
 
     # files: target equivarea adjoint weights
     ## DO NOT PULL EQUIVAREA WEIGHTS, use the one in STABILITY/
 
-
     # pull needed files, start folder
-    with redirect_folder( folder, pull, link ) as push:
+    with redirect_folder(folder, pull, link) as push:
         with redirect_output(log_direct):
 
             konfig = copy.deepcopy(config)
-            ztate  = copy.deepcopy(state)
+            ztate = copy.deepcopy(state)
 
             # TODO: GENERALIZE
             konfig.AOA = konfig.AOA + step
 
             # let's start somethin somthin
             del ztate.GRADIENTS[base_name]
-            #ztate.find_files(konfig)
+            # ztate.find_files(konfig)
 
             # the gradient
-            grads_1 = gradient(base_name,'CONTINUOUS_ADJOINT',konfig,ztate)
-
+            grads_1 = gradient(base_name, "CONTINUOUS_ADJOINT", konfig, ztate)
 
     # ----------------------------------------------------
     #  DIFFERENCING
     # ----------------------------------------------------
 
-    grads = [ ( g_1 - g_0 ) / step
-              for g_1,g_0 in zip(grads_1,grads_0) ]
+    grads = [(g_1 - g_0) / step for g_1, g_0 in zip(grads_1, grads_0)]
 
     state.GRADIENTS[func_name] = grads
     grads_out = su2util.ordered_bunch()
@@ -451,20 +466,44 @@ def stability( func_name, config, state=None, step=1e-2 ):
 #  Multipoint Functions
 # ----------------------------------------------------------------------
 
-def multipoint( func_name, config, state=None, step=1e-2 ):
 
-    mach_list = config['MULTIPOINT_MACH_NUMBER'].replace("(", "").replace(")", "").split(',')
-    reynolds_list = config['MULTIPOINT_REYNOLDS_NUMBER'].replace("(", "").replace(")", "").split(',')
-    freestream_temp_list = config['MULTIPOINT_FREESTREAM_TEMPERATURE'].replace("(", "").replace(")", "").split(',')
-    freestream_press_list = config['MULTIPOINT_FREESTREAM_PRESSURE'].replace("(", "").replace(")", "").split(',')
-    aoa_list = config['MULTIPOINT_AOA'].replace("(", "").replace(")", "").split(',')
-    sideslip_list = config['MULTIPOINT_SIDESLIP_ANGLE'].replace("(", "").replace(")", "").split(',')
-    target_cl_list = config['MULTIPOINT_TARGET_CL'].replace("(", "").replace(")", "").split(',')
-    weight_list = config['MULTIPOINT_WEIGHT'].replace("(", "").replace(")", "").split(',')
+def multipoint(func_name, config, state=None, step=1e-2):
+
+    mach_list = (
+        config["MULTIPOINT_MACH_NUMBER"].replace("(", "").replace(")", "").split(",")
+    )
+    reynolds_list = (
+        config["MULTIPOINT_REYNOLDS_NUMBER"]
+        .replace("(", "")
+        .replace(")", "")
+        .split(",")
+    )
+    freestream_temp_list = (
+        config["MULTIPOINT_FREESTREAM_TEMPERATURE"]
+        .replace("(", "")
+        .replace(")", "")
+        .split(",")
+    )
+    freestream_press_list = (
+        config["MULTIPOINT_FREESTREAM_PRESSURE"]
+        .replace("(", "")
+        .replace(")", "")
+        .split(",")
+    )
+    aoa_list = config["MULTIPOINT_AOA"].replace("(", "").replace(")", "").split(",")
+    sideslip_list = (
+        config["MULTIPOINT_SIDESLIP_ANGLE"].replace("(", "").replace(")", "").split(",")
+    )
+    target_cl_list = (
+        config["MULTIPOINT_TARGET_CL"].replace("(", "").replace(")", "").split(",")
+    )
+    weight_list = (
+        config["MULTIPOINT_WEIGHT"].replace("(", "").replace(")", "").split(",")
+    )
     solution_flow_list = su2io.expand_multipoint(config.SOLUTION_FILENAME, config)
     solution_adj_list = su2io.expand_multipoint(config.SOLUTION_ADJ_FILENAME, config)
-    flow_meta_list = su2io.expand_multipoint('flow.meta', config)
-    restart_sol = config['RESTART_SOL']
+    flow_meta_list = su2io.expand_multipoint("flow.meta", config)
+    restart_sol = config["RESTART_SOL"]
     grads = []
     folder = []
     for i in range(len(weight_list)):
@@ -472,11 +511,11 @@ def multipoint( func_name, config, state=None, step=1e-2 ):
         folder.append(0)
 
     for i in range(len(weight_list)):
-        folder[i] = 'MULTIPOINT_' + str(i)
+        folder[i] = "MULTIPOINT_" + str(i)
 
     opt_names = []
     for key in su2io.historyOutFields:
-        if su2io.historyOutFields[key]['TYPE'] == 'COEFFICIENT':
+        if su2io.historyOutFields[key]["TYPE"] == "COEFFICIENT":
             opt_names.append(key)
 
     # ----------------------------------------------------
@@ -485,31 +524,31 @@ def multipoint( func_name, config, state=None, step=1e-2 ):
 
     # initialize
     state = su2io.State(state)
-    if not 'MESH' in state.FILES:
-        state.FILES.MESH = config['MESH_FILENAME']
+    if not "MESH" in state.FILES:
+        state.FILES.MESH = config["MESH_FILENAME"]
     special_cases = su2io.get_specialCases(config)
 
     # find base func name
-    matches = [ k for k in opt_names if k in func_name ]
+    matches = [k for k in opt_names if k in func_name]
     if not len(matches) == 1:
-        raise Exception('could not find multipoint function name')
+        raise Exception("could not find multipoint function name")
     base_name = matches[0]
 
-    ADJ_NAME = 'ADJOINT_' + base_name
-    MULTIPOINT_ADJ_NAME = 'MULTIPOINT_' + ADJ_NAME
+    ADJ_NAME = "ADJOINT_" + base_name
+    MULTIPOINT_ADJ_NAME = "MULTIPOINT_" + ADJ_NAME
 
     # console output
-    if config.get('CONSOLE','VERBOSE') in ['QUIET','CONCISE']:
-        log_direct = 'log_Direct.out'
+    if config.get("CONSOLE", "VERBOSE") in ["QUIET", "CONCISE"]:
+        log_direct = "log_Direct.out"
     else:
         log_direct = None
 
-#    # ----------------------------------------------------
-#    #  Update Mesh
-#    # ----------------------------------------------------
-#
-#    # does decomposition and deformation
-#    info = update_mesh(config,state)
+    #    # ----------------------------------------------------
+    #    #  Update Mesh
+    #    # ----------------------------------------------------
+    #
+    #    # does decomposition and deformation
+    #    info = update_mesh(config,state)
 
     # ----------------------------------------------------
     #  FIRST POINT
@@ -531,18 +570,18 @@ def multipoint( func_name, config, state=None, step=1e-2 ):
 
     # If flow.meta file for the first point is available, rename it before using it
     if os.path.exists(flow_meta_list[0]):
-        os.rename(flow_meta_list[0], 'flow.meta')
-        state.FILES['FLOW_META'] = 'flow.meta'
+        os.rename(flow_meta_list[0], "flow.meta")
+        state.FILES["FLOW_META"] = "flow.meta"
 
-    grads[0] = gradient(base_name,'DISCRETE_ADJOINT',config,state)
+    grads[0] = gradient(base_name, "DISCRETE_ADJOINT", config, state)
 
     src = os.getcwd()
-    src = os.path.abspath(src).rstrip('/') + '/' + ADJ_NAME + '/'
+    src = os.path.abspath(src).rstrip("/") + "/" + ADJ_NAME + "/"
 
     # change name of flow.meta back to multipoint name
-    if os.path.exists('flow.meta'):
-        os.rename('flow.meta',flow_meta_list[0])
-        state.FILES['FLOW_META'] = flow_meta_list[0]
+    if os.path.exists("flow.meta"):
+        os.rename("flow.meta", flow_meta_list[0])
+        state.FILES["FLOW_META"] = flow_meta_list[0]
 
     # ----------------------------------------------------
     #  Run Multipoint
@@ -550,11 +589,12 @@ def multipoint( func_name, config, state=None, step=1e-2 ):
 
     # files to pull
     files = state.FILES
-    pull = []; link = []
+    pull = []
+    link = []
 
     # files: mesh
-    name = files['MESH']
-    name = su2io.expand_part(name,config)
+    name = files["MESH"]
+    name = su2io.expand_part(name, config)
     link.extend(name)
 
     # files: direct solution
@@ -563,127 +603,137 @@ def multipoint( func_name, config, state=None, step=1e-2 ):
     # files: adjoint solution
     if ADJ_NAME in files:
         name = files[ADJ_NAME]
-        name = su2io.expand_time(name,config)
+        name = su2io.expand_time(name, config)
         link.extend(name)
         solution_adj_list[0] = files[ADJ_NAME]
     else:
-        config['RESTART_SOL'] = 'NO'
+        config["RESTART_SOL"] = "NO"
 
     # files: target equivarea adjoint weights
     ## DO NOT PULL EQUIVAREA WEIGHTS, use the one in MULTIPOINT/
 
     # pull needed files, start folder
-    with redirect_folder( folder[0], pull, link ) as push:
+    with redirect_folder(folder[0], pull, link) as push:
         with redirect_output(log_direct):
 
             konfig = copy.deepcopy(config)
-            ztate  = copy.deepcopy(state)
+            ztate = copy.deepcopy(state)
 
             dst = os.getcwd()
-            dst = os.path.abspath(dst).rstrip('/')+'/'
+            dst = os.path.abspath(dst).rstrip("/") + "/"
 
             # make unix link
             string = "ln -s " + src + " " + dst
             string_list = string.split()
             subprocess.Popen(string_list)
 
-    for i in range(len(weight_list)-1):
+    for i in range(len(weight_list) - 1):
 
         konfig = copy.deepcopy(config)
-        ztate  = copy.deepcopy(state)
+        ztate = copy.deepcopy(state)
         # Reset RESTART_SOL to original value
-        konfig['RESTART_SOL'] = restart_sol
+        konfig["RESTART_SOL"] = restart_sol
         # Set correct config option names
-        konfig.SOLUTION_FILENAME = solution_flow_list[i+1]
-        konfig.SOLUTION_ADJ_FILENAME = solution_adj_list[i+1]
+        konfig.SOLUTION_FILENAME = solution_flow_list[i + 1]
+        konfig.SOLUTION_ADJ_FILENAME = solution_adj_list[i + 1]
 
         # Delete file run in previous case
         if ADJ_NAME in ztate.FILES:
             del ztate.FILES[ADJ_NAME]
 
         # Update ADJOINT filename with MULTIPOINT_ADJOINT filename
-        if MULTIPOINT_ADJ_NAME in state.FILES and state.FILES[MULTIPOINT_ADJ_NAME][i+1]:
-            ztate.FILES[ADJ_NAME] = state.FILES[MULTIPOINT_ADJ_NAME][i+1]
-
-        if 'MULTIPOINT_MESH_FILENAME' in ztate.FILES:
-            if 'deform' in ztate.FILES.MESH:
-                ztate.FILES.MESH = su2io.add_suffix(ztate.FILES.MULTIPOINT_MESH_FILENAME[i+1],'deform')
-                konfig.MESH_FILENAME= su2io.add_suffix(ztate.FILES.MULTIPOINT_MESH_FILENAME[i+1],'deform')
+        if (
+            MULTIPOINT_ADJ_NAME in state.FILES
+            and state.FILES[MULTIPOINT_ADJ_NAME][i + 1]
+        ):
+            ztate.FILES[ADJ_NAME] = state.FILES[MULTIPOINT_ADJ_NAME][i + 1]
+
+        if "MULTIPOINT_MESH_FILENAME" in ztate.FILES:
+            if "deform" in ztate.FILES.MESH:
+                ztate.FILES.MESH = su2io.add_suffix(
+                    ztate.FILES.MULTIPOINT_MESH_FILENAME[i + 1], "deform"
+                )
+                konfig.MESH_FILENAME = su2io.add_suffix(
+                    ztate.FILES.MULTIPOINT_MESH_FILENAME[i + 1], "deform"
+                )
             else:
-                ztate.FILES.MESH = ztate.FILES.MULTIPOINT_MESH_FILENAME[i+1]
-                konfig.MESH_FILENAME= ztate.FILES.MULTIPOINT_MESH_FILENAME[i+1]
+                ztate.FILES.MESH = ztate.FILES.MULTIPOINT_MESH_FILENAME[i + 1]
+                konfig.MESH_FILENAME = ztate.FILES.MULTIPOINT_MESH_FILENAME[i + 1]
 
         # use flow.meta file from relevant point
-        if 'MULTIPOINT_FLOW_META' in state.FILES and state.FILES.MULTIPOINT_FLOW_META[i+1]:
-            ztate.FILES['FLOW_META'] = state.FILES.MULTIPOINT_FLOW_META[i+1]
+        if (
+            "MULTIPOINT_FLOW_META" in state.FILES
+            and state.FILES.MULTIPOINT_FLOW_META[i + 1]
+        ):
+            ztate.FILES["FLOW_META"] = state.FILES.MULTIPOINT_FLOW_META[i + 1]
 
         files = ztate.FILES
         link = []
-        files['DIRECT'] = state.FILES.MULTIPOINT_DIRECT[i+1]
+        files["DIRECT"] = state.FILES.MULTIPOINT_DIRECT[i + 1]
 
         # files: mesh
-        name = files['MESH']
-        name = su2io.expand_part(name,konfig)
+        name = files["MESH"]
+        name = su2io.expand_part(name, konfig)
         link.extend(name)
 
         # files: direct solution
-        if 'DIRECT' in files:
-            name = files['DIRECT']
-            name = su2io.expand_time(name,konfig)
-            link.extend( name )
+        if "DIRECT" in files:
+            name = files["DIRECT"]
+            name = su2io.expand_time(name, konfig)
+            link.extend(name)
 
         # files: adjoint solution
         if ADJ_NAME in files:
             name = files[ADJ_NAME]
-            name = su2io.expand_time(name,konfig)
+            name = su2io.expand_time(name, konfig)
             link.extend(name)
         else:
-            konfig['RESTART_SOL'] = 'NO'
+            konfig["RESTART_SOL"] = "NO"
 
         # files: meta data of solution
-        if 'FLOW_META' in files:
-            pull.append(files['FLOW_META'])
+        if "FLOW_META" in files:
+            pull.append(files["FLOW_META"])
 
         # pull needed files, start folder
-        with redirect_folder( folder[i+1], pull, link ) as push:
+        with redirect_folder(folder[i + 1], pull, link) as push:
             with redirect_output(log_direct):
 
                 # Set the multipoint options
-                konfig.AOA = aoa_list[i+1]
-                konfig.SIDESLIP_ANGLE = sideslip_list[i+1]
-                konfig.MACH_NUMBER = mach_list[i+1]
-                konfig.REYNOLDS_NUMBER = reynolds_list[i+1]
-                konfig.FREESTREAM_TEMPERATURE = freestream_temp_list[i+1]
-                konfig.FREESTREAM_PRESSURE = freestream_press_list[i+1]
-                konfig.TARGET_CL = target_cl_list[i+1]
+                konfig.AOA = aoa_list[i + 1]
+                konfig.SIDESLIP_ANGLE = sideslip_list[i + 1]
+                konfig.MACH_NUMBER = mach_list[i + 1]
+                konfig.REYNOLDS_NUMBER = reynolds_list[i + 1]
+                konfig.FREESTREAM_TEMPERATURE = freestream_temp_list[i + 1]
+                konfig.FREESTREAM_PRESSURE = freestream_press_list[i + 1]
+                konfig.TARGET_CL = target_cl_list[i + 1]
 
                 # rename meta data to flow.meta
-                if 'FLOW_META' in ztate.FILES:
-                    os.rename(ztate.FILES.MULTIPOINT_FLOW_META[i+1], 'flow.meta')
-                    ztate.FILES['FLOW_META'] = 'flow.meta'
+                if "FLOW_META" in ztate.FILES:
+                    os.rename(ztate.FILES.MULTIPOINT_FLOW_META[i + 1], "flow.meta")
+                    ztate.FILES["FLOW_META"] = "flow.meta"
 
                 # let's start somethin somthin
                 ztate.GRADIENTS.clear()
 
                 # the gradient
-                grads[i+1] = gradient(base_name,'DISCRETE_ADJOINT',konfig,ztate)
+                grads[i + 1] = gradient(base_name, "DISCRETE_ADJOINT", konfig, ztate)
 
                 # rename meta data to multipoint name
-                if os.path.exists('flow.meta'):
-                    os.rename('flow.meta', flow_meta_list[i+1])
+                if os.path.exists("flow.meta"):
+                    os.rename("flow.meta", flow_meta_list[i + 1])
 
                 # adjoint files to push
                 dst = os.getcwd()
-                dst = os.path.abspath(dst).rstrip('/')+'/'+ztate.FILES[ADJ_NAME]
+                dst = os.path.abspath(dst).rstrip("/") + "/" + ztate.FILES[ADJ_NAME]
                 name = ztate.FILES[ADJ_NAME]
-                solution_adj_list[i+1] = name
-                name = su2io.expand_zones(name,konfig)
-                name = su2io.expand_time(name,konfig)
+                solution_adj_list[i + 1] = name
+                name = su2io.expand_zones(name, konfig)
+                name = su2io.expand_time(name, konfig)
                 push.extend(name)
 
         # Link adjoint solution to MULTIPOINT_# folder
         src = os.getcwd()
-        src = os.path.abspath(src).rstrip('/')+'/'+ztate.FILES[ADJ_NAME]
+        src = os.path.abspath(src).rstrip("/") + "/" + ztate.FILES[ADJ_NAME]
 
         # make unix link
         string = "ln -s " + src + " " + dst
@@ -704,7 +754,9 @@ def multipoint( func_name, config, state=None, step=1e-2 ):
     for variable in range(len(grads[0])):
         grad[variable] = 0.0
         for point in range(len(weight_list)):
-            grad[variable] = grad[variable] + float(weight_list[point])*grads[point][variable]
+            grad[variable] = (
+                grad[variable] + float(weight_list[point]) * grads[point][variable]
+            )
 
     state.GRADIENTS[func_name] = grad
     grads_out = su2util.ordered_bunch()
@@ -717,32 +769,33 @@ def multipoint( func_name, config, state=None, step=1e-2 ):
 #  Finite Difference Gradients
 # ----------------------------------------------------------------------
 
-def findiff( config, state=None ):
-    """ vals = SU2.eval.findiff(config,state=None)
 
-        Evaluates the aerodynamics gradients using
-        finite differencing with:
-            SU2.eval.func()
-            SU2.run.deform()
-            SU2.run.direct()
+def findiff(config, state=None):
+    """vals = SU2.eval.findiff(config,state=None)
+
+    Evaluates the aerodynamics gradients using
+    finite differencing with:
+        SU2.eval.func()
+        SU2.run.deform()
+        SU2.run.direct()
 
-        Assumptions:
-            Config is already setup for deformation.
-            Mesh may or may not be deformed.
-            Updates config and state by reference.
-            Gradient Redundancy if state.GRADIENTS has the key func_name.
-            Direct Redundancy if state.FUNCTIONS has key func_name.
+    Assumptions:
+        Config is already setup for deformation.
+        Mesh may or may not be deformed.
+        Updates config and state by reference.
+        Gradient Redundancy if state.GRADIENTS has the key func_name.
+        Direct Redundancy if state.FUNCTIONS has key func_name.
 
-        Executes in:
-            ./FINDIFF
+    Executes in:
+        ./FINDIFF
 
-        Inputs:
-            config - an SU2 config
-            state  - optional, an SU2 state
+    Inputs:
+        config - an SU2 config
+        state  - optional, an SU2 state
 
-        Outputs:
-            A Bunch() with keys of objective function names
-            and values of list of floats of gradient values
+    Outputs:
+        A Bunch() with keys of objective function names
+        and values of list of floats of gradient values
     """
 
     # ----------------------------------------------------
@@ -752,28 +805,28 @@ def findiff( config, state=None ):
     # initialize
     state = su2io.State(state)
     special_cases = su2io.get_specialCases(config)
-    Definition_DV = config['DEFINITION_DV']
+    Definition_DV = config["DEFINITION_DV"]
 
     # console output
-    if config.get('CONSOLE','VERBOSE') in ['QUIET','CONCISE']:
-        log_findiff = 'log_FinDiff.out'
+    if config.get("CONSOLE", "VERBOSE") in ["QUIET", "CONCISE"]:
+        log_findiff = "log_FinDiff.out"
     else:
         log_findiff = None
 
     # evaluate step length or set default value
-    if 'FIN_DIFF_STEP' in config:
+    if "FIN_DIFF_STEP" in config:
         step = float(config.FIN_DIFF_STEP)
     else:
         step = 0.001
 
     opt_names = []
-    for i in range(config['NZONES']):
+    for i in range(config["NZONES"]):
         for key in sorted(su2io.historyOutFields):
-            if su2io.historyOutFields[key]['TYPE'] == 'COEFFICIENT':
-                if (config['NZONES'] == 1):
+            if su2io.historyOutFields[key]["TYPE"] == "COEFFICIENT":
+                if config["NZONES"] == 1:
                     opt_names.append(key)
                 else:
-                    opt_names.append(key + '[' + str(i) + ']')
+                    opt_names.append(key + "[" + str(i) + "]")
 
     # ----------------------------------------------------
     #  Redundancy Check
@@ -782,7 +835,7 @@ def findiff( config, state=None ):
     # master redundancy check
     findiff_todo = all([key in state.GRADIENTS for key in opt_names])
     if findiff_todo:
-        grads = state['GRADIENTS']
+        grads = state["GRADIENTS"]
         return copy.deepcopy(grads)
 
     # ----------------------------------------------------
@@ -790,17 +843,17 @@ def findiff( config, state=None ):
     # ----------------------------------------------------
 
     # run
-    func_base = function( 'ALL', config, state )
+    func_base = function("ALL", config, state)
 
     # ----------------------------------------------------
     #  Plot Setup
     # ----------------------------------------------------
 
-    grad_filename  = config['GRAD_OBJFUNC_FILENAME']
-    grad_filename  = os.path.splitext( grad_filename )[0]
-    output_format  = config['TABULAR_FORMAT']
+    grad_filename = config["GRAD_OBJFUNC_FILENAME"]
+    grad_filename = os.path.splitext(grad_filename)[0]
+    output_format = config["TABULAR_FORMAT"]
     plot_extension = su2io.get_extension(output_format)
-    grad_filename  = grad_filename + '_findiff' + plot_extension
+    grad_filename = grad_filename + "_findiff" + plot_extension
 
     # ----------------------------------------------------
     #  Finite Difference Steps
@@ -810,108 +863,109 @@ def findiff( config, state=None ):
     konfig = copy.deepcopy(config)
 
     # check deformation setup
-    n_dv = sum(Definition_DV['SIZE'])
-    deform_set = konfig['DV_KIND'] == Definition_DV['KIND']
+    n_dv = sum(Definition_DV["SIZE"])
+    deform_set = konfig["DV_KIND"] == Definition_DV["KIND"]
     if not deform_set:
         dvs_base = [0.0] * n_dv
-        konfig.unpack_dvs(dvs_base,dvs_base)
+        konfig.unpack_dvs(dvs_base, dvs_base)
     else:
-        dvs_base = konfig['DV_VALUE_NEW']
+        dvs_base = konfig["DV_VALUE_NEW"]
 
     # initialize gradients
-    func_keys = ['VARIABLE'] + opt_names + ['FINDIFF_STEP']
+    func_keys = ["VARIABLE"] + opt_names + ["FINDIFF_STEP"]
     grads = su2util.ordered_bunch.fromkeys(func_keys)
-    for key in grads.keys(): grads[key] = []
+    for key in grads.keys():
+        grads[key] = []
 
     # step vector
-    if isinstance(step,list):
-        assert n_dv == len(step) , 'unexpected step vector length'
+    if isinstance(step, list):
+        assert n_dv == len(step), "unexpected step vector length"
     else:
         step = [step] * n_dv
 
     # files to pull
-    files = state['FILES']
-    pull = []; link = []
-    pull.extend(config.get('CONFIG_LIST',[]))
+    files = state["FILES"]
+    pull = []
+    link = []
+    pull.extend(config.get("CONFIG_LIST", []))
     # files: mesh
-    name = files['MESH']
-    name = su2io.expand_part(name,konfig)
+    name = files["MESH"]
+    name = su2io.expand_part(name, konfig)
     link.extend(name)
     # files: direct solution
-    if 'DIRECT' in files:
-        name = files['DIRECT']
-        name = su2io.expand_time(name,config)
+    if "DIRECT" in files:
+        name = files["DIRECT"]
+        name = su2io.expand_time(name, config)
         link.extend(name)
 
     # files: restart solution for dual-time stepping first and second order
-    if 'RESTART_FILE_1' in files:
-        name = files['RESTART_FILE_1']
+    if "RESTART_FILE_1" in files:
+        name = files["RESTART_FILE_1"]
         pull.append(name)
-    if 'RESTART_FILE_2' in files:
-        name = files['RESTART_FILE_2']
+    if "RESTART_FILE_2" in files:
+        name = files["RESTART_FILE_2"]
         pull.append(name)
 
     # files: target equivarea distribution
-    if 'EQUIV_AREA' in special_cases and 'TARGET_EA' in files:
-        pull.append(files['TARGET_EA'])
+    if "EQUIV_AREA" in special_cases and "TARGET_EA" in files:
+        pull.append(files["TARGET_EA"])
 
     # files: target pressure distribution
-    if 'INV_DESIGN_CP' in special_cases and 'TARGET_CP' in files:
-        pull.append(files['TARGET_CP'])
+    if "INV_DESIGN_CP" in special_cases and "TARGET_CP" in files:
+        pull.append(files["TARGET_CP"])
 
     # files: target heat flux distribution
-    if 'INV_DESIGN_HEATFLUX' in special_cases and 'TARGET_HEATFLUX' in files:
-        pull.append(files['TARGET_HEATFLUX'])
-
+    if "INV_DESIGN_HEATFLUX" in special_cases and "TARGET_HEATFLUX" in files:
+        pull.append(files["TARGET_HEATFLUX"])
 
     # output redirection
-    with redirect_folder('FINDIFF',pull,link) as push:
+    with redirect_folder("FINDIFF", pull, link) as push:
         with redirect_output(log_findiff):
 
             # iterate each dv
             for i_dv in range(n_dv):
 
                 this_step = step[i_dv]
-                temp_config_name = 'config_FINDIFF_%i.cfg' % i_dv
+                temp_config_name = "config_FINDIFF_%i.cfg" % i_dv
 
-                this_dvs    = copy.deepcopy(dvs_base)
+                this_dvs = copy.deepcopy(dvs_base)
                 this_konfig = copy.deepcopy(konfig)
                 this_dvs[i_dv] = this_dvs[i_dv] + this_step
 
                 this_state = su2io.State()
-                this_state.FILES = copy.deepcopy( state.FILES )
-                this_konfig.unpack_dvs(this_dvs,dvs_base)
+                this_state.FILES = copy.deepcopy(state.FILES)
+                this_konfig.unpack_dvs(this_dvs, dvs_base)
 
                 this_konfig.dump(temp_config_name)
 
                 # Direct Solution, findiff step
-                func_step = function( 'ALL', this_konfig, this_state )
+                func_step = function("ALL", this_konfig, this_state)
 
                 # remove deform step files
                 meshfiles = this_state.FILES.MESH
-                meshfiles = su2io.expand_part(meshfiles,this_konfig)
-                for name in meshfiles: os.remove(name)
+                meshfiles = su2io.expand_part(meshfiles, this_konfig)
+                for name in meshfiles:
+                    os.remove(name)
 
                 for key in grads.keys():
-                    if key == 'VARIABLE' or key == 'FINDIFF_STEP':
+                    if key == "VARIABLE" or key == "FINDIFF_STEP":
                         pass
                     elif not key in func_step:
                         del grads[key]
 
                 # calc finite difference and store
                 for key in grads.keys():
-                    if key == 'VARIABLE':
+                    if key == "VARIABLE":
                         grads[key].append(i_dv)
-                    elif key == 'FINDIFF_STEP':
+                    elif key == "FINDIFF_STEP":
                         grads[key].append(this_step)
                     else:
-                        this_grad = ( func_step[key] - func_base[key] ) / this_step
+                        this_grad = (func_step[key] - func_base[key]) / this_step
                         grads[key].append(this_grad)
 
-
                 #: for each grad name
 
-                su2util.write_plot(grad_filename,output_format,grads)
+                su2util.write_plot(grad_filename, output_format, grads)
                 os.remove(temp_config_name)
 
             #: for each dv
@@ -919,14 +973,15 @@ def findiff( config, state=None ):
     #: with output redirection
 
     # remove plot items
-    del grads['VARIABLE']
-    del grads['FINDIFF_STEP']
+    del grads["VARIABLE"]
+    del grads["FINDIFF_STEP"]
     state.GRADIENTS.update(grads)
 
     # return results
     grads = copy.deepcopy(grads)
     return grads
 
+
 #: def findiff()
 
 
@@ -934,29 +989,30 @@ def findiff( config, state=None ):
 #  Geometric Gradients
 # ----------------------------------------------------------------------
 
-def geometry( func_name, config, state=None ):
-    """ val = SU2.eval.geometry(config,state=None)
 
-        Evaluates geometry with the following:
-            SU2.run.deform()
-            SU2.run.geometry()
+def geometry(func_name, config, state=None):
+    """val = SU2.eval.geometry(config,state=None)
 
-        Assumptions:
-            Config is already setup for deformation.
-            Mesh may or may not be deformed.
-            Updates config and state by reference.
-            Redundancy if state.FUNCTIONS does not have func_name.
+    Evaluates geometry with the following:
+        SU2.run.deform()
+        SU2.run.geometry()
 
-        Executes in:
-            ./GEOMETRY
+    Assumptions:
+        Config is already setup for deformation.
+        Mesh may or may not be deformed.
+        Updates config and state by reference.
+        Redundancy if state.FUNCTIONS does not have func_name.
 
-        Inputs:
-            config    - an SU2 config
-            state     - optional, an SU2 state
+    Executes in:
+        ./GEOMETRY
 
-        Outputs:
-            Bunch() of functions with keys of objective function names
-            and values of objective function floats.
+    Inputs:
+        config    - an SU2 config
+        state     - optional, an SU2 state
+
+    Outputs:
+        Bunch() of functions with keys of objective function names
+        and values of objective function floats.
     """
 
     # ----------------------------------------------------
@@ -965,13 +1021,13 @@ def geometry( func_name, config, state=None ):
 
     # initialize
     state = su2io.State(state)
-    if not 'MESH' in state.FILES:
-        state.FILES.MESH = config['MESH_FILENAME']
+    if not "MESH" in state.FILES:
+        state.FILES.MESH = config["MESH_FILENAME"]
     special_cases = su2io.get_specialCases(config)
 
     # console output
-    if config.get('CONSOLE','VERBOSE') in ['QUIET','CONCISE']:
-        log_geom = 'log_Geometry.out'
+    if config.get("CONSOLE", "VERBOSE") in ["QUIET", "CONCISE"]:
+        log_geom = "log_Geometry.out"
     else:
         log_geom = None
 
@@ -982,35 +1038,35 @@ def geometry( func_name, config, state=None ):
     # does decomposition and deformation
     # info = update_mesh(config,state)
 
-
     # ----------------------------------------------------
     #  Geometry Solution
     # ----------------------------------------------------
 
     # redundancy check
     geometry_done = func_name in state.GRADIENTS
-    #geometry_done = all([key in state.FUNCTIONS for key in su2io.optnames_geo])
+    # geometry_done = all([key in state.FUNCTIONS for key in su2io.optnames_geo])
     if not geometry_done:
 
         # files to pull
         files = state.FILES
-        pull = []; link = []
+        pull = []
+        link = []
 
         # files: mesh
-        name = files['MESH']
-        name = su2io.expand_part(name,config)
+        name = files["MESH"]
+        name = su2io.expand_part(name, config)
         link.extend(name)
 
         # update function name
         ## TODO
 
         # output redirection
-        with redirect_folder( 'GEOMETRY', pull, link ) as push:
+        with redirect_folder("GEOMETRY", pull, link) as push:
             with redirect_output(log_geom):
 
                 # setup config
                 config.GEO_PARAM = func_name
-                config.GEO_MODE  = 'GRADIENT'
+                config.GEO_MODE = "GRADIENT"
 
                 # # RUN GEOMETRY SOLUTION # #
                 info = su2run.geometry(config)
@@ -1022,14 +1078,14 @@ def geometry( func_name, config, state=None ):
 
     #: if not redundant
 
-
     # return output
     grads = su2util.ordered_bunch()
     for key in su2io.optnames_geo:
-        if key in state['GRADIENTS']:
-            grads[key] = state['GRADIENTS'][key]
+        if key in state["GRADIENTS"]:
+            grads[key] = state["GRADIENTS"][key]
     return grads
 
+
 #: def geometry()
 
 
@@ -1037,34 +1093,35 @@ def geometry( func_name, config, state=None ):
 #  Direct Differentiation Gradients
 # ----------------------------------------------------------------------
 
-def directdiff( config, state=None ):
-    """ vals = SU2.eval.directdiff(config,state=None)
-
-        Evaluates the aerodynamics gradients using
-        direct differentiation with:
-            SU2.eval.func()
-            SU2.run.deform()
-            SU2.run.direct()
-
-        Assumptions:
-            Config is already setup for deformation.
-            Mesh may or may not be deformed.
-            Updates config and state by reference.
-            Gradient Redundancy if state.GRADIENTS has the key func_name.
-            Direct Redundancy if state.FUNCTIONS has key func_name.
-
-        Executes in:
-            ./DIRECTDIFF
-
-        Inputs:
-            config - an SU2 config
-            state  - optional, an SU2 state
-            step   - finite difference step size, as a float or
-                     list of floats of length n_DV
-
-        Outputs:
-            A Bunch() with keys of objective function names
-            and values of list of floats of gradient values
+
+def directdiff(config, state=None):
+    """vals = SU2.eval.directdiff(config,state=None)
+
+    Evaluates the aerodynamics gradients using
+    direct differentiation with:
+        SU2.eval.func()
+        SU2.run.deform()
+        SU2.run.direct()
+
+    Assumptions:
+        Config is already setup for deformation.
+        Mesh may or may not be deformed.
+        Updates config and state by reference.
+        Gradient Redundancy if state.GRADIENTS has the key func_name.
+        Direct Redundancy if state.FUNCTIONS has key func_name.
+
+    Executes in:
+        ./DIRECTDIFF
+
+    Inputs:
+        config - an SU2 config
+        state  - optional, an SU2 state
+        step   - finite difference step size, as a float or
+                 list of floats of length n_DV
+
+    Outputs:
+        A Bunch() with keys of objective function names
+        and values of list of floats of gradient values
     """
 
     # ----------------------------------------------------
@@ -1074,11 +1131,11 @@ def directdiff( config, state=None ):
     # initialize
     state = su2io.State(state)
     special_cases = su2io.get_specialCases(config)
-    Definition_DV = config['DEFINITION_DV']
+    Definition_DV = config["DEFINITION_DV"]
 
     # console output
-    if config.get('CONSOLE','VERBOSE') in ['QUIET','CONCISE']:
-        log_directdiff = 'log_DirectDiff.out'
+    if config.get("CONSOLE", "VERBOSE") in ["QUIET", "CONCISE"]:
+        log_directdiff = "log_DirectDiff.out"
     else:
         log_directdiff = None
 
@@ -1089,23 +1146,23 @@ def directdiff( config, state=None ):
     # master redundancy check
     opt_names = []
     for key in sorted(su2io.historyOutFields):
-        if su2io.historyOutFields[key]['TYPE'] == 'COEFFICIENT':
+        if su2io.historyOutFields[key]["TYPE"] == "COEFFICIENT":
             opt_names.append(key)
 
     directdiff_todo = all([key in state.GRADIENTS for key in opt_names])
     if directdiff_todo:
-        grads = state['GRADIENTS']
+        grads = state["GRADIENTS"]
         return copy.deepcopy(grads)
 
     # ----------------------------------------------------
     #  Plot Setup
     # ----------------------------------------------------
 
-    grad_filename  = config['GRAD_OBJFUNC_FILENAME']
-    grad_filename  = os.path.splitext( grad_filename )[0]
-    output_format  = config.get('TABULAR_FORMAT', 'CSV')
+    grad_filename = config["GRAD_OBJFUNC_FILENAME"]
+    grad_filename = os.path.splitext(grad_filename)[0]
+    output_format = config.get("TABULAR_FORMAT", "CSV")
     plot_extension = su2io.get_extension(output_format)
-    grad_filename  = grad_filename + '_directdiff' + plot_extension
+    grad_filename = grad_filename + "_directdiff" + plot_extension
 
     # ----------------------------------------------------
     # Direct Differentiation Evaluation
@@ -1114,84 +1171,86 @@ def directdiff( config, state=None ):
     # local config
     konfig = copy.deepcopy(config)
 
-    n_dv = sum(Definition_DV['SIZE'])
+    n_dv = sum(Definition_DV["SIZE"])
 
     # initialize gradients
     func_keys = opt_names
-    func_keys = ['VARIABLE'] + func_keys
+    func_keys = ["VARIABLE"] + func_keys
     grads = su2util.ordered_bunch.fromkeys(func_keys)
-    for key in grads.keys(): grads[key] = []
+    for key in grads.keys():
+        grads[key] = []
 
     # files to pull
-    files = state['FILES']
-    pull = []; link = []
+    files = state["FILES"]
+    pull = []
+    link = []
     # files: mesh
-    name = files['MESH']
-    name = su2io.expand_part(name,konfig)
+    name = files["MESH"]
+    name = su2io.expand_part(name, konfig)
     link.extend(name)
 
-    if 'FLOW_META' in files:
-        pull.append(files['FLOW_META'])
+    if "FLOW_META" in files:
+        pull.append(files["FLOW_META"])
 
     # files: direct solution
-    if 'DIRECT' in files:
-        name = files['DIRECT']
-        name = su2io.expand_time(name,config)
+    if "DIRECT" in files:
+        name = files["DIRECT"]
+        name = su2io.expand_time(name, config)
         link.extend(name)
 
     # files: target equivarea distribution
-    if 'EQUIV_AREA' in special_cases and 'TARGET_EA' in files:
-        pull.append(files['TARGET_EA'])
+    if "EQUIV_AREA" in special_cases and "TARGET_EA" in files:
+        pull.append(files["TARGET_EA"])
 
     # files: target pressure distribution
-    if 'INV_DESIGN_CP' in special_cases and 'TARGET_CP' in files:
-        pull.append(files['TARGET_CP'])
+    if "INV_DESIGN_CP" in special_cases and "TARGET_CP" in files:
+        pull.append(files["TARGET_CP"])
 
     # files: target heat flux distribution
-    if 'INV_DESIGN_HEATFLUX' in special_cases and 'TARGET_HEATFLUX' in files:
-        pull.append(files['TARGET_HEATFLUX'])
+    if "INV_DESIGN_HEATFLUX" in special_cases and "TARGET_HEATFLUX" in files:
+        pull.append(files["TARGET_HEATFLUX"])
 
     # output redirection
-    with redirect_folder('DIRECTDIFF',pull,link) as push:
+    with redirect_folder("DIRECTDIFF", pull, link) as push:
         with redirect_output(log_directdiff):
 
             # iterate each dv
             for i_dv in range(n_dv):
 
-                temp_config_name = 'config_DIRECTDIFF_%i.cfg' % i_dv
+                temp_config_name = "config_DIRECTDIFF_%i.cfg" % i_dv
 
                 this_konfig = copy.deepcopy(konfig)
 
-                this_dvs = [0.0]*n_dv
+                this_dvs = [0.0] * n_dv
                 this_dvs[i_dv] = 1.0
-                this_dvs_old = [0.0]*n_dv
+                this_dvs_old = [0.0] * n_dv
                 this_dvs_old[i_dv] = 1.0
                 this_state = su2io.State()
-                this_state.FILES = copy.deepcopy( state.FILES )
+                this_state.FILES = copy.deepcopy(state.FILES)
                 this_konfig.unpack_dvs(this_dvs, this_dvs_old)
 
                 this_konfig.dump(temp_config_name)
 
                 # Direct Solution
-                func_step = function( 'ALL', this_konfig, this_state )
+                func_step = function("ALL", this_konfig, this_state)
 
                 # delete keys not returned by the solver
                 for key in grads.keys():
-                    if key == 'VARIABLE':
+                    if key == "VARIABLE":
                         pass
-                    elif not 'D_' + key in func_step:
+                    elif not "D_" + key in func_step:
                         del grads[key]
 
                 # store
                 for key in grads.keys():
-                    if key == 'VARIABLE':
+                    if key == "VARIABLE":
                         grads[key].append(i_dv)
                     else:
-                        this_grad = func_step['D_' + key]
+                        this_grad = func_step["D_" + key]
                         grads[key].append(this_grad)
                 #: for each grad name
 
-                su2util.write_plot(grad_filename,output_format,grads)
+                su2util.write_plot(grad_filename, output_format, grads)
                 os.remove(temp_config_name)
 
             #: for each dv
@@ -1199,7 +1258,7 @@ def directdiff( config, state=None ):
     #: with output redirection
 
     # remove plot items
-    del grads['VARIABLE']
+    del grads["VARIABLE"]
     state.GRADIENTS.update(grads)
     state.update(this_state)
 
@@ -1207,5 +1266,5 @@ def directdiff( config, state=None ):
     grads = copy.deepcopy(grads)
     return grads
 
-#: def directdiff()
 
+#: def directdiff()
diff --git a/SU2_PY/SU2/io/__init__.py b/SU2_PY/SU2/io/__init__.py
index d79c0aa59c2..8b222a5d021 100644
--- a/SU2_PY/SU2/io/__init__.py
+++ b/SU2_PY/SU2/io/__init__.py
@@ -1,11 +1,11 @@
 # SU2/io/__init__.py
 
-from .tools    import *
+from .tools import *
 from .redirect import output as redirect_output
 from .redirect import folder as redirect_folder
-from .data     import load_data, save_data
+from .data import load_data, save_data
 from .filelock import filelock
 
-from .config   import Config
-from .state    import State_Factory as State
+from .config import Config
+from .state import State_Factory as State
 from .historyMap import history_header_map as historyOutFields
diff --git a/SU2_PY/SU2/io/config.py b/SU2_PY/SU2/io/config.py
index 2376dcf0408..e80e61ff900 100755
--- a/SU2_PY/SU2/io/config.py
+++ b/SU2_PY/SU2/io/config.py
@@ -45,56 +45,57 @@
 #  Configuration Class
 # ----------------------------------------------------------------------
 
+
 class Config(ordered_bunch):
-    """ config = SU2.io.Config(filename="")
-
-        Starts a config class, an extension of
-        ordered_bunch()
-
-        use 1: initialize by reading config file
-            config = SU2.io.Config('filename')
-        use 2: initialize from dictionary or bunch
-            config = SU2.io.Config(param_dict)
-        use 3: initialize empty
-            config = SU2.io.Config()
-
-        Parameters can be accessed by item or attribute
-        ie: config['MESH_FILENAME'] or config.MESH_FILENAME
-
-        Methods:
-            read()       - read from a config file
-            write()      - write to a config file (requires existing file)
-            dump()       - dump a raw config file
-            unpack_dvs() - unpack a design vector
-            diff()       - returns the difference from another config
-            dist()       - computes the distance from another config
+    """config = SU2.io.Config(filename="")
+
+    Starts a config class, an extension of
+    ordered_bunch()
+
+    use 1: initialize by reading config file
+        config = SU2.io.Config('filename')
+    use 2: initialize from dictionary or bunch
+        config = SU2.io.Config(param_dict)
+    use 3: initialize empty
+        config = SU2.io.Config()
+
+    Parameters can be accessed by item or attribute
+    ie: config['MESH_FILENAME'] or config.MESH_FILENAME
+
+    Methods:
+        read()       - read from a config file
+        write()      - write to a config file (requires existing file)
+        dump()       - dump a raw config file
+        unpack_dvs() - unpack a design vector
+        diff()       - returns the difference from another config
+        dist()       - computes the distance from another config
     """
 
-    _filename = 'config.cfg'
+    _filename = "config.cfg"
 
-    def __init__(self,*args,**kwarg):
+    def __init__(self, *args, **kwarg):
 
         # look for filename in inputs
-        if args and isinstance(args[0],str):
+        if args and isinstance(args[0], str):
             filename = args[0]
             args = args[1:]
-        elif 'filename' in kwarg:
-            filename = kwarg['filename']
-            del kwarg['filename']
+        elif "filename" in kwarg:
+            filename = kwarg["filename"]
+            del kwarg["filename"]
         else:
-            filename = ''
+            filename = ""
 
         # initialize ordered bunch
-        super(Config,self).__init__(*args,**kwarg)
+        super(Config, self).__init__(*args, **kwarg)
 
         # read config if it exists
         if filename:
             try:
                 self.read(filename)
             except IOError:
-                print('Could not find config file: %s' % filename)
+                print("Could not find config file: %s" % filename)
             except:
-                print('Unexpected error: ', sys.exc_info()[0])
+                print("Unexpected error: ", sys.exc_info()[0])
                 raise
         self._filename = filename
 
@@ -104,81 +105,82 @@ def __init__(self,*args,**kwarg):
             diff_objective = self.get("OBJECTIVE_FUNCTION")
             constrFuncFields = self.get("OPT_CONSTRAINT")
 
-            #OPT_OBJECTIVES
-            if bool (objFuncsFields):
+            # OPT_OBJECTIVES
+            if bool(objFuncsFields):
                 for key in objFuncsFields:
                     tavg_keyGroup = "TAVG_" + historyOutFields[key]["GROUP"]
-                    if  not tavg_keyGroup in histFields:
+                    if not tavg_keyGroup in histFields:
                         histFields.append(tavg_keyGroup)
 
                     dtavg_keyGroup = "D_TAVG_" + historyOutFields[key]["GROUP"]
                     if not dtavg_keyGroup in histFields:
                         histFields.append(dtavg_keyGroup)
 
-            #OPT_CONSTRAINTS
-            if bool (constrFuncFields):
+            # OPT_CONSTRAINTS
+            if bool(constrFuncFields):
                 for key in constrFuncFields:
                     eqIneqConstrFunc = constrFuncFields.get(key)
                     for key_inner in eqIneqConstrFunc:
                         tavg_keyGroup = "TAVG_" + historyOutFields[key_inner]["GROUP"]
-                        if  not tavg_keyGroup in histFields:
+                        if not tavg_keyGroup in histFields:
                             histFields.append(tavg_keyGroup)
 
-            #DIRECT_DIFF Field
+            # DIRECT_DIFF Field
             if diff_objective in historyOutFields:
                 tavg_keyGroup = "TAVG_" + historyOutFields[diff_objective]["GROUP"]
-                if  not tavg_keyGroup in histFields:
+                if not tavg_keyGroup in histFields:
                     histFields.append(tavg_keyGroup)
 
                 dtavg_keyGroup = "D_TAVG_" + historyOutFields[diff_objective]["GROUP"]
                 if not dtavg_keyGroup in histFields:
                     histFields.append(dtavg_keyGroup)
 
-            self["HISTORY_OUTPUT"]= histFields
-
+            self["HISTORY_OUTPUT"] = histFields
 
-    def read(self,filename):
-        """ reads from a config file """
+    def read(self, filename):
+        """reads from a config file"""
         konfig = read_config(filename)
         self.update(konfig)
 
-    def write(self,filename=''):
-        """ updates an existing config file """
-        if not filename: filename = self._filename
-        assert os.path.exists(filename) , 'must write over an existing config file'
-        write_config(filename,self)
+    def write(self, filename=""):
+        """updates an existing config file"""
+        if not filename:
+            filename = self._filename
+        assert os.path.exists(filename), "must write over an existing config file"
+        write_config(filename, self)
 
-    def dump(self,filename=''):
-        """ dumps all items in the config bunch, without comments """
-        if not filename: filename = self._filename
-        dump_config(filename,self)
+    def dump(self, filename=""):
+        """dumps all items in the config bunch, without comments"""
+        if not filename:
+            filename = self._filename
+        dump_config(filename, self)
 
-    def __getattr__(self,k):
+    def __getattr__(self, k):
         try:
-            return super(Config,self).__getattr__(k)
+            return super(Config, self).__getattr__(k)
         except AttributeError:
-            raise AttributeError('Config parameter not found')
+            raise AttributeError("Config parameter not found")
 
-    def __getitem__(self,k):
+    def __getitem__(self, k):
         try:
-            return super(Config,self).__getitem__(k)
+            return super(Config, self).__getitem__(k)
         except KeyError:
-            raise KeyError('Config parameter not found: %s' % k)
+            raise KeyError("Config parameter not found: %s" % k)
 
-    def unpack_dvs(self,dv_new,dv_old=None):
-        """ updates config with design variable vectors
-            will scale according to each DEFINITION_DV scale parameter
+    def unpack_dvs(self, dv_new, dv_old=None):
+        """updates config with design variable vectors
+        will scale according to each DEFINITION_DV scale parameter
 
-            Modifies:
-                DV_KIND
-                DV_MARKER
-                DV_PARAM
-                DV_VALUE_OLD
-                DV_VALUE_NEW
+        Modifies:
+            DV_KIND
+            DV_MARKER
+            DV_PARAM
+            DV_VALUE_OLD
+            DV_VALUE_NEW
 
-            Inputs:
-                dv_new - list or array of new dv values
-                dv_old - optional, list or array of old dv values, defaults to zeros
+        Inputs:
+            dv_new - list or array of new dv values
+            dv_old - optional, list or array of old dv values, defaults to zeros
 
         """
 
@@ -186,96 +188,95 @@ def unpack_dvs(self,dv_new,dv_old=None):
         dv_old = copy.deepcopy(dv_old)
 
         # handle unpacking cases
-        def_dv = self['DEFINITION_DV']
+        def_dv = self["DEFINITION_DV"]
 
-        n_dv   = sum(def_dv['SIZE'])
+        n_dv = sum(def_dv["SIZE"])
 
-        if not dv_old: dv_old = [0.0]*n_dv
-        assert len(dv_new) == len(dv_old) , 'unexpected design vector length'
+        if not dv_old:
+            dv_old = [0.0] * n_dv
+        assert len(dv_new) == len(dv_old), "unexpected design vector length"
 
         # handle param
-        param_dv = self['DV_PARAM']
+        param_dv = self["DV_PARAM"]
 
         # apply scale
-        dv_scales = def_dv['SCALE']
+        dv_scales = def_dv["SCALE"]
 
         k = 0
         for i, dv_scl in enumerate(dv_scales):
-            for j in range(def_dv['SIZE'][i]):
-                dv_new[k] = dv_new[k]*dv_scl;
-                dv_old[k] = dv_old[k]*dv_scl;
+            for j in range(def_dv["SIZE"][i]):
+                dv_new[k] = dv_new[k] * dv_scl
+                dv_old[k] = dv_old[k] * dv_scl
                 k = k + 1
 
         # Change the parameters of the design variables
 
-        self['DV_KIND'] = def_dv['KIND']
-        param_dv['PARAM'] = def_dv['PARAM']
-        param_dv['FFDTAG'] = def_dv['FFDTAG']
-        param_dv['SIZE']   = def_dv['SIZE']
+        self["DV_KIND"] = def_dv["KIND"]
+        param_dv["PARAM"] = def_dv["PARAM"]
+        param_dv["FFDTAG"] = def_dv["FFDTAG"]
+        param_dv["SIZE"] = def_dv["SIZE"]
 
-        self.update({ 'DV_VALUE_OLD'     : dv_old              ,
-                      'DV_VALUE_NEW'     : dv_new              })
+        self.update({"DV_VALUE_OLD": dv_old, "DV_VALUE_NEW": dv_new})
 
-    def __eq__(self,konfig):
-        return super(Config,self).__eq__(konfig)
-    def __ne__(self,konfig):
-        return super(Config,self).__ne__(konfig)
+    def __eq__(self, konfig):
+        return super(Config, self).__eq__(konfig)
 
+    def __ne__(self, konfig):
+        return super(Config, self).__ne__(konfig)
 
     def local_files(self):
-        """ removes path prefix from all *_FILENAME params
-        """
+        """removes path prefix from all *_FILENAME params"""
         for key, value in self.items():
-            if key.split('_')[-1] == 'FILENAME':
+            if key.split("_")[-1] == "FILENAME":
                 self[key] = os.path.basename(value)
 
-    def diff(self,konfig):
-        """ compares self to another config
+    def diff(self, konfig):
+        """compares self to another config
 
-            Inputs:
-                konfig - a second config
+        Inputs:
+            konfig - a second config
 
-            Outputs:
-                config_diff - a config containing only the differing
-                    keys, each with values of a list of the different
-                    config values.
-                for example:
-                config_diff.MATH_PROBLEM = ['DIRECT','CONTINUOUS_ADJOINT']
+        Outputs:
+            config_diff - a config containing only the differing
+                keys, each with values of a list of the different
+                config values.
+            for example:
+            config_diff.MATH_PROBLEM = ['DIRECT','CONTINUOUS_ADJOINT']
 
         """
 
         keys = set([])
-        keys.update( self.keys() )
-        keys.update( konfig.keys() )
+        keys.update(self.keys())
+        keys.update(konfig.keys())
 
         konfig_diff = Config()
 
         for key in keys:
-            value1 = self.get(key,None)
-            value2 = konfig.get(key,None)
+            value1 = self.get(key, None)
+            value2 = konfig.get(key, None)
             if not value1 == value2:
-                konfig_diff[key] = [value1,value2]
+                konfig_diff[key] = [value1, value2]
 
         return konfig_diff
 
-    def dist(self,konfig,keys_check='ALL'):
-        """ calculates a distance to another config
+    def dist(self, konfig, keys_check="ALL"):
+        """calculates a distance to another config
 
-            Inputs:
-                konfig     - a second config
-                keys_check - optional, a list of keys to check
+        Inputs:
+            konfig     - a second config
+            keys_check - optional, a list of keys to check
 
-            Outputs:
-                distance   - a float
+        Outputs:
+            distance   - a float
 
-            Currently only works for DV_VALUE_NEW and DV_VALUE_OLD
-            Returns a large value otherwise
+        Currently only works for DV_VALUE_NEW and DV_VALUE_OLD
+        Returns a large value otherwise
 
         """
 
         konfig_diff = self.diff(konfig)
 
-        if keys_check == 'ALL':
+        if keys_check == "ALL":
             keys_check = konfig_diff.keys()
 
         distance = 0.0
@@ -286,14 +287,13 @@ def dist(self,konfig,keys_check='ALL'):
                 val1 = konfig_diff[key][0]
                 val2 = konfig_diff[key][1]
 
-                if key in ['DV_VALUE_NEW',
-                           'DV_VALUE_OLD']:
-                    val1 = np.array( val1 )
-                    val2 = np.array( val2 )
-                    this_diff = np.sqrt( np.sum( (val1-val2)**2 ) )
+                if key in ["DV_VALUE_NEW", "DV_VALUE_OLD"]:
+                    val1 = np.array(val1)
+                    val2 = np.array(val2)
+                    this_diff = np.sqrt(np.sum((val1 - val2) ** 2))
 
                 else:
-                    print('Warning, unexpected config difference')
+                    print("Warning, unexpected config difference")
                     this_diff = inf
 
                 distance += this_diff
@@ -304,28 +304,26 @@ def dist(self,konfig,keys_check='ALL'):
         return distance
 
     def __repr__(self):
-        #return '<Config> %s' % self._filename
+        # return '<Config> %s' % self._filename
         return self.__str__()
 
     def __str__(self):
-        output = 'Config: %s' % self._filename
-        for k,v in self.items():
-            output +=  '\n    %s= %s' % (k,v)
+        output = "Config: %s" % self._filename
+        for k, v in self.items():
+            output += "\n    %s= %s" % (k, v)
         return output
-#: class Config
-
-
-
 
 
+#: class Config
 
 
 # -------------------------------------------------------------------
 #  Get SU2 Configuration Parameters
 # -------------------------------------------------------------------
 
+
 def read_config(filename):
-    """ reads a config file """
+    """reads a config file"""
 
     # initialize output dictionary
     data_dict = OrderedDict()
@@ -340,12 +338,12 @@ def read_config(filename):
             break
 
         # remove line returns
-        line = line.strip('\r\n').strip()
+        line = line.strip("\r\n").strip()
 
-        if (len(line) == 0):
+        if len(line) == 0:
             continue
         # make sure it has useful data
-        if (line[0] == '%'):
+        if line[0] == "%":
             continue
 
         # --- Check if there is a line continuation character at the
@@ -354,34 +352,40 @@ def read_config(filename):
         # If there is a statement after a cont. char
         # throw an error. ---*/
 
-        while(line[0].endswith('\\') or len(line.split('\\')) > 1):
+        while line[0].endswith("\\") or len(line.split("\\")) > 1:
             tmp_line = input_file.readline()
             tmp_line = tmp_line.strip()
-            assert len(tmp_line.split('=')) <= 1, ('Statement found after line '
-                                                   'continuation character in config file %s' % tmp_line)
-            if (not tmp_line.startswith('%')):
-                line = line.split('\\')[0]
-                line += ' ' + tmp_line
+            assert len(tmp_line.split("=")) <= 1, (
+                "Statement found after line "
+                "continuation character in config file %s" % tmp_line
+            )
+            if not tmp_line.startswith("%"):
+                line = line.split("\\")[0]
+                line += " " + tmp_line
 
         # split across equals sign
-        line = line.split("=",1)
+        line = line.split("=", 1)
         this_param = line[0].strip()
         this_value = line[1].strip()
 
-        assert this_param not in data_dict, ('Config file has multiple specifications of %s' % this_param )
+        assert this_param not in data_dict, (
+            "Config file has multiple specifications of %s" % this_param
+        )
         for case in switch(this_param):
 
             # comma delimited lists of strings with or without paren's
-            if case("MARKER_EULER")      or\
-               case("MARKER_FAR")        or\
-               case("MARKER_PLOTTING")   or\
-               case("MARKER_MONITORING") or\
-               case("MARKER_SYM")        or\
-               case("DV_KIND")           :
+            if (
+                case("MARKER_EULER")
+                or case("MARKER_FAR")
+                or case("MARKER_PLOTTING")
+                or case("MARKER_MONITORING")
+                or case("MARKER_SYM")
+                or case("DV_KIND")
+            ):
                 # remove white space
-                this_value = ''.join(this_value.split())
+                this_value = "".join(this_value.split())
                 # remove parens
-                this_value = this_value.strip('()')
+                this_value = this_value.strip("()")
                 # split by comma
                 data_dict[this_param] = this_value.split(",")
                 break
@@ -389,80 +393,102 @@ def read_config(filename):
             # semicolon delimited lists of comma delimited lists of floats
             if case("DV_PARAM"):
                 # remove white space
-                info_General = ''.join(this_value.split())
+                info_General = "".join(this_value.split())
                 # split by semicolon
-                info_General = info_General.split(';')
+                info_General = info_General.split(";")
                 # build list of dv params, convert string to float
                 dv_Parameters = []
-                dv_FFDTag     = []
-                dv_Size       = []
+                dv_FFDTag = []
+                dv_Size = []
 
                 for this_dvParam in info_General:
-                    this_dvParam = this_dvParam.strip('()')
+                    this_dvParam = this_dvParam.strip("()")
                     this_dvParam = this_dvParam.split(",")
-                    this_dvSize  = 1
+                    this_dvSize = 1
 
                     # if FFD change the first element to work with numbers and float(x)
-                    if data_dict["DV_KIND"][0] in ['FFD_SETTING','FFD_ANGLE_OF_ATTACK','FFD_CONTROL_POINT','FFD_NACELLE','FFD_GULL','FFD_TWIST_2D','FFD_TWIST','FFD_ROTATION','FFD_CAMBER','FFD_THICKNESS','FFD_CONTROL_POINT_2D','FFD_CAMBER_2D','FFD_THICKNESS_2D']:
+                    if data_dict["DV_KIND"][0] in [
+                        "FFD_SETTING",
+                        "FFD_ANGLE_OF_ATTACK",
+                        "FFD_CONTROL_POINT",
+                        "FFD_NACELLE",
+                        "FFD_GULL",
+                        "FFD_TWIST_2D",
+                        "FFD_TWIST",
+                        "FFD_ROTATION",
+                        "FFD_CAMBER",
+                        "FFD_THICKNESS",
+                        "FFD_CONTROL_POINT_2D",
+                        "FFD_CAMBER_2D",
+                        "FFD_THICKNESS_2D",
+                    ]:
                         this_dvFFDTag = this_dvParam[0]
-                        this_dvParam[0] = '0'
+                        this_dvParam[0] = "0"
                     else:
                         this_dvFFDTag = []
 
-                    if not data_dict["DV_KIND"][0] in ['NO_DEFORMATION']:
-                        this_dvParam = [ float(x) for x in this_dvParam ]
+                    if not data_dict["DV_KIND"][0] in ["NO_DEFORMATION"]:
+                        this_dvParam = [float(x) for x in this_dvParam]
 
-                    if data_dict["DV_KIND"][0] in ['FFD_CONTROL_POINT_2D']:
+                    if data_dict["DV_KIND"][0] in ["FFD_CONTROL_POINT_2D"]:
                         if this_dvParam[3] == 0 and this_dvParam[4] == 0:
                             this_dvSize = 2
 
-                    if data_dict["DV_KIND"][0]in ['FFD_CONTROL_POINT']:
-                        if this_dvParam[4] == 0 and this_dvParam[5] == 0 and this_dvParam[6] == 0:
+                    if data_dict["DV_KIND"][0] in ["FFD_CONTROL_POINT"]:
+                        if (
+                            this_dvParam[4] == 0
+                            and this_dvParam[5] == 0
+                            and this_dvParam[6] == 0
+                        ):
                             this_dvSize = 3
 
-                    dv_FFDTag     = dv_FFDTag     + [this_dvFFDTag]
+                    dv_FFDTag = dv_FFDTag + [this_dvFFDTag]
                     dv_Parameters = dv_Parameters + [this_dvParam]
-                    dv_Size       = dv_Size       + [this_dvSize]
+                    dv_Size = dv_Size + [this_dvSize]
 
-            # store in a dictionary
-                dv_Definitions = { 'FFDTAG' : dv_FFDTag     ,
-                                   'PARAM'  : dv_Parameters ,
-                                   'SIZE'   : dv_Size}
+                # store in a dictionary
+                dv_Definitions = {
+                    "FFDTAG": dv_FFDTag,
+                    "PARAM": dv_Parameters,
+                    "SIZE": dv_Size,
+                }
 
                 data_dict[this_param] = dv_Definitions
                 break
 
             # comma delimited lists of floats
-            if case("DV_VALUE_OLD")    or\
-               case("DV_VALUE_NEW")    or\
-               case("DV_VALUE")        :
+            if case("DV_VALUE_OLD") or case("DV_VALUE_NEW") or case("DV_VALUE"):
                 # remove white space
-                this_value = ''.join(this_value.split())
+                this_value = "".join(this_value.split())
                 # split by comma, map to float, store in dictionary
-                data_dict[this_param] = list(map(float,this_value.split(",")))
+                data_dict[this_param] = list(map(float, this_value.split(",")))
                 break
 
             # float parameters
-            if case("MACH_NUMBER")            or\
-               case("AOA")                    or\
-               case("FIN_DIFF_STEP")          or\
-               case("CFL_NUMBER")             or\
-               case("HB_PERIOD")              or\
-               case("WRT_SOL_FREQ")           :
+            if (
+                case("MACH_NUMBER")
+                or case("AOA")
+                or case("FIN_DIFF_STEP")
+                or case("CFL_NUMBER")
+                or case("HB_PERIOD")
+                or case("WRT_SOL_FREQ")
+            ):
                 data_dict[this_param] = float(this_value)
                 break
 
             # int parameters
-            if case("NUMBER_PART")            or\
-               case("AVAILABLE_PROC")         or\
-               case("ITER")               or\
-               case("TIME_INSTANCES")         or\
-               case("UNST_ADJOINT_ITER")      or\
-               case("ITER_AVERAGE_OBJ")       or\
-               case("INNER_ITER")             or\
-               case("OUTER_ITER")             or\
-               case("TIME_ITER")             or\
-               case("ADAPT_CYCLES")           :
+            if (
+                case("NUMBER_PART")
+                or case("AVAILABLE_PROC")
+                or case("ITER")
+                or case("TIME_INSTANCES")
+                or case("UNST_ADJOINT_ITER")
+                or case("ITER_AVERAGE_OBJ")
+                or case("INNER_ITER")
+                or case("OUTER_ITER")
+                or case("TIME_ITER")
+                or case("ADAPT_CYCLES")
+            ):
                 data_dict[this_param] = int(this_value)
                 break
 
@@ -482,154 +508,199 @@ def read_config(filename):
             # unitary design variable definition
             if case("DEFINITION_DV"):
                 # remove white space
-                this_value = ''.join(this_value.split())
+                this_value = "".join(this_value.split())
                 # split into unitary definitions
                 info_Unitary = this_value.split(";")
                 # process each Design Variable
-                dv_Kind       = []
-                dv_Scale      = []
-                dv_Markers    = []
-                dv_FFDTag     = []
+                dv_Kind = []
+                dv_Scale = []
+                dv_Markers = []
+                dv_FFDTag = []
                 dv_Parameters = []
-                dv_Size       = []
+                dv_Size = []
 
                 for this_General in info_Unitary:
-                    if not this_General: continue
+                    if not this_General:
+                        continue
                     # split each unitary definition into one general definition
-                    info_General = this_General.strip("()").split("|") # check for needed strip()?
+                    info_General = this_General.strip("()").split(
+                        "|"
+                    )  # check for needed strip()?
                     # split information for dv Kinds
-                    info_Kind    = info_General[0].split(",")
+                    info_Kind = info_General[0].split(",")
                     # pull processed dv values
-                    this_dvKind       = get_dvKind( int( info_Kind[0] ) )
-                    this_dvScale      = float( info_Kind[1] )
-                    this_dvMarkers    = info_General[1].split(",")
-                    this_dvSize       = 1
+                    this_dvKind = get_dvKind(int(info_Kind[0]))
+                    this_dvScale = float(info_Kind[1])
+                    this_dvMarkers = info_General[1].split(",")
+                    this_dvSize = 1
 
-                    if this_dvKind=='MACH_NUMBER' or this_dvKind=='AOA':
+                    if this_dvKind == "MACH_NUMBER" or this_dvKind == "AOA":
                         this_dvParameters = []
                     else:
                         this_dvParameters = info_General[2].split(",")
                         # if FFD change the first element to work with numbers and float(x), save also the tag
-                        if this_dvKind in ['FFD_SETTING','FFD_ANGLE_OF_ATTACK','FFD_CONTROL_POINT','FFD_NACELLE','FFD_GULL','FFD_TWIST','FFD_TWIST_2D','FFD_TWIST_ANGLE','FFD_ROTATION','FFD_CAMBER','FFD_THICKNESS','FFD_CONTROL_POINT_2D','FFD_CAMBER_2D','FFD_THICKNESS_2D']:
-                          this_dvFFDTag = this_dvParameters[0]
-                          this_dvParameters[0] = '0'
+                        if this_dvKind in [
+                            "FFD_SETTING",
+                            "FFD_ANGLE_OF_ATTACK",
+                            "FFD_CONTROL_POINT",
+                            "FFD_NACELLE",
+                            "FFD_GULL",
+                            "FFD_TWIST",
+                            "FFD_TWIST_2D",
+                            "FFD_TWIST_ANGLE",
+                            "FFD_ROTATION",
+                            "FFD_CAMBER",
+                            "FFD_THICKNESS",
+                            "FFD_CONTROL_POINT_2D",
+                            "FFD_CAMBER_2D",
+                            "FFD_THICKNESS_2D",
+                        ]:
+                            this_dvFFDTag = this_dvParameters[0]
+                            this_dvParameters[0] = "0"
                         else:
-                          this_dvFFDTag = []
+                            this_dvFFDTag = []
 
-                        this_dvParameters = [ float(x) for x in this_dvParameters ]
+                        this_dvParameters = [float(x) for x in this_dvParameters]
 
-                        if this_dvKind in ['FFD_CONTROL_POINT_2D']:
+                        if this_dvKind in ["FFD_CONTROL_POINT_2D"]:
                             if this_dvParameters[3] == 0 and this_dvParameters[4] == 0:
                                 this_dvSize = 2
 
-                        if this_dvKind in ['FFD_CONTROL_POINT']:
-                            if this_dvParameters[4] == 0 and this_dvParameters[5] == 0 and this_dvParameters[6] == 0:
+                        if this_dvKind in ["FFD_CONTROL_POINT"]:
+                            if (
+                                this_dvParameters[4] == 0
+                                and this_dvParameters[5] == 0
+                                and this_dvParameters[6] == 0
+                            ):
                                 this_dvSize = 3
 
                     # add to lists
-                    dv_Kind       = dv_Kind       + [this_dvKind]
-                    dv_Scale      = dv_Scale      + [this_dvScale]
-                    dv_Markers    = dv_Markers    + [this_dvMarkers]
-                    dv_FFDTag     = dv_FFDTag     + [this_dvFFDTag]
+                    dv_Kind = dv_Kind + [this_dvKind]
+                    dv_Scale = dv_Scale + [this_dvScale]
+                    dv_Markers = dv_Markers + [this_dvMarkers]
+                    dv_FFDTag = dv_FFDTag + [this_dvFFDTag]
                     dv_Parameters = dv_Parameters + [this_dvParameters]
-                    dv_Size       = dv_Size       + [this_dvSize]
+                    dv_Size = dv_Size + [this_dvSize]
                 # store in a dictionary
-                dv_Definitions = { 'KIND'   : dv_Kind       ,
-                                   'SCALE'  : dv_Scale      ,
-                                   'MARKER' : dv_Markers    ,
-                                   'FFDTAG' : dv_FFDTag     ,
-                                   'PARAM'  : dv_Parameters ,
-                                   'SIZE'   : dv_Size}
+                dv_Definitions = {
+                    "KIND": dv_Kind,
+                    "SCALE": dv_Scale,
+                    "MARKER": dv_Markers,
+                    "FFDTAG": dv_FFDTag,
+                    "PARAM": dv_Parameters,
+                    "SIZE": dv_Size,
+                }
 
                 # save to output dictionary
                 data_dict[this_param] = dv_Definitions
                 break
 
             # unitary objective definition
-            if case('OPT_OBJECTIVE'):
+            if case("OPT_OBJECTIVE"):
                 # remove white space
-                this_value = ''.join(this_value.split())
-                #split by ;
-                this_def=OrderedDict()
+                this_value = "".join(this_value.split())
+                # split by ;
+                this_def = OrderedDict()
                 this_value = this_value.split(";")
 
-                for  this_obj in this_value:
+                for this_obj in this_value:
                     # split by scale
                     this_obj = this_obj.split("*")
-                    this_name  = this_obj[0]
+                    this_name = this_obj[0]
                     this_scale = 1.0
                     if len(this_obj) > 1:
-                        this_scale = float( this_obj[1] )
+                        this_scale = float(this_obj[1])
                     # check for penalty-based constraint function
-                    for this_sgn in ['<','>','=']:
-                        if this_sgn in this_name: break
-                    this_obj = this_name.strip('()').split(this_sgn)
-                    if len(this_obj)>1:
+                    for this_sgn in ["<", ">", "="]:
+                        if this_sgn in this_name:
+                            break
+                    this_obj = this_name.strip("()").split(this_sgn)
+                    if len(this_obj) > 1:
                         this_type = this_sgn
                         this_val = this_obj[1]
                     else:
-                        this_type = 'DEFAULT'
-                        this_val  = 0.0
+                        this_type = "DEFAULT"
+                        this_val = 0.0
                     this_name = this_obj[0]
                     # Print an error and exit if the same key appears twice
-                    if (this_name in this_def):
-                      raise SystemExit('Multiple occurrences of the same objective in the OPT_OBJECTIVE definition are not currently supported. To evaluate one objective over multiple surfaces, list the objective once.')
+                    if this_name in this_def:
+                        raise SystemExit(
+                            "Multiple occurrences of the same objective in the OPT_OBJECTIVE definition are not currently supported. To evaluate one objective over multiple surfaces, list the objective once."
+                        )
                     # Set up dict for objective, including scale, whether it is a penalty, and constraint value
-                    this_def.update({ this_name : {'SCALE':this_scale, 'OBJTYPE':this_type, 'VALUE':this_val} })
+                    this_def.update(
+                        {
+                            this_name: {
+                                "SCALE": this_scale,
+                                "OBJTYPE": this_type,
+                                "VALUE": this_val,
+                            }
+                        }
+                    )
                     # OPT_OBJECTIVE has to appear after MARKER_MONITORING in the .cfg, maybe catch that here
-                    if (len(data_dict['MARKER_MONITORING'])>1):
-                        this_def[this_name]['MARKER'] = data_dict['MARKER_MONITORING'][len(this_def)-1]
+                    if len(data_dict["MARKER_MONITORING"]) > 1:
+                        this_def[this_name]["MARKER"] = data_dict["MARKER_MONITORING"][
+                            len(this_def) - 1
+                        ]
                     else:
-                        this_def[this_name]['MARKER'] = data_dict['MARKER_MONITORING'][0]
+                        this_def[this_name]["MARKER"] = data_dict["MARKER_MONITORING"][
+                            0
+                        ]
 
                 # save to output dictionary
                 data_dict[this_param] = this_def
                 break
 
             # unitary constraint definition
-            if case('OPT_CONSTRAINT'):
+            if case("OPT_CONSTRAINT"):
                 # remove white space
-                this_value = ''.join(this_value.split())
+                this_value = "".join(this_value.split())
                 # check for none case
-                if this_value == 'NONE':
-                    data_dict[this_param] = {'EQUALITY':OrderedDict(), 'INEQUALITY':OrderedDict()}
+                if this_value == "NONE":
+                    data_dict[this_param] = {
+                        "EQUALITY": OrderedDict(),
+                        "INEQUALITY": OrderedDict(),
+                    }
                     break
                 # split definitions
-                this_value = this_value.split(';')
+                this_value = this_value.split(";")
                 this_def = OrderedDict()
                 for this_con in this_value:
-                    if not this_con: continue # if no definition
+                    if not this_con:
+                        continue  # if no definition
                     # defaults
-                    this_obj = 'NONE'
-                    this_sgn = '='
+                    this_obj = "NONE"
+                    this_sgn = "="
                     this_scl = 1.0
                     this_val = 0.0
                     # split scale if present
-                    this_con = this_con.split('*')
+                    this_con = this_con.split("*")
                     if len(this_con) > 1:
-                        this_scl = float( this_con[1] )
+                        this_scl = float(this_con[1])
                     this_con = this_con[0]
                     # find sign
-                    for this_sgn in ['<','>','=']:
-                        if this_sgn in this_con: break
+                    for this_sgn in ["<", ">", "="]:
+                        if this_sgn in this_con:
+                            break
                     # split sign, store objective and value
-                    this_con = this_con.strip('()').split(this_sgn)
-                    assert len(this_con) == 2 , 'incorrect constraint definition'
+                    this_con = this_con.strip("()").split(this_sgn)
+                    assert len(this_con) == 2, "incorrect constraint definition"
                     this_obj = this_con[0]
-                    this_val = float( this_con[1] )
+                    this_val = float(this_con[1])
                     # store in dictionary
-                    this_def[this_obj] = { 'SIGN'  : this_sgn ,
-                                           'VALUE' : this_val ,
-                                           'SCALE' : this_scl  }
+                    this_def[this_obj] = {
+                        "SIGN": this_sgn,
+                        "VALUE": this_val,
+                        "SCALE": this_scl,
+                    }
                 #: for each constraint definition
                 # sort constraints by type
-                this_sort = { 'EQUALITY'   : OrderedDict() ,
-                              'INEQUALITY' : OrderedDict()  }
-                for key,value in this_def.items():
-                    if value['SIGN'] == '=':
-                        this_sort['EQUALITY'][key]   = value
+                this_sort = {"EQUALITY": OrderedDict(), "INEQUALITY": OrderedDict()}
+                for key, value in this_def.items():
+                    if value["SIGN"] == "=":
+                        this_sort["EQUALITY"][key] = value
                     else:
-                        this_sort['INEQUALITY'][key] = value
+                        this_sort["INEQUALITY"][key] = value
                 #: for each definition
                 # save to output dictionary
                 data_dict[this_param] = this_sort
@@ -647,198 +718,223 @@ def read_config(filename):
 
     #: for line
 
-    if 'OPT_CONSTRAINT' in data_dict:
-        if 'BUFFET' in data_dict['OPT_CONSTRAINT']['EQUALITY'] or 'BUFFET' in data_dict['OPT_CONSTRAINT']['INEQUALITY']:
-            data_dict['BUFFET_MONITORING'] = "YES"
-
-    if 'OPT_OBJECTIVE' in data_dict:
-        if 'BUFFET' in data_dict['OPT_OBJECTIVE']:
-            data_dict['BUFFET_MONITORING'] = "YES"
-
-    #hack - twl
-    if 'DV_VALUE_NEW' not in data_dict:
-        data_dict['DV_VALUE_NEW'] = [0]
-    if 'DV_VALUE_OLD' not in data_dict:
-        data_dict['DV_VALUE_OLD'] = [0]
-    if 'OPT_ITERATIONS' not in data_dict:
-        data_dict['OPT_ITERATIONS'] = 100
-    if 'OPT_ACCURACY' not in data_dict:
-        data_dict['OPT_ACCURACY'] = 1e-10
-    if 'OPT_RELAX_FACTOR' not in data_dict:
-        data_dict['OPT_RELAX_FACTOR'] = 1.0
-    if 'OPT_GRADIENT_FACTOR' not in data_dict:
-        data_dict['OPT_GRADIENT_FACTOR'] = 1.0
-    if 'OPT_BOUND_UPPER' not in data_dict:
-        data_dict['OPT_BOUND_UPPER'] = 1e10
-    if 'OPT_BOUND_LOWER' not in data_dict:
-        data_dict['OPT_BOUND_LOWER'] = -1e10
-    if 'OPT_COMBINE_OBJECTIVE' not in data_dict:
-        data_dict['OPT_COMBINE_OBJECTIVE'] = "NO"
-    if 'OPT_CONSTRAINT' not in data_dict:
-        data_dict['OPT_CONSTRAINT'] =  {'INEQUALITY': OrderedDict(), 'EQUALITY': OrderedDict()}
-    if 'VALUE_OBJFUNC_FILENAME' not in data_dict:
-        data_dict['VALUE_OBJFUNC_FILENAME'] = 'of_eval.dat'
-    if 'GRAD_OBJFUNC_FILENAME' not in data_dict:
-        data_dict['GRAD_OBJFUNC_FILENAME'] = 'of_grad.dat'
-    if 'AOA' not in data_dict:
-        data_dict['AOA'] = 0.0
-    if 'SIDESLIP_ANGLE' not in data_dict:
-        data_dict['SIDESLIP_ANGLE'] = 0.0
-    if 'MACH_NUMBER' not in data_dict:
-        data_dict['MACH_NUMBER'] = 0.0
-    if 'REYNOLDS_NUMBER' not in data_dict:
-        data_dict['REYNOLDS_NUMBER'] = 0.0
-    if 'TARGET_CL' not in data_dict:
-        data_dict['TARGET_CL'] = 0.0
-    if 'FREESTREAM_PRESSURE' not in data_dict:
-        data_dict['FREESTREAM_PRESSURE'] = 101325.0
-    if 'FREESTREAM_TEMPERATURE' not in data_dict:
-        data_dict['FREESTREAM_TEMPERATURE'] = 288.15
-    if 'MARKER_OUTLET' not in data_dict:
-        data_dict['MARKER_OUTLET'] = '(NONE)'
+    if "OPT_CONSTRAINT" in data_dict:
+        if (
+            "BUFFET" in data_dict["OPT_CONSTRAINT"]["EQUALITY"]
+            or "BUFFET" in data_dict["OPT_CONSTRAINT"]["INEQUALITY"]
+        ):
+            data_dict["BUFFET_MONITORING"] = "YES"
+
+    if "OPT_OBJECTIVE" in data_dict:
+        if "BUFFET" in data_dict["OPT_OBJECTIVE"]:
+            data_dict["BUFFET_MONITORING"] = "YES"
+
+    # hack - twl
+    if "DV_VALUE_NEW" not in data_dict:
+        data_dict["DV_VALUE_NEW"] = [0]
+    if "DV_VALUE_OLD" not in data_dict:
+        data_dict["DV_VALUE_OLD"] = [0]
+    if "OPT_ITERATIONS" not in data_dict:
+        data_dict["OPT_ITERATIONS"] = 100
+    if "OPT_ACCURACY" not in data_dict:
+        data_dict["OPT_ACCURACY"] = 1e-10
+    if "OPT_RELAX_FACTOR" not in data_dict:
+        data_dict["OPT_RELAX_FACTOR"] = 1.0
+    if "OPT_GRADIENT_FACTOR" not in data_dict:
+        data_dict["OPT_GRADIENT_FACTOR"] = 1.0
+    if "OPT_BOUND_UPPER" not in data_dict:
+        data_dict["OPT_BOUND_UPPER"] = 1e10
+    if "OPT_BOUND_LOWER" not in data_dict:
+        data_dict["OPT_BOUND_LOWER"] = -1e10
+    if "OPT_COMBINE_OBJECTIVE" not in data_dict:
+        data_dict["OPT_COMBINE_OBJECTIVE"] = "NO"
+    if "OPT_CONSTRAINT" not in data_dict:
+        data_dict["OPT_CONSTRAINT"] = {
+            "INEQUALITY": OrderedDict(),
+            "EQUALITY": OrderedDict(),
+        }
+    if "VALUE_OBJFUNC_FILENAME" not in data_dict:
+        data_dict["VALUE_OBJFUNC_FILENAME"] = "of_eval.dat"
+    if "GRAD_OBJFUNC_FILENAME" not in data_dict:
+        data_dict["GRAD_OBJFUNC_FILENAME"] = "of_grad.dat"
+    if "AOA" not in data_dict:
+        data_dict["AOA"] = 0.0
+    if "SIDESLIP_ANGLE" not in data_dict:
+        data_dict["SIDESLIP_ANGLE"] = 0.0
+    if "MACH_NUMBER" not in data_dict:
+        data_dict["MACH_NUMBER"] = 0.0
+    if "REYNOLDS_NUMBER" not in data_dict:
+        data_dict["REYNOLDS_NUMBER"] = 0.0
+    if "TARGET_CL" not in data_dict:
+        data_dict["TARGET_CL"] = 0.0
+    if "FREESTREAM_PRESSURE" not in data_dict:
+        data_dict["FREESTREAM_PRESSURE"] = 101325.0
+    if "FREESTREAM_TEMPERATURE" not in data_dict:
+        data_dict["FREESTREAM_TEMPERATURE"] = 288.15
+    if "MARKER_OUTLET" not in data_dict:
+        data_dict["MARKER_OUTLET"] = "(NONE)"
 
     #
     # Multipoints requires some particular default values
     #
     multipoints = 1
-    if 'MULTIPOINT_WEIGHT' not in data_dict:
-      data_dict['MULTIPOINT_WEIGHT'] = "(1.0)"
-      multipoints = 1
+    if "MULTIPOINT_WEIGHT" not in data_dict:
+        data_dict["MULTIPOINT_WEIGHT"] = "(1.0)"
+        multipoints = 1
     else:
-      multipoints = len(data_dict['MULTIPOINT_WEIGHT'].replace("(", "").replace(")", "").split(','))
-
-    if 'MULTIPOINT_MACH_NUMBER' not in data_dict:
-      Mach_Value = data_dict['MACH_NUMBER']
-      Mach_List = "("
-      for i in range(multipoints):
-        if i != 0: Mach_List +=  ", "
-        Mach_List +=  str(Mach_Value)
-      Mach_List += ")"
-      data_dict['MULTIPOINT_MACH_NUMBER'] = Mach_List
-
-    if 'MULTIPOINT_AOA' not in data_dict:
-      Alpha_Value = data_dict['AOA']
-      Alpha_List = "("
-      for i in range(multipoints):
-        if i != 0: Alpha_List +=  ", "
-        Alpha_List +=  str(Alpha_Value)
-      Alpha_List += ")"
-      data_dict['MULTIPOINT_AOA'] = Alpha_List
-
-    if 'MULTIPOINT_SIDESLIP_ANGLE' not in data_dict:
-      Beta_Value = data_dict['SIDESLIP_ANGLE']
-      Beta_List = "("
-      for i in range(multipoints):
-        if i != 0: Beta_List +=  ", "
-        Beta_List +=  str(Beta_Value)
-      Beta_List += ")"
-      data_dict['MULTIPOINT_SIDESLIP_ANGLE'] = Beta_List
-
-    if 'MULTIPOINT_REYNOLDS_NUMBER' not in data_dict:
-      Reynolds_Value = data_dict['REYNOLDS_NUMBER']
-      Reynolds_List = "("
-      for i in range(multipoints):
-        if i != 0: Reynolds_List +=  ", "
-        Reynolds_List +=  str(Reynolds_Value)
-      Reynolds_List += ")"
-      data_dict['MULTIPOINT_REYNOLDS_NUMBER'] = Reynolds_List
-
-    if 'MULTIPOINT_TARGET_CL' not in data_dict:
-      TargetCLValue = data_dict['TARGET_CL']
-      TargetCL_List = "("
-      for i in range(multipoints):
-        if i != 0: TargetCL_List +=  ", "
-        TargetCL_List +=  str(TargetCLValue)
-      TargetCL_List += ")"
-      data_dict['MULTIPOINT_TARGET_CL'] = TargetCL_List
-
-    if 'MULTIPOINT_FREESTREAM_PRESSURE' not in data_dict:
-      Pressure_Value = data_dict['FREESTREAM_PRESSURE']
-      Pressure_List = "("
-      for i in range(multipoints):
-        if i != 0: Pressure_List +=  ", "
-        Pressure_List +=  str(Pressure_Value)
-      Pressure_List += ")"
-      data_dict['MULTIPOINT_FREESTREAM_PRESSURE'] = Pressure_List
-
-    if 'MULTIPOINT_FREESTREAM_TEMPERATURE' not in data_dict:
-      Temperature_Value = data_dict['FREESTREAM_TEMPERATURE']
-      Temperature_List = "("
-      for i in range(multipoints):
-        if i != 0: Temperature_List +=  ", "
-        Temperature_List +=  str(Temperature_Value)
-      Temperature_List += ")"
-      data_dict['MULTIPOINT_FREESTREAM_TEMPERATURE'] = Temperature_List
-
-    if 'MULTIPOINT_OUTLET_VALUE' not in data_dict:
-      if 'NONE' in data_dict['MARKER_OUTLET']:
-        Outlet_Value = 0.0
-      else:
-        Outlet_Value = data_dict['MARKER_OUTLET'].replace("(", "").replace(")", "").split(',')[1]
-      Outlet_Value_List = "("
-      for i in range(multipoints):
-        if i != 0: Outlet_Value_List +=  ", "
-        Outlet_Value_List +=  str(Outlet_Value)
-      Outlet_Value_List += ")"
-      data_dict['MULTIPOINT_OUTLET_VALUE'] = Outlet_Value_List
-
-    if 'MULTIPOINT_MESH_FILENAME' not in data_dict:
-      Mesh_Filename = data_dict['MESH_FILENAME']
-      Mesh_List = "("
-      for i in range(multipoints):
-        if i != 0: Mesh_List +=  ", "
-        Mesh_List +=  str(Mesh_Filename)
-      Mesh_List += ")"
-      data_dict['MULTIPOINT_MESH_FILENAME'] = Mesh_List
-
-    if 'HISTORY_OUTPUT' not in data_dict:
-        data_dict['HISTORY_OUTPUT'] = ['ITER', 'RMS_RES']
+        multipoints = len(
+            data_dict["MULTIPOINT_WEIGHT"].replace("(", "").replace(")", "").split(",")
+        )
+
+    if "MULTIPOINT_MACH_NUMBER" not in data_dict:
+        Mach_Value = data_dict["MACH_NUMBER"]
+        Mach_List = "("
+        for i in range(multipoints):
+            if i != 0:
+                Mach_List += ", "
+            Mach_List += str(Mach_Value)
+        Mach_List += ")"
+        data_dict["MULTIPOINT_MACH_NUMBER"] = Mach_List
+
+    if "MULTIPOINT_AOA" not in data_dict:
+        Alpha_Value = data_dict["AOA"]
+        Alpha_List = "("
+        for i in range(multipoints):
+            if i != 0:
+                Alpha_List += ", "
+            Alpha_List += str(Alpha_Value)
+        Alpha_List += ")"
+        data_dict["MULTIPOINT_AOA"] = Alpha_List
+
+    if "MULTIPOINT_SIDESLIP_ANGLE" not in data_dict:
+        Beta_Value = data_dict["SIDESLIP_ANGLE"]
+        Beta_List = "("
+        for i in range(multipoints):
+            if i != 0:
+                Beta_List += ", "
+            Beta_List += str(Beta_Value)
+        Beta_List += ")"
+        data_dict["MULTIPOINT_SIDESLIP_ANGLE"] = Beta_List
+
+    if "MULTIPOINT_REYNOLDS_NUMBER" not in data_dict:
+        Reynolds_Value = data_dict["REYNOLDS_NUMBER"]
+        Reynolds_List = "("
+        for i in range(multipoints):
+            if i != 0:
+                Reynolds_List += ", "
+            Reynolds_List += str(Reynolds_Value)
+        Reynolds_List += ")"
+        data_dict["MULTIPOINT_REYNOLDS_NUMBER"] = Reynolds_List
+
+    if "MULTIPOINT_TARGET_CL" not in data_dict:
+        TargetCLValue = data_dict["TARGET_CL"]
+        TargetCL_List = "("
+        for i in range(multipoints):
+            if i != 0:
+                TargetCL_List += ", "
+            TargetCL_List += str(TargetCLValue)
+        TargetCL_List += ")"
+        data_dict["MULTIPOINT_TARGET_CL"] = TargetCL_List
+
+    if "MULTIPOINT_FREESTREAM_PRESSURE" not in data_dict:
+        Pressure_Value = data_dict["FREESTREAM_PRESSURE"]
+        Pressure_List = "("
+        for i in range(multipoints):
+            if i != 0:
+                Pressure_List += ", "
+            Pressure_List += str(Pressure_Value)
+        Pressure_List += ")"
+        data_dict["MULTIPOINT_FREESTREAM_PRESSURE"] = Pressure_List
+
+    if "MULTIPOINT_FREESTREAM_TEMPERATURE" not in data_dict:
+        Temperature_Value = data_dict["FREESTREAM_TEMPERATURE"]
+        Temperature_List = "("
+        for i in range(multipoints):
+            if i != 0:
+                Temperature_List += ", "
+            Temperature_List += str(Temperature_Value)
+        Temperature_List += ")"
+        data_dict["MULTIPOINT_FREESTREAM_TEMPERATURE"] = Temperature_List
+
+    if "MULTIPOINT_OUTLET_VALUE" not in data_dict:
+        if "NONE" in data_dict["MARKER_OUTLET"]:
+            Outlet_Value = 0.0
+        else:
+            Outlet_Value = (
+                data_dict["MARKER_OUTLET"]
+                .replace("(", "")
+                .replace(")", "")
+                .split(",")[1]
+            )
+        Outlet_Value_List = "("
+        for i in range(multipoints):
+            if i != 0:
+                Outlet_Value_List += ", "
+            Outlet_Value_List += str(Outlet_Value)
+        Outlet_Value_List += ")"
+        data_dict["MULTIPOINT_OUTLET_VALUE"] = Outlet_Value_List
+
+    if "MULTIPOINT_MESH_FILENAME" not in data_dict:
+        Mesh_Filename = data_dict["MESH_FILENAME"]
+        Mesh_List = "("
+        for i in range(multipoints):
+            if i != 0:
+                Mesh_List += ", "
+            Mesh_List += str(Mesh_Filename)
+        Mesh_List += ")"
+        data_dict["MULTIPOINT_MESH_FILENAME"] = Mesh_List
+
+    if "HISTORY_OUTPUT" not in data_dict:
+        data_dict["HISTORY_OUTPUT"] = ["ITER", "RMS_RES"]
 
     #
     # Default values for optimization parameters (needed for some eval functions
     # that can be called outside of an opt. context.
     #
-    if 'OBJECTIVE_FUNCTION' not in data_dict:
-        data_dict['OBJECTIVE_FUNCTION']='DRAG'
-    if 'DV_KIND' not in data_dict:
-        data_dict['DV_KIND']=['FFD_SETTING']
-    if 'DV_PARAM' not in data_dict:
-        data_dict['DV_PARAM']={'FFDTAG': ['1'], 'PARAM': [[0.0, 0.5]], 'SIZE': [1]}
-    if 'DEFINITION_DV' not in data_dict:
-        data_dict['DEFINITION_DV']={'FFDTAG': [[]],
-            'KIND': ['HICKS_HENNE'],
-            'MARKER': [['WING']],
-            'PARAM': [[0.0, 0.05]],
-            'SCALE': [1.0],
-            'SIZE': [1]}
-    if 'VALUE_OBJFUNC_FILENAME' not in data_dict:
-        data_dict['VALUE_OBJFUNC_FILENAME'] = 'of_eval.dat'
-    if 'GRAD_OBJFUNC_FILENAME' not in data_dict:
-        data_dict['GRAD_OBJFUNC_FILENAME'] = 'of_grad.dat'
+    if "OBJECTIVE_FUNCTION" not in data_dict:
+        data_dict["OBJECTIVE_FUNCTION"] = "DRAG"
+    if "DV_KIND" not in data_dict:
+        data_dict["DV_KIND"] = ["FFD_SETTING"]
+    if "DV_PARAM" not in data_dict:
+        data_dict["DV_PARAM"] = {"FFDTAG": ["1"], "PARAM": [[0.0, 0.5]], "SIZE": [1]}
+    if "DEFINITION_DV" not in data_dict:
+        data_dict["DEFINITION_DV"] = {
+            "FFDTAG": [[]],
+            "KIND": ["HICKS_HENNE"],
+            "MARKER": [["WING"]],
+            "PARAM": [[0.0, 0.05]],
+            "SCALE": [1.0],
+            "SIZE": [1],
+        }
+    if "VALUE_OBJFUNC_FILENAME" not in data_dict:
+        data_dict["VALUE_OBJFUNC_FILENAME"] = "of_eval.dat"
+    if "GRAD_OBJFUNC_FILENAME" not in data_dict:
+        data_dict["GRAD_OBJFUNC_FILENAME"] = "of_grad.dat"
 
     return data_dict
 
-#: def read_config()
 
+#: def read_config()
 
 
 # -------------------------------------------------------------------
 #  Set SU2 Configuration Parameters
 # -------------------------------------------------------------------
 
-def write_config(filename,param_dict):
-    """ updates an existing config file """
 
-    temp_filename = filename+"_tmp"
-    shutil.copy(filename,temp_filename)
-    output_file = open(filename,"w")
+def write_config(filename, param_dict):
+    """updates an existing config file"""
+
+    temp_filename = filename + "_tmp"
+    shutil.copy(filename, temp_filename)
+    output_file = open(filename, "w")
 
     # break pointers
     param_dict = copy.deepcopy(param_dict)
 
     for raw_line in open(temp_filename):
         # remove line returns
-        line = raw_line.strip('\r\n')
+        line = raw_line.strip("\r\n")
 
         # make sure it has useful data
         if not "=" in line:
@@ -848,7 +944,7 @@ def write_config(filename,param_dict):
         # split across equals sign
         line = line.split("=")
         this_param = line[0].strip()
-        old_value  = line[1].strip()
+        old_value = line[1].strip()
 
         # skip if parameter unwanted
         if this_param not in param_dict:
@@ -863,43 +959,52 @@ def write_config(filename,param_dict):
         for case in switch(this_param):
 
             # comma delimited list of floats
-            if case("DV_VALUE_NEW") : pass
-            if case("DV_VALUE_OLD") : pass
-            if case("DV_VALUE")     :
+            if case("DV_VALUE_NEW"):
+                pass
+            if case("DV_VALUE_OLD"):
+                pass
+            if case("DV_VALUE"):
                 n_lists = len(new_value)
                 for i_value in range(n_lists):
                     output_file.write("%s" % new_value[i_value])
-                    if i_value+1 < n_lists:
+                    if i_value + 1 < n_lists:
                         output_file.write(", ")
                 break
 
             # comma delimited list of strings no paren's
-            if case("DV_KIND")            : pass
-            if case("TASKS")              : pass
-            if case("GRADIENTS")          :
-                if not isinstance(new_value,list):
-                    new_value = [ new_value ]
+            if case("DV_KIND"):
+                pass
+            if case("TASKS"):
+                pass
+            if case("GRADIENTS"):
+                if not isinstance(new_value, list):
+                    new_value = [new_value]
                 n_lists = len(new_value)
                 for i_value in range(n_lists):
                     output_file.write(new_value[i_value])
-                    if i_value+1 < n_lists:
+                    if i_value + 1 < n_lists:
                         output_file.write(", ")
                 break
 
             # comma delimited list of strings inside paren's
-            if case("MARKER_EULER")      : pass
-            if case("MARKER_FAR")        : pass
-            if case("MARKER_PLOTTING")   : pass
-            if case("MARKER_MONITORING") : pass
-            if case("MARKER_SYM")        : pass
-            if case("DV_MARKER") :
-                if not isinstance(new_value,list):
-                    new_value = [ new_value ]
+            if case("MARKER_EULER"):
+                pass
+            if case("MARKER_FAR"):
+                pass
+            if case("MARKER_PLOTTING"):
+                pass
+            if case("MARKER_MONITORING"):
+                pass
+            if case("MARKER_SYM"):
+                pass
+            if case("DV_MARKER"):
+                if not isinstance(new_value, list):
+                    new_value = [new_value]
                 output_file.write("( ")
                 n_lists = len(new_value)
                 for i_value in range(n_lists):
                     output_file.write(new_value[i_value])
-                    if i_value+1 < n_lists:
+                    if i_value + 1 < n_lists:
                         output_file.write(", ")
                 output_file.write(" )")
                 break
@@ -908,7 +1013,7 @@ def write_config(filename,param_dict):
                 output_file.write("(")
                 for i_value in range(n_lists):
                     output_file.write(new_value[i_value])
-                    if i_value+1 < n_lists:
+                    if i_value + 1 < n_lists:
                         output_file.write(", ")
                 output_file.write(")")
                 break
@@ -918,7 +1023,7 @@ def write_config(filename,param_dict):
                 output_file.write("(")
                 for i_value in range(n_lists):
                     output_file.write(new_value[i_value])
-                    if i_value+1 < n_lists:
+                    if i_value + 1 < n_lists:
                         output_file.write(", ")
                 output_file.write(")")
                 break
@@ -927,123 +1032,159 @@ def write_config(filename,param_dict):
                 n_lists = len(new_value)
                 for i_value in range(n_lists):
                     output_file.write(new_value[i_value])
-                    if i_value+1 < n_lists:
+                    if i_value + 1 < n_lists:
                         output_file.write(", ")
                 break
 
             # semicolon delimited lists of comma delimited lists
-            if case("DV_PARAM") :
+            if case("DV_PARAM"):
 
-                assert isinstance(new_value['PARAM'],list) , 'incorrect specification of DV_PARAM'
-                if not isinstance(new_value['PARAM'][0],list): new_value = [ new_value ]
+                assert isinstance(
+                    new_value["PARAM"], list
+                ), "incorrect specification of DV_PARAM"
+                if not isinstance(new_value["PARAM"][0], list):
+                    new_value = [new_value]
 
-                for i_value in range(len(new_value['PARAM'])):
+                for i_value in range(len(new_value["PARAM"])):
 
                     output_file.write("( ")
-                    this_param_list = new_value['PARAM'][i_value]
-                    this_ffd_list = new_value['FFDTAG'][i_value]
+                    this_param_list = new_value["PARAM"][i_value]
+                    this_ffd_list = new_value["FFDTAG"][i_value]
                     n_lists = len(this_param_list)
 
                     if this_ffd_list != []:
-                      output_file.write("%s, " % this_ffd_list)
-                      for j_value in range(1,n_lists):
-                        output_file.write("%s" % this_param_list[j_value])
-                        if j_value+1 < n_lists:
-                          output_file.write(", ")
+                        output_file.write("%s, " % this_ffd_list)
+                        for j_value in range(1, n_lists):
+                            output_file.write("%s" % this_param_list[j_value])
+                            if j_value + 1 < n_lists:
+                                output_file.write(", ")
                     else:
-                      for j_value in range(n_lists):
-                        output_file.write("%s" % this_param_list[j_value])
-                        if j_value+1 < n_lists:
-                          output_file.write(", ")
+                        for j_value in range(n_lists):
+                            output_file.write("%s" % this_param_list[j_value])
+                            if j_value + 1 < n_lists:
+                                output_file.write(", ")
 
                     output_file.write(") ")
-                    if i_value+1 < len(new_value['PARAM']):
+                    if i_value + 1 < len(new_value["PARAM"]):
                         output_file.write("; ")
                 break
 
             # int parameters
-            if case("NUMBER_PART")            : pass
-            if case("ADAPT_CYCLES")           : pass
-            if case("TIME_INSTANCES")         : pass
-            if case("AVAILABLE_PROC")         : pass
-            if case("UNST_ADJOINT_ITER")      : pass
-            if case("ITER")              or\
-               case("TIME_ITER")         or\
-               case("INNER_ITER")        or\
-               case("OUTER_ITER"):
+            if case("NUMBER_PART"):
+                pass
+            if case("ADAPT_CYCLES"):
+                pass
+            if case("TIME_INSTANCES"):
+                pass
+            if case("AVAILABLE_PROC"):
+                pass
+            if case("UNST_ADJOINT_ITER"):
+                pass
+            if (
+                case("ITER")
+                or case("TIME_ITER")
+                or case("INNER_ITER")
+                or case("OUTER_ITER")
+            ):
                 output_file.write("%i" % new_value)
                 break
 
-            if case("DEFINITION_DV") :
-                n_dv = len(new_value['KIND'])
+            if case("DEFINITION_DV"):
+                n_dv = len(new_value["KIND"])
                 if not n_dv:
                     output_file.write("NONE")
                 for i_dv in range(n_dv):
-                    this_kind = new_value['KIND'][i_dv]
+                    this_kind = new_value["KIND"][i_dv]
                     output_file.write("( ")
-                    output_file.write("%i , " % get_dvID(this_kind) )
-                    output_file.write("%s " % new_value['SCALE'][i_dv])
+                    output_file.write("%i , " % get_dvID(this_kind))
+                    output_file.write("%s " % new_value["SCALE"][i_dv])
                     output_file.write("| ")
                     # markers
-                    n_mark = len(new_value['MARKER'][i_dv])
+                    n_mark = len(new_value["MARKER"][i_dv])
                     for i_mark in range(n_mark):
-                        output_file.write("%s " % new_value['MARKER'][i_dv][i_mark])
-                        if i_mark+1 < n_mark:
+                        output_file.write("%s " % new_value["MARKER"][i_dv][i_mark])
+                        if i_mark + 1 < n_mark:
                             output_file.write(", ")
                     #: for each marker
-                    if not this_kind in ['AOA','MACH_NUMBER']:
+                    if not this_kind in ["AOA", "MACH_NUMBER"]:
                         output_file.write(" | ")
                         # params
-                        if this_kind in ['FFD_SETTING','FFD_ANGLE_OF_ATTACK','FFD_CONTROL_POINT','FFD_NACELLE','FFD_GULL','FFD_TWIST_ANGLE','FFD_TWIST','FFD_TWIST_2D','FFD_ROTATION','FFD_CAMBER','FFD_THICKNESS','FFD_CONTROL_POINT_2D','FFD_CAMBER_2D','FFD_THICKNESS_2D']:
-                            n_param = len(new_value['PARAM'][i_dv])
-                            output_file.write("%s , " % new_value['FFDTAG'][i_dv])
-                            for i_param in range(1,n_param):
-                                output_file.write("%s " % new_value['PARAM'][i_dv][i_param])
-                                if i_param+1 < n_param:
+                        if this_kind in [
+                            "FFD_SETTING",
+                            "FFD_ANGLE_OF_ATTACK",
+                            "FFD_CONTROL_POINT",
+                            "FFD_NACELLE",
+                            "FFD_GULL",
+                            "FFD_TWIST_ANGLE",
+                            "FFD_TWIST",
+                            "FFD_TWIST_2D",
+                            "FFD_ROTATION",
+                            "FFD_CAMBER",
+                            "FFD_THICKNESS",
+                            "FFD_CONTROL_POINT_2D",
+                            "FFD_CAMBER_2D",
+                            "FFD_THICKNESS_2D",
+                        ]:
+                            n_param = len(new_value["PARAM"][i_dv])
+                            output_file.write("%s , " % new_value["FFDTAG"][i_dv])
+                            for i_param in range(1, n_param):
+                                output_file.write(
+                                    "%s " % new_value["PARAM"][i_dv][i_param]
+                                )
+                                if i_param + 1 < n_param:
                                     output_file.write(", ")
                         else:
-                            n_param = len(new_value['PARAM'][i_dv])
+                            n_param = len(new_value["PARAM"][i_dv])
                             for i_param in range(n_param):
-                                output_file.write("%s " % new_value['PARAM'][i_dv][i_param])
-                                if i_param+1 < n_param:
+                                output_file.write(
+                                    "%s " % new_value["PARAM"][i_dv][i_param]
+                                )
+                                if i_param + 1 < n_param:
                                     output_file.write(", ")
 
                         #: for each param
                     output_file.write(" )")
-                    if i_dv+1 < n_dv:
+                    if i_dv + 1 < n_dv:
                         output_file.write("; ")
                 #: for each dv
                 break
 
             if case("OPT_OBJECTIVE"):
                 n_obj = 0
-                for name,value in new_value.items():
-                    if n_obj>0: output_file.write("; ")
-                    if value['OBJTYPE']=='DEFAULT':
-                        output_file.write( "%s * %s " % (name,value['SCALE']) )
+                for name, value in new_value.items():
+                    if n_obj > 0:
+                        output_file.write("; ")
+                    if value["OBJTYPE"] == "DEFAULT":
+                        output_file.write("%s * %s " % (name, value["SCALE"]))
                     else:
-                        output_file.write( "( %s %s %s ) * %s"
-                                           % (name, value['OBJTYPE'], value['VALUE'], value['SCALE']) )
+                        output_file.write(
+                            "( %s %s %s ) * %s"
+                            % (name, value["OBJTYPE"], value["VALUE"], value["SCALE"])
+                        )
                     n_obj += 1
                 break
 
             if case("OPT_CONSTRAINT"):
                 i_con = 0
-                for con_type in ['EQUALITY','INEQUALITY']:
+                for con_type in ["EQUALITY", "INEQUALITY"]:
                     this_con = new_value[con_type]
-                    for name,value in this_con.items():
-                        if i_con>0: output_file.write("; ")
-                        output_file.write( "( %s %s %s ) * %s"
-                                          % (name, value['SIGN'], value['VALUE'], value['SCALE']) )
+                    for name, value in this_con.items():
+                        if i_con > 0:
+                            output_file.write("; ")
+                        output_file.write(
+                            "( %s %s %s ) * %s"
+                            % (name, value["SIGN"], value["VALUE"], value["SCALE"])
+                        )
                         i_con += 1
                     #: for each constraint
                 #: for each constraint type
-                if not i_con: output_file.write("NONE")
+                if not i_con:
+                    output_file.write("NONE")
                 break
 
             # default, assume string, integer or unformatted float
             if case():
-                output_file.write('%s' % new_value)
+                output_file.write("%s" % new_value)
                 break
 
         #: for case
@@ -1058,29 +1199,32 @@ def write_config(filename,param_dict):
 
     # check that all params were used
     for this_param in param_dict.keys():
-        if not this_param in ['JOB_NUMBER']:
-            print('Warning: Parameter %s not found in config file and was not written' % (this_param))
+        if not this_param in ["JOB_NUMBER"]:
+            print(
+                "Warning: Parameter %s not found in config file and was not written"
+                % (this_param)
+            )
 
     output_file.close()
     os.remove(temp_filename)
 
+
 #: def write_config()
 
 
-def dump_config(filename,config):
-    ''' dumps a raw config file with all options in config
-        and no comments
-    '''
+def dump_config(filename, config):
+    """dumps a raw config file with all options in config
+    and no comments
+    """
 
     # HACK - twl
-    if 'DV_VALUE_NEW' in config:
+    if "DV_VALUE_NEW" in config:
         config.DV_VALUE = config.DV_VALUE_NEW
 
-    config_file = open(filename,'w')
+    config_file = open(filename, "w")
     # write dummy file
     for key in config.keys():
-        config_file.write( '%s= 0 \n' % key )
+        config_file.write("%s= 0 \n" % key)
     config_file.close()
     # dump data
-    write_config(filename,config)
-
+    write_config(filename, config)
diff --git a/SU2_PY/SU2/io/config_options.py b/SU2_PY/SU2/io/config_options.py
index 6423e8499d0..1fda9691abd 100644
--- a/SU2_PY/SU2/io/config_options.py
+++ b/SU2_PY/SU2/io/config_options.py
@@ -29,130 +29,139 @@
 
 from ..util import ordered_bunch
 
+
 class OptionError(Exception):
     pass
 
-class Option(object):
 
+class Option(object):
     def __init__(self):
         self.val = ""
 
     def __get__(self):
         return self.val
 
-    def __set__(self,newval):
+    def __set__(self, newval):
         self.val = newval
 
+
 #: class Option
 
-class MathProblem(Option):
 
-    def __init__(self,*args,**kwarg):
-        super(MathProblem,self).__init__(*args,**kwarg)
-        self.validoptions = ['DIRECT','CONTINUOUS_ADJOINT','LINEARIZED']
+class MathProblem(Option):
+    def __init__(self, *args, **kwarg):
+        super(MathProblem, self).__init__(*args, **kwarg)
+        self.validoptions = ["DIRECT", "CONTINUOUS_ADJOINT", "LINEARIZED"]
 
-    def __set__(self,newval):
+    def __set__(self, newval):
         if not self.newval in self.validoptions:
-            raise OptionError("Invalid option. Valid options are: %s"%self.validoptions)
-        super(MathProblem,self).__set__(newval)
+            raise OptionError(
+                "Invalid option. Valid options are: %s" % self.validoptions
+            )
+        super(MathProblem, self).__set__(newval)
+
 
 #: class MathProblem
 
+
 class DEFINITION_DV(ordered_bunch):
-    """ SU2.io.config.DEFINITION_DV()
-
-        List of design variables (Design variables are separated by semicolons)
-        2D Design variables
-    	   -FFD_CONTROL_POINT_2D (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-           -FFD_CAMBER_2D 	 (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-	   -FFD_THICKNESS_2D 	 (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-	   -FFD_TWIST_2D    	 (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-   	   -HICKS_HENNE 	 (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
- 	   -ANGLE_OF_ATTACK	 ( 101, Scale | Mark. List | 1.0 )
-
-	3D Design variables
- 	   -FFD_CONTROL_POINT    (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
- 	   -FFD_NACELLE          (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-  	   -FFD_GULL             (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
- 	   -FFD_CAMBER      	 (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-     	   -FFD_TWIST    	 (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-           -FFD_THICKNESS 	 (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-  	   -FFD_ROTATION	 (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-	   -FFD_ANGLE_OF_ATTACK  (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-
-	Global design variables
-	   -TRANSLATION  ( 1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
- 	   -ROTATION	 ( 2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
+    """SU2.io.config.DEFINITION_DV()
+
+    List of design variables (Design variables are separated by semicolons)
+    2D Design variables
+       -FFD_CONTROL_POINT_2D (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
+       -FFD_CAMBER_2D 	 (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
+       -FFD_THICKNESS_2D 	 (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
+       -FFD_TWIST_2D    	 (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
+       -HICKS_HENNE 	 (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
+       -ANGLE_OF_ATTACK	 ( 101, Scale | Mark. List | 1.0 )
+
+    3D Design variables
+       -FFD_CONTROL_POINT    (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
+       -FFD_NACELLE          (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
+       -FFD_GULL             (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
+       -FFD_CAMBER      	 (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
+       -FFD_TWIST    	 (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
+       -FFD_THICKNESS 	 (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
+       -FFD_ROTATION	 (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
+       -FFD_ANGLE_OF_ATTACK  (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
+
+    Global design variables
+       -TRANSLATION  ( 1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
+       -ROTATION	 ( 2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
 
     """
 
-    def __init__(self,*args,**kwarg):
+    def __init__(self, *args, **kwarg):
         ordered_bunch.__init__(self)
-        self.KIND   = []
-        self.SCALE  = []
+        self.KIND = []
+        self.SCALE = []
         self.MARKER = []
         self.FFDTAG = []
-        self.PARAM  = []
-        self.update(ordered_bunch(*args,**kwarg))
-
-    def append(self,new_dv):
-        self.KIND.  append(new_dv['KIND'])
-        self.SCALE. append(new_dv['SCALE'])
-        self.MARKER.append(new_dv['MARKER'])
-        self.FFDTAG.append(new_dv['FFDTAG'])
-        self.PARAM. append(new_dv['PARAM'])
-
-    def extend(self,new_dvs):
-        assert isinstance(new_dvs,DEFINITION_DV) , 'input must be of type DEFINITION_DV'
-        self.KIND.  extend(new_dvs['KIND'])
-        self.SCALE. extend(new_dvs['SCALE'])
-        self.MARKER.extend(new_dvs['MARKER'])
-        self.FFDTAG.extend(new_dvs['FFDTAG'])
-        self.PARAM. extend(new_dvs['PARAM'])
+        self.PARAM = []
+        self.update(ordered_bunch(*args, **kwarg))
+
+    def append(self, new_dv):
+        self.KIND.append(new_dv["KIND"])
+        self.SCALE.append(new_dv["SCALE"])
+        self.MARKER.append(new_dv["MARKER"])
+        self.FFDTAG.append(new_dv["FFDTAG"])
+        self.PARAM.append(new_dv["PARAM"])
+
+    def extend(self, new_dvs):
+        assert isinstance(new_dvs, DEFINITION_DV), "input must be of type DEFINITION_DV"
+        self.KIND.extend(new_dvs["KIND"])
+        self.SCALE.extend(new_dvs["SCALE"])
+        self.MARKER.extend(new_dvs["MARKER"])
+        self.FFDTAG.extend(new_dvs["FFDTAG"])
+        self.PARAM.extend(new_dvs["PARAM"])
+
 
 #: class DEFINITION_DV
 
+
 class DV_KIND(ordered_bunch):
-  """ SU2.io.config.DV_KIND()
-
-        List of design variables (Design variables are separated by semicolons)
-        2D Design variables
-    	   -FFD_CONTROL_POINT_2D (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-           -FFD_CAMBER_2D 	 (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
-	   -FFD_THICKNESS_2D 	 (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-	   -FFD_TWIST_2D    	 (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
-   	   -HICKS_HENNE 	 (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
- 	   -ANGLE_OF_ATTACK	 ( 101, Scale | Mark. List | 1.0 )
-
-	3D Design variables
- 	   -FFD_CONTROL_POINT    (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
- 	   -FFD_NACELLE          (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
-  	   -FFD_GULL             (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
- 	   -FFD_CAMBER      	 (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-     	   -FFD_TWIST    	 (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-           -FFD_THICKNESS 	 (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-  	   -FFD_ROTATION	 (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-	   -FFD_ANGLE_OF_ATTACK  (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
-
-	Global design variables
-	   -TRANSLATION  ( 1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
- 	   -ROTATION	 ( 2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
+    """SU2.io.config.DV_KIND()
+
+    List of design variables (Design variables are separated by semicolons)
+    2D Design variables
+       -FFD_CONTROL_POINT_2D (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
+       -FFD_CAMBER_2D 	 (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
+       -FFD_THICKNESS_2D 	 (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
+       -FFD_TWIST_2D    	 (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
+       -HICKS_HENNE 	 (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
+       -ANGLE_OF_ATTACK	 ( 101, Scale | Mark. List | 1.0 )
+
+    3D Design variables
+       -FFD_CONTROL_POINT    (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
+       -FFD_NACELLE          (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
+       -FFD_GULL             (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
+       -FFD_CAMBER      	 (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
+       -FFD_TWIST    	 (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
+       -FFD_THICKNESS 	 (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
+       -FFD_ROTATION	 (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
+       -FFD_ANGLE_OF_ATTACK  (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
+
+    Global design variables
+       -TRANSLATION  ( 1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
+       -ROTATION	 ( 2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
 
     """
 
-  def __init__(self,*args,**kwarg):
-    ordered_bunch.__init__(self)
-    self.FFDTAG = []
-    self.PARAM  = []
-    self.update(ordered_bunch(*args,**kwarg))
+    def __init__(self, *args, **kwarg):
+        ordered_bunch.__init__(self)
+        self.FFDTAG = []
+        self.PARAM = []
+        self.update(ordered_bunch(*args, **kwarg))
+
+    def append(self, new_dv):
+        self.FFDTAG.append(new_dv["FFDTAG"])
+        self.PARAM.append(new_dv["PARAM"])
 
-  def append(self,new_dv):
-    self.FFDTAG.append(new_dv['FFDTAG'])
-    self.PARAM. append(new_dv['PARAM'])
+    def extend(self, new_dvs):
+        assert isinstance(new_dvs, DV_KIND), "input must be of type DV_KIND"
+        self.FFDTAG.extend(new_dvs["FFDTAG"])
+        self.PARAM.extend(new_dvs["PARAM"])
 
-  def extend(self,new_dvs):
-    assert isinstance(new_dvs,DV_KIND) , 'input must be of type DV_KIND'
-    self.FFDTAG.extend(new_dvs['FFDTAG'])
-    self.PARAM. extend(new_dvs['PARAM'])
 
 #: class DV_KIND
diff --git a/SU2_PY/SU2/io/data.py b/SU2_PY/SU2/io/data.py
index ee667f0d18d..a666b3643e4 100644
--- a/SU2_PY/SU2/io/data.py
+++ b/SU2_PY/SU2/io/data.py
@@ -30,6 +30,7 @@
 # ----------------------------------------------------------------------
 
 import os, sys, shutil, copy
+
 if sys.version_info[0] > 2:
     # Py3 pickle now manage both accelerated cPickle and pure python pickle
     # See https://docs.python.org/3/whatsnew/3.0.html#library-changes, 4th item.
@@ -44,67 +45,69 @@
 #  Load a Dictionary of Data
 # -------------------------------------------------------------------
 
-def load_data( file_name, var_names=None   ,
-               file_format = 'infer'       ,
-               core_name   = 'python_data'  ):
-    """ data = load_data( file_name, var_names=None   ,
-                          file_format = 'infer'       ,
-                          core_name   = 'python_data'  )
-
-        loads dictionary of data from python pickle or matlab struct
-
-        Inputs:
-            file_name   - data file name
-            var_names   - variable names to read
-            file_format - 'infer', 'pickle', or 'matlab'
-            core_name   - data is stored under a dictionary with this name
-
-        default looks for variable 'python_data' in file_name
-        file_format = pickle, will return any python object
-        file_format = matlab, will return strings or float lists and
-        requires scipy.io.loadmat
-        file_format = infer (default), will infer format from extention
-        ('.mat','.pkl')
+
+def load_data(file_name, var_names=None, file_format="infer", core_name="python_data"):
+    """data = load_data( file_name, var_names=None   ,
+                      file_format = 'infer'       ,
+                      core_name   = 'python_data'  )
+
+    loads dictionary of data from python pickle or matlab struct
+
+    Inputs:
+        file_name   - data file name
+        var_names   - variable names to read
+        file_format - 'infer', 'pickle', or 'matlab'
+        core_name   - data is stored under a dictionary with this name
+
+    default looks for variable 'python_data' in file_name
+    file_format = pickle, will return any python object
+    file_format = matlab, will return strings or float lists and
+    requires scipy.io.loadmat
+    file_format = infer (default), will infer format from extention
+    ('.mat','.pkl')
     """
 
     try:
         import scipy.io
+
         scipy_loaded = True
     except ImportError:
         scipy_loaded = False
 
     if not os.path.exists(file_name):
-        raise Exception('File does not exist: %s' % file_name)
+        raise Exception("File does not exist: %s" % file_name)
 
     # process file format
-    if file_format == 'infer':
-        if   os.path.splitext(file_name)[1] == '.mat':
-            file_format = 'matlab'
-        elif os.path.splitext(file_name)[1] == '.pkl':
-            file_format = 'pickle'
-    assert file_format in ['matlab','pickle'] , 'unsupported file format'
+    if file_format == "infer":
+        if os.path.splitext(file_name)[1] == ".mat":
+            file_format = "matlab"
+        elif os.path.splitext(file_name)[1] == ".pkl":
+            file_format = "pickle"
+    assert file_format in ["matlab", "pickle"], "unsupported file format"
 
     # get filelock
     with filelock(file_name):
 
         # LOAD MATLAB
-        if file_format == 'matlab' and scipy_loaded:
-            input_data = scipy.io.loadmat( file_name        = file_name ,
-                                           squeeze_me       = False     ,
-                                           chars_as_strings = True      ,
-                                           struct_as_record = True       )
+        if file_format == "matlab" and scipy_loaded:
+            input_data = scipy.io.loadmat(
+                file_name=file_name,
+                squeeze_me=False,
+                chars_as_strings=True,
+                struct_as_record=True,
+            )
             # pull core variable
-            assert (core_name in input_data) , 'core data not found'
+            assert core_name in input_data, "core data not found"
             input_data = input_data[core_name]
 
             # convert recarray to dictionary
             input_data = rec2dict(input_data)
 
         # LOAD PICKLE
-        elif file_format == 'pickle':
+        elif file_format == "pickle":
             input_data = load_pickle(file_name)
             # pull core variable
-            assert (core_name in input_data) , 'core data not found'
+            assert core_name in input_data, "core data not found"
             input_data = input_data[core_name]
 
         #: if file_format
@@ -114,8 +117,10 @@ def load_data( file_name, var_names=None   ,
     # load specified varname into dictionary
     if var_names != None:
         # check for one item name array
-        if isinstance(var_names,str):
-            var_names = [var_names,]
+        if isinstance(var_names, str):
+            var_names = [
+                var_names,
+            ]
         for key in input_data.keys():
             if not key in var_names:
                 del input_data[key]
@@ -124,53 +129,55 @@ def load_data( file_name, var_names=None   ,
 
     return input_data
 
-#: def load()
 
+#: def load()
 
 
 # -------------------------------------------------------------------
 #  Save a Dictionary of Data
 # -------------------------------------------------------------------
 
-def save_data( file_name, data_dict, append=False ,
+
+def save_data(
+    file_name, data_dict, append=False, file_format="infer", core_name="python_data"
+):
+    """save_data( file_name, data_dict, append=False ,
                file_format = 'infer'              ,
                core_name='python_data'             ):
-    """ save_data( file_name, data_dict, append=False ,
-                   file_format = 'infer'              ,
-                   core_name='python_data'             ):
-
-        Inputs:
-            file_name   - data file name
-            data_dict   - a dictionary or bunch to write
-            append      - True/False to append existing data
-            file_format - 'infer', 'pickle', or 'matlab'
-            core_name   - data is stored under a dictionary with this name
-
-        file_format = pickle, will save any pickleable python object
-        file_format = matlab, will save strings or float lists and
-        requires scipy.io.loadmat
-        file_format = infer (default), will infer format from extention
-        ('.mat','.pkl')
-
-        matlab format saves data file from matlab 5 and later
-        will save nested dictionaries into nested matlab structures
-        cannot save classes and modules
-        uses scipy.io.loadmat
+
+    Inputs:
+        file_name   - data file name
+        data_dict   - a dictionary or bunch to write
+        append      - True/False to append existing data
+        file_format - 'infer', 'pickle', or 'matlab'
+        core_name   - data is stored under a dictionary with this name
+
+    file_format = pickle, will save any pickleable python object
+    file_format = matlab, will save strings or float lists and
+    requires scipy.io.loadmat
+    file_format = infer (default), will infer format from extention
+    ('.mat','.pkl')
+
+    matlab format saves data file from matlab 5 and later
+    will save nested dictionaries into nested matlab structures
+    cannot save classes and modules
+    uses scipy.io.loadmat
     """
 
     try:
         import scipy.io
+
         scipy_loaded = True
     except ImportError:
         scipy_loaded = False
 
     # process file format
-    if file_format == 'infer':
-        if   os.path.splitext(file_name)[1] == '.mat':
-            file_format = 'matlab'
-        elif os.path.splitext(file_name)[1] == '.pkl':
-            file_format = 'pickle'
-    assert file_format in ['matlab','pickle'] , 'unsupported file format'
+    if file_format == "infer":
+        if os.path.splitext(file_name)[1] == ".mat":
+            file_format = "matlab"
+        elif os.path.splitext(file_name)[1] == ".pkl":
+            file_format = "pickle"
+    assert file_format in ["matlab", "pickle"], "unsupported file format"
 
     # get filelock
     with filelock(file_name):
@@ -180,34 +187,38 @@ def save_data( file_name, data_dict, append=False ,
         if append == True and os.path.exists(file_name):
             # check file exists
             if not os.path.exists(file_name):
-                raise Exception('Cannot append, file does not exist: %s' % file_name)
+                raise Exception("Cannot append, file does not exist: %s" % file_name)
             # load old data
-            data_dict_old = load( file_name   = file_name   ,
-                                  var_names   = None        ,
-                                  file_format = file_format ,
-                                  core_name   = core_name    )
+            data_dict_old = load(
+                file_name=file_name,
+                var_names=None,
+                file_format=file_format,
+                core_name=core_name,
+            )
             # check for keys not in new data
-            for key,value in data_dict_old.iteritems():
-                if not(key in data_dict):
+            for key, value in data_dict_old.iteritems():
+                if not (key in data_dict):
                     data_dict[key] = value
             #: for each dict item
         #: if append
 
         # save to core name
-        data_dict = {core_name : data_dict}
+        data_dict = {core_name: data_dict}
 
         # SAVE MATLAB
-        if file_format == 'matlab':
+        if file_format == "matlab":
             # bunch it
             data_dict = mat_bunch(data_dict)
             # save it
-            scipy.io.savemat( file_name = file_name ,
-                              mdict     = data_dict,
-                              format    = '5',        # matlab 5 .mat format
-                              oned_as   = 'column' )
-        elif file_format == 'pickle':
+            scipy.io.savemat(
+                file_name=file_name,
+                mdict=data_dict,
+                format="5",  # matlab 5 .mat format
+                oned_as="column",
+            )
+        elif file_format == "pickle":
             # save it
-            save_pickle(file_name,data_dict)
+            save_pickle(file_name, data_dict)
 
         #: if file_format
 
@@ -215,26 +226,27 @@ def save_data( file_name, data_dict, append=False ,
 
     return
 
-#: def save()
 
+#: def save()
 
 
 # -------------------------------------------------------------------
 #  Load Pickle
 # -------------------------------------------------------------------
 
+
 def load_pickle(file_name):
-    """ data = load_pickle(file_name)
-        loads a pickle with core_data dictionaries
-        assumes first entry is a list of all following data names
-        returns dictionary of data
+    """data = load_pickle(file_name)
+    loads a pickle with core_data dictionaries
+    assumes first entry is a list of all following data names
+    returns dictionary of data
     """
-    pkl_file = open(file_name,'rb')
-    #names = safe_unpickle.loadf(pkl_file)
+    pkl_file = open(file_name, "rb")
+    # names = safe_unpickle.loadf(pkl_file)
     names = pickle.load(pkl_file)
-    data_dict = dict.fromkeys(names,[])
+    data_dict = dict.fromkeys(names, [])
     for key in names:
-        #data_dict[key] = safe_unpickle.loadf(pkl_file)
+        # data_dict[key] = safe_unpickle.loadf(pkl_file)
         data_dict[key] = pickle.load(pkl_file)
     pkl_file.close()
     return data_dict
@@ -244,12 +256,13 @@ def load_pickle(file_name):
 #  Save Pickle
 # -------------------------------------------------------------------
 
+
 def save_pickle(file_name, data_dict):
-    """ save_pickle(file_name, data_dict)
-        saves a core data dictionary
-        first pickle entry is a list of all following data names
+    """save_pickle(file_name, data_dict)
+    saves a core data dictionary
+    first pickle entry is a list of all following data names
     """
-    pkl_file = open(file_name, 'wb')
+    pkl_file = open(file_name, "wb")
     names = list(data_dict.keys())
     pickle.dump(names, pkl_file)
     for key in names:
@@ -261,84 +274,84 @@ def save_pickle(file_name, data_dict):
 #  Safe UnPickle
 # -------------------------------------------------------------------
 
-#class safe_unpickle(pickle.Unpickler):
-    #''' adds some safety to unpickling
-        #checks that only supported classes are loaded
-        #original source from http://nadiana.com/python-pickle-insecure#comment-144
-    #'''
-
-    ## modules : classes considered safe
-    #PICKLE_SAFE = {
-        #'copy_reg'        : ['_reconstructor']  ,
-        #'__builtin__'     : ['object']          ,
-        #'numpy'           : ['dtype','ndarray'] ,
-        #'numpy.core.multiarray' : ['scalar','_reconstruct'] ,
-        #'collections'     : ['OrderedDict']     ,
-        #'SU2.io.state'    : ['State']           , # SU2 Specific
-        #'SU2.io.config'   : ['Config']          ,
-        #'SU2.eval.design' : ['Design']          ,
-        #'SU2.opt.project' : ['Project']         ,
-        #'SU2.util.ordered_bunch' : ['OrderedBunch'] ,
-        #'SU2.util.bunch'  : ['Bunch']           ,
-        #'tasks_general'   : ['General_Task']    ,
-        #'tasks_project'   : ['Project','Job']   ,
-        #'tasks_su2'       : ['Decomp','Deform','Direct','Cont_Adjoint',
-                             #'Multiple_Cont_Adjoint','Finite_Diff','Adapt'] ,
-    #}
-
-    ## make sets
-    #for key in PICKLE_SAFE.keys():
-        #PICKLE_SAFE[key] = set(PICKLE_SAFE[key])
-
-    ## check for save module/class
-    #def find_class(self, module, name):
-        #if not module in self.PICKLE_SAFE:
-            #raise pickle.UnpicklingError(
-                #'Attempting to unpickle unsafe module %s' % module
-            #)
-        #__import__(module)
-        #mod = sys.modules[module]
-        #if not name in self.PICKLE_SAFE[module]:
-            #raise pickle.UnpicklingError(
-                #'Attempting to unpickle unsafe class %s' % name
-            #)
-        #klass = getattr(mod, name)
-        #return klass
-
-    ## extend the load() and loads() methods
-    #@classmethod
-    #def loadf(self, pickle_file): # loads a file like pickle.load()
-        #return self(pickle_file).load()
-    #@classmethod
-    #def loads(self, pickle_string): #loads a string like pickle.loads()
-        #return self(StringIO.StringIO(pickle_string)).load()
-
+# class safe_unpickle(pickle.Unpickler):
+#''' adds some safety to unpickling
+# checks that only supported classes are loaded
+# original source from http://nadiana.com/python-pickle-insecure#comment-144
+#'''
+
+## modules : classes considered safe
+# PICKLE_SAFE = {
+#'copy_reg'        : ['_reconstructor']  ,
+#'__builtin__'     : ['object']          ,
+#'numpy'           : ['dtype','ndarray'] ,
+#'numpy.core.multiarray' : ['scalar','_reconstruct'] ,
+#'collections'     : ['OrderedDict']     ,
+#'SU2.io.state'    : ['State']           , # SU2 Specific
+#'SU2.io.config'   : ['Config']          ,
+#'SU2.eval.design' : ['Design']          ,
+#'SU2.opt.project' : ['Project']         ,
+#'SU2.util.ordered_bunch' : ['OrderedBunch'] ,
+#'SU2.util.bunch'  : ['Bunch']           ,
+#'tasks_general'   : ['General_Task']    ,
+#'tasks_project'   : ['Project','Job']   ,
+#'tasks_su2'       : ['Decomp','Deform','Direct','Cont_Adjoint',
+#'Multiple_Cont_Adjoint','Finite_Diff','Adapt'] ,
+# }
+
+## make sets
+# for key in PICKLE_SAFE.keys():
+# PICKLE_SAFE[key] = set(PICKLE_SAFE[key])
+
+## check for save module/class
+# def find_class(self, module, name):
+# if not module in self.PICKLE_SAFE:
+# raise pickle.UnpicklingError(
+#'Attempting to unpickle unsafe module %s' % module
+# )
+# __import__(module)
+# mod = sys.modules[module]
+# if not name in self.PICKLE_SAFE[module]:
+# raise pickle.UnpicklingError(
+#'Attempting to unpickle unsafe class %s' % name
+# )
+# klass = getattr(mod, name)
+# return klass
+
+## extend the load() and loads() methods
+# @classmethod
+# def loadf(self, pickle_file): # loads a file like pickle.load()
+# return self(pickle_file).load()
+# @classmethod
+# def loads(self, pickle_string): #loads a string like pickle.loads()
+# return self(StringIO.StringIO(pickle_string)).load()
 
 
 # -------------------------------------------------------------------
 #  Convert Record Array to Dictionary
 # -------------------------------------------------------------------
 
+
 def rec2dict(array_in):
-    """ converts numpy record array to dictionary of lists
-        needed for loading matlab data
-        assumes array comes from scipy.io.loadmat, with
-        squeeze_me = False and struct_as_record = True
+    """converts numpy record array to dictionary of lists
+    needed for loading matlab data
+    assumes array comes from scipy.io.loadmat, with
+    squeeze_me = False and struct_as_record = True
     """
 
     import numpy
 
-    assert isinstance(array_in,numpy.ndarray) , 'input must be a numpy record array'
+    assert isinstance(array_in, numpy.ndarray), "input must be a numpy record array"
 
     # make sure it's not an object array
-    if array_in.dtype == numpy.dtype('object'):
+    if array_in.dtype == numpy.dtype("object"):
         array_in = array_in.tolist()
 
     # get record keys/names
     keys = array_in.dtype.names
 
     # start output dictionary
-    dataout = dict.fromkeys(keys,[])
+    dataout = dict.fromkeys(keys, [])
 
     for key in keys:
 
@@ -346,11 +359,11 @@ def rec2dict(array_in):
         value = array_in[key].tolist()[0][0]
 
         # convert string
-        if isinstance(value[0],unicode):
+        if isinstance(value[0], unicode):
             value = str(value[0])
 
         # convert array
-        elif isinstance(value,numpy.ndarray):
+        elif isinstance(value, numpy.ndarray):
             # check for another struct level
             if value.dtype.names == None:
                 value = value.tolist()
@@ -363,6 +376,7 @@ def rec2dict(array_in):
 
     return dataout
 
+
 #: def rec2dict()
 
 
@@ -370,30 +384,31 @@ def rec2dict(array_in):
 #  Flatten a List
 # -------------------------------------------------------------------
 
+
 def flatten_list(input_list):
-    ''' flatten an irregular list of lists of any depth
-    '''
+    """flatten an irregular list of lists of any depth"""
     output_list = []
     for value in input_list:
-        if isinstance(value,list):
-            output_list.extend( flatten_list(value) ) # telescope
+        if isinstance(value, list):
+            output_list.extend(flatten_list(value))  # telescope
         else:
             output_list.append(value)
     return output_list
 
-#: def flatten_list()
 
+#: def flatten_list()
 
 
 # -------------------------------------------------------------------
 #  Append Lists in a Nested Dictionary
 # -------------------------------------------------------------------
 
-def append_nestdict(base_dict,add_dict):
-    """ append_nestdict(base_dict,add_dict)
-        appends base_dict with add_dict, allowing for
-        updating nested dictionaries
-        will update base_dict in place
+
+def append_nestdict(base_dict, add_dict):
+    """append_nestdict(base_dict,add_dict)
+    appends base_dict with add_dict, allowing for
+    updating nested dictionaries
+    will update base_dict in place
     """
 
     # break pointer
@@ -404,18 +419,19 @@ def append_nestdict(base_dict,add_dict):
 
         # ensure base_dict key exists and is a list
         if not base_dict.has_key(key):
-            if isinstance( add_dict[key] , dict ):
+            if isinstance(add_dict[key], dict):
                 base_dict[key] = {}
             else:
                 base_dict[key] = []
-        elif not (    isinstance( base_dict[key] , list )
-                   or isinstance( base_dict[key] , dict ) ):
-            assert not isinstance( add_dict[key] , dict ) , 'base[key] is not a dictionary while add[key] is'
+        elif not (isinstance(base_dict[key], list) or isinstance(base_dict[key], dict)):
+            assert not isinstance(
+                add_dict[key], dict
+            ), "base[key] is not a dictionary while add[key] is"
             base_dict[key] = [base_dict[key]]
 
         # append list or telescope
-        if isinstance( base_dict[key] , dict ):
-            append_nestdict(base_dict[key],add_dict[key]) # telescope
+        if isinstance(base_dict[key], dict):
+            append_nestdict(base_dict[key], add_dict[key])  # telescope
         else:
             base_dict[key].append(add_dict[key])
 
@@ -424,28 +440,27 @@ def append_nestdict(base_dict,add_dict):
     # base_dict will be updated through its pointer
     return
 
-#: def append_nestdict()
-
-
-
-
 
+#: def append_nestdict()
 
 
 # -------------------------------------------------------------------
 #  Matlab Bunch Class
 # -------------------------------------------------------------------
 
+
 class mat_bunch:
-    """ replicates dictionary functionality with class dot structure
-        for output of dictionaries to matlab
+    """replicates dictionary functionality with class dot structure
+    for output of dictionaries to matlab
     """
 
     def __init__(self, d):
         for k, v in d.items():
             if isinstance(v, dict):
-                if len(v): v = mat_bunch(v)
-                else:      v = []
+                if len(v):
+                    v = mat_bunch(v)
+                else:
+                    v = []
             self.__dict__[k] = v
 
     def __dict__(self):
@@ -454,27 +469,31 @@ def __dict__(self):
     # items
     def keys(self):
         return self.__dict__.keys()
+
     def values(self):
         return self.__dict__.values()
+
     def items(self):
         return self.__dict__.items()
 
     # dictionary get/set/etc
-    def __getitem__(self,k):
+    def __getitem__(self, k):
         return self.__dict__[k]
-    def __setitem__(self,k,v):
+
+    def __setitem__(self, k, v):
         self.__dict__[k] = v
-    def __delitem__(self,k):
+
+    def __delitem__(self, k):
         del self.__dict__[k]
+
     def __str__(self):
-        print_format = '%s: %s'
+        print_format = "%s: %s"
         state = []
-        for k,v in self.__dict__.items():
-            if isinstance(v,mat_bunch):
-                v = '%i-item mat_bunch' % len(v.items())
-            state.append(print_format % (k,v) )
-        return '\n'.join(state)
-
-#: class mat_bunch
+        for k, v in self.__dict__.items():
+            if isinstance(v, mat_bunch):
+                v = "%i-item mat_bunch" % len(v.items())
+            state.append(print_format % (k, v))
+        return "\n".join(state)
 
 
+#: class mat_bunch
diff --git a/SU2_PY/SU2/io/filelock.py b/SU2_PY/SU2/io/filelock.py
index 87da207295f..1a6a15b19ae 100644
--- a/SU2_PY/SU2/io/filelock.py
+++ b/SU2_PY/SU2/io/filelock.py
@@ -32,27 +32,27 @@
 #  File Lock Class
 # -------------------------------------------------------------------
 class filelock(object):
-    """ A file locking mechanism that has context-manager support so
-        you can use it in a with statement.
-
-        Example:
-        with filelock("test.txt", timeout=2, delay=0.5):
-            print("Lock acquired.")
-            # Do something with the locked file
-
-        Inputs:
-            file_name - filename to lock
-            timeout   - default 10sec, maximum timeout to wait for lock
-            delay     - default 0.05sec, delay between each attempt to lock
-                        number incremented with a random perturbation
-
-        original source: Evan Fosmark, BSD license
-        http://www.evanfosmark.com/2009/01/cross-platform-file-locking-support-in-python/
+    """A file locking mechanism that has context-manager support so
+    you can use it in a with statement.
+
+    Example:
+    with filelock("test.txt", timeout=2, delay=0.5):
+        print("Lock acquired.")
+        # Do something with the locked file
+
+    Inputs:
+        file_name - filename to lock
+        timeout   - default 10sec, maximum timeout to wait for lock
+        delay     - default 0.05sec, delay between each attempt to lock
+                    number incremented with a random perturbation
+
+    original source: Evan Fosmark, BSD license
+    http://www.evanfosmark.com/2009/01/cross-platform-file-locking-support-in-python/
     """
 
-    def __init__(self, file_name, timeout=10, delay=.05):
-        """ Prepare the file locker. Specify the file to lock and optionally
-            the maximum timeout and the delay between each attempt to lock.
+    def __init__(self, file_name, timeout=10, delay=0.05):
+        """Prepare the file locker. Specify the file to lock and optionally
+        the maximum timeout and the delay between each attempt to lock.
         """
         self.is_locked = False
         self.lockfile = os.path.join(os.getcwd(), "%s.lock" % file_name)
@@ -60,63 +60,62 @@ def __init__(self, file_name, timeout=10, delay=.05):
         self.timeout = timeout
         self.delay = delay
 
-
     def acquire(self):
-        """ Acquire the lock, if possible. If the lock is in use, it check again
-            every `wait` seconds. It does this until it either gets the lock or
-            exceeds `timeout` number of seconds, in which case it throws
-            an exception.
+        """Acquire the lock, if possible. If the lock is in use, it check again
+        every `wait` seconds. It does this until it either gets the lock or
+        exceeds `timeout` number of seconds, in which case it throws
+        an exception.
         """
         start_time = time.time()
         while True:
             try:
-                self.fd = os.open(self.lockfile, os.O_CREAT|os.O_EXCL|os.O_RDWR)
-                break;
+                self.fd = os.open(self.lockfile, os.O_CREAT | os.O_EXCL | os.O_RDWR)
+                break
             except OSError as e:
                 if e.errno != errno.EEXIST:
                     raise
                 if (time.time() - start_time) >= self.timeout:
-                    raise FileLockException("FileLock timeout occured for %s" % self.lockfile)
-                delay = self.delay*( 1. + 0.2*random() )
+                    raise FileLockException(
+                        "FileLock timeout occured for %s" % self.lockfile
+                    )
+                delay = self.delay * (1.0 + 0.2 * random())
                 time.sleep(delay)
         self.is_locked = True
 
-
     def release(self):
-        """ Get rid of the lock by deleting the lockfile.
-            When working in a `with` statement, this gets automatically
-            called at the end.
+        """Get rid of the lock by deleting the lockfile.
+        When working in a `with` statement, this gets automatically
+        called at the end.
         """
         if self.is_locked:
             os.close(self.fd)
             os.unlink(self.lockfile)
             self.is_locked = False
 
-
     def __enter__(self):
-        """ Activated when used in the with statement.
-            Should automatically acquire a lock to be used in the with block.
+        """Activated when used in the with statement.
+        Should automatically acquire a lock to be used in the with block.
         """
         if not self.is_locked:
             self.acquire()
         return self
 
-
     def __exit__(self, type, value, traceback):
-        """ Activated at the end of the with statement.
-            It automatically releases the lock if it isn't locked.
+        """Activated at the end of the with statement.
+        It automatically releases the lock if it isn't locked.
         """
         if self.is_locked:
             self.release()
 
-
     def __del__(self):
-        """ Make sure that the FileLock instance doesn't leave a lockfile
-            lying around.
+        """Make sure that the FileLock instance doesn't leave a lockfile
+        lying around.
         """
         self.release()
 
+
 class FileLockException(Exception):
     pass
 
+
 #: class filelock
diff --git a/SU2_PY/SU2/io/historyMap.py b/SU2_PY/SU2/io/historyMap.py
index 1e16597389c..aca169155e2 100644
--- a/SU2_PY/SU2/io/historyMap.py
+++ b/SU2_PY/SU2/io/historyMap.py
@@ -1,1480 +1,2011 @@
-history_header_map = {'ADJOINT_DISP_X': {'DESCRIPTION': 'Root-mean square residual of the adjoint '
-                                   'of the X displacements.',
-                    'GROUP': 'RMS_RES',
-                    'HEADER': 'rms[Ux_adj]',
-                    'TYPE': 'RESIDUAL'},
- 'ADJOINT_DISP_Y': {'DESCRIPTION': 'Root-mean square residual of the adjoint '
-                                   'of the Y displacements.',
-                    'GROUP': 'RMS_RES',
-                    'HEADER': 'rms[Uy_adj]',
-                    'TYPE': 'RESIDUAL'},
- 'ADJOINT_DISP_Z': {'DESCRIPTION': 'Root-mean square residual of the adjoint '
-                                   'of the Z displacements.',
-                    'GROUP': 'RMS_RES',
-                    'HEADER': 'rms[Uz_adj]',
-                    'TYPE': 'RESIDUAL'},
- 'ADJOINT_SOLEXTRA': {'DESCRIPTION': 'Adjoint value of the first extra '
-                                     'Solution.',
-                      'GROUP': 'ADJOINT_SOLEXTRA',
-                      'HEADER': 'Adjoint_SolExtra',
-                      'TYPE': 'COEFFICIENT'},
- 'AOA': {'DESCRIPTION': 'Angle of attack',
-         'GROUP': 'AOA',
-         'HEADER': 'AoA',
-         'TYPE': 'DEFAULT'},
- 'AVG_CFL': {'DESCRIPTION': 'Current average of the local CFL numbers',
-             'GROUP': 'CFL_NUMBER',
-             'HEADER': 'Avg CFL',
-             'TYPE': 'DEFAULT'},
- 'AVG_DENSITY': {'DESCRIPTION': 'Total average density on all markers set in '
-                                'MARKER_ANALYZE',
-                 'GROUP': 'FLOW_COEFF',
-                 'HEADER': 'Avg_Density',
-                 'TYPE': 'COEFFICIENT'},
- 'AVG_ENTHALPY': {'DESCRIPTION': 'Total average enthalpy on all markers set in '
-                                 'MARKER_ANALYZE',
-                  'GROUP': 'FLOW_COEFF',
-                  'HEADER': 'Avg_Enthalpy',
-                  'TYPE': 'COEFFICIENT'},
- 'AVG_NORMALVEL': {'DESCRIPTION': 'Total average normal velocity on all '
-                                  'markers set in MARKER_ANALYZE',
-                   'GROUP': 'FLOW_COEFF',
-                   'HEADER': 'Avg_NormalVel',
-                   'TYPE': 'COEFFICIENT'},
- 'AVG_TEMPERATURE': {'DESCRIPTION': 'Average temperature on all surfaces '
-                                    'defined in MARKER_MONITORING',
-                     'GROUP': 'HEAT',
-                     'HEADER': 'AvgTemp',
-                     'TYPE': 'COEFFICIENT'},
- 'BGS_ADJ_DENSITY': {'DESCRIPTION': 'BGS residual of the adjoint density.',
-                     'GROUP': 'BGS_RES',
-                     'HEADER': 'bgs[A_Rho]',
-                     'TYPE': 'RESIDUAL'},
- 'BGS_ADJ_DISP_X': {'DESCRIPTION': 'BGS residual of the adjoint X '
-                                   'displacement.',
-                    'GROUP': 'BGS_RES',
-                    'HEADER': 'bgs[A_Ux]',
-                    'TYPE': 'RESIDUAL'},
- 'BGS_ADJ_DISP_Y': {'DESCRIPTION': 'BGS residual of the adjoint Y '
-                                   'displacement.',
-                    'GROUP': 'BGS_RES',
-                    'HEADER': 'bgs[A_Uy]',
-                    'TYPE': 'RESIDUAL'},
- 'BGS_ADJ_DISP_Z': {'DESCRIPTION': 'BGS residual of the adjoint Z '
-                                   'displacement.',
-                    'GROUP': 'BGS_RES',
-                    'HEADER': 'bgs[A_Uz]',
-                    'TYPE': 'RESIDUAL'},
- 'BGS_ADJ_DISSIPATION': {'DESCRIPTION': 'BGS residual of the adjoint '
-                                        'dissipation.',
-                         'GROUP': 'BGS_RES',
-                         'HEADER': 'bgs[A_w]',
-                         'TYPE': 'RESIDUAL'},
- 'BGS_ADJ_ENERGY': {'DESCRIPTION': 'BGS residual of the adjoint energy.',
-                    'GROUP': 'BGS_RES',
-                    'HEADER': 'bgs[A_E]',
-                    'TYPE': 'RESIDUAL'},
- 'BGS_ADJ_MOMENTUM-X': {'DESCRIPTION': 'BGS residual of the adjoint momentum '
-                                       'x-component',
-                        'GROUP': 'BGS_RES',
-                        'HEADER': 'bgs[A_RhoU]',
-                        'TYPE': 'RESIDUAL'},
- 'BGS_ADJ_MOMENTUM-Y': {'DESCRIPTION': 'BGS residual of the adjoint momentum '
-                                       'y-component',
-                        'GROUP': 'BGS_RES',
-                        'HEADER': 'bgs[A_RhoV]',
-                        'TYPE': 'RESIDUAL'},
- 'BGS_ADJ_MOMENTUM-Z': {'DESCRIPTION': 'BGS residual of the adjoint momentum '
-                                       'z-component',
-                        'GROUP': 'BGS_RES',
-                        'HEADER': 'bgs[A_RhoW]',
-                        'TYPE': 'RESIDUAL'},
- 'BGS_ADJ_NU_TILDE': {'DESCRIPTION': 'BGS residual of the adjoint nu tilde.',
-                      'GROUP': 'BGS_RES',
-                      'HEADER': 'bgs[A_nu]',
-                      'TYPE': 'RESIDUAL'},
- 'BGS_ADJ_PRESSURE': {'DESCRIPTION': 'BGS residual of the adjoint Pressure.',
-                      'GROUP': 'BGS_RES',
-                      'HEADER': 'bgs[A_Rho]',
-                      'TYPE': 'RESIDUAL'},
- 'BGS_ADJ_RAD_ENERGY': {'DESCRIPTION': 'BGS residual  of the P1 radiative '
-                                       'energy.',
-                        'GROUP': 'BGS_RES',
-                        'HEADER': 'bgs[A_P1]',
-                        'TYPE': 'RESIDUAL'},
- 'BGS_ADJ_SPECIES_" + std::to_string(iVar': {'DESCRIPTION': 'BGS residual of '
-                                                            'the adjoint '
-                                                            'transported '
-                                                            'species.',
-                                             'GROUP': 'BGS_RES',
-                                             'HEADER': 'bgs[A_rho*Y_" + '
-                                                       'std::to_string(iVar) + '
-                                                       '"]',
-                                             'TYPE': 'RESIDUAL'},
- 'BGS_ADJ_TEMPERATURE': {'DESCRIPTION': 'BGS residual of the adjoint '
-                                        'temperature.',
-                         'GROUP': 'BGS_RES',
-                         'HEADER': 'bgs[A_T]',
-                         'TYPE': 'RESIDUAL'},
- 'BGS_ADJ_TKE': {'DESCRIPTION': 'BGS residual of the adjoint kinetic energy.',
-                 'GROUP': 'BGS_RES',
-                 'HEADER': 'bgs[A_k]',
-                 'TYPE': 'RESIDUAL'},
- 'BGS_ADJ_VELOCITY-X': {'DESCRIPTION': 'BGS residual of the adjoint Velocity '
-                                       'x-component',
-                        'GROUP': 'BGS_RES',
-                        'HEADER': 'bgs[A_RhoU]',
-                        'TYPE': 'RESIDUAL'},
- 'BGS_ADJ_VELOCITY-Y': {'DESCRIPTION': 'BGS residual of the adjoint Velocity '
-                                       'y-component',
-                        'GROUP': 'BGS_RES',
-                        'HEADER': 'bgs[A_RhoV]',
-                        'TYPE': 'RESIDUAL'},
- 'BGS_ADJ_VELOCITY-Z': {'DESCRIPTION': 'BGS residual of the adjoint Velocity '
-                                       'z-component',
-                        'GROUP': 'BGS_RES',
-                        'HEADER': 'bgs[A_RhoW]',
-                        'TYPE': 'RESIDUAL'},
- 'BGS_DENSITY': {'DESCRIPTION': 'BGS residual of the density.',
-                 'GROUP': 'BGS_RES',
-                 'HEADER': 'bgs[Rho]',
-                 'TYPE': 'RESIDUAL'},
- 'BGS_DISP_X': {'DESCRIPTION': 'BGS residual of X displacement',
-                'GROUP': 'BGS_RES',
-                'HEADER': 'bgs[DispX]',
-                'TYPE': 'RESIDUAL'},
- 'BGS_DISP_Y': {'DESCRIPTION': 'BGS residual of Y displacement',
-                'GROUP': 'BGS_RES',
-                'HEADER': 'bgs[DispY]',
-                'TYPE': 'RESIDUAL'},
- 'BGS_DISP_Z': {'DESCRIPTION': 'BGS residual of Z displacement',
-                'GROUP': 'BGS_RES',
-                'HEADER': 'bgs[DispZ]',
-                'TYPE': 'RESIDUAL'},
- 'BGS_DISSIPATION': {'DESCRIPTION': 'BGS residual of dissipation (SST model).',
-                     'GROUP': 'BGS_RES',
-                     'HEADER': 'bgs[w]',
-                     'TYPE': 'RESIDUAL'},
- 'BGS_ENERGY': {'DESCRIPTION': 'BGS residual of the energy.',
-                'GROUP': 'BGS_RES',
-                'HEADER': 'bgs[RhoE]',
-                'TYPE': 'RESIDUAL'},
- 'BGS_MOMENTUM-X': {'DESCRIPTION': 'BGS residual of the momentum x-component.',
-                    'GROUP': 'BGS_RES',
-                    'HEADER': 'bgs[RhoU]',
-                    'TYPE': 'RESIDUAL'},
- 'BGS_MOMENTUM-Y': {'DESCRIPTION': 'BGS residual of the momentum y-component.',
-                    'GROUP': 'BGS_RES',
-                    'HEADER': 'bgs[RhoV]',
-                    'TYPE': 'RESIDUAL'},
- 'BGS_NU_TILDE': {'DESCRIPTION': 'BGS residual of nu tilde (SA model).',
-                  'GROUP': 'BGS_RES',
-                  'HEADER': 'bgs[nu]',
-                  'TYPE': 'RESIDUAL'},
- 'BGS_PRESSURE': {'DESCRIPTION': 'BGS residual of the pressure.',
-                  'GROUP': 'BGS_RES',
-                  'HEADER': 'bgs[P]',
-                  'TYPE': 'RESIDUAL'},
- 'BGS_SPECIES_" + std::to_string(iVar': {'DESCRIPTION': 'BGS residual of '
-                                                        'transported species.',
-                                         'GROUP': 'BGS_RES',
-                                         'HEADER': 'bgs[rho*Y_" + '
-                                                   'std::to_string(iVar)+"]',
-                                         'TYPE': 'RESIDUAL'},
- 'BGS_TEMPERATURE': {'DESCRIPTION': 'Block-Gauss-Seidel residual of the '
-                                    'temperature',
-                     'GROUP': 'BGS_RES',
-                     'HEADER': 'bgs[T]',
-                     'TYPE': 'RESIDUAL'},
- 'BGS_TKE': {'DESCRIPTION': 'BGS residual of kinetic energy (SST model).',
-             'GROUP': 'BGS_RES',
-             'HEADER': 'bgs[k]',
-             'TYPE': 'RESIDUAL'},
- 'BGS_VELOCITY-X': {'DESCRIPTION': 'BGS residual of the velocity x-component.',
-                    'GROUP': 'BGS_RES',
-                    'HEADER': 'bgs[U]',
-                    'TYPE': 'RESIDUAL'},
- 'BGS_VELOCITY-Y': {'DESCRIPTION': 'BGS residual of the velocity y-component.',
-                    'GROUP': 'BGS_RES',
-                    'HEADER': 'bgs[V]',
-                    'TYPE': 'RESIDUAL'},
- 'BGS_VELOCITY-Z': {'DESCRIPTION': 'BGS residual of the velocity z-component.',
-                    'GROUP': 'BGS_RES',
-                    'HEADER': 'bgs[W]',
-                    'TYPE': 'RESIDUAL'},
- 'BUFFET': {'DESCRIPTION': 'Buffet sensor',
-            'GROUP': 'AERO_COEFF',
-            'HEADER': 'Buffet',
-            'TYPE': 'COEFFICIENT'},
- 'CFL_NUMBER': {'DESCRIPTION': 'Current value of the CFL number',
-                'GROUP': 'CFL_NUMBER',
-                'HEADER': 'CFL number',
-                'TYPE': 'DEFAULT'},
- 'CHANGE_IN_AOA': {'DESCRIPTION': 'Last change in Angle of Attack by Fixed CL '
-                                  'Driver',
-                   'GROUP': 'FIXED_CL',
-                   'HEADER': 'Change_in_AOA',
-                   'TYPE': 'RESIDUAL'},
- 'CL_DRIVER_COMMAND': {'DESCRIPTION': "CL Driver's control command",
-                       'GROUP': 'FIXED_CL',
-                       'HEADER': 'CL_Driver_Command',
-                       'TYPE': 'RESIDUAL'},
- 'COMBO': {'DESCRIPTION': 'Combined obj. function value.',
-           'GROUP': 'COMBO',
-           'HEADER': 'ComboObj',
-           'TYPE': 'COEFFICIENT'},
- 'DEFORM_ITER': {'DESCRIPTION': 'Linear solver iterations for the mesh '
-                                'deformation',
-                 'GROUP': 'DEFORM',
-                 'HEADER': 'DeformIter',
-                 'TYPE': 'DEFAULT'},
- 'DEFORM_MAX_VOLUME': {'DESCRIPTION': 'Maximum volume in the mesh',
-                       'GROUP': 'DEFORM',
-                       'HEADER': 'MaxVolume',
-                       'TYPE': 'DEFAULT'},
- 'DEFORM_MIN_VOLUME': {'DESCRIPTION': 'Minimum volume in the mesh',
-                       'GROUP': 'DEFORM',
-                       'HEADER': 'MinVolume',
-                       'TYPE': 'DEFAULT'},
- 'DEFORM_RESIDUAL': {'DESCRIPTION': 'Residual of the linear solver for the '
-                                    'mesh deformation',
-                     'GROUP': 'DEFORM',
-                     'HEADER': 'DeformRes',
-                     'TYPE': 'DEFAULT'},
- 'DELTA_CL': {'DESCRIPTION': 'Difference between Target CL and current CL',
-              'GROUP': 'FIXED_CL',
-              'HEADER': 'Delta_CL',
-              'TYPE': 'COEFFICIENT'},
- 'DRAG': {'DESCRIPTION': 'Total drag coefficient on all surfaces set with '
-                         'MARKER_MONITORING',
-          'GROUP': 'AERO_COEFF',
-          'HEADER': 'CD',
-          'TYPE': 'COEFFICIENT'},
- 'D_ADJOINT_SOLEXTRA': {'DESCRIPTION': 'Derivative value',
-                        'GROUP': 'D_ADJOINT_SOLEXTRA',
-                        'HEADER': 'd[Adjoint_SolExtra]',
-                        'TYPE': 'D_COEFFICIENT'},
- 'D_AVG_DENSITY': {'DESCRIPTION': 'Derivative value',
-                   'GROUP': 'D_FLOW_COEFF',
-                   'HEADER': 'd[Avg_Density]',
-                   'TYPE': 'D_COEFFICIENT'},
- 'D_AVG_ENTHALPY': {'DESCRIPTION': 'Derivative value',
-                    'GROUP': 'D_FLOW_COEFF',
-                    'HEADER': 'd[Avg_Enthalpy]',
-                    'TYPE': 'D_COEFFICIENT'},
- 'D_AVG_NORMALVEL': {'DESCRIPTION': 'Derivative value',
-                     'GROUP': 'D_FLOW_COEFF',
-                     'HEADER': 'd[Avg_NormalVel]',
-                     'TYPE': 'D_COEFFICIENT'},
- 'D_AVG_TEMPERATURE': {'DESCRIPTION': 'Derivative value',
-                       'GROUP': 'D_HEAT',
-                       'HEADER': 'd[AvgTemp]',
-                       'TYPE': 'D_COEFFICIENT'},
- 'D_BUFFET': {'DESCRIPTION': 'Derivative value',
-              'GROUP': 'D_AERO_COEFF',
-              'HEADER': 'd[Buffet]',
-              'TYPE': 'D_COEFFICIENT'},
- 'D_COMBO': {'DESCRIPTION': 'Derivative value',
-             'GROUP': 'D_COMBO',
-             'HEADER': 'd[ComboObj]',
-             'TYPE': 'D_COEFFICIENT'},
- 'D_DELTA_CL': {'DESCRIPTION': 'Derivative value',
-                'GROUP': 'D_FIXED_CL',
-                'HEADER': 'd[Delta_CL]',
-                'TYPE': 'D_COEFFICIENT'},
- 'D_DRAG': {'DESCRIPTION': 'Derivative value',
-            'GROUP': 'D_AERO_COEFF',
-            'HEADER': 'd[CD]',
-            'TYPE': 'D_COEFFICIENT'},
- 'D_EFFICIENCY': {'DESCRIPTION': 'Derivative value',
-                  'GROUP': 'D_AERO_COEFF',
-                  'HEADER': 'd[CEff]',
-                  'TYPE': 'D_COEFFICIENT'},
- 'D_EQUIVALENT_AREA': {'DESCRIPTION': 'Derivative value',
-                       'GROUP': 'D_EQUIVALENT_AREA',
-                       'HEADER': 'd[CEquiv_Area]',
-                       'TYPE': 'D_COEFFICIENT'},
- 'D_FIGURE_OF_MERIT': {'DESCRIPTION': 'Derivative value',
-                       'GROUP': 'D_ROTATING_FRAME',
-                       'HEADER': 'd[CMerit]',
-                       'TYPE': 'D_COEFFICIENT'},
- 'D_FORCE_X': {'DESCRIPTION': 'Derivative value',
-               'GROUP': 'D_AERO_COEFF',
-               'HEADER': 'd[CFx]',
-               'TYPE': 'D_COEFFICIENT'},
- 'D_FORCE_Y': {'DESCRIPTION': 'Derivative value',
-               'GROUP': 'D_AERO_COEFF',
-               'HEADER': 'd[CFy]',
-               'TYPE': 'D_COEFFICIENT'},
- 'D_FORCE_Z': {'DESCRIPTION': 'Derivative value',
-               'GROUP': 'D_AERO_COEFF',
-               'HEADER': 'd[CFz]',
-               'TYPE': 'D_COEFFICIENT'},
- 'D_INVERSE_DESIGN_PRESSURE': {'DESCRIPTION': 'Derivative value',
-                               'GROUP': 'D_CP_DIFF',
-                               'HEADER': 'd[Cp_Diff]',
-                               'TYPE': 'D_COEFFICIENT'},
- 'D_LIFT': {'DESCRIPTION': 'Derivative value',
-            'GROUP': 'D_AERO_COEFF',
-            'HEADER': 'd[CL]',
-            'TYPE': 'D_COEFFICIENT'},
- 'D_MAXIMUM_HEATFLUX': {'DESCRIPTION': 'Derivative value',
-                        'GROUP': 'D_HEAT',
-                        'HEADER': 'd[MaxHF]',
-                        'TYPE': 'D_COEFFICIENT'},
- 'D_MOMENT_X': {'DESCRIPTION': 'Derivative value',
-                'GROUP': 'D_AERO_COEFF',
-                'HEADER': 'd[CMx]',
-                'TYPE': 'D_COEFFICIENT'},
- 'D_MOMENT_Y': {'DESCRIPTION': 'Derivative value',
-                'GROUP': 'D_AERO_COEFF',
-                'HEADER': 'd[CMy]',
-                'TYPE': 'D_COEFFICIENT'},
- 'D_MOMENT_Z': {'DESCRIPTION': 'Derivative value',
-                'GROUP': 'D_AERO_COEFF',
-                'HEADER': 'd[CMz]',
-                'TYPE': 'D_COEFFICIENT'},
- 'D_REFERENCE_GEOMETRY': {'DESCRIPTION': 'Derivative value',
-                          'GROUP': 'D_STRUCT_COEFF',
-                          'HEADER': 'd[RefGeom]',
-                          'TYPE': 'D_COEFFICIENT'},
- 'D_REFERENCE_NODE': {'DESCRIPTION': 'Derivative value',
-                      'GROUP': 'D_STRUCT_COEFF',
-                      'HEADER': 'd[RefNode]',
-                      'TYPE': 'D_COEFFICIENT'},
- 'D_SENS_AOA': {'DESCRIPTION': 'Derivative value',
-                'GROUP': 'D_SENSITIVITY',
-                'HEADER': 'd[Sens_AoA]',
-                'TYPE': 'D_COEFFICIENT'},
- 'D_SENS_GEO': {'DESCRIPTION': 'Derivative value',
-                'GROUP': 'D_SENSITIVITY',
-                'HEADER': 'd[Sens_Geo]',
-                'TYPE': 'D_COEFFICIENT'},
- 'D_SENS_MACH': {'DESCRIPTION': 'Derivative value',
-                 'GROUP': 'D_SENSITIVITY',
-                 'HEADER': 'd[Sens_Mach]',
-                 'TYPE': 'D_COEFFICIENT'},
- 'D_SENS_PRESS': {'DESCRIPTION': 'Derivative value',
-                  'GROUP': 'D_SENSITIVITY',
-                  'HEADER': 'd[Sens_Press]',
-                  'TYPE': 'D_COEFFICIENT'},
- 'D_SENS_PRESS_OUT': {'DESCRIPTION': 'Derivative value',
-                      'GROUP': 'D_SENSITIVITY',
-                      'HEADER': 'd[Sens_Pout]',
-                      'TYPE': 'D_COEFFICIENT'},
- 'D_SENS_TEMP': {'DESCRIPTION': 'Derivative value',
-                 'GROUP': 'D_SENSITIVITY',
-                 'HEADER': 'd[Sens_Temp]',
-                 'TYPE': 'D_COEFFICIENT'},
- 'D_SENS_VEL_IN': {'DESCRIPTION': 'Derivative value',
-                   'GROUP': 'D_SENSITIVITY',
-                   'HEADER': 'd[Sens_Vin]',
-                   'TYPE': 'D_COEFFICIENT'},
- 'D_SIDEFORCE': {'DESCRIPTION': 'Derivative value',
-                 'GROUP': 'D_AERO_COEFF',
-                 'HEADER': 'd[CSF]',
-                 'TYPE': 'D_COEFFICIENT'},
- 'D_STRESS_PENALTY': {'DESCRIPTION': 'Derivative value',
-                      'GROUP': 'D_STRUCT_COEFF',
-                      'HEADER': 'd[StressPen]',
-                      'TYPE': 'D_COEFFICIENT'},
- 'D_SURFACE_MACH': {'DESCRIPTION': 'Derivative value',
-                    'GROUP': 'D_FLOW_COEFF',
-                    'HEADER': 'd[Avg_Mach]',
-                    'TYPE': 'D_COEFFICIENT'},
- 'D_SURFACE_MASSFLOW': {'DESCRIPTION': 'Derivative value',
-                        'GROUP': 'D_FLOW_COEFF',
-                        'HEADER': 'd[Avg_Massflow]',
-                        'TYPE': 'D_COEFFICIENT'},
- 'D_SURFACE_MOM_DISTORTION': {'DESCRIPTION': 'Derivative value',
-                              'GROUP': 'D_FLOW_COEFF',
-                              'HEADER': 'd[Momentum_Distortion]',
-                              'TYPE': 'D_COEFFICIENT'},
- 'D_SURFACE_PRESSURE_DROP': {'DESCRIPTION': 'Derivative value',
-                             'GROUP': 'D_FLOW_COEFF',
-                             'HEADER': 'd[Pressure_Drop]',
-                             'TYPE': 'D_COEFFICIENT'},
- 'D_SURFACE_SECONDARY': {'DESCRIPTION': 'Derivative value',
-                         'GROUP': 'D_FLOW_COEFF',
-                         'HEADER': 'd[Secondary_Strength]',
-                         'TYPE': 'D_COEFFICIENT'},
- 'D_SURFACE_SECOND_OVER_UNIFORM': {'DESCRIPTION': 'Derivative value',
-                                   'GROUP': 'D_FLOW_COEFF',
-                                   'HEADER': 'd[Secondary_Over_Uniformity]',
-                                   'TYPE': 'D_COEFFICIENT'},
- 'D_SURFACE_SPECIES_" + std::to_string(iVar': {'DESCRIPTION': 'Derivative '
-                                                              'value',
-                                               'GROUP': 'D_SPECIES_COEFF',
-                                               'HEADER': 'd[Avg_Species_" + '
-                                                         'std::to_string(iVar]',
-                                               'TYPE': 'D_COEFFICIENT'},
- 'D_SURFACE_STATIC_PRESSURE': {'DESCRIPTION': 'Derivative value',
-                               'GROUP': 'D_FLOW_COEFF',
-                               'HEADER': 'd[Avg_Press]',
-                               'TYPE': 'D_COEFFICIENT'},
- 'D_SURFACE_STATIC_TEMPERATURE': {'DESCRIPTION': 'Derivative value',
-                                  'GROUP': 'D_FLOW_COEFF',
-                                  'HEADER': 'd[Avg_Temp]',
-                                  'TYPE': 'D_COEFFICIENT'},
- 'D_SURFACE_TOTAL_PRESSURE': {'DESCRIPTION': 'Derivative value',
-                              'GROUP': 'D_FLOW_COEFF',
-                              'HEADER': 'd[Avg_TotalPress]',
-                              'TYPE': 'D_COEFFICIENT'},
- 'D_SURFACE_TOTAL_TEMPERATURE': {'DESCRIPTION': 'Derivative value',
-                                 'GROUP': 'D_FLOW_COEFF',
-                                 'HEADER': 'd[Avg_TotalTemp]',
-                                 'TYPE': 'D_COEFFICIENT'},
- 'D_SURFACE_UNIFORMITY': {'DESCRIPTION': 'Derivative value',
-                          'GROUP': 'D_FLOW_COEFF',
-                          'HEADER': 'd[Uniformity]',
-                          'TYPE': 'D_COEFFICIENT'},
- 'D_THRUST': {'DESCRIPTION': 'Derivative value',
-              'GROUP': 'D_ROTATING_FRAME',
-              'HEADER': 'd[CT]',
-              'TYPE': 'D_COEFFICIENT'},
- 'D_TOPOL_COMPLIANCE': {'DESCRIPTION': 'Derivative value',
-                        'GROUP': 'D_STRUCT_COEFF',
-                        'HEADER': 'd[TopComp]',
-                        'TYPE': 'D_COEFFICIENT'},
- 'D_TOPOL_DISCRETENESS': {'DESCRIPTION': 'Derivative value',
-                          'GROUP': 'D_STRUCT_COEFF',
-                          'HEADER': 'd[TopDisc]',
-                          'TYPE': 'D_COEFFICIENT'},
- 'D_TORQUE': {'DESCRIPTION': 'Derivative value',
-              'GROUP': 'D_ROTATING_FRAME',
-              'HEADER': 'd[CQ]',
-              'TYPE': 'D_COEFFICIENT'},
- 'D_TOTAL_HEATFLUX': {'DESCRIPTION': 'Derivative value',
-                      'GROUP': 'D_HEAT',
-                      'HEADER': 'd[HF]',
-                      'TYPE': 'D_COEFFICIENT'},
- 'D_VOLUME_FRACTION': {'DESCRIPTION': 'Derivative value',
-                       'GROUP': 'D_STRUCT_COEFF',
-                       'HEADER': 'd[VolFrac]',
-                       'TYPE': 'D_COEFFICIENT'},
- 'EFFICIENCY': {'DESCRIPTION': 'Total lift-to-drag ratio on all surfaces set '
-                               'with MARKER_MONITORING',
-                'GROUP': 'AERO_COEFF',
-                'HEADER': 'CEff',
-                'TYPE': 'COEFFICIENT'},
- 'EQUIVALENT_AREA': {'DESCRIPTION': 'Equivalent area',
-                     'GROUP': 'EQUIVALENT_AREA',
-                     'HEADER': 'CEquiv_Area',
-                     'TYPE': 'COEFFICIENT'},
- 'FIGURE_OF_MERIT': {'DESCRIPTION': 'Thrust over torque',
-                     'GROUP': 'ROTATING_FRAME',
-                     'HEADER': 'CMerit',
-                     'TYPE': 'COEFFICIENT'},
- 'FORCE_X': {'DESCRIPTION': 'Total force x-component on all surfaces set with '
-                            'MARKER_MONITORING',
-             'GROUP': 'AERO_COEFF',
-             'HEADER': 'CFx',
-             'TYPE': 'COEFFICIENT'},
- 'FORCE_Y': {'DESCRIPTION': 'Total force y-component on all surfaces set with '
-                            'MARKER_MONITORING',
-             'GROUP': 'AERO_COEFF',
-             'HEADER': 'CFy',
-             'TYPE': 'COEFFICIENT'},
- 'FORCE_Z': {'DESCRIPTION': 'Total force z-component on all surfaces set with '
-                            'MARKER_MONITORING',
-             'GROUP': 'AERO_COEFF',
-             'HEADER': 'CFz',
-             'TYPE': 'COEFFICIENT'},
- 'INVERSE_DESIGN_PRESSURE': {'DESCRIPTION': 'Cp difference for inverse design',
-                             'GROUP': 'CP_DIFF',
-                             'HEADER': 'Cp_Diff',
-                             'TYPE': 'COEFFICIENT'},
- 'LIFT': {'DESCRIPTION': 'Total lift coefficient on all surfaces set with '
-                         'MARKER_MONITORING',
-          'GROUP': 'AERO_COEFF',
-          'HEADER': 'CL',
-          'TYPE': 'COEFFICIENT'},
- 'LINSOL_ITER': {'DESCRIPTION': 'Number of iterations of the linear solver.',
-                 'GROUP': 'LINSOL',
-                 'HEADER': 'LinSolIter',
-                 'TYPE': 'DEFAULT'},
- 'LINSOL_ITER_SPECIES': {'DESCRIPTION': 'Number of iterations of the linear '
-                                        'solver for species solver.',
-                         'GROUP': 'LINSOL',
-                         'HEADER': 'LinSolIterSpecies',
-                         'TYPE': 'DEFAULT'},
- 'LINSOL_ITER_TURB': {'DESCRIPTION': 'Number of iterations of the linear '
-                                     'solver for turbulence.',
-                      'GROUP': 'LINSOL',
-                      'HEADER': 'LinSolIterTurb',
-                      'TYPE': 'DEFAULT'},
- 'LINSOL_RESIDUAL': {'DESCRIPTION': 'Residual of the linear solver.',
-                     'GROUP': 'LINSOL',
-                     'HEADER': 'LinSolRes',
-                     'TYPE': 'DEFAULT'},
- 'LINSOL_RESIDUAL_SPECIES': {'DESCRIPTION': 'Residual of the linear solver for '
-                                            'species solver.',
-                             'GROUP': 'LINSOL',
-                             'HEADER': 'LinSolResSpecies',
-                             'TYPE': 'DEFAULT'},
- 'LINSOL_RESIDUAL_TURB': {'DESCRIPTION': 'Residual of the linear solver for '
-                                         'turbulence.',
-                          'GROUP': 'LINSOL',
-                          'HEADER': 'LinSolResTurb',
-                          'TYPE': 'DEFAULT'},
- 'LOAD_INCREMENT': {'DESCRIPTION': 'LOAD_INCREMENT',
-                    'GROUP': 'Percent of total load (incremental',
-                    'HEADER': 'Load[%]',
-                    'TYPE': 'DEFAULT'},
- 'LOAD_RAMP': {'DESCRIPTION': 'LOAD_RAMP',
-               'GROUP': 'Fraction of total load (ramped',
-               'HEADER': 'Load_Ramp',
-               'TYPE': 'DEFAULT'},
- 'MAXIMUM_HEATFLUX': {'DESCRIPTION': 'Maximum heatflux on all surfaces defined '
-                                     'in MARKER_MONITORING',
-                      'GROUP': 'HEAT',
-                      'HEADER': 'MaxHF',
-                      'TYPE': 'COEFFICIENT'},
- 'MAX_ADJ_DENSITY': {'DESCRIPTION': 'Maximum residual of the adjoint density.',
-                     'GROUP': 'MAX_RES',
-                     'HEADER': 'max[A_Rho]',
-                     'TYPE': 'RESIDUAL'},
- 'MAX_ADJ_DISSIPATION': {'DESCRIPTION': 'Maximum residual of the adjoint '
-                                        'dissipation.',
-                         'GROUP': 'MAX_RES',
-                         'HEADER': 'max[A_w]',
-                         'TYPE': 'RESIDUAL'},
- 'MAX_ADJ_ENERGY': {'DESCRIPTION': 'Maximum residual of the adjoint energy.',
-                    'GROUP': 'MAX_RES',
-                    'HEADER': 'max[A_E]',
-                    'TYPE': 'RESIDUAL'},
- 'MAX_ADJ_MOMENTUM-X': {'DESCRIPTION': 'Maximum residual of the adjoint '
-                                       'momentum x-component',
-                        'GROUP': 'MAX_RES',
-                        'HEADER': 'max[A_RhoU]',
-                        'TYPE': 'RESIDUAL'},
- 'MAX_ADJ_MOMENTUM-Y': {'DESCRIPTION': 'Maximum residual of the adjoint '
-                                       'momentum y-component',
-                        'GROUP': 'MAX_RES',
-                        'HEADER': 'max[A_RhoV]',
-                        'TYPE': 'RESIDUAL'},
- 'MAX_ADJ_MOMENTUM-Z': {'DESCRIPTION': 'Maximum residual of the adjoint '
-                                       'momentum z-component',
-                        'GROUP': 'MAX_RES',
-                        'HEADER': 'max[A_RhoW]',
-                        'TYPE': 'RESIDUAL'},
- 'MAX_ADJ_NU_TILDE': {'DESCRIPTION': 'Maximum residual of the adjoint nu '
-                                     'tilde.',
-                      'GROUP': 'MAX_RES',
-                      'HEADER': 'max[A_nu]',
-                      'TYPE': 'RESIDUAL'},
- 'MAX_ADJ_PRESSURE': {'DESCRIPTION': 'Maximum residual of the adjoint '
-                                     'Pressure.',
-                      'GROUP': 'MAX_RES',
-                      'HEADER': 'max[A_Rho]',
-                      'TYPE': 'RESIDUAL'},
- 'MAX_ADJ_SPECIES_" + std::to_string(iVar': {'DESCRIPTION': 'Maximum residual '
-                                                            'of the adjoint '
-                                                            'transported '
-                                                            'species.',
-                                             'GROUP': 'MAX_RES',
-                                             'HEADER': 'max[A_rho*Y_" + '
-                                                       'std::to_string(iVar) + '
-                                                       '"]',
-                                             'TYPE': 'RESIDUAL'},
- 'MAX_ADJ_TEMPERATURE': {'DESCRIPTION': 'Maximum residual of the temperature.',
-                         'GROUP': 'MAX_RES',
-                         'HEADER': 'max[A_T]',
-                         'TYPE': 'RESIDUAL'},
- 'MAX_ADJ_TKE': {'DESCRIPTION': 'Maximum residual of the adjoint kinetic '
-                                'energy.',
-                 'GROUP': 'MAX_RES',
-                 'HEADER': 'max[A_k]',
-                 'TYPE': 'RESIDUAL'},
- 'MAX_ADJ_VELOCITY-X': {'DESCRIPTION': 'Maximum residual of the adjoint '
-                                       'Velocity x-component',
-                        'GROUP': 'MAX_RES',
-                        'HEADER': 'max[A_RhoU]',
-                        'TYPE': 'RESIDUAL'},
- 'MAX_ADJ_VELOCITY-Y': {'DESCRIPTION': 'Maximum residual of the adjoint '
-                                       'Velocity y-component',
-                        'GROUP': 'MAX_RES',
-                        'HEADER': 'max[A_RhoV]',
-                        'TYPE': 'RESIDUAL'},
- 'MAX_ADJ_VELOCITY-Z': {'DESCRIPTION': 'Maximum residual of the adjoint '
-                                       'Velocity z-component',
-                        'GROUP': 'MAX_RES',
-                        'HEADER': 'max[A_RhoW]',
-                        'TYPE': 'RESIDUAL'},
- 'MAX_CFL': {'DESCRIPTION': 'Current maximum of the local CFL numbers',
-             'GROUP': 'CFL_NUMBER',
-             'HEADER': 'Max CFL',
-             'TYPE': 'DEFAULT'},
- 'MAX_DELTA_TIME': {'DESCRIPTION': 'Current maximum local time step',
-                    'GROUP': 'CFL_NUMBER',
-                    'HEADER': 'Max DT',
-                    'TYPE': 'DEFAULT'},
- 'MAX_DENSITY': {'DESCRIPTION': 'Maximum square residual of the density.',
-                 'GROUP': 'MAX_RES',
-                 'HEADER': 'max[Rho]',
-                 'TYPE': 'RESIDUAL'},
- 'MAX_DISSIPATION': {'DESCRIPTION': 'Maximum residual of dissipation (SST '
-                                    'model).',
-                     'GROUP': 'MAX_RES',
-                     'HEADER': 'max[w]',
-                     'TYPE': 'RESIDUAL'},
- 'MAX_ENERGY': {'DESCRIPTION': 'Maximum residual of the energy.',
-                'GROUP': 'MAX_RES',
-                'HEADER': 'max[RhoE]',
-                'TYPE': 'RESIDUAL'},
- 'MAX_MOMENTUM-X': {'DESCRIPTION': 'Maximum square residual of the momentum '
-                                   'x-component.',
-                    'GROUP': 'MAX_RES',
-                    'HEADER': 'max[RhoU]',
-                    'TYPE': 'RESIDUAL'},
- 'MAX_MOMENTUM-Y': {'DESCRIPTION': 'Maximum square residual of the momentum '
-                                   'y-component.',
-                    'GROUP': 'MAX_RES',
-                    'HEADER': 'max[RhoV]',
-                    'TYPE': 'RESIDUAL'},
- 'MAX_NU_TILDE': {'DESCRIPTION': 'Maximum residual of nu tilde (SA model).',
-                  'GROUP': 'MAX_RES',
-                  'HEADER': 'max[nu]',
-                  'TYPE': 'RESIDUAL'},
- 'MAX_PRESSURE': {'DESCRIPTION': 'Maximum residual of the pressure.',
-                  'GROUP': 'MAX_RES',
-                  'HEADER': 'max[P]',
-                  'TYPE': 'RESIDUAL'},
- 'MAX_SPECIES_" + std::to_string(iVar': {'DESCRIPTION': 'Maximum residual of '
-                                                        'transported species.',
-                                         'GROUP': 'MAX_RES',
-                                         'HEADER': 'max[rho*Y_" + '
-                                                   'std::to_string(iVar)+"]',
-                                         'TYPE': 'RESIDUAL'},
- 'MAX_TEMPERATURE': {'DESCRIPTION': 'Maximum residual of the temperature',
-                     'GROUP': 'MAX_RES',
-                     'HEADER': 'max[T]',
-                     'TYPE': 'RESIDUAL'},
- 'MAX_TKE': {'DESCRIPTION': 'Maximum residual of kinetic energy (SST model).',
-             'GROUP': 'MAX_RES',
-             'HEADER': 'max[k]',
-             'TYPE': 'RESIDUAL'},
- 'MAX_VELOCITY-X': {'DESCRIPTION': 'Maximum residual of the velocity '
-                                   'x-component.',
-                    'GROUP': 'MAX_RES',
-                    'HEADER': 'max[U]',
-                    'TYPE': 'RESIDUAL'},
- 'MAX_VELOCITY-Y': {'DESCRIPTION': 'Maximum residual of the velocity '
-                                   'y-component.',
-                    'GROUP': 'MAX_RES',
-                    'HEADER': 'max[V]',
-                    'TYPE': 'RESIDUAL'},
- 'MAX_VELOCITY-Z': {'DESCRIPTION': 'Maximum residual of the velocity '
-                                   'z-component.',
-                    'GROUP': 'MAX_RES',
-                    'HEADER': 'max[W]',
-                    'TYPE': 'RESIDUAL'},
- 'MIN_CFL': {'DESCRIPTION': 'Current minimum of the local CFL numbers',
-             'GROUP': 'CFL_NUMBER',
-             'HEADER': 'Min CFL',
-             'TYPE': 'DEFAULT'},
- 'MIN_DELTA_TIME': {'DESCRIPTION': 'Current minimum local time step',
-                    'GROUP': 'CFL_NUMBER',
-                    'HEADER': 'Min DT',
-                    'TYPE': 'DEFAULT'},
- 'MOMENT_X': {'DESCRIPTION': 'Total momentum x-component on all surfaces set '
-                             'with MARKER_MONITORING',
-              'GROUP': 'AERO_COEFF',
-              'HEADER': 'CMx',
-              'TYPE': 'COEFFICIENT'},
- 'MOMENT_Y': {'DESCRIPTION': 'Total momentum y-component on all surfaces set '
-                             'with MARKER_MONITORING',
-              'GROUP': 'AERO_COEFF',
-              'HEADER': 'CMy',
-              'TYPE': 'COEFFICIENT'},
- 'MOMENT_Z': {'DESCRIPTION': 'Total momentum z-component on all surfaces set '
-                             'with MARKER_MONITORING',
-              'GROUP': 'AERO_COEFF',
-              'HEADER': 'CMz',
-              'TYPE': 'COEFFICIENT'},
- 'PREV_AOA': {'DESCRIPTION': 'Angle of Attack at the previous iteration of the '
-                             'Fixed CL driver',
-              'GROUP': 'FIXED_CL',
-              'HEADER': 'Previous_AOA',
-              'TYPE': 'DEFAULT'},
- 'REFERENCE_GEOMETRY': {'DESCRIPTION': 'L2 norm of difference wrt reference '
-                                       'geometry',
-                        'GROUP': 'STRUCT_COEFF',
-                        'HEADER': 'RefGeom',
-                        'TYPE': 'COEFFICIENT'},
- 'REFERENCE_NODE': {'DESCRIPTION': 'Distance to reference node',
-                    'GROUP': 'STRUCT_COEFF',
-                    'HEADER': 'RefNode',
-                    'TYPE': 'COEFFICIENT'},
- 'RMS_ADJ_DENSITY': {'DESCRIPTION': 'Root-mean square residual of the adjoint '
-                                    'density.',
-                     'GROUP': 'RMS_RES',
-                     'HEADER': 'rms[A_Rho]',
-                     'TYPE': 'RESIDUAL'},
- 'RMS_ADJ_DISSIPATION': {'DESCRIPTION': 'Root-mean square residual of the '
-                                        'adjoint dissipation.',
-                         'GROUP': 'RMS_RES',
-                         'HEADER': 'rms[A_w]',
-                         'TYPE': 'RESIDUAL'},
- 'RMS_ADJ_ENERGY': {'DESCRIPTION': 'Root-mean square residual of the adjoint '
-                                   'energy.',
-                    'GROUP': 'RMS_RES',
-                    'HEADER': 'rms[A_E]',
-                    'TYPE': 'RESIDUAL'},
- 'RMS_ADJ_MOMENTUM-X': {'DESCRIPTION': 'Root-mean square residual of the '
-                                       'adjoint momentum x-component.',
-                        'GROUP': 'RMS_RES',
-                        'HEADER': 'rms[A_RhoU]',
-                        'TYPE': 'RESIDUAL'},
- 'RMS_ADJ_MOMENTUM-Y': {'DESCRIPTION': 'Root-mean square residual of the '
-                                       'adjoint momentum y-component.',
-                        'GROUP': 'RMS_RES',
-                        'HEADER': 'rms[A_RhoV]',
-                        'TYPE': 'RESIDUAL'},
- 'RMS_ADJ_MOMENTUM-Z': {'DESCRIPTION': 'Root-mean square residual of the '
-                                       'adjoint momentum z-component.',
-                        'GROUP': 'RMS_RES',
-                        'HEADER': 'rms[A_RhoW]',
-                        'TYPE': 'RESIDUAL'},
- 'RMS_ADJ_NU_TILDE': {'DESCRIPTION': 'Root-mean square residual of the adjoint '
-                                     'nu tilde.',
-                      'GROUP': 'RMS_RES',
-                      'HEADER': 'rms[A_nu]',
-                      'TYPE': 'RESIDUAL'},
- 'RMS_ADJ_PRESSURE': {'DESCRIPTION': 'Root-mean square residual of the adjoint '
-                                     'Pressure.',
-                      'GROUP': 'RMS_RES',
-                      'HEADER': 'rms[A_P]',
-                      'TYPE': 'RESIDUAL'},
- 'RMS_ADJ_RAD_ENERGY': {'DESCRIPTION': 'Root-mean square residual of the P1 '
-                                       'radiative energy.',
-                        'GROUP': 'RMS_RES',
-                        'HEADER': 'rms[A_P1]',
-                        'TYPE': 'RESIDUAL'},
- 'RMS_ADJ_SPECIES_" + std::to_string(iVar': {'DESCRIPTION': 'Root-mean square '
-                                                            'residual of the '
-                                                            'adjoint '
-                                                            'transported '
-                                                            'species.',
-                                             'GROUP': 'RMS_RES',
-                                             'HEADER': 'rms[A_rho*Y_" + '
-                                                       'std::to_string(iVar) + '
-                                                       '"]',
-                                             'TYPE': 'RESIDUAL'},
- 'RMS_ADJ_TEMPERATURE': {'DESCRIPTION': 'Root-mean square residual of the '
-                                        'adjoint temperature.',
-                         'GROUP': 'RMS_RES',
-                         'HEADER': 'rms[A_T]',
-                         'TYPE': 'RESIDUAL'},
- 'RMS_ADJ_TKE': {'DESCRIPTION': 'Root-mean square residual of the adjoint '
-                                'kinetic energy.',
-                 'GROUP': 'RMS_RES',
-                 'HEADER': 'rms[A_k]',
-                 'TYPE': 'RESIDUAL'},
- 'RMS_ADJ_VELOCITY-X': {'DESCRIPTION': 'Root-mean square residual of the '
-                                       'adjoint Velocity x-component.',
-                        'GROUP': 'RMS_RES',
-                        'HEADER': 'rms[A_U]',
-                        'TYPE': 'RESIDUAL'},
- 'RMS_ADJ_VELOCITY-Y': {'DESCRIPTION': 'Root-mean square residual of the '
-                                       'adjoint Velocity y-component.',
-                        'GROUP': 'RMS_RES',
-                        'HEADER': 'rms[A_V]',
-                        'TYPE': 'RESIDUAL'},
- 'RMS_ADJ_VELOCITY-Z': {'DESCRIPTION': 'Root-mean square residual of the '
-                                       'adjoint Velocity z-component.',
-                        'GROUP': 'RMS_RES',
-                        'HEADER': 'rms[A_W]',
-                        'TYPE': 'RESIDUAL'},
- 'RMS_DENSITY': {'DESCRIPTION': 'Root-mean square residual of the density.',
-                 'GROUP': 'RMS_RES',
-                 'HEADER': 'rms[Rho]',
-                 'TYPE': 'RESIDUAL'},
- 'RMS_DISP_X': {'DESCRIPTION': 'Residual of X displacement',
-                'GROUP': 'RMS_RES',
-                'HEADER': 'rms[DispX]',
-                'TYPE': 'RESIDUAL'},
- 'RMS_DISP_Y': {'DESCRIPTION': 'Residual of Y displacement',
-                'GROUP': 'RMS_RES',
-                'HEADER': 'rms[DispY]',
-                'TYPE': 'RESIDUAL'},
- 'RMS_DISP_Z': {'DESCRIPTION': 'Residual of Z displacement',
-                'GROUP': 'RMS_RES',
-                'HEADER': 'rms[DispZ]',
-                'TYPE': 'RESIDUAL'},
- 'RMS_DISSIPATION': {'DESCRIPTION': 'Root-mean square residual of dissipation '
-                                    '(SST model).',
-                     'GROUP': 'RMS_RES',
-                     'HEADER': 'rms[w]',
-                     'TYPE': 'RESIDUAL'},
- 'RMS_ENERGY': {'DESCRIPTION': 'Root-mean square residual of the energy.',
-                'GROUP': 'RMS_RES',
-                'HEADER': 'rms[RhoE]',
-                'TYPE': 'RESIDUAL'},
- 'RMS_ETOL': {'DESCRIPTION': 'Norm of energy/work increment',
-              'GROUP': 'RMS_RES',
-              'HEADER': 'rms[E]',
-              'TYPE': 'RESIDUAL'},
- 'RMS_MOMENTUM-X': {'DESCRIPTION': 'Root-mean square residual of the momentum '
-                                   'x-component.',
-                    'GROUP': 'RMS_RES',
-                    'HEADER': 'rms[RhoU]',
-                    'TYPE': 'RESIDUAL'},
- 'RMS_MOMENTUM-Y': {'DESCRIPTION': 'Root-mean square residual of the momentum '
-                                   'y-component.',
-                    'GROUP': 'RMS_RES',
-                    'HEADER': 'rms[RhoV]',
-                    'TYPE': 'RESIDUAL'},
- 'RMS_NU_TILDE': {'DESCRIPTION': 'Root-mean square residual of nu tilde (SA '
-                                 'model).',
-                  'GROUP': 'RMS_RES',
-                  'HEADER': 'rms[nu]',
-                  'TYPE': 'RESIDUAL'},
- 'RMS_PRESSURE': {'DESCRIPTION': 'Root-mean square residual of the pressure.',
-                  'GROUP': 'RMS_RES',
-                  'HEADER': 'rms[P]',
-                  'TYPE': 'RESIDUAL'},
- 'RMS_RTOL': {'DESCRIPTION': 'Norm of residual',
-              'GROUP': 'RMS_RES',
-              'HEADER': 'rms[R]',
-              'TYPE': 'RESIDUAL'},
- 'RMS_SPECIES_" + std::to_string(iVar': {'DESCRIPTION': 'Root-mean square '
-                                                        'residual of '
-                                                        'transported species.',
-                                         'GROUP': 'RMS_RES',
-                                         'HEADER': 'rms[rho*Y_" + '
-                                                   'std::to_string(iVar)+"]',
-                                         'TYPE': 'RESIDUAL'},
- 'RMS_TEMPERATURE': {'DESCRIPTION': 'Root mean square residual of the '
-                                    'temperature',
-                     'GROUP': 'RMS_RES',
-                     'HEADER': 'rms[T]',
-                     'TYPE': 'RESIDUAL'},
- 'RMS_TKE': {'DESCRIPTION': 'Root-mean square residual of kinetic energy (SST '
-                            'model).',
-             'GROUP': 'RMS_RES',
-             'HEADER': 'rms[k]',
-             'TYPE': 'RESIDUAL'},
- 'RMS_UTOL': {'DESCRIPTION': 'Norm of displacement increment',
-              'GROUP': 'RMS_RES',
-              'HEADER': 'rms[U]',
-              'TYPE': 'RESIDUAL'},
- 'RMS_VELOCITY-X': {'DESCRIPTION': 'Root-mean square residual of the velocity '
-                                   'x-component.',
-                    'GROUP': 'RMS_RES',
-                    'HEADER': 'rms[U]',
-                    'TYPE': 'RESIDUAL'},
- 'RMS_VELOCITY-Y': {'DESCRIPTION': 'Root-mean square residual of the velocity '
-                                   'y-component.',
-                    'GROUP': 'RMS_RES',
-                    'HEADER': 'rms[V]',
-                    'TYPE': 'RESIDUAL'},
- 'SENS_AOA': {'DESCRIPTION': 'Sensitivity of the objective function with '
-                             'respect to the angle of attack (only for '
-                             'compressible solver).',
-              'GROUP': 'SENSITIVITY',
-              'HEADER': 'Sens_AoA',
-              'TYPE': 'COEFFICIENT'},
- 'SENS_E': {'DESCRIPTION': 'd Objective / d Elasticity modulus',
-            'GROUP': 'SENSITIVITY',
-            'HEADER': 'Sens[E]',
-            'TYPE': 'DEFAULT'},
- 'SENS_GEO': {'DESCRIPTION': 'Sum of the geometrical sensitivities on all '
-                             'markers set in MARKER_MONITORING.',
-              'GROUP': 'SENSITIVITY',
-              'HEADER': 'Sens_Geo',
-              'TYPE': 'COEFFICIENT'},
- 'SENS_MACH': {'DESCRIPTION': 'Sensitivity of the objective function with '
-                              'respect to the Mach number (only of '
-                              'compressible solver).',
-               'GROUP': 'SENSITIVITY',
-               'HEADER': 'Sens_Mach',
-               'TYPE': 'COEFFICIENT'},
- 'SENS_NU': {'DESCRIPTION': 'd Objective / d Poisson ratio',
-             'GROUP': 'SENSITIVITY',
-             'HEADER': 'Sens[Nu]',
-             'TYPE': 'DEFAULT'},
- 'SENS_PRESS': {'DESCRIPTION': 'Sensitivity of the objective function with '
-                               'respect to the far-field pressure.',
-                'GROUP': 'SENSITIVITY',
-                'HEADER': 'Sens_Press',
-                'TYPE': 'COEFFICIENT'},
- 'SENS_PRESS_OUT': {'DESCRIPTION': 'Sensitivity of the objective function with '
-                                   'respect to the outlet pressure.',
-                    'GROUP': 'SENSITIVITY',
-                    'HEADER': 'Sens_Pout',
-                    'TYPE': 'COEFFICIENT'},
- 'SENS_TEMP': {'DESCRIPTION': 'Sensitivity of the objective function with '
-                              'respect to the far-field temperature.',
-               'GROUP': 'SENSITIVITY',
-               'HEADER': 'Sens_Temp',
-               'TYPE': 'COEFFICIENT'},
- 'SENS_VEL_IN': {'DESCRIPTION': 'Sensitivity of the objective function with '
-                                'respect to the inlet velocity.',
-                 'GROUP': 'SENSITIVITY',
-                 'HEADER': 'Sens_Vin',
-                 'TYPE': 'COEFFICIENT'},
- 'SIDEFORCE': {'DESCRIPTION': 'Total sideforce coefficient on all surfaces set '
-                              'with MARKER_MONITORING',
-               'GROUP': 'AERO_COEFF',
-               'HEADER': 'CSF',
-               'TYPE': 'COEFFICIENT'},
- 'STREAMWISE_DP': {'DESCRIPTION': 'Pressure drop in streamwise periodic flow',
-                   'GROUP': 'STREAMWISE_PERIODIC',
-                   'HEADER': 'SWDeltaP',
-                   'TYPE': 'DEFAULT'},
- 'STREAMWISE_HEAT': {'DESCRIPTION': 'Integrated heat for streamwise periodic '
-                                    'flow',
-                     'GROUP': 'STREAMWISE_PERIODIC',
-                     'HEADER': 'SWHeat',
-                     'TYPE': 'DEFAULT'},
- 'STREAMWISE_MASSFLOW': {'DESCRIPTION': 'Massflow in streamwise periodic flow',
-                         'GROUP': 'STREAMWISE_PERIODIC',
-                         'HEADER': 'SWMassflow',
-                         'TYPE': 'DEFAULT'},
- 'STRESS_PENALTY': {'DESCRIPTION': 'Aggregate stress penalty',
-                    'GROUP': 'STRUCT_COEFF',
-                    'HEADER': 'StressPen',
-                    'TYPE': 'COEFFICIENT'},
- 'SURFACE_MACH': {'DESCRIPTION': 'Total average mach number on all markers set '
-                                 'in MARKER_ANALYZE',
-                  'GROUP': 'FLOW_COEFF',
-                  'HEADER': 'Avg_Mach',
-                  'TYPE': 'COEFFICIENT'},
- 'SURFACE_MASSFLOW': {'DESCRIPTION': 'Total average mass flow on all markers '
-                                     'set in MARKER_ANALYZE',
-                      'GROUP': 'FLOW_COEFF',
-                      'HEADER': 'Avg_Massflow',
-                      'TYPE': 'COEFFICIENT'},
- 'SURFACE_MOM_DISTORTION': {'DESCRIPTION': 'Total momentum distortion on all '
-                                           'markers set in MARKER_ANALYZE',
-                            'GROUP': 'FLOW_COEFF',
-                            'HEADER': 'Momentum_Distortion',
-                            'TYPE': 'COEFFICIENT'},
- 'SURFACE_PRESSURE_DROP': {'DESCRIPTION': 'Total pressure drop on all markers '
-                                          'set in MARKER_ANALYZE',
-                           'GROUP': 'FLOW_COEFF',
-                           'HEADER': 'Pressure_Drop',
-                           'TYPE': 'COEFFICIENT'},
- 'SURFACE_SECONDARY': {'DESCRIPTION': 'Total secondary strength on all markers '
-                                      'set in MARKER_ANALYZE',
-                       'GROUP': 'FLOW_COEFF',
-                       'HEADER': 'Secondary_Strength',
-                       'TYPE': 'COEFFICIENT'},
- 'SURFACE_SECOND_OVER_UNIFORM': {'DESCRIPTION': 'Total secondary over '
-                                                'uniformity on all markers set '
-                                                'in MARKER_ANALYZE',
-                                 'GROUP': 'FLOW_COEFF',
-                                 'HEADER': 'Secondary_Over_Uniformity',
-                                 'TYPE': 'COEFFICIENT'},
- 'SURFACE_SPECIES_" + std::to_string(iVar': {'DESCRIPTION': 'Total average '
-                                                            'species " + '
-                                                            'std::to_string(iVar) '
-                                                            '+ " on all '
-                                                            'markers set in '
-                                                            'MARKER_ANALYZE',
-                                             'GROUP': 'SPECIES_COEFF',
-                                             'HEADER': 'Avg_Species_" + '
-                                                       'std::to_string(iVar',
-                                             'TYPE': 'COEFFICIENT'},
- 'SURFACE_SPECIES_VARIANCE': {'DESCRIPTION': 'Total species variance',
-                              'GROUP': 'SPECIES_COEFF',
-                              'HEADER': 'Species_Variance',
-                              'TYPE': 'DEFAULT'},
- 'SURFACE_STATIC_PRESSURE': {'DESCRIPTION': 'Total average pressure on all '
-                                            'markers set in MARKER_ANALYZE',
-                             'GROUP': 'FLOW_COEFF',
-                             'HEADER': 'Avg_Press',
-                             'TYPE': 'COEFFICIENT'},
- 'SURFACE_STATIC_TEMPERATURE': {'DESCRIPTION': 'Total average temperature on '
-                                               'all markers set in '
-                                               'MARKER_ANALYZE',
-                                'GROUP': 'FLOW_COEFF',
-                                'HEADER': 'Avg_Temp',
-                                'TYPE': 'COEFFICIENT'},
- 'SURFACE_TOTAL_PRESSURE': {'DESCRIPTION': 'Total average total pressure on '
-                                           'all markers set in MARKER_ANALYZE',
-                            'GROUP': 'FLOW_COEFF',
-                            'HEADER': 'Avg_TotalPress',
-                            'TYPE': 'COEFFICIENT'},
- 'SURFACE_TOTAL_TEMPERATURE': {'DESCRIPTION': 'Total average total temperature '
-                                              'all markers set in '
-                                              'MARKER_ANALYZE',
-                               'GROUP': 'FLOW_COEFF',
-                               'HEADER': 'Avg_TotalTemp',
-                               'TYPE': 'COEFFICIENT'},
- 'SURFACE_UNIFORMITY': {'DESCRIPTION': 'Total flow uniformity on all markers '
-                                       'set in MARKER_ANALYZE',
-                        'GROUP': 'FLOW_COEFF',
-                        'HEADER': 'Uniformity',
-                        'TYPE': 'COEFFICIENT'},
- 'TAVG_ADJOINT_SOLEXTRA': {'DESCRIPTION': 'weighted time average value',
-                           'GROUP': 'TAVG_ADJOINT_SOLEXTRA',
-                           'HEADER': 'tavg[Adjoint_SolExtra]',
-                           'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_AVG_DENSITY': {'DESCRIPTION': 'weighted time average value',
-                      'GROUP': 'TAVG_FLOW_COEFF',
-                      'HEADER': 'tavg[Avg_Density]',
-                      'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_AVG_ENTHALPY': {'DESCRIPTION': 'weighted time average value',
-                       'GROUP': 'TAVG_FLOW_COEFF',
-                       'HEADER': 'tavg[Avg_Enthalpy]',
-                       'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_AVG_NORMALVEL': {'DESCRIPTION': 'weighted time average value',
-                        'GROUP': 'TAVG_FLOW_COEFF',
-                        'HEADER': 'tavg[Avg_NormalVel]',
-                        'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_AVG_TEMPERATURE': {'DESCRIPTION': 'weighted time average value',
-                          'GROUP': 'TAVG_HEAT',
-                          'HEADER': 'tavg[AvgTemp]',
-                          'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_BUFFET': {'DESCRIPTION': 'weighted time average value',
-                 'GROUP': 'TAVG_AERO_COEFF',
-                 'HEADER': 'tavg[Buffet]',
-                 'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_COMBO': {'DESCRIPTION': 'weighted time average value',
-                'GROUP': 'TAVG_COMBO',
-                'HEADER': 'tavg[ComboObj]',
-                'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_DELTA_CL': {'DESCRIPTION': 'weighted time average value',
-                   'GROUP': 'TAVG_FIXED_CL',
-                   'HEADER': 'tavg[Delta_CL]',
-                   'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_DRAG': {'DESCRIPTION': 'weighted time average value',
-               'GROUP': 'TAVG_AERO_COEFF',
-               'HEADER': 'tavg[CD]',
-               'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_D_ADJOINT_SOLEXTRA': {'DESCRIPTION': 'weighted time average derivative '
-                                            'value',
-                             'GROUP': 'TAVG_D_ADJOINT_SOLEXTRA',
-                             'HEADER': 'dtavg[Adjoint_SolExtra]',
-                             'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_AVG_DENSITY': {'DESCRIPTION': 'weighted time average derivative value',
-                        'GROUP': 'TAVG_D_FLOW_COEFF',
-                        'HEADER': 'dtavg[Avg_Density]',
-                        'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_AVG_ENTHALPY': {'DESCRIPTION': 'weighted time average derivative '
-                                        'value',
-                         'GROUP': 'TAVG_D_FLOW_COEFF',
-                         'HEADER': 'dtavg[Avg_Enthalpy]',
-                         'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_AVG_NORMALVEL': {'DESCRIPTION': 'weighted time average derivative '
-                                         'value',
-                          'GROUP': 'TAVG_D_FLOW_COEFF',
-                          'HEADER': 'dtavg[Avg_NormalVel]',
-                          'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_AVG_TEMPERATURE': {'DESCRIPTION': 'weighted time average derivative '
-                                           'value',
-                            'GROUP': 'TAVG_D_HEAT',
-                            'HEADER': 'dtavg[AvgTemp]',
-                            'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_BUFFET': {'DESCRIPTION': 'weighted time average derivative value',
-                   'GROUP': 'TAVG_D_AERO_COEFF',
-                   'HEADER': 'dtavg[Buffet]',
-                   'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_COMBO': {'DESCRIPTION': 'weighted time average derivative value',
-                  'GROUP': 'TAVG_D_COMBO',
-                  'HEADER': 'dtavg[ComboObj]',
-                  'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_DELTA_CL': {'DESCRIPTION': 'weighted time average derivative value',
-                     'GROUP': 'TAVG_D_FIXED_CL',
-                     'HEADER': 'dtavg[Delta_CL]',
-                     'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_DRAG': {'DESCRIPTION': 'weighted time average derivative value',
-                 'GROUP': 'TAVG_D_AERO_COEFF',
-                 'HEADER': 'dtavg[CD]',
-                 'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_EFFICIENCY': {'DESCRIPTION': 'weighted time average derivative value',
-                       'GROUP': 'TAVG_D_AERO_COEFF',
-                       'HEADER': 'dtavg[CEff]',
-                       'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_EQUIVALENT_AREA': {'DESCRIPTION': 'weighted time average derivative '
-                                           'value',
-                            'GROUP': 'TAVG_D_EQUIVALENT_AREA',
-                            'HEADER': 'dtavg[CEquiv_Area]',
-                            'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_FIGURE_OF_MERIT': {'DESCRIPTION': 'weighted time average derivative '
-                                           'value',
-                            'GROUP': 'TAVG_D_ROTATING_FRAME',
-                            'HEADER': 'dtavg[CMerit]',
-                            'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_FORCE_X': {'DESCRIPTION': 'weighted time average derivative value',
-                    'GROUP': 'TAVG_D_AERO_COEFF',
-                    'HEADER': 'dtavg[CFx]',
-                    'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_FORCE_Y': {'DESCRIPTION': 'weighted time average derivative value',
-                    'GROUP': 'TAVG_D_AERO_COEFF',
-                    'HEADER': 'dtavg[CFy]',
-                    'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_FORCE_Z': {'DESCRIPTION': 'weighted time average derivative value',
-                    'GROUP': 'TAVG_D_AERO_COEFF',
-                    'HEADER': 'dtavg[CFz]',
-                    'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_INVERSE_DESIGN_PRESSURE': {'DESCRIPTION': 'weighted time average '
-                                                   'derivative value',
-                                    'GROUP': 'TAVG_D_CP_DIFF',
-                                    'HEADER': 'dtavg[Cp_Diff]',
-                                    'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_LIFT': {'DESCRIPTION': 'weighted time average derivative value',
-                 'GROUP': 'TAVG_D_AERO_COEFF',
-                 'HEADER': 'dtavg[CL]',
-                 'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_MAXIMUM_HEATFLUX': {'DESCRIPTION': 'weighted time average derivative '
-                                            'value',
-                             'GROUP': 'TAVG_D_HEAT',
-                             'HEADER': 'dtavg[MaxHF]',
-                             'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_MOMENT_X': {'DESCRIPTION': 'weighted time average derivative value',
-                     'GROUP': 'TAVG_D_AERO_COEFF',
-                     'HEADER': 'dtavg[CMx]',
-                     'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_MOMENT_Y': {'DESCRIPTION': 'weighted time average derivative value',
-                     'GROUP': 'TAVG_D_AERO_COEFF',
-                     'HEADER': 'dtavg[CMy]',
-                     'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_MOMENT_Z': {'DESCRIPTION': 'weighted time average derivative value',
-                     'GROUP': 'TAVG_D_AERO_COEFF',
-                     'HEADER': 'dtavg[CMz]',
-                     'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_REFERENCE_GEOMETRY': {'DESCRIPTION': 'weighted time average '
-                                              'derivative value',
-                               'GROUP': 'TAVG_D_STRUCT_COEFF',
-                               'HEADER': 'dtavg[RefGeom]',
-                               'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_REFERENCE_NODE': {'DESCRIPTION': 'weighted time average derivative '
-                                          'value',
-                           'GROUP': 'TAVG_D_STRUCT_COEFF',
-                           'HEADER': 'dtavg[RefNode]',
-                           'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_SENS_AOA': {'DESCRIPTION': 'weighted time average derivative value',
-                     'GROUP': 'TAVG_D_SENSITIVITY',
-                     'HEADER': 'dtavg[Sens_AoA]',
-                     'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_SENS_GEO': {'DESCRIPTION': 'weighted time average derivative value',
-                     'GROUP': 'TAVG_D_SENSITIVITY',
-                     'HEADER': 'dtavg[Sens_Geo]',
-                     'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_SENS_MACH': {'DESCRIPTION': 'weighted time average derivative value',
-                      'GROUP': 'TAVG_D_SENSITIVITY',
-                      'HEADER': 'dtavg[Sens_Mach]',
-                      'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_SENS_PRESS': {'DESCRIPTION': 'weighted time average derivative value',
-                       'GROUP': 'TAVG_D_SENSITIVITY',
-                       'HEADER': 'dtavg[Sens_Press]',
-                       'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_SENS_PRESS_OUT': {'DESCRIPTION': 'weighted time average derivative '
-                                          'value',
-                           'GROUP': 'TAVG_D_SENSITIVITY',
-                           'HEADER': 'dtavg[Sens_Pout]',
-                           'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_SENS_TEMP': {'DESCRIPTION': 'weighted time average derivative value',
-                      'GROUP': 'TAVG_D_SENSITIVITY',
-                      'HEADER': 'dtavg[Sens_Temp]',
-                      'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_SENS_VEL_IN': {'DESCRIPTION': 'weighted time average derivative value',
-                        'GROUP': 'TAVG_D_SENSITIVITY',
-                        'HEADER': 'dtavg[Sens_Vin]',
-                        'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_SIDEFORCE': {'DESCRIPTION': 'weighted time average derivative value',
-                      'GROUP': 'TAVG_D_AERO_COEFF',
-                      'HEADER': 'dtavg[CSF]',
-                      'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_STRESS_PENALTY': {'DESCRIPTION': 'weighted time average derivative '
-                                          'value',
-                           'GROUP': 'TAVG_D_STRUCT_COEFF',
-                           'HEADER': 'dtavg[StressPen]',
-                           'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_SURFACE_MACH': {'DESCRIPTION': 'weighted time average derivative '
-                                        'value',
-                         'GROUP': 'TAVG_D_FLOW_COEFF',
-                         'HEADER': 'dtavg[Avg_Mach]',
-                         'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_SURFACE_MASSFLOW': {'DESCRIPTION': 'weighted time average derivative '
-                                            'value',
-                             'GROUP': 'TAVG_D_FLOW_COEFF',
-                             'HEADER': 'dtavg[Avg_Massflow]',
-                             'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_SURFACE_MOM_DISTORTION': {'DESCRIPTION': 'weighted time average '
-                                                  'derivative value',
-                                   'GROUP': 'TAVG_D_FLOW_COEFF',
-                                   'HEADER': 'dtavg[Momentum_Distortion]',
-                                   'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_SURFACE_PRESSURE_DROP': {'DESCRIPTION': 'weighted time average '
-                                                 'derivative value',
-                                  'GROUP': 'TAVG_D_FLOW_COEFF',
-                                  'HEADER': 'dtavg[Pressure_Drop]',
-                                  'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_SURFACE_SECONDARY': {'DESCRIPTION': 'weighted time average derivative '
-                                             'value',
-                              'GROUP': 'TAVG_D_FLOW_COEFF',
-                              'HEADER': 'dtavg[Secondary_Strength]',
-                              'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_SURFACE_SECOND_OVER_UNIFORM': {'DESCRIPTION': 'weighted time average '
-                                                       'derivative value',
-                                        'GROUP': 'TAVG_D_FLOW_COEFF',
-                                        'HEADER': 'dtavg[Secondary_Over_Uniformity]',
-                                        'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_SURFACE_SPECIES_" + std::to_string(iVar': {'DESCRIPTION': 'weighted '
-                                                                   'time '
-                                                                   'average '
-                                                                   'derivative '
-                                                                   'value',
-                                                    'GROUP': 'TAVG_D_SPECIES_COEFF',
-                                                    'HEADER': 'dtavg[Avg_Species_" '
-                                                              '+ '
-                                                              'std::to_string(iVar]',
-                                                    'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_SURFACE_STATIC_PRESSURE': {'DESCRIPTION': 'weighted time average '
-                                                   'derivative value',
-                                    'GROUP': 'TAVG_D_FLOW_COEFF',
-                                    'HEADER': 'dtavg[Avg_Press]',
-                                    'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_SURFACE_STATIC_TEMPERATURE': {'DESCRIPTION': 'weighted time average '
-                                                      'derivative value',
-                                       'GROUP': 'TAVG_D_FLOW_COEFF',
-                                       'HEADER': 'dtavg[Avg_Temp]',
-                                       'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_SURFACE_TOTAL_PRESSURE': {'DESCRIPTION': 'weighted time average '
-                                                  'derivative value',
-                                   'GROUP': 'TAVG_D_FLOW_COEFF',
-                                   'HEADER': 'dtavg[Avg_TotalPress]',
-                                   'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_SURFACE_TOTAL_TEMPERATURE': {'DESCRIPTION': 'weighted time average '
-                                                     'derivative value',
-                                      'GROUP': 'TAVG_D_FLOW_COEFF',
-                                      'HEADER': 'dtavg[Avg_TotalTemp]',
-                                      'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_SURFACE_UNIFORMITY': {'DESCRIPTION': 'weighted time average '
-                                              'derivative value',
-                               'GROUP': 'TAVG_D_FLOW_COEFF',
-                               'HEADER': 'dtavg[Uniformity]',
-                               'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_THRUST': {'DESCRIPTION': 'weighted time average derivative value',
-                   'GROUP': 'TAVG_D_ROTATING_FRAME',
-                   'HEADER': 'dtavg[CT]',
-                   'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_TOPOL_COMPLIANCE': {'DESCRIPTION': 'weighted time average derivative '
-                                            'value',
-                             'GROUP': 'TAVG_D_STRUCT_COEFF',
-                             'HEADER': 'dtavg[TopComp]',
-                             'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_TOPOL_DISCRETENESS': {'DESCRIPTION': 'weighted time average '
-                                              'derivative value',
-                               'GROUP': 'TAVG_D_STRUCT_COEFF',
-                               'HEADER': 'dtavg[TopDisc]',
-                               'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_TORQUE': {'DESCRIPTION': 'weighted time average derivative value',
-                   'GROUP': 'TAVG_D_ROTATING_FRAME',
-                   'HEADER': 'dtavg[CQ]',
-                   'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_TOTAL_HEATFLUX': {'DESCRIPTION': 'weighted time average derivative '
-                                          'value',
-                           'GROUP': 'TAVG_D_HEAT',
-                           'HEADER': 'dtavg[HF]',
-                           'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_D_VOLUME_FRACTION': {'DESCRIPTION': 'weighted time average derivative '
-                                           'value',
-                            'GROUP': 'TAVG_D_STRUCT_COEFF',
-                            'HEADER': 'dtavg[VolFrac]',
-                            'TYPE': 'TAVG_D_COEFFICIENT'},
- 'TAVG_EFFICIENCY': {'DESCRIPTION': 'weighted time average value',
-                     'GROUP': 'TAVG_AERO_COEFF',
-                     'HEADER': 'tavg[CEff]',
-                     'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_EQUIVALENT_AREA': {'DESCRIPTION': 'weighted time average value',
-                          'GROUP': 'TAVG_EQUIVALENT_AREA',
-                          'HEADER': 'tavg[CEquiv_Area]',
-                          'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_FIGURE_OF_MERIT': {'DESCRIPTION': 'weighted time average value',
-                          'GROUP': 'TAVG_ROTATING_FRAME',
-                          'HEADER': 'tavg[CMerit]',
-                          'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_FORCE_X': {'DESCRIPTION': 'weighted time average value',
-                  'GROUP': 'TAVG_AERO_COEFF',
-                  'HEADER': 'tavg[CFx]',
-                  'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_FORCE_Y': {'DESCRIPTION': 'weighted time average value',
-                  'GROUP': 'TAVG_AERO_COEFF',
-                  'HEADER': 'tavg[CFy]',
-                  'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_FORCE_Z': {'DESCRIPTION': 'weighted time average value',
-                  'GROUP': 'TAVG_AERO_COEFF',
-                  'HEADER': 'tavg[CFz]',
-                  'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_INVERSE_DESIGN_PRESSURE': {'DESCRIPTION': 'weighted time average value',
-                                  'GROUP': 'TAVG_CP_DIFF',
-                                  'HEADER': 'tavg[Cp_Diff]',
-                                  'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_LIFT': {'DESCRIPTION': 'weighted time average value',
-               'GROUP': 'TAVG_AERO_COEFF',
-               'HEADER': 'tavg[CL]',
-               'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_MAXIMUM_HEATFLUX': {'DESCRIPTION': 'weighted time average value',
-                           'GROUP': 'TAVG_HEAT',
-                           'HEADER': 'tavg[MaxHF]',
-                           'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_MOMENT_X': {'DESCRIPTION': 'weighted time average value',
-                   'GROUP': 'TAVG_AERO_COEFF',
-                   'HEADER': 'tavg[CMx]',
-                   'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_MOMENT_Y': {'DESCRIPTION': 'weighted time average value',
-                   'GROUP': 'TAVG_AERO_COEFF',
-                   'HEADER': 'tavg[CMy]',
-                   'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_MOMENT_Z': {'DESCRIPTION': 'weighted time average value',
-                   'GROUP': 'TAVG_AERO_COEFF',
-                   'HEADER': 'tavg[CMz]',
-                   'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_REFERENCE_GEOMETRY': {'DESCRIPTION': 'weighted time average value',
-                             'GROUP': 'TAVG_STRUCT_COEFF',
-                             'HEADER': 'tavg[RefGeom]',
-                             'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_REFERENCE_NODE': {'DESCRIPTION': 'weighted time average value',
-                         'GROUP': 'TAVG_STRUCT_COEFF',
-                         'HEADER': 'tavg[RefNode]',
-                         'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_SENS_AOA': {'DESCRIPTION': 'weighted time average value',
-                   'GROUP': 'TAVG_SENSITIVITY',
-                   'HEADER': 'tavg[Sens_AoA]',
-                   'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_SENS_GEO': {'DESCRIPTION': 'weighted time average value',
-                   'GROUP': 'TAVG_SENSITIVITY',
-                   'HEADER': 'tavg[Sens_Geo]',
-                   'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_SENS_MACH': {'DESCRIPTION': 'weighted time average value',
-                    'GROUP': 'TAVG_SENSITIVITY',
-                    'HEADER': 'tavg[Sens_Mach]',
-                    'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_SENS_PRESS': {'DESCRIPTION': 'weighted time average value',
-                     'GROUP': 'TAVG_SENSITIVITY',
-                     'HEADER': 'tavg[Sens_Press]',
-                     'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_SENS_PRESS_OUT': {'DESCRIPTION': 'weighted time average value',
-                         'GROUP': 'TAVG_SENSITIVITY',
-                         'HEADER': 'tavg[Sens_Pout]',
-                         'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_SENS_TEMP': {'DESCRIPTION': 'weighted time average value',
-                    'GROUP': 'TAVG_SENSITIVITY',
-                    'HEADER': 'tavg[Sens_Temp]',
-                    'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_SENS_VEL_IN': {'DESCRIPTION': 'weighted time average value',
-                      'GROUP': 'TAVG_SENSITIVITY',
-                      'HEADER': 'tavg[Sens_Vin]',
-                      'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_SIDEFORCE': {'DESCRIPTION': 'weighted time average value',
-                    'GROUP': 'TAVG_AERO_COEFF',
-                    'HEADER': 'tavg[CSF]',
-                    'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_STRESS_PENALTY': {'DESCRIPTION': 'weighted time average value',
-                         'GROUP': 'TAVG_STRUCT_COEFF',
-                         'HEADER': 'tavg[StressPen]',
-                         'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_SURFACE_MACH': {'DESCRIPTION': 'weighted time average value',
-                       'GROUP': 'TAVG_FLOW_COEFF',
-                       'HEADER': 'tavg[Avg_Mach]',
-                       'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_SURFACE_MASSFLOW': {'DESCRIPTION': 'weighted time average value',
-                           'GROUP': 'TAVG_FLOW_COEFF',
-                           'HEADER': 'tavg[Avg_Massflow]',
-                           'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_SURFACE_MOM_DISTORTION': {'DESCRIPTION': 'weighted time average value',
-                                 'GROUP': 'TAVG_FLOW_COEFF',
-                                 'HEADER': 'tavg[Momentum_Distortion]',
-                                 'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_SURFACE_PRESSURE_DROP': {'DESCRIPTION': 'weighted time average value',
-                                'GROUP': 'TAVG_FLOW_COEFF',
-                                'HEADER': 'tavg[Pressure_Drop]',
-                                'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_SURFACE_SECONDARY': {'DESCRIPTION': 'weighted time average value',
-                            'GROUP': 'TAVG_FLOW_COEFF',
-                            'HEADER': 'tavg[Secondary_Strength]',
-                            'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_SURFACE_SECOND_OVER_UNIFORM': {'DESCRIPTION': 'weighted time average '
-                                                     'value',
-                                      'GROUP': 'TAVG_FLOW_COEFF',
-                                      'HEADER': 'tavg[Secondary_Over_Uniformity]',
-                                      'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_SURFACE_SPECIES_" + std::to_string(iVar': {'DESCRIPTION': 'weighted '
-                                                                 'time average '
-                                                                 'value',
-                                                  'GROUP': 'TAVG_SPECIES_COEFF',
-                                                  'HEADER': 'tavg[Avg_Species_" '
-                                                            '+ '
-                                                            'std::to_string(iVar]',
-                                                  'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_SURFACE_STATIC_PRESSURE': {'DESCRIPTION': 'weighted time average value',
-                                  'GROUP': 'TAVG_FLOW_COEFF',
-                                  'HEADER': 'tavg[Avg_Press]',
-                                  'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_SURFACE_STATIC_TEMPERATURE': {'DESCRIPTION': 'weighted time average '
-                                                    'value',
-                                     'GROUP': 'TAVG_FLOW_COEFF',
-                                     'HEADER': 'tavg[Avg_Temp]',
-                                     'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_SURFACE_TOTAL_PRESSURE': {'DESCRIPTION': 'weighted time average value',
-                                 'GROUP': 'TAVG_FLOW_COEFF',
-                                 'HEADER': 'tavg[Avg_TotalPress]',
-                                 'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_SURFACE_TOTAL_TEMPERATURE': {'DESCRIPTION': 'weighted time average '
-                                                   'value',
-                                    'GROUP': 'TAVG_FLOW_COEFF',
-                                    'HEADER': 'tavg[Avg_TotalTemp]',
-                                    'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_SURFACE_UNIFORMITY': {'DESCRIPTION': 'weighted time average value',
-                             'GROUP': 'TAVG_FLOW_COEFF',
-                             'HEADER': 'tavg[Uniformity]',
-                             'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_THRUST': {'DESCRIPTION': 'weighted time average value',
-                 'GROUP': 'TAVG_ROTATING_FRAME',
-                 'HEADER': 'tavg[CT]',
-                 'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_TOPOL_COMPLIANCE': {'DESCRIPTION': 'weighted time average value',
-                           'GROUP': 'TAVG_STRUCT_COEFF',
-                           'HEADER': 'tavg[TopComp]',
-                           'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_TOPOL_DISCRETENESS': {'DESCRIPTION': 'weighted time average value',
-                             'GROUP': 'TAVG_STRUCT_COEFF',
-                             'HEADER': 'tavg[TopDisc]',
-                             'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_TORQUE': {'DESCRIPTION': 'weighted time average value',
-                 'GROUP': 'TAVG_ROTATING_FRAME',
-                 'HEADER': 'tavg[CQ]',
-                 'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_TOTAL_HEATFLUX': {'DESCRIPTION': 'weighted time average value',
-                         'GROUP': 'TAVG_HEAT',
-                         'HEADER': 'tavg[HF]',
-                         'TYPE': 'TAVG_COEFFICIENT'},
- 'TAVG_VOLUME_FRACTION': {'DESCRIPTION': 'weighted time average value',
-                          'GROUP': 'TAVG_STRUCT_COEFF',
-                          'HEADER': 'tavg[VolFrac]',
-                          'TYPE': 'TAVG_COEFFICIENT'},
- 'THRUST': {'DESCRIPTION': 'Thrust coefficient',
-            'GROUP': 'ROTATING_FRAME',
-            'HEADER': 'CT',
-            'TYPE': 'COEFFICIENT'},
- 'TOPOL_COMPLIANCE': {'DESCRIPTION': 'Structural compliance',
-                      'GROUP': 'STRUCT_COEFF',
-                      'HEADER': 'TopComp',
-                      'TYPE': 'COEFFICIENT'},
- 'TOPOL_DISCRETENESS': {'DESCRIPTION': 'Discreteness of the material '
-                                       'distribution',
-                        'GROUP': 'STRUCT_COEFF',
-                        'HEADER': 'TopDisc',
-                        'TYPE': 'COEFFICIENT'},
- 'TORQUE': {'DESCRIPTION': 'Torque coefficient',
-            'GROUP': 'ROTATING_FRAME',
-            'HEADER': 'CQ',
-            'TYPE': 'COEFFICIENT'},
- 'TOTAL_HEATFLUX': {'DESCRIPTION': 'Total heatflux on all surfaces defined in '
-                                   'MARKER_MONITORING',
-                    'GROUP': 'HEAT',
-                    'HEADER': 'HF',
-                    'TYPE': 'COEFFICIENT'},
- 'VMS': {'DESCRIPTION': 'VMS',
-         'GROUP': 'Maximum Von-Misses stress',
-         'HEADER': 'VonMises',
-         'TYPE': 'DEFAULT'},
- 'VOLUME_FRACTION': {'DESCRIPTION': 'Fraction of solid material',
-                     'GROUP': 'STRUCT_COEFF',
-                     'HEADER': 'VolFrac',
-                     'TYPE': 'COEFFICIENT'}}
+history_header_map = {
+    "ADJOINT_DISP_X": {
+        "DESCRIPTION": "Root-mean square residual of the adjoint "
+        "of the X displacements.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[Ux_adj]",
+        "TYPE": "RESIDUAL",
+    },
+    "ADJOINT_DISP_Y": {
+        "DESCRIPTION": "Root-mean square residual of the adjoint "
+        "of the Y displacements.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[Uy_adj]",
+        "TYPE": "RESIDUAL",
+    },
+    "ADJOINT_DISP_Z": {
+        "DESCRIPTION": "Root-mean square residual of the adjoint "
+        "of the Z displacements.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[Uz_adj]",
+        "TYPE": "RESIDUAL",
+    },
+    "ADJOINT_SOLEXTRA": {
+        "DESCRIPTION": "Adjoint value of the first extra " "Solution.",
+        "GROUP": "ADJOINT_SOLEXTRA",
+        "HEADER": "Adjoint_SolExtra",
+        "TYPE": "COEFFICIENT",
+    },
+    "AOA": {
+        "DESCRIPTION": "Angle of attack",
+        "GROUP": "AOA",
+        "HEADER": "AoA",
+        "TYPE": "DEFAULT",
+    },
+    "AVG_CFL": {
+        "DESCRIPTION": "Current average of the local CFL numbers",
+        "GROUP": "CFL_NUMBER",
+        "HEADER": "Avg CFL",
+        "TYPE": "DEFAULT",
+    },
+    "AVG_DENSITY": {
+        "DESCRIPTION": "Total average density on all markers set in " "MARKER_ANALYZE",
+        "GROUP": "FLOW_COEFF",
+        "HEADER": "Avg_Density",
+        "TYPE": "COEFFICIENT",
+    },
+    "AVG_ENTHALPY": {
+        "DESCRIPTION": "Total average enthalpy on all markers set in " "MARKER_ANALYZE",
+        "GROUP": "FLOW_COEFF",
+        "HEADER": "Avg_Enthalpy",
+        "TYPE": "COEFFICIENT",
+    },
+    "AVG_NORMALVEL": {
+        "DESCRIPTION": "Total average normal velocity on all "
+        "markers set in MARKER_ANALYZE",
+        "GROUP": "FLOW_COEFF",
+        "HEADER": "Avg_NormalVel",
+        "TYPE": "COEFFICIENT",
+    },
+    "AVG_TEMPERATURE": {
+        "DESCRIPTION": "Average temperature on all surfaces "
+        "defined in MARKER_MONITORING",
+        "GROUP": "HEAT",
+        "HEADER": "AvgTemp",
+        "TYPE": "COEFFICIENT",
+    },
+    "BGS_ADJ_DENSITY": {
+        "DESCRIPTION": "BGS residual of the adjoint density.",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[A_Rho]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_ADJ_DISP_X": {
+        "DESCRIPTION": "BGS residual of the adjoint X " "displacement.",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[A_Ux]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_ADJ_DISP_Y": {
+        "DESCRIPTION": "BGS residual of the adjoint Y " "displacement.",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[A_Uy]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_ADJ_DISP_Z": {
+        "DESCRIPTION": "BGS residual of the adjoint Z " "displacement.",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[A_Uz]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_ADJ_DISSIPATION": {
+        "DESCRIPTION": "BGS residual of the adjoint " "dissipation.",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[A_w]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_ADJ_ENERGY": {
+        "DESCRIPTION": "BGS residual of the adjoint energy.",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[A_E]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_ADJ_MOMENTUM-X": {
+        "DESCRIPTION": "BGS residual of the adjoint momentum " "x-component",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[A_RhoU]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_ADJ_MOMENTUM-Y": {
+        "DESCRIPTION": "BGS residual of the adjoint momentum " "y-component",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[A_RhoV]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_ADJ_MOMENTUM-Z": {
+        "DESCRIPTION": "BGS residual of the adjoint momentum " "z-component",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[A_RhoW]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_ADJ_NU_TILDE": {
+        "DESCRIPTION": "BGS residual of the adjoint nu tilde.",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[A_nu]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_ADJ_PRESSURE": {
+        "DESCRIPTION": "BGS residual of the adjoint Pressure.",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[A_Rho]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_ADJ_RAD_ENERGY": {
+        "DESCRIPTION": "BGS residual  of the P1 radiative " "energy.",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[A_P1]",
+        "TYPE": "RESIDUAL",
+    },
+    'BGS_ADJ_SPECIES_" + std::to_string(iVar': {
+        "DESCRIPTION": "BGS residual of " "the adjoint " "transported " "species.",
+        "GROUP": "BGS_RES",
+        "HEADER": 'bgs[A_rho*Y_" + ' "std::to_string(iVar) + " '"]',
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_ADJ_TEMPERATURE": {
+        "DESCRIPTION": "BGS residual of the adjoint " "temperature.",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[A_T]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_ADJ_TKE": {
+        "DESCRIPTION": "BGS residual of the adjoint kinetic energy.",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[A_k]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_ADJ_VELOCITY-X": {
+        "DESCRIPTION": "BGS residual of the adjoint Velocity " "x-component",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[A_RhoU]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_ADJ_VELOCITY-Y": {
+        "DESCRIPTION": "BGS residual of the adjoint Velocity " "y-component",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[A_RhoV]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_ADJ_VELOCITY-Z": {
+        "DESCRIPTION": "BGS residual of the adjoint Velocity " "z-component",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[A_RhoW]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_DENSITY": {
+        "DESCRIPTION": "BGS residual of the density.",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[Rho]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_DISP_X": {
+        "DESCRIPTION": "BGS residual of X displacement",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[DispX]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_DISP_Y": {
+        "DESCRIPTION": "BGS residual of Y displacement",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[DispY]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_DISP_Z": {
+        "DESCRIPTION": "BGS residual of Z displacement",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[DispZ]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_DISSIPATION": {
+        "DESCRIPTION": "BGS residual of dissipation (SST model).",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[w]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_ENERGY": {
+        "DESCRIPTION": "BGS residual of the energy.",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[RhoE]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_MOMENTUM-X": {
+        "DESCRIPTION": "BGS residual of the momentum x-component.",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[RhoU]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_MOMENTUM-Y": {
+        "DESCRIPTION": "BGS residual of the momentum y-component.",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[RhoV]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_NU_TILDE": {
+        "DESCRIPTION": "BGS residual of nu tilde (SA model).",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[nu]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_PRESSURE": {
+        "DESCRIPTION": "BGS residual of the pressure.",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[P]",
+        "TYPE": "RESIDUAL",
+    },
+    'BGS_SPECIES_" + std::to_string(iVar': {
+        "DESCRIPTION": "BGS residual of " "transported species.",
+        "GROUP": "BGS_RES",
+        "HEADER": 'bgs[rho*Y_" + ' 'std::to_string(iVar)+"]',
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_TEMPERATURE": {
+        "DESCRIPTION": "Block-Gauss-Seidel residual of the " "temperature",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[T]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_TKE": {
+        "DESCRIPTION": "BGS residual of kinetic energy (SST model).",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[k]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_VELOCITY-X": {
+        "DESCRIPTION": "BGS residual of the velocity x-component.",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[U]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_VELOCITY-Y": {
+        "DESCRIPTION": "BGS residual of the velocity y-component.",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[V]",
+        "TYPE": "RESIDUAL",
+    },
+    "BGS_VELOCITY-Z": {
+        "DESCRIPTION": "BGS residual of the velocity z-component.",
+        "GROUP": "BGS_RES",
+        "HEADER": "bgs[W]",
+        "TYPE": "RESIDUAL",
+    },
+    "BUFFET": {
+        "DESCRIPTION": "Buffet sensor",
+        "GROUP": "AERO_COEFF",
+        "HEADER": "Buffet",
+        "TYPE": "COEFFICIENT",
+    },
+    "CFL_NUMBER": {
+        "DESCRIPTION": "Current value of the CFL number",
+        "GROUP": "CFL_NUMBER",
+        "HEADER": "CFL number",
+        "TYPE": "DEFAULT",
+    },
+    "CHANGE_IN_AOA": {
+        "DESCRIPTION": "Last change in Angle of Attack by Fixed CL " "Driver",
+        "GROUP": "FIXED_CL",
+        "HEADER": "Change_in_AOA",
+        "TYPE": "RESIDUAL",
+    },
+    "CL_DRIVER_COMMAND": {
+        "DESCRIPTION": "CL Driver's control command",
+        "GROUP": "FIXED_CL",
+        "HEADER": "CL_Driver_Command",
+        "TYPE": "RESIDUAL",
+    },
+    "COMBO": {
+        "DESCRIPTION": "Combined obj. function value.",
+        "GROUP": "COMBO",
+        "HEADER": "ComboObj",
+        "TYPE": "COEFFICIENT",
+    },
+    "DEFORM_ITER": {
+        "DESCRIPTION": "Linear solver iterations for the mesh " "deformation",
+        "GROUP": "DEFORM",
+        "HEADER": "DeformIter",
+        "TYPE": "DEFAULT",
+    },
+    "DEFORM_MAX_VOLUME": {
+        "DESCRIPTION": "Maximum volume in the mesh",
+        "GROUP": "DEFORM",
+        "HEADER": "MaxVolume",
+        "TYPE": "DEFAULT",
+    },
+    "DEFORM_MIN_VOLUME": {
+        "DESCRIPTION": "Minimum volume in the mesh",
+        "GROUP": "DEFORM",
+        "HEADER": "MinVolume",
+        "TYPE": "DEFAULT",
+    },
+    "DEFORM_RESIDUAL": {
+        "DESCRIPTION": "Residual of the linear solver for the " "mesh deformation",
+        "GROUP": "DEFORM",
+        "HEADER": "DeformRes",
+        "TYPE": "DEFAULT",
+    },
+    "DELTA_CL": {
+        "DESCRIPTION": "Difference between Target CL and current CL",
+        "GROUP": "FIXED_CL",
+        "HEADER": "Delta_CL",
+        "TYPE": "COEFFICIENT",
+    },
+    "DRAG": {
+        "DESCRIPTION": "Total drag coefficient on all surfaces set with "
+        "MARKER_MONITORING",
+        "GROUP": "AERO_COEFF",
+        "HEADER": "CD",
+        "TYPE": "COEFFICIENT",
+    },
+    "D_ADJOINT_SOLEXTRA": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_ADJOINT_SOLEXTRA",
+        "HEADER": "d[Adjoint_SolExtra]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_AVG_DENSITY": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_FLOW_COEFF",
+        "HEADER": "d[Avg_Density]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_AVG_ENTHALPY": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_FLOW_COEFF",
+        "HEADER": "d[Avg_Enthalpy]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_AVG_NORMALVEL": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_FLOW_COEFF",
+        "HEADER": "d[Avg_NormalVel]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_AVG_TEMPERATURE": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_HEAT",
+        "HEADER": "d[AvgTemp]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_BUFFET": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_AERO_COEFF",
+        "HEADER": "d[Buffet]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_COMBO": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_COMBO",
+        "HEADER": "d[ComboObj]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_DELTA_CL": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_FIXED_CL",
+        "HEADER": "d[Delta_CL]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_DRAG": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_AERO_COEFF",
+        "HEADER": "d[CD]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_EFFICIENCY": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_AERO_COEFF",
+        "HEADER": "d[CEff]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_EQUIVALENT_AREA": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_EQUIVALENT_AREA",
+        "HEADER": "d[CEquiv_Area]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_FIGURE_OF_MERIT": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_ROTATING_FRAME",
+        "HEADER": "d[CMerit]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_FORCE_X": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_AERO_COEFF",
+        "HEADER": "d[CFx]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_FORCE_Y": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_AERO_COEFF",
+        "HEADER": "d[CFy]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_FORCE_Z": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_AERO_COEFF",
+        "HEADER": "d[CFz]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_INVERSE_DESIGN_PRESSURE": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_CP_DIFF",
+        "HEADER": "d[Cp_Diff]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_LIFT": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_AERO_COEFF",
+        "HEADER": "d[CL]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_MAXIMUM_HEATFLUX": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_HEAT",
+        "HEADER": "d[MaxHF]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_MOMENT_X": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_AERO_COEFF",
+        "HEADER": "d[CMx]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_MOMENT_Y": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_AERO_COEFF",
+        "HEADER": "d[CMy]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_MOMENT_Z": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_AERO_COEFF",
+        "HEADER": "d[CMz]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_REFERENCE_GEOMETRY": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_STRUCT_COEFF",
+        "HEADER": "d[RefGeom]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_REFERENCE_NODE": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_STRUCT_COEFF",
+        "HEADER": "d[RefNode]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_SENS_AOA": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_SENSITIVITY",
+        "HEADER": "d[Sens_AoA]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_SENS_GEO": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_SENSITIVITY",
+        "HEADER": "d[Sens_Geo]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_SENS_MACH": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_SENSITIVITY",
+        "HEADER": "d[Sens_Mach]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_SENS_PRESS": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_SENSITIVITY",
+        "HEADER": "d[Sens_Press]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_SENS_PRESS_OUT": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_SENSITIVITY",
+        "HEADER": "d[Sens_Pout]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_SENS_TEMP": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_SENSITIVITY",
+        "HEADER": "d[Sens_Temp]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_SENS_VEL_IN": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_SENSITIVITY",
+        "HEADER": "d[Sens_Vin]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_SIDEFORCE": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_AERO_COEFF",
+        "HEADER": "d[CSF]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_STRESS_PENALTY": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_STRUCT_COEFF",
+        "HEADER": "d[StressPen]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_SURFACE_MACH": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_FLOW_COEFF",
+        "HEADER": "d[Avg_Mach]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_SURFACE_MASSFLOW": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_FLOW_COEFF",
+        "HEADER": "d[Avg_Massflow]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_SURFACE_MOM_DISTORTION": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_FLOW_COEFF",
+        "HEADER": "d[Momentum_Distortion]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_SURFACE_PRESSURE_DROP": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_FLOW_COEFF",
+        "HEADER": "d[Pressure_Drop]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_SURFACE_SECONDARY": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_FLOW_COEFF",
+        "HEADER": "d[Secondary_Strength]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_SURFACE_SECOND_OVER_UNIFORM": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_FLOW_COEFF",
+        "HEADER": "d[Secondary_Over_Uniformity]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    'D_SURFACE_SPECIES_" + std::to_string(iVar': {
+        "DESCRIPTION": "Derivative " "value",
+        "GROUP": "D_SPECIES_COEFF",
+        "HEADER": 'd[Avg_Species_" + ' "std::to_string(iVar]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_SURFACE_STATIC_PRESSURE": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_FLOW_COEFF",
+        "HEADER": "d[Avg_Press]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_SURFACE_STATIC_TEMPERATURE": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_FLOW_COEFF",
+        "HEADER": "d[Avg_Temp]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_SURFACE_TOTAL_PRESSURE": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_FLOW_COEFF",
+        "HEADER": "d[Avg_TotalPress]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_SURFACE_TOTAL_TEMPERATURE": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_FLOW_COEFF",
+        "HEADER": "d[Avg_TotalTemp]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_SURFACE_UNIFORMITY": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_FLOW_COEFF",
+        "HEADER": "d[Uniformity]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_THRUST": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_ROTATING_FRAME",
+        "HEADER": "d[CT]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_TOPOL_COMPLIANCE": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_STRUCT_COEFF",
+        "HEADER": "d[TopComp]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_TOPOL_DISCRETENESS": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_STRUCT_COEFF",
+        "HEADER": "d[TopDisc]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_TORQUE": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_ROTATING_FRAME",
+        "HEADER": "d[CQ]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_TOTAL_HEATFLUX": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_HEAT",
+        "HEADER": "d[HF]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "D_VOLUME_FRACTION": {
+        "DESCRIPTION": "Derivative value",
+        "GROUP": "D_STRUCT_COEFF",
+        "HEADER": "d[VolFrac]",
+        "TYPE": "D_COEFFICIENT",
+    },
+    "EFFICIENCY": {
+        "DESCRIPTION": "Total lift-to-drag ratio on all surfaces set "
+        "with MARKER_MONITORING",
+        "GROUP": "AERO_COEFF",
+        "HEADER": "CEff",
+        "TYPE": "COEFFICIENT",
+    },
+    "EQUIVALENT_AREA": {
+        "DESCRIPTION": "Equivalent area",
+        "GROUP": "EQUIVALENT_AREA",
+        "HEADER": "CEquiv_Area",
+        "TYPE": "COEFFICIENT",
+    },
+    "FIGURE_OF_MERIT": {
+        "DESCRIPTION": "Thrust over torque",
+        "GROUP": "ROTATING_FRAME",
+        "HEADER": "CMerit",
+        "TYPE": "COEFFICIENT",
+    },
+    "FORCE_X": {
+        "DESCRIPTION": "Total force x-component on all surfaces set with "
+        "MARKER_MONITORING",
+        "GROUP": "AERO_COEFF",
+        "HEADER": "CFx",
+        "TYPE": "COEFFICIENT",
+    },
+    "FORCE_Y": {
+        "DESCRIPTION": "Total force y-component on all surfaces set with "
+        "MARKER_MONITORING",
+        "GROUP": "AERO_COEFF",
+        "HEADER": "CFy",
+        "TYPE": "COEFFICIENT",
+    },
+    "FORCE_Z": {
+        "DESCRIPTION": "Total force z-component on all surfaces set with "
+        "MARKER_MONITORING",
+        "GROUP": "AERO_COEFF",
+        "HEADER": "CFz",
+        "TYPE": "COEFFICIENT",
+    },
+    "INVERSE_DESIGN_PRESSURE": {
+        "DESCRIPTION": "Cp difference for inverse design",
+        "GROUP": "CP_DIFF",
+        "HEADER": "Cp_Diff",
+        "TYPE": "COEFFICIENT",
+    },
+    "LIFT": {
+        "DESCRIPTION": "Total lift coefficient on all surfaces set with "
+        "MARKER_MONITORING",
+        "GROUP": "AERO_COEFF",
+        "HEADER": "CL",
+        "TYPE": "COEFFICIENT",
+    },
+    "LINSOL_ITER": {
+        "DESCRIPTION": "Number of iterations of the linear solver.",
+        "GROUP": "LINSOL",
+        "HEADER": "LinSolIter",
+        "TYPE": "DEFAULT",
+    },
+    "LINSOL_ITER_SPECIES": {
+        "DESCRIPTION": "Number of iterations of the linear "
+        "solver for species solver.",
+        "GROUP": "LINSOL",
+        "HEADER": "LinSolIterSpecies",
+        "TYPE": "DEFAULT",
+    },
+    "LINSOL_ITER_TURB": {
+        "DESCRIPTION": "Number of iterations of the linear " "solver for turbulence.",
+        "GROUP": "LINSOL",
+        "HEADER": "LinSolIterTurb",
+        "TYPE": "DEFAULT",
+    },
+    "LINSOL_RESIDUAL": {
+        "DESCRIPTION": "Residual of the linear solver.",
+        "GROUP": "LINSOL",
+        "HEADER": "LinSolRes",
+        "TYPE": "DEFAULT",
+    },
+    "LINSOL_RESIDUAL_SPECIES": {
+        "DESCRIPTION": "Residual of the linear solver for " "species solver.",
+        "GROUP": "LINSOL",
+        "HEADER": "LinSolResSpecies",
+        "TYPE": "DEFAULT",
+    },
+    "LINSOL_RESIDUAL_TURB": {
+        "DESCRIPTION": "Residual of the linear solver for " "turbulence.",
+        "GROUP": "LINSOL",
+        "HEADER": "LinSolResTurb",
+        "TYPE": "DEFAULT",
+    },
+    "LOAD_INCREMENT": {
+        "DESCRIPTION": "LOAD_INCREMENT",
+        "GROUP": "Percent of total load (incremental",
+        "HEADER": "Load[%]",
+        "TYPE": "DEFAULT",
+    },
+    "LOAD_RAMP": {
+        "DESCRIPTION": "LOAD_RAMP",
+        "GROUP": "Fraction of total load (ramped",
+        "HEADER": "Load_Ramp",
+        "TYPE": "DEFAULT",
+    },
+    "MAXIMUM_HEATFLUX": {
+        "DESCRIPTION": "Maximum heatflux on all surfaces defined "
+        "in MARKER_MONITORING",
+        "GROUP": "HEAT",
+        "HEADER": "MaxHF",
+        "TYPE": "COEFFICIENT",
+    },
+    "MAX_ADJ_DENSITY": {
+        "DESCRIPTION": "Maximum residual of the adjoint density.",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[A_Rho]",
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_ADJ_DISSIPATION": {
+        "DESCRIPTION": "Maximum residual of the adjoint " "dissipation.",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[A_w]",
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_ADJ_ENERGY": {
+        "DESCRIPTION": "Maximum residual of the adjoint energy.",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[A_E]",
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_ADJ_MOMENTUM-X": {
+        "DESCRIPTION": "Maximum residual of the adjoint " "momentum x-component",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[A_RhoU]",
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_ADJ_MOMENTUM-Y": {
+        "DESCRIPTION": "Maximum residual of the adjoint " "momentum y-component",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[A_RhoV]",
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_ADJ_MOMENTUM-Z": {
+        "DESCRIPTION": "Maximum residual of the adjoint " "momentum z-component",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[A_RhoW]",
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_ADJ_NU_TILDE": {
+        "DESCRIPTION": "Maximum residual of the adjoint nu " "tilde.",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[A_nu]",
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_ADJ_PRESSURE": {
+        "DESCRIPTION": "Maximum residual of the adjoint " "Pressure.",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[A_Rho]",
+        "TYPE": "RESIDUAL",
+    },
+    'MAX_ADJ_SPECIES_" + std::to_string(iVar': {
+        "DESCRIPTION": "Maximum residual " "of the adjoint " "transported " "species.",
+        "GROUP": "MAX_RES",
+        "HEADER": 'max[A_rho*Y_" + ' "std::to_string(iVar) + " '"]',
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_ADJ_TEMPERATURE": {
+        "DESCRIPTION": "Maximum residual of the temperature.",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[A_T]",
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_ADJ_TKE": {
+        "DESCRIPTION": "Maximum residual of the adjoint kinetic " "energy.",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[A_k]",
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_ADJ_VELOCITY-X": {
+        "DESCRIPTION": "Maximum residual of the adjoint " "Velocity x-component",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[A_RhoU]",
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_ADJ_VELOCITY-Y": {
+        "DESCRIPTION": "Maximum residual of the adjoint " "Velocity y-component",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[A_RhoV]",
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_ADJ_VELOCITY-Z": {
+        "DESCRIPTION": "Maximum residual of the adjoint " "Velocity z-component",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[A_RhoW]",
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_CFL": {
+        "DESCRIPTION": "Current maximum of the local CFL numbers",
+        "GROUP": "CFL_NUMBER",
+        "HEADER": "Max CFL",
+        "TYPE": "DEFAULT",
+    },
+    "MAX_DELTA_TIME": {
+        "DESCRIPTION": "Current maximum local time step",
+        "GROUP": "CFL_NUMBER",
+        "HEADER": "Max DT",
+        "TYPE": "DEFAULT",
+    },
+    "MAX_DENSITY": {
+        "DESCRIPTION": "Maximum square residual of the density.",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[Rho]",
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_DISSIPATION": {
+        "DESCRIPTION": "Maximum residual of dissipation (SST " "model).",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[w]",
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_ENERGY": {
+        "DESCRIPTION": "Maximum residual of the energy.",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[RhoE]",
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_MOMENTUM-X": {
+        "DESCRIPTION": "Maximum square residual of the momentum " "x-component.",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[RhoU]",
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_MOMENTUM-Y": {
+        "DESCRIPTION": "Maximum square residual of the momentum " "y-component.",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[RhoV]",
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_NU_TILDE": {
+        "DESCRIPTION": "Maximum residual of nu tilde (SA model).",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[nu]",
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_PRESSURE": {
+        "DESCRIPTION": "Maximum residual of the pressure.",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[P]",
+        "TYPE": "RESIDUAL",
+    },
+    'MAX_SPECIES_" + std::to_string(iVar': {
+        "DESCRIPTION": "Maximum residual of " "transported species.",
+        "GROUP": "MAX_RES",
+        "HEADER": 'max[rho*Y_" + ' 'std::to_string(iVar)+"]',
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_TEMPERATURE": {
+        "DESCRIPTION": "Maximum residual of the temperature",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[T]",
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_TKE": {
+        "DESCRIPTION": "Maximum residual of kinetic energy (SST model).",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[k]",
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_VELOCITY-X": {
+        "DESCRIPTION": "Maximum residual of the velocity " "x-component.",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[U]",
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_VELOCITY-Y": {
+        "DESCRIPTION": "Maximum residual of the velocity " "y-component.",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[V]",
+        "TYPE": "RESIDUAL",
+    },
+    "MAX_VELOCITY-Z": {
+        "DESCRIPTION": "Maximum residual of the velocity " "z-component.",
+        "GROUP": "MAX_RES",
+        "HEADER": "max[W]",
+        "TYPE": "RESIDUAL",
+    },
+    "MIN_CFL": {
+        "DESCRIPTION": "Current minimum of the local CFL numbers",
+        "GROUP": "CFL_NUMBER",
+        "HEADER": "Min CFL",
+        "TYPE": "DEFAULT",
+    },
+    "MIN_DELTA_TIME": {
+        "DESCRIPTION": "Current minimum local time step",
+        "GROUP": "CFL_NUMBER",
+        "HEADER": "Min DT",
+        "TYPE": "DEFAULT",
+    },
+    "MOMENT_X": {
+        "DESCRIPTION": "Total momentum x-component on all surfaces set "
+        "with MARKER_MONITORING",
+        "GROUP": "AERO_COEFF",
+        "HEADER": "CMx",
+        "TYPE": "COEFFICIENT",
+    },
+    "MOMENT_Y": {
+        "DESCRIPTION": "Total momentum y-component on all surfaces set "
+        "with MARKER_MONITORING",
+        "GROUP": "AERO_COEFF",
+        "HEADER": "CMy",
+        "TYPE": "COEFFICIENT",
+    },
+    "MOMENT_Z": {
+        "DESCRIPTION": "Total momentum z-component on all surfaces set "
+        "with MARKER_MONITORING",
+        "GROUP": "AERO_COEFF",
+        "HEADER": "CMz",
+        "TYPE": "COEFFICIENT",
+    },
+    "PREV_AOA": {
+        "DESCRIPTION": "Angle of Attack at the previous iteration of the "
+        "Fixed CL driver",
+        "GROUP": "FIXED_CL",
+        "HEADER": "Previous_AOA",
+        "TYPE": "DEFAULT",
+    },
+    "REFERENCE_GEOMETRY": {
+        "DESCRIPTION": "L2 norm of difference wrt reference " "geometry",
+        "GROUP": "STRUCT_COEFF",
+        "HEADER": "RefGeom",
+        "TYPE": "COEFFICIENT",
+    },
+    "REFERENCE_NODE": {
+        "DESCRIPTION": "Distance to reference node",
+        "GROUP": "STRUCT_COEFF",
+        "HEADER": "RefNode",
+        "TYPE": "COEFFICIENT",
+    },
+    "RMS_ADJ_DENSITY": {
+        "DESCRIPTION": "Root-mean square residual of the adjoint " "density.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[A_Rho]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_ADJ_DISSIPATION": {
+        "DESCRIPTION": "Root-mean square residual of the " "adjoint dissipation.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[A_w]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_ADJ_ENERGY": {
+        "DESCRIPTION": "Root-mean square residual of the adjoint " "energy.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[A_E]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_ADJ_MOMENTUM-X": {
+        "DESCRIPTION": "Root-mean square residual of the "
+        "adjoint momentum x-component.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[A_RhoU]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_ADJ_MOMENTUM-Y": {
+        "DESCRIPTION": "Root-mean square residual of the "
+        "adjoint momentum y-component.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[A_RhoV]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_ADJ_MOMENTUM-Z": {
+        "DESCRIPTION": "Root-mean square residual of the "
+        "adjoint momentum z-component.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[A_RhoW]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_ADJ_NU_TILDE": {
+        "DESCRIPTION": "Root-mean square residual of the adjoint " "nu tilde.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[A_nu]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_ADJ_PRESSURE": {
+        "DESCRIPTION": "Root-mean square residual of the adjoint " "Pressure.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[A_P]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_ADJ_RAD_ENERGY": {
+        "DESCRIPTION": "Root-mean square residual of the P1 " "radiative energy.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[A_P1]",
+        "TYPE": "RESIDUAL",
+    },
+    'RMS_ADJ_SPECIES_" + std::to_string(iVar': {
+        "DESCRIPTION": "Root-mean square "
+        "residual of the "
+        "adjoint "
+        "transported "
+        "species.",
+        "GROUP": "RMS_RES",
+        "HEADER": 'rms[A_rho*Y_" + ' "std::to_string(iVar) + " '"]',
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_ADJ_TEMPERATURE": {
+        "DESCRIPTION": "Root-mean square residual of the " "adjoint temperature.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[A_T]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_ADJ_TKE": {
+        "DESCRIPTION": "Root-mean square residual of the adjoint " "kinetic energy.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[A_k]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_ADJ_VELOCITY-X": {
+        "DESCRIPTION": "Root-mean square residual of the "
+        "adjoint Velocity x-component.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[A_U]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_ADJ_VELOCITY-Y": {
+        "DESCRIPTION": "Root-mean square residual of the "
+        "adjoint Velocity y-component.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[A_V]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_ADJ_VELOCITY-Z": {
+        "DESCRIPTION": "Root-mean square residual of the "
+        "adjoint Velocity z-component.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[A_W]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_DENSITY": {
+        "DESCRIPTION": "Root-mean square residual of the density.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[Rho]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_DISP_X": {
+        "DESCRIPTION": "Residual of X displacement",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[DispX]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_DISP_Y": {
+        "DESCRIPTION": "Residual of Y displacement",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[DispY]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_DISP_Z": {
+        "DESCRIPTION": "Residual of Z displacement",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[DispZ]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_DISSIPATION": {
+        "DESCRIPTION": "Root-mean square residual of dissipation " "(SST model).",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[w]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_ENERGY": {
+        "DESCRIPTION": "Root-mean square residual of the energy.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[RhoE]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_ETOL": {
+        "DESCRIPTION": "Norm of energy/work increment",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[E]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_MOMENTUM-X": {
+        "DESCRIPTION": "Root-mean square residual of the momentum " "x-component.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[RhoU]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_MOMENTUM-Y": {
+        "DESCRIPTION": "Root-mean square residual of the momentum " "y-component.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[RhoV]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_NU_TILDE": {
+        "DESCRIPTION": "Root-mean square residual of nu tilde (SA " "model).",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[nu]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_PRESSURE": {
+        "DESCRIPTION": "Root-mean square residual of the pressure.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[P]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_RTOL": {
+        "DESCRIPTION": "Norm of residual",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[R]",
+        "TYPE": "RESIDUAL",
+    },
+    'RMS_SPECIES_" + std::to_string(iVar': {
+        "DESCRIPTION": "Root-mean square " "residual of " "transported species.",
+        "GROUP": "RMS_RES",
+        "HEADER": 'rms[rho*Y_" + ' 'std::to_string(iVar)+"]',
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_TEMPERATURE": {
+        "DESCRIPTION": "Root mean square residual of the " "temperature",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[T]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_TKE": {
+        "DESCRIPTION": "Root-mean square residual of kinetic energy (SST " "model).",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[k]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_UTOL": {
+        "DESCRIPTION": "Norm of displacement increment",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[U]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_VELOCITY-X": {
+        "DESCRIPTION": "Root-mean square residual of the velocity " "x-component.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[U]",
+        "TYPE": "RESIDUAL",
+    },
+    "RMS_VELOCITY-Y": {
+        "DESCRIPTION": "Root-mean square residual of the velocity " "y-component.",
+        "GROUP": "RMS_RES",
+        "HEADER": "rms[V]",
+        "TYPE": "RESIDUAL",
+    },
+    "SENS_AOA": {
+        "DESCRIPTION": "Sensitivity of the objective function with "
+        "respect to the angle of attack (only for "
+        "compressible solver).",
+        "GROUP": "SENSITIVITY",
+        "HEADER": "Sens_AoA",
+        "TYPE": "COEFFICIENT",
+    },
+    "SENS_E": {
+        "DESCRIPTION": "d Objective / d Elasticity modulus",
+        "GROUP": "SENSITIVITY",
+        "HEADER": "Sens[E]",
+        "TYPE": "DEFAULT",
+    },
+    "SENS_GEO": {
+        "DESCRIPTION": "Sum of the geometrical sensitivities on all "
+        "markers set in MARKER_MONITORING.",
+        "GROUP": "SENSITIVITY",
+        "HEADER": "Sens_Geo",
+        "TYPE": "COEFFICIENT",
+    },
+    "SENS_MACH": {
+        "DESCRIPTION": "Sensitivity of the objective function with "
+        "respect to the Mach number (only of "
+        "compressible solver).",
+        "GROUP": "SENSITIVITY",
+        "HEADER": "Sens_Mach",
+        "TYPE": "COEFFICIENT",
+    },
+    "SENS_NU": {
+        "DESCRIPTION": "d Objective / d Poisson ratio",
+        "GROUP": "SENSITIVITY",
+        "HEADER": "Sens[Nu]",
+        "TYPE": "DEFAULT",
+    },
+    "SENS_PRESS": {
+        "DESCRIPTION": "Sensitivity of the objective function with "
+        "respect to the far-field pressure.",
+        "GROUP": "SENSITIVITY",
+        "HEADER": "Sens_Press",
+        "TYPE": "COEFFICIENT",
+    },
+    "SENS_PRESS_OUT": {
+        "DESCRIPTION": "Sensitivity of the objective function with "
+        "respect to the outlet pressure.",
+        "GROUP": "SENSITIVITY",
+        "HEADER": "Sens_Pout",
+        "TYPE": "COEFFICIENT",
+    },
+    "SENS_TEMP": {
+        "DESCRIPTION": "Sensitivity of the objective function with "
+        "respect to the far-field temperature.",
+        "GROUP": "SENSITIVITY",
+        "HEADER": "Sens_Temp",
+        "TYPE": "COEFFICIENT",
+    },
+    "SENS_VEL_IN": {
+        "DESCRIPTION": "Sensitivity of the objective function with "
+        "respect to the inlet velocity.",
+        "GROUP": "SENSITIVITY",
+        "HEADER": "Sens_Vin",
+        "TYPE": "COEFFICIENT",
+    },
+    "SIDEFORCE": {
+        "DESCRIPTION": "Total sideforce coefficient on all surfaces set "
+        "with MARKER_MONITORING",
+        "GROUP": "AERO_COEFF",
+        "HEADER": "CSF",
+        "TYPE": "COEFFICIENT",
+    },
+    "STREAMWISE_DP": {
+        "DESCRIPTION": "Pressure drop in streamwise periodic flow",
+        "GROUP": "STREAMWISE_PERIODIC",
+        "HEADER": "SWDeltaP",
+        "TYPE": "DEFAULT",
+    },
+    "STREAMWISE_HEAT": {
+        "DESCRIPTION": "Integrated heat for streamwise periodic " "flow",
+        "GROUP": "STREAMWISE_PERIODIC",
+        "HEADER": "SWHeat",
+        "TYPE": "DEFAULT",
+    },
+    "STREAMWISE_MASSFLOW": {
+        "DESCRIPTION": "Massflow in streamwise periodic flow",
+        "GROUP": "STREAMWISE_PERIODIC",
+        "HEADER": "SWMassflow",
+        "TYPE": "DEFAULT",
+    },
+    "STRESS_PENALTY": {
+        "DESCRIPTION": "Aggregate stress penalty",
+        "GROUP": "STRUCT_COEFF",
+        "HEADER": "StressPen",
+        "TYPE": "COEFFICIENT",
+    },
+    "SURFACE_MACH": {
+        "DESCRIPTION": "Total average mach number on all markers set "
+        "in MARKER_ANALYZE",
+        "GROUP": "FLOW_COEFF",
+        "HEADER": "Avg_Mach",
+        "TYPE": "COEFFICIENT",
+    },
+    "SURFACE_MASSFLOW": {
+        "DESCRIPTION": "Total average mass flow on all markers "
+        "set in MARKER_ANALYZE",
+        "GROUP": "FLOW_COEFF",
+        "HEADER": "Avg_Massflow",
+        "TYPE": "COEFFICIENT",
+    },
+    "SURFACE_MOM_DISTORTION": {
+        "DESCRIPTION": "Total momentum distortion on all "
+        "markers set in MARKER_ANALYZE",
+        "GROUP": "FLOW_COEFF",
+        "HEADER": "Momentum_Distortion",
+        "TYPE": "COEFFICIENT",
+    },
+    "SURFACE_PRESSURE_DROP": {
+        "DESCRIPTION": "Total pressure drop on all markers " "set in MARKER_ANALYZE",
+        "GROUP": "FLOW_COEFF",
+        "HEADER": "Pressure_Drop",
+        "TYPE": "COEFFICIENT",
+    },
+    "SURFACE_SECONDARY": {
+        "DESCRIPTION": "Total secondary strength on all markers "
+        "set in MARKER_ANALYZE",
+        "GROUP": "FLOW_COEFF",
+        "HEADER": "Secondary_Strength",
+        "TYPE": "COEFFICIENT",
+    },
+    "SURFACE_SECOND_OVER_UNIFORM": {
+        "DESCRIPTION": "Total secondary over "
+        "uniformity on all markers set "
+        "in MARKER_ANALYZE",
+        "GROUP": "FLOW_COEFF",
+        "HEADER": "Secondary_Over_Uniformity",
+        "TYPE": "COEFFICIENT",
+    },
+    'SURFACE_SPECIES_" + std::to_string(iVar': {
+        "DESCRIPTION": "Total average "
+        'species " + '
+        "std::to_string(iVar) "
+        '+ " on all '
+        "markers set in "
+        "MARKER_ANALYZE",
+        "GROUP": "SPECIES_COEFF",
+        "HEADER": 'Avg_Species_" + ' "std::to_string(iVar",
+        "TYPE": "COEFFICIENT",
+    },
+    "SURFACE_SPECIES_VARIANCE": {
+        "DESCRIPTION": "Total species variance",
+        "GROUP": "SPECIES_COEFF",
+        "HEADER": "Species_Variance",
+        "TYPE": "DEFAULT",
+    },
+    "SURFACE_STATIC_PRESSURE": {
+        "DESCRIPTION": "Total average pressure on all " "markers set in MARKER_ANALYZE",
+        "GROUP": "FLOW_COEFF",
+        "HEADER": "Avg_Press",
+        "TYPE": "COEFFICIENT",
+    },
+    "SURFACE_STATIC_TEMPERATURE": {
+        "DESCRIPTION": "Total average temperature on "
+        "all markers set in "
+        "MARKER_ANALYZE",
+        "GROUP": "FLOW_COEFF",
+        "HEADER": "Avg_Temp",
+        "TYPE": "COEFFICIENT",
+    },
+    "SURFACE_TOTAL_PRESSURE": {
+        "DESCRIPTION": "Total average total pressure on "
+        "all markers set in MARKER_ANALYZE",
+        "GROUP": "FLOW_COEFF",
+        "HEADER": "Avg_TotalPress",
+        "TYPE": "COEFFICIENT",
+    },
+    "SURFACE_TOTAL_TEMPERATURE": {
+        "DESCRIPTION": "Total average total temperature "
+        "all markers set in "
+        "MARKER_ANALYZE",
+        "GROUP": "FLOW_COEFF",
+        "HEADER": "Avg_TotalTemp",
+        "TYPE": "COEFFICIENT",
+    },
+    "SURFACE_UNIFORMITY": {
+        "DESCRIPTION": "Total flow uniformity on all markers " "set in MARKER_ANALYZE",
+        "GROUP": "FLOW_COEFF",
+        "HEADER": "Uniformity",
+        "TYPE": "COEFFICIENT",
+    },
+    "TAVG_ADJOINT_SOLEXTRA": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_ADJOINT_SOLEXTRA",
+        "HEADER": "tavg[Adjoint_SolExtra]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_AVG_DENSITY": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_FLOW_COEFF",
+        "HEADER": "tavg[Avg_Density]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_AVG_ENTHALPY": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_FLOW_COEFF",
+        "HEADER": "tavg[Avg_Enthalpy]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_AVG_NORMALVEL": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_FLOW_COEFF",
+        "HEADER": "tavg[Avg_NormalVel]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_AVG_TEMPERATURE": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_HEAT",
+        "HEADER": "tavg[AvgTemp]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_BUFFET": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_AERO_COEFF",
+        "HEADER": "tavg[Buffet]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_COMBO": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_COMBO",
+        "HEADER": "tavg[ComboObj]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_DELTA_CL": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_FIXED_CL",
+        "HEADER": "tavg[Delta_CL]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_DRAG": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_AERO_COEFF",
+        "HEADER": "tavg[CD]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_D_ADJOINT_SOLEXTRA": {
+        "DESCRIPTION": "weighted time average derivative " "value",
+        "GROUP": "TAVG_D_ADJOINT_SOLEXTRA",
+        "HEADER": "dtavg[Adjoint_SolExtra]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_AVG_DENSITY": {
+        "DESCRIPTION": "weighted time average derivative value",
+        "GROUP": "TAVG_D_FLOW_COEFF",
+        "HEADER": "dtavg[Avg_Density]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_AVG_ENTHALPY": {
+        "DESCRIPTION": "weighted time average derivative " "value",
+        "GROUP": "TAVG_D_FLOW_COEFF",
+        "HEADER": "dtavg[Avg_Enthalpy]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_AVG_NORMALVEL": {
+        "DESCRIPTION": "weighted time average derivative " "value",
+        "GROUP": "TAVG_D_FLOW_COEFF",
+        "HEADER": "dtavg[Avg_NormalVel]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_AVG_TEMPERATURE": {
+        "DESCRIPTION": "weighted time average derivative " "value",
+        "GROUP": "TAVG_D_HEAT",
+        "HEADER": "dtavg[AvgTemp]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_BUFFET": {
+        "DESCRIPTION": "weighted time average derivative value",
+        "GROUP": "TAVG_D_AERO_COEFF",
+        "HEADER": "dtavg[Buffet]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_COMBO": {
+        "DESCRIPTION": "weighted time average derivative value",
+        "GROUP": "TAVG_D_COMBO",
+        "HEADER": "dtavg[ComboObj]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_DELTA_CL": {
+        "DESCRIPTION": "weighted time average derivative value",
+        "GROUP": "TAVG_D_FIXED_CL",
+        "HEADER": "dtavg[Delta_CL]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_DRAG": {
+        "DESCRIPTION": "weighted time average derivative value",
+        "GROUP": "TAVG_D_AERO_COEFF",
+        "HEADER": "dtavg[CD]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_EFFICIENCY": {
+        "DESCRIPTION": "weighted time average derivative value",
+        "GROUP": "TAVG_D_AERO_COEFF",
+        "HEADER": "dtavg[CEff]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_EQUIVALENT_AREA": {
+        "DESCRIPTION": "weighted time average derivative " "value",
+        "GROUP": "TAVG_D_EQUIVALENT_AREA",
+        "HEADER": "dtavg[CEquiv_Area]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_FIGURE_OF_MERIT": {
+        "DESCRIPTION": "weighted time average derivative " "value",
+        "GROUP": "TAVG_D_ROTATING_FRAME",
+        "HEADER": "dtavg[CMerit]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_FORCE_X": {
+        "DESCRIPTION": "weighted time average derivative value",
+        "GROUP": "TAVG_D_AERO_COEFF",
+        "HEADER": "dtavg[CFx]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_FORCE_Y": {
+        "DESCRIPTION": "weighted time average derivative value",
+        "GROUP": "TAVG_D_AERO_COEFF",
+        "HEADER": "dtavg[CFy]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_FORCE_Z": {
+        "DESCRIPTION": "weighted time average derivative value",
+        "GROUP": "TAVG_D_AERO_COEFF",
+        "HEADER": "dtavg[CFz]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_INVERSE_DESIGN_PRESSURE": {
+        "DESCRIPTION": "weighted time average " "derivative value",
+        "GROUP": "TAVG_D_CP_DIFF",
+        "HEADER": "dtavg[Cp_Diff]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_LIFT": {
+        "DESCRIPTION": "weighted time average derivative value",
+        "GROUP": "TAVG_D_AERO_COEFF",
+        "HEADER": "dtavg[CL]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_MAXIMUM_HEATFLUX": {
+        "DESCRIPTION": "weighted time average derivative " "value",
+        "GROUP": "TAVG_D_HEAT",
+        "HEADER": "dtavg[MaxHF]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_MOMENT_X": {
+        "DESCRIPTION": "weighted time average derivative value",
+        "GROUP": "TAVG_D_AERO_COEFF",
+        "HEADER": "dtavg[CMx]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_MOMENT_Y": {
+        "DESCRIPTION": "weighted time average derivative value",
+        "GROUP": "TAVG_D_AERO_COEFF",
+        "HEADER": "dtavg[CMy]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_MOMENT_Z": {
+        "DESCRIPTION": "weighted time average derivative value",
+        "GROUP": "TAVG_D_AERO_COEFF",
+        "HEADER": "dtavg[CMz]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_REFERENCE_GEOMETRY": {
+        "DESCRIPTION": "weighted time average " "derivative value",
+        "GROUP": "TAVG_D_STRUCT_COEFF",
+        "HEADER": "dtavg[RefGeom]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_REFERENCE_NODE": {
+        "DESCRIPTION": "weighted time average derivative " "value",
+        "GROUP": "TAVG_D_STRUCT_COEFF",
+        "HEADER": "dtavg[RefNode]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_SENS_AOA": {
+        "DESCRIPTION": "weighted time average derivative value",
+        "GROUP": "TAVG_D_SENSITIVITY",
+        "HEADER": "dtavg[Sens_AoA]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_SENS_GEO": {
+        "DESCRIPTION": "weighted time average derivative value",
+        "GROUP": "TAVG_D_SENSITIVITY",
+        "HEADER": "dtavg[Sens_Geo]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_SENS_MACH": {
+        "DESCRIPTION": "weighted time average derivative value",
+        "GROUP": "TAVG_D_SENSITIVITY",
+        "HEADER": "dtavg[Sens_Mach]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_SENS_PRESS": {
+        "DESCRIPTION": "weighted time average derivative value",
+        "GROUP": "TAVG_D_SENSITIVITY",
+        "HEADER": "dtavg[Sens_Press]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_SENS_PRESS_OUT": {
+        "DESCRIPTION": "weighted time average derivative " "value",
+        "GROUP": "TAVG_D_SENSITIVITY",
+        "HEADER": "dtavg[Sens_Pout]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_SENS_TEMP": {
+        "DESCRIPTION": "weighted time average derivative value",
+        "GROUP": "TAVG_D_SENSITIVITY",
+        "HEADER": "dtavg[Sens_Temp]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_SENS_VEL_IN": {
+        "DESCRIPTION": "weighted time average derivative value",
+        "GROUP": "TAVG_D_SENSITIVITY",
+        "HEADER": "dtavg[Sens_Vin]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_SIDEFORCE": {
+        "DESCRIPTION": "weighted time average derivative value",
+        "GROUP": "TAVG_D_AERO_COEFF",
+        "HEADER": "dtavg[CSF]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_STRESS_PENALTY": {
+        "DESCRIPTION": "weighted time average derivative " "value",
+        "GROUP": "TAVG_D_STRUCT_COEFF",
+        "HEADER": "dtavg[StressPen]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_SURFACE_MACH": {
+        "DESCRIPTION": "weighted time average derivative " "value",
+        "GROUP": "TAVG_D_FLOW_COEFF",
+        "HEADER": "dtavg[Avg_Mach]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_SURFACE_MASSFLOW": {
+        "DESCRIPTION": "weighted time average derivative " "value",
+        "GROUP": "TAVG_D_FLOW_COEFF",
+        "HEADER": "dtavg[Avg_Massflow]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_SURFACE_MOM_DISTORTION": {
+        "DESCRIPTION": "weighted time average " "derivative value",
+        "GROUP": "TAVG_D_FLOW_COEFF",
+        "HEADER": "dtavg[Momentum_Distortion]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_SURFACE_PRESSURE_DROP": {
+        "DESCRIPTION": "weighted time average " "derivative value",
+        "GROUP": "TAVG_D_FLOW_COEFF",
+        "HEADER": "dtavg[Pressure_Drop]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_SURFACE_SECONDARY": {
+        "DESCRIPTION": "weighted time average derivative " "value",
+        "GROUP": "TAVG_D_FLOW_COEFF",
+        "HEADER": "dtavg[Secondary_Strength]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_SURFACE_SECOND_OVER_UNIFORM": {
+        "DESCRIPTION": "weighted time average " "derivative value",
+        "GROUP": "TAVG_D_FLOW_COEFF",
+        "HEADER": "dtavg[Secondary_Over_Uniformity]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    'TAVG_D_SURFACE_SPECIES_" + std::to_string(iVar': {
+        "DESCRIPTION": "weighted " "time " "average " "derivative " "value",
+        "GROUP": "TAVG_D_SPECIES_COEFF",
+        "HEADER": 'dtavg[Avg_Species_" ' "+ " "std::to_string(iVar]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_SURFACE_STATIC_PRESSURE": {
+        "DESCRIPTION": "weighted time average " "derivative value",
+        "GROUP": "TAVG_D_FLOW_COEFF",
+        "HEADER": "dtavg[Avg_Press]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_SURFACE_STATIC_TEMPERATURE": {
+        "DESCRIPTION": "weighted time average " "derivative value",
+        "GROUP": "TAVG_D_FLOW_COEFF",
+        "HEADER": "dtavg[Avg_Temp]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_SURFACE_TOTAL_PRESSURE": {
+        "DESCRIPTION": "weighted time average " "derivative value",
+        "GROUP": "TAVG_D_FLOW_COEFF",
+        "HEADER": "dtavg[Avg_TotalPress]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_SURFACE_TOTAL_TEMPERATURE": {
+        "DESCRIPTION": "weighted time average " "derivative value",
+        "GROUP": "TAVG_D_FLOW_COEFF",
+        "HEADER": "dtavg[Avg_TotalTemp]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_SURFACE_UNIFORMITY": {
+        "DESCRIPTION": "weighted time average " "derivative value",
+        "GROUP": "TAVG_D_FLOW_COEFF",
+        "HEADER": "dtavg[Uniformity]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_THRUST": {
+        "DESCRIPTION": "weighted time average derivative value",
+        "GROUP": "TAVG_D_ROTATING_FRAME",
+        "HEADER": "dtavg[CT]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_TOPOL_COMPLIANCE": {
+        "DESCRIPTION": "weighted time average derivative " "value",
+        "GROUP": "TAVG_D_STRUCT_COEFF",
+        "HEADER": "dtavg[TopComp]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_TOPOL_DISCRETENESS": {
+        "DESCRIPTION": "weighted time average " "derivative value",
+        "GROUP": "TAVG_D_STRUCT_COEFF",
+        "HEADER": "dtavg[TopDisc]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_TORQUE": {
+        "DESCRIPTION": "weighted time average derivative value",
+        "GROUP": "TAVG_D_ROTATING_FRAME",
+        "HEADER": "dtavg[CQ]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_TOTAL_HEATFLUX": {
+        "DESCRIPTION": "weighted time average derivative " "value",
+        "GROUP": "TAVG_D_HEAT",
+        "HEADER": "dtavg[HF]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_D_VOLUME_FRACTION": {
+        "DESCRIPTION": "weighted time average derivative " "value",
+        "GROUP": "TAVG_D_STRUCT_COEFF",
+        "HEADER": "dtavg[VolFrac]",
+        "TYPE": "TAVG_D_COEFFICIENT",
+    },
+    "TAVG_EFFICIENCY": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_AERO_COEFF",
+        "HEADER": "tavg[CEff]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_EQUIVALENT_AREA": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_EQUIVALENT_AREA",
+        "HEADER": "tavg[CEquiv_Area]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_FIGURE_OF_MERIT": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_ROTATING_FRAME",
+        "HEADER": "tavg[CMerit]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_FORCE_X": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_AERO_COEFF",
+        "HEADER": "tavg[CFx]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_FORCE_Y": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_AERO_COEFF",
+        "HEADER": "tavg[CFy]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_FORCE_Z": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_AERO_COEFF",
+        "HEADER": "tavg[CFz]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_INVERSE_DESIGN_PRESSURE": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_CP_DIFF",
+        "HEADER": "tavg[Cp_Diff]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_LIFT": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_AERO_COEFF",
+        "HEADER": "tavg[CL]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_MAXIMUM_HEATFLUX": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_HEAT",
+        "HEADER": "tavg[MaxHF]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_MOMENT_X": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_AERO_COEFF",
+        "HEADER": "tavg[CMx]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_MOMENT_Y": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_AERO_COEFF",
+        "HEADER": "tavg[CMy]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_MOMENT_Z": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_AERO_COEFF",
+        "HEADER": "tavg[CMz]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_REFERENCE_GEOMETRY": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_STRUCT_COEFF",
+        "HEADER": "tavg[RefGeom]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_REFERENCE_NODE": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_STRUCT_COEFF",
+        "HEADER": "tavg[RefNode]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_SENS_AOA": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_SENSITIVITY",
+        "HEADER": "tavg[Sens_AoA]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_SENS_GEO": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_SENSITIVITY",
+        "HEADER": "tavg[Sens_Geo]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_SENS_MACH": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_SENSITIVITY",
+        "HEADER": "tavg[Sens_Mach]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_SENS_PRESS": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_SENSITIVITY",
+        "HEADER": "tavg[Sens_Press]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_SENS_PRESS_OUT": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_SENSITIVITY",
+        "HEADER": "tavg[Sens_Pout]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_SENS_TEMP": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_SENSITIVITY",
+        "HEADER": "tavg[Sens_Temp]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_SENS_VEL_IN": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_SENSITIVITY",
+        "HEADER": "tavg[Sens_Vin]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_SIDEFORCE": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_AERO_COEFF",
+        "HEADER": "tavg[CSF]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_STRESS_PENALTY": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_STRUCT_COEFF",
+        "HEADER": "tavg[StressPen]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_SURFACE_MACH": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_FLOW_COEFF",
+        "HEADER": "tavg[Avg_Mach]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_SURFACE_MASSFLOW": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_FLOW_COEFF",
+        "HEADER": "tavg[Avg_Massflow]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_SURFACE_MOM_DISTORTION": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_FLOW_COEFF",
+        "HEADER": "tavg[Momentum_Distortion]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_SURFACE_PRESSURE_DROP": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_FLOW_COEFF",
+        "HEADER": "tavg[Pressure_Drop]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_SURFACE_SECONDARY": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_FLOW_COEFF",
+        "HEADER": "tavg[Secondary_Strength]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_SURFACE_SECOND_OVER_UNIFORM": {
+        "DESCRIPTION": "weighted time average " "value",
+        "GROUP": "TAVG_FLOW_COEFF",
+        "HEADER": "tavg[Secondary_Over_Uniformity]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    'TAVG_SURFACE_SPECIES_" + std::to_string(iVar': {
+        "DESCRIPTION": "weighted " "time average " "value",
+        "GROUP": "TAVG_SPECIES_COEFF",
+        "HEADER": 'tavg[Avg_Species_" ' "+ " "std::to_string(iVar]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_SURFACE_STATIC_PRESSURE": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_FLOW_COEFF",
+        "HEADER": "tavg[Avg_Press]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_SURFACE_STATIC_TEMPERATURE": {
+        "DESCRIPTION": "weighted time average " "value",
+        "GROUP": "TAVG_FLOW_COEFF",
+        "HEADER": "tavg[Avg_Temp]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_SURFACE_TOTAL_PRESSURE": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_FLOW_COEFF",
+        "HEADER": "tavg[Avg_TotalPress]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_SURFACE_TOTAL_TEMPERATURE": {
+        "DESCRIPTION": "weighted time average " "value",
+        "GROUP": "TAVG_FLOW_COEFF",
+        "HEADER": "tavg[Avg_TotalTemp]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_SURFACE_UNIFORMITY": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_FLOW_COEFF",
+        "HEADER": "tavg[Uniformity]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_THRUST": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_ROTATING_FRAME",
+        "HEADER": "tavg[CT]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_TOPOL_COMPLIANCE": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_STRUCT_COEFF",
+        "HEADER": "tavg[TopComp]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_TOPOL_DISCRETENESS": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_STRUCT_COEFF",
+        "HEADER": "tavg[TopDisc]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_TORQUE": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_ROTATING_FRAME",
+        "HEADER": "tavg[CQ]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_TOTAL_HEATFLUX": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_HEAT",
+        "HEADER": "tavg[HF]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "TAVG_VOLUME_FRACTION": {
+        "DESCRIPTION": "weighted time average value",
+        "GROUP": "TAVG_STRUCT_COEFF",
+        "HEADER": "tavg[VolFrac]",
+        "TYPE": "TAVG_COEFFICIENT",
+    },
+    "THRUST": {
+        "DESCRIPTION": "Thrust coefficient",
+        "GROUP": "ROTATING_FRAME",
+        "HEADER": "CT",
+        "TYPE": "COEFFICIENT",
+    },
+    "TOPOL_COMPLIANCE": {
+        "DESCRIPTION": "Structural compliance",
+        "GROUP": "STRUCT_COEFF",
+        "HEADER": "TopComp",
+        "TYPE": "COEFFICIENT",
+    },
+    "TOPOL_DISCRETENESS": {
+        "DESCRIPTION": "Discreteness of the material " "distribution",
+        "GROUP": "STRUCT_COEFF",
+        "HEADER": "TopDisc",
+        "TYPE": "COEFFICIENT",
+    },
+    "TORQUE": {
+        "DESCRIPTION": "Torque coefficient",
+        "GROUP": "ROTATING_FRAME",
+        "HEADER": "CQ",
+        "TYPE": "COEFFICIENT",
+    },
+    "TOTAL_HEATFLUX": {
+        "DESCRIPTION": "Total heatflux on all surfaces defined in " "MARKER_MONITORING",
+        "GROUP": "HEAT",
+        "HEADER": "HF",
+        "TYPE": "COEFFICIENT",
+    },
+    "VMS": {
+        "DESCRIPTION": "VMS",
+        "GROUP": "Maximum Von-Misses stress",
+        "HEADER": "VonMises",
+        "TYPE": "DEFAULT",
+    },
+    "VOLUME_FRACTION": {
+        "DESCRIPTION": "Fraction of solid material",
+        "GROUP": "STRUCT_COEFF",
+        "HEADER": "VolFrac",
+        "TYPE": "COEFFICIENT",
+    },
+}
diff --git a/SU2_PY/SU2/io/redirect.py b/SU2_PY/SU2/io/redirect.py
index 9f2d4e4f4ac..b81a80d2e82 100644
--- a/SU2_PY/SU2/io/redirect.py
+++ b/SU2_PY/SU2/io/redirect.py
@@ -37,34 +37,35 @@
 # -------------------------------------------------------------------
 # original source: http://stackoverflow.com/questions/6796492/python-temporarily-redirect-stdout-stderr
 class output(object):
-    ''' with SU2.io.redirect_output(stdout,stderr)
+    """with SU2.io.redirect_output(stdout,stderr)
 
-        Temporarily redirects sys.stdout and sys.stderr when used in
-        a 'with' contextmanager
+    Temporarily redirects sys.stdout and sys.stderr when used in
+    a 'with' contextmanager
 
-        Example:
-        with SU2.io.redirect_output('stdout.txt','stderr.txt'):
-            sys.stdout.write("standard out")
-            sys.stderr.write("stanrard error")
-            # code
-        #: with output redirection
+    Example:
+    with SU2.io.redirect_output('stdout.txt','stderr.txt'):
+        sys.stdout.write("standard out")
+        sys.stderr.write("stanrard error")
+        # code
+    #: with output redirection
 
-        Inputs:
-            stdout - None, a filename, or a file stream
-            stderr - None, a filename, or a file stream
-        None will not redirect outptu
+    Inputs:
+        stdout - None, a filename, or a file stream
+        stderr - None, a filename, or a file stream
+    None will not redirect outptu
+
+    """
 
-    '''
     def __init__(self, stdout=None, stderr=None):
 
         _newout = False
         _newerr = False
 
-        if isinstance(stdout,str):
-            stdout = open(stdout,'a')
+        if isinstance(stdout, str):
+            stdout = open(stdout, "a")
             _newout = True
-        if isinstance(stderr,str):
-            stderr = open(stderr,'a')
+        if isinstance(stderr, str):
+            stderr = open(stderr, "a")
             _newerr = True
 
         self._stdout = stdout or sys.stdout
@@ -74,11 +75,13 @@ def __init__(self, stdout=None, stderr=None):
 
     def __enter__(self):
         self.old_stdout, self.old_stderr = sys.stdout, sys.stderr
-        self.old_stdout.flush(); self.old_stderr.flush()
+        self.old_stdout.flush()
+        self.old_stderr.flush()
         sys.stdout, sys.stderr = self._stdout, self._stderr
 
     def __exit__(self, exc_type, exc_value, traceback):
-        self._stdout.flush(); self._stderr.flush()
+        self._stdout.flush()
+        self._stderr.flush()
         sys.stdout = self.old_stdout
         sys.stderr = self.old_stderr
 
@@ -87,6 +90,7 @@ def __exit__(self, exc_type, exc_value, traceback):
         if self._newerr:
             self._stderr.close()
 
+
 #: class output()
 
 
@@ -94,83 +98,87 @@ def __exit__(self, exc_type, exc_value, traceback):
 #  Folder Redirection
 # -------------------------------------------------------------------
 class folder(object):
-    ''' with SU2.io.redirect_folder(folder,pull,link,force) as push
-
-        Temporarily redirects to a working folder, pulling
-        and pushing needed files
+    """with SU2.io.redirect_folder(folder,pull,link,force) as push
 
-        Example:
+    Temporarily redirects to a working folder, pulling
+    and pushing needed files
 
-        folder = 'temp'
-        pull   = ['file1.txt','file2.txt']
-        link   = ['file3.big']
-        force  = True
+    Example:
 
-        # original path
-        import os
-        print(os.getcwd())
+    folder = 'temp'
+    pull   = ['file1.txt','file2.txt']
+    link   = ['file3.big']
+    force  = True
 
-        # enter folder
-        with SU2.io.redirect_folder(folder,pull,link,force) as push:
-            print(os.getcwd())
-            # code
-            push.append('file4.txt')
-        #: with folder redirection
+    # original path
+    import os
+    print(os.getcwd())
 
-        # returned to original path
+    # enter folder
+    with SU2.io.redirect_folder(folder,pull,link,force) as push:
         print(os.getcwd())
-
-        Inputs:
-            folder - working folder, relative or absolute
-            pull   - list of files to pull (copy to working folder)
-            link   - list of files to link (symbolic link in working folder)
-            force  - True/False overwrite existing files in working folder
-
-        Targets:
-            push   - list of files to push (copy to originating path)
-
-        Notes:
-            push must be appended or extended, not overwritten
-            links in Windows not supported, will simply copy
-    '''
-
-    def __init__(self, folder, pull=None, link=None, force=True ):
-        ''' folder redirection initialization
-            see help( folder ) for more info
-        '''
-
-        if pull is None: pull = []
-        if link is None: link = []
-
-        if not isinstance(pull,list) : pull = [pull]
-        if not isinstance(link,list) : link = [link]
+        # code
+        push.append('file4.txt')
+    #: with folder redirection
+
+    # returned to original path
+    print(os.getcwd())
+
+    Inputs:
+        folder - working folder, relative or absolute
+        pull   - list of files to pull (copy to working folder)
+        link   - list of files to link (symbolic link in working folder)
+        force  - True/False overwrite existing files in working folder
+
+    Targets:
+        push   - list of files to push (copy to originating path)
+
+    Notes:
+        push must be appended or extended, not overwritten
+        links in Windows not supported, will simply copy
+    """
+
+    def __init__(self, folder, pull=None, link=None, force=True):
+        """folder redirection initialization
+        see help( folder ) for more info
+        """
+
+        if pull is None:
+            pull = []
+        if link is None:
+            link = []
+
+        if not isinstance(pull, list):
+            pull = [pull]
+        if not isinstance(link, list):
+            link = [link]
 
         origin = os.getcwd()
-        origin = os.path.abspath(origin).rstrip('/')+'/'
-        folder = os.path.abspath(folder).rstrip('/')+'/'
+        origin = os.path.abspath(origin).rstrip("/") + "/"
+        folder = os.path.abspath(folder).rstrip("/") + "/"
 
         self.origin = origin
         self.folder = folder
-        self.pull   = copy.deepcopy(pull)
-        self.push   = []
-        self.link   = copy.deepcopy(link)
-        self.force  = force
+        self.pull = copy.deepcopy(pull)
+        self.push = []
+        self.link = copy.deepcopy(link)
+        self.force = force
 
     def __enter__(self):
 
         origin = self.origin  # absolute path
         folder = self.folder  # absolute path
-        pull   = self.pull
-        push   = self.push
-        link   = self.link
-        force  = self.force
+        pull = self.pull
+        push = self.push
+        link = self.link
+        force = self.force
 
         # check for no folder change
         if folder == origin:
             return []
 
         # relative folder path
-        #relative = os.path.relpath(folder,origin)
+        # relative = os.path.relpath(folder,origin)
 
         # check, make folder
         if not os.path.exists(folder):
@@ -180,23 +188,29 @@ def __enter__(self):
         for name in pull:
             old_name = os.path.abspath(name)
             new_name = os.path.split(name)[-1]
-            new_name = os.path.join(folder,new_name)
-            if old_name == new_name: continue
-            if os.path.exists( new_name ):
-                if force: os.remove( new_name )
-                else: continue
-            shutil.copy(old_name,new_name)
+            new_name = os.path.join(folder, new_name)
+            if old_name == new_name:
+                continue
+            if os.path.exists(new_name):
+                if force:
+                    os.remove(new_name)
+                else:
+                    continue
+            shutil.copy(old_name, new_name)
 
         # make links
         for name in link:
             old_name = os.path.abspath(name)
             new_name = os.path.split(name)[-1]
-            new_name = os.path.join(folder,new_name)
-            if old_name == new_name: continue
-            if os.path.exists( new_name ):
-                if force: os.remove( new_name )
-                else: continue
-            make_link(old_name,new_name)
+            new_name = os.path.join(folder, new_name)
+            if old_name == new_name:
+                continue
+            if os.path.exists(new_name):
+                if force:
+                    os.remove(new_name)
+                else:
+                    continue
+            make_link(old_name, new_name)
 
         # change directory
         os.chdir(folder)
@@ -208,8 +222,8 @@ def __exit__(self, exc_type, exc_value, traceback):
 
         origin = self.origin
         folder = self.folder
-        push   = self.push
-        force  = self.force
+        push = self.push
+        force = self.force
 
         # check for no folder change
         if folder == origin:
@@ -220,26 +234,33 @@ def __exit__(self, exc_type, exc_value, traceback):
 
             old_name = os.path.abspath(name)
             name = os.path.split(name)[-1]
-            new_name = os.path.join(origin,name)
+            new_name = os.path.join(origin, name)
 
             # links
             if os.path.islink(old_name):
                 source = os.path.realpath(old_name)
-                if source == new_name: continue
-                if os.path.exists( new_name ):
-                    if force: os.remove( new_name )
-                    else: continue
-                make_link(source,new_name)
+                if source == new_name:
+                    continue
+                if os.path.exists(new_name):
+                    if force:
+                        os.remove(new_name)
+                    else:
+                        continue
+                make_link(source, new_name)
 
             # moves
             else:
-                if old_name == new_name: continue
-                if os.path.exists( new_name ):
-                    if force: os.remove( new_name )
-                    else: continue
-                shutil.move(old_name,new_name)
+                if old_name == new_name:
+                    continue
+                if os.path.exists(new_name):
+                    if force:
+                        os.remove(new_name)
+                    else:
+                        continue
+                shutil.move(old_name, new_name)
 
         # change directory
         os.chdir(origin)
 
+
 #: class folder()
diff --git a/SU2_PY/SU2/io/state.py b/SU2_PY/SU2/io/state.py
index 5350df9fdbc..3203c10a012 100644
--- a/SU2_PY/SU2/io/state.py
+++ b/SU2_PY/SU2/io/state.py
@@ -30,8 +30,17 @@
 # ----------------------------------------------------------------------
 
 import os, sys, shutil, copy, time
-from ..io   import expand_part, expand_zones, expand_time, get_adjointSuffix, add_suffix, \
-                   get_specialCases, Config, expand_multipoint, optnames_multi
+from ..io import (
+    expand_part,
+    expand_zones,
+    expand_time,
+    get_adjointSuffix,
+    add_suffix,
+    get_specialCases,
+    Config,
+    expand_multipoint,
+    optnames_multi,
+)
 from ..util import bunch
 from ..util import ordered_bunch
 
@@ -40,82 +49,92 @@
 #  State Factory
 # ----------------------------------------------------------------------
 
-def State_Factory(state=None,config=None):
-    """ state = SU2.io.State()
-
-        Starts a state class, an extension of ordered_bunch().
-        Stores data generated while traversing SU2 tool chain
-
-        Fields:
-            FUNCTIONS - ordered bunch of objective function values
-            GRADIENTS - ordered bunch of gradient value lists
-            VARIABLES - ordered bunch of variables
-            FILES     - ordered bunch of file types
-            HISTORY   - ordered bunch of history information
-
-        Fields can be accessed by item or attribute
-        ie: state['FUNCTIONS'] or state.FUNCTIONS
-
-        Methods:
-            update()        - updates self with another state
-            pullnlink()     - returns files to pull and link
-            design_vector() - vectorizes design variables
-            find_files()    - finds existing mesh and solutions
-
-        Example of a filled state:
-        FUNCTIONS:
-            LIFT: 0.2353065809
-            DRAG: 0.042149736
-            SIDEFORCE: 0.0
-            MOMENT_X: 0.0
-            MOMENT_Y: 0.0
-            MOMENT_Z: 0.046370243
-            FORCE_X: 0.0370065195
-            FORCE_Y: 0.2361700759
-            FORCE_Z: 0.0
-            EFFICIENCY: 5.5826347517
-        GRADIENTS:
-            DRAG: [0.133697, 0.41473, 0.698497, (...)
-        VARIABLES:
-            DV_VALUE_NEW: [0.002, 0.002, 0.002, (...)
-        FILES:
-            MESH: mesh.su2
-            DIRECT: solution_flow.dat
-            ADJOINT_DRAG: solution_adj_cd.dat
-            FLOW_META: flow.meta
-            MULTIPOINT_DIRECT: [solution_flow_point0.dat solution_flow_point1.dat, ...]
-            MULTIPOINT_ADJOINT_DRAG: [solution_adj_point0_cd.dat solution_adj_point1_cd.dat, ...]
-            MULTIPOINT_MESH_FILENAME: [mesh_0.su2, mesh_1.su2, ... ]
-            MULTIPOINT_FLOW_META: [flow_point0.meta, flow_point1.meta, ...]
-        HISTORY:
-            DIRECT: {ITERATION=[1.0, 2.0, 3.0, (...)
-            ADJOINT_DRAG: {ITERATION=[1.0, 2.0, 3.0, (...)
-        WND_CAUCHY_DATA:
-            TIME_ITER
-            UNST_ADJOINT_ITER
-            ITER_AVERAGE_OBJ
+
+def State_Factory(state=None, config=None):
+    """state = SU2.io.State()
+
+    Starts a state class, an extension of ordered_bunch().
+    Stores data generated while traversing SU2 tool chain
+
+    Fields:
+        FUNCTIONS - ordered bunch of objective function values
+        GRADIENTS - ordered bunch of gradient value lists
+        VARIABLES - ordered bunch of variables
+        FILES     - ordered bunch of file types
+        HISTORY   - ordered bunch of history information
+
+    Fields can be accessed by item or attribute
+    ie: state['FUNCTIONS'] or state.FUNCTIONS
+
+    Methods:
+        update()        - updates self with another state
+        pullnlink()     - returns files to pull and link
+        design_vector() - vectorizes design variables
+        find_files()    - finds existing mesh and solutions
+
+    Example of a filled state:
+    FUNCTIONS:
+        LIFT: 0.2353065809
+        DRAG: 0.042149736
+        SIDEFORCE: 0.0
+        MOMENT_X: 0.0
+        MOMENT_Y: 0.0
+        MOMENT_Z: 0.046370243
+        FORCE_X: 0.0370065195
+        FORCE_Y: 0.2361700759
+        FORCE_Z: 0.0
+        EFFICIENCY: 5.5826347517
+    GRADIENTS:
+        DRAG: [0.133697, 0.41473, 0.698497, (...)
+    VARIABLES:
+        DV_VALUE_NEW: [0.002, 0.002, 0.002, (...)
+    FILES:
+        MESH: mesh.su2
+        DIRECT: solution_flow.dat
+        ADJOINT_DRAG: solution_adj_cd.dat
+        FLOW_META: flow.meta
+        MULTIPOINT_DIRECT: [solution_flow_point0.dat solution_flow_point1.dat, ...]
+        MULTIPOINT_ADJOINT_DRAG: [solution_adj_point0_cd.dat solution_adj_point1_cd.dat, ...]
+        MULTIPOINT_MESH_FILENAME: [mesh_0.su2, mesh_1.su2, ... ]
+        MULTIPOINT_FLOW_META: [flow_point0.meta, flow_point1.meta, ...]
+    HISTORY:
+        DIRECT: {ITERATION=[1.0, 2.0, 3.0, (...)
+        ADJOINT_DRAG: {ITERATION=[1.0, 2.0, 3.0, (...)
+    WND_CAUCHY_DATA:
+        TIME_ITER
+        UNST_ADJOINT_ITER
+        ITER_AVERAGE_OBJ
 
     """
 
-    if isinstance(state,Config) and not config:
+    if isinstance(state, Config) and not config:
         config = state
         state = None
 
     if not state is None:
-        assert isinstance(state,State) , 'input is must be a state instance'
+        assert isinstance(state, State), "input is must be a state instance"
         return state
 
     NewClass = State()
 
-    for key in ['FUNCTIONS','GRADIENTS','VARIABLES','FILES','HISTORY','WND_CAUCHY_DATA']:
+    for key in [
+        "FUNCTIONS",
+        "GRADIENTS",
+        "VARIABLES",
+        "FILES",
+        "HISTORY",
+        "WND_CAUCHY_DATA",
+    ]:
         NewClass[key] = ordered_bunch()
 
     if config:
         NewClass.find_files(config)
         # WND_Convergence Data
-        NewClass['WND_CAUCHY_DATA'] = {'TIME_ITER': config['TIME_ITER'],
-                                       'UNST_ADJOINT_ITER': config['UNST_ADJOINT_ITER'],
-                                       'ITER_AVERAGE_OBJ': config['ITER_AVERAGE_OBJ']}
+        NewClass["WND_CAUCHY_DATA"] = {
+            "TIME_ITER": config["TIME_ITER"],
+            "UNST_ADJOINT_ITER": config["UNST_ADJOINT_ITER"],
+            "ITER_AVERAGE_OBJ": config["ITER_AVERAGE_OBJ"],
+        }
 
     return NewClass
 
@@ -124,155 +143,157 @@ def State_Factory(state=None,config=None):
 #  State Class
 # ----------------------------------------------------------------------
 
+
 class State(ordered_bunch):
-    """ state = SU2.io.state.State()
+    """state = SU2.io.state.State()
 
-        This is the State class that should be generated with the
-        Factory Function SU2.io.state.State_Factory()
+    This is the State class that should be generated with the
+    Factory Function SU2.io.state.State_Factory()
 
-        Parameters:
-            none, should be loaded with State_Factory()
+    Parameters:
+        none, should be loaded with State_Factory()
 
-        Methods:
-            update()        - updates self with another state
-            pullnlink()     - returns files to pull and link
-            design_vector() - vectorizes design variables
-            find_files()    - finds existing mesh and solutions
+    Methods:
+        update()        - updates self with another state
+        pullnlink()     - returns files to pull and link
+        design_vector() - vectorizes design variables
+        find_files()    - finds existing mesh and solutions
 
     """
 
     _timestamp = 0
 
-    def update(self,ztate):
-        """ Updates self given another state
-        """
+    def update(self, ztate):
+        """Updates self given another state"""
 
-        if not ztate: return
-        assert isinstance(ztate,State) , 'must update with another State-type'
+        if not ztate:
+            return
+        assert isinstance(ztate, State), "must update with another State-type"
         for key in self.keys():
-            if isinstance(ztate[key],dict):
-                self[key].update( ztate[key] )
+            if isinstance(ztate[key], dict):
+                self[key].update(ztate[key])
             elif ztate[key]:
                 self[key] = ztate[key]
 
         self.set_timestamp()
 
-
     def __repr__(self):
         return self.__str__()
 
     def __str__(self):
-        output = 'STATE:'
+        output = "STATE:"
         for k1, v1 in self.items():
-            output += '\n    %s:' % k1
-            if isinstance(v1,dict):
+            output += "\n    %s:" % k1
+            if isinstance(v1, dict):
                 for k2, v2 in v1.items():
-                    output += '\n        %s: %s' % (k2,v2)
+                    output += "\n        %s: %s" % (k2, v2)
             else:
-                output += '\n        %s' % v1
+                output += "\n        %s" % v1
         return output
 
-    def pullnlink(self,config):
-        """ pull,link = SU2.io.State.pullnlink(config)
-            returns lists pull and link of files for folder
-            redirection, based on a given config
+    def pullnlink(self, config):
+        """pull,link = SU2.io.State.pullnlink(config)
+        returns lists pull and link of files for folder
+        redirection, based on a given config
         """
 
-        pull = []; link = []
+        pull = []
+        link = []
 
         # choose files to pull and link
         for key, value in self.FILES.items():
             # link big files
-            if key == 'MESH':
+            if key == "MESH":
                 # mesh (merged or partitioned)
-                value = expand_part(value,config)
+                value = expand_part(value, config)
                 link.extend(value)
-            elif key == 'DIRECT':
+            elif key == "DIRECT":
                 # direct solution
-                value = expand_zones(value,config)
-                value = expand_time(value,config)
+                value = expand_zones(value, config)
+                value = expand_time(value, config)
                 link.extend(value)
-            elif 'ADJOINT_' in key and  (not 'MULTIPOINT' in key):
+            elif "ADJOINT_" in key and (not "MULTIPOINT" in key):
                 # adjoint solution
-                value = expand_zones(value,config)
-                value = expand_time(value,config)
+                value = expand_zones(value, config)
+                value = expand_time(value, config)
                 link.extend(value)
-            elif 'MULTIPOINT' in key:
+            elif "MULTIPOINT" in key:
                 # multipoint files
-                if key != 'MULTIPOINT_MESH_FILENAME':
+                if key != "MULTIPOINT_MESH_FILENAME":
                     # DIRECT and ADJOINT files
-                    value = expand_zones(value,config)
-                    value = expand_time(value,config)
+                    value = expand_zones(value, config)
+                    value = expand_time(value, config)
                 for elem in value:
                     if elem:
                         link.append(elem)
-            #elif key == 'STABILITY':
-                #pass
+            # elif key == 'STABILITY':
+            # pass
             # copy all other files
             else:
                 pull.append(value)
 
         #: for each filename
 
-        return pull,link
+        return pull, link
 
     def design_vector(self):
-        """ vectorizes State.VARIABLES
-        """
+        """vectorizes State.VARIABLES"""
         vector = []
         for value in self.VARIABLES.values():
-            if isinstance(value,dict):
+            if isinstance(value, dict):
                 for v in value.values():
                     vector.append(v)
-            elif not isinstance(value,list):
+            elif not isinstance(value, list):
                 value = [value]
             vector.extend(value)
         return vector
 
-    def find_files(self,config):
-        """ SU2.io.State.find_files(config)
-            finds mesh and solution files for a given config.
-            updates state.FILES with filenames.
-            files already logged in state are not overridden.
-            will ignore solutions if config.RESTART_SOL == 'NO'.
+    def find_files(self, config):
+        """SU2.io.State.find_files(config)
+        finds mesh and solution files for a given config.
+        updates state.FILES with filenames.
+        files already logged in state are not overridden.
+        will ignore solutions if config.RESTART_SOL == 'NO'.
         """
 
         files = self.FILES
 
-        mesh_name     = config.MESH_FILENAME
-        if config.get('READ_BINARY_RESTART', 'YES') == 'NO':
-            if not 'RESTART_ASCII' in config.get('OUTPUT_FILES',['RESTART']):
-                print ('RESTART_ASCII must be in OUTPUT_FILES if READ_BINARY_RESTART is set to NO')
+        mesh_name = config.MESH_FILENAME
+        if config.get("READ_BINARY_RESTART", "YES") == "NO":
+            if not "RESTART_ASCII" in config.get("OUTPUT_FILES", ["RESTART"]):
+                print(
+                    "RESTART_ASCII must be in OUTPUT_FILES if READ_BINARY_RESTART is set to NO"
+                )
                 sys.exit()
 
-        direct_name   = config.SOLUTION_FILENAME
-        adjoint_name  = config.SOLUTION_ADJ_FILENAME
+        direct_name = config.SOLUTION_FILENAME
+        adjoint_name = config.SOLUTION_ADJ_FILENAME
 
-        if 'RESTART_ASCII' in config.get('OUTPUT_FILES', ['RESTART']):
-            direct_name = direct_name.split('.')[0] + '.csv'
-            adjoint_name = adjoint_name.split('.')[0] + '.csv'
+        if "RESTART_ASCII" in config.get("OUTPUT_FILES", ["RESTART"]):
+            direct_name = direct_name.split(".")[0] + ".csv"
+            adjoint_name = adjoint_name.split(".")[0] + ".csv"
         else:
-            direct_name = direct_name.split('.')[0] + '.dat'
-            adjoint_name = adjoint_name.split('.')[0] + '.dat'
+            direct_name = direct_name.split(".")[0] + ".dat"
+            adjoint_name = adjoint_name.split(".")[0] + ".dat"
 
-        targetea_name = 'TargetEA.dat'
-        targetcp_name = 'TargetCp.dat'
-        targetheatflux_name = 'TargetHeatFlux.dat'
+        targetea_name = "TargetEA.dat"
+        targetcp_name = "TargetCp.dat"
+        targetheatflux_name = "TargetHeatFlux.dat"
 
         adj_map = get_adjointSuffix()
-        restart = config.RESTART_SOL == 'YES'
+        restart = config.RESTART_SOL == "YES"
         special_cases = get_specialCases(config)
 
-        if config.get('OPT_OBJECTIVE'):
-            def_objs = config['OPT_OBJECTIVE']
+        if config.get("OPT_OBJECTIVE"):
+            def_objs = config["OPT_OBJECTIVE"]
             objectives = def_objs.keys()
             multipoint = any(elem in optnames_multi for elem in objectives)
         else:
             multipoint = False
 
-        def register_file(label,filename):
+        def register_file(label, filename):
             if not label in files:
-                if label.split('_')[0] in ['DIRECT', 'ADJOINT']:
+                if label.split("_")[0] in ["DIRECT", "ADJOINT"]:
                     names = expand_zones(filename, config)
                     found = False
                     for name in names:
@@ -284,107 +305,121 @@ def register_file(label,filename):
 
                     if found:
                         files[label] = filename
-                        print('Found: %s' % filename)
+                        print("Found: %s" % filename)
 
-                elif label.split('_')[0] in ['MULTIPOINT']:
+                elif label.split("_")[0] in ["MULTIPOINT"]:
                     # if multipoint, list of files needs to be added
-                    file_list= [];
+                    file_list = []
                     for name in filename:
                         if os.path.exists(name):
                             file_list.append(name)
-                            print('Found: %s' % name)
+                            print("Found: %s" % name)
                         else:
                             # if file doesn't exist, enter empty string as placeholder
-                            file_list.append('')
-		            # If even one of the multipoint files is found, add the list
+                            file_list.append("")
+                    # If even one of the multipoint files is found, add the list
                     if any(file for file in file_list):
                         files[label] = file_list
                 else:
                     if os.path.exists(filename):
                         files[label] = filename
-                        print('Found: %s' % filename)
+                        print("Found: %s" % filename)
             else:
-                if label.split("_")[0] in ['DIRECT', 'ADJOINT']:
+                if label.split("_")[0] in ["DIRECT", "ADJOINT"]:
                     for name in expand_zones(files[label], config):
-                        assert os.path.exists(name), 'state expected file: %s' % filename
-                elif label.split('_')[0] in ['MULTIPOINT']:
+                        assert os.path.exists(name), (
+                            "state expected file: %s" % filename
+                        )
+                elif label.split("_")[0] in ["MULTIPOINT"]:
                     for name in expand_zones(files[label], config):
                         if name:
                             if not os.path.exists(name):
-                                raise AssertionError('state expected file: %s' % name)
+                                raise AssertionError("state expected file: %s" % name)
                 else:
-                    assert os.path.exists(files[label]) , 'state expected file: %s' % filename
+                    assert os.path.exists(files[label]), (
+                        "state expected file: %s" % filename
+                    )
+
         #: register_file()
 
         # mesh
         if multipoint:
-            mesh_list = [elem.strip() for elem in config['MULTIPOINT_MESH_FILENAME'].replace("(", "").replace(")", "").split(',')]
+            mesh_list = [
+                elem.strip()
+                for elem in config["MULTIPOINT_MESH_FILENAME"]
+                .replace("(", "")
+                .replace(")", "")
+                .split(",")
+            ]
             if len(set(mesh_list)) > 1:
                 # Only register MULTIPOINT_MESH_FILENAME if multiple meshes are specified
-                register_file('MULTIPOINT_MESH_FILENAME', mesh_list)
+                register_file("MULTIPOINT_MESH_FILENAME", mesh_list)
             mesh_name = mesh_list[0]
 
-        register_file('MESH',mesh_name)
+        register_file("MESH", mesh_name)
 
         # old style restart
-        if not 'RESTART_FILE_1' in files.keys():
+        if not "RESTART_FILE_1" in files.keys():
             # direct solutions
             if restart:
-                register_file('DIRECT',direct_name)
+                register_file("DIRECT", direct_name)
                 if multipoint:
-                    name_list = expand_multipoint(direct_name,config)
-                    name_list = expand_zones(name_list,config)
-                    register_file('MULTIPOINT_DIRECT',name_list)
+                    name_list = expand_multipoint(direct_name, config)
+                    name_list = expand_zones(name_list, config)
+                    register_file("MULTIPOINT_DIRECT", name_list)
 
             # flow meta data file
             if restart:
-                register_file('FLOW_META','flow.meta')
+                register_file("FLOW_META", "flow.meta")
                 if multipoint:
-                    name_list = expand_multipoint('flow.meta',config)
-                    register_file('MULTIPOINT_FLOW_META',name_list)
+                    name_list = expand_multipoint("flow.meta", config)
+                    register_file("MULTIPOINT_FLOW_META", name_list)
 
             # adjoint solutions
             if restart:
                 for obj, suff in adj_map.items():
-                    ADJ_LABEL = 'ADJOINT_' + obj
-                    adjoint_name_suffixed = add_suffix(adjoint_name,suff)
-                    register_file(ADJ_LABEL,adjoint_name_suffixed)
+                    ADJ_LABEL = "ADJOINT_" + obj
+                    adjoint_name_suffixed = add_suffix(adjoint_name, suff)
+                    register_file(ADJ_LABEL, adjoint_name_suffixed)
                     if multipoint:
-                        name_list = expand_zones(add_suffix(expand_multipoint(adjoint_name,config), suff), config)
-                        multipoint_adj_name = 'MULTIPOINT_' + ADJ_LABEL
+                        name_list = expand_zones(
+                            add_suffix(expand_multipoint(adjoint_name, config), suff),
+                            config,
+                        )
+                        multipoint_adj_name = "MULTIPOINT_" + ADJ_LABEL
                         register_file(multipoint_adj_name, name_list)
 
         # equivalent area
-        if 'EQUIV_AREA' in special_cases:
-            register_file('TARGET_EA',targetea_name)
+        if "EQUIV_AREA" in special_cases:
+            register_file("TARGET_EA", targetea_name)
 
         # pressure inverse design
-        if 'INV_DESIGN_CP' in special_cases:
-            register_file('TARGET_CP',targetcp_name)
+        if "INV_DESIGN_CP" in special_cases:
+            register_file("TARGET_CP", targetcp_name)
 
         # heat flux inverse design
-        if 'INV_DESIGN_HEATFLUX' in special_cases:
-            register_file('TARGET_HEATFLUX',targetheatflux_name)
+        if "INV_DESIGN_HEATFLUX" in special_cases:
+            register_file("TARGET_HEATFLUX", targetheatflux_name)
 
         return
 
-    def __setitem__(self,k,v):
+    def __setitem__(self, k, v):
         if self._initialized:
             self.set_timestamp()
-        super(State,self).__setitem__(k,v)
+        super(State, self).__setitem__(k, v)
 
     def set_timestamp(self):
         self._timestamp = time.time()
 
     def tic(self):
-        """ timestamp = State.tic()
-            returns the time that this state was last modified
+        """timestamp = State.tic()
+        returns the time that this state was last modified
         """
         return self._timestamp
 
-    def toc(self,timestamp):
-        """ updated = State.toc(timestamp)
-            returns True if state was modified since last timestamp
+    def toc(self, timestamp):
+        """updated = State.toc(timestamp)
+        returns True if state was modified since last timestamp
         """
         return self._timestamp > timestamp
 
diff --git a/SU2_PY/SU2/io/tools.py b/SU2_PY/SU2/io/tools.py
index 00a52e16cd2..52b51d9ae54 100755
--- a/SU2_PY/SU2/io/tools.py
+++ b/SU2_PY/SU2/io/tools.py
@@ -38,9 +38,10 @@
 #  Read SU2_DOT Gradient Values
 # -------------------------------------------------------------------
 
-def read_gradients( Grad_filename , scale = 1.0):
-    """ reads the raw gradients from the gradient file
-        returns a list of floats
+
+def read_gradients(Grad_filename, scale=1.0):
+    """reads the raw gradients from the gradient file
+    returns a list of floats
     """
 
     # open file and skip first line
@@ -58,6 +59,7 @@ def read_gradients( Grad_filename , scale = 1.0):
 
     return grad_vals
 
+
 #: def read_gradients()
 
 
@@ -65,34 +67,36 @@ def read_gradients( Grad_filename , scale = 1.0):
 #  Read All Data from a Plot File
 # -------------------------------------------------------------------
 
-def read_plot( filename ):
-    """ reads a plot file
-        returns an ordered bunch with the headers for keys
-        and a list of each header's floats for values.
+
+def read_plot(filename):
+    """reads a plot file
+    returns an ordered bunch with the headers for keys
+    and a list of each header's floats for values.
     """
 
-    extension = os.path.splitext( filename )[1]
+    extension = os.path.splitext(filename)[1]
 
     # open history file
     plot_file = open(filename)
 
     # title?
     line = plot_file.readline()
-    if line.startswith('TITLE'):
-        title = line.split('=')[1] .strip() # not used right now
+    if line.startswith("TITLE"):
+        title = line.split("=")[1].strip()  # not used right now
         line = plot_file.readline()
 
-    if line.startswith('VARIABLES'):
-          line = plot_file.readline()
+    if line.startswith("VARIABLES"):
+        line = plot_file.readline()
 
     line = line.split(",")
-    Variables = [ x.strip().strip('"') for x in line ]
+    Variables = [x.strip().strip('"') for x in line]
     n_Vars = len(Variables)
 
     # initialize plot data dictionary
     plot_data = ordered_bunch.fromkeys(Variables)
     # must default each value to avoid pointer problems
-    for key in plot_data.keys(): plot_data[key] = []
+    for key in plot_data.keys():
+        plot_data[key] = []
 
     # zone list
     zones = []
@@ -104,26 +108,26 @@ def read_plot( filename ):
         if not line:
             break
 
-        #zone?
-        if line.startswith('ZONE'):
-            zone = line.split('=')[1].strip('" ')
+        # zone?
+        if line.startswith("ZONE"):
+            zone = line.split("=")[1].strip('" ')
             zones.append(zone)
             continue
 
         # split line
-        line_data = line.strip().split(',')
-        line_data = [ float(x.strip()) for x in line_data ]
+        line_data = line.strip().split(",")
+        line_data = [float(x.strip()) for x in line_data]
 
         # store to dictionary
         for i_Var in range(n_Vars):
             this_variable = Variables[i_Var]
-            plot_data[this_variable] = plot_data[this_variable] + [ line_data[i_Var] ]
+            plot_data[this_variable] = plot_data[this_variable] + [line_data[i_Var]]
 
     #: for each line
 
     # check for number of zones
     if len(zones) > 1:
-        raise IOError('multiple zones not supported')
+        raise IOError("multiple zones not supported")
 
     # done
     plot_file.close()
@@ -134,18 +138,19 @@ def read_plot( filename ):
 #  Read All Data from History File
 # -------------------------------------------------------------------
 
-def read_history( History_filename, nZones = 1):
-    """ reads a history file
-        returns an ordered bunch with the history file headers for keys
-        and a list of each header's floats for values.
-        if header is an optimization objective, its name is mapped to
-        the optimization name.
-        Iter and Time(min) headers are mapped to ITERATION and TIME
-        respectively.
+
+def read_history(History_filename, nZones=1):
+    """reads a history file
+    returns an ordered bunch with the history file headers for keys
+    and a list of each header's floats for values.
+    if header is an optimization objective, its name is mapped to
+    the optimization name.
+    Iter and Time(min) headers are mapped to ITERATION and TIME
+    respectively.
     """
 
     # read plot file
-    plot_data = read_plot( History_filename )
+    plot_data = read_plot(History_filename)
 
     # initialize history data dictionary
     history_data = ordered_bunch()
@@ -155,39 +160,41 @@ def read_history( History_filename, nZones = 1):
         var = key
         for field in historyOutFields:
 
-            if key == historyOutFields[field]['HEADER'] and nZones == 1:
+            if key == historyOutFields[field]["HEADER"] and nZones == 1:
                 var = field
 
-            if key.split('[')[0] == historyOutFields[field]['HEADER'] and nZones > 1:
-                var = field + '[' + key.split('[')[1]
+            if key.split("[")[0] == historyOutFields[field]["HEADER"] and nZones > 1:
+                var = field + "[" + key.split("[")[1]
 
         history_data[var] = plot_data[key]
 
     return history_data
 
-#: def read_history()
 
+#: def read_history()
 
 
 # -------------------------------------------------------------------
 #  Define Dictionary Map for Header Names
 # -------------------------------------------------------------------
 
-def get_headerMap(nZones = 1):
+
+def get_headerMap(nZones=1):
 
     headerMap = dict()
     for outputField in historyOutFields:
-        headerMap[outputField] = historyOutFields[outputField]['HEADER']
+        headerMap[outputField] = historyOutFields[outputField]["HEADER"]
 
     return headerMap
 
-def getTurboPerfIndex(nZones = 1):
 
-  if int(nZones) > 1:
-    index = int(nZones) + int(int(nZones)/2.0) + 1
-  else:
-    index = 1
-  return index
+def getTurboPerfIndex(nZones=1):
+
+    if int(nZones) > 1:
+        index = int(nZones) + int(int(nZones) / 2.0) + 1
+    else:
+        index = 1
+    return index
 
 
 #: def get_headerMap()
@@ -199,66 +206,71 @@ def getTurboPerfIndex(nZones = 1):
 
 #: optnames_stab
 
-optnames_stab = [ "D_LIFT_D_ALPHA"               ,
-                  "D_DRAG_D_ALPHA"               ,
-                  "D_SIDEFORCE_D_ALPHA"          ,
-                  "D_MOMENT_X_D_ALPHA"           ,
-                  "D_MOMENT_Y_D_ALPHA"           ,
-                  "D_MOMENT_Z_D_ALPHA"           ,
-                ]
+optnames_stab = [
+    "D_LIFT_D_ALPHA",
+    "D_DRAG_D_ALPHA",
+    "D_SIDEFORCE_D_ALPHA",
+    "D_MOMENT_X_D_ALPHA",
+    "D_MOMENT_Y_D_ALPHA",
+    "D_MOMENT_Z_D_ALPHA",
+]
 
 #: Multipoint Optimizer Function Names
 
 # optnames_multi = ['{}_{}'.format('MULTIPOINT', a) for a in optnames_aero]
 
-optnames_multi = [ "MULTIPOINT_LIFT"               ,
-                   "MULTIPOINT_DRAG"               ,
-                   "MULTIPOINT_SIDEFORCE"          ,
-                   "MULTIPOINT_MOMENT_X"           ,
-                   "MULTIPOINT_MOMENT_Y"           ,
-                   "MULTIPOINT_MOMENT_Z"           ,
-                   "MULTIPOINT_CUSTOM_OBJFUNC"]
+optnames_multi = [
+    "MULTIPOINT_LIFT",
+    "MULTIPOINT_DRAG",
+    "MULTIPOINT_SIDEFORCE",
+    "MULTIPOINT_MOMENT_X",
+    "MULTIPOINT_MOMENT_Y",
+    "MULTIPOINT_MOMENT_Z",
+    "MULTIPOINT_CUSTOM_OBJFUNC",
+]
 
 # Geometric Optimizer Function Names
-optnames_geo = [ "AIRFOIL_AREA"                   ,
-                 "AIRFOIL_THICKNESS"              ,
-                 "AIRFOIL_CHORD"                  ,
-                 "AIRFOIL_LE_RADIUS"              ,
-                 "AIRFOIL_TOC"                    ,
-                 "AIRFOIL_ALPHA"                  ,
-                 "FUSELAGE_VOLUME"        ,
-                 "FUSELAGE_WETTED_AREA"   ,
-                 "FUSELAGE_MIN_WIDTH"     ,
-                 "FUSELAGE_MAX_WIDTH"     ,
-                 "FUSELAGE_MIN_WATERLINE_WIDTH"  ,
-                 "FUSELAGE_MAX_WATERLINE_WIDTH"  ,
-                 "FUSELAGE_MIN_HEIGHT"    ,
-                 "FUSELAGE_MAX_HEIGHT"    ,
-                 "FUSELAGE_MAX_CURVATURE" ,
-                 "WING_VOLUME"            ,
-                 "WING_MIN_THICKNESS" ,
-                 "WING_MAX_THICKNESS" ,
-                 "WING_MIN_CHORD"         ,
-                 "WING_MAX_CHORD"         ,
-                 "WING_MIN_LE_RADIUS"     ,
-                 "WING_MAX_LE_RADIUS"     ,
-                 "WING_MIN_TOC"           ,
-                 "WING_MAX_TOC"           ,
-                 "WING_OBJFUN_MIN_TOC"    ,
-                 "WING_MAX_TWIST"         ,
-                 "WING_MAX_CURVATURE"     ,
-                 "WING_MAX_DIHEDRAL"           ,
-                 "NACELLE_VOLUME"            ,
-                 "NACELLE_MIN_THICKNESS"     ,
-                 "NACELLE_MAX_THICKNESS"     ,
-                 "NACELLE_MIN_CHORD"         ,
-                 "NACELLE_MAX_CHORD"         ,
-                 "NACELLE_MIN_LE_RADIUS"     ,
-                 "NACELLE_MAX_LE_RADIUS"     ,
-                 "NACELLE_MIN_TOC"           ,
-                 "NACELLE_MAX_TOC"           ,
-                 "NACELLE_OBJFUN_MIN_TOC"    ,
-                 "NACELLE_MAX_TWIST"         ]
+optnames_geo = [
+    "AIRFOIL_AREA",
+    "AIRFOIL_THICKNESS",
+    "AIRFOIL_CHORD",
+    "AIRFOIL_LE_RADIUS",
+    "AIRFOIL_TOC",
+    "AIRFOIL_ALPHA",
+    "FUSELAGE_VOLUME",
+    "FUSELAGE_WETTED_AREA",
+    "FUSELAGE_MIN_WIDTH",
+    "FUSELAGE_MAX_WIDTH",
+    "FUSELAGE_MIN_WATERLINE_WIDTH",
+    "FUSELAGE_MAX_WATERLINE_WIDTH",
+    "FUSELAGE_MIN_HEIGHT",
+    "FUSELAGE_MAX_HEIGHT",
+    "FUSELAGE_MAX_CURVATURE",
+    "WING_VOLUME",
+    "WING_MIN_THICKNESS",
+    "WING_MAX_THICKNESS",
+    "WING_MIN_CHORD",
+    "WING_MAX_CHORD",
+    "WING_MIN_LE_RADIUS",
+    "WING_MAX_LE_RADIUS",
+    "WING_MIN_TOC",
+    "WING_MAX_TOC",
+    "WING_OBJFUN_MIN_TOC",
+    "WING_MAX_TWIST",
+    "WING_MAX_CURVATURE",
+    "WING_MAX_DIHEDRAL",
+    "NACELLE_VOLUME",
+    "NACELLE_MIN_THICKNESS",
+    "NACELLE_MAX_THICKNESS",
+    "NACELLE_MIN_CHORD",
+    "NACELLE_MAX_CHORD",
+    "NACELLE_MIN_LE_RADIUS",
+    "NACELLE_MAX_LE_RADIUS",
+    "NACELLE_MIN_TOC",
+    "NACELLE_MAX_TOC",
+    "NACELLE_OBJFUN_MIN_TOC",
+    "NACELLE_MAX_TWIST",
+]
 
 PerStation = []
 for i in range(20):
@@ -278,16 +290,18 @@ def getTurboPerfIndex(nZones = 1):
 #: optnames_geo
 
 # per-surface functions
-per_surface_map = {"LIFT"       :   "CL" ,
-                  "DRAG"        :   "CD" ,
-                  "SIDEFORCE"   :   "CSF"  ,
-                  "MOMENT_X"    :   "CMx"   ,
-                  "MOMENT_Y"    :   "CMy"   ,
-                  "MOMENT_Z"    :   "CMz"   ,
-                  "FORCE_X"     :   "CFx"   ,
-                  "FORCE_Y"     :   "CFy"   ,
-                  "FORCE_Z"     :   "CFz"   ,
-                  "EFFICIENCY"  :   "CL/CD" }
+per_surface_map = {
+    "LIFT": "CL",
+    "DRAG": "CD",
+    "SIDEFORCE": "CSF",
+    "MOMENT_X": "CMx",
+    "MOMENT_Y": "CMy",
+    "MOMENT_Z": "CMz",
+    "FORCE_X": "CFx",
+    "FORCE_Y": "CFy",
+    "FORCE_Z": "CFz",
+    "EFFICIENCY": "CL/CD",
+}
 
 # -------------------------------------------------------------------
 #  Include per-surface output from History File
@@ -297,29 +311,35 @@ def update_persurface(config, state):
     header_map = get_headerMap()
     for base in per_surface_map:
         base2 = per_surface_map[base]
-        for marker in config['MARKER_MONITORING']:
-            if not (base2+'_'+marker) in header_map:
-                header_map[base2+'_'+marker] = base2+'_'+marker
+        for marker in config["MARKER_MONITORING"]:
+            if not (base2 + "_" + marker) in header_map:
+                header_map[base2 + "_" + marker] = base2 + "_" + marker
     # Update the function values in state to include the per-surface quantities
-    if 'DIRECT' in state['HISTORY']:
+    if "DIRECT" in state["HISTORY"]:
         for base in per_surface_map:
             base2 = per_surface_map[base]
-            for marker in config['MARKER_MONITORING']:
-                if (base2+'_'+marker) in state['HISTORY']['DIRECT']:
-                    state['FUNCTIONS'][base2+'_'+marker] = state['HISTORY']['DIRECT'][base2+'_'+marker][-1]
+            for marker in config["MARKER_MONITORING"]:
+                if (base2 + "_" + marker) in state["HISTORY"]["DIRECT"]:
+                    state["FUNCTIONS"][base2 + "_" + marker] = state["HISTORY"][
+                        "DIRECT"
+                    ][base2 + "_" + marker][-1]
+
 
 # -------------------------------------------------------------------
 #  Read Aerodynamic Function Values from History File
 # -------------------------------------------------------------------
 
-def read_aerodynamics( History_filename , nZones = 1, special_cases=[], final_avg=0, wnd_fct = 'SQUARE' ):
-    """ values = read_aerodynamics(historyname, special_cases=[])
-        read aerodynamic function values from history file
 
-        Outputs:
-            dictionary with function keys and thier values
-            if special cases has 'TIME_MARCHING', returns time averaged data
-            otherwise returns final value from history file
+def read_aerodynamics(
+    History_filename, nZones=1, special_cases=[], final_avg=0, wnd_fct="SQUARE"
+):
+    """values = read_aerodynamics(historyname, special_cases=[])
+    read aerodynamic function values from history file
+
+    Outputs:
+        dictionary with function keys and thier values
+        if special cases has 'TIME_MARCHING', returns time averaged data
+        otherwise returns final value from history file
     """
 
     # read the history data
@@ -330,69 +350,101 @@ def read_aerodynamics( History_filename , nZones = 1, special_cases=[], final_av
     for this_objfun in historyOutFields:
         if nZones == 1:
             if this_objfun in history_data:
-                if historyOutFields[this_objfun]['TYPE'] == 'COEFFICIENT' or historyOutFields[this_objfun]['TYPE'] == 'D_COEFFICIENT':
+                if (
+                    historyOutFields[this_objfun]["TYPE"] == "COEFFICIENT"
+                    or historyOutFields[this_objfun]["TYPE"] == "D_COEFFICIENT"
+                ):
                     Func_Values[this_objfun] = history_data[this_objfun]
         else:
             for iZone in range(nZones):
-                if this_objfun + '[' + str(iZone) + ']' in history_data:
-                    if historyOutFields[this_objfun]['TYPE'] == 'COEFFICIENT' or historyOutFields[this_objfun]['TYPE'] == 'D_COEFFICIENT':
-                        Func_Values[this_objfun + '[' + str(iZone) + ']'] = history_data[this_objfun + '[' + str(iZone) + ']']
-
-    if 'TIME_MARCHING' in special_cases:
+                if this_objfun + "[" + str(iZone) + "]" in history_data:
+                    if (
+                        historyOutFields[this_objfun]["TYPE"] == "COEFFICIENT"
+                        or historyOutFields[this_objfun]["TYPE"] == "D_COEFFICIENT"
+                    ):
+                        Func_Values[
+                            this_objfun + "[" + str(iZone) + "]"
+                        ] = history_data[this_objfun + "[" + str(iZone) + "]"]
+
+    if "TIME_MARCHING" in special_cases:
         # for unsteady cases, average time-accurate objective function values
         for key, value in Func_Values.items():
-            if historyOutFields[key]['TYPE'] == 'COEFFICIENT':
-                if not history_data.get('TAVG_'+ key):
-                    raise KeyError('Key ' + historyOutFields['TAVG_'+ key]['HEADER'] + ' was not found in history output.')
-                Func_Values[key] = history_data['TAVG_'+ key][-1]
-            elif historyOutFields[key]['TYPE'] == 'D_COEFFICIENT':
-                if not history_data.get('TAVG_' + key):
-                    raise KeyError('Key ' + historyOutFields['TAVG_' + key]['HEADER'] + ' was not found in history output.')
-                Func_Values[key] = history_data['TAVG_' + key][-1]
+            if historyOutFields[key]["TYPE"] == "COEFFICIENT":
+                if not history_data.get("TAVG_" + key):
+                    raise KeyError(
+                        "Key "
+                        + historyOutFields["TAVG_" + key]["HEADER"]
+                        + " was not found in history output."
+                    )
+                Func_Values[key] = history_data["TAVG_" + key][-1]
+            elif historyOutFields[key]["TYPE"] == "D_COEFFICIENT":
+                if not history_data.get("TAVG_" + key):
+                    raise KeyError(
+                        "Key "
+                        + historyOutFields["TAVG_" + key]["HEADER"]
+                        + " was not found in history output."
+                    )
+                Func_Values[key] = history_data["TAVG_" + key][-1]
     else:
         # in steady cases take only last value.
         for key, value in Func_Values.iteritems():
             if not history_data.get(key):
-                raise KeyError('Key ' + historyOutFields[key]['HEADER'] + ' was not found in history output.')
+                raise KeyError(
+                    "Key "
+                    + historyOutFields[key]["HEADER"]
+                    + " was not found in history output."
+                )
             Func_Values[key] = value[-1]
 
     return Func_Values
 
+
 #: def read_aerodynamics()
 
 # -------------------------------------------------------------------
 #  Get Objective Function Sign
 # -------------------------------------------------------------------
 
-def get_objectiveSign( ObjFun_name ):
-    """ returns -1 for maximization problems:
-            LIFT
-            EFFICIENCY
-            THRUST
-            FIGURE_OF_MERIT
-            MASS_FLOW_RATE
-            SURFACE_TOTAL_PRESSURE
-            SURFACE_STATIC_PRESSURE
-            SURFACE_MASSFLOW
-            SURFACE_MACH
-            TOTAL_STATIC_EFFICIENCY
-        returns +1 otherwise
+
+def get_objectiveSign(ObjFun_name):
+    """returns -1 for maximization problems:
+        LIFT
+        EFFICIENCY
+        THRUST
+        FIGURE_OF_MERIT
+        MASS_FLOW_RATE
+        SURFACE_TOTAL_PRESSURE
+        SURFACE_STATIC_PRESSURE
+        SURFACE_MASSFLOW
+        SURFACE_MACH
+        TOTAL_STATIC_EFFICIENCY
+    returns +1 otherwise
     """
 
     # flip sign for maximization problems
-    if ObjFun_name == "LIFT"            : return -1.0
-    if ObjFun_name == "EFFICIENCY"      : return -1.0
-    if ObjFun_name == "THRUST"          : return -1.0
-    if ObjFun_name == "FIGURE_OF_MERIT" : return -1.0
-    if ObjFun_name == "SURFACE_TOTAL_PRESSURE"  : return -1.0
-    if ObjFun_name == "SURFACE_STATIC_PRESSURE" : return -1.0
-    if ObjFun_name == "SURFACE_MASSFLOW"        : return -1.0
-    if ObjFun_name == "SURFACE_MACH"            : return -1.0
-    if ObjFun_name == "TOTAL_STATIC_EFFICIENCY" :return -1.0
+    if ObjFun_name == "LIFT":
+        return -1.0
+    if ObjFun_name == "EFFICIENCY":
+        return -1.0
+    if ObjFun_name == "THRUST":
+        return -1.0
+    if ObjFun_name == "FIGURE_OF_MERIT":
+        return -1.0
+    if ObjFun_name == "SURFACE_TOTAL_PRESSURE":
+        return -1.0
+    if ObjFun_name == "SURFACE_STATIC_PRESSURE":
+        return -1.0
+    if ObjFun_name == "SURFACE_MASSFLOW":
+        return -1.0
+    if ObjFun_name == "SURFACE_MACH":
+        return -1.0
+    if ObjFun_name == "TOTAL_STATIC_EFFICIENCY":
+        return -1.0
 
     # otherwise
     return 1.0
 
+
 #: def get_objectiveSign()
 
 
@@ -400,16 +452,17 @@ def get_objectiveSign( ObjFun_name ):
 #  Get Constraint Sign
 # -------------------------------------------------------------------
 
-def get_constraintSign( sign ):
-    """ gets +/-1 given a constraint sign < or > respectively
-        inequality constraint is posed as c(x) < 0
+
+def get_constraintSign(sign):
+    """gets +/-1 given a constraint sign < or > respectively
+    inequality constraint is posed as c(x) < 0
     """
-    sign_map = { '>' : -1.0 ,
-                 '<' : +1.0  }
-    assert not sign=='=' , 'Sign "=" not valid'
+    sign_map = {">": -1.0, "<": +1.0}
+    assert not sign == "=", 'Sign "=" not valid'
 
     return sign_map[sign]
 
+
 #: def get_constraintSign()
 
 
@@ -417,68 +470,72 @@ def get_constraintSign( sign ):
 #  Get Adjoint Filename Suffix
 # -------------------------------------------------------------------
 
+
 def get_adjointSuffix(objective_function=None):
-    """ gets the adjoint suffix given an objective function """
+    """gets the adjoint suffix given an objective function"""
 
     # adjoint name map
-    name_map = { "DRAG"                        : "cd"        ,
-                 "LIFT"                        : "cl"        ,
-                 "SIDEFORCE"                   : "csf"       ,
-                 "MOMENT_X"                    : "cmx"       ,
-                 "MOMENT_Y"                    : "cmy"       ,
-                 "MOMENT_Z"                    : "cmz"       ,
-                 "FORCE_X"                     : "cfx"       ,
-                 "FORCE_Y"                     : "cfy"       ,
-                 "FORCE_Z"                     : "cfz"       ,
-                 "EFFICIENCY"                  : "eff"       ,
-                 "INVERSE_DESIGN_PRESSURE"     : "invpress"  ,
-                 "INVERSE_DESIGN_HEAT"         : "invheat"   ,
-                 "MAXIMUM_HEATFLUX"            : "maxheat"   ,
-                 "TOTAL_HEATFLUX"              : "totheat"   ,
-                 "EQUIVALENT_AREA"             : "ea"        ,
-                 "NEARFIELD_PRESSURE"          : "nfp"       ,
-                 "THRUST"                      : "ct"        ,
-                 "TORQUE"                      : "cq"        ,
-                 "FIGURE_OF_MERIT"             : "merit"     ,
-                 "BUFFET"                      : "buffet"    ,
-                 "SURFACE_TOTAL_PRESSURE"      : "pt"        ,
-                 "SURFACE_STATIC_PRESSURE"     : "pe"        ,
-                 "SURFACE_MASSFLOW"            : "mfr"       ,
-                 "SURFACE_MACH"                : "mach"      ,
-                 "SURFACE_UNIFORMITY"          : "uniform"   ,
-                 "SURFACE_SECONDARY"           : "second"    ,
-                 "SURFACE_MOM_DISTORTION"      : "distort"   ,
-                 "SURFACE_SECOND_OVER_UNIFORM" : "sou"       ,
-                 "SURFACE_PRESSURE_DROP"       : "dp"        ,
-                 "CUSTOM_OBJFUNC"              : "custom"    ,
-                 "KINETIC_ENERGY_LOSS"         : "ke"        ,
-                 "TOTAL_PRESSURE_LOSS"         : "pl"        ,
-                 "ENTROPY_GENERATION"          : "entg"      ,
-                 "EULERIAN_WORK"               : "ew"        ,
-                 "FLOW_ANGLE_OUT"              : "fao"       ,
-                 "FLOW_ANGLE_IN"               : "fai"       ,
-                 "MASS_FLOW_OUT"               : "mfo"       ,
-                 "MASS_FLOW_IN"                : "mfi"       ,
-                 "TOTAL_EFFICIENCY"            : "teff"      ,
-                 "TOTAL_STATIC_EFFICIENCY"     : "tseff"     ,
-                 "COMBO"                       : "combo"}
+    name_map = {
+        "DRAG": "cd",
+        "LIFT": "cl",
+        "SIDEFORCE": "csf",
+        "MOMENT_X": "cmx",
+        "MOMENT_Y": "cmy",
+        "MOMENT_Z": "cmz",
+        "FORCE_X": "cfx",
+        "FORCE_Y": "cfy",
+        "FORCE_Z": "cfz",
+        "EFFICIENCY": "eff",
+        "INVERSE_DESIGN_PRESSURE": "invpress",
+        "INVERSE_DESIGN_HEAT": "invheat",
+        "MAXIMUM_HEATFLUX": "maxheat",
+        "TOTAL_HEATFLUX": "totheat",
+        "EQUIVALENT_AREA": "ea",
+        "NEARFIELD_PRESSURE": "nfp",
+        "THRUST": "ct",
+        "TORQUE": "cq",
+        "FIGURE_OF_MERIT": "merit",
+        "BUFFET": "buffet",
+        "SURFACE_TOTAL_PRESSURE": "pt",
+        "SURFACE_STATIC_PRESSURE": "pe",
+        "SURFACE_MASSFLOW": "mfr",
+        "SURFACE_MACH": "mach",
+        "SURFACE_UNIFORMITY": "uniform",
+        "SURFACE_SECONDARY": "second",
+        "SURFACE_MOM_DISTORTION": "distort",
+        "SURFACE_SECOND_OVER_UNIFORM": "sou",
+        "SURFACE_PRESSURE_DROP": "dp",
+        "CUSTOM_OBJFUNC": "custom",
+        "KINETIC_ENERGY_LOSS": "ke",
+        "TOTAL_PRESSURE_LOSS": "pl",
+        "ENTROPY_GENERATION": "entg",
+        "EULERIAN_WORK": "ew",
+        "FLOW_ANGLE_OUT": "fao",
+        "FLOW_ANGLE_IN": "fai",
+        "MASS_FLOW_OUT": "mfo",
+        "MASS_FLOW_IN": "mfi",
+        "TOTAL_EFFICIENCY": "teff",
+        "TOTAL_STATIC_EFFICIENCY": "tseff",
+        "COMBO": "combo",
+    }
 
     # if none or false, return map
     if not objective_function:
         return name_map
     else:
         # remove white space
-        objective = ''.join(objective_function.split())
+        objective = "".join(objective_function.split())
         objective = objective.split(",")
         nObj = len(objective)
-        if (nObj>1):
+        if nObj > 1:
             return "combo"
         if objective[0] in name_map:
             return name_map[objective[0]]
 
         # otherwise...
         else:
-            raise Exception('Unrecognized adjoint function name')
+            raise Exception("Unrecognized adjoint function name")
+
 
 #: def get_adjointSuffix()
 
@@ -486,388 +543,483 @@ def get_adjointSuffix(objective_function=None):
 #  Add a Suffix
 # -------------------------------------------------------------------
 
-def add_suffix(base_name,suffix):
-    """ suffix_name = add_suffix(base_name,suffix)
-        adds suffix to a filename, accounting for file type extension
-        example:
-            base_name   = 'input.txt'
-            suffix      = 'new'
-            suffix_name = 'input_new.txt'
+
+def add_suffix(base_name, suffix):
+    """suffix_name = add_suffix(base_name,suffix)
+    adds suffix to a filename, accounting for file type extension
+    example:
+        base_name   = 'input.txt'
+        suffix      = 'new'
+        suffix_name = 'input_new.txt'
     """
     if isinstance(base_name, list):
         suffix_name = []
         for name in base_name:
             name_split = os.path.splitext(name)
-            suffix_name.append(name_split[0] + '_' + suffix + name_split[1])
+            suffix_name.append(name_split[0] + "_" + suffix + name_split[1])
     else:
         base_name = os.path.splitext(base_name)
-        suffix_name = base_name[0] + '_' + suffix + base_name[1]
+        suffix_name = base_name[0] + "_" + suffix + base_name[1]
 
     return suffix_name
 
-#: def add_suffix()
 
+#: def add_suffix()
 
 
 # -------------------------------------------------------------------
 #  Get Design Variable ID Map
 # -------------------------------------------------------------------
 
+
 def get_dvMap():
-    """ get dictionary that maps design variable
-        kind id number to name """
-    dv_map = { 0   : "NO_DEFORMATION"        ,
-               1   : "TRANSLATION"           ,
-               2   : "ROTATION"              ,
-               3   : "SCALE"                 ,
-               10  : "FFD_SETTING"           ,
-               11  : "FFD_CONTROL_POINT"     ,
-               12  : "FFD_NACELLE"           ,
-               13  : "FFD_GULL"              ,
-               14  : "FFD_CAMBER"            ,
-               15  : "FFD_TWIST"             ,
-               16  : "FFD_THICKNESS"         ,
-               18  : "FFD_ROTATION"          ,
-               19  : "FFD_CONTROL_POINT_2D"  ,
-               20  : "FFD_CAMBER_2D"         ,
-               21  : "FFD_THICKNESS_2D"      ,
-               22  : "FFD_TWIST_2D"          ,
-               23  : "FFD_CONTROL_SURFACE"   ,
-               24  : "FFD_ANGLE_OF_ATTACK"   ,
-               30  : "HICKS_HENNE"           ,
-               31  : "PARABOLIC"             ,
-               32  : "NACA_4DIGITS"          ,
-               33  : "AIRFOIL"               ,
-               34  : "CST"                   ,
-               35  : "SURFACE_BUMP"          ,
-               36  : "SURFACE_FILE"          ,
-               40  : "DV_EFIELD"             ,
-               41  : "DV_YOUNG"              ,
-               42  : "DV_POISSON"            ,
-               43  : "DV_RHO"                ,
-               44  : "DV_RHO_DL"             ,
-               50  : "TRANSLATE_GRID"        ,
-               51  : "ROTATE_GRID"           ,
-               52  : "SCALE_GRID"            ,
-               101 : "ANGLE_OF_ATTACK"       }
+    """get dictionary that maps design variable
+    kind id number to name"""
+    dv_map = {
+        0: "NO_DEFORMATION",
+        1: "TRANSLATION",
+        2: "ROTATION",
+        3: "SCALE",
+        10: "FFD_SETTING",
+        11: "FFD_CONTROL_POINT",
+        12: "FFD_NACELLE",
+        13: "FFD_GULL",
+        14: "FFD_CAMBER",
+        15: "FFD_TWIST",
+        16: "FFD_THICKNESS",
+        18: "FFD_ROTATION",
+        19: "FFD_CONTROL_POINT_2D",
+        20: "FFD_CAMBER_2D",
+        21: "FFD_THICKNESS_2D",
+        22: "FFD_TWIST_2D",
+        23: "FFD_CONTROL_SURFACE",
+        24: "FFD_ANGLE_OF_ATTACK",
+        30: "HICKS_HENNE",
+        31: "PARABOLIC",
+        32: "NACA_4DIGITS",
+        33: "AIRFOIL",
+        34: "CST",
+        35: "SURFACE_BUMP",
+        36: "SURFACE_FILE",
+        40: "DV_EFIELD",
+        41: "DV_YOUNG",
+        42: "DV_POISSON",
+        43: "DV_RHO",
+        44: "DV_RHO_DL",
+        50: "TRANSLATE_GRID",
+        51: "ROTATE_GRID",
+        52: "SCALE_GRID",
+        101: "ANGLE_OF_ATTACK",
+    }
 
     return dv_map
 
+
 #: def get_dvMap()
 
 # -------------------------------------------------------------------
 #  Get Design Variable Kind Name from ID
 # -------------------------------------------------------------------
-def get_dvKind( kindID ):
-    """ get design variable kind name from id number """
+def get_dvKind(kindID):
+    """get design variable kind name from id number"""
     dv_map = get_dvMap()
     try:
-        return dv_map[ kindID ]
+        return dv_map[kindID]
     except KeyError:
-        raise Exception('Unrecognized Design Variable ID')
+        raise Exception("Unrecognized Design Variable ID")
+
+
 # def get_dvKind()
 
 # -------------------------------------------------------------------
 #  Get Design Variable Kind ID from Name
 # -------------------------------------------------------------------
-def get_dvID( kindName ):
-    """ get design variable kind id number from name """
+def get_dvID(kindName):
+    """get design variable kind id number from name"""
     dv_map = get_dvMap()
-    id_map = dict((v,k) for (k,v) in dv_map.items())
+    id_map = dict((v, k) for (k, v) in dv_map.items())
     try:
-        return id_map[ kindName ]
+        return id_map[kindName]
     except KeyError:
-        raise Exception('Unrecognized Design Variable Name: %s' , kindName)
-#: def get_dvID()
+        raise Exception("Unrecognized Design Variable Name: %s", kindName)
 
 
+#: def get_dvID()
+
 
 # -------------------------------------------------------------------
 #  Get Gradient File Header
 # -------------------------------------------------------------------
 
-def get_gradFileFormat(grad_type,plot_format,kindID,special_cases=[]):
+
+def get_gradFileFormat(grad_type, plot_format, kindID, special_cases=[]):
 
     # start header, build a list of strings and join at the end
-    header       = []
+    header = []
     write_format = []
 
     # handle plot formating
-    if (plot_format == 'TECPLOT'):
-        header.append('VARIABLES=')
-    elif (plot_format == 'CSV'):
+    if plot_format == "TECPLOT":
+        header.append("VARIABLES=")
+    elif plot_format == "CSV":
         pass
-    else: raise Exception('output plot format not recognized')
+    else:
+        raise Exception("output plot format not recognized")
 
     # Case: continuous adjoint
-    if grad_type == 'CONTINUOUS_ADJOINT':
+    if grad_type == "CONTINUOUS_ADJOINT":
         header.append(r'"iVar","Gradient","FinDiff_Step"')
-        write_format.append(r'%4d, %.10f, %f')
+        write_format.append(r"%4d, %.10f, %f")
 
     # Case: finite difference
-    elif grad_type == 'FINITE_DIFFERENCE':
-        header.append(r'"iVar","Grad_CL","Grad_CD","Grad_CSF","Grad_CMx","Grad_CMy","Grad_CMz","Grad_CFx","Grad_CFy","Grad_CFz","Grad_CL/CD","Grad_Custom_ObjFunc","Grad_HeatFlux_Total","Grad_HeatFlux_Maximum","Grad_Temperature_Total"')
-        write_format.append(r'%4d, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f')
+    elif grad_type == "FINITE_DIFFERENCE":
+        header.append(
+            r'"iVar","Grad_CL","Grad_CD","Grad_CSF","Grad_CMx","Grad_CMy","Grad_CMz","Grad_CFx","Grad_CFy","Grad_CFz","Grad_CL/CD","Grad_Custom_ObjFunc","Grad_HeatFlux_Total","Grad_HeatFlux_Maximum","Grad_Temperature_Total"'
+        )
+        write_format.append(
+            r"%4d, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f"
+        )
 
         for key in special_cases:
-            if key == "ROTATING_FRAME" :
+            if key == "ROTATING_FRAME":
                 header.append(r',"Grad_CMerit","Grad_CT","Grad_CQ"')
                 write_format.append(", %.10f, %.10f, %.10f")
-            if key == "EQUIV_AREA"     :
+            if key == "EQUIV_AREA":
                 header.append(r',"Grad_CEquivArea","Grad_CNearFieldOF"')
                 write_format.append(", %.10f, %.10f")
-            if key == "ENGINE"     :
-                header.append(r',"Grad_AeroCDrag","Grad_SolidCDrag","Grad_Radial_Distortion","Grad_Circumferential_Distortion"')
+            if key == "ENGINE":
+                header.append(
+                    r',"Grad_AeroCDrag","Grad_SolidCDrag","Grad_Radial_Distortion","Grad_Circumferential_Distortion"'
+                )
                 write_format.append(", %.10f, %.10f, %.10f, %.10f")
-            if key == "1D_OUTPUT"     :
-                header.append(r',"Grad_Avg_TotalPress","Grad_Avg_Mach","Grad_Avg_Temperature","Grad_MassFlowRate","Grad_Avg_Pressure","Grad_Avg_Density","Grad_Avg_Velocity","Grad_Avg_Enthalpy"')
-                write_format.append(", %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f")
-            if key == "INV_DESIGN_CP"     :
+            if key == "1D_OUTPUT":
+                header.append(
+                    r',"Grad_Avg_TotalPress","Grad_Avg_Mach","Grad_Avg_Temperature","Grad_MassFlowRate","Grad_Avg_Pressure","Grad_Avg_Density","Grad_Avg_Velocity","Grad_Avg_Enthalpy"'
+                )
+                write_format.append(
+                    ", %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f"
+                )
+            if key == "INV_DESIGN_CP":
                 header.append(r',"Grad_Cp_Diff"')
                 write_format.append(", %.10f")
-            if key == "INV_DESIGN_HEATFLUX"     :
+            if key == "INV_DESIGN_HEATFLUX":
                 header.append(r',"Grad_HeatFlux_Diff"')
                 write_format.append(", %.10f")
 
     # otherwise...
-    else: raise Exception('Unrecognized Gradient Type')
+    else:
+        raise Exception("Unrecognized Gradient Type")
 
     # design variable parameters
-    if kindID == "FFD_CONTROL_POINT_2D"  :
+    if kindID == "FFD_CONTROL_POINT_2D":
         header.append(r',"FFD_Box_ID","xIndex","yIndex","xAxis","yAxis"')
-        write_format.append(r', %s, %s, %s, %s, %s')
-    elif kindID == "FFD_CAMBER_2D"         :
+        write_format.append(r", %s, %s, %s, %s, %s")
+    elif kindID == "FFD_CAMBER_2D":
         header.append(r',"FFD_Box_ID","xIndex"')
-        write_format.append(r', %s, %s')
-    elif kindID == "FFD_THICKNESS_2D"      :
+        write_format.append(r", %s, %s")
+    elif kindID == "FFD_THICKNESS_2D":
         header.append(r',"FFD_Box_ID","xIndex"')
-        write_format.append(r', %s, %s')
-    elif kindID == "HICKS_HENNE"        :
+        write_format.append(r", %s, %s")
+    elif kindID == "HICKS_HENNE":
         header.append(r',"Up/Down","Loc_Max"')
-        write_format.append(r', %s, %s')
-    elif kindID == "SURFACE_BUMP"        :
+        write_format.append(r", %s, %s")
+    elif kindID == "SURFACE_BUMP":
         header.append(r',"Loc_Start","Loc_End","Loc_Max"')
-        write_format.append(r', %s, %s, %s')
-    elif kindID == "CST"        :
+        write_format.append(r", %s, %s, %s")
+    elif kindID == "CST":
         header.append(r',"Up/Down","Kulfan number", "Total Kulfan numbers"')
-        write_format.append(r', %s, %s', '%s')
-    elif kindID == "FAIRING"       :
+        write_format.append(r", %s, %s", "%s")
+    elif kindID == "FAIRING":
         header.append(r',"ControlPoint_Index","Theta_Disp","R_Disp"')
-        write_format.append(r', %s, %s, %s')
-    elif kindID == "NACA_4DIGITS"       :
+        write_format.append(r", %s, %s, %s")
+    elif kindID == "NACA_4DIGITS":
         header.append(r',"1st_digit","2nd_digit","3rd&4th_digits"')
-        write_format.append(r', %s, %s, %s')
-    elif kindID == "TRANSLATION"       :
+        write_format.append(r", %s, %s, %s")
+    elif kindID == "TRANSLATION":
         header.append(r',"x_Disp","y_Disp","z_Disp"')
-        write_format.append(r', %s, %s, %s')
-    elif kindID == "ROTATION"           :
+        write_format.append(r", %s, %s, %s")
+    elif kindID == "ROTATION":
         header.append(r',"x_Orig","y_Orig","z_Orig","x_End","y_End","z_End"')
-        write_format.append(r', %s, %s, %s, %s, %s, %s')
-    elif kindID == "FFD_CONTROL_POINT"  :
-        header.append(r',"FFD_Box_ID","xIndex","yIndex","zIndex","xAxis","yAxis","zAxis"')
-        write_format.append(r', %s, %s, %s, %s, %s, %s, %s')
-    elif kindID == "FFD_DIHEDRAL_ANGLE" :
-        header.append(r',"FFD_Box_ID","x_Orig","y_Orig","z_Orig","x_End","y_End","z_End"')
-        write_format.append(r', %s, %s, %s, %s, %s, %s, %s')
-    elif kindID == "FFD_TWIST_ANGLE"    :
-        header.append(r',"FFD_Box_ID","x_Orig","y_Orig","z_Orig","x_End","y_End","z_End"')
-        write_format.append(r', %s, %s, %s, %s, %s, %s, %s')
-    elif kindID == "FFD_ROTATION"       :
-        header.append(r',"FFD_Box_ID","x_Orig","y_Orig","z_Orig","x_End","y_End","z_End"')
-        write_format.append(r', %s, %s, %s, %s, %s, %s, %s')
-    elif kindID == "FFD_CAMBER"         :
+        write_format.append(r", %s, %s, %s, %s, %s, %s")
+    elif kindID == "FFD_CONTROL_POINT":
+        header.append(
+            r',"FFD_Box_ID","xIndex","yIndex","zIndex","xAxis","yAxis","zAxis"'
+        )
+        write_format.append(r", %s, %s, %s, %s, %s, %s, %s")
+    elif kindID == "FFD_DIHEDRAL_ANGLE":
+        header.append(
+            r',"FFD_Box_ID","x_Orig","y_Orig","z_Orig","x_End","y_End","z_End"'
+        )
+        write_format.append(r", %s, %s, %s, %s, %s, %s, %s")
+    elif kindID == "FFD_TWIST_ANGLE":
+        header.append(
+            r',"FFD_Box_ID","x_Orig","y_Orig","z_Orig","x_End","y_End","z_End"'
+        )
+        write_format.append(r", %s, %s, %s, %s, %s, %s, %s")
+    elif kindID == "FFD_ROTATION":
+        header.append(
+            r',"FFD_Box_ID","x_Orig","y_Orig","z_Orig","x_End","y_End","z_End"'
+        )
+        write_format.append(r", %s, %s, %s, %s, %s, %s, %s")
+    elif kindID == "FFD_CAMBER":
         header.append(r',"FFD_Box_ID","xIndex","yIndex"')
-        write_format.append(r', %s, %s, %s')
-    elif kindID == "FFD_THICKNESS"      :
+        write_format.append(r", %s, %s, %s")
+    elif kindID == "FFD_THICKNESS":
         header.append(r',"FFD_Box_ID","xIndex","yIndex"')
-        write_format.append(r', %s, %s, %s')
-    elif kindID == "ANGLE_OF_ATTACK"      : pass
-    elif kindID == "FFD_ANGLE_OF_ATTACK"  : pass
+        write_format.append(r", %s, %s, %s")
+    elif kindID == "ANGLE_OF_ATTACK":
+        pass
+    elif kindID == "FFD_ANGLE_OF_ATTACK":
+        pass
 
     # otherwise...
-    else: raise Exception('Unrecognized Design Variable Kind')
+    else:
+        raise Exception("Unrecognized Design Variable Kind")
 
     # finite difference step
-    if grad_type == 'FINITE_DIFFERENCE':
+    if grad_type == "FINITE_DIFFERENCE":
         header.append(r',"FinDiff_Step"')
-        write_format.append(r', %.10f')
+        write_format.append(r", %.10f")
 
     # finish format
-    header.append('\n')
-    write_format.append('\n')
+    header.append("\n")
+    write_format.append("\n")
 
-    header       = ''.join(header)
-    write_format = ''.join(write_format)
+    header = "".join(header)
+    write_format = "".join(write_format)
 
-    return [header,write_format]
+    return [header, write_format]
 
-#: def get_gradFileFormat()
 
+#: def get_gradFileFormat()
 
 
 # -------------------------------------------------------------------
 #  Get Optimization File Header
 # -------------------------------------------------------------------
 
-def get_optFileFormat(plot_format,special_cases=None, nZones = 1):
 
-    if special_cases is None: special_cases = []
+def get_optFileFormat(plot_format, special_cases=None, nZones=1):
+
+    if special_cases is None:
+        special_cases = []
 
     # start header, build a list of strings and join at the end
-    header_list   = []
-    header_format = ''
-    write_format  = []
+    header_list = []
+    header_format = ""
+    write_format = []
 
     # handle plot formating
-    if (plot_format == 'TECPLOT'):
-        header_format = header_format + 'VARIABLES='
-    elif (plot_format == 'CSV'):
+    if plot_format == "TECPLOT":
+        header_format = header_format + "VARIABLES="
+    elif plot_format == "CSV":
         pass
-    else: raise Exception('output plot format not recognized')
+    else:
+        raise Exception("output plot format not recognized")
 
     # start header
-    header_list.extend(["Iteration","CL","CD","CSF","CMx","CMy","CMz","CFx","CFy","CFz","CL/CD","Custom_ObjFunc","HeatFlux_Total","HeatFlux_Maximum","Temperature_Total"])
-    write_format.append(r'%4d, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f')
+    header_list.extend(
+        [
+            "Iteration",
+            "CL",
+            "CD",
+            "CSF",
+            "CMx",
+            "CMy",
+            "CMz",
+            "CFx",
+            "CFy",
+            "CFz",
+            "CL/CD",
+            "Custom_ObjFunc",
+            "HeatFlux_Total",
+            "HeatFlux_Maximum",
+            "Temperature_Total",
+        ]
+    )
+    write_format.append(
+        r"%4d, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f"
+    )
 
     # special cases
     for key in special_cases:
-        if key == "ROTATING_FRAME" :
-            header_list.extend(["CMerit","CT","CQ"])
-            write_format.append(r', %.10f, %.10f, %.10f')
-        if key == "EQUIV_AREA"     :
-            header_list.extend(["CEquivArea","CNearFieldOF"])
-            write_format.append(r', %.10f, %.10f')
-        if key == "ENGINE"     :
-            header_list.extend(["AeroCDrag","SolidCDrag","Radial_Distortion","Circumferential_Distortion"])
-            write_format.append(r', %.10f, %.10f, %.10f, %.10f')
+        if key == "ROTATING_FRAME":
+            header_list.extend(["CMerit", "CT", "CQ"])
+            write_format.append(r", %.10f, %.10f, %.10f")
+        if key == "EQUIV_AREA":
+            header_list.extend(["CEquivArea", "CNearFieldOF"])
+            write_format.append(r", %.10f, %.10f")
+        if key == "ENGINE":
+            header_list.extend(
+                [
+                    "AeroCDrag",
+                    "SolidCDrag",
+                    "Radial_Distortion",
+                    "Circumferential_Distortion",
+                ]
+            )
+            write_format.append(r", %.10f, %.10f, %.10f, %.10f")
         if key == "1D_OUTPUT":
-            header_list.extend(["AreaAvg_TotalPress","AreaAvg_Mach","AreaAvg_Temperature","MassFlowRate","Avg_Pressure","Avg_Density","Avg_Velocity","Avg_Enthalpy"])
-            write_format.append(r', %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f')
-        if key == "INV_DESIGN_CP"     :
+            header_list.extend(
+                [
+                    "AreaAvg_TotalPress",
+                    "AreaAvg_Mach",
+                    "AreaAvg_Temperature",
+                    "MassFlowRate",
+                    "Avg_Pressure",
+                    "Avg_Density",
+                    "Avg_Velocity",
+                    "Avg_Enthalpy",
+                ]
+            )
+            write_format.append(
+                r", %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f, %.10f"
+            )
+        if key == "INV_DESIGN_CP":
             header_list.extend(["Cp_Diff"])
-            write_format.append(r', %.10f')
-        if key == "INV_DESIGN_HEATFLUX"     :
+            write_format.append(r", %.10f")
+        if key == "INV_DESIGN_HEATFLUX":
             header_list.extend(["HeatFlux_Diff"])
-            write_format.append(r', %.10f')
+            write_format.append(r", %.10f")
 
     # finish formats
-    header_format = (header_format) + ('"') + ('","').join(header_list) + ('"') + (' \n')
-    write_format  = ''.join(write_format)  + ' \n'
+    header_format = (
+        (header_format) + ('"') + ('","').join(header_list) + ('"') + (" \n")
+    )
+    write_format = "".join(write_format) + " \n"
 
     # build list of objective function names
     header_vars = []
     map_dict = get_headerMap(nZones)
     for variable in header_list:
-        assert variable in map_dict, 'unrecognized header variable'
+        assert variable in map_dict, "unrecognized header variable"
         header_vars.append(map_dict[variable])
 
     # done
-    return [header_format,header_vars,write_format]
+    return [header_format, header_vars, write_format]
 
-#: def get_optFileFormat()
 
+#: def get_optFileFormat()
 
 
 # -------------------------------------------------------------------
 #  Get Extension Name
 # -------------------------------------------------------------------
 
+
 def get_extension(output_format):
 
-    if (output_format == "PARAVIEW")        : return ".csv"
-    if (output_format == "PARAVIEW_BINARY") : return ".csv"
-    if (output_format == "TECPLOT")         : return ".dat"
-    if (output_format == "TECPLOT_BINARY")  : return ".szplt"
-    if (output_format == "SOLUTION")        : return ".dat"
-    if (output_format == "RESTART")         : return ".dat"
-    if (output_format == "CONFIG")          : return ".cfg"
-    if (output_format == "CSV")         : return ".csv"
+    if output_format == "PARAVIEW":
+        return ".csv"
+    if output_format == "PARAVIEW_BINARY":
+        return ".csv"
+    if output_format == "TECPLOT":
+        return ".dat"
+    if output_format == "TECPLOT_BINARY":
+        return ".szplt"
+    if output_format == "SOLUTION":
+        return ".dat"
+    if output_format == "RESTART":
+        return ".dat"
+    if output_format == "CONFIG":
+        return ".cfg"
+    if output_format == "CSV":
+        return ".csv"
     # otherwise
     raise Exception("Output Format Unknown")
 
-#: def get_extension()
 
+#: def get_extension()
 
 
 # -------------------------------------------------------------------
 #  Check Special Case
 # -------------------------------------------------------------------
 def get_specialCases(config):
-    """ returns a list of special physical problems that were
-        specified in the config file, and set to 'yes'
+    """returns a list of special physical problems that were
+    specified in the config file, and set to 'yes'
     """
 
-    all_special_cases = [ 'ROTATING_FRAME'                   ,
-                          'EQUIV_AREA'                       ,
-                          '1D_OUTPUT'                        ,
-                          'INV_DESIGN_CP'                    ,
-                          'INV_DESIGN_HEATFLUX'              ]
+    all_special_cases = [
+        "ROTATING_FRAME",
+        "EQUIV_AREA",
+        "1D_OUTPUT",
+        "INV_DESIGN_CP",
+        "INV_DESIGN_HEATFLUX",
+    ]
 
     special_cases = []
     for key in all_special_cases:
-        if key in config and config[key] == 'YES':
+        if key in config and config[key] == "YES":
             special_cases.append(key)
-        if 'SOLVER' in config and config['SOLVER'] == key:
+        if "SOLVER" in config and config["SOLVER"] == key:
             special_cases.append(key)
 
-    if config.get('TIME_MARCHING','NO') != 'NO':
-        special_cases.append('TIME_MARCHING')
+    if config.get("TIME_MARCHING", "NO") != "NO":
+        special_cases.append("TIME_MARCHING")
 
     # no support for more than one special case
     if len(special_cases) > 1:
-        error_str = 'Currently cannot support ' + ' and '.join(special_cases) + ' at once'
+        error_str = (
+            "Currently cannot support " + " and ".join(special_cases) + " at once"
+        )
         raise Exception(error_str)
 
     # Special case for harmonic balance
-    if 'TIME_MARCHING' in config and config['TIME_MARCHING'] == 'HARMONIC_BALANCE':
-        special_cases.append('HARMONIC_BALANCE')
+    if "TIME_MARCHING" in config and config["TIME_MARCHING"] == "HARMONIC_BALANCE":
+        special_cases.append("HARMONIC_BALANCE")
 
     # Special case for rotating frame
-    if 'GRID_MOVEMENT_KIND' in config and config['GRID_MOVEMENT_KIND'] == 'ROTATING_FRAME':
-        special_cases.append('ROTATING_FRAME')
+    if (
+        "GRID_MOVEMENT_KIND" in config
+        and config["GRID_MOVEMENT_KIND"] == "ROTATING_FRAME"
+    ):
+        special_cases.append("ROTATING_FRAME")
 
     return special_cases
 
+
 #: def get_specialCases()
 
 # -------------------------------------------------------------------
 #  Check Fluid Structure Interaction
 # -------------------------------------------------------------------
 def get_multizone(config):
-    """ returns a list of special physical problems that were
-        specified in the config file, and set to 'yes'
+    """returns a list of special physical problems that were
+    specified in the config file, and set to 'yes'
     """
 
-    all_multizone_problems = ['FLUID_STRUCTURE_INTERACTION']
+    all_multizone_problems = ["FLUID_STRUCTURE_INTERACTION"]
 
     multizone = []
     for key in all_multizone_problems:
-        if 'SOLVER' in config and config['SOLVER'] == key:
+        if "SOLVER" in config and config["SOLVER"] == key:
             multizone.append(key)
 
     return multizone
 
+
 #: def get_multizone()
 
 
-def next_folder(folder_format,num_format='%03d'):
-    """ folder = next_folder(folder_format,num_format='%03d')
-        finds the next folder with given format
+def next_folder(folder_format, num_format="%03d"):
+    """folder = next_folder(folder_format,num_format='%03d')
+    finds the next folder with given format
 
-        Inputs:
-            folder_format - folder name with wild card (*) to mark expansion
-            num_format    - %d formating to expand the wild card with
+    Inputs:
+        folder_format - folder name with wild card (*) to mark expansion
+        num_format    - %d formating to expand the wild card with
 
-        Outputs:
-            folder - a folder with the next index number inserted in
-            the wild card, first index is 1
+    Outputs:
+        folder - a folder with the next index number inserted in
+        the wild card, first index is 1
     """
 
-    assert '*' in folder_format , 'wildcard (*) missing in folder_format name'
+    assert "*" in folder_format, "wildcard (*) missing in folder_format name"
 
     folders = glob.glob(folder_format)
-    split   = folder_format.split('*')
-    folder  = folder_format.replace('*',num_format)
+    split = folder_format.split("*")
+    folder = folder_format.replace("*", num_format)
 
     if folders:
         # find folder number, could be done with regex...
@@ -881,7 +1033,7 @@ def next_folder(folder_format,num_format='%03d'):
         max_i = int(max_folder)
 
         # increment folder number
-        folder = folder % (max_i+1)
+        folder = folder % (max_i + 1)
     else:
         # first folder, number 1
         folder = folder % 1
@@ -889,23 +1041,27 @@ def next_folder(folder_format,num_format='%03d'):
     return folder
 
 
-def expand_part(name,config):
+def expand_part(name, config):
     names = [name]
     return names
 
-def expand_time(name,config):
-    if 'TIME_MARCHING' in get_specialCases(config):
-        n_time = config['UNST_ADJOINT_ITER']
+
+def expand_time(name, config):
+    if "TIME_MARCHING" in get_specialCases(config):
+        n_time = config["UNST_ADJOINT_ITER"]
         n_start_time = 0
-        if config.get('TIME_DOMAIN', 'NO') == 'YES' and config.get('RESTART_SOL','NO') == 'YES':
-            n_start_time = int(config['RESTART_ITER'])
+        if (
+            config.get("TIME_DOMAIN", "NO") == "YES"
+            and config.get("RESTART_SOL", "NO") == "YES"
+        ):
+            n_start_time = int(config["RESTART_ITER"])
         if not isinstance(name, list):
-            name_pat = add_suffix(name,'%05d')
-            names = [name_pat%i for i in range(n_start_time, n_time)]
+            name_pat = add_suffix(name, "%05d")
+            names = [name_pat % i for i in range(n_start_time, n_time)]
         else:
             for n in range(len(name)):
-                name_pat = add_suffix(name[n], '%05d')
-                names    = [name_pat%i for i in range(n_start_time, n_time)]
+                name_pat = add_suffix(name[n], "%05d")
+                names = [name_pat % i for i in range(n_start_time, n_time)]
     else:
         if not isinstance(name, list):
             names = [name]
@@ -913,16 +1069,17 @@ def expand_time(name,config):
             names = name
     return names
 
+
 def expand_zones(name, config):
     names = []
     if int(config.NZONES) > 1:
         if not isinstance(name, list):
-            name_pat = add_suffix(name,'%d')
-            names = [name_pat%i for i in range(int(config.NZONES))]
+            name_pat = add_suffix(name, "%d")
+            names = [name_pat % i for i in range(int(config.NZONES))]
         else:
             for n in range(len(name)):
-                name_pat = add_suffix(name[n], '%d')
-                names.extend([name_pat%i for i in range(int(config.NZONES))])
+                name_pat = add_suffix(name[n], "%d")
+                names.extend([name_pat % i for i in range(int(config.NZONES))])
 
     else:
         if not isinstance(name, list):
@@ -931,34 +1088,35 @@ def expand_zones(name, config):
             names = name
     return names
 
-def expand_multipoint(name,config):
-    def_objs = config['OPT_OBJECTIVE']
+
+def expand_multipoint(name, config):
+    def_objs = config["OPT_OBJECTIVE"]
     objectives = def_objs.keys()
     names = []
-    n_multipoint = len(config['MULTIPOINT_WEIGHT'].split(','))
+    n_multipoint = len(config["MULTIPOINT_WEIGHT"].split(","))
 
     if any(elem in optnames_multi for elem in objectives):
         if not isinstance(name, list):
-            if '_point0' not in name:
-                name_pat = add_suffix(name,'point%d')
-                names = [name_pat%i for i in range(n_multipoint)]
+            if "_point0" not in name:
+                name_pat = add_suffix(name, "point%d")
+                names = [name_pat % i for i in range(n_multipoint)]
             else:
-                name_parts = name.split('_point0')
+                name_parts = name.split("_point0")
                 name_base = name_parts[0]
                 name_suff = name_parts[1]
-                name_pat = name_base + '_point%d' + name_suff
-                names = [name_pat%i for i in range(n_multipoint)]
+                name_pat = name_base + "_point%d" + name_suff
+                names = [name_pat % i for i in range(n_multipoint)]
         else:
             for n in range(len(name)):
-                if '_point0' not in name:
-                    name_pat = add_suffix(name[n], 'point%d')
-                    names.extend([name_pat%i for i in range(n_multipoint)])
+                if "_point0" not in name:
+                    name_pat = add_suffix(name[n], "point%d")
+                    names.extend([name_pat % i for i in range(n_multipoint)])
                 else:
-                    name_parts = name[n].split('_point0')
+                    name_parts = name[n].split("_point0")
                     name_base = name_parts[0]
                     name_suff = name_parts[1]
-                    name_pat = name_base + '_point%d' + name_suff
-                    names.extend([name_pat%i for i in range(n_multipoint)])
+                    name_pat = name_base + "_point%d" + name_suff
+                    names.extend([name_pat % i for i in range(n_multipoint)])
     else:
         if not isinstance(name, list):
             names = [name]
@@ -967,23 +1125,23 @@ def expand_multipoint(name,config):
     return names
 
 
+def make_link(src, dst):
+    """make_link(src,dst)
+    makes a relative link
+    Inputs:
+        src - source file
+        dst - destination to place link
 
-def make_link(src,dst):
-    """ make_link(src,dst)
-        makes a relative link
-        Inputs:
-            src - source file
-            dst - destination to place link
-
-        Windows links currently unsupported, will copy file instead
+    Windows links currently unsupported, will copy file instead
     """
 
-    if os.path.exists(src): # , 'source file does not exist \n%s' % src
+    if os.path.exists(src):  # , 'source file does not exist \n%s' % src
 
-        if os.name == 'nt':
+        if os.name == "nt":
             # can't make a link in windows, need to look for other options
-            if os.path.exists(dst): os.remove(dst)
-            shutil.copy(src,dst)
+            if os.path.exists(dst):
+                os.remove(dst)
+            shutil.copy(src, dst)
 
         else:
             # find real file, incase source itself is a link
@@ -994,91 +1152,99 @@ def make_link(src,dst):
             dst = os.path.normpath(dst)
 
             # check for self referencing
-            if src == dst: return
+            if src == dst:
+                return
 
             # find relative folder path
-            srcfolder = os.path.join( os.path.split(src)[0] ) + '/'
-            dstfolder = os.path.join( os.path.split(dst)[0] ) + '/'
-            srcfolder = os.path.relpath(srcfolder,dstfolder)
-            src = os.path.join( srcfolder, os.path.split(src)[1] )
+            srcfolder = os.path.join(os.path.split(src)[0]) + "/"
+            dstfolder = os.path.join(os.path.split(dst)[0]) + "/"
+            srcfolder = os.path.relpath(srcfolder, dstfolder)
+            src = os.path.join(srcfolder, os.path.split(src)[1])
 
             # make unix link
-            if os.path.exists(dst): os.remove(dst)
-            os.symlink(src,dst)
-
-def restart2solution(config,state={}):
-    """ restart2solution(config,state={})
-        moves restart file to solution file,
-        optionally updates state
-        direct or adjoint is read from config
-        adjoint objective is read from config
+            if os.path.exists(dst):
+                os.remove(dst)
+            os.symlink(src, dst)
+
+
+def restart2solution(config, state={}):
+    """restart2solution(config,state={})
+    moves restart file to solution file,
+    optionally updates state
+    direct or adjoint is read from config
+    adjoint objective is read from config
     """
 
     # direct solution
-    if config.MATH_PROBLEM == 'DIRECT':
-        restart  = config.RESTART_FILENAME
+    if config.MATH_PROBLEM == "DIRECT":
+        restart = config.RESTART_FILENAME
         solution = config.SOLUTION_FILENAME
-        restart = restart.split('.')[0]
-        solution = solution.split('.')[0]
+        restart = restart.split(".")[0]
+        solution = solution.split(".")[0]
 
-        if 'RESTART_ASCII' in config.get('OUTPUT_FILES', ['RESTART_BINARY']):
-            restart += '.csv'
-            solution += '.csv'
+        if "RESTART_ASCII" in config.get("OUTPUT_FILES", ["RESTART_BINARY"]):
+            restart += ".csv"
+            solution += ".csv"
         else:
-            restart += '.dat'
-            solution += '.dat'
+            restart += ".dat"
+            solution += ".dat"
 
         # expand zones
-        restarts  = expand_zones(restart,config)
-        solutions = expand_zones(solution,config)
+        restarts = expand_zones(restart, config)
+        solutions = expand_zones(solution, config)
         # expand unsteady time
-        restarts  = expand_time(restarts,config)
-        solutions = expand_time(solutions,config)
+        restarts = expand_time(restarts, config)
+        solutions = expand_time(solutions, config)
 
         # move
-        for res,sol in zip(restarts,solutions):
+        for res, sol in zip(restarts, solutions):
             if os.path.exists(res):
-                shutil.move( res , sol )
+                shutil.move(res, sol)
         # update state
         if state:
             state.FILES.DIRECT = solution
-            if os.path.exists('flow.meta'):
-                state.FILES.FLOW_META = 'flow.meta'
+            if os.path.exists("flow.meta"):
+                state.FILES.FLOW_META = "flow.meta"
 
     # adjoint solution
-    elif any([config.MATH_PROBLEM == 'CONTINUOUS_ADJOINT', config.MATH_PROBLEM == 'DISCRETE_ADJOINT']):
-        restart  = config.RESTART_ADJ_FILENAME
+    elif any(
+        [
+            config.MATH_PROBLEM == "CONTINUOUS_ADJOINT",
+            config.MATH_PROBLEM == "DISCRETE_ADJOINT",
+        ]
+    ):
+        restart = config.RESTART_ADJ_FILENAME
         solution = config.SOLUTION_ADJ_FILENAME
-        restart = restart.split('.')[0]
-        solution = solution.split('.')[0]
+        restart = restart.split(".")[0]
+        solution = solution.split(".")[0]
 
-        if 'RESTART_ASCII' in config.get('OUTPUT_FILES', ['RESTART_BINARY']):
-            restart += '.csv'
-            solution += '.csv'
+        if "RESTART_ASCII" in config.get("OUTPUT_FILES", ["RESTART_BINARY"]):
+            restart += ".csv"
+            solution += ".csv"
         else:
-            restart += '.dat'
-            solution += '.dat'
+            restart += ".dat"
+            solution += ".dat"
         # add suffix
         func_name = config.OBJECTIVE_FUNCTION
-        suffix    = get_adjointSuffix(func_name)
-        restart   = add_suffix(restart,suffix)
-        solution  = add_suffix(solution,suffix)
+        suffix = get_adjointSuffix(func_name)
+        restart = add_suffix(restart, suffix)
+        solution = add_suffix(solution, suffix)
         # expand zones
-        restarts  = expand_zones(restart,config)
-        solutions = expand_zones(solution,config)
+        restarts = expand_zones(restart, config)
+        solutions = expand_zones(solution, config)
         # expand unsteady time
-        restarts  = expand_time(restarts,config)
-        solutions = expand_time(solutions,config)
+        restarts = expand_time(restarts, config)
+        solutions = expand_time(solutions, config)
 
         # move
-        for res,sol in zip(restarts,solutions):
-            shutil.move( res , sol )
+        for res, sol in zip(restarts, solutions):
+            shutil.move(res, sol)
         # udpate state
         if "," in func_name:
-            func_name="COMBO"
-        ADJ_NAME = 'ADJOINT_' + func_name
-        if state: state.FILES[ADJ_NAME] = solution
+            func_name = "COMBO"
+        ADJ_NAME = "ADJOINT_" + func_name
+        if state:
+            state.FILES[ADJ_NAME] = solution
 
     else:
-        raise Exception('unknown math problem')
-
+        raise Exception("unknown math problem")
diff --git a/SU2_PY/SU2/opt/project.py b/SU2_PY/SU2/opt/project.py
index f8cd6cd218e..b5b4c301780 100644
--- a/SU2_PY/SU2/opt/project.py
+++ b/SU2_PY/SU2/opt/project.py
@@ -34,13 +34,14 @@
 
 import os, sys, shutil, copy, glob, time
 import numpy as np
-from .. import io   as su2io
+from .. import io as su2io
 from .. import eval as su2eval
 from .. import util as su2util
 from ..io import redirect_folder
 from ..io import historyOutFields
 from warnings import warn, simplefilter
-#simplefilter(Warning,'ignore')
+
+# simplefilter(Warning,'ignore')
 
 inf = 1.0e20
 
@@ -49,61 +50,61 @@
 #  Project Class
 # -------------------------------------------------------------------
 
+
 class Project(object):
-    """ project = SU2.opt.Project(self,config,state=None,
-                                  designs=[],folder='.')
-
-        Starts a project class to manage multiple designs
-
-        Runs multiple design classes, avoiding redundancy
-        Looks for closest design on restart
-        Currently only based on DV_VALUE_NEW
-        Exposes all methods of SU2.eval.design
-
-        Attributes:
-             config  - base config
-             state   - base state
-             files   - base files
-             designs - list of designs
-             folder  - project working folder
-             results - project design results
-
-        Methods:
-            Optimizer Interface
-            The following methods take a design vector for input
-            as a list (shape n) or numpy array (shape n or nx1 or 1xn).
-            Values are returned as floats or lists or lists of lists.
-            See SU2.eval.obj_f, etc for more detail.
-
-            obj_f(dvs)     - objective function              : float
-            obj_df(dvs)    - objective function derivatives  : list
-            con_ceq(dvs)   - equality constraints            : list
-            con_dceq(dvs)  - equality constraint derivatives : list[list]
-            con_cieq(dvs)  - inequality constraints          : list
-            con_dcieq(dvs) - inequality constraint gradients : list[list]
-
-            Functional Interface
-            The following methods take an objective function name for input.
-            func(func_name,config)        - function of specified name
-            grad(func_name,method,config) - gradient of specified name,
-                                            where method is 'CONTINUOUS_ADJOINT' or 'FINDIFF'
-            setup config for given dvs with
-            config = project.unpack_dvs(dvs)
+    """project = SU2.opt.Project(self,config,state=None,
+                              designs=[],folder='.')
+
+    Starts a project class to manage multiple designs
+
+    Runs multiple design classes, avoiding redundancy
+    Looks for closest design on restart
+    Currently only based on DV_VALUE_NEW
+    Exposes all methods of SU2.eval.design
+
+    Attributes:
+         config  - base config
+         state   - base state
+         files   - base files
+         designs - list of designs
+         folder  - project working folder
+         results - project design results
+
+    Methods:
+        Optimizer Interface
+        The following methods take a design vector for input
+        as a list (shape n) or numpy array (shape n or nx1 or 1xn).
+        Values are returned as floats or lists or lists of lists.
+        See SU2.eval.obj_f, etc for more detail.
+
+        obj_f(dvs)     - objective function              : float
+        obj_df(dvs)    - objective function derivatives  : list
+        con_ceq(dvs)   - equality constraints            : list
+        con_dceq(dvs)  - equality constraint derivatives : list[list]
+        con_cieq(dvs)  - inequality constraints          : list
+        con_dcieq(dvs) - inequality constraint gradients : list[list]
+
+        Functional Interface
+        The following methods take an objective function name for input.
+        func(func_name,config)        - function of specified name
+        grad(func_name,method,config) - gradient of specified name,
+                                        where method is 'CONTINUOUS_ADJOINT' or 'FINDIFF'
+        setup config for given dvs with
+        config = project.unpack_dvs(dvs)
     """
 
-    _design_folder = 'DESIGNS/DSN_*'
-    _design_number = '%03d'
-
+    _design_folder = "DESIGNS/DSN_*"
+    _design_number = "%03d"
 
-    def __init__( self, config, state=None ,
-                  designs=None, folder='.' ,
-                  warn = True                ):
+    def __init__(self, config, state=None, designs=None, folder=".", warn=True):
 
-        folder = folder.rstrip('/')+'/'
-        if '*' in folder: folder = su2io.next_folder(folder)
-        if designs is None: designs = []
+        folder = folder.rstrip("/") + "/"
+        if "*" in folder:
+            folder = su2io.next_folder(folder)
+        if designs is None:
+            designs = []
 
-        print('New Project: %s' % (folder))
+        print("New Project: %s" % (folder))
 
         # setup config
         config = copy.deepcopy(config)
@@ -111,22 +112,22 @@ def __init__( self, config, state=None ,
         # data_dict creation does not preserve the ordering of the config file.
         # This section ensures that the order of markers and objectives match
         # It is only needed when more than one objective is used.
-        def_objs = config['OPT_OBJECTIVE']
-        if len(def_objs)>1:
+        def_objs = config["OPT_OBJECTIVE"]
+        if len(def_objs) > 1:
             objectives = def_objs.keys()
             marker_monitoring = []
             weights = []
             for i_obj, this_obj in enumerate(objectives):
-                marker_monitoring+=[def_objs[this_obj]['MARKER']]
-                weights+=[str(def_objs[this_obj]['SCALE'])]
-            config['MARKER_MONITORING'] = marker_monitoring
-            config['OBJECTIVE_WEIGHT'] = ",".join(weights)
-            config['OBJECTIVE_FUNCTION'] = ",".join(objectives)
+                marker_monitoring += [def_objs[this_obj]["MARKER"]]
+                weights += [str(def_objs[this_obj]["SCALE"])]
+            config["MARKER_MONITORING"] = marker_monitoring
+            config["OBJECTIVE_WEIGHT"] = ",".join(weights)
+            config["OBJECTIVE_FUNCTION"] = ",".join(objectives)
 
         for this_obj in def_objs:
             if this_obj in su2io.optnames_multi:
-                this_obj = this_obj.split('_')[1]
-            group = historyOutFields[this_obj]['GROUP']
+                this_obj = this_obj.split("_")[1]
+            group = historyOutFields[this_obj]["GROUP"]
             if not group in config.HISTORY_OUTPUT:
                 config.HISTORY_OUTPUT.append(group)
 
@@ -134,76 +135,80 @@ def __init__( self, config, state=None ,
         if state is None:
             state = su2io.State()
         else:
-            state  = copy.deepcopy(state)
-            state  = su2io.State(state)
+            state = copy.deepcopy(state)
+            state = su2io.State(state)
         state.find_files(config)
 
-        if 'MESH' not in state.FILES:
-            raise Exception('Could not find mesh file: %s' % config.MESH_FILENAME)
+        if "MESH" not in state.FILES:
+            raise Exception("Could not find mesh file: %s" % config.MESH_FILENAME)
 
-        self.config  = config      # base config
-        self.state   = state       # base state
-        self.files   = state.FILES # base files
-        self.designs = designs     # design list
-        self.folder  = folder      # project folder
-        self.results = su2util.ordered_bunch() # project design results
+        self.config = config  # base config
+        self.state = state  # base state
+        self.files = state.FILES  # base files
+        self.designs = designs  # design list
+        self.folder = folder  # project folder
+        self.results = su2util.ordered_bunch()  # project design results
 
         # output filenames
-        self.filename = 'project.pkl'
-        self.results_filename = 'results.pkl'
+        self.filename = "project.pkl"
+        self.results_filename = "results.pkl"
 
         # initialize folder with files
-        pull,link = state.pullnlink(config)
+        pull, link = state.pullnlink(config)
 
-        with redirect_folder(folder,pull,link,force=True):
+        with redirect_folder(folder, pull, link, force=True):
 
             # look for existing designs
             folders = glob.glob(self._design_folder)
-            if len(folders)>0:
-                sys.stdout.write('Removing old designs in 10s.')
+            if len(folders) > 0:
+                sys.stdout.write("Removing old designs in 10s.")
                 sys.stdout.flush()
-                if warn: time.sleep(10)
-                sys.stdout.write(' Done!\n\n')
-                for f in folders: shutil.rmtree(f)
+                if warn:
+                    time.sleep(10)
+                sys.stdout.write(" Done!\n\n")
+                for f in folders:
+                    shutil.rmtree(f)
             #: if existing designs
 
             # save project
-            su2io.save_data(self.filename,self)
+            su2io.save_data(self.filename, self)
 
         return
 
-    def _eval(self,config,func,*args):
-        """ evalautes a config, checking for existing designs
-        """
+    def _eval(self, config, func, *args):
+        """evalautes a config, checking for existing designs"""
 
-        konfig = copy.deepcopy(config) # design config
-        config = self.config           # project config
-        state  = self.state            # project state
-        folder = self.folder           # project folder
+        konfig = copy.deepcopy(config)  # design config
+        config = self.config  # project config
+        state = self.state  # project state
+        folder = self.folder  # project folder
         filename = self.filename
 
         # check folder
-        assert os.path.exists(folder) , 'cannot find project folder %s' % folder
+        assert os.path.exists(folder), "cannot find project folder %s" % folder
 
         # list project files to pull and link
-        pull,link = state.pullnlink(config)
+        pull, link = state.pullnlink(config)
 
         # project folder redirection, don't overwrite files
-        with redirect_folder(folder,pull,link,force=False) as push:
+        with redirect_folder(folder, pull, link, force=False) as push:
 
             # start design
             design = self.new_design(konfig)
 
-            if config.get('CONSOLE','VERBOSE') == 'VERBOSE':
-                print(os.path.join(self.folder,design.folder))
+            if config.get("CONSOLE", "VERBOSE") == "VERBOSE":
+                print(os.path.join(self.folder, design.folder))
             timestamp = design.state.tic()
 
             # set right option in design config.
-            if konfig.get('TIME_DOMAIN', 'NO') == 'YES' and konfig.get('RESTART_SOL', 'NO') == 'YES':
-                design.config['RESTART_SOL'] = 'YES'
+            if (
+                konfig.get("TIME_DOMAIN", "NO") == "YES"
+                and konfig.get("RESTART_SOL", "NO") == "YES"
+            ):
+                design.config["RESTART_SOL"] = "YES"
 
             # run design+
-            vals = design._eval(func,*args)
+            vals = design._eval(func, *args)
 
             # check for update
             if design.state.toc(timestamp):
@@ -215,7 +220,7 @@ def _eval(self,config,func,*args):
                 self.plot_results()
 
                 # save data
-                su2io.save_data(filename,self)
+                su2io.save_data(filename, self)
 
             #: if updated
 
@@ -224,157 +229,160 @@ def _eval(self,config,func,*args):
         # done, return output
         return vals
 
-    def unpack_dvs(self,dvs):
+    def unpack_dvs(self, dvs):
         dvs = copy.deepcopy(dvs)
-        konfig = copy.deepcopy( self.config )
-        if isinstance(dvs, np.ndarray): dvs = dvs.tolist()
+        konfig = copy.deepcopy(self.config)
+        if isinstance(dvs, np.ndarray):
+            dvs = dvs.tolist()
         konfig.unpack_dvs(dvs)
         return konfig, dvs
 
-    def obj_f(self,dvs):
+    def obj_f(self, dvs):
         func = su2eval.obj_f
-        konfig,dvs = self.unpack_dvs(dvs)
-        return self._eval(konfig, func,dvs)
+        konfig, dvs = self.unpack_dvs(dvs)
+        return self._eval(konfig, func, dvs)
 
-    def obj_df(self,dvs):
+    def obj_df(self, dvs):
         func = su2eval.obj_df
-        konfig,dvs = self.unpack_dvs(dvs)
-        return self._eval(konfig, func,dvs)
+        konfig, dvs = self.unpack_dvs(dvs)
+        return self._eval(konfig, func, dvs)
 
-    def con_ceq(self,dvs):
+    def con_ceq(self, dvs):
         func = su2eval.con_ceq
-        konfig,dvs = self.unpack_dvs(dvs)
-        return self._eval(konfig, func,dvs)
+        konfig, dvs = self.unpack_dvs(dvs)
+        return self._eval(konfig, func, dvs)
 
-    def con_dceq(self,dvs):
+    def con_dceq(self, dvs):
         func = su2eval.con_dceq
-        konfig,dvs = self.unpack_dvs(dvs)
-        return self._eval(konfig, func,dvs)
+        konfig, dvs = self.unpack_dvs(dvs)
+        return self._eval(konfig, func, dvs)
 
-    def con_cieq(self,dvs):
+    def con_cieq(self, dvs):
         func = su2eval.con_cieq
-        konfig,dvs = self.unpack_dvs(dvs)
-        return self._eval(konfig, func,dvs)
+        konfig, dvs = self.unpack_dvs(dvs)
+        return self._eval(konfig, func, dvs)
 
-    def con_dcieq(self,dvs):
+    def con_dcieq(self, dvs):
         func = su2eval.con_dcieq
-        konfig,dvs = self.unpack_dvs(dvs)
-        return self._eval(konfig, func,dvs)
+        konfig, dvs = self.unpack_dvs(dvs)
+        return self._eval(konfig, func, dvs)
 
-    def func(self,func_name,config):
+    def func(self, func_name, config):
         func = su2eval.func
         konfig = copy.deepcopy(config)
         return self._eval(konfig, func, func_name)
 
-    def grad(self,func_name,method,config):
+    def grad(self, func_name, method, config):
         func = su2eval.grad
         konfig = copy.deepcopy(config)
-        return self._eval(konfig, func, func_name,method)
+        return self._eval(konfig, func, func_name, method)
 
-    def user(self,user_func,config,*args):
+    def user(self, user_func, config, *args):
         raise NotImplementedError
-        #return self._eval(config, user_func,*args)
+        # return self._eval(config, user_func,*args)
 
-    def add_design(self,config):
-        #func = su2eval.touch # hack - TWL
+    def add_design(self, config):
+        # func = su2eval.touch # hack - TWL
         func = su2eval.skip
         konfig = copy.deepcopy(config)
         return self._eval(konfig, func)
 
-    def new_design(self,config):
-        """ finds an existing design for given config
-            or starts a new design with a closest design
-            used for restart data
+    def new_design(self, config):
+        """finds an existing design for given config
+        or starts a new design with a closest design
+        used for restart data
         """
-         # local konfig
+        # local konfig
         konfig = copy.deepcopy(config)
         # find closest design
-        closest,delta = self.closest_design(konfig)
+        closest, delta = self.closest_design(konfig)
         # found existing design
         if delta == 0.0 and closest:
             design = closest
         # start new design
         else:
-            design = self.init_design(konfig,closest)
+            design = self.init_design(konfig, closest)
         #: if new design
         return design
 
-    def get_design(self,config):
+    def get_design(self, config):
         konfig = copy.deepcopy(config)
-        closest,delta = self.closest_design(konfig)
+        closest, delta = self.closest_design(konfig)
         if delta == 0.0 and closest:
             design = closest
         else:
-            raise Exception('design not found for this config')
+            raise Exception("design not found for this config")
         return design
 
-    def closest_design(self,config):
-        """ looks for an existing or closest design
-            given a config
+    def closest_design(self, config):
+        """looks for an existing or closest design
+        given a config
         """
 
         designs = self.designs
 
-        keys_check = ['DV_VALUE_NEW']
+        keys_check = ["DV_VALUE_NEW"]
 
         if not designs:
-            return [] , inf
+            return [], inf
 
         diffs = []
         for this_design in designs:
             this_config = this_design.config
-            distance = config.dist(this_config,keys_check)
+            distance = config.dist(this_config, keys_check)
             diffs.append(distance)
 
         #: for each design
 
         # pick closest design
         i_min = np.argmin(diffs)
-        delta  = diffs[i_min]
+        delta = diffs[i_min]
         closest = designs[i_min]
 
         return closest, delta
 
-    def init_design(self,config,closest=None):
-        """ starts a new design
-            works in project folder
+    def init_design(self, config, closest=None):
+        """starts a new design
+        works in project folder
         """
 
         konfig = copy.deepcopy(config)
-        ztate  = copy.deepcopy(self.state)
-        if closest is None: closest = []
+        ztate = copy.deepcopy(self.state)
+        if closest is None:
+            closest = []
 
         # use closest design as seed
         if closest:
             # copy useful state info
             seed_folder = closest.folder
-            seed_files  = closest.files
+            seed_files = closest.files
             for key in seed_files.keys():
                 # ignore mesh
-                if key == 'MESH': continue
+                if key == "MESH":
+                    continue
                 # build file path
                 name = seed_files[key]
-                if isinstance(name,list):
+                if isinstance(name, list):
                     built_name = []
                     for elem in name:
-                        built_name.append(os.path.join(seed_folder,elem))
+                        built_name.append(os.path.join(seed_folder, elem))
                     ztate.FILES[key] = built_name
                 else:
-                    name = os.path.join(seed_folder,name)
+                    name = os.path.join(seed_folder, name)
                     # update pull files
                     ztate.FILES[key] = name
 
         # name new folder
-        folder = self._design_folder.replace('*',self._design_number)
+        folder = self._design_folder.replace("*", self._design_number)
         folder = folder % (len(self.designs) + 1)
 
         # start new design (pulls files to folder)
-        design = su2eval.Design(konfig,ztate,folder)
+        design = su2eval.Design(konfig, ztate, folder)
 
         # update local state filenames ( ??? why not in Design() )
         for key in design.files:
             name = design.files[key]
-            if isinstance(name,list):
+            if isinstance(name, list):
                 built_name = []
                 for elem in name:
                     built_name.append(os.path.split(elem)[-1])
@@ -388,22 +396,22 @@ def init_design(self,config,closest=None):
 
         return design
 
-    def compile_results(self,default=np.nan):
-        """ results = SU2.opt.Project.compile_results(default=np.nan)
-            builds a Bunch() of design results
+    def compile_results(self, default=np.nan):
+        """results = SU2.opt.Project.compile_results(default=np.nan)
+        builds a Bunch() of design results
 
-            Inputs:
-                default - value for missing values
+        Inputs:
+            default - value for missing values
 
-            Outputs:
-                results - state with items filled with list of
-                values ordered by each design iteration.
+        Outputs:
+            results - state with items filled with list of
+            values ordered by each design iteration.
 
-                results.VARIABLES
-                results.FUNCTIONS
-                results.GRADIENTS
-                results.HISTORY.DIRECT
-                results.HISTORY.ADJOINT_*
+            results.VARIABLES
+            results.FUNCTIONS
+            results.GRADIENTS
+            results.HISTORY.DIRECT
+            results.HISTORY.ADJOINT_*
 
         """
 
@@ -415,7 +423,7 @@ def compile_results(self,default=np.nan):
         n_dv = 0
 
         # populate fields
-        for i,design in enumerate(self.designs):
+        for i, design in enumerate(self.designs):
             for key in design.state.FUNCTIONS.keys():
                 results.FUNCTIONS[key] = []
             for key in design.state.GRADIENTS.keys():
@@ -425,20 +433,20 @@ def compile_results(self,default=np.nan):
                     results.HISTORY[TYPE] = su2util.ordered_bunch()
                 for key in design.state.HISTORY[TYPE].keys():
                     results.HISTORY[TYPE][key] = []
-            this_ndv = len( design.state.design_vector() )
+            this_ndv = len(design.state.design_vector())
 
             # check design vectors are of same length
             if i == 0:
                 n_dv = this_ndv
             else:
                 if n_dv != this_ndv:
-                    warn('different dv vector length during compile_results()')
+                    warn("different dv vector length during compile_results()")
         #: for each design
 
         # populate results
         for design in self.designs:
             this_designvector = design.state.design_vector()
-            results.VARIABLES.append( this_designvector )
+            results.VARIABLES.append(this_designvector)
             for key in results.FUNCTIONS.keys():
                 if key in design.state.FUNCTIONS:
                     new_func = design.state.FUNCTIONS[key]
@@ -449,14 +457,16 @@ def compile_results(self,default=np.nan):
                 if key in design.state.GRADIENTS:
                     new_grad = design.state.GRADIENTS[key]
                 else:
-                    new_grad = [default] * len( this_designvector )
+                    new_grad = [default] * len(this_designvector)
                 results.GRADIENTS[key].append(new_grad)
             for TYPE in results.HISTORY.keys():
                 for key in results.HISTORY[TYPE].keys():
                     if key in results.FUNCTIONS.keys():
                         new_func = results.FUNCTIONS[key][-1]
-                    elif ( TYPE in design.state.HISTORY.keys() and
-                            key in design.state.HISTORY[TYPE].keys() ):
+                    elif (
+                        TYPE in design.state.HISTORY.keys()
+                        and key in design.state.HISTORY[TYPE].keys()
+                    ):
                         new_func = design.state.HISTORY[TYPE][key][-1]
                     else:
                         new_func = default
@@ -465,52 +475,52 @@ def compile_results(self,default=np.nan):
 
         # save
         self.results = results
-        su2io.save_data(filename,results)
+        su2io.save_data(filename, results)
 
         return self.results
 
     def deep_compile(self):
-        """ Project.deep_compile()
-            recompiles project using design files saved in each design folder
-            useful if designs were run outside of project class
+        """Project.deep_compile()
+        recompiles project using design files saved in each design folder
+        useful if designs were run outside of project class
         """
 
         project_folder = self.folder
         designs = self.designs
 
         with su2io.redirect_folder(project_folder):
-            for i_dsn,design in enumerate(designs):
-                design_filename = os.path.join(design.folder,design.filename)
+            for i_dsn, design in enumerate(designs):
+                design_filename = os.path.join(design.folder, design.filename)
                 self.designs[i_dsn] = su2io.load_data(design_filename)
 
             self.compile_results()
-            su2io.save_data(self.filename,self)
+            su2io.save_data(self.filename, self)
 
         return
 
     def plot_results(self):
-        """ writes a tecplot file for plotting design results
-        """
+        """writes a tecplot file for plotting design results"""
         output_format = self.config.TABULAR_FORMAT
-        functions     = self.results.FUNCTIONS
-        history       = self.results.HISTORY
+        functions = self.results.FUNCTIONS
+        history = self.results.HISTORY
 
         results_plot = su2util.ordered_bunch()
-        results_plot.EVALUATION = range(1,len(self.designs)+1)
+        results_plot.EVALUATION = range(1, len(self.designs) + 1)
         results_plot.update(functions)
-        results_plot.update(history.get('DIRECT',{}))
+        results_plot.update(history.get("DIRECT", {}))
 
-        if (output_format == 'CSV'):
-          su2util.write_plot('history_project.csv',output_format,results_plot)
+        if output_format == "CSV":
+            su2util.write_plot("history_project.csv", output_format, results_plot)
         else:
-          su2util.write_plot('history_project.dat',output_format,results_plot)
+            su2util.write_plot("history_project.dat", output_format, results_plot)
 
     def save(self):
         with su2io.redirect_folder(self.folder):
-            su2io.save_data(self.filename,self)
+            su2io.save_data(self.filename, self)
 
     def __repr__(self):
-        return '<Project> with %i <Design>' % len(self.designs)
+        return "<Project> with %i <Design>" % len(self.designs)
+
     def __str__(self):
         output = self.__repr__()
         return output
diff --git a/SU2_PY/SU2/opt/scipy_tools.py b/SU2_PY/SU2/opt/scipy_tools.py
index 012d785e22d..3dbe18f83bc 100644
--- a/SU2_PY/SU2/opt/scipy_tools.py
+++ b/SU2_PY/SU2/opt/scipy_tools.py
@@ -39,442 +39,488 @@
 #  Scipy SLSQP
 # -------------------------------------------------------------------
 
-def scipy_slsqp(project,x0=None,xb=None,its=100,accu=1e-10,grads=True):
-    """ result = scipy_slsqp(project,x0=[],xb=[],its=100,accu=1e-10)
 
-        Runs the Scipy implementation of SLSQP with
-        an SU2 project
+def scipy_slsqp(project, x0=None, xb=None, its=100, accu=1e-10, grads=True):
+    """result = scipy_slsqp(project,x0=[],xb=[],its=100,accu=1e-10)
 
-        Inputs:
-            project - an SU2 project
-            x0      - optional, initial guess
-            xb      - optional, design variable bounds
-            its     - max outer iterations, default 100
-            accu    - accuracy, default 1e-10
+    Runs the Scipy implementation of SLSQP with
+    an SU2 project
 
-        Outputs:
-           result - the outputs from scipy.fmin_slsqp
+    Inputs:
+        project - an SU2 project
+        x0      - optional, initial guess
+        xb      - optional, design variable bounds
+        its     - max outer iterations, default 100
+        accu    - accuracy, default 1e-10
+
+    Outputs:
+       result - the outputs from scipy.fmin_slsqp
     """
 
     # import scipy optimizer
     from scipy.optimize import fmin_slsqp
 
     # handle input cases
-    if x0 is None: x0 = []
-    if xb is None: xb = []
+    if x0 is None:
+        x0 = []
+    if xb is None:
+        xb = []
 
     # function handles
-    func           = obj_f
-    f_eqcons       = con_ceq
-    f_ieqcons      = con_cieq
+    func = obj_f
+    f_eqcons = con_ceq
+    f_ieqcons = con_cieq
 
     # gradient handles
-    if project.config.get('GRADIENT_METHOD','NONE') == 'NONE':
-        fprime         = None
-        fprime_eqcons  = None
+    if project.config.get("GRADIENT_METHOD", "NONE") == "NONE":
+        fprime = None
+        fprime_eqcons = None
         fprime_ieqcons = None
     else:
-        fprime         = obj_df
-        fprime_eqcons  = con_dceq
+        fprime = obj_df
+        fprime_eqcons = con_dceq
         fprime_ieqcons = con_dcieq
 
     # number of design variables
-    dv_size = project.config['DEFINITION_DV']['SIZE']
-    n_dv = sum( dv_size)
+    dv_size = project.config["DEFINITION_DV"]["SIZE"]
+    n_dv = sum(dv_size)
     project.n_dv = n_dv
 
     # Initial guess
-    if not x0: x0 = [0.0]*n_dv
+    if not x0:
+        x0 = [0.0] * n_dv
 
     # prescale x0
-    dv_scales = project.config['DEFINITION_DV']['SCALE']
+    dv_scales = project.config["DEFINITION_DV"]["SCALE"]
     k = 0
     for i, dv_scl in enumerate(dv_scales):
         for j in range(dv_size[i]):
-            x0[k] =x0[k]/dv_scl;
+            x0[k] = x0[k] / dv_scl
             k = k + 1
 
     # scale accuracy
-    obj = project.config['OPT_OBJECTIVE']
+    obj = project.config["OPT_OBJECTIVE"]
     obj_scale = []
     for this_obj in obj.keys():
-        obj_scale = obj_scale + [obj[this_obj]['SCALE']]
+        obj_scale = obj_scale + [obj[this_obj]["SCALE"]]
 
     # Only scale the accuracy for single-objective problems:
-    if len(obj.keys())==1:
-        accu = accu*obj_scale[0]
+    if len(obj.keys()) == 1:
+        accu = accu * obj_scale[0]
 
     # scale accuracy
     eps = 1.0e-04
 
     # optimizer summary
-    sys.stdout.write('Sequential Least SQuares Programming (SLSQP) parameters:\n')
-    sys.stdout.write('Number of design variables: ' + str(len(dv_size)) + ' ( ' + str(n_dv) + ' ) \n' )
-    sys.stdout.write('Objective function scaling factor: ' + str(obj_scale) + '\n')
-    sys.stdout.write('Maximum number of iterations: ' + str(its) + '\n')
-    sys.stdout.write('Requested accuracy: ' + str(accu) + '\n')
-    sys.stdout.write('Initial guess for the independent variable(s): ' + str(x0) + '\n')
-    sys.stdout.write('Lower and upper bound for each independent variable: ' + str(xb) + '\n\n')
+    sys.stdout.write("Sequential Least SQuares Programming (SLSQP) parameters:\n")
+    sys.stdout.write(
+        "Number of design variables: " + str(len(dv_size)) + " ( " + str(n_dv) + " ) \n"
+    )
+    sys.stdout.write("Objective function scaling factor: " + str(obj_scale) + "\n")
+    sys.stdout.write("Maximum number of iterations: " + str(its) + "\n")
+    sys.stdout.write("Requested accuracy: " + str(accu) + "\n")
+    sys.stdout.write("Initial guess for the independent variable(s): " + str(x0) + "\n")
+    sys.stdout.write(
+        "Lower and upper bound for each independent variable: " + str(xb) + "\n\n"
+    )
 
     # Run Optimizer
-    outputs = fmin_slsqp( x0             = x0             ,
-                          func           = func           ,
-                          f_eqcons       = f_eqcons       ,
-                          f_ieqcons      = f_ieqcons      ,
-                          fprime         = fprime         ,
-                          fprime_eqcons  = fprime_eqcons  ,
-                          fprime_ieqcons = fprime_ieqcons ,
-                          args           = (project,)     ,
-                          bounds         = xb             ,
-                          iter           = its            ,
-                          iprint         = 2              ,
-                          full_output    = True           ,
-                          acc            = accu           ,
-                          epsilon        = eps            )
+    outputs = fmin_slsqp(
+        x0=x0,
+        func=func,
+        f_eqcons=f_eqcons,
+        f_ieqcons=f_ieqcons,
+        fprime=fprime,
+        fprime_eqcons=fprime_eqcons,
+        fprime_ieqcons=fprime_ieqcons,
+        args=(project,),
+        bounds=xb,
+        iter=its,
+        iprint=2,
+        full_output=True,
+        acc=accu,
+        epsilon=eps,
+    )
 
     # Done
     return outputs
 
+
 # -------------------------------------------------------------------
 #  Scipy CG
 # -------------------------------------------------------------------
 
-def scipy_cg(project,x0=None,xb=None,its=100,accu=1e-10,grads=True):
-    """ result = scipy_cg(project,x0=[],xb=[],its=100,accu=1e-10)
 
-        Runs the Scipy implementation of CG with
-        an SU2 project
+def scipy_cg(project, x0=None, xb=None, its=100, accu=1e-10, grads=True):
+    """result = scipy_cg(project,x0=[],xb=[],its=100,accu=1e-10)
+
+    Runs the Scipy implementation of CG with
+    an SU2 project
 
-        Inputs:
-            project - an SU2 project
-            x0      - optional, initial guess
-            xb      - optional, design variable bounds
-            its     - max outer iterations, default 100
-            accu    - accuracy, default 1e-10
+    Inputs:
+        project - an SU2 project
+        x0      - optional, initial guess
+        xb      - optional, design variable bounds
+        its     - max outer iterations, default 100
+        accu    - accuracy, default 1e-10
 
-        Outputs:
-           result - the outputs from scipy.fmin_slsqp
+    Outputs:
+       result - the outputs from scipy.fmin_slsqp
     """
 
     # import scipy optimizer
     from scipy.optimize import fmin_cg
 
     # handle input cases
-    if x0 is None: x0 = []
-    if xb is None: xb = []
+    if x0 is None:
+        x0 = []
+    if xb is None:
+        xb = []
 
     # function handles
-    func           = obj_f
+    func = obj_f
 
     # gradient handles
-    if project.config.get('GRADIENT_METHOD','NONE') == 'NONE':
-        fprime         = None
+    if project.config.get("GRADIENT_METHOD", "NONE") == "NONE":
+        fprime = None
     else:
-        fprime         = obj_df
+        fprime = obj_df
 
     # number of design variables
-    n_dv = len( project.config['DEFINITION_DV']['KIND'] )
+    n_dv = len(project.config["DEFINITION_DV"]["KIND"])
     project.n_dv = n_dv
 
     # Initial guess
-    if not x0: x0 = [0.0]*n_dv
+    if not x0:
+        x0 = [0.0] * n_dv
 
     # prescale x0
-    dv_scales = project.config['DEFINITION_DV']['SCALE']
-    x0 = [ x0[i]/dv_scl for i,dv_scl in enumerate(dv_scales) ]
+    dv_scales = project.config["DEFINITION_DV"]["SCALE"]
+    x0 = [x0[i] / dv_scl for i, dv_scl in enumerate(dv_scales)]
 
     # scale accuracy
-    obj = project.config['OPT_OBJECTIVE']
-    obj_scale = obj[obj.keys()[0]]['SCALE']
-    accu = accu*obj_scale
+    obj = project.config["OPT_OBJECTIVE"]
+    obj_scale = obj[obj.keys()[0]]["SCALE"]
+    accu = accu * obj_scale
 
     # scale accuracy
     eps = 1.0e-04
 
     # optimizer summary
-    sys.stdout.write('Conjugate gradient (CG) parameters:\n')
-    sys.stdout.write('Number of design variables: ' + str(n_dv) + '\n')
-    sys.stdout.write('Objective function scaling factor: ' + str(obj_scale) + '\n')
-    sys.stdout.write('Maximum number of iterations: ' + str(its) + '\n')
-    sys.stdout.write('Requested accuracy: ' + str(accu) + '\n')
-    sys.stdout.write('Initial guess for the independent variable(s): ' + str(x0) + '\n')
-    sys.stdout.write('Lower and upper bound for each independent variable: ' + str(xb) + '\n\n')
+    sys.stdout.write("Conjugate gradient (CG) parameters:\n")
+    sys.stdout.write("Number of design variables: " + str(n_dv) + "\n")
+    sys.stdout.write("Objective function scaling factor: " + str(obj_scale) + "\n")
+    sys.stdout.write("Maximum number of iterations: " + str(its) + "\n")
+    sys.stdout.write("Requested accuracy: " + str(accu) + "\n")
+    sys.stdout.write("Initial guess for the independent variable(s): " + str(x0) + "\n")
+    sys.stdout.write(
+        "Lower and upper bound for each independent variable: " + str(xb) + "\n\n"
+    )
 
     # Evaluate the objective function (only 1st iteration)
-    obj_f(x0,project)
+    obj_f(x0, project)
 
     # Run Optimizer
-    outputs = fmin_cg( x0             = x0             ,
-                       f              = func           ,
-                       fprime         = fprime         ,
-                       args           = (project,)     ,
-                       gtol           = accu           ,
-                       epsilon        = eps            ,
-                       maxiter        = its            ,
-                       full_output    = True           ,
-                       disp           = True           ,
-                       retall         = True           )
-
+    outputs = fmin_cg(
+        x0=x0,
+        f=func,
+        fprime=fprime,
+        args=(project,),
+        gtol=accu,
+        epsilon=eps,
+        maxiter=its,
+        full_output=True,
+        disp=True,
+        retall=True,
+    )
 
     # Done
     return outputs
 
+
 # -------------------------------------------------------------------
 #  Scipy BFGS
 # -------------------------------------------------------------------
 
-def scipy_bfgs(project,x0=None,xb=None,its=100,accu=1e-10,grads=True):
-    """ result = scipy_bfgs(project,x0=[],xb=[],its=100,accu=1e-10)
 
-        Runs the Scipy implementation of BFGS with
-        an SU2 project
+def scipy_bfgs(project, x0=None, xb=None, its=100, accu=1e-10, grads=True):
+    """result = scipy_bfgs(project,x0=[],xb=[],its=100,accu=1e-10)
 
-        Inputs:
-            project - an SU2 project
-            x0      - optional, initial guess
-            xb      - optional, design variable bounds
-            its     - max outer iterations, default 100
-            accu    - accuracy, default 1e-10
+    Runs the Scipy implementation of BFGS with
+    an SU2 project
 
-        Outputs:
-           result - the outputs from scipy.fmin_slsqp
+    Inputs:
+        project - an SU2 project
+        x0      - optional, initial guess
+        xb      - optional, design variable bounds
+        its     - max outer iterations, default 100
+        accu    - accuracy, default 1e-10
+
+    Outputs:
+       result - the outputs from scipy.fmin_slsqp
     """
 
     # import scipy optimizer
     from scipy.optimize import fmin_bfgs
 
     # handle input cases
-    if x0 is None: x0 = []
-    if xb is None: xb = []
+    if x0 is None:
+        x0 = []
+    if xb is None:
+        xb = []
 
     # function handles
-    func           = obj_f
+    func = obj_f
 
     # gradient handles
-    if project.config.get('GRADIENT_METHOD','NONE') == 'NONE':
-        fprime         = None
+    if project.config.get("GRADIENT_METHOD", "NONE") == "NONE":
+        fprime = None
     else:
-        fprime         = obj_df
+        fprime = obj_df
 
     # number of design variables
-    n_dv = len( project.config['DEFINITION_DV']['KIND'] )
+    n_dv = len(project.config["DEFINITION_DV"]["KIND"])
     project.n_dv = n_dv
 
     # Initial guess
-    if not x0: x0 = [0.0]*n_dv
+    if not x0:
+        x0 = [0.0] * n_dv
 
     # prescale x0
-    dv_scales = project.config['DEFINITION_DV']['SCALE']
-    x0 = [ x0[i]/dv_scl for i,dv_scl in enumerate(dv_scales) ]
+    dv_scales = project.config["DEFINITION_DV"]["SCALE"]
+    x0 = [x0[i] / dv_scl for i, dv_scl in enumerate(dv_scales)]
 
     # scale accuracy
-    obj = project.config['OPT_OBJECTIVE']
-    obj_scale = obj[obj.keys()[0]]['SCALE']
-    accu = accu*obj_scale
+    obj = project.config["OPT_OBJECTIVE"]
+    obj_scale = obj[obj.keys()[0]]["SCALE"]
+    accu = accu * obj_scale
 
     # scale accuracy
     eps = 1.0e-04
 
     # optimizer summary
-    sys.stdout.write('Broyden-Fletcher-Goldfarb-Shanno (BFGS) parameters:\n')
-    sys.stdout.write('Number of design variables: ' + str(n_dv) + '\n')
-    sys.stdout.write('Objective function scaling factor: ' + str(obj_scale) + '\n')
-    sys.stdout.write('Maximum number of iterations: ' + str(its) + '\n')
-    sys.stdout.write('Requested accuracy: ' + str(accu) + '\n')
-    sys.stdout.write('Initial guess for the independent variable(s): ' + str(x0) + '\n')
-    sys.stdout.write('Lower and upper bound for each independent variable: ' + str(xb) + '\n\n')
+    sys.stdout.write("Broyden-Fletcher-Goldfarb-Shanno (BFGS) parameters:\n")
+    sys.stdout.write("Number of design variables: " + str(n_dv) + "\n")
+    sys.stdout.write("Objective function scaling factor: " + str(obj_scale) + "\n")
+    sys.stdout.write("Maximum number of iterations: " + str(its) + "\n")
+    sys.stdout.write("Requested accuracy: " + str(accu) + "\n")
+    sys.stdout.write("Initial guess for the independent variable(s): " + str(x0) + "\n")
+    sys.stdout.write(
+        "Lower and upper bound for each independent variable: " + str(xb) + "\n\n"
+    )
 
     # Evaluate the objective function (only 1st iteration)
-    obj_f(x0,project)
+    obj_f(x0, project)
 
     # Run Optimizer
-    outputs = fmin_bfgs( x0             = x0             ,
-                         f              = func           ,
-                         fprime         = fprime         ,
-                         args           = (project,)     ,
-                         gtol           = accu           ,
-                         epsilon        = eps            ,
-                         maxiter        = its            ,
-                         full_output    = True           ,
-                         disp           = True           ,
-                         retall         = True           )
+    outputs = fmin_bfgs(
+        x0=x0,
+        f=func,
+        fprime=fprime,
+        args=(project,),
+        gtol=accu,
+        epsilon=eps,
+        maxiter=its,
+        full_output=True,
+        disp=True,
+        retall=True,
+    )
 
     # Done
     return outputs
 
-def scipy_powell(project,x0=None,xb=None,its=100,accu=1e-10,grads=False):
-    """ result = scipy_powell(project,x0=[],xb=[],its=100,accu=1e-10)
 
-        Runs the Scipy implementation of Powell's method with
-        an SU2 project
+def scipy_powell(project, x0=None, xb=None, its=100, accu=1e-10, grads=False):
+    """result = scipy_powell(project,x0=[],xb=[],its=100,accu=1e-10)
+
+    Runs the Scipy implementation of Powell's method with
+    an SU2 project
 
-        Inputs:
-            project - an SU2 project
-            x0      - optional, initial guess
-            xb      - optional, design variable bounds
-            its     - max outer iterations, default 100
-            accu    - accuracy, default 1e-10
+    Inputs:
+        project - an SU2 project
+        x0      - optional, initial guess
+        xb      - optional, design variable bounds
+        its     - max outer iterations, default 100
+        accu    - accuracy, default 1e-10
 
-        Outputs:
-           result - the outputs from scipy.fmin_slsqp
+    Outputs:
+       result - the outputs from scipy.fmin_slsqp
     """
 
     # import scipy optimizer
     from scipy.optimize import fmin_powell
 
     # handle input cases
-    if x0 is None: x0 = []
+    if x0 is None:
+        x0 = []
 
     # function handles
-    func           = obj_f
+    func = obj_f
 
     # number of design variables
-    n_dv = len( project.config['DEFINITION_DV']['KIND'] )
+    n_dv = len(project.config["DEFINITION_DV"]["KIND"])
     project.n_dv = n_dv
 
     # Initial guess
-    if not x0: x0 = [0.0]*n_dv
+    if not x0:
+        x0 = [0.0] * n_dv
 
     # prescale x0
-    dv_scales = project.config['DEFINITION_DV']['SCALE']
-    x0 = [ x0[i]/dv_scl for i,dv_scl in enumerate(dv_scales) ]
+    dv_scales = project.config["DEFINITION_DV"]["SCALE"]
+    x0 = [x0[i] / dv_scl for i, dv_scl in enumerate(dv_scales)]
 
     # scale accuracy
-    obj = project.config['OPT_OBJECTIVE']
-    obj_scale = obj[obj.keys()[0]]['SCALE']
-    accu = accu*obj_scale
+    obj = project.config["OPT_OBJECTIVE"]
+    obj_scale = obj[obj.keys()[0]]["SCALE"]
+    accu = accu * obj_scale
 
     # scale accuracy
     eps = 1.0e-04
 
     # optimizer summary
-    sys.stdout.write('Powells method parameters:\n')
-    sys.stdout.write('Number of design variables: ' + str(n_dv) + '\n')
-    sys.stdout.write('Objective function scaling factor: ' + str(obj_scale) + '\n')
-    sys.stdout.write('Maximum number of iterations: ' + str(its) + '\n')
-    sys.stdout.write('Requested accuracy: ' + str(accu) + '\n')
+    sys.stdout.write("Powells method parameters:\n")
+    sys.stdout.write("Number of design variables: " + str(n_dv) + "\n")
+    sys.stdout.write("Objective function scaling factor: " + str(obj_scale) + "\n")
+    sys.stdout.write("Maximum number of iterations: " + str(its) + "\n")
+    sys.stdout.write("Requested accuracy: " + str(accu) + "\n")
 
     # Evaluate the objective function (only 1st iteration)
-    obj_f(x0,project)
+    obj_f(x0, project)
 
     # Run Optimizer
-    outputs = fmin_powell( x0             = x0             ,
-                           func           = func           ,
-                           args           = (project,)     ,
-                           ftol           = accu           ,
-                           maxiter        = its            ,
-                           full_output    = True           ,
-                           disp           = True           ,
-                           retall         = True           )
+    outputs = fmin_powell(
+        x0=x0,
+        func=func,
+        args=(project,),
+        ftol=accu,
+        maxiter=its,
+        full_output=True,
+        disp=True,
+        retall=True,
+    )
 
     # Done
     return outputs
 
-def obj_f(x,project):
-    """ obj = obj_f(x,project)
 
-        Objective Function
-        SU2 Project interface to scipy.fmin_slsqp
+def obj_f(x, project):
+    """obj = obj_f(x,project)
 
-        su2:         minimize f(x), list[nobj]
-        scipy_slsqp: minimize f(x), float
+    Objective Function
+    SU2 Project interface to scipy.fmin_slsqp
+
+    su2:         minimize f(x), list[nobj]
+    scipy_slsqp: minimize f(x), float
     """
 
     obj_list = project.obj_f(x)
     obj = 0
     for this_obj in obj_list:
-        obj = obj+this_obj
+        obj = obj + this_obj
 
     return obj
 
-def obj_df(x,project):
-    """ dobj = obj_df(x,project)
 
-        Objective Function Gradients
-        SU2 Project interface to scipy.fmin_slsqp
+def obj_df(x, project):
+    """dobj = obj_df(x,project)
+
+    Objective Function Gradients
+    SU2 Project interface to scipy.fmin_slsqp
 
-        su2:         df(x), list[nobj x dim]
-        scipy_slsqp: df(x), ndarray[dim]
+    su2:         df(x), list[nobj x dim]
+    scipy_slsqp: df(x), ndarray[dim]
     """
 
     dobj_list = project.obj_df(x)
-    dobj=[0.0]*len(dobj_list[0])
+    dobj = [0.0] * len(dobj_list[0])
 
     for this_dobj in dobj_list:
-        idv=0
+        idv = 0
         for this_dv_dobj in this_dobj:
-            dobj[idv] = dobj[idv]+this_dv_dobj;
-            idv+=1
-    dobj = array( dobj )
+            dobj[idv] = dobj[idv] + this_dv_dobj
+            idv += 1
+    dobj = array(dobj)
 
     return dobj
 
-def con_ceq(x,project):
-    """ cons = con_ceq(x,project)
 
-        Equality Constraint Functions
-        SU2 Project interface to scipy.fmin_slsqp
+def con_ceq(x, project):
+    """cons = con_ceq(x,project)
 
-        su2:         ceq(x) = 0.0, list[nceq]
-        scipy_slsqp: ceq(x) = 0.0, ndarray[nceq]
+    Equality Constraint Functions
+    SU2 Project interface to scipy.fmin_slsqp
+
+    su2:         ceq(x) = 0.0, list[nceq]
+    scipy_slsqp: ceq(x) = 0.0, ndarray[nceq]
     """
 
     cons = project.con_ceq(x)
 
-    if cons: cons = array(cons)
-    else:    cons = zeros([0])
+    if cons:
+        cons = array(cons)
+    else:
+        cons = zeros([0])
 
     return cons
 
-def con_dceq(x,project):
-    """ dcons = con_dceq(x,project)
 
-        Equality Constraint Gradients
-        SU2 Project interface to scipy.fmin_slsqp
+def con_dceq(x, project):
+    """dcons = con_dceq(x,project)
 
-        su2:         dceq(x), list[nceq x dim]
-        scipy_slsqp: dceq(x), ndarray[nceq x dim]
+    Equality Constraint Gradients
+    SU2 Project interface to scipy.fmin_slsqp
+
+    su2:         dceq(x), list[nceq x dim]
+    scipy_slsqp: dceq(x), ndarray[nceq x dim]
     """
 
     dcons = project.con_dceq(x)
 
     dim = project.n_dv
-    if dcons: dcons = array(dcons)
-    else:     dcons = zeros([0,dim])
+    if dcons:
+        dcons = array(dcons)
+    else:
+        dcons = zeros([0, dim])
 
     return dcons
 
-def con_cieq(x,project):
-    """ cons = con_cieq(x,project)
 
-        Inequality Constraints
-        SU2 Project interface to scipy.fmin_slsqp
+def con_cieq(x, project):
+    """cons = con_cieq(x,project)
 
-        su2:         cieq(x) < 0.0, list[ncieq]
-        scipy_slsqp: cieq(x) > 0.0, ndarray[ncieq]
+    Inequality Constraints
+    SU2 Project interface to scipy.fmin_slsqp
+
+    su2:         cieq(x) < 0.0, list[ncieq]
+    scipy_slsqp: cieq(x) > 0.0, ndarray[ncieq]
     """
 
     cons = project.con_cieq(x)
 
-    if cons: cons = array(cons)
-    else:    cons = zeros([0])
+    if cons:
+        cons = array(cons)
+    else:
+        cons = zeros([0])
 
     return -cons
 
-def con_dcieq(x,project):
-    """ dcons = con_dcieq(x,project)
 
-        Inequality Constraint Gradients
-        SU2 Project interface to scipy.fmin_slsqp
+def con_dcieq(x, project):
+    """dcons = con_dcieq(x,project)
 
-        su2:         dcieq(x), list[ncieq x dim]
-        scipy_slsqp: dcieq(x), ndarray[ncieq x dim]
+    Inequality Constraint Gradients
+    SU2 Project interface to scipy.fmin_slsqp
+
+    su2:         dcieq(x), list[ncieq x dim]
+    scipy_slsqp: dcieq(x), ndarray[ncieq x dim]
     """
 
     dcons = project.con_dcieq(x)
 
     dim = project.n_dv
-    if dcons: dcons = array(dcons)
-    else:     dcons = zeros([0,dim])
+    if dcons:
+        dcons = array(dcons)
+    else:
+        dcons = zeros([0, dim])
 
     return -dcons
diff --git a/SU2_PY/SU2/run/__init__.py b/SU2_PY/SU2/run/__init__.py
index 0e092f51e71..7396a698fd1 100644
--- a/SU2_PY/SU2/run/__init__.py
+++ b/SU2_PY/SU2/run/__init__.py
@@ -1,17 +1,10 @@
 # SU2/run/__init__.py
 
-from .interface import (
-    build_command     ,
-    run_command       ,
-    CFD               ,
-    DEF               ,
-    DOT               ,
-    SOL               ,
-    SOL_FSI)
+from .interface import build_command, run_command, CFD, DEF, DOT, SOL, SOL_FSI
 
-from .direct     import direct
-from .adjoint    import adjoint
+from .direct import direct
+from .adjoint import adjoint
 from .projection import projection
-from .deform     import deform
-from .geometry   import geometry
-from .merge      import merge
+from .deform import deform
+from .geometry import geometry
+from .merge import merge
diff --git a/SU2_PY/SU2/run/adjoint.py b/SU2_PY/SU2/run/adjoint.py
index 42a18d7b14e..a9bd9b32b9a 100644
--- a/SU2_PY/SU2/run/adjoint.py
+++ b/SU2_PY/SU2/run/adjoint.py
@@ -31,78 +31,83 @@
 
 import copy
 
-from .. import io  as su2io
-from .merge     import merge     as su2merge
-from .interface import CFD       as SU2_CFD
+from .. import io as su2io
+from .merge import merge as su2merge
+from .interface import CFD as SU2_CFD
 
 # ----------------------------------------------------------------------
 #  Adjoint Simulation
 # ----------------------------------------------------------------------
 
-def adjoint( config ):
-    """ info = SU2.run.adjoint(config)
 
-        Runs an adjoint analysis with:
-            SU2.run.decomp()
-            SU2.run.CFD()
-            SU2.run.merge()
+def adjoint(config):
+    """info = SU2.run.adjoint(config)
 
-        Assumptions:
-            Does not run Gradient Projection
-            Does not rename restart filename to solution filename
-            Adds 'adjoint' suffix to convergence filename
+    Runs an adjoint analysis with:
+        SU2.run.decomp()
+        SU2.run.CFD()
+        SU2.run.merge()
 
-        Outputs:
-            info - SU2 State with keys:
-                HISTORY.ADJOINT_NAME
-                FILES.ADJOINT_NAME
+    Assumptions:
+        Does not run Gradient Projection
+        Does not rename restart filename to solution filename
+        Adds 'adjoint' suffix to convergence filename
 
-        Updates:
-            config.MATH_PROBLEM
+    Outputs:
+        info - SU2 State with keys:
+            HISTORY.ADJOINT_NAME
+            FILES.ADJOINT_NAME
 
-        Executes in:
-            ./
+    Updates:
+        config.MATH_PROBLEM
+
+    Executes in:
+        ./
     """
 
     # local copy
     konfig = copy.deepcopy(config)
 
     # setup problem
-    if konfig.get('GRADIENT_METHOD', 'CONTINUOUS_ADJOINT') == 'DISCRETE_ADJOINT':
-        konfig['MATH_PROBLEM']  = 'DISCRETE_ADJOINT'
+    if konfig.get("GRADIENT_METHOD", "CONTINUOUS_ADJOINT") == "DISCRETE_ADJOINT":
+        konfig["MATH_PROBLEM"] = "DISCRETE_ADJOINT"
     else:
-        konfig['MATH_PROBLEM']  = 'CONTINUOUS_ADJOINT'
+        konfig["MATH_PROBLEM"] = "CONTINUOUS_ADJOINT"
 
-    konfig['CONV_FILENAME'] = konfig['CONV_FILENAME'] + '_adjoint'
+    konfig["CONV_FILENAME"] = konfig["CONV_FILENAME"] + "_adjoint"
 
     # Run Solution
     SU2_CFD(konfig)
 
     # merge
-    konfig['SOLUTION_ADJ_FILENAME'] = konfig['RESTART_ADJ_FILENAME']
+    konfig["SOLUTION_ADJ_FILENAME"] = konfig["RESTART_ADJ_FILENAME"]
     su2merge(konfig)
 
     # filenames
-    plot_format      = konfig.get('TABULAR_FORMAT', 'CSV')
-    plot_extension   = su2io.get_extension(plot_format)
-    history_filename = konfig['CONV_FILENAME'] + plot_extension
-    special_cases    = su2io.get_specialCases(konfig)
+    plot_format = konfig.get("TABULAR_FORMAT", "CSV")
+    plot_extension = su2io.get_extension(plot_format)
+    history_filename = konfig["CONV_FILENAME"] + plot_extension
+    special_cases = su2io.get_specialCases(konfig)
 
     # get history
-    history = su2io.read_history( history_filename, config.NZONES )
+    history = su2io.read_history(history_filename, config.NZONES)
 
     # update super config
-    config.update({ 'MATH_PROBLEM' : konfig['MATH_PROBLEM'] ,
-                    'OBJECTIVE_FUNCTION'  : konfig['OBJECTIVE_FUNCTION']   })
+    config.update(
+        {
+            "MATH_PROBLEM": konfig["MATH_PROBLEM"],
+            "OBJECTIVE_FUNCTION": konfig["OBJECTIVE_FUNCTION"],
+        }
+    )
 
     # files out
-    objective    = konfig['OBJECTIVE_FUNCTION']
+    objective = konfig["OBJECTIVE_FUNCTION"]
     if "," in objective:
-            objective="COMBO"
-    adj_title    = 'ADJOINT_' + objective
-    suffix       = su2io.get_adjointSuffix(objective)
-    restart_name = konfig['RESTART_FILENAME']
-    restart_name = su2io.add_suffix(restart_name,suffix)
+        objective = "COMBO"
+    adj_title = "ADJOINT_" + objective
+    suffix = su2io.get_adjointSuffix(objective)
+    restart_name = konfig["RESTART_FILENAME"]
+    restart_name = su2io.add_suffix(restart_name, suffix)
 
     # info out
     info = su2io.State()
diff --git a/SU2_PY/SU2/run/deform.py b/SU2_PY/SU2/run/deform.py
index 2c8de878a15..6f2638672bf 100644
--- a/SU2_PY/SU2/run/deform.py
+++ b/SU2_PY/SU2/run/deform.py
@@ -31,7 +31,7 @@
 
 import copy
 
-from .. import io  as su2io
+from .. import io as su2io
 from .interface import DEF as SU2_DEF
 
 
@@ -39,66 +39,75 @@
 #  Mesh Deformation
 # ----------------------------------------------------------------------
 
-def deform ( config, dv_new=None, dv_old=None ):
-    """ info = SU2.run.deform(config,dv_new=[],dv_old=[])
 
-        Deforms mesh with:
-            SU2.run.decomp()
-            SU2.run.DEF()
+def deform(config, dv_new=None, dv_old=None):
+    """info = SU2.run.deform(config,dv_new=[],dv_old=[])
 
-        Assumptions:
-            If optional dv_new ommitted, config is setup for deformation
-            If using dv_old, must provide dv_new
-            Adds 'deform' suffix to mesh output name
+    Deforms mesh with:
+        SU2.run.decomp()
+        SU2.run.DEF()
 
-        Outputs:
-            info - SU2 State with keys:
-                HISTORY.ADJOINT_NAME
-                FILES.ADJOINT_NAME
+    Assumptions:
+        If optional dv_new ommitted, config is setup for deformation
+        If using dv_old, must provide dv_new
+        Adds 'deform' suffix to mesh output name
 
-        Updates:
-            config.MESH_FILENAME
-            config.DV_VALUE_OLD = config.DV_VALUE_NEW
+    Outputs:
+        info - SU2 State with keys:
+            HISTORY.ADJOINT_NAME
+            FILES.ADJOINT_NAME
 
-        Executes in:
-            ./
+    Updates:
+        config.MESH_FILENAME
+        config.DV_VALUE_OLD = config.DV_VALUE_NEW
+
+    Executes in:
+        ./
     """
 
-    if dv_new is None: dv_new = []
-    if dv_old is None: dv_old = []
+    if dv_new is None:
+        dv_new = []
+    if dv_old is None:
+        dv_old = []
 
     # error check
-    if dv_old and not dv_new: raise Exception('must provide dv_old with dv_new')
+    if dv_old and not dv_new:
+        raise Exception("must provide dv_old with dv_new")
 
     # local copy
     konfig = copy.deepcopy(config)
 
     # unpack design variables
-    if dv_new: konfig.unpack_dvs(dv_new,dv_old)
+    if dv_new:
+        konfig.unpack_dvs(dv_new, dv_old)
 
     # redundancy check
-    if konfig['DV_VALUE_NEW'] == konfig['DV_VALUE_OLD']:
+    if konfig["DV_VALUE_NEW"] == konfig["DV_VALUE_OLD"]:
         info = su2io.State()
         info.FILES.MESH = konfig.MESH_FILENAME
         info.VARIABLES.DV_VALUE_NEW = konfig.DV_VALUE_NEW
         return info
 
     # setup mesh name
-    suffix = 'deform'
-    mesh_name = konfig['MESH_FILENAME']
-    meshname_suffixed = su2io.add_suffix( mesh_name , suffix )
-    konfig['MESH_OUT_FILENAME'] = meshname_suffixed
+    suffix = "deform"
+    mesh_name = konfig["MESH_FILENAME"]
+    meshname_suffixed = su2io.add_suffix(mesh_name, suffix)
+    konfig["MESH_OUT_FILENAME"] = meshname_suffixed
 
     # Run Deformation
     SU2_DEF(konfig)
 
     # update super config
-    config.update({ 'MESH_FILENAME' : konfig['MESH_OUT_FILENAME'] ,
-                    'DV_KIND'       : konfig['DV_KIND']           ,
-                    'DV_MARKER'     : konfig['DV_MARKER']         ,
-                    'DV_PARAM'      : konfig['DV_PARAM']          ,
-                    'DV_VALUE_OLD'  : konfig['DV_VALUE_NEW']      ,
-                    'DV_VALUE_NEW'  : konfig['DV_VALUE_NEW']      })
+    config.update(
+        {
+            "MESH_FILENAME": konfig["MESH_OUT_FILENAME"],
+            "DV_KIND": konfig["DV_KIND"],
+            "DV_MARKER": konfig["DV_MARKER"],
+            "DV_PARAM": konfig["DV_PARAM"],
+            "DV_VALUE_OLD": konfig["DV_VALUE_NEW"],
+            "DV_VALUE_NEW": konfig["DV_VALUE_NEW"],
+        }
+    )
     # not modified: config['MESH_OUT_FILENAME']
 
     # info out
@@ -108,4 +117,5 @@ def deform ( config, dv_new=None, dv_old=None ):
 
     return info
 
+
 #: def deform()
diff --git a/SU2_PY/SU2/run/direct.py b/SU2_PY/SU2/run/direct.py
index 6ce9dd050d9..2bbe23b1884 100644
--- a/SU2_PY/SU2/run/direct.py
+++ b/SU2_PY/SU2/run/direct.py
@@ -31,47 +31,48 @@
 
 import copy
 
-from .. import io  as su2io
-from .merge     import merge     as su2merge
-from .interface import CFD       as SU2_CFD
+from .. import io as su2io
+from .merge import merge as su2merge
+from .interface import CFD as SU2_CFD
 
 # ----------------------------------------------------------------------
 #  Direct Simulation
 # ----------------------------------------------------------------------
 
-def direct ( config ):
-    """ info = SU2.run.direct(config)
 
-        Runs an adjoint analysis with:
-            SU2.run.decomp()
-            SU2.run.CFD()
-            SU2.run.merge()
+def direct(config):
+    """info = SU2.run.direct(config)
 
-        Assumptions:
-            Does not rename restart filename to solution filename
-            Adds 'direct' suffix to convergence filename
+    Runs an adjoint analysis with:
+        SU2.run.decomp()
+        SU2.run.CFD()
+        SU2.run.merge()
 
-        Outputs:
-            info - SU2 State with keys:
-                FUNCTIONS
-                HISTORY.DIRECT
-                FILES.DIRECT
+    Assumptions:
+        Does not rename restart filename to solution filename
+        Adds 'direct' suffix to convergence filename
 
-        Updates:
-            config.MATH_PROBLEM
+    Outputs:
+        info - SU2 State with keys:
+            FUNCTIONS
+            HISTORY.DIRECT
+            FILES.DIRECT
 
-        Executes in:
-            ./
+    Updates:
+        config.MATH_PROBLEM
+
+    Executes in:
+        ./
     """
 
     # local copy
     konfig = copy.deepcopy(config)
 
     # setup direct problem
-    konfig['MATH_PROBLEM']  = 'DIRECT'
-    konfig['CONV_FILENAME'] = konfig['CONV_FILENAME'] + '_direct'
+    konfig["MATH_PROBLEM"] = "DIRECT"
+    konfig["CONV_FILENAME"] = konfig["CONV_FILENAME"] + "_direct"
 
-    direct_diff = konfig.get('DIRECT_DIFF','NO') == "YES"
+    direct_diff = konfig.get("DIRECT_DIFF", "NO") == "YES"
 
     # Run Solution
     SU2_CFD(konfig)
@@ -80,61 +81,73 @@ def direct ( config ):
     multizone_cases = su2io.get_multizone(konfig)
 
     # merge
-    konfig['SOLUTION_FILENAME'] = konfig['RESTART_FILENAME']
-    if 'FLUID_STRUCTURE_INTERACTION' in multizone_cases:
-        konfig['SOLUTION_FILENAME'] = konfig['RESTART_FILENAME']
+    konfig["SOLUTION_FILENAME"] = konfig["RESTART_FILENAME"]
+    if "FLUID_STRUCTURE_INTERACTION" in multizone_cases:
+        konfig["SOLUTION_FILENAME"] = konfig["RESTART_FILENAME"]
 
     # filenames
-    plot_format      = konfig.get('TABULAR_FORMAT', 'CSV')
-    plot_extension   = su2io.get_extension(plot_format)
+    plot_format = konfig.get("TABULAR_FORMAT", "CSV")
+    plot_extension = su2io.get_extension(plot_format)
 
     # adapt the history_filename, if a restart solution is chosen
     # check for 'RESTART_ITER' is to avoid forced restart situation in "compute_polar.py"...
-    if konfig.get('RESTART_SOL','NO') == 'YES' and konfig.get('RESTART_ITER',1) != 1:
-        if konfig.get('CONFIG_LIST',[]) != []:
-            konfig['CONV_FILENAME'] = 'config_CFD' # master cfg is always config_CFD. Hardcoded names are prob nt ideal.
-        restart_iter = '_'+str(konfig['RESTART_ITER']).zfill(5)
-        history_filename = konfig['CONV_FILENAME'] + restart_iter + plot_extension
+    if konfig.get("RESTART_SOL", "NO") == "YES" and konfig.get("RESTART_ITER", 1) != 1:
+        if konfig.get("CONFIG_LIST", []) != []:
+            konfig[
+                "CONV_FILENAME"
+            ] = "config_CFD"  # master cfg is always config_CFD. Hardcoded names are prob nt ideal.
+        restart_iter = "_" + str(konfig["RESTART_ITER"]).zfill(5)
+        history_filename = konfig["CONV_FILENAME"] + restart_iter + plot_extension
     else:
-        if konfig.get('CONFIG_LIST',[]) != []:
-            konfig['CONV_FILENAME'] = 'config_CFD'
-        history_filename = konfig['CONV_FILENAME'] + plot_extension
-
+        if konfig.get("CONFIG_LIST", []) != []:
+            konfig["CONV_FILENAME"] = "config_CFD"
+        history_filename = konfig["CONV_FILENAME"] + plot_extension
 
-    special_cases    = su2io.get_specialCases(konfig)
+    special_cases = su2io.get_specialCases(konfig)
 
     # averaging final iterations
-    final_avg = config.get('ITER_AVERAGE_OBJ',0)
+    final_avg = config.get("ITER_AVERAGE_OBJ", 0)
     # get chosen windowing function, default is square
-    wnd_fct = config.get('WINDOW_FUNCTION', 'SQUARE')
+    wnd_fct = config.get("WINDOW_FUNCTION", "SQUARE")
 
     # get history and objectives
-    history      = su2io.read_history( history_filename , config.NZONES)
-    aerodynamics = su2io.read_aerodynamics( history_filename , config.NZONES, special_cases, final_avg, wnd_fct )
+    history = su2io.read_history(history_filename, config.NZONES)
+    aerodynamics = su2io.read_aerodynamics(
+        history_filename, config.NZONES, special_cases, final_avg, wnd_fct
+    )
 
     # update super config
-    config.update({ 'MATH_PROBLEM' : konfig['MATH_PROBLEM']  })
+    config.update({"MATH_PROBLEM": konfig["MATH_PROBLEM"]})
 
     # info out
     info = su2io.State()
-    info.FUNCTIONS.update( aerodynamics )
-    info.FILES.DIRECT = konfig['RESTART_FILENAME']
-    if 'INV_DESIGN_CP' in special_cases:
-        info.FILES.TARGET_CP = 'TargetCp.dat'
-    if 'INV_DESIGN_HEATFLUX' in special_cases:
-        info.FILES.TARGET_HEATFLUX = 'TargetHeatFlux.dat'
+    info.FUNCTIONS.update(aerodynamics)
+    info.FILES.DIRECT = konfig["RESTART_FILENAME"]
+    if "INV_DESIGN_CP" in special_cases:
+        info.FILES.TARGET_CP = "TargetCp.dat"
+    if "INV_DESIGN_HEATFLUX" in special_cases:
+        info.FILES.TARGET_HEATFLUX = "TargetHeatFlux.dat"
     info.HISTORY.DIRECT = history
 
-    '''If WINDOW_CAUCHY_CRIT is activated and the time marching converged before the final time has been reached,
-       store the information for the adjoint run'''
-    if config.get('WINDOW_CAUCHY_CRIT', 'NO') == 'YES' and config.TIME_MARCHING != 'NO':
-        konfig['TIME_ITER'] = int(info.HISTORY.DIRECT.Time_Iter[-1] + 1)  # update the last iteration
-        if konfig['UNST_ADJOINT_ITER'] > konfig['TIME_ITER']:
-            konfig['ITER_AVERAGE_OBJ'] = max(0,konfig['ITER_AVERAGE_OBJ'] -(konfig['UNST_ADJOINT_ITER']-konfig['TIME_ITER']))
-            konfig['UNST_ADJOINT_ITER'] = konfig['TIME_ITER']
-
-        info['WND_CAUCHY_DATA'] = {'TIME_ITER': konfig['TIME_ITER'], 'UNST_ADJOINT_ITER': konfig['UNST_ADJOINT_ITER'],
-                                   'ITER_AVERAGE_OBJ': konfig['ITER_AVERAGE_OBJ']}
+    """If WINDOW_CAUCHY_CRIT is activated and the time marching converged before the final time has been reached,
+       store the information for the adjoint run"""
+    if config.get("WINDOW_CAUCHY_CRIT", "NO") == "YES" and config.TIME_MARCHING != "NO":
+        konfig["TIME_ITER"] = int(
+            info.HISTORY.DIRECT.Time_Iter[-1] + 1
+        )  # update the last iteration
+        if konfig["UNST_ADJOINT_ITER"] > konfig["TIME_ITER"]:
+            konfig["ITER_AVERAGE_OBJ"] = max(
+                0,
+                konfig["ITER_AVERAGE_OBJ"]
+                - (konfig["UNST_ADJOINT_ITER"] - konfig["TIME_ITER"]),
+            )
+            konfig["UNST_ADJOINT_ITER"] = konfig["TIME_ITER"]
+
+        info["WND_CAUCHY_DATA"] = {
+            "TIME_ITER": konfig["TIME_ITER"],
+            "UNST_ADJOINT_ITER": konfig["UNST_ADJOINT_ITER"],
+            "ITER_AVERAGE_OBJ": konfig["ITER_AVERAGE_OBJ"],
+        }
 
     su2merge(konfig)
 
diff --git a/SU2_PY/SU2/run/geometry.py b/SU2_PY/SU2/run/geometry.py
index 5180d6862b0..63ccef8c88f 100644
--- a/SU2_PY/SU2/run/geometry.py
+++ b/SU2_PY/SU2/run/geometry.py
@@ -31,66 +31,68 @@
 
 import copy
 
-from .. import io  as su2io
-from .interface import GEO       as SU2_GEO
+from .. import io as su2io
+from .interface import GEO as SU2_GEO
 from ..util import ordered_bunch
 
 # ----------------------------------------------------------------------
 #  Direct Simulation
 # ----------------------------------------------------------------------
 
-def geometry ( config , step = 1e-3 ):
-    """ info = SU2.run.geometry(config)
 
-        Runs an geometry analysis with:
-            SU2.run.decomp()
-            SU2.run.GEO()
+def geometry(config, step=1e-3):
+    """info = SU2.run.geometry(config)
 
-        Assumptions:
-            Performs both function and gradient analysis
+    Runs an geometry analysis with:
+        SU2.run.decomp()
+        SU2.run.GEO()
 
-        Inputs:
-            config - an SU2 configuration
-            step   - gradient finite difference step if config.GEO_MODE=GRADIENT
+    Assumptions:
+        Performs both function and gradient analysis
 
-        Outputs:
-            info - SU2 State with keys:
-                FUNCTIONS
-                GRADIENTS
+    Inputs:
+        config - an SU2 configuration
+        step   - gradient finite difference step if config.GEO_MODE=GRADIENT
 
-        Updates:
+    Outputs:
+        info - SU2 State with keys:
+            FUNCTIONS
+            GRADIENTS
 
-        Executes in:
-            ./
+    Updates:
+
+    Executes in:
+        ./
     """
 
     # local copy
     konfig = copy.deepcopy(config)
 
     # unpack
-    function_name = konfig['GEO_PARAM']
-    tabular_format = konfig.get('TABULAR_FORMAT', 'CSV')
-    func_filename  = konfig['VALUE_OBJFUNC_FILENAME']
-    grad_filename  = konfig['GRAD_OBJFUNC_FILENAME']
-
-    if tabular_format == 'CSV':
-        func_filename = func_filename.split('.')[0] + '.csv'
-        grad_filename = grad_filename.split('.')[0] + '.csv'
+    function_name = konfig["GEO_PARAM"]
+    tabular_format = konfig.get("TABULAR_FORMAT", "CSV")
+    func_filename = konfig["VALUE_OBJFUNC_FILENAME"]
+    grad_filename = konfig["GRAD_OBJFUNC_FILENAME"]
+
+    if tabular_format == "CSV":
+        func_filename = func_filename.split(".")[0] + ".csv"
+        grad_filename = grad_filename.split(".")[0] + ".csv"
     else:
-        func_filename = func_filename.split('.')[0] + '.dat'
-        grad_filename = grad_filename.split('.')[0] + '.dat'
-
+        func_filename = func_filename.split(".")[0] + ".dat"
+        grad_filename = grad_filename.split(".")[0] + ".dat"
 
     # choose dv values
-    Definition_DV = konfig['DEFINITION_DV']
-    n_DV          = len(Definition_DV['KIND'])
-    if isinstance(step,list):
-        assert len(step) == n_DV , 'unexpected step vector length'
+    Definition_DV = konfig["DEFINITION_DV"]
+    n_DV = len(Definition_DV["KIND"])
+    if isinstance(step, list):
+        assert len(step) == n_DV, "unexpected step vector length"
     else:
-        step = [step]*n_DV
-    dv_old = [0.0]*n_DV # SU2_DOT input requirement, assumes linear superposition of design variables
+        step = [step] * n_DV
+    dv_old = [
+        0.0
+    ] * n_DV  # SU2_DOT input requirement, assumes linear superposition of design variables
     dv_new = step
-    konfig.unpack_dvs(dv_new,dv_old)
+    konfig.unpack_dvs(dv_new, dv_old)
 
     # Run Solution
     SU2_GEO(konfig)
@@ -99,15 +101,15 @@ def geometry ( config , step = 1e-3 ):
     info = su2io.State()
 
     # get function values
-    if konfig.GEO_MODE == 'FUNCTION':
+    if konfig.GEO_MODE == "FUNCTION":
         functions = su2io.tools.read_plot(func_filename)
-        for key,value in functions.items():
+        for key, value in functions.items():
             functions[key] = value[0]
-        info.FUNCTIONS.update( functions )
+        info.FUNCTIONS.update(functions)
 
     # get gradient_values
-    if konfig.GEO_MODE == 'GRADIENT':
+    if konfig.GEO_MODE == "GRADIENT":
         gradients = su2io.tools.read_plot(grad_filename)
-        info.GRADIENTS.update( gradients )
+        info.GRADIENTS.update(gradients)
 
     return info
diff --git a/SU2_PY/SU2/run/interface.py b/SU2_PY/SU2/run/interface.py
index cf9df54768f..330e66ba93f 100644
--- a/SU2_PY/SU2/run/interface.py
+++ b/SU2_PY/SU2/run/interface.py
@@ -38,196 +38,206 @@
 #  Setup
 # ------------------------------------------------------------
 
-SU2_RUN = os.environ['SU2_RUN']
-sys.path.append( SU2_RUN )
-quote = '"' if sys.platform == 'win32' else ''
+SU2_RUN = os.environ["SU2_RUN"]
+sys.path.append(SU2_RUN)
+quote = '"' if sys.platform == "win32" else ""
 
 # SU2 suite run command template
-base_Command = os.path.join(SU2_RUN, '%s')
+base_Command = os.path.join(SU2_RUN, "%s")
 
 # check for slurm
-slurm_job = 'SLURM_JOBID' in os.environ
+slurm_job = "SLURM_JOBID" in os.environ
 
 # Check for custom mpi command
-user_defined = 'SU2_MPI_COMMAND' in os.environ
+user_defined = "SU2_MPI_COMMAND" in os.environ
 
 # set mpi command
 if user_defined:
-    mpi_Command = os.environ['SU2_MPI_COMMAND']
+    mpi_Command = os.environ["SU2_MPI_COMMAND"]
 elif slurm_job:
-    mpi_Command = 'srun -n %i %s'
-elif not which('mpirun') is None:
-    mpi_Command = 'mpirun -n %i %s'
-elif not which('mpiexec') is None:
-    mpi_Command = 'mpiexec -n %i %s'
+    mpi_Command = "srun -n %i %s"
+elif not which("mpirun") is None:
+    mpi_Command = "mpirun -n %i %s"
+elif not which("mpiexec") is None:
+    mpi_Command = "mpiexec -n %i %s"
 else:
-    mpi_Command = ''
+    mpi_Command = ""
 
 from .. import EvaluationFailure, DivergenceFailure
+
 return_code_map = {
-    1 : EvaluationFailure ,
-    2 : DivergenceFailure ,
+    1: EvaluationFailure,
+    2: DivergenceFailure,
 }
 
 # ------------------------------------------------------------
 #  SU2 Suite Interface Functions
 # ------------------------------------------------------------
 
+
 def CFD(config):
-    """ run SU2_CFD
-        partitions set by config.NUMBER_PART
+    """run SU2_CFD
+    partitions set by config.NUMBER_PART
     """
     konfig = copy.deepcopy(config)
 
-    direct_diff = not konfig.get('DIRECT_DIFF',"") in ["NONE", ""]
+    direct_diff = not konfig.get("DIRECT_DIFF", "") in ["NONE", ""]
 
-    auto_diff = konfig.MATH_PROBLEM == 'DISCRETE_ADJOINT'
+    auto_diff = konfig.MATH_PROBLEM == "DISCRETE_ADJOINT"
 
     if direct_diff:
-        tempname = 'config_CFD_DIRECTDIFF.cfg'
+        tempname = "config_CFD_DIRECTDIFF.cfg"
 
         konfig.dump(tempname)
 
-        processes = konfig['NUMBER_PART']
+        processes = konfig["NUMBER_PART"]
 
-        the_Command = 'SU2_CFD_DIRECTDIFF%s %s' % (quote, tempname)
+        the_Command = "SU2_CFD_DIRECTDIFF%s %s" % (quote, tempname)
 
     elif auto_diff:
-        tempname = 'config_CFD_AD.cfg'
+        tempname = "config_CFD_AD.cfg"
         konfig.dump(tempname)
 
-        processes = konfig['NUMBER_PART']
+        processes = konfig["NUMBER_PART"]
 
-        the_Command = 'SU2_CFD_AD%s %s' % (quote, tempname)
+        the_Command = "SU2_CFD_AD%s %s" % (quote, tempname)
 
     else:
-        tempname = 'config_CFD.cfg'
+        tempname = "config_CFD.cfg"
         konfig.dump(tempname)
 
-        processes = konfig['NUMBER_PART']
+        processes = konfig["NUMBER_PART"]
 
-        the_Command = 'SU2_CFD%s %s' % (quote, tempname)
+        the_Command = "SU2_CFD%s %s" % (quote, tempname)
 
-    the_Command = build_command( the_Command, processes )
-    run_command( the_Command )
+    the_Command = build_command(the_Command, processes)
+    run_command(the_Command)
 
-    #os.remove(tempname)
+    # os.remove(tempname)
 
     return
 
+
 def DEF(config):
-    """ run SU2_DEF
-        partitions set by config.NUMBER_PART
-        forced to run in serial, expects merged mesh input
+    """run SU2_DEF
+    partitions set by config.NUMBER_PART
+    forced to run in serial, expects merged mesh input
     """
     konfig = copy.deepcopy(config)
 
-    tempname = 'config_DEF.cfg'
+    tempname = "config_DEF.cfg"
     konfig.dump(tempname)
 
     # must run with rank 1
-    processes = konfig['NUMBER_PART']
+    processes = konfig["NUMBER_PART"]
 
-    the_Command = 'SU2_DEF%s %s' % (quote, tempname)
-    the_Command = build_command( the_Command, processes )
-    run_command( the_Command )
+    the_Command = "SU2_DEF%s %s" % (quote, tempname)
+    the_Command = build_command(the_Command, processes)
+    run_command(the_Command)
 
-    #os.remove(tempname)
+    # os.remove(tempname)
 
     return
 
+
 def DOT(config):
-    """ run SU2_DOT
-        partitions set by config.NUMBER_PART
+    """run SU2_DOT
+    partitions set by config.NUMBER_PART
     """
     konfig = copy.deepcopy(config)
 
-    auto_diff = konfig.MATH_PROBLEM == 'DISCRETE_ADJOINT' or konfig.get('AUTO_DIFF','NO') == 'YES'
+    auto_diff = (
+        konfig.MATH_PROBLEM == "DISCRETE_ADJOINT"
+        or konfig.get("AUTO_DIFF", "NO") == "YES"
+    )
 
     if auto_diff:
 
-        tempname = 'config_DOT_AD.cfg'
+        tempname = "config_DOT_AD.cfg"
         konfig.dump(tempname)
 
-        processes = konfig['NUMBER_PART']
+        processes = konfig["NUMBER_PART"]
 
-        the_Command = 'SU2_DOT_AD%s %s' % (quote, tempname)
+        the_Command = "SU2_DOT_AD%s %s" % (quote, tempname)
     else:
 
-        tempname = 'config_DOT.cfg'
+        tempname = "config_DOT.cfg"
         konfig.dump(tempname)
 
-        processes = konfig['NUMBER_PART']
+        processes = konfig["NUMBER_PART"]
 
-        the_Command = 'SU2_DOT%s %s' % (quote, tempname)
+        the_Command = "SU2_DOT%s %s" % (quote, tempname)
 
-    the_Command = build_command( the_Command, processes )
-    run_command( the_Command )
+    the_Command = build_command(the_Command, processes)
+    run_command(the_Command)
 
-    #os.remove(tempname)
+    # os.remove(tempname)
 
     return
 
+
 def GEO(config):
-    """ run SU2_GEO
-        partitions set by config.NUMBER_PART
-        forced to run in serial
+    """run SU2_GEO
+    partitions set by config.NUMBER_PART
+    forced to run in serial
     """
     konfig = copy.deepcopy(config)
 
-    tempname = 'config_GEO.cfg'
+    tempname = "config_GEO.cfg"
     konfig.dump(tempname)
 
     # must run with rank 1
-    processes = konfig['NUMBER_PART']
+    processes = konfig["NUMBER_PART"]
 
-    the_Command = 'SU2_GEO%s %s' % (quote, tempname)
-    the_Command = build_command( the_Command , processes )
-    run_command( the_Command )
+    the_Command = "SU2_GEO%s %s" % (quote, tempname)
+    the_Command = build_command(the_Command, processes)
+    run_command(the_Command)
 
-    #os.remove(tempname)
+    # os.remove(tempname)
 
     return
 
+
 def SOL(config):
-    """ run SU2_SOL
-      partitions set by config.NUMBER_PART
+    """run SU2_SOL
+    partitions set by config.NUMBER_PART
     """
 
     konfig = copy.deepcopy(config)
 
-    tempname = 'config_SOL.cfg'
+    tempname = "config_SOL.cfg"
     konfig.dump(tempname)
 
     # must run with rank 1
-    processes = konfig['NUMBER_PART']
+    processes = konfig["NUMBER_PART"]
 
-    the_Command = 'SU2_SOL%s %s' % (quote, tempname)
-    the_Command = build_command( the_Command , processes )
-    run_command( the_Command )
+    the_Command = "SU2_SOL%s %s" % (quote, tempname)
+    the_Command = build_command(the_Command, processes)
+    run_command(the_Command)
 
-    #os.remove(tempname)
+    # os.remove(tempname)
 
     return
 
+
 def SOL_FSI(config):
-    """ run SU2_SOL for FSI problems
-      partitions set by config.NUMBER_PART
+    """run SU2_SOL for FSI problems
+    partitions set by config.NUMBER_PART
     """
 
     konfig = copy.deepcopy(config)
 
-    tempname = 'config_SOL.cfg'
+    tempname = "config_SOL.cfg"
     konfig.dump(tempname)
 
     # must run with rank 1
-    processes = konfig['NUMBER_PART']
+    processes = konfig["NUMBER_PART"]
 
-    the_Command = 'SU2_SOL%s %s 2' % (quote, tempname)
-    the_Command = build_command( the_Command , processes )
-    run_command( the_Command )
+    the_Command = "SU2_SOL%s %s 2" % (quote, tempname)
+    the_Command = build_command(the_Command, processes)
+    run_command(the_Command)
 
-    #os.remove(tempname)
+    # os.remove(tempname)
 
     return
 
@@ -236,33 +246,43 @@ def SOL_FSI(config):
 #  Helper functions
 # ------------------------------------------------------------
 
-def build_command( the_Command , processes=0 ):
-    """ builds an mpi command for given number of processes """
+
+def build_command(the_Command, processes=0):
+    """builds an mpi command for given number of processes"""
     the_Command = quote + (base_Command % the_Command)
     if processes > 1:
         if not mpi_Command:
-            raise RuntimeError('could not find an mpi interface')
-        the_Command = mpi_Command % (processes,the_Command)
+            raise RuntimeError("could not find an mpi interface")
+        the_Command = mpi_Command % (processes, the_Command)
     return the_Command
 
-def run_command( Command ):
-    """ runs os command with subprocess
-        checks for errors from command
+
+def run_command(Command):
+    """runs os command with subprocess
+    checks for errors from command
     """
 
     sys.stdout.flush()
 
-    proc = subprocess.Popen( Command, shell=True    ,
-                             stdout=sys.stdout      ,
-                             stderr=subprocess.PIPE  )
+    proc = subprocess.Popen(
+        Command, shell=True, stdout=sys.stdout, stderr=subprocess.PIPE
+    )
     return_code = proc.wait()
     message = proc.stderr.read().decode()
 
     if return_code < 0:
-        message = "SU2 process was terminated by signal '%s'\n%s" % (-return_code,message)
+        message = "SU2 process was terminated by signal '%s'\n%s" % (
+            -return_code,
+            message,
+        )
         raise SystemExit(message)
     elif return_code > 0:
-        message = "Path = %s\nCommand = %s\nSU2 process returned error '%s'\n%s" % (os.path.abspath(','),Command,return_code,message)
+        message = "Path = %s\nCommand = %s\nSU2 process returned error '%s'\n%s" % (
+            os.path.abspath(","),
+            Command,
+            return_code,
+            message,
+        )
         if return_code in return_code_map.keys():
             exception = return_code_map[return_code]
         else:
@@ -272,4 +292,3 @@ def run_command( Command ):
         sys.stdout.write(message)
 
     return return_code
-
diff --git a/SU2_PY/SU2/run/merge.py b/SU2_PY/SU2/run/merge.py
index e520df3b440..2e66d14cfc3 100644
--- a/SU2_PY/SU2/run/merge.py
+++ b/SU2_PY/SU2/run/merge.py
@@ -28,7 +28,7 @@
 # ----------------------------------------------------------------------
 
 import os, sys, shutil, copy
-from .. import io  as su2io
+from .. import io as su2io
 from .interface import SOL as SU2_SOL
 from .interface import SOL_FSI as SU2_SOL_FSI
 
@@ -36,32 +36,33 @@
 #  Merge Mesh
 # ----------------------------------------------------------------------
 
-def merge( config ):
-    """ info = SU2.run.merge(config)
 
-        Merges mesh with:
-            SU2.run.SOL()    (volume merging)
-            internal scripts (surface merging)
+def merge(config):
+    """info = SU2.run.merge(config)
 
-        Assumptions:
-            config.NUMBER_PART is set
-            Skip if config.NUMBER_PART > 1
+    Merges mesh with:
+        SU2.run.SOL()    (volume merging)
+        internal scripts (surface merging)
 
-        Inputs:
-            config - an SU2 config
+    Assumptions:
+        config.NUMBER_PART is set
+        Skip if config.NUMBER_PART > 1
 
-        Ouputs:
-            info - an empty SU2 State
+    Inputs:
+        config - an SU2 config
 
-        Executes in:
-            ./
+    Ouputs:
+        info - an empty SU2 State
+
+    Executes in:
+        ./
     """
 
     # local copy
     konfig = copy.deepcopy(config)
 
     # check if needed
-    partitions = konfig['NUMBER_PART']
+    partitions = konfig["NUMBER_PART"]
     if partitions <= 1:
         return su2io.State()
 
@@ -72,10 +73,10 @@ def merge( config ):
     multizone_cases = su2io.get_multizone(konfig)
 
     # # MERGING # #
-    if 'FLUID_STRUCTURE_INTERACTION' in multizone_cases:
+    if "FLUID_STRUCTURE_INTERACTION" in multizone_cases:
         merge_multizone(konfig)
     else:
-        if 'WRT_UNSTEADY' in special_cases:
+        if "WRT_UNSTEADY" in special_cases:
             merge_unsteady(konfig)
         else:
             merge_solution(konfig)
@@ -85,38 +86,45 @@ def merge( config ):
 
     return info
 
+
 #: merge
 
-def merge_unsteady( config, begintime=0, endtime=None ):
+
+def merge_unsteady(config, begintime=0, endtime=None):
 
     if not endtime:
         endtime = config.EXT_ITER
 
     # SU2_SOL handles unsteady volume merge
-    merge_solution( config )
+    merge_solution(config)
 
     return
 
+
 #: def merge_unsteady()
 
-def merge_solution( config ):
-    """ SU2.io.merge.merge_solution(config)
-        general volume surface merging with SU2_SOL
+
+def merge_solution(config):
+    """SU2.io.merge.merge_solution(config)
+    general volume surface merging with SU2_SOL
     """
 
-    SU2_SOL( config )
+    SU2_SOL(config)
 
     return
 
+
 #: merge_solution( config )
 
-def merge_multizone( config, begintime=0, endtime=None ):
+
+def merge_multizone(config, begintime=0, endtime=None):
 
     if not endtime:
         endtime = config.TIME_ITER
 
-    SU2_SOL_FSI( config )
+    SU2_SOL_FSI(config)
 
     return
 
+
 #: merge_solution( config )
diff --git a/SU2_PY/SU2/run/projection.py b/SU2_PY/SU2/run/projection.py
index 6b4ced709bf..fb39aa863a7 100644
--- a/SU2_PY/SU2/run/projection.py
+++ b/SU2_PY/SU2/run/projection.py
@@ -31,7 +31,7 @@
 
 import os, sys, shutil, copy
 
-from .. import io   as su2io
+from .. import io as su2io
 from .. import util as su2util
 from .interface import DOT as SU2_DOT
 
@@ -40,54 +40,59 @@
 #  Gradient Projection
 # ----------------------------------------------------------------------
 
-def projection( config, state={}, step = 1e-3 ):
-    """ info = SU2.run.projection(config,state,step=1e-3)
 
-        Runs an gradient projection with:
-            SU2.run.decomp()
-            SU2.run.DOT()
+def projection(config, state={}, step=1e-3):
+    """info = SU2.run.projection(config,state,step=1e-3)
 
-        Assumptions:
-            Writes tecplot file of gradients
-            Adds objective suffix to gradient plot filename
+    Runs an gradient projection with:
+        SU2.run.decomp()
+        SU2.run.DOT()
 
-        Inputs:
-            config - an SU2 config
-            state  - only required when using external custom DV
-            step   - a float or list of floats for geometry sensitivity
-                     finite difference step
+    Assumptions:
+        Writes tecplot file of gradients
+        Adds objective suffix to gradient plot filename
 
-        Outputs:
-            info - SU2 State with keys:
-                GRADIENTS.<config.OBJECTIVE_FUNCTION>
+    Inputs:
+        config - an SU2 config
+        state  - only required when using external custom DV
+        step   - a float or list of floats for geometry sensitivity
+                 finite difference step
 
-        Updates:
-            config.MATH_PROBLEM
+    Outputs:
+        info - SU2 State with keys:
+            GRADIENTS.<config.OBJECTIVE_FUNCTION>
 
-        Executes in:
-            ./
+    Updates:
+        config.MATH_PROBLEM
+
+    Executes in:
+        ./
     """
     # local copy
     konfig = copy.deepcopy(config)
 
     # choose dv values
-    Definition_DV = konfig['DEFINITION_DV']
-    n_DV          = sum(Definition_DV['SIZE'])
-    if isinstance(step,list):
-        assert len(step) == n_DV , 'unexpected step vector length'
+    Definition_DV = konfig["DEFINITION_DV"]
+    n_DV = sum(Definition_DV["SIZE"])
+    if isinstance(step, list):
+        assert len(step) == n_DV, "unexpected step vector length"
     else:
-        step = [step]*n_DV
-    dv_old = [0.0]*n_DV # SU2_DOT input requirement, assumes linear superposition of design variables
+        step = [step] * n_DV
+    dv_old = [
+        0.0
+    ] * n_DV  # SU2_DOT input requirement, assumes linear superposition of design variables
     dv_new = step
-    konfig.unpack_dvs(dv_new,dv_old)
+    konfig.unpack_dvs(dv_new, dv_old)
 
     # filenames
-    objective      = konfig['OBJECTIVE_FUNCTION']
-    grad_filename  = konfig['GRAD_OBJFUNC_FILENAME']
-    output_format  = konfig.get('TABULAR_FORMAT', 'CSV')
+    objective = konfig["OBJECTIVE_FUNCTION"]
+    grad_filename = konfig["GRAD_OBJFUNC_FILENAME"]
+    output_format = konfig.get("TABULAR_FORMAT", "CSV")
     plot_extension = su2io.get_extension(output_format)
-    adj_suffix     = su2io.get_adjointSuffix(objective)
-    grad_plotname  = os.path.splitext(grad_filename)[0] + '_' + adj_suffix + plot_extension
+    adj_suffix = su2io.get_adjointSuffix(objective)
+    grad_plotname = (
+        os.path.splitext(grad_filename)[0] + "_" + adj_suffix + plot_extension
+    )
 
     # Run Projection
     SU2_DOT(konfig)
@@ -100,19 +105,19 @@ def projection( config, state={}, step = 1e-3 ):
 
     # Write Gradients
     data_plot = su2util.ordered_bunch()
-    data_plot['VARIABLE']     = range(len(raw_gradients))
-    data_plot['GRADIENT']     = raw_gradients
-    data_plot['FINDIFF_STEP'] = step
-    su2util.write_plot(grad_plotname,output_format,data_plot)
+    data_plot["VARIABLE"] = range(len(raw_gradients))
+    data_plot["GRADIENT"] = raw_gradients
+    data_plot["FINDIFF_STEP"] = step
+    su2util.write_plot(grad_plotname, output_format, data_plot)
 
     # gradient output dictionary
-    objective = objective.split(',')
-    if (len(objective)>1 ):
-        objective = ['COMBO']
+    objective = objective.split(",")
+    if len(objective) > 1:
+        objective = ["COMBO"]
 
-    gradients = { objective[0] : raw_gradients }
+    gradients = {objective[0]: raw_gradients}
 
     # info out
-    info.GRADIENTS.update( gradients )
+    info.GRADIENTS.update(gradients)
 
     return info
diff --git a/SU2_PY/SU2/util/__init__.py b/SU2_PY/SU2/util/__init__.py
index 27184c17739..6819e27197f 100644
--- a/SU2_PY/SU2/util/__init__.py
+++ b/SU2_PY/SU2/util/__init__.py
@@ -1,8 +1,8 @@
-from .switch        import switch
-from .bunch import Bunch        as bunch
-from .ordered_dict import OrderedDict  as ordered_dict
+from .switch import switch
+from .bunch import Bunch as bunch
+from .ordered_dict import OrderedDict as ordered_dict
 from .ordered_bunch import OrderedBunch as ordered_bunch
-from .plot          import write_plot, tecplot, paraview
-from .lhc_unif      import lhc_unif
-from .mp_eval       import mp_eval
-from .which         import which
+from .plot import write_plot, tecplot, paraview
+from .lhc_unif import lhc_unif
+from .mp_eval import mp_eval
+from .which import which
diff --git a/SU2_PY/SU2/util/bunch.py b/SU2_PY/SU2/util/bunch.py
index 603671fed53..f2bf6f87824 100644
--- a/SU2_PY/SU2/util/bunch.py
+++ b/SU2_PY/SU2/util/bunch.py
@@ -1,7 +1,7 @@
 #!/usr/bin/env python
 
 """ Bunch is a subclass of dict with attribute-style access.
-    
+
     >>> b = Bunch()
     >>> b.hello = 'world'
     >>> b.hello
@@ -14,99 +14,100 @@
     True
     >>> b.foo is b['foo']
     True
-    
+
     It is safe to import * from this module:
-    
+
         __all__ = ('Bunch', 'bunchify','unbunchify')
-    
+
     un/bunchify provide dictionary conversion; Bunches can also be
     converted via Bunch.to/fromDict().
-    
+
     original source:
     https://pypi.python.org/pypi/bunch
 """
 
+
 class Bunch(dict):
-    """ A dictionary that provides attribute-style access.
-        
-        >>> b = Bunch()
-        >>> b.hello = 'world'
-        >>> b.hello
-        'world'
-        >>> b['hello'] += "!"
-        >>> b.hello
-        'world!'
-        >>> b.foo = Bunch(lol=True)
-        >>> b.foo.lol
-        True
-        >>> b.foo is b['foo']
-        True
-        
-        A Bunch is a subclass of dict; it supports all the methods a dict does...
-        
-        >>> b.keys()
-        ['foo', 'hello']
-        
-        Including update()...
-        
-        >>> b.update({ 'ponies': 'are pretty!' }, hello=42)
-        >>> print(repr(b))
-        Bunch(foo=Bunch(lol=True), hello=42, ponies='are pretty!')
-        
-        As well as iteration...
-        
-        >>> [ (k,b[k]) for k in b ]
-        [('ponies', 'are pretty!'), ('foo', Bunch(lol=True)), ('hello', 42)]
-        
-        And "splats".
-        
-        >>> "The {knights} who say {ni}!".format(**Bunch(knights='lolcats', ni='can haz'))
-        'The lolcats who say can haz!'
-        
-        See unbunchify/Bunch.toDict, bunchify/Bunch.fromDict for notes about conversion.
+    """A dictionary that provides attribute-style access.
+
+    >>> b = Bunch()
+    >>> b.hello = 'world'
+    >>> b.hello
+    'world'
+    >>> b['hello'] += "!"
+    >>> b.hello
+    'world!'
+    >>> b.foo = Bunch(lol=True)
+    >>> b.foo.lol
+    True
+    >>> b.foo is b['foo']
+    True
+
+    A Bunch is a subclass of dict; it supports all the methods a dict does...
+
+    >>> b.keys()
+    ['foo', 'hello']
+
+    Including update()...
+
+    >>> b.update({ 'ponies': 'are pretty!' }, hello=42)
+    >>> print(repr(b))
+    Bunch(foo=Bunch(lol=True), hello=42, ponies='are pretty!')
+
+    As well as iteration...
+
+    >>> [ (k,b[k]) for k in b ]
+    [('ponies', 'are pretty!'), ('foo', Bunch(lol=True)), ('hello', 42)]
+
+    And "splats".
+
+    >>> "The {knights} who say {ni}!".format(**Bunch(knights='lolcats', ni='can haz'))
+    'The lolcats who say can haz!'
+
+    See unbunchify/Bunch.toDict, bunchify/Bunch.fromDict for notes about conversion.
     """
-    
+
     def __contains__(self, k):
-        """ >>> b = Bunch(ponies='are pretty!')
-            >>> 'ponies' in b
-            True
-            >>> 'foo' in b
-            False
-            >>> b['foo'] = 42
-            >>> 'foo' in b
-            True
-            >>> b.hello = 'hai'
-            >>> 'hello' in b
-            True
+        """>>> b = Bunch(ponies='are pretty!')
+        >>> 'ponies' in b
+        True
+        >>> 'foo' in b
+        False
+        >>> b['foo'] = 42
+        >>> 'foo' in b
+        True
+        >>> b.hello = 'hai'
+        >>> 'hello' in b
+        True
         """
         try:
             return hasattr(self, k) or dict.__contains__(self, k)
         except:
             return False
-    
-    # only called if k not found in normal places 
+
+    # only called if k not found in normal places
     def __getattr__(self, k):
-        """ Gets key if it exists, otherwise throws AttributeError.
-            
-            nb. __getattr__ is only called if key is not found in normal places.
-            
-            >>> b = Bunch(bar='baz', lol={})
-            >>> b.foo
-            Traceback (most recent call last):
-                ...
-            AttributeError: foo
-            
-            >>> b.bar
-            'baz'
-            >>> getattr(b, 'bar')
-            'baz'
-            >>> b['bar']
-            'baz'
-            
-            >>> b.lol is b['lol']
-            True
-            >>> b.lol is getattr(b, 'lol')
-            True
+        """Gets key if it exists, otherwise throws AttributeError.
+
+        nb. __getattr__ is only called if key is not found in normal places.
+
+        >>> b = Bunch(bar='baz', lol={})
+        >>> b.foo
+        Traceback (most recent call last):
+            ...
+        AttributeError: foo
+
+        >>> b.bar
+        'baz'
+        >>> getattr(b, 'bar')
+        'baz'
+        >>> b['bar']
+        'baz'
+
+        >>> b.lol is b['lol']
+        True
+        >>> b.lol is getattr(b, 'lol')
+        True
         """
         try:
             # Throws exception if not in prototype chain
@@ -116,22 +117,22 @@ def __getattr__(self, k):
                 return self[k]
             except KeyError:
                 raise AttributeError(k)
-    
+
     def __setattr__(self, k, v):
-        """ Sets attribute k if it exists, otherwise sets key k. A KeyError
-            raised by set-item (only likely if you subclass Bunch) will 
-            propagate as an AttributeError instead.
-            
-            >>> b = Bunch(foo='bar', this_is='useful when subclassing')
-            >>> b.values                            #doctest: +ELLIPSIS
-            <built-in method values of Bunch object at 0x...>
-            >>> b.values = 'uh oh'
-            >>> b.values
-            'uh oh'
-            >>> b['values']
-            Traceback (most recent call last):
-                ...
-            KeyError: 'values'
+        """Sets attribute k if it exists, otherwise sets key k. A KeyError
+        raised by set-item (only likely if you subclass Bunch) will
+        propagate as an AttributeError instead.
+
+        >>> b = Bunch(foo='bar', this_is='useful when subclassing')
+        >>> b.values                            #doctest: +ELLIPSIS
+        <built-in method values of Bunch object at 0x...>
+        >>> b.values = 'uh oh'
+        >>> b.values
+        'uh oh'
+        >>> b['values']
+        Traceback (most recent call last):
+            ...
+        KeyError: 'values'
         """
         try:
             # Throws exception if not in prototype chain
@@ -143,22 +144,22 @@ def __setattr__(self, k, v):
                 raise AttributeError(k)
         else:
             object.__setattr__(self, k, v)
-    
+
     def __delattr__(self, k):
-        """ Deletes attribute k if it exists, otherwise deletes key k. A KeyError
-            raised by deleting the key--such as when the key is missing--will
-            propagate as an AttributeError instead.
-            
-            >>> b = Bunch(lol=42)
-            >>> del b.values
-            Traceback (most recent call last):
-                ...
-            AttributeError: 'Bunch' object attribute 'values' is read-only
-            >>> del b.lol
-            >>> b.lol
-            Traceback (most recent call last):
-                ...
-            AttributeError: lol
+        """Deletes attribute k if it exists, otherwise deletes key k. A KeyError
+        raised by deleting the key--such as when the key is missing--will
+        propagate as an AttributeError instead.
+
+        >>> b = Bunch(lol=42)
+        >>> del b.values
+        Traceback (most recent call last):
+            ...
+        AttributeError: 'Bunch' object attribute 'values' is read-only
+        >>> del b.lol
+        >>> b.lol
+        Traceback (most recent call last):
+            ...
+        AttributeError: lol
         """
         try:
             # Throws exception if not in prototype chain
@@ -170,56 +171,54 @@ def __delattr__(self, k):
                 raise AttributeError(k)
         else:
             object.__delattr__(self, k)
-    
+
     def toDict(self):
-        """ Recursively converts a bunch back into a dictionary.
-            
-            >>> b = Bunch(foo=Bunch(lol=True), hello=42, ponies='are pretty!')
-            >>> b.toDict()
-            {'ponies': 'are pretty!', 'foo': {'lol': True}, 'hello': 42}
-            
-            See unbunchify for more info.
+        """Recursively converts a bunch back into a dictionary.
+
+        >>> b = Bunch(foo=Bunch(lol=True), hello=42, ponies='are pretty!')
+        >>> b.toDict()
+        {'ponies': 'are pretty!', 'foo': {'lol': True}, 'hello': 42}
+
+        See unbunchify for more info.
         """
         return unbunchify(self)
-    
+
     def __repr__(self):
-        """ Invertible* string-form of a Bunch.
-            
-            >>> b = Bunch(foo=Bunch(lol=True), hello=42, ponies='are pretty!')
-            >>> print(repr(b))
-            Bunch(foo=Bunch(lol=True), hello=42, ponies='are pretty!')
-            >>> eval(repr(b))
-            Bunch(foo=Bunch(lol=True), hello=42, ponies='are pretty!')
-            
-            (*) Invertible so long as collection contents are each repr-invertible.
+        """Invertible* string-form of a Bunch.
+
+        >>> b = Bunch(foo=Bunch(lol=True), hello=42, ponies='are pretty!')
+        >>> print(repr(b))
+        Bunch(foo=Bunch(lol=True), hello=42, ponies='are pretty!')
+        >>> eval(repr(b))
+        Bunch(foo=Bunch(lol=True), hello=42, ponies='are pretty!')
+
+        (*) Invertible so long as collection contents are each repr-invertible.
         """
         keys = self.keys()
         keys.sort()
-        args = ', '.join(['%s=%r' % (key, self[key]) for key in keys])
-        return '%s(%s)' % (self.__class__.__name__, args)
-    
+        args = ", ".join(["%s=%r" % (key, self[key]) for key in keys])
+        return "%s(%s)" % (self.__class__.__name__, args)
+
     def __str__(self):
-        """ String-form of a OrderedBunch.
-        """
+        """String-form of a OrderedBunch."""
         keys = self.keys()
         keys.sort()
-        args = ', '.join(['%s=%r' % (key, self[key]) for key in keys])
-        return '{%s}' % args
-    
+        args = ", ".join(["%s=%r" % (key, self[key]) for key in keys])
+        return "{%s}" % args
+
     @staticmethod
     def fromDict(d):
-        """ Recursively transforms a dictionary into a Bunch via copy.
-            
-            >>> b = Bunch.fromDict({'urmom': {'sez': {'what': 'what'}}})
-            >>> b.urmom.sez.what
-            'what'
-            
-            See bunchify for more info.
+        """Recursively transforms a dictionary into a Bunch via copy.
+
+        >>> b = Bunch.fromDict({'urmom': {'sez': {'what': 'what'}}})
+        >>> b.urmom.sez.what
+        'what'
+
+        See bunchify for more info.
         """
         return bunchify(d)
 
 
-
 # While we could convert abstract types like Mapping or Iterable, I think
 # bunchify is more likely to "do what you mean" if it is conservative about
 # casting (ex: isinstance(str,Iterable) == True ).
@@ -227,54 +226,56 @@ def fromDict(d):
 # Should you disagree, it is not difficult to duplicate this function with
 # more aggressive coercion to suit your own purposes.
 
+
 def bunchify(x):
-    """ Recursively transforms a dictionary into a Bunch via copy.
-        
-        >>> b = bunchify({'urmom': {'sez': {'what': 'what'}}})
-        >>> b.urmom.sez.what
-        'what'
-        
-        bunchify can handle intermediary dicts, lists and tuples (as well as 
-        their subclasses), but ymmv on custom datatypes.
-        
-        >>> b = bunchify({ 'lol': ('cats', {'hah':'i win again'}), 
-        ...         'hello': [{'french':'salut', 'german':'hallo'}] })
-        >>> b.hello[0].french
-        'salut'
-        >>> b.lol[1].hah
-        'i win again'
-        
-        nb. As dicts are not hashable, they cannot be nested in sets/frozensets.
+    """Recursively transforms a dictionary into a Bunch via copy.
+
+    >>> b = bunchify({'urmom': {'sez': {'what': 'what'}}})
+    >>> b.urmom.sez.what
+    'what'
+
+    bunchify can handle intermediary dicts, lists and tuples (as well as
+    their subclasses), but ymmv on custom datatypes.
+
+    >>> b = bunchify({ 'lol': ('cats', {'hah':'i win again'}),
+    ...         'hello': [{'french':'salut', 'german':'hallo'}] })
+    >>> b.hello[0].french
+    'salut'
+    >>> b.lol[1].hah
+    'i win again'
+
+    nb. As dicts are not hashable, they cannot be nested in sets/frozensets.
     """
     if isinstance(x, dict):
-        return Bunch( (k, bunchify(v)) for k,v in x.iteritems() )
+        return Bunch((k, bunchify(v)) for k, v in x.iteritems())
     elif isinstance(x, (list, tuple)):
-        return type(x)( bunchify(v) for v in x )
+        return type(x)(bunchify(v) for v in x)
     else:
         return x
 
+
 def unbunchify(x):
-    """ Recursively converts a Bunch into a dictionary.
-        
-        >>> b = Bunch(foo=Bunch(lol=True), hello=42, ponies='are pretty!')
-        >>> unbunchify(b)
-        {'ponies': 'are pretty!', 'foo': {'lol': True}, 'hello': 42}
-        
-        unbunchify will handle intermediary dicts, lists and tuples (as well as
-        their subclasses), but ymmv on custom datatypes.
-        
-        >>> b = Bunch(foo=['bar', Bunch(lol=True)], hello=42, 
-        ...         ponies=('are pretty!', Bunch(lies='are trouble!')))
-        >>> unbunchify(b) #doctest: +NORMALIZE_WHITESPACE
-        {'ponies': ('are pretty!', {'lies': 'are trouble!'}), 
-         'foo': ['bar', {'lol': True}], 'hello': 42}
-        
-        nb. As dicts are not hashable, they cannot be nested in sets/frozensets.
+    """Recursively converts a Bunch into a dictionary.
+
+    >>> b = Bunch(foo=Bunch(lol=True), hello=42, ponies='are pretty!')
+    >>> unbunchify(b)
+    {'ponies': 'are pretty!', 'foo': {'lol': True}, 'hello': 42}
+
+    unbunchify will handle intermediary dicts, lists and tuples (as well as
+    their subclasses), but ymmv on custom datatypes.
+
+    >>> b = Bunch(foo=['bar', Bunch(lol=True)], hello=42,
+    ...         ponies=('are pretty!', Bunch(lies='are trouble!')))
+    >>> unbunchify(b) #doctest: +NORMALIZE_WHITESPACE
+    {'ponies': ('are pretty!', {'lies': 'are trouble!'}),
+     'foo': ['bar', {'lol': True}], 'hello': 42}
+
+    nb. As dicts are not hashable, they cannot be nested in sets/frozensets.
     """
     if isinstance(x, dict):
-        return dict( (k, unbunchify(v)) for k,v in x.iteritems() )
+        return dict((k, unbunchify(v)) for k, v in x.iteritems())
     elif isinstance(x, (list, tuple)):
-        return type(x)( unbunchify(v) for v in x )
+        return type(x)(unbunchify(v) for v in x)
     else:
         return x
 
@@ -286,116 +287,110 @@ def unbunchify(x):
         import json
     except ImportError:
         import simplejson as json
-    
+
     def toJSON(self, **options):
-        """ Serializes this Bunch to JSON. Accepts the same keyword options as `json.dumps()`.
-            
-            >>> b = Bunch(foo=Bunch(lol=True), hello=42, ponies='are pretty!')
-            >>> json.dumps(b)
-            '{"ponies": "are pretty!", "foo": {"lol": true}, "hello": 42}'
-            >>> b.toJSON()
-            '{"ponies": "are pretty!", "foo": {"lol": true}, "hello": 42}'
+        """Serializes this Bunch to JSON. Accepts the same keyword options as `json.dumps()`.
+
+        >>> b = Bunch(foo=Bunch(lol=True), hello=42, ponies='are pretty!')
+        >>> json.dumps(b)
+        '{"ponies": "are pretty!", "foo": {"lol": true}, "hello": 42}'
+        >>> b.toJSON()
+        '{"ponies": "are pretty!", "foo": {"lol": true}, "hello": 42}'
         """
         return json.dumps(self, **options)
-    
+
     Bunch.toJSON = toJSON
-    
+
 except ImportError:
     pass
 
 
-
-
 try:
     # Attempt to register ourself with PyYAML as a representer
     import yaml
     from yaml.representer import Representer, SafeRepresenter
-    
+
     def from_yaml(loader, node):
-        """ PyYAML support for Bunches using the tag `!bunch` and `!bunch.Bunch`.
-            
-            >>> import yaml
-            >>> yaml.load('''
-            ... Flow style: !bunch.Bunch { Clark: Evans, Brian: Ingerson, Oren: Ben-Kiki }
-            ... Block style: !bunch
-            ...   Clark : Evans
-            ...   Brian : Ingerson
-            ...   Oren  : Ben-Kiki
-            ... ''') #doctest: +NORMALIZE_WHITESPACE
-            {'Flow style': Bunch(Brian='Ingerson', Clark='Evans', Oren='Ben-Kiki'), 
-             'Block style': Bunch(Brian='Ingerson', Clark='Evans', Oren='Ben-Kiki')}
-            
-            This module registers itself automatically to cover both Bunch and any 
-            subclasses. Should you want to customize the representation of a subclass,
-            simply register it with PyYAML yourself.
+        """PyYAML support for Bunches using the tag `!bunch` and `!bunch.Bunch`.
+
+        >>> import yaml
+        >>> yaml.load('''
+        ... Flow style: !bunch.Bunch { Clark: Evans, Brian: Ingerson, Oren: Ben-Kiki }
+        ... Block style: !bunch
+        ...   Clark : Evans
+        ...   Brian : Ingerson
+        ...   Oren  : Ben-Kiki
+        ... ''') #doctest: +NORMALIZE_WHITESPACE
+        {'Flow style': Bunch(Brian='Ingerson', Clark='Evans', Oren='Ben-Kiki'),
+         'Block style': Bunch(Brian='Ingerson', Clark='Evans', Oren='Ben-Kiki')}
+
+        This module registers itself automatically to cover both Bunch and any
+        subclasses. Should you want to customize the representation of a subclass,
+        simply register it with PyYAML yourself.
         """
         data = Bunch()
         yield data
         value = loader.construct_mapping(node)
         data.update(value)
-    
-    
+
     def to_yaml_safe(dumper, data):
-        """ Converts Bunch to a normal mapping node, making it appear as a
-            dict in the YAML output.
-            
-            >>> b = Bunch(foo=['bar', Bunch(lol=True)], hello=42)
-            >>> import yaml
-            >>> yaml.safe_dump(b, default_flow_style=True)
-            '{foo: [bar, {lol: true}], hello: 42}\\n'
+        """Converts Bunch to a normal mapping node, making it appear as a
+        dict in the YAML output.
+
+        >>> b = Bunch(foo=['bar', Bunch(lol=True)], hello=42)
+        >>> import yaml
+        >>> yaml.safe_dump(b, default_flow_style=True)
+        '{foo: [bar, {lol: true}], hello: 42}\\n'
         """
         return dumper.represent_dict(data)
-    
+
     def to_yaml(dumper, data):
-        """ Converts Bunch to a representation node.
-            
-            >>> b = Bunch(foo=['bar', Bunch(lol=True)], hello=42)
-            >>> import yaml
-            >>> yaml.dump(b, default_flow_style=True)
-            '!bunch.Bunch {foo: [bar, !bunch.Bunch {lol: true}], hello: 42}\\n'
+        """Converts Bunch to a representation node.
+
+        >>> b = Bunch(foo=['bar', Bunch(lol=True)], hello=42)
+        >>> import yaml
+        >>> yaml.dump(b, default_flow_style=True)
+        '!bunch.Bunch {foo: [bar, !bunch.Bunch {lol: true}], hello: 42}\\n'
         """
-        return dumper.represent_mapping(u'!bunch.Bunch', data)
-    
-    
-    yaml.add_constructor(u'!bunch', from_yaml)
-    yaml.add_constructor(u'!bunch.Bunch', from_yaml)
-    
+        return dumper.represent_mapping("!bunch.Bunch", data)
+
+    yaml.add_constructor("!bunch", from_yaml)
+    yaml.add_constructor("!bunch.Bunch", from_yaml)
+
     SafeRepresenter.add_representer(Bunch, to_yaml_safe)
     SafeRepresenter.add_multi_representer(Bunch, to_yaml_safe)
-    
+
     Representer.add_representer(Bunch, to_yaml)
     Representer.add_multi_representer(Bunch, to_yaml)
-    
-    
+
     # Instance methods for YAML conversion
     def toYAML(self, **options):
-        """ Serializes this Bunch to YAML, using `yaml.safe_dump()` if 
-            no `Dumper` is provided. See the PyYAML documentation for more info.
-            
-            >>> b = Bunch(foo=['bar', Bunch(lol=True)], hello=42)
-            >>> import yaml
-            >>> yaml.safe_dump(b, default_flow_style=True)
-            '{foo: [bar, {lol: true}], hello: 42}\\n'
-            >>> b.toYAML(default_flow_style=True)
-            '{foo: [bar, {lol: true}], hello: 42}\\n'
-            >>> yaml.dump(b, default_flow_style=True)
-            '!bunch.Bunch {foo: [bar, !bunch.Bunch {lol: true}], hello: 42}\\n'
-            >>> b.toYAML(Dumper=yaml.Dumper, default_flow_style=True)
-            '!bunch.Bunch {foo: [bar, !bunch.Bunch {lol: true}], hello: 42}\\n'
+        """Serializes this Bunch to YAML, using `yaml.safe_dump()` if
+        no `Dumper` is provided. See the PyYAML documentation for more info.
+
+        >>> b = Bunch(foo=['bar', Bunch(lol=True)], hello=42)
+        >>> import yaml
+        >>> yaml.safe_dump(b, default_flow_style=True)
+        '{foo: [bar, {lol: true}], hello: 42}\\n'
+        >>> b.toYAML(default_flow_style=True)
+        '{foo: [bar, {lol: true}], hello: 42}\\n'
+        >>> yaml.dump(b, default_flow_style=True)
+        '!bunch.Bunch {foo: [bar, !bunch.Bunch {lol: true}], hello: 42}\\n'
+        >>> b.toYAML(Dumper=yaml.Dumper, default_flow_style=True)
+        '!bunch.Bunch {foo: [bar, !bunch.Bunch {lol: true}], hello: 42}\\n'
         """
         opts = dict(indent=4, default_flow_style=False)
         opts.update(options)
-        if 'Dumper' not in opts:
+        if "Dumper" not in opts:
             return yaml.safe_dump(self, **opts)
         else:
             return yaml.dump(self, **opts)
-    
+
     def fromYAML(*args, **kwargs):
-        return bunchify( yaml.load(*args, **kwargs) )
-    
+        return bunchify(yaml.load(*args, **kwargs))
+
     Bunch.toYAML = Bunch.__repr__ = toYAML
     Bunch.fromYAML = staticmethod(fromYAML)
-    
+
 except ImportError:
     pass
-
diff --git a/SU2_PY/SU2/util/filter_adjoint.py b/SU2_PY/SU2/util/filter_adjoint.py
index b59283535dd..a7e1df79247 100644
--- a/SU2_PY/SU2/util/filter_adjoint.py
+++ b/SU2_PY/SU2/util/filter_adjoint.py
@@ -38,6 +38,7 @@
 # plotting with matplotlib
 try:
     import pylab as plt
+
     pylab_imported = True
 except ImportError:
     pylab_imported = False
@@ -49,24 +50,43 @@
 def main():
 
     # Command Line Options
-    parser=OptionParser()
-    parser.add_option( "-f", "--file",       dest="filename",
-                       help="read config from FILE", metavar="FILE" )
-    parser.add_option( "-t", "--type",       dest="filter_type",  default='LAPLACE',
-                       help="apply filter TYPE", metavar="TYPE" )
-    parser.add_option( "-m", "--marker",     dest="marker_name",  default='airfoil',
-                        help="use marker named TAG", metavar="TAG" )
-    parser.add_option( "-c", "--chord",      dest="chord_length", default=1.0,
-                        help="reference CHORD length", metavar="CHORD" )
-
-    (options, args)=parser.parse_args()
-    options.chord_length = float( options.chord_length )
+    parser = OptionParser()
+    parser.add_option(
+        "-f", "--file", dest="filename", help="read config from FILE", metavar="FILE"
+    )
+    parser.add_option(
+        "-t",
+        "--type",
+        dest="filter_type",
+        default="LAPLACE",
+        help="apply filter TYPE",
+        metavar="TYPE",
+    )
+    parser.add_option(
+        "-m",
+        "--marker",
+        dest="marker_name",
+        default="airfoil",
+        help="use marker named TAG",
+        metavar="TAG",
+    )
+    parser.add_option(
+        "-c",
+        "--chord",
+        dest="chord_length",
+        default=1.0,
+        help="reference CHORD length",
+        metavar="CHORD",
+    )
+
+    (options, args) = parser.parse_args()
+    options.chord_length = float(options.chord_length)
 
     # run filter
-    process_surface_adjoint( options.filename     ,
-                             options.filter_type  ,
-                             options.marker_name  ,
-                             options.chord_length  )
+    process_surface_adjoint(
+        options.filename, options.filter_type, options.marker_name, options.chord_length
+    )
+
 
 #: def main()
 
@@ -74,57 +94,55 @@ def main():
 # -------------------------------------------------------------------
 #  PROCESS SURFACE ADJOINT
 # -------------------------------------------------------------------
-def process_surface_adjoint( config_filename       ,
-                             filter_type='LAPLACE' ,
-                             marker_name='airfoil' ,
-                             chord_length=1.0       ):
+def process_surface_adjoint(
+    config_filename, filter_type="LAPLACE", marker_name="airfoil", chord_length=1.0
+):
 
-    print('')
-    print('-------------------------------------------------------------------------')
-    print('|                 SU2 Suite (Process Surface Adjoint)                   |')
-    print('-------------------------------------------------------------------------')
-    print('')
+    print("")
+    print("-------------------------------------------------------------------------")
+    print("|                 SU2 Suite (Process Surface Adjoint)                   |")
+    print("-------------------------------------------------------------------------")
+    print("")
 
     # some other defaults
-    c_clip   = 0.01 # percent chord to truncate
-    fft_copy = 5    # number of times to copy the fft signal
-    smth_len = 0.05 # percent chord smoothing window length
-    lapl_len = 1e-4 # laplace smoothing parameter
+    c_clip = 0.01  # percent chord to truncate
+    fft_copy = 5  # number of times to copy the fft signal
+    smth_len = 0.05  # percent chord smoothing window length
+    lapl_len = 1e-4  # laplace smoothing parameter
 
     # read config file
     config_data = libSU2.Get_ConfigParams(config_filename)
-    surface_filename = config_data['SURFACE_ADJ_FILENAME'] + '.csv'
+    surface_filename = config_data["SURFACE_ADJ_FILENAME"] + ".csv"
     print(surface_filename)
-    mesh_filename    = config_data['MESH_FILENAME']
-    gradient         = config_data['OBJECTIVE_FUNCTION']
+    mesh_filename = config_data["MESH_FILENAME"]
+    gradient = config_data["OBJECTIVE_FUNCTION"]
 
-    print('Config filename = %s' % config_filename)
-    print('Surface filename = %s' % surface_filename)
-    print('Filter Type = %s' % filter_type)
+    print("Config filename = %s" % config_filename)
+    print("Surface filename = %s" % surface_filename)
+    print("Filter Type = %s" % filter_type)
 
     # read adjoint data
-    adj_data = np.genfromtxt( surface_filename    ,
-                              dtype       = float ,
-                              delimiter   = ','   ,
-                              skip_header = 1      )
+    adj_data = np.genfromtxt(
+        surface_filename, dtype=float, delimiter=",", skip_header=1
+    )
 
     # read mesh data
     mesh_data = libSU2_mesh.Read_Mesh(mesh_filename)
 
     # proces adjoint data
-    P      = map(int, adj_data[:,0] )
-    X      = adj_data[:,6].copy()
-    Y      = adj_data[:,7].copy()
-    Sens   = adj_data[:,1].copy()
-    PsiRho = adj_data[:,2].copy()
-    I      = range(0,len(P)) # important - for unsorting durring write
+    P = map(int, adj_data[:, 0])
+    X = adj_data[:, 6].copy()
+    Y = adj_data[:, 7].copy()
+    Sens = adj_data[:, 1].copy()
+    PsiRho = adj_data[:, 2].copy()
+    I = range(0, len(P))  # important - for unsorting durring write
 
     # store in dict by point index
-    adj_data_dict = dict( zip( P , zip(X,Y,Sens,PsiRho,I) ) )
+    adj_data_dict = dict(zip(P, zip(X, Y, Sens, PsiRho, I)))
 
     # sort airfoil points
-    iP_sorted,_ = libSU2_mesh.sort_Airfoil(mesh_data,marker_name)
-    assert(len(iP_sorted) == len(P))
+    iP_sorted, _ = libSU2_mesh.sort_Airfoil(mesh_data, marker_name)
+    assert len(iP_sorted) == len(P)
 
     # rebuild airfoil loop
     i = 0
@@ -132,56 +150,59 @@ def process_surface_adjoint( config_filename       ,
         # the adjoint data entry
         this_adj_data = adj_data_dict[this_P]
         # re-sort
-        P[i]      = this_P
-        X[i]      = this_adj_data[0]
-        Y[i]      = this_adj_data[1]
-        Sens[i]   = this_adj_data[2]
+        P[i] = this_P
+        X[i] = this_adj_data[0]
+        Y[i] = this_adj_data[1]
+        Sens[i] = this_adj_data[2]
         PsiRho[i] = this_adj_data[3]
-        I[i]      = this_adj_data[4]
+        I[i] = this_adj_data[4]
         # next
-        i = i+1
+        i = i + 1
     #: for each point
 
     # calculate arc length
-    S = np.sqrt( np.diff(X)**2 + np.diff(Y)**2 ) / chord_length
-    S = np.cumsum( np.hstack([ 0 , S ]) )
+    S = np.sqrt(np.diff(X) ** 2 + np.diff(Y) ** 2) / chord_length
+    S = np.cumsum(np.hstack([0, S]))
 
     # tail trucating, by arc length
-    I_clip_lo = S < S[0]  + c_clip
+    I_clip_lo = S < S[0] + c_clip
     I_clip_hi = S > S[-1] - c_clip
-    S_clip    = S.copy()
+    S_clip = S.copy()
     Sens_clip = Sens.copy()
     Sens_clip[I_clip_hi] = Sens_clip[I_clip_hi][0]
     Sens_clip[I_clip_lo] = Sens_clip[I_clip_lo][-1]
 
-
     # some edge length statistics
     dS_clip = np.diff(S_clip)
-    min_dS  = np.min ( dS_clip )
-    mean_dS = np.mean( dS_clip )
-    max_dS  = np.max ( dS_clip )
-    #print 'min_dS = %.4e ; mean_dS = %.4e ; max_dS = %.4e' % ( min_dS , mean_dS , max_dS )
+    min_dS = np.min(dS_clip)
+    mean_dS = np.mean(dS_clip)
+    max_dS = np.max(dS_clip)
+    # print 'min_dS = %.4e ; mean_dS = %.4e ; max_dS = %.4e' % ( min_dS , mean_dS , max_dS )
 
     # --------------------------------------------
     #  APPLY FILTER
 
-    if filter_type == 'FOURIER':
-        Freq_notch = [ 1/max_dS, np.inf ] # the notch frequencies
-        Sens_filter,Frequency,Power = fft_filter( S_clip,Sens_clip, Freq_notch, fft_copy )
-        #Sens_filter = smooth(S_clip,Sens_filter, 0.03,'blackman') # post smoothing
-
-    elif filter_type == 'WINDOW':
-        Sens_filter   = window( S_clip, Sens_clip, smth_len, 'blackman' )
-
-    elif filter_type == 'LAPLACE':
-        Sens_filter   = laplace( S_clip, Sens_clip, lapl_len )
-
-    elif filter_type == 'SHARPEN':
-        Sens_smooth   = smooth( S_clip, Sens_clip  , smth_len/5, 'blackman' ) # pre smoothing
-        Sens_smoother = smooth( S_clip, Sens_smooth, smth_len  , 'blackman' )
-        Sens_filter = Sens_smooth + (Sens_smooth - Sens_smoother)             # sharpener
+    if filter_type == "FOURIER":
+        Freq_notch = [1 / max_dS, np.inf]  # the notch frequencies
+        Sens_filter, Frequency, Power = fft_filter(
+            S_clip, Sens_clip, Freq_notch, fft_copy
+        )
+        # Sens_filter = smooth(S_clip,Sens_filter, 0.03,'blackman') # post smoothing
+
+    elif filter_type == "WINDOW":
+        Sens_filter = window(S_clip, Sens_clip, smth_len, "blackman")
+
+    elif filter_type == "LAPLACE":
+        Sens_filter = laplace(S_clip, Sens_clip, lapl_len)
+
+    elif filter_type == "SHARPEN":
+        Sens_smooth = smooth(
+            S_clip, Sens_clip, smth_len / 5, "blackman"
+        )  # pre smoothing
+        Sens_smoother = smooth(S_clip, Sens_smooth, smth_len, "blackman")
+        Sens_filter = Sens_smooth + (Sens_smooth - Sens_smoother)  # sharpener
     else:
-        raise Exception('unknown filter type')
+        raise Exception("unknown filter type")
 
     # --------------------------------------------
     #  PLOTTING
@@ -191,50 +212,50 @@ def process_surface_adjoint( config_filename       ,
         # start plot
         fig = plt.figure(gradient)
         plt.clf()
-        #if not fig.axes:          # for comparing two filter calls
-            #plt.subplot(1,1,1)
-        #ax = fig.axes[0]
-        #if len(ax.lines) == 4:
-            #ax.lines.pop(0)
-            #ax.lines.pop(0)
+        # if not fig.axes:          # for comparing two filter calls
+        # plt.subplot(1,1,1)
+        # ax = fig.axes[0]
+        # if len(ax.lines) == 4:
+        # ax.lines.pop(0)
+        # ax.lines.pop(0)
 
         # SENSITIVITY
-        plt.plot(S     ,Sens       ,color='b') # original
-        plt.plot(S_clip,Sens_filter,color='r') # filtered
+        plt.plot(S, Sens, color="b")  # original
+        plt.plot(S_clip, Sens_filter, color="r")  # filtered
 
-        plt.xlim(-0.1,2.1)
-        plt.ylim(-5,5)
-        plt.xlabel('Arc Length')
-        plt.ylabel('Surface Sensitivity')
+        plt.xlim(-0.1, 2.1)
+        plt.ylim(-5, 5)
+        plt.xlabel("Arc Length")
+        plt.ylabel("Surface Sensitivity")
 
-        #if len(ax.lines) == 4:
-            #seq = [2, 2, 7, 2]
-            #ax.lines[0].set_dashes(seq)
-            #ax.lines[1].set_dashes(seq)
+        # if len(ax.lines) == 4:
+        # seq = [2, 2, 7, 2]
+        # ax.lines[0].set_dashes(seq)
+        # ax.lines[1].set_dashes(seq)
 
-        plot_filename = os.path.splitext(surface_filename)[0] + '.png'
-        plt.savefig('Sens_'+plot_filename,dpi=300)
+        plot_filename = os.path.splitext(surface_filename)[0] + ".png"
+        plt.savefig("Sens_" + plot_filename, dpi=300)
 
         # zoom in
-        plt.ylim(-0.4,0.4)
-        plt.savefig('Sens_zoom_'+plot_filename,dpi=300)
+        plt.ylim(-0.4, 0.4)
+        plt.savefig("Sens_zoom_" + plot_filename, dpi=300)
 
         # SPECTRAL
-        if filter_type == 'FOURIER':
+        if filter_type == "FOURIER":
 
-            plt.figure('SPECTRAL')
+            plt.figure("SPECTRAL")
             plt.clf()
 
-            plt.plot(Frequency,Power)
+            plt.plot(Frequency, Power)
 
-            #plt.xlim(0,Freq_notch[0]+10)
-            plt.xlim(0,200)
-            plt.ylim(0,0.15)
+            # plt.xlim(0,Freq_notch[0]+10)
+            plt.xlim(0, 200)
+            plt.ylim(0, 0.15)
 
-            plt.xlabel('Frequency (1/C)')
-            plt.ylabel('Surface Sensitivity Spectal Power')
+            plt.xlabel("Frequency (1/C)")
+            plt.ylabel("Surface Sensitivity Spectal Power")
 
-            plt.savefig('Spectral_'+plot_filename,dpi=300)
+            plt.savefig("Spectral_" + plot_filename, dpi=300)
 
         #: if spectral plot
 
@@ -244,12 +265,12 @@ def process_surface_adjoint( config_filename       ,
     #  SAVE SURFACE FILE
 
     # reorder back to input surface points
-    Sens_out    = np.zeros(len(S))
-    Sens_out[I] = Sens_filter # left over from sort
-    adj_data[:,1] = Sens_out
+    Sens_out = np.zeros(len(S))
+    Sens_out[I] = Sens_filter  # left over from sort
+    adj_data[:, 1] = Sens_out
 
     # get surface header
-    surface_orig = open(surface_filename,'r')
+    surface_orig = open(surface_filename, "r")
     header = surface_orig.readline()
     surface_orig.close()
 
@@ -258,31 +279,33 @@ def process_surface_adjoint( config_filename       ,
     prefix_names = prefix_names.values()
 
     # add filter prefix, before adjoint prefix
-    surface_filename_split = surface_filename.rstrip('.csv').split('_')
+    surface_filename_split = surface_filename.rstrip(".csv").split("_")
     if surface_filename_split[-1] in prefix_names:
-        surface_filename_split = surface_filename_split[0:-1] + ['filtered'] + [surface_filename_split[-1]]
+        surface_filename_split = (
+            surface_filename_split[0:-1] + ["filtered"] + [surface_filename_split[-1]]
+        )
     else:
-        surface_filename_split = surface_filename_split + ['filtered']
-    surface_filename_new = '_'.join(surface_filename_split) + '.csv'
+        surface_filename_split = surface_filename_split + ["filtered"]
+    surface_filename_new = "_".join(surface_filename_split) + ".csv"
 
     # write filtered surface file (only updates Sensitivity)
-    surface_new = open(surface_filename_new,'w')
+    surface_new = open(surface_filename_new, "w")
     surface_new.write(header)
     for row in adj_data:
-        for i,value in enumerate(row):
+        for i, value in enumerate(row):
             if i > 0:
-                surface_new.write(', ')
+                surface_new.write(", ")
             if i == 0:
-                surface_new.write('%i' % value )
+                surface_new.write("%i" % value)
             else:
-                surface_new.write('%.16e' % value )
-        surface_new.write('\n')
+                surface_new.write("%.16e" % value)
+        surface_new.write("\n")
     surface_new.close()
 
+    print("")
+    print("----------------- Exit Success (Process Surface Adjoint) ----------------")
+    print("")
 
-    print('')
-    print('----------------- Exit Success (Process Surface Adjoint) ----------------')
-    print('')
 
 #: def process_surface_adjoint()
 
@@ -291,45 +314,48 @@ def process_surface_adjoint( config_filename       ,
 #  LAPLACIAN SMOOTHING
 # -------------------------------------------------------------------
 
-def laplace(t,x,e):
-    ''' Laplacian filter
-        input:
-            t - time sample vector
-            x - signal vector x(t)
-            e - smoother coefficient (e>0)
 
-        output:
-            y: smoothed signal at t
-    '''
+def laplace(t, x, e):
+    """Laplacian filter
+    input:
+        t - time sample vector
+        x - signal vector x(t)
+        e - smoother coefficient (e>0)
+
+    output:
+        y: smoothed signal at t
+    """
 
     n_x = len(x)
 
     # padding
-    t_1 = t[ 0] + t[-2]-t[-1]
-    t_2 = t[-1] + t[ 1]-t[ 0]
-    t_p = np.hstack([ t_1  , t , t_2   ])
-    x_p = np.hstack([ x[0] , x , x[-1] ])
+    t_1 = t[0] + t[-2] - t[-1]
+    t_2 = t[-1] + t[1] - t[0]
+    t_p = np.hstack([t_1, t, t_2])
+    x_p = np.hstack([x[0], x, x[-1]])
 
     # finite differencing
-    dt_f = t_p[2:  ] - t_p[1:-1]
+    dt_f = t_p[2:] - t_p[1:-1]
     dt_b = t_p[1:-1] - t_p[0:-2]
-    dt_c = t_p[2:  ] - t_p[0:-2]
+    dt_c = t_p[2:] - t_p[0:-2]
 
     # diagonal coefficients
-    Coeff = e * 2.0 / (dt_b*dt_f*dt_c)
-    diag_c =  Coeff*dt_c
-    diag_f = -Coeff*dt_b
-    diag_b = -Coeff*dt_f
+    Coeff = e * 2.0 / (dt_b * dt_f * dt_c)
+    diag_c = Coeff * dt_c
+    diag_f = -Coeff * dt_b
+    diag_b = -Coeff * dt_f
 
     # system matrix
-    A = ( np.diag(diag_c      , 0) +
-          np.diag(diag_f[0:-1], 1) +
-          np.diag(diag_b[1:  ],-1) +
-          np.diag(np.ones(n_x), 0)  )
+    A = (
+        np.diag(diag_c, 0)
+        + np.diag(diag_f[0:-1], 1)
+        + np.diag(diag_b[1:], -1)
+        + np.diag(np.ones(n_x), 0)
+    )
 
     # periodic conditions
-    #A[1,-1] = dt_b[0]
-    #A[-1,1] = dt_f[-1]
+    # A[1,-1] = dt_b[0]
+    # A[-1,1] = dt_f[-1]
 
     # rhs
     b = np.array([x]).T
@@ -338,26 +364,27 @@ def laplace(t,x,e):
 
     # signal start
     i_d = 0
-    A[i_d,:] = 0.0
-    A[i_d,i_d]   = 1.0        # dirichlet
-    #A[i_d,i_d+1] =  1.0       # neuman
-    #A[i_d,i_d]   = -1.0
-    #b[i_d] = 0.0 #x[i_d+1]-x[i_d]
+    A[i_d, :] = 0.0
+    A[i_d, i_d] = 1.0  # dirichlet
+    # A[i_d,i_d+1] =  1.0       # neuman
+    # A[i_d,i_d]   = -1.0
+    # b[i_d] = 0.0 #x[i_d+1]-x[i_d]
 
     # signal end
-    i_d = n_x-1
-    A[i_d,:] = 0.0
-    A[i_d,i_d]   = 1.0        # dirichlet
-    #A[i_d,i_d]   =  1.0       # neuman
-    #A[i_d,i_d-1] = -1.0
-    #b[i_d] = 0.0 #x[i_d]-x[i_d-1]
+    i_d = n_x - 1
+    A[i_d, :] = 0.0
+    A[i_d, i_d] = 1.0  # dirichlet
+    # A[i_d,i_d]   =  1.0       # neuman
+    # A[i_d,i_d-1] = -1.0
+    # b[i_d] = 0.0 #x[i_d]-x[i_d-1]
 
     # solve
-    y = np.linalg.solve(A,b)
-    y = y[:,0]
+    y = np.linalg.solve(A, b)
+    y = y[:, 0]
 
     return y
 
+
 #: def laplace
 
 
@@ -365,54 +392,55 @@ def laplace(t,x,e):
 #  FFT NOTCH FILTER
 # -------------------------------------------------------------------
 
-def fft_filter(t,x,n,c=1):
-    ''' Notch filter with Fast Fourier Transform
-        input:
-            t = input time vector
-            x = input signal vector
-            n = [low,high] frequency range to supress
-            c = number of times to duplicate signal
 
-        output:
-            y = smoothed signal at t
+def fft_filter(t, x, n, c=1):
+    """Notch filter with Fast Fourier Transform
+    input:
+        t = input time vector
+        x = input signal vector
+        n = [low,high] frequency range to supress
+        c = number of times to duplicate signal
 
-        signal will be interpolated to constant spacing
-    '''
+    output:
+        y = smoothed signal at t
+
+    signal will be interpolated to constant spacing
+    """
 
-    assert(c>0)
+    assert c > 0
 
     # choose sampling frequency
-    min_dt  = np.min( np.diff(t) )
-    Ts = min_dt/2
-    Fs = 1/Ts
+    min_dt = np.min(np.diff(t))
+    Ts = min_dt / 2
+    Fs = 1 / Ts
 
     # interpolate to constant spacing
-    nt_lin = int( t[-1]/Ts )
-    t_lin = np.linspace(0,t[-1],nt_lin)
-    x_lin = np.interp(t_lin,t,x)
+    nt_lin = int(t[-1] / Ts)
+    t_lin = np.linspace(0, t[-1], nt_lin)
+    x_lin = np.interp(t_lin, t, x)
 
     # pad last index
-    t_lin = np.hstack([ t_lin , t_lin[0:10]+t_lin[-1] ])
-    x_lin = np.hstack([ x_lin , np.ones(10)*x_lin[-1] ])
+    t_lin = np.hstack([t_lin, t_lin[0:10] + t_lin[-1]])
+    x_lin = np.hstack([x_lin, np.ones(10) * x_lin[-1]])
 
     # copy signal
-    for ic in range(c-1):
-        t_lin = np.hstack([ t_lin[0:-2] , t_lin[1:]+t_lin[-1] ])
-        x_lin = np.hstack([ x_lin[0:-2] , x_lin[1:] ])
+    for ic in range(c - 1):
+        t_lin = np.hstack([t_lin[0:-2], t_lin[1:] + t_lin[-1]])
+        x_lin = np.hstack([x_lin[0:-2], x_lin[1:]])
     nt = len(t_lin)
 
     # perform fourier transform
-    nxtpow2 = int(math.log(nt, 2))+1 # next power of 2
-    nfft = 2**nxtpow2                # fft efficiency
-    P = np.fft.rfft(x_lin,nfft)      # the transform
-    a = np.angle(P)                  # complex
-    p = np.absolute(P)               # complex
-    p = p/nt                         # normalize
-    p = 2*p[0:(nfft/2)]              # symmetric
-    a = a[0:(nfft/2)]                # symmetric
+    nxtpow2 = int(math.log(nt, 2)) + 1  # next power of 2
+    nfft = 2**nxtpow2  # fft efficiency
+    P = np.fft.rfft(x_lin, nfft)  # the transform
+    a = np.angle(P)  # complex
+    p = np.absolute(P)  # complex
+    p = p / nt  # normalize
+    p = 2 * p[0 : (nfft / 2)]  # symmetric
+    a = a[0 : (nfft / 2)]  # symmetric
 
     # frequency domain
-    F = np.arange(0,nfft/2) * Fs/nfft
+    F = np.arange(0, nfft / 2) * Fs / nfft
 
     # for return
     Freq = F.copy()
@@ -421,30 +449,31 @@ def fft_filter(t,x,n,c=1):
     #  THE NOTCH FILTER
 
     # filter multiplier
-    k = np.ones(nfft/2)
+    k = np.ones(nfft / 2)
 
     # clip power within notch frequencies
-    I_fil = np.logical_and( F>n[0] , F<n[1] )
+    I_fil = np.logical_and(F > n[0], F < n[1])
     k[I_fil] = 0.0
 
     # change the power spectrum
-    p = p*k
+    p = p * k
 
     # For Return
     Pow = p.copy()
 
     # untransform
-    p = p*nt/2.
-    p = np.hstack( [ p , p[::-1] ] )
-    a = np.hstack( [ a , -a[::-1] ] )
-    P = p*(np.cos(a) + 1j*np.sin(a))
-    y_lin = np.fft.irfft(P,nfft)       # the inverse transform
+    p = p * nt / 2.0
+    p = np.hstack([p, p[::-1]])
+    a = np.hstack([a, -a[::-1]])
+    P = p * (np.cos(a) + 1j * np.sin(a))
+    y_lin = np.fft.irfft(P, nfft)  # the inverse transform
     y_lin = y_lin[0:nt]
 
     # interpolate back to given t
-    y = np.interp(t,t_lin,y_lin)
+    y = np.interp(t, t_lin, y_lin)
+
+    return y, Freq, Pow
 
-    return y,Freq,Pow
 
 # def: fft_filter()
 
@@ -453,7 +482,8 @@ def fft_filter(t,x,n,c=1):
 #  WINDOWED SMOOTHING
 # -------------------------------------------------------------------
 
-def window(t,x,window_delta,window='hanning'):
+
+def window(t, x, window_delta, window="hanning"):
     """Smooth the data using a window with requested size and shape
 
     original source:
@@ -474,39 +504,42 @@ def window(t,x,window_delta,window='hanning'):
     if x.ndim != 1:
         raise ValueError("smooth only accepts 1 dimension arrays.")
 
-    if window not in ['flat', 'hanning', 'hamming', 'bartlett', 'blackman']:
-        raise ValueError("Window is not of 'flat', 'hanning', 'hamming', 'bartlett', 'blackman'")
+    if window not in ["flat", "hanning", "hamming", "bartlett", "blackman"]:
+        raise ValueError(
+            "Window is not of 'flat', 'hanning', 'hamming', 'bartlett', 'blackman'"
+        )
 
     # interpolate to constant time sample width
-    min_dt = np.min( np.diff(t) )
-    Ts = min_dt/2
-    nt_lin = int( t[-1]/Ts )
-    t_lin = np.linspace(0,t[-1],nt_lin)
-    x_lin = np.interp(t_lin,t,x)
+    min_dt = np.min(np.diff(t))
+    Ts = min_dt / 2
+    nt_lin = int(t[-1] / Ts)
+    t_lin = np.linspace(0, t[-1], nt_lin)
+    x_lin = np.interp(t_lin, t, x)
 
     # window sample length
-    window_len = int( window_delta / Ts )
+    window_len = int(window_delta / Ts)
 
     # padding
-    s=np.r_[x_lin[window_len-1:0:-1],x_lin,x_lin[-1:-window_len:-1]]
+    s = np.r_[x_lin[window_len - 1 : 0 : -1], x_lin, x_lin[-1:-window_len:-1]]
 
     # window template
-    if window == 'flat': #moving average
-        w=np.ones(window_len,'d')
+    if window == "flat":  # moving average
+        w = np.ones(window_len, "d")
     else:
-        w=eval('np.'+window+'(window_len)')
+        w = eval("np." + window + "(window_len)")
 
     # the filter
-    y_lin = np.convolve(w/w.sum(),s,mode='valid')
+    y_lin = np.convolve(w / w.sum(), s, mode="valid")
 
     # remove padding
-    y_lin = y_lin[((window_len-1)/2):-(window_len/2)]
+    y_lin = y_lin[((window_len - 1) / 2) : -(window_len / 2)]
 
     # interpolate back to given t
-    y = np.interp(t,t_lin,y_lin)
+    y = np.interp(t, t_lin, y_lin)
 
     return y
 
+
 #: def window()
 
 
@@ -514,7 +547,5 @@ def window(t,x,window_delta,window='hanning'):
 #  Run Main from Command Line
 # -----------------------------------------------------------------
 
-if __name__ == '__main__':
+if __name__ == "__main__":
     main()
-
-
diff --git a/SU2_PY/SU2/util/lhc_unif.py b/SU2_PY/SU2/util/lhc_unif.py
index 6ede6ff694b..84cadb64543 100644
--- a/SU2_PY/SU2/util/lhc_unif.py
+++ b/SU2_PY/SU2/util/lhc_unif.py
@@ -1,89 +1,91 @@
 import numpy as np
 
-def lhc_unif(XB,NS,XI=None,maxits=10):
-    ''' XS = lhc_unif(XB,NS,XI=None,maxits=10):
-        
-        Latin Hypercube Sampling with uniform density
-        Iterates to maximize minimum L2 distance
-        Accepts an array of points to respect while sampling
-        
-        Inputs:
-            XB          - ndim x 2 array of [lower,upper] bounds
-            NS          - number of new points to sample
-            XI = None   - ni x ndim array of initial points to respect
-            maxits = 10 - maximum number of iterations
-        
-        Outputs:
-            XS - ns x ndim array of sampled points
-    '''
-    
+
+def lhc_unif(XB, NS, XI=None, maxits=10):
+    """XS = lhc_unif(XB,NS,XI=None,maxits=10):
+
+    Latin Hypercube Sampling with uniform density
+    Iterates to maximize minimum L2 distance
+    Accepts an array of points to respect while sampling
+
+    Inputs:
+        XB          - ndim x 2 array of [lower,upper] bounds
+        NS          - number of new points to sample
+        XI = None   - ni x ndim array of initial points to respect
+        maxits = 10 - maximum number of iterations
+
+    Outputs:
+        XS - ns x ndim array of sampled points
+    """
+
     # dimension
     XB = np.atleast_2d(XB)
     ND = XB.shape[0]
-    
+
     # initial points to respect
     if XI is None:
-        XI = np.empty([0,ND])
+        XI = np.empty([0, ND])
     else:
         XI = np.atleast_2d(XI)
-       
+
     # output points
     XO = []
-    
+
     # initialize
-    mindiff = 0;
-    
+    mindiff = 0
+
     # maximize minimum distance
     for it in range(maxits):
-        
+
         # samples
-        S = np.zeros([NS,ND])
-        
+        S = np.zeros([NS, ND])
+
         # populate samples
         for i_d in range(ND):
-            S[:,i_d] = ( np.random.random([1,NS]) + np.random.permutation(NS) ) / NS
-        XS = S*(XB[:,1]-XB[:,0]) + XB[:,0]        
-        
+            S[:, i_d] = (np.random.random([1, NS]) + np.random.permutation(NS)) / NS
+        XS = S * (XB[:, 1] - XB[:, 0]) + XB[:, 0]
+
         # add initial points
-        XX = np.vstack([ XI , XS ])
-        
+        XX = np.vstack([XI, XS])
+
         # calc distances
         vecdiff = vec_dist(XX)[0]
-        
+
         # update
         if vecdiff > mindiff:
             mindiff = vecdiff
             XO = XX
-        
+
     #: for iterate
-    
+
     return XO
 
-def vec_dist(X,P=None):
-    ''' calculates distance between points in matrix X 
-        with each other, or optionally to given point P
-        returns min, max and matrix/vector of distances
-    '''
-    
+
+def vec_dist(X, P=None):
+    """calculates distance between points in matrix X
+    with each other, or optionally to given point P
+    returns min, max and matrix/vector of distances
+    """
+
     # distance matrix among X
     if P is None:
-        
-        nK,nD = X.shape
-        
-        d = np.zeros([nK,nK,nD])
+
+        nK, nD = X.shape
+
+        d = np.zeros([nK, nK, nD])
         for iD in range(nD):
-            d[:,:,iD] = np.array([X[:,iD]])-np.array([X[:,iD]]).T
-        D = np.sqrt( np.sum( d**2 , 2 ) )
-        
-        diag_inf = np.diag( np.ones([nK])*np.inf )
-        dmin = np.min(np.min( D + diag_inf ))
-        dmax = np.max(np.max( D ))
-        
+            d[:, :, iD] = np.array([X[:, iD]]) - np.array([X[:, iD]]).T
+        D = np.sqrt(np.sum(d**2, 2))
+
+        diag_inf = np.diag(np.ones([nK]) * np.inf)
+        dmin = np.min(np.min(D + diag_inf))
+        dmax = np.max(np.max(D))
+
     # distance vector to P
     else:
-        assert P.shape[0] == 1 , 'P must be a horizontal vector'
-        D = np.array([ np.sqrt( np.sum( (X-P)**2 , 1 ) ) ]).T
+        assert P.shape[0] == 1, "P must be a horizontal vector"
+        D = np.array([np.sqrt(np.sum((X - P) ** 2, 1))]).T
         dmin = D.min()
         dmax = D.max()
-        
-    return (dmin,dmax,D)
\ No newline at end of file
+
+    return (dmin, dmax, D)
diff --git a/SU2_PY/SU2/util/misc.py b/SU2_PY/SU2/util/misc.py
index e90e901da33..aa5bbab5b0f 100644
--- a/SU2_PY/SU2/util/misc.py
+++ b/SU2_PY/SU2/util/misc.py
@@ -1,18 +1,17 @@
-
 import numpy as np
 
-def check_array(A,oned_as='row'):
-    ''' ensures A is an array and at least of rank 2
-    '''
-    if not isinstance(A,np.ndarray):
+
+def check_array(A, oned_as="row"):
+    """ensures A is an array and at least of rank 2"""
+    if not isinstance(A, np.ndarray):
         A = np.array(A)
     if np.rank(A) < 2:
         A = np.array(np.matrix(A))
-        if oned_as == 'row':
+        if oned_as == "row":
             pass
-        elif oned_as == 'col':
+        elif oned_as == "col":
             A = A.T
         else:
             raise Exception("oned_as must be 'row' or 'col' ")
-            
-    return A
\ No newline at end of file
+
+    return A
diff --git a/SU2_PY/SU2/util/mp_eval.py b/SU2_PY/SU2/util/mp_eval.py
index b97583d894e..2e9414d6928 100644
--- a/SU2_PY/SU2/util/mp_eval.py
+++ b/SU2_PY/SU2/util/mp_eval.py
@@ -7,123 +7,122 @@
     # In Py3, range corresponds to Py2 xrange
     xrange = range
 
+
 class mp_eval(object):
-    
-    def __init__(self,function,num_procs=None):
-        
+    def __init__(self, function, num_procs=None):
+
         self.__name__ = function.__name__
-        
-        tasks    = mp.JoinableQueue()
-        results  = mp.Queue()
+
+        tasks = mp.JoinableQueue()
+        results = mp.Queue()
         function = TaskMaster(function)
-        
+
         if num_procs is None:
             num_procs = mp.cpu_count()
-            
-        procs = [ QueueMaster( tasks, results, function ) 
-                  for i in xrange(num_procs) ]
-        
-        self.tasks    = tasks
-        self.results  = results
+
+        procs = [QueueMaster(tasks, results, function) for i in xrange(num_procs)]
+
+        self.tasks = tasks
+        self.results = results
         self.function = function
-        self.procs    = procs
-        
+        self.procs = procs
+
         return
-    
-    def __call__(self,inputs):
-        
-        tasks   = self.tasks
+
+    def __call__(self, inputs):
+
+        tasks = self.tasks
         results = self.results
-        
-        if isinstance(inputs,np.ndarray):
+
+        if isinstance(inputs, np.ndarray):
             n_inputs = inputs.shape[0]
-        elif isinstance(inputs,list):
+        elif isinstance(inputs, list):
             n_inputs = len(inputs)
         else:
-            raise Exception('unsupported input')
-        
-        for i_input,this_input in enumerate(inputs):
-            this_job = { 'index'  : i_input    ,
-                         'input'  : this_input ,
-                         'result' : None        }
-            tasks.put( this_job )
-        #end
+            raise Exception("unsupported input")
+
+        for i_input, this_input in enumerate(inputs):
+            this_job = {"index": i_input, "input": this_input, "result": None}
+            tasks.put(this_job)
+        # end
 
         # wait for tasks
-        tasks.join() 
-        
+        tasks.join()
+
         # pull results
-        result_list = [ [] ]*n_inputs
+        result_list = [[]] * n_inputs
         for i in xrange(n_inputs):
             result = results.get()
-            i_result = result['index']
-            result_list[i_result] = result['result']
-        
+            i_result = result["index"]
+            result_list[i_result] = result["result"]
+
         return result_list
 
     def __del__(self):
-        
+
         for proc in self.procs:
             self.tasks.put(None)
-        self.tasks.join()       
-        
+        self.tasks.join()
+
         return
 
-class QueueMaster(mp.Process):
 
-    def __init__(self,task_queue,result_queue,task_class=None):
+class QueueMaster(mp.Process):
+    def __init__(self, task_queue, result_queue, task_class=None):
         mp.Process.__init__(self)
-        self.task_queue   = task_queue
+        self.task_queue = task_queue
         self.result_queue = result_queue
-        self.task_class   = task_class
-        self.daemon       = True
+        self.task_class = task_class
+        self.daemon = True
         self.start()
 
     def run(self):
         proc_name = self.name
         parentPID = os.getppid()
-        
+
         while True:
-            
+
             if os.getppid() != parentPID:
-                break # parent died
+                break  # parent died
 
             this_job = self.task_queue.get()
 
             if this_job is None:
                 self.task_queue.task_done()
-                break # kill signal
-            
-            this_input = this_job['input']
-            this_task  = self.task_class
+                break  # kill signal
+
+            this_input = this_job["input"]
+            this_task = self.task_class
 
             this_data = this_task(*this_input)
-            this_job['result'] = this_data
+            this_job["result"] = this_data
             self.result_queue.put(this_job)
-            
+
             self.task_queue.task_done()
-            
+
         #: while alive
-        
+
         return
 
+
 class TaskMaster(object):
-    
     def __init__(self, func):
-        self.func  = func
-    def __call__(self, *arg, **kwarg):  
+        self.func = func
+
+    def __call__(self, *arg, **kwarg):
         # makes object callable
         result = self.func(*arg, **kwarg)
         return result
+
     def __str__(self):
-        return '%s' % self.func
+        return "%s" % self.func
 
     # pickling
-    #def __getstate__(self):
-        #dict = self.__dict__.copy()
-        #data_dict = cloudpickle.dumps(dict)
-        #return data_dict
-
-    #def __setstate__(self,data_dict):
-        #self.__dict__ = pickle.loads(data_dict)
-        #return    
+    # def __getstate__(self):
+    # dict = self.__dict__.copy()
+    # data_dict = cloudpickle.dumps(dict)
+    # return data_dict
+
+    # def __setstate__(self,data_dict):
+    # self.__dict__ = pickle.loads(data_dict)
+    # return
diff --git a/SU2_PY/SU2/util/ordered_bunch.py b/SU2_PY/SU2/util/ordered_bunch.py
index bc615ffdab0..e763bea6969 100644
--- a/SU2_PY/SU2/util/ordered_bunch.py
+++ b/SU2_PY/SU2/util/ordered_bunch.py
@@ -1,7 +1,7 @@
 #!/usr/bin/env python
 
 """ OrderedBunch is a subclass of OrderedDict with attribute-style access.
-    
+
     >>> b = OrderedBunch()
     >>> b.hello = 'world'
     >>> b.hello
@@ -14,14 +14,14 @@
     True
     >>> b.foo is b['foo']
     True
-    
+
     It is safe to import * from this module:
-    
+
         __all__ = ('OrderedBunch', 'ordered_bunchify','ordered_unbunchify')
-    
+
     ordered_un/bunchify provide dictionary conversion; Bunches can also be
     converted via OrderedBunch.to/fromOrderedDict().
-    
+
     original source:
     https://pypi.python.org/pypi/bunch
 """
@@ -29,101 +29,100 @@
 from .ordered_dict import OrderedDict
 
 ## Compatability Issues...
-#try:
+# try:
 #    from collections import OrderedDict
-#except ImportError:
+# except ImportError:
 #    from ordered_dict import OrderedDict
 
 
 class OrderedBunch(OrderedDict):
-    """ A dictionary that provides attribute-style access.
-        
-        >>> b = OrderedBunch()
-        >>> b.hello = 'world'
-        >>> b.hello
-        'world'
-        >>> b['hello'] += "!"
-        >>> b.hello
-        'world!'
-        >>> b.foo = OrderedBunch(lol=True)
-        >>> b.foo.lol
-        True
-        >>> b.foo is b['foo']
-        True
-        
-        A OrderedBunch is a subclass of dict; it supports all the methods a dict does...
-        
-        >>> b.keys()
-        ['foo', 'hello']
-        
-        Including update()...
-        
-        >>> b.update({ 'ponies': 'are pretty!' }, hello=42)
-        >>> print(repr(b))
-        OrderedBunch(foo=OrderedBunch(lol=True), hello=42, ponies='are pretty!')
-        
-        As well as iteration...
-        
-        >>> [ (k,b[k]) for k in b ]
-        [('ponies', 'are pretty!'), ('foo', OrderedBunch(lol=True)), ('hello', 42)]
-        
-        And "splats".
-        
-        >>> "The {knights} who say {ni}!".format(**OrderedBunch(knights='lolcats', ni='can haz'))
-        'The lolcats who say can haz!'
-        
-        See ordered_unbunchify/OrderedBunch.toOrderedDict, ordered_bunchify/OrderedBunch.fromOrderedDict for notes about conversion.
+    """A dictionary that provides attribute-style access.
+
+    >>> b = OrderedBunch()
+    >>> b.hello = 'world'
+    >>> b.hello
+    'world'
+    >>> b['hello'] += "!"
+    >>> b.hello
+    'world!'
+    >>> b.foo = OrderedBunch(lol=True)
+    >>> b.foo.lol
+    True
+    >>> b.foo is b['foo']
+    True
+
+    A OrderedBunch is a subclass of dict; it supports all the methods a dict does...
+
+    >>> b.keys()
+    ['foo', 'hello']
+
+    Including update()...
+
+    >>> b.update({ 'ponies': 'are pretty!' }, hello=42)
+    >>> print(repr(b))
+    OrderedBunch(foo=OrderedBunch(lol=True), hello=42, ponies='are pretty!')
+
+    As well as iteration...
+
+    >>> [ (k,b[k]) for k in b ]
+    [('ponies', 'are pretty!'), ('foo', OrderedBunch(lol=True)), ('hello', 42)]
+
+    And "splats".
+
+    >>> "The {knights} who say {ni}!".format(**OrderedBunch(knights='lolcats', ni='can haz'))
+    'The lolcats who say can haz!'
+
+    See ordered_unbunchify/OrderedBunch.toOrderedDict, ordered_bunchify/OrderedBunch.fromOrderedDict for notes about conversion.
     """
-    
+
     _initialized = False
-    
-    def __init__(self,*args,**kwarg):
-        """ initializes the ordered dict
-        """
-        super(OrderedBunch,self).__init__(*args,**kwarg)
+
+    def __init__(self, *args, **kwarg):
+        """initializes the ordered dict"""
+        super(OrderedBunch, self).__init__(*args, **kwarg)
         self._initialized = True
-    
+
     def __contains__(self, k):
-        """ >>> b = OrderedBunch(ponies='are pretty!')
-            >>> 'ponies' in b
-            True
-            >>> 'foo' in b
-            False
-            >>> b['foo'] = 42
-            >>> 'foo' in b
-            True
-            >>> b.hello = 'hai'
-            >>> 'hello' in b
-            True
+        """>>> b = OrderedBunch(ponies='are pretty!')
+        >>> 'ponies' in b
+        True
+        >>> 'foo' in b
+        False
+        >>> b['foo'] = 42
+        >>> 'foo' in b
+        True
+        >>> b.hello = 'hai'
+        >>> 'hello' in b
+        True
         """
         try:
             return hasattr(self, k) or dict.__contains__(self, k)
         except:
             return False
-    
-    # only called if k not found in normal places 
+
+    # only called if k not found in normal places
     def __getattr__(self, k):
-        """ Gets key if it exists, otherwise throws AttributeError.
-            
-            nb. __getattr__ is only called if key is not found in normal places.
-            
-            >>> b = OrderedBunch(bar='baz', lol={})
-            >>> b.foo
-            Traceback (most recent call last):
-                ...
-            AttributeError: foo
-            
-            >>> b.bar
-            'baz'
-            >>> getattr(b, 'bar')
-            'baz'
-            >>> b['bar']
-            'baz'
-            
-            >>> b.lol is b['lol']
-            True
-            >>> b.lol is getattr(b, 'lol')
-            True
+        """Gets key if it exists, otherwise throws AttributeError.
+
+        nb. __getattr__ is only called if key is not found in normal places.
+
+        >>> b = OrderedBunch(bar='baz', lol={})
+        >>> b.foo
+        Traceback (most recent call last):
+            ...
+        AttributeError: foo
+
+        >>> b.bar
+        'baz'
+        >>> getattr(b, 'bar')
+        'baz'
+        >>> b['bar']
+        'baz'
+
+        >>> b.lol is b['lol']
+        True
+        >>> b.lol is getattr(b, 'lol')
+        True
         """
         try:
             # Throws exception if not in prototype chain
@@ -133,28 +132,28 @@ def __getattr__(self, k):
                 return self[k]
             except KeyError:
                 raise AttributeError(k)
-    
+
     def __setattr__(self, k, v):
-        """ Sets attribute k if it exists, otherwise sets key k. A KeyError
-            raised by set-item (only likely if you subclass OrderedBunch) will 
-            propagate as an AttributeError instead.
-            
-            >>> b = OrderedBunch(foo='bar', this_is='useful when subclassing')
-            >>> b.values                            #doctest: +ELLIPSIS
-            <built-in method values of OrderedBunch object at 0x...>
-            >>> b.values = 'uh oh'
-            >>> b.values
-            'uh oh'
-            >>> b['values']
-            Traceback (most recent call last):
-                ...
-            KeyError: 'values'
+        """Sets attribute k if it exists, otherwise sets key k. A KeyError
+        raised by set-item (only likely if you subclass OrderedBunch) will
+        propagate as an AttributeError instead.
+
+        >>> b = OrderedBunch(foo='bar', this_is='useful when subclassing')
+        >>> b.values                            #doctest: +ELLIPSIS
+        <built-in method values of OrderedBunch object at 0x...>
+        >>> b.values = 'uh oh'
+        >>> b.values
+        'uh oh'
+        >>> b['values']
+        Traceback (most recent call last):
+            ...
+        KeyError: 'values'
         """
-        
+
         if not self._initialized:
             # for OrderedDict initialization
             return object.__setattr__(self, k, v)
-        
+
         try:
             # Throws exception if not in prototype chain
             object.__getattribute__(self, k)
@@ -165,22 +164,22 @@ def __setattr__(self, k, v):
                 raise AttributeError(k)
         else:
             object.__setattr__(self, k, v)
-    
+
     def __delattr__(self, k):
-        """ Deletes attribute k if it exists, otherwise deletes key k. A KeyError
-            raised by deleting the key--such as when the key is missing--will
-            propagate as an AttributeError instead.
-            
-            >>> b = OrderedBunch(lol=42)
-            >>> del b.values
-            Traceback (most recent call last):
-                ...
-            AttributeError: 'OrderedBunch' object attribute 'values' is read-only
-            >>> del b.lol
-            >>> b.lol
-            Traceback (most recent call last):
-                ...
-            AttributeError: lol
+        """Deletes attribute k if it exists, otherwise deletes key k. A KeyError
+        raised by deleting the key--such as when the key is missing--will
+        propagate as an AttributeError instead.
+
+        >>> b = OrderedBunch(lol=42)
+        >>> del b.values
+        Traceback (most recent call last):
+            ...
+        AttributeError: 'OrderedBunch' object attribute 'values' is read-only
+        >>> del b.lol
+        >>> b.lol
+        Traceback (most recent call last):
+            ...
+        AttributeError: lol
         """
         try:
             # Throws exception if not in prototype chain
@@ -192,54 +191,52 @@ def __delattr__(self, k):
                 raise AttributeError(k)
         else:
             object.__delattr__(self, k)
-    
+
     def toOrderedDict(self):
-        """ Recursively converts a bunch back into a dictionary.
-            
-            >>> b = OrderedBunch(OrderedBunchunch(lol=True), hello=42, ponies='are pretty!')
-            >>> b.toOrderedDict()
-            {'ponies': 'are pretty!', 'foo': {'lol': True}, 'hello': 42}
-            
-            See ordered_unbunchify for more info.
+        """Recursively converts a bunch back into a dictionary.
+
+        >>> b = OrderedBunch(OrderedBunchunch(lol=True), hello=42, ponies='are pretty!')
+        >>> b.toOrderedDict()
+        {'ponies': 'are pretty!', 'foo': {'lol': True}, 'hello': 42}
+
+        See ordered_unbunchify for more info.
         """
         return ordered_unbunchify(self)
-    
+
     def __repr__(self):
-        """ Invertible* string-form of a OrderedBunch.
-            
-            >>> b = OrderedBunch(foo=OrderedBunch(lol=True), hello=42, ponies='are pretty!')
-            >>> print(repr(b))
-            OrderedBunch(foo=OrderedBunch(lol=True), hello=42, ponies='are pretty!')
-            >>> eval(repr(b))
-            OrderedBunch(foo=OrderedBunch(lol=True), hello=42, ponies='are pretty!')
-            
-            (*) Invertible so long as collection contents are each repr-invertible.
+        """Invertible* string-form of a OrderedBunch.
+
+        >>> b = OrderedBunch(foo=OrderedBunch(lol=True), hello=42, ponies='are pretty!')
+        >>> print(repr(b))
+        OrderedBunch(foo=OrderedBunch(lol=True), hello=42, ponies='are pretty!')
+        >>> eval(repr(b))
+        OrderedBunch(foo=OrderedBunch(lol=True), hello=42, ponies='are pretty!')
+
+        (*) Invertible so long as collection contents are each repr-invertible.
         """
         keys = self.keys()
-        args = ', '.join(['%s=%r' % (key, self[key]) for key in keys])
-        return '%s(%s)' % (self.__class__.__name__, args)
-    
+        args = ", ".join(["%s=%r" % (key, self[key]) for key in keys])
+        return "%s(%s)" % (self.__class__.__name__, args)
+
     def __str__(self):
-        """ String-form of a Bunch.
-        """
+        """String-form of a Bunch."""
         keys = self.keys()
-        args = ', '.join(['%s=%r' % (key, self[key]) for key in keys])
-        return '{%s}' % args    
-    
+        args = ", ".join(["%s=%r" % (key, self[key]) for key in keys])
+        return "{%s}" % args
+
     @staticmethod
     def fromOrderedDict(d):
-        """ Recursively transforms a dictionary into a OrderedBunch via copy.
-            
-            >>> b = OrderedBunch.fromOrderedDict({'urmom': {'sez': {'what': 'what'}}})
-            >>> b.urmom.sez.what
-            'what'
-            
-            See ordered_bunchify for more info.
+        """Recursively transforms a dictionary into a OrderedBunch via copy.
+
+        >>> b = OrderedBunch.fromOrderedDict({'urmom': {'sez': {'what': 'what'}}})
+        >>> b.urmom.sez.what
+        'what'
+
+        See ordered_bunchify for more info.
         """
         return ordered_bunchify(d)
 
 
-
 # While we could convert abstract types like Mapping or Iterable, I think
 # ordered_bunchify is more likely to "do what you mean" if it is conservative about
 # casting (ex: isinstance(str,Iterable) == True ).
@@ -247,56 +244,58 @@ def fromOrderedDict(d):
 # Should you disagree, it is not difficult to duplicate this function with
 # more aggressive coercion to suit your own purposes.
 
+
 def ordered_bunchify(x):
-    """ Recursively transforms a dictionary into a OrderedBunch via copy.
-        
-        >>> b = ordered_bunchify({'urmom': {'sez': {'what': 'what'}}})
-        >>> b.urmom.sez.what
-        'what'
-        
-        ordered_bunchify can handle intermediary dicts, lists and tuples (as well as 
-        their subclasses), but ymmv on custom datatypes.
-        
-        >>> b = ordered_bunchify({ 'lol': ('cats', {'hah':'i win again'}), 
-        ...         'hello': [{'french':'salut', 'german':'hallo'}] })
-        >>> b.hello[0].french
-        'salut'
-        >>> b.lol[1].hah
-        'i win again'
-        
-        nb. As dicts are not hashable, they cannot be nested in sets/frozensets.
+    """Recursively transforms a dictionary into a OrderedBunch via copy.
+
+    >>> b = ordered_bunchify({'urmom': {'sez': {'what': 'what'}}})
+    >>> b.urmom.sez.what
+    'what'
+
+    ordered_bunchify can handle intermediary dicts, lists and tuples (as well as
+    their subclasses), but ymmv on custom datatypes.
+
+    >>> b = ordered_bunchify({ 'lol': ('cats', {'hah':'i win again'}),
+    ...         'hello': [{'french':'salut', 'german':'hallo'}] })
+    >>> b.hello[0].french
+    'salut'
+    >>> b.lol[1].hah
+    'i win again'
+
+    nb. As dicts are not hashable, they cannot be nested in sets/frozensets.
     """
     if isinstance(x, dict):
-        return OrderedBunch( (k, ordered_bunchify(v)) for k,v in x.iteritems() )
+        return OrderedBunch((k, ordered_bunchify(v)) for k, v in x.iteritems())
     elif isinstance(x, (list, tuple)):
-        return type(x)( ordered_bunchify(v) for v in x )
+        return type(x)(ordered_bunchify(v) for v in x)
     else:
         return x
 
+
 def ordered_unbunchify(x):
-    """ Recursively converts a OrderedBunch into a dictionary.
-        
-        >>> b = OrderedBunch(foo=OrderedBunch(lol=True), hello=42, ponies='are pretty!')
-        >>> ordered_unbunchify(b)
-        {'ponies': 'are pretty!', 'foo': {'lol': True}, 'hello': 42}
-        
-        ordered_unbunchify will handle intermediary dicts, lists and tuples (as well as
-        their subclasses), but ymmv on custom datatypes.
-        
-        >>> b = OrderedBunch(foo=['bar', OrderedBunch(lol=True)], hello=42, 
-        ...         ponies=('are pretty!', OrderedBunch(lies='are trouble!')))
-        >>> ordered_unbunchify(b) #doctest: +NORMALIZE_WHITESPACE
-        {'ponies': ('are pretty!', {'lies': 'are trouble!'}), 
-         'foo': ['bar', {'lol': True}], 'hello': 42}
-        
-        nb. As dicts are not hashable, they cannot be nested in sets/frozensets.
+    """Recursively converts a OrderedBunch into a dictionary.
+
+    >>> b = OrderedBunch(foo=OrderedBunch(lol=True), hello=42, ponies='are pretty!')
+    >>> ordered_unbunchify(b)
+    {'ponies': 'are pretty!', 'foo': {'lol': True}, 'hello': 42}
+
+    ordered_unbunchify will handle intermediary dicts, lists and tuples (as well as
+    their subclasses), but ymmv on custom datatypes.
+
+    >>> b = OrderedBunch(foo=['bar', OrderedBunch(lol=True)], hello=42,
+    ...         ponies=('are pretty!', OrderedBunch(lies='are trouble!')))
+    >>> ordered_unbunchify(b) #doctest: +NORMALIZE_WHITESPACE
+    {'ponies': ('are pretty!', {'lies': 'are trouble!'}),
+     'foo': ['bar', {'lol': True}], 'hello': 42}
+
+    nb. As dicts are not hashable, they cannot be nested in sets/frozensets.
     """
     if isinstance(x, OrderedDict):
-        return OrderedDict( (k, ordered_unbunchify(v)) for k,v in x.iteritems() )    
+        return OrderedDict((k, ordered_unbunchify(v)) for k, v in x.iteritems())
     elif isinstance(x, dict):
-        return dict( (k, ordered_unbunchify(v)) for k,v in x.iteritems() )
+        return dict((k, ordered_unbunchify(v)) for k, v in x.iteritems())
     elif isinstance(x, (list, tuple)):
-        return type(x)( ordered_unbunchify(v) for v in x )
+        return type(x)(ordered_unbunchify(v) for v in x)
     else:
         return x
 
@@ -308,115 +307,110 @@ def ordered_unbunchify(x):
         import json
     except ImportError:
         import simplejson as json
-    
+
     def toJSON(self, **options):
-        """ Serializes this OrderedBunch to JSON. Accepts the same keyword options as `json.dumps()`.
-            
-            >>> b = OrderedBunch(foo=OrderedBunch(lol=True), hello=42, ponies='are pretty!')
-            >>> json.dumps(b)
-            '{"ponies": "are pretty!", "foo": {"lol": true}, "hello": 42}'
-            >>> b.toJSON()
-            '{"ponies": "are pretty!", "foo": {"lol": true}, "hello": 42}'
+        """Serializes this OrderedBunch to JSON. Accepts the same keyword options as `json.dumps()`.
+
+        >>> b = OrderedBunch(foo=OrderedBunch(lol=True), hello=42, ponies='are pretty!')
+        >>> json.dumps(b)
+        '{"ponies": "are pretty!", "foo": {"lol": true}, "hello": 42}'
+        >>> b.toJSON()
+        '{"ponies": "are pretty!", "foo": {"lol": true}, "hello": 42}'
         """
         return json.dumps(self, **options)
-    
+
     OrderedBunch.toJSON = toJSON
-    
+
 except ImportError:
     pass
 
 
-
-
 try:
     # Attempt to register ourself with PyYAML as a representer
     import yaml
     from yaml.representer import Representer, SafeRepresenter
-    
+
     def from_yaml(loader, node):
-        """ PyYAML support for Bunches using the tag `!bunch` and `!bunch.OrderedBunch`.
-            
-            >>> import yaml
-            >>> yaml.load('''
-            ... Flow style: !bunch.OrderedBunch { Clark: Evans, Brian: Ingerson, Oren: Ben-Kiki }
-            ... Block style: !bunch
-            ...   Clark : Evans
-            ...   Brian : Ingerson
-            ...   Oren  : Ben-Kiki
-            ... ''') #doctest: +NORMALIZE_WHITESPACE
-            {'Flow style': OrderedBunch(Brian='Ingerson', Clark='Evans', Oren='Ben-Kiki'), 
-             'Block style': OrderedBunch(Brian='Ingerson', Clark='Evans', Oren='Ben-Kiki')}
-            
-            This module registers itself automatically to cover both OrderedBunch and any 
-            subclasses. Should you want to customize the representation of a subclass,
-            simply register it with PyYAML yourself.
+        """PyYAML support for Bunches using the tag `!bunch` and `!bunch.OrderedBunch`.
+
+        >>> import yaml
+        >>> yaml.load('''
+        ... Flow style: !bunch.OrderedBunch { Clark: Evans, Brian: Ingerson, Oren: Ben-Kiki }
+        ... Block style: !bunch
+        ...   Clark : Evans
+        ...   Brian : Ingerson
+        ...   Oren  : Ben-Kiki
+        ... ''') #doctest: +NORMALIZE_WHITESPACE
+        {'Flow style': OrderedBunch(Brian='Ingerson', Clark='Evans', Oren='Ben-Kiki'),
+         'Block style': OrderedBunch(Brian='Ingerson', Clark='Evans', Oren='Ben-Kiki')}
+
+        This module registers itself automatically to cover both OrderedBunch and any
+        subclasses. Should you want to customize the representation of a subclass,
+        simply register it with PyYAML yourself.
         """
         data = OrderedBunch()
         yield data
         value = loader.construct_mapping(node)
         data.update(value)
-    
-    
+
     def to_yaml_safe(dumper, data):
-        """ Converts OrderedBunch to a normal mapping node, making it appear as a
-            dict in the YAML output.
-            
-            >>> b = OrderedBunch(foo=['bar', OrderedBunch(lol=True)], hello=42)
-            >>> import yaml
-            >>> yaml.safe_dump(b, default_flow_style=True)
-            '{foo: [bar, {lol: true}], hello: 42}\\n'
+        """Converts OrderedBunch to a normal mapping node, making it appear as a
+        dict in the YAML output.
+
+        >>> b = OrderedBunch(foo=['bar', OrderedBunch(lol=True)], hello=42)
+        >>> import yaml
+        >>> yaml.safe_dump(b, default_flow_style=True)
+        '{foo: [bar, {lol: true}], hello: 42}\\n'
         """
         return dumper.represent_dict(data)
-    
+
     def to_yaml(dumper, data):
-        """ Converts OrderedBunch to a representation node.
-            
-            >>> b = OrderedBunch(foo=['bar', OrderedBunch(lol=True)], hello=42)
-            >>> import yaml
-            >>> yaml.dump(b, default_flow_style=True)
-            '!bunch.OrderedBunch {foo: [bar, !bunch.OrderedBunch {lol: true}], hello: 42}\\n'
+        """Converts OrderedBunch to a representation node.
+
+        >>> b = OrderedBunch(foo=['bar', OrderedBunch(lol=True)], hello=42)
+        >>> import yaml
+        >>> yaml.dump(b, default_flow_style=True)
+        '!bunch.OrderedBunch {foo: [bar, !bunch.OrderedBunch {lol: true}], hello: 42}\\n'
         """
-        return dumper.represent_mapping(u'!orderedbunch.OrderedBunch', data)
-    
-    
-    yaml.add_constructor(u'!orderedbunch', from_yaml)
-    yaml.add_constructor(u'!orderedbunch.OrderedBunch', from_yaml)
-    
+        return dumper.represent_mapping("!orderedbunch.OrderedBunch", data)
+
+    yaml.add_constructor("!orderedbunch", from_yaml)
+    yaml.add_constructor("!orderedbunch.OrderedBunch", from_yaml)
+
     SafeRepresenter.add_representer(OrderedBunch, to_yaml_safe)
     SafeRepresenter.add_multi_representer(OrderedBunch, to_yaml_safe)
-    
+
     Representer.add_representer(OrderedBunch, to_yaml)
     Representer.add_multi_representer(OrderedBunch, to_yaml)
-    
-    
+
     # Instance methods for YAML conversion
     def toYAML(self, **options):
-        """ Serializes this OrderedBunch to YAML, using `yaml.safe_dump()` if 
-            no `Dumper` is provided. See the PyYAML documentation for more info.
-            
-            >>> b = OrderedBunch(foo=['bar', OrderedBunch(lol=True)], hello=42)
-            >>> import yaml
-            >>> yaml.safe_dump(b, default_flow_style=True)
-            '{foo: [bar, {lol: true}], hello: 42}\\n'
-            >>> b.toYAML(default_flow_style=True)
-            '{foo: [bar, {lol: true}], hello: 42}\\n'
-            >>> yaml.dump(b, default_flow_style=True)
-            '!bunch.OrderedBunch {foo: [bar, !bunch.OrderedBunch {lol: true}], hello: 42}\\n'
-            >>> b.toYAML(Dumper=yaml.Dumper, default_flow_style=True)
-            '!bunch.OrderedBunch {foo: [bar, !bunch.OrderedBunch {lol: true}], hello: 42}\\n'
+        """Serializes this OrderedBunch to YAML, using `yaml.safe_dump()` if
+        no `Dumper` is provided. See the PyYAML documentation for more info.
+
+        >>> b = OrderedBunch(foo=['bar', OrderedBunch(lol=True)], hello=42)
+        >>> import yaml
+        >>> yaml.safe_dump(b, default_flow_style=True)
+        '{foo: [bar, {lol: true}], hello: 42}\\n'
+        >>> b.toYAML(default_flow_style=True)
+        '{foo: [bar, {lol: true}], hello: 42}\\n'
+        >>> yaml.dump(b, default_flow_style=True)
+        '!bunch.OrderedBunch {foo: [bar, !bunch.OrderedBunch {lol: true}], hello: 42}\\n'
+        >>> b.toYAML(Dumper=yaml.Dumper, default_flow_style=True)
+        '!bunch.OrderedBunch {foo: [bar, !bunch.OrderedBunch {lol: true}], hello: 42}\\n'
         """
         opts = dict(indent=4, default_flow_style=False)
         opts.update(options)
-        if 'Dumper' not in opts:
+        if "Dumper" not in opts:
             return yaml.safe_dump(self, **opts)
         else:
             return yaml.dump(self, **opts)
-    
+
     def fromYAML(*args, **kwargs):
-        return ordered_bunchify( yaml.load(*args, **kwargs) )
-    
+        return ordered_bunchify(yaml.load(*args, **kwargs))
+
     OrderedBunch.toYAML = OrderedBunch.__repr__ = toYAML
     OrderedBunch.fromYAML = staticmethod(fromYAML)
-    
+
 except ImportError:
     pass
diff --git a/SU2_PY/SU2/util/ordered_dict.py b/SU2_PY/SU2/util/ordered_dict.py
index 0813b65a13a..c2d244f4b50 100644
--- a/SU2_PY/SU2/util/ordered_dict.py
+++ b/SU2_PY/SU2/util/ordered_dict.py
@@ -1,4 +1,3 @@
-
 """ Backport of OrderedDict() class that runs on Python 2.4, 2.5, 2.6, 2.7 and pypy.
     Passes Python2.7's test suite and incorporates all the latest updates.
     {{{ http://code.activestate.com/recipes/576693/ (r9)
@@ -21,6 +20,7 @@
 
 class OrderedDict(dict):
     """Dictionary that remembers insertion order"""
+
     # An inherited dict maps keys to values.
     # The inherited dict provides __getitem__, __len__, __contains__, and get.
     # The remaining methods are order-aware.
@@ -32,23 +32,23 @@ class OrderedDict(dict):
     # Each link is stored as a list of length three:  [PREV, NEXT, KEY].
 
     def __init__(self, *args, **kwds):
-        '''Initialize an ordered dictionary.  Signature is the same as for
+        """Initialize an ordered dictionary.  Signature is the same as for
         regular dictionaries, but keyword arguments are not recommended
         because their insertion order is arbitrary.
 
-        '''
+        """
         if len(args) > 1:
-            raise TypeError('expected at most 1 arguments, got %d' % len(args))
+            raise TypeError("expected at most 1 arguments, got %d" % len(args))
         try:
             self.__root
         except AttributeError:
-            self.__root = root = []                     # sentinel node
+            self.__root = root = []  # sentinel node
             root[:] = [root, root, None]
             self.__map = {}
         self.__update(*args, **kwds)
 
     def __setitem__(self, key, value, dict_setitem=dict.__setitem__):
-        'od.__setitem__(i, y) <==> od[i]=y'
+        "od.__setitem__(i, y) <==> od[i]=y"
         # Setting a new item creates a new link which goes at the end of the linked
         # list, and the inherited dictionary is updated with the new key/value pair.
         if key not in self:
@@ -58,7 +58,7 @@ def __setitem__(self, key, value, dict_setitem=dict.__setitem__):
         dict_setitem(self, key, value)
 
     def __delitem__(self, key, dict_delitem=dict.__delitem__):
-        'od.__delitem__(y) <==> del od[y]'
+        "od.__delitem__(y) <==> del od[y]"
         # Deleting an existing item uses self.__map to find the link which is
         # then removed by updating the links in the predecessor and successor nodes.
         dict_delitem(self, key)
@@ -67,7 +67,7 @@ def __delitem__(self, key, dict_delitem=dict.__delitem__):
         link_next[0] = link_prev
 
     def __iter__(self):
-        'od.__iter__() <==> iter(od)'
+        "od.__iter__() <==> iter(od)"
         root = self.__root
         curr = root[1]
         while curr is not root:
@@ -75,7 +75,7 @@ def __iter__(self):
             curr = curr[1]
 
     def __reversed__(self):
-        'od.__reversed__() <==> reversed(od)'
+        "od.__reversed__() <==> reversed(od)"
         root = self.__root
         curr = root[0]
         while curr is not root:
@@ -83,7 +83,7 @@ def __reversed__(self):
             curr = curr[0]
 
     def clear(self):
-        'od.clear() -> None.  Remove all items from od.'
+        "od.clear() -> None.  Remove all items from od."
         try:
             for node in self.__map.itervalues():
                 del node[:]
@@ -95,12 +95,12 @@ def clear(self):
         dict.clear(self)
 
     def popitem(self, last=True):
-        '''od.popitem() -> (k, v), return and remove a (key, value) pair.
+        """od.popitem() -> (k, v), return and remove a (key, value) pair.
         Pairs are returned in LIFO order if last is true or FIFO order if false.
 
-        '''
+        """
         if not self:
-            raise KeyError('dictionary is empty')
+            raise KeyError("dictionary is empty")
         root = self.__root
         if last:
             link = root[0]
@@ -120,45 +120,47 @@ def popitem(self, last=True):
     # -- the following methods do not depend on the internal structure --
 
     def keys(self):
-        'od.keys() -> list of keys in od'
+        "od.keys() -> list of keys in od"
         return list(self)
 
     def values(self):
-        'od.values() -> list of values in od'
+        "od.values() -> list of values in od"
         return [self[key] for key in self]
 
     def items(self):
-        'od.items() -> list of (key, value) pairs in od'
+        "od.items() -> list of (key, value) pairs in od"
         return [(key, self[key]) for key in self]
 
     def iterkeys(self):
-        'od.iterkeys() -> an iterator over the keys in od'
+        "od.iterkeys() -> an iterator over the keys in od"
         return iter(self)
 
     def itervalues(self):
-        'od.itervalues -> an iterator over the values in od'
+        "od.itervalues -> an iterator over the values in od"
         for k in self:
             yield self[k]
 
     def iteritems(self):
-        'od.iteritems -> an iterator over the (key, value) items in od'
+        "od.iteritems -> an iterator over the (key, value) items in od"
         for k in self:
             yield (k, self[k])
 
     def update(*args, **kwds):
-        '''od.update(E, **F) -> None.  Update od from dict/iterable E and F.
+        """od.update(E, **F) -> None.  Update od from dict/iterable E and F.
 
         If E is a dict instance, does:           for k in E: od[k] = E[k]
         If E has a .keys() method, does:         for k in E.keys(): od[k] = E[k]
         Or if E is an iterable of items, does:   for k, v in E: od[k] = v
         In either case, this is followed by:     for k, v in F.items(): od[k] = v
 
-        '''
+        """
         if len(args) > 2:
-            raise TypeError('update() takes at most 2 positional '
-                            'arguments (%d given)' % (len(args),))
+            raise TypeError(
+                "update() takes at most 2 positional "
+                "arguments (%d given)" % (len(args),)
+            )
         elif not args:
-            raise TypeError('update() takes at least 1 argument (0 given)')
+            raise TypeError("update() takes at least 1 argument (0 given)")
         self = args[0]
         # Make progressively weaker assumptions about "other"
         other = ()
@@ -167,7 +169,7 @@ def update(*args, **kwds):
         if isinstance(other, dict):
             for key in other:
                 self[key] = other[key]
-        elif hasattr(other, 'keys'):
+        elif hasattr(other, "keys"):
             for key in other.keys():
                 self[key] = other[key]
         else:
@@ -181,10 +183,10 @@ def update(*args, **kwds):
     __marker = object()
 
     def pop(self, key, default=__marker):
-        '''od.pop(k[,d]) -> v, remove specified key and return the corresponding value.
+        """od.pop(k[,d]) -> v, remove specified key and return the corresponding value.
         If key is not found, d is returned if given, otherwise KeyError is raised.
 
-        '''
+        """
         if key in self:
             result = self[key]
             del self[key]
@@ -194,27 +196,27 @@ def pop(self, key, default=__marker):
         return default
 
     def setdefault(self, key, default=None):
-        'od.setdefault(k[,d]) -> od.get(k,d), also set od[k]=d if k not in od'
+        "od.setdefault(k[,d]) -> od.get(k,d), also set od[k]=d if k not in od"
         if key in self:
             return self[key]
         self[key] = default
         return default
 
     def __repr__(self, _repr_running={}):
-        'od.__repr__() <==> repr(od)'
+        "od.__repr__() <==> repr(od)"
         call_key = id(self), _get_ident()
         if call_key in _repr_running:
-            return '...'
+            return "..."
         _repr_running[call_key] = 1
         try:
             if not self:
-                return '%s()' % (self.__class__.__name__,)
-            return '%s(%r)' % (self.__class__.__name__, self.items())
+                return "%s()" % (self.__class__.__name__,)
+            return "%s(%r)" % (self.__class__.__name__, self.items())
         finally:
             del _repr_running[call_key]
 
     def __reduce__(self):
-        'Return state information for pickling'
+        "Return state information for pickling"
         items = [[k, self[k]] for k in self]
         inst_dict = vars(self).copy()
         for k in vars(OrderedDict()):
@@ -224,27 +226,27 @@ def __reduce__(self):
         return self.__class__, (items,)
 
     def copy(self):
-        'od.copy() -> a shallow copy of od'
+        "od.copy() -> a shallow copy of od"
         return self.__class__(self)
 
     @classmethod
     def fromkeys(cls, iterable, value=None):
-        '''OD.fromkeys(S[, v]) -> New ordered dictionary with keys from S
+        """OD.fromkeys(S[, v]) -> New ordered dictionary with keys from S
         and values equal to v (which defaults to None).
 
-        '''
+        """
         d = cls()
         for key in iterable:
             d[key] = value
         return d
 
     def __eq__(self, other):
-        '''od.__eq__(y) <==> od==y.  Comparison to another OD is order-sensitive
+        """od.__eq__(y) <==> od==y.  Comparison to another OD is order-sensitive
         while comparison to a regular mapping is order-insensitive.
 
-        '''
+        """
         if isinstance(other, OrderedDict):
-            return len(self)==len(other) and self.items() == other.items()
+            return len(self) == len(other) and self.items() == other.items()
         return dict.__eq__(self, other)
 
     def __ne__(self, other):
@@ -263,4 +265,6 @@ def viewvalues(self):
     def viewitems(self):
         "od.viewitems() -> a set-like object providing a view on od's items"
         return ItemsView(self)
+
+
 ## end of http://code.activestate.com/recipes/576693/ }}}
diff --git a/SU2_PY/SU2/util/plot.py b/SU2_PY/SU2/util/plot.py
index d07a510f37d..1591c7849e1 100644
--- a/SU2_PY/SU2/util/plot.py
+++ b/SU2_PY/SU2/util/plot.py
@@ -26,67 +26,71 @@
 # License along with SU2. If not, see <http://www.gnu.org/licenses/>.
 
 
-def write_plot(filename,plot_format,data_plot,keys_plot=None):
-    """ write_plot(filename,plot_format,data_plot,keys_plot=[])
-        writes a tecplot or paraview plot of dictionary data
-        data_plot is a dictionary of lists with equal length
-        if data_plot is an ordered dictionary, will output in order
-        otherwise use keys_plot to specify the order of output
+def write_plot(filename, plot_format, data_plot, keys_plot=None):
+    """write_plot(filename,plot_format,data_plot,keys_plot=[])
+    writes a tecplot or paraview plot of dictionary data
+    data_plot is a dictionary of lists with equal length
+    if data_plot is an ordered dictionary, will output in order
+    otherwise use keys_plot to specify the order of output
     """
 
     default_spacing = 16
-    indent_spacing  = 0
+    indent_spacing = 0
 
-    if keys_plot is None: keys_plot = []
+    if keys_plot is None:
+        keys_plot = []
 
     if not keys_plot:
         keys_plot = data_plot.keys()
 
-    keys_print  = [ '"'+key+'"' for key in keys_plot ]
+    keys_print = ['"' + key + '"' for key in keys_plot]
     keys_space = [default_spacing] * len(keys_plot)
 
-    header = ''
-    if (plot_format == 'TECPLOT'):
-        header = 'VARIABLES='
+    header = ""
+    if plot_format == "TECPLOT":
+        header = "VARIABLES="
         indent_spacing += 10
-    indent_spacing = ' '*indent_spacing
+    indent_spacing = " " * indent_spacing
 
     n_lines = 0
-    for i,key in enumerate(keys_plot):
+    for i, key in enumerate(keys_plot):
         # check vector lengths
         value = data_plot[key]
         if i == 0:
             n_lines = len(value)
         else:
-            assert n_lines == len(value) , 'unequal plot vector lengths'
+            assert n_lines == len(value), "unequal plot vector lengths"
 
         # check spacing
         if len(key) > keys_space[i]:
             keys_space[i] = len(key)
         keys_space[i] = "%-" + str(keys_space[i]) + "s"
 
-    plotfile = open(filename,'w')
+    plotfile = open(filename, "w")
     plotfile.write(header)
-    for i,key in enumerate(keys_print):
-        if i > 0: plotfile.write(", ")
+    for i, key in enumerate(keys_print):
+        if i > 0:
+            plotfile.write(", ")
         plotfile.write(keys_space[i] % key)
-    plotfile.write('\n')
+    plotfile.write("\n")
 
     for i_line in range(n_lines):
         plotfile.write(indent_spacing)
-        for j,key in enumerate(keys_plot):
+        for j, key in enumerate(keys_plot):
             value = data_plot[key]
-            if j > 0: plotfile.write(", ")
+            if j > 0:
+                plotfile.write(", ")
             plotfile.write(keys_space[j] % value[i_line])
-        plotfile.write('\n')
+        plotfile.write("\n")
 
     plotfile.close()
 
     return
 
-def tecplot(filename,data_plot,keys_plot=[]):
-    write_plot(filename,'TECPLOT',data_plot,keys_plot)
 
-def paraview(filename,data_plot,keys_plot=[]):
-    write_plot(filename,'CSV',data_plot,keys_plot)
+def tecplot(filename, data_plot, keys_plot=[]):
+    write_plot(filename, "TECPLOT", data_plot, keys_plot)
 
+
+def paraview(filename, data_plot, keys_plot=[]):
+    write_plot(filename, "CSV", data_plot, keys_plot)
diff --git a/SU2_PY/SU2/util/polarSweepLib.py b/SU2_PY/SU2/util/polarSweepLib.py
index 7d79f1b3dde..f242769a43a 100755
--- a/SU2_PY/SU2/util/polarSweepLib.py
+++ b/SU2_PY/SU2/util/polarSweepLib.py
@@ -1,4 +1,3 @@
-
 # \file polarSweepLib.py
 #  \brief Functions library for compute_polar.py script.
 #  \author E Arad
@@ -28,979 +27,1188 @@
 from numpy import *
 
 
-def parLocator(keyWord,b,n,iDoNot,verbose):
+def parLocator(keyWord, b, n, iDoNot, verbose):
 
-#---- -- locate the relevant line in base input file
-# --- do not select line iDoNot (unless it is -1)
-#
-    keyWord=keyWord.lower()
-    iFocus=-1
+    # ---- -- locate the relevant line in base input file
+    # --- do not select line iDoNot (unless it is -1)
+    #
+    keyWord = keyWord.lower()
+    iFocus = -1
     icol = -1
     for i in range(1, n):
 
-        lineString=str(b[i]).lower()
-# check if : exist in line
+        lineString = str(b[i]).lower()
+        # check if : exist in line
         try:
-            icol=lineString.index(':')
+            icol = lineString.index(":")
         except ValueError:
-             pass   # do nothing
-        if icol > -1 :
-# verify that this line was not commented out
+            pass  # do nothing
+        if icol > -1:
+            # verify that this line was not commented out
             try:
-                ii=lineString[:icol-1].index('#')
-                pass   # do nothing
+                ii = lineString[: icol - 1].index("#")
+                pass  # do nothing
             except ValueError:
-# This line wasn't commented out
+                # This line wasn't commented out
                 try:
-                    ii=lineString.index(keyWord)
+                    ii = lineString.index(keyWord)
                     if i != iDoNot:
-# string.index and not string.find is used here, since index raises
-# exception when search is failed
+                        # string.index and not string.find is used here, since index raises
+                        # exception when search is failed
                         if verbose:
-                            print('parLocator: '+str(i)+' found:  '+str(b[i]))
-                        iFocus=i
+                            print("parLocator: " + str(i) + " found:  " + str(b[i]))
+                        iFocus = i
                         break
                     else:
-                        iFocus=-1
+                        iFocus = -1
                 except ValueError:
-                    pass   # do nothing
+                    pass  # do nothing
 
     if iFocus == -1:
         if verbose:
-            print('parLocator: Keyword ->'+str(keyWord)+'<-  not found')
+            print("parLocator: Keyword ->" + str(keyWord) + "<-  not found")
     return iFocus
 
-def stringLocator(keyWord,b,n,verbose):
 
-#---- -- locate the relevant line in a file
-#
-    keyWord=keyWord.lower()
-    iFocus=-1
+def stringLocator(keyWord, b, n, verbose):
+
+    # ---- -- locate the relevant line in a file
+    #
+    keyWord = keyWord.lower()
+    iFocus = -1
     for i in range(1, n):
-        lineString=str(b[i]).lower()
+        lineString = str(b[i]).lower()
         try:
-            ii=lineString.index(keyWord)
+            ii = lineString.index(keyWord)
             if verbose:
-                print('parLocator: '+str(i)+' found:  '+str(b[i]))
-            iFocus=i
+                print("parLocator: " + str(i) + " found:  " + str(b[i]))
+            iFocus = i
             break
         except ValueError:
-            pass   # do nothing
+            pass  # do nothing
 
     if iFocus == -1:
         if verbose:
-            print('parLocator: Keyword ->'+str(keyWord)+'<-  not found')
+            print("parLocator: Keyword ->" + str(keyWord) + "<-  not found")
 
     return iFocus
 
 
-def readList(dataFile,iLine,verbose):
+def readList(dataFile, iLine, verbose):
 
     from numpy import size
-#
-#----read list from file to a local float list
-#
-    listDataLine=dataFile[iLine]
-    icol=listDataLine.index(':')
-    Data=listDataLine[icol+1:]
-    lData=Data.split(',')
-    nData=size(lData)
+
+    #
+    # ----read list from file to a local float list
+    #
+    listDataLine = dataFile[iLine]
+    icol = listDataLine.index(":")
+    Data = listDataLine[icol + 1 :]
+    lData = Data.split(",")
+    nData = size(lData)
 
     if verbose:
-        print('readList nData = '+str(nData))
-    fData=map(float,lData)
+        print("readList nData = " + str(nData))
+    fData = map(float, lData)
     return list(fData), nData
 
-def readParameter(dataFile,nLines,keyWord,iDoNot,verbose):
+
+def readParameter(dataFile, nLines, keyWord, iDoNot, verbose):
 
     from numpy import size
-#
-#----read a parameter from a file-list
-#
-    keyWord=keyWord.lower()
-    ipar = parLocator(keyWord,dataFile,nLines,iDoNot,verbose)
+
+    #
+    # ----read a parameter from a file-list
+    #
+    keyWord = keyWord.lower()
+    ipar = parLocator(keyWord, dataFile, nLines, iDoNot, verbose)
     if ipar == -1:
         if verbose:
-            print(' failed to locate '+keyWord+' in base input file; Set value to 1')
+            print(
+                " failed to locate " + keyWord + " in base input file; Set value to 1"
+            )
         paVal = 1
     else:
-        paLine=dataFile[ipar]
-        icol=paLine.index(':')
+        paLine = dataFile[ipar]
+        icol = paLine.index(":")
         try:
-            iComment=paLine.index('#')
-            paVal=paLine[icol+1:iComment-1].lower()
+            iComment = paLine.index("#")
+            paVal = paLine[icol + 1 : iComment - 1].lower()
         except ValueError:
-            paVal=paLine[icol+1:].lower()
+            paVal = paLine[icol + 1 :].lower()
 
     if verbose:
         if ipar != -1:
-            print(keyWord + ' = ' + paVal)
+            print(keyWord + " = " + paVal)
 
-    return paVal,ipar
+    return paVal, ipar
 
-def setContribution(dataFile,nLines,keyWord,iDoNot,verbose):
+
+def setContribution(dataFile, nLines, keyWord, iDoNot, verbose):
 
     from numpy import size
     import string
-#
-# default values
-#
-    nameText=''
+
+    #
+    # default values
+    #
+    nameText = ""
     removeContribution = False
-#
-#----Determine if a given amily contribute to force
-#
-# Start by locating lines setting contribution
-#
-    keyWord=keyWord.lower()
-    ipar = parLocator(keyWord,dataFile,nLines,iDoNot,verbose)
+    #
+    # ----Determine if a given amily contribute to force
+    #
+    # Start by locating lines setting contribution
+    #
+    keyWord = keyWord.lower()
+    ipar = parLocator(keyWord, dataFile, nLines, iDoNot, verbose)
     if ipar == -1:
         if verbose:
-            print(' failed to locate '+keyWord+' in base input file; Set value to 1')
+            print(
+                " failed to locate " + keyWord + " in base input file; Set value to 1"
+            )
         paVal = 1
     else:
-        paLine=dataFile[ipar]
-        icol=paLine.index(':')
+        paLine = dataFile[ipar]
+        icol = paLine.index(":")
 
-# Now identify the first part of this line
+        # Now identify the first part of this line
         firstPart = paLine[0:icol]
 
-# now find out where the standard text ends
-        iBF=firstPart.lower().index('family')+6
-        nameText=string.join( firstPart[iBF:].split(), "")
+        # now find out where the standard text ends
+        iBF = firstPart.lower().index("family") + 6
+        nameText = string.join(firstPart[iBF:].split(), "")
 
-# component name located. Now check about its contribution
+        # component name located. Now check about its contribution
         try:
-            iComment=paLine.index('#')
-            secondPart=paLine[icol+1:iComment-1].lower()
+            iComment = paLine.index("#")
+            secondPart = paLine[icol + 1 : iComment - 1].lower()
         except ValueError:
-            secondPart=paLine[icol+1:].lower()
+            secondPart = paLine[icol + 1 :].lower()
 
-# find the second colon of this line
-        icol2=secondPart.index(':')
+        # find the second colon of this line
+        icol2 = secondPart.index(":")
         try:
-            iComment=secondPart.index('#')
-            yesNoText=secondPart[icol2+1:iComment-1].lower()
+            iComment = secondPart.index("#")
+            yesNoText = secondPart[icol2 + 1 : iComment - 1].lower()
         except ValueError:
-            yesNoText=secondPart[icol2+1:].lower()
+            yesNoText = secondPart[icol2 + 1 :].lower()
 
         try:
-            noFound=yesNoText.lower().index('no')
+            noFound = yesNoText.lower().index("no")
             removeContribution = True
         except ValueError:
-             removeContribution = False
+            removeContribution = False
 
     if verbose:
         if ipar != -1:
-            print(' part: '+nameText+' remove contribution: '+str(removeContribution))
+            print(
+                " part: "
+                + nameText
+                + " remove contribution: "
+                + str(removeContribution)
+            )
 
-    return nameText,removeContribution,ipar
+    return nameText, removeContribution, ipar
 
 
-def setPolaraType(ctrl,nc,verbose):
+def setPolaraType(ctrl, nc, verbose):
 
-# scan the control file and determine polara type and angles
-# Determine pitch direction from control file
-# ---------------------------------------------------
+    # scan the control file and determine polara type and angles
+    # Determine pitch direction from control file
+    # ---------------------------------------------------
 
-    keyWordPitchAxis='pitch axis'
-    iPA = parLocator(keyWordPitchAxis,ctrl,nc,-1,verbose)
+    keyWordPitchAxis = "pitch axis"
+    iPA = parLocator(keyWordPitchAxis, ctrl, nc, -1, verbose)
 
     if iPA == -1:
-        PA='z' # This is the default
+        PA = "z"  # This is the default
     else:
-        paLine=ctrl[iPA]
-        icol=paLine.index(':')
-        paVal=paLine[icol+1:].lower()
-        zFound = 'z' in paVal
+        paLine = ctrl[iPA]
+        icol = paLine.index(":")
+        paVal = paLine[icol + 1 :].lower()
+        zFound = "z" in paVal
         if zFound:
-            PA='z'
+            PA = "z"
         else:
-            yFound = 'y' in paVal
+            yFound = "y" in paVal
             if yFound:
-                PA='y'
+                PA = "y"
             else:
-                raise SystemExit('ERROR in control file: only Y or Z can be given for control keyWord  ->'+keyWordPitchAxis+'<-')
+                raise SystemExit(
+                    "ERROR in control file: only Y or Z can be given for control keyWord  ->"
+                    + keyWordPitchAxis
+                    + "<-"
+                )
 
     if verbose:
-        print('Pitch axis is '+PA.upper())
-#
-# angles definitions:
-#   alpha ... angle of attack
-#   beta  ... side-slip angle
-#   phi   ... roll angle
-#
-# Note: Actually alpha here is the angle of rotation about the above-defined pitch axis
-#       Thus, by replacing the pitch-axis, all that is said here about alpha is actually for beta
-#
-# Several combinations of angles are possible:
-#------------------------------------------------
-# 1. Polar-sweep in alpha per given phi                        ...... polarVar   = aoa
-# 2. Polar-sweep in alpha per given beta (side slip angle)     ...... polarVar   = aoa
-# 3. Polar-sweep in phi per given alpha                        ...... polarVar   = phi
-# 4. Mach ramp  (single values for alpha, phi or both permitted)  ... polarVar   = MachRampNumbers
-#
-# Note: Seting a list of both phi and beta is impossible
-#       For mach ramp you can specify alpha, phi (or both), but not a list of either of them
-#
-# Now let us find out which angles are specified in the control file, to figure out polarSweepType and polarVar
-#
-    keyWordListAOA='angles of attack'
-    iListAOA = parLocator(keyWordListAOA,ctrl,nc,-1,verbose)
-    keyWordListPhi='roll angles'
-    iListPhi = parLocator(keyWordListPhi,ctrl,nc,-1,verbose)
-    keyWordListBeta='side slip angle'
-    iListBeta = parLocator(keyWordListBeta,ctrl,nc,-1,verbose)
-    keyWordListMRN='mach ramp numbers'
-    iListMRN =  parLocator(keyWordListMRN,ctrl,nc,-1,verbose)
-
-#
-# Check first if this is a Mach ramp session
-#
-    if iListMRN > -1 :
-         polarSweepType=4 ; # This is a Mach rmp session
-         polarVar='MachRampNumbers'
-         MachList,nMach=readList(ctrl,iListMRN,verbose);
-#
-# Now check if any angle was specified
-#
-         if iListBeta == -1 :
-              nBeta=0 ; beta=[ ];
-              velDirOption = 1; # Velocity dirction vector v(alpha,phi). May be overwritten below
-         else:
-              beta,nBeta=readList(ctrl,iListBeta,verbose)
-              velDirOption = 2; # Velocity dirction vector v(alpha,beta)
-              if nBeta > 1 :
-                  raise SystemExit('ERROR in control file: >>>>>>>> nBeta > 1 in a Mach Ramp session <<<<<<<<')
-
-         if iListAOA == -1:
-             if velDirOption == 2 :
-                 alpha = [0.0]; nAalpha =1;
-             else:
-                 alpha =[ ]  ; nAalpha=0;
-                 velDirOption = 0; # No specification of Velocity dirction vector. May be overwritten below
-         else:
-             alpha,nAalpha=readList(ctrl,iListAOA,verbose)
-             if nAalpha > 1 :
-                  raise SystemExit('ERROR in control file: >>>>>>>>  nAlpha > 1 in a Mach Ramp session  <<<<<<<<')
-
-         if iListPhi == -1 :
-             if velDirOption != 1 :
-                 phi = [ ] ; nPhi = 0;
-             else:
-                 phi = [0.0] ; nPhi = 1;
-         else:
-             phi,nPhi=readList(ctrl,iListPhi,verbose);
-             if nPhi > 1 :
-                 raise SystemExit('ERROR in control file:  >>>>>>>> nPhi > 1 in a Mach Ramp session  <<<<<<<<')
-             if velDirOption == 0 :
-                 #    if phi is specified, then this is a alpha,phi case, with alpha = 0
-                 velDirOption = 1; alpha = [0.0];  nAalpha =1;
-
-
-
-         if nPhi + nBeta >= 2 :
-             raise SystemExit('ERROR in control file:  >>>>>>>> Both phi and Beta specified  (in a Mach Ramp session)  <<<<<<<<')
-
-
+        print("Pitch axis is " + PA.upper())
+    #
+    # angles definitions:
+    #   alpha ... angle of attack
+    #   beta  ... side-slip angle
+    #   phi   ... roll angle
+    #
+    # Note: Actually alpha here is the angle of rotation about the above-defined pitch axis
+    #       Thus, by replacing the pitch-axis, all that is said here about alpha is actually for beta
+    #
+    # Several combinations of angles are possible:
+    # ------------------------------------------------
+    # 1. Polar-sweep in alpha per given phi                        ...... polarVar   = aoa
+    # 2. Polar-sweep in alpha per given beta (side slip angle)     ...... polarVar   = aoa
+    # 3. Polar-sweep in phi per given alpha                        ...... polarVar   = phi
+    # 4. Mach ramp  (single values for alpha, phi or both permitted)  ... polarVar   = MachRampNumbers
+    #
+    # Note: Seting a list of both phi and beta is impossible
+    #       For mach ramp you can specify alpha, phi (or both), but not a list of either of them
+    #
+    # Now let us find out which angles are specified in the control file, to figure out polarSweepType and polarVar
+    #
+    keyWordListAOA = "angles of attack"
+    iListAOA = parLocator(keyWordListAOA, ctrl, nc, -1, verbose)
+    keyWordListPhi = "roll angles"
+    iListPhi = parLocator(keyWordListPhi, ctrl, nc, -1, verbose)
+    keyWordListBeta = "side slip angle"
+    iListBeta = parLocator(keyWordListBeta, ctrl, nc, -1, verbose)
+    keyWordListMRN = "mach ramp numbers"
+    iListMRN = parLocator(keyWordListMRN, ctrl, nc, -1, verbose)
+
+    #
+    # Check first if this is a Mach ramp session
+    #
+    if iListMRN > -1:
+        polarSweepType = 4
+        # This is a Mach rmp session
+        polarVar = "MachRampNumbers"
+        MachList, nMach = readList(ctrl, iListMRN, verbose)
+        #
+        # Now check if any angle was specified
+        #
+        if iListBeta == -1:
+            nBeta = 0
+            beta = []
+            velDirOption = 1
+            # Velocity dirction vector v(alpha,phi). May be overwritten below
+        else:
+            beta, nBeta = readList(ctrl, iListBeta, verbose)
+            velDirOption = 2
+            # Velocity dirction vector v(alpha,beta)
+            if nBeta > 1:
+                raise SystemExit(
+                    "ERROR in control file: >>>>>>>> nBeta > 1 in a Mach Ramp session <<<<<<<<"
+                )
+
+        if iListAOA == -1:
+            if velDirOption == 2:
+                alpha = [0.0]
+                nAalpha = 1
+            else:
+                alpha = []
+                nAalpha = 0
+                velDirOption = 0
+                # No specification of Velocity dirction vector. May be overwritten below
+        else:
+            alpha, nAalpha = readList(ctrl, iListAOA, verbose)
+            if nAalpha > 1:
+                raise SystemExit(
+                    "ERROR in control file: >>>>>>>>  nAlpha > 1 in a Mach Ramp session  <<<<<<<<"
+                )
+
+        if iListPhi == -1:
+            if velDirOption != 1:
+                phi = []
+                nPhi = 0
+            else:
+                phi = [0.0]
+                nPhi = 1
+        else:
+            phi, nPhi = readList(ctrl, iListPhi, verbose)
+            if nPhi > 1:
+                raise SystemExit(
+                    "ERROR in control file:  >>>>>>>> nPhi > 1 in a Mach Ramp session  <<<<<<<<"
+                )
+            if velDirOption == 0:
+                #    if phi is specified, then this is a alpha,phi case, with alpha = 0
+                velDirOption = 1
+                alpha = [0.0]
+                nAalpha = 1
+
+        if nPhi + nBeta >= 2:
+            raise SystemExit(
+                "ERROR in control file:  >>>>>>>> Both phi and Beta specified  (in a Mach Ramp session)  <<<<<<<<"
+            )
 
     else:
-#
-# this is not a mach ramp
-        MachList=[ ]; nMach=0;
-#
-# So, this is a polar-sweep and not mach ramp.
-# Now find out polarSweepType (1,2,or 3)
-#
-
-        if iListPhi == -1 :
-            if  iListBeta == -1 :
-                polarSweepType=1 ;
-                polarVar='aoa' ;  # phi/beta not found. Polar sweep in alpha for phi=beta=0
-                velDirOption = 1; #  Velocity dirction vector v(alpha,phi).
-                phi = [0.0] ; nPhi = 1;
-                nBeta=0 ; beta=[ ];
+        #
+        # this is not a mach ramp
+        MachList = []
+        nMach = 0
+        #
+        # So, this is a polar-sweep and not mach ramp.
+        # Now find out polarSweepType (1,2,or 3)
+        #
+
+        if iListPhi == -1:
+            if iListBeta == -1:
+                polarSweepType = 1
+                polarVar = "aoa"
+                # phi/beta not found. Polar sweep in alpha for phi=beta=0
+                velDirOption = 1
+                #  Velocity dirction vector v(alpha,phi).
+                phi = [0.0]
+                nPhi = 1
+                nBeta = 0
+                beta = []
             else:
-#         beta was found in control file, phi is not there; check how about alpha
-                nPhi = 0 ; phi=[ ];
-                polarSweepType=2 ;
-                polarVar='aoa' ;
-                velDirOption = 2; #  Velocity dirction vector v(alpha,beta).
-                beta,nBeta=readList(ctrl,iListBeta,verbose)
-                if nBeta > 1 :
-                    raise SystemExit('ERROR in control file: nBeta > 1. For polar sweep in beta exchange pitch-axis and use aoa')
-
-            if  iListAOA == -1 :
-                raise SystemExit('ERROR in control file: phi and alpha are missing. Polar sweep not defined')
-
-            alpha,nAalpha=readList(ctrl,iListAOA,verbose)
+                #         beta was found in control file, phi is not there; check how about alpha
+                nPhi = 0
+                phi = []
+                polarSweepType = 2
+                polarVar = "aoa"
+                velDirOption = 2
+                #  Velocity dirction vector v(alpha,beta).
+                beta, nBeta = readList(ctrl, iListBeta, verbose)
+                if nBeta > 1:
+                    raise SystemExit(
+                        "ERROR in control file: nBeta > 1. For polar sweep in beta exchange pitch-axis and use aoa"
+                    )
+
+            if iListAOA == -1:
+                raise SystemExit(
+                    "ERROR in control file: phi and alpha are missing. Polar sweep not defined"
+                )
+
+            alpha, nAalpha = readList(ctrl, iListAOA, verbose)
 
         else:
-#
-#      phi was found in control file, so beta must not be there
-#
+            #
+            #      phi was found in control file, so beta must not be there
+            #
             if iListBeta > -1:
-                raise SystemExit('ERROR in control file: both phi and beta specified.  Polar sweep not defined ')
-
-            nBeta=0 ; beta=[ ];
-            velDirOption = 1; #  Velocity dirction vector v(alpha,phi).
-#
-#     Check now if alpha appears
-#
-            if  iListAOA == -1 :
-#
-#     phi found in control file, but alpha is missing, so it is a polar-sweep in phi with alpha=0
-#
-                polarSweepType=3 ;
-                polarVar='phi' ; alpha =[0.0]  ; nAalpha=1
+                raise SystemExit(
+                    "ERROR in control file: both phi and beta specified.  Polar sweep not defined "
+                )
+
+            nBeta = 0
+            beta = []
+            velDirOption = 1
+            #  Velocity dirction vector v(alpha,phi).
+            #
+            #     Check now if alpha appears
+            #
+            if iListAOA == -1:
+                #
+                #     phi found in control file, but alpha is missing, so it is a polar-sweep in phi with alpha=0
+                #
+                polarSweepType = 3
+                polarVar = "phi"
+                alpha = [0.0]
+                nAalpha = 1
 
             else:
-#
-#     Both alpha and phi found in control file. Find out which one is a list
-#
-                alpha,nAalpha=readList(ctrl,iListAOA,verbose)
+                #
+                #     Both alpha and phi found in control file. Find out which one is a list
+                #
+                alpha, nAalpha = readList(ctrl, iListAOA, verbose)
 
-            phi,nPhi=readList(ctrl,iListPhi,verbose)
+            phi, nPhi = readList(ctrl, iListPhi, verbose)
 
             if nAalpha == 1:
-                if nPhi > 1 :
-                    polarSweepType=3
-                    polarVar='phi'
+                if nPhi > 1:
+                    polarSweepType = 3
+                    polarVar = "phi"
                 else:
-                    polarSweepType=1
-                    polarVar='aoa'
+                    polarSweepType = 1
+                    polarVar = "aoa"
 
-                nBeta=0; beta=[ ];
+                nBeta = 0
+                beta = []
             else:
-#
-#-----that is nAlpha > 1
-#
-                if nPhi > 1 :
-                    raise SystemExit('ERROR in control file: read lists in both alpha and phi.  Polar sweep not defined ')
-
-                polarSweepType=1 ;
-                polarVar='aoa'; nBeta=0; beta=[ ];
-
-#
-# Here we end the long if cycle, refrring to Mach ramp or angle sweep
-
-#-------------------------------------------------------------------------------------------
+                #
+                # -----that is nAlpha > 1
+                #
+                if nPhi > 1:
+                    raise SystemExit(
+                        "ERROR in control file: read lists in both alpha and phi.  Polar sweep not defined "
+                    )
+
+                polarSweepType = 1
+                polarVar = "aoa"
+                nBeta = 0
+                beta = []
+
+    #
+    # Here we end the long if cycle, refrring to Mach ramp or angle sweep
+
+    # -------------------------------------------------------------------------------------------
     if verbose:
-        if polarSweepType == 1 :
-            print('Sweep type: '+str(polarSweepType)+' in alpha. nAalpha = '+str(nAalpha)+' phi = '+str(phi))
-        elif polarSweepType == 2 :
-            print('Sweep type: '+str(polarSweepType)+' in alpha. nAalpha = '+str(nAalpha)+' beta = '+str(beta))
-        elif polarSweepType == 3 :
-            print('Sweep type: '+str(polarSweepType)+' in phi. nPhi = '+str(nPhi)+' alpha = ',str(alpha))
-        elif polarSweepType == 4 :
-            print('Sweep type: '+str(polarSweepType)+' in Mach. nMach = '+str(nMach))
-
-    return PA,polarSweepType,velDirOption,nAalpha,nBeta,nPhi,nMach,alpha,beta,phi,MachList,polarVar
-
-def setVelDir(velDirOption,PA,alphar,phir,betar):
-
-# set the velocity direction
-    from numpy import sin,cos,tan,size
-
-#
-# Check for alpha and if we are dealing with values greater than 88deg (near 90)
-# In such cases cases change to  sin cos formualtion
-#
-
-    a88=1.5359 #   88 degrees
-    if velDirOption == 2 :
-
-        if PA == 'z':
-            if alphar < a88 :
-                dv1 = [cos(betar)  for x in alphar]
-                dv2 = tan(alphar)*cos(betar)
+        if polarSweepType == 1:
+            print(
+                "Sweep type: "
+                + str(polarSweepType)
+                + " in alpha. nAalpha = "
+                + str(nAalpha)
+                + " phi = "
+                + str(phi)
+            )
+        elif polarSweepType == 2:
+            print(
+                "Sweep type: "
+                + str(polarSweepType)
+                + " in alpha. nAalpha = "
+                + str(nAalpha)
+                + " beta = "
+                + str(beta)
+            )
+        elif polarSweepType == 3:
+            print(
+                "Sweep type: "
+                + str(polarSweepType)
+                + " in phi. nPhi = "
+                + str(nPhi)
+                + " alpha = ",
+                str(alpha),
+            )
+        elif polarSweepType == 4:
+            print(
+                "Sweep type: " + str(polarSweepType) + " in Mach. nMach = " + str(nMach)
+            )
+
+    return (
+        PA,
+        polarSweepType,
+        velDirOption,
+        nAalpha,
+        nBeta,
+        nPhi,
+        nMach,
+        alpha,
+        beta,
+        phi,
+        MachList,
+        polarVar,
+    )
+
+
+def setVelDir(velDirOption, PA, alphar, phir, betar):
+
+    # set the velocity direction
+    from numpy import sin, cos, tan, size
+
+    #
+    # Check for alpha and if we are dealing with values greater than 88deg (near 90)
+    # In such cases cases change to  sin cos formualtion
+    #
+
+    a88 = 1.5359  #   88 degrees
+    if velDirOption == 2:
+
+        if PA == "z":
+            if alphar < a88:
+                dv1 = [cos(betar) for x in alphar]
+                dv2 = tan(alphar) * cos(betar)
                 dv3 = [sin(betar) for x in alphar]
             else:
-                dv1 = cos(betar)*cos(alphar)
-                dv2 = sin(alphar)*cos(betar)
-                dv3 = sin(betar)*cos(alphar)
+                dv1 = cos(betar) * cos(alphar)
+                dv2 = sin(alphar) * cos(betar)
+                dv3 = sin(betar) * cos(alphar)
         else:
-            if alphar < a88 :
-                dv1 = [cos(betar)  for x in alphar]
-                dv2 = [sin(betar)  for x in alphar]
-                dv3 = tan(alphar)*cos(betar)
+            if alphar < a88:
+                dv1 = [cos(betar) for x in alphar]
+                dv2 = [sin(betar) for x in alphar]
+                dv3 = tan(alphar) * cos(betar)
             else:
-                dv1 = cos(betar)*cos(alphar)
-                dv2 = sin(betar)*cos(alphar)
-                dv3 = sin(alphar)*cos(betar)
+                dv1 = cos(betar) * cos(alphar)
+                dv2 = sin(betar) * cos(alphar)
+                dv3 = sin(alphar) * cos(betar)
     else:
 
-        if size(alphar) > size(phir) :
-            dummyVec=alphar
+        if size(alphar) > size(phir):
+            dummyVec = alphar
         else:
-            dummyVec=phir
+            dummyVec = phir
 
-        if PA == 'z':
-            if alphar < a88 :
-                 dv1=[1.0 for x in dummyVec ]
-                 dv2=tan(alphar)*cos(phir)
-                 dv3=tan(alphar)*sin(phir)
+        if PA == "z":
+            if alphar < a88:
+                dv1 = [1.0 for x in dummyVec]
+                dv2 = tan(alphar) * cos(phir)
+                dv3 = tan(alphar) * sin(phir)
             else:
-                if size(alphar) > 1 :
-                    dv1= cos(alphar)
+                if size(alphar) > 1:
+                    dv1 = cos(alphar)
                 else:
-                    dv1=[cos(alphar) for x in dummyVec ]
+                    dv1 = [cos(alphar) for x in dummyVec]
 
-                dv2=sin(alphar)*cos(phir)
-                dv3=sin(alphar)*sin(phir)
+                dv2 = sin(alphar) * cos(phir)
+                dv3 = sin(alphar) * sin(phir)
         else:
-           if alphar < a88 :
-               dv1=[1.0  for x in dummyVec ]
-               dv2=tan(alphar)*sin(phir)
-               dv3=tan(alphar)*cos(phir)
-           else:
-               if size(alphar) > 1 :
-                   dv1= cos(alphar)
-               else:
-                   dv1=[cos(alphar) for x in dummyVec ]
-               dv2=sin(alphar)*sin(phir)
-               dv3=sin(alphar)*cos(phir)
-
-    return dv1,dv2,dv3
-
-def processAddAngle(addRunStr,nPolara,parAngle,angleEqualCriterion):
-#
-#---------------------------------------------------------------------
-# Process the list of interactively added angles.
-# Note that parAngle can receive also MachList
-#--------------------------------------------------------------------
+            if alphar < a88:
+                dv1 = [1.0 for x in dummyVec]
+                dv2 = tan(alphar) * sin(phir)
+                dv3 = tan(alphar) * cos(phir)
+            else:
+                if size(alphar) > 1:
+                    dv1 = cos(alphar)
+                else:
+                    dv1 = [cos(alphar) for x in dummyVec]
+                dv2 = sin(alphar) * sin(phir)
+                dv3 = sin(alphar) * cos(phir)
+
+    return dv1, dv2, dv3
 
 
-#------------ create a list out of entered angles
+def processAddAngle(addRunStr, nPolara, parAngle, angleEqualCriterion):
+    #
+    # ---------------------------------------------------------------------
+    # Process the list of interactively added angles.
+    # Note that parAngle can receive also MachList
+    # --------------------------------------------------------------------
 
-    addRunList=addRunStr.split(',')
-    fAddRunListRaw=map(float,addRunList)
-    fAddRunList=sort(fAddRunListRaw)
-    nAddRun=size(fAddRunList)
+    # ------------ create a list out of entered angles
 
-#------- By default, do not compute the cases in input file, since they were computed already
+    addRunList = addRunStr.split(",")
+    fAddRunListRaw = map(float, addRunList)
+    fAddRunList = sort(fAddRunListRaw)
+    nAddRun = size(fAddRunList)
 
-    computeCase=[False for j in range(0,nPolara+nAddRun)]
-    rerunCase = [False for j in range(0,nPolara+nAddRun)]
+    # ------- By default, do not compute the cases in input file, since they were computed already
 
+    computeCase = [False for j in range(0, nPolara + nAddRun)]
+    rerunCase = [False for j in range(0, nPolara + nAddRun)]
 
-#----- Now, for each  new angle/Mach verify if it is a rerun or inserted new value
+    # ----- Now, for each  new angle/Mach verify if it is a rerun or inserted new value
 
-    closestAngle=[0 for i in range(0,nAddRun)]
-    for i in range(0,nAddRun):
+    closestAngle = [0 for i in range(0, nAddRun)]
+    for i in range(0, nAddRun):
 
-        diff=[abs(fAddRunList[i]-x) for x in parAngle]
-        iClose=diff.index(min(diff))
-        closestAngle[i]=parAngle[iClose]
+        diff = [abs(fAddRunList[i] - x) for x in parAngle]
+        iClose = diff.index(min(diff))
+        closestAngle[i] = parAngle[iClose]
         if min(diff) < angleEqualCriterion:
-            computeCase[iClose]=True
-            rerunCase[iClose]=True
+            computeCase[iClose] = True
+            rerunCase[iClose] = True
 
         else:
 
             if fAddRunList[i] > closestAngle[i]:
-                ii=iClose+1
+                ii = iClose + 1
             else:
-                ii=iClose
+                ii = iClose
 
-            tmpAng1=parAngle[:ii]
+            tmpAng1 = parAngle[:ii]
             tmpAng1.append(fAddRunList[i])
-            tmpAng2=parAngle[ii:]
+            tmpAng2 = parAngle[ii:]
             tmpAng1.extend(tmpAng2)
 
-            parAngle=tmpAng1
-            nPolara=nPolara+1
-            computeCase[ii]=True
+            parAngle = tmpAng1
+            nPolara = nPolara + 1
+            computeCase[ii] = True
 
+    return nPolara, parAngle, computeCase, rerunCase
 
-    return  nPolara,parAngle,computeCase,rerunCase
 
-def updatedControlFile(ctrl,nc,parAngle,ctrlFile,verbose):
+def updatedControlFile(ctrl, nc, parAngle, ctrlFile, verbose):
 
-# generate a modified control file for case with addRun options
+    # generate a modified control file for case with addRun options
 
     import os
-#
-#-- get a proper list of updated parameter-angle
-    st1=str(parAngle)
-    updatedAngleList=st1[1:-1]
-# Now let us find out which angles are specified in the control file, to figure out polarSweepType and polarVar
-#
-    keyWordListAOA='angles of attack'
-    iListAOA = parLocator(keyWordListAOA,ctrl,nc,-1,verbose)
-    keyWordListPhi='roll angles'
-    iListPhi = parLocator(keyWordListPhi,ctrl,nc,-1,verbose)
-    keyWordListBeta='side slip angle'
-    iListBeta = parLocator(keyWordListBeta,ctrl,nc,-1,verbose)
-    keyWordListMRN='mach ramp numbers'
-    iListMRN =  parLocator(keyWordListMRN,ctrl,nc,-1,verbose)
-#
-# Check first if this is a Mach ramp session
-#
-    if iListMRN > -1 :
-         polarSweepType=4 ; # This is a Mach rmp session
-         polarVar='MachRampNumbers'
-         MachList,nMach=readList(ctrl,iListMRN,verbose);
-#
-# Now check if any angle was specified
-#
-         if iListBeta == -1 :
-              nBeta=0 ; beta=[ ];
-              velDirOption = 1; # Velocity dirction vector v(alpha,phi). May be overwritten below
-         else:
-              beta,nBeta=readList(ctrl,iListBeta,verbose)
-              velDirOption = 2; # Velocity dirction vector v(alpha,beta)
-              if nBeta > 1 :
-                  raise SystemExit('ERROR in control file: >>>>>>>> nBeta > 1 in a Mach Ramp session <<<<<<<<')
-
-         if iListAOA == -1:
-             if velDirOption == 2 :
-                 alpha = [0.0]; nAalpha =1;
-             else:
-                 alpha =[ ]  ; nAalpha=0;
-                 velDirOption = 0; # No specification of Velocity dirction vector. May be overwritten below
-         else:
-             alpha,nAalpha=readList(ctrl,iListAOA,verbose)
-             if nAalpha > 1 :
-                  raise SystemExit('ERROR in control file: >>>>>>>>  nAlpha > 1 in a Mach Ramp session  <<<<<<<<')
-
-             if iListPhi == -1 :
-                 if velDirOption != 1 :
-                     phi = [ ] ; nPhi = 0;
-                 else:
-                     phi = [0.0] ; nPhi = 1;
-             else:
-                 phi,nPhi=readList(ctrl,iListPhi,verbose);
-                 if nPhi > 1 :
-                     raise SystemExit('ERROR in control file:  >>>>>>>> nPhi > 1 in a Mach Ramp session  <<<<<<<<')
-                 if velDirOption == 0 :
-#    if phi is specified, then this is a alpha,phi case, with alpha = 0
-                     velDirOption = 1; alpha = [0.0];  nAalpha =1;
-
-         if nPhi + nBeta >= 2 :
-             raise SystemExit('ERROR in control file:  >>>>>>>> Both phi and Beta specified  (in a Mach Ramp session)  <<<<<<<<')
-
-         ctrl[iListMRN]=' Mach ramp numbers :  '+updatedAngleList+'\n'
 
-    else:
-#
-# this is not a mach ramp
-        MachList=[ ]; nMach=0;
-        if iListPhi == -1 :
-            if  iListBeta == -1 :
-                polarSweepType=1 ;
-                polarVar='aoa' ;  # phi/beta not found. Polar sweep in alpha for phi=beta=0
-                phi = [0.0] ; nPhi = 1;
-                nBeta=0 ; beta=[ ];
+    #
+    # -- get a proper list of updated parameter-angle
+    st1 = str(parAngle)
+    updatedAngleList = st1[1:-1]
+    # Now let us find out which angles are specified in the control file, to figure out polarSweepType and polarVar
+    #
+    keyWordListAOA = "angles of attack"
+    iListAOA = parLocator(keyWordListAOA, ctrl, nc, -1, verbose)
+    keyWordListPhi = "roll angles"
+    iListPhi = parLocator(keyWordListPhi, ctrl, nc, -1, verbose)
+    keyWordListBeta = "side slip angle"
+    iListBeta = parLocator(keyWordListBeta, ctrl, nc, -1, verbose)
+    keyWordListMRN = "mach ramp numbers"
+    iListMRN = parLocator(keyWordListMRN, ctrl, nc, -1, verbose)
+    #
+    # Check first if this is a Mach ramp session
+    #
+    if iListMRN > -1:
+        polarSweepType = 4
+        # This is a Mach rmp session
+        polarVar = "MachRampNumbers"
+        MachList, nMach = readList(ctrl, iListMRN, verbose)
+        #
+        # Now check if any angle was specified
+        #
+        if iListBeta == -1:
+            nBeta = 0
+            beta = []
+            velDirOption = 1
+            # Velocity dirction vector v(alpha,phi). May be overwritten below
+        else:
+            beta, nBeta = readList(ctrl, iListBeta, verbose)
+            velDirOption = 2
+            # Velocity dirction vector v(alpha,beta)
+            if nBeta > 1:
+                raise SystemExit(
+                    "ERROR in control file: >>>>>>>> nBeta > 1 in a Mach Ramp session <<<<<<<<"
+                )
+
+        if iListAOA == -1:
+            if velDirOption == 2:
+                alpha = [0.0]
+                nAalpha = 1
             else:
-#         beta was found in control file, phi is not there; check how about alpha
-                nPhi = 0 ; phi=[ ];
-                polarSweepType=2 ;
-                polarVar='aoa' ;
-                beta,nBeta=readList(ctrl,iListBeta,verbose)
-                if nBeta > 1 :
-                    raise SystemExit('ERROR in control file: nBeta > 1. For polar sweep in beta exchange pitch-axis and use aoa')
-
-            if  iListAOA == -1 :
-                raise SystemExit('ERROR in control file: phi and alpha are missing. Polar sweep not defined')
+                alpha = []
+                nAalpha = 0
+                velDirOption = 0
+                # No specification of Velocity dirction vector. May be overwritten below
+        else:
+            alpha, nAalpha = readList(ctrl, iListAOA, verbose)
+            if nAalpha > 1:
+                raise SystemExit(
+                    "ERROR in control file: >>>>>>>>  nAlpha > 1 in a Mach Ramp session  <<<<<<<<"
+                )
+
+            if iListPhi == -1:
+                if velDirOption != 1:
+                    phi = []
+                    nPhi = 0
+                else:
+                    phi = [0.0]
+                    nPhi = 1
+            else:
+                phi, nPhi = readList(ctrl, iListPhi, verbose)
+                if nPhi > 1:
+                    raise SystemExit(
+                        "ERROR in control file:  >>>>>>>> nPhi > 1 in a Mach Ramp session  <<<<<<<<"
+                    )
+                if velDirOption == 0:
+                    #    if phi is specified, then this is a alpha,phi case, with alpha = 0
+                    velDirOption = 1
+                    alpha = [0.0]
+                    nAalpha = 1
+
+        if nPhi + nBeta >= 2:
+            raise SystemExit(
+                "ERROR in control file:  >>>>>>>> Both phi and Beta specified  (in a Mach Ramp session)  <<<<<<<<"
+            )
+
+        ctrl[iListMRN] = " Mach ramp numbers :  " + updatedAngleList + "\n"
 
-            alpha,nAalpha=readList(ctrl,iListAOA,verbose)
-            ctrl[iListAOA]=' angles of attack :  '+updatedAngleList+'\n'
+    else:
+        #
+        # this is not a mach ramp
+        MachList = []
+        nMach = 0
+        if iListPhi == -1:
+            if iListBeta == -1:
+                polarSweepType = 1
+                polarVar = "aoa"
+                # phi/beta not found. Polar sweep in alpha for phi=beta=0
+                phi = [0.0]
+                nPhi = 1
+                nBeta = 0
+                beta = []
+            else:
+                #         beta was found in control file, phi is not there; check how about alpha
+                nPhi = 0
+                phi = []
+                polarSweepType = 2
+                polarVar = "aoa"
+                beta, nBeta = readList(ctrl, iListBeta, verbose)
+                if nBeta > 1:
+                    raise SystemExit(
+                        "ERROR in control file: nBeta > 1. For polar sweep in beta exchange pitch-axis and use aoa"
+                    )
+
+            if iListAOA == -1:
+                raise SystemExit(
+                    "ERROR in control file: phi and alpha are missing. Polar sweep not defined"
+                )
+
+            alpha, nAalpha = readList(ctrl, iListAOA, verbose)
+            ctrl[iListAOA] = " angles of attack :  " + updatedAngleList + "\n"
 
         else:
-#      phi was found in control file, so beta must not be there
+            #      phi was found in control file, so beta must not be there
             if iListBeta > -1:
-                raise SystemExit('ERROR in control file: both phi and beta specified.  Polar sweep not defined ')
-
-            nBeta=0 ; beta=[ ];
-#     Check now if alpha appears
-            if  iListAOA == -1 :
-#     phi found in control file, but alpha is missing, so it is a polar-sweep in phi with alpha=0
-                polarSweepType=3 ;
-                polarVar='phi' ; alpha =[0.0]  ; nAalpha=1
+                raise SystemExit(
+                    "ERROR in control file: both phi and beta specified.  Polar sweep not defined "
+                )
+
+            nBeta = 0
+            beta = []
+            #     Check now if alpha appears
+            if iListAOA == -1:
+                #     phi found in control file, but alpha is missing, so it is a polar-sweep in phi with alpha=0
+                polarSweepType = 3
+                polarVar = "phi"
+                alpha = [0.0]
+                nAalpha = 1
 
             else:
-#
-#     Both alpha and phi found in control file. Find out which one is a list
-#
-                alpha,nAalpha=readList(ctrl,iListAOA,verbose)
-                if nAalpha > 1 :
-                    ctrl[iListAOA]=' angles of attack :  '+updatedAngleList+'\n'
-
-            phi,nPhi=readList(ctrl,iListPhi,verbose)
+                #
+                #     Both alpha and phi found in control file. Find out which one is a list
+                #
+                alpha, nAalpha = readList(ctrl, iListAOA, verbose)
+                if nAalpha > 1:
+                    ctrl[iListAOA] = " angles of attack :  " + updatedAngleList + "\n"
+
+            phi, nPhi = readList(ctrl, iListPhi, verbose)
             if nPhi > 1:
-                ctrl[iListPhi]=' roll angles :  '+updatedAngleList+'\n'
+                ctrl[iListPhi] = " roll angles :  " + updatedAngleList + "\n"
 
-# Prepare a backup of control file
+    # Prepare a backup of control file
 
-    shutil.copy2(ctrlFile, ctrlFile+'.bck')
-#
-# --- Write down the updated file
-    fc=open(ctrlFile,'w')
+    shutil.copy2(ctrlFile, ctrlFile + ".bck")
+    #
+    # --- Write down the updated file
+    fc = open(ctrlFile, "w")
     fc.writelines(ctrl)
     fc.close()
 
-    print('More cases were added. Original ctrl file saved at '+ctrlFile+'.bck File '+ctrlFile+' updated')
-
+    print(
+        "More cases were added. Original ctrl file saved at "
+        + ctrlFile
+        + ".bck File "
+        + ctrlFile
+        + " updated"
+    )
 
     return
 
-def retrievePhysicalData(b,n,polarSweepType,verbose):
 
-# scan the control file and retrieve physical data parameters and their location
-# Included are Mach and reynolds number (non-dim group)
-#              Pref, rho_ref, Tref (ref group)
-# ---------------------------------------------------
-#
-# physical data, needed for Mach ramp
-#
-    keyWord='mach for coefficients'
-    MachNumCoef,iparMcoeff=readParameter(b,n,keyWord,-1,verbose)
-    keyWord='mach'
-    MachNum,iprMach=readParameter(b,n,keyWord,iparMcoeff,verbose)  # look for Mach, but avoid Mach for coefficients
-    keyWord='reynolds length (in meter)'
-    ReNumRefLength,iprDRe=readParameter(b,n,keyWord,-1,verbose)
-    keyWord='reynolds'
-    ReNum,iprRe=readParameter(b,n,keyWord,iprDRe,verbose)
-    sNonDimNum=[MachNum,MachNumCoef,ReNum,ReNumRefLength]
-    nonDimNum=map(float,sNonDimNum)
-    nonDimNumLoc=[iprMach,iparMcoeff,iprRe,iprDRe]
-#
-# the next set of parameters might, or might not appear in base input file
-# If they appear, they should be updated in a Mach ramp. All 3 of them are needed.
-#
+def retrievePhysicalData(b, n, polarSweepType, verbose):
+
+    # scan the control file and retrieve physical data parameters and their location
+    # Included are Mach and reynolds number (non-dim group)
+    #              Pref, rho_ref, Tref (ref group)
+    # ---------------------------------------------------
+    #
+    # physical data, needed for Mach ramp
+    #
+    keyWord = "mach for coefficients"
+    MachNumCoef, iparMcoeff = readParameter(b, n, keyWord, -1, verbose)
+    keyWord = "mach"
+    MachNum, iprMach = readParameter(
+        b, n, keyWord, iparMcoeff, verbose
+    )  # look for Mach, but avoid Mach for coefficients
+    keyWord = "reynolds length (in meter)"
+    ReNumRefLength, iprDRe = readParameter(b, n, keyWord, -1, verbose)
+    keyWord = "reynolds"
+    ReNum, iprRe = readParameter(b, n, keyWord, iprDRe, verbose)
+    sNonDimNum = [MachNum, MachNumCoef, ReNum, ReNumRefLength]
+    nonDimNum = map(float, sNonDimNum)
+    nonDimNumLoc = [iprMach, iparMcoeff, iprRe, iprDRe]
+    #
+    # the next set of parameters might, or might not appear in base input file
+    # If they appear, they should be updated in a Mach ramp. All 3 of them are needed.
+    #
     refParNo = 0
-    keyWord='Reference pressure (in Pa)'
-    pRef,iprPr=readParameter(b,n,keyWord,-1,verbose)
-    if iprPr > -1 :
-        refParNo =refParNo + 1;
+    keyWord = "Reference pressure (in Pa)"
+    pRef, iprPr = readParameter(b, n, keyWord, -1, verbose)
+    if iprPr > -1:
+        refParNo = refParNo + 1
 
-    keyWord='Reference density (in kg/m^3)'
-    rhoRef,iprRho=readParameter(b,n,keyWord,-1,verbose)
+    keyWord = "Reference density (in kg/m^3)"
+    rhoRef, iprRho = readParameter(b, n, keyWord, -1, verbose)
     if iprRho > -1:
-        refParNo =refParNo + 1;
+        refParNo = refParNo + 1
 
-    keyWord='Reference temperature (in K)'
-    TRef,iprT=readParameter(b,n,keyWord,-1,verbose)
+    keyWord = "Reference temperature (in K)"
+    TRef, iprT = readParameter(b, n, keyWord, -1, verbose)
     if iprT > -1:
-        refParNo =refParNo + 1;
+        refParNo = refParNo + 1
 
-    if refParNo == 3 :
+    if refParNo == 3:
         refParExist = True
-    elif refParNo  == 0 :
+    elif refParNo == 0:
         refParExist = False
     else:
-        if polarSweepType == 4 :
-            raise SystemExit('ERROR in control file: in Mach ramp, base file should include (Pr,rho_r,Tr) or none of them')
+        if polarSweepType == 4:
+            raise SystemExit(
+                "ERROR in control file: in Mach ramp, base file should include (Pr,rho_r,Tr) or none of them"
+            )
 
     if refParExist:
-        sRefPar=[pRef,rhoRef,TRef]
-        refPar=map(float,sRefPar)
-        refParLoc=[iprPr,iprRho,iprT]
-#
-# Thermodynamic properties
-#
-    keyWord='Constant specific heat ratio'
-    gamma,iprGamma=readParameter(b,n,keyWord,-1,verbose)
-    keyWord='Gas constant (J/(kg K))'
-    rGas,iprGasC=readParameter(b,n,keyWord,-1,verbose)
-    keyWord='Free stream temperature (in K)'
-    TFreeS,iprTFreeS=readParameter(b,n,keyWord,-1,verbose)
-
-    sThermoPar=[gamma,rGas,TFreeS]
-    thermoPar=map(float,sThermoPar)
-    thermoParLoc=[iprGamma,iprGasC,iprTFreeS]
+        sRefPar = [pRef, rhoRef, TRef]
+        refPar = map(float, sRefPar)
+        refParLoc = [iprPr, iprRho, iprT]
+    #
+    # Thermodynamic properties
+    #
+    keyWord = "Constant specific heat ratio"
+    gamma, iprGamma = readParameter(b, n, keyWord, -1, verbose)
+    keyWord = "Gas constant (J/(kg K))"
+    rGas, iprGasC = readParameter(b, n, keyWord, -1, verbose)
+    keyWord = "Free stream temperature (in K)"
+    TFreeS, iprTFreeS = readParameter(b, n, keyWord, -1, verbose)
+
+    sThermoPar = [gamma, rGas, TFreeS]
+    thermoPar = map(float, sThermoPar)
+    thermoParLoc = [iprGamma, iprGasC, iprTFreeS]
 
     if verbose:
-        print('base case parameters of Mach ramp')
-        print('---------------------------------')
-        print(' M = '+sNonDimNum[0]+' Reynolds = '+sNonDimNum[2])
+        print("base case parameters of Mach ramp")
+        print("---------------------------------")
+        print(" M = " + sNonDimNum[0] + " Reynolds = " + sNonDimNum[2])
         if refParExist:
-            print(' Pref = '+str(refPar[0])+' rhor = '+str(refPar[1])+' Tr = '+str(refPar[2]))
-            print(' gamma = '+str(thermoPar[0])+ ' Gas Const = '+str(thermoPar[1])+' T_freeStream = '+str(thermoPar[2]))
-
-
-    return nonDimNum,nonDimNumLoc,refParExist,refPar,refParLoc,thermoPar,thermoParLoc
+            print(
+                " Pref = "
+                + str(refPar[0])
+                + " rhor = "
+                + str(refPar[1])
+                + " Tr = "
+                + str(refPar[2])
+            )
+            print(
+                " gamma = "
+                + str(thermoPar[0])
+                + " Gas Const = "
+                + str(thermoPar[1])
+                + " T_freeStream = "
+                + str(thermoPar[2])
+            )
+
+    return (
+        nonDimNum,
+        nonDimNumLoc,
+        refParExist,
+        refPar,
+        refParLoc,
+        thermoPar,
+        thermoParLoc,
+    )
+
+
+def fMachIsentropic(Mach, Gamma):
+
+    # Isentropic relation of Mach
+    # ---------------------------------------------------
+    #
+    fMach = 1.0 + (Gamma - 1.0) / 2.0 * Mach * Mach
+    return fMach
 
-def fMachIsentropic(Mach,Gamma):
 
-# Isentropic relation of Mach
-# ---------------------------------------------------
-#
-    fMach = 1.0 + (Gamma-1.0)/2.0*Mach*Mach;
-    return fMach
 #
 #
-def extractUy(filename,outFile,inDepVar,depVar,verbose):
+def extractUy(filename, outFile, inDepVar, depVar, verbose):
 
     import os
     import sys
 
+    # --------------- read the  file
 
-#--------------- read the  file
-
-    fc=open(filename,'r')
-    data=fc.readlines()
-    nc=size(data)
+    fc = open(filename, "r")
+    data = fc.readlines()
+    nc = size(data)
     fc.close()
-    print(str(nc)+' lines were written from file '+filename+'. File closed')
+    print(str(nc) + " lines were written from file " + filename + ". File closed")
 
-# --------------Retreive the variables names in the Tecplot file
+    # --------------Retreive the variables names in the Tecplot file
 
-    ivb=stringLocator('VARIABLES',data,nc,verbose)
+    ivb = stringLocator("VARIABLES", data, nc, verbose)
     if ivb == -1:
-        raise SystemExit('ERROR: failed to trace VARIABLES list in input file')
+        raise SystemExit("ERROR: failed to trace VARIABLES list in input file")
 
-    izo=stringLocator('ZONE',data,nc,verbose)
+    izo = stringLocator("ZONE", data, nc, verbose)
     if izo == -1:
-        raise SystemExit('ERROR: failed to trace ZONE list in input file')
+        raise SystemExit("ERROR: failed to trace ZONE list in input file")
 
-    izo=izo-1  #  last variables line
-    print('list of variables traced between lines '+str(ivb)+' and ',str(izo))
+    izo = izo - 1  #  last variables line
+    print("list of variables traced between lines " + str(ivb) + " and ", str(izo))
 
-    varListLines=data[ivb:izo]
-    nV=len(varListLines)
-    varList=[]
-    iX=-1
-    iY=-1
+    varListLines = data[ivb:izo]
+    nV = len(varListLines)
+    varList = []
+    iX = -1
+    iY = -1
     for i in range(0, nV):
-        i1=varListLines[i].index('"')+1
-        i2=varListLines[i].rindex('"')
+        i1 = varListLines[i].index('"') + 1
+        i2 = varListLines[i].rindex('"')
         varList.append(varListLines[i][i1:i2])
         if iX == -1:
             try:
-                ifound= varList[i].index(inDepVar)
-                iX=i
+                ifound = varList[i].index(inDepVar)
+                iX = i
             except ValueError:
-                pass   # do nothing
+                pass  # do nothing
         if iY == -1:
             try:
-                ifound= varList[i].index(depVar)
-                iY=i
+                ifound = varList[i].index(depVar)
+                iY = i
             except ValueError:
-                pass   # do nothing
-
-    print('inDepVar: '+inDepVar+' : '+str(iX+1)+' . DepVar: '+depVar+' : '+str(iY+1)+' of '+str(nV)+' variables')
-
-# find out how many nodes
-
-    inodes=stringLocator('Nodes',data,nc,verbose)
+                pass  # do nothing
+
+    print(
+        "inDepVar: "
+        + inDepVar
+        + " : "
+        + str(iX + 1)
+        + " . DepVar: "
+        + depVar
+        + " : "
+        + str(iY + 1)
+        + " of "
+        + str(nV)
+        + " variables"
+    )
+
+    # find out how many nodes
+
+    inodes = stringLocator("Nodes", data, nc, verbose)
     if inodes == -1:
-        raise SystemExit('ERROR: failed to trace nodes in input file')
-
-    i1=data[inodes].index('=')+1
-    i2=data[inodes].index(',')
-    Nodes=int(data[inodes][i1:i2])
-    print('Nodes = ',str(Nodes))
-#
-# now map the whole matrix
-#
-    i1=inodes+3
-    i2=i1+Nodes
-    X=[]; Y=[]
-    for i in range(i1+1, i2):
-        ff=map(float,data[i][1:-1].split(' '))
+        raise SystemExit("ERROR: failed to trace nodes in input file")
+
+    i1 = data[inodes].index("=") + 1
+    i2 = data[inodes].index(",")
+    Nodes = int(data[inodes][i1:i2])
+    print("Nodes = ", str(Nodes))
+    #
+    # now map the whole matrix
+    #
+    i1 = inodes + 3
+    i2 = i1 + Nodes
+    X = []
+    Y = []
+    for i in range(i1 + 1, i2):
+        ff = map(float, data[i][1:-1].split(" "))
         X.append(ff[iX])
         Y.append(ff[iY])
 
-    nP=len(X)
+    nP = len(X)
 
-#------       sorting by X
+    # ------       sorting by X
 
-    ind = lexsort((Y,X))
-    Xs=take(X,ind)
-    Ys=take(Y,ind)
-# write down to a simple 2-columns file
-    foc=open(outFile,'w')
-    fileHeader = '      '+inDepVar+'                     '+depVar
-    foc.write('% '+fileHeader+' \n% -----------------------------------\n%\n')
-    for  i in range(0,nP):
-        Line1=    '   %10.5f    %14.5g  '%(Xs[i],Ys[i])+'  \n'
+    ind = lexsort((Y, X))
+    Xs = take(X, ind)
+    Ys = take(Y, ind)
+    # write down to a simple 2-columns file
+    foc = open(outFile, "w")
+    fileHeader = "      " + inDepVar + "                     " + depVar
+    foc.write("% " + fileHeader + " \n% -----------------------------------\n%\n")
+    for i in range(0, nP):
+        Line1 = "   %10.5f    %14.5g  " % (Xs[i], Ys[i]) + "  \n"
         foc.write(Line1)
     foc.close()
 
+
 #    numpy.plot(Xs,Ys,"-b")
 
 
 #
-def loadArray(Fin,nCol):
-#
-# load a polar-sweep file as an array
-#
-    f=open(Fin,'r')
-    b=f.readlines()
-    n=size(b)
+def loadArray(Fin, nCol):
+    #
+    # load a polar-sweep file as an array
+    #
+    f = open(Fin, "r")
+    b = f.readlines()
+    n = size(b)
     f.close()
-#
-    data=[]
-    nd=0;
-    for i in range(0,n):
-        sline=b[i].replace('   ',' ').replace('  ',' ').replace('  ',' ').replace('  ',' ').strip().split(' ')
-        sv=size(sline)
+    #
+    data = []
+    nd = 0
+    for i in range(0, n):
+        sline = (
+            b[i]
+            .replace("   ", " ")
+            .replace("  ", " ")
+            .replace("  ", " ")
+            .replace("  ", " ")
+            .strip()
+            .split(" ")
+        )
+        sv = size(sline)
         if sv == nCol:
             try:
-                dd=map(float,sline)
+                dd = map(float, sline)
                 data.append(dd)
-                nd=nd+1;
+                nd = nd + 1
             except ValueError:
-                pass # do nothing
-
-    return data,nd
-
-def locateSteps(d,nd,nCol):
-#
-# read polarsweep files and identify steps
-#
-    eps=0.001
-    nColD=nCol-2  # cxbase and quality are not checked
-    a=array(d)
-    dx=diff(a[:,0],n=1,axis=0)
-    nStairs=[]
-    for ic in range(1,nColD):
-        dy=diff(a[:,ic],n=1,axis=0)
-        dydx=dy/dx
-        adydx=abs(dydx)
-        madydx=adydx.mean(axis=0)
-        mmxadydx=max(adydx)
-        mmnadydx=min(adydx)
-        madydx2=(mmxadydx+mmnadydx)/2
-        iic=where(adydx<eps*madydx)
-        iic2=where(adydx<eps*madydx2)
-        nStairs.append(size(iic)+size(iic2))
-
-    nStM=max(nStairs)
+                pass  # do nothing
+
+    return data, nd
+
+
+def locateSteps(d, nd, nCol):
+    #
+    # read polarsweep files and identify steps
+    #
+    eps = 0.001
+    nColD = nCol - 2  # cxbase and quality are not checked
+    a = array(d)
+    dx = diff(a[:, 0], n=1, axis=0)
+    nStairs = []
+    for ic in range(1, nColD):
+        dy = diff(a[:, ic], n=1, axis=0)
+        dydx = dy / dx
+        adydx = abs(dydx)
+        madydx = adydx.mean(axis=0)
+        mmxadydx = max(adydx)
+        mmnadydx = min(adydx)
+        madydx2 = (mmxadydx + mmnadydx) / 2
+        iic = where(adydx < eps * madydx)
+        iic2 = where(adydx < eps * madydx2)
+        nStairs.append(size(iic) + size(iic2))
+
+    nStM = max(nStairs)
     if nStM > 0:
-        fst=open('stairs','w')
-        fst.write('%  \n%     Polara stairs report  \n%  \n')
-        fst.write('%  Note that the identified number might be something between the correct number of stairs \n')
-        fst.write('%   and 2X this number since since 2 criteria are added in the search script \n \n ')
-        Headers=['CX ','CY ','CZ ','Cmx','Cmy','Cmz']
-        for ic in range(0,nColD-1):
-             refLine1=   Headers[ic]+': Number of stairs identified: %i \n '%(nStairs[ic])
-             fst.write(refLine1)
+        fst = open("stairs", "w")
+        fst.write("%  \n%     Polara stairs report  \n%  \n")
+        fst.write(
+            "%  Note that the identified number might be something between the correct number of stairs \n"
+        )
+        fst.write(
+            "%   and 2X this number since since 2 criteria are added in the search script \n \n "
+        )
+        Headers = ["CX ", "CY ", "CZ ", "Cmx", "Cmy", "Cmz"]
+        for ic in range(0, nColD - 1):
+            refLine1 = Headers[ic] + ": Number of stairs identified: %i \n " % (
+                nStairs[ic]
+            )
+            fst.write(refLine1)
 
         fst.close()
-    return nStairs,nStM
+    return nStairs, nStM
+
 
 def find_index(ar, eps):
-#
-# locate array components that are > eps
-#
-    ia=[]
+    #
+    # locate array components that are > eps
+    #
+    ia = []
     for i, v in enumerate(ar):
         if v > eps:
             ia.append(i)
     return ia
 
-def testComponentSum(cbdOutput,verbose):
-#
-# check cbd summation
-#
 
-    coeffNames=['Cfx','Cfy','Cfz','Cmx','Cmy','Cmz']
+def testComponentSum(cbdOutput, verbose):
+    #
+    # check cbd summation
+    #
+
+    coeffNames = ["Cfx", "Cfy", "Cfz", "Cmx", "Cmy", "Cmz"]
     try:
-        fd=open(cbdOutput,'r');
-        d=fd.readlines()
-        nd=size(d)
+        fd = open(cbdOutput, "r")
+        d = fd.readlines()
+        nd = size(d)
         fd.close()
         if verbose:
-            print('CBD file '+cbdOutput+' loaded by testComponentSum')
+            print("CBD file " + cbdOutput + " loaded by testComponentSum")
 
     except IOError:
-        raise SystemExit('testComponentSum: Failed to find file '+cbdOutput)
-
-# now read the numerical values from the cdb file
-
-    data,nd=loadArray(cbdOutput,6)
-# transpose the array
-    td=zip(*data)
-# now check correct som for each variable
-    eps=0.01
-    errorA=[]
-    sumD=[]
-    for i in range(0,6):
-        fsumD=sum(td[i][:-1])
+        raise SystemExit("testComponentSum: Failed to find file " + cbdOutput)
+
+    # now read the numerical values from the cdb file
+
+    data, nd = loadArray(cbdOutput, 6)
+    # transpose the array
+    td = zip(*data)
+    # now check correct som for each variable
+    eps = 0.01
+    errorA = []
+    sumD = []
+    for i in range(0, 6):
+        fsumD = sum(td[i][:-1])
         sumD.append(fsumD)
-        if abs(td[i][nd-1]) > eps:
-            error=abs((fsumD-td[i][nd-1])/td[i][nd-1])
+        if abs(td[i][nd - 1]) > eps:
+            error = abs((fsumD - td[i][nd - 1]) / td[i][nd - 1])
         else:
-            error=0
+            error = 0
         errorA.append(error)
 
-    iErr=find_index(errorA, 0.005)
-    nER=size(iErr)
+    iErr = find_index(errorA, 0.005)
+    nER = size(iErr)
     if nER > 0:
-        print('testComponentSum: Error is components sumation in file '+cbdOutput)
-        for i in range(0,nER):
-            print('Error found in '+coeffNames[iErr[i]]+' Error = '+str(100*errorA[iErr[i]])+' %')
-
-        corrDataLine='  %12.5e  %12.5e  %12.5e  %12.5e  %12.5e  %12.5e  '%(sumD[0],sumD[1],
-                                                                           sumD[2],sumD[3],sumD[4],sumD[5])
+        print("testComponentSum: Error is components sumation in file " + cbdOutput)
+        for i in range(0, nER):
+            print(
+                "Error found in "
+                + coeffNames[iErr[i]]
+                + " Error = "
+                + str(100 * errorA[iErr[i]])
+                + " %"
+            )
+
+        corrDataLine = "  %12.5e  %12.5e  %12.5e  %12.5e  %12.5e  %12.5e  " % (
+            sumD[0],
+            sumD[1],
+            sumD[2],
+            sumD[3],
+            sumD[4],
+            sumD[5],
+        )
     else:
-        corrDataLine=' '
-    return nER,corrDataLine
+        corrDataLine = " "
+    return nER, corrDataLine
+
 
-def retreiveNumPar(ctrl,nc,keyWord,parType,verbose):
+def retreiveNumPar(ctrl, nc, keyWord, parType, verbose):
     # get the parameter from the control file. Set it to unity if not found
     # parType: 1  -> integer   2 -> float
-#
-    ipar = parLocator(keyWord,ctrl,nc,-1,verbose)
+    #
+    ipar = parLocator(keyWord, ctrl, nc, -1, verbose)
     if ipar == -1:
- #  default value
+        #  default value
         if parType == 1:
             parVal = 1
         else:
             parVal = 1.0
     else:
-        PARLine=ctrl[ipar]
-        icol=PARLine.index(':')
+        PARLine = ctrl[ipar]
+        icol = PARLine.index(":")
         if parType == 1:
-            parVal= int(PARLine[icol+1:])
+            parVal = int(PARLine[icol + 1 :])
         else:
-            parVal=float(PARLine[icol+1:])
+            parVal = float(PARLine[icol + 1 :])
     return parVal
 
+
 # -----------------------------------------------------
 
-def loadData(filename,delim):
-# read a 2D data from a file, separated by delim
-# (may be , (comma) or ' ' (space )
-#
-# do array(dout)  (in calling) to obtain result as an array (numpy imported)
-# dout=loadData(filename,delim)
-# v=array(dout)
+
+def loadData(filename, delim):
+    # read a 2D data from a file, separated by delim
+    # (may be , (comma) or ' ' (space )
+    #
+    # do array(dout)  (in calling) to obtain result as an array (numpy imported)
+    # dout=loadData(filename,delim)
+    # v=array(dout)
 
     import csv
-#    import numpy
 
-    data=[]
-    with open(filename, 'rb') as f:
-#-avoid NULL  error
+    #    import numpy
 
-        reader = csv.reader((line.replace('\0','').replace('   ',' ').replace('  ',' ').strip() for line in f),delimiter=delim)
+    data = []
+    with open(filename, "rb") as f:
+        # -avoid NULL  error
 
-        data=[' ']
+        reader = csv.reader(
+            (
+                line.replace("\0", "").replace("   ", " ").replace("  ", " ").strip()
+                for line in f
+            ),
+            delimiter=delim,
+        )
+
+        data = [" "]
         for row in reader:
             try:
 
                 data.append(map(float, row))
             except ValueError:
-                print('Line doesnt match map float: ')
+                print("Line doesnt match map float: ")
                 print(row)
     # check square matrix
-    N1=len(data[0])
-    dout=[]
-    for i in range(1,len(data)):
+    N1 = len(data[0])
+    dout = []
+    for i in range(1, len(data)):
         if N1 <= 1:
-            N1=len(data[i])
-        if len(data[i]) != N1 :
-            print('WARNING: Line '+str(i)+': size does not match. Skipped')
+            N1 = len(data[i])
+        if len(data[i]) != N1:
+            print("WARNING: Line " + str(i) + ": size does not match. Skipped")
         else:
             dout.append(data[i])
 
-    #adout=array(dout)
+    # adout=array(dout)
 
     return dout
-
-
-
diff --git a/SU2_PY/SU2/util/switch.py b/SU2_PY/SU2/util/switch.py
index b42eaf6e9dd..821b6568a67 100644
--- a/SU2_PY/SU2/util/switch.py
+++ b/SU2_PY/SU2/util/switch.py
@@ -1,35 +1,36 @@
 # -------------------------------------------------------------------
 #  Switch Class
-# -------------------------------------------------------------------  
+# -------------------------------------------------------------------
 # source: Brian Beck, PSF License, ActiveState Code
 #         http://code.activestate.com/recipes/410692/
 
+
 class switch(object):
-    """ Readable switch construction
-    
-        Example:
-        
-        c = 'z'
-        for case in switch(c):
-            if case('a'): pass # only necessary if the rest of the suite is empty
-            if case('b'): pass
-            # ...
-            if case('y'): pass
-            if case('z'):
-                print("c is lowercase!")
-                break
-            if case('A'): pass
-            # ...
-            if case('Z'):
-                print("c is uppercase!")
-                break
-            if case(): # default
-                print("I dunno what c was!")
-        
-        source: Brian Beck, PSF License, ActiveState Code
-        http://code.activestate.com/recipes/410692/
+    """Readable switch construction
+
+    Example:
+
+    c = 'z'
+    for case in switch(c):
+        if case('a'): pass # only necessary if the rest of the suite is empty
+        if case('b'): pass
+        # ...
+        if case('y'): pass
+        if case('z'):
+            print("c is lowercase!")
+            break
+        if case('A'): pass
+        # ...
+        if case('Z'):
+            print("c is uppercase!")
+            break
+        if case(): # default
+            print("I dunno what c was!")
+
+    source: Brian Beck, PSF License, ActiveState Code
+    http://code.activestate.com/recipes/410692/
     """
-    
+
     def __init__(self, value):
         self.value = value
         self.fall = False
@@ -38,15 +39,16 @@ def __iter__(self):
         """Return the match method once, then stop"""
         yield self.match
         raise StopIteration
-    
+
     def match(self, *args):
         """Indicate whether or not to enter a case suite"""
         if self.fall or not args:
             return True
-        elif self.value in args: 
+        elif self.value in args:
             self.fall = True
             return True
         else:
             return False
-        
+
+
 #: class switch()
diff --git a/SU2_PY/SU2/util/which.py b/SU2_PY/SU2/util/which.py
index 512c7e954e1..115b7905a88 100644
--- a/SU2_PY/SU2/util/which.py
+++ b/SU2_PY/SU2/util/which.py
@@ -28,14 +28,15 @@
 
 import os
 
+
 def which(program):
-    """ which(program_name)
-        finds the location of the program_name if it is on PATH
-        returns None if program cannot be found
-        does not test for .exe extension on windows
+    """which(program_name)
+    finds the location of the program_name if it is on PATH
+    returns None if program cannot be found
+    does not test for .exe extension on windows
 
-        original source:
-        http://stackoverflow.com/questions/377017/test-if-executable-exists-in-python
+    original source:
+    http://stackoverflow.com/questions/377017/test-if-executable-exists-in-python
     """
 
     fpath, fname = os.path.split(program)
@@ -45,15 +46,13 @@ def which(program):
     else:
         for path in os.environ["PATH"].split(os.pathsep):
             path = path.strip('"')
-            for ext in ['','.exe','.bat']:
-                exe_file = os.path.join(path, (program+ext))
+            for ext in ["", ".exe", ".bat"]:
+                exe_file = os.path.join(path, (program + ext))
                 if is_exe(exe_file):
                     return exe_file
 
     return None
 
+
 def is_exe(fpath):
     return os.path.isfile(fpath) and os.access(fpath, os.X_OK)
-
-
-
diff --git a/SU2_PY/SU2_CFD.py b/SU2_PY/SU2_CFD.py
index 22e58169db8..39c0eab38fb 100755
--- a/SU2_PY/SU2_CFD.py
+++ b/SU2_PY/SU2_CFD.py
@@ -30,85 +30,147 @@
 # ----------------------------------------------------------------------
 
 from __future__ import division, print_function, absolute_import
-from optparse import OptionParser	# use a parser for configuration
-import SU2				# imports SU2 python tools
-import pysu2			# imports the SU2 wrapped module
+from optparse import OptionParser  # use a parser for configuration
+import SU2  # imports SU2 python tools
+import pysu2  # imports the SU2 wrapped module
 
 # -------------------------------------------------------------------
 #  Main
 # -------------------------------------------------------------------
 
+
 def main():
 
-  # Command line options
-  parser=OptionParser()
-  parser.add_option("-f", "--file", dest="filename", help="Read config from FILE", metavar="FILE")
-  parser.add_option("--nDim", dest="nDim", default=2, help="Define the number of DIMENSIONS",
-                    metavar="DIMENSIONS")
-  parser.add_option("--nZone", dest="nZone", default=1, help="Define the number of ZONES", metavar="NZONE")
-  parser.add_option("--parallel", action="store_true",
-                    help="Specify if we need to initialize MPI", dest="with_MPI", default=False)
-  parser.add_option("--fsi", dest="fsi", default="False", help="Launch the FSI driver", metavar="FSI")
-  parser.add_option("--fem", dest="fem", default="False", help="Launch the FEM driver (General driver)", metavar="FEM")
-  parser.add_option("--harmonic_balance", dest="harmonic_balance", default="False",
-                    help="Launch the Harmonic Balance (HB) driver", metavar="HB")
-  parser.add_option("--poisson_equation", dest="poisson_equation", default="False",
-                    help="Launch the poisson equation driver (General driver)", metavar="POIS_EQ")
-  parser.add_option("--wave_equation", dest="wave_equation", default="False",
-                    help="Launch the wave equation driver (General driver)", metavar="WAVE_EQ")
-  parser.add_option("--heat_equation", dest="heat_equation", default="False",
-                    help="Launch the heat equation driver (General driver)", metavar="HEAT_EQ")
-
-  (options, args) = parser.parse_args()
-  options.nDim  = int( options.nDim )
-  options.nZone = int( options.nZone )
-  options.fsi = options.fsi.upper() == 'TRUE'
-  options.fem = options.fem.upper() == 'TRUE'
-  options.harmonic_balance = options.harmonic_balance.upper() == 'TRUE'
-  options.poisson_equation = options.poisson_equation.upper() == 'TRUE'
-  options.wave_equation    = options.wave_equation.upper()    == 'TRUE'
-  options.heat_equation    = options.heat_equation.upper()    == 'TRUE'
-
-  if options.filename == None:
-    raise Exception("No config file provided. Use -f flag")
-
-  if options.with_MPI == True:
-    from mpi4py import MPI			# use mpi4py for parallel run (also valid for serial)
-    comm = MPI.COMM_WORLD
-  else:
-    comm = 0
-
-  # Initialize the corresponding driver of SU2, this includes solver preprocessing
-  try:
-    if (options.nZone == 1) and ( options.fem or options.poisson_equation or options.wave_equation or options.heat_equation ):
-      SU2Driver = pysu2.CSinglezoneDriver(options.filename, options.nZone, comm);
-    elif options.harmonic_balance:
-      SU2Driver = pysu2.CHBDriver(options.filename, options.nZone, comm);
-    elif (options.nZone >= 2):
-      SU2Driver = pysu2.CMultizoneDriver(options.filename, options.nZone, comm);
-    else:
-      SU2Driver = pysu2.CSinglezoneDriver(options.filename, options.nZone, comm);
-  except TypeError as exception:
-    print('A TypeError occured in pysu2.CDriver : ',exception)
+    # Command line options
+    parser = OptionParser()
+    parser.add_option(
+        "-f", "--file", dest="filename", help="Read config from FILE", metavar="FILE"
+    )
+    parser.add_option(
+        "--nDim",
+        dest="nDim",
+        default=2,
+        help="Define the number of DIMENSIONS",
+        metavar="DIMENSIONS",
+    )
+    parser.add_option(
+        "--nZone",
+        dest="nZone",
+        default=1,
+        help="Define the number of ZONES",
+        metavar="NZONE",
+    )
+    parser.add_option(
+        "--parallel",
+        action="store_true",
+        help="Specify if we need to initialize MPI",
+        dest="with_MPI",
+        default=False,
+    )
+    parser.add_option(
+        "--fsi",
+        dest="fsi",
+        default="False",
+        help="Launch the FSI driver",
+        metavar="FSI",
+    )
+    parser.add_option(
+        "--fem",
+        dest="fem",
+        default="False",
+        help="Launch the FEM driver (General driver)",
+        metavar="FEM",
+    )
+    parser.add_option(
+        "--harmonic_balance",
+        dest="harmonic_balance",
+        default="False",
+        help="Launch the Harmonic Balance (HB) driver",
+        metavar="HB",
+    )
+    parser.add_option(
+        "--poisson_equation",
+        dest="poisson_equation",
+        default="False",
+        help="Launch the poisson equation driver (General driver)",
+        metavar="POIS_EQ",
+    )
+    parser.add_option(
+        "--wave_equation",
+        dest="wave_equation",
+        default="False",
+        help="Launch the wave equation driver (General driver)",
+        metavar="WAVE_EQ",
+    )
+    parser.add_option(
+        "--heat_equation",
+        dest="heat_equation",
+        default="False",
+        help="Launch the heat equation driver (General driver)",
+        metavar="HEAT_EQ",
+    )
+
+    (options, args) = parser.parse_args()
+    options.nDim = int(options.nDim)
+    options.nZone = int(options.nZone)
+    options.fsi = options.fsi.upper() == "TRUE"
+    options.fem = options.fem.upper() == "TRUE"
+    options.harmonic_balance = options.harmonic_balance.upper() == "TRUE"
+    options.poisson_equation = options.poisson_equation.upper() == "TRUE"
+    options.wave_equation = options.wave_equation.upper() == "TRUE"
+    options.heat_equation = options.heat_equation.upper() == "TRUE"
+
+    if options.filename == None:
+        raise Exception("No config file provided. Use -f flag")
+
     if options.with_MPI == True:
-      print('ERROR : You are trying to initialize MPI with a serial build of the wrapper. Please, remove the --parallel option that is incompatible with a serial build.')
+        from mpi4py import MPI  # use mpi4py for parallel run (also valid for serial)
+
+        comm = MPI.COMM_WORLD
     else:
-      print('ERROR : You are trying to launch a computation without initializing MPI but the wrapper has been built in parallel. Please add the --parallel option in order to initialize MPI for the wrapper.')
-    return
+        comm = 0
+
+    # Initialize the corresponding driver of SU2, this includes solver preprocessing
+    try:
+        if (options.nZone == 1) and (
+            options.fem
+            or options.poisson_equation
+            or options.wave_equation
+            or options.heat_equation
+        ):
+            SU2Driver = pysu2.CSinglezoneDriver(options.filename, options.nZone, comm)
+        elif options.harmonic_balance:
+            SU2Driver = pysu2.CHBDriver(options.filename, options.nZone, comm)
+        elif options.nZone >= 2:
+            SU2Driver = pysu2.CMultizoneDriver(options.filename, options.nZone, comm)
+        else:
+            SU2Driver = pysu2.CSinglezoneDriver(options.filename, options.nZone, comm)
+    except TypeError as exception:
+        print("A TypeError occured in pysu2.CDriver : ", exception)
+        if options.with_MPI == True:
+            print(
+                "ERROR : You are trying to initialize MPI with a serial build of the wrapper. Please, remove the --parallel option that is incompatible with a serial build."
+            )
+        else:
+            print(
+                "ERROR : You are trying to launch a computation without initializing MPI but the wrapper has been built in parallel. Please add the --parallel option in order to initialize MPI for the wrapper."
+            )
+        return
+
+    # Launch the solver for the entire computation
+    SU2Driver.StartSolver()
 
-  # Launch the solver for the entire computation
-  SU2Driver.StartSolver()
+    # Postprocess the solver and exit cleanly
+    SU2Driver.Postprocessing()
 
-  # Postprocess the solver and exit cleanly
-  SU2Driver.Postprocessing()
+    if SU2Driver != None:
+        del SU2Driver
 
-  if SU2Driver != None:
-    del SU2Driver
 
 # -------------------------------------------------------------------
 #  Run Main Program
 # -------------------------------------------------------------------
 
 # this is only accessed if running from command prompt
-if __name__ == '__main__':
+if __name__ == "__main__":
     main()
diff --git a/SU2_PY/SU2_Nastran/pysu2_nastran.py b/SU2_PY/SU2_Nastran/pysu2_nastran.py
index 216bc22740f..e629d3d6d5a 100644
--- a/SU2_PY/SU2_Nastran/pysu2_nastran.py
+++ b/SU2_PY/SU2_Nastran/pysu2_nastran.py
@@ -37,1007 +37,1142 @@
 #  Config class
 # ----------------------------------------------------------------------
 
-class ImposedMotionClass:
-
-  def __init__(self,time0,typeOfMotion,parameters,mode):
-
-    self.time0 = time0
-    self.typeOfMotion = typeOfMotion
-    self.mode = mode
-
-    self.amplitude = parameters["AMPLITUDE"]
-    self.timeStart = parameters["TIME_START"]
-    if "TIME_STOP" in parameters.keys():
-      self.timeStop  = parameters["TIME_STOP"]
-    else:
-      self.timeStop = inf
-
-    if self.typeOfMotion == "SINUSOIDAL":
-      self.bias = parameters["BIAS"]
-      self.frequency = parameters["FREQUENCY"]
-
-    elif self.typeOfMotion == "BLENDED_STEP":
-      self.kmax = parameters["K_MAX"]
-      self.vinf = parameters["V_INF"]
-      self.lref = parameters["L_REF"]
-      self.tmax = 2*pi/self.kmax*self.lref/self.vinf
-      self.omega0 = 1/2*self.kmax
-
-    else:
-      raise Exception('Imposed function {} not found, please implement it in pysu2_nastran.py'.format(self.tipo))
 
+class ImposedMotionClass:
+    def __init__(self, time0, typeOfMotion, parameters, mode):
 
-  def GetDispl(self,time):
-    time = time - self.time0 - self.timeStart
-    if self.typeOfMotion == "SINUSOIDAL":
-      if (time < 0.0) or (time > self.timeStop):
-        return 0.0
-      return self.bias+self.amplitude*sin(2*pi*self.frequency*time)
-
-    if self.typeOfMotion == "BLENDED_STEP":
-      if (time < 0.0) or (time > self.timeStop):
-        return 0.0
-      if time < self.tmax:
-        return self.amplitude/2.0*(1.0-cos(self.omega0*time*self.vinf/self.lref))
-      return self.amplitude
-
-
-  def GetVel(self,time):
-    time = time - self.time0 - self.timeStart
-
-    if self.typeOfMotion == "SINUSOIDAL":
-      if (time < 0.0) or (time > self.timeStop):
-        return 0.0
-      return self.amplitude*cos(2*pi*self.frequency*time)*2*pi*self.frequency
+        self.time0 = time0
+        self.typeOfMotion = typeOfMotion
+        self.mode = mode
 
-    if self.typeOfMotion == "BLENDED_STEP":
-      if (time < 0.0) or (time > self.timeStop):
-        return 0.0
-      if time < self.tmax:
-        return self.amplitude/2.0*sin(self.omega0*time*self.vinf/self.lref)*(self.omega0*self.vinf/self.lref)
-      return 0.0
+        self.amplitude = parameters["AMPLITUDE"]
+        self.timeStart = parameters["TIME_START"]
+        if "TIME_STOP" in parameters.keys():
+            self.timeStop = parameters["TIME_STOP"]
+        else:
+            self.timeStop = inf
 
-  def GetAcc(self,time):
-    time = time - self.time0 - self.timeStart
+        if self.typeOfMotion == "SINUSOIDAL":
+            self.bias = parameters["BIAS"]
+            self.frequency = parameters["FREQUENCY"]
 
-    if self.typeOfMotion == "SINUSOIDAL":
-      if (time < 0.0) or (time > self.timeStop):
-        return 0.0
-      return -self.amplitude*sin(2*pi*self.frequency*time)*(2*pi*self.frequency)**2
+        elif self.typeOfMotion == "BLENDED_STEP":
+            self.kmax = parameters["K_MAX"]
+            self.vinf = parameters["V_INF"]
+            self.lref = parameters["L_REF"]
+            self.tmax = 2 * pi / self.kmax * self.lref / self.vinf
+            self.omega0 = 1 / 2 * self.kmax
 
-    if self.typeOfMotion == "BLENDED_STEP":
-      if (time < 0.0) or (time > self.timeStop):
-        return 0.0
-      if time < self.tmax:
-        return self.amplitude/2.0*cos(self.omega0*time*self.vinf/self.lref)*(self.omega0*self.vinf/self.lref)**2
-      return 0.0
+        else:
+            raise Exception(
+                "Imposed function {} not found, please implement it in pysu2_nastran.py".format(
+                    self.tipo
+                )
+            )
+
+    def GetDispl(self, time):
+        time = time - self.time0 - self.timeStart
+        if self.typeOfMotion == "SINUSOIDAL":
+            if (time < 0.0) or (time > self.timeStop):
+                return 0.0
+            return self.bias + self.amplitude * sin(2 * pi * self.frequency * time)
+
+        if self.typeOfMotion == "BLENDED_STEP":
+            if (time < 0.0) or (time > self.timeStop):
+                return 0.0
+            if time < self.tmax:
+                return (
+                    self.amplitude
+                    / 2.0
+                    * (1.0 - cos(self.omega0 * time * self.vinf / self.lref))
+                )
+            return self.amplitude
+
+    def GetVel(self, time):
+        time = time - self.time0 - self.timeStart
+
+        if self.typeOfMotion == "SINUSOIDAL":
+            if (time < 0.0) or (time > self.timeStop):
+                return 0.0
+            return (
+                self.amplitude
+                * cos(2 * pi * self.frequency * time)
+                * 2
+                * pi
+                * self.frequency
+            )
+
+        if self.typeOfMotion == "BLENDED_STEP":
+            if (time < 0.0) or (time > self.timeStop):
+                return 0.0
+            if time < self.tmax:
+                return (
+                    self.amplitude
+                    / 2.0
+                    * sin(self.omega0 * time * self.vinf / self.lref)
+                    * (self.omega0 * self.vinf / self.lref)
+                )
+            return 0.0
+
+    def GetAcc(self, time):
+        time = time - self.time0 - self.timeStart
+
+        if self.typeOfMotion == "SINUSOIDAL":
+            if (time < 0.0) or (time > self.timeStop):
+                return 0.0
+            return (
+                -self.amplitude
+                * sin(2 * pi * self.frequency * time)
+                * (2 * pi * self.frequency) ** 2
+            )
+
+        if self.typeOfMotion == "BLENDED_STEP":
+            if (time < 0.0) or (time > self.timeStop):
+                return 0.0
+            if time < self.tmax:
+                return (
+                    self.amplitude
+                    / 2.0
+                    * cos(self.omega0 * time * self.vinf / self.lref)
+                    * (self.omega0 * self.vinf / self.lref) ** 2
+                )
+            return 0.0
 
 
 class RefSystem:
+    def __init__(self):
+        self.CID = 0
+        self.RID = 0
+        self.Origin = np.array([[0.0], [0.0], [0.0]])
+        self.Rot = np.array([[0.0, 0.0, 0.0], [0.0, 0.0, 0.0], [0.0, 0.0, 0.0]])
 
-  def __init__(self):
-    self.CID = 0
-    self.RID = 0
-    self.Origin = np.array([[0.],[0.],[0.]])
-    self.Rot = np.array([[0.,0.,0.],[0.,0.,0.],[0.,0.,0.]])
+    def SetOrigin(self, A):
+        AX, AY, AZ = A
+        self.Origin[0] = AX
+        self.Origin[1] = AY
+        self.Origin[2] = AZ
 
-  def SetOrigin(self,A):
-    AX , AY , AZ = A
-    self.Origin[0] =  AX
-    self.Origin[1] =  AY
-    self.Origin[2] =  AZ
+    def SetRotMatrix(self, x, y, z):
+        self.Rot = np.array(
+            [[x[0], y[0], z[0]], [x[1], y[1], z[1]], [x[2], y[2], z[2]]]
+        )
 
-  def SetRotMatrix(self,x,y,z):
-    self.Rot = np.array([[x[0],y[0],z[0]],[x[1],y[1],z[1]],[x[2],y[2],z[2]]])
+    def SetCID(self, CID):
+        self.CID = CID
 
-  def SetCID(self,CID):
-    self.CID = CID
+    def SetRID(self, RID):
+        self.RID = RID
 
-  def SetRID(self,RID):
-    self.RID = RID
+    def GetOrigin(self):
+        return self.Origin
 
-  def GetOrigin(self):
-    return self.Origin
+    def GetRotMatrix(self):
+        return self.Rot
 
-  def GetRotMatrix(self):
-    return self.Rot
+    def GetRID(self):
+        return self.RID
 
-  def GetRID(self):
-    return self.RID
+    def GetCID(self):
+        return self.CID
 
-  def GetCID(self):
-    return self.CID
 
 class Point:
-  """
-  Class containing data regarding all the structural nodes.
-  Coord0: Coordinates at the initial time iteration.
-  Coord: Coordinates at the current time iteration.
-  Coord_n: Coordinates at the previous time iteration.
-  Vel: Velocity at the current time iteration.
-  Vel_n: Velocity at the previous time iteration.
-  Force: Nodal force provided by the aerodynamics.
-  ID: ID of the node.
-  CP: Coordinate system definition of the position.
-  CD: Coordinate system definition of the output coming from Nastran.
-  """
-
-  def __init__(self):
-    self.Coord0 = np.zeros((3,1))
-    self.Coord = np.zeros((3,1))
-    self.Coord_n = np.zeros((3,1))
-    self.Vel = np.zeros((3,1))
-    self.Vel_n = np.zeros((3,1))
-    self.Force = np.zeros((3,1))
-    self.ID = 0
-    self.CP = 0
-    self.CD = 0
-
-  def GetCoord0(self):
-    return self.Coord0
-
-  def GetCoord(self):
-    return self.Coord
-
-  def GetCoord_n(self):
-    return self.Coord_n
-
-  def GetVel(self):
-    return self.Vel
-
-  def GetVel_n(self):
-    return self.Vel_n
-
-  def GetForce(self):
-    return self.Force
-
-  def GetID(self):
-    return self.ID
-
-  def GetCP(self):
-    return self.CP
-
-  def GetCD(self):
-    return self.CD
-
-  def SetCoord0(self, val_Coord):
-    x, y, z = val_Coord
-    self.Coord0[0] = x
-    self.Coord0[1] = y
-    self.Coord0[2] = z
-
-  def SetCoord(self, val_Coord):
-    x, y, z = val_Coord
-    self.Coord[0] = x
-    self.Coord[1] = y
-    self.Coord[2] = z
-
-  def SetCoord_n(self, val_Coord):
-    x, y, z = val_Coord
-    self.Coord_n[0] = x
-    self.Coord_n[1] = y
-    self.Coord_n[2] = z
-
-  def SetVel(self, val_Vel):
-    vx, vy, vz = val_Vel
-    self.Vel[0] = vx
-    self.Vel[1] = vy
-    self.Vel[2] = vz
-
-  def SetVel_n(self, val_Vel):
-    vx, vy, vz = val_Vel
-    self.Vel_n[0] = vx
-    self.Vel_n[1] = vy
-    self.Vel_n[2] = vz
-
-  def SetForce(self, val_Force):
-    fx, fy, fz = val_Force
-    self.Force[0] = fx
-    self.Force[1] = fy
-    self.Force[2] = fz
-
-  def SetID(self, ID):
-    self.ID = ID
-
-  def SetCP(self,CP):
-    self.CP = CP
-
-  def SetCD(self,CD):
-    self.CD = CD
-
-  def updateCoordVel(self):
-    self.Coord_n = np.copy(self.Coord)
-    self.Vel_n = np.copy(self.Vel)
-
-class Solver:
-  """
-  Structural solver main class.
-  It contains all the required methods for the coupling with SU2.
-  """
-
-  def __init__(self, config_fileName, ImposedMotion):
     """
-    Constructor of the structural solver class.
+    Class containing data regarding all the structural nodes.
+    Coord0: Coordinates at the initial time iteration.
+    Coord: Coordinates at the current time iteration.
+    Coord_n: Coordinates at the previous time iteration.
+    Vel: Velocity at the current time iteration.
+    Vel_n: Velocity at the previous time iteration.
+    Force: Nodal force provided by the aerodynamics.
+    ID: ID of the node.
+    CP: Coordinate system definition of the position.
+    CD: Coordinate system definition of the output coming from Nastran.
     """
 
-    self.Config_file = config_fileName
-    self.Config = {}
-
-    print("\n")
-    print(" Configuring the structural tester solver for FSI simulation ".center(80,"-"))
-    self.__readConfig()
-
-    self.Mesh_file = self.Config['MESH_FILE']
-    self.Punch_file = self.Config['PUNCH_FILE']
-    self.FSI_marker = self.Config['MOVING_MARKER']
-    self.Unsteady = (self.Config['TIME_MARCHING']=="YES")
-    self.ImposedMotion = ImposedMotion
-    if self.Unsteady:
-      print('Dynamic computation.')
-    self.nDof = self.Config['NMODES']
-    print("Reading number of modes from file")
-
-
-    # Structural properties
-    print("Reading the modal and stiffnes matrix from file")
-    self.ModalDamping = self.Config['MODAL_DAMPING']
-    if self.ModalDamping == 0:
-        print("The structural model is undamped")
-    else:
-        print("Assuming {}% of modal damping".format(self.ModalDamping*100))
-
-    self.deltaT = self.Config['DELTA_T']
-    self.rhoAlphaGen = self.Config['RHO']
-
-    self.nPoint = int()
-    self.nMarker = int()
-    self.nRefSys = int()
-    self.node = []
-    self.markers = {}
-    self.refsystems = []
-    self.ImposedMotionToSet = True
-    self.ImposedMotionFunction = []
-
-    print("\n")
-    print(" Reading the mesh ".center(80,"-"))
-    self.__readNastranMesh()
-
-    print("\n")
-    print(" Creating the structural model ".center(80,"-"))
-    self.__setStructuralMatrices()
-
-    print("\n")
-    print(" Setting the integration parameters ".center(80,"-"))
-    self.__setIntegrationParameters()
-    self.__setInitialConditions()
-
-    # Prepare the output file
-    if self.Config["RESTART_SOL"]=="NO":
-      histFile = open('StructHistoryModal.dat', "w")
-      header = 'Time\t' + 'Time Iteration\t' + 'FSI Iteration\t'
-      for imode in range(self.nDof):
-        header = header + 'q' + str(imode+1) + '\t' + 'qdot' + str(imode+1) + '\t' + 'qddot' + str(imode+1) + '\t'
-      header = header + '\n'
-      histFile.write(header)
-      histFile.close()
-    else:
-      self.__setRestart()
-
-  def __readConfig(self):
-    """
-    This methods obtains the configuration options from the structural solver input
-    file.
-    """
-
-    with open(self.Config_file) as configfile:
-      while 1:
-        line = configfile.readline()
-        if not line:
-          break
-
-        # remove line returns
-        line = line.strip('\r\n')
-        # make sure it has useful data
-        if (not "=" in line) or (line[0] == '%'):
-          continue
-        # split across equal sign
-        line = line.split("=",1)
-        this_param = line[0].strip()
-        this_value = line[1].strip()
-
-        #integer values
-        if (this_param == "NMODES") or \
-           (this_param == "RESTART_ITER"):
-          self.Config[this_param] = int(this_value)
-
-
-        #float values
-        elif (this_param == "DELTA_T") or \
-             (this_param == "MODAL_DAMPING") or \
-             (this_param == "RHO"):
-          self.Config[this_param] = float(this_value)
-
-
-        #string values
-        elif (this_param == "TIME_MARCHING") or \
-             (this_param == "MESH_FILE") or \
-             (this_param == "PUNCH_FILE") or \
-             (this_param == "RESTART_SOL") or \
-             (this_param == "MOVING_MARKER"):
-          self.Config[this_param] = this_value
-
-
-        #lists values
-        elif (this_param == "INITIAL_MODES") or \
-             (this_param == "IMPOSED_MODES") or \
-             (this_param == "IMPOSED_PARAMETERS"):
-          self.Config[this_param] = eval(this_value)
+    def __init__(self):
+        self.Coord0 = np.zeros((3, 1))
+        self.Coord = np.zeros((3, 1))
+        self.Coord_n = np.zeros((3, 1))
+        self.Vel = np.zeros((3, 1))
+        self.Vel_n = np.zeros((3, 1))
+        self.Force = np.zeros((3, 1))
+        self.ID = 0
+        self.CP = 0
+        self.CD = 0
 
+    def GetCoord0(self):
+        return self.Coord0
 
-        else:
-          raise Exception('{} is an invalid option !'.format(this_param))
-
-
-
-  def __readNastranMesh(self):
-      """
-      This method reads the nastran 3D mesh.
-      """
-
-      def nastran_float(s):
-        if s.find('E') == -1:
-          s = s.replace('-','e-')
-          s = s.replace('+','e+')
-          if s[0] == 'e':
-            s = s[1:]
-        return float(s)
-
-      self.nMarker = 0
-      self.nPoint = 0
-      self.nRefSys = 0
-
-      with open(self.Mesh_file,'r') as meshfile:
-        print('Opened mesh file ' + self.Mesh_file + '.')
-        while 1:
-          line = meshfile.readline()
-          if not line:
-            break
-
-          pos = line.find('GRID')
-          if pos  ==  30:
-            line = line.strip('\r\n')
-            self.node.append(Point())
-            line = line[30:]
-            ID = int(line[8:16])
-            CP = self.__checkBlankField(line[16:24])
-            x = nastran_float(line[24:32])
-            y = nastran_float(line[32:40])
-            z = nastran_float(line[40:48])
-            if CP != 0:
-              for iRefSys in range(self.nRefSys):
-                if self.refsystems[iRefSys].GetCID()==CP:
-                  break
-              if self.refsystems[iRefSys].GetCID()!=CP:
-                raise Exception('Definition reference {} system not found'.format(CP))
-              DeltaPos = self.refsystems[iRefSys].GetOrigin()
-              RotatedPos = self.refsystems[iRefSys].GetRotMatrix().dot(np.array([[x],[y],[z]]))
-              x = RotatedPos[0]+DeltaPos[0]
-              y = RotatedPos[1]+DeltaPos[1]
-              z = RotatedPos[2]+DeltaPos[2]
-            CD = self.__checkBlankField(line[48:56])
-            self.node[self.nPoint].SetCoord((x,y,z))
-            self.node[self.nPoint].SetID(ID)
-            self.node[self.nPoint].SetCP(CP)
-            self.node[self.nPoint].SetCD(CD)
-            self.node[self.nPoint].SetCoord0((x,y,z))
-            self.node[self.nPoint].SetCoord_n((x,y,z))
-            self.nPoint += 1
-            continue
-
-          pos = line.find('CORD2R')
-          if pos == 30:
-            line = line.strip('\r\n')
-            self.refsystems.append(RefSystem())
-            line = line[30:]
-            CID = int(line[8:16])
-            self.refsystems[self.nRefSys].SetCID(CID)
-            RID = int(line[16:24])
-            if RID!=0:
-              raise Exception('ERROR: Reference system {} must be defined with respect to global reference system'.format(CID))
-            self.refsystems[self.nRefSys].SetRID(RID)
-            AX = nastran_float(line[24:32])
-            AY = nastran_float(line[32:40])
-            AZ = nastran_float(line[40:48])
-            BX = nastran_float(line[48:56])
-            BY = nastran_float(line[56:64])
-            BZ = nastran_float(line[64:72])
-            z_direction = np.array([BX-AX,BY-AY,BZ-AZ])
-            z_direction = z_direction/linalg.norm(z_direction)
-            line = meshfile.readline()
-            line = line.strip('\r\n')
-            line = line[30:]
-            CX = nastran_float(line[8:16])
-            CY = nastran_float(line[16:24])
-            CZ = nastran_float(line[24:32])
-            y_direction = np.cross(z_direction,[CX-AX,CY-AY,CZ-AZ])
-            y_direction = y_direction/linalg.norm(y_direction)
-            x_direction = np.cross(y_direction,z_direction)
-            x_direction = x_direction/linalg.norm(x_direction)
-            self.refsystems[self.nRefSys].SetRotMatrix(x_direction,y_direction,z_direction)
-            self.refsystems[self.nRefSys].SetOrigin((AX,AY,AZ))
-            self.nRefSys += 1
-            continue
-
-          pos = line.find("SET1")
-          if pos == 30:
-              line = line.strip('\r\n')
-              line = line[37:]
-              line = line.split()
-              existValue = True
-              markerTag = line.pop(0)
-              self.markers[markerTag] = []
-              while existValue:
-                  if line[0] == "+":
-                      line = meshfile.readline()
-                      line = line.strip('\r\n')
-                      line = line[37:]
-                      line = line.split()
-                  ID = int(line.pop(0))
-                  for iPoint in range(self.nPoint):
-                      if self.node[iPoint].GetID() == ID:
-                          break
-                  if (iPoint == (self.nPoint-1)) and (self.node[iPoint].GetID() != ID):
-                      raise Exception("Point {} in the set {} was not found in the mesh".format(ID,markerTag))
-                  self.markers[markerTag].append(iPoint)
-                  existValue = len(line)>=1
-              self.nMarker += 1
-              continue
-
-      if not any(self.FSI_marker in key for key in self.markers.keys()):
-          raise Exception("The FSI marker was not found in the available sets")
-
-      self.markers[self.FSI_marker].sort()
-
-      print("Number of points: {}".format(self.nPoint))
-      print("Number of markers: {}".format(self.nMarker))
-      print("Number of reference systems: {}".format(self.nRefSys))
-      print("Moving marker: {}".format(self.FSI_marker))
-      print("Number of points in the moving marker".format(len(self.markers[self.FSI_marker])))
-
-  def __checkBlankField(self, string):
-    """
-    This method considers that Nastran apply 0 when the reference system is not specified
-    """
-
-    if string == ' '*8:
-      return int(0)
-    return int(string)
+    def GetCoord(self):
+        return self.Coord
 
+    def GetCoord_n(self):
+        return self.Coord_n
 
-  def __setStructuralMatrices(self):
-    """
-    This method reads the punch file and obtains the modal shapes and modal stiffnesses.
-    """
-
-    self.M = np.zeros((self.nDof, self.nDof))
-    self.K = np.zeros((self.nDof, self.nDof))
-    self.C = np.zeros((self.nDof, self.nDof))
-
-    self.q = np.zeros((self.nDof, 1))
-    self.qdot = np.zeros((self.nDof, 1))
-    self.qddot = np.zeros((self.nDof, 1))
-    self.a = np.zeros((self.nDof, 1))
-
-    self.q_n = np.zeros((self.nDof, 1))
-    self.qdot_n = np.zeros((self.nDof, 1))
-    self.qddot_n = np.zeros((self.nDof, 1))
-    self.a_n = np.zeros((self.nDof, 1))
-
-    self.F = np.zeros((self.nDof, 1))
-
-    self.Ux = np.zeros((self.nPoint,self.nDof))
-    self.Uy = np.zeros((self.nPoint,self.nDof))
-    self.Uz = np.zeros((self.nPoint,self.nDof))
-
-    with open(self.Punch_file,'r') as punchfile:
-      print('Opened punch file ' + self.Punch_file + '.')
-      while 1:
-        line = punchfile.readline()
-        if not line:
-          break
-
-        pos = line.find('MODE ')
-        if pos != -1:
-          line = line.strip('\r\n').split()
-          n = int(line[5])
-          imode = n-1
-          k_i = float(line[2])
-          self.M[imode][imode] = 1
-          self.K[imode][imode] = k_i
-          w_i = sqrt(k_i)
-          self.C[imode][imode] = 2 * self.ModalDamping * w_i
-          iPoint = 0
-          for indexIter in range(self.nPoint):
-            line = punchfile.readline()
-            line = line.strip('\r\n').split()
-            if line[1]=='G':
-              ux = float(line[2])
-              uy = float(line[3])
-              uz = float(line[4])
-              if self.node[iPoint].GetCD()!=0:
-                for iRefSys in range(self.nRefSys):
-                  if self.refsystems[iRefSys].GetCID()==self.node[iPoint].GetCD():
-                    break
-                if self.refsystems[iRefSys].GetCID()!=self.node[iPoint].GetCD():
-                  raise Exception('Output reference {} system not found'.format(self.node[iPoint].GetCD()))
-                RotatedOutput = self.refsystems[iRefSys].GetRotMatrix().dot(np.array([[ux],[uy],[uz]]))
-                ux = RotatedOutput[0]
-                uy = RotatedOutput[1]
-                uz = RotatedOutput[2]
-              self.Ux[iPoint][imode] = ux
-              self.Uy[iPoint][imode] = uy
-              self.Uz[iPoint][imode] = uz
-              iPoint = iPoint + 1
-              line = punchfile.readline()
-            if line[1]=='S':
-              line = punchfile.readline()
-
-          if n == self.nDof:
-            break
-
-    self.__setNonDiagonalStructuralMatrices()
-
-    self.UxT = self.Ux.transpose()
-    self.UyT = self.Uy.transpose()
-    self.UzT = self.Uz.transpose()
-
-    if n<self.nDof:
-        raise Exception('ERROR: available {} degrees of freedom instead of {} as requested'.format(n,self.nDof))
-    else:
-        print('Using {} degrees of freedom'.format(n))
-
-
-  def __setNonDiagonalStructuralMatrices(self):
-    """
-    This method is part of an advanced feature of this solver that allows to set
-    nondiagonal matrices for the structural modes.
-    """
+    def GetVel(self):
+        return self.Vel
 
-    K_updated = self.__readNonDiagonalMatrix('NDK')
-    M_updated = self.__readNonDiagonalMatrix('NDM')
-    C_updated = self.__readNonDiagonalMatrix('NDC')
-    if K_updated and M_updated and (not C_updated):
-      print('Setting modal damping')
-      self.__setNonDiagonalDamping()
-    elif (not K_updated) and (not M_updated):
-      print('Modal stiffness and mass matrices are diagonal')
-    elif (not K_updated) and M_updated:
-      raise Exception('Non-Diagonal stiffness matrix is missing')
-    elif (not M_updated) and K_updated:
-      raise Exception('Non-Diagonal mass matrix is missing')
-
-  def __readNonDiagonalMatrix(self,keyword):
-    """
-    This method reads from the punch file the definition of nondiagonal structural
-    matrices.
-    """
+    def GetVel_n(self):
+        return self.Vel_n
 
-    matrixUpdated = False
-
-    with open(self.Punch_file,'r') as punchfile:
-
-      while 1:
-        line = punchfile.readline()
-        if not line:
-          break
-
-        pos = line.find(keyword)
-        if pos != -1:
-          while 1:
-            line = punchfile.readline()
-            line = line.strip('\r\n').split()
-            if line[0] != '-CONT-':
-              i = int(line[0])-1
-              j = 0
-              el = line[1:]
-              ne = len(el)
-            elif line[0] == '-CONT-':
-              el = line[1:]
-              ne = len(el)
-            if keyword == 'NDK':
-              self.K[i][j:j+ne] = np.array(el)
-            elif keyword == 'NDM':
-              self.M[i][j:j+ne] = np.array(el)
-            elif keyword == 'NDC':
-              self.C[i][j:j+ne] = np.array(el)
-            j = j+ne
-            if i+1 == self.nDof and j == self.nDof:
-              matrixUpdated = True
-              break
-
-    return matrixUpdated
-
-
-  def __setNonDiagonalDamping(self):
-
-    D , V = linalg.eig(self.K,self.M)
-    D = D.real
-    D = np.sqrt(D)
-    Mmodal = ((V.transpose()).dot(self.M)).dot(V)
-    Mmodal = np.diag(Mmodal)
-    C = 2 * self.ModalDamping * np.multiply(D,Mmodal)
-    C = np.diag(C)
-    Vinv = linalg.inv(V)
-    C = C.dot(Vinv)
-    VinvT = Vinv.transpose()
-    self.C = VinvT.dot(C)
-
-  def __setIntegrationParameters(self):
-    """
-    This method uses the time step size to define the integration parameters.
-    """
+    def GetForce(self):
+        return self.Force
 
-    self.alpha_m = (2.0*self.rhoAlphaGen-1.0)/(self.rhoAlphaGen+1.0)
-    self.alpha_f = (self.rhoAlphaGen)/(self.rhoAlphaGen+1.0)
-    self.gamma = 0.5+self.alpha_f-self.alpha_m
-    self.beta = 0.25*(self.gamma+0.5)**2
+    def GetID(self):
+        return self.ID
 
-    self.gammaPrime = self.gamma/(self.deltaT*self.beta)
-    self.betaPrime = (1.0-self.alpha_m)/((self.deltaT**2)*self.beta*(1.0-self.alpha_f))
+    def GetCP(self):
+        return self.CP
 
-    print('Time integration with the alpha-generalized algorithm.')
-    print('rho : {}'.format(self.rhoAlphaGen))
-    print('alpha_m : {}'.format(self.alpha_m))
-    print('alpha_f : {}'.format(self.alpha_f))
-    print('gamma : {}'.format(self.gamma))
-    print('beta : {}'.format(self.beta))
-    print('gammaPrime : {}'.format(self.gammaPrime))
-    print('betaPrime : {}'.format(self.betaPrime))
+    def GetCD(self):
+        return self.CD
 
-  def __setInitialConditions(self):
-    """
-    This method uses the list of initial modal amplitudes to set the initial conditions
-    """
+    def SetCoord0(self, val_Coord):
+        x, y, z = val_Coord
+        self.Coord0[0] = x
+        self.Coord0[1] = y
+        self.Coord0[2] = z
 
-    print('Setting initial conditions.')
+    def SetCoord(self, val_Coord):
+        x, y, z = val_Coord
+        self.Coord[0] = x
+        self.Coord[1] = y
+        self.Coord[2] = z
 
-    print('Using modal amplitudes from config file')
-    for imode in range(self.nDof):
-        if imode in self.Config["INITIAL_MODES"].keys():
-            self.q[imode] = float(self.Config["INITIAL_MODES"][imode])
-            self.q_n[imode] = float(self.Config["INITIAL_MODES"][imode])
+    def SetCoord_n(self, val_Coord):
+        x, y, z = val_Coord
+        self.Coord_n[0] = x
+        self.Coord_n[1] = y
+        self.Coord_n[2] = z
 
-    RHS = np.zeros((self.nDof,1))
-    RHS += self.F
-    RHS -= self.C.dot(self.qdot)
-    RHS -= self.K.dot(self.q)
-    self.qddot = linalg.solve(self.M, RHS)
-    self.qddot_n = np.copy(self.qddot)
-    self.a = np.copy(self.qddot)
-    self.a_n = np.copy(self.qddot)
+    def SetVel(self, val_Vel):
+        vx, vy, vz = val_Vel
+        self.Vel[0] = vx
+        self.Vel[1] = vy
+        self.Vel[2] = vz
 
-  def __reset(self, vector):
-    """
-    This method set to zero any vector.
-    """
+    def SetVel_n(self, val_Vel):
+        vx, vy, vz = val_Vel
+        self.Vel_n[0] = vx
+        self.Vel_n[1] = vy
+        self.Vel_n[2] = vz
 
-    for ii in range(vector.shape[0]):
-      vector[ii] = 0.0
+    def SetForce(self, val_Force):
+        fx, fy, fz = val_Force
+        self.Force[0] = fx
+        self.Force[1] = fy
+        self.Force[2] = fz
 
-  def __computeInterfacePosVel(self, initialize):
-    """
-    This method uses the mode shapes to compute, based on the modal velocities, the
-    nodal velocities at the interface.
-    """
+    def SetID(self, ID):
+        self.ID = ID
 
-    # Multiply the modal matrices with modal amplitudes
-    X_vel = self.Ux.dot(self.qdot)
-    Y_vel = self.Uy.dot(self.qdot)
-    Z_vel = self.Uz.dot(self.qdot)
+    def SetCP(self, CP):
+        self.CP = CP
 
-    X_disp = self.Ux.dot(self.q)
-    Y_disp = self.Uy.dot(self.q)
-    Z_disp = self.Uz.dot(self.q)
+    def SetCD(self, CD):
+        self.CD = CD
 
-    for iPoint in range(self.nPoint):
-      coord0 = self.node[iPoint].GetCoord0()
-      self.node[iPoint].SetCoord((X_disp[iPoint]+coord0[0],Y_disp[iPoint]+coord0[1],Z_disp[iPoint]+coord0[2]))
-      self.node[iPoint].SetVel((X_vel[iPoint],Y_vel[iPoint],Z_vel[iPoint]))
+    def updateCoordVel(self):
+        self.Coord_n = np.copy(self.Coord)
+        self.Vel_n = np.copy(self.Vel)
 
-      if initialize:
-        self.node[iPoint].SetCoord_n((X_disp[iPoint]+coord0[0],Y_disp[iPoint]+coord0[1],Z_disp[iPoint]+coord0[2]))
-        self.node[iPoint].SetVel_n((X_vel[iPoint],Y_vel[iPoint],Z_vel[iPoint]))
 
-  def __setRestart(self):
+class Solver:
     """
-    This method sets all the variables needed for the correct restart.
+    Structural solver main class.
+    It contains all the required methods for the coupling with SU2.
     """
 
-    #read the Structhistory to obtain the mode amplitudes
-    nM1Set = False
-    nSet = False
-    firstLineRead = False
-    couplingLineRead = False
-
-    with open('StructHistoryModal.dat','r') as file:
-      print('Opened history file StructHistoryModal.dat.')
-      line = file.readline()
-      while 1:
-        line = file.readline()
-        if not line:
-          break
-        line = line.strip('\r\n').split()
-
-        # The old time_0 for imposed motion can either be the first line of the StructHistoryModal, if TimeIterTreshold was -1 (immediate coupling), or the second line. In the former case, time_0 is 0.0, so it is easy to recognize it
-        if not firstLineRead:
-          firstLineRead = True
-          if float(line[0])==0.0:
-            couplingLineRead = True
-            self.timeStartCoupling = 0.0
+    def __init__(self, config_fileName, ImposedMotion):
+        """
+        Constructor of the structural solver class.
+        """
+
+        self.Config_file = config_fileName
+        self.Config = {}
+
+        print("\n")
+        print(
+            " Configuring the structural tester solver for FSI simulation ".center(
+                80, "-"
+            )
+        )
+        self.__readConfig()
+
+        self.Mesh_file = self.Config["MESH_FILE"]
+        self.Punch_file = self.Config["PUNCH_FILE"]
+        self.FSI_marker = self.Config["MOVING_MARKER"]
+        self.Unsteady = self.Config["TIME_MARCHING"] == "YES"
+        self.ImposedMotion = ImposedMotion
+        if self.Unsteady:
+            print("Dynamic computation.")
+        self.nDof = self.Config["NMODES"]
+        print("Reading number of modes from file")
+
+        # Structural properties
+        print("Reading the modal and stiffnes matrix from file")
+        self.ModalDamping = self.Config["MODAL_DAMPING"]
+        if self.ModalDamping == 0:
+            print("The structural model is undamped")
         else:
-          if couplingLineRead:
-            pass
-          else:
-            self.timeStartCoupling = float(line[0])
-            couplingLineRead = True
-
-        if int(line[1])==(self.Config["RESTART_ITER"]-2):
-          index = 0
-          for index_mode in range(self.nDof):
-            self.q[index_mode] = float(line[index+3])
-            self.qdot[index_mode] = float(line[index+4])
-            self.qddot[index_mode] = float(line[index+5])
-            index += 3
-          del index
-          #push back the mode amplitudes velocities and accelerations
-          self.__computeInterfacePosVel(True)
-          self.q_n = np.copy(self.q)
-          self.qdot_n = np.copy(self.qdot)
-          self.qddot_n = np.copy(self.qddot)
-          self.a_n = np.copy(self.a)
-          nM1Set = True
-        if int(line[1])==(self.Config["RESTART_ITER"]-1):
-          index = 0
-          for index_mode in range(self.nDof):
-            self.q[index_mode] = float(line[index+3])
-            self.qdot[index_mode] = float(line[index+4])
-            self.qddot[index_mode] = float(line[index+5])
-            index += 3
-          del index
-          self.__computeInterfacePosVel(False)
-          nSet = True
-          break
-
-    if (not nM1Set) or (not nSet):
-      raise Exception('The restart iteration was not found in the structural history')
-
-
-  def __temporalIteration(self,time):
-    """
-    This method integrates in time the solution.
-    """
-
-    self.__reset(self.q)
-    self.__reset(self.qdot)
-    self.__reset(self.qddot)
-    self.__reset(self.a)
-
-    if not self.ImposedMotion:
-      eps = 1e-6
-
-      self.__SetLoads()
-
-      # Prediction step
-
-      self.a += (self.alpha_f)/(1-self.alpha_m)*self.qddot_n
-      self.a -= (self.alpha_m)/(1-self.alpha_m)*self.a_n
-
-      self.q = np.copy(self.q_n)
-      self.q += self.deltaT*self.qdot_n
-      self.q += (0.5-self.beta)*self.deltaT*self.deltaT*self.a_n
-      self.q += self.deltaT*self.deltaT*self.beta*self.a
-
-      self.qdot = np.copy(self.qdot_n)
-      self.qdot += (1-self.gamma)*self.deltaT*self.a_n
-      self.qdot += self.deltaT*self.gamma*self.a
-
-      # Correction step
-      res = self.__ComputeResidual()
-
-      while linalg.norm(res) >= eps:
-        St = self.__TangentOperator()
-        Deltaq = -1*(linalg.solve(St,res))
-        self.q += Deltaq
-        self.qdot += self.gammaPrime*Deltaq
-        self.qddot += self.betaPrime*Deltaq
-        res = self.__ComputeResidual()
-
-      self.a += (1-self.alpha_f)/(1-self.alpha_m)*self.qddot
-    else:
-      if self.ImposedMotionToSet:
+            print("Assuming {}% of modal damping".format(self.ModalDamping * 100))
+
+        self.deltaT = self.Config["DELTA_T"]
+        self.rhoAlphaGen = self.Config["RHO"]
+
+        self.nPoint = int()
+        self.nMarker = int()
+        self.nRefSys = int()
+        self.node = []
+        self.markers = {}
+        self.refsystems = []
+        self.ImposedMotionToSet = True
+        self.ImposedMotionFunction = []
+
+        print("\n")
+        print(" Reading the mesh ".center(80, "-"))
+        self.__readNastranMesh()
+
+        print("\n")
+        print(" Creating the structural model ".center(80, "-"))
+        self.__setStructuralMatrices()
+
+        print("\n")
+        print(" Setting the integration parameters ".center(80, "-"))
+        self.__setIntegrationParameters()
+        self.__setInitialConditions()
+
+        # Prepare the output file
         if self.Config["RESTART_SOL"] == "NO":
-          # If yes we already set it in the __setRestart function
-          self.timeStartCoupling = time
-        iImposedFunc = 0
-        for imode in self.Config["IMPOSED_MODES"].keys():
-          for isuperposed in range(len(self.Config["IMPOSED_MODES"][imode])):
-            typeOfMotion = self.Config["IMPOSED_MODES"][imode][isuperposed]
-            parameters = self.Config["IMPOSED_PARAMETERS"][imode][isuperposed]
-            self.ImposedMotionFunction.append(ImposedMotionClass(self.timeStartCoupling, typeOfMotion, parameters, imode))
-            iImposedFunc += 1
-        self.ImposedMotionToSet = False
-      for iImposedFunc in range(len(self.ImposedMotionFunction)):
-        imode = self.ImposedMotionFunction[iImposedFunc].mode
-        self.q[imode] += self.ImposedMotionFunction[iImposedFunc].GetDispl(time)
-        self.qdot[imode] += self.ImposedMotionFunction[iImposedFunc].GetVel(time)
-        self.qddot[imode] += self.ImposedMotionFunction[iImposedFunc].GetAcc(time)
-      self.a = np.copy(self.qddot)
-
-
-  def __SetLoads(self):
-    """
-    This method uses the nodal forces and the mode shapes to obtain the modal forces.
-    """
-    nodeList = self.markers[self.FSI_marker]
-    FX = np.zeros((self.nPoint, 1))
-    FY = np.zeros((self.nPoint, 1))
-    FZ = np.zeros((self.nPoint, 1))
-    for iPoint in nodeList:
-      Force = self.node[iPoint].GetForce()
-      FX[iPoint] = float(Force[0])
-      FY[iPoint] = float(Force[1])
-      FZ[iPoint] = float(Force[2])
-    self.F = self.UxT.dot(FX) + self.UyT.dot(FY) + self.UzT.dot(FZ)
-
-  def __ComputeResidual(self):
-    """
-    This method computes the residual for integration.
-    """
-
-    res = self.M.dot(self.qddot) + self.C.dot(self.qdot) + self.K.dot(self.q) - self.F
-
-    return res
-
-  def __TangentOperator(self):
-    """
-    This method computes the tangent operator for solution.
-    """
-
-    # The problem is linear, so the tangent operator is straightforward.
-    St = self.betaPrime*self.M + self.gammaPrime*self.C + self.K
-
-    return St
-
-  def exit(self):
-    """
-    This method cleanly exits the structural solver.
-    """
-
-    print("\n**************** Exiting the structural tester solver ****************")
-
-  def run(self,time):
-    """
-    This method is the main function for advancing the solution of one time step.
-    """
-    self.__temporalIteration(time)
-    header = 'Time\t'
-    for imode in range(min([self.nDof,5])):
-      header = header + 'q' + str(imode+1) + '\t' + 'qdot' + str(imode+1) + '\t' + 'qddot' + str(imode+1) + '\t'
-    header = header + '\n'
-    print(header)
-    line = '{:6.4f}'.format(time) + '\t'
-    for imode in range(min([self.nDof,5])):
-      line = line + '{:6.4f}'.format(float(self.q[imode])) + '\t' + '{:6.4f}'.format(float(self.qdot[imode])) + '\t' + '{:6.4f}'.format(float(self.qddot[imode])) + '\t'
-    line =  line + '\n'
-    print(line)
-    self.__computeInterfacePosVel(False)
-
-  def activateMode(self, iMode):
-    """
-    This method is used to artificially set only one mode activated, thus
-    with non zero amplitude.
-    """
-    self.__reset(self.q)
-    self.q[iMode] = 1.0
-    self.__computeInterfacePosVel(True)
-
-  def setInitialDisplacements(self):
-    """
-    This method provides public access to the method __computeInterfacePosVel and
-    sets velocities for previous time steps.
-    """
-
-    self.__computeInterfacePosVel(True)
-
-  def writeSolution(self, time, timeIter, FSIIter):
-    """
-    This method is the main function for output. It writes the file StructHistoryModal.dat
-    """
-
-    # Modal History
-    histFile = open('StructHistoryModal.dat', "a")
-    line = str(time) + '\t' + str(timeIter) + '\t' + str(FSIIter) + '\t'
-    for imode in range(self.nDof):
-      line = line + str(float(self.q[imode])) + '\t' + str(float(self.qdot[imode])) + '\t' + str(float(self.qddot[imode])) + '\t'
-    line =  line + '\n'
-    histFile.write(line)
-    histFile.close()
-
-  def updateSolution(self):
-    """
-    This method updates the solution.
-    """
-
-    self.q_n = np.copy(self.q)
-    self.qdot_n = np.copy(self.qdot)
-    self.qddot_n = np.copy(self.qddot)
-    self.a_n = np.copy(self.a)
-    self.__reset(self.q)
-    self.__reset(self.qdot)
-    self.__reset(self.qddot)
-    self.__reset(self.a)
-
-    for iPoint in range(self.nPoint):
-      self.node[iPoint].updateCoordVel()
-
-
-  def applyload(self, iVertex, fx, fy, fz):
-    """
-    This method can be accessed from outside to set the nodal forces.
-    """
-    iPoint = self.getVertexGlobalIndex(self.FSI_marker, iVertex)
-    self.node[iPoint].SetForce((fx,fy,fz))
+            histFile = open("StructHistoryModal.dat", "w")
+            header = "Time\t" + "Time Iteration\t" + "FSI Iteration\t"
+            for imode in range(self.nDof):
+                header = (
+                    header
+                    + "q"
+                    + str(imode + 1)
+                    + "\t"
+                    + "qdot"
+                    + str(imode + 1)
+                    + "\t"
+                    + "qddot"
+                    + str(imode + 1)
+                    + "\t"
+                )
+            header = header + "\n"
+            histFile.write(header)
+            histFile.close()
+        else:
+            self.__setRestart()
+
+    def __readConfig(self):
+        """
+        This methods obtains the configuration options from the structural solver input
+        file.
+        """
+
+        with open(self.Config_file) as configfile:
+            while 1:
+                line = configfile.readline()
+                if not line:
+                    break
 
-  def getNumberOfModes(self):
-    """
-    This method provides the number of degrees of freedom used in
-    the structural solver.
-    """
-    return self.nDof
+                # remove line returns
+                line = line.strip("\r\n")
+                # make sure it has useful data
+                if (not "=" in line) or (line[0] == "%"):
+                    continue
+                # split across equal sign
+                line = line.split("=", 1)
+                this_param = line[0].strip()
+                this_value = line[1].strip()
+
+                # integer values
+                if (this_param == "NMODES") or (this_param == "RESTART_ITER"):
+                    self.Config[this_param] = int(this_value)
+
+                # float values
+                elif (
+                    (this_param == "DELTA_T")
+                    or (this_param == "MODAL_DAMPING")
+                    or (this_param == "RHO")
+                ):
+                    self.Config[this_param] = float(this_value)
+
+                # string values
+                elif (
+                    (this_param == "TIME_MARCHING")
+                    or (this_param == "MESH_FILE")
+                    or (this_param == "PUNCH_FILE")
+                    or (this_param == "RESTART_SOL")
+                    or (this_param == "MOVING_MARKER")
+                ):
+                    self.Config[this_param] = this_value
+
+                # lists values
+                elif (
+                    (this_param == "INITIAL_MODES")
+                    or (this_param == "IMPOSED_MODES")
+                    or (this_param == "IMPOSED_PARAMETERS")
+                ):
+                    self.Config[this_param] = eval(this_value)
+
+                else:
+                    raise Exception("{} is an invalid option !".format(this_param))
+
+    def __readNastranMesh(self):
+        """
+        This method reads the nastran 3D mesh.
+        """
+
+        def nastran_float(s):
+            if s.find("E") == -1:
+                s = s.replace("-", "e-")
+                s = s.replace("+", "e+")
+                if s[0] == "e":
+                    s = s[1:]
+            return float(s)
+
+        self.nMarker = 0
+        self.nPoint = 0
+        self.nRefSys = 0
+
+        with open(self.Mesh_file, "r") as meshfile:
+            print("Opened mesh file " + self.Mesh_file + ".")
+            while 1:
+                line = meshfile.readline()
+                if not line:
+                    break
 
-  def getFSIMarkerID(self):
-    """
-    This method provides the ID of the interface marker
-    """
-    return self.FSI_marker
+                pos = line.find("GRID")
+                if pos == 30:
+                    line = line.strip("\r\n")
+                    self.node.append(Point())
+                    line = line[30:]
+                    ID = int(line[8:16])
+                    CP = self.__checkBlankField(line[16:24])
+                    x = nastran_float(line[24:32])
+                    y = nastran_float(line[32:40])
+                    z = nastran_float(line[40:48])
+                    if CP != 0:
+                        for iRefSys in range(self.nRefSys):
+                            if self.refsystems[iRefSys].GetCID() == CP:
+                                break
+                        if self.refsystems[iRefSys].GetCID() != CP:
+                            raise Exception(
+                                "Definition reference {} system not found".format(CP)
+                            )
+                        DeltaPos = self.refsystems[iRefSys].GetOrigin()
+                        RotatedPos = (
+                            self.refsystems[iRefSys]
+                            .GetRotMatrix()
+                            .dot(np.array([[x], [y], [z]]))
+                        )
+                        x = RotatedPos[0] + DeltaPos[0]
+                        y = RotatedPos[1] + DeltaPos[1]
+                        z = RotatedPos[2] + DeltaPos[2]
+                    CD = self.__checkBlankField(line[48:56])
+                    self.node[self.nPoint].SetCoord((x, y, z))
+                    self.node[self.nPoint].SetID(ID)
+                    self.node[self.nPoint].SetCP(CP)
+                    self.node[self.nPoint].SetCD(CD)
+                    self.node[self.nPoint].SetCoord0((x, y, z))
+                    self.node[self.nPoint].SetCoord_n((x, y, z))
+                    self.nPoint += 1
+                    continue
+
+                pos = line.find("CORD2R")
+                if pos == 30:
+                    line = line.strip("\r\n")
+                    self.refsystems.append(RefSystem())
+                    line = line[30:]
+                    CID = int(line[8:16])
+                    self.refsystems[self.nRefSys].SetCID(CID)
+                    RID = int(line[16:24])
+                    if RID != 0:
+                        raise Exception(
+                            "ERROR: Reference system {} must be defined with respect to global reference system".format(
+                                CID
+                            )
+                        )
+                    self.refsystems[self.nRefSys].SetRID(RID)
+                    AX = nastran_float(line[24:32])
+                    AY = nastran_float(line[32:40])
+                    AZ = nastran_float(line[40:48])
+                    BX = nastran_float(line[48:56])
+                    BY = nastran_float(line[56:64])
+                    BZ = nastran_float(line[64:72])
+                    z_direction = np.array([BX - AX, BY - AY, BZ - AZ])
+                    z_direction = z_direction / linalg.norm(z_direction)
+                    line = meshfile.readline()
+                    line = line.strip("\r\n")
+                    line = line[30:]
+                    CX = nastran_float(line[8:16])
+                    CY = nastran_float(line[16:24])
+                    CZ = nastran_float(line[24:32])
+                    y_direction = np.cross(z_direction, [CX - AX, CY - AY, CZ - AZ])
+                    y_direction = y_direction / linalg.norm(y_direction)
+                    x_direction = np.cross(y_direction, z_direction)
+                    x_direction = x_direction / linalg.norm(x_direction)
+                    self.refsystems[self.nRefSys].SetRotMatrix(
+                        x_direction, y_direction, z_direction
+                    )
+                    self.refsystems[self.nRefSys].SetOrigin((AX, AY, AZ))
+                    self.nRefSys += 1
+                    continue
+
+                pos = line.find("SET1")
+                if pos == 30:
+                    line = line.strip("\r\n")
+                    line = line[37:]
+                    line = line.split()
+                    existValue = True
+                    markerTag = line.pop(0)
+                    self.markers[markerTag] = []
+                    while existValue:
+                        if line[0] == "+":
+                            line = meshfile.readline()
+                            line = line.strip("\r\n")
+                            line = line[37:]
+                            line = line.split()
+                        ID = int(line.pop(0))
+                        for iPoint in range(self.nPoint):
+                            if self.node[iPoint].GetID() == ID:
+                                break
+                        if (iPoint == (self.nPoint - 1)) and (
+                            self.node[iPoint].GetID() != ID
+                        ):
+                            raise Exception(
+                                "Point {} in the set {} was not found in the mesh".format(
+                                    ID, markerTag
+                                )
+                            )
+                        self.markers[markerTag].append(iPoint)
+                        existValue = len(line) >= 1
+                    self.nMarker += 1
+                    continue
+
+        if not any(self.FSI_marker in key for key in self.markers.keys()):
+            raise Exception("The FSI marker was not found in the available sets")
+
+        self.markers[self.FSI_marker].sort()
+
+        print("Number of points: {}".format(self.nPoint))
+        print("Number of markers: {}".format(self.nMarker))
+        print("Number of reference systems: {}".format(self.nRefSys))
+        print("Moving marker: {}".format(self.FSI_marker))
+        print(
+            "Number of points in the moving marker".format(
+                len(self.markers[self.FSI_marker])
+            )
+        )
+
+    def __checkBlankField(self, string):
+        """
+        This method considers that Nastran apply 0 when the reference system is not specified
+        """
+
+        if string == " " * 8:
+            return int(0)
+        return int(string)
+
+    def __setStructuralMatrices(self):
+        """
+        This method reads the punch file and obtains the modal shapes and modal stiffnesses.
+        """
+
+        self.M = np.zeros((self.nDof, self.nDof))
+        self.K = np.zeros((self.nDof, self.nDof))
+        self.C = np.zeros((self.nDof, self.nDof))
+
+        self.q = np.zeros((self.nDof, 1))
+        self.qdot = np.zeros((self.nDof, 1))
+        self.qddot = np.zeros((self.nDof, 1))
+        self.a = np.zeros((self.nDof, 1))
+
+        self.q_n = np.zeros((self.nDof, 1))
+        self.qdot_n = np.zeros((self.nDof, 1))
+        self.qddot_n = np.zeros((self.nDof, 1))
+        self.a_n = np.zeros((self.nDof, 1))
+
+        self.F = np.zeros((self.nDof, 1))
+
+        self.Ux = np.zeros((self.nPoint, self.nDof))
+        self.Uy = np.zeros((self.nPoint, self.nDof))
+        self.Uz = np.zeros((self.nPoint, self.nDof))
+
+        with open(self.Punch_file, "r") as punchfile:
+            print("Opened punch file " + self.Punch_file + ".")
+            while 1:
+                line = punchfile.readline()
+                if not line:
+                    break
 
-  def getNumberOfSolidInterfaceNodes(self, markerID):
+                pos = line.find("MODE ")
+                if pos != -1:
+                    line = line.strip("\r\n").split()
+                    n = int(line[5])
+                    imode = n - 1
+                    k_i = float(line[2])
+                    self.M[imode][imode] = 1
+                    self.K[imode][imode] = k_i
+                    w_i = sqrt(k_i)
+                    self.C[imode][imode] = 2 * self.ModalDamping * w_i
+                    iPoint = 0
+                    for indexIter in range(self.nPoint):
+                        line = punchfile.readline()
+                        line = line.strip("\r\n").split()
+                        if line[1] == "G":
+                            ux = float(line[2])
+                            uy = float(line[3])
+                            uz = float(line[4])
+                            if self.node[iPoint].GetCD() != 0:
+                                for iRefSys in range(self.nRefSys):
+                                    if (
+                                        self.refsystems[iRefSys].GetCID()
+                                        == self.node[iPoint].GetCD()
+                                    ):
+                                        break
+                                if (
+                                    self.refsystems[iRefSys].GetCID()
+                                    != self.node[iPoint].GetCD()
+                                ):
+                                    raise Exception(
+                                        "Output reference {} system not found".format(
+                                            self.node[iPoint].GetCD()
+                                        )
+                                    )
+                                RotatedOutput = (
+                                    self.refsystems[iRefSys]
+                                    .GetRotMatrix()
+                                    .dot(np.array([[ux], [uy], [uz]]))
+                                )
+                                ux = RotatedOutput[0]
+                                uy = RotatedOutput[1]
+                                uz = RotatedOutput[2]
+                            self.Ux[iPoint][imode] = ux
+                            self.Uy[iPoint][imode] = uy
+                            self.Uz[iPoint][imode] = uz
+                            iPoint = iPoint + 1
+                            line = punchfile.readline()
+                        if line[1] == "S":
+                            line = punchfile.readline()
+
+                    if n == self.nDof:
+                        break
+
+        self.__setNonDiagonalStructuralMatrices()
+
+        self.UxT = self.Ux.transpose()
+        self.UyT = self.Uy.transpose()
+        self.UzT = self.Uz.transpose()
+
+        if n < self.nDof:
+            raise Exception(
+                "ERROR: available {} degrees of freedom instead of {} as requested".format(
+                    n, self.nDof
+                )
+            )
+        else:
+            print("Using {} degrees of freedom".format(n))
+
+    def __setNonDiagonalStructuralMatrices(self):
+        """
+        This method is part of an advanced feature of this solver that allows to set
+        nondiagonal matrices for the structural modes.
+        """
+
+        K_updated = self.__readNonDiagonalMatrix("NDK")
+        M_updated = self.__readNonDiagonalMatrix("NDM")
+        C_updated = self.__readNonDiagonalMatrix("NDC")
+        if K_updated and M_updated and (not C_updated):
+            print("Setting modal damping")
+            self.__setNonDiagonalDamping()
+        elif (not K_updated) and (not M_updated):
+            print("Modal stiffness and mass matrices are diagonal")
+        elif (not K_updated) and M_updated:
+            raise Exception("Non-Diagonal stiffness matrix is missing")
+        elif (not M_updated) and K_updated:
+            raise Exception("Non-Diagonal mass matrix is missing")
+
+    def __readNonDiagonalMatrix(self, keyword):
+        """
+        This method reads from the punch file the definition of nondiagonal structural
+        matrices.
+        """
+
+        matrixUpdated = False
+
+        with open(self.Punch_file, "r") as punchfile:
+
+            while 1:
+                line = punchfile.readline()
+                if not line:
+                    break
 
-    return len(self.markers[markerID])
+                pos = line.find(keyword)
+                if pos != -1:
+                    while 1:
+                        line = punchfile.readline()
+                        line = line.strip("\r\n").split()
+                        if line[0] != "-CONT-":
+                            i = int(line[0]) - 1
+                            j = 0
+                            el = line[1:]
+                            ne = len(el)
+                        elif line[0] == "-CONT-":
+                            el = line[1:]
+                            ne = len(el)
+                        if keyword == "NDK":
+                            self.K[i][j : j + ne] = np.array(el)
+                        elif keyword == "NDM":
+                            self.M[i][j : j + ne] = np.array(el)
+                        elif keyword == "NDC":
+                            self.C[i][j : j + ne] = np.array(el)
+                        j = j + ne
+                        if i + 1 == self.nDof and j == self.nDof:
+                            matrixUpdated = True
+                            break
+
+        return matrixUpdated
+
+    def __setNonDiagonalDamping(self):
+
+        D, V = linalg.eig(self.K, self.M)
+        D = D.real
+        D = np.sqrt(D)
+        Mmodal = ((V.transpose()).dot(self.M)).dot(V)
+        Mmodal = np.diag(Mmodal)
+        C = 2 * self.ModalDamping * np.multiply(D, Mmodal)
+        C = np.diag(C)
+        Vinv = linalg.inv(V)
+        C = C.dot(Vinv)
+        VinvT = Vinv.transpose()
+        self.C = VinvT.dot(C)
+
+    def __setIntegrationParameters(self):
+        """
+        This method uses the time step size to define the integration parameters.
+        """
+
+        self.alpha_m = (2.0 * self.rhoAlphaGen - 1.0) / (self.rhoAlphaGen + 1.0)
+        self.alpha_f = (self.rhoAlphaGen) / (self.rhoAlphaGen + 1.0)
+        self.gamma = 0.5 + self.alpha_f - self.alpha_m
+        self.beta = 0.25 * (self.gamma + 0.5) ** 2
+
+        self.gammaPrime = self.gamma / (self.deltaT * self.beta)
+        self.betaPrime = (1.0 - self.alpha_m) / (
+            (self.deltaT**2) * self.beta * (1.0 - self.alpha_f)
+        )
+
+        print("Time integration with the alpha-generalized algorithm.")
+        print("rho : {}".format(self.rhoAlphaGen))
+        print("alpha_m : {}".format(self.alpha_m))
+        print("alpha_f : {}".format(self.alpha_f))
+        print("gamma : {}".format(self.gamma))
+        print("beta : {}".format(self.beta))
+        print("gammaPrime : {}".format(self.gammaPrime))
+        print("betaPrime : {}".format(self.betaPrime))
+
+    def __setInitialConditions(self):
+        """
+        This method uses the list of initial modal amplitudes to set the initial conditions
+        """
+
+        print("Setting initial conditions.")
+
+        print("Using modal amplitudes from config file")
+        for imode in range(self.nDof):
+            if imode in self.Config["INITIAL_MODES"].keys():
+                self.q[imode] = float(self.Config["INITIAL_MODES"][imode])
+                self.q_n[imode] = float(self.Config["INITIAL_MODES"][imode])
+
+        RHS = np.zeros((self.nDof, 1))
+        RHS += self.F
+        RHS -= self.C.dot(self.qdot)
+        RHS -= self.K.dot(self.q)
+        self.qddot = linalg.solve(self.M, RHS)
+        self.qddot_n = np.copy(self.qddot)
+        self.a = np.copy(self.qddot)
+        self.a_n = np.copy(self.qddot)
+
+    def __reset(self, vector):
+        """
+        This method set to zero any vector.
+        """
+
+        for ii in range(vector.shape[0]):
+            vector[ii] = 0.0
+
+    def __computeInterfacePosVel(self, initialize):
+        """
+        This method uses the mode shapes to compute, based on the modal velocities, the
+        nodal velocities at the interface.
+        """
+
+        # Multiply the modal matrices with modal amplitudes
+        X_vel = self.Ux.dot(self.qdot)
+        Y_vel = self.Uy.dot(self.qdot)
+        Z_vel = self.Uz.dot(self.qdot)
+
+        X_disp = self.Ux.dot(self.q)
+        Y_disp = self.Uy.dot(self.q)
+        Z_disp = self.Uz.dot(self.q)
+
+        for iPoint in range(self.nPoint):
+            coord0 = self.node[iPoint].GetCoord0()
+            self.node[iPoint].SetCoord(
+                (
+                    X_disp[iPoint] + coord0[0],
+                    Y_disp[iPoint] + coord0[1],
+                    Z_disp[iPoint] + coord0[2],
+                )
+            )
+            self.node[iPoint].SetVel((X_vel[iPoint], Y_vel[iPoint], Z_vel[iPoint]))
+
+            if initialize:
+                self.node[iPoint].SetCoord_n(
+                    (
+                        X_disp[iPoint] + coord0[0],
+                        Y_disp[iPoint] + coord0[1],
+                        Z_disp[iPoint] + coord0[2],
+                    )
+                )
+                self.node[iPoint].SetVel_n(
+                    (X_vel[iPoint], Y_vel[iPoint], Z_vel[iPoint])
+                )
+
+    def __setRestart(self):
+        """
+        This method sets all the variables needed for the correct restart.
+        """
+
+        # read the Structhistory to obtain the mode amplitudes
+        nM1Set = False
+        nSet = False
+        firstLineRead = False
+        couplingLineRead = False
+
+        with open("StructHistoryModal.dat", "r") as file:
+            print("Opened history file StructHistoryModal.dat.")
+            line = file.readline()
+            while 1:
+                line = file.readline()
+                if not line:
+                    break
+                line = line.strip("\r\n").split()
+
+                # The old time_0 for imposed motion can either be the first line of the StructHistoryModal, if TimeIterTreshold was -1 (immediate coupling), or the second line. In the former case, time_0 is 0.0, so it is easy to recognize it
+                if not firstLineRead:
+                    firstLineRead = True
+                    if float(line[0]) == 0.0:
+                        couplingLineRead = True
+                        self.timeStartCoupling = 0.0
+                else:
+                    if couplingLineRead:
+                        pass
+                    else:
+                        self.timeStartCoupling = float(line[0])
+                        couplingLineRead = True
+
+                if int(line[1]) == (self.Config["RESTART_ITER"] - 2):
+                    index = 0
+                    for index_mode in range(self.nDof):
+                        self.q[index_mode] = float(line[index + 3])
+                        self.qdot[index_mode] = float(line[index + 4])
+                        self.qddot[index_mode] = float(line[index + 5])
+                        index += 3
+                    del index
+                    # push back the mode amplitudes velocities and accelerations
+                    self.__computeInterfacePosVel(True)
+                    self.q_n = np.copy(self.q)
+                    self.qdot_n = np.copy(self.qdot)
+                    self.qddot_n = np.copy(self.qddot)
+                    self.a_n = np.copy(self.a)
+                    nM1Set = True
+                if int(line[1]) == (self.Config["RESTART_ITER"] - 1):
+                    index = 0
+                    for index_mode in range(self.nDof):
+                        self.q[index_mode] = float(line[index + 3])
+                        self.qdot[index_mode] = float(line[index + 4])
+                        self.qddot[index_mode] = float(line[index + 5])
+                        index += 3
+                    del index
+                    self.__computeInterfacePosVel(False)
+                    nSet = True
+                    break
 
-  def getVertexGlobalIndex(self, markerID, iVertex):
+        if (not nM1Set) or (not nSet):
+            raise Exception(
+                "The restart iteration was not found in the structural history"
+            )
 
-    # This solver is serial, thus global=local
-    return self.markers[markerID][iVertex]
+    def __temporalIteration(self, time):
+        """
+        This method integrates in time the solution.
+        """
 
-  def getInterfaceNodePosInit(self, markerID, iVertex):
+        self.__reset(self.q)
+        self.__reset(self.qdot)
+        self.__reset(self.qddot)
+        self.__reset(self.a)
 
-    iPoint = self.markers[markerID][iVertex]
-    Coord0 = self.node[iPoint].GetCoord0()
-    return Coord0
+        if not self.ImposedMotion:
+            eps = 1e-6
 
-  def getInterfaceNodeDisp(self, markerID, iVertex):
+            self.__SetLoads()
 
-    iPoint = self.markers[markerID][iVertex]
-    Coord = self.node[iPoint].GetCoord()
-    Coord0 = self.node[iPoint].GetCoord0()
-    return (Coord-Coord0)
+            # Prediction step
 
-  def getInterfaceNodeVel(self, markerID, iVertex):
+            self.a += (self.alpha_f) / (1 - self.alpha_m) * self.qddot_n
+            self.a -= (self.alpha_m) / (1 - self.alpha_m) * self.a_n
 
-    iPoint = self.markers[markerID][iVertex]
-    Vel = self.node[iPoint].GetVel()
-    return Vel
+            self.q = np.copy(self.q_n)
+            self.q += self.deltaT * self.qdot_n
+            self.q += (0.5 - self.beta) * self.deltaT * self.deltaT * self.a_n
+            self.q += self.deltaT * self.deltaT * self.beta * self.a
 
-  def getInterfaceNodeVelNm1(self, markerID, iVertex):
+            self.qdot = np.copy(self.qdot_n)
+            self.qdot += (1 - self.gamma) * self.deltaT * self.a_n
+            self.qdot += self.deltaT * self.gamma * self.a
 
-    iPoint = self.markers[markerID][iVertex]
-    Vel = self.node[iPoint].GetVel_n()
-    return Vel
+            # Correction step
+            res = self.__ComputeResidual()
 
-  def IsAHaloNode(self, markerID, iVertex):
+            while linalg.norm(res) >= eps:
+                St = self.__TangentOperator()
+                Deltaq = -1 * (linalg.solve(St, res))
+                self.q += Deltaq
+                self.qdot += self.gammaPrime * Deltaq
+                self.qddot += self.betaPrime * Deltaq
+                res = self.__ComputeResidual()
 
-    # There are no halo nodes in this solver as it is serial
-    iPoint = self.markers[markerID][iVertex]
-    halo = False
-    return halo
+            self.a += (1 - self.alpha_f) / (1 - self.alpha_m) * self.qddot
+        else:
+            if self.ImposedMotionToSet:
+                if self.Config["RESTART_SOL"] == "NO":
+                    # If yes we already set it in the __setRestart function
+                    self.timeStartCoupling = time
+                iImposedFunc = 0
+                for imode in self.Config["IMPOSED_MODES"].keys():
+                    for isuperposed in range(len(self.Config["IMPOSED_MODES"][imode])):
+                        typeOfMotion = self.Config["IMPOSED_MODES"][imode][isuperposed]
+                        parameters = self.Config["IMPOSED_PARAMETERS"][imode][
+                            isuperposed
+                        ]
+                        self.ImposedMotionFunction.append(
+                            ImposedMotionClass(
+                                self.timeStartCoupling, typeOfMotion, parameters, imode
+                            )
+                        )
+                        iImposedFunc += 1
+                self.ImposedMotionToSet = False
+            for iImposedFunc in range(len(self.ImposedMotionFunction)):
+                imode = self.ImposedMotionFunction[iImposedFunc].mode
+                self.q[imode] += self.ImposedMotionFunction[iImposedFunc].GetDispl(time)
+                self.qdot[imode] += self.ImposedMotionFunction[iImposedFunc].GetVel(
+                    time
+                )
+                self.qddot[imode] += self.ImposedMotionFunction[iImposedFunc].GetAcc(
+                    time
+                )
+            self.a = np.copy(self.qddot)
+
+    def __SetLoads(self):
+        """
+        This method uses the nodal forces and the mode shapes to obtain the modal forces.
+        """
+        nodeList = self.markers[self.FSI_marker]
+        FX = np.zeros((self.nPoint, 1))
+        FY = np.zeros((self.nPoint, 1))
+        FZ = np.zeros((self.nPoint, 1))
+        for iPoint in nodeList:
+            Force = self.node[iPoint].GetForce()
+            FX[iPoint] = float(Force[0])
+            FY[iPoint] = float(Force[1])
+            FZ[iPoint] = float(Force[2])
+        self.F = self.UxT.dot(FX) + self.UyT.dot(FY) + self.UzT.dot(FZ)
+
+    def __ComputeResidual(self):
+        """
+        This method computes the residual for integration.
+        """
+
+        res = (
+            self.M.dot(self.qddot) + self.C.dot(self.qdot) + self.K.dot(self.q) - self.F
+        )
+
+        return res
+
+    def __TangentOperator(self):
+        """
+        This method computes the tangent operator for solution.
+        """
+
+        # The problem is linear, so the tangent operator is straightforward.
+        St = self.betaPrime * self.M + self.gammaPrime * self.C + self.K
+
+        return St
+
+    def exit(self):
+        """
+        This method cleanly exits the structural solver.
+        """
+
+        print(
+            "\n**************** Exiting the structural tester solver ****************"
+        )
+
+    def run(self, time):
+        """
+        This method is the main function for advancing the solution of one time step.
+        """
+        self.__temporalIteration(time)
+        header = "Time\t"
+        for imode in range(min([self.nDof, 5])):
+            header = (
+                header
+                + "q"
+                + str(imode + 1)
+                + "\t"
+                + "qdot"
+                + str(imode + 1)
+                + "\t"
+                + "qddot"
+                + str(imode + 1)
+                + "\t"
+            )
+        header = header + "\n"
+        print(header)
+        line = "{:6.4f}".format(time) + "\t"
+        for imode in range(min([self.nDof, 5])):
+            line = (
+                line
+                + "{:6.4f}".format(float(self.q[imode]))
+                + "\t"
+                + "{:6.4f}".format(float(self.qdot[imode]))
+                + "\t"
+                + "{:6.4f}".format(float(self.qddot[imode]))
+                + "\t"
+            )
+        line = line + "\n"
+        print(line)
+        self.__computeInterfacePosVel(False)
+
+    def activateMode(self, iMode):
+        """
+        This method is used to artificially set only one mode activated, thus
+        with non zero amplitude.
+        """
+        self.__reset(self.q)
+        self.q[iMode] = 1.0
+        self.__computeInterfacePosVel(True)
+
+    def setInitialDisplacements(self):
+        """
+        This method provides public access to the method __computeInterfacePosVel and
+        sets velocities for previous time steps.
+        """
+
+        self.__computeInterfacePosVel(True)
+
+    def writeSolution(self, time, timeIter, FSIIter):
+        """
+        This method is the main function for output. It writes the file StructHistoryModal.dat
+        """
+
+        # Modal History
+        histFile = open("StructHistoryModal.dat", "a")
+        line = str(time) + "\t" + str(timeIter) + "\t" + str(FSIIter) + "\t"
+        for imode in range(self.nDof):
+            line = (
+                line
+                + str(float(self.q[imode]))
+                + "\t"
+                + str(float(self.qdot[imode]))
+                + "\t"
+                + str(float(self.qddot[imode]))
+                + "\t"
+            )
+        line = line + "\n"
+        histFile.write(line)
+        histFile.close()
+
+    def updateSolution(self):
+        """
+        This method updates the solution.
+        """
+
+        self.q_n = np.copy(self.q)
+        self.qdot_n = np.copy(self.qdot)
+        self.qddot_n = np.copy(self.qddot)
+        self.a_n = np.copy(self.a)
+        self.__reset(self.q)
+        self.__reset(self.qdot)
+        self.__reset(self.qddot)
+        self.__reset(self.a)
+
+        for iPoint in range(self.nPoint):
+            self.node[iPoint].updateCoordVel()
+
+    def applyload(self, iVertex, fx, fy, fz):
+        """
+        This method can be accessed from outside to set the nodal forces.
+        """
+        iPoint = self.getVertexGlobalIndex(self.FSI_marker, iVertex)
+        self.node[iPoint].SetForce((fx, fy, fz))
+
+    def getNumberOfModes(self):
+        """
+        This method provides the number of degrees of freedom used in
+        the structural solver.
+        """
+        return self.nDof
+
+    def getFSIMarkerID(self):
+        """
+        This method provides the ID of the interface marker
+        """
+        return self.FSI_marker
+
+    def getNumberOfSolidInterfaceNodes(self, markerID):
+
+        return len(self.markers[markerID])
+
+    def getVertexGlobalIndex(self, markerID, iVertex):
+
+        # This solver is serial, thus global=local
+        return self.markers[markerID][iVertex]
+
+    def getInterfaceNodePosInit(self, markerID, iVertex):
+
+        iPoint = self.markers[markerID][iVertex]
+        Coord0 = self.node[iPoint].GetCoord0()
+        return Coord0
+
+    def getInterfaceNodeDisp(self, markerID, iVertex):
+
+        iPoint = self.markers[markerID][iVertex]
+        Coord = self.node[iPoint].GetCoord()
+        Coord0 = self.node[iPoint].GetCoord0()
+        return Coord - Coord0
+
+    def getInterfaceNodeVel(self, markerID, iVertex):
+
+        iPoint = self.markers[markerID][iVertex]
+        Vel = self.node[iPoint].GetVel()
+        return Vel
+
+    def getInterfaceNodeVelNm1(self, markerID, iVertex):
+
+        iPoint = self.markers[markerID][iVertex]
+        Vel = self.node[iPoint].GetVel_n()
+        return Vel
+
+    def IsAHaloNode(self, markerID, iVertex):
+
+        # There are no halo nodes in this solver as it is serial
+        iPoint = self.markers[markerID][iVertex]
+        halo = False
+        return halo
diff --git a/SU2_PY/change_version_number.py b/SU2_PY/change_version_number.py
index e08811e006b..4786a9eedd3 100755
--- a/SU2_PY/change_version_number.py
+++ b/SU2_PY/change_version_number.py
@@ -28,37 +28,50 @@
 # make print(*args) function available in PY2.6+, does'nt work on PY < 2.6
 from __future__ import print_function
 from optparse import OptionParser
+
 # Run the script from the base directory (ie $SU2HOME). Grep will search directories recursively for matches in version number
-import os,sys
+import os, sys
 
 parser = OptionParser()
-parser.add_option("-v", "--version", dest="version",
-                  help="the new version number", metavar="VERSION")
-parser.add_option("-r", "--releasename", dest="releasename",
-                  help="Name of the new release", metavar="RELEASENAME")
-parser.add_option("-y", action="store_true", dest="yes", help="Answer yes to all questions", metavar="YES")
-(options, args)=parser.parse_args()
+parser.add_option(
+    "-v", "--version", dest="version", help="the new version number", metavar="VERSION"
+)
+parser.add_option(
+    "-r",
+    "--releasename",
+    dest="releasename",
+    help="Name of the new release",
+    metavar="RELEASENAME",
+)
+parser.add_option(
+    "-y",
+    action="store_true",
+    dest="yes",
+    help="Answer yes to all questions",
+    metavar="YES",
+)
+(options, args) = parser.parse_args()
 
 if not options.version:
     parser.error("new version number must be provided with -v option")
 
-oldvers  = '7.5.1 "Blackbird"'
-oldvers_q= r'7.5.1 \"Blackbird\"'
-newvers  = str(options.version) + ' "' + str(options.releasename) + '"'
-newvers_q= str(options.version) + ' \\"' + str(options.releasename) + '\\"'
-#oldvers = 'Copyright 2012-2023, SU2'
-#oldvers_q = oldvers
-#newvers = 'Copyright 2012-2023, SU2'
-#newvers_q = newvers
+oldvers = '7.5.1 "Blackbird"'
+oldvers_q = r"7.5.1 \"Blackbird\""
+newvers = str(options.version) + ' "' + str(options.releasename) + '"'
+newvers_q = str(options.version) + ' \\"' + str(options.releasename) + '\\"'
+# oldvers = 'Copyright 2012-2023, SU2'
+# oldvers_q = oldvers
+# newvers = 'Copyright 2012-2023, SU2'
+# newvers_q = newvers
 
 if sys.version_info[0] > 2:
-  # In PY3, raw_input is replaced with input.
-  # For original input behaviour, just write eval(input())
-  raw_input = input
+    # In PY3, raw_input is replaced with input.
+    # For original input behaviour, just write eval(input())
+    raw_input = input
 
 
-if os.path.exists('version.txt'):
-  os.remove('version.txt')
+if os.path.exists("version.txt"):
+    os.remove("version.txt")
 
 # Grep flag cheatsheet:
 # -I : Ignore binary files
@@ -67,35 +80,41 @@
 # -r : search directory recursively
 # -v : Omit search string (.svn omitted, line containing ISC is CGNS related)
 
-#TODO: replace with portable instructions. This works only on unix systems
-os.system("grep -IFwr '%s' *|grep -vF '.svn' |grep -v ISC > version.txt"%oldvers)
-os.system("grep -IFwr '%s' --exclude='version.txt' *|grep -vF '.svn' |grep -v ISC >> version.txt"%oldvers_q)
+# TODO: replace with portable instructions. This works only on unix systems
+os.system("grep -IFwr '%s' *|grep -vF '.svn' |grep -v ISC > version.txt" % oldvers)
+os.system(
+    "grep -IFwr '%s' --exclude='version.txt' *|grep -vF '.svn' |grep -v ISC >> version.txt"
+    % oldvers_q
+)
 
 # Create a list of files to adjust
 filelist = []
-f = open('version.txt','r')
+f = open("version.txt", "r")
 for line in f.readlines():
-  candidate = line.split(':')[0]
-  if not candidate in filelist:
-    filelist.append(candidate)
+    candidate = line.split(":")[0]
+    if not candidate in filelist:
+        filelist.append(candidate)
 f.close()
 print(filelist)
 
 # Prompt user before continuing
-yorn = ''
-while(not yorn.lower()=='y' and not options.yes):
-  yorn = raw_input('Replace %s with %s and %s with %s in the listed files? [Y/N]: '%(oldvers,newvers, oldvers_q, newvers_q))
-  if yorn.lower()=='n':
-    print('The file version.txt contains matches of oldvers')
-    sys.exit()
+yorn = ""
+while not yorn.lower() == "y" and not options.yes:
+    yorn = raw_input(
+        "Replace %s with %s and %s with %s in the listed files? [Y/N]: "
+        % (oldvers, newvers, oldvers_q, newvers_q)
+    )
+    if yorn.lower() == "n":
+        print("The file version.txt contains matches of oldvers")
+        sys.exit()
 
 # Loop through and correct all files
 for fname in filelist:
-  s = open(fname,'r').read()
-  s_new = s.replace(oldvers,newvers)
-  s_new = s_new.replace(oldvers_q, newvers_q)
-  f = open(fname,'w')
-  f.write(s_new)
-  f.close()
+    s = open(fname, "r").read()
+    s_new = s.replace(oldvers, newvers)
+    s_new = s_new.replace(oldvers_q, newvers_q)
+    f = open(fname, "w")
+    f.write(s_new)
+    f.close()
 
-os.system('rm -rf version.txt')
+os.system("rm -rf version.txt")
diff --git a/SU2_PY/compute_multipoint.py b/SU2_PY/compute_multipoint.py
index d4e41067a3d..e4641791028 100755
--- a/SU2_PY/compute_multipoint.py
+++ b/SU2_PY/compute_multipoint.py
@@ -33,17 +33,24 @@
 
 # Command Line Options
 parser = OptionParser()
-parser.add_option("-f", "--file", dest="filename",
-                  help="read config from FILE", metavar="FILE")
-parser.add_option("-n", "--partitions", dest="partitions", default=2,
-                  help="number of PARTITIONS", metavar="PARTITIONS")
+parser.add_option(
+    "-f", "--file", dest="filename", help="read config from FILE", metavar="FILE"
+)
+parser.add_option(
+    "-n",
+    "--partitions",
+    dest="partitions",
+    default=2,
+    help="number of PARTITIONS",
+    metavar="PARTITIONS",
+)
 
-(options, args)=parser.parse_args()
-options.partitions = int( options.partitions )
+(options, args) = parser.parse_args()
+options.partitions = int(options.partitions)
 
 # load config, start state
 config = SU2.io.Config(options.filename)
-state  = SU2.io.State()
+state = SU2.io.State()
 
 # prepare config
 config.NUMBER_PART = options.partitions
@@ -52,8 +59,10 @@
 state.find_files(config)
 
 # run su2
-multipoint_drag = SU2.eval.func('MULTIPOINT_DRAG',config,state)
-grad_multipoint_drag= SU2.eval.grad('MULTIPOINT_DRAG','CONTINUOUS_ADJOINT',config,state)
+multipoint_drag = SU2.eval.func("MULTIPOINT_DRAG", config, state)
+grad_multipoint_drag = SU2.eval.grad(
+    "MULTIPOINT_DRAG", "CONTINUOUS_ADJOINT", config, state
+)
 
-print('MULTIPOINT_DRAG     =', multipoint_drag)
-print('GRADIENT MULTIPOINT_DRAG =', grad_multipoint_drag)
+print("MULTIPOINT_DRAG     =", multipoint_drag)
+print("GRADIENT MULTIPOINT_DRAG =", grad_multipoint_drag)
diff --git a/SU2_PY/compute_polar.py b/SU2_PY/compute_polar.py
index af8562caaf7..dd974e37293 100755
--- a/SU2_PY/compute_polar.py
+++ b/SU2_PY/compute_polar.py
@@ -27,7 +27,7 @@
 #
 #
 # Several combinations of angles are possible:
-#------------------------------------------------
+# ------------------------------------------------
 # 1. Polar-sweep in alpha per given phi                        ...... polarVar   = aoa
 # 2. Polar-sweep in alpha per given beta (side slip angle)     ...... polarVar   = aoa
 # 3. Polar-sweep in phi per given alpha                        ...... polarVar   = phi
@@ -42,113 +42,197 @@
 # imports
 import os, sys, shutil
 from optparse import OptionParser
-sys.path.append(os.environ['SU2_RUN'])
+
+sys.path.append(os.environ["SU2_RUN"])
 import SU2
 import SU2.util.polarSweepLib as psl
 import copy
 import numpy as np
 
+
 def main():
     # Command Line Options
     parser = OptionParser()
-    parser.add_option("-c", "--ctrl", dest="ctrlFile",
-                      help="reads polar control parameters from FILE (default:polarCtrl.in) ",
-                      metavar="FILE", default="polarCtrl.in")
-    parser.add_option("-n", "--partitions", dest="partitions", default=2,
-                      help="number of PARTITIONS", metavar="PARTITIONS")
-    parser.add_option("-i", "--iterations", dest="iterations", default=-1,
-                      help="number of ITERATIONS", metavar="ITERATIONS")
-    parser.add_option("-d", "--dimension", dest="geomDim", default=2,
-                      help="Geometry dimension (2 or 3)", metavar="geomDim")
-    parser.add_option("-w", "--Wind", action="store_true", dest="Wind", default=False,
-                      help=" Wind system (default is body system)")
-    parser.add_option("-v", "--Verbose", action="store_true", dest="verbose", default=False,
-                      help=" Verbose printout (if activated)")
+    parser.add_option(
+        "-c",
+        "--ctrl",
+        dest="ctrlFile",
+        help="reads polar control parameters from FILE (default:polarCtrl.in) ",
+        metavar="FILE",
+        default="polarCtrl.in",
+    )
+    parser.add_option(
+        "-n",
+        "--partitions",
+        dest="partitions",
+        default=2,
+        help="number of PARTITIONS",
+        metavar="PARTITIONS",
+    )
+    parser.add_option(
+        "-i",
+        "--iterations",
+        dest="iterations",
+        default=-1,
+        help="number of ITERATIONS",
+        metavar="ITERATIONS",
+    )
+    parser.add_option(
+        "-d",
+        "--dimension",
+        dest="geomDim",
+        default=2,
+        help="Geometry dimension (2 or 3)",
+        metavar="geomDim",
+    )
+    parser.add_option(
+        "-w",
+        "--Wind",
+        action="store_true",
+        dest="Wind",
+        default=False,
+        help=" Wind system (default is body system)",
+    )
+    parser.add_option(
+        "-v",
+        "--Verbose",
+        action="store_true",
+        dest="verbose",
+        default=False,
+        help=" Verbose printout (if activated)",
+    )
 
     (options, args) = parser.parse_args()
     options.partitions = int(options.partitions)
     options.iterations = int(options.iterations)
     options.geomDim = int(options.geomDim)
 
-    d2r = np.pi/180
+    d2r = np.pi / 180
     #
     sweepOption = []
-    sweepOption.append(' Polar sweep type: 1. Sweep in AOA per given roll angle')
-    sweepOption.append(' Polar sweep type: 2. Sweep in AOA per given sideslip-angle')
-    sweepOption.append(' Polar sweep type: 3. Sweep in phi per given AOA')
-    sweepOption.append(' Polar sweep type: 4. Mach ramp (single- value AOA and  sideslip-angle')
+    sweepOption.append(" Polar sweep type: 1. Sweep in AOA per given roll angle")
+    sweepOption.append(" Polar sweep type: 2. Sweep in AOA per given sideslip-angle")
+    sweepOption.append(" Polar sweep type: 3. Sweep in phi per given AOA")
+    sweepOption.append(
+        " Polar sweep type: 4. Mach ramp (single- value AOA and  sideslip-angle"
+    )
 
     #
-    #--------------- now read the parameters control file and parse it
+    # --------------- now read the parameters control file and parse it
 
-    fc = open(options.ctrlFile, 'r')
+    fc = open(options.ctrlFile, "r")
     ctrl = fc.readlines()
     nc = np.size(ctrl)
     fc.close()
 
-    print(str(nc)+" lines read from control file: "+options.ctrlFile)
-
-    PA, polarSweepType, velDirOption, nAlpha, nBeta, nPhi, nMach, \
-        alpha, beta, phi, MachList, polarVar = \
-                                               psl.setPolaraType(ctrl, nc, options.verbose)
+    print(str(nc) + " lines read from control file: " + options.ctrlFile)
+
+    (
+        PA,
+        polarSweepType,
+        velDirOption,
+        nAlpha,
+        nBeta,
+        nPhi,
+        nMach,
+        alpha,
+        beta,
+        phi,
+        MachList,
+        polarVar,
+    ) = psl.setPolaraType(ctrl, nc, options.verbose)
 
     if options.verbose:
-        velDirOptionLegend = ['V(alpha,phi)', 'V(alpha,beta)']
-        print('>>>  Control file details: Pitch axis is '+\
-              PA+'. Polar sweep type is '+str(polarSweepType)+\
-              '; polarVar = '+polarVar)
-        print('>>>  Velocity definiton: '+velDirOptionLegend[velDirOption-1])
-        print('>>>  nAalpha = '+str(nAlpha)+'; nBeta = '+str(nBeta)+\
-              '; nPhi = '+str(nPhi)+'; nMach = '+str(nMach))
+        velDirOptionLegend = ["V(alpha,phi)", "V(alpha,beta)"]
+        print(
+            ">>>  Control file details: Pitch axis is "
+            + PA
+            + ". Polar sweep type is "
+            + str(polarSweepType)
+            + "; polarVar = "
+            + polarVar
+        )
+        print(">>>  Velocity definiton: " + velDirOptionLegend[velDirOption - 1])
+        print(
+            ">>>  nAalpha = "
+            + str(nAlpha)
+            + "; nBeta = "
+            + str(nBeta)
+            + "; nPhi = "
+            + str(nPhi)
+            + "; nMach = "
+            + str(nMach)
+        )
     if polarSweepType < 4:
         nPolara = max(nAlpha, nPhi)
     else:
         nPolara = nMach
 
-    #-------------Configuration base file ----------------------
-    inputbaseFileString = 'input base file'
+    # -------------Configuration base file ----------------------
+    inputbaseFileString = "input base file"
     keyWordInputbaseFile = inputbaseFileString.lower()
     iBaseInputF = psl.parLocator(keyWordInputbaseFile, ctrl, nc, -1, options.verbose)
     bIFLine = ctrl[iBaseInputF]
-    icol = bIFLine.index(':')
-    sBIF = bIFLine[icol+1:]
-    inputbaseFile = sBIF.strip(' ')
-    inputbaseFile = inputbaseFile.strip('\n')
-
-    print(' ')
-    print('--------------------------------------------------------------------------------------')
-    print(' ')
-    print('Configuration file: ' + inputbaseFile)
-    print('PolarSweepType = '+str(polarSweepType)+' Polar sweep in '+polarVar+' using '+\
-          str(nPolara)+' angles/Mach No ')
-    print(' ')
-    print('--------------------------------------------------------------------------------------')
-    print(' ')
+    icol = bIFLine.index(":")
+    sBIF = bIFLine[icol + 1 :]
+    inputbaseFile = sBIF.strip(" ")
+    inputbaseFile = inputbaseFile.strip("\n")
+
+    print(" ")
+    print(
+        "--------------------------------------------------------------------------------------"
+    )
+    print(" ")
+    print("Configuration file: " + inputbaseFile)
+    print(
+        "PolarSweepType = "
+        + str(polarSweepType)
+        + " Polar sweep in "
+        + polarVar
+        + " using "
+        + str(nPolara)
+        + " angles/Mach No "
+    )
+    print(" ")
+    print(
+        "--------------------------------------------------------------------------------------"
+    )
+    print(" ")
 
     if polarSweepType == 4:
-        nPolara = 1 # prevent angles inner loop
+        nPolara = 1  # prevent angles inner loop
     if options.geomDim not in [2, 3]:
-        raise SystemExit('ERROR: dimension can be either 2 or 3 (-d parameter)  ')
+        raise SystemExit("ERROR: dimension can be either 2 or 3 (-d parameter)  ")
 
     if options.Wind:
-        outSystem = 'Wind'
+        outSystem = "Wind"
     else:
-        outSystem = 'Body'
+        outSystem = "Body"
 
     print(" ")
-    print("===============================================================================")
-    print("   Polar sweep in "+str(options.geomDim)+"D ; output in "+outSystem+" system")
-    print("===============================================================================")
+    print(
+        "==============================================================================="
+    )
+    print(
+        "   Polar sweep in "
+        + str(options.geomDim)
+        + "D ; output in "
+        + outSystem
+        + " system"
+    )
+    print(
+        "==============================================================================="
+    )
     print(" ")
 
     # load config, start state
     config = SU2.io.Config(inputbaseFile)
     state = SU2.io.State()
     # Set SU2 defaults units, if definitions are not included in the cfg file
-    if 'SYSTEM_MEASUREMENTS' not in config:
-        config.SYSTEM_MEASUREMENTS = 'SI'
-    if config.SOLVER == 'NAVIER_STOKES':
-        if 'REYNOLDS_LENGTH' not in config:
+    if "SYSTEM_MEASUREMENTS" not in config:
+        config.SYSTEM_MEASUREMENTS = "SI"
+    if config.SOLVER == "NAVIER_STOKES":
+        if "REYNOLDS_LENGTH" not in config:
             config.REYNOLDS_LENGTH = 1.0
 
     # prepare config
@@ -164,14 +248,14 @@ def main():
     results = SU2.util.bunch()
 
     if nMach == 0:
-        if 'MACH_NUMBER' in config:
+        if "MACH_NUMBER" in config:
             MachList.append(config.MACH_NUMBER)
         else:
             MachList.append(0.5)
         nMach = 1
 
     if nAlpha == 0:
-        if 'AOA' in config:
+        if "AOA" in config:
             alpha.append(config.AOA)
         else:
             alpha.append(0.0)
@@ -186,30 +270,30 @@ def main():
 
     if nBeta == 0:
         if noPhi_in_CTRL:
-            if 'SIDESLIP_ANGLE' in config:
+            if "SIDESLIP_ANGLE" in config:
                 beta.append(config.SIDESLIP_ANGLE)
             else:
                 beta.append(0.0)
             nBeta = 1
         else:
             if polarSweepType < 4:  # alpha sweep with phi set
-                tAlpha = [np.tan(d2r*x) for x in alpha]
-                tPhi = [np.tan(d2r*x) for x in phi]
-                tb = [x*y  for y in tAlpha for x in tPhi]
-                beta = [np.arctan(x)/d2r for x in tb]
+                tAlpha = [np.tan(d2r * x) for x in alpha]
+                tPhi = [np.tan(d2r * x) for x in phi]
+                tb = [x * y for y in tAlpha for x in tPhi]
+                beta = [np.arctan(x) / d2r for x in tb]
                 nBeta = np.size(beta)
-            else:   # Mach ramp
-                if 'SIDESLIP_ANGLE' in config:
+            else:  # Mach ramp
+                if "SIDESLIP_ANGLE" in config:
                     beta.append(config.SIDESLIP_ANGLE)
                 else:
                     beta.append(0.0)
                 nBeta = 1
 
     if options.verbose:
-        print('>>> alpha: '+str(alpha))
-        print('>>> beta:  '+str(beta))
-        print('>>> phi:   '+str(phi))
-        print('>>> Mach   '+str(MachList))
+        print(">>> alpha: " + str(alpha))
+        print(">>> beta:  " + str(beta))
+        print(">>> phi:   " + str(phi))
+        print(">>> Mach   " + str(MachList))
 
     results.AOA = alpha
     results.MACH = MachList
@@ -232,96 +316,104 @@ def main():
     results.MOMENT_Z = []
 
     if polarSweepType == 4:
-        outFile = 'machRamp_aoa' + str(alpha[0]) + '.dat'
+        outFile = "machRamp_aoa" + str(alpha[0]) + ".dat"
     else:
-        outFile = 'Polar_M' + str(MachList[0]) + '.dat'
+        outFile = "Polar_M" + str(MachList[0]) + ".dat"
     bufsize = 12
     #
-    #----------- Prepare output header ---------------
+    # ----------- Prepare output header ---------------
     #
-    if config.SYSTEM_MEASUREMENTS == 'SI':
-        length_dimension = 'm'
+    if config.SYSTEM_MEASUREMENTS == "SI":
+        length_dimension = "m"
     else:
-        length_dimension = 'in'
-    f = open(outFile, 'w', bufsize)
+        length_dimension = "in"
+    f = open(outFile, "w", bufsize)
     if options.verbose:
-        print('Opening polar sweep file: ' + outFile)
-    f.write('% \n%  Main coefficients for a polar sweep \n% \n%  ')
-    f.write(sweepOption[polarSweepType-1])
+        print("Opening polar sweep file: " + outFile)
+    f.write("% \n%  Main coefficients for a polar sweep \n% \n%  ")
+    f.write(sweepOption[polarSweepType - 1])
     if polarSweepType == 1:
-        satxt = '  ;  Roll angle = %7.2f '%(phi[0])
+        satxt = "  ;  Roll angle = %7.2f " % (phi[0])
     elif polarSweepType == 2:
-        satxt = '  ;  Sideslip angle = %7.2f '%(beta[0])
+        satxt = "  ;  Sideslip angle = %7.2f " % (beta[0])
     elif polarSweepType == 3:
-        satxt = ' ;   AOA = %7.2f '%(alpha[0])
+        satxt = " ;   AOA = %7.2f " % (alpha[0])
     elif polarSweepType == 4:
-        satxt = '  ;  AOA = %7.2f Side slip angle = %7.2f ; '%(alpha[0], beta[0])
+        satxt = "  ;  AOA = %7.2f Side slip angle = %7.2f ; " % (alpha[0], beta[0])
     f.write(satxt)
-    f.write('\n% \n')
-    f.write('% ================== Reference parameteres ======================\n%\n')
+    f.write("\n% \n")
+    f.write("% ================== Reference parameteres ======================\n%\n")
     XR = config.REF_ORIGIN_MOMENT_X
     YR = config.REF_ORIGIN_MOMENT_Y
     ZR = config.REF_ORIGIN_MOMENT_Z
-    f.write('%  Reference point for moments   : [ ')
-    line_text = '%s , %s , %s ]  [ %s ] '%(XR, YR, ZR, length_dimension)
+    f.write("%  Reference point for moments   : [ ")
+    line_text = "%s , %s , %s ]  [ %s ] " % (XR, YR, ZR, length_dimension)
     f.write(line_text)
-    f.write('\n')
-    f.write('%  Reference area and length: ')
-    line_text = 'Aref : %s Lref : %s  [ %s ] '%(config.REF_AREA, config.REF_AREA, length_dimension)
+    f.write("\n")
+    f.write("%  Reference area and length: ")
+    line_text = "Aref : %s Lref : %s  [ %s ] " % (
+        config.REF_AREA,
+        config.REF_AREA,
+        length_dimension,
+    )
     f.write(line_text)
-    f.write('\n%  ')
-    line_text = 'Mach : %7.2f  ,  '%(config.MACH_NUMBER)
+    f.write("\n%  ")
+    line_text = "Mach : %7.2f  ,  " % (config.MACH_NUMBER)
     f.write(line_text)
-    if config.SOLVER == 'NAVIER_STOKES':
-        line_text = 'Reynolds Number  :  %s   '%(config.REYNOLDS_NUMBER)
+    if config.SOLVER == "NAVIER_STOKES":
+        line_text = "Reynolds Number  :  %s   " % (config.REYNOLDS_NUMBER)
         f.write(line_text)
-        line_text = 'Reynolds length :   %s   [ %s ] '%(config.REYNOLDS_LENGTH, length_dimension)
+        line_text = "Reynolds length :   %s   [ %s ] " % (
+            config.REYNOLDS_LENGTH,
+            length_dimension,
+        )
     else:
-        line_text = 'Physical problem : %s '%( config.SOLVER)
+        line_text = "Physical problem : %s " % (config.SOLVER)
     f.write(line_text)
-    f.write('\n%  ')
-    rho = float(config.FREESTREAM_PRESSURE)/\
-          (float(config.GAS_CONSTANT)*float(config.FREESTREAM_TEMPERATURE))
-    line_text = 'Reference pressure : %s  ,'%(config.FREESTREAM_PRESSURE)
+    f.write("\n%  ")
+    rho = float(config.FREESTREAM_PRESSURE) / (
+        float(config.GAS_CONSTANT) * float(config.FREESTREAM_TEMPERATURE)
+    )
+    line_text = "Reference pressure : %s  ," % (config.FREESTREAM_PRESSURE)
     f.write(line_text)
-    line_text = '  Reference density : %7.4f  , '%(rho)
+    line_text = "  Reference density : %7.4f  , " % (rho)
     f.write(line_text)
-    line_text = '  Reference Temperature : %s '%(config.FREESTREAM_TEMPERATURE)
+    line_text = "  Reference Temperature : %s " % (config.FREESTREAM_TEMPERATURE)
     f.write(line_text)
-    f.write('\n%  ')
-    line_text = 'Constant specific heat ratio  : %s  ,   '%(config.GAMMA_VALUE)
+    f.write("\n%  ")
+    line_text = "Constant specific heat ratio  : %s  ,   " % (config.GAMMA_VALUE)
     f.write(line_text)
-    line_text = 'Gas constant :  %s  '%(config.GAS_CONSTANT)
+    line_text = "Gas constant :  %s  " % (config.GAS_CONSTANT)
     f.write(line_text)
-    f.write('\n%  ')
-    line_text = 'Grid file :  %s  '%(config.MESH_FILENAME)
+    f.write("\n%  ")
+    line_text = "Grid file :  %s  " % (config.MESH_FILENAME)
     f.write(line_text)
-    f.write('\n%  ')
+    f.write("\n%  ")
     symmmetry_exists = False
-    if 'MARKER_SYM' in config:
-        if config.MARKER_SYM != 'NONE':
+    if "MARKER_SYM" in config:
+        if config.MARKER_SYM != "NONE":
             symmmetry_exists = True
     if symmmetry_exists:
-        line_text = 'Symmetry surface :  yes'
+        line_text = "Symmetry surface :  yes"
     else:
-        line_text = 'Symmetry surface :  no'
+        line_text = "Symmetry surface :  no"
     f.write(line_text)
-    f.write('\n% \n')
+    f.write("\n% \n")
     # -----------------   end reference parameter section --------------
     if options.Wind:
-        f.write('% AOA,  Mach,       CL,         CD,            ')
+        f.write("% AOA,  Mach,       CL,         CD,            ")
         if options.geomDim == 3:
-            f.write('CY,           ')
+            f.write("CY,           ")
     else:
         if options.geomDim == 2:
-            f.write('% AOA,  Mach,       CX,          CY,            ')
+            f.write("% AOA,  Mach,       CX,          CY,            ")
         else:
-            f.write('% AOA,  Mach,       CX,          CZ,          CY,            ')
+            f.write("% AOA,  Mach,       CX,          CZ,          CY,            ")
 
     if options.geomDim == 3:
-        f.write('Cmx,         Cmz,           Cmy  \n')
+        f.write("Cmx,         Cmz,           Cmy  \n")
     else:
-        f.write('        Cmz \n')
+        f.write("        Cmz \n")
 
     firstSweepPoint = True
     # iterate mach
@@ -340,35 +432,39 @@ def main():
                 SIDESLIP_ANGLE = beta[0]
 
             if options.verbose:
-                print('Sweep step '+str(j)+': Mach = '+str(MachNumber)+\
-                      ', aoa = ', str(AngleAttack)+', beta = '+str(SIDESLIP_ANGLE))
+                print(
+                    "Sweep step " + str(j) + ": Mach = " + str(MachNumber) + ", aoa = ",
+                    str(AngleAttack) + ", beta = " + str(SIDESLIP_ANGLE),
+                )
 
             # local config and state
             konfig = copy.deepcopy(config)
             # enable restart in polar sweep
-            konfig.DISCARD_INFILES = 'YES'
+            konfig.DISCARD_INFILES = "YES"
             ztate = copy.deepcopy(state)
             #
             # The eval functions below requires definition of various optimization
             # variables, though we are handling here only a direct solution.
             # So, if they are missing in the cfg file (and only then), some dummy values are
             # introduced here
-            if  'OBJECTIVE_FUNCTION' not in konfig:
-                konfig.OBJECTIVE_FUNCTION = 'DRAG'
-            if 'DV_KIND' not in konfig:
-                konfig.DV_KIND = ['FFD_SETTING']
-            if 'DV_PARAM' not in konfig:
-                konfig.DV_PARAM = {'FFDTAG': ['1'], 'PARAM': [[0.0, 0.5]], 'SIZE': [1]}
-            if 'DEFINITION_DV' not in konfig:
-                konfig.DEFINITION_DV = {'FFDTAG': [[]],
-                                        'KIND': ['HICKS_HENNE'],
-                                        'MARKER': [['WING']],
-                                        'PARAM': [[0.0, 0.05]],
-                                        'SCALE': [1.0],
-                                        'SIZE': [1]}
-            if 'OPT_OBJECTIVE' not in konfig:
+            if "OBJECTIVE_FUNCTION" not in konfig:
+                konfig.OBJECTIVE_FUNCTION = "DRAG"
+            if "DV_KIND" not in konfig:
+                konfig.DV_KIND = ["FFD_SETTING"]
+            if "DV_PARAM" not in konfig:
+                konfig.DV_PARAM = {"FFDTAG": ["1"], "PARAM": [[0.0, 0.5]], "SIZE": [1]}
+            if "DEFINITION_DV" not in konfig:
+                konfig.DEFINITION_DV = {
+                    "FFDTAG": [[]],
+                    "KIND": ["HICKS_HENNE"],
+                    "MARKER": [["WING"]],
+                    "PARAM": [[0.0, 0.05]],
+                    "SCALE": [1.0],
+                    "SIZE": [1],
+                }
+            if "OPT_OBJECTIVE" not in konfig:
                 obj = {}
-                obj['DRAG'] = {'SCALE':1.e-2, 'OBJTYPE':'DEFAULT', 'MARKER': 'None'}
+                obj["DRAG"] = {"SCALE": 1.0e-2, "OBJTYPE": "DEFAULT", "MARKER": "None"}
                 konfig.OPT_OBJECTIVE = obj
             #
             # --------- end of dummy optimization variables definition section ---------
@@ -378,42 +474,42 @@ def main():
             konfig.AOA = AngleAttack
             konfig.SIDESLIP_ANGLE = SIDESLIP_ANGLE
             konfig.MACH_NUMBER = MachNumber
-            caseName = 'DIRECT_M_' + str(MachNumber) + '_AOA_' + str(AngleAttack)
-            print('Mach = ', konfig.MACH_NUMBER, 'AOA = ', konfig.AOA)
-            print('case :' + caseName)
+            caseName = "DIRECT_M_" + str(MachNumber) + "_AOA_" + str(AngleAttack)
+            print("Mach = ", konfig.MACH_NUMBER, "AOA = ", konfig.AOA)
+            print("case :" + caseName)
 
             if firstSweepPoint:
                 # if caseName exists copy the restart file from it for run continuation
                 # Continue from previous sweep point if this is not he first
                 if os.path.isdir(caseName):
-                    command = 'cp '+caseName+'/'+config.SOLUTION_FILENAME+' .'
+                    command = "cp " + caseName + "/" + config.SOLUTION_FILENAME + " ."
                     if options.verbose:
                         print(command)
-                    shutil.copy2(caseName+'/'+config.SOLUTION_FILENAME, os.getcwd())
-                    konfig.RESTART_SOL = 'YES'
+                    shutil.copy2(caseName + "/" + config.SOLUTION_FILENAME, os.getcwd())
+                    konfig.RESTART_SOL = "YES"
                 else:
-                    konfig.RESTART_SOL = 'NO'
+                    konfig.RESTART_SOL = "NO"
                 firstSweepPoint = False
             else:
-                konfig.RESTART_SOL = 'YES'
-            if  konfig.RESTART_SOL == 'YES':
+                konfig.RESTART_SOL = "YES"
+            if konfig.RESTART_SOL == "YES":
                 ztate.FILES.DIRECT = config.SOLUTION_FILENAME
             # run su2
             if options.Wind:
-                drag = SU2.eval.func('DRAG', konfig, ztate)
-                lift = SU2.eval.func('LIFT', konfig, ztate)
+                drag = SU2.eval.func("DRAG", konfig, ztate)
+                lift = SU2.eval.func("LIFT", konfig, ztate)
                 if options.geomDim == 3:
-                    sideforce = SU2.eval.func('SIDEFORCE', konfig, ztate)
+                    sideforce = SU2.eval.func("SIDEFORCE", konfig, ztate)
             else:
-                force_x = SU2.eval.func('FORCE_X', konfig, ztate)
-                force_y = SU2.eval.func('FORCE_Y', konfig, ztate)
+                force_x = SU2.eval.func("FORCE_X", konfig, ztate)
+                force_y = SU2.eval.func("FORCE_Y", konfig, ztate)
                 if options.geomDim == 3:
-                    force_z = SU2.eval.func('FORCE_Z', konfig, ztate)
+                    force_z = SU2.eval.func("FORCE_Z", konfig, ztate)
 
-            momentz = SU2.eval.func('MOMENT_Z', konfig, ztate)
+            momentz = SU2.eval.func("MOMENT_Z", konfig, ztate)
             if options.geomDim == 3:
-                momentx = SU2.eval.func('MOMENT_X', konfig, ztate)
-                momenty = SU2.eval.func('MOMENT_Y', konfig, ztate)
+                momentx = SU2.eval.func("MOMENT_X", konfig, ztate)
+                momenty = SU2.eval.func("MOMENT_Y", konfig, ztate)
 
             # append results
 
@@ -433,64 +529,73 @@ def main():
                 results.MOMENT_X.append(momentx)
                 results.MOMENT_Y.append(momenty)
 
-            output = '  ' + str(AngleAttack) + ",   "+str(MachNumber)+", "
+            output = "  " + str(AngleAttack) + ",   " + str(MachNumber) + ", "
 
             if options.Wind:
-                output = output+ str(lift) + ", " + str(drag)
+                output = output + str(lift) + ", " + str(drag)
                 if options.geomDim == 3:
-                    output = output+", "+str(sideforce)
+                    output = output + ", " + str(sideforce)
             else:
                 if options.geomDim == 2:
-                    output = output+ str(force_x) + ", " + str(force_y)
+                    output = output + str(force_x) + ", " + str(force_y)
                 else:
-                    output = output + str(force_x) + ", " + str(force_z) + ", " + str(force_y)
+                    output = (
+                        output
+                        + str(force_x)
+                        + ", "
+                        + str(force_z)
+                        + ", "
+                        + str(force_y)
+                    )
             if options.geomDim == 3:
                 output = output + ", " + str(momentx) + ", " + str(momentz) + ", "
                 output = output + str(momenty) + " \n"
             else:
-                output = output+", "+str(momentz)+" \n"
+                output = output + ", " + str(momentz) + " \n"
 
             f.write(output)
             # save data
-            SU2.io.save_data('results.pkl', results)
-            shutil.copy2('results.pkl', 'DIRECT')
-            shutil.copy2(config.SOLUTION_FILENAME, 'DIRECT')
+            SU2.io.save_data("results.pkl", results)
+            shutil.copy2("results.pkl", "DIRECT")
+            shutil.copy2(config.SOLUTION_FILENAME, "DIRECT")
 
             if os.path.isdir(caseName):
-                command = 'cat '+caseName+\
-                          '/history_direct.dat DIRECT/history_direct.dat > tmp && mv tmp '+\
-                          'DIRECT/history_direct.dat'
+                command = (
+                    "cat "
+                    + caseName
+                    + "/history_direct.dat DIRECT/history_direct.dat > tmp && mv tmp "
+                    + "DIRECT/history_direct.dat"
+                )
                 if options.verbose:
                     print(command)
                 os.system(command)
                 shutil.rmtree(caseName)
 
-            command = 'cp -p -R DIRECT '+caseName
+            command = "cp -p -R DIRECT " + caseName
             if options.verbose:
                 print(command)
-            shutil.copytree('DIRECT', caseName)
+            shutil.copytree("DIRECT", caseName)
 
     # Close open file
     f.close()
-    if os.path.isdir('DIRECT'):
-        shutil.rmtree('DIRECT')
+    if os.path.isdir("DIRECT"):
+        shutil.rmtree("DIRECT")
     if os.path.isfile(config.SOLUTION_FILENAME):
         os.remove(config.SOLUTION_FILENAME)
-    if os.path.isfile('results.pkl'):
-        os.remove('results.pkl')
-    print('Post sweep cleanup completed')
+    if os.path.isfile("results.pkl"):
+        os.remove("results.pkl")
+    print("Post sweep cleanup completed")
 
     #         sys.exit(0)
 
-    #----------------------------------------------------------#
+    # ----------------------------------------------------------#
 
     #: for each angle
 
     # plotting
-    #plt.figure()
-    #plt.plot( results.MACH_NUMBER, results.AOA , results.LIFT , results.DRAG )
-    #plt.show()
-
+    # plt.figure()
+    # plt.plot( results.MACH_NUMBER, results.AOA , results.LIFT , results.DRAG )
+    # plt.show()
 
 
 if __name__ == "__main__":
diff --git a/SU2_PY/compute_stability.py b/SU2_PY/compute_stability.py
index d2284274df0..b727782d7de 100755
--- a/SU2_PY/compute_stability.py
+++ b/SU2_PY/compute_stability.py
@@ -34,35 +34,50 @@
 
 # Command Line Options
 parser = OptionParser()
-parser.add_option("-f", "--file", dest="filename",
-                  help="read config from FILE", metavar="FILE")
-parser.add_option("-n", "--partitions", dest="partitions", default=2,
-                  help="number of PARTITIONS", metavar="PARTITIONS")
-parser.add_option("-i", "--iterations", dest="iterations", default=99999,
-                  help="number of ITERATIONS", metavar="ITERATIONS")
+parser.add_option(
+    "-f", "--file", dest="filename", help="read config from FILE", metavar="FILE"
+)
+parser.add_option(
+    "-n",
+    "--partitions",
+    dest="partitions",
+    default=2,
+    help="number of PARTITIONS",
+    metavar="PARTITIONS",
+)
+parser.add_option(
+    "-i",
+    "--iterations",
+    dest="iterations",
+    default=99999,
+    help="number of ITERATIONS",
+    metavar="ITERATIONS",
+)
 
-(options, args)=parser.parse_args()
-options.partitions = int( options.partitions )
-options.iterations = int( options.iterations )
+(options, args) = parser.parse_args()
+options.partitions = int(options.partitions)
+options.iterations = int(options.iterations)
 
 # load config, start state
 config = SU2.io.Config(options.filename)
-state  = SU2.io.State()
+state = SU2.io.State()
 
 # prepare config
 config.NUMBER_PART = options.partitions
-config.EXT_ITER    = options.iterations
+config.EXT_ITER = options.iterations
 
 # find solution files if they exist
 state.find_files(config)
 
 # run su2
-drag_alpha = SU2.eval.func('D_DRAG_D_ALPHA',config,state)
-moment_y_alpha= SU2.eval.func('D_MOMENT_Z_D_ALPHA',config,state)
+drag_alpha = SU2.eval.func("D_DRAG_D_ALPHA", config, state)
+moment_y_alpha = SU2.eval.func("D_MOMENT_Z_D_ALPHA", config, state)
 
-grad_moment_y_alpha= SU2.eval.grad('D_MOMENT_Z_D_ALPHA','CONTINUOUS_ADJOINT',config,state)
+grad_moment_y_alpha = SU2.eval.grad(
+    "D_MOMENT_Z_D_ALPHA", "CONTINUOUS_ADJOINT", config, state
+)
 
-print('D_DRAG_D_ALPHA     =' , drag_alpha)
-print('D_MOMENT_Y_D_ALPHA =' , moment_y_alpha)
+print("D_DRAG_D_ALPHA     =", drag_alpha)
+print("D_MOMENT_Y_D_ALPHA =", moment_y_alpha)
 
-print('DD_MOMENT_Y_D_ALPHA_D_X =', grad_moment_y_alpha)
+print("DD_MOMENT_Y_D_ALPHA_D_X =", grad_moment_y_alpha)
diff --git a/SU2_PY/compute_uncertainty.py b/SU2_PY/compute_uncertainty.py
index 3d2f0905aeb..1184719deef 100755
--- a/SU2_PY/compute_uncertainty.py
+++ b/SU2_PY/compute_uncertainty.py
@@ -32,57 +32,81 @@
 import shutil
 import copy
 import os.path
-sys.path.append(os.environ['SU2_RUN'])
+
+sys.path.append(os.environ["SU2_RUN"])
 import SU2
 
+
 def main():
-# Command Line Options
+    # Command Line Options
     parser = OptionParser()
-    parser.add_option("-f", "--file", dest="filename",
-                      help="read config from FILE", metavar="FILE")
-    parser.add_option("-n", "--partitions", dest="partitions", default=1,
-                      help="number of PARTITIONS", metavar="PARTITIONS")
-    parser.add_option("-u", "--underRelaxation", dest="uq_urlx", default=0.1,
-                      help="under relaxation factor", metavar="UQ_URLX")
-    parser.add_option("-b", "--deltaB", dest="uq_delta_b", default=1.0,
-                      help="magnitude of perturbation", metavar="UQ_DELTA_B")
-
-    (options, args)=parser.parse_args()
-    options.partitions = int( options.partitions )
+    parser.add_option(
+        "-f", "--file", dest="filename", help="read config from FILE", metavar="FILE"
+    )
+    parser.add_option(
+        "-n",
+        "--partitions",
+        dest="partitions",
+        default=1,
+        help="number of PARTITIONS",
+        metavar="PARTITIONS",
+    )
+    parser.add_option(
+        "-u",
+        "--underRelaxation",
+        dest="uq_urlx",
+        default=0.1,
+        help="under relaxation factor",
+        metavar="UQ_URLX",
+    )
+    parser.add_option(
+        "-b",
+        "--deltaB",
+        dest="uq_delta_b",
+        default=1.0,
+        help="magnitude of perturbation",
+        metavar="UQ_DELTA_B",
+    )
+
+    (options, args) = parser.parse_args()
+    options.partitions = int(options.partitions)
     # check the typecasting
-    options.beta_delta = float( options.uq_delta_b )
+    options.beta_delta = float(options.uq_delta_b)
     options.urlx = float(options.uq_urlx)
 
     # load config, start state
     config = SU2.io.Config(options.filename)
-    state  = SU2.io.State()
+    state = SU2.io.State()
 
     # find solution files if they exist
     state.find_files(config)
 
     # prepare config
     config.NUMBER_PART = options.partitions
-    config.SST_OPTIONS = 'UQ'
+    config.SST_OPTIONS = "UQ"
     config.UQ_DELTA_B = options.beta_delta
     config.UQ_URLX = options.urlx
-    config.UQ_PERMUTE = 'NO'
-
+    config.UQ_PERMUTE = "NO"
 
     # perform eigenvalue perturbations
-    for comp in range(1,4):
-        print('\n\n =================== Performing ' + str(comp) + '  Component Perturbation =================== \n\n')
+    for comp in range(1, 4):
+        print(
+            "\n\n =================== Performing "
+            + str(comp)
+            + "  Component Perturbation =================== \n\n"
+        )
 
         # make copies
         konfig = copy.deepcopy(config)
-        ztate  = copy.deepcopy(state)
+        ztate = copy.deepcopy(state)
 
         # set componentality
         konfig.UQ_COMPONENT = comp
 
         # send output to a folder
-        folderName = str(comp)+'c/'
+        folderName = str(comp) + "c/"
         if os.path.isdir(folderName):
-           shutil.rmtree(folderName)
+            shutil.rmtree(folderName)
         os.mkdir(folderName)
         sendOutputFiles(konfig, folderName)
 
@@ -95,19 +119,20 @@ def main():
         info = SU2.run.merge(konfig)
         ztate.update(info)
 
-
-    print('\n\n =================== Performing p1c1 Component Perturbation =================== \n\n')
+    print(
+        "\n\n =================== Performing p1c1 Component Perturbation =================== \n\n"
+    )
 
     # make copies
     konfig = copy.deepcopy(config)
-    ztate  = copy.deepcopy(state)
+    ztate = copy.deepcopy(state)
 
     # set componentality
     konfig.UQ_COMPONENT = 1
-    konfig.UQ_PERMUTE = 'YES'
+    konfig.UQ_PERMUTE = "YES"
 
     # send output to a folder
-    folderName = 'p1c1/'
+    folderName = "p1c1/"
     if os.path.isdir(folderName):
         shutil.rmtree(folderName)
     os.mkdir(folderName)
@@ -122,18 +147,20 @@ def main():
     info = SU2.run.merge(konfig)
     state.update(info)
 
-    print('\n\n =================== Performing p1c2 Component Perturbation =================== \n\n')
+    print(
+        "\n\n =================== Performing p1c2 Component Perturbation =================== \n\n"
+    )
 
     # make copies
     konfig = copy.deepcopy(config)
-    ztate  = copy.deepcopy(state)
+    ztate = copy.deepcopy(state)
 
     # set componentality
     konfig.UQ_COMPONENT = 2
-    konfig.UQ_PERMUTE = 'YES'
+    konfig.UQ_PERMUTE = "YES"
 
     # send output to a folder
-    folderName = 'p1c2/'
+    folderName = "p1c2/"
     if os.path.isdir(folderName):
         shutil.rmtree(folderName)
     os.mkdir(folderName)
@@ -148,9 +175,10 @@ def main():
     info = SU2.run.merge(konfig)
     ztate.update(info)
 
-def sendOutputFiles( config, folderName = ''):
+
+def sendOutputFiles(config, folderName=""):
     config.CONV_FILENAME = folderName + config.CONV_FILENAME
-    #config.BREAKDOWN_FILENAME = folderName + config.BREAKDOWN_FILENAME
+    # config.BREAKDOWN_FILENAME = folderName + config.BREAKDOWN_FILENAME
     config.RESTART_FILENAME = folderName + config.RESTART_FILENAME
     config.VOLUME_FILENAME = folderName + config.VOLUME_FILENAME
     config.SURFACE_FILENAME = folderName + config.SURFACE_FILENAME
diff --git a/SU2_PY/config_gui.py b/SU2_PY/config_gui.py
index 3cf13878c7a..293a6c92c9f 100755
--- a/SU2_PY/config_gui.py
+++ b/SU2_PY/config_gui.py
@@ -38,282 +38,328 @@
 # Values of ctrldict are lists (optlist) of lists (option_data)
 # option_data takes the form [option_name, option_value, StaticText,Control]
 
-class YesNoBox(wx.CheckBox):
-  '''The regular checkbox returns True or False, this one returns YES or NO to match the SU2 config format.'''
-
-  def __init__(self, parent, *args, **kwargs):
-    wx.CheckBox.__init__(self, parent, *args, **kwargs)
-
-  def GetValue(self):
-    if self.Value:
-      return "YES"
-    else:
-      return "NO"
-
-  def SetValue(self,stringval):
-    if stringval=="YES":
-      self.Value=True
-    else:
-      self.Value=False
-
-class LabeledComboBox():
-  '''Wrap a StaticText and TextCtrl into a single object'''
-
-  def __init__(self,parent,option_name,txtlabel,option_default,option_values,option_type,option_description):
-    self.label       = wx.StaticText(parent,label=txtlabel+", "+option_type)
-    self.option_name = option_name
-    self.control     = wx.ComboBox(parent,value=option_default,choices=option_values)
-    self.control.SetSize((400,20))
-    self.sizer       = wx.BoxSizer(wx.HORIZONTAL)
-    self.sizer.Add(self.label,wx.EXPAND)
-    self.sizer.AddSpacer(20)
-    self.sizer.Add(self.control,wx.EXPAND)
-    self.sizer.SetMinSize((400,20))
-
-    self.option_default     = option_default
-    self.option_type        = option_type
-    self.option_description = option_description
-
-  def GetSizer(self):
-    return self.sizer
-
-  def GetValue(self):
-    return self.control.GetValue()
-
-  def SetValue(self,val):
-    self.control.SetValue(val)
 
-  def SetDefaultValue(self):
-    self.control.SetValue(self.option_default)
+class YesNoBox(wx.CheckBox):
+    """The regular checkbox returns True or False, this one returns YES or NO to match the SU2 config format."""
 
-  def GetCtrl(self):
-    return self.control
+    def __init__(self, parent, *args, **kwargs):
+        wx.CheckBox.__init__(self, parent, *args, **kwargs)
 
-class LabeledTextCtrl():
-  '''Wrap a StaticText and TextCtrl into a single object'''
+    def GetValue(self):
+        if self.Value:
+            return "YES"
+        else:
+            return "NO"
 
-  def __init__(self,parent,option_name,txtlabel,option_default,option_type):
-    self.label       = wx.StaticText(parent,label=txtlabel+", "+option_type)
-    self.option_name = option_name
-    self.control     = wx.TextCtrl(parent,value=option_default)
-    self.control.SetSize((400,20))
-    self.sizer       = wx.BoxSizer(wx.HORIZONTAL)
-    self.sizer.Add(self.label,wx.EXPAND)
-    self.sizer.AddSpacer(20)
-    self.sizer.Add(self.control,wx.EXPAND)
-    self.sizer.SetMinSize((400,20))
+    def SetValue(self, stringval):
+        if stringval == "YES":
+            self.Value = True
+        else:
+            self.Value = False
 
-    self.option_default = option_default
-    self.option_type    = option_type
 
-  def GetSizer(self):
-    return self.sizer
+class LabeledComboBox:
+    """Wrap a StaticText and TextCtrl into a single object"""
 
-  def GetValue(self):
-    return self.control.GetValue()
+    def __init__(
+        self,
+        parent,
+        option_name,
+        txtlabel,
+        option_default,
+        option_values,
+        option_type,
+        option_description,
+    ):
+        self.label = wx.StaticText(parent, label=txtlabel + ", " + option_type)
+        self.option_name = option_name
+        self.control = wx.ComboBox(parent, value=option_default, choices=option_values)
+        self.control.SetSize((400, 20))
+        self.sizer = wx.BoxSizer(wx.HORIZONTAL)
+        self.sizer.Add(self.label, wx.EXPAND)
+        self.sizer.AddSpacer(20)
+        self.sizer.Add(self.control, wx.EXPAND)
+        self.sizer.SetMinSize((400, 20))
 
-  def SetValue(self,val):
-    self.control.SetValue(val)
+        self.option_default = option_default
+        self.option_type = option_type
+        self.option_description = option_description
 
-  def SetDefaultValue(self):
-    self.control.SetValue(self.option_default)
+    def GetSizer(self):
+        return self.sizer
 
-  def GetCtrl(self):
-    return self.control
+    def GetValue(self):
+        return self.control.GetValue()
 
-class config_gui(wx.Frame):
-  def __init__(self,option_data):
+    def SetValue(self, val):
+        self.control.SetValue(val)
 
-    # wx Initialization
-    wx.Frame.__init__(self, None, title="SU2 config file editor")
+    def SetDefaultValue(self):
+        self.control.SetValue(self.option_default)
 
-    # Define the main sizers
-    self.frame_sizer  = wx.BoxSizer(wx.HORIZONTAL)
-    self.main_sizer   = wx.BoxSizer(wx.HORIZONTAL)
-    self.left_sizer   = wx.BoxSizer(wx.VERTICAL)
-    self.right_sizer  = wx.BoxSizer(wx.VERTICAL)
+    def GetCtrl(self):
+        return self.control
 
-    # Use a scrolled panel on the right side
-    self.main_panel   = wx.Panel(self)
-    self.scroll_sizer = wx.BoxSizer(wx.VERTICAL)
-    self.right_panel  = sp.ScrolledPanel(self.main_panel,size=(500,500))
-    self.right_panel.SetupScrolling()
 
-    # Left side - list of option categories
-    self.list_ctrl = wx.ListCtrl(self.main_panel,style=wx.LC_REPORT|wx.BORDER_SUNKEN,size=(300,600))
-    self.list_ctrl.InsertColumn(0, 'Option Category')
+class LabeledTextCtrl:
+    """Wrap a StaticText and TextCtrl into a single object"""
 
-    bigfont = wx.Font(20,wx.MODERN,wx.NORMAL,wx.BOLD)
+    def __init__(self, parent, option_name, txtlabel, option_default, option_type):
+        self.label = wx.StaticText(parent, label=txtlabel + ", " + option_type)
+        self.option_name = option_name
+        self.control = wx.TextCtrl(parent, value=option_default)
+        self.control.SetSize((400, 20))
+        self.sizer = wx.BoxSizer(wx.HORIZONTAL)
+        self.sizer.Add(self.label, wx.EXPAND)
+        self.sizer.AddSpacer(20)
+        self.sizer.Add(self.control, wx.EXPAND)
+        self.sizer.SetMinSize((400, 20))
 
-    # Read the option_data and build controls
-    self.ctrldict  = {}
-    self.optlabels = {}
-    for j,category in enumerate(option_data):
+        self.option_default = option_default
+        self.option_type = option_type
 
-      self.list_ctrl.InsertStringItem(j, category)  # Add category to left size list
+    def GetSizer(self):
+        return self.sizer
 
-      self.optlabels[category] = wx.StaticText(self.right_panel,label=category)
-      self.optlabels[category].SetFont(bigfont)
+    def GetValue(self):
+        return self.control.GetValue()
 
-      if j>0:
-        self.scroll_sizer.AddSpacer(20)
-      self.scroll_sizer.Add(self.optlabels[category],wx.EXPAND)
+    def SetValue(self, val):
+        self.control.SetValue(val)
 
-      self.ctrldict[category] = []
-      yctr = 0
-      for j,opt in enumerate(option_data[category]):
-        if opt.option_type in ["EnumOption","MathProblem","SpecialOption","ConvectOption"]:
-          self.ctrldict[category].append(LabeledComboBox(self.right_panel,opt.option_name,opt.option_name,opt.option_default,opt.option_values,opt.option_type,opt.option_description))
-        else:
-          self.ctrldict[category].append(LabeledTextCtrl(self.right_panel,opt.option_name,opt.option_name,opt.option_default,opt.option_type))
-
-      for control in self.ctrldict[category]:
-        self.scroll_sizer.Add(control.GetSizer(),wx.EXPAND)     # Add each control to the sizer
-        self.lastctrl = control.GetCtrl()
-
-    # Set right_panel to scroll vertically
-    self.right_panel.SetSizer(self.scroll_sizer)
-
-    # Set up menu
-    menuBar = wx.MenuBar()
-    m_file = wx.Menu()
-    m_save = m_file.Append(wx.ID_SAVE, "&Save", "Save an SU2 .cfg file")
-    m_open = m_file.Append(wx.ID_OPEN, "&Open", "Load an SU2 .cfg file")
-    m_exit = m_file.Append(wx.ID_EXIT, "E&xit", "Close window and exit program.")
-
-    menuBar.Append(m_file, "&File")
-    self.SetMenuBar(menuBar)
-    self.CreateStatusBar()
-
-    # Specify which functions to call when stuff is changed
-    self.Bind(wx.EVT_LIST_ITEM_SELECTED, self.list_click, self.list_ctrl)
-    self.Bind(wx.EVT_MENU, self.OnSave, m_save)
-    self.Bind(wx.EVT_MENU, self.OnOpen, m_open)
-    self.Bind(wx.EVT_SIZE, self.OnResize)
-    self.right_panel.SetAutoLayout(1)
-
-    # Add it all to the panel and draw
-    self.left_sizer.SetMinSize((300,600))
-    self.right_sizer.SetMinSize((300,600))
-    self.list_ctrl.SetColumnWidth(0,500)
-
-    self.left_sizer.Add(self.list_ctrl,0,wx.EXPAND)
-    self.right_sizer.Add(self.right_panel,0,wx.EXPAND)
-    self.main_sizer.Add(self.left_sizer,0,wx.EXPAND)
-    self.main_sizer.Add(self.right_sizer,0,wx.EXPAND)
-    self.frame_sizer.Add(self.main_sizer,0,wx.EXPAND)
-
-    self.main_panel.SetSizer(self.main_sizer)
-    self.SetSizer(self.frame_sizer)
-    self.SetInitialSize()
-
-  def OnCheck(self,event):
-    print(event)
-    print(dir(event))
-    print(event.GetEventObject())
-    print(event.GetEventObject().GetValue())
-
-  def OnResize(self,event):
-  # There is surely a better way to do this....
-    framesize = self.GetSize()
-    self.main_panel.SetSize(framesize)
-    self.list_ctrl.SetSize((300,framesize[1]-50))
-    self.right_panel.SetSize((framesize[0]-300,framesize[1]-50))
-
-
-  def OnSave(self,event):
-
-    # Dialog to set output filename
-    SaveDialog = wx.FileDialog(self,style=wx.FD_SAVE,wildcard='*.cfg')
-    SaveDialog.ShowModal()
-    outfile    = SaveDialog.GetPath()
-
-    f = open(outfile,'w')
-
-    for category,optlist in self.ctrldict.items():
-      f.write('%% %s \n'%category)
-      for option in optlist:
-        value = option.GetValue()
-        if not value=="":
-          f.write('%s=%s\n'%(option.option_name,option.GetValue()))
-    f.close()
-
-  def OnOpen(self,event):
-
-    # Dialog to select file
-    OpenDialog = wx.FileDialog(self,wildcard='*.cfg')
-    OpenDialog.ShowModal()
-    infile     = OpenDialog.GetPath()
-
-    # Open file, Load values into a dictionary
-    cfgfile    = open(infile,'r')
-    infiledict = {}
-    lines      = cfgfile.readlines()
-    for line in lines:
-      if (line[0]=='%' or line.find('=')==-1): # Skip lines w/o = sign
-        continue
-      else:    # Get value
-        key,val=[text.strip() for text in line.split('=')]
-        key = key.upper()    # AoA should work as well as AOA
-        infiledict[key] = val
-
-    # Loop through controls and set them to the new values
-    for category,optlist in self.ctrldict.items():
-      for option in optlist:
-        if option.option_name in infiledict:
-          option.SetValue(infiledict[option.option_name])
-        else:
-          option.SetValue("")
-
-  def OnClose(self,event):
-    sys.exit(1)
+    def SetDefaultValue(self):
+        self.control.SetValue(self.option_default)
 
-  def OnAbout(self,event):
-    print("OnAbout")
+    def GetCtrl(self):
+        return self.control
 
-  def list_click(self, event):
 
-    category = event.GetText()
-
-    self.right_panel.ScrollChildIntoView(self.lastctrl)
-    self.right_panel.ScrollChildIntoView(self.optlabels[category])
+class config_gui(wx.Frame):
+    def __init__(self, option_data):
+
+        # wx Initialization
+        wx.Frame.__init__(self, None, title="SU2 config file editor")
+
+        # Define the main sizers
+        self.frame_sizer = wx.BoxSizer(wx.HORIZONTAL)
+        self.main_sizer = wx.BoxSizer(wx.HORIZONTAL)
+        self.left_sizer = wx.BoxSizer(wx.VERTICAL)
+        self.right_sizer = wx.BoxSizer(wx.VERTICAL)
+
+        # Use a scrolled panel on the right side
+        self.main_panel = wx.Panel(self)
+        self.scroll_sizer = wx.BoxSizer(wx.VERTICAL)
+        self.right_panel = sp.ScrolledPanel(self.main_panel, size=(500, 500))
+        self.right_panel.SetupScrolling()
+
+        # Left side - list of option categories
+        self.list_ctrl = wx.ListCtrl(
+            self.main_panel, style=wx.LC_REPORT | wx.BORDER_SUNKEN, size=(300, 600)
+        )
+        self.list_ctrl.InsertColumn(0, "Option Category")
+
+        bigfont = wx.Font(20, wx.MODERN, wx.NORMAL, wx.BOLD)
+
+        # Read the option_data and build controls
+        self.ctrldict = {}
+        self.optlabels = {}
+        for j, category in enumerate(option_data):
+
+            self.list_ctrl.InsertStringItem(
+                j, category
+            )  # Add category to left size list
+
+            self.optlabels[category] = wx.StaticText(self.right_panel, label=category)
+            self.optlabels[category].SetFont(bigfont)
+
+            if j > 0:
+                self.scroll_sizer.AddSpacer(20)
+            self.scroll_sizer.Add(self.optlabels[category], wx.EXPAND)
+
+            self.ctrldict[category] = []
+            yctr = 0
+            for j, opt in enumerate(option_data[category]):
+                if opt.option_type in [
+                    "EnumOption",
+                    "MathProblem",
+                    "SpecialOption",
+                    "ConvectOption",
+                ]:
+                    self.ctrldict[category].append(
+                        LabeledComboBox(
+                            self.right_panel,
+                            opt.option_name,
+                            opt.option_name,
+                            opt.option_default,
+                            opt.option_values,
+                            opt.option_type,
+                            opt.option_description,
+                        )
+                    )
+                else:
+                    self.ctrldict[category].append(
+                        LabeledTextCtrl(
+                            self.right_panel,
+                            opt.option_name,
+                            opt.option_name,
+                            opt.option_default,
+                            opt.option_type,
+                        )
+                    )
+
+            for control in self.ctrldict[category]:
+                self.scroll_sizer.Add(
+                    control.GetSizer(), wx.EXPAND
+                )  # Add each control to the sizer
+                self.lastctrl = control.GetCtrl()
+
+        # Set right_panel to scroll vertically
+        self.right_panel.SetSizer(self.scroll_sizer)
+
+        # Set up menu
+        menuBar = wx.MenuBar()
+        m_file = wx.Menu()
+        m_save = m_file.Append(wx.ID_SAVE, "&Save", "Save an SU2 .cfg file")
+        m_open = m_file.Append(wx.ID_OPEN, "&Open", "Load an SU2 .cfg file")
+        m_exit = m_file.Append(wx.ID_EXIT, "E&xit", "Close window and exit program.")
+
+        menuBar.Append(m_file, "&File")
+        self.SetMenuBar(menuBar)
+        self.CreateStatusBar()
+
+        # Specify which functions to call when stuff is changed
+        self.Bind(wx.EVT_LIST_ITEM_SELECTED, self.list_click, self.list_ctrl)
+        self.Bind(wx.EVT_MENU, self.OnSave, m_save)
+        self.Bind(wx.EVT_MENU, self.OnOpen, m_open)
+        self.Bind(wx.EVT_SIZE, self.OnResize)
+        self.right_panel.SetAutoLayout(1)
+
+        # Add it all to the panel and draw
+        self.left_sizer.SetMinSize((300, 600))
+        self.right_sizer.SetMinSize((300, 600))
+        self.list_ctrl.SetColumnWidth(0, 500)
+
+        self.left_sizer.Add(self.list_ctrl, 0, wx.EXPAND)
+        self.right_sizer.Add(self.right_panel, 0, wx.EXPAND)
+        self.main_sizer.Add(self.left_sizer, 0, wx.EXPAND)
+        self.main_sizer.Add(self.right_sizer, 0, wx.EXPAND)
+        self.frame_sizer.Add(self.main_sizer, 0, wx.EXPAND)
+
+        self.main_panel.SetSizer(self.main_sizer)
+        self.SetSizer(self.frame_sizer)
+        self.SetInitialSize()
+
+    def OnCheck(self, event):
+        print(event)
+        print(dir(event))
+        print(event.GetEventObject())
+        print(event.GetEventObject().GetValue())
+
+    def OnResize(self, event):
+        # There is surely a better way to do this....
+        framesize = self.GetSize()
+        self.main_panel.SetSize(framesize)
+        self.list_ctrl.SetSize((300, framesize[1] - 50))
+        self.right_panel.SetSize((framesize[0] - 300, framesize[1] - 50))
+
+    def OnSave(self, event):
+
+        # Dialog to set output filename
+        SaveDialog = wx.FileDialog(self, style=wx.FD_SAVE, wildcard="*.cfg")
+        SaveDialog.ShowModal()
+        outfile = SaveDialog.GetPath()
+
+        f = open(outfile, "w")
+
+        for category, optlist in self.ctrldict.items():
+            f.write("%% %s \n" % category)
+            for option in optlist:
+                value = option.GetValue()
+                if not value == "":
+                    f.write("%s=%s\n" % (option.option_name, option.GetValue()))
+        f.close()
+
+    def OnOpen(self, event):
+
+        # Dialog to select file
+        OpenDialog = wx.FileDialog(self, wildcard="*.cfg")
+        OpenDialog.ShowModal()
+        infile = OpenDialog.GetPath()
+
+        # Open file, Load values into a dictionary
+        cfgfile = open(infile, "r")
+        infiledict = {}
+        lines = cfgfile.readlines()
+        for line in lines:
+            if line[0] == "%" or line.find("=") == -1:  # Skip lines w/o = sign
+                continue
+            else:  # Get value
+                key, val = [text.strip() for text in line.split("=")]
+                key = key.upper()  # AoA should work as well as AOA
+                infiledict[key] = val
+
+        # Loop through controls and set them to the new values
+        for category, optlist in self.ctrldict.items():
+            for option in optlist:
+                if option.option_name in infiledict:
+                    option.SetValue(infiledict[option.option_name])
+                else:
+                    option.SetValue("")
+
+    def OnClose(self, event):
+        sys.exit(1)
+
+    def OnAbout(self, event):
+        print("OnAbout")
+
+    def list_click(self, event):
+
+        category = event.GetText()
+
+        self.right_panel.ScrollChildIntoView(self.lastctrl)
+        self.right_panel.ScrollChildIntoView(self.optlabels[category])
 
 
 def prepare_data():
-  """ Method to get configuration data from source files.
-      Outputs a dictionary of categories as keys and lists of config_options as values
-  """
-
-  # These variables should point to the configuration files
-  su2_basedir = os.environ['SU2_HOME']
-  config_cpp = os.path.join(su2_basedir,'Common/src/config_structure.cpp')
-  config_hpp = os.path.join(su2_basedir,'Common/include/option_structure.hpp')
-
-  # Check that files exist
-  if not os.path.isfile(config_cpp):
-    sys.exit('Could not find cpp file, please check that su2_basedir is set correctly in config_gui.py')
-  if not os.path.isfile(config_hpp):
-    sys.exit('Could not find hpp file, please check that su2_basedir is set correctly in config_gui.py')
-
-  # Run the parser
-  option_list = parse_config(config_cpp, config_hpp)
-
-  # Organize data into dictionary with categories as keys
-  option_data = {}
-  for opt in option_list:
-    if not opt.option_category in option_data:
-      option_data[opt.option_category] = []
-    option_data[opt.option_category].append(opt)
-
-  return option_data
-
-if __name__=="__main__":
-
-  # Read source files, get option data
-  option_data = prepare_data()
-
-  # Launch GUI
-  app = wx.App(None)
-  frame = config_gui(option_data)
-  frame.Show()
-  app.MainLoop()
+    """Method to get configuration data from source files.
+    Outputs a dictionary of categories as keys and lists of config_options as values
+    """
+
+    # These variables should point to the configuration files
+    su2_basedir = os.environ["SU2_HOME"]
+    config_cpp = os.path.join(su2_basedir, "Common/src/config_structure.cpp")
+    config_hpp = os.path.join(su2_basedir, "Common/include/option_structure.hpp")
+
+    # Check that files exist
+    if not os.path.isfile(config_cpp):
+        sys.exit(
+            "Could not find cpp file, please check that su2_basedir is set correctly in config_gui.py"
+        )
+    if not os.path.isfile(config_hpp):
+        sys.exit(
+            "Could not find hpp file, please check that su2_basedir is set correctly in config_gui.py"
+        )
+
+    # Run the parser
+    option_list = parse_config(config_cpp, config_hpp)
+
+    # Organize data into dictionary with categories as keys
+    option_data = {}
+    for opt in option_list:
+        if not opt.option_category in option_data:
+            option_data[opt.option_category] = []
+        option_data[opt.option_category].append(opt)
+
+    return option_data
+
+
+if __name__ == "__main__":
+
+    # Read source files, get option data
+    option_data = prepare_data()
+
+    # Launch GUI
+    app = wx.App(None)
+    frame = config_gui(option_data)
+    frame.Show()
+    app.MainLoop()
diff --git a/SU2_PY/continuous_adjoint.py b/SU2_PY/continuous_adjoint.py
index 071f4b9a4ea..bf3358cbe8f 100755
--- a/SU2_PY/continuous_adjoint.py
+++ b/SU2_PY/continuous_adjoint.py
@@ -27,39 +27,69 @@
 
 import os, sys
 from optparse import OptionParser
-sys.path.append(os.environ['SU2_RUN'])
+
+sys.path.append(os.environ["SU2_RUN"])
 import SU2
 
 # -------------------------------------------------------------------
 #  Main
 # -------------------------------------------------------------------
 
+
 def main():
 
     # Command Line Options
-    parser=OptionParser()
-    parser.add_option("-f", "--file",       dest="filename",
-                      help="read config from FILE", metavar="FILE")
-    parser.add_option("-n", "--partitions", dest="partitions", default=1,
-                      help="number of PARTITIONS", metavar="PARTITIONS")
-    parser.add_option("-c", "--compute",    dest="compute",    default="True",
-                      help="COMPUTE direct and adjoint problem", metavar="COMPUTE")
-    parser.add_option("-s", "--step",       dest="step",       default=1E-4,
-                      help="DOT finite difference STEP", metavar="STEP")
-    parser.add_option("-z", "--zones", dest="nzones", default="1",
-                      help="Number of Zones", metavar="ZONES")
-
-    (options, args)=parser.parse_args()
-    options.partitions  = int( options.partitions )
-    options.step        = float( options.step )
-    options.compute     = options.compute.upper() == 'TRUE'
-    options.nzones      = int( options.nzones )
-
-    continuous_adjoint( options.filename    ,
-                        options.partitions  ,
-                        options.compute     ,
-                        options.step        ,
-                        options.nzones       )
+    parser = OptionParser()
+    parser.add_option(
+        "-f", "--file", dest="filename", help="read config from FILE", metavar="FILE"
+    )
+    parser.add_option(
+        "-n",
+        "--partitions",
+        dest="partitions",
+        default=1,
+        help="number of PARTITIONS",
+        metavar="PARTITIONS",
+    )
+    parser.add_option(
+        "-c",
+        "--compute",
+        dest="compute",
+        default="True",
+        help="COMPUTE direct and adjoint problem",
+        metavar="COMPUTE",
+    )
+    parser.add_option(
+        "-s",
+        "--step",
+        dest="step",
+        default=1e-4,
+        help="DOT finite difference STEP",
+        metavar="STEP",
+    )
+    parser.add_option(
+        "-z",
+        "--zones",
+        dest="nzones",
+        default="1",
+        help="Number of Zones",
+        metavar="ZONES",
+    )
+
+    (options, args) = parser.parse_args()
+    options.partitions = int(options.partitions)
+    options.step = float(options.step)
+    options.compute = options.compute.upper() == "TRUE"
+    options.nzones = int(options.nzones)
+
+    continuous_adjoint(
+        options.filename,
+        options.partitions,
+        options.compute,
+        options.step,
+        options.nzones,
+    )
+
 
 #: def main()
 
@@ -68,31 +98,28 @@ def main():
 #  Continuous Adjoint
 # -------------------------------------------------------------------
 
-def continuous_adjoint( filename           ,
-                        partitions  = 0    ,
-                        compute     = True ,
-                        step        = 1e-4 ,
-                        nzones      = 1     ):
+
+def continuous_adjoint(filename, partitions=0, compute=True, step=1e-4, nzones=1):
 
     # Config
     config = SU2.io.Config(filename)
     config.NUMBER_PART = partitions
-    config.NZONES      = int( nzones )
+    config.NZONES = int(nzones)
 
     # State
     state = SU2.io.State()
 
     # Force CSV output in order to compute gradients
 
-    if not 'OUTPUT_FILES' in config:
-        config['OUTPUT_FILES'] = ['RESTART']
+    if not "OUTPUT_FILES" in config:
+        config["OUTPUT_FILES"] = ["RESTART"]
 
-    if not 'SURFACE_CSV' in config['OUTPUT_FILES']:
-        config['OUTPUT_FILES'].append('SURFACE_CSV')
+    if not "SURFACE_CSV" in config["OUTPUT_FILES"]:
+        config["OUTPUT_FILES"].append("SURFACE_CSV")
 
     # check for existing files
     if not compute:
-        config.RESTART_SOL = 'YES'
+        config.RESTART_SOL = "YES"
         state.find_files(config)
     else:
         state.FILES.MESH = config.MESH_FILENAME
@@ -101,7 +128,7 @@ def continuous_adjoint( filename           ,
     if compute:
         info = SU2.run.direct(config)
         state.update(info)
-        SU2.io.restart2solution(config,state)
+        SU2.io.restart2solution(config, state)
 
     # Adjoint Solution
 
@@ -109,21 +136,20 @@ def continuous_adjoint( filename           ,
     if compute:
         info = SU2.run.adjoint(config)
         state.update(info)
-    info = SU2.run.projection(config,state, step)
+    info = SU2.run.projection(config, state, step)
     state.update(info)
 
     return state
 
+
 #: continuous_adjoint()
 
 # -------------------------------------------------------------------
 #  Alternate Forumulation
 # -------------------------------------------------------------------
 
-def continuous_design( filename           ,
-                       partitions  = 0    ,
-                       compute     = True ,
-                       step        = 1e-4  ):
+
+def continuous_design(filename, partitions=0, compute=True, step=1e-4):
 
     # TODO:
     # step
@@ -144,7 +170,7 @@ def continuous_design( filename           ,
         state.FILES.MESH = config.MESH_FILENAME
 
     # Adjoint Gradient
-    grads = SU2.eval.grad( ADJ_NAME, 'CONTINUOUS_ADJOINT', config, state )
+    grads = SU2.eval.grad(ADJ_NAME, "CONTINUOUS_ADJOINT", config, state)
 
     return state
 
@@ -154,6 +180,5 @@ def continuous_design( filename           ,
 # -------------------------------------------------------------------
 
 # this is only accessed if running from command prompt
-if __name__ == '__main__':
+if __name__ == "__main__":
     main()
-
diff --git a/SU2_PY/convert_to_csv.py b/SU2_PY/convert_to_csv.py
index c3811b6627e..32b13cace83 100755
--- a/SU2_PY/convert_to_csv.py
+++ b/SU2_PY/convert_to_csv.py
@@ -28,17 +28,24 @@
 from optparse import OptionParser
 import os
 
-parser = OptionParser(usage = "%prog -i INPUT_FILE",
-        description = 'This script converts SU2 ASCII restart files generated with a version prior v7 to the CSV format')
-parser.add_option("-i", "--inputfile", dest="infile",
-                  help="ASCII restart file (*.dat)", metavar="INPUT_FILE")
-(options, args)=parser.parse_args()
+parser = OptionParser(
+    usage="%prog -i INPUT_FILE",
+    description="This script converts SU2 ASCII restart files generated with a version prior v7 to the CSV format",
+)
+parser.add_option(
+    "-i",
+    "--inputfile",
+    dest="infile",
+    help="ASCII restart file (*.dat)",
+    metavar="INPUT_FILE",
+)
+(options, args) = parser.parse_args()
 
 
 infile = open(options.infile, "r")
-out_name = options.infile.split('.')[0] + ".csv"
-if (os.path.isfile(out_name)):
-    print('File ' + out_name + ' already exists.')
+out_name = options.infile.split(".")[0] + ".csv"
+if os.path.isfile(out_name):
+    print("File " + out_name + " already exists.")
     exit(1)
 outfile = open(out_name, "w")
 
@@ -50,8 +57,8 @@
     line = line.split()
     for i, val in enumerate(line):
         outfile.write(val.strip())
-        if i != len(line)-1:
-            outfile.write(', ')
-    outfile.write('\n')
+        if i != len(line) - 1:
+            outfile.write(", ")
+    outfile.write("\n")
 
-print('Converted ' + options.infile + ' to ' + out_name)
+print("Converted " + options.infile + " to " + out_name)
diff --git a/SU2_PY/direct_differentiation.py b/SU2_PY/direct_differentiation.py
index c885a58eaec..d81eef0f83a 100755
--- a/SU2_PY/direct_differentiation.py
+++ b/SU2_PY/direct_differentiation.py
@@ -28,34 +28,56 @@
 from __future__ import division, print_function, absolute_import
 import os, sys, shutil
 from optparse import OptionParser
-sys.path.append(os.environ['SU2_RUN'])
+
+sys.path.append(os.environ["SU2_RUN"])
 import SU2
 
 # -------------------------------------------------------------------
 #  Main
 # -------------------------------------------------------------------
 
+
 def main():
 
     parser = OptionParser()
-    parser.add_option("-f", "--file",       dest="filename",
-                      help="read config from FILE", metavar="FILE")
-    parser.add_option("-n", "--partitions", dest="partitions", default=1,
-                      help="number of PARTITIONS", metavar="PARTITIONS")
-    parser.add_option("-q", "--quiet",      dest="quiet",      default='False',
-                      help="output QUIET to log files", metavar="QUIET")
-    parser.add_option("-z", "--zones", dest="nzones", default="1",
-                      help="Number of Zones", metavar="ZONES")
-
-    (options, args)=parser.parse_args()
-    options.partitions = int( options.partitions )
-    options.quiet      = options.quiet.upper() == 'TRUE'
-    options.nzones     = int( options.nzones )
-
-    direct_differentiation( options.filename   ,
-                            options.partitions ,
-                            options.quiet      ,
-                            options.nzones      )
+    parser.add_option(
+        "-f", "--file", dest="filename", help="read config from FILE", metavar="FILE"
+    )
+    parser.add_option(
+        "-n",
+        "--partitions",
+        dest="partitions",
+        default=1,
+        help="number of PARTITIONS",
+        metavar="PARTITIONS",
+    )
+    parser.add_option(
+        "-q",
+        "--quiet",
+        dest="quiet",
+        default="False",
+        help="output QUIET to log files",
+        metavar="QUIET",
+    )
+    parser.add_option(
+        "-z",
+        "--zones",
+        dest="nzones",
+        default="1",
+        help="Number of Zones",
+        metavar="ZONES",
+    )
+
+    (options, args) = parser.parse_args()
+    options.partitions = int(options.partitions)
+    options.quiet = options.quiet.upper() == "TRUE"
+    options.nzones = int(options.nzones)
+
+    direct_differentiation(
+        options.filename, options.partitions, options.quiet, options.nzones
+    )
+
+
 #: def main()
 
 
@@ -63,18 +85,16 @@ def main():
 #  Direct Differentation Function
 # -------------------------------------------------------------------
 
-def direct_differentiation( filename           ,
-                            partitions = 0     ,
-                            quiet      = False ,
-                            nzones     = 1      ):
+
+def direct_differentiation(filename, partitions=0, quiet=False, nzones=1):
     # Config
     config = SU2.io.Config(filename)
     config.NUMBER_PART = partitions
-    config.NZONES      = int(nzones)
-    config["DIRECT_DIFF"] = 'DESIGN_VARIABLES'
+    config.NZONES = int(nzones)
+    config["DIRECT_DIFF"] = "DESIGN_VARIABLES"
 
     if quiet:
-        config.CONSOLE = 'CONCISE'
+        config.CONSOLE = "CONCISE"
 
     # State
     state = SU2.io.State()
@@ -82,44 +102,59 @@ def direct_differentiation( filename           ,
 
     foundDerivativeField = False
     for fields in SU2.io.historyOutFields:
-        group = SU2.io.historyOutFields[fields]['GROUP']
+        group = SU2.io.historyOutFields[fields]["GROUP"]
         if group in config.HISTORY_OUTPUT:
-            if SU2.io.historyOutFields[fields]['TYPE'] == 'D_COEFFICIENT':
+            if SU2.io.historyOutFields[fields]["TYPE"] == "D_COEFFICIENT":
                 foundDerivativeField = True
 
     if not foundDerivativeField:
-        sys.exit('No derivative field found in HISTORY_OUTPUT')
+        sys.exit("No derivative field found in HISTORY_OUTPUT")
 
     # link restart files to subfolder DIRECTDIFF, if restart solution is selected
-    if config.get('TIME_DOMAIN', 'NO') == 'YES' and config.get('RESTART_SOL', 'NO') == 'YES':
+    if (
+        config.get("TIME_DOMAIN", "NO") == "YES"
+        and config.get("RESTART_SOL", "NO") == "YES"
+    ):
         # check if directory DIRECTDIFF/DIRECT exists, if not, create
-        if not os.path.isdir('DIRECTDIFF/DIRECT'):
-            if not os.path.isdir('DIRECTDIFF'):
-                os.mkdir('DIRECTDIFF')
-            os.mkdir('DIRECTDIFF/DIRECT')
-
-        restart_name = config['RESTART_FILENAME'].split('.')[0]
-        restart_filename = restart_name + '_' + str(int(config['RESTART_ITER']) - 1).zfill(5) + '.dat'
-        if not os.path.isfile('DIRECTDIFF/DIRECT/' + restart_filename):
-            #throw, if restart file does not exist
+        if not os.path.isdir("DIRECTDIFF/DIRECT"):
+            if not os.path.isdir("DIRECTDIFF"):
+                os.mkdir("DIRECTDIFF")
+            os.mkdir("DIRECTDIFF/DIRECT")
+
+        restart_name = config["RESTART_FILENAME"].split(".")[0]
+        restart_filename = (
+            restart_name + "_" + str(int(config["RESTART_ITER"]) - 1).zfill(5) + ".dat"
+        )
+        if not os.path.isfile("DIRECTDIFF/DIRECT/" + restart_filename):
+            # throw, if restart file does not exist
             if not os.path.isfile(restart_filename):
-                sys.exit("Error: Restart file <" + restart_filename + "> not found." )
-            shutil.copyfile(restart_filename, 'DIRECTDIFF/DIRECT/' + restart_filename)
+                sys.exit("Error: Restart file <" + restart_filename + "> not found.")
+            shutil.copyfile(restart_filename, "DIRECTDIFF/DIRECT/" + restart_filename)
 
         # use only, if time integration is second order
-        if config.get('TIME_MARCHING', 'NO') == 'DUAL_TIME_STEPPING-2ND_ORDER':
-            restart_filename = restart_name + '_' + str(int(config['RESTART_ITER']) - 2).zfill(5) + '.dat'
-            if not os.path.isfile('DIRECTDIFF/DIRECT/' + restart_filename):
+        if config.get("TIME_MARCHING", "NO") == "DUAL_TIME_STEPPING-2ND_ORDER":
+            restart_filename = (
+                restart_name
+                + "_"
+                + str(int(config["RESTART_ITER"]) - 2).zfill(5)
+                + ".dat"
+            )
+            if not os.path.isfile("DIRECTDIFF/DIRECT/" + restart_filename):
                 # throw, if restart file does not exist
                 if not os.path.isfile(restart_filename):
-                    sys.exit("Error: Restart file <" + restart_filename + "> not found.")
-                shutil.copyfile(restart_filename, 'DIRECTDIFF/DIRECT/' + restart_filename)
+                    sys.exit(
+                        "Error: Restart file <" + restart_filename + "> not found."
+                    )
+                shutil.copyfile(
+                    restart_filename, "DIRECTDIFF/DIRECT/" + restart_filename
+                )
 
     # Direct Differentiation Gradients
-    SU2.eval.gradients.directdiff(config,state)
+    SU2.eval.gradients.directdiff(config, state)
 
     return state
 
+
 #: finite_differences()
 
 
@@ -128,5 +163,5 @@ def direct_differentiation( filename           ,
 # -------------------------------------------------------------------
 
 # this is only accessed if running from command prompt
-if __name__ == '__main__':
+if __name__ == "__main__":
     main()
diff --git a/SU2_PY/discrete_adjoint.py b/SU2_PY/discrete_adjoint.py
index 816e3a1d68c..8afb09b2555 100755
--- a/SU2_PY/discrete_adjoint.py
+++ b/SU2_PY/discrete_adjoint.py
@@ -27,44 +27,76 @@
 
 import os, sys, copy
 from optparse import OptionParser
-sys.path.append(os.environ['SU2_RUN'])
+
+sys.path.append(os.environ["SU2_RUN"])
 import SU2
 
 # -------------------------------------------------------------------
 #  Main
 # -------------------------------------------------------------------
 
+
 def main():
 
     # Command Line Options
-    parser=OptionParser()
-    parser.add_option("-f", "--file",       dest="filename",
-                      help="read config from FILE", metavar="FILE")
-    parser.add_option("-n", "--partitions", dest="partitions", default=1,
-                      help="number of PARTITIONS", metavar="PARTITIONS")
-    parser.add_option("-s", "--step",       dest="step",       default=1E-4,
-                      help="DOT finite difference STEP", metavar="STEP")
-    parser.add_option("-v", "--validate", dest="validate", default="False",
-                      help="Validate the gradient using direct diff. mode", metavar="VALIDATION")
-    parser.add_option("-z", "--zones", dest="nzones", default="1",
-                      help="Number of Zones", metavar="ZONES")
-    parser.add_option("-m", "--mode", dest="mode", default="all",
-                      help="Determine the calculation mode \n <all> : compute primal & adjoint problem & gradient (DEFAULT) \n <adj> : compute adjoint (with primal restart) & gradient \n <grad>: compute gradient (with primal and adjoint restarts)", metavar="MODE")
-
-    (options, args)=parser.parse_args()
-    options.partitions  = int( options.partitions )
-    options.step        = float( options.step )
-    options.validate    = options.validate.upper() == 'TRUE'
-    options.nzones      = int( options.nzones )
+    parser = OptionParser()
+    parser.add_option(
+        "-f", "--file", dest="filename", help="read config from FILE", metavar="FILE"
+    )
+    parser.add_option(
+        "-n",
+        "--partitions",
+        dest="partitions",
+        default=1,
+        help="number of PARTITIONS",
+        metavar="PARTITIONS",
+    )
+    parser.add_option(
+        "-s",
+        "--step",
+        dest="step",
+        default=1e-4,
+        help="DOT finite difference STEP",
+        metavar="STEP",
+    )
+    parser.add_option(
+        "-v",
+        "--validate",
+        dest="validate",
+        default="False",
+        help="Validate the gradient using direct diff. mode",
+        metavar="VALIDATION",
+    )
+    parser.add_option(
+        "-z",
+        "--zones",
+        dest="nzones",
+        default="1",
+        help="Number of Zones",
+        metavar="ZONES",
+    )
+    parser.add_option(
+        "-m",
+        "--mode",
+        dest="mode",
+        default="all",
+        help="Determine the calculation mode \n <all> : compute primal & adjoint problem & gradient (DEFAULT) \n <adj> : compute adjoint (with primal restart) & gradient \n <grad>: compute gradient (with primal and adjoint restarts)",
+        metavar="MODE",
+    )
+
+    (options, args) = parser.parse_args()
+    options.partitions = int(options.partitions)
+    options.step = float(options.step)
+    options.validate = options.validate.upper() == "TRUE"
+    options.nzones = int(options.nzones)
 
     if options.mode != "all" and options.mode != "adj" and options.mode != "grad":
-        sys.exit('Infeasible input for --mode. Use --help for more information')
+        sys.exit("Infeasible input for --mode. Use --help for more information")
+
+    discrete_adjoint(
+        options.filename, options.partitions, options.step, options.nzones, options.mode
+    )
 
-    discrete_adjoint( options.filename    ,
-                      options.partitions  ,
-                      options.step        ,
-                      options.nzones       ,
-                      options.mode)
 
 #: def main()
 
@@ -73,24 +105,21 @@ def main():
 #  Discrete Adjoint
 # -------------------------------------------------------------------
 
-def discrete_adjoint( filename           ,
-                      partitions  = 0    ,
-                      step        = 1e-4 ,
-                      nzones      = 1,
-                      mode = "all"):
+
+def discrete_adjoint(filename, partitions=0, step=1e-4, nzones=1, mode="all"):
     # Config
     config = SU2.io.Config(filename)
     config.NUMBER_PART = partitions
-    config.NZONES      = int( nzones )
+    config.NZONES = int(nzones)
 
     # State
     state = SU2.io.State()
 
-    config['GRADIENT_METHOD'] = 'DISCRETE_ADJOINT'
+    config["GRADIENT_METHOD"] = "DISCRETE_ADJOINT"
 
     # check for existing files
     if mode == "grad":
-        config.RESTART_SOL = 'YES'
+        config.RESTART_SOL = "YES"
         state.find_files(config)
     else:
         state.FILES.MESH = config.MESH_FILENAME
@@ -105,48 +134,54 @@ def discrete_adjoint( filename           ,
         # Update konfig
         konfig = copy.deepcopy(config)
 
-        if konfig.get('WINDOW_CAUCHY_CRIT', 'NO') == 'YES' and konfig.TIME_MARCHING != 'NO':
-            konfig['TIME_ITER'] = info.WND_CAUCHY_DATA['TIME_ITER']
-            konfig['ITER_AVERAGE_OBJ'] = info.WND_CAUCHY_DATA['ITER_AVERAGE_OBJ']
-            konfig['UNST_ADJOINT_ITER'] = info.WND_CAUCHY_DATA['UNST_ADJOINT_ITER']
+        if (
+            konfig.get("WINDOW_CAUCHY_CRIT", "NO") == "YES"
+            and konfig.TIME_MARCHING != "NO"
+        ):
+            konfig["TIME_ITER"] = info.WND_CAUCHY_DATA["TIME_ITER"]
+            konfig["ITER_AVERAGE_OBJ"] = info.WND_CAUCHY_DATA["ITER_AVERAGE_OBJ"]
+            konfig["UNST_ADJOINT_ITER"] = info.WND_CAUCHY_DATA["UNST_ADJOINT_ITER"]
 
-        SU2.io.restart2solution(konfig,state)
+        SU2.io.restart2solution(konfig, state)
 
     # Adjoint Solution
 
     # Run all-at-once
     if mode == "all" or mode == "adj":
         restart_sol_activated = False
-        if konfig.get('TIME_DOMAIN','NO') == 'YES' and konfig.get('RESTART_SOL','NO') == 'YES':
+        if (
+            konfig.get("TIME_DOMAIN", "NO") == "YES"
+            and konfig.get("RESTART_SOL", "NO") == "YES"
+        ):
             restart_sol_activated = True
-            original_time_iter = konfig['TIME_ITER']
-            konfig['TIME_ITER'] = konfig['TIME_ITER'] - int(konfig['RESTART_ITER'])
-            konfig.RESTART_SOL = 'NO'
+            original_time_iter = konfig["TIME_ITER"]
+            konfig["TIME_ITER"] = konfig["TIME_ITER"] - int(konfig["RESTART_ITER"])
+            konfig.RESTART_SOL = "NO"
         info = SU2.run.adjoint(konfig)
         state.update(info)
 
         # Workaround, since expandTime relies on UNST_ADJOINT_ITER to determine number of solution files.
         if restart_sol_activated:
-            konfig['UNST_ADJOINT_ITER'] =  original_time_iter - int(konfig['RESTART_ITER'])
-        SU2.io.restart2solution(konfig,state)
+            konfig["UNST_ADJOINT_ITER"] = original_time_iter - int(
+                konfig["RESTART_ITER"]
+            )
+        SU2.io.restart2solution(konfig, state)
         # reset changed time-iter values for the remaining program to original values
     # Gradient Projection
-    info = SU2.run.projection(konfig,step)
+    info = SU2.run.projection(konfig, step)
     state.update(info)
 
     return state
 
+
 #: continuous_adjoint()
 
 # -------------------------------------------------------------------
 #  Alternate Formulation
 # -------------------------------------------------------------------
 
-def discrete_design( filename           ,
-                       partitions  = 0    ,
-                       compute     = True ,
-                       step        = 1e-4 ,
-                       validation  = False):
+
+def discrete_design(filename, partitions=0, compute=True, step=1e-4, validation=False):
 
     # TODO:
     # step
@@ -155,7 +190,7 @@ def discrete_design( filename           ,
     config = SU2.io.Config(filename)
     config.NUMBER_PART = partitions
 
-    config['GRADIENT_METHOD'] = 'DISCRETE_ADJOINT'
+    config["GRADIENT_METHOD"] = "DISCRETE_ADJOINT"
 
     ADJ_NAME = config.OBJECTIVE_FUNCTION
 
@@ -166,49 +201,45 @@ def discrete_design( filename           ,
 
     grads_directdiff = []
 
-#    if validation:
-#        state_directdiff.find_files(config)
-#        konfig = copy.deepcopy(config)
-#        konfig['DIRECT_DIFF'] = "DESIGN_VARIABLES"
-#        grad_directdiff = SU2.eval.gradients.directdiff(konfig,state_directdiff)
-#        state['FILES']['DIRECT'] = 'DIRECTDIFF/' + state_directdiff['FILES']['DIRECT']
-#        state['FUNCTIONS'] = state_directdiff['FUNCTIONS']
+    #    if validation:
+    #        state_directdiff.find_files(config)
+    #        konfig = copy.deepcopy(config)
+    #        konfig['DIRECT_DIFF'] = "DESIGN_VARIABLES"
+    #        grad_directdiff = SU2.eval.gradients.directdiff(konfig,state_directdiff)
+    #        state['FILES']['DIRECT'] = 'DIRECTDIFF/' + state_directdiff['FILES']['DIRECT']
+    #        state['FUNCTIONS'] = state_directdiff['FUNCTIONS']
 
     # check for existing files
-    if any([not compute, validation]) :
+    if any([not compute, validation]):
         state.find_files(config)
     else:
         state.FILES.MESH = config.MESH_FILENAME
 
     # Adjoint Gradient
-    grads = SU2.eval.grad( ADJ_NAME, config['GRADIENT_METHOD'], config, state )
-
-#    if validation:
-#        Definition_DV = config['DEFINITION_DV']
-#        n_dv = len(Definition_DV['KIND'])
-#        grads_dd  = grad_directdiff[ADJ_NAME]
-#        print("Validation Summary")
-#        print("--------------------------")
-#        print("VARIABLE   " + "DISCRETE ADJOINT"  + "  DIRECT DIFFERENTIATION" + "  ERROR (%)")
-#        for idv in range(n_dv):
-#            if abs(grads[idv]) > abs(grads_dd[idv]):
-#                this_err = abs(grads[idv]/grads_dd[idv])
-#            else:
-#                this_err = abs(grads_dd[idv]/grads[idv])
-
-#            print(str(idv) + "         " + str(grads[idv]) + "         " + str(grads_dd[idv]) + "        " + str((this_err-1)*100)  + ' %')
-
+    grads = SU2.eval.grad(ADJ_NAME, config["GRADIENT_METHOD"], config, state)
+
+    #    if validation:
+    #        Definition_DV = config['DEFINITION_DV']
+    #        n_dv = len(Definition_DV['KIND'])
+    #        grads_dd  = grad_directdiff[ADJ_NAME]
+    #        print("Validation Summary")
+    #        print("--------------------------")
+    #        print("VARIABLE   " + "DISCRETE ADJOINT"  + "  DIRECT DIFFERENTIATION" + "  ERROR (%)")
+    #        for idv in range(n_dv):
+    #            if abs(grads[idv]) > abs(grads_dd[idv]):
+    #                this_err = abs(grads[idv]/grads_dd[idv])
+    #            else:
+    #                this_err = abs(grads_dd[idv]/grads[idv])
+
+    #            print(str(idv) + "         " + str(grads[idv]) + "         " + str(grads_dd[idv]) + "        " + str((this_err-1)*100)  + ' %')
 
     return state
 
 
-
-
 # -------------------------------------------------------------------
 #  Run Main Program
 # -------------------------------------------------------------------
 
 # this is only accessed if running from command prompt
-if __name__ == '__main__':
+if __name__ == "__main__":
     main()
-
diff --git a/SU2_PY/documentation.txt b/SU2_PY/documentation.txt
index 70cb6ba69e5..d4ef8e157fb 100644
--- a/SU2_PY/documentation.txt
+++ b/SU2_PY/documentation.txt
@@ -1,4 +1,4 @@
-goals - 
+goals -
 cascading levels of functionality
 lower levels stand on their own, and provide usefulness to
 higher levels when asked
@@ -43,7 +43,7 @@ SU2.run.deform(config,dv_new=[])
 	pointer updated config
 		'MESH_FILENAME' = 'MESH_FILENAME'+'_deform'
 		'DV_VALUE_OLD' = 'DV_VALUE_NEW'
-	
+
 SU2.run.direct(config)
 	checks decomp
 	ensures config:
@@ -56,12 +56,12 @@ SU2.run.direct(config)
 		'FUNCTIONS' - dict of function:value
 		'HISTORY' - dict of col_header:iteration history
 		'FILES' - dict of useful file names
-	
+
 SU2.run.adjoint(config)
 	checks decomp
 	ensures config:
 		'MATH_PROBLEM' = 'CONTINUOUS_ADJOINT'
-		'CONV_FILENAME' = 'CONFIG_FILENAME' + '_adjoint'	
+		'CONV_FILENAME' = 'CONFIG_FILENAME' + '_adjoint'
 	run CFD
 	read history
 	does not move restart to solution
@@ -69,7 +69,7 @@ SU2.run.adjoint(config)
 	returns dictionary 'info' with keys:
 		'HISTORY' - dict of col_header:iteration history
 		'FILES' - dict of useful file names
-	
+
 SU2.run.projection(config,step=1e-4)
 	assumes linear superposition of design variables
 	checks decomp
@@ -85,7 +85,7 @@ SU2.run.projection(config,step=1e-4)
 level2 - objective and gradient analysis, redundancy protection
 upstream pointer update of config and state
 config - controls SU2
-state  - stores design information 
+state  - stores design information
 
 STATE
 	FILES
@@ -107,7 +107,7 @@ STATE
 		LIFT
 		DRAG
 		MOMENT_Z
-	
+
 SU2.eval.functions.function()
 aliased to SU2.eval.func()
 	runs the aerodynamics and geometry control functions
@@ -121,11 +121,11 @@ SU2.eval.functions.aerodynamics()
 		direct solution
 	evaluates each step in its own folder, returning state.FILES to the super folder
 	updates config and state by pointer
-	
+
 
 SU2.eval.functions.geometry()
     todo ...
-    
+
 SU2.eval.gradients.gradient()
 aliased to SU2.eval.grad()
 
@@ -136,17 +136,17 @@ SU2.eval.gradients.adjoint()
 		adjoint solution
 	evaluates each step in its own folder, returning state.FILES to the super folder
 	updates config and state by pointer
-    
-    
+
+
 SU2.eval.gradients.findiff()
 	runs with redundancy protection (using state):
         functions()
             decom, deform, direct
         finite difference evaluation of functions()
-	finite difference steps performed in the FINDIFF folder, removed when completed    
+	finite difference steps performed in the FINDIFF folder, removed when completed
 	updates config and state by pointer
 
-    
+
 level3 - design management
 major assumption - one design, one config, one state
 start a new design if a new config is needed
@@ -167,8 +167,8 @@ SU2.eval.design(config,state,folder)
         con_dceq()  equality constraint derivatives
         con_cieq()  inequality constraints
         con_dcieq() inequality constraint gradients
-    
-    
+
+
 level4 - project managent
 SU2.opt.project(config,state,folder)
     runs multiple design classes, again avoiding redundancy
@@ -179,7 +179,7 @@ SU2.opt.project(config,state,folder)
 level5 - optimization
 SU2.opt.scipy_slsqp(project)
     sets up and runs a scipy slsqp optimization
-    
+
 FILE IO
 
 level0 - in/out/mod
@@ -192,14 +192,14 @@ class SU2.io.config(dict)
 	config.unpack_dvs(dv_new.dv_old)
 	config.__diff__(konfig)
 	config.__eq__(konfig)
-	
+
 	config.read_history()
 	config.read_aerodynamics()
 	config.rename_restart()
-	
+
 SU2.io.read_history( name )
 SU2.io.read_aerodynamics( hist_name, special_cases )
-	
+
 level1 - files translate,modify,plotting
 
 SU2.io.add_suffix(name,suffix)
@@ -207,15 +207,3 @@ SU2.io.resurrect_restart(config,state)
 
 SU2.io.plot.adjoint_gradient(config,grad_dict)
 SU2.io.plot.findiff_gradient(config,grad_dict)
-
-
-
-
-
-
-
-
-
-
-
-
diff --git a/SU2_PY/finite_differences.py b/SU2_PY/finite_differences.py
index 6777d50e068..d6684b3706b 100755
--- a/SU2_PY/finite_differences.py
+++ b/SU2_PY/finite_differences.py
@@ -27,34 +27,56 @@
 
 import os, sys
 from optparse import OptionParser
-sys.path.append(os.environ['SU2_RUN'])
+
+sys.path.append(os.environ["SU2_RUN"])
 import SU2
 
 # -------------------------------------------------------------------
 #  Main
 # -------------------------------------------------------------------
 
+
 def main():
 
     parser = OptionParser()
-    parser.add_option("-f", "--file",       dest="filename",
-                      help="read config from FILE", metavar="FILE")
-    parser.add_option("-n", "--partitions", dest="partitions", default=1,
-                      help="number of PARTITIONS", metavar="PARTITIONS")
-    parser.add_option("-q", "--quiet",      dest="quiet",      default='False',
-                      help="output QUIET to log files", metavar="QUIET")
-    parser.add_option("-z", "--zones", dest="nzones", default="1",
-                        help="Number of Zones", metavar="ZONES")
-
-    (options, args)=parser.parse_args()
-    options.partitions = int( options.partitions )
-    options.quiet      = options.quiet.upper() == 'TRUE'
-    options.nzones     = int( options.nzones )
-
-    finite_differences( options.filename   ,
-                        options.partitions ,
-                        options.quiet      ,
-                        options.nzones      )
+    parser.add_option(
+        "-f", "--file", dest="filename", help="read config from FILE", metavar="FILE"
+    )
+    parser.add_option(
+        "-n",
+        "--partitions",
+        dest="partitions",
+        default=1,
+        help="number of PARTITIONS",
+        metavar="PARTITIONS",
+    )
+    parser.add_option(
+        "-q",
+        "--quiet",
+        dest="quiet",
+        default="False",
+        help="output QUIET to log files",
+        metavar="QUIET",
+    )
+    parser.add_option(
+        "-z",
+        "--zones",
+        dest="nzones",
+        default="1",
+        help="Number of Zones",
+        metavar="ZONES",
+    )
+
+    (options, args) = parser.parse_args()
+    options.partitions = int(options.partitions)
+    options.quiet = options.quiet.upper() == "TRUE"
+    options.nzones = int(options.nzones)
+
+    finite_differences(
+        options.filename, options.partitions, options.quiet, options.nzones
+    )
+
+
 #: def main()
 
 
@@ -62,42 +84,55 @@ def main():
 #  Finite Differences Function
 # -------------------------------------------------------------------
 
-def finite_differences( filename           ,
-                        partitions = 0     ,
-                        quiet      = False ,
-                        nzones     = 1      ):
+
+def finite_differences(filename, partitions=0, quiet=False, nzones=1):
     # Config
     config = SU2.io.Config(filename)
     config.NUMBER_PART = partitions
-    config.NZONES      = int( nzones )
+    config.NZONES = int(nzones)
 
     if quiet:
-        config.CONSOLE = 'CONCISE'
+        config.CONSOLE = "CONCISE"
 
     # State
     state = SU2.io.State()
     state.find_files(config)
 
     # add restart files to state.FILES
-    if config.get('TIME_DOMAIN', 'NO') == 'YES' and config.get('RESTART_SOL', 'NO') == 'YES':
-        restart_name = config['RESTART_FILENAME'].split('.')[0]
-        restart_filename = restart_name + '_' + str(int(config['RESTART_ITER'])-1).zfill(5) + '.dat'
-        if not os.path.isfile(restart_filename): # throw, if restart files does not exist
+    if (
+        config.get("TIME_DOMAIN", "NO") == "YES"
+        and config.get("RESTART_SOL", "NO") == "YES"
+    ):
+        restart_name = config["RESTART_FILENAME"].split(".")[0]
+        restart_filename = (
+            restart_name + "_" + str(int(config["RESTART_ITER"]) - 1).zfill(5) + ".dat"
+        )
+        if not os.path.isfile(
+            restart_filename
+        ):  # throw, if restart files does not exist
             sys.exit("Error: Restart file <" + restart_filename + "> not found.")
-        state['FILES']['RESTART_FILE_1'] = restart_filename
+        state["FILES"]["RESTART_FILE_1"] = restart_filename
 
         # use only, if time integration is second order
-        if config.get('TIME_MARCHING', 'NO') == 'DUAL_TIME_STEPPING-2ND_ORDER':
-            restart_filename = restart_name + '_' + str(int(config['RESTART_ITER'])-2).zfill(5) + '.dat'
-            if not os.path.isfile(restart_filename): # throw, if restart files does not exist
+        if config.get("TIME_MARCHING", "NO") == "DUAL_TIME_STEPPING-2ND_ORDER":
+            restart_filename = (
+                restart_name
+                + "_"
+                + str(int(config["RESTART_ITER"]) - 2).zfill(5)
+                + ".dat"
+            )
+            if not os.path.isfile(
+                restart_filename
+            ):  # throw, if restart files does not exist
                 sys.exit("Error: Restart file <" + restart_filename + "> not found.")
-            state['FILES']['RESTART_FILE_2'] =restart_filename
+            state["FILES"]["RESTART_FILE_2"] = restart_filename
 
     # Finite Difference Gradients
-    SU2.eval.gradients.findiff(config,state)
+    SU2.eval.gradients.findiff(config, state)
 
     return state
 
+
 #: finite_differences()
 
 
@@ -106,5 +141,5 @@ def finite_differences( filename           ,
 # -------------------------------------------------------------------
 
 # this is only accessed if running from command prompt
-if __name__ == '__main__':
+if __name__ == "__main__":
     main()
diff --git a/SU2_PY/fsi_computation.py b/SU2_PY/fsi_computation.py
index 0735485a18f..4e644b49b24 100644
--- a/SU2_PY/fsi_computation.py
+++ b/SU2_PY/fsi_computation.py
@@ -34,194 +34,226 @@
 import shutil
 import copy
 import time as timer
-from math import *	# use mathematical expressions
-from optparse import OptionParser	# use a parser for configuration
+from math import *  # use mathematical expressions
+from optparse import OptionParser  # use a parser for configuration
 
 # imports the CFD (SU2) module for FSI computation
 import pysu2
-import FSI_tools as FSI	# imports FSI python tools
+import FSI_tools as FSI  # imports FSI python tools
 
 # -------------------------------------------------------------------
 #  Main
 # -------------------------------------------------------------------
 
+
 def main():
 
-  # --- Get the FSI conig file name form the command line options --- #
-  parser=OptionParser()
-  parser.add_option("-f", "--file",       dest="filename",
-                      help="read config from FILE", metavar="FILE")
-  parser.add_option("--parallel", action="store_true",
-                      help="Specify if we need to initialize MPI", dest="with_MPI", default=False)
-
-  (options, args)=parser.parse_args()
-
-  if options.with_MPI:
-    from mpi4py import MPI  # MPI is initialized from now by python and can be continued in C++
-    comm = MPI.COMM_WORLD
-    myid = comm.Get_rank()
-    numberPart = comm.Get_size()
-    have_MPI = True
-  else:
-    comm = 0
-    myid = 0
-    numberPart = 1
-    have_MPI = False
-
-  rootProcess = 0
-
-  # --- Set the working directory --- #
-  if myid == rootProcess:
-      if os.getcwd() not in sys.path:
-        sys.path.append(os.getcwd())
-        print("Setting working directory : {}".format(os.getcwd()))
-      else:
-        print("Working directory is set to {}".format(os.getcwd()))
-
-  if have_MPI:
-    comm.barrier()
-
-  # starts timer
-  start = timer.time()
-
-  confFile = str(options.filename)
-
-  FSI_config = FSI.FSIConfig(confFile, comm) 		# FSI configuration file
-  CFD_ConFile = FSI_config['CFD_CONFIG_FILE_NAME']	# CFD configuration file
-  CSD_ConFile = FSI_config['CSD_CONFIG_FILE_NAME']	# CSD configuration file
-
-  CSD_Solver = FSI_config['CSD_SOLVER']			# CSD solver
-
-  if have_MPI:
-    comm.barrier()
-
-  # --- Initialize the fluid solver --- #
-  if myid == rootProcess:
-    print("\n")
-    print(" Initializing fluid solver ".center(80,"*"))
-  try:
-    FluidSolver = pysu2.CSinglezoneDriver(CFD_ConFile, 1, comm)
-  except TypeError as exception:
-    print('A TypeError occured in pysu2.CSinglezoneDriver : ',exception)
-    if have_MPI:
-      print('ERROR : You are trying to initialize MPI with a serial build of the wrapper. Please, remove the --parallel option that is incompatible with a serial build.')
+    # --- Get the FSI conig file name form the command line options --- #
+    parser = OptionParser()
+    parser.add_option(
+        "-f", "--file", dest="filename", help="read config from FILE", metavar="FILE"
+    )
+    parser.add_option(
+        "--parallel",
+        action="store_true",
+        help="Specify if we need to initialize MPI",
+        dest="with_MPI",
+        default=False,
+    )
+
+    (options, args) = parser.parse_args()
+
+    if options.with_MPI:
+        from mpi4py import (
+            MPI,
+        )  # MPI is initialized from now by python and can be continued in C++
+
+        comm = MPI.COMM_WORLD
+        myid = comm.Get_rank()
+        numberPart = comm.Get_size()
+        have_MPI = True
     else:
-      print('ERROR : You are trying to launch a computation without initializing MPI but the wrapper has been built in parallel. Please add the --parallel option in order to initialize MPI for the wrapper.')
-    return
+        comm = 0
+        myid = 0
+        numberPart = 1
+        have_MPI = False
 
-  if have_MPI:
-    comm.barrier()
+    rootProcess = 0
 
-  # --- Initialize the solid solver --- #
-  # Serial solvers
-  if CSD_Solver in ["NATIVE"]:
+    # --- Set the working directory --- #
     if myid == rootProcess:
-      print("\n")
-      print(" Initializing solid solver ".center(80,"*"))
-      if CSD_Solver == 'NATIVE':
-        from SU2_Nastran import pysu2_nastran
-        if FSI_config["IMPOSED_MOTION"] == "NO":
-          SolidSolver = pysu2_nastran.Solver(CSD_ConFile,False)
+        if os.getcwd() not in sys.path:
+            sys.path.append(os.getcwd())
+            print("Setting working directory : {}".format(os.getcwd()))
         else:
-          SolidSolver = pysu2_nastran.Solver(CSD_ConFile,True)
-    else:
-      SolidSolver = None
-  # Parallel solvers
-  # For now we are only using serial solvers
-  else:
-    raise Exception('\n Invalid solid solver option')
-
-  if have_MPI:
-    comm.barrier()
-
-  # --- Initialize and set the FSI interface (coupling environement) --- #
-  if myid == rootProcess:
-    print("\n")
-    print(" Initializing FSI interface ".center(80,"*"))
-  if have_MPI:
-    comm.barrier()
-  FSIInterface = FSI.Interface(FSI_config, FluidSolver, SolidSolver, have_MPI)
-
-  if myid == rootProcess:
-    print("\n")
-    print(" Connect fluid and solid solvers ".center(80,"*"))
-  if have_MPI:
-    comm.barrier()
-  FSIInterface.connect(FSI_config, FluidSolver, SolidSolver)
-
-  if myid == rootProcess:
-    print("\n")
-    print(" Mapping fluid-solid interfaces ".center(80,"*"))
-  if have_MPI:
-    comm.barrier()
-  FSIInterface.interfaceMapping(FluidSolver, SolidSolver, FSI_config)
-
-  if have_MPI:
-    comm.barrier()
-
-  if FSI_config["MAPPING_MODES"] == "NO":
-    # --- Launch a steady or unsteady FSI computation --- #
-    if FSI_config['TIME_MARCHING'] == "YES":
-      try:
-        FSIInterface.UnsteadyFSI(FSI_config, FluidSolver, SolidSolver)
-      except NameError as exception:
-        if myid == rootProcess:
-          print('An NameError occured in FSIInterface.UnsteadyFSI : ',exception)
-      except TypeError as exception:
-        if myid == rootProcess:
-          print('A TypeError occured in FSIInterface.UnsteadyFSI : ',exception)
-      except KeyboardInterrupt as exception :
-        if myid == rootProcess:
-          print('A KeyboardInterrupt occured in FSIInterface.UnsteadyFSI : ',exception)
-    else:
-      try:
-        FSIInterface.SteadyFSI(FSI_config, FluidSolver, SolidSolver)
-      except NameError as exception:
-        if myid == rootProcess:
-          print('An NameError occured in FSIInterface.SteadyFSI : ',exception)
-      except TypeError as exception:
-        if myid == rootProcess:
-          print('A TypeError occured in FSIInterface.SteadyFSI : ',exception)
-      except KeyboardInterrupt as exception :
-        if myid == rootProcess:
-          print('A KeyboardInterrupt occured in FSIInterface.SteadyFSI : ',exception)
-  else:
+            print("Working directory is set to {}".format(os.getcwd()))
+
+    if have_MPI:
+        comm.barrier()
+
+    # starts timer
+    start = timer.time()
+
+    confFile = str(options.filename)
+
+    FSI_config = FSI.FSIConfig(confFile, comm)  # FSI configuration file
+    CFD_ConFile = FSI_config["CFD_CONFIG_FILE_NAME"]  # CFD configuration file
+    CSD_ConFile = FSI_config["CSD_CONFIG_FILE_NAME"]  # CSD configuration file
+
+    CSD_Solver = FSI_config["CSD_SOLVER"]  # CSD solver
+
+    if have_MPI:
+        comm.barrier()
+
+    # --- Initialize the fluid solver --- #
+    if myid == rootProcess:
+        print("\n")
+        print(" Initializing fluid solver ".center(80, "*"))
     try:
-      FSIInterface.MapModes(FSI_config, FluidSolver, SolidSolver)
-    except NameError as exception:
-      if myid == rootProcess:
-        print('An NameError occured in FSIInterface.MapModes : ',exception)
+        FluidSolver = pysu2.CSinglezoneDriver(CFD_ConFile, 1, comm)
     except TypeError as exception:
-      if myid == rootProcess:
-        print('A TypeError occured in FSIInterface.MapModes : ',exception)
-    except KeyboardInterrupt as exception :
-      if myid == rootProcess:
-        print('A KeyboardInterrupt occured in FSIInterface.MapModes : ',exception)
+        print("A TypeError occured in pysu2.CSinglezoneDriver : ", exception)
+        if have_MPI:
+            print(
+                "ERROR : You are trying to initialize MPI with a serial build of the wrapper. Please, remove the --parallel option that is incompatible with a serial build."
+            )
+        else:
+            print(
+                "ERROR : You are trying to launch a computation without initializing MPI but the wrapper has been built in parallel. Please add the --parallel option in order to initialize MPI for the wrapper."
+            )
+        return
 
-  if have_MPI:
-    comm.barrier()
+    if have_MPI:
+        comm.barrier()
 
-  # --- Exit cleanly the fluid and solid solvers --- #
-  FluidSolver.Postprocessing()
-  if myid == rootProcess:
-      SolidSolver.exit()
+    # --- Initialize the solid solver --- #
+    # Serial solvers
+    if CSD_Solver in ["NATIVE"]:
+        if myid == rootProcess:
+            print("\n")
+            print(" Initializing solid solver ".center(80, "*"))
+            if CSD_Solver == "NATIVE":
+                from SU2_Nastran import pysu2_nastran
+
+                if FSI_config["IMPOSED_MOTION"] == "NO":
+                    SolidSolver = pysu2_nastran.Solver(CSD_ConFile, False)
+                else:
+                    SolidSolver = pysu2_nastran.Solver(CSD_ConFile, True)
+        else:
+            SolidSolver = None
+    # Parallel solvers
+    # For now we are only using serial solvers
+    else:
+        raise Exception("\n Invalid solid solver option")
+
+    if have_MPI:
+        comm.barrier()
+
+    # --- Initialize and set the FSI interface (coupling environement) --- #
+    if myid == rootProcess:
+        print("\n")
+        print(" Initializing FSI interface ".center(80, "*"))
+    if have_MPI:
+        comm.barrier()
+    FSIInterface = FSI.Interface(FSI_config, FluidSolver, SolidSolver, have_MPI)
+
+    if myid == rootProcess:
+        print("\n")
+        print(" Connect fluid and solid solvers ".center(80, "*"))
+    if have_MPI:
+        comm.barrier()
+    FSIInterface.connect(FSI_config, FluidSolver, SolidSolver)
+
+    if myid == rootProcess:
+        print("\n")
+        print(" Mapping fluid-solid interfaces ".center(80, "*"))
+    if have_MPI:
+        comm.barrier()
+    FSIInterface.interfaceMapping(FluidSolver, SolidSolver, FSI_config)
 
-  if have_MPI:
-    comm.barrier()
+    if have_MPI:
+        comm.barrier()
+
+    if FSI_config["MAPPING_MODES"] == "NO":
+        # --- Launch a steady or unsteady FSI computation --- #
+        if FSI_config["TIME_MARCHING"] == "YES":
+            try:
+                FSIInterface.UnsteadyFSI(FSI_config, FluidSolver, SolidSolver)
+            except NameError as exception:
+                if myid == rootProcess:
+                    print(
+                        "An NameError occured in FSIInterface.UnsteadyFSI : ", exception
+                    )
+            except TypeError as exception:
+                if myid == rootProcess:
+                    print(
+                        "A TypeError occured in FSIInterface.UnsteadyFSI : ", exception
+                    )
+            except KeyboardInterrupt as exception:
+                if myid == rootProcess:
+                    print(
+                        "A KeyboardInterrupt occured in FSIInterface.UnsteadyFSI : ",
+                        exception,
+                    )
+        else:
+            try:
+                FSIInterface.SteadyFSI(FSI_config, FluidSolver, SolidSolver)
+            except NameError as exception:
+                if myid == rootProcess:
+                    print(
+                        "An NameError occured in FSIInterface.SteadyFSI : ", exception
+                    )
+            except TypeError as exception:
+                if myid == rootProcess:
+                    print("A TypeError occured in FSIInterface.SteadyFSI : ", exception)
+            except KeyboardInterrupt as exception:
+                if myid == rootProcess:
+                    print(
+                        "A KeyboardInterrupt occured in FSIInterface.SteadyFSI : ",
+                        exception,
+                    )
+    else:
+        try:
+            FSIInterface.MapModes(FSI_config, FluidSolver, SolidSolver)
+        except NameError as exception:
+            if myid == rootProcess:
+                print("An NameError occured in FSIInterface.MapModes : ", exception)
+        except TypeError as exception:
+            if myid == rootProcess:
+                print("A TypeError occured in FSIInterface.MapModes : ", exception)
+        except KeyboardInterrupt as exception:
+            if myid == rootProcess:
+                print(
+                    "A KeyboardInterrupt occured in FSIInterface.MapModes : ", exception
+                )
+
+    if have_MPI:
+        comm.barrier()
+
+    # --- Exit cleanly the fluid and solid solvers --- #
+    FluidSolver.Postprocessing()
+    if myid == rootProcess:
+        SolidSolver.exit()
+
+    if have_MPI:
+        comm.barrier()
 
-  # stops timer
-  stop = timer.time()
-  elapsedTime = stop-start
+    # stops timer
+    stop = timer.time()
+    elapsedTime = stop - start
 
-  if myid == rootProcess:
-    print("\n Computation successfully performed in {} seconds.".format(elapsedTime))
+    if myid == rootProcess:
+        print(
+            "\n Computation successfully performed in {} seconds.".format(elapsedTime)
+        )
+
+    return
 
-  return
 
 # -------------------------------------------------------------------
 #  Run Main Program
 # -------------------------------------------------------------------
 
 # --- This is only accessed if running from command prompt --- #
-if __name__ == '__main__':
+if __name__ == "__main__":
     main()
diff --git a/SU2_PY/merge_solution.py b/SU2_PY/merge_solution.py
index e7a0c3954e5..87f7ae06f1b 100755
--- a/SU2_PY/merge_solution.py
+++ b/SU2_PY/merge_solution.py
@@ -32,36 +32,44 @@
 #  Main
 # -------------------------------------------------------------------
 
+
 def main():
 
     parser = OptionParser()
-    parser.add_option("-f", "--file", dest="filename",
-                      help="read config from FILE", metavar="FILE")
-    parser.add_option("-n", "--partitions", dest="partitions", default=-1,
-                      help="number of PARTITIONS", metavar="PARTITIONS")
+    parser.add_option(
+        "-f", "--file", dest="filename", help="read config from FILE", metavar="FILE"
+    )
+    parser.add_option(
+        "-n",
+        "--partitions",
+        dest="partitions",
+        default=-1,
+        help="number of PARTITIONS",
+        metavar="PARTITIONS",
+    )
 
-    (options, args)=parser.parse_args()
+    (options, args) = parser.parse_args()
     options.partitions = int(options.partitions)
 
-    merge_solution( options.filename   ,
-                    options.partitions  )
+    merge_solution(options.filename, options.partitions)
 
 
 # -------------------------------------------------------------------
 #  MERGE SOLUTION
 # -------------------------------------------------------------------
 
-def merge_solution( filename        ,
-                    partitions = -1  ):
+
+def merge_solution(filename, partitions=-1):
 
     config = SU2.io.Config(filename)
 
-    if partitions > -1 :
+    if partitions > -1:
         config.NUMBER_PART = partitions
 
     SU2.run.merge(config)
 
+
 #: def merge_solution()
 
-if __name__ == '__main__':
+if __name__ == "__main__":
     main()
diff --git a/SU2_PY/mesh_deformation.py b/SU2_PY/mesh_deformation.py
index 37eecb19544..b77b0269d0c 100755
--- a/SU2_PY/mesh_deformation.py
+++ b/SU2_PY/mesh_deformation.py
@@ -27,28 +27,38 @@
 
 import os, sys
 from optparse import OptionParser
-sys.path.append(os.environ['SU2_RUN'])
+
+sys.path.append(os.environ["SU2_RUN"])
 import SU2
 
 # -------------------------------------------------------------------
 #  Main
 # -------------------------------------------------------------------
 
+
 def main():
 
     # Command Line Options
     parser = OptionParser()
-    parser.add_option("-f", "--file", dest="filename",
-                      help="read config from FILE", metavar="FILE")
-    parser.add_option("-n", "--partitions", dest="partitions", default=2,
-                      help="number of PARTITIONS", metavar="PARTITIONS")
-
-    (options, args)=parser.parse_args()
-    options.partitions = int( options.partitions )
+    parser.add_option(
+        "-f", "--file", dest="filename", help="read config from FILE", metavar="FILE"
+    )
+    parser.add_option(
+        "-n",
+        "--partitions",
+        dest="partitions",
+        default=2,
+        help="number of PARTITIONS",
+        metavar="PARTITIONS",
+    )
+
+    (options, args) = parser.parse_args()
+    options.partitions = int(options.partitions)
 
     # Run Parallel Comutation
-    mesh_deformation ( options.filename    ,
-                       options.partitions   )
+    mesh_deformation(options.filename, options.partitions)
+
+
 #: def main()
 
 
@@ -56,8 +66,8 @@ def main():
 #  Parallel Computation Function
 # -------------------------------------------------------------------
 
-def mesh_deformation( filename           ,
-                      partitions  = 2     ):
+
+def mesh_deformation(filename, partitions=2):
 
     # Config
     config = SU2.io.Config(filename)
@@ -75,6 +85,7 @@ def mesh_deformation( filename           ,
 
     return state
 
+
 #: mesh_deformation()
 
 
@@ -83,7 +94,5 @@ def mesh_deformation( filename           ,
 # -------------------------------------------------------------------
 
 # this is only accessed if running from command prompt
-if __name__ == '__main__':
+if __name__ == "__main__":
     main()
-
-
diff --git a/SU2_PY/package_tests.py b/SU2_PY/package_tests.py
index b15f475b408..186f86e4ec5 100755
--- a/SU2_PY/package_tests.py
+++ b/SU2_PY/package_tests.py
@@ -29,7 +29,8 @@
 from __future__ import print_function
 
 import os, sys, copy
-sys.path.append(os.environ['SU2_RUN'])
+
+sys.path.append(os.environ["SU2_RUN"])
 import SU2
 
 from collections import OrderedDict
@@ -58,89 +59,97 @@
 
 def main():
 
-    #io0()       # working
-    #io1()
-    #level0()    # working
-    #level1()    # working
-    #level2()    # working
-    #level3()    # working
-    #level4()    # working
-    #level5()    # working
+    # io0()       # working
+    # io1()
+    # level0()    # working
+    # level1()    # working
+    # level2()    # working
+    # level3()    # working
+    # level4()    # working
+    # level5()    # working
+
+    print("DONE!")
 
-    print('DONE!')
 
 def io0():
-    folder='test_io0'; pull='config_NACA0012.cfg'; link='mesh_NACA0012.su2'
-    with SU2.io.redirect_folder(folder,pull,link):
+    folder = "test_io0"
+    pull = "config_NACA0012.cfg"
+    link = "mesh_NACA0012.su2"
+    with SU2.io.redirect_folder(folder, pull, link):
 
-        config_name = 'config_NACA0012.cfg'
+        config_name = "config_NACA0012.cfg"
         config = SU2.io.Config(filename=config_name)
 
         print(config)
 
-
         config.ADAPT_CYCLES
-        config['ADAPT_CYCLES']
+        config["ADAPT_CYCLES"]
 
-        config.dump('out.cfg')
+        config.dump("out.cfg")
 
         konfig = copy.deepcopy(config)
-        konfig['TASKS'] = ['TEST']
-        konfig['NUMBER_PART'] = 0
+        konfig["TASKS"] = ["TEST"]
+        konfig["NUMBER_PART"] = 0
 
         config_diff = config.diff(konfig)
 
         print(config_diff)
 
-
     wait = 0
 
+
 def io1():
 
     option = SU2.io.config.MathProblem()
 
-    option = 'DIRECT'
+    option = "DIRECT"
 
     wait = 0
 
+
 def level0():
-    folder='test_level0'; pull='config_NACA0012.cfg'; link='mesh_NACA0012.su2'
-    with SU2.io.redirect_folder(folder,pull,link):
+    folder = "test_level0"
+    pull = "config_NACA0012.cfg"
+    link = "mesh_NACA0012.su2"
+    with SU2.io.redirect_folder(folder, pull, link):
 
         # Setup
-        config_name = 'config_NACA0012.cfg'
+        config_name = "config_NACA0012.cfg"
         config = SU2.io.Config(config_name)
         config.EXT_ITER = 9
         config.NUMBER_PART = 2
 
         SU2.run.CFD(config)
 
+
 def level1():
-    folder='test_level1'; pull='config_NACA0012.cfg'; link='mesh_NACA0012.su2'
-    with SU2.io.redirect_folder(folder,pull,link):
+    folder = "test_level1"
+    pull = "config_NACA0012.cfg"
+    link = "mesh_NACA0012.su2"
+    with SU2.io.redirect_folder(folder, pull, link):
 
         # Setup
-        config_name = 'config_NACA0012.cfg'
+        config_name = "config_NACA0012.cfg"
         config = SU2.io.Config(config_name)
-        config['NUMBER_PART'] = 2
-        config['EXT_ITER'] = 9
+        config["NUMBER_PART"] = 2
+        config["EXT_ITER"] = 9
 
         state = SU2.io.State()
 
         # Deformation
-        dv_new = [0.002]*38
-        info = SU2.run.deform(config,dv_new)
+        dv_new = [0.002] * 38
+        info = SU2.run.deform(config, dv_new)
         state.update(info)
 
         # Direct Solution
         info = SU2.run.direct(config)
         state.update(info)
-        SU2.io.restart2solution(config,state)
+        SU2.io.restart2solution(config, state)
 
         # Adjoint Solution
         info = SU2.run.adjoint(config)
         state.update(info)
-        SU2.io.restart2solution(config,state)
+        SU2.io.restart2solution(config, state)
 
         # Gradient Projection
         info = SU2.run.projection(config)
@@ -148,143 +157,159 @@ def level1():
 
         print(state)
 
-        SU2.io.save_data('state.pkl',state)
-        data = SU2.io.load_data('state.pkl')
+        SU2.io.save_data("state.pkl", state)
+        data = SU2.io.load_data("state.pkl")
 
-        SU2.io.save_data('config.pkl',config)
-        data = SU2.io.load_data('config.pkl')
+        SU2.io.save_data("config.pkl", config)
+        data = SU2.io.load_data("config.pkl")
 
     wait = 0
 
+
 def level2():
-    folder='test_level2'; pull='config_NACA0012.cfg'; link='mesh_NACA0012.su2'
-    with SU2.io.redirect_folder(folder,pull,link):
+    folder = "test_level2"
+    pull = "config_NACA0012.cfg"
+    link = "mesh_NACA0012.su2"
+    with SU2.io.redirect_folder(folder, pull, link):
 
         # Setup
-        config_name = 'config_NACA0012.cfg'
+        config_name = "config_NACA0012.cfg"
         config = SU2.io.Config(config_name)
-        config['NUMBER_PART'] = 2
-        config['EXT_ITER'] = 9
-        dv_new = [0.0]*38
-        #dv_new[10] = 0.05
+        config["NUMBER_PART"] = 2
+        config["EXT_ITER"] = 9
+        dv_new = [0.0] * 38
+        # dv_new[10] = 0.05
         config.unpack_dvs(dv_new)
 
         state = SU2.io.State()
 
-        #with SU2.io.redirect.folder(folder='JOB_001',link='mesh_NACA0012.su2'):
+        # with SU2.io.redirect.folder(folder='JOB_001',link='mesh_NACA0012.su2'):
         #    grad = SU2.eval.grad( 'DRAG', 'FINDIFF', config, state )
 
-        with SU2.io.redirect_folder(folder='JOB_001',link='mesh_NACA0012.su2'):
-            func  = SU2.eval.func( 'LIFT', config, state )
-            grads = SU2.eval.grad( 'LIFT', 'CONTINUOUS_ADJOINT', config, state )
+        with SU2.io.redirect_folder(folder="JOB_001", link="mesh_NACA0012.su2"):
+            func = SU2.eval.func("LIFT", config, state)
+            grads = SU2.eval.grad("LIFT", "CONTINUOUS_ADJOINT", config, state)
 
-        with SU2.io.redirect_folder(folder='JOB_001',link='mesh_NACA0012.su2'):
-            func  = SU2.eval.func( 'DRAG', config, state ) # will not run direct
-            grads = SU2.eval.grad( 'LIFT', 'CONTINUOUS_ADJOINT', config, state ) # will not run adjoint
-            grads = SU2.eval.grad( 'DRAG', 'CONTINUOUS_ADJOINT', config, state ) # will run adjoint
+        with SU2.io.redirect_folder(folder="JOB_001", link="mesh_NACA0012.su2"):
+            func = SU2.eval.func("DRAG", config, state)  # will not run direct
+            grads = SU2.eval.grad(
+                "LIFT", "CONTINUOUS_ADJOINT", config, state
+            )  # will not run adjoint
+            grads = SU2.eval.grad(
+                "DRAG", "CONTINUOUS_ADJOINT", config, state
+            )  # will run adjoint
 
     wait = 0
 
+
 def level3():
-    folder='test_level3'; pull='config_NACA0012.cfg'; link='mesh_NACA0012.su2'
-    with SU2.io.redirect_folder(folder,pull,link):
+    folder = "test_level3"
+    pull = "config_NACA0012.cfg"
+    link = "mesh_NACA0012.su2"
+    with SU2.io.redirect_folder(folder, pull, link):
 
         # Setup
-        config_name = 'config_NACA0012.cfg'
+        config_name = "config_NACA0012.cfg"
         config = SU2.io.Config(config_name)
-        config['NUMBER_PART'] = 2
-        config['EXT_ITER'] = 9
+        config["NUMBER_PART"] = 2
+        config["EXT_ITER"] = 9
 
         # initialize design state
         state = SU2.io.State()
         state.find_files(config)
 
         # start design
-        design = SU2.eval.Design(config,state)
+        design = SU2.eval.Design(config, state)
 
         # run design with dv change
-        dv_new = [0.0]*38
+        dv_new = [0.0] * 38
         vals = design.obj_f(dv_new)
         vals = design.obj_df(dv_new)
         vals = design.con_ceq(dv_new)
         vals = design.con_dceq(dv_new)
         vals = design.con_cieq(dv_new)
         vals = design.con_dcieq(dv_new)
-        vals = design.func('LIFT')
-        vals = design.grad('LIFT','CONTINUOUS_ADJOINT')
+        vals = design.func("LIFT")
+        vals = design.grad("LIFT", "CONTINUOUS_ADJOINT")
 
-        SU2.io.save_data('design.pkl',design)
-        data = SU2.io.load_data('design.pkl')
+        SU2.io.save_data("design.pkl", design)
+        data = SU2.io.load_data("design.pkl")
 
     wait = 0
 
+
 def level4():
-    folder='test_level4'; pull='config_NACA0012.cfg'; link='mesh_NACA0012.su2'
-    with SU2.io.redirect_folder(folder,pull,link):
+    folder = "test_level4"
+    pull = "config_NACA0012.cfg"
+    link = "mesh_NACA0012.su2"
+    with SU2.io.redirect_folder(folder, pull, link):
 
         # Setup
-        config_name = 'config_NACA0012.cfg'
+        config_name = "config_NACA0012.cfg"
         config = SU2.io.Config(config_name)
-        config['NUMBER_PART'] = 2
-        config['EXT_ITER'] = 9
-        config.CONSOLE = 'QUIET'
+        config["NUMBER_PART"] = 2
+        config["EXT_ITER"] = 9
+        config.CONSOLE = "QUIET"
 
         # initialize design state
         state = SU2.io.State()
         state.find_files(config)
 
         # initialize project
-        project = SU2.opt.Project(config,state)
+        project = SU2.opt.Project(config, state)
 
         # run project with dv changes
-        dv_new = [0.0]*38
+        dv_new = [0.0] * 38
         vals = project.obj_f(dv_new)
         vals = project.obj_df(dv_new)
 
-        dv_new = [-0.005]*38
+        dv_new = [-0.005] * 38
         vals = project.obj_f(dv_new)
 
-        dv_new = [0.0]*38
+        dv_new = [0.0] * 38
         dv_new[9] = -0.02
         vals = project.obj_f(dv_new)
 
-        dv_new = [0.005]*38
-        vals = project.obj_f(dv_new) # will not rerun solutions
+        dv_new = [0.005] * 38
+        vals = project.obj_f(dv_new)  # will not rerun solutions
 
-        SU2.io.save_data('project.pkl',project)
-        data = SU2.io.load_data('project.pkl')
+        SU2.io.save_data("project.pkl", project)
+        data = SU2.io.load_data("project.pkl")
 
         data = project.data
 
     wait = 0
     print("Done!")
 
+
 def level5():
-    folder='test_level5'; pull='config_NACA0012.cfg'; link='mesh_NACA0012.su2'
-    with SU2.io.redirect_folder(folder,pull,link):
+    folder = "test_level5"
+    pull = "config_NACA0012.cfg"
+    link = "mesh_NACA0012.su2"
+    with SU2.io.redirect_folder(folder, pull, link):
 
         # Setup
-        config_name = 'config_NACA0012.cfg'
+        config_name = "config_NACA0012.cfg"
         config = SU2.io.Config(config_name)
-        config['NUMBER_PART'] = 2
-        config['EXT_ITER'] = 9
-        config['CONSOLE'] = 'CONCISE'
+        config["NUMBER_PART"] = 2
+        config["EXT_ITER"] = 9
+        config["CONSOLE"] = "CONCISE"
 
         # set optimization problem
         obj = {}
-        obj['DRAG'] = {'SCALE':1.e-2}
+        obj["DRAG"] = {"SCALE": 1.0e-2}
 
         cons = {}
-        cons['EQUALITY'] = {}
-        cons['INEQUALITY'] = {}
-        cons['INEQUALITY']['LIFT']     = {'SIGN':'>','VALUE':0.328188,'SCALE':1e-1}
-        cons['INEQUALITY']['MOMENT_Z'] = {'SIGN':'>','VALUE':0.034068,'SCALE':1e-2}
+        cons["EQUALITY"] = {}
+        cons["INEQUALITY"] = {}
+        cons["INEQUALITY"]["LIFT"] = {"SIGN": ">", "VALUE": 0.328188, "SCALE": 1e-1}
+        cons["INEQUALITY"]["MOMENT_Z"] = {"SIGN": ">", "VALUE": 0.034068, "SCALE": 1e-2}
 
         def_dv = config.DEFINITION_DV
-        n_dv   = sum(def_dv['KIND'])
-        def_dv['SCALE'] = [1.e0]*n_dv
+        n_dv = sum(def_dv["KIND"])
+        def_dv["SCALE"] = [1.0e0] * n_dv
 
-        config.OPT_OBJECTIVE  = obj
+        config.OPT_OBJECTIVE = obj
         config.OPT_CONSTRAINT = cons
 
         # initialize design state
@@ -292,17 +317,18 @@ def level5():
         state.find_files(config)
 
         # initialize project
-        project = SU2.opt.Project(config,state)
+        project = SU2.opt.Project(config, state)
 
         # optimization setup
-        x0 = [0.0]*n_dv
-        xb = [] #[[-0.02,0.02]]*n_dv
+        x0 = [0.0] * n_dv
+        xb = []  # [[-0.02,0.02]]*n_dv
         its = 20
 
         # optimize
-        SU2.opt.SLSQP(project,x0,xb,its)
+        SU2.opt.SLSQP(project, x0, xb, its)
 
     wait = 0
 
-if __name__ == '__main__':
+
+if __name__ == "__main__":
     main()
diff --git a/SU2_PY/parallel_computation.py b/SU2_PY/parallel_computation.py
index 001ce0c5eba..a20a5bfb088 100755
--- a/SU2_PY/parallel_computation.py
+++ b/SU2_PY/parallel_computation.py
@@ -27,34 +27,48 @@
 
 import os, sys
 from optparse import OptionParser
-sys.path.append(os.environ['SU2_RUN'])
+
+sys.path.append(os.environ["SU2_RUN"])
 import SU2
 
 # -------------------------------------------------------------------
 #  Main
 # -------------------------------------------------------------------
 
+
 def main():
 
     # Command Line Options
-    parser=OptionParser()
-    parser.add_option("-f", "--file",       dest="filename",
-                      help="read config from FILE", metavar="FILE")
-    parser.add_option("-n", "--partitions", dest="partitions", default=2,
-                      help="number of PARTITIONS", metavar="PARTITIONS")
-    parser.add_option("-c", "--compute",    dest="compute",    default="True",
-                      help="COMPUTE direct and adjoint problem", metavar="COMPUTE")
-
-    (options, args)=parser.parse_args()
-    options.partitions  = int( options.partitions )
-    options.compute     = options.compute.upper() == 'TRUE'
+    parser = OptionParser()
+    parser.add_option(
+        "-f", "--file", dest="filename", help="read config from FILE", metavar="FILE"
+    )
+    parser.add_option(
+        "-n",
+        "--partitions",
+        dest="partitions",
+        default=2,
+        help="number of PARTITIONS",
+        metavar="PARTITIONS",
+    )
+    parser.add_option(
+        "-c",
+        "--compute",
+        dest="compute",
+        default="True",
+        help="COMPUTE direct and adjoint problem",
+        metavar="COMPUTE",
+    )
+
+    (options, args) = parser.parse_args()
+    options.partitions = int(options.partitions)
+    options.compute = options.compute.upper() == "TRUE"
 
     if options.filename == None:
         raise Exception("No config file provided. Use -f flag")
 
-    parallel_computation( options.filename    ,
-                          options.partitions  ,
-                          options.compute      )
+    parallel_computation(options.filename, options.partitions, options.compute)
+
 
 #: def main()
 
@@ -63,9 +77,8 @@ def main():
 #  CFD Solution
 # -------------------------------------------------------------------
 
-def parallel_computation( filename           ,
-                          partitions  = 0    ,
-                          compute     = True  ):
+
+def parallel_computation(filename, partitions=0, compute=True):
 
     # Config
     config = SU2.io.Config(filename)
@@ -89,15 +102,16 @@ def parallel_computation( filename           ,
     state.update(info)
 
     # Solution merging
-    if config.MATH_PROBLEM == 'DIRECT':
+    if config.MATH_PROBLEM == "DIRECT":
         config.SOLUTION_FILENAME = config.RESTART_FILENAME
-    elif config.MATH_PROBLEM in ['CONTINUOUS_ADJOINT', 'DISCRETE_ADJOINT']:
+    elif config.MATH_PROBLEM in ["CONTINUOUS_ADJOINT", "DISCRETE_ADJOINT"]:
         config.SOLUTION_ADJ_FILENAME = config.RESTART_ADJ_FILENAME
     info = SU2.run.merge(config)
     state.update(info)
 
     return state
 
+
 #: parallel_computation()
 
 
@@ -106,6 +120,5 @@ def parallel_computation( filename           ,
 # -------------------------------------------------------------------
 
 # this is only accessed if running from command prompt
-if __name__ == '__main__':
+if __name__ == "__main__":
     main()
-
diff --git a/SU2_PY/parallel_computation_fsi.py b/SU2_PY/parallel_computation_fsi.py
index e0983038149..20a33338240 100755
--- a/SU2_PY/parallel_computation_fsi.py
+++ b/SU2_PY/parallel_computation_fsi.py
@@ -27,34 +27,48 @@
 
 import os, sys, shutil, copy
 from optparse import OptionParser
-sys.path.append(os.environ['SU2_RUN'])
+
+sys.path.append(os.environ["SU2_RUN"])
 import SU2
 
 # -------------------------------------------------------------------
 #  Main
 # -------------------------------------------------------------------
 
+
 def main():
 
     # Command Line Options
-    parser=OptionParser()
-    parser.add_option("-f", "--file",       dest="filename",
-                      help="read config from FILE", metavar="FILE")
-    parser.add_option("-n", "--partitions", dest="partitions", default=2,
-                      help="number of PARTITIONS", metavar="PARTITIONS")
-    parser.add_option("-c", "--compute",    dest="compute",    default="True",
-                      help="COMPUTE direct and adjoint problem", metavar="COMPUTE")
-
-    (options, args)=parser.parse_args()
-    options.partitions  = int( options.partitions )
-    options.compute     = options.compute.upper() == 'TRUE'
+    parser = OptionParser()
+    parser.add_option(
+        "-f", "--file", dest="filename", help="read config from FILE", metavar="FILE"
+    )
+    parser.add_option(
+        "-n",
+        "--partitions",
+        dest="partitions",
+        default=2,
+        help="number of PARTITIONS",
+        metavar="PARTITIONS",
+    )
+    parser.add_option(
+        "-c",
+        "--compute",
+        dest="compute",
+        default="True",
+        help="COMPUTE direct and adjoint problem",
+        metavar="COMPUTE",
+    )
+
+    (options, args) = parser.parse_args()
+    options.partitions = int(options.partitions)
+    options.compute = options.compute.upper() == "TRUE"
 
     if options.filename == None:
         raise Exception("No config file provided. Use -f flag")
 
-    parallel_computation( options.filename    ,
-                          options.partitions  ,
-                          options.compute      )
+    parallel_computation(options.filename, options.partitions, options.compute)
+
 
 #: def main()
 
@@ -63,9 +77,8 @@ def main():
 #  CFD Solution
 # -------------------------------------------------------------------
 
-def parallel_computation( filename           ,
-                          partitions  = 0    ,
-                          compute     = True  ):
+
+def parallel_computation(filename, partitions=0, compute=True):
 
     # Config
     config = SU2.io.Config(filename)
@@ -85,9 +98,9 @@ def parallel_computation( filename           ,
     state.update(info)
 
     # Solution merging
-    if config.SOLVER == 'FEM_ELASTICITY':
+    if config.SOLVER == "FEM_ELASTICITY":
         config.SOLUTION_FILENAME = config.RESTART_FILENAME
-    elif config.SOLVER == 'FLUID_STRUCTURE_INTERACTION':
+    elif config.SOLVER == "FLUID_STRUCTURE_INTERACTION":
         config.SOLUTION_FILENAME = config.RESTART_FILENAME
         config.SOLUTION_FILENAME = config.RESTART_FILENAME
 
@@ -96,6 +109,7 @@ def parallel_computation( filename           ,
 
     return state
 
+
 #: parallel_computation()
 
 
@@ -104,6 +118,5 @@ def parallel_computation( filename           ,
 # -------------------------------------------------------------------
 
 # this is only accessed if running from command prompt
-if __name__ == '__main__':
+if __name__ == "__main__":
     main()
-
diff --git a/SU2_PY/parse_config.py b/SU2_PY/parse_config.py
index 66d386d68f2..aa57502a683 100755
--- a/SU2_PY/parse_config.py
+++ b/SU2_PY/parse_config.py
@@ -28,226 +28,275 @@
 # make print(*args) function available in PY2.6+, does'nt work on PY < 2.6
 from __future__ import print_function
 
-import os,sys,xlwt
+import os, sys, xlwt
 
 # note: requires xlwt for spreadsheet output
 # http://pypi.python.org/pypi/xlwt
 
-class config_option:
-  option_name        = ""
-  option_type        = ""
-  option_category    = ""
-  option_values      = []
-  option_default     = ""
-  option_description = ""
-
-  def __init__(self,name,otype,category,values,default,description):
-    self.option_name        = name
-    self.option_type        = otype
-    self.option_category    = category
-    self.option_values      = values
-    self.option_default      = default
-    self.option_description = description
-
-  def print_data(self):
-    print('Option Name: %s '%        self.option_name)
-    print('Option Type: %s '%        self.option_type)
-    print('Option Category: %s '%    self.option_category)
-    print('Option values: ',         self.option_values)
-    print('Option default: %s'%      self.option_default)
-    print('Option description: %s '% self.option_description)
-    print('')
-
-def parse_config(config_cpp, config_hpp):
-
-  # List of option types
-  option_types = ['AddEnumOption', 'AddMathProblem', 'AddSpecialOption', 'AddScalarOption', 'AddMarkerOption', 'AddMarkerPeriodic', 'AddMarkerDirichlet', 'AddMarkerInlet', 'AddMarkerOutlet', 'AddMarkerDisplacement', 'AddMarkerLoad', 'AddMarkerFlowLoad', 'AddArrayOption', 'AddListOption', 'AddConvectOption', 'AddEnumListOption', 'AddDVParamOption']
-
-  # Build a dictionary of enum options from hpp file
-  enum_options = {}
-  f = open(config_hpp,'r')
-  while(1):  # Find beginning of enum definitions
-    s = f.readline()
-    if s.find('BEGIN_CONFIG_ENUMS') >-1:
-      break
-  while(1):
-    s = f.readline()
-    if s.find('END_CONFIG_ENUMS')>-1:
-      break   # Reached end
-
-    if s.find('CCreateMap')>-1:
-      dict_key = (s.split('=')[0]).split('>')[1].strip()
-      dict_val = []
-      while(1):
-        s2 = f.readline()
-        thisval = s2.split('"')[1]
-        dict_val.append(thisval)
-        if s2.find(';')>-1:
-          break;
-      enum_options[dict_key] = dict_val
-  f.close()
-
-  # Temporary: For now, build a list of all of the schemes
-  scheme_list   = enum_options['Upwind_Map']
-  scheme_list.extend(enum_options['Centered_Map'][1:])
-  # Read the Options section of config_structure.cpp into a list of strings
-  lines = []
-  f = open(config_cpp,'r')
-  while(1):
-    s = f.readline()
-    if s.find('BEGIN_CONFIG_OPTIONS')>-1:
-      break
-  while(1):
-    s = f.readline()
-    # Check if we've reached the end
-    if s.find('END_CONFIG_OPTIONS')>-1:
-      break
-    lines.append(s)
-  f.close()
-
-  option_list = []
-  present_category = "None"
-  #----- Main text parsing loop -----
-  for j,line in enumerate(lines):
-
-    # Check for a category description
-    if line.find('CONFIG_CATEGORY')>-1:
-      present_category = line.split(':')[1].strip().strip('*/').strip()
-      print(present_category)
-
-    # Check for an option type
-    for option_type in option_types:
-      if line.find(option_type)>-1:  # Found an option
-        # Get option name
-        name = line.split('"')[1]
-
-        # Permitted values
-        values = ['YES','NO']
-        if option_type=='AddEnumOption':
-          try:
-            enum_mapname = line.split(',')[2].strip()
-            values = enum_options[enum_mapname]
-          except KeyError:
-            print("KeyError, key=%s"%enum_mapname)
-            print("enum_options: ",enum_options)
-            sys.exit(1)
-          except TypeError:
-            print("TypeError, key=%s"%enum_mapname)
-            print("enum_options: ",enum_options)
-            sys.exit(1)
-        elif option_type=='AddMathProblem':
-          values = ['DIRECT','CONTINUOUS_ADJOINT','LINEARIZED']
-        elif option_type=='AddScalarOption':
-          values = ['A scalar constant']
-        elif option_type in ('AddMarkerOption', 'AddMarkerPeriodic', 'AddMarkerDirichlet', 'AddMarkerInlet', 'AddMarkerOutlet', 'AddMarkerDisplacement', 'AddMarkerLoad', 'AddMarkerFlowLoad'):
-          values = ['Valid marker name from grid file']
-        elif option_type == 'AddArrayOption':
-          values = ['Array']
-        elif option_type == 'AddListOption':
-          values = ['List']
-        elif option_type == 'AddConvectOption':
-          values = scheme_list
-          print("Convect Option: ", name)
-        elif option_type == 'AddEnumListOption':
-          values = ['Enum list']
-        elif option_type == 'AddDVParamOption':
-          values = ['DV Param']
-
-        # A first pass at finding the default value (Check the last item in parenthesis)
-        jdefault = j
-        while(lines[jdefault].find(';')==-1):
-          jdefault = jdefault+1
-        default = lines[jdefault].strip().strip(');').split(',')[-1].strip().strip('"')
-
-        # A whole bunch of corrections for what the default should be...
-        if default.find('string("')==0:
-          default = default.split('"')[1]
-        if default=="default_vec_3d":
-          default = '(1.0, 100.0, 1.0)'
-        if default=="default_vec_6d":
-          default = '( -1E15, -1E15, -1E15, 1E15, 1E15, 1E15 )'
-        if option_type == "AddMathProblem":
-          default = 'DIRECT'
-        if option_type == "AddConvectOption":
-          default = 'ROE-1ST_ORDER'
-        if default == 'RK_Alpha_Step':
-          default = '( 0.66667, 0.66667, 1.000000 )'
-        if default == 'RK_Beta_Step':
-          default = '( 1.00000, 0.00000, 0.00000 )'
-
-        if default=='false':
-          default='NO'
-        elif default=='true':
-          default='YES'
-
-        # Check for a description tag
-        description = "No description"
-        if lines[j-1].find('DESCRIPTION')>-1:
-          description = lines[j-1].split(':')[1].strip().strip('*/').strip()
-
-        # Add a new option
-        option_list.append(config_option(name,option_type[3:],present_category,values,default,description))
-
-        break
-
-  return option_list
-
-def print_all(option_list):
-  # Dumps the option list to screen
-  for option in option_list:
-    option.print_data()
-
-def make_spreadsheet(filename, option_list):
-
-  wbk   = xlwt.Workbook()
 
-  sheet_name = ""
-  jp = 0
-  for j,opt in enumerate(option_list):
-    jp = jp+1
-    if not sheet_name==opt.option_category:
-      # Create new sheet for new category
-      sheet_name = opt.option_category
-      sheet = wbk.add_sheet(sheet_name[:31].replace('/','-'))
-
-      # Write spreadsheet header
-      sheet.write(0,0,'Option Name')
-      sheet.write(0,1,'Option Type')
-      sheet.write(0,2,'Option Category')
-      sheet.write(0,3,'Option Values')
-      sheet.write(0,4,'Option Default')
-      sheet.write(0,5,'Option Description')
-      jp = 1
-
-
-    sheet.write(jp,0,opt.option_name)
-    sheet.write(jp,1,opt.option_type)
-    sheet.write(jp,2,opt.option_category)
-    sheet.write(jp,3,(',').join(opt.option_values))
-    sheet.write(jp,4,opt.option_default)
-    sheet.write(jp,5,opt.option_description)
-
-  wbk.save(filename)
+class config_option:
+    option_name = ""
+    option_type = ""
+    option_category = ""
+    option_values = []
+    option_default = ""
+    option_description = ""
+
+    def __init__(self, name, otype, category, values, default, description):
+        self.option_name = name
+        self.option_type = otype
+        self.option_category = category
+        self.option_values = values
+        self.option_default = default
+        self.option_description = description
+
+    def print_data(self):
+        print("Option Name: %s " % self.option_name)
+        print("Option Type: %s " % self.option_type)
+        print("Option Category: %s " % self.option_category)
+        print("Option values: ", self.option_values)
+        print("Option default: %s" % self.option_default)
+        print("Option description: %s " % self.option_description)
+        print("")
 
 
+def parse_config(config_cpp, config_hpp):
 
-if __name__=="__main__":
+    # List of option types
+    option_types = [
+        "AddEnumOption",
+        "AddMathProblem",
+        "AddSpecialOption",
+        "AddScalarOption",
+        "AddMarkerOption",
+        "AddMarkerPeriodic",
+        "AddMarkerDirichlet",
+        "AddMarkerInlet",
+        "AddMarkerOutlet",
+        "AddMarkerDisplacement",
+        "AddMarkerLoad",
+        "AddMarkerFlowLoad",
+        "AddArrayOption",
+        "AddListOption",
+        "AddConvectOption",
+        "AddEnumListOption",
+        "AddDVParamOption",
+    ]
+
+    # Build a dictionary of enum options from hpp file
+    enum_options = {}
+    f = open(config_hpp, "r")
+    while 1:  # Find beginning of enum definitions
+        s = f.readline()
+        if s.find("BEGIN_CONFIG_ENUMS") > -1:
+            break
+    while 1:
+        s = f.readline()
+        if s.find("END_CONFIG_ENUMS") > -1:
+            break  # Reached end
+
+        if s.find("CCreateMap") > -1:
+            dict_key = (s.split("=")[0]).split(">")[1].strip()
+            dict_val = []
+            while 1:
+                s2 = f.readline()
+                thisval = s2.split('"')[1]
+                dict_val.append(thisval)
+                if s2.find(";") > -1:
+                    break
+            enum_options[dict_key] = dict_val
+    f.close()
+
+    # Temporary: For now, build a list of all of the schemes
+    scheme_list = enum_options["Upwind_Map"]
+    scheme_list.extend(enum_options["Centered_Map"][1:])
+    # Read the Options section of config_structure.cpp into a list of strings
+    lines = []
+    f = open(config_cpp, "r")
+    while 1:
+        s = f.readline()
+        if s.find("BEGIN_CONFIG_OPTIONS") > -1:
+            break
+    while 1:
+        s = f.readline()
+        # Check if we've reached the end
+        if s.find("END_CONFIG_OPTIONS") > -1:
+            break
+        lines.append(s)
+    f.close()
+
+    option_list = []
+    present_category = "None"
+    # ----- Main text parsing loop -----
+    for j, line in enumerate(lines):
+
+        # Check for a category description
+        if line.find("CONFIG_CATEGORY") > -1:
+            present_category = line.split(":")[1].strip().strip("*/").strip()
+            print(present_category)
+
+        # Check for an option type
+        for option_type in option_types:
+            if line.find(option_type) > -1:  # Found an option
+                # Get option name
+                name = line.split('"')[1]
+
+                # Permitted values
+                values = ["YES", "NO"]
+                if option_type == "AddEnumOption":
+                    try:
+                        enum_mapname = line.split(",")[2].strip()
+                        values = enum_options[enum_mapname]
+                    except KeyError:
+                        print("KeyError, key=%s" % enum_mapname)
+                        print("enum_options: ", enum_options)
+                        sys.exit(1)
+                    except TypeError:
+                        print("TypeError, key=%s" % enum_mapname)
+                        print("enum_options: ", enum_options)
+                        sys.exit(1)
+                elif option_type == "AddMathProblem":
+                    values = ["DIRECT", "CONTINUOUS_ADJOINT", "LINEARIZED"]
+                elif option_type == "AddScalarOption":
+                    values = ["A scalar constant"]
+                elif option_type in (
+                    "AddMarkerOption",
+                    "AddMarkerPeriodic",
+                    "AddMarkerDirichlet",
+                    "AddMarkerInlet",
+                    "AddMarkerOutlet",
+                    "AddMarkerDisplacement",
+                    "AddMarkerLoad",
+                    "AddMarkerFlowLoad",
+                ):
+                    values = ["Valid marker name from grid file"]
+                elif option_type == "AddArrayOption":
+                    values = ["Array"]
+                elif option_type == "AddListOption":
+                    values = ["List"]
+                elif option_type == "AddConvectOption":
+                    values = scheme_list
+                    print("Convect Option: ", name)
+                elif option_type == "AddEnumListOption":
+                    values = ["Enum list"]
+                elif option_type == "AddDVParamOption":
+                    values = ["DV Param"]
+
+                # A first pass at finding the default value (Check the last item in parenthesis)
+                jdefault = j
+                while lines[jdefault].find(";") == -1:
+                    jdefault = jdefault + 1
+                default = (
+                    lines[jdefault]
+                    .strip()
+                    .strip(");")
+                    .split(",")[-1]
+                    .strip()
+                    .strip('"')
+                )
+
+                # A whole bunch of corrections for what the default should be...
+                if default.find('string("') == 0:
+                    default = default.split('"')[1]
+                if default == "default_vec_3d":
+                    default = "(1.0, 100.0, 1.0)"
+                if default == "default_vec_6d":
+                    default = "( -1E15, -1E15, -1E15, 1E15, 1E15, 1E15 )"
+                if option_type == "AddMathProblem":
+                    default = "DIRECT"
+                if option_type == "AddConvectOption":
+                    default = "ROE-1ST_ORDER"
+                if default == "RK_Alpha_Step":
+                    default = "( 0.66667, 0.66667, 1.000000 )"
+                if default == "RK_Beta_Step":
+                    default = "( 1.00000, 0.00000, 0.00000 )"
+
+                if default == "false":
+                    default = "NO"
+                elif default == "true":
+                    default = "YES"
+
+                # Check for a description tag
+                description = "No description"
+                if lines[j - 1].find("DESCRIPTION") > -1:
+                    description = lines[j - 1].split(":")[1].strip().strip("*/").strip()
+
+                # Add a new option
+                option_list.append(
+                    config_option(
+                        name,
+                        option_type[3:],
+                        present_category,
+                        values,
+                        default,
+                        description,
+                    )
+                )
+
+                break
+
+    return option_list
 
-  # These variables should point to the configuration files
-  su2_home = os.environ['SU2_HOME']
-  config_cpp = os.path.join(su2_home,'Common/src/config_structure.cpp')
-  config_hpp = os.path.join(su2_home,'Common/include/option_structure.hpp')
 
-  # Check that files exist
-  if not os.path.isfile(config_cpp):
-    sys.exit('Could not find cpp file, please check that su2_basedir is set correctly in parse_config.py')
-  if not os.path.isfile(config_hpp):
-    sys.exit('Could not find hpp file, please check that su2_basedir is set correctly in parse_config.py')
+def print_all(option_list):
+    # Dumps the option list to screen
+    for option in option_list:
+        option.print_data()
 
-  # Run the parser
-  option_list = parse_config(config_cpp, config_hpp)
 
-  # Dump parsed data to screen
-  print_all(option_list)
+def make_spreadsheet(filename, option_list):
 
-  #make_spreadsheet('out.xls',option_list)
+    wbk = xlwt.Workbook()
+
+    sheet_name = ""
+    jp = 0
+    for j, opt in enumerate(option_list):
+        jp = jp + 1
+        if not sheet_name == opt.option_category:
+            # Create new sheet for new category
+            sheet_name = opt.option_category
+            sheet = wbk.add_sheet(sheet_name[:31].replace("/", "-"))
+
+            # Write spreadsheet header
+            sheet.write(0, 0, "Option Name")
+            sheet.write(0, 1, "Option Type")
+            sheet.write(0, 2, "Option Category")
+            sheet.write(0, 3, "Option Values")
+            sheet.write(0, 4, "Option Default")
+            sheet.write(0, 5, "Option Description")
+            jp = 1
+
+        sheet.write(jp, 0, opt.option_name)
+        sheet.write(jp, 1, opt.option_type)
+        sheet.write(jp, 2, opt.option_category)
+        sheet.write(jp, 3, (",").join(opt.option_values))
+        sheet.write(jp, 4, opt.option_default)
+        sheet.write(jp, 5, opt.option_description)
+
+    wbk.save(filename)
+
+
+if __name__ == "__main__":
+
+    # These variables should point to the configuration files
+    su2_home = os.environ["SU2_HOME"]
+    config_cpp = os.path.join(su2_home, "Common/src/config_structure.cpp")
+    config_hpp = os.path.join(su2_home, "Common/include/option_structure.hpp")
+
+    # Check that files exist
+    if not os.path.isfile(config_cpp):
+        sys.exit(
+            "Could not find cpp file, please check that su2_basedir is set correctly in parse_config.py"
+        )
+    if not os.path.isfile(config_hpp):
+        sys.exit(
+            "Could not find hpp file, please check that su2_basedir is set correctly in parse_config.py"
+        )
+
+    # Run the parser
+    option_list = parse_config(config_cpp, config_hpp)
+
+    # Dump parsed data to screen
+    print_all(option_list)
+
+    # make_spreadsheet('out.xls',option_list)
diff --git a/SU2_PY/profiling.py b/SU2_PY/profiling.py
index d257257f520..a8894197ffd 100755
--- a/SU2_PY/profiling.py
+++ b/SU2_PY/profiling.py
@@ -32,69 +32,82 @@
 from matplotlib import mlab
 
 parser = OptionParser()
-parser.add_option("-f", "--file", dest="file",
-                  help="profiling CSV file", metavar="FILE")
-(options, args)=parser.parse_args()
+parser.add_option(
+    "-f", "--file", dest="file", help="profiling CSV file", metavar="FILE"
+)
+(options, args) = parser.parse_args()
 
 # Store the file name
 filename = options.file
 
 # Load the csv file with the profiling data
-profile = mlab.csv2rec(filename, comments='#', skiprows=0, checkrows=0)
+profile = mlab.csv2rec(filename, comments="#", skiprows=0, checkrows=0)
 
 # Get total number of groups
 maxID = 0
 for val in range(len(profile.function_name)):
-  if profile.function_id[val] > maxID:
-    maxID = profile.function_id[val]
+    if profile.function_id[val] > maxID:
+        maxID = profile.function_id[val]
 
 # Get some arrays for sorting out the groups
-labels  = [[] for i in range(maxID)]
-fracs   = [[] for i in range(maxID)]
+labels = [[] for i in range(maxID)]
+fracs = [[] for i in range(maxID)]
 explode = [[] for i in range(maxID)]
-calls   = [[] for i in range(maxID)]
+calls = [[] for i in range(maxID)]
 
 # Process the profiling data into group IDs
 for val in range(len(profile.function_name)):
-  labels[profile.function_id[val]-1].append(profile.function_name[val])
-  fracs[profile.function_id[val]-1].append(profile.avg_total_time[val])
-  explode[profile.function_id[val]-1].append(0)
-  calls[profile.function_id[val]-1].append(profile.n_calls[val])
+    labels[profile.function_id[val] - 1].append(profile.function_name[val])
+    fracs[profile.function_id[val] - 1].append(profile.avg_total_time[val])
+    explode[profile.function_id[val] - 1].append(0)
+    calls[profile.function_id[val] - 1].append(profile.n_calls[val])
 
 # Loop over each of the group IDs and make figures
 for val in range(maxID):
 
-  #Create a Pie chart to see the time spent in each subroutine
-  fig = plt.figure(figsize=[18, 8])
-  ax  = fig.add_subplot(121)
-  ax.set_title("Total Time Spent in Each Function");
-
-  # Sort the pieces to make it pretty
-  fracs[val], labels[val],calls[val] = (list(x) for x in zip(*sorted(zip(fracs[val], labels[val], calls[val]))))
-
-  # Call to make the pie chart
-  pie_wedge_collection = ax.pie(fracs[val], explode=explode[val], labels=labels[val],labeldistance=1.05, autopct='%1.1f%%', shadow=False, startangle=0);
-  for pie_wedge in pie_wedge_collection[0]:
-    pie_wedge.set_edgecolor('white')
-
-  # Sort the number of calls again for the bar chart
-  calls[val], labels[val]  = (list(x) for x in zip(*sorted(zip(calls[val], labels[val]))))
-
-  # Create a bar chart for the number of function calls
-  ax = fig.add_subplot(122)
-  ax.set_title("Number of Function Calls");
-  width = 0.35
-  ax.bar(range(len(calls[val])), calls[val], width=width)
-  ax.set_xticks(np.arange(len(calls[val])) + width/2)
-  ax.set_xticklabels(labels[val])
-  ax.set_xlabel('Function')
-  ax.set_ylabel('Calls')
-  fig.autofmt_xdate()
-  fig.subplots_adjust(wspace=0.5)
-
-  # Save a figure for this group
-  filename = 'profile_group_' + str(val) + '.png'
-  fig.savefig(filename,format='png')
-
-  # Uncomment the next line to open the plots on the screen
-  show()
+    # Create a Pie chart to see the time spent in each subroutine
+    fig = plt.figure(figsize=[18, 8])
+    ax = fig.add_subplot(121)
+    ax.set_title("Total Time Spent in Each Function")
+
+    # Sort the pieces to make it pretty
+    fracs[val], labels[val], calls[val] = (
+        list(x) for x in zip(*sorted(zip(fracs[val], labels[val], calls[val])))
+    )
+
+    # Call to make the pie chart
+    pie_wedge_collection = ax.pie(
+        fracs[val],
+        explode=explode[val],
+        labels=labels[val],
+        labeldistance=1.05,
+        autopct="%1.1f%%",
+        shadow=False,
+        startangle=0,
+    )
+    for pie_wedge in pie_wedge_collection[0]:
+        pie_wedge.set_edgecolor("white")
+
+    # Sort the number of calls again for the bar chart
+    calls[val], labels[val] = (
+        list(x) for x in zip(*sorted(zip(calls[val], labels[val])))
+    )
+
+    # Create a bar chart for the number of function calls
+    ax = fig.add_subplot(122)
+    ax.set_title("Number of Function Calls")
+    width = 0.35
+    ax.bar(range(len(calls[val])), calls[val], width=width)
+    ax.set_xticks(np.arange(len(calls[val])) + width / 2)
+    ax.set_xticklabels(labels[val])
+    ax.set_xlabel("Function")
+    ax.set_ylabel("Calls")
+    fig.autofmt_xdate()
+    fig.subplots_adjust(wspace=0.5)
+
+    # Save a figure for this group
+    filename = "profile_group_" + str(val) + ".png"
+    fig.savefig(filename, format="png")
+
+    # Uncomment the next line to open the plots on the screen
+    show()
diff --git a/SU2_PY/pySU2/numpy.i b/SU2_PY/pySU2/numpy.i
index e86dfc47137..b8fdaeb1f0c 100644
--- a/SU2_PY/pySU2/numpy.i
+++ b/SU2_PY/pySU2/numpy.i
@@ -3164,4 +3164,3 @@
 #endif
 
 #endif /* SWIGPYTHON */
-
diff --git a/SU2_PY/set_ffd_design_var.py b/SU2_PY/set_ffd_design_var.py
index d9cef1d8387..6c5c798c3ad 100755
--- a/SU2_PY/set_ffd_design_var.py
+++ b/SU2_PY/set_ffd_design_var.py
@@ -32,217 +32,391 @@
 from numpy import *
 
 parser = OptionParser()
-parser.add_option("-i", "--iDegree", dest="iDegree", default=4,
-                  help="i degree of the FFD box", metavar="IDEGREE")
-parser.add_option("-j", "--jDegree", dest="jDegree", default=4,
-                  help="j degree of the FFD box", metavar="JDEGREE")
-parser.add_option("-k", "--kDegree", dest="kDegree", default=1,
-                  help="k degree of the FFD box", metavar="KDEGREE")
-parser.add_option("-b", "--ffdid", dest="ffd_id", default=0,
-                  help="ID of the FFD box", metavar="FFD_ID")
-parser.add_option("-m", "--marker", dest="marker",
-                  help="marker name of the design surface", metavar="MARKER")
-parser.add_option("-a", "--axis", dest="axis",
-                  help="axis to define twist 'x_Orig, y_Orig, z_Orig, x_End, y_End, z_End'", metavar="AXIS")
-parser.add_option("-s", "--scale", dest="scale", default=1.0,
-                  help="scale factor for the bump functions", metavar="SCALE")
-parser.add_option("-d", "--dimension", dest="dimension", default=3.0,
-                  help="dimension of the problem", metavar="DIMENSION")
-
-(options, args)=parser.parse_args()
+parser.add_option(
+    "-i",
+    "--iDegree",
+    dest="iDegree",
+    default=4,
+    help="i degree of the FFD box",
+    metavar="IDEGREE",
+)
+parser.add_option(
+    "-j",
+    "--jDegree",
+    dest="jDegree",
+    default=4,
+    help="j degree of the FFD box",
+    metavar="JDEGREE",
+)
+parser.add_option(
+    "-k",
+    "--kDegree",
+    dest="kDegree",
+    default=1,
+    help="k degree of the FFD box",
+    metavar="KDEGREE",
+)
+parser.add_option(
+    "-b",
+    "--ffdid",
+    dest="ffd_id",
+    default=0,
+    help="ID of the FFD box",
+    metavar="FFD_ID",
+)
+parser.add_option(
+    "-m",
+    "--marker",
+    dest="marker",
+    help="marker name of the design surface",
+    metavar="MARKER",
+)
+parser.add_option(
+    "-a",
+    "--axis",
+    dest="axis",
+    help="axis to define twist 'x_Orig, y_Orig, z_Orig, x_End, y_End, z_End'",
+    metavar="AXIS",
+)
+parser.add_option(
+    "-s",
+    "--scale",
+    dest="scale",
+    default=1.0,
+    help="scale factor for the bump functions",
+    metavar="SCALE",
+)
+parser.add_option(
+    "-d",
+    "--dimension",
+    dest="dimension",
+    default=3.0,
+    help="dimension of the problem",
+    metavar="DIMENSION",
+)
+
+(options, args) = parser.parse_args()
 
 # Process options
-options.iOrder  = int(options.iDegree) + 1
-options.jOrder  = int(options.jDegree) + 1
-options.kOrder  = int(options.kDegree) + 1
-options.ffd_id  = str(options.ffd_id)
+options.iOrder = int(options.iDegree) + 1
+options.jOrder = int(options.jDegree) + 1
+options.kOrder = int(options.kDegree) + 1
+options.ffd_id = str(options.ffd_id)
 options.marker = str(options.marker)
 options.axis = str(options.axis)
-options.scale  = float(options.scale)
-options.dim  = int(options.dimension)
+options.scale = float(options.scale)
+options.dim = int(options.dimension)
 
 if options.dim == 3:
 
-  print(" ")
-  print("% FFD_CONTROL_POINT (X)")
-
-  iVariable = 0
-  dvList = "DEFINITION_DV= "
-  for kIndex in range(options.kOrder):
+    print(" ")
+    print("% FFD_CONTROL_POINT (X)")
+
+    iVariable = 0
+    dvList = "DEFINITION_DV= "
+    for kIndex in range(options.kOrder):
+        for jIndex in range(options.jOrder):
+            for iIndex in range(options.iOrder):
+                iVariable = iVariable + 1
+                dvList = (
+                    dvList
+                    + "( 11, "
+                    + str(options.scale)
+                    + " | "
+                    + options.marker
+                    + " | "
+                )
+                dvList = (
+                    dvList
+                    + options.ffd_id
+                    + ", "
+                    + str(iIndex)
+                    + ", "
+                    + str(jIndex)
+                    + ", "
+                    + str(kIndex)
+                    + ", 1.0, 0.0, 0.0 )"
+                )
+                if iVariable < (options.iOrder * (options.jOrder) * options.kOrder):
+                    dvList = dvList + "; "
+
+    print(dvList)
+
+    print(" ")
+    print("% FFD_CONTROL_POINT (Y)")
+
+    iVariable = 0
+    dvList = "DEFINITION_DV= "
+    for kIndex in range(options.kOrder):
+        for jIndex in range(options.jOrder):
+            for iIndex in range(options.iOrder):
+                iVariable = iVariable + 1
+                dvList = (
+                    dvList
+                    + "( 11, "
+                    + str(options.scale)
+                    + " | "
+                    + options.marker
+                    + " | "
+                )
+                dvList = (
+                    dvList
+                    + options.ffd_id
+                    + ", "
+                    + str(iIndex)
+                    + ", "
+                    + str(jIndex)
+                    + ", "
+                    + str(kIndex)
+                    + ", 0.0, 1.0, 0.0 )"
+                )
+                if iVariable < (options.iOrder * (options.jOrder) * options.kOrder):
+                    dvList = dvList + "; "
+
+    print(dvList)
+
+    print(" ")
+    print("% FFD_CONTROL_POINT (Z)")
+
+    iVariable = 0
+    dvList = "DEFINITION_DV= "
+    for kIndex in range(options.kOrder):
+        for jIndex in range(options.jOrder):
+            for iIndex in range(options.iOrder):
+                iVariable = iVariable + 1
+                dvList = (
+                    dvList
+                    + "( 11, "
+                    + str(options.scale)
+                    + " | "
+                    + options.marker
+                    + " | "
+                )
+                dvList = (
+                    dvList
+                    + options.ffd_id
+                    + ", "
+                    + str(iIndex)
+                    + ", "
+                    + str(jIndex)
+                    + ", "
+                    + str(kIndex)
+                    + ", 0.0, 0.0, 1.0 )"
+                )
+                if iVariable < (options.iOrder * (options.jOrder) * options.kOrder):
+                    dvList = dvList + "; "
+
+    print(dvList)
+
+    print(" ")
+    print("% FFD_NACELLE (RHO)")
+
+    iVariable = 0
+    dvList = "DEFINITION_DV= "
+    for kIndex in range(options.kOrder):
+        for jIndex in range(1 + options.jOrder / 2):
+            for iIndex in range(options.iOrder):
+                iVariable = iVariable + 1
+                dvList = (
+                    dvList
+                    + "( 12, "
+                    + str(options.scale)
+                    + " | "
+                    + options.marker
+                    + " | "
+                )
+                dvList = (
+                    dvList
+                    + options.ffd_id
+                    + ", "
+                    + str(iIndex)
+                    + ", "
+                    + str(jIndex)
+                    + ", "
+                    + str(kIndex)
+                    + ", 1.0, 0.0 )"
+                )
+                if iVariable < (
+                    options.iOrder * (1 + options.jOrder / 2) * options.kOrder
+                ):
+                    dvList = dvList + "; "
+
+    print(dvList)
+
+    print(" ")
+    print("% FFD_NACELLE (PHI)")
+
+    iVariable = 0
+    dvList = "DEFINITION_DV= "
+    for kIndex in range(options.kOrder):
+        for jIndex in range(1 + options.jOrder / 2):
+            for iIndex in range(options.iOrder):
+                iVariable = iVariable + 1
+                dvList = (
+                    dvList
+                    + "( 12, "
+                    + str(options.scale)
+                    + " | "
+                    + options.marker
+                    + " | "
+                )
+                dvList = (
+                    dvList
+                    + options.ffd_id
+                    + ", "
+                    + str(iIndex)
+                    + ", "
+                    + str(jIndex)
+                    + ", "
+                    + str(kIndex)
+                    + ", 0.0, 1.0 )"
+                )
+                if iVariable < (
+                    options.iOrder * (1 + options.jOrder / 2) * options.kOrder
+                ):
+                    dvList = dvList + "; "
+
+    print(dvList)
+
+    print(" ")
+    print("% FFD_CONTROL_POINT (Z) (MULTIPLE INTERSECTIONS)")
+
+    iVariable = 0
+    dvList = "DEFINITION_DV= "
+    for kIndex in range(options.kOrder - 4):
+        for jIndex in range(options.jOrder - 4):
+            for iIndex in range(options.iOrder - 4):
+                iVariable = iVariable + 1
+                dvList = (
+                    dvList
+                    + "( 11, "
+                    + str(options.scale)
+                    + " | "
+                    + options.marker
+                    + " | "
+                )
+                dvList = (
+                    dvList
+                    + options.ffd_id
+                    + ", "
+                    + str(iIndex + 2)
+                    + ", "
+                    + str(jIndex + 2)
+                    + ", "
+                    + str(kIndex + 2)
+                    + ", 0.0, 0.0, 1.0 )"
+                )
+                if iVariable < (options.iOrder * (options.jOrder) * options.kOrder):
+                    dvList = dvList + "; "
+
+    print(dvList)
+
+    print(" ")
+    print("% FFD_CAMBER, FFD_TWIST, FFD_THICKNESS")
+
+    iVariable = 0
+    dvList = "DEFINITION_DV= "
     for jIndex in range(options.jOrder):
-      for iIndex in range(options.iOrder):
-        iVariable = iVariable + 1
-        dvList = dvList + "( 11, " + str(options.scale) + " | " + options.marker + " | "
-        dvList = dvList + options.ffd_id + ", " + str(iIndex) + ", " + str(jIndex) + ", " + str(kIndex) + ", 1.0, 0.0, 0.0 )"
-        if iVariable < (options.iOrder*(options.jOrder)*options.kOrder):
-          dvList = dvList + "; "
-
-
-  print(dvList)
-
-  print(" ")
-  print("% FFD_CONTROL_POINT (Y)")
-
-  iVariable = 0
-  dvList = "DEFINITION_DV= "
-  for kIndex in range(options.kOrder):
+        for iIndex in range(options.iOrder):
+            iVariable = iVariable + 1
+            dvList = (
+                dvList + "( 14, " + str(options.scale) + " | " + options.marker + " | "
+            )
+            dvList = (
+                dvList + options.ffd_id + ", " + str(iIndex) + ", " + str(jIndex) + " )"
+            )
+            dvList = dvList + "; "
+    iVariable = 0
     for jIndex in range(options.jOrder):
-      for iIndex in range(options.iOrder):
         iVariable = iVariable + 1
-        dvList = dvList + "( 11, " + str(options.scale) + " | " + options.marker + " | "
-        dvList = dvList + options.ffd_id + ", " + str(iIndex) + ", " + str(jIndex) + ", " + str(kIndex) + ", 0.0, 1.0, 0.0 )"
-        if iVariable < (options.iOrder*(options.jOrder)*options.kOrder):
-          dvList = dvList + "; "
-
-
-  print(dvList)
-
-  print(" ")
-  print("% FFD_CONTROL_POINT (Z)")
-
-  iVariable = 0
-  dvList = "DEFINITION_DV= "
-  for kIndex in range(options.kOrder):
+        dvList = dvList + "( 15, " + str(options.scale) + " | " + options.marker + " | "
+        dvList = (
+            dvList + options.ffd_id + ", " + str(jIndex) + ", " + options.axis + " )"
+        )
+        if iVariable < (options.jOrder):
+            dvList = dvList + "; "
+    iVariable = 0
     for jIndex in range(options.jOrder):
-      for iIndex in range(options.iOrder):
-        iVariable = iVariable + 1
-        dvList = dvList + "( 11, " + str(options.scale) + " | " + options.marker + " | "
-        dvList = dvList + options.ffd_id + ", " + str(iIndex) + ", " + str(jIndex) + ", " + str(kIndex) + ", 0.0, 0.0, 1.0 )"
-        if iVariable < (options.iOrder*(options.jOrder)*options.kOrder):
-          dvList = dvList + "; "
-
-
-  print(dvList)
-
-  print(" ")
-  print("% FFD_NACELLE (RHO)")
-
-  iVariable = 0
-  dvList = "DEFINITION_DV= "
-  for kIndex in range(options.kOrder):
-    for jIndex in range(1+options.jOrder/2):
-      for iIndex in range(options.iOrder):
-        iVariable = iVariable + 1
-        dvList = dvList + "( 12, " + str(options.scale) + " | " + options.marker + " | "
-        dvList = dvList + options.ffd_id + ", " + str(iIndex) + ", " + str(jIndex) + ", " + str(kIndex) + ", 1.0, 0.0 )"
-        if iVariable < (options.iOrder*(1+options.jOrder/2)*options.kOrder):
-          dvList = dvList + "; "
-
-
-  print(dvList)
-
-  print(" ")
-  print("% FFD_NACELLE (PHI)")
-
-  iVariable = 0
-  dvList = "DEFINITION_DV= "
-  for kIndex in range(options.kOrder):
-    for jIndex in range(1+options.jOrder/2):
-      for iIndex in range(options.iOrder):
-        iVariable = iVariable + 1
-        dvList = dvList + "( 12, " + str(options.scale) + " | " + options.marker + " | "
-        dvList = dvList + options.ffd_id + ", " + str(iIndex) + ", " + str(jIndex) + ", " + str(kIndex) + ", 0.0, 1.0 )"
-        if iVariable < (options.iOrder*(1+options.jOrder/2)*options.kOrder):
-          dvList = dvList + "; "
-
-
-  print(dvList)
-
-  print(" ")
-  print("% FFD_CONTROL_POINT (Z) (MULTIPLE INTERSECTIONS)")
-
-  iVariable = 0
-  dvList = "DEFINITION_DV= "
-  for kIndex in range(options.kOrder-4):
-    for jIndex in range(options.jOrder-4):
-      for iIndex in range(options.iOrder-4):
-        iVariable = iVariable + 1
-        dvList = dvList + "( 11, " + str(options.scale) + " | " + options.marker + " | "
-        dvList = dvList + options.ffd_id + ", " + str(iIndex+2) + ", " + str(jIndex+2) + ", " + str(kIndex+2) + ", 0.0, 0.0, 1.0 )"
-        if iVariable < (options.iOrder*(options.jOrder)*options.kOrder):
-          dvList = dvList + "; "
-
-
-  print(dvList)
-
-  print(" ")
-  print("% FFD_CAMBER, FFD_TWIST, FFD_THICKNESS")
-
-  iVariable = 0
-  dvList = "DEFINITION_DV= "
-  for jIndex in range(options.jOrder):
-    for iIndex in range(options.iOrder):
-      iVariable = iVariable + 1
-      dvList = dvList + "( 14, " + str(options.scale) + " | " + options.marker + " | "
-      dvList = dvList + options.ffd_id + ", " + str(iIndex) + ", " + str(jIndex) + " )"
-      dvList = dvList + "; "
-  iVariable = 0
-  for jIndex in range(options.jOrder):
-    iVariable = iVariable + 1
-    dvList = dvList + "( 15, " + str(options.scale) + " | " + options.marker + " | "
-    dvList = dvList + options.ffd_id + ", " + str(jIndex) + ", " + options.axis + " )"
-    if iVariable < (options.jOrder):
-      dvList = dvList + "; "
-  iVariable = 0
-  for jIndex in range(options.jOrder):
-    for iIndex in range(options.iOrder):
-      iVariable = iVariable + 1
-      dvList = dvList + "( 16, " + str(options.scale) + " | " + options.marker + " | "
-      dvList = dvList + options.ffd_id + ", " + str(iIndex) + ", " + str(jIndex) + " )"
-      dvList = dvList + "; "
-
-
-
-  print(dvList)
+        for iIndex in range(options.iOrder):
+            iVariable = iVariable + 1
+            dvList = (
+                dvList + "( 16, " + str(options.scale) + " | " + options.marker + " | "
+            )
+            dvList = (
+                dvList + options.ffd_id + ", " + str(iIndex) + ", " + str(jIndex) + " )"
+            )
+            dvList = dvList + "; "
+
+    print(dvList)
 
 if options.dim == 2:
 
-  print(" ")
-  print("% FFD_CONTROL_POINT_2D (X)")
+    print(" ")
+    print("% FFD_CONTROL_POINT_2D (X)")
 
-  iVariable = 0
-  dvList = "DEFINITION_DV= "
-  for jIndex in range(options.jOrder):
+    iVariable = 0
+    dvList = "DEFINITION_DV= "
+    for jIndex in range(options.jOrder):
+        for iIndex in range(options.iOrder):
+            iVariable = iVariable + 1
+            dvList = (
+                dvList + "( 19, " + str(options.scale) + " | " + options.marker + " | "
+            )
+            dvList = (
+                dvList
+                + options.ffd_id
+                + ", "
+                + str(iIndex)
+                + ", "
+                + str(jIndex)
+                + ", 1.0, 0.0 )"
+            )
+            if iVariable < (options.iOrder * options.jOrder):
+                dvList = dvList + "; "
+
+    print(dvList)
+
+    print(" ")
+    print("% FFD_CONTROL_POINT_2D (Y)")
+
+    iVariable = 0
+    dvList = "DEFINITION_DV= "
+    for jIndex in range(options.jOrder):
+        for iIndex in range(options.iOrder):
+            iVariable = iVariable + 1
+            dvList = (
+                dvList + "( 19, " + str(options.scale) + " | " + options.marker + " | "
+            )
+            dvList = (
+                dvList
+                + options.ffd_id
+                + ", "
+                + str(iIndex)
+                + ", "
+                + str(jIndex)
+                + ", 0.0, 1.0 )"
+            )
+            if iVariable < (options.iOrder * options.jOrder):
+                dvList = dvList + "; "
+
+    print(dvList)
+
+    print(" ")
+    print("FFD_CAMBER_2D & FFD_THICKNESS_2D")
+
+    iVariable = 0
+    dvList = "DEFINITION_DV= "
     for iIndex in range(options.iOrder):
-      iVariable = iVariable + 1
-      dvList = dvList + "( 19, " + str(options.scale) + " | " + options.marker + " | "
-      dvList = dvList + options.ffd_id + ", " + str(iIndex) + ", " + str(jIndex) + ", 1.0, 0.0 )"
-      if iVariable < (options.iOrder*options.jOrder):
+        iVariable = iVariable + 1
+        dvList = dvList + "( 20, " + str(options.scale) + " | " + options.marker + " | "
+        dvList = dvList + options.ffd_id + ", " + str(iIndex) + " )"
         dvList = dvList + "; "
-
-  print(dvList)
-
-  print(" ")
-  print("% FFD_CONTROL_POINT_2D (Y)")
-
-  iVariable = 0
-  dvList = "DEFINITION_DV= "
-  for jIndex in range(options.jOrder):
+    iVariable = 0
     for iIndex in range(options.iOrder):
-      iVariable = iVariable + 1
-      dvList = dvList + "( 19, " + str(options.scale) + " | " + options.marker + " | "
-      dvList = dvList + options.ffd_id + ", " + str(iIndex) + ", " + str(jIndex) + ", 0.0, 1.0 )"
-      if iVariable < (options.iOrder*options.jOrder):
-        dvList = dvList + "; "
+        iVariable = iVariable + 1
+        dvList = dvList + "( 21, " + str(options.scale) + " | " + options.marker + " | "
+        dvList = dvList + options.ffd_id + ", " + str(iIndex) + " )"
+        if iVariable < (options.iOrder):
+            dvList = dvList + "; "
 
-  print(dvList)
-
-  print(" ")
-  print("FFD_CAMBER_2D & FFD_THICKNESS_2D")
-
-  iVariable = 0
-  dvList = "DEFINITION_DV= "
-  for iIndex in range(options.iOrder):
-    iVariable = iVariable + 1
-    dvList = dvList + "( 20, " + str(options.scale) + " | " + options.marker + " | "
-    dvList = dvList + options.ffd_id + ", " + str(iIndex) + " )"
-    dvList = dvList + "; "
-  iVariable = 0
-  for iIndex in range(options.iOrder):
-    iVariable = iVariable + 1
-    dvList = dvList + "( 21, " + str(options.scale) + " | " + options.marker + " | "
-    dvList = dvList + options.ffd_id + ", " + str(iIndex) + " )"
-    if iVariable < (options.iOrder):
-      dvList = dvList + "; "
-
-  print(dvList)
+    print(dvList)
diff --git a/SU2_PY/shape_optimization.py b/SU2_PY/shape_optimization.py
index 34397c4e708..20cf15d4038 100755
--- a/SU2_PY/shape_optimization.py
+++ b/SU2_PY/shape_optimization.py
@@ -27,124 +27,247 @@
 
 import os, sys, shutil
 from optparse import OptionParser
-sys.path.append(os.environ['SU2_RUN'])
+
+sys.path.append(os.environ["SU2_RUN"])
 import SU2
 
 # -------------------------------------------------------------------
 #  Main
 # -------------------------------------------------------------------
 
+
 def main():
 
-    parser=OptionParser()
-    parser.add_option("-f", "--file", dest="filename",
-                      help="read config from FILE", metavar="FILE")
-    parser.add_option("-r", "--name", dest="projectname", default='',
-                      help="try to restart from project file NAME", metavar="NAME")
-    parser.add_option("-n", "--partitions", dest="partitions", default=1,
-                      help="number of PARTITIONS", metavar="PARTITIONS")
-    parser.add_option("-g", "--gradient", dest="gradient", default="DISCRETE_ADJOINT",
-                      help="Method for computing the GRADIENT (CONTINUOUS_ADJOINT, DISCRETE_ADJOINT, FINDIFF, NONE)", metavar="GRADIENT")
-    parser.add_option("-o", "--optimization", dest="optimization", default="SLSQP",
-                      help="OPTIMIZATION techique (SLSQP, CG, BFGS, POWELL)", metavar="OPTIMIZATION")
-    parser.add_option("-q", "--quiet", dest="quiet", default="True",
-                      help="True/False Quiet all SU2 output (optimizer output only)", metavar="QUIET")
-    parser.add_option("-z", "--zones", dest="nzones", default="1",
-                      help="Number of Zones", metavar="ZONES")
-
-
-    (options, args)=parser.parse_args()
+    parser = OptionParser()
+    parser.add_option(
+        "-f", "--file", dest="filename", help="read config from FILE", metavar="FILE"
+    )
+    parser.add_option(
+        "-r",
+        "--name",
+        dest="projectname",
+        default="",
+        help="try to restart from project file NAME",
+        metavar="NAME",
+    )
+    parser.add_option(
+        "-n",
+        "--partitions",
+        dest="partitions",
+        default=1,
+        help="number of PARTITIONS",
+        metavar="PARTITIONS",
+    )
+    parser.add_option(
+        "-g",
+        "--gradient",
+        dest="gradient",
+        default="DISCRETE_ADJOINT",
+        help="Method for computing the GRADIENT (CONTINUOUS_ADJOINT, DISCRETE_ADJOINT, FINDIFF, NONE)",
+        metavar="GRADIENT",
+    )
+    parser.add_option(
+        "-o",
+        "--optimization",
+        dest="optimization",
+        default="SLSQP",
+        help="OPTIMIZATION techique (SLSQP, CG, BFGS, POWELL)",
+        metavar="OPTIMIZATION",
+    )
+    parser.add_option(
+        "-q",
+        "--quiet",
+        dest="quiet",
+        default="True",
+        help="True/False Quiet all SU2 output (optimizer output only)",
+        metavar="QUIET",
+    )
+    parser.add_option(
+        "-z",
+        "--zones",
+        dest="nzones",
+        default="1",
+        help="Number of Zones",
+        metavar="ZONES",
+    )
+
+    (options, args) = parser.parse_args()
 
     # process inputs
-    options.partitions  = int( options.partitions )
-    options.quiet       = options.quiet.upper() == 'TRUE'
-    options.gradient    = options.gradient.upper()
-    options.nzones      = int( options.nzones )
-
-    sys.stdout.write('\n-------------------------------------------------------------------------\n')
-    sys.stdout.write('|    ___ _   _ ___                                                      |\n')
-    sys.stdout.write('|   / __| | | |_  )   Release 7.5.1 \"Blackbird\"                         |\n')
-    sys.stdout.write('|   \\__ \\ |_| |/ /                                                      |\n')
-    sys.stdout.write('|   |___/\\___//___|   Aerodynamic Shape Optimization Script             |\n')
-    sys.stdout.write('|                                                                       |\n')
-    sys.stdout.write('-------------------------------------------------------------------------\n')
-    sys.stdout.write('| SU2 Project Website: https://su2code.github.io                        |\n')
-    sys.stdout.write('|                                                                       |\n')
-    sys.stdout.write('| The SU2 Project is maintained by the SU2 Foundation                   |\n')
-    sys.stdout.write('| (http://su2foundation.org)                                            |\n')
-    sys.stdout.write('-------------------------------------------------------------------------\n')
-    sys.stdout.write('| Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)                |\n')
-    sys.stdout.write('|                                                                       |\n')
-    sys.stdout.write('| SU2 is free software; you can redistribute it and/or                  |\n')
-    sys.stdout.write('| modify it under the terms of the GNU Lesser General Public            |\n')
-    sys.stdout.write('| License as published by the Free Software Foundation; either          |\n')
-    sys.stdout.write('| version 2.1 of the License, or (at your option) any later version.    |\n')
-    sys.stdout.write('|                                                                       |\n')
-    sys.stdout.write('| SU2 is distributed in the hope that it will be useful,                |\n')
-    sys.stdout.write('| but WITHOUT ANY WARRANTY; without even the implied warranty of        |\n')
-    sys.stdout.write('| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |\n')
-    sys.stdout.write('| Lesser General Public License for more details.                       |\n')
-    sys.stdout.write('|                                                                       |\n')
-    sys.stdout.write('| You should have received a copy of the GNU Lesser General Public      |\n')
-    sys.stdout.write('| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |\n')
-    sys.stdout.write('-------------------------------------------------------------------------\n')
-
-    shape_optimization( options.filename    ,
-                        options.projectname ,
-                        options.partitions  ,
-                        options.gradient    ,
-                        options.optimization ,
-                        options.quiet       ,
-                        options.nzones      )
+    options.partitions = int(options.partitions)
+    options.quiet = options.quiet.upper() == "TRUE"
+    options.gradient = options.gradient.upper()
+    options.nzones = int(options.nzones)
+
+    sys.stdout.write(
+        "\n-------------------------------------------------------------------------\n"
+    )
+    sys.stdout.write(
+        "|    ___ _   _ ___                                                      |\n"
+    )
+    sys.stdout.write(
+        '|   / __| | | |_  )   Release 7.5.1 "Blackbird"                         |\n'
+    )
+    sys.stdout.write(
+        "|   \\__ \\ |_| |/ /                                                      |\n"
+    )
+    sys.stdout.write(
+        "|   |___/\\___//___|   Aerodynamic Shape Optimization Script             |\n"
+    )
+    sys.stdout.write(
+        "|                                                                       |\n"
+    )
+    sys.stdout.write(
+        "-------------------------------------------------------------------------\n"
+    )
+    sys.stdout.write(
+        "| SU2 Project Website: https://su2code.github.io                        |\n"
+    )
+    sys.stdout.write(
+        "|                                                                       |\n"
+    )
+    sys.stdout.write(
+        "| The SU2 Project is maintained by the SU2 Foundation                   |\n"
+    )
+    sys.stdout.write(
+        "| (http://su2foundation.org)                                            |\n"
+    )
+    sys.stdout.write(
+        "-------------------------------------------------------------------------\n"
+    )
+    sys.stdout.write(
+        "| Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)                |\n"
+    )
+    sys.stdout.write(
+        "|                                                                       |\n"
+    )
+    sys.stdout.write(
+        "| SU2 is free software; you can redistribute it and/or                  |\n"
+    )
+    sys.stdout.write(
+        "| modify it under the terms of the GNU Lesser General Public            |\n"
+    )
+    sys.stdout.write(
+        "| License as published by the Free Software Foundation; either          |\n"
+    )
+    sys.stdout.write(
+        "| version 2.1 of the License, or (at your option) any later version.    |\n"
+    )
+    sys.stdout.write(
+        "|                                                                       |\n"
+    )
+    sys.stdout.write(
+        "| SU2 is distributed in the hope that it will be useful,                |\n"
+    )
+    sys.stdout.write(
+        "| but WITHOUT ANY WARRANTY; without even the implied warranty of        |\n"
+    )
+    sys.stdout.write(
+        "| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |\n"
+    )
+    sys.stdout.write(
+        "| Lesser General Public License for more details.                       |\n"
+    )
+    sys.stdout.write(
+        "|                                                                       |\n"
+    )
+    sys.stdout.write(
+        "| You should have received a copy of the GNU Lesser General Public      |\n"
+    )
+    sys.stdout.write(
+        "| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |\n"
+    )
+    sys.stdout.write(
+        "-------------------------------------------------------------------------\n"
+    )
+
+    shape_optimization(
+        options.filename,
+        options.projectname,
+        options.partitions,
+        options.gradient,
+        options.optimization,
+        options.quiet,
+        options.nzones,
+    )
+
 
 #: main()
 
-def shape_optimization( filename                           ,
-                        projectname = ''                   ,
-                        partitions  = 0                    ,
-                        gradient    = 'CONTINUOUS_ADJOINT' ,
-                        optimization = 'SLSQP'             ,
-                        quiet       = False                ,
-                        nzones      = 1                    ):
+
+def shape_optimization(
+    filename,
+    projectname="",
+    partitions=0,
+    gradient="CONTINUOUS_ADJOINT",
+    optimization="SLSQP",
+    quiet=False,
+    nzones=1,
+):
     # Config
     config = SU2.io.Config(filename)
     config.NUMBER_PART = partitions
-    config.NZONES      = int( nzones )
-    if quiet: config.CONSOLE = 'CONCISE'
+    config.NZONES = int(nzones)
+    if quiet:
+        config.CONSOLE = "CONCISE"
     config.GRADIENT_METHOD = gradient
 
-    its               = int ( config.OPT_ITERATIONS )                      # number of opt iterations
-    bound_upper       = float ( config.OPT_BOUND_UPPER )                   # variable bound to be scaled by the line search
-    bound_lower       = float ( config.OPT_BOUND_LOWER )                   # variable bound to be scaled by the line search
-    relax_factor      = float ( config.OPT_RELAX_FACTOR )                  # line search scale
-    gradient_factor   = float ( config.OPT_GRADIENT_FACTOR )               # objective function and gradient scale
-    def_dv            = config.DEFINITION_DV                               # complete definition of the desing variable
-    n_dv              = sum(def_dv['SIZE'])                                # number of design variables
-    accu              = float ( config.OPT_ACCURACY ) * gradient_factor    # optimizer accuracy
-    x0                = [0.0]*n_dv # initial design
-    xb_low            = [float(bound_lower)/float(relax_factor)]*n_dv      # lower dv bound it includes the line search acceleration factor
-    xb_up             = [float(bound_upper)/float(relax_factor)]*n_dv      # upper dv bound it includes the line search acceleration fa
-    xb                = list(zip(xb_low, xb_up)) # design bounds
+    its = int(config.OPT_ITERATIONS)  # number of opt iterations
+    bound_upper = float(
+        config.OPT_BOUND_UPPER
+    )  # variable bound to be scaled by the line search
+    bound_lower = float(
+        config.OPT_BOUND_LOWER
+    )  # variable bound to be scaled by the line search
+    relax_factor = float(config.OPT_RELAX_FACTOR)  # line search scale
+    gradient_factor = float(
+        config.OPT_GRADIENT_FACTOR
+    )  # objective function and gradient scale
+    def_dv = config.DEFINITION_DV  # complete definition of the desing variable
+    n_dv = sum(def_dv["SIZE"])  # number of design variables
+    accu = float(config.OPT_ACCURACY) * gradient_factor  # optimizer accuracy
+    x0 = [0.0] * n_dv  # initial design
+    xb_low = [
+        float(bound_lower) / float(relax_factor)
+    ] * n_dv  # lower dv bound it includes the line search acceleration factor
+    xb_up = [
+        float(bound_upper) / float(relax_factor)
+    ] * n_dv  # upper dv bound it includes the line search acceleration fa
+    xb = list(zip(xb_low, xb_up))  # design bounds
 
     # State
     state = SU2.io.State()
     state.find_files(config)
 
     # add restart files to state.FILES
-    if config.get('TIME_DOMAIN', 'NO') == 'YES' and config.get('RESTART_SOL', 'NO') == 'YES' and gradient != 'CONTINUOUS_ADJOINT':
-        restart_name = config['RESTART_FILENAME'].split('.')[0]
-        restart_filename = restart_name + '_' + str(int(config['RESTART_ITER'])-1).zfill(5) + '.dat'
-        if not os.path.isfile(restart_filename): # throw, if restart files does not exist
+    if (
+        config.get("TIME_DOMAIN", "NO") == "YES"
+        and config.get("RESTART_SOL", "NO") == "YES"
+        and gradient != "CONTINUOUS_ADJOINT"
+    ):
+        restart_name = config["RESTART_FILENAME"].split(".")[0]
+        restart_filename = (
+            restart_name + "_" + str(int(config["RESTART_ITER"]) - 1).zfill(5) + ".dat"
+        )
+        if not os.path.isfile(
+            restart_filename
+        ):  # throw, if restart files does not exist
             sys.exit("Error: Restart file <" + restart_filename + "> not found.")
-        state['FILES']['RESTART_FILE_1'] = restart_filename
+        state["FILES"]["RESTART_FILE_1"] = restart_filename
 
         # use only, if time integration is second order
-        if config.get('TIME_MARCHING', 'NO') == 'DUAL_TIME_STEPPING-2ND_ORDER':
-            restart_filename = restart_name + '_' + str(int(config['RESTART_ITER'])-2).zfill(5) + '.dat'
-            if not os.path.isfile(restart_filename): # throw, if restart files does not exist
+        if config.get("TIME_MARCHING", "NO") == "DUAL_TIME_STEPPING-2ND_ORDER":
+            restart_filename = (
+                restart_name
+                + "_"
+                + str(int(config["RESTART_ITER"]) - 2).zfill(5)
+                + ".dat"
+            )
+            if not os.path.isfile(
+                restart_filename
+            ):  # throw, if restart files does not exist
                 sys.exit("Error: Restart file <" + restart_filename + "> not found.")
-            state['FILES']['RESTART_FILE_2'] =restart_filename
-
+            state["FILES"]["RESTART_FILE_2"] = restart_filename
 
     # Project
 
@@ -152,25 +275,25 @@ def shape_optimization( filename                           ,
         project = SU2.io.load_data(projectname)
         project.config = config
     else:
-        project = SU2.opt.Project(config,state)
+        project = SU2.opt.Project(config, state)
 
     # Optimize
-    if optimization == 'SLSQP':
-      SU2.opt.SLSQP(project,x0,xb,its,accu)
-    if optimization == 'CG':
-      SU2.opt.CG(project,x0,xb,its,accu)
-    if optimization == 'BFGS':
-      SU2.opt.BFGS(project,x0,xb,its,accu)
-    if optimization == 'POWELL':
-      SU2.opt.POWELL(project,x0,xb,its,accu)
-
+    if optimization == "SLSQP":
+        SU2.opt.SLSQP(project, x0, xb, its, accu)
+    if optimization == "CG":
+        SU2.opt.CG(project, x0, xb, its, accu)
+    if optimization == "BFGS":
+        SU2.opt.BFGS(project, x0, xb, its, accu)
+    if optimization == "POWELL":
+        SU2.opt.POWELL(project, x0, xb, its, accu)
 
     # rename project file
     if projectname:
-        shutil.move('project.pkl',projectname)
+        shutil.move("project.pkl", projectname)
 
     return project
 
+
 #: shape_optimization()
 
 
@@ -179,6 +302,5 @@ def shape_optimization( filename                           ,
 # -------------------------------------------------------------------
 
 # this is only accessed if running from command prompt
-if __name__ == '__main__':
+if __name__ == "__main__":
     main()
-
diff --git a/SU2_PY/topology_optimization.py b/SU2_PY/topology_optimization.py
index c8b211c93e6..45a8818d4ac 100755
--- a/SU2_PY/topology_optimization.py
+++ b/SU2_PY/topology_optimization.py
@@ -45,26 +45,26 @@
 
 ####### SETUP #######
 
-obj_scale = 1/1.25e-3 # scale the objective so that it starts at 1-4
-con_scale = 1/0.5     # 1 over upper bound (e.g. max volume)
-var_scale = 1.0       # variable scale
+obj_scale = 1 / 1.25e-3  # scale the objective so that it starts at 1-4
+con_scale = 1 / 0.5  # 1 over upper bound (e.g. max volume)
+var_scale = 1.0  # variable scale
 
 # maximum number of iterations
 maxJev_t = 1000
 # max iters for gray initialization, i.e. soft filter settings
 maxJev_i = 200
 # num iters between updates of the filter settings and constraint penalty factor
-nJev_u   = 40
+nJev_u = 40
 
 # tolerances
-ftol_u = 1e-5    # during updates
-ftol_f = 1e-7    # final iteration
+ftol_u = 1e-5  # during updates
+ftol_f = 1e-7  # final iteration
 # the exterior penalty method is used to impose the constraint,
 # this is the maximum constraint violation, below it the penalty factor is not increased
-htol   = 5e-3
+htol = 5e-3
 
 # general options for L-BFGS-B
-options={'disp': True, 'maxcor': 10, 'ftol': ftol_u, 'gtol': 1e-18}
+options = {"disp": True, "maxcor": 10, "ftol": ftol_u, "gtol": 1e-18}
 
 # these are the commands for the direct and adjoint runs, modify to run parallel
 commands = ["SU2_CFD ", "SU2_CFD_AD "]
@@ -85,344 +85,409 @@
 
 ####### SU2 Driver #######
 
+
 class Driver:
-  def __init__(self,commands,inputFile,configFiles,outputFiles):
-    self._inputFile  = inputFile
-    self._objValFile = "history.csv"
-    self._objDerFile = outputFiles[0]
-    self._conValFile = "history.csv"
-    self._conDerFile = outputFiles[1]
-    self._objValCommand = commands[0]+configFiles[0]+" > objval.stdout"
-    self._objDerCommand = commands[1]+configFiles[1]+" > objder.stdout"
-    self._conDerCommand = commands[1]+configFiles[2]+" > conval.stdout"
-  #end
-
-  def _assert_isfinite(self,val):
-    if math.isinf(val) or math.isnan(val):
-      raise ValueError
-  #end
-
-  def _write_input(self,x):
-    fid = open(self._inputFile,"w")
-    lines = ["\n"]
-    for val in x:
-      lines.append("0  0  0  0  0  "+str(val/var_scale)+"\n")
-    #end
-    fid.writelines(lines)
-    fid.close()
-  #end
-
-  def obj_val(self,x):
-    # write inputs
-    self._write_input(x)
-
-    # clear previous output and run direct solver
-    try:    os.remove(self._objValFile)
-    except: pass
-
-    try:
-      sp.call(self._objValCommand,shell=True)
-      with open(self._objValFile,"r") as fid:
-        lines = fid.readlines()
-      for col,name in enumerate(lines[0].split(",")):
-        if "TopComp" in name:
-          val = float(lines[1].split(",")[col])
-          break
-      # the return code of mpirun is useless, we test the value of the function
-      self._assert_isfinite(val)
-    except:
-      raise RuntimeError("Objective function evaluation failed")
-    #end
-
-    return val*obj_scale
-  #end
-
-  def obj_der(self,x):
-    # inputs written in obj_val_driver
-
-    # clear previous output and run direct solver
-    try:    os.remove(self._objDerFile)
-    except: pass
-    N = x.shape[0]
-    y = np.ndarray((N,))
-
-    try:
-      # main command
-      sp.call(self._objDerCommand,shell=True)
-
-      fid = open(self._objDerFile,"r"); lines = fid.readlines(); fid.close()
-      for i in range(N):
-        val = float(lines[i][0:-1])
-        self._assert_isfinite(val)
-        y[i] = val*obj_scale/var_scale
-      #end
-    except:
-      raise RuntimeError("Objective gradient evaluation failed")
-    #end
-
-    return y
-  #end
-
-  def con_val(self,x):
-    # inputs written in obj_val_driver
-
-    try:
-      with open(self._conValFile,"r") as fid:
-        lines = fid.readlines()
-      for col,name in enumerate(lines[0].split(",")):
-        if "VolFrac" in name:
-          val = float(lines[1].split(",")[col])
-          break
-      self._assert_isfinite(val)
-    except:
-      raise RuntimeError("Constraint function evaluation failed")
-    #end
-
-    return val*con_scale-1
-  #end
-
-  def con_der(self,x):
-    # inputs written in obj_val_driver
-
-    # clear previous output and run solver
-    try:    os.remove(self._conDerFile)
-    except: pass
-    N = x.shape[0]
-    y = np.ndarray((N,))
-
-    # read result
-    try:
-      sp.call(self._conDerCommand,shell=True)
-
-      fid = open(self._conDerFile,"r"); lines = fid.readlines(); fid.close()
-      for i in range(N):
-        val = float(lines[i][0:-1])
-        self._assert_isfinite(val)
-        y[i] = val*con_scale/var_scale
-      #end
-    except:
-      raise RuntimeError("Constraint function evaluation failed")
-    #end
-
-    return y
-  #end
-#end
+    def __init__(self, commands, inputFile, configFiles, outputFiles):
+        self._inputFile = inputFile
+        self._objValFile = "history.csv"
+        self._objDerFile = outputFiles[0]
+        self._conValFile = "history.csv"
+        self._conDerFile = outputFiles[1]
+        self._objValCommand = commands[0] + configFiles[0] + " > objval.stdout"
+        self._objDerCommand = commands[1] + configFiles[1] + " > objder.stdout"
+        self._conDerCommand = commands[1] + configFiles[2] + " > conval.stdout"
+
+    # end
+
+    def _assert_isfinite(self, val):
+        if math.isinf(val) or math.isnan(val):
+            raise ValueError
+
+    # end
+
+    def _write_input(self, x):
+        fid = open(self._inputFile, "w")
+        lines = ["\n"]
+        for val in x:
+            lines.append("0  0  0  0  0  " + str(val / var_scale) + "\n")
+        # end
+        fid.writelines(lines)
+        fid.close()
+
+    # end
+
+    def obj_val(self, x):
+        # write inputs
+        self._write_input(x)
+
+        # clear previous output and run direct solver
+        try:
+            os.remove(self._objValFile)
+        except:
+            pass
+
+        try:
+            sp.call(self._objValCommand, shell=True)
+            with open(self._objValFile, "r") as fid:
+                lines = fid.readlines()
+            for col, name in enumerate(lines[0].split(",")):
+                if "TopComp" in name:
+                    val = float(lines[1].split(",")[col])
+                    break
+            # the return code of mpirun is useless, we test the value of the function
+            self._assert_isfinite(val)
+        except:
+            raise RuntimeError("Objective function evaluation failed")
+        # end
+
+        return val * obj_scale
+
+    # end
+
+    def obj_der(self, x):
+        # inputs written in obj_val_driver
+
+        # clear previous output and run direct solver
+        try:
+            os.remove(self._objDerFile)
+        except:
+            pass
+        N = x.shape[0]
+        y = np.ndarray((N,))
+
+        try:
+            # main command
+            sp.call(self._objDerCommand, shell=True)
+
+            fid = open(self._objDerFile, "r")
+            lines = fid.readlines()
+            fid.close()
+            for i in range(N):
+                val = float(lines[i][0:-1])
+                self._assert_isfinite(val)
+                y[i] = val * obj_scale / var_scale
+            # end
+        except:
+            raise RuntimeError("Objective gradient evaluation failed")
+        # end
+
+        return y
+
+    # end
+
+    def con_val(self, x):
+        # inputs written in obj_val_driver
+
+        try:
+            with open(self._conValFile, "r") as fid:
+                lines = fid.readlines()
+            for col, name in enumerate(lines[0].split(",")):
+                if "VolFrac" in name:
+                    val = float(lines[1].split(",")[col])
+                    break
+            self._assert_isfinite(val)
+        except:
+            raise RuntimeError("Constraint function evaluation failed")
+        # end
+
+        return val * con_scale - 1
+
+    # end
+
+    def con_der(self, x):
+        # inputs written in obj_val_driver
+
+        # clear previous output and run solver
+        try:
+            os.remove(self._conDerFile)
+        except:
+            pass
+        N = x.shape[0]
+        y = np.ndarray((N,))
+
+        # read result
+        try:
+            sp.call(self._conDerCommand, shell=True)
+
+            fid = open(self._conDerFile, "r")
+            lines = fid.readlines()
+            fid.close()
+            for i in range(N):
+                val = float(lines[i][0:-1])
+                self._assert_isfinite(val)
+                y[i] = val * con_scale / var_scale
+            # end
+        except:
+            raise RuntimeError("Constraint function evaluation failed")
+        # end
+
+        return y
+
+    # end
+
+
+# end
 
 
 ####### Helpers #######
 
 # updates the parameters in the config files
-def update_settings(fnames,params):
-  for fname in fnames:
-    fid = open(fname,"r"); lines = fid.readlines(); fid.close()
+def update_settings(fnames, params):
+    for fname in fnames:
+        fid = open(fname, "r")
+        lines = fid.readlines()
+        fid.close()
 
-    for param in params:
-      for i in range(len(lines)):
-        if lines[i].startswith(param.name()):
-          lines[i] = param.name()+"= "+repr(param.value())+"\n"
-          break
-        #end
-      #end
-    #end
+        for param in params:
+            for i in range(len(lines)):
+                if lines[i].startswith(param.name()):
+                    lines[i] = param.name() + "= " + repr(param.value()) + "\n"
+                    break
+                # end
+            # end
+        # end
 
-    fid = open(fname,"w"); fid.writelines(lines); fid.close()
-  #end
-#end
+        fid = open(fname, "w")
+        fid.writelines(lines)
+        fid.close()
+    # end
+
+
+# end
 
 
 # use a list as a function
 class ValueList:
-  def __init__(self,values):
-    self._values = values
-    self._ub = len(values)-1
-  def val(self,idx):
-    return self._values[min(idx,self._ub)]
-#end
+    def __init__(self, values):
+        self._values = values
+        self._ub = len(values) - 1
+
+    def val(self, idx):
+        return self._values[min(idx, self._ub)]
+
+
+# end
 
 
 # helper class to hold parameters that are ramped
 class IncrParam:
-  def __init__(self,name,init,incr,maxi,func=None):
-    self._name = name
-    self._init = init
-    self._incr = incr
-    self._maxi = maxi
-    self._func = func
-    self._value = 0
-    self.reset()
-  #end
-
-  def name(self):
-    return self._name
-
-  def reset(self):
-    self._value = self._init
-
-  def update(self):
-    self._value = min(self._value+self._incr,self._maxi)
-
-  def finished(self):
-    return self._value == self._maxi
-
-  def value(self):
-    if self._func == None:
-      return self._value
-    else:
-      return self._func(self._value)
-    #end
-  #end
-#end
+    def __init__(self, name, init, incr, maxi, func=None):
+        self._name = name
+        self._init = init
+        self._incr = incr
+        self._maxi = maxi
+        self._func = func
+        self._value = 0
+        self.reset()
+
+    # end
+
+    def name(self):
+        return self._name
+
+    def reset(self):
+        self._value = self._init
+
+    def update(self):
+        self._value = min(self._value + self._incr, self._maxi)
+
+    def finished(self):
+        return self._value == self._maxi
+
+    def value(self):
+        if self._func == None:
+            return self._value
+        else:
+            return self._func(self._value)
+        # end
+
+    # end
+
+
+# end
 
 
 # Exterior penalty method wrapper
 class ExteriorPenaltyMethod:
-  def __init__(self,driver,r0=8,rmax=1024,c=2):
-    self._driver = driver
-    self._r  = r0
-    self._c  = c
-    self._rmax = rmax
-    self._fval = 0
-    self._hval = 0
-    # timers
-    self._funTime = 0
-    self._jacTime = 0
-  #end
-
-  def fun(self,x):
-    self._funTime -= time.time()
-    f = self._driver.obj_val(x)
-    h = self._driver.con_val(x)
-    self._funTime += time.time()
-    self._fval = f
-    self._hval = h
-    return f+self._r*max(0.0,h)*h
-  #end
-
-  def jac(self,x):
-    self._jacTime -= time.time()
-    df = self._driver.obj_der(x)
-    dh = self._driver.con_der(x)
-    self._jacTime += time.time()
-
-    # log current values of f and h
-    hisfile.write(repr(self._fval)+"  "+repr(self._hval)+"\n")
-    hisfile.flush()
-
-    return df+2*self._r*max(0.0,self._hval)*dh
-  #end
-
-  def update(self):
-    self._r = min(self._r*self._c,self._rmax)
-  #end
-#end
+    def __init__(self, driver, r0=8, rmax=1024, c=2):
+        self._driver = driver
+        self._r = r0
+        self._c = c
+        self._rmax = rmax
+        self._fval = 0
+        self._hval = 0
+        # timers
+        self._funTime = 0
+        self._jacTime = 0
+
+    # end
+
+    def fun(self, x):
+        self._funTime -= time.time()
+        f = self._driver.obj_val(x)
+        h = self._driver.con_val(x)
+        self._funTime += time.time()
+        self._fval = f
+        self._hval = h
+        return f + self._r * max(0.0, h) * h
+
+    # end
+
+    def jac(self, x):
+        self._jacTime -= time.time()
+        df = self._driver.obj_der(x)
+        dh = self._driver.con_der(x)
+        self._jacTime += time.time()
+
+        # log current values of f and h
+        hisfile.write(repr(self._fval) + "  " + repr(self._hval) + "\n")
+        hisfile.flush()
+
+        return df + 2 * self._r * max(0.0, self._hval) * dh
+
+    # end
+
+    def update(self):
+        self._r = min(self._r * self._c, self._rmax)
+
+    # end
+
+
+# end
 
 
 ####### RUN OPTIMIZATION #######
 
 paramValues = ValueList(filterParam)
-params = [IncrParam("TOPOL_OPTIM_KERNEL_PARAM",0,1,len(filterParam)-1,paramValues.val)]
+params = [
+    IncrParam("TOPOL_OPTIM_KERNEL_PARAM", 0, 1, len(filterParam) - 1, paramValues.val)
+]
 
-obj = ExteriorPenaltyMethod(Driver(commands,inputFile,fnames,outputFiles))
+obj = ExteriorPenaltyMethod(Driver(commands, inputFile, fnames, outputFiles))
 
-logfile = open("optimization.log","w")
-hisfile = open("optimization.his","w")
+logfile = open("optimization.log", "w")
+hisfile = open("optimization.his", "w")
 
 line = "### Optimization Started ###\n"
-print(line); logfile.write(line+"\n"); logfile.flush()
+print(line)
+logfile.write(line + "\n")
+logfile.flush()
 
 totTime = -time.time()
-nJacEval = 0; nFunEval = 0; itCount = 0;
+nJacEval = 0
+nFunEval = 0
+itCount = 0
 
 # initial values and bounds
-fid = open(inputFile,"r"); N = len(fid.readlines())-1; fid.close()
-x  = np.ones((N,))*var_scale/con_scale
+fid = open(inputFile, "r")
+N = len(fid.readlines()) - 1
+fid.close()
+x = np.ones((N,)) * var_scale / con_scale
 lb = np.zeros((N,))
-ub = np.ones((N,))*var_scale
-bounds = np.array((lb,ub),float).transpose()
+ub = np.ones((N,)) * var_scale
+bounds = np.array((lb, ub), float).transpose()
 
 ## 1st Phase: Run with "gray" filter settings ##
 # get the constraint and function within some tolerance
 line = "1: Gray filter (initialization)"
-print(line); logfile.write(line+"\n"); logfile.flush()
+print(line)
+logfile.write(line + "\n")
+logfile.flush()
 
-update_settings(fnames,params)
+update_settings(fnames, params)
 success = False
 
 while nJacEval < maxJev_i:
-  options["maxiter"] = min(nJev_u,maxJev_i-nJacEval)
-
-  optimum = scipy.optimize.minimize(obj.fun, x, method="L-BFGS-B", jac=obj.jac,
-                                    bounds=bounds, options=options)
-  itCount += 1
-  x = optimum.x
-  nJacEval += optimum.nit
-  nFunEval += optimum.nfev
-
-  line = " Iter {:d}: f= {:f}  h= {:e}  r= {:f}  nfev= {:d}  njev= {:d}".\
-    format(itCount, obj._fval, obj._hval, obj._r, optimum.nfev, optimum.nit)
-  print(line); logfile.write(line+"\n"); logfile.flush()
-
-  if obj._hval > htol: # increase penalty
-    obj.update()
-  elif optimum.success: # check convergence
-    success = True
-    break
-  else: # continue until convergence or maxJev_i
-    pass
-  #end
-#end
+    options["maxiter"] = min(nJev_u, maxJev_i - nJacEval)
+
+    optimum = scipy.optimize.minimize(
+        obj.fun, x, method="L-BFGS-B", jac=obj.jac, bounds=bounds, options=options
+    )
+    itCount += 1
+    x = optimum.x
+    nJacEval += optimum.nit
+    nFunEval += optimum.nfev
+
+    line = " Iter {:d}: f= {:f}  h= {:e}  r= {:f}  nfev= {:d}  njev= {:d}".format(
+        itCount, obj._fval, obj._hval, obj._r, optimum.nfev, optimum.nit
+    )
+    print(line)
+    logfile.write(line + "\n")
+    logfile.flush()
+
+    if obj._hval > htol:  # increase penalty
+        obj.update()
+    elif optimum.success:  # check convergence
+        success = True
+        break
+    else:  # continue until convergence or maxJev_i
+        pass
+    # end
+# end
 tmp = inputFile.split(".")
-shutil.copy(inputFile,tmp[0]+"_gray."+tmp[1])
+shutil.copy(inputFile, tmp[0] + "_gray." + tmp[1])
 
-if not(success):
-  line = " Initialization did not converge to desired tolerances"
-  print(line); logfile.write(line+"\n"); logfile.flush()
-#end
+if not (success):
+    line = " Initialization did not converge to desired tolerances"
+    print(line)
+    logfile.write(line + "\n")
+    logfile.flush()
+# end
 
 ## 2nd Phase: Make filter more "black-white" ##
 line = "\n2: Black-White filter"
-print(line); logfile.write(line+"\n"); logfile.flush()
+print(line)
+logfile.write(line + "\n")
+logfile.flush()
 
 options["maxiter"] = nJev_u
 finalIter = False
 
-while nJacEval < maxJev_t and not(finalIter):
-  finalIter = True
-  for i in range(len(params)):
-    params[i].update()
-    finalIter &= params[i].finished()
-  #end
-  update_settings(fnames,params)
-  if obj._hval > htol: obj.update()
-
-  options["ftol"] = (ftol_u,ftol_f)[int(finalIter)]
-  options["maxiter"] = max(nJev_u,(maxJev_t-nJacEval)*int(finalIter))
-
-  optimum = scipy.optimize.minimize(obj.fun, x, method="L-BFGS-B", jac=obj.jac,
-                                    bounds=bounds, options=options)
-  itCount += 1
-  x = optimum.x
-  nJacEval += optimum.nit
-  nFunEval += optimum.nfev
-
-  line = " Iter {:d}: f= {:f}  h= {:e}  r= {:f}  nfev= {:d}  njev= {:d}".\
-    format(itCount, obj._fval, obj._hval, obj._r, optimum.nfev, optimum.nit)
-  print(line); logfile.write(line+"\n"); logfile.flush()
-#end
+while nJacEval < maxJev_t and not (finalIter):
+    finalIter = True
+    for i in range(len(params)):
+        params[i].update()
+        finalIter &= params[i].finished()
+    # end
+    update_settings(fnames, params)
+    if obj._hval > htol:
+        obj.update()
+
+    options["ftol"] = (ftol_u, ftol_f)[int(finalIter)]
+    options["maxiter"] = max(nJev_u, (maxJev_t - nJacEval) * int(finalIter))
+
+    optimum = scipy.optimize.minimize(
+        obj.fun, x, method="L-BFGS-B", jac=obj.jac, bounds=bounds, options=options
+    )
+    itCount += 1
+    x = optimum.x
+    nJacEval += optimum.nit
+    nFunEval += optimum.nfev
+
+    line = " Iter {:d}: f= {:f}  h= {:e}  r= {:f}  nfev= {:d}  njev= {:d}".format(
+        itCount, obj._fval, obj._hval, obj._r, optimum.nfev, optimum.nit
+    )
+    print(line)
+    logfile.write(line + "\n")
+    logfile.flush()
+# end
 tmp = inputFile.split(".")
-shutil.copy(inputFile,tmp[0]+"_bw."+tmp[1])
+shutil.copy(inputFile, tmp[0] + "_bw." + tmp[1])
 
 success = finalIter and obj._hval < htol and optimum.success
 totTime += time.time()
 
-line = "\n### Optimization Finished ###\n"+\
-       "Summary: "+("Failure\n","Success\n")[int(success)]+\
-       "  fval: {:f}  hval: {:e}\n".format(obj._fval,obj._hval)+\
-       "Details:\n"+\
-       "  iter: {:d}  ttot: {:f}s\n".format(itCount,totTime)+\
-       "  nfev: {:d}  tfev: {:f}s\n".format(nFunEval,obj._funTime)+\
-       "  njev: {:d}  tjev: {:f}s\n".format(nJacEval,obj._jacTime)
-print(line); logfile.write(line+"\n")
+line = (
+    "\n### Optimization Finished ###\n"
+    + "Summary: "
+    + ("Failure\n", "Success\n")[int(success)]
+    + "  fval: {:f}  hval: {:e}\n".format(obj._fval, obj._hval)
+    + "Details:\n"
+    + "  iter: {:d}  ttot: {:f}s\n".format(itCount, totTime)
+    + "  nfev: {:d}  tfev: {:f}s\n".format(nFunEval, obj._funTime)
+    + "  njev: {:d}  tjev: {:f}s\n".format(nJacEval, obj._jacTime)
+)
+print(line)
+logfile.write(line + "\n")
 logfile.close()
 hisfile.close()
-
diff --git a/SU2_PY/updateHistoryMap.py b/SU2_PY/updateHistoryMap.py
index 8f4dca9972e..d391dfa9d83 100644
--- a/SU2_PY/updateHistoryMap.py
+++ b/SU2_PY/updateHistoryMap.py
@@ -26,79 +26,82 @@
 # License along with SU2. If not, see <http://www.gnu.org/licenses/>.
 import os, pprint
 
-su2_home = os.environ['SU2_HOME']
+su2_home = os.environ["SU2_HOME"]
 
-fileList = ['CFlowOutput.cpp',
-'CFlowIncOutput.cpp',
-'CFlowCompOutput.cpp',
-'CHeatOutput.cpp',
-'CFlowCompFEMOutput.cpp',
-'CElasticityOutput.cpp',
-'CAdjFlowOutput.cpp',
-'CAdjHeatOutput.cpp',
-'CAdjFlowIncOutput.cpp',
-'CAdjFlowCompOutput.cpp',
-'CAdjElasticityOutput.cpp']
+fileList = [
+    "CFlowOutput.cpp",
+    "CFlowIncOutput.cpp",
+    "CFlowCompOutput.cpp",
+    "CHeatOutput.cpp",
+    "CFlowCompFEMOutput.cpp",
+    "CElasticityOutput.cpp",
+    "CAdjFlowOutput.cpp",
+    "CAdjHeatOutput.cpp",
+    "CAdjFlowIncOutput.cpp",
+    "CAdjFlowCompOutput.cpp",
+    "CAdjElasticityOutput.cpp",
+]
+
+fileList = [os.path.join(su2_home, "SU2_CFD/src/output/" + i) for i in fileList]
 
-fileList = [os.path.join(su2_home, 'SU2_CFD/src/output/' + i) for i in fileList]
 
 def parse_output(files):
     outputFields = dict()
 
     for file in files:
-        print('Parsing ' + file)
-        f = open(file,'r')
-        while(1):
-            s = f.readline().strip(' ')
+        print("Parsing " + file)
+        f = open(file, "r")
+        while 1:
+            s = f.readline().strip(" ")
             if not s:
                 break
-            if s.startswith('AddHistoryOutput('):
-                s = s.replace('AddHistoryOutput', '').strip('()').split(',')
+            if s.startswith("AddHistoryOutput("):
+                s = s.replace("AddHistoryOutput", "").strip("()").split(",")
                 curOutputField = dict()
                 name = s[0].strip(' ()"\n;')
-                curOutputField['HEADER']  = s[1].strip(' ()"\n;')
-                curOutputField['GROUP']   = s[3].strip(' ()"\n;')
-                curOutputField['DESCRIPTION'] = s[4].strip(' ()"\n;')
+                curOutputField["HEADER"] = s[1].strip(' ()"\n;')
+                curOutputField["GROUP"] = s[3].strip(' ()"\n;')
+                curOutputField["DESCRIPTION"] = s[4].strip(' ()"\n;')
                 if len(s) == 6:
-                    curOutputField['TYPE'] = s[5].strip(' ()"\n;').split('::')[1]
+                    curOutputField["TYPE"] = s[5].strip(' ()"\n;').split("::")[1]
                 else:
-                    curOutputField['TYPE'] = 'DEFAULT'
+                    curOutputField["TYPE"] = "DEFAULT"
                 outputFields[name] = curOutputField
         f.close()
 
     addedOutputFields = dict()
 
     for field in outputFields:
-        if outputFields[field]['TYPE'] == 'COEFFICIENT':
+        if outputFields[field]["TYPE"] == "COEFFICIENT":
             curOutputField = dict()
-            name = 'D_' + field
-            curOutputField['HEADER'] = 'd[' + outputFields[field]['HEADER'] + ']'
-            curOutputField['GROUP'] = 'D_' + outputFields[field]['GROUP']
-            curOutputField['TYPE'] = 'D_COEFFICIENT'
-            curOutputField['DESCRIPTION'] = 'Derivative value'
+            name = "D_" + field
+            curOutputField["HEADER"] = "d[" + outputFields[field]["HEADER"] + "]"
+            curOutputField["GROUP"] = "D_" + outputFields[field]["GROUP"]
+            curOutputField["TYPE"] = "D_COEFFICIENT"
+            curOutputField["DESCRIPTION"] = "Derivative value"
             addedOutputFields[name] = curOutputField
 
-            name = 'TAVG_' + field
+            name = "TAVG_" + field
             curOutputField = dict()
-            curOutputField['HEADER'] = 'tavg[' + outputFields[field]['HEADER'] + ']'
-            curOutputField['GROUP'] = 'TAVG_' + outputFields[field]['GROUP']
-            curOutputField['TYPE'] = 'TAVG_COEFFICIENT'
-            curOutputField['DESCRIPTION'] = 'weighted time average value'
+            curOutputField["HEADER"] = "tavg[" + outputFields[field]["HEADER"] + "]"
+            curOutputField["GROUP"] = "TAVG_" + outputFields[field]["GROUP"]
+            curOutputField["TYPE"] = "TAVG_COEFFICIENT"
+            curOutputField["DESCRIPTION"] = "weighted time average value"
             addedOutputFields[name] = curOutputField
 
-            name = 'TAVG_D_' + field
+            name = "TAVG_D_" + field
             curOutputField = dict()
-            curOutputField['HEADER'] = 'dtavg[' + outputFields[field]['HEADER'] + ']'
-            curOutputField['GROUP'] = 'TAVG_D_' + outputFields[field]['GROUP']
-            curOutputField['TYPE'] = 'TAVG_D_COEFFICIENT'
-            curOutputField['DESCRIPTION'] = 'weighted time average derivative value'
+            curOutputField["HEADER"] = "dtavg[" + outputFields[field]["HEADER"] + "]"
+            curOutputField["GROUP"] = "TAVG_D_" + outputFields[field]["GROUP"]
+            curOutputField["TYPE"] = "TAVG_D_COEFFICIENT"
+            curOutputField["DESCRIPTION"] = "weighted time average derivative value"
             addedOutputFields[name] = curOutputField
 
-
     outputFields.update(addedOutputFields)
-    f = open(os.path.join(su2_home, 'SU2_PY/SU2/io/historyMap.py'), 'w')
-    f.write('history_header_map = ')
+    f = open(os.path.join(su2_home, "SU2_PY/SU2/io/historyMap.py"), "w")
+    f.write("history_header_map = ")
     pprint.pprint(outputFields, f)
     f.close()
 
+
 parse_output(fileList)
diff --git a/SU2_SOL/include/SU2_SOL.hpp b/SU2_SOL/include/SU2_SOL.hpp
index 8be627e7f17..47e9c842f15 100644
--- a/SU2_SOL/include/SU2_SOL.hpp
+++ b/SU2_SOL/include/SU2_SOL.hpp
@@ -26,7 +26,6 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #pragma once
 
 #include "../../Common/include/parallelization/mpi_structure.hpp"
@@ -37,7 +36,7 @@
 #include "../../Common/include/geometry/CPhysicalGeometry.hpp"
 #include "../../Common/include/CConfig.hpp"
 
-
-void WriteFiles(CConfig *config, CGeometry* geometry, CSolver** solver_container, COutput* output, unsigned long TimeIter);
+void WriteFiles(CConfig* config, CGeometry* geometry, CSolver** solver_container, COutput* output,
+                unsigned long TimeIter);
 
 using namespace std;
diff --git a/SU2_SOL/src/SU2_SOL.cpp b/SU2_SOL/src/SU2_SOL.cpp
index cf71364744e..feeeb4ca74a 100644
--- a/SU2_SOL/src/SU2_SOL.cpp
+++ b/SU2_SOL/src/SU2_SOL.cpp
@@ -25,13 +25,11 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
-
 #include "../include/SU2_SOL.hpp"
 
 using namespace std;
 
-int main(int argc, char *argv[]) {
-
+int main(int argc, char* argv[]) {
   unsigned short iZone, iInst;
   su2double StartTime = 0.0, StopTime = 0.0, UsedTime = 0.0;
 
@@ -39,7 +37,7 @@ int main(int argc, char *argv[]) {
 
   /*--- MPI initialization ---*/
 
-  SU2_MPI::Init(&argc,&argv);
+  SU2_MPI::Init(&argc, &argv);
   SU2_MPI::Comm MPICommunicator = SU2_MPI::GetComm();
 
   const int rank = SU2_MPI::GetRank();
@@ -47,32 +45,35 @@ int main(int argc, char *argv[]) {
 
   /*--- Pointer to different structures that will be used throughout the entire code ---*/
 
-  COutput **output                = nullptr;
-  CGeometry ***geometry_container = nullptr;
-  CSolver ***solver_container     = nullptr;
-  CConfig **config_container      = nullptr;
-  CConfig *driver_config          = nullptr;
-  unsigned short *nInst           = nullptr;
+  COutput** output = nullptr;
+  CGeometry*** geometry_container = nullptr;
+  CSolver*** solver_container = nullptr;
+  CConfig** config_container = nullptr;
+  CConfig* driver_config = nullptr;
+  unsigned short* nInst = nullptr;
 
   /*--- Load in the number of zones and spatial dimensions in the mesh file (if no config
    file is specified, default.cfg is used) ---*/
 
-  if (argc == 2 || argc == 3) { strcpy(config_file_name,argv[1]); }
-  else { strcpy(config_file_name, "default.cfg"); }
+  if (argc == 2 || argc == 3) {
+    strcpy(config_file_name, argv[1]);
+  } else {
+    strcpy(config_file_name, "default.cfg");
+  }
 
-  CConfig *config = nullptr;
+  CConfig* config = nullptr;
   config = new CConfig(config_file_name, SU2_COMPONENT::SU2_SOL);
 
   const auto nZone = config->GetnZone();
 
   /*--- Definition of the containers per zones ---*/
 
-  solver_container = new CSolver**[nZone] ();
-  config_container = new CConfig*[nZone] ();
-  geometry_container = new CGeometry**[nZone] ();
+  solver_container = new CSolver**[nZone]();
+  config_container = new CConfig*[nZone]();
+  geometry_container = new CGeometry**[nZone]();
   nInst = new unsigned short[nZone];
   driver_config = nullptr;
-  output = new COutput*[nZone] ();
+  output = new COutput*[nZone]();
 
   for (iZone = 0; iZone < nZone; iZone++) {
     nInst[iZone] = 1;
@@ -92,21 +93,19 @@ int main(int argc, char *argv[]) {
    differential equation on a single block, unstructured mesh. ---*/
 
   for (iZone = 0; iZone < nZone; iZone++) {
-
     /*--- Definition of the configuration option class for all zones. In this
      constructor, the input configuration file is parsed and all options are
      read and stored. ---*/
 
-    if (driver_config->GetnConfigFiles() > 0){
+    if (driver_config->GetnConfigFiles() > 0) {
       strcpy(zone_file_name, driver_config->GetConfigFilename(iZone).c_str());
       config_container[iZone] = new CConfig(driver_config, zone_file_name, SU2_COMPONENT::SU2_SOL, iZone, nZone, true);
-    }
-    else{
-      config_container[iZone] = new CConfig(driver_config, config_file_name, SU2_COMPONENT::SU2_SOL, iZone, nZone, true);
+    } else {
+      config_container[iZone] =
+          new CConfig(driver_config, config_file_name, SU2_COMPONENT::SU2_SOL, iZone, nZone, true);
     }
 
     config_container[iZone]->SetMPICommunicator(MPICommunicator);
-
   }
 
   /*--- Set the multizone part of the problem. ---*/
@@ -119,7 +118,6 @@ int main(int argc, char *argv[]) {
 
   /*--- Read the geometry for each zone ---*/
   for (iZone = 0; iZone < nZone; iZone++) {
-
     /*--- Determine whether or not the FEM solver is used, which decides the
      type of geometry classes that are instantiated. ---*/
     const bool fem_solver = config_container[iZone]->GetFEMSolver();
@@ -131,8 +129,7 @@ int main(int argc, char *argv[]) {
     geometry_container[iZone] = new CGeometry*[nInst[iZone]];
     solver_container[iZone] = new CSolver*[nInst[iZone]];
 
-    for (iInst = 0; iInst < nInst[iZone]; iInst++){
-
+    for (iInst = 0; iInst < nInst[iZone]; iInst++) {
       /*--- Allocate solver. ---*/
       solver_container[iZone][iInst] = nullptr;
 
@@ -140,7 +137,7 @@ int main(int argc, char *argv[]) {
 
       /*--- Definition of the geometry class to store the primal grid in the partitioning process. ---*/
 
-      CGeometry *geometry_aux = nullptr;
+      CGeometry* geometry_aux = nullptr;
 
       /*--- All ranks process the grid and call ParMETIS for partitioning ---*/
 
@@ -148,8 +145,10 @@ int main(int argc, char *argv[]) {
 
       /*--- Color the initial grid and set the send-receive domains (ParMETIS) ---*/
 
-      if ( fem_solver ) geometry_aux->SetColorFEMGrid_Parallel(config_container[iZone]);
-      else              geometry_aux->SetColorGrid_Parallel(config_container[iZone]);
+      if (fem_solver)
+        geometry_aux->SetColorFEMGrid_Parallel(config_container[iZone]);
+      else
+        geometry_aux->SetColorGrid_Parallel(config_container[iZone]);
 
       /*--- Allocate the memory of the current domain, and divide the grid between the nodes ---*/
 
@@ -157,15 +156,14 @@ int main(int argc, char *argv[]) {
 
       /*--- Build the grid data structures using the ParMETIS coloring. ---*/
 
-      if( fem_solver ) {
-        switch( config_container[iZone]->GetKind_FEM_Flow() ) {
+      if (fem_solver) {
+        switch (config_container[iZone]->GetKind_FEM_Flow()) {
           case DG: {
             geometry_container[iZone][iInst] = new CMeshFEM_DG(geometry_aux, config_container[iZone]);
             break;
           }
         }
-      }
-      else {
+      } else {
         geometry_container[iZone][iInst] = new CPhysicalGeometry(geometry_aux, config_container[iZone]);
       }
 
@@ -183,7 +181,7 @@ int main(int argc, char *argv[]) {
 
       /*--- Create the vertex structure (required for MPI) ---*/
 
-      if (rank == MASTER_NODE) cout << "Identify vertices." <<endl;
+      if (rank == MASTER_NODE) cout << "Identify vertices." << endl;
       geometry_container[iZone][iInst]->SetVertex(config_container[iZone]);
 
       /*--- Store the global to local mapping after preprocessing. ---*/
@@ -193,15 +191,15 @@ int main(int argc, char *argv[]) {
 
       /*--- Create the point-to-point MPI communication structures for the fvm solver. ---*/
 
-      if (!fem_solver) geometry_container[iZone][iInst]->PreprocessP2PComms(geometry_container[iZone][iInst], config_container[iZone]);
+      if (!fem_solver)
+        geometry_container[iZone][iInst]->PreprocessP2PComms(geometry_container[iZone][iInst], config_container[iZone]);
 
       /* Test for a fem solver, because some more work must be done. */
 
       if (fem_solver) {
-
         /*--- Carry out a dynamic cast to CMeshFEM_DG, such that it is not needed to
          define all virtual functions in the base class CGeometry. ---*/
-        CMeshFEM_DG *DGMesh = dynamic_cast<CMeshFEM_DG *>(geometry_container[iZone][iInst]);
+        CMeshFEM_DG* DGMesh = dynamic_cast<CMeshFEM_DG*>(geometry_container[iZone][iInst]);
 
         /*--- Determine the standard elements for the volume elements. ---*/
         if (rank == MASTER_NODE) cout << "Creating standard volume elements." << endl;
@@ -213,7 +211,6 @@ int main(int argc, char *argv[]) {
         DGMesh->CreateFaces(config_container[iZone]);
       }
     }
-
   }
 
   const bool fsi = config_container[ZONE_0]->GetFSI_Simulation();
@@ -224,17 +221,15 @@ int main(int argc, char *argv[]) {
   StartTime = SU2_MPI::Wtime();
 
   if (rank == MASTER_NODE)
-    cout << endl <<"------------------------- Solution Postprocessing -----------------------" << endl;
+    cout << endl << "------------------------- Solution Postprocessing -----------------------" << endl;
 
   /*---  Check whether this is an FSI, fluid unsteady, harmonic balance or structural dynamic simulation and call the
    solution merging routines accordingly.---*/
 
   if (multizone) {
-
     bool TimeDomain = driver_config->GetTime_Domain();
 
-    if (TimeDomain){
-
+    if (TimeDomain) {
       su2double Physical_dt, Physical_t;
       unsigned long TimeIter = 0;
       bool StopCalc = false;
@@ -243,83 +238,81 @@ int main(int argc, char *argv[]) {
       Physical_dt = driver_config->GetTime_Step();
 
       /*--- Check for an unsteady restart. Update TimeIter if necessary. ---*/
-      if (driver_config->GetRestart()){
+      if (driver_config->GetRestart()) {
         TimeIter = driver_config->GetRestart_Iter();
       }
 
       /*--- Instantiate the solvers for each zone. ---*/
-      for (iZone = 0; iZone < nZone; iZone++){
+      for (iZone = 0; iZone < nZone; iZone++) {
         config_container[iZone]->SetiInst(INST_0);
         config_container[iZone]->SetTimeIter(TimeIter);
-        solver_container[iZone][INST_0] = new CBaselineSolver(geometry_container[iZone][INST_0], config_container[iZone]);
+        solver_container[iZone][INST_0] =
+            new CBaselineSolver(geometry_container[iZone][INST_0], config_container[iZone]);
 
-        output[iZone] = new CBaselineOutput(config_container[iZone], geometry_container[iZone][INST_0]->GetnDim(), solver_container[iZone][INST_0]);
+        output[iZone] = new CBaselineOutput(config_container[iZone], geometry_container[iZone][INST_0]->GetnDim(),
+                                            solver_container[iZone][INST_0]);
         output[iZone]->PreprocessVolumeOutput(config_container[iZone]);
         output[iZone]->PreprocessHistoryOutput(config_container[iZone], false);
-
       }
 
       /*--- Loop over the whole time domain ---*/
       while (TimeIter < driver_config->GetnTime_Iter()) {
-
         /*--- Check if the maximum time has been surpassed. ---*/
-        Physical_t  = (TimeIter+1)*Physical_dt;
-        if (Physical_t >=  driver_config->GetMax_Time())
-          StopCalc = true;
-
-        if ((TimeIter+1 == driver_config->GetnTime_Iter()) || // The last time iteration
-            (StopCalc) || // We have surpassed the requested time
-            ((TimeIter == 0) || (TimeIter % config_container[ZONE_0]->GetVolumeOutputFrequency(0) == 0)) // The iteration has been requested
-          ){
-          if (rank == MASTER_NODE) cout << "Writing the volume solution for time step " << TimeIter << ", t = " << Physical_t << " s ." << endl;
+        Physical_t = (TimeIter + 1) * Physical_dt;
+        if (Physical_t >= driver_config->GetMax_Time()) StopCalc = true;
+
+        if ((TimeIter + 1 == driver_config->GetnTime_Iter()) ||  // The last time iteration
+            (StopCalc) ||                                        // We have surpassed the requested time
+            ((TimeIter == 0) || (TimeIter % config_container[ZONE_0]->GetVolumeOutputFrequency(0) ==
+                                 0))  // The iteration has been requested
+        ) {
+          if (rank == MASTER_NODE)
+            cout << "Writing the volume solution for time step " << TimeIter << ", t = " << Physical_t << " s ."
+                 << endl;
 
           /*--- Load the restart for all the zones. ---*/
-          for (iZone = 0; iZone < nZone; iZone++){
-
+          for (iZone = 0; iZone < nZone; iZone++) {
             /*--- Set the current iteration number in the config class. ---*/
             config_container[iZone]->SetTimeIter(TimeIter);
             /*--- So far, only enabled for single-instance problems ---*/
             config_container[iZone]->SetiInst(INST_0);
-            solver_container[iZone][INST_0]->LoadRestart(geometry_container[iZone], &solver_container[iZone], config_container[iZone], TimeIter, true);
+            solver_container[iZone][INST_0]->LoadRestart(geometry_container[iZone], &solver_container[iZone],
+                                                         config_container[iZone], TimeIter, true);
           }
 
-
-          for (iZone = 0; iZone < nZone; iZone++){
-
-            WriteFiles(config_container[iZone], geometry_container[iZone][INST_0], &solver_container[iZone][INST_0], output[iZone], TimeIter);
-
+          for (iZone = 0; iZone < nZone; iZone++) {
+            WriteFiles(config_container[iZone], geometry_container[iZone][INST_0], &solver_container[iZone][INST_0],
+                       output[iZone], TimeIter);
           }
         }
 
         TimeIter++;
         if (StopCalc) break;
       }
-    }
-    else {
-
+    } else {
       /*--- Steady simulation: merge the solution files for each zone. ---*/
       for (iZone = 0; iZone < nZone; iZone++) {
         config_container[iZone]->SetiInst(INST_0);
         /*--- Definition of the solution class ---*/
-        solver_container[iZone][INST_0] = new CBaselineSolver(geometry_container[iZone][INST_0], config_container[iZone]);
-        solver_container[iZone][INST_0]->LoadRestart(geometry_container[iZone], &solver_container[iZone], config_container[iZone], 0, true);
-        output[iZone] = new CBaselineOutput(config_container[iZone], geometry_container[iZone][INST_0]->GetnDim(), solver_container[iZone][INST_0]);
+        solver_container[iZone][INST_0] =
+            new CBaselineSolver(geometry_container[iZone][INST_0], config_container[iZone]);
+        solver_container[iZone][INST_0]->LoadRestart(geometry_container[iZone], &solver_container[iZone],
+                                                     config_container[iZone], 0, true);
+        output[iZone] = new CBaselineOutput(config_container[iZone], geometry_container[iZone][INST_0]->GetnDim(),
+                                            solver_container[iZone][INST_0]);
         output[iZone]->PreprocessVolumeOutput(config_container[iZone]);
         output[iZone]->PreprocessHistoryOutput(config_container[iZone], false);
-
       }
-      for (iZone = 0; iZone < nZone; iZone++){
-
-        WriteFiles(config_container[iZone], geometry_container[iZone][INST_0], &solver_container[iZone][INST_0], output[iZone], 0);
-
+      for (iZone = 0; iZone < nZone; iZone++) {
+        WriteFiles(config_container[iZone], geometry_container[iZone][INST_0], &solver_container[iZone][INST_0],
+                   output[iZone], 0);
       }
     }
 
-  }
-  else if (fsi){
-
-    if (nZone < 2){
-      SU2_MPI::Error("For multizone computations, please add the number of zones as a second argument for SU2_SOL.", CURRENT_FUNCTION);
+  } else if (fsi) {
+    if (nZone < 2) {
+      SU2_MPI::Error("For multizone computations, please add the number of zones as a second argument for SU2_SOL.",
+                     CURRENT_FUNCTION);
     }
 
     su2double Physical_dt, Physical_t;
@@ -328,29 +321,25 @@ int main(int argc, char *argv[]) {
     bool SolutionInstantiatedFlow = false, SolutionInstantiatedFEM = false;
 
     /*--- Check for an unsteady restart. Update ExtIter if necessary. ---*/
-    if (config_container[ZONE_0]->GetRestart()){
+    if (config_container[ZONE_0]->GetRestart()) {
       TimeIterFlow = config_container[ZONE_0]->GetRestart_Iter();
       TimeIterFEM = config_container[ZONE_1]->GetRestart_Iter();
       if (TimeIterFlow != TimeIterFEM) {
-        SU2_MPI::Error("For multizone computations, please add the number of zones as a second argument for SU2_SOL.", CURRENT_FUNCTION);
-      }
-      else {
+        SU2_MPI::Error("For multizone computations, please add the number of zones as a second argument for SU2_SOL.",
+                       CURRENT_FUNCTION);
+      } else {
         TimeIter = TimeIterFlow;
       }
     }
 
-
     while (TimeIter < config_container[ZONE_0]->GetnTime_Iter()) {
-
       /*--- Check several conditions in order to merge the correct time step files. ---*/
 
       Physical_dt = config_container[ZONE_0]->GetDelta_UnstTime();
-      Physical_t  = (TimeIter+1)*Physical_dt;
-      if (Physical_t >=  config_container[ZONE_0]->GetTotal_UnstTime())
-        StopCalc = true;
+      Physical_t = (TimeIter + 1) * Physical_dt;
+      if (Physical_t >= config_container[ZONE_0]->GetTotal_UnstTime()) StopCalc = true;
 
-      if (
-          ((TimeIter+1 == config_container[ZONE_0]->GetnTime_Iter()) ||
+      if (((TimeIter + 1 == config_container[ZONE_0]->GetnTime_Iter()) ||
            ((TimeIter % config_container[ZONE_0]->GetVolumeOutputFrequency(0) == 0) && (TimeIter != 0) &&
             !((config_container[ZONE_0]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
               (config_container[ZONE_0]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND))) ||
@@ -361,13 +350,11 @@ int main(int argc, char *argv[]) {
 
           &&
 
-          ((TimeIter+1 == config_container[ZONE_1]->GetnTime_Iter()) ||
-           (StopCalc) ||
+          ((TimeIter + 1 == config_container[ZONE_1]->GetnTime_Iter()) || (StopCalc) ||
            ((config_container[ZONE_1]->GetTime_Domain()) &&
             ((TimeIter == 0) || (TimeIter % config_container[ZONE_1]->GetVolumeOutputFrequency(0) == 0))))
 
-          ){
-
+      ) {
         /*--- Set the current iteration number in the config class. ---*/
         config_container[ZONE_0]->SetTimeIter(TimeIter);
         config_container[ZONE_1]->SetTimeIter(TimeIter);
@@ -377,38 +364,46 @@ int main(int argc, char *argv[]) {
         /*--- For the fluid zone (ZONE_0) ---*/
         /*--- Either instantiate the solution class or load a restart file. ---*/
         if (SolutionInstantiatedFlow == false &&
-            (TimeIter == 0 || ((config_container[ZONE_0]->GetRestart() && (SU2_TYPE::Int(TimeIter) == SU2_TYPE::Int(config_container[ZONE_0]->GetRestart_Iter()))) ||
-                               TimeIter % config_container[ZONE_0]->GetVolumeOutputFrequency(0) == 0 ||
-                               TimeIter+1 == config_container[ZONE_0]->GetnTime_Iter()))) {
-          solver_container[ZONE_0][INST_0] = new CBaselineSolver(geometry_container[ZONE_0][INST_0], config_container[ZONE_0]);
-          output[ZONE_0] = new CBaselineOutput(config_container[ZONE_0], geometry_container[ZONE_0][INST_0]->GetnDim(), solver_container[ZONE_0][INST_0]);
+            (TimeIter == 0 ||
+             ((config_container[ZONE_0]->GetRestart() &&
+               (SU2_TYPE::Int(TimeIter) == SU2_TYPE::Int(config_container[ZONE_0]->GetRestart_Iter()))) ||
+              TimeIter % config_container[ZONE_0]->GetVolumeOutputFrequency(0) == 0 ||
+              TimeIter + 1 == config_container[ZONE_0]->GetnTime_Iter()))) {
+          solver_container[ZONE_0][INST_0] =
+              new CBaselineSolver(geometry_container[ZONE_0][INST_0], config_container[ZONE_0]);
+          output[ZONE_0] = new CBaselineOutput(config_container[ZONE_0], geometry_container[ZONE_0][INST_0]->GetnDim(),
+                                               solver_container[ZONE_0][INST_0]);
           output[ZONE_0]->PreprocessVolumeOutput(config_container[ZONE_0]);
           output[ZONE_0]->PreprocessHistoryOutput(config_container[ZONE_0], false);
 
           SolutionInstantiatedFlow = true;
         }
-          solver_container[ZONE_0][INST_0]->LoadRestart_FSI(geometry_container[ZONE_0][INST_0], config_container[ZONE_0], TimeIter);
-
+        solver_container[ZONE_0][INST_0]->LoadRestart_FSI(geometry_container[ZONE_0][INST_0], config_container[ZONE_0],
+                                                          TimeIter);
 
         /*--- For the structural zone (ZONE_1) ---*/
         /*--- Either instantiate the solution class or load a restart file. ---*/
         /*--- Either instantiate the solution class or load a restart file. ---*/
         if (SolutionInstantiatedFEM == false &&
-            (TimeIter == 0 || ((config_container[ZONE_1]->GetRestart() && (SU2_TYPE::Int(TimeIter) == SU2_TYPE::Int(config_container[ZONE_1]->GetRestart_Iter()))) ||
-                               TimeIter % config_container[ZONE_1]->GetVolumeOutputFrequency(0) == 0 ||
-                               TimeIter+1 == config_container[ZONE_1]->GetnTime_Iter()))) {
-          solver_container[ZONE_1][INST_0] = new CBaselineSolver(geometry_container[ZONE_1][INST_0], config_container[ZONE_1]);
-          output[ZONE_1] = new CBaselineOutput(config_container[ZONE_1], geometry_container[ZONE_1][INST_0]->GetnDim(), solver_container[ZONE_1][INST_0]);
+            (TimeIter == 0 ||
+             ((config_container[ZONE_1]->GetRestart() &&
+               (SU2_TYPE::Int(TimeIter) == SU2_TYPE::Int(config_container[ZONE_1]->GetRestart_Iter()))) ||
+              TimeIter % config_container[ZONE_1]->GetVolumeOutputFrequency(0) == 0 ||
+              TimeIter + 1 == config_container[ZONE_1]->GetnTime_Iter()))) {
+          solver_container[ZONE_1][INST_0] =
+              new CBaselineSolver(geometry_container[ZONE_1][INST_0], config_container[ZONE_1]);
+          output[ZONE_1] = new CBaselineOutput(config_container[ZONE_1], geometry_container[ZONE_1][INST_0]->GetnDim(),
+                                               solver_container[ZONE_1][INST_0]);
           output[ZONE_1]->PreprocessVolumeOutput(config_container[ZONE_1]);
           SolutionInstantiatedFEM = true;
         }
-          solver_container[ZONE_1][INST_0]->LoadRestart_FSI(geometry_container[ZONE_1][INST_0], config_container[ZONE_1], TimeIter);
+        solver_container[ZONE_1][INST_0]->LoadRestart_FSI(geometry_container[ZONE_1][INST_0], config_container[ZONE_1],
+                                                          TimeIter);
 
         if (rank == MASTER_NODE) cout << "Writing the volume solution for time step " << TimeIter << "." << endl;
-        for (iZone = 0; iZone < nZone; iZone++){
-
-          WriteFiles(config_container[iZone], geometry_container[iZone][INST_0], &solver_container[iZone][INST_0], output[iZone], TimeIter);
-
+        for (iZone = 0; iZone < nZone; iZone++) {
+          WriteFiles(config_container[iZone], geometry_container[iZone][INST_0], &solver_container[iZone][INST_0],
+                     output[iZone], TimeIter);
         }
       }
 
@@ -417,70 +412,63 @@ int main(int argc, char *argv[]) {
     }
 
   } else if (fem_solver) {
-
     if (config->GetTime_Domain()) {
-
       /*--- Unsteady DG simulation: merge all unsteady time steps. First,
        find the frequency and total number of files to write. ---*/
 
       su2double Physical_dt, Physical_t;
       unsigned long TimeIter = 0;
       bool StopCalc = false;
-      bool *SolutionInstantiated = new bool[nZone];
+      bool* SolutionInstantiated = new bool[nZone];
 
-      for (iZone = 0; iZone < nZone; iZone++)
-        SolutionInstantiated[iZone] = false;
+      for (iZone = 0; iZone < nZone; iZone++) SolutionInstantiated[iZone] = false;
 
       /*--- Check for an unsteady restart. Update ExtIter if necessary. ---*/
       if (config_container[ZONE_0]->GetTime_Domain() && config_container[ZONE_0]->GetRestart())
         TimeIter = config_container[ZONE_0]->GetRestart_Iter();
 
       while (TimeIter < config_container[ZONE_0]->GetnTime_Iter()) {
-
         /*--- Check several conditions in order to merge the correct time step files. ---*/
         Physical_dt = config_container[ZONE_0]->GetDelta_UnstTime();
-        Physical_t  = (TimeIter+1)*Physical_dt;
-        if (Physical_t >=  config_container[ZONE_0]->GetTotal_UnstTime())
-          StopCalc = true;
+        Physical_t = (TimeIter + 1) * Physical_dt;
+        if (Physical_t >= config_container[ZONE_0]->GetTotal_UnstTime()) StopCalc = true;
 
-        if ((TimeIter+1 == config_container[ZONE_0]->GetnTime_Iter()) ||
+        if ((TimeIter + 1 == config_container[ZONE_0]->GetnTime_Iter()) ||
             ((TimeIter % config_container[ZONE_0]->GetVolumeOutputFrequency(0) == 0) && (TimeIter != 0) &&
              !(config_container[ZONE_0]->GetTime_Marching() == TIME_MARCHING::TIME_STEPPING)) ||
             (StopCalc) ||
             ((config_container[ZONE_0]->GetTime_Marching() == TIME_MARCHING::TIME_STEPPING) &&
              ((TimeIter == 0) || (TimeIter % config_container[ZONE_0]->GetVolumeOutputFrequency(0) == 0)))) {
+          /*--- Read in the restart file for this time step ---*/
+          for (iZone = 0; iZone < nZone; iZone++) {
+            /*--- Set the current iteration number in the config class. ---*/
+            config_container[iZone]->SetTimeIter(TimeIter);
 
-              /*--- Read in the restart file for this time step ---*/
-              for (iZone = 0; iZone < nZone; iZone++) {
-
-                /*--- Set the current iteration number in the config class. ---*/
-                config_container[iZone]->SetTimeIter(TimeIter);
-
-                /*--- Either instantiate the solution class or load a restart file. ---*/
-                if (SolutionInstantiated[iZone] == false &&
-                    (TimeIter == 0 ||
-                     (config_container[ZONE_0]->GetRestart() && ((long)TimeIter == SU2_TYPE::Int(config_container[ZONE_0]->GetRestart_Iter()) ||
-                                                                                  TimeIter % config_container[ZONE_0]->GetVolumeOutputFrequency(0) == 0 ||
-                                                                                  TimeIter+1 == config_container[ZONE_0]->GetnTime_Iter())))) {
-
-                  solver_container[iZone][INST_0] = new CBaselineSolver_FEM(geometry_container[iZone][INST_0], config_container[iZone]);
-                  output[iZone] = new CBaselineOutput(config_container[ZONE_0], geometry_container[ZONE_0][INST_0]->GetnDim(), solver_container[ZONE_0][INST_0]);
-                  output[iZone]->PreprocessVolumeOutput(config_container[ZONE_0]);
-                  output[iZone]->PreprocessHistoryOutput(config_container[ZONE_0], false);
-                  SolutionInstantiated[iZone] = true;
-                }
-                solver_container[iZone][INST_0]->LoadRestart(&geometry_container[iZone][INST_0], &solver_container[iZone],
-                                                             config_container[iZone], (int)TimeIter, true);
-              }
-
-              if (rank == MASTER_NODE)
-                cout << "Writing the volume solution for time step " << TimeIter << "." << endl;
-
-              for (iZone = 0; iZone < nZone; iZone++){
+            /*--- Either instantiate the solution class or load a restart file. ---*/
+            if (SolutionInstantiated[iZone] == false &&
+                (TimeIter == 0 || (config_container[ZONE_0]->GetRestart() &&
+                                   ((long)TimeIter == SU2_TYPE::Int(config_container[ZONE_0]->GetRestart_Iter()) ||
+                                    TimeIter % config_container[ZONE_0]->GetVolumeOutputFrequency(0) == 0 ||
+                                    TimeIter + 1 == config_container[ZONE_0]->GetnTime_Iter())))) {
+              solver_container[iZone][INST_0] =
+                  new CBaselineSolver_FEM(geometry_container[iZone][INST_0], config_container[iZone]);
+              output[iZone] =
+                  new CBaselineOutput(config_container[ZONE_0], geometry_container[ZONE_0][INST_0]->GetnDim(),
+                                      solver_container[ZONE_0][INST_0]);
+              output[iZone]->PreprocessVolumeOutput(config_container[ZONE_0]);
+              output[iZone]->PreprocessHistoryOutput(config_container[ZONE_0], false);
+              SolutionInstantiated[iZone] = true;
+            }
+            solver_container[iZone][INST_0]->LoadRestart(&geometry_container[iZone][INST_0], &solver_container[iZone],
+                                                         config_container[iZone], (int)TimeIter, true);
+          }
 
-                WriteFiles(config_container[iZone], geometry_container[iZone][INST_0], &solver_container[iZone][INST_0], output[iZone], TimeIter);
+          if (rank == MASTER_NODE) cout << "Writing the volume solution for time step " << TimeIter << "." << endl;
 
-              }
+          for (iZone = 0; iZone < nZone; iZone++) {
+            WriteFiles(config_container[iZone], geometry_container[iZone][INST_0], &solver_container[iZone][INST_0],
+                       output[iZone], TimeIter);
+          }
         }
 
         TimeIter++;
@@ -488,55 +476,50 @@ int main(int argc, char *argv[]) {
       }
 
     } else {
+      /*--- Steady simulation: merge the single solution file. ---*/
 
-    /*--- Steady simulation: merge the single solution file. ---*/
-
-    for (iZone = 0; iZone < nZone; iZone++) {
-      /*--- Definition of the solution class ---*/
-
-      solver_container[iZone][INST_0] = new CBaselineSolver_FEM(geometry_container[iZone][INST_0], config_container[iZone]);
-      output[iZone] = new CBaselineOutput(config_container[ZONE_0], geometry_container[ZONE_0][INST_0]->GetnDim(), solver_container[ZONE_0][INST_0]);
-      output[iZone]->PreprocessVolumeOutput(config_container[ZONE_0]);
-      output[iZone]->PreprocessHistoryOutput(config_container[ZONE_0], false);
-      solver_container[iZone][INST_0]->LoadRestart(&geometry_container[iZone][INST_0], &solver_container[iZone], config_container[iZone], 0, true);
-    }
-
-    for (iZone = 0; iZone < nZone; iZone++){
+      for (iZone = 0; iZone < nZone; iZone++) {
+        /*--- Definition of the solution class ---*/
 
-      WriteFiles(config_container[iZone], geometry_container[iZone][INST_0], &solver_container[iZone][INST_0], output[iZone], 0);
+        solver_container[iZone][INST_0] =
+            new CBaselineSolver_FEM(geometry_container[iZone][INST_0], config_container[iZone]);
+        output[iZone] = new CBaselineOutput(config_container[ZONE_0], geometry_container[ZONE_0][INST_0]->GetnDim(),
+                                            solver_container[ZONE_0][INST_0]);
+        output[iZone]->PreprocessVolumeOutput(config_container[ZONE_0]);
+        output[iZone]->PreprocessHistoryOutput(config_container[ZONE_0], false);
+        solver_container[iZone][INST_0]->LoadRestart(&geometry_container[iZone][INST_0], &solver_container[iZone],
+                                                     config_container[iZone], 0, true);
+      }
 
+      for (iZone = 0; iZone < nZone; iZone++) {
+        WriteFiles(config_container[iZone], geometry_container[iZone][INST_0], &solver_container[iZone][INST_0],
+                   output[iZone], 0);
+      }
     }
-    }
-
-  }
-  else {
 
+  } else {
     if (config_container[ZONE_0]->GetTime_Domain()) {
-
       /*--- Unsteady simulation: merge all unsteady time steps. First,
        find the frequency and total number of files to write. ---*/
 
       su2double Physical_dt, Physical_t;
       unsigned long TimeIter = 0;
       bool StopCalc = false;
-      bool *SolutionInstantiated = new bool[nZone];
+      bool* SolutionInstantiated = new bool[nZone];
 
-      for (iZone = 0; iZone < nZone; iZone++)
-        SolutionInstantiated[iZone] = false;
+      for (iZone = 0; iZone < nZone; iZone++) SolutionInstantiated[iZone] = false;
 
       /*--- Check for an unsteady restart. Update ExtIter if necessary. ---*/
       if (config_container[ZONE_0]->GetTime_Domain() && config_container[ZONE_0]->GetRestart())
         TimeIter = config_container[ZONE_0]->GetRestart_Iter();
 
       while (TimeIter < config_container[ZONE_0]->GetnTime_Iter()) {
-
         /*--- Check several conditions in order to merge the correct time step files. ---*/
         Physical_dt = config_container[ZONE_0]->GetTime_Step();
-        Physical_t  = (TimeIter+1)*Physical_dt;
-        if (Physical_t >=  config_container[ZONE_0]->GetMax_Time())
-          StopCalc = true;
+        Physical_t = (TimeIter + 1) * Physical_dt;
+        if (Physical_t >= config_container[ZONE_0]->GetMax_Time()) StopCalc = true;
 
-        if ((TimeIter+1 == config_container[ZONE_0]->GetnTime_Iter()) ||
+        if ((TimeIter + 1 == config_container[ZONE_0]->GetnTime_Iter()) ||
             ((TimeIter % config_container[ZONE_0]->GetVolumeOutputFrequency(0) == 0) && (TimeIter != 0) &&
              !((config_container[ZONE_0]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
                (config_container[ZONE_0]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND))) ||
@@ -544,41 +527,37 @@ int main(int argc, char *argv[]) {
             (((config_container[ZONE_0]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
               (config_container[ZONE_0]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND)) &&
              ((TimeIter == 0) || (TimeIter % config_container[ZONE_0]->GetVolumeOutputFrequency(0) == 0)))) {
+          /*--- Read in the restart file for this time step ---*/
+          for (iZone = 0; iZone < nZone; iZone++) {
+            /*--- Set the current iteration number in the config class. ---*/
+            config_container[iZone]->SetTimeIter(TimeIter);
 
+            /*--- Either instantiate the solution class or load a restart file. ---*/
+            if (SolutionInstantiated[iZone] == false &&
+                (TimeIter == 0 || (config_container[ZONE_0]->GetRestart() &&
+                                   ((long)TimeIter == SU2_TYPE::Int(config_container[ZONE_0]->GetRestart_Iter()) ||
+                                    TimeIter % config_container[ZONE_0]->GetVolumeOutputFrequency(0) == 0 ||
+                                    TimeIter + 1 == config_container[ZONE_0]->GetnTime_Iter())))) {
+              solver_container[iZone][INST_0] =
+                  new CBaselineSolver(geometry_container[iZone][INST_0], config_container[iZone]);
+              output[iZone] = new CBaselineOutput(config_container[iZone], geometry_container[iZone][INST_0]->GetnDim(),
+                                                  solver_container[iZone][INST_0]);
+              output[iZone]->PreprocessVolumeOutput(config_container[iZone]);
+              output[iZone]->PreprocessHistoryOutput(config_container[iZone], false);
+
+              SolutionInstantiated[iZone] = true;
+            }
+            config_container[iZone]->SetiInst(INST_0);
+            solver_container[iZone][INST_0]->LoadRestart(geometry_container[iZone], &solver_container[iZone],
+                                                         config_container[iZone], TimeIter, true);
+          }
 
+          if (rank == MASTER_NODE) cout << "Writing the volume solution for time step " << TimeIter << "." << endl;
 
-              /*--- Read in the restart file for this time step ---*/
-              for (iZone = 0; iZone < nZone; iZone++) {
-
-                /*--- Set the current iteration number in the config class. ---*/
-                config_container[iZone]->SetTimeIter(TimeIter);
-
-                /*--- Either instantiate the solution class or load a restart file. ---*/
-                if (SolutionInstantiated[iZone] == false &&
-                    (TimeIter == 0 || (config_container[ZONE_0]->GetRestart() && ((long)TimeIter ==  SU2_TYPE::Int(config_container[ZONE_0]->GetRestart_Iter()) ||
-                                                                                  TimeIter % config_container[ZONE_0]->GetVolumeOutputFrequency(0) == 0 ||
-                                                                                  TimeIter+1 == config_container[ZONE_0]->GetnTime_Iter())))) {
-                  solver_container[iZone][INST_0] = new CBaselineSolver(geometry_container[iZone][INST_0], config_container[iZone]);
-                  output[iZone] = new CBaselineOutput(config_container[iZone], geometry_container[iZone][INST_0]->GetnDim(), solver_container[iZone][INST_0]);
-                  output[iZone]->PreprocessVolumeOutput(config_container[iZone]);
-                  output[iZone]->PreprocessHistoryOutput(config_container[iZone], false);
-
-                  SolutionInstantiated[iZone] = true;
-                }
-                  config_container[iZone]->SetiInst(INST_0);
-                  solver_container[iZone][INST_0]->LoadRestart(geometry_container[iZone], &solver_container[iZone], config_container[iZone], TimeIter, true);
-              }
-
-              if (rank == MASTER_NODE)
-                cout << "Writing the volume solution for time step " << TimeIter << "." << endl;
-
-              for (iZone = 0; iZone < nZone; iZone++){
-
-                WriteFiles(config_container[iZone], geometry_container[iZone][INST_0], &solver_container[iZone][INST_0], output[iZone], TimeIter);
-
-              }
-
-
+          for (iZone = 0; iZone < nZone; iZone++) {
+            WriteFiles(config_container[iZone], geometry_container[iZone][INST_0], &solver_container[iZone][INST_0],
+                       output[iZone], TimeIter);
+          }
         }
 
         TimeIter++;
@@ -588,19 +567,19 @@ int main(int argc, char *argv[]) {
     }
 
     else if (config_container[ZONE_0]->GetTime_Marching() == TIME_MARCHING::HARMONIC_BALANCE) {
-
       /*--- Read in the restart file for this time step ---*/
       for (iZone = 0; iZone < nZone; iZone++) {
-
-        for (iInst = 0; iInst < nInst[iZone]; iInst++){
-
+        for (iInst = 0; iInst < nInst[iZone]; iInst++) {
           config_container[iZone]->SetiInst(iInst);
           config_container[iZone]->SetTimeIter(iInst);
 
           /*--- Either instantiate the solution class or load a restart file. ---*/
-          solver_container[iZone][iInst] = new CBaselineSolver(geometry_container[iZone][iInst], config_container[iZone]);
-          solver_container[iZone][iInst]->LoadRestart(geometry_container[iZone], &solver_container[iZone], config_container[iZone], iInst, true);
-          output[iZone] = new CBaselineOutput(config_container[iZone], geometry_container[iZone][iInst]->GetnDim(), solver_container[iZone][iInst]);
+          solver_container[iZone][iInst] =
+              new CBaselineSolver(geometry_container[iZone][iInst], config_container[iZone]);
+          solver_container[iZone][iInst]->LoadRestart(geometry_container[iZone], &solver_container[iZone],
+                                                      config_container[iZone], iInst, true);
+          output[iZone] = new CBaselineOutput(config_container[iZone], geometry_container[iZone][iInst]->GetnDim(),
+                                              solver_container[iZone][iInst]);
           output[iZone]->PreprocessVolumeOutput(config_container[iZone]);
           output[iZone]->PreprocessHistoryOutput(config_container[iZone], false);
 
@@ -609,17 +588,14 @@ int main(int argc, char *argv[]) {
             cout << "Storing the volume solution for time instance " << iInst << "." << endl;
           }
 
-          WriteFiles(config_container[iZone], geometry_container[iZone][iInst], &solver_container[iZone][iInst], output[iZone], iInst);
-
+          WriteFiles(config_container[iZone], geometry_container[iZone][iInst], &solver_container[iZone][iInst],
+                     output[iZone], iInst);
         }
-
       }
 
-
     }
 
-    else if (config_container[ZONE_0]->GetTime_Domain()){
-
+    else if (config_container[ZONE_0]->GetTime_Domain()) {
       /*--- Dynamic simulation: merge all unsteady time steps. First,
        find the frequency and total number of files to write. ---*/
 
@@ -628,117 +604,112 @@ int main(int argc, char *argv[]) {
       bool StopCalc = false;
       bool SolutionInstantiated = false;
 
-
       /*--- Check for an dynamic restart (structural analysis). Update ExtIter if necessary. ---*/
-      if (config_container[ZONE_0]->GetKind_Solver() == MAIN_SOLVER::FEM_ELASTICITY && config_container[ZONE_0]->GetRestart())
+      if (config_container[ZONE_0]->GetKind_Solver() == MAIN_SOLVER::FEM_ELASTICITY &&
+          config_container[ZONE_0]->GetRestart())
         TimeIter = config_container[ZONE_0]->GetRestart_Iter();
 
       while (TimeIter < config_container[ZONE_0]->GetnTime_Iter()) {
-
         /*--- Check several conditions in order to merge the correct time step files. ---*/
         /*--- If the solver is structural, the total and delta_t are obtained from different functions. ---*/
 
         Physical_dt = config_container[ZONE_0]->GetTime_Step();
-        Physical_t  = (TimeIter+1)*Physical_dt;
-        if (Physical_t >=  config_container[ZONE_0]->GetMax_Time())
-          StopCalc = true;
+        Physical_t = (TimeIter + 1) * Physical_dt;
+        if (Physical_t >= config_container[ZONE_0]->GetMax_Time()) StopCalc = true;
 
-        if ((TimeIter+1 == config_container[ZONE_0]->GetnTime_Iter()) ||
-            (StopCalc) ||
+        if ((TimeIter + 1 == config_container[ZONE_0]->GetnTime_Iter()) || (StopCalc) ||
             ((config_container[ZONE_0]->GetTime_Domain()) &&
              ((TimeIter == 0) || (TimeIter % config_container[ZONE_0]->GetVolumeOutputFrequency(0) == 0)))) {
+          /*--- Set the current iteration number in the config class. ---*/
+          config_container[ZONE_0]->SetTimeIter(TimeIter);
+
+          /*--- Read in the restart file for this time step ---*/
+          for (iZone = 0; iZone < nZone; iZone++) {
+            /*--- Either instantiate the solution class or load a restart file. ---*/
+            if (SolutionInstantiated == false &&
+                (TimeIter == 0 ||
+                 ((config_container[ZONE_0]->GetRestart() &&
+                   (SU2_TYPE::Int(TimeIter) == SU2_TYPE::Int(config_container[ZONE_0]->GetRestart_Iter()))) ||
+                  TimeIter % config_container[ZONE_0]->GetVolumeOutputFrequency(0) == 0 ||
+                  TimeIter + 1 == config_container[ZONE_0]->GetnTime_Iter()))) {
+              solver_container[iZone][INST_0] =
+                  new CBaselineSolver(geometry_container[iZone][INST_0], config_container[iZone]);
+              output[iZone] = new CBaselineOutput(config_container[iZone], geometry_container[iZone][INST_0]->GetnDim(),
+                                                  solver_container[iZone][INST_0]);
+              output[iZone]->PreprocessVolumeOutput(config_container[iZone]);
+              output[iZone]->PreprocessHistoryOutput(config_container[iZone], false);
+
+              SolutionInstantiated = true;
+            }
+            config_container[iZone]->SetiInst(INST_0);
+            solver_container[iZone][INST_0]->LoadRestart(geometry_container[iZone], &solver_container[iZone],
+                                                         config_container[iZone], TimeIter, true);
+          }
 
-              /*--- Set the current iteration number in the config class. ---*/
-              config_container[ZONE_0]->SetTimeIter(TimeIter);
-
-              /*--- Read in the restart file for this time step ---*/
-              for (iZone = 0; iZone < nZone; iZone++) {
-
-                /*--- Either instantiate the solution class or load a restart file. ---*/
-                if (SolutionInstantiated == false &&
-                    (TimeIter == 0 || ((config_container[ZONE_0]->GetRestart() && (SU2_TYPE::Int(TimeIter) ==  SU2_TYPE::Int(config_container[ZONE_0]->GetRestart_Iter()))) ||
-                                       TimeIter % config_container[ZONE_0]->GetVolumeOutputFrequency(0)  == 0 ||
-                                       TimeIter+1 == config_container[ZONE_0]->GetnTime_Iter()))) {
-                  solver_container[iZone][INST_0] = new CBaselineSolver(geometry_container[iZone][INST_0], config_container[iZone]);
-                  output[iZone] = new CBaselineOutput(config_container[iZone], geometry_container[iZone][INST_0]->GetnDim(), solver_container[iZone][INST_0]);
-                  output[iZone]->PreprocessVolumeOutput(config_container[iZone]);
-                  output[iZone]->PreprocessHistoryOutput(config_container[iZone], false);
-
-                  SolutionInstantiated = true;
-                }
-                config_container[iZone]->SetiInst(INST_0);
-                solver_container[iZone][INST_0]->LoadRestart(geometry_container[iZone], &solver_container[iZone], config_container[iZone], TimeIter, true);
-              }
-
-              if (rank == MASTER_NODE)
-                cout << "Writing the volume solution for time step " << TimeIter << "." << endl;
-              for (iZone = 0; iZone < nZone; iZone++){
-
-                WriteFiles(config_container[iZone], geometry_container[iZone][INST_0], &solver_container[iZone][INST_0], output[iZone], TimeIter);
-
-              }
+          if (rank == MASTER_NODE) cout << "Writing the volume solution for time step " << TimeIter << "." << endl;
+          for (iZone = 0; iZone < nZone; iZone++) {
+            WriteFiles(config_container[iZone], geometry_container[iZone][INST_0], &solver_container[iZone][INST_0],
+                       output[iZone], TimeIter);
+          }
         }
 
         TimeIter++;
         if (StopCalc) break;
       }
 
-      }
+    }
 
     else {
-
       /*--- Steady simulation: merge the single solution file. ---*/
 
       for (iZone = 0; iZone < nZone; iZone++) {
         config_container[iZone]->SetiInst(INST_0);
         /*--- Definition of the solution class ---*/
-        solver_container[iZone][INST_0] = new CBaselineSolver(geometry_container[iZone][INST_0], config_container[iZone]);
-        solver_container[iZone][INST_0]->LoadRestart(geometry_container[iZone], &solver_container[iZone], config_container[iZone], 0, true);
-        output[iZone] = new CBaselineOutput(config_container[iZone], geometry_container[iZone][INST_0]->GetnDim(), solver_container[iZone][INST_0]);
+        solver_container[iZone][INST_0] =
+            new CBaselineSolver(geometry_container[iZone][INST_0], config_container[iZone]);
+        solver_container[iZone][INST_0]->LoadRestart(geometry_container[iZone], &solver_container[iZone],
+                                                     config_container[iZone], 0, true);
+        output[iZone] = new CBaselineOutput(config_container[iZone], geometry_container[iZone][INST_0]->GetnDim(),
+                                            solver_container[iZone][INST_0]);
         output[iZone]->PreprocessVolumeOutput(config_container[iZone]);
         output[iZone]->PreprocessHistoryOutput(config_container[iZone], false);
-
       }
-      for (iZone = 0; iZone < nZone; iZone++){
-
-        WriteFiles(config_container[iZone], geometry_container[iZone][INST_0], &solver_container[iZone][INST_0], output[iZone], 0);
-
+      for (iZone = 0; iZone < nZone; iZone++) {
+        WriteFiles(config_container[iZone], geometry_container[iZone][INST_0], &solver_container[iZone][INST_0],
+                   output[iZone], 0);
       }
     }
-
   }
 
   delete config;
   config = nullptr;
 
   if (rank == MASTER_NODE)
-    cout << endl <<"------------------------- Solver Postprocessing -------------------------" << endl;
+    cout << endl << "------------------------- Solver Postprocessing -------------------------" << endl;
 
   if (geometry_container != nullptr) {
     for (iZone = 0; iZone < nZone; iZone++) {
-      for (iInst = 0; iInst < nInst[iZone]; iInst++){
+      for (iInst = 0; iInst < nInst[iZone]; iInst++) {
         if (geometry_container[iZone][iInst] != nullptr) {
           delete geometry_container[iZone][iInst];
         }
       }
-      if (geometry_container[iZone] != nullptr)
-        delete [] geometry_container[iZone];
+      if (geometry_container[iZone] != nullptr) delete[] geometry_container[iZone];
     }
-    delete [] geometry_container;
+    delete[] geometry_container;
   }
   if (rank == MASTER_NODE) cout << "Deleted CGeometry container." << endl;
 
   if (solver_container != nullptr) {
     for (iZone = 0; iZone < nZone; iZone++) {
-      for (iInst = 0; iInst < nInst[iZone]; iInst++){
+      for (iInst = 0; iInst < nInst[iZone]; iInst++) {
         if (solver_container[iZone][iInst] != nullptr) {
           delete solver_container[iZone][iInst];
         }
       }
-      if (solver_container[iZone] != nullptr)
-        delete [] solver_container[iZone];
+      if (solver_container[iZone] != nullptr) delete[] solver_container[iZone];
     }
-    delete [] solver_container;
+    delete[] solver_container;
   }
   if (rank == MASTER_NODE) cout << "Deleted CSolver class." << endl;
 
@@ -748,7 +719,7 @@ int main(int argc, char *argv[]) {
         delete config_container[iZone];
       }
     }
-    delete [] config_container;
+    delete[] config_container;
   }
   if (rank == MASTER_NODE) cout << "Deleted CConfig container." << endl;
 
@@ -758,7 +729,7 @@ int main(int argc, char *argv[]) {
         delete output[iZone];
       }
     }
-    delete [] output;
+    delete[] output;
   }
   if (rank == MASTER_NODE) cout << "Deleted COutput class." << endl;
 
@@ -769,16 +740,19 @@ int main(int argc, char *argv[]) {
 
   /*--- Compute/print the total time for performance benchmarking. ---*/
 
-  UsedTime = StopTime-StartTime;
+  UsedTime = StopTime - StartTime;
   if (rank == MASTER_NODE) {
-    cout << "\nCompleted in " << fixed << UsedTime << " seconds on "<< size;
-    if (size == 1) cout << " core." << endl; else cout << " cores." << endl;
+    cout << "\nCompleted in " << fixed << UsedTime << " seconds on " << size;
+    if (size == 1)
+      cout << " core." << endl;
+    else
+      cout << " cores." << endl;
   }
 
   /*--- Exit the solver cleanly ---*/
 
   if (rank == MASTER_NODE)
-    cout << endl <<"------------------------- Exit Success (SU2_SOL) ------------------------" << endl << endl;
+    cout << endl << "------------------------- Exit Success (SU2_SOL) ------------------------" << endl << endl;
 
   /*--- Finalize MPI parallelization ---*/
   SU2_MPI::Finalize();
@@ -786,8 +760,8 @@ int main(int argc, char *argv[]) {
   return EXIT_SUCCESS;
 }
 
-void WriteFiles(CConfig *config, CGeometry* geometry, CSolver** solver_container, COutput *output, unsigned long TimeIter){
-
+void WriteFiles(CConfig* config, CGeometry* geometry, CSolver** solver_container, COutput* output,
+                unsigned long TimeIter) {
   /*--- Load history data (volume output might require some values) --- */
 
   output->SetHistory_Output(geometry, solver_container, config, TimeIter, 0, 0);
@@ -802,12 +776,10 @@ void WriteFiles(CConfig *config, CGeometry* geometry, CSolver** solver_container
 
   output->SetSurface_Filename(config->GetSurfCoeff_FileName());
 
-  for (unsigned short iFile = 0; iFile < config->GetnVolumeOutputFiles(); iFile++){
+  for (unsigned short iFile = 0; iFile < config->GetnVolumeOutputFiles(); iFile++) {
     auto FileFormat = config->GetVolumeOutputFiles();
-    if (FileFormat[iFile] != OUTPUT_TYPE::RESTART_ASCII &&
-        FileFormat[iFile] != OUTPUT_TYPE::RESTART_BINARY &&
+    if (FileFormat[iFile] != OUTPUT_TYPE::RESTART_ASCII && FileFormat[iFile] != OUTPUT_TYPE::RESTART_BINARY &&
         FileFormat[iFile] != OUTPUT_TYPE::CSV)
       output->WriteToFile(config, geometry, FileFormat[iFile]);
   }
-
 }
diff --git a/UnitTests/Common/containers/CLookupTable_tests.cpp b/UnitTests/Common/containers/CLookupTable_tests.cpp
index 22cb17e393e..f17049ec341 100644
--- a/UnitTests/Common/containers/CLookupTable_tests.cpp
+++ b/UnitTests/Common/containers/CLookupTable_tests.cpp
@@ -35,25 +35,23 @@
 #include "../../../Common/include/containers/CLookUpTable.hpp"
 #include "../../../Common/include/containers/CFileReaderLUT.hpp"
 
-
 TEST_CASE("LUTreader", "[tabulated chemistry]") {
-
   /*--- smaller and trivial lookup table ---*/
 
-  CLookUpTable look_up_table("src/SU2/UnitTests/Common/containers/lookuptable.drg","ProgressVariable","EnthalpyTot");
+  CLookUpTable look_up_table("src/SU2/UnitTests/Common/containers/lookuptable.drg", "ProgressVariable", "EnthalpyTot");
 
   /*--- string names of the controlling variables ---*/
 
   string name_CV1 = "ProgressVariable";
   string name_CV2 = "EnthalpyTot";
 
- /*--- look up a single value for density ---*/
+  /*--- look up a single value for density ---*/
 
   su2double prog = 0.55;
   su2double enth = -0.5;
   string look_up_tag = "Density";
   su2double look_up_dat;
-  look_up_table.LookUp_XY(look_up_tag, &look_up_dat, prog, enth); 
+  look_up_table.LookUp_XY(look_up_tag, &look_up_dat, prog, enth);
   CHECK(look_up_dat == Approx(1.02));
 
   /*--- look up a single value for viscosity ---*/
@@ -61,11 +59,11 @@ TEST_CASE("LUTreader", "[tabulated chemistry]") {
   prog = 0.6;
   enth = 0.9;
   look_up_tag = "Viscosity";
-  look_up_table.LookUp_XY(look_up_tag, &look_up_dat, prog, enth); 
+  look_up_table.LookUp_XY(look_up_tag, &look_up_dat, prog, enth);
   CHECK(look_up_dat == Approx(0.0000674286));
 
   /* find the table limits */
-  
+
   auto limitsEnth = look_up_table.GetTableLimitsY();
   CHECK(SU2_TYPE::GetValue(*limitsEnth.first) == Approx(-1.0));
   CHECK(SU2_TYPE::GetValue(*limitsEnth.second) == Approx(1.0));
@@ -79,43 +77,42 @@ TEST_CASE("LUTreader", "[tabulated chemistry]") {
   prog = 1.10;
   enth = 1.1;
   look_up_tag = "Density";
-  look_up_table.LookUp_XY(look_up_tag, &look_up_dat, prog, enth); 
+  look_up_table.LookUp_XY(look_up_tag, &look_up_dat, prog, enth);
   CHECK(look_up_dat == Approx(1.1738796125));
-
 }
 
 TEST_CASE("LUTreader_3D", "[tabulated chemistry]") {
-
   /*--- smaller and trivial lookup table ---*/
-  
-  CLookUpTable look_up_table("src/SU2/UnitTests/Common/containers/lookuptable_3D.drg","ProgressVariable","EnthalpyTot");
+
+  CLookUpTable look_up_table("src/SU2/UnitTests/Common/containers/lookuptable_3D.drg", "ProgressVariable",
+                             "EnthalpyTot");
 
   /*--- string names of the controlling variables ---*/
 
   string name_CV1 = "ProgressVariable";
   string name_CV2 = "EnthalpyTot";
 
- /*--- look up a single value for density ---*/
+  /*--- look up a single value for density ---*/
 
   su2double prog = 0.55;
-  su2double enth = -0.5; 
+  su2double enth = -0.5;
   su2double mfrac = 0.5;
   string look_up_tag = "Density";
   su2double look_up_dat;
-  look_up_table.LookUp_XYZ(look_up_tag, &look_up_dat, prog, enth, mfrac); 
+  look_up_table.LookUp_XYZ(look_up_tag, &look_up_dat, prog, enth, mfrac);
   CHECK(look_up_dat == Approx(1.02));
 
   /*--- look up a single value for viscosity ---*/
 
   prog = 0.6;
-  enth = 0.9; 
+  enth = 0.9;
   mfrac = 0.8;
   look_up_tag = "Viscosity";
-  look_up_table.LookUp_XYZ(look_up_tag, &look_up_dat, prog, enth, mfrac); 
+  look_up_table.LookUp_XYZ(look_up_tag, &look_up_dat, prog, enth, mfrac);
   CHECK(look_up_dat == Approx(0.0000674286));
 
   /* find the table limits */
-  
+
   auto limitsEnth = look_up_table.GetTableLimitsY();
   CHECK(SU2_TYPE::GetValue(*limitsEnth.first) == Approx(-1.0));
   CHECK(SU2_TYPE::GetValue(*limitsEnth.second) == Approx(1.0));
@@ -130,7 +127,6 @@ TEST_CASE("LUTreader_3D", "[tabulated chemistry]") {
   enth = 1.1;
   mfrac = 2.0;
   look_up_tag = "Density";
-  look_up_table.LookUp_XYZ(look_up_tag, &look_up_dat, prog, enth, mfrac); 
+  look_up_table.LookUp_XYZ(look_up_tag, &look_up_dat, prog, enth, mfrac);
   CHECK(look_up_dat == Approx(1.1738796125));
- 
 }
diff --git a/UnitTests/Common/geometry/CGeometry_test.cpp b/UnitTests/Common/geometry/CGeometry_test.cpp
index be8992699c1..edd24e82ec0 100644
--- a/UnitTests/Common/geometry/CGeometry_test.cpp
+++ b/UnitTests/Common/geometry/CGeometry_test.cpp
@@ -30,44 +30,41 @@
 
 std::unique_ptr<UnitQuadTestCase> TestCase;
 
-TEST_CASE("Geometry constructor", "[Geometry]"){
-
+TEST_CASE("Geometry constructor", "[Geometry]") {
   cout.rdbuf(nullptr);
 
   TestCase = std::unique_ptr<UnitQuadTestCase>(new UnitQuadTestCase());
 
   TestCase->InitConfig();
 
-  auto aux_geometry =  std::unique_ptr<CGeometry>(new CPhysicalGeometry(TestCase->config.get(), 0, 1));
+  auto aux_geometry = std::unique_ptr<CGeometry>(new CPhysicalGeometry(TestCase->config.get(), 0, 1));
 
-  CHECK(aux_geometry->GetnPoint()    == 125);
-  CHECK(aux_geometry->GetnElem()     == 64);
+  CHECK(aux_geometry->GetnPoint() == 125);
+  CHECK(aux_geometry->GetnElem() == 64);
   CHECK(aux_geometry->GetnElemHexa() == 64);
-  CHECK(aux_geometry->GetnEdge()     == 0);
+  CHECK(aux_geometry->GetnEdge() == 0);
   CHECK(aux_geometry->GetnElem_Bound(0) == 16);
   CHECK(aux_geometry->GetnElem_Bound(5) == 16);
 
   TestCase->geometry = std::unique_ptr<CGeometry>(new CPhysicalGeometry(aux_geometry.get(), TestCase->config.get()));
 
-  CHECK(TestCase->geometry->GetnPoint()    == 125);
-  CHECK(TestCase->geometry->GetnElem()     == 64);
+  CHECK(TestCase->geometry->GetnPoint() == 125);
+  CHECK(TestCase->geometry->GetnElem() == 64);
   CHECK(TestCase->geometry->GetnElemHexa() == 64);
-  CHECK(TestCase->geometry->GetnEdge()     == 0);
+  CHECK(TestCase->geometry->GetnEdge() == 0);
   CHECK(TestCase->geometry->GetnElem_Bound(0) == 16);
   CHECK(TestCase->geometry->GetnElem_Bound(5) == 16);
 
   cout.rdbuf(TestCase->orig_buf);
-
 }
 
-TEST_CASE("Set Send/Recv", "[Geometry]"){
+TEST_CASE("Set Send/Recv", "[Geometry]") {
   TestCase->geometry->SetSendReceive(TestCase->config.get());
 
   /*---- No check yet, since unit tests run in serial at the moment ---*/
 }
 
-TEST_CASE("Set Boundaries", "[Geometry]"){
-
+TEST_CASE("Set Boundaries", "[Geometry]") {
   TestCase->geometry->SetBoundaries(TestCase->config.get());
 
   CHECK(TestCase->config->GetMarker_All_KindBC(0) == CUSTOM_BOUNDARY);
@@ -76,75 +73,63 @@ TEST_CASE("Set Boundaries", "[Geometry]"){
   CHECK(TestCase->config->GetSolid_Wall(3));
 }
 
-TEST_CASE("Set Point Connectivity", "[Geometry]"){
-
+TEST_CASE("Set Point Connectivity", "[Geometry]") {
   TestCase->geometry->SetPoint_Connectivity();
 
-  CHECK(TestCase->geometry->nodes->GetnElem(55)     == 4);
-  CHECK(TestCase->geometry->nodes->GetElem(30, 2)   == 16);
-  CHECK(TestCase->geometry->nodes->GetnNeighbor(3)  == 4);
-  CHECK(TestCase->geometry->nodes->GetPoint(99, 2)  == 98);
+  CHECK(TestCase->geometry->nodes->GetnElem(55) == 4);
+  CHECK(TestCase->geometry->nodes->GetElem(30, 2) == 16);
+  CHECK(TestCase->geometry->nodes->GetnNeighbor(3) == 4);
+  CHECK(TestCase->geometry->nodes->GetPoint(99, 2) == 98);
 }
 
-TEST_CASE("Set elem connectivity", "[Geometry]"){
-
+TEST_CASE("Set elem connectivity", "[Geometry]") {
   TestCase->geometry->SetElement_Connectivity();
 
   CHECK(TestCase->geometry->elem[14]->GetnFaces() == 6);
   CHECK(TestCase->geometry->elem[14]->GetNeighbor_Elements(1) == 15);
-
 }
 
-TEST_CASE("Set bound volume", "[Geometry]"){
-
+TEST_CASE("Set bound volume", "[Geometry]") {
   TestCase->geometry->SetBoundVolume();
 
   CHECK(TestCase->geometry->bound[0][10]->GetDomainElement() == 40);
   CHECK(TestCase->geometry->bound[4][10]->GetDomainElement() == 10);
-
 }
 
-TEST_CASE("Set Edges", "[Geometry]"){
-
+TEST_CASE("Set Edges", "[Geometry]") {
   TestCase->geometry->SetEdges();
 
   CHECK(TestCase->geometry->edges->GetnNodes() == 2);
-  CHECK(TestCase->geometry->edges->GetNode(42,0) == 15);
-  CHECK(TestCase->geometry->edges->GetNode(87,1) == 57);
-
+  CHECK(TestCase->geometry->edges->GetNode(42, 0) == 15);
+  CHECK(TestCase->geometry->edges->GetNode(87, 1) == 57);
 }
 
-TEST_CASE("Set vertex", "[Geometry]"){
-
+TEST_CASE("Set vertex", "[Geometry]") {
   TestCase->geometry->SetVertex(TestCase->config.get());
 
   CHECK(TestCase->geometry->GetnVertex(0) == 25);
   CHECK(TestCase->geometry->vertex[0][20]->GetNode() == 100);
   CHECK(TestCase->geometry->nodes->GetVertex(100, 0) == 20);
   CHECK(TestCase->geometry->nodes->GetVertex(1, 0) == -1);
-
 }
 
-TEST_CASE("Set control volume", "[Geometry]"){
-
+TEST_CASE("Set control volume", "[Geometry]") {
   TestCase->geometry->SetControlVolume(TestCase->config.get(), ALLOCATE);
 
   CHECK(TestCase->geometry->elem[42]->GetCG(0) == 0.625);
-  CHECK(TestCase->geometry->elem[3]->GetCG(1)  == 0.125);
+  CHECK(TestCase->geometry->elem[3]->GetCG(1) == 0.125);
   CHECK(TestCase->geometry->elem[25]->GetCG(2) == 0.375);
 
   CHECK(TestCase->geometry->nodes->GetVolume(42) == Approx(0.015625));
 
   CHECK(TestCase->geometry->edges->GetNormal(32)[0] == 0.03125);
-  CHECK(TestCase->geometry->edges->GetNormal(5)[1]  == 0.0);
+  CHECK(TestCase->geometry->edges->GetNormal(5)[1] == 0.0);
   CHECK(TestCase->geometry->edges->GetNormal(10)[2] == 0.03125);
 
   CHECK(TestCase->config->GetDomainVolume() == Approx(1.0));
-
 }
 
-TEST_CASE("Set bound control volume", "[Geometry]"){
-
+TEST_CASE("Set bound control volume", "[Geometry]") {
   TestCase->geometry->SetBoundControlVolume(TestCase->config.get(), ALLOCATE);
 
   CHECK(TestCase->geometry->bound[1][4]->GetCG(0) == 1.0);
@@ -153,6 +138,5 @@ TEST_CASE("Set bound control volume", "[Geometry]"){
 
   CHECK(TestCase->geometry->vertex[0][4]->GetNormal()[0] == -0.0625);
   CHECK(TestCase->geometry->vertex[3][2]->GetNormal()[1] == -0.0625);
-  CHECK(TestCase->geometry->vertex[5][3]->GetNormal()[2] ==  0.03125);
-
+  CHECK(TestCase->geometry->vertex[5][3]->GetNormal()[2] == 0.03125);
 }
diff --git a/UnitTests/Common/geometry/dual_grid/CDualGrid_tests.cpp b/UnitTests/Common/geometry/dual_grid/CDualGrid_tests.cpp
index a0eb34f1a22..2193446fe84 100644
--- a/UnitTests/Common/geometry/dual_grid/CDualGrid_tests.cpp
+++ b/UnitTests/Common/geometry/dual_grid/CDualGrid_tests.cpp
@@ -32,41 +32,47 @@
 #include "../../../Common/include/geometry/dual_grid/CVertex.hpp"
 
 TEST_CASE("Volume Computation", "[Dual Grid]") {
-
   su2double Coord_FaceiPoint[3];
   su2double Coord_FaceElem_CG[3];
   su2double Coord_Elem_CG[3];
   su2double Coord_Edge_CG[3];
   su2double scaling = 100;
 
-  Coord_FaceiPoint[0]  = scaling*0.664995; Coord_FaceiPoint[1]  = scaling*1.1462;  Coord_FaceiPoint[2]  = scaling*0.00926223;
-  Coord_FaceElem_CG[0] = scaling*0.655997; Coord_FaceElem_CG[1] = scaling*1.13054; Coord_FaceElem_CG[2] = scaling*0.00945181;
-  Coord_Elem_CG[0]     = scaling*0.653846; Coord_Elem_CG[1]     = scaling*1.12927; Coord_Elem_CG[2]     = scaling*0.00835789;
-  Coord_Edge_CG[0]     = scaling*0.664943; Coord_Edge_CG[1]     = scaling*1.14623; Coord_Edge_CG[2]     = scaling*0.00935524;
+  Coord_FaceiPoint[0] = scaling * 0.664995;
+  Coord_FaceiPoint[1] = scaling * 1.1462;
+  Coord_FaceiPoint[2] = scaling * 0.00926223;
+  Coord_FaceElem_CG[0] = scaling * 0.655997;
+  Coord_FaceElem_CG[1] = scaling * 1.13054;
+  Coord_FaceElem_CG[2] = scaling * 0.00945181;
+  Coord_Elem_CG[0] = scaling * 0.653846;
+  Coord_Elem_CG[1] = scaling * 1.12927;
+  Coord_Elem_CG[2] = scaling * 0.00835789;
+  Coord_Edge_CG[0] = scaling * 0.664943;
+  Coord_Edge_CG[1] = scaling * 1.14623;
+  Coord_Edge_CG[2] = scaling * 0.00935524;
 
-  SECTION("2D Edge"){
+  SECTION("2D Edge") {
     su2double volume = CEdge::GetVolume(Coord_FaceiPoint, Coord_Edge_CG, Coord_Elem_CG);
     REQUIRE(volume == Approx(0.00607415));
   }
 
-  SECTION("3D Edge"){
+  SECTION("3D Edge") {
     su2double volume = CEdge::GetVolume(Coord_FaceiPoint, Coord_Edge_CG, Coord_FaceElem_CG, Coord_Elem_CG);
     REQUIRE(volume == Approx(0.000546832));
   }
 
   CVertex vertex2d(0, 2);
-  SECTION("2D Vertex"){
+  SECTION("2D Vertex") {
     vertex2d.SetNodes_Coord(Coord_Edge_CG, Coord_Elem_CG);
     REQUIRE(vertex2d.GetNormal()[0] == Approx(-1.696));
     REQUIRE(vertex2d.GetNormal()[1] == Approx(1.1097));
   }
 
   CVertex vertex3d(0, 3);
-  SECTION("3D Vertex"){
+  SECTION("3D Vertex") {
     vertex3d.SetNodes_Coord(Coord_Edge_CG, Coord_FaceElem_CG, Coord_Elem_CG);
     REQUIRE(vertex3d.GetNormal()[0] == Approx(-0.0864312));
     REQUIRE(vertex3d.GetNormal()[1] == Approx(0.0499696));
     REQUIRE(vertex3d.GetNormal()[2] == Approx(0.111938));
   }
-
 }
diff --git a/UnitTests/Common/geometry/primal_grid/CPrimalGrid_tests.cpp b/UnitTests/Common/geometry/primal_grid/CPrimalGrid_tests.cpp
index e8282665a60..5323fc0da56 100644
--- a/UnitTests/Common/geometry/primal_grid/CPrimalGrid_tests.cpp
+++ b/UnitTests/Common/geometry/primal_grid/CPrimalGrid_tests.cpp
@@ -31,36 +31,50 @@
 #include "../../../Common/include/geometry/primal_grid/CHexahedron.hpp"
 
 TEST_CASE("Center of gravity computation", "[Primal Grid]") {
-
   const int nDim = 3;
 
-  su2double **coordinates = new su2double*[8];
-  for (int i = 0; i < 8; i++){
+  su2double** coordinates = new su2double*[8];
+  for (int i = 0; i < 8; i++) {
     coordinates[i] = new su2double[nDim];
   }
-  coordinates[0][0] = 7.946516948817000e-01; coordinates[0][1] = 0.000000000000000e+00; coordinates[0][2] = -1.530741281331000e-03;
-  coordinates[1][0] = 7.946538480939001e-01; coordinates[1][1] = 0.000000000000000e+00; coordinates[1][2] = -1.554823763559000e-03;
-  coordinates[2][0] = 4.613089666440000e-01; coordinates[2][1] = 0.000000000000000e+00; coordinates[2][2] = -3.089699212314000e-03;
-  coordinates[3][0] = 7.831152624057000e-01; coordinates[3][1] = 0.000000000000000e+00; coordinates[3][2] = -1.530741281331000e-03;
-  coordinates[4][0] = 8.322953467911001e-01; coordinates[4][1] = 1.324931278110000e-01; coordinates[4][2] = -1.456502113362000e-03;
-  coordinates[5][0] = 8.322984569865000e-01; coordinates[5][1] = 1.336230857244000e-01; coordinates[5][2] = -1.480923128397000e-03;
-  coordinates[6][0] = 8.213630099601000e-01; coordinates[6][1] = 1.326360771765000e-01; coordinates[6][2] = -2.941176615903000e-03;
-  coordinates[7][0] = 8.213597801418000e-01; coordinates[7][1] = 1.326371537826000e-01; coordinates[7][2] = -2.916814216089000e-03;
+  coordinates[0][0] = 7.946516948817000e-01;
+  coordinates[0][1] = 0.000000000000000e+00;
+  coordinates[0][2] = -1.530741281331000e-03;
+  coordinates[1][0] = 7.946538480939001e-01;
+  coordinates[1][1] = 0.000000000000000e+00;
+  coordinates[1][2] = -1.554823763559000e-03;
+  coordinates[2][0] = 4.613089666440000e-01;
+  coordinates[2][1] = 0.000000000000000e+00;
+  coordinates[2][2] = -3.089699212314000e-03;
+  coordinates[3][0] = 7.831152624057000e-01;
+  coordinates[3][1] = 0.000000000000000e+00;
+  coordinates[3][2] = -1.530741281331000e-03;
+  coordinates[4][0] = 8.322953467911001e-01;
+  coordinates[4][1] = 1.324931278110000e-01;
+  coordinates[4][2] = -1.456502113362000e-03;
+  coordinates[5][0] = 8.322984569865000e-01;
+  coordinates[5][1] = 1.336230857244000e-01;
+  coordinates[5][2] = -1.480923128397000e-03;
+  coordinates[6][0] = 8.213630099601000e-01;
+  coordinates[6][1] = 1.326360771765000e-01;
+  coordinates[6][2] = -2.941176615903000e-03;
+  coordinates[7][0] = 8.213597801418000e-01;
+  coordinates[7][1] = 1.326371537826000e-01;
+  coordinates[7][2] = -2.916814216089000e-03;
 
-#define REQUIRE_CG(name, x, y, z) \
-  name.SetCoord_CG(nDim, coordinates);   \
+#define REQUIRE_CG(name, x, y, z)      \
+  name.SetCoord_CG(nDim, coordinates); \
   REQUIRE(name.GetCG(0) == Approx(x)); \
   REQUIRE(name.GetCG(1) == Approx(y)); \
   REQUIRE(name.GetCG(2) == Approx(z));
 
   // It is sufficient to test the CG computation for Hexahedron.
   // Routine is the same for all elements (impl. in CPrimalGrid)
-  CHexahedron hexa(0,1,2,3,4,5,6,7);
+  CHexahedron hexa(0, 1, 2, 3, 4, 5, 6, 7);
   REQUIRE_CG(hexa, 0.7676307957, 0.0664236806, -0.0020626777);
 
-  for (int i = 0; i < 8; i++){
-    delete [] coordinates[i];
+  for (int i = 0; i < 8; i++) {
+    delete[] coordinates[i];
   }
-  delete [] coordinates;
-
+  delete[] coordinates;
 }
diff --git a/UnitTests/Common/simple_ad_test.cpp b/UnitTests/Common/simple_ad_test.cpp
index 3fc3dc0da29..32e2b22db83 100644
--- a/UnitTests/Common/simple_ad_test.cpp
+++ b/UnitTests/Common/simple_ad_test.cpp
@@ -31,9 +31,7 @@
 
 #include "../../Common/include/basic_types/datatype_structure.hpp"
 
-su2double func(const su2double& x) {
-  return x * x * x;
-}
+su2double func(const su2double& x) { return x * x * x; }
 
 /*---
  * This test case is based off of Tutorial 2 in the CoDiPack
@@ -42,7 +40,6 @@ su2double func(const su2double& x) {
  * SU2 wrapper functions have been substituted for the CoDiPack calls.
  * ---*/
 TEST_CASE("Simple AD Test", "[AD tests]") {
-
   su2double x = 4.0;
 
   AD::StartRecording();
diff --git a/UnitTests/Common/simple_directdiff_test.cpp b/UnitTests/Common/simple_directdiff_test.cpp
index 8cc0772d624..2b97810dd28 100644
--- a/UnitTests/Common/simple_directdiff_test.cpp
+++ b/UnitTests/Common/simple_directdiff_test.cpp
@@ -31,9 +31,7 @@
 
 #include "../../Common/include/basic_types/datatype_structure.hpp"
 
-su2double func(const su2double& x) {
-  return x * x * x;
-}
+su2double func(const su2double& x) { return x * x * x; }
 
 /*---
  * This test case is based off of Tutorial 1 in the CoDiPack
diff --git a/UnitTests/Common/toolboxes/C1DInterpolation_tests.cpp b/UnitTests/Common/toolboxes/C1DInterpolation_tests.cpp
index 379c653d7ae..026763295fb 100644
--- a/UnitTests/Common/toolboxes/C1DInterpolation_tests.cpp
+++ b/UnitTests/Common/toolboxes/C1DInterpolation_tests.cpp
@@ -31,24 +31,23 @@
 #include <vector>
 #include "../../../Common/include/toolboxes/C1DInterpolation.hpp"
 
-su2double myPoly(su2double x) { return 1 + x*(-1 + x*(-1 + x)); }
+su2double myPoly(su2double x) { return 1 + x * (-1 + x * (-1 + x)); }
 
 TEST_CASE("C1DInterpolation", "[Toolboxes]") {
-
   std::vector<su2double> x{{-1.5, -1.0, -0.8, -0.6, -0.4, -0.2, 0, 0.2, 0.4, 0.6, 0.8, 1.0, 1.2, 1.4, 2.0}}, y;
 
   for (auto v : x) y.push_back(myPoly(v));
 
   /*--- piece-wise linear ---*/
-  CLinearInterpolation L(x,y);
+  CLinearInterpolation L(x, y);
 
   /*--- natural spline ---*/
-  CCubicSpline S0(x,y);
+  CCubicSpline S0(x, y);
 
   /*--- analytical end conditions ---*/
-  CCubicSpline S1(x,y, CCubicSpline::SECOND, -11.0, CCubicSpline::FIRST, 7.0);
+  CCubicSpline S1(x, y, CCubicSpline::SECOND, -11.0, CCubicSpline::FIRST, 7.0);
 
-  CCubicSpline S2(x,y, CCubicSpline::FIRST, 8.75, CCubicSpline::SECOND, 10.0);
+  CCubicSpline S2(x, y, CCubicSpline::FIRST, 8.75, CCubicSpline::SECOND, 10.0);
 
   /*--- at the knots ---*/
   for (auto v : x) {
@@ -59,7 +58,7 @@ TEST_CASE("C1DInterpolation", "[Toolboxes]") {
   }
 
   /*--- away from the knots ---*/
-  for (auto& v : x) v = std::min(v+0.1, 2.0);
+  for (auto& v : x) v = std::min(v + 0.1, 2.0);
 
   for (auto v : x) {
     auto ref = myPoly(v);
@@ -69,8 +68,7 @@ TEST_CASE("C1DInterpolation", "[Toolboxes]") {
   }
 
   /*--- Checks that intervals are mapped correctly ---*/
-  for (size_t i = 1; i < x.size()-2; ++i) {
-    CHECK(L(x[i]) == Approx(0.5*(y[i]+y[i+1])));
+  for (size_t i = 1; i < x.size() - 2; ++i) {
+    CHECK(L(x[i]) == Approx(0.5 * (y[i] + y[i + 1])));
   }
 }
-
diff --git a/UnitTests/Common/toolboxes/CQuasiNewtonInvLeastSquares_tests.cpp b/UnitTests/Common/toolboxes/CQuasiNewtonInvLeastSquares_tests.cpp
index d27e55cfd20..2d336ce7db9 100644
--- a/UnitTests/Common/toolboxes/CQuasiNewtonInvLeastSquares_tests.cpp
+++ b/UnitTests/Common/toolboxes/CQuasiNewtonInvLeastSquares_tests.cpp
@@ -33,48 +33,40 @@
 
 struct Problem {
   static constexpr int N = 4;
-  const passivedouble coeffs[N][N] = {{0.5, -0.7, 0.2, 3.0},
-                                      {1.0, -0.2, -0.6, 0.0},
-                                      {0.1, 0.2, 3.14, -1.0},
-                                      {-1.0, -0.4, 0.0, 1.6}};
+  const passivedouble coeffs[N][N] = {
+      {0.5, -0.7, 0.2, 3.0}, {1.0, -0.2, -0.6, 0.0}, {0.1, 0.2, 3.14, -1.0}, {-1.0, -0.4, 0.0, 1.6}};
   /*--- Row sum, sol should be {1.0}. ---*/
   const passivedouble rhs[N] = {3.0, 0.2, 2.44, 0.2};
   passivedouble sol[N] = {0.0};
 
-  template<class T>
+  template <class T>
   void iterate(const T& x) {
-    for(int i=0; i<N; ++i) {
-      sol[i] = x(i,0) + rhs[i];
-      for(int j=0; j<N; ++j)
-        sol[i] -= coeffs[i][j] * x(j,0);
+    for (int i = 0; i < N; ++i) {
+      sol[i] = x(i, 0) + rhs[i];
+      for (int j = 0; j < N; ++j) sol[i] -= coeffs[i][j] * x(j, 0);
     }
   }
 };
 
-template<class P, class Q>
+template <class P, class Q>
 void iterate(P& p, Q& q) {
   p.iterate(q);
-  for(int i=0; i<P::N; ++i)
-    q.FPresult(i,0) = p.sol[i];
+  for (int i = 0; i < P::N; ++i) q.FPresult(i, 0) = p.sol[i];
   q.compute();
 }
 
 TEST_CASE("QN-ILS", "[Toolboxes]") {
   Problem p;
-  CQuasiNewtonInvLeastSquares<passivedouble> qnils(Problem::N+1, Problem::N, 1);
+  CQuasiNewtonInvLeastSquares<passivedouble> qnils(Problem::N + 1, Problem::N, 1);
 
   /*--- Solve ---*/
-  for(int i=0; i<=Problem::N; ++i)
-    iterate(p, qnils);
+  for (int i = 0; i <= Problem::N; ++i) iterate(p, qnils);
 
   /*--- Check we solved in N+1 iterations. ---*/
-  for(int i=0; i<Problem::N; ++i)
-    CHECK(qnils(i,0) == Approx(1.0));
+  for (int i = 0; i < Problem::N; ++i) CHECK(qnils(i, 0) == Approx(1.0));
 
   /*--- Check we don't break a converged problem. ---*/
   iterate(p, qnils);
 
-  for(int i=0; i<Problem::N; ++i)
-    CHECK(qnils(i,0) == Approx(1.0));
+  for (int i = 0; i < Problem::N; ++i) CHECK(qnils(i, 0) == Approx(1.0));
 }
-
diff --git a/UnitTests/Common/toolboxes/ndflattener_tests.cpp b/UnitTests/Common/toolboxes/ndflattener_tests.cpp
index 7393443db59..25d2e85d4e8 100644
--- a/UnitTests/Common/toolboxes/ndflattener_tests.cpp
+++ b/UnitTests/Common/toolboxes/ndflattener_tests.cpp
@@ -28,24 +28,24 @@
 #include "catch.hpp"
 #include "../../Common/include/toolboxes/ndflattener.hpp"
 
-TEST_CASE("NdFlattener Test", "[NdFlattener]"){
-
-  int rank_; SU2_MPI::Comm_rank(SU2_MPI::GetComm(), &rank_);
-  int size_; SU2_MPI::Comm_size(SU2_MPI::GetComm(), &size_);
+TEST_CASE("NdFlattener Test", "[NdFlattener]") {
+  int rank_;
+  SU2_MPI::Comm_rank(SU2_MPI::GetComm(), &rank_);
+  int size_;
+  SU2_MPI::Comm_size(SU2_MPI::GetComm(), &size_);
   const size_t rank = rank_, size = size_;
 
   /*-- Provide non-flat array --*/
   su2double** A = new su2double*[2];
-  A[0] = new su2double[2]; A[0][0] = 0.0; A[0][1] = 1.0;
-  A[1] = new su2double[3+rank];
-  for(size_t i=0; i<3+rank; i++)
-    A[1][i] = 2.0 + rank + i;
+  A[0] = new su2double[2];
+  A[0][0] = 0.0;
+  A[0][1] = 1.0;
+  A[1] = new su2double[3 + rank];
+  for (size_t i = 0; i < 3 + rank; i++) A[1][i] = 2.0 + rank + i;
 
   /*-- Accessor --*/
-  auto f = std::make_pair( (size_t)2,  [rank,A](int i) {
-    return std::make_pair( (size_t)(i==0?2:(3+rank)), [rank,A,i](int j){
-      return  A[i][j];
-    });
+  auto f = std::make_pair((size_t)2, [rank, A](int i) {
+    return std::make_pair((size_t)(i == 0 ? 2 : (3 + rank)), [rank, A, i](int j) { return A[i][j]; });
   });
 
   /*-- Read into flattening structure --*/
@@ -56,12 +56,12 @@ TEST_CASE("NdFlattener Test", "[NdFlattener]"){
   A[0][0] = 0.5;
 
   /*-- Check structure --*/
-  REQUIRE( nd2.size() == 2 );
-  REQUIRE( nd2[0][0] == 0.0 );
-  REQUIRE( nd2[0][1] == 1.0 );
-  REQUIRE( nd2[1].size() == 3 + rank );
-  for(size_t i=0; i<3+rank; i++){
-    REQUIRE( nd2[1][i] == 2.0 + rank + i );
+  REQUIRE(nd2.size() == 2);
+  REQUIRE(nd2[0][0] == 0.0);
+  REQUIRE(nd2[0][1] == 1.0);
+  REQUIRE(nd2[1].size() == 3 + rank);
+  for (size_t i = 0; i < 3 + rank; i++) {
+    REQUIRE(nd2[1][i] == 2.0 + rank + i);
   }
 
   /*-- Modify structure. --*/
@@ -72,70 +72,68 @@ TEST_CASE("NdFlattener Test", "[NdFlattener]"){
   NdFlattener<3> nd3(Nd_MPI_Environment(), nd2);
 
   /*-- Check gathered structure, non-const look-up. --*/
-  REQUIRE( nd3.size() == size );
-  for(size_t r=0; r<size; r++){
-    REQUIRE( nd3[r].size() == 2 );
-    REQUIRE( nd3[r][0][0] == 0.7 );
-    REQUIRE( nd3[r][0][1] == 1.7 );
-    REQUIRE( nd3[r][1].size() == 3 + r );
-    for(size_t i=0; i<3+r; i++){
-      REQUIRE( nd3[r][1][i] == 2.0 + r + i );
+  REQUIRE(nd3.size() == size);
+  for (size_t r = 0; r < size; r++) {
+    REQUIRE(nd3[r].size() == 2);
+    REQUIRE(nd3[r][0][0] == 0.7);
+    REQUIRE(nd3[r][0][1] == 1.7);
+    REQUIRE(nd3[r][1].size() == 3 + r);
+    for (size_t i = 0; i < 3 + r; i++) {
+      REQUIRE(nd3[r][1][i] == 2.0 + r + i);
     }
   }
 
   /*-- Check gathered structure, const look-up. --*/
   const NdFlattener<3>& nd3_const = nd3;
-  REQUIRE( nd3_const.size() == size );
-  for(size_t r=0; r<size; r++){
-    REQUIRE( nd3_const[r].size() == 2 );
-    REQUIRE( nd3_const[r][0][0] == 0.7 );
-    REQUIRE( nd3_const[r][0][1] == 1.7 );
-    REQUIRE( nd3_const[r][1].size() == 3 + r );
-    for(size_t i=0; i<3+r; i++){
-      REQUIRE( nd3_const[r][1][i] == 2.0 + r + i );
+  REQUIRE(nd3_const.size() == size);
+  for (size_t r = 0; r < size; r++) {
+    REQUIRE(nd3_const[r].size() == 2);
+    REQUIRE(nd3_const[r][0][0] == 0.7);
+    REQUIRE(nd3_const[r][0][1] == 1.7);
+    REQUIRE(nd3_const[r][1].size() == 3 + r);
+    for (size_t i = 0; i < 3 + r; i++) {
+      REQUIRE(nd3_const[r][1][i] == 2.0 + r + i);
     }
   }
 
-
   /*-- Reread modified A and check again. --*/
   nd2.initialize_or_refresh(f);
   nd3.refresh(Nd_MPI_Environment(), nd2);
-  REQUIRE( nd3.size() == size );
-  for(size_t r=0; r<size; r++){
-    REQUIRE( nd3[r].size() == 2 );
-    REQUIRE( nd3[r][0][0] == 0.5 );
-    REQUIRE( nd3[r][0][1] == 1.0 );
-    REQUIRE( nd3[r][1].size() == 3 + r );
-    for(size_t i=0; i<3+r; i++){
-      REQUIRE( nd3[r][1][i] == 2.0 + r + i );
+  REQUIRE(nd3.size() == size);
+  for (size_t r = 0; r < size; r++) {
+    REQUIRE(nd3[r].size() == 2);
+    REQUIRE(nd3[r][0][0] == 0.5);
+    REQUIRE(nd3[r][0][1] == 1.0);
+    REQUIRE(nd3[r][1].size() == 3 + r);
+    for (size_t i = 0; i < 3 + r; i++) {
+      REQUIRE(nd3[r][1][i] == 2.0 + r + i);
     }
   }
 
   /*-- Check 1D functionality, communicating unsigned long data. --*/
-  NdFlattener<1,unsigned long> a1(
-    std::make_pair( (size_t)(3+rank),  [rank,A](int i) {
-      return (unsigned long)(2+rank+i);
-    })
-  );
+  NdFlattener<1, unsigned long> a1(
+      std::make_pair((size_t)(3 + rank), [rank, A](int i) { return (unsigned long)(2 + rank + i); }));
   const NdFlattener<1, unsigned long>& a1_const = a1;
-  REQUIRE( a1.size() == 3 + rank );
-  for(size_t i=0; i<3+rank; i++){
-    REQUIRE( a1[i] == 2 + rank + i );
-    REQUIRE( a1_const[i] == 2 + rank + i );
+  REQUIRE(a1.size() == 3 + rank);
+  for (size_t i = 0; i < 3 + rank; i++) {
+    REQUIRE(a1[i] == 2 + rank + i);
+    REQUIRE(a1_const[i] == 2 + rank + i);
   }
   a1[0] = 1;
-  REQUIRE( a1_const.data()[0] == 1 );
+  REQUIRE(a1_const.data()[0] == 1);
   a1.data()[0] = 2 + rank;
-  REQUIRE( a1_const[0] == 2 + rank );
+  REQUIRE(a1_const[0] == 2 + rank);
   const NdFlattener<2, unsigned long> a2_const(Nd_MPI_Environment(MPI_UNSIGNED_LONG), a1);
-  REQUIRE( a2_const.size() == size );
-  for(size_t r=0; r<size; r++){
-    REQUIRE( a2_const[r].size() == 3 + r );
-    for(size_t i=0; i<3+r; i++){
-      REQUIRE( a2_const[r][i] == 2 + r + i );
+  REQUIRE(a2_const.size() == size);
+  for (size_t r = 0; r < size; r++) {
+    REQUIRE(a2_const[r].size() == 3 + r);
+    for (size_t i = 0; i < 3 + r; i++) {
+      REQUIRE(a2_const[r][i] == 2 + r + i);
     }
   }
 
   /*-- free stuff --*/
-  delete[] A[0]; delete[] A[1]; delete[] A;
+  delete[] A[0];
+  delete[] A[1];
+  delete[] A;
 }
diff --git a/UnitTests/Common/vectorization.cpp b/UnitTests/Common/vectorization.cpp
index b061caedcbd..22fa454f961 100644
--- a/UnitTests/Common/vectorization.cpp
+++ b/UnitTests/Common/vectorization.cpp
@@ -30,27 +30,25 @@
 
 using namespace std;
 
-template<class T, class U>
+template <class T, class U>
 struct arithmeticFun {
-  static T f(T A, T B, T C, T D, U x, U y) {
-    return pow( (A+B-x*C)/y + pow(A*x-C/D, y), D);
-  }
+  static T f(T A, T B, T C, T D, U x, U y) { return pow((A + B - x * C) / y + pow(A * x - C / D, y), D); }
 };
 
-template<class T, class U>
+template <class T, class U>
 struct logicFun {
   static T f(T A, T B, T C, T D, U x, U y) {
     // (B < A || B >= C) && ...
-    return fmax(B < A, B >= fmin(C,-D)) * (abs(A) == abs(x)) * (abs(C) != abs(y));
+    return fmax(B < A, B >= fmin(C, -D)) * (abs(A) == abs(x)) * (abs(C) != abs(y));
   }
 };
 
-template<template<class,class> class Fun, class T, class U>
+template <template <class, class> class Fun, class T, class U>
 void computeAndCheck(T A, T B, T C, T D, U x, U y) {
-  const auto result = Fun<T,U>::f(A, B, C, D, x, y);
+  const auto result = Fun<T, U>::f(A, B, C, D, x, y);
 
-  for (size_t k=0; k<T::Size; ++k) {
-    CHECK(result[k] == Fun<U,U>::f(A[k], B[k], C[k], D[k], x, y));
+  for (size_t k = 0; k < T::Size; ++k) {
+    CHECK(result[k] == Fun<U, U>::f(A[k], B[k], C[k], D[k], x, y));
   }
 }
 
@@ -61,11 +59,11 @@ TEST_CASE("SIMD INT", "[Vectorization]") {
   Int A = 1, B = -3, C = 5, D = 2;
   int x = -1, y = 2;
 
-  computeAndCheck<arithmeticFun>(A, B, C, D, x ,y);
-  computeAndCheck<logicFun>(A, B, C, D, x ,y);
+  computeAndCheck<arithmeticFun>(A, B, C, D, x, y);
+  computeAndCheck<logicFun>(A, B, C, D, x, y);
 
-  Int t = sign(A)+sign(B+C);
-  for (size_t k=0; k<Int::Size; ++k) {
+  Int t = sign(A) + sign(B + C);
+  for (size_t k = 0; k < Int::Size; ++k) {
     CHECK(t[k] == 2);
   }
 }
@@ -77,12 +75,11 @@ TEST_CASE("SIMD DOUBLE", "[Vectorization]") {
   Double A = 1, B = -3, C = 5, D = 2;
   double x = -1, y = 2;
 
-  computeAndCheck<arithmeticFun>(A, B, C, D, x ,y);
-  computeAndCheck<logicFun>(A, B, C, D, x ,y);
+  computeAndCheck<arithmeticFun>(A, B, C, D, x, y);
+  computeAndCheck<logicFun>(A, B, C, D, x, y);
 
-  Double t = sqrt(pow(B,2)*C + D*y + A+x);
-  for (size_t k=0; k<Double::Size; ++k) {
+  Double t = sqrt(pow(B, 2) * C + D * y + A + x);
+  for (size_t k = 0; k < Double::Size; ++k) {
     CHECK(t[k] == 7);
   }
 }
-
diff --git a/UnitTests/SU2_CFD/gradients.cpp b/UnitTests/SU2_CFD/gradients.cpp
index 1f3b5ab0499..0b0beaaf24e 100644
--- a/UnitTests/SU2_CFD/gradients.cpp
+++ b/UnitTests/SU2_CFD/gradients.cpp
@@ -98,7 +98,6 @@ struct GradientTestBase {
 };
 
 struct LinearFunction : public GradientTestBase {
-
   const unsigned long nVar = 1;
   const su2double constant = -1.0;
   const su2double slope[3] = {1.0, 2.0, 3.0};
@@ -106,7 +105,7 @@ struct LinearFunction : public GradientTestBase {
   /*!
    * \brief Return manufactured value.
    */
-  su2double operator() (unsigned long iPoint, unsigned long) const {
+  su2double operator()(unsigned long iPoint, unsigned long) const {
     const auto coord = geometry->nodes->GetCoord(iPoint);
     return constant + GeometryToolbox::DotProduct(geometry->GetnDim(), slope, coord);
   }
@@ -114,52 +113,44 @@ struct LinearFunction : public GradientTestBase {
   /*!
    * \brief Return reference value.
    */
-  su2double grad(unsigned long, unsigned long, unsigned long iDim) const {
-    return slope[iDim];
-  }
+  su2double grad(unsigned long, unsigned long, unsigned long iDim) const { return slope[iDim]; }
 };
 
-template<class T, class U>
+template <class T, class U>
 void check(const T& ref, const U& calc, su2double tol = 1e-9) {
   su2double err = 0.0;
   for (auto iPoint = 0ul; iPoint < calc.length(); ++iPoint) {
     for (auto iVar = 0ul; iVar < calc.rows(); ++iVar)
       for (auto iDim = 0ul; iDim < calc.cols(); ++iDim)
-        err = max(err, abs(calc(iPoint,iVar,iDim) - ref.grad(iPoint,iVar,iDim)));
+        err = max(err, abs(calc(iPoint, iVar, iDim) - ref.grad(iPoint, iVar, iDim)));
   }
   CHECK(err < tol);
 }
 
-template<class TestField>
+template <class TestField>
 void testGreenGauss() {
   TestField field;
   C3DDoubleMatrix gradient(field.geometry->GetnPoint(), field.nVar, field.geometry->GetnDim());
 
-  computeGradientsGreenGauss(nullptr, SOLUTION, PERIODIC_NONE, *field.geometry.get(),
-                             *field.config.get(), field, 0, field.nVar, gradient);
+  computeGradientsGreenGauss(nullptr, SOLUTION, PERIODIC_NONE, *field.geometry.get(), *field.config.get(), field, 0,
+                             field.nVar, gradient);
   check(field, gradient);
 }
 
-template<class TestField>
+template <class TestField>
 void testLeastSquares(bool weighted) {
   TestField field;
   const auto nDim = field.geometry->GetnDim();
   C3DDoubleMatrix R(field.geometry->GetnPoint(), nDim, nDim);
   C3DDoubleMatrix gradient(field.geometry->GetnPoint(), field.nVar, nDim);
 
-  computeGradientsLeastSquares(nullptr, SOLUTION, PERIODIC_NONE, *field.geometry.get(),
-                               *field.config.get(), weighted, field, 0, field.nVar, gradient, R);
+  computeGradientsLeastSquares(nullptr, SOLUTION, PERIODIC_NONE, *field.geometry.get(), *field.config.get(), weighted,
+                               field, 0, field.nVar, gradient, R);
   check(field, gradient);
 }
 
-TEST_CASE("GG", "[Gradients]") {
-  testGreenGauss<LinearFunction>();
-}
+TEST_CASE("GG", "[Gradients]") { testGreenGauss<LinearFunction>(); }
 
-TEST_CASE("LS", "[Gradients]") {
-  testLeastSquares<LinearFunction>(false);
-}
+TEST_CASE("LS", "[Gradients]") { testLeastSquares<LinearFunction>(false); }
 
-TEST_CASE("WLS", "[Gradients]") {
-  testLeastSquares<LinearFunction>(true);
-}
+TEST_CASE("WLS", "[Gradients]") { testLeastSquares<LinearFunction>(true); }
diff --git a/UnitTests/SU2_CFD/numerics/CNumerics_tests.cpp b/UnitTests/SU2_CFD/numerics/CNumerics_tests.cpp
index 8287627dc20..0f1110b0c70 100644
--- a/UnitTests/SU2_CFD/numerics/CNumerics_tests.cpp
+++ b/UnitTests/SU2_CFD/numerics/CNumerics_tests.cpp
@@ -30,11 +30,11 @@
 #include "../../../SU2_CFD/include/numerics/CNumerics.hpp"
 
 TEST_CASE("NTS blending has a minimum of 0.05", "[Upwind/central blending]") {
-
   std::stringstream config_options;
 
   config_options << "SOLVER= NAVIER_STOKES" << std::endl;
-  config_options << "ROE_LOW_DISSIPATION= " << "NTS" << std::endl;
+  config_options << "ROE_LOW_DISSIPATION= "
+                 << "NTS" << std::endl;
   config_options << "REYNOLDS_NUMBER= 5" << std::endl;
 
   /*--- Setup ---*/
@@ -49,11 +49,8 @@ TEST_CASE("NTS blending has a minimum of 0.05", "[Upwind/central blending]") {
   /*--- Test ---*/
 
   CNumerics numerics;
-  const su2double dissipation_ij = numerics.GetRoe_Dissipation(dissipation_i,
-                                                               dissipation_j,
-                                                               sensor_i,
-                                                               sensor_j,
-                                                               config);
+  const su2double dissipation_ij =
+      numerics.GetRoe_Dissipation(dissipation_i, dissipation_j, sensor_i, sensor_j, config);
 
   REQUIRE(dissipation_ij >= 0.05);
 
@@ -61,4 +58,3 @@ TEST_CASE("NTS blending has a minimum of 0.05", "[Upwind/central blending]") {
 
   delete config;
 }
-
diff --git a/UnitTests/SU2_CFD/windowing.cpp b/UnitTests/SU2_CFD/windowing.cpp
index c711c6f74db..1cb8e3f21d4 100644
--- a/UnitTests/SU2_CFD/windowing.cpp
+++ b/UnitTests/SU2_CFD/windowing.cpp
@@ -37,8 +37,8 @@ struct CWindowingTest {
   static constexpr size_t MAX_INNER_ITERATIONS = 5;
 
   /*!
-  * \brief Calculates sample value at the specified time-step. Simple SIN function.
-  */
+   * \brief Calculates sample value at the specified time-step. Simple SIN function.
+   */
   static su2double GetSampleAtIteration(unsigned long currentTimeStep) {
     return 0.5 * sin(0.1 * currentTimeStep + 2) + 1.;
   }
@@ -47,10 +47,10 @@ struct CWindowingTest {
    * \brief Perform averaging over simulated inner and outer solver iterations.
    */
   static su2double calcAverage(WINDOW_FUNCTION win, unsigned long nIterations, unsigned long startIteration) {
-    CWindowedAverage avg{win}; // Create averaging object with the specified window.
+    CWindowedAverage avg{win};  // Create averaging object with the specified window.
     su2double previousSample = 0.;
     su2double currentSample = 0.;
-    su2double input = 0.;   // Value that is specified as actual input to the addValue function.
+    su2double input = 0.;  // Value that is specified as actual input to the addValue function.
     su2double weightPrevious = 0.;
     su2double weightCurrent = 0.;
     // Simulate solver time-steps
diff --git a/UnitTests/UnitQuadTestCase.hpp b/UnitTests/UnitQuadTestCase.hpp
index 4c78fec4e18..9d582291b99 100644
--- a/UnitTests/UnitQuadTestCase.hpp
+++ b/UnitTests/UnitQuadTestCase.hpp
@@ -76,8 +76,7 @@ struct UnitQuadTestCase {
    */
   void InitSolver() {
     cout.rdbuf(nullptr);
-    solver = CSolverFactory::CreateSolverContainer(config.get()->GetKind_Solver(),
-                                                   config.get(), geometry.get(), 0);
+    solver = CSolverFactory::CreateSolverContainer(config.get()->GetKind_Solver(), config.get(), geometry.get(), 0);
     cout.rdbuf(orig_buf);
   }
 
@@ -112,8 +111,7 @@ struct UnitQuadTestCase {
    * \brief Desctructor
    */
   ~UnitQuadTestCase() {
-    if (solver != nullptr)
-      delete solver[FLOW_SOL];
+    if (solver != nullptr) delete solver[FLOW_SOL];
     delete[] solver;
   }
 };
diff --git a/UnitTests/test_driver.cpp b/UnitTests/test_driver.cpp
index b38ba907c8f..a8ffcd3c8ce 100644
--- a/UnitTests/test_driver.cpp
+++ b/UnitTests/test_driver.cpp
@@ -34,8 +34,7 @@
 #include "../../../Common/include/parallelization/mpi_structure.hpp"
 #include "../../../Common/include/option_structure.hpp"
 
-int main(int argc, char *argv[]) {
-
+int main(int argc, char* argv[]) {
   /*--- Startup MPI, if supported ---*/
 #if defined(HAVE_OMP) && defined(HAVE_MPI)
   int provided;
diff --git a/docker/build/Dockerfile b/docker/build/Dockerfile
index 0061deb97d9..75dad6d1595 100644
--- a/docker/build/Dockerfile
+++ b/docker/build/Dockerfile
@@ -16,7 +16,7 @@ RUN apt-get update && apt-get install -y \
  && rm -rf /var/lib/apt/lists/* \
  && update-alternatives --install /usr/bin/python python /usr/bin/python3 10 \
  && /usr/sbin/update-ccache-symlinks \
- && echo 'export PATH="/usr/lib/ccache:$PATH"' | tee -a ~/.bashrc 
+ && echo 'export PATH="/usr/lib/ccache:$PATH"' | tee -a ~/.bashrc
 
 # Copies your code file from your action repository to the filesystem path `/` of the container
 COPY compileSU2.sh /compileSU2.sh
diff --git a/docker/build/compileSU2.sh b/docker/build/compileSU2.sh
index 6e6f32f2606..735e4f1e9de 100755
--- a/docker/build/compileSU2.sh
+++ b/docker/build/compileSU2.sh
@@ -1,14 +1,14 @@
 #!/bin/sh -l
 
 echo "SU2 v7 Docker Compilation Container"
-usage="$(basename "$0") [-h] [-f build_flags] [-b branch_name] 
+usage="$(basename "$0") [-h] [-f build_flags] [-b branch_name]
 where:
     -h  show this help text
     -f  meson build flags (ignored if a directory \"docker_build\" is found at /src/SU2).
     -b  branch name (if not given, existing SU2 directory must be mounted in /src/SU2).
 
 Compiled binaries can be found at /install/. Mount that directory for access.
-Note: If you specify a working directory using the --workdir option for docker, 
+Note: If you specify a working directory using the --workdir option for docker,
       append this directory to all paths above (e.g. use --workdir=/tmp if running in user mode)."
 
 flags=""
@@ -24,7 +24,7 @@ if [ "$#" -ne 0 ]; then
             -f)
                     flags=$2
                     shift 2
-                ;;  
+                ;;
             -b)
                     branch=$2
                     shift 2
@@ -67,5 +67,3 @@ else
 fi
 
 ./ninja -C docker_build install
-
-
diff --git a/docker/test/runTests.sh b/docker/test/runTests.sh
index 66227871ccb..9cb55113c99 100755
--- a/docker/test/runTests.sh
+++ b/docker/test/runTests.sh
@@ -6,7 +6,7 @@
 # $4 : Path of the installation directory
 # $5 : Test script to execute
 
-usage="$(basename "$0") [-h] [-t tutorial_branch] [-b su2_branch] [-c testcases_branch] [-s test_script] 
+usage="$(basename "$0") [-h] [-t tutorial_branch] [-b su2_branch] [-c testcases_branch] [-s test_script]
 where:
     -h  show this help text
     -t  branch of su2code/Tutorials repo
@@ -19,7 +19,7 @@ where:
 
 Compiled binaries must be mounted at /install/ !
 
-Note: If you specify a working directory using the --workdir option for docker, 
+Note: If you specify a working directory using the --workdir option for docker,
       append this directory to all paths above (e.g. use --workdir=/tmp if running in user mode)."
 
 su2branch=""
@@ -122,4 +122,3 @@ else
     echo "Tests failed"
     exit 1
 fi
-
diff --git a/doxyfile b/doxyfile
index 89643a0cc9e..b249d12d1b1 100755
--- a/doxyfile
+++ b/doxyfile
@@ -162,7 +162,7 @@ FULL_PATH_NAMES        = YES
 # will be relative from the directory where doxygen is started.
 # This tag requires that the tag FULL_PATH_NAMES is set to YES.
 
-STRIP_FROM_PATH        = 
+STRIP_FROM_PATH        =
 
 # The STRIP_FROM_INC_PATH tag can be used to strip a user-defined part of the
 # path mentioned in the documentation of a class, which tells the reader which
@@ -833,7 +833,7 @@ RECURSIVE              = YES
 # Note that relative paths are relative to the directory from which doxygen is
 # run.
 
-EXCLUDE                = 
+EXCLUDE                =
 
 # The EXCLUDE_SYMLINKS tag can be used to select whether or not files or
 # directories that are symbolic links (a Unix file system feature) are excluded
diff --git a/meson.py b/meson.py
index e8601a8e599..e58b9fa3b09 100755
--- a/meson.py
+++ b/meson.py
@@ -26,24 +26,35 @@
 # License along with SU2. If not, see <http://www.gnu.org/licenses/>.
 
 import sys, os
+
 sys.path.append(sys.path[0])
 import preconfigure
 
 
-if __name__ == '__main__':
-  if sys.version_info[0] < 3:
-    raise Exception("Script must be run using Python 3")
-
-  # Preconfigure
-  preconfigure.run(own_meson = True)
-
-  # Add paths for meson and ninja to environment
-  os.environ["NINJA"] = sys.path[0] + os.path.sep + "ninja"
-  if os.name == 'nt':
-    os.environ["NINJA"] = os.environ["NINJA"] + '.exe'
-  if os.path.exists(sys.path[0] + os.path.sep + 'externals' + os.path.sep + 'meson' + os.path.sep + 'mesonbuild'):
-    sys.path.insert(0, str(sys.path[0] + os.path.sep + 'externals' +os.path.sep + 'meson'))
-
-  from mesonbuild import mesonmain
-
-  sys.exit(mesonmain.main())
+if __name__ == "__main__":
+    if sys.version_info[0] < 3:
+        raise Exception("Script must be run using Python 3")
+
+    # Preconfigure
+    preconfigure.run(own_meson=True)
+
+    # Add paths for meson and ninja to environment
+    os.environ["NINJA"] = sys.path[0] + os.path.sep + "ninja"
+    if os.name == "nt":
+        os.environ["NINJA"] = os.environ["NINJA"] + ".exe"
+    if os.path.exists(
+        sys.path[0]
+        + os.path.sep
+        + "externals"
+        + os.path.sep
+        + "meson"
+        + os.path.sep
+        + "mesonbuild"
+    ):
+        sys.path.insert(
+            0, str(sys.path[0] + os.path.sep + "externals" + os.path.sep + "meson")
+        )
+
+    from mesonbuild import mesonmain
+
+    sys.exit(mesonmain.main())
diff --git a/meson_scripts/check_dir.py b/meson_scripts/check_dir.py
index bf58d102e92..f67b4ca6532 100644
--- a/meson_scripts/check_dir.py
+++ b/meson_scripts/check_dir.py
@@ -4,11 +4,13 @@
 import sys
 import os
 
-def check_dir(fn: Path): 
-  return os.path.exists(fn)
+
+def check_dir(fn: Path):
+    return os.path.exists(fn)
+
 
 if __name__ == "__main__":
-  p = argparse.ArgumentParser()
-  p.add_argument("path", help="path to check")
-  P = p.parse_args()
-  sys.exit(not check_dir(P.path))
+    p = argparse.ArgumentParser()
+    p.add_argument("path", help="path to check")
+    P = p.parse_args()
+    sys.exit(not check_dir(P.path))
diff --git a/meson_scripts/extract_file.py b/meson_scripts/extract_file.py
index f5d1bcef546..693dc056956 100644
--- a/meson_scripts/extract_file.py
+++ b/meson_scripts/extract_file.py
@@ -1,62 +1,66 @@
 #!/usr/bin/env python3
-from pathlib import Path 
+from pathlib import Path
 import argparse
 import zipfile
 import tarfile
 
-def extract_zip(fn: Path, outpath: Path, overwrite: bool = False): 
-  outpath = Path(outpath).expanduser().resolve() # need .resolve() in case intermediate relative dir doesn’t exist
-  if outpath.is_dir() and not overwrite:
-    return
-  fn = Path(fn).expanduser().resolve()
-  with zipfile.ZipFile(fn) as z:
-    z.extractall(str(outpath))
+
+def extract_zip(fn: Path, outpath: Path, overwrite: bool = False):
+    outpath = (
+        Path(outpath).expanduser().resolve()
+    )  # need .resolve() in case intermediate relative dir doesn’t exist
+    if outpath.is_dir() and not overwrite:
+        return
+    fn = Path(fn).expanduser().resolve()
+    with zipfile.ZipFile(fn) as z:
+        z.extractall(str(outpath))
 
 
 def extract_tar(fn: Path, outpath: Path, overwrite: bool = False):
-  outpath = Path(outpath).expanduser().resolve() # need .resolve() in case intermediate relative dir doesn’t exist
-  print(outpath)
-  if outpath.is_dir() and not overwrite:
-    return
-  fn = Path(fn).expanduser().resolve()
-  if not fn.is_file():
-    raise FileNotFoundError(fn)  # keep this, tarfile gives confusing error
-  with tarfile.open(fn) as z:
-    
-    import os
-    
-    def is_within_directory(directory, target):
-        
-        abs_directory = os.path.abspath(directory)
-        abs_target = os.path.abspath(target)
-    
-        prefix = os.path.commonprefix([abs_directory, abs_target])
-        
-        return prefix == abs_directory
-    
-    def safe_extract(tar, path=".", members=None, *, numeric_owner=False):
-    
-        for member in tar.getmembers():
-            member_path = os.path.join(path, member.name)
-            if not is_within_directory(path, member_path):
-                raise Exception("Attempted Path Traversal in Tar File")
-    
-        tar.extractall(path, members, numeric_owner=numeric_owner) 
-        
-    
-    safe_extract(z, str(outpath))
+    outpath = (
+        Path(outpath).expanduser().resolve()
+    )  # need .resolve() in case intermediate relative dir doesn’t exist
+    print(outpath)
+    if outpath.is_dir() and not overwrite:
+        return
+    fn = Path(fn).expanduser().resolve()
+    if not fn.is_file():
+        raise FileNotFoundError(fn)  # keep this, tarfile gives confusing error
+    with tarfile.open(fn) as z:
+
+        import os
+
+        def is_within_directory(directory, target):
+
+            abs_directory = os.path.abspath(directory)
+            abs_target = os.path.abspath(target)
+
+            prefix = os.path.commonprefix([abs_directory, abs_target])
+
+            return prefix == abs_directory
+
+        def safe_extract(tar, path=".", members=None, *, numeric_owner=False):
+
+            for member in tar.getmembers():
+                member_path = os.path.join(path, member.name)
+                if not is_within_directory(path, member_path):
+                    raise Exception("Attempted Path Traversal in Tar File")
+
+            tar.extractall(path, members, numeric_owner=numeric_owner)
+
+        safe_extract(z, str(outpath))
 
 
 if __name__ == "__main__":
-  p = argparse.ArgumentParser()
-  p.add_argument("infile", help="compressed file to extract")
-  p.add_argument("outpath", help="path to extract into")
-  P = p.parse_args()
-
-  infile = Path(P.infile)
-  if infile.suffix.lower() == ".zip":
-    extract_zip(infile, P.outpath, True)
-  elif infile.suffix.lower() in (".tar", ".gz", ".bz2", ".xz"):
-    extract_tar(infile, P.outpath, True)
-  else:
-    raise ValueError("Not sure how to decompress {}".format(infile))
+    p = argparse.ArgumentParser()
+    p.add_argument("infile", help="compressed file to extract")
+    p.add_argument("outpath", help="path to extract into")
+    P = p.parse_args()
+
+    infile = Path(P.infile)
+    if infile.suffix.lower() == ".zip":
+        extract_zip(infile, P.outpath, True)
+    elif infile.suffix.lower() in (".tar", ".gz", ".bz2", ".xz"):
+        extract_tar(infile, P.outpath, True)
+    else:
+        raise ValueError("Not sure how to decompress {}".format(infile))
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index e6edac57458..3f0b0646a6f 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -28,241 +28,284 @@
 
 import sys, os, subprocess, urllib.request, zipfile, time
 
+
 def remove_file(path, retries=3, sleep=0.1):
-  for i in range(retries):
-    try:
-      os.remove(path)
-    except OSError:
-      time.sleep(sleep)
+    for i in range(retries):
+        try:
+            os.remove(path)
+        except OSError:
+            time.sleep(sleep)
+        else:
+            break
+
+
+def init_submodules(
+    method="auto",
+    own_meson=False,
+    own_codi=True,
+    own_medi=True,
+    own_opdi=True,
+    own_mpp=True,
+    own_cool=True,
+    own_mel=True,
+):
+
+    cur_dir = sys.path[0]
+
+    # This information of the modules is used if projects was not cloned using git
+    # The sha tag must be maintained manually to point to the correct commit
+    sha_version_codi = "427c2dc754a628ad3c9310c766c988ac5ce21bc7"
+    github_repo_codi = "https://github.com/scicompkl/CoDiPack"
+    sha_version_medi = "aafc2d1966ba1233640af737e71c77c1a86183fd"
+    github_repo_medi = "https://github.com/SciCompKL/MeDiPack"
+    sha_version_opdi = "f33b507c24f7448d4cf4df16ab5c53ea254b8774"
+    github_repo_opdi = "https://github.com/SciCompKL/OpDiLib"
+    sha_version_meson = "41c650a040d50e0912d268af7a903a9ce1456dfa"
+    github_repo_meson = "https://github.com/mesonbuild/meson"
+    sha_version_ninja = "52649de2c56b63f42bc59513d51286531c595b44"
+    github_repo_ninja = "https://github.com/ninja-build/ninja"
+    sha_version_mpp = "5ff579f43781cae07411e5ab46291c9971536be6"
+    github_repo_mpp = "https://github.com/mutationpp/Mutationpp"
+    sha_version_coolprop = "0ce42fcf3bb2c373512bc825a4f0c1973a78f307"
+    github_repo_coolprop = "https://github.com/CoolProp/CoolProp"
+    sha_version_mel = "2484cd3258ef800a10e361016cb341834ee7930b"
+    github_repo_mel = "https://github.com/pcarruscag/MEL"
+
+    medi_name = "MeDiPack"
+    codi_name = "CoDiPack"
+    opdi_name = "OpDiLib"
+    meson_name = "meson"
+    ninja_name = "ninja"
+    mpp_name = "Mutationpp"
+    coolprop_name = "CoolProp"
+    mel_name = "MEL"
+    base_path = cur_dir + os.path.sep + "externals" + os.path.sep
+    alt_name_medi = base_path + "medi"
+    alt_name_codi = base_path + "codi"
+    alt_name_opdi = base_path + "opdi"
+    alt_name_meson = base_path + "meson"
+    alt_name_ninja = base_path + "ninja"
+    alt_name_mel = base_path + "mel"
+    alt_name_mpp = cur_dir + os.path.sep + "subprojects" + os.path.sep + "Mutationpp"
+    alt_name_coolprop = cur_dir + os.path.sep + "subprojects" + os.path.sep + "CoolProp"
+
+    if method == "auto":
+        is_git = is_git_directory(cur_dir)
+    elif method == "git":
+        is_git = True
+    elif method == "url":
+        is_git = False
     else:
-      break
-
-
-def init_submodules(method = 'auto',
-                    own_meson = False,
-                    own_codi = True,
-                    own_medi = True,
-                    own_opdi = True,
-                    own_mpp  = True,
-                    own_cool = True,
-                    own_mel  = True):
-
-  cur_dir = sys.path[0]
-
-  # This information of the modules is used if projects was not cloned using git
-  # The sha tag must be maintained manually to point to the correct commit
-  sha_version_codi = '427c2dc754a628ad3c9310c766c988ac5ce21bc7'
-  github_repo_codi = 'https://github.com/scicompkl/CoDiPack'
-  sha_version_medi = 'aafc2d1966ba1233640af737e71c77c1a86183fd'
-  github_repo_medi = 'https://github.com/SciCompKL/MeDiPack'
-  sha_version_opdi = 'f33b507c24f7448d4cf4df16ab5c53ea254b8774'
-  github_repo_opdi = 'https://github.com/SciCompKL/OpDiLib'
-  sha_version_meson = '41c650a040d50e0912d268af7a903a9ce1456dfa'
-  github_repo_meson = 'https://github.com/mesonbuild/meson'
-  sha_version_ninja = '52649de2c56b63f42bc59513d51286531c595b44'
-  github_repo_ninja = 'https://github.com/ninja-build/ninja'
-  sha_version_mpp = '5ff579f43781cae07411e5ab46291c9971536be6'
-  github_repo_mpp = 'https://github.com/mutationpp/Mutationpp'
-  sha_version_coolprop = '0ce42fcf3bb2c373512bc825a4f0c1973a78f307'
-  github_repo_coolprop = 'https://github.com/CoolProp/CoolProp'
-  sha_version_mel = '2484cd3258ef800a10e361016cb341834ee7930b'
-  github_repo_mel = 'https://github.com/pcarruscag/MEL'
-
-  medi_name = 'MeDiPack'
-  codi_name = 'CoDiPack'
-  opdi_name = 'OpDiLib'
-  meson_name = 'meson'
-  ninja_name= 'ninja'
-  mpp_name= 'Mutationpp'
-  coolprop_name= 'CoolProp'
-  mel_name = 'MEL'
-  base_path = cur_dir + os.path.sep + 'externals' + os.path.sep
-  alt_name_medi = base_path + 'medi'
-  alt_name_codi = base_path + 'codi'
-  alt_name_opdi = base_path + 'opdi'
-  alt_name_meson = base_path + 'meson'
-  alt_name_ninja = base_path + 'ninja'
-  alt_name_mel = base_path + 'mel'
-  alt_name_mpp = cur_dir + os.path.sep + 'subprojects' + os.path.sep  + 'Mutationpp'
-  alt_name_coolprop = cur_dir + os.path.sep + 'subprojects' + os.path.sep + 'CoolProp'
-
-  if method == 'auto':
-    is_git = is_git_directory(cur_dir)
-  elif method == 'git':
-    is_git = True
-  elif method == 'url':
-    is_git = False
-  else:
-    print('Invalid method')
-    sys.exit(1)
-
-  # If directory was cloned using git, use submodule feature
-  # to check and initialize submodules if necessary
-  if is_git:
-    if own_codi:
-      submodule_status(alt_name_codi, sha_version_codi)
-    if own_medi:
-      submodule_status(alt_name_medi, sha_version_medi)
-    if own_opdi:
-      submodule_status(alt_name_opdi, sha_version_opdi)
-    if own_meson:
-      submodule_status(alt_name_meson, sha_version_meson)
-      submodule_status(alt_name_ninja, sha_version_ninja)
-    if own_mpp:
-      submodule_status(alt_name_mpp, sha_version_mpp)
-    if own_cool:
-      submodule_status(alt_name_coolprop, sha_version_coolprop)
-    if own_mel:
-      submodule_status(alt_name_mel, sha_version_mel)
-  # Otherwise download the zip file from git
-  else:
-    if own_codi:
-      download_module(codi_name, alt_name_codi, github_repo_codi, sha_version_codi)
-    if own_medi:
-      download_module(medi_name, alt_name_medi, github_repo_medi, sha_version_medi)
-    if own_opdi:
-      download_module(opdi_name, alt_name_opdi, github_repo_opdi, sha_version_opdi)
-    if own_meson:
-      download_module(meson_name, alt_name_meson, github_repo_meson, sha_version_meson)
-      download_module(ninja_name, alt_name_ninja, github_repo_ninja, sha_version_ninja)
-    if own_mpp:
-      download_module(mpp_name, alt_name_mpp, github_repo_mpp, sha_version_mpp)
-    if own_cool:
-      download_module(coolprop_name, alt_name_coolprop, github_repo_coolprop, sha_version_coolprop)
-    if own_mel:
-      download_module(mel_name, alt_name_mel, github_repo_mel, sha_version_mel)
-
-
-def is_git_directory(path = '.'):
-  try:
-     p = subprocess.call(["git", "branch"], stderr=subprocess.STDOUT, stdout=open(os.devnull, 'w'), cwd=path)
-  except FileNotFoundError:
-     print("git command not found. Using fall-back method to init submodules")
-     return False
-  except subprocess.CalledProcessError:
-     print("Directory was not cloned using git. Using fall-back method to init submodules")
-     return False
-  return p == 0
+        print("Invalid method")
+        sys.exit(1)
+
+    # If directory was cloned using git, use submodule feature
+    # to check and initialize submodules if necessary
+    if is_git:
+        if own_codi:
+            submodule_status(alt_name_codi, sha_version_codi)
+        if own_medi:
+            submodule_status(alt_name_medi, sha_version_medi)
+        if own_opdi:
+            submodule_status(alt_name_opdi, sha_version_opdi)
+        if own_meson:
+            submodule_status(alt_name_meson, sha_version_meson)
+            submodule_status(alt_name_ninja, sha_version_ninja)
+        if own_mpp:
+            submodule_status(alt_name_mpp, sha_version_mpp)
+        if own_cool:
+            submodule_status(alt_name_coolprop, sha_version_coolprop)
+        if own_mel:
+            submodule_status(alt_name_mel, sha_version_mel)
+    # Otherwise download the zip file from git
+    else:
+        if own_codi:
+            download_module(
+                codi_name, alt_name_codi, github_repo_codi, sha_version_codi
+            )
+        if own_medi:
+            download_module(
+                medi_name, alt_name_medi, github_repo_medi, sha_version_medi
+            )
+        if own_opdi:
+            download_module(
+                opdi_name, alt_name_opdi, github_repo_opdi, sha_version_opdi
+            )
+        if own_meson:
+            download_module(
+                meson_name, alt_name_meson, github_repo_meson, sha_version_meson
+            )
+            download_module(
+                ninja_name, alt_name_ninja, github_repo_ninja, sha_version_ninja
+            )
+        if own_mpp:
+            download_module(mpp_name, alt_name_mpp, github_repo_mpp, sha_version_mpp)
+        if own_cool:
+            download_module(
+                coolprop_name,
+                alt_name_coolprop,
+                github_repo_coolprop,
+                sha_version_coolprop,
+            )
+        if own_mel:
+            download_module(mel_name, alt_name_mel, github_repo_mel, sha_version_mel)
+
+
+def is_git_directory(path="."):
+    try:
+        p = subprocess.call(
+            ["git", "branch"],
+            stderr=subprocess.STDOUT,
+            stdout=open(os.devnull, "w"),
+            cwd=path,
+        )
+    except FileNotFoundError:
+        print("git command not found. Using fall-back method to init submodules")
+        return False
+    except subprocess.CalledProcessError:
+        print(
+            "Directory was not cloned using git. Using fall-back method to init submodules"
+        )
+        return False
+    return p == 0
+
 
 def submodule_status(path, sha_commit):
-  if not os.path.exists(path + os.path.sep + sha_commit):
-
-    # Check the status of the submodule
-    status = subprocess.run(['git', 'submodule','status', path], stdout=subprocess.PIPE, check = True, cwd = sys.path[0]).stdout.decode('utf-8')
-    # The first character of the output indicates the status of the submodule
-    # '+' : The submodule does not match the SHA-1 currently in the index of the repository
-    # '-' : The submodule is not initialized
-    # ' ' : Correct version of submodule is initialized
-    status_indicator = status[0][0]
-    if status_indicator == '+':
-      # Write a warning that the sha tags do not match
-      sys.stderr.write('WARNING: the currently checked out submodule commit in '
-                        + path + ' does not match the SHA-1 found in the index.\n')
-      sys.stderr.write('Use \'git submodule update --init '+ path + '\' to reset the module if necessary.\n')
-    elif status_indicator == '-':
-      # Initialize the submodule if necessary
-      print('Initialize submodule ' + path + ' using git ... ')
-      subprocess.run(['git', 'submodule', 'update', '--init', path], check = True, cwd = sys.path[0])
-      # to update CoolProp external libraries
-    if sha_commit == '0ce42fcf3bb2c373512bc825a4f0c1973a78f307':
-      # update coolprop
-      original_path = os.getcwd()
-      print('update CoolProp')
-      absolute_path = sys.path[0]
-      relative_path = "subprojects/CoolProp"
-      full_path = os.path.join(absolute_path, relative_path)
-      os.chdir(full_path)
-      print(full_path)
-      subprocess.run(['git', 'submodule', 'init'])
-      subprocess.run(['git', 'submodule', 'update'])
-      print(original_path)
-      os.chdir(original_path)
-      print('CoolProp updated')
-      # Check that the SHA tag stored in this file matches the one stored in the git index
-    cur_sha_commit = status[1:].split(' ')[0]
-    if (cur_sha_commit != sha_commit):
-      print('SHA-1 tag stored in index does not match SHA tag stored in this script.')
+    if not os.path.exists(path + os.path.sep + sha_commit):
+
+        # Check the status of the submodule
+        status = subprocess.run(
+            ["git", "submodule", "status", path],
+            stdout=subprocess.PIPE,
+            check=True,
+            cwd=sys.path[0],
+        ).stdout.decode("utf-8")
+        # The first character of the output indicates the status of the submodule
+        # '+' : The submodule does not match the SHA-1 currently in the index of the repository
+        # '-' : The submodule is not initialized
+        # ' ' : Correct version of submodule is initialized
+        status_indicator = status[0][0]
+        if status_indicator == "+":
+            # Write a warning that the sha tags do not match
+            sys.stderr.write(
+                "WARNING: the currently checked out submodule commit in "
+                + path
+                + " does not match the SHA-1 found in the index.\n"
+            )
+            sys.stderr.write(
+                "Use 'git submodule update --init "
+                + path
+                + "' to reset the module if necessary.\n"
+            )
+        elif status_indicator == "-":
+            # Initialize the submodule if necessary
+            print("Initialize submodule " + path + " using git ... ")
+            subprocess.run(
+                ["git", "submodule", "update", "--init", path],
+                check=True,
+                cwd=sys.path[0],
+            )
+            # to update CoolProp external libraries
+        if sha_commit == "0ce42fcf3bb2c373512bc825a4f0c1973a78f307":
+            # update coolprop
+            original_path = os.getcwd()
+            print("update CoolProp")
+            absolute_path = sys.path[0]
+            relative_path = "subprojects/CoolProp"
+            full_path = os.path.join(absolute_path, relative_path)
+            os.chdir(full_path)
+            print(full_path)
+            subprocess.run(["git", "submodule", "init"])
+            subprocess.run(["git", "submodule", "update"])
+            print(original_path)
+            os.chdir(original_path)
+            print("CoolProp updated")
+            # Check that the SHA tag stored in this file matches the one stored in the git index
+        cur_sha_commit = status[1:].split(" ")[0]
+        if cur_sha_commit != sha_commit:
+            print(
+                "SHA-1 tag stored in index does not match SHA tag stored in this script."
+            )
 
 
 def download_module(name, alt_name, git_repo, commit_sha):
 
-  # ZipFile does not preserve file permissions.
-  # This is a workaround for that problem:
-  # https://stackoverflow.com/questions/39296101/python-zipfile-removes-execute-permissions-from-binaries
-  class MyZipFile(zipfile.ZipFile):
-    def _extract_member(self, member, targetpath, pwd):
-      if not isinstance(member, zipfile.ZipInfo):
-        member = self.getinfo(member)
-
-      targetpath = super()._extract_member(member, targetpath, pwd)
+    # ZipFile does not preserve file permissions.
+    # This is a workaround for that problem:
+    # https://stackoverflow.com/questions/39296101/python-zipfile-removes-execute-permissions-from-binaries
+    class MyZipFile(zipfile.ZipFile):
+        def _extract_member(self, member, targetpath, pwd):
+            if not isinstance(member, zipfile.ZipInfo):
+                member = self.getinfo(member)
 
-      attr = member.external_attr >> 16
-      if attr != 0:
-        os.chmod(targetpath, attr)
-      return targetpath
+            targetpath = super()._extract_member(member, targetpath, pwd)
 
-  # Where to download the module into
-  target_dir = os.path.dirname(alt_name)
+            attr = member.external_attr >> 16
+            if attr != 0:
+                os.chmod(targetpath, attr)
+            return targetpath
 
-  # File tag used to mark modules downloaded by this method.
-  module_identifier = os.path.join(alt_name, commit_sha)
+    # Where to download the module into
+    target_dir = os.path.dirname(alt_name)
 
-  if not os.path.exists(module_identifier):
+    # File tag used to mark modules downloaded by this method.
+    module_identifier = os.path.join(alt_name, commit_sha)
 
-    if os.path.exists(alt_name) and os.listdir(alt_name):
-      print('Directory ' + alt_name + ' is not empty')
-      print('Maybe submodules are already cloned with git?')
-      sys.exit(1)
+    if not os.path.exists(module_identifier):
 
-    else:
-      print('Downloading ' + name + ' \'' + commit_sha + '\'')
+        if os.path.exists(alt_name) and os.listdir(alt_name):
+            print("Directory " + alt_name + " is not empty")
+            print("Maybe submodules are already cloned with git?")
+            sys.exit(1)
 
-      filename = commit_sha + '.zip'
-      filepath = os.path.join(sys.path[0], filename)
-      alt_filename = name + "-" + filename
-      alt_filepath = os.path.join(sys.path[0], alt_filename)
+        else:
+            print("Downloading " + name + " '" + commit_sha + "'")
 
-      url = git_repo + '/archive/' + filename
+            filename = commit_sha + ".zip"
+            filepath = os.path.join(sys.path[0], filename)
+            alt_filename = name + "-" + filename
+            alt_filepath = os.path.join(sys.path[0], alt_filename)
 
-      if not os.path.exists(filepath) and not os.path.exists(alt_filepath):
-        try:
-          urllib.request.urlretrieve (url, commit_sha + '.zip')
-        except Exception as e:
-          print(e)
-          print('Download of module ' + name + ' failed.')
-          print('Get archive at ' + url)
-          print('and place it in the source code root folder')
-          print('Run meson.py again')
-          sys.exit()
+            url = git_repo + "/archive/" + filename
 
-      # Detect filename (changes have been noted)
-      if not os.path.exists(filepath):
-        filepath = alt_filepath
+            if not os.path.exists(filepath) and not os.path.exists(alt_filepath):
+                try:
+                    urllib.request.urlretrieve(url, commit_sha + ".zip")
+                except Exception as e:
+                    print(e)
+                    print("Download of module " + name + " failed.")
+                    print("Get archive at " + url)
+                    print("and place it in the source code root folder")
+                    print("Run meson.py again")
+                    sys.exit()
 
-      # Unzip file
-      zipf = MyZipFile(filepath)
-      zipf.extractall(target_dir)
+            # Detect filename (changes have been noted)
+            if not os.path.exists(filepath):
+                filepath = alt_filepath
 
-      # Remove directory if exists
-      if os.path.exists(alt_name):
-        os.rmdir(alt_name)
+            # Unzip file
+            zipf = MyZipFile(filepath)
+            zipf.extractall(target_dir)
 
-      os.rename(os.path.join(target_dir, name + '-' + commit_sha), alt_name)
+            # Remove directory if exists
+            if os.path.exists(alt_name):
+                os.rmdir(alt_name)
 
-      # Delete zip file
-      remove_file(filepath)
+            os.rename(os.path.join(target_dir, name + "-" + commit_sha), alt_name)
 
-      # Create identifier
-      f = open(module_identifier, 'w')
-      f.close()
+            # Delete zip file
+            remove_file(filepath)
 
+            # Create identifier
+            f = open(module_identifier, "w")
+            f.close()
 
-if __name__ == '__main__':
-  if sys.version_info[0] < 3:
-    raise Exception("Script must be run using Python 3")
 
-  # Set up the build environment, i.e. clone or download all submodules
-  init_submodules(sys.argv[1])
+if __name__ == "__main__":
+    if sys.version_info[0] < 3:
+        raise Exception("Script must be run using Python 3")
 
-  sys.exit(0)
+    # Set up the build environment, i.e. clone or download all submodules
+    init_submodules(sys.argv[1])
 
+    sys.exit(0)
diff --git a/preconfigure.py b/preconfigure.py
index 7e27d2e2a97..9085809e1df 100755
--- a/preconfigure.py
+++ b/preconfigure.py
@@ -27,102 +27,122 @@
 
 import sys, os, subprocess, shutil, urllib.request, zipfile
 from pathlib import Path
-sys.path.append(sys.path[0] + os.path.sep + 'meson_scripts')
+
+sys.path.append(sys.path[0] + os.path.sep + "meson_scripts")
 from init import init_submodules
 from init import remove_file
 
+
 def build_ninja():
 
-  # If we are on windows, we don't need to compile ninja, we just download the executable
-  if os.name == 'nt':
-    ninja_exe_url = 'https://github.com/ninja-build/ninja/releases/download/v1.9.0/ninja-win.zip'
-
-    # Try to execute ninja, if it fails, download .exe from github
-    try:
-      subprocess.run([sys.path[0] + os.path.sep + 'ninja.exe', '--version'], stdout=subprocess.PIPE)
-    except OSError:
-      print ('Downloading ninja ... ')
-      try:
-        urllib.request.urlretrieve (ninja_exe_url,'ninja-win.zip')
-      except:
-        print(e)
-        print('Download of ninja executable failed.')
-        print('Get archive at ' + ninja_exe_url)
-        print('extract ninja.exe in the source code root folder.')
-        print('Run meson.py again.')
-        sys.exit(1)
-
-      zipf = zipfile.ZipFile(sys.path[0] + os.path.sep + 'ninja-win.zip')
-      zipf.extractall(sys.path[0])
-      remove_file(sys.path[0] + os.path.sep + 'ninja-win.zip')
-  else:
-    ninjapath = sys.path[0] + os.path.sep + 'externals' + os.path.sep + 'ninja'
-    try:
-      subprocess.run([sys.path[0] + os.path.sep + 'ninja', '--version'], stdout=subprocess.PIPE)
-    except OSError:
-      print("ninja executable not found. Building ...")
-      subprocess.run(['python3', 'configure.py', '--bootstrap'], cwd=ninjapath)
-      shutil.copy(ninjapath+ os.path.sep + 'ninja', '.')
-
-def run(own_meson = False,
-        own_codi = True,
-        own_medi = True,
-        own_opdi = True,
-        own_mpp  = True,
-        own_cool = True,
-        own_mel  = True):
-
-  # Set up the build environment, i.e. clone or download submodules
-  init_submodules(method = 'auto',
-                  own_meson = own_meson,
-                  own_codi = own_codi,
-                  own_medi = own_medi,
-                  own_opdi = own_opdi,
-                  own_mpp  = own_mpp ,
-                  own_cool = own_cool,
-                  own_mel  = own_mel)
-
-  if (own_meson):
-    # Build ninja if it cannot be found
-    build_ninja()
-
-  # Leave a timestamp
-  Path('su2preconfig.timestamp').touch()
-
-
-if __name__ == '__main__':
-  if sys.version_info[0] < 3:
-    raise Exception("Script must be run using Python 3")
-
-  import argparse
-  parser = argparse.ArgumentParser()
-  parser.add_argument("--with-own-meson",
-                      help="download own copies of Meson and Ninja",
-                      action="store_true")
-  parser.add_argument("--no-codi",
-                      help="do not download own copy of CoDiPack",
-                      action="store_false")
-  parser.add_argument("--no-medi",
-                      help="do not download own copy of MeDiPack",
-                      action="store_false")
-  parser.add_argument("--no-opdi",
-                      help="do not download own copy of OpDiLib",
-                      action="store_false")
-  parser.add_argument("--no-mpp",
-                      help="do not download own copy of Mutationpp",
-                      action="store_false")
-  parser.add_argument("--no-coolprop",
-                      help="do not download own copy of CoolProp",
-                      action="store_false")
-  parser.add_argument("--no-mel",
-                      help="do not download own copy of MEL",
-                      action="store_false")
-  args = parser.parse_args()
-
-  run(own_meson = args.with_own_meson,
-      own_codi = args.no_codi,
-      own_medi = args.no_medi,
-      own_opdi = args.no_opdi,
-      own_mpp  = args.no_mpp,
-      own_cool = args.no_coolprop,
-      own_mel  = args.no_mel)
+    # If we are on windows, we don't need to compile ninja, we just download the executable
+    if os.name == "nt":
+        ninja_exe_url = "https://github.com/ninja-build/ninja/releases/download/v1.9.0/ninja-win.zip"
+
+        # Try to execute ninja, if it fails, download .exe from github
+        try:
+            subprocess.run(
+                [sys.path[0] + os.path.sep + "ninja.exe", "--version"],
+                stdout=subprocess.PIPE,
+            )
+        except OSError:
+            print("Downloading ninja ... ")
+            try:
+                urllib.request.urlretrieve(ninja_exe_url, "ninja-win.zip")
+            except:
+                print(e)
+                print("Download of ninja executable failed.")
+                print("Get archive at " + ninja_exe_url)
+                print("extract ninja.exe in the source code root folder.")
+                print("Run meson.py again.")
+                sys.exit(1)
+
+            zipf = zipfile.ZipFile(sys.path[0] + os.path.sep + "ninja-win.zip")
+            zipf.extractall(sys.path[0])
+            remove_file(sys.path[0] + os.path.sep + "ninja-win.zip")
+    else:
+        ninjapath = sys.path[0] + os.path.sep + "externals" + os.path.sep + "ninja"
+        try:
+            subprocess.run(
+                [sys.path[0] + os.path.sep + "ninja", "--version"],
+                stdout=subprocess.PIPE,
+            )
+        except OSError:
+            print("ninja executable not found. Building ...")
+            subprocess.run(["python3", "configure.py", "--bootstrap"], cwd=ninjapath)
+            shutil.copy(ninjapath + os.path.sep + "ninja", ".")
+
+
+def run(
+    own_meson=False,
+    own_codi=True,
+    own_medi=True,
+    own_opdi=True,
+    own_mpp=True,
+    own_cool=True,
+    own_mel=True,
+):
+
+    # Set up the build environment, i.e. clone or download submodules
+    init_submodules(
+        method="auto",
+        own_meson=own_meson,
+        own_codi=own_codi,
+        own_medi=own_medi,
+        own_opdi=own_opdi,
+        own_mpp=own_mpp,
+        own_cool=own_cool,
+        own_mel=own_mel,
+    )
+
+    if own_meson:
+        # Build ninja if it cannot be found
+        build_ninja()
+
+    # Leave a timestamp
+    Path("su2preconfig.timestamp").touch()
+
+
+if __name__ == "__main__":
+    if sys.version_info[0] < 3:
+        raise Exception("Script must be run using Python 3")
+
+    import argparse
+
+    parser = argparse.ArgumentParser()
+    parser.add_argument(
+        "--with-own-meson",
+        help="download own copies of Meson and Ninja",
+        action="store_true",
+    )
+    parser.add_argument(
+        "--no-codi", help="do not download own copy of CoDiPack", action="store_false"
+    )
+    parser.add_argument(
+        "--no-medi", help="do not download own copy of MeDiPack", action="store_false"
+    )
+    parser.add_argument(
+        "--no-opdi", help="do not download own copy of OpDiLib", action="store_false"
+    )
+    parser.add_argument(
+        "--no-mpp", help="do not download own copy of Mutationpp", action="store_false"
+    )
+    parser.add_argument(
+        "--no-coolprop",
+        help="do not download own copy of CoolProp",
+        action="store_false",
+    )
+    parser.add_argument(
+        "--no-mel", help="do not download own copy of MEL", action="store_false"
+    )
+    args = parser.parse_args()
+
+    run(
+        own_meson=args.with_own_meson,
+        own_codi=args.no_codi,
+        own_medi=args.no_medi,
+        own_opdi=args.no_opdi,
+        own_mpp=args.no_mpp,
+        own_cool=args.no_coolprop,
+        own_mel=args.no_mel,
+    )

From 205c48259061dbd14ed1198b8558be645ad111f8 Mon Sep 17 00:00:00 2001
From: snow54 <yuukiutsumi@yahoo.co.jp>
Date: Fri, 17 Mar 2023 10:32:02 +0900
Subject: [PATCH 293/656] Fix condition to set penalty function

---
 SU2_PY/SU2/eval/design.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/SU2_PY/SU2/eval/design.py b/SU2_PY/SU2/eval/design.py
index 82768dcd42f..4603b1e9541 100644
--- a/SU2_PY/SU2/eval/design.py
+++ b/SU2_PY/SU2/eval/design.py
@@ -269,7 +269,7 @@ def obj_p(config,state,this_obj,def_objs):
         (def_objs[this_obj]['OBJTYPE']=='<' and funcval > constraint )):
         penalty = (constraint - funcval)**2.0
     # If 'DEFAULT' objtype this returns the function value.
-    else:
+    elif (def_objs[this_obj]['OBJTYPE']=='DEFAULT'):
         penalty = funcval
     return penalty
 

From 2371e91d1985046047f8b79ce56ea6939f463f43 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Fri, 17 Mar 2023 13:49:14 +0100
Subject: [PATCH 294/656] Remove unused variable.

---
 TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py | 2 --
 1 file changed, 2 deletions(-)

diff --git a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
index bf5aa2c1fdf..3b59e063bef 100755
--- a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
@@ -56,10 +56,8 @@ def main():
   if options.with_MPI == True:
     from mpi4py import MPI
     comm = MPI.COMM_WORLD
-    rank = comm.Get_rank()
   else:
     comm = 0
-    rank = 0
 
   # Initialize the corresponding driver of SU2, this includes solver preprocessing
   SU2Driver = pysu2.CDiscAdjSinglezoneDriver(options.filename, options.nZone, comm);

From a3ce60341154e46f2f9e1dc667f6c89e7b767d80 Mon Sep 17 00:00:00 2001
From: Kursat Yurt <kursatyurt@gmail.com>
Date: Fri, 17 Mar 2023 19:01:02 +0100
Subject: [PATCH 295/656] Format file

---
 SU2_PY/SU2/eval/design.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/SU2_PY/SU2/eval/design.py b/SU2_PY/SU2/eval/design.py
index 3790c3697c6..bac8c91987d 100644
--- a/SU2_PY/SU2/eval/design.py
+++ b/SU2_PY/SU2/eval/design.py
@@ -279,7 +279,7 @@ def obj_p(config, state, this_obj, def_objs):
     ):
         penalty = (constraint - funcval) ** 2.0
     # If 'DEFAULT' objtype this returns the function value.
-    elif (def_objs[this_obj]['OBJTYPE']=='DEFAULT'):
+    elif def_objs[this_obj]["OBJTYPE"] == "DEFAULT":
         penalty = funcval
     return penalty
 

From 45e6a04db3bbeda695ada63aa93dfdbd59d90450 Mon Sep 17 00:00:00 2001
From: Kursat Yurt <kursatyurt@gmail.com>
Date: Fri, 17 Mar 2023 19:30:26 +0100
Subject: [PATCH 296/656] Resolve merge conflict

---
 SU2_DEF/src/drivers/CDeformationDriver.cpp        | 14 --------------
 SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp | 14 --------------
 2 files changed, 28 deletions(-)

diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 70b90ed6d44..c73e6427bf4 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -36,20 +36,6 @@ using namespace std;
 
 CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
     : CDriverBase(confFile, 1, MPICommunicator) {
-<<<<<<< HEAD
-/*--- Initialize MeDiPack (must also be here to initialize it from Python) ---*/
-#ifdef HAVE_MPI
-#if defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)
-  SU2_MPI::Init_AMPI();
-#endif
-#endif
-
-  SU2_MPI::SetComm(MPICommunicator);
-
-  rank = SU2_MPI::GetRank();
-  size = SU2_MPI::GetSize();
-=======
->>>>>>> origin/develop
 
   /*--- Preprocessing of the config files. ---*/
 
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index 754fcb4523d..de1cd9025ae 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -42,20 +42,6 @@ using namespace std;
 
 CDiscAdjDeformationDriver::CDiscAdjDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
     : CDriverBase(confFile, 1, MPICommunicator) {
-<<<<<<< HEAD
-/*--- Initialize MeDiPack (must also be here to initialize it from Python). ---*/
-#ifdef HAVE_MPI
-#if defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE)
-  SU2_MPI::Init_AMPI();
-#endif
-#endif
-
-  SU2_MPI::SetComm(MPICommunicator);
-
-  rank = SU2_MPI::GetRank();
-  size = SU2_MPI::GetSize();
-=======
->>>>>>> origin/develop
 
   /*--- Preprocessing of the config files. ---*/
 

From 18fbded984111e0294d45c2a4b48b8a18278b852 Mon Sep 17 00:00:00 2001
From: Kursat Yurt <kursatyurt@gmail.com>
Date: Fri, 17 Mar 2023 19:30:55 +0100
Subject: [PATCH 297/656] Reformat

---
 SU2_DEF/src/drivers/CDeformationDriver.cpp        | 1 -
 SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp | 1 -
 2 files changed, 2 deletions(-)

diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index c73e6427bf4..b8675df432c 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -36,7 +36,6 @@ using namespace std;
 
 CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
     : CDriverBase(confFile, 1, MPICommunicator) {
-
   /*--- Preprocessing of the config files. ---*/
 
   Input_Preprocessing();
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index de1cd9025ae..7131e975725 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -42,7 +42,6 @@ using namespace std;
 
 CDiscAdjDeformationDriver::CDiscAdjDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
     : CDriverBase(confFile, 1, MPICommunicator) {
-
   /*--- Preprocessing of the config files. ---*/
 
   Input_Preprocessing();

From a8e20103776852e0cd68463159d739f3f1064ca3 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 18 Mar 2023 19:08:29 -0700
Subject: [PATCH 298/656] cleanup the CHT and FSI interface

---
 SU2_CFD/include/drivers/CDriver.hpp           |  72 +-------
 SU2_CFD/include/drivers/CDriverBase.hpp       |  66 +++++++
 SU2_CFD/include/solvers/CHeatSolver.hpp       |   4 +-
 SU2_CFD/src/drivers/CDriver.cpp               |   2 +-
 SU2_CFD/src/python_wrapper_structure.cpp      | 166 +-----------------
 SU2_PY/FSI_tools/FSIInterface.py              |   2 +-
 .../flow_load_sens/run_adjoint.py             |   2 +-
 .../launch_unsteady_CHT_FlatPlate.py          |   2 +-
 .../translating_NACA0012/run_su2.py           |   2 +-
 9 files changed, 79 insertions(+), 239 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index ae50e59e2f1..a84d3471c15 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -256,12 +256,13 @@ class CDriver : public CDriverBase {
                                  CVolumetricMovement*& grid_movement, CSurfaceMovement*& surface_movement) const;
 
   /*!
-   * \brief Initialize Python interface functionalities
+   * \brief Initialize Python interface functionalities. When using multigrid,
+   * it is important to call this after modifying custom boundary values.
    * \param[in] config - Definition of the particular problem.
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] solver - Container vector with all the solutions.
    */
-  void PythonInterface_Preprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver);
+  void PythonInterfacePreprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver);
 
   /*!
    * \brief Preprocess the output container.
@@ -477,54 +478,6 @@ class CDriver : public CDriverBase {
    */
   string GetSurfaceFileName() const;
 
-  /*!
-   * \brief Get the temperature at a vertex on a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Temperature of the vertex.
-   */
-  passivedouble GetVertexTemperature(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Set the temperature of a vertex on a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \param[in] val_WallTemp - Value of the temperature.
-   */
-  void SetVertexTemperature(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallTemp);
-
-  /*!
-   * \brief Get the heat flux at a vertex on a specified marker (3 components).
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return True if the vertex is a halo node.
-   */
-  vector<passivedouble> GetVertexHeatFluxes(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Get the wall normal component of the heat flux at a vertex on a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Wall normal component of the heat flux at the vertex.
-   */
-  passivedouble GetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Set the wall normal component of the heat flux at a vertex on a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \param[in] val_WallHeatFlux - Value of the normal heat flux.
-   */
-  void SetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallHeatFlux);
-
-  /*!
-   * \brief Get the thermal conductivity at a vertex on a specified marker.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Thermal conductivity at the vertex.
-   */
-  passivedouble GetThermalConductivity(unsigned short iMarker, unsigned long iVertex) const;
-
   /*!
    * \brief Preprocess the inlets via file input for all solvers.
    * \param[in] solver_container - Container vector with all the solutions.
@@ -553,17 +506,6 @@ class CDriver : public CDriverBase {
    */
   vector<passivedouble> GetMeshDisp_Sensitivity(unsigned short iMarker, unsigned long iVertex) const;
 
-  /*!
-   * \brief Set the load in X direction for the structural solver.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \param[in] LoadX - Value of the load in the direction X.
-   * \param[in] LoadX - Value of the load in the direction Y.
-   * \param[in] LoadX - Value of the load in the direction Z.
-   */
-  void SetFEA_Loads(unsigned short iMarker, unsigned long iVertex, passivedouble LoadX, passivedouble LoadY,
-                    passivedouble LoadZ);
-
   /*!
    * \brief Get the sensitivity of the flow loads for the structural solver.
    * \param[in] iMarker - Marker identifier.
@@ -574,14 +516,6 @@ class CDriver : public CDriverBase {
    */
   vector<passivedouble> GetFlowLoad_Sensitivity(unsigned short iMarker, unsigned long iVertex) const;
 
-  /*!
-   * \brief Get the flow load (from the extra step - the repeated methods should be unified once the postprocessing
-   * strategy is in place).
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   */
-  vector<passivedouble> GetFlowLoad(unsigned short iMarker, unsigned long iVertex) const;
-
   /*!
    * \brief Set the adjoint of the flow tractions (from the extra step -
    * the repeated methods should be unified once the postprocessing strategy is in place).
diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index 9d6c60334af..9182eb5ca40 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -422,6 +422,72 @@ class CDriverBase {
         const_cast<su2activematrix&>(solver->GetNodes()->GetPrimitive()), main_geometry->vertex[iMarker],
         main_geometry->GetnVertex(iMarker), "MarkerPrimitives", false);
   }
+
+  /*!
+   * \brief Set the temperature of a vertex on a specified marker (MARKER_PYTHON_CUSTOM).
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \param[in] WallTemp - Value of the temperature.
+   */
+  inline void SetMarkerCustomTemperature(unsigned short iMarker, unsigned long iVertex, passivedouble WallTemp)  {
+    main_geometry->SetCustomBoundaryTemperature(iMarker, iVertex, WallTemp);
+  }
+
+  /*!
+   * \brief Set the wall normal heat flux at a vertex on a specified marker (MARKER_PYTHON_CUSTOM).
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \param[in] WallHeatFlux - Value of the normal heat flux.
+   */
+  inline void SetMarkerCustomNormalHeatFlux(unsigned short iMarker, unsigned long iVertex, passivedouble WallHeatFlux) {
+    main_geometry->SetCustomBoundaryHeatFlux(iMarker, iVertex, WallHeatFlux);
+  }
+
+  /*!
+   * \brief Get the wall normal heat flux at a vertex on a specified marker of the flow or heat solver.
+   * \param[in] iSolver - Solver identifier, should be either a flow solver or the heat solver.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \return Wall normal component of the heat flux at the vertex.
+   */
+  inline passivedouble GetMarkerNormalHeatFlux(unsigned short iSolver, unsigned short iMarker, unsigned long iVertex) const {
+    if (iSolver != HEAT_SOL && iSolver != FLOW_SOL) {
+      SU2_MPI::Error("Normal heat flux is only available for flow or heat solvers.");
+    }
+    return SU2_TYPE::GetValue(GetSolverAndCheckMarker(iSolver, iMarker)->GetHeatFlux(iMarker, iVertex));
+  }
+
+  /*!
+   * \brief Sets the nodal force for the structural solver at a vertex of a marker.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \param[in] force - Force vector.
+   */
+  inline void SetMarkerCustomFEALoad(unsigned short iMarker, unsigned long iVertex, std::vector<passivedouble> force) {
+    auto* solver = GetSolverAndCheckMarker(FEA_SOL, iMarker);
+    std::array<su2double, 3> load{};
+    for (auto iDim = 0u; iDim < GetNumberDimensions(); ++iDim) load[iDim] = force[iDim];
+    const auto iPoint = GetMarkerNode(iMarker, iVertex);
+    solver->GetNodes()->Set_FlowTraction(iPoint, load);
+  }
+
+  /*!
+   * \brief Get the fluid force at a vertex of a solid wall marker of the flow solver.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   */
+  vector<passivedouble> GetMarkerFlowLoad(unsigned short iMarker, unsigned long iVertex) const {
+    vector<passivedouble> FlowLoad(GetNumberDimensions(), 0.0);
+    const auto* solver = GetSolverAndCheckMarker(FLOW_SOL, iMarker);
+
+    if (main_config->GetSolid_Wall(iMarker)) {
+      for (auto iDim = 0u; iDim < GetNumberDimensions(); ++iDim) {
+        FlowLoad[iDim] = SU2_TYPE::GetValue(solver->GetVertexTractions(iMarker, iVertex, iDim));
+      }
+    }
+    return FlowLoad;
+  }
+
 /// \}
 
  protected:
diff --git a/SU2_CFD/include/solvers/CHeatSolver.hpp b/SU2_CFD/include/solvers/CHeatSolver.hpp
index 2074d479a6a..ce97728dad6 100644
--- a/SU2_CFD/include/solvers/CHeatSolver.hpp
+++ b/SU2_CFD/include/solvers/CHeatSolver.hpp
@@ -401,5 +401,7 @@ class CHeatSolver final : public CScalarSolver<CHeatVariable> {
    * \param[in] val_vertex - Vertex of the marker <i>val_marker</i> where the coefficient is evaluated.
    * \return Value of the heat flux.
    */
-  inline su2double GetHeatFlux(unsigned short val_marker, unsigned long val_vertex) const override { return HeatFlux[val_marker][val_vertex]; }
+  inline su2double GetHeatFlux(unsigned short val_marker, unsigned long val_vertex) const override {
+    return HeatFlux[val_marker][val_vertex];
+  }
 };
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index cf69fefeddd..462d1e71d89 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -266,7 +266,7 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
   }
 
 
-  PythonInterface_Preprocessing(config_container, geometry_container, solver_container);
+  PythonInterfacePreprocessing(config_container, geometry_container, solver_container);
 
 
   /*--- Preprocessing time is reported now, but not included in the next compute portion. ---*/
diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index cc7cd689005..f93a116636e 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -29,11 +29,11 @@
 #include "../include/drivers/CDriver.hpp"
 #include "../include/drivers/CSinglezoneDriver.hpp"
 
-void CDriver::PythonInterface_Preprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver) {
+void CDriver::PythonInterfacePreprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver) {
   int rank = MASTER_NODE;
   SU2_MPI::Comm_rank(SU2_MPI::GetComm(), &rank);
 
-  /* --- Initialize boundary conditions customization, this is achieved through the Python wrapper. --- */
+  /*--- Initialize boundary conditions customization, this is achieved through the Python wrapper. --- */
   for (iZone = 0; iZone < nZone; iZone++) {
     if (config[iZone]->GetnMarker_PyCustom() > 0) {
       if (rank == MASTER_NODE) cout << "----------------- Python Interface Preprocessing ( Zone " << iZone << " ) -----------------" << endl;
@@ -172,123 +172,6 @@ passivedouble CDriver::GetUnsteadyTimeStep() const {
 
 string CDriver::GetSurfaceFileName() const { return config_container[ZONE_0]->GetSurfCoeff_FileName(); }
 
-///////////////////////////////////////////////////////////////////////////////
-/* Functions related to CHT solver                                           */
-///////////////////////////////////////////////////////////////////////////////
-
-passivedouble CDriver::GetVertexTemperature(unsigned short iMarker, unsigned long iVertex) const {
-  unsigned long iPoint;
-  su2double vertexWallTemp(0.0);
-
-  bool compressible = (config_container[ZONE_0]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-
-  if (geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint) && compressible) {
-    vertexWallTemp = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetTemperature(iPoint);
-  }
-
-  return SU2_TYPE::GetValue(vertexWallTemp);
-}
-
-void CDriver::SetVertexTemperature(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallTemp) {
-  geometry_container[ZONE_0][INST_0][MESH_0]->SetCustomBoundaryTemperature(iMarker, iVertex, val_WallTemp);
-}
-
-vector<passivedouble> CDriver::GetVertexHeatFluxes(unsigned short iMarker, unsigned long iVertex) const {
-  unsigned long iPoint;
-  unsigned short iDim;
-  su2double Prandtl_Lam = config_container[ZONE_0]->GetPrandtl_Lam();
-  su2double Gas_Constant = config_container[ZONE_0]->GetGas_ConstantND();
-  su2double Gamma = config_container[ZONE_0]->GetGamma();
-  su2double Gamma_Minus_One = Gamma - 1.0;
-  su2double Cp = (Gamma / Gamma_Minus_One) * Gas_Constant;
-  su2double laminar_viscosity, thermal_conductivity;
-  vector<su2double> GradT(3, 0.0);
-  vector<su2double> HeatFlux(3, 0.0);
-  vector<passivedouble> HeatFluxPassive(3, 0.0);
-
-  bool compressible = (config_container[ZONE_0]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-
-  if (compressible) {
-    laminar_viscosity = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
-    thermal_conductivity = Cp * (laminar_viscosity / Prandtl_Lam);
-    for (iDim = 0; iDim < nDim; iDim++) {
-      GradT[iDim] = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetGradient_Primitive(iPoint, 0, iDim);
-      HeatFlux[iDim] = -thermal_conductivity * GradT[iDim];
-    }
-  }
-
-  HeatFluxPassive[0] = SU2_TYPE::GetValue(HeatFlux[0]);
-  HeatFluxPassive[1] = SU2_TYPE::GetValue(HeatFlux[1]);
-  HeatFluxPassive[2] = SU2_TYPE::GetValue(HeatFlux[2]);
-
-  return HeatFluxPassive;
-}
-
-passivedouble CDriver::GetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex) const {
-  unsigned long iPoint;
-  unsigned short iDim;
-  su2double vertexWallHeatFlux;
-  su2double Prandtl_Lam = config_container[ZONE_0]->GetPrandtl_Lam();
-  su2double Gas_Constant = config_container[ZONE_0]->GetGas_ConstantND();
-  su2double Gamma = config_container[ZONE_0]->GetGamma();
-  su2double Gamma_Minus_One = Gamma - 1.0;
-  su2double Cp = (Gamma / Gamma_Minus_One) * Gas_Constant;
-  su2double Area;
-  su2double laminar_viscosity, thermal_conductivity, dTdn;
-  su2double *Normal, GradT[3] = {0.0, 0.0, 0.0}, UnitNormal[3] = {0.0, 0.0, 0.0};
-
-  bool compressible = (config_container[ZONE_0]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
-
-  vertexWallHeatFlux = 0.0;
-  dTdn = 0.0;
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-
-  if (geometry_container[ZONE_0][INST_0][MESH_0]->nodes->GetDomain(iPoint) && compressible) {
-    Normal = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNormal();
-
-    Area = GeometryToolbox::Norm(nDim, Normal);
-
-    for (iDim = 0; iDim < nDim; iDim++) UnitNormal[iDim] = Normal[iDim] / Area;
-
-    laminar_viscosity = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
-    thermal_conductivity = Cp * (laminar_viscosity / Prandtl_Lam);
-    /*Compute wall heat flux (normal to the wall) based on computed temperature gradient*/
-    for (iDim = 0; iDim < nDim; iDim++) {
-      GradT[iDim] = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetGradient_Primitive(iPoint, 0, iDim);
-      dTdn += GradT[iDim] * UnitNormal[iDim];
-    }
-
-    vertexWallHeatFlux = -thermal_conductivity * dTdn;
-  }
-
-  return SU2_TYPE::GetValue(vertexWallHeatFlux);
-}
-
-void CDriver::SetVertexNormalHeatFlux(unsigned short iMarker, unsigned long iVertex, passivedouble val_WallHeatFlux) {
-  geometry_container[ZONE_0][INST_0][MESH_0]->SetCustomBoundaryHeatFlux(iMarker, iVertex, val_WallHeatFlux);
-}
-
-passivedouble CDriver::GetThermalConductivity(unsigned short iMarker, unsigned long iVertex) const {
-  unsigned long iPoint;
-  su2double Prandtl_Lam = config_container[ZONE_0]->GetPrandtl_Lam();
-  su2double Gas_Constant = config_container[ZONE_0]->GetGas_ConstantND();
-  su2double Gamma = config_container[ZONE_0]->GetGamma();
-  su2double Gamma_Minus_One = Gamma - 1.0;
-  su2double Cp = (Gamma / Gamma_Minus_One) * Gas_Constant;
-  su2double laminar_viscosity, thermal_conductivity;
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  laminar_viscosity = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetNodes()->GetLaminarViscosity(iPoint);
-  thermal_conductivity = Cp * (laminar_viscosity / Prandtl_Lam);
-
-  return SU2_TYPE::GetValue(thermal_conductivity);
-}
-
 ////////////////////////////////////////////////////////////////////////////////
 /* Functions related to the management of markers                             */
 ////////////////////////////////////////////////////////////////////////////////
@@ -305,7 +188,6 @@ vector<string> CDriver::GetCHTMarkerTags() const {
       tags.push_back(config_container[ZONE_0]->GetMarker_All_TagBound(iMarker));
     }
   }
-
   return tags;
 }
 
@@ -321,7 +203,6 @@ vector<string> CDriver::GetInletMarkerTags() const {
       tags.push_back(config_container[ZONE_0]->GetMarker_All_TagBound(iMarker));
     }
   }
-
   return tags;
 }
 
@@ -429,22 +310,6 @@ void CDriver::BoundaryConditionsUpdate() {
   }
 }
 
-////////////////////////////////////////////////////////////////////////////////
-/* Functions related to finite elements                                       */
-////////////////////////////////////////////////////////////////////////////////
-
-void CDriver::SetFEA_Loads(unsigned short iMarker, unsigned long iVertex, passivedouble LoadX, passivedouble LoadY,
-                           passivedouble LoadZ) {
-  unsigned long iPoint;
-  su2double NodalForce[3] = {0.0, 0.0, 0.0};
-  NodalForce[0] = LoadX;
-  NodalForce[1] = LoadY;
-  NodalForce[2] = LoadZ;
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL]->GetNodes()->Set_FlowTraction(iPoint, NodalForce);
-}
-
 ////////////////////////////////////////////////////////////////////////////////
 /* Functions related to adjoint simulations                                   */
 ////////////////////////////////////////////////////////////////////////////////
@@ -528,30 +393,3 @@ void CDriver::SetSourceTerm_VelAdjoint(unsigned short iMarker, unsigned long iVe
   solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 1, val_AdjointY);
   if (geometry->GetnDim() == 3) solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 2, val_AdjointZ);
 }
-
-////////////////////////////////////////////////////////////////////////////////
-/* Functions related to flow loads                                             */
-////////////////////////////////////////////////////////////////////////////////
-
-vector<passivedouble> CDriver::GetFlowLoad(unsigned short iMarker, unsigned long iVertex) const {
-  vector<su2double> FlowLoad(3, 0.0);
-  vector<passivedouble> FlowLoad_passive(3, 0.0);
-
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL];
-  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-
-  if (config_container[ZONE_0]->GetSolid_Wall(iMarker)) {
-    FlowLoad[0] = solver->GetVertexTractions(iMarker, iVertex, 0);
-    FlowLoad[1] = solver->GetVertexTractions(iMarker, iVertex, 1);
-    if (geometry->GetnDim() == 3)
-      FlowLoad[2] = solver->GetVertexTractions(iMarker, iVertex, 2);
-    else
-      FlowLoad[2] = 0.0;
-  }
-
-  FlowLoad_passive[0] = SU2_TYPE::GetValue(FlowLoad[0]);
-  FlowLoad_passive[1] = SU2_TYPE::GetValue(FlowLoad[1]);
-  FlowLoad_passive[2] = SU2_TYPE::GetValue(FlowLoad[2]);
-
-  return FlowLoad_passive;
-}
diff --git a/SU2_PY/FSI_tools/FSIInterface.py b/SU2_PY/FSI_tools/FSIInterface.py
index 88c030ff6a0..75e0b753b34 100644
--- a/SU2_PY/FSI_tools/FSIInterface.py
+++ b/SU2_PY/FSI_tools/FSIInterface.py
@@ -1464,7 +1464,7 @@ def getFluidInterfaceNodalForce(self, FSI_config, FluidSolver):
         for iVertex in range(self.nLocalFluidInterfaceNodes):
             GlobalIndex = FluidSolver.GetNodeGlobalIndex(FluidSolver.GetMarkerNode(self.fluidInterfaceIdentifier, iVertex))
             if GlobalIndex not in self.FluidHaloNodeList[myid].keys():
-              loadX, loadY, loadZ = FluidSolver.GetFlowLoad(self.fluidInterfaceIdentifier, iVertex)
+              loadX, loadY, loadZ = FluidSolver.GetMarkerFlowLoad(self.fluidInterfaceIdentifier, iVertex)
               iGlobalVertex = self.__getGlobalIndex('fluid', myid, localIndex)
               self.fluidLoads_array_X.setValues([iGlobalVertex], loadX)
               self.fluidLoads_array_Y.setValues([iGlobalVertex], loadY)
diff --git a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
index e254137fc27..520b54e4ca8 100755
--- a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
@@ -85,7 +85,7 @@ def main():
     comm.Barrier()
 
   # Define the load at the target vertex
-  SU2Driver.SetFEA_Loads(MarkerID,5,0,-0.005,0)
+  SU2Driver.SetMarkerCustomFEALoad(MarkerID, 5, (0, -0.005, 0))
 
   # Time iteration preprocessing
   SU2Driver.Preprocess(0)
diff --git a/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py b/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
index 2374bade7a7..0d79e9a6d42 100755
--- a/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
+++ b/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
@@ -110,7 +110,7 @@ def main():
     WallTemp = 293.0 + 57.0*sin(2*pi*time)
     # Set this temperature to all the vertices on the specified CHT marker
     for iVertex in range(nVertex_CHTMarker):
-      SU2Driver.SetVertexTemperature(CHTMarkerID, iVertex, WallTemp)
+      SU2Driver.SetMarkerCustomTemperature(CHTMarkerID, iVertex, WallTemp)
 
     # Tell the SU2 drive to update the boundary conditions
     SU2Driver.BoundaryConditionsUpdate()
diff --git a/TestCases/py_wrapper/translating_NACA0012/run_su2.py b/TestCases/py_wrapper/translating_NACA0012/run_su2.py
index 7d638c92b08..f184b8fd7f9 100644
--- a/TestCases/py_wrapper/translating_NACA0012/run_su2.py
+++ b/TestCases/py_wrapper/translating_NACA0012/run_su2.py
@@ -49,7 +49,7 @@ def save_forces(self):
             solver_marker_id = solver_marker_ids[marker]
             n_vertices = self.FluidSolver.GetNumberMarkerNodes(solver_marker_id)
             for i_vertex in range(n_vertices):
-                fxyz = self.FluidSolver.GetFlowLoad(solver_marker_id, i_vertex)
+                fxyz = self.FluidSolver.GetMarkerFlowLoad(solver_marker_id, i_vertex)
                 iPoint = self.FluidSolver.GetMarkerNode(solver_marker_id, i_vertex)
                 GlobalIndex = self.FluidSolver.GetNodeGlobalIndex(iPoint)
                 f.write('{}, {:.2f}, {:.2f}, {:.2f}\n'.format(GlobalIndex, fxyz[0], fxyz[1], fxyz[2]))

From e4c0eaf785fd575229ddbfa66e91e3d460b87e99 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 18 Mar 2023 21:48:11 -0700
Subject: [PATCH 299/656] remove unnecessary deletes in python scripts

---
 .../py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py      | 3 ---
 .../py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py     | 3 ---
 .../flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py      | 2 --
 .../flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py    | 2 --
 4 files changed, 10 deletions(-)

diff --git a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
index 6d11bfd33af..8a860bd562e 100755
--- a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
@@ -121,9 +121,6 @@ def main():
   # Postprocess the solver and exit cleanly
   SU2Driver.Postprocessing()
 
-  if SU2Driver != None:
-    del SU2Driver
-
 
 
 # -------------------------------------------------------------------
diff --git a/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
index 69e7baccc10..1bb933599ae 100755
--- a/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
@@ -118,9 +118,6 @@ def main():
   # Postprocess the solver and exit cleanly
   SU2Driver.Postprocessing()
 
-  if SU2Driver != None:
-    del SU2Driver
-
 
 
 # -------------------------------------------------------------------
diff --git a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
index 0efc10666df..608630d8b5f 100755
--- a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
+++ b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
@@ -137,8 +137,6 @@ def main():
   # Postprocess the solver and exit cleanly
   SU2Driver.Postprocessing()
 
-  if SU2Driver != None:
-    del SU2Driver
 
 # -------------------------------------------------------------------
 #  Run Main Program
diff --git a/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py b/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
index 0d79e9a6d42..9a96ead26e3 100755
--- a/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
+++ b/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
@@ -129,8 +129,6 @@ def main():
     TimeIter += 1
     time += deltaT
 
-  if SU2Driver != None:
-    del SU2Driver
 
 # -------------------------------------------------------------------
 #  Run Main Program

From 6330b6211da453218c2c330c4d8829ce9fba6ca2 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Sun, 19 Mar 2023 13:42:12 +0100
Subject: [PATCH 300/656] Further reduced MLP class dependence on SU2 code

---
 .../multilayer_perceptron/CIOMap.hpp          |  2 +-
 .../multilayer_perceptron/CLayer.hpp          |  6 +--
 .../multilayer_perceptron/CLookUp_ANN.hpp     | 15 +++++---
 .../multilayer_perceptron/CNeuralNetwork.hpp  |  9 ++---
 .../multilayer_perceptron/CNeuron.hpp         |  2 +-
 .../CReadNeuralNetwork.hpp                    |  2 +-
 .../multilayer_perceptron/CIOMap.cpp          |  4 +-
 .../multilayer_perceptron/CLookUp_ANN.cpp     | 38 ++++++++++---------
 .../multilayer_perceptron/CNeuralNetwork.cpp  |  2 +-
 .../CReadNeuralNetwork.cpp                    | 15 ++++----
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        |  3 +-
 11 files changed, 53 insertions(+), 45 deletions(-)

diff --git a/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp b/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
index dfc1b4b508c..7cb7bf3c782 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
@@ -33,7 +33,7 @@
 #include <string>
 #include <vector>
 
-#include "../../linear_algebra/blas_structure.hpp"
+#include "../../containers/C2DContainer.hpp"
 #include "CLookUp_ANN.hpp"
 
 namespace MLPToolbox {
diff --git a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
index 45e4304df4d..4171de0e2ba 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
@@ -30,9 +30,9 @@
 #include <cstdlib>
 #include <iostream>
 #include <limits>
+#include <vector>
 
-#include "../../CConfig.hpp"
-#include "../../linear_algebra/blas_structure.hpp"
+#include "../../containers/C2DContainer.hpp"
 #include "CNeuron.hpp"
 
 namespace MLPToolbox {
@@ -146,7 +146,7 @@ class CLayer {
    * \brief Get the activation function name applied to this layer
    * \return name of the activation function
    */
-  string GetActivationType() const { return activation_type; }
+  std::string GetActivationType() const { return activation_type; }
 };
 
 }  // namespace MLPToolbox
diff --git a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
index dc5b51f60e3..8dc74de9c3e 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
@@ -34,8 +34,7 @@
 #include <string>
 #include <vector>
 
-#include "../../CConfig.hpp"
-#include "../../linear_algebra/blas_structure.hpp"
+#include "../../containers/C2DContainer.hpp"
 #include "CIOMap.hpp"
 #include "CNeuralNetwork.hpp"
 
@@ -53,7 +52,6 @@ class CLookUp_ANN {
    */
 
  private:
-  int rank{0};
   su2vector<CNeuralNetwork> NeuralNetworks; /*!< std::vector containing all loaded neural networks. */
 
   unsigned short number_of_variables; /*!< Number of loaded ANNs. */
@@ -108,9 +106,14 @@ class CLookUp_ANN {
    * \param[in] variable_names - variable names to map to ANN inputs or outputs
    * \param[in] input - map to inputs (true) or outputs (false)
    */
-  std::vector<pair<std::size_t, std::size_t>> FindVariableIndices(std::size_t i_ANN,
-                                                                  su2vector<std::string> variable_names,
-                                                                  bool input) const;
+  std::vector<std::pair<std::size_t, std::size_t>> FindVariableIndices(std::size_t i_ANN,
+                                                                       su2vector<std::string> variable_names,
+                                                                       bool input) const;
+
+  /*!
+   * \brief Display architectural information on the loaded MLPs
+   */
+  void DisplayNetworkInfo() const;
 };
 
 }  // namespace MLPToolbox
\ No newline at end of file
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
index 9961a2a7d7c..a6001b2dace 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
@@ -34,8 +34,7 @@
 #include <limits>
 #include <map>
 
-#include "../../CConfig.hpp"
-#include "../../linear_algebra/blas_structure.hpp"
+#include "../../containers/C2DContainer.hpp"
 #include "CLayer.hpp"
 
 namespace MLPToolbox {
@@ -104,7 +103,7 @@ class CNeuralNetwork {
 
   su2vector<ENUM_ACTIVATION_FUNCTION>
       activation_function_types;               /*!< Activation function type for each layer in the network. */
-  su2vector<string> activation_function_names; /*!< Activation function name for each layer in the network. */
+  su2vector<std::string> activation_function_names; /*!< Activation function name for each layer in the network. */
 
  public:
   ~CNeuralNetwork() {
@@ -213,7 +212,7 @@ class CNeuralNetwork {
    * \param[in] input_max - Maximum input value.
    */
   void SetInputNorm(unsigned long iInput, su2double input_min, su2double input_max) {
-    input_norm[iInput] = make_pair(input_min, input_max);
+    input_norm[iInput] = std::make_pair(input_min, input_max);
   }
 
   /*!
@@ -223,7 +222,7 @@ class CNeuralNetwork {
    * \param[in] input_max - Maximum output value.
    */
   void SetOutputNorm(unsigned long iOutput, su2double output_min, su2double output_max) {
-    output_norm[iOutput] = make_pair(output_min, output_max);
+    output_norm[iOutput] = std::make_pair(output_min, output_max);
   }
 
   std::pair<su2double, su2double> GetInputNorm(unsigned long iInput) const { return input_norm[iInput]; }
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
index 03c7a4d3212..da37e3cbe18 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
@@ -31,7 +31,7 @@
 #include <iostream>
 #include <limits>
 
-#include "../../CConfig.hpp"
+#include "../../containers/C2DContainer.hpp"
 
 namespace MLPToolbox {
 class CNeuron {
diff --git a/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
index af5657f0f78..9408a130578 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
@@ -32,7 +32,7 @@
 #include <limits>
 #include <vector>
 
-#include "../../CConfig.hpp"
+#include "../../containers/C2DContainer.hpp"
 namespace MLPToolbox {
 
 class CReadNeuralNetwork {
diff --git a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
index a53247b7c5a..e81f589c919 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
@@ -61,13 +61,13 @@ void MLPToolbox::CIOMap::PairVariableswithMLPs(CLookUp_ANN* MLP_collection, su2v
   // Looping over the loaded MLPs to check wether the MLP inputs match with the call inputs
   for (size_t iMLP = 0; iMLP < MLP_collection->GetNANNs(); iMLP++) {
     // Mapped call inputs to MLP inputs
-    std::vector<pair<size_t, size_t>> Input_Indices = MLP_collection->FindVariableIndices(iMLP, inputs, true);
+    std::vector<std::pair<size_t, size_t>> Input_Indices = MLP_collection->FindVariableIndices(iMLP, inputs, true);
     isInput = Input_Indices.size() > 0;
 
     if (isInput) {
       // Only when the MLP inputs match with a portion of the call inputs are the output variable checks performed
 
-      std::vector<pair<size_t, size_t>> Output_Indices = MLP_collection->FindVariableIndices(iMLP, outputs, false);
+      std::vector<std::pair<size_t, size_t>> Output_Indices = MLP_collection->FindVariableIndices(iMLP, outputs, false);
       isOutput = Output_Indices.size() > 0;
 
       if (isOutput) {
diff --git a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
index 2f8281bdb4c..7a65e5a1b59 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
@@ -39,27 +39,14 @@
 using namespace std;
 
 MLPToolbox::CLookUp_ANN::CLookUp_ANN(const unsigned short n_inputs, const string* input_filenames) {
-#ifdef HAVE_MPI
-  MPI_Comm_rank(MPI_COMM_WORLD, &rank);
-#endif
-  if (rank == MASTER_NODE) cout << "Generating ANN collection" << endl;
-
+  /*--- Define collection of MLPs for regression purposes ---*/
   number_of_variables = n_inputs;
 
   NeuralNetworks.resize(n_inputs);
-  
-  if (rank == MASTER_NODE) {
-    cout << setfill(' ');
-    cout << endl;
-    cout << "+------------------------------------------------------------------+\n";
-    cout << "|                 Multi-Layer Perceptron (MLP) info                |\n";
-    cout << "+------------------------------------------------------------------+" << endl;
-  }
 
+  /*--- Generate an MLP for every filename provided ---*/
   for (auto i_MLP = 0u; i_MLP < n_inputs; i_MLP++) {
-    if (rank == MASTER_NODE) cout << "Generating neural network for " << input_filenames[i_MLP] << endl;
     GenerateANN(NeuralNetworks[i_MLP], input_filenames[i_MLP]);
-    if (rank == MASTER_NODE) NeuralNetworks[i_MLP].DisplayNetwork();
   }
 }
 
@@ -217,10 +204,11 @@ bool MLPToolbox::CLookUp_ANN::CheckUseOfInputs(su2vector<string>& input_names, C
       inputs_are_present = false;
     };
   }
+  /*--- Raise error if input variables are missing ---*/
   if (missing_inputs.size() > 0) {
     string message{"Inputs "};
     for (size_t iVar = 0; iVar < missing_inputs.size(); iVar++) message += missing_inputs[iVar] + " ";
-    SU2_MPI::Error(message + "are not present in any loaded ANN.", CURRENT_FUNCTION);
+    throw std::invalid_argument(message + "are not present in any loaded ANN.");
   }
   return inputs_are_present;
 }
@@ -248,10 +236,26 @@ bool MLPToolbox::CLookUp_ANN::CheckUseOfOutputs(su2vector<string>& output_names,
       outputs_are_present = false;
     };
   }
+  /*--- Raise error if any outputs are missing ---*/
   if (missing_outputs.size() > 0) {
     string message{"Outputs "};
     for (size_t iVar = 0; iVar < missing_outputs.size(); iVar++) message += missing_outputs[iVar] + " ";
-    SU2_MPI::Error(message + "are not present in any loaded ANN.", CURRENT_FUNCTION);
+    throw std::invalid_argument( message + "are not present in any loaded ANN.");
   }
   return outputs_are_present;
+}
+
+void MLPToolbox::CLookUp_ANN::DisplayNetworkInfo() const {
+  /*--- Display network information on the loaded MLPs ---*/
+
+  cout << setfill(' ');
+  cout << endl;
+  cout << "+------------------------------------------------------------------+\n";
+  cout << "|                 Multi-Layer Perceptron (MLP) info                |\n";
+  cout << "+------------------------------------------------------------------+" << endl;
+
+  /* For every loaded MLP, display the inputs, outputs, activation functions, and architecture. */
+  for (auto i_MLP = 0u; i_MLP < NeuralNetworks.size(); i_MLP++) {
+    NeuralNetworks[i_MLP].DisplayNetwork();
+  }
 }
\ No newline at end of file
diff --git a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
index a45c2d749fa..9c98dcc5fe2 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
@@ -197,7 +197,7 @@ void MLPToolbox::CNeuralNetwork::Predict(su2vector<su2double>& inputs, bool comp
           for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
             x = total_layers[iLayer]->GetInput(iNeuron);
 
-            y = 0.5 * x * (1 + tanh(sqrt(2 / PI_NUMBER) * (x + 0.044715 * pow(x, 3))));
+            y = 0.5 * x * (1 + tanh(0.7978845608028654 * (x + 0.044715 * pow(x, 3))));
             total_layers[iLayer]->SetOutput(iNeuron, y);
             if (compute_gradient) {
               dy_dx = 0.5 * (tanh(0.0356774 * pow(x, 3) + 0.797885 * x) + (0.107032 * pow(x, 3) + 0.797885 * x) *
diff --git a/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
index ced1a17a518..7790229b532 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
@@ -26,7 +26,8 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 #include "../../../include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp"
-
+#include <iostream>
+#include <fstream>
 using namespace std;
 
 MLPToolbox::CReadNeuralNetwork::CReadNeuralNetwork(string filename_in) { filename = filename_in; }
@@ -35,7 +36,7 @@ void MLPToolbox::CReadNeuralNetwork::ReadMLPFile() {
   ifstream file_stream;
   file_stream.open(filename.c_str(), ifstream::in);
   if (!file_stream.is_open()) {
-    SU2_MPI::Error(string("There is no MLP file called ") + filename, CURRENT_FUNCTION);
+    throw std::invalid_argument( "There is no MLP file called " + filename);
   }
 
   string line, word;
@@ -62,7 +63,7 @@ void MLPToolbox::CReadNeuralNetwork::ReadMLPFile() {
     if (line.compare("[neurons per layer]") == 0) {
       /* In case layer count was not yet provided, return an error */
       if (!found_layercount) {
-        SU2_MPI::Error("No layer count provided before defining neuron count per layer", CURRENT_FUNCTION);
+        throw std::invalid_argument( "No layer count provided before defining neuron count per layer");
       }
       /* Loop over layer count and size neuron count and bias count per layer accordingly */
       for (auto iLayer = 0u; iLayer < n_layers; iLayer++) {
@@ -86,7 +87,7 @@ void MLPToolbox::CReadNeuralNetwork::ReadMLPFile() {
     /* Read layer activation function types */
     if (line.compare("[activation function]") == 0) {
       if (!found_layercount) {
-        SU2_MPI::Error("No layer count provided before providing layer activation functions", CURRENT_FUNCTION);
+        throw std::invalid_argument( "No layer count provided before providing layer activation functions" );
       }
       for (auto iLayer = 0u; iLayer < n_layers; iLayer++) {
         getline(file_stream, line);
@@ -132,7 +133,7 @@ void MLPToolbox::CReadNeuralNetwork::ReadMLPFile() {
       }
 
       if (output_names.size() != (n_neurons[n_neurons.size() - 1])) {
-        SU2_MPI::Error("Number of output variable names inconsistent with number of MLP outputs", CURRENT_FUNCTION);
+        throw std::invalid_argument("No layer count provided before providing layer activation functions");
       }
     }
 
@@ -158,10 +159,10 @@ void MLPToolbox::CReadNeuralNetwork::ReadMLPFile() {
 
   /* Error checking */
   if (!found_input_names) {
-    SU2_MPI::Error("No MLP input variable names provided", CURRENT_FUNCTION);
+    throw std::invalid_argument("No MLP input variable names provided");
   }
   if (!found_output_names) {
-    SU2_MPI::Error("No MLP output variable names provided", CURRENT_FUNCTION);
+    throw std::invalid_argument("No MLP input variable names provided");
   }
 
   /* Read weights for each layer */
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index e76c01013bd..03e47f8c07a 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -37,6 +37,7 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
   switch (Kind_DataDriven_Method) {
     case ENUM_DATADRIVEN_METHOD::MLP:
       lookup_mlp = new MLPToolbox::CLookUp_ANN(config->GetNDataDriven_Files(), config->GetDataDriven_FileNames());
+      if (rank == MASTER_NODE) lookup_mlp->DisplayNetworkInfo();
       break;
     case ENUM_DATADRIVEN_METHOD::LUT:
       lookup_table = new CLookUpTable(config->GetDataDriven_Filename(), "Density", "Energy");
@@ -47,7 +48,7 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
 
   /*--- Relaxation factor and tolerance for Newton solvers. ---*/
   Newton_Relaxation = config->GetRelaxation_DataDriven();
-  Newton_Tolerance = 2e-10;
+  Newton_Tolerance = 1e-10;
   MaxIter_Newton = 50;
 
   /*--- Preprocessing of inputs and outputs for the interpolation method. ---*/

From d1992b21226269c2847f938dac99186aba49d68a Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 20 Mar 2023 10:36:19 +0100
Subject: [PATCH 301/656] Rebased with develop

---
 externals/codi | 2 +-
 externals/medi | 2 +-
 externals/opdi | 2 +-
 3 files changed, 3 insertions(+), 3 deletions(-)

diff --git a/externals/codi b/externals/codi
index 96ac78ec5bc..427c2dc754a 160000
--- a/externals/codi
+++ b/externals/codi
@@ -1 +1 @@
-Subproject commit 96ac78ec5bcc5ac25b785e79b16ed76fca22d736
+Subproject commit 427c2dc754a628ad3c9310c766c988ac5ce21bc7
diff --git a/externals/medi b/externals/medi
index 6aef76912e7..aafc2d1966b 160000
--- a/externals/medi
+++ b/externals/medi
@@ -1 +1 @@
-Subproject commit 6aef76912e7099c4f08c9705848797ca9e8070da
+Subproject commit aafc2d1966ba1233640af737e71c77c1a86183fd
diff --git a/externals/opdi b/externals/opdi
index 1aabf5bd1ed..f33b507c24f 160000
--- a/externals/opdi
+++ b/externals/opdi
@@ -1 +1 @@
-Subproject commit 1aabf5bd1ed77611742eb655002f2ac7a3dddef9
+Subproject commit f33b507c24f7448d4cf4df16ab5c53ea254b8774

From d169234ffafc2355a34a0e013a4140bee42dcf13 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Mon, 20 Mar 2023 02:37:30 -0700
Subject: [PATCH 302/656] cleanup adjoint accessors

---
 SU2_CFD/include/drivers/CDriver.hpp           |  43 -------
 SU2_CFD/include/drivers/CDriverBase.hpp       | 108 ++++++++++++++++--
 SU2_CFD/src/drivers/CDriverBase.cpp           |   8 +-
 SU2_CFD/src/python_wrapper_structure.cpp      |  84 --------------
 SU2_PY/FSI_tools/FSIInterface.py              |   4 +-
 .../deforming_bump_in_channel/run.py          |   2 +-
 .../flow_load_sens/run_adjoint.py             |   2 +-
 .../mesh_disp_sens/run_adjoint.py             |   2 +-
 .../launch_flatPlate_rigidMotion.py           |   2 +-
 9 files changed, 109 insertions(+), 146 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index a84d3471c15..ab9e9b60052 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -498,49 +498,6 @@ class CDriver : public CDriverBase {
    */
   vector<string> GetInletMarkerTags() const;
 
-  /*!
-   * \brief Return the sensitivities of the mesh boundary vertices.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \return Vector of sensitivities.
-   */
-  vector<passivedouble> GetMeshDisp_Sensitivity(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Get the sensitivity of the flow loads for the structural solver.
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \param[in] LoadX - Value of the load in the direction X.
-   * \param[in] LoadX - Value of the load in the direction Y.
-   * \param[in] LoadX - Value of the load in the direction Z.
-   */
-  vector<passivedouble> GetFlowLoad_Sensitivity(unsigned short iMarker, unsigned long iVertex) const;
-
-  /*!
-   * \brief Set the adjoint of the flow tractions (from the extra step -
-   * the repeated methods should be unified once the postprocessing strategy is in place).
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \param[in] val_AdjointX - Value of the adjoint in the direction X.
-   * \param[in] val_AdjointY - Value of the adjoint in the direction Y.
-   * \param[in] val_AdjointZ - Value of the adjoint in the direction Z.
-   */
-  void SetFlowLoad_Adjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
-                           passivedouble val_AdjointY, passivedouble val_AdjointZ);
-
-  /*!
-   * \brief Set the adjoint of the structural displacements (from an outside source)
-   * \param[in] iMarker - Marker identifier.
-   * \param[in] iVertex - Vertex identifier.
-   * \param[in] val_AdjointX - Value of the adjoint in the direction X.
-   * \param[in] val_AdjointY - Value of the adjoint in the direction Y.
-   * \param[in] val_AdjointZ - Value of the adjoint in the direction Z.
-   */
-  void SetSourceTerm_DispAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
-                                 passivedouble val_AdjointY, passivedouble val_AdjointZ);
-  void SetSourceTerm_VelAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
-                                passivedouble val_AdjointY, passivedouble val_AdjointZ);
-
   /*!
    * \brief Set the position of the heat source.
    * \param[in] alpha - Angle of rotation respect to Z axis.
diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index 9182eb5ca40..a34ebe98b11 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -318,15 +318,15 @@ class CDriverBase {
    * \param[in] iVertex - Marker vertex index.
    * \return Node displacements (nDim).
    */
-  vector<passivedouble> GetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex) const;
+  vector<passivedouble> GetMarkerDisplacement(unsigned short iMarker, unsigned long iVertex) const;
 
   /*!
-   * \brief Set the displacements of a marker vertex.
+   * \brief Set the mesh displacements of a marker vertex.
    * \param[in] iMarker - Marker index.
    * \param[in] iVertex - Marker vertex index.
    * \param[in] values - Node displacements (nDim).
    */
-  void SetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values);
+  void SetMarkerCustomDisplacement(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values);
 
   /*!
    * \brief Get the velocities of a marker vertex.
@@ -334,7 +334,7 @@ class CDriverBase {
    * \param[in] iVertex - Marker vertex index.
    * \return Node velocities (nDim).
    */
-  vector<passivedouble> GetMarkerVelocities(unsigned short iMarker, unsigned long iVertex) const;
+  vector<passivedouble> GetMarkerMeshVelocity(unsigned short iMarker, unsigned long iVertex) const;
 
   /*!
    * \brief Set the velocities of a marker vertex.
@@ -342,7 +342,7 @@ class CDriverBase {
    * \param[in] iVertex - Marker vertex index.
    * \param[in] values - Node velocities (nDim).
    */
-  void SetMarkerVelocities(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values);
+  void SetMarkerCustomMeshVelocity(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values);
 
   /*!
    * \brief Communicate the boundary mesh displacements.
@@ -452,13 +452,14 @@ class CDriverBase {
    */
   inline passivedouble GetMarkerNormalHeatFlux(unsigned short iSolver, unsigned short iMarker, unsigned long iVertex) const {
     if (iSolver != HEAT_SOL && iSolver != FLOW_SOL) {
-      SU2_MPI::Error("Normal heat flux is only available for flow or heat solvers.");
+      SU2_MPI::Error("Normal heat flux is only available for flow or heat solvers.", CURRENT_FUNCTION);
     }
     return SU2_TYPE::GetValue(GetSolverAndCheckMarker(iSolver, iMarker)->GetHeatFlux(iMarker, iVertex));
   }
 
   /*!
    * \brief Sets the nodal force for the structural solver at a vertex of a marker.
+   * \note This can be the input of the FEA solver in an FSI setting.
    * \param[in] iMarker - Marker identifier.
    * \param[in] iVertex - Vertex identifier.
    * \param[in] force - Force vector.
@@ -468,15 +469,17 @@ class CDriverBase {
     std::array<su2double, 3> load{};
     for (auto iDim = 0u; iDim < GetNumberDimensions(); ++iDim) load[iDim] = force[iDim];
     const auto iPoint = GetMarkerNode(iMarker, iVertex);
-    solver->GetNodes()->Set_FlowTraction(iPoint, load);
+    solver->GetNodes()->Set_FlowTraction(iPoint, load.data());
   }
 
   /*!
    * \brief Get the fluid force at a vertex of a solid wall marker of the flow solver.
+   * \note This can be the output of the flow solver in an FSI setting to then apply it to a structural solver.
    * \param[in] iMarker - Marker identifier.
    * \param[in] iVertex - Vertex identifier.
+   * \return Vector of loads.
    */
-  vector<passivedouble> GetMarkerFlowLoad(unsigned short iMarker, unsigned long iVertex) const {
+  inline vector<passivedouble> GetMarkerFlowLoad(unsigned short iMarker, unsigned long iVertex) const {
     vector<passivedouble> FlowLoad(GetNumberDimensions(), 0.0);
     const auto* solver = GetSolverAndCheckMarker(FLOW_SOL, iMarker);
 
@@ -488,6 +491,93 @@ class CDriverBase {
     return FlowLoad;
   }
 
+  /*!
+   * \brief Set the adjoint of the flow tractions of the flow solver.
+   * \note This can be the input of the flow solver in an adjoint FSI setting.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \param[in] adjointLoad - Vector of adjoint loads.
+   */
+  inline void SetMarkerCustomFlowLoadAdjoint(unsigned short iMarker, unsigned long iVertex,
+                                             vector<passivedouble> adjointLoad) {
+    auto* solver = GetSolverAndCheckMarker(FLOW_SOL, iMarker);
+    for (auto iDim = 0u; iDim < GetNumberDimensions(); ++iDim) {
+      solver->StoreVertexTractionsAdjoint(iMarker, iVertex, iDim, adjointLoad[iDim]);
+    }
+  }
+
+  /*!
+   * \brief Get the sensitivities of the displacements of the mesh boundary vertices.
+   * \note This can be the output of the flow solver in an adjoint FSI setting.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \return Vector of sensitivities.
+   */
+  inline vector<passivedouble> GetMarkerDisplacementSensitivity(unsigned short iMarker, unsigned long iVertex) const {
+    const auto nDim = GetNumberDimensions();
+    const auto iPoint = GetMarkerNode(iMarker, iVertex);
+    auto* nodes = GetSolverAndCheckMarker(ADJMESH_SOL)->GetNodes();
+
+    vector<passivedouble> sens(nDim, 0.0);
+    for (auto iDim = 0u; iDim < nDim; ++iDim) {
+      sens[iDim] = SU2_TYPE::GetValue(nodes->GetBoundDisp_Sens(iPoint, iDim));
+    }
+    return sens;
+  }
+
+  /*!
+   * \brief Get the sensitivity of the FEA loads of the structural solver (via the adjoint structural solver).
+   * \note This can be the output of the FEA solver in an adjoint FSI setting.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \returns Vector of sensitivities.
+   */
+  inline vector<passivedouble> GetMarkerFEALoadSensitivity(unsigned short iMarker, unsigned long iVertex) const {
+    const auto nDim = GetNumberDimensions();
+    const auto iPoint = GetMarkerNode(iMarker, iVertex);
+    auto* nodes = GetSolverAndCheckMarker(ADJFEA_SOL)->GetNodes();
+
+    vector<passivedouble> sens(nDim, 0.0);
+    for (auto iDim = 0u; iDim < nDim; ++iDim) {
+      sens[iDim] = SU2_TYPE::GetValue(nodes->GetFlowTractionSensitivity(iPoint, iDim));
+    }
+    return sens;
+  }
+
+  /*!
+   * \brief Set the adjoint of the structural displacements.
+   * \note This can be the input of the FEA solver in an adjoint FSI setting.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \param[in] adjointDisplacement - Vector of adjoint displacements.
+   */
+  inline void SetMarkerCustomFEADisplacementAdjoint(unsigned short iMarker, unsigned long iVertex,
+                                                    vector<passivedouble> adjointDisplacement) {
+    const auto iPoint = GetMarkerNode(iMarker, iVertex);
+    auto* nodes = GetSolverAndCheckMarker(ADJFEA_SOL)->GetNodes();
+
+    for (auto iDim = 0u; iDim < GetNumberDimensions(); ++iDim) {
+      nodes->SetSourceTerm_DispAdjoint(iPoint, iDim, adjointDisplacement[iDim]);
+    }
+  }
+
+  /*!
+   * \brief Set the adjoint of the structural velocities.
+   * \note This can be the input of the FEA solver in an unsteady adjoint FSI setting.
+   * \param[in] iMarker - Marker identifier.
+   * \param[in] iVertex - Vertex identifier.
+   * \param[in] adjointVelocity - Vector of adjoint velocities.
+   */
+  inline void SetMarkerCustomFEAVelocityAdjoint(unsigned short iMarker, unsigned long iVertex,
+                                                vector<passivedouble> adjointVelocity) {
+    const auto iPoint = GetMarkerNode(iMarker, iVertex);
+    auto* nodes = GetSolverAndCheckMarker(ADJFEA_SOL)->GetNodes();
+
+    for (auto iDim = 0u; iDim < GetNumberDimensions(); ++iDim) {
+      nodes->SetSourceTerm_VelAdjoint(iPoint, iDim, adjointVelocity[iDim]);
+    }
+  }
+
 /// \}
 
  protected:
@@ -495,7 +585,7 @@ class CDriverBase {
    * \brief Automates some boilerplate of accessing solution fields for the python wrapper.
    */
   inline CSolver* GetSolverAndCheckMarker(unsigned short iSolver,
-                                          unsigned short iMarker = std::numeric_limits<unsigned short>::max()) {
+                                          unsigned short iMarker = std::numeric_limits<unsigned short>::max()) const {
     if (iMarker < std::numeric_limits<unsigned short>::max() && iMarker > GetNumberMarkers()) {
       SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
     }
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index 76ce8c42f5a..03d72e2d0d8 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -360,7 +360,7 @@ vector<passivedouble> CDriverBase::GetMarkerVertexNormals(unsigned short iMarker
   return values;
 }
 
-vector<passivedouble> CDriverBase::GetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex) const {
+vector<passivedouble> CDriverBase::GetMarkerDisplacement(unsigned short iMarker, unsigned long iVertex) const {
   vector<passivedouble> values(nDim, 0.0);
 
   if (main_config->GetDeform_Mesh()) {
@@ -373,7 +373,7 @@ vector<passivedouble> CDriverBase::GetMarkerDisplacements(unsigned short iMarker
   return values;
 }
 
-void CDriverBase::SetMarkerDisplacements(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
+void CDriverBase::SetMarkerCustomDisplacement(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
   if (!main_config->GetDeform_Mesh()) {
     SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
   }
@@ -387,7 +387,7 @@ void CDriverBase::SetMarkerDisplacements(unsigned short iMarker, unsigned long i
   }
 }
 
-vector<passivedouble> CDriverBase::GetMarkerVelocities(unsigned short iMarker, unsigned long iVertex) const {
+vector<passivedouble> CDriverBase::GetMarkerMeshVelocity(unsigned short iMarker, unsigned long iVertex) const {
   vector<passivedouble> values(nDim, 0.0);
 
   if (main_config->GetDeform_Mesh()) {
@@ -400,7 +400,7 @@ vector<passivedouble> CDriverBase::GetMarkerVelocities(unsigned short iMarker, u
   return values;
 }
 
-void CDriverBase::SetMarkerVelocities(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
+void CDriverBase::SetMarkerCustomMeshVelocity(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
   if (!main_config->GetDeform_Mesh()) {
     SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
   }
diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index f93a116636e..6e089b600a1 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -309,87 +309,3 @@ void CDriver::BoundaryConditionsUpdate() {
     geometry_container[iZone][INST_0][MESH_0]->UpdateCustomBoundaryConditions(geometry_container[iZone][INST_0],config_container[iZone]);
   }
 }
-
-////////////////////////////////////////////////////////////////////////////////
-/* Functions related to adjoint simulations                                   */
-////////////////////////////////////////////////////////////////////////////////
-
-vector<passivedouble> CDriver::GetMeshDisp_Sensitivity(unsigned short iMarker, unsigned long iVertex) const {
-  unsigned long iPoint;
-  vector<su2double> Disp_Sens(3, 0.0);
-  vector<passivedouble> Disp_Sens_passive(3, 0.0);
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][ADJMESH_SOL];
-  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-
-  Disp_Sens[0] = solver->GetNodes()->GetBoundDisp_Sens(iPoint, 0);
-  Disp_Sens[1] = solver->GetNodes()->GetBoundDisp_Sens(iPoint, 1);
-  if (geometry->GetnDim() == 3)
-    Disp_Sens[2] = solver->GetNodes()->GetBoundDisp_Sens(iPoint, 2);
-  else
-    Disp_Sens[2] = 0.0;
-
-  Disp_Sens_passive[0] = SU2_TYPE::GetValue(Disp_Sens[0]);
-  Disp_Sens_passive[1] = SU2_TYPE::GetValue(Disp_Sens[1]);
-  Disp_Sens_passive[2] = SU2_TYPE::GetValue(Disp_Sens[2]);
-
-  return Disp_Sens_passive;
-}
-
-vector<passivedouble> CDriver::GetFlowLoad_Sensitivity(unsigned short iMarker, unsigned long iVertex) const {
-  unsigned long iPoint;
-  vector<su2double> FlowLoad_Sens(3, 0.0);
-  vector<passivedouble> FlowLoad_Sens_passive(3, 0.0);
-
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
-  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-
-  FlowLoad_Sens[0] = solver->GetNodes()->GetFlowTractionSensitivity(iPoint, 0);
-  FlowLoad_Sens[1] = solver->GetNodes()->GetFlowTractionSensitivity(iPoint, 1);
-  if (geometry->GetnDim() == 3)
-    FlowLoad_Sens[2] = solver->GetNodes()->GetFlowTractionSensitivity(iPoint, 2);
-  else
-    FlowLoad_Sens[2] = 0.0;
-
-  FlowLoad_Sens_passive[0] = SU2_TYPE::GetValue(FlowLoad_Sens[0]);
-  FlowLoad_Sens_passive[1] = SU2_TYPE::GetValue(FlowLoad_Sens[1]);
-  FlowLoad_Sens_passive[2] = SU2_TYPE::GetValue(FlowLoad_Sens[2]);
-
-  return FlowLoad_Sens_passive;
-}
-
-void CDriver::SetFlowLoad_Adjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
-                                  passivedouble val_AdjointY, passivedouble val_AdjointZ) {
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL];
-  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-
-  solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 0, val_AdjointX);
-  solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 1, val_AdjointY);
-  if (geometry->GetnDim() == 3) solver->StoreVertexTractionsAdjoint(iMarker, iVertex, 2, val_AdjointZ);
-}
-
-void CDriver::SetSourceTerm_DispAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
-                                        passivedouble val_AdjointY, passivedouble val_AdjointZ) {
-  unsigned long iPoint;
-
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
-  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-  iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-
-  solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 0, val_AdjointX);
-  solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 1, val_AdjointY);
-  if (geometry->GetnDim() == 3) solver->GetNodes()->SetSourceTerm_DispAdjoint(iPoint, 2, val_AdjointZ);
-}
-
-void CDriver::SetSourceTerm_VelAdjoint(unsigned short iMarker, unsigned long iVertex, passivedouble val_AdjointX,
-                                       passivedouble val_AdjointY, passivedouble val_AdjointZ) {
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][ADJFEA_SOL];
-  CGeometry* geometry = geometry_container[ZONE_0][INST_0][MESH_0];
-  const auto iPoint = geometry_container[ZONE_0][INST_0][MESH_0]->vertex[iMarker][iVertex]->GetNode();
-
-  solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 0, val_AdjointX);
-  solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 1, val_AdjointY);
-  if (geometry->GetnDim() == 3) solver->GetNodes()->SetSourceTerm_VelAdjoint(iPoint, 2, val_AdjointZ);
-}
diff --git a/SU2_PY/FSI_tools/FSIInterface.py b/SU2_PY/FSI_tools/FSIInterface.py
index 67fb51f9eb1..7711a8b3707 100644
--- a/SU2_PY/FSI_tools/FSIInterface.py
+++ b/SU2_PY/FSI_tools/FSIInterface.py
@@ -2082,7 +2082,7 @@ def setFluidInterfaceVarCoord(self, FluidSolver):
             )
             if GlobalIndex in self.FluidHaloNodeList[myid].keys():
                 DispX, DispY, DispZ = self.haloNodesDisplacements[GlobalIndex]
-                FluidSolver.SetMarkerDisplacements(
+                FluidSolver.SetMarkerCustomDisplacement(
                     self.fluidInterfaceIdentifier,
                     int(iVertex),
                     np.array([DispX, DispY, DispZ]),
@@ -2091,7 +2091,7 @@ def setFluidInterfaceVarCoord(self, FluidSolver):
                 DispX = self.localFluidInterface_array_DispX[localIndex]
                 DispY = self.localFluidInterface_array_DispY[localIndex]
                 DispZ = self.localFluidInterface_array_DispZ[localIndex]
-                FluidSolver.SetMarkerDisplacements(
+                FluidSolver.SetMarkerCustomDisplacement(
                     self.fluidInterfaceIdentifier,
                     int(iVertex),
                     np.array([DispX, DispY, DispZ]),
diff --git a/TestCases/py_wrapper/deforming_bump_in_channel/run.py b/TestCases/py_wrapper/deforming_bump_in_channel/run.py
index 715e81c1cea..36bf97d34e1 100755
--- a/TestCases/py_wrapper/deforming_bump_in_channel/run.py
+++ b/TestCases/py_wrapper/deforming_bump_in_channel/run.py
@@ -67,7 +67,7 @@ def main():
     # Apply the surface deformation.
     for iVertex in range(nVertex):
       dy = np.real(DeformFunction(CoordX[iVertex] - 0.9, time))
-      SU2Driver.SetMarkerDisplacements(MarkerID, iVertex, (0.0, dy))
+      SU2Driver.SetMarkerCustomDisplacement(MarkerID, iVertex, (0.0, dy))
 
     # Time iteration preprocessing.
     SU2Driver.Preprocess(TimeIter)
diff --git a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
index 8a860bd562e..d5829bd9184 100755
--- a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
@@ -109,7 +109,7 @@ def main():
     disp=[]
 
     # Recover the sensitivity
-    sens.append(SU2Driver.GetFlowLoad_Sensitivity(MarkerID,5))
+    sens.append(SU2Driver.GetMarkerFEALoadSensitivity(MarkerID, 5))
 
     fea_sol = SU2Driver.GetSolverIndices()["FEA"]
     marker_disp = SU2Driver.MarkerSolution(fea_sol, MarkerID)
diff --git a/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
index 1bb933599ae..b3f5d2decad 100755
--- a/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
@@ -110,7 +110,7 @@ def main():
   # Sensitivities of the marker
   print("\n------------------------------ Sensitivities -----------------------------\n")
   for iVertex in range(nVertex_Marker):
-    sensX, sensY, sensZ = SU2Driver.GetMeshDisp_Sensitivity(MarkerID, iVertex)
+    sensX, sensY, sensZ = SU2Driver.GetMarkerDisplacementSensitivity(MarkerID, iVertex)
 
     if (iVertex == 30) and rank == 0:
       print(1000,1000,iVertex, sensX, sensY, sensZ)
diff --git a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
index 608630d8b5f..112d5d9a14b 100755
--- a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
+++ b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
@@ -115,7 +115,7 @@ def main():
     value = 0.0, 0.0175*sin(2*pi*time)
 
     for iVertex in range(nVertex_MovingMarker):
-      SU2Driver.SetMarkerDisplacements(MovingMarkerID, int(iVertex), value)
+      SU2Driver.SetMarkerCustomDisplacement(MovingMarkerID, int(iVertex), value)
 
     # Time iteration preprocessing
     SU2Driver.Preprocess(TimeIter)

From 87e5d66b8b9b5a3356f0292720d50a00bc4111df Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 20 Mar 2023 13:41:10 +0100
Subject: [PATCH 303/656] Improved formatting of MLP classes

---
 .../toolboxes/multilayer_perceptron/CIOMap.hpp   |  2 +-
 .../multilayer_perceptron/CLookUp_ANN.hpp        |  2 +-
 .../multilayer_perceptron/CNeuralNetwork.hpp     |  2 +-
 .../toolboxes/multilayer_perceptron/CNeuron.hpp  |  2 +-
 .../multilayer_perceptron/CReadNeuralNetwork.hpp |  2 +-
 Common/src/toolboxes/meson.build                 |  1 -
 .../toolboxes/multilayer_perceptron/CIOMap.cpp   |  2 +-
 .../toolboxes/multilayer_perceptron/CLayer.cpp   |  2 +-
 .../multilayer_perceptron/CLookUp_ANN.cpp        |  2 +-
 .../multilayer_perceptron/CReadNeuralNetwork.cpp |  2 +-
 .../multilayer_perceptron/simple_mlp.mlp         | 16 ++++++++--------
 config_template.cfg                              |  8 ++++----
 externals/codi                                   |  2 +-
 externals/medi                                   |  2 +-
 externals/opdi                                   |  2 +-
 15 files changed, 24 insertions(+), 25 deletions(-)

diff --git a/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp b/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
index 7cb7bf3c782..5263823b460 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
@@ -187,4 +187,4 @@ class CIOMap
     return MLP_input;
   }
 };
-}  // namespace MLPToolbox
\ No newline at end of file
+}  // namespace MLPToolbox
diff --git a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
index 8dc74de9c3e..4c4a65a9a67 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
@@ -116,4 +116,4 @@ class CLookUp_ANN {
   void DisplayNetworkInfo() const;
 };
 
-}  // namespace MLPToolbox
\ No newline at end of file
+}  // namespace MLPToolbox
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
index a6001b2dace..5f1140b93b9 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
@@ -316,4 +316,4 @@ class CNeuralNetwork {
   }
 };
 
-}  // namespace MLPToolbox
\ No newline at end of file
+}  // namespace MLPToolbox
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
index da37e3cbe18..a84b8c5de74 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
@@ -118,4 +118,4 @@ class CNeuron {
   su2double GetGradient(std::size_t iInput) const { return doutput_dinputs[iInput]; }
 };
 
-}  // namespace MLPToolbox
\ No newline at end of file
+}  // namespace MLPToolbox
diff --git a/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
index 9408a130578..1963b6b24d8 100644
--- a/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
+++ b/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
@@ -153,4 +153,4 @@ class CReadNeuralNetwork {
    */
   std::string GetOutputName(std::size_t iOutput) const { return output_names[iOutput]; }
 };
-}  // namespace MLPToolbox
\ No newline at end of file
+}  // namespace MLPToolbox
diff --git a/Common/src/toolboxes/meson.build b/Common/src/toolboxes/meson.build
index 4c6d76c0b1c..e51c9e0f6e0 100644
--- a/Common/src/toolboxes/meson.build
+++ b/Common/src/toolboxes/meson.build
@@ -11,4 +11,3 @@ common_src += files(['multilayer_perceptron/CLookUp_ANN.cpp',
                      'multilayer_perceptron/CNeuralNetwork.cpp',
                      'multilayer_perceptron/CLayer.cpp',
                      'multilayer_perceptron/CReadNeuralNetwork.cpp'])
-
diff --git a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
index e81f589c919..ec4245f487d 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
@@ -78,4 +78,4 @@ void MLPToolbox::CIOMap::PairVariableswithMLPs(CLookUp_ANN* MLP_collection, su2v
       }
     }
   }
-}
\ No newline at end of file
+}
diff --git a/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp b/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp
index 16282a23809..86e6a05076b 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp
@@ -46,4 +46,4 @@ void MLPToolbox::CLayer::SetNNeurons(unsigned long n_neurons) {
       neurons[i].SetNumber(i + 1);
     }
   }
-}
\ No newline at end of file
+}
diff --git a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
index 7a65e5a1b59..7a2894bcd58 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
@@ -258,4 +258,4 @@ void MLPToolbox::CLookUp_ANN::DisplayNetworkInfo() const {
   for (auto i_MLP = 0u; i_MLP < NeuralNetworks.size(); i_MLP++) {
     NeuralNetworks[i_MLP].DisplayNetwork();
   }
-}
\ No newline at end of file
+}
diff --git a/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
index 7790229b532..8956397b259 100644
--- a/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
+++ b/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
@@ -204,4 +204,4 @@ string MLPToolbox::CReadNeuralNetwork::SkipToFlag(ifstream* file_stream, string
   if ((*file_stream).eof()) cout << "line not in file!" << endl;
 
   return line;
-}
\ No newline at end of file
+}
diff --git a/UnitTests/Common/toolboxes/multilayer_perceptron/simple_mlp.mlp b/UnitTests/Common/toolboxes/multilayer_perceptron/simple_mlp.mlp
index 01fb20bd102..5336c8d6047 100644
--- a/UnitTests/Common/toolboxes/multilayer_perceptron/simple_mlp.mlp
+++ b/UnitTests/Common/toolboxes/multilayer_perceptron/simple_mlp.mlp
@@ -31,17 +31,17 @@ z
 
 [weights per layer]
 <layer>
--4.1729342937469482e-01	-2.2465672492980957e+00	+1.1258139610290527e+00	-7.0158332586288452e-01	
-+1.1477893590927124e+00	+2.5089375674724579e-02	+2.6767715811729431e-01	+1.0031684637069702e+00	
+-4.1729342937469482e-01	-2.2465672492980957e+00	+1.1258139610290527e+00	-7.0158332586288452e-01
++1.1477893590927124e+00	+2.5089375674724579e-02	+2.6767715811729431e-01	+1.0031684637069702e+00
 </layer>
 <layer>
-+2.5062826275825500e-01	
--6.2471812963485718e-01	
--2.0578651130199432e-01	
-+2.6085931062698364e-01	
++2.5062826275825500e-01
+-6.2471812963485718e-01
+-2.0578651130199432e-01
++2.6085931062698364e-01
 </layer>
 
 [biases per layer]
 +0.0000000000000000e+00	+0.0000000000000000e+00	+0.0000000000000000e+00
-+7.5714819133281708e-02	+7.7316933870315552e-01	-4.4279521703720093e-01	+4.1041103005409241e-01	
-+2.8878501057624817e-01	
++7.5714819133281708e-02	+7.7316933870315552e-01	-4.4279521703720093e-01	+4.1041103005409241e-01
++2.8878501057624817e-01
diff --git a/config_template.cfg b/config_template.cfg
index 4d939845f06..2edcbc0ac21 100644
--- a/config_template.cfg
+++ b/config_template.cfg
@@ -370,14 +370,14 @@ GAS_COMPOSITION= (0.77, 0.23, 0.0, 0.0, 0.0)
 FROZEN_MIXTURE= NO
 
 %
-% Datadriven fluid model 
-% For data-driven fluid models, an interpolation algorithm is used to retrieve the thermodynamic state for a given density and internal energy 
+% Datadriven fluid model
+% For data-driven fluid models, an interpolation algorithm is used to retrieve the thermodynamic state for a given density and internal energy
 
 % Interpolation method for thermodynamic state calculation (only MLP is supported for now)
-INTERPOLATION_METHOD= MLP 
+INTERPOLATION_METHOD= MLP
 
 % Name of the input file containing the information required for the interpolator to function
-FILENAME_INTERPOLATOR= MLP_collection.mlp 
+FILENAME_INTERPOLATOR= MLP_collection.mlp
 
 % Relaxation factor for the Newton solvers in the data-driven fluid model
 DATADRIVEN_NEWTON_RELAXATION= 0.05
diff --git a/externals/codi b/externals/codi
index 427c2dc754a..96ac78ec5bc 160000
--- a/externals/codi
+++ b/externals/codi
@@ -1 +1 @@
-Subproject commit 427c2dc754a628ad3c9310c766c988ac5ce21bc7
+Subproject commit 96ac78ec5bcc5ac25b785e79b16ed76fca22d736
diff --git a/externals/medi b/externals/medi
index aafc2d1966b..6aef76912e7 160000
--- a/externals/medi
+++ b/externals/medi
@@ -1 +1 @@
-Subproject commit aafc2d1966ba1233640af737e71c77c1a86183fd
+Subproject commit 6aef76912e7099c4f08c9705848797ca9e8070da
diff --git a/externals/opdi b/externals/opdi
index f33b507c24f..1aabf5bd1ed 160000
--- a/externals/opdi
+++ b/externals/opdi
@@ -1 +1 @@
-Subproject commit f33b507c24f7448d4cf4df16ab5c53ea254b8774
+Subproject commit 1aabf5bd1ed77611742eb655002f2ac7a3dddef9

From 504f2d041260625c1d3ab83c419ecb2e62110db7 Mon Sep 17 00:00:00 2001
From: Kursat Yurt <kursatyurt@gmail.com>
Date: Mon, 20 Mar 2023 16:24:05 +0100
Subject: [PATCH 304/656] Ignore cache files

---
 .gitignore | 3 +++
 1 file changed, 3 insertions(+)

diff --git a/.gitignore b/.gitignore
index 8b56bc5e603..2177d44e12e 100644
--- a/.gitignore
+++ b/.gitignore
@@ -100,3 +100,6 @@ ninja
 
 # Ignore SU2 pre-configuration timestamp created by preconfigure.py
 su2preconfig.timestamp
+
+# Clangd server files
+.cache

From e4c598225a0ec1abf3235751dc7c7e991e92a686 Mon Sep 17 00:00:00 2001
From: Kursat Yurt <kursatyurt@gmail.com>
Date: Mon, 20 Mar 2023 19:34:06 +0100
Subject: [PATCH 305/656] Change Postprocessing to Finalize

---
 SU2_CFD/include/drivers/CDriver.hpp                   |  2 +-
 SU2_CFD/include/drivers/CDriverBase.hpp               |  4 ++--
 SU2_CFD/src/SU2_CFD.cpp                               |  4 ++--
 SU2_CFD/src/drivers/CDriver.cpp                       |  4 ++--
 SU2_CFD/src/drivers/CDriverBase.cpp                   |  2 +-
 SU2_DEF/include/drivers/CDeformationDriver.hpp        |  2 +-
 SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp |  2 +-
 SU2_DEF/src/SU2_DEF.cpp                               |  2 +-
 SU2_DEF/src/drivers/CDeformationDriver.cpp            | 11 +++++------
 SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp     |  7 +++----
 SU2_DOT/src/SU2_DOT.cpp                               |  2 +-
 SU2_GEO/src/SU2_GEO.cpp                               |  2 +-
 SU2_PY/SU2_CFD.py                                     |  4 ++--
 SU2_PY/fsi_computation.py                             |  2 +-
 SU2_SOL/src/SU2_SOL.cpp                               |  2 +-
 TestCases/py_wrapper/deforming_bump_in_channel/run.py |  4 ++--
 .../disc_adj_fea/flow_load_sens/run_adjoint.py        |  4 ++--
 .../disc_adj_flow/mesh_disp_sens/run_adjoint.py       |  4 ++--
 .../launch_flatPlate_rigidMotion.py                   |  4 ++--
 19 files changed, 33 insertions(+), 35 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index ae50e59e2f1..2631ae4ae01 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -364,7 +364,7 @@ class CDriver : public CDriverBase {
   /*!
    * \brief Deallocation routine
    */
-  void Postprocessing();
+  void Finalize();
 
   /*!
    * \brief A virtual member.
diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index 9d6c60334af..4cc8920d4b2 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -120,7 +120,7 @@ class CDriverBase {
   /*!
    * \brief A virtual member.
    */
-  virtual void Postprocessing(){}
+  virtual void Finalize(){}
 
 /// \addtogroup PySU2
 /// @{
@@ -446,7 +446,7 @@ class CDriverBase {
   /*!
    * \brief Delete containers.
    */
-  void CommonPostprocessing();
+  void CommonFinalize();
 
   /*!
    * \brief Read in the config and mesh files.
diff --git a/SU2_CFD/src/SU2_CFD.cpp b/SU2_CFD/src/SU2_CFD.cpp
index 11e8720cfb3..c11ceb54156 100644
--- a/SU2_CFD/src/SU2_CFD.cpp
+++ b/SU2_CFD/src/SU2_CFD.cpp
@@ -154,9 +154,9 @@ int main(int argc, char *argv[]) {
 
   driver->StartSolver();
 
-  /*--- Postprocess all the containers, close history file, exit SU2. ---*/
+  /*--- Finalize solver, delete all the containers, close history file, exit SU2. ---*/
 
-  driver->Postprocessing();
+  driver->Finalize();
 
   delete driver;
 
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index 14dc54017a4..8f157b47394 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -346,7 +346,7 @@ void CDriver::SetContainers_Null(){
 }
 
 
-void CDriver::Postprocessing() {
+void CDriver::Finalize() {
 
   const bool wrt_perf = config_container[ZONE_0]->GetWrt_Performance();
 
@@ -363,7 +363,7 @@ void CDriver::Postprocessing() {
   }
 
   if (rank == MASTER_NODE)
-    cout << endl <<"------------------------- Solver Postprocessing -------------------------" << endl;
+    cout << endl <<"------------------------- Finalizing Solver -------------------------" << endl;
 
   for (iZone = 0; iZone < nZone; iZone++) {
     for (iInst = 0; iInst < nInst[iZone]; iInst++){
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index 76ce8c42f5a..e9848534929 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -84,7 +84,7 @@ void CDriverBase::SetContainers_Null() {
   }
 }
 
-void CDriverBase::CommonPostprocessing() {
+void CDriverBase::CommonFinalize() {
 
   if (numerics_container != nullptr) {
     for (iZone = 0; iZone < nZone; iZone++) {
diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index 563221af6ee..ed63059e972 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -66,7 +66,7 @@ class CDeformationDriver : public CDriverBase {
   /*!
    * \brief Deallocation routine.
    */
-  void Postprocessing();
+  void Finalize();
 
   /*!
    * \brief Communicate boundary mesh displacements.
diff --git a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
index 24afea50a4d..55c3140348c 100644
--- a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
@@ -57,7 +57,7 @@ class CDiscAdjDeformationDriver : public CDriverBase {
   /*!
    * \brief Deallocation routine.
    */
-  void Postprocessing();
+  void Finalize();
 
  protected:
   /*!
diff --git a/SU2_DEF/src/SU2_DEF.cpp b/SU2_DEF/src/SU2_DEF.cpp
index 63c8bff70e6..504e80d9a87 100644
--- a/SU2_DEF/src/SU2_DEF.cpp
+++ b/SU2_DEF/src/SU2_DEF.cpp
@@ -63,7 +63,7 @@ int main(int argc, char* argv[]) {
 
   /*--- Postprocess all the containers, close history file, and exit SU2. ---*/
 
-  driver.Postprocessing();
+  driver.Finalize();
 
   /*--- Finalize MPI parallelization. ---*/
 
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index b8675df432c..6aa13a0d6c3 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -535,9 +535,8 @@ void CDeformationDriver::Output() {
   }
 }
 
-void CDeformationDriver::Postprocessing() {
-  if (rank == MASTER_NODE)
-    cout << "\n------------------------- Solver Postprocessing -------------------------" << endl;
+void CDeformationDriver::Finalize() {
+  if (rank == MASTER_NODE) cout << "\n------------------------- Finalize Solver -------------------------" << endl;
 
   if (driver_config->GetDeform_Mesh()) {
     for (iZone = 0; iZone < nZone; iZone++) {
@@ -550,7 +549,7 @@ void CDeformationDriver::Postprocessing() {
         delete[] numerics_container[iZone][INST_0][MESH_0];
         delete[] numerics_container[iZone][INST_0];
       }
-      /*--- The remaining levels in the container are deleted in CommonPostprocessing ---*/
+      /*--- The remaining levels in the container are deleted in CommonFinalize ---*/
     }
 
     for (iZone = 0; iZone < nZone; iZone++) {
@@ -559,11 +558,11 @@ void CDeformationDriver::Postprocessing() {
         delete[] solver_container[iZone][INST_0][MESH_0];
         delete[] solver_container[iZone][INST_0];
       }
-      /*--- The remaining levels in the container are deleted in CommonPostprocessing ---*/
+      /*--- The remaining levels in the container are deleted in CommonFinalize ---*/
     }
   }
 
-  CommonPostprocessing();
+  CommonFinalize();
 
   /*--- Exit the solver cleanly. ---*/
 
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index 7131e975725..775515de672 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -367,16 +367,15 @@ void CDiscAdjDeformationDriver::Run() {
   OutputGradient(Gradient, config_container[ZONE_0], Gradient_file);
 }
 
-void CDiscAdjDeformationDriver::Postprocessing() {
+void CDiscAdjDeformationDriver::Finalize() {
   for (auto iDV = 0u; iDV < config_container[ZONE_0]->GetnDV(); iDV++) {
     delete[] Gradient[iDV];
   }
   delete[] Gradient;
 
-  if (rank == MASTER_NODE)
-    cout << "\n------------------------- Solver Postprocessing -------------------------" << endl;
+  if (rank == MASTER_NODE) cout << "\n------------------------- Finalize Solver  -------------------------" << endl;
 
-  CommonPostprocessing();
+  CommonFinalize();
 
   /*--- Exit the solver cleanly. ---*/
 
diff --git a/SU2_DOT/src/SU2_DOT.cpp b/SU2_DOT/src/SU2_DOT.cpp
index 95c6e48b9b9..cc02b7fb9d5 100644
--- a/SU2_DOT/src/SU2_DOT.cpp
+++ b/SU2_DOT/src/SU2_DOT.cpp
@@ -66,7 +66,7 @@ int main(int argc, char* argv[]) {
 
   /*--- Postprocess all the containers, close history file, and exit SU2. ---*/
 
-  driver.Postprocessing();
+  driver.Finalize();
 
   /*--- Finalize AD. ---*/
 
diff --git a/SU2_GEO/src/SU2_GEO.cpp b/SU2_GEO/src/SU2_GEO.cpp
index 59ec6cf2107..78ce7faeb54 100644
--- a/SU2_GEO/src/SU2_GEO.cpp
+++ b/SU2_GEO/src/SU2_GEO.cpp
@@ -1429,7 +1429,7 @@ int main(int argc, char* argv[]) {
   }
 
   if (rank == MASTER_NODE)
-    cout << endl << "------------------------- Solver Postprocessing -------------------------" << endl;
+    cout << endl << "------------------------- Finalize Solver -------------------------" << endl;
 
   delete[] Xcoord_Airfoil;
   delete[] Ycoord_Airfoil;
diff --git a/SU2_PY/SU2_CFD.py b/SU2_PY/SU2_CFD.py
index 39c0eab38fb..0ffe32fc6a7 100755
--- a/SU2_PY/SU2_CFD.py
+++ b/SU2_PY/SU2_CFD.py
@@ -160,8 +160,8 @@ def main():
     # Launch the solver for the entire computation
     SU2Driver.StartSolver()
 
-    # Postprocess the solver and exit cleanly
-    SU2Driver.Postprocessing()
+    # Finalize the solver and exit cleanly
+    SU2Driver.Finalize()
 
     if SU2Driver != None:
         del SU2Driver
diff --git a/SU2_PY/fsi_computation.py b/SU2_PY/fsi_computation.py
index 4e644b49b24..9abda6639d4 100644
--- a/SU2_PY/fsi_computation.py
+++ b/SU2_PY/fsi_computation.py
@@ -231,7 +231,7 @@ def main():
         comm.barrier()
 
     # --- Exit cleanly the fluid and solid solvers --- #
-    FluidSolver.Postprocessing()
+    FluidSolver.Finalize()
     if myid == rootProcess:
         SolidSolver.exit()
 
diff --git a/SU2_SOL/src/SU2_SOL.cpp b/SU2_SOL/src/SU2_SOL.cpp
index feeeb4ca74a..3f7a3385165 100644
--- a/SU2_SOL/src/SU2_SOL.cpp
+++ b/SU2_SOL/src/SU2_SOL.cpp
@@ -685,7 +685,7 @@ int main(int argc, char* argv[]) {
   config = nullptr;
 
   if (rank == MASTER_NODE)
-    cout << endl << "------------------------- Solver Postprocessing -------------------------" << endl;
+    cout << endl << "------------------------- Finalize Solver -------------------------" << endl;
 
   if (geometry_container != nullptr) {
     for (iZone = 0; iZone < nZone; iZone++) {
diff --git a/TestCases/py_wrapper/deforming_bump_in_channel/run.py b/TestCases/py_wrapper/deforming_bump_in_channel/run.py
index 715e81c1cea..1455b7dbee5 100755
--- a/TestCases/py_wrapper/deforming_bump_in_channel/run.py
+++ b/TestCases/py_wrapper/deforming_bump_in_channel/run.py
@@ -88,8 +88,8 @@ def main():
     TimeIter += 1
     time += deltaT
 
-  # Postprocess the solver and exit cleanly
-  SU2Driver.Postprocessing()
+  # Finalize the solver and exit cleanly
+  SU2Driver.Finalize()
 
 
 # Imposed deformation
diff --git a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
index 3b59e063bef..56e6d62e805 100755
--- a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
@@ -118,8 +118,8 @@ def main():
     print("Sens[0]\tSens[1]\tDisp[0]\tDisp[1]\t")
     print(100, 100, sens[0][0], sens[0][1], disp[0][0], disp[0][1])
 
-  # Postprocess the solver and exit cleanly
-  SU2Driver.Postprocessing()
+  # Finalize the solver and exit cleanly
+  SU2Driver.Finalize()
 
   if SU2Driver != None:
     del SU2Driver
diff --git a/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
index 69e7baccc10..c041455ae08 100755
--- a/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
@@ -115,8 +115,8 @@ def main():
     if (iVertex == 30) and rank == 0:
       print(1000,1000,iVertex, sensX, sensY, sensZ)
 
-  # Postprocess the solver and exit cleanly
-  SU2Driver.Postprocessing()
+  # Finalize the solver and exit cleanly
+  SU2Driver.Finalize()
 
   if SU2Driver != None:
     del SU2Driver
diff --git a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
index 0efc10666df..010b27e86a4 100755
--- a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
+++ b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
@@ -134,8 +134,8 @@ def main():
     TimeIter += 1
     time += deltaT
 
-  # Postprocess the solver and exit cleanly
-  SU2Driver.Postprocessing()
+  # Finalize the solver and exit cleanly
+  SU2Driver.Finalize()
 
   if SU2Driver != None:
     del SU2Driver

From 5dcb9d723745467f460c70ad3eaf455b0626a062 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Mon, 20 Mar 2023 22:25:09 +0000
Subject: [PATCH 306/656] more changes for consistency

---
 SU2_CFD/include/drivers/CDriver.hpp      | 12 ----
 SU2_CFD/include/drivers/CDriverBase.hpp  | 61 +++++++++++++++--
 SU2_CFD/src/drivers/CDriverBase.cpp      | 84 +++++++++---------------
 SU2_CFD/src/python_wrapper_structure.cpp | 30 ---------
 4 files changed, 85 insertions(+), 102 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index ab9e9b60052..16d8b83824a 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -486,18 +486,6 @@ class CDriver : public CDriverBase {
    */
   void Inlet_Preprocessing(CSolver*** solver, CGeometry** geometry, CConfig* config) const;
 
-  /*!
-   * \brief Get all the CHT boundary marker tags.
-   * \return List of CHT boundary markers tags.
-   */
-  vector<string> GetCHTMarkerTags() const;
-
-  /*!
-   * \brief Get all the inlet boundary marker tags.
-   * \return List of inlet boundary markers tags.
-   */
-  vector<string> GetInletMarkerTags() const;
-
   /*!
    * \brief Set the position of the heat source.
    * \param[in] alpha - Angle of rotation respect to Z axis.
diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index a34ebe98b11..8e36df10118 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -264,6 +264,18 @@ class CDriverBase {
    */
   vector<string> GetDeformableMarkerTags() const;
 
+  /*!
+   * \brief Get all the CHT boundary marker tags.
+   * \return List of CHT boundary markers tags.
+   */
+  vector<string> GetCHTMarkerTags() const;
+
+  /*!
+   * \brief Get all the inlet boundary marker tags.
+   * \return List of inlet boundary markers tags.
+   */
+  vector<string> GetInletMarkerTags() const;
+
   /*!
    * \brief Get the number of elements in the marker.
    * \param[in] iMarker - Marker index.
@@ -313,36 +325,70 @@ class CDriverBase {
                                                bool normalize = false) const;
 
   /*!
-   * \brief Get the displacements of a marker vertex.
+   * \brief Get the displacements currently imposed of a marker vertex.
    * \param[in] iMarker - Marker index.
    * \param[in] iVertex - Marker vertex index.
    * \return Node displacements (nDim).
    */
-  vector<passivedouble> GetMarkerDisplacement(unsigned short iMarker, unsigned long iVertex) const;
+  inline vector<passivedouble> GetMarkerDisplacement(unsigned short iMarker, unsigned long iVertex) const {
+    vector<passivedouble> disp(GetNumberDimensions(), 0.0);
+    const auto iPoint = GetMarkerNode(iMarker, iVertex);
+    auto* nodes = GetSolverAndCheckMarker(MESH_SOL)->GetNodes();
+
+    for (auto iDim = 0u; iDim < GetNumberDimensions(); ++iDim) {
+      disp[iDim] = SU2_TYPE::GetValue(nodes->GetBound_Disp(iPoint, iDim));
+    }
+    return disp;
+  }
 
   /*!
    * \brief Set the mesh displacements of a marker vertex.
+   * \note This can be the input of the flow solver in an FSI setting.
    * \param[in] iMarker - Marker index.
    * \param[in] iVertex - Marker vertex index.
    * \param[in] values - Node displacements (nDim).
    */
-  void SetMarkerCustomDisplacement(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values);
+  inline void SetMarkerCustomDisplacement(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
+    const auto iPoint = GetMarkerNode(iMarker, iVertex);
+    auto* nodes = GetSolverAndCheckMarker(MESH_SOL)->GetNodes();
+
+    for (auto iDim = 0u; iDim < GetNumberDimensions(); iDim++) {
+      nodes->SetBound_Disp(iPoint, iDim, values[iDim]);
+    }
+  }
 
   /*!
-   * \brief Get the velocities of a marker vertex.
+   * \brief Get the mesh velocities currently imposed on a marker vertex.
    * \param[in] iMarker - Marker index.
    * \param[in] iVertex - Marker vertex index.
    * \return Node velocities (nDim).
    */
-  vector<passivedouble> GetMarkerMeshVelocity(unsigned short iMarker, unsigned long iVertex) const;
+  inline vector<passivedouble> GetMarkerMeshVelocity(unsigned short iMarker, unsigned long iVertex) const {
+    vector<passivedouble> vel(GetNumberDimensions(), 0.0);
+    const auto iPoint = GetMarkerNode(iMarker, iVertex);
+    auto* nodes = GetSolverAndCheckMarker(MESH_SOL)->GetNodes();
+
+    for (auto iDim = 0u; iDim < GetNumberDimensions(); ++iDim) {
+      vel[iDim] = SU2_TYPE::GetValue(nodes->GetBound_Vel(iPoint, iDim));
+    }
+    return vel;
+  }
 
   /*!
    * \brief Set the velocities of a marker vertex.
+   * \note This can be the input of the flow solver in an unsteady FSI setting.
    * \param[in] iMarker - Marker index.
    * \param[in] iVertex - Marker vertex index.
    * \param[in] values - Node velocities (nDim).
    */
-  void SetMarkerCustomMeshVelocity(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values);
+  inline void SetMarkerCustomMeshVelocity(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
+    const auto iPoint = GetMarkerNode(iMarker, iVertex);
+    auto* nodes = GetSolverAndCheckMarker(MESH_SOL)->GetNodes();
+
+    for (auto iDim = 0u; iDim < GetNumberDimensions(); iDim++) {
+      nodes->SetBound_Vel(iPoint, iDim, values[iDim]);
+    }
+  }
 
   /*!
    * \brief Communicate the boundary mesh displacements.
@@ -425,6 +471,7 @@ class CDriverBase {
 
   /*!
    * \brief Set the temperature of a vertex on a specified marker (MARKER_PYTHON_CUSTOM).
+   * \note This can be the input of a heat or flow solver in a CHT setting.
    * \param[in] iMarker - Marker identifier.
    * \param[in] iVertex - Vertex identifier.
    * \param[in] WallTemp - Value of the temperature.
@@ -435,6 +482,7 @@ class CDriverBase {
 
   /*!
    * \brief Set the wall normal heat flux at a vertex on a specified marker (MARKER_PYTHON_CUSTOM).
+   * \note This can be the input of a heat or flow solver in a CHT setting.
    * \param[in] iMarker - Marker identifier.
    * \param[in] iVertex - Vertex identifier.
    * \param[in] WallHeatFlux - Value of the normal heat flux.
@@ -445,6 +493,7 @@ class CDriverBase {
 
   /*!
    * \brief Get the wall normal heat flux at a vertex on a specified marker of the flow or heat solver.
+   * \note This can be the output of a heat or flow solver in a CHT setting.
    * \param[in] iSolver - Solver identifier, should be either a flow solver or the heat solver.
    * \param[in] iMarker - Marker identifier.
    * \param[in] iVertex - Vertex identifier.
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index 03d72e2d0d8..0fada5f043f 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -303,6 +303,36 @@ vector<string> CDriverBase::GetDeformableMarkerTags() const {
   return tags;
 }
 
+vector<string> CDriverBase::GetCHTMarkerTags() const {
+  vector<string> tags;
+  const auto nMarker = main_config->GetnMarker_All();
+
+  // The CHT markers can be identified as the markers that are customizable with a BC type HEAT_FLUX or ISOTHERMAL.
+  for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
+    if ((main_config->GetMarker_All_KindBC(iMarker) == HEAT_FLUX ||
+         main_config->GetMarker_All_KindBC(iMarker) == ISOTHERMAL) &&
+        main_config->GetMarker_All_PyCustom(iMarker)) {
+      tags.push_back(main_config->GetMarker_All_TagBound(iMarker));
+    }
+  }
+  return tags;
+}
+
+vector<string> CDriverBase::GetInletMarkerTags() const {
+  vector<string> tags;
+  const auto nMarker = main_config->GetnMarker_All();
+
+  for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
+    bool isCustomizable = main_config->GetMarker_All_PyCustom(iMarker);
+    bool isInlet = (main_config->GetMarker_All_KindBC(iMarker) == INLET_FLOW);
+
+    if (isCustomizable && isInlet) {
+      tags.push_back(main_config->GetMarker_All_TagBound(iMarker));
+    }
+  }
+  return tags;
+}
+
 unsigned long CDriverBase::GetNumberMarkerElements(unsigned short iMarker) const {
   if (iMarker >= GetNumberMarkers()) {
     SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
@@ -360,60 +390,6 @@ vector<passivedouble> CDriverBase::GetMarkerVertexNormals(unsigned short iMarker
   return values;
 }
 
-vector<passivedouble> CDriverBase::GetMarkerDisplacement(unsigned short iMarker, unsigned long iVertex) const {
-  vector<passivedouble> values(nDim, 0.0);
-
-  if (main_config->GetDeform_Mesh()) {
-    const auto iPoint = GetMarkerNode(iMarker, iVertex);
-    for (auto iDim = 0u; iDim < nDim; iDim++) {
-      const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetBound_Disp(iPoint, iDim);
-      values[iDim] = SU2_TYPE::GetValue(value);
-    }
-  }
-  return values;
-}
-
-void CDriverBase::SetMarkerCustomDisplacement(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
-  if (!main_config->GetDeform_Mesh()) {
-    SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
-  }
-  if (values.size() != nDim) {
-    SU2_MPI::Error("Invalid number of dimensions!", CURRENT_FUNCTION);
-  }
-  const auto iPoint = GetMarkerNode(iMarker, iVertex);
-
-  for (auto iDim = 0u; iDim < nDim; iDim++) {
-    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->SetBound_Disp(iPoint, iDim, values[iDim]);
-  }
-}
-
-vector<passivedouble> CDriverBase::GetMarkerMeshVelocity(unsigned short iMarker, unsigned long iVertex) const {
-  vector<passivedouble> values(nDim, 0.0);
-
-  if (main_config->GetDeform_Mesh()) {
-    const auto iPoint = GetMarkerNode(iMarker, iVertex);
-    for (auto iDim = 0u; iDim < nDim; iDim++) {
-      const su2double value = solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetBound_Vel(iPoint, iDim);
-      values[iDim] = SU2_TYPE::GetValue(value);
-    }
-  }
-  return values;
-}
-
-void CDriverBase::SetMarkerCustomMeshVelocity(unsigned short iMarker, unsigned long iVertex, vector<passivedouble> values) {
-  if (!main_config->GetDeform_Mesh()) {
-    SU2_MPI::Error("Mesh solver is not defined!", CURRENT_FUNCTION);
-  }
-  if (values.size() != nDim) {
-    SU2_MPI::Error("Invalid number of dimensions!", CURRENT_FUNCTION);
-  }
-  const auto iPoint = GetMarkerNode(iMarker, iVertex);
-
-  for (auto iDim = 0u; iDim < nDim; iDim++) {
-    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->SetBound_Vel(iPoint, iDim, values[iDim]);
-  }
-}
-
 void CDriverBase::CommunicateMeshDisplacements(void) {
   solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->InitiateComms(main_geometry, main_config, MESH_DISPLACEMENTS);
   solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->CompleteComms(main_geometry, main_config, MESH_DISPLACEMENTS);
diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index 6e089b600a1..2585121a29e 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -176,36 +176,6 @@ string CDriver::GetSurfaceFileName() const { return config_container[ZONE_0]->Ge
 /* Functions related to the management of markers                             */
 ////////////////////////////////////////////////////////////////////////////////
 
-vector<string> CDriver::GetCHTMarkerTags() const {
-  vector<string> tags;
-  const auto nMarker = config_container[ZONE_0]->GetnMarker_All();
-
-  // The CHT markers can be identified as the markers that are customizable with a BC type HEAT_FLUX or ISOTHERMAL.
-  for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
-    if ((config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == HEAT_FLUX ||
-         config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == ISOTHERMAL) &&
-        config_container[ZONE_0]->GetMarker_All_PyCustom(iMarker)) {
-      tags.push_back(config_container[ZONE_0]->GetMarker_All_TagBound(iMarker));
-    }
-  }
-  return tags;
-}
-
-vector<string> CDriver::GetInletMarkerTags() const {
-  vector<string> tags;
-  const auto nMarker = config_container[ZONE_0]->GetnMarker_All();
-
-  for (auto iMarker = 0u; iMarker < nMarker; iMarker++) {
-    bool isCustomizable = config_container[ZONE_0]->GetMarker_All_PyCustom(iMarker);
-    bool isInlet = (config_container[ZONE_0]->GetMarker_All_KindBC(iMarker) == INLET_FLOW);
-
-    if (isCustomizable && isInlet) {
-      tags.push_back(config_container[ZONE_0]->GetMarker_All_TagBound(iMarker));
-    }
-  }
-  return tags;
-}
-
 void CDriver::SetHeatSource_Position(passivedouble alpha, passivedouble pos_x, passivedouble pos_y,
                                      passivedouble pos_z) {
   CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][RAD_SOL];

From b97e68ca840b342ce13480900b76ac61f2c6fd3d Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 21 Mar 2023 17:40:38 +0100
Subject: [PATCH 307/656] pulled develop

---
 externals/codi | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/externals/codi b/externals/codi
index 96ac78ec5bc..8cdb2a2e623 160000
--- a/externals/codi
+++ b/externals/codi
@@ -1 +1 @@
-Subproject commit 96ac78ec5bcc5ac25b785e79b16ed76fca22d736
+Subproject commit 8cdb2a2e6231ede6343294ac9af748b3ea105ecd

From 19cf1e40fe1ee1754258589fa92d01075d6613d5 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Tue, 21 Mar 2023 20:05:18 +0000
Subject: [PATCH 308/656] fix vector unpacking

---
 SU2_PY/FSI_tools/FSIInterface.py                       | 10 ++++++----
 .../disc_adj_flow/mesh_disp_sens/run_adjoint.py        |  4 ++--
 TestCases/py_wrapper/translating_NACA0012/run_su2.py   |  2 +-
 3 files changed, 9 insertions(+), 7 deletions(-)

diff --git a/SU2_PY/FSI_tools/FSIInterface.py b/SU2_PY/FSI_tools/FSIInterface.py
index 7711a8b3707..fa58b5f901d 100644
--- a/SU2_PY/FSI_tools/FSIInterface.py
+++ b/SU2_PY/FSI_tools/FSIInterface.py
@@ -2048,13 +2048,15 @@ def getFluidInterfaceNodalForce(self, FSI_config, FluidSolver):
                 FluidSolver.GetMarkerNode(self.fluidInterfaceIdentifier, iVertex)
             )
             if GlobalIndex not in self.FluidHaloNodeList[myid].keys():
-                loadX, loadY, loadZ = FluidSolver.GetMarkerFlowLoad(
+                load = FluidSolver.GetMarkerFlowLoad(
                     self.fluidInterfaceIdentifier, iVertex
                 )
                 iGlobalVertex = self.__getGlobalIndex("fluid", myid, localIndex)
-                self.fluidLoads_array_X.setValues([iGlobalVertex], loadX)
-                self.fluidLoads_array_Y.setValues([iGlobalVertex], loadY)
-                self.fluidLoads_array_Z.setValues([iGlobalVertex], loadZ)
+                self.fluidLoads_array_X.setValues([iGlobalVertex], load[0])
+                self.fluidLoads_array_Y.setValues([iGlobalVertex], load[1])
+                self.fluidLoads_array_Z.setValues(
+                    [iGlobalVertex], load[2] if len(load) == 3 else 0.0
+                )
                 localIndex += 1
 
         self.fluidLoads_array_X.assemblyBegin()
diff --git a/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
index 4bc88b3bd25..a613757019d 100755
--- a/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
@@ -110,10 +110,10 @@ def main():
   # Sensitivities of the marker
   print("\n------------------------------ Sensitivities -----------------------------\n")
   for iVertex in range(nVertex_Marker):
-    sensX, sensY, sensZ = SU2Driver.GetMarkerDisplacementSensitivity(MarkerID, iVertex)
+    sensX, sensY = SU2Driver.GetMarkerDisplacementSensitivity(MarkerID, iVertex)
 
     if (iVertex == 30) and rank == 0:
-      print(1000,1000,iVertex, sensX, sensY, sensZ)
+      print(1000, 1000, iVertex, sensX, sensY, 0.0)
 
   # Finalize the solver and exit cleanly
   SU2Driver.Finalize()
diff --git a/TestCases/py_wrapper/translating_NACA0012/run_su2.py b/TestCases/py_wrapper/translating_NACA0012/run_su2.py
index f184b8fd7f9..f6fffc21c55 100644
--- a/TestCases/py_wrapper/translating_NACA0012/run_su2.py
+++ b/TestCases/py_wrapper/translating_NACA0012/run_su2.py
@@ -52,7 +52,7 @@ def save_forces(self):
                 fxyz = self.FluidSolver.GetMarkerFlowLoad(solver_marker_id, i_vertex)
                 iPoint = self.FluidSolver.GetMarkerNode(solver_marker_id, i_vertex)
                 GlobalIndex = self.FluidSolver.GetNodeGlobalIndex(iPoint)
-                f.write('{}, {:.2f}, {:.2f}, {:.2f}\n'.format(GlobalIndex, fxyz[0], fxyz[1], fxyz[2]))
+                f.write('{}, {:.2f}, {:.2f}, {:.2f}\n'.format(GlobalIndex, fxyz[0], fxyz[1], 0.0))
         f.close()
 
 cfd_interface = SU2Interface('config.cfg')

From 790de98a24ac7722650e38ae8a926eeaf3216df7 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?K=C3=BCr=C5=9Fat=20Yurt?=
 <57598663+kursatyurt@users.noreply.github.com>
Date: Tue, 21 Mar 2023 22:14:38 +0100
Subject: [PATCH 309/656] Change serial runs in parallel regression to parallel
 (#1977)

* Change serial runs in parallel regression to parallel

* Update expected values

Co-authored-by: Nijso <bigfootedrockmidget@hotmail.com>
---
 TestCases/parallel_regression.py | 15 ++-------------
 1 file changed, 2 insertions(+), 13 deletions(-)

diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index af2cb7ddc9f..1b359311076 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -615,7 +615,6 @@ def main():
     fem_ns_sphere.cfg_file  = "fem_Sphere_reg.cfg"
     fem_ns_sphere.test_iter = 10
     fem_ns_sphere.test_vals = [-0.288121,0.240324,0.000258,21.797363] #last 4 columns
-    fem_ns_sphere.command   = TestCase.Command(exec = "SU2_CFD")
     test_list.append(fem_ns_sphere)
 
     # Unsteady sphere ADER
@@ -624,7 +623,6 @@ def main():
     fem_ns_sphere_ader.cfg_file  = "fem_Sphere_reg_ADER.cfg"
     fem_ns_sphere_ader.test_iter = 10
     fem_ns_sphere_ader.test_vals = [-35.000000,-35.000000,0.000047,31.110911] #last 4 columns
-    fem_ns_sphere_ader.command   = TestCase.Command(exec = "SU2_CFD")
     test_list.append(fem_ns_sphere_ader)
 
     # Unsteady cylinder
@@ -633,7 +631,6 @@ def main():
     fem_ns_unsteady_cylinder.cfg_file  = "fem_unst_cylinder.cfg"
     fem_ns_unsteady_cylinder.test_iter = 11
     fem_ns_unsteady_cylinder.test_vals = [-3.558582,-3.014464,-0.038927,1.383983] #last 4 columns
-    fem_ns_unsteady_cylinder.command   = TestCase.Command(exec = "SU2_CFD")
     fem_ns_unsteady_cylinder.unsteady  = True
     test_list.append(fem_ns_unsteady_cylinder)
 
@@ -643,7 +640,6 @@ def main():
     fem_ns_unsteady_cylinder_ader.cfg_file  = "fem_unst_cylinder_ADER.cfg"
     fem_ns_unsteady_cylinder_ader.test_iter = 11
     fem_ns_unsteady_cylinder_ader.test_vals = [-35.000000,-35.000000,-0.041003,1.391339] #last 4 columns
-    fem_ns_unsteady_cylinder_ader.command   = TestCase.Command(exec = "SU2_CFD")
     fem_ns_unsteady_cylinder_ader.unsteady  = True
     test_list.append(fem_ns_unsteady_cylinder_ader)
 
@@ -1106,7 +1102,6 @@ def main():
     bars_SST_2D.cfg_file  = "bars.cfg"
     bars_SST_2D.test_iter = 13
     bars_SST_2D.test_vals = [13.000000, -0.604409, -1.523885]
-    bars_SST_2D.command   = TestCase.Command(exec = "SU2_CFD")
     bars_SST_2D.multizone = True
     test_list.append(bars_SST_2D)
 
@@ -1115,8 +1110,7 @@ def main():
     slinc_steady.cfg_dir   = "sliding_interface/incompressible_steady"
     slinc_steady.cfg_file  = "config.cfg"
     slinc_steady.test_iter = 19
-    slinc_steady.test_vals = [19.000000, -1.803732, -2.108492] #last 3 columns
-    slinc_steady.command   = TestCase.Command(exec = "SU2_CFD")
+    slinc_steady.test_vals = [19.000000, -1.778863, -2.040209] #last 3 columns
     slinc_steady.timeout   = 100
     slinc_steady.tol       = 0.00002
     slinc_steady.multizone = True
@@ -1232,7 +1226,6 @@ def main():
     cht_incompressible.cfg_file  = "cht_2d_3cylinders.cfg"
     cht_incompressible.test_iter = 10
     cht_incompressible.test_vals = [-2.128826, -0.588813, -0.588813, -0.588813] #last 4 columns
-    cht_incompressible.command   = TestCase.Command(exec = "SU2_CFD")
     cht_incompressible.multizone = True
     test_list.append(cht_incompressible)
 
@@ -1241,8 +1234,7 @@ def main():
     cht_compressible.cfg_dir   = "coupled_cht/comp_2d"
     cht_compressible.cfg_file  = "cht_2d_3cylinders.cfg"
     cht_compressible.test_iter = 10
-    cht_compressible.test_vals = [-4.256032, -0.532728, -0.532729, -0.532728]
-    cht_compressible.command   = TestCase.Command(exec = "SU2_CFD")
+    cht_compressible.test_vals = [-4.256053, -0.532725, -0.532725, -0.532726]
     cht_compressible.multizone = True
     test_list.append(cht_compressible)
 
@@ -1387,7 +1379,6 @@ def main():
     ringleb_dg_euler.cfg_file  = "ringleb_dg.cfg"
     ringleb_dg_euler.test_iter = 100
     ringleb_dg_euler.test_vals = [-5.136652, -4.724941, 0.000000, 0.000000] #last 4 columns
-    ringleb_dg_euler.command   = TestCase.Command(exec = "SU2_CFD")
     ringleb_dg_euler.tol       = 0.0001
     test_list.append(ringleb_dg_euler)
 
@@ -1397,7 +1388,6 @@ def main():
     mms_dg_ns.cfg_file  = "lam_mms_dg.cfg"
     mms_dg_ns.test_iter = 100
     mms_dg_ns.test_vals = [-1.845393, 3.520699, 0.000000, 0.000000] #last 4 columns
-    mms_dg_ns.command   = TestCase.Command(exec = "SU2_CFD")
     mms_dg_ns.tol       = 0.0001
     test_list.append(mms_dg_ns)
 
@@ -1407,7 +1397,6 @@ def main():
     mms_dg_ns_3d.cfg_file  = "lam_mms_dg_3d.cfg"
     mms_dg_ns_3d.test_iter = 100
     mms_dg_ns_3d.test_vals = [-0.146826, 5.356413, 0.000000, 0.000000] #last 4 columns
-    mms_dg_ns_3d.command   = TestCase.Command(exec = "SU2_CFD")
     mms_dg_ns_3d.tol       = 0.0001
     test_list.append(mms_dg_ns_3d)
 

From d82182d6dedaeb858103a4e39e469233cc06334a Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Fri, 24 Mar 2023 17:43:30 +0100
Subject: [PATCH 310/656] Relax tolerances of python wrapper hybrid AD tests.

---
 TestCases/hybrid_regression_AD.py | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/TestCases/hybrid_regression_AD.py b/TestCases/hybrid_regression_AD.py
index bf8891e91d3..1f1507c8874 100644
--- a/TestCases/hybrid_regression_AD.py
+++ b/TestCases/hybrid_regression_AD.py
@@ -234,7 +234,7 @@ def main():
     pywrapper_FEA_AD_FlowLoad.test_vals     = [-0.131742, -0.553318, -0.000364, -0.003101] #last 4 columns
     pywrapper_FEA_AD_FlowLoad.command       = TestCase.Command(exec = "python", param = "run_adjoint.py --parallel -f")
     pywrapper_FEA_AD_FlowLoad.timeout       = 1600
-    pywrapper_FEA_AD_FlowLoad.tol           = 0.000001
+    pywrapper_FEA_AD_FlowLoad.tol           = 1e-4
     pywrapper_FEA_AD_FlowLoad.new_output    = False
     test_list.append(pywrapper_FEA_AD_FlowLoad)
     pass_list.append(pywrapper_FEA_AD_FlowLoad.run_test())
@@ -247,7 +247,7 @@ def main():
     pywrapper_CFD_AD_MeshDisp.test_vals     = [30.000000, -2.520967, 1.375188, 0.000000] #last 4 columns
     pywrapper_CFD_AD_MeshDisp.command       = TestCase.Command(exec = "python", param = "run_adjoint.py --parallel -f")
     pywrapper_CFD_AD_MeshDisp.timeout       = 1600
-    pywrapper_CFD_AD_MeshDisp.tol           = 0.000001
+    pywrapper_CFD_AD_MeshDisp.tol           = 1e-4
     pywrapper_CFD_AD_MeshDisp.new_output    = False
     test_list.append(pywrapper_CFD_AD_MeshDisp)
     pass_list.append(pywrapper_CFD_AD_MeshDisp.run_test())

From 4e69e2ef7541348980cbdf9cd8ce572cfaa31630 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 25 Mar 2023 17:26:56 +0000
Subject: [PATCH 311/656] avoid mixing the important output groups

---
 SU2_CFD/include/output/CFlowOutput.hpp |  6 +++---
 SU2_CFD/src/output/CFlowCompOutput.cpp |  6 +++---
 SU2_CFD/src/output/CFlowIncOutput.cpp  |  6 +++---
 SU2_CFD/src/output/CFlowOutput.cpp     | 30 ++++++++++++++++++++------
 SU2_CFD/src/output/CNEMOCompOutput.cpp |  6 +++---
 5 files changed, 35 insertions(+), 19 deletions(-)

diff --git a/SU2_CFD/include/output/CFlowOutput.hpp b/SU2_CFD/include/output/CFlowOutput.hpp
index 9020076486e..e18d04f82d4 100644
--- a/SU2_CFD/include/output/CFlowOutput.hpp
+++ b/SU2_CFD/include/output/CFlowOutput.hpp
@@ -115,20 +115,20 @@ class CFlowOutput : public CFVMOutput{
    * \note The order of fields in restart files is fixed. Therefore the split-up.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetVolumeOutputFields_ScalarSolution(const CConfig* config);
+  void SetVolumeOutputFieldsScalarSolution(const CConfig* config);
 
   /*!
    * \brief Add scalar (turbulence/species) volume solution fields for a point (FVMComp, FVMInc, FVMNEMO).
    * \note The order of fields in restart files is fixed. Therefore the split-up.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetVolumeOutputFields_ScalarResidual(const CConfig* config);
+  void SetVolumeOutputFieldsScalarResidual(const CConfig* config);
 
   /*!
    * \brief Add scalar (turbulence/species) volume limiter fields (and more) for a point (FVMComp, FVMInc, FVMNEMO).
    * \param[in] config - Definition of the particular problem.
    */
-  void SetVolumeOutputFields_ScalarLimiter(const CConfig* config);
+  void SetVolumeOutputFieldsScalarMisc(const CConfig* config);
 
   /*!
    * \brief Set all scalar (turbulence/species) volume field values for a point.
diff --git a/SU2_CFD/src/output/CFlowCompOutput.cpp b/SU2_CFD/src/output/CFlowCompOutput.cpp
index 953c1d9015f..ed330053a78 100644
--- a/SU2_CFD/src/output/CFlowCompOutput.cpp
+++ b/SU2_CFD/src/output/CFlowCompOutput.cpp
@@ -222,7 +222,7 @@ void CFlowCompOutput::SetVolumeOutputFields(CConfig *config){
     AddVolumeOutput("MOMENTUM-Z", "Momentum_z", "SOLUTION", "z-component of the momentum vector");
   AddVolumeOutput("ENERGY",     "Energy",     "SOLUTION", "Energy");
 
-  SetVolumeOutputFields_ScalarSolution(config);
+  SetVolumeOutputFieldsScalarSolution(config);
 
   // Grid velocity
   if (gridMovement){
@@ -258,7 +258,7 @@ void CFlowCompOutput::SetVolumeOutputFields(CConfig *config){
     AddVolumeOutput("RES_MOMENTUM-Z", "Residual_Momentum_z", "RESIDUAL", "Residual of the z-momentum component");
   AddVolumeOutput("RES_ENERGY", "Residual_Energy", "RESIDUAL", "Residual of the energy");
 
-  SetVolumeOutputFields_ScalarResidual(config);
+  SetVolumeOutputFieldsScalarResidual(config);
 
   if (config->GetKind_SlopeLimit_Flow() != LIMITER::NONE && config->GetKind_SlopeLimit_Flow() != LIMITER::VAN_ALBADA_EDGE) {
     AddVolumeOutput("LIMITER_VELOCITY-X", "Limiter_Velocity_x", "LIMITER", "Limiter value of the x-velocity");
@@ -271,7 +271,7 @@ void CFlowCompOutput::SetVolumeOutputFields(CConfig *config){
     AddVolumeOutput("LIMITER_ENTHALPY", "Limiter_Enthalpy", "LIMITER", "Limiter value of the enthalpy");
   }
 
-  SetVolumeOutputFields_ScalarLimiter(config);
+  SetVolumeOutputFieldsScalarMisc(config);
 
   // Roe Low Dissipation
   if (config->GetKind_RoeLowDiss() != NO_ROELOWDISS) {
diff --git a/SU2_CFD/src/output/CFlowIncOutput.cpp b/SU2_CFD/src/output/CFlowIncOutput.cpp
index 29aeef9e015..01d91eec96a 100644
--- a/SU2_CFD/src/output/CFlowIncOutput.cpp
+++ b/SU2_CFD/src/output/CFlowIncOutput.cpp
@@ -298,7 +298,7 @@ void CFlowIncOutput::SetVolumeOutputFields(CConfig *config){
   if (heat || weakly_coupled_heat)
     AddVolumeOutput("TEMPERATURE",  "Temperature","SOLUTION", "Temperature");
 
-  SetVolumeOutputFields_ScalarSolution(config);
+  SetVolumeOutputFieldsScalarSolution(config);
 
   // Radiation variables
   if (config->AddRadiation())
@@ -344,7 +344,7 @@ void CFlowIncOutput::SetVolumeOutputFields(CConfig *config){
   if (config->GetEnergy_Equation())
     AddVolumeOutput("RES_TEMPERATURE", "Residual_Temperature", "RESIDUAL", "Residual of the temperature");
 
-  SetVolumeOutputFields_ScalarResidual(config);
+  SetVolumeOutputFieldsScalarResidual(config);
 
   if (config->GetKind_SlopeLimit_Flow() != LIMITER::NONE && config->GetKind_SlopeLimit_Flow() != LIMITER::VAN_ALBADA_EDGE) {
     AddVolumeOutput("LIMITER_PRESSURE", "Limiter_Pressure", "LIMITER", "Limiter value of the pressure");
@@ -356,7 +356,7 @@ void CFlowIncOutput::SetVolumeOutputFields(CConfig *config){
       AddVolumeOutput("LIMITER_TEMPERATURE", "Limiter_Temperature", "LIMITER", "Limiter value of the temperature");
   }
 
-  SetVolumeOutputFields_ScalarLimiter(config);
+  SetVolumeOutputFieldsScalarMisc(config);
 
   // Streamwise Periodicity
   if(streamwisePeriodic) {
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index ed0fb0f3a16..1f746db5558 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -1130,7 +1130,9 @@ void CFlowOutput::LoadHistoryData_Scalar(const CConfig* config, const CSolver* c
   }
 }
 
-void CFlowOutput::SetVolumeOutputFields_ScalarSolution(const CConfig* config){
+void CFlowOutput::SetVolumeOutputFieldsScalarSolution(const CConfig* config){
+  /*--- Only place outputs of the "SOLUTION" group here. ---*/
+
   switch (TurbModelFamily(config->GetKind_Turb_Model())) {
     case TURB_FAMILY::SA:
       AddVolumeOutput("NU_TILDE", "Nu_Tilde", "SOLUTION", "Spalart-Allmaras variable");
@@ -1149,9 +1151,6 @@ void CFlowOutput::SetVolumeOutputFields_ScalarSolution(const CConfig* config){
     case TURB_TRANS_MODEL::LM:
       AddVolumeOutput("INTERMITTENCY", "LM_gamma", "SOLUTION", "LM intermittency");
       AddVolumeOutput("RE_THETA_T", "LM_Re_t", "SOLUTION", "LM RE_THETA_T");
-      AddVolumeOutput("INTERMITTENCY_SEP", "LM_gamma_sep", "PRIMITIVE", "LM intermittency");
-      AddVolumeOutput("INTERMITTENCY_EFF", "LM_gamma_eff", "PRIMITIVE", "LM RE_THETA_T");
-      AddVolumeOutput("TURB_INDEX", "Turb_index", "PRIMITIVE", "Turbulence index");
       break;
 
     case TURB_TRANS_MODEL::NONE:
@@ -1165,7 +1164,9 @@ void CFlowOutput::SetVolumeOutputFields_ScalarSolution(const CConfig* config){
   }
 }
 
-void CFlowOutput::SetVolumeOutputFields_ScalarResidual(const CConfig* config) {
+void CFlowOutput::SetVolumeOutputFieldsScalarResidual(const CConfig* config) {
+  /*--- Only place outputs of the "RESIDUAL" group here. ---*/
+
   switch (TurbModelFamily(config->GetKind_Turb_Model())){
     case TURB_FAMILY::SA:
       AddVolumeOutput("RES_NU_TILDE", "Residual_Nu_Tilde", "RESIDUAL", "Residual of the Spalart-Allmaras variable");
@@ -1193,12 +1194,13 @@ void CFlowOutput::SetVolumeOutputFields_ScalarResidual(const CConfig* config) {
   if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
     for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++){
       AddVolumeOutput("RES_SPECIES_" + std::to_string(iVar), "Residual_Species_" + std::to_string(iVar), "RESIDUAL", "Residual of the transported species " + std::to_string(iVar));
-      AddVolumeOutput("DIFFUSIVITY_" + std::to_string(iVar), "Diffusivity_" + std::to_string(iVar), "PRIMITIVE", "Diffusivity of the transported species " + std::to_string(iVar));
     }
   }
 }
 
-void CFlowOutput::SetVolumeOutputFields_ScalarLimiter(const CConfig* config) {
+void CFlowOutput::SetVolumeOutputFieldsScalarMisc(const CConfig* config) {
+  /*--- Place "PRIMITIVE", "LIMITER", and other groups here. ---*/
+
   if (config->GetKind_SlopeLimit_Turb() != LIMITER::NONE) {
     switch (TurbModelFamily(config->GetKind_Turb_Model())) {
       case TURB_FAMILY::SA:
@@ -1220,6 +1222,20 @@ void CFlowOutput::SetVolumeOutputFields_ScalarLimiter(const CConfig* config) {
       for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++)
         AddVolumeOutput("LIMITER_SPECIES_" + std::to_string(iVar), "Limiter_Species_" + std::to_string(iVar), "LIMITER", "Limiter value of the transported species " + std::to_string(iVar));
     }
+    for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
+      AddVolumeOutput("DIFFUSIVITY_" + std::to_string(iVar), "Diffusivity_" + std::to_string(iVar), "PRIMITIVE", "Diffusivity of the transported species " + std::to_string(iVar));
+    }
+  }
+
+  switch (config->GetKind_Trans_Model()) {
+    case TURB_TRANS_MODEL::LM:
+      AddVolumeOutput("INTERMITTENCY_SEP", "LM_gamma_sep", "PRIMITIVE", "LM intermittency");
+      AddVolumeOutput("INTERMITTENCY_EFF", "LM_gamma_eff", "PRIMITIVE", "LM RE_THETA_T");
+      AddVolumeOutput("TURB_INDEX", "Turb_index", "PRIMITIVE", "Turbulence index");
+      break;
+
+    case TURB_TRANS_MODEL::NONE:
+      break;
   }
 
   if (config->GetKind_Turb_Model() != TURB_MODEL::NONE) {
diff --git a/SU2_CFD/src/output/CNEMOCompOutput.cpp b/SU2_CFD/src/output/CNEMOCompOutput.cpp
index e2c799e269f..7ad99be195e 100644
--- a/SU2_CFD/src/output/CNEMOCompOutput.cpp
+++ b/SU2_CFD/src/output/CNEMOCompOutput.cpp
@@ -224,7 +224,7 @@ void CNEMOCompOutput::SetVolumeOutputFields(CConfig *config){
   AddVolumeOutput("ENERGY",       "Energy",     "SOLUTION", "Energy");
   AddVolumeOutput("ENERGY_VE",    "Energy_ve",  "SOLUTION", "Energy_ve");
 
-  SetVolumeOutputFields_ScalarSolution(config);
+  SetVolumeOutputFieldsScalarSolution(config);
 
   //Auxiliary variables for post-processment
   for(iSpecies = 0; iSpecies < nSpecies; iSpecies++)
@@ -271,7 +271,7 @@ void CNEMOCompOutput::SetVolumeOutputFields(CConfig *config){
   AddVolumeOutput("RES_ENERGY",    "Residual_Energy",    "RESIDUAL", "Residual of the energy");
   AddVolumeOutput("RES_ENERGY_VE", "Residual_Energy_ve", "RESIDUAL", "Residual of the energy_ve");
 
-  SetVolumeOutputFields_ScalarResidual(config);
+  SetVolumeOutputFieldsScalarResidual(config);
 
   if (config->GetKind_SlopeLimit_Flow() != LIMITER::NONE && config->GetKind_SlopeLimit_Flow() != LIMITER::VAN_ALBADA_EDGE) {
     // Limiter values
@@ -283,7 +283,7 @@ void CNEMOCompOutput::SetVolumeOutputFields(CConfig *config){
     AddVolumeOutput("LIMITER_ENERGY", "Limiter_Energy", "LIMITER", "Limiter value of the energy");
   }
 
-  SetVolumeOutputFields_ScalarLimiter(config);
+  SetVolumeOutputFieldsScalarMisc(config);
 
   AddCommonFVMOutputs(config);
 

From 0cb655e5eec06f2d53ee45edfc7a90159642837e Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 25 Mar 2023 19:10:27 +0000
Subject: [PATCH 312/656] expose all history outputs

---
 SU2_CFD/include/drivers/CDriver.hpp        | 154 ++++++++-------------
 SU2_CFD/include/drivers/CDriverBase.hpp    |  53 ++++++-
 SU2_CFD/include/output/COutput.hpp         |  17 ++-
 SU2_CFD/src/output/CFlowOutput.cpp         |   3 +
 SU2_CFD/src/python_wrapper_structure.cpp   | 100 -------------
 SU2_DEF/src/drivers/CDeformationDriver.cpp |   8 +-
 6 files changed, 121 insertions(+), 214 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index 9b3eae14a3a..44258e8bb4f 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -356,6 +356,58 @@ class CDriver : public CDriverBase {
    */
   void Print_DirectResidual(RECORDING kind_recording);
 
+  /*!
+   * \brief Set the solution of all solvers (adjoint or primal) in a zone.
+   * \param[in] iZone - Index of the zone.
+   * \param[in] adjoint - True to consider adjoint solvers instead of primal.
+   * \param[in] solution - Solution object with interface (iPoint,iVar).
+   * \tparam Old - If true set "old solutions" instead.
+   */
+  template <class Container, bool Old = false>
+  void SetAllSolutions(unsigned short iZone, bool adjoint, const Container& solution) {
+    const auto nPoint = geometry_container[iZone][INST_0][MESH_0]->GetnPoint();
+    for (auto iSol = 0u, offset = 0u; iSol < MAX_SOLS; ++iSol) {
+      auto solver = solver_container[iZone][INST_0][MESH_0][iSol];
+      if (!(solver && (solver->GetAdjoint() == adjoint))) continue;
+      for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint)
+        for (auto iVar = 0ul; iVar < solver->GetnVar(); ++iVar)
+          if (!Old) {
+            solver->GetNodes()->SetSolution(iPoint, iVar, solution(iPoint, offset + iVar));
+          } else {
+            solver->GetNodes()->SetSolution_Old(iPoint, iVar, solution(iPoint, offset + iVar));
+          }
+      offset += solver->GetnVar();
+    }
+  }
+
+  /*!
+   * \brief Set the "old solution" of all solvers (adjoint or primal) in a zone.
+   */
+  template <class Container>
+  void SetAllSolutionsOld(unsigned short iZone, bool adjoint, const Container& solution) {
+    SetAllSolutions<Container, true>(iZone, adjoint, solution);
+  }
+
+  /*!
+   * \brief Get the solution of all solvers (adjoint or primal) in a zone.
+   * \param[in] iZone - Index of the zone.
+   * \param[in] adjoint - True to consider adjoint solvers instead of primal.
+   * \param[out] solution - Solution object with interface (iPoint,iVar).
+   */
+  template <class Container>
+  void GetAllSolutions(unsigned short iZone, bool adjoint, Container& solution) const {
+    const auto nPoint = geometry_container[iZone][INST_0][MESH_0]->GetnPoint();
+    for (auto iSol = 0u, offset = 0u; iSol < MAX_SOLS; ++iSol) {
+      auto solver = solver_container[iZone][INST_0][MESH_0][iSol];
+      if (!(solver && (solver->GetAdjoint() == adjoint))) continue;
+      const auto& sol = solver->GetNodes()->GetSolution();
+      for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint)
+        for (auto iVar = 0ul; iVar < solver->GetnVar(); ++iVar)
+          solution(iPoint, offset + iVar) = SU2_TYPE::GetValue(sol(iPoint, iVar));
+      offset += solver->GetnVar();
+    }
+  }
+
  public:
   /*!
    * \brief Launch the computation for all zones and all physics.
@@ -413,56 +465,14 @@ class CDriver : public CDriverBase {
   void BoundaryConditionsUpdate();
 
   /*!
-   * \brief Get the total drag.
-   * \return Total drag.
-   */
-  passivedouble Get_Drag() const;
-
-  /*!
-   * \brief Get the total lift.
-   * \return Total lift.
-   */
-  passivedouble Get_Lift() const;
-
-  /*!
-   * \brief Get the total x moment.
-   * \return Total x moment.
-   */
-  passivedouble Get_Mx() const;
-
-  /*!
-   * \brief Get the total y moment.
-   * \return Total y moment.
-   */
-  passivedouble Get_My() const;
-
-  /*!
-   * \brief Get the total z moment.
-   * \return Total z moment.
-   */
-  passivedouble Get_Mz() const;
-
-  /*!
-   * \brief Get the total drag coefficient.
-   * \return Total drag coefficient.
-   */
-  passivedouble Get_DragCoeff() const;
-
-  /*!
-   * \brief Get the total lift coefficient.
-   * \return Total lift coefficient.
-   */
-  passivedouble Get_LiftCoeff() const;
-
-  /*!
-   * \brief Get the number of external iterations.
-   * \return Number of external iterations.
+   * \brief Get the number of time iterations.
+   * \return Number of time iterations.
    */
   unsigned long GetNumberTimeIter() const;
 
   /*!
-   * \brief Get the current external iteration.
-   * \return Current external iteration.
+   * \brief Get the current time iteration.
+   * \return Current time iteration.
    */
   unsigned long GetTimeIter() const;
 
@@ -518,58 +528,6 @@ class CDriver : public CDriverBase {
     }
     return nVar;
   }
-
-  /*!
-   * \brief Set the solution of all solvers (adjoint or primal) in a zone.
-   * \param[in] iZone - Index of the zone.
-   * \param[in] adjoint - True to consider adjoint solvers instead of primal.
-   * \param[in] solution - Solution object with interface (iPoint,iVar).
-   * \tparam Old - If true set "old solutions" instead.
-   */
-  template <class Container, bool Old = false>
-  void SetAllSolutions(unsigned short iZone, bool adjoint, const Container& solution) {
-    const auto nPoint = geometry_container[iZone][INST_0][MESH_0]->GetnPoint();
-    for (auto iSol = 0u, offset = 0u; iSol < MAX_SOLS; ++iSol) {
-      auto solver = solver_container[iZone][INST_0][MESH_0][iSol];
-      if (!(solver && (solver->GetAdjoint() == adjoint))) continue;
-      for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint)
-        for (auto iVar = 0ul; iVar < solver->GetnVar(); ++iVar)
-          if (!Old) {
-            solver->GetNodes()->SetSolution(iPoint, iVar, solution(iPoint, offset + iVar));
-          } else {
-            solver->GetNodes()->SetSolution_Old(iPoint, iVar, solution(iPoint, offset + iVar));
-          }
-      offset += solver->GetnVar();
-    }
-  }
-
-  /*!
-   * \brief Set the "old solution" of all solvers (adjoint or primal) in a zone.
-   */
-  template <class Container>
-  void SetAllSolutionsOld(unsigned short iZone, bool adjoint, const Container& solution) {
-    SetAllSolutions<Container, true>(iZone, adjoint, solution);
-  }
-
-  /*!
-   * \brief Get the solution of all solvers (adjoint or primal) in a zone.
-   * \param[in] iZone - Index of the zone.
-   * \param[in] adjoint - True to consider adjoint solvers instead of primal.
-   * \param[out] solution - Solution object with interface (iPoint,iVar).
-   */
-  template <class Container>
-  void GetAllSolutions(unsigned short iZone, bool adjoint, Container& solution) const {
-    const auto nPoint = geometry_container[iZone][INST_0][MESH_0]->GetnPoint();
-    for (auto iSol = 0u, offset = 0u; iSol < MAX_SOLS; ++iSol) {
-      auto solver = solver_container[iZone][INST_0][MESH_0][iSol];
-      if (!(solver && (solver->GetAdjoint() == adjoint))) continue;
-      const auto& sol = solver->GetNodes()->GetSolution();
-      for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint)
-        for (auto iVar = 0ul; iVar < solver->GetnVar(); ++iVar)
-          solution(iPoint, offset + iVar) = SU2_TYPE::GetValue(sol(iPoint, iVar));
-      offset += solver->GetnVar();
-    }
-  }
 };
 
 /*!
diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index b6ceafcd4dc..ae4581c74b2 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -107,11 +107,6 @@ class CDriverBase {
    */
   virtual void Update(){}
 
-  /*!
-   * \brief A virtual member.
-   */
-  virtual void Update_Legacy(){}
-
   /*!
    * \brief A virtual member.
    */
@@ -125,6 +120,54 @@ class CDriverBase {
 /// \addtogroup PySU2
 /// @{
 
+  /*!
+   * \brief Get the list of available outputs.
+   * \return List of output names.
+   */
+  inline vector<string> GetOutputNames() const { return output_container[MESH_0]->GetHistoryOutput_List(); }
+
+  /*!
+   * \brief Get the value of one of the available history outputs.
+   * \return Value of the output.
+   */
+  inline passivedouble GetOutputValue(std::string output_name) const {
+    return SU2_TYPE::GetValue(output_container[MESH_0]->GetHistoryFieldValue(output_name));
+  }
+
+  /*!
+   * \brief Get the list of available surface outputs on **both** MARKER_MONITORING and MARKER_ANALYZE.
+   * \return List of surface output names.
+   */
+  inline vector<string> GetMarkerOutputNames() const {
+    return output_container[MESH_0]->GetHistoryOutputPerSurface_List();
+  }
+
+  /*!
+   * \brief Get the value of one of the available surface outputs at a given MARKER_MONITORING.
+   * \return Value of the output.
+   */
+  inline passivedouble GetMarkerMonitoringOutputValue(std::string output_name, std::string marker_monitoring) const {
+    for (auto iMarker = 0u; iMarker < main_config->GetnMarker_Monitoring(); ++iMarker) {
+      if (marker_monitoring == main_config->GetMarker_Monitoring_TagBound(iMarker))
+        return SU2_TYPE::GetValue(output_container[MESH_0]->GetHistoryFieldValuePerSurface(output_name, iMarker));
+    }
+    SU2_MPI::Error(marker_monitoring + " is not in MARKER_MONITORING.", CURRENT_FUNCTION);
+    return 0;
+  }
+
+  /*!
+   * \brief Get the value of one of the available surface outputs at a given MARKER_ANALYZE.
+   * \return Value of the output.
+   */
+  inline passivedouble GetMarkerAnalyzeOutputValue(std::string output_name, std::string marker_analyze) const {
+    for (auto iMarker = 0u; iMarker < main_config->GetnMarker_Analyze(); ++iMarker) {
+      if (marker_analyze == main_config->GetMarker_Analyze_TagBound(iMarker))
+        return SU2_TYPE::GetValue(output_container[MESH_0]->GetHistoryFieldValuePerSurface(output_name, iMarker));
+    }
+    SU2_MPI::Error(marker_analyze + " is not in MARKER_ANALYZE.", CURRENT_FUNCTION);
+    return 0;
+  }
+
   /*!
    * \brief Get the number of design variables.
    * \return Number of design variables.
diff --git a/SU2_CFD/include/output/COutput.hpp b/SU2_CFD/include/output/COutput.hpp
index 2dfe0683563..7163dd5dd45 100644
--- a/SU2_CFD/include/output/COutput.hpp
+++ b/SU2_CFD/include/output/COutput.hpp
@@ -446,8 +446,11 @@ class COutput {
    * \param[in] field - Name of the field
    * \return Value of the field
    */
-  su2double GetHistoryFieldValue(const string& field) const {
-    return historyOutput_Map.at(field).value;
+  su2double GetHistoryFieldValue(const string& name) const {
+    auto it = historyOutput_Map.find(name);
+    if (it != historyOutput_Map.end()) return it->second.value;
+    SU2_MPI::Error("Cannot find output field with name " + name, CURRENT_FUNCTION);
+    return 0;
   }
 
  /*!
@@ -456,8 +459,11 @@ class COutput {
   * \param[in] iMarker - Index of the surface marker
   * \return Value of the field
   */
-  su2double GetHistoryFieldValuePerSurface(const string& field, unsigned short iMarker) const {
-    return historyOutputPerSurface_Map.at(field)[iMarker].value;
+  su2double GetHistoryFieldValuePerSurface(const string& name, unsigned short iMarker) const {
+    auto it = historyOutputPerSurface_Map.find(name);
+    if (it != historyOutputPerSurface_Map.end()) return it->second[iMarker].value;
+    SU2_MPI::Error("Cannot find output field with name " + name, CURRENT_FUNCTION);
+    return 0;
   }
 
   /*!
@@ -634,7 +640,7 @@ class COutput {
     if (it != historyOutput_Map.end()){
       it->second.value = value;
     } else {
-      SU2_MPI::Error(string("Cannot find output field with name ") + name, CURRENT_FUNCTION);
+      SU2_MPI::Error("Cannot find output field with name " + name, CURRENT_FUNCTION);
     }
   }
 
@@ -718,7 +724,6 @@ class COutput {
     volumeOutput_List.push_back(name);
   }
 
-
   /*!
    * \brief Set the value of a volume output field
    * \param[in] name - Name of the field.
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index ed0fb0f3a16..6abcdf13620 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -1352,6 +1352,8 @@ void CFlowOutput::LoadSurfaceData(CConfig *config, CGeometry *geometry, CSolver
 void CFlowOutput::AddAerodynamicCoefficients(const CConfig* config) {
 
   /// BEGIN_GROUP: AERO_COEFF, DESCRIPTION: Sum of the aerodynamic coefficients and forces on all surfaces (markers) set with MARKER_MONITORING.
+  /// DESCRIPTION: Reference force for aerodynamic coefficients
+  AddHistoryOutput("REFERENCE_FORCE", "RefForce", ScreenOutputFormat::FIXED, "AERO_COEFF", "Reference force used to compute aerodynamic coefficients", HistoryFieldType::COEFFICIENT);
   /// DESCRIPTION: Drag coefficient
   AddHistoryOutput("DRAG",       "CD",   ScreenOutputFormat::FIXED, "AERO_COEFF", "Total drag coefficient on all surfaces set with MARKER_MONITORING", HistoryFieldType::COEFFICIENT);
   /// DESCRIPTION: Lift coefficient
@@ -1409,6 +1411,7 @@ void CFlowOutput::AddAerodynamicCoefficients(const CConfig* config) {
 
 void CFlowOutput::SetAerodynamicCoefficients(const CConfig* config, const CSolver* flow_solver){
 
+  SetHistoryOutputValue("REFERENCE_FORCE", flow_solver->GetAeroCoeffsReferenceForce());
   SetHistoryOutputValue("DRAG", flow_solver->GetTotal_CD());
   SetHistoryOutputValue("LIFT", flow_solver->GetTotal_CL());
   if (nDim == 3)
diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index 2585121a29e..675c24e045a 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -58,106 +58,6 @@ void CDriver::PythonInterfacePreprocessing(CConfig** config, CGeometry**** geome
   }
 }
 
-/////////////////////////////////////////////////////////////////////////////
-/* Functions related to the global performance indices (Lift, Drag, etc.)  */
-/////////////////////////////////////////////////////////////////////////////
-
-passivedouble CDriver::Get_Drag() const {
-  unsigned short val_iZone = ZONE_0;
-  unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
-  su2double CDrag, factor, val_Drag;
-
-  /*--- Calculate drag force based on drag coefficient ---*/
-  factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
-  CDrag = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CD();
-
-  val_Drag = CDrag * factor;
-
-  return SU2_TYPE::GetValue(val_Drag);
-}
-
-passivedouble CDriver::Get_Lift() const {
-  unsigned short val_iZone = ZONE_0;
-  unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
-  su2double CLift, factor, val_Lift;
-
-  /*--- Calculate drag force based on drag coefficient ---*/
-  factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
-  CLift = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CL();
-
-  val_Lift = CLift * factor;
-
-  return SU2_TYPE::GetValue(val_Lift);
-}
-
-passivedouble CDriver::Get_Mx() const {
-  unsigned short val_iZone = ZONE_0;
-  unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
-  su2double CMx, RefLengthCoeff, factor, val_Mx;
-
-  RefLengthCoeff = config_container[val_iZone]->GetRefLength();
-
-  /*--- Calculate moment around x-axis based on coefficients ---*/
-  factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
-  CMx = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMx();
-
-  val_Mx = CMx * factor * RefLengthCoeff;
-
-  return SU2_TYPE::GetValue(val_Mx);
-}
-
-passivedouble CDriver::Get_My() const {
-  unsigned short val_iZone = ZONE_0;
-  unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
-  su2double CMy, RefLengthCoeff, factor, val_My;
-
-  RefLengthCoeff = config_container[val_iZone]->GetRefLength();
-
-  /*--- Calculate moment around x-axis based on coefficients ---*/
-  factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
-  CMy = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMy();
-
-  val_My = CMy * factor * RefLengthCoeff;
-
-  return SU2_TYPE::GetValue(val_My);
-}
-
-passivedouble CDriver::Get_Mz() const {
-  unsigned short val_iZone = ZONE_0;
-  unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
-  su2double CMz, RefLengthCoeff, factor, val_Mz;
-
-  RefLengthCoeff = config_container[val_iZone]->GetRefLength();
-
-  /*--- Calculate moment around z-axis based on coefficients ---*/
-  factor = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAeroCoeffsReferenceForce();
-  CMz = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMz();
-
-  val_Mz = CMz * factor * RefLengthCoeff;
-
-  return SU2_TYPE::GetValue(val_Mz);
-}
-
-passivedouble CDriver::Get_DragCoeff() const {
-  unsigned short val_iZone = ZONE_0;
-  unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
-  su2double CDrag;
-
-  CDrag = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CD();
-
-  return SU2_TYPE::GetValue(CDrag);
-}
-
-passivedouble CDriver::Get_LiftCoeff() const {
-  unsigned short val_iZone = ZONE_0;
-  unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
-  su2double CLift;
-
-  CLift = solver_container[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CL();
-
-  return SU2_TYPE::GetValue(CLift);
-}
-
 //////////////////////////////////////////////////////////////////////////////////
 /* Functions to obtain global parameters from SU2 (time steps, delta t, etc.)   */
 //////////////////////////////////////////////////////////////////////////////////
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 6aa13a0d6c3..3fab1454e09 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -268,11 +268,7 @@ void CDeformationDriver::Run() {
 
   /*--- Surface grid deformation using design variables. ---*/
 
-  if (driver_config->GetDeform_Mesh()) {
-    Update();
-  } else {
-    Update_Legacy();
-  }
+  Update();
 
   /*--- Synchronization point after a single solver iteration. Compute the wall clock time required. ---*/
 
@@ -294,6 +290,8 @@ void CDeformationDriver::Run() {
 }
 
 void CDeformationDriver::Update() {
+  if (!driver_config->GetDeform_Mesh()) return Update_Legacy();
+
   for (iZone = 0; iZone < nZone; iZone++) {
     /*--- Set the stiffness of each element mesh into the mesh numerics. ---*/
 

From 24b94df03eea1638cf33dcef005c8a793dc6e7dc Mon Sep 17 00:00:00 2001
From: Kursat Yurt <kursatyurt@gmail.com>
Date: Sun, 26 Mar 2023 03:10:40 +0200
Subject: [PATCH 313/656] refactor driver method names

---
 .../drivers/CDiscAdjMultizoneDriver.hpp       | 12 +--
 .../drivers/CDiscAdjSinglezoneDriver.hpp      |  2 +-
 SU2_CFD/include/drivers/CDriver.hpp           | 82 +++++++++----------
 SU2_CFD/include/drivers/CDriverBase.hpp       | 14 ++--
 SU2_CFD/include/drivers/CMultizoneDriver.hpp  |  8 +-
 SU2_CFD/include/drivers/CSinglezoneDriver.hpp |  2 +-
 .../src/drivers/CDiscAdjMultizoneDriver.cpp   | 34 ++++----
 .../src/drivers/CDiscAdjSinglezoneDriver.cpp  |  8 +-
 SU2_CFD/src/drivers/CDriver.cpp               | 76 ++++++++---------
 SU2_CFD/src/drivers/CDriverBase.cpp           |  2 +-
 SU2_CFD/src/drivers/CMultizoneDriver.cpp      | 16 ++--
 SU2_CFD/src/drivers/CSinglezoneDriver.cpp     |  4 +-
 SU2_CFD/src/python_wrapper_structure.cpp      | 18 ++--
 SU2_DEF/src/drivers/CDeformationDriver.cpp    |  2 +-
 .../src/drivers/CDiscAdjDeformationDriver.cpp |  2 +-
 15 files changed, 140 insertions(+), 142 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDiscAdjMultizoneDriver.hpp b/SU2_CFD/include/drivers/CDiscAdjMultizoneDriver.hpp
index 7e417e70349..3f61be0904b 100644
--- a/SU2_CFD/include/drivers/CDiscAdjMultizoneDriver.hpp
+++ b/SU2_CFD/include/drivers/CDiscAdjMultizoneDriver.hpp
@@ -211,7 +211,7 @@ class CDiscAdjMultizoneDriver : public CMultizoneDriver {
   /*!
    * \brief Initialize the adjoint value of the objective function.
    */
-  void SetAdj_ObjFunction();
+  void SetAdjObjFunction();
 
   /*!
    * \brief Summary of all routines to evaluate the adjoints in iZone.
@@ -236,31 +236,31 @@ class CDiscAdjMultizoneDriver : public CMultizoneDriver {
    * \brief Add Solution vector to External.
    * \param[in] iZone - Zone index.
    */
-  void Add_Solution_To_External(unsigned short iZone);
+  void AddSolutionToExternal(unsigned short iZone);
 
   /*!
    * \brief Puts dual time derivative vector to External.
    */
-  void Set_External_To_DualTimeDer();
+  void SetExternalToDualTimeDer();
 
   /*!
    * \brief Add External_Old vector to Solution.
    * \param[in] iZone - Zone index.
    */
-  void Add_External_To_Solution(unsigned short iZone);
+  void AddExternalToSolution(unsigned short iZone);
 
   /*!
    * \brief Puts Solution into SolutionOld.
    * \param[in] iZone - Zone index.
    */
-  void Set_SolutionOld_To_Solution(unsigned short iZone);
+  void SetSolutionOldToSolution(unsigned short iZone);
 
   /*!
    * \brief Extract contribution of iZone to jZone with BGS relaxation.
    * \param[in] iZone - Source zone (the one that was initialized).
    * \param[in] jZone - Target zone (the one that transfers to iZone in the primal problem).
    */
-  void Update_Cross_Term(unsigned short iZone, unsigned short jZone);
+  void UpdateCrossTerm(unsigned short iZone, unsigned short jZone);
 
   /*!
    * \brief Compute BGS residuals.
diff --git a/SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp b/SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp
index 8b0960565a4..206f245e400 100644
--- a/SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp
+++ b/SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp
@@ -111,7 +111,7 @@ class CDiscAdjSinglezoneDriver : public CSinglezoneDriver {
   /*!
    * \brief Initialize the adjoint value of the objective function.
    */
-  void SetAdj_ObjFunction(void);
+  void SetAdjObjFunction(void);
 
   /*!
    * \brief Record the main computational path.
diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index 9b3eae14a3a..1657d1b4c00 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -97,25 +97,25 @@ class CDriver : public CDriverBase {
   /*!
    * \brief Destructor of the class.
    */
-  virtual ~CDriver(void);
+  ~CDriver(void) override;
 
   /*!
    * \brief A virtual member.
    */
-  virtual void Run(){};
+  void Run() override{};
 
  protected:
   /*!
-   * \brief Init_Containers
+   * \brief Initialize containers. 
    */
-  void SetContainers_Null();
+  void SetContainersNull();
 
   /*!
    * \brief Read in the config and mesh files.
    * \param[in] config - Definition of the particular problem.
    * \param[in] driver_config - Definition of the driver configuration.
    */
-  void Input_Preprocessing(CConfig**& config, CConfig*& driver_config);
+  void InputPreprocessing(CConfig**& config, CConfig*& driver_config);
 
   /*!
    * \brief Construction of the edge-based data structure and the multi-grid structure.
@@ -123,7 +123,7 @@ class CDriver : public CDriverBase {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] dummy - Definition of the dummy driver.
    */
-  void Geometrical_Preprocessing(CConfig* config, CGeometry**& geometry, bool dummy);
+  void GeometricalPreprocessing(CConfig* config, CGeometry**& geometry, bool dummy);
 
   /*!
    * \brief Do the geometrical preprocessing for the DG FEM solver.
@@ -144,7 +144,7 @@ class CDriver : public CDriverBase {
    * \param[in] config - Definition of the particular problem.
    * \param[in] iteration - Pointer to the iteration container to be instantiated.
    */
-  void Iteration_Preprocessing(CConfig* config, CIteration*& iteration) const;
+  void IterationPreprocessing(CConfig* config, CIteration*& iteration) const;
 
   /*!
    * \brief Definition and allocation of all solution classes.
@@ -152,7 +152,7 @@ class CDriver : public CDriverBase {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] solver - Container vector with all the solutions.
    */
-  void Solver_Preprocessing(CConfig* config, CGeometry** geometry, CSolver***& solver);
+  void SolverPreprocessing(CConfig* config, CGeometry** geometry, CSolver***& solver);
 
   /*!
    * \brief Restart of the solvers from the restart files.
@@ -161,7 +161,7 @@ class CDriver : public CDriverBase {
    * \param[in] config - Definition of the particular problem.
    * \param[in] update_geo - Boolean to indicate if geometry should be updated.
    */
-  void Solver_Restart(CSolver*** solver, CGeometry** geometry, CConfig* config, bool update_geo);
+  void SolverRestart(CSolver*** solver, CGeometry** geometry, CConfig* config, bool update_geo);
 
   /*!
    * \brief Definition and allocation of all solution classes.
@@ -170,7 +170,7 @@ class CDriver : public CDriverBase {
    * \param[in] config - Definition of the particular problem.
    * \param[in] val_iInst - Current solver instance.
    */
-  void Solver_Postprocessing(CSolver**** solver, CGeometry** geometry, CConfig* config, unsigned short val_iInst);
+  void SolverPostprocessing(CSolver**** solver, CGeometry** geometry, CConfig* config, unsigned short val_iInst);
 
   /*!
    * \brief Definition and allocation of all integration classes.
@@ -178,7 +178,7 @@ class CDriver : public CDriverBase {
    * \param[in] solver - Container vector with all the solutions.
    * \param[in] integration - Container vector with all the integration methods.
    */
-  void Integration_Preprocessing(CConfig* config, CSolver** solver, CIntegration**& integration) const;
+  void IntegrationPreprocessing(CConfig* config, CSolver** solver, CIntegration**& integration) const;
 
   /*!
    * \brief Definition and allocation of all integration classes.
@@ -187,7 +187,7 @@ class CDriver : public CDriverBase {
    * \param[in] config - Definition of the particular problem.
    * \param[in] val_iInst - Current solver instance.
    */
-  void Integration_Postprocessing(CIntegration*** integration, CGeometry** geometry, CConfig* config,
+  void IntegrationPostprocessing(CIntegration*** integration, CGeometry** geometry, CConfig* config,
                                   unsigned short val_iInst);
 
   /*!
@@ -199,7 +199,7 @@ class CDriver : public CDriverBase {
    * \param[in] interface - Class defining the physical transfer of information.
    * \param[in] interpolation -  Object defining the interpolation.
    */
-  void Interface_Preprocessing(CConfig** config, CSolver***** solver, CGeometry**** geometry,
+  void InterfacePreprocessing(CConfig** config, CSolver***** solver, CGeometry**** geometry,
                                unsigned short** interface_types, CInterface*** interface,
                                vector<vector<unique_ptr<CInterpolator>>>& interpolation);
 
@@ -210,7 +210,7 @@ class CDriver : public CDriverBase {
    * \param[in] solver - Container vector with all the solutions.
    * \param[in] numerics - Description of the numerical method (the way in which the equations are solved).
    */
-  void Numerics_Preprocessing(CConfig* config, CGeometry** geometry, CSolver*** solver, CNumerics****& numerics) const;
+  void NumericsPreprocessing(CConfig* config, CGeometry** geometry, CSolver*** solver, CNumerics****& numerics) const;
 
   /*!
    * \brief Helper to instantiate turbulence numerics specialized for different flow solvers.
@@ -240,7 +240,7 @@ class CDriver : public CDriverBase {
    * \param[in] config - Definition of the particular problem.
    * \param[in] val_iInst - Current solver instance.
    */
-  void Numerics_Postprocessing(CNumerics***** numerics, CSolver*** solver, CGeometry** geometry, CConfig* config,
+  void NumericsPostprocessing(CNumerics***** numerics, CSolver*** solver, CGeometry** geometry, CConfig* config,
                                unsigned short val_iInst);
 
   /*!
@@ -252,7 +252,7 @@ class CDriver : public CDriverBase {
    * \param[in] grid_movement - Volume grid movement classes of the problem.
    * \param[in] surface_movement - Surface movement classes of the problem.
    */
-  void DynamicMesh_Preprocessing(CConfig* config, CGeometry** geometry, CSolver*** solver, CIteration* iteration,
+  void DynamicMeshPreprocessing(CConfig* config, CGeometry** geometry, CSolver*** solver, CIteration* iteration,
                                  CVolumetricMovement*& grid_movement, CSurfaceMovement*& surface_movement) const;
 
   /*!
@@ -271,7 +271,7 @@ class CDriver : public CDriverBase {
    * \param[in] output_container - Container vector with all the outputs.
    * \param[in] driver_output - Definition of the driver output.
    */
-  void Output_Preprocessing(CConfig** config, CConfig* driver_config, COutput**& output_container,
+  void OutputPreprocessing(CConfig** config, CConfig* driver_config, COutput**& output_container,
                             COutput*& driver_output);
 
   /*!
@@ -279,7 +279,7 @@ class CDriver : public CDriverBase {
    * \param[in] config - Definition of the particular problem.
    * \param[in] geometry - Geometrical definition of the problem.
    */
-  void StaticMesh_Preprocessing(const CConfig* config, CGeometry** geometry);
+  void StaticMeshPreprocessing(const CConfig* config, CGeometry** geometry);
 
   /*!
    * \brief Initiate value for static mesh movement such as the gridVel for the ROTATING frame.
@@ -288,7 +288,7 @@ class CDriver : public CDriverBase {
    * \param[in] solver - Container vector with all the solutions.
    * \param[in] interface - Class defining the physical transfer of information.
    */
-  void Turbomachinery_Preprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver,
+  void TurbomachineryPreprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver,
                                     CInterface*** interface);
 
   /*!
@@ -296,28 +296,28 @@ class CDriver : public CDriverBase {
    * \param[in] donorZone - zone in which the displacements will be predicted.
    * \param[in] targetZone - zone which receives the predicted displacements.
    */
-  virtual void Predict_Displacements(unsigned short donorZone, unsigned short targetZone) {}
+  virtual void PredictDisplacements(unsigned short donorZone, unsigned short targetZone) {}
 
   /*!
    * \brief A virtual member.
    * \param[in] donorZone - zone in which the tractions will be predicted.
    * \param[in] targetZone - zone which receives the predicted traction.
    */
-  virtual void Predict_Tractions(unsigned short donorZone, unsigned short targetZone) {}
+  virtual void PredictTractions(unsigned short donorZone, unsigned short targetZone) {}
 
   /*!
    * \brief A virtual member.
    * \param[in] donorZone - zone in which the displacements will be transferred.
    * \param[in] targetZone - zone which receives the tractions transferred.
    */
-  virtual void Transfer_Displacements(unsigned short donorZone, unsigned short targetZone) {}
+  virtual void TransferDisplacements(unsigned short donorZone, unsigned short targetZone) {}
 
   /*!
    * \brief A virtual member.
    * \param[in] donorZone - zone from which the tractions will be transferred.
    * \param[in] targetZone - zone which receives the tractions transferred.
    */
-  virtual void Transfer_Tractions(unsigned short donorZone, unsigned short targetZone) {}
+  virtual void TransferTractions(unsigned short donorZone, unsigned short targetZone) {}
 
   /*!
    * \brief A virtual member.
@@ -325,7 +325,7 @@ class CDriver : public CDriverBase {
    * \param[in] targetZone - destination of the information.
    * \param[in] iOuterIter - Fluid-Structure Interaction subiteration.
    */
-  virtual void Relaxation_Displacements(unsigned short donorZone, unsigned short targetZone, unsigned long iOuterIter) {}
+  virtual void RelaxationDisplacements(unsigned short donorZone, unsigned short targetZone, unsigned long iOuterIter) {}
 
   /*!
    * \brief A virtual member.
@@ -333,28 +333,28 @@ class CDriver : public CDriverBase {
    * \param[in] targetZone - destination of the information.
    * \param[in] iOuterIter - Fluid-Structure Interaction subiteration.
    */
-  virtual void Relaxation_Tractions(unsigned short donorZone, unsigned short targetZone, unsigned long iOuterIter) {}
+  virtual void RelaxationTractions(unsigned short donorZone, unsigned short targetZone, unsigned long iOuterIter) {}
 
   /*!
    * \brief A virtual member to run a Block Gauss-Seidel iteration in multi-zone problems.
    */
-  virtual void Run_GaussSeidel() {}
+  virtual void RunGaussSeidel() {}
 
   /*!
    * \brief A virtual member to run a Block-Jacobi iteration in multi-zone problems.
    */
-  virtual void Run_Jacobi() {}
+  virtual void RunJacobi() {}
 
   /*!
    * \brief A virtual member.
    */
-  virtual void Update() {}
+  void Update() override {}
 
   /*!
    * \brief Print out the direct residuals.
    * \param[in] kind_recording - Type of recording (full list in ENUM_RECORDING, option_structure.hpp)
    */
-  void Print_DirectResidual(RECORDING kind_recording);
+  void PrintDirectResidual(RECORDING kind_recording);
 
  public:
   /*!
@@ -365,7 +365,7 @@ class CDriver : public CDriverBase {
   /*!
    * \brief Deallocation routine
    */
-  void Finalize();
+  void Finalize() override;
 
   /*!
    * \brief A virtual member.
@@ -416,43 +416,43 @@ class CDriver : public CDriverBase {
    * \brief Get the total drag.
    * \return Total drag.
    */
-  passivedouble Get_Drag() const;
+  passivedouble GetDrag() const;
 
   /*!
    * \brief Get the total lift.
    * \return Total lift.
    */
-  passivedouble Get_Lift() const;
+  passivedouble GetLift() const;
 
   /*!
    * \brief Get the total x moment.
    * \return Total x moment.
    */
-  passivedouble Get_Mx() const;
+  passivedouble GetMx() const;
 
   /*!
    * \brief Get the total y moment.
    * \return Total y moment.
    */
-  passivedouble Get_My() const;
+  passivedouble GetMy() const;
 
   /*!
    * \brief Get the total z moment.
    * \return Total z moment.
    */
-  passivedouble Get_Mz() const;
+  passivedouble GetMz() const;
 
   /*!
    * \brief Get the total drag coefficient.
    * \return Total drag coefficient.
    */
-  passivedouble Get_DragCoeff() const;
+  passivedouble GetDragCoeff() const;
 
   /*!
    * \brief Get the total lift coefficient.
    * \return Total lift coefficient.
    */
-  passivedouble Get_LiftCoeff() const;
+  passivedouble GetLiftCoeff() const;
 
   /*!
    * \brief Get the number of external iterations.
@@ -484,7 +484,7 @@ class CDriver : public CDriverBase {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void Inlet_Preprocessing(CSolver*** solver, CGeometry** geometry, CConfig* config) const;
+  void InletPreprocessing(CSolver*** solver, CGeometry** geometry, CConfig* config) const;
 
   /*!
    * \brief Set the position of the heat source.
@@ -493,14 +493,14 @@ class CDriver : public CDriverBase {
    * \param[in] pos_y - Position Y.
    * \param[in] pos_z - Position Z.
    */
-  void SetHeatSource_Position(passivedouble alpha, passivedouble pos_x, passivedouble pos_y, passivedouble pos_z);
+  void SetHeatSourcePosition(passivedouble alpha, passivedouble pos_x, passivedouble pos_y, passivedouble pos_z);
 
   /*!
    * \brief Set the direction of the inlet.
    * \param[in] iMarker - Marker index.
    * \param[in] alpha - Angle (Zpos).
    */
-  void SetInlet_Angle(unsigned short iMarker, passivedouble alpha);
+  void SetInletAngle(unsigned short iMarker, passivedouble alpha);
 
 /// \}
 
@@ -636,7 +636,7 @@ class CFluidDriver : public CDriver {
   /*!
    * \brief Transfer data among different zones (multiple zone).
    */
-  void Transfer_Data(unsigned short donorZone, unsigned short targetZone);
+  void TransferData(unsigned short donorZone, unsigned short targetZone);
 };
 
 /*!
diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index b6ceafcd4dc..9b94835febf 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -110,7 +110,7 @@ class CDriverBase {
   /*!
    * \brief A virtual member.
    */
-  virtual void Update_Legacy(){}
+  virtual void UpdateLegacy(){}
 
   /*!
    * \brief A virtual member.
@@ -646,7 +646,7 @@ class CDriverBase {
   /*!
    * \brief Initialize containers.
    */
-  void SetContainers_Null();
+  void SetContainersNull();
 
   /*!
    * \brief Delete containers.
@@ -658,7 +658,7 @@ class CDriverBase {
    * \param[in] config - Definition of the particular problem.
    * \param[in] driver_config - Definition of the driver configuration.
    */
-  void Input_Preprocessing(CConfig**& config, CConfig*& driver_config);
+  void InputPreprocessing(CConfig**& config, CConfig*& driver_config);
 
   /*!
    * \brief Construction of the edge-based data structure and the multi-grid structure.
@@ -666,7 +666,7 @@ class CDriverBase {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] dummy - Definition of the dummy driver.
    */
-  void Geometrical_Preprocessing(CConfig* config, CGeometry**& geometry, bool dummy);
+  void GeometricalPreprocessing(CConfig* config, CGeometry**& geometry, bool dummy);
 
   /*!
    * \brief Definition and allocation of all solution classes.
@@ -674,7 +674,7 @@ class CDriverBase {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] solver - Container vector with all the solutions.
    */
-  void Solver_Preprocessing(CConfig* config, CGeometry** geometry, CSolver***& solver);
+  void SolverPreprocessing(CConfig* config, CGeometry** geometry, CSolver***& solver);
 
   /*!
    * \brief Definition and allocation of all solver classes.
@@ -683,7 +683,7 @@ class CDriverBase {
    * \param[in] solver - Container vector with all the solutions.
    * \param[in] numerics - Description of the numerical method (the way in which the equations are solved).
    */
-  void Numerics_Preprocessing(CConfig* config, CGeometry** geometry, CSolver*** solver, CNumerics****& numerics) const;
+  void NumericsPreprocessing(CConfig* config, CGeometry** geometry, CSolver*** solver, CNumerics****& numerics) const;
 
   /*!
    * \brief Preprocess the output container.
@@ -692,6 +692,6 @@ class CDriverBase {
    * \param[in] output_container - Container vector with all the outputs.
    * \param[in] driver_output - Definition of the driver output.
    */
-  void Output_Preprocessing(CConfig** config, CConfig* driver_config, COutput**& output_container,
+  void OutputPreprocessing(CConfig** config, CConfig* driver_config, COutput**& output_container,
                             COutput*& driver_output);
 };
diff --git a/SU2_CFD/include/drivers/CMultizoneDriver.hpp b/SU2_CFD/include/drivers/CMultizoneDriver.hpp
index 91fe6234a71..e1f9d05dd9a 100644
--- a/SU2_CFD/include/drivers/CMultizoneDriver.hpp
+++ b/SU2_CFD/include/drivers/CMultizoneDriver.hpp
@@ -92,13 +92,11 @@ class CMultizoneDriver : public CDriver {
   /*!
    * \brief Run a Block Gauss-Seidel iteration in all physical zones.
    */
-  void Run_GaussSeidel() override;
-
+  void RunGaussSeidel() override;
   /*!
    * \brief Run a Block-Jacobi iteration in all physical zones.
    */
-  void Run_Jacobi() override;
-
+  void RunJacobi() override;
   /*!
    * \brief Update the dual-time solution within multiple zones.
    */
@@ -128,7 +126,7 @@ class CMultizoneDriver : public CDriver {
    * \brief Routine to provide all the desired physical transfers between the different zones during one iteration.
    * \return Boolean that determines whether the mesh needs to be updated for this particular transfer
    */
-  bool Transfer_Data(unsigned short donorZone, unsigned short targetZone);
+  bool TransferData(unsigned short donorZone, unsigned short targetZone);
 
   /*!
    * \brief Check if simulation converged and return appropriate boolean.
diff --git a/SU2_CFD/include/drivers/CSinglezoneDriver.hpp b/SU2_CFD/include/drivers/CSinglezoneDriver.hpp
index 5cfd90acb01..8f7a11f9ba4 100644
--- a/SU2_CFD/include/drivers/CSinglezoneDriver.hpp
+++ b/SU2_CFD/include/drivers/CSinglezoneDriver.hpp
@@ -113,6 +113,6 @@ class CSinglezoneDriver : public CDriver {
   /*!
    * \brief Runtime_Parsing
    */
-  virtual void Runtime_Options();
+  virtual void RuntimeOptions();
 
 };
diff --git a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
index 882e8a8e0d8..8ace258cfc4 100644
--- a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
@@ -153,7 +153,7 @@ void CDiscAdjMultizoneDriver::Preprocess(unsigned long TimeIter) {
           mat = 0.0;
 
     /*--- Initialize external with dynamic contributions. ---*/
-    Set_External_To_DualTimeDer();
+    SetExternalToDualTimeDer();
   }
 
 }
@@ -245,7 +245,7 @@ bool CDiscAdjMultizoneDriver::Iterate(unsigned short iZone, unsigned long iInner
   /*--- This is done explicitly here for multizone cases, only in inner iterations and not when
    *    extracting cross terms so that the adjoint residuals in each zone still make sense. ---*/
 
-  if (!KrylovMode) Set_SolutionOld_To_Solution(iZone);
+  if (!KrylovMode) SetSolutionOldToSolution(iZone);
 
   /*--- Print out the convergence data to screen and history file. ---*/
 
@@ -262,7 +262,7 @@ void CDiscAdjMultizoneDriver::KrylovInnerIters(unsigned short iZone) {
 
   GetAdjointRHS(iZone, AdjRHS[iZone]);
 
-  Add_External_To_Solution(iZone);
+  AddExternalToSolution(iZone);
 
   GetAllSolutions(iZone, true, AdjSol[iZone]);
 
@@ -388,7 +388,7 @@ void CDiscAdjMultizoneDriver::Run() {
           /*--- Add off-diagonal contribution (including the OF gradient) to Solution. ---*/
 
           if (no_restart || (iInnerIter > 0)) {
-            Add_External_To_Solution(iZone);
+            AddExternalToSolution(iZone);
           }
           else {
             /*--- If we restarted, Solution already has all contributions,
@@ -424,7 +424,7 @@ void CDiscAdjMultizoneDriver::Run() {
 
           /*--- Extract the cross-term performing a relaxed update of it and of the sum (External) for jZone. ---*/
 
-          Update_Cross_Term(iZone, jZone);
+          UpdateCrossTerm(iZone, jZone);
         }
       }
 
@@ -470,7 +470,7 @@ bool CDiscAdjMultizoneDriver::EvaluateObjectiveFunctionGradient() {
   RecordingState = RECORDING::CLEAR_INDICES;
 
   AD::ClearAdjoints();
-  SetAdj_ObjFunction();
+  SetAdjObjFunction();
   AD::ComputeAdjoint(OBJECTIVE_FUNCTION, START);
 
   /*--- Initialize External with the objective function gradient. ---*/
@@ -481,7 +481,7 @@ bool CDiscAdjMultizoneDriver::EvaluateObjectiveFunctionGradient() {
 
     iteration_container[iZone][INST_0]->IterateDiscAdj(geometry_container, solver_container,
                                                        config_container, iZone, INST_0, false);
-    Add_Solution_To_External(iZone);
+    AddSolutionToExternal(iZone);
 
     for (unsigned short iSol=0; iSol < MAX_SOLS; iSol++) {
       auto solver = solver_container[iZone][INST_0][MESH_0][iSol];
@@ -512,7 +512,7 @@ void CDiscAdjMultizoneDriver::EvaluateSensitivities(unsigned long Iter, bool for
 
     Set_Solution_To_BGSSolution_k(iZone);
 
-    Add_External_To_Solution(iZone);
+    AddExternalToSolution(iZone);
 
     iteration_container[iZone][INST_0]->InitializeAdjoint(solver_container, geometry_container,
                                                           config_container, iZone, INST_0);
@@ -520,7 +520,7 @@ void CDiscAdjMultizoneDriver::EvaluateSensitivities(unsigned long Iter, bool for
 
   /*--- Initialize the adjoint of the objective function with 1.0. ---*/
 
-  SetAdj_ObjFunction();
+  SetAdjObjFunction();
 
   /*--- Interpret the stored information by calling the corresponding routine of the AD tool. ---*/
 
@@ -666,7 +666,7 @@ void CDiscAdjMultizoneDriver::SetRecording(RECORDING kind_recording, Kind_Tape t
                                                          config_container, iZone, INST_0);
       AD::Push_TapePosition(); /// leave_zone
     }
-    Print_DirectResidual(kind_recording);
+    PrintDirectResidual(kind_recording);
   }
 
   if (kind_recording != RECORDING::CLEAR_INDICES && driver_config->GetWrt_AD_Statistics()) {
@@ -763,7 +763,7 @@ void CDiscAdjMultizoneDriver::SetObjFunction(RECORDING kind_recording) {
   }
 }
 
-void CDiscAdjMultizoneDriver::SetAdj_ObjFunction() {
+void CDiscAdjMultizoneDriver::SetAdjObjFunction() {
 
   const auto IterAvg_Obj = config_container[ZONE_0]->GetIter_Avg_Objective();
   su2double seeding = 1.0;
@@ -861,7 +861,7 @@ void CDiscAdjMultizoneDriver::HandleDataTransfer() {
     for (unsigned short jZone = 0; jZone < nZone; jZone++){
       /*--- The target zone is iZone ---*/
       if (jZone != iZone && interface_container[jZone][iZone] != nullptr) {
-        DeformMesh |= Transfer_Data(jZone, iZone);
+        DeformMesh |= TransferData(jZone, iZone);
       }
     }
 
@@ -873,7 +873,7 @@ void CDiscAdjMultizoneDriver::HandleDataTransfer() {
   }
 }
 
-void CDiscAdjMultizoneDriver::Add_Solution_To_External(unsigned short iZone) {
+void CDiscAdjMultizoneDriver::AddSolutionToExternal(unsigned short iZone) {
 
   for (unsigned short iSol=0; iSol < MAX_SOLS; iSol++) {
     auto solver = solver_container[iZone][INST_0][MESH_0][iSol];
@@ -882,7 +882,7 @@ void CDiscAdjMultizoneDriver::Add_Solution_To_External(unsigned short iZone) {
   }
 }
 
-void CDiscAdjMultizoneDriver::Set_External_To_DualTimeDer() {
+void CDiscAdjMultizoneDriver::SetExternalToDualTimeDer() {
 
   for (unsigned short iZone = 0; iZone < nZone; iZone++) {
     for (unsigned short iSol=0; iSol < MAX_SOLS; iSol++) {
@@ -893,7 +893,7 @@ void CDiscAdjMultizoneDriver::Set_External_To_DualTimeDer() {
   }
 }
 
-void CDiscAdjMultizoneDriver::Add_External_To_Solution(unsigned short iZone) {
+void CDiscAdjMultizoneDriver::AddExternalToSolution(unsigned short iZone) {
 
   for (unsigned short iSol=0; iSol < MAX_SOLS; iSol++) {
     auto solver = solver_container[iZone][INST_0][MESH_0][iSol];
@@ -902,7 +902,7 @@ void CDiscAdjMultizoneDriver::Add_External_To_Solution(unsigned short iZone) {
   }
 }
 
-void CDiscAdjMultizoneDriver::Set_SolutionOld_To_Solution(unsigned short iZone) {
+void CDiscAdjMultizoneDriver::SetSolutionOldToSolution(unsigned short iZone) {
 
   for (unsigned short iSol=0; iSol < MAX_SOLS; iSol++) {
     auto solver = solver_container[iZone][INST_0][MESH_0][iSol];
@@ -911,7 +911,7 @@ void CDiscAdjMultizoneDriver::Set_SolutionOld_To_Solution(unsigned short iZone)
   }
 }
 
-void CDiscAdjMultizoneDriver::Update_Cross_Term(unsigned short iZone, unsigned short jZone) {
+void CDiscAdjMultizoneDriver::UpdateCrossTerm(unsigned short iZone, unsigned short jZone) {
 
   for (unsigned short iSol=0; iSol < MAX_SOLS; iSol++) {
     auto solver = solver_container[jZone][INST_0][MESH_0][iSol];
diff --git a/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
index ef4e4e690d0..4b93d3396c3 100644
--- a/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
@@ -173,7 +173,7 @@ void CDiscAdjSinglezoneDriver::Run() {
 
     /*--- Initialize the adjoint of the objective function with 1.0. ---*/
 
-    SetAdj_ObjFunction();
+    SetAdjObjFunction();
 
     /*--- Interpret the stored information by calling the corresponding routine of the AD tool. ---*/
 
@@ -320,7 +320,7 @@ void CDiscAdjSinglezoneDriver::SetRecording(RECORDING kind_recording){
 
 }
 
-void CDiscAdjSinglezoneDriver::SetAdj_ObjFunction(){
+void CDiscAdjSinglezoneDriver::SetAdjObjFunction(){
 
   const auto IterAvg_Obj = config->GetIter_Avg_Objective();
   su2double seeding = 1.0;
@@ -429,7 +429,7 @@ void CDiscAdjSinglezoneDriver::DirectRun(RECORDING kind_recording){
 
   /*--- Print the direct residual to screen ---*/
 
-  Print_DirectResidual(kind_recording);
+  PrintDirectResidual(kind_recording);
 
 }
 
@@ -462,7 +462,7 @@ void CDiscAdjSinglezoneDriver::SecondaryRecording(){
 
   /*--- Initialize the adjoint of the objective function with 1.0. ---*/
 
-  SetAdj_ObjFunction();
+  SetAdjObjFunction();
 
   /*--- Interpret the stored information by calling the corresponding routine of the AD tool. ---*/
 
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index a5881a197de..f1bb3500382 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -115,11 +115,11 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
 
   /*--- Initialize containers with null --- */
 
-  SetContainers_Null();
+  SetContainersNull();
 
   /*--- Preprocessing of the config files. ---*/
 
-  Input_Preprocessing(config_container, driver_config);
+  InputPreprocessing(config_container, driver_config);
 
   /*--- Retrieve dimension from mesh file ---*/
 
@@ -128,7 +128,7 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
 
   /*--- Output preprocessing ---*/
 
-  Output_Preprocessing(config_container, driver_config, output_container, driver_output);
+  OutputPreprocessing(config_container, driver_config, output_container, driver_output);
 
 
   for (iZone = 0; iZone < nZone; iZone++) {
@@ -158,7 +158,7 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
        identified and linked, face areas and volumes of the dual mesh cells are
        computed, and the multigrid levels are created using an agglomeration procedure. ---*/
 
-      Geometrical_Preprocessing(config_container[iZone], geometry_container[iZone][iInst], dry_run);
+      GeometricalPreprocessing(config_container[iZone], geometry_container[iZone][iInst], dry_run);
 
     }
   }
@@ -181,7 +181,7 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
        fluxes, loops over the nodes to compute source terms, and routines for
        imposing various boundary condition type for the PDE. ---*/
 
-      Solver_Preprocessing(config_container[iZone], geometry_container[iZone][iInst], solver_container[iZone][iInst]);
+      SolverPreprocessing(config_container[iZone], geometry_container[iZone][iInst], solver_container[iZone][iInst]);
 
       /*--- Definition of the numerical method class:
        numerics_container[#ZONES][#INSTANCES][#MG_GRIDS][#EQ_SYSTEMS][#EQ_TERMS].
@@ -190,7 +190,7 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
        data structure (centered, upwind, galerkin), as well as any source terms
        (piecewise constant reconstruction) evaluated in each dual mesh volume. ---*/
 
-      Numerics_Preprocessing(config_container[iZone], geometry_container[iZone][iInst],
+      NumericsPreprocessing(config_container[iZone], geometry_container[iZone][iInst],
                              solver_container[iZone][iInst], numerics_container[iZone][iInst]);
 
       /*--- Definition of the integration class: integration_container[#ZONES][#INSTANCES][#EQ_SYSTEMS].
@@ -199,7 +199,7 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
        the residual at each node, R(U) and then integrates the equations to a
        steady state or time-accurately. ---*/
 
-      Integration_Preprocessing(config_container[iZone], solver_container[iZone][iInst][MESH_0],
+      IntegrationPreprocessing(config_container[iZone], solver_container[iZone][iInst][MESH_0],
                                 integration_container[iZone][iInst]);
 
       /*--- Instantiate the type of physics iteration to be executed within each zone. For
@@ -207,16 +207,16 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
        different physics in different zones (fluid-structure interaction), or couple multiple
        systems tightly within a single zone by creating a new iteration class (e.g., RANS). ---*/
 
-      Iteration_Preprocessing(config_container[iZone], iteration_container[iZone][iInst]);
+      IterationPreprocessing(config_container[iZone], iteration_container[iZone][iInst]);
 
       /*--- Dynamic mesh processing.  ---*/
 
-      DynamicMesh_Preprocessing(config_container[iZone], geometry_container[iZone][iInst], solver_container[iZone][iInst],
+      DynamicMeshPreprocessing(config_container[iZone], geometry_container[iZone][iInst], solver_container[iZone][iInst],
                                 iteration_container[iZone][iInst], grid_movement[iZone][iInst], surface_movement[iZone]);
 
       /*--- Static mesh processing.  ---*/
 
-      StaticMesh_Preprocessing(config_container[iZone], geometry_container[iZone][iInst]);
+      StaticMeshPreprocessing(config_container[iZone], geometry_container[iZone][iInst]);
 
     }
 
@@ -233,14 +233,14 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
     if (rank == MASTER_NODE)
       cout << endl <<"------------------- Multizone Interface Preprocessing -------------------" << endl;
 
-    Interface_Preprocessing(config_container, solver_container, geometry_container,
+    InterfacePreprocessing(config_container, solver_container, geometry_container,
                             interface_types, interface_container, interpolator_container);
   }
 
   if (fsi) {
     for (iZone = 0; iZone < nZone; iZone++) {
       for (iInst = 0; iInst < nInst[iZone]; iInst++){
-        Solver_Restart(solver_container[iZone][iInst], geometry_container[iZone][iInst],
+        SolverRestart(solver_container[iZone][iInst], geometry_container[iZone][iInst],
                        config_container[iZone], true);
       }
     }
@@ -250,7 +250,7 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
     if (rank == MASTER_NODE)
       cout << endl <<"---------------------- Turbomachinery Preprocessing ---------------------" << endl;
 
-    Turbomachinery_Preprocessing(config_container, geometry_container, solver_container, interface_container);
+    TurbomachineryPreprocessing(config_container, geometry_container, solver_container, interface_container);
   }
 
 
@@ -295,7 +295,7 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
 
 }
 
-void CDriver::SetContainers_Null(){
+void CDriver::SetContainersNull(){
 
   /*--- Create pointers to all of the classes that may be used throughout
    the SU2_CFD code. In general, the pointers are instantiated down a
@@ -367,7 +367,7 @@ void CDriver::Finalize() {
 
   for (iZone = 0; iZone < nZone; iZone++) {
     for (iInst = 0; iInst < nInst[iZone]; iInst++){
-      Numerics_Postprocessing(numerics_container[iZone], solver_container[iZone][iInst],
+      NumericsPostprocessing(numerics_container[iZone], solver_container[iZone][iInst],
           geometry_container[iZone][iInst], config_container[iZone], iInst);
     }
     delete [] numerics_container[iZone];
@@ -377,7 +377,7 @@ void CDriver::Finalize() {
 
   for (iZone = 0; iZone < nZone; iZone++) {
     for (iInst = 0; iInst < nInst[iZone]; iInst++){
-      Integration_Postprocessing(integration_container[iZone],
+      IntegrationPostprocessing(integration_container[iZone],
           geometry_container[iZone][iInst],
           config_container[iZone],
           iInst);
@@ -389,7 +389,7 @@ void CDriver::Finalize() {
 
   for (iZone = 0; iZone < nZone; iZone++) {
     for (iInst = 0; iInst < nInst[iZone]; iInst++){
-      Solver_Postprocessing(solver_container[iZone],
+      SolverPostprocessing(solver_container[iZone],
           geometry_container[iZone][iInst],
           config_container[iZone],
           iInst);
@@ -549,7 +549,7 @@ void CDriver::Finalize() {
 }
 
 
-void CDriver::Input_Preprocessing(CConfig **&config, CConfig *&driver_config) {
+void CDriver::InputPreprocessing(CConfig **&config, CConfig *&driver_config) {
 
   char zone_file_name[MAX_STRING_SIZE];
 
@@ -601,7 +601,7 @@ void CDriver::Input_Preprocessing(CConfig **&config, CConfig *&driver_config) {
   fsi = config_container[ZONE_0]->GetFSI_Simulation();
 }
 
-void CDriver::Geometrical_Preprocessing(CConfig* config, CGeometry **&geometry, bool dummy){
+void CDriver::GeometricalPreprocessing(CConfig* config, CGeometry **&geometry, bool dummy){
 
   if (!dummy){
     if (rank == MASTER_NODE)
@@ -1014,7 +1014,7 @@ void CDriver::Geometrical_Preprocessing_DGFEM(CConfig* config, CGeometry **&geom
 
 }
 
-void CDriver::Solver_Preprocessing(CConfig* config, CGeometry** geometry, CSolver ***&solver) {
+void CDriver::SolverPreprocessing(CConfig* config, CGeometry** geometry, CSolver ***&solver) {
 
   MAIN_SOLVER kindSolver = config->GetKind_Solver();
 
@@ -1037,15 +1037,15 @@ void CDriver::Solver_Preprocessing(CConfig* config, CGeometry** geometry, CSolve
   /*--- Restart solvers, for FSI the geometry cannot be updated because the interpolation classes
    * should always use the undeformed mesh (otherwise the results would not be repeatable). ---*/
 
-  if (!fsi) Solver_Restart(solver, geometry, config, true);
+  if (!fsi) SolverRestart(solver, geometry, config, true);
 
   /*--- Set up any necessary inlet profiles ---*/
 
-  Inlet_Preprocessing(solver, geometry, config);
+  InletPreprocessing(solver, geometry, config);
 
 }
 
-void CDriver::Inlet_Preprocessing(CSolver ***solver, CGeometry **geometry,
+void CDriver::InletPreprocessing(CSolver ***solver, CGeometry **geometry,
                                   CConfig *config) const {
 
   /*--- Adjust iteration number for unsteady restarts. ---*/
@@ -1117,7 +1117,7 @@ void CDriver::Inlet_Preprocessing(CSolver ***solver, CGeometry **geometry,
 
 }
 
-void CDriver::Solver_Restart(CSolver ***solver, CGeometry **geometry,
+void CDriver::SolverRestart(CSolver ***solver, CGeometry **geometry,
                              CConfig *config, bool update_geo) {
 
   /*--- Check for restarts and use the LoadRestart() routines. ---*/
@@ -1172,7 +1172,7 @@ void CDriver::Solver_Restart(CSolver ***solver, CGeometry **geometry,
 
 }
 
-void CDriver::Solver_Postprocessing(CSolver ****solver, CGeometry **geometry,
+void CDriver::SolverPostprocessing(CSolver ****solver, CGeometry **geometry,
                                     CConfig *config, unsigned short val_iInst) {
 
   for (int iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
@@ -1187,7 +1187,7 @@ void CDriver::Solver_Postprocessing(CSolver ****solver, CGeometry **geometry,
 
 }
 
-void CDriver::Integration_Preprocessing(CConfig *config, CSolver **solver, CIntegration **&integration) const {
+void CDriver::IntegrationPreprocessing(CConfig *config, CSolver **solver, CIntegration **&integration) const {
 
   if (rank == MASTER_NODE)
     cout << endl <<"----------------- Integration Preprocessing ( Zone " << config->GetiZone() <<" ) ------------------" << endl;
@@ -1198,7 +1198,7 @@ void CDriver::Integration_Preprocessing(CConfig *config, CSolver **solver, CInte
 
 }
 
-void CDriver::Integration_Postprocessing(CIntegration ***integration, CGeometry **geometry, CConfig *config, unsigned short val_iInst) {
+void CDriver::IntegrationPostprocessing(CIntegration ***integration, CGeometry **geometry, CConfig *config, unsigned short val_iInst) {
 
   for (unsigned int iSol = 0; iSol < MAX_SOLS; iSol++){
     delete integration[val_iInst][iSol];
@@ -1447,7 +1447,7 @@ template void CDriver::InstantiateSpeciesNumerics<CIncEulerVariable::CIndices<un
 template void CDriver::InstantiateSpeciesNumerics<CNEMOEulerVariable::CIndices<unsigned short>>(
     unsigned short, int, const CConfig*, const CSolver*, CNumerics****&) const;
 
-void CDriver::Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***solver, CNumerics ****&numerics) const {
+void CDriver::NumericsPreprocessing(CConfig *config, CGeometry **geometry, CSolver ***solver, CNumerics ****&numerics) const {
 
   if (rank == MASTER_NODE)
     cout << endl <<"------------------- Numerics Preprocessing ( Zone " << config->GetiZone() <<" ) -------------------" << endl;
@@ -2370,7 +2370,7 @@ void CDriver::Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSol
 
 }
 
-void CDriver::Numerics_Postprocessing(CNumerics *****numerics, CSolver***, CGeometry**,
+void CDriver::NumericsPostprocessing(CNumerics *****numerics, CSolver***, CGeometry**,
                                       CConfig *config, unsigned short val_iInst) {
 
   for (unsigned short iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
@@ -2389,7 +2389,7 @@ void CDriver::Numerics_Postprocessing(CNumerics *****numerics, CSolver***, CGeom
 
 }
 
-void CDriver::Iteration_Preprocessing(CConfig* config, CIteration *&iteration) const {
+void CDriver::IterationPreprocessing(CConfig* config, CIteration *&iteration) const {
 
   if (rank == MASTER_NODE)
     cout << endl <<"------------------- Iteration Preprocessing ( Zone " << config->GetiZone() <<" ) ------------------" << endl;
@@ -2398,7 +2398,7 @@ void CDriver::Iteration_Preprocessing(CConfig* config, CIteration *&iteration) c
 
 }
 
-void CDriver::DynamicMesh_Preprocessing(CConfig *config, CGeometry **geometry, CSolver ***solver, CIteration* iteration,
+void CDriver::DynamicMeshPreprocessing(CConfig *config, CGeometry **geometry, CSolver ***solver, CIteration* iteration,
                                         CVolumetricMovement *&grid_movement, CSurfaceMovement *&surface_movement) const{
 
   /*--- Instantiate the geometry movement classes for the solution of unsteady
@@ -2439,7 +2439,7 @@ void CDriver::DynamicMesh_Preprocessing(CConfig *config, CGeometry **geometry, C
 
 }
 
-void CDriver::Interface_Preprocessing(CConfig **config, CSolver***** solver, CGeometry**** geometry,
+void CDriver::InterfacePreprocessing(CConfig **config, CSolver***** solver, CGeometry**** geometry,
                                       unsigned short** interface_types, CInterface ***interface,
                                       vector<vector<unique_ptr<CInterpolator> > >& interpolation) {
 
@@ -2565,7 +2565,7 @@ void CDriver::Interface_Preprocessing(CConfig **config, CSolver***** solver, CGe
 
 }
 
-void CDriver::StaticMesh_Preprocessing(const CConfig *config, CGeometry** geometry){
+void CDriver::StaticMeshPreprocessing(const CConfig *config, CGeometry** geometry){
 
   unsigned short iMGlevel, iMGfine;
   unsigned short Kind_Grid_Movement;
@@ -2655,7 +2655,7 @@ void CDriver::StaticMesh_Preprocessing(const CConfig *config, CGeometry** geomet
 
 }
 
-void CDriver::Output_Preprocessing(CConfig **config, CConfig *driver_config, COutput **&output, COutput *&driver_output){
+void CDriver::OutputPreprocessing(CConfig **config, CConfig *driver_config, COutput **&output, COutput *&driver_output){
 
   /*--- Definition of the output class (one for each zone). The output class
    manages the writing of all restart, volume solution, surface solution,
@@ -2694,7 +2694,7 @@ void CDriver::Output_Preprocessing(CConfig **config, CConfig *driver_config, COu
 }
 
 
-void CDriver::Turbomachinery_Preprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver,
+void CDriver::TurbomachineryPreprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver,
                                            CInterface*** interface){
 
   unsigned short donorZone,targetZone, nMarkerInt, iMarkerInt;
@@ -2826,7 +2826,7 @@ void CDriver::Turbomachinery_Preprocessing(CConfig** config, CGeometry**** geome
 
 CDriver::~CDriver(void) {}
 
-void CDriver::Print_DirectResidual(RECORDING kind_recording) {
+void CDriver::PrintDirectResidual(RECORDING kind_recording) {
 
   if (!(rank == MASTER_NODE && kind_recording == RECORDING::SOLUTION_VARIABLES)) return;
 
@@ -3075,7 +3075,7 @@ void CFluidDriver::Run() {
     for (iZone = 0; iZone < nZone; iZone++)
       for (jZone = 0; jZone < nZone; jZone++)
         if(jZone != iZone && interface_container[iZone][jZone] != nullptr)
-          Transfer_Data(iZone, jZone);
+          TransferData(iZone, jZone);
 
     /*--- For each zone runs one single iteration ---*/
 
@@ -3098,7 +3098,7 @@ void CFluidDriver::Run() {
 
 }
 
-void CFluidDriver::Transfer_Data(unsigned short donorZone, unsigned short targetZone) {
+void CFluidDriver::TransferData(unsigned short donorZone, unsigned short targetZone) {
 
   auto BroadcastData = [&](unsigned int solIdx) {
     interface_container[donorZone][targetZone]->BroadcastData(*interpolator_container[donorZone][targetZone].get(),
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index 408321ef4d9..309e75adaa8 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -64,7 +64,7 @@ CDriverBase::CDriverBase(char* confFile, unsigned short val_nZone, SU2_Comm MPIC
 
 CDriverBase::~CDriverBase(void) {}
 
-void CDriverBase::SetContainers_Null() {
+void CDriverBase::SetContainersNull() {
   /*--- Create pointers to all the classes that may be used by drivers. In general, the pointers are instantiated
    * down a hierarchy over all zones, multi-grid levels, equation sets, and equation terms as described in the comments
    * below. ---*/
diff --git a/SU2_CFD/src/drivers/CMultizoneDriver.cpp b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
index 99c64c233f5..1c5c313db19 100644
--- a/SU2_CFD/src/drivers/CMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
@@ -183,8 +183,8 @@ void CMultizoneDriver::StartSolver() {
     /*--- Run a block iteration of the multizone problem. ---*/
 
     switch (driver_config->GetKind_MZSolver()){
-      case ENUM_MULTIZONE::MZ_BLOCK_GAUSS_SEIDEL: Run_GaussSeidel(); break;  // Block Gauss-Seidel iteration
-      case ENUM_MULTIZONE::MZ_BLOCK_JACOBI: Run_Jacobi(); break;             // Block-Jacobi iteration
+      case ENUM_MULTIZONE::MZ_BLOCK_GAUSS_SEIDEL: RunGaussSeidel(); break;  // Block Gauss-Seidel iteration
+      case ENUM_MULTIZONE::MZ_BLOCK_JACOBI: RunJacobi(); break;             // Block-Jacobi iteration
     }
 
     /*--- Update the solution for dual time stepping strategy ---*/
@@ -273,7 +273,7 @@ void CMultizoneDriver::Preprocess(unsigned long TimeIter) {
 
 }
 
-void CMultizoneDriver::Run_GaussSeidel() {
+void CMultizoneDriver::RunGaussSeidel() {
 
   unsigned short UpdateMesh;
   bool DeformMesh = false;
@@ -300,7 +300,7 @@ void CMultizoneDriver::Run_GaussSeidel() {
       for (auto jZone = 0u; jZone < nZone; jZone++){
         /*--- The target zone is iZone ---*/
         if (jZone != iZone){
-          DeformMesh = Transfer_Data(jZone, iZone);
+          DeformMesh = TransferData(jZone, iZone);
           if (DeformMesh) UpdateMesh+=1;
         }
       }
@@ -323,7 +323,7 @@ void CMultizoneDriver::Run_GaussSeidel() {
 
 }
 
-void CMultizoneDriver::Run_Jacobi() {
+void CMultizoneDriver::RunJacobi() {
 
   unsigned short UpdateMesh;
   bool DeformMesh = false;
@@ -349,7 +349,7 @@ void CMultizoneDriver::Run_Jacobi() {
       for (auto jZone = 0u; jZone < nZone; jZone++){
         /*--- The target zone is iZone ---*/
         if (jZone != iZone && interface_container[iZone][jZone] != nullptr){
-          DeformMesh = Transfer_Data(jZone, iZone);
+          DeformMesh = TransferData(jZone, iZone);
           if (DeformMesh) UpdateMesh+=1;
         }
       }
@@ -434,7 +434,7 @@ void CMultizoneDriver::Update() {
     for (auto jZone = 0u; jZone < nZone; jZone++){
       /*--- The target zone is iZone ---*/
       if (jZone != iZone){
-        UpdateMesh += Transfer_Data(jZone, iZone);
+        UpdateMesh += TransferData(jZone, iZone);
       }
     }
     /*--- If a mesh update is required due to the transfer of data ---*/
@@ -532,7 +532,7 @@ void CMultizoneDriver::DynamicMeshUpdate(unsigned short val_iZone, unsigned long
   }
 }
 
-bool CMultizoneDriver::Transfer_Data(unsigned short donorZone, unsigned short targetZone) {
+bool CMultizoneDriver::TransferData(unsigned short donorZone, unsigned short targetZone) {
 
   bool UpdateMesh = false;
 
diff --git a/SU2_CFD/src/drivers/CSinglezoneDriver.cpp b/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
index fe4bd854e1a..50a16ad2a0b 100644
--- a/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
@@ -114,7 +114,7 @@ void CSinglezoneDriver::Preprocess(unsigned long TimeIter) {
 
   /*--- Set runtime option ---*/
 
-  Runtime_Options();
+  RuntimeOptions();
 
   /*--- Set the current time iteration in the config ---*/
 
@@ -308,7 +308,7 @@ bool CSinglezoneDriver::Monitor(unsigned long TimeIter){
   return StopCalc;
 }
 
-void CSinglezoneDriver::Runtime_Options(){
+void CSinglezoneDriver::RuntimeOptions(){
 
   ifstream runtime_configfile;
 
diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index 2585121a29e..d9ee52bc66e 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -62,7 +62,7 @@ void CDriver::PythonInterfacePreprocessing(CConfig** config, CGeometry**** geome
 /* Functions related to the global performance indices (Lift, Drag, etc.)  */
 /////////////////////////////////////////////////////////////////////////////
 
-passivedouble CDriver::Get_Drag() const {
+passivedouble CDriver::GetDrag() const {
   unsigned short val_iZone = ZONE_0;
   unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
   su2double CDrag, factor, val_Drag;
@@ -76,7 +76,7 @@ passivedouble CDriver::Get_Drag() const {
   return SU2_TYPE::GetValue(val_Drag);
 }
 
-passivedouble CDriver::Get_Lift() const {
+passivedouble CDriver::GetLift() const {
   unsigned short val_iZone = ZONE_0;
   unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
   su2double CLift, factor, val_Lift;
@@ -90,7 +90,7 @@ passivedouble CDriver::Get_Lift() const {
   return SU2_TYPE::GetValue(val_Lift);
 }
 
-passivedouble CDriver::Get_Mx() const {
+passivedouble CDriver::GetMx() const {
   unsigned short val_iZone = ZONE_0;
   unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
   su2double CMx, RefLengthCoeff, factor, val_Mx;
@@ -106,7 +106,7 @@ passivedouble CDriver::Get_Mx() const {
   return SU2_TYPE::GetValue(val_Mx);
 }
 
-passivedouble CDriver::Get_My() const {
+passivedouble CDriver::GetMy() const {
   unsigned short val_iZone = ZONE_0;
   unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
   su2double CMy, RefLengthCoeff, factor, val_My;
@@ -122,7 +122,7 @@ passivedouble CDriver::Get_My() const {
   return SU2_TYPE::GetValue(val_My);
 }
 
-passivedouble CDriver::Get_Mz() const {
+passivedouble CDriver::GetMz() const {
   unsigned short val_iZone = ZONE_0;
   unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
   su2double CMz, RefLengthCoeff, factor, val_Mz;
@@ -138,7 +138,7 @@ passivedouble CDriver::Get_Mz() const {
   return SU2_TYPE::GetValue(val_Mz);
 }
 
-passivedouble CDriver::Get_DragCoeff() const {
+passivedouble CDriver::GetDragCoeff() const {
   unsigned short val_iZone = ZONE_0;
   unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
   su2double CDrag;
@@ -148,7 +148,7 @@ passivedouble CDriver::Get_DragCoeff() const {
   return SU2_TYPE::GetValue(CDrag);
 }
 
-passivedouble CDriver::Get_LiftCoeff() const {
+passivedouble CDriver::GetLiftCoeff() const {
   unsigned short val_iZone = ZONE_0;
   unsigned short FinestMesh = config_container[val_iZone]->GetFinestMesh();
   su2double CLift;
@@ -176,7 +176,7 @@ string CDriver::GetSurfaceFileName() const { return config_container[ZONE_0]->Ge
 /* Functions related to the management of markers                             */
 ////////////////////////////////////////////////////////////////////////////////
 
-void CDriver::SetHeatSource_Position(passivedouble alpha, passivedouble pos_x, passivedouble pos_y,
+void CDriver::SetHeatSourcePosition(passivedouble alpha, passivedouble pos_x, passivedouble pos_y,
                                      passivedouble pos_z) {
   CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][RAD_SOL];
 
@@ -186,7 +186,7 @@ void CDriver::SetHeatSource_Position(passivedouble alpha, passivedouble pos_x, p
   solver->SetVolumetricHeatSource(geometry_container[ZONE_0][INST_0][MESH_0], config_container[ZONE_0]);
 }
 
-void CDriver::SetInlet_Angle(unsigned short iMarker, passivedouble alpha) {
+void CDriver::SetInletAngle(unsigned short iMarker, passivedouble alpha) {
   su2double alpha_rad = alpha * PI_NUMBER / 180.0;
 
   unsigned long iVertex;
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 6aa13a0d6c3..b5f1af5f3cc 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -86,7 +86,7 @@ void CDeformationDriver::Input_Preprocessing() {
 
   /*--- Initialize containers. --- */
 
-  SetContainers_Null();
+  SetContainersNull();
 
   /*--- Loop over all zones to initialize the various classes. In most
    cases, nZone is equal to one. This represents the solution of a partial
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index 775515de672..9c15b8f913d 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -94,7 +94,7 @@ void CDiscAdjDeformationDriver::Input_Preprocessing() {
 
   /*--- Initialize containers. --- */
 
-  SetContainers_Null();
+  SetContainersNull();
 
   /*--- Loop over all zones to initialize the various classes. In most
    * cases, nZone is equal to one. This represents the solution of a partial

From bc0bcea36179f7331c5120209a356e957794162e Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 26 Mar 2023 09:44:31 +0100
Subject: [PATCH 314/656] deprecate cusp and make it an error to use
 MUSCL_FLOW=YES with centered schemes

---
 Common/include/option_structure.hpp           |   2 -
 Common/src/CConfig.cpp                        |  17 +-
 QuickStart/inv_NACA0012.cfg                   |  12 +-
 .../include/numerics/flow/convection/cusp.hpp |  69 -------
 SU2_CFD/src/drivers/CDriver.cpp               |  14 --
 SU2_CFD/src/numerics/flow/convection/cusp.cpp | 187 ------------------
 .../aeroelastic/aeroelastic_NACA64A010.cfg    |   4 +-
 .../cont_adj_euler/naca0012/inv_NACA0012.cfg  |   5 +-
 .../naca0012/inv_NACA0012_FD.cfg              |   5 +-
 .../naca0012/inv_NACA0012_discadj.cfg         |   3 -
 .../cont_adj_euler/oneram6/inv_ONERAM6.cfg    |   2 -
 .../cont_adj_rans/naca0012/turb_nasa.cfg      |   3 -
 .../naca0012/turb_nasa_binary.cfg             |   3 -
 .../cont_adj_rans/oneram6/turb_ONERAM6.cfg    |   3 -
 .../control_surface/inv_ONERAM6_moving.cfg    |   3 -
 .../control_surface/inv_ONERAM6_setting.cfg   |   3 -
 .../coupled_cht/comp_2d/flow_cylinder.cfg     |   2 -
 .../deformation/naca0012/def_NACA0012.cfg     |   4 +-
 .../naca0012/surface_file_NACA0012.cfg        |   2 -
 .../naca0012/incomp_NACA0012_disc.cfg         |   2 -
 TestCases/euler/CRM/inv_CRM_JST.cfg           |   2 -
 TestCases/euler/biparabolic/BIPARABOLIC.cfg   |   4 +-
 TestCases/euler/channel/inv_channel.cfg       |   4 +-
 TestCases/euler/channel/inv_channel_RK.cfg    |   2 -
 TestCases/euler/naca0012/inv_NACA0012.cfg     |   4 +-
 TestCases/euler/oneram6/inv_ONERAM6.cfg       |   2 -
 TestCases/fixed_cl/naca0012/inv_NACA0012.cfg  |   4 +-
 .../naca0012/inv_NACA0012_ContAdj.cfg         |   6 +-
 TestCases/gust/inv_gust_NACA0012.cfg          |   4 +-
 TestCases/harmonic_balance/HB.cfg             |   6 +-
 .../pitching_NACA64A010.cfg                   |   4 +-
 .../pitching_oneram6/pitching_ONERAM6.cfg     |   4 +-
 .../steady_inverse_design/inv_NACA0012.cfg    |   4 +-
 .../pitching_naca64a010/turb_NACA64A010.cfg   |   4 +-
 .../pitching_oneram6/turb_ONERAM6.cfg         |   2 -
 .../steady_oneram6/turb_ONERAM6.cfg           |   2 -
 TestCases/polar/naca0012/inv_NACA0012.cfg     |   2 -
 .../turb_NACA0012_sst_multigrid_restart.cfg   |   2 -
 TestCases/rans/rae2822/turb_SA_RAE2822.cfg    |   2 -
 TestCases/rans/rae2822/turb_SST_RAE2822.cfg   |   2 -
 .../rans/rae2822/turb_SST_SUST_RAE2822.cfg    |   2 -
 TestCases/rans/s809/trans_s809.cfg            |   2 -
 .../caradonna_tung/rot_caradonna_tung.cfg     |   2 -
 TestCases/rotating/naca0012/rot_NACA0012.cfg  |   2 -
 .../sliding_interface/bars_SST_2D/bars.cfg    |   2 -
 .../pitching_NACA64A010.cfg                   |   2 -
 .../turb_NACA64A010.cfg                       |   4 +-
 config_template.cfg                           |  14 +-
 48 files changed, 39 insertions(+), 402 deletions(-)
 delete mode 100644 SU2_CFD/include/numerics/flow/convection/cusp.hpp
 delete mode 100644 SU2_CFD/src/numerics/flow/convection/cusp.cpp

diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index ef433e22a83..4c934f0612b 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -820,7 +820,6 @@ enum class UPWIND {
   MSW,                    /*!< \brief Modified Steger-Warming method. */
   TURKEL,                 /*!< \brief Roe-Turkel's upwind numerical method. */
   SLAU,                   /*!< \brief Simple Low-Dissipation AUSM numerical method. */
-  CUSP,                   /*!< \brief Convective upwind and split pressure numerical method. */
   CONVECTIVE_TEMPLATE,    /*!< \brief Template for new numerical method . */
   L2ROE,                  /*!< \brief L2ROE numerical method . */
   LMROE,                  /*!< \brief Rieper's Low Mach ROE numerical method . */
@@ -844,7 +843,6 @@ static const MapType<std::string, UPWIND> Upwind_Map = {
   MakePair("HLLC", UPWIND::HLLC)
   MakePair("SW", UPWIND::SW)
   MakePair("MSW", UPWIND::MSW)
-  MakePair("CUSP", UPWIND::CUSP)
   MakePair("SCALAR_UPWIND", UPWIND::SCALAR_UPWIND)
   MakePair("BOUNDED_SCALAR", UPWIND::BOUNDED_SCALAR)
   MakePair("CONVECTIVE_TEMPLATE", UPWIND::CONVECTIVE_TEMPLATE)
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 0821cd6075a..66ce4bdbd5c 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -1909,7 +1909,7 @@ void CConfig::SetConfig_Options() {
    *  \n DESCRIPTION: Convective numerical method for the adjoint solver.
    *  \n OPTIONS:  See \link Upwind_Map \endlink , \link Centered_Map \endlink. Note: not all methods are guaranteed to be implemented for the adjoint solver. \ingroup Config */
   addConvectOption("CONV_NUM_METHOD_ADJFLOW", Kind_ConvNumScheme_AdjFlow, Kind_Centered_AdjFlow, Kind_Upwind_AdjFlow);
-  /*!\brief MUSCL_FLOW \n DESCRIPTION: Check if the MUSCL scheme should be used \ingroup Config*/
+  /*!\brief MUSCL_ADJFLOW \n DESCRIPTION: Check if the MUSCL scheme should be used \ingroup Config*/
   addBoolOption("MUSCL_ADJFLOW", MUSCL_AdjFlow, true);
   /*!\brief SLOPE_LIMITER_ADJFLOW
      * DESCRIPTION: Slope limiter for the adjoint solution. \n OPTIONS: See \link Limiter_Map \endlink \n DEFAULT VENKATAKRISHNAN \ingroup Config*/
@@ -1920,7 +1920,7 @@ void CConfig::SetConfig_Options() {
   /*!\brief LAX_SENSOR_COEFF \n DESCRIPTION: 1st order artificial dissipation coefficients for the adjoint Lax-Friedrichs method. \ingroup Config*/
   addDoubleOption("ADJ_LAX_SENSOR_COEFF", Kappa_1st_AdjFlow, 0.15);
 
-  /*!\brief MUSCL_FLOW \n DESCRIPTION: Check if the MUSCL scheme should be used \ingroup Config*/
+  /*!\brief MUSCL_TURB \n DESCRIPTION: Check if the MUSCL scheme should be used \ingroup Config*/
   addBoolOption("MUSCL_TURB", MUSCL_Turb, false);
   /*!\brief SLOPE_LIMITER_TURB
    *  \n DESCRIPTION: Slope limiter  \n OPTIONS: See \link Limiter_Map \endlink \n DEFAULT VENKATAKRISHNAN \ingroup Config*/
@@ -1929,7 +1929,7 @@ void CConfig::SetConfig_Options() {
    *  \n DESCRIPTION: Convective numerical method \ingroup Config*/
   addConvectOption("CONV_NUM_METHOD_TURB", Kind_ConvNumScheme_Turb, Kind_Centered_Turb, Kind_Upwind_Turb);
 
-  /*!\brief MUSCL_FLOW \n DESCRIPTION: Check if the MUSCL scheme should be used \ingroup Config*/
+  /*!\brief MUSCL_ADJTURB \n DESCRIPTION: Check if the MUSCL scheme should be used \ingroup Config*/
   addBoolOption("MUSCL_ADJTURB", MUSCL_AdjTurb, false);
   /*!\brief SLOPE_LIMITER_ADJTURB
    *  \n DESCRIPTION: Slope limiter \n OPTIONS: See \link Limiter_Map \endlink \n DEFAULT VENKATAKRISHNAN \ingroup Config */
@@ -1944,7 +1944,7 @@ void CConfig::SetConfig_Options() {
   /*!\brief CONV_NUM_METHOD_SPECIES \n DESCRIPTION: Convective numerical method for species transport \ingroup Config*/
   addConvectOption("CONV_NUM_METHOD_SPECIES", Kind_ConvNumScheme_Species, Kind_Centered_Species, Kind_Upwind_Species);
 
-  /*!\brief MUSCL_FLOW \n DESCRIPTION: Check if the MUSCL scheme should be used \ingroup Config*/
+  /*!\brief MUSCL_HEAT \n DESCRIPTION: Check if the MUSCL scheme should be used \ingroup Config*/
   addBoolOption("MUSCL_HEAT", MUSCL_Heat, false);
   /*!\brief SLOPE_LIMITER_HEAT \n DESCRIPTION: Slope limiter \n OPTIONS: See \link Limiter_Map \endlink \n DEFAULT NONE \ingroup Config*/
   addEnumOption("SLOPE_LIMITER_HEAT", Kind_SlopeLimit_Heat, Limiter_Map, LIMITER::NONE);
@@ -3560,6 +3560,14 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
   SetScalarDefaults(MUSCL_Heat, Kind_ConvNumScheme_Heat, Kind_Upwind_Heat, Kind_SlopeLimit_Heat);
   SetScalarDefaults(MUSCL_Species, Kind_ConvNumScheme_Species, Kind_Upwind_Species, Kind_SlopeLimit_Species);
 
+  if (MUSCL_Flow && (Kind_ConvNumScheme_Flow == SPACE_CENTERED)) {
+    if (OptionIsSet("MUSCL_FLOW")) {
+      SU2_MPI::Error("Centered schemes do not use MUSCL reconstruction (use MUSCL_FLOW= NO).", CURRENT_FUNCTION);
+    } else {
+      MUSCL_Flow = false;
+    }
+  }
+
   if (!MUSCL_Flow || (Kind_ConvNumScheme_Flow == SPACE_CENTERED)) Kind_SlopeLimit_Flow = LIMITER::NONE;
   if (!MUSCL_AdjFlow || (Kind_ConvNumScheme_AdjFlow == SPACE_CENTERED)) Kind_SlopeLimit_AdjFlow = LIMITER::NONE;
   if (!MUSCL_AdjTurb || (Kind_ConvNumScheme_AdjTurb == SPACE_CENTERED)) Kind_SlopeLimit_AdjTurb = LIMITER::NONE;
@@ -6642,7 +6650,6 @@ void CConfig::SetOutput(SU2_COMPONENT val_software, unsigned short val_izone) {
         if (Kind_Upwind_Flow == UPWIND::HLLC)   cout << "HLLC solver for the flow inviscid terms."<< endl;
         if (Kind_Upwind_Flow == UPWIND::SW)     cout << "Steger-Warming solver for the flow inviscid terms."<< endl;
         if (Kind_Upwind_Flow == UPWIND::MSW)    cout << "Modified Steger-Warming solver for the flow inviscid terms."<< endl;
-        if (Kind_Upwind_Flow == UPWIND::CUSP)   cout << "CUSP solver for the flow inviscid terms."<< endl;
         if (Kind_Upwind_Flow == UPWIND::L2ROE)  cout << "L2ROE Low Mach ROE solver for the flow inviscid terms."<< endl;
         if (Kind_Upwind_Flow == UPWIND::LMROE)  cout << "Rieper Low Mach ROE solver for the flow inviscid terms."<< endl;
         if (Kind_Upwind_Flow == UPWIND::SLAU)   cout << "Simple Low-Dissipation AUSM solver for the flow inviscid terms."<< endl;
diff --git a/QuickStart/inv_NACA0012.cfg b/QuickStart/inv_NACA0012.cfg
index a4668268b9c..8876c69dd7c 100644
--- a/QuickStart/inv_NACA0012.cfg
+++ b/QuickStart/inv_NACA0012.cfg
@@ -146,17 +146,9 @@ MG_DAMP_PROLONGATION= 1.0
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
-CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
-MUSCL_FLOW= YES
+% Convective numerical method
 %
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN_WANG
+CONV_NUM_METHOD_FLOW= JST
 %
 % 2nd and 4th order artificial dissipation coefficients
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
diff --git a/SU2_CFD/include/numerics/flow/convection/cusp.hpp b/SU2_CFD/include/numerics/flow/convection/cusp.hpp
deleted file mode 100644
index 526e0d412f2..00000000000
--- a/SU2_CFD/include/numerics/flow/convection/cusp.hpp
+++ /dev/null
@@ -1,69 +0,0 @@
-/*!
- * \file cusp.hpp
- * \brief Declaration of the CUSP numerics class.
- * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-
-#pragma once
-
-#include "../../CNumerics.hpp"
-
-/*!
- * \class CUpwCUSP_Flow
- * \brief Class for centered scheme - CUSP.
- * \ingroup ConvDiscr
- * \author F. Palacios
- */
-class CUpwCUSP_Flow final : public CNumerics {
-
-private:
-  su2double Velocity_i[MAXNDIM], Velocity_j[MAXNDIM], *ProjFlux_i, *ProjFlux_j;
-  bool implicit;
-
-  su2double* Flux;        /*!< \brief The flux accross the face. */
-  su2double** Jacobian_i; /*!< \brief The Jacobian w.r.t. point i after computation. */
-  su2double** Jacobian_j; /*!< \brief The Jacobian w.r.t. point j after computation. */
-public:
-
-  /*!
-   * \brief Constructor of the class.
-   * \param[in] val_nDim - Number of dimension of the problem.
-   * \param[in] val_nVar - Number of variables of the problem.
-   * \param[in] config - Definition of the particular problem.
-   */
-  CUpwCUSP_Flow(unsigned short val_nDim, unsigned short val_nVar, const CConfig* config);
-
-  /*!
-   * \brief Destructor of the class.
-   */
-  ~CUpwCUSP_Flow(void) override;
-
-  /*!
-   * \brief Compute the flow residual using a JST method.
-   * \param[in] config - Definition of the particular problem.
-   * \return A lightweight const-view (read-only) of the residual/flux and Jacobians.
-   */
-  ResidualType<> ComputeResidual(const CConfig* config) override;
-
-};
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index a5881a197de..e754a7f2598 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -1783,13 +1783,6 @@ void CDriver::Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSol
               }
               break;
 
-            case UPWIND::CUSP:
-              for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-                numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwCUSP_Flow(nDim, nVar_Flow, config);
-                numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwCUSP_Flow(nDim, nVar_Flow, config);
-              }
-              break;
-
             default:
               SU2_MPI::Error("Invalid upwind scheme or not implemented.", CURRENT_FUNCTION);
               break;
@@ -2048,13 +2041,6 @@ void CDriver::Numerics_Preprocessing(CConfig *config, CGeometry **geometry, CSol
         }
         break;
 
-      case UPWIND::CUSP:
-        for (iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
-          numerics[iMGlevel][FLOW_SOL][conv_term] = new CUpwCUSP_Flow(nDim, nVar_Flow, config);
-          numerics[iMGlevel][FLOW_SOL][conv_bound_term] = new CUpwCUSP_Flow(nDim, nVar_Flow, config);
-        }
-        break;
-
       default:
         SU2_MPI::Error("Riemann solver not implemented.", CURRENT_FUNCTION);
         break;
diff --git a/SU2_CFD/src/numerics/flow/convection/cusp.cpp b/SU2_CFD/src/numerics/flow/convection/cusp.cpp
deleted file mode 100644
index 030844cb352..00000000000
--- a/SU2_CFD/src/numerics/flow/convection/cusp.cpp
+++ /dev/null
@@ -1,187 +0,0 @@
-/*!
- * \file cusp.cpp
- * \brief Implementation of the CUSP scheme.
- * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-
-#include "../../../../include/numerics/flow/convection/cusp.hpp"
-#include "../../../../../Common/include/toolboxes/geometry_toolbox.hpp"
-
-CUpwCUSP_Flow::CUpwCUSP_Flow(unsigned short val_nDim, unsigned short val_nVar, const CConfig* config) : CNumerics(val_nDim, val_nVar, config) {
-
-  implicit = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
-
-  Gamma = config->GetGamma();
-  Gamma_Minus_One = Gamma - 1.0;
-
-  if (config->GetDynamic_Grid() && (SU2_MPI::GetRank() == MASTER_NODE))
-    cout << "WARNING: Grid velocities are NOT yet considered by the CUSP scheme." << endl;
-
-  /*--- Allocate some structures ---*/
-  Flux = new su2double [nVar];
-  ProjFlux_i = new su2double [nVar];
-  ProjFlux_j = new su2double [nVar];
-  Jacobian_i = new su2double* [nVar];
-  Jacobian_j = new su2double* [nVar];
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
-    Jacobian_i[iVar] = new su2double [nVar];
-    Jacobian_j[iVar] = new su2double [nVar];
-  }
-}
-
-CUpwCUSP_Flow::~CUpwCUSP_Flow(void) {
-  delete [] Flux;
-  delete [] ProjFlux_i;
-  delete [] ProjFlux_j;
-  for (unsigned short iVar = 0; iVar < nVar; iVar++) {
-    delete [] Jacobian_i[iVar];
-    delete [] Jacobian_j[iVar];
-  }
-  delete [] Jacobian_i;
-  delete [] Jacobian_j;
-}
-
-CNumerics::ResidualType<> CUpwCUSP_Flow::ComputeResidual(const CConfig* config) {
-
-  implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
-
-  unsigned short iDim, iVar;
-  su2double Diff_U[5] = {0.0};
-
-  AD::SetPreaccIn(Normal, nDim);
-  AD::SetPreaccIn(V_i, nDim+4);
-  AD::SetPreaccIn(V_j, nDim+4);
-
-  /*--- Pressure, density, enthalpy, energy, and velocity at points i and j ---*/
-
-  Pressure_i = V_i[nDim+1];     Pressure_j = V_j[nDim+1];
-  Density_i  = V_i[nDim+2];     Density_j  = V_j[nDim+2];
-  Enthalpy_i = V_i[nDim+3];     Enthalpy_j = V_j[nDim+3];
-  su2double Energy_i = Enthalpy_i - Pressure_i/Density_i;
-  su2double Energy_j = Enthalpy_j - Pressure_j/Density_j;
-
-  su2double sq_vel_i = 0.0, sq_vel_j = 0.0;
-  for (iDim = 0; iDim < nDim; iDim++) {
-    Velocity_i[iDim] = V_i[iDim+1];
-    Velocity_j[iDim] = V_j[iDim+1];
-    sq_vel_i += Velocity_i[iDim]*Velocity_i[iDim];
-    sq_vel_j += Velocity_j[iDim]*Velocity_j[iDim];
-  }
-
-  /*-- Face area and unit normal ---*/
-
-  Area = GeometryToolbox::Norm(nDim, Normal);
-
-  for (iDim = 0; iDim < nDim; iDim++)
-    UnitNormal[iDim] = Normal[iDim]/Area;
-
-  /*--- Computes differences of conservative variables, with a correction for the enthalpy ---*/
-
-  Diff_U[0] = Density_i - Density_j;
-  for (iDim = 0; iDim < nDim; iDim++)
-    Diff_U[iDim+1] = Density_i*Velocity_i[iDim] - Density_j*Velocity_j[iDim];
-  Diff_U[nVar-1] = Density_i*Enthalpy_i - Density_j*Enthalpy_j;
-
-  /*--- Get left and right fluxes ---*/
-
-  GetInviscidProjFlux(&Density_i, Velocity_i, &Pressure_i, &Enthalpy_i, UnitNormal, ProjFlux_i);
-  GetInviscidProjFlux(&Density_j, Velocity_j, &Pressure_j, &Enthalpy_j, UnitNormal, ProjFlux_j);
-
-  /*--- Compute dissipation parameters based on Roe-averaged values ---*/
-
-  su2double Beta, Nu_c;
-
-  su2double R = sqrt(Density_j/Density_i), ProjVelocity = 0.0, sq_vel = 0.0;
-
-  for (iDim = 0; iDim < nDim; iDim++) {
-    su2double MeanVel = (R*Velocity_j[iDim]+Velocity_i[iDim])/(R+1.0);
-    ProjVelocity += MeanVel*UnitNormal[iDim];
-    sq_vel += MeanVel*MeanVel;
-  }
-  su2double MeanEnthalpy = (R*Enthalpy_j+Enthalpy_i)/(R+1.0);
-  su2double MeanSoundSpeed = sqrt(Gamma_Minus_One*fabs(MeanEnthalpy-0.5*sq_vel));
-
-  su2double Mach = ProjVelocity / MeanSoundSpeed;
-
-  su2double tmp1 = 0.5*(Gamma+1.0)/Gamma*ProjVelocity;
-  su2double tmp2 = sqrt(pow(tmp1-ProjVelocity/Gamma, 2.0) + pow(MeanSoundSpeed,2.0)/Gamma);
-  su2double LamdaNeg = tmp1 - tmp2, LamdaPos = tmp1 + tmp2;
-
-  if (fabs(Mach) >= 1.0) Beta = Mach/fabs(Mach);
-  else if (Mach  >= 0.0) Beta = max(0.0, (ProjVelocity + LamdaNeg)/(ProjVelocity - LamdaNeg));
-  else                   Beta =-max(0.0, (ProjVelocity + LamdaPos)/(ProjVelocity - LamdaPos));
-
-  if (fabs(Mach) >= 1.0) Nu_c = 0.0;
-  else {
-    if      (Beta > 0.0) Nu_c =-(1.0+Beta)*LamdaNeg;
-    else if (Beta < 0.0) Nu_c = (1.0-Beta)*LamdaPos;
-    /*--- Limit the minimum scalar dissipation ---*/
-    else Nu_c = max(fabs(ProjVelocity), config->GetEntropyFix_Coeff()*MeanSoundSpeed);
-  }
-
-  /*--- Compute the residual ---*/
-
-  for (iVar = 0; iVar < nVar; iVar++)
-    Flux[iVar] = 0.5*((1.0+Beta)*ProjFlux_i[iVar] + (1.0-Beta)*ProjFlux_j[iVar] + Nu_c*Diff_U[iVar])*Area;
-
-  /*--- Jacobian computation ---*/
-
-  if (implicit) {
-
-    /*--- Flux average and difference contributions ---*/
-
-    GetInviscidProjJac(Velocity_i, &Energy_i, Normal, 0.5*(1.0+Beta), Jacobian_i);
-    GetInviscidProjJac(Velocity_j, &Energy_j, Normal, 0.5*(1.0-Beta), Jacobian_j);
-
-    /*--- Solution difference (scalar dissipation) contribution ---*/
-
-    su2double cte_0 = 0.5*Nu_c*Area*config->GetCent_Jac_Fix_Factor();
-
-    /*--- n-1 diagonal entries ---*/
-
-    for (iVar = 0; iVar < (nVar-1); iVar++) {
-      Jacobian_i[iVar][iVar] += cte_0;
-      Jacobian_j[iVar][iVar] -= cte_0;
-    }
-
-    /*--- Last rows ---*/
-
-    Jacobian_i[nVar-1][0] += cte_0*Gamma_Minus_One*0.5*sq_vel_i;
-    for (iDim = 0; iDim < nDim; iDim++)
-      Jacobian_i[nVar-1][iDim+1] -= cte_0*Gamma_Minus_One*Velocity_i[iDim];
-    Jacobian_i[nVar-1][nVar-1] += cte_0*Gamma;
-
-    Jacobian_j[nVar-1][0] -= cte_0*Gamma_Minus_One*0.5*sq_vel_j;
-    for (iDim = 0; iDim < nDim; iDim++)
-      Jacobian_j[nVar-1][iDim+1] += cte_0*Gamma_Minus_One*Velocity_j[iDim];
-    Jacobian_j[nVar-1][nVar-1] -= cte_0*Gamma;
-
-  }
-
-  AD::SetPreaccOut(Flux, nVar);
-  AD::EndPreacc();
-
-  return ResidualType<>(Flux, Jacobian_i, Jacobian_j);
-
-}
diff --git a/TestCases/aeroelastic/aeroelastic_NACA64A010.cfg b/TestCases/aeroelastic/aeroelastic_NACA64A010.cfg
index 944406b2c93..8f7fdb4048d 100644
--- a/TestCases/aeroelastic/aeroelastic_NACA64A010.cfg
+++ b/TestCases/aeroelastic/aeroelastic_NACA64A010.cfg
@@ -122,8 +122,6 @@ MG_DAMP_PROLONGATION= 0.75
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 ENTROPY_FIX_COEFF= 0.001
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
@@ -157,5 +155,5 @@ RESTART_FILENAME= restart_flow.dat
 VOLUME_FILENAME= flow
 SURFACE_FILENAME= surface_flow
 OUTPUT_WRT_FREQ= 1000
-SCREEN_OUTPUT= (TIME_ITER, INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG_ON_SURFACE, PLUNGE, PITCH) 
+SCREEN_OUTPUT= (TIME_ITER, INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG_ON_SURFACE, PLUNGE, PITCH)
 OUTPUT_FILES= (RESTART_ASCII)
\ No newline at end of file
diff --git a/TestCases/cont_adj_euler/naca0012/inv_NACA0012.cfg b/TestCases/cont_adj_euler/naca0012/inv_NACA0012.cfg
index faac3cd114f..292545e17be 100644
--- a/TestCases/cont_adj_euler/naca0012/inv_NACA0012.cfg
+++ b/TestCases/cont_adj_euler/naca0012/inv_NACA0012.cfg
@@ -70,9 +70,6 @@ MG_DAMP_PROLONGATION= 1.0
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-VENKAT_LIMITER_COEFF= 0.03
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
@@ -128,7 +125,7 @@ GRAD_OBJFUNC_FILENAME= of_grad.dat
 SURFACE_FILENAME= surface_flow
 SURFACE_ADJ_FILENAME= surface_adjoint
 OUTPUT_WRT_FREQ= 250
-SCREEN_OUTPUT = (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_GEO, SENS_AOA, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG) 
+SCREEN_OUTPUT = (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_GEO, SENS_AOA, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
 HISTORY_OUTPUT= (ITER, RMS_RES, AERO_COEFF, SENSITIVITY)
 VOLUME_OUTPUT= (COORDINATES, SOLUTION, PRESSURE, TEMPERATURE, SENSITIVITY)
 OUTPUT_FILES=(RESTART_ASCII, PARAVIEW, SURFACE_CSV)
diff --git a/TestCases/cont_adj_euler/naca0012/inv_NACA0012_FD.cfg b/TestCases/cont_adj_euler/naca0012/inv_NACA0012_FD.cfg
index 7be820a3240..fca45524600 100644
--- a/TestCases/cont_adj_euler/naca0012/inv_NACA0012_FD.cfg
+++ b/TestCases/cont_adj_euler/naca0012/inv_NACA0012_FD.cfg
@@ -69,9 +69,6 @@ MG_DAMP_PROLONGATION= 1.0
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-VENKAT_LIMITER_COEFF= 0.03
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
@@ -135,4 +132,4 @@ OUTPUT_FILES=(RESTART_ASCII, PARAVIEW)
 %
 OPT_OBJECTIVE= DRAG * 0.001
 OPT_CONSTRAINT= ( LIFT > 0.327 ) * 0.001; ( MOMENT_Z > 0.0 ) * 0.001; ( AIRFOIL_THICKNESS > 0.12 ) * 0.001
-DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 ); 
+DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 );
diff --git a/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg b/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg
index 49bda853bcd..824e6c15caa 100644
--- a/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg
+++ b/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg
@@ -51,9 +51,6 @@ ITER= 150
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-VENKAT_LIMITER_COEFF= 0.03
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
diff --git a/TestCases/cont_adj_euler/oneram6/inv_ONERAM6.cfg b/TestCases/cont_adj_euler/oneram6/inv_ONERAM6.cfg
index d1d287831e9..c7b8b52b73e 100644
--- a/TestCases/cont_adj_euler/oneram6/inv_ONERAM6.cfg
+++ b/TestCases/cont_adj_euler/oneram6/inv_ONERAM6.cfg
@@ -79,8 +79,6 @@ MG_DAMP_PROLONGATION= 0.9
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= NONE
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
diff --git a/TestCases/cont_adj_rans/naca0012/turb_nasa.cfg b/TestCases/cont_adj_rans/naca0012/turb_nasa.cfg
index 7b30c1faadc..9d46631ea8f 100644
--- a/TestCases/cont_adj_rans/naca0012/turb_nasa.cfg
+++ b/TestCases/cont_adj_rans/naca0012/turb_nasa.cfg
@@ -58,9 +58,6 @@ LINEAR_SOLVER_ITER= 20
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-VENKAT_LIMITER_COEFF= 0.01
 JST_SENSOR_COEFF= ( 0.5, 0.005 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
diff --git a/TestCases/cont_adj_rans/naca0012/turb_nasa_binary.cfg b/TestCases/cont_adj_rans/naca0012/turb_nasa_binary.cfg
index f1eca8847fa..01749d1b3e3 100644
--- a/TestCases/cont_adj_rans/naca0012/turb_nasa_binary.cfg
+++ b/TestCases/cont_adj_rans/naca0012/turb_nasa_binary.cfg
@@ -59,9 +59,6 @@ LINEAR_SOLVER_ITER= 20
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-VENKAT_LIMITER_COEFF= 0.01
 JST_SENSOR_COEFF= ( 0.5, 0.005 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
diff --git a/TestCases/cont_adj_rans/oneram6/turb_ONERAM6.cfg b/TestCases/cont_adj_rans/oneram6/turb_ONERAM6.cfg
index 706099e9e7b..2e52829fc48 100644
--- a/TestCases/cont_adj_rans/oneram6/turb_ONERAM6.cfg
+++ b/TestCases/cont_adj_rans/oneram6/turb_ONERAM6.cfg
@@ -70,9 +70,6 @@ MG_DAMP_PROLONGATION= 0.7
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-VENKAT_LIMITER_COEFF= 0.03
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
diff --git a/TestCases/control_surface/inv_ONERAM6_moving.cfg b/TestCases/control_surface/inv_ONERAM6_moving.cfg
index bb09bb3f21b..ad7d458ca4c 100644
--- a/TestCases/control_surface/inv_ONERAM6_moving.cfg
+++ b/TestCases/control_surface/inv_ONERAM6_moving.cfg
@@ -70,9 +70,6 @@ MG_DAMP_PROLONGATION= 0.9
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-VENKAT_LIMITER_COEFF= 0.03
 JST_SENSOR_COEFF= ( 0.5, 0.04 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
diff --git a/TestCases/control_surface/inv_ONERAM6_setting.cfg b/TestCases/control_surface/inv_ONERAM6_setting.cfg
index 1cbf9a9bfbc..43bf414dec5 100644
--- a/TestCases/control_surface/inv_ONERAM6_setting.cfg
+++ b/TestCases/control_surface/inv_ONERAM6_setting.cfg
@@ -70,9 +70,6 @@ MG_DAMP_PROLONGATION= 0.9
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-VENKAT_LIMITER_COEFF= 0.03
 JST_SENSOR_COEFF= ( 0.5, 0.04 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
diff --git a/TestCases/coupled_cht/comp_2d/flow_cylinder.cfg b/TestCases/coupled_cht/comp_2d/flow_cylinder.cfg
index 3b7870d310b..218cc7fa470 100644
--- a/TestCases/coupled_cht/comp_2d/flow_cylinder.cfg
+++ b/TestCases/coupled_cht/comp_2d/flow_cylinder.cfg
@@ -49,8 +49,6 @@ LINEAR_SOLVER_ITER= 5
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= NONE
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
diff --git a/TestCases/deformation/naca0012/def_NACA0012.cfg b/TestCases/deformation/naca0012/def_NACA0012.cfg
index 73834aa2ee6..5135ac45b2f 100644
--- a/TestCases/deformation/naca0012/def_NACA0012.cfg
+++ b/TestCases/deformation/naca0012/def_NACA0012.cfg
@@ -74,8 +74,6 @@ MG_DAMP_PROLONGATION= 1.0
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
@@ -90,7 +88,7 @@ TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-DV_KIND= HICKS_HENNE 
+DV_KIND= HICKS_HENNE
 DV_MARKER= ( airfoil )
 DV_PARAM= ( 1, 0.5 )
 DV_VALUE= 0.1
diff --git a/TestCases/deformation/naca0012/surface_file_NACA0012.cfg b/TestCases/deformation/naca0012/surface_file_NACA0012.cfg
index 18a61153927..f39721c4322 100644
--- a/TestCases/deformation/naca0012/surface_file_NACA0012.cfg
+++ b/TestCases/deformation/naca0012/surface_file_NACA0012.cfg
@@ -74,8 +74,6 @@ MG_DAMP_PROLONGATION= 1.0
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
diff --git a/TestCases/disc_adj_incomp_euler/naca0012/incomp_NACA0012_disc.cfg b/TestCases/disc_adj_incomp_euler/naca0012/incomp_NACA0012_disc.cfg
index 879ca518d47..f6d4b5efa5f 100644
--- a/TestCases/disc_adj_incomp_euler/naca0012/incomp_NACA0012_disc.cfg
+++ b/TestCases/disc_adj_incomp_euler/naca0012/incomp_NACA0012_disc.cfg
@@ -60,8 +60,6 @@ MG_DAMP_PROLONGATION= 1.0
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= NONE
 VENKAT_LIMITER_COEFF= 0.001
 JST_SENSOR_COEFF= ( 0.0, 0.01 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
diff --git a/TestCases/euler/CRM/inv_CRM_JST.cfg b/TestCases/euler/CRM/inv_CRM_JST.cfg
index b7e48db4b5f..287c9bcefd7 100644
--- a/TestCases/euler/CRM/inv_CRM_JST.cfg
+++ b/TestCases/euler/CRM/inv_CRM_JST.cfg
@@ -65,8 +65,6 @@ MG_DAMP_PROLONGATION= 0.9
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 VENKAT_LIMITER_COEFF= 0.03
 JST_SENSOR_COEFF= ( 0.5, 0.04 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
diff --git a/TestCases/euler/biparabolic/BIPARABOLIC.cfg b/TestCases/euler/biparabolic/BIPARABOLIC.cfg
index 86368ceaa21..c3787da951d 100644
--- a/TestCases/euler/biparabolic/BIPARABOLIC.cfg
+++ b/TestCases/euler/biparabolic/BIPARABOLIC.cfg
@@ -54,7 +54,7 @@ EXT_ITER= 99999999
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-MGLEVEL= 3 
+MGLEVEL= 3
 MGCYCLE= V_CYCLE
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
@@ -65,8 +65,6 @@ MG_DAMP_PROLONGATION= 0.95
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 VENKAT_LIMITER_COEFF= 0.03
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
diff --git a/TestCases/euler/channel/inv_channel.cfg b/TestCases/euler/channel/inv_channel.cfg
index 279bbacdf65..9acd1819ac4 100644
--- a/TestCases/euler/channel/inv_channel.cfg
+++ b/TestCases/euler/channel/inv_channel.cfg
@@ -10,7 +10,7 @@
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
-%                               
+%
 SOLVER= EULER
 MATH_PROBLEM= DIRECT
 RESTART_SOL= NO
@@ -73,8 +73,6 @@ MG_DAMP_PROLONGATION= 0.9
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 VENKAT_LIMITER_COEFF= 0.03
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
diff --git a/TestCases/euler/channel/inv_channel_RK.cfg b/TestCases/euler/channel/inv_channel_RK.cfg
index 6a4b2731bdb..edcf30b313c 100644
--- a/TestCases/euler/channel/inv_channel_RK.cfg
+++ b/TestCases/euler/channel/inv_channel_RK.cfg
@@ -66,8 +66,6 @@ MG_DAMP_PROLONGATION= 0.9
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 VENKAT_LIMITER_COEFF= 0.03
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= RUNGE-KUTTA_EXPLICIT
diff --git a/TestCases/euler/naca0012/inv_NACA0012.cfg b/TestCases/euler/naca0012/inv_NACA0012.cfg
index 607879da57d..9f998d9e087 100644
--- a/TestCases/euler/naca0012/inv_NACA0012.cfg
+++ b/TestCases/euler/naca0012/inv_NACA0012.cfg
@@ -71,8 +71,6 @@ MG_DAMP_PROLONGATION= 1.0
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
@@ -87,7 +85,7 @@ TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-DV_KIND= HICKS_HENNE 
+DV_KIND= HICKS_HENNE
 DV_MARKER= ( airfoil )
 DV_PARAM= ( 1, 0.5 )
 DV_VALUE= 0.01
diff --git a/TestCases/euler/oneram6/inv_ONERAM6.cfg b/TestCases/euler/oneram6/inv_ONERAM6.cfg
index ec5e0f93aa0..c7f38f4d194 100644
--- a/TestCases/euler/oneram6/inv_ONERAM6.cfg
+++ b/TestCases/euler/oneram6/inv_ONERAM6.cfg
@@ -79,8 +79,6 @@ MG_DAMP_PROLONGATION= 0.9
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= NONE
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
diff --git a/TestCases/fixed_cl/naca0012/inv_NACA0012.cfg b/TestCases/fixed_cl/naca0012/inv_NACA0012.cfg
index 8d7b8c46ae7..1a762d295e7 100644
--- a/TestCases/fixed_cl/naca0012/inv_NACA0012.cfg
+++ b/TestCases/fixed_cl/naca0012/inv_NACA0012.cfg
@@ -78,8 +78,6 @@ MG_DAMP_PROLONGATION= 1.0
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
@@ -94,7 +92,7 @@ TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-DV_KIND= HICKS_HENNE 
+DV_KIND= HICKS_HENNE
 DV_MARKER= ( airfoil )
 DV_PARAM= ( 1, 0.5 )
 DV_VALUE= 0.01
diff --git a/TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg b/TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg
index df4c8cb355d..98a0ff215be 100644
--- a/TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg
+++ b/TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg
@@ -79,8 +79,6 @@ MG_DAMP_PROLONGATION= 1.0
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
@@ -95,7 +93,7 @@ TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-DV_KIND= HICKS_HENNE 
+DV_KIND= HICKS_HENNE
 DV_MARKER= ( airfoil )
 DV_PARAM= ( 1, 0.5 )
 DV_VALUE= 0.01
@@ -132,7 +130,7 @@ GRAD_OBJFUNC_FILENAME= of_grad.dat
 SURFACE_FILENAME= surface_flow
 SURFACE_ADJ_FILENAME= surface_adjoint
 OUTPUT_WRT_FREQ= 250
-SCREEN_OUTPUT = (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_GEO, SENS_AOA) 
+SCREEN_OUTPUT = (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_GEO, SENS_AOA)
 OUTPUT_FILES= (RESTART_ASCII)
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
diff --git a/TestCases/gust/inv_gust_NACA0012.cfg b/TestCases/gust/inv_gust_NACA0012.cfg
index 4cf8daa5f62..b34aca695d2 100644
--- a/TestCases/gust/inv_gust_NACA0012.cfg
+++ b/TestCases/gust/inv_gust_NACA0012.cfg
@@ -46,7 +46,7 @@ MACH_MOTION= 0.2
 % --------------------------- GUST SIMULATION ---------------------------------%
 %
 % The gust simulation requires the GRID_MOVEMENT flag to be set to YES.
-% and the GRID_MOVEMENT_KIND to be set to GUST or any of the other options. 
+% and the GRID_MOVEMENT_KIND to be set to GUST or any of the other options.
 % Apply a wind gust (NO, YES)
 WIND_GUST = YES
 GUST_TYPE = SINE
@@ -102,8 +102,6 @@ MG_DAMP_PROLONGATION= 0.75
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 ENTROPY_FIX_COEFF= 0.001
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
diff --git a/TestCases/harmonic_balance/HB.cfg b/TestCases/harmonic_balance/HB.cfg
index a8cc80f3495..d73c5d4d591 100644
--- a/TestCases/harmonic_balance/HB.cfg
+++ b/TestCases/harmonic_balance/HB.cfg
@@ -27,7 +27,7 @@ GRID_MOVEMENT= RIGID_MOTION
 MOTION_ORIGIN= ( 0.248 0.0 0.0 )
 PITCHING_OMEGA= ( 0.0 0.0 106.69842)
 PITCHING_AMPL= ( 0.0 0.0 1.01 )
- 
+
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
 MACH_NUMBER= 0.796
@@ -67,8 +67,6 @@ LINEAR_SOLVER_ITER= 5
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= NONE
 VENKAT_LIMITER_COEFF= 0.03
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
@@ -129,4 +127,4 @@ OUTPUT_WRT_FREQ= 500
 %
 OPT_OBJECTIVE= DRAG * 0.001
 OPT_CONSTRAINT= NONE
-DEFINITION_DV= ( 30, 1.0 | airfoil | 1, 0.75 ) 
+DEFINITION_DV= ( 30, 1.0 | airfoil | 1, 0.75 )
diff --git a/TestCases/optimization_euler/pitching_naca64a010/pitching_NACA64A010.cfg b/TestCases/optimization_euler/pitching_naca64a010/pitching_NACA64A010.cfg
index d8aab437132..406613be3c0 100644
--- a/TestCases/optimization_euler/pitching_naca64a010/pitching_NACA64A010.cfg
+++ b/TestCases/optimization_euler/pitching_naca64a010/pitching_NACA64A010.cfg
@@ -41,7 +41,7 @@ PITCHING_OMEGA_Z= 106.69842
 PITCHING_AMPL_X= 0.0
 PITCHING_AMPL_Y= 0.0
 PITCHING_AMPL_Z= 1.01
- 
+
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
 MACH_NUMBER= 0.796
@@ -97,8 +97,6 @@ MG_DAMP_PROLONGATION= 0.9
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 VENKAT_LIMITER_COEFF= 0.1
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
diff --git a/TestCases/optimization_euler/pitching_oneram6/pitching_ONERAM6.cfg b/TestCases/optimization_euler/pitching_oneram6/pitching_ONERAM6.cfg
index 5ef926bb5d8..64f4ba796f6 100644
--- a/TestCases/optimization_euler/pitching_oneram6/pitching_ONERAM6.cfg
+++ b/TestCases/optimization_euler/pitching_oneram6/pitching_ONERAM6.cfg
@@ -90,8 +90,6 @@ MG_DAMP_PROLONGATION= 0.9
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 VENKAT_LIMITER_COEFF= 0.03
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
@@ -144,7 +142,7 @@ OUTPUT_WRT_FREQ= 1
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-DV_KIND= FFD_SETTING 
+DV_KIND= FFD_SETTING
 DV_MARKER= ( UPPER_SIDE, LOWER_SIDE, TIP )
 DV_PARAM= ( 0, 1, 0, 0, 0.0, 0.0, 1.0 )
 DV_VALUE= 0.0
diff --git a/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg b/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg
index 1095bbd5948..c7cdd4ed539 100644
--- a/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg
+++ b/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg
@@ -74,8 +74,6 @@ MG_DAMP_PROLONGATION= 1.0
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
@@ -90,7 +88,7 @@ TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-DV_KIND= HICKS_HENNE 
+DV_KIND= HICKS_HENNE
 DV_MARKER= ( airfoil )
 DV_PARAM= ( 1, 0.5 )
 DV_VALUE= 0.01
diff --git a/TestCases/optimization_rans/pitching_naca64a010/turb_NACA64A010.cfg b/TestCases/optimization_rans/pitching_naca64a010/turb_NACA64A010.cfg
index 854a28c9699..ee9dd398136 100644
--- a/TestCases/optimization_rans/pitching_naca64a010/turb_NACA64A010.cfg
+++ b/TestCases/optimization_rans/pitching_naca64a010/turb_NACA64A010.cfg
@@ -32,7 +32,7 @@ MACH_MOTION= 0.796
 MOTION_ORIGIN= 0.248 0.0 0.0
 PITCHING_OMEGA= 0.0 0.0 106.69842
 PITCHING_AMPL= 0.0 0.0 1.01
- 
+
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
 MACH_NUMBER= 0.796
@@ -89,8 +89,6 @@ MG_DAMP_PROLONGATION= 0.7
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 VENKAT_LIMITER_COEFF= 0.03
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
diff --git a/TestCases/optimization_rans/pitching_oneram6/turb_ONERAM6.cfg b/TestCases/optimization_rans/pitching_oneram6/turb_ONERAM6.cfg
index d943deff183..d37f0cb5b32 100644
--- a/TestCases/optimization_rans/pitching_oneram6/turb_ONERAM6.cfg
+++ b/TestCases/optimization_rans/pitching_oneram6/turb_ONERAM6.cfg
@@ -88,8 +88,6 @@ MG_DAMP_PROLONGATION= 0.7
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 VENKAT_LIMITER_COEFF= 0.03
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
diff --git a/TestCases/optimization_rans/steady_oneram6/turb_ONERAM6.cfg b/TestCases/optimization_rans/steady_oneram6/turb_ONERAM6.cfg
index 259e678ec14..5d343bf53e7 100644
--- a/TestCases/optimization_rans/steady_oneram6/turb_ONERAM6.cfg
+++ b/TestCases/optimization_rans/steady_oneram6/turb_ONERAM6.cfg
@@ -70,8 +70,6 @@ MG_DAMP_PROLONGATION= 0.7
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 VENKAT_LIMITER_COEFF= 0.03
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
diff --git a/TestCases/polar/naca0012/inv_NACA0012.cfg b/TestCases/polar/naca0012/inv_NACA0012.cfg
index 663f763adfa..4bf598695c3 100644
--- a/TestCases/polar/naca0012/inv_NACA0012.cfg
+++ b/TestCases/polar/naca0012/inv_NACA0012.cfg
@@ -75,8 +75,6 @@ MG_DAMP_PROLONGATION= 1.0
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_multigrid_restart.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_multigrid_restart.cfg
index 294e470fc32..327f55dad3c 100644
--- a/TestCases/rans/naca0012/turb_NACA0012_sst_multigrid_restart.cfg
+++ b/TestCases/rans/naca0012/turb_NACA0012_sst_multigrid_restart.cfg
@@ -105,8 +105,6 @@ MG_DAMP_PROLONGATION= 0.8
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 ENTROPY_FIX_COEFF= 0.0
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
diff --git a/TestCases/rans/rae2822/turb_SA_RAE2822.cfg b/TestCases/rans/rae2822/turb_SA_RAE2822.cfg
index 33c811fc61f..17b6e2071f5 100644
--- a/TestCases/rans/rae2822/turb_SA_RAE2822.cfg
+++ b/TestCases/rans/rae2822/turb_SA_RAE2822.cfg
@@ -62,8 +62,6 @@ MG_DAMP_PROLONGATION= 0.95
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 VENKAT_LIMITER_COEFF= 0.03
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
diff --git a/TestCases/rans/rae2822/turb_SST_RAE2822.cfg b/TestCases/rans/rae2822/turb_SST_RAE2822.cfg
index 6ff0416c4ab..e867e993ec2 100644
--- a/TestCases/rans/rae2822/turb_SST_RAE2822.cfg
+++ b/TestCases/rans/rae2822/turb_SST_RAE2822.cfg
@@ -66,8 +66,6 @@ MG_DAMP_PROLONGATION= 0.95
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= NONE
 VENKAT_LIMITER_COEFF= 0.03
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
diff --git a/TestCases/rans/rae2822/turb_SST_SUST_RAE2822.cfg b/TestCases/rans/rae2822/turb_SST_SUST_RAE2822.cfg
index 6c25dd63049..42f3ec6079e 100644
--- a/TestCases/rans/rae2822/turb_SST_SUST_RAE2822.cfg
+++ b/TestCases/rans/rae2822/turb_SST_SUST_RAE2822.cfg
@@ -67,8 +67,6 @@ MG_DAMP_PROLONGATION= 0.95
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= NONE
 VENKAT_LIMITER_COEFF= 0.03
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
diff --git a/TestCases/rans/s809/trans_s809.cfg b/TestCases/rans/s809/trans_s809.cfg
index 60ef01253e6..733d2729700 100644
--- a/TestCases/rans/s809/trans_s809.cfg
+++ b/TestCases/rans/s809/trans_s809.cfg
@@ -66,8 +66,6 @@ MG_DAMP_PROLONGATION= 0.95
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= NONE
 VENKAT_LIMITER_COEFF= 0.03
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
diff --git a/TestCases/rotating/caradonna_tung/rot_caradonna_tung.cfg b/TestCases/rotating/caradonna_tung/rot_caradonna_tung.cfg
index 1ab945c73a6..944dc7c99c3 100644
--- a/TestCases/rotating/caradonna_tung/rot_caradonna_tung.cfg
+++ b/TestCases/rotating/caradonna_tung/rot_caradonna_tung.cfg
@@ -76,8 +76,6 @@ MG_DAMP_PROLONGATION= 0.9
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
diff --git a/TestCases/rotating/naca0012/rot_NACA0012.cfg b/TestCases/rotating/naca0012/rot_NACA0012.cfg
index 26c1ad79747..ea880d64c3d 100644
--- a/TestCases/rotating/naca0012/rot_NACA0012.cfg
+++ b/TestCases/rotating/naca0012/rot_NACA0012.cfg
@@ -78,8 +78,6 @@ MG_DAMP_PROLONGATION= 0.95
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 VENKAT_LIMITER_COEFF= 0.03
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
diff --git a/TestCases/sliding_interface/bars_SST_2D/bars.cfg b/TestCases/sliding_interface/bars_SST_2D/bars.cfg
index 02c1183f074..0f2557b9bfd 100644
--- a/TestCases/sliding_interface/bars_SST_2D/bars.cfg
+++ b/TestCases/sliding_interface/bars_SST_2D/bars.cfg
@@ -102,8 +102,6 @@ MG_DAMP_PROLONGATION= 0.75
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= NONE
 VENKAT_LIMITER_COEFF= 0.02
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
diff --git a/TestCases/unsteady/pitching_naca64a010_euler/pitching_NACA64A010.cfg b/TestCases/unsteady/pitching_naca64a010_euler/pitching_NACA64A010.cfg
index 90f3e25f814..d9f0910c39a 100644
--- a/TestCases/unsteady/pitching_naca64a010_euler/pitching_NACA64A010.cfg
+++ b/TestCases/unsteady/pitching_naca64a010_euler/pitching_NACA64A010.cfg
@@ -93,8 +93,6 @@ MG_DAMP_PROLONGATION= 0.9
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 VENKAT_LIMITER_COEFF= 0.1
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
diff --git a/TestCases/unsteady/pitching_naca64a010_rans/turb_NACA64A010.cfg b/TestCases/unsteady/pitching_naca64a010_rans/turb_NACA64A010.cfg
index ac34070b960..3f510d03e30 100644
--- a/TestCases/unsteady/pitching_naca64a010_rans/turb_NACA64A010.cfg
+++ b/TestCases/unsteady/pitching_naca64a010_rans/turb_NACA64A010.cfg
@@ -34,7 +34,7 @@ MACH_MOTION= 0.796
 MOTION_ORIGIN= 0.248 0.0 0.0
 PITCHING_OMEGA= 0.0 0.0 106.69842
 PITCHING_AMPL= 0.0 0.0 1.01
- 
+
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
 MACH_NUMBER= 0.796
@@ -91,8 +91,6 @@ MG_DAMP_PROLONGATION= 0.7
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 VENKAT_LIMITER_COEFF= 0.03
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
diff --git a/config_template.cfg b/config_template.cfg
index 08acc5eedc7..7a30a6d6fc8 100644
--- a/config_template.cfg
+++ b/config_template.cfg
@@ -1095,23 +1095,23 @@ CUSTOM_OBJFUNC= 'DRAG + 10 * pow(fmax(0.4-LIFT, 0), 2)'
 %           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
 %
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
+% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG, BARTH_JESPERSEN, VAN_ALBADA_EDGE)
+%
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 %
 % Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
 %           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_TURB= NO
 %
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
+% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG, BARTH_JESPERSEN)
+%
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
 %
 % Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
 %           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJFLOW= YES
 %
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
+% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
 %                SHARP_EDGES, WALL_DISTANCE)
 SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
 %
@@ -1119,7 +1119,7 @@ SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
 %           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_ADJTURB= NO
 %
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE)
+% Slope limiter (see SLOPE_LIMITER_ADJFLOW)
 SLOPE_LIMITER_ADJTURB= VENKATAKRISHNAN
 %
 % Coefficient for the Venkat's limiter (upwind scheme). A larger values decrease
@@ -1210,7 +1210,7 @@ MG_DAMP_PROLONGATION= 0.75
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, JST_KE, JST_MAT, LAX-FRIEDRICH, CUSP, ROE, AUSM,
+% Convective numerical method (JST, JST_KE, JST_MAT, LAX-FRIEDRICH, ROE, AUSM,
 %                              AUSMPLUSUP, AUSMPLUSUP2, AUSMPLUSM, HLLC, TURKEL_PREC,
 %                              SW, MSW, FDS, SLAU, SLAU2, L2ROE, LMROE)
 CONV_NUM_METHOD_FLOW= ROE

From 94b5c70632cc47609798be30e43af30b41073678 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 26 Mar 2023 10:13:10 +0100
Subject: [PATCH 315/656] fix meson

---
 SU2_CFD/src/meson.build | 1 -
 1 file changed, 1 deletion(-)

diff --git a/SU2_CFD/src/meson.build b/SU2_CFD/src/meson.build
index 03fe477787d..23fbeee0627 100644
--- a/SU2_CFD/src/meson.build
+++ b/SU2_CFD/src/meson.build
@@ -122,7 +122,6 @@ su2_cfd_src += files(['numerics/CNumerics.cpp',
                       'numerics/flow/convection/roe.cpp',
                       'numerics/flow/convection/fds.cpp',
                       'numerics/flow/convection/fvs.cpp',
-                      'numerics/flow/convection/cusp.cpp',
                       'numerics/flow/convection/hllc.cpp',
                       'numerics/flow/convection/ausm_slau.cpp',
                       'numerics/flow/convection/centered.cpp',

From e68082115cde16eb8dc4caa6ada397bc2d5d3244 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 26 Mar 2023 10:32:45 +0100
Subject: [PATCH 316/656] fix include

---
 SU2_CFD/src/drivers/CDriver.cpp | 1 -
 1 file changed, 1 deletion(-)

diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index e754a7f2598..0ea1830519e 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -61,7 +61,6 @@
 #include "../../include/numerics/flow/convection/roe.hpp"
 #include "../../include/numerics/flow/convection/fds.hpp"
 #include "../../include/numerics/flow/convection/fvs.hpp"
-#include "../../include/numerics/flow/convection/cusp.hpp"
 #include "../../include/numerics/flow/convection/hllc.hpp"
 #include "../../include/numerics/flow/convection/ausm_slau.hpp"
 #include "../../include/numerics/flow/convection/centered.hpp"

From d350b08305f4d01784585a7d1ef0d3cc2c4a57c5 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 26 Mar 2023 12:59:32 +0100
Subject: [PATCH 317/656] continuous adjoint fixes

---
 Common/src/CConfig.cpp                        |  7 +++++++
 QuickStart/inv_NACA0012.cfg                   |  8 -------
 SU2_CFD/src/variables/CFlowVariable.cpp       |  2 +-
 .../cont_adj_euler/oneram6/inv_ONERAM6.cfg    |  2 --
 .../cont_adj_rans/naca0012/turb_nasa.cfg      |  2 --
 .../naca0012/turb_nasa_binary.cfg             |  2 --
 .../control_surface/inv_ONERAM6_moving.cfg    |  2 --
 .../control_surface/inv_ONERAM6_setting.cfg   |  2 --
 .../deformation/naca0012/def_NACA0012.cfg     |  2 --
 .../naca0012/surface_file_NACA0012.cfg        |  2 --
 .../disc_adj_euler/arina2k/Arina2KRS.cfg      | 15 +------------
 .../cylinder3D/inv_cylinder3D.cfg             | 21 ++++---------------
 TestCases/euler/CRM/inv_CRM_JST.cfg           |  2 --
 TestCases/euler/biparabolic/BIPARABOLIC.cfg   |  2 --
 TestCases/euler/naca0012/inv_NACA0012.cfg     |  2 --
 TestCases/euler/oneram6/inv_ONERAM6.cfg       |  2 --
 TestCases/fixed_cl/naca0012/inv_NACA0012.cfg  |  2 --
 .../naca0012/inv_NACA0012_ContAdj.cfg         |  2 --
 TestCases/harmonic_balance/HB.cfg             |  2 --
 .../nonequilibrium/invwedge/invwedge_lax.cfg  |  9 +++-----
 .../pitching_NACA64A010.cfg                   |  2 --
 .../pitching_oneram6/pitching_ONERAM6.cfg     |  2 --
 .../steady_inverse_design/inv_NACA0012.cfg    |  2 --
 .../pitching_naca64a010/turb_NACA64A010.cfg   |  2 --
 .../pitching_oneram6/turb_ONERAM6.cfg         |  2 --
 TestCases/polar/naca0012/inv_NACA0012.cfg     |  2 --
 .../unsteady_CHT_FlatPlate_Conf.cfg           | 13 ------------
 .../turb_NACA0012_sst_multigrid_restart.cfg   |  2 --
 TestCases/rans/rae2822/turb_SA_RAE2822.cfg    |  2 --
 TestCases/rotating/naca0012/rot_NACA0012.cfg  |  2 --
 .../pitching_NACA64A010.cfg                   |  2 --
 .../turb_NACA64A010.cfg                       |  2 --
 32 files changed, 16 insertions(+), 109 deletions(-)

diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 66ce4bdbd5c..0e8199669fd 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -3567,6 +3567,13 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
       MUSCL_Flow = false;
     }
   }
+  if (MUSCL_AdjFlow && (Kind_ConvNumScheme_AdjFlow == SPACE_CENTERED)) {
+    if (OptionIsSet("MUSCL_ADJFLOW")) {
+      SU2_MPI::Error("Centered schemes do not use MUSCL reconstruction (use MUSCL_ADJFLOW= NO).", CURRENT_FUNCTION);
+    } else {
+      MUSCL_AdjFlow = false;
+    }
+  }
 
   if (!MUSCL_Flow || (Kind_ConvNumScheme_Flow == SPACE_CENTERED)) Kind_SlopeLimit_Flow = LIMITER::NONE;
   if (!MUSCL_AdjFlow || (Kind_ConvNumScheme_AdjFlow == SPACE_CENTERED)) Kind_SlopeLimit_AdjFlow = LIMITER::NONE;
diff --git a/QuickStart/inv_NACA0012.cfg b/QuickStart/inv_NACA0012.cfg
index 8876c69dd7c..7f30c73c42a 100644
--- a/QuickStart/inv_NACA0012.cfg
+++ b/QuickStart/inv_NACA0012.cfg
@@ -161,14 +161,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
 %
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
-MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
-SLOPE_LIMITER_ADJFLOW= NONE
-%
 % Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.01
 %
diff --git a/SU2_CFD/src/variables/CFlowVariable.cpp b/SU2_CFD/src/variables/CFlowVariable.cpp
index 09bc5e0f889..1fdfd484523 100644
--- a/SU2_CFD/src/variables/CFlowVariable.cpp
+++ b/SU2_CFD/src/variables/CFlowVariable.cpp
@@ -50,7 +50,7 @@ CFlowVariable::CFlowVariable(unsigned long npoint, unsigned long ndim, unsigned
 
   Primitive.resize(nPoint, nPrimVar) = su2double(0.0);
 
-  if (config->GetMUSCL_Flow() || config->GetViscous()) {
+  if (config->GetMUSCL_Flow() || config->GetViscous() || config->GetContinuous_Adjoint()) {
     Gradient_Primitive.resize(nPoint, nPrimVarGrad, nDim, 0.0);
   }
 
diff --git a/TestCases/cont_adj_euler/oneram6/inv_ONERAM6.cfg b/TestCases/cont_adj_euler/oneram6/inv_ONERAM6.cfg
index c7b8b52b73e..d23b4072609 100644
--- a/TestCases/cont_adj_euler/oneram6/inv_ONERAM6.cfg
+++ b/TestCases/cont_adj_euler/oneram6/inv_ONERAM6.cfg
@@ -85,8 +85,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/cont_adj_rans/naca0012/turb_nasa.cfg b/TestCases/cont_adj_rans/naca0012/turb_nasa.cfg
index 9d46631ea8f..ca0506980a6 100644
--- a/TestCases/cont_adj_rans/naca0012/turb_nasa.cfg
+++ b/TestCases/cont_adj_rans/naca0012/turb_nasa.cfg
@@ -72,8 +72,6 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.002 )
 CFL_REDUCTION_ADJFLOW= 0.25
diff --git a/TestCases/cont_adj_rans/naca0012/turb_nasa_binary.cfg b/TestCases/cont_adj_rans/naca0012/turb_nasa_binary.cfg
index 01749d1b3e3..df636cd5fcd 100644
--- a/TestCases/cont_adj_rans/naca0012/turb_nasa_binary.cfg
+++ b/TestCases/cont_adj_rans/naca0012/turb_nasa_binary.cfg
@@ -73,8 +73,6 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.002 )
 CFL_REDUCTION_ADJFLOW= 0.25
diff --git a/TestCases/control_surface/inv_ONERAM6_moving.cfg b/TestCases/control_surface/inv_ONERAM6_moving.cfg
index ad7d458ca4c..d9db83c262d 100644
--- a/TestCases/control_surface/inv_ONERAM6_moving.cfg
+++ b/TestCases/control_surface/inv_ONERAM6_moving.cfg
@@ -77,8 +77,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.04 )
 CFL_REDUCTION_ADJFLOW= 0.5
diff --git a/TestCases/control_surface/inv_ONERAM6_setting.cfg b/TestCases/control_surface/inv_ONERAM6_setting.cfg
index 43bf414dec5..d29f8702234 100644
--- a/TestCases/control_surface/inv_ONERAM6_setting.cfg
+++ b/TestCases/control_surface/inv_ONERAM6_setting.cfg
@@ -77,8 +77,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.04 )
 CFL_REDUCTION_ADJFLOW= 0.5
diff --git a/TestCases/deformation/naca0012/def_NACA0012.cfg b/TestCases/deformation/naca0012/def_NACA0012.cfg
index 5135ac45b2f..9f5d4a7a883 100644
--- a/TestCases/deformation/naca0012/def_NACA0012.cfg
+++ b/TestCases/deformation/naca0012/def_NACA0012.cfg
@@ -80,8 +80,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/deformation/naca0012/surface_file_NACA0012.cfg b/TestCases/deformation/naca0012/surface_file_NACA0012.cfg
index f39721c4322..8896ecd9454 100644
--- a/TestCases/deformation/naca0012/surface_file_NACA0012.cfg
+++ b/TestCases/deformation/naca0012/surface_file_NACA0012.cfg
@@ -80,8 +80,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/disc_adj_euler/arina2k/Arina2KRS.cfg b/TestCases/disc_adj_euler/arina2k/Arina2KRS.cfg
index 0adc1f99fef..a6020dacefc 100644
--- a/TestCases/disc_adj_euler/arina2k/Arina2KRS.cfg
+++ b/TestCases/disc_adj_euler/arina2k/Arina2KRS.cfg
@@ -20,7 +20,7 @@ RESTART_SOL= NO
 DISCARD_INFILES= NO
 SYSTEM_MEASUREMENTS= SI
 
-% -------------------- COMPRESSIBLE FREE-STREAM 
+% -------------------- COMPRESSIBLE FREE-STREAM
 %
 MACH_NUMBER= 0.2395
 AOA= 0.0
@@ -94,21 +94,8 @@ OBJECTIVE_WEIGHT = 1.0
 
 % ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
 %
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-MUSCL_TURB= NO
-SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
-MUSCL_ADJTURB= NO
-SLOPE_LIMITER_ADJTURB= VENKATAKRISHNAN
-VENKAT_LIMITER_COEFF= 0.05
-ADJ_SHARP_LIMITER_COEFF= 3.0
-LIMITER_ITER= 999999
 LAX_SENSOR_COEFF= 0.15
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-ADJ_LAX_SENSOR_COEFF= 0.15
-ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
diff --git a/TestCases/disc_adj_euler/cylinder3D/inv_cylinder3D.cfg b/TestCases/disc_adj_euler/cylinder3D/inv_cylinder3D.cfg
index 6490cb0e66a..bb26a568109 100644
--- a/TestCases/disc_adj_euler/cylinder3D/inv_cylinder3D.cfg
+++ b/TestCases/disc_adj_euler/cylinder3D/inv_cylinder3D.cfg
@@ -17,7 +17,7 @@ MATH_PROBLEM= DISCRETE_ADJOINT
 RESTART_SOL= NO
 DISCARD_INFILES= NO
 SYSTEM_MEASUREMENTS= SI
-REORIENT_ELEMENTS= NO 
+REORIENT_ELEMENTS= NO
 HISTORY_OUTPUT= (ITER, RMS_RES, SENSITIVITY)
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
@@ -38,7 +38,7 @@ REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
 MARKER_EULER= (CYLINDER_DOWN, CYLINDER_UP, SIDE, WALL)
-INLET_TYPE= MASS_FLOW 
+INLET_TYPE= MASS_FLOW
 MARKER_INLET= ( IN, 1.22498, 102.089, 1.0, 0.0, 0.0 )
 MARKER_OUTLET= ( OUT, 101325 )
 
@@ -48,7 +48,7 @@ MARKER_PLOTTING = ( CYLINDER_DOWN, CYLINDER_UP )
 MARKER_MONITORING = ( CYLINDER_DOWN, CYLINDER_UP )
 MARKER_DESIGNING = ( CYLINDER_DOWN, CYLINDER_UP )
 MARKER_ANALYZE = ( IN, OUT )
-MARKER_ANALYZE_AVERAGE = AREA 
+MARKER_ANALYZE_AVERAGE = AREA
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
@@ -56,25 +56,12 @@ NUM_METHOD_GRAD= GREEN_GAUSS
 CFL_NUMBER= 10.0
 CFL_ADAPT= NO
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.25, 50.0 )
-OBJECTIVE_FUNCTION= LIFT 
+OBJECTIVE_FUNCTION= LIFT
 
 % ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
 %
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-MUSCL_TURB= NO
-SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
-MUSCL_ADJTURB= NO
-SLOPE_LIMITER_ADJTURB= VENKATAKRISHNAN
-VENKAT_LIMITER_COEFF= 0.05
-ADJ_SHARP_LIMITER_COEFF= 3.0
-LIMITER_ITER= 999999
 LAX_SENSOR_COEFF= 0.15
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-ADJ_LAX_SENSOR_COEFF= 0.15
-ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
diff --git a/TestCases/euler/CRM/inv_CRM_JST.cfg b/TestCases/euler/CRM/inv_CRM_JST.cfg
index 287c9bcefd7..4e5e9839caa 100644
--- a/TestCases/euler/CRM/inv_CRM_JST.cfg
+++ b/TestCases/euler/CRM/inv_CRM_JST.cfg
@@ -73,8 +73,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.04 )
 CFL_REDUCTION_ADJFLOW= 0.5
diff --git a/TestCases/euler/biparabolic/BIPARABOLIC.cfg b/TestCases/euler/biparabolic/BIPARABOLIC.cfg
index c3787da951d..94a1aee34ca 100644
--- a/TestCases/euler/biparabolic/BIPARABOLIC.cfg
+++ b/TestCases/euler/biparabolic/BIPARABOLIC.cfg
@@ -73,8 +73,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= EQUIVALENT_AREA
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.8
diff --git a/TestCases/euler/naca0012/inv_NACA0012.cfg b/TestCases/euler/naca0012/inv_NACA0012.cfg
index 9f998d9e087..98af59604f8 100644
--- a/TestCases/euler/naca0012/inv_NACA0012.cfg
+++ b/TestCases/euler/naca0012/inv_NACA0012.cfg
@@ -77,8 +77,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/euler/oneram6/inv_ONERAM6.cfg b/TestCases/euler/oneram6/inv_ONERAM6.cfg
index c7f38f4d194..043a66e1910 100644
--- a/TestCases/euler/oneram6/inv_ONERAM6.cfg
+++ b/TestCases/euler/oneram6/inv_ONERAM6.cfg
@@ -85,8 +85,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/fixed_cl/naca0012/inv_NACA0012.cfg b/TestCases/fixed_cl/naca0012/inv_NACA0012.cfg
index 1a762d295e7..e83ac88b86f 100644
--- a/TestCases/fixed_cl/naca0012/inv_NACA0012.cfg
+++ b/TestCases/fixed_cl/naca0012/inv_NACA0012.cfg
@@ -84,8 +84,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg b/TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg
index 98a0ff215be..ba4bb1f9f9a 100644
--- a/TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg
+++ b/TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg
@@ -85,8 +85,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/harmonic_balance/HB.cfg b/TestCases/harmonic_balance/HB.cfg
index d73c5d4d591..b34daa826e0 100644
--- a/TestCases/harmonic_balance/HB.cfg
+++ b/TestCases/harmonic_balance/HB.cfg
@@ -75,8 +75,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.6
diff --git a/TestCases/nonequilibrium/invwedge/invwedge_lax.cfg b/TestCases/nonequilibrium/invwedge/invwedge_lax.cfg
index 0ca7867ae3d..d5b025f9ab4 100644
--- a/TestCases/nonequilibrium/invwedge/invwedge_lax.cfg
+++ b/TestCases/nonequilibrium/invwedge/invwedge_lax.cfg
@@ -47,9 +47,6 @@ LINEAR_SOLVER_ITER= 5
 % -----------------------------------------------------------------------%
 %
 CONV_NUM_METHOD_FLOW= LAX-FRIEDRICH
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-VENKAT_LIMITER_COEFF= 0.05
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
@@ -63,11 +60,11 @@ CONV_CAUCHY_EPS= 1E-10
 %
 MESH_FILENAME= invwedge.su2
 MESH_FORMAT= SU2
-SOLUTION_FILENAME= restart_flow.dat  
-TABULAR_FORMAT= TECPLOT 
+SOLUTION_FILENAME= restart_flow.dat
+TABULAR_FORMAT= TECPLOT
 CONV_FILENAME= convergence
 RESTART_FILENAME= restart_flow.dat
 VOLUME_FILENAME= soln_volume
-SURFACE_FILENAME= soln_surface     
+SURFACE_FILENAME= soln_surface
 OUTPUT_WRT_FREQ= 100
 OUTPUT_FILES= (RESTART_ASCII, PARAVIEW_ASCII)
diff --git a/TestCases/optimization_euler/pitching_naca64a010/pitching_NACA64A010.cfg b/TestCases/optimization_euler/pitching_naca64a010/pitching_NACA64A010.cfg
index 406613be3c0..f4e9b0862ed 100644
--- a/TestCases/optimization_euler/pitching_naca64a010/pitching_NACA64A010.cfg
+++ b/TestCases/optimization_euler/pitching_naca64a010/pitching_NACA64A010.cfg
@@ -105,8 +105,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/optimization_euler/pitching_oneram6/pitching_ONERAM6.cfg b/TestCases/optimization_euler/pitching_oneram6/pitching_ONERAM6.cfg
index 64f4ba796f6..e056a0664da 100644
--- a/TestCases/optimization_euler/pitching_oneram6/pitching_ONERAM6.cfg
+++ b/TestCases/optimization_euler/pitching_oneram6/pitching_ONERAM6.cfg
@@ -97,8 +97,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.25
diff --git a/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg b/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg
index c7cdd4ed539..b98662f4560 100644
--- a/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg
+++ b/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg
@@ -80,8 +80,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/optimization_rans/pitching_naca64a010/turb_NACA64A010.cfg b/TestCases/optimization_rans/pitching_naca64a010/turb_NACA64A010.cfg
index ee9dd398136..0d327d0e90f 100644
--- a/TestCases/optimization_rans/pitching_naca64a010/turb_NACA64A010.cfg
+++ b/TestCases/optimization_rans/pitching_naca64a010/turb_NACA64A010.cfg
@@ -104,8 +104,6 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.01 )
 CFL_REDUCTION_ADJFLOW= 0.9
diff --git a/TestCases/optimization_rans/pitching_oneram6/turb_ONERAM6.cfg b/TestCases/optimization_rans/pitching_oneram6/turb_ONERAM6.cfg
index d37f0cb5b32..ce6db99717a 100644
--- a/TestCases/optimization_rans/pitching_oneram6/turb_ONERAM6.cfg
+++ b/TestCases/optimization_rans/pitching_oneram6/turb_ONERAM6.cfg
@@ -103,8 +103,6 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/polar/naca0012/inv_NACA0012.cfg b/TestCases/polar/naca0012/inv_NACA0012.cfg
index 4bf598695c3..b083add885f 100644
--- a/TestCases/polar/naca0012/inv_NACA0012.cfg
+++ b/TestCases/polar/naca0012/inv_NACA0012.cfg
@@ -80,8 +80,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/py_wrapper/flatPlate_unsteady_CHT/unsteady_CHT_FlatPlate_Conf.cfg b/TestCases/py_wrapper/flatPlate_unsteady_CHT/unsteady_CHT_FlatPlate_Conf.cfg
index 481b6bea1d4..04c73f951bf 100644
--- a/TestCases/py_wrapper/flatPlate_unsteady_CHT/unsteady_CHT_FlatPlate_Conf.cfg
+++ b/TestCases/py_wrapper/flatPlate_unsteady_CHT/unsteady_CHT_FlatPlate_Conf.cfg
@@ -115,21 +115,8 @@ SENS_REMOVE_SHARP= NO
 
 % ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
 %
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-MUSCL_TURB= NO
-SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
-MUSCL_ADJTURB= NO
-SLOPE_LIMITER_ADJTURB= VENKATAKRISHNAN
-VENKAT_LIMITER_COEFF= 0.05
-ADJ_SHARP_LIMITER_COEFF= 3.0
-LIMITER_ITER= 999999
 LAX_SENSOR_COEFF= 0.15
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-ADJ_LAX_SENSOR_COEFF= 0.15
-ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_multigrid_restart.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_multigrid_restart.cfg
index 327f55dad3c..15af3903f87 100644
--- a/TestCases/rans/naca0012/turb_NACA0012_sst_multigrid_restart.cfg
+++ b/TestCases/rans/naca0012/turb_NACA0012_sst_multigrid_restart.cfg
@@ -119,8 +119,6 @@ CFL_REDUCTION_TURB= 1.0
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 CFL_REDUCTION_ADJFLOW= 0.8
diff --git a/TestCases/rans/rae2822/turb_SA_RAE2822.cfg b/TestCases/rans/rae2822/turb_SA_RAE2822.cfg
index 17b6e2071f5..a2e55937a88 100644
--- a/TestCases/rans/rae2822/turb_SA_RAE2822.cfg
+++ b/TestCases/rans/rae2822/turb_SA_RAE2822.cfg
@@ -75,8 +75,6 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.01 )
 CFL_REDUCTION_ADJFLOW= 0.75
diff --git a/TestCases/rotating/naca0012/rot_NACA0012.cfg b/TestCases/rotating/naca0012/rot_NACA0012.cfg
index ea880d64c3d..608002221ad 100644
--- a/TestCases/rotating/naca0012/rot_NACA0012.cfg
+++ b/TestCases/rotating/naca0012/rot_NACA0012.cfg
@@ -86,8 +86,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/unsteady/pitching_naca64a010_euler/pitching_NACA64A010.cfg b/TestCases/unsteady/pitching_naca64a010_euler/pitching_NACA64A010.cfg
index d9f0910c39a..bd7083dd7b1 100644
--- a/TestCases/unsteady/pitching_naca64a010_euler/pitching_NACA64A010.cfg
+++ b/TestCases/unsteady/pitching_naca64a010_euler/pitching_NACA64A010.cfg
@@ -101,8 +101,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/unsteady/pitching_naca64a010_rans/turb_NACA64A010.cfg b/TestCases/unsteady/pitching_naca64a010_rans/turb_NACA64A010.cfg
index 3f510d03e30..e2a0beda284 100644
--- a/TestCases/unsteady/pitching_naca64a010_rans/turb_NACA64A010.cfg
+++ b/TestCases/unsteady/pitching_naca64a010_rans/turb_NACA64A010.cfg
@@ -106,8 +106,6 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.01 )
 CFL_REDUCTION_ADJFLOW= 0.9

From 68bf5902d5163207bba3b8b332728d6884632ca7 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Mon, 27 Mar 2023 07:22:20 +0100
Subject: [PATCH 318/656] fix un init bool

---
 Common/src/CConfig.cpp | 18 +++++++++---------
 1 file changed, 9 insertions(+), 9 deletions(-)

diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 0e8199669fd..ea45d2d0159 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -5157,8 +5157,7 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
     Mesh_Box_Size[1] = 33;
     Mesh_Box_Size[2] = 33;
   } else if (nMesh_Box_Size != 3) {
-    SU2_MPI::Error(string("MESH_BOX_SIZE specified without 3 values.\n"),
-                   CURRENT_FUNCTION);
+    SU2_MPI::Error("MESH_BOX_SIZE specified without 3 values.\n", CURRENT_FUNCTION);
   }
 
   /* Force the lowest memory preconditioner when direct solvers are used. */
@@ -5175,8 +5174,8 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
   if (DiscreteAdjoint) {
 #if !defined CODI_REVERSE_TYPE
     if (Kind_SU2 == SU2_COMPONENT::SU2_CFD) {
-      SU2_MPI::Error(string("SU2_CFD: Config option MATH_PROBLEM= DISCRETE_ADJOINT requires AD support!\n") +
-                     string("Please use SU2_CFD_AD (configuration/compilation is done using the preconfigure.py script)."),
+      SU2_MPI::Error("SU2_CFD: Config option MATH_PROBLEM= DISCRETE_ADJOINT requires AD support!\n"
+                     "Please use SU2_CFD_AD (configuration/compilation is done using the preconfigure.py script).",
                      CURRENT_FUNCTION);
     }
 #endif
@@ -5190,8 +5189,8 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
       Restart_Flow = false;
 
       if (Unst_AdjointIter- long(nTimeIter) < 0){
-        SU2_MPI::Error(string("Invalid iteration number requested for unsteady adjoint.\n" ) +
-                       string("Make sure EXT_ITER is larger or equal than UNST_ADJOINT_ITER."),
+        SU2_MPI::Error("Invalid iteration number requested for unsteady adjoint.\n"
+                       "Make sure EXT_ITER is larger or equal than UNST_ADJOINT_ITER.",
                        CURRENT_FUNCTION);
       }
 
@@ -5250,8 +5249,7 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
    turbulence model. */
 
   if (MUSCL_AdjTurb) {
-    SU2_MPI::Error(string("MUSCL_ADJTURB= YES not currently supported.\n") +
-                   string("Please select MUSCL_ADJTURB= NO (first-order)."),
+    SU2_MPI::Error("MUSCL_ADJTURB= YES not currently supported.\nPlease select MUSCL_ADJTURB= NO (first-order).",
                    CURRENT_FUNCTION);
   }
 
@@ -5272,9 +5270,11 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
        we also want to avoid recomputation. */
 
       ReconstructionGradientRequired = false;
-      Kind_Gradient_Method_Recon     = Kind_Gradient_Method;
+      Kind_Gradient_Method_Recon = Kind_Gradient_Method;
     }
 
+  } else {
+    ReconstructionGradientRequired = false;
   }
 
   if (ReconstructionGradientRequired && GetFluidProblem() && Kind_ConvNumScheme_Flow == SPACE_CENTERED)

From cda1c50ff481d72274df76eda6770015d3a36e5e Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Mon, 27 Mar 2023 08:32:12 +0100
Subject: [PATCH 319/656] fix more testcases

---
 TestCases/disc_adj_heat/disc_adj_heat.cfg                 | 2 --
 .../harmonic_balance/hb_rans_preconditioning/davis.cfg    | 8 +-------
 .../pitching_naca0015_rans_inc/config_incomp_turb_sa.cfg  | 3 ---
 3 files changed, 1 insertion(+), 12 deletions(-)

diff --git a/TestCases/disc_adj_heat/disc_adj_heat.cfg b/TestCases/disc_adj_heat/disc_adj_heat.cfg
index a2509c72d08..2b3ad200e75 100644
--- a/TestCases/disc_adj_heat/disc_adj_heat.cfg
+++ b/TestCases/disc_adj_heat/disc_adj_heat.cfg
@@ -107,8 +107,6 @@ LINEAR_SOLVER_ITER= 10
 
 CONV_NUM_METHOD_FLOW= JST
 
-MUSCL_FLOW= YES
-
 JST_SENSOR_COEFF= ( 0.5, 0.05 )
 
 TIME_DISCRE_FLOW= EULER_IMPLICIT
diff --git a/TestCases/harmonic_balance/hb_rans_preconditioning/davis.cfg b/TestCases/harmonic_balance/hb_rans_preconditioning/davis.cfg
index 9ab79f61443..07e6b6d0fab 100644
--- a/TestCases/harmonic_balance/hb_rans_preconditioning/davis.cfg
+++ b/TestCases/harmonic_balance/hb_rans_preconditioning/davis.cfg
@@ -67,16 +67,10 @@ LINEAR_SOLVER_PREC= LU_SGS
 LINEAR_SOLVER_ERROR= 1E-4
 LINEAR_SOLVER_ITER= 5
 
-% ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
-%
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-VENKAT_LIMITER_COEFF= 0.05
-JST_SENSOR_COEFF= ( 0.5, 0.02 )
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
+JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
diff --git a/TestCases/unsteady/pitching_naca0015_rans_inc/config_incomp_turb_sa.cfg b/TestCases/unsteady/pitching_naca0015_rans_inc/config_incomp_turb_sa.cfg
index ee33ca1ee9c..0f84217b43d 100644
--- a/TestCases/unsteady/pitching_naca0015_rans_inc/config_incomp_turb_sa.cfg
+++ b/TestCases/unsteady/pitching_naca0015_rans_inc/config_incomp_turb_sa.cfg
@@ -67,10 +67,7 @@ LIMITER_ITER= 99999
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= JST
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= NONE
 TIME_DISCRE_FLOW= EULER_IMPLICIT
-RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %

From 4ed142f26c791217f149c774491443905aeb7dc2 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?K=C3=BCr=C5=9Fat=20Yurt?=
 <57598663+kursatyurt@users.noreply.github.com>
Date: Mon, 27 Mar 2023 19:44:19 +0200
Subject: [PATCH 320/656] Refactor Output classes method names (#1987)

* Refactor Output classes method names to CamelCase
---
 SU2_CFD/include/output/CAdjFlowCompOutput.hpp |   2 +-
 SU2_CFD/include/output/CAdjFlowIncOutput.hpp  |   2 +-
 SU2_CFD/include/output/CAdjFlowOutput.hpp     |  10 +-
 SU2_CFD/include/output/CElasticityOutput.hpp  |   2 +-
 SU2_CFD/include/output/CFlowCompFEMOutput.hpp |   2 +-
 SU2_CFD/include/output/CFlowCompOutput.hpp    |   4 +-
 SU2_CFD/include/output/CFlowIncOutput.hpp     |   2 +-
 SU2_CFD/include/output/CFlowOutput.hpp        |  21 +-
 SU2_CFD/include/output/CMultizoneOutput.hpp   |   6 +-
 SU2_CFD/include/output/CNEMOCompOutput.hpp    |   4 +-
 SU2_CFD/include/output/COutput.hpp            |  54 ++---
 SU2_CFD/include/output/COutputLegacy.hpp      |  22 +-
 .../output/filewriter/CCGNSFileWriter.hpp     |   2 +-
 .../output/filewriter/CCSVFileWriter.hpp      |   2 +-
 .../include/output/filewriter/CFileWriter.hpp |  10 +-
 .../output/filewriter/CParallelDataSorter.hpp |   6 +-
 .../filewriter/CParaviewBinaryFileWriter.hpp  |   2 +-
 .../output/filewriter/CParaviewFileWriter.hpp |   2 +-
 .../filewriter/CParaviewVTMFileWriter.hpp     |   2 +-
 .../filewriter/CParaviewXMLFileWriter.hpp     |   2 +-
 .../output/filewriter/CSTLFileWriter.hpp      |   2 +-
 .../filewriter/CSU2BinaryFileWriter.hpp       |   2 +-
 .../output/filewriter/CSU2FileWriter.hpp      |   2 +-
 .../output/filewriter/CSU2MeshFileWriter.hpp  |   2 +-
 .../filewriter/CTecplotBinaryFileWriter.hpp   |   2 +-
 .../output/filewriter/CTecplotFileWriter.hpp  |   2 +-
 .../include/output/tools/CWindowingTools.hpp  |   2 +-
 .../src/drivers/CDiscAdjMultizoneDriver.cpp   |   8 +-
 .../src/drivers/CDiscAdjSinglezoneDriver.cpp  |   6 +-
 SU2_CFD/src/drivers/CDriver.cpp               |  10 +-
 SU2_CFD/src/drivers/CMultizoneDriver.cpp      |   6 +-
 SU2_CFD/src/drivers/CSinglezoneDriver.cpp     |   2 +-
 .../src/iteration/CDiscAdjFEAIteration.cpp    |   2 +-
 .../src/iteration/CDiscAdjFluidIteration.cpp  |   2 +-
 .../src/iteration/CDiscAdjHeatIteration.cpp   |   2 +-
 SU2_CFD/src/iteration/CFEAIteration.cpp       |   2 +-
 SU2_CFD/src/iteration/CFluidIteration.cpp     |   4 +-
 SU2_CFD/src/iteration/CIteration.cpp          |   2 +-
 SU2_CFD/src/output/CAdjFlowCompOutput.cpp     |  12 +-
 SU2_CFD/src/output/CAdjFlowIncOutput.cpp      |  12 +-
 SU2_CFD/src/output/CAdjFlowOutput.cpp         |  10 +-
 SU2_CFD/src/output/CElasticityOutput.cpp      |   2 +-
 SU2_CFD/src/output/CFlowCompFEMOutput.cpp     |   2 +-
 SU2_CFD/src/output/CFlowCompOutput.cpp        |  20 +-
 SU2_CFD/src/output/CFlowIncOutput.cpp         |   8 +-
 SU2_CFD/src/output/CFlowOutput.cpp            |  30 +--
 SU2_CFD/src/output/CMultizoneOutput.cpp       |  10 +-
 SU2_CFD/src/output/CNEMOCompOutput.cpp        |  16 +-
 SU2_CFD/src/output/COutput.cpp                |  88 ++++----
 .../src/output/filewriter/CCGNSFileWriter.cpp |   4 +-
 .../src/output/filewriter/CCSVFileWriter.cpp  |   2 +-
 .../output/filewriter/CParallelDataSorter.cpp |   2 +-
 .../filewriter/CParaviewBinaryFileWriter.cpp  |   4 +-
 .../output/filewriter/CParaviewFileWriter.cpp |  68 +++---
 .../filewriter/CParaviewVTMFileWriter.cpp     |   6 +-
 .../filewriter/CParaviewXMLFileWriter.cpp     |   4 +-
 .../src/output/filewriter/CSTLFileWriter.cpp  |  12 +-
 .../filewriter/CSU2BinaryFileWriter.cpp       |   2 +-
 .../src/output/filewriter/CSU2FileWriter.cpp  |   4 +-
 .../output/filewriter/CSU2MeshFileWriter.cpp  |  14 +-
 .../filewriter/CTecplotBinaryFileWriter.cpp   | 206 +++++++++---------
 .../output/filewriter/CTecplotFileWriter.cpp  |  56 ++---
 .../src/output/output_structure_legacy.cpp    |  36 +--
 SU2_CFD/src/output/tools/CWindowingTools.cpp  |   2 +-
 SU2_DEF/src/drivers/CDeformationDriver.cpp    |   6 +-
 .../src/drivers/CDiscAdjDeformationDriver.cpp |   6 +-
 SU2_SOL/src/SU2_SOL.cpp                       |   8 +-
 UnitTests/SU2_CFD/windowing.cpp               |   2 +-
 68 files changed, 436 insertions(+), 437 deletions(-)

diff --git a/SU2_CFD/include/output/CAdjFlowCompOutput.hpp b/SU2_CFD/include/output/CAdjFlowCompOutput.hpp
index ffa0759cb63..0474657f6c6 100644
--- a/SU2_CFD/include/output/CAdjFlowCompOutput.hpp
+++ b/SU2_CFD/include/output/CAdjFlowCompOutput.hpp
@@ -92,6 +92,6 @@ class CAdjFlowCompOutput final: public CAdjFlowOutput {
    * \param[in] config - Definition of the particular problem.
    * \return <TRUE> if the residuals should be initialized.
    */
-  bool SetInit_Residuals(const CConfig *config) override;
+  bool SetInitResiduals(const CConfig *config) override ;
 
 };
diff --git a/SU2_CFD/include/output/CAdjFlowIncOutput.hpp b/SU2_CFD/include/output/CAdjFlowIncOutput.hpp
index fb70e926778..98f2ff1c8a2 100644
--- a/SU2_CFD/include/output/CAdjFlowIncOutput.hpp
+++ b/SU2_CFD/include/output/CAdjFlowIncOutput.hpp
@@ -99,6 +99,6 @@ class CAdjFlowIncOutput final: public CAdjFlowOutput {
    * \param[in] config - Definition of the particular problem.
    * \return <TRUE> if the residuals should be initialized.
    */
-  bool SetInit_Residuals(const CConfig *config) override;
+  bool SetInitResiduals(const CConfig *config) override ;
 
 };
diff --git a/SU2_CFD/include/output/CAdjFlowOutput.hpp b/SU2_CFD/include/output/CAdjFlowOutput.hpp
index 6a1bbd83a20..ce1a6958c09 100644
--- a/SU2_CFD/include/output/CAdjFlowOutput.hpp
+++ b/SU2_CFD/include/output/CAdjFlowOutput.hpp
@@ -64,26 +64,26 @@ class CAdjFlowOutput : public COutput {
   /*!
    * \brief Add scalar (turbulence/species) history fields for the linear solver (FVMComp, FVMInc, FVMNEMO).
    */
-  void AddHistoryOutputFields_AdjScalarLinsol(const CConfig* config);
+  void AddHistoryOutputFieldsAdjScalarLinsol(const CConfig* config);
 
   /*!
    * \brief Set all scalar (turbulence/species) history field values.
    */
-  void LoadHistoryData_AdjScalar(const CConfig* config, const CSolver* const* solver);
+  void LoadHistoryDataAdjScalar(const CConfig* config, const CSolver* const* solver);
 
   /*!
    * \brief Add scalar (turbulence/species) volume solution fields for a point (FVMComp, FVMInc, FVMNEMO).
    * \note The order of fields in restart files is fixed. Therefore the split-up.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetVolumeOutputFields_AdjScalarSolution(const CConfig* config);
+  void SetVolumeOutputFieldsAdjScalarSolution(const CConfig* config);
 
   /*!
    * \brief Add scalar (turbulence/species) volume solution fields for a point (FVMComp, FVMInc, FVMNEMO).
    * \note The order of fields in restart files is fixed. Therefore the split-up.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetVolumeOutputFields_AdjScalarResidual(const CConfig* config);
+  void SetVolumeOutputFieldsAdjScalarResidual(const CConfig* config);
 
   /*!
    * \brief Set all scalar (turbulence/species) volume field values for a point.
@@ -91,5 +91,5 @@ class CAdjFlowOutput : public COutput {
    * \param[in] solver - The container holding all solution data.
    * \param[in] iPoint - Index of the point.
    */
-  void LoadVolumeData_AdjScalar(const CConfig* config, const CSolver* const* solver, const unsigned long iPoint);
+  void LoadVolumeDataAdjScalar(const CConfig* config, const CSolver* const* solver, const unsigned long iPoint);
 };
diff --git a/SU2_CFD/include/output/CElasticityOutput.hpp b/SU2_CFD/include/output/CElasticityOutput.hpp
index 3ae1f695c0c..ad052b009f9 100644
--- a/SU2_CFD/include/output/CElasticityOutput.hpp
+++ b/SU2_CFD/include/output/CElasticityOutput.hpp
@@ -82,6 +82,6 @@ class CElasticityOutput final: public COutput {
    * \param[in] config - Definition of the particular problem.
    * \return <TRUE> if the residuals should be initialized.
    */
-  bool SetInit_Residuals(const CConfig *config) override;
+  bool SetInitResiduals(const CConfig *config) override ;
 
 };
diff --git a/SU2_CFD/include/output/CFlowCompFEMOutput.hpp b/SU2_CFD/include/output/CFlowCompFEMOutput.hpp
index 73d5f4ca1f9..3444b3e01f8 100644
--- a/SU2_CFD/include/output/CFlowCompFEMOutput.hpp
+++ b/SU2_CFD/include/output/CFlowCompFEMOutput.hpp
@@ -89,6 +89,6 @@ class CFlowCompFEMOutput final: public CFlowOutput {
    * \param[in] config - Definition of the particular problem.
    * \return <TRUE> if the residuals should be initialized.
    */
-  bool SetInit_Residuals(const CConfig *config) override;
+  bool SetInitResiduals(const CConfig *config) override ;
 
 };
diff --git a/SU2_CFD/include/output/CFlowCompOutput.hpp b/SU2_CFD/include/output/CFlowCompOutput.hpp
index e509ad1e01f..fbf27d36f43 100644
--- a/SU2_CFD/include/output/CFlowCompOutput.hpp
+++ b/SU2_CFD/include/output/CFlowCompOutput.hpp
@@ -79,7 +79,7 @@ class CFlowCompOutput final: public CFlowOutput {
    * \param[in] config - Definition of the particular problem.
    * \return <TRUE> if the residuals should be initialized.
    */
-  bool SetInit_Residuals(const CConfig *config) override;
+  bool SetInitResiduals(const CConfig *config) override ;
 
   /*!
    * \brief Write any additional output defined for the current solver.
@@ -91,5 +91,5 @@ class CFlowCompOutput final: public CFlowOutput {
    * \brief Determines if the history file output.
    * \param[in] config - Definition of the particular problem.
    */
-  bool WriteHistoryFile_Output(const CConfig *config) override;
+  bool WriteHistoryFileOutput(const CConfig *config) override ;
 };
diff --git a/SU2_CFD/include/output/CFlowIncOutput.hpp b/SU2_CFD/include/output/CFlowIncOutput.hpp
index 7578f3a7cd2..bdb7a23c5cb 100644
--- a/SU2_CFD/include/output/CFlowIncOutput.hpp
+++ b/SU2_CFD/include/output/CFlowIncOutput.hpp
@@ -83,6 +83,6 @@ class CFlowIncOutput final: public CFlowOutput {
    * \param[in] config - Definition of the particular problem.
    * \return <TRUE> if the residuals should be initialized.
    */
-  bool SetInit_Residuals(const CConfig *config) override;
+  bool SetInitResiduals(const CConfig *config) override ;
 
 };
diff --git a/SU2_CFD/include/output/CFlowOutput.hpp b/SU2_CFD/include/output/CFlowOutput.hpp
index e18d04f82d4..a3893cfb23c 100644
--- a/SU2_CFD/include/output/CFlowOutput.hpp
+++ b/SU2_CFD/include/output/CFlowOutput.hpp
@@ -80,7 +80,7 @@ class CFlowOutput : public CFVMOutput{
    * \param[in] Surface_MassFlow_Abs_Total - Massflow on all Marker_Analyze
    * \param[in] Surface_Area_Total - Area of all Marker_Analyze
    */
-  void SetAnalyzeSurface_SpeciesVariance(const CSolver* const*solver, const CGeometry *geometry, CConfig *config,
+  void SetAnalyzeSurfaceSpeciesVariance(const CSolver* const*solver, const CGeometry *geometry, CConfig *config,
                                          const su2activematrix& Surface_Species_Total,
                                          const vector<su2double>& Surface_MassFlow_Abs_Total,
                                          const vector<su2double>& Surface_Area_Total);
@@ -103,12 +103,12 @@ class CFlowOutput : public CFVMOutput{
   /*!
    * \brief Add scalar (turbulence/species) history fields for the linear solver (FVMComp, FVMInc, FVMNEMO).
    */
-  void AddHistoryOutputFields_ScalarLinsol(const CConfig* config);
+  void AddHistoryOutputFieldsScalarLinsol(const CConfig* config);
 
   /*!
    * \brief Set all scalar (turbulence/species) history field values.
    */
-  void LoadHistoryData_Scalar(const CConfig* config, const CSolver* const* solver);
+  void LoadHistoryDataScalar(const CConfig* config, const CSolver* const* solver);
 
   /*!
    * \brief Add scalar (turbulence/species) volume solution fields for a point (FVMComp, FVMInc, FVMNEMO).
@@ -137,7 +137,7 @@ class CFlowOutput : public CFVMOutput{
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] iPoint - Index of the point.
    */
-  void LoadVolumeData_Scalar(const CConfig* config, const CSolver* const* solver, const CGeometry* geometry,
+  void LoadVolumeDataScalar(const CConfig* config, const CSolver* const* solver, const CGeometry* geometry,
                              const unsigned long iPoint);
 
   /*!
@@ -180,7 +180,7 @@ class CFlowOutput : public CFVMOutput{
   /*!
    * \brief Add CP inverse design output as history fields
    */
-  void Add_CpInverseDesignOutput();
+  void AddCpInverseDesignOutput();
 
   /*!
    * \brief Set CP inverse design output field values (and also into the solver).
@@ -188,12 +188,12 @@ class CFlowOutput : public CFVMOutput{
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void Set_CpInverseDesign(CSolver *solver, const CGeometry *geometry, const CConfig *config);
+  void SetCpInverseDesign(CSolver *solver, const CGeometry *geometry, const CConfig *config);
 
   /*!
    * \brief Add nearfield inverse design output as history fields
    */
-  void Add_NearfieldInverseDesignOutput();
+  void AddNearfieldInverseDesignOutput();
 
   /*!
    * \brief Set nearfield inverse design output field values (and also into the solver).
@@ -201,7 +201,7 @@ class CFlowOutput : public CFVMOutput{
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void Set_NearfieldInverseDesign(CSolver *solver, const CGeometry *geometry, const CConfig *config);
+  void SetNearfieldInverseDesign(CSolver *solver, const CGeometry *geometry, const CConfig *config);
 
   /*!
    * \brief Compute the custom outputs.
@@ -223,7 +223,7 @@ class CFlowOutput : public CFVMOutput{
    * \return Value of the Q criteration at the node
    */
   template<class T>
-  su2double GetQ_Criterion(const T& VelocityGradient) const {
+  su2double GetQCriterion(const T& VelocityGradient) const {
 
     /*--- Make a 3D copy of the gradient so we do not have worry about nDim ---*/
 
@@ -296,8 +296,7 @@ class CFlowOutput : public CFVMOutput{
    * \param[in] force_writing - boolean that forces writing of volume output
    * \param[in] iFile - index to the file that we need to consider for volume output
    */
-  bool WriteVolume_Output(CConfig *config, unsigned long Iter, bool force_writing, unsigned short iFile) override;
-
+  bool WriteVolumeOutput(CConfig *config, unsigned long Iter, bool force_writing, unsigned short iFile) override; 
   /*!
    * \brief Write the forces breakdown file
    * \param[in] config - Definition of the particular problem per zone.
diff --git a/SU2_CFD/include/output/CMultizoneOutput.hpp b/SU2_CFD/include/output/CMultizoneOutput.hpp
index 920683b5455..abff2d28af1 100644
--- a/SU2_CFD/include/output/CMultizoneOutput.hpp
+++ b/SU2_CFD/include/output/CMultizoneOutput.hpp
@@ -80,17 +80,17 @@ class CMultizoneOutput final: public COutput {
    * \brief Determines if the history file output.
    * \param[in] config - Definition of the particular problem.
    */
-  bool WriteHistoryFile_Output(const CConfig *config) override;
+  bool WriteHistoryFileOutput(const CConfig *config) override ;
 
   /*!
    * \brief Determines if the screen header should be written.
    * \param[in] config - Definition of the particular problem.
    */
-  bool WriteScreen_Header(const CConfig *config) override;
+  bool WriteScreenHeader(const CConfig *config) override ;
 
   /*!
    * \brief Determines if the screen header should be written.
    * \param[in] config - Definition of the particular problem.
    */
-  bool WriteScreen_Output(const CConfig *config) override;
+  bool WriteScreenOutput(const CConfig *config) override ;
 };
diff --git a/SU2_CFD/include/output/CNEMOCompOutput.hpp b/SU2_CFD/include/output/CNEMOCompOutput.hpp
index 86700af74cb..248dc78ced2 100644
--- a/SU2_CFD/include/output/CNEMOCompOutput.hpp
+++ b/SU2_CFD/include/output/CNEMOCompOutput.hpp
@@ -79,7 +79,7 @@ class CNEMOCompOutput final: public CFlowOutput {
    * \param[in] config - Definition of the particular problem.
    * \return <TRUE> if the residuals should be initialized.
    */
-  bool SetInit_Residuals(const CConfig *config) override;
+  bool SetInitResiduals(const CConfig *config) override ;
 
   /*!
    * \brief Write any additional output defined for the current solver.
@@ -91,5 +91,5 @@ class CNEMOCompOutput final: public CFlowOutput {
    * \brief Determines if the history file output.
    * \param[in] config - Definition of the particular problem.
    */
-  bool WriteHistoryFile_Output(const CConfig *config) override;
+  bool WriteHistoryFileOutput(const CConfig *config) override ;
 };
diff --git a/SU2_CFD/include/output/COutput.hpp b/SU2_CFD/include/output/COutput.hpp
index 2dfe0683563..847ddc77f69 100644
--- a/SU2_CFD/include/output/COutput.hpp
+++ b/SU2_CFD/include/output/COutput.hpp
@@ -179,7 +179,7 @@ class COutput {
     std::vector<const su2double*> symbolValues;
     bool ready = false;
 
-    su2double eval() const {
+    su2double Eval() const {
       return mel::Eval<su2double>(expression, [&](int i) {return *symbolValues[i];});
     }
   };
@@ -227,7 +227,7 @@ class COutput {
      point. For example, it can be a wrapper to the primitives pointer, in which case varIndices needs to be setup
      with primitive indices. ---*/
     template <class Variables>
-    su2double eval(const Variables& vars) const {
+    su2double Eval(const Variables& vars) const {
       return mel::Eval<su2double>(expression, [&](int iSymbol) {return vars(varIndices[iSymbol]);});
     }
   };
@@ -342,7 +342,7 @@ class COutput {
    * \param[in] config - Definition of the particular problem.
    * \param[in] solver_container - The container holding all solution data.
    */
-  void Load_Data(CGeometry *geometry, CConfig *config, CSolver **solver_container);
+  void LoadData(CGeometry *geometry, CConfig *config, CSolver **solver_container);
 
   /*!
    * \brief Preprocess the history output by setting the history fields and opening the history file.
@@ -369,7 +369,7 @@ class COutput {
    * \param[in] OuterIter - Value of outer iteration index
    * \param[in] InnerIter - Value of the inner iteration index
    */
-  void SetHistory_Output(CGeometry *geometry, CSolver **solver_container, CConfig *config,
+  void SetHistoryOutput(CGeometry *geometry, CSolver **solver_container, CConfig *config,
                          unsigned long TimeIter, unsigned long OuterIter, unsigned long InnerIter);
 
   /*!
@@ -378,7 +378,7 @@ class COutput {
    * \param[in] solver_container - Container vector with all the solutions.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetHistory_Output(CGeometry *geometry, CSolver **solver_container, CConfig *config);
+  void SetHistoryOutput(CGeometry *geometry, CSolver **solver_container, CConfig *config);
 
   /*!
    *  Collects history data from the individual output per zone,
@@ -390,44 +390,44 @@ class COutput {
    * \param[in] TimeIter - Value of the time iteration index
    * \param[in] OuterIter - Value of outer iteration index
    */
-  void SetMultizoneHistory_Output(COutput** output, CConfig **config, CConfig *driver_config,
+  void SetMultizoneHistoryOutput(COutput** output, CConfig **config, CConfig *driver_config,
                                   unsigned long TimeIter, unsigned long OuterIter);
 
   /*!
    * \brief Sets the volume output filename
    * \param[in] filename - the new filename
    */
-  inline void SetVolume_Filename(string filename) {volumeFilename = filename;}
+  inline void SetVolumeFilename(string filename) {volumeFilename = filename;}
 
   /*!
    * \brief Sets the surface output filename
    * \param[in] filename - the new filename
    */
-  inline void SetSurface_Filename(string filename) {surfaceFilename = filename;}
+  inline void SetSurfaceFilename(string filename) {surfaceFilename = filename;}
 
   /*!
    * \brief Returns the current volume filename
    * \return - The current volume filename
    */
-  inline string GetVolume_Filename() {return volumeFilename;}
+  inline string GetVolumeFilename() {return volumeFilename;}
 
   /*!
    * \brief Returns the current surface filename
    * \return - The current surface filename
    */
-  inline string GetSurface_Filename() {return surfaceFilename;}
+  inline string GetSurfaceFilename() {return surfaceFilename;}
 
   /*!
    * \brief Sets the restart filename
    * \param[in] filename - the new filename
    */
-  inline void SetRestart_Filename(string filename) {restartFilename = filename;}
+  inline void SetRestartFilename(string filename) {restartFilename = filename;}
 
   /*!
    * \brief Returns the current restart filename
    * \return - The current restart filename
    */
-  inline string GetRestart_Filename() {return restartFilename;}
+  inline string GetRestartFilename() {return restartFilename;}
 
   /*!
    * \brief Set the current iteration indices
@@ -479,7 +479,7 @@ class COutput {
    * \brief Get the list of all output fields
    * \return Vector container all output fields
    */
-  const vector<string>& GetHistoryOutput_List() const {
+  const vector<string>& GetHistoryOutputList() const {
     return historyOutput_List;
   }
 
@@ -487,7 +487,7 @@ class COutput {
    * \brief Get the list of all per-surface fields
    * \return Vector container all output per-surface fields
    */
-  const vector<string>& GetHistoryOutputPerSurface_List() const {
+  const vector<string>& GetHistoryOutputPerSurfaceList() const {
     return historyOutputPerSurface_List;
   }
 
@@ -513,7 +513,7 @@ class COutput {
    * \param[in] Iteration - Index of the current iteration.
    * \return Boolean indicating whether the problem is converged.
    */
-  bool Convergence_Monitoring(CConfig *config, unsigned long Iteration);
+  bool ConvergenceMonitoring(CConfig *config, unsigned long Iteration);
 
   /*!
    * \brief Print a summary of the convergence to screen.
@@ -559,7 +559,7 @@ class COutput {
    * \param[in] force_writing - If <TRUE>, writing of output files is forced without checking the output frequency.
    * \return <TRUE> if output files have been written to disk.
    */
-  bool SetResult_Files(CGeometry *geometry, CConfig *config, CSolver** solver_container,
+  bool SetResultFiles(CGeometry *geometry, CConfig *config, CSolver** solver_container,
                        unsigned long iter, bool force_writing = false);
 
   /*!
@@ -588,25 +588,25 @@ class COutput {
    * \brief Set the history file header
    * \param[in] config - Definition of the particular problem.
    */
-  void SetHistoryFile_Header(const CConfig *config);
+  void SetHistoryFileHeader(const CConfig *config);
 
   /*!
    * \brief Write the history file output
    * \param[in] config - Definition of the particular problem.
    */
-  void SetHistoryFile_Output(const CConfig *config);
+  void SetHistoryFileOutput(const CConfig *config);
 
   /*!
    * \brief Write the screen header.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetScreen_Header(const CConfig *config);
+  void SetScreenHeader(const CConfig *config);
 
   /*!
    * \brief Write the screen output.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetScreen_Output(const CConfig *config);
+  void SetScreenOutput(const CConfig *config);
 
   /*!
    * \brief Add a new field to the history output.
@@ -765,13 +765,13 @@ class COutput {
    * \brief Postprocess_HistoryData
    * \param[in] config - Definition of the particular problem.
    */
-  void Postprocess_HistoryData(CConfig *config);
+  void PostprocessHistoryData(CConfig *config);
 
   /*!
    * \brief Postprocess_HistoryFields
    * \param[in] config - Definition of the particular problem.
    */
-  void Postprocess_HistoryFields(CConfig *config);
+  void PostprocessHistoryFields(CConfig *config);
 
   /*!
    * \brief Check whether we should print output.
@@ -838,19 +838,19 @@ class COutput {
    * \brief Determines if the history file output.
    * \param[in] config - Definition of the particular problem.
    */
-  virtual bool WriteHistoryFile_Output(const CConfig *config);
+  virtual bool WriteHistoryFileOutput(const CConfig *config);
 
   /*!
    * \brief Determines if the screen header should be written.
    * \param[in] config - Definition of the particular problem.
    */
-  virtual bool WriteScreen_Header(const CConfig *config);
+  virtual bool WriteScreenHeader(const CConfig *config);
 
   /*!
    * \brief Determines if the screen header should be written.
    * \param[in] config - Definition of the particular problem.
    */
-  virtual bool WriteScreen_Output(const CConfig *config);
+  virtual bool WriteScreenOutput(const CConfig *config);
 
   /*!
    * \brief Determines if the the volume output should be written.
@@ -859,7 +859,7 @@ class COutput {
    * \param[in] force_writing - boolean that forces writing of volume output
    * \param[in] iFile - index to the file that we need to consider for volume output
    */
-  virtual bool WriteVolume_Output(CConfig *config, unsigned long Iter, bool force_writing, unsigned short iFile);
+  virtual bool WriteVolumeOutput(CConfig *config, unsigned long Iter, bool force_writing, unsigned short iFile);
 
   /*!
    * \brief Set the values of the volume output fields for a point.
@@ -887,7 +887,7 @@ class COutput {
    * \param[in] config - Definition of the particular problem.
    * \return <TRUE> if the residuals should be initialized.
    */
-  inline virtual bool SetInit_Residuals(const CConfig *config) {return false;}
+  inline virtual bool SetInitResiduals(const CConfig *config) {return false;}
 
   /*!
    * \brief Set the values of the volume output fields for a surface point.
diff --git a/SU2_CFD/include/output/COutputLegacy.hpp b/SU2_CFD/include/output/COutputLegacy.hpp
index d3ee97c6251..a1b413a95ee 100644
--- a/SU2_CFD/include/output/COutputLegacy.hpp
+++ b/SU2_CFD/include/output/COutputLegacy.hpp
@@ -134,7 +134,7 @@ class COutputLegacy {
    * \param[in] config - Definition of the particular problem.
    * \param[in] iExtIter - Current external (time) iteration.
    */
-  void SetCp_InverseDesign(CSolver *solver_container, CGeometry *geometry, CConfig *config,
+  void SetCpInverseDesign(CSolver *solver_container, CGeometry *geometry, CConfig *config,
                          unsigned long iExtIter);
 
   /*!
@@ -144,7 +144,7 @@ class COutputLegacy {
    * \param[in] config - Definition of the particular problem.
    * \param[in] iExtIter - Current external (time) iteration.
    */
-  void SetHeatFlux_InverseDesign(CSolver *solver_container, CGeometry *geometry, CConfig *config,
+  void SetHeatFluxInverseDesign(CSolver *solver_container, CGeometry *geometry, CConfig *config,
                         unsigned long iExtIter);
 
   /*!
@@ -154,7 +154,7 @@ class COutputLegacy {
    * \param[in] config - Definition of the particular problem.
    * \param[in] output - Create output files.
    */
-  void SpecialOutput_SpanLoad(CSolver *solver, CGeometry *geometry, CConfig *config, bool output) const;
+  void SpecialOutputSpanLoad(CSolver *solver, CGeometry *geometry, CConfig *config, bool output) const;
 
   /*!
    * \brief Writes one dimensional output.
@@ -164,7 +164,7 @@ class COutputLegacy {
    * \param[in] config - Definition of the particular problem.
    * \param[in] output - Create output files.
    */
-  void SpecialOutput_AnalyzeSurface(CSolver *solver, CGeometry *geometry, CConfig *config, bool output) const;
+  void SpecialOutputAnalyzeSurface(CSolver *solver, CGeometry *geometry, CConfig *config, bool output) const;
 
   /*!
    * \brief Create and write the file with the flow coefficient on the surface.
@@ -175,14 +175,14 @@ class COutputLegacy {
    * \param[in] val_iZone - Current zone number in the grid file.
    * \param[in] output - Create output files.
    */
-  void SpecialOutput_Distortion(CSolver *solver, CGeometry *geometry, CConfig *config, bool output) const;
+  void SpecialOutputDistortion(CSolver *solver, CGeometry *geometry, CConfig *config, bool output) const;
 
   /*!
    * \brief Write the header of the history file.
    * \param[in] ConvHist_file - Pointer to the convergence history file (which is defined in the main subroutine).
    * \param[in] config - Definition of the particular problem.
    */
-  void SetConvHistory_Header(ofstream *ConvHist_file, CConfig *config, unsigned short val_iZone, unsigned short val_iInst);
+  void SetConvHistoryHeader(ofstream *ConvHist_file, CConfig *config, unsigned short val_iZone, unsigned short val_iInst);
 
   /*!
    * \brief Write the history file and the convergence on the screen for serial computations.
@@ -195,7 +195,7 @@ class COutputLegacy {
    * \param[in] timeused - Current number of clock tick in the computation (related with total time).
    * \param[in] val_nZone - iZone index.
    */
-  void SetConvHistory_Body(ofstream *ConvHist_file, CGeometry ****geometry, CSolver *****solver_container, CConfig **config,
+  void SetConvHistoryBody(ofstream *ConvHist_file, CGeometry ****geometry, CSolver *****solver_container, CConfig **config,
                               CIntegration ****integration, bool DualTime, su2double timeused, unsigned short val_iZone, unsigned short val_iInst);
 
   /*!
@@ -205,7 +205,7 @@ class COutputLegacy {
    * \param[in] config - Definition of the particular problem.
    * \param[in] output - Create output files.
    */
-  void SpecialOutput_ForcesBreakdown(CSolver *****solver, CGeometry ****geometry, CConfig **config, unsigned short val_iZone, bool output) const;
+  void SpecialOutputForcesBreakdown(CSolver *****solver, CGeometry ****geometry, CConfig **config, unsigned short val_iZone, bool output) const;
 
   /*!
    * \brief Compute .
@@ -230,7 +230,7 @@ class COutputLegacy {
    * \param[in] val_nZone - iZone index.
    * \param[in] output - Create output files.
    */
-  void SpecialOutput_Turbo(CSolver *****solver_container, CGeometry ****geometry, CConfig **config, unsigned short val_iZone, bool output);
+  void SpecialOutputTurbo(CSolver *****solver_container, CGeometry ****geometry, CConfig **config, unsigned short val_iZone, bool output);
 
   /*!
    * \brief Give the Entropy Generation performance parameters for turbomachinery.
@@ -261,7 +261,7 @@ class COutputLegacy {
    * \param[in] val_iZone - Zone index.
    * \param[in] output - Create output files.
    */
-  void SpecialOutput_HarmonicBalance(CSolver *****solver, CGeometry ****geometry, CConfig **config, unsigned short iZone, unsigned short val_nZone, bool output) const;
+  void SpecialOutputHarmonicBalance(CSolver *****solver, CGeometry ****geometry, CConfig **config, unsigned short iZone, unsigned short val_nZone, bool output) const;
 
   /*!
    * \brief Writes the special output files.
@@ -272,7 +272,7 @@ class COutputLegacy {
    * \param[in] val_iZone - Total number of domains in the grid file.
    * \param[in] val_nZone - Total number of domains in the grid file.
    */
-  void SetSpecial_Output(CSolver *****solver_container, CGeometry ****geometry, CConfig **config,
+  void SetSpecialOutput(CSolver *****solver_container, CGeometry ****geometry, CConfig **config,
                          unsigned long iExtIter, unsigned short val_nZone);
 
 };
diff --git a/SU2_CFD/include/output/filewriter/CCGNSFileWriter.hpp b/SU2_CFD/include/output/filewriter/CCGNSFileWriter.hpp
index e31a81ea60c..d0ac4fd10cb 100644
--- a/SU2_CFD/include/output/filewriter/CCGNSFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CCGNSFileWriter.hpp
@@ -81,7 +81,7 @@ class CCGNSFileWriter final : public CFileWriter {
    * \brief Write sorted data to file in CGNS file format.
    * \param[in] val_filename - The name of the file.
    */
-  void Write_Data(string val_filename) override;
+  void WriteData(string val_filename) override ;
 
  private:
 #ifdef HAVE_CGNS
diff --git a/SU2_CFD/include/output/filewriter/CCSVFileWriter.hpp b/SU2_CFD/include/output/filewriter/CCSVFileWriter.hpp
index 9cdd7ad57f6..5858632e7e0 100644
--- a/SU2_CFD/include/output/filewriter/CCSVFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CCSVFileWriter.hpp
@@ -54,7 +54,7 @@ class CCSVFileWriter final: public CFileWriter{
    * \brief Write sorted data to file in CSV file format
    * \param[in] val_filename - The name of the file
    */
-  void Write_Data(string val_filename) override;
+  void WriteData(string val_filename) override ;
 
 };
 
diff --git a/SU2_CFD/include/output/filewriter/CFileWriter.hpp b/SU2_CFD/include/output/filewriter/CFileWriter.hpp
index 9ff8b88593e..fa551311791 100644
--- a/SU2_CFD/include/output/filewriter/CFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CFileWriter.hpp
@@ -67,7 +67,7 @@ class CFileWriter{
    * \param[in] filename - Name of the file.
    * \return
    */
-  inline unsigned long Determine_Filesize(std::string filename){
+  inline unsigned long DetermineFilesize(std::string filename){
       struct stat stat_buf;
       int rc = stat(filename.c_str(), &stat_buf);
       return rc == 0 ? stat_buf.st_size : -1;
@@ -119,23 +119,23 @@ class CFileWriter{
    * \brief Write sorted data to file
    * \param[in] val_filename - The name of the file
    */
-  virtual void Write_Data(string val_filename){}
+  virtual void WriteData(string val_filename){}
 
   /*!
    * \brief Get the bandwith used for the last writing
    */
-  su2double Get_Bandwidth() const {return bandwidth;}
+  su2double GetBandwidth() const {return bandwidth;}
 
   /*!
    * \brief Get the filesize of the last written file.
    */
-  su2double Get_Filesize() const {return fileSize;}
+  su2double GetFilesize() const {return fileSize;}
 
   /*!
    * \brief Get the used time of the last file writing.
    * \return The time used to write to file.
    */
-  su2double Get_UsedTime() const {return usedTime;}
+  su2double GetUsedTime() const {return usedTime;}
 
 protected:
 
diff --git a/SU2_CFD/include/output/filewriter/CParallelDataSorter.hpp b/SU2_CFD/include/output/filewriter/CParallelDataSorter.hpp
index 6b82833ae5c..d9a4f0ba7ff 100644
--- a/SU2_CFD/include/output/filewriter/CParallelDataSorter.hpp
+++ b/SU2_CFD/include/output/filewriter/CParallelDataSorter.hpp
@@ -246,7 +246,7 @@ class CParallelDataSorter{
    * \input iNode - The node ID
    * \return the connected node.
    */
-  unsigned long GetElem_Connectivity(GEO_TYPE type, unsigned long iElem, unsigned long iNode) const ;
+  unsigned long GetElemConnectivity(GEO_TYPE type, unsigned long iElem, unsigned long iNode) const ;
 
   /*!
    * \brief Beginning node ID of the linear partition owned by a specific processor.
@@ -315,11 +315,11 @@ class CParallelDataSorter{
    * \param[in] iField - Index of the field
    * \param[in] data - Value of the field
    */
-  void SetUnsorted_Data(unsigned long iPoint, unsigned short iField, su2double data){
+  void SetUnsortedData(unsigned long iPoint, unsigned short iField, su2double data){
     connSend[Index[iPoint] + iField] = SU2_TYPE::GetValue(data);
   }
 
-  passivedouble GetUnsorted_Data(unsigned long iPoint, unsigned short iField) const {
+  passivedouble GetUnsortedData(unsigned long iPoint, unsigned short iField) const {
     return connSend[Index[iPoint] + iField];
   }
 
diff --git a/SU2_CFD/include/output/filewriter/CParaviewBinaryFileWriter.hpp b/SU2_CFD/include/output/filewriter/CParaviewBinaryFileWriter.hpp
index 1e7680d8763..bf3e93e8879 100644
--- a/SU2_CFD/include/output/filewriter/CParaviewBinaryFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CParaviewBinaryFileWriter.hpp
@@ -59,7 +59,7 @@ class CParaviewBinaryFileWriter final: public CFileWriter{
    * \brief Write sorted data to file in paraview binary file format
    * \param[in] val_filename - The name of the file
    */
-  void Write_Data(string val_filename) override;
+  void WriteData(string val_filename) override ;
 
 private:
 
diff --git a/SU2_CFD/include/output/filewriter/CParaviewFileWriter.hpp b/SU2_CFD/include/output/filewriter/CParaviewFileWriter.hpp
index e09b2c37c8f..736812abf88 100644
--- a/SU2_CFD/include/output/filewriter/CParaviewFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CParaviewFileWriter.hpp
@@ -52,7 +52,7 @@ class CParaviewFileWriter final: public CFileWriter{
    * \brief Write sorted data to file in paraview file format
    * \param[in] val_filename - The name of the file
    */
-  void Write_Data(string val_filename) override;
+  void WriteData(string val_filename) override ;
 
 };
 
diff --git a/SU2_CFD/include/output/filewriter/CParaviewVTMFileWriter.hpp b/SU2_CFD/include/output/filewriter/CParaviewVTMFileWriter.hpp
index 86b8cfe2350..6804b55651d 100644
--- a/SU2_CFD/include/output/filewriter/CParaviewVTMFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CParaviewVTMFileWriter.hpp
@@ -99,7 +99,7 @@ class CParaviewVTMFileWriter final: public CFileWriter{
    * \brief Write sorted data to file in paraview binary file format
    * \param[in] val_filename - The name of the file
    */
-  void Write_Data(string val_filename) override;
+  void WriteData(string val_filename) override ;
 
     /*!
    * \brief Write all data of the zones, boundaries into the folder
diff --git a/SU2_CFD/include/output/filewriter/CParaviewXMLFileWriter.hpp b/SU2_CFD/include/output/filewriter/CParaviewXMLFileWriter.hpp
index ea0546bd97f..ab2368defd8 100644
--- a/SU2_CFD/include/output/filewriter/CParaviewXMLFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CParaviewXMLFileWriter.hpp
@@ -80,7 +80,7 @@ class CParaviewXMLFileWriter final: public CFileWriter{
   /*!
    * \brief Write sorted data to file in paraview binary file format
    */
-  void Write_Data(string val_filename) override;
+  void WriteData(string val_filename) override ;
 
 private:
 
diff --git a/SU2_CFD/include/output/filewriter/CSTLFileWriter.hpp b/SU2_CFD/include/output/filewriter/CSTLFileWriter.hpp
index 53029423523..5c639dfe241 100644
--- a/SU2_CFD/include/output/filewriter/CSTLFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CSTLFileWriter.hpp
@@ -115,7 +115,7 @@ class CSTLFileWriter final : public CFileWriter{
    * \brief Write sorted data to file in STL file format
    * \param[in] val_filename - The name of the file
    */
-  void Write_Data(string val_filename) override;
+  void WriteData(string val_filename) override ;
 
 };
 
diff --git a/SU2_CFD/include/output/filewriter/CSU2BinaryFileWriter.hpp b/SU2_CFD/include/output/filewriter/CSU2BinaryFileWriter.hpp
index 19f95172ec2..988da36bbc0 100644
--- a/SU2_CFD/include/output/filewriter/CSU2BinaryFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CSU2BinaryFileWriter.hpp
@@ -53,6 +53,6 @@ class CSU2BinaryFileWriter final: public CFileWriter{
    * \brief Write sorted data to file in SU2 binary file format
    * \param[in] filename - The filename to write
    */
-  void Write_Data(string filename) override;
+  void WriteData(string filename) override ;
 
 };
diff --git a/SU2_CFD/include/output/filewriter/CSU2FileWriter.hpp b/SU2_CFD/include/output/filewriter/CSU2FileWriter.hpp
index c7ae345e9ac..b3edb0ff0bf 100644
--- a/SU2_CFD/include/output/filewriter/CSU2FileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CSU2FileWriter.hpp
@@ -47,7 +47,7 @@ class CSU2FileWriter final: public CFileWriter{
    * \brief Write sorted data to file in SU2 ASCII file format
    * \param[in] val_filename - The name of the file
    */
-  void Write_Data(string val_filename) override;
+  void WriteData(string val_filename) override ;
 
 };
 
diff --git a/SU2_CFD/include/output/filewriter/CSU2MeshFileWriter.hpp b/SU2_CFD/include/output/filewriter/CSU2MeshFileWriter.hpp
index 1a2ff43f252..3967be09a28 100644
--- a/SU2_CFD/include/output/filewriter/CSU2MeshFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CSU2MeshFileWriter.hpp
@@ -53,7 +53,7 @@ class CSU2MeshFileWriter final: public CFileWriter{
    * \brief Write sorted data to file in SU2 mesh file format
    * \param[in] val_filename - The name of the file
    */
-  void Write_Data(string val_filename) override;
+  void WriteData(string val_filename) override ;
 
 };
 
diff --git a/SU2_CFD/include/output/filewriter/CTecplotBinaryFileWriter.hpp b/SU2_CFD/include/output/filewriter/CTecplotBinaryFileWriter.hpp
index 2975cd2c727..532b7728fb5 100644
--- a/SU2_CFD/include/output/filewriter/CTecplotBinaryFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CTecplotBinaryFileWriter.hpp
@@ -61,7 +61,7 @@ class CTecplotBinaryFileWriter final: public CFileWriter{
    * \brief Write sorted data to file in tecplot binary file format
    * \param[in] val_filename - The name of the file
    */
-  void Write_Data(string val_filename) override;
+  void WriteData(string val_filename) override ;
 
   /*!
    * \brief Calculate the partitioning of nodes to determine:
diff --git a/SU2_CFD/include/output/filewriter/CTecplotFileWriter.hpp b/SU2_CFD/include/output/filewriter/CTecplotFileWriter.hpp
index 1c9a49b0ac1..92f2f729772 100644
--- a/SU2_CFD/include/output/filewriter/CTecplotFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CTecplotFileWriter.hpp
@@ -58,7 +58,7 @@ class CTecplotFileWriter final: public CFileWriter{
    * \brief Write sorted data to file in tecplot ASCII file format
    * \param[in] val_filename - The name of the file
    */
-  void Write_Data(string val_filename) override;
+  void WriteData(string val_filename) override ;
 
 };
 
diff --git a/SU2_CFD/include/output/tools/CWindowingTools.hpp b/SU2_CFD/include/output/tools/CWindowingTools.hpp
index 5fc3e22fc3c..9a6a2e67b65 100644
--- a/SU2_CFD/include/output/tools/CWindowingTools.hpp
+++ b/SU2_CFD/include/output/tools/CWindowingTools.hpp
@@ -105,7 +105,7 @@ class CWindowedAverage:CWindowingTools{
    * \param currentIter - current time Iteration
    * \param startIter - iteration to start the windowed-time average.
    */
-  void addValue(su2double valIn, unsigned long curTimeIter,unsigned long startIter = 0);
+  void AddValue(su2double valIn, unsigned long curTimeIter,unsigned long startIter = 0);
 
 private:
   /*!
diff --git a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
index 882e8a8e0d8..0964cc32a66 100644
--- a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
@@ -436,7 +436,7 @@ void CDiscAdjMultizoneDriver::Run() {
 
     /*--- Set the multizone output. ---*/
 
-    driver_output->SetMultizoneHistory_Output(output_container, config_container, driver_config, TimeIter, iOuterIter);
+    driver_output->SetMultizoneHistoryOutput(output_container, config_container, driver_config, TimeIter, iOuterIter);
 
     /*--- Check for convergence. ---*/
 
@@ -729,19 +729,19 @@ void CDiscAdjMultizoneDriver::SetObjFunction(RECORDING kind_recording) {
           solvers[HEAT_SOL]->Heat_Fluxes(geometry, solvers, config);
         }
 
-        direct_output[iZone]->SetHistory_Output(geometry, solvers, config);
+        direct_output[iZone]->SetHistoryOutput(geometry, solvers, config);
         ObjFunc += solvers[FLOW_SOL]->GetTotal_ComboObj();
         break;
 
       case MAIN_SOLVER::DISC_ADJ_HEAT:
         solvers[HEAT_SOL]->Heat_Fluxes(geometry, solvers, config);
-        direct_output[iZone]->SetHistory_Output(geometry, solvers, config);
+        direct_output[iZone]->SetHistoryOutput(geometry, solvers, config);
         ObjFunc += solvers[HEAT_SOL]->GetTotal_ComboObj();
         break;
 
       case MAIN_SOLVER::DISC_ADJ_FEM:
         solvers[FEA_SOL]->Postprocessing(geometry, config, numerics_container[iZone][INST_0][MESH_0][FEA_SOL], true);
-        direct_output[iZone]->SetHistory_Output(geometry, solvers, config);
+        direct_output[iZone]->SetHistoryOutput(geometry, solvers, config);
         ObjFunc += solvers[FEA_SOL]->GetTotal_ComboObj();
         break;
 
diff --git a/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
index ef4e4e690d0..8379d50cba5 100644
--- a/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
@@ -357,7 +357,7 @@ void CDiscAdjSinglezoneDriver::SetObjFunction(){
 
     /*--- Surface based obj. function ---*/
 
-    direct_output->SetHistory_Output(geometry, solver, config, config->GetTimeIter(),
+    direct_output->SetHistoryOutput(geometry, solver, config, config->GetTimeIter(),
                                      config->GetOuterIter(), config->GetInnerIter());
     ObjFunc += solver[FLOW_SOL]->GetTotal_ComboObj();
 
@@ -386,7 +386,7 @@ void CDiscAdjSinglezoneDriver::SetObjFunction(){
     break;
 
   case MAIN_SOLVER::DISC_ADJ_HEAT:
-    direct_output->SetHistory_Output(geometry, solver, config, config->GetTimeIter(),
+    direct_output->SetHistoryOutput(geometry, solver, config, config->GetTimeIter(),
                                      config->GetOuterIter(), config->GetInnerIter());
     ObjFunc = solver[HEAT_SOL]->GetTotal_ComboObj();
     break;
@@ -394,7 +394,7 @@ void CDiscAdjSinglezoneDriver::SetObjFunction(){
   case MAIN_SOLVER::DISC_ADJ_FEM:
     solver[FEA_SOL]->Postprocessing(geometry, config, numerics_container[ZONE_0][INST_0][MESH_0][FEA_SOL], true);
 
-    direct_output->SetHistory_Output(geometry, solver, config, config->GetTimeIter(),
+    direct_output->SetHistoryOutput(geometry, solver, config, config->GetTimeIter(),
                                    config->GetOuterIter(), config->GetInnerIter());
     ObjFunc = solver[FEA_SOL]->GetTotal_ComboObj();
     break;
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index a5881a197de..8e70c3149f1 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -3191,7 +3191,7 @@ void CFluidDriver::Output(unsigned long InnerIter) {
 
     for (iInst = 0; iInst < nInst[iZone]; ++iInst) {
       config_container[iZone]->SetiInst(iInst);
-      output_container[iZone]->SetResult_Files(geometry_container[iZone][iInst][MESH_0],
+      output_container[iZone]->SetResultFiles(geometry_container[iZone][iInst][MESH_0],
                                                config_container[iZone],
                                                solver_container[iZone][iInst][MESH_0],
                                                InnerIter, StopCalc);
@@ -3218,7 +3218,7 @@ CTurbomachineryDriver::CTurbomachineryDriver(char* confFile, unsigned short val_
     if (rank == MASTER_NODE){
       ConvHist_file[iZone] = new ofstream[nInst[iZone]];
       for (iInst = 0; iInst < nInst[iZone]; iInst++) {
-        output_legacy->SetConvHistory_Header(&ConvHist_file[iZone][iInst], config_container[iZone], iZone, iInst);
+        output_legacy->SetConvHistoryHeader(&ConvHist_file[iZone][iInst], config_container[iZone], iZone, iInst);
       }
     }
   }
@@ -3340,7 +3340,7 @@ bool CTurbomachineryDriver::Monitor(unsigned long ExtIter) {
 
   for (iZone = 0; iZone < nZone; iZone++) {
     for (iInst = 0; iInst < nInst[iZone]; iInst++)
-      output_legacy->SetConvHistory_Body(&ConvHist_file[iZone][iInst], geometry_container, solver_container,
+      output_legacy->SetConvHistoryBody(&ConvHist_file[iZone][iInst], geometry_container, solver_container,
           config_container, integration_container, false, UsedTime, iZone, iInst);
   }
 
@@ -3467,7 +3467,7 @@ CHBDriver::CHBDriver(char* confFile,
     if (rank == MASTER_NODE){
       ConvHist_file[iZone] = new ofstream[nInst[iZone]];
       for (iInst = 0; iInst < nInst[iZone]; iInst++) {
-        output_legacy->SetConvHistory_Header(&ConvHist_file[iZone][iInst], config_container[iZone], iZone, iInst);
+        output_legacy->SetConvHistoryHeader(&ConvHist_file[iZone][iInst], config_container[iZone], iZone, iInst);
       }
     }
   }
@@ -3515,7 +3515,7 @@ void CHBDriver::Run() {
 
   for (iZone = 0; iZone < nZone; iZone++) {
     for (iInst = 0; iInst < nInst[iZone]; iInst++)
-      output_legacy->SetConvHistory_Body(&ConvHist_file[iZone][iInst], geometry_container, solver_container,
+      output_legacy->SetConvHistoryBody(&ConvHist_file[iZone][iInst], geometry_container, solver_container,
           config_container, integration_container, false, UsedTime, iZone, iInst);
   }
 
diff --git a/SU2_CFD/src/drivers/CMultizoneDriver.cpp b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
index 99c64c233f5..cd3b3c9dcb4 100644
--- a/SU2_CFD/src/drivers/CMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
@@ -409,13 +409,13 @@ bool CMultizoneDriver::OuterConvergence(unsigned long OuterIter) {
 
     /*--- Make sure that everything is loaded into the output container. ---*/
 
-    output_container[iZone]->SetHistory_Output(geometry_container[iZone][INST_0][MESH_0], solvers, config_container[iZone]);
+    output_container[iZone]->SetHistoryOutput(geometry_container[iZone][INST_0][MESH_0], solvers, config_container[iZone]);
 
   }
 
   /*--- Print out the convergence data to screen and history file. ---*/
 
-  driver_output->SetMultizoneHistory_Output(output_container, config_container, driver_config,
+  driver_output->SetMultizoneHistoryOutput(output_container, config_container, driver_config,
                                             driver_config->GetTimeIter(), driver_config->GetOuterIter());
 
   return driver_output->GetConvergence();
@@ -467,7 +467,7 @@ void CMultizoneDriver::Output(unsigned long TimeIter) {
   bool wrote_files = false;
 
   for (iZone = 0; iZone < nZone; iZone++){
-    wrote_files = output_container[iZone]->SetResult_Files(geometry_container[iZone][INST_0][MESH_0],
+    wrote_files = output_container[iZone]->SetResultFiles(geometry_container[iZone][INST_0][MESH_0],
                                                             config_container[iZone],
                                                             solver_container[iZone][INST_0][MESH_0], TimeIter, StopCalc );
   }
diff --git a/SU2_CFD/src/drivers/CSinglezoneDriver.cpp b/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
index fe4bd854e1a..898e5712831 100644
--- a/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
@@ -199,7 +199,7 @@ void CSinglezoneDriver::Output(unsigned long TimeIter) {
 
   StartTime = SU2_MPI::Wtime();
 
-  bool wrote_files = output_container[ZONE_0]->SetResult_Files(geometry_container[ZONE_0][INST_0][MESH_0],
+  bool wrote_files = output_container[ZONE_0]->SetResultFiles(geometry_container[ZONE_0][INST_0][MESH_0],
                                                                config_container[ZONE_0],
                                                                solver_container[ZONE_0][INST_0][MESH_0],
                                                                TimeIter, StopCalc);
diff --git a/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
index 83090a045fb..99536c54ae5 100644
--- a/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
@@ -309,7 +309,7 @@ bool CDiscAdjFEAIteration::Monitor(COutput* output, CIntegration**** integration
                                    CFreeFormDefBox*** FFDBox, unsigned short iZone, unsigned short iInst) {
   /*--- Write the convergence history (only screen output) ---*/
 
-  output->SetHistory_Output(geometry[iZone][INST_0][MESH_0], solver[iZone][INST_0][MESH_0], config[iZone],
+  output->SetHistoryOutput(geometry[iZone][INST_0][MESH_0], solver[iZone][INST_0][MESH_0], config[iZone],
                             config[iZone]->GetTimeIter(), config[iZone]->GetOuterIter(),
                             config[iZone]->GetInnerIter());
 
diff --git a/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
index 2776d3c19ab..34cc6a94e7c 100644
--- a/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
@@ -633,7 +633,7 @@ bool CDiscAdjFluidIteration::Monitor(COutput* output, CIntegration**** integrati
 
   /*--- Write the convergence history for the fluid (only screen output) ---*/
 
-  output->SetHistory_Output(geometry[iZone][INST_0][MESH_0], solver[iZone][INST_0][MESH_0], config[iZone],
+  output->SetHistoryOutput(geometry[iZone][INST_0][MESH_0], solver[iZone][INST_0][MESH_0], config[iZone],
                             config[iZone]->GetTimeIter(), config[iZone]->GetOuterIter(),
                             config[iZone]->GetInnerIter());
 
diff --git a/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
index 67c2f8fe863..572ea54c49e 100644
--- a/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
@@ -252,7 +252,7 @@ bool CDiscAdjHeatIteration::Monitor(COutput* output, CIntegration**** integratio
                                     CSurfaceMovement** surface_movement, CVolumetricMovement*** grid_movement,
                                     CFreeFormDefBox*** FFDBox, unsigned short val_iZone, unsigned short val_iInst) {
 
-  output->SetHistory_Output(geometry[val_iZone][INST_0][MESH_0], solver[val_iZone][INST_0][MESH_0], config[val_iZone],
+  output->SetHistoryOutput(geometry[val_iZone][INST_0][MESH_0], solver[val_iZone][INST_0][MESH_0], config[val_iZone],
                             config[val_iZone]->GetTimeIter(), config[val_iZone]->GetOuterIter(),
                             config[val_iZone]->GetInnerIter());
 
diff --git a/SU2_CFD/src/iteration/CFEAIteration.cpp b/SU2_CFD/src/iteration/CFEAIteration.cpp
index 2f560f05cf8..45ded06c7ee 100644
--- a/SU2_CFD/src/iteration/CFEAIteration.cpp
+++ b/SU2_CFD/src/iteration/CFEAIteration.cpp
@@ -253,7 +253,7 @@ bool CFEAIteration::Monitor(COutput* output, CIntegration**** integration, CGeom
   UsedTime = StopTime - StartTime;
 
   if (config[val_iZone]->GetMultizone_Problem() || config[val_iZone]->GetSinglezone_Driver()) {
-    output->SetHistory_Output(geometry[val_iZone][val_iInst][MESH_0], solver[val_iZone][val_iInst][MESH_0],
+    output->SetHistoryOutput(geometry[val_iZone][val_iInst][MESH_0], solver[val_iZone][val_iInst][MESH_0],
                               config[val_iZone], config[val_iZone]->GetTimeIter(), config[val_iZone]->GetOuterIter(),
                               config[val_iZone]->GetInnerIter());
   }
diff --git a/SU2_CFD/src/iteration/CFluidIteration.cpp b/SU2_CFD/src/iteration/CFluidIteration.cpp
index db7a7a18be4..db2192f6442 100644
--- a/SU2_CFD/src/iteration/CFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CFluidIteration.cpp
@@ -219,7 +219,7 @@ bool CFluidIteration::Monitor(COutput* output, CIntegration**** integration, CGe
   UsedTime = StopTime - StartTime;
 
   if (config[val_iZone]->GetMultizone_Problem() || config[val_iZone]->GetSinglezone_Driver()) {
-    output->SetHistory_Output(geometry[val_iZone][INST_0][MESH_0], solver[val_iZone][INST_0][MESH_0], config[val_iZone],
+    output->SetHistoryOutput(geometry[val_iZone][INST_0][MESH_0], solver[val_iZone][INST_0][MESH_0], config[val_iZone],
                               config[val_iZone]->GetTimeIter(), config[val_iZone]->GetOuterIter(),
                               config[val_iZone]->GetInnerIter());
   }
@@ -541,7 +541,7 @@ bool CFluidIteration::MonitorFixed_CL(COutput *output, CGeometry *geometry, CSol
     /* --- Print convergence history and volume files since fixed CL mode has converged--- */
     if (rank == MASTER_NODE) output->PrintConvergenceSummary();
 
-    output->SetResult_Files(geometry, config, solver,
+    output->SetResultFiles(geometry, config, solver,
                             config->GetInnerIter(), true);
 
     /* --- Set finite difference mode in config (disables output) --- */
diff --git a/SU2_CFD/src/iteration/CIteration.cpp b/SU2_CFD/src/iteration/CIteration.cpp
index 5b2eaa5cef1..940df64be07 100644
--- a/SU2_CFD/src/iteration/CIteration.cpp
+++ b/SU2_CFD/src/iteration/CIteration.cpp
@@ -175,6 +175,6 @@ void CIteration::SetMesh_Deformation(CGeometry** geometry, CSolver** solver, CNu
 
 void CIteration::Output(COutput* output, CGeometry**** geometry, CSolver***** solver, CConfig** config,
                         unsigned long InnerIter, bool StopCalc, unsigned short val_iZone, unsigned short val_iInst) {
-  output->SetResult_Files(geometry[val_iZone][INST_0][MESH_0], config[val_iZone], solver[val_iZone][INST_0][MESH_0],
+  output->SetResultFiles(geometry[val_iZone][INST_0][MESH_0], config[val_iZone], solver[val_iZone][INST_0][MESH_0],
                           InnerIter);
 }
diff --git a/SU2_CFD/src/output/CAdjFlowCompOutput.cpp b/SU2_CFD/src/output/CAdjFlowCompOutput.cpp
index 3125e783b47..cac0326c221 100644
--- a/SU2_CFD/src/output/CAdjFlowCompOutput.cpp
+++ b/SU2_CFD/src/output/CAdjFlowCompOutput.cpp
@@ -164,7 +164,7 @@ void CAdjFlowCompOutput::SetHistoryOutputFields(CConfig *config) {
   AddHistoryOutput("LINSOL_ITER", "LinSolIter", ScreenOutputFormat::INTEGER, "LINSOL", "Number of iterations of the linear solver.");
   AddHistoryOutput("LINSOL_RESIDUAL", "LinSolRes", ScreenOutputFormat::FIXED, "LINSOL", "Residual of the linear solver.");
 
-  AddHistoryOutputFields_AdjScalarLinsol(config);
+  AddHistoryOutputFieldsAdjScalarLinsol(config);
 
   if (config->GetDeform_Mesh()) {
     AddHistoryOutput("DEFORM_ITER", "DeformIter", ScreenOutputFormat::INTEGER, "DEFORM", "Linear solver iterations for the mesh deformation");
@@ -224,7 +224,7 @@ void CAdjFlowCompOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, C
     SetHistoryOutputValue("DEFORM_RESIDUAL", log10(mesh_solver->System.GetResidual()));
   }
 
-  LoadHistoryData_AdjScalar(config, solver);
+  LoadHistoryDataAdjScalar(config, solver);
 }
 
 void CAdjFlowCompOutput::SetVolumeOutputFields(CConfig *config) {
@@ -248,7 +248,7 @@ void CAdjFlowCompOutput::SetVolumeOutputFields(CConfig *config) {
   /// DESCRIPTION: Adjoint energy.
   AddVolumeOutput("ADJ_ENERGY", "Adjoint_Energy", "SOLUTION", "Adjoint energy");
 
-  SetVolumeOutputFields_AdjScalarSolution(config);
+  SetVolumeOutputFieldsAdjScalarSolution(config);
   /// END_GROUP
 
   /// BEGIN_GROUP: RESIDUAL, DESCRIPTION: Residuals of the SOLUTION variables.
@@ -264,7 +264,7 @@ void CAdjFlowCompOutput::SetVolumeOutputFields(CConfig *config) {
   /// DESCRIPTION: Residual of the adjoint energy.
   AddVolumeOutput("RES_ADJ_ENERGY", "Residual_Adjoint_Energy", "RESIDUAL", "Residual of the adjoint energy");
 
-  SetVolumeOutputFields_AdjScalarResidual(config);
+  SetVolumeOutputFieldsAdjScalarResidual(config);
   /// END_GROUP
 
   /// BEGIN_GROUP: SENSITIVITY, DESCRIPTION: Geometrical sensitivities of the current objective function.
@@ -317,7 +317,7 @@ void CAdjFlowCompOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CS
   if (nDim == 3)
     SetVolumeOutputValue("SENSITIVITY-Z", iPoint, Node_AdjFlow->GetSensitivity(iPoint, 2));
 
-  LoadVolumeData_AdjScalar(config, solver, iPoint);
+  LoadVolumeDataAdjScalar(config, solver, iPoint);
 }
 
 void CAdjFlowCompOutput::LoadSurfaceData(CConfig *config, CGeometry *geometry, CSolver **solver, unsigned long iPoint, unsigned short iMarker, unsigned long iVertex) {
@@ -327,7 +327,7 @@ void CAdjFlowCompOutput::LoadSurfaceData(CConfig *config, CGeometry *geometry, C
 }
 
 
-bool CAdjFlowCompOutput::SetInit_Residuals(const CConfig *config) {
+bool CAdjFlowCompOutput::SetInitResiduals(const CConfig *config) {
 
   return ((config->GetTime_Marching() != TIME_MARCHING::STEADY) && (curInnerIter == 0)) ||
          ((config->GetTime_Marching() == TIME_MARCHING::STEADY) && (curInnerIter < 2));
diff --git a/SU2_CFD/src/output/CAdjFlowIncOutput.cpp b/SU2_CFD/src/output/CAdjFlowIncOutput.cpp
index a87d03aa6cf..93c89ca6ada 100644
--- a/SU2_CFD/src/output/CAdjFlowIncOutput.cpp
+++ b/SU2_CFD/src/output/CAdjFlowIncOutput.cpp
@@ -188,7 +188,7 @@ void CAdjFlowIncOutput::SetHistoryOutputFields(CConfig *config) {
   AddHistoryOutput("LINSOL_ITER", "LinSolIter", ScreenOutputFormat::INTEGER, "LINSOL", "Number of iterations of the linear solver.");
   AddHistoryOutput("LINSOL_RESIDUAL", "LinSolRes", ScreenOutputFormat::FIXED, "LINSOL", "Residual of the linear solver.");
 
-  AddHistoryOutputFields_AdjScalarLinsol(config);
+  AddHistoryOutputFieldsAdjScalarLinsol(config);
 
   if (config->GetDeform_Mesh()) {
     AddHistoryOutput("DEFORM_ITER", "DeformIter", ScreenOutputFormat::INTEGER, "DEFORM", "Linear solver iterations for the mesh deformation");
@@ -274,7 +274,7 @@ void CAdjFlowIncOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, CS
     SetHistoryOutputValue("DEFORM_RESIDUAL", log10(mesh_solver->System.GetResidual()));
   }
 
-  LoadHistoryData_AdjScalar(config, solver);
+  LoadHistoryDataAdjScalar(config, solver);
 }
 
 void CAdjFlowIncOutput::SetVolumeOutputFields(CConfig *config) {
@@ -299,7 +299,7 @@ void CAdjFlowIncOutput::SetVolumeOutputFields(CConfig *config) {
   }
   AddVolumeOutput("ADJ_TEMPERATURE", "Adjoint_Temperature", "SOLUTION",  "Adjoint temperature");
 
-  SetVolumeOutputFields_AdjScalarSolution(config);
+  SetVolumeOutputFieldsAdjScalarSolution(config);
 
   if (config->AddRadiation()) {
     AddVolumeOutput("ADJ_P1_ENERGY",  "Adjoint_Energy(P1)", "SOLUTION", "Adjoint radiative energy");
@@ -329,7 +329,7 @@ void CAdjFlowIncOutput::SetVolumeOutputFields(CConfig *config) {
   /// DESCRIPTION: Residual of the adjoint energy.
   AddVolumeOutput("RES_ADJ_TEMPERATURE", "Residual_Adjoint_Heat", "RESIDUAL", "Residual of the adjoint temperature");
 
-  SetVolumeOutputFields_AdjScalarResidual(config);
+  SetVolumeOutputFieldsAdjScalarResidual(config);
 
   if (config->AddRadiation()) {
     AddVolumeOutput("RES_P1_ENERGY",  "Residual_Adjoint_Energy_P1", "RESIDUAL", "Residual of adjoint radiative energy");
@@ -412,7 +412,7 @@ void CAdjFlowIncOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSo
     SetVolumeOutputValue("SENSITIVITY-Z", iPoint, Node_AdjFlow->GetSensitivity(iPoint, 2));
   }
 
-  LoadVolumeData_AdjScalar(config, solver, iPoint);
+  LoadVolumeDataAdjScalar(config, solver, iPoint);
 }
 
 void CAdjFlowIncOutput::LoadSurfaceData(CConfig *config, CGeometry *geometry, CSolver **solver, unsigned long iPoint, unsigned short iMarker, unsigned long iVertex) {
@@ -422,7 +422,7 @@ void CAdjFlowIncOutput::LoadSurfaceData(CConfig *config, CGeometry *geometry, CS
 }
 
 
-bool CAdjFlowIncOutput::SetInit_Residuals(const CConfig *config) {
+bool CAdjFlowIncOutput::SetInitResiduals(const CConfig *config) {
 
   return (config->GetTime_Marching() != TIME_MARCHING::STEADY && (curInnerIter == 0))||
          (config->GetTime_Marching() == TIME_MARCHING::STEADY && (curTimeIter < 2));
diff --git a/SU2_CFD/src/output/CAdjFlowOutput.cpp b/SU2_CFD/src/output/CAdjFlowOutput.cpp
index 647fe42fcbd..bf80b6c807f 100644
--- a/SU2_CFD/src/output/CAdjFlowOutput.cpp
+++ b/SU2_CFD/src/output/CAdjFlowOutput.cpp
@@ -114,7 +114,7 @@ void CAdjFlowOutput::AddHistoryOutputFields_AdjScalarBGS_RES(const CConfig* conf
   }
 }
 
-void CAdjFlowOutput::AddHistoryOutputFields_AdjScalarLinsol(const CConfig* config) {
+void CAdjFlowOutput::AddHistoryOutputFieldsAdjScalarLinsol(const CConfig* config) {
   if ((turb_model != TURB_MODEL::NONE) && !frozen_visc) {
     AddHistoryOutput("LINSOL_ITER_TURB", "LinSolIterTurb", ScreenOutputFormat::INTEGER, "LINSOL", "Number of iterations of the linear solver for turbulence.");
     AddHistoryOutput("LINSOL_RESIDUAL_TURB", "LinSolResTurb", ScreenOutputFormat::FIXED, "LINSOL", "Residual of the linear solver for turbulence.");
@@ -127,7 +127,7 @@ void CAdjFlowOutput::AddHistoryOutputFields_AdjScalarLinsol(const CConfig* confi
 }
 // clang-format on
 
-void CAdjFlowOutput::LoadHistoryData_AdjScalar(const CConfig* config, const CSolver* const* solver) {
+void CAdjFlowOutput::LoadHistoryDataAdjScalar(const CConfig* config, const CSolver* const* solver) {
   const auto adjturb_solver = solver[ADJTURB_SOL];
   const auto adjspecies_solver = solver[ADJSPECIES_SOL];
 
@@ -174,7 +174,7 @@ void CAdjFlowOutput::LoadHistoryData_AdjScalar(const CConfig* config, const CSol
   }
 }
 
-void CAdjFlowOutput::SetVolumeOutputFields_AdjScalarSolution(const CConfig* config) {
+void CAdjFlowOutput::SetVolumeOutputFieldsAdjScalarSolution(const CConfig* config) {
   if (!frozen_visc) {
     switch (TurbModelFamily(turb_model)) {
       case TURB_FAMILY::SA:
@@ -200,7 +200,7 @@ void CAdjFlowOutput::SetVolumeOutputFields_AdjScalarSolution(const CConfig* conf
   }
 }
 
-void CAdjFlowOutput::SetVolumeOutputFields_AdjScalarResidual(const CConfig* config) {
+void CAdjFlowOutput::SetVolumeOutputFieldsAdjScalarResidual(const CConfig* config) {
   if (!frozen_visc) {
     switch (TurbModelFamily(turb_model)) {
       case TURB_FAMILY::SA:
@@ -229,7 +229,7 @@ void CAdjFlowOutput::SetVolumeOutputFields_AdjScalarResidual(const CConfig* conf
   }
 }
 
-void CAdjFlowOutput::LoadVolumeData_AdjScalar(const CConfig* config, const CSolver* const* solver,
+void CAdjFlowOutput::LoadVolumeDataAdjScalar(const CConfig* config, const CSolver* const* solver,
                                               const unsigned long iPoint) {
   const auto Node_AdjTurb =
       ((turb_model != TURB_MODEL::NONE) && !frozen_visc) ? solver[ADJTURB_SOL]->GetNodes() : nullptr;
diff --git a/SU2_CFD/src/output/CElasticityOutput.cpp b/SU2_CFD/src/output/CElasticityOutput.cpp
index 9bdf5d5eabf..365901ba548 100644
--- a/SU2_CFD/src/output/CElasticityOutput.cpp
+++ b/SU2_CFD/src/output/CElasticityOutput.cpp
@@ -266,7 +266,7 @@ void CElasticityOutput::SetVolumeOutputFields(CConfig *config){
   }
 }
 
-bool CElasticityOutput::SetInit_Residuals(const CConfig *config){
+bool CElasticityOutput::SetInitResiduals(const CConfig *config){
 
   return (config->GetTime_Domain() == NO && (curInnerIter  == 0));
 
diff --git a/SU2_CFD/src/output/CFlowCompFEMOutput.cpp b/SU2_CFD/src/output/CFlowCompFEMOutput.cpp
index 50212107c17..e0417d57fa0 100644
--- a/SU2_CFD/src/output/CFlowCompFEMOutput.cpp
+++ b/SU2_CFD/src/output/CFlowCompFEMOutput.cpp
@@ -265,7 +265,7 @@ void CFlowCompFEMOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, C
 
 }
 
-bool CFlowCompFEMOutput::SetInit_Residuals(const CConfig *config){
+bool CFlowCompFEMOutput::SetInitResiduals(const CConfig *config){
 
   return (config->GetTime_Marching() != TIME_MARCHING::STEADY && (curInnerIter == 0))||
          (config->GetTime_Marching() == TIME_MARCHING::STEADY && (curTimeIter < 2));
diff --git a/SU2_CFD/src/output/CFlowCompOutput.cpp b/SU2_CFD/src/output/CFlowCompOutput.cpp
index ed330053a78..0e8e6b78613 100644
--- a/SU2_CFD/src/output/CFlowCompOutput.cpp
+++ b/SU2_CFD/src/output/CFlowCompOutput.cpp
@@ -162,7 +162,7 @@ void CFlowCompOutput::SetHistoryOutputFields(CConfig *config){
   /// DESCRIPTION: Linear solver iterations
   AddHistoryOutput("LINSOL_ITER", "Linear_Solver_Iterations", ScreenOutputFormat::INTEGER, "LINSOL", "Number of iterations of the linear solver.");
   AddHistoryOutput("LINSOL_RESIDUAL", "LinSolRes", ScreenOutputFormat::FIXED, "LINSOL", "Residual of the linear solver.");
-  AddHistoryOutputFields_ScalarLinsol(config);
+  AddHistoryOutputFieldsScalarLinsol(config);
 
   AddHistoryOutput("MIN_DELTA_TIME", "Min DT", ScreenOutputFormat::SCIENTIFIC, "CFL_NUMBER", "Current minimum local time step");
   AddHistoryOutput("MAX_DELTA_TIME", "Max DT", ScreenOutputFormat::SCIENTIFIC, "CFL_NUMBER", "Current maximum local time step");
@@ -203,9 +203,9 @@ void CFlowCompOutput::SetHistoryOutputFields(CConfig *config){
 
   AddRotatingFrameCoefficients();
 
-  Add_CpInverseDesignOutput();
+  AddCpInverseDesignOutput();
 
-  Add_NearfieldInverseDesignOutput();
+  AddNearfieldInverseDesignOutput();
 
 }
 
@@ -345,7 +345,7 @@ void CFlowCompOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolv
     SetVolumeOutputValue("ROE_DISSIPATION", iPoint, Node_Flow->GetRoe_Dissipation(iPoint));
   }
 
-  LoadVolumeData_Scalar(config, solver, geometry, iPoint);
+  LoadVolumeDataScalar(config, solver, geometry, iPoint);
 
   LoadCommonFVMOutputs(config, geometry, iPoint);
 
@@ -413,7 +413,7 @@ void CFlowCompOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, CSol
     SetHistoryOutputValue("CL_DRIVER_COMMAND", flow_solver->GetAoA_inc());
   }
 
-  LoadHistoryData_Scalar(config, solver);
+  LoadHistoryDataScalar(config, solver);
 
   /*--- Set the analyse surface history values --- */
 
@@ -435,11 +435,11 @@ void CFlowCompOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, CSol
 
   /*--- Set Cp diff fields ---*/
 
-  Set_CpInverseDesign(flow_solver, geometry, config);
+  SetCpInverseDesign(flow_solver, geometry, config);
 
   /*--- Set nearfield diff fields ---*/
 
-  if (config->GetEquivArea()) Set_NearfieldInverseDesign(flow_solver, geometry, config);
+  if (config->GetEquivArea()) SetNearfieldInverseDesign(flow_solver, geometry, config);
 
   /*--- Keep this as last, since it uses the history values that were set. ---*/
 
@@ -449,7 +449,7 @@ void CFlowCompOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, CSol
 
 }
 
-bool CFlowCompOutput::SetInit_Residuals(const CConfig *config){
+bool CFlowCompOutput::SetInitResiduals(const CConfig *config){
 
   return (config->GetTime_Marching() != TIME_MARCHING::STEADY && (curInnerIter == 0))||
          (config->GetTime_Marching() == TIME_MARCHING::STEADY && (curInnerIter < 2));
@@ -463,6 +463,6 @@ void CFlowCompOutput::SetAdditionalScreenOutput(const CConfig *config){
   }
 }
 
-bool CFlowCompOutput::WriteHistoryFile_Output(const CConfig *config) {
-  return !config->GetFinite_Difference_Mode() && COutput::WriteHistoryFile_Output(config);
+bool CFlowCompOutput::WriteHistoryFileOutput(const CConfig *config) {
+  return !config->GetFinite_Difference_Mode() && COutput::WriteHistoryFileOutput(config);
 }
diff --git a/SU2_CFD/src/output/CFlowIncOutput.cpp b/SU2_CFD/src/output/CFlowIncOutput.cpp
index 01d91eec96a..122ebb26a34 100644
--- a/SU2_CFD/src/output/CFlowIncOutput.cpp
+++ b/SU2_CFD/src/output/CFlowIncOutput.cpp
@@ -158,7 +158,7 @@ void CFlowIncOutput::SetHistoryOutputFields(CConfig *config){
   /// DESCRIPTION: Linear solver iterations
   AddHistoryOutput("LINSOL_ITER", "LinSolIter", ScreenOutputFormat::INTEGER, "LINSOL", "Number of iterations of the linear solver.");
   AddHistoryOutput("LINSOL_RESIDUAL", "LinSolRes", ScreenOutputFormat::FIXED, "LINSOL", "Residual of the linear solver.");
-  AddHistoryOutputFields_ScalarLinsol(config);
+  AddHistoryOutputFieldsScalarLinsol(config);
 
   AddHistoryOutput("MIN_DELTA_TIME", "Min DT", ScreenOutputFormat::SCIENTIFIC, "CFL_NUMBER", "Current minimum local time step");
   AddHistoryOutput("MAX_DELTA_TIME", "Max DT", ScreenOutputFormat::SCIENTIFIC, "CFL_NUMBER", "Current maximum local time step");
@@ -256,7 +256,7 @@ void CFlowIncOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, CSolv
   SetHistoryOutputValue("MAX_CFL", flow_solver->GetMax_CFL_Local());
   SetHistoryOutputValue("AVG_CFL", flow_solver->GetAvg_CFL_Local());
 
-  LoadHistoryData_Scalar(config, solver);
+  LoadHistoryDataScalar(config, solver);
 
   if(streamwisePeriodic) {
     SetHistoryOutputValue("STREAMWISE_MASSFLOW", flow_solver->GetStreamwisePeriodicValues().Streamwise_Periodic_MassFlow);
@@ -432,7 +432,7 @@ void CFlowIncOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolve
   }
 
   // All turbulence and species outputs.
-  LoadVolumeData_Scalar(config, solver, geometry, iPoint);
+  LoadVolumeDataScalar(config, solver, geometry, iPoint);
 
   // Streamwise Periodicity
   if(streamwisePeriodic) {
@@ -444,7 +444,7 @@ void CFlowIncOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolve
   LoadCommonFVMOutputs(config, geometry, iPoint);
 }
 
-bool CFlowIncOutput::SetInit_Residuals(const CConfig *config){
+bool CFlowIncOutput::SetInitResiduals(const CConfig *config){
 
   return (config->GetTime_Marching() != TIME_MARCHING::STEADY && (curInnerIter == 0))||
          (config->GetTime_Marching() == TIME_MARCHING::STEADY && (curInnerIter < 2));
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index 1f746db5558..f9c355d70cf 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -543,7 +543,7 @@ void CFlowOutput::SetAnalyzeSurface(const CSolver* const*solver, const CGeometry
     for (unsigned short iVar = 0; iVar < nSpecies; iVar++)
       SetHistoryOutputValue("SURFACE_SPECIES_" + std::to_string(iVar), Tot_Surface_Species[iVar]);
 
-    SetAnalyzeSurface_SpeciesVariance(solver, geometry, config, Surface_Species_Total, Surface_MassFlow_Abs_Total,
+    SetAnalyzeSurfaceSpeciesVariance(solver, geometry, config, Surface_Species_Total, Surface_MassFlow_Abs_Total,
                                       Surface_Area_Total);
   }
 
@@ -631,7 +631,7 @@ void CFlowOutput::SetAnalyzeSurface(const CSolver* const*solver, const CGeometry
   std::cout << std::resetiosflags(std::cout.flags());
 }
 
-void CFlowOutput::SetAnalyzeSurface_SpeciesVariance(const CSolver* const*solver, const CGeometry *geometry,
+void CFlowOutput::SetAnalyzeSurfaceSpeciesVariance(const CSolver* const*solver, const CGeometry *geometry,
                                                     CConfig *config, const su2activematrix& Surface_Species_Total,
                                                     const vector<su2double>& Surface_MassFlow_Abs_Total,
                                                     const vector<su2double>& Surface_Area_Total) {
@@ -858,7 +858,7 @@ void CFlowOutput::SetCustomOutputs(const CSolver* const* solver, const CGeometry
         /*--- Functions only reference other history outputs. ---*/
         return *output.otherOutputs[i - CustomOutput::NOT_A_VARIABLE];
       };
-      SetHistoryOutputValue(output.name, output.eval(Functor));
+      SetHistoryOutputValue(output.name, output.Eval(Functor));
       continue;
     }
 
@@ -885,7 +885,7 @@ void CFlowOutput::SetCustomOutputs(const CSolver* const* solver, const CGeometry
     if (output.type == OperationType::PROBE) {
       su2double value = std::numeric_limits<su2double>::max();
       if (output.iPoint != CustomOutput::PROBE_NOT_OWNED) {
-        value = output.eval(MakeFunctor(output.iPoint));
+        value = output.Eval(MakeFunctor(output.iPoint));
       }
       su2double tmp = value;
       SU2_MPI::Allreduce(&tmp, &value, 1, MPI_DOUBLE, MPI_MIN, SU2_MPI::GetComm());
@@ -918,7 +918,7 @@ void CFlowOutput::SetCustomOutputs(const CSolver* const* solver, const CGeometry
           }
           weight *= GetAxiFactor(axisymmetric, *geometry->nodes, iPoint, iMarker);
           local_integral[1] += weight;
-          local_integral[0] += weight * output.eval(MakeFunctor(iPoint));
+          local_integral[0] += weight * output.Eval(MakeFunctor(iPoint));
         }
         END_SU2_OMP_FOR
       }
@@ -1052,7 +1052,7 @@ void CFlowOutput::AddHistoryOutputFields_ScalarBGS_RES(const CConfig* config) {
   }
 }
 
-void CFlowOutput::AddHistoryOutputFields_ScalarLinsol(const CConfig* config) {
+void CFlowOutput::AddHistoryOutputFieldsScalarLinsol(const CConfig* config) {
   if (config->GetKind_Turb_Model() != TURB_MODEL::NONE) {
     AddHistoryOutput("LINSOL_ITER_TURB", "LinSolIterTurb", ScreenOutputFormat::INTEGER, "LINSOL", "Number of iterations of the linear solver for turbulence solver.");
     AddHistoryOutput("LINSOL_RESIDUAL_TURB", "LinSolResTurb", ScreenOutputFormat::FIXED, "LINSOL", "Residual of the linear solver for turbulence solver.");
@@ -1070,7 +1070,7 @@ void CFlowOutput::AddHistoryOutputFields_ScalarLinsol(const CConfig* config) {
 }
 // clang-format on
 
-void CFlowOutput::LoadHistoryData_Scalar(const CConfig* config, const CSolver* const* solver) {
+void CFlowOutput::LoadHistoryDataScalar(const CConfig* config, const CSolver* const* solver) {
   switch (TurbModelFamily(config->GetKind_Turb_Model())) {
     case TURB_FAMILY::SA:
       SetHistoryOutputValue("RMS_NU_TILDE", log10(solver[TURB_SOL]->GetRes_RMS(0)));
@@ -1264,7 +1264,7 @@ void CFlowOutput::SetVolumeOutputFieldsScalarMisc(const CConfig* config) {
   }
 }
 
-void CFlowOutput::LoadVolumeData_Scalar(const CConfig* config, const CSolver* const* solver, const CGeometry* geometry,
+void CFlowOutput::LoadVolumeDataScalar(const CConfig* config, const CSolver* const* solver, const CGeometry* geometry,
                                         const unsigned long iPoint) {
   const auto* turb_solver = solver[TURB_SOL];
   const auto* trans_solver = solver[TRANS_SOL];
@@ -1281,7 +1281,7 @@ void CFlowOutput::LoadVolumeData_Scalar(const CConfig* config, const CSolver* co
     } else {
       SetVolumeOutputValue("VORTICITY", iPoint, Node_Flow->GetVorticity(iPoint)[2]);
     }
-    SetVolumeOutputValue("Q_CRITERION", iPoint, GetQ_Criterion(Node_Flow->GetVelocityGradient(iPoint)));
+    SetVolumeOutputValue("Q_CRITERION", iPoint, GetQCriterion(Node_Flow->GetVelocityGradient(iPoint)));
   }
 
   const bool limiter = (config->GetKind_SlopeLimit_Turb() != LIMITER::NONE);
@@ -1517,12 +1517,12 @@ void CFlowOutput::SetRotatingFrameCoefficients(const CSolver* flow_solver) {
   SetHistoryOutputValue("FIGURE_OF_MERIT", flow_solver->GetTotal_CMerit());
 }
 
-void CFlowOutput::Add_CpInverseDesignOutput(){
+void CFlowOutput::AddCpInverseDesignOutput(){
 
   AddHistoryOutput("INVERSE_DESIGN_PRESSURE", "Cp_Diff", ScreenOutputFormat::FIXED, "CP_DIFF", "Cp difference for inverse design", HistoryFieldType::COEFFICIENT);
 }
 
-void CFlowOutput::Set_CpInverseDesign(CSolver *solver, const CGeometry *geometry, const CConfig *config){
+void CFlowOutput::SetCpInverseDesign(CSolver *solver, const CGeometry *geometry, const CConfig *config){
 
   /*--- Prepare to read the surface pressure files (CSV) ---*/
 
@@ -1610,12 +1610,12 @@ void CFlowOutput::Set_CpInverseDesign(CSolver *solver, const CGeometry *geometry
 
 }
 
-void CFlowOutput::Add_NearfieldInverseDesignOutput(){
+void CFlowOutput::AddNearfieldInverseDesignOutput(){
 
   AddHistoryOutput("EQUIVALENT_AREA", "CEquiv_Area", ScreenOutputFormat::SCIENTIFIC, "EQUIVALENT_AREA", "Equivalent area", HistoryFieldType::COEFFICIENT);
 }
 
-void CFlowOutput::Set_NearfieldInverseDesign(CSolver *solver, const CGeometry *geometry, const CConfig *config){
+void CFlowOutput::SetNearfieldInverseDesign(CSolver *solver, const CGeometry *geometry, const CConfig *config){
 
   ofstream EquivArea_file;
   su2double auxXCoord, auxYCoord, auxZCoord, InverseDesign = 0.0, DeltaX,
@@ -3604,7 +3604,7 @@ void CFlowOutput::WriteForcesBreakdown(const CConfig* config, const CSolver* flo
   // clang-format on
 }
 
-bool CFlowOutput::WriteVolume_Output(CConfig *config, unsigned long Iter, bool force_writing, unsigned short iFile){
+bool CFlowOutput::WriteVolumeOutput(CConfig *config, unsigned long Iter, bool force_writing, unsigned short iFile){
 
   bool writeRestart = false;
   auto FileFormat = config->GetVolumeOutputFiles();
@@ -3721,7 +3721,7 @@ void CFlowOutput::SetFixedCLScreenOutput(const CConfig *config){
     else
       FixedCLSummary << "Changed AoA by" << historyOutput_Map["CL_DRIVER_COMMAND"].value;
     FixedCLSummary.PrintFooter();
-    SetScreen_Header(config);
+    SetScreenHeader(config);
   }
 
   else if (config->GetFinite_Difference_Mode() && historyOutput_Map["AOA"].value == historyOutput_Map["PREV_AOA"].value){
diff --git a/SU2_CFD/src/output/CMultizoneOutput.cpp b/SU2_CFD/src/output/CMultizoneOutput.cpp
index f157fb39d74..a9e0833c422 100644
--- a/SU2_CFD/src/output/CMultizoneOutput.cpp
+++ b/SU2_CFD/src/output/CMultizoneOutput.cpp
@@ -123,7 +123,7 @@ void CMultizoneOutput::SetMultizoneHistoryOutputFields(const COutput* const* out
     zoneIndex = "[" + PrintingToolbox::to_string(iZone) + "]";
 
     /*--- For all the variables per solver ---*/
-    for (const auto& nameSinglezone : output[iZone]->GetHistoryOutput_List()) {
+    for (const auto& nameSinglezone : output[iZone]->GetHistoryOutputList()) {
 
       if (nameSinglezone != "TIME_ITER" && nameSinglezone != "OUTER_ITER") {
 
@@ -151,7 +151,7 @@ void CMultizoneOutput::SetMultizoneHistoryOutputFields(const COutput* const* out
     /*--- Add the PerSurface outputs. ---*/
     const auto& ZoneHistoryPerSurfaceFields = output[iZone]->GetHistoryPerSurfaceFields();
 
-    for (const auto& nameSinglezone : output[iZone]->GetHistoryOutputPerSurface_List()) {
+    for (const auto& nameSinglezone : output[iZone]->GetHistoryOutputPerSurfaceList()) {
 
       const auto& field = ZoneHistoryPerSurfaceFields.at(nameSinglezone);
 
@@ -186,7 +186,7 @@ void CMultizoneOutput::SetMultizoneHistoryOutputFields(const COutput* const* out
   AddHistoryOutput("COMBO", "ComboObj", ScreenOutputFormat::SCIENTIFIC, "COMBO", "Combined obj. function value.", HistoryFieldType::COEFFICIENT);
 }
 
-bool CMultizoneOutput::WriteScreen_Header(const CConfig *config) {
+bool CMultizoneOutput::WriteScreenHeader(const CConfig *config) {
 
   /*--- Print header if the outer iteration is zero or zonal convergence is printed ---*/
 
@@ -202,7 +202,7 @@ bool CMultizoneOutput::WriteScreen_Header(const CConfig *config) {
   return false;
 }
 
-bool CMultizoneOutput::WriteScreen_Output(const CConfig *config) {
+bool CMultizoneOutput::WriteScreenOutput(const CConfig *config) {
 
   unsigned long ScreenWrt_Freq_Outer = config->GetScreen_Wrt_Freq(1);
   unsigned long ScreenWrt_Freq_Time  = config->GetScreen_Wrt_Freq(0);
@@ -228,7 +228,7 @@ bool CMultizoneOutput::WriteScreen_Output(const CConfig *config) {
   return true;
 }
 
-bool CMultizoneOutput::WriteHistoryFile_Output(const CConfig *config){
+bool CMultizoneOutput::WriteHistoryFileOutput(const CConfig *config){
 
   unsigned long HistoryWrt_Freq_Outer = config->GetHistory_Wrt_Freq(1);
   unsigned long HistoryWrt_Freq_Time  = config->GetHistory_Wrt_Freq(0);
diff --git a/SU2_CFD/src/output/CNEMOCompOutput.cpp b/SU2_CFD/src/output/CNEMOCompOutput.cpp
index 7ad99be195e..a4eba6ff6da 100644
--- a/SU2_CFD/src/output/CNEMOCompOutput.cpp
+++ b/SU2_CFD/src/output/CNEMOCompOutput.cpp
@@ -169,7 +169,7 @@ void CNEMOCompOutput::SetHistoryOutputFields(CConfig *config){
   /// DESCRIPTION: Linear solver iterations
   AddHistoryOutput("LINSOL_ITER", "Linear_Solver_Iterations", ScreenOutputFormat::INTEGER, "LINSOL", "Number of iterations of the linear solver.");
   AddHistoryOutput("LINSOL_RESIDUAL", "LinSolRes", ScreenOutputFormat::FIXED, "LINSOL", "Residual of the linear solver.");
-  AddHistoryOutputFields_ScalarLinsol(config);
+  AddHistoryOutputFieldsScalarLinsol(config);
 
   AddHistoryOutput("MIN_CFL", "Min CFL", ScreenOutputFormat::SCIENTIFIC, "CFL_NUMBER", "Current minimum of the local CFL numbers");
   AddHistoryOutput("MAX_CFL", "Max CFL", ScreenOutputFormat::SCIENTIFIC, "CFL_NUMBER", "Current maximum of the local CFL numbers");
@@ -202,7 +202,7 @@ void CNEMOCompOutput::SetHistoryOutputFields(CConfig *config){
 
   AddRotatingFrameCoefficients();
 
-  Add_CpInverseDesignOutput();
+  AddCpInverseDesignOutput();
 
 }
 
@@ -364,7 +364,7 @@ void CNEMOCompOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolv
     }
   }
 
-  LoadVolumeData_Scalar(config, solver, geometry, iPoint);
+  LoadVolumeDataScalar(config, solver, geometry, iPoint);
 
   LoadCommonFVMOutputs(config, geometry, iPoint);
 
@@ -434,7 +434,7 @@ void CNEMOCompOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, CSol
     SetHistoryOutputValue("CL_DRIVER_COMMAND", NEMO_solver->GetAoA_inc());
   }
 
-  LoadHistoryData_Scalar(config, solver);
+  LoadHistoryDataScalar(config, solver);
 
   /*--- Set the analyse surface history values --- */
 
@@ -450,7 +450,7 @@ void CNEMOCompOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, CSol
 
   /*--- Set Cp diff fields ---*/
 
-  Set_CpInverseDesign(NEMO_solver, geometry, config);
+  SetCpInverseDesign(NEMO_solver, geometry, config);
 
   /*--- Keep this as last, since it uses the history values that were set. ---*/
 
@@ -460,7 +460,7 @@ void CNEMOCompOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, CSol
 
 }
 
-bool CNEMOCompOutput::SetInit_Residuals(const CConfig *config){
+bool CNEMOCompOutput::SetInitResiduals(const CConfig *config){
 
   return (config->GetTime_Marching() != TIME_MARCHING::STEADY && (curInnerIter == 0))||
          (config->GetTime_Marching() == TIME_MARCHING::STEADY && (curInnerIter < 2));
@@ -474,6 +474,6 @@ void CNEMOCompOutput::SetAdditionalScreenOutput(const CConfig *config){
   }
 }
 
-bool CNEMOCompOutput::WriteHistoryFile_Output(const CConfig *config) {
-  return !config->GetFinite_Difference_Mode() && COutput::WriteHistoryFile_Output(config);
+bool CNEMOCompOutput::WriteHistoryFileOutput(const CConfig *config) {
+  return !config->GetFinite_Difference_Mode() && COutput::WriteHistoryFileOutput(config);
 }
diff --git a/SU2_CFD/src/output/COutput.cpp b/SU2_CFD/src/output/COutput.cpp
index aa743aa0610..646cc521c93 100644
--- a/SU2_CFD/src/output/COutput.cpp
+++ b/SU2_CFD/src/output/COutput.cpp
@@ -183,7 +183,7 @@ COutput::~COutput(void) {
 
 }
 
-void COutput::SetHistory_Output(CGeometry *geometry,
+void COutput::SetHistoryOutput(CGeometry *geometry,
                                   CSolver **solver_container,
                                   CConfig *config,
                                   unsigned long TimeIter,
@@ -201,9 +201,9 @@ void COutput::SetHistory_Output(CGeometry *geometry,
 
   LoadHistoryData(config, geometry, solver_container);
 
-  Convergence_Monitoring(config, curInnerIter);
+  ConvergenceMonitoring(config, curInnerIter);
 
-  Postprocess_HistoryData(config);
+  PostprocessHistoryData(config);
 
   MonitorTimeConvergence(config, curTimeIter);
 
@@ -211,7 +211,7 @@ void COutput::SetHistory_Output(CGeometry *geometry,
 
 }
 
-void COutput::SetHistory_Output(CGeometry *geometry,
+void COutput::SetHistoryOutput(CGeometry *geometry,
                                 CSolver **solver_container,
                                 CConfig *config) {
 
@@ -221,13 +221,13 @@ void COutput::SetHistory_Output(CGeometry *geometry,
 
   LoadHistoryData(config, geometry, solver_container);
 
-  Convergence_Monitoring(config, curInnerIter);
+  ConvergenceMonitoring(config, curInnerIter);
 
-  Postprocess_HistoryData(config);
+  PostprocessHistoryData(config);
 
 }
 
-void COutput::SetMultizoneHistory_Output(COutput **output, CConfig **config, CConfig *driver_config, unsigned long TimeIter, unsigned long OuterIter){
+void COutput::SetMultizoneHistoryOutput(COutput **output, CConfig **config, CConfig *driver_config, unsigned long TimeIter, unsigned long OuterIter){
 
   curTimeIter  = TimeIter;
   curAbsTimeIter = TimeIter - driver_config->GetRestart_Iter();
@@ -239,9 +239,9 @@ void COutput::SetMultizoneHistory_Output(COutput **output, CConfig **config, CCo
 
   LoadMultizoneHistoryData(output, config);
 
-  Convergence_Monitoring(driver_config, curOuterIter);
+  ConvergenceMonitoring(driver_config, curOuterIter);
 
-  Postprocess_HistoryData(driver_config);
+  PostprocessHistoryData(driver_config);
 
   MonitorTimeConvergence(driver_config, curTimeIter);
 
@@ -253,11 +253,11 @@ void COutput::OutputScreenAndHistory(CConfig *config) {
 
   if (rank == MASTER_NODE && !noWriting) {
 
-    if (WriteHistoryFile_Output(config)) SetHistoryFile_Output(config);
+    if (WriteHistoryFileOutput(config)) SetHistoryFileOutput(config);
 
-    if (WriteScreen_Header(config)) SetScreen_Header(config);
+    if (WriteScreenHeader(config)) SetScreenHeader(config);
 
-    if (WriteScreen_Output(config)) SetScreen_Output(config);
+    if (WriteScreenOutput(config)) SetScreenOutput(config);
 
   }
 }
@@ -285,7 +285,7 @@ void COutput::SetCustomAndComboObjectives(int idxSol, const CConfig *config, CSo
     if (!customObjFunc.ready) {
       SetupCustomHistoryOutput(config->GetCustomObjFunc(), customObjFunc);
     }
-    solver[idxSol]->SetTotal_Custom_ObjFunc(customObjFunc.eval());
+    solver[idxSol]->SetTotal_Custom_ObjFunc(customObjFunc.Eval());
   }
   solver[idxSol]->Evaluate_ObjFunc(config, solver);
   SetHistoryOutputValue("COMBO", solver[idxSol]->GetTotal_ComboObj());
@@ -318,7 +318,7 @@ void COutput::AllocateDataSorters(CConfig *config, CGeometry *geometry){
 
 }
 
-void COutput::Load_Data(CGeometry *geometry, CConfig *config, CSolver** solver_container){
+void COutput::LoadData(CGeometry *geometry, CConfig *config, CSolver** solver_container){
 
   /*--- Check if the data sorters are allocated, if not, allocate them. --- */
 
@@ -857,17 +857,17 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
 
     /*--- Write data to file ---*/
 
-    fileWriter->Write_Data(fileName);
+    fileWriter->WriteData(fileName);
 
-    su2double BandWidth = fileWriter->Get_Bandwidth();
+    su2double BandWidth = fileWriter->GetBandwidth();
 
     /*--- Write data with iteration number to file ---*/
 
     if (!filename_iter.empty() && !config->GetWrt_Restart_Overwrite()){
-      fileWriter->Write_Data(filename_iter);
+      fileWriter->WriteData(filename_iter);
 
       /*--- overwrite bandwidth ---*/
-      BandWidth = fileWriter->Get_Bandwidth();
+      BandWidth = fileWriter->GetBandwidth();
 
     }
 
@@ -902,7 +902,7 @@ bool COutput::GetCauchyCorrectedTimeConvergence(const CConfig *config){
   return TimeConvergence;
 }
 
-bool COutput::SetResult_Files(CGeometry *geometry, CConfig *config, CSolver** solver_container,
+bool COutput::SetResultFiles(CGeometry *geometry, CConfig *config, CSolver** solver_container,
                               unsigned long iter, bool force_writing) {
 
   bool isFileWrite = false, dataIsLoaded = false;
@@ -917,7 +917,7 @@ bool COutput::SetResult_Files(CGeometry *geometry, CConfig *config, CSolver** so
     /*--- Collect the volume data from the solvers.
      *  If time-domain is enabled, we also load the data although we don't output it,
      *  since we might want to do time-averaging. ---*/
-    const bool write_file = WriteVolume_Output(config, iter, force_writing || cauchyTimeConverged, iFile);
+    const bool write_file = WriteVolumeOutput(config, iter, force_writing || cauchyTimeConverged, iFile);
 
     if ((write_file || config->GetTime_Domain()) && !dataIsLoaded) {
       LoadDataIntoSorter(config, geometry, solver_container);
@@ -986,7 +986,7 @@ void COutput::PrintConvergenceSummary(){
   ConvSummary.PrintFooter();
 }
 
-bool COutput::Convergence_Monitoring(CConfig *config, unsigned long Iteration) {
+bool COutput::ConvergenceMonitoring(CConfig *config, unsigned long Iteration) {
 
   convergence = true;
 
@@ -1145,7 +1145,7 @@ bool COutput::MonitorTimeConvergence(CConfig *config, unsigned long TimeIteratio
   return TimeConvergence;
 }
 
-void COutput::SetHistoryFile_Header(const CConfig *config) {
+void COutput::SetHistoryFileHeader(const CConfig *config) {
 
   unsigned short iField_Output = 0,
       iReqField = 0,
@@ -1189,7 +1189,7 @@ void COutput::SetHistoryFile_Header(const CConfig *config) {
 }
 
 
-void COutput::SetHistoryFile_Output(const CConfig *config) {
+void COutput::SetHistoryFileOutput(const CConfig *config) {
 
   if (requestedHistoryFieldCache.empty()) {
     for (const auto& fieldIdentifier : historyOutput_List){
@@ -1221,14 +1221,14 @@ void COutput::SetHistoryFile_Output(const CConfig *config) {
   histFile.flush();
 }
 
-void COutput::SetScreen_Header(const CConfig *config) {
+void COutput::SetScreenHeader(const CConfig *config) {
   if (config->GetMultizone_Problem())
     multiZoneHeaderTable->PrintHeader();
   convergenceTable->PrintHeader();
 }
 
 
-void COutput::SetScreen_Output(const CConfig *config) {
+void COutput::SetScreenOutput(const CConfig *config) {
 
   if (requestedScreenFieldCache.empty()) {
     for (const auto& RequestedField : requestedScreenFields) {
@@ -1286,7 +1286,7 @@ void COutput::PreprocessHistoryOutput(CConfig *config, bool wrt){
 
   /*--- Postprocess the history fields. Creates new fields based on the ones set in the child classes ---*/
 
-  Postprocess_HistoryFields(config);
+  PostprocessHistoryFields(config);
 
   /*--- We use a fixed size of the file output summary table ---*/
 
@@ -1333,7 +1333,7 @@ void COutput::PreprocessMultizoneHistoryOutput(COutput **output, CConfig **confi
 
   /*--- Postprocess the history fields. Creates new fields based on the ones set in the child classes ---*/
 
-  Postprocess_HistoryFields(driver_config);
+  PostprocessHistoryFields(driver_config);
 
   /*--- We use a fixed size of the file output summary table ---*/
 
@@ -1382,7 +1382,7 @@ void COutput::PrepareHistoryFile(CConfig *config){
 
   /*--- Add the header to the history file. ---*/
 
-  SetHistoryFile_Header(config);
+  SetHistoryFileHeader(config);
 
 }
 
@@ -1773,7 +1773,7 @@ void COutput::SetVolumeOutputValue(string name, unsigned long iPoint, su2double
       const short Offset = volumeOutput_Map.at(name).offset;
       fieldIndexCache.push_back(Offset);
       if (Offset != -1){
-        volumeDataSorter->SetUnsorted_Data(iPoint, Offset, value);
+        volumeDataSorter->SetUnsortedData(iPoint, Offset, value);
       }
     } else {
       SU2_MPI::Error(string("Cannot find output field with name ") + name, CURRENT_FUNCTION);
@@ -1784,7 +1784,7 @@ void COutput::SetVolumeOutputValue(string name, unsigned long iPoint, su2double
 
     const short Offset = fieldIndexCache[cachePosition++];
     if (Offset != -1){
-      volumeDataSorter->SetUnsorted_Data(iPoint, Offset, value);
+      volumeDataSorter->SetUnsortedData(iPoint, Offset, value);
     }
     if (cachePosition == fieldIndexCache.size()){
       cachePosition = 0;
@@ -1805,7 +1805,7 @@ su2double COutput::GetVolumeOutputValue(string name, unsigned long iPoint){
       const short Offset = volumeOutput_Map.at(name).offset;
       fieldGetIndexCache.push_back(Offset);
       if (Offset != -1){
-        return volumeDataSorter->GetUnsorted_Data(iPoint, Offset);
+        return volumeDataSorter->GetUnsortedData(iPoint, Offset);
       }
     } else {
       SU2_MPI::Error(string("Cannot find output field with name ") + name, CURRENT_FUNCTION);
@@ -1820,7 +1820,7 @@ su2double COutput::GetVolumeOutputValue(string name, unsigned long iPoint){
       curGetFieldIndex = 0;
     }
     if (Offset != -1){
-      return volumeDataSorter->GetUnsorted_Data(iPoint, Offset);
+      return volumeDataSorter->GetUnsortedData(iPoint, Offset);
     }
   }
 
@@ -1842,10 +1842,10 @@ void COutput::SetAvgVolumeOutputValue(string name, unsigned long iPoint, su2doub
       fieldIndexCache.push_back(Offset);
       if (Offset != -1){
 
-        const su2double old_value = volumeDataSorter->GetUnsorted_Data(iPoint, Offset);
+        const su2double old_value = volumeDataSorter->GetUnsortedData(iPoint, Offset);
         const su2double new_value = value * scaling + old_value *( 1.0 - scaling);
 
-        volumeDataSorter->SetUnsorted_Data(iPoint, Offset, new_value);
+        volumeDataSorter->SetUnsortedData(iPoint, Offset, new_value);
       }
     } else {
       SU2_MPI::Error(string("Cannot find output field with name ") + name, CURRENT_FUNCTION);
@@ -1857,10 +1857,10 @@ void COutput::SetAvgVolumeOutputValue(string name, unsigned long iPoint, su2doub
     const short Offset = fieldIndexCache[cachePosition++];
     if (Offset != -1){
 
-      const su2double old_value = volumeDataSorter->GetUnsorted_Data(iPoint, Offset);
+      const su2double old_value = volumeDataSorter->GetUnsortedData(iPoint, Offset);
       const su2double new_value = value * scaling + old_value *( 1.0 - scaling);
 
-      volumeDataSorter->SetUnsorted_Data(iPoint, Offset, new_value);
+      volumeDataSorter->SetUnsortedData(iPoint, Offset, new_value);
     }
     if (cachePosition == fieldIndexCache.size()){
       cachePosition = 0;
@@ -1869,7 +1869,7 @@ void COutput::SetAvgVolumeOutputValue(string name, unsigned long iPoint, su2doub
 
 }
 
-void COutput::Postprocess_HistoryData(CConfig *config){
+void COutput::PostprocessHistoryData(CConfig *config){
 
   map<string, pair<su2double, int> > Average;
   map<string, int> Count;
@@ -1878,7 +1878,7 @@ void COutput::Postprocess_HistoryData(CConfig *config){
     const string &fieldIdentifier = historyOutput_List[iField];
     const HistoryOutputField &currentField = historyOutput_Map.at(fieldIdentifier);
     if (currentField.fieldType == HistoryFieldType::RESIDUAL){
-      if ( SetInit_Residuals(config) || (currentField.value > initialResiduals[fieldIdentifier]) ) {
+      if ( SetInitResiduals(config) || (currentField.value > initialResiduals[fieldIdentifier]) ) {
         initialResiduals[fieldIdentifier] = currentField.value;
       }
       SetHistoryOutputValue("REL_" + fieldIdentifier,
@@ -1896,7 +1896,7 @@ void COutput::Postprocess_HistoryData(CConfig *config){
           it = windowedTimeAverages.insert({fieldIdentifier, CWindowedAverage(config->GetKindWindow())}).first;
         }
         auto& timeAverage = it->second;
-        timeAverage.addValue(currentField.value,config->GetTimeIter(), config->GetStartWindowIteration()); //Collecting Values for Windowing
+        timeAverage.AddValue(currentField.value,config->GetTimeIter(), config->GetStartWindowIteration()); //Collecting Values for Windowing
         SetHistoryOutputValue("TAVG_" + fieldIdentifier, timeAverage.GetVal());
         if (config->GetDirectDiff() != NO_DERIVATIVE) {
           SetHistoryOutputValue("D_TAVG_" + fieldIdentifier, SU2_TYPE::GetDerivative(timeAverage.GetVal()));
@@ -1918,7 +1918,7 @@ void COutput::Postprocess_HistoryData(CConfig *config){
   }
 }
 
-void COutput::Postprocess_HistoryFields(CConfig *config){
+void COutput::PostprocessHistoryFields(CConfig *config){
 
   map<string, bool> Average;
   map<string, string> AverageGroupName = {{"BGS_RES", "bgs"},{"RMS_RES","rms"},{"MAX_RES", "max"}};
@@ -1995,7 +1995,7 @@ void COutput::Postprocess_HistoryFields(CConfig *config){
   }
 }
 
-bool COutput::WriteScreen_Header(const CConfig *config) {
+bool COutput::WriteScreenHeader(const CConfig *config) {
 
   unsigned long RestartIter = 0;
 
@@ -2047,7 +2047,7 @@ bool COutput::WriteScreen_Header(const CConfig *config) {
   return false;
 }
 
-bool COutput::WriteScreen_Output(const CConfig *config) {
+bool COutput::WriteScreenOutput(const CConfig *config) {
 
   unsigned long ScreenWrt_Freq_Inner = config->GetScreen_Wrt_Freq(2);
   unsigned long ScreenWrt_Freq_Outer = config->GetScreen_Wrt_Freq(1);
@@ -2088,7 +2088,7 @@ bool COutput::WriteScreen_Output(const CConfig *config) {
 
 }
 
-bool COutput::WriteHistoryFile_Output(const CConfig *config) {
+bool COutput::WriteHistoryFileOutput(const CConfig *config) {
 
   unsigned long HistoryWrt_Freq_Inner = config->GetHistory_Wrt_Freq(2);
   unsigned long HistoryWrt_Freq_Outer = config->GetHistory_Wrt_Freq(1);
@@ -2129,7 +2129,7 @@ bool COutput::WriteHistoryFile_Output(const CConfig *config) {
 
 }
 
-bool COutput::WriteVolume_Output(CConfig *config, unsigned long Iter, bool force_writing, unsigned short iFile){
+bool COutput::WriteVolumeOutput(CConfig *config, unsigned long Iter, bool force_writing, unsigned short iFile){
 
   if (config->GetTime_Domain()){
 
diff --git a/SU2_CFD/src/output/filewriter/CCGNSFileWriter.cpp b/SU2_CFD/src/output/filewriter/CCGNSFileWriter.cpp
index 4f1cfcb41cd..a84676bc275 100644
--- a/SU2_CFD/src/output/filewriter/CCGNSFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CCGNSFileWriter.cpp
@@ -32,7 +32,7 @@ const string CCGNSFileWriter::fileExt = ".cgns";
 CCGNSFileWriter::CCGNSFileWriter(CParallelDataSorter* valDataSorter, bool isSurf)
     : CFileWriter(valDataSorter, fileExt), isSurface(isSurf) {}
 
-void CCGNSFileWriter::Write_Data(string val_filename) {
+void CCGNSFileWriter::WriteData(string val_filename) {
 
 #ifdef HAVE_CGNS
 
@@ -199,7 +199,7 @@ void CCGNSFileWriter::WriteConnectivity(GEO_TYPE type, const string& SectionName
   for (unsigned long iElem = 0; iElem < nLocalElem; iElem++) {
     for (unsigned long iPoint = 0; iPoint < nPointsElem; iPoint++) {
       sendBufferConnectivity[iPoint + nPointsElem * iElem] =
-          static_cast<cgsize_t>(dataSorter->GetElem_Connectivity(type, iElem, iPoint));
+          static_cast<cgsize_t>(dataSorter->GetElemConnectivity(type, iElem, iPoint));
     }
   }
 
diff --git a/SU2_CFD/src/output/filewriter/CCSVFileWriter.cpp b/SU2_CFD/src/output/filewriter/CCSVFileWriter.cpp
index b1dfef3f5d2..08a67d5e013 100644
--- a/SU2_CFD/src/output/filewriter/CCSVFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CCSVFileWriter.cpp
@@ -36,7 +36,7 @@ CCSVFileWriter::~CCSVFileWriter(){
 
 }
 
-void CCSVFileWriter::Write_Data(string val_filename){
+void CCSVFileWriter::WriteData(string val_filename){
 
   /*--- Routine to write the surface CSV files (ASCII). We
    assume here that, as an ASCII file, it is safer to merge the
diff --git a/SU2_CFD/src/output/filewriter/CParallelDataSorter.cpp b/SU2_CFD/src/output/filewriter/CParallelDataSorter.cpp
index b11a4b24cde..a3b372183bd 100644
--- a/SU2_CFD/src/output/filewriter/CParallelDataSorter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParallelDataSorter.cpp
@@ -330,7 +330,7 @@ void CParallelDataSorter::PrepareSendBuffers(std::vector<unsigned long>& globalI
 
 }
 
-unsigned long CParallelDataSorter::GetElem_Connectivity(GEO_TYPE type, unsigned long iElem, unsigned long iNode) const {
+unsigned long CParallelDataSorter::GetElemConnectivity(GEO_TYPE type, unsigned long iElem, unsigned long iNode) const {
 
   switch (type) {
     case LINE:
diff --git a/SU2_CFD/src/output/filewriter/CParaviewBinaryFileWriter.cpp b/SU2_CFD/src/output/filewriter/CParaviewBinaryFileWriter.cpp
index aa22fb41f52..530c1de149a 100644
--- a/SU2_CFD/src/output/filewriter/CParaviewBinaryFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParaviewBinaryFileWriter.cpp
@@ -48,7 +48,7 @@ CParaviewBinaryFileWriter::~CParaviewBinaryFileWriter(){
 
 }
 
-void CParaviewBinaryFileWriter::Write_Data(string val_filename){
+void CParaviewBinaryFileWriter::WriteData(string val_filename){
 
   if (!dataSorter->GetConnectivitySorted()){
     SU2_MPI::Error("Connectivity must be sorted.", CURRENT_FUNCTION);
@@ -146,7 +146,7 @@ void CParaviewBinaryFileWriter::Write_Data(string val_filename){
     for (iElem = 0; iElem < nElem; iElem++) {
       connBuf[iStorage+0] = nPoints;
       for (iNode = 0; iNode < nPoints; iNode++){
-        connBuf[iStorage+iNode+1] = int(dataSorter->GetElem_Connectivity(type, iElem, iNode)-1);
+        connBuf[iStorage+iNode+1] = int(dataSorter->GetElemConnectivity(type, iElem, iNode)-1);
       }
       iStorage += nPoints + 1;
     }
diff --git a/SU2_CFD/src/output/filewriter/CParaviewFileWriter.cpp b/SU2_CFD/src/output/filewriter/CParaviewFileWriter.cpp
index 0b9d0ff41e0..05f8b95133d 100644
--- a/SU2_CFD/src/output/filewriter/CParaviewFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParaviewFileWriter.cpp
@@ -35,7 +35,7 @@ CParaviewFileWriter::CParaviewFileWriter(CParallelDataSorter *valDataSorter) :
 
 CParaviewFileWriter::~CParaviewFileWriter(){}
 
-void CParaviewFileWriter::Write_Data(string val_filename){
+void CParaviewFileWriter::WriteData(string val_filename){
 
   /*--- We append the pre-defined suffix (extension) to the filename (prefix) ---*/
   val_filename.append(fileExt);
@@ -139,63 +139,63 @@ void CParaviewFileWriter::Write_Data(string val_filename){
 
       for (iElem = 0; iElem < nParallel_Line; iElem++) {
         Paraview_File << N_POINTS_LINE << "\t";
-        Paraview_File << dataSorter->GetElem_Connectivity(LINE, iElem, 0)-1 << "\t";
-        Paraview_File << dataSorter->GetElem_Connectivity(LINE, iElem, 1)-1 << "\t";
+        Paraview_File << dataSorter->GetElemConnectivity(LINE, iElem, 0)-1 << "\t";
+        Paraview_File << dataSorter->GetElemConnectivity(LINE, iElem, 1)-1 << "\t";
       }
 
       for (iElem = 0; iElem < nParallel_Tria; iElem++) {
         Paraview_File << N_POINTS_TRIANGLE << "\t";
-        Paraview_File <<  dataSorter->GetElem_Connectivity(TRIANGLE, iElem, 0)-1 << "\t";
-        Paraview_File <<  dataSorter->GetElem_Connectivity(TRIANGLE, iElem, 1)-1 << "\t";
-        Paraview_File <<  dataSorter->GetElem_Connectivity(TRIANGLE, iElem, 2)-1 << "\t";
+        Paraview_File <<  dataSorter->GetElemConnectivity(TRIANGLE, iElem, 0)-1 << "\t";
+        Paraview_File <<  dataSorter->GetElemConnectivity(TRIANGLE, iElem, 1)-1 << "\t";
+        Paraview_File <<  dataSorter->GetElemConnectivity(TRIANGLE, iElem, 2)-1 << "\t";
       }
 
       for (iElem = 0; iElem < nParallel_Quad; iElem++) {
         Paraview_File << N_POINTS_QUADRILATERAL << "\t";
-        Paraview_File <<  dataSorter->GetElem_Connectivity(QUADRILATERAL, iElem, 0)-1 << "\t";
-        Paraview_File <<  dataSorter->GetElem_Connectivity(QUADRILATERAL, iElem, 1)-1 << "\t";
-        Paraview_File <<  dataSorter->GetElem_Connectivity(QUADRILATERAL, iElem, 2)-1 << "\t";
-        Paraview_File <<  dataSorter->GetElem_Connectivity(QUADRILATERAL, iElem, 3)-1 << "\t";
+        Paraview_File <<  dataSorter->GetElemConnectivity(QUADRILATERAL, iElem, 0)-1 << "\t";
+        Paraview_File <<  dataSorter->GetElemConnectivity(QUADRILATERAL, iElem, 1)-1 << "\t";
+        Paraview_File <<  dataSorter->GetElemConnectivity(QUADRILATERAL, iElem, 2)-1 << "\t";
+        Paraview_File <<  dataSorter->GetElemConnectivity(QUADRILATERAL, iElem, 3)-1 << "\t";
       }
 
 
       for (iElem = 0; iElem < nParallel_Tetr; iElem++) {
         Paraview_File << N_POINTS_TETRAHEDRON << "\t";
-        Paraview_File << dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 0)-1 << "\t"
-                      << dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 1)-1 << "\t";
-        Paraview_File << dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 2)-1 << "\t"
-                      << dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 3)-1 << "\t";
+        Paraview_File << dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 0)-1 << "\t"
+                      << dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 1)-1 << "\t";
+        Paraview_File << dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 2)-1 << "\t"
+                      << dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 3)-1 << "\t";
       }
 
       for (iElem = 0; iElem < nParallel_Hexa; iElem++) {
         Paraview_File << N_POINTS_HEXAHEDRON << "\t";
-        Paraview_File << dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 0)-1 << "\t"
-                      << dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 1)-1 << "\t";
-        Paraview_File << dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 2)-1 << "\t"
-                      << dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 3)-1 << "\t";
-        Paraview_File << dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 4)-1 << "\t"
-                      << dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 5)-1 << "\t";
-        Paraview_File << dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 6)-1 << "\t"
-                      << dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 7)-1 << "\t";
+        Paraview_File << dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 0)-1 << "\t"
+                      << dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 1)-1 << "\t";
+        Paraview_File << dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 2)-1 << "\t"
+                      << dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 3)-1 << "\t";
+        Paraview_File << dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 4)-1 << "\t"
+                      << dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 5)-1 << "\t";
+        Paraview_File << dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 6)-1 << "\t"
+                      << dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 7)-1 << "\t";
       }
 
       for (iElem = 0; iElem < nParallel_Pris; iElem++) {
         Paraview_File << N_POINTS_PRISM << "\t";
-        Paraview_File << dataSorter->GetElem_Connectivity(PRISM, iElem, 0)-1 << "\t"
-                      << dataSorter->GetElem_Connectivity(PRISM, iElem, 1)-1 << "\t";
-        Paraview_File << dataSorter->GetElem_Connectivity(PRISM, iElem, 2)-1 << "\t"
-                      << dataSorter->GetElem_Connectivity(PRISM, iElem, 3)-1 << "\t";
-        Paraview_File << dataSorter->GetElem_Connectivity(PRISM, iElem, 4)-1 << "\t"
-                      << dataSorter->GetElem_Connectivity(PRISM, iElem, 5)-1 << "\t";
+        Paraview_File << dataSorter->GetElemConnectivity(PRISM, iElem, 0)-1 << "\t"
+                      << dataSorter->GetElemConnectivity(PRISM, iElem, 1)-1 << "\t";
+        Paraview_File << dataSorter->GetElemConnectivity(PRISM, iElem, 2)-1 << "\t"
+                      << dataSorter->GetElemConnectivity(PRISM, iElem, 3)-1 << "\t";
+        Paraview_File << dataSorter->GetElemConnectivity(PRISM, iElem, 4)-1 << "\t"
+                      << dataSorter->GetElemConnectivity(PRISM, iElem, 5)-1 << "\t";
       }
 
       for (iElem = 0; iElem < nParallel_Pyra; iElem++) {
         Paraview_File << N_POINTS_PYRAMID << "\t";
-        Paraview_File << dataSorter->GetElem_Connectivity(PYRAMID, iElem, 0)-1 << "\t"
-                      << dataSorter->GetElem_Connectivity(PYRAMID, iElem, 1)-1 << "\t";
-        Paraview_File << dataSorter->GetElem_Connectivity(PYRAMID, iElem, 2)-1 << "\t"
-                      << dataSorter->GetElem_Connectivity(PYRAMID, iElem, 3)-1 << "\t";
-        Paraview_File << dataSorter->GetElem_Connectivity(PYRAMID, iElem, 4)-1 << "\t";
+        Paraview_File << dataSorter->GetElemConnectivity(PYRAMID, iElem, 0)-1 << "\t"
+                      << dataSorter->GetElemConnectivity(PYRAMID, iElem, 1)-1 << "\t";
+        Paraview_File << dataSorter->GetElemConnectivity(PYRAMID, iElem, 2)-1 << "\t"
+                      << dataSorter->GetElemConnectivity(PYRAMID, iElem, 3)-1 << "\t";
+        Paraview_File << dataSorter->GetElemConnectivity(PYRAMID, iElem, 4)-1 << "\t";
       }
 
     }    Paraview_File.flush();
@@ -362,7 +362,7 @@ void CParaviewFileWriter::Write_Data(string val_filename){
 
   usedTime = stopTime-startTime;
 
-  fileSize = Determine_Filesize(val_filename);
+  fileSize = DetermineFilesize(val_filename);
 
   /*--- Compute and store the bandwidth ---*/
 
diff --git a/SU2_CFD/src/output/filewriter/CParaviewVTMFileWriter.cpp b/SU2_CFD/src/output/filewriter/CParaviewVTMFileWriter.cpp
index 6e17ec84a01..98bc3bdc511 100644
--- a/SU2_CFD/src/output/filewriter/CParaviewVTMFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParaviewVTMFileWriter.cpp
@@ -47,7 +47,7 @@ CParaviewVTMFileWriter::~CParaviewVTMFileWriter(){
 
 }
 
-void CParaviewVTMFileWriter::Write_Data(string val_filename){
+void CParaviewVTMFileWriter::WriteData(string val_filename){
 
   /*--- We append the pre-defined suffix (extension) to the filename (prefix) ---*/
   val_filename.append(fileExt);
@@ -97,7 +97,7 @@ void CParaviewVTMFileWriter::AddDataset(string foldername, string name, string f
   /*--- Create an XML writer and dump data into file ---*/
 
   CParaviewXMLFileWriter XMLWriter(dataSorter);
-  XMLWriter.Write_Data(fullFilename);
+  XMLWriter.WriteData(fullFilename);
 
   /*--- Add the dataset to the vtm file ---*/
 
@@ -107,7 +107,7 @@ void CParaviewVTMFileWriter::AddDataset(string foldername, string name, string f
 
   nWrittenDatasets++;
 
-  accumulatedBandwidth += XMLWriter.Get_Bandwidth();
+  accumulatedBandwidth += XMLWriter.GetBandwidth();
 
   bandwidth = accumulatedBandwidth/nWrittenDatasets;
 }
diff --git a/SU2_CFD/src/output/filewriter/CParaviewXMLFileWriter.cpp b/SU2_CFD/src/output/filewriter/CParaviewXMLFileWriter.cpp
index fb1572744e8..ff3e489a3a5 100644
--- a/SU2_CFD/src/output/filewriter/CParaviewXMLFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParaviewXMLFileWriter.cpp
@@ -49,7 +49,7 @@ CParaviewXMLFileWriter::~CParaviewXMLFileWriter(){
 
 }
 
-void CParaviewXMLFileWriter::Write_Data(string val_filename){
+void CParaviewXMLFileWriter::WriteData(string val_filename){
 
   if (!dataSorter->GetConnectivitySorted()){
     SU2_MPI::Error("Connectivity must be sorted.", CURRENT_FUNCTION);
@@ -216,7 +216,7 @@ void CParaviewXMLFileWriter::Write_Data(string val_filename){
   auto copyToBuffer = [&](GEO_TYPE type, unsigned long nElem, unsigned short nPoints){
     for (iElem = 0; iElem < nElem; iElem++) {
       for (iNode = 0; iNode < nPoints; iNode++){
-        connBuf[iStorage+iNode] = int(dataSorter->GetElem_Connectivity(type, iElem, iNode)-1);
+        connBuf[iStorage+iNode] = int(dataSorter->GetElemConnectivity(type, iElem, iNode)-1);
       }
       iStorage += nPoints;
       offsetBuf[iElemID++] = int(iStorage + dataSorter->GetnElemConnCumulative(rank));
diff --git a/SU2_CFD/src/output/filewriter/CSTLFileWriter.cpp b/SU2_CFD/src/output/filewriter/CSTLFileWriter.cpp
index 673e7727666..602e4844d09 100644
--- a/SU2_CFD/src/output/filewriter/CSTLFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CSTLFileWriter.cpp
@@ -41,7 +41,7 @@ CSTLFileWriter::CSTLFileWriter(CParallelDataSorter *valDataSorter) :
 CSTLFileWriter::~CSTLFileWriter(){}
 
 
-void CSTLFileWriter::Write_Data(string val_filename){
+void CSTLFileWriter::WriteData(string val_filename){
 
   /*--- We append the pre-defined suffix (extension) to the filename (prefix) ---*/
   val_filename.append(fileExt);
@@ -133,12 +133,12 @@ void CSTLFileWriter::ReprocessElementConnectivity(){
 
   /* Gather a list of nodes we refer to but are not outputting, because they are not present on this rank. */
   for (unsigned long i = 0; i < nParallel_Tria * N_POINTS_TRIANGLE; ++i)
-    if (dataSorter->FindProcessor(dataSorter->GetElem_Connectivity(TRIANGLE, 0, i)-1) != rank)
-      halo_nodes.push_back(dataSorter->GetElem_Connectivity(TRIANGLE, 0, i)-1);
+    if (dataSorter->FindProcessor(dataSorter->GetElemConnectivity(TRIANGLE, 0, i)-1) != rank)
+      halo_nodes.push_back(dataSorter->GetElemConnectivity(TRIANGLE, 0, i)-1);
 
   for (unsigned long i = 0; i < nParallel_Quad * N_POINTS_QUADRILATERAL; ++i)
-    if (dataSorter->FindProcessor(dataSorter->GetElem_Connectivity(QUADRILATERAL, 0, i)-1) != rank)
-      halo_nodes.push_back(dataSorter->GetElem_Connectivity(QUADRILATERAL, 0, i)-1);
+    if (dataSorter->FindProcessor(dataSorter->GetElemConnectivity(QUADRILATERAL, 0, i)-1) != rank)
+      halo_nodes.push_back(dataSorter->GetElemConnectivity(QUADRILATERAL, 0, i)-1);
 
   /* Sorted list of halo nodes for this MPI rank. */
   sorted_halo_nodes.assign(halo_nodes.begin(), halo_nodes.end());
@@ -294,7 +294,7 @@ void CSTLFileWriter::StoreCoordData(enum GEO_TYPE elemType,
   /*--- Write Triangle-Point-Coordinates subsequently in a local send buffer. ---*/
   for (iElem = 0; iElem < nLocalElements; iElem++) {
     for (auto node : nodeList) {
-      globalNodeNumber = dataSorter->GetElem_Connectivity(elemType, iElem, node) - 1;
+      globalNodeNumber = dataSorter->GetElemConnectivity(elemType, iElem, node) - 1;
       localNodeNumber = globalNodeNumber - dataSorter->GetNodeBegin(rank);
 
       for (auto iVar = 0; iVar < 3; iVar++){
diff --git a/SU2_CFD/src/output/filewriter/CSU2BinaryFileWriter.cpp b/SU2_CFD/src/output/filewriter/CSU2BinaryFileWriter.cpp
index c782050d288..8b2fa973f00 100644
--- a/SU2_CFD/src/output/filewriter/CSU2BinaryFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CSU2BinaryFileWriter.cpp
@@ -37,7 +37,7 @@ CSU2BinaryFileWriter::~CSU2BinaryFileWriter(){
 
 }
 
-void CSU2BinaryFileWriter::Write_Data(string val_filename){
+void CSU2BinaryFileWriter::WriteData(string val_filename){
 
   /*--- Local variables ---*/
 
diff --git a/SU2_CFD/src/output/filewriter/CSU2FileWriter.cpp b/SU2_CFD/src/output/filewriter/CSU2FileWriter.cpp
index abffd7d7a55..1c81b799d6a 100644
--- a/SU2_CFD/src/output/filewriter/CSU2FileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CSU2FileWriter.cpp
@@ -32,7 +32,7 @@ const string CSU2FileWriter::fileExt = ".csv";
 CSU2FileWriter::CSU2FileWriter(CParallelDataSorter *valDataSorter) :
   CFileWriter(valDataSorter, fileExt){}
 
-void CSU2FileWriter::Write_Data(string val_filename){
+void CSU2FileWriter::WriteData(string val_filename){
 
   ofstream restart_file;
   const vector<string> fieldNames = dataSorter->GetFieldNames();
@@ -89,7 +89,7 @@ void CSU2FileWriter::Write_Data(string val_filename){
 
   /*--- Determine the file size ---*/
 
-  fileSize = Determine_Filesize(val_filename);
+  fileSize = DetermineFilesize(val_filename);
 
   /*--- Compute and store the bandwidth ---*/
 
diff --git a/SU2_CFD/src/output/filewriter/CSU2MeshFileWriter.cpp b/SU2_CFD/src/output/filewriter/CSU2MeshFileWriter.cpp
index 6ffbfd63304..8caf248dd74 100644
--- a/SU2_CFD/src/output/filewriter/CSU2MeshFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CSU2MeshFileWriter.cpp
@@ -34,7 +34,7 @@ CSU2MeshFileWriter::CSU2MeshFileWriter(CParallelDataSorter *valDataSorter,
                                        unsigned short valiZone, unsigned short valnZone) :
    CFileWriter(valDataSorter, fileExt), iZone(valiZone), nZone(valnZone) {}
 
-void CSU2MeshFileWriter::Write_Data(string val_filename) {
+void CSU2MeshFileWriter::WriteData(string val_filename) {
 
   ofstream output_file;
 
@@ -78,38 +78,38 @@ void CSU2MeshFileWriter::Write_Data(string val_filename) {
       for (auto iElem = 0ul; iElem < dataSorter->GetnElem(TRIANGLE); iElem++) {
         output_file << "5\t";
         for (auto iNode = 0u; iNode < N_POINTS_TRIANGLE; ++iNode)
-          output_file << dataSorter->GetElem_Connectivity(TRIANGLE, iElem, iNode) - 1 << "\t";
+          output_file << dataSorter->GetElemConnectivity(TRIANGLE, iElem, iNode) - 1 << "\t";
         output_file << nElem + offset << "\n"; nElem++;
       }
       for (auto iElem = 0ul; iElem < dataSorter->GetnElem(QUADRILATERAL); iElem++) {
         output_file << "9\t";
         for (auto iNode = 0u; iNode < N_POINTS_QUADRILATERAL; ++iNode)
-          output_file << dataSorter->GetElem_Connectivity(QUADRILATERAL, iElem, iNode) - 1 << "\t";
+          output_file << dataSorter->GetElemConnectivity(QUADRILATERAL, iElem, iNode) - 1 << "\t";
         output_file << nElem + offset << "\n"; nElem++;
       }
       for (auto iElem = 0ul; iElem < dataSorter->GetnElem(TETRAHEDRON); iElem++) {
         output_file << "10\t";
         for (auto iNode = 0u; iNode < N_POINTS_TETRAHEDRON; ++iNode)
-          output_file << dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, iNode) - 1 << "\t";
+          output_file << dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, iNode) - 1 << "\t";
         output_file << nElem + offset << "\n"; nElem++;
       }
       for (auto iElem = 0ul; iElem < dataSorter->GetnElem(HEXAHEDRON); iElem++) {
         output_file << "12\t";
         for (auto iNode = 0u; iNode < N_POINTS_HEXAHEDRON; ++iNode)
-          output_file << dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, iNode) - 1 << "\t";
+          output_file << dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, iNode) - 1 << "\t";
         output_file << nElem + offset << "\n"; nElem++;
       }
       for (auto iElem = 0ul; iElem < dataSorter->GetnElem(PRISM); iElem++) {
         output_file << "13\t";
         for (auto iNode = 0u; iNode < N_POINTS_PRISM; ++iNode)
-          output_file << dataSorter->GetElem_Connectivity(PRISM, iElem, iNode) - 1 << "\t";
+          output_file << dataSorter->GetElemConnectivity(PRISM, iElem, iNode) - 1 << "\t";
         output_file << nElem + offset << "\n"; nElem++;
       }
 
       for (auto iElem = 0ul; iElem < dataSorter->GetnElem(PYRAMID); iElem++) {
         output_file << "14\t";
         for (auto iNode = 0u; iNode < N_POINTS_PYRAMID; ++iNode)
-          output_file << dataSorter->GetElem_Connectivity(PYRAMID, iElem, iNode) - 1 << "\t";
+          output_file << dataSorter->GetElemConnectivity(PYRAMID, iElem, iNode) - 1 << "\t";
         output_file << nElem + offset << "\n"; nElem++;
       }
 
diff --git a/SU2_CFD/src/output/filewriter/CTecplotBinaryFileWriter.cpp b/SU2_CFD/src/output/filewriter/CTecplotBinaryFileWriter.cpp
index 1342cb73cbc..38a5cc20ccc 100644
--- a/SU2_CFD/src/output/filewriter/CTecplotBinaryFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CTecplotBinaryFileWriter.cpp
@@ -39,7 +39,7 @@ CTecplotBinaryFileWriter::CTecplotBinaryFileWriter(CParallelDataSorter *valDataS
 
 CTecplotBinaryFileWriter::~CTecplotBinaryFileWriter(){}
 
-void CTecplotBinaryFileWriter::Write_Data(string val_filename){
+void CTecplotBinaryFileWriter::WriteData(string val_filename){
 
   /*--- We append the pre-defined suffix (extension) to the filename (prefix) ---*/
   val_filename.append(fileExt);
@@ -160,34 +160,34 @@ void CTecplotBinaryFileWriter::Write_Data(string val_filename){
     /* Gather a list of nodes we refer to but are not outputting. */
 
     for (unsigned long i = 0; i < nParallel_Tria * N_POINTS_TRIANGLE; ++i)
-      if ((unsigned long)dataSorter->GetElem_Connectivity(TRIANGLE, 0, i) <= dataSorter->GetNodeBegin(rank) ||
-          dataSorter->GetNodeEnd(rank) < (unsigned long)dataSorter->GetElem_Connectivity(TRIANGLE, 0, i))
-        halo_nodes.insert(dataSorter->GetElem_Connectivity(TRIANGLE, 0, i));
+      if ((unsigned long)dataSorter->GetElemConnectivity(TRIANGLE, 0, i) <= dataSorter->GetNodeBegin(rank) ||
+          dataSorter->GetNodeEnd(rank) < (unsigned long)dataSorter->GetElemConnectivity(TRIANGLE, 0, i))
+        halo_nodes.insert(dataSorter->GetElemConnectivity(TRIANGLE, 0, i));
 
     for (unsigned long i = 0; i < nParallel_Quad * N_POINTS_QUADRILATERAL; ++i)
-      if ((unsigned long)dataSorter->GetElem_Connectivity(QUADRILATERAL, 0, i) <= dataSorter->GetNodeBegin(rank) ||
-          dataSorter->GetNodeEnd(rank) < (unsigned long)dataSorter->GetElem_Connectivity(QUADRILATERAL, 0, i))
-        halo_nodes.insert(dataSorter->GetElem_Connectivity(QUADRILATERAL, 0, i));
+      if ((unsigned long)dataSorter->GetElemConnectivity(QUADRILATERAL, 0, i) <= dataSorter->GetNodeBegin(rank) ||
+          dataSorter->GetNodeEnd(rank) < (unsigned long)dataSorter->GetElemConnectivity(QUADRILATERAL, 0, i))
+        halo_nodes.insert(dataSorter->GetElemConnectivity(QUADRILATERAL, 0, i));
 
     for (unsigned long i = 0; i < nParallel_Tetr * N_POINTS_TETRAHEDRON; ++i)
-      if ((unsigned long)dataSorter->GetElem_Connectivity(TETRAHEDRON, 0, i) <= dataSorter->GetNodeBegin(rank) ||
-          dataSorter->GetNodeEnd(rank) < (unsigned long)dataSorter->GetElem_Connectivity(TETRAHEDRON, 0, i))
-        halo_nodes.insert(dataSorter->GetElem_Connectivity(TETRAHEDRON, 0, i));
+      if ((unsigned long)dataSorter->GetElemConnectivity(TETRAHEDRON, 0, i) <= dataSorter->GetNodeBegin(rank) ||
+          dataSorter->GetNodeEnd(rank) < (unsigned long)dataSorter->GetElemConnectivity(TETRAHEDRON, 0, i))
+        halo_nodes.insert(dataSorter->GetElemConnectivity(TETRAHEDRON, 0, i));
 
     for (unsigned long i = 0; i < nParallel_Hexa * N_POINTS_HEXAHEDRON; ++i)
-      if ((unsigned long)dataSorter->GetElem_Connectivity(HEXAHEDRON, 0, i) <= dataSorter->GetNodeBegin(rank) ||
-          dataSorter->GetNodeEnd(rank) < (unsigned long)dataSorter->GetElem_Connectivity(HEXAHEDRON, 0, i))
-        halo_nodes.insert(dataSorter->GetElem_Connectivity(HEXAHEDRON, 0, i));
+      if ((unsigned long)dataSorter->GetElemConnectivity(HEXAHEDRON, 0, i) <= dataSorter->GetNodeBegin(rank) ||
+          dataSorter->GetNodeEnd(rank) < (unsigned long)dataSorter->GetElemConnectivity(HEXAHEDRON, 0, i))
+        halo_nodes.insert(dataSorter->GetElemConnectivity(HEXAHEDRON, 0, i));
 
     for (unsigned long i = 0; i < nParallel_Pris * N_POINTS_PRISM; ++i)
-      if ((unsigned long)dataSorter->GetElem_Connectivity(PRISM, 0, i) <= dataSorter->GetNodeBegin(rank) ||
-          dataSorter->GetNodeEnd(rank) < (unsigned long)dataSorter->GetElem_Connectivity(PRISM, 0, i))
-        halo_nodes.insert(dataSorter->GetElem_Connectivity(PRISM, 0, i));
+      if ((unsigned long)dataSorter->GetElemConnectivity(PRISM, 0, i) <= dataSorter->GetNodeBegin(rank) ||
+          dataSorter->GetNodeEnd(rank) < (unsigned long)dataSorter->GetElemConnectivity(PRISM, 0, i))
+        halo_nodes.insert(dataSorter->GetElemConnectivity(PRISM, 0, i));
 
     for (unsigned long i = 0; i < nParallel_Pyra * N_POINTS_PYRAMID; ++i)
-      if ((unsigned long)dataSorter->GetElem_Connectivity(PYRAMID, 0, i) <= dataSorter->GetNodeBegin(rank) ||
-          dataSorter->GetNodeEnd(rank) < (unsigned long)dataSorter->GetElem_Connectivity(PYRAMID, 0, i))
-        halo_nodes.insert(dataSorter->GetElem_Connectivity(PYRAMID, 0, i));
+      if ((unsigned long)dataSorter->GetElemConnectivity(PYRAMID, 0, i) <= dataSorter->GetNodeBegin(rank) ||
+          dataSorter->GetNodeEnd(rank) < (unsigned long)dataSorter->GetElemConnectivity(PYRAMID, 0, i))
+        halo_nodes.insert(dataSorter->GetElemConnectivity(PYRAMID, 0, i));
 
     /* Sorted list of halo nodes for this MPI rank. */
     sorted_halo_nodes.assign(halo_nodes.begin(), halo_nodes.end());
@@ -376,11 +376,11 @@ void CTecplotBinaryFileWriter::Write_Data(string val_filename){
   : GetHaloNodeNumber(n, dataSorter->GetNodeEnd(rank) - dataSorter->GetNodeBegin(rank), sorted_halo_nodes)
 
     for (iElem = 0; err == 0 && iElem < nParallel_Tetr; iElem++) {
-      nodes[0] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 0));
-      nodes[1] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 1));
-      nodes[2] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 2));
+      nodes[0] = MAKE_LOCAL(dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 0));
+      nodes[1] = MAKE_LOCAL(dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 1));
+      nodes[2] = MAKE_LOCAL(dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 2));
       nodes[3] = nodes[2];
-      nodes[4] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 3));
+      nodes[4] = MAKE_LOCAL(dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 3));
       nodes[5] = nodes[4];
       nodes[6] = nodes[4];
       nodes[7] = nodes[4];
@@ -389,37 +389,37 @@ void CTecplotBinaryFileWriter::Write_Data(string val_filename){
     }
 
     for (iElem = 0; err == 0 && iElem < nParallel_Hexa; iElem++) {
-      nodes[0] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 0));
-      nodes[1] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 1));
-      nodes[2] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 2));
-      nodes[3] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 3));
-      nodes[4] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 4));
-      nodes[5] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 5));
-      nodes[6] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 6));
-      nodes[7] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 7));
+      nodes[0] = MAKE_LOCAL(dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 0));
+      nodes[1] = MAKE_LOCAL(dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 1));
+      nodes[2] = MAKE_LOCAL(dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 2));
+      nodes[3] = MAKE_LOCAL(dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 3));
+      nodes[4] = MAKE_LOCAL(dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 4));
+      nodes[5] = MAKE_LOCAL(dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 5));
+      nodes[6] = MAKE_LOCAL(dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 6));
+      nodes[7] = MAKE_LOCAL(dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 7));
       err = tecZoneNodeMapWrite64(file_handle, zone, rank + 1, 1, 8, nodes);
       if (err) cout << rank << ": Error outputting Tecplot node values." << endl;
     }
 
     for (iElem = 0; err == 0 && iElem < nParallel_Pris; iElem++) {
-      nodes[0] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(PRISM, iElem, 0));
-      nodes[1] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(PRISM, iElem, 1));
+      nodes[0] = MAKE_LOCAL(dataSorter->GetElemConnectivity(PRISM, iElem, 0));
+      nodes[1] = MAKE_LOCAL(dataSorter->GetElemConnectivity(PRISM, iElem, 1));
       nodes[2] = nodes[1];
-      nodes[3] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(PRISM, iElem, 2));
-      nodes[4] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(PRISM, iElem, 3));
-      nodes[5] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(PRISM, iElem, 4));
+      nodes[3] = MAKE_LOCAL(dataSorter->GetElemConnectivity(PRISM, iElem, 2));
+      nodes[4] = MAKE_LOCAL(dataSorter->GetElemConnectivity(PRISM, iElem, 3));
+      nodes[5] = MAKE_LOCAL(dataSorter->GetElemConnectivity(PRISM, iElem, 4));
       nodes[6] = nodes[5];
-      nodes[7] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(PRISM, iElem, 5));
+      nodes[7] = MAKE_LOCAL(dataSorter->GetElemConnectivity(PRISM, iElem, 5));
       err = tecZoneNodeMapWrite64(file_handle, zone, rank + 1, 1, 8, nodes);
       if (err) cout << rank << ": Error outputting Tecplot node values." << endl;
     }
 
     for (iElem = 0; err == 0 && iElem < nParallel_Pyra; iElem++) {
-      nodes[0] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(PYRAMID, iElem, 0));
-      nodes[1] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(PYRAMID, iElem, 1));
-      nodes[2] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(PYRAMID, iElem, 2));
-      nodes[3] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(PYRAMID, iElem, 3));
-      nodes[4] = MAKE_LOCAL(dataSorter->GetElem_Connectivity(PYRAMID, iElem, 4));
+      nodes[0] = MAKE_LOCAL(dataSorter->GetElemConnectivity(PYRAMID, iElem, 0));
+      nodes[1] = MAKE_LOCAL(dataSorter->GetElemConnectivity(PYRAMID, iElem, 1));
+      nodes[2] = MAKE_LOCAL(dataSorter->GetElemConnectivity(PYRAMID, iElem, 2));
+      nodes[3] = MAKE_LOCAL(dataSorter->GetElemConnectivity(PYRAMID, iElem, 3));
+      nodes[4] = MAKE_LOCAL(dataSorter->GetElemConnectivity(PYRAMID, iElem, 4));
       nodes[5] = nodes[4];
       nodes[6] = nodes[4];
       nodes[7] = nodes[4];
@@ -440,26 +440,26 @@ void CTecplotBinaryFileWriter::Write_Data(string val_filename){
       for(int iRank = 0; iRank < size; ++iRank) {
         if (iRank == rank) {
           for (iElem = 0; err == 0 && iElem < nParallel_Line; iElem++) {
-            nodes[0] = dataSorter->GetElem_Connectivity(LINE, iElem, 0);
-            nodes[1] = dataSorter->GetElem_Connectivity(LINE, iElem, 1);
+            nodes[0] = dataSorter->GetElemConnectivity(LINE, iElem, 0);
+            nodes[1] = dataSorter->GetElemConnectivity(LINE, iElem, 1);
             err = tecZoneNodeMapWrite64(file_handle, zone, 0, 1, 2, nodes);
             if (err) cout << rank << ": Error outputting Tecplot node values." << endl;
           }
 
           for (iElem = 0; err == 0 && iElem < nParallel_Tria; iElem++) {
-            nodes[0] = dataSorter->GetElem_Connectivity(TRIANGLE, iElem, 0);
-            nodes[1] = dataSorter->GetElem_Connectivity(TRIANGLE, iElem, 1);
-            nodes[2] = dataSorter->GetElem_Connectivity(TRIANGLE, iElem, 2);
-            nodes[3] = dataSorter->GetElem_Connectivity(TRIANGLE, iElem, 2);
+            nodes[0] = dataSorter->GetElemConnectivity(TRIANGLE, iElem, 0);
+            nodes[1] = dataSorter->GetElemConnectivity(TRIANGLE, iElem, 1);
+            nodes[2] = dataSorter->GetElemConnectivity(TRIANGLE, iElem, 2);
+            nodes[3] = dataSorter->GetElemConnectivity(TRIANGLE, iElem, 2);
             err = tecZoneNodeMapWrite64(file_handle, zone, 0, 1, 4, nodes);
             if (err) cout << rank << ": Error outputting Tecplot node values." << endl;
           }
 
           for (iElem = 0; err == 0 && iElem < nParallel_Quad; iElem++) {
-            nodes[0] = dataSorter->GetElem_Connectivity(QUADRILATERAL, iElem, 0);
-            nodes[1] = dataSorter->GetElem_Connectivity(QUADRILATERAL, iElem, 1);
-            nodes[2] = dataSorter->GetElem_Connectivity(QUADRILATERAL, iElem, 2);
-            nodes[3] = dataSorter->GetElem_Connectivity(QUADRILATERAL, iElem, 3);
+            nodes[0] = dataSorter->GetElemConnectivity(QUADRILATERAL, iElem, 0);
+            nodes[1] = dataSorter->GetElemConnectivity(QUADRILATERAL, iElem, 1);
+            nodes[2] = dataSorter->GetElemConnectivity(QUADRILATERAL, iElem, 2);
+            nodes[3] = dataSorter->GetElemConnectivity(QUADRILATERAL, iElem, 3);
             err = tecZoneNodeMapWrite64(file_handle, zone, 0, 1, 4, nodes);
             if (err) cout << rank << ": Error outputting Tecplot node values." << endl;
           }
@@ -481,22 +481,22 @@ void CTecplotBinaryFileWriter::Write_Data(string val_filename){
       vector<int64_t> connectivity;
       connectivity.reserve(connectivity_size);
       for (iElem = 0; err == 0 && iElem < nParallel_Line; iElem++) {
-        connectivity.push_back(dataSorter->GetElem_Connectivity(LINE, iElem, 0));
-        connectivity.push_back(dataSorter->GetElem_Connectivity(LINE, iElem, 0));
+        connectivity.push_back(dataSorter->GetElemConnectivity(LINE, iElem, 0));
+        connectivity.push_back(dataSorter->GetElemConnectivity(LINE, iElem, 0));
       }
 
       for (iElem = 0; err == 0 && iElem < nParallel_Tria; iElem++) {
-        connectivity.push_back(dataSorter->GetElem_Connectivity(TRIANGLE, iElem, 0));
-        connectivity.push_back(dataSorter->GetElem_Connectivity(TRIANGLE, iElem, 1));
-        connectivity.push_back(dataSorter->GetElem_Connectivity(TRIANGLE, iElem, 2));
-        connectivity.push_back(dataSorter->GetElem_Connectivity(TRIANGLE, iElem, 2));
+        connectivity.push_back(dataSorter->GetElemConnectivity(TRIANGLE, iElem, 0));
+        connectivity.push_back(dataSorter->GetElemConnectivity(TRIANGLE, iElem, 1));
+        connectivity.push_back(dataSorter->GetElemConnectivity(TRIANGLE, iElem, 2));
+        connectivity.push_back(dataSorter->GetElemConnectivity(TRIANGLE, iElem, 2));
       }
 
       for (iElem = 0; err == 0 && iElem < nParallel_Quad; iElem++) {
-        connectivity.push_back(dataSorter->GetElem_Connectivity(QUADRILATERAL, iElem, 0));
-        connectivity.push_back(dataSorter->GetElem_Connectivity(QUADRILATERAL, iElem, 1));
-        connectivity.push_back(dataSorter->GetElem_Connectivity(QUADRILATERAL, iElem, 2));
-        connectivity.push_back(dataSorter->GetElem_Connectivity(QUADRILATERAL, iElem, 3));
+        connectivity.push_back(dataSorter->GetElemConnectivity(QUADRILATERAL, iElem, 0));
+        connectivity.push_back(dataSorter->GetElemConnectivity(QUADRILATERAL, iElem, 1));
+        connectivity.push_back(dataSorter->GetElemConnectivity(QUADRILATERAL, iElem, 2));
+        connectivity.push_back(dataSorter->GetElemConnectivity(QUADRILATERAL, iElem, 3));
       }
 
       if (connectivity.empty()) connectivity.resize(1); /* Avoid crash */
@@ -508,71 +508,71 @@ void CTecplotBinaryFileWriter::Write_Data(string val_filename){
   int64_t nodes[8];
 
   for (iElem = 0; err == 0 && iElem < nParallel_Tria; iElem++) {
-    nodes[0] = dataSorter->GetElem_Connectivity(TRIANGLE, iElem, 0);
-    nodes[1] = dataSorter->GetElem_Connectivity(TRIANGLE, iElem, 1);
-    nodes[2] = dataSorter->GetElem_Connectivity(TRIANGLE, iElem, 2);
-    nodes[3] = dataSorter->GetElem_Connectivity(TRIANGLE, iElem, 2);
+    nodes[0] = dataSorter->GetElemConnectivity(TRIANGLE, iElem, 0);
+    nodes[1] = dataSorter->GetElemConnectivity(TRIANGLE, iElem, 1);
+    nodes[2] = dataSorter->GetElemConnectivity(TRIANGLE, iElem, 2);
+    nodes[3] = dataSorter->GetElemConnectivity(TRIANGLE, iElem, 2);
     err = tecZoneNodeMapWrite64(file_handle, zone, rank, 1, 4, nodes);
     if (err) cout << rank << ": Error outputting Tecplot node values." << endl;
   }
 
   for (iElem = 0; err == 0 && iElem < nParallel_Quad; iElem++) {
-    nodes[0] = dataSorter->GetElem_Connectivity(QUADRILATERAL, iElem, 0);
-    nodes[1] = dataSorter->GetElem_Connectivity(QUADRILATERAL, iElem, 1);
-    nodes[2] = dataSorter->GetElem_Connectivity(QUADRILATERAL, iElem, 2);
-    nodes[3] = dataSorter->GetElem_Connectivity(QUADRILATERAL, iElem, 3);
+    nodes[0] = dataSorter->GetElemConnectivity(QUADRILATERAL, iElem, 0);
+    nodes[1] = dataSorter->GetElemConnectivity(QUADRILATERAL, iElem, 1);
+    nodes[2] = dataSorter->GetElemConnectivity(QUADRILATERAL, iElem, 2);
+    nodes[3] = dataSorter->GetElemConnectivity(QUADRILATERAL, iElem, 3);
     err = tecZoneNodeMapWrite64(file_handle, zone, rank, 1, 4, nodes);
     if (err) cout << rank << ": Error outputting Tecplot node values." << endl;
   }
 
   for (iElem = 0; err == 0 && iElem < nParallel_Tetr; iElem++) {
-    nodes[0] = dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 0);
-    nodes[1] = dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 1);
-    nodes[2] = dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 2);
-    nodes[3] = dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 2);
-    nodes[4] = dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 3);
-    nodes[5] = dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 3);
-    nodes[6] = dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 3);
-    nodes[7] = dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 3);
+    nodes[0] = dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 0);
+    nodes[1] = dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 1);
+    nodes[2] = dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 2);
+    nodes[3] = dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 2);
+    nodes[4] = dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 3);
+    nodes[5] = dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 3);
+    nodes[6] = dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 3);
+    nodes[7] = dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 3);
     err = tecZoneNodeMapWrite64(file_handle, zone, rank, 1, 8, nodes);
     if (err) cout << rank << ": Error outputting Tecplot node values." << endl;
   }
 
   for (iElem = 0; err == 0 && iElem < nParallel_Hexa; iElem++) {
-    nodes[0] = dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 0);
-    nodes[1] = dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 1);
-    nodes[2] = dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 2);
-    nodes[3] = dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 3);
-    nodes[4] = dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 4);
-    nodes[5] = dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 5);
-    nodes[6] = dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 6);
-    nodes[7] = dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 7);
+    nodes[0] = dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 0);
+    nodes[1] = dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 1);
+    nodes[2] = dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 2);
+    nodes[3] = dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 3);
+    nodes[4] = dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 4);
+    nodes[5] = dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 5);
+    nodes[6] = dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 6);
+    nodes[7] = dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 7);
     err = tecZoneNodeMapWrite64(file_handle, zone, rank, 1, 8, nodes);
     if (err) cout << rank << ": Error outputting Tecplot node values." << endl;
   }
 
   for (iElem = 0; err == 0 && iElem < nParallel_Pris; iElem++) {
-    nodes[0] = dataSorter->GetElem_Connectivity(PRISM, iElem, 0);
-    nodes[1] = dataSorter->GetElem_Connectivity(PRISM, iElem, 1);
-    nodes[2] = dataSorter->GetElem_Connectivity(PRISM, iElem, 1);
-    nodes[3] = dataSorter->GetElem_Connectivity(PRISM, iElem, 2);
-    nodes[4] = dataSorter->GetElem_Connectivity(PRISM, iElem, 3);
-    nodes[5] = dataSorter->GetElem_Connectivity(PRISM, iElem, 4);
-    nodes[6] = dataSorter->GetElem_Connectivity(PRISM, iElem, 4);
-    nodes[7] = dataSorter->GetElem_Connectivity(PRISM, iElem, 5);
+    nodes[0] = dataSorter->GetElemConnectivity(PRISM, iElem, 0);
+    nodes[1] = dataSorter->GetElemConnectivity(PRISM, iElem, 1);
+    nodes[2] = dataSorter->GetElemConnectivity(PRISM, iElem, 1);
+    nodes[3] = dataSorter->GetElemConnectivity(PRISM, iElem, 2);
+    nodes[4] = dataSorter->GetElemConnectivity(PRISM, iElem, 3);
+    nodes[5] = dataSorter->GetElemConnectivity(PRISM, iElem, 4);
+    nodes[6] = dataSorter->GetElemConnectivity(PRISM, iElem, 4);
+    nodes[7] = dataSorter->GetElemConnectivity(PRISM, iElem, 5);
     err = tecZoneNodeMapWrite64(file_handle, zone, rank, 1, 8, nodes);
     if (err) cout << rank << ": Error outputting Tecplot node values." << endl;
   }
 
   for (iElem = 0; err == 0 && iElem < nParallel_Pyra; iElem++) {
-    nodes[0] = dataSorter->GetElem_Connectivity(PYRAMID, iElem, 0);
-    nodes[1] = dataSorter->GetElem_Connectivity(PYRAMID, iElem, 1);
-    nodes[2] = dataSorter->GetElem_Connectivity(PYRAMID, iElem, 2);
-    nodes[3] = dataSorter->GetElem_Connectivity(PYRAMID, iElem, 3);
-    nodes[4] = dataSorter->GetElem_Connectivity(PYRAMID, iElem, 4);
-    nodes[5] = dataSorter->GetElem_Connectivity(PYRAMID, iElem, 4);
-    nodes[6] = dataSorter->GetElem_Connectivity(PYRAMID, iElem, 4);
-    nodes[7] = dataSorter->GetElem_Connectivity(PYRAMID, iElem, 4);
+    nodes[0] = dataSorter->GetElemConnectivity(PYRAMID, iElem, 0);
+    nodes[1] = dataSorter->GetElemConnectivity(PYRAMID, iElem, 1);
+    nodes[2] = dataSorter->GetElemConnectivity(PYRAMID, iElem, 2);
+    nodes[3] = dataSorter->GetElemConnectivity(PYRAMID, iElem, 3);
+    nodes[4] = dataSorter->GetElemConnectivity(PYRAMID, iElem, 4);
+    nodes[5] = dataSorter->GetElemConnectivity(PYRAMID, iElem, 4);
+    nodes[6] = dataSorter->GetElemConnectivity(PYRAMID, iElem, 4);
+    nodes[7] = dataSorter->GetElemConnectivity(PYRAMID, iElem, 4);
     err = tecZoneNodeMapWrite64(file_handle, zone, rank, 1, 8, nodes);
     if (err) cout << rank << ": Error outputting Tecplot node values." << endl;
   }
@@ -592,7 +592,7 @@ void CTecplotBinaryFileWriter::Write_Data(string val_filename){
 
   usedTime = stopTime-startTime;
 
-  fileSize = Determine_Filesize(val_filename);
+  fileSize = DetermineFilesize(val_filename);
 
   /*--- Compute and store the bandwidth ---*/
 
diff --git a/SU2_CFD/src/output/filewriter/CTecplotFileWriter.cpp b/SU2_CFD/src/output/filewriter/CTecplotFileWriter.cpp
index 52fd61e6aa9..5ecf07ad5de 100644
--- a/SU2_CFD/src/output/filewriter/CTecplotFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CTecplotFileWriter.cpp
@@ -35,7 +35,7 @@ CTecplotFileWriter::CTecplotFileWriter(CParallelDataSorter *valDataSorter,
 
 CTecplotFileWriter::~CTecplotFileWriter(){}
 
-void CTecplotFileWriter::Write_Data(string val_filename){
+void CTecplotFileWriter::WriteData(string val_filename){
 
   /*--- We append the pre-defined suffix (extension) to the filename (prefix) ---*/
   val_filename.append(fileExt);
@@ -156,51 +156,51 @@ void CTecplotFileWriter::Write_Data(string val_filename){
     if (rank == iProcessor) {
 
       for (iElem = 0; iElem < nParallel_Line; iElem++) {
-        Tecplot_File << dataSorter->GetElem_Connectivity(LINE, iElem, 0) << "\t";
-        Tecplot_File << dataSorter->GetElem_Connectivity(LINE, iElem, 1)<< "\n";
+        Tecplot_File << dataSorter->GetElemConnectivity(LINE, iElem, 0) << "\t";
+        Tecplot_File << dataSorter->GetElemConnectivity(LINE, iElem, 1)<< "\n";
       }
 
 
       for (iElem = 0; iElem < nParallel_Tria; iElem++) {
-        Tecplot_File << dataSorter->GetElem_Connectivity(TRIANGLE, iElem, 0) << "\t";
-        Tecplot_File << dataSorter->GetElem_Connectivity(TRIANGLE, iElem, 1) << "\t";
-        Tecplot_File << dataSorter->GetElem_Connectivity(TRIANGLE, iElem, 2) << "\t";
-        Tecplot_File << dataSorter->GetElem_Connectivity(TRIANGLE, iElem, 2) << "\n";
+        Tecplot_File << dataSorter->GetElemConnectivity(TRIANGLE, iElem, 0) << "\t";
+        Tecplot_File << dataSorter->GetElemConnectivity(TRIANGLE, iElem, 1) << "\t";
+        Tecplot_File << dataSorter->GetElemConnectivity(TRIANGLE, iElem, 2) << "\t";
+        Tecplot_File << dataSorter->GetElemConnectivity(TRIANGLE, iElem, 2) << "\n";
       }
 
       for (iElem = 0; iElem < nParallel_Quad; iElem++) {
-        Tecplot_File << dataSorter->GetElem_Connectivity(QUADRILATERAL, iElem, 0) << "\t";
-        Tecplot_File << dataSorter->GetElem_Connectivity(QUADRILATERAL, iElem, 1) << "\t";
-        Tecplot_File << dataSorter->GetElem_Connectivity(QUADRILATERAL, iElem, 2) << "\t";
-        Tecplot_File << dataSorter->GetElem_Connectivity(QUADRILATERAL, iElem, 3) << "\n";
+        Tecplot_File << dataSorter->GetElemConnectivity(QUADRILATERAL, iElem, 0) << "\t";
+        Tecplot_File << dataSorter->GetElemConnectivity(QUADRILATERAL, iElem, 1) << "\t";
+        Tecplot_File << dataSorter->GetElemConnectivity(QUADRILATERAL, iElem, 2) << "\t";
+        Tecplot_File << dataSorter->GetElemConnectivity(QUADRILATERAL, iElem, 3) << "\n";
       }
 
       for (iElem = 0; iElem < nParallel_Tetr; iElem++) {
-        Tecplot_File << dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 0) << "\t" << dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 1) << "\t";
-        Tecplot_File << dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 2) << "\t" << dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 2) << "\t";
-        Tecplot_File << dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 3) << "\t" << dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 3) << "\t";
-        Tecplot_File << dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 3) << "\t" << dataSorter->GetElem_Connectivity(TETRAHEDRON, iElem, 3) << "\n";
+        Tecplot_File << dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 0) << "\t" << dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 1) << "\t";
+        Tecplot_File << dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 2) << "\t" << dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 2) << "\t";
+        Tecplot_File << dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 3) << "\t" << dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 3) << "\t";
+        Tecplot_File << dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 3) << "\t" << dataSorter->GetElemConnectivity(TETRAHEDRON, iElem, 3) << "\n";
       }
 
       for (iElem = 0; iElem < nParallel_Hexa; iElem++) {
-        Tecplot_File << dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 0) << "\t" << dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 1) << "\t";
-        Tecplot_File << dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 2) << "\t" << dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 3) << "\t";
-        Tecplot_File << dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 4) << "\t" << dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 5) << "\t";
-        Tecplot_File << dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 6) << "\t" << dataSorter->GetElem_Connectivity(HEXAHEDRON, iElem, 7) << "\n";
+        Tecplot_File << dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 0) << "\t" << dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 1) << "\t";
+        Tecplot_File << dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 2) << "\t" << dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 3) << "\t";
+        Tecplot_File << dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 4) << "\t" << dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 5) << "\t";
+        Tecplot_File << dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 6) << "\t" << dataSorter->GetElemConnectivity(HEXAHEDRON, iElem, 7) << "\n";
       }
 
       for (iElem = 0; iElem < nParallel_Pris; iElem++) {
-        Tecplot_File << dataSorter->GetElem_Connectivity(PRISM, iElem, 0) << "\t" << dataSorter->GetElem_Connectivity(PRISM, iElem, 1) << "\t";
-        Tecplot_File << dataSorter->GetElem_Connectivity(PRISM, iElem, 1) << "\t" << dataSorter->GetElem_Connectivity(PRISM, iElem, 2) << "\t";
-        Tecplot_File << dataSorter->GetElem_Connectivity(PRISM, iElem, 3) << "\t" << dataSorter->GetElem_Connectivity(PRISM, iElem, 4) << "\t";
-        Tecplot_File << dataSorter->GetElem_Connectivity(PRISM, iElem, 4) << "\t" << dataSorter->GetElem_Connectivity(PRISM, iElem, 5) << "\n";
+        Tecplot_File << dataSorter->GetElemConnectivity(PRISM, iElem, 0) << "\t" << dataSorter->GetElemConnectivity(PRISM, iElem, 1) << "\t";
+        Tecplot_File << dataSorter->GetElemConnectivity(PRISM, iElem, 1) << "\t" << dataSorter->GetElemConnectivity(PRISM, iElem, 2) << "\t";
+        Tecplot_File << dataSorter->GetElemConnectivity(PRISM, iElem, 3) << "\t" << dataSorter->GetElemConnectivity(PRISM, iElem, 4) << "\t";
+        Tecplot_File << dataSorter->GetElemConnectivity(PRISM, iElem, 4) << "\t" << dataSorter->GetElemConnectivity(PRISM, iElem, 5) << "\n";
       }
 
       for (iElem = 0; iElem < nParallel_Pyra; iElem++) {
-        Tecplot_File << dataSorter->GetElem_Connectivity(PYRAMID, iElem, 0) << "\t" << dataSorter->GetElem_Connectivity(PYRAMID, iElem, 1) << "\t";
-        Tecplot_File << dataSorter->GetElem_Connectivity(PYRAMID, iElem, 2) << "\t" << dataSorter->GetElem_Connectivity(PYRAMID, iElem, 3) << "\t";
-        Tecplot_File << dataSorter->GetElem_Connectivity(PYRAMID, iElem, 4) << "\t" << dataSorter->GetElem_Connectivity(PYRAMID, iElem, 4) << "\t";
-        Tecplot_File << dataSorter->GetElem_Connectivity(PYRAMID, iElem, 4) << "\t" << dataSorter->GetElem_Connectivity(PYRAMID, iElem, 4) << "\n";
+        Tecplot_File << dataSorter->GetElemConnectivity(PYRAMID, iElem, 0) << "\t" << dataSorter->GetElemConnectivity(PYRAMID, iElem, 1) << "\t";
+        Tecplot_File << dataSorter->GetElemConnectivity(PYRAMID, iElem, 2) << "\t" << dataSorter->GetElemConnectivity(PYRAMID, iElem, 3) << "\t";
+        Tecplot_File << dataSorter->GetElemConnectivity(PYRAMID, iElem, 4) << "\t" << dataSorter->GetElemConnectivity(PYRAMID, iElem, 4) << "\t";
+        Tecplot_File << dataSorter->GetElemConnectivity(PYRAMID, iElem, 4) << "\t" << dataSorter->GetElemConnectivity(PYRAMID, iElem, 4) << "\n";
       }
 
 
@@ -219,7 +219,7 @@ void CTecplotFileWriter::Write_Data(string val_filename){
 
   usedTime = stopTime-startTime;
 
-  fileSize = Determine_Filesize(val_filename);
+  fileSize = DetermineFilesize(val_filename);
 
   /*--- Compute and store the bandwidth ---*/
 
diff --git a/SU2_CFD/src/output/output_structure_legacy.cpp b/SU2_CFD/src/output/output_structure_legacy.cpp
index cdf6a468c74..40e495d6b66 100644
--- a/SU2_CFD/src/output/output_structure_legacy.cpp
+++ b/SU2_CFD/src/output/output_structure_legacy.cpp
@@ -340,7 +340,7 @@ COutputLegacy::~COutputLegacy(void) {
   }
 }
 
-void COutputLegacy::SetConvHistory_Header(ofstream *ConvHist_file, CConfig *config, unsigned short val_iZone, unsigned short val_iInst) {
+void COutputLegacy::SetConvHistoryHeader(ofstream *ConvHist_file, CConfig *config, unsigned short val_iZone, unsigned short val_iInst) {
   char cstr[200], turb_resid[1000], adj_turb_resid[1000];
   unsigned short iMarker_Monitoring;
   string Monitoring_Tag, monitoring_coeff, aeroelastic_coeff, turbo_coeff;
@@ -590,7 +590,7 @@ void COutputLegacy::SetConvHistory_Header(ofstream *ConvHist_file, CConfig *conf
 }
 
 
-void COutputLegacy::SetConvHistory_Body(ofstream *ConvHist_file,
+void COutputLegacy::SetConvHistoryBody(ofstream *ConvHist_file,
                                   CGeometry ****geometry,
                                   CSolver *****solver_container,
                                   CConfig **config,
@@ -650,21 +650,21 @@ void COutputLegacy::SetConvHistory_Body(ofstream *ConvHist_file,
           /*--- For specific applications, evaluate and plot the surface. ---*/
 
           if (config[val_iZone]->GetnMarker_Analyze() != 0) {
-            SpecialOutput_AnalyzeSurface(solver_container[val_iZone][val_iInst][MESH_0][FLOW_SOL],
+            SpecialOutputAnalyzeSurface(solver_container[val_iZone][val_iInst][MESH_0][FLOW_SOL],
                                          geometry[val_iZone][val_iInst][MESH_0], config[val_iZone], output_files);
           }
 
           /*--- For specific applications, evaluate and plot the surface. ---*/
 
           if ((config[val_iZone]->GetnMarker_Analyze() != 0) && compressible) {
-            SpecialOutput_Distortion(solver_container[val_iZone][val_iInst][MESH_0][FLOW_SOL],
+            SpecialOutputDistortion(solver_container[val_iZone][val_iInst][MESH_0][FLOW_SOL],
                                      geometry[val_iZone][val_iInst][MESH_0], config[val_iZone], output_files);
           }
 
           /*--- For specific applications, evaluate and plot the cp coefficent at different stations. ---*/
 
           if (config[val_iZone]->GetPlot_Section_Forces()) {
-            SpecialOutput_SpanLoad(solver_container[val_iZone][val_iInst][MESH_0][FLOW_SOL],
+            SpecialOutputSpanLoad(solver_container[val_iZone][val_iInst][MESH_0][FLOW_SOL],
                                    geometry[val_iZone][val_iInst][MESH_0], config[val_iZone], output_files);
           }
 
@@ -677,18 +677,18 @@ void COutputLegacy::SetConvHistory_Body(ofstream *ConvHist_file,
       /*--- Output a file with the forces breakdown. ---*/
 
       if (config[val_iZone]->GetTime_Marching() == TIME_MARCHING::HARMONIC_BALANCE) {
-        SpecialOutput_HarmonicBalance(solver_container, geometry, config, val_iInst, nInst, output_files);
+        SpecialOutputHarmonicBalance(solver_container, geometry, config, val_iInst, nInst, output_files);
       }
 
       /*--- Compute span-wise values file for turbomachinery. ---*/
 
       if (config[val_iZone]->GetBoolTurbomachinery()) {
-        SpecialOutput_Turbo(solver_container, geometry, config, val_iZone, output_files);
+        SpecialOutputTurbo(solver_container, geometry, config, val_iZone, output_files);
       }
 
       /*--- Output a file with the forces breakdown. ---*/
 
-      SpecialOutput_ForcesBreakdown(solver_container, geometry, config, val_iZone, output_files);
+      SpecialOutputForcesBreakdown(solver_container, geometry, config, val_iZone, output_files);
 
       if ((rank == MASTER_NODE) && output_files) cout << "-------------------------------------------------------------------------" << endl << endl;
 
@@ -2424,7 +2424,7 @@ void COutputLegacy::SetConvHistory_Body(ofstream *ConvHist_file,
   }
 }
 
-void COutputLegacy::SpecialOutput_ForcesBreakdown(CSolver *****solver, CGeometry ****geometry, CConfig **config, unsigned short val_iZone, bool output) const {
+void COutputLegacy::SpecialOutputForcesBreakdown(CSolver *****solver, CGeometry ****geometry, CConfig **config, unsigned short val_iZone, bool output) const {
 
   char cstr[200];
   unsigned short iDim, iMarker_Monitoring;
@@ -4278,7 +4278,7 @@ void COutputLegacy::SpecialOutput_ForcesBreakdown(CSolver *****solver, CGeometry
 
 }
 
-void COutputLegacy::SpecialOutput_SpanLoad(CSolver *solver, CGeometry *geometry, CConfig *config, bool output) const {
+void COutputLegacy::SpecialOutputSpanLoad(CSolver *solver, CGeometry *geometry, CConfig *config, bool output) const {
 
   short iSection, nSection;
   unsigned long iVertex, iPoint, Trailing_Point;
@@ -4694,7 +4694,7 @@ void COutputLegacy::SpecialOutput_SpanLoad(CSolver *solver, CGeometry *geometry,
 }
 
 
-void COutputLegacy::SetCp_InverseDesign(CSolver *solver_container, CGeometry *geometry, CConfig *config, unsigned long iExtIter) {
+void COutputLegacy::SetCpInverseDesign(CSolver *solver_container, CGeometry *geometry, CConfig *config, unsigned long iExtIter) {
 
   unsigned short iMarker, icommas, Boundary, iDim;
   unsigned long iVertex, iPoint, (*Point2Vertex)[2], nPointLocal = 0, nPointGlobal = 0;
@@ -4845,7 +4845,7 @@ void COutputLegacy::SetCp_InverseDesign(CSolver *solver_container, CGeometry *ge
 
 }
 
-void COutputLegacy::SetHeatFlux_InverseDesign(CSolver *solver_container, CGeometry *geometry, CConfig *config, unsigned long iExtIter) {
+void COutputLegacy::SetHeatFluxInverseDesign(CSolver *solver_container, CGeometry *geometry, CConfig *config, unsigned long iExtIter) {
 
   unsigned short iMarker, icommas, Boundary, iDim;
   unsigned long iVertex, iPoint, (*Point2Vertex)[2], nPointLocal = 0, nPointGlobal = 0;
@@ -4998,7 +4998,7 @@ void COutputLegacy::SetHeatFlux_InverseDesign(CSolver *solver_container, CGeomet
 
 
 
-void COutputLegacy::SpecialOutput_Distortion(CSolver *solver, CGeometry *geometry, CConfig *config, bool output) const {
+void COutputLegacy::SpecialOutputDistortion(CSolver *solver, CGeometry *geometry, CConfig *config, bool output) const {
 
   unsigned short iMarker, iDim, iMarker_Analyze;
   unsigned long iPoint, iVertex;
@@ -6349,7 +6349,7 @@ void COutputLegacy::WriteTurboPerfConvHistory(CConfig *config){
 
 }
 
-void COutputLegacy::SpecialOutput_Turbo(CSolver *****solver, CGeometry ****geometry, CConfig **config,
+void COutputLegacy::SpecialOutputTurbo(CSolver *****solver, CGeometry ****geometry, CConfig **config,
                                        unsigned short val_iZone, bool output) {
 
   string inMarker_Tag, outMarker_Tag, inMarkerTag_Mix;
@@ -6602,7 +6602,7 @@ void COutputLegacy::SpecialOutput_Turbo(CSolver *****solver, CGeometry ****geome
   }
 }
 
-void COutputLegacy::SpecialOutput_HarmonicBalance(CSolver *****solver, CGeometry ****geometry, CConfig **config, unsigned short iInst, unsigned short val_nInst, bool output) const {
+void COutputLegacy::SpecialOutputHarmonicBalance(CSolver *****solver, CGeometry ****geometry, CConfig **config, unsigned short iInst, unsigned short val_nInst, bool output) const {
 
   /*--- Write file with flow quantities for harmonic balance HB ---*/
   ofstream HB_output_file;
@@ -6693,7 +6693,7 @@ void COutputLegacy::SpecialOutput_HarmonicBalance(CSolver *****solver, CGeometry
   delete [] averages;
 }
 
-void COutputLegacy::SetSpecial_Output(CSolver *****solver_container,
+void COutputLegacy::SetSpecialOutput(CSolver *****solver_container,
                                        CGeometry ****geometry,
                                        CConfig **config,
                                        unsigned long iExtIter,
@@ -6708,13 +6708,13 @@ void COutputLegacy::SetSpecial_Output(CSolver *****solver_container,
 
     /*--- Output a file with the forces breakdown. ---*/
     if (config[iZone]->GetWrt_ForcesBreakdown())
-      SpecialOutput_ForcesBreakdown(solver_container, geometry, config, iZone, special_output);
+      SpecialOutputForcesBreakdown(solver_container, geometry, config, iZone, special_output);
 
   }
 
 }
 
-void COutputLegacy::SpecialOutput_AnalyzeSurface(CSolver *solver, CGeometry *geometry, CConfig *config, bool output) const {
+void COutputLegacy::SpecialOutputAnalyzeSurface(CSolver *solver, CGeometry *geometry, CConfig *config, bool output) const {
 
   unsigned short iDim, iMarker, iMarker_Analyze;
   unsigned long iVertex, iPoint;
diff --git a/SU2_CFD/src/output/tools/CWindowingTools.cpp b/SU2_CFD/src/output/tools/CWindowingTools.cpp
index 1178fb06db4..b14190b897c 100644
--- a/SU2_CFD/src/output/tools/CWindowingTools.cpp
+++ b/SU2_CFD/src/output/tools/CWindowingTools.cpp
@@ -66,7 +66,7 @@ su2double CWindowingTools::BumpWindow(unsigned long curTimeIter, unsigned long e
    * and it acts as a normalization constant */
 }
 
-void CWindowedAverage::addValue(su2double valIn, unsigned long curTimeIter,unsigned long startIter){
+void CWindowedAverage::AddValue(su2double valIn, unsigned long curTimeIter,unsigned long startIter){
   if (curTimeIter < startIter) return;  // Averaging not yet started.
   const unsigned long windowWidth = curTimeIter - startIter + 1;  // Calculate total width of window for this iteration
   if (curTimeIter != lastTimeIter) {           // Handle new timestep
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 6aa13a0d6c3..d78fc102eac 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -499,15 +499,15 @@ void CDeformationDriver::Output() {
 
     /*--- Load the data. --- */
 
-    output_container[iZone]->Load_Data(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], nullptr);
+    output_container[iZone]->LoadData(geometry_container[iZone][INST_0][MESH_0], config_container[iZone], nullptr);
 
     output_container[iZone]->WriteToFile(config_container[iZone], geometry_container[iZone][INST_0][MESH_0],
                                          OUTPUT_TYPE::MESH, driver_config->GetMesh_Out_FileName());
 
     /*--- Set the file names for the visualization files. ---*/
 
-    output_container[iZone]->SetVolume_Filename("volume_deformed");
-    output_container[iZone]->SetSurface_Filename("surface_deformed");
+    output_container[iZone]->SetVolumeFilename("volume_deformed");
+    output_container[iZone]->SetSurfaceFilename("surface_deformed");
 
     for (unsigned short iFile = 0; iFile < config_container[iZone]->GetnVolumeOutputFiles(); iFile++) {
       auto FileFormat = config_container[iZone]->GetVolumeOutputFiles();
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index 775515de672..9e40f154243 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -881,15 +881,15 @@ void CDiscAdjDeformationDriver::SetSensitivity_Files(CGeometry**** geometry, CCo
 
     /*--- Load the data. --- */
 
-    output->Load_Data(geometry[iZone][INST_0][MESH_0], config[iZone], &solver);
+    output->LoadData(geometry[iZone][INST_0][MESH_0], config[iZone], &solver);
 
     /*--- Set the surface filename. ---*/
 
-    output->SetSurface_Filename(config[iZone]->GetSurfSens_FileName());
+    output->SetSurfaceFilename(config[iZone]->GetSurfSens_FileName());
 
     /*--- Set the volume filename. ---*/
 
-    output->SetVolume_Filename(config[iZone]->GetVolSens_FileName());
+    output->SetVolumeFilename(config[iZone]->GetVolSens_FileName());
 
     /*--- Write to file. ---*/
 
diff --git a/SU2_SOL/src/SU2_SOL.cpp b/SU2_SOL/src/SU2_SOL.cpp
index 3f7a3385165..1d8aa6093b9 100644
--- a/SU2_SOL/src/SU2_SOL.cpp
+++ b/SU2_SOL/src/SU2_SOL.cpp
@@ -764,17 +764,17 @@ void WriteFiles(CConfig* config, CGeometry* geometry, CSolver** solver_container
                 unsigned long TimeIter) {
   /*--- Load history data (volume output might require some values) --- */
 
-  output->SetHistory_Output(geometry, solver_container, config, TimeIter, 0, 0);
+  output->SetHistoryOutput(geometry, solver_container, config, TimeIter, 0, 0);
 
   /*--- Load the data --- */
 
-  output->Load_Data(geometry, config, solver_container);
+  output->LoadData(geometry, config, solver_container);
 
   /*--- Set the filenames ---*/
 
-  output->SetVolume_Filename(config->GetVolume_FileName());
+  output->SetVolumeFilename(config->GetVolume_FileName());
 
-  output->SetSurface_Filename(config->GetSurfCoeff_FileName());
+  output->SetSurfaceFilename(config->GetSurfCoeff_FileName());
 
   for (unsigned short iFile = 0; iFile < config->GetnVolumeOutputFiles(); iFile++) {
     auto FileFormat = config->GetVolumeOutputFiles();
diff --git a/UnitTests/SU2_CFD/windowing.cpp b/UnitTests/SU2_CFD/windowing.cpp
index 1cb8e3f21d4..960e28e4fc0 100644
--- a/UnitTests/SU2_CFD/windowing.cpp
+++ b/UnitTests/SU2_CFD/windowing.cpp
@@ -63,7 +63,7 @@ struct CWindowingTest {
         weightCurrent = innerIteration;
         // Simulate gradual change of sample during inner iterations.
         input = (weightPrevious * previousSample + weightCurrent * currentSample) / (weightCurrent + weightPrevious);
-        avg.addValue(input, outerIteration, startIteration);
+        avg.AddValue(input, outerIteration, startIteration);
       }
     }
     return avg.GetVal();

From 1c990e093eb861bdaac88bd8e2e36c5143c66ddb Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 28 Mar 2023 15:10:42 +0200
Subject: [PATCH 321/656] Replaced multi-layer perceptron classes with external
 submodule

---
 .github/workflows/regression.yml              |   2 +-
 .gitmodules                                   |   3 +
 .../multilayer_perceptron/CIOMap.hpp          | 190 ---------
 .../multilayer_perceptron/CLayer.hpp          | 152 --------
 .../multilayer_perceptron/CLookUp_ANN.hpp     | 119 ------
 .../multilayer_perceptron/CNeuralNetwork.hpp  | 319 ---------------
 .../multilayer_perceptron/CNeuron.hpp         | 121 ------
 .../CReadNeuralNetwork.hpp                    | 156 --------
 Common/src/toolboxes/meson.build              |   6 -
 .../multilayer_perceptron/CIOMap.cpp          |  81 ----
 .../multilayer_perceptron/CLayer.cpp          |  49 ---
 .../multilayer_perceptron/CLookUp_ANN.cpp     | 261 -------------
 .../multilayer_perceptron/CNeuralNetwork.cpp  | 366 ------------------
 .../CReadNeuralNetwork.cpp                    | 207 ----------
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp    |  18 +-
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        |  21 +-
 .../CLookUp_ANN_tests.cpp                     |  35 +-
 externals/medi                                |   2 +-
 externals/meson                               |   2 +-
 externals/ninja                               |   2 +-
 externals/opdi                                |   2 +-
 meson.build                                   |  15 +-
 meson_options.txt                             |   1 +
 meson_scripts/init.py                         |  11 +-
 preconfigure.py                               |   6 +
 subprojects/CoolProp                          |   2 +-
 subprojects/MLPCpp                            |   1 +
 subprojects/Mutationpp                        |   2 +-
 28 files changed, 90 insertions(+), 2062 deletions(-)
 delete mode 100644 Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
 delete mode 100644 Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
 delete mode 100644 Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
 delete mode 100644 Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
 delete mode 100644 Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
 delete mode 100644 Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
 delete mode 100644 Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
 delete mode 100644 Common/src/toolboxes/multilayer_perceptron/CLayer.cpp
 delete mode 100644 Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
 delete mode 100644 Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
 delete mode 100644 Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
 create mode 160000 subprojects/MLPCpp

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 01a61c8c949..7459b112429 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -26,7 +26,7 @@ jobs:
         config_set: [BaseMPI, ReverseMPI, ForwardMPI, BaseNoMPI, ReverseNoMPI, ForwardNoMPI, BaseOMP, ReverseOMP, ForwardOMP]
         include:
           - config_set: BaseMPI
-            flags: '-Denable-pywrapper=true -Denable-coolprop=true -Denable-tests=true --warnlevel=2 --werror'
+            flags: '-Denable-pywrapper=true -Denable-coolprop=true -Denable-mlpcpp=true -Denable-tests=true --warnlevel=2 --werror'
           - config_set: ReverseMPI
             flags: '-Denable-autodiff=true -Denable-normal=false -Denable-pywrapper=true -Denable-tests=true --warnlevel=3 --werror'
           - config_set: ForwardMPI
diff --git a/.gitmodules b/.gitmodules
index c7e70424d90..2c655cb36da 100644
--- a/.gitmodules
+++ b/.gitmodules
@@ -24,3 +24,6 @@
 [submodule "externals/mel"]
 	path = externals/mel
 	url = https://github.com/pcarruscag/MEL.git
+[submodule "subprojects/MLPCpp"]
+	path = subprojects/MLPCpp
+	url = https://github.com/EvertBunschoten/MLPCpp.git
diff --git a/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp b/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
deleted file mode 100644
index 5263823b460..00000000000
--- a/Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp
+++ /dev/null
@@ -1,190 +0,0 @@
-/*!
- * \file CIOMap.hpp
- * \brief Declaration of input-to-output mapping class for artifical neural networks
- * \author E. Bunschoten
- * \version 7.5.1 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-#pragma once
-
-#include <cmath>
-#include <cstdlib>
-#include <iostream>
-#include <limits>
-#include <string>
-#include <vector>
-
-#include "../../containers/C2DContainer.hpp"
-#include "CLookUp_ANN.hpp"
-
-namespace MLPToolbox {
-
-class CLookUp_ANN;
-
-class CIOMap
-/*!
- *\class CIOMap
- *\brief This class is used by the CLookUp_ANN class to assign user-defined inputs
- * and outputs to loaded multi-layer perceptrons. When a look-up operation is called
- * with a specific CIOMap, the multi-layer perceptrons are evaluated with input and
- * output variables coinciding with the desired input and output variable names.
- *
- *
- * For example, in a custom, data-driven fluid model, MLP's are used for thermodynamic state
- * definition. There are three MLP's loaded. MLP_1 predicts temperature and specific heat
- * based on density and energy. MLP_2 predicts pressure and speed of sound based on density and
- * energy as well. MLP_3 predicts density and energy based on pressure and temperature.
- * During a certain look-up operation in the CFluidModel, temperature, speed of sound and pressure
- * are needed for a given density and energy. What the CIOMap does is to point to MLP_1 for
- * temperature evalutation, and to MLP_2 for pressure and speed of sound evaluation. MLP_3 is
- * not considered, as the respective inputs and outputs don't match with the function call
- * inputs and outputs.
- *
- *  call variables:      MLP inputs:                     MLP outputs:           call outputs:
- *
- *                        2--> energy --|            |--> temperature --> 1
- *                                      |--> MLP_1 --|
- *  1:density            1--> density --|            |--> c_p                   1:temperature
- *  2:energy                                                                    2:speed of sound
- *                       1--> density --|            |--> pressure --> 3        3:pressure
- *                                      |--> MLP_2 --|
- *                        2--> energy --|            |--> speed of sound --> 2
- *
- *                           pressure --|            |--> density
- *                                      |--> MLP_3 --|
- *                        temperature --|            |--> energy
- *
- *
- * \author E.Bunschoten
- */
-
-{
- private:
-  std::vector<std::size_t> MLP_indices; /*!< Loaded MLP index */
-
-  std::vector<std::vector<std::pair<std::size_t, std::size_t>>>
-      Input_Map,  /*!< Mapping of call variable inputs to matching MLP inputs */
-      Output_Map; /*!< Mapping of call variable outputs to matching MLP outputs */
-
- public:
-  /*!
-   * \brief CIOMap class constructor;
-   * \param[in] MLP_collection - Pointer to CLookUp_ANN class for which the input-output amap is to be created
-   * \param[in] inputs - Input names for the call function. These should match with at least one of the MLP inputs.
-   * \param[in] outputs - Output names for the call function. These should match with at least one of the MLP outputs.
-   */
-  CIOMap(CLookUp_ANN* MLP_collection, su2vector<std::string>& inputs, su2vector<std::string>& outputs);
-
-  /*!
-   * \brief Set MLP index in IO map
-   * \param[in] iMLP - loaded MLP index
-   */
-  void PushMLPindex(std::size_t iMLP) { MLP_indices.push_back(iMLP); }
-
-  /*!
-  * \brief Pair call inputs and outputs with the inputs and outputs of
-          the loaded MLPs
-  * \param[in] MLP_collection - pointer to MLP collection class
-  * \param[in] inputs - vector with call input variable names
-  * \param[in] outputs - vector with call output variable names
-  */
-  void PairVariableswithMLPs(CLookUp_ANN* MLP_collection, su2vector<std::string>& inputs,
-                             su2vector<std::string>& outputs);
-
-  /*!
-   * \brief Get the number of MLPs in the current IO map
-   * \return number of MLPs with matching inputs and output(s)
-   */
-  std::size_t GetNMLPs() const { return MLP_indices.size(); }
-
-  /*!
-   * \brief Get the loaded MLP index
-   * \return MLP index
-   */
-  std::size_t GetMLPIndex(std::size_t i_Map) const { return MLP_indices[i_Map]; }
-
-  /*!
-   * \brief Get the call input variable index
-   * \param[in] i_Map - input-output mapping index of the IO map
-   * \param[in] iInput - input index of the call input variable
-   * \return MLP input variable index
-   */
-  std::size_t GetInputIndex(std::size_t i_Map, std::size_t iInput) const { return Input_Map[i_Map][iInput].first; }
-
-  /*!
-   * \brief Get the call output variable index
-   * \param[in] i_Map - input-output mapping index of the IO map
-   * \param[in] iOutput - output index of the call input variable
-   * \return call variable output index
-   */
-  std::size_t GetOutputIndex(std::size_t i_Map, std::size_t iOutput) const { return Output_Map[i_Map][iOutput].first; }
-
-  /*!
-   * \brief Get the MLP output variable index
-   * \param[in] i_Map - input-output mapping index of the IO map
-   * \param[in] iOutput - output index of the call input variable
-   * \return MLP output variable index
-   */
-  std::size_t GetMLPOutputIndex(std::size_t i_Map, std::size_t iOutput) const {
-    return Output_Map[i_Map][iOutput].second;
-  }
-
-  /*!
-   * \brief Get the number of matching output variables between the call and MLP outputs
-   * \param[in] i_Map - input-output mapping index of the IO map
-   * \return Number of matching variables between the loaded MLP and call variables
-   */
-  std::size_t GetNMappedOutputs(std::size_t i_Map) const { return Output_Map[i_Map].size(); }
-
-  /*!
-   * \brief Get the mapping of MLP outputs matching to call outputs
-   * \param[in] i_Map - input-output mapping index of the IO map
-   * \return Mapping of MLP output variables to call variables
-   */
-  std::vector<std::pair<std::size_t, std::size_t>> GetOutputMapping(std::size_t i_map) const {
-    return Output_Map[i_map];
-  }
-
-  /*!
-   * \brief Get the mapping of MLP inputs to call inputs
-   * \param[in] i_Map - input-output mapping index of the IO map
-   * \return Mapping of MLP input variables to call inputs
-   */
-  std::vector<std::pair<std::size_t, std::size_t>> GetInputMapping(std::size_t i_map) const { return Input_Map[i_map]; }
-
-  /*!
-   * \brief Get the mapped inputs for the MLP at i_Map
-   * \param[in] i_Map - input-output mapping index of the IO map
-   * \param[in] inputs - call inputs
-   * \return Vector with call inputs in the correct order of the loaded MLP
-   */
-  su2vector<su2double> GetMLPInputs(std::size_t i_Map, su2vector<su2double>& inputs) const {
-    su2vector<su2double> MLP_input;
-    MLP_input.resize(Input_Map[i_Map].size());
-
-    for (std::size_t iInput = 0; iInput < Input_Map[i_Map].size(); iInput++) {
-      MLP_input[iInput] = inputs[GetInputIndex(i_Map, iInput)];
-    }
-    return MLP_input;
-  }
-};
-}  // namespace MLPToolbox
diff --git a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp b/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
deleted file mode 100644
index 4171de0e2ba..00000000000
--- a/Common/include/toolboxes/multilayer_perceptron/CLayer.hpp
+++ /dev/null
@@ -1,152 +0,0 @@
-/*!
- * \file CLayer.hpp
- * \brief Declaration of artificial neural network interpolation class
- * \author E. Bunschoten
- * \version 7.5.1 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-#pragma once
-
-#include <cmath>
-#include <cstdlib>
-#include <iostream>
-#include <limits>
-#include <vector>
-
-#include "../../containers/C2DContainer.hpp"
-#include "CNeuron.hpp"
-
-namespace MLPToolbox {
-class CLayer {
-  /*!
-   *\class CLayer
-   *\brief This class functions as one of the hidden, input, or output layers in the multi-layer perceptron
-   * class. The CLayer class is used to communicate information (activation function inputs and outputs and gradients)
-   * between the CNeuralNetwork class and the CNeuron class. Currently, only a single activation function
-   * can be applied to the neuron inputs within the layer.
-   */
- private:
-  unsigned long number_of_neurons; /*!< Neuron count in current layer */
-  su2vector<CNeuron> neurons;      /*!< Array of neurons in current layer */
-  bool is_input;                   /*!< Input layer identifyer */
-  std::string activation_type;     /*!< Activation function type applied to the current layer*/
- public:
-  CLayer();
-  CLayer(unsigned long n_neurons);
-  /*!
-   * \brief Set current layer neuron count
-   * \param[in] n_neurons - Number of neurons in this layer
-   */
-  void SetNNeurons(unsigned long n_neurons);
-
-  /*!
-   * \brief Get the current layer neuron count
-   * \return Neuron count
-   */
-  unsigned long GetNNeurons() const { return number_of_neurons; }
-
-  /*!
-   * \brief Define current layer as input layer
-   * \param[in] input - input layer identifyer
-   */
-  void SetInput(bool def) { is_input = def; }
-
-  /*!
-   * \brief Get input layer identifyer
-   * \return input layer identifyer
-   */
-  bool IsInput() const { return is_input; }
-
-  /*!
-   * \brief Set the output value of a neuron in the layer
-   * \param[in] i_neuron - Neuron index
-   * \param[in] output_value - Activation function output
-   */
-  void SetOutput(std::size_t i_neuron, su2double value) { neurons[i_neuron].SetOutput(value); }
-
-  /*!
-   * \brief Get the output value of a neuron in the layer
-   * \param[in] i_neuron - Neuron index
-   * \return Neuron output value
-   */
-  su2double GetOutput(std::size_t i_neuron) const { return neurons[i_neuron].GetOutput(); }
-
-  /*!
-   * \brief Set the input value of a neuron in the layer
-   * \param[in] i_neuron - Neuron index
-   * \param[in] input_value - Activation function input
-   */
-  void SetInput(std::size_t i_neuron, su2double value) { neurons[i_neuron].SetInput(value); }
-
-  /*!
-   * \brief Get the input value of a neuron in the layer
-   * \param[in] i_neuron - Neuron index
-   * \return Neuron input value
-   */
-  su2double GetInput(std::size_t i_neuron) const { return neurons[i_neuron].GetInput(); }
-
-  /*!
-   * \brief Set the bias value of a neuron in the layer
-   * \param[in] i_neuron - Neuron index
-   * \param[in] bias_value - Bias value
-   */
-  void SetBias(std::size_t i_neuron, su2double value) { neurons[i_neuron].SetBias(value); }
-
-  /*!
-   * \brief Get the bias value of a neuron in the layer
-   * \param[in] i_neuron - Neuron index
-   * \return Neuron bias value
-   */
-  su2double GetBias(std::size_t i_neuron) const { return neurons[i_neuron].GetBias(); }
-
-  /*!
-   * \brief Get the output-input gradient of a neuron in the layer
-   * \param[in] i_neuron - Neuron index
-   * \return Gradient of neuron output wrt input
-   */
-  su2double GetdYdX(std::size_t i_neuron, std::size_t iInput) const { return neurons[i_neuron].GetGradient(iInput); }
-
-  /*!
-   * \brief Get the output-input gradient of a neuron in the layer
-   * \param[in] i_neuron - Neuron index
-   * \return Gradient of neuron output wrt input
-   */
-  void SetdYdX(std::size_t i_neuron, std::size_t iInput, su2double dy_dx) {
-    neurons[i_neuron].SetGradient(iInput, dy_dx);
-  }
-
-  /*!
-   * \brief Size neuron output derivative wrt network inputs.
-   * \param[in] nInputs - Number of network inputs.
-   */
-  void SizeGradients(std::size_t nInputs) {
-    for (auto iNeuron = 0u; iNeuron < number_of_neurons; iNeuron++) neurons[iNeuron].SizeGradient(nInputs);
-  }
-
-  /*!
-   * \brief Get the activation function name applied to this layer
-   * \return name of the activation function
-   */
-  std::string GetActivationType() const { return activation_type; }
-};
-
-}  // namespace MLPToolbox
diff --git a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp b/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
deleted file mode 100644
index 4c4a65a9a67..00000000000
--- a/Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp
+++ /dev/null
@@ -1,119 +0,0 @@
-/*!
- * \file CLookUp_ANN.hpp
- * \brief Declaration of artificial neural network interpolation class
- * \author E. Bunschoten
- * \version 7.5.1 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-
-#pragma once
-
-#include <cmath>
-#include <cstdlib>
-#include <iostream>
-#include <limits>
-#include <string>
-#include <vector>
-
-#include "../../containers/C2DContainer.hpp"
-#include "CIOMap.hpp"
-#include "CNeuralNetwork.hpp"
-
-namespace MLPToolbox {
-
-class CLookUp_ANN {
-  /*!
-   *\class CLookUp_ANN
-   *\brief This class allows for the evaluation of one or more multi-layer perceptrons in for example
-   * thermodynamic state look-up operations. The multi-layer perceptrons are loaded in the order listed
-   * in the MLP collection file. Each multi-layer perceptron is generated based on the
-   * architecture described in its respective input file. When evaluating the MLP collection, an
-   * input-output map is used to find the correct MLP corresponding to the call function inputs and
-   * outputs.
-   */
-
- private:
-  su2vector<CNeuralNetwork> NeuralNetworks; /*!< std::vector containing all loaded neural networks. */
-
-  unsigned short number_of_variables; /*!< Number of loaded ANNs. */
-
-  /*!
-   * \brief Load ANN architecture
-   * \param[in] ANN - pointer to target NeuralNetwork class
-   * \param[in] filename - filename containing ANN architecture information
-   */
-  void GenerateANN(CNeuralNetwork& ANN, std::string filename);
-
- public:
-  /*!
-   * \brief ANN collection class constructor
-   * \param[in] n_inputs - Number of MLP files to be loaded.
-   * \param[in] input_filenames - String array containing MLP input file names.
-   */
-  CLookUp_ANN(const unsigned short n_inputs, const std::string* input_filenames);
-
-  /*!
-   * \brief Evaluate loaded ANNs for given inputs and outputs
-   * \param[in] input_output_map - input-output map coupling desired inputs and outputs to loaded ANNs
-   * \param[in] inputs - input values
-   * \param[in] outputs - pointers to output variables
-   * \returns Within output normalization range.
-   */
-  unsigned long PredictANN(CIOMap* input_output_map, su2vector<su2double>& inputs, su2vector<su2double*>& outputs);
-
-  /*!
-   * \brief Get number of loaded ANNs
-   * \return number of loaded ANNs
-   */
-  std::size_t GetNANNs() const { return NeuralNetworks.size(); }
-
-  /*!
-   * \brief Check if all output variables are present in the loaded ANNs
-   * \param[in] output_names - output variable names to check
-   * \param[in] input_output_map - pointer to input-output map to be checked
-   */
-  bool CheckUseOfOutputs(su2vector<std::string>& output_names, CIOMap* input_output_map) const;
-
-  /*!
-   * \brief Check if all input variables are present in the loaded ANNs
-   * \param[in] input_names - input variable names to check
-   * \param[in] input_output_map - pointer to input-output map to be checked
-   */
-  bool CheckUseOfInputs(su2vector<std::string>& input_names, CIOMap* input_output_map) const;
-
-  /*!
-   * \brief Map variable names to ANN inputs or outputs
-   * \param[in] i_ANN - loaded ANN index
-   * \param[in] variable_names - variable names to map to ANN inputs or outputs
-   * \param[in] input - map to inputs (true) or outputs (false)
-   */
-  std::vector<std::pair<std::size_t, std::size_t>> FindVariableIndices(std::size_t i_ANN,
-                                                                       su2vector<std::string> variable_names,
-                                                                       bool input) const;
-
-  /*!
-   * \brief Display architectural information on the loaded MLPs
-   */
-  void DisplayNetworkInfo() const;
-};
-
-}  // namespace MLPToolbox
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
deleted file mode 100644
index 5f1140b93b9..00000000000
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp
+++ /dev/null
@@ -1,319 +0,0 @@
-/*!
- * \file CNeuralNetwork.hpp
- * \brief Declaration of the neural network class
- * \author E.C.Bunschoten
- * \version 7.5.1 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-
-#pragma once
-
-#include <cmath>
-#include <cstdlib>
-#include <cstring>
-#include <iostream>
-#include <limits>
-#include <map>
-
-#include "../../containers/C2DContainer.hpp"
-#include "CLayer.hpp"
-
-namespace MLPToolbox {
-class CNeuralNetwork {
-  /*!
-   *\class CNeuralNetwork
-   *\brief The CNeuralNetwork class allows for the evaluation of a loaded MLP architecture for
-   * a given set of inputs. The class also contains a list of the various supported activation
-   * function types (linear, relu, elu, gelu, selu, sigmoid, swish, tanh, exp)which can be
-   * applied to the layers in the network. Currently, only dense, feed-forward type neural
-   * nets are supported in this implementation.
-   */
- private:
-  su2vector<std::string> input_names, /*!< MLP input variable names. */
-      output_names;                   /*!< MLP output variable names. */
-
-  unsigned long n_hidden_layers = 0; /*!< Number of hidden layers (layers between input and output layer). */
-
-  CLayer *inputLayer = nullptr, /*!< Pointer to network input layer. */
-      *outputLayer = nullptr;   /*!< Pointer to network output layer. */
-
-  std::vector<CLayer*> hiddenLayers; /*!< Hidden layer collection. */
-  su2vector<CLayer*> total_layers;   /*!< Hidden layers plus in/output layers */
-
-  su2vector<su2activematrix> weights_mat; /*!< Weights of synapses connecting layers */
-
-  su2vector<std::pair<su2double, su2double>> input_norm, /*!< Normalization factors for network inputs */
-      output_norm;                                       /*!< Normalization factors for network outputs */
-
-  su2vector<su2double> last_inputs; /*!< Inputs from previous lookup operation. Evaluation of the network */
-                                    /*!< is skipped if current inputs are the same as the last inputs. */
-
-  su2double* ANN_outputs;                /*!< Pointer to network outputs */
-  su2matrix<su2double> dOutputs_dInputs; /*!< Network output derivatives w.r.t inputs */
-
-  /*!
-   * \brief Available activation function enumeration.
-   */
-  enum class ENUM_ACTIVATION_FUNCTION {
-    NONE = 0,
-    LINEAR = 1,
-    RELU = 2,
-    ELU = 3,
-    GELU = 4,
-    SELU = 5,
-    SIGMOID = 6,
-    SWISH = 7,
-    TANH = 8,
-    EXPONENTIAL = 9
-  };
-
-  /*!
-   * \brief Available activation function map.
-   */
-  std::map<std::string, ENUM_ACTIVATION_FUNCTION> activation_function_map{
-      {"none", ENUM_ACTIVATION_FUNCTION::NONE},
-      {"linear", ENUM_ACTIVATION_FUNCTION::LINEAR},
-      {"elu", ENUM_ACTIVATION_FUNCTION::ELU},
-      {"relu", ENUM_ACTIVATION_FUNCTION::RELU},
-      {"gelu", ENUM_ACTIVATION_FUNCTION::GELU},
-      {"selu", ENUM_ACTIVATION_FUNCTION::SELU},
-      {"sigmoid", ENUM_ACTIVATION_FUNCTION::SIGMOID},
-      {"swish", ENUM_ACTIVATION_FUNCTION::SWISH},
-      {"tanh", ENUM_ACTIVATION_FUNCTION::TANH},
-      {"exponential", ENUM_ACTIVATION_FUNCTION::EXPONENTIAL}};
-
-  su2vector<ENUM_ACTIVATION_FUNCTION>
-      activation_function_types;               /*!< Activation function type for each layer in the network. */
-  su2vector<std::string> activation_function_names; /*!< Activation function name for each layer in the network. */
-
- public:
-  ~CNeuralNetwork() {
-    delete inputLayer;
-    delete outputLayer;
-    for (std::size_t i = 1; i < total_layers.size() - 1; i++) {
-      delete total_layers[i];
-    }
-    delete[] ANN_outputs;
-  };
-  /*!
-   * \brief Set the input layer of the network.
-   * \param[in] n_neurons - Number of inputs
-   */
-  void DefineInputLayer(unsigned long n_neurons);
-
-  /*!
-   * \brief Set the output layer of the network.
-   * \param[in] n_neurons - Number of outputs
-   */
-  void DefineOutputLayer(unsigned long n_neurons);
-
-  /*!
-   * \brief Add a hidden layer to the network
-   * \param[in] n_neurons - Hidden layer size.
-   */
-  void PushHiddenLayer(unsigned long n_neurons);
-
-  /*!
-   * \brief Set the weight value of a specific synapse.
-   * \param[in] i_layer - current layer.
-   * \param[in] i_neuron - neuron index in current layer.
-   * \param[in] j_neuron - neuron index of connecting neuron.
-   * \param[in] value - weight value.
-   */
-  void SetWeight(unsigned long i_layer, unsigned long i_neuron, unsigned long j_neuron, su2double value) {
-    weights_mat[i_layer][j_neuron][i_neuron] = value;
-  };
-
-  /*!
-   * \brief Set bias value at a specific neuron.
-   * \param[in] i_layer - Layer index.
-   * \param[in] i_neuron - Neuron index of current layer.
-   * \param[in] value - Bias value.
-   */
-  void SetBias(unsigned long i_layer, unsigned long i_neuron, su2double value) {
-    total_layers[i_layer]->SetBias(i_neuron, value);
-  }
-
-  /*!
-   * \brief Set layer activation function.
-   * \param[in] i_layer - Layer index.
-   * \param[in] input - Activation function name.
-   */
-  void SetActivationFunction(unsigned long i_layer, std::string input);
-
-  /*!
-   * \brief Display the network architecture in the terminal.
-   */
-  void DisplayNetwork() const;
-
-  /*!
-   * \brief Size the weight layers in the network according to its architecture.
-   */
-  void SizeWeights();
-
-  /*!
-   * \brief Size the vector of previous inputs.
-   * \param[in] n_inputs - Number of inputs.
-   */
-  void SizeInputs(unsigned long n_inputs) {
-    last_inputs.resize(n_inputs);
-    for (unsigned long iInput = 0; iInput < n_inputs; iInput++) last_inputs[iInput] = 0.0;
-  }
-
-  /*!
-   * \brief Get the number of connecting regions in the network.
-   * \returns number of spaces in between layers.
-   */
-  unsigned long GetNWeightLayers() const { return total_layers.size() - 1; }
-
-  /*!
-   * \brief Get the total number of layers in the network
-   * \returns number of netowork layers.
-   */
-  unsigned long GetNLayers() const { return total_layers.size(); }
-
-  /*!
-   * \brief Get neuron count in a layer.
-   * \param[in] iLayer - Layer index.
-   * \returns number of neurons in the layer.
-   */
-  unsigned long GetNNeurons(unsigned long iLayer) const { return total_layers[iLayer]->GetNNeurons(); }
-
-  /*!
-   * \brief Evaluate the network.
-   * \param[in] inputs - Network input variable values.
-   * \param[in] compute_gradient - Compute the derivatives of the outputs wrt inputs.
-   */
-  void Predict(su2vector<su2double>& inputs, bool compute_gradient = false);
-
-  /*!
-   * \brief Set the normalization factors for the input layer
-   * \param[in] iInput - Input index.
-   * \param[in] input_min - Minimum input value.
-   * \param[in] input_max - Maximum input value.
-   */
-  void SetInputNorm(unsigned long iInput, su2double input_min, su2double input_max) {
-    input_norm[iInput] = std::make_pair(input_min, input_max);
-  }
-
-  /*!
-   * \brief Set the normalization factors for the output layer
-   * \param[in] iOutput - Input index.
-   * \param[in] input_min - Minimum output value.
-   * \param[in] input_max - Maximum output value.
-   */
-  void SetOutputNorm(unsigned long iOutput, su2double output_min, su2double output_max) {
-    output_norm[iOutput] = std::make_pair(output_min, output_max);
-  }
-
-  std::pair<su2double, su2double> GetInputNorm(unsigned long iInput) const { return input_norm[iInput]; }
-
-  std::pair<su2double, su2double> GetOutputNorm(unsigned long iOutput) const { return output_norm[iOutput]; }
-  /*!
-   * \brief Add an output variable name to the network.
-   * \param[in] input - Input variable name.
-   */
-  void SetOutputName(size_t iOutput, std::string input) { output_names[iOutput] = input; }
-
-  /*!
-   * \brief Add an input variable name to the network.
-   * \param[in] output - Output variable name.
-   */
-  void SetInputName(size_t iInput, std::string input) { input_names[iInput] = input; }
-
-  /*!
-   * \brief Get network input variable name.
-   * \param[in] iInput - Input variable index.
-   * \returns input variable name.
-   */
-  std::string GetInputName(std::size_t iInput) const { return input_names[iInput]; }
-
-  /*!
-   * \brief Get network output variable name.
-   * \param[in] iOutput - Output variable index.
-   * \returns output variable name.
-   */
-  std::string GetOutputName(std::size_t iOutput) const { return output_names[iOutput]; }
-
-  /*!
-   * \brief Get network number of inputs.
-   * \returns Number of network inputs
-   */
-  std::size_t GetnInputs() const { return input_names.size(); }
-
-  /*!
-   * \brief Get network number of outputs.
-   * \returns Number of network outputs
-   */
-  std::size_t GetnOutputs() const { return output_names.size(); }
-
-  /*!
-   * \brief Get network evaluation output.
-   * \param[in] iOutput - output index.
-   * \returns Prediction value.
-   */
-  su2double GetANNOutput(std::size_t iOutput) const { return ANN_outputs[iOutput]; }
-
-  /*!
-   * \brief Get network output derivative w.r.t specific input.
-   * \param[in] iOutput - output variable index.
-   * \param[in] iInput - input variable index.
-   * \returns Output derivative w.r.t input.
-   */
-  su2double GetdOutputdInput(std::size_t iOutput, std::size_t iInput) const {
-    return dOutputs_dInputs[iOutput][iInput];
-  }
-
-  /*!
-   * \brief Set the activation function array size.
-   * \param[in] n_layers - network layer count.
-   */
-  void SizeActivationFunctions(unsigned long n_layers) {
-    activation_function_types.resize(n_layers);
-    activation_function_names.resize(n_layers);
-  }
-
-  /*!
-   * \brief Compute neuron activation function input.
-   * \param[in] iLayer - Network layer index.
-   * \param[in] iNeuron - Layer neuron index.
-   * \returns Neuron activation function input.
-   */
-  su2double ComputeX(std::size_t iLayer, std::size_t iNeuron) const {
-    su2double x;
-    x = total_layers[iLayer]->GetBias(iNeuron);
-    std::size_t nNeurons_previous = total_layers[iLayer - 1]->GetNNeurons();
-    for (std::size_t jNeuron = 0; jNeuron < nNeurons_previous; jNeuron++) {
-      x += weights_mat[iLayer - 1][iNeuron][jNeuron] * total_layers[iLayer - 1]->GetOutput(jNeuron);
-    }
-    return x;
-  }
-  su2double ComputedOutputdInput(std::size_t iLayer, std::size_t iNeuron, std::size_t iInput) const {
-    su2double doutput_dinput = 0;
-    for (auto jNeuron = 0u; jNeuron < total_layers[iLayer - 1]->GetNNeurons(); jNeuron++) {
-      doutput_dinput += weights_mat[iLayer - 1][iNeuron][jNeuron] * total_layers[iLayer - 1]->GetdYdX(jNeuron, iInput);
-    }
-    return doutput_dinput;
-  }
-};
-
-}  // namespace MLPToolbox
diff --git a/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp b/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
deleted file mode 100644
index a84b8c5de74..00000000000
--- a/Common/include/toolboxes/multilayer_perceptron/CNeuron.hpp
+++ /dev/null
@@ -1,121 +0,0 @@
-/*!
- * \file CNeuron.hpp
- * \brief Declaration of artificial neural network perceptron class
- * \author E. Bunschoten
- * \version 7.5.1 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-#pragma once
-
-#include <cmath>
-#include <cstdlib>
-#include <iostream>
-#include <limits>
-
-#include "../../containers/C2DContainer.hpp"
-
-namespace MLPToolbox {
-class CNeuron {
-  /*!
-   *\class CNeuron
-   *\brief This class functions as a neuron within the CLayer class, making up the
-   * CNeuralNetwork class. The CNeuron class functions as a location to store activation
-   * function inputs and outputs, as well as gradients and biases. These are accessed
-   * through the CLayer class for network evalution operations.
-   */
- private:
-  unsigned long i_neuron; /*!< Neuron identification number */
-  su2double output{0},    /*!< Output value of the current neuron */
-      input{0},           /*!< Input value of the current neuron */
-      doutput_dinput{0},  /*!< Gradient of output with respect to input */
-      bias{0};            /*!< Bias value at current neuron */
-  su2vector<su2double> doutput_dinputs;
-
- public:
-  /*!
-   * \brief Set neuron identification number
-   * \param[in] input - Identification number
-   */
-  void SetNumber(unsigned long input) { i_neuron = input; }
-
-  /*!
-   * \brief Get neuron identification number
-   * \return Identification number
-   */
-  unsigned long GetNumber() const { return i_neuron; }
-
-  /*!
-   * \brief Set neuron output value
-   * \param[in] input - activation function output value
-   */
-  void SetOutput(su2double input) { output = input; }
-
-  /*!
-   * \brief Get neuron output value
-   * \return Output value
-   */
-  su2double GetOutput() const { return output; }
-
-  /*!
-   * \brief Set neuron input value
-   * \param[in] input - activation function input value
-   */
-  void SetInput(su2double x) { input = x; }
-
-  /*!
-   * \brief Get neuron input value
-   * \return input value
-   */
-  su2double GetInput() const { return input; }
-
-  /*!
-   * \brief Set neuron bias
-   * \param[in] input - bias value
-   */
-  void SetBias(su2double input) { bias = input; }
-
-  /*!
-   * \brief Get neuron bias value
-   * \return bias value
-   */
-  su2double GetBias() const { return bias; }
-
-  /*!
-   * \brief Size the derivative of the neuron output wrt MLP inputs.
-   * \param[in] nInputs - Number of MLP inputs.
-   */
-  void SizeGradient(std::size_t nInputs) { doutput_dinputs.resize(nInputs); }
-
-  /*!
-   * \brief Set neuron output gradient with respect to its input value
-   * \param[in] input - Derivative of activation function with respect to input
-   */
-  void SetGradient(std::size_t iInput, su2double input) { doutput_dinputs[iInput] = input; }
-
-  /*!
-   * \brief Get neuron output gradient with respect to input value
-   * \return output gradient wrt input value
-   */
-  su2double GetGradient(std::size_t iInput) const { return doutput_dinputs[iInput]; }
-};
-
-}  // namespace MLPToolbox
diff --git a/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp b/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
deleted file mode 100644
index 1963b6b24d8..00000000000
--- a/Common/include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp
+++ /dev/null
@@ -1,156 +0,0 @@
-/*!
- * \file CReadNeuralNetwork.hpp
- * \brief Declaration of MLP input file reader class
- * \author E. Bunschoten
- * \version 7.5.1 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-#pragma once
-
-#include <cmath>
-#include <cstdlib>
-#include <iostream>
-#include <limits>
-#include <vector>
-
-#include "../../containers/C2DContainer.hpp"
-namespace MLPToolbox {
-
-class CReadNeuralNetwork {
- private:
-  su2vector<std::string> input_names, /*!< Input variable names. */
-      output_names;                   /*!< Output variable names. */
-
-  std::string filename; /*!< MLP input filename. */
-
-  unsigned long n_layers; /*!< Network total layer count. */
-
-  su2vector<unsigned long> n_neurons; /*!<  Neuron count per layer. */
-
-  su2vector<su2activematrix> weights_mat; /*!< Network synapse weights. */
-
-  su2vector<su2vector<su2double>> biases_mat; /*!< Bias values per neuron. */
-
-  su2vector<std::string> activation_functions; /*!< Activation function per layer. */
-
-  su2vector<std::pair<su2double, su2double>> input_norm, /*!< Input variable normalization values (min, max). */
-      output_norm;                                       /*!< Output variable normalization values (min, max). */
- public:
-  /*!
-   * \brief CReadNeuralNetwork class constructor
-   * \param[in] filename_in - .mlp input file name containing network information.
-   */
-  CReadNeuralNetwork(std::string filename_in);
-
-  /*!
-   * \brief Read input file and store necessary information
-   */
-  void ReadMLPFile();
-
-  /*!
-   * \brief Go to a specific line in file.
-   * \param[in] file_stream - input file stream.
-   * \param[in] flag - line to be skipped to.
-   * \returns flag line
-   */
-  std::string SkipToFlag(std::ifstream* file_stream, std::string flag);
-
-  /*!
-   * \brief Get number of read input variables.
-   * \returns Number of neurons in the input layer.
-   */
-  unsigned long GetNInputs() const { return n_neurons[0]; }
-
-  /*!
-   * \brief Get number of read output variables.
-   * \returns Number of neurons in the output layer.
-   */
-  unsigned long GetNOutputs() const { return n_neurons[n_layers - 1]; }
-
-  /*!
-   * \brief Get total number of layers in the network.
-   * \returns Total layer count.
-   */
-  unsigned long GetNlayers() const { return n_layers; }
-
-  /*!
-   * \brief Get neuron count of a specific layer.
-   * \param[in] iLayer - Total layer index.
-   * \returns Number of neurons in the layer.
-   */
-  unsigned long GetNneurons(std::size_t iLayer) const { return n_neurons[iLayer]; }
-
-  /*!
-   * \brief Get synapse weight between two neurons in subsequent layers.
-   * \param[in] iLayer - Total layer index.
-   * \param[in] iNeuron - Neuron index in layer with index iLayer.
-   * \param[in] jNeuron - Neuron index in subsequent layer.
-   * \returns Weight value
-   */
-  su2double GetWeight(std::size_t iLayer, std::size_t iNeuron, std::size_t jNeuron) const {
-    return weights_mat[iLayer][iNeuron][jNeuron];
-  }
-
-  /*!
-   * \brief Get bias value of specific neuron.
-   * \param[in] iLayer - Total layer index.
-   * \param[in] iNeuron - Neuron index.
-   * \returns Bias value
-   */
-  su2double GetBias(std::size_t iLayer, std::size_t iNeuron) const { return biases_mat[iLayer][iNeuron]; }
-
-  /*!
-   * \brief Get input variable normalization values.
-   * \param[in] iInput - Input variable index.
-   * \returns Input normalization values (min first, max second)
-   */
-  std::pair<su2double, su2double> GetInputNorm(std::size_t iInput) const { return input_norm[iInput]; }
-
-  /*!
-   * \brief Get output variable normalization values.
-   * \param[in] iOutput - Input variable index.
-   * \returns Output normalization values (min first, max second)
-   */
-  std::pair<su2double, su2double> GetOutputNorm(std::size_t iOutput) const { return output_norm[iOutput]; }
-
-  /*!
-   * \brief Get layer activation function type.
-   * \param[in] iLayer - Total layer index.
-   * \returns Layer activation function type.
-   */
-  std::string GetActivationFunction(std::size_t iLayer) const { return activation_functions[iLayer]; }
-
-  /*!
-   * \brief Get input variable name.
-   * \param[in] iInput - Input variable index.
-   * \returns Input variable name.
-   */
-  std::string GetInputName(std::size_t iInput) const { return input_names[iInput]; }
-
-  /*!
-   * \brief Get output variable name.
-   * \param[in] iOutput - Output variable index.
-   * \returns Output variable name.
-   */
-  std::string GetOutputName(std::size_t iOutput) const { return output_names[iOutput]; }
-};
-}  // namespace MLPToolbox
diff --git a/Common/src/toolboxes/meson.build b/Common/src/toolboxes/meson.build
index e51c9e0f6e0..d95ffad5992 100644
--- a/Common/src/toolboxes/meson.build
+++ b/Common/src/toolboxes/meson.build
@@ -5,9 +5,3 @@ common_src += files(['CLinearPartitioner.cpp',
                      'CSymmetricMatrix.cpp'])
 
 subdir('MMS')
-
-common_src += files(['multilayer_perceptron/CLookUp_ANN.cpp',
-                     'multilayer_perceptron/CIOMap.cpp',
-                     'multilayer_perceptron/CNeuralNetwork.cpp',
-                     'multilayer_perceptron/CLayer.cpp',
-                     'multilayer_perceptron/CReadNeuralNetwork.cpp'])
diff --git a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp b/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
deleted file mode 100644
index ec4245f487d..00000000000
--- a/Common/src/toolboxes/multilayer_perceptron/CIOMap.cpp
+++ /dev/null
@@ -1,81 +0,0 @@
-/*!
- * \file CIOMap.cpp
- * \brief Implementation of the input-output mapping class for the
- *      use of multi-layer perceptrons in SU2
- * \author E. Bunschoten
- * \version 7.5.1 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-
-#include <cmath>
-#include <fstream>
-#include <iostream>
-#include <string>
-
-#include "../../../include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp"
-#include "../../../include/toolboxes/multilayer_perceptron/CIOMap.hpp"
-
-MLPToolbox::CIOMap::CIOMap(CLookUp_ANN* MLP_collection, su2vector<std::string>& inputs,
-                           su2vector<std::string>& outputs) {
-  /* Generate an input-output map given a set of call inputs and call outputs. These inputs
-mapped to the inputs of the loaded MLPs in the MLP_collection object. The call outputs are
-then matched to the MLPs with matching inputs.
-*/
-  PairVariableswithMLPs(MLP_collection, inputs, outputs);
-
-  // Perform checks on input-output validity
-  if (outputs.size() > 0) {
-    // Check wether all call inputs are used
-    MLP_collection->CheckUseOfInputs(inputs, this);
-
-    // Check wether all call outputs are present in the MLP collection
-    MLP_collection->CheckUseOfOutputs(outputs, this);
-  }
-}
-void MLPToolbox::CIOMap::PairVariableswithMLPs(CLookUp_ANN* MLP_collection, su2vector<std::string>& inputs,
-                                               su2vector<std::string>& outputs) {
-  /*
-  In this function, the call inputs and outputs are matched to those within the MLP collection.
-  */
-  bool isInput, isOutput;
-
-  // Looping over the loaded MLPs to check wether the MLP inputs match with the call inputs
-  for (size_t iMLP = 0; iMLP < MLP_collection->GetNANNs(); iMLP++) {
-    // Mapped call inputs to MLP inputs
-    std::vector<std::pair<size_t, size_t>> Input_Indices = MLP_collection->FindVariableIndices(iMLP, inputs, true);
-    isInput = Input_Indices.size() > 0;
-
-    if (isInput) {
-      // Only when the MLP inputs match with a portion of the call inputs are the output variable checks performed
-
-      std::vector<std::pair<size_t, size_t>> Output_Indices = MLP_collection->FindVariableIndices(iMLP, outputs, false);
-      isOutput = Output_Indices.size() > 0;
-
-      if (isOutput) {
-        // Update input and output mapping if both inputs and outputs match
-        MLP_indices.push_back(iMLP);
-        Input_Map.push_back(Input_Indices);
-        Output_Map.push_back(Output_Indices);
-      }
-    }
-  }
-}
diff --git a/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp b/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp
deleted file mode 100644
index 86e6a05076b..00000000000
--- a/Common/src/toolboxes/multilayer_perceptron/CLayer.cpp
+++ /dev/null
@@ -1,49 +0,0 @@
-/*!
- * \file CLayer.cpp
- * \brief Implementation of the Layer class to be used in the NeuralNetwork
- *      class
- * \author E. Bunschoten
- * \version 7.5.1 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-#include "../../../include/toolboxes/multilayer_perceptron/CLayer.hpp"
-
-#include <cstring>
-using namespace std;
-
-MLPToolbox::CLayer::CLayer() : CLayer(1) {}
-
-MLPToolbox::CLayer::CLayer(unsigned long n_neurons) : number_of_neurons{n_neurons}, is_input{false} {
-  neurons.resize(n_neurons);
-  for (size_t i = 0; i < number_of_neurons; i++) {
-    neurons[i].SetNumber(i + 1);
-  }
-}
-
-void MLPToolbox::CLayer::SetNNeurons(unsigned long n_neurons) {
-  if (number_of_neurons != n_neurons) {
-    neurons.resize(n_neurons);
-    for (size_t i = 0; i < number_of_neurons; i++) {
-      neurons[i].SetNumber(i + 1);
-    }
-  }
-}
diff --git a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp b/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
deleted file mode 100644
index 7a2894bcd58..00000000000
--- a/Common/src/toolboxes/multilayer_perceptron/CLookUp_ANN.cpp
+++ /dev/null
@@ -1,261 +0,0 @@
-/*!
- * \file CLookUp_ANN.cpp
- * \brief Implementation of the multi-layer perceptron class to be
- *      used for look-up operations.
- * \author E.C.Bunschoten
- * \version 7.5.1 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-#include "../../../include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp"
-
-#include <cmath>
-#include <fstream>
-#include <iomanip>
-#include <iostream>
-#include <string>
-
-#include "../../../include/toolboxes/multilayer_perceptron/CIOMap.hpp"
-#include "../../../include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp"
-
-using namespace std;
-
-MLPToolbox::CLookUp_ANN::CLookUp_ANN(const unsigned short n_inputs, const string* input_filenames) {
-  /*--- Define collection of MLPs for regression purposes ---*/
-  number_of_variables = n_inputs;
-
-  NeuralNetworks.resize(n_inputs);
-
-  /*--- Generate an MLP for every filename provided ---*/
-  for (auto i_MLP = 0u; i_MLP < n_inputs; i_MLP++) {
-    GenerateANN(NeuralNetworks[i_MLP], input_filenames[i_MLP]);
-  }
-}
-
-vector<pair<size_t, size_t>> MLPToolbox::CLookUp_ANN::FindVariableIndices(size_t i_ANN,
-                                                                          su2vector<string> variable_names,
-                                                                          bool input) const {
-  /*--- Find loaded MLPs that have the same input variable names as the variables listed in variable_names ---*/
-
-  vector<pair<size_t, size_t>> variable_indices;
-  auto nVar = input ? NeuralNetworks[i_ANN].GetnInputs() : NeuralNetworks[i_ANN].GetnOutputs();
-
-  for (auto iVar = 0u; iVar < nVar; iVar++) {
-    for (auto jVar = 0u; jVar < variable_names.size(); jVar++) {
-      string ANN_varname = input ? NeuralNetworks[i_ANN].GetInputName(iVar) : NeuralNetworks[i_ANN].GetOutputName(iVar);
-      if (variable_names[jVar].compare(ANN_varname) == 0) {
-        variable_indices.push_back(make_pair(jVar, iVar));
-      }
-    }
-  }
-  return variable_indices;
-}
-
-unsigned long MLPToolbox::CLookUp_ANN::PredictANN(CIOMap* input_output_map, su2vector<su2double>& inputs,
-                                                  su2vector<su2double*>& outputs) {
-  /*--- Evaluate MLP based on target input and output variables ---*/
-  bool within_range,              // Within MLP training set range.
-      MLP_was_evaluated = false;  // MLP was evaluated within training set range.
-
-  /* If queries lie outside the training data set, the nearest MLP will be evaluated through extrapolation. */
-  su2double distance_to_query = 1e20;  // Overall smallest distance between training data set middle and query.
-  size_t i_ANN_nearest = 0,            // Index of nearest MLP.
-      i_map_nearest = 0;               // Index of nearest iomap index.
-
-  for (auto i_map = 0u; i_map < input_output_map->GetNMLPs(); i_map++) {
-    within_range = true;
-    auto i_ANN = input_output_map->GetMLPIndex(i_map);
-    auto ANN_inputs = input_output_map->GetMLPInputs(i_map, inputs);
-
-    su2double distance_to_query_i = 0;
-    for (auto i_input = 0u; i_input < ANN_inputs.size(); i_input++) {
-      auto ANN_input_limits = NeuralNetworks[i_ANN].GetInputNorm(i_input);
-
-      /* Check if query input lies outside MLP training range */
-      if ((ANN_inputs[i_input] < ANN_input_limits.first) || (ANN_inputs[i_input] > ANN_input_limits.second)) {
-        within_range = false;
-      }
-
-      /* Calculate distance between MLP training range center point and query */
-      su2double middle = 0.5 * (ANN_input_limits.second + ANN_input_limits.first);
-      distance_to_query_i +=
-          pow((ANN_inputs[i_input] - middle) / (ANN_input_limits.second - ANN_input_limits.first), 2);
-    }
-
-    /* Evaluate MLP when query inputs lie within training data range */
-    if (within_range) {
-      NeuralNetworks[i_ANN].Predict(ANN_inputs);
-      MLP_was_evaluated = true;
-      for (auto i = 0u; i < input_output_map->GetNMappedOutputs(i_map); i++) {
-        *outputs[input_output_map->GetOutputIndex(i_map, i)] =
-            NeuralNetworks[i_ANN].GetANNOutput(input_output_map->GetMLPOutputIndex(i_map, i));
-      }
-    }
-
-    /* Update minimum distance to query */
-    if (sqrt(distance_to_query_i) < distance_to_query) {
-      i_ANN_nearest = i_ANN;
-      distance_to_query = distance_to_query_i;
-      i_map_nearest = i_map;
-    }
-  }
-  /* Evaluate nearest MLP in case no query data within range is found */
-  if (!MLP_was_evaluated) {
-    auto ANN_inputs = input_output_map->GetMLPInputs(i_map_nearest, inputs);
-    NeuralNetworks[i_ANN_nearest].Predict(ANN_inputs);
-    for (auto i = 0u; i < input_output_map->GetNMappedOutputs(i_map_nearest); i++) {
-      *outputs[input_output_map->GetOutputIndex(i_map_nearest, i)] =
-          NeuralNetworks[i_ANN_nearest].GetANNOutput(input_output_map->GetMLPOutputIndex(i_map_nearest, i));
-    }
-  }
-
-  /* Return 1 if query data lies outside the range of any of the loaded MLPs */
-  return MLP_was_evaluated ? 0 : 1;
-}
-
-void MLPToolbox::CLookUp_ANN::GenerateANN(CNeuralNetwork& ANN, string fileName) {
-  /*--- Generate MLP architecture based on information in MLP input file ---*/
-
-  /* Read MLP input file */
-  CReadNeuralNetwork Reader = CReadNeuralNetwork(fileName);
-
-  /* Read MLP input file */
-  Reader.ReadMLPFile();
-
-  /* Generate basic layer architectures */
-  ANN.DefineInputLayer(Reader.GetNInputs());
-  ANN.SizeInputs(Reader.GetNInputs());
-  for (auto iInput = 0u; iInput < Reader.GetNInputs(); iInput++) {
-    ANN.SetInputName(iInput, Reader.GetInputName(iInput));
-  }
-  for (auto iLayer = 1u; iLayer < Reader.GetNlayers() - 1; iLayer++) {
-    ANN.PushHiddenLayer(Reader.GetNneurons(iLayer));
-  }
-  ANN.DefineOutputLayer(Reader.GetNOutputs());
-  for (auto iOutput = 0u; iOutput < Reader.GetNOutputs(); iOutput++) {
-    ANN.SetOutputName(iOutput, Reader.GetOutputName(iOutput));
-  }
-
-  /* Size weights of each layer */
-  ANN.SizeWeights();
-
-  /* Define weights and activation functions */
-  ANN.SizeActivationFunctions(ANN.GetNWeightLayers() + 1);
-  for (auto i_layer = 0u; i_layer < ANN.GetNWeightLayers(); i_layer++) {
-    ANN.SetActivationFunction(i_layer, Reader.GetActivationFunction(i_layer));
-    for (auto i_neuron = 0u; i_neuron < ANN.GetNNeurons(i_layer); i_neuron++) {
-      for (auto j_neuron = 0u; j_neuron < ANN.GetNNeurons(i_layer + 1); j_neuron++) {
-        ANN.SetWeight(i_layer, i_neuron, j_neuron, Reader.GetWeight(i_layer, i_neuron, j_neuron));
-      }
-    }
-  }
-  ANN.SetActivationFunction(ANN.GetNWeightLayers(), Reader.GetActivationFunction(ANN.GetNWeightLayers()));
-
-  /* Set neuron biases */
-  for (auto i_layer = 0u; i_layer < ANN.GetNWeightLayers() + 1; i_layer++) {
-    for (auto i_neuron = 0u; i_neuron < ANN.GetNNeurons(i_layer); i_neuron++) {
-      ANN.SetBias(i_layer, i_neuron, Reader.GetBias(i_layer, i_neuron));
-    }
-  }
-
-  /* Define input and output layer normalization values */
-  for (auto iInput = 0u; iInput < Reader.GetNInputs(); iInput++) {
-    ANN.SetInputNorm(iInput, Reader.GetInputNorm(iInput).first, Reader.GetInputNorm(iInput).second);
-  }
-  for (auto iOutput = 0u; iOutput < Reader.GetNOutputs(); iOutput++) {
-    ANN.SetOutputNorm(iOutput, Reader.GetOutputNorm(iOutput).first, Reader.GetOutputNorm(iOutput).second);
-  }
-}
-
-bool MLPToolbox::CLookUp_ANN::CheckUseOfInputs(su2vector<string>& input_names, CIOMap* input_output_map) const {
-  /*--- Check wether all input variables are in the loaded MLPs ---*/
-  vector<string> missing_inputs;
-  bool inputs_are_present{true};
-  for (auto iInput = 0u; iInput < input_names.size(); iInput++) {
-    bool found_input = false;
-    for (auto i_map = 0u; i_map < input_output_map->GetNMLPs(); i_map++) {
-      auto input_map = input_output_map->GetInputMapping(i_map);
-      for (auto jInput = 0u; jInput < input_map.size(); jInput++) {
-        if (input_map[jInput].first == iInput) {
-          found_input = true;
-        }
-      }
-    }
-    if (!found_input) {
-      missing_inputs.push_back(input_names[iInput]);
-      inputs_are_present = false;
-    };
-  }
-  /*--- Raise error if input variables are missing ---*/
-  if (missing_inputs.size() > 0) {
-    string message{"Inputs "};
-    for (size_t iVar = 0; iVar < missing_inputs.size(); iVar++) message += missing_inputs[iVar] + " ";
-    throw std::invalid_argument(message + "are not present in any loaded ANN.");
-  }
-  return inputs_are_present;
-}
-
-bool MLPToolbox::CLookUp_ANN::CheckUseOfOutputs(su2vector<string>& output_names, CIOMap* input_output_map) const {
-  /*--- Check wether all output variables are in the loaded MLPs ---*/
-
-  vector<string> missing_outputs;
-  bool outputs_are_present{true};
-  /* Looping over the target outputs */
-  for (auto iOutput = 0u; iOutput < output_names.size(); iOutput++) {
-    bool found_output{false};
-
-    /* Looping over all the selected ANNs */
-    for (auto i_map = 0u; i_map < input_output_map->GetNMLPs(); i_map++) {
-      auto output_map = input_output_map->GetOutputMapping(i_map);
-
-      /* Looping over the outputs of the output map of the current ANN */
-      for (auto jOutput = 0u; jOutput < output_map.size(); jOutput++) {
-        if (output_map[jOutput].first == iOutput) found_output = true;
-      }
-    }
-    if (!found_output) {
-      missing_outputs.push_back(output_names[iOutput]);
-      outputs_are_present = false;
-    };
-  }
-  /*--- Raise error if any outputs are missing ---*/
-  if (missing_outputs.size() > 0) {
-    string message{"Outputs "};
-    for (size_t iVar = 0; iVar < missing_outputs.size(); iVar++) message += missing_outputs[iVar] + " ";
-    throw std::invalid_argument( message + "are not present in any loaded ANN.");
-  }
-  return outputs_are_present;
-}
-
-void MLPToolbox::CLookUp_ANN::DisplayNetworkInfo() const {
-  /*--- Display network information on the loaded MLPs ---*/
-
-  cout << setfill(' ');
-  cout << endl;
-  cout << "+------------------------------------------------------------------+\n";
-  cout << "|                 Multi-Layer Perceptron (MLP) info                |\n";
-  cout << "+------------------------------------------------------------------+" << endl;
-
-  /* For every loaded MLP, display the inputs, outputs, activation functions, and architecture. */
-  for (auto i_MLP = 0u; i_MLP < NeuralNetworks.size(); i_MLP++) {
-    NeuralNetworks[i_MLP].DisplayNetwork();
-  }
-}
diff --git a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
deleted file mode 100644
index 9c98dcc5fe2..00000000000
--- a/Common/src/toolboxes/multilayer_perceptron/CNeuralNetwork.cpp
+++ /dev/null
@@ -1,366 +0,0 @@
-/*!
- * \file CNeuralNetwork.cpp
- * \brief Implementation of the NeuralNetwork class to be used
- *      for evaluation of multi-layer perceptrons.
- * \author E.C.Bunschoten
- * \version 7.5.1 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-#include "../../../include/toolboxes/multilayer_perceptron/CNeuralNetwork.hpp"
-
-#include <iomanip>
-#include <iostream>
-#include <map>
-
-#include "../../../include/toolboxes/multilayer_perceptron/CLayer.hpp"
-#include "../../../include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp"
-
-using namespace std;
-
-void MLPToolbox::CNeuralNetwork::Predict(su2vector<su2double>& inputs, bool compute_gradient) {
-  /*--- Evaluate MLP for given inputs ---*/
-
-  su2double y = 0, dy_dx = 0;  // Activation function output.
-  bool same_point = true;
-  /* Normalize input and check if inputs are the same w.r.t last evaluation */
-  for (auto iNeuron = 0u; iNeuron < inputLayer->GetNNeurons(); iNeuron++) {
-    su2double x_norm =
-        (inputs[iNeuron] - input_norm[iNeuron].first) / (input_norm[iNeuron].second - input_norm[iNeuron].first);
-    if (abs(x_norm - inputLayer->GetOutput(iNeuron)) > 0) same_point = false;
-    inputLayer->SetOutput(iNeuron, x_norm);
-
-    if (compute_gradient)
-      inputLayer->SetdYdX(iNeuron, iNeuron, 1 / (input_norm[iNeuron].second - input_norm[iNeuron].first));
-  }
-  /* Skip evaluation process if current point is the same as during the previous evaluation */
-  if (!same_point) {
-    su2double alpha = 1.67326324;
-    su2double lambda = 1.05070098;
-    /* Traverse MLP and compute inputs and outputs for the neurons in each layer */
-    for (auto iLayer = 1u; iLayer < n_hidden_layers + 2; iLayer++) {
-      auto nNeurons_current = total_layers[iLayer]->GetNNeurons();  // Neuron count of current layer
-      su2double x;                                                  // Neuron input value
-
-      /* Compute and store input value for each neuron */
-      for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
-        x = ComputeX(iLayer, iNeuron);
-        total_layers[iLayer]->SetInput(iNeuron, x);
-        if (compute_gradient) {
-          for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
-            dy_dx = ComputedOutputdInput(iLayer, iNeuron, iInput);
-            total_layers[iLayer]->SetdYdX(iNeuron, iInput, dy_dx);
-          }
-        }
-      }
-
-      /* Compute and store neuron output based on activation function */
-      switch (activation_function_types[iLayer]) {
-        case ENUM_ACTIVATION_FUNCTION::ELU:
-          for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
-            x = total_layers[iLayer]->GetInput(iNeuron);
-            if (x > 0) {
-              y = x;
-              if (compute_gradient) dy_dx = 1.0;
-            } else {
-              y = exp(x) - 1;
-              if (compute_gradient) dy_dx = exp(x);
-            }
-            total_layers[iLayer]->SetOutput(iNeuron, y);
-            if (compute_gradient) {
-              for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
-                total_layers[iLayer]->SetdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->GetdYdX(iNeuron, iInput));
-              }
-            }
-          }
-          break;
-        case ENUM_ACTIVATION_FUNCTION::LINEAR:
-          for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
-            x = total_layers[iLayer]->GetInput(iNeuron);
-            y = x;
-            total_layers[iLayer]->SetOutput(iNeuron, y);
-            if (compute_gradient) {
-              dy_dx = 1.0;
-              for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
-                total_layers[iLayer]->SetdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->GetdYdX(iNeuron, iInput));
-              }
-            }
-          }
-          break;
-        case ENUM_ACTIVATION_FUNCTION::EXPONENTIAL:
-          for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
-            x = total_layers[iLayer]->GetInput(iNeuron);
-            y = exp(x);
-            total_layers[iLayer]->SetOutput(iNeuron, y);
-            if (compute_gradient) {
-              dy_dx = 1.0;
-              for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
-                total_layers[iLayer]->SetdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->GetdYdX(iNeuron, iInput));
-              }
-            }
-          }
-          break;
-        case ENUM_ACTIVATION_FUNCTION::RELU:
-          for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
-            x = total_layers[iLayer]->GetInput(iNeuron);
-            if (x > 0) {
-              y = x;
-              if (compute_gradient) dy_dx = 1.0;
-            } else {
-              y = 0.0;
-              if (compute_gradient) dy_dx = 0.0;
-            }
-            total_layers[iLayer]->SetOutput(iNeuron, y);
-            if (compute_gradient) {
-              for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
-                total_layers[iLayer]->SetdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->GetdYdX(iNeuron, iInput));
-              }
-            }
-          }
-          break;
-        case ENUM_ACTIVATION_FUNCTION::SWISH:
-          for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
-            x = total_layers[iLayer]->GetInput(iNeuron);
-            y = x / (1 + exp(-x));
-            total_layers[iLayer]->SetOutput(iNeuron, y);
-            if (compute_gradient) {
-              dy_dx = exp(x) * (x + exp(x) + 1) / pow(exp(x) + 1, 2);
-              for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
-                total_layers[iLayer]->SetdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->GetdYdX(iNeuron, iInput));
-              }
-            }
-          }
-          break;
-        case ENUM_ACTIVATION_FUNCTION::TANH:
-          for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
-            x = total_layers[iLayer]->GetInput(iNeuron);
-            y = tanh(x);
-            total_layers[iLayer]->SetOutput(iNeuron, y);
-            if (compute_gradient) {
-              dy_dx = 1 / pow(cosh(x), 2);
-              for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
-                total_layers[iLayer]->SetdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->GetdYdX(iNeuron, iInput));
-              }
-            }
-          }
-          break;
-        case ENUM_ACTIVATION_FUNCTION::SIGMOID:
-          for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
-            x = total_layers[iLayer]->GetInput(iNeuron);
-            y = 1.0 / (1 + exp(-x));
-            total_layers[iLayer]->SetOutput(iNeuron, y);
-            if (compute_gradient) {
-              dy_dx = exp(-x) / pow(exp(-x) + 1, 2);
-              for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
-                total_layers[iLayer]->SetdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->GetdYdX(iNeuron, iInput));
-              }
-            }
-          }
-          break;
-        case ENUM_ACTIVATION_FUNCTION::SELU:
-          for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
-            x = total_layers[iLayer]->GetInput(iNeuron);
-            if (x > 0.0) {
-              y = lambda * x;
-              if (compute_gradient) dy_dx = lambda;
-            } else {
-              y = lambda * alpha * (exp(x) - 1);
-              if (compute_gradient) dy_dx = lambda * alpha * exp(x);
-            }
-            total_layers[iLayer]->SetOutput(iNeuron, y);
-            if (compute_gradient) {
-              for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
-                total_layers[iLayer]->SetdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->GetdYdX(iNeuron, iInput));
-              }
-            }
-          }
-          break;
-        case ENUM_ACTIVATION_FUNCTION::GELU:
-          for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
-            x = total_layers[iLayer]->GetInput(iNeuron);
-
-            y = 0.5 * x * (1 + tanh(0.7978845608028654 * (x + 0.044715 * pow(x, 3))));
-            total_layers[iLayer]->SetOutput(iNeuron, y);
-            if (compute_gradient) {
-              dy_dx = 0.5 * (tanh(0.0356774 * pow(x, 3) + 0.797885 * x) + (0.107032 * pow(x, 3) + 0.797885 * x) *
-                                                                              pow(cosh(x), -2) *
-                                                                              (0.0356774 * pow(x, 3) + 0.797885 * x));
-              for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
-                total_layers[iLayer]->SetdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->GetdYdX(iNeuron, iInput));
-              }
-            }
-          }
-          break;
-        case ENUM_ACTIVATION_FUNCTION::NONE:
-          for (auto iNeuron = 0u; iNeuron < nNeurons_current; iNeuron++) {
-            y = 0.0;
-            total_layers[iLayer]->SetOutput(iNeuron, y);
-            if (compute_gradient) {
-              dy_dx = 0.0;
-              for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
-                total_layers[iLayer]->SetdYdX(iNeuron, iInput, dy_dx * total_layers[iLayer]->GetdYdX(iNeuron, iInput));
-              }
-            }
-          }
-          break;
-        default:
-          break;
-      }  // activation_function_types
-    }
-  }
-  /* Compute and de-normalize MLP output */
-  for (auto iNeuron = 0u; iNeuron < outputLayer->GetNNeurons(); iNeuron++) {
-    su2double y_norm = outputLayer->GetOutput(iNeuron);
-    y = y_norm * (output_norm[iNeuron].second - output_norm[iNeuron].first) + output_norm[iNeuron].first;
-    if (compute_gradient) {
-      dy_dx = (output_norm[iNeuron].second - output_norm[iNeuron].first);
-      for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++) {
-        outputLayer->SetdYdX(iNeuron, iInput, dy_dx * outputLayer->GetdYdX(iNeuron, iInput));
-        dOutputs_dInputs[iNeuron][iInput] = outputLayer->GetdYdX(iNeuron, iInput);
-      }
-    }
-    /* Storing output value */
-    ANN_outputs[iNeuron] = y;
-  }
-}
-
-void MLPToolbox::CNeuralNetwork::DefineInputLayer(unsigned long n_neurons) {
-  /*--- Define the input layer of the network ---*/
-  inputLayer = new CLayer(n_neurons);
-
-  /* Mark layer as input layer */
-  inputLayer->SetInput(true);
-  input_norm.resize(n_neurons);
-  input_names.resize(n_neurons);
-}
-
-void MLPToolbox::CNeuralNetwork::DefineOutputLayer(unsigned long n_neurons) {
-  /*--- Define the output layer of the network ---*/
-  outputLayer = new CLayer(n_neurons);
-  output_norm.resize(n_neurons);
-  output_names.resize(n_neurons);
-}
-
-void MLPToolbox::CNeuralNetwork::PushHiddenLayer(unsigned long n_neurons) {
-  /*--- Add a hidden layer to the network ---*/
-  CLayer* newLayer = new CLayer(n_neurons);
-  hiddenLayers.push_back(newLayer);
-  n_hidden_layers++;
-}
-
-void MLPToolbox::CNeuralNetwork::SizeWeights() {
-  /*--- Size weight matrices based on neuron counts in each layer ---*/
-
-  /* Generate vector containing input, output, and hidden layer references */
-  total_layers.resize(n_hidden_layers + 2);
-  total_layers[0] = inputLayer;
-  for (auto iLayer = 0u; iLayer < n_hidden_layers; iLayer++) {
-    total_layers[iLayer + 1] = hiddenLayers[iLayer];
-  }
-  total_layers[total_layers.size() - 1] = outputLayer;
-
-  weights_mat.resize(n_hidden_layers + 1);
-  weights_mat[0].resize(hiddenLayers[0]->GetNNeurons(), inputLayer->GetNNeurons());
-  for (auto iLayer = 1u; iLayer < n_hidden_layers; iLayer++) {
-    weights_mat[iLayer].resize(hiddenLayers[iLayer]->GetNNeurons(), hiddenLayers[iLayer - 1]->GetNNeurons());
-  }
-  weights_mat[n_hidden_layers].resize(outputLayer->GetNNeurons(), hiddenLayers[n_hidden_layers - 1]->GetNNeurons());
-
-  ANN_outputs = new su2double[outputLayer->GetNNeurons()];
-  dOutputs_dInputs.resize(outputLayer->GetNNeurons(), inputLayer->GetNNeurons());
-  for (auto iLayer = 0u; iLayer < n_hidden_layers + 2; iLayer++) {
-    total_layers[iLayer]->SizeGradients(inputLayer->GetNNeurons());
-  }
-}
-
-void MLPToolbox::CNeuralNetwork::DisplayNetwork() const {
-  /*--- Display information on the MLP architecture ---*/
-  int display_width = 54;
-  int column_width = int(display_width / 3.0) - 1;
-
-  /*--- Input layer information ---*/
-  cout << "+" << setfill('-') << setw(display_width) << right << "+" << endl;
-  cout << setfill(' ');
-  cout << "|" << left << setw(display_width - 1) << "Input Layer Information:"
-       << "|" << endl;
-  cout << "+" << setfill('-') << setw(display_width) << right << "+" << endl;
-  cout << setfill(' ');
-  cout << "|" << left << setw(column_width) << "Input Variable:"
-       << "|" << left << setw(column_width) << "Lower limit:"
-       << "|" << left << setw(column_width) << "Upper limit:"
-       << "|" << endl;
-  cout << "+" << setfill('-') << setw(display_width) << right << "+" << endl;
-  cout << setfill(' ');
-
-  /*--- Hidden layer information ---*/
-  for (auto iInput = 0u; iInput < inputLayer->GetNNeurons(); iInput++)
-    cout << "|" << left << setw(column_width) << to_string(iInput + 1) + ": " + input_names[iInput] << "|" << right
-         << setw(column_width) << input_norm[iInput].first << "|" << right << setw(column_width)
-         << input_norm[iInput].second << "|" << endl;
-  cout << "+" << setfill('-') << setw(display_width) << right << "+" << endl;
-  cout << setfill(' ');
-  cout << "|" << left << setw(display_width - 1) << "Hidden Layers Information:"
-       << "|" << endl;
-  cout << "+" << setfill('-') << setw(display_width) << right << "+" << endl;
-  cout << setfill(' ');
-  cout << "|" << setw(column_width) << left << "Layer index"
-       << "|" << setw(column_width) << left << "Neuron count"
-       << "|" << setw(column_width) << left << "Function"
-       << "|" << endl;
-  cout << "+" << setfill('-') << setw(display_width) << right << "+" << endl;
-  cout << setfill(' ');
-  for (auto iLayer = 0u; iLayer < n_hidden_layers; iLayer++)
-    cout << "|" << setw(column_width) << right << iLayer + 1 << "|" << setw(column_width) << right
-         << hiddenLayers[iLayer]->GetNNeurons() << "|" << setw(column_width) << right
-         << activation_function_names[iLayer + 1] << "|" << endl;
-  cout << "+" << setfill('-') << setw(display_width) << right << "+" << endl;
-  cout << setfill(' ');
-
-  /*--- Output layer information ---*/
-  cout << "|" << left << setw(display_width - 1) << "Output Layer Information:"
-       << "|" << endl;
-  cout << "+" << setfill('-') << setw(display_width) << right << "+" << endl;
-  cout << setfill(' ');
-  cout << "|" << left << setw(column_width) << "Output Variable:"
-       << "|" << left << setw(column_width) << "Lower limit:"
-       << "|" << left << setw(column_width) << "Upper limit:"
-       << "|" << endl;
-  cout << "+" << setfill('-') << setw(display_width) << right << "+" << endl;
-  cout << setfill(' ');
-  for (auto iOutput = 0u; iOutput < outputLayer->GetNNeurons(); iOutput++)
-    cout << "|" << left << setw(column_width) << to_string(iOutput + 1) + ": " + output_names[iOutput] << "|" << right
-         << setw(column_width) << output_norm[iOutput].first << "|" << right << setw(column_width)
-         << output_norm[iOutput].second << "|" << endl;
-  cout << "+" << setfill('-') << setw(display_width) << right << "+" << endl;
-  cout << setfill(' ');
-  cout << endl;
-}
-
-void MLPToolbox::CNeuralNetwork::SetActivationFunction(unsigned long i_layer, string input) {
-  /*--- Translate activation function name from input file to a number ---*/
-
-  activation_function_names[i_layer] = input;
-
-  // Set activation function type in current layer.
-  activation_function_types[i_layer] = activation_function_map.find(input)->second;
-
-  return;
-}
diff --git a/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp b/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
deleted file mode 100644
index 8956397b259..00000000000
--- a/Common/src/toolboxes/multilayer_perceptron/CReadNeuralNetwork.cpp
+++ /dev/null
@@ -1,207 +0,0 @@
-/*!
- * \file ReadNeuralNetwork.cpp
- * \brief Implementation of the reader class to read .mlp input files
- *      used to set up multi-layer perceptrons.
- * \author E.C.Bunschoten
- * \version 7.5.1 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-#include "../../../include/toolboxes/multilayer_perceptron/CReadNeuralNetwork.hpp"
-#include <iostream>
-#include <fstream>
-using namespace std;
-
-MLPToolbox::CReadNeuralNetwork::CReadNeuralNetwork(string filename_in) { filename = filename_in; }
-
-void MLPToolbox::CReadNeuralNetwork::ReadMLPFile() {
-  ifstream file_stream;
-  file_stream.open(filename.c_str(), ifstream::in);
-  if (!file_stream.is_open()) {
-    throw std::invalid_argument( "There is no MLP file called " + filename);
-  }
-
-  string line, word;
-  bool eoHeader = false, found_layercount = false, found_input_names = false, found_output_names = false;
-
-  /* Read general architecture information from file header */
-
-  line = SkipToFlag(&file_stream, "<header>");
-
-  while (getline(file_stream, line) && !eoHeader) {
-    /* Read layer count */
-    if (line.compare("[number of layers]") == 0) {
-      getline(file_stream, line);
-      n_layers = stoul(line);
-      n_neurons.resize(n_layers);
-      biases_mat.resize(n_layers);
-      weights_mat.resize(n_layers - 1);
-      activation_functions.resize(n_layers);
-
-      found_layercount = true;
-    }
-
-    /* Set number of neurons for each layer */
-    if (line.compare("[neurons per layer]") == 0) {
-      /* In case layer count was not yet provided, return an error */
-      if (!found_layercount) {
-        throw std::invalid_argument( "No layer count provided before defining neuron count per layer");
-      }
-      /* Loop over layer count and size neuron count and bias count per layer accordingly */
-      for (auto iLayer = 0u; iLayer < n_layers; iLayer++) {
-        getline(file_stream, line);
-        n_neurons[iLayer] = stoul(line);
-        biases_mat[iLayer].resize(n_neurons[iLayer]);
-      }
-      /* Loop over spaces between layers and size the weight matrices accordingly */
-      for (auto iLayer = 0u; iLayer < n_layers - 1; iLayer++) {
-        weights_mat[iLayer].resize(n_neurons[iLayer], n_neurons[iLayer + 1]);
-      }
-      /* Size input and output normalization and set default values */
-      input_norm.resize(n_neurons[0]);
-      for (auto iNeuron = 0u; iNeuron < n_neurons[0]; iNeuron++) input_norm[iNeuron] = make_pair(0, 1);
-
-      output_norm.resize(n_neurons[n_neurons.size() - 1]);
-      for (auto iNeuron = 0u; iNeuron < n_neurons[n_neurons.size() - 1]; iNeuron++)
-        output_norm[iNeuron] = make_pair(0, 1);
-    }
-
-    /* Read layer activation function types */
-    if (line.compare("[activation function]") == 0) {
-      if (!found_layercount) {
-        throw std::invalid_argument( "No layer count provided before providing layer activation functions" );
-      }
-      for (auto iLayer = 0u; iLayer < n_layers; iLayer++) {
-        getline(file_stream, line);
-        istringstream activation_stream(line);
-        activation_stream >> word;
-        activation_functions[iLayer] = word;
-      }
-    }
-
-    /* Read MLP input variable names */
-    if (line.compare("[input names]") == 0) {
-      found_input_names = true;
-      input_names.resize(n_neurons[0]);
-      for (auto iInput = 0u; iInput < n_neurons[0]; iInput++) {
-        getline(file_stream, line);
-        input_names[iInput] = line;
-      }
-    }
-
-    /* In case input normalization is applied, read upper and lower input bounds */
-    if (line.compare("[input normalization]") == 0) {
-      for (auto iInput = 0u; iInput < input_norm.size(); iInput++) {
-        getline(file_stream, line);
-        if (line.compare("") != 0) {
-          istringstream input_norm_stream(line);
-          input_norm_stream >> word;
-          su2double input_min = stold(word);
-          input_norm_stream >> word;
-          su2double input_max = stold(word);
-          input_norm[iInput] = make_pair(input_min, input_max);
-        }
-      }
-    }
-
-    /* Read MLP output variable names */
-    if (line.compare("[output names]") == 0) {
-      found_output_names = true;
-      auto n_outputs = n_neurons[n_neurons.size() - 1];
-      output_names.resize(n_outputs);
-      for (auto iOutput = 0u; iOutput < n_outputs; iOutput++) {
-        getline(file_stream, line);
-        output_names[iOutput] = line;
-      }
-
-      if (output_names.size() != (n_neurons[n_neurons.size() - 1])) {
-        throw std::invalid_argument("No layer count provided before providing layer activation functions");
-      }
-    }
-
-    /* In case output normalization is applied, read upper and lower output bounds */
-    if (line.compare("[output normalization]") == 0) {
-      for (auto iOutput = 0u; iOutput < output_norm.size(); iOutput++) {
-        getline(file_stream, line);
-        if (line.compare("") != 0) {
-          istringstream output_norm_stream(line);
-          output_norm_stream >> word;
-          su2double output_min = stold(word);
-          output_norm_stream >> word;
-          su2double output_max = stold(word);
-          output_norm[iOutput] = make_pair(output_min, output_max);
-        }
-      }
-    }
-
-    if (line.compare("</header>") == 0) {
-      eoHeader = true;
-    }
-  }  // eoHeader
-
-  /* Error checking */
-  if (!found_input_names) {
-    throw std::invalid_argument("No MLP input variable names provided");
-  }
-  if (!found_output_names) {
-    throw std::invalid_argument("No MLP input variable names provided");
-  }
-
-  /* Read weights for each layer */
-  line = SkipToFlag(&file_stream, "[weights per layer]");
-  for (auto iLayer = 0u; iLayer < n_layers - 1; iLayer++) {
-    getline(file_stream, line);
-    for (auto iNeuron = 0u; iNeuron < n_neurons[iLayer]; iNeuron++) {
-      getline(file_stream, line);
-      istringstream weight_stream(line);
-      for (auto jNeuron = 0u; jNeuron < n_neurons[iLayer + 1]; jNeuron++) {
-        weight_stream >> word;
-        weights_mat[iLayer][iNeuron][jNeuron] = stold(word);
-      }
-    }
-    getline(file_stream, line);
-  }
-
-  /* Read biases for each neuron */
-  line = SkipToFlag(&file_stream, "[biases per layer]");
-  for (auto iLayer = 0u; iLayer < n_layers; iLayer++) {
-    getline(file_stream, line);
-    istringstream bias_stream(line);
-    for (auto iNeuron = 0u; iNeuron < n_neurons[iLayer]; iNeuron++) {
-      bias_stream >> word;
-      biases_mat[iLayer][iNeuron] = stold(word);
-    }
-  }
-}
-
-string MLPToolbox::CReadNeuralNetwork::SkipToFlag(ifstream* file_stream, string flag) {
-  /*--- Search file for a line and set it as the current line in the file stream ---*/
-  string line;
-  getline(*file_stream, line);
-
-  while (line.compare(flag) != 0 && !(*file_stream).eof()) {
-    getline(*file_stream, line);
-  }
-
-  if ((*file_stream).eof()) cout << "line not in file!" << endl;
-
-  return line;
-}
diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index fe97fbe2e3f..ae519633d89 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -2,7 +2,7 @@
  * \file CDataDrivenFluid.hpp
  * \brief Defines a template fluid model class using multilayer perceptrons
  *  for theromodynamic state definition
- * \author E.Bunschoten
+ * \author E.C.Bunschoten
  * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
@@ -28,15 +28,19 @@
 
 #pragma once
 
+#include <vector>
 #include "../../../Common/include/containers/CLookUpTable.hpp"
-#include "../../../Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp"
+#include "CLookUp_ANN.hpp"
+#if defined(HAVE_MLPCPP)
+#define USE_MLPCPP
+#endif
 #include "CFluidModel.hpp"
 
 /*!
  * \class CDataDrivenFluid
  * \brief Template class for fluid model definition using multi-layer perceptrons for
  * fluid dynamic state definition.
- * \author: E.Bunschoten.
+ * \author: E.C.Bunschoten.
  */
 class CDataDrivenFluid : public CFluidModel {
  protected:
@@ -59,16 +63,16 @@ class CDataDrivenFluid : public CFluidModel {
       d2sdedrho,      /*!< \brief Entropy second derivative w.r.t. density and static energy */
       d2sdrho2;       /*!< \brief Entropy second derivative w.r.t. static density */
 
-  su2vector<string>
+  vector<string>
       input_names_rhoe,   // Data-driven method input variable names of the independent variables (density, energy).
       output_names_rhoe;  // Output variable names listed in the data-driven method input file name.
 
-  su2vector<su2double*> outputs_rhoe;  // Pointers to output variables.
+  vector<double*> outputs_rhoe;  // Pointers to output variables.
 
   /*--- Class variables for the multi-layer perceptron method ---*/
   MLPToolbox::CLookUp_ANN* lookup_mlp;  // multi-layer perceptron collection.
   MLPToolbox::CIOMap* iomap_rhoe;       // input-output map.
-  su2vector<su2double> MLP_inputs;      // inputs for the multi-layer perceptron look-up operation.
+  vector<double> MLP_inputs;            // inputs for the multi-layer perceptron look-up operation.
 
   /*--- Class variables for the look-up table method ---*/
   CLookUpTable* lookup_table;
@@ -182,4 +186,4 @@ class CDataDrivenFluid : public CFluidModel {
    * \return Newton solver iteration count at termination.
    */
   unsigned long GetnIter_Newton() override { return nIter_Newton; }
-};
\ No newline at end of file
+};
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 03e47f8c07a..8ecf040ae26 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -1,7 +1,7 @@
 /*!
  * \file CDataDrivenFluid.cpp
  * \brief Source of the data-driven fluid model class
- * \author E.Bunschoten M.Mayer A.Capiello
+ * \author E.C.Bunschoten M.Mayer A.Capiello
  * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
@@ -36,8 +36,12 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
   /*--- Set up interpolation algorithm according to data-driven method. Currently only MLP's are supported. ---*/
   switch (Kind_DataDriven_Method) {
     case ENUM_DATADRIVEN_METHOD::MLP:
+#ifdef HAVE_MLPCPP
       lookup_mlp = new MLPToolbox::CLookUp_ANN(config->GetNDataDriven_Files(), config->GetDataDriven_FileNames());
       if (rank == MASTER_NODE) lookup_mlp->DisplayNetworkInfo();
+#else
+      SU2_MPI::Error("SU2 was not compiled with MLPCpp enabled (-Denable-mlpcpp=true).", CURRENT_FUNCTION);
+#endif
       break;
     case ENUM_DATADRIVEN_METHOD::LUT:
       lookup_table = new CLookUpTable(config->GetDataDriven_Filename(), "Density", "Energy");
@@ -102,9 +106,11 @@ void CDataDrivenFluid::MapInputs_to_Outputs() {
 
   /*--- Further preprocessing of input and output variables ---*/
   if (Kind_DataDriven_Method == ENUM_DATADRIVEN_METHOD::MLP) {
-    /*--- Map MLP inputs to outputs ---*/
+/*--- Map MLP inputs to outputs ---*/
+#ifdef HAVE_MLPCPP
     iomap_rhoe = new MLPToolbox::CIOMap(lookup_mlp, input_names_rhoe, output_names_rhoe);
     MLP_inputs.resize(2);
+#endif
   }
 }
 
@@ -362,10 +368,11 @@ void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
 unsigned long CDataDrivenFluid::Predict_MLP(su2double rho, su2double e) {
   MLP_inputs[idx_rho] = rho;
   MLP_inputs[idx_e] = e;
-
-  /* Evaluate MLP collection for the given values for density and energy */
-  unsigned long exit_code = lookup_mlp->PredictANN(iomap_rhoe, MLP_inputs, outputs_rhoe);
-
+  unsigned long exit_code = 0;
+/* Evaluate MLP collection for the given values for density and energy */
+#ifdef HAVE_MLPCPP
+  exit_code = lookup_mlp->PredictANN(iomap_rhoe, MLP_inputs, outputs_rhoe);
+#endif
   /* Apply exponential transformation to the MLP outputs for the first and second
      derivative of the entropy w.r.t density */
   // Optional:
@@ -405,4 +412,4 @@ void CDataDrivenFluid::Evaluate_Dataset(su2double rho, su2double e) {
     default:
       break;
   }
-}
\ No newline at end of file
+}
diff --git a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
index 7f125adb6ae..a484cb5f1ed 100644
--- a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
+++ b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
@@ -1,7 +1,7 @@
 /*!
  * \file CLookUp_ANN_tests.cpp
- * \brief Unit tests for NdFlattener template classes.
- * \author M. Aehle
+ * \brief Unit tests for CLookUp_ANN and CIOMap classes.
+ * \author E.C.Bunschoten
  * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
@@ -27,18 +27,24 @@
 
 #include "catch.hpp"
 #include "../../../../Common/include/CConfig.hpp"
-#include "../../../../Common/include/toolboxes/multilayer_perceptron/CLookUp_ANN.hpp"
-#include "../../../../Common/include/toolboxes/multilayer_perceptron/CIOMap.hpp"
+#include "CLookUp_ANN.hpp"
+#if defined(HAVE_MLPCPP)
+#define USE_MLPCPP
+#endif
+#include <vector>
 
-TEST_CASE("LookUp ANN test", "[LookUpANN]"){
+TEST_CASE("LookUp ANN test", "[LookUpANN]") {
   std::string MLP_input_files[] = {"src/SU2/UnitTests/Common/toolboxes/multilayer_perceptron/simple_mlp.mlp"};
   unsigned short n_MLPs = 1;
+#ifdef USE_MLPCPP
   MLPToolbox::CLookUp_ANN ANN(n_MLPs, MLP_input_files);
-  su2vector<std::string> MLP_input_names,
-                           MLP_output_names;
-  su2vector<su2double> MLP_inputs;
-  su2vector<su2double*> MLP_outputs;
-  su2double x,y,z;
+#else
+  SU2_MPI::Error("SU2 was not compiled with MLPCpp enabled (-Denable-mlpcpp=true).", CURRENT_FUNCTION);
+#endif
+  std::vector<std::string> MLP_input_names, MLP_output_names;
+  std::vector<double> MLP_inputs;
+  std::vector<double*> MLP_outputs;
+  su2double x, y, z;
 
   /*--- Define MLP inputs and outputs ---*/
   MLP_input_names.resize(2);
@@ -51,16 +57,19 @@ TEST_CASE("LookUp ANN test", "[LookUpANN]"){
   MLP_output_names[0] = "z";
   MLP_outputs[0] = &z;
 
-  /*--- Generate input-output map ---*/
+/*--- Generate input-output map ---*/
+#ifdef USE_MLPCPP
   MLPToolbox::CIOMap iomap(&ANN, MLP_input_names, MLP_output_names);
-
+#endif
   /*--- MLP evaluation on point in the middle of the training data range ---*/
   x = 1.0;
   y = -0.5;
 
   MLP_inputs[0] = x;
   MLP_inputs[1] = y;
+#ifdef USE_MLPCPP
   ANN.PredictANN(&iomap, MLP_inputs, MLP_outputs);
+#endif
   CHECK(z == Approx(0.344829));
 
   /*--- MLP evaluation on point outside the training data range ---*/
@@ -68,6 +77,8 @@ TEST_CASE("LookUp ANN test", "[LookUpANN]"){
   y = -10;
   MLP_inputs[0] = x;
   MLP_inputs[1] = y;
+#ifdef USE_MLPCPP
   ANN.PredictANN(&iomap, MLP_inputs, MLP_outputs);
+#endif
   CHECK(z == Approx(0.012737));
 }
diff --git a/externals/medi b/externals/medi
index 6aef76912e7..aafc2d1966b 160000
--- a/externals/medi
+++ b/externals/medi
@@ -1 +1 @@
-Subproject commit 6aef76912e7099c4f08c9705848797ca9e8070da
+Subproject commit aafc2d1966ba1233640af737e71c77c1a86183fd
diff --git a/externals/meson b/externals/meson
index 41c650a040d..be092c252e1 160000
--- a/externals/meson
+++ b/externals/meson
@@ -1 +1 @@
-Subproject commit 41c650a040d50e0912d268af7a903a9ce1456dfa
+Subproject commit be092c252e180d2c7e1fc6639d9ebc56aac80fd1
diff --git a/externals/ninja b/externals/ninja
index 52649de2c56..2d9083b2608 160000
--- a/externals/ninja
+++ b/externals/ninja
@@ -1 +1 @@
-Subproject commit 52649de2c56b63f42bc59513d51286531c595b44
+Subproject commit 2d9083b2608bd60c31583193d321d13a81a75beb
diff --git a/externals/opdi b/externals/opdi
index 1aabf5bd1ed..f33b507c24f 160000
--- a/externals/opdi
+++ b/externals/opdi
@@ -1 +1 @@
-Subproject commit 1aabf5bd1ed77611742eb655002f2ac7a3dddef9
+Subproject commit f33b507c24f7448d4cf4df16ab5c53ea254b8774
diff --git a/meson.build b/meson.build
index 2aa544f949c..196c31da7ff 100644
--- a/meson.build
+++ b/meson.build
@@ -259,6 +259,19 @@ if get_option('enable-coolprop')
   endif
 endif
 
+if get_option('enable-mlpcpp')
+  cmake = import('cmake')
+  cmake_opts = cmake.subproject_options()
+  cmake_opts.set_override_option('warning_level', '0')
+  cmake_opts.add_cmake_defines({
+    'CMAKE_MAKE_PROGRAM': meson.source_root() + '/ninja',
+    'CMAKE_POSITION_INDEPENDENT_CODE': 'ON'
+  })
+  mlpcpp_subproj = cmake.subproject('MLPCpp', options: cmake_opts)
+  mlpcpp_dep = mlpcpp_subproj.dependency('MLPCpp')
+  su2_deps += mlpcpp_dep
+  su2_cpp_args += '-DHAVE_MLPCPP'
+endif
 
 if omp and get_option('enable-autodiff')
   py = find_program('python3','python')
@@ -325,7 +338,7 @@ message('''---------------------------------------------------------------------
 '''.format(get_option('prefix')+'/bin', meson.source_root(), get_option('enable-tecio'), get_option('enable-cgns'),
            get_option('enable-autodiff'), get_option('enable-directdiff'), get_option('enable-pywrapper'), get_option('enable-mkl'),
            get_option('enable-openblas'), get_option('enable-pastix'), get_option('enable-mixedprec'), get_option('enable-librom'), get_option('enable-coolprop'),
-           meson.build_root().startswith(meson.source_root()) ? meson.build_root().split('/')[-1] : meson.build_root()))
+           get_option('enable-mlpcpp'), meson.build_root().startswith(meson.source_root()) ? meson.build_root().split('/')[-1] : meson.build_root()))
 
 if get_option('enable-mpp')
   message(''' To run SU2 with Mutation++ library, add these lines to your .bashrc file:
diff --git a/meson_options.txt b/meson_options.txt
index acb2f627d26..f31f9a0fc57 100644
--- a/meson_options.txt
+++ b/meson_options.txt
@@ -19,6 +19,7 @@ option('enable-mixedprec', type : 'boolean', value : false, description: 'use si
 option('extra-deps', type : 'string', value : '', description: 'comma-separated list of extra (custom) dependencies to add for compilation')
 option('enable-mpp',  type : 'boolean', value : false, description: 'enable Mutation++ support')
 option('enable-coolprop',  type : 'boolean', value : false, description: 'enable CoolProp support')
+option('enable-mlpcpp', type : 'boolean', value : false, description: 'enable MLPCpp support')
 option('opdi-backend', type : 'combo', choices : ['auto', 'macro', 'ompt'], value : 'auto', description: 'OpDiLib backend choice')
 option('codi-tape', type : 'combo', choices : ['JacobianLinear', 'JacobianIndex'], value : 'JacobianLinear', description: 'CoDiPack tape choice')
 option('opdi-shared-read-opt', type : 'boolean', value : true, description : 'OpDiLib shared reading optimization')
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 3f0b0646a6f..86c01392aba 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -48,6 +48,7 @@ def init_submodules(
     own_mpp=True,
     own_cool=True,
     own_mel=True,
+    own_mlpcpp=True,
 ):
 
     cur_dir = sys.path[0]
@@ -70,6 +71,8 @@ def init_submodules(
     github_repo_coolprop = "https://github.com/CoolProp/CoolProp"
     sha_version_mel = "2484cd3258ef800a10e361016cb341834ee7930b"
     github_repo_mel = "https://github.com/pcarruscag/MEL"
+    sha_version_mlpcpp = "2c6e14e867657490c29de102b3d30b92d02544a1"
+    github_repo_mlpcpp = "https://github.com/EvertBunschoten/MLPCpp"
 
     medi_name = "MeDiPack"
     codi_name = "CoDiPack"
@@ -79,6 +82,8 @@ def init_submodules(
     mpp_name = "Mutationpp"
     coolprop_name = "CoolProp"
     mel_name = "MEL"
+    mlpcpp_name = "MLPCpp"
+
     base_path = cur_dir + os.path.sep + "externals" + os.path.sep
     alt_name_medi = base_path + "medi"
     alt_name_codi = base_path + "codi"
@@ -88,6 +93,7 @@ def init_submodules(
     alt_name_mel = base_path + "mel"
     alt_name_mpp = cur_dir + os.path.sep + "subprojects" + os.path.sep + "Mutationpp"
     alt_name_coolprop = cur_dir + os.path.sep + "subprojects" + os.path.sep + "CoolProp"
+    alt_name_mlpcpp = cur_dir + os.path.sep + "subprojects" + os.path.sep + "MLPCpp"
 
     if method == "auto":
         is_git = is_git_directory(cur_dir)
@@ -117,6 +123,8 @@ def init_submodules(
             submodule_status(alt_name_coolprop, sha_version_coolprop)
         if own_mel:
             submodule_status(alt_name_mel, sha_version_mel)
+        if own_mlpcpp:
+            submodule_status(alt_name_mlpcpp, sha_version_mlpcpp)
     # Otherwise download the zip file from git
     else:
         if own_codi:
@@ -149,7 +157,8 @@ def init_submodules(
             )
         if own_mel:
             download_module(mel_name, alt_name_mel, github_repo_mel, sha_version_mel)
-
+        if own_mlpcpp:
+            download_module(mlpcpp_name, alt_name_mlpcpp, github_repo_mlpcpp, sha_version_mlpcpp)
 
 def is_git_directory(path="."):
     try:
diff --git a/preconfigure.py b/preconfigure.py
index 9085809e1df..61d63abd89a 100755
--- a/preconfigure.py
+++ b/preconfigure.py
@@ -135,6 +135,11 @@ def run(
     parser.add_argument(
         "--no-mel", help="do not download own copy of MEL", action="store_false"
     )
+    parser.add_argument(
+        "--no-mlpcpp",
+        help="do not download copy of MLpCpp",
+        action="store_false",
+    )
     args = parser.parse_args()
 
     run(
@@ -145,4 +150,5 @@ def run(
         own_mpp=args.no_mpp,
         own_cool=args.no_coolprop,
         own_mel=args.no_mel,
+        own_mlp=args.no_mlpcpp,
     )
diff --git a/subprojects/CoolProp b/subprojects/CoolProp
index 0ce42fcf3bb..abcb4a53a94 160000
--- a/subprojects/CoolProp
+++ b/subprojects/CoolProp
@@ -1 +1 @@
-Subproject commit 0ce42fcf3bb2c373512bc825a4f0c1973a78f307
+Subproject commit abcb4a53a949e081bae7d9af4807681abe3e57fd
diff --git a/subprojects/MLPCpp b/subprojects/MLPCpp
new file mode 160000
index 00000000000..9d1b09e8865
--- /dev/null
+++ b/subprojects/MLPCpp
@@ -0,0 +1 @@
+Subproject commit 9d1b09e8865a4d142fe97ee3dd0ebb71bd36b3ad
diff --git a/subprojects/Mutationpp b/subprojects/Mutationpp
index 5ff579f4378..4cb6e3a05c1 160000
--- a/subprojects/Mutationpp
+++ b/subprojects/Mutationpp
@@ -1 +1 @@
-Subproject commit 5ff579f43781cae07411e5ab46291c9971536be6
+Subproject commit 4cb6e3a05c15f49ffd346dc9f185ccc3459728b0

From c3d32a6ada4cd825f1c2ae60e5e446176d69dde9 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 28 Mar 2023 16:18:24 +0200
Subject: [PATCH 322/656] Updated submodules and fixed build error

---
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp |  4 ++--
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp     | 11 ++++++-----
 externals/meson                            |  2 +-
 meson_scripts/init.py                      |  7 +++++--
 subprojects/MLPCpp                         |  2 +-
 5 files changed, 15 insertions(+), 11 deletions(-)

diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index ae519633d89..8e6dd792551 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -31,7 +31,7 @@
 #include <vector>
 #include "../../../Common/include/containers/CLookUpTable.hpp"
 #include "CLookUp_ANN.hpp"
-#if defined(HAVE_MLPCPP)
+#if defined(HAVE_MLPCPP) && !defined(CODI_FORWARD_TYPE) && !defined(CODI_REVERSE_TYPE)
 #define USE_MLPCPP
 #endif
 #include "CFluidModel.hpp"
@@ -67,7 +67,7 @@ class CDataDrivenFluid : public CFluidModel {
       input_names_rhoe,   // Data-driven method input variable names of the independent variables (density, energy).
       output_names_rhoe;  // Output variable names listed in the data-driven method input file name.
 
-  vector<double*> outputs_rhoe;  // Pointers to output variables.
+  vector<su2double*> outputs_rhoe;  // Pointers to output variables.
 
   /*--- Class variables for the multi-layer perceptron method ---*/
   MLPToolbox::CLookUp_ANN* lookup_mlp;  // multi-layer perceptron collection.
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 8ecf040ae26..20f2d0fa0ef 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -36,7 +36,7 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
   /*--- Set up interpolation algorithm according to data-driven method. Currently only MLP's are supported. ---*/
   switch (Kind_DataDriven_Method) {
     case ENUM_DATADRIVEN_METHOD::MLP:
-#ifdef HAVE_MLPCPP
+#ifdef USE_MLPCPP
       lookup_mlp = new MLPToolbox::CLookUp_ANN(config->GetNDataDriven_Files(), config->GetDataDriven_FileNames());
       if (rank == MASTER_NODE) lookup_mlp->DisplayNetworkInfo();
 #else
@@ -107,7 +107,7 @@ void CDataDrivenFluid::MapInputs_to_Outputs() {
   /*--- Further preprocessing of input and output variables ---*/
   if (Kind_DataDriven_Method == ENUM_DATADRIVEN_METHOD::MLP) {
 /*--- Map MLP inputs to outputs ---*/
-#ifdef HAVE_MLPCPP
+#ifdef USE_MLPCPP
     iomap_rhoe = new MLPToolbox::CIOMap(lookup_mlp, input_names_rhoe, output_names_rhoe);
     MLP_inputs.resize(2);
 #endif
@@ -366,11 +366,12 @@ void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
 }
 
 unsigned long CDataDrivenFluid::Predict_MLP(su2double rho, su2double e) {
-  MLP_inputs[idx_rho] = rho;
-  MLP_inputs[idx_e] = e;
+
   unsigned long exit_code = 0;
 /* Evaluate MLP collection for the given values for density and energy */
-#ifdef HAVE_MLPCPP
+#ifdef USE_MLPCPP
+  MLP_inputs[idx_rho] = rho;
+  MLP_inputs[idx_e] = e;
   exit_code = lookup_mlp->PredictANN(iomap_rhoe, MLP_inputs, outputs_rhoe);
 #endif
   /* Apply exponential transformation to the MLP outputs for the first and second
diff --git a/externals/meson b/externals/meson
index be092c252e1..c4cc14c27c7 160000
--- a/externals/meson
+++ b/externals/meson
@@ -1 +1 @@
-Subproject commit be092c252e180d2c7e1fc6639d9ebc56aac80fd1
+Subproject commit c4cc14c27c7e46f65b410dbdd0f87dd73427b20d
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 86c01392aba..17ec689553b 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -71,7 +71,7 @@ def init_submodules(
     github_repo_coolprop = "https://github.com/CoolProp/CoolProp"
     sha_version_mel = "2484cd3258ef800a10e361016cb341834ee7930b"
     github_repo_mel = "https://github.com/pcarruscag/MEL"
-    sha_version_mlpcpp = "2c6e14e867657490c29de102b3d30b92d02544a1"
+    sha_version_mlpcpp = "78e8c7d8aa2759d891f27ed94d1b1506f328e254"
     github_repo_mlpcpp = "https://github.com/EvertBunschoten/MLPCpp"
 
     medi_name = "MeDiPack"
@@ -158,7 +158,10 @@ def init_submodules(
         if own_mel:
             download_module(mel_name, alt_name_mel, github_repo_mel, sha_version_mel)
         if own_mlpcpp:
-            download_module(mlpcpp_name, alt_name_mlpcpp, github_repo_mlpcpp, sha_version_mlpcpp)
+            download_module(
+                mlpcpp_name, alt_name_mlpcpp, github_repo_mlpcpp, sha_version_mlpcpp
+            )
+
 
 def is_git_directory(path="."):
     try:
diff --git a/subprojects/MLPCpp b/subprojects/MLPCpp
index 9d1b09e8865..78e8c7d8aa2 160000
--- a/subprojects/MLPCpp
+++ b/subprojects/MLPCpp
@@ -1 +1 @@
-Subproject commit 9d1b09e8865a4d142fe97ee3dd0ebb71bd36b3ad
+Subproject commit 78e8c7d8aa2759d891f27ed94d1b1506f328e254

From 2496a35bb22022aa9af86ac36df5a21a538c3757 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Wed, 29 Mar 2023 12:12:39 +0200
Subject: [PATCH 323/656] Pulled develop

---
 externals/meson        | 2 +-
 externals/ninja        | 2 +-
 externals/opdi         | 2 +-
 subprojects/CoolProp   | 2 +-
 subprojects/Mutationpp | 2 +-
 5 files changed, 5 insertions(+), 5 deletions(-)

diff --git a/externals/meson b/externals/meson
index c4cc14c27c7..41c650a040d 160000
--- a/externals/meson
+++ b/externals/meson
@@ -1 +1 @@
-Subproject commit c4cc14c27c7e46f65b410dbdd0f87dd73427b20d
+Subproject commit 41c650a040d50e0912d268af7a903a9ce1456dfa
diff --git a/externals/ninja b/externals/ninja
index 2d9083b2608..52649de2c56 160000
--- a/externals/ninja
+++ b/externals/ninja
@@ -1 +1 @@
-Subproject commit 2d9083b2608bd60c31583193d321d13a81a75beb
+Subproject commit 52649de2c56b63f42bc59513d51286531c595b44
diff --git a/externals/opdi b/externals/opdi
index f33b507c24f..1aabf5bd1ed 160000
--- a/externals/opdi
+++ b/externals/opdi
@@ -1 +1 @@
-Subproject commit f33b507c24f7448d4cf4df16ab5c53ea254b8774
+Subproject commit 1aabf5bd1ed77611742eb655002f2ac7a3dddef9
diff --git a/subprojects/CoolProp b/subprojects/CoolProp
index abcb4a53a94..0ce42fcf3bb 160000
--- a/subprojects/CoolProp
+++ b/subprojects/CoolProp
@@ -1 +1 @@
-Subproject commit abcb4a53a949e081bae7d9af4807681abe3e57fd
+Subproject commit 0ce42fcf3bb2c373512bc825a4f0c1973a78f307
diff --git a/subprojects/Mutationpp b/subprojects/Mutationpp
index 4cb6e3a05c1..5ff579f4378 160000
--- a/subprojects/Mutationpp
+++ b/subprojects/Mutationpp
@@ -1 +1 @@
-Subproject commit 4cb6e3a05c15f49ffd346dc9f185ccc3459728b0
+Subproject commit 5ff579f43781cae07411e5ab46291c9971536be6

From 6a346ff288188d34b3e6c32d4c18834107be9d6b Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Wed, 29 Mar 2023 15:45:11 +0200
Subject: [PATCH 324/656] Changed sha code for MLPCpp to refer to main branch

---
 meson_scripts/init.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 17ec689553b..4fb10b43013 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -71,7 +71,7 @@ def init_submodules(
     github_repo_coolprop = "https://github.com/CoolProp/CoolProp"
     sha_version_mel = "2484cd3258ef800a10e361016cb341834ee7930b"
     github_repo_mel = "https://github.com/pcarruscag/MEL"
-    sha_version_mlpcpp = "78e8c7d8aa2759d891f27ed94d1b1506f328e254"
+    sha_version_mlpcpp = "0de8d8c86bbf70e461a7e15cbe355084109d16c0"
     github_repo_mlpcpp = "https://github.com/EvertBunschoten/MLPCpp"
 
     medi_name = "MeDiPack"

From ca70b571232edcd27aee8569d4f26af957ff541b Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Wed, 29 Mar 2023 20:29:26 +0200
Subject: [PATCH 325/656] Checkout right submodule SHA codes

---
 externals/codi     | 2 +-
 externals/opdi     | 2 +-
 subprojects/MLPCpp | 2 +-
 3 files changed, 3 insertions(+), 3 deletions(-)

diff --git a/externals/codi b/externals/codi
index 8cdb2a2e623..427c2dc754a 160000
--- a/externals/codi
+++ b/externals/codi
@@ -1 +1 @@
-Subproject commit 8cdb2a2e6231ede6343294ac9af748b3ea105ecd
+Subproject commit 427c2dc754a628ad3c9310c766c988ac5ce21bc7
diff --git a/externals/opdi b/externals/opdi
index 1aabf5bd1ed..f33b507c24f 160000
--- a/externals/opdi
+++ b/externals/opdi
@@ -1 +1 @@
-Subproject commit 1aabf5bd1ed77611742eb655002f2ac7a3dddef9
+Subproject commit f33b507c24f7448d4cf4df16ab5c53ea254b8774
diff --git a/subprojects/MLPCpp b/subprojects/MLPCpp
index 78e8c7d8aa2..0de8d8c86bb 160000
--- a/subprojects/MLPCpp
+++ b/subprojects/MLPCpp
@@ -1 +1 @@
-Subproject commit 78e8c7d8aa2759d891f27ed94d1b1506f328e254
+Subproject commit 0de8d8c86bbf70e461a7e15cbe355084109d16c0

From 6647e7bcffd89bd09cdbe47a5cd23836cb5971ba Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Wed, 29 Mar 2023 20:59:15 +0100
Subject: [PATCH 326/656] const& and use functions in test

---
 SU2_CFD/include/drivers/CDriverBase.hpp              | 12 +++++++-----
 .../py_wrapper/deforming_bump_in_channel/run.py      |  5 +++++
 2 files changed, 12 insertions(+), 5 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index ae4581c74b2..0ca229de19d 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -124,13 +124,13 @@ class CDriverBase {
    * \brief Get the list of available outputs.
    * \return List of output names.
    */
-  inline vector<string> GetOutputNames() const { return output_container[MESH_0]->GetHistoryOutput_List(); }
+  inline vector<string> GetOutputNames() const { return output_container[MESH_0]->GetHistoryOutputList(); }
 
   /*!
    * \brief Get the value of one of the available history outputs.
    * \return Value of the output.
    */
-  inline passivedouble GetOutputValue(std::string output_name) const {
+  inline passivedouble GetOutputValue(const std::string& output_name) const {
     return SU2_TYPE::GetValue(output_container[MESH_0]->GetHistoryFieldValue(output_name));
   }
 
@@ -139,14 +139,15 @@ class CDriverBase {
    * \return List of surface output names.
    */
   inline vector<string> GetMarkerOutputNames() const {
-    return output_container[MESH_0]->GetHistoryOutputPerSurface_List();
+    return output_container[MESH_0]->GetHistoryOutputPerSurfaceList();
   }
 
   /*!
    * \brief Get the value of one of the available surface outputs at a given MARKER_MONITORING.
    * \return Value of the output.
    */
-  inline passivedouble GetMarkerMonitoringOutputValue(std::string output_name, std::string marker_monitoring) const {
+  inline passivedouble GetMarkerMonitoringOutputValue(const std::string& output_name,
+                                                      const std::string& marker_monitoring) const {
     for (auto iMarker = 0u; iMarker < main_config->GetnMarker_Monitoring(); ++iMarker) {
       if (marker_monitoring == main_config->GetMarker_Monitoring_TagBound(iMarker))
         return SU2_TYPE::GetValue(output_container[MESH_0]->GetHistoryFieldValuePerSurface(output_name, iMarker));
@@ -159,7 +160,8 @@ class CDriverBase {
    * \brief Get the value of one of the available surface outputs at a given MARKER_ANALYZE.
    * \return Value of the output.
    */
-  inline passivedouble GetMarkerAnalyzeOutputValue(std::string output_name, std::string marker_analyze) const {
+  inline passivedouble GetMarkerAnalyzeOutputValue(const std::string& output_name,
+                                                   const std::string& marker_analyze) const {
     for (auto iMarker = 0u; iMarker < main_config->GetnMarker_Analyze(); ++iMarker) {
       if (marker_analyze == main_config->GetMarker_Analyze_TagBound(iMarker))
         return SU2_TYPE::GetValue(output_container[MESH_0]->GetHistoryFieldValuePerSurface(output_name, iMarker));
diff --git a/TestCases/py_wrapper/deforming_bump_in_channel/run.py b/TestCases/py_wrapper/deforming_bump_in_channel/run.py
index 3228b6ae9a4..894315baff0 100755
--- a/TestCases/py_wrapper/deforming_bump_in_channel/run.py
+++ b/TestCases/py_wrapper/deforming_bump_in_channel/run.py
@@ -88,6 +88,11 @@ def main():
     TimeIter += 1
     time += deltaT
 
+  # Check the value of an output to cover the functionality in a regression test.
+  assert 'DRAG' in SU2Driver.GetOutputNames()
+  assert abs(SU2Driver.GetOutputValue('DRAG') -
+             SU2Driver.GetMarkerMonitoringOutputValue('DRAG_ON_SURFACE', MarkerName)) < np.finfo(float).eps
+
   # Finalize the solver and exit cleanly
   SU2Driver.Finalize()
 

From cafd89b0e30e6cc04bf3f883da76071202a020cc Mon Sep 17 00:00:00 2001
From: Kursat Yurt <kursatyurt@gmail.com>
Date: Thu, 30 Mar 2023 14:55:19 +0200
Subject: [PATCH 327/656] Change "SetContainersNull" to "InitializeContainers"

---
 SU2_CFD/include/drivers/CDriverBase.hpp           | 2 +-
 SU2_CFD/src/drivers/CDriverBase.cpp               | 2 +-
 SU2_DEF/src/drivers/CDeformationDriver.cpp        | 2 +-
 SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp | 2 +-
 4 files changed, 4 insertions(+), 4 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index 7745c6a27ff..ff714f6b797 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -691,7 +691,7 @@ class CDriverBase {
   /*!
    * \brief Initialize containers.
    */
-  void SetContainersNull();
+  void InitializeContainers();
 
   /*!
    * \brief Delete containers.
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index 309e75adaa8..431cf67dd6e 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -64,7 +64,7 @@ CDriverBase::CDriverBase(char* confFile, unsigned short val_nZone, SU2_Comm MPIC
 
 CDriverBase::~CDriverBase(void) {}
 
-void CDriverBase::SetContainersNull() {
+void CDriverBase::InitializeContainers() {
   /*--- Create pointers to all the classes that may be used by drivers. In general, the pointers are instantiated
    * down a hierarchy over all zones, multi-grid levels, equation sets, and equation terms as described in the comments
    * below. ---*/
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 92aca774ff9..3473e1b6720 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -86,7 +86,7 @@ void CDeformationDriver::Input_Preprocessing() {
 
   /*--- Initialize containers. --- */
 
-  SetContainersNull();
+  InitializeContainers();
 
   /*--- Loop over all zones to initialize the various classes. In most
    cases, nZone is equal to one. This represents the solution of a partial
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index 514a7f67c4d..087e5d04376 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -94,7 +94,7 @@ void CDiscAdjDeformationDriver::Input_Preprocessing() {
 
   /*--- Initialize containers. --- */
 
-  SetContainersNull();
+  InitializeContainers();
 
   /*--- Loop over all zones to initialize the various classes. In most
    * cases, nZone is equal to one. This represents the solution of a partial

From 4516eb46d3a490c344be8bac538e2d12ff26875a Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Thu, 30 Mar 2023 15:18:22 +0200
Subject: [PATCH 328/656] Removed inclusion of CLookUp_ANN submodule in case
 mlpcpp is disabled

---
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp                  | 6 ++++--
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp                      | 2 ++
 .../toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp   | 2 +-
 3 files changed, 7 insertions(+), 3 deletions(-)

diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index 8e6dd792551..007eb884c39 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -30,8 +30,8 @@
 
 #include <vector>
 #include "../../../Common/include/containers/CLookUpTable.hpp"
+#if defined(HAVE_MLPCPP)
 #include "CLookUp_ANN.hpp"
-#if defined(HAVE_MLPCPP) && !defined(CODI_FORWARD_TYPE) && !defined(CODI_REVERSE_TYPE)
 #define USE_MLPCPP
 #endif
 #include "CFluidModel.hpp"
@@ -70,9 +70,11 @@ class CDataDrivenFluid : public CFluidModel {
   vector<su2double*> outputs_rhoe;  // Pointers to output variables.
 
   /*--- Class variables for the multi-layer perceptron method ---*/
+#ifdef USE_MLPCPP
   MLPToolbox::CLookUp_ANN* lookup_mlp;  // multi-layer perceptron collection.
   MLPToolbox::CIOMap* iomap_rhoe;       // input-output map.
-  vector<double> MLP_inputs;            // inputs for the multi-layer perceptron look-up operation.
+#endif
+  vector<su2double> MLP_inputs;            // inputs for the multi-layer perceptron look-up operation.
 
   /*--- Class variables for the look-up table method ---*/
   CLookUpTable* lookup_table;
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 20f2d0fa0ef..0316e4d1d12 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -66,8 +66,10 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
 CDataDrivenFluid::~CDataDrivenFluid() {
   switch (Kind_DataDriven_Method) {
     case ENUM_DATADRIVEN_METHOD::MLP:
+#ifdef USE_MLPCPP
       delete iomap_rhoe;
       delete lookup_mlp;
+#endif
       break;
     case ENUM_DATADRIVEN_METHOD::LUT:
       delete lookup_table;
diff --git a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
index a484cb5f1ed..5d8f5f90957 100644
--- a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
+++ b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
@@ -27,8 +27,8 @@
 
 #include "catch.hpp"
 #include "../../../../Common/include/CConfig.hpp"
-#include "CLookUp_ANN.hpp"
 #if defined(HAVE_MLPCPP)
+#include "CLookUp_ANN.hpp"
 #define USE_MLPCPP
 #endif
 #include <vector>

From 76b475b4353d2470501d139f31c01f50d638306b Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Thu, 30 Mar 2023 16:36:52 +0200
Subject: [PATCH 329/656] Improved clang formatting and fixed build error

---
 .github/workflows/regression.yml                   |  2 +-
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp         |  2 +-
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp             |  1 -
 .../multilayer_perceptron/CLookUp_ANN_tests.cpp    | 14 +++-----------
 4 files changed, 5 insertions(+), 14 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 7459b112429..edce87f05e8 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -32,7 +32,7 @@ jobs:
           - config_set: ForwardMPI
             flags: '-Denable-directdiff=true -Denable-normal=false -Denable-tests=true --warnlevel=3 --werror'
           - config_set: BaseNoMPI
-            flags: '-Denable-pywrapper=true -Denable-openblas=true -Dwith-mpi=disabled -Denable-tests=true --warnlevel=3 --werror'
+            flags: '-Denable-pywrapper=true -Denable-openblas=true -Dwith-mpi=disabled -Denable-mlpcpp=true -Denable-tests=true --warnlevel=3 --werror'
           - config_set: ReverseNoMPI
             flags: '-Denable-autodiff=true -Denable-normal=false -Dwith-mpi=disabled -Denable-pywrapper=true -Denable-tests=true --warnlevel=3 --werror'
           - config_set: ForwardNoMPI
diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index 007eb884c39..7fcbdae492c 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -74,7 +74,7 @@ class CDataDrivenFluid : public CFluidModel {
   MLPToolbox::CLookUp_ANN* lookup_mlp;  // multi-layer perceptron collection.
   MLPToolbox::CIOMap* iomap_rhoe;       // input-output map.
 #endif
-  vector<su2double> MLP_inputs;            // inputs for the multi-layer perceptron look-up operation.
+  vector<su2double> MLP_inputs;  // inputs for the multi-layer perceptron look-up operation.
 
   /*--- Class variables for the look-up table method ---*/
   CLookUpTable* lookup_table;
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 0316e4d1d12..568b23d17ec 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -368,7 +368,6 @@ void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
 }
 
 unsigned long CDataDrivenFluid::Predict_MLP(su2double rho, su2double e) {
-
   unsigned long exit_code = 0;
 /* Evaluate MLP collection for the given values for density and energy */
 #ifdef USE_MLPCPP
diff --git a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
index 5d8f5f90957..e1c05996086 100644
--- a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
+++ b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
@@ -33,14 +33,11 @@
 #endif
 #include <vector>
 
+#ifdef USE_MLPCPP
 TEST_CASE("LookUp ANN test", "[LookUpANN]") {
   std::string MLP_input_files[] = {"src/SU2/UnitTests/Common/toolboxes/multilayer_perceptron/simple_mlp.mlp"};
   unsigned short n_MLPs = 1;
-#ifdef USE_MLPCPP
   MLPToolbox::CLookUp_ANN ANN(n_MLPs, MLP_input_files);
-#else
-  SU2_MPI::Error("SU2 was not compiled with MLPCpp enabled (-Denable-mlpcpp=true).", CURRENT_FUNCTION);
-#endif
   std::vector<std::string> MLP_input_names, MLP_output_names;
   std::vector<double> MLP_inputs;
   std::vector<double*> MLP_outputs;
@@ -57,19 +54,15 @@ TEST_CASE("LookUp ANN test", "[LookUpANN]") {
   MLP_output_names[0] = "z";
   MLP_outputs[0] = &z;
 
-/*--- Generate input-output map ---*/
-#ifdef USE_MLPCPP
+  /*--- Generate input-output map ---*/
   MLPToolbox::CIOMap iomap(&ANN, MLP_input_names, MLP_output_names);
-#endif
   /*--- MLP evaluation on point in the middle of the training data range ---*/
   x = 1.0;
   y = -0.5;
 
   MLP_inputs[0] = x;
   MLP_inputs[1] = y;
-#ifdef USE_MLPCPP
   ANN.PredictANN(&iomap, MLP_inputs, MLP_outputs);
-#endif
   CHECK(z == Approx(0.344829));
 
   /*--- MLP evaluation on point outside the training data range ---*/
@@ -77,8 +70,7 @@ TEST_CASE("LookUp ANN test", "[LookUpANN]") {
   y = -10;
   MLP_inputs[0] = x;
   MLP_inputs[1] = y;
-#ifdef USE_MLPCPP
   ANN.PredictANN(&iomap, MLP_inputs, MLP_outputs);
-#endif
   CHECK(z == Approx(0.012737));
 }
+#endif

From 53cb6e56c748a74740405207b17a94ea5a4e7750 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Thu, 30 Mar 2023 17:15:48 +0200
Subject: [PATCH 330/656] Fixed clang-format using pre-commit

---
 Docs/docmain.hpp | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/Docs/docmain.hpp b/Docs/docmain.hpp
index 70809a35804..fcda1b961ec 100644
--- a/Docs/docmain.hpp
+++ b/Docs/docmain.hpp
@@ -228,6 +228,6 @@
 
 /*!
  * \defgroup Multi-Layer Perceptrons (MLP)
- * \brief Data look up and interpolation via dense, feed-forward multi-layer perceptrons. 
+ * \brief Data look up and interpolation via dense, feed-forward multi-layer perceptrons.
  * \ingroup Toolboxes
-*/
+ */

From 55dc1b564fb2ebe32325bf4a9029bc154897649e Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Thu, 30 Mar 2023 19:14:11 +0200
Subject: [PATCH 331/656] Pulled develop

---
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp | 6 ------
 preconfigure.py                        | 4 +++-
 2 files changed, 3 insertions(+), 7 deletions(-)

diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 568b23d17ec..78bf25716f1 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -375,12 +375,6 @@ unsigned long CDataDrivenFluid::Predict_MLP(su2double rho, su2double e) {
   MLP_inputs[idx_e] = e;
   exit_code = lookup_mlp->PredictANN(iomap_rhoe, MLP_inputs, outputs_rhoe);
 #endif
-  /* Apply exponential transformation to the MLP outputs for the first and second
-     derivative of the entropy w.r.t density */
-  // Optional:
-  // dsdrho_e = -exp(dsdrho_e);
-  // d2sdrho2 = exp(d2sdrho2);
-
   return exit_code;
 }
 
diff --git a/preconfigure.py b/preconfigure.py
index 61d63abd89a..c6dc0220a5f 100755
--- a/preconfigure.py
+++ b/preconfigure.py
@@ -81,6 +81,7 @@ def run(
     own_mpp=True,
     own_cool=True,
     own_mel=True,
+    own_mlpcpp=True,
 ):
 
     # Set up the build environment, i.e. clone or download submodules
@@ -93,6 +94,7 @@ def run(
         own_mpp=own_mpp,
         own_cool=own_cool,
         own_mel=own_mel,
+        own_mlpcpp=own_mlpcpp,
     )
 
     if own_meson:
@@ -150,5 +152,5 @@ def run(
         own_mpp=args.no_mpp,
         own_cool=args.no_coolprop,
         own_mel=args.no_mel,
-        own_mlp=args.no_mlpcpp,
+        own_mlpcpp=args.no_mlpcpp,
     )

From 72858e8928d3b4943b410a3d890c224d51f436cc Mon Sep 17 00:00:00 2001
From: Kursat Yurt <kursatyurt@gmail.com>
Date: Fri, 31 Mar 2023 09:00:28 +0200
Subject: [PATCH 332/656] Rewording regarding to Initialize/Finalize.

Some more rewording

Remove underscore
---
 SU2_CFD/include/drivers/CDriver.hpp           | 44 +++++-----
 SU2_CFD/include/drivers/CDriverBase.hpp       |  6 +-
 SU2_CFD/src/drivers/CDriver.cpp               | 86 +++++++++----------
 SU2_CFD/src/python_wrapper_structure.cpp      |  2 +-
 .../include/drivers/CDeformationDriver.hpp    | 10 +--
 SU2_DEF/src/drivers/CDeformationDriver.cpp    | 20 ++---
 6 files changed, 84 insertions(+), 84 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index c78370bfc69..d0772a6b5d3 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -108,14 +108,14 @@ class CDriver : public CDriverBase {
   /*!
    * \brief Initialize containers. 
    */
-  void SetContainersNull();
+  void InitializeContainers();
 
   /*!
    * \brief Read in the config and mesh files.
    * \param[in] config - Definition of the particular problem.
    * \param[in] driver_config - Definition of the driver configuration.
    */
-  void InputPreprocessing(CConfig**& config, CConfig*& driver_config);
+  void PreprocessInput(CConfig**& config, CConfig*& driver_config);
 
   /*!
    * \brief Construction of the edge-based data structure and the multi-grid structure.
@@ -123,28 +123,28 @@ class CDriver : public CDriverBase {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] dummy - Definition of the dummy driver.
    */
-  void GeometricalPreprocessing(CConfig* config, CGeometry**& geometry, bool dummy);
+  void InitializeGeometry(CConfig* config, CGeometry**& geometry, bool dummy);
 
   /*!
    * \brief Do the geometrical preprocessing for the DG FEM solver.
    * \param[in] config - Definition of the particular problem.
    * \param[in] geometry - Geometrical definition of the problem.
    */
-  void Geometrical_Preprocessing_DGFEM(CConfig* config, CGeometry**& geometry);
+  void InitializeGeometryDGFEM(CConfig* config, CGeometry**& geometry);
 
   /*!
-   * \brief Geometrical_Preprocessing_FVM
+   * \brief InitializeGeometryFVM
    * \param[in] config - Definition of the particular problem.
    * \param[in] geometry - Geometrical definition of the problem.
    */
-  void Geometrical_Preprocessing_FVM(CConfig* config, CGeometry**& geometry);
+  void InitializeGeometryFVM(CConfig* config, CGeometry**& geometry);
 
   /*!
    * \brief Definition of the physics iteration class or within a single zone.
    * \param[in] config - Definition of the particular problem.
    * \param[in] iteration - Pointer to the iteration container to be instantiated.
    */
-  void IterationPreprocessing(CConfig* config, CIteration*& iteration) const;
+  void PreprocessIteration(CConfig* config, CIteration*& iteration) const;
 
   /*!
    * \brief Definition and allocation of all solution classes.
@@ -152,7 +152,7 @@ class CDriver : public CDriverBase {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] solver - Container vector with all the solutions.
    */
-  void SolverPreprocessing(CConfig* config, CGeometry** geometry, CSolver***& solver);
+  void InitializeSolver(CConfig* config, CGeometry** geometry, CSolver***& solver);
 
   /*!
    * \brief Restart of the solvers from the restart files.
@@ -161,7 +161,7 @@ class CDriver : public CDriverBase {
    * \param[in] config - Definition of the particular problem.
    * \param[in] update_geo - Boolean to indicate if geometry should be updated.
    */
-  void SolverRestart(CSolver*** solver, CGeometry** geometry, CConfig* config, bool update_geo);
+  void RestartSolver(CSolver*** solver, CGeometry** geometry, CConfig* config, bool update_geo);
 
   /*!
    * \brief Definition and allocation of all solution classes.
@@ -170,7 +170,7 @@ class CDriver : public CDriverBase {
    * \param[in] config - Definition of the particular problem.
    * \param[in] val_iInst - Current solver instance.
    */
-  void SolverPostprocessing(CSolver**** solver, CGeometry** geometry, CConfig* config, unsigned short val_iInst);
+  void FinalizeSolver(CSolver**** solver, CGeometry** geometry, CConfig* config, unsigned short val_iInst);
 
   /*!
    * \brief Definition and allocation of all integration classes.
@@ -178,7 +178,7 @@ class CDriver : public CDriverBase {
    * \param[in] solver - Container vector with all the solutions.
    * \param[in] integration - Container vector with all the integration methods.
    */
-  void IntegrationPreprocessing(CConfig* config, CSolver** solver, CIntegration**& integration) const;
+  void InitializeIntegration(CConfig* config, CSolver** solver, CIntegration**& integration) const;
 
   /*!
    * \brief Definition and allocation of all integration classes.
@@ -187,7 +187,7 @@ class CDriver : public CDriverBase {
    * \param[in] config - Definition of the particular problem.
    * \param[in] val_iInst - Current solver instance.
    */
-  void IntegrationPostprocessing(CIntegration*** integration, CGeometry** geometry, CConfig* config,
+  void FinalizeIntegration(CIntegration*** integration, CGeometry** geometry, CConfig* config,
                                   unsigned short val_iInst);
 
   /*!
@@ -199,7 +199,7 @@ class CDriver : public CDriverBase {
    * \param[in] interface - Class defining the physical transfer of information.
    * \param[in] interpolation -  Object defining the interpolation.
    */
-  void InterfacePreprocessing(CConfig** config, CSolver***** solver, CGeometry**** geometry,
+  void InitializeInterface(CConfig** config, CSolver***** solver, CGeometry**** geometry,
                                unsigned short** interface_types, CInterface*** interface,
                                vector<vector<unique_ptr<CInterpolator>>>& interpolation);
 
@@ -210,7 +210,7 @@ class CDriver : public CDriverBase {
    * \param[in] solver - Container vector with all the solutions.
    * \param[in] numerics - Description of the numerical method (the way in which the equations are solved).
    */
-  void NumericsPreprocessing(CConfig* config, CGeometry** geometry, CSolver*** solver, CNumerics****& numerics) const;
+  void InitializeNumerics(CConfig* config, CGeometry** geometry, CSolver*** solver, CNumerics****& numerics) const;
 
   /*!
    * \brief Helper to instantiate turbulence numerics specialized for different flow solvers.
@@ -240,7 +240,7 @@ class CDriver : public CDriverBase {
    * \param[in] config - Definition of the particular problem.
    * \param[in] val_iInst - Current solver instance.
    */
-  void NumericsPostprocessing(CNumerics***** numerics, CSolver*** solver, CGeometry** geometry, CConfig* config,
+  void FinalizeNumerics(CNumerics***** numerics, CSolver*** solver, CGeometry** geometry, CConfig* config,
                                unsigned short val_iInst);
 
   /*!
@@ -252,7 +252,7 @@ class CDriver : public CDriverBase {
    * \param[in] grid_movement - Volume grid movement classes of the problem.
    * \param[in] surface_movement - Surface movement classes of the problem.
    */
-  void DynamicMeshPreprocessing(CConfig* config, CGeometry** geometry, CSolver*** solver, CIteration* iteration,
+  void PreprocessDynamicMesh(CConfig* config, CGeometry** geometry, CSolver*** solver, CIteration* iteration,
                                  CVolumetricMovement*& grid_movement, CSurfaceMovement*& surface_movement) const;
 
   /*!
@@ -262,7 +262,7 @@ class CDriver : public CDriverBase {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] solver - Container vector with all the solutions.
    */
-  void PythonInterfacePreprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver);
+  void PreprocessPythonInterface(CConfig** config, CGeometry**** geometry, CSolver***** solver);
 
   /*!
    * \brief Preprocess the output container.
@@ -271,7 +271,7 @@ class CDriver : public CDriverBase {
    * \param[in] output_container - Container vector with all the outputs.
    * \param[in] driver_output - Definition of the driver output.
    */
-  void OutputPreprocessing(CConfig** config, CConfig* driver_config, COutput**& output_container,
+  void PreprocessOutput(CConfig** config, CConfig* driver_config, COutput**& output_container,
                             COutput*& driver_output);
 
   /*!
@@ -279,7 +279,7 @@ class CDriver : public CDriverBase {
    * \param[in] config - Definition of the particular problem.
    * \param[in] geometry - Geometrical definition of the problem.
    */
-  void StaticMeshPreprocessing(const CConfig* config, CGeometry** geometry);
+  void PreprocessStaticMesh(const CConfig* config, CGeometry** geometry);
 
   /*!
    * \brief Initiate value for static mesh movement such as the gridVel for the ROTATING frame.
@@ -288,7 +288,7 @@ class CDriver : public CDriverBase {
    * \param[in] solver - Container vector with all the solutions.
    * \param[in] interface - Class defining the physical transfer of information.
    */
-  void TurbomachineryPreprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver,
+  void PreprocessTurbomachinery(CConfig** config, CGeometry**** geometry, CSolver***** solver,
                                     CInterface*** interface);
 
   /*!
@@ -494,7 +494,7 @@ class CDriver : public CDriverBase {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void InletPreprocessing(CSolver*** solver, CGeometry** geometry, CConfig* config) const;
+  void PreprocessInlet(CSolver*** solver, CGeometry** geometry, CConfig* config) const;
 
   /*!
    * \brief Set the position of the heat source.
@@ -691,7 +691,7 @@ class CHBDriver : public CFluidDriver {
    * \brief Computation of the Harmonic Balance operator matrix for harmonic balance.
    * \author A. Rubino, S. Nimmagadda
    */
-  void ComputeHB_Operator();
+  void ComputeHBOperator();
 
   /*!
    * \brief Update the solution for the Harmonic Balance.
diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index ff714f6b797..96595b365f5 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -711,7 +711,7 @@ class CDriverBase {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] dummy - Definition of the dummy driver.
    */
-  void GeometricalPreprocessing(CConfig* config, CGeometry**& geometry, bool dummy);
+  void InitializeGeometry(CConfig* config, CGeometry**& geometry, bool dummy);
 
   /*!
    * \brief Definition and allocation of all solution classes.
@@ -719,7 +719,7 @@ class CDriverBase {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] solver - Container vector with all the solutions.
    */
-  void SolverPreprocessing(CConfig* config, CGeometry** geometry, CSolver***& solver);
+  void InitializeSolver(CConfig* config, CGeometry** geometry, CSolver***& solver);
 
   /*!
    * \brief Definition and allocation of all solver classes.
@@ -728,7 +728,7 @@ class CDriverBase {
    * \param[in] solver - Container vector with all the solutions.
    * \param[in] numerics - Description of the numerical method (the way in which the equations are solved).
    */
-  void NumericsPreprocessing(CConfig* config, CGeometry** geometry, CSolver*** solver, CNumerics****& numerics) const;
+  void InitializeNumerics(CConfig* config, CGeometry** geometry, CSolver*** solver, CNumerics****& numerics) const;
 
   /*!
    * \brief Preprocess the output container.
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index da0e1216732..fb788d47eb5 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -114,11 +114,11 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
 
   /*--- Initialize containers with null --- */
 
-  SetContainersNull();
+  InitializeContainers();
 
   /*--- Preprocessing of the config files. ---*/
 
-  InputPreprocessing(config_container, driver_config);
+  PreprocessInput(config_container, driver_config);
 
   /*--- Retrieve dimension from mesh file ---*/
 
@@ -127,7 +127,7 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
 
   /*--- Output preprocessing ---*/
 
-  OutputPreprocessing(config_container, driver_config, output_container, driver_output);
+  PreprocessOutput(config_container, driver_config, output_container, driver_output);
 
 
   for (iZone = 0; iZone < nZone; iZone++) {
@@ -157,7 +157,7 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
        identified and linked, face areas and volumes of the dual mesh cells are
        computed, and the multigrid levels are created using an agglomeration procedure. ---*/
 
-      GeometricalPreprocessing(config_container[iZone], geometry_container[iZone][iInst], dry_run);
+      InitializeGeometry(config_container[iZone], geometry_container[iZone][iInst], dry_run);
 
     }
   }
@@ -180,7 +180,7 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
        fluxes, loops over the nodes to compute source terms, and routines for
        imposing various boundary condition type for the PDE. ---*/
 
-      SolverPreprocessing(config_container[iZone], geometry_container[iZone][iInst], solver_container[iZone][iInst]);
+      InitializeSolver(config_container[iZone], geometry_container[iZone][iInst], solver_container[iZone][iInst]);
 
       /*--- Definition of the numerical method class:
        numerics_container[#ZONES][#INSTANCES][#MG_GRIDS][#EQ_SYSTEMS][#EQ_TERMS].
@@ -189,7 +189,7 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
        data structure (centered, upwind, galerkin), as well as any source terms
        (piecewise constant reconstruction) evaluated in each dual mesh volume. ---*/
 
-      NumericsPreprocessing(config_container[iZone], geometry_container[iZone][iInst],
+      InitializeNumerics(config_container[iZone], geometry_container[iZone][iInst],
                              solver_container[iZone][iInst], numerics_container[iZone][iInst]);
 
       /*--- Definition of the integration class: integration_container[#ZONES][#INSTANCES][#EQ_SYSTEMS].
@@ -198,7 +198,7 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
        the residual at each node, R(U) and then integrates the equations to a
        steady state or time-accurately. ---*/
 
-      IntegrationPreprocessing(config_container[iZone], solver_container[iZone][iInst][MESH_0],
+      InitializeIntegration(config_container[iZone], solver_container[iZone][iInst][MESH_0],
                                 integration_container[iZone][iInst]);
 
       /*--- Instantiate the type of physics iteration to be executed within each zone. For
@@ -206,16 +206,16 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
        different physics in different zones (fluid-structure interaction), or couple multiple
        systems tightly within a single zone by creating a new iteration class (e.g., RANS). ---*/
 
-      IterationPreprocessing(config_container[iZone], iteration_container[iZone][iInst]);
+      PreprocessIteration(config_container[iZone], iteration_container[iZone][iInst]);
 
       /*--- Dynamic mesh processing.  ---*/
 
-      DynamicMeshPreprocessing(config_container[iZone], geometry_container[iZone][iInst], solver_container[iZone][iInst],
+      PreprocessDynamicMesh(config_container[iZone], geometry_container[iZone][iInst], solver_container[iZone][iInst],
                                 iteration_container[iZone][iInst], grid_movement[iZone][iInst], surface_movement[iZone]);
 
       /*--- Static mesh processing.  ---*/
 
-      StaticMeshPreprocessing(config_container[iZone], geometry_container[iZone][iInst]);
+      PreprocessStaticMesh(config_container[iZone], geometry_container[iZone][iInst]);
 
     }
 
@@ -232,14 +232,14 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
     if (rank == MASTER_NODE)
       cout << endl <<"------------------- Multizone Interface Preprocessing -------------------" << endl;
 
-    InterfacePreprocessing(config_container, solver_container, geometry_container,
+    InitializeInterface(config_container, solver_container, geometry_container,
                             interface_types, interface_container, interpolator_container);
   }
 
   if (fsi) {
     for (iZone = 0; iZone < nZone; iZone++) {
       for (iInst = 0; iInst < nInst[iZone]; iInst++){
-        SolverRestart(solver_container[iZone][iInst], geometry_container[iZone][iInst],
+        RestartSolver(solver_container[iZone][iInst], geometry_container[iZone][iInst],
                        config_container[iZone], true);
       }
     }
@@ -249,11 +249,11 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
     if (rank == MASTER_NODE)
       cout << endl <<"---------------------- Turbomachinery Preprocessing ---------------------" << endl;
 
-    TurbomachineryPreprocessing(config_container, geometry_container, solver_container, interface_container);
+    PreprocessTurbomachinery(config_container, geometry_container, solver_container, interface_container);
   }
 
 
-  PythonInterfacePreprocessing(config_container, geometry_container, solver_container);
+  PreprocessPythonInterface(config_container, geometry_container, solver_container);
 
 
   /*--- Preprocessing time is reported now, but not included in the next compute portion. ---*/
@@ -294,7 +294,7 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
 
 }
 
-void CDriver::SetContainersNull(){
+void CDriver::InitializeContainers(){
 
   /*--- Create pointers to all of the classes that may be used throughout
    the SU2_CFD code. In general, the pointers are instantiated down a
@@ -366,7 +366,7 @@ void CDriver::Finalize() {
 
   for (iZone = 0; iZone < nZone; iZone++) {
     for (iInst = 0; iInst < nInst[iZone]; iInst++){
-      NumericsPostprocessing(numerics_container[iZone], solver_container[iZone][iInst],
+      FinalizeNumerics(numerics_container[iZone], solver_container[iZone][iInst],
           geometry_container[iZone][iInst], config_container[iZone], iInst);
     }
     delete [] numerics_container[iZone];
@@ -376,7 +376,7 @@ void CDriver::Finalize() {
 
   for (iZone = 0; iZone < nZone; iZone++) {
     for (iInst = 0; iInst < nInst[iZone]; iInst++){
-      IntegrationPostprocessing(integration_container[iZone],
+      FinalizeIntegration(integration_container[iZone],
           geometry_container[iZone][iInst],
           config_container[iZone],
           iInst);
@@ -388,7 +388,7 @@ void CDriver::Finalize() {
 
   for (iZone = 0; iZone < nZone; iZone++) {
     for (iInst = 0; iInst < nInst[iZone]; iInst++){
-      SolverPostprocessing(solver_container[iZone],
+      FinalizeSolver(solver_container[iZone],
           geometry_container[iZone][iInst],
           config_container[iZone],
           iInst);
@@ -548,7 +548,7 @@ void CDriver::Finalize() {
 }
 
 
-void CDriver::InputPreprocessing(CConfig **&config, CConfig *&driver_config) {
+void CDriver::PreprocessInput(CConfig **&config, CConfig *&driver_config) {
 
   char zone_file_name[MAX_STRING_SIZE];
 
@@ -600,7 +600,7 @@ void CDriver::InputPreprocessing(CConfig **&config, CConfig *&driver_config) {
   fsi = config_container[ZONE_0]->GetFSI_Simulation();
 }
 
-void CDriver::GeometricalPreprocessing(CConfig* config, CGeometry **&geometry, bool dummy){
+void CDriver::InitializeGeometry(CConfig* config, CGeometry **&geometry, bool dummy){
 
   if (!dummy){
     if (rank == MASTER_NODE)
@@ -609,13 +609,13 @@ void CDriver::GeometricalPreprocessing(CConfig* config, CGeometry **&geometry, b
     if( fem_solver ) {
       switch( config->GetKind_FEM_Flow() ) {
         case DG: {
-            Geometrical_Preprocessing_DGFEM(config, geometry);
+            InitializeGeometryDGFEM(config, geometry);
             break;
           }
       }
     }
     else {
-      Geometrical_Preprocessing_FVM(config, geometry);
+      InitializeGeometryFVM(config, geometry);
     }
   } else {
     if (rank == MASTER_NODE)
@@ -701,7 +701,7 @@ void CDriver::GeometricalPreprocessing(CConfig* config, CGeometry **&geometry, b
   main_geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 }
 
-void CDriver::Geometrical_Preprocessing_FVM(CConfig *config, CGeometry **&geometry) {
+void CDriver::InitializeGeometryFVM(CConfig *config, CGeometry **&geometry) {
 
   unsigned short iZone = config->GetiZone(), iMGlevel;
   unsigned short requestedMGlevels = config->GetnMGLevels();
@@ -921,7 +921,7 @@ void CDriver::Geometrical_Preprocessing_FVM(CConfig *config, CGeometry **&geomet
 
 }
 
-void CDriver::Geometrical_Preprocessing_DGFEM(CConfig* config, CGeometry **&geometry) {
+void CDriver::InitializeGeometryDGFEM(CConfig* config, CGeometry **&geometry) {
 
   /*--- Definition of the geometry class to store the primal grid in the partitioning process. ---*/
   /*--- All ranks process the grid and call ParMETIS for partitioning ---*/
@@ -1007,13 +1007,13 @@ void CDriver::Geometrical_Preprocessing_DGFEM(CConfig* config, CGeometry **&geom
 
   for(unsigned short iMGlevel=1; iMGlevel<=config->GetnMGLevels(); iMGlevel++) {
 
-    SU2_MPI::Error("Geometrical_Preprocessing_DGFEM: Coarse grid levels not implemented yet.",
+    SU2_MPI::Error("InitializeGeometryDGFEM: Coarse grid levels not implemented yet.",
                    CURRENT_FUNCTION);
   }
 
 }
 
-void CDriver::SolverPreprocessing(CConfig* config, CGeometry** geometry, CSolver ***&solver) {
+void CDriver::InitializeSolver(CConfig* config, CGeometry** geometry, CSolver ***&solver) {
 
   MAIN_SOLVER kindSolver = config->GetKind_Solver();
 
@@ -1036,15 +1036,15 @@ void CDriver::SolverPreprocessing(CConfig* config, CGeometry** geometry, CSolver
   /*--- Restart solvers, for FSI the geometry cannot be updated because the interpolation classes
    * should always use the undeformed mesh (otherwise the results would not be repeatable). ---*/
 
-  if (!fsi) SolverRestart(solver, geometry, config, true);
+  if (!fsi) RestartSolver(solver, geometry, config, true);
 
   /*--- Set up any necessary inlet profiles ---*/
 
-  InletPreprocessing(solver, geometry, config);
+  PreprocessInlet(solver, geometry, config);
 
 }
 
-void CDriver::InletPreprocessing(CSolver ***solver, CGeometry **geometry,
+void CDriver::PreprocessInlet(CSolver ***solver, CGeometry **geometry,
                                   CConfig *config) const {
 
   /*--- Adjust iteration number for unsteady restarts. ---*/
@@ -1116,7 +1116,7 @@ void CDriver::InletPreprocessing(CSolver ***solver, CGeometry **geometry,
 
 }
 
-void CDriver::SolverRestart(CSolver ***solver, CGeometry **geometry,
+void CDriver::RestartSolver(CSolver ***solver, CGeometry **geometry,
                              CConfig *config, bool update_geo) {
 
   /*--- Check for restarts and use the LoadRestart() routines. ---*/
@@ -1171,7 +1171,7 @@ void CDriver::SolverRestart(CSolver ***solver, CGeometry **geometry,
 
 }
 
-void CDriver::SolverPostprocessing(CSolver ****solver, CGeometry **geometry,
+void CDriver::FinalizeSolver(CSolver ****solver, CGeometry **geometry,
                                     CConfig *config, unsigned short val_iInst) {
 
   for (int iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
@@ -1186,7 +1186,7 @@ void CDriver::SolverPostprocessing(CSolver ****solver, CGeometry **geometry,
 
 }
 
-void CDriver::IntegrationPreprocessing(CConfig *config, CSolver **solver, CIntegration **&integration) const {
+void CDriver::InitializeIntegration(CConfig *config, CSolver **solver, CIntegration **&integration) const {
 
   if (rank == MASTER_NODE)
     cout << endl <<"----------------- Integration Preprocessing ( Zone " << config->GetiZone() <<" ) ------------------" << endl;
@@ -1197,7 +1197,7 @@ void CDriver::IntegrationPreprocessing(CConfig *config, CSolver **solver, CInteg
 
 }
 
-void CDriver::IntegrationPostprocessing(CIntegration ***integration, CGeometry **geometry, CConfig *config, unsigned short val_iInst) {
+void CDriver::FinalizeIntegration(CIntegration ***integration, CGeometry **geometry, CConfig *config, unsigned short val_iInst) {
 
   for (unsigned int iSol = 0; iSol < MAX_SOLS; iSol++){
     delete integration[val_iInst][iSol];
@@ -1446,7 +1446,7 @@ template void CDriver::InstantiateSpeciesNumerics<CIncEulerVariable::CIndices<un
 template void CDriver::InstantiateSpeciesNumerics<CNEMOEulerVariable::CIndices<unsigned short>>(
     unsigned short, int, const CConfig*, const CSolver*, CNumerics****&) const;
 
-void CDriver::NumericsPreprocessing(CConfig *config, CGeometry **geometry, CSolver ***solver, CNumerics ****&numerics) const {
+void CDriver::InitializeNumerics(CConfig *config, CGeometry **geometry, CSolver ***solver, CNumerics ****&numerics) const {
 
   if (rank == MASTER_NODE)
     cout << endl <<"------------------- Numerics Preprocessing ( Zone " << config->GetiZone() <<" ) -------------------" << endl;
@@ -2355,7 +2355,7 @@ void CDriver::NumericsPreprocessing(CConfig *config, CGeometry **geometry, CSolv
 
 }
 
-void CDriver::NumericsPostprocessing(CNumerics *****numerics, CSolver***, CGeometry**,
+void CDriver::FinalizeNumerics(CNumerics *****numerics, CSolver***, CGeometry**,
                                       CConfig *config, unsigned short val_iInst) {
 
   for (unsigned short iMGlevel = 0; iMGlevel <= config->GetnMGLevels(); iMGlevel++) {
@@ -2374,7 +2374,7 @@ void CDriver::NumericsPostprocessing(CNumerics *****numerics, CSolver***, CGeome
 
 }
 
-void CDriver::IterationPreprocessing(CConfig* config, CIteration *&iteration) const {
+void CDriver::PreprocessIteration(CConfig* config, CIteration *&iteration) const {
 
   if (rank == MASTER_NODE)
     cout << endl <<"------------------- Iteration Preprocessing ( Zone " << config->GetiZone() <<" ) ------------------" << endl;
@@ -2383,7 +2383,7 @@ void CDriver::IterationPreprocessing(CConfig* config, CIteration *&iteration) co
 
 }
 
-void CDriver::DynamicMeshPreprocessing(CConfig *config, CGeometry **geometry, CSolver ***solver, CIteration* iteration,
+void CDriver::PreprocessDynamicMesh(CConfig *config, CGeometry **geometry, CSolver ***solver, CIteration* iteration,
                                         CVolumetricMovement *&grid_movement, CSurfaceMovement *&surface_movement) const{
 
   /*--- Instantiate the geometry movement classes for the solution of unsteady
@@ -2424,7 +2424,7 @@ void CDriver::DynamicMeshPreprocessing(CConfig *config, CGeometry **geometry, CS
 
 }
 
-void CDriver::InterfacePreprocessing(CConfig **config, CSolver***** solver, CGeometry**** geometry,
+void CDriver::InitializeInterface(CConfig **config, CSolver***** solver, CGeometry**** geometry,
                                       unsigned short** interface_types, CInterface ***interface,
                                       vector<vector<unique_ptr<CInterpolator> > >& interpolation) {
 
@@ -2550,7 +2550,7 @@ void CDriver::InterfacePreprocessing(CConfig **config, CSolver***** solver, CGeo
 
 }
 
-void CDriver::StaticMeshPreprocessing(const CConfig *config, CGeometry** geometry){
+void CDriver::PreprocessStaticMesh(const CConfig *config, CGeometry** geometry){
 
   unsigned short iMGlevel, iMGfine;
   unsigned short Kind_Grid_Movement;
@@ -2640,7 +2640,7 @@ void CDriver::StaticMeshPreprocessing(const CConfig *config, CGeometry** geometr
 
 }
 
-void CDriver::OutputPreprocessing(CConfig **config, CConfig *driver_config, COutput **&output, COutput *&driver_output){
+void CDriver::PreprocessOutput(CConfig **config, CConfig *driver_config, COutput **&output, COutput *&driver_output){
 
   /*--- Definition of the output class (one for each zone). The output class
    manages the writing of all restart, volume solution, surface solution,
@@ -2679,7 +2679,7 @@ void CDriver::OutputPreprocessing(CConfig **config, CConfig *driver_config, COut
 }
 
 
-void CDriver::TurbomachineryPreprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver,
+void CDriver::PreprocessTurbomachinery(CConfig** config, CGeometry**** geometry, CSolver***** solver,
                                            CInterface*** interface){
 
   unsigned short donorZone,targetZone, nMarkerInt, iMarkerInt;
@@ -3587,7 +3587,7 @@ void CHBDriver::SetHarmonicBalance(unsigned short iInst) {
   period /= config_container[ZONE_0]->GetTime_Ref();
 
   if (InnerIter == 0)
-    ComputeHB_Operator();
+    ComputeHBOperator();
 
   /*--- Compute various source terms for explicit direct, implicit direct, and adjoint problems ---*/
   /*--- Loop over all grid levels ---*/
@@ -3842,7 +3842,7 @@ void CHBDriver::StabilizeHarmonicBalance() {
 
 }
 
-void CHBDriver::ComputeHB_Operator() {
+void CHBDriver::ComputeHBOperator() {
 
   const   complex<su2double> J(0.0,1.0);
   unsigned short i, j, k, iInst;
diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index c3583210666..1d7bfb5bb67 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -29,7 +29,7 @@
 #include "../include/drivers/CDriver.hpp"
 #include "../include/drivers/CSinglezoneDriver.hpp"
 
-void CDriver::PythonInterfacePreprocessing(CConfig** config, CGeometry**** geometry, CSolver***** solver) {
+void CDriver::PreprocessPythonInterface(CConfig** config, CGeometry**** geometry, CSolver***** solver) {
   int rank = MASTER_NODE;
   SU2_MPI::Comm_rank(SU2_MPI::GetComm(), &rank);
 
diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index ed63059e972..24d640e30fb 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -77,27 +77,27 @@ class CDeformationDriver : public CDriverBase {
   /*!
    * \brief Read in the config and mesh files.
    */
-  void Input_Preprocessing();
+  void PreprocessInput();
 
   /*!
    * \brief Construction of the edge-based data structure.
    */
-  void Geometrical_Preprocessing();
+  void InitializeGeometry();
 
   /*!
    * \brief Preprocess the output container.
    */
-  void Output_Preprocessing();
+  void PreprocessOutput();
 
   /*!
    * \brief Preprocess the mesh solver container.
    */
-  void Solver_Preprocessing();
+  void InitializeSolver();
 
   /*!
    * \brief Preprocess the numerics container.
    */
-  void Numerics_Preprocessing();
+  void InitializeNumerics();
 
   /*!
    * \brief Mesh deformation based on linear elasticity solver (CMeshSolver).
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 3473e1b6720..7f40c2d8c9c 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -38,7 +38,7 @@ CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
     : CDriverBase(confFile, 1, MPICommunicator) {
   /*--- Preprocessing of the config files. ---*/
 
-  Input_Preprocessing();
+  PreprocessInput();
 
   /*--- Set up a timer for performance benchmarking. ---*/
 
@@ -46,20 +46,20 @@ CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
 
   /*--- Preprocessing of the geometry for all zones. ---*/
 
-  Geometrical_Preprocessing();
+  InitializeGeometry();
 
   /*--- Preprocessing of the output for all zones. ---*/
 
-  Output_Preprocessing();
+  PreprocessOutput();
 
   if (driver_config->GetDeform_Mesh()) {
     /*--- Preprocessing of the mesh solver for all zones. ---*/
 
-    Solver_Preprocessing();
+    InitializeSolver();
 
     /*--- Preprocessing of the mesh solver for all zones. ---*/
 
-    Numerics_Preprocessing();
+    InitializeNumerics();
   }
 
   /*--- Preprocessing time is reported now, but not included in the next compute portion. ---*/
@@ -73,7 +73,7 @@ CDeformationDriver::CDeformationDriver(char* confFile, SU2_Comm MPICommunicator)
   UsedTimeCompute = 0.0;
 }
 
-void CDeformationDriver::Input_Preprocessing() {
+void CDeformationDriver::PreprocessInput() {
   /*--- Initialize a char to store the zone filename. ---*/
 
   char zone_file_name[MAX_STRING_SIZE];
@@ -123,7 +123,7 @@ void CDeformationDriver::Input_Preprocessing() {
   main_config = config_container[ZONE_0];
 }
 
-void CDeformationDriver::Geometrical_Preprocessing() {
+void CDeformationDriver::InitializeGeometry() {
   for (iZone = 0; iZone < nZone; iZone++) {
     /*--- Definition of the geometry class to store the primal grid in the partitioning process. ---*/
 
@@ -206,7 +206,7 @@ void CDeformationDriver::Geometrical_Preprocessing() {
   main_geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 }
 
-void CDeformationDriver::Output_Preprocessing() {
+void CDeformationDriver::PreprocessOutput() {
   for (iZone = 0; iZone < nZone; iZone++) {
     /*--- Allocate the mesh output. ---*/
 
@@ -223,7 +223,7 @@ void CDeformationDriver::Output_Preprocessing() {
   }
 }
 
-void CDeformationDriver::Solver_Preprocessing() {
+void CDeformationDriver::InitializeSolver() {
   for (iZone = 0; iZone < nZone; iZone++) {
     unsigned short nInst_Zone = nInst[iZone];
     unsigned short nMesh = 1;
@@ -237,7 +237,7 @@ void CDeformationDriver::Solver_Preprocessing() {
   }
 }
 
-void CDeformationDriver::Numerics_Preprocessing() {
+void CDeformationDriver::InitializeNumerics() {
   for (iZone = 0; iZone < nZone; iZone++) {
     unsigned short nInst_Zone = nInst[iZone];
     unsigned short nMesh = 1;

From fc06604935ca848b13c81d2c5a18fcad1d9cd518 Mon Sep 17 00:00:00 2001
From: Kursat Yurt <kursatyurt@gmail.com>
Date: Fri, 31 Mar 2023 12:50:37 +0200
Subject: [PATCH 333/656] Apply checks

---
 Common/include/CConfig.hpp                    | 324 +++++++-------
 Common/include/containers/CLookUpTable.hpp    |   2 +-
 Common/include/geometry/CGeometry.hpp         |  16 +-
 Common/include/geometry/CPhysicalGeometry.hpp |   7 +-
 .../meshreader/CCGNSMeshReaderFVM.hpp         |   2 +-
 .../include/grid_movement/CFreeFormDefBox.hpp |  24 +-
 .../grid_movement/CSurfaceMovement.hpp        |   2 +-
 Common/include/linear_algebra/CSysSolve.hpp   |   4 +-
 .../include/parallelization/mpi_structure.cpp |   2 +-
 .../include/parallelization/mpi_structure.hpp |   2 +-
 Common/include/toolboxes/C1DInterpolation.hpp |   2 +-
 Common/src/CConfig.cpp                        | 413 +++++++++---------
 Common/src/adt/CADTElemClass.cpp              |   6 +-
 Common/src/adt/CADTPointsOnlyClass.cpp        |   2 +-
 Common/src/containers/CFileReaderLUT.cpp      |   4 +-
 Common/src/containers/CLookUpTable.cpp        |   8 +-
 Common/src/containers/CTrapezoidalMap.cpp     |   2 +-
 Common/src/fem/fem_cgns_elements.cpp          |  10 +-
 .../src/fem/fem_gauss_jacobi_quadrature.cpp   |  11 +-
 Common/src/fem/fem_geometry_structure.cpp     | 102 ++---
 Common/src/fem/fem_integration_rules.cpp      |  14 +-
 Common/src/fem/fem_standard_element.cpp       |  32 +-
 .../src/fem/geometry_structure_fem_part.cpp   |  80 ++--
 Common/src/geometry/CGeometry.cpp             |  72 ++-
 Common/src/geometry/CMultiGridGeometry.cpp    |  30 +-
 Common/src/geometry/CMultiGridQueue.cpp       |   8 +-
 Common/src/geometry/CPhysicalGeometry.cpp     | 225 +++++-----
 Common/src/geometry/dual_grid/CDualGrid.cpp   |   2 +-
 Common/src/geometry/dual_grid/CEdge.cpp       |   2 +-
 Common/src/geometry/elements/CElement.cpp     |   2 +-
 .../geometry/meshreader/CBoxMeshReaderFVM.cpp |   2 +-
 .../meshreader/CCGNSMeshReaderFVM.cpp         |  29 +-
 .../meshreader/CSU2ASCIIMeshReaderFVM.cpp     |  24 +-
 .../primal_grid/CPrimalGridBoundFEM.cpp       |   2 +-
 Common/src/geometry/primal_grid/CPrism.cpp    |   2 +-
 Common/src/grid_movement/CBSplineBlending.cpp |   2 +-
 Common/src/grid_movement/CBezierBlending.cpp  |   2 +-
 .../src/grid_movement/CFreeFormBlending.cpp   |   4 +-
 Common/src/grid_movement/CFreeFormDefBox.cpp  |  59 ++-
 Common/src/grid_movement/CGridMovement.cpp    |   4 +-
 Common/src/grid_movement/CSurfaceMovement.cpp | 118 +++--
 .../src/grid_movement/CVolumetricMovement.cpp |   6 +-
 .../CIsoparametric.cpp                        |   2 +-
 .../interface_interpolation/CSlidingMesh.cpp  |   6 +-
 Common/src/linear_algebra/CSysMatrix.cpp      |   2 +-
 Common/src/linear_algebra/CSysSolve.cpp       |   4 +-
 Common/src/linear_algebra/blas_structure.cpp  |   2 +-
 Common/src/toolboxes/C1DInterpolation.cpp     |   4 +-
 Common/src/toolboxes/MMS/CIncTGVSolution.cpp  |   4 +-
 .../toolboxes/MMS/CInviscidVortexSolution.cpp |   4 +-
 .../toolboxes/MMS/CMMSIncEulerSolution.cpp    |   6 +-
 .../src/toolboxes/MMS/CMMSIncNSSolution.cpp   |   6 +-
 .../MMS/CMMSNSTwoHalfCirclesSolution.cpp      |   6 +-
 .../MMS/CMMSNSTwoHalfSpheresSolution.cpp      |   6 +-
 .../toolboxes/MMS/CMMSNSUnitQuadSolution.cpp  |   6 +-
 .../MMS/CMMSNSUnitQuadSolutionWallBC.cpp      |   6 +-
 .../src/toolboxes/MMS/CNSUnitQuadSolution.cpp |   4 +-
 Common/src/toolboxes/MMS/CRinglebSolution.cpp |   4 +-
 Common/src/toolboxes/MMS/CTGVSolution.cpp     |   6 +-
 .../toolboxes/MMS/CUserDefinedSolution.cpp    |   6 +-
 .../toolboxes/MMS/CVerificationSolution.cpp   |   8 +-
 Common/src/toolboxes/printing_toolbox.cpp     |   1 -
 Common/src/wall_model.cpp                     |   6 +-
 SU2_CFD/include/fluid/CCoolProp.hpp           |   2 +-
 SU2_CFD/include/numerics/CNumerics.hpp        |   2 +-
 SU2_CFD/include/output/COutput.hpp            |   6 +-
 SU2_CFD/include/output/COutputLegacy.hpp      |   2 +-
 .../output/filewriter/CCGNSFileWriter.hpp     |   2 +-
 .../filewriter/CParaviewVTMFileWriter.hpp     |   4 +-
 SU2_CFD/include/solvers/CSolver.hpp           |   6 +-
 SU2_CFD/src/CMarkerProfileReaderFVM.cpp       |  28 +-
 SU2_CFD/src/definition_structure.cpp          |  10 +-
 .../src/drivers/CDiscAdjSinglezoneDriver.cpp  |   2 +-
 SU2_CFD/src/drivers/CDriver.cpp               |  54 +--
 SU2_CFD/src/drivers/CDriverBase.cpp           |   4 +-
 SU2_CFD/src/drivers/CMultizoneDriver.cpp      |   2 +-
 SU2_CFD/src/drivers/CSinglezoneDriver.cpp     |   6 +-
 SU2_CFD/src/fluid/CCoolProp.cpp               |   4 +-
 SU2_CFD/src/fluid/CFluidScalar.cpp            |   3 +-
 SU2_CFD/src/fluid/CNEMOGas.cpp                |   2 +-
 SU2_CFD/src/fluid/CSU2TCLib.cpp               |   8 +-
 .../src/integration/CIntegrationFactory.cpp   |   2 +-
 .../src/integration/CMultiGridIntegration.cpp |   6 +-
 SU2_CFD/src/interfaces/CInterface.cpp         |  10 +-
 .../src/iteration/CDiscAdjFEAIteration.cpp    |   2 +-
 SU2_CFD/src/iteration/CFluidIteration.cpp     |   2 +-
 SU2_CFD/src/numerics/CNumerics.cpp            |   6 +-
 SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp   |   2 +-
 SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp  |   4 +-
 SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp    |   2 +-
 .../numerics/NEMO/convection/ausm_slau.cpp    |   2 +-
 SU2_CFD/src/numerics/NEMO/convection/lax.cpp  |   2 +-
 SU2_CFD/src/numerics/NEMO/convection/msw.cpp  |   2 +-
 SU2_CFD/src/numerics/NEMO/convection/roe.cpp  |   2 +-
 .../continuous_adjoint/adj_convection.cpp     |  10 +-
 .../continuous_adjoint/adj_diffusion.cpp      |   8 +-
 .../continuous_adjoint/adj_sources.cpp        |  13 +-
 .../numerics/elasticity/CFEAElasticity.cpp    |   2 +-
 .../elasticity/CFEANonlinearElasticity.cpp    |  10 +-
 .../numerics/flow/convection/ausm_slau.cpp    |   4 +-
 .../src/numerics/flow/convection/centered.cpp |   4 +-
 SU2_CFD/src/numerics/flow/convection/fds.cpp  |   2 +-
 SU2_CFD/src/numerics/flow/convection/fvs.cpp  |   2 +-
 SU2_CFD/src/numerics/flow/convection/hllc.cpp |   4 +-
 SU2_CFD/src/numerics/flow/convection/roe.cpp  |   6 +-
 SU2_CFD/src/numerics/template.cpp             |  12 +-
 SU2_CFD/src/output/CAdjElasticityOutput.cpp   |   2 +-
 SU2_CFD/src/output/CAdjFlowCompOutput.cpp     |   2 +-
 SU2_CFD/src/output/CAdjFlowIncOutput.cpp      |   2 +-
 SU2_CFD/src/output/CAdjHeatOutput.cpp         |   2 +-
 SU2_CFD/src/output/CBaselineOutput.cpp        |   2 +-
 SU2_CFD/src/output/CFlowCompFEMOutput.cpp     |   4 +-
 SU2_CFD/src/output/CFlowOutput.cpp            |  11 +-
 SU2_CFD/src/output/CMeshOutput.cpp            |   2 +-
 SU2_CFD/src/output/COutput.cpp                |  37 +-
 SU2_CFD/src/output/COutputFactory.cpp         |   2 +-
 .../src/output/filewriter/CCGNSFileWriter.cpp |   4 +-
 .../src/output/filewriter/CCSVFileWriter.cpp  |  10 +-
 .../src/output/filewriter/CFEMDataSorter.cpp  |   4 +-
 .../src/output/filewriter/CFVMDataSorter.cpp  |   4 +-
 .../output/filewriter/CParallelDataSorter.cpp |   2 +-
 .../output/filewriter/CParallelFileWriter.cpp |  10 +-
 .../filewriter/CParaviewBinaryFileWriter.cpp  |  13 +-
 .../output/filewriter/CParaviewFileWriter.cpp |   2 +-
 .../filewriter/CParaviewVTMFileWriter.cpp     |  16 +-
 .../filewriter/CParaviewXMLFileWriter.cpp     |  13 +-
 .../src/output/filewriter/CSTLFileWriter.cpp  |  14 +-
 .../filewriter/CSU2BinaryFileWriter.cpp       |   4 +-
 .../output/filewriter/CSU2MeshFileWriter.cpp  |   6 +-
 .../filewriter/CSurfaceFEMDataSorter.cpp      |   4 +-
 .../filewriter/CSurfaceFVMDataSorter.cpp      |  16 +-
 .../filewriter/CTecplotBinaryFileWriter.cpp   |  48 +-
 .../output/filewriter/CTecplotFileWriter.cpp  |   2 +-
 .../src/output/output_structure_legacy.cpp    | 164 +++----
 SU2_CFD/src/output/tools/CWindowingTools.cpp  |  12 +-
 SU2_CFD/src/solvers/CAdjEulerSolver.cpp       |  13 +-
 SU2_CFD/src/solvers/CAdjNSSolver.cpp          |  56 ++-
 SU2_CFD/src/solvers/CAdjTurbSolver.cpp        |   4 +-
 SU2_CFD/src/solvers/CBaselineSolver.cpp       |  16 +-
 SU2_CFD/src/solvers/CBaselineSolver_FEM.cpp   |   6 +-
 SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp     |   2 +-
 SU2_CFD/src/solvers/CDiscAdjSolver.cpp        |   2 +-
 SU2_CFD/src/solvers/CEulerSolver.cpp          | 197 +++++----
 SU2_CFD/src/solvers/CFEASolver.cpp            |   8 +-
 SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp   | 170 +++----
 SU2_CFD/src/solvers/CFEM_DG_NSSolver.cpp      |   8 +-
 .../src/solvers/CGradientSmoothingSolver.cpp  |   4 +-
 SU2_CFD/src/solvers/CIncEulerSolver.cpp       |  22 +-
 SU2_CFD/src/solvers/CMeshSolver.cpp           |   2 +-
 SU2_CFD/src/solvers/CNEMOEulerSolver.cpp      |  20 +-
 SU2_CFD/src/solvers/CRadP1Solver.cpp          |   4 +-
 SU2_CFD/src/solvers/CRadSolver.cpp            |   2 +-
 SU2_CFD/src/solvers/CSolver.cpp               |  44 +-
 SU2_CFD/src/solvers/CSpeciesSolver.cpp        |   2 +-
 SU2_CFD/src/solvers/CTemplateSolver.cpp       |   4 +-
 SU2_CFD/src/variables/CMeshElement.cpp        |   2 +-
 SU2_CFD/src/variables/CNEMOEulerVariable.cpp  |   2 +-
 SU2_CFD/src/variables/CNEMONSVariable.cpp     |   2 +-
 SU2_DEF/src/drivers/CDeformationDriver.cpp    |   2 +-
 .../src/drivers/CDiscAdjDeformationDriver.cpp |  23 +-
 SU2_GEO/src/SU2_GEO.cpp                       |   4 +-
 SU2_SOL/src/SU2_SOL.cpp                       |  20 +-
 162 files changed, 1505 insertions(+), 1583 deletions(-)

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index ba5190f4b24..fcd79d3f9ef 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -1254,19 +1254,19 @@ class CConfig {
   /*!< \brief addDoubleOption creates a config file parser for an option with the given name whose
    value can be represented by a su2double.*/
 
-  void addDoubleOption(const string name, su2double & option_field, su2double default_value);
+  void addDoubleOption(const string& name, su2double & option_field, su2double default_value);
 
-  void addStringOption(const string name, string & option_field, string default_value);
+  void addStringOption(const string& name, string & option_field, string default_value);
 
-  void addIntegerOption(const string name, int & option_field, int default_value);
+  void addIntegerOption(const string& name, int & option_field, int default_value);
 
-  void addUnsignedLongOption(const string name, unsigned long & option_field, unsigned long default_value);
+  void addUnsignedLongOption(const string& name, unsigned long & option_field, unsigned long default_value);
 
-  void addUnsignedShortOption(const string name, unsigned short & option_field, unsigned short default_value);
+  void addUnsignedShortOption(const string& name, unsigned short & option_field, unsigned short default_value);
 
-  void addLongOption(const string name, long & option_field, long default_value);
+  void addLongOption(const string& name, long & option_field, long default_value);
 
-  void addBoolOption(const string name, bool & option_field, bool default_value);
+  void addBoolOption(const string& name, bool & option_field, bool default_value);
 
   // enum types work differently than all of the others because there are a small number of valid
   // string entries for the type. One must also provide a list of all the valid strings of that type.
@@ -1277,48 +1277,48 @@ class CConfig {
   template <class Tenum, class Tfield>
   void addEnumListOption(const string name, unsigned short& input_size, Tfield*& option_field, const map<string,Tenum>& enum_map);
 
-  void addDoubleArrayOption(const string name, const int size, su2double* option_field);
+  void addDoubleArrayOption(const string& name, const int size, su2double* option_field);
 
-  void addUShortArrayOption(const string name, const int size, unsigned short* option_field);
+  void addUShortArrayOption(const string& name, const int size, unsigned short* option_field);
 
-  void addDoubleListOption(const string name, unsigned short & size, su2double * & option_field);
+  void addDoubleListOption(const string& name, unsigned short & size, su2double * & option_field);
 
-  void addShortListOption(const string name, unsigned short & size, short * & option_field);
+  void addShortListOption(const string& name, unsigned short & size, short * & option_field);
 
-  void addUShortListOption(const string name, unsigned short & size, unsigned short * & option_field);
+  void addUShortListOption(const string& name, unsigned short & size, unsigned short * & option_field);
 
-  void addULongListOption(const string name, unsigned short & size, unsigned long * & option_field);
+  void addULongListOption(const string& name, unsigned short & size, unsigned long * & option_field);
 
-  void addStringListOption(const string name, unsigned short & num_marker, string* & option_field);
+  void addStringListOption(const string& name, unsigned short & num_marker, string* & option_field);
 
-  void addConvectOption(const string name, unsigned short & space_field, CENTERED & centered_field, UPWIND & upwind_field);
+  void addConvectOption(const string& name, unsigned short & space_field, CENTERED & centered_field, UPWIND & upwind_field);
 
-  void addConvectFEMOption(const string name, unsigned short & space_field, unsigned short & fem_field);
+  void addConvectFEMOption(const string& name, unsigned short & space_field, unsigned short & fem_field);
 
-  void addMathProblemOption(const string name, bool & ContinuousAdjoint, const bool & ContinuousAdjoint_default,
+  void addMathProblemOption(const string& name, bool & ContinuousAdjoint, const bool & ContinuousAdjoint_default,
                             bool & DiscreteAdjoint, const bool & DiscreteAdjoint_default,
                             bool & Restart_Flow, const bool & Restart_Flow_default);
 
-  void addDVParamOption(const string name, unsigned short & nDV_field, su2double** & paramDV, string* & FFDTag,
+  void addDVParamOption(const string& name, unsigned short & nDV_field, su2double** & paramDV, string* & FFDTag,
                         unsigned short* & design_variable);
 
-  void addDVValueOption(const string name, unsigned short* & nDVValue_field, su2double** & valueDV, unsigned short & nDV_field,  su2double** & paramDV,
+  void addDVValueOption(const string& name, unsigned short* & nDVValue_field, su2double** & valueDV, unsigned short & nDV_field,  su2double** & paramDV,
                         unsigned short* & design_variable);
 
-  void addFFDDefOption(const string name, unsigned short & nFFD_field, su2double** & coordFFD, string* & FFDTag);
+  void addFFDDefOption(const string& name, unsigned short & nFFD_field, su2double** & coordFFD, string* & FFDTag);
 
-  void addFFDDegreeOption(const string name, unsigned short & nFFD_field, unsigned short** & degreeFFD);
+  void addFFDDegreeOption(const string& name, unsigned short & nFFD_field, unsigned short** & degreeFFD);
 
-  void addStringDoubleListOption(const string name, unsigned short & list_size, string * & string_field,
+  void addStringDoubleListOption(const string& name, unsigned short & list_size, string * & string_field,
                                  su2double* & double_field);
 
-  void addInletOption(const string name, unsigned short & nMarker_Inlet, string * & Marker_Inlet,
+  void addInletOption(const string& name, unsigned short & nMarker_Inlet, string * & Marker_Inlet,
                       su2double* & Ttotal, su2double* & Ptotal, su2double** & FlowDir);
 
-  void addInletSpeciesOption(const string name, unsigned short & nMarker_Inlet_Species, string * & Marker_Inlet_Species,
+  void addInletSpeciesOption(const string& name, unsigned short & nMarker_Inlet_Species, string * & Marker_Inlet_Species,
                              su2double** & inlet_species_val, unsigned short & nSpecies_per_Inlet);
 
-  void addInletTurbOption(const string name, unsigned short& nMarker_Inlet_Turb, string*& Marker_Inlet_Turb,
+  void addInletTurbOption(const string& name, unsigned short& nMarker_Inlet_Turb, string*& Marker_Inlet_Turb,
                           su2double** & Turb_Properties, unsigned short & nTurb_Properties);
 
   template <class Tenum>
@@ -1329,7 +1329,7 @@ class CConfig {
   void addGilesOption(const string name, unsigned short & nMarker_Giles, string * & Marker_Giles, unsigned short* & option_field, const map<string, Tenum> & enum_map,
                      su2double* & var1, su2double* & var2, su2double** & FlowDir, su2double* & relaxfactor1, su2double* & relaxfactor2);
 
-  void addExhaustOption(const string name, unsigned short & nMarker_Exhaust, string * & Marker_Exhaust,
+  void addExhaustOption(const string& name, unsigned short & nMarker_Exhaust, string * & Marker_Exhaust,
                         su2double* & Ttotal, su2double* & Ptotal);
 
   void addPeriodicOption(const string & name, unsigned short & nMarker_PerBound,
@@ -1347,7 +1347,7 @@ class CConfig {
                              string* &string_field,            WALL_FUNCTIONS* &val_Kind_WF,
                              unsigned short** &val_IntInfo_WF, su2double** &val_DoubleInfo_WF);
 
-  void addPythonOption(const string name);
+  void addPythonOption(const string& name);
 
 public:
 
@@ -1425,7 +1425,7 @@ class CConfig {
    * \param[in] val_format - Format of the file with the grid information.
    * \return Total number of zones in the grid file.
    */
-  static unsigned short GetnZone(string val_mesh_filename, unsigned short val_format);
+  static unsigned short GetnZone(const string& val_mesh_filename, unsigned short val_format);
 
   /*!
    * \brief Gets the number of dimensions in the mesh file
@@ -1433,7 +1433,7 @@ class CConfig {
    * \param[in] val_format - Format of the file with the grid information.
    * \return Total number of domains in the grid file.
    */
-  static unsigned short GetnDim(string val_mesh_filename, unsigned short val_format);
+  static unsigned short GetnDim(const string& val_mesh_filename, unsigned short val_format);
 
   /*!
    * \brief Initializes pointers to null
@@ -4912,7 +4912,7 @@ class CConfig {
    * \brief Get the type of incompressible inlet from the list.
    * \return Kind of the incompressible inlet.
    */
-  INLET_TYPE GetKind_Inc_Inlet(string val_marker) const;
+  INLET_TYPE GetKind_Inc_Inlet(const string& val_marker) const;
 
   /*!
    * \brief Get the total number of types in Kind_Inc_Inlet list
@@ -4930,7 +4930,7 @@ class CConfig {
    * \brief Get the type of incompressible outlet from the list.
    * \return Kind of the incompressible outlet.
    */
-  INC_OUTLET_TYPE GetKind_Inc_Outlet(string val_marker) const;
+  INC_OUTLET_TYPE GetKind_Inc_Outlet(const string& val_marker) const;
 
   /*!
    * \brief Get the damping factor applied to velocity updates at incompressible pressure inlets.
@@ -5485,7 +5485,7 @@ class CConfig {
    * \param[in] Iter - the current iteration
    * \return The new filename
    */
-  string GetFilename(string filename, string ext, int Iter) const;
+  string GetFilename(string filename, const string& ext, int Iter) const;
 
   /*!
    * \brief Add steady iteration number to the filename (does not overwrite previous files)
@@ -5500,7 +5500,7 @@ class CConfig {
    * \brief Append the zone index to the restart or the solution files.
    * \return Name of the restart file for the flow variables.
    */
-  string GetMultizone_FileName(string val_filename, int val_iZone, string ext) const;
+  string GetMultizone_FileName(string val_filename, int val_iZone, const string& ext) const;
 
   /*!
    * \brief Append the zone index to the restart or the solution files.
@@ -5509,7 +5509,7 @@ class CConfig {
    * \param[in] ext - the filename extension.
    * \return Name of the restart file for the flow variables.
    */
-  string GetMultizone_HistoryFileName(string val_filename, int val_iZone, string ext) const;
+  string GetMultizone_HistoryFileName(string val_filename, int val_iZone, const string& ext) const;
 
   /*!
    * \brief Append the instance index to the restart or the solution files.
@@ -5518,7 +5518,7 @@ class CConfig {
    * \param[in] ext - the filename extension.
    * \return Name of the restart file for the flow variables.
    */
-  string GetMultiInstance_FileName(string val_filename, int val_iInst, string ext) const;
+  string GetMultiInstance_FileName(string val_filename, int val_iInst, const string& ext) const;
 
   /*!
    * \brief Append the instance index to the restart or the solution files.
@@ -5589,7 +5589,7 @@ class CConfig {
    * \param[in] ext - the filename extension.
    * \return Name of the file with the iteration number for an unsteady solution file.
    */
-  string GetUnsteady_FileName(string val_filename, int val_iter, string ext) const;
+  string GetUnsteady_FileName(string val_filename, int val_iter, const string& ext) const;
 
   /*!
    * \brief Append the input filename string with the appropriate objective function extension.
@@ -6147,7 +6147,7 @@ class CConfig {
    * \note When we read the config file, it stores the markers in a particular vector.
    * \return Index in the config information of the marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_CfgFile_TagBound(string val_marker) const;
+  unsigned short GetMarker_CfgFile_TagBound(const string& val_marker) const;
 
   /*!
    * \brief Get the name in the config information of the marker number <i>val_marker</i>.
@@ -6160,115 +6160,115 @@ class CConfig {
    * \brief Get the boundary information (kind of boundary) in the config information of the marker <i>val_marker</i>.
    * \return Kind of boundary in the config information of the marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_CfgFile_KindBC(string val_marker) const;
+  unsigned short GetMarker_CfgFile_KindBC(const string& val_marker) const;
 
   /*!
    * \brief Get the monitoring information from the config definition for the marker <i>val_marker</i>.
    * \return Monitoring information of the boundary in the config information for the marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_CfgFile_Monitoring(string val_marker) const;
+  unsigned short GetMarker_CfgFile_Monitoring(const string& val_marker) const;
 
   /*!
    * \brief Get the monitoring information from the config definition for the marker <i>val_marker</i>.
    * \return Monitoring information of the boundary in the config information for the marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_CfgFile_GeoEval(string val_marker) const;
+  unsigned short GetMarker_CfgFile_GeoEval(const string& val_marker) const;
 
   /*!
    * \brief Get the monitoring information from the config definition for the marker <i>val_marker</i>.
    * \return Monitoring information of the boundary in the config information for the marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_CfgFile_Designing(string val_marker) const;
+  unsigned short GetMarker_CfgFile_Designing(const string& val_marker) const;
 
   /*!
    * \brief Get the plotting information from the config definition for the marker <i>val_marker</i>.
    * \return Plotting information of the boundary in the config information for the marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_CfgFile_Plotting(string val_marker) const;
+  unsigned short GetMarker_CfgFile_Plotting(const string& val_marker) const;
 
   /*!
    * \brief Get the plotting information from the config definition for the marker <i>val_marker</i>.
    * \return Plotting information of the boundary in the config information for the marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_CfgFile_Analyze(string val_marker) const;
+  unsigned short GetMarker_CfgFile_Analyze(const string& val_marker) const;
 
   /*!
    * \brief Get the multi-physics interface information from the config definition for the marker <i>val_marker</i>.
    * \return Plotting information of the boundary in the config information for the marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_CfgFile_ZoneInterface(string val_marker) const;
+  unsigned short GetMarker_CfgFile_ZoneInterface(const string& val_marker) const;
 
   /*!
    * \brief Get the TurboPerformance information from the config definition for the marker <i>val_marker</i>.
    * \return TurboPerformance information of the boundary in the config information for the marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_CfgFile_Turbomachinery(string val_marker) const;
+  unsigned short GetMarker_CfgFile_Turbomachinery(const string& val_marker) const;
 
   /*!
    * \brief Get the TurboPerformance flag information from the config definition for the marker <i>val_marker</i>.
    * \return TurboPerformance flag information of the boundary in the config information for the marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_CfgFile_TurbomachineryFlag(string val_marker) const;
+  unsigned short GetMarker_CfgFile_TurbomachineryFlag(const string& val_marker) const;
 
   /*!
    * \brief Get the MixingPlane interface information from the config definition for the marker <i>val_marker</i>.
    * \return Plotting information of the boundary in the config information for the marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_CfgFile_MixingPlaneInterface(string val_marker) const;
+  unsigned short GetMarker_CfgFile_MixingPlaneInterface(const string& val_marker) const;
 
   /*!
    * \brief Get the DV information from the config definition for the marker <i>val_marker</i>.
    * \return DV information of the boundary in the config information for the marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_CfgFile_DV(string val_marker) const;
+  unsigned short GetMarker_CfgFile_DV(const string& val_marker) const;
 
   /*!
    * \brief Get the motion information from the config definition for the marker <i>val_marker</i>.
    * \return Motion information of the boundary in the config information for the marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_CfgFile_Moving(string val_marker) const;
+  unsigned short GetMarker_CfgFile_Moving(const string& val_marker) const;
 
   /*!
    * \brief Get the gradient boundary information from the config definition for the marker <i>val_marker</i>.
    * \return Gradient boundary information of the boundary in the config information for the marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_CfgFile_SobolevBC(string val_marker) const;
+  unsigned short GetMarker_CfgFile_SobolevBC(const string& val_marker) const;
 
   /*!
    * \brief Get the DEFORM_MESH information from the config definition for the marker <i>val_marker</i>.
    * \return DEFORM_MESH information of the boundary in the config information for the marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_CfgFile_Deform_Mesh(string val_marker) const;
+  unsigned short GetMarker_CfgFile_Deform_Mesh(const string& val_marker) const;
 
   /*!
    * \brief Get the DEFORM_MESH_SYM_PLANE information from the config definition for the marker <i>val_marker</i>.
    * \return DEFORM_MESH_SYM_PLANE information of the boundary in the config information for the marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_CfgFile_Deform_Mesh_Sym_Plane(string val_marker) const;
+  unsigned short GetMarker_CfgFile_Deform_Mesh_Sym_Plane(const string& val_marker) const;
 
   /*!
    * \brief Get the Fluid_Load information from the config definition for the marker <i>val_marker</i>.
    * \return Fluid_Load information of the boundary in the config information for the marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_CfgFile_Fluid_Load(string val_marker) const;
+  unsigned short GetMarker_CfgFile_Fluid_Load(const string& val_marker) const;
 
   /*!
    * \brief Get the Python customization information from the config definition for the marker <i>val_marker</i>.
    * \return Python customization information of the boundary in the config information for the marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_CfgFile_PyCustom(string val_marker) const;
+  unsigned short GetMarker_CfgFile_PyCustom(const string& val_marker) const;
 
   /*!
    * \brief Get the periodic information from the config definition of the marker <i>val_marker</i>.
    * \return Periodic information of the boundary in the config information of the marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_CfgFile_PerBound(string val_marker) const;
+  unsigned short GetMarker_CfgFile_PerBound(const string& val_marker) const;
 
   /*!
    * \brief  Get the name of the marker <i>val_marker</i>.
    * \return The interface which owns that marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_ZoneInterface(string val_marker) const;
+  unsigned short GetMarker_ZoneInterface(const string& val_marker) const;
 
   /*!
    * \brief  Get the name of the marker <i>val_iMarker</i>.
@@ -6458,17 +6458,17 @@ class CConfig {
   /*!
    * \brief Center of rotation for a rotational periodic boundary.
    */
-  const su2double *GetPeriodicRotCenter(string val_marker) const;
+  const su2double *GetPeriodicRotCenter(const string& val_marker) const;
 
   /*!
    * \brief Angles of rotation for a rotational periodic boundary.
    */
-  const su2double *GetPeriodicRotAngles(string val_marker) const;
+  const su2double *GetPeriodicRotAngles(const string& val_marker) const;
 
   /*!
    * \brief Translation vector for a translational periodic boundary.
    */
-  const su2double *GetPeriodicTranslation(string val_marker) const;
+  const su2double *GetPeriodicTranslation(const string& val_marker) const;
 
   /*!
    * \brief Get the translation vector for a periodic transformation.
@@ -6481,79 +6481,79 @@ class CConfig {
    * \brief Get the rotationally periodic donor marker for boundary <i>val_marker</i>.
    * \return Periodic donor marker from the config information for the marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_Periodic_Donor(string val_marker) const;
+  unsigned short GetMarker_Periodic_Donor(const string& val_marker) const;
 
   /*!
    * \brief Get the origin of the actuator disk.
    */
-  su2double GetActDisk_NetThrust(string val_marker) const;
+  su2double GetActDisk_NetThrust(const string& val_marker) const;
 
   /*!
    * \brief Get the origin of the actuator disk.
    */
-  su2double GetActDisk_Power(string val_marker) const;
+  su2double GetActDisk_Power(const string& val_marker) const;
 
   /*!
    * \brief Get the origin of the actuator disk.
    */
-  su2double GetActDisk_MassFlow(string val_marker) const;
+  su2double GetActDisk_MassFlow(const string& val_marker) const;
 
   /*!
    * \brief Get the origin of the actuator disk.
    */
-  su2double GetActDisk_Mach(string val_marker) const;
+  su2double GetActDisk_Mach(const string& val_marker) const;
 
   /*!
    * \brief Get the origin of the actuator disk.
    */
-  su2double GetActDisk_Force(string val_marker) const;
+  su2double GetActDisk_Force(const string& val_marker) const;
 
   /*!
    * \brief Get the origin of the actuator disk.
    */
-  su2double GetActDisk_BCThrust(string val_marker) const;
+  su2double GetActDisk_BCThrust(const string& val_marker) const;
 
   /*!
    * \brief Get the origin of the actuator disk.
    */
-  su2double GetActDisk_BCThrust_Old(string val_marker) const;
+  su2double GetActDisk_BCThrust_Old(const string& val_marker) const;
 
   /*!
    * \brief Get the tip radius of th actuator disk.
    */
-  su2double GetActDisk_Area(string val_marker) const;
+  su2double GetActDisk_Area(const string& val_marker) const;
 
   /*!
    * \brief Get the tip radius of th actuator disk.
    */
-  su2double GetActDisk_ReverseMassFlow(string val_marker) const;
+  su2double GetActDisk_ReverseMassFlow(const string& val_marker) const;
 
   /*!
    * \brief Get the thrust corffient of the actuator disk.
    */
-  su2double GetActDisk_PressJump(string val_marker, unsigned short val_index) const;
+  su2double GetActDisk_PressJump(const string& val_marker, unsigned short val_index) const;
 
   /*!
    * \brief Get the thrust corffient of the actuator disk.
    */
-  su2double GetActDisk_TempJump(string val_marker, unsigned short val_index) const;
+  su2double GetActDisk_TempJump(const string& val_marker, unsigned short val_index) const;
 
   /*!
    * \brief Get the rev / min of the actuator disk.
    */
-  su2double GetActDisk_Omega(string val_marker, unsigned short val_index) const;
+  su2double GetActDisk_Omega(const string& val_marker, unsigned short val_index) const;
 
   /*!
    * \brief Get Actuator Disk Outlet for boundary <i>val_marker</i> (actuator disk inlet).
    * \return Actuator Disk Outlet from the config information for the marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_CfgFile_ActDiskOutlet(string val_marker) const;
+  unsigned short GetMarker_CfgFile_ActDiskOutlet(const string& val_marker) const;
 
   /*!
    * \brief Get Actuator Disk Outlet for boundary <i>val_marker</i> (actuator disk inlet).
    * \return Actuator Disk Outlet from the config information for the marker <i>val_marker</i>.
    */
-  unsigned short GetMarker_CfgFile_EngineExhaust(string val_marker) const;
+  unsigned short GetMarker_CfgFile_EngineExhaust(const string& val_marker) const;
 
   /*!
    * \brief Get the internal index for a moving boundary <i>val_marker</i>.
@@ -6596,13 +6596,13 @@ class CConfig {
    * \brief Get the internal index for a Fluid_Load boundary <i>val_marker</i>.
    * \return Internal index for a Fluid_Load boundary <i>val_marker</i>.
    */
-  unsigned short GetMarker_Fluid_Load(string val_marker) const;
+  unsigned short GetMarker_Fluid_Load(const string& val_marker) const;
 
   /*!
    * \brief Get the internal index for a gradient boundary condition <i>val_marker</i>.
    * \return Internal index for a gradient boundary  condition <i>val_marker</i>.
    */
-  unsigned short GetMarker_SobolevBC(string val_marker) const;
+  unsigned short GetMarker_SobolevBC(const string& val_marker) const;
 
   /*!
    * \brief Get the name of the surface defined in the geometry file.
@@ -6657,35 +6657,35 @@ class CConfig {
    * \param[in] val_index - Index corresponding to the inlet boundary.
    * \return The total temperature.
    */
-  su2double GetExhaust_Temperature_Target(string val_index) const;
+  su2double GetExhaust_Temperature_Target(const string& val_index) const;
 
   /*!
    * \brief Get the total temperature at an inlet boundary.
    * \param[in] val_index - Index corresponding to the inlet boundary.
    * \return The total temperature.
    */
-  su2double GetInlet_Ttotal(string val_index) const;
+  su2double GetInlet_Ttotal(const string& val_index) const;
 
   /*!
    * \brief Get the temperature at a supersonic inlet boundary.
    * \param[in] val_index - Index corresponding to the inlet boundary.
    * \return The inlet density.
    */
-  su2double GetInlet_Temperature(string val_index) const;
+  su2double GetInlet_Temperature(const string& val_index) const;
 
   /*!
    * \brief Get the pressure at a supersonic inlet boundary.
    * \param[in] val_index - Index corresponding to the inlet boundary.
    * \return The inlet pressure.
    */
-  su2double GetInlet_Pressure(string val_index) const;
+  su2double GetInlet_Pressure(const string& val_index) const;
 
   /*!
    * \brief Get the velocity vector at a supersonic inlet boundary.
    * \param[in] val_index - Index corresponding to the inlet boundary.
    * \return The inlet velocity vector.
    */
-  const su2double* GetInlet_Velocity(string val_index) const;
+  const su2double* GetInlet_Velocity(const string& val_index) const;
 
   /*!
    * \brief Get the mass fraction vector for a NEMO inlet boundary.
@@ -6706,35 +6706,35 @@ class CConfig {
    * \param[in] val_index - Index corresponding to the inlet boundary.
    * \return The total pressure.
    */
-  su2double GetInlet_Ptotal(string val_index) const;
+  su2double GetInlet_Ptotal(const string& val_index) const;
 
   /*!
    * \brief Set the total pressure at an inlet boundary.
    * \param[in] val_pressure - Pressure value at the inlet boundary.
    * \param[in] val_index - Index corresponding to the inlet boundary.
    */
-  void SetInlet_Ptotal(su2double val_pressure, string val_marker);
+  void SetInlet_Ptotal(su2double val_pressure, const string& val_marker);
 
   /*!
    * \brief Get the species values at an inlet boundary
    * \param[in] val_index - Index corresponding to the inlet boundary.
    * \return The inlet species values.
    */
-  const su2double* GetInlet_SpeciesVal(string val_index) const;
+  const su2double* GetInlet_SpeciesVal(const string& val_index) const;
 
   /*!
    * \brief Get the turbulent properties values at an inlet boundary
    * \param[in] val_index - Index corresponding to the inlet boundary.
    * \return The inlet turbulent values.
    */
-  const su2double* GetInlet_TurbVal(string val_index) const;
+  const su2double* GetInlet_TurbVal(const string& val_index) const;
 
   /*!
    * \brief Get the total pressure at an nacelle boundary.
    * \param[in] val_index - Index corresponding to the inlet boundary.
    * \return The total pressure.
    */
-  su2double GetExhaust_Pressure_Target(string val_index) const;
+  su2double GetExhaust_Pressure_Target(const string& val_index) const;
 
   /*!
    * \brief Value of the CFL reduction in turbulence problems.
@@ -6753,97 +6753,97 @@ class CConfig {
    * \param[in] val_index - Index corresponding to the inlet boundary.
    * \return The flow direction vector.
    */
-  const su2double* GetInlet_FlowDir(string val_index) const;
+  const su2double* GetInlet_FlowDir(const string& val_index) const;
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
    * \param[in] val_index - Index corresponding to the outlet boundary.
    * \return The outlet pressure.
    */
-  su2double GetOutlet_Pressure(string val_index) const;
+  su2double GetOutlet_Pressure(const string& val_index) const;
 
   /*!
    * \brief Set the back pressure (static) at an outlet boundary.
    * \param[in] val_pressure - Pressure value at the outlet boundary.
    * \param[in] val_index - Index corresponding to the outlet boundary.
    */
-  void SetOutlet_Pressure(su2double val_pressure, string val_marker);
+  void SetOutlet_Pressure(su2double val_pressure, const string& val_marker);
 
   /*!
    * \brief Get the var 1 at Riemann boundary.
    * \param[in] val_marker - Index corresponding to the Riemann boundary.
    * \return The var1
    */
-  su2double GetRiemann_Var1(string val_marker) const;
+  su2double GetRiemann_Var1(const string& val_marker) const;
 
   /*!
    * \brief Get the var 2 at Riemann boundary.
    * \param[in] val_marker - Index corresponding to the Riemann boundary.
    * \return The var2
    */
-  su2double GetRiemann_Var2(string val_marker) const;
+  su2double GetRiemann_Var2(const string& val_marker) const;
 
   /*!
    * \brief Get the Flowdir at Riemann boundary.
    * \param[in] val_marker - Index corresponding to the Riemann boundary.
    * \return The Flowdir
    */
-  const su2double* GetRiemann_FlowDir(string val_marker) const;
+  const su2double* GetRiemann_FlowDir(const string& val_marker) const;
 
   /*!
    * \brief Get Kind Data of Riemann boundary.
    * \param[in] val_marker - Index corresponding to the Riemann boundary.
    * \return Kind data
    */
-  unsigned short GetKind_Data_Riemann(string val_marker) const;
+  unsigned short GetKind_Data_Riemann(const string& val_marker) const;
 
   /*!
    * \brief Get the var 1 for the Giels BC.
    * \param[in] val_marker - Index corresponding to the Giles BC.
    * \return The var1
    */
-  su2double GetGiles_Var1(string val_marker) const;
+  su2double GetGiles_Var1(const string& val_marker) const;
 
   /*!
    * \brief Get the var 2 for the Giles boundary.
    * \param[in] val_marker - Index corresponding to the Giles BC.
    * \return The var2
    */
-  su2double GetGiles_Var2(string val_marker) const;
+  su2double GetGiles_Var2(const string& val_marker) const;
 
   /*!
    * \brief Get the Flowdir for the Giles BC.
    * \param[in] val_marker - Index corresponding to the Giles BC.
    * \return The Flowdir
    */
-  const su2double* GetGiles_FlowDir(string val_marker) const;
+  const su2double* GetGiles_FlowDir(const string& val_marker) const;
 
   /*!
    * \brief Get Kind Data for the Giles BC.
    * \param[in] val_marker - Index corresponding to the Giles BC.
    * \return Kind data
    */
-  unsigned short GetKind_Data_Giles(string val_marker) const;
+  unsigned short GetKind_Data_Giles(const string& val_marker) const;
 
   /*!
    * \brief Set the var 1 for Giles BC.
    * \param[in] val_marker - Index corresponding to the Giles BC.
    */
-  void SetGiles_Var1(su2double newVar1, string val_marker);
+  void SetGiles_Var1(su2double newVar1, const string& val_marker);
 
   /*!
    * \brief Get the relax factor for the average component for the Giles BC.
    * \param[in] val_marker - Index corresponding to the Giles BC.
    * \return The relax factor for the average component
    */
-  su2double GetGiles_RelaxFactorAverage(string val_marker) const;
+  su2double GetGiles_RelaxFactorAverage(const string& val_marker) const;
 
   /*!
    * \brief Get the relax factor for the fourier component for the Giles BC.
    * \param[in] val_marker - Index corresponding to the Giles BC.
    * \return The relax factor for the fourier component
    */
-  su2double GetGiles_RelaxFactorFourier(string val_marker) const;
+  su2double GetGiles_RelaxFactorFourier(const string& val_marker) const;
 
   /*!
    * \brief Get the outlet pressure imposed as BC for internal flow.
@@ -6922,35 +6922,35 @@ class CConfig {
    * \param[in] val_index - Index corresponding to the isothermal boundary.
    * \return The wall temperature.
    */
-  su2double GetIsothermal_Temperature(string val_index) const;
+  su2double GetIsothermal_Temperature(const string& val_index) const;
 
   /*!
    * \brief Get the wall heat flux on a constant heat flux boundary.
    * \param[in] val_index - Index corresponding to the constant heat flux boundary.
    * \return The heat flux.
    */
-  su2double GetWall_HeatFlux(string val_index) const;
+  su2double GetWall_HeatFlux(const string& val_index) const;
 
   /*!
    * \brief Get the heat transfer coefficient on a heat transfer boundary.
    * \param[in] val_index - Index corresponding to the heat transfer boundary.
    * \return The heat transfer coefficient.
    */
-  su2double GetWall_HeatTransfer_Coefficient(string val_index) const;
+  su2double GetWall_HeatTransfer_Coefficient(const string& val_index) const;
 
   /*!
    * \brief Get the temperature at inifinty on a heat transfer boundary.
    * \param[in] val_index - Index corresponding to the heat transfer boundary.
    * \return The temperature at infinity.
    */
-  su2double GetWall_HeatTransfer_Temperature(string val_index) const;
+  su2double GetWall_HeatTransfer_Temperature(const string& val_index) const;
 
   /*!
    * \brief Get the wall function treatment for the given boundary marker.
    * \param[in] val_marker - String of the viscous wall marker.
    * \return The type of wall function treatment.
    */
-  WALL_FUNCTIONS GetWallFunction_Treatment(string val_marker) const;
+  WALL_FUNCTIONS GetWallFunction_Treatment(const string& val_marker) const;
 
   /*!
    * \brief Get the additional integer info for the wall function treatment
@@ -6958,7 +6958,7 @@ class CConfig {
    * \param[in] val_marker - String of the viscous wall marker.
    * \return Pointer to the integer info for the given marker.
    */
-  const unsigned short* GetWallFunction_IntInfo(string val_marker) const;
+  const unsigned short* GetWallFunction_IntInfo(const string& val_marker) const;
 
   /*!
    * \brief Get the additional double info for the wall function treatment
@@ -6966,7 +6966,7 @@ class CConfig {
    * \param[in] val_marker - String of the viscous wall marker.
    * \return Pointer to the double info for the given marker.
    */
-  const su2double* GetWallFunction_DoubleInfo(string val_marker) const;
+  const su2double* GetWallFunction_DoubleInfo(const string& val_marker) const;
 
   /*!
    * \brief Get the type of wall and roughness height on a wall boundary (Heatflux or Isothermal).
@@ -6980,35 +6980,35 @@ class CConfig {
    * \param[in] val_index - Index corresponding to the engine inflow boundary.
    * \return Target (pressure, massflow, etc) .
    */
-  su2double GetEngineInflow_Target(string val_marker) const;
+  su2double GetEngineInflow_Target(const string& val_marker) const;
 
   /*!
    * \brief Get the fan face Mach number at an engine inflow boundary.
    * \param[in] val_marker - Name of the boundary.
    * \return The fan face Mach number.
    */
-  su2double GetInflow_Mach(string val_marker) const;
+  su2double GetInflow_Mach(const string& val_marker) const;
 
   /*!
    * \brief Get the back pressure (static) at an engine inflow boundary.
    * \param[in] val_marker - Name of the boundary.
    * \return The engine inflow pressure.
    */
-  su2double GetInflow_Pressure(string val_marker) const;
+  su2double GetInflow_Pressure(const string& val_marker) const;
 
   /*!
    * \brief Get the mass flow rate at an engine inflow boundary.
    * \param[in] val_marker - Name of the boundary.
    * \return The engine mass flow rate.
    */
-  su2double GetInflow_MassFlow(string val_marker) const;
+  su2double GetInflow_MassFlow(const string& val_marker) const;
 
   /*!
    * \brief Get the percentage of reverse flow at an engine inflow boundary.
    * \param[in] val_marker - Name of the boundary.
    * \return The percentage of reverse flow.
    */
-  su2double GetInflow_ReverseMassFlow(string val_marker) const;
+  su2double GetInflow_ReverseMassFlow(const string& val_marker) const;
 
   /*!
    * \brief Get the percentage of reverse flow at an engine inflow boundary.
@@ -7022,98 +7022,98 @@ class CConfig {
    * \param[in] val_marker - Name of the boundary.
    * \return The total pressure.
    */
-  su2double GetInflow_TotalPressure(string val_marker) const;
+  su2double GetInflow_TotalPressure(const string& val_marker) const;
 
   /*!
    * \brief Get the temperature (static) at an engine inflow boundary.
    * \param[in] val_marker - Name of the boundary.
    * \return The engine inflow temperature.
    */
-  su2double GetInflow_Temperature(string val_marker) const;
+  su2double GetInflow_Temperature(const string& val_marker) const;
 
   /*!
    * \brief Get the total temperature at an engine inflow boundary.
    * \param[in] val_marker - Name of the boundary.
    * \return The engine inflow total temperature.
    */
-  su2double GetInflow_TotalTemperature(string val_marker) const;
+  su2double GetInflow_TotalTemperature(const string& val_marker) const;
 
   /*!
    * \brief Get the ram drag at an engine inflow boundary.
    * \param[in] val_marker - Name of the boundary.
    * \return The engine inflow ram drag.
    */
-  su2double GetInflow_RamDrag(string val_marker) const;
+  su2double GetInflow_RamDrag(const string& val_marker) const;
 
   /*!
    * \brief Get the force balance at an engine inflow boundary.
    * \param[in] val_marker - Name of the boundary.
    * \return The engine inflow force balance.
    */
-  su2double GetInflow_Force(string val_marker) const;
+  su2double GetInflow_Force(const string& val_marker) const;
 
   /*!
    * \brief Get the power at an engine inflow boundary.
    * \param[in] val_marker - Name of the boundary.
    * \return The engine inflow power.
    */
-  su2double GetInflow_Power(string val_marker) const;
+  su2double GetInflow_Power(const string& val_marker) const;
 
   /*!
    * \brief Get the back pressure (static) at an engine exhaust boundary.
    * \param[in] val_marker - Name of the boundary.
    * \return The engine exhaust pressure.
    */
-  su2double GetExhaust_Pressure(string val_marker) const;
+  su2double GetExhaust_Pressure(const string& val_marker) const;
 
   /*!
    * \brief Get the temperature (static) at an engine exhaust boundary.
    * \param[in] val_marker - Name of the boundary.
    * \return The engine exhaust temperature.
    */
-  su2double GetExhaust_Temperature(string val_marker) const;
+  su2double GetExhaust_Temperature(const string& val_marker) const;
 
   /*!
    * \brief Get the massflow at an engine exhaust boundary.
    * \param[in] val_marker - Name of the boundary.
    * \return The engine exhaust massflow.
    */
-  su2double GetExhaust_MassFlow(string val_marker) const;
+  su2double GetExhaust_MassFlow(const string& val_marker) const;
 
   /*!
    * \brief Get the total pressure at an engine exhaust boundary.
    * \param[in] val_marker - Name of the boundary.
    * \return The engine exhaust total pressure.
    */
-  su2double GetExhaust_TotalPressure(string val_marker) const;
+  su2double GetExhaust_TotalPressure(const string& val_marker) const;
 
   /*!
    * \brief Get the total temperature at an engine exhaust boundary.
    * \param[in] val_marker - Name of the boundary.
    * \return The total temperature.
    */
-  su2double GetExhaust_TotalTemperature(string val_marker) const;
+  su2double GetExhaust_TotalTemperature(const string& val_marker) const;
 
   /*!
    * \brief Get the gross thrust at an engine exhaust boundary.
    * \param[in] val_marker - Name of the boundary.
    * \return Gross thrust.
    */
-  su2double GetExhaust_GrossThrust(string val_marker) const;
+  su2double GetExhaust_GrossThrust(const string& val_marker) const;
 
   /*!
    * \brief Get the force balance at an engine exhaust boundary.
    * \param[in] val_marker - Name of the boundary.
    * \return Force balance.
    */
-  su2double GetExhaust_Force(string val_marker) const;
+  su2double GetExhaust_Force(const string& val_marker) const;
 
   /*!
    * \brief Get the power at an engine exhaust boundary.
    * \param[in] val_marker - Name of the boundary.
    * \return Power.
    */
-  su2double GetExhaust_Power(string val_marker) const;
+  su2double GetExhaust_Power(const string& val_marker) const;
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
@@ -7345,14 +7345,14 @@ class CConfig {
    * \param[in] val_index - Index corresponding to the outlet boundary.
    * \return The outlet pressure.
    */
-  su2double GetActDiskInlet_Temperature(string val_marker) const;
+  su2double GetActDiskInlet_Temperature(const string& val_marker) const;
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
    * \param[in] val_index - Index corresponding to the outlet boundary.
    * \return The outlet pressure.
    */
-  su2double GetActDiskInlet_TotalTemperature(string val_marker) const;
+  su2double GetActDiskInlet_TotalTemperature(const string& val_marker) const;
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
@@ -7373,21 +7373,21 @@ class CConfig {
    * \param[in] val_index - Index corresponding to the outlet boundary.
    * \return The outlet pressure.
    */
-  su2double GetActDiskOutlet_Temperature(string val_marker) const;
+  su2double GetActDiskOutlet_Temperature(const string& val_marker) const;
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
    * \param[in] val_index - Index corresponding to the outlet boundary.
    * \return The outlet pressure.
    */
-  su2double GetActDiskOutlet_TotalTemperature(string val_marker) const;
+  su2double GetActDiskOutlet_TotalTemperature(const string& val_marker) const;
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
    * \param[in] val_index - Index corresponding to the outlet boundary.
    * \return The outlet pressure.
    */
-  su2double GetActDiskInlet_MassFlow(string val_marker) const;
+  su2double GetActDiskInlet_MassFlow(const string& val_marker) const;
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
@@ -7401,7 +7401,7 @@ class CConfig {
    * \param[in] val_index - Index corresponding to the outlet boundary.
    * \return The outlet pressure.
    */
-  su2double GetActDiskOutlet_MassFlow(string val_marker) const;
+  su2double GetActDiskOutlet_MassFlow(const string& val_marker) const;
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
@@ -7415,14 +7415,14 @@ class CConfig {
    * \param[in] val_index - Index corresponding to the outlet boundary.
    * \return The outlet pressure.
    */
-  su2double GetActDiskInlet_Pressure(string val_marker) const;
+  su2double GetActDiskInlet_Pressure(const string& val_marker) const;
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
    * \param[in] val_index - Index corresponding to the outlet boundary.
    * \return The outlet pressure.
    */
-  su2double GetActDiskInlet_TotalPressure(string val_marker) const;
+  su2double GetActDiskInlet_TotalPressure(const string& val_marker) const;
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
@@ -7513,21 +7513,21 @@ class CConfig {
    * \param[in] val_index - Index corresponding to the outlet boundary.
    * \return The outlet pressure.
    */
-  su2double GetActDiskInlet_RamDrag(string val_marker) const;
+  su2double GetActDiskInlet_RamDrag(const string& val_marker) const;
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
    * \param[in] val_index - Index corresponding to the outlet boundary.
    * \return The outlet pressure.
    */
-  su2double GetActDiskInlet_Force(string val_marker) const;
+  su2double GetActDiskInlet_Force(const string& val_marker) const;
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
    * \param[in] val_index - Index corresponding to the outlet boundary.
    * \return The outlet pressure.
    */
-  su2double GetActDiskInlet_Power(string val_marker) const;
+  su2double GetActDiskInlet_Power(const string& val_marker) const;
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
@@ -7583,7 +7583,7 @@ class CConfig {
    * \param[in] val_index - Index corresponding to the outlet boundary.
    * \return The outlet pressure.
    */
-  su2double GetOutlet_MassFlow(string val_marker) const;
+  su2double GetOutlet_MassFlow(const string& val_marker) const;
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
@@ -7597,7 +7597,7 @@ class CConfig {
    * \param[in] val_index - Index corresponding to the outlet boundary.
    * \return The outlet pressure.
    */
-  su2double GetOutlet_Density(string val_marker) const;
+  su2double GetOutlet_Density(const string& val_marker) const;
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
@@ -7611,7 +7611,7 @@ class CConfig {
    * \param[in] val_index - Index corresponding to the outlet boundary.
    * \return The outlet pressure.
    */
-  su2double GetOutlet_Area(string val_marker) const;
+  su2double GetOutlet_Area(const string& val_marker) const;
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
@@ -7807,7 +7807,7 @@ class CConfig {
    * \param[in] val_index - Index corresponding to the outlet boundary.
    * \return The outlet pressure.
    */
-  void SetActDisk_BCThrust(string val_marker, su2double val_actdisk_bcthrust);
+  void SetActDisk_BCThrust(const string& val_marker, su2double val_actdisk_bcthrust);
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
@@ -7821,7 +7821,7 @@ class CConfig {
    * \param[in] val_index - Index corresponding to the outlet boundary.
    * \return The outlet pressure.
    */
-  void SetActDisk_BCThrust_Old(string val_marker, su2double val_actdisk_bcthrust_old);
+  void SetActDisk_BCThrust_Old(const string& val_marker, su2double val_actdisk_bcthrust_old);
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
@@ -8045,35 +8045,35 @@ class CConfig {
    * \param[in] val_index - Index corresponding to the outlet boundary.
    * \return The outlet pressure.
    */
-  su2double GetActDiskOutlet_Pressure(string val_marker) const;
+  su2double GetActDiskOutlet_Pressure(const string& val_marker) const;
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
    * \param[in] val_index - Index corresponding to the outlet boundary.
    * \return The outlet pressure.
    */
-  su2double GetActDiskOutlet_TotalPressure(string val_marker) const;
+  su2double GetActDiskOutlet_TotalPressure(const string& val_marker) const;
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
    * \param[in] val_index - Index corresponding to the outlet boundary.
    * \return The outlet pressure.
    */
-  su2double GetActDiskOutlet_GrossThrust(string val_marker) const;
+  su2double GetActDiskOutlet_GrossThrust(const string& val_marker) const;
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
    * \param[in] val_index - Index corresponding to the outlet boundary.
    * \return The outlet pressure.
    */
-  su2double GetActDiskOutlet_Force(string val_marker) const;
+  su2double GetActDiskOutlet_Force(const string& val_marker) const;
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
    * \param[in] val_index - Index corresponding to the outlet boundary.
    * \return The outlet pressure.
    */
-  su2double GetActDiskOutlet_Power(string val_marker) const;
+  su2double GetActDiskOutlet_Power(const string& val_marker) const;
 
   /*!
    * \brief Get the back pressure (static) at an outlet boundary.
@@ -8115,91 +8115,91 @@ class CConfig {
    * \param[in] val_index - Index corresponding to the displacement boundary.
    * \return The displacement value.
    */
-  su2double GetDispl_Value(string val_index) const;
+  su2double GetDispl_Value(const string& val_index) const;
 
   /*!
    * \brief Get the force value at an load boundary.
    * \param[in] val_index - Index corresponding to the load boundary.
    * \return The load value.
    */
-  su2double GetLoad_Value(string val_index) const;
+  su2double GetLoad_Value(const string& val_index) const;
 
   /*!
    * \brief Get the constant value at a damper boundary.
    * \param[in] val_index - Index corresponding to the load boundary.
    * \return The damper constant.
    */
-  su2double GetDamper_Constant(string val_index) const;
+  su2double GetDamper_Constant(const string& val_index) const;
 
   /*!
    * \brief Get the force value at a load boundary defined in cartesian coordinates.
    * \param[in] val_index - Index corresponding to the load boundary.
    * \return The load value.
    */
-  su2double GetLoad_Dir_Value(string val_index) const;
+  su2double GetLoad_Dir_Value(const string& val_index) const;
 
   /*!
    * \brief Get the force multiplier at a load boundary in cartesian coordinates.
    * \param[in] val_index - Index corresponding to the load boundary.
    * \return The load multiplier.
    */
-  su2double GetLoad_Dir_Multiplier(string val_index) const;
+  su2double GetLoad_Dir_Multiplier(const string& val_index) const;
 
   /*!
    * \brief Get the force value at a load boundary defined in cartesian coordinates.
    * \param[in] val_index - Index corresponding to the load boundary.
    * \return The load value.
    */
-  su2double GetDisp_Dir_Value(string val_index) const;
+  su2double GetDisp_Dir_Value(const string& val_index) const;
 
   /*!
    * \brief Get the force multiplier at a load boundary in cartesian coordinates.
    * \param[in] val_index - Index corresponding to the load boundary.
    * \return The load multiplier.
    */
-  su2double GetDisp_Dir_Multiplier(string val_index) const;
+  su2double GetDisp_Dir_Multiplier(const string& val_index) const;
 
   /*!
    * \brief Get the force direction at a loaded boundary in cartesian coordinates.
    * \param[in] val_index - Index corresponding to the load boundary.
    * \return The load direction.
    */
-  const su2double* GetLoad_Dir(string val_index) const;
+  const su2double* GetLoad_Dir(const string& val_index) const;
 
   /*!
    * \brief Get the force direction at a loaded boundary in cartesian coordinates.
    * \param[in] val_index - Index corresponding to the load boundary.
    * \return The load direction.
    */
-  const su2double* GetDisp_Dir(string val_index) const;
+  const su2double* GetDisp_Dir(const string& val_index) const;
 
   /*!
    * \brief Get the amplitude of the sine-wave at a load boundary defined in cartesian coordinates.
    * \param[in] val_index - Index corresponding to the load boundary.
    * \return The load value.
    */
-  su2double GetLoad_Sine_Amplitude(string val_index) const;
+  su2double GetLoad_Sine_Amplitude(const string& val_index) const;
 
   /*!
    * \brief Get the frequency of the sine-wave at a load boundary in cartesian coordinates.
    * \param[in] val_index - Index corresponding to the load boundary.
    * \return The load frequency.
    */
-  su2double GetLoad_Sine_Frequency(string val_index) const;
+  su2double GetLoad_Sine_Frequency(const string& val_index) const;
 
   /*!
    * \brief Get the force direction at a sine-wave loaded boundary in cartesian coordinates.
    * \param[in] val_index - Index corresponding to the load boundary.
    * \return The load direction.
    */
-  const su2double* GetLoad_Sine_Dir(string val_index) const;
+  const su2double* GetLoad_Sine_Dir(const string& val_index) const;
 
   /*!
    * \brief Get the force value at an load boundary.
    * \param[in] val_index - Index corresponding to the load boundary.
    * \return The load value.
    */
-  su2double GetFlowLoad_Value(string val_index) const;
+  su2double GetFlowLoad_Value(const string& val_index) const;
 
   /*!
    * \brief Cyclic pitch amplitude for rotor blades.
@@ -8616,7 +8616,7 @@ class CConfig {
    * \param[in] val_function_name - string for the name of the profiled subroutine.
    * \param[in] val_group_id - string for the name of the profiled subroutine.
    */
-  void Tock(double val_start_time, string val_function_name, int val_group_id);
+  void Tock(double val_start_time, const string& val_function_name, int val_group_id);
 
   /*!
    * \brief Write a CSV file containing the results of the profiling.
@@ -9360,7 +9360,7 @@ class CConfig {
    * \param[in] val_index - Index corresponding to the boundary.
    * \return The wall emissivity.
    */
-  su2double GetWall_Emissivity(string val_index) const;
+  su2double GetWall_Emissivity(const string& val_index) const;
 
   /*!
    * \brief Get the value of the CFL condition for radiation solvers.
diff --git a/Common/include/containers/CLookUpTable.hpp b/Common/include/containers/CLookUpTable.hpp
index c9920cb508e..f6cd4c91bb8 100644
--- a/Common/include/containers/CLookUpTable.hpp
+++ b/Common/include/containers/CLookUpTable.hpp
@@ -271,7 +271,7 @@ class CLookUpTable {
                                                               const su2double val_CV3);
 
  public:
-  CLookUpTable(const std::string& file_name_lut, const std::string& name_CV1_in, const std::string& name_CV2_in);
+  CLookUpTable(const std::string& file_name_lut, std::string name_CV1_in, std::string name_CV2_in);
 
   /*!
    * \brief print information to screen.
diff --git a/Common/include/geometry/CGeometry.hpp b/Common/include/geometry/CGeometry.hpp
index dd5f936fe49..2822d430072 100644
--- a/Common/include/geometry/CGeometry.hpp
+++ b/Common/include/geometry/CGeometry.hpp
@@ -405,7 +405,7 @@ class CGeometry {
    * \param[in] countPerPeriodicPoint - Number of variables per point.
    */
   void PostPeriodicRecvs(CGeometry* geometry, const CConfig* config, unsigned short commType,
-                         unsigned short countPerPeriodicPoint);
+                         unsigned short countPerPeriodicPoint) const;
 
   /*!
    * \brief Routine to launch a single non-blocking send once the buffer is loaded for a periodic commucation.
@@ -959,33 +959,33 @@ class CGeometry {
    * \param[in] config - Definition of the particular problem.
    * \param[in] print - Display information on screen.
    */
-  void SetRotationalVelocity(const CConfig* config, bool print = false);
+  void SetRotationalVelocity(const CConfig* config, bool print = false) const;
 
   /*!
    * \brief Set the rotational velocity of the points on the shroud markers to 0.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetShroudVelocity(const CConfig* config);
+  void SetShroudVelocity(const CConfig* config) const;
 
   /*!
    * \brief Set the translational velocity at each node.
    * \param[in] config - Definition of the particular problem.
    * \param[in] print - Display information on screen.
    */
-  void SetTranslationalVelocity(const CConfig* config, bool print = false);
+  void SetTranslationalVelocity(const CConfig* config, bool print = false) const;
 
   /*!
    * \brief Set the translational/rotational velocity for all moving walls.
    * \param[in] config - Definition of the particular problem.
    * \param[in] print - Display information on screen.
    */
-  void SetWallVelocity(const CConfig* config, bool print = false);
+  void SetWallVelocity(const CConfig* config, bool print = false) const;
 
   /*!
    * \brief Set the grid velocity via finite differencing at each node.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetGridVelocity(const CConfig* config);
+  void SetGridVelocity(const CConfig* config) const;
 
   /*!
    * \brief A virtual member.
@@ -1020,7 +1020,7 @@ class CGeometry {
    * \brief Find and store all vertices on a sharp corner in the geometry.
    * \param[in] config - Definition of the particular problem.
    */
-  void ComputeSurf_Curvature(CConfig* config);
+  void ComputeSurf_Curvature(CConfig* config) const;
 
   /*!
    * \brief A virtual member.
@@ -1678,7 +1678,7 @@ class CGeometry {
   /*!
    * \brief Compute and store the volume of the primal elements.
    */
-  void SetElemVolume();
+  void SetElemVolume() const;
 
   /*!
    * \brief Set the multigrid index for the current geometry object.
diff --git a/Common/include/geometry/CPhysicalGeometry.hpp b/Common/include/geometry/CPhysicalGeometry.hpp
index b02db55c0a4..0f881daeea9 100644
--- a/Common/include/geometry/CPhysicalGeometry.hpp
+++ b/Common/include/geometry/CPhysicalGeometry.hpp
@@ -282,7 +282,8 @@ class CPhysicalGeometry final : public CGeometry {
    * \param[in] val_iZone - Domain to be read from the grid file.
    * \param[in] val_nZone - Total number of domains in the grid file.
    */
-  void Read_Mesh_FVM(CConfig* config, string val_mesh_filename, unsigned short val_iZone, unsigned short val_nZone);
+  void Read_Mesh_FVM(CConfig* config, const string& val_mesh_filename, unsigned short val_iZone,
+                     unsigned short val_nZone);
 
   /*!
    * \brief Reads for the FEM solver the geometry of the grid and adjust the boundary
@@ -292,7 +293,7 @@ class CPhysicalGeometry final : public CGeometry {
    * \param[in] val_iZone - Domain to be read from the grid file.
    * \param[in] val_nZone - Total number of domains in the grid file.
    */
-  void Read_SU2_Format_Parallel_FEM(CConfig* config, string val_mesh_filename, unsigned short val_iZone,
+  void Read_SU2_Format_Parallel_FEM(CConfig* config, const string& val_mesh_filename, unsigned short val_iZone,
                                     unsigned short val_nZone);
 
   /*!
@@ -303,7 +304,7 @@ class CPhysicalGeometry final : public CGeometry {
    * \param[in] val_iZone - Domain to be read from the grid file.
    * \param[in] val_nZone - Total number of domains in the grid file.
    */
-  void Read_CGNS_Format_Parallel_FEM(CConfig* config, string val_mesh_filename, unsigned short val_iZone,
+  void Read_CGNS_Format_Parallel_FEM(CConfig* config, const string& val_mesh_filename, unsigned short val_iZone,
                                      unsigned short val_nZone);
 
   /*!
diff --git a/Common/include/geometry/meshreader/CCGNSMeshReaderFVM.hpp b/Common/include/geometry/meshreader/CCGNSMeshReaderFVM.hpp
index 5b65f4d925b..198589808cf 100644
--- a/Common/include/geometry/meshreader/CCGNSMeshReaderFVM.hpp
+++ b/Common/include/geometry/meshreader/CCGNSMeshReaderFVM.hpp
@@ -63,7 +63,7 @@ class CCGNSMeshReaderFVM : public CMeshReaderFVM {
    * \brief Open the CGNS file and checks for errors.
    * \param[in] val_filename - string name of the CGNS file to be read.
    */
-  void OpenCGNSFile(string val_filename);
+  void OpenCGNSFile(const string& val_filename);
 
   /*!
    * \brief Reads all CGNS database metadata and checks for errors.
diff --git a/Common/include/grid_movement/CFreeFormDefBox.hpp b/Common/include/grid_movement/CFreeFormDefBox.hpp
index 70a1d3adcec..30aa1ae17f0 100644
--- a/Common/include/grid_movement/CFreeFormDefBox.hpp
+++ b/Common/include/grid_movement/CFreeFormDefBox.hpp
@@ -292,7 +292,7 @@ class CFreeFormDefBox : public CGridMovement {
    *        and find the position of the control points for the FFDBox
    * \param[in] FFDBox - Original FFDBox where we want to compute the control points.
    */
-  void SetSupportCPChange(CFreeFormDefBox* FFDBox);
+  void SetSupportCPChange(CFreeFormDefBox* FFDBox) const;
 
   /*!
    * \brief Set the number of corner points.
@@ -439,7 +439,7 @@ class CFreeFormDefBox : public CGridMovement {
   /*!
    * \brief Set the control points in a parallelepiped (hexahedron).
    */
-  void SetControlPoints_Parallelepiped(void);
+  void SetControlPoints_Parallelepiped(void) const;
 
   /*!
    * \brief Set the control points of the final chuck in a unitary hexahedron free form.
@@ -502,49 +502,49 @@ class CFreeFormDefBox : public CGridMovement {
    * \brief Set Cylindrical to Cartesians_ControlPoints.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetCyl2Cart_ControlPoints(CConfig* config);
+  void SetCyl2Cart_ControlPoints(CConfig* config) const;
 
   /*!
    * \brief Set Cartesians to Cylindrical ControlPoints.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetCart2Cyl_ControlPoints(CConfig* config);
+  void SetCart2Cyl_ControlPoints(CConfig* config) const;
 
   /*!
    * \brief Set Cylindrical to Cartesians_CornerPoints.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetCyl2Cart_CornerPoints(CConfig* config);
+  void SetCyl2Cart_CornerPoints(CConfig* config) const;
 
   /*!
    * \brief Set Cartesians to Cylindrical CornerPoints.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetCart2Cyl_CornerPoints(CConfig* config);
+  void SetCart2Cyl_CornerPoints(CConfig* config) const;
 
   /*!
    * \brief Set Spherical to Cartesians ControlPoints.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetSphe2Cart_ControlPoints(CConfig* config);
+  void SetSphe2Cart_ControlPoints(CConfig* config) const;
 
   /*!
    * \brief SetCartesians to Spherical ControlPoints.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetCart2Sphe_ControlPoints(CConfig* config);
+  void SetCart2Sphe_ControlPoints(CConfig* config) const;
 
   /*!
    * \brief Set Spherical to Cartesians_CornerPoints.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetSphe2Cart_CornerPoints(CConfig* config);
+  void SetSphe2Cart_CornerPoints(CConfig* config) const;
 
   /*!
    * \brief Set Cartesians to Spherical Corner Points.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetCart2Sphe_CornerPoints(CConfig* config);
+  void SetCart2Sphe_CornerPoints(CConfig* config) const;
 
   /*!
    * \brief Set the cartesian coords of a point in R^3 and convert them to the parametric coords of
@@ -710,7 +710,7 @@ class CFreeFormDefBox : public CGridMovement {
    *        which? diff_thiss will tell us ; E.G.: dim=2, diff_this=1 => we use the third coordinate of the control
    *        points, and derivate de v-Bersntein polynomial (use m-1 when summing!!).
    */
-  su2double GetDerivative3(su2double* uvw, unsigned short dim, unsigned short diff_this, unsigned short* lmn);
+  su2double GetDerivative3(su2double* uvw, unsigned short dim, unsigned short diff_this, unsigned short* lmn) const;
 
   /*!
    * \brief An auxiliary routine to help us compute the Hessian of F(u, v, w) = ||X(u, v, w)-(x, y, z)||^2 =
@@ -742,7 +742,7 @@ class CFreeFormDefBox : public CGridMovement {
    * \return __________.
    */
   su2double GetDerivative5(su2double* uvw, unsigned short dim, unsigned short diff_this, unsigned short diff_this_also,
-                           unsigned short* lmn);
+                           unsigned short* lmn) const;
 
   /*!
    * \brief Euclidean norm of a vector.
diff --git a/Common/include/grid_movement/CSurfaceMovement.hpp b/Common/include/grid_movement/CSurfaceMovement.hpp
index 28eca93c343..6a8382d1571 100644
--- a/Common/include/grid_movement/CSurfaceMovement.hpp
+++ b/Common/include/grid_movement/CSurfaceMovement.hpp
@@ -433,7 +433,7 @@ class CSurfaceMovement : public CGridMovement {
    * \param[in] FFDBox - Array with all the free forms FFDBoxes of the computation.
    * \param[in] val_mesh_filename - Name of the grid input file.
    */
-  void ReadFFDInfo(CGeometry* geometry, CConfig* config, CFreeFormDefBox** FFDBox, string val_mesh_filename);
+  void ReadFFDInfo(CGeometry* geometry, CConfig* config, CFreeFormDefBox** FFDBox, const string& val_mesh_filename);
 
   /*!
    * \brief Read the free form information from the grid input file.
diff --git a/Common/include/linear_algebra/CSysSolve.hpp b/Common/include/linear_algebra/CSysSolve.hpp
index 0a5ed8f52a0..02569f8b396 100644
--- a/Common/include/linear_algebra/CSysSolve.hpp
+++ b/Common/include/linear_algebra/CSysSolve.hpp
@@ -191,7 +191,7 @@ class CSysSolve {
    *
    * \pre the ostream object os should be open
    */
-  void WriteHeader(std::string solver, ScalarType restol, ScalarType resinit) const;
+  void WriteHeader(const std::string& solver, ScalarType restol, ScalarType resinit) const;
 
   /*!
    * \brief writes residual convergence data for one iteration to a stream
@@ -208,7 +208,7 @@ class CSysSolve {
    * \param[in] iter - current iteration
    * \param[in] res - the residual norm
    */
-  void WriteFinalResidual(std::string solver, unsigned long iter, ScalarType res) const;
+  void WriteFinalResidual(const std::string& solver, unsigned long iter, ScalarType res) const;
 
   /*!
    * \brief writes the convergence warning
diff --git a/Common/include/parallelization/mpi_structure.cpp b/Common/include/parallelization/mpi_structure.cpp
index 43b2c86a239..c55dc625eba 100644
--- a/Common/include/parallelization/mpi_structure.cpp
+++ b/Common/include/parallelization/mpi_structure.cpp
@@ -44,7 +44,7 @@ int CBaseMPIWrapper::MinRankError;
 bool CBaseMPIWrapper::winMinRankErrorInUse = false;
 CBaseMPIWrapper::Win CBaseMPIWrapper::winMinRankError;
 
-void CBaseMPIWrapper::Error(std::string ErrorMsg, std::string FunctionName) {
+void CBaseMPIWrapper::Error(const std::string& ErrorMsg, const std::string& FunctionName) {
   /* Set MinRankError to Rank, as the error message is called on this rank. */
   MinRankError = Rank;
   int flag = 0;
diff --git a/Common/include/parallelization/mpi_structure.hpp b/Common/include/parallelization/mpi_structure.hpp
index 1df7281ccbd..470b8c4a479 100644
--- a/Common/include/parallelization/mpi_structure.hpp
+++ b/Common/include/parallelization/mpi_structure.hpp
@@ -108,7 +108,7 @@ class CBaseMPIWrapper {
   static void CopyData(const void* sendbuf, void* recvbuf, int size, Datatype datatype, int recvshift = 0,
                        int sendshift = 0);
 
-  static void Error(std::string ErrorMsg, std::string FunctionName);
+  static void Error(const std::string& ErrorMsg, const std::string& FunctionName);
 
   static inline int GetRank() { return Rank; }
 
diff --git a/Common/include/toolboxes/C1DInterpolation.hpp b/Common/include/toolboxes/C1DInterpolation.hpp
index aa00b3f2999..5625a6f022e 100644
--- a/Common/include/toolboxes/C1DInterpolation.hpp
+++ b/Common/include/toolboxes/C1DInterpolation.hpp
@@ -192,5 +192,5 @@ std::vector<su2double> CorrectedInletValues(const std::vector<su2double>& Inlet_
  * \param[in] nDim - the dimensions of the problem.
  * \param[in] nColumns - the number of columns in the final interpolated data
  */
-void PrintInletInterpolatedData(const std::vector<su2double>& Inlet_Data_Interpolated, std::string Marker,
+void PrintInletInterpolatedData(const std::vector<su2double>& Inlet_Data_Interpolated, const std::string& Marker,
                                 unsigned long nVertex, unsigned short nDim, unsigned short nColumns);
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index ea45d2d0159..5fd2e130f81 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -26,6 +26,8 @@
  */
 
 #define ENABLE_MAPS
+#include <utility>
+
 #include "../include/CConfig.hpp"
 #undef ENABLE_MAPS
 
@@ -282,7 +284,7 @@ void CConfig::SetMPICommunicator(SU2_MPI::Comm Communicator) {
 
 }
 
-void CConfig::addDoubleOption(const string name, su2double & option_field, su2double default_value) {
+void CConfig::addDoubleOption(const string& name, su2double & option_field, su2double default_value) {
   // Check if the key is already in the map. If this fails, it is coder error
   // and not user error, so throw.
   assert(option_map.find(name) == option_map.end());
@@ -301,43 +303,43 @@ void CConfig::addDoubleOption(const string name, su2double & option_field, su2do
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addStringOption(const string name, string & option_field, string default_value) {
+void CConfig::addStringOption(const string& name, string & option_field, string default_value) {
 
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
-  COptionBase* val = new COptionString(name, option_field, default_value);
+  COptionBase* val = new COptionString(name, option_field, std::move(default_value));
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addIntegerOption(const string name, int & option_field, int default_value) {
+void CConfig::addIntegerOption(const string& name, int & option_field, int default_value) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
   COptionBase* val = new COptionInt(name, option_field, default_value);
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addUnsignedLongOption(const string name, unsigned long & option_field, unsigned long default_value) {
+void CConfig::addUnsignedLongOption(const string& name, unsigned long & option_field, unsigned long default_value) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
   COptionBase* val = new COptionULong(name, option_field, default_value);
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addUnsignedShortOption(const string name, unsigned short & option_field, unsigned short default_value) {
+void CConfig::addUnsignedShortOption(const string& name, unsigned short & option_field, unsigned short default_value) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
   COptionBase* val = new COptionUShort(name, option_field, default_value);
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addLongOption(const string name, long & option_field, long default_value) {
+void CConfig::addLongOption(const string& name, long & option_field, long default_value) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
   COptionBase* val = new COptionLong(name, option_field, default_value);
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addBoolOption(const string name, bool & option_field, bool default_value) {
+void CConfig::addBoolOption(const string& name, bool & option_field, bool default_value) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
   COptionBase* val = new COptionBool(name, option_field, default_value);
@@ -352,7 +354,6 @@ void CConfig::addEnumOption(const string name, TField& option_field, const map<s
   all_options.insert(pair<string, bool>(name, true));
   COptionBase* val = new COptionEnum<Tenum, TField>(name, enum_map, option_field, default_value);
   option_map.insert(pair<string, COptionBase *>(name, val));
-  return;
 }
 
 // input_size is the number of options read in from the config file
@@ -365,70 +366,70 @@ void CConfig::addEnumListOption(const string name, unsigned short& input_size, T
   option_map.insert( pair<string, COptionBase*>(name, val) );
 }
 
-void CConfig::addDoubleArrayOption(const string name, const int size, su2double* option_field) {
+void CConfig::addDoubleArrayOption(const string& name, const int size, su2double* option_field) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
   COptionBase* val = new COptionArray<su2double>(name, size, option_field);
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addUShortArrayOption(const string name, const int size, unsigned short* option_field) {
+void CConfig::addUShortArrayOption(const string& name, const int size, unsigned short* option_field) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
   COptionBase* val = new COptionArray<unsigned short>(name, size, option_field);
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addDoubleListOption(const string name, unsigned short & size, su2double * & option_field) {
+void CConfig::addDoubleListOption(const string& name, unsigned short & size, su2double * & option_field) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
   COptionBase* val = new COptionDoubleList(name, size, option_field);
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addShortListOption(const string name, unsigned short & size, short * & option_field) {
+void CConfig::addShortListOption(const string& name, unsigned short & size, short * & option_field) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
   COptionBase* val = new COptionShortList(name, size, option_field);
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addUShortListOption(const string name, unsigned short & size, unsigned short * & option_field) {
+void CConfig::addUShortListOption(const string& name, unsigned short & size, unsigned short * & option_field) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
   COptionBase* val = new COptionUShortList(name, size, option_field);
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addULongListOption(const string name, unsigned short & size, unsigned long * & option_field) {
+void CConfig::addULongListOption(const string& name, unsigned short & size, unsigned long * & option_field) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
   COptionBase* val = new COptionULongList(name, size, option_field);
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addStringListOption(const string name, unsigned short & num_marker, string* & option_field) {
+void CConfig::addStringListOption(const string& name, unsigned short & num_marker, string* & option_field) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
   COptionBase* val = new COptionStringList(name, num_marker, option_field);
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addConvectOption(const string name, unsigned short & space_field, CENTERED & centered_field, UPWIND & upwind_field) {
+void CConfig::addConvectOption(const string& name, unsigned short & space_field, CENTERED & centered_field, UPWIND & upwind_field) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
   COptionBase* val = new COptionConvect(name, space_field, centered_field, upwind_field);
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addConvectFEMOption(const string name, unsigned short & space_field, unsigned short & fem_field) {
+void CConfig::addConvectFEMOption(const string& name, unsigned short & space_field, unsigned short & fem_field) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
   COptionBase* val = new COptionFEMConvect(name, space_field, fem_field);
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addMathProblemOption(const string name, bool & ContinuousAdjoint, const bool & ContinuousAdjoint_default,
+void CConfig::addMathProblemOption(const string& name, bool & ContinuousAdjoint, const bool & ContinuousAdjoint_default,
                           bool & DiscreteAdjoint, const bool & DiscreteAdjoint_default,
                           bool & Restart_Flow, const bool & Restart_Flow_default) {
   assert(option_map.find(name) == option_map.end());
@@ -437,7 +438,7 @@ void CConfig::addMathProblemOption(const string name, bool & ContinuousAdjoint,
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addDVParamOption(const string name, unsigned short & nDV_field, su2double** & paramDV, string* & FFDTag,
+void CConfig::addDVParamOption(const string& name, unsigned short & nDV_field, su2double** & paramDV, string* & FFDTag,
                       unsigned short* & design_variable) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
@@ -445,7 +446,7 @@ void CConfig::addDVParamOption(const string name, unsigned short & nDV_field, su
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addDVValueOption(const string name, unsigned short* & nDVValue_field, su2double** & valueDV, unsigned short & nDV_field,  su2double** & paramDV,
+void CConfig::addDVValueOption(const string& name, unsigned short* & nDVValue_field, su2double** & valueDV, unsigned short & nDV_field,  su2double** & paramDV,
                       unsigned short* & design_variable) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
@@ -453,21 +454,21 @@ void CConfig::addDVValueOption(const string name, unsigned short* & nDVValue_fie
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addFFDDefOption(const string name, unsigned short & nFFD_field, su2double** & coordFFD, string* & FFDTag) {
+void CConfig::addFFDDefOption(const string& name, unsigned short & nFFD_field, su2double** & coordFFD, string* & FFDTag) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
   COptionBase* val = new COptionFFDDef(name, nFFD_field, coordFFD, FFDTag);
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addFFDDegreeOption(const string name, unsigned short & nFFD_field, unsigned short** & degreeFFD) {
+void CConfig::addFFDDegreeOption(const string& name, unsigned short & nFFD_field, unsigned short** & degreeFFD) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
   COptionBase* val = new COptionFFDDegree(name, nFFD_field, degreeFFD);
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addStringDoubleListOption(const string name, unsigned short & list_size, string * & string_field,
+void CConfig::addStringDoubleListOption(const string& name, unsigned short & list_size, string * & string_field,
                                         su2double* & double_field) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
@@ -475,7 +476,7 @@ void CConfig::addStringDoubleListOption(const string name, unsigned short & list
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addInletOption(const string name, unsigned short & nMarker_Inlet, string * & Marker_Inlet,
+void CConfig::addInletOption(const string& name, unsigned short & nMarker_Inlet, string * & Marker_Inlet,
                     su2double* & Ttotal, su2double* & Ptotal, su2double** & FlowDir) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
@@ -483,7 +484,7 @@ void CConfig::addInletOption(const string name, unsigned short & nMarker_Inlet,
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addInletSpeciesOption(const string name, unsigned short & nMarker_Inlet_Species,
+void CConfig::addInletSpeciesOption(const string& name, unsigned short & nMarker_Inlet_Species,
                                     string * & Marker_Inlet_Species, su2double** & inlet_species_val,
                                     unsigned short & nSpecies_per_Inlet) {
   assert(option_map.find(name) == option_map.end());
@@ -493,7 +494,7 @@ void CConfig::addInletSpeciesOption(const string name, unsigned short & nMarker_
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addInletTurbOption(const string name, unsigned short& nMarker_Inlet_Turb, string*& Marker_Inlet_Turb,
+void CConfig::addInletTurbOption(const string& name, unsigned short& nMarker_Inlet_Turb, string*& Marker_Inlet_Turb,
                                  su2double**& Turb_Properties_val, unsigned short& nTurb_Properties) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
@@ -520,7 +521,7 @@ void CConfig::addGilesOption(const string name, unsigned short & nMarker_Giles,
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addExhaustOption(const string name, unsigned short & nMarker_Exhaust, string * & Marker_Exhaust,
+void CConfig::addExhaustOption(const string& name, unsigned short & nMarker_Exhaust, string * & Marker_Exhaust,
                                su2double* & Ttotal, su2double* & Ptotal) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
@@ -566,14 +567,14 @@ void CConfig::addWallFunctionOption(const string &name, unsigned short &list_siz
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-void CConfig::addPythonOption(const string name) {
+void CConfig::addPythonOption(const string& name) {
   assert(option_map.find(name) == option_map.end());
   all_options.insert(pair<string, bool>(name, true));
   COptionBase* val = new COptionPython(name);
   option_map.insert(pair<string, COptionBase *>(name, val));
 }
 
-unsigned short CConfig::GetnZone(string val_mesh_filename, unsigned short val_format) {
+unsigned short CConfig::GetnZone(const string& val_mesh_filename, unsigned short val_format) {
 
   int nZone = 1; /* Default value if nothing is specified. */
 
@@ -695,7 +696,7 @@ unsigned short CConfig::GetnZone(string val_mesh_filename, unsigned short val_fo
 
 }
 
-unsigned short CConfig::GetnDim(string val_mesh_filename, unsigned short val_format) {
+unsigned short CConfig::GetnDim(const string& val_mesh_filename, unsigned short val_format) {
 
   short nDim = -1;
 
@@ -807,7 +808,7 @@ unsigned short CConfig::GetnDim(string val_mesh_filename, unsigned short val_for
   return (unsigned short) nDim;
 }
 
-void CConfig::SetPointersNull(void) {
+void CConfig::SetPointersNull() {
 
   Marker_CfgFile_GeoEval      = nullptr;   Marker_All_GeoEval       = nullptr;
   Marker_CfgFile_Monitoring   = nullptr;   Marker_All_Monitoring    = nullptr;
@@ -2960,7 +2961,7 @@ void CConfig::SetConfig_Parsing(istream& config_buffer){
      * If there is a statement after a cont. char
      * throw an error. ---*/
 
-     if (text_line.size() && (text_line.front() != '%')){
+     if (!text_line.empty() && (text_line.front() != '%')){
        while (text_line.back() == '\\' ||
               (PrintingToolbox::split(text_line, '\\').size() > 1)){
          string tmp;
@@ -3115,7 +3116,7 @@ void CConfig::SetConfig_Parsing(istream& config_buffer){
 
   /*--- See if there were any errors parsing the config file ---*/
 
-  if (errorString.size() != 0) {
+  if (!errorString.empty()) {
     SU2_MPI::Error(errorString, CURRENT_FUNCTION);
   }
 }
@@ -3128,7 +3129,7 @@ void CConfig::SetDefaultFromConfig(CConfig *config){
 
   while (iter != all_options.end()){
     curr_iter = iter++;
-    if (config->option_map[curr_iter->first]->GetValue().size() > 0 && !noInheritance[curr_iter->first]){
+    if (!config->option_map[curr_iter->first]->GetValue().empty() && !noInheritance[curr_iter->first]){
       option_map[curr_iter->first]->SetValue(config->option_map[curr_iter->first]->GetValue());
       all_options.erase(curr_iter);
     }
@@ -3139,8 +3140,8 @@ void CConfig::SetDefault(){
 
   /*--- Set the default values for all of the options that weren't set ---*/
 
-  for (map<string, bool>::iterator iter = all_options.begin(); iter != all_options.end(); ++iter) {
-    if (option_map[iter->first]->GetValue().size() == 0)
+  for (auto iter = all_options.begin(); iter != all_options.end(); ++iter) {
+    if (option_map[iter->first]->GetValue().empty())
       option_map[iter->first]->SetDefault();
   }
 }
@@ -3218,13 +3219,13 @@ bool CConfig::SetRunTime_Parsing(char case_filename[MAX_STRING_SIZE]) {
 
   /*--- Set the default values for all of the options that weren't set ---*/
 
-  for (map<string, bool>::iterator iter = all_options.begin(); iter != all_options.end(); ++iter) {
+  for (auto iter = all_options.begin(); iter != all_options.end(); ++iter) {
     option_map[iter->first]->SetDefault();
   }
 
   /*--- See if there were any errors parsing the runtime file ---*/
 
-  if (errorString.size() != 0) {
+  if (!errorString.empty()) {
     SU2_MPI::Error(errorString, CURRENT_FUNCTION);
   }
 
@@ -3489,7 +3490,7 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
         SU2_MPI::Error(string("For RANS problems, use NONE, STANDARD_WALL_FUNCTION or EQUILIBRIUM_WALL_MODEL.\n"), CURRENT_FUNCTION);
 
       if (Kind_WallFunctions[iMarker] == WALL_FUNCTIONS::STANDARD_FUNCTION) {
-        if (!((Kind_Solver == MAIN_SOLVER::RANS) || (Kind_Solver == MAIN_SOLVER::INC_RANS)))
+        if ((Kind_Solver != MAIN_SOLVER::RANS) && (Kind_Solver != MAIN_SOLVER::INC_RANS))
           SU2_MPI::Error(string("Wall model STANDARD_FUNCTION only available for RANS or INC_RANS.\n"), CURRENT_FUNCTION);
         if (nRough_Wall != 0)
           SU2_MPI::Error(string("Wall model STANDARD_FUNCTION and WALL_ROUGHNESS migh not be compatible. Checking required!\n"), CURRENT_FUNCTION);
@@ -4360,8 +4361,7 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
 
   /*--- Set the boolean flag if we are carrying out an aeroelastic simulation. ---*/
 
-  if (GetGrid_Movement() && (GetSurface_Movement(AEROELASTIC) || GetSurface_Movement(AEROELASTIC_RIGID_MOTION))) Aeroelastic_Simulation = true;
-  else Aeroelastic_Simulation = false;
+  Aeroelastic_Simulation = GetGrid_Movement() && (GetSurface_Movement(AEROELASTIC) || GetSurface_Movement(AEROELASTIC_RIGID_MOTION));
 
   /*--- Initializing the size for the solutions of the Aeroelastic problem. ---*/
 
@@ -4423,7 +4423,7 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
   /*--- Make the MG_PreSmooth, MG_PostSmooth, and MG_CorrecSmooth
    arrays consistent with nMGLevels ---*/
 
-  unsigned short * tmp_smooth = new unsigned short[nMGLevels+1];
+  auto * tmp_smooth = new unsigned short[nMGLevels+1];
 
   if ((nMG_PreSmooth != nMGLevels+1) && (nMG_PreSmooth != 0)) {
     if (nMG_PreSmooth > nMGLevels+1) {
@@ -4891,7 +4891,7 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
 
   if (Kind_Solver == MAIN_SOLVER::INC_EULER) {
     /*--- Force inviscid problems to use constant density and disable energy. ---*/
-    if (Kind_DensityModel != INC_DENSITYMODEL::CONSTANT || Energy_Equation == true) {
+    if (Kind_DensityModel != INC_DENSITYMODEL::CONSTANT || Energy_Equation) {
       SU2_MPI::Error("Inviscid incompressible problems must be constant density (no energy eqn.).\n Use DENSITY_MODEL= CONSTANT and ENERGY_EQUATION= NO.", CURRENT_FUNCTION);
     }
   }
@@ -5331,8 +5331,7 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
   /*--- Specifying a deforming surface requires a mesh deformation solver. ---*/
   if (GetSurface_Movement(DEFORMING)) Deform_Mesh = true;
 
-  if (GetGasModel() == "ARGON") {monoatomic = true;}
-  else {monoatomic = false;}
+  monoatomic = GetGasModel() == "ARGON";
 
   /*--- Set number of Turbulence Variables. ---*/
   switch (TurbModelFamily(Kind_Turb_Model)) {
@@ -5404,7 +5403,7 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
           CURRENT_FUNCTION);
 
     // Helper function that checks scalar variable bounds,
-    auto checkScalarBounds = [&](su2double scalar, string name, su2double lowerBound, su2double upperBound) {
+    auto checkScalarBounds = [&](su2double scalar, const string& name, su2double lowerBound, su2double upperBound) {
       if (scalar < lowerBound || scalar > upperBound)
         SU2_MPI::Error(string("Variable: ") + name + string(", is out of bounds."), CURRENT_FUNCTION);
     };
@@ -7544,7 +7543,7 @@ bool CConfig::TokenizeString(string & str, string & option_name,
   const string delimiters(" (){}:,\t\n\v\f\r");
   // check for comments or empty string
   string::size_type pos, last_pos;
-  pos = str.find_first_of("%");
+  pos = str.find_first_of('%');
   if ( (str.length() == 0) || (pos == 0) ) {
     // str is empty or a comment line, so no option here
     return false;
@@ -7562,7 +7561,7 @@ bool CConfig::TokenizeString(string & str, string & option_name,
 
   // find the equals sign and split string
   string name_part, value_part;
-  pos = str.find("=");
+  pos = str.find('=');
   if (pos == string::npos) {
     cerr << "Error in TokenizeString(): "
     << "line in the configuration file with no \"=\" sign."
@@ -7618,7 +7617,7 @@ bool CConfig::TokenizeString(string & str, string & option_name,
     // find next "non-delimiter"
     pos = value_part.find_first_of(delimiters, last_pos);
   }
-  if (option_value.size() == 0) {
+  if (option_value.empty()) {
     cerr << "Error in TokenizeString(): "
     << "option " << option_name << " in configuration file with no value assigned."
     << endl;
@@ -7653,7 +7652,7 @@ bool CConfig::TokenizeString(string & str, string & option_name,
         *it = before_semi;
         it++;
         vector<string> to_insert;
-        to_insert.push_back(";");
+        to_insert.emplace_back(";");
         if (!after_semi.empty())
           to_insert.push_back(after_semi);
         option_value.insert(it, to_insert.begin(), to_insert.end());
@@ -7682,11 +7681,7 @@ bool CConfig::TokenizeString(string & str, string & option_name,
         continue;
       }
     }
-    if (it->compare(";") == 0) {
-      semi_at_prev = true;
-    } else {
-      semi_at_prev = false;
-    }
+    semi_at_prev = it->compare(";") == 0;
     it++;
   }
 
@@ -7699,7 +7694,7 @@ bool CConfig::TokenizeString(string & str, string & option_name,
   return true;
 }
 
-unsigned short CConfig::GetMarker_CfgFile_TagBound(string val_marker) const {
+unsigned short CConfig::GetMarker_CfgFile_TagBound(const string& val_marker) const {
 
   unsigned short iMarker_CfgFile;
 
@@ -7715,133 +7710,133 @@ string CConfig::GetMarker_CfgFile_TagBound(unsigned short val_marker) const {
   return Marker_CfgFile_TagBound[val_marker];
 }
 
-unsigned short CConfig::GetMarker_CfgFile_KindBC(string val_marker) const {
+unsigned short CConfig::GetMarker_CfgFile_KindBC(const string& val_marker) const {
   unsigned short iMarker_CfgFile;
   for (iMarker_CfgFile = 0; iMarker_CfgFile < nMarker_CfgFile; iMarker_CfgFile++)
     if (Marker_CfgFile_TagBound[iMarker_CfgFile] == val_marker) break;
   return Marker_CfgFile_KindBC[iMarker_CfgFile];
 }
 
-unsigned short CConfig::GetMarker_CfgFile_Monitoring(string val_marker) const {
+unsigned short CConfig::GetMarker_CfgFile_Monitoring(const string& val_marker) const {
   unsigned short iMarker_CfgFile;
   for (iMarker_CfgFile = 0; iMarker_CfgFile < nMarker_CfgFile; iMarker_CfgFile++)
     if (Marker_CfgFile_TagBound[iMarker_CfgFile] == val_marker) break;
   return Marker_CfgFile_Monitoring[iMarker_CfgFile];
 }
 
-unsigned short CConfig::GetMarker_CfgFile_GeoEval(string val_marker) const {
+unsigned short CConfig::GetMarker_CfgFile_GeoEval(const string& val_marker) const {
   unsigned short iMarker_CfgFile;
   for (iMarker_CfgFile = 0; iMarker_CfgFile < nMarker_CfgFile; iMarker_CfgFile++)
     if (Marker_CfgFile_TagBound[iMarker_CfgFile] == val_marker) break;
   return Marker_CfgFile_GeoEval[iMarker_CfgFile];
 }
 
-unsigned short CConfig::GetMarker_CfgFile_Designing(string val_marker) const {
+unsigned short CConfig::GetMarker_CfgFile_Designing(const string& val_marker) const {
   unsigned short iMarker_CfgFile;
   for (iMarker_CfgFile = 0; iMarker_CfgFile < nMarker_CfgFile; iMarker_CfgFile++)
     if (Marker_CfgFile_TagBound[iMarker_CfgFile] == val_marker) break;
   return Marker_CfgFile_Designing[iMarker_CfgFile];
 }
 
-unsigned short CConfig::GetMarker_CfgFile_Plotting(string val_marker) const {
+unsigned short CConfig::GetMarker_CfgFile_Plotting(const string& val_marker) const {
   unsigned short iMarker_CfgFile;
   for (iMarker_CfgFile = 0; iMarker_CfgFile < nMarker_CfgFile; iMarker_CfgFile++)
     if (Marker_CfgFile_TagBound[iMarker_CfgFile] == val_marker) break;
   return Marker_CfgFile_Plotting[iMarker_CfgFile];
 }
 
-unsigned short CConfig::GetMarker_CfgFile_Analyze(string val_marker) const {
+unsigned short CConfig::GetMarker_CfgFile_Analyze(const string& val_marker) const {
   unsigned short iMarker_CfgFile;
   for (iMarker_CfgFile = 0; iMarker_CfgFile < nMarker_CfgFile; iMarker_CfgFile++)
     if (Marker_CfgFile_TagBound[iMarker_CfgFile] == val_marker) break;
   return Marker_CfgFile_Analyze[iMarker_CfgFile];
 }
 
-unsigned short CConfig::GetMarker_CfgFile_ZoneInterface(string val_marker) const {
+unsigned short CConfig::GetMarker_CfgFile_ZoneInterface(const string& val_marker) const {
   unsigned short iMarker_CfgFile;
   for (iMarker_CfgFile = 0; iMarker_CfgFile < nMarker_CfgFile; iMarker_CfgFile++)
     if (Marker_CfgFile_TagBound[iMarker_CfgFile] == val_marker) break;
   return Marker_CfgFile_ZoneInterface[iMarker_CfgFile];
 }
 
-unsigned short CConfig::GetMarker_CfgFile_Turbomachinery(string val_marker) const {
+unsigned short CConfig::GetMarker_CfgFile_Turbomachinery(const string& val_marker) const {
   unsigned short iMarker_CfgFile;
   for (iMarker_CfgFile = 0; iMarker_CfgFile < nMarker_CfgFile; iMarker_CfgFile++)
     if (Marker_CfgFile_TagBound[iMarker_CfgFile] == val_marker) break;
   return Marker_CfgFile_Turbomachinery[iMarker_CfgFile];
 }
 
-unsigned short CConfig::GetMarker_CfgFile_TurbomachineryFlag(string val_marker) const {
+unsigned short CConfig::GetMarker_CfgFile_TurbomachineryFlag(const string& val_marker) const {
   unsigned short iMarker_CfgFile;
   for (iMarker_CfgFile = 0; iMarker_CfgFile < nMarker_CfgFile; iMarker_CfgFile++)
     if (Marker_CfgFile_TagBound[iMarker_CfgFile] == val_marker) break;
   return Marker_CfgFile_TurbomachineryFlag[iMarker_CfgFile];
 }
 
-unsigned short CConfig::GetMarker_CfgFile_MixingPlaneInterface(string val_marker) const {
+unsigned short CConfig::GetMarker_CfgFile_MixingPlaneInterface(const string& val_marker) const {
   unsigned short iMarker_CfgFile;
   for (iMarker_CfgFile = 0; iMarker_CfgFile < nMarker_CfgFile; iMarker_CfgFile++)
     if (Marker_CfgFile_TagBound[iMarker_CfgFile] == val_marker) break;
   return Marker_CfgFile_MixingPlaneInterface[iMarker_CfgFile];
 }
 
-unsigned short CConfig::GetMarker_CfgFile_DV(string val_marker) const {
+unsigned short CConfig::GetMarker_CfgFile_DV(const string& val_marker) const {
   unsigned short iMarker_CfgFile;
   for (iMarker_CfgFile = 0; iMarker_CfgFile < nMarker_CfgFile; iMarker_CfgFile++)
     if (Marker_CfgFile_TagBound[iMarker_CfgFile] == val_marker) break;
   return Marker_CfgFile_DV[iMarker_CfgFile];
 }
 
-unsigned short CConfig::GetMarker_CfgFile_Moving(string val_marker) const {
+unsigned short CConfig::GetMarker_CfgFile_Moving(const string& val_marker) const {
   unsigned short iMarker_CfgFile;
   for (iMarker_CfgFile = 0; iMarker_CfgFile < nMarker_CfgFile; iMarker_CfgFile++)
     if (Marker_CfgFile_TagBound[iMarker_CfgFile] == val_marker) break;
   return Marker_CfgFile_Moving[iMarker_CfgFile];
 }
 
-unsigned short CConfig::GetMarker_CfgFile_Deform_Mesh(string val_marker) const {
+unsigned short CConfig::GetMarker_CfgFile_Deform_Mesh(const string& val_marker) const {
   unsigned short iMarker_CfgFile;
   for (iMarker_CfgFile = 0; iMarker_CfgFile < nMarker_CfgFile; iMarker_CfgFile++)
     if (Marker_CfgFile_TagBound[iMarker_CfgFile] == val_marker) break;
   return Marker_CfgFile_Deform_Mesh[iMarker_CfgFile];
 }
 
-unsigned short CConfig::GetMarker_CfgFile_Deform_Mesh_Sym_Plane(string val_marker) const {
+unsigned short CConfig::GetMarker_CfgFile_Deform_Mesh_Sym_Plane(const string& val_marker) const {
   unsigned short iMarker_CfgFile;
   for (iMarker_CfgFile = 0; iMarker_CfgFile < nMarker_CfgFile; iMarker_CfgFile++)
     if (Marker_CfgFile_TagBound[iMarker_CfgFile] == val_marker) break;
   return Marker_CfgFile_Deform_Mesh_Sym_Plane[iMarker_CfgFile];
 }
 
-unsigned short CConfig::GetMarker_CfgFile_Fluid_Load(string val_marker) const {
+unsigned short CConfig::GetMarker_CfgFile_Fluid_Load(const string& val_marker) const {
   unsigned short iMarker_CfgFile;
   for (iMarker_CfgFile = 0; iMarker_CfgFile < nMarker_CfgFile; iMarker_CfgFile++)
     if (Marker_CfgFile_TagBound[iMarker_CfgFile] == val_marker) break;
   return Marker_CfgFile_Fluid_Load[iMarker_CfgFile];
 }
 
-unsigned short CConfig::GetMarker_CfgFile_PyCustom(string val_marker) const {
+unsigned short CConfig::GetMarker_CfgFile_PyCustom(const string& val_marker) const {
   unsigned short iMarker_CfgFile;
   for (iMarker_CfgFile=0; iMarker_CfgFile < nMarker_CfgFile; iMarker_CfgFile++)
     if (Marker_CfgFile_TagBound[iMarker_CfgFile] == val_marker) break;
   return Marker_CfgFile_PyCustom[iMarker_CfgFile];
 }
 
-unsigned short CConfig::GetMarker_CfgFile_PerBound(string val_marker) const {
+unsigned short CConfig::GetMarker_CfgFile_PerBound(const string& val_marker) const {
   unsigned short iMarker_CfgFile;
   for (iMarker_CfgFile = 0; iMarker_CfgFile < nMarker_CfgFile; iMarker_CfgFile++)
     if (Marker_CfgFile_TagBound[iMarker_CfgFile] == val_marker) break;
   return Marker_CfgFile_PerBound[iMarker_CfgFile];
 }
 
-unsigned short CConfig::GetMarker_ZoneInterface(string val_marker) const {
+unsigned short CConfig::GetMarker_ZoneInterface(const string& val_marker) const {
   unsigned short iMarker_CfgFile;
   for (iMarker_CfgFile = 0; iMarker_CfgFile < nMarker_CfgFile; iMarker_CfgFile++)
     if (Marker_CfgFile_TagBound[iMarker_CfgFile] == val_marker) break;
   return Marker_CfgFile_ZoneInterface[iMarker_CfgFile];
 }
 
-unsigned short CConfig::GetMarker_CfgFile_SobolevBC(string val_marker) const {
+unsigned short CConfig::GetMarker_CfgFile_SobolevBC(const string& val_marker) const {
   unsigned short iMarker_CfgFile;
   for (iMarker_CfgFile = 0; iMarker_CfgFile < nMarker_CfgFile; iMarker_CfgFile++)
     if (Marker_CfgFile_TagBound[iMarker_CfgFile] == val_marker) break;
@@ -7876,8 +7871,8 @@ bool CConfig::GetSolid_Wall(unsigned short iMarker) const {
 
 void CConfig::SetSurface_Movement(unsigned short iMarker, unsigned short kind_movement) {
 
-  unsigned short* new_surface_movement = new unsigned short[nMarker_Moving + 1];
-  string* new_marker_moving = new string[nMarker_Moving+1];
+  auto* new_surface_movement = new unsigned short[nMarker_Moving + 1];
+  auto* new_marker_moving = new string[nMarker_Moving+1];
 
   for (unsigned short iMarker_Moving = 0; iMarker_Moving < nMarker_Moving; iMarker_Moving++){
     new_surface_movement[iMarker_Moving] = Kind_SurfaceMovement[iMarker_Moving];
@@ -7906,7 +7901,7 @@ CConfig::~CConfig() {
 
   /*--- Delete all of the option objects in the global option map ---*/
 
-  for(map<string, COptionBase*>::iterator itr = option_map.begin(); itr != option_map.end(); itr++) {
+  for(auto itr = option_map.begin(); itr != option_map.end(); itr++) {
     delete itr->second;
   }
 
@@ -8116,11 +8111,11 @@ CConfig::~CConfig() {
   delete [] FreeStreamTurboNormal;
 }
 
-string CConfig::GetFilename(string filename, string ext, int timeIter) const {
+string CConfig::GetFilename(string filename, const string& ext, int timeIter) const {
 
   /*--- Remove any extension --- */
 
-  unsigned short lastindex = filename.find_last_of(".");
+  unsigned short lastindex = filename.find_last_of('.');
   filename = filename.substr(0, lastindex);
 
   /*--- Add the extension --- */
@@ -8150,9 +8145,9 @@ string CConfig::GetFilename_Iter(const string& filename_iter, unsigned long curI
   return iter_ss.str();
 }
 
-string CConfig::GetUnsteady_FileName(string val_filename, int val_iter, string ext) const {
+string CConfig::GetUnsteady_FileName(string val_filename, int val_iter, const string& ext) const {
 
-  string UnstExt="", UnstFilename = val_filename;
+  string UnstExt, UnstFilename = std::move(val_filename);
   char buffer[50];
 
   /*--- Check that a positive value iteration is requested (for now). ---*/
@@ -8161,7 +8156,7 @@ string CConfig::GetUnsteady_FileName(string val_filename, int val_iter, string e
     SU2_MPI::Error("Requesting a negative iteration number for the restart file!!", CURRENT_FUNCTION);
   }
 
-  unsigned short lastindex = UnstFilename.find_last_of(".");
+  unsigned short lastindex = UnstFilename.find_last_of('.');
   UnstFilename = UnstFilename.substr(0, lastindex);
 
   /*--- Append iteration number for unsteady cases ---*/
@@ -8181,12 +8176,12 @@ string CConfig::GetUnsteady_FileName(string val_filename, int val_iter, string e
   return UnstFilename;
 }
 
-string CConfig::GetMultizone_FileName(string val_filename, int val_iZone, string ext) const {
+string CConfig::GetMultizone_FileName(string val_filename, int val_iZone, const string& ext) const {
 
-    string multizone_filename = val_filename;
+    string multizone_filename = std::move(val_filename);
     char buffer[50];
 
-    unsigned short lastindex = multizone_filename.find_last_of(".");
+    unsigned short lastindex = multizone_filename.find_last_of('.');
     multizone_filename = multizone_filename.substr(0, lastindex);
 
     if (Multizone_Problem) {
@@ -8198,11 +8193,11 @@ string CConfig::GetMultizone_FileName(string val_filename, int val_iZone, string
     return multizone_filename;
 }
 
-string CConfig::GetMultizone_HistoryFileName(string val_filename, int val_iZone, string ext) const {
+string CConfig::GetMultizone_HistoryFileName(string val_filename, int val_iZone, const string& ext) const {
 
-    string multizone_filename = val_filename;
+    string multizone_filename = std::move(val_filename);
     char buffer[50];
-    unsigned short lastindex = multizone_filename.find_last_of(".");
+    unsigned short lastindex = multizone_filename.find_last_of('.');
     multizone_filename = multizone_filename.substr(0, lastindex);
     if (Multizone_Problem) {
         SPRINTF (buffer, "_%d", SU2_TYPE::Int(val_iZone));
@@ -8212,12 +8207,12 @@ string CConfig::GetMultizone_HistoryFileName(string val_filename, int val_iZone,
     return multizone_filename;
 }
 
-string CConfig::GetMultiInstance_FileName(string val_filename, int val_iInst, string ext) const {
+string CConfig::GetMultiInstance_FileName(string val_filename, int val_iInst, const string& ext) const {
 
-  string multizone_filename = val_filename;
+  string multizone_filename = std::move(val_filename);
   char buffer[50];
 
-  unsigned short lastindex = multizone_filename.find_last_of(".");
+  unsigned short lastindex = multizone_filename.find_last_of('.');
   multizone_filename = multizone_filename.substr(0, lastindex);
   SPRINTF (buffer, "_%d", SU2_TYPE::Int(val_iInst));
   multizone_filename.append(string(buffer));
@@ -8227,10 +8222,10 @@ string CConfig::GetMultiInstance_FileName(string val_filename, int val_iInst, st
 
 string CConfig::GetMultiInstance_HistoryFileName(string val_filename, int val_iInst) const {
 
-  string multizone_filename = val_filename;
+  string multizone_filename = std::move(val_filename);
   char buffer[50];
 
-  unsigned short lastindex = multizone_filename.find_last_of(".");
+  unsigned short lastindex = multizone_filename.find_last_of('.');
   multizone_filename = multizone_filename.substr(0, lastindex);
   SPRINTF (buffer, "_%d", SU2_TYPE::Int(val_iInst));
   multizone_filename.append(string(buffer));
@@ -8240,13 +8235,13 @@ string CConfig::GetMultiInstance_HistoryFileName(string val_filename, int val_iI
 
 string CConfig::GetObjFunc_Extension(string val_filename) const {
 
-  string AdjExt, Filename = val_filename;
+  string AdjExt, Filename = std::move(val_filename);
 
   if (ContinuousAdjoint || DiscreteAdjoint) {
 
     /*--- Remove filename extension (.dat) ---*/
 
-    unsigned short lastindex = Filename.find_last_of(".");
+    unsigned short lastindex = Filename.find_last_of('.');
     Filename = Filename.substr(0, lastindex);
 
     if (nObj==1) {
@@ -8475,28 +8470,28 @@ void CConfig::SetGlobalParam(MAIN_SOLVER val_solver,
   }
 }
 
-const su2double* CConfig::GetPeriodicRotCenter(string val_marker) const {
+const su2double* CConfig::GetPeriodicRotCenter(const string& val_marker) const {
   unsigned short iMarker_PerBound;
   for (iMarker_PerBound = 0; iMarker_PerBound < nMarker_PerBound; iMarker_PerBound++)
     if (Marker_PerBound[iMarker_PerBound] == val_marker) break;
   return Periodic_RotCenter[iMarker_PerBound];
 }
 
-const su2double* CConfig::GetPeriodicRotAngles(string val_marker) const {
+const su2double* CConfig::GetPeriodicRotAngles(const string& val_marker) const {
   unsigned short iMarker_PerBound;
   for (iMarker_PerBound = 0; iMarker_PerBound < nMarker_PerBound; iMarker_PerBound++)
     if (Marker_PerBound[iMarker_PerBound] == val_marker) break;
   return Periodic_RotAngles[iMarker_PerBound];
 }
 
-const su2double* CConfig::GetPeriodicTranslation(string val_marker) const {
+const su2double* CConfig::GetPeriodicTranslation(const string& val_marker) const {
   unsigned short iMarker_PerBound;
   for (iMarker_PerBound = 0; iMarker_PerBound < nMarker_PerBound; iMarker_PerBound++)
     if (Marker_PerBound[iMarker_PerBound] == val_marker) break;
   return Periodic_Translation[iMarker_PerBound];
 }
 
-unsigned short CConfig::GetMarker_Periodic_Donor(string val_marker) const {
+unsigned short CConfig::GetMarker_Periodic_Donor(const string& val_marker) const {
   unsigned short iMarker_PerBound, jMarker_PerBound, kMarker_All;
 
   /*--- Find the marker for this periodic boundary. ---*/
@@ -8514,7 +8509,7 @@ unsigned short CConfig::GetMarker_Periodic_Donor(string val_marker) const {
   return kMarker_All;
 }
 
-su2double CConfig::GetActDisk_NetThrust(string val_marker) const {
+su2double CConfig::GetActDisk_NetThrust(const string& val_marker) const {
   unsigned short iMarker_ActDisk;
   for (iMarker_ActDisk = 0; iMarker_ActDisk < nMarker_ActDiskInlet; iMarker_ActDisk++)
     if ((Marker_ActDiskInlet[iMarker_ActDisk] == val_marker) ||
@@ -8522,7 +8517,7 @@ su2double CConfig::GetActDisk_NetThrust(string val_marker) const {
   return ActDisk_NetThrust[iMarker_ActDisk];
 }
 
-su2double CConfig::GetActDisk_Power(string val_marker) const {
+su2double CConfig::GetActDisk_Power(const string& val_marker) const {
   unsigned short iMarker_ActDisk;
   for (iMarker_ActDisk = 0; iMarker_ActDisk < nMarker_ActDiskInlet; iMarker_ActDisk++)
     if ((Marker_ActDiskInlet[iMarker_ActDisk] == val_marker) ||
@@ -8530,7 +8525,7 @@ su2double CConfig::GetActDisk_Power(string val_marker) const {
   return ActDisk_Power[iMarker_ActDisk];
 }
 
-su2double CConfig::GetActDisk_MassFlow(string val_marker) const {
+su2double CConfig::GetActDisk_MassFlow(const string& val_marker) const {
   unsigned short iMarker_ActDisk;
   for (iMarker_ActDisk = 0; iMarker_ActDisk < nMarker_ActDiskInlet; iMarker_ActDisk++)
     if ((Marker_ActDiskInlet[iMarker_ActDisk] == val_marker) ||
@@ -8538,7 +8533,7 @@ su2double CConfig::GetActDisk_MassFlow(string val_marker) const {
   return ActDisk_MassFlow[iMarker_ActDisk];
 }
 
-su2double CConfig::GetActDisk_Mach(string val_marker) const {
+su2double CConfig::GetActDisk_Mach(const string& val_marker) const {
   unsigned short iMarker_ActDisk;
   for (iMarker_ActDisk = 0; iMarker_ActDisk < nMarker_ActDiskInlet; iMarker_ActDisk++)
     if ((Marker_ActDiskInlet[iMarker_ActDisk] == val_marker) ||
@@ -8546,7 +8541,7 @@ su2double CConfig::GetActDisk_Mach(string val_marker) const {
   return ActDisk_Mach[iMarker_ActDisk];
 }
 
-su2double CConfig::GetActDisk_Force(string val_marker) const {
+su2double CConfig::GetActDisk_Force(const string& val_marker) const {
   unsigned short iMarker_ActDisk;
   for (iMarker_ActDisk = 0; iMarker_ActDisk < nMarker_ActDiskInlet; iMarker_ActDisk++)
     if ((Marker_ActDiskInlet[iMarker_ActDisk] == val_marker) ||
@@ -8554,7 +8549,7 @@ su2double CConfig::GetActDisk_Force(string val_marker) const {
   return ActDisk_Force[iMarker_ActDisk];
 }
 
-su2double CConfig::GetActDisk_BCThrust(string val_marker) const {
+su2double CConfig::GetActDisk_BCThrust(const string& val_marker) const {
   unsigned short iMarker_ActDisk;
   for (iMarker_ActDisk = 0; iMarker_ActDisk < nMarker_ActDiskInlet; iMarker_ActDisk++)
     if ((Marker_ActDiskInlet[iMarker_ActDisk] == val_marker) ||
@@ -8562,7 +8557,7 @@ su2double CConfig::GetActDisk_BCThrust(string val_marker) const {
   return ActDisk_BCThrust[iMarker_ActDisk];
 }
 
-su2double CConfig::GetActDisk_BCThrust_Old(string val_marker) const {
+su2double CConfig::GetActDisk_BCThrust_Old(const string& val_marker) const {
   unsigned short iMarker_ActDisk;
   for (iMarker_ActDisk = 0; iMarker_ActDisk < nMarker_ActDiskInlet; iMarker_ActDisk++)
     if ((Marker_ActDiskInlet[iMarker_ActDisk] == val_marker) ||
@@ -8570,7 +8565,7 @@ su2double CConfig::GetActDisk_BCThrust_Old(string val_marker) const {
   return ActDisk_BCThrust_Old[iMarker_ActDisk];
 }
 
-void CConfig::SetActDisk_BCThrust(string val_marker, su2double val_actdisk_bcthrust) {
+void CConfig::SetActDisk_BCThrust(const string& val_marker, su2double val_actdisk_bcthrust) {
   unsigned short iMarker_ActDisk;
   for (iMarker_ActDisk = 0; iMarker_ActDisk < nMarker_ActDiskInlet; iMarker_ActDisk++)
     if ((Marker_ActDiskInlet[iMarker_ActDisk] == val_marker) ||
@@ -8578,7 +8573,7 @@ void CConfig::SetActDisk_BCThrust(string val_marker, su2double val_actdisk_bcthr
   ActDisk_BCThrust[iMarker_ActDisk] = val_actdisk_bcthrust;
 }
 
-void CConfig::SetActDisk_BCThrust_Old(string val_marker, su2double val_actdisk_bcthrust_old) {
+void CConfig::SetActDisk_BCThrust_Old(const string& val_marker, su2double val_actdisk_bcthrust_old) {
   unsigned short iMarker_ActDisk;
   for (iMarker_ActDisk = 0; iMarker_ActDisk < nMarker_ActDiskInlet; iMarker_ActDisk++)
     if ((Marker_ActDiskInlet[iMarker_ActDisk] == val_marker) ||
@@ -8586,7 +8581,7 @@ void CConfig::SetActDisk_BCThrust_Old(string val_marker, su2double val_actdisk_b
   ActDisk_BCThrust_Old[iMarker_ActDisk] = val_actdisk_bcthrust_old;
 }
 
-su2double CConfig::GetActDisk_Area(string val_marker) const {
+su2double CConfig::GetActDisk_Area(const string& val_marker) const {
   unsigned short iMarker_ActDisk;
   for (iMarker_ActDisk = 0; iMarker_ActDisk < nMarker_ActDiskInlet; iMarker_ActDisk++)
     if ((Marker_ActDiskInlet[iMarker_ActDisk] == val_marker) ||
@@ -8594,7 +8589,7 @@ su2double CConfig::GetActDisk_Area(string val_marker) const {
   return ActDisk_Area[iMarker_ActDisk];
 }
 
-su2double CConfig::GetActDisk_ReverseMassFlow(string val_marker) const {
+su2double CConfig::GetActDisk_ReverseMassFlow(const string& val_marker) const {
   unsigned short iMarker_ActDisk;
   for (iMarker_ActDisk = 0; iMarker_ActDisk < nMarker_ActDiskInlet; iMarker_ActDisk++)
     if ((Marker_ActDiskInlet[iMarker_ActDisk] == val_marker) ||
@@ -8602,7 +8597,7 @@ su2double CConfig::GetActDisk_ReverseMassFlow(string val_marker) const {
   return ActDisk_ReverseMassFlow[iMarker_ActDisk];
 }
 
-su2double CConfig::GetActDisk_PressJump(string val_marker, unsigned short val_value) const {
+su2double CConfig::GetActDisk_PressJump(const string& val_marker, unsigned short val_value) const {
   unsigned short iMarker_ActDisk;
   for (iMarker_ActDisk = 0; iMarker_ActDisk < nMarker_ActDiskInlet; iMarker_ActDisk++)
     if ((Marker_ActDiskInlet[iMarker_ActDisk] == val_marker) ||
@@ -8610,7 +8605,7 @@ su2double CConfig::GetActDisk_PressJump(string val_marker, unsigned short val_va
   return ActDisk_PressJump[iMarker_ActDisk][val_value];
 }
 
-su2double CConfig::GetActDisk_TempJump(string val_marker, unsigned short val_value) const {
+su2double CConfig::GetActDisk_TempJump(const string& val_marker, unsigned short val_value) const {
   unsigned short iMarker_ActDisk;
   for (iMarker_ActDisk = 0; iMarker_ActDisk < nMarker_ActDiskInlet; iMarker_ActDisk++)
     if ((Marker_ActDiskInlet[iMarker_ActDisk] == val_marker) ||
@@ -8618,7 +8613,7 @@ su2double CConfig::GetActDisk_TempJump(string val_marker, unsigned short val_val
   return ActDisk_TempJump[iMarker_ActDisk][val_value];;
 }
 
-su2double CConfig::GetActDisk_Omega(string val_marker, unsigned short val_value) const {
+su2double CConfig::GetActDisk_Omega(const string& val_marker, unsigned short val_value) const {
   unsigned short iMarker_ActDisk;
   for (iMarker_ActDisk = 0; iMarker_ActDisk < nMarker_ActDiskInlet; iMarker_ActDisk++)
     if ((Marker_ActDiskInlet[iMarker_ActDisk] == val_marker) ||
@@ -8626,28 +8621,28 @@ su2double CConfig::GetActDisk_Omega(string val_marker, unsigned short val_value)
   return ActDisk_Omega[iMarker_ActDisk][val_value];;
 }
 
-su2double CConfig::GetOutlet_MassFlow(string val_marker) const {
+su2double CConfig::GetOutlet_MassFlow(const string& val_marker) const {
   unsigned short iMarker_Outlet;
   for (iMarker_Outlet = 0; iMarker_Outlet < nMarker_Outlet; iMarker_Outlet++)
     if ((Marker_Outlet[iMarker_Outlet] == val_marker)) break;
   return Outlet_MassFlow[iMarker_Outlet];
 }
 
-su2double CConfig::GetOutlet_Density(string val_marker) const {
+su2double CConfig::GetOutlet_Density(const string& val_marker) const {
   unsigned short iMarker_Outlet;
   for (iMarker_Outlet = 0; iMarker_Outlet < nMarker_Outlet; iMarker_Outlet++)
     if ((Marker_Outlet[iMarker_Outlet] == val_marker)) break;
   return Outlet_Density[iMarker_Outlet];
 }
 
-su2double CConfig::GetOutlet_Area(string val_marker) const {
+su2double CConfig::GetOutlet_Area(const string& val_marker) const {
   unsigned short iMarker_Outlet;
   for (iMarker_Outlet = 0; iMarker_Outlet < nMarker_Outlet; iMarker_Outlet++)
     if ((Marker_Outlet[iMarker_Outlet] == val_marker)) break;
   return Outlet_Area[iMarker_Outlet];
 }
 
-unsigned short CConfig::GetMarker_CfgFile_ActDiskOutlet(string val_marker) const {
+unsigned short CConfig::GetMarker_CfgFile_ActDiskOutlet(const string& val_marker) const {
   unsigned short iMarker_ActDisk, kMarker_All;
 
   /*--- Find the marker for this actuator disk inlet. ---*/
@@ -8663,7 +8658,7 @@ unsigned short CConfig::GetMarker_CfgFile_ActDiskOutlet(string val_marker) const
   return kMarker_All;
 }
 
-unsigned short CConfig::GetMarker_CfgFile_EngineExhaust(string val_marker) const {
+unsigned short CConfig::GetMarker_CfgFile_EngineExhaust(const string& val_marker) const {
   unsigned short iMarker_Engine, kMarker_All;
 
   /*--- Find the marker for this engine inflow. ---*/
@@ -8736,7 +8731,7 @@ unsigned short CConfig::GetMarker_Deform_Mesh_Sym_Plane(const string& val_marker
   return iMarker;
 }
 
-unsigned short CConfig::GetMarker_Fluid_Load(string val_marker) const {
+unsigned short CConfig::GetMarker_Fluid_Load(const string& val_marker) const {
   unsigned short iMarker_Fluid_Load;
 
   /*--- Find the marker for this interface boundary. ---*/
@@ -8746,7 +8741,7 @@ unsigned short CConfig::GetMarker_Fluid_Load(string val_marker) const {
   return iMarker_Fluid_Load;
 }
 
-unsigned short CConfig::GetMarker_SobolevBC(string val_marker) const {
+unsigned short CConfig::GetMarker_SobolevBC(const string& val_marker) const {
   unsigned short iMarker_Sobolev;
 
   /*--- Find the marker for this moving boundary. ---*/
@@ -8756,91 +8751,91 @@ unsigned short CConfig::GetMarker_SobolevBC(string val_marker) const {
   return iMarker_Sobolev;
 }
 
-su2double CConfig::GetExhaust_Temperature_Target(string val_marker) const {
+su2double CConfig::GetExhaust_Temperature_Target(const string& val_marker) const {
   unsigned short iMarker_EngineExhaust;
   for (iMarker_EngineExhaust = 0; iMarker_EngineExhaust < nMarker_EngineExhaust; iMarker_EngineExhaust++)
     if (Marker_EngineExhaust[iMarker_EngineExhaust] == val_marker) break;
   return Exhaust_Temperature_Target[iMarker_EngineExhaust];
 }
 
-su2double CConfig::GetExhaust_Pressure_Target(string val_marker) const {
+su2double CConfig::GetExhaust_Pressure_Target(const string& val_marker) const {
   unsigned short iMarker_EngineExhaust;
   for (iMarker_EngineExhaust = 0; iMarker_EngineExhaust < nMarker_EngineExhaust; iMarker_EngineExhaust++)
     if (Marker_EngineExhaust[iMarker_EngineExhaust] == val_marker) break;
   return Exhaust_Pressure_Target[iMarker_EngineExhaust];
 }
 
-INLET_TYPE CConfig::GetKind_Inc_Inlet(string val_marker) const {
+INLET_TYPE CConfig::GetKind_Inc_Inlet(const string& val_marker) const {
   unsigned short iMarker_Inlet;
   for (iMarker_Inlet = 0; iMarker_Inlet < nMarker_Inlet; iMarker_Inlet++)
     if (Marker_Inlet[iMarker_Inlet] == val_marker) break;
   return Kind_Inc_Inlet[iMarker_Inlet];
 }
 
-INC_OUTLET_TYPE CConfig::GetKind_Inc_Outlet(string val_marker) const {
+INC_OUTLET_TYPE CConfig::GetKind_Inc_Outlet(const string& val_marker) const {
   unsigned short iMarker_Outlet;
   for (iMarker_Outlet = 0; iMarker_Outlet < nMarker_Outlet; iMarker_Outlet++)
     if (Marker_Outlet[iMarker_Outlet] == val_marker) break;
   return Kind_Inc_Outlet[iMarker_Outlet];
 }
 
-su2double CConfig::GetInlet_Ttotal(string val_marker) const {
+su2double CConfig::GetInlet_Ttotal(const string& val_marker) const {
   unsigned short iMarker_Inlet;
   for (iMarker_Inlet = 0; iMarker_Inlet < nMarker_Inlet; iMarker_Inlet++)
     if (Marker_Inlet[iMarker_Inlet] == val_marker) break;
   return Inlet_Ttotal[iMarker_Inlet];
 }
 
-su2double CConfig::GetInlet_Ptotal(string val_marker) const {
+su2double CConfig::GetInlet_Ptotal(const string& val_marker) const {
   unsigned short iMarker_Inlet;
   for (iMarker_Inlet = 0; iMarker_Inlet < nMarker_Inlet; iMarker_Inlet++)
     if (Marker_Inlet[iMarker_Inlet] == val_marker) break;
   return Inlet_Ptotal[iMarker_Inlet];
 }
 
-void CConfig::SetInlet_Ptotal(su2double val_pressure, string val_marker) {
+void CConfig::SetInlet_Ptotal(su2double val_pressure, const string& val_marker) {
   unsigned short iMarker_Inlet;
   for (iMarker_Inlet = 0; iMarker_Inlet < nMarker_Inlet; iMarker_Inlet++)
     if (Marker_Inlet[iMarker_Inlet] == val_marker)
       Inlet_Ptotal[iMarker_Inlet] = val_pressure;
 }
 
-const su2double* CConfig::GetInlet_FlowDir(string val_marker) const {
+const su2double* CConfig::GetInlet_FlowDir(const string& val_marker) const {
   unsigned short iMarker_Inlet;
   for (iMarker_Inlet = 0; iMarker_Inlet < nMarker_Inlet; iMarker_Inlet++)
     if (Marker_Inlet[iMarker_Inlet] == val_marker) break;
   return Inlet_FlowDir[iMarker_Inlet];
 }
 
-su2double CConfig::GetInlet_Temperature(string val_marker) const {
+su2double CConfig::GetInlet_Temperature(const string& val_marker) const {
   unsigned short iMarker_Supersonic_Inlet;
   for (iMarker_Supersonic_Inlet = 0; iMarker_Supersonic_Inlet < nMarker_Supersonic_Inlet; iMarker_Supersonic_Inlet++)
     if (Marker_Supersonic_Inlet[iMarker_Supersonic_Inlet] == val_marker) break;
   return Inlet_Temperature[iMarker_Supersonic_Inlet];
 }
 
-su2double CConfig::GetInlet_Pressure(string val_marker) const {
+su2double CConfig::GetInlet_Pressure(const string& val_marker) const {
   unsigned short iMarker_Supersonic_Inlet;
   for (iMarker_Supersonic_Inlet = 0; iMarker_Supersonic_Inlet < nMarker_Supersonic_Inlet; iMarker_Supersonic_Inlet++)
     if (Marker_Supersonic_Inlet[iMarker_Supersonic_Inlet] == val_marker) break;
   return Inlet_Pressure[iMarker_Supersonic_Inlet];
 }
 
-const su2double* CConfig::GetInlet_Velocity(string val_marker) const {
+const su2double* CConfig::GetInlet_Velocity(const string& val_marker) const {
   unsigned short iMarker_Supersonic_Inlet;
   for (iMarker_Supersonic_Inlet = 0; iMarker_Supersonic_Inlet < nMarker_Supersonic_Inlet; iMarker_Supersonic_Inlet++)
     if (Marker_Supersonic_Inlet[iMarker_Supersonic_Inlet] == val_marker) break;
   return Inlet_Velocity[iMarker_Supersonic_Inlet];
 }
 
-const su2double* CConfig::GetInlet_SpeciesVal(string val_marker) const {
+const su2double* CConfig::GetInlet_SpeciesVal(const string& val_marker) const {
   unsigned short iMarker_Inlet_Species;
   for (iMarker_Inlet_Species = 0; iMarker_Inlet_Species < nMarker_Inlet_Species; iMarker_Inlet_Species++)
     if (Marker_Inlet_Species[iMarker_Inlet_Species] == val_marker) break;
   return Inlet_SpeciesVal[iMarker_Inlet_Species];
 }
 
-const su2double* CConfig::GetInlet_TurbVal(string val_marker) const {
+const su2double* CConfig::GetInlet_TurbVal(const string& val_marker) const {
   /*--- If Turbulent Inlet is not provided for the marker, return free stream values. ---*/
   for (auto iMarker = 0u; iMarker < nMarker_Inlet_Turb; iMarker++) {
     if (Marker_Inlet_Turb[iMarker] == val_marker) return Inlet_TurbVal[iMarker];
@@ -8852,91 +8847,91 @@ const su2double* CConfig::GetInlet_TurbVal(string val_marker) const {
   }
 }
 
-su2double CConfig::GetOutlet_Pressure(string val_marker) const {
+su2double CConfig::GetOutlet_Pressure(const string& val_marker) const {
   unsigned short iMarker_Outlet;
   for (iMarker_Outlet = 0; iMarker_Outlet < nMarker_Outlet; iMarker_Outlet++)
     if (Marker_Outlet[iMarker_Outlet] == val_marker) break;
   return Outlet_Pressure[iMarker_Outlet];
 }
 
-void CConfig::SetOutlet_Pressure(su2double val_pressure, string val_marker) {
+void CConfig::SetOutlet_Pressure(su2double val_pressure, const string& val_marker) {
   unsigned short iMarker_Outlet;
   for (iMarker_Outlet = 0; iMarker_Outlet < nMarker_Outlet; iMarker_Outlet++)
     if (Marker_Outlet[iMarker_Outlet] == val_marker)
       Outlet_Pressure[iMarker_Outlet] = val_pressure;
 }
 
-su2double CConfig::GetRiemann_Var1(string val_marker) const {
+su2double CConfig::GetRiemann_Var1(const string& val_marker) const {
   unsigned short iMarker_Riemann;
   for (iMarker_Riemann = 0; iMarker_Riemann < nMarker_Riemann; iMarker_Riemann++)
     if (Marker_Riemann[iMarker_Riemann] == val_marker) break;
   return Riemann_Var1[iMarker_Riemann];
 }
 
-su2double CConfig::GetRiemann_Var2(string val_marker) const {
+su2double CConfig::GetRiemann_Var2(const string& val_marker) const {
   unsigned short iMarker_Riemann;
   for (iMarker_Riemann = 0; iMarker_Riemann < nMarker_Riemann; iMarker_Riemann++)
     if (Marker_Riemann[iMarker_Riemann] == val_marker) break;
   return Riemann_Var2[iMarker_Riemann];
 }
 
-const su2double* CConfig::GetRiemann_FlowDir(string val_marker) const {
+const su2double* CConfig::GetRiemann_FlowDir(const string& val_marker) const {
   unsigned short iMarker_Riemann;
   for (iMarker_Riemann = 0; iMarker_Riemann < nMarker_Riemann; iMarker_Riemann++)
     if (Marker_Riemann[iMarker_Riemann] == val_marker) break;
   return Riemann_FlowDir[iMarker_Riemann];
 }
 
-unsigned short CConfig::GetKind_Data_Riemann(string val_marker) const {
+unsigned short CConfig::GetKind_Data_Riemann(const string& val_marker) const {
   unsigned short iMarker_Riemann;
   for (iMarker_Riemann = 0; iMarker_Riemann < nMarker_Riemann; iMarker_Riemann++)
     if (Marker_Riemann[iMarker_Riemann] == val_marker) break;
   return Kind_Data_Riemann[iMarker_Riemann];
 }
 
-su2double CConfig::GetGiles_Var1(string val_marker) const {
+su2double CConfig::GetGiles_Var1(const string& val_marker) const {
   unsigned short iMarker_Giles;
   for (iMarker_Giles = 0; iMarker_Giles < nMarker_Giles; iMarker_Giles++)
     if (Marker_Giles[iMarker_Giles] == val_marker) break;
   return Giles_Var1[iMarker_Giles];
 }
 
-void CConfig::SetGiles_Var1(su2double newVar1, string val_marker) {
+void CConfig::SetGiles_Var1(su2double newVar1, const string& val_marker) {
   unsigned short iMarker_Giles;
   for (iMarker_Giles = 0; iMarker_Giles < nMarker_Giles; iMarker_Giles++)
     if (Marker_Giles[iMarker_Giles] == val_marker) break;
   Giles_Var1[iMarker_Giles] = newVar1;
 }
 
-su2double CConfig::GetGiles_Var2(string val_marker) const {
+su2double CConfig::GetGiles_Var2(const string& val_marker) const {
   unsigned short iMarker_Giles;
   for (iMarker_Giles = 0; iMarker_Giles < nMarker_Giles; iMarker_Giles++)
     if (Marker_Giles[iMarker_Giles] == val_marker) break;
   return Giles_Var2[iMarker_Giles];
 }
 
-su2double CConfig::GetGiles_RelaxFactorAverage(string val_marker) const {
+su2double CConfig::GetGiles_RelaxFactorAverage(const string& val_marker) const {
   unsigned short iMarker_Giles;
   for (iMarker_Giles = 0; iMarker_Giles < nMarker_Giles; iMarker_Giles++)
     if (Marker_Giles[iMarker_Giles] == val_marker) break;
   return RelaxFactorAverage[iMarker_Giles];
 }
 
-su2double CConfig::GetGiles_RelaxFactorFourier(string val_marker) const {
+su2double CConfig::GetGiles_RelaxFactorFourier(const string& val_marker) const {
   unsigned short iMarker_Giles;
   for (iMarker_Giles = 0; iMarker_Giles < nMarker_Giles; iMarker_Giles++)
     if (Marker_Giles[iMarker_Giles] == val_marker) break;
   return RelaxFactorFourier[iMarker_Giles];
 }
 
-const su2double* CConfig::GetGiles_FlowDir(string val_marker) const {
+const su2double* CConfig::GetGiles_FlowDir(const string& val_marker) const {
   unsigned short iMarker_Giles;
   for (iMarker_Giles = 0; iMarker_Giles < nMarker_Giles; iMarker_Giles++)
     if (Marker_Giles[iMarker_Giles] == val_marker) break;
   return Giles_FlowDir[iMarker_Giles];
 }
 
-unsigned short CConfig::GetKind_Data_Giles(string val_marker) const {
+unsigned short CConfig::GetKind_Data_Giles(const string& val_marker) const {
   unsigned short iMarker_Giles;
   for (iMarker_Giles = 0; iMarker_Giles < nMarker_Giles; iMarker_Giles++)
     if (Marker_Giles[iMarker_Giles] == val_marker) break;
@@ -9113,7 +9108,7 @@ void CConfig::SetIncPressureOut_BC(su2double val_pressure) {
 
 }
 
-su2double CConfig::GetIsothermal_Temperature(string val_marker) const {
+su2double CConfig::GetIsothermal_Temperature(const string& val_marker) const {
 
   for (unsigned short iMarker_Isothermal = 0; iMarker_Isothermal < nMarker_Isothermal; iMarker_Isothermal++)
     if (Marker_Isothermal[iMarker_Isothermal] == val_marker)
@@ -9122,7 +9117,7 @@ su2double CConfig::GetIsothermal_Temperature(string val_marker) const {
   return Isothermal_Temperature[0];
 }
 
-su2double CConfig::GetWall_HeatFlux(string val_marker) const {
+su2double CConfig::GetWall_HeatFlux(const string& val_marker) const {
 
   for (unsigned short iMarker_HeatFlux = 0; iMarker_HeatFlux < nMarker_HeatFlux; iMarker_HeatFlux++)
     if (Marker_HeatFlux[iMarker_HeatFlux] == val_marker)
@@ -9131,7 +9126,7 @@ su2double CConfig::GetWall_HeatFlux(string val_marker) const {
   return Heat_Flux[0];
 }
 
-su2double CConfig::GetWall_HeatTransfer_Coefficient(string val_marker) const {
+su2double CConfig::GetWall_HeatTransfer_Coefficient(const string& val_marker) const {
 
   for (unsigned short iMarker_HeatTransfer = 0; iMarker_HeatTransfer < nMarker_HeatTransfer; iMarker_HeatTransfer++)
     if (Marker_HeatTransfer[iMarker_HeatTransfer] == val_marker)
@@ -9140,7 +9135,7 @@ su2double CConfig::GetWall_HeatTransfer_Coefficient(string val_marker) const {
   return HeatTransfer_Coeff[0];
 }
 
-su2double CConfig::GetWall_HeatTransfer_Temperature(string val_marker) const {
+su2double CConfig::GetWall_HeatTransfer_Temperature(const string& val_marker) const {
 
   for (unsigned short iMarker_HeatTransfer = 0; iMarker_HeatTransfer < nMarker_HeatTransfer; iMarker_HeatTransfer++)
     if (Marker_HeatTransfer[iMarker_HeatTransfer] == val_marker)
@@ -9160,7 +9155,7 @@ pair<WALL_TYPE, su2double> CConfig::GetWallRoughnessProperties(const string& val
   return make_pair(roughness > 0 ? WALL_TYPE::ROUGH : WALL_TYPE::SMOOTH, roughness);
 }
 
-WALL_FUNCTIONS CConfig::GetWallFunction_Treatment(string val_marker) const {
+WALL_FUNCTIONS CConfig::GetWallFunction_Treatment(const string& val_marker) const {
 
   WALL_FUNCTIONS WallFunction = WALL_FUNCTIONS::NONE;
 
@@ -9174,7 +9169,7 @@ WALL_FUNCTIONS CConfig::GetWallFunction_Treatment(string val_marker) const {
   return WallFunction;
 }
 
-const unsigned short* CConfig::GetWallFunction_IntInfo(string val_marker) const {
+const unsigned short* CConfig::GetWallFunction_IntInfo(const string& val_marker) const {
   unsigned short *intInfo = nullptr;
 
   for(unsigned short iMarker=0; iMarker<nMarker_WallFunctions; iMarker++) {
@@ -9187,7 +9182,7 @@ const unsigned short* CConfig::GetWallFunction_IntInfo(string val_marker) const
   return intInfo;
 }
 
-const su2double* CConfig::GetWallFunction_DoubleInfo(string val_marker) const {
+const su2double* CConfig::GetWallFunction_DoubleInfo(const string& val_marker) const {
   su2double *doubleInfo = nullptr;
 
   for(unsigned short iMarker=0; iMarker<nMarker_WallFunctions; iMarker++) {
@@ -9200,336 +9195,336 @@ const su2double* CConfig::GetWallFunction_DoubleInfo(string val_marker) const {
   return doubleInfo;
 }
 
-su2double CConfig::GetEngineInflow_Target(string val_marker) const {
+su2double CConfig::GetEngineInflow_Target(const string& val_marker) const {
   unsigned short iMarker_EngineInflow;
   for (iMarker_EngineInflow = 0; iMarker_EngineInflow < nMarker_EngineInflow; iMarker_EngineInflow++)
     if (Marker_EngineInflow[iMarker_EngineInflow] == val_marker) break;
   return EngineInflow_Target[iMarker_EngineInflow];
 }
 
-su2double CConfig::GetInflow_Pressure(string val_marker) const {
+su2double CConfig::GetInflow_Pressure(const string& val_marker) const {
   unsigned short iMarker_EngineInflow;
   for (iMarker_EngineInflow = 0; iMarker_EngineInflow < nMarker_EngineInflow; iMarker_EngineInflow++)
     if (Marker_EngineInflow[iMarker_EngineInflow] == val_marker) break;
   return Inflow_Pressure[iMarker_EngineInflow];
 }
 
-su2double CConfig::GetInflow_MassFlow(string val_marker) const {
+su2double CConfig::GetInflow_MassFlow(const string& val_marker) const {
   unsigned short iMarker_EngineInflow;
   for (iMarker_EngineInflow = 0; iMarker_EngineInflow < nMarker_EngineInflow; iMarker_EngineInflow++)
     if (Marker_EngineInflow[iMarker_EngineInflow] == val_marker) break;
   return Inflow_MassFlow[iMarker_EngineInflow];
 }
 
-su2double CConfig::GetInflow_ReverseMassFlow(string val_marker) const {
+su2double CConfig::GetInflow_ReverseMassFlow(const string& val_marker) const {
   unsigned short iMarker_EngineInflow;
   for (iMarker_EngineInflow = 0; iMarker_EngineInflow < nMarker_EngineInflow; iMarker_EngineInflow++)
     if (Marker_EngineInflow[iMarker_EngineInflow] == val_marker) break;
   return Inflow_ReverseMassFlow[iMarker_EngineInflow];
 }
 
-su2double CConfig::GetInflow_TotalPressure(string val_marker) const {
+su2double CConfig::GetInflow_TotalPressure(const string& val_marker) const {
   unsigned short iMarker_EngineInflow;
   for (iMarker_EngineInflow = 0; iMarker_EngineInflow < nMarker_EngineInflow; iMarker_EngineInflow++)
     if (Marker_EngineInflow[iMarker_EngineInflow] == val_marker) break;
   return Inflow_TotalPressure[iMarker_EngineInflow];
 }
 
-su2double CConfig::GetInflow_Temperature(string val_marker) const {
+su2double CConfig::GetInflow_Temperature(const string& val_marker) const {
   unsigned short iMarker_EngineInflow;
   for (iMarker_EngineInflow = 0; iMarker_EngineInflow < nMarker_EngineInflow; iMarker_EngineInflow++)
     if (Marker_EngineInflow[iMarker_EngineInflow] == val_marker) break;
   return Inflow_Temperature[iMarker_EngineInflow];
 }
 
-su2double CConfig::GetInflow_TotalTemperature(string val_marker) const {
+su2double CConfig::GetInflow_TotalTemperature(const string& val_marker) const {
   unsigned short iMarker_EngineInflow;
   for (iMarker_EngineInflow = 0; iMarker_EngineInflow < nMarker_EngineInflow; iMarker_EngineInflow++)
     if (Marker_EngineInflow[iMarker_EngineInflow] == val_marker) break;
   return Inflow_TotalTemperature[iMarker_EngineInflow];
 }
 
-su2double CConfig::GetInflow_RamDrag(string val_marker) const {
+su2double CConfig::GetInflow_RamDrag(const string& val_marker) const {
   unsigned short iMarker_EngineInflow;
   for (iMarker_EngineInflow = 0; iMarker_EngineInflow < nMarker_EngineInflow; iMarker_EngineInflow++)
     if (Marker_EngineInflow[iMarker_EngineInflow] == val_marker) break;
   return Inflow_RamDrag[iMarker_EngineInflow];
 }
 
-su2double CConfig::GetInflow_Force(string val_marker) const {
+su2double CConfig::GetInflow_Force(const string& val_marker) const {
   unsigned short iMarker_EngineInflow;
   for (iMarker_EngineInflow = 0; iMarker_EngineInflow < nMarker_EngineInflow; iMarker_EngineInflow++)
     if (Marker_EngineInflow[iMarker_EngineInflow] == val_marker) break;
   return Inflow_Force[iMarker_EngineInflow];
 }
 
-su2double CConfig::GetInflow_Power(string val_marker) const {
+su2double CConfig::GetInflow_Power(const string& val_marker) const {
   unsigned short iMarker_EngineInflow;
   for (iMarker_EngineInflow = 0; iMarker_EngineInflow < nMarker_EngineInflow; iMarker_EngineInflow++)
     if (Marker_EngineInflow[iMarker_EngineInflow] == val_marker) break;
   return Inflow_Power[iMarker_EngineInflow];
 }
 
-su2double CConfig::GetInflow_Mach(string val_marker) const {
+su2double CConfig::GetInflow_Mach(const string& val_marker) const {
   unsigned short iMarker_EngineInflow;
   for (iMarker_EngineInflow = 0; iMarker_EngineInflow < nMarker_EngineInflow; iMarker_EngineInflow++)
     if (Marker_EngineInflow[iMarker_EngineInflow] == val_marker) break;
   return Inflow_Mach[iMarker_EngineInflow];
 }
 
-su2double CConfig::GetExhaust_Pressure(string val_marker) const {
+su2double CConfig::GetExhaust_Pressure(const string& val_marker) const {
   unsigned short iMarker_EngineExhaust;
   for (iMarker_EngineExhaust = 0; iMarker_EngineExhaust < nMarker_EngineExhaust; iMarker_EngineExhaust++)
     if (Marker_EngineExhaust[iMarker_EngineExhaust] == val_marker) break;
   return Exhaust_Pressure[iMarker_EngineExhaust];
 }
 
-su2double CConfig::GetExhaust_Temperature(string val_marker) const {
+su2double CConfig::GetExhaust_Temperature(const string& val_marker) const {
   unsigned short iMarker_EngineExhaust;
   for (iMarker_EngineExhaust = 0; iMarker_EngineExhaust < nMarker_EngineExhaust; iMarker_EngineExhaust++)
     if (Marker_EngineExhaust[iMarker_EngineExhaust] == val_marker) break;
   return Exhaust_Temperature[iMarker_EngineExhaust];
 }
 
-su2double CConfig::GetExhaust_MassFlow(string val_marker) const {
+su2double CConfig::GetExhaust_MassFlow(const string& val_marker) const {
   unsigned short iMarker_EngineExhaust;
   for (iMarker_EngineExhaust = 0; iMarker_EngineExhaust < nMarker_EngineExhaust; iMarker_EngineExhaust++)
     if (Marker_EngineExhaust[iMarker_EngineExhaust] == val_marker) break;
   return Exhaust_MassFlow[iMarker_EngineExhaust];
 }
 
-su2double CConfig::GetExhaust_TotalPressure(string val_marker) const {
+su2double CConfig::GetExhaust_TotalPressure(const string& val_marker) const {
   unsigned short iMarker_EngineExhaust;
   for (iMarker_EngineExhaust = 0; iMarker_EngineExhaust < nMarker_EngineExhaust; iMarker_EngineExhaust++)
     if (Marker_EngineExhaust[iMarker_EngineExhaust] == val_marker) break;
   return Exhaust_TotalPressure[iMarker_EngineExhaust];
 }
 
-su2double CConfig::GetExhaust_TotalTemperature(string val_marker) const {
+su2double CConfig::GetExhaust_TotalTemperature(const string& val_marker) const {
   unsigned short iMarker_EngineExhaust;
   for (iMarker_EngineExhaust = 0; iMarker_EngineExhaust < nMarker_EngineExhaust; iMarker_EngineExhaust++)
     if (Marker_EngineExhaust[iMarker_EngineExhaust] == val_marker) break;
   return Exhaust_TotalTemperature[iMarker_EngineExhaust];
 }
 
-su2double CConfig::GetExhaust_GrossThrust(string val_marker) const {
+su2double CConfig::GetExhaust_GrossThrust(const string& val_marker) const {
   unsigned short iMarker_EngineExhaust;
   for (iMarker_EngineExhaust = 0; iMarker_EngineExhaust < nMarker_EngineExhaust; iMarker_EngineExhaust++)
     if (Marker_EngineExhaust[iMarker_EngineExhaust] == val_marker) break;
   return Exhaust_GrossThrust[iMarker_EngineExhaust];
 }
 
-su2double CConfig::GetExhaust_Force(string val_marker) const {
+su2double CConfig::GetExhaust_Force(const string& val_marker) const {
   unsigned short iMarker_EngineExhaust;
   for (iMarker_EngineExhaust = 0; iMarker_EngineExhaust < nMarker_EngineExhaust; iMarker_EngineExhaust++)
     if (Marker_EngineExhaust[iMarker_EngineExhaust] == val_marker) break;
   return Exhaust_Force[iMarker_EngineExhaust];
 }
 
-su2double CConfig::GetExhaust_Power(string val_marker) const {
+su2double CConfig::GetExhaust_Power(const string& val_marker) const {
   unsigned short iMarker_EngineExhaust;
   for (iMarker_EngineExhaust = 0; iMarker_EngineExhaust < nMarker_EngineExhaust; iMarker_EngineExhaust++)
     if (Marker_EngineExhaust[iMarker_EngineExhaust] == val_marker) break;
   return Exhaust_Power[iMarker_EngineExhaust];
 }
 
-su2double CConfig::GetActDiskInlet_Pressure(string val_marker) const {
+su2double CConfig::GetActDiskInlet_Pressure(const string& val_marker) const {
   unsigned short iMarker_ActDiskInlet;
   for (iMarker_ActDiskInlet = 0; iMarker_ActDiskInlet < nMarker_ActDiskInlet; iMarker_ActDiskInlet++)
     if (Marker_ActDiskInlet[iMarker_ActDiskInlet] == val_marker) break;
   return ActDiskInlet_Pressure[iMarker_ActDiskInlet];
 }
 
-su2double CConfig::GetActDiskInlet_TotalPressure(string val_marker) const {
+su2double CConfig::GetActDiskInlet_TotalPressure(const string& val_marker) const {
   unsigned short iMarker_ActDiskInlet;
   for (iMarker_ActDiskInlet = 0; iMarker_ActDiskInlet < nMarker_ActDiskInlet; iMarker_ActDiskInlet++)
     if (Marker_ActDiskInlet[iMarker_ActDiskInlet] == val_marker) break;
   return ActDiskInlet_TotalPressure[iMarker_ActDiskInlet];
 }
 
-su2double CConfig::GetActDiskInlet_RamDrag(string val_marker) const {
+su2double CConfig::GetActDiskInlet_RamDrag(const string& val_marker) const {
   unsigned short iMarker_ActDiskInlet;
   for (iMarker_ActDiskInlet = 0; iMarker_ActDiskInlet < nMarker_ActDiskInlet; iMarker_ActDiskInlet++)
     if (Marker_ActDiskInlet[iMarker_ActDiskInlet] == val_marker) break;
   return ActDiskInlet_RamDrag[iMarker_ActDiskInlet];
 }
 
-su2double CConfig::GetActDiskInlet_Force(string val_marker) const {
+su2double CConfig::GetActDiskInlet_Force(const string& val_marker) const {
   unsigned short iMarker_ActDiskInlet;
   for (iMarker_ActDiskInlet = 0; iMarker_ActDiskInlet < nMarker_ActDiskInlet; iMarker_ActDiskInlet++)
     if (Marker_ActDiskInlet[iMarker_ActDiskInlet] == val_marker) break;
   return ActDiskInlet_Force[iMarker_ActDiskInlet];
 }
 
-su2double CConfig::GetActDiskInlet_Power(string val_marker) const {
+su2double CConfig::GetActDiskInlet_Power(const string& val_marker) const {
   unsigned short iMarker_ActDiskInlet;
   for (iMarker_ActDiskInlet = 0; iMarker_ActDiskInlet < nMarker_ActDiskInlet; iMarker_ActDiskInlet++)
     if (Marker_ActDiskInlet[iMarker_ActDiskInlet] == val_marker) break;
   return ActDiskInlet_Power[iMarker_ActDiskInlet];
 }
 
-su2double CConfig::GetActDiskOutlet_Pressure(string val_marker) const {
+su2double CConfig::GetActDiskOutlet_Pressure(const string& val_marker) const {
   unsigned short iMarker_ActDiskOutlet;
   for (iMarker_ActDiskOutlet = 0; iMarker_ActDiskOutlet < nMarker_ActDiskOutlet; iMarker_ActDiskOutlet++)
     if (Marker_ActDiskOutlet[iMarker_ActDiskOutlet] == val_marker) break;
   return ActDiskOutlet_Pressure[iMarker_ActDiskOutlet];
 }
 
-su2double CConfig::GetActDiskOutlet_TotalPressure(string val_marker) const {
+su2double CConfig::GetActDiskOutlet_TotalPressure(const string& val_marker) const {
   unsigned short iMarker_ActDiskOutlet;
   for (iMarker_ActDiskOutlet = 0; iMarker_ActDiskOutlet < nMarker_ActDiskOutlet; iMarker_ActDiskOutlet++)
     if (Marker_ActDiskOutlet[iMarker_ActDiskOutlet] == val_marker) break;
   return ActDiskOutlet_TotalPressure[iMarker_ActDiskOutlet];
 }
 
-su2double CConfig::GetActDiskOutlet_GrossThrust(string val_marker) const {
+su2double CConfig::GetActDiskOutlet_GrossThrust(const string& val_marker) const {
   unsigned short iMarker_ActDiskOutlet;
   for (iMarker_ActDiskOutlet = 0; iMarker_ActDiskOutlet < nMarker_ActDiskOutlet; iMarker_ActDiskOutlet++)
     if (Marker_ActDiskOutlet[iMarker_ActDiskOutlet] == val_marker) break;
   return ActDiskOutlet_GrossThrust[iMarker_ActDiskOutlet];
 }
 
-su2double CConfig::GetActDiskOutlet_Force(string val_marker) const {
+su2double CConfig::GetActDiskOutlet_Force(const string& val_marker) const {
   unsigned short iMarker_ActDiskOutlet;
   for (iMarker_ActDiskOutlet = 0; iMarker_ActDiskOutlet < nMarker_ActDiskOutlet; iMarker_ActDiskOutlet++)
     if (Marker_ActDiskOutlet[iMarker_ActDiskOutlet] == val_marker) break;
   return ActDiskOutlet_Force[iMarker_ActDiskOutlet];
 }
 
-su2double CConfig::GetActDiskOutlet_Power(string val_marker) const {
+su2double CConfig::GetActDiskOutlet_Power(const string& val_marker) const {
   unsigned short iMarker_ActDiskOutlet;
   for (iMarker_ActDiskOutlet = 0; iMarker_ActDiskOutlet < nMarker_ActDiskOutlet; iMarker_ActDiskOutlet++)
     if (Marker_ActDiskOutlet[iMarker_ActDiskOutlet] == val_marker) break;
   return ActDiskOutlet_Power[iMarker_ActDiskOutlet];
 }
 
-su2double CConfig::GetActDiskInlet_Temperature(string val_marker) const {
+su2double CConfig::GetActDiskInlet_Temperature(const string& val_marker) const {
   unsigned short iMarker_ActDiskInlet;
   for (iMarker_ActDiskInlet = 0; iMarker_ActDiskInlet < nMarker_ActDiskInlet; iMarker_ActDiskInlet++)
     if (Marker_ActDiskInlet[iMarker_ActDiskInlet] == val_marker) break;
   return ActDiskInlet_Temperature[iMarker_ActDiskInlet];
 }
 
-su2double CConfig::GetActDiskInlet_TotalTemperature(string val_marker) const {
+su2double CConfig::GetActDiskInlet_TotalTemperature(const string& val_marker) const {
   unsigned short iMarker_ActDiskInlet;
   for (iMarker_ActDiskInlet = 0; iMarker_ActDiskInlet < nMarker_ActDiskInlet; iMarker_ActDiskInlet++)
     if (Marker_ActDiskInlet[iMarker_ActDiskInlet] == val_marker) break;
   return ActDiskInlet_TotalTemperature[iMarker_ActDiskInlet];
 }
 
-su2double CConfig::GetActDiskOutlet_Temperature(string val_marker) const {
+su2double CConfig::GetActDiskOutlet_Temperature(const string& val_marker) const {
   unsigned short iMarker_ActDiskOutlet;
   for (iMarker_ActDiskOutlet = 0; iMarker_ActDiskOutlet < nMarker_ActDiskOutlet; iMarker_ActDiskOutlet++)
     if (Marker_ActDiskOutlet[iMarker_ActDiskOutlet] == val_marker) break;
   return ActDiskOutlet_Temperature[iMarker_ActDiskOutlet];
 }
 
-su2double CConfig::GetActDiskOutlet_TotalTemperature(string val_marker) const {
+su2double CConfig::GetActDiskOutlet_TotalTemperature(const string& val_marker) const {
   unsigned short iMarker_ActDiskOutlet;
   for (iMarker_ActDiskOutlet = 0; iMarker_ActDiskOutlet < nMarker_ActDiskOutlet; iMarker_ActDiskOutlet++)
     if (Marker_ActDiskOutlet[iMarker_ActDiskOutlet] == val_marker) break;
   return ActDiskOutlet_TotalTemperature[iMarker_ActDiskOutlet];
 }
 
-su2double CConfig::GetActDiskInlet_MassFlow(string val_marker) const {
+su2double CConfig::GetActDiskInlet_MassFlow(const string& val_marker) const {
   unsigned short iMarker_ActDiskInlet;
   for (iMarker_ActDiskInlet = 0; iMarker_ActDiskInlet < nMarker_ActDiskInlet; iMarker_ActDiskInlet++)
     if (Marker_ActDiskInlet[iMarker_ActDiskInlet] == val_marker) break;
   return ActDiskInlet_MassFlow[iMarker_ActDiskInlet];
 }
 
-su2double CConfig::GetActDiskOutlet_MassFlow(string val_marker) const {
+su2double CConfig::GetActDiskOutlet_MassFlow(const string& val_marker) const {
   unsigned short iMarker_ActDiskOutlet;
   for (iMarker_ActDiskOutlet = 0; iMarker_ActDiskOutlet < nMarker_ActDiskOutlet; iMarker_ActDiskOutlet++)
     if (Marker_ActDiskOutlet[iMarker_ActDiskOutlet] == val_marker) break;
   return ActDiskOutlet_MassFlow[iMarker_ActDiskOutlet];
 }
 
-su2double CConfig::GetDispl_Value(string val_marker) const {
+su2double CConfig::GetDispl_Value(const string& val_marker) const {
   unsigned short iMarker_Displacement;
   for (iMarker_Displacement = 0; iMarker_Displacement < nMarker_Displacement; iMarker_Displacement++)
     if (Marker_Displacement[iMarker_Displacement] == val_marker) break;
   return Displ_Value[iMarker_Displacement];
 }
 
-su2double CConfig::GetLoad_Value(string val_marker) const {
+su2double CConfig::GetLoad_Value(const string& val_marker) const {
   unsigned short iMarker_Load;
   for (iMarker_Load = 0; iMarker_Load < nMarker_Load; iMarker_Load++)
     if (Marker_Load[iMarker_Load] == val_marker) break;
   return Load_Value[iMarker_Load];
 }
 
-su2double CConfig::GetDamper_Constant(string val_marker) const {
+su2double CConfig::GetDamper_Constant(const string& val_marker) const {
   unsigned short iMarker_Damper;
   for (iMarker_Damper = 0; iMarker_Damper < nMarker_Damper; iMarker_Damper++)
     if (Marker_Damper[iMarker_Damper] == val_marker) break;
   return Damper_Constant[iMarker_Damper];
 }
 
-su2double CConfig::GetLoad_Dir_Value(string val_marker) const {
+su2double CConfig::GetLoad_Dir_Value(const string& val_marker) const {
   unsigned short iMarker_Load_Dir;
   for (iMarker_Load_Dir = 0; iMarker_Load_Dir < nMarker_Load_Dir; iMarker_Load_Dir++)
     if (Marker_Load_Dir[iMarker_Load_Dir] == val_marker) break;
   return Load_Dir_Value[iMarker_Load_Dir];
 }
 
-su2double CConfig::GetLoad_Dir_Multiplier(string val_marker) const {
+su2double CConfig::GetLoad_Dir_Multiplier(const string& val_marker) const {
   unsigned short iMarker_Load_Dir;
   for (iMarker_Load_Dir = 0; iMarker_Load_Dir < nMarker_Load_Dir; iMarker_Load_Dir++)
     if (Marker_Load_Dir[iMarker_Load_Dir] == val_marker) break;
   return Load_Dir_Multiplier[iMarker_Load_Dir];
 }
 
-su2double CConfig::GetDisp_Dir_Value(string val_marker) const {
+su2double CConfig::GetDisp_Dir_Value(const string& val_marker) const {
   unsigned short iMarker_Disp_Dir;
   for (iMarker_Disp_Dir = 0; iMarker_Disp_Dir < nMarker_Disp_Dir; iMarker_Disp_Dir++)
     if (Marker_Disp_Dir[iMarker_Disp_Dir] == val_marker) break;
   return Disp_Dir_Value[iMarker_Disp_Dir];
 }
 
-su2double CConfig::GetDisp_Dir_Multiplier(string val_marker) const {
+su2double CConfig::GetDisp_Dir_Multiplier(const string& val_marker) const {
   unsigned short iMarker_Disp_Dir;
   for (iMarker_Disp_Dir = 0; iMarker_Disp_Dir < nMarker_Disp_Dir; iMarker_Disp_Dir++)
     if (Marker_Disp_Dir[iMarker_Disp_Dir] == val_marker) break;
   return Disp_Dir_Multiplier[iMarker_Disp_Dir];
 }
 
-const su2double* CConfig::GetLoad_Dir(string val_marker) const {
+const su2double* CConfig::GetLoad_Dir(const string& val_marker) const {
   unsigned short iMarker_Load_Dir;
   for (iMarker_Load_Dir = 0; iMarker_Load_Dir < nMarker_Load_Dir; iMarker_Load_Dir++)
     if (Marker_Load_Dir[iMarker_Load_Dir] == val_marker) break;
   return Load_Dir[iMarker_Load_Dir];
 }
 
-const su2double* CConfig::GetDisp_Dir(string val_marker) const {
+const su2double* CConfig::GetDisp_Dir(const string& val_marker) const {
   unsigned short iMarker_Disp_Dir;
   for (iMarker_Disp_Dir = 0; iMarker_Disp_Dir < nMarker_Disp_Dir; iMarker_Disp_Dir++)
     if (Marker_Disp_Dir[iMarker_Disp_Dir] == val_marker) break;
   return Disp_Dir[iMarker_Disp_Dir];
 }
 
-su2double CConfig::GetLoad_Sine_Amplitude(string val_marker) const {
+su2double CConfig::GetLoad_Sine_Amplitude(const string& val_marker) const {
   unsigned short iMarker_Load_Sine;
   for (iMarker_Load_Sine = 0; iMarker_Load_Sine < nMarker_Load_Sine; iMarker_Load_Sine++)
     if (Marker_Load_Sine[iMarker_Load_Sine] == val_marker) break;
   return Load_Sine_Amplitude[iMarker_Load_Sine];
 }
 
-su2double CConfig::GetLoad_Sine_Frequency(string val_marker) const {
+su2double CConfig::GetLoad_Sine_Frequency(const string& val_marker) const {
   unsigned short iMarker_Load_Sine;
   for (iMarker_Load_Sine = 0; iMarker_Load_Sine < nMarker_Load_Sine; iMarker_Load_Sine++)
     if (Marker_Load_Sine[iMarker_Load_Sine] == val_marker) break;
   return Load_Sine_Frequency[iMarker_Load_Sine];
 }
 
-const su2double* CConfig::GetLoad_Sine_Dir(string val_marker) const {
+const su2double* CConfig::GetLoad_Sine_Dir(const string& val_marker) const {
   unsigned short iMarker_Load_Sine;
   for (iMarker_Load_Sine = 0; iMarker_Load_Sine < nMarker_Load_Sine; iMarker_Load_Sine++)
     if (Marker_Load_Sine[iMarker_Load_Sine] == val_marker) break;
   return Load_Sine_Dir[iMarker_Load_Sine];
 }
 
-su2double CConfig::GetWall_Emissivity(string val_marker) const {
+su2double CConfig::GetWall_Emissivity(const string& val_marker) const {
 
   unsigned short iMarker_Emissivity = 0;
 
@@ -9541,7 +9536,7 @@ su2double CConfig::GetWall_Emissivity(string val_marker) const {
   return Wall_Emissivity[iMarker_Emissivity];
 }
 
-su2double CConfig::GetFlowLoad_Value(string val_marker) const {
+su2double CConfig::GetFlowLoad_Value(const string& val_marker) const {
   unsigned short iMarker_FlowLoad;
   for (iMarker_FlowLoad = 0; iMarker_FlowLoad < nMarker_FlowLoad; iMarker_FlowLoad++)
     if (Marker_FlowLoad[iMarker_FlowLoad] == val_marker) break;
@@ -9570,7 +9565,7 @@ void CConfig::Tick(double *val_start_time) {
 
 }
 
-void CConfig::Tock(double val_start_time, string val_function_name, int val_group_id) {
+void CConfig::Tock(double val_start_time, const string& val_function_name, int val_group_id) {
 
 #ifdef PROFILE
 
@@ -9590,7 +9585,7 @@ void CConfig::Tock(double val_start_time, string val_function_name, int val_grou
 
 }
 
-void CConfig::SetProfilingCSV(void) {
+void CConfig::SetProfilingCSV() {
 
 #ifdef PROFILE
 
@@ -9809,7 +9804,7 @@ void CConfig::GEMM_Tock(double val_start_time, int M, int N, int K) const {
 
 }
 
-void CConfig::GEMMProfilingCSV(void) {
+void CConfig::GEMMProfilingCSV() {
 
 #ifdef PROFILE
 
@@ -10008,11 +10003,11 @@ void CConfig::SetMultizone(const CConfig *driver_config, const CConfig* const* c
     if (config_container[iZone]->GetMultizone_Mesh() != GetMultizone_Mesh()){
       SU2_MPI::Error("Option MULTIZONE_MESH must be the same in all zones.", CURRENT_FUNCTION);
     }
-    if(config_container[iZone]->GetWnd_Cauchy_Crit() == true){
+    if(config_container[iZone]->GetWnd_Cauchy_Crit()){
       SU2_MPI::Error("Option WINDOW_CAUCHY_CRIT must be deactivated for multizone problems.", CURRENT_FUNCTION);
     }
   }
-  if(driver_config->GetWnd_Cauchy_Crit() == true){
+  if(driver_config->GetWnd_Cauchy_Crit()){
     SU2_MPI::Error("Option WINDOW_CAUCHY_CRIT must be deactivated for multizone problems.", CURRENT_FUNCTION);
   }
 
diff --git a/Common/src/adt/CADTElemClass.cpp b/Common/src/adt/CADTElemClass.cpp
index 2c94ba5cbbe..72659d0fad6 100644
--- a/Common/src/adt/CADTElemClass.cpp
+++ b/Common/src/adt/CADTElemClass.cpp
@@ -328,7 +328,7 @@ bool CADTElemClass::DetermineContainingElement_impl(vector<unsigned long>& front
           is empty the entire tree has been traversed and a break can be made
           from the infinite loop. ---*/
     frontLeaves = frontLeavesNew;
-    if (frontLeaves.size() == 0) break;
+    if (frontLeaves.empty()) break;
   }
 
   /* If this point is reached, no element is found that contains the coordinate
@@ -425,7 +425,7 @@ void CADTElemClass::DetermineNearestElement_impl(vector<CBBoxTargetClass>& BBoxT
 
             /* Store this bounding box in BBoxTargets and update the currently
                stored value of the distance squared. */
-            BBoxTargets.push_back(CBBoxTargetClass(kk, posDist2, guarDist2));
+            BBoxTargets.emplace_back(kk, posDist2, guarDist2);
             dist = min(dist, guarDist2);
           }
         } else {
@@ -477,7 +477,7 @@ void CADTElemClass::DetermineNearestElement_impl(vector<CBBoxTargetClass>& BBoxT
           is empty the entire tree has been traversed and a break can be made
           from the infinite loop. ---*/
     frontLeaves = frontLeavesNew;
-    if (frontLeaves.size() == 0) break;
+    if (frontLeaves.empty()) break;
   }
 
   /*----------------------------------------------------------------------------*/
diff --git a/Common/src/adt/CADTPointsOnlyClass.cpp b/Common/src/adt/CADTPointsOnlyClass.cpp
index 0503996c47c..c03e07dafbf 100644
--- a/Common/src/adt/CADTPointsOnlyClass.cpp
+++ b/Common/src/adt/CADTPointsOnlyClass.cpp
@@ -220,7 +220,7 @@ void CADTPointsOnlyClass::DetermineNearestNode_impl(vector<unsigned long>& front
           is empty the entire tree has been traversed and a break can be made
           from the infinite loop. ---*/
     frontLeaves = frontLeavesNew;
-    if (frontLeaves.size() == 0) break;
+    if (frontLeaves.empty()) break;
   }
 
   AD::EndPassive(wasActive);
diff --git a/Common/src/containers/CFileReaderLUT.cpp b/Common/src/containers/CFileReaderLUT.cpp
index 5362a81406f..d71f4e9ee3a 100644
--- a/Common/src/containers/CFileReaderLUT.cpp
+++ b/Common/src/containers/CFileReaderLUT.cpp
@@ -150,7 +150,7 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
       for (unsigned long i = 0; i < n_variables; i++) {
         /*--- grab a single line ---*/
         GetNextNonEmptyLine(file_stream, line);
-        names_var[i] = line.substr(line.find(":") + 1);
+        names_var[i] = line.substr(line.find(':') + 1);
       }
     }
 
@@ -325,7 +325,7 @@ void CFileReaderLUT::ReadRawLUT(const string& file_name) {
 }
 
 void CFileReaderLUT::SkipToFlag(ifstream& file_stream, const string& current_line, const string& flag) const {
-  string next_line = "";
+  string next_line;
 
   /*--- compare current line to flag and return if equal ---*/
   if (current_line.compare(flag) == 0) return;
diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index 8b56e1dd74f..130f53bfc18 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -25,6 +25,8 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
+#include <utility>
+
 #include "../../../Common/include/containers/CLookUpTable.hpp"
 
 #include "../../../Common/include/linear_algebra/blas_structure.hpp"
@@ -32,8 +34,8 @@
 
 using namespace std;
 
-CLookUpTable::CLookUpTable(const string& var_file_name_lut, const string& name_CV1_in, const string& name_CV2_in)
-    : file_name_lut{var_file_name_lut}, name_CV1{name_CV1_in}, name_CV2{name_CV2_in} {
+CLookUpTable::CLookUpTable(const string& var_file_name_lut, string name_CV1_in, string name_CV2_in)
+    : file_name_lut{var_file_name_lut}, name_CV1{std::move(name_CV1_in)}, name_CV2{std::move(name_CV2_in)} {
   rank = SU2_MPI::GetRank();
 
   LoadTableRaw(var_file_name_lut);
@@ -163,7 +165,7 @@ void CLookUpTable::FindTableLimits(const string& name_cv1, const string& name_cv
   }
 
   if (table_dim == 3) {
-    limits_table_z = minmax_element(&z_values_levels[0], &z_values_levels[0] + z_values_levels.cols());
+    limits_table_z = minmax_element(z_values_levels.data(), z_values_levels.data() + z_values_levels.cols());
   }
 }
 
diff --git a/Common/src/containers/CTrapezoidalMap.cpp b/Common/src/containers/CTrapezoidalMap.cpp
index ef415928437..22f45868a8f 100644
--- a/Common/src/containers/CTrapezoidalMap.cpp
+++ b/Common/src/containers/CTrapezoidalMap.cpp
@@ -99,7 +99,7 @@ CTrapezoidalMap::CTrapezoidalMap(const su2double* samples_x, const su2double* sa
        * (vertical edges are automatically discarded) */
       if (((edge_limits_x[i_edge][0] <= band_lower_x) and (edge_limits_x[i_edge][1] >= band_upper_x)) or
           ((edge_limits_x[i_edge][1] <= band_lower_x) and (edge_limits_x[i_edge][0] >= band_upper_x))) {
-        y_edge_at_band_mid[i_band].push_back(make_pair(0.0, 0));
+        y_edge_at_band_mid[i_band].emplace_back(0.0, 0);
 
         x_0 = edge_limits_x[i_edge][0];
         y_0 = edge_limits_y[i_edge][0];
diff --git a/Common/src/fem/fem_cgns_elements.cpp b/Common/src/fem/fem_cgns_elements.cpp
index 4069b164321..876793af42e 100644
--- a/Common/src/fem/fem_cgns_elements.cpp
+++ b/Common/src/fem/fem_cgns_elements.cpp
@@ -84,10 +84,10 @@ void CCGNSElementType::ReadBoundaryConnectivityRange(const int fn, const int iBa
   if (elemType == MIXED) {
     vector<cgsize_t> connCGNSOffsetVec(iEnd - iBeg + 2);
     if (cg_poly_elements_partial_read(fn, iBase, iZone, connID, iBeg, iEnd, connCGNSVec.data(),
-                                      connCGNSOffsetVec.data(), NULL) != CG_OK)
+                                      connCGNSOffsetVec.data(), nullptr) != CG_OK)
       cg_error_exit();
   } else {
-    if (cg_elements_partial_read(fn, iBase, iZone, connID, iBeg, iEnd, connCGNSVec.data(), NULL) != CG_OK)
+    if (cg_elements_partial_read(fn, iBase, iZone, connID, iBeg, iEnd, connCGNSVec.data(), nullptr) != CG_OK)
       cg_error_exit();
   }
 
@@ -167,11 +167,11 @@ void CCGNSElementType::ReadConnectivityRange(const int fn, const int iBase, cons
   if (elemType == MIXED) {
     vector<cgsize_t> connCGNSOffsetVec(iEnd - iBeg + 2);
     if (cg_poly_elements_partial_read(fn, iBase, iZone, connID, iBeg, iEnd, connCGNSVec.data(),
-                                      connCGNSOffsetVec.data(), NULL) != CG_OK)
+                                      connCGNSOffsetVec.data(), nullptr) != CG_OK)
       cg_error_exit();
 
   } else {
-    if (cg_elements_partial_read(fn, iBase, iZone, connID, iBeg, iEnd, connCGNSVec.data(), NULL) != CG_OK)
+    if (cg_elements_partial_read(fn, iBase, iZone, connID, iBeg, iEnd, connCGNSVec.data(), nullptr) != CG_OK)
       cg_error_exit();
   }
 
@@ -320,7 +320,7 @@ unsigned short CCGNSElementType::DetermineElementDimensionMixed(const int fn, co
   /* Read the data of the first element in this section. */
   vector<cgsize_t> buf(sizeNeeded);
   vector<cgsize_t> buf_offset(2, 0);
-  if (cg_poly_elements_partial_read(fn, iBase, iZone, connID, indBeg, indBeg, buf.data(), buf_offset.data(), NULL) !=
+  if (cg_poly_elements_partial_read(fn, iBase, iZone, connID, indBeg, indBeg, buf.data(), buf_offset.data(), nullptr) !=
       CG_OK)
     cg_error_exit();
 
diff --git a/Common/src/fem/fem_gauss_jacobi_quadrature.cpp b/Common/src/fem/fem_gauss_jacobi_quadrature.cpp
index 124a90d166b..d7c3c06d74a 100644
--- a/Common/src/fem/fem_gauss_jacobi_quadrature.cpp
+++ b/Common/src/fem/fem_gauss_jacobi_quadrature.cpp
@@ -83,7 +83,7 @@ void CGaussJacobiQuadrature::GetQuadraturePoints(const passivedouble alpha, cons
                                                  const passivedouble a, const passivedouble b,
                                                  vector<passivedouble>& GJPoints, vector<passivedouble>& GJWeights) {
   /*--- Determine the number of integration points. Check if the number makes sense. ---*/
-  unsigned int nIntPoints = (unsigned int)GJPoints.size();
+  auto nIntPoints = (unsigned int)GJPoints.size();
   if (nIntPoints < 1 || nIntPoints > 100)
     SU2_MPI::Error("Invalid number of Gauss Jacobi integration points", CURRENT_FUNCTION);
 
@@ -176,8 +176,6 @@ void CGaussJacobiQuadrature::cdgqf(int nt, int kind, passivedouble alpha, passiv
 
   delete[] aj;
   delete[] bj;
-
-  return;
 }
 //****************************************************************************80
 
@@ -269,8 +267,6 @@ void CGaussJacobiQuadrature::cgqf(int nt, int kind, passivedouble alpha, passive
 
   delete[] mlt;
   delete[] ndx;
-
-  return;
 }
 //****************************************************************************80
 
@@ -650,7 +646,6 @@ void CGaussJacobiQuadrature::imtqlx(int n, passivedouble d[], passivedouble e[],
       z[k - 1] = p;
     }
   }
-  return;
 }
 //****************************************************************************80
 
@@ -740,7 +735,6 @@ void CGaussJacobiQuadrature::parchk(int kind, int m, passivedouble alpha, passiv
       exit(1);
     }
   }
-  return;
 }
 //****************************************************************************80
 
@@ -1027,7 +1021,6 @@ void CGaussJacobiQuadrature::scqf(int nt, const passivedouble t[], const int mlt
       }
     }
   }
-  return;
 }
 //****************************************************************************80
 
@@ -1111,6 +1104,4 @@ void CGaussJacobiQuadrature::sgqf(int nt, const passivedouble aj[], passivedoubl
   for (i = 0; i < nt; i++) {
     wts[i] = wts[i] * wts[i];
   }
-
-  return;
 }
diff --git a/Common/src/fem/fem_geometry_structure.cpp b/Common/src/fem/fem_geometry_structure.cpp
index 375f7fefd39..e226fc2ce9b 100644
--- a/Common/src/fem/fem_geometry_structure.cpp
+++ b/Common/src/fem/fem_geometry_structure.cpp
@@ -137,10 +137,7 @@ bool CSortFaces::operator()(const CFaceOfElement& f0, const CFaceOfElement& f1)
       } else {
         /* One face is a local face and the other is not. Make sure that
            the local faces are numbered first. */
-        if (face0IsLocal)
-          return true;
-        else
-          return false;
+        return face0IsLocal;
       }
     } else if (elemIDMax0 >= nVolElemTot && elemIDMax1 >= nVolElemTot) {
       /* Both faces are non-matching internal faces. Sort them according to
@@ -345,7 +342,7 @@ CMeshFEM::CMeshFEM(CGeometry* geometry, CConfig* config) {
 
     /*--- Sort nodeIDs in increasing order and remove the double entities. ---*/
     sort(nodeIDs.begin(), nodeIDs.end());
-    vector<long>::iterator lastNodeID = unique(nodeIDs.begin(), nodeIDs.end());
+    auto lastNodeID = unique(nodeIDs.begin(), nodeIDs.end());
     nodeIDs.erase(lastNodeID, nodeIDs.end());
 
     /*--- Add the number of node IDs and the node IDs itself to longSendBuf[i]. ---*/
@@ -564,9 +561,8 @@ CMeshFEM::CMeshFEM(CGeometry* geometry, CConfig* config) {
          the elements with constant and non-constant Jacobians are
          considered the same. */
       if (JacConstant) {
-        const unsigned short orderExactStraight =
-            (unsigned short)ceil(nPolySol * config->GetQuadrature_Factor_Straight());
-        const unsigned short orderExactCurved = (unsigned short)ceil(nPolySol * config->GetQuadrature_Factor_Curved());
+        const auto orderExactStraight = (unsigned short)ceil(nPolySol * config->GetQuadrature_Factor_Straight());
+        const auto orderExactCurved = (unsigned short)ceil(nPolySol * config->GetQuadrature_Factor_Curved());
         if (orderExactStraight == orderExactCurved) JacConstant = false;
       }
 
@@ -594,9 +590,9 @@ CMeshFEM::CMeshFEM(CGeometry* geometry, CConfig* config) {
             if (shortRecvBuf[i][indS + 2]) {
               /* The face is owned by this element. As the neighboring element
                  is not owned, this implies that a halo element must be created. */
-              haloElements.push_back(
-                  CUnsignedLong2T(longRecvBuf[i][indL], shortRecvBuf[i][indS] + 1)); /* The +1, because haloElements */
-            }                                                                        /* are unsigned longs.          */
+              haloElements.emplace_back(longRecvBuf[i][indL],
+                                        shortRecvBuf[i][indS] + 1); /* The +1, because haloElements */
+            }                                                       /* are unsigned longs.          */
             else {
               /* The face is not owned by this element and therefore it is owned
                  by the neighboring element on a different rank. Consequently the
@@ -608,7 +604,7 @@ CMeshFEM::CMeshFEM(CGeometry* geometry, CConfig* config) {
       }
 
       /* Store the required data for this element in ownedElements. */
-      ownedElements.push_back(CReorderElements(globalID, timeLevel, commSol, VTK_Type, nPolySol, JacConstant));
+      ownedElements.emplace_back(globalID, timeLevel, commSol, VTK_Type, nPolySol, JacConstant);
     }
 
     /* Skip the part with the node numbers. */
@@ -632,7 +628,7 @@ CMeshFEM::CMeshFEM(CGeometry* geometry, CConfig* config) {
           /* Check for an external donor. If external, store it in
              haloElements with no periodic transformation. */
           if (!binary_search(globalElemID.begin(), globalElemID.end(), longRecvBuf[i][indL]))
-            haloElements.push_back(CUnsignedLong2T(longRecvBuf[i][indL], 0));
+            haloElements.emplace_back(longRecvBuf[i][indL], 0);
         }
       }
     }
@@ -640,7 +636,7 @@ CMeshFEM::CMeshFEM(CGeometry* geometry, CConfig* config) {
 
   /* Sort the halo elements in increasing order and remove the double entities. */
   sort(haloElements.begin(), haloElements.end());
-  vector<CUnsignedLong2T>::iterator lastHalo = unique(haloElements.begin(), haloElements.end());
+  auto lastHalo = unique(haloElements.begin(), haloElements.end());
   haloElements.erase(lastHalo, haloElements.end());
 
   /* Determine the maximum global time level and possibly reset the number
@@ -885,7 +881,7 @@ CMeshFEM::CMeshFEM(CGeometry* geometry, CConfig* config) {
 
     for (long j = 0; j < nElemBuf; ++j) {
       const long j3 = 3 * j;
-      haloData.push_back(CLong3T(longSecondRecvBuf[i][j3 + 2], longSecondRecvBuf[i][j3], longSecondRecvBuf[i][j3 + 1]));
+      haloData.emplace_back(longSecondRecvBuf[i][j3 + 2], longSecondRecvBuf[i][j3], longSecondRecvBuf[i][j3 + 1]);
     }
 
     /* Release the memory of this receive buffer. */
@@ -1006,7 +1002,7 @@ CMeshFEM::CMeshFEM(CGeometry* geometry, CConfig* config) {
     for (unsigned long j = 0; j < nElemBuf; ++j) {
       const unsigned long elemID = longSecondRecvBuf[i][2 * j];
 
-      map<unsigned long, unsigned long>::iterator MMI = mapGlobalElemIDToInd.find(elemID);
+      auto MMI = mapGlobalElemIDToInd.find(elemID);
       if (MMI == mapGlobalElemIDToInd.end())
         SU2_MPI::Error("Entry not found in mapGlobalElemIDToInd", CURRENT_FUNCTION);
 
@@ -1048,7 +1044,7 @@ CMeshFEM::CMeshFEM(CGeometry* geometry, CConfig* config) {
 
   /* Determine the number of different element types present. */
   map<unsigned short, unsigned short> mapElemTypeToInd;
-  for (vector<CReorderElements>::iterator OEI = ownedElements.begin(); OEI != ownedElements.end(); ++OEI) {
+  for (auto OEI = ownedElements.begin(); OEI != ownedElements.end(); ++OEI) {
     const unsigned short elType = OEI->GetElemType();
 
     if (mapElemTypeToInd.find(elType) == mapElemTypeToInd.end()) {
@@ -1071,7 +1067,7 @@ CMeshFEM::CMeshFEM(CGeometry* geometry, CConfig* config) {
     }
   }
 
-  for (vector<CReorderElements>::iterator OEI = ownedElements.begin(); OEI != ownedElements.end(); ++OEI) {
+  for (auto OEI = ownedElements.begin(); OEI != ownedElements.end(); ++OEI) {
     const unsigned short elType = OEI->GetElemType();
     map<unsigned short, unsigned short>::const_iterator MI = mapElemTypeToInd.find(elType);
     unsigned short ind = MI->second + 1;
@@ -1085,7 +1081,7 @@ CMeshFEM::CMeshFEM(CGeometry* geometry, CConfig* config) {
   /* Loop again over the owned elements and check if elements, which do not
      have to send their solution, should be flagged as such in order to improve
      the gemm performance. */
-  for (vector<CReorderElements>::iterator OEI = ownedElements.begin(); OEI != ownedElements.end(); ++OEI) {
+  for (auto OEI = ownedElements.begin(); OEI != ownedElements.end(); ++OEI) {
     /* Check for an internal element, i.e. an element for which the solution
        does not need to be communicated. */
     if (!OEI->GetCommSolution()) {
@@ -1189,7 +1185,7 @@ CMeshFEM::CMeshFEM(CGeometry* geometry, CConfig* config) {
       unsigned short nDOFsGrid = shortRecvBuf[i][indS + 3];
       unsigned short nFaces = shortRecvBuf[i][indS + 5];
 
-      map<unsigned long, unsigned long>::iterator MMI = mapGlobalElemIDToInd.find(globalID);
+      auto MMI = mapGlobalElemIDToInd.find(globalID);
       unsigned long ind = MMI->second;
 
       indS += 8;
@@ -1246,7 +1242,7 @@ CMeshFEM::CMeshFEM(CGeometry* geometry, CConfig* config) {
 
     /* Start of the Reverse Cuthil McKee renumbering. */
     vector<unsigned long> frontElements(1, indBeg);
-    while (frontElements.size()) {
+    while (!frontElements.empty()) {
       /* Vector, which stores the front for the next round. */
       vector<unsigned long> frontElementsNew;
 
@@ -1337,7 +1333,7 @@ CMeshFEM::CMeshFEM(CGeometry* geometry, CConfig* config) {
     for (long j = 0; j < longRecvBuf[i][0]; ++j) {
       /* Determine the location in volElem where this data must be stored. */
       unsigned long elemID = longRecvBuf[i][indL++];
-      map<unsigned long, unsigned long>::iterator MMI = mapGlobalElemIDToInd.find(elemID);
+      auto MMI = mapGlobalElemIDToInd.find(elemID);
       unsigned long ind = MMI->second;
 
       /* Store the data. */
@@ -1424,7 +1420,7 @@ CMeshFEM::CMeshFEM(CGeometry* geometry, CConfig* config) {
 
   /* Sort meshPoints in increasing order and remove the double entities. */
   sort(meshPoints.begin(), meshPoints.end());
-  vector<CPointFEM>::iterator lastPoint = unique(meshPoints.begin(), meshPoints.end());
+  auto lastPoint = unique(meshPoints.begin(), meshPoints.end());
   meshPoints.erase(lastPoint, meshPoints.end());
 
   /* Clear the contents of the map globalPointIDToLocalInd and fill
@@ -1478,7 +1474,7 @@ CMeshFEM::CMeshFEM(CGeometry* geometry, CConfig* config) {
       const unsigned long j2 = 2 * j;
 
       const unsigned long elemID = longSecondRecvBuf[i][j2];
-      map<unsigned long, unsigned long>::iterator MMI = mapGlobalElemIDToInd.find(elemID);
+      auto MMI = mapGlobalElemIDToInd.find(elemID);
       if (MMI == mapGlobalElemIDToInd.end())
         SU2_MPI::Error("Entry not found in mapGlobalElemIDToInd", CURRENT_FUNCTION);
 
@@ -1526,7 +1522,7 @@ CMeshFEM::CMeshFEM(CGeometry* geometry, CConfig* config) {
 
       for (unsigned short k = 0; k < volElem[indV].nDOFsGrid; ++k) {
         longSendBuf[i].push_back(volElem[indV].nodeIDsGrid[k]);
-        nodeIDs.push_back(CUnsignedLong2T(volElem[indV].nodeIDsGrid[k], elemBuf[j].long1));
+        nodeIDs.emplace_back(volElem[indV].nodeIDsGrid[k], elemBuf[j].long1);
       }
 
       for (unsigned short k = 0; k < volElem[indV].nFaces; ++k)
@@ -1535,7 +1531,7 @@ CMeshFEM::CMeshFEM(CGeometry* geometry, CConfig* config) {
 
     /* Sort nodeIDs in increasing order and remove the double entities. */
     sort(nodeIDs.begin(), nodeIDs.end());
-    vector<CUnsignedLong2T>::iterator lastNodeID = unique(nodeIDs.begin(), nodeIDs.end());
+    auto lastNodeID = unique(nodeIDs.begin(), nodeIDs.end());
     nodeIDs.erase(lastNodeID, nodeIDs.end());
 
     /* Add the number of node IDs and the node IDs itself to longSendBuf[i]
@@ -1662,7 +1658,7 @@ CMeshFEM::CMeshFEM(CGeometry* geometry, CConfig* config) {
 
     for (long j = 0; j < longRecvBuf[i][0]; ++j) {
       const unsigned short nFaces = shortRecvBuf[i][indS + 6];
-      haloElemInfo.push_back(CLong3T(shortRecvBuf[i][indS + 7], sourceRank[i], j));
+      haloElemInfo.emplace_back(shortRecvBuf[i][indS + 7], sourceRank[i], j);
       indS += nFaces + 8;
     }
   }
@@ -2272,7 +2268,7 @@ void CMeshFEM::SetPositive_ZArea(CConfig* config) {
 
 CMeshFEM_DG::CMeshFEM_DG(CGeometry* geometry, CConfig* config) : CMeshFEM(geometry, config) {}
 
-void CMeshFEM_DG::SetGlobal_to_Local_Point(void) {
+void CMeshFEM_DG::SetGlobal_to_Local_Point() {
   Global_to_Local_Point.clear();
   unsigned long ii = 0;
   for (unsigned long i = 0; i < nVolElemOwned; ++i) {
@@ -2282,7 +2278,7 @@ void CMeshFEM_DG::SetGlobal_to_Local_Point(void) {
   }
 }
 
-void CMeshFEM_DG::CoordinatesIntegrationPoints(void) {
+void CMeshFEM_DG::CoordinatesIntegrationPoints() {
   /*--------------------------------------------------------------------*/
   /*--- Step 1: The integration points of the owned volume elements. ---*/
   /*--------------------------------------------------------------------*/
@@ -2386,7 +2382,7 @@ void CMeshFEM_DG::CoordinatesIntegrationPoints(void) {
   }
 }
 
-void CMeshFEM_DG::CoordinatesSolDOFs(void) {
+void CMeshFEM_DG::CoordinatesSolDOFs() {
   /*--- Loop over the owned elements to compute the coordinates
         of the solution DOFs. ---*/
   for (unsigned long l = 0; l < nVolElemOwned; ++l) {
@@ -2457,10 +2453,8 @@ void CMeshFEM_DG::CreateFaces(CConfig* config) {
          is set to false. Hence it is only needed to carry out this check for faces
          with a constant Jacobian. This is done to reduce the number of standard elements. */
       if (thisFace.JacFaceIsConsideredConstant) {
-        unsigned short orderExactStraight =
-            (unsigned short)ceil(thisFace.nPolyGrid0 * config->GetQuadrature_Factor_Straight());
-        unsigned short orderExactCurved =
-            (unsigned short)ceil(thisFace.nPolyGrid0 * config->GetQuadrature_Factor_Curved());
+        auto orderExactStraight = (unsigned short)ceil(thisFace.nPolyGrid0 * config->GetQuadrature_Factor_Straight());
+        auto orderExactCurved = (unsigned short)ceil(thisFace.nPolyGrid0 * config->GetQuadrature_Factor_Curved());
 
         if (orderExactStraight == orderExactCurved) {
           orderExactStraight = (unsigned short)ceil(thisFace.nPolySol0 * config->GetQuadrature_Factor_Straight());
@@ -2894,15 +2888,15 @@ void CMeshFEM_DG::CreateFaces(CConfig* config) {
 
       /* Create the new standard elements if no match was found. */
       if (j == standardMatchingFacesSol.size()) {
-        standardMatchingFacesSol.push_back(CFEMStandardInternalFace(
-            VTK_Type, localFaces[i].elemType0, localFaces[i].nPolySol0, localFaces[i].elemType1,
-            localFaces[i].nPolySol1, localFaces[i].JacFaceIsConsideredConstant, swapFaceInElementSide0,
-            swapFaceInElementSide1, config));
+        standardMatchingFacesSol.emplace_back(VTK_Type, localFaces[i].elemType0, localFaces[i].nPolySol0,
+                                              localFaces[i].elemType1, localFaces[i].nPolySol1,
+                                              localFaces[i].JacFaceIsConsideredConstant, swapFaceInElementSide0,
+                                              swapFaceInElementSide1, config);
 
-        standardMatchingFacesGrid.push_back(CFEMStandardInternalFace(
+        standardMatchingFacesGrid.emplace_back(
             VTK_Type, localFaces[i].elemType0, localFaces[i].nPolyGrid0, localFaces[i].elemType1,
             localFaces[i].nPolyGrid1, localFaces[i].JacFaceIsConsideredConstant, swapFaceInElementSide0,
-            swapFaceInElementSide1, config, standardMatchingFacesSol[j].GetOrderExact()));
+            swapFaceInElementSide1, config, standardMatchingFacesSol[j].GetOrderExact());
         matchingFaces[ii].indStandardElement = j;
       }
 
@@ -3078,13 +3072,12 @@ void CMeshFEM_DG::CreateFaces(CConfig* config) {
 
         /* Create the new standard elements if no match was found. */
         if (j == standardBoundaryFacesSol.size()) {
-          standardBoundaryFacesSol.push_back(
-              CFEMStandardBoundaryFace(VTK_Type, localFaces[i].elemType0, localFaces[i].nPolySol0,
-                                       localFaces[i].JacFaceIsConsideredConstant, swapFaceInElement, config));
+          standardBoundaryFacesSol.emplace_back(VTK_Type, localFaces[i].elemType0, localFaces[i].nPolySol0,
+                                                localFaces[i].JacFaceIsConsideredConstant, swapFaceInElement, config);
 
-          standardBoundaryFacesGrid.push_back(CFEMStandardBoundaryFace(
-              VTK_Type, localFaces[i].elemType0, localFaces[i].nPolyGrid0, localFaces[i].JacFaceIsConsideredConstant,
-              swapFaceInElement, config, standardBoundaryFacesSol[j].GetOrderExact()));
+          standardBoundaryFacesGrid.emplace_back(VTK_Type, localFaces[i].elemType0, localFaces[i].nPolyGrid0,
+                                                 localFaces[i].JacFaceIsConsideredConstant, swapFaceInElement, config,
+                                                 standardBoundaryFacesSol[j].GetOrderExact());
           surfElem[ii].indStandardElement = j;
         }
       }
@@ -3131,13 +3124,13 @@ void CMeshFEM_DG::CreateStandardVolumeElements(CConfig* config) {
 
     /* Create the new standard elements if no match was found. */
     if (j == standardElementsSol.size()) {
-      standardElementsSol.push_back(
-          CFEMStandardElement(volElem[i].VTK_Type, volElem[i].nPolySol, volElem[i].JacIsConsideredConstant, config));
+      standardElementsSol.emplace_back(volElem[i].VTK_Type, volElem[i].nPolySol, volElem[i].JacIsConsideredConstant,
+                                       config);
 
-      standardElementsGrid.push_back(
-          CFEMStandardElement(volElem[i].VTK_Type, volElem[i].nPolyGrid, volElem[i].JacIsConsideredConstant, config,
-                              standardElementsSol[j].GetOrderExact(), standardElementsSol[j].GetRDOFs(),
-                              standardElementsSol[j].GetSDOFs(), standardElementsSol[j].GetTDOFs()));
+      standardElementsGrid.emplace_back(volElem[i].VTK_Type, volElem[i].nPolyGrid, volElem[i].JacIsConsideredConstant,
+                                        config, standardElementsSol[j].GetOrderExact(),
+                                        standardElementsSol[j].GetRDOFs(), standardElementsSol[j].GetSDOFs(),
+                                        standardElementsSol[j].GetTDOFs());
       volElem[i].indStandardElement = j;
     }
   }
@@ -3293,8 +3286,7 @@ void CMeshFEM_DG::SetSendReceive(const CConfig* config) {
 
   /* Store the rotationally periodic indices in rotPerMarkers. */
   rotPerMarkers.reserve(mapRotationalPeriodicToInd.size());
-  for (map<short, unsigned short>::iterator SMI = mapRotationalPeriodicToInd.begin();
-       SMI != mapRotationalPeriodicToInd.end(); ++SMI)
+  for (auto SMI = mapRotationalPeriodicToInd.begin(); SMI != mapRotationalPeriodicToInd.end(); ++SMI)
     rotPerMarkers.push_back(SMI->first);
 
   /* Resize the first index of rotPerHalos to the correct size. */
@@ -4846,7 +4838,7 @@ void CMeshFEM_DG::MetricTermsMatchingFaces(CConfig* config) {
   }
 }
 
-void CMeshFEM_DG::LengthScaleVolumeElements(void) {
+void CMeshFEM_DG::LengthScaleVolumeElements() {
   /* Initialize the length scale of the elements to zero. */
   for (unsigned long i = 0; i < nVolElemTot; ++i) volElem[i].lenScale = 0.0;
 
diff --git a/Common/src/fem/fem_integration_rules.cpp b/Common/src/fem/fem_integration_rules.cpp
index 0335b3f62cc..0766466cad7 100644
--- a/Common/src/fem/fem_integration_rules.cpp
+++ b/Common/src/fem/fem_integration_rules.cpp
@@ -32,7 +32,7 @@
 /*         Private member functions of CFEMStandardElementBase.                     */
 /*----------------------------------------------------------------------------------*/
 
-void CFEMStandardElementBase::IntegrationPointsLine(void) {
+void CFEMStandardElementBase::IntegrationPointsLine() {
   /*--- Allocate the memory for the integration points
         and weights and determine them.                ---*/
   nIntegration = orderExact / 2 + 1;
@@ -42,7 +42,7 @@ void CFEMStandardElementBase::IntegrationPointsLine(void) {
   GaussLegendrePoints1D(rIntegration, wIntegration);
 }
 
-void CFEMStandardElementBase::IntegrationPointsQuadrilateral(void) {
+void CFEMStandardElementBase::IntegrationPointsQuadrilateral() {
   /*--- The 2D quadrature rule is a tensor product of the 1D Gauss-Legendre
         quadrature rule. First determine the number of integration points in 1D,
         which is stored in M, and determine them.                    ---*/
@@ -68,7 +68,7 @@ void CFEMStandardElementBase::IntegrationPointsQuadrilateral(void) {
   }
 }
 
-void CFEMStandardElementBase::IntegrationPointsPrism(void) {
+void CFEMStandardElementBase::IntegrationPointsPrism() {
   /*--- The 3D quadrature rule for a prism is a tensor product of the 1D Gauss-Legendre
         quadrature rule with the triangle quadrature rule. Determine the number of
         integration points in 1D, which is stored in M, and the actual integration
@@ -105,7 +105,7 @@ void CFEMStandardElementBase::IntegrationPointsPrism(void) {
   }
 }
 
-void CFEMStandardElementBase::IntegrationPointsHexahedron(void) {
+void CFEMStandardElementBase::IntegrationPointsHexahedron() {
   /*--- The 3D quadrature rule is a tensor product of the 1D Gauss-Legendre
         quadrature rule. Determine the number of integration points in 1D, which
         is stored in M, and the actual integration 1D integration points. ---*/
@@ -135,7 +135,7 @@ void CFEMStandardElementBase::IntegrationPointsHexahedron(void) {
   }
 }
 
-void CFEMStandardElementBase::IntegrationPointsTriangle(void) {
+void CFEMStandardElementBase::IntegrationPointsTriangle() {
   /*--- Set the number of integration points, depending on the order of
         polynomials that must be integrated exactly. ---*/
   switch (orderExact) {
@@ -5524,7 +5524,7 @@ void CFEMStandardElementBase::IntegrationPointsTriangle(void) {
   }
 }
 
-void CFEMStandardElementBase::IntegrationPointsTetrahedron(void) {
+void CFEMStandardElementBase::IntegrationPointsTetrahedron() {
   /*--- Set the number of integration points, depending on the order of
         polynomials that must be integrated exactly. ---*/
   switch (orderExact) {
@@ -10258,7 +10258,7 @@ void CFEMStandardElementBase::IntegrationPointsTetrahedron(void) {
   }
 }
 
-void CFEMStandardElementBase::IntegrationPointsPyramid(void) {
+void CFEMStandardElementBase::IntegrationPointsPyramid() {
   /*--- The 3D quadrature rule for a pyramid is obtained by transforming the
         standard pyramid into a standard hexahedron by means of the Duffy
         transformation. On the created hexahedron a tensor product rule is used,
diff --git a/Common/src/fem/fem_standard_element.cpp b/Common/src/fem/fem_standard_element.cpp
index 84d0103f699..4ffc791cfad 100644
--- a/Common/src/fem/fem_standard_element.cpp
+++ b/Common/src/fem/fem_standard_element.cpp
@@ -1795,9 +1795,9 @@ CFEMStandardElement::CFEMStandardElement(unsigned short val_VTK_Type, unsigned s
      residual can be computed with one matrix multiplication when the fluxes
      are known. */
   unsigned short nDim;
-  if (dtLagBasisIntegration.size())
+  if (!dtLagBasisIntegration.empty())
     nDim = 3;
-  else if (dsLagBasisIntegration.size())
+  else if (!dsLagBasisIntegration.empty())
     nDim = 2;
   else
     nDim = 1;
@@ -2141,7 +2141,7 @@ void CFEMStandardElement::CreateBasisFunctionsAndMatrixDerivatives(
   for (unsigned long i = 0; i < dtLagBasisLoc.size(); ++i, ++ii) matDerBasis[ii] = dtLagBasisLoc[i];
 }
 
-void CFEMStandardElement::DataStandardLine(void) {
+void CFEMStandardElement::DataStandardLine() {
   /*--- Determine the Lagrangian basis functions and its derivatives
         in the integration points. ---*/
   vector<su2double> matVandermondeInvDummy;
@@ -2163,7 +2163,7 @@ void CFEMStandardElement::DataStandardLine(void) {
   VTK_Type2 = NONE;
 }
 
-void CFEMStandardElement::DataStandardTriangle(void) {
+void CFEMStandardElement::DataStandardTriangle() {
   /*--- Determine the Lagrangian basis functions and its derivatives
         in the integration points. ---*/
   vector<su2double> matVandermondeInvDummy;
@@ -2191,7 +2191,7 @@ void CFEMStandardElement::DataStandardTriangle(void) {
   VTK_Type2 = NONE;
 }
 
-void CFEMStandardElement::DataStandardQuadrilateral(void) {
+void CFEMStandardElement::DataStandardQuadrilateral() {
   /*--- Determine the Lagrangian basis functions and its derivatives
         in the integration points. ---*/
   vector<su2double> matVandermondeInvDummy;
@@ -2223,7 +2223,7 @@ void CFEMStandardElement::DataStandardQuadrilateral(void) {
   VTK_Type2 = NONE;
 }
 
-void CFEMStandardElement::DataStandardTetrahedron(void) {
+void CFEMStandardElement::DataStandardTetrahedron() {
   /*--- Determine the Lagrangian basis functions and its derivatives
         in the integration points. ---*/
   vector<su2double> matVandermondeInvDummy;
@@ -2274,7 +2274,7 @@ void CFEMStandardElement::DataStandardTetrahedron(void) {
   VTK_Type2 = NONE;
 }
 
-void CFEMStandardElement::DataStandardPyramid(void) {
+void CFEMStandardElement::DataStandardPyramid() {
   /*--- Determine the Lagrangian basis functions and its derivatives
         in the integration points. ---*/
   vector<su2double> matVandermondeInvDummy;
@@ -2330,7 +2330,7 @@ void CFEMStandardElement::DataStandardPyramid(void) {
   VTK_Type2 = TETRAHEDRON;
 }
 
-void CFEMStandardElement::DataStandardPrism(void) {
+void CFEMStandardElement::DataStandardPrism() {
   /*--- Determine the Lagrangian basis functions and its derivatives
         in the integration points. ---*/
   vector<su2double> matVandermondeInvDummy;
@@ -2387,7 +2387,7 @@ void CFEMStandardElement::DataStandardPrism(void) {
   VTK_Type2 = NONE;
 }
 
-void CFEMStandardElement::DataStandardHexahedron(void) {
+void CFEMStandardElement::DataStandardHexahedron() {
   /*--- Determine the Lagrangian basis functions and its derivatives
         in the integration points. ---*/
   vector<su2double> matVandermondeInvDummy;
@@ -2447,7 +2447,7 @@ void CFEMStandardElement::DataStandardHexahedron(void) {
   VTK_Type2 = NONE;
 }
 
-void CFEMStandardElement::SubConnTetrahedron(void) {
+void CFEMStandardElement::SubConnTetrahedron() {
   /*--- Initialize the number of DOFs for the current edges to the number of
         DOFs of the edges present in the tetrahedron. Also initialize the
         current k offset to zero.    ---*/
@@ -2639,7 +2639,7 @@ void CFEMStandardElement::SubConnTetrahedron(void) {
   }
 }
 
-void CFEMStandardElement::SubConnPyramid(void) {
+void CFEMStandardElement::SubConnPyramid() {
   /*--- Initialize the number of DOFs for the current edges to the number of
         DOFs of the edges on the base of the pyramid. Also initialize the
         current k offset to zero.     ---*/
@@ -2785,7 +2785,7 @@ void CFEMStandardElement::SubConnPyramid(void) {
   }
 }
 
-void CFEMStandardElement::SubConnPrism(void) {
+void CFEMStandardElement::SubConnPrism() {
   /*--- Determine the number of DOFs for a triangle. This is the offset in
         k-direction, the structured direction of a prisms.    ---*/
   unsigned short nDOFTria = (nPoly + 1) * (nPoly + 2) / 2;
@@ -2853,7 +2853,7 @@ void CFEMStandardElement::SubConnPrism(void) {
   }
 }
 
-void CFEMStandardElement::SubConnHexahedron(void) {
+void CFEMStandardElement::SubConnHexahedron() {
   /*--- Determine the nodal offset in j- and k-direction. ---*/
   unsigned short jOff = nPoly + 1;
   unsigned short kOff = jOff * jOff;
@@ -3371,7 +3371,7 @@ CFEMStandardInternalFace::CFEMStandardInternalFace(unsigned short val_VTK_TypeFa
   /*--- Also create the transpose of the matDerBasisElemIntegrationSide0 and
         matDerBasisElemIntegrationSide1, such that the residual of the
         symmetrizing terms can be computed efficiently. ---*/
-  const unsigned short nDim = dtLagBasisElemIntegrationSide0.size() ? 3 : 2;
+  const unsigned short nDim = !dtLagBasisElemIntegrationSide0.empty() ? 3 : 2;
 
   ii = 0;
   for (unsigned short j = 0; j < nDOFsElemSide0; ++j) {
@@ -3567,7 +3567,7 @@ CFEMStandardBoundaryFace::CFEMStandardBoundaryFace(unsigned short val_VTK_TypeFa
 
   /*--- Also create the transpose of the matDerBasisElemIntegration, such that
         the residual of the symmetrizing terms can be computed efficiently. ---*/
-  const unsigned short nDim = dtLagBasisElemIntegration.size() ? 3 : 2;
+  const unsigned short nDim = !dtLagBasisElemIntegration.empty() ? 3 : 2;
 
   ii = 0;
   for (unsigned short j = 0; j < nDOFsElem; ++j) {
@@ -3580,7 +3580,7 @@ CFEMStandardBoundaryFace::CFEMStandardBoundaryFace(unsigned short val_VTK_TypeFa
   }
 }
 
-unsigned short CFEMStandardBoundaryFace::GetNDOFsPerSubFace(void) const {
+unsigned short CFEMStandardBoundaryFace::GetNDOFsPerSubFace() const {
   /*--- Distinguish between the possible element types for a boundary surface
         and set the number nDOFs for a subface accordingly. ---*/
   unsigned short nDOFsSubface = 0;
diff --git a/Common/src/fem/geometry_structure_fem_part.cpp b/Common/src/fem/geometry_structure_fem_part.cpp
index 3e6853176d8..929abe37abe 100644
--- a/Common/src/fem/geometry_structure_fem_part.cpp
+++ b/Common/src/fem/geometry_structure_fem_part.cpp
@@ -155,7 +155,7 @@ void CFaceOfElement::Copy(const CFaceOfElement& other) {
   elem0IsOwner = other.elem0IsOwner;
 }
 
-void CFaceOfElement::CreateUniqueNumberingWithOrientation(void) {
+void CFaceOfElement::CreateUniqueNumberingWithOrientation() {
   /*--- Determine the element type and create the unique numbering accordingly. ---*/
   bool swapElements = false;
   switch (nCornerPoints) {
@@ -300,7 +300,7 @@ bool CMatchingFace::operator<(const CMatchingFace& other) const {
   return false;
 }
 
-void CMatchingFace::SortFaceCoordinates(void) {
+void CMatchingFace::SortFaceCoordinates() {
   /*--- Determine the tolerance for a matching point for this face. This is
         accomplished by computing the minimum distance between the points of
         the face, multiplied by a relative tolerance.        ---*/
@@ -363,7 +363,7 @@ void CMatchingFace::Copy(const CMatchingFace& other) {
   tolForMatching = other.tolForMatching;
 }
 
-void CPhysicalGeometry::Read_SU2_Format_Parallel_FEM(CConfig* config, string val_mesh_filename,
+void CPhysicalGeometry::Read_SU2_Format_Parallel_FEM(CConfig* config, const string& val_mesh_filename,
                                                      unsigned short val_iZone, unsigned short val_nZone) {
   string text_line, Marker_Tag;
   ifstream mesh_file;
@@ -437,7 +437,7 @@ void CPhysicalGeometry::Read_SU2_Format_Parallel_FEM(CConfig* config, string val
 
     position = text_line.find("NDIME=", 0);
     if (position != string::npos) {
-      if (domain_flag == false) {
+      if (!domain_flag) {
         text_line.erase(0, 6);
         nDim = atoi(text_line.c_str());
         if (rank == MASTER_NODE) {
@@ -682,7 +682,7 @@ void CPhysicalGeometry::Read_SU2_Format_Parallel_FEM(CConfig* config, string val
         text_line.erase(remove(text_line.begin(), text_line.end(), '\r'), text_line.end());
         text_line.erase(remove(text_line.begin(), text_line.end(), '\n'), text_line.end());
 
-        Marker_Tag = text_line.c_str();
+        Marker_Tag = text_line;
 
         /*--- Read the number of elements for this marker. ---*/
         getline(mesh_file, text_line);
@@ -802,7 +802,7 @@ void CPhysicalGeometry::Read_SU2_Format_Parallel_FEM(CConfig* config, string val
   mesh_file.close();
 }
 
-void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig* config, string val_mesh_filename,
+void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig* config, const string& val_mesh_filename,
                                                       unsigned short val_iZone, unsigned short val_nZone) {
 #ifdef HAVE_CGNS
 
@@ -1147,7 +1147,7 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig* config, string va
   for (int i = 0; i < size; ++i) {
     startingIndRanksInNode[i + 1] = startingIndRanksInNode[i] + nodeBuf[i].size();
 
-    if (nodeBuf[i].size()) {
+    if (!nodeBuf[i].empty()) {
       ++nRankSend;
       sendToRank[i] = 1;
     }
@@ -1162,7 +1162,7 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig* config, string va
   vector<SU2_MPI::Request> sendReqs(nRankSend);
   nRankSend = 0;
   for (int i = 0; i < size; ++i) {
-    if (nodeBuf[i].size()) {
+    if (!nodeBuf[i].empty()) {
       SU2_MPI::Isend(nodeBuf[i].data(), nodeBuf[i].size(), MPI_UNSIGNED_LONG, i, i, SU2_MPI::GetComm(),
                      &sendReqs[nRankSend]);
       ++nRankSend;
@@ -1324,7 +1324,7 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig* config, string va
   /*--- Determine the number of messages this rank will send and receive. ---*/
   nRankSend = 0;
   for (int i = 0; i < size; ++i) {
-    if (faceBuf[i].size()) {
+    if (!faceBuf[i].empty()) {
       ++nRankSend;
       sendToRank[i] = 1;
     } else {
@@ -1338,7 +1338,7 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig* config, string va
   sendReqs.resize(nRankSend);
   nRankSend = 0;
   for (int i = 0; i < size; ++i) {
-    if (faceBuf[i].size()) {
+    if (!faceBuf[i].empty()) {
       SU2_MPI::Isend(faceBuf[i].data(), faceBuf[i].size(), MPI_UNSIGNED_LONG, i, i + 4, SU2_MPI::GetComm(),
                      &sendReqs[nRankSend]);
       ++nRankSend;
@@ -1618,7 +1618,7 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig* config, string va
     /*--- Determine the number of messages this rank will send and receive. ---*/
     nRankSend = 0;
     for (int i = 0; i < size; ++i) {
-      if (faceBuf[i].size()) {
+      if (!faceBuf[i].empty()) {
         ++nRankSend;
         sendToRank[i] = 1;
       } else {
@@ -1632,7 +1632,7 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig* config, string va
     sendReqs.resize(nRankSend);
     nRankSend = 0;
     for (int i = 0; i < size; ++i) {
-      if (faceBuf[i].size()) {
+      if (!faceBuf[i].empty()) {
         SU2_MPI::Isend(faceBuf[i].data(), faceBuf[i].size(), MPI_UNSIGNED_LONG, i, i + 5, SU2_MPI::GetComm(),
                        &sendReqs[nRankSend]);
         ++nRankSend;
@@ -1665,9 +1665,9 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig* config, string va
       int ii = 0;
       while (ii < sizeMess) {
         /* Store the data for this boundary element. */
-        const unsigned short VTK_Type = (unsigned short)boundElemRecvBuf[ii++];
-        const unsigned short nPolyGrid = (unsigned short)boundElemRecvBuf[ii++];
-        const unsigned short nDOFsGrid = (unsigned short)boundElemRecvBuf[ii++];
+        const auto VTK_Type = (unsigned short)boundElemRecvBuf[ii++];
+        const auto nPolyGrid = (unsigned short)boundElemRecvBuf[ii++];
+        const auto nDOFsGrid = (unsigned short)boundElemRecvBuf[ii++];
 
         const unsigned long globalBoundElemID = boundElemRecvBuf[ii++];
         const unsigned long* Nodes = boundElemRecvBuf.data() + ii;
@@ -1714,7 +1714,7 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig* config, string va
     /*--- Determine the number of messages this rank will send and receive. ---*/
     nRankSend = 0;
     for (int i = 0; i < size; ++i) {
-      if (nodeBuf[i].size()) {
+      if (!nodeBuf[i].empty()) {
         ++nRankSend;
         sendToRank[i] = 1;
       } else {
@@ -1728,7 +1728,7 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig* config, string va
     sendReqs.resize(nRankSend);
     nRankSend = 0;
     for (int i = 0; i < size; ++i) {
-      if (nodeBuf[i].size()) {
+      if (!nodeBuf[i].empty()) {
         SU2_MPI::Isend(nodeBuf[i].data(), nodeBuf[i].size(), MPI_UNSIGNED_LONG, i, i + 6, SU2_MPI::GetComm(),
                        &sendReqs[nRankSend]);
         ++nRankSend;
@@ -1757,9 +1757,9 @@ void CPhysicalGeometry::Read_CGNS_Format_Parallel_FEM(CConfig* config, string va
       int ii = 0;
       while (ii < sizeMess) {
         /* Store the data for this boundary element. */
-        const unsigned short VTK_Type = (unsigned short)boundElemRecvBuf[ii++];
-        const unsigned short nPolyGrid = (unsigned short)boundElemRecvBuf[ii++];
-        const unsigned short nDOFsGrid = (unsigned short)boundElemRecvBuf[ii++];
+        const auto VTK_Type = (unsigned short)boundElemRecvBuf[ii++];
+        const auto nPolyGrid = (unsigned short)boundElemRecvBuf[ii++];
+        const auto nDOFsGrid = (unsigned short)boundElemRecvBuf[ii++];
 
         const unsigned long globalBoundElemID = boundElemRecvBuf[ii++];
         const unsigned long domainElementID = boundElemRecvBuf[ii++];
@@ -2518,7 +2518,7 @@ void CPhysicalGeometry::SetColorFEMGrid_Parallel(CConfig* config) {
     idx_t numflag = 0;              // C-numbering.
     idx_t ncon = 2;                 // Number of constraints.
     real_t ubvec[] = {1.05, 1.05};  // Tolerances for the vertex weights, recommended value is 1.05.
-    idx_t nparts = (idx_t)size;     // Number of subdomains. Must be number of MPI ranks.
+    auto nparts = (idx_t)size;      // Number of subdomains. Must be number of MPI ranks.
     idx_t options[METIS_NOPTIONS];  // Just use the default options.
     METIS_SetDefaultOptions(options);
     options[1] = 0;
@@ -2781,7 +2781,7 @@ void CPhysicalGeometry::DeterminePeriodicFacesFEMGrid(CConfig* config, vector<CF
         facesDonor.resize(sizeGlobal);
         cS = cL = cD = 0;
 
-        for (vector<CMatchingFace>::iterator fIt = facesDonor.begin(); fIt != facesDonor.end(); ++fIt) {
+        for (auto fIt = facesDonor.begin(); fIt != facesDonor.end(); ++fIt) {
           fIt->nCornerPoints = shortGlobBuf[cS++];
           fIt->nDim = shortGlobBuf[cS++];
           fIt->nPoly = shortGlobBuf[cS++];
@@ -2928,8 +2928,7 @@ void CPhysicalGeometry::DetermineFEMConstantJacobiansAndLenScale(CConfig* config
       if (standardVolumeElements[ii].SameStandardElement(VTK_Type, nPolyGrid, true)) break;
     }
 
-    if (ii == standardVolumeElements.size())
-      standardVolumeElements.push_back(CFEMStandardElement(VTK_Type, nPolyGrid, true, config));
+    if (ii == standardVolumeElements.size()) standardVolumeElements.emplace_back(VTK_Type, nPolyGrid, true, config);
 
     /*--- Allocate the memory for some help vectors to carry out the matrix
           product to determine the derivatives of the coordinates w.r.t.
@@ -3060,8 +3059,7 @@ void CPhysicalGeometry::DetermineFEMConstantJacobiansAndLenScale(CConfig* config
         if (standardFaceElements[jj].SameStandardElement(VTK_Type, nPolyGrid, true)) break;
       }
 
-      if (jj == standardFaceElements.size())
-        standardFaceElements.push_back(CFEMStandardElement(VTK_Type, nPolyGrid, true, config));
+      if (jj == standardFaceElements.size()) standardFaceElements.emplace_back(VTK_Type, nPolyGrid, true, config);
 
       /*--- Set the pointer to store the face connectivity of this face. ---*/
       unsigned short* connFace = nullptr;
@@ -3264,8 +3262,7 @@ void CPhysicalGeometry::DetermineDonorElementsWallFunctions(CConfig* config) {
       if (standardVolumeElements[ii].SameStandardElement(VTK_Parent, nPolyGrid, true)) break;
     }
 
-    if (ii == standardVolumeElements.size())
-      standardVolumeElements.push_back(CFEMStandardElement(VTK_Parent, nPolyGrid, true, config));
+    if (ii == standardVolumeElements.size()) standardVolumeElements.emplace_back(VTK_Parent, nPolyGrid, true, config);
 
     /* Determine the necessary data for splitting the element in its linear
        sub-elements. */
@@ -3434,11 +3431,9 @@ void CPhysicalGeometry::DetermineDonorElementsWallFunctions(CConfig* config) {
             }
 
             if (ii == standardBoundaryFacesSol.size()) {
-              standardBoundaryFacesSol.push_back(
-                  CFEMStandardBoundaryFace(VTK_Type, VTK_Elem, nPolySol, constJac, false, config));
-              standardBoundaryFacesGrid.push_back(
-                  CFEMStandardBoundaryFace(VTK_Type, VTK_Elem, nPolyGrid, constJac, false, config,
-                                           standardBoundaryFacesSol[ii].GetOrderExact()));
+              standardBoundaryFacesSol.emplace_back(VTK_Type, VTK_Elem, nPolySol, constJac, false, config);
+              standardBoundaryFacesGrid.emplace_back(VTK_Type, VTK_Elem, nPolyGrid, constJac, false, config,
+                                                     standardBoundaryFacesSol[ii].GetOrderExact());
             }
 
             /* Get the required information from the standard element. */
@@ -3798,7 +3793,7 @@ void CPhysicalGeometry::DetermineTimeLevelElements(CConfig* config, const vector
 
   /*--- Initialize the time level of external elements to zero.
         First the externals from the faces. ---*/
-  for (vector<CFaceOfElement>::const_iterator FI = localFaces.begin(); FI != localFaces.end(); ++FI) {
+  for (auto FI = localFaces.begin(); FI != localFaces.end(); ++FI) {
     if (FI->elemID1 < Global_nElem) {  // Safeguard against non-matching faces.
 
       if (FI->elemID1 < beg_node[rank] || FI->elemID1 >= beg_node[rank] + nElem) {
@@ -3878,7 +3873,7 @@ void CPhysicalGeometry::DetermineTimeLevelElements(CConfig* config, const vector
   for (int i = 0; i < size; ++i) {
     if (recvFromRank[i]) {
       sort(sendBufAddExternals[i].begin(), sendBufAddExternals[i].end());
-      vector<unsigned long>::iterator lastElem = unique(sendBufAddExternals[i].begin(), sendBufAddExternals[i].end());
+      auto lastElem = unique(sendBufAddExternals[i].begin(), sendBufAddExternals[i].end());
       sendBufAddExternals[i].erase(lastElem, sendBufAddExternals[i].end());
 
       SU2_MPI::Isend(sendBufAddExternals[i].data(), sendBufAddExternals[i].size(), MPI_UNSIGNED_LONG, i, i,
@@ -4070,7 +4065,7 @@ void CPhysicalGeometry::DetermineTimeLevelElements(CConfig* config, const vector
 
   for (int i = 0; i < nRankRecv; ++i, ++MRI) {
     sort(recvElem[i].begin(), recvElem[i].end());
-    vector<unsigned long>::iterator lastElem = unique(recvElem[i].begin(), recvElem[i].end());
+    auto lastElem = unique(recvElem[i].begin(), recvElem[i].end());
     recvElem[i].erase(lastElem, recvElem[i].end());
 
     SU2_MPI::Isend(recvElem[i].data(), recvElem[i].size(), MPI_UNSIGNED_LONG, MRI->first, MRI->first,
@@ -4244,7 +4239,7 @@ void CPhysicalGeometry::DetermineTimeLevelElements(CConfig* config, const vector
 
       /*--- Loop over the matching faces and update the time levels of the
             adjacent elements, if needed. ---*/
-      for (vector<CFaceOfElement>::const_iterator FI = localFaces.begin(); FI != localFaces.end(); ++FI) {
+      for (auto FI = localFaces.begin(); FI != localFaces.end(); ++FI) {
         /* Safeguard against non-matching faces. */
         if (FI->elemID1 < Global_nElem) {
           /* Local element ID of the first element. Per definition this is
@@ -4454,8 +4449,7 @@ void CPhysicalGeometry::ComputeFEMGraphWeights(CConfig* config, const vector<CFa
       if (standardElements[ii].SameStandardElement(VTK_Type, nPolySol, JacIsConstant)) break;
     }
 
-    if (ii == standardElements.size())
-      standardElements.push_back(CFEMStandardElement(VTK_Type, nPolySol, JacIsConstant, config));
+    if (ii == standardElements.size()) standardElements.emplace_back(VTK_Type, nPolySol, JacIsConstant, config);
 
     /* Initialize the computational work for this element, which is stored
        in the 1st vertex weight. */
@@ -4528,9 +4522,8 @@ void CPhysicalGeometry::ComputeFEMGraphWeights(CConfig* config, const vector<CFa
           }
 
           if (ii == standardMatchingFaces.size())
-            standardMatchingFaces.push_back(CFEMStandardInternalFace(VTK_Type_Face, low->elemType0, low->nPolySol0,
-                                                                     low->elemType1, low->nPolySol1, JacIsConstant,
-                                                                     false, false, config));
+            standardMatchingFaces.emplace_back(VTK_Type_Face, low->elemType0, low->nPolySol0, low->elemType1,
+                                               low->nPolySol1, JacIsConstant, false, false, config);
 
           /* Update the computational work for this element, i.e. the 1st
              vertex weight. */
@@ -4547,8 +4540,7 @@ void CPhysicalGeometry::ComputeFEMGraphWeights(CConfig* config, const vector<CFa
         }
 
         if (ii == standardBoundaryFaces.size())
-          standardBoundaryFaces.push_back(
-              CFEMStandardBoundaryFace(VTK_Type_Face, VTK_Type, nPolySol, JacIsConstant, false, config));
+          standardBoundaryFaces.emplace_back(VTK_Type_Face, VTK_Type, nPolySol, JacIsConstant, false, config);
 
         /* Update the computational work for this element, i.e. the 1st
            vertex weight. */
diff --git a/Common/src/geometry/CGeometry.cpp b/Common/src/geometry/CGeometry.cpp
index 8035608ebc9..c678147097b 100644
--- a/Common/src/geometry/CGeometry.cpp
+++ b/Common/src/geometry/CGeometry.cpp
@@ -33,9 +33,9 @@
 #include "../../include/toolboxes/geometry_toolbox.hpp"
 #include "../../include/toolboxes/ndflattener.hpp"
 
-CGeometry::CGeometry(void) : size(SU2_MPI::GetSize()), rank(SU2_MPI::GetRank()) {}
+CGeometry::CGeometry() : size(SU2_MPI::GetSize()), rank(SU2_MPI::GetRank()) {}
 
-CGeometry::~CGeometry(void) {
+CGeometry::~CGeometry() {
   unsigned long iElem, iElem_Bound, iVertex;
   unsigned short iMarker;
 
@@ -940,7 +940,7 @@ void CGeometry::PreprocessPeriodicComms(CGeometry* geometry, CConfig* config) {
    the recv rank can quickly loop through the buffers to unpack the data. ---*/
 
   unsigned short nPackets = 2;
-  unsigned long* idSend = new unsigned long[nPoint_PeriodicSend[nPeriodicSend] * nPackets];
+  auto* idSend = new unsigned long[nPoint_PeriodicSend[nPeriodicSend] * nPackets];
   for (iSend = 0; iSend < nPoint_PeriodicSend[nPeriodicSend] * nPackets; iSend++) idSend[iSend] = 0;
 
   /*--- Build the lists of local index and periodic marker index values. ---*/
@@ -987,7 +987,7 @@ void CGeometry::PreprocessPeriodicComms(CGeometry* geometry, CConfig* config) {
   /*--- Allocate arrays for receiving the periodic point index and marker
    index to the recv rank so that it can store the local values. ---*/
 
-  unsigned long* idRecv = new unsigned long[nPoint_PeriodicRecv[nPeriodicRecv] * nPackets];
+  auto* idRecv = new unsigned long[nPoint_PeriodicRecv[nPeriodicRecv] * nPackets];
   for (iRecv = 0; iRecv < nPoint_PeriodicRecv[nPeriodicRecv] * nPackets; iRecv++) idRecv[iRecv] = 0;
 
 #ifdef HAVE_MPI
@@ -1128,7 +1128,7 @@ void CGeometry::AllocatePeriodicComms(unsigned short countPerPeriodicPoint) {
 }
 
 void CGeometry::PostPeriodicRecvs(CGeometry* geometry, const CConfig* config, unsigned short commType,
-                                  unsigned short countPerPeriodicPoint) {
+                                  unsigned short countPerPeriodicPoint) const {
   /*--- In parallel, communicate the data with non-blocking send/recv. ---*/
 
 #ifdef HAVE_MPI
@@ -1270,7 +1270,7 @@ su2double CGeometry::Point2Plane_Distance(const su2double* Coord, const su2doubl
   return distance;
 }
 
-void CGeometry::SetEdges(void) {
+void CGeometry::SetEdges() {
   nEdge = 0;
   for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
     for (auto iNode = 0u; iNode < nodes->GetnPoint(iPoint); iNode++) {
@@ -1302,7 +1302,7 @@ void CGeometry::SetEdges(void) {
   edges->SetPaddingNodes();
 }
 
-void CGeometry::SetFaces(void) {
+void CGeometry::SetFaces() {
   //  unsigned long iPoint, jPoint, iFace;
   //  unsigned short jNode, iNode;
   //  long TestFace = 0;
@@ -1333,12 +1333,12 @@ void CGeometry::SetFaces(void) {
   //    }
 }
 
-void CGeometry::TestGeometry(void) const {
+void CGeometry::TestGeometry() const {
   ofstream para_file;
 
   para_file.open("test_geometry.dat", ios::out);
 
-  su2double* Normal = new su2double[nDim];
+  auto* Normal = new su2double[nDim];
 
   for (unsigned long iEdge = 0; iEdge < nEdge; iEdge++) {
     para_file << "Edge index: " << iEdge << endl;
@@ -1515,11 +1515,7 @@ bool CGeometry::SegmentIntersectsLine(const su2double point0[2], const su2double
 
   length = diff0_A * diff0_A + diff1_A * diff1_A;
 
-  if ((dist0 > length) || (dist1 > length)) {
-    return false;
-  }
-
-  return true;
+  return !((dist0 > length) || (dist1 > length));
 }
 
 bool CGeometry::SegmentIntersectsTriangle(su2double point0[3], const su2double point1[3], su2double vert0[3],
@@ -1618,7 +1614,7 @@ void CGeometry::ComputeAirfoil_Section(su2double* Plane_P0, su2double* Plane_Nor
   /*--- Grid movement is stored using a vertices information,
    we should go from vertex to points ---*/
 
-  if (original_surface == false) {
+  if (!original_surface) {
     Coord_Variation = new su2double*[nPoint];
     for (iPoint = 0; iPoint < nPoint; iPoint++) Coord_Variation[iPoint] = new su2double[nDim];
 
@@ -1722,7 +1718,7 @@ void CGeometry::ComputeAirfoil_Section(su2double* Plane_P0, su2double* Plane_Nor
             Variable_P1 = 0.0;
 
             for (iDim = 0; iDim < nDim; iDim++) {
-              if (original_surface == true) {
+              if (original_surface) {
                 Segment_P0[iDim] = nodes->GetCoord(iPoint, iDim);
                 Segment_P1[iDim] = nodes->GetCoord(jPoint, iDim);
               } else {
@@ -1759,7 +1755,7 @@ void CGeometry::ComputeAirfoil_Section(su2double* Plane_P0, su2double* Plane_Nor
             else if (nDim == 3) {
               intersect = SegmentIntersectsPlane(Segment_P0, Segment_P1, Variable_P0, Variable_P1, Plane_P0,
                                                  Plane_Normal, Intersection, Variable_Interp);
-              if (intersect == true) {
+              if (intersect) {
                 if (PointIndex == 0) {
                   Xcoord_Index0.push_back(Intersection[0]);
                   Ycoord_Index0.push_back(Intersection[1]);
@@ -1785,7 +1781,7 @@ void CGeometry::ComputeAirfoil_Section(su2double* Plane_P0, su2double* Plane_Nor
     }
   }
 
-  if (original_surface == false) {
+  if (!original_surface) {
     for (iPoint = 0; iPoint < nPoint; iPoint++) delete[] Coord_Variation[iPoint];
     delete[] Coord_Variation;
   }
@@ -1894,7 +1890,7 @@ void CGeometry::ComputeAirfoil_Section(su2double* Plane_P0, su2double* Plane_Nor
 
 #endif
 
-  if ((rank == MASTER_NODE) && (Xcoord_Index0.size() != 0)) {
+  if ((rank == MASTER_NODE) && (!Xcoord_Index0.empty())) {
     /*--- Remove singular edges ---*/
 
     bool Remove;
@@ -1925,7 +1921,7 @@ void CGeometry::ComputeAirfoil_Section(su2double* Plane_P0, su2double* Plane_Nor
         }
         if (Remove) break;
       }
-    } while (Remove == true);
+    } while (Remove);
 
     /*--- Remove repeated edges computing distance, this could happend because the MPI ---*/
 
@@ -1993,7 +1989,7 @@ void CGeometry::ComputeAirfoil_Section(su2double* Plane_P0, su2double* Plane_Nor
         if (Remove) break;
       }
 
-    } while (Remove == true);
+    } while (Remove);
 
     if (Xcoord_Index0.size() != 1) {
       /*--- Rotate from the Y-Z plane to the X-Z plane to reuse the rest of subroutines  ---*/
@@ -2322,7 +2318,7 @@ void CGeometry::ComputeAirfoil_Section(su2double* Plane_P0, su2double* Plane_Nor
           break;
         }
 
-      } while (Xcoord_Index0.size() != 0);
+      } while (!Xcoord_Index0.empty());
 
       /*--- Clean the vector before using them again for storing the upper or the lower side ---*/
 
@@ -2525,7 +2521,7 @@ void CGeometry::ComputeSurf_Straightness(CConfig* config, bool print_on_screen)
           RefUnitNormal_defined = false;
           iVertex = 0;
 
-          while (bound_is_straight[iMarker] == true && iVertex < nVertex[iMarker]) {
+          while (bound_is_straight[iMarker] && iVertex < nVertex[iMarker]) {
             vertex[iMarker][iVertex]->GetNormal(Normal.data());
             UnitNormal = Normal;
 
@@ -2595,7 +2591,7 @@ void CGeometry::ComputeSurf_Straightness(CConfig* config, bool print_on_screen)
         if (config->GetMarker_CfgFile_KindBC(config->GetMarker_CfgFile_TagBound(iMarker_Global)) == SYMMETRY_PLANE ||
             config->GetMarker_CfgFile_KindBC(config->GetMarker_CfgFile_TagBound(iMarker_Global)) == EULER_WALL) {
           cout << "Boundary marker " << config->GetMarker_CfgFile_TagBound(iMarker_Global) << " is";
-          if (Buff_Recv_isStraight[iMarker_Global] == false) cout << " NOT";
+          if (!static_cast<bool>(Buff_Recv_isStraight[iMarker_Global])) cout << " NOT";
           if (nDim == 2) cout << " a single straight." << endl;
           if (nDim == 3) cout << " a single plane." << endl;
         }  // if sym or euler
@@ -2604,7 +2600,7 @@ void CGeometry::ComputeSurf_Straightness(CConfig* config, bool print_on_screen)
   }        // if print_on_scren
 }
 
-void CGeometry::ComputeSurf_Curvature(CConfig* config) {
+void CGeometry::ComputeSurf_Curvature(CConfig* config) const {
   unsigned short iMarker, iNeigh_Point, iDim, iNode, iNeighbor_Nodes, Neighbor_Node;
   unsigned long Neighbor_Point, iVertex, iPoint, jPoint, iElem_Bound, iEdge, nLocalVertex, MaxLocalVertex,
       *Buffer_Send_nVertex, *Buffer_Receive_nVertex, TotalnPointDomain;
@@ -3004,14 +3000,14 @@ void CGeometry::FilterValuesAtElementCG(const vector<su2double>& filter_radius,
   GetGlobalElementAdjacencyMatrix(neighbour_start, neighbour_idx);
 
   /*--- Element centroids and volumes. ---*/
-  su2double *cg_elem = new su2double[Global_nElemDomain * nDim], *vol_elem = new su2double[Global_nElemDomain];
+  auto *cg_elem = new su2double[Global_nElemDomain * nDim], *vol_elem = new su2double[Global_nElemDomain];
 #ifdef HAVE_MPI
   /*--- Number of subdomain each point is part of. ---*/
   vector<char> halo_detect(Global_nElemDomain);
 #endif
 
   /*--- Inputs of a filter stage, like with CG and volumes, each processor needs to see everything. ---*/
-  su2double* work_values = new su2double[Global_nElemDomain];
+  auto* work_values = new su2double[Global_nElemDomain];
 
   /*--- When gathering the neighborhood of each element we use a vector of booleans to indicate
   whether an element is already added to the list of neighbors (one vector per thread). ---*/
@@ -3052,7 +3048,7 @@ void CGeometry::FilterValuesAtElementCG(const vector<su2double>& filter_radius,
 
     /*--- Share with all processors ---*/
     BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
-      su2double* dbl_buffer = new su2double[Global_nElemDomain * nDim];
+      auto* dbl_buffer = new su2double[Global_nElemDomain * nDim];
       SU2_MPI::Allreduce(cg_elem, dbl_buffer, Global_nElemDomain * nDim, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
       swap(dbl_buffer, cg_elem);
       delete[] dbl_buffer;
@@ -3102,7 +3098,7 @@ void CGeometry::FilterValuesAtElementCG(const vector<su2double>& filter_radius,
 #ifdef HAVE_MPI
       /*--- Share with all processors ---*/
       BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
-        su2double* buffer = new su2double[Global_nElemDomain];
+        auto* buffer = new su2double[Global_nElemDomain];
         SU2_MPI::Allreduce(work_values, buffer, Global_nElemDomain, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
         swap(buffer, work_values);
         delete[] buffer;
@@ -3217,7 +3213,7 @@ void CGeometry::GetGlobalElementAdjacencyMatrix(vector<unsigned long>& neighbour
 
   /*--- Determine how much space we need for the adjacency matrix by counting the
   neighbours of each element, i.e. its number of faces---*/
-  unsigned short* nFaces_elem = new unsigned short[Global_nElemDomain];
+  auto* nFaces_elem = new unsigned short[Global_nElemDomain];
 
   SU2_OMP_PARALLEL {
     SU2_OMP_FOR_STAT(256)
@@ -3235,7 +3231,7 @@ void CGeometry::GetGlobalElementAdjacencyMatrix(vector<unsigned long>& neighbour
 #ifdef HAVE_MPI
   /*--- Share with all processors ---*/
   {
-    unsigned short* buffer = new unsigned short[Global_nElemDomain];
+    auto* buffer = new unsigned short[Global_nElemDomain];
     MPI_Allreduce(nFaces_elem, buffer, Global_nElemDomain, MPI_UNSIGNED_SHORT, MPI_MAX, SU2_MPI::GetComm());
     /*--- swap pointers and delete old data to keep the same variable name after reduction ---*/
     swap(buffer, nFaces_elem);
@@ -3356,7 +3352,7 @@ bool CGeometry::GetRadialNeighbourhood(const unsigned long iElem_global, const p
   return finished;
 }
 
-void CGeometry::SetElemVolume() {
+void CGeometry::SetElemVolume() const {
   SU2_OMP_PARALLEL {
     /*--- Create a bank of elements to avoid instantiating inside loop. ---*/
     CElement* elements[4] = {nullptr, nullptr, nullptr, nullptr};
@@ -3424,7 +3420,7 @@ void CGeometry::SetElemVolume() {
   END_SU2_OMP_PARALLEL
 }
 
-void CGeometry::SetRotationalVelocity(const CConfig* config, bool print) {
+void CGeometry::SetRotationalVelocity(const CConfig* config, bool print) const {
   unsigned long iPoint;
   unsigned short iDim;
 
@@ -3475,7 +3471,7 @@ void CGeometry::SetRotationalVelocity(const CConfig* config, bool print) {
   }
 }
 
-void CGeometry::SetShroudVelocity(const CConfig* config) {
+void CGeometry::SetShroudVelocity(const CConfig* config) const {
   unsigned long iPoint, iVertex;
   unsigned short iMarker, iMarkerShroud;
   su2double RotVel[3] = {0.0, 0.0, 0.0};
@@ -3493,7 +3489,7 @@ void CGeometry::SetShroudVelocity(const CConfig* config) {
   }
 }
 
-void CGeometry::SetTranslationalVelocity(const CConfig* config, bool print) {
+void CGeometry::SetTranslationalVelocity(const CConfig* config, bool print) const {
   su2double xDot[3] = {0.0, 0.0, 0.0};
 
   /*--- Get the translational velocity vector from config ---*/
@@ -3512,7 +3508,7 @@ void CGeometry::SetTranslationalVelocity(const CConfig* config, bool print) {
   for (unsigned long iPoint = 0; iPoint < nPoint; iPoint++) nodes->SetGridVel(iPoint, xDot);
 }
 
-void CGeometry::SetWallVelocity(const CConfig* config, bool print) {
+void CGeometry::SetWallVelocity(const CConfig* config, bool print) const {
   const su2double L_Ref = config->GetLength_Ref();
   const su2double Omega_Ref = config->GetOmega_Ref();
   const su2double Vel_Ref = config->GetVelocity_Ref();
@@ -3571,7 +3567,7 @@ void CGeometry::SetWallVelocity(const CConfig* config, bool print) {
   }
 }
 
-void CGeometry::SetGridVelocity(const CConfig* config) {
+void CGeometry::SetGridVelocity(const CConfig* config) const {
   /*--- Get timestep and whether to use 1st or 2nd order backward finite differences ---*/
 
   bool FirstOrder = (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST);
@@ -3620,7 +3616,7 @@ const CCompressedSparsePatternUL& CGeometry::GetSparsePattern(ConnectivityType t
   return *pattern;
 }
 
-const CEdgeToNonZeroMapUL& CGeometry::GetEdgeToSparsePatternMap(void) {
+const CEdgeToNonZeroMapUL& CGeometry::GetEdgeToSparsePatternMap() {
   if (edgeToCSRMap.empty()) {
     if (finiteVolumeCSRFill0.empty()) {
       finiteVolumeCSRFill0 = buildCSRPattern(*this, ConnectivityType::FiniteVolume, 0ul);
diff --git a/Common/src/geometry/CMultiGridGeometry.cpp b/Common/src/geometry/CMultiGridGeometry.cpp
index e131d569df0..87b97af6a2f 100644
--- a/Common/src/geometry/CMultiGridGeometry.cpp
+++ b/Common/src/geometry/CMultiGridGeometry.cpp
@@ -77,7 +77,7 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry* fine_grid, CConfig* config, un
        belongs to this physical domain, and it meets the geometrical
        criteria, the agglomeration is studied. ---*/
 
-      if ((fine_grid->nodes->GetAgglomerate(iPoint) == false) && (fine_grid->nodes->GetDomain(iPoint)) &&
+      if ((!fine_grid->nodes->GetAgglomerate(iPoint)) && (fine_grid->nodes->GetDomain(iPoint)) &&
           (GeometricalCheck(iPoint, fine_grid, config))) {
         unsigned short nChildren = 1;
 
@@ -114,12 +114,8 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry* fine_grid, CConfig* config, un
          markers is SEND_RECEIVE ---*/
 
         if (counter == 2) {
-          if ((config->GetMarker_All_KindBC(copy_marker[0]) == SEND_RECEIVE) ||
-              (config->GetMarker_All_KindBC(copy_marker[1]) == SEND_RECEIVE)) {
-            agglomerate_seed = true;
-          } else {
-            agglomerate_seed = false;
-          }
+          agglomerate_seed = (config->GetMarker_All_KindBC(copy_marker[0]) == SEND_RECEIVE) ||
+                             (config->GetMarker_All_KindBC(copy_marker[1]) == SEND_RECEIVE);
         }
 
         /*--- If there are more than 2 markers, the aglomeration will be discarted ---*/
@@ -190,7 +186,7 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry* fine_grid, CConfig* config, un
     for (auto iVertex = 0ul; iVertex < fine_grid->GetnVertex(iMarker); iVertex++) {
       const auto iPoint = fine_grid->vertex[iMarker][iVertex]->GetNode();
 
-      if ((fine_grid->nodes->GetAgglomerate(iPoint) == false) && (fine_grid->nodes->GetDomain(iPoint))) {
+      if ((!fine_grid->nodes->GetAgglomerate(iPoint)) && (fine_grid->nodes->GetDomain(iPoint))) {
         fine_grid->nodes->SetParent_CV(iPoint, Index_CoarseCV);
         nodes->SetChildren_CV(Index_CoarseCV, 0, iPoint);
         nodes->SetnChildren_CV(Index_CoarseCV, 1);
@@ -227,7 +223,7 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry* fine_grid, CConfig* config, un
     /*--- If the element has not being previously agglomerated, belongs to the physical domain,
      and satisfies several geometrical criteria then the seed CV is accepted for agglomeration. ---*/
 
-    if ((fine_grid->nodes->GetAgglomerate(iPoint) == false) && (fine_grid->nodes->GetDomain(iPoint)) &&
+    if ((!fine_grid->nodes->GetAgglomerate(iPoint)) && (fine_grid->nodes->GetDomain(iPoint)) &&
         (GeometricalCheck(iPoint, fine_grid, config))) {
       unsigned short nChildren = 1;
 
@@ -249,7 +245,7 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry* fine_grid, CConfig* config, un
       for (auto CVPoint : fine_grid->nodes->GetPoints(iPoint)) {
         /*--- Determine if the CVPoint can be agglomerated ---*/
 
-        if ((fine_grid->nodes->GetAgglomerate(CVPoint) == false) && (fine_grid->nodes->GetDomain(CVPoint)) &&
+        if ((!fine_grid->nodes->GetAgglomerate(CVPoint)) && (fine_grid->nodes->GetDomain(CVPoint)) &&
             (GeometricalCheck(CVPoint, fine_grid, config))) {
           /*--- We set the value of the parent ---*/
 
@@ -278,7 +274,7 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry* fine_grid, CConfig* config, un
       for (auto CVPoint : Suitable_Indirect_Neighbors) {
         /*--- The new point can be agglomerated ---*/
 
-        if ((fine_grid->nodes->GetAgglomerate(CVPoint) == false) && (fine_grid->nodes->GetDomain(CVPoint))) {
+        if ((!fine_grid->nodes->GetAgglomerate(CVPoint)) && (fine_grid->nodes->GetDomain(CVPoint))) {
           /*--- We set the value of the parent ---*/
 
           fine_grid->nodes->SetParent_CV(CVPoint, Index_CoarseCV);
@@ -314,7 +310,7 @@ CMultiGridGeometry::CMultiGridGeometry(CGeometry* fine_grid, CConfig* config, un
   /*--- Convert any point that was not agglomerated into a coarse point. ---*/
 
   for (auto iPoint = 0ul; iPoint < fine_grid->GetnPoint(); iPoint++) {
-    if ((fine_grid->nodes->GetAgglomerate(iPoint) == false) && (fine_grid->nodes->GetDomain(iPoint))) {
+    if ((!fine_grid->nodes->GetAgglomerate(iPoint)) && (fine_grid->nodes->GetDomain(iPoint))) {
       fine_grid->nodes->SetParent_CV(iPoint, Index_CoarseCV);
       if (fine_grid->nodes->GetAgglomerate_Indirect(iPoint)) nodes->SetAgglomerate_Indirect(Index_CoarseCV, true);
       nodes->SetChildren_CV(Index_CoarseCV, 0, iPoint);
@@ -508,7 +504,7 @@ bool CMultiGridGeometry::SetBoundAgglomeration(unsigned long CVPoint, short mark
   /*--- Basic condition, the point has not being previously agglomerated, it belongs to the domain,
    and has passed some basic geometrical checks. ---*/
 
-  if ((fine_grid->nodes->GetAgglomerate(CVPoint) == false) && (fine_grid->nodes->GetDomain(CVPoint)) &&
+  if ((!fine_grid->nodes->GetAgglomerate(CVPoint)) && (fine_grid->nodes->GetDomain(CVPoint)) &&
       (GeometricalCheck(CVPoint, fine_grid, config))) {
     /*--- If the point belongs to a boundary, its type must be compatible with the seed marker. ---*/
 
@@ -967,8 +963,8 @@ void CMultiGridGeometry::SetMultiGridWallHeatFlux(const CGeometry* fine_grid, un
     unsigned short marker;
     su2double* target;
 
-    su2double Get(unsigned long iVertex) { return fine_grid->GetCustomBoundaryHeatFlux(marker, iVertex); }
-    void Set(unsigned long iVertex, const su2double& val) { target[iVertex] = val; }
+    su2double Get(unsigned long iVertex) const { return fine_grid->GetCustomBoundaryHeatFlux(marker, iVertex); }
+    void Set(unsigned long iVertex, const su2double& val) const { target[iVertex] = val; }
 
   } wall_heat_flux;
 
@@ -985,8 +981,8 @@ void CMultiGridGeometry::SetMultiGridWallTemperature(const CGeometry* fine_grid,
     unsigned short marker;
     su2double* target;
 
-    su2double Get(unsigned long iVertex) { return fine_grid->GetCustomBoundaryTemperature(marker, iVertex); }
-    void Set(unsigned long iVertex, const su2double& val) { target[iVertex] = val; }
+    su2double Get(unsigned long iVertex) const { return fine_grid->GetCustomBoundaryTemperature(marker, iVertex); }
+    void Set(unsigned long iVertex, const su2double& val) const { target[iVertex] = val; }
 
   } wall_temperature;
 
diff --git a/Common/src/geometry/CMultiGridQueue.cpp b/Common/src/geometry/CMultiGridQueue.cpp
index cc6a16a8b4d..8fda68fa507 100644
--- a/Common/src/geometry/CMultiGridQueue.cpp
+++ b/Common/src/geometry/CMultiGridQueue.cpp
@@ -122,7 +122,7 @@ void CMultiGridQueue::RedPriorityCV(unsigned long redPoint) {
   AddCV(redPoint, numberNeighbors - 1);
 }
 
-void CMultiGridQueue::VisualizeQueue(void) const {
+void CMultiGridQueue::VisualizeQueue() const {
   cout << endl;
   unsigned short iQ = 0;
   for (const auto& Q : QueueCV) {
@@ -134,13 +134,13 @@ void CMultiGridQueue::VisualizeQueue(void) const {
   }
 }
 
-void CMultiGridQueue::VisualizePriority(void) const {
+void CMultiGridQueue::VisualizePriority() const {
   for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint) {
     cout << "Control Volume: " << iPoint << " Priority: " << Priority[iPoint] << endl;
   }
 }
 
-bool CMultiGridQueue::EmptyQueue(void) const {
+bool CMultiGridQueue::EmptyQueue() const {
   /*--- In case there is only the no agglomerated elements (size 1), check
    *    if they can be agglomerated or if we have already finished. ---*/
 
@@ -154,7 +154,7 @@ bool CMultiGridQueue::EmptyQueue(void) const {
   return true;
 }
 
-unsigned long CMultiGridQueue::TotalCV(void) const {
+unsigned long CMultiGridQueue::TotalCV() const {
   unsigned long TotalCV = 0;
   for (const auto& Q : QueueCV) TotalCV += Q.size();
   return TotalCV;
diff --git a/Common/src/geometry/CPhysicalGeometry.cpp b/Common/src/geometry/CPhysicalGeometry.cpp
index 8496dcb6491..6ecfb42c140 100644
--- a/Common/src/geometry/CPhysicalGeometry.cpp
+++ b/Common/src/geometry/CPhysicalGeometry.cpp
@@ -304,7 +304,7 @@ CPhysicalGeometry::CPhysicalGeometry(CGeometry* geometry, CConfig* config) : CGe
   delete[] Elem_ID_BoundQuad_Linear;
 }
 
-CPhysicalGeometry::~CPhysicalGeometry(void) {
+CPhysicalGeometry::~CPhysicalGeometry() {
   delete[] Local_to_Global_Point;
 
   /*--- Free up memory from turbomachinery performance computation  ---*/
@@ -443,7 +443,7 @@ CPhysicalGeometry::~CPhysicalGeometry(void) {
   }
 }
 
-void CPhysicalGeometry::SetGlobal_to_Local_Point(void) {
+void CPhysicalGeometry::SetGlobal_to_Local_Point() {
   Global_to_Local_Point.clear();
   for (unsigned long iPoint = 0; iPoint < nPointDomain; iPoint++) {
     Global_to_Local_Point[nodes->GetGlobalIndex(iPoint)] = iPoint;
@@ -594,18 +594,18 @@ void CPhysicalGeometry::DistributeColoring(const CConfig* config, CGeometry* geo
 
   /*--- Allocate arrays for sending the global ID. ---*/
 
-  unsigned long* idSend = new unsigned long[nPoint_Send[size]];
+  auto* idSend = new unsigned long[nPoint_Send[size]];
   for (iSend = 0; iSend < nPoint_Send[size]; iSend++) idSend[iSend] = 0;
 
   /*--- Allocate memory to hold the colors that we are sending. ---*/
 
-  unsigned long* colorSend = new unsigned long[nPoint_Send[size]];
+  auto* colorSend = new unsigned long[nPoint_Send[size]];
   for (iSend = 0; iSend < nPoint_Send[size]; iSend++) colorSend[iSend] = 0;
 
   /*--- Create an index variable to keep track of our index
    positions as we load up the send buffer. ---*/
 
-  unsigned long* index = new unsigned long[size];
+  auto* index = new unsigned long[size];
   for (iProc = 0; iProc < size; iProc++) index[iProc] = nPoint_Send[iProc];
 
   /*--- Now load up our buffers with the Global IDs and colors. ---*/
@@ -648,10 +648,10 @@ void CPhysicalGeometry::DistributeColoring(const CConfig* config, CGeometry* geo
    we do not include our own rank in the communications. We will
    directly copy our own data later. ---*/
 
-  unsigned long* colorRecv = new unsigned long[nPoint_Recv[size]];
+  auto* colorRecv = new unsigned long[nPoint_Recv[size]];
   for (iRecv = 0; iRecv < nPoint_Recv[size]; iRecv++) colorRecv[iRecv] = 0;
 
-  unsigned long* idRecv = new unsigned long[nPoint_Recv[size]];
+  auto* idRecv = new unsigned long[nPoint_Recv[size]];
   for (iRecv = 0; iRecv < nPoint_Recv[size]; iRecv++) idRecv[iRecv] = 0;
 
   /*--- Allocate memory for the MPI requests if we need to communicate. ---*/
@@ -835,16 +835,16 @@ void CPhysicalGeometry::DistributeVolumeConnectivity(const CConfig* config, CGeo
 
   /*--- Allocate arrays for storing element global index. ---*/
 
-  unsigned long* idSend = new unsigned long[nElem_Send[size]];
+  auto* idSend = new unsigned long[nElem_Send[size]];
   for (iSend = 0; iSend < nElem_Send[size]; iSend++) idSend[iSend] = 0;
 
   /*--- Create an index variable to keep track of our index
    position as we load up the send buffer. ---*/
 
-  unsigned long* index = new unsigned long[size];
+  auto* index = new unsigned long[size];
   for (iProc = 0; iProc < size; iProc++) index[iProc] = NODES_PER_ELEMENT * nElem_Send[iProc];
 
-  unsigned long* idIndex = new unsigned long[size];
+  auto* idIndex = new unsigned long[size];
   for (iProc = 0; iProc < size; iProc++) idIndex[iProc] = nElem_Send[iProc];
 
   /*--- Loop through our elements and load the elems and their
@@ -903,7 +903,7 @@ void CPhysicalGeometry::DistributeVolumeConnectivity(const CConfig* config, CGeo
   connRecv = new unsigned long[NODES_PER_ELEMENT * nElem_Recv[size]];
   for (iRecv = 0; iRecv < NODES_PER_ELEMENT * nElem_Recv[size]; iRecv++) connRecv[iRecv] = 0;
 
-  unsigned long* idRecv = new unsigned long[nElem_Recv[size]];
+  auto* idRecv = new unsigned long[nElem_Recv[size]];
   for (iRecv = 0; iRecv < nElem_Recv[size]; iRecv++) idRecv[iRecv] = 0;
 
   /*--- Allocate memory for the MPI requests if we need to communicate. ---*/
@@ -1118,12 +1118,12 @@ void CPhysicalGeometry::DistributePoints(const CConfig* config, CGeometry* geome
 
   /*--- Allocate arrays for sending the global ID. ---*/
 
-  unsigned long* idSend = new unsigned long[nPoint_Send[size]];
+  auto* idSend = new unsigned long[nPoint_Send[size]];
   for (iSend = 0; iSend < nPoint_Send[size]; iSend++) idSend[iSend] = 0;
 
   /*--- Allocate memory to hold the colors that we are sending. ---*/
 
-  unsigned long* colorSend = new unsigned long[nPoint_Send[size]];
+  auto* colorSend = new unsigned long[nPoint_Send[size]];
   for (iSend = 0; iSend < nPoint_Send[size]; iSend++) colorSend[iSend] = 0;
 
   /*--- Allocate memory to hold the coordinates that we are sending. ---*/
@@ -1135,10 +1135,10 @@ void CPhysicalGeometry::DistributePoints(const CConfig* config, CGeometry* geome
   /*--- Create index variables to keep track of our index
    positions as we load up the send buffer. ---*/
 
-  unsigned long* index = new unsigned long[size];
+  auto* index = new unsigned long[size];
   for (iProc = 0; iProc < size; iProc++) index[iProc] = nPoint_Send[iProc];
 
-  unsigned long* coordIndex = new unsigned long[size];
+  auto* coordIndex = new unsigned long[size];
   for (iProc = 0; iProc < size; iProc++) coordIndex[iProc] = nDim * nPoint_Send[iProc];
 
   /*--- Now load up our buffers with the colors, ids, and coords. ---*/
@@ -1189,10 +1189,10 @@ void CPhysicalGeometry::DistributePoints(const CConfig* config, CGeometry* geome
    we do not include our own rank in the communications. We will
    directly copy our own data later. ---*/
 
-  unsigned long* colorRecv = new unsigned long[nPoint_Recv[size]];
+  auto* colorRecv = new unsigned long[nPoint_Recv[size]];
   for (iRecv = 0; iRecv < nPoint_Recv[size]; iRecv++) colorRecv[iRecv] = 0;
 
-  unsigned long* idRecv = new unsigned long[nPoint_Recv[size]];
+  auto* idRecv = new unsigned long[nPoint_Recv[size]];
   for (iRecv = 0; iRecv < nPoint_Recv[size]; iRecv++) idRecv[iRecv] = 0;
 
   su2double* coordRecv = nullptr;
@@ -1426,10 +1426,10 @@ void CPhysicalGeometry::PartitionSurfaceConnectivity(CConfig* config, CGeometry*
     /*--- Create an index variable to keep track of our index
      position as we load up the send buffer. ---*/
 
-    unsigned long* index = new unsigned long[size];
+    auto* index = new unsigned long[size];
     for (iProc = 0; iProc < size; iProc++) index[iProc] = NODES_PER_ELEMENT * nElem_Send[iProc];
 
-    unsigned long* markerIndex = new unsigned long[size];
+    auto* markerIndex = new unsigned long[size];
     for (iProc = 0; iProc < size; iProc++) markerIndex[iProc] = nElem_Send[iProc];
 
     /*--- Loop through our elements and load the elems and their
@@ -1500,10 +1500,10 @@ void CPhysicalGeometry::PartitionSurfaceConnectivity(CConfig* config, CGeometry*
   connRecv = new unsigned long[NODES_PER_ELEMENT * nElem_Recv[size]];
   for (iRecv = 0; iRecv < NODES_PER_ELEMENT * nElem_Recv[size]; iRecv++) connRecv[iRecv] = 0;
 
-  unsigned long* markerRecv = new unsigned long[nElem_Recv[size]];
+  auto* markerRecv = new unsigned long[nElem_Recv[size]];
   for (iRecv = 0; iRecv < nElem_Recv[size]; iRecv++) markerRecv[iRecv] = 0;
 
-  unsigned long* idRecv = new unsigned long[nElem_Recv[size]];
+  auto* idRecv = new unsigned long[nElem_Recv[size]];
   for (iRecv = 0; iRecv < nElem_Recv[size]; iRecv++) idRecv[iRecv] = 0;
 
   /*--- Allocate memory for the MPI requests if we need to communicate. ---*/
@@ -1766,19 +1766,19 @@ void CPhysicalGeometry::DistributeSurfaceConnectivity(CConfig* config, CGeometry
 
   /*--- Allocate arrays for storing the marker global index. ---*/
 
-  unsigned long* markerSend = new unsigned long[nElem_Send[size]];
+  auto* markerSend = new unsigned long[nElem_Send[size]];
   for (iSend = 0; iSend < nElem_Send[size]; iSend++) markerSend[iSend] = 0;
 
-  unsigned long* idSend = new unsigned long[nElem_Send[size]];
+  auto* idSend = new unsigned long[nElem_Send[size]];
   for (iSend = 0; iSend < nElem_Send[size]; iSend++) idSend[iSend] = 0;
 
   /*--- Create an index variable to keep track of our index
    position as we load up the send buffer. ---*/
 
-  unsigned long* index = new unsigned long[size];
+  auto* index = new unsigned long[size];
   for (iProc = 0; iProc < size; iProc++) index[iProc] = NODES_PER_ELEMENT * nElem_Send[iProc];
 
-  unsigned long* markerIndex = new unsigned long[size];
+  auto* markerIndex = new unsigned long[size];
   for (iProc = 0; iProc < size; iProc++) markerIndex[iProc] = nElem_Send[iProc];
 
   /*--- Loop through our elements and load the elems and their
@@ -1839,10 +1839,10 @@ void CPhysicalGeometry::DistributeSurfaceConnectivity(CConfig* config, CGeometry
   connRecv = new unsigned long[NODES_PER_ELEMENT * nElem_Recv[size]];
   for (iRecv = 0; iRecv < NODES_PER_ELEMENT * nElem_Recv[size]; iRecv++) connRecv[iRecv] = 0;
 
-  unsigned long* markerRecv = new unsigned long[nElem_Recv[size]];
+  auto* markerRecv = new unsigned long[nElem_Recv[size]];
   for (iRecv = 0; iRecv < nElem_Recv[size]; iRecv++) markerRecv[iRecv] = 0;
 
-  unsigned long* idRecv = new unsigned long[nElem_Recv[size]];
+  auto* idRecv = new unsigned long[nElem_Recv[size]];
   for (iRecv = 0; iRecv < nElem_Recv[size]; iRecv++) idRecv[iRecv] = 0;
 
   /*--- Allocate memory for the MPI requests if we need to communicate. ---*/
@@ -2016,7 +2016,7 @@ void CPhysicalGeometry::DistributeMarkerTags(CConfig* config, CGeometry* geometr
     for (iChar = 0; iChar < MAX_STRING_SIZE; iChar++) {
       str_buf[iChar] = mpi_str_buf[index + iChar];
     }
-    Marker_Tags.push_back(str_buf);
+    Marker_Tags.emplace_back(str_buf);
     config->SetMarker_All_TagBound(iMarker, str_buf);
     config->SetMarker_All_SendRecv(iMarker, NO);
   }
@@ -2973,7 +2973,7 @@ void CPhysicalGeometry::SetSendReceive(const CConfig* config) {
   unsigned long iVertex, LocalNode;
   unsigned short nMarker_Max = config->GetnMarker_Max();
   unsigned long iPoint, jPoint, iElem, nDomain, iDomain, jDomain;
-  unsigned long* nVertexDomain = new unsigned long[nMarker_Max];
+  auto* nVertexDomain = new unsigned long[nMarker_Max];
   unsigned short iNode, jNode;
   vector<unsigned long>::iterator it;
 
@@ -3062,7 +3062,7 @@ void CPhysicalGeometry::SetSendReceive(const CConfig* config) {
    and save the local value. ---*/
 
   for (iDomain = 0; iDomain < nDomain; iDomain++) {
-    if (SendDomainLocal[iDomain].size() != 0) {
+    if (!SendDomainLocal[iDomain].empty()) {
       nVertexDomain[nMarker] = SendDomainLocal[iDomain].size();
       for (iVertex = 0; iVertex < nVertexDomain[nMarker]; iVertex++) {
         MI = Global_to_Local_Point.find(SendDomainLocal[iDomain][iVertex]);
@@ -3082,7 +3082,7 @@ void CPhysicalGeometry::SetSendReceive(const CConfig* config) {
 
   /*--- Add the new MPI receive boundaries, reset the transformation, and save the local value ---*/
   for (iDomain = 0; iDomain < nDomain; iDomain++) {
-    if (ReceivedDomainLocal[iDomain].size() != 0) {
+    if (!ReceivedDomainLocal[iDomain].empty()) {
       nVertexDomain[nMarker] = ReceivedDomainLocal[iDomain].size();
       for (iVertex = 0; iVertex < nVertexDomain[nMarker]; iVertex++) {
         MI = Global_to_Local_Point.find(ReceivedDomainLocal[iDomain][iVertex]);
@@ -3104,17 +3104,17 @@ void CPhysicalGeometry::SetSendReceive(const CConfig* config) {
   Counter_Send = 0;
   Counter_Receive = 0;
   for (iDomain = 0; iDomain < nDomain; iDomain++)
-    if (SendDomainLocal[iDomain].size() != 0) Counter_Send++;
+    if (!SendDomainLocal[iDomain].empty()) Counter_Send++;
 
   for (iDomain = 0; iDomain < nDomain; iDomain++)
-    if (ReceivedDomainLocal[iDomain].size() != 0) Counter_Receive++;
+    if (!ReceivedDomainLocal[iDomain].empty()) Counter_Receive++;
 
   iMarkerSend = nMarker - Counter_Send - Counter_Receive;
   iMarkerReceive = nMarker - Counter_Receive;
 
   /*--- First we do the send ---*/
   for (iDomain = 0; iDomain < nDomain; iDomain++) {
-    if (SendDomainLocal[iDomain].size() != 0) {
+    if (!SendDomainLocal[iDomain].empty()) {
       for (iVertex = 0; iVertex < GetnElem_Bound(iMarkerSend); iVertex++) {
         LocalNode = SendDomainLocal[iDomain][iVertex];
         bound[iMarkerSend][iVertex] = new CVertexMPI(LocalNode);
@@ -3127,7 +3127,7 @@ void CPhysicalGeometry::SetSendReceive(const CConfig* config) {
 
   /*--- Second we do the receive ---*/
   for (iDomain = 0; iDomain < nDomain; iDomain++) {
-    if (ReceivedDomainLocal[iDomain].size() != 0) {
+    if (!ReceivedDomainLocal[iDomain].empty()) {
       for (iVertex = 0; iVertex < GetnElem_Bound(iMarkerReceive); iVertex++) {
         LocalNode = ReceivedDomainLocal[iDomain][iVertex];
         bound[iMarkerReceive][iVertex] = new CVertexMPI(LocalNode);
@@ -3431,7 +3431,7 @@ void CPhysicalGeometry::SetBoundaries(CConfig* config) {
   delete[] nElem_Bound_Copy;
 }
 
-void CPhysicalGeometry::Read_Mesh_FVM(CConfig* config, string val_mesh_filename, unsigned short val_iZone,
+void CPhysicalGeometry::Read_Mesh_FVM(CConfig* config, const string& val_mesh_filename, unsigned short val_iZone,
                                       unsigned short val_nZone) {
   /*--- Initialize counters for local/global points & elements ---*/
 
@@ -3682,7 +3682,7 @@ void CPhysicalGeometry::LoadUnpartitionedSurfaceElements(CConfig* config, CMeshR
 
       /*--- Get the string name for this marker. ---*/
 
-      string Marker_Tag = sectionNames[iMarker];
+      const string& Marker_Tag = sectionNames[iMarker];
 
       /* Get the marker info and surface connectivity from the mesh object. */
 
@@ -4607,7 +4607,7 @@ void CPhysicalGeometry::SetRCM_Ordering(CConfig* config) {
   }
 }
 
-void CPhysicalGeometry::SetElement_Connectivity(void) {
+void CPhysicalGeometry::SetElement_Connectivity() {
   unsigned short first_elem_face, second_elem_face, iFace, iNode, jElem;
   unsigned long face_point, Test_Elem, iElem;
 
@@ -4639,7 +4639,7 @@ void CPhysicalGeometry::SetElement_Connectivity(void) {
       }
 }
 
-void CPhysicalGeometry::SetBoundVolume(void) {
+void CPhysicalGeometry::SetBoundVolume() {
   unsigned short cont, iMarker, iElem, iNode_Domain, iNode_Surface;
   unsigned long Point_Domain, Point_Surface, Point, iElem_Surface, iElem_Domain;
   bool CheckVol;
@@ -5007,8 +5007,8 @@ void CPhysicalGeometry::SetTurboVertex(CConfig* config, unsigned short val_iZone
 #ifdef HAVE_MPI
   unsigned short iSize, kSize = 0, jSize;
   su2double MyMin, MyIntMin, MyMax;
-  su2double *x_gb = NULL, *y_gb = NULL, *z_gb = NULL, *angCoord_gb = NULL, *deltaAngCoord_gb = NULL;
-  bool* checkAssign_gb = NULL;
+  su2double *x_gb = nullptr, *y_gb = nullptr, *z_gb = nullptr, *angCoord_gb = nullptr, *deltaAngCoord_gb = nullptr;
+  bool* checkAssign_gb = nullptr;
   unsigned long My_nVert;
 
 #endif
@@ -5676,7 +5676,7 @@ void CPhysicalGeometry::SetTurboVertex(CConfig* config, unsigned short val_iZone
     char buffer[50];
 
     if (GetnZone() > 1) {
-      unsigned short lastindex = multizone_filename.find_last_of(".");
+      unsigned short lastindex = multizone_filename.find_last_of('.');
       multizone_filename = multizone_filename.substr(0, lastindex);
       SPRINTF(buffer, "_%d.dat", SU2_TYPE::Int(val_iZone));
       multizone_filename.append(string(buffer));
@@ -5897,7 +5897,8 @@ void CPhysicalGeometry::SetAvgTurboValue(CConfig* config, unsigned short val_iZo
 
   bool grid_movement = config->GetGrid_Movement();
 #ifdef HAVE_MPI
-  su2double MyTotalArea, MyTotalRadius, *MyTotalTurboNormal = NULL, *MyTotalNormal = NULL, *MyTotalGridVel = NULL;
+  su2double MyTotalArea, MyTotalRadius, *MyTotalTurboNormal = nullptr, *MyTotalNormal = nullptr,
+                                        *MyTotalGridVel = nullptr;
 #endif
 
   /*--- Intialization of the vector for the interested boundary ---*/
@@ -6165,8 +6166,8 @@ void CPhysicalGeometry::GatherInOutAverageValues(CConfig* config, bool allocate)
   for (iSpan = 0; iSpan < nSpanWiseSections + 1; iSpan++) {
 #ifdef HAVE_MPI
     unsigned short i, n1, n2, n1t, n2t;
-    su2double *TurbGeoIn = NULL, *TurbGeoOut = NULL;
-    su2double *TotTurbGeoIn = NULL, *TotTurbGeoOut = NULL;
+    su2double *TurbGeoIn = nullptr, *TurbGeoOut = nullptr;
+    su2double *TotTurbGeoIn = nullptr, *TotTurbGeoOut = nullptr;
     int* TotMarkerTP;
 
     n1 = 6;
@@ -6378,8 +6379,8 @@ void CPhysicalGeometry::MatchActuator_Disk(const CConfig* config) {
         Donor = ACTDISK_INLET;
       }
 
-      unsigned long* Buffer_Send_nVertex = new unsigned long[1];
-      unsigned long* Buffer_Receive_nVertex = new unsigned long[nProcessor];
+      auto* Buffer_Send_nVertex = new unsigned long[1];
+      auto* Buffer_Receive_nVertex = new unsigned long[nProcessor];
 
       if ((iBC == 0) && (rank == MASTER_NODE)) cout << "Set Actuator Disk inlet boundary conditions." << endl;
       if ((iBC == 1) && (rank == MASTER_NODE)) cout << "Set Actuator Disk outlet boundary conditions." << endl;
@@ -6408,17 +6409,17 @@ void CPhysicalGeometry::MatchActuator_Disk(const CConfig* config) {
 
       /*--- Array dimensionalization --*/
 
-      su2double* Buffer_Send_Coord = new su2double[MaxLocalVertex_ActDisk * nDim];
-      unsigned long* Buffer_Send_Point = new unsigned long[MaxLocalVertex_ActDisk];
-      unsigned long* Buffer_Send_GlobalIndex = new unsigned long[MaxLocalVertex_ActDisk];
-      unsigned long* Buffer_Send_Vertex = new unsigned long[MaxLocalVertex_ActDisk];
-      unsigned long* Buffer_Send_Marker = new unsigned long[MaxLocalVertex_ActDisk];
+      auto* Buffer_Send_Coord = new su2double[MaxLocalVertex_ActDisk * nDim];
+      auto* Buffer_Send_Point = new unsigned long[MaxLocalVertex_ActDisk];
+      auto* Buffer_Send_GlobalIndex = new unsigned long[MaxLocalVertex_ActDisk];
+      auto* Buffer_Send_Vertex = new unsigned long[MaxLocalVertex_ActDisk];
+      auto* Buffer_Send_Marker = new unsigned long[MaxLocalVertex_ActDisk];
 
-      su2double* Buffer_Receive_Coord = new su2double[nProcessor * MaxLocalVertex_ActDisk * nDim];
-      unsigned long* Buffer_Receive_Point = new unsigned long[nProcessor * MaxLocalVertex_ActDisk];
-      unsigned long* Buffer_Receive_GlobalIndex = new unsigned long[nProcessor * MaxLocalVertex_ActDisk];
-      unsigned long* Buffer_Receive_Vertex = new unsigned long[nProcessor * MaxLocalVertex_ActDisk];
-      unsigned long* Buffer_Receive_Marker = new unsigned long[nProcessor * MaxLocalVertex_ActDisk];
+      auto* Buffer_Receive_Coord = new su2double[nProcessor * MaxLocalVertex_ActDisk * nDim];
+      auto* Buffer_Receive_Point = new unsigned long[nProcessor * MaxLocalVertex_ActDisk];
+      auto* Buffer_Receive_GlobalIndex = new unsigned long[nProcessor * MaxLocalVertex_ActDisk];
+      auto* Buffer_Receive_Vertex = new unsigned long[nProcessor * MaxLocalVertex_ActDisk];
+      auto* Buffer_Receive_Marker = new unsigned long[nProcessor * MaxLocalVertex_ActDisk];
 
       unsigned long nBuffer_Coord = MaxLocalVertex_ActDisk * nDim;
       unsigned long nBuffer_Point = MaxLocalVertex_ActDisk;
@@ -6628,8 +6629,8 @@ void CPhysicalGeometry::MatchPeriodic(const CConfig* config, unsigned short val_
   /*--- Communicate our local periodic point count globally
    and receive the counts of periodic points from all other ranks.---*/
 
-  unsigned long* Buffer_Send_nVertex = new unsigned long[1];
-  unsigned long* Buffer_Recv_nVertex = new unsigned long[nProcessor];
+  auto* Buffer_Send_nVertex = new unsigned long[1];
+  auto* Buffer_Recv_nVertex = new unsigned long[nProcessor];
 
   Buffer_Send_nVertex[0] = nLocalVertex_Periodic;
 
@@ -6643,17 +6644,17 @@ void CPhysicalGeometry::MatchPeriodic(const CConfig* config, unsigned short val_
   /*--- Prepare buffers to send the information for each
    periodic point to all ranks so that we can match pairs. ---*/
 
-  su2double* Buffer_Send_Coord = new su2double[MaxLocalVertex_Periodic * nDim];
-  unsigned long* Buffer_Send_Point = new unsigned long[MaxLocalVertex_Periodic];
-  unsigned long* Buffer_Send_GlobalIndex = new unsigned long[MaxLocalVertex_Periodic];
-  unsigned long* Buffer_Send_Vertex = new unsigned long[MaxLocalVertex_Periodic];
-  unsigned long* Buffer_Send_Marker = new unsigned long[MaxLocalVertex_Periodic];
+  auto* Buffer_Send_Coord = new su2double[MaxLocalVertex_Periodic * nDim];
+  auto* Buffer_Send_Point = new unsigned long[MaxLocalVertex_Periodic];
+  auto* Buffer_Send_GlobalIndex = new unsigned long[MaxLocalVertex_Periodic];
+  auto* Buffer_Send_Vertex = new unsigned long[MaxLocalVertex_Periodic];
+  auto* Buffer_Send_Marker = new unsigned long[MaxLocalVertex_Periodic];
 
-  su2double* Buffer_Recv_Coord = new su2double[nProcessor * MaxLocalVertex_Periodic * nDim];
-  unsigned long* Buffer_Recv_Point = new unsigned long[nProcessor * MaxLocalVertex_Periodic];
-  unsigned long* Buffer_Recv_GlobalIndex = new unsigned long[nProcessor * MaxLocalVertex_Periodic];
-  unsigned long* Buffer_Recv_Vertex = new unsigned long[nProcessor * MaxLocalVertex_Periodic];
-  unsigned long* Buffer_Recv_Marker = new unsigned long[nProcessor * MaxLocalVertex_Periodic];
+  auto* Buffer_Recv_Coord = new su2double[nProcessor * MaxLocalVertex_Periodic * nDim];
+  auto* Buffer_Recv_Point = new unsigned long[nProcessor * MaxLocalVertex_Periodic];
+  auto* Buffer_Recv_GlobalIndex = new unsigned long[nProcessor * MaxLocalVertex_Periodic];
+  auto* Buffer_Recv_Vertex = new unsigned long[nProcessor * MaxLocalVertex_Periodic];
+  auto* Buffer_Recv_Marker = new unsigned long[nProcessor * MaxLocalVertex_Periodic];
 
   unsigned long nBuffer_Coord = MaxLocalVertex_Periodic * nDim;
   unsigned long nBuffer_Point = MaxLocalVertex_Periodic;
@@ -7364,11 +7365,11 @@ void CPhysicalGeometry::VisualizeControlVolume(const CConfig* config) const {
   Tecplot_File << "TITLE= \"Visualization of the control volume\"" << endl;
 
   if (nDim == 2) {
-    Tecplot_File << "VARIABLES = \"x\",\"y\" " << endl;
+    Tecplot_File << R"(VARIABLES = "x","y" )" << endl;
     Tecplot_File << "ZONE NODES= " << counter * 2 << ", ELEMENTS= ";
     Tecplot_File << counter << ", DATAPACKING=POINT, ZONETYPE=FEQUADRILATERAL" << endl;
   } else {
-    Tecplot_File << "VARIABLES = \"x\",\"y\",\"z\" " << endl;
+    Tecplot_File << R"(VARIABLES = "x","y","z" )" << endl;
     Tecplot_File << "ZONE NODES= " << counter * 3 << ", ELEMENTS= ";
     Tecplot_File << counter << ", DATAPACKING=POINT, ZONETYPE=FEBRICK" << endl;
   }
@@ -7539,8 +7540,8 @@ void CPhysicalGeometry::SetTecPlot(char mesh_filename[MAX_STRING_SIZE], bool new
   if (new_file) {
     Tecplot_File.open(mesh_filename, ios::out);
     Tecplot_File << "TITLE= \"Visualization of the volumetric grid\"" << endl;
-    if (nDim == 2) Tecplot_File << "VARIABLES = \"x\",\"y\" " << endl;
-    if (nDim == 3) Tecplot_File << "VARIABLES = \"x\",\"y\",\"z\" " << endl;
+    if (nDim == 2) Tecplot_File << R"(VARIABLES = "x","y" )" << endl;
+    if (nDim == 3) Tecplot_File << R"(VARIABLES = "x","y","z" )" << endl;
   } else
     Tecplot_File.open(mesh_filename, ios::out | ios::app);
 
@@ -7629,8 +7630,8 @@ void CPhysicalGeometry::SetBoundTecPlot(char mesh_filename[MAX_STRING_SIZE], boo
   if (new_file) {
     Tecplot_File.open(mesh_filename, ios::out);
     Tecplot_File << "TITLE= \"Visualization of the surface grid\"" << endl;
-    if (nDim == 2) Tecplot_File << "VARIABLES = \"x\",\"y\" " << endl;
-    if (nDim == 3) Tecplot_File << "VARIABLES = \"x\",\"y\",\"z\" " << endl;
+    if (nDim == 2) Tecplot_File << R"(VARIABLES = "x","y" )" << endl;
+    if (nDim == 3) Tecplot_File << R"(VARIABLES = "x","y","z" )" << endl;
   } else
     Tecplot_File.open(mesh_filename, ios::out | ios::app);
 
@@ -8211,7 +8212,7 @@ void CPhysicalGeometry::SetBoundSensitivity(CConfig* config) {
       PrintingToolbox::trim(split_line[iField]);
     }
 
-    std::vector<string>::iterator it = std::find(split_line.begin(), split_line.end(), "\"Surface_Sensitivity\"");
+    auto it = std::find(split_line.begin(), split_line.end(), "\"Surface_Sensitivity\"");
 
     if (it == split_line.end()) {
       SU2_MPI::Error("Surface sensitivity not found in file.", CURRENT_FUNCTION);
@@ -8221,7 +8222,7 @@ void CPhysicalGeometry::SetBoundSensitivity(CConfig* config) {
 
     while (getline(Surface_file, text_line)) {
       for (icommas = 0; icommas < 50; icommas++) {
-        position = text_line.find(",", 0);
+        position = text_line.find(',', 0);
         if (position != string::npos) text_line.erase(position, 1);
       }
       stringstream point_line(text_line);
@@ -8442,14 +8443,14 @@ void CPhysicalGeometry::SetSensitivity(CConfig* config) {
     /*--- Now parse the string names and load into the config class in case
      we need them for writing visualization files (SU2_SOL). ---*/
 
-    config->fields.push_back("Point_ID");
+    config->fields.emplace_back("Point_ID");
     for (iVar = 0; iVar < nFields; iVar++) {
       index = iVar * CGNS_STRING_SIZE;
       for (iChar = 0; iChar < (unsigned long)CGNS_STRING_SIZE; iChar++) {
         str_buf[iChar] = mpi_str_buf[index + iChar];
       }
       field_buf.append(str_buf);
-      config->fields.push_back(field_buf.c_str());
+      config->fields.emplace_back(field_buf.c_str());
       field_buf.clear();
     }
 
@@ -8471,7 +8472,7 @@ void CPhysicalGeometry::SetSensitivity(CConfig* config) {
      points which are distributed throughout the file in blocks of nVar_Restart data. ---*/
 
     int* blocklen = new int[GetnPointDomain()];
-    MPI_Aint* displace = new MPI_Aint[GetnPointDomain()];
+    auto* displace = new MPI_Aint[GetnPointDomain()];
 
     counter = 0;
     for (iPoint_Global = 0; iPoint_Global < GetGlobal_nPointDomain(); iPoint_Global++) {
@@ -8540,9 +8541,9 @@ void CPhysicalGeometry::SetSensitivity(CConfig* config) {
 
 #endif
 
-    std::vector<string>::iterator itx = std::find(config->fields.begin(), config->fields.end(), "Sensitivity_x");
-    std::vector<string>::iterator ity = std::find(config->fields.begin(), config->fields.end(), "Sensitivity_y");
-    std::vector<string>::iterator itz = std::find(config->fields.begin(), config->fields.end(), "Sensitivity_z");
+    auto itx = std::find(config->fields.begin(), config->fields.end(), "Sensitivity_x");
+    auto ity = std::find(config->fields.begin(), config->fields.end(), "Sensitivity_y");
+    auto itz = std::find(config->fields.begin(), config->fields.end(), "Sensitivity_z");
 
     if (itx == config->fields.end()) {
       SU2_MPI::Error("Sensitivity x not found in file.", CURRENT_FUNCTION);
@@ -8690,9 +8691,9 @@ void CPhysicalGeometry::SetSensitivity(CConfig* config) {
       PrintingToolbox::trim(fields[iField]);
     }
 
-    std::vector<string>::iterator itx = std::find(fields.begin(), fields.end(), "\"Sensitivity_x\"");
-    std::vector<string>::iterator ity = std::find(fields.begin(), fields.end(), "\"Sensitivity_y\"");
-    std::vector<string>::iterator itz = std::find(fields.begin(), fields.end(), "\"Sensitivity_z\"");
+    auto itx = std::find(fields.begin(), fields.end(), "\"Sensitivity_x\"");
+    auto ity = std::find(fields.begin(), fields.end(), "\"Sensitivity_y\"");
+    auto itz = std::find(fields.begin(), fields.end(), "\"Sensitivity_z\"");
 
     if (itx == fields.end()) {
       SU2_MPI::Error("Sensitivity x not found in file.", CURRENT_FUNCTION);
@@ -8926,9 +8927,9 @@ su2double CPhysicalGeometry::Compute_MaxThickness(su2double* Plane_P0, su2double
   Zcoord_Trailing = Zcoord_Airfoil[0];
 
   for (iVertex = 0; iVertex < Xcoord_Airfoil.size(); iVertex++) {
-    Xcoord_Airfoil_.push_back(Xcoord_Airfoil[iVertex] - Xcoord_Trailing);
-    Ycoord_Airfoil_.push_back(Ycoord_Airfoil[iVertex] - Ycoord_Trailing);
-    Zcoord_Airfoil_.push_back(Zcoord_Airfoil[iVertex] - Zcoord_Trailing);
+    Xcoord_Airfoil_.emplace_back(Xcoord_Airfoil[iVertex] - Xcoord_Trailing);
+    Ycoord_Airfoil_.emplace_back(Ycoord_Airfoil[iVertex] - Ycoord_Trailing);
+    Zcoord_Airfoil_.emplace_back(Zcoord_Airfoil[iVertex] - Zcoord_Trailing);
   }
 
   /*--- Rotate the airfoil ---*/
@@ -9369,9 +9370,9 @@ su2double CPhysicalGeometry::Compute_Thickness(su2double* Plane_P0, su2double* P
   Zcoord_Trailing = Zcoord_Airfoil[0];
 
   for (iVertex = 0; iVertex < Xcoord_Airfoil.size(); iVertex++) {
-    Xcoord_Airfoil_.push_back(Xcoord_Airfoil[iVertex] - Xcoord_Trailing);
-    Ycoord_Airfoil_.push_back(Ycoord_Airfoil[iVertex] - Ycoord_Trailing);
-    Zcoord_Airfoil_.push_back(Zcoord_Airfoil[iVertex] - Zcoord_Trailing);
+    Xcoord_Airfoil_.emplace_back(Xcoord_Airfoil[iVertex] - Xcoord_Trailing);
+    Ycoord_Airfoil_.emplace_back(Ycoord_Airfoil[iVertex] - Ycoord_Trailing);
+    Zcoord_Airfoil_.emplace_back(Zcoord_Airfoil[iVertex] - Zcoord_Trailing);
   }
 
   /*--- Rotate the airfoil ---*/
@@ -9593,16 +9594,16 @@ void CPhysicalGeometry::Compute_Wing(CConfig* config, bool original_surface, su2
   Curvature = new su2double[nPlane];
   Dihedral = new su2double[nPlane];
 
-  su2double** LeadingEdge = new su2double*[nPlane];
+  auto** LeadingEdge = new su2double*[nPlane];
   for (iPlane = 0; iPlane < nPlane; iPlane++) LeadingEdge[iPlane] = new su2double[nDim];
 
-  su2double** TrailingEdge = new su2double*[nPlane];
+  auto** TrailingEdge = new su2double*[nPlane];
   for (iPlane = 0; iPlane < nPlane; iPlane++) TrailingEdge[iPlane] = new su2double[nDim];
 
-  su2double** Plane_P0 = new su2double*[nPlane];
+  auto** Plane_P0 = new su2double*[nPlane];
   for (iPlane = 0; iPlane < nPlane; iPlane++) Plane_P0[iPlane] = new su2double[nDim];
 
-  su2double** Plane_Normal = new su2double*[nPlane];
+  auto** Plane_Normal = new su2double*[nPlane];
   for (iPlane = 0; iPlane < nPlane; iPlane++) Plane_Normal[iPlane] = new su2double[nDim];
 
   MinPlane = config->GetStations_Bounds(0);
@@ -9745,11 +9746,11 @@ void CPhysicalGeometry::Compute_Wing(CConfig* config, bool original_surface, su2
     /*--- Set the curvature and dihedral angles at the extremes ---*/
 
     if (nPlane > 1) {
-      if ((Xcoord_Airfoil[0].size() != 0) && (Xcoord_Airfoil[1].size() != 0)) {
+      if ((!Xcoord_Airfoil[0].empty()) && (!Xcoord_Airfoil[1].empty())) {
         Curvature[0] = Curvature[1];
         Dihedral[0] = Dihedral[1];
       }
-      if ((Xcoord_Airfoil[nPlane - 1].size() != 0) && (Xcoord_Airfoil[nPlane - 2].size() != 0)) {
+      if ((!Xcoord_Airfoil[nPlane - 1].empty()) && (!Xcoord_Airfoil[nPlane - 2].empty())) {
         Curvature[nPlane - 1] = Curvature[nPlane - 2];
       }
     }
@@ -9782,10 +9783,10 @@ void CPhysicalGeometry::Compute_Wing(CConfig* config, bool original_surface, su2
       if (iPlane == 0) {
         Section_File << "TITLE = \"Aircraft Slices\"" << endl;
         if (config->GetSystemMeasurements() == US)
-          Section_File << "VARIABLES = \"x (in)\", \"y (in)\", \"z (in)\", \"x<sub>2D</sub>/c\", \"y<sub>2D</sub>/c\""
+          Section_File << R"lit(VARIABLES = "x (in)", "y (in)", "z (in)", "x<sub>2D</sub>/c", "y<sub>2D</sub>/c")lit"
                        << endl;
         else
-          Section_File << "VARIABLES = \"x (m)\", \"y (m)\", \"z (m)\", \"x<sub>2D</sub>/c\", \"y<sub>2D</sub>/c\""
+          Section_File << R"lit(VARIABLES = "x (m)", "y (m)", "z (m)", "x<sub>2D</sub>/c", "y<sub>2D</sub>/c")lit"
                        << endl;
       }
 
@@ -9909,16 +9910,16 @@ void CPhysicalGeometry::Compute_Fuselage(CConfig* config, bool original_surface,
   Height = new su2double[nPlane];
   Curvature = new su2double[nPlane];
 
-  su2double** LeadingEdge = new su2double*[nPlane];
+  auto** LeadingEdge = new su2double*[nPlane];
   for (iPlane = 0; iPlane < nPlane; iPlane++) LeadingEdge[iPlane] = new su2double[nDim];
 
-  su2double** TrailingEdge = new su2double*[nPlane];
+  auto** TrailingEdge = new su2double*[nPlane];
   for (iPlane = 0; iPlane < nPlane; iPlane++) TrailingEdge[iPlane] = new su2double[nDim];
 
-  su2double** Plane_P0 = new su2double*[nPlane];
+  auto** Plane_P0 = new su2double*[nPlane];
   for (iPlane = 0; iPlane < nPlane; iPlane++) Plane_P0[iPlane] = new su2double[nDim];
 
-  su2double** Plane_Normal = new su2double*[nPlane];
+  auto** Plane_Normal = new su2double*[nPlane];
   for (iPlane = 0; iPlane < nPlane; iPlane++) Plane_Normal[iPlane] = new su2double[nDim];
 
   MinPlane = config->GetStations_Bounds(0);
@@ -10045,10 +10046,10 @@ void CPhysicalGeometry::Compute_Fuselage(CConfig* config, bool original_surface,
     /*--- Set the curvature and dihedral angles at the extremes ---*/
 
     if (nPlane > 1) {
-      if ((Xcoord_Airfoil[0].size() != 0) && (Xcoord_Airfoil[1].size() != 0)) {
+      if ((!Xcoord_Airfoil[0].empty()) && (!Xcoord_Airfoil[1].empty())) {
         Curvature[0] = Curvature[1];
       }
-      if ((Xcoord_Airfoil[nPlane - 1].size() != 0) && (Xcoord_Airfoil[nPlane - 2].size() != 0)) {
+      if ((!Xcoord_Airfoil[nPlane - 1].empty()) && (!Xcoord_Airfoil[nPlane - 2].empty())) {
         Curvature[nPlane - 1] = Curvature[nPlane - 2];
       }
     }
@@ -10195,16 +10196,16 @@ void CPhysicalGeometry::Compute_Nacelle(CConfig* config, bool original_surface,
   ToC = new su2double[nPlane];
   Twist = new su2double[nPlane];
 
-  su2double** LeadingEdge = new su2double*[nPlane];
+  auto** LeadingEdge = new su2double*[nPlane];
   for (iPlane = 0; iPlane < nPlane; iPlane++) LeadingEdge[iPlane] = new su2double[nDim];
 
-  su2double** TrailingEdge = new su2double*[nPlane];
+  auto** TrailingEdge = new su2double*[nPlane];
   for (iPlane = 0; iPlane < nPlane; iPlane++) TrailingEdge[iPlane] = new su2double[nDim];
 
-  su2double** Plane_P0 = new su2double*[nPlane];
+  auto** Plane_P0 = new su2double*[nPlane];
   for (iPlane = 0; iPlane < nPlane; iPlane++) Plane_P0[iPlane] = new su2double[nDim];
 
-  su2double** Plane_Normal = new su2double*[nPlane];
+  auto** Plane_Normal = new su2double*[nPlane];
   for (iPlane = 0; iPlane < nPlane; iPlane++) Plane_Normal[iPlane] = new su2double[nDim];
 
   MinAngle = config->GetStations_Bounds(0);
@@ -10377,10 +10378,10 @@ void CPhysicalGeometry::Compute_Nacelle(CConfig* config, bool original_surface,
       if (iPlane == 0) {
         Section_File << "TITLE = \"Nacelle Slices\"" << endl;
         if (config->GetSystemMeasurements() == US)
-          Section_File << "VARIABLES = \"x (in)\", \"y (in)\", \"z (in)\", \"x<sub>2D</sub>/c\", \"y<sub>2D</sub>/c\""
+          Section_File << R"lit(VARIABLES = "x (in)", "y (in)", "z (in)", "x<sub>2D</sub>/c", "y<sub>2D</sub>/c")lit"
                        << endl;
         else
-          Section_File << "VARIABLES = \"x (m)\", \"y (m)\", \"z (m)\", \"x<sub>2D</sub>/c\", \"y<sub>2D</sub>/c\""
+          Section_File << R"lit(VARIABLES = "x (m)", "y (m)", "z (m)", "x<sub>2D</sub>/c", "y<sub>2D</sub>/c")lit"
                        << endl;
       }
 
diff --git a/Common/src/geometry/dual_grid/CDualGrid.cpp b/Common/src/geometry/dual_grid/CDualGrid.cpp
index 2a277094bc6..99813fab93f 100644
--- a/Common/src/geometry/dual_grid/CDualGrid.cpp
+++ b/Common/src/geometry/dual_grid/CDualGrid.cpp
@@ -31,4 +31,4 @@ unsigned short CDualGrid::nDim = 0;
 
 CDualGrid::CDualGrid(unsigned short val_nDim) { nDim = val_nDim; }
 
-CDualGrid::~CDualGrid() {}
+CDualGrid::~CDualGrid() = default;
diff --git a/Common/src/geometry/dual_grid/CEdge.cpp b/Common/src/geometry/dual_grid/CEdge.cpp
index d3a45abeee1..5b3197d3f2f 100644
--- a/Common/src/geometry/dual_grid/CEdge.cpp
+++ b/Common/src/geometry/dual_grid/CEdge.cpp
@@ -38,7 +38,7 @@ CEdge::CEdge(unsigned long nEdge_, unsigned long nDim)
   Normal.resize(nEdgeSIMD, nDim) = su2double(0.0);
 }
 
-void CEdge::SetZeroValues(void) { Normal = su2double(0.0); }
+void CEdge::SetZeroValues() { Normal = su2double(0.0); }
 
 su2double CEdge::GetVolume(const su2double* coord_Edge_CG, const su2double* coord_FaceElem_CG,
                            const su2double* coord_Elem_CG, const su2double* coord_Point) {
diff --git a/Common/src/geometry/elements/CElement.cpp b/Common/src/geometry/elements/CElement.cpp
index 91c41d7ff9a..2c4c5dd38a3 100644
--- a/Common/src/geometry/elements/CElement.cpp
+++ b/Common/src/geometry/elements/CElement.cpp
@@ -65,7 +65,7 @@ CElement::CElement(unsigned short ngauss, unsigned short nnodes, unsigned short
   ClearElement();
 }
 
-void CElement::ClearElement(void) {
+void CElement::ClearElement() {
   Mab.setConstant(0.0);
   Kt_a.setConstant(0.0);
   FDL_a.setConstant(0.0);
diff --git a/Common/src/geometry/meshreader/CBoxMeshReaderFVM.cpp b/Common/src/geometry/meshreader/CBoxMeshReaderFVM.cpp
index 7d63be15052..6c14dc3a064 100644
--- a/Common/src/geometry/meshreader/CBoxMeshReaderFVM.cpp
+++ b/Common/src/geometry/meshreader/CBoxMeshReaderFVM.cpp
@@ -63,7 +63,7 @@ CBoxMeshReaderFVM::CBoxMeshReaderFVM(CConfig* val_config, unsigned short val_iZo
   ComputeBoxSurfaceConnectivity();
 }
 
-CBoxMeshReaderFVM::~CBoxMeshReaderFVM(void) {}
+CBoxMeshReaderFVM::~CBoxMeshReaderFVM() = default;
 
 void CBoxMeshReaderFVM::ComputeBoxPointCoordinates() {
   /* Set the global count of points based on the grid dimensions. */
diff --git a/Common/src/geometry/meshreader/CCGNSMeshReaderFVM.cpp b/Common/src/geometry/meshreader/CCGNSMeshReaderFVM.cpp
index 8c5019c9c53..81f5d1100ff 100644
--- a/Common/src/geometry/meshreader/CCGNSMeshReaderFVM.cpp
+++ b/Common/src/geometry/meshreader/CCGNSMeshReaderFVM.cpp
@@ -71,10 +71,10 @@ CCGNSMeshReaderFVM::CCGNSMeshReaderFVM(CConfig* val_config, unsigned short val_i
 #endif
 }
 
-CCGNSMeshReaderFVM::~CCGNSMeshReaderFVM(void) {}
+CCGNSMeshReaderFVM::~CCGNSMeshReaderFVM() = default;
 
 #ifdef HAVE_CGNS
-void CCGNSMeshReaderFVM::OpenCGNSFile(string val_filename) {
+void CCGNSMeshReaderFVM::OpenCGNSFile(const string& val_filename) {
   /*--- Check whether the supplied file is truly a CGNS file. ---*/
 
   int file_type;
@@ -227,7 +227,7 @@ void CCGNSMeshReaderFVM::ReadCGNSPointCoordinates() {
    +1 for CGNS convention. ---*/
 
   cgsize_t range_min = (cgsize_t)pointPartitioner.GetFirstIndexOnRank(rank) + 1;
-  cgsize_t range_max = (cgsize_t)pointPartitioner.GetLastIndexOnRank(rank);
+  auto range_max = (cgsize_t)pointPartitioner.GetLastIndexOnRank(rank);
 
   /*--- Loop over each set of coordinates. ---*/
 
@@ -340,7 +340,7 @@ void CCGNSMeshReaderFVM::ReadCGNSSectionMetadata() {
       /* Retrieve the connectivity information for the first element. */
 
       if (cg_poly_elements_partial_read(cgnsFileID, cgnsBase, cgnsZone, s + 1, startE, startE, connElemCGNS.data(),
-                                        connOffsetCGNS.data(), NULL) != CG_OK)
+                                        connOffsetCGNS.data(), nullptr) != CG_OK)
         cg_error_exit();
 
       /* The element type is in the first position of the connectivity
@@ -448,12 +448,12 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
       if (cg_poly_elements_partial_read(cgnsFileID, cgnsBase, cgnsZone, val_section + 1,
                                         (cgsize_t)elementPartitioner.GetFirstIndexOnRank(rank),
                                         (cgsize_t)elementPartitioner.GetLastIndexOnRank(rank), connElemCGNS.data(),
-                                        connOffsetCGNS.data(), NULL) != CG_OK)
+                                        connOffsetCGNS.data(), nullptr) != CG_OK)
         cg_error_exit();
     } else {
       if (cg_elements_partial_read(
               cgnsFileID, cgnsBase, cgnsZone, val_section + 1, (cgsize_t)elementPartitioner.GetFirstIndexOnRank(rank),
-              (cgsize_t)elementPartitioner.GetLastIndexOnRank(rank), connElemCGNS.data(), NULL) != CG_OK)
+              (cgsize_t)elementPartitioner.GetLastIndexOnRank(rank), connElemCGNS.data(), nullptr) != CG_OK)
         cg_error_exit();
     }
   }
@@ -629,7 +629,7 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
    We have assumed a constant message size of a hex element (8 nodes)
    + 2 extra values for the ID and VTK. ---*/
 
-  unsigned long *connSend = NULL, iSend = 0;
+  unsigned long *connSend = nullptr, iSend = 0;
   unsigned long sendSize = (unsigned long)SU2_CONN_SIZE * nElem_Send[size];
   connSend = new unsigned long[sendSize];
   for (iSend = 0; iSend < sendSize; iSend++) connSend[iSend] = 0;
@@ -688,15 +688,15 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
    we do not include our own rank in the communications. We will
    directly copy our own data later. ---*/
 
-  unsigned long *connRecv = NULL, iRecv = 0;
+  unsigned long *connRecv = nullptr, iRecv = 0;
   unsigned long recvSize = (unsigned long)SU2_CONN_SIZE * nElem_Recv[size];
   connRecv = new unsigned long[recvSize];
   for (iRecv = 0; iRecv < recvSize; iRecv++) connRecv[iRecv] = 0;
 
   /*--- Allocate memory for the MPI requests if we will communicate. ---*/
 
-  SU2_MPI::Request* connSendReq = NULL;
-  SU2_MPI::Request* connRecvReq = NULL;
+  SU2_MPI::Request* connSendReq = nullptr;
+  SU2_MPI::Request* connRecvReq = nullptr;
 
   if (nSends > 0) {
     connSendReq = new SU2_MPI::Request[nSends];
@@ -754,8 +754,8 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
 
   /*--- Free temporary memory from communications ---*/
 
-  if (connSendReq != NULL) delete[] connSendReq;
-  if (connRecvReq != NULL) delete[] connRecvReq;
+  if (connSendReq != nullptr) delete[] connSendReq;
+  if (connRecvReq != nullptr) delete[] connRecvReq;
 
   delete[] connSend;
   delete[] connRecv;
@@ -832,10 +832,11 @@ void CCGNSMeshReaderFVM::ReadCGNSSurfaceSection(int val_section) {
     if (elemType == MIXED || elemType == NGON_n || elemType == NFACE_n) {
       vector<cgsize_t> connOffsetTemp(nElems[val_section] + 1, 0);
       if (cg_poly_elements_partial_read(cgnsFileID, cgnsBase, cgnsZone, val_section + 1, startE, endE,
-                                        connElemTemp.data(), connOffsetTemp.data(), NULL) != CG_OK)
+                                        connElemTemp.data(), connOffsetTemp.data(), nullptr) != CG_OK)
         cg_error_exit();
     } else {
-      if (cg_elements_read(cgnsFileID, cgnsBase, cgnsZone, val_section + 1, connElemTemp.data(), NULL)) cg_error_exit();
+      if (cg_elements_read(cgnsFileID, cgnsBase, cgnsZone, val_section + 1, connElemTemp.data(), nullptr))
+        cg_error_exit();
     }
 
     /*--- Allocate the memory for the data structure used to carry
diff --git a/Common/src/geometry/meshreader/CSU2ASCIIMeshReaderFVM.cpp b/Common/src/geometry/meshreader/CSU2ASCIIMeshReaderFVM.cpp
index 272dafd79ed..a32c290c4d9 100644
--- a/Common/src/geometry/meshreader/CSU2ASCIIMeshReaderFVM.cpp
+++ b/Common/src/geometry/meshreader/CSU2ASCIIMeshReaderFVM.cpp
@@ -310,14 +310,14 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
         text_line.erase(0, 11);
         string::size_type position;
         for (unsigned short iChar = 0; iChar < 20; iChar++) {
-          position = text_line.find(" ", 0);
+          position = text_line.find(' ', 0);
           if (position != string::npos) text_line.erase(position, 1);
-          position = text_line.find("\r", 0);
+          position = text_line.find('\r', 0);
           if (position != string::npos) text_line.erase(position, 1);
-          position = text_line.find("\n", 0);
+          position = text_line.find('\n', 0);
           if (position != string::npos) text_line.erase(position, 1);
         }
-        string Marker_Tag = text_line.c_str();
+        string Marker_Tag = text_line;
 
         getline(mesh_file, text_line);
         text_line.erase(0, 13);
@@ -414,14 +414,14 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
           if (dimension == 3) {
             /*--- Check the begning of the list ---*/
 
-            if (!((EdgeBegin[0] == EdgeBegin[1]) && (EdgeEnd[0] == EdgeEnd[1]))) {
+            if ((EdgeBegin[0] != EdgeBegin[1]) || (EdgeEnd[0] != EdgeEnd[1])) {
               PerimeterPoint.push_back(EdgeBegin[0]);
               PerimeterPoint.push_back(EdgeEnd[0]);
             }
 
             for (iEdge = 1; iEdge < nEdges - 1; iEdge++) {
-              bool Check_1 = !((EdgeBegin[iEdge] == EdgeBegin[iEdge - 1]) && (EdgeEnd[iEdge] == EdgeEnd[iEdge - 1]));
-              bool Check_2 = !((EdgeBegin[iEdge] == EdgeBegin[iEdge + 1]) && (EdgeEnd[iEdge] == EdgeEnd[iEdge + 1]));
+              bool Check_1 = (EdgeBegin[iEdge] != EdgeBegin[iEdge - 1]) || (EdgeEnd[iEdge] != EdgeEnd[iEdge - 1]);
+              bool Check_2 = (EdgeBegin[iEdge] != EdgeBegin[iEdge + 1]) || (EdgeEnd[iEdge] != EdgeEnd[iEdge + 1]);
               if ((Check_1 && Check_2)) {
                 PerimeterPoint.push_back(EdgeBegin[iEdge]);
                 PerimeterPoint.push_back(EdgeEnd[iEdge]);
@@ -430,7 +430,7 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
 
             /*--- Check the  end of the list ---*/
 
-            if (!((EdgeBegin[nEdges - 1] == EdgeBegin[nEdges - 2]) && (EdgeEnd[nEdges - 1] == EdgeEnd[nEdges - 2]))) {
+            if ((EdgeBegin[nEdges - 1] != EdgeBegin[nEdges - 2]) || (EdgeEnd[nEdges - 1] != EdgeEnd[nEdges - 2])) {
               PerimeterPoint.push_back(EdgeBegin[nEdges - 1]);
               PerimeterPoint.push_back(EdgeEnd[nEdges - 1]);
             }
@@ -444,7 +444,7 @@ void CSU2ASCIIMeshReaderFVM::SplitActuatorDiskSurface() {
             }
 
             sort(ActDiskPoint_Front.begin(), ActDiskPoint_Front.end());
-            vector<unsigned long>::iterator it = unique(ActDiskPoint_Front.begin(), ActDiskPoint_Front.end());
+            auto it = unique(ActDiskPoint_Front.begin(), ActDiskPoint_Front.end());
             ActDiskPoint_Front.resize(it - ActDiskPoint_Front.begin());
 
             /*--- Check the begning of the list ---*/
@@ -959,11 +959,11 @@ void CSU2ASCIIMeshReaderFVM::ReadSurfaceElementConnectivity(const bool single_pa
       string::size_type position;
 
       for (unsigned short iChar = 0; iChar < 20; iChar++) {
-        position = text_line.find(" ", 0);
+        position = text_line.find(' ', 0);
         if (position != string::npos) text_line.erase(position, 1);
-        position = text_line.find("\r", 0);
+        position = text_line.find('\r', 0);
         if (position != string::npos) text_line.erase(position, 1);
-        position = text_line.find("\n", 0);
+        position = text_line.find('\n', 0);
         if (position != string::npos) text_line.erase(position, 1);
       }
       markerNames[iMarker] = text_line;
diff --git a/Common/src/geometry/primal_grid/CPrimalGridBoundFEM.cpp b/Common/src/geometry/primal_grid/CPrimalGridBoundFEM.cpp
index bd33fb325e5..f748cf6b298 100644
--- a/Common/src/geometry/primal_grid/CPrimalGridBoundFEM.cpp
+++ b/Common/src/geometry/primal_grid/CPrimalGridBoundFEM.cpp
@@ -98,7 +98,7 @@ void CPrimalGridBoundFEM::GetCornerPointsAllFaces(unsigned short& nFaces, unsign
   for (unsigned short j = 0; j < nPointsPerFace[0]; ++j) faceConn[0][j] = Nodes[thisFaceConn[j]];
 }
 
-void CPrimalGridBoundFEM::RemoveMultipleDonorsWallFunctions(void) {
+void CPrimalGridBoundFEM::RemoveMultipleDonorsWallFunctions() {
   /* Sort donorElementsWallFunctions in increasing order and remove the
      the double entities. */
   std::sort(donorElementsWallFunctions.begin(), donorElementsWallFunctions.end());
diff --git a/Common/src/geometry/primal_grid/CPrism.cpp b/Common/src/geometry/primal_grid/CPrism.cpp
index c3998a0ba0b..72726ab08be 100644
--- a/Common/src/geometry/primal_grid/CPrism.cpp
+++ b/Common/src/geometry/primal_grid/CPrism.cpp
@@ -45,7 +45,7 @@ CPrism::CPrism(unsigned long val_point_0, unsigned long val_point_1, unsigned lo
   Nodes[5] = val_point_5;
 }
 
-void CPrism::Change_Orientation(void) {
+void CPrism::Change_Orientation() {
   std::swap(Nodes[0], Nodes[1]);
   std::swap(Nodes[3], Nodes[4]);
 }
diff --git a/Common/src/grid_movement/CBSplineBlending.cpp b/Common/src/grid_movement/CBSplineBlending.cpp
index 8dad4572be6..29a1dda3f73 100644
--- a/Common/src/grid_movement/CBSplineBlending.cpp
+++ b/Common/src/grid_movement/CBSplineBlending.cpp
@@ -32,7 +32,7 @@ CBSplineBlending::CBSplineBlending(short val_order, short n_controlpoints) : CFr
   SetOrder(val_order, n_controlpoints);
 }
 
-CBSplineBlending::~CBSplineBlending() {}
+CBSplineBlending::~CBSplineBlending() = default;
 
 void CBSplineBlending::SetOrder(short val_order, short n_controlpoints) {
   unsigned short iKnot;
diff --git a/Common/src/grid_movement/CBezierBlending.cpp b/Common/src/grid_movement/CBezierBlending.cpp
index d24ebdbb974..0de026c0dba 100644
--- a/Common/src/grid_movement/CBezierBlending.cpp
+++ b/Common/src/grid_movement/CBezierBlending.cpp
@@ -30,7 +30,7 @@
 
 CBezierBlending::CBezierBlending(short val_order, short n_controlpoints) { SetOrder(val_order, n_controlpoints); }
 
-CBezierBlending::~CBezierBlending() {}
+CBezierBlending::~CBezierBlending() = default;
 
 void CBezierBlending::SetOrder(short val_order, short n_controlpoints) {
   Order = val_order;
diff --git a/Common/src/grid_movement/CFreeFormBlending.cpp b/Common/src/grid_movement/CFreeFormBlending.cpp
index 50aa23a131f..dbac22dc8a6 100644
--- a/Common/src/grid_movement/CFreeFormBlending.cpp
+++ b/Common/src/grid_movement/CFreeFormBlending.cpp
@@ -27,6 +27,6 @@
 
 #include "../../include/grid_movement/CFreeFormBlending.hpp"
 
-CFreeFormBlending::CFreeFormBlending() {}
+CFreeFormBlending::CFreeFormBlending() = default;
 
-CFreeFormBlending::~CFreeFormBlending() {}
+CFreeFormBlending::~CFreeFormBlending() = default;
diff --git a/Common/src/grid_movement/CFreeFormDefBox.cpp b/Common/src/grid_movement/CFreeFormDefBox.cpp
index 0d0ca8351c3..f1540771192 100644
--- a/Common/src/grid_movement/CFreeFormDefBox.cpp
+++ b/Common/src/grid_movement/CFreeFormDefBox.cpp
@@ -29,7 +29,7 @@
 #include "../../include/grid_movement/CBezierBlending.hpp"
 #include "../../include/grid_movement/CBSplineBlending.hpp"
 
-CFreeFormDefBox::CFreeFormDefBox(void) : CGridMovement() {}
+CFreeFormDefBox::CFreeFormDefBox() : CGridMovement() {}
 
 CFreeFormDefBox::CFreeFormDefBox(const unsigned short Degree[], unsigned short BSplineOrder[],
                                  unsigned short kind_blending)
@@ -107,7 +107,7 @@ CFreeFormDefBox::CFreeFormDefBox(const unsigned short Degree[], unsigned short B
   }
 }
 
-CFreeFormDefBox::~CFreeFormDefBox(void) {
+CFreeFormDefBox::~CFreeFormDefBox() {
   unsigned short iOrder, jOrder, kOrder, iCornerPoints, iDim;
 
   for (iOrder = 0; iOrder < lOrder; iOrder++) {
@@ -149,9 +149,9 @@ CFreeFormDefBox::~CFreeFormDefBox(void) {
   delete[] BlendingFunction;
 }
 
-void CFreeFormDefBox::SetUnitCornerPoints(void) {
+void CFreeFormDefBox::SetUnitCornerPoints() {
   unsigned short iDim;
-  su2double* coord = new su2double[nDim];
+  auto* coord = new su2double[nDim];
 
   for (iDim = 0; iDim < nDim; iDim++) coord[iDim] = 0.0;
 
@@ -191,7 +191,7 @@ void CFreeFormDefBox::SetUnitCornerPoints(void) {
   delete[] coord;
 }
 
-void CFreeFormDefBox::SetControlPoints_Parallelepiped(void) {
+void CFreeFormDefBox::SetControlPoints_Parallelepiped() const {
   unsigned short iDim, iDegree, jDegree, kDegree;
 
   /*--- Set base control points according to the notation of Vtk for hexahedrons ---*/
@@ -265,14 +265,14 @@ void CFreeFormDefBox::SetSupportCP(CFreeFormDefBox* FFDBox) {
       }
 }
 
-void CFreeFormDefBox::SetSupportCPChange(CFreeFormDefBox* FFDBox) {
+void CFreeFormDefBox::SetSupportCPChange(CFreeFormDefBox* FFDBox) const {
   unsigned short iDim, iOrder, jOrder, kOrder;
   su2double *CartCoordNew, *ParamCoord;
   unsigned short lOrder = FFDBox->GetlOrder();
   unsigned short mOrder = FFDBox->GetmOrder();
   unsigned short nOrder = FFDBox->GetnOrder();
 
-  su2double**** ParamCoord_SupportCP = new su2double***[lOrder];
+  auto**** ParamCoord_SupportCP = new su2double***[lOrder];
   for (iOrder = 0; iOrder < lOrder; iOrder++) {
     ParamCoord_SupportCP[iOrder] = new su2double**[mOrder];
     for (jOrder = 0; jOrder < mOrder; jOrder++) {
@@ -310,7 +310,7 @@ void CFreeFormDefBox::SetSupportCPChange(CFreeFormDefBox* FFDBox) {
   }
 }
 
-void CFreeFormDefBox::SetCart2Cyl_ControlPoints(CConfig* config) {
+void CFreeFormDefBox::SetCart2Cyl_ControlPoints(CConfig* config) const {
   unsigned short iDegree, jDegree, kDegree;
   su2double CartCoord[3];
   su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
@@ -354,7 +354,7 @@ void CFreeFormDefBox::SetCart2Cyl_ControlPoints(CConfig* config) {
   }
 }
 
-void CFreeFormDefBox::SetCyl2Cart_ControlPoints(CConfig* config) {
+void CFreeFormDefBox::SetCyl2Cart_ControlPoints(CConfig* config) const {
   unsigned short iDegree, jDegree, kDegree;
   su2double PolarCoord[3];
 
@@ -386,7 +386,7 @@ void CFreeFormDefBox::SetCyl2Cart_ControlPoints(CConfig* config) {
   }
 }
 
-void CFreeFormDefBox::SetCart2Cyl_CornerPoints(CConfig* config) {
+void CFreeFormDefBox::SetCart2Cyl_CornerPoints(CConfig* config) const {
   unsigned short iCornerPoint;
   su2double* CartCoord;
   su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
@@ -408,7 +408,7 @@ void CFreeFormDefBox::SetCart2Cyl_CornerPoints(CConfig* config) {
   }
 }
 
-void CFreeFormDefBox::SetCyl2Cart_CornerPoints(CConfig* config) {
+void CFreeFormDefBox::SetCyl2Cart_CornerPoints(CConfig* config) const {
   unsigned short iCornerPoint;
   su2double* PolarCoord;
   su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
@@ -430,7 +430,7 @@ void CFreeFormDefBox::SetCyl2Cart_CornerPoints(CConfig* config) {
   }
 }
 
-void CFreeFormDefBox::SetCart2Sphe_ControlPoints(CConfig* config) {
+void CFreeFormDefBox::SetCart2Sphe_ControlPoints(CConfig* config) const {
   unsigned short iDegree, jDegree, kDegree;
   su2double CartCoord[3];
   su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
@@ -476,7 +476,7 @@ void CFreeFormDefBox::SetCart2Sphe_ControlPoints(CConfig* config) {
   }
 }
 
-void CFreeFormDefBox::SetSphe2Cart_ControlPoints(CConfig* config) {
+void CFreeFormDefBox::SetSphe2Cart_ControlPoints(CConfig* config) const {
   unsigned short iDegree, jDegree, kDegree;
   su2double PolarCoord[3];
 
@@ -508,7 +508,7 @@ void CFreeFormDefBox::SetSphe2Cart_ControlPoints(CConfig* config) {
   }
 }
 
-void CFreeFormDefBox::SetCart2Sphe_CornerPoints(CConfig* config) {
+void CFreeFormDefBox::SetCart2Sphe_CornerPoints(CConfig* config) const {
   unsigned short iCornerPoint;
   su2double* CartCoord;
   su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
@@ -530,7 +530,7 @@ void CFreeFormDefBox::SetCart2Sphe_CornerPoints(CConfig* config) {
   }
 }
 
-void CFreeFormDefBox::SetSphe2Cart_CornerPoints(CConfig* config) {
+void CFreeFormDefBox::SetSphe2Cart_CornerPoints(CConfig* config) const {
   unsigned short iCornerPoint;
   su2double* PolarCoord;
   su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
@@ -573,10 +573,7 @@ void CFreeFormDefBox::SetCGNS(CGeometry* geometry, unsigned short iFFDBox, bool
 
   SPRINTF(FFDBox_filename, "ffd_boxes.cgns");
 
-  if ((original) && (iFFDBox == 0))
-    new_file = true;
-  else
-    new_file = false;
+  new_file = (original) && (iFFDBox == 0);
 
   if (new_file) {
     cgns_err = cg_open(FFDBox_filename, CG_MODE_WRITE, &FFDBox_cgns_file);
@@ -614,7 +611,7 @@ void CFreeFormDefBox::SetCGNS(CGeometry* geometry, unsigned short iFFDBox, bool
     pointlen *= dims[ii];
   }
 
-  passivedouble* buffer = new passivedouble[pointlen];
+  auto* buffer = new passivedouble[pointlen];
   SPRINTF(zonename, "SU2_Zone_%d", SU2_TYPE::Int(iFFDBox));
 
   cgns_err = cg_zone_write(FFDBox_cgns_file, cgns_base, zonename, dims, CGNS_ENUMV(Structured), &cgns_zone);
@@ -668,18 +665,15 @@ void CFreeFormDefBox::SetTecplot(CGeometry* geometry, unsigned short iFFDBox, bo
 
   SPRINTF(FFDBox_filename, "ffd_boxes.dat");
 
-  if ((original) && (iFFDBox == 0))
-    new_file = true;
-  else
-    new_file = false;
+  new_file = (original) && (iFFDBox == 0);
 
   if (new_file) {
     FFDBox_file.open(FFDBox_filename, ios::out);
     FFDBox_file << "TITLE = \"Visualization of the FFD boxes generated by SU2_DEF.\"" << endl;
     if (nDim == 2)
-      FFDBox_file << "VARIABLES = \"x\", \"y\"" << endl;
+      FFDBox_file << R"(VARIABLES = "x", "y")" << endl;
     else
-      FFDBox_file << "VARIABLES = \"x\", \"y\", \"z\"" << endl;
+      FFDBox_file << R"(VARIABLES = "x", "y", "z")" << endl;
   } else
     FFDBox_file.open(FFDBox_filename, ios::out | ios::app);
 
@@ -727,10 +721,7 @@ void CFreeFormDefBox::SetParaview(CGeometry* geometry, unsigned short iFFDBox, b
 
   nDim = geometry->GetnDim();
 
-  if (original)
-    new_file = true;
-  else
-    new_file = false;
+  new_file = original;
 
   if (new_file)
     SPRINTF(FFDBox_filename, "ffd_boxes_%d.vtk", SU2_TYPE::Int(iFFDBox));
@@ -1138,11 +1129,11 @@ su2double CFreeFormDefBox::GetDerivative2(su2double* uvw, unsigned short dim, co
 }
 
 su2double CFreeFormDefBox::GetDerivative3(su2double* uvw, unsigned short dim, unsigned short diff_this,
-                                          unsigned short* lmn) {
+                                          unsigned short* lmn) const {
   unsigned short iDegree, jDegree, kDegree, iDim;
   su2double value = 0;
 
-  unsigned short* ijk = new unsigned short[nDim];
+  auto* ijk = new unsigned short[nDim];
 
   for (iDim = 0; iDim < nDim; iDim++) ijk[iDim] = 0;
 
@@ -1180,11 +1171,11 @@ su2double CFreeFormDefBox::GetDerivative4(su2double* uvw, unsigned short val_dif
 }
 
 su2double CFreeFormDefBox::GetDerivative5(su2double* uvw, unsigned short dim, unsigned short diff_this,
-                                          unsigned short diff_this_also, unsigned short* lmn) {
+                                          unsigned short diff_this_also, unsigned short* lmn) const {
   unsigned short iDegree, jDegree, kDegree, iDim;
   su2double value = 0.0;
 
-  unsigned short* ijk = new unsigned short[nDim];
+  auto* ijk = new unsigned short[nDim];
 
   for (iDim = 0; iDim < nDim; iDim++) ijk[iDim] = 0;
 
diff --git a/Common/src/grid_movement/CGridMovement.cpp b/Common/src/grid_movement/CGridMovement.cpp
index 656583439b4..e11b46b4ae6 100644
--- a/Common/src/grid_movement/CGridMovement.cpp
+++ b/Common/src/grid_movement/CGridMovement.cpp
@@ -27,6 +27,6 @@
 
 #include "../../include/grid_movement/CGridMovement.hpp"
 
-CGridMovement::CGridMovement(void) {}
+CGridMovement::CGridMovement() = default;
 
-CGridMovement::~CGridMovement(void) {}
+CGridMovement::~CGridMovement() = default;
diff --git a/Common/src/grid_movement/CSurfaceMovement.cpp b/Common/src/grid_movement/CSurfaceMovement.cpp
index 0834e05c426..1c3b49a8b96 100644
--- a/Common/src/grid_movement/CSurfaceMovement.cpp
+++ b/Common/src/grid_movement/CSurfaceMovement.cpp
@@ -28,7 +28,7 @@
 #include "../../include/grid_movement/CSurfaceMovement.hpp"
 #include "../../include/toolboxes/C1DInterpolation.hpp"
 
-CSurfaceMovement::CSurfaceMovement(void) : CGridMovement() {
+CSurfaceMovement::CSurfaceMovement() : CGridMovement() {
   size = SU2_MPI::GetSize();
   rank = SU2_MPI::GetRank();
 
@@ -37,7 +37,7 @@ CSurfaceMovement::CSurfaceMovement(void) : CGridMovement() {
   FFDBoxDefinition = false;
 }
 
-CSurfaceMovement::~CSurfaceMovement(void) {}
+CSurfaceMovement::~CSurfaceMovement() = default;
 
 vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry* geometry, CConfig* config) {
   unsigned short iFFDBox, iDV, iLevel, iChild, iParent, jFFDBox, iMarker;
@@ -1314,30 +1314,12 @@ void CSurfaceMovement::CheckFFDIntersections(CGeometry* geometry, CConfig* confi
 
 #endif
 
-    if (Code[0] != 0)
-      IPlane_Intersect_A = true;
-    else
-      IPlane_Intersect_A = false;
-    if (Code[1] != 0)
-      IPlane_Intersect_B = true;
-    else
-      IPlane_Intersect_B = false;
-    if (Code[2] != 0)
-      JPlane_Intersect_A = true;
-    else
-      JPlane_Intersect_A = false;
-    if (Code[3] != 0)
-      JPlane_Intersect_B = true;
-    else
-      JPlane_Intersect_B = false;
-    if (Code[4] != 0)
-      KPlane_Intersect_A = true;
-    else
-      KPlane_Intersect_A = false;
-    if (Code[5] != 0)
-      KPlane_Intersect_B = true;
-    else
-      KPlane_Intersect_B = false;
+    IPlane_Intersect_A = Code[0] != 0;
+    IPlane_Intersect_B = Code[1] != 0;
+    JPlane_Intersect_A = Code[2] != 0;
+    JPlane_Intersect_B = Code[3] != 0;
+    KPlane_Intersect_A = Code[4] != 0;
+    KPlane_Intersect_B = Code[5] != 0;
 
     /*--- Screen output ---*/
 
@@ -1730,7 +1712,7 @@ bool CSurfaceMovement::SetFFDCPChange_2D(CGeometry* geometry, CConfig* config, C
   /*--- Set control points to its original value (even if the
    design variable is not in this box) ---*/
 
-  if (ResetDef == true) {
+  if (ResetDef) {
     for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
   }
 
@@ -1869,7 +1851,7 @@ bool CSurfaceMovement::SetFFDCPChange(CGeometry* geometry, CConfig* config, CFre
   /*--- Set control points to its original value (even if the
    design variable is not in this box) ---*/
 
-  if (ResetDef == true) {
+  if (ResetDef) {
     FFDBox->SetOriginalControlPoints();
     for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
   }
@@ -2010,7 +1992,7 @@ bool CSurfaceMovement::SetFFDGull(CGeometry* geometry, CConfig* config, CFreeFor
   /*--- Set control points to its original value (even if the
    design variable is not in this box) ---*/
 
-  if (ResetDef == true) {
+  if (ResetDef) {
     FFDBox->SetOriginalControlPoints();
     for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
   }
@@ -2062,7 +2044,7 @@ bool CSurfaceMovement::SetFFDNacelle(CGeometry* geometry, CConfig* config, CFree
   /*--- Set control points to its original value (even if the
    design variable is not in this box) ---*/
 
-  if (ResetDef == true) {
+  if (ResetDef) {
     FFDBox->SetOriginalControlPoints();
     for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
   }
@@ -2183,7 +2165,7 @@ bool CSurfaceMovement::SetFFDCamber_2D(CGeometry* geometry, CConfig* config, CFr
   /*--- Set control points to its original value (even if the
    design variable is not in this box) ---*/
 
-  if (ResetDef == true) {
+  if (ResetDef) {
     for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
   }
 
@@ -2226,7 +2208,7 @@ bool CSurfaceMovement::SetFFDThickness_2D(CGeometry* geometry, CConfig* config,
   /*--- Set control points to its original value (even if the
    design variable is not in this box) ---*/
 
-  if (ResetDef == true) {
+  if (ResetDef) {
     for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
   }
 
@@ -2274,7 +2256,7 @@ bool CSurfaceMovement::SetFFDCamber(CGeometry* geometry, CConfig* config, CFreeF
   /*--- Set control points to its original value (even if the
    design variable is not in this box) ---*/
 
-  if (ResetDef == true) {
+  if (ResetDef) {
     for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
   }
 
@@ -2344,7 +2326,7 @@ bool CSurfaceMovement::SetFFDThickness(CGeometry* geometry, CConfig* config, CFr
   /*--- Set control points to its original value (even if the
    design variable is not in this box) ---*/
 
-  if (ResetDef == true) {
+  if (ResetDef) {
     for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
   }
 
@@ -2407,7 +2389,7 @@ bool CSurfaceMovement::SetFFDTwist(CGeometry* geometry, CConfig* config, CFreeFo
   /*--- Set control points to its original value (even if the
    design variable is not in this box) ---*/
 
-  if (ResetDef == true) {
+  if (ResetDef) {
     for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
   }
 
@@ -2552,7 +2534,7 @@ bool CSurfaceMovement::SetFFDRotation(CGeometry* geometry, CConfig* config, CFre
   /*--- Set control points to its original value (even if the
    design variable is not in this box) ---*/
 
-  if (ResetDef == true) {
+  if (ResetDef) {
     for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
   }
 
@@ -2632,7 +2614,7 @@ bool CSurfaceMovement::SetFFDControl_Surface(CGeometry* geometry, CConfig* confi
   /*--- Set control points to its original value (even if the
    design variable is not in this box) ---*/
 
-  if (ResetDef == true) {
+  if (ResetDef) {
     for (iFFDBox = 0; iFFDBox < nFFDBox; iFFDBox++) ResetFFDBox[iFFDBox]->SetOriginalControlPoints();
   }
 
@@ -2719,7 +2701,7 @@ void CSurfaceMovement::SetHicksHenne(CGeometry* boundary, CConfig* config, unsig
 
   /*--- Reset airfoil deformation if first deformation or if it required by the solver ---*/
 
-  if ((iDV == 0) || (ResetDef == true)) {
+  if ((iDV == 0) || (ResetDef)) {
     for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++)
       for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
         VarCoord[0] = 0.0;
@@ -2897,7 +2879,7 @@ void CSurfaceMovement::SetSurface_Bump(CGeometry* boundary, CConfig* config, uns
 
   /*--- Reset airfoil deformation if first deformation or if it required by the solver ---*/
 
-  if ((iDV == 0) || (ResetDef == true)) {
+  if ((iDV == 0) || (ResetDef)) {
     for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++)
       for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
         VarCoord[0] = 0.0;
@@ -2957,7 +2939,7 @@ void CSurfaceMovement::SetCST(CGeometry* boundary, CConfig* config, unsigned sho
 
   /*--- Reset airfoil deformation if first deformation or if it required by the solver ---*/
 
-  if ((iDV == 0) || (ResetDef == true)) {
+  if ((iDV == 0) || (ResetDef)) {
     for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++)
       for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
         VarCoord[0] = 0.0;
@@ -3158,7 +3140,7 @@ void CSurfaceMovement::SetRotation(CGeometry* boundary, CConfig* config, unsigne
 
   /*--- Reset airfoil deformation if first deformation or if it required by the solver ---*/
 
-  if ((iDV == 0) || (ResetDef == true)) {
+  if ((iDV == 0) || (ResetDef)) {
     for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++)
       for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
         VarCoord[0] = 0.0;
@@ -3242,7 +3224,7 @@ void CSurfaceMovement::SetTranslation(CGeometry* boundary, CConfig* config, unsi
 
   /*--- Reset airfoil deformation if first deformation or if it required by the solver ---*/
 
-  if ((iDV == 0) || (ResetDef == true)) {
+  if ((iDV == 0) || (ResetDef)) {
     for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++)
       for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
         VarCoord[0] = 0.0;
@@ -3280,7 +3262,7 @@ void CSurfaceMovement::SetScale(CGeometry* boundary, CConfig* config, unsigned s
 
   /*--- Reset airfoil deformation if first deformation or if it required by the solver ---*/
 
-  if ((iDV == 0) || (ResetDef == true)) {
+  if ((iDV == 0) || (ResetDef)) {
     for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++)
       for (iVertex = 0; iVertex < boundary->nVertex[iMarker]; iVertex++) {
         VarCoord[0] = 0.0;
@@ -3436,7 +3418,7 @@ void CSurfaceMovement::SetBoundary_Flutter3D(CGeometry* geometry, CConfig* confi
   short iFFDBox;
   su2double movement[3] = {0.0, 0.0, 0.0};
   bool* move = new bool[nFFDBox];
-  unsigned short* index = new unsigned short[3];
+  auto* index = new unsigned short[3];
 
   move[0] = true;
   move[1] = true;
@@ -3499,7 +3481,7 @@ void CSurfaceMovement::SetExternal_Deformation(CGeometry* geometry, CConfig* con
        physical time, so perform mesh motion in reverse. ---*/
       unsigned long nFlowIter = config->GetnTime_Iter() - 1;
       flowIter = nFlowIter - iter;
-      unsigned short lastindex = DV_Filename.find_last_of(".");
+      unsigned short lastindex = DV_Filename.find_last_of('.');
       DV_Filename = DV_Filename.substr(0, lastindex);
       if ((SU2_TYPE::Int(flowIter) >= 0) && (SU2_TYPE::Int(flowIter) < 10))
         SPRINTF(buffer, "_0000%d.dat", SU2_TYPE::Int(flowIter));
@@ -3515,7 +3497,7 @@ void CSurfaceMovement::SetExternal_Deformation(CGeometry* geometry, CConfig* con
     } else {
       /*--- Forward time for the direct problem ---*/
       flowIter = iter;
-      unsigned short lastindex = DV_Filename.find_last_of(".");
+      unsigned short lastindex = DV_Filename.find_last_of('.');
       DV_Filename = DV_Filename.substr(0, lastindex);
       if ((SU2_TYPE::Int(flowIter) >= 0) && (SU2_TYPE::Int(flowIter) < 10))
         SPRINTF(buffer, "_0000%d.dat", SU2_TYPE::Int(flowIter));
@@ -3846,7 +3828,7 @@ void CSurfaceMovement::SetAirfoil(CGeometry* boundary, CConfig* config) {
       /*--- Store the coordinates in vectors ---*/
 
       Xcoord.push_back(Airfoil_Coord[0]);
-      Ycoord.push_back(Airfoil_Coord[1] * factor * AirfoilScale);
+      Ycoord.emplace_back(Airfoil_Coord[1] * factor * AirfoilScale);
     }
   }
   if (strcmp(AirfoilFormat, "Lednicer") == 0) {
@@ -3907,8 +3889,8 @@ void CSurfaceMovement::SetAirfoil(CGeometry* boundary, CConfig* config) {
     Ycoord.insert(Ycoord.begin(), 0.0);
   }
   if (AddEnd) {
-    Xcoord.push_back(1.0);
-    Ycoord.push_back(0.0);
+    Xcoord.emplace_back(1.0);
+    Ycoord.emplace_back(0.0);
   }
 
   /*--- Change the orientation (depend on the input file, and the mesh file) ---*/
@@ -4032,7 +4014,7 @@ void CSurfaceMovement::SetAirfoil(CGeometry* boundary, CConfig* config) {
 }
 
 void CSurfaceMovement::ReadFFDInfo(CGeometry* geometry, CConfig* config, CFreeFormDefBox** FFDBox,
-                                   string val_mesh_filename) {
+                                   const string& val_mesh_filename) {
   string text_line, iTag;
   ifstream mesh_file;
   su2double CPcoord[3], coord[] = {0, 0, 0};
@@ -4121,15 +4103,15 @@ void CSurfaceMovement::ReadFFDInfo(CGeometry* geometry, CConfig* config, CFreeFo
 
         string::size_type position;
         for (iChar = 0; iChar < 20; iChar++) {
-          position = text_line.find(" ", 0);
+          position = text_line.find(' ', 0);
           if (position != string::npos) text_line.erase(position, 1);
-          position = text_line.find("\r", 0);
+          position = text_line.find('\r', 0);
           if (position != string::npos) text_line.erase(position, 1);
-          position = text_line.find("\n", 0);
+          position = text_line.find('\n', 0);
           if (position != string::npos) text_line.erase(position, 1);
         }
 
-        string TagFFDBox = text_line.c_str();
+        string TagFFDBox = text_line;
 
         if (rank == MASTER_NODE) cout << "FFD box tag: " << TagFFDBox << ". ";
 
@@ -4244,15 +4226,15 @@ void CSurfaceMovement::ReadFFDInfo(CGeometry* geometry, CConfig* config, CFreeFo
 
           string::size_type position;
           for (iChar = 0; iChar < 20; iChar++) {
-            position = text_line.find(" ", 0);
+            position = text_line.find(' ', 0);
             if (position != string::npos) text_line.erase(position, 1);
-            position = text_line.find("\r", 0);
+            position = text_line.find('\r', 0);
             if (position != string::npos) text_line.erase(position, 1);
-            position = text_line.find("\n", 0);
+            position = text_line.find('\n', 0);
             if (position != string::npos) text_line.erase(position, 1);
           }
 
-          string ParentFFDBox = text_line.c_str();
+          string ParentFFDBox = text_line;
           FFDBox[iFFDBox]->SetParentFFDBox(ParentFFDBox);
         }
 
@@ -4270,15 +4252,15 @@ void CSurfaceMovement::ReadFFDInfo(CGeometry* geometry, CConfig* config, CFreeFo
 
           string::size_type position;
           for (iChar = 0; iChar < 20; iChar++) {
-            position = text_line.find(" ", 0);
+            position = text_line.find(' ', 0);
             if (position != string::npos) text_line.erase(position, 1);
-            position = text_line.find("\r", 0);
+            position = text_line.find('\r', 0);
             if (position != string::npos) text_line.erase(position, 1);
-            position = text_line.find("\n", 0);
+            position = text_line.find('\n', 0);
             if (position != string::npos) text_line.erase(position, 1);
           }
 
-          string ChildFFDBox = text_line.c_str();
+          string ChildFFDBox = text_line;
           FFDBox[iFFDBox]->SetChildFFDBox(ChildFFDBox);
         }
 
@@ -4738,19 +4720,19 @@ void CSurfaceMovement::MergeFFDInfo(CGeometry* geometry, CConfig* config) {
 
     /*--- Send and Recv buffers. ---*/
 
-    su2double* Buffer_Send_X = new su2double[MaxLocalPoint];
+    auto* Buffer_Send_X = new su2double[MaxLocalPoint];
     su2double* Buffer_Recv_X = nullptr;
 
-    su2double* Buffer_Send_Y = new su2double[MaxLocalPoint];
+    auto* Buffer_Send_Y = new su2double[MaxLocalPoint];
     su2double* Buffer_Recv_Y = nullptr;
 
-    su2double* Buffer_Send_Z = new su2double[MaxLocalPoint];
+    auto* Buffer_Send_Z = new su2double[MaxLocalPoint];
     su2double* Buffer_Recv_Z = nullptr;
 
-    unsigned long* Buffer_Send_Point = new unsigned long[MaxLocalPoint];
+    auto* Buffer_Send_Point = new unsigned long[MaxLocalPoint];
     unsigned long* Buffer_Recv_Point = nullptr;
 
-    unsigned short* Buffer_Send_MarkerIndex_CfgFile = new unsigned short[MaxLocalPoint];
+    auto* Buffer_Send_MarkerIndex_CfgFile = new unsigned short[MaxLocalPoint];
     unsigned short* Buffer_Recv_MarkerIndex_CfgFile = nullptr;
 
     /*--- Prepare the receive buffers in the master node only. ---*/
@@ -4907,7 +4889,7 @@ void CSurfaceMovement::WriteFFDInfo(CSurfaceMovement** surface_movement, CGeomet
     /*--- Read the name of the output file ---*/
 
     auto str = config[ZONE_0]->GetMesh_Out_FileName();
-    unsigned short lastindex = str.find_last_of(".");
+    unsigned short lastindex = str.find_last_of('.');
     str = str.substr(0, lastindex) + ".su2";
 
     output_file.precision(15);
diff --git a/Common/src/grid_movement/CVolumetricMovement.cpp b/Common/src/grid_movement/CVolumetricMovement.cpp
index b1c9ff10f7d..abb1e140968 100644
--- a/Common/src/grid_movement/CVolumetricMovement.cpp
+++ b/Common/src/grid_movement/CVolumetricMovement.cpp
@@ -29,7 +29,7 @@
 #include "../../include/adt/CADTPointsOnlyClass.hpp"
 #include "../../include/toolboxes/geometry_toolbox.hpp"
 
-CVolumetricMovement::CVolumetricMovement(void) : CGridMovement(), System(LINEAR_SOLVER_MODE::MESH_DEFORM) {}
+CVolumetricMovement::CVolumetricMovement() : CGridMovement(), System(LINEAR_SOLVER_MODE::MESH_DEFORM) {}
 
 CVolumetricMovement::CVolumetricMovement(CGeometry* geometry, CConfig* config)
     : CGridMovement(), System(LINEAR_SOLVER_MODE::MESH_DEFORM) {
@@ -54,7 +54,7 @@ CVolumetricMovement::CVolumetricMovement(CGeometry* geometry, CConfig* config)
   }
 }
 
-CVolumetricMovement::~CVolumetricMovement(void) {}
+CVolumetricMovement::~CVolumetricMovement() = default;
 
 void CVolumetricMovement::UpdateGridCoord(CGeometry* geometry, CConfig* config) {
   unsigned short iDim;
@@ -1824,7 +1824,7 @@ void CVolumetricMovement::UpdateGridCoord_Derivatives(CGeometry* geometry, CConf
                                                       bool ForwardProjectionDerivative) {
   unsigned short iDim, iMarker;
   unsigned long iPoint, total_index, iVertex;
-  su2double* new_coord = new su2double[3];
+  auto* new_coord = new su2double[3];
 
   SU2_COMPONENT Kind_SU2 = config->GetKind_SU2();
 
diff --git a/Common/src/interface_interpolation/CIsoparametric.cpp b/Common/src/interface_interpolation/CIsoparametric.cpp
index f8ed1c6b588..19a68a3b423 100644
--- a/Common/src/interface_interpolation/CIsoparametric.cpp
+++ b/Common/src/interface_interpolation/CIsoparametric.cpp
@@ -40,7 +40,7 @@ CIsoparametric::CIsoparametric(CGeometry**** geometry_container, const CConfig*
   SetTransferCoeff(config);
 }
 
-void CIsoparametric::PrintStatistics(void) const {
+void CIsoparametric::PrintStatistics() const {
   if (rank != MASTER_NODE) return;
   cout << "  Maximum distance to closest donor element: " << MaxDistance << ".\n"
        << "  Interpolation clipped for " << ErrorCounter << " (" << ErrorRate << "%) target vertices." << endl;
diff --git a/Common/src/interface_interpolation/CSlidingMesh.cpp b/Common/src/interface_interpolation/CSlidingMesh.cpp
index ca01a7d43df..9e1cfbef8f5 100644
--- a/Common/src/interface_interpolation/CSlidingMesh.cpp
+++ b/Common/src/interface_interpolation/CSlidingMesh.cpp
@@ -548,11 +548,11 @@ void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
 
               /*--- Check if the node to visit is already listed in the data structure to avoid double visits ---*/
 
-              check = 0;
+              check = false;
 
               for (jj = 0; jj < nAlreadyVisited; jj++) {
                 if (donor_iPoint == alreadyVisitedDonor[jj]) {
-                  check = 1;
+                  check = true;
                   break;
                 }
               }
@@ -560,7 +560,7 @@ void CSlidingMesh::SetTransferCoeff(const CConfig* const* config) {
               if (check == 0 && ToVisit != nullptr) {
                 for (jj = 0; jj < nToVisit; jj++)
                   if (donor_iPoint == ToVisit[jj]) {
-                    check = 1;
+                    check = true;
                     break;
                   }
               }
diff --git a/Common/src/linear_algebra/CSysMatrix.cpp b/Common/src/linear_algebra/CSysMatrix.cpp
index fa84ecfa131..073fe40cdae 100644
--- a/Common/src/linear_algebra/CSysMatrix.cpp
+++ b/Common/src/linear_algebra/CSysMatrix.cpp
@@ -62,7 +62,7 @@ CSysMatrix<ScalarType>::CSysMatrix() : rank(SU2_MPI::GetRank()), size(SU2_MPI::G
 }
 
 template <class ScalarType>
-CSysMatrix<ScalarType>::~CSysMatrix(void) {
+CSysMatrix<ScalarType>::~CSysMatrix() {
   delete[] omp_partitions;
   MemoryAllocation::aligned_free(ILU_matrix);
   MemoryAllocation::aligned_free(matrix);
diff --git a/Common/src/linear_algebra/CSysSolve.cpp b/Common/src/linear_algebra/CSysSolve.cpp
index fdebc018574..fbaf2fd1def 100644
--- a/Common/src/linear_algebra/CSysSolve.cpp
+++ b/Common/src/linear_algebra/CSysSolve.cpp
@@ -161,7 +161,7 @@ void CSysSolve<ScalarType>::ModGramSchmidt(int i, su2matrix<ScalarType>& Hsbg,
 }
 
 template <class ScalarType>
-void CSysSolve<ScalarType>::WriteHeader(string solver, ScalarType restol, ScalarType resinit) const {
+void CSysSolve<ScalarType>::WriteHeader(const string& solver, ScalarType restol, ScalarType resinit) const {
   cout << "\n# " << solver << " residual history\n";
   cout << "# Residual tolerance target = " << restol << "\n";
   cout << "# Initial residual norm     = " << resinit << endl;
@@ -173,7 +173,7 @@ void CSysSolve<ScalarType>::WriteHistory(unsigned long iter, ScalarType res) con
 }
 
 template <class ScalarType>
-void CSysSolve<ScalarType>::WriteFinalResidual(string solver, unsigned long iter, ScalarType res) const {
+void CSysSolve<ScalarType>::WriteFinalResidual(const string& solver, unsigned long iter, ScalarType res) const {
   cout << "# " << solver << " final (true) residual:\n";
   cout << "# Iteration = " << iter << ": |res|/|res0| = " << res << ".\n" << endl;
 }
diff --git a/Common/src/linear_algebra/blas_structure.cpp b/Common/src/linear_algebra/blas_structure.cpp
index 5a1ec172b11..42313022abc 100644
--- a/Common/src/linear_algebra/blas_structure.cpp
+++ b/Common/src/linear_algebra/blas_structure.cpp
@@ -42,7 +42,7 @@ extern "C" void dgemv_(char*, const int*, const int*, const passivedouble*, cons
 #endif
 
 /* Constructor. Initialize the const member variables, if needed. */
-CBlasStructure::CBlasStructure(void)
+CBlasStructure::CBlasStructure()
 #if !(defined(HAVE_LIBXSMM) || defined(HAVE_BLAS) || defined(HAVE_MKL)) || \
     (defined(CODI_REVERSE_TYPE) || defined(CODI_FORWARD_TYPE))
     : mc(256),
diff --git a/Common/src/toolboxes/C1DInterpolation.cpp b/Common/src/toolboxes/C1DInterpolation.cpp
index abae1672389..263c3f1ba57 100644
--- a/Common/src/toolboxes/C1DInterpolation.cpp
+++ b/Common/src/toolboxes/C1DInterpolation.cpp
@@ -202,8 +202,8 @@ vector<su2double> CorrectedInletValues(const vector<su2double>& Inlet_Interpolat
   return Inlet_Values;
 }
 
-void PrintInletInterpolatedData(const vector<su2double>& Inlet_Data_Interpolated, string Marker, unsigned long nVertex,
-                                unsigned short nDim, unsigned short nColumns) {
+void PrintInletInterpolatedData(const vector<su2double>& Inlet_Data_Interpolated, const string& Marker,
+                                unsigned long nVertex, unsigned short nDim, unsigned short nColumns) {
   ofstream myfile;
   myfile.precision(16);
   myfile.open("Interpolated_Data_" + Marker + ".dat", ios_base::out);
diff --git a/Common/src/toolboxes/MMS/CIncTGVSolution.cpp b/Common/src/toolboxes/MMS/CIncTGVSolution.cpp
index 9baa1999c18..26d2652c0a9 100644
--- a/Common/src/toolboxes/MMS/CIncTGVSolution.cpp
+++ b/Common/src/toolboxes/MMS/CIncTGVSolution.cpp
@@ -27,7 +27,7 @@
 
 #include "../../../include/toolboxes/MMS/CIncTGVSolution.hpp"
 
-CIncTGVSolution::CIncTGVSolution(void) : CVerificationSolution() {}
+CIncTGVSolution::CIncTGVSolution() : CVerificationSolution() {}
 
 CIncTGVSolution::CIncTGVSolution(unsigned short val_nDim, unsigned short val_nVar, unsigned short val_iMesh,
                                  CConfig* config)
@@ -88,7 +88,7 @@ CIncTGVSolution::CIncTGVSolution(unsigned short val_nDim, unsigned short val_nVa
   if (nDim != 2) SU2_MPI::Error("2D calculation required for the incompressible Taylor Green Vortex", CURRENT_FUNCTION);
 }
 
-CIncTGVSolution::~CIncTGVSolution(void) {}
+CIncTGVSolution::~CIncTGVSolution() = default;
 
 void CIncTGVSolution::GetBCState(const su2double* val_coords, const su2double val_t, su2double* val_solution) const {
   /*--- The exact solution is prescribed on the boundaries. ---*/
diff --git a/Common/src/toolboxes/MMS/CInviscidVortexSolution.cpp b/Common/src/toolboxes/MMS/CInviscidVortexSolution.cpp
index 2dc8e090197..15cf0943f8c 100644
--- a/Common/src/toolboxes/MMS/CInviscidVortexSolution.cpp
+++ b/Common/src/toolboxes/MMS/CInviscidVortexSolution.cpp
@@ -27,7 +27,7 @@
 
 #include "../../../include/toolboxes/MMS/CInviscidVortexSolution.hpp"
 
-CInviscidVortexSolution::CInviscidVortexSolution(void) : CVerificationSolution() {}
+CInviscidVortexSolution::CInviscidVortexSolution() : CVerificationSolution() {}
 
 CInviscidVortexSolution::CInviscidVortexSolution(unsigned short val_nDim, unsigned short val_nVar,
                                                  unsigned short val_iMesh, CConfig* config)
@@ -82,7 +82,7 @@ CInviscidVortexSolution::CInviscidVortexSolution(unsigned short val_nDim, unsign
     SU2_MPI::Error("Free-stream density must be 1.0 for the inviscid vortex", CURRENT_FUNCTION);
 }
 
-CInviscidVortexSolution::~CInviscidVortexSolution(void) {}
+CInviscidVortexSolution::~CInviscidVortexSolution() = default;
 
 void CInviscidVortexSolution::GetBCState(const su2double* val_coords, const su2double val_t,
                                          su2double* val_solution) const {
diff --git a/Common/src/toolboxes/MMS/CMMSIncEulerSolution.cpp b/Common/src/toolboxes/MMS/CMMSIncEulerSolution.cpp
index 9c6e28ee18e..a53ca290c6e 100644
--- a/Common/src/toolboxes/MMS/CMMSIncEulerSolution.cpp
+++ b/Common/src/toolboxes/MMS/CMMSIncEulerSolution.cpp
@@ -27,7 +27,7 @@
 
 #include "../../../include/toolboxes/MMS/CMMSIncEulerSolution.hpp"
 
-CMMSIncEulerSolution::CMMSIncEulerSolution(void) : CVerificationSolution() {}
+CMMSIncEulerSolution::CMMSIncEulerSolution() : CVerificationSolution() {}
 
 CMMSIncEulerSolution::CMMSIncEulerSolution(unsigned short val_nDim, unsigned short val_nVar, unsigned short val_iMesh,
                                            CConfig* config)
@@ -78,7 +78,7 @@ CMMSIncEulerSolution::CMMSIncEulerSolution(unsigned short val_nDim, unsigned sho
                    CURRENT_FUNCTION);
 }
 
-CMMSIncEulerSolution::~CMMSIncEulerSolution(void) {}
+CMMSIncEulerSolution::~CMMSIncEulerSolution() = default;
 
 void CMMSIncEulerSolution::GetBCState(const su2double* val_coords, const su2double val_t,
                                       su2double* val_solution) const {
@@ -128,4 +128,4 @@ void CMMSIncEulerSolution::GetMMSSourceTerm(const su2double* val_coords, const s
   val_source[nVar - 1] = 0.0;
 }
 
-bool CMMSIncEulerSolution::IsManufacturedSolution(void) const { return true; }
+bool CMMSIncEulerSolution::IsManufacturedSolution() const { return true; }
diff --git a/Common/src/toolboxes/MMS/CMMSIncNSSolution.cpp b/Common/src/toolboxes/MMS/CMMSIncNSSolution.cpp
index 8cf32d65407..b7a4e5dbe52 100644
--- a/Common/src/toolboxes/MMS/CMMSIncNSSolution.cpp
+++ b/Common/src/toolboxes/MMS/CMMSIncNSSolution.cpp
@@ -27,7 +27,7 @@
 
 #include "../../../include/toolboxes/MMS/CMMSIncNSSolution.hpp"
 
-CMMSIncNSSolution::CMMSIncNSSolution(void) : CVerificationSolution() {}
+CMMSIncNSSolution::CMMSIncNSSolution() : CVerificationSolution() {}
 
 CMMSIncNSSolution::CMMSIncNSSolution(unsigned short val_nDim, unsigned short val_nVar, unsigned short val_iMesh,
                                      CConfig* config)
@@ -82,7 +82,7 @@ CMMSIncNSSolution::CMMSIncNSSolution(unsigned short val_nDim, unsigned short val
                    CURRENT_FUNCTION);
 }
 
-CMMSIncNSSolution::~CMMSIncNSSolution(void) {}
+CMMSIncNSSolution::~CMMSIncNSSolution() = default;
 
 void CMMSIncNSSolution::GetBCState(const su2double* val_coords, const su2double val_t, su2double* val_solution) const {
   /*--- The exact solution is prescribed on the boundaries. ---*/
@@ -142,4 +142,4 @@ void CMMSIncNSSolution::GetMMSSourceTerm(const su2double* val_coords, const su2d
   val_source[nVar - 1] = 0.0;
 }
 
-bool CMMSIncNSSolution::IsManufacturedSolution(void) const { return true; }
+bool CMMSIncNSSolution::IsManufacturedSolution() const { return true; }
diff --git a/Common/src/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.cpp b/Common/src/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.cpp
index 70f6cee1164..ec53a82b6b0 100644
--- a/Common/src/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.cpp
+++ b/Common/src/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.cpp
@@ -27,7 +27,7 @@
 
 #include "../../../include/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.hpp"
 
-CMMSNSTwoHalfCirclesSolution::CMMSNSTwoHalfCirclesSolution(void) : CVerificationSolution() {}
+CMMSNSTwoHalfCirclesSolution::CMMSNSTwoHalfCirclesSolution() : CVerificationSolution() {}
 
 CMMSNSTwoHalfCirclesSolution::CMMSNSTwoHalfCirclesSolution(unsigned short val_nDim, unsigned short val_nVar,
                                                            unsigned short val_iMesh, CConfig* config)
@@ -99,7 +99,7 @@ CMMSNSTwoHalfCirclesSolution::CMMSNSTwoHalfCirclesSolution(unsigned short val_nD
     SU2_MPI::Error("Constant Prandtl number must be selected for the MMS NS Two Half Circles case", CURRENT_FUNCTION);
 }
 
-CMMSNSTwoHalfCirclesSolution::~CMMSNSTwoHalfCirclesSolution(void) {}
+CMMSNSTwoHalfCirclesSolution::~CMMSNSTwoHalfCirclesSolution() = default;
 
 void CMMSNSTwoHalfCirclesSolution::GetBCState(const su2double* val_coords, const su2double val_t,
                                               su2double* val_solution) const {
@@ -307,4 +307,4 @@ void CMMSNSTwoHalfCirclesSolution::GetMMSSourceTerm(const su2double* val_coords,
   val_source[nDim + 1] /= Velocity_Ref * Pressure_Ref;
 }
 
-bool CMMSNSTwoHalfCirclesSolution::IsManufacturedSolution(void) const { return true; }
+bool CMMSNSTwoHalfCirclesSolution::IsManufacturedSolution() const { return true; }
diff --git a/Common/src/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.cpp b/Common/src/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.cpp
index b86cc10b24a..8497f333a06 100644
--- a/Common/src/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.cpp
+++ b/Common/src/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.cpp
@@ -27,7 +27,7 @@
 
 #include "../../../include/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.hpp"
 
-CMMSNSTwoHalfSpheresSolution::CMMSNSTwoHalfSpheresSolution(void) : CVerificationSolution() {}
+CMMSNSTwoHalfSpheresSolution::CMMSNSTwoHalfSpheresSolution() : CVerificationSolution() {}
 
 CMMSNSTwoHalfSpheresSolution::CMMSNSTwoHalfSpheresSolution(unsigned short val_nDim, unsigned short val_nVar,
                                                            unsigned short val_iMesh, CConfig* config)
@@ -102,7 +102,7 @@ CMMSNSTwoHalfSpheresSolution::CMMSNSTwoHalfSpheresSolution(unsigned short val_nD
     SU2_MPI::Error("Constant Prandtl number must be selected for the MMS NS Two Half Spheres case", CURRENT_FUNCTION);
 }
 
-CMMSNSTwoHalfSpheresSolution::~CMMSNSTwoHalfSpheresSolution(void) {}
+CMMSNSTwoHalfSpheresSolution::~CMMSNSTwoHalfSpheresSolution() = default;
 
 void CMMSNSTwoHalfSpheresSolution::GetBCState(const su2double* val_coords, const su2double val_t,
                                               su2double* val_solution) const {
@@ -387,4 +387,4 @@ void CMMSNSTwoHalfSpheresSolution::GetMMSSourceTerm(const su2double* val_coords,
   val_source[4] /= Velocity_Ref * Pressure_Ref;
 }
 
-bool CMMSNSTwoHalfSpheresSolution::IsManufacturedSolution(void) const { return true; }
+bool CMMSNSTwoHalfSpheresSolution::IsManufacturedSolution() const { return true; }
diff --git a/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolution.cpp b/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolution.cpp
index 39721dca2d1..4e268c5b492 100644
--- a/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolution.cpp
+++ b/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolution.cpp
@@ -27,7 +27,7 @@
 
 #include "../../../include/toolboxes/MMS/CMMSNSUnitQuadSolution.hpp"
 
-CMMSNSUnitQuadSolution::CMMSNSUnitQuadSolution(void) : CVerificationSolution() {}
+CMMSNSUnitQuadSolution::CMMSNSUnitQuadSolution() : CVerificationSolution() {}
 
 CMMSNSUnitQuadSolution::CMMSNSUnitQuadSolution(unsigned short val_nDim, unsigned short val_nVar,
                                                unsigned short val_iMesh, CConfig* config)
@@ -107,7 +107,7 @@ CMMSNSUnitQuadSolution::CMMSNSUnitQuadSolution(unsigned short val_nDim, unsigned
     SU2_MPI::Error("Constant Prandtl number must be selected for the MMS NS Unit Quad case", CURRENT_FUNCTION);
 }
 
-CMMSNSUnitQuadSolution::~CMMSNSUnitQuadSolution(void) {}
+CMMSNSUnitQuadSolution::~CMMSNSUnitQuadSolution() = default;
 
 void CMMSNSUnitQuadSolution::GetBCState(const su2double* val_coords, const su2double val_t,
                                         su2double* val_solution) const {
@@ -383,4 +383,4 @@ void CMMSNSUnitQuadSolution::GetMMSSourceTerm(const su2double* val_coords, const
   val_source[nDim + 1] = t564 + t565 + t566 + t567;
 }
 
-bool CMMSNSUnitQuadSolution::IsManufacturedSolution(void) const { return true; }
+bool CMMSNSUnitQuadSolution::IsManufacturedSolution() const { return true; }
diff --git a/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.cpp b/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.cpp
index 8fb480d4e4c..8c5814c3e89 100644
--- a/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.cpp
+++ b/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.cpp
@@ -27,7 +27,7 @@
 
 #include "../../../include/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.hpp"
 
-CMMSNSUnitQuadSolutionWallBC::CMMSNSUnitQuadSolutionWallBC(void) : CVerificationSolution() {}
+CMMSNSUnitQuadSolutionWallBC::CMMSNSUnitQuadSolutionWallBC() : CVerificationSolution() {}
 
 CMMSNSUnitQuadSolutionWallBC::CMMSNSUnitQuadSolutionWallBC(unsigned short val_nDim, unsigned short val_nVar,
                                                            unsigned short val_iMesh, CConfig* config)
@@ -105,7 +105,7 @@ CMMSNSUnitQuadSolutionWallBC::CMMSNSUnitQuadSolutionWallBC(unsigned short val_nD
                    CURRENT_FUNCTION);
 }
 
-CMMSNSUnitQuadSolutionWallBC::~CMMSNSUnitQuadSolutionWallBC(void) {}
+CMMSNSUnitQuadSolutionWallBC::~CMMSNSUnitQuadSolutionWallBC() = default;
 
 void CMMSNSUnitQuadSolutionWallBC::GetBCState(const su2double* val_coords, const su2double val_t,
                                               su2double* val_solution) const {
@@ -226,4 +226,4 @@ void CMMSNSUnitQuadSolutionWallBC::GetMMSSourceTerm(const su2double* val_coords,
   val_source[nDim + 1] /= Velocity_Ref * Pressure_Ref;
 }
 
-bool CMMSNSUnitQuadSolutionWallBC::IsManufacturedSolution(void) const { return true; }
+bool CMMSNSUnitQuadSolutionWallBC::IsManufacturedSolution() const { return true; }
diff --git a/Common/src/toolboxes/MMS/CNSUnitQuadSolution.cpp b/Common/src/toolboxes/MMS/CNSUnitQuadSolution.cpp
index b98995b1d50..e15253a40c8 100644
--- a/Common/src/toolboxes/MMS/CNSUnitQuadSolution.cpp
+++ b/Common/src/toolboxes/MMS/CNSUnitQuadSolution.cpp
@@ -27,7 +27,7 @@
 
 #include "../../../include/toolboxes/MMS/CNSUnitQuadSolution.hpp"
 
-CNSUnitQuadSolution::CNSUnitQuadSolution(void) : CVerificationSolution() {}
+CNSUnitQuadSolution::CNSUnitQuadSolution() : CVerificationSolution() {}
 
 CNSUnitQuadSolution::CNSUnitQuadSolution(unsigned short val_nDim, unsigned short val_nVar, unsigned short val_iMesh,
                                          CConfig* config)
@@ -78,7 +78,7 @@ CNSUnitQuadSolution::CNSUnitQuadSolution(unsigned short val_nDim, unsigned short
     SU2_MPI::Error("Laminar Prandtl number must be larger than 1.e+20 for the NS Unit Quad case", CURRENT_FUNCTION);
 }
 
-CNSUnitQuadSolution::~CNSUnitQuadSolution(void) {}
+CNSUnitQuadSolution::~CNSUnitQuadSolution() = default;
 
 void CNSUnitQuadSolution::GetBCState(const su2double* val_coords, const su2double val_t,
                                      su2double* val_solution) const {
diff --git a/Common/src/toolboxes/MMS/CRinglebSolution.cpp b/Common/src/toolboxes/MMS/CRinglebSolution.cpp
index ed2870662fd..0ae993520c7 100644
--- a/Common/src/toolboxes/MMS/CRinglebSolution.cpp
+++ b/Common/src/toolboxes/MMS/CRinglebSolution.cpp
@@ -27,7 +27,7 @@
 
 #include "../../../include/toolboxes/MMS/CRinglebSolution.hpp"
 
-CRinglebSolution::CRinglebSolution(void) : CVerificationSolution() {}
+CRinglebSolution::CRinglebSolution() : CVerificationSolution() {}
 
 CRinglebSolution::CRinglebSolution(unsigned short val_nDim, unsigned short val_nVar, unsigned short val_iMesh,
                                    CConfig* config)
@@ -64,7 +64,7 @@ CRinglebSolution::CRinglebSolution(unsigned short val_nDim, unsigned short val_n
     SU2_MPI::Error("Standard air or ideal gas must be selected for the Ringleb case", CURRENT_FUNCTION);
 }
 
-CRinglebSolution::~CRinglebSolution(void) {}
+CRinglebSolution::~CRinglebSolution() = default;
 
 void CRinglebSolution::GetBCState(const su2double* val_coords, const su2double val_t, su2double* val_solution) const {
   /*--- The exact solution is prescribed on the boundaries for the
diff --git a/Common/src/toolboxes/MMS/CTGVSolution.cpp b/Common/src/toolboxes/MMS/CTGVSolution.cpp
index f561b9b54a6..e30b004e7a4 100644
--- a/Common/src/toolboxes/MMS/CTGVSolution.cpp
+++ b/Common/src/toolboxes/MMS/CTGVSolution.cpp
@@ -27,7 +27,7 @@
 
 #include "../../../include/toolboxes/MMS/CTGVSolution.hpp"
 
-CTGVSolution::CTGVSolution(void) : CVerificationSolution() {}
+CTGVSolution::CTGVSolution() : CVerificationSolution() {}
 
 CTGVSolution::CTGVSolution(unsigned short val_nDim, unsigned short val_nVar, unsigned short val_iMesh, CConfig* config)
     : CVerificationSolution(val_nDim, val_nVar, val_iMesh, config) {
@@ -78,7 +78,7 @@ CTGVSolution::CTGVSolution(unsigned short val_nDim, unsigned short val_nVar, uns
     SU2_MPI::Error("Constant Prandtl number must be selected for the Taylor Green Vortex", CURRENT_FUNCTION);
 }
 
-CTGVSolution::~CTGVSolution(void) {}
+CTGVSolution::~CTGVSolution() = default;
 
 void CTGVSolution::GetSolution(const su2double* val_coords, const su2double val_t, su2double* val_solution) const {
   /* The initial conditions are set for the Taylor-Green vortex case, which
@@ -113,4 +113,4 @@ void CTGVSolution::GetSolution(const su2double* val_coords, const su2double val_
   val_solution[nVar - 1] = p * ovGm1 + 0.5 * rho * (u * u + v * v);
 }
 
-bool CTGVSolution::ExactSolutionKnown(void) const { return false; }
+bool CTGVSolution::ExactSolutionKnown() const { return false; }
diff --git a/Common/src/toolboxes/MMS/CUserDefinedSolution.cpp b/Common/src/toolboxes/MMS/CUserDefinedSolution.cpp
index da2806cfcd2..aee58f83778 100644
--- a/Common/src/toolboxes/MMS/CUserDefinedSolution.cpp
+++ b/Common/src/toolboxes/MMS/CUserDefinedSolution.cpp
@@ -27,7 +27,7 @@
 
 #include "../../../include/toolboxes/MMS/CUserDefinedSolution.hpp"
 
-CUserDefinedSolution::CUserDefinedSolution(void) : CVerificationSolution() {}
+CUserDefinedSolution::CUserDefinedSolution() : CVerificationSolution() {}
 
 CUserDefinedSolution::CUserDefinedSolution(unsigned short val_nDim, unsigned short val_nVar, unsigned short val_iMesh,
                                            CConfig* config)
@@ -45,7 +45,7 @@ CUserDefinedSolution::CUserDefinedSolution(unsigned short val_nDim, unsigned sho
   SU2_MPI::Error("User must implement this function", CURRENT_FUNCTION);
 }
 
-CUserDefinedSolution::~CUserDefinedSolution(void) {}
+CUserDefinedSolution::~CUserDefinedSolution() = default;
 
 void CUserDefinedSolution::GetBCState(const su2double* val_coords, const su2double val_t,
                                       su2double* val_solution) const {
@@ -62,7 +62,7 @@ void CUserDefinedSolution::GetMMSSourceTerm(const su2double* val_coords, const s
   SU2_MPI::Error("User must implement this function", CURRENT_FUNCTION);
 }
 
-bool CUserDefinedSolution::IsManufacturedSolution(void) const {
+bool CUserDefinedSolution::IsManufacturedSolution() const {
   SU2_MPI::Error("User must implement this function", CURRENT_FUNCTION);
   return false; /* True if manufactured. */
 }
diff --git a/Common/src/toolboxes/MMS/CVerificationSolution.cpp b/Common/src/toolboxes/MMS/CVerificationSolution.cpp
index ff8687aad87..23746572e34 100644
--- a/Common/src/toolboxes/MMS/CVerificationSolution.cpp
+++ b/Common/src/toolboxes/MMS/CVerificationSolution.cpp
@@ -27,7 +27,7 @@
 
 #include "../../../include/toolboxes/MMS/CVerificationSolution.hpp"
 
-CVerificationSolution::CVerificationSolution(void) {
+CVerificationSolution::CVerificationSolution() {
   /*--- Initialize the pointers to NULL. ---*/
   Error_RMS = nullptr;
   Error_Max = nullptr;
@@ -65,7 +65,7 @@ CVerificationSolution::CVerificationSolution(unsigned short val_nDim, unsigned s
   }
 }
 
-CVerificationSolution::~CVerificationSolution(void) {
+CVerificationSolution::~CVerificationSolution() {
   /*--- Release the memory of the pointers, if allocated. ---*/
   delete[] Error_RMS;
   delete[] Error_Max;
@@ -102,9 +102,9 @@ void CVerificationSolution::GetMMSSourceTerm(const su2double* val_coords, const
   for (unsigned short iVar = 0; iVar < nVar; ++iVar) val_source[iVar] = 0.0;
 }
 
-bool CVerificationSolution::IsManufacturedSolution(void) const { return false; }
+bool CVerificationSolution::IsManufacturedSolution() const { return false; }
 
-bool CVerificationSolution::ExactSolutionKnown(void) const { return true; }
+bool CVerificationSolution::ExactSolutionKnown() const { return true; }
 
 void CVerificationSolution::GetLocalError(const su2double* val_coords, const su2double val_t,
                                           const su2double* val_solution, su2double* val_error) const {
diff --git a/Common/src/toolboxes/printing_toolbox.cpp b/Common/src/toolboxes/printing_toolbox.cpp
index 7153bcf1b98..daaac9a53e7 100644
--- a/Common/src/toolboxes/printing_toolbox.cpp
+++ b/Common/src/toolboxes/printing_toolbox.cpp
@@ -27,7 +27,6 @@
 
 #include <stdexcept>
 #include <iomanip>
-#include <stdexcept>
 #include "../../include/toolboxes/printing_toolbox.hpp"
 
 PrintingToolbox::CTablePrinter::CTablePrinter(std::ostream* output, const std::string& separator) {
diff --git a/Common/src/wall_model.cpp b/Common/src/wall_model.cpp
index 639466be7a8..008b3e60999 100644
--- a/Common/src/wall_model.cpp
+++ b/Common/src/wall_model.cpp
@@ -135,7 +135,7 @@ void CWallModel1DEQ::WallShearStressAndHeatFlux(const su2double tExchange, const
   su2double qWall_prev = 0.0;
   su2double mut, nu, mu_lam, rho, utau, y_plus, D;
 
-  while (converged == false) {
+  while (!converged) {
     iter += 1;
     if (iter == max_iter) converged = true;
 
@@ -262,7 +262,7 @@ void CWallModel1DEQ::WallShearStressAndHeatFlux(const su2double tExchange, const
       rhs[i] = -tmp[i + 1] + tmp[i];
     }
 
-    if (HeatFlux_Prescribed == true) {
+    if (HeatFlux_Prescribed) {
       /* dT/dy = 0 -> Twall = T[1] */
       h_wall = c_p * T[1];
     }
@@ -350,7 +350,7 @@ void CWallModelLogLaw::WallShearStressAndHeatFlux(const su2double tExchange, con
   unsigned short iter = 0, max_iter = 50;
   const su2double tol = 1e-3;
 
-  while (converged == false) {
+  while (!converged) {
     iter += 1;
     if (iter == max_iter) converged = true;
 
diff --git a/SU2_CFD/include/fluid/CCoolProp.hpp b/SU2_CFD/include/fluid/CCoolProp.hpp
index 9d241a4b000..d101427253e 100644
--- a/SU2_CFD/include/fluid/CCoolProp.hpp
+++ b/SU2_CFD/include/fluid/CCoolProp.hpp
@@ -66,7 +66,7 @@ class CCoolProp final : public CFluidModel {
   /*!
    * \brief Constructor of the class.
    */
-  CCoolProp(string fluidname);
+  CCoolProp(const string& fluidname);
 
 #ifdef USE_COOLPROP
   /*!
diff --git a/SU2_CFD/include/numerics/CNumerics.hpp b/SU2_CFD/include/numerics/CNumerics.hpp
index e8682cc8da5..9483f4c4979 100644
--- a/SU2_CFD/include/numerics/CNumerics.hpp
+++ b/SU2_CFD/include/numerics/CNumerics.hpp
@@ -1520,7 +1520,7 @@ class CNumerics {
    * \brief Computes a basis of orthogonal vectors from a supplied vector
    * \param[in] config - Normal vector
    */
-  void CreateBasis(const su2double *val_Normal, su2double* l, su2double* m);
+  void CreateBasis(const su2double *val_Normal, su2double* l, su2double* m) const;
 
   /*!
    * \brief Set the value of the Tauwall
diff --git a/SU2_CFD/include/output/COutput.hpp b/SU2_CFD/include/output/COutput.hpp
index 70788bf4997..2b2b093fbc9 100644
--- a/SU2_CFD/include/output/COutput.hpp
+++ b/SU2_CFD/include/output/COutput.hpp
@@ -729,7 +729,7 @@ class COutput {
    * \param[in] name - Name of the field.
    * \param[in] iPoint - The point location in the field.
    */
-  su2double GetVolumeOutputValue(string name, unsigned long iPoint);
+  su2double GetVolumeOutputValue(const string& name, unsigned long iPoint);
 
   /*!
    * \brief Set the value of a volume output field
@@ -737,7 +737,7 @@ class COutput {
    * \param[in] iPoint - The point location in the field.
    * \param[in] value - The new value of this field.
    */
-  void SetVolumeOutputValue(string name, unsigned long iPoint, su2double value);
+  void SetVolumeOutputValue(const string& name, unsigned long iPoint, su2double value);
 
   /*!
    * \brief Set the value of a volume output field
@@ -745,7 +745,7 @@ class COutput {
    * \param[in] iPoint - The point location in the field.
    * \param[in] value - The new value of this field.
    */
-  void SetAvgVolumeOutputValue(string name, unsigned long iPoint, su2double value);
+  void SetAvgVolumeOutputValue(const string& name, unsigned long iPoint, su2double value);
 
   /*!
    * \brief CheckHistoryOutput
diff --git a/SU2_CFD/include/output/COutputLegacy.hpp b/SU2_CFD/include/output/COutputLegacy.hpp
index a1b413a95ee..26df9f5fed6 100644
--- a/SU2_CFD/include/output/COutputLegacy.hpp
+++ b/SU2_CFD/include/output/COutputLegacy.hpp
@@ -273,7 +273,7 @@ class COutputLegacy {
    * \param[in] val_nZone - Total number of domains in the grid file.
    */
   void SetSpecialOutput(CSolver *****solver_container, CGeometry ****geometry, CConfig **config,
-                         unsigned long iExtIter, unsigned short val_nZone);
+                         unsigned long iExtIter, unsigned short val_nZone) const;
 
 };
 
diff --git a/SU2_CFD/include/output/filewriter/CCGNSFileWriter.hpp b/SU2_CFD/include/output/filewriter/CCGNSFileWriter.hpp
index d0ac4fd10cb..1bbe79b1aa3 100644
--- a/SU2_CFD/include/output/filewriter/CCGNSFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CCGNSFileWriter.hpp
@@ -88,7 +88,7 @@ class CCGNSFileWriter final : public CFileWriter {
   /*!
    * \brief Initialize CGNS mesh file.
    */
-  void InitializeMeshFile(string val_filename);
+  void InitializeMeshFile(const string& val_filename);
 
   /*!
    * \brief Write i-th coordinate to file in CGNS file format.
diff --git a/SU2_CFD/include/output/filewriter/CParaviewVTMFileWriter.hpp b/SU2_CFD/include/output/filewriter/CParaviewVTMFileWriter.hpp
index 6804b55651d..51636622128 100644
--- a/SU2_CFD/include/output/filewriter/CParaviewVTMFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CParaviewVTMFileWriter.hpp
@@ -110,7 +110,7 @@ class CParaviewVTMFileWriter final: public CFileWriter{
    * \param[in] surfaceDataSorter - sorted surface data
    * \param[in] geometry - the geometry of the problem
    */
-  void WriteFolderData(string foldername, CConfig *config,
+  void WriteFolderData(const string& foldername, CConfig *config,
                        string multiZoneHeaderString,
                        CParallelDataSorter* volumeDataSorter,
                        CParallelDataSorter* surfaceDataSorter,
@@ -124,7 +124,7 @@ class CParaviewVTMFileWriter final: public CFileWriter{
    * \param[in] dataSorter - Datasorter object containing the actual data. Note, data must be sorted.
    */
   //void AddDataset(string name, string file, CParallelDataSorter* dataSorter);
-  void AddDataset(string foldername, string name, string file, CParallelDataSorter* dataSorter);
+  void AddDataset(const string& foldername, string name, const string& file, CParallelDataSorter* dataSorter);
 
   /*!
    * \brief Start a new block
diff --git a/SU2_CFD/include/solvers/CSolver.hpp b/SU2_CFD/include/solvers/CSolver.hpp
index 9ac3d17f6a2..cdfa1946151 100644
--- a/SU2_CFD/include/solvers/CSolver.hpp
+++ b/SU2_CFD/include/solvers/CSolver.hpp
@@ -560,7 +560,7 @@ class CSolver {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetGridVel_Gradient(CGeometry *geometry, const CConfig *config);
+  void SetGridVel_Gradient(CGeometry *geometry, const CConfig *config) const;
 
   /*!
    * \brief Compute slope limiter.
@@ -592,7 +592,7 @@ class CSolver {
    * \param[in] geometry - Geometrical definition of the problem.
    * \param[in] config - Definition of the particular problem.
    */
-  void Restart_OldGeometry(CGeometry *geometry, CConfig *config);
+  void Restart_OldGeometry(CGeometry *geometry, CConfig *config) const;
 
   /*!
    * \brief A virtual member.
@@ -3434,7 +3434,7 @@ class CSolver {
   void Read_SU2_Restart_Metadata(CGeometry *geometry,
                                  CConfig *config,
                                  bool adjoint_run,
-                                 string val_filename) const;
+                                 const string& val_filename) const;
 
   /*!
    * \brief Load a inlet profile data from file into a particular solver.
diff --git a/SU2_CFD/src/CMarkerProfileReaderFVM.cpp b/SU2_CFD/src/CMarkerProfileReaderFVM.cpp
index cf6090d15c7..2ee6fe9ec29 100644
--- a/SU2_CFD/src/CMarkerProfileReaderFVM.cpp
+++ b/SU2_CFD/src/CMarkerProfileReaderFVM.cpp
@@ -25,6 +25,8 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
+#include <utility>
+
 #include "../include/CMarkerProfileReaderFVM.hpp"
 
 CMarkerProfileReaderFVM::CMarkerProfileReaderFVM(CGeometry      *val_geometry,
@@ -44,11 +46,11 @@ CMarkerProfileReaderFVM::CMarkerProfileReaderFVM(CGeometry      *val_geometry,
   this->geometry  = val_geometry;
   dimension       = geometry->GetnDim();
 
-  filename     = val_filename;
+  filename     = std::move(val_filename);
   markerType   = val_kind_marker;
   numberOfVars = val_number_vars;
-  columnNames  = val_columnNames;
-  columnValues = val_columnValues;
+  columnNames  = std::move(val_columnNames);
+  columnValues = std::move(val_columnValues);
 
   /* Attempt to open the specified file. */
   ifstream profile_file;
@@ -68,7 +70,7 @@ CMarkerProfileReaderFVM::CMarkerProfileReaderFVM(CGeometry      *val_geometry,
 
 }
 
-CMarkerProfileReaderFVM::~CMarkerProfileReaderFVM(void) { }
+CMarkerProfileReaderFVM::~CMarkerProfileReaderFVM() = default;
 
 void CMarkerProfileReaderFVM::ReadMarkerProfile() {
 
@@ -100,11 +102,11 @@ void CMarkerProfileReaderFVM::ReadMarkerProfile() {
         getline (profile_file, text_line);
         text_line.erase (0,11);
         for (unsigned short iChar = 0; iChar < 20; iChar++) {
-          position = text_line.find( " ", 0 );  if (position != string::npos) text_line.erase (position,1);
-          position = text_line.find( "\r", 0 ); if (position != string::npos) text_line.erase (position,1);
-          position = text_line.find( "\n", 0 ); if (position != string::npos) text_line.erase (position,1);
+          position = text_line.find( ' ', 0 );  if (position != string::npos) text_line.erase (position,1);
+          position = text_line.find( '\r', 0 ); if (position != string::npos) text_line.erase (position,1);
+          position = text_line.find( '\n', 0 ); if (position != string::npos) text_line.erase (position,1);
         }
-        profileTags.push_back(text_line.c_str());
+        profileTags.emplace_back(text_line.c_str());
 
         /*--- read NROW ---*/
         getline (profile_file, text_line);
@@ -134,7 +136,7 @@ void CMarkerProfileReaderFVM::ReadMarkerProfile() {
 
   profile_file.close();
 
-  if (nmarkFound==false) {
+  if (!nmarkFound) {
     SU2_MPI::Error("While opening profile file, no \"NMARK=\" specification was found", CURRENT_FUNCTION);
   }
 
@@ -242,10 +244,10 @@ void CMarkerProfileReaderFVM::MergeProfileMarkers() {
 
   /*--- Send and Recv buffers. ---*/
 
-  su2double *Buffer_Send_X = new su2double[MaxLocalPoint];
+  auto *Buffer_Send_X = new su2double[MaxLocalPoint];
   su2double *Buffer_Recv_X = nullptr;
 
-  su2double *Buffer_Send_Y = new su2double[MaxLocalPoint];
+  auto *Buffer_Send_Y = new su2double[MaxLocalPoint];
   su2double *Buffer_Recv_Y = nullptr;
 
   su2double *Buffer_Send_Z = nullptr, *Buffer_Recv_Z = nullptr;
@@ -354,8 +356,8 @@ void CMarkerProfileReaderFVM::MergeProfileMarkers() {
         for (iChar = 0; iChar < MAX_STRING_SIZE; iChar++) {
           str_buf[iChar] = Buffer_Recv_Str[index + iChar];
         }
-        Marker_Tags.push_back(str_buf);
-        profileTags.push_back(str_buf);
+        Marker_Tags.emplace_back(str_buf);
+        profileTags.emplace_back(str_buf);
       }
     }
 
diff --git a/SU2_CFD/src/definition_structure.cpp b/SU2_CFD/src/definition_structure.cpp
index 9a56d219a89..415e36a6421 100644
--- a/SU2_CFD/src/definition_structure.cpp
+++ b/SU2_CFD/src/definition_structure.cpp
@@ -116,7 +116,7 @@ void Partition_Analysis(CGeometry *geometry, CConfig *config) {
     /*--- Prepare and open the file ---*/
     Profile_File.open("partitioning.csv");
     /*--- Create the CSV header ---*/
-    Profile_File << "\"Rank\", \"nNeighbors\", \"nPointTotal\", \"nEdge\", \"nPointGhost\", \"nSendTotal\", \"nRecvTotal\", \"nElemTotal\", \"nElemBoundary\", \"nElemHalo\", \"nnz\"" << endl;
+    Profile_File << R"("Rank", "nNeighbors", "nPointTotal", "nEdge", "nPointGhost", "nSendTotal", "nRecvTotal", "nElemTotal", "nElemBoundary", "nElemHalo", "nnz")" << endl;
     Profile_File.close();
   }
   SU2_MPI::Barrier(SU2_MPI::GetComm());
@@ -157,7 +157,7 @@ void Partition_Analysis_FEM(CGeometry *geometry, CConfig *config) {
 
   /*--- Create an object of the class CMeshFEM_DG and retrieve the necessary
    geometrical information for the FEM DG solver. ---*/
-  CMeshFEM_DG *DGGeometry = dynamic_cast<CMeshFEM_DG *>(geometry);
+  auto *DGGeometry = dynamic_cast<CMeshFEM_DG *>(geometry);
 
   unsigned long nVolElemOwned = DGGeometry->GetNVolElemOwned();
   CVolumeElementFEM *volElem = DGGeometry->GetVolElem();
@@ -182,7 +182,7 @@ void Partition_Analysis_FEM(CGeometry *geometry, CConfig *config) {
   /*--- Determine the total number of elements and DOFS to be send. ---*/
   for(unsigned long i=0; i<ranksSend.size(); ++i) {
 
-    const unsigned int nElemSend = (unsigned int)elementsSend[i].size();
+    const auto nElemSend = (unsigned int)elementsSend[i].size();
 
     nElemSendTotal += nElemSend;
 
@@ -195,7 +195,7 @@ void Partition_Analysis_FEM(CGeometry *geometry, CConfig *config) {
   /*--- Determine the total number of elements and DOFS to be received. ---*/
   for(unsigned long i=0; i<ranksRecv.size(); ++i) {
 
-    const unsigned int nElemRecv = (unsigned int)elementsRecv[i].size();
+    const auto nElemRecv = (unsigned int)elementsRecv[i].size();
 
     nElemRecvTotal += nElemRecv;
 
@@ -215,7 +215,7 @@ void Partition_Analysis_FEM(CGeometry *geometry, CConfig *config) {
     /*--- Prepare and open the file ---*/
     Profile_File.open("partitioning.csv");
     /*--- Create the CSV header ---*/
-    Profile_File << "\"Rank\", \"nNeighSend\",  \"nNeighRecv\", \"nElemOwned\", \"nElemSendTotal\", \"nElemRecvTotal\", \"nDOFOwned\", \"nDOFSendTotal\", \"nDOFRecvTotal\"" << endl;
+    Profile_File << R"("Rank", "nNeighSend",  "nNeighRecv", "nElemOwned", "nElemSendTotal", "nElemRecvTotal", "nDOFOwned", "nDOFSendTotal", "nDOFRecvTotal")" << endl;
     Profile_File.close();
   }
   SU2_MPI::Barrier(SU2_MPI::GetComm());
diff --git a/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
index 440d311d6c1..bfefb036231 100644
--- a/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
@@ -122,7 +122,7 @@ CDiscAdjSinglezoneDriver::CDiscAdjSinglezoneDriver(char* confFile,
 
 }
 
-CDiscAdjSinglezoneDriver::~CDiscAdjSinglezoneDriver(void) {
+CDiscAdjSinglezoneDriver::~CDiscAdjSinglezoneDriver() {
 
   delete direct_iteration;
   delete direct_output;
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index fb788d47eb5..7b9621280f9 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -103,7 +103,7 @@
 #ifdef VTUNEPROF
 #include <ittnotify.h>
 #endif
-#include <fenv.h>
+#include <cfenv>
 
 CDriver::CDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator, bool dummy_geo) :
 CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false), fem_solver(false), dry_run(dummy_geo) {
@@ -961,7 +961,7 @@ void CDriver::InitializeGeometryDGFEM(CConfig* config, CGeometry **&geometry) {
 
   /*--- Carry out a dynamic cast to CMeshFEM_DG, such that it is not needed to
        define all virtual functions in the base class CGeometry. ---*/
-  CMeshFEM_DG *DGMesh = dynamic_cast<CMeshFEM_DG *>(geometry[MESH_0]);
+  auto *DGMesh = dynamic_cast<CMeshFEM_DG *>(geometry[MESH_0]);
 
   /*--- Determine the standard elements for the volume elements. ---*/
   if (rank == MASTER_NODE) cout << "Creating standard volume elements." << endl;
@@ -2623,7 +2623,7 @@ void CDriver::PreprocessStaticMesh(const CConfig *config, CGeometry** geometry){
 
     /*--- Carry out a dynamic cast to CMeshFEM_DG, such that it is not needed to
          define all virtual functions in the base class CGeometry. ---*/
-    CMeshFEM_DG *DGMesh = dynamic_cast<CMeshFEM_DG *>(geometry[MESH_0]);
+    auto *DGMesh = dynamic_cast<CMeshFEM_DG *>(geometry[MESH_0]);
 
     /*--- Initialize the static mesh movement, if necessary. ---*/
     const unsigned short Kind_Grid_Movement = config->GetKind_GridMovement();
@@ -2809,11 +2809,11 @@ void CDriver::PreprocessTurbomachinery(CConfig** config, CGeometry**** geometry,
 
 }
 
-CDriver::~CDriver(void) {}
+CDriver::~CDriver() = default;
 
 void CDriver::PrintDirectResidual(RECORDING kind_recording) {
 
-  if (!(rank == MASTER_NODE && kind_recording == RECORDING::SOLUTION_VARIABLES)) return;
+  if (rank != MASTER_NODE || kind_recording != RECORDING::SOLUTION_VARIABLES) return;
 
   const bool multizone = config_container[ZONE_0]->GetMultizone_Problem();
 
@@ -2930,7 +2930,7 @@ CFluidDriver::CFluidDriver(char* confFile, unsigned short val_nZone, SU2_Comm MP
   Max_Iter = config_container[ZONE_0]->GetnInner_Iter();
 }
 
-CFluidDriver::~CFluidDriver(void) { }
+CFluidDriver::~CFluidDriver() = default;
 
 void CFluidDriver::StartSolver(){
 
@@ -3213,7 +3213,7 @@ CTurbomachineryDriver::CTurbomachineryDriver(char* confFile, unsigned short val_
   }
 }
 
-CTurbomachineryDriver::~CTurbomachineryDriver(void) {
+CTurbomachineryDriver::~CTurbomachineryDriver() {
   if (rank == MASTER_NODE){
     /*--- Close the convergence history file. ---*/
     for (iZone = 0; iZone < nZone; iZone++) {
@@ -3460,7 +3460,7 @@ CHBDriver::CHBDriver(char* confFile,
 
 }
 
-CHBDriver::~CHBDriver(void) {
+CHBDriver::~CHBDriver() {
 
   unsigned short kInst;
 
@@ -3573,11 +3573,11 @@ void CHBDriver::SetHarmonicBalance(unsigned short iInst) {
   unsigned long InnerIter = config_container[ZONE_0]->GetInnerIter();
 
   /*--- Retrieve values from the config file ---*/
-  su2double *U = new su2double[nVar];
-  su2double *U_old = new su2double[nVar];
-  su2double *Psi = new su2double[nVar];
-  su2double *Psi_old = new su2double[nVar];
-  su2double *Source = new su2double[nVar];
+  auto *U = new su2double[nVar];
+  auto *U_old = new su2double[nVar];
+  auto *Psi = new su2double[nVar];
+  auto *Psi_old = new su2double[nVar];
+  auto *Source = new su2double[nVar];
   su2double deltaU, deltaPsi;
 
   /*--- Compute period of oscillation ---*/
@@ -3649,8 +3649,8 @@ void CHBDriver::SetHarmonicBalance(unsigned short iInst) {
 
     /*--- Extra variables needed if we have a turbulence model. ---*/
     unsigned short nVar_Turb = solver_container[ZONE_0][INST_0][MESH_0][TURB_SOL]->GetnVar();
-    su2double *U_Turb = new su2double[nVar_Turb];
-    su2double *Source_Turb = new su2double[nVar_Turb];
+    auto *U_Turb = new su2double[nVar_Turb];
+    auto *Source_Turb = new su2double[nVar_Turb];
 
     /*--- Loop over only the finest mesh level (turbulence is always solved
      on the original grid only). ---*/
@@ -3690,12 +3690,12 @@ void CHBDriver::StabilizeHarmonicBalance() {
   bool adjoint = (config_container[ZONE_0]->GetContinuous_Adjoint());
 
   /*--- Retrieve values from the config file ---*/
-  su2double *Source     = new su2double[nInstHB];
-  su2double *Source_old = new su2double[nInstHB];
+  auto *Source     = new su2double[nInstHB];
+  auto *Source_old = new su2double[nInstHB];
   su2double Delta;
 
-  su2double **Pinv     = new su2double*[nInstHB];
-  su2double **P        = new su2double*[nInstHB];
+  auto **Pinv     = new su2double*[nInstHB];
+  auto **P        = new su2double*[nInstHB];
   for (iInst = 0; iInst < nInstHB; iInst++) {
     Pinv[iInst]       = new su2double[nInstHB];
     P[iInst]          = new su2double[nInstHB];
@@ -3725,7 +3725,7 @@ void CHBDriver::StabilizeHarmonicBalance() {
       /*--- Invert stabilization matrix Pinv with Gauss elimination---*/
 
       /*--  A temporary matrix to hold the inverse, dynamically allocated ---*/
-      su2double **temp = new su2double*[nInstHB];
+      auto **temp = new su2double*[nInstHB];
       for (i = 0; i < nInstHB; i++) {
         temp[i] = new su2double[2 * nInstHB];
       }
@@ -3847,10 +3847,10 @@ void CHBDriver::ComputeHBOperator() {
   const   complex<su2double> J(0.0,1.0);
   unsigned short i, j, k, iInst;
 
-  su2double *Omega_HB       = new su2double[nInstHB];
-  complex<su2double> **E    = new complex<su2double>*[nInstHB];
-  complex<su2double> **Einv = new complex<su2double>*[nInstHB];
-  complex<su2double> **DD   = new complex<su2double>*[nInstHB];
+  auto *Omega_HB       = new su2double[nInstHB];
+  auto **E    = new complex<su2double>*[nInstHB];
+  auto **Einv = new complex<su2double>*[nInstHB];
+  auto **DD   = new complex<su2double>*[nInstHB];
   for (iInst = 0; iInst < nInstHB; iInst++) {
     E[iInst]    = new complex<su2double>[nInstHB];
     Einv[iInst] = new complex<su2double>[nInstHB];
@@ -3889,7 +3889,7 @@ void CHBDriver::ComputeHBOperator() {
   /*---  Invert inverse harmonic balance Einv with Gauss elimination ---*/
 
   /*--  A temporary matrix to hold the inverse, dynamically allocated ---*/
-  complex<su2double> **temp = new complex<su2double>*[nInstHB];
+  auto **temp = new complex<su2double>*[nInstHB];
   for (i = 0; i < nInstHB; i++) {
     temp[i] = new complex<su2double>[2 * nInstHB];
   }
@@ -3963,10 +3963,10 @@ void CHBDriver::ComputeHBOperator() {
 
 
   /*---  Temporary matrix for performing product  ---*/
-  complex<su2double> **Temp    = new complex<su2double>*[nInstHB];
+  auto **Temp    = new complex<su2double>*[nInstHB];
 
   /*---  Temporary complex HB operator  ---*/
-  complex<su2double> **Dcpx    = new complex<su2double>*[nInstHB];
+  auto **Dcpx    = new complex<su2double>*[nInstHB];
 
   for (iInst = 0; iInst < nInstHB; iInst++){
     Temp[iInst]    = new complex<su2double>[nInstHB];
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index 431cf67dd6e..ff07e7d1e48 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -62,7 +62,7 @@ CDriverBase::CDriverBase(char* confFile, unsigned short val_nZone, SU2_Comm MPIC
   AD::Initialize();
 }
 
-CDriverBase::~CDriverBase(void) {}
+CDriverBase::~CDriverBase() = default;
 
 void CDriverBase::InitializeContainers() {
   /*--- Create pointers to all the classes that may be used by drivers. In general, the pointers are instantiated
@@ -390,7 +390,7 @@ vector<passivedouble> CDriverBase::GetMarkerVertexNormals(unsigned short iMarker
   return values;
 }
 
-void CDriverBase::CommunicateMeshDisplacements(void) {
+void CDriverBase::CommunicateMeshDisplacements() {
   solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->InitiateComms(main_geometry, main_config, MESH_DISPLACEMENTS);
   solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->CompleteComms(main_geometry, main_config, MESH_DISPLACEMENTS);
 }
diff --git a/SU2_CFD/src/drivers/CMultizoneDriver.cpp b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
index a1de120c8a8..cd93263313f 100644
--- a/SU2_CFD/src/drivers/CMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
@@ -117,7 +117,7 @@ CMultizoneDriver::CMultizoneDriver(char* confFile, unsigned short val_nZone, SU2
 
 }
 
-CMultizoneDriver::~CMultizoneDriver(void) {
+CMultizoneDriver::~CMultizoneDriver() {
 
   for (iZone = 0; iZone < nZone; iZone++){
     delete [] init_res[iZone];
diff --git a/SU2_CFD/src/drivers/CSinglezoneDriver.cpp b/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
index 8289409a44f..cb4c0bea458 100644
--- a/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
@@ -41,9 +41,7 @@ CSinglezoneDriver::CSinglezoneDriver(char* confFile,
   TimeIter = 0;
 }
 
-CSinglezoneDriver::~CSinglezoneDriver(void) {
-
-}
+CSinglezoneDriver::~CSinglezoneDriver() = default;
 
 void CSinglezoneDriver::StartSolver() {
 
@@ -319,7 +317,7 @@ void CSinglezoneDriver::RuntimeOptions(){
   /*--- If succeeded create a temporary config object ---*/
 
   if (runtime_configfile.good()){
-    CConfig *runtime = new CConfig(runtime_file_name, config_container[ZONE_0]);
+    auto *runtime = new CConfig(runtime_file_name, config_container[ZONE_0]);
     delete runtime;
   }
 
diff --git a/SU2_CFD/src/fluid/CCoolProp.cpp b/SU2_CFD/src/fluid/CCoolProp.cpp
index 4a3b443252b..ff7436b2ccc 100644
--- a/SU2_CFD/src/fluid/CCoolProp.cpp
+++ b/SU2_CFD/src/fluid/CCoolProp.cpp
@@ -31,7 +31,7 @@
 #include "AbstractState.h"
 #include "CoolProp.h"
 
-CCoolProp::CCoolProp(string fluidname) : CFluidModel() {
+CCoolProp::CCoolProp(const string &fluidname) : CFluidModel() {
   fluid_entity = std::unique_ptr<CoolProp::AbstractState>(CoolProp::AbstractState::factory("HEOS", fluidname));
   Gas_Constant = fluid_entity->gas_constant() / fluid_entity->molar_mass();
   Pressure_Critical = fluid_entity->p_critical();
@@ -124,7 +124,7 @@ void CCoolProp::ComputeDerivativeNRBC_Prho(su2double P, su2double rho) {
 }
 
 #else
-CCoolProp::CCoolProp(string fluidname) {
+CCoolProp::CCoolProp(const string& fluidname) {
   SU2_MPI::Error(
       "SU2 was not compiled with CoolProp (-Denable-coolprop=true). Note that CoolProp cannot be used with directdiff "
       "or autodiff",
diff --git a/SU2_CFD/src/fluid/CFluidScalar.cpp b/SU2_CFD/src/fluid/CFluidScalar.cpp
index 429b2c2f580..fd439c6bb64 100644
--- a/SU2_CFD/src/fluid/CFluidScalar.cpp
+++ b/SU2_CFD/src/fluid/CFluidScalar.cpp
@@ -27,9 +27,8 @@
 
 #include "../../include/fluid/CFluidScalar.hpp"
 
-#include <math.h>
-
 #include <cmath>
+
 #include <numeric>
 
 #include "../../include/fluid/CConstantConductivity.hpp"
diff --git a/SU2_CFD/src/fluid/CNEMOGas.cpp b/SU2_CFD/src/fluid/CNEMOGas.cpp
index 55319a34add..f293726c947 100644
--- a/SU2_CFD/src/fluid/CNEMOGas.cpp
+++ b/SU2_CFD/src/fluid/CNEMOGas.cpp
@@ -157,7 +157,7 @@ void CNEMOGas::ComputedPdU(const su2double *V, const vector<su2double>& val_eves
 
   // Note: Electron energy not included properly.
 
-  if (val_dPdU == NULL) {
+  if (val_dPdU == nullptr) {
     SU2_MPI::Error("Array dPdU not allocated!", CURRENT_FUNCTION);
   }
 
diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 1c0babca6b5..9e4d63b12ff 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1160,7 +1160,7 @@ CSU2TCLib::CSU2TCLib(const CConfig* config, unsigned short val_nDim, bool viscou
   else            { nHeavy = nSpecies;   nEl = 0; }
 }
 
-CSU2TCLib::~CSU2TCLib(){}
+CSU2TCLib::~CSU2TCLib()= default;
 
 void CSU2TCLib::SetTDStateRhosTTv(vector<su2double>& val_rhos, su2double val_temperature, su2double val_temperature_ve){
 
@@ -1327,7 +1327,7 @@ vector<su2double>& CSU2TCLib::ComputeSpeciesEve(su2double val_T, bool vibe_only)
       }
       Eel = Ru/MolarMass[iSpecies] * (num/denom);
     }
-    if (vibe_only == true) {eves[iSpecies] = Ev;}
+    if (vibe_only) {eves[iSpecies] = Ev;}
     else {eves[iSpecies] = Ev + Eel;}
   }
 
@@ -2062,13 +2062,13 @@ void CSU2TCLib::ThermalConductivitiesGY(){
     if (denom_re <= 0.0) denom_re = EPS;
 
     /*--- Translational contribution to thermal conductivity ---*/
-    if (!(ionization && iSpecies == 0)) ThermalCond_tr += ((15.0/4.0)*kb*gam_i/denom_t);
+    if (!ionization || iSpecies != 0) ThermalCond_tr += ((15.0/4.0)*kb*gam_i/denom_t);
 
     /*--- Rotational contribution to thermal conductivity ---*/
     if (RotationModes[iSpecies] != 0.0) ThermalCond_tr += (kb*gam_i/denom_r);
 
     /*--- Vibrational-electronic contribution to thermal conductivity ---*/
-    if (!(ionization && iSpecies == 0) && RotationModes[iSpecies] != 0.0) ThermalCond_ve += (kb*Cvve/R*gam_i / denom_r);
+    if ((!ionization || iSpecies != 0) && RotationModes[iSpecies] != 0.0) ThermalCond_ve += (kb*Cvve/R*gam_i / denom_r);
     
     if (ionization && iSpecies == 0) ThermalCond_ve += ((15.0/4.0)*kb*gam_i/(1.45*denom_re));
   }
diff --git a/SU2_CFD/src/integration/CIntegrationFactory.cpp b/SU2_CFD/src/integration/CIntegrationFactory.cpp
index d9fe95cfa40..0da1709b5d1 100644
--- a/SU2_CFD/src/integration/CIntegrationFactory.cpp
+++ b/SU2_CFD/src/integration/CIntegrationFactory.cpp
@@ -35,7 +35,7 @@
 CIntegration** CIntegrationFactory::CreateIntegrationContainer(MAIN_SOLVER kindMainSolver,
                                                                const CSolver* const* solver_container){
 
-  CIntegration **integration = new CIntegration* [MAX_SOLS]();
+  auto **integration = new CIntegration* [MAX_SOLS]();
 
   for (unsigned int iSol = 0; iSol < MAX_SOLS; iSol++){
     if (solver_container[iSol] != nullptr){
diff --git a/SU2_CFD/src/integration/CMultiGridIntegration.cpp b/SU2_CFD/src/integration/CMultiGridIntegration.cpp
index 36c75cb525f..e14f36a1255 100644
--- a/SU2_CFD/src/integration/CMultiGridIntegration.cpp
+++ b/SU2_CFD/src/integration/CMultiGridIntegration.cpp
@@ -311,7 +311,7 @@ void CMultiGridIntegration::GetProlongated_Correction(unsigned short RunTime_EqS
 
   const unsigned short nVar = sol_coarse->GetnVar();
 
-  su2double *Solution = new su2double[nVar];
+  auto *Solution = new su2double[nVar];
 
   SU2_OMP_FOR_STAT(roundUpDiv(geo_coarse->GetnPointDomain(), omp_get_num_threads()))
   for (Point_Coarse = 0; Point_Coarse < geo_coarse->GetnPointDomain(); Point_Coarse++) {
@@ -506,7 +506,7 @@ void CMultiGridIntegration::SetForcing_Term(CSolver *sol_fine, CSolver *sol_coar
   const unsigned short nVar = sol_coarse->GetnVar();
   su2double factor = config->GetDamp_Res_Restric();
 
-  su2double *Residual = new su2double[nVar];
+  auto *Residual = new su2double[nVar];
 
   SU2_OMP_FOR_STAT(roundUpDiv(geo_coarse->GetnPointDomain(), omp_get_num_threads()))
   for (Point_Coarse = 0; Point_Coarse < geo_coarse->GetnPointDomain(); Point_Coarse++) {
@@ -619,7 +619,7 @@ void CMultiGridIntegration::SetRestricted_Gradient(unsigned short RunTime_EqSyst
   const unsigned short nDim = geo_coarse->GetnDim();
   const unsigned short nVar = sol_coarse->GetnVar();
 
-  su2double **Gradient = new su2double* [nVar];
+  auto **Gradient = new su2double* [nVar];
   for (iVar = 0; iVar < nVar; iVar++)
     Gradient[iVar] = new su2double [nDim];
 
diff --git a/SU2_CFD/src/interfaces/CInterface.cpp b/SU2_CFD/src/interfaces/CInterface.cpp
index 1507e004c25..6053709a30c 100644
--- a/SU2_CFD/src/interfaces/CInterface.cpp
+++ b/SU2_CFD/src/interfaces/CInterface.cpp
@@ -31,7 +31,7 @@
 #include "../../../Common/include/geometry/CGeometry.hpp"
 #include "../../include/solvers/CSolver.hpp"
 
-CInterface::CInterface(void) :
+CInterface::CInterface() :
   rank(SU2_MPI::GetRank()),
   size(SU2_MPI::GetSize()) {
 }
@@ -49,7 +49,7 @@ CInterface::CInterface(unsigned short val_nVar, unsigned short val_nConst) :
   valAggregated      = true;
 }
 
-CInterface::~CInterface(void) {
+CInterface::~CInterface() {
 
   delete [] Physical_Constants;
   delete [] Donor_Variable;
@@ -343,9 +343,9 @@ void CInterface::AllgatherAverage(CSolver *donor_solution, CSolver *target_solut
 
 #ifdef HAVE_MPI
   int iSize;
-  su2double *BuffAvgPressureDonor = NULL, *BuffAvgDensityDonor = NULL, *BuffAvgNormalVelDonor = NULL,
-      *BuffAvg3DVelDonor = NULL, *BuffAvgTangVelDonor = NULL, *BuffAvgNuDonor = NULL,
-      *BuffAvgKineDonor = NULL, *BuffAvgOmegaDonor = NULL;
+  su2double *BuffAvgPressureDonor = nullptr, *BuffAvgDensityDonor = nullptr, *BuffAvgNormalVelDonor = nullptr,
+      *BuffAvg3DVelDonor = nullptr, *BuffAvgTangVelDonor = nullptr, *BuffAvgNuDonor = nullptr,
+      *BuffAvgKineDonor = nullptr, *BuffAvgOmegaDonor = nullptr;
   int nSpanSize, *BuffMarkerDonor;
 #endif
 
diff --git a/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
index 99536c54ae5..4a6e61dfc2c 100644
--- a/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
@@ -62,7 +62,7 @@ CDiscAdjFEAIteration::CDiscAdjFEAIteration(const CConfig *config) : CIteration(c
   }
 }
 
-CDiscAdjFEAIteration::~CDiscAdjFEAIteration(void) {}
+CDiscAdjFEAIteration::~CDiscAdjFEAIteration() = default;
 
 void CDiscAdjFEAIteration::Preprocess(COutput* output, CIntegration**** integration, CGeometry**** geometry,
                                       CSolver***** solver, CNumerics****** numerics, CConfig** config,
diff --git a/SU2_CFD/src/iteration/CFluidIteration.cpp b/SU2_CFD/src/iteration/CFluidIteration.cpp
index db2192f6442..7f7107f2ccb 100644
--- a/SU2_CFD/src/iteration/CFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CFluidIteration.cpp
@@ -512,7 +512,7 @@ void CFluidIteration::InitializeVortexDistribution(unsigned long& nVortex, vecto
   while (file.good()) {
     getline(file, line);
     std::stringstream ss(line);
-    if (line.size() != 0) {  // ignore blank lines if they exist.
+    if (!line.empty()) {  // ignore blank lines if they exist.
       ss >> x_temp;
       ss >> y_temp;
       ss >> vort_strength_temp;
diff --git a/SU2_CFD/src/numerics/CNumerics.cpp b/SU2_CFD/src/numerics/CNumerics.cpp
index 12a83bf7daa..ed3a3c3e90d 100644
--- a/SU2_CFD/src/numerics/CNumerics.cpp
+++ b/SU2_CFD/src/numerics/CNumerics.cpp
@@ -31,7 +31,7 @@
 #include "../../include/numerics/CNumerics.hpp"
 #include "../../include/fluid/CFluidModel.hpp"
 
-CNumerics::CNumerics(void) {
+CNumerics::CNumerics() {
 
   Proj_Flux_Tensor  = nullptr;
 
@@ -75,7 +75,7 @@ CNumerics::CNumerics(unsigned short val_nDim, unsigned short val_nVar,
 
 }
 
-CNumerics::~CNumerics(void) {
+CNumerics::~CNumerics() {
 
   // visc
   delete [] Proj_Flux_Tensor;
@@ -1603,7 +1603,7 @@ void CNumerics::GetPrimitive2Conservative (const su2double *val_Mean_PrimVar,
   }
 }
 
-void CNumerics::CreateBasis(const su2double *val_Normal, su2double* l, su2double* m) {
+void CNumerics::CreateBasis(const su2double *val_Normal, su2double* l, su2double* m) const {
 
   unsigned short iDim;
   su2double modm, modl;
diff --git a/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp b/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp
index 0e13032a0a9..2f6b5c1712b 100644
--- a/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp
+++ b/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp
@@ -75,7 +75,7 @@ CNEMONumerics::CNEMONumerics(unsigned short val_nDim, unsigned short val_nVar,
     }
 }
 
-CNEMONumerics::~CNEMONumerics(void) {
+CNEMONumerics::~CNEMONumerics() {
 
   delete fluidmodel;
 }
diff --git a/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp b/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
index 336093761fa..a72e3f3fb83 100644
--- a/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
+++ b/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
@@ -69,7 +69,7 @@ CAvgGrad_NEMO::CAvgGrad_NEMO(unsigned short val_nDim,
 
 }
 
-CAvgGrad_NEMO::~CAvgGrad_NEMO(void) {
+CAvgGrad_NEMO::~CAvgGrad_NEMO() {
 
   delete [] PrimVar_i;
   delete [] PrimVar_j;
@@ -230,7 +230,7 @@ CAvgGradCorrected_NEMO::CAvgGradCorrected_NEMO(unsigned short val_nDim,
 
 }
 
-CAvgGradCorrected_NEMO::~CAvgGradCorrected_NEMO(void) {
+CAvgGradCorrected_NEMO::~CAvgGradCorrected_NEMO() {
 
   delete [] PrimVar_i;
   delete [] PrimVar_j;
diff --git a/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp b/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp
index 6f115117834..d99ea8702a4 100644
--- a/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp
+++ b/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp
@@ -49,7 +49,7 @@ CSource_NEMO::CSource_NEMO(unsigned short val_nDim,
     jacobian[iVar] = new su2double [nVar]();
 }
 
-CSource_NEMO::~CSource_NEMO(void) {
+CSource_NEMO::~CSource_NEMO() {
 
   /*--- Deallocate arrays ---*/
 
diff --git a/SU2_CFD/src/numerics/NEMO/convection/ausm_slau.cpp b/SU2_CFD/src/numerics/NEMO/convection/ausm_slau.cpp
index aa85f0c0a74..2370183c45d 100644
--- a/SU2_CFD/src/numerics/NEMO/convection/ausm_slau.cpp
+++ b/SU2_CFD/src/numerics/NEMO/convection/ausm_slau.cpp
@@ -59,7 +59,7 @@ CUpwAUSM_SLAU_Base_NEMO::CUpwAUSM_SLAU_Base_NEMO(unsigned short val_nDim, unsign
   }
 }
 
-CUpwAUSM_SLAU_Base_NEMO::~CUpwAUSM_SLAU_Base_NEMO(void) {
+CUpwAUSM_SLAU_Base_NEMO::~CUpwAUSM_SLAU_Base_NEMO() {
   delete[] rhos_i;
   delete[] rhos_j;
 
diff --git a/SU2_CFD/src/numerics/NEMO/convection/lax.cpp b/SU2_CFD/src/numerics/NEMO/convection/lax.cpp
index 4757897675c..abd7353f714 100644
--- a/SU2_CFD/src/numerics/NEMO/convection/lax.cpp
+++ b/SU2_CFD/src/numerics/NEMO/convection/lax.cpp
@@ -57,7 +57,7 @@ CCentLax_NEMO::CCentLax_NEMO(unsigned short val_nDim,
   }
 }
 
-CCentLax_NEMO::~CCentLax_NEMO(void) {
+CCentLax_NEMO::~CCentLax_NEMO() {
 
   delete [] Diff_U;
   delete [] MeanU;
diff --git a/SU2_CFD/src/numerics/NEMO/convection/msw.cpp b/SU2_CFD/src/numerics/NEMO/convection/msw.cpp
index 986ad8a0186..e3cf801a647 100644
--- a/SU2_CFD/src/numerics/NEMO/convection/msw.cpp
+++ b/SU2_CFD/src/numerics/NEMO/convection/msw.cpp
@@ -70,7 +70,7 @@ CUpwMSW_NEMO::CUpwMSW_NEMO(unsigned short val_nDim, unsigned short val_nVar,
   }
 }
 
-CUpwMSW_NEMO::~CUpwMSW_NEMO(void) {
+CUpwMSW_NEMO::~CUpwMSW_NEMO() {
 
   delete [] Diff_U;
   delete [] Fc_i;
diff --git a/SU2_CFD/src/numerics/NEMO/convection/roe.cpp b/SU2_CFD/src/numerics/NEMO/convection/roe.cpp
index 518e1a87d1a..5d8fa7a4813 100644
--- a/SU2_CFD/src/numerics/NEMO/convection/roe.cpp
+++ b/SU2_CFD/src/numerics/NEMO/convection/roe.cpp
@@ -62,7 +62,7 @@ CUpwRoe_NEMO::CUpwRoe_NEMO(unsigned short val_nDim, unsigned short val_nVar,
   }
 }
 
-CUpwRoe_NEMO::~CUpwRoe_NEMO(void) {
+CUpwRoe_NEMO::~CUpwRoe_NEMO() {
 
   delete [] Diff_U;
   delete [] RoeU;
diff --git a/SU2_CFD/src/numerics/continuous_adjoint/adj_convection.cpp b/SU2_CFD/src/numerics/continuous_adjoint/adj_convection.cpp
index 86074441ca1..6f09425c5c0 100644
--- a/SU2_CFD/src/numerics/continuous_adjoint/adj_convection.cpp
+++ b/SU2_CFD/src/numerics/continuous_adjoint/adj_convection.cpp
@@ -45,7 +45,7 @@ CCentLax_AdjFlow::CCentLax_AdjFlow(unsigned short val_nDim, unsigned short val_n
 
 }
 
-CCentLax_AdjFlow::~CCentLax_AdjFlow(void) {
+CCentLax_AdjFlow::~CCentLax_AdjFlow() {
 
   delete [] Diff_Psi; delete [] MeanPhi;
   delete [] Velocity_i; delete [] Velocity_j;
@@ -253,7 +253,7 @@ CCentJST_AdjFlow::CCentJST_AdjFlow(unsigned short val_nDim, unsigned short val_n
 
 }
 
-CCentJST_AdjFlow::~CCentJST_AdjFlow(void) {
+CCentJST_AdjFlow::~CCentJST_AdjFlow() {
 
   delete [] Diff_Psi; delete [] Diff_Lapl;
   delete [] Velocity_i; delete [] Velocity_j;
@@ -483,7 +483,7 @@ CUpwRoe_AdjFlow::CUpwRoe_AdjFlow(unsigned short val_nDim, unsigned short val_nVa
 
 }
 
-CUpwRoe_AdjFlow::~CUpwRoe_AdjFlow(void) {
+CUpwRoe_AdjFlow::~CUpwRoe_AdjFlow() {
 
   delete [] Residual_Roe;
   delete [] RoeVelocity;
@@ -769,7 +769,7 @@ CUpwLin_AdjTurb::CUpwLin_AdjTurb(unsigned short val_nDim, unsigned short val_nVa
   Velocity_i = new su2double [nDim];
 }
 
-CUpwLin_AdjTurb::~CUpwLin_AdjTurb(void) {
+CUpwLin_AdjTurb::~CUpwLin_AdjTurb() {
   delete [] Velocity_i;
 }
 
@@ -808,7 +808,7 @@ CUpwSca_AdjTurb::CUpwSca_AdjTurb(unsigned short val_nDim, unsigned short val_nVa
   Velocity_j = new su2double [nDim];
 }
 
-CUpwSca_AdjTurb::~CUpwSca_AdjTurb(void) {
+CUpwSca_AdjTurb::~CUpwSca_AdjTurb() {
   delete [] Velocity_i;
   delete [] Velocity_j;
 }
diff --git a/SU2_CFD/src/numerics/continuous_adjoint/adj_diffusion.cpp b/SU2_CFD/src/numerics/continuous_adjoint/adj_diffusion.cpp
index a2a450e457a..55acc909554 100644
--- a/SU2_CFD/src/numerics/continuous_adjoint/adj_diffusion.cpp
+++ b/SU2_CFD/src/numerics/continuous_adjoint/adj_diffusion.cpp
@@ -46,7 +46,7 @@ CAvgGrad_AdjFlow::CAvgGrad_AdjFlow(unsigned short val_nDim, unsigned short val_n
 
 }
 
-CAvgGrad_AdjFlow::~CAvgGrad_AdjFlow(void) {
+CAvgGrad_AdjFlow::~CAvgGrad_AdjFlow() {
   delete [] Velocity_i;
   delete [] Velocity_j;
   delete [] Mean_Velocity;
@@ -164,7 +164,7 @@ CAvgGradCorrected_AdjFlow::CAvgGradCorrected_AdjFlow(unsigned short val_nDim, un
 
 }
 
-CAvgGradCorrected_AdjFlow::~CAvgGradCorrected_AdjFlow(void) {
+CAvgGradCorrected_AdjFlow::~CAvgGradCorrected_AdjFlow() {
 
   delete [] Velocity_i;
   delete [] Velocity_j;
@@ -298,7 +298,7 @@ CAvgGrad_AdjTurb::CAvgGrad_AdjTurb(unsigned short val_nDim, unsigned short val_n
     Mean_GradTurbPsi[iVar] = new su2double [nDim];
 }
 
-CAvgGrad_AdjTurb::~CAvgGrad_AdjTurb(void) {
+CAvgGrad_AdjTurb::~CAvgGrad_AdjTurb() {
   delete [] Edge_Vector;
   delete [] Proj_Mean_GradTurbPsi_Kappa;
   delete [] Proj_Mean_GradTurbPsi_Edge;
@@ -419,7 +419,7 @@ CAvgGradCorrected_AdjTurb::CAvgGradCorrected_AdjTurb(unsigned short val_nDim, un
     Mean_GradTurbPsi[iVar] = new su2double [nDim];
 }
 
-CAvgGradCorrected_AdjTurb::~CAvgGradCorrected_AdjTurb(void) {
+CAvgGradCorrected_AdjTurb::~CAvgGradCorrected_AdjTurb() {
   delete [] Edge_Vector;
   delete [] Proj_Mean_GradTurbPsi_Kappa;
   delete [] Proj_Mean_GradTurbPsi_Edge;
diff --git a/SU2_CFD/src/numerics/continuous_adjoint/adj_sources.cpp b/SU2_CFD/src/numerics/continuous_adjoint/adj_sources.cpp
index 276321ff978..379d6125fd1 100644
--- a/SU2_CFD/src/numerics/continuous_adjoint/adj_sources.cpp
+++ b/SU2_CFD/src/numerics/continuous_adjoint/adj_sources.cpp
@@ -29,7 +29,7 @@
 
 CSourceAxisymmetric_AdjFlow::CSourceAxisymmetric_AdjFlow(unsigned short val_nDim, unsigned short val_nVar, CConfig *config) : CNumerics(val_nDim, val_nVar, config) { }
 
-CSourceAxisymmetric_AdjFlow::~CSourceAxisymmetric_AdjFlow(void) { }
+CSourceAxisymmetric_AdjFlow::~CSourceAxisymmetric_AdjFlow() = default;
 
 void CSourceAxisymmetric_AdjFlow::ComputeResidual(su2double *val_residual, su2double **Jacobian_ii, CConfig *config) {
 
@@ -88,7 +88,7 @@ CSourceConservative_AdjFlow::CSourceConservative_AdjFlow(unsigned short val_nDim
     Mean_PrimVar_Grad[iVar] = new su2double [nDim];
 }
 
-CSourceConservative_AdjFlow::~CSourceConservative_AdjFlow(void) {
+CSourceConservative_AdjFlow::~CSourceConservative_AdjFlow() {
   delete [] Mean_Residual;
   delete [] Residual_j;
   delete [] Residual_i;
@@ -238,7 +238,7 @@ void CSourceConservative_AdjFlow::ComputeResidual (su2double *val_residual, CCon
 CSourceRotatingFrame_AdjFlow::CSourceRotatingFrame_AdjFlow(unsigned short val_nDim, unsigned short val_nVar, CConfig *config) :
                               CNumerics(val_nDim, val_nVar, config) { }
 
-CSourceRotatingFrame_AdjFlow::~CSourceRotatingFrame_AdjFlow(void) { }
+CSourceRotatingFrame_AdjFlow::~CSourceRotatingFrame_AdjFlow() = default;
 
 void CSourceRotatingFrame_AdjFlow::ComputeResidual(su2double *val_residual, su2double **val_Jacobian_i, CConfig *config) {
 
@@ -325,7 +325,7 @@ CSourceViscous_AdjFlow::CSourceViscous_AdjFlow(unsigned short val_nDim, unsigned
 
 }
 
-CSourceViscous_AdjFlow::~CSourceViscous_AdjFlow(void) {
+CSourceViscous_AdjFlow::~CSourceViscous_AdjFlow() {
   unsigned short iDim;
 
   for (iDim = 0; iDim < nDim; iDim++) {
@@ -615,8 +615,7 @@ CSourceConservative_AdjTurb::CSourceConservative_AdjTurb(unsigned short val_nDim
 
 }
 
-CSourceConservative_AdjTurb::~CSourceConservative_AdjTurb(void) {
-}
+CSourceConservative_AdjTurb::~CSourceConservative_AdjTurb() = default;
 
 void CSourceConservative_AdjTurb::ComputeResidual(su2double *val_residual, su2double **val_Jacobian_i, su2double **val_Jacobian_j, CConfig *config) {
 
@@ -658,7 +657,7 @@ CSourcePieceWise_AdjTurb::CSourcePieceWise_AdjTurb(unsigned short val_nDim, unsi
     tau[iDim] = new su2double [nDim];
 }
 
-CSourcePieceWise_AdjTurb::~CSourcePieceWise_AdjTurb(void) {
+CSourcePieceWise_AdjTurb::~CSourcePieceWise_AdjTurb() {
   delete [] Velocity;
 
   for (unsigned short iDim = 0; iDim < nDim; iDim++)
diff --git a/SU2_CFD/src/numerics/elasticity/CFEAElasticity.cpp b/SU2_CFD/src/numerics/elasticity/CFEAElasticity.cpp
index 70fc75c3b9c..6fd3a35042c 100644
--- a/SU2_CFD/src/numerics/elasticity/CFEAElasticity.cpp
+++ b/SU2_CFD/src/numerics/elasticity/CFEAElasticity.cpp
@@ -139,7 +139,7 @@ CFEAElasticity::CFEAElasticity(unsigned short val_nDim, unsigned short val_nVar,
   }
 }
 
-CFEAElasticity::~CFEAElasticity(void) {
+CFEAElasticity::~CFEAElasticity() {
 
   unsigned short iVar;
   unsigned short nStrain = (nDim==2) ? DIM_STRAIN_2D : DIM_STRAIN_3D;
diff --git a/SU2_CFD/src/numerics/elasticity/CFEANonlinearElasticity.cpp b/SU2_CFD/src/numerics/elasticity/CFEANonlinearElasticity.cpp
index 82829b1d510..6dea30ef6ee 100644
--- a/SU2_CFD/src/numerics/elasticity/CFEANonlinearElasticity.cpp
+++ b/SU2_CFD/src/numerics/elasticity/CFEANonlinearElasticity.cpp
@@ -86,7 +86,7 @@ CFEANonlinearElasticity::CFEANonlinearElasticity(unsigned short val_nDim, unsign
   EField_Ref_Mod    = nullptr;
   EField_Curr_Unit  = nullptr;
 
-  if (maxwell_stress == true) {
+  if (maxwell_stress) {
 
     const su2double *Electric_Field_Dir = config->Get_Electric_Field_Dir();
     unsigned short iVar, iDim;
@@ -168,7 +168,7 @@ CFEANonlinearElasticity::CFEANonlinearElasticity(unsigned short val_nDim, unsign
 
 }
 
-CFEANonlinearElasticity::~CFEANonlinearElasticity(void) {
+CFEANonlinearElasticity::~CFEANonlinearElasticity() {
 
   unsigned short iVar;
 
@@ -642,7 +642,7 @@ void CFEANonlinearElasticity::SetElectric_Properties(const CElement *element, co
 
 }
 
-void CFEANonlinearElasticity::Compute_FmT_Mat(void) {
+void CFEANonlinearElasticity::Compute_FmT_Mat() {
 
   FmT_Mat[0][0] = (F_Mat[1][1]*F_Mat[2][2] - F_Mat[1][2]*F_Mat[2][1]) / J_F;
   FmT_Mat[0][1] = (F_Mat[1][2]*F_Mat[2][0] - F_Mat[2][2]*F_Mat[1][0]) / J_F;
@@ -658,7 +658,7 @@ void CFEANonlinearElasticity::Compute_FmT_Mat(void) {
 
 }
 
-void CFEANonlinearElasticity::Compute_Isochoric_F_b(void) {
+void CFEANonlinearElasticity::Compute_Isochoric_F_b() {
 
   unsigned short iVar, jVar, kVar;
 
@@ -684,7 +684,7 @@ void CFEANonlinearElasticity::Compute_Isochoric_F_b(void) {
 
 }
 
-void CFEANonlinearElasticity::Assign_cijkl_D_Mat(void) {
+void CFEANonlinearElasticity::Assign_cijkl_D_Mat() {
 
   unsigned short iVar, jVar;
 
diff --git a/SU2_CFD/src/numerics/flow/convection/ausm_slau.cpp b/SU2_CFD/src/numerics/flow/convection/ausm_slau.cpp
index 8cd12d5184f..3d0286a0757 100644
--- a/SU2_CFD/src/numerics/flow/convection/ausm_slau.cpp
+++ b/SU2_CFD/src/numerics/flow/convection/ausm_slau.cpp
@@ -60,7 +60,7 @@ CUpwAUSMPLUS_SLAU_Base_Flow::CUpwAUSMPLUS_SLAU_Base_Flow(unsigned short val_nDim
   }
 }
 
-CUpwAUSMPLUS_SLAU_Base_Flow::~CUpwAUSMPLUS_SLAU_Base_Flow(void) {
+CUpwAUSMPLUS_SLAU_Base_Flow::~CUpwAUSMPLUS_SLAU_Base_Flow() {
 
   delete [] psi_i;
   delete [] psi_j;
@@ -812,7 +812,7 @@ CUpwAUSM_Flow::CUpwAUSM_Flow(unsigned short val_nDim, unsigned short val_nVar, c
   }
 }
 
-CUpwAUSM_Flow::~CUpwAUSM_Flow(void) {
+CUpwAUSM_Flow::~CUpwAUSM_Flow() {
 
   delete [] Flux;
   delete [] Diff_U;
diff --git a/SU2_CFD/src/numerics/flow/convection/centered.cpp b/SU2_CFD/src/numerics/flow/convection/centered.cpp
index 62fb21fa4de..88ba161f45d 100644
--- a/SU2_CFD/src/numerics/flow/convection/centered.cpp
+++ b/SU2_CFD/src/numerics/flow/convection/centered.cpp
@@ -60,7 +60,7 @@ CCentLaxInc_Flow::CCentLaxInc_Flow(unsigned short val_nDim, unsigned short val_n
 
 }
 
-CCentLaxInc_Flow::~CCentLaxInc_Flow(void) {
+CCentLaxInc_Flow::~CCentLaxInc_Flow() {
 
   delete [] Diff_V;
   delete [] Velocity_i;
@@ -282,7 +282,7 @@ CCentJSTInc_Flow::CCentJSTInc_Flow(unsigned short val_nDim, unsigned short val_n
 
 }
 
-CCentJSTInc_Flow::~CCentJSTInc_Flow(void) {
+CCentJSTInc_Flow::~CCentJSTInc_Flow() {
 
   delete [] Diff_V;
   delete [] Diff_Lapl;
diff --git a/SU2_CFD/src/numerics/flow/convection/fds.cpp b/SU2_CFD/src/numerics/flow/convection/fds.cpp
index 5277d3834e8..1df4b04f35f 100644
--- a/SU2_CFD/src/numerics/flow/convection/fds.cpp
+++ b/SU2_CFD/src/numerics/flow/convection/fds.cpp
@@ -58,7 +58,7 @@ CUpwFDSInc_Flow::CUpwFDSInc_Flow(unsigned short val_nDim, unsigned short val_nVa
 
 }
 
-CUpwFDSInc_Flow::~CUpwFDSInc_Flow(void) {
+CUpwFDSInc_Flow::~CUpwFDSInc_Flow() {
 
   delete [] Flux;
   delete [] Diff_V;
diff --git a/SU2_CFD/src/numerics/flow/convection/fvs.cpp b/SU2_CFD/src/numerics/flow/convection/fvs.cpp
index 6e16b7dba1d..a156a1b7c31 100644
--- a/SU2_CFD/src/numerics/flow/convection/fvs.cpp
+++ b/SU2_CFD/src/numerics/flow/convection/fvs.cpp
@@ -65,7 +65,7 @@ CUpwMSW_Flow::CUpwMSW_Flow(unsigned short val_nDim, unsigned short val_nVar, con
 
 }
 
-CUpwMSW_Flow::~CUpwMSW_Flow(void) {
+CUpwMSW_Flow::~CUpwMSW_Flow() {
 
   delete [] Fc_i;
   delete [] Fc_j;
diff --git a/SU2_CFD/src/numerics/flow/convection/hllc.cpp b/SU2_CFD/src/numerics/flow/convection/hllc.cpp
index 6fa329f1221..44acc4c806e 100644
--- a/SU2_CFD/src/numerics/flow/convection/hllc.cpp
+++ b/SU2_CFD/src/numerics/flow/convection/hllc.cpp
@@ -59,7 +59,7 @@ CUpwHLLC_Flow::CUpwHLLC_Flow(unsigned short val_nDim, unsigned short val_nVar, c
   }
 }
 
-CUpwHLLC_Flow::~CUpwHLLC_Flow(void) {
+CUpwHLLC_Flow::~CUpwHLLC_Flow() {
 
   delete [] IntermediateState;
   delete [] dSm_dU;
@@ -583,7 +583,7 @@ CUpwGeneralHLLC_Flow::CUpwGeneralHLLC_Flow(unsigned short val_nDim, unsigned sho
   }
 }
 
-CUpwGeneralHLLC_Flow::~CUpwGeneralHLLC_Flow(void) {
+CUpwGeneralHLLC_Flow::~CUpwGeneralHLLC_Flow() {
 
   delete [] IntermediateState;
   delete [] dSm_dU;
diff --git a/SU2_CFD/src/numerics/flow/convection/roe.cpp b/SU2_CFD/src/numerics/flow/convection/roe.cpp
index 5dbce713115..75cf2fa2bce 100644
--- a/SU2_CFD/src/numerics/flow/convection/roe.cpp
+++ b/SU2_CFD/src/numerics/flow/convection/roe.cpp
@@ -61,7 +61,7 @@ CUpwRoeBase_Flow::CUpwRoeBase_Flow(unsigned short val_nDim, unsigned short val_n
 
 }
 
-CUpwRoeBase_Flow::~CUpwRoeBase_Flow(void) {
+CUpwRoeBase_Flow::~CUpwRoeBase_Flow() {
 
   delete [] Flux;
   delete [] Diff_U;
@@ -477,7 +477,7 @@ CUpwTurkel_Flow::CUpwTurkel_Flow(unsigned short val_nDim, unsigned short val_nVa
   }
 }
 
-CUpwTurkel_Flow::~CUpwTurkel_Flow(void) {
+CUpwTurkel_Flow::~CUpwTurkel_Flow() {
 
   delete [] Flux;
   delete [] Diff_U;
@@ -709,7 +709,7 @@ CUpwGeneralRoe_Flow::CUpwGeneralRoe_Flow(unsigned short val_nDim, unsigned short
   }
 }
 
-CUpwGeneralRoe_Flow::~CUpwGeneralRoe_Flow(void) {
+CUpwGeneralRoe_Flow::~CUpwGeneralRoe_Flow() {
 
   delete [] Flux;
   delete [] Diff_U;
diff --git a/SU2_CFD/src/numerics/template.cpp b/SU2_CFD/src/numerics/template.cpp
index d81bba8d32f..b0c07932c81 100644
--- a/SU2_CFD/src/numerics/template.cpp
+++ b/SU2_CFD/src/numerics/template.cpp
@@ -32,9 +32,7 @@ CConvective_Template::CConvective_Template(unsigned short val_nDim, unsigned sho
 
 }
 
-CConvective_Template::~CConvective_Template(void) {
-
-}
+CConvective_Template::~CConvective_Template() = default;
 
 void CConvective_Template::ComputeResidual(su2double *val_residual, su2double **val_Jacobian_i,
                                            su2double **val_Jacobian_j, CConfig *config) {
@@ -46,9 +44,7 @@ CViscous_Template::CViscous_Template(unsigned short val_nDim, unsigned short val
 
 }
 
-CViscous_Template::~CViscous_Template(void) {
-
-}
+CViscous_Template::~CViscous_Template() = default;
 
 void CViscous_Template::ComputeResidual(su2double *val_residual, su2double **val_Jacobian_i,
                                         su2double **val_Jacobian_j, CConfig *config) {
@@ -61,9 +57,7 @@ CSource_Template::CSource_Template(unsigned short val_nDim, unsigned short val_n
 
 }
 
-CSource_Template::~CSource_Template(void) {
-
-}
+CSource_Template::~CSource_Template() = default;
 
 void CSource_Template::ComputeResidual(su2double *val_residual, su2double **val_Jacobian_i, CConfig *config) {
 
diff --git a/SU2_CFD/src/output/CAdjElasticityOutput.cpp b/SU2_CFD/src/output/CAdjElasticityOutput.cpp
index d0a1e00d0f8..8ed7017aba2 100644
--- a/SU2_CFD/src/output/CAdjElasticityOutput.cpp
+++ b/SU2_CFD/src/output/CAdjElasticityOutput.cpp
@@ -93,7 +93,7 @@ CAdjElasticityOutput::CAdjElasticityOutput(CConfig *config, unsigned short nDim)
 
 }
 
-CAdjElasticityOutput::~CAdjElasticityOutput(void) {}
+CAdjElasticityOutput::~CAdjElasticityOutput() = default;
 
 void CAdjElasticityOutput::SetHistoryOutputFields(CConfig *config){
 
diff --git a/SU2_CFD/src/output/CAdjFlowCompOutput.cpp b/SU2_CFD/src/output/CAdjFlowCompOutput.cpp
index cac0326c221..7555b7ca6c3 100644
--- a/SU2_CFD/src/output/CAdjFlowCompOutput.cpp
+++ b/SU2_CFD/src/output/CAdjFlowCompOutput.cpp
@@ -91,7 +91,7 @@ CAdjFlowCompOutput::CAdjFlowCompOutput(CConfig *config, unsigned short nDim) : C
 
 }
 
-CAdjFlowCompOutput::~CAdjFlowCompOutput(void) {}
+CAdjFlowCompOutput::~CAdjFlowCompOutput() = default;
 
 void CAdjFlowCompOutput::SetHistoryOutputFields(CConfig *config) {
 
diff --git a/SU2_CFD/src/output/CAdjFlowIncOutput.cpp b/SU2_CFD/src/output/CAdjFlowIncOutput.cpp
index 93c89ca6ada..6b58c2206b2 100644
--- a/SU2_CFD/src/output/CAdjFlowIncOutput.cpp
+++ b/SU2_CFD/src/output/CAdjFlowIncOutput.cpp
@@ -97,7 +97,7 @@ CAdjFlowIncOutput::CAdjFlowIncOutput(CConfig *config, unsigned short nDim) : CAd
 
 }
 
-CAdjFlowIncOutput::~CAdjFlowIncOutput(void) {}
+CAdjFlowIncOutput::~CAdjFlowIncOutput() = default;
 
 void CAdjFlowIncOutput::SetHistoryOutputFields(CConfig *config) {
 
diff --git a/SU2_CFD/src/output/CAdjHeatOutput.cpp b/SU2_CFD/src/output/CAdjHeatOutput.cpp
index a908ee6e059..65d5679b8ca 100644
--- a/SU2_CFD/src/output/CAdjHeatOutput.cpp
+++ b/SU2_CFD/src/output/CAdjHeatOutput.cpp
@@ -88,7 +88,7 @@ CAdjHeatOutput::CAdjHeatOutput(CConfig *config, unsigned short nDim) : COutput(c
 
 }
 
-CAdjHeatOutput::~CAdjHeatOutput(void) {}
+CAdjHeatOutput::~CAdjHeatOutput() = default;
 
 void CAdjHeatOutput::SetHistoryOutputFields(CConfig *config){
 
diff --git a/SU2_CFD/src/output/CBaselineOutput.cpp b/SU2_CFD/src/output/CBaselineOutput.cpp
index 167173fa183..8493335393e 100644
--- a/SU2_CFD/src/output/CBaselineOutput.cpp
+++ b/SU2_CFD/src/output/CBaselineOutput.cpp
@@ -67,7 +67,7 @@ CBaselineOutput::CBaselineOutput(CConfig *config, unsigned short nDim, CSolver*
 
 }
 
-CBaselineOutput::~CBaselineOutput(void) {}
+CBaselineOutput::~CBaselineOutput() = default;
 
 void CBaselineOutput::SetVolumeOutputFields(CConfig *config){
 
diff --git a/SU2_CFD/src/output/CFlowCompFEMOutput.cpp b/SU2_CFD/src/output/CFlowCompFEMOutput.cpp
index e0417d57fa0..91ce4393034 100644
--- a/SU2_CFD/src/output/CFlowCompFEMOutput.cpp
+++ b/SU2_CFD/src/output/CFlowCompFEMOutput.cpp
@@ -81,7 +81,7 @@ CFlowCompFEMOutput::CFlowCompFEMOutput(CConfig *config, unsigned short nDim) : C
 
 }
 
-CFlowCompFEMOutput::~CFlowCompFEMOutput(void) {}
+CFlowCompFEMOutput::~CFlowCompFEMOutput() = default;
 
 
 
@@ -165,7 +165,7 @@ void CFlowCompFEMOutput::LoadVolumeDataFEM(CConfig *config, CGeometry *geometry,
   /*--- Create an object of the class CMeshFEM_DG and retrieve the necessary
    geometrical information for the FEM DG solver. ---*/
 
-  CMeshFEM_DG *DGGeometry = dynamic_cast<CMeshFEM_DG *>(geometry);
+  auto *DGGeometry = dynamic_cast<CMeshFEM_DG *>(geometry);
 
   CVolumeElementFEM *volElem  = DGGeometry->GetVolElem();
 
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index 5be001f5a5a..1026b3d13e2 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -1479,7 +1479,8 @@ void CFlowOutput::AddHeatCoefficients(const CConfig* config) {
   AddHistoryOutput("MAXIMUM_HEATFLUX", "maxHF", ScreenOutputFormat::SCIENTIFIC, "HEAT", "Maximum heatflux across all surfaces set with MARKER_MONITORING.", HistoryFieldType::COEFFICIENT);
 
   vector<string> Marker_Monitoring;
-  for (auto iMarker = 0u; iMarker < config->GetnMarker_Monitoring(); iMarker++) {
+  Marker_Monitoring.reserve(config->GetnMarker_Monitoring());
+for (auto iMarker = 0u; iMarker < config->GetnMarker_Monitoring(); iMarker++) {
     Marker_Monitoring.push_back(config->GetMarker_Monitoring_TagBound(iMarker));
   }
   /// DESCRIPTION:  Total heatflux
@@ -2145,7 +2146,7 @@ void CFlowOutput::WriteForcesBreakdown(const CConfig* config, const CSolver* flo
 
   auto fileName = config->GetBreakdown_FileName();
   if (unsteady) {
-    const auto lastindex = fileName.find_last_of(".");
+    const auto lastindex = fileName.find_last_of('.');
     const auto ext = fileName.substr(lastindex, fileName.size());
     fileName = fileName.substr(0, lastindex);
     fileName = config->GetFilename(fileName, ext, curTimeIter);
@@ -3626,8 +3627,8 @@ bool CFlowOutput::WriteVolumeOutput(CConfig *config, unsigned long Iter, bool fo
     /* only write 'double' files for the restart files */
     if ((config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND) &&
       ((Iter == 0) || (Iter % config->GetVolumeOutputFrequency(iFile) == 0) ||
-      (((Iter+1) % config->GetVolumeOutputFrequency(iFile) == 0) && writeRestart==true) || // Restarts need 2 old solutions.
-      (((Iter+2) == config->GetnTime_Iter()) && writeRestart==true))){      // The last timestep is written anyway but one needs the step before for restarts.
+      (((Iter+1) % config->GetVolumeOutputFrequency(iFile) == 0) && writeRestart) || // Restarts need 2 old solutions.
+      (((Iter+2) == config->GetnTime_Iter()) && writeRestart))){      // The last timestep is written anyway but one needs the step before for restarts.
       return true;
     }
   } else {
@@ -3635,7 +3636,7 @@ bool CFlowOutput::WriteVolumeOutput(CConfig *config, unsigned long Iter, bool fo
     return ((Iter > 0) && Iter % config->GetVolumeOutputFrequency(iFile) == 0) || force_writing;
   }
 
-  return false || force_writing;
+  return force_writing;
 }
 
 void CFlowOutput::SetTimeAveragedFields(){
diff --git a/SU2_CFD/src/output/CMeshOutput.cpp b/SU2_CFD/src/output/CMeshOutput.cpp
index b06c2441463..4d5c6e1dd1e 100644
--- a/SU2_CFD/src/output/CMeshOutput.cpp
+++ b/SU2_CFD/src/output/CMeshOutput.cpp
@@ -46,7 +46,7 @@ CMeshOutput::CMeshOutput(CConfig *config, unsigned short nDim) : COutput(config,
 
 }
 
-CMeshOutput::~CMeshOutput(void) {}
+CMeshOutput::~CMeshOutput() = default;
 
 void CMeshOutput::SetVolumeOutputFields(CConfig *config){
 
diff --git a/SU2_CFD/src/output/COutput.cpp b/SU2_CFD/src/output/COutput.cpp
index 646cc521c93..9e95c9b4614 100644
--- a/SU2_CFD/src/output/COutput.cpp
+++ b/SU2_CFD/src/output/COutput.cpp
@@ -172,7 +172,7 @@ COutput::COutput(const CConfig *config, unsigned short ndim, bool fem_output):
 
 }
 
-COutput::~COutput(void) {
+COutput::~COutput() {
 
   delete convergenceTable;
   delete multiZoneHeaderTable;
@@ -339,7 +339,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
   CFileWriter *fileWriter = nullptr;
 
   /*--- if it is still present, strip the extension (suffix) from the filename ---*/
-  unsigned short lastindex = fileName.find_last_of(".");
+  unsigned short lastindex = fileName.find_last_of('.');
   fileName = fileName.substr(0, lastindex);
 
   string filename_iter, extension;
@@ -581,7 +581,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
 
         /*--- We cast the pointer to its true type, to avoid virtual functions ---*/
 
-        CParaviewVTMFileWriter* vtmWriter = dynamic_cast<CParaviewVTMFileWriter*>(fileWriter);
+        auto* vtmWriter = dynamic_cast<CParaviewVTMFileWriter*>(fileWriter);
 
         /*--- then we write the data into the folder---*/
         vtmWriter->WriteFolderData(fileName, config, multiZoneHeaderString, volumeDataSorter,surfaceDataSorter, geometry);
@@ -1123,8 +1123,7 @@ bool COutput::MonitorTimeConvergence(CConfig *config, unsigned long TimeIteratio
             }
             WndCauchy_Value /= nWndCauchy_Elems;
           }
-          if (WndCauchy_Value >= wndCauchyEps){fieldConverged = false;}
-          else{fieldConverged = true;}
+          fieldConverged = WndCauchy_Value < wndCauchyEps;
 
           /*--- Start monitoring only if the current iteration is larger than the
            *  number of cauchy elements and the number of start-up iterations ---*/
@@ -1595,13 +1594,13 @@ void COutput::PreprocessVolumeOutput(CConfig *config){
   /*---Coordinates and solution groups must be always in the output.
    * If they are not requested, add them here. ---*/
 
-  vector<string>::iterator itCoord = std::find(requestedVolumeFields.begin(),
+  auto itCoord = std::find(requestedVolumeFields.begin(),
                                           requestedVolumeFields.end(), "COORDINATES");
   if (itCoord == requestedVolumeFields.end()){
     requestedVolumeFields.emplace_back("COORDINATES");
     nRequestedVolumeFields++;
   }
-  vector<string>::iterator itSol = std::find(requestedVolumeFields.begin(),
+  auto itSol = std::find(requestedVolumeFields.begin(),
                                           requestedVolumeFields.end(), "SOLUTION");
   if (itSol == requestedVolumeFields.end()){
     requestedVolumeFields.emplace_back("SOLUTION");
@@ -1698,7 +1697,7 @@ void COutput::LoadDataIntoSorter(CConfig* config, CGeometry* geometry, CSolver**
     /*--- Create an object of the class CMeshFEM_DG and retrieve the necessary
      geometrical information for the FEM DG solver. ---*/
 
-    CMeshFEM_DG *DGGeometry = dynamic_cast<CMeshFEM_DG *>(geometry);
+    auto *DGGeometry = dynamic_cast<CMeshFEM_DG *>(geometry);
 
     unsigned long nVolElemOwned = DGGeometry->GetNVolElemOwned();
 
@@ -1761,7 +1760,7 @@ void COutput::LoadDataIntoSorter(CConfig* config, CGeometry* geometry, CSolver**
   }
 }
 
-void COutput::SetVolumeOutputValue(string name, unsigned long iPoint, su2double value){
+void COutput::SetVolumeOutputValue(const string& name, unsigned long iPoint, su2double value){
 
   if (buildFieldIndexCache){
 
@@ -1793,7 +1792,7 @@ void COutput::SetVolumeOutputValue(string name, unsigned long iPoint, su2double
 
 }
 
-su2double COutput::GetVolumeOutputValue(string name, unsigned long iPoint){
+su2double COutput::GetVolumeOutputValue(const string& name, unsigned long iPoint){
 
   if (buildFieldIndexCache){
 
@@ -1827,7 +1826,7 @@ su2double COutput::GetVolumeOutputValue(string name, unsigned long iPoint){
   return 0.0;
 }
 
-void COutput::SetAvgVolumeOutputValue(string name, unsigned long iPoint, su2double value){
+void COutput::SetAvgVolumeOutputValue(const string& name, unsigned long iPoint, su2double value){
 
   const su2double scaling = 1.0 / su2double(curAbsTimeIter + 1);
 
@@ -1908,7 +1907,7 @@ void COutput::PostprocessHistoryData(CConfig *config){
     }
   }
 
-  map<string, pair<su2double, int> >::iterator it = Average.begin();
+  auto it = Average.begin();
   for (it = Average.begin(); it != Average.end(); it++){
     const su2double& value = it->second.first;
     const int& count = it->second.second;
@@ -1933,7 +1932,7 @@ void COutput::PostprocessHistoryFields(CConfig *config){
     }
   }
 
-  map<string, bool>::iterator it = Average.begin();
+  auto it = Average.begin();
   for (it = Average.begin(); it != Average.end(); it++){
     if (AverageGroupName.count(it->first) > 0) {
       AddHistoryOutput("AVG_" + it->first, "avg[" + AverageGroupName[it->first] + "]", ScreenOutputFormat::FIXED,
@@ -2254,7 +2253,7 @@ void COutput::SetCustomOutputs(const CConfig* config) {
         break;
       }
 
-      customOutputs.push_back(CustomOutput());
+      customOutputs.emplace_back();
       auto& output = customOutputs.back();
 
       output.name = std::move(name);
@@ -2331,7 +2330,7 @@ void COutput::PrintHistoryFields() const {
       if (!perSurf) {
         Field = &historyOutput_Map.at(outputName);
       } else {
-        Field = &historyOutputPerSurface_Map.at(outputName)[0];
+        Field = historyOutputPerSurface_Map.at(outputName).data();
       }
       if (perSurf || !Field->description.empty()) {
         NameSize = std::max(NameSize, outputName.size());
@@ -2360,7 +2359,7 @@ void COutput::PrintHistoryFields() const {
       if (!perSurf) {
         Field = &historyOutput_Map.at(outputName);
       } else {
-        Field = &historyOutputPerSurface_Map.at(outputName)[0];
+        Field = historyOutputPerSurface_Map.at(outputName).data();
       }
 
       if (!perSurf && Field->description.empty()) continue;
@@ -2419,7 +2418,7 @@ void COutput::PrintHistoryFields() const {
           break;
       }
 
-      if (Field.description != "")
+      if (!Field.description.empty())
         ModifierTable << historyOutput_List[iField] << Field.outputGroup << type << Field.description;
 
       GroupVisited[Field.outputGroup] = true;
@@ -2442,7 +2441,7 @@ void COutput::PrintVolumeFields(){
 
       VolumeOutputField &Field = volumeOutput_Map.at(volumeOutput_List[iField]);
 
-      if (Field.description != ""){
+      if (!Field.description.empty()){
         if (volumeOutput_List[iField].size() > NameSize){
           NameSize = volumeOutput_List[iField].size();
         }
@@ -2468,7 +2467,7 @@ void COutput::PrintVolumeFields(){
 
       VolumeOutputField &Field = volumeOutput_Map.at(volumeOutput_List[iField]);
 
-      if (Field.description != "")
+      if (!Field.description.empty())
         VolumeFieldTable << volumeOutput_List[iField] << Field.outputGroup << Field.description;
 
     }
diff --git a/SU2_CFD/src/output/COutputFactory.cpp b/SU2_CFD/src/output/COutputFactory.cpp
index fe0de7c9397..5db87d58fc5 100644
--- a/SU2_CFD/src/output/COutputFactory.cpp
+++ b/SU2_CFD/src/output/COutputFactory.cpp
@@ -93,7 +93,7 @@ COutput* COutputFactory::CreateMultizoneOutput(CConfig *driverConfig, CConfig**
 
 COutputLegacy* COutputFactory::CreateLegacyOutput(CConfig *config){
 
-  COutputLegacy* output = new COutputLegacy(config);
+  auto* output = new COutputLegacy(config);
 
   return output;
 
diff --git a/SU2_CFD/src/output/filewriter/CCGNSFileWriter.cpp b/SU2_CFD/src/output/filewriter/CCGNSFileWriter.cpp
index a84676bc275..8436698b3c2 100644
--- a/SU2_CFD/src/output/filewriter/CCGNSFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CCGNSFileWriter.cpp
@@ -77,7 +77,7 @@ void CCGNSFileWriter::WriteData(string val_filename) {
 }
 
 #ifdef HAVE_CGNS
-void CCGNSFileWriter::InitializeMeshFile(string val_filename) {
+void CCGNSFileWriter::InitializeMeshFile(const string& val_filename) {
   if (!dataSorter->GetConnectivitySorted()) {
     SU2_MPI::Error("Connectivity must be sorted.", CURRENT_FUNCTION);
   }
@@ -131,7 +131,7 @@ void CCGNSFileWriter::WriteField(int iField, const string& FieldName) {
 
   /*--- Coordinate vector is written in blocks, one for each process. ---*/
   cgsize_t nodeBegin = 1;
-  cgsize_t nodeEnd = static_cast<cgsize_t>(nLocalPoints);
+  auto nodeEnd = static_cast<cgsize_t>(nLocalPoints);
 
   if (isCoord) {
     int CoordinateNumber;
diff --git a/SU2_CFD/src/output/filewriter/CCSVFileWriter.cpp b/SU2_CFD/src/output/filewriter/CCSVFileWriter.cpp
index 08a67d5e013..0ec0ba89b9d 100644
--- a/SU2_CFD/src/output/filewriter/CCSVFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CCSVFileWriter.cpp
@@ -29,12 +29,10 @@
 #include "../../../include/output/filewriter/CParallelDataSorter.hpp"
 
 CCSVFileWriter::CCSVFileWriter(CParallelDataSorter *valDataSorter) :
-  CFileWriter(valDataSorter, std::move(".csv")){}
+  CFileWriter(valDataSorter, ".csv"){}
 
 
-CCSVFileWriter::~CCSVFileWriter(){
-
-}
+CCSVFileWriter::~CCSVFileWriter()= default;
 
 void CCSVFileWriter::WriteData(string val_filename){
 
@@ -79,10 +77,10 @@ void CCSVFileWriter::WriteData(string val_filename){
 
   /*--- Allocate buffers for send/recv of the data and global IDs. ---*/
 
-  su2double *bufD_Send = new su2double[MaxLocalVertex_Surface*fieldNames.size()]();
+  auto *bufD_Send = new su2double[MaxLocalVertex_Surface*fieldNames.size()]();
   su2double *bufD_Recv = nullptr;
 
-  unsigned long *bufL_Send = new unsigned long [MaxLocalVertex_Surface]();
+  auto *bufL_Send = new unsigned long [MaxLocalVertex_Surface]();
   unsigned long *bufL_Recv = nullptr;
 
   /*--- Load send buffers with the local data on this rank. ---*/
diff --git a/SU2_CFD/src/output/filewriter/CFEMDataSorter.cpp b/SU2_CFD/src/output/filewriter/CFEMDataSorter.cpp
index 0bb123b0c50..4fd7bdf780d 100644
--- a/SU2_CFD/src/output/filewriter/CFEMDataSorter.cpp
+++ b/SU2_CFD/src/output/filewriter/CFEMDataSorter.cpp
@@ -37,7 +37,7 @@ CFEMDataSorter::CFEMDataSorter(CConfig *config, CGeometry *geometry, const vecto
   /*--- Create an object of the class CMeshFEM_DG and retrieve the necessary
    geometrical information for the FEM DG solver. ---*/
 
-  CMeshFEM_DG *DGGeometry = dynamic_cast<CMeshFEM_DG *>(geometry);
+  auto *DGGeometry = dynamic_cast<CMeshFEM_DG *>(geometry);
 
   unsigned long nVolElemOwned = DGGeometry->GetNVolElemOwned();
   CVolumeElementFEM *volElem  = DGGeometry->GetVolElem();
@@ -126,7 +126,7 @@ void CFEMDataSorter::SortVolumetricConnectivity(CConfig *config, CGeometry *geom
 
   /*--- Create an object of the class CMeshFEM_DG and retrieve the necessary
         geometrical information for the FEM DG solver. ---*/
-  CMeshFEM_DG *DGGeometry = dynamic_cast<CMeshFEM_DG *>(geometry);
+  auto *DGGeometry = dynamic_cast<CMeshFEM_DG *>(geometry);
 
   unsigned long nVolElemOwned = DGGeometry->GetNVolElemOwned();
   CVolumeElementFEM *volElem  = DGGeometry->GetVolElem();
diff --git a/SU2_CFD/src/output/filewriter/CFVMDataSorter.cpp b/SU2_CFD/src/output/filewriter/CFVMDataSorter.cpp
index fc7c0f6c811..664142e3901 100644
--- a/SU2_CFD/src/output/filewriter/CFVMDataSorter.cpp
+++ b/SU2_CFD/src/output/filewriter/CFVMDataSorter.cpp
@@ -258,10 +258,10 @@ void CFVMDataSorter::SortVolumetricConnectivity(CConfig *config,
   /*--- Create an index variable to keep track of our index
    position as we load up the send buffer. ---*/
 
-  unsigned long *index = new unsigned long[size]();
+  auto *index = new unsigned long[size]();
   for (int ii=0; ii < size; ii++) index[ii] = NODES_PER_ELEMENT*nElem_Send[ii];
 
-  unsigned long *haloIndex = new unsigned long[size]();
+  auto *haloIndex = new unsigned long[size]();
   for (int ii=0; ii < size; ii++) haloIndex[ii] = nElem_Send[ii];
 
   /*--- Loop through our elements and load the elems and their
diff --git a/SU2_CFD/src/output/filewriter/CParallelDataSorter.cpp b/SU2_CFD/src/output/filewriter/CParallelDataSorter.cpp
index a3b372183bd..f4b57b34f3b 100644
--- a/SU2_CFD/src/output/filewriter/CParallelDataSorter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParallelDataSorter.cpp
@@ -32,7 +32,7 @@
 CParallelDataSorter::CParallelDataSorter(CConfig *config, const vector<string> &valFieldNames) :
   rank(SU2_MPI::GetRank()),
   size(SU2_MPI::GetSize()),
-  fieldNames(std::move(valFieldNames)) {
+  fieldNames(valFieldNames) {
 
   GlobalField_Counter = fieldNames.size();
 
diff --git a/SU2_CFD/src/output/filewriter/CParallelFileWriter.cpp b/SU2_CFD/src/output/filewriter/CParallelFileWriter.cpp
index 1a4f8c5d5cb..7f448c880cf 100644
--- a/SU2_CFD/src/output/filewriter/CParallelFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParallelFileWriter.cpp
@@ -25,10 +25,12 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
+#include <utility>
+
 #include "../../../include/output/filewriter/CFileWriter.hpp"
 
 CFileWriter::CFileWriter(CParallelDataSorter *valDataSorter, string valFileExt):
-  fileExt(valFileExt),
+  fileExt(std::move(valFileExt)),
   dataSorter(valDataSorter){
 
   rank = SU2_MPI::GetRank();
@@ -40,7 +42,7 @@ CFileWriter::CFileWriter(CParallelDataSorter *valDataSorter, string valFileExt):
 }
 
 CFileWriter::CFileWriter(string valFileExt):
-  fileExt(valFileExt){
+  fileExt(std::move(valFileExt)){
 
   rank = SU2_MPI::GetRank();
   size = SU2_MPI::GetSize();
@@ -50,9 +52,7 @@ CFileWriter::CFileWriter(string valFileExt):
 
 }
 
-CFileWriter::~CFileWriter(){
-
-}
+CFileWriter::~CFileWriter()= default;
 
 bool CFileWriter::WriteMPIBinaryDataAll(const void *data, unsigned long sizeInBytes,
                                         unsigned long totalSizeInBytes, unsigned long offsetInBytes){
diff --git a/SU2_CFD/src/output/filewriter/CParaviewBinaryFileWriter.cpp b/SU2_CFD/src/output/filewriter/CParaviewBinaryFileWriter.cpp
index 530c1de149a..677bee21961 100644
--- a/SU2_CFD/src/output/filewriter/CParaviewBinaryFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParaviewBinaryFileWriter.cpp
@@ -39,14 +39,11 @@ CParaviewBinaryFileWriter::CParaviewBinaryFileWriter(CParallelDataSorter *valDat
   bigEndian = false;
   unsigned int i = 1;
   char *c = (char*)&i;
-  if (*c) bigEndian = false;
-  else bigEndian = true;
+  bigEndian = *c == 0;
 }
 
 
-CParaviewBinaryFileWriter::~CParaviewBinaryFileWriter(){
-
-}
+CParaviewBinaryFileWriter::~CParaviewBinaryFileWriter()= default;
 
 void CParaviewBinaryFileWriter::WriteData(string val_filename){
 
@@ -97,7 +94,7 @@ void CParaviewBinaryFileWriter::WriteData(string val_filename){
       if (nDim == 2 && iDim == 2) {
         dataBufferFloat[iPoint*NCOORDS + iDim] = 0.0;
       } else {
-        float val = (float)dataSorter->GetData(iDim, iPoint);
+        auto val = (float)dataSorter->GetData(iDim, iPoint);
         dataBufferFloat[iPoint*NCOORDS + iDim] = val;
       }
     }
@@ -178,7 +175,7 @@ void CParaviewBinaryFileWriter::WriteData(string val_filename){
   /*--- Load/write the cell type for all elements in the file. ---*/
 
   vector<int> typeBuf(myElem);
-  vector<int>::iterator typeIter = typeBuf.begin();
+  auto typeIter = typeBuf.begin();
 
   std::fill(typeIter, typeIter+nParallel_Line, LINE);          typeIter += nParallel_Line;
   std::fill(typeIter, typeIter+nParallel_Tria, TRIANGLE);      typeIter += nParallel_Tria;
@@ -285,7 +282,7 @@ void CParaviewBinaryFileWriter::WriteData(string val_filename){
        This will be replaced with a derived data type most likely. ---*/
 
       for (iPoint = 0; iPoint < myPoint; iPoint++) {
-        float val = (float)dataSorter->GetData(VarCounter,iPoint);
+        auto val = (float)dataSorter->GetData(VarCounter,iPoint);
         dataBufferFloat[iPoint] = val;
       }
 
diff --git a/SU2_CFD/src/output/filewriter/CParaviewFileWriter.cpp b/SU2_CFD/src/output/filewriter/CParaviewFileWriter.cpp
index 05f8b95133d..9e3c7726ac1 100644
--- a/SU2_CFD/src/output/filewriter/CParaviewFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParaviewFileWriter.cpp
@@ -33,7 +33,7 @@ CParaviewFileWriter::CParaviewFileWriter(CParallelDataSorter *valDataSorter) :
   CFileWriter(valDataSorter, fileExt){}
 
 
-CParaviewFileWriter::~CParaviewFileWriter(){}
+CParaviewFileWriter::~CParaviewFileWriter()= default;
 
 void CParaviewFileWriter::WriteData(string val_filename){
 
diff --git a/SU2_CFD/src/output/filewriter/CParaviewVTMFileWriter.cpp b/SU2_CFD/src/output/filewriter/CParaviewVTMFileWriter.cpp
index 98bc3bdc511..2b67324b64d 100644
--- a/SU2_CFD/src/output/filewriter/CParaviewVTMFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParaviewVTMFileWriter.cpp
@@ -25,6 +25,8 @@
  * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
  */
 
+#include <utility>
+
 #include "../../../include/output/filewriter/CParaviewVTMFileWriter.hpp"
 #include "../../../include/output/filewriter/CParaviewXMLFileWriter.hpp"
 #include "../../../../Common/include/toolboxes/printing_toolbox.hpp"
@@ -43,9 +45,7 @@ CParaviewVTMFileWriter::CParaviewVTMFileWriter(su2double valTime,
 }
 
 
-CParaviewVTMFileWriter::~CParaviewVTMFileWriter(){
-
-}
+CParaviewVTMFileWriter::~CParaviewVTMFileWriter()= default;
 
 void CParaviewVTMFileWriter::WriteData(string val_filename){
 
@@ -63,7 +63,7 @@ void CParaviewVTMFileWriter::WriteData(string val_filename){
       multiBlockFile.open(val_filename.c_str(), ios::app);
 
     if (iZone == 0){
-      multiBlockFile << "<VTKFile type=\"vtkMultiBlockDataSet\" version=\"1.0\">" << endl;
+      multiBlockFile << R"(<VTKFile type="vtkMultiBlockDataSet" version="1.0">)" << endl;
       multiBlockFile << "<vtkMultiBlockDataSet>" << endl;
     }
 
@@ -87,7 +87,7 @@ void CParaviewVTMFileWriter::WriteData(string val_filename){
 
 }
 
-void CParaviewVTMFileWriter::AddDataset(string foldername, string name, string file, CParallelDataSorter* dataSorter){
+void CParaviewVTMFileWriter::AddDataset(const string& foldername, string name, const string& file, CParallelDataSorter* dataSorter){
 
   /*--- Construct the full file name incl. folder ---*/
   /*--- Note that the folder name is simply the filename ---*/
@@ -101,7 +101,7 @@ void CParaviewVTMFileWriter::AddDataset(string foldername, string name, string f
 
   /*--- Add the dataset to the vtm file ---*/
 
-  AddDataset(name, fullFilename + CParaviewXMLFileWriter::fileExt);
+  AddDataset(std::move(name), fullFilename + CParaviewXMLFileWriter::fileExt);
 
   /*--- Update the bandwidth ---*/
 
@@ -114,7 +114,7 @@ void CParaviewVTMFileWriter::AddDataset(string foldername, string name, string f
 
 
 
-void CParaviewVTMFileWriter::WriteFolderData(string foldername, CConfig *config,
+void CParaviewVTMFileWriter::WriteFolderData(const string& foldername, CConfig *config,
                                              string multiZoneHeaderString,
                                              CParallelDataSorter* volumeDataSorter,
                                              CParallelDataSorter* surfaceDataSorter,
@@ -133,7 +133,7 @@ void CParaviewVTMFileWriter::WriteFolderData(string foldername, CConfig *config,
 
    /*--- Open a block for the zone ---*/
 
-  StartBlock(multiZoneHeaderString);
+  StartBlock(std::move(multiZoneHeaderString));
 
   StartBlock("Internal");
   AddDataset(foldername,"Internal", "Internal", volumeDataSorter);
diff --git a/SU2_CFD/src/output/filewriter/CParaviewXMLFileWriter.cpp b/SU2_CFD/src/output/filewriter/CParaviewXMLFileWriter.cpp
index ff3e489a3a5..2b453723b08 100644
--- a/SU2_CFD/src/output/filewriter/CParaviewXMLFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParaviewXMLFileWriter.cpp
@@ -40,14 +40,11 @@ CParaviewXMLFileWriter::CParaviewXMLFileWriter(CParallelDataSorter *valDataSorte
   bigEndian = false;
   unsigned int i = 1;
   char *c = (char*)&i;
-  if (*c) bigEndian = false;
-  else bigEndian = true;
+  bigEndian = *c == 0;
 
 }
 
-CParaviewXMLFileWriter::~CParaviewXMLFileWriter(){
-
-}
+CParaviewXMLFileWriter::~CParaviewXMLFileWriter()= default;
 
 void CParaviewXMLFileWriter::WriteData(string val_filename){
 
@@ -197,7 +194,7 @@ void CParaviewXMLFileWriter::WriteData(string val_filename){
       if (nDim == 2 && iDim == 2) {
         dataBufferFloat[iPoint*NCOORDS + iDim] = 0.0;
       } else {
-        float val = (float)dataSorter->GetData(iDim, iPoint);
+        auto val = (float)dataSorter->GetData(iDim, iPoint);
         dataBufferFloat[iPoint*NCOORDS + iDim] = val;
       }
     }
@@ -238,7 +235,7 @@ void CParaviewXMLFileWriter::WriteData(string val_filename){
   /*--- Load/write the cell type for all elements in the file. ---*/
 
   vector<uint8_t> typeBuf(myElem);
-  vector<uint8_t>::iterator typeIter = typeBuf.begin();
+  auto typeIter = typeBuf.begin();
 
   std::fill(typeIter, typeIter+nParallel_Line, LINE);          typeIter += nParallel_Line;
   std::fill(typeIter, typeIter+nParallel_Tria, TRIANGLE);      typeIter += nParallel_Tria;
@@ -306,7 +303,7 @@ void CParaviewXMLFileWriter::WriteData(string val_filename){
        This will be replaced with a derived data type most likely. ---*/
 
       for (iPoint = 0; iPoint < myPoint; iPoint++) {
-        float val = (float)dataSorter->GetData(VarCounter,iPoint);
+        auto val = (float)dataSorter->GetData(VarCounter,iPoint);
         dataBufferFloat[iPoint] = val;
       }
 
diff --git a/SU2_CFD/src/output/filewriter/CSTLFileWriter.cpp b/SU2_CFD/src/output/filewriter/CSTLFileWriter.cpp
index 602e4844d09..3258836e479 100644
--- a/SU2_CFD/src/output/filewriter/CSTLFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CSTLFileWriter.cpp
@@ -38,7 +38,7 @@ CSTLFileWriter::CSTLFileWriter(CParallelDataSorter *valDataSorter) :
   CFileWriter(valDataSorter, fileExt){}
 
 
-CSTLFileWriter::~CSTLFileWriter(){}
+CSTLFileWriter::~CSTLFileWriter()= default;
 
 
 void CSTLFileWriter::WriteData(string val_filename){
@@ -161,7 +161,7 @@ void CSTLFileWriter::ReprocessElementConnectivity(){
   for (unsigned long i = 0; i < num_halo_nodes; ++i)
     ++num_nodes_to_receive[neighbor_partitions[i]];
   num_nodes_to_send.resize(size);
-  SU2_MPI::Alltoall(&num_nodes_to_receive[0], 1, MPI_INT, &num_nodes_to_send[0], 1, MPI_INT, SU2_MPI::GetComm());
+  SU2_MPI::Alltoall(num_nodes_to_receive.data(), 1, MPI_INT, num_nodes_to_send.data(), 1, MPI_INT, SU2_MPI::GetComm());
 
   /* Now send the global node numbers whose data we need,
      and receive the same from all other ranks.
@@ -184,8 +184,8 @@ void CSTLFileWriter::ReprocessElementConnectivity(){
      (sorted_halo_nodes) whose data we need to receive, and receiving
      lists of nodes whose data we need to send. */
   if (sorted_halo_nodes.empty()) sorted_halo_nodes.resize(1); /* Avoid crash. */
-  SU2_MPI::Alltoallv(&sorted_halo_nodes[0], &num_nodes_to_receive[0], &nodes_to_receive_displacements[0], MPI_UNSIGNED_LONG,
-                     &nodes_to_send[0],     &num_nodes_to_send[0],    &nodes_to_send_displacements[0],    MPI_UNSIGNED_LONG,
+  SU2_MPI::Alltoallv(sorted_halo_nodes.data(), num_nodes_to_receive.data(), nodes_to_receive_displacements.data(), MPI_UNSIGNED_LONG,
+                     nodes_to_send.data(),     num_nodes_to_send.data(),    nodes_to_send_displacements.data(),    MPI_UNSIGNED_LONG,
                      SU2_MPI::GetComm());
 
   /* Now actually send and receive the data */
@@ -213,8 +213,8 @@ void CSTLFileWriter::ReprocessElementConnectivity(){
 
   }
 
-  SU2_MPI::Alltoallv(&data_to_send[0],  &num_values_to_send[0],    &values_to_send_displacements[0],    MPI_DOUBLE,
-                     &halo_var_data[0], &num_values_to_receive[0], &values_to_receive_displacements[0], MPI_DOUBLE,
+  SU2_MPI::Alltoallv(data_to_send.data(),  num_values_to_send.data(),    values_to_send_displacements.data(),    MPI_DOUBLE,
+                     halo_var_data.data(), num_values_to_receive.data(), values_to_receive_displacements.data(), MPI_DOUBLE,
                      SU2_MPI::GetComm());
 }
 
@@ -313,7 +313,7 @@ void CSTLFileWriter::StoreCoordData(enum GEO_TYPE elemType,
 
 passivedouble CSTLFileWriter::GetHaloNodeValue(unsigned long global_node_number, unsigned short iVar) {
 
-  vector<unsigned long>::iterator it = lower_bound(sorted_halo_nodes.begin(), sorted_halo_nodes.end(), global_node_number);
+  auto it = lower_bound(sorted_halo_nodes.begin(), sorted_halo_nodes.end(), global_node_number);
   int offset = distance(sorted_halo_nodes.begin(), it);
   int id = 0;
 
diff --git a/SU2_CFD/src/output/filewriter/CSU2BinaryFileWriter.cpp b/SU2_CFD/src/output/filewriter/CSU2BinaryFileWriter.cpp
index 8b2fa973f00..39ec96fa178 100644
--- a/SU2_CFD/src/output/filewriter/CSU2BinaryFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CSU2BinaryFileWriter.cpp
@@ -33,9 +33,7 @@ CSU2BinaryFileWriter::CSU2BinaryFileWriter(CParallelDataSorter *valDataSorter)
   CFileWriter(valDataSorter, fileExt){}
 
 
-CSU2BinaryFileWriter::~CSU2BinaryFileWriter(){
-
-}
+CSU2BinaryFileWriter::~CSU2BinaryFileWriter()= default;
 
 void CSU2BinaryFileWriter::WriteData(string val_filename){
 
diff --git a/SU2_CFD/src/output/filewriter/CSU2MeshFileWriter.cpp b/SU2_CFD/src/output/filewriter/CSU2MeshFileWriter.cpp
index 8caf248dd74..13b0798d982 100644
--- a/SU2_CFD/src/output/filewriter/CSU2MeshFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CSU2MeshFileWriter.cpp
@@ -193,11 +193,11 @@ void CSU2MeshFileWriter::WriteData(string val_filename) {
         getline(input_file, text_line);
         text_line.erase(0,11);
         for (int iChar = 0; iChar < 20; iChar++) {
-          position = text_line.find(" ", 0);
+          position = text_line.find(' ', 0);
           if (position != string::npos) text_line.erase(position,1);
-          position = text_line.find("\r", 0);
+          position = text_line.find('\r', 0);
           if (position != string::npos) text_line.erase(position,1);
-          position = text_line.find("\n", 0);
+          position = text_line.find('\n', 0);
           if (position != string::npos) text_line.erase(position,1);
         }
         string Marker_Tag = text_line;
diff --git a/SU2_CFD/src/output/filewriter/CSurfaceFEMDataSorter.cpp b/SU2_CFD/src/output/filewriter/CSurfaceFEMDataSorter.cpp
index d8cdda2b214..e92587ae898 100644
--- a/SU2_CFD/src/output/filewriter/CSurfaceFEMDataSorter.cpp
+++ b/SU2_CFD/src/output/filewriter/CSurfaceFEMDataSorter.cpp
@@ -41,7 +41,7 @@ CSurfaceFEMDataSorter::CSurfaceFEMDataSorter(CConfig *config, CGeometry *geometr
   /*--- Create an object of the class CMeshFEM_DG and retrieve the necessary
    geometrical information for the FEM DG solver. ---*/
 
-  CMeshFEM_DG *DGGeometry = dynamic_cast<CMeshFEM_DG *>(geometry);
+  auto *DGGeometry = dynamic_cast<CMeshFEM_DG *>(geometry);
 
   unsigned long nVolElemOwned = DGGeometry->GetNVolElemOwned();
   CVolumeElementFEM *volElem  = DGGeometry->GetVolElem();
@@ -371,7 +371,7 @@ void CSurfaceFEMDataSorter::SortSurfaceConnectivity(CConfig *config, CGeometry *
 
     /*--- Create an object of the class CMeshFEM_DG and retrieve the necessary
           geometrical information for the FEM DG solver. ---*/
-    CMeshFEM_DG *DGGeometry = dynamic_cast<CMeshFEM_DG *>(geometry);
+    auto *DGGeometry = dynamic_cast<CMeshFEM_DG *>(geometry);
 
     unsigned long nVolElemOwned = DGGeometry->GetNVolElemOwned();
     CVolumeElementFEM *volElem  = DGGeometry->GetVolElem();
diff --git a/SU2_CFD/src/output/filewriter/CSurfaceFVMDataSorter.cpp b/SU2_CFD/src/output/filewriter/CSurfaceFVMDataSorter.cpp
index 7031c11190e..29c9347880e 100644
--- a/SU2_CFD/src/output/filewriter/CSurfaceFVMDataSorter.cpp
+++ b/SU2_CFD/src/output/filewriter/CSurfaceFVMDataSorter.cpp
@@ -188,12 +188,12 @@ void CSurfaceFVMDataSorter::SortOutputData() {
 
   /*--- Allocate arrays for sending the global ID. ---*/
 
-  unsigned long *idSend = new unsigned long[nElem_Send[size]]();
+  auto *idSend = new unsigned long[nElem_Send[size]]();
 
   /*--- Create an index variable to keep track of our index
    positions as we load up the send buffer. ---*/
 
-  unsigned long *idIndex = new unsigned long[size]();
+  auto *idIndex = new unsigned long[size]();
   for (int ii=0; ii < size; ii++) idIndex[ii] = nElem_Send[ii];
 
   /*--- Now loop back through the local connectivities for the surface
@@ -304,7 +304,7 @@ void CSurfaceFVMDataSorter::SortOutputData() {
    we do not include our own rank in the communications. We will
    directly copy our own data later. ---*/
 
-  unsigned long *idRecv = new unsigned long[nElem_Recv[size]]();
+  auto *idRecv = new unsigned long[nElem_Recv[size]]();
 
 #ifdef HAVE_MPI
   /*--- We need double the number of messages to send both the conn.
@@ -454,8 +454,8 @@ void CSurfaceFVMDataSorter::SortOutputData() {
    create a new mapping using two arrays, which will need to be
    communicated. We use our mask again here.  ---*/
 
-  unsigned long *globalP = new unsigned long[nPoints]();
-  unsigned long *renumbP = new unsigned long[nPoints]();
+  auto *globalP = new unsigned long[nPoints]();
+  auto *renumbP = new unsigned long[nPoints]();
 
   count = 0;
   for (iPoint = 0; iPoint < volumeSorter->GetnPoints(); iPoint++) {
@@ -545,7 +545,7 @@ void CSurfaceFVMDataSorter::SortOutputData() {
   /*--- Create an index variable to keep track of our index
    position as we load up the send buffer. ---*/
 
-  unsigned long *index = new unsigned long[size]();
+  auto *index = new unsigned long[size]();
   for (int ii=0; ii < size; ii++) index[ii] = nElem_Send[ii];
 
   /*--- Loop back through and load up the buffers for the global IDs
@@ -1241,10 +1241,10 @@ void CSurfaceFVMDataSorter::SortSurfaceConnectivity(CConfig *config, CGeometry *
   /*--- Create an index variable to keep track of our index
    position as we load up the send buffer. ---*/
 
-  unsigned long *index = new unsigned long[size];
+  auto *index = new unsigned long[size];
   for (int ii=0; ii < size; ii++) index[ii] = NODES_PER_ELEMENT*nElem_Send[ii];
 
-  unsigned long *haloIndex = new unsigned long[size];
+  auto *haloIndex = new unsigned long[size];
   for (int ii=0; ii < size; ii++) haloIndex[ii] = nElem_Send[ii];
 
   /*--- Loop through our elements and load the elems and their
diff --git a/SU2_CFD/src/output/filewriter/CTecplotBinaryFileWriter.cpp b/SU2_CFD/src/output/filewriter/CTecplotBinaryFileWriter.cpp
index 38a5cc20ccc..539191ca1de 100644
--- a/SU2_CFD/src/output/filewriter/CTecplotBinaryFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CTecplotBinaryFileWriter.cpp
@@ -37,7 +37,7 @@ CTecplotBinaryFileWriter::CTecplotBinaryFileWriter(CParallelDataSorter *valDataS
                                                    unsigned long valTimeIter, su2double valTimeStep) :
   CFileWriter(valDataSorter, fileExt), timeIter(valTimeIter), timeStep(valTimeStep){}
 
-CTecplotBinaryFileWriter::~CTecplotBinaryFileWriter(){}
+CTecplotBinaryFileWriter::~CTecplotBinaryFileWriter()= default;
 
 void CTecplotBinaryFileWriter::WriteData(string val_filename){
 
@@ -81,9 +81,9 @@ void CTecplotBinaryFileWriter::WriteData(string val_filename){
   }
   tecplot_variable_names << fieldNames[fieldNames.size()-1];
 
-  void* file_handle = NULL;
+  void* file_handle = nullptr;
   int32_t err = tecFileWriterOpen(val_filename.c_str(), data_set_title.c_str(), tecplot_variable_names.str().c_str(),
-    FILEFORMAT_SZL, FILETYPE_FULL, (int32_t)FieldDataType_Double, NULL, &file_handle);
+    FILEFORMAT_SZL, FILETYPE_FULL, (int32_t)FieldDataType_Double, nullptr, &file_handle);
   if (err) cout << "Error opening Tecplot file '" << val_filename << "'" << endl;
 
 #ifdef HAVE_MPI
@@ -128,7 +128,7 @@ void CTecplotBinaryFileWriter::WriteData(string val_filename){
 
   int32_t zone;
   vector<int32_t> value_locations(fieldNames.size(), 1); /* Nodal variables. */
-  err = tecZoneCreateFE(file_handle, "Zone", zone_type, num_nodes, num_cells, NULL, NULL, &value_locations[0], NULL, 0, 0, 0, &zone);
+  err = tecZoneCreateFE(file_handle, "Zone", zone_type, num_nodes, num_cells, nullptr, nullptr, value_locations.data(), nullptr, 0, 0, 0, &zone);
   if (err) cout << rank << ": Error creating Tecplot zone." << endl;
   if (is_unsteady) {
     err = tecZoneSetUnsteadyOptions(file_handle, zone, solution_time, timeIter + 1);
@@ -154,7 +154,7 @@ void CTecplotBinaryFileWriter::WriteData(string val_filename){
     partition_owners.reserve(size);
     for (int32_t iRank = 0; iRank < size; ++iRank)
       partition_owners.push_back(iRank);
-    err = tecZoneMapPartitionsToMPIRanks(file_handle, zone, size, &partition_owners[0]);
+    err = tecZoneMapPartitionsToMPIRanks(file_handle, zone, size, partition_owners.data());
     if (err) cout << rank << ": Error assigning MPI ranks for Tecplot zone partitions." << endl;
 
     /* Gather a list of nodes we refer to but are not outputting. */
@@ -211,14 +211,14 @@ void CTecplotBinaryFileWriter::WriteData(string val_filename){
       neighbor_nodes[i] = static_cast<int64_t>(node_number);
     }
     err = tecFEPartitionCreate64(file_handle, zone, rank + 1, partition_num_nodes, partition_num_cells,
-      static_cast<int64_t>(num_halo_nodes), &halo_node_local_numbers[0], &neighbor_partitions[0], &neighbor_nodes[0], 0, NULL);
+      static_cast<int64_t>(num_halo_nodes), halo_node_local_numbers.data(), neighbor_partitions.data(), neighbor_nodes.data(), 0, nullptr);
     if (err) cout << rank << ": Error creating Tecplot zone partition." << endl;
 
     /* Gather halo node data. First, tell each rank how many nodes' worth of data we need from them. */
     for (size_t i = 0; i < num_halo_nodes; ++i)
       ++num_nodes_to_receive[neighbor_partitions[i] - 1];
     vector<int> num_nodes_to_send(size);
-    SU2_MPI::Alltoall(&num_nodes_to_receive[0], 1, MPI_INT, &num_nodes_to_send[0], 1, MPI_INT, SU2_MPI::GetComm());
+    SU2_MPI::Alltoall(num_nodes_to_receive.data(), 1, MPI_INT, num_nodes_to_send.data(), 1, MPI_INT, SU2_MPI::GetComm());
 
     /* Now send the global node numbers whose data we need,
        and receive the same from all other ranks.
@@ -239,8 +239,8 @@ void CTecplotBinaryFileWriter::WriteData(string val_filename){
        (sorted_halo_nodes) whose data we need to receive, and receiving
        lists of nodes whose data we need to send. */
     if (sorted_halo_nodes.empty()) sorted_halo_nodes.resize(1); /* Avoid crash. */
-    SU2_MPI::Alltoallv(&sorted_halo_nodes[0], &num_nodes_to_receive[0], &nodes_to_receive_displacements[0], MPI_UNSIGNED_LONG,
-                       &nodes_to_send[0],     &num_nodes_to_send[0],    &nodes_to_send_displacements[0],    MPI_UNSIGNED_LONG,
+    SU2_MPI::Alltoallv(sorted_halo_nodes.data(), num_nodes_to_receive.data(), nodes_to_receive_displacements.data(), MPI_UNSIGNED_LONG,
+                       nodes_to_send.data(),     num_nodes_to_send.data(),    nodes_to_send_displacements.data(),    MPI_UNSIGNED_LONG,
                        SU2_MPI::GetComm());
 
     /* Now actually send and receive the data */
@@ -262,8 +262,8 @@ void CTecplotBinaryFileWriter::WriteData(string val_filename){
           data_to_send[index++] =dataSorter->GetData(iVar,node_offset);
         }
     }
-    CBaseMPIWrapper::Alltoallv(&data_to_send[0],  &num_values_to_send[0],    &values_to_send_displacements[0],    MPI_DOUBLE,
-                       &halo_var_data[0], &num_values_to_receive[0], &values_to_receive_displacements[0], MPI_DOUBLE,
+    CBaseMPIWrapper::Alltoallv(data_to_send.data(),  num_values_to_send.data(),    values_to_send_displacements.data(),    MPI_DOUBLE,
+                       halo_var_data.data(), num_values_to_receive.data(), values_to_receive_displacements.data(), MPI_DOUBLE,
                        SU2_MPI::GetComm());
   }
   else {
@@ -279,7 +279,7 @@ void CTecplotBinaryFileWriter::WriteData(string val_filename){
     for (iVar = 0; err == 0 && iVar < fieldNames.size(); iVar++) {
       for(unsigned long i = 0; i < dataSorter->GetnPoints(); ++i)
         values_to_write[i] = dataSorter->GetData(iVar, i);
-      err = tecZoneVarWriteDoubleValues(file_handle, zone, iVar + 1, rank + 1, dataSorter->GetnPoints(), &values_to_write[0]);
+      err = tecZoneVarWriteDoubleValues(file_handle, zone, iVar + 1, rank + 1, dataSorter->GetnPoints(), values_to_write.data());
       if (err) cout << rank << ": Error outputting Tecplot variable values." << endl;
       for (int iRank = 0; err == 0 && iRank < size; ++iRank) {
         if (num_nodes_to_receive[iRank] > 0) {
@@ -294,7 +294,7 @@ void CTecplotBinaryFileWriter::WriteData(string val_filename){
       vector<passivedouble> var_data;
       unsigned long nPoint = dataSorter->GetnPoints();
       vector<unsigned long> num_points(size);
-      SU2_MPI::Gather(&nPoint, 1, MPI_UNSIGNED_LONG, &num_points[0], 1, MPI_UNSIGNED_LONG, MASTER_NODE, SU2_MPI::GetComm());
+      SU2_MPI::Gather(&nPoint, 1, MPI_UNSIGNED_LONG, num_points.data(), 1, MPI_UNSIGNED_LONG, MASTER_NODE, SU2_MPI::GetComm());
 
       for(int iRank = 0; iRank < size; ++iRank) {
         int64_t rank_num_points = num_points[iRank];
@@ -306,13 +306,13 @@ void CTecplotBinaryFileWriter::WriteData(string val_filename){
               values_to_write.resize(rank_num_points);
               for(unsigned long i = 0; i < (unsigned long)rank_num_points; ++i)
                 values_to_write[i] = dataSorter->GetData(iVar,i);
-              err = tecZoneVarWriteDoubleValues(file_handle, zone, iVar + 1, 0, rank_num_points, &values_to_write[0]);
+              err = tecZoneVarWriteDoubleValues(file_handle, zone, iVar + 1, 0, rank_num_points, values_to_write.data());
               if (err) cout << rank << ": Error outputting Tecplot variable values." << endl;
             }
           }
           else { /* Receive data from other rank. */
             var_data.resize(max((int64_t)1, (int64_t)fieldNames.size() * rank_num_points));
-            CBaseMPIWrapper::Recv(&var_data[0], fieldNames.size() * rank_num_points, MPI_DOUBLE, iRank, iRank, SU2_MPI::GetComm(), MPI_STATUS_IGNORE);
+            CBaseMPIWrapper::Recv(var_data.data(), fieldNames.size() * rank_num_points, MPI_DOUBLE, iRank, iRank, SU2_MPI::GetComm(), MPI_STATUS_IGNORE);
             for (iVar = 0; err == 0 && iVar < fieldNames.size(); iVar++) {
               err = tecZoneVarWriteDoubleValues(file_handle, zone, iVar + 1, 0, rank_num_points, &var_data[iVar * rank_num_points]);
               if (err) cout << rank << ": Error outputting Tecplot surface variable values." << endl;
@@ -324,7 +324,7 @@ void CTecplotBinaryFileWriter::WriteData(string val_filename){
     else { /* Send data to MASTER_NODE */
       unsigned long nPoint = dataSorter->GetnPoints();
 
-      SU2_MPI::Gather(&nPoint, 1, MPI_UNSIGNED_LONG, NULL, 1, MPI_UNSIGNED_LONG, MASTER_NODE, SU2_MPI::GetComm());
+      SU2_MPI::Gather(&nPoint, 1, MPI_UNSIGNED_LONG, nullptr, 1, MPI_UNSIGNED_LONG, MASTER_NODE, SU2_MPI::GetComm());
 
       vector<passivedouble> var_data;
       size_t var_data_size = fieldNames.size() * dataSorter->GetnPoints();
@@ -333,8 +333,8 @@ void CTecplotBinaryFileWriter::WriteData(string val_filename){
           for(unsigned long i = 0; i < dataSorter->GetnPoints(); ++i)
             var_data.push_back(dataSorter->GetData(iVar,i));
 
-      if (var_data.size() > 0)
-        CBaseMPIWrapper::Send(&var_data[0], static_cast<int>(var_data.size()), MPI_DOUBLE, MASTER_NODE, rank, SU2_MPI::GetComm());
+      if (!var_data.empty())
+        CBaseMPIWrapper::Send(var_data.data(), static_cast<int>(var_data.size()), MPI_DOUBLE, MASTER_NODE, rank, SU2_MPI::GetComm());
     }
   }
 
@@ -435,7 +435,7 @@ void CTecplotBinaryFileWriter::WriteData(string val_filename){
 
       vector<unsigned long> connectivity_sizes(size);
       unsigned long unused = 0;
-      SU2_MPI::Gather(&unused, 1, MPI_UNSIGNED_LONG, &connectivity_sizes[0], 1, MPI_UNSIGNED_LONG, MASTER_NODE, SU2_MPI::GetComm());
+      SU2_MPI::Gather(&unused, 1, MPI_UNSIGNED_LONG, connectivity_sizes.data(), 1, MPI_UNSIGNED_LONG, MASTER_NODE, SU2_MPI::GetComm());
       vector<int64_t> connectivity;
       for(int iRank = 0; iRank < size; ++iRank) {
         if (iRank == rank) {
@@ -466,8 +466,8 @@ void CTecplotBinaryFileWriter::WriteData(string val_filename){
 
         } else { /* Receive node map and write out. */
           connectivity.resize(max((unsigned long)1, connectivity_sizes[iRank]));
-          SU2_MPI::Recv(&connectivity[0], connectivity_sizes[iRank], MPI_UNSIGNED_LONG, iRank, iRank, SU2_MPI::GetComm(), MPI_STATUS_IGNORE);
-          err = tecZoneNodeMapWrite64(file_handle, zone, 0, 1, connectivity_sizes[iRank], &connectivity[0]);
+          SU2_MPI::Recv(connectivity.data(), connectivity_sizes[iRank], MPI_UNSIGNED_LONG, iRank, iRank, SU2_MPI::GetComm(), MPI_STATUS_IGNORE);
+          err = tecZoneNodeMapWrite64(file_handle, zone, 0, 1, connectivity_sizes[iRank], connectivity.data());
           if (err) cout << rank << ": Error outputting Tecplot node values." << endl;
         }
       }
@@ -477,7 +477,7 @@ void CTecplotBinaryFileWriter::WriteData(string val_filename){
 
       unsigned long connectivity_size;
       connectivity_size = 2 * nParallel_Line + 4 * (nParallel_Tria + nParallel_Quad);
-      SU2_MPI::Gather(&connectivity_size, 1, MPI_UNSIGNED_LONG, NULL, 1, MPI_UNSIGNED_LONG, MASTER_NODE, SU2_MPI::GetComm());
+      SU2_MPI::Gather(&connectivity_size, 1, MPI_UNSIGNED_LONG, nullptr, 1, MPI_UNSIGNED_LONG, MASTER_NODE, SU2_MPI::GetComm());
       vector<int64_t> connectivity;
       connectivity.reserve(connectivity_size);
       for (iElem = 0; err == 0 && iElem < nParallel_Line; iElem++) {
@@ -500,7 +500,7 @@ void CTecplotBinaryFileWriter::WriteData(string val_filename){
       }
 
       if (connectivity.empty()) connectivity.resize(1); /* Avoid crash */
-      SU2_MPI::Send(&connectivity[0], connectivity_size, MPI_UNSIGNED_LONG, MASTER_NODE, rank, SU2_MPI::GetComm());
+      SU2_MPI::Send(connectivity.data(), connectivity_size, MPI_UNSIGNED_LONG, MASTER_NODE, rank, SU2_MPI::GetComm());
     }
   }
 #else
@@ -602,7 +602,7 @@ void CTecplotBinaryFileWriter::WriteData(string val_filename){
 
 int64_t CTecplotBinaryFileWriter::GetHaloNodeNumber(unsigned long global_node_number, unsigned long last_local_node, vector<unsigned long> const &halo_node_list)
 {
-  vector<unsigned long>::const_iterator it = lower_bound(halo_node_list.begin(), halo_node_list.end(), global_node_number);
+  auto it = lower_bound(halo_node_list.begin(), halo_node_list.end(), global_node_number);
   assert(it != halo_node_list.end());
   assert(*it == global_node_number);
   /* When C++11 is universally available, replace the following mouthful with "auto" */
diff --git a/SU2_CFD/src/output/filewriter/CTecplotFileWriter.cpp b/SU2_CFD/src/output/filewriter/CTecplotFileWriter.cpp
index 5ecf07ad5de..5b04ebd5c15 100644
--- a/SU2_CFD/src/output/filewriter/CTecplotFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CTecplotFileWriter.cpp
@@ -33,7 +33,7 @@ CTecplotFileWriter::CTecplotFileWriter(CParallelDataSorter *valDataSorter,
                                        unsigned long valTimeIter, su2double valTimeStep) :
   CFileWriter(valDataSorter, fileExt), timeIter(valTimeIter), timeStep(valTimeStep){}
 
-CTecplotFileWriter::~CTecplotFileWriter(){}
+CTecplotFileWriter::~CTecplotFileWriter()= default;
 
 void CTecplotFileWriter::WriteData(string val_filename){
 
diff --git a/SU2_CFD/src/output/output_structure_legacy.cpp b/SU2_CFD/src/output/output_structure_legacy.cpp
index 40e495d6b66..a41081f403e 100644
--- a/SU2_CFD/src/output/output_structure_legacy.cpp
+++ b/SU2_CFD/src/output/output_structure_legacy.cpp
@@ -219,7 +219,7 @@ COutputLegacy::COutputLegacy(CConfig *config) {
   }
 }
 
-COutputLegacy::~COutputLegacy(void) {
+COutputLegacy::~COutputLegacy() {
   /* delete pointers initialized at construction*/
   /* Coords and Conn_*(Connectivity) have their own dealloc functions */
   /* Data is taken care of in DeallocateSolution function */
@@ -405,25 +405,25 @@ void COutputLegacy::SetConvHistoryHeader(ofstream *ConvHist_file, CConfig *confi
 
   /*--- Header for the coefficients ---*/
 
-  char flow_coeff[]= ",\"CL\",\"CD\",\"CSF\",\"CMx\",\"CMy\",\"CMz\",\"CFx\",\"CFy\",\"CFz\",\"CL/CD\",\"AoA\",\"Custom_ObjFunc\"";
-  char heat_coeff[]= ",\"HeatFlux_Total\",\"HeatFlux_Maximum\",\"Temperature_Total\"";
-  char equivalent_area_coeff[]= ",\"CEquivArea\",\"CNearFieldOF\"";
+  char flow_coeff[]= R"(,"CL","CD","CSF","CMx","CMy","CMz","CFx","CFy","CFz","CL/CD","AoA","Custom_ObjFunc")";
+  char heat_coeff[]= R"(,"HeatFlux_Total","HeatFlux_Maximum","Temperature_Total")";
+  char equivalent_area_coeff[]= R"(,"CEquivArea","CNearFieldOF")";
   char buffet_coeff[]= ",\"Buffet_Metric\"";
-  char engine_coeff[]= ",\"NetThrust\",\"Power\",\"AeroCDrag\",\"SolidCDrag\",\"Radial_Distortion\",\"Circumferential_Distortion\"";
-  char rotating_frame_coeff[]= ",\"CMerit\",\"CT\",\"CQ\"";
-  char fem_coeff[]= ",\"VM_Stress\",\"Force_Coeff\"";
+  char engine_coeff[]= R"(,"NetThrust","Power","AeroCDrag","SolidCDrag","Radial_Distortion","Circumferential_Distortion")";
+  char rotating_frame_coeff[]= R"(,"CMerit","CT","CQ")";
+  char fem_coeff[]= R"(,"VM_Stress","Force_Coeff")";
   char fem_incload[]= ",\"IncLoad\"";
-  char adj_coeff[]= ",\"Sens_Geo\",\"Sens_Mach\",\"Sens_AoA\",\"Sens_Press\",\"Sens_Temp\",\"Sens_AoS\"";
-  char adj_inc_coeff[]=",\"Sens_Geo\",\"Sens_Vin\",\"Sens_Pout\",\"Sens_Temp\"";
-  char adj_turbo_coeff[]=",\"Sens_Geo\",\"Sens_PressOut\",\"Sens_TotTempIn\"";
-  char surface_outputs[]= ",\"Avg_MassFlow\",\"Avg_Mach\",\"Avg_Temp\",\"Avg_Press\",\"Avg_Density\",\"Avg_Enthalpy\",\"Avg_NormalVel\",\"Uniformity\",\"Secondary_Strength\",\"Momentum_Distortion\",\"Secondary_Over_Uniformity\",\"Avg_TotalTemp\",\"Avg_TotalPress\",\"Pressure_Drop\"";
+  char adj_coeff[]= R"(,"Sens_Geo","Sens_Mach","Sens_AoA","Sens_Press","Sens_Temp","Sens_AoS")";
+  char adj_inc_coeff[]=R"(,"Sens_Geo","Sens_Vin","Sens_Pout","Sens_Temp")";
+  char adj_turbo_coeff[]=R"(,"Sens_Geo","Sens_PressOut","Sens_TotTempIn")";
+  char surface_outputs[]= R"(,"Avg_MassFlow","Avg_Mach","Avg_Temp","Avg_Press","Avg_Density","Avg_Enthalpy","Avg_NormalVel","Uniformity","Secondary_Strength","Momentum_Distortion","Secondary_Over_Uniformity","Avg_TotalTemp","Avg_TotalPress","Pressure_Drop")";
   char Cp_inverse_design[]= ",\"Cp_Diff\"";
   char Heat_inverse_design[]= ",\"HeatFlux_Diff\"";
-  char d_flow_coeff[] = ",\"D(CL)\",\"D(CD)\",\"D(CSF)\",\"D(CMx)\",\"D(CMy)\",\"D(CMz)\",\"D(CFx)\",\"D(CFy)\",\"D(CFz)\",\"D(CL/CD)\",\"D(Custom_ObjFunc)\"";
+  char d_flow_coeff[] = R"lit(,"D(CL)","D(CD)","D(CSF)","D(CMx)","D(CMy)","D(CMz)","D(CFx)","D(CFy)","D(CFz)","D(CL/CD)","D(Custom_ObjFunc)")lit";
   char d_thermal_coeff[] = ",\"D(HeatFlux_Total)\",\"D(HeatFlux_Maximum)\"";
-  char d_engine[] = ",\"D(NetThrust)\",\"D(Power)\",\"D(AeroCDrag)\",\"D(SolidCDrag)\",\"D(Radial_Distortion)\",\"D(Circumferential_Distortion)\"";
-  char d_turbo_coeff[] = ",\"D(TotalPressureLoss_0)\",\"D(FlowAngleOut_0)\",\"D(TotalEfficency)\",\"D(TotalStaticEfficiency)\", \"D(EntropyGen)\"";
-  char d_surface_outputs[]= ",\"D(Uniformity)\",\"D(Secondary_Strength)\",\"D(Momentum_Distortion)\",\"D(Secondary_Over_Uniformity)\",\"D(Pressure_Drop)\"";
+  char d_engine[] = R"lit(,"D(NetThrust)","D(Power)","D(AeroCDrag)","D(SolidCDrag)","D(Radial_Distortion)","D(Circumferential_Distortion)")lit";
+  char d_turbo_coeff[] = R"lit(,"D(TotalPressureLoss_0)","D(FlowAngleOut_0)","D(TotalEfficency)","D(TotalStaticEfficiency)", "D(EntropyGen)")lit";
+  char d_surface_outputs[]= R"lit(,"D(Uniformity)","D(Secondary_Strength)","D(Momentum_Distortion)","D(Secondary_Over_Uniformity)","D(Pressure_Drop)")lit";
 
   /*--- Find the markers being monitored and create a header for them ---*/
 
@@ -474,14 +474,14 @@ void COutputLegacy::SetConvHistoryHeader(ofstream *ConvHist_file, CConfig *confi
 
   /*--- Header for the residuals ---*/
 
-  char flow_resid[]= ",\"Res_Flow[0]\",\"Res_Flow[1]\",\"Res_Flow[2]\",\"Res_Flow[3]\",\"Res_Flow[4]\"";
-  char adj_flow_resid[]= ",\"Res_AdjFlow[0]\",\"Res_AdjFlow[1]\",\"Res_AdjFlow[2]\",\"Res_AdjFlow[3]\",\"Res_AdjFlow[4]\"";
+  char flow_resid[]= R"(,"Res_Flow[0]","Res_Flow[1]","Res_Flow[2]","Res_Flow[3]","Res_Flow[4]")";
+  char adj_flow_resid[]= R"(,"Res_AdjFlow[0]","Res_AdjFlow[1]","Res_AdjFlow[2]","Res_AdjFlow[3]","Res_AdjFlow[4]")";
   switch (config->GetKind_Turb_Model()) {
     case TURB_MODEL::SA:
       SPRINTF (turb_resid, ",\"Res_Turb[0]\"");
       break;
     case TURB_MODEL::SST:
-      SPRINTF (turb_resid, ",\"Res_Turb[0]\",\"Res_Turb[1]\"");
+      SPRINTF (turb_resid, R"(,"Res_Turb[0]","Res_Turb[1]")");
       break;
     default: break;
   }
@@ -490,11 +490,11 @@ void COutputLegacy::SetConvHistoryHeader(ofstream *ConvHist_file, CConfig *confi
       SPRINTF (adj_turb_resid, ",\"Res_AdjTurb[0]\"");
       break;
     case TURB_MODEL::SST:
-      SPRINTF (adj_turb_resid, ",\"Res_AdjTurb[0]\",\"Res_AdjTurb[1]\"");
+      SPRINTF (adj_turb_resid, R"(,"Res_AdjTurb[0]","Res_AdjTurb[1]")");
       break;
     default: break;
   }
-  char fem_resid[]= ",\"Res_FEM[0]\",\"Res_FEM[1]\",\"Res_FEM[2]\"";
+  char fem_resid[]= R"(,"Res_FEM[0]","Res_FEM[1]","Res_FEM[2]")";
   char heat_resid[]= ",\"Res_Heat\"";
   char rad_resid[]= ",\"Res_P1-rad\"";
 
@@ -1563,8 +1563,8 @@ void COutputLegacy::SetConvHistoryBody(ofstream *ConvHist_file,
       }
       if ((val_iZone == 0 && val_iInst == 0)|| fluid_structure){
         /*--- Write the screen header---*/
-        if (  (!fem && ((write_heads) && !(!DualTime_Iteration && Unsteady))) ||
-            (fem && ((write_heads_FEM) && !(!DualTime_Iteration && nonlinear_analysis)))
+        if (  (!fem && ((write_heads) && (DualTime_Iteration || !Unsteady))) ||
+            (fem && ((write_heads_FEM) && (DualTime_Iteration || !nonlinear_analysis)))
         ) {
 
           if (!fem) {
@@ -4400,7 +4400,7 @@ void COutputLegacy::SpecialOutputSpanLoad(CSolver *solver, CGeometry *geometry,
                                        CPressure, Xcoord_Airfoil, Ycoord_Airfoil, Zcoord_Airfoil,
                                        CPressure_Airfoil, true, config);
 
-      if ((rank == MASTER_NODE) && (Xcoord_Airfoil.size() == 0)) {
+      if ((rank == MASTER_NODE) && (Xcoord_Airfoil.empty())) {
         if ((config->GetGeo_Description() == FUSELAGE) || (config->GetGeo_Description() == WING))
           cout << endl << "Please check the config file, the section (" << Plane_P0[0] <<", " << Plane_P0[1] <<", " << Plane_P0[2] << ") has not been detected." << endl;
         if (config->GetGeo_Description() == NACELLE)
@@ -4485,7 +4485,7 @@ void COutputLegacy::SpecialOutputSpanLoad(CSolver *solver, CGeometry *geometry,
 
       /*--- Output the pressure on each section (tecplot format) ---*/
 
-      if ((rank == MASTER_NODE) && (Xcoord_Airfoil.size() != 0)) {
+      if ((rank == MASTER_NODE) && (!Xcoord_Airfoil.empty())) {
 
         /*--- Find leading and trailing edge ---*/
 
@@ -4535,7 +4535,7 @@ void COutputLegacy::SpecialOutputSpanLoad(CSolver *solver, CGeometry *geometry,
           if (iSection == 0) {
             Cp_File.open("cp_sections.dat", ios::out);
             Cp_File << "TITLE = \"Airfoil sections\"" << endl;
-            Cp_File << "VARIABLES = \"x/c\",\"C<sub>p</sub>\",\"x\",\"y\",\"z\",\"y/c\",\"z/c\"" << endl;
+            Cp_File << R"(VARIABLES = "x/c","C<sub>p</sub>","x","y","z","y/c","z/c")" << endl;
           } else
             Cp_File.open("cp_sections.dat", ios::app);
 
@@ -4652,12 +4652,12 @@ void COutputLegacy::SpecialOutputSpanLoad(CSolver *solver, CGeometry *geometry,
 
             if ((config->GetTabular_FileFormat() == TAB_OUTPUT::TAB_CSV)) {
               Load_File.open("load_distribution.csv", ios::out);
-              Load_File << "\"Percent Semispan\",\"Sectional C_L\",\"Spanload (c C_L / c_ref) \",\"Elliptic Spanload\"" << endl;
+              Load_File << R"("Percent Semispan","Sectional C_L","Spanload (c C_L / c_ref) ","Elliptic Spanload")" << endl;
             }
             else {
               Load_File.open("load_distribution.dat", ios::out);
               Load_File << "TITLE = \"Load distribution\"" << endl;
-              Load_File << "VARIABLES = \"Percent Semispan\",\"Sectional C<sub>L</sub>\",\"Spanload (c C<sub>L</sub> / c<sub>ref</sub>) \",\"Elliptic Spanload\"" << endl;
+              Load_File << R"(VARIABLES = "Percent Semispan","Sectional C<sub>L</sub>","Spanload (c C<sub>L</sub> / c<sub>ref</sub>) ","Elliptic Spanload")" << endl;
               Load_File << "ZONE T=\"Wing load distribution\"" << endl;
             }
           } else {
@@ -4778,7 +4778,7 @@ void COutputLegacy::SetCpInverseDesign(CSolver *solver_container, CGeometry *geo
 
     while (getline(Surface_file, text_line)) {
       for (icommas = 0; icommas < 50; icommas++) {
-        position = text_line.find( ",", 0 );
+        position = text_line.find( ',', 0 );
         if (position!=string::npos) text_line.erase (position,1);
       }
       stringstream  point_line(text_line);
@@ -4929,7 +4929,7 @@ void COutputLegacy::SetHeatFluxInverseDesign(CSolver *solver_container, CGeometr
 
     while (getline(Surface_file, text_line)) {
       for (icommas = 0; icommas < 50; icommas++) {
-        position = text_line.find( ",", 0 );
+        position = text_line.find( ',', 0 );
         if (position!=string::npos) text_line.erase (position,1);
       }
       stringstream  point_line(text_line);
@@ -5053,7 +5053,7 @@ void COutputLegacy::SpecialOutputDistortion(CSolver *solver, CGeometry *geometry
     }
     else {
       SurfFlow_file <<"TITLE = \"Surface Analysis\"" <<endl;
-      SurfFlow_file <<"VARIABLES = \"y(in)\", \"z(in)\", \"PT/PT<sub>inf</sub>\", \"TT/TT<sub>inf</sub>\", \"P/P<sub>inf</sub>\", \"T/T<sub>inf</sub>\", \"v<sub>x</sub>/v<sub>inf</sub>\", \"v<sub>y</sub>/v<sub>inf</sub>\", \"v<sub>z</sub>/v<sub>inf</sub>\", \"<greek>a</greek> (deg)\", \"<greek>b</greek> (deg)\", \"Mach\", \"Filtered <greek>a</greek> (deg)\", \"Filtered <greek>b</greek> (deg)\", \"Filtered Mach\"" << endl;
+      SurfFlow_file <<R"lit(VARIABLES = "y(in)", "z(in)", "PT/PT<sub>inf</sub>", "TT/TT<sub>inf</sub>", "P/P<sub>inf</sub>", "T/T<sub>inf</sub>", "v<sub>x</sub>/v<sub>inf</sub>", "v<sub>y</sub>/v<sub>inf</sub>", "v<sub>z</sub>/v<sub>inf</sub>", "<greek>a</greek> (deg)", "<greek>b</greek> (deg)", "Mach", "Filtered <greek>a</greek> (deg)", "Filtered <greek>b</greek> (deg)", "Filtered Mach")lit" << endl;
     }
 
   }
@@ -6374,7 +6374,7 @@ void COutputLegacy::SpecialOutputTurbo(CSolver *****solver, CGeometry ****geomet
     spanwise_performance_filename = "TURBOMACHINERY/inflow_spanwise_thermodynamic_values.dat";
     char buffer[50];
     if (nZone > 1){
-      unsigned short lastindex      =  spanwise_performance_filename.find_last_of(".");
+      unsigned short lastindex      =  spanwise_performance_filename.find_last_of('.');
       spanwise_performance_filename =  spanwise_performance_filename.substr(0, lastindex);
       SPRINTF (buffer, "_%d.dat", SU2_TYPE::Int(val_iZone));
       spanwise_performance_filename.append(string(buffer));
@@ -6430,7 +6430,7 @@ void COutputLegacy::SpecialOutputTurbo(CSolver *****solver, CGeometry ****geomet
     /*--- Writing Span wise outflow thermodynamic quantities. ---*/
     spanwise_performance_filename = "TURBOMACHINERY/outflow_spanwise_thermodynamic_values.dat";
     if (nZone > 1){
-      unsigned short lastindex      =  spanwise_performance_filename.find_last_of(".");
+      unsigned short lastindex      =  spanwise_performance_filename.find_last_of('.');
       spanwise_performance_filename =  spanwise_performance_filename.substr(0, lastindex);
       SPRINTF (buffer, "_%d.dat", SU2_TYPE::Int(val_iZone));
       spanwise_performance_filename.append(string(buffer));
@@ -6486,7 +6486,7 @@ void COutputLegacy::SpecialOutputTurbo(CSolver *****solver, CGeometry ****geomet
     /*--- Writing Span wise inflow kinematic quantities. ---*/
     spanwise_performance_filename = "TURBOMACHINERY/inflow_spanwise_kinematic_values.dat";
     if (nZone > 1){
-      unsigned short lastindex      =  spanwise_performance_filename.find_last_of(".");
+      unsigned short lastindex      =  spanwise_performance_filename.find_last_of('.');
       spanwise_performance_filename =  spanwise_performance_filename.substr(0, lastindex);
       SPRINTF (buffer, "_%d.dat", SU2_TYPE::Int(val_iZone));
       spanwise_performance_filename.append(string(buffer));
@@ -6544,7 +6544,7 @@ void COutputLegacy::SpecialOutputTurbo(CSolver *****solver, CGeometry ****geomet
     /*--- Writing Span wise outflow thermodynamic quantities. ---*/
     spanwise_performance_filename = "TURBOMACHINERY/outflow_spanwise_kinematic_values.dat";
     if (nZone > 1){
-      unsigned short lastindex      =  spanwise_performance_filename.find_last_of(".");
+      unsigned short lastindex      =  spanwise_performance_filename.find_last_of('.');
       spanwise_performance_filename =  spanwise_performance_filename.substr(0, lastindex);
       SPRINTF (buffer, "_%d.dat", SU2_TYPE::Int(val_iZone));
       spanwise_performance_filename.append(string(buffer));
@@ -6619,7 +6619,7 @@ void COutputLegacy::SpecialOutputHarmonicBalance(CSolver *****solver, CGeometry
   /*--- Allocate memory for send buffer ---*/
   sbuf_var = new su2double[nVar_output];
 
-  su2double *averages = new su2double[nVar_output];
+  auto *averages = new su2double[nVar_output];
   for (iVar = 0; iVar < nVar_output; iVar++)
     averages[iVar] = 0;
 
@@ -6629,13 +6629,13 @@ void COutputLegacy::SpecialOutputHarmonicBalance(CSolver *****solver, CGeometry
 
     HB_output_file.precision(15);
     HB_output_file.open("HB_output.csv", ios::out);
-    HB_output_file <<  "\"time_instance\",\"CL\",\"CD\",\"CMx\",\"CMy\",\"CMz\"" << endl;
+    HB_output_file <<  R"("time_instance","CL","CD","CMx","CMy","CMz")" << endl;
 
     mean_HB_file.precision(15);
     if (current_iter == 0 && iInst == 1) {
       mean_HB_file.open("history_HB.plt", ios::trunc);
       mean_HB_file << "TITLE = \"SU2 HARMONIC BALANCE SIMULATION\"" << endl;
-      mean_HB_file <<  "VARIABLES = \"Iteration\",\"CL\",\"CD\",\"CMx\",\"CMy\",\"CMz\",\"CT\",\"CQ\",\"CMerit\"" << endl;
+      mean_HB_file <<  R"(VARIABLES = "Iteration","CL","CD","CMx","CMy","CMz","CT","CQ","CMerit")" << endl;
       mean_HB_file << "ZONE T= \"Average Convergence History\"" << endl;
     }
     else
@@ -6697,7 +6697,7 @@ void COutputLegacy::SetSpecialOutput(CSolver *****solver_container,
                                        CGeometry ****geometry,
                                        CConfig **config,
                                        unsigned long iExtIter,
-                                       unsigned short val_nZone) {
+                                       unsigned short val_nZone) const {
 
   bool special_output = false;
   unsigned short iZone;
@@ -6736,21 +6736,21 @@ void COutputLegacy::SpecialOutputAnalyzeSurface(CSolver *solver, CGeometry *geom
   bool axisymmetric               = config->GetAxisymmetric();
   unsigned short nMarker_Analyze  = config->GetnMarker_Analyze();
 
-  su2double  *Vector                    = new su2double[nDim];
-  su2double  *Surface_MassFlow          = new su2double[nMarker];
-  su2double  *Surface_Mach              = new su2double[nMarker];
-  su2double  *Surface_Temperature       = new su2double[nMarker];
-  su2double  *Surface_Density           = new su2double[nMarker];
-  su2double  *Surface_Enthalpy          = new su2double[nMarker];
-  su2double  *Surface_NormalVelocity    = new su2double[nMarker];
-  su2double  *Surface_StreamVelocity2   = new su2double[nMarker];
-  su2double  *Surface_TransvVelocity2   = new su2double[nMarker];
-  su2double  *Surface_Pressure          = new su2double[nMarker];
-  su2double  *Surface_TotalTemperature  = new su2double[nMarker];
-  su2double  *Surface_TotalPressure     = new su2double[nMarker];
-  su2double  *Surface_VelocityIdeal     = new su2double[nMarker];
-  su2double  *Surface_Area              = new su2double[nMarker];
-  su2double  *Surface_MassFlow_Abs      = new su2double[nMarker];
+  auto  *Vector                    = new su2double[nDim];
+  auto  *Surface_MassFlow          = new su2double[nMarker];
+  auto  *Surface_Mach              = new su2double[nMarker];
+  auto  *Surface_Temperature       = new su2double[nMarker];
+  auto  *Surface_Density           = new su2double[nMarker];
+  auto  *Surface_Enthalpy          = new su2double[nMarker];
+  auto  *Surface_NormalVelocity    = new su2double[nMarker];
+  auto  *Surface_StreamVelocity2   = new su2double[nMarker];
+  auto  *Surface_TransvVelocity2   = new su2double[nMarker];
+  auto  *Surface_Pressure          = new su2double[nMarker];
+  auto  *Surface_TotalTemperature  = new su2double[nMarker];
+  auto  *Surface_TotalPressure     = new su2double[nMarker];
+  auto  *Surface_VelocityIdeal     = new su2double[nMarker];
+  auto  *Surface_Area              = new su2double[nMarker];
+  auto  *Surface_MassFlow_Abs      = new su2double[nMarker];
 
   /*--- Compute the numerical fan face Mach number, and the total area of the inflow ---*/
 
@@ -6867,35 +6867,35 @@ void COutputLegacy::SpecialOutputAnalyzeSurface(CSolver *solver, CGeometry *geom
 
   /*--- Copy to the appropriate structure ---*/
 
-  su2double *Surface_MassFlow_Local          = new su2double [nMarker_Analyze];
-  su2double *Surface_Mach_Local              = new su2double [nMarker_Analyze];
-  su2double *Surface_Temperature_Local       = new su2double [nMarker_Analyze];
-  su2double *Surface_Density_Local           = new su2double [nMarker_Analyze];
-  su2double *Surface_Enthalpy_Local          = new su2double [nMarker_Analyze];
-  su2double *Surface_NormalVelocity_Local    = new su2double [nMarker_Analyze];
-  su2double *Surface_StreamVelocity2_Local   = new su2double [nMarker_Analyze];
-  su2double *Surface_TransvVelocity2_Local   = new su2double [nMarker_Analyze];
-  su2double *Surface_Pressure_Local          = new su2double [nMarker_Analyze];
-  su2double *Surface_TotalTemperature_Local  = new su2double [nMarker_Analyze];
-  su2double *Surface_TotalPressure_Local     = new su2double [nMarker_Analyze];
-  su2double *Surface_Area_Local              = new su2double [nMarker_Analyze];
-  su2double *Surface_MassFlow_Abs_Local      = new su2double [nMarker_Analyze];
-
-  su2double *Surface_MassFlow_Total          = new su2double [nMarker_Analyze];
-  su2double *Surface_Mach_Total              = new su2double [nMarker_Analyze];
-  su2double *Surface_Temperature_Total       = new su2double [nMarker_Analyze];
-  su2double *Surface_Density_Total           = new su2double [nMarker_Analyze];
-  su2double *Surface_Enthalpy_Total          = new su2double [nMarker_Analyze];
-  su2double *Surface_NormalVelocity_Total    = new su2double [nMarker_Analyze];
-  su2double *Surface_StreamVelocity2_Total   = new su2double [nMarker_Analyze];
-  su2double *Surface_TransvVelocity2_Total   = new su2double [nMarker_Analyze];
-  su2double *Surface_Pressure_Total          = new su2double [nMarker_Analyze];
-  su2double *Surface_TotalTemperature_Total  = new su2double [nMarker_Analyze];
-  su2double *Surface_TotalPressure_Total     = new su2double [nMarker_Analyze];
-  su2double *Surface_Area_Total              = new su2double [nMarker_Analyze];
-  su2double *Surface_MassFlow_Abs_Total      = new su2double [nMarker_Analyze];
-
-  su2double *Surface_MomentumDistortion_Total = new su2double [nMarker_Analyze];
+  auto *Surface_MassFlow_Local          = new su2double [nMarker_Analyze];
+  auto *Surface_Mach_Local              = new su2double [nMarker_Analyze];
+  auto *Surface_Temperature_Local       = new su2double [nMarker_Analyze];
+  auto *Surface_Density_Local           = new su2double [nMarker_Analyze];
+  auto *Surface_Enthalpy_Local          = new su2double [nMarker_Analyze];
+  auto *Surface_NormalVelocity_Local    = new su2double [nMarker_Analyze];
+  auto *Surface_StreamVelocity2_Local   = new su2double [nMarker_Analyze];
+  auto *Surface_TransvVelocity2_Local   = new su2double [nMarker_Analyze];
+  auto *Surface_Pressure_Local          = new su2double [nMarker_Analyze];
+  auto *Surface_TotalTemperature_Local  = new su2double [nMarker_Analyze];
+  auto *Surface_TotalPressure_Local     = new su2double [nMarker_Analyze];
+  auto *Surface_Area_Local              = new su2double [nMarker_Analyze];
+  auto *Surface_MassFlow_Abs_Local      = new su2double [nMarker_Analyze];
+
+  auto *Surface_MassFlow_Total          = new su2double [nMarker_Analyze];
+  auto *Surface_Mach_Total              = new su2double [nMarker_Analyze];
+  auto *Surface_Temperature_Total       = new su2double [nMarker_Analyze];
+  auto *Surface_Density_Total           = new su2double [nMarker_Analyze];
+  auto *Surface_Enthalpy_Total          = new su2double [nMarker_Analyze];
+  auto *Surface_NormalVelocity_Total    = new su2double [nMarker_Analyze];
+  auto *Surface_StreamVelocity2_Total   = new su2double [nMarker_Analyze];
+  auto *Surface_TransvVelocity2_Total   = new su2double [nMarker_Analyze];
+  auto *Surface_Pressure_Total          = new su2double [nMarker_Analyze];
+  auto *Surface_TotalTemperature_Total  = new su2double [nMarker_Analyze];
+  auto *Surface_TotalPressure_Total     = new su2double [nMarker_Analyze];
+  auto *Surface_Area_Total              = new su2double [nMarker_Analyze];
+  auto *Surface_MassFlow_Abs_Total      = new su2double [nMarker_Analyze];
+
+  auto *Surface_MomentumDistortion_Total = new su2double [nMarker_Analyze];
 
   for (iMarker_Analyze = 0; iMarker_Analyze < nMarker_Analyze; iMarker_Analyze++) {
     Surface_MassFlow_Local[iMarker_Analyze]          = 0.0;
diff --git a/SU2_CFD/src/output/tools/CWindowingTools.cpp b/SU2_CFD/src/output/tools/CWindowingTools.cpp
index b14190b897c..98626abfcbb 100644
--- a/SU2_CFD/src/output/tools/CWindowingTools.cpp
+++ b/SU2_CFD/src/output/tools/CWindowingTools.cpp
@@ -40,17 +40,17 @@ su2double CWindowingTools::GetWndWeight(WINDOW_FUNCTION windowId, unsigned long
 }
 
 su2double CWindowingTools::HannWindow(unsigned long curTimeIter, unsigned long endTimeIter) {
-  su2double currTimeDouble = static_cast<su2double>(curTimeIter);
+  auto currTimeDouble = static_cast<su2double>(curTimeIter);
   if(endTimeIter==0) return 0; //Catch div by zero error, if window length is zero
-  su2double endTimeDouble = static_cast<su2double>(endTimeIter);
+  auto endTimeDouble = static_cast<su2double>(endTimeIter);
   su2double tau = currTimeDouble/endTimeDouble;
   return 1.0-cos(2*PI_NUMBER*tau);
 }
 
 su2double CWindowingTools::HannSquaredWindow(unsigned long curTimeIter, unsigned long endTimeIter) {
-  su2double currTimeDouble = static_cast<su2double>(curTimeIter);
+  auto currTimeDouble = static_cast<su2double>(curTimeIter);
   if(endTimeIter==0) return 0; //Catch div by zero error, if window length is zero
-  su2double endTimeDouble = static_cast<su2double>(endTimeIter);
+  auto endTimeDouble = static_cast<su2double>(endTimeIter);
   su2double tau = currTimeDouble/endTimeDouble;
   return 2.0/3.0*(1-cos(2*PI_NUMBER*tau))*(1-cos(2*PI_NUMBER*tau));
 }
@@ -58,8 +58,8 @@ su2double CWindowingTools::HannSquaredWindow(unsigned long curTimeIter, unsigned
 su2double CWindowingTools::BumpWindow(unsigned long curTimeIter, unsigned long endTimeIter) {
   if(curTimeIter==0) return 0;
   if(curTimeIter==endTimeIter) return 0;
-  su2double currTimeDouble = static_cast<su2double>(curTimeIter);
-  su2double endTimeDouble = static_cast<su2double>(endTimeIter);
+  auto currTimeDouble = static_cast<su2double>(curTimeIter);
+  auto endTimeDouble = static_cast<su2double>(endTimeIter);
   su2double tau = currTimeDouble/endTimeDouble;
   return 1.0/0.00702986*(exp(-1/(tau-tau*tau)));
   /* 0.00702986 equals the integral of exp(-1/(tau-tau*tau)) from 0 to 1,
diff --git a/SU2_CFD/src/solvers/CAdjEulerSolver.cpp b/SU2_CFD/src/solvers/CAdjEulerSolver.cpp
index e16446e7785..034fe16adcc 100644
--- a/SU2_CFD/src/solvers/CAdjEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CAdjEulerSolver.cpp
@@ -29,7 +29,7 @@
 #include "../../include/solvers/CAdjEulerSolver.hpp"
 #include "../../../Common/include/toolboxes/geometry_toolbox.hpp"
 
-CAdjEulerSolver::CAdjEulerSolver(void) : CSolver() {
+CAdjEulerSolver::CAdjEulerSolver() : CSolver() {
 
   /*--- Array initialization ---*/
   Phi_Inf = nullptr;
@@ -271,8 +271,7 @@ CAdjEulerSolver::CAdjEulerSolver(CGeometry *geometry, CConfig *config, unsigned
 
   /*--- Define solver parameters needed for execution of destructor ---*/
 
-  if (config->GetKind_ConvNumScheme_AdjFlow() == SPACE_CENTERED) space_centered = true;
-  else space_centered = false;
+  space_centered = config->GetKind_ConvNumScheme_AdjFlow() == SPACE_CENTERED;
 
 
   /*--- Calculate area monitored for area-averaged-outflow-quantity-based objectives ---*/
@@ -348,7 +347,7 @@ CAdjEulerSolver::CAdjEulerSolver(CGeometry *geometry, CConfig *config, unsigned
   SolverName = "ADJ.FLOW";
 }
 
-CAdjEulerSolver::~CAdjEulerSolver(void) {
+CAdjEulerSolver::~CAdjEulerSolver() {
   unsigned short iVar, iMarker;
 
   delete [] Phi_Inf;
@@ -400,10 +399,10 @@ void CAdjEulerSolver::Set_MPI_ActDisk(CSolver **solver_container, CGeometry *geo
   /*--- Define buffer vector interior domain ---*/
 
   su2double        *Buffer_Send_AdjVar          = nullptr;
-  su2double        *iAdjVar          = new su2double [nVar];
+  auto        *iAdjVar          = new su2double [nVar];
 
-  unsigned long *nPointTotal_s = new unsigned long[size];
-  unsigned long *nPointTotal_r = new unsigned long[size];
+  auto *nPointTotal_s = new unsigned long[size];
+  auto *nPointTotal_r = new unsigned long[size];
 
   unsigned long Buffer_Size_AdjVar          = 0;
   unsigned long PointTotal_Counter = 0;
diff --git a/SU2_CFD/src/solvers/CAdjNSSolver.cpp b/SU2_CFD/src/solvers/CAdjNSSolver.cpp
index 8ad4ef3e7cf..75e5e65558b 100644
--- a/SU2_CFD/src/solvers/CAdjNSSolver.cpp
+++ b/SU2_CFD/src/solvers/CAdjNSSolver.cpp
@@ -30,7 +30,7 @@
 #include "../../include/variables/CAdjNSVariable.hpp"
 #include "../../../Common/include/toolboxes/geometry_toolbox.hpp"
 
-CAdjNSSolver::CAdjNSSolver(void) : CAdjEulerSolver() { }
+CAdjNSSolver::CAdjNSSolver() : CAdjEulerSolver() { }
 
 CAdjNSSolver::CAdjNSSolver(CGeometry *geometry, CConfig *config, unsigned short iMesh) : CAdjEulerSolver() {
   unsigned long iPoint, iVertex;
@@ -292,9 +292,7 @@ CAdjNSSolver::CAdjNSSolver(CGeometry *geometry, CConfig *config, unsigned short
 
 }
 
-CAdjNSSolver::~CAdjNSSolver(void) {
-
-}
+CAdjNSSolver::~CAdjNSSolver() = default;
 
 
 void CAdjNSSolver::SetTime_Step(CGeometry *geometry, CSolver **solver_container, CConfig *config,
@@ -600,25 +598,25 @@ void CAdjNSSolver::Viscous_Sensitivity(CGeometry *geometry, CSolver **solver_con
   dp_drv, dp_drw, dp_drE, dH_dr, dH_dru, dH_drv, dH_drw, dH_drE, H, D[3][3], Dd[3], Mach_Inf, eps, scale = 1.0,
   RefVel2, RefDensity, Mach2Vel, *Velocity_Inf, factor;
 
-  su2double *USens = new su2double[nVar];
-  su2double *UnitNormal = new su2double[nDim];
-  su2double *normal_grad_vel = new su2double[nDim];
-  su2double *tang_deriv_psi5 = new su2double[nDim];
-  su2double *tang_deriv_T = new su2double[nDim];
-  su2double **Sigma = new su2double* [nDim];
+  auto *USens = new su2double[nVar];
+  auto *UnitNormal = new su2double[nDim];
+  auto *normal_grad_vel = new su2double[nDim];
+  auto *tang_deriv_psi5 = new su2double[nDim];
+  auto *tang_deriv_T = new su2double[nDim];
+  auto **Sigma = new su2double* [nDim];
 
   for (iDim = 0; iDim < nDim; iDim++)
     Sigma[iDim] = new su2double [nDim];
 
-  su2double *normal_grad_gridvel = new su2double[nDim];
-  su2double *normal_grad_v_ux =new su2double[nDim];
-  su2double **Sigma_Psi5v = new su2double* [nDim];
+  auto *normal_grad_gridvel = new su2double[nDim];
+  auto *normal_grad_v_ux =new su2double[nDim];
+  auto **Sigma_Psi5v = new su2double* [nDim];
   for (iDim = 0; iDim < nDim; iDim++)
     Sigma_Psi5v[iDim] = new su2double [nDim];
-  su2double **tau = new su2double* [nDim];
+  auto **tau = new su2double* [nDim];
   for (iDim = 0; iDim < nDim; iDim++)
     tau[iDim] = new su2double [nDim];
-  su2double *Velocity = new su2double[nDim];
+  auto *Velocity = new su2double[nDim];
 
   bool rotating_frame    = config->GetRotating_Frame();
   bool grid_movement     = config->GetGrid_Movement();
@@ -1200,17 +1198,17 @@ void CAdjNSSolver::BC_HeatFlux_Wall(CGeometry *geometry, CSolver **solver_contai
   su2double Prandtl_Lam  = config->GetPrandtl_Lam();
   su2double Prandtl_Turb = config->GetPrandtl_Turb();
 
-  su2double *Psi = new su2double[nVar];
-  su2double **Tau = new su2double*[nDim];
+  auto *Psi = new su2double[nVar];
+  auto **Tau = new su2double*[nDim];
   for (iDim = 0; iDim < nDim; iDim++)
     Tau[iDim] = new su2double [nDim];
-  su2double *Velocity = new su2double[nDim];
-  su2double *Normal = new su2double[nDim];
-  su2double *Edge_Vector = new su2double[nDim];
-  su2double **GradPhi = new su2double*[nDim];
+  auto *Velocity = new su2double[nDim];
+  auto *Normal = new su2double[nDim];
+  auto *Edge_Vector = new su2double[nDim];
+  auto **GradPhi = new su2double*[nDim];
   for (iDim = 0; iDim < nDim; iDim++)
     GradPhi[iDim] = new su2double [nDim];
-  su2double *GradPsiE = new su2double [nDim];
+  auto *GradPsiE = new su2double [nDim];
 
   /*--- Loop over all of the vertices on this boundary marker ---*/
 
@@ -1551,21 +1549,21 @@ void CAdjNSSolver::BC_Isothermal_Wall(CGeometry *geometry, CSolver **solver_cont
   Sigma_yz5, eta_xx, eta_yy, eta_zz, eta_xy, eta_xz, eta_yz;
   su2double kGTdotn=0.0, Area=0.0, Xi=0.0;
 
-  su2double *Psi = new su2double[nVar];
-  su2double **Tau = new su2double* [nDim];
+  auto *Psi = new su2double[nVar];
+  auto **Tau = new su2double* [nDim];
   for (iDim = 0; iDim < nDim; iDim++)
     Tau[iDim] = new su2double [nDim];
-  su2double *Velocity = new su2double[nDim];
-  su2double *Normal = new su2double[nDim];
+  auto *Velocity = new su2double[nDim];
+  auto *Normal = new su2double[nDim];
 
-  su2double **GradPhi = new su2double* [nDim];
+  auto **GradPhi = new su2double* [nDim];
   for (iDim = 0; iDim < nDim; iDim++)
     GradPhi[iDim] = new su2double [nDim];
-  su2double *GradPsiE = new su2double [nDim];
+  auto *GradPsiE = new su2double [nDim];
   su2double *GradT;// = new su2double[nDim];
   su2double *GradP;
   su2double *GradDens;
-  su2double *dPoRho2 = new su2double[nDim];
+  auto *dPoRho2 = new su2double[nDim];
 
   bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
   bool grid_movement  = config->GetGrid_Movement();
diff --git a/SU2_CFD/src/solvers/CAdjTurbSolver.cpp b/SU2_CFD/src/solvers/CAdjTurbSolver.cpp
index e6e9ad5724e..704f4f786d0 100644
--- a/SU2_CFD/src/solvers/CAdjTurbSolver.cpp
+++ b/SU2_CFD/src/solvers/CAdjTurbSolver.cpp
@@ -28,7 +28,7 @@
 
 #include "../../include/solvers/CAdjTurbSolver.hpp"
 
-CAdjTurbSolver::CAdjTurbSolver(void) : CSolver() {}
+CAdjTurbSolver::CAdjTurbSolver() : CSolver() {}
 
 CAdjTurbSolver::CAdjTurbSolver(CGeometry *geometry, CConfig *config, unsigned short iMesh) : CSolver() {
 
@@ -163,7 +163,7 @@ CAdjTurbSolver::CAdjTurbSolver(CGeometry *geometry, CConfig *config, unsigned sh
 
 }
 
-CAdjTurbSolver::~CAdjTurbSolver(void) {
+CAdjTurbSolver::~CAdjTurbSolver() {
   delete nodes;
 }
 
diff --git a/SU2_CFD/src/solvers/CBaselineSolver.cpp b/SU2_CFD/src/solvers/CBaselineSolver.cpp
index 03a305abc42..97a4c04d15e 100644
--- a/SU2_CFD/src/solvers/CBaselineSolver.cpp
+++ b/SU2_CFD/src/solvers/CBaselineSolver.cpp
@@ -26,10 +26,12 @@
  */
 
 
+#include <utility>
+
 #include "../../include/solvers/CBaselineSolver.hpp"
 #include "../../../Common/include/toolboxes/printing_toolbox.hpp"
 
-CBaselineSolver::CBaselineSolver(void) : CSolver() { }
+CBaselineSolver::CBaselineSolver() : CSolver() { }
 
 CBaselineSolver::CBaselineSolver(CGeometry *geometry, CConfig *config) {
 
@@ -61,7 +63,7 @@ CBaselineSolver::CBaselineSolver(CGeometry *geometry, CConfig *config, unsigned
   nPoint = geometry->GetnPoint();
   nDim = geometry->GetnDim();
   nVar = val_nvar;
-  fields = field_names;
+  fields = std::move(field_names);
 
   /*--- Allocate the node variables ---*/
 
@@ -210,7 +212,7 @@ void CBaselineSolver::SetOutputVariables(CGeometry *geometry, CConfig *config) {
     SU2_MPI::Bcast(mpi_str_buf, nVar*CGNS_STRING_SIZE, MPI_CHAR,
                    MASTER_NODE, SU2_MPI::GetComm());
 
-    fields.push_back("Point_ID");
+    fields.emplace_back("Point_ID");
 
     for (iVar = 0; iVar < nVar; iVar++) {
       index = iVar*CGNS_STRING_SIZE;
@@ -220,7 +222,7 @@ void CBaselineSolver::SetOutputVariables(CGeometry *geometry, CConfig *config) {
       }
       field_buf.append(str_buf);
       field_buf.append("\"");
-      fields.push_back(field_buf.c_str());
+      fields.emplace_back(field_buf.c_str());
       field_buf.clear();
     }
 
@@ -359,7 +361,7 @@ void CBaselineSolver::LoadRestart(CGeometry **geometry, CSolver ***solver, CConf
   bool steady_restart = config->GetSteadyRestart();
   TURB_MODEL turb_model = config->GetKind_Turb_Model();
 
-  su2double *Coord = new su2double [nDim];
+  auto *Coord = new su2double [nDim];
   for (iDim = 0; iDim < nDim; iDim++)
     Coord[iDim] = 0.0;
 
@@ -519,7 +521,7 @@ void CBaselineSolver::LoadRestart_FSI(CGeometry *geometry, CConfig *config, int
   }
 
   unsigned short nVar_Local = Restart_Vars[1];
-  su2double *Solution_Local = new su2double[nVar_Local];
+  auto *Solution_Local = new su2double[nVar_Local];
 
   int counter = 0;
   long iPoint_Local = 0; unsigned long iPoint_Global = 0;
@@ -554,6 +556,6 @@ void CBaselineSolver::LoadRestart_FSI(CGeometry *geometry, CConfig *config, int
 
 }
 
-CBaselineSolver::~CBaselineSolver(void) {
+CBaselineSolver::~CBaselineSolver() {
   delete nodes;
 }
diff --git a/SU2_CFD/src/solvers/CBaselineSolver_FEM.cpp b/SU2_CFD/src/solvers/CBaselineSolver_FEM.cpp
index a15877d0d4e..bf213f5df36 100644
--- a/SU2_CFD/src/solvers/CBaselineSolver_FEM.cpp
+++ b/SU2_CFD/src/solvers/CBaselineSolver_FEM.cpp
@@ -29,7 +29,7 @@
 #include "../../include/solvers/CBaselineSolver_FEM.hpp"
 
 
-CBaselineSolver_FEM::CBaselineSolver_FEM(void) : CSolver() { }
+CBaselineSolver_FEM::CBaselineSolver_FEM() : CSolver() { }
 
 CBaselineSolver_FEM::CBaselineSolver_FEM(CGeometry *geometry, CConfig *config) {
 
@@ -43,7 +43,7 @@ CBaselineSolver_FEM::CBaselineSolver_FEM(CGeometry *geometry, CConfig *config) {
    the computation of the external faces may be more efficient when
    using multiple threads. ---*/
 
-  CMeshFEM_DG *DGGeometry = dynamic_cast<CMeshFEM_DG *>(geometry);
+  auto *DGGeometry = dynamic_cast<CMeshFEM_DG *>(geometry);
 
   nVolElemTot   = DGGeometry->GetNVolElemTot();
   nVolElemOwned = DGGeometry->GetNVolElemOwned();
@@ -385,4 +385,4 @@ void CBaselineSolver_FEM::LoadRestart(CGeometry **geometry, CSolver ***solver, C
 
 }
 
-CBaselineSolver_FEM::~CBaselineSolver_FEM(void) { }
+CBaselineSolver_FEM::~CBaselineSolver_FEM() = default;
diff --git a/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp b/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
index e82e61288a2..f11c9f580b6 100644
--- a/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
+++ b/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
@@ -451,7 +451,7 @@ void CDiscAdjFEASolver::ReadDV(const CConfig *config) {
     nDV = values.size();
     DV.resize(nDV);
     unsigned short iDV = 0;
-    for (auto x : values) DV[iDV++] = x;
+    for (const auto& x : values) DV[iDV++] = x;
 
   }
 
diff --git a/SU2_CFD/src/solvers/CDiscAdjSolver.cpp b/SU2_CFD/src/solvers/CDiscAdjSolver.cpp
index 29f42b3fc94..d6d94cf0d58 100644
--- a/SU2_CFD/src/solvers/CDiscAdjSolver.cpp
+++ b/SU2_CFD/src/solvers/CDiscAdjSolver.cpp
@@ -112,7 +112,7 @@ CDiscAdjSolver::CDiscAdjSolver(CGeometry *geometry, CConfig *config, CSolver *di
   }
 }
 
-CDiscAdjSolver::~CDiscAdjSolver(void) { delete nodes; }
+CDiscAdjSolver::~CDiscAdjSolver() { delete nodes; }
 
 void CDiscAdjSolver::SetRecording(CGeometry* geometry, CConfig *config){
 
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index 97fa79e6d15..547cc8c307c 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -77,7 +77,7 @@ CEulerSolver::CEulerSolver(CGeometry *geometry, CConfig *config,
   /*--- Check for a restart file to evaluate if there is a change in the angle of attack
    before computing all the non-dimesional quantities. ---*/
 
-  if (!(!restart || (iMesh != MESH_0) || nZone > 1) && config->GetFixed_CL_Mode()) {
+  if (restart && (iMesh == MESH_0) && nZone <= 1 && config->GetFixed_CL_Mode()) {
 
     /*--- Modify file name for a dual-time unsteady restart ---*/
 
@@ -335,7 +335,7 @@ CEulerSolver::CEulerSolver(CGeometry *geometry, CConfig *config,
     SU2_MPI::Error("Oops! The CEulerSolver static array sizes are not large enough.",CURRENT_FUNCTION);
 }
 
-CEulerSolver::~CEulerSolver(void) {
+CEulerSolver::~CEulerSolver() {
 
   for(auto& model : FluidModel) delete model;
 }
@@ -458,9 +458,9 @@ void CEulerSolver::Set_MPI_ActDisk(CSolver **solver_container, CGeometry *geomet
   su2double *Buffer_Send_PrimVar = nullptr;
   long      *Buffer_Send_Data    = nullptr;
 
-  unsigned long *nPointTotal_s = new unsigned long[size];
-  unsigned long *nPointTotal_r = new unsigned long[size];
-  su2double *iPrimVar = new su2double [nPrimVar_];
+  auto *nPointTotal_s = new unsigned long[size];
+  auto *nPointTotal_r = new unsigned long[size];
+  auto *iPrimVar = new su2double [nPrimVar_];
 
   unsigned long Buffer_Size_PrimVar = 0;
   unsigned long Buffer_Size_Data    = 0;
@@ -2559,32 +2559,32 @@ void CEulerSolver::GetPower_Properties(CGeometry *geometry, CConfig *config, uns
 
   if (Evaluate_BC) {
 
-    su2double *Inlet_MassFlow         = new su2double [config->GetnMarker_All()]();
-    su2double *Inlet_ReverseMassFlow  = new su2double [config->GetnMarker_All()]();
-    su2double *Inlet_Pressure         = new su2double [config->GetnMarker_All()]();
-    su2double *Inlet_Mach             = new su2double [config->GetnMarker_All()]();
-    su2double *Inlet_MaxPressure      = new su2double [config->GetnMarker_All()]();
-    su2double *Inlet_MinPressure      = new su2double [config->GetnMarker_All()]();
-    su2double *Inlet_TotalPressure    = new su2double [config->GetnMarker_All()]();
-    su2double *Inlet_Temperature      = new su2double [config->GetnMarker_All()]();
-    su2double *Inlet_TotalTemperature = new su2double [config->GetnMarker_All()]();
-    su2double *Inlet_Area             = new su2double [config->GetnMarker_All()]();
-    su2double *Inlet_RamDrag          = new su2double [config->GetnMarker_All()]();
-    su2double *Inlet_Force            = new su2double [config->GetnMarker_All()]();
-    su2double *Inlet_Power            = new su2double [config->GetnMarker_All()]();
-    su2double *Inlet_XCG              = new su2double [config->GetnMarker_All()]();
-    su2double *Inlet_YCG              = new su2double [config->GetnMarker_All()]();
-    su2double *Inlet_ZCG              = new su2double [config->GetnMarker_All()]();
-
-    su2double *Outlet_MassFlow         = new su2double [config->GetnMarker_All()]();
-    su2double *Outlet_Pressure         = new su2double [config->GetnMarker_All()]();
-    su2double *Outlet_TotalPressure    = new su2double [config->GetnMarker_All()]();
-    su2double *Outlet_Temperature      = new su2double [config->GetnMarker_All()]();
-    su2double *Outlet_TotalTemperature = new su2double [config->GetnMarker_All()]();
-    su2double *Outlet_Area             = new su2double [config->GetnMarker_All()]();
-    su2double *Outlet_GrossThrust      = new su2double [config->GetnMarker_All()]();
-    su2double *Outlet_Force            = new su2double [config->GetnMarker_All()]();
-    su2double *Outlet_Power            = new su2double [config->GetnMarker_All()]();
+    auto *Inlet_MassFlow         = new su2double [config->GetnMarker_All()]();
+    auto *Inlet_ReverseMassFlow  = new su2double [config->GetnMarker_All()]();
+    auto *Inlet_Pressure         = new su2double [config->GetnMarker_All()]();
+    auto *Inlet_Mach             = new su2double [config->GetnMarker_All()]();
+    auto *Inlet_MaxPressure      = new su2double [config->GetnMarker_All()]();
+    auto *Inlet_MinPressure      = new su2double [config->GetnMarker_All()]();
+    auto *Inlet_TotalPressure    = new su2double [config->GetnMarker_All()]();
+    auto *Inlet_Temperature      = new su2double [config->GetnMarker_All()]();
+    auto *Inlet_TotalTemperature = new su2double [config->GetnMarker_All()]();
+    auto *Inlet_Area             = new su2double [config->GetnMarker_All()]();
+    auto *Inlet_RamDrag          = new su2double [config->GetnMarker_All()]();
+    auto *Inlet_Force            = new su2double [config->GetnMarker_All()]();
+    auto *Inlet_Power            = new su2double [config->GetnMarker_All()]();
+    auto *Inlet_XCG              = new su2double [config->GetnMarker_All()]();
+    auto *Inlet_YCG              = new su2double [config->GetnMarker_All()]();
+    auto *Inlet_ZCG              = new su2double [config->GetnMarker_All()]();
+
+    auto *Outlet_MassFlow         = new su2double [config->GetnMarker_All()]();
+    auto *Outlet_Pressure         = new su2double [config->GetnMarker_All()]();
+    auto *Outlet_TotalPressure    = new su2double [config->GetnMarker_All()]();
+    auto *Outlet_Temperature      = new su2double [config->GetnMarker_All()]();
+    auto *Outlet_TotalTemperature = new su2double [config->GetnMarker_All()]();
+    auto *Outlet_Area             = new su2double [config->GetnMarker_All()]();
+    auto *Outlet_GrossThrust      = new su2double [config->GetnMarker_All()]();
+    auto *Outlet_Force            = new su2double [config->GetnMarker_All()]();
+    auto *Outlet_Power            = new su2double [config->GetnMarker_All()]();
 
     /*--- Comute MassFlow, average temp, press, etc. ---*/
 
@@ -2723,59 +2723,59 @@ void CEulerSolver::GetPower_Properties(CGeometry *geometry, CConfig *config, uns
 
     /*--- Copy to the appropriate structure ---*/
 
-    su2double *Inlet_MassFlow_Local             = new su2double [nMarker_Inlet]();
-    su2double *Inlet_ReverseMassFlow_Local      = new su2double [nMarker_Inlet]();
-    su2double *Inlet_Temperature_Local          = new su2double [nMarker_Inlet]();
-    su2double *Inlet_TotalTemperature_Local     = new su2double [nMarker_Inlet]();
-    su2double *Inlet_Pressure_Local             = new su2double [nMarker_Inlet]();
-    su2double *Inlet_Mach_Local                 = new su2double [nMarker_Inlet]();
-    su2double *Inlet_MinPressure_Local          = new su2double [nMarker_Inlet]();
-    su2double *Inlet_MaxPressure_Local          = new su2double [nMarker_Inlet]();
-    su2double *Inlet_Power_Local                = new su2double [nMarker_Inlet]();
-    su2double *Inlet_TotalPressure_Local        = new su2double [nMarker_Inlet]();
-    su2double *Inlet_RamDrag_Local              = new su2double [nMarker_Inlet]();
-    su2double *Inlet_Force_Local                = new su2double [nMarker_Inlet]();
-    su2double *Inlet_Area_Local                 = new su2double [nMarker_Inlet]();
-    su2double *Inlet_XCG_Local                  = new su2double [nMarker_Inlet]();
-    su2double *Inlet_YCG_Local                  = new su2double [nMarker_Inlet]();
-    su2double *Inlet_ZCG_Local                  = new su2double [nMarker_Inlet]();
-
-    su2double *Inlet_MassFlow_Total             = new su2double [nMarker_Inlet]();
-    su2double *Inlet_ReverseMassFlow_Total      = new su2double [nMarker_Inlet]();
-    su2double *Inlet_Pressure_Total             = new su2double [nMarker_Inlet]();
-    su2double *Inlet_Mach_Total                 = new su2double [nMarker_Inlet]();
-    su2double *Inlet_MinPressure_Total          = new su2double [nMarker_Inlet]();
-    su2double *Inlet_MaxPressure_Total          = new su2double [nMarker_Inlet]();
-    su2double *Inlet_Power_Total                = new su2double [nMarker_Inlet]();
-    su2double *Inlet_TotalPressure_Total        = new su2double [nMarker_Inlet]();
-    su2double *Inlet_Temperature_Total          = new su2double [nMarker_Inlet]();
-    su2double *Inlet_TotalTemperature_Total     = new su2double [nMarker_Inlet]();
-    su2double *Inlet_RamDrag_Total              = new su2double [nMarker_Inlet]();
-    su2double *Inlet_Force_Total                = new su2double [nMarker_Inlet]();
-    su2double *Inlet_Area_Total                 = new su2double [nMarker_Inlet]();
-    su2double *Inlet_XCG_Total                  = new su2double [nMarker_Inlet]();
-    su2double *Inlet_YCG_Total                  = new su2double [nMarker_Inlet]();
-    su2double *Inlet_ZCG_Total                  = new su2double [nMarker_Inlet]();
-
-    su2double *Outlet_MassFlow_Local            = new su2double [nMarker_Outlet]();
-    su2double *Outlet_Pressure_Local            = new su2double [nMarker_Outlet]();
-    su2double *Outlet_TotalPressure_Local       = new su2double [nMarker_Outlet]();
-    su2double *Outlet_Temperature_Local         = new su2double [nMarker_Outlet]();
-    su2double *Outlet_TotalTemperature_Local    = new su2double [nMarker_Outlet]();
-    su2double *Outlet_GrossThrust_Local         = new su2double [nMarker_Outlet]();
-    su2double *Outlet_Force_Local               = new su2double [nMarker_Outlet]();
-    su2double *Outlet_Power_Local               = new su2double [nMarker_Outlet]();
-    su2double *Outlet_Area_Local                = new su2double [nMarker_Outlet]();
-
-    su2double *Outlet_MassFlow_Total            = new su2double [nMarker_Outlet]();
-    su2double *Outlet_Pressure_Total            = new su2double [nMarker_Outlet]();
-    su2double *Outlet_TotalPressure_Total       = new su2double [nMarker_Outlet]();
-    su2double *Outlet_Temperature_Total         = new su2double [nMarker_Outlet]();
-    su2double *Outlet_TotalTemperature_Total    = new su2double [nMarker_Outlet]();
-    su2double *Outlet_GrossThrust_Total         = new su2double [nMarker_Outlet]();
-    su2double *Outlet_Force_Total               = new su2double [nMarker_Outlet]();
-    su2double *Outlet_Power_Total               = new su2double [nMarker_Outlet]();
-    su2double *Outlet_Area_Total                = new su2double [nMarker_Outlet]();
+    auto *Inlet_MassFlow_Local             = new su2double [nMarker_Inlet]();
+    auto *Inlet_ReverseMassFlow_Local      = new su2double [nMarker_Inlet]();
+    auto *Inlet_Temperature_Local          = new su2double [nMarker_Inlet]();
+    auto *Inlet_TotalTemperature_Local     = new su2double [nMarker_Inlet]();
+    auto *Inlet_Pressure_Local             = new su2double [nMarker_Inlet]();
+    auto *Inlet_Mach_Local                 = new su2double [nMarker_Inlet]();
+    auto *Inlet_MinPressure_Local          = new su2double [nMarker_Inlet]();
+    auto *Inlet_MaxPressure_Local          = new su2double [nMarker_Inlet]();
+    auto *Inlet_Power_Local                = new su2double [nMarker_Inlet]();
+    auto *Inlet_TotalPressure_Local        = new su2double [nMarker_Inlet]();
+    auto *Inlet_RamDrag_Local              = new su2double [nMarker_Inlet]();
+    auto *Inlet_Force_Local                = new su2double [nMarker_Inlet]();
+    auto *Inlet_Area_Local                 = new su2double [nMarker_Inlet]();
+    auto *Inlet_XCG_Local                  = new su2double [nMarker_Inlet]();
+    auto *Inlet_YCG_Local                  = new su2double [nMarker_Inlet]();
+    auto *Inlet_ZCG_Local                  = new su2double [nMarker_Inlet]();
+
+    auto *Inlet_MassFlow_Total             = new su2double [nMarker_Inlet]();
+    auto *Inlet_ReverseMassFlow_Total      = new su2double [nMarker_Inlet]();
+    auto *Inlet_Pressure_Total             = new su2double [nMarker_Inlet]();
+    auto *Inlet_Mach_Total                 = new su2double [nMarker_Inlet]();
+    auto *Inlet_MinPressure_Total          = new su2double [nMarker_Inlet]();
+    auto *Inlet_MaxPressure_Total          = new su2double [nMarker_Inlet]();
+    auto *Inlet_Power_Total                = new su2double [nMarker_Inlet]();
+    auto *Inlet_TotalPressure_Total        = new su2double [nMarker_Inlet]();
+    auto *Inlet_Temperature_Total          = new su2double [nMarker_Inlet]();
+    auto *Inlet_TotalTemperature_Total     = new su2double [nMarker_Inlet]();
+    auto *Inlet_RamDrag_Total              = new su2double [nMarker_Inlet]();
+    auto *Inlet_Force_Total                = new su2double [nMarker_Inlet]();
+    auto *Inlet_Area_Total                 = new su2double [nMarker_Inlet]();
+    auto *Inlet_XCG_Total                  = new su2double [nMarker_Inlet]();
+    auto *Inlet_YCG_Total                  = new su2double [nMarker_Inlet]();
+    auto *Inlet_ZCG_Total                  = new su2double [nMarker_Inlet]();
+
+    auto *Outlet_MassFlow_Local            = new su2double [nMarker_Outlet]();
+    auto *Outlet_Pressure_Local            = new su2double [nMarker_Outlet]();
+    auto *Outlet_TotalPressure_Local       = new su2double [nMarker_Outlet]();
+    auto *Outlet_Temperature_Local         = new su2double [nMarker_Outlet]();
+    auto *Outlet_TotalTemperature_Local    = new su2double [nMarker_Outlet]();
+    auto *Outlet_GrossThrust_Local         = new su2double [nMarker_Outlet]();
+    auto *Outlet_Force_Local               = new su2double [nMarker_Outlet]();
+    auto *Outlet_Power_Local               = new su2double [nMarker_Outlet]();
+    auto *Outlet_Area_Local                = new su2double [nMarker_Outlet]();
+
+    auto *Outlet_MassFlow_Total            = new su2double [nMarker_Outlet]();
+    auto *Outlet_Pressure_Total            = new su2double [nMarker_Outlet]();
+    auto *Outlet_TotalPressure_Total       = new su2double [nMarker_Outlet]();
+    auto *Outlet_Temperature_Total         = new su2double [nMarker_Outlet]();
+    auto *Outlet_TotalTemperature_Total    = new su2double [nMarker_Outlet]();
+    auto *Outlet_GrossThrust_Total         = new su2double [nMarker_Outlet]();
+    auto *Outlet_Force_Total               = new su2double [nMarker_Outlet]();
+    auto *Outlet_Power_Total               = new su2double [nMarker_Outlet]();
+    auto *Outlet_Area_Total                = new su2double [nMarker_Outlet]();
 
     /*--- Copy the values to the local array for MPI ---*/
 
@@ -3519,12 +3519,11 @@ void CEulerSolver::SetActDisk_BCThrust(CGeometry *geometry, CSolver **solver_con
 
       if ((InnerIter % Iter_Fixed_NetThrust == 0) && (InnerIter != 0)) {
         BCThrust_Counter++;
-        if ((BCThrust_Counter != 0) &&
+        Update_BCThrust_Bool = (BCThrust_Counter != 0) &&
             (BCThrust_Counter != 1) &&
             (BCThrust_Counter != Update_BCThrust) &&
             (BCThrust_Counter != Update_BCThrust + 2) &&
-            (BCThrust_Counter != Update_BCThrust + 4) ) Update_BCThrust_Bool = true;
-        else Update_BCThrust_Bool = false;
+            (BCThrust_Counter != Update_BCThrust + 4);
       }
 
       /*--- Store the update boolean for use on other mesh levels in the MG ---*/
@@ -4342,7 +4341,7 @@ void CEulerSolver::BC_Far_Field(CGeometry *geometry, CSolver **solver_container,
   bool viscous        = config->GetViscous();
   bool tkeNeeded = config->GetKind_Turb_Model() == TURB_MODEL::SST;
 
-  su2double *Normal = new su2double[nDim];
+  auto *Normal = new su2double[nDim];
 
   /*--- Loop over all the vertices on this boundary marker ---*/
 
@@ -6829,7 +6828,7 @@ void CEulerSolver::BC_Outlet(CGeometry *geometry, CSolver **solver_container,
   bool gravity = (config->GetGravityForce());
   bool tkeNeeded = (config->GetKind_Turb_Model() == TURB_MODEL::SST);
 
-  su2double *Normal = new su2double[nDim];
+  auto *Normal = new su2double[nDim];
 
   /*--- Loop over all the vertices on this boundary marker ---*/
 
@@ -7085,7 +7084,7 @@ void CEulerSolver::BC_Supersonic_Outlet(CGeometry *geometry, CSolver **solver_co
   bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
   string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
 
-  su2double *Normal = new su2double[nDim];
+  auto *Normal = new su2double[nDim];
 
   /*--- Supersonic outlet flow: there are no ingoing characteristics,
    so all flow variables can should be interpolated from the domain. ---*/
@@ -7213,7 +7212,7 @@ void CEulerSolver::BC_Engine_Inflow(CGeometry *geometry, CSolver **solver_contai
   su2double Baseline_Press = 0.75 * config->GetPressure_FreeStreamND();
   bool Engine_HalfModel = config->GetEngine_HalfModel();
 
-  su2double *Normal = new su2double[nDim];
+  auto *Normal = new su2double[nDim];
 
 
   if (Kind_Engine_Inflow == FAN_FACE_MACH) {
@@ -7429,7 +7428,7 @@ void CEulerSolver::BC_Engine_Exhaust(CGeometry *geometry, CSolver **solver_conta
   su2double DampingFactor = config->GetDamp_Engine_Exhaust();
   su2double Baseline_Press = 0.75 * config->GetPressure_FreeStreamND();
 
-  su2double *Normal = new su2double[nDim];
+  auto *Normal = new su2double[nDim];
 
   /*--- Retrieve the specified exhaust pressure in the engine (non-dimensional). ---*/
 
@@ -7719,8 +7718,8 @@ void CEulerSolver::BC_ActDisk(CGeometry *geometry, CSolver **solver_container, C
   bool ratio              = (config->GetActDisk_Jump() == RATIO);
   su2double SecondaryFlow = config->GetSecondaryFlow_ActDisk();
 
-  su2double *Normal = new su2double[nDim];
-  su2double *Flow_Dir = new su2double[nDim];
+  auto *Normal = new su2double[nDim];
+  auto *Flow_Dir = new su2double[nDim];
 
   /*--- Loop over all the vertices on this boundary marker ---*/
 
@@ -8519,7 +8518,7 @@ void CEulerSolver::PreprocessAverage(CSolver **solver, CGeometry *geometry, CCon
     SU2_MPI::Allreduce(&MyTotalAreaDensity, &TotalAreaDensity, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
     SU2_MPI::Allreduce(&MyTotalAreaPressure, &TotalAreaPressure, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
 
-    su2double* MyTotalAreaVelocity = new su2double[nDim];
+    auto* MyTotalAreaVelocity = new su2double[nDim];
 
     for (iDim = 0; iDim < nDim; iDim++) {
       MyTotalAreaVelocity[iDim] = TotalAreaVelocity[iDim];
@@ -8867,7 +8866,7 @@ void CEulerSolver::TurboAverageProcess(CSolver **solver, CGeometry *geometry, CC
     TotalMassKine = Allreduce(TotalMassKine);
     TotalMassOmega = Allreduce(TotalMassOmega);
 
-    su2double* buffer = new su2double[max(nVar,nDim)];
+    auto* buffer = new su2double[max(nVar,nDim)];
 
     auto Allreduce_inplace = [buffer](int size, su2double* x) {
       SU2_MPI::Allreduce(x, buffer, size, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
@@ -9267,9 +9266,9 @@ void CEulerSolver::GatherInOutAverageValues(CConfig *config, CGeometry *geometry
 
 #ifdef HAVE_MPI
     unsigned short i, n1, n2, n1t,n2t;
-    su2double *TurbPerfIn= NULL,*TurbPerfOut= NULL;
-    su2double *TotTurbPerfIn = NULL,*TotTurbPerfOut = NULL;
-    int *TotMarkerTP = NULL;
+    su2double *TurbPerfIn= nullptr,*TurbPerfOut= nullptr;
+    su2double *TotTurbPerfIn = nullptr,*TotTurbPerfOut = nullptr;
+    int *TotMarkerTP = nullptr;
 
     n1          = 8;
     n2          = 8;
diff --git a/SU2_CFD/src/solvers/CFEASolver.cpp b/SU2_CFD/src/solvers/CFEASolver.cpp
index 4f30cb91450..57495c3d829 100644
--- a/SU2_CFD/src/solvers/CFEASolver.cpp
+++ b/SU2_CFD/src/solvers/CFEASolver.cpp
@@ -119,7 +119,7 @@ CFEASolver::CFEASolver(CGeometry *geometry, CConfig *config) : CFEASolverBase(ge
   if (dynamic) nSolVar = 3 * nVar;
   else nSolVar = nVar;
 
-  su2double* SolInit = new su2double[nSolVar]();
+  auto* SolInit = new su2double[nSolVar]();
 
   /*--- Initialize from zero everywhere ---*/
 
@@ -215,7 +215,7 @@ CFEASolver::CFEASolver(CGeometry *geometry, CConfig *config) : CFEASolverBase(ge
   SolverName = "FEA";
 }
 
-CFEASolver::~CFEASolver(void) {
+CFEASolver::~CFEASolver() {
 
   if (element_properties != nullptr) {
     for (unsigned long iElem = 0; iElem < nElement; iElem++)
@@ -3213,13 +3213,13 @@ void CFEASolver::FilterElementDensities(CGeometry *geometry, const CConfig *conf
   {
     ENUM_FILTER_KERNEL type;
     config->GetTopology_Optim_Kernel(iKernel,type,param,radius);
-    kernels.push_back(make_pair(type,param));
+    kernels.emplace_back(type,param);
     filter_radius.push_back(radius);
   }
   search_lim = config->GetTopology_Search_Limit();
   config->GetTopology_Optim_Projection(type,param);
 
-  su2double *physical_rho = new su2double [nElement];
+  auto *physical_rho = new su2double [nElement];
 
   /*--- "Rectify" the input, initialize the physical density with
   the design density (the filter function works in-place). ---*/
diff --git a/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp b/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
index 1a12467366a..877611c3787 100644
--- a/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
@@ -33,9 +33,11 @@
 #include "../../include/fluid/CPengRobinson.hpp"
 #include "../../include/fluid/CCoolProp.hpp"
 
-#define SIZE_ARR_NORM 8
+enum {
+SIZE_ARR_NORM = 8
+};
 
-CFEM_DG_EulerSolver::CFEM_DG_EulerSolver(void) : CSolver() {
+CFEM_DG_EulerSolver::CFEM_DG_EulerSolver() : CSolver() {
 
   /*--- Basic array initialization ---*/
 
@@ -153,7 +155,7 @@ CFEM_DG_EulerSolver::CFEM_DG_EulerSolver(CGeometry *geometry, CConfig *config, u
 
   /*--- Create an object of the class CMeshFEM_DG and retrieve the necessary
         geometrical information for the FEM DG solver. ---*/
-  CMeshFEM_DG *DGGeometry = dynamic_cast<CMeshFEM_DG *>(geometry);
+  auto *DGGeometry = dynamic_cast<CMeshFEM_DG *>(geometry);
 
   nVolElemTot   = DGGeometry->GetNVolElemTot();
   nVolElemOwned = DGGeometry->GetNVolElemOwned();
@@ -727,7 +729,7 @@ CFEM_DG_EulerSolver::CFEM_DG_EulerSolver(CGeometry *geometry, CConfig *config, u
   SolverName = "DG.FLOW";
 }
 
-CFEM_DG_EulerSolver::~CFEM_DG_EulerSolver(void) {
+CFEM_DG_EulerSolver::~CFEM_DG_EulerSolver() {
 
   delete FluidModel;
   delete blasFunctions;
@@ -1961,13 +1963,13 @@ void CFEM_DG_EulerSolver::SetUpTaskList(CConfig *config) {
       if(elemEnd > elemBeg) {
         prevInd[0] = indexInList[CTaskDefinition::ADER_UPDATE_SOLUTION][0];
         indexInList[CTaskDefinition::ADER_PREDICTOR_STEP_COMM_ELEMENTS][0] = (int)tasksList.size();
-        tasksList.push_back(CTaskDefinition(CTaskDefinition::ADER_PREDICTOR_STEP_COMM_ELEMENTS, 0, prevInd[0]));
+        tasksList.emplace_back(CTaskDefinition::ADER_PREDICTOR_STEP_COMM_ELEMENTS, 0, prevInd[0]);
       }
 
       /* Initiate the communication of elements of level 0, if there is
          something to be communicated. */
 #ifdef HAVE_MPI
-      if( commRequests[0].size() ) {
+      if( !commRequests[0].empty() ) {
         if(elemEnd > elemBeg)   // Data needs to be computed before sending.
           prevInd[0] = indexInList[CTaskDefinition::ADER_PREDICTOR_STEP_COMM_ELEMENTS][0];
         else                    // Data only needs to be received.
@@ -1978,8 +1980,8 @@ void CFEM_DG_EulerSolver::SetUpTaskList(CConfig *config) {
 
         /* Create the task. */
         indexInList[CTaskDefinition::INITIATE_MPI_COMMUNICATION][0] = tasksList.size();
-        tasksList.push_back(CTaskDefinition(CTaskDefinition::INITIATE_MPI_COMMUNICATION, 0,
-                                            prevInd[0], prevInd[1]));
+        tasksList.emplace_back(CTaskDefinition::INITIATE_MPI_COMMUNICATION, 0,
+                                            prevInd[0], prevInd[1]);
       }
 #endif
 
@@ -1997,13 +1999,13 @@ void CFEM_DG_EulerSolver::SetUpTaskList(CConfig *config) {
         if(elemEnd > elemBeg) {
           prevInd[0] = indexInList[CTaskDefinition::ADER_UPDATE_SOLUTION][nL];
           indexInList[CTaskDefinition::ADER_PREDICTOR_STEP_COMM_ELEMENTS][nL] = (int)tasksList.size();
-          tasksList.push_back(CTaskDefinition(CTaskDefinition::ADER_PREDICTOR_STEP_COMM_ELEMENTS, nL, prevInd[0]));
+          tasksList.emplace_back(CTaskDefinition::ADER_PREDICTOR_STEP_COMM_ELEMENTS, nL, prevInd[0]);
         }
 
         /* Initiate the communication of elements of level nL, if there is
            something to be communicated. */
 #ifdef HAVE_MPI
-        if( commRequests[nL].size() ) {
+        if( !commRequests[nL].empty() ) {
           if(elemEnd > elemBeg)   // Data needs to be computed before sending.
             prevInd[0] = indexInList[CTaskDefinition::ADER_PREDICTOR_STEP_COMM_ELEMENTS][nL];
           else                    // Data only needs to be received.
@@ -2014,8 +2016,8 @@ void CFEM_DG_EulerSolver::SetUpTaskList(CConfig *config) {
 
           /* Create the actual task. */
           indexInList[CTaskDefinition::INITIATE_MPI_COMMUNICATION][nL] = tasksList.size();
-          tasksList.push_back(CTaskDefinition(CTaskDefinition::INITIATE_MPI_COMMUNICATION, nL,
-                                              prevInd[0], prevInd[1]));
+          tasksList.emplace_back(CTaskDefinition::INITIATE_MPI_COMMUNICATION, nL,
+                                              prevInd[0], prevInd[1]);
         }
 #endif
       }
@@ -2028,18 +2030,18 @@ void CFEM_DG_EulerSolver::SetUpTaskList(CConfig *config) {
       if(elemEnd > elemBeg) {
         prevInd[0] = indexInList[CTaskDefinition::ADER_UPDATE_SOLUTION][0];
         indexInList[CTaskDefinition::ADER_PREDICTOR_STEP_INTERNAL_ELEMENTS][0] = (int)tasksList.size();
-        tasksList.push_back(CTaskDefinition(CTaskDefinition::ADER_PREDICTOR_STEP_INTERNAL_ELEMENTS, 0, prevInd[0]));
+        tasksList.emplace_back(CTaskDefinition::ADER_PREDICTOR_STEP_INTERNAL_ELEMENTS, 0, prevInd[0]);
       }
 
       /* Determine the tasks to be completed before the communication of time
          level 0 can be completed. */
       prevInd[0] = prevInd[1] = prevInd[2] = -1;
 #ifdef HAVE_MPI
-      if( commRequests[0].size() )
+      if( !commRequests[0].empty() )
         prevInd[0] = indexInList[CTaskDefinition::INITIATE_MPI_COMMUNICATION][0];
 #endif
 
-      if( elementsSendSelfComm[0].size() ) {
+      if( !elementsSendSelfComm[0].empty() ) {
         prevInd[1] = indexInList[CTaskDefinition::ADER_PREDICTOR_STEP_COMM_ELEMENTS][0];
         prevInd[2] = indexInList[CTaskDefinition::ADER_PREDICTOR_STEP_INTERNAL_ELEMENTS][0];
       }
@@ -2051,8 +2053,8 @@ void CFEM_DG_EulerSolver::SetUpTaskList(CConfig *config) {
          to be completed. */
       if(prevInd[0] > -1) {
         indexInList[CTaskDefinition::COMPLETE_MPI_COMMUNICATION][0] = (int)tasksList.size();
-        tasksList.push_back(CTaskDefinition(CTaskDefinition::COMPLETE_MPI_COMMUNICATION, 0,
-                                            prevInd[0], prevInd[1], prevInd[2]));
+        tasksList.emplace_back(CTaskDefinition::COMPLETE_MPI_COMMUNICATION, 0,
+                                            prevInd[0], prevInd[1], prevInd[2]);
       }
 
       /* Check if the time level is not nTimeLevels-1. In that case carry out
@@ -2070,18 +2072,18 @@ void CFEM_DG_EulerSolver::SetUpTaskList(CConfig *config) {
         if(elemEnd > elemBeg) {
           prevInd[0] = indexInList[CTaskDefinition::ADER_UPDATE_SOLUTION][nL];
           indexInList[CTaskDefinition::ADER_PREDICTOR_STEP_INTERNAL_ELEMENTS][nL] = (int)tasksList.size();
-          tasksList.push_back(CTaskDefinition(CTaskDefinition::ADER_PREDICTOR_STEP_INTERNAL_ELEMENTS, nL, prevInd[0]));
+          tasksList.emplace_back(CTaskDefinition::ADER_PREDICTOR_STEP_INTERNAL_ELEMENTS, nL, prevInd[0]);
         }
 
         /* Determine the tasks to be completed before the communication of time
            level nL can be completed. */
         prevInd[0] = prevInd[1] = prevInd[2] = -1;
 #ifdef HAVE_MPI
-        if( commRequests[nL].size() )
+        if( !commRequests[nL].empty() )
           prevInd[0] = indexInList[CTaskDefinition::INITIATE_MPI_COMMUNICATION][nL];
 #endif
 
-        if( elementsSendSelfComm[nL].size() ) {
+        if( !elementsSendSelfComm[nL].empty() ) {
           prevInd[1] = indexInList[CTaskDefinition::ADER_PREDICTOR_STEP_COMM_ELEMENTS][nL];
           prevInd[2] = indexInList[CTaskDefinition::ADER_PREDICTOR_STEP_INTERNAL_ELEMENTS][nL];
         }
@@ -2093,8 +2095,8 @@ void CFEM_DG_EulerSolver::SetUpTaskList(CConfig *config) {
            to be completed. */
         if(prevInd[0] > -1) {
           indexInList[CTaskDefinition::COMPLETE_MPI_COMMUNICATION][nL] = (int)tasksList.size();
-          tasksList.push_back(CTaskDefinition(CTaskDefinition::COMPLETE_MPI_COMMUNICATION, nL,
-                                              prevInd[0], prevInd[1], prevInd[2]));
+          tasksList.emplace_back(CTaskDefinition::COMPLETE_MPI_COMMUNICATION, nL,
+                                              prevInd[0], prevInd[1], prevInd[2]);
         }
       }
 
@@ -2160,8 +2162,8 @@ void CFEM_DG_EulerSolver::SetUpTaskList(CConfig *config) {
 
             /* Create the task. */
             indexInList[CTaskDefinition::ADER_TIME_INTERPOLATE_OWNED_ELEMENTS][level] = (int)tasksList.size();
-            tasksList.push_back(CTaskDefinition(CTaskDefinition::ADER_TIME_INTERPOLATE_OWNED_ELEMENTS,
-                                                level, prevInd[0], prevInd[1], prevInd[2], prevInd[3], prevInd[4]));
+            tasksList.emplace_back(CTaskDefinition::ADER_TIME_INTERPOLATE_OWNED_ELEMENTS,
+                                                level, prevInd[0], prevInd[1], prevInd[2], prevInd[3], prevInd[4]);
 
             /* The info on the integration point and whether or not this
                time integration corresponds to the second part for the
@@ -2174,8 +2176,8 @@ void CFEM_DG_EulerSolver::SetUpTaskList(CConfig *config) {
                including the adjacent ones. */
             prevInd[0] = indexInList[CTaskDefinition::ADER_TIME_INTERPOLATE_OWNED_ELEMENTS][level];
             indexInList[CTaskDefinition::SHOCK_CAPTURING_VISCOSITY_OWNED_ELEMENTS][level] = (int)tasksList.size();
-            tasksList.push_back(CTaskDefinition(CTaskDefinition::SHOCK_CAPTURING_VISCOSITY_OWNED_ELEMENTS,
-                                                level, prevInd[0]));
+            tasksList.emplace_back(CTaskDefinition::SHOCK_CAPTURING_VISCOSITY_OWNED_ELEMENTS,
+                                                level, prevInd[0]);
           }
 
           /* The solution of the halo elements of the current time level and
@@ -2220,8 +2222,8 @@ void CFEM_DG_EulerSolver::SetUpTaskList(CConfig *config) {
 
             /* Create the task. */
             indexInList[CTaskDefinition::ADER_TIME_INTERPOLATE_HALO_ELEMENTS][level] = (int)tasksList.size();
-            tasksList.push_back(CTaskDefinition(CTaskDefinition::ADER_TIME_INTERPOLATE_HALO_ELEMENTS,
-                                                level, prevInd[0], prevInd[1]));
+            tasksList.emplace_back(CTaskDefinition::ADER_TIME_INTERPOLATE_HALO_ELEMENTS,
+                                                level, prevInd[0], prevInd[1]);
 
             /* The info on the integration point and whether or not this
                time integration corresponds to the second part for the
@@ -2234,8 +2236,8 @@ void CFEM_DG_EulerSolver::SetUpTaskList(CConfig *config) {
                including the adjacent ones. */
             prevInd[0] = indexInList[CTaskDefinition::ADER_TIME_INTERPOLATE_HALO_ELEMENTS][level];
             indexInList[CTaskDefinition::SHOCK_CAPTURING_VISCOSITY_HALO_ELEMENTS][level] = (int)tasksList.size();
-            tasksList.push_back(CTaskDefinition(CTaskDefinition::SHOCK_CAPTURING_VISCOSITY_HALO_ELEMENTS,
-                                                level, prevInd[0]));
+            tasksList.emplace_back(CTaskDefinition::SHOCK_CAPTURING_VISCOSITY_HALO_ELEMENTS,
+                                                level, prevInd[0]);
           }
 
           /* Check whether there are boundary conditions that involve halo elements. */
@@ -2247,8 +2249,8 @@ void CFEM_DG_EulerSolver::SetUpTaskList(CConfig *config) {
 
             /* Create the task for the boundary conditions that involve halo elements. */
             indexInList[CTaskDefinition::BOUNDARY_CONDITIONS_DEPEND_ON_HALO][level] = (int)tasksList.size();
-            tasksList.push_back(CTaskDefinition(CTaskDefinition::BOUNDARY_CONDITIONS_DEPEND_ON_HALO,
-                                                level, prevInd[0], prevInd[1]));
+            tasksList.emplace_back(CTaskDefinition::BOUNDARY_CONDITIONS_DEPEND_ON_HALO,
+                                                level, prevInd[0], prevInd[1]);
           }
 
           /* Compute the surface residuals for this time level that involve
@@ -2271,15 +2273,15 @@ void CFEM_DG_EulerSolver::SetUpTaskList(CConfig *config) {
 
             /* Create the task for the surface residual. */
             indexInList[CTaskDefinition::SURFACE_RESIDUAL_HALO_ELEMENTS][level] = (int)tasksList.size();
-            tasksList.push_back(CTaskDefinition(CTaskDefinition::SURFACE_RESIDUAL_HALO_ELEMENTS,
-                                                level, prevInd[0], prevInd[1], prevInd[2]));
+            tasksList.emplace_back(CTaskDefinition::SURFACE_RESIDUAL_HALO_ELEMENTS,
+                                                level, prevInd[0], prevInd[1], prevInd[2]);
 
             /* Create the task to accumulate the surface residuals of the halo
                elements. Make sure to set the integration point for this task. */
             prevInd[0] = indexInList[CTaskDefinition::SURFACE_RESIDUAL_HALO_ELEMENTS][level];
             indexInList[CTaskDefinition::ADER_ACCUMULATE_SPACETIME_RESIDUAL_HALO_ELEMENTS][level] = (int)tasksList.size();
-            tasksList.push_back(CTaskDefinition(CTaskDefinition::ADER_ACCUMULATE_SPACETIME_RESIDUAL_HALO_ELEMENTS,
-                                                level, prevInd[0]));
+            tasksList.emplace_back(CTaskDefinition::ADER_ACCUMULATE_SPACETIME_RESIDUAL_HALO_ELEMENTS,
+                                                level, prevInd[0]);
             tasksList.back().intPointADER = intPoint;
           }
 
@@ -2295,14 +2297,14 @@ void CFEM_DG_EulerSolver::SetUpTaskList(CConfig *config) {
             bool commData = false;
 
 #ifdef HAVE_MPI
-            if( commRequests[level].size() ) commData = true;
+            if( !commRequests[level].empty() ) commData = true;
 #endif
-            if(commData || elementsSendSelfComm[level].size()) {
+            if(commData || !elementsSendSelfComm[level].empty()) {
 
               /* Determine the dependencies before the reverse communication
                  can start. */
               prevInd[0] = indexInList[CTaskDefinition::ADER_ACCUMULATE_SPACETIME_RESIDUAL_HALO_ELEMENTS][level];
-              if( haloElemAdjLowTimeLevel[level].size() )
+              if( !haloElemAdjLowTimeLevel[level].empty() )
                 prevInd[1] = indexInList[CTaskDefinition::ADER_ACCUMULATE_SPACETIME_RESIDUAL_HALO_ELEMENTS][level-1];
               else
                 prevInd[1] = -1;
@@ -2311,8 +2313,8 @@ void CFEM_DG_EulerSolver::SetUpTaskList(CConfig *config) {
 
               /* Create the task. */
               indexInList[CTaskDefinition::INITIATE_REVERSE_MPI_COMMUNICATION][level] = (int)tasksList.size();
-              tasksList.push_back(CTaskDefinition(CTaskDefinition::INITIATE_REVERSE_MPI_COMMUNICATION,
-                                                  level, prevInd[0], prevInd[1], prevInd[2]));
+              tasksList.emplace_back(CTaskDefinition::INITIATE_REVERSE_MPI_COMMUNICATION,
+                                                  level, prevInd[0], prevInd[1], prevInd[2]);
             }
           }
 
@@ -2333,18 +2335,18 @@ void CFEM_DG_EulerSolver::SetUpTaskList(CConfig *config) {
 
             /* Create the tasks. */
             indexInList[CTaskDefinition::VOLUME_RESIDUAL][level] = (int)tasksList.size();
-            tasksList.push_back(CTaskDefinition(CTaskDefinition::VOLUME_RESIDUAL, level,
-                                                prevInd[0], prevInd[1]));
+            tasksList.emplace_back(CTaskDefinition::VOLUME_RESIDUAL, level,
+                                                prevInd[0], prevInd[1]);
 
             indexInList[CTaskDefinition::BOUNDARY_CONDITIONS_DEPEND_ON_OWNED][level] = (int)tasksList.size();
-            tasksList.push_back(CTaskDefinition(CTaskDefinition::BOUNDARY_CONDITIONS_DEPEND_ON_OWNED, level,
-                                                prevInd[0], prevInd[1]));
+            tasksList.emplace_back(CTaskDefinition::BOUNDARY_CONDITIONS_DEPEND_ON_OWNED, level,
+                                                prevInd[0], prevInd[1]);
 
             if(nMatchingInternalFacesLocalElem[level+1] >
                nMatchingInternalFacesLocalElem[level]) {
               indexInList[CTaskDefinition::SURFACE_RESIDUAL_OWNED_ELEMENTS][level] = (int)tasksList.size();
-              tasksList.push_back(CTaskDefinition(CTaskDefinition::SURFACE_RESIDUAL_OWNED_ELEMENTS,
-                                                  level, prevInd[0], prevInd[1]));
+              tasksList.emplace_back(CTaskDefinition::SURFACE_RESIDUAL_OWNED_ELEMENTS,
+                                                  level, prevInd[0], prevInd[1]);
             }
           }
 
@@ -2361,8 +2363,8 @@ void CFEM_DG_EulerSolver::SetUpTaskList(CConfig *config) {
 
             /* Create the task. */
             indexInList[CTaskDefinition::ADER_ACCUMULATE_SPACETIME_RESIDUAL_OWNED_ELEMENTS][level] = (int)tasksList.size();
-            tasksList.push_back(CTaskDefinition(CTaskDefinition::ADER_ACCUMULATE_SPACETIME_RESIDUAL_OWNED_ELEMENTS,
-                                                level, prevInd[0], prevInd[1], prevInd[2], prevInd[3], prevInd[4]));
+            tasksList.emplace_back(CTaskDefinition::ADER_ACCUMULATE_SPACETIME_RESIDUAL_OWNED_ELEMENTS,
+                                                level, prevInd[0], prevInd[1], prevInd[2], prevInd[3], prevInd[4]);
             tasksList.back().intPointADER = intPoint;
           }
 
@@ -2374,23 +2376,23 @@ void CFEM_DG_EulerSolver::SetUpTaskList(CConfig *config) {
             bool commData = false;
 
 #ifdef HAVE_MPI
-            if( commRequests[level].size() ) commData = true;
+            if( !commRequests[level].empty() ) commData = true;
 #endif
-            if(commData || elementsSendSelfComm[level].size()) {
+            if(commData || !elementsSendSelfComm[level].empty()) {
 
               /* Determine the dependencies before the reverse communication
                  can be completed. */
               prevInd[0] = indexInList[CTaskDefinition::INITIATE_REVERSE_MPI_COMMUNICATION][level];
               prevInd[1] = indexInList[CTaskDefinition::ADER_ACCUMULATE_SPACETIME_RESIDUAL_OWNED_ELEMENTS][level];
-              if( ownedElemAdjLowTimeLevel[level].size() )
+              if( !ownedElemAdjLowTimeLevel[level].empty() )
                 prevInd[2] = indexInList[CTaskDefinition::ADER_ACCUMULATE_SPACETIME_RESIDUAL_OWNED_ELEMENTS][level-1];
               else
                 prevInd[2] = -1;
 
               /* Create the task. */
               indexInList[CTaskDefinition::COMPLETE_REVERSE_MPI_COMMUNICATION][level] = (int)tasksList.size();
-              tasksList.push_back(CTaskDefinition(CTaskDefinition::COMPLETE_REVERSE_MPI_COMMUNICATION,
-                                                  level, prevInd[0], prevInd[1], prevInd[2]));
+              tasksList.emplace_back(CTaskDefinition::COMPLETE_REVERSE_MPI_COMMUNICATION,
+                                                  level, prevInd[0], prevInd[1], prevInd[2]);
             }
           }
 
@@ -2411,20 +2413,20 @@ void CFEM_DG_EulerSolver::SetUpTaskList(CConfig *config) {
              added to the dependency list. */
           prevInd[0] = indexInList[CTaskDefinition::COMPLETE_REVERSE_MPI_COMMUNICATION][level];
           prevInd[1] = indexInList[CTaskDefinition::ADER_ACCUMULATE_SPACETIME_RESIDUAL_OWNED_ELEMENTS][level];
-          if( ownedElemAdjLowTimeLevel[level].size() )
+          if( !ownedElemAdjLowTimeLevel[level].empty() )
             prevInd[2] = indexInList[CTaskDefinition::ADER_ACCUMULATE_SPACETIME_RESIDUAL_OWNED_ELEMENTS][level-1];
           else
             prevInd[2] = -1;
 
           indexInList[CTaskDefinition::MULTIPLY_INVERSE_MASS_MATRIX][level] = (int)tasksList.size();
-          tasksList.push_back(CTaskDefinition(CTaskDefinition::MULTIPLY_INVERSE_MASS_MATRIX,
-                                               level, prevInd[0], prevInd[1], prevInd[2]));
+          tasksList.emplace_back(CTaskDefinition::MULTIPLY_INVERSE_MASS_MATRIX,
+                                               level, prevInd[0], prevInd[1], prevInd[2]);
 
           /* Compute the new state vector for this time level. */
           prevInd[0] = indexInList[CTaskDefinition::MULTIPLY_INVERSE_MASS_MATRIX][level];
           indexInList[CTaskDefinition::ADER_UPDATE_SOLUTION][level] = (int)tasksList.size();
-          tasksList.push_back(CTaskDefinition(CTaskDefinition::ADER_UPDATE_SOLUTION,
-                                               level, prevInd[0]));
+          tasksList.emplace_back(CTaskDefinition::ADER_UPDATE_SOLUTION,
+                                               level, prevInd[0]);
         }
       }
 
@@ -2495,20 +2497,20 @@ void CFEM_DG_EulerSolver::SetUpTaskList(CConfig *config) {
     /* relatively short tasks list, which can be set easily.                  */
     /*------------------------------------------------------------------------*/
 
-    tasksList.push_back(CTaskDefinition(CTaskDefinition::INITIATE_MPI_COMMUNICATION,                   0));                   // Task  0
-    tasksList.push_back(CTaskDefinition(CTaskDefinition::SHOCK_CAPTURING_VISCOSITY_OWNED_ELEMENTS,     0));                   // Task  1
-    tasksList.push_back(CTaskDefinition(CTaskDefinition::VOLUME_RESIDUAL,                              0,  1));               // Task  2
-    tasksList.push_back(CTaskDefinition(CTaskDefinition::COMPLETE_MPI_COMMUNICATION,                   0,  0));               // Task  3
-    tasksList.push_back(CTaskDefinition(CTaskDefinition::SHOCK_CAPTURING_VISCOSITY_HALO_ELEMENTS,      0,  3));               // Task  4
-    tasksList.push_back(CTaskDefinition(CTaskDefinition::SURFACE_RESIDUAL_HALO_ELEMENTS,               0,  1, 4));            // Task  5
-    tasksList.push_back(CTaskDefinition(CTaskDefinition::BOUNDARY_CONDITIONS_DEPEND_ON_HALO,           0,  1, 3));            // Task  6
-    tasksList.push_back(CTaskDefinition(CTaskDefinition::SUM_UP_RESIDUAL_CONTRIBUTIONS_HALO_ELEMENTS,  0,  5));               // Task  7
-    tasksList.push_back(CTaskDefinition(CTaskDefinition::INITIATE_REVERSE_MPI_COMMUNICATION,           0,  7));               // Task  8
-    tasksList.push_back(CTaskDefinition(CTaskDefinition::SURFACE_RESIDUAL_OWNED_ELEMENTS,              0,  1));               // Task  9
-    tasksList.push_back(CTaskDefinition(CTaskDefinition::BOUNDARY_CONDITIONS_DEPEND_ON_OWNED,          0,  1));               // Task 10
-    tasksList.push_back(CTaskDefinition(CTaskDefinition::COMPLETE_REVERSE_MPI_COMMUNICATION,           0,  2, 8));            // Task 11
-    tasksList.push_back(CTaskDefinition(CTaskDefinition::SUM_UP_RESIDUAL_CONTRIBUTIONS_OWNED_ELEMENTS, 0,  2, 6, 9, 10, 11)); // Task 12
-    tasksList.push_back(CTaskDefinition(CTaskDefinition::MULTIPLY_INVERSE_MASS_MATRIX,                 0, 12));               // Task 13
+    tasksList.emplace_back(CTaskDefinition::INITIATE_MPI_COMMUNICATION,                   0);                   // Task  0
+    tasksList.emplace_back(CTaskDefinition::SHOCK_CAPTURING_VISCOSITY_OWNED_ELEMENTS,     0);                   // Task  1
+    tasksList.emplace_back(CTaskDefinition::VOLUME_RESIDUAL,                              0,  1);               // Task  2
+    tasksList.emplace_back(CTaskDefinition::COMPLETE_MPI_COMMUNICATION,                   0,  0);               // Task  3
+    tasksList.emplace_back(CTaskDefinition::SHOCK_CAPTURING_VISCOSITY_HALO_ELEMENTS,      0,  3);               // Task  4
+    tasksList.emplace_back(CTaskDefinition::SURFACE_RESIDUAL_HALO_ELEMENTS,               0,  1, 4);            // Task  5
+    tasksList.emplace_back(CTaskDefinition::BOUNDARY_CONDITIONS_DEPEND_ON_HALO,           0,  1, 3);            // Task  6
+    tasksList.emplace_back(CTaskDefinition::SUM_UP_RESIDUAL_CONTRIBUTIONS_HALO_ELEMENTS,  0,  5);               // Task  7
+    tasksList.emplace_back(CTaskDefinition::INITIATE_REVERSE_MPI_COMMUNICATION,           0,  7);               // Task  8
+    tasksList.emplace_back(CTaskDefinition::SURFACE_RESIDUAL_OWNED_ELEMENTS,              0,  1);               // Task  9
+    tasksList.emplace_back(CTaskDefinition::BOUNDARY_CONDITIONS_DEPEND_ON_OWNED,          0,  1);               // Task 10
+    tasksList.emplace_back(CTaskDefinition::COMPLETE_REVERSE_MPI_COMMUNICATION,           0,  2, 8);            // Task 11
+    tasksList.emplace_back(CTaskDefinition::SUM_UP_RESIDUAL_CONTRIBUTIONS_OWNED_ELEMENTS, 0,  2, 6, 9, 10, 11); // Task 12
+    tasksList.emplace_back(CTaskDefinition::MULTIPLY_INVERSE_MASS_MATRIX,                 0, 12);               // Task 13
   }
 }
 
@@ -2622,14 +2624,14 @@ void CFEM_DG_EulerSolver::Prepare_MPI_Communication(const CMeshFEM *FEMGeometry,
        for this time level. Self communication is excluded. */
     int nRankRecv = 0;
     for(unsigned long i=0; i<ranksRecv.size(); ++i) {
-      if((ranksRecv[i] != rank) && elemRecvPerTimeLevel[level][i].size()) ++nRankRecv;
+      if((ranksRecv[i] != rank) && !elemRecvPerTimeLevel[level][i].empty()) ++nRankRecv;
     }
 
     /* Determine the number of ranks to which data will be send
        for this time level. Self communication is excluded. */
     int nRankSend = 0;
     for(unsigned long i=0; i<ranksSend.size(); ++i) {
-      if((ranksSend[i] != rank) && elemSendPerTimeLevel[level][i].size()) ++nRankSend;
+      if((ranksSend[i] != rank) && !elemSendPerTimeLevel[level][i].empty()) ++nRankSend;
     }
 
     /* Allocate the memory for the second index of the vectors that
@@ -2645,7 +2647,7 @@ void CFEM_DG_EulerSolver::Prepare_MPI_Communication(const CMeshFEM *FEMGeometry,
     /* Determine the receive information. */
     nRankRecv = 0;
     for(unsigned long i=0; i<ranksRecv.size(); ++i) {
-      if((ranksRecv[i] != rank) && elemRecvPerTimeLevel[level][i].size()) {
+      if((ranksRecv[i] != rank) && !elemRecvPerTimeLevel[level][i].empty()) {
 
         /* Copy the elements to be received and the rank from where they come. */
         elementsRecvMPIComm[level][nRankRecv] = elemRecvPerTimeLevel[level][i];
@@ -2669,7 +2671,7 @@ void CFEM_DG_EulerSolver::Prepare_MPI_Communication(const CMeshFEM *FEMGeometry,
     /* Determine the send information. */
     nRankSend = 0;
     for(unsigned long i=0; i<ranksSend.size(); ++i) {
-      if((ranksSend[i] != rank) && elemSendPerTimeLevel[level][i].size()) {
+      if((ranksSend[i] != rank) && !elemSendPerTimeLevel[level][i].empty()) {
 
         /* Copy the elements to be sent and the rank to where they are sent. */
         elementsSendMPIComm[level][nRankSend] = elemSendPerTimeLevel[level][i];
@@ -2754,7 +2756,7 @@ void CFEM_DG_EulerSolver::Initiate_MPI_Communication(CConfig *config,
 #ifdef HAVE_MPI
 
   /* Check if there is anything to communicate. */
-  if( commRequests[timeLevel].size() ) {
+  if( !commRequests[timeLevel].empty() ) {
 
     /* Set the pointer to the memory, whose data must be communicated.
        This depends on the time integration scheme used. For ADER the data of
@@ -2842,7 +2844,7 @@ bool CFEM_DG_EulerSolver::Complete_MPI_Communication(CConfig *config,
   /*-----------------------------------------------------------------------*/
 
 #ifdef HAVE_MPI
-  if( commRequests[timeLevel].size() ) {
+  if( !commRequests[timeLevel].empty() ) {
 
     /*--- There are communication requests to be completed. Check if these
           requests must be completed. In that case Waitall is used.
@@ -3017,7 +3019,7 @@ void CFEM_DG_EulerSolver::Initiate_MPI_ReverseCommunication(CConfig *config,
 #ifdef HAVE_MPI
 
   /* Check if there is anything to communicate. */
-  if( commRequests[timeLevel].size() ) {
+  if( !commRequests[timeLevel].empty() ) {
 
     /* Loop over the number of ranks from which this rank receives data in
        the original communication pattern. In the reverse pattern, data
@@ -3077,7 +3079,7 @@ bool CFEM_DG_EulerSolver::Complete_MPI_ReverseCommunication(CConfig *config,
   /*-----------------------------------------------------------------------*/
 
   /* Check if there are any requests to complete for this time level. */
-  if( commRequests[timeLevel].size() ) {
+  if( !commRequests[timeLevel].empty() ) {
 
     /*--- There are communication requests to be completed. Check if these
           requests must be completed. In that case Waitall is used.
@@ -4155,7 +4157,7 @@ void CFEM_DG_EulerSolver::ADER_SpaceTimeIntegration(CGeometry *geometry,  CSolve
   Postprocessing(geometry, solver_container, config, iMesh);
 }
 
-void CFEM_DG_EulerSolver::TolerancesADERPredictorStep(void) {
+void CFEM_DG_EulerSolver::TolerancesADERPredictorStep() {
 
   /* Determine the maximum values of the conservative variables of the
      locally stored DOFs. Make a distinction between 2D and 3D for
@@ -6734,7 +6736,7 @@ void CFEM_DG_EulerSolver::MultiplyResidualByInverseMassMatrix(
        that the test is performed with the lumpedMassMatrix and not with
        massMatrix. The reason is that for implicit time stepping schemes
        both arrays may be in use. */
-    if( volElem[l].lumpedMassMatrix.size() ) {
+    if( !volElem[l].lumpedMassMatrix.empty() ) {
 
       /* Multiply the residual with the inverse of the lumped mass matrix. */
       for(unsigned short i=0; i<volElem[l].nDOFsSol; ++i) {
@@ -9497,7 +9499,7 @@ void CFEM_DG_EulerSolver::LoadRestart(CGeometry **geometry, CSolver ***solver, C
 #endif
 
   if (rbuf_NotMatching != 0)
-    SU2_MPI::Error(string("The solution file ") + restart_filename.data() +
+    SU2_MPI::Error(string("The solution file ") + restart_filename +
                    string(" doesn't match with the mesh file!\n") +
                    string("It could be empty lines at the end of the file."),
                    CURRENT_FUNCTION);
diff --git a/SU2_CFD/src/solvers/CFEM_DG_NSSolver.cpp b/SU2_CFD/src/solvers/CFEM_DG_NSSolver.cpp
index 414983c6679..a84746c83c2 100644
--- a/SU2_CFD/src/solvers/CFEM_DG_NSSolver.cpp
+++ b/SU2_CFD/src/solvers/CFEM_DG_NSSolver.cpp
@@ -29,9 +29,11 @@
 #include "../../include/solvers/CFEM_DG_NSSolver.hpp"
 #include "../../../Common/include/toolboxes/printing_toolbox.hpp"
 
-#define SIZE_ARR_NORM 8
+enum {
+SIZE_ARR_NORM = 8
+};
 
-CFEM_DG_NSSolver::CFEM_DG_NSSolver(void) : CFEM_DG_EulerSolver() {
+CFEM_DG_NSSolver::CFEM_DG_NSSolver() : CFEM_DG_EulerSolver() {
 
   /*--- Basic array initialization ---*/
   CD_Visc  = nullptr; CL_Visc  = nullptr; CSF_Visc = nullptr; CEff_Visc = nullptr;
@@ -150,7 +152,7 @@ CFEM_DG_NSSolver::CFEM_DG_NSSolver(CGeometry *geometry, CConfig *config, unsigne
   }
 }
 
-CFEM_DG_NSSolver::~CFEM_DG_NSSolver(void) {
+CFEM_DG_NSSolver::~CFEM_DG_NSSolver() {
 
         delete [] CD_Visc;
         delete [] CL_Visc;
diff --git a/SU2_CFD/src/solvers/CGradientSmoothingSolver.cpp b/SU2_CFD/src/solvers/CGradientSmoothingSolver.cpp
index 226d49962f0..09b391e8505 100644
--- a/SU2_CFD/src/solvers/CGradientSmoothingSolver.cpp
+++ b/SU2_CFD/src/solvers/CGradientSmoothingSolver.cpp
@@ -163,7 +163,7 @@ CGradientSmoothingSolver::CGradientSmoothingSolver(CGeometry *geometry, CConfig
   SolverName = "SOBOLEV";
 }
 
-CGradientSmoothingSolver::~CGradientSmoothingSolver(void) {
+CGradientSmoothingSolver::~CGradientSmoothingSolver() {
 
   delete nodes;
 
@@ -1001,7 +1001,7 @@ void CGradientSmoothingSolver::Complete_Surface_StiffMatrix(const CGeometry* geo
 
   /*--- Assembling the stiffness matrix on the design surface means the Jacobian is the identity for nodes inside the domain. ---*/
   for (unsigned long iPoint = 0ul; iPoint < geometry->GetnPointDomain(); iPoint++){
-    if (visited[iPoint]==false) {
+    if (!visited[iPoint]) {
       Jacobian.AddVal2Diag(iPoint, 1.0);
     }
   }
diff --git a/SU2_CFD/src/solvers/CIncEulerSolver.cpp b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
index 19b620825e1..e148eb731d3 100644
--- a/SU2_CFD/src/solvers/CIncEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
@@ -65,7 +65,7 @@ CIncEulerSolver::CIncEulerSolver(CGeometry *geometry, CConfig *config, unsigned
   /*--- Check for a restart file to evaluate if there is a change in the angle of attack
    before computing all the non-dimesional quantities. ---*/
 
-  if (!(!restart || (iMesh != MESH_0) || nZone > 1)) {
+  if (restart && (iMesh == MESH_0) && nZone <= 1) {
 
     /*--- Multizone problems require the number of the zone to be appended. ---*/
 
@@ -230,7 +230,7 @@ CIncEulerSolver::CIncEulerSolver(CGeometry *geometry, CConfig *config, unsigned
     SU2_MPI::Error("Oops! The CIncEulerSolver static array sizes are not large enough.", CURRENT_FUNCTION);
 }
 
-CIncEulerSolver::~CIncEulerSolver(void) {
+CIncEulerSolver::~CIncEulerSolver() {
 
   for(auto& model : FluidModel) delete model;
 }
@@ -2884,9 +2884,9 @@ void CIncEulerSolver::GetOutlet_Properties(CGeometry *geometry, CConfig *config,
 
   if (Evaluate_BC) {
 
-    su2double *Outlet_MassFlow = new su2double[config->GetnMarker_All()];
-    su2double *Outlet_Density  = new su2double[config->GetnMarker_All()];
-    su2double *Outlet_Area     = new su2double[config->GetnMarker_All()];
+    auto *Outlet_MassFlow = new su2double[config->GetnMarker_All()];
+    auto *Outlet_Density  = new su2double[config->GetnMarker_All()];
+    auto *Outlet_Area     = new su2double[config->GetnMarker_All()];
 
     /*--- Comute MassFlow, average temp, press, etc. ---*/
 
@@ -2944,13 +2944,13 @@ void CIncEulerSolver::GetOutlet_Properties(CGeometry *geometry, CConfig *config,
 
     /*--- Copy to the appropriate structure ---*/
 
-    su2double *Outlet_MassFlow_Local = new su2double[nMarker_Outlet];
-    su2double *Outlet_Density_Local  = new su2double[nMarker_Outlet];
-    su2double *Outlet_Area_Local     = new su2double[nMarker_Outlet];
+    auto *Outlet_MassFlow_Local = new su2double[nMarker_Outlet];
+    auto *Outlet_Density_Local  = new su2double[nMarker_Outlet];
+    auto *Outlet_Area_Local     = new su2double[nMarker_Outlet];
 
-    su2double *Outlet_MassFlow_Total = new su2double[nMarker_Outlet];
-    su2double *Outlet_Density_Total  = new su2double[nMarker_Outlet];
-    su2double *Outlet_Area_Total     = new su2double[nMarker_Outlet];
+    auto *Outlet_MassFlow_Total = new su2double[nMarker_Outlet];
+    auto *Outlet_Density_Total  = new su2double[nMarker_Outlet];
+    auto *Outlet_Area_Total     = new su2double[nMarker_Outlet];
 
     for (iMarker_Outlet = 0; iMarker_Outlet < nMarker_Outlet; iMarker_Outlet++) {
       Outlet_MassFlow_Local[iMarker_Outlet] = 0.0;
diff --git a/SU2_CFD/src/solvers/CMeshSolver.cpp b/SU2_CFD/src/solvers/CMeshSolver.cpp
index d9fdecb9f06..3da0b843e6b 100644
--- a/SU2_CFD/src/solvers/CMeshSolver.cpp
+++ b/SU2_CFD/src/solvers/CMeshSolver.cpp
@@ -755,7 +755,7 @@ void CMeshSolver::SetBoundaryDisplacements(CGeometry *geometry, CConfig *config,
 
 }
 
-void CMeshSolver::SetDualTime_Mesh(void){
+void CMeshSolver::SetDualTime_Mesh(){
 
   nodes->Set_Solution_time_n1();
   nodes->Set_Solution_time_n();
diff --git a/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp b/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
index c82685c752a..cea4549b09e 100644
--- a/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
@@ -65,7 +65,7 @@ CNEMOEulerSolver::CNEMOEulerSolver(CGeometry *geometry, CConfig *config,
 
   /*--- Check for a restart file to evaluate if there is a change in the AoA
   before non-dimensionalizing ---*/
-  if (!(!restart || (iMesh != MESH_0) || nZone >1 )) {
+  if (restart && (iMesh == MESH_0) && nZone <=1 ) {
 
     /*--- Modify file name for a dual-time unsteady restart ---*/
     if (dual_time) {
@@ -229,7 +229,7 @@ CNEMOEulerSolver::CNEMOEulerSolver(CGeometry *geometry, CConfig *config,
 
 }
 
-CNEMOEulerSolver::~CNEMOEulerSolver(void) {
+CNEMOEulerSolver::~CNEMOEulerSolver() {
 
   delete node_infty;
   delete FluidModel;
@@ -665,7 +665,7 @@ su2double CNEMOEulerSolver::ComputeConsistentExtrapolation(CNEMOGas *fluidmodel,
   // This block of code copies a vector to corresponding pointer.
   auto it = val_eves;
   auto& ref = fluidmodel->ComputeSpeciesEve(V[TVE_INDEX]);
-  for (auto v : ref) {
+  for (const auto& v : ref) {
     *it = v;  ++it;
   }
 
@@ -1627,12 +1627,12 @@ void CNEMOEulerSolver::BC_Inlet(CGeometry *geometry, CSolver **solver_container,
   INLET_TYPE Kind_Inlet = config->GetKind_Inlet();
   string Marker_Tag         = config->GetMarker_All_TagBound(val_marker);
 
-  su2double *U_domain = new su2double[nVar];      su2double *U_inlet = new su2double[nVar];
-  su2double *V_domain = new su2double[nPrimVar];  su2double *V_inlet = new su2double[nPrimVar];
-  su2double *Normal   = new su2double[nDim];
+  auto *U_domain = new su2double[nVar];      auto *U_inlet = new su2double[nVar];
+  auto *V_domain = new su2double[nPrimVar];  auto *V_inlet = new su2double[nPrimVar];
+  auto *Normal   = new su2double[nDim];
 
   nSpecies = config->GetnSpecies();
-  su2double *Spec_Density = new su2double[nSpecies];
+  auto *Spec_Density = new su2double[nSpecies];
   for (auto iSpecies = 0ul; iSpecies<nSpecies; iSpecies++)
     Spec_Density[iSpecies] = 0.0;               /*--- To avoid a compiler warning. ---*/
 
@@ -1895,10 +1895,10 @@ void CNEMOEulerSolver::BC_Outlet(CGeometry *geometry, CSolver **solver_container
   const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
 
   su2double *U_domain;
-  su2double *U_outlet = new su2double[nVar];
+  auto *U_outlet = new su2double[nVar];
   su2double *V_domain, *V_outlet;
-  su2double *Normal   = new su2double[nDim];
-  su2double *Ys       = new su2double[nSpecies];
+  auto *Normal   = new su2double[nDim];
+  auto *Ys       = new su2double[nSpecies];
 
   const unsigned short T_INDEX       = nodes->GetTIndex();
   const unsigned short TVE_INDEX     = nodes->GetTveIndex();
diff --git a/SU2_CFD/src/solvers/CRadP1Solver.cpp b/SU2_CFD/src/solvers/CRadP1Solver.cpp
index e1f6ef80d1f..13f6f76a1cf 100644
--- a/SU2_CFD/src/solvers/CRadP1Solver.cpp
+++ b/SU2_CFD/src/solvers/CRadP1Solver.cpp
@@ -29,7 +29,7 @@
 #include "../../include/variables/CRadP1Variable.hpp"
 #include "../../../Common/include/toolboxes/geometry_toolbox.hpp"
 
-CRadP1Solver::CRadP1Solver(void) : CRadSolver() {
+CRadP1Solver::CRadP1Solver() : CRadSolver() {
 
 }
 
@@ -130,7 +130,7 @@ CRadP1Solver::CRadP1Solver(CGeometry* geometry, CConfig *config) : CRadSolver(ge
   SolverName = "RAD";
 }
 
-CRadP1Solver::~CRadP1Solver(void) {
+CRadP1Solver::~CRadP1Solver() {
 
   delete nodes;
 
diff --git a/SU2_CFD/src/solvers/CRadSolver.cpp b/SU2_CFD/src/solvers/CRadSolver.cpp
index 5b03fa966e0..2b5451e5398 100644
--- a/SU2_CFD/src/solvers/CRadSolver.cpp
+++ b/SU2_CFD/src/solvers/CRadSolver.cpp
@@ -28,7 +28,7 @@
 #include "../../include/solvers/CRadSolver.hpp"
 #include "../../include/variables/CRadVariable.hpp"
 
-CRadSolver::CRadSolver(void) : CSolver() {
+CRadSolver::CRadSolver() : CSolver() {
 
 }
 
diff --git a/SU2_CFD/src/solvers/CSolver.cpp b/SU2_CFD/src/solvers/CSolver.cpp
index 357b43dee86..6223385e808 100644
--- a/SU2_CFD/src/solvers/CSolver.cpp
+++ b/SU2_CFD/src/solvers/CSolver.cpp
@@ -121,7 +121,7 @@ CSolver::CSolver(LINEAR_SOLVER_MODE linear_solver_mode) : System(linear_solver_m
 
 }
 
-CSolver::~CSolver(void) {
+CSolver::~CSolver() {
 
   unsigned short iVar;
 
@@ -362,12 +362,12 @@ void CSolver::InitiatePeriodicComms(CGeometry *geometry,
 
   unsigned long iPoint, msg_offset, buf_offset, iPeriodic;
 
-  su2double *Diff      = new su2double[nVar];
-  su2double *Und_Lapl  = new su2double[nVar];
-  su2double *Sol_Min   = new su2double[nPrimVarGrad];
-  su2double *Sol_Max   = new su2double[nPrimVarGrad];
-  su2double *rotPrim_i = new su2double[nPrimVar];
-  su2double *rotPrim_j = new su2double[nPrimVar];
+  auto *Diff      = new su2double[nVar];
+  auto *Und_Lapl  = new su2double[nVar];
+  auto *Sol_Min   = new su2double[nPrimVarGrad];
+  auto *Sol_Max   = new su2double[nPrimVarGrad];
+  auto *rotPrim_i = new su2double[nPrimVar];
+  auto *rotPrim_j = new su2double[nPrimVar];
 
   su2double Sensor_i = 0.0, Sensor_j = 0.0, Pressure_i, Pressure_j;
   const su2double *Coord_i, *Coord_j;
@@ -638,7 +638,7 @@ void CSolver::InitiatePeriodicComms(CGeometry *geometry,
                 /*--- Both points inside the domain, or both in the boundary ---*/
                 /*--- iPoint inside the domain, jPoint on the boundary ---*/
 
-                if (!(boundary_i && !boundary_j)) {
+                if (!boundary_i || boundary_j) {
                   if (geometry->nodes->GetDomain(iPoint)){
                     for (iVar = 0; iVar< nVar; iVar++)
                     Und_Lapl[iVar] -= Diff[iVar];
@@ -698,7 +698,7 @@ void CSolver::InitiatePeriodicComms(CGeometry *geometry,
                 /*--- Both points inside domain, or both on boundary ---*/
                 /*--- iPoint inside the domain, jPoint on the boundary ---*/
 
-                if (!(boundary_i && !boundary_j)) {
+                if (!boundary_i || boundary_j) {
                   if (geometry->nodes->GetDomain(iPoint)) {
                     Sensor_i += (Pressure_j - Pressure_i);
                     Sensor_j += (Pressure_i + Pressure_j);
@@ -1020,7 +1020,7 @@ void CSolver::CompletePeriodicComms(CGeometry *geometry,
   /*--- Status is global so all threads can see the result of Waitany. ---*/
   static SU2_MPI::Status status;
 
-  su2double *Diff = new su2double[nVar];
+  auto *Diff = new su2double[nVar];
 
   su2double Time_Step, Volume;
 
@@ -1802,7 +1802,7 @@ void CSolver::AdaptCFLNumber(CGeometry **geometry,
         unsigned long signChanges = 0;
         su2double totalChange = 0.0;
         auto prev = NonLinRes_Series.front();
-        for (auto val : NonLinRes_Series) {
+        for (const auto& val : NonLinRes_Series) {
           totalChange += val;
           signChanges += (prev > 0) ^ (val > 0);
           prev = val;
@@ -2231,7 +2231,7 @@ void CSolver::Update_Cross_Term(CConfig *config, su2passivematrix &cross_term) {
   }
 }
 
-void CSolver::SetGridVel_Gradient(CGeometry *geometry, const CConfig *config) {
+void CSolver::SetGridVel_Gradient(CGeometry *geometry, const CConfig *config) const {
 
   /// TODO: No comms needed for this gradient? The Rmatrix should be allocated somewhere.
 
@@ -2570,7 +2570,7 @@ void CSolver::SolveTypicalSectionWingModel(CGeometry *geometry, su2double Cl, su
 
 }
 
-void CSolver::Restart_OldGeometry(CGeometry *geometry, CConfig *config) {
+void CSolver::Restart_OldGeometry(CGeometry *geometry, CConfig *config) const {
 
   BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS {
 
@@ -3026,7 +3026,7 @@ void CSolver::Read_SU2_Restart_Binary(CGeometry *geometry, const CConfig *config
   /*--- Now parse the string names and load into the config class in case
    we need them for writing visualization files (SU2_SOL). ---*/
 
-  fields.push_back("Point_ID");
+  fields.emplace_back("Point_ID");
   for (auto iVar = 0u; iVar < nFields; iVar++) {
     const auto index = iVar*CGNS_STRING_SIZE;
     string field_buf("\"");
@@ -3035,7 +3035,7 @@ void CSolver::Read_SU2_Restart_Binary(CGeometry *geometry, const CConfig *config
     }
     field_buf.append(str_buf);
     field_buf.append("\"");
-    fields.push_back(field_buf.c_str());
+    fields.emplace_back(field_buf.c_str());
   }
 
   /*--- Free string buffer memory. ---*/
@@ -3321,7 +3321,7 @@ void CSolver::InterpolateRestartData(const CGeometry *geometry, const CConfig *c
   }
 }
 
-void CSolver::Read_SU2_Restart_Metadata(CGeometry *geometry, CConfig *config, bool adjoint, string val_filename) const {
+void CSolver::Read_SU2_Restart_Metadata(CGeometry *geometry, CConfig *config, bool adjoint, const string& val_filename) const {
 
   su2double AoA_ = config->GetAoA();
   su2double AoS_ = config->GetAoS();
@@ -3430,7 +3430,7 @@ void CSolver::Read_SU2_Restart_Metadata(CGeometry *geometry, CConfig *config, bo
 
   /*--- Angle of attack ---*/
 
-  if (config->GetDiscard_InFiles() == false) {
+  if (!config->GetDiscard_InFiles()) {
     if ((config->GetAoA() != AoA_) && (rank == MASTER_NODE)) {
       cout.precision(6);
       cout <<"WARNING: AoA in the solution file (" << AoA_ << " deg.) +" << endl;
@@ -3446,7 +3446,7 @@ void CSolver::Read_SU2_Restart_Metadata(CGeometry *geometry, CConfig *config, bo
 
   /*--- Sideslip angle ---*/
 
-  if (config->GetDiscard_InFiles() == false) {
+  if (!config->GetDiscard_InFiles()) {
     if ((config->GetAoS() != AoS_) && (rank == MASTER_NODE)) {
       cout.precision(6);
       cout <<"WARNING: AoS in the solution file (" << AoS_ << " deg.) +" << endl;
@@ -3461,7 +3461,7 @@ void CSolver::Read_SU2_Restart_Metadata(CGeometry *geometry, CConfig *config, bo
 
   /*--- BCThrust ---*/
 
-  if (config->GetDiscard_InFiles() == false) {
+  if (!config->GetDiscard_InFiles()) {
     if ((config->GetInitial_BCThrust() != BCThrust_) && (rank == MASTER_NODE))
       cout <<"WARNING: SU2 will use the initial BC Thrust provided in the solution file: " << BCThrust_ << " lbs." << endl;
     config->SetInitial_BCThrust(BCThrust_);
@@ -3472,7 +3472,7 @@ void CSolver::Read_SU2_Restart_Metadata(CGeometry *geometry, CConfig *config, bo
   }
 
 
-  if (config->GetDiscard_InFiles() == false) {
+  if (!config->GetDiscard_InFiles()) {
 
     if ((config->GetdCD_dCL() != dCD_dCL_) && (rank == MASTER_NODE))
       cout <<"WARNING: SU2 will use the dCD/dCL provided in the direct solution file: " << dCD_dCL_ << "." << endl;
@@ -3508,7 +3508,7 @@ void CSolver::Read_SU2_Restart_Metadata(CGeometry *geometry, CConfig *config, bo
 
   }
 
-  if (config->GetDiscard_InFiles() == false) {
+  if (!config->GetDiscard_InFiles()) {
     if ((config->GetStreamwise_Periodic_PressureDrop() != SPPressureDrop_) && (rank == MASTER_NODE))
       cout <<"WARNING: SU2 will use the STREAMWISE_PERIODIC_PRESSURE_DROP provided in the direct solution file: " << std::setprecision(16) << SPPressureDrop_ << endl;
     config->SetStreamwise_Periodic_PressureDrop(SPPressureDrop_);
@@ -3520,7 +3520,7 @@ void CSolver::Read_SU2_Restart_Metadata(CGeometry *geometry, CConfig *config, bo
 
   /*--- External iteration ---*/
 
-  if ((config->GetDiscard_InFiles() == false) && (!adjoint || (adjoint && config->GetRestart())))
+  if ((!config->GetDiscard_InFiles()) && (!adjoint || (adjoint && config->GetRestart())))
     config->SetExtIter_OffSet(InnerIter_);
 
 }
diff --git a/SU2_CFD/src/solvers/CSpeciesSolver.cpp b/SU2_CFD/src/solvers/CSpeciesSolver.cpp
index b401b162f8a..43a88edf3ea 100644
--- a/SU2_CFD/src/solvers/CSpeciesSolver.cpp
+++ b/SU2_CFD/src/solvers/CSpeciesSolver.cpp
@@ -568,7 +568,7 @@ void CSpeciesSolver::Source_Residual(CGeometry *geometry, CSolver **solver_conta
 
       numerics->SetScalarVar(nodes->GetSolution(iPoint), nullptr);
 
-      numerics->SetDiffusionCoeff(nodes->GetDiffusivity(iPoint), 0);
+      numerics->SetDiffusionCoeff(nodes->GetDiffusivity(iPoint), nullptr);
 
       /*--- Set volume of the dual cell. ---*/
 
diff --git a/SU2_CFD/src/solvers/CTemplateSolver.cpp b/SU2_CFD/src/solvers/CTemplateSolver.cpp
index 133e441cd03..df2dd61085e 100644
--- a/SU2_CFD/src/solvers/CTemplateSolver.cpp
+++ b/SU2_CFD/src/solvers/CTemplateSolver.cpp
@@ -28,11 +28,11 @@
 
 #include "../../include/solvers/CTemplateSolver.hpp"
 
-CTemplateSolver::CTemplateSolver(void) : CSolver() { }
+CTemplateSolver::CTemplateSolver() : CSolver() { }
 
 CTemplateSolver::CTemplateSolver(CGeometry *geometry, CConfig *config) : CSolver() { }
 
-CTemplateSolver::~CTemplateSolver(void) { }
+CTemplateSolver::~CTemplateSolver() = default;
 
 void CTemplateSolver::Preprocessing(CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, unsigned short iRKStep, unsigned short RunTime_EqSystem, bool Output) { }
 
diff --git a/SU2_CFD/src/variables/CMeshElement.cpp b/SU2_CFD/src/variables/CMeshElement.cpp
index f0ddf7ab66b..f7eb725d329 100644
--- a/SU2_CFD/src/variables/CMeshElement.cpp
+++ b/SU2_CFD/src/variables/CMeshElement.cpp
@@ -28,7 +28,7 @@
 
 #include "../../include/variables/CMeshElement.hpp"
 
-CMeshElement::CMeshElement(void){
+CMeshElement::CMeshElement(){
 
   Ref_Volume = 1.0;           /*!< \brief Store the reference volume of the element. */
   Curr_Volume = 1.0;          /*!< \brief Store the current volume of the element. */
diff --git a/SU2_CFD/src/variables/CNEMOEulerVariable.cpp b/SU2_CFD/src/variables/CNEMOEulerVariable.cpp
index 268219fec5a..2c448786a29 100644
--- a/SU2_CFD/src/variables/CNEMOEulerVariable.cpp
+++ b/SU2_CFD/src/variables/CNEMOEulerVariable.cpp
@@ -26,7 +26,7 @@
  */
 
 #include "../../include/variables/CNEMOEulerVariable.hpp"
-#include <math.h>
+#include <cmath>
 
 CNEMOEulerVariable::CNEMOEulerVariable(su2double val_pressure,
                                        const su2double *val_massfrac,
diff --git a/SU2_CFD/src/variables/CNEMONSVariable.cpp b/SU2_CFD/src/variables/CNEMONSVariable.cpp
index d0f09b4bf65..05341d2b02a 100644
--- a/SU2_CFD/src/variables/CNEMONSVariable.cpp
+++ b/SU2_CFD/src/variables/CNEMONSVariable.cpp
@@ -26,7 +26,7 @@
  */
 
 #include "../../include/variables/CNEMONSVariable.hpp"
-#include <math.h>
+#include <cmath>
 
 CNEMONSVariable::CNEMONSVariable(su2double val_pressure,
                                  const su2double *val_massfrac,
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 7f40c2d8c9c..7de363a4431 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -568,7 +568,7 @@ void CDeformationDriver::Finalize() {
     cout << "\n------------------------- Exit Success (SU2_DEF) ------------------------" << endl << endl;
 }
 
-void CDeformationDriver::CommunicateMeshDisplacements(void) {
+void CDeformationDriver::CommunicateMeshDisplacements() {
   solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->InitiateComms(geometry_container[ZONE_0][INST_0][MESH_0],
                                                                     config_container[ZONE_0], MESH_DISPLACEMENTS);
   solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->CompleteComms(geometry_container[ZONE_0][INST_0][MESH_0],
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index 087e5d04376..3c4963a3d12 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -213,7 +213,7 @@ void CDiscAdjDeformationDriver::Geometrical_Preprocessing() {
         /*--- Carry out a dynamic cast to CMeshFEM_DG, such that it is not needed to
          * define all virtual functions in the base class CGeometry. ---*/
 
-        CMeshFEM_DG* DGMesh = dynamic_cast<CMeshFEM_DG*>(geometry_container[iZone][iInst][MESH_0]);
+        auto* DGMesh = dynamic_cast<CMeshFEM_DG*>(geometry_container[iZone][iInst][MESH_0]);
 
         /*--- Determine the standard elements for the volume elements. ---*/
 
@@ -767,7 +767,7 @@ void CDiscAdjDeformationDriver::OutputGradient(su2double** Gradient, CConfig* co
       /*--- Print the kind of design variable on screen. ---*/
 
       cout << endl << "Design variable (";
-      for (std::map<string, ENUM_PARAM>::const_iterator it = Param_Map.begin(); it != Param_Map.end(); ++it) {
+      for (auto it = Param_Map.begin(); it != Param_Map.end(); ++it) {
         if (it->second == config->GetDesign_Variable(iDV)) {
           cout << it->first << ") number " << iDV << "." << endl;
         }
@@ -775,8 +775,7 @@ void CDiscAdjDeformationDriver::OutputGradient(su2double** Gradient, CConfig* co
 
       /*--- Print the kind of objective function to screen. ---*/
 
-      for (std::map<string, ENUM_OBJECTIVE>::const_iterator it = Objective_Map.begin(); it != Objective_Map.end();
-           ++it) {
+      for (auto it = Objective_Map.begin(); it != Objective_Map.end(); ++it) {
         if (it->second == config->GetKind_ObjFunc()) {
           cout << it->first << " gradient : ";
           if (iDV == 0) Gradient_file << it->first << " gradient " << endl;
@@ -818,18 +817,18 @@ void CDiscAdjDeformationDriver::SetSensitivity_Files(CGeometry**** geometry, CCo
     /*--- We create a baseline solver to easily merge the sensitivity information. ---*/
 
     vector<string> fieldnames;
-    fieldnames.push_back("\"Point\"");
-    fieldnames.push_back("\"x\"");
-    fieldnames.push_back("\"y\"");
+    fieldnames.emplace_back("\"Point\"");
+    fieldnames.emplace_back("\"x\"");
+    fieldnames.emplace_back("\"y\"");
     if (nDim == 3) {
-      fieldnames.push_back("\"z\"");
+      fieldnames.emplace_back("\"z\"");
     }
-    fieldnames.push_back("\"Sensitivity_x\"");
-    fieldnames.push_back("\"Sensitivity_y\"");
+    fieldnames.emplace_back("\"Sensitivity_x\"");
+    fieldnames.emplace_back("\"Sensitivity_y\"");
     if (nDim == 3) {
-      fieldnames.push_back("\"Sensitivity_z\"");
+      fieldnames.emplace_back("\"Sensitivity_z\"");
     }
-    fieldnames.push_back("\"Surface_Sensitivity\"");
+    fieldnames.emplace_back("\"Surface_Sensitivity\"");
 
     solver = new CBaselineSolver(geometry[iZone][INST_0][MESH_0], config[iZone], nVar + nDim, fieldnames);
 
diff --git a/SU2_GEO/src/SU2_GEO.cpp b/SU2_GEO/src/SU2_GEO.cpp
index 78ce7faeb54..eb0cb5c151e 100644
--- a/SU2_GEO/src/SU2_GEO.cpp
+++ b/SU2_GEO/src/SU2_GEO.cpp
@@ -612,7 +612,7 @@ int main(int argc, char* argv[]) {
 
     /*--- Write the objective function in a external file ---*/
     string filename = config_container[ZONE_0]->GetObjFunc_Value_FileName();
-    unsigned short lastindex = filename.find_last_of(".");
+    unsigned short lastindex = filename.find_last_of('.');
     filename = filename.substr(0, lastindex);
     if (tabTecplot)
       filename += ".dat";
@@ -730,7 +730,7 @@ int main(int argc, char* argv[]) {
     /*--- Write the gradient in a external file ---*/
     if (rank == MASTER_NODE) {
       string filename = config_container[ZONE_0]->GetObjFunc_Grad_FileName();
-      unsigned short lastindex = filename.find_last_of(".");
+      unsigned short lastindex = filename.find_last_of('.');
       filename = filename.substr(0, lastindex);
       if (tabTecplot)
         filename += ".dat";
diff --git a/SU2_SOL/src/SU2_SOL.cpp b/SU2_SOL/src/SU2_SOL.cpp
index 1d8aa6093b9..a68498b0e07 100644
--- a/SU2_SOL/src/SU2_SOL.cpp
+++ b/SU2_SOL/src/SU2_SOL.cpp
@@ -199,7 +199,7 @@ int main(int argc, char* argv[]) {
       if (fem_solver) {
         /*--- Carry out a dynamic cast to CMeshFEM_DG, such that it is not needed to
          define all virtual functions in the base class CGeometry. ---*/
-        CMeshFEM_DG* DGMesh = dynamic_cast<CMeshFEM_DG*>(geometry_container[iZone][iInst]);
+        auto* DGMesh = dynamic_cast<CMeshFEM_DG*>(geometry_container[iZone][iInst]);
 
         /*--- Determine the standard elements for the volume elements. ---*/
         if (rank == MASTER_NODE) cout << "Creating standard volume elements." << endl;
@@ -341,8 +341,8 @@ int main(int argc, char* argv[]) {
 
       if (((TimeIter + 1 == config_container[ZONE_0]->GetnTime_Iter()) ||
            ((TimeIter % config_container[ZONE_0]->GetVolumeOutputFrequency(0) == 0) && (TimeIter != 0) &&
-            !((config_container[ZONE_0]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
-              (config_container[ZONE_0]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND))) ||
+            (config_container[ZONE_0]->GetTime_Marching() != TIME_MARCHING::DT_STEPPING_1ST) &&
+            (config_container[ZONE_0]->GetTime_Marching() != TIME_MARCHING::DT_STEPPING_2ND)) ||
            (StopCalc) ||
            (((config_container[ZONE_0]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
              (config_container[ZONE_0]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND)) &&
@@ -363,7 +363,7 @@ int main(int argc, char* argv[]) {
 
         /*--- For the fluid zone (ZONE_0) ---*/
         /*--- Either instantiate the solution class or load a restart file. ---*/
-        if (SolutionInstantiatedFlow == false &&
+        if (!SolutionInstantiatedFlow &&
             (TimeIter == 0 ||
              ((config_container[ZONE_0]->GetRestart() &&
                (SU2_TYPE::Int(TimeIter) == SU2_TYPE::Int(config_container[ZONE_0]->GetRestart_Iter()))) ||
@@ -384,7 +384,7 @@ int main(int argc, char* argv[]) {
         /*--- For the structural zone (ZONE_1) ---*/
         /*--- Either instantiate the solution class or load a restart file. ---*/
         /*--- Either instantiate the solution class or load a restart file. ---*/
-        if (SolutionInstantiatedFEM == false &&
+        if (!SolutionInstantiatedFEM &&
             (TimeIter == 0 ||
              ((config_container[ZONE_1]->GetRestart() &&
                (SU2_TYPE::Int(TimeIter) == SU2_TYPE::Int(config_container[ZONE_1]->GetRestart_Iter()))) ||
@@ -445,7 +445,7 @@ int main(int argc, char* argv[]) {
             config_container[iZone]->SetTimeIter(TimeIter);
 
             /*--- Either instantiate the solution class or load a restart file. ---*/
-            if (SolutionInstantiated[iZone] == false &&
+            if (!SolutionInstantiated[iZone] &&
                 (TimeIter == 0 || (config_container[ZONE_0]->GetRestart() &&
                                    ((long)TimeIter == SU2_TYPE::Int(config_container[ZONE_0]->GetRestart_Iter()) ||
                                     TimeIter % config_container[ZONE_0]->GetVolumeOutputFrequency(0) == 0 ||
@@ -521,8 +521,8 @@ int main(int argc, char* argv[]) {
 
         if ((TimeIter + 1 == config_container[ZONE_0]->GetnTime_Iter()) ||
             ((TimeIter % config_container[ZONE_0]->GetVolumeOutputFrequency(0) == 0) && (TimeIter != 0) &&
-             !((config_container[ZONE_0]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
-               (config_container[ZONE_0]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND))) ||
+             (config_container[ZONE_0]->GetTime_Marching() != TIME_MARCHING::DT_STEPPING_1ST) &&
+             (config_container[ZONE_0]->GetTime_Marching() != TIME_MARCHING::DT_STEPPING_2ND)) ||
             (StopCalc) ||
             (((config_container[ZONE_0]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
               (config_container[ZONE_0]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND)) &&
@@ -533,7 +533,7 @@ int main(int argc, char* argv[]) {
             config_container[iZone]->SetTimeIter(TimeIter);
 
             /*--- Either instantiate the solution class or load a restart file. ---*/
-            if (SolutionInstantiated[iZone] == false &&
+            if (!SolutionInstantiated[iZone] &&
                 (TimeIter == 0 || (config_container[ZONE_0]->GetRestart() &&
                                    ((long)TimeIter == SU2_TYPE::Int(config_container[ZONE_0]->GetRestart_Iter()) ||
                                     TimeIter % config_container[ZONE_0]->GetVolumeOutputFrequency(0) == 0 ||
@@ -626,7 +626,7 @@ int main(int argc, char* argv[]) {
           /*--- Read in the restart file for this time step ---*/
           for (iZone = 0; iZone < nZone; iZone++) {
             /*--- Either instantiate the solution class or load a restart file. ---*/
-            if (SolutionInstantiated == false &&
+            if (!SolutionInstantiated &&
                 (TimeIter == 0 ||
                  ((config_container[ZONE_0]->GetRestart() &&
                    (SU2_TYPE::Int(TimeIter) == SU2_TYPE::Int(config_container[ZONE_0]->GetRestart_Iter()))) ||

From 23283bbc0663b4c7a06678fe9e4b5b409b58b87b Mon Sep 17 00:00:00 2001
From: Kursat Yurt <kursatyurt@gmail.com>
Date: Fri, 31 Mar 2023 16:55:12 +0200
Subject: [PATCH 334/656] Revert false flags

---
 Common/include/geometry/CGeometry.hpp         | 14 ++++++-------
 .../include/grid_movement/CFreeFormDefBox.hpp | 20 +++++++++----------
 Common/src/geometry/CGeometry.cpp             | 16 +++++++--------
 3 files changed, 25 insertions(+), 25 deletions(-)

diff --git a/Common/include/geometry/CGeometry.hpp b/Common/include/geometry/CGeometry.hpp
index 2822d430072..fa9fc53cd60 100644
--- a/Common/include/geometry/CGeometry.hpp
+++ b/Common/include/geometry/CGeometry.hpp
@@ -405,7 +405,7 @@ class CGeometry {
    * \param[in] countPerPeriodicPoint - Number of variables per point.
    */
   void PostPeriodicRecvs(CGeometry* geometry, const CConfig* config, unsigned short commType,
-                         unsigned short countPerPeriodicPoint) const;
+                         unsigned short countPerPeriodicPoint);
 
   /*!
    * \brief Routine to launch a single non-blocking send once the buffer is loaded for a periodic commucation.
@@ -959,33 +959,33 @@ class CGeometry {
    * \param[in] config - Definition of the particular problem.
    * \param[in] print - Display information on screen.
    */
-  void SetRotationalVelocity(const CConfig* config, bool print = false) const;
+  void SetRotationalVelocity(const CConfig* config, bool print = false);
 
   /*!
    * \brief Set the rotational velocity of the points on the shroud markers to 0.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetShroudVelocity(const CConfig* config) const;
+  void SetShroudVelocity(const CConfig* config);
 
   /*!
    * \brief Set the translational velocity at each node.
    * \param[in] config - Definition of the particular problem.
    * \param[in] print - Display information on screen.
    */
-  void SetTranslationalVelocity(const CConfig* config, bool print = false) const;
+  void SetTranslationalVelocity(const CConfig* config, bool print = false);
 
   /*!
    * \brief Set the translational/rotational velocity for all moving walls.
    * \param[in] config - Definition of the particular problem.
    * \param[in] print - Display information on screen.
    */
-  void SetWallVelocity(const CConfig* config, bool print = false) const;
+  void SetWallVelocity(const CConfig* config, bool print = false);
 
   /*!
    * \brief Set the grid velocity via finite differencing at each node.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetGridVelocity(const CConfig* config) const;
+  void SetGridVelocity(const CConfig* config);
 
   /*!
    * \brief A virtual member.
@@ -1020,7 +1020,7 @@ class CGeometry {
    * \brief Find and store all vertices on a sharp corner in the geometry.
    * \param[in] config - Definition of the particular problem.
    */
-  void ComputeSurf_Curvature(CConfig* config) const;
+  void ComputeSurf_Curvature(CConfig* config);
 
   /*!
    * \brief A virtual member.
diff --git a/Common/include/grid_movement/CFreeFormDefBox.hpp b/Common/include/grid_movement/CFreeFormDefBox.hpp
index 30aa1ae17f0..87ff31993a6 100644
--- a/Common/include/grid_movement/CFreeFormDefBox.hpp
+++ b/Common/include/grid_movement/CFreeFormDefBox.hpp
@@ -292,7 +292,7 @@ class CFreeFormDefBox : public CGridMovement {
    *        and find the position of the control points for the FFDBox
    * \param[in] FFDBox - Original FFDBox where we want to compute the control points.
    */
-  void SetSupportCPChange(CFreeFormDefBox* FFDBox) const;
+  void SetSupportCPChange(CFreeFormDefBox* FFDBox);
 
   /*!
    * \brief Set the number of corner points.
@@ -439,7 +439,7 @@ class CFreeFormDefBox : public CGridMovement {
   /*!
    * \brief Set the control points in a parallelepiped (hexahedron).
    */
-  void SetControlPoints_Parallelepiped(void) const;
+  void SetControlPoints_Parallelepiped(void);
 
   /*!
    * \brief Set the control points of the final chuck in a unitary hexahedron free form.
@@ -502,49 +502,49 @@ class CFreeFormDefBox : public CGridMovement {
    * \brief Set Cylindrical to Cartesians_ControlPoints.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetCyl2Cart_ControlPoints(CConfig* config) const;
+  void SetCyl2Cart_ControlPoints(CConfig* config);
 
   /*!
    * \brief Set Cartesians to Cylindrical ControlPoints.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetCart2Cyl_ControlPoints(CConfig* config) const;
+  void SetCart2Cyl_ControlPoints(CConfig* config);
 
   /*!
    * \brief Set Cylindrical to Cartesians_CornerPoints.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetCyl2Cart_CornerPoints(CConfig* config) const;
+  void SetCyl2Cart_CornerPoints(CConfig* config);
 
   /*!
    * \brief Set Cartesians to Cylindrical CornerPoints.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetCart2Cyl_CornerPoints(CConfig* config) const;
+  void SetCart2Cyl_CornerPoints(CConfig* config);
 
   /*!
    * \brief Set Spherical to Cartesians ControlPoints.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetSphe2Cart_ControlPoints(CConfig* config) const;
+  void SetSphe2Cart_ControlPoints(CConfig* config);
 
   /*!
    * \brief SetCartesians to Spherical ControlPoints.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetCart2Sphe_ControlPoints(CConfig* config) const;
+  void SetCart2Sphe_ControlPoints(CConfig* config);
 
   /*!
    * \brief Set Spherical to Cartesians_CornerPoints.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetSphe2Cart_CornerPoints(CConfig* config) const;
+  void SetSphe2Cart_CornerPoints(CConfig* config);
 
   /*!
    * \brief Set Cartesians to Spherical Corner Points.
    * \param[in] config - Definition of the particular problem.
    */
-  void SetCart2Sphe_CornerPoints(CConfig* config) const;
+  void SetCart2Sphe_CornerPoints(CConfig* config);
 
   /*!
    * \brief Set the cartesian coords of a point in R^3 and convert them to the parametric coords of
diff --git a/Common/src/geometry/CGeometry.cpp b/Common/src/geometry/CGeometry.cpp
index c678147097b..7f4626e4f98 100644
--- a/Common/src/geometry/CGeometry.cpp
+++ b/Common/src/geometry/CGeometry.cpp
@@ -1128,7 +1128,7 @@ void CGeometry::AllocatePeriodicComms(unsigned short countPerPeriodicPoint) {
 }
 
 void CGeometry::PostPeriodicRecvs(CGeometry* geometry, const CConfig* config, unsigned short commType,
-                                  unsigned short countPerPeriodicPoint) const {
+                                  unsigned short countPerPeriodicPoint) {
   /*--- In parallel, communicate the data with non-blocking send/recv. ---*/
 
 #ifdef HAVE_MPI
@@ -2600,7 +2600,7 @@ void CGeometry::ComputeSurf_Straightness(CConfig* config, bool print_on_screen)
   }        // if print_on_scren
 }
 
-void CGeometry::ComputeSurf_Curvature(CConfig* config) const {
+void CGeometry::ComputeSurf_Curvature(CConfig* config) {
   unsigned short iMarker, iNeigh_Point, iDim, iNode, iNeighbor_Nodes, Neighbor_Node;
   unsigned long Neighbor_Point, iVertex, iPoint, jPoint, iElem_Bound, iEdge, nLocalVertex, MaxLocalVertex,
       *Buffer_Send_nVertex, *Buffer_Receive_nVertex, TotalnPointDomain;
@@ -3352,7 +3352,7 @@ bool CGeometry::GetRadialNeighbourhood(const unsigned long iElem_global, const p
   return finished;
 }
 
-void CGeometry::SetElemVolume() const {
+void CGeometry::SetElemVolume() {
   SU2_OMP_PARALLEL {
     /*--- Create a bank of elements to avoid instantiating inside loop. ---*/
     CElement* elements[4] = {nullptr, nullptr, nullptr, nullptr};
@@ -3420,7 +3420,7 @@ void CGeometry::SetElemVolume() const {
   END_SU2_OMP_PARALLEL
 }
 
-void CGeometry::SetRotationalVelocity(const CConfig* config, bool print) const {
+void CGeometry::SetRotationalVelocity(const CConfig* config, bool print) {
   unsigned long iPoint;
   unsigned short iDim;
 
@@ -3471,7 +3471,7 @@ void CGeometry::SetRotationalVelocity(const CConfig* config, bool print) const {
   }
 }
 
-void CGeometry::SetShroudVelocity(const CConfig* config) const {
+void CGeometry::SetShroudVelocity(const CConfig* config) {
   unsigned long iPoint, iVertex;
   unsigned short iMarker, iMarkerShroud;
   su2double RotVel[3] = {0.0, 0.0, 0.0};
@@ -3489,7 +3489,7 @@ void CGeometry::SetShroudVelocity(const CConfig* config) const {
   }
 }
 
-void CGeometry::SetTranslationalVelocity(const CConfig* config, bool print) const {
+void CGeometry::SetTranslationalVelocity(const CConfig* config, bool print) {
   su2double xDot[3] = {0.0, 0.0, 0.0};
 
   /*--- Get the translational velocity vector from config ---*/
@@ -3508,7 +3508,7 @@ void CGeometry::SetTranslationalVelocity(const CConfig* config, bool print) cons
   for (unsigned long iPoint = 0; iPoint < nPoint; iPoint++) nodes->SetGridVel(iPoint, xDot);
 }
 
-void CGeometry::SetWallVelocity(const CConfig* config, bool print) const {
+void CGeometry::SetWallVelocity(const CConfig* config, bool print) {
   const su2double L_Ref = config->GetLength_Ref();
   const su2double Omega_Ref = config->GetOmega_Ref();
   const su2double Vel_Ref = config->GetVelocity_Ref();
@@ -3567,7 +3567,7 @@ void CGeometry::SetWallVelocity(const CConfig* config, bool print) const {
   }
 }
 
-void CGeometry::SetGridVelocity(const CConfig* config) const {
+void CGeometry::SetGridVelocity(const CConfig* config) {
   /*--- Get timestep and whether to use 1st or 2nd order backward finite differences ---*/
 
   bool FirstOrder = (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST);

From cb1c3d1e7c3c738ef9f06aa3dbc3ed340a85aaf3 Mon Sep 17 00:00:00 2001
From: Kursat Yurt <kursatyurt@gmail.com>
Date: Fri, 31 Mar 2023 16:58:08 +0200
Subject: [PATCH 335/656] Revert false flags-2

---
 SU2_CFD/include/numerics/CNumerics.hpp | 2 +-
 SU2_CFD/src/numerics/CNumerics.cpp     | 4 ++--
 2 files changed, 3 insertions(+), 3 deletions(-)

diff --git a/SU2_CFD/include/numerics/CNumerics.hpp b/SU2_CFD/include/numerics/CNumerics.hpp
index 9483f4c4979..e8682cc8da5 100644
--- a/SU2_CFD/include/numerics/CNumerics.hpp
+++ b/SU2_CFD/include/numerics/CNumerics.hpp
@@ -1520,7 +1520,7 @@ class CNumerics {
    * \brief Computes a basis of orthogonal vectors from a supplied vector
    * \param[in] config - Normal vector
    */
-  void CreateBasis(const su2double *val_Normal, su2double* l, su2double* m) const;
+  void CreateBasis(const su2double *val_Normal, su2double* l, su2double* m);
 
   /*!
    * \brief Set the value of the Tauwall
diff --git a/SU2_CFD/src/numerics/CNumerics.cpp b/SU2_CFD/src/numerics/CNumerics.cpp
index ed3a3c3e90d..082eceffb22 100644
--- a/SU2_CFD/src/numerics/CNumerics.cpp
+++ b/SU2_CFD/src/numerics/CNumerics.cpp
@@ -31,7 +31,7 @@
 #include "../../include/numerics/CNumerics.hpp"
 #include "../../include/fluid/CFluidModel.hpp"
 
-CNumerics::CNumerics() {
+CNumerics::CNumerics(void) {
 
   Proj_Flux_Tensor  = nullptr;
 
@@ -75,7 +75,7 @@ CNumerics::CNumerics(unsigned short val_nDim, unsigned short val_nVar,
 
 }
 
-CNumerics::~CNumerics() {
+CNumerics::~CNumerics(void) {
 
   // visc
   delete [] Proj_Flux_Tensor;

From 822b092f6c15dad2e28f9b6b81d921afea91a4cd Mon Sep 17 00:00:00 2001
From: Kursat Yurt <kursatyurt@gmail.com>
Date: Fri, 31 Mar 2023 17:15:50 +0200
Subject: [PATCH 336/656] Add tidy file to repo

---
 .clang-tidy                                  |  5 +++++
 Common/include/geometry/CGeometry.hpp        |  8 ++++----
 Common/src/grid_movement/CFreeFormDefBox.cpp | 20 ++++++++++----------
 SU2_CFD/src/numerics/CNumerics.cpp           |  2 +-
 4 files changed, 20 insertions(+), 15 deletions(-)
 create mode 100644 .clang-tidy

diff --git a/.clang-tidy b/.clang-tidy
new file mode 100644
index 00000000000..397fec948e8
--- /dev/null
+++ b/.clang-tidy
@@ -0,0 +1,5 @@
+Checks: '-*,modernize-avoid-bind,modernize-deprecated-headers,modernize-deprecated-ios-base-aliases,modernize-macro-to-enum,modernize-pass-by-value,modernize-raw-string-literal,modernize-redundant-void-arg,modernize-replace-auto-ptr,modernize-replace-disallow-copy-and-assign-macro,modernize-replace-random-shuffle,modernize-return-braced-init-list,modernize-shrink-to-fit,modernize-unary-static-assert,modernize-use-auto,modernize-use-bool-literals,modernize-use-default-member-init,modernize-use-emplace,modernize-use-equals-default,modernize-use-equals-delete,modernize-use-noexcept,modernize-use-nullptr,modernize-use-override,modernize-use-transparent-functors,modernize-use-using,readability-const-return-type,readability-avoid-const-params-in-decls,readability-container-data-pointer,readability-container-size-empty,readability-delete-null-pointer,readability-duplicate-include,readability-non-const-parameter,readability-redundant-access-specifiers,readability-redundant-control-flow,readability-redundant-declaration,readability-redundant-function-ptr-dereference,readability-redundant-smartptr-get,readability-redundant-string-cstr,readability-redundant-string-init,readability-simplify-boolean-expr,readability-simplify-subscript-expr,performance-*'
+CheckOptions:
+  - {key: modernize-use-override.AllowOverrideAndFinal, value: 'true'}
+  - {key: performance-unnecessary-copy-initialization.AllowedTypes, value: 'su2double'}
+  - {key: performance-unnecessary-value-param.AllowedTypes, value: 'su2double'}
diff --git a/Common/include/geometry/CGeometry.hpp b/Common/include/geometry/CGeometry.hpp
index fa9fc53cd60..22280ddf04f 100644
--- a/Common/include/geometry/CGeometry.hpp
+++ b/Common/include/geometry/CGeometry.hpp
@@ -45,9 +45,9 @@ extern "C" {
 #include <sstream>
 #include <cmath>
 #include <algorithm>
-#include <string.h>
-#include <stdio.h>
-#include <stdlib.h>
+#include <cstring>
+#include <cstdio>
+#include <cstdlib>
 #include <climits>
 #include <memory>
 #include <unordered_map>
@@ -1678,7 +1678,7 @@ class CGeometry {
   /*!
    * \brief Compute and store the volume of the primal elements.
    */
-  void SetElemVolume() const;
+  void SetElemVolume();
 
   /*!
    * \brief Set the multigrid index for the current geometry object.
diff --git a/Common/src/grid_movement/CFreeFormDefBox.cpp b/Common/src/grid_movement/CFreeFormDefBox.cpp
index f1540771192..2872b22aebd 100644
--- a/Common/src/grid_movement/CFreeFormDefBox.cpp
+++ b/Common/src/grid_movement/CFreeFormDefBox.cpp
@@ -191,7 +191,7 @@ void CFreeFormDefBox::SetUnitCornerPoints() {
   delete[] coord;
 }
 
-void CFreeFormDefBox::SetControlPoints_Parallelepiped() const {
+void CFreeFormDefBox::SetControlPoints_Parallelepiped() {
   unsigned short iDim, iDegree, jDegree, kDegree;
 
   /*--- Set base control points according to the notation of Vtk for hexahedrons ---*/
@@ -265,7 +265,7 @@ void CFreeFormDefBox::SetSupportCP(CFreeFormDefBox* FFDBox) {
       }
 }
 
-void CFreeFormDefBox::SetSupportCPChange(CFreeFormDefBox* FFDBox) const {
+void CFreeFormDefBox::SetSupportCPChange(CFreeFormDefBox* FFDBox) {
   unsigned short iDim, iOrder, jOrder, kOrder;
   su2double *CartCoordNew, *ParamCoord;
   unsigned short lOrder = FFDBox->GetlOrder();
@@ -310,7 +310,7 @@ void CFreeFormDefBox::SetSupportCPChange(CFreeFormDefBox* FFDBox) const {
   }
 }
 
-void CFreeFormDefBox::SetCart2Cyl_ControlPoints(CConfig* config) const {
+void CFreeFormDefBox::SetCart2Cyl_ControlPoints(CConfig* config) {
   unsigned short iDegree, jDegree, kDegree;
   su2double CartCoord[3];
   su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
@@ -354,7 +354,7 @@ void CFreeFormDefBox::SetCart2Cyl_ControlPoints(CConfig* config) const {
   }
 }
 
-void CFreeFormDefBox::SetCyl2Cart_ControlPoints(CConfig* config) const {
+void CFreeFormDefBox::SetCyl2Cart_ControlPoints(CConfig* config) {
   unsigned short iDegree, jDegree, kDegree;
   su2double PolarCoord[3];
 
@@ -386,7 +386,7 @@ void CFreeFormDefBox::SetCyl2Cart_ControlPoints(CConfig* config) const {
   }
 }
 
-void CFreeFormDefBox::SetCart2Cyl_CornerPoints(CConfig* config) const {
+void CFreeFormDefBox::SetCart2Cyl_CornerPoints(CConfig* config) {
   unsigned short iCornerPoint;
   su2double* CartCoord;
   su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
@@ -408,7 +408,7 @@ void CFreeFormDefBox::SetCart2Cyl_CornerPoints(CConfig* config) const {
   }
 }
 
-void CFreeFormDefBox::SetCyl2Cart_CornerPoints(CConfig* config) const {
+void CFreeFormDefBox::SetCyl2Cart_CornerPoints(CConfig* config) {
   unsigned short iCornerPoint;
   su2double* PolarCoord;
   su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
@@ -430,7 +430,7 @@ void CFreeFormDefBox::SetCyl2Cart_CornerPoints(CConfig* config) const {
   }
 }
 
-void CFreeFormDefBox::SetCart2Sphe_ControlPoints(CConfig* config) const {
+void CFreeFormDefBox::SetCart2Sphe_ControlPoints(CConfig* config) {
   unsigned short iDegree, jDegree, kDegree;
   su2double CartCoord[3];
   su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
@@ -476,7 +476,7 @@ void CFreeFormDefBox::SetCart2Sphe_ControlPoints(CConfig* config) const {
   }
 }
 
-void CFreeFormDefBox::SetSphe2Cart_ControlPoints(CConfig* config) const {
+void CFreeFormDefBox::SetSphe2Cart_ControlPoints(CConfig* config) {
   unsigned short iDegree, jDegree, kDegree;
   su2double PolarCoord[3];
 
@@ -508,7 +508,7 @@ void CFreeFormDefBox::SetSphe2Cart_ControlPoints(CConfig* config) const {
   }
 }
 
-void CFreeFormDefBox::SetCart2Sphe_CornerPoints(CConfig* config) const {
+void CFreeFormDefBox::SetCart2Sphe_CornerPoints(CConfig* config) {
   unsigned short iCornerPoint;
   su2double* CartCoord;
   su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
@@ -530,7 +530,7 @@ void CFreeFormDefBox::SetCart2Sphe_CornerPoints(CConfig* config) const {
   }
 }
 
-void CFreeFormDefBox::SetSphe2Cart_CornerPoints(CConfig* config) const {
+void CFreeFormDefBox::SetSphe2Cart_CornerPoints(CConfig* config) {
   unsigned short iCornerPoint;
   su2double* PolarCoord;
   su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
diff --git a/SU2_CFD/src/numerics/CNumerics.cpp b/SU2_CFD/src/numerics/CNumerics.cpp
index 082eceffb22..12a83bf7daa 100644
--- a/SU2_CFD/src/numerics/CNumerics.cpp
+++ b/SU2_CFD/src/numerics/CNumerics.cpp
@@ -1603,7 +1603,7 @@ void CNumerics::GetPrimitive2Conservative (const su2double *val_Mean_PrimVar,
   }
 }
 
-void CNumerics::CreateBasis(const su2double *val_Normal, su2double* l, su2double* m) const {
+void CNumerics::CreateBasis(const su2double *val_Normal, su2double* l, su2double* m) {
 
   unsigned short iDim;
   su2double modm, modl;

From 0363953315ab02500dad7875ceb5b6d6e2f28507 Mon Sep 17 00:00:00 2001
From: Kursat Yurt <kursatyurt@gmail.com>
Date: Fri, 31 Mar 2023 17:22:16 +0200
Subject: [PATCH 337/656] Add else after return

---
 .clang-tidy                                   |  2 +-
 Common/src/CConfig.cpp                        | 10 ++++------
 Common/src/fem/fem_geometry_structure.cpp     |  9 ++++-----
 Common/src/geometry/CGeometry.cpp             |  2 +-
 .../meshreader/CCGNSMeshReaderFVM.cpp         |  4 ++--
 Common/src/grid_movement/CBezierBlending.cpp  | 15 +++++++-------
 SU2_CFD/src/drivers/CDriver.cpp               |  3 +--
 SU2_CFD/src/drivers/CMultizoneDriver.cpp      |  4 ++--
 SU2_CFD/src/fluid/CSU2TCLib.cpp               | 19 ++++++++----------
 SU2_CFD/src/interfaces/CInterface.cpp         | 20 ++++++++-----------
 SU2_CFD/src/iteration/CFEAIteration.cpp       |  5 ++---
 SU2_CFD/src/iteration/CFluidIteration.cpp     |  5 ++---
 SU2_CFD/src/numerics/CNumerics.cpp            |  4 ++--
 SU2_CFD/src/output/CFlowOutput.cpp            |  5 ++---
 SU2_CFD/src/output/COutput.cpp                |  5 ++---
 SU2_CFD/src/variables/CNEMOEulerVariable.cpp  |  4 ++--
 .../src/drivers/CDiscAdjDeformationDriver.cpp | 19 +++++++++---------
 17 files changed, 59 insertions(+), 76 deletions(-)

diff --git a/.clang-tidy b/.clang-tidy
index 397fec948e8..f752385dc08 100644
--- a/.clang-tidy
+++ b/.clang-tidy
@@ -1,4 +1,4 @@
-Checks: '-*,modernize-avoid-bind,modernize-deprecated-headers,modernize-deprecated-ios-base-aliases,modernize-macro-to-enum,modernize-pass-by-value,modernize-raw-string-literal,modernize-redundant-void-arg,modernize-replace-auto-ptr,modernize-replace-disallow-copy-and-assign-macro,modernize-replace-random-shuffle,modernize-return-braced-init-list,modernize-shrink-to-fit,modernize-unary-static-assert,modernize-use-auto,modernize-use-bool-literals,modernize-use-default-member-init,modernize-use-emplace,modernize-use-equals-default,modernize-use-equals-delete,modernize-use-noexcept,modernize-use-nullptr,modernize-use-override,modernize-use-transparent-functors,modernize-use-using,readability-const-return-type,readability-avoid-const-params-in-decls,readability-container-data-pointer,readability-container-size-empty,readability-delete-null-pointer,readability-duplicate-include,readability-non-const-parameter,readability-redundant-access-specifiers,readability-redundant-control-flow,readability-redundant-declaration,readability-redundant-function-ptr-dereference,readability-redundant-smartptr-get,readability-redundant-string-cstr,readability-redundant-string-init,readability-simplify-boolean-expr,readability-simplify-subscript-expr,performance-*'
+Checks: '-*,modernize-avoid-bind,modernize-deprecated-headers,modernize-deprecated-ios-base-aliases,modernize-macro-to-enum,modernize-pass-by-value,modernize-raw-string-literal,modernize-redundant-void-arg,modernize-replace-auto-ptr,modernize-replace-disallow-copy-and-assign-macro,modernize-replace-random-shuffle,modernize-return-braced-init-list,modernize-shrink-to-fit,modernize-unary-static-assert,modernize-use-auto,modernize-use-bool-literals,modernize-use-default-member-init,modernize-use-emplace,modernize-use-equals-default,modernize-use-equals-delete,modernize-use-noexcept,modernize-use-nullptr,modernize-use-override,modernize-use-transparent-functors,modernize-use-using,readability-const-return-type,readability-avoid-const-params-in-decls,readability-container-data-pointer,readability-container-size-empty,readability-delete-null-pointer,readability-duplicate-include,readability-non-const-parameter,readability-redundant-access-specifiers,readability-redundant-control-flow,readability-redundant-declaration,readability-redundant-function-ptr-dereference,readability-redundant-smartptr-get,readability-redundant-string-cstr,readability-redundant-string-init,readability-simplify-boolean-expr,readability-simplify-subscript-expr,readability-else-after-return,performance-*'
 CheckOptions:
   - {key: modernize-use-override.AllowOverrideAndFinal, value: 'true'}
   - {key: performance-unnecessary-copy-initialization.AllowedTypes, value: 'su2double'}
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 5fd2e130f81..bf936e6e8fc 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -7659,9 +7659,8 @@ bool CConfig::TokenizeString(string & str, string & option_name,
       }
       it = option_value.begin(); // go back to beginning; not efficient
       continue;
-    } else {
-      it++;
-    }
+    }       it++;
+
   }
 #if 0
   cout << "option value(s) = ";
@@ -8842,9 +8841,8 @@ const su2double* CConfig::GetInlet_TurbVal(const string& val_marker) const {
   }
   if (Kind_Turb_Model == TURB_MODEL::SST) {
     return TurbIntensityAndViscRatioFreeStream;
-  } else {
-    return &NuFactor_FreeStream;
-  }
+  }     return &NuFactor_FreeStream;
+
 }
 
 su2double CConfig::GetOutlet_Pressure(const string& val_marker) const {
diff --git a/Common/src/fem/fem_geometry_structure.cpp b/Common/src/fem/fem_geometry_structure.cpp
index e226fc2ce9b..1cc219596f3 100644
--- a/Common/src/fem/fem_geometry_structure.cpp
+++ b/Common/src/fem/fem_geometry_structure.cpp
@@ -134,11 +134,10 @@ bool CSortFaces::operator()(const CFaceOfElement& f0, const CFaceOfElement& f1)
            to their element ID's in order to increase cache performance. */
         if (elemIDMin0 != elemIDMin1) return elemIDMin0 < elemIDMin1;
         return elemIDMax0 < elemIDMax1;
-      } else {
-        /* One face is a local face and the other is not. Make sure that
-           the local faces are numbered first. */
-        return face0IsLocal;
-      }
+      } /* One face is a local face and the other is not. Make sure that
+   the local faces are numbered first. */
+      return face0IsLocal;
+
     } else if (elemIDMax0 >= nVolElemTot && elemIDMax1 >= nVolElemTot) {
       /* Both faces are non-matching internal faces. Sort them according to
          their relevant element ID. The time level is not taken into account
diff --git a/Common/src/geometry/CGeometry.cpp b/Common/src/geometry/CGeometry.cpp
index 7f4626e4f98..cc5c84e54f3 100644
--- a/Common/src/geometry/CGeometry.cpp
+++ b/Common/src/geometry/CGeometry.cpp
@@ -1515,7 +1515,7 @@ bool CGeometry::SegmentIntersectsLine(const su2double point0[2], const su2double
 
   length = diff0_A * diff0_A + diff1_A * diff1_A;
 
-  return !((dist0 > length) || (dist1 > length));
+  return (dist0 <= length) && (dist1 <= length);
 }
 
 bool CGeometry::SegmentIntersectsTriangle(su2double point0[3], const su2double point1[3], su2double vert0[3],
diff --git a/Common/src/geometry/meshreader/CCGNSMeshReaderFVM.cpp b/Common/src/geometry/meshreader/CCGNSMeshReaderFVM.cpp
index 81f5d1100ff..2d8db05e9c8 100644
--- a/Common/src/geometry/meshreader/CCGNSMeshReaderFVM.cpp
+++ b/Common/src/geometry/meshreader/CCGNSMeshReaderFVM.cpp
@@ -754,8 +754,8 @@ void CCGNSMeshReaderFVM::ReadCGNSVolumeSection(int val_section) {
 
   /*--- Free temporary memory from communications ---*/
 
-  if (connSendReq != nullptr) delete[] connSendReq;
-  if (connRecvReq != nullptr) delete[] connRecvReq;
+  delete[] connSendReq;
+  delete[] connRecvReq;
 
   delete[] connSend;
   delete[] connRecv;
diff --git a/Common/src/grid_movement/CBezierBlending.cpp b/Common/src/grid_movement/CBezierBlending.cpp
index 0de026c0dba..0d8feebc645 100644
--- a/Common/src/grid_movement/CBezierBlending.cpp
+++ b/Common/src/grid_movement/CBezierBlending.cpp
@@ -88,15 +88,14 @@ su2double CBezierBlending::GetBernsteinDerivative(short val_n, short val_i, su2d
   if (val_i == 0) {
     value = val_n * (-GetBernsteinDerivative(val_n - 1, val_i, val_t, val_order_der - 1));
     return value;
+  }
+  if (val_n == 0) {
+    value = val_t;
+    return value;
   } else {
-    if (val_n == 0) {
-      value = val_t;
-      return value;
-    } else {
-      value = val_n * (GetBernsteinDerivative(val_n - 1, val_i - 1, val_t, val_order_der - 1) -
-                       GetBernsteinDerivative(val_n - 1, val_i, val_t, val_order_der - 1));
-      return value;
-    }
+    value = val_n * (GetBernsteinDerivative(val_n - 1, val_i - 1, val_t, val_order_der - 1) -
+                     GetBernsteinDerivative(val_n - 1, val_i, val_t, val_order_der - 1));
+    return value;
   }
 
   return value;
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index 7b9621280f9..91378f64b1f 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -2821,8 +2821,7 @@ void CDriver::PrintDirectResidual(RECORDING kind_recording) {
   auto iVar_iZone2string = [&](unsigned short ivar, unsigned short izone) {
     if (multizone)
       return "[" + std::to_string(ivar) + "][" + std::to_string(izone) + "]";
-    else
-      return "[" + std::to_string(ivar) + "]";
+          return "[" + std::to_string(ivar) + "]";
   };
 
   /*--- Print residuals in the first iteration ---*/
diff --git a/SU2_CFD/src/drivers/CMultizoneDriver.cpp b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
index cd93263313f..4f2c83aa085 100644
--- a/SU2_CFD/src/drivers/CMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
@@ -620,7 +620,7 @@ bool CMultizoneDriver::Monitor(unsigned long TimeIter){
 
     return (MaxIterationsReached || InnerConvergence);
   }
-  else { // i.e. unsteady simulation
+  // i.e. unsteady simulation
 
     /*--- Check whether the outer time integration has reached the final time ---*/
     const auto TimeConvergence = GetTimeConvergence();
@@ -641,7 +641,7 @@ bool CMultizoneDriver::Monitor(unsigned long TimeIter){
     }
 
     return (FinalTimeReached || MaxIterationsReached);
-  }
+ 
 
 }
 
diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 9e4d63b12ff..67cd77b343e 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -1581,7 +1581,7 @@ void CSU2TCLib::ComputeKeqConstants(unsigned short val_Reaction) {
     for (ii = 0; ii < 5; ii++)
       A[ii] = RxnConstantTable(0,ii);
     return;
-  } else if (iIndex >= 5) {
+  } if (iIndex >= 5) {
     for (ii = 0; ii < 5; ii++)
       A[ii] = RxnConstantTable(5,ii);
     return;
@@ -1902,7 +1902,7 @@ su2double CSU2TCLib::ComputeCollisionCrossSection(unsigned iSpecies, unsigned jS
 
     if (Omega11(iSpecies, jSpecies, 0) == 1.0 && d1) {
       return 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_a*T_star*(1 - C1_a * exp(-c1_a * T_star))+1);
-    } else if (Omega11(iSpecies, jSpecies, 0) == -1.0 && d1) {
+    } if (Omega11(iSpecies, jSpecies, 0) == -1.0 && d1) {
       return 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D1_r*T_star*(1 - C1_r * exp(-c1_r * T_star))+1);
     } else if (Omega22(iSpecies, jSpecies, 0) == 1.0 && !d1) {
       return 1E-20 * 5E15 * pi * pow((debyeLength / T), 2) * log(D2_a*T_star*(1 - C2_a * exp(-c2_a * T_star))+1);
@@ -1913,9 +1913,8 @@ su2double CSU2TCLib::ComputeCollisionCrossSection(unsigned iSpecies, unsigned jS
   } else {
     if (d1) {
       return 1E-20 * Omega11(iSpecies,jSpecies,3) * pow(T, Omega11(iSpecies,jSpecies,0)*log(T)*log(T) + Omega11(iSpecies,jSpecies,1)*log(T) + Omega11(iSpecies,jSpecies,2));
-    } else {
-      return 1E-20 * Omega22(iSpecies,jSpecies,3) * pow(T, Omega22(iSpecies,jSpecies,0)*log(T)*log(T) + Omega22(iSpecies,jSpecies,1)*log(T) + Omega22(iSpecies,jSpecies,2));
-    }
+    }       return 1E-20 * Omega22(iSpecies,jSpecies,3) * pow(T, Omega22(iSpecies,jSpecies,0)*log(T)*log(T) + Omega22(iSpecies,jSpecies,1)*log(T) + Omega22(iSpecies,jSpecies,2));
+   
   }
 }
 
@@ -2169,9 +2168,8 @@ vector<su2double>& CSU2TCLib::ComputeTemperatures(vector<su2double>& val_rhos, s
       NRconvg = true;
       Tve = Tve2;
       break;
-    } else {
-      Tve = Tve2;
-    }
+    }       Tve = Tve2;
+   
   }
 
   // If the Newton-Raphson method has converged, assign the value of Tve.
@@ -2186,10 +2184,9 @@ vector<su2double>& CSU2TCLib::ComputeTemperatures(vector<su2double>& val_rhos, s
       if (fabs(rhoEve_t - rhoEve) < Btol) {
         Bconvg = true;
         break;
-      } else {
-        if (rhoEve_t > rhoEve) Tve2 = Tve;
+      }         if (rhoEve_t > rhoEve) Tve2 = Tve;
         else                  Tve_o = Tve;
-      }
+     
     }
   }
 
diff --git a/SU2_CFD/src/interfaces/CInterface.cpp b/SU2_CFD/src/interfaces/CInterface.cpp
index 6053709a30c..dc068205324 100644
--- a/SU2_CFD/src/interfaces/CInterface.cpp
+++ b/SU2_CFD/src/interfaces/CInterface.cpp
@@ -227,11 +227,10 @@ void CInterface::PreprocessAverage(CGeometry *donor_geometry, CGeometry *target_
       /*--- Exit the for loop: we have found the local index for Mixing-Plane interface ---*/
       break;
     }
-    else {
-      /*--- If the tag hasn't matched any tag within the donor markers ---*/
+          /*--- If the tag hasn't matched any tag within the donor markers ---*/
       Marker_Donor = -1;
       Donor_Flag   = -1;
-    }
+   
   }
 
 #ifdef HAVE_MPI
@@ -273,10 +272,9 @@ void CInterface::PreprocessAverage(CGeometry *donor_geometry, CGeometry *target_
       /*--- Exit the for loop: we have found the local index for iMarkerFSI on the FEA side ---*/
       break;
     }
-    else {
-      /*--- If the tag hasn't matched any tag within the Flow markers ---*/
+          /*--- If the tag hasn't matched any tag within the Flow markers ---*/
       Marker_Target = -1;
-    }
+   
   }
 
   if (Marker_Target != -1 && Marker_Donor != -1){
@@ -418,10 +416,9 @@ void CInterface::AllgatherAverage(CSolver *donor_solution, CSolver *target_solut
       /*--- Exit the for loop: we have found the local index for Mixing-Plane interface ---*/
       break;
     }
-    else {
-      /*--- If the tag hasn't matched any tag within the donor markers ---*/
+          /*--- If the tag hasn't matched any tag within the donor markers ---*/
       Marker_Donor = -1;
-    }
+   
   }
   /*--- Here we want to make available the quantities for all the processors and collect them in a buffer
    * for each span of the donor the span-wise height vector also so
@@ -534,10 +531,9 @@ void CInterface::AllgatherAverage(CSolver *donor_solution, CSolver *target_solut
       /*--- Exit the for loop: we have found the local index for iMarkerFSI on the FEA side ---*/
       break;
     }
-    else {
-      /*--- If the tag hasn't matched any tag within the Flow markers ---*/
+          /*--- If the tag hasn't matched any tag within the Flow markers ---*/
       Marker_Target = -1;
-    }
+   
   }
 
 
diff --git a/SU2_CFD/src/iteration/CFEAIteration.cpp b/SU2_CFD/src/iteration/CFEAIteration.cpp
index 45ded06c7ee..95e477d92c9 100644
--- a/SU2_CFD/src/iteration/CFEAIteration.cpp
+++ b/SU2_CFD/src/iteration/CFEAIteration.cpp
@@ -87,12 +87,11 @@ void CFEAIteration::Iterate(COutput* output, CIntegration**** integration, CGeom
       if (disc_adj_fem) {
         config[val_iZone]->SetInnerIter(CurIter);
         break;
-      } else {
-        StopCalc = Monitor(output, integration, geometry, solver, numerics, config, surface_movement, grid_movement,
+      }         StopCalc = Monitor(output, integration, geometry, solver, numerics, config, surface_movement, grid_movement,
                            FFDBox, val_iZone, INST_0);
 
         if (StopCalc && (IntIter > 0)) break;
-      }
+     
     }
 
   } else {
diff --git a/SU2_CFD/src/iteration/CFluidIteration.cpp b/SU2_CFD/src/iteration/CFluidIteration.cpp
index 7f7107f2ccb..f6feb7d9d58 100644
--- a/SU2_CFD/src/iteration/CFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CFluidIteration.cpp
@@ -588,9 +588,8 @@ void CFluidIteration::SetDualTime_Aeroelastic(CConfig* config) const {
         Monitoring_Tag = config->GetMarker_Monitoring_TagBound(iMarker_Monitoring);
         Marker_Tag = config->GetMarker_All_TagBound(iMarker);
         if (Marker_Tag == Monitoring_Tag) { owner = 1; break;
-        } else {
-          owner = 0;
-        }
+        }           owner = 0;
+       
 
       }
       plunge = config->GetAeroelastic_plunge(iMarker_Monitoring);
diff --git a/SU2_CFD/src/numerics/CNumerics.cpp b/SU2_CFD/src/numerics/CNumerics.cpp
index 12a83bf7daa..1393c14a20a 100644
--- a/SU2_CFD/src/numerics/CNumerics.cpp
+++ b/SU2_CFD/src/numerics/CNumerics.cpp
@@ -31,7 +31,7 @@
 #include "../../include/numerics/CNumerics.hpp"
 #include "../../include/fluid/CFluidModel.hpp"
 
-CNumerics::CNumerics(void) {
+CNumerics::CNumerics() {
 
   Proj_Flux_Tensor  = nullptr;
 
@@ -75,7 +75,7 @@ CNumerics::CNumerics(unsigned short val_nDim, unsigned short val_nVar,
 
 }
 
-CNumerics::~CNumerics(void) {
+CNumerics::~CNumerics() {
 
   // visc
   delete [] Proj_Flux_Tensor;
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index 1026b3d13e2..3fc02d126e7 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -873,9 +873,8 @@ void CFlowOutput::SetCustomOutputs(const CSolver* const* solver, const CGeometry
           const auto varIdx = i % CustomOutput::MAX_VARS_PER_SOLVER;
           if (solIdx == FLOW_SOL) {
             return flowNodes->GetPrimitive(iPoint, varIdx);
-          } else {
-            return solver[solIdx]->GetNodes()->GetSolution(iPoint, varIdx);
-          }
+          }             return solver[solIdx]->GetNodes()->GetSolution(iPoint, varIdx);
+         
         } else {
           return *output.otherOutputs[i - CustomOutput::NOT_A_VARIABLE];
         }
diff --git a/SU2_CFD/src/output/COutput.cpp b/SU2_CFD/src/output/COutput.cpp
index 9e95c9b4614..7c76bbf50bc 100644
--- a/SU2_CFD/src/output/COutput.cpp
+++ b/SU2_CFD/src/output/COutput.cpp
@@ -2134,9 +2134,8 @@ bool COutput::WriteVolumeOutput(CConfig *config, unsigned long Iter, bool force_
 
     return ((Iter % config->GetVolumeOutputFrequency(iFile) == 0)) || force_writing;
   }
-  else {
-    return ((Iter > 0) && (Iter % config->GetVolumeOutputFrequency(iFile) == 0)) || force_writing;
-  }
+      return ((Iter > 0) && (Iter % config->GetVolumeOutputFrequency(iFile) == 0)) || force_writing;
+ 
 }
 
 void COutput::SetCommonHistoryFields() {
diff --git a/SU2_CFD/src/variables/CNEMOEulerVariable.cpp b/SU2_CFD/src/variables/CNEMOEulerVariable.cpp
index 2c448786a29..e0a9836034a 100644
--- a/SU2_CFD/src/variables/CNEMOEulerVariable.cpp
+++ b/SU2_CFD/src/variables/CNEMOEulerVariable.cpp
@@ -228,12 +228,12 @@ bool CNEMOEulerVariable::Cons2PrimVar(su2double *U, su2double *V,
 
   // Determine if the temperature lies within the acceptable range
   if (V[T_INDEX] <= Tmin)      { nonPhys = true; return nonPhys;}
-  else if (V[T_INDEX] >= Tmax) { nonPhys = true; return nonPhys;}
+  if (V[T_INDEX] >= Tmax) { nonPhys = true; return nonPhys;}
   else if (V[T_INDEX] != V[T_INDEX]){ nonPhys = true; return nonPhys;}
 
   if (!monoatomic){
     if (V[TVE_INDEX] <= Tvemin)      { nonPhys = true; return nonPhys;}
-    else if (V[TVE_INDEX] >= Tvemax) { nonPhys = true; return nonPhys;}
+    if (V[TVE_INDEX] >= Tvemax) { nonPhys = true; return nonPhys;}
     else if (V[TVE_INDEX] != V[TVE_INDEX]){ nonPhys = true; return nonPhys;}
   }
   else {V[TVE_INDEX] = Tve_Freestream;}
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index 3c4963a3d12..5645b8b7bdc 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -302,17 +302,16 @@ void CDiscAdjDeformationDriver::Run() {
   for (iZone = 0; iZone < nZone; iZone++) {
     if (!config_container[iZone]->GetDiscrete_Adjoint()) {
       continue;
+    }
+    if (rank == MASTER_NODE)
+      cout << "\n---------------------- Mesh sensitivity computation ---------------------" << endl;
+    if (config_container[iZone]->GetDiscrete_Adjoint() && config_container[iZone]->GetSmoothGradient() &&
+        config_container[iZone]->GetSobMode() == ENUM_SOBOLEV_MODUS::MESH_LEVEL) {
+      DerivativeTreatment_MeshSensitivity(geometry_container[iZone][INST_0][MESH_0], config_container[iZone],
+                                          grid_movement[iZone][INST_0]);
     } else {
-      if (rank == MASTER_NODE)
-        cout << "\n---------------------- Mesh sensitivity computation ---------------------" << endl;
-      if (config_container[iZone]->GetDiscrete_Adjoint() && config_container[iZone]->GetSmoothGradient() &&
-          config_container[iZone]->GetSobMode() == ENUM_SOBOLEV_MODUS::MESH_LEVEL) {
-        DerivativeTreatment_MeshSensitivity(geometry_container[iZone][INST_0][MESH_0], config_container[iZone],
-                                            grid_movement[iZone][INST_0]);
-      } else {
-        grid_movement[iZone][INST_0]->SetVolume_Deformation(geometry_container[iZone][INST_0][MESH_0],
-                                                            config_container[iZone], false, true);
-      }
+      grid_movement[iZone][INST_0]->SetVolume_Deformation(geometry_container[iZone][INST_0][MESH_0],
+                                                          config_container[iZone], false, true);
     }
   }
 

From 5303d9166c01b17838244b5b2f06316d7dabb511 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Sat, 1 Apr 2023 16:16:31 +0200
Subject: [PATCH 338/656] Made MLPCpp submodule compatible with adjoint

---
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp |  2 +-
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp     |  7 ++++++-
 meson.build                                | 10 ----------
 meson_scripts/init.py                      |  2 +-
 subprojects/MLPCpp                         |  2 +-
 5 files changed, 9 insertions(+), 14 deletions(-)

diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index 7fcbdae492c..bbbb0be7e4c 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -31,7 +31,7 @@
 #include <vector>
 #include "../../../Common/include/containers/CLookUpTable.hpp"
 #if defined(HAVE_MLPCPP)
-#include "CLookUp_ANN.hpp"
+#include "../../../subprojects/MLPCpp/include/CLookUp_ANN.hpp"
 #define USE_MLPCPP
 #endif
 #include "CFluidModel.hpp"
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 78bf25716f1..b8e4b3f7415 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -26,6 +26,10 @@
  */
 
 #include "../../include/fluid/CDataDrivenFluid.hpp"
+#if defined(HAVE_MLPCPP)
+#include "../../../subprojects/MLPCpp/include/CLookUp_ANN.hpp"
+#define USE_MLPCPP
+#endif
 
 CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
 #ifdef HAVE_MPI
@@ -110,7 +114,8 @@ void CDataDrivenFluid::MapInputs_to_Outputs() {
   if (Kind_DataDriven_Method == ENUM_DATADRIVEN_METHOD::MLP) {
 /*--- Map MLP inputs to outputs ---*/
 #ifdef USE_MLPCPP
-    iomap_rhoe = new MLPToolbox::CIOMap(lookup_mlp, input_names_rhoe, output_names_rhoe);
+    iomap_rhoe = new MLPToolbox::CIOMap(input_names_rhoe, output_names_rhoe);
+    lookup_mlp->PairVariableswithMLPs(*iomap_rhoe);
     MLP_inputs.resize(2);
 #endif
   }
diff --git a/meson.build b/meson.build
index 196c31da7ff..cbfdacc0e12 100644
--- a/meson.build
+++ b/meson.build
@@ -260,16 +260,6 @@ if get_option('enable-coolprop')
 endif
 
 if get_option('enable-mlpcpp')
-  cmake = import('cmake')
-  cmake_opts = cmake.subproject_options()
-  cmake_opts.set_override_option('warning_level', '0')
-  cmake_opts.add_cmake_defines({
-    'CMAKE_MAKE_PROGRAM': meson.source_root() + '/ninja',
-    'CMAKE_POSITION_INDEPENDENT_CODE': 'ON'
-  })
-  mlpcpp_subproj = cmake.subproject('MLPCpp', options: cmake_opts)
-  mlpcpp_dep = mlpcpp_subproj.dependency('MLPCpp')
-  su2_deps += mlpcpp_dep
   su2_cpp_args += '-DHAVE_MLPCPP'
 endif
 
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 4fb10b43013..59f9d711236 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -71,7 +71,7 @@ def init_submodules(
     github_repo_coolprop = "https://github.com/CoolProp/CoolProp"
     sha_version_mel = "2484cd3258ef800a10e361016cb341834ee7930b"
     github_repo_mel = "https://github.com/pcarruscag/MEL"
-    sha_version_mlpcpp = "0de8d8c86bbf70e461a7e15cbe355084109d16c0"
+    sha_version_mlpcpp = "a0fbc274934071331fc90b06bde6bef812cb2e42"
     github_repo_mlpcpp = "https://github.com/EvertBunschoten/MLPCpp"
 
     medi_name = "MeDiPack"
diff --git a/subprojects/MLPCpp b/subprojects/MLPCpp
index 0de8d8c86bb..a0fbc274934 160000
--- a/subprojects/MLPCpp
+++ b/subprojects/MLPCpp
@@ -1 +1 @@
-Subproject commit 0de8d8c86bbf70e461a7e15cbe355084109d16c0
+Subproject commit a0fbc274934071331fc90b06bde6bef812cb2e42

From 64c2029e94e252bf44da7a8638797acf73920912 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Sat, 1 Apr 2023 23:41:30 +0200
Subject: [PATCH 339/656] Fixed CLookUp_ANN unit test with new MLP class format

---
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        | 46 +++++++++----------
 .../CLookUp_ANN_tests.cpp                     |  5 +-
 2 files changed, 26 insertions(+), 25 deletions(-)

diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index b8e4b3f7415..9ee38e22abb 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -165,11 +165,11 @@ void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
   bool converged = false;  // Convergence flag
   unsigned long Iter = 0;
 
-  su2double delta_P,  // Pressure residual
-      delta_T,        // Temperature residual
-      delta_rho,      // Density step size
-      delta_e,        // Energy step size
-      determinant;    // Jacobian determinant
+  su2double delta_P,
+      delta_T,    
+      delta_rho,
+      delta_e,
+      determinant;
   /*--- Initiating Newton solver ---*/
   while (!converged && (Iter < MaxIter_Newton)) {
     /*--- Determine thermodynamic state based on current density and energy*/
@@ -213,11 +213,11 @@ void CDataDrivenFluid::SetEnergy_Prho(su2double P, su2double rho) {
   /*--- Setting initial values for energy ---*/
   su2double e = e_start;
 
-  bool converged = false;  // Convergence flag
+  bool converged = false;
   unsigned long Iter = 0;
 
-  su2double delta_P,  // Pressure residual
-      delta_e;        // Energy step size
+  su2double delta_P,
+      delta_e;
 
   while (!converged && (Iter < MaxIter_Newton)) {
     /*--- Determine thermodynamic state based on current density and energy*/
@@ -249,11 +249,11 @@ void CDataDrivenFluid::SetTDState_rhoT(su2double rho, su2double T) {
   /*--- Setting initial values for density and energy ---*/
   su2double e = e_start;
 
-  bool converged = false;  // Convergence flag
+  bool converged = false;
   unsigned long Iter = 0;
 
-  su2double delta_T,  // Temperature residual
-      delta_e;        // Energy increment
+  su2double delta_T,
+      delta_e;
 
   /*--- Initiating Newton solver ---*/
   while (!converged && (Iter < MaxIter_Newton)) {
@@ -285,14 +285,14 @@ void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
   /*--- Setting initial values for density and energy ---*/
   su2double rho = rho_start, e = e_start;
 
-  bool converged = false;  // Convergence flag
+  bool converged = false;
   unsigned long Iter = 0;
 
-  su2double delta_h,  // Enthalpy
-      delta_s,        // Entropy residual
-      delta_rho,      // Density step size
-      delta_e,        // Energy step size
-      determinant;    // Jacobian determinant
+  su2double delta_h,
+      delta_s,
+      delta_rho,
+      delta_e,
+      determinant;
 
   /*--- Initiating Newton solver ---*/
   while (!converged && (Iter < MaxIter_Newton)) {
@@ -331,14 +331,14 @@ void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
   /*--- Setting initial values for density and energy ---*/
   su2double rho = rho_start, e = e_start;
 
-  bool converged = false;  // Convergence flag
+  bool converged = false;
   unsigned long Iter = 0;
 
-  su2double delta_P,  // Enthalpy
-      delta_s,        // Entropy residual
-      delta_rho,      // Density step size
-      delta_e,        // Energy step size
-      determinant;    // Jacobian determinant
+  su2double delta_P,
+      delta_s,
+      delta_rho,
+      delta_e,
+      determinant;
 
   /*--- Initiating Newton solver ---*/
   while (!converged && (Iter < MaxIter_Newton)) {
diff --git a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
index e1c05996086..a495ea3358e 100644
--- a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
+++ b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
@@ -28,7 +28,7 @@
 #include "catch.hpp"
 #include "../../../../Common/include/CConfig.hpp"
 #if defined(HAVE_MLPCPP)
-#include "CLookUp_ANN.hpp"
+#include "../../../../subprojects/MLPCpp/include/CLookUp_ANN.hpp"
 #define USE_MLPCPP
 #endif
 #include <vector>
@@ -55,7 +55,8 @@ TEST_CASE("LookUp ANN test", "[LookUpANN]") {
   MLP_outputs[0] = &z;
 
   /*--- Generate input-output map ---*/
-  MLPToolbox::CIOMap iomap(&ANN, MLP_input_names, MLP_output_names);
+  MLPToolbox::CIOMap iomap(MLP_input_names, MLP_output_names);
+  ANN.PairVariableswithMLPs(iomap);
   /*--- MLP evaluation on point in the middle of the training data range ---*/
   x = 1.0;
   y = -0.5;

From 20d8ce86e9a4a0ade732c3ffd95c4122e749934b Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 2 Apr 2023 09:57:21 +0100
Subject: [PATCH 340/656] reduce public interface, cleanup obsolete code

---
 .../drivers/CDiscAdjMultizoneDriver.hpp       |   6 +-
 .../drivers/CDiscAdjSinglezoneDriver.hpp      |  69 ++++-----
 SU2_CFD/include/drivers/CDriver.hpp           | 145 +++++++-----------
 SU2_CFD/include/drivers/CDriverBase.hpp       |  15 --
 SU2_CFD/include/drivers/CMultizoneDriver.hpp  |  72 ++++-----
 SU2_CFD/include/drivers/CSinglezoneDriver.hpp |  17 +-
 SU2_CFD/include/integration/CIntegration.hpp  |  38 -----
 .../iteration/CDiscAdjFluidIteration.hpp      |  19 ---
 .../iteration/CDiscAdjHeatIteration.hpp       |  19 ---
 SU2_CFD/src/drivers/CDriver.cpp               |  77 +---------
 SU2_CFD/src/drivers/CMultizoneDriver.cpp      |  21 +--
 SU2_CFD/src/drivers/CSinglezoneDriver.cpp     |  41 ++---
 SU2_CFD/src/integration/CIntegration.cpp      |   3 -
 .../src/integration/CMultiGridIntegration.cpp |   3 +
 SU2_CFD/src/iteration/CAdjFluidIteration.cpp  |  13 +-
 .../src/iteration/CDiscAdjFluidIteration.cpp  |  14 --
 .../src/iteration/CDiscAdjHeatIteration.cpp   |  15 --
 SU2_CFD/src/iteration/CFEAIteration.cpp       |  15 --
 SU2_CFD/src/iteration/CFluidIteration.cpp     |  14 --
 SU2_CFD/src/iteration/CHeatIteration.cpp      |   2 -
 SU2_CFD/src/python_wrapper_structure.cpp      |  43 ------
 .../include/drivers/CDeformationDriver.hpp    |  28 ++--
 .../drivers/CDiscAdjDeformationDriver.hpp     |   4 +-
 SU2_DEF/src/SU2_DEF.cpp                       |   4 -
 SU2_DEF/src/drivers/CDeformationDriver.cpp    |  23 +--
 SU2_PY/FSI_tools/FSIInterface.py              |   2 -
 26 files changed, 182 insertions(+), 540 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDiscAdjMultizoneDriver.hpp b/SU2_CFD/include/drivers/CDiscAdjMultizoneDriver.hpp
index 3f61be0904b..dee86ad3f19 100644
--- a/SU2_CFD/include/drivers/CDiscAdjMultizoneDriver.hpp
+++ b/SU2_CFD/include/drivers/CDiscAdjMultizoneDriver.hpp
@@ -141,8 +141,6 @@ class CDiscAdjMultizoneDriver : public CMultizoneDriver {
    */
   void StartSolver() override;
 
-protected:
-
   /*!
    * \brief Preprocess the multizone iteration
    */
@@ -153,6 +151,8 @@ class CDiscAdjMultizoneDriver : public CMultizoneDriver {
    */
   void Run() override;
 
+protected:
+
   /*!
    * \brief Run one inner iteration for a given zone.
    * \return The result of "monitor".
@@ -272,7 +272,7 @@ class CDiscAdjMultizoneDriver : public CMultizoneDriver {
    * \brief gets Convergence on physical time scale, (deactivated in adjoint case)
    * \return false
    */
-  inline bool GetTimeConvergence() const override {return false;}
+  inline bool GetTimeConvergence() const override { return false; }
 
   /*!
    * \brief Get the external of all adjoint solvers in a zone.
diff --git a/SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp b/SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp
index 206f245e400..105eecc3abe 100644
--- a/SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp
+++ b/SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp
@@ -57,40 +57,6 @@ class CDiscAdjSinglezoneDriver : public CSinglezoneDriver {
 
   COutputLegacy* output_legacy;
 
-public:
-
-  /*!
-   * \brief Constructor of the class.
-   * \param[in] confFile - Configuration file name.
-   * \param[in] val_nZone - Total number of zones.
-   * \param[in] val_nDim - Total number of dimensions.
-   * \param[in] MPICommunicator - MPI communicator for SU2.
-   */
-  CDiscAdjSinglezoneDriver(char* confFile,
-             unsigned short val_nZone,
-             SU2_Comm MPICommunicator);
-
-  /*!
-   * \brief Destructor of the class.
-   */
-  ~CDiscAdjSinglezoneDriver(void) override;
-
-  /*!
-   * \brief Preprocess the single-zone iteration
-   * \param[in] TimeIter - index of the current time-step.
-   */
-  void Preprocess(unsigned long TimeIter) override;
-
-  /*!
-   * \brief Run a single iteration of the discrete adjoint solver with a single zone.
-   */
-  void Run(void) override;
-
-  /*!
-   * \brief Postprocess the adjoint iteration for ZONE_0.
-   */
-  void Postprocess(void) override;
-
   /*!
    * \brief Record one iteration of a flow iteration in within multiple zones.
    * \param[in] kind_recording - Type of recording (full list in ENUM_RECORDING, option_structure.hpp)
@@ -127,6 +93,39 @@ class CDiscAdjSinglezoneDriver : public CSinglezoneDriver {
    * \brief gets Convergence on physical time scale, (deactivated in adjoint case)
    * \return false
    */
-  inline bool GetTimeConvergence() const override {return false;};
+  inline bool GetTimeConvergence() const override { return false; }
 
+public:
+
+  /*!
+   * \brief Constructor of the class.
+   * \param[in] confFile - Configuration file name.
+   * \param[in] val_nZone - Total number of zones.
+   * \param[in] val_nDim - Total number of dimensions.
+   * \param[in] MPICommunicator - MPI communicator for SU2.
+   */
+  CDiscAdjSinglezoneDriver(char* confFile,
+             unsigned short val_nZone,
+             SU2_Comm MPICommunicator);
+
+  /*!
+   * \brief Destructor of the class.
+   */
+  ~CDiscAdjSinglezoneDriver(void) override;
+
+  /*!
+   * \brief Preprocess the single-zone iteration
+   * \param[in] TimeIter - index of the current time-step.
+   */
+  void Preprocess(unsigned long TimeIter) override;
+
+  /*!
+   * \brief Run a single iteration of the discrete adjoint solver with a single zone.
+   */
+  void Run(void) override;
+
+  /*!
+   * \brief Postprocess the adjoint iteration for ZONE_0.
+   */
+  void Postprocess(void) override;
 };
diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index d0772a6b5d3..2cf991bb0b7 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -106,7 +106,7 @@ class CDriver : public CDriverBase {
 
  protected:
   /*!
-   * \brief Initialize containers. 
+   * \brief Initialize containers.
    */
   void InitializeContainers();
 
@@ -154,6 +154,14 @@ class CDriver : public CDriverBase {
    */
   void InitializeSolver(CConfig* config, CGeometry** geometry, CSolver***& solver);
 
+  /*!
+   * \brief Preprocess the inlets via file input for all solvers.
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void PreprocessInlet(CSolver*** solver, CGeometry** geometry, CConfig* config) const;
+
   /*!
    * \brief Restart of the solvers from the restart files.
    * \param[in] solver - Container vector with all the solutions.
@@ -335,21 +343,6 @@ class CDriver : public CDriverBase {
    */
   virtual void RelaxationTractions(unsigned short donorZone, unsigned short targetZone, unsigned long iOuterIter) {}
 
-  /*!
-   * \brief A virtual member to run a Block Gauss-Seidel iteration in multi-zone problems.
-   */
-  virtual void RunGaussSeidel() {}
-
-  /*!
-   * \brief A virtual member to run a Block-Jacobi iteration in multi-zone problems.
-   */
-  virtual void RunJacobi() {}
-
-  /*!
-   * \brief A virtual member.
-   */
-  void Update() override {}
-
   /*!
    * \brief Print out the direct residuals.
    * \param[in] kind_recording - Type of recording (full list in ENUM_RECORDING, option_structure.hpp)
@@ -408,6 +401,21 @@ class CDriver : public CDriverBase {
     }
   }
 
+  /*!
+   * \brief Sum the number of primal or adjoint variables for all solvers in a given zone.
+   * \param[in] iZone - Index of the zone.
+   * \param[in] adjoint - True to consider adjoint solvers instead of primal.
+   * \return Total number of solution variables.
+   */
+  unsigned short GetTotalNumberOfVariables(unsigned short iZone, bool adjoint) const {
+    unsigned short nVar = 0;
+    for (auto iSol = 0u; iSol < MAX_SOLS; iSol++) {
+      auto solver = solver_container[iZone][INST_0][MESH_0][iSol];
+      if (solver && (solver->GetAdjoint() == adjoint)) nVar += solver->GetnVar();
+    }
+    return nVar;
+  }
+
  public:
   /*!
    * \brief Launch the computation for all zones and all physics.
@@ -419,11 +427,6 @@ class CDriver : public CDriverBase {
    */
   void Finalize() override;
 
-  /*!
-   * \brief A virtual member.
-   */
-  virtual void ResetConvergence();
-
   /*!
    * \brief Perform some pre-processing before an iteration of the physics.
    */
@@ -446,10 +449,9 @@ class CDriver : public CDriverBase {
   virtual void DynamicMeshUpdate(unsigned long TimeIter) {}
 
   /*!
-   * \brief Perform a dynamic mesh deformation, including grid velocity computation and update of the multi-grid
-   * structure.
+   * \brief Update the dual-time solution.
    */
-  virtual void DynamicMeshUpdate(unsigned short val_iZone, unsigned long TimeIter) {}
+  virtual void Update() {}
 
   /*!
    * \brief Perform a mesh deformation as initial condition.
@@ -488,14 +490,6 @@ class CDriver : public CDriverBase {
    */
   string GetSurfaceFileName() const;
 
-  /*!
-   * \brief Preprocess the inlets via file input for all solvers.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] config - Definition of the particular problem.
-   */
-  void PreprocessInlet(CSolver*** solver, CGeometry** geometry, CConfig* config) const;
-
   /*!
    * \brief Set the position of the heat source.
    * \param[in] alpha - Angle of rotation respect to Z axis.
@@ -513,21 +507,6 @@ class CDriver : public CDriverBase {
   void SetInletAngle(unsigned short iMarker, passivedouble alpha);
 
 /// \}
-
-  /*!
-   * \brief Sum the number of primal or adjoint variables for all solvers in a given zone.
-   * \param[in] iZone - Index of the zone.
-   * \param[in] adjoint - True to consider adjoint solvers instead of primal.
-   * \return Total number of solution variables.
-   */
-  unsigned short GetTotalNumberOfVariables(unsigned short iZone, bool adjoint) const {
-    unsigned short nVar = 0;
-    for (auto iSol = 0u; iSol < MAX_SOLS; iSol++) {
-      auto solver = solver_container[iZone][INST_0][MESH_0][iSol];
-      if (solver && (solver->GetAdjoint() == adjoint)) nVar += solver->GetnVar();
-    }
-    return nVar;
-  }
 };
 
 /*!
@@ -540,7 +519,6 @@ class CFluidDriver : public CDriver {
  protected:
   unsigned long Max_Iter;
 
- protected:
   /*!
    * \brief Constructor of the class.
    * \param[in] confFile - Configuration file name.
@@ -549,6 +527,11 @@ class CFluidDriver : public CDriver {
    */
   CFluidDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator);
 
+  /*!
+   * \brief Transfer data among different zones (multiple zone).
+   */
+  void TransferData(unsigned short donorZone, unsigned short targetZone);
+
  public:
   /*!
    * \brief Destructor of the class.
@@ -590,11 +573,6 @@ class CFluidDriver : public CDriver {
    * structure (multiple zone).
    */
   void DynamicMeshUpdate(unsigned long TimeIter) override;
-
-  /*!
-   * \brief Transfer data among different zones (multiple zone).
-   */
-  void TransferData(unsigned short donorZone, unsigned short targetZone);
 };
 
 /*!
@@ -607,6 +585,16 @@ class CTurbomachineryDriver : public CFluidDriver {
  private:
   COutputLegacy* output_legacy;
 
+  /*!
+   * \brief Set Mixing Plane interface within multiple zones.
+   */
+  void SetMixingPlane(unsigned short iZone);
+
+  /*!
+   * \brief Set Mixing Plane interface within multiple zones.
+   */
+  void SetTurboPerformance(unsigned short targetZone);
+
  public:
   /*!
    * \brief Constructor of the class.
@@ -627,16 +615,6 @@ class CTurbomachineryDriver : public CFluidDriver {
 
   void Run() override;
 
-  /*!
-   * \brief Set Mixing Plane interface within multiple zones.
-   */
-  void SetMixingPlane(unsigned short iZone);
-
-  /*!
-   * \brief Set Mixing Plane interface within multiple zones.
-   */
-  void SetTurboPerformance(unsigned short targetZone);
-
   /*!
    * \brief Monitor the computation.
    */
@@ -655,25 +633,6 @@ class CHBDriver : public CFluidDriver {
   unsigned short nInstHB;
   su2double** D; /*!< \brief Harmonic Balance operator. */
 
- public:
-  /*!
-   * \brief Constructor of the class.
-   * \param[in] confFile - Configuration file name.
-   * \param[in] val_nZone - Total number of zones.
-   * \param[in] MPICommunicator - MPI communicator for SU2.
-   */
-  CHBDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator);
-
-  /*!
-   * \brief Destructor of the class.
-   */
-  ~CHBDriver(void) override;
-
-  /*!
-   * \brief Run a single iteration of a Harmonic Balance problem.
-   */
-  void Run() override;
-
   /*!
    * \brief Computation and storage of the Harmonic Balance method source terms.
    * \author T. Economon, K. Naik
@@ -693,13 +652,27 @@ class CHBDriver : public CFluidDriver {
    */
   void ComputeHBOperator();
 
+ public:
   /*!
-   * \brief Update the solution for the Harmonic Balance.
+   * \brief Constructor of the class.
+   * \param[in] confFile - Configuration file name.
+   * \param[in] val_nZone - Total number of zones.
+   * \param[in] MPICommunicator - MPI communicator for SU2.
    */
-  void Update() override;
+  CHBDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator);
+
+  /*!
+   * \brief Destructor of the class.
+   */
+  ~CHBDriver(void) override;
+
+  /*!
+   * \brief Run a single iteration of a Harmonic Balance problem.
+   */
+  void Run() override;
 
   /*!
-   * \brief Reset the convergence flag (set to false) of the solver for the Harmonic Balance.
+   * \brief Update the solution for the Harmonic Balance.
    */
-  void ResetConvergence() override;
+  void Update() override;
 };
diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index 96595b365f5..4e79537a829 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -92,26 +92,11 @@ class CDriverBase {
    */
   virtual ~CDriverBase(void);
 
-  /*!
-   * \brief A virtual member.
-   */
-  virtual void Preprocessing(){}
-
   /*!
    * \brief A virtual member.
    */
   virtual void Run(){}
 
-  /*!
-   * \brief A virtual member.
-   */
-  virtual void Update(){}
-
-  /*!
-   * \brief A virtual member.
-   */
-  virtual void Output(){}
-
   /*!
    * \brief A virtual member.
    */
diff --git a/SU2_CFD/include/drivers/CMultizoneDriver.hpp b/SU2_CFD/include/drivers/CMultizoneDriver.hpp
index e1f9d05dd9a..8106db28174 100644
--- a/SU2_CFD/include/drivers/CMultizoneDriver.hpp
+++ b/SU2_CFD/include/drivers/CMultizoneDriver.hpp
@@ -57,6 +57,43 @@ class CMultizoneDriver : public CDriver {
 
   bool *prefixed_motion;     /*!< \brief Determines if a fixed motion is imposed in the config file. */
 
+  /*!
+   * \brief Perform a dynamic mesh deformation, including grid velocity computation and update of the multigrid structure.
+   */
+  void DynamicMeshUpdate(unsigned short val_iZone, unsigned long TimeIter);
+
+  /*!
+   * \brief Use a corrector step to prevent convergence issues.
+   */
+  void Corrector(unsigned short val_iZone);
+
+  /*!
+   * \brief Run a Block Gauss-Seidel iteration in all physical zones.
+   */
+  void RunGaussSeidel();
+
+  /*!
+   * \brief Run a Block-Jacobi iteration in all physical zones.
+   */
+  void RunJacobi();
+
+  /*!
+   * \brief Routine to provide all the desired physical transfers between the different zones during one iteration.
+   * \return Boolean that determines whether the mesh needs to be updated for this particular transfer
+   */
+  bool TransferData(unsigned short donorZone, unsigned short targetZone);
+
+  /*!
+   * \brief Check the convergence at the outer level.
+   */
+  bool OuterConvergence(unsigned long OuterIter);
+
+  /*!
+   * \brief  Returns whether all specified windowed-time-averaged ouputs have been converged
+   * \return Boolean indicating whether the problem is converged.
+   */
+  virtual bool GetTimeConvergence() const;
+
 public:
 
   /*!
@@ -84,19 +121,6 @@ class CMultizoneDriver : public CDriver {
    */
   void Preprocess(unsigned long TimeIter) override;
 
-  /*!
-   * \brief Use a corrector step to prevent convergence issues.
-   */
-  void Corrector(unsigned short val_iZone);
-
-  /*!
-   * \brief Run a Block Gauss-Seidel iteration in all physical zones.
-   */
-  void RunGaussSeidel() override;
-  /*!
-   * \brief Run a Block-Jacobi iteration in all physical zones.
-   */
-  void RunJacobi() override;
   /*!
    * \brief Update the dual-time solution within multiple zones.
    */
@@ -107,37 +131,15 @@ class CMultizoneDriver : public CDriver {
    */
   void Output(unsigned long TimeIter) override;
 
-  /*!
-   * \brief Check the convergence at the outer level.
-   */
-  bool OuterConvergence(unsigned long OuterIter);
-
   /*!
    * \brief Perform a dynamic mesh deformation, included grid velocity computation and the update of the multigrid structure (multiple zone).
    */
   void DynamicMeshUpdate(unsigned long TimeIter) override;
 
-  /*!
-   * \brief Perform a dynamic mesh deformation, including grid velocity computation and update of the multigrid structure.
-   */
-  void DynamicMeshUpdate(unsigned short val_iZone, unsigned long TimeIter) override;
-
-  /*!
-   * \brief Routine to provide all the desired physical transfers between the different zones during one iteration.
-   * \return Boolean that determines whether the mesh needs to be updated for this particular transfer
-   */
-  bool TransferData(unsigned short donorZone, unsigned short targetZone);
-
   /*!
    * \brief Check if simulation converged and return appropriate boolean.
    * \param[in] TimeIter - Current time iteration.
    * \return Boolean that indicates to stop the iteration loop.
    */
   bool Monitor(unsigned long TimeIter) override;
-
-  /*!
-   * \brief  Returns whether all specified windowed-time-averaged ouputs have been converged
-   * \return Boolean indicating whether the problem is converged.
-   */
-  virtual bool GetTimeConvergence() const;
 };
diff --git a/SU2_CFD/include/drivers/CSinglezoneDriver.hpp b/SU2_CFD/include/drivers/CSinglezoneDriver.hpp
index 8f7a11f9ba4..07cc41c2d51 100644
--- a/SU2_CFD/include/drivers/CSinglezoneDriver.hpp
+++ b/SU2_CFD/include/drivers/CSinglezoneDriver.hpp
@@ -41,6 +41,12 @@ class CSinglezoneDriver : public CDriver {
 
   unsigned long TimeIter;
 
+  /*!
+     * \brief  Returns whether all specified windowed-time-averaged ouputs have been converged
+     * \return Boolean indicating whether the problem is converged.
+     */
+  virtual bool GetTimeConvergence() const;
+
 public:
 
   /*!
@@ -104,15 +110,4 @@ class CSinglezoneDriver : public CDriver {
    */
   bool Monitor(unsigned long TimeIter) override;
 
-  /*!
-     * \brief  Returns whether all specified windowed-time-averaged ouputs have been converged
-     * \return Boolean indicating whether the problem is converged.
-     */
-  virtual bool GetTimeConvergence() const;
-
-  /*!
-   * \brief Runtime_Parsing
-   */
-  virtual void RuntimeOptions();
-
 };
diff --git a/SU2_CFD/include/integration/CIntegration.hpp b/SU2_CFD/include/integration/CIntegration.hpp
index a8908178aaf..577d908c8d0 100644
--- a/SU2_CFD/include/integration/CIntegration.hpp
+++ b/SU2_CFD/include/integration/CIntegration.hpp
@@ -48,9 +48,6 @@ class CIntegration {
 protected:
   int rank,      /*!< \brief MPI Rank. */
   size;          /*!< \brief MPI Size. */
-  bool Convergence,   /*!< \brief To indicate if the flow solver (direct, adjoint, or linearized) has converged or not. */
-  Convergence_FSI,    /*!< \brief To indicate if the FSI problem has converged or not. */
-  Convergence_FullMG;  /*!< \brief To indicate if the full multigrid has converged or not. */
 
   /*!
    * \brief Do the space integration of the numerical system.
@@ -88,41 +85,6 @@ class CIntegration {
    */
   virtual ~CIntegration(void) = default;
 
-  /*!
-   * \brief Get the indicator of the convergence for the direct, adjoint and linearized problem.
-   * \return <code>TRUE</code> means that the convergence criteria is satisfied;
-   *         otherwise <code>FALSE</code>.
-   */
-  inline bool GetConvergence(void) const { return Convergence; }
-
-  /*!
-   * \brief Get the indicator of the convergence for the Fluid-Structure Interaction problem.
-   * \return <code>TRUE</code> means that the convergence criteria is satisfied;
-   *         otherwise <code>FALSE</code>.
-   */
-  inline bool GetConvergence_FSI(void) const { return Convergence_FSI; }
-
-  /*!
-   * \brief Set the indicator of the convergence.
-   * \param[in] value - <code>TRUE</code> means that the convergence criteria is satisfied;
-   *            otherwise <code>FALSE</code>.
-   */
-  inline void SetConvergence(bool value) { Convergence = value; }
-
-  /*!
-   * \brief Set the indicator of the convergence for FSI.
-   * \param[in] valueFSI - <code>TRUE</code> means that the convergence criteria for FSI is satisfied;
-   *            otherwise <code>FALSE</code>.
-   */
-  inline void SetConvergence_FSI(bool valueFSI) { Convergence_FSI = valueFSI; }
-
-  /*!
-   * \brief Get the indicator of the convergence for the full multigrid problem.
-   * \return <code>TRUE</code> means that the convergence criteria is satisfied;
-   *         otherwise <code>FALSE</code>.
-   */
-  inline bool GetConvergence_FullMG(void) const { return Convergence_FullMG; }
-
   /*!
    * \brief Save the geometry at different time steps.
    * \param[in] geometry - Geometrical definition of the problem.
diff --git a/SU2_CFD/include/iteration/CDiscAdjFluidIteration.hpp b/SU2_CFD/include/iteration/CDiscAdjFluidIteration.hpp
index 65c37ad3c9b..6bf38d45af0 100644
--- a/SU2_CFD/include/iteration/CDiscAdjFluidIteration.hpp
+++ b/SU2_CFD/include/iteration/CDiscAdjFluidIteration.hpp
@@ -94,25 +94,6 @@ class CDiscAdjFluidIteration final : public CIteration {
   void IterateDiscAdj(CGeometry**** geometry, CSolver***** solver, CConfig** config,
                       unsigned short val_iZone, unsigned short val_iInst, bool CrossTerm) override;
 
-  /*!
-   * \brief Updates the containers for the discrete adjoint fluid system.
-   * \param[in] output - Pointer to the COutput class.
-   * \param[in] integration - Container vector with all the integration methods.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] solver - Container vector with all the solutions.
-   * \param[in] numerics - Description of the numerical method (the way in which the equations are solved).
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] surface_movement - Surface movement classes of the problem.
-   * \param[in] grid_movement - Volume grid movement classes of the problem.
-   * \param[in] FFDBox - FFD FFDBoxes of the problem.
-   * \param[in] val_iZone - Index of the zone.
-   * \param[in] val_iInst - Index of the instance
-   */
-  void Update(COutput* output, CIntegration**** integration, CGeometry**** geometry, CSolver***** solver,
-              CNumerics****** numerics, CConfig** config, CSurfaceMovement** surface_movement,
-              CVolumetricMovement*** grid_movement, CFreeFormDefBox*** FFDBox, unsigned short val_iZone,
-              unsigned short val_iInst) override;
-
   /*!
    * \brief Monitors the convergence and other metrics for the discrete adjoint fluid system.
    * \param[in] output - Pointer to the COutput class.
diff --git a/SU2_CFD/include/iteration/CDiscAdjHeatIteration.hpp b/SU2_CFD/include/iteration/CDiscAdjHeatIteration.hpp
index c5d0c0c2b02..390c5ba6a54 100644
--- a/SU2_CFD/include/iteration/CDiscAdjHeatIteration.hpp
+++ b/SU2_CFD/include/iteration/CDiscAdjHeatIteration.hpp
@@ -88,25 +88,6 @@ class CDiscAdjHeatIteration final : public CIteration {
   void IterateDiscAdj(CGeometry**** geometry, CSolver***** solver, CConfig** config,
                       unsigned short val_iZone, unsigned short val_iInst, bool CrossTerm) override;
 
-  /*!
-   * \brief Perform a single iteration of the adjoint heat problem.
-   * \param[in] output - Pointer to the COutput class.
-   * \param[in] integration - Container vector with all the integration methods.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] solver - Container vector with all the solutions.
-   * \param[in] numerics - Description of the numerical method (the way in which the equations are solved).
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] surface_movement - Surface movement classes of the problem.
-   * \param[in] grid_movement - Volume grid movement classes of the problem.
-   * \param[in] FFDBox - FFD FFDBoxes of the problem.
-   * \param[in] val_iZone - Index of the zone.
-   * \param[in] val_iInst - Index of the instance layer.
-   */
-  void Update(COutput* output, CIntegration**** integration, CGeometry**** geometry, CSolver***** solver,
-              CNumerics****** numerics, CConfig** config, CSurfaceMovement** surface_movement,
-              CVolumetricMovement*** grid_movement, CFreeFormDefBox*** FFDBox, unsigned short val_iZone,
-              unsigned short val_iInst) override;
-
   /*!
    * \brief Monitors the convergence and other metrics for the discrete adjoint heat problem.
    */
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index fb788d47eb5..457162bf12b 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -1044,8 +1044,7 @@ void CDriver::InitializeSolver(CConfig* config, CGeometry** geometry, CSolver **
 
 }
 
-void CDriver::PreprocessInlet(CSolver ***solver, CGeometry **geometry,
-                                  CConfig *config) const {
+void CDriver::PreprocessInlet(CSolver ***solver, CGeometry **geometry, CConfig *config) const {
 
   /*--- Adjust iteration number for unsteady restarts. ---*/
 
@@ -3018,7 +3017,7 @@ void CFluidDriver::Preprocess(unsigned long Iter) {
 
 void CFluidDriver::Run() {
 
-  unsigned short iZone, jZone, checkConvergence;
+  unsigned short iZone, jZone;
   unsigned long IntIter, nIntIter;
   bool unsteady;
 
@@ -3070,15 +3069,7 @@ void CFluidDriver::Run() {
                                                   config_container, surface_movement, grid_movement, FFDBox, iZone, INST_0);
     }
 
-    /*--- Check convergence in each zone --*/
-
-    checkConvergence = 0;
-    for (iZone = 0; iZone < nZone; iZone++)
-    checkConvergence += (int) integration_container[iZone][INST_0][FLOW_SOL]->GetConvergence();
-
-    /*--- If convergence was reached in every zone --*/
-
-  if (checkConvergence == nZone) break;
+    /// TODO: Check convergence in each zone.
   }
 
 }
@@ -3143,22 +3134,7 @@ bool CFluidDriver::Monitor(unsigned long ExtIter) {
   /*--- Check whether the current simulation has reached the specified
    convergence criteria, and set StopCalc to true, if so. ---*/
 
-  switch (config_container[ZONE_0]->GetKind_Solver()) {
-    case MAIN_SOLVER::EULER: case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::RANS:
-    case MAIN_SOLVER::NEMO_EULER: case MAIN_SOLVER::NEMO_NAVIER_STOKES:
-      StopCalc = integration_container[ZONE_0][INST_0][FLOW_SOL]->GetConvergence(); break;
-    case MAIN_SOLVER::HEAT_EQUATION:
-      StopCalc = integration_container[ZONE_0][INST_0][HEAT_SOL]->GetConvergence(); break;
-    case MAIN_SOLVER::FEM_ELASTICITY:
-      StopCalc = integration_container[ZONE_0][INST_0][FEA_SOL]->GetConvergence(); break;
-    case MAIN_SOLVER::ADJ_EULER: case MAIN_SOLVER::ADJ_NAVIER_STOKES: case MAIN_SOLVER::ADJ_RANS:
-    case MAIN_SOLVER::DISC_ADJ_EULER: case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_RANS:
-    case MAIN_SOLVER::DISC_ADJ_INC_EULER: case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_INC_RANS:
-    case MAIN_SOLVER::DISC_ADJ_FEM_EULER: case MAIN_SOLVER::DISC_ADJ_FEM_NS: case MAIN_SOLVER::DISC_ADJ_FEM_RANS:
-      StopCalc = integration_container[ZONE_0][INST_0][ADJFLOW_SOL]->GetConvergence(); break;
-    default:
-      break;
-  }
+  /// TODO: Get convergence from the output class
 
   /*--- Set StopCalc to true if max. number of iterations has been reached ---*/
 
@@ -3401,25 +3377,10 @@ bool CTurbomachineryDriver::Monitor(unsigned long ExtIter) {
     }
   }
 
-
   /*--- Check whether the current simulation has reached the specified
    convergence criteria, and set StopCalc to true, if so. ---*/
 
-  switch (config_container[ZONE_0]->GetKind_Solver()) {
-  case MAIN_SOLVER::EULER: case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::RANS:
-  case MAIN_SOLVER::INC_EULER: case MAIN_SOLVER::INC_NAVIER_STOKES: case MAIN_SOLVER::INC_RANS:
-  case MAIN_SOLVER::NEMO_EULER: case MAIN_SOLVER::NEMO_NAVIER_STOKES:
-    StopCalc = integration_container[ZONE_0][INST_0][FLOW_SOL]->GetConvergence();
-    break;
-  case MAIN_SOLVER::DISC_ADJ_EULER: case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_RANS:
-  case MAIN_SOLVER::DISC_ADJ_INC_EULER: case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_INC_RANS:
-  case MAIN_SOLVER::DISC_ADJ_FEM_EULER: case MAIN_SOLVER::DISC_ADJ_FEM_NS: case MAIN_SOLVER::DISC_ADJ_FEM_RANS:
-    StopCalc = integration_container[ZONE_0][INST_0][ADJFLOW_SOL]->GetConvergence();
-    break;
-  default:
-    break;
-
-  }
+  /// TODO: Get convergence from the output class
 
   /*--- Set StopCalc to true if max. number of iterations has been reached ---*/
 
@@ -3531,34 +3492,6 @@ void CHBDriver::Update() {
 
 }
 
-void CHBDriver::ResetConvergence() {
-
-  for(iInst = 0; iInst < nZone; iInst++) {
-    switch (config_container[ZONE_0]->GetKind_Solver()) {
-
-    case MAIN_SOLVER::EULER: case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::RANS:
-      integration_container[ZONE_0][iInst][FLOW_SOL]->SetConvergence(false);
-      if (config_container[ZONE_0]->GetKind_Solver() == MAIN_SOLVER::RANS) integration_container[ZONE_0][iInst][TURB_SOL]->SetConvergence(false);
-      if(config_container[ZONE_0]->GetKind_Trans_Model() == TURB_TRANS_MODEL::LM) integration_container[ZONE_0][iInst][TRANS_SOL]->SetConvergence(false);
-      break;
-
-    case MAIN_SOLVER::FEM_ELASTICITY:
-      integration_container[ZONE_0][iInst][FEA_SOL]->SetConvergence(false);
-      break;
-
-    case MAIN_SOLVER::ADJ_EULER: case MAIN_SOLVER::ADJ_NAVIER_STOKES: case MAIN_SOLVER::ADJ_RANS: case MAIN_SOLVER::DISC_ADJ_EULER: case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_RANS:
-      integration_container[ZONE_0][iInst][ADJFLOW_SOL]->SetConvergence(false);
-      if( (config_container[ZONE_0]->GetKind_Solver() == MAIN_SOLVER::ADJ_RANS) || (config_container[ZONE_0]->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_RANS) )
-        integration_container[ZONE_0][iInst][ADJTURB_SOL]->SetConvergence(false);
-      break;
-
-    default:
-      SU2_MPI::Error("Harmonic Balance has not been set up for this solver.", CURRENT_FUNCTION);
-    }
-  }
-
-}
-
 void CHBDriver::SetHarmonicBalance(unsigned short iInst) {
 
   unsigned short iVar, jInst, iMGlevel;
diff --git a/SU2_CFD/src/drivers/CMultizoneDriver.cpp b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
index a1de120c8a8..4bd72f6752f 100644
--- a/SU2_CFD/src/drivers/CMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
@@ -443,13 +443,6 @@ void CMultizoneDriver::Update() {
     iteration_container[iZone][INST_0]->Update(output_container[iZone], integration_container, geometry_container,
         solver_container, numerics_container, config_container,
         surface_movement, grid_movement, FFDBox, iZone, INST_0);
-
-    /*--- Set the Convergence_FSI boolean to false for the next time step ---*/
-    for (unsigned short iSol = 0; iSol < MAX_SOLS-1; iSol++){
-      if (integration_container[iZone][INST_0][iSol] != nullptr){
-        integration_container[iZone][INST_0][iSol]->SetConvergence_FSI(false);
-      }
-    }
   }
 
 }
@@ -611,9 +604,9 @@ bool CMultizoneDriver::Monitor(unsigned long TimeIter){
     const bool MaxIterationsReached = (OuterIter+1 >= nOuterIter);
 
     if ((MaxIterationsReached || InnerConvergence) && (rank == MASTER_NODE)) {
-      cout << endl << "----------------------------- Solver Exit -------------------------------" << endl;
+      cout << "\n----------------------------- Solver Exit -------------------------------" << endl;
       if (InnerConvergence) cout << "All convergence criteria satisfied." << endl;
-      else cout << endl << "Maximum number of iterations reached (OUTER_ITER = " << OuterIter+1 << ") before convergence." << endl;
+      else cout << "\nMaximum number of iterations reached (OUTER_ITER = " << OuterIter+1 << ") before convergence." << endl;
       driver_output->PrintConvergenceSummary();
       cout << "-------------------------------------------------------------------------" << endl;
     }
@@ -633,10 +626,10 @@ bool CMultizoneDriver::Monitor(unsigned long TimeIter){
     const bool MaxIterationsReached = (TimeIter+1 >= nTimeIter);
 
     if ((TimeConvergence || FinalTimeReached || MaxIterationsReached) && (rank == MASTER_NODE)){
-      cout << endl << "----------------------------- Solver Exit -------------------------------";
-      if (TimeConvergence)  cout << endl << "All windowed time-averaged convergence criteria are fullfilled." << endl;
-      if (FinalTimeReached) cout << endl << "Maximum time reached (MAX_TIME = " << MaxTime << "s)." << endl;
-      else cout << endl << "Maximum number of time iterations reached (TIME_ITER = " << nTimeIter << ")." << endl;
+      cout << "\n----------------------------- Solver Exit -------------------------------";
+      if (TimeConvergence)  cout << "\nAll windowed time-averaged convergence criteria are fullfilled." << endl;
+      if (FinalTimeReached) cout << "\nMaximum time reached (MAX_TIME = " << MaxTime << "s)." << endl;
+      else cout << "\nMaximum number of time iterations reached (TIME_ITER = " << nTimeIter << ")." << endl;
       cout << "-------------------------------------------------------------------------" << endl;
     }
 
@@ -646,5 +639,5 @@ bool CMultizoneDriver::Monitor(unsigned long TimeIter){
 }
 
 bool CMultizoneDriver::GetTimeConvergence() const{
-    return output_container[ZONE_0]->GetCauchyCorrectedTimeConvergence(config_container[ZONE_0]);
+  return output_container[ZONE_0]->GetCauchyCorrectedTimeConvergence(config_container[ZONE_0]);
 }
diff --git a/SU2_CFD/src/drivers/CSinglezoneDriver.cpp b/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
index 8289409a44f..73668884259 100644
--- a/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
@@ -112,10 +112,6 @@ void CSinglezoneDriver::StartSolver() {
 
 void CSinglezoneDriver::Preprocess(unsigned long TimeIter) {
 
-  /*--- Set runtime option ---*/
-
-  RuntimeOptions();
-
   /*--- Set the current time iteration in the config ---*/
 
   config_container[ZONE_0]->SetTimeIter(TimeIter);
@@ -262,13 +258,13 @@ bool CSinglezoneDriver::Monitor(unsigned long TimeIter){
 
   if (TimeDomain == NO){
 
-    InnerConvergence     = output_container[ZONE_0]->GetConvergence();
+    InnerConvergence = output_container[ZONE_0]->GetConvergence();
     MaxIterationsReached = InnerIter+1 >= nInnerIter;
 
     if ((MaxIterationsReached || InnerConvergence) && (rank == MASTER_NODE)) {
-      cout << endl << "----------------------------- Solver Exit -------------------------------" << endl;
+      cout << "\n----------------------------- Solver Exit -------------------------------" << endl;
       if (InnerConvergence) cout << "All convergence criteria satisfied." << endl;
-      else cout << endl << "Maximum number of iterations reached (ITER = " << nInnerIter << ") before convergence." << endl;
+      else cout << "\nMaximum number of iterations reached (ITER = " << nInnerIter << ") before convergence." << endl;
       output_container[ZONE_0]->PrintConvergenceSummary();
       cout << "-------------------------------------------------------------------------" << endl;
     }
@@ -276,25 +272,23 @@ bool CSinglezoneDriver::Monitor(unsigned long TimeIter){
     StopCalc = MaxIterationsReached || InnerConvergence;
   }
 
-
-
   if (TimeDomain == YES) {
 
     /*--- Check whether the outer time integration has reached the final time ---*/
 
     TimeConvergence = GetTimeConvergence();
 
-    FinalTimeReached     = CurTime >= MaxTime;
+    FinalTimeReached = CurTime >= MaxTime;
     MaxIterationsReached = TimeIter+1 >= nTimeIter;
 
     if ((FinalTimeReached || MaxIterationsReached || TimeConvergence) && (rank == MASTER_NODE)){
-      cout << endl << "----------------------------- Solver Exit -------------------------------";
-      if (TimeConvergence)     cout << endl << "All windowed time-averaged convergence criteria are fullfilled." << endl;
-      if (FinalTimeReached)     cout << endl << "Maximum time reached (MAX_TIME = " << MaxTime << "s)." << endl;
-      if (MaxIterationsReached) cout << endl << "Maximum number of time iterations reached (TIME_ITER = " << nTimeIter << ")." << endl;
+      cout << "\n----------------------------- Solver Exit -------------------------------";
+      if (TimeConvergence) cout << "\nAll windowed time-averaged convergence criteria are fullfilled." << endl;
+      if (FinalTimeReached) cout << "\nMaximum time reached (MAX_TIME = " << MaxTime << "s)." << endl;
+      if (MaxIterationsReached) cout << "\nMaximum number of time iterations reached (TIME_ITER = " << nTimeIter << ")." << endl;
       cout << "-------------------------------------------------------------------------" << endl;
     }
-    StopCalc = FinalTimeReached || MaxIterationsReached|| TimeConvergence;
+    StopCalc = FinalTimeReached || MaxIterationsReached || TimeConvergence;
   }
 
   /*--- Reset the inner convergence --- */
@@ -308,23 +302,6 @@ bool CSinglezoneDriver::Monitor(unsigned long TimeIter){
   return StopCalc;
 }
 
-void CSinglezoneDriver::RuntimeOptions(){
-
-  ifstream runtime_configfile;
-
-  /*--- Try to open the runtime config file ---*/
-
-  runtime_configfile.open(runtime_file_name, ios::in);
-
-  /*--- If succeeded create a temporary config object ---*/
-
-  if (runtime_configfile.good()){
-    CConfig *runtime = new CConfig(runtime_file_name, config_container[ZONE_0]);
-    delete runtime;
-  }
-
-}
-
 bool CSinglezoneDriver::GetTimeConvergence() const{
   return output_container[ZONE_0]->GetCauchyCorrectedTimeConvergence(config_container[ZONE_0]);
 }
diff --git a/SU2_CFD/src/integration/CIntegration.cpp b/SU2_CFD/src/integration/CIntegration.cpp
index 347e5b4a4b3..1da64f36a32 100644
--- a/SU2_CFD/src/integration/CIntegration.cpp
+++ b/SU2_CFD/src/integration/CIntegration.cpp
@@ -32,9 +32,6 @@
 CIntegration::CIntegration() {
   rank = SU2_MPI::GetRank();
   size = SU2_MPI::GetSize();
-  Convergence = false;
-  Convergence_FSI = false;
-  Convergence_FullMG = false;
 }
 
 void CIntegration::Space_Integration(CGeometry *geometry,
diff --git a/SU2_CFD/src/integration/CMultiGridIntegration.cpp b/SU2_CFD/src/integration/CMultiGridIntegration.cpp
index 36c75cb525f..c3b8df8401b 100644
--- a/SU2_CFD/src/integration/CMultiGridIntegration.cpp
+++ b/SU2_CFD/src/integration/CMultiGridIntegration.cpp
@@ -83,6 +83,9 @@ void CMultiGridIntegration::MultiGrid_Iteration(CGeometry ****geometry,
 
   unsigned short FinestMesh = config[iZone]->GetFinestMesh();
 
+  /// TODO: This was always false.
+  const bool Convergence_FullMG = false;
+
   if (!config[iZone]->GetRestart() && FullMG && direct && ( Convergence_FullMG && (FinestMesh != MESH_0 ))) {
 
     SetProlongated_Solution(RunTime_EqSystem,
diff --git a/SU2_CFD/src/iteration/CAdjFluidIteration.cpp b/SU2_CFD/src/iteration/CAdjFluidIteration.cpp
index 282223b46ad..c3c0cce8a02 100644
--- a/SU2_CFD/src/iteration/CAdjFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CAdjFluidIteration.cpp
@@ -162,17 +162,13 @@ void CAdjFluidIteration::Update(COutput* output, CIntegration**** integration, C
                                 CSolver***** solver, CNumerics****** numerics, CConfig** config,
                                 CSurfaceMovement** surface_movement, CVolumetricMovement*** grid_movement,
                                 CFreeFormDefBox*** FFDBox, unsigned short val_iZone, unsigned short val_iInst) {
-  su2double Physical_dt, Physical_t;
-  unsigned short iMesh;
-  unsigned long TimeIter = config[ZONE_0]->GetTimeIter();
-
   /*--- Dual time stepping strategy ---*/
 
   if ((config[val_iZone]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
       (config[val_iZone]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND)) {
     /*--- Update dual time solver ---*/
 
-    for (iMesh = 0; iMesh <= config[val_iZone]->GetnMGLevels(); iMesh++) {
+    for (unsigned short iMesh = 0; iMesh <= config[val_iZone]->GetnMGLevels(); iMesh++) {
       integration[val_iZone][val_iInst][ADJFLOW_SOL]->SetDualTime_Solver(
           geometry[val_iZone][val_iInst][iMesh], solver[val_iZone][val_iInst][iMesh][ADJFLOW_SOL], config[val_iZone],
           iMesh);
@@ -180,13 +176,6 @@ void CAdjFluidIteration::Update(COutput* output, CIntegration**** integration, C
       integration[val_iZone][val_iInst][ADJFLOW_SOL]->SetDualTime_Geometry(
           geometry[val_iZone][val_iInst][iMesh], solver[val_iZone][val_iInst][iMesh][MESH_SOL], config[val_iZone],
           iMesh);
-
-      integration[val_iZone][val_iInst][ADJFLOW_SOL]->SetConvergence(false);
     }
-
-    Physical_dt = config[val_iZone]->GetDelta_UnstTime();
-    Physical_t = (TimeIter + 1) * Physical_dt;
-    if (Physical_t >= config[val_iZone]->GetTotal_UnstTime())
-      integration[val_iZone][val_iInst][ADJFLOW_SOL]->SetConvergence(true);
   }
 }
diff --git a/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
index 34cc6a94e7c..6e10e9df4fc 100644
--- a/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
@@ -609,20 +609,6 @@ void CDiscAdjFluidIteration::RegisterOutput(CSolver***** solver, CGeometry**** g
   END_SU2_OMP_PARALLEL
 }
 
-void CDiscAdjFluidIteration::Update(COutput* output, CIntegration**** integration, CGeometry**** geometry,
-                                    CSolver***** solver, CNumerics****** numerics, CConfig** config,
-                                    CSurfaceMovement** surface_movement, CVolumetricMovement*** grid_movement,
-                                    CFreeFormDefBox*** FFDBox, unsigned short iZone, unsigned short iInst) {
-  /*--- Dual time stepping strategy ---*/
-
-  if ((config[iZone]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
-      (config[iZone]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND)) {
-    for (unsigned short iMesh = 0; iMesh <= config[iZone]->GetnMGLevels(); iMesh++) {
-      integration[iZone][iInst][ADJFLOW_SOL]->SetConvergence(false);
-    }
-  }
-}
-
 bool CDiscAdjFluidIteration::Monitor(COutput* output, CIntegration**** integration, CGeometry**** geometry,
                                      CSolver***** solver, CNumerics****** numerics, CConfig** config,
                                      CSurfaceMovement** surface_movement, CVolumetricMovement*** grid_movement,
diff --git a/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
index 572ea54c49e..a12cb43bdc0 100644
--- a/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
@@ -232,21 +232,6 @@ void CDiscAdjHeatIteration::RegisterOutput(CSolver***** solver, CGeometry**** ge
   solver[iZone][iInst][MESH_0][ADJHEAT_SOL]->RegisterOutput(geometry[iZone][iInst][MESH_0], config[iZone]);
 }
 
-void CDiscAdjHeatIteration::Update(COutput* output, CIntegration**** integration, CGeometry**** geometry,
-                                   CSolver***** solver, CNumerics****** numerics, CConfig** config,
-                                   CSurfaceMovement** surface_movement, CVolumetricMovement*** grid_movement,
-                                   CFreeFormDefBox*** FFDBox, unsigned short val_iZone, unsigned short val_iInst) {
-
-  /*--- Dual time stepping strategy ---*/
-
-  if ((config[val_iZone]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
-      (config[val_iZone]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND)) {
-    for (auto iMesh = 0u; iMesh <= config[val_iZone]->GetnMGLevels(); iMesh++) {
-      integration[val_iZone][val_iInst][ADJHEAT_SOL]->SetConvergence(false);
-    }
-  }
-}
-
 bool CDiscAdjHeatIteration::Monitor(COutput* output, CIntegration**** integration, CGeometry**** geometry,
                                     CSolver***** solver, CNumerics****** numerics, CConfig** config,
                                     CSurfaceMovement** surface_movement, CVolumetricMovement*** grid_movement,
diff --git a/SU2_CFD/src/iteration/CFEAIteration.cpp b/SU2_CFD/src/iteration/CFEAIteration.cpp
index 45ded06c7ee..c827f28467e 100644
--- a/SU2_CFD/src/iteration/CFEAIteration.cpp
+++ b/SU2_CFD/src/iteration/CFEAIteration.cpp
@@ -48,9 +48,6 @@ void CFEAIteration::Iterate(COutput* output, CIntegration**** integration, CGeom
   CIntegration* feaIntegration = integration[val_iZone][val_iInst][FEA_SOL];
   CSolver* feaSolver = solver[val_iZone][val_iInst][MESH_0][FEA_SOL];
 
-  /*--- Set the convergence monitor to false, to prevent the solver to stop in intermediate FSI subiterations ---*/
-  feaIntegration->SetConvergence(false);
-
   /*--- FEA equations ---*/
   config[val_iZone]->SetGlobalParam(MAIN_SOLVER::FEM_ELASTICITY, RUNTIME_FEA_SYS);
 
@@ -187,7 +184,6 @@ void CFEAIteration::Update(COutput* output, CIntegration**** integration, CGeome
                            CNumerics****** numerics, CConfig** config, CSurfaceMovement** surface_movement,
                            CVolumetricMovement*** grid_movement, CFreeFormDefBox*** FFDBox, unsigned short val_iZone,
                            unsigned short val_iInst) {
-  const auto TimeIter = config[val_iZone]->GetTimeIter();
   const bool dynamic = (config[val_iZone]->GetTime_Domain());
   const bool fsi = config[val_iZone]->GetFSI_Simulation();
 
@@ -199,14 +195,6 @@ void CFEAIteration::Update(COutput* output, CIntegration**** integration, CGeome
     integration[val_iZone][val_iInst][FEA_SOL]->SetDualTime_Solver(
         geometry[val_iZone][val_iInst][MESH_0], solver[val_iZone][val_iInst][MESH_0][FEA_SOL], config[val_iZone],
         MESH_0);
-    integration[val_iZone][val_iInst][FEA_SOL]->SetConvergence(false);
-
-    /*--- Verify convergence criteria (based on total time) ---*/
-
-    const su2double Physical_dt = config[val_iZone]->GetDelta_DynTime();
-    const su2double Physical_t = (TimeIter + 1) * Physical_dt;
-    if (Physical_t >= config[val_iZone]->GetTotal_DynTime())
-      integration[val_iZone][val_iInst][FEA_SOL]->SetConvergence(true);
 
   } else if (fsi) {
     /*--- For FSI problems, output the relaxed result, which is the one transferred into the fluid domain (for restart
@@ -272,7 +260,4 @@ void CFEAIteration::Solve(COutput* output, CIntegration**** integration, CGeomet
   if (multizone && !config[val_iZone]->GetTime_Domain()) {
     Output(output, geometry, solver, config, config[val_iZone]->GetOuterIter(), false, val_iZone, val_iInst);
   }
-
-  /*--- Set the structural convergence to false (to make sure outer subiterations converge) ---*/
-  integration[val_iZone][val_iInst][FEA_SOL]->SetConvergence(false);
 }
diff --git a/SU2_CFD/src/iteration/CFluidIteration.cpp b/SU2_CFD/src/iteration/CFluidIteration.cpp
index db2192f6442..7d2fa63b74f 100644
--- a/SU2_CFD/src/iteration/CFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CFluidIteration.cpp
@@ -171,8 +171,6 @@ void CFluidIteration::Update(COutput* output, CIntegration**** integration, CGeo
       integration[val_iZone][val_iInst][FLOW_SOL]->SetDualTime_Geometry(geometry[val_iZone][val_iInst][iMesh],
                                                                         solver[val_iZone][val_iInst][iMesh][MESH_SOL],
                                                                         config[val_iZone], iMesh);
-
-      integration[val_iZone][val_iInst][FLOW_SOL]->SetConvergence(false);
     }
 
     SetDualTime_Aeroelastic(config[val_iZone]);
@@ -185,7 +183,6 @@ void CFluidIteration::Update(COutput* output, CIntegration**** integration, CGeo
       integration[val_iZone][val_iInst][TURB_SOL]->SetDualTime_Solver(geometry[val_iZone][val_iInst][MESH_0],
                                                                       solver[val_iZone][val_iInst][MESH_0][TURB_SOL],
                                                                       config[val_iZone], MESH_0);
-      integration[val_iZone][val_iInst][TURB_SOL]->SetConvergence(false);
     }
 
     /*--- Update dual time solver for the transition model ---*/
@@ -194,7 +191,6 @@ void CFluidIteration::Update(COutput* output, CIntegration**** integration, CGeo
       integration[val_iZone][val_iInst][TRANS_SOL]->SetDualTime_Solver(geometry[val_iZone][val_iInst][MESH_0],
                                                                        solver[val_iZone][val_iInst][MESH_0][TRANS_SOL],
                                                                        config[val_iZone], MESH_0);
-      integration[val_iZone][val_iInst][TRANS_SOL]->SetConvergence(false);
     }
 
     /*--- Update dual time solver for the weakly coupled energy equation ---*/
@@ -203,7 +199,6 @@ void CFluidIteration::Update(COutput* output, CIntegration**** integration, CGeo
       integration[val_iZone][val_iInst][HEAT_SOL]->SetDualTime_Solver(geometry[val_iZone][val_iInst][MESH_0],
                                                                       solver[val_iZone][val_iInst][MESH_0][HEAT_SOL],
                                                                       config[val_iZone], MESH_0);
-      integration[val_iZone][val_iInst][HEAT_SOL]->SetConvergence(false);
     }
   }
 }
@@ -296,15 +291,6 @@ void CFluidIteration::Solve(COutput* output, CIntegration**** integration, CGeom
 
   if (multizone && steady) {
     Output(output, geometry, solver, config, config[val_iZone]->GetOuterIter(), StopCalc, val_iZone, val_iInst);
-
-    /*--- Set the convergence to false (to make sure outer subiterations converge) ---*/
-
-    if (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::HEAT_EQUATION) {
-      integration[val_iZone][INST_0][HEAT_SOL]->SetConvergence(false);
-    }
-    else {
-      integration[val_iZone][INST_0][FLOW_SOL]->SetConvergence(false);
-    }
   }
 }
 
diff --git a/SU2_CFD/src/iteration/CHeatIteration.cpp b/SU2_CFD/src/iteration/CHeatIteration.cpp
index e90bcde5144..45c8d6f8e68 100644
--- a/SU2_CFD/src/iteration/CHeatIteration.cpp
+++ b/SU2_CFD/src/iteration/CHeatIteration.cpp
@@ -58,8 +58,6 @@ void CHeatIteration::Update(COutput* output, CIntegration**** integration, CGeom
       integration[val_iZone][val_iInst][HEAT_SOL]->SetDualTime_Geometry(geometry[val_iZone][val_iInst][iMesh],
                                                                         solver[val_iZone][val_iInst][iMesh][MESH_SOL],
                                                                         config[val_iZone], iMesh);
-
-      integration[val_iZone][val_iInst][HEAT_SOL]->SetConvergence(false);
     }
   }
 }
diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index 1d7bfb5bb67..3626baaae5a 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -101,49 +101,6 @@ void CDriver::SetInletAngle(unsigned short iMarker, passivedouble alpha) {
 /* Functions related to simulation control, high level functions (reset convergence, set initial mesh, etc.)   */
 /////////////////////////////////////////////////////////////////////////////////////////////////////////////////
 
-void CDriver::ResetConvergence() {
-  for (auto iZone = 0u; iZone < nZone; iZone++) {
-    switch (main_config->GetKind_Solver()) {
-      case MAIN_SOLVER::EULER:
-      case MAIN_SOLVER::NAVIER_STOKES:
-      case MAIN_SOLVER::RANS:
-      case MAIN_SOLVER::INC_EULER:
-      case MAIN_SOLVER::INC_NAVIER_STOKES:
-      case MAIN_SOLVER::INC_RANS:
-      case MAIN_SOLVER::NEMO_EULER:
-      case MAIN_SOLVER::NEMO_NAVIER_STOKES:
-        integration_container[iZone][INST_0][FLOW_SOL]->SetConvergence(false);
-        if (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::RANS)
-          integration_container[iZone][INST_0][TURB_SOL]->SetConvergence(false);
-        if (config_container[iZone]->GetKind_Trans_Model() == TURB_TRANS_MODEL::LM)
-          integration_container[iZone][INST_0][TRANS_SOL]->SetConvergence(false);
-        break;
-
-      case MAIN_SOLVER::FEM_ELASTICITY:
-        integration_container[iZone][INST_0][FEA_SOL]->SetConvergence(false);
-        break;
-
-      case MAIN_SOLVER::ADJ_EULER:
-      case MAIN_SOLVER::ADJ_NAVIER_STOKES:
-      case MAIN_SOLVER::ADJ_RANS:
-      case MAIN_SOLVER::DISC_ADJ_EULER:
-      case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES:
-      case MAIN_SOLVER::DISC_ADJ_RANS:
-      case MAIN_SOLVER::DISC_ADJ_INC_EULER:
-      case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES:
-      case MAIN_SOLVER::DISC_ADJ_INC_RANS:
-        integration_container[iZone][INST_0][ADJFLOW_SOL]->SetConvergence(false);
-        if ((config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::ADJ_RANS) ||
-            (config_container[iZone]->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_RANS))
-          integration_container[iZone][INST_0][ADJTURB_SOL]->SetConvergence(false);
-        break;
-
-      default:
-        break;
-    }
-  }
-}
-
 void CSinglezoneDriver::SetInitialMesh() {
   DynamicMeshUpdate(0);
 
diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index 24d640e30fb..cfdd8830d88 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -48,30 +48,15 @@ class CDeformationDriver : public CDriverBase {
    */
   CDeformationDriver(char* confFile, SU2_Comm MPICommunicator);
 
-  /*!
-   * \brief Preprocess the driver data.
-   */
-  void Preprocess();
-
   /*!
    * \brief Launch the driver computation.
    */
-  void Run();
-
-  /*!
-   * \brief Output the mesh.
-   */
-  void Output();
+  void Run() override;
 
   /*!
    * \brief Deallocation routine.
    */
-  void Finalize();
-
-  /*!
-   * \brief Communicate boundary mesh displacements.
-   */
-  void CommunicateMeshDisplacements(void);
+  void Finalize() override;
 
  protected:
   /*!
@@ -99,13 +84,18 @@ class CDeformationDriver : public CDriverBase {
    */
   void InitializeNumerics();
 
+  /*!
+   * \brief Output the mesh.
+   */
+  void OutputFiles();
+
   /*!
    * \brief Mesh deformation based on linear elasticity solver (CMeshSolver).
    */
-  void Update();
+  void DeformMesh();
 
   /*!
    * \brief Mesh deformation based on legacy implementation.
    */
-  void Update_Legacy();
+  void DeformLegacy();
 };
diff --git a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
index 55c3140348c..93bf81a55c5 100644
--- a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
@@ -52,12 +52,12 @@ class CDiscAdjDeformationDriver : public CDriverBase {
   /*!
    * \brief Launch the driver computation.
    */
-  void Run();
+  void Run() override;
 
   /*!
    * \brief Deallocation routine.
    */
-  void Finalize();
+  void Finalize() override;
 
  protected:
   /*!
diff --git a/SU2_DEF/src/SU2_DEF.cpp b/SU2_DEF/src/SU2_DEF.cpp
index 504e80d9a87..ccf25daf49e 100644
--- a/SU2_DEF/src/SU2_DEF.cpp
+++ b/SU2_DEF/src/SU2_DEF.cpp
@@ -53,10 +53,6 @@ int main(int argc, char* argv[]) {
 
   CDeformationDriver driver(config_file_name, comm);
 
-  /*--- Preprocess the solver data. ---*/
-
-  driver.Preprocess();
-
   /*--- Launch the main external loop of the solver. ---*/
 
   driver.Run();
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 7f40c2d8c9c..914eae2f1c2 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -161,7 +161,7 @@ void CDeformationDriver::InitializeGeometry() {
     /*--- Computational grid preprocessing. ---*/
 
     if (rank == MASTER_NODE)
-      cout << endl << "----------------------- Preprocessing computations ----------------------" << endl;
+      cout << "\n----------------------- Preprocessing computations ----------------------" << endl;
 
     /*--- Compute elements surrounding points, points surrounding points. ---*/
 
@@ -259,8 +259,6 @@ void CDeformationDriver::InitializeNumerics() {
   }
 }
 
-void CDeformationDriver::Preprocess() {}
-
 void CDeformationDriver::Run() {
   /* --- Start measuring computation time. ---*/
 
@@ -268,7 +266,7 @@ void CDeformationDriver::Run() {
 
   /*--- Surface grid deformation using design variables. ---*/
 
-  Update();
+  DeformMesh();
 
   /*--- Synchronization point after a single solver iteration. Compute the wall clock time required. ---*/
 
@@ -286,11 +284,11 @@ void CDeformationDriver::Run() {
 
   /*--- Output the deformed mesh. ---*/
 
-  Output();
+  OutputFiles();
 }
 
-void CDeformationDriver::Update() {
-  if (!driver_config->GetDeform_Mesh()) return Update_Legacy();
+void CDeformationDriver::DeformMesh() {
+  if (!driver_config->GetDeform_Mesh()) return DeformLegacy();
 
   for (iZone = 0; iZone < nZone; iZone++) {
     /*--- Set the stiffness of each element mesh into the mesh numerics. ---*/
@@ -309,7 +307,7 @@ void CDeformationDriver::Update() {
   }
 }
 
-void CDeformationDriver::Update_Legacy() {
+void CDeformationDriver::DeformLegacy() {
   for (iZone = 0; iZone < nZone; iZone++) {
     if (config_container[iZone]->GetDesign_Variable(0) != NO_DEFORMATION) {
       unsigned short nInst_Zone = nInst[iZone];
@@ -471,7 +469,7 @@ void CDeformationDriver::Update_Legacy() {
   }
 }
 
-void CDeformationDriver::Output() {
+void CDeformationDriver::OutputFiles() {
   /*--- Output deformed grid for visualization, if requested (surface and volumetric), in parallel
    requires to move all the data to the master node. ---*/
 
@@ -567,10 +565,3 @@ void CDeformationDriver::Finalize() {
   if (rank == MASTER_NODE)
     cout << "\n------------------------- Exit Success (SU2_DEF) ------------------------" << endl << endl;
 }
-
-void CDeformationDriver::CommunicateMeshDisplacements(void) {
-  solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->InitiateComms(geometry_container[ZONE_0][INST_0][MESH_0],
-                                                                    config_container[ZONE_0], MESH_DISPLACEMENTS);
-  solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->CompleteComms(geometry_container[ZONE_0][INST_0][MESH_0],
-                                                                    config_container[ZONE_0], MESH_DISPLACEMENTS);
-}
diff --git a/SU2_PY/FSI_tools/FSIInterface.py b/SU2_PY/FSI_tools/FSIInterface.py
index fa58b5f901d..176f26c394f 100644
--- a/SU2_PY/FSI_tools/FSIInterface.py
+++ b/SU2_PY/FSI_tools/FSIInterface.py
@@ -2660,7 +2660,6 @@ def UnsteadyFSI(self, FSI_config, FluidSolver, SolidSolver):
                 )
                 self.MPIBarrier()
                 if myid in self.fluidSolverProcessors:
-                    FluidSolver.ResetConvergence()
                     FluidSolver.Run()
                     self.MPIBarrier()
                     FluidSolver.Postprocess()
@@ -2777,7 +2776,6 @@ def SteadyFSI(self, FSI_config, FluidSolver, SolidSolver):
             # --- Fluid solver call for FSI subiteration ---#
 
             if myid in self.fluidSolverProcessors:
-                FluidSolver.ResetConvergence()  # This is setting to zero the convergence in the integrator, important to reset it.
                 # The mesh will be deformed in the context of the preprocessor, there is no need to set the initial
                 # mesh pushing back the solution to avoid spurious velocities, as the velocity is not computed at all
                 self.MPIPrint("\nPerforming static mesh deformation...\n")

From 08290727add5706f9ca1cc575e288b003f9cb015 Mon Sep 17 00:00:00 2001
From: Nijso <bigfootedrockmidget@hotmail.com>
Date: Tue, 4 Apr 2023 13:15:48 +0200
Subject: [PATCH 341/656] Fix writing of multiple inlet profiles when using MPI
 (#1999)

* fix mpi communication for multiple inlet profiles
---
 Common/include/option_structure.hpp         |  2 +-
 SU2_CFD/include/CMarkerProfileReaderFVM.hpp |  2 +
 SU2_CFD/src/CMarkerProfileReaderFVM.cpp     | 93 ++++++++++++++-------
 3 files changed, 68 insertions(+), 29 deletions(-)

diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index 4c934f0612b..cc5b578c011 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -74,7 +74,7 @@ const unsigned int EXIT_DIVERGENCE = 2;   /*!< \brief Exit code (divergence). */
 
 const unsigned int MAX_PARAMETERS = 10;       /*!< \brief Maximum number of parameters for a design variable definition. */
 const unsigned int MAX_NUMBER_PERIODIC = 10;  /*!< \brief Maximum number of periodic boundary conditions. */
-const unsigned int MAX_STRING_SIZE = 200;     /*!< \brief Maximum number of domains. */
+const unsigned int MAX_STRING_SIZE = 400;     /*!< \brief Maximum size of a generic string. */
 const unsigned int MAX_NUMBER_FFD = 15;       /*!< \brief Maximum number of FFDBoxes for the FFD. */
 enum: unsigned int{MAX_SOLS = 13};            /*!< \brief Maximum number of solutions at the same time (dimension of solution container array). */
 const unsigned int MAX_TERMS = 7;             /*!< \brief Maximum number of terms in the numerical equations (dimension of solver container array). */
diff --git a/SU2_CFD/include/CMarkerProfileReaderFVM.hpp b/SU2_CFD/include/CMarkerProfileReaderFVM.hpp
index d44929296e4..5f1d6c6bcad 100644
--- a/SU2_CFD/include/CMarkerProfileReaderFVM.hpp
+++ b/SU2_CFD/include/CMarkerProfileReaderFVM.hpp
@@ -71,6 +71,8 @@ class CMarkerProfileReaderFVM {
 
   vector<unsigned long> numberOfRowsInProfile;  /*!< \brief Auxiliary structure for holding the number of rows for a particular marker in a profile file. */
   vector<unsigned long> numberOfColumnsInProfile;  /*!< \brief Auxiliary structure for holding the number of columns for a particular marker in a profile file. */
+  vector<string> totalColumnNames; /*!< \brief Names of the columns for the profile, one for each inlet marker. */
+  vector<string> totalColumnValues; /*!< \brief Initial values for the profile, constructed from MARKER_INLET. */
 
   vector<vector<passivedouble> > profileData;  /*!< \brief Auxiliary structure for holding the data values from a profile file. */
   vector<vector<vector<su2double> > > profileCoords;  /*!< \brief Data structure for holding the merged inlet boundary coordinates from all ranks. */
diff --git a/SU2_CFD/src/CMarkerProfileReaderFVM.cpp b/SU2_CFD/src/CMarkerProfileReaderFVM.cpp
index cf6090d15c7..71486e2ea07 100644
--- a/SU2_CFD/src/CMarkerProfileReaderFVM.cpp
+++ b/SU2_CFD/src/CMarkerProfileReaderFVM.cpp
@@ -207,6 +207,9 @@ void CMarkerProfileReaderFVM::MergeProfileMarkers() {
   unsigned long index, iChar;
 
   char str_buf[MAX_STRING_SIZE];
+  char name_buf[MAX_STRING_SIZE];
+  char value_buf[MAX_STRING_SIZE];
+
   vector<string> Marker_Tags;
 
   vector<unsigned long> nRowCum_Counter;
@@ -219,6 +222,7 @@ void CMarkerProfileReaderFVM::MergeProfileMarkers() {
   nLocalPoint = 0; numberOfProfiles = 0;
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
     if (config->GetMarker_All_KindBC(iMarker) == markerType) {
+
       numberOfProfiles++;
       for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
         iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
@@ -238,7 +242,8 @@ void CMarkerProfileReaderFVM::MergeProfileMarkers() {
   SU2_MPI::Gather(&Buffer_Send_nPoin, 1, MPI_UNSIGNED_LONG,
                   Buffer_Recv_nPoin, 1, MPI_UNSIGNED_LONG, MASTER_NODE, SU2_MPI::GetComm());
   SU2_MPI::Allreduce(&nLocalPoint, &MaxLocalPoint, 1, MPI_UNSIGNED_LONG, MPI_MAX, SU2_MPI::GetComm());
-  SU2_MPI::Allreduce(&numberOfProfiles, &maxProfiles, 1, MPI_UNSIGNED_LONG, MPI_MAX, SU2_MPI::GetComm());
+  SU2_MPI::Reduce(&numberOfProfiles, &maxProfiles, 1, MPI_UNSIGNED_LONG, MPI_SUM, MASTER_NODE,
+                  SU2_MPI::GetComm());
 
   /*--- Send and Recv buffers. ---*/
 
@@ -254,6 +259,12 @@ void CMarkerProfileReaderFVM::MergeProfileMarkers() {
   char *Buffer_Send_Str = new char[MaxLocalPoint*MAX_STRING_SIZE];
   char *Buffer_Recv_Str = nullptr;
 
+  char *Buffer_Send_Name = new char[MaxLocalPoint*MAX_STRING_SIZE];
+  char *Buffer_Recv_Name = nullptr;
+
+  char *Buffer_Send_Value = new char[MaxLocalPoint*MAX_STRING_SIZE];
+  char *Buffer_Recv_Value = nullptr;
+
   /*--- Prepare the receive buffers in the master node only. ---*/
 
   if (rank == MASTER_NODE) {
@@ -261,7 +272,10 @@ void CMarkerProfileReaderFVM::MergeProfileMarkers() {
     Buffer_Recv_X = new su2double[nProcessor*MaxLocalPoint];
     Buffer_Recv_Y = new su2double[nProcessor*MaxLocalPoint];
     if (dimension == 3) Buffer_Recv_Z = new su2double[nProcessor*MaxLocalPoint];
+
     Buffer_Recv_Str = new char[nProcessor*MaxLocalPoint*MAX_STRING_SIZE];
+    Buffer_Recv_Name = new char[nProcessor*MaxLocalPoint*MAX_STRING_SIZE];
+    Buffer_Recv_Value = new char[nProcessor*MaxLocalPoint*MAX_STRING_SIZE];
 
     /*--- Sum total number of nodes to be written and allocate arrays ---*/
 
@@ -275,6 +289,9 @@ void CMarkerProfileReaderFVM::MergeProfileMarkers() {
       profileCoords[iMarker].resize(dimension);
     }
 
+    totalColumnNames.resize(maxProfiles);
+    totalColumnValues.resize(maxProfiles);
+
   }
 
   /*--- Main communication routine. Loop over each coordinate and perform
@@ -316,6 +333,16 @@ void CMarkerProfileReaderFVM::MergeProfileMarkers() {
           SPRINTF(&Buffer_Send_Str[jPoint*MAX_STRING_SIZE], "%s",
                   config->GetMarker_All_TagBound(iMarker).c_str());
 
+          /*--- Store the column names ---*/
+
+          SPRINTF(&Buffer_Send_Name[jPoint*MAX_STRING_SIZE], "%s",
+                  columnNames[iMarker].c_str());
+
+           /*--- Store the column values ---*/
+
+         SPRINTF(&Buffer_Send_Value[jPoint*MAX_STRING_SIZE], "%s",
+                  columnValues[iMarker].c_str());
+
           /*--- Increment jPoint as the counter. We need this because iPoint
            may include halo nodes that we skip over during this loop. ---*/
 
@@ -339,11 +366,18 @@ void CMarkerProfileReaderFVM::MergeProfileMarkers() {
   SU2_MPI::Gather(Buffer_Send_Str, (int)MaxLocalPoint*MAX_STRING_SIZE, MPI_CHAR,
                   Buffer_Recv_Str, (int)MaxLocalPoint*MAX_STRING_SIZE, MPI_CHAR, MASTER_NODE, SU2_MPI::GetComm());
 
+  SU2_MPI::Gather(Buffer_Send_Name, (int)MaxLocalPoint*MAX_STRING_SIZE, MPI_CHAR,
+                  Buffer_Recv_Name, (int)MaxLocalPoint*MAX_STRING_SIZE, MPI_CHAR, MASTER_NODE, SU2_MPI::GetComm());
+  SU2_MPI::Gather(Buffer_Send_Value, (int)MaxLocalPoint*MAX_STRING_SIZE, MPI_CHAR,
+                  Buffer_Recv_Value, (int)MaxLocalPoint*MAX_STRING_SIZE, MPI_CHAR, MASTER_NODE, SU2_MPI::GetComm());
+
   /*--- The master node unpacks and sorts this variable by marker tag. ---*/
 
   if (rank == MASTER_NODE) {
 
     profileTags.clear();
+    totalColumnNames.clear();
+    totalColumnValues.clear();
 
     /*--- First, parse the marker tags to count how many total profile markers
      we have now on the master. ---*/
@@ -353,30 +387,34 @@ void CMarkerProfileReaderFVM::MergeProfileMarkers() {
         index = (iProcessor*MaxLocalPoint + iPoint)*MAX_STRING_SIZE;
         for (iChar = 0; iChar < MAX_STRING_SIZE; iChar++) {
           str_buf[iChar] = Buffer_Recv_Str[index + iChar];
+          name_buf[iChar] = Buffer_Recv_Name[index + iChar];
+          value_buf[iChar] = Buffer_Recv_Value[index + iChar];
         }
+
         Marker_Tags.push_back(str_buf);
-        profileTags.push_back(str_buf);
-      }
-    }
 
-    /*--- Remove the duplicate profile marker strings. From 1 per point to 1 per marker. ---*/
+        /*--- only add if not already in the list ---*/
+        if (std::find(profileTags.begin(), profileTags.end(), str_buf) == profileTags.end()) {
+          profileTags.push_back(str_buf);
+          totalColumnNames.push_back(name_buf);
+          totalColumnValues.push_back(value_buf);
+        }
 
-    profileTags.erase(unique(profileTags.begin(),
-                             profileTags.end()),
-                      profileTags.end());
+      }
 
-    /*--- Store the unique number of markers for writing later. ---*/
+    }
 
     numberOfProfiles = profileTags.size();
 
     /*--- Count the number of rows (nodes) per marker. ---*/
 
-    numberOfRowsInProfile.resize(numberOfProfiles,0.0);
+    numberOfRowsInProfile.resize(maxProfiles,0.0);
     jPoint = 0;
     for (iProcessor = 0; iProcessor < nProcessor; iProcessor++) {
       for (iPoint = 0; iPoint < Buffer_Recv_nPoin[iProcessor]; iPoint++) {
-        for (iMarker = 0; iMarker < numberOfProfiles; iMarker++) {
+        for (iMarker = 0; iMarker < maxProfiles; iMarker++) {
           if (profileTags[iMarker] == Marker_Tags[jPoint]) {
+
             numberOfRowsInProfile[iMarker]++;
           }
         }
@@ -389,7 +427,7 @@ void CMarkerProfileReaderFVM::MergeProfileMarkers() {
     jPoint = 0; kPoint = 0;
     for (iProcessor = 0; iProcessor < nProcessor; iProcessor++) {
       for (iPoint = 0; iPoint < Buffer_Recv_nPoin[iProcessor]; iPoint++) {
-        for (iMarker = 0; iMarker < numberOfProfiles; iMarker++) {
+        for (iMarker = 0; iMarker < maxProfiles; iMarker++) {
 
           if (profileTags[iMarker] == Marker_Tags[kPoint]) {
 
@@ -415,22 +453,26 @@ void CMarkerProfileReaderFVM::MergeProfileMarkers() {
       jPoint = (iProcessor+1)*MaxLocalPoint;
 
     }
+
   }
 
   /*--- Immediately release the temporary data buffers. ---*/
-
   delete [] Buffer_Send_X;
   delete [] Buffer_Send_Y;
   delete [] Buffer_Send_Z;
   delete [] Buffer_Send_Str;
+  delete [] Buffer_Send_Name;
+  delete [] Buffer_Send_Value;
+
   if (rank == MASTER_NODE) {
     delete [] Buffer_Recv_X;
     delete [] Buffer_Recv_Y;
      delete [] Buffer_Recv_Z;
     delete [] Buffer_Recv_nPoin;
     delete [] Buffer_Recv_Str;
+    delete [] Buffer_Recv_Name;
+    delete [] Buffer_Recv_Value;
   }
-
 }
 
 void CMarkerProfileReaderFVM::WriteMarkerProfileTemplate() {
@@ -448,43 +490,38 @@ void CMarkerProfileReaderFVM::WriteMarkerProfileTemplate() {
   if (rank == MASTER_NODE) {
 
     ofstream node_file("example_"+filename);
-
     node_file << "NMARK= " << numberOfProfiles << endl;
 
-    unsigned short iMarkerCounter = 0;
-    for (unsigned short iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-      if (config->GetMarker_All_KindBC(iMarker) == markerType) {
+    for (unsigned long iMarker = 0; iMarker < numberOfProfiles; iMarker++) {
 
         /*--- Access the default data for this marker. ---*/
-
-        string Marker_Tag = profileTags[iMarkerCounter];
+        string Marker_Tag = profileTags[iMarker];
 
         /*--- Header information for this marker. ---*/
 
         node_file << "MARKER_TAG= " << Marker_Tag              << endl;
-        node_file << "NROW="        << numberOfRowsInProfile[iMarkerCounter] << endl;
+        node_file << "NROW="        << numberOfRowsInProfile[iMarker] << endl;
         node_file << "NCOL="        << nColumns          << endl;
 
+
         /*--- header line (names of the columns) --- */
-        node_file << columnNames[iMarkerCounter] << endl;
+        node_file << totalColumnNames[iMarker] << endl;
 
         node_file << setprecision(15);
         node_file << std::scientific;
 
         /*--- Loop over the data structure and write the coords and vars. ---*/
 
-        for (unsigned long iPoint = 0; iPoint < numberOfRowsInProfile[iMarkerCounter]; iPoint++) {
-
+        for (unsigned long iPoint = 0; iPoint < numberOfRowsInProfile[iMarker]; iPoint++) {
           for (unsigned short iDim = 0; iDim < dimension; iDim++) {
-            node_file << profileCoords[iMarkerCounter][iDim][iPoint] << "\t";
+            node_file << profileCoords[iMarker][iDim][iPoint] << "\t";
           }
 
-          node_file << columnValues[iMarkerCounter] << endl;
+          node_file << totalColumnValues[iMarker] << endl;
 
         }
 
-        iMarkerCounter++;
-      }
+
     } // iMarker
     node_file.close();
 

From 302071df83def3ba6360e4f3687c52f0f00a359c Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Tue, 4 Apr 2023 14:03:05 +0100
Subject: [PATCH 342/656] run turbo problems with the single and multizone
 drivers

---
 Common/include/CConfig.hpp                    |   2 +-
 Common/include/option_structure.hpp           |   6 -
 Common/src/CConfig.cpp                        |   5 -
 .../drivers/CDiscAdjSinglezoneDriver.hpp      |   2 -
 SU2_CFD/include/drivers/CDriver.hpp           |  54 +--
 SU2_CFD/include/drivers/CMultizoneDriver.hpp  |  13 +
 SU2_CFD/src/SU2_CFD.cpp                       |  14 +-
 .../src/drivers/CDiscAdjSinglezoneDriver.cpp  |  24 --
 SU2_CFD/src/drivers/CDriver.cpp               | 318 +++++-------------
 SU2_CFD/src/drivers/CMultizoneDriver.cpp      |  55 ++-
 SU2_CFD/src/drivers/CSinglezoneDriver.cpp     |   3 +
 .../transonic_stator_2D/transonic_stator.cfg  |   2 +-
 .../transonic_stator_restart.cfg              |   2 +-
 13 files changed, 158 insertions(+), 342 deletions(-)

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index ba5190f4b24..228b71ee5ac 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -1147,7 +1147,7 @@ class CConfig {
   unsigned long *VolumeOutputFrequencies; /*!< \brief list containing the writing frequencies */
 
   bool Multizone_Mesh;            /*!< \brief Determines if the mesh contains multiple zones. */
-  bool SinglezoneDriver;          /*!< \brief Determines if the single-zone driver is used. (TEMPORARY) */
+  bool SinglezoneDriver = true;   /*!< \brief Determines if the single-zone driver is used. (TEMPORARY) */
   bool Wrt_ZoneConv;              /*!< \brief Write the convergence history of each individual zone to screen. */
   bool Wrt_ZoneHist;              /*!< \brief Write the convergence history of each individual zone to file. */
   bool SpecialOutput,             /*!< \brief Determines if the special output is written. */
diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index 4c934f0612b..f08831944da 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -1869,9 +1869,6 @@ enum ENUM_OBJECTIVE {
   SURFACE_SPECIES_0 = 58,       /*!< \brief Surface Avg. Species_0 objective function definition. */
   SURFACE_SPECIES_VARIANCE = 59,/*!< \brief Species Variance objective function definition. */
   CUSTOM_OBJFUNC = 31,          /*!< \brief Custom objective function definition. */
-  FLOW_ANGLE_OUT = 46,
-  MASS_FLOW_IN = 47,
-  ENTROPY_GENERATION = 50,
   REFERENCE_GEOMETRY = 60,      /*!< \brief Norm of displacements with respect to target geometry. */
   REFERENCE_NODE = 61,          /*!< \brief Objective function defined as the difference of a particular node respect to a reference position. */
   VOLUME_FRACTION = 62,         /*!< \brief Volume average physical density, for material-based topology optimization applications. */
@@ -1914,9 +1911,6 @@ static const MapType<std::string, ENUM_OBJECTIVE> Objective_Map = {
   MakePair("SURFACE_SPECIES_0", SURFACE_SPECIES_0)
   MakePair("SURFACE_SPECIES_VARIANCE", SURFACE_SPECIES_VARIANCE)
   MakePair("CUSTOM_OBJFUNC", CUSTOM_OBJFUNC)
-  MakePair("FLOW_ANGLE_OUT", FLOW_ANGLE_OUT)
-  MakePair("MASS_FLOW_IN", MASS_FLOW_IN)
-  MakePair("ENTROPY_GENERATION",  ENTROPY_GENERATION)
   MakePair("REFERENCE_GEOMETRY", REFERENCE_GEOMETRY)
   MakePair("REFERENCE_NODE", REFERENCE_NODE)
   MakePair("VOLUME_FRACTION", VOLUME_FRACTION)
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index ea45d2d0159..ffe963b7418 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -2512,8 +2512,6 @@ void CConfig::SetConfig_Options() {
   addDoubleOption("TIME_STEP", Time_Step, 0.0);
   /* DESCRIPTION: Total Physical Time for time-domain problems (s) */
   addDoubleOption("MAX_TIME", Max_Time, 1.0);
-  /* DESCRIPTION: Determines if the single-zone driver is used. (TEMPORARY) */
-  addBoolOption("SINGLEZONE_DRIVER", SinglezoneDriver, true);
   /* DESCRIPTION: Determines if the special output is written out */
   addBoolOption("SPECIAL_OUTPUT", SpecialOutput, false);
 
@@ -8285,9 +8283,6 @@ string CConfig::GetObjFunc_Extension(string val_filename) const {
         case SURFACE_SPECIES_VARIANCE:    AdjExt = "_specvar";  break;
         case SURFACE_MACH:                AdjExt = "_mach";     break;
         case CUSTOM_OBJFUNC:              AdjExt = "_custom";   break;
-        case FLOW_ANGLE_OUT:              AdjExt = "_fao";      break;
-        case MASS_FLOW_IN:                AdjExt = "_mfi";      break;
-        case ENTROPY_GENERATION:          AdjExt = "_entg";     break;
         case REFERENCE_GEOMETRY:          AdjExt = "_refgeom";  break;
         case REFERENCE_NODE:              AdjExt = "_refnode";  break;
         case VOLUME_FRACTION:             AdjExt = "_volfrac";  break;
diff --git a/SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp b/SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp
index 105eecc3abe..8f8a6c19238 100644
--- a/SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp
+++ b/SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp
@@ -55,8 +55,6 @@ class CDiscAdjSinglezoneDriver : public CSinglezoneDriver {
   COutput *direct_output;
   CNumerics ***numerics;                        /*!< \brief Container vector with all the numerics. */
 
-  COutputLegacy* output_legacy;
-
   /*!
    * \brief Record one iteration of a flow iteration in within multiple zones.
    * \param[in] kind_recording - Type of recording (full list in ENUM_RECORDING, option_structure.hpp)
diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index 2cf991bb0b7..54adf5c0d35 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -51,7 +51,6 @@ class COutput;
 
 class CDriver : public CDriverBase {
  protected:
-  char runtime_file_name[MAX_STRING_SIZE];
   su2double
       UsedTimeOutput; /*!< \brief Elapsed time between Start and Stop point of the timer for tracking output phase.*/
 
@@ -299,6 +298,13 @@ class CDriver : public CDriverBase {
   void PreprocessTurbomachinery(CConfig** config, CGeometry**** geometry, CSolver***** solver,
                                     CInterface*** interface);
 
+  /*!
+   * \brief Ramp some simulation settings for turbomachinery problems.
+   * \param[in] iter - Iteration for the ramp (can be outer or time depending on type of simulation).
+   * \note TODO This is not compatible with inner iterations because they are delegated to the iteration class.
+   */
+  void RampTurbomachineryValues(unsigned long iter);
+
   /*!
    * \brief A virtual member.
    * \param[in] donorZone - zone in which the displacements will be predicted.
@@ -575,52 +581,6 @@ class CFluidDriver : public CDriver {
   void DynamicMeshUpdate(unsigned long TimeIter) override;
 };
 
-/*!
- * \class CTurbomachineryDriver
- * \ingroup Drivers
- * \brief Class for driving an iteration for turbomachinery flow analysis.
- * \author S. Vitale
- */
-class CTurbomachineryDriver : public CFluidDriver {
- private:
-  COutputLegacy* output_legacy;
-
-  /*!
-   * \brief Set Mixing Plane interface within multiple zones.
-   */
-  void SetMixingPlane(unsigned short iZone);
-
-  /*!
-   * \brief Set Mixing Plane interface within multiple zones.
-   */
-  void SetTurboPerformance(unsigned short targetZone);
-
- public:
-  /*!
-   * \brief Constructor of the class.
-   * \param[in] confFile - Configuration file name.
-   * \param[in] val_nZone - Total number of zones.
-   * \param[in] MPICommunicator - MPI communicator for SU2.
-   */
-  CTurbomachineryDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator);
-
-  /*!
-   * \brief Destructor of the class.
-   */
-  ~CTurbomachineryDriver(void) override;
-
-  /*!
-   * \brief Run a single iteration of the physics within multiple zones.
-   */
-
-  void Run() override;
-
-  /*!
-   * \brief Monitor the computation.
-   */
-  bool Monitor(unsigned long TimeIter) override;
-};
-
 /*!
  * \class CHBDriver
  * \ingroup Drivers
diff --git a/SU2_CFD/include/drivers/CMultizoneDriver.hpp b/SU2_CFD/include/drivers/CMultizoneDriver.hpp
index 8106db28174..afff04b8eac 100644
--- a/SU2_CFD/include/drivers/CMultizoneDriver.hpp
+++ b/SU2_CFD/include/drivers/CMultizoneDriver.hpp
@@ -83,6 +83,19 @@ class CMultizoneDriver : public CDriver {
    */
   bool TransferData(unsigned short donorZone, unsigned short targetZone);
 
+  /*!
+   * \brief Set Mixing Plane interface within multiple zones.
+   */
+  void SetMixingPlane(unsigned short donorZone);
+
+  /*!
+   * \brief Transfer the local turboperfomance quantities (for each blade row) from all the donorZones to the
+   * targetZone (ZONE_0).
+   * \note IMPORTANT: This approach of multi-zone performances rely upon the fact that turbomachinery markers follow
+   * the natural (stator-rotor) development of the real machine.
+   */
+  void SetTurboPerformance();
+
   /*!
    * \brief Check the convergence at the outer level.
    */
diff --git a/SU2_CFD/src/SU2_CFD.cpp b/SU2_CFD/src/SU2_CFD.cpp
index c11ceb54156..fce69de5fd0 100644
--- a/SU2_CFD/src/SU2_CFD.cpp
+++ b/SU2_CFD/src/SU2_CFD.cpp
@@ -96,7 +96,6 @@ int main(int argc, char *argv[]) {
 
   const CConfig config(config_file_name, SU2_COMPONENT::SU2_CFD);
   const unsigned short nZone = config.GetnZone();
-  const bool turbo = config.GetBoolTurbomachinery();
 
   /*--- First, given the basic information about the number of zones and the
    solver types from the config, instantiate the appropriate driver for the problem
@@ -112,7 +111,7 @@ int main(int argc, char *argv[]) {
     driver = new CDummyDriver(config_file_name, nZone, MPICommunicator);
 
   }
-  else if ((!multizone && !harmonic_balance && !turbo) || (turbo && disc_adj)) {
+  else if (!multizone && !harmonic_balance) {
 
     /*--- Generic single zone problem: instantiate the single zone driver class. ---*/
     if (nZone != 1)
@@ -126,7 +125,7 @@ int main(int argc, char *argv[]) {
     }
 
   }
-  else if (multizone && !turbo) {
+  else if (multizone) {
 
     /*--- Generic multizone problems. ---*/
     if (disc_adj) {
@@ -137,18 +136,13 @@ int main(int argc, char *argv[]) {
     }
 
   }
-  else if (harmonic_balance) {
+  else {
+    assert(harmonic_balance);
 
     /*--- Harmonic balance problem: instantiate the Harmonic Balance driver class. ---*/
     driver = new CHBDriver(config_file_name, nZone, MPICommunicator);
 
   }
-  else if (turbo) {
-
-    /*--- Turbomachinery problem. ---*/
-    driver = new CTurbomachineryDriver(config_file_name, nZone, MPICommunicator);
-
-  } /*--- These are all the possible cases ---*/
 
   /*--- Launch the main external loop of the solver. ---*/
 
diff --git a/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
index 440d311d6c1..5f64b68455a 100644
--- a/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
@@ -66,7 +66,6 @@ CDiscAdjSinglezoneDriver::CDiscAdjSinglezoneDriver(char* confFile,
 
     if (config->GetBoolTurbomachinery()) {
       direct_iteration = new CTurboIteration(config);
-      output_legacy = COutputFactory::CreateLegacyOutput(config_container[ZONE_0]);
     }
     else { direct_iteration = CIterationFactory::CreateIteration(MAIN_SOLVER::EULER, config); }
 
@@ -360,29 +359,6 @@ void CDiscAdjSinglezoneDriver::SetObjFunction(){
     direct_output->SetHistoryOutput(geometry, solver, config, config->GetTimeIter(),
                                      config->GetOuterIter(), config->GetInnerIter());
     ObjFunc += solver[FLOW_SOL]->GetTotal_ComboObj();
-
-    /*--- These calls to be moved to a generic framework at a next stage        ---*/
-    /*--- Some things that are currently hacked into output must be reorganized ---*/
-    if (config->GetBoolTurbomachinery()) {
-      output_legacy->ComputeTurboPerformance(solver[FLOW_SOL], geometry, config);
-
-      unsigned short nMarkerTurboPerf = config->GetnMarker_TurboPerformance();
-      unsigned short nSpanSections = config->GetnSpanWiseSections();
-
-      switch (config_container[ZONE_0]->GetKind_ObjFunc()){
-      case ENTROPY_GENERATION:
-        ObjFunc += output_legacy->GetEntropyGen(nMarkerTurboPerf-1, nSpanSections);
-        break;
-      case FLOW_ANGLE_OUT:
-        ObjFunc += output_legacy->GetFlowAngleOut(nMarkerTurboPerf-1, nSpanSections);
-        break;
-      case MASS_FLOW_IN:
-        ObjFunc += output_legacy->GetMassFlowIn(nMarkerTurboPerf-1, nSpanSections);
-        break;
-      default:
-        break;
-      }
-    }
     break;
 
   case MAIN_SOLVER::DISC_ADJ_HEAT:
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index 457162bf12b..22590e18259 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -340,8 +340,6 @@ void CDriver::InitializeContainers(){
     nInst[iZone] = 1;
   }
 
-  strcpy(runtime_file_name, "runtime.dat");
-
 }
 
 
@@ -2720,7 +2718,7 @@ void CDriver::PreprocessTurbomachinery(CConfig** config, CGeometry**** geometry,
     solver[iZone][INST_0][MESH_0][FLOW_SOL]->InitTurboContainers(geometry[iZone][INST_0][MESH_0],config[iZone]);
   }
 
-//TODO(turbo) make it general for turbo HB
+  // TODO(turbo): make it general for turbo HB
   if (rank == MASTER_NODE) cout<<"Compute inflow and outflow average geometric quantities." << endl;
   for (iZone = 0; iZone < nZone; iZone++) {
     geometry[iZone][INST_0][MESH_0]->SetAvgTurboValue(config[iZone], iZone, INFLOW, true);
@@ -2925,6 +2923,82 @@ void CDriver::PrintDirectResidual(RECORDING kind_recording) {
 
 }
 
+void CDriver::RampTurbomachineryValues(unsigned long iter) {
+  auto* config = config_container[ZONE_0];
+
+  /*--- ROTATING FRAME Ramp: Compute the updated rotational velocity. ---*/
+  if (config->GetGrid_Movement() && config->GetRampRotatingFrame()) {
+    const unsigned long rampFreq = SU2_TYPE::Int(config->GetRampRotatingFrame_Coeff(1));
+    const unsigned long finalRamp_Iter = SU2_TYPE::Int(config->GetRampRotatingFrame_Coeff(2));
+    const su2double rot_z_ini = config->GetRampRotatingFrame_Coeff(0);
+    const bool print = false;
+
+    if(iter % rampFreq == 0 && iter <= finalRamp_Iter){
+
+      for (auto iZone = 0u; iZone < nZone; iZone++) {
+        const su2double rot_z_final = config_container[iZone]->GetFinalRotation_Rate_Z();
+
+        if (fabs(rot_z_final) > 0.0) {
+          const su2double rot_z = rot_z_ini + iter * ( rot_z_final - rot_z_ini) / finalRamp_Iter;
+          config_container[iZone]->SetRotation_Rate(2, rot_z);
+          if (rank == MASTER_NODE && print && iter > 0) {
+            cout << "\nUpdated rotating frame grid velocities for zone " << iZone << ".\n";
+          }
+          geometry_container[iZone][INST_0][MESH_0]->SetRotationalVelocity(config_container[iZone], print);
+          geometry_container[iZone][INST_0][MESH_0]->SetShroudVelocity(config_container[iZone]);
+        }
+      }
+
+      for (auto iZone = 0u; iZone < nZone; iZone++) {
+        geometry_container[iZone][INST_0][MESH_0]->SetAvgTurboValue(config_container[iZone], iZone, INFLOW, false);
+        geometry_container[iZone][INST_0][MESH_0]->SetAvgTurboValue(config_container[iZone],iZone, OUTFLOW, false);
+        geometry_container[iZone][INST_0][MESH_0]->GatherInOutAverageValues(config_container[iZone], false);
+      }
+
+      for (auto iZone = 1u; iZone < nZone; iZone++) {
+        interface_container[iZone][ZONE_0]->GatherAverageTurboGeoValues(
+            geometry_container[iZone][INST_0][MESH_0], geometry_container[ZONE_0][INST_0][MESH_0], iZone);
+      }
+    }
+  }
+
+  /*--- Outlet Pressure Ramp: Compute the updated pressure. ---*/
+  if (config->GetRampOutletPressure()) {
+    const unsigned long rampFreq = SU2_TYPE::Int(config->GetRampOutletPressure_Coeff(1));
+    const unsigned long finalRamp_Iter = SU2_TYPE::Int(config->GetRampOutletPressure_Coeff(2));
+    const su2double outPres_ini = config->GetRampOutletPressure_Coeff(0);
+    const su2double outPres_final = config->GetFinalOutletPressure();
+
+    if (iter % rampFreq == 0 && iter <= finalRamp_Iter) {
+      const su2double outPres = outPres_ini + iter * (outPres_final - outPres_ini) / finalRamp_Iter;
+      if (rank == MASTER_NODE) config->SetMonitotOutletPressure(outPres);
+
+      for (auto iZone = 0u; iZone < nZone; iZone++) {
+        for (auto iMarker = 0; iMarker < config_container[iZone]->GetnMarker_All(); iMarker++) {
+          const auto KindBC = config_container[iZone]->GetMarker_All_KindBC(iMarker);
+          const auto Marker_Tag = config_container[iZone]->GetMarker_All_TagBound(iMarker);
+          unsigned short KindBCOption;
+          switch (KindBC) {
+            case RIEMANN_BOUNDARY:
+              KindBCOption = config_container[iZone]->GetKind_Data_Riemann(Marker_Tag);
+              if (KindBCOption == STATIC_PRESSURE || KindBCOption == RADIAL_EQUILIBRIUM) {
+                SU2_MPI::Error("Outlet pressure ramp only implemented for NRBC", CURRENT_FUNCTION);
+              }
+              break;
+            case GILES_BOUNDARY:
+              KindBCOption = config_container[iZone]->GetKind_Data_Giles(Marker_Tag);
+              if (KindBCOption == STATIC_PRESSURE || KindBCOption == STATIC_PRESSURE_1D ||
+                  KindBCOption == RADIAL_EQUILIBRIUM ) {
+                config_container[iZone]->SetGiles_Var1(outPres, Marker_Tag);
+              }
+              break;
+          }
+        }
+      }
+    }
+  }
+}
+
 CFluidDriver::CFluidDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator) : CDriver(confFile, val_nZone, MPICommunicator, false) {
   Max_Iter = config_container[ZONE_0]->GetnInner_Iter();
 }
@@ -3113,6 +3187,7 @@ void CFluidDriver::DynamicMeshUpdate(unsigned long TimeIter) {
   }
 
 }
+
 bool CFluidDriver::Monitor(unsigned long ExtIter) {
 
   /*--- Synchronization point after a single solver iteration. Compute the
@@ -3123,14 +3198,6 @@ bool CFluidDriver::Monitor(unsigned long ExtIter) {
   IterCount++;
   UsedTime = (StopTime - StartTime) + UsedTimeCompute;
 
-  /*--- Check if there is any change in the runtime parameters ---*/
-
-  CConfig *runtime = nullptr;
-  strcpy(runtime_file_name, "runtime.dat");
-  runtime = new CConfig(runtime_file_name, config_container[ZONE_0]);
-  runtime->SetTimeIter(ExtIter);
-  delete runtime;
-
   /*--- Check whether the current simulation has reached the specified
    convergence criteria, and set StopCalc to true, if so. ---*/
 
@@ -3144,7 +3211,6 @@ bool CFluidDriver::Monitor(unsigned long ExtIter) {
 
 }
 
-
 void CFluidDriver::Output(unsigned long InnerIter) {
 
   for (iZone = 0; iZone < nZone; iZone++) {
@@ -3162,234 +3228,6 @@ void CFluidDriver::Output(unsigned long InnerIter) {
 
 }
 
-
-CTurbomachineryDriver::CTurbomachineryDriver(char* confFile, unsigned short val_nZone,
-                                             SU2_Comm MPICommunicator):
-                                             CFluidDriver(confFile, val_nZone, MPICommunicator) {
-
-  output_legacy = COutputFactory::CreateLegacyOutput(config_container[ZONE_0]);
-
-  /*--- LEGACY OUTPUT (going to be removed soon) --- */
-
-  /*--- Open the convergence history file ---*/
-  ConvHist_file = nullptr;
-  ConvHist_file = new ofstream*[nZone];
-  for (iZone = 0; iZone < nZone; iZone++) {
-    ConvHist_file[iZone] = nullptr;
-    if (rank == MASTER_NODE){
-      ConvHist_file[iZone] = new ofstream[nInst[iZone]];
-      for (iInst = 0; iInst < nInst[iZone]; iInst++) {
-        output_legacy->SetConvHistoryHeader(&ConvHist_file[iZone][iInst], config_container[iZone], iZone, iInst);
-      }
-    }
-  }
-
-  if (nZone > 1){
-    Max_Iter = config_container[ZONE_0]->GetnOuter_Iter();
-  }
-}
-
-CTurbomachineryDriver::~CTurbomachineryDriver(void) {
-  if (rank == MASTER_NODE){
-    /*--- Close the convergence history file. ---*/
-    for (iZone = 0; iZone < nZone; iZone++) {
-      for (iInst = 0; iInst < 1; iInst++) {
-        ConvHist_file[iZone][iInst].close();
-      }
-      delete [] ConvHist_file[iZone];
-    }
-    delete [] ConvHist_file;
-  }
-}
-
-void CTurbomachineryDriver::Run() {
-
-  /*--- Run a single iteration of a multi-zone problem by looping over all
-   zones and executing the iterations. Note that data transers between zones
-   and other intermediate procedures may be required. ---*/
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    iteration_container[iZone][INST_0]->Preprocess(output_container[iZone], integration_container, geometry_container,
-                                           solver_container, numerics_container, config_container,
-                                           surface_movement, grid_movement, FFDBox, iZone, INST_0);
-  }
-
-  /* --- Update the mixing-plane interface ---*/
-  for (iZone = 0; iZone < nZone; iZone++) {
-    if(mixingplane)SetMixingPlane(iZone);
-  }
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    iteration_container[iZone][INST_0]->Iterate(output_container[iZone], integration_container, geometry_container,
-                                        solver_container, numerics_container, config_container,
-                                        surface_movement, grid_movement, FFDBox, iZone, INST_0);
-  }
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    iteration_container[iZone][INST_0]->Postprocess(output_container[iZone], integration_container, geometry_container,
-                                      solver_container, numerics_container, config_container,
-                                      surface_movement, grid_movement, FFDBox, iZone, INST_0);
-  }
-
-  if (rank == MASTER_NODE){
-    SetTurboPerformance(ZONE_0);
-  }
-
-
-}
-
-void CTurbomachineryDriver::SetMixingPlane(unsigned short donorZone){
-
-  unsigned short targetZone, nMarkerInt, iMarkerInt ;
-  nMarkerInt     = config_container[donorZone]->GetnMarker_MixingPlaneInterface()/2;
-
-  /* --- transfer the average value from the donorZone to the targetZone*/
-  for (iMarkerInt = 1; iMarkerInt <= nMarkerInt; iMarkerInt++){
-    for (targetZone = 0; targetZone < nZone; targetZone++) {
-      if (targetZone != donorZone){
-        interface_container[donorZone][targetZone]->AllgatherAverage(solver_container[donorZone][INST_0][MESH_0][FLOW_SOL],solver_container[targetZone][INST_0][MESH_0][FLOW_SOL],
-            geometry_container[donorZone][INST_0][MESH_0],geometry_container[targetZone][INST_0][MESH_0],
-            config_container[donorZone], config_container[targetZone], iMarkerInt );
-      }
-    }
-  }
-}
-
-void CTurbomachineryDriver::SetTurboPerformance(unsigned short targetZone){
-
-  unsigned short donorZone;
-  //IMPORTANT this approach of multi-zone performances rely upon the fact that turbomachinery markers follow the natural (stator-rotor) development of the real machine.
-  /* --- transfer the local turboperfomance quantities (for each blade)  from all the donorZones to the targetZone (ZONE_0) ---*/
-  for (donorZone = 1; donorZone < nZone; donorZone++) {
-    interface_container[donorZone][targetZone]->GatherAverageValues(solver_container[donorZone][INST_0][MESH_0][FLOW_SOL],solver_container[targetZone][INST_0][MESH_0][FLOW_SOL], donorZone);
-  }
-
-  /* --- compute turboperformance for each stage and the global machine ---*/
-
- output_legacy->ComputeTurboPerformance(solver_container[targetZone][INST_0][MESH_0][FLOW_SOL], geometry_container[targetZone][INST_0][MESH_0], config_container[targetZone]);
-
-}
-
-
-bool CTurbomachineryDriver::Monitor(unsigned long ExtIter) {
-
-  su2double rot_z_ini, rot_z_final ,rot_z;
-  su2double outPres_ini, outPres_final, outPres;
-  unsigned long rampFreq, finalRamp_Iter;
-  unsigned short iMarker, KindBC, KindBCOption;
-  string Marker_Tag;
-
-  bool print;
-
-  /*--- Synchronization point after a single solver iteration. Compute the
-   wall clock time required. ---*/
-
-  StopTime = SU2_MPI::Wtime();
-
-  IterCount++;
-  UsedTime = (StopTime - StartTime);
-
-
-  /*--- Check if there is any change in the runtime parameters ---*/
-  CConfig *runtime = nullptr;
-  strcpy(runtime_file_name, "runtime.dat");
-  runtime = new CConfig(runtime_file_name, config_container[ZONE_0]);
-  runtime->SetInnerIter(ExtIter);
-  delete runtime;
-
-  /*--- Update the convergence history file (serial and parallel computations). ---*/
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    for (iInst = 0; iInst < nInst[iZone]; iInst++)
-      output_legacy->SetConvHistoryBody(&ConvHist_file[iZone][iInst], geometry_container, solver_container,
-          config_container, integration_container, false, UsedTime, iZone, iInst);
-  }
-
-  /*--- ROTATING FRAME Ramp: Compute the updated rotational velocity. ---*/
-  if (config_container[ZONE_0]->GetGrid_Movement() && config_container[ZONE_0]->GetRampRotatingFrame()) {
-    rampFreq       = SU2_TYPE::Int(config_container[ZONE_0]->GetRampRotatingFrame_Coeff(1));
-    finalRamp_Iter = SU2_TYPE::Int(config_container[ZONE_0]->GetRampRotatingFrame_Coeff(2));
-    rot_z_ini = config_container[ZONE_0]->GetRampRotatingFrame_Coeff(0);
-    print = false;
-    if(ExtIter % rampFreq == 0 &&  ExtIter <= finalRamp_Iter){
-
-      for (iZone = 0; iZone < nZone; iZone++) {
-        rot_z_final = config_container[iZone]->GetFinalRotation_Rate_Z();
-        if(abs(rot_z_final) > 0.0){
-          rot_z = rot_z_ini + ExtIter*( rot_z_final - rot_z_ini)/finalRamp_Iter;
-          config_container[iZone]->SetRotation_Rate(2, rot_z);
-          if(rank == MASTER_NODE && print && ExtIter > 0) {
-            cout << endl << " Updated rotating frame grid velocities";
-            cout << " for zone " << iZone << "." << endl;
-          }
-          geometry_container[iZone][INST_0][MESH_0]->SetRotationalVelocity(config_container[iZone], print);
-          geometry_container[iZone][INST_0][MESH_0]->SetShroudVelocity(config_container[iZone]);
-        }
-      }
-
-      for (iZone = 0; iZone < nZone; iZone++) {
-        geometry_container[iZone][INST_0][MESH_0]->SetAvgTurboValue(config_container[iZone], iZone, INFLOW, false);
-        geometry_container[iZone][INST_0][MESH_0]->SetAvgTurboValue(config_container[iZone],iZone, OUTFLOW, false);
-        geometry_container[iZone][INST_0][MESH_0]->GatherInOutAverageValues(config_container[iZone], false);
-
-      }
-
-      for (iZone = 1; iZone < nZone; iZone++) {
-        interface_container[iZone][ZONE_0]->GatherAverageTurboGeoValues(geometry_container[iZone][INST_0][MESH_0],geometry_container[ZONE_0][INST_0][MESH_0], iZone);
-      }
-
-    }
-  }
-
-
-  /*--- Outlet Pressure Ramp: Compute the updated rotational velocity. ---*/
-  if (config_container[ZONE_0]->GetRampOutletPressure()) {
-    rampFreq       = SU2_TYPE::Int(config_container[ZONE_0]->GetRampOutletPressure_Coeff(1));
-    finalRamp_Iter = SU2_TYPE::Int(config_container[ZONE_0]->GetRampOutletPressure_Coeff(2));
-    outPres_ini    = config_container[ZONE_0]->GetRampOutletPressure_Coeff(0);
-    outPres_final  = config_container[ZONE_0]->GetFinalOutletPressure();
-
-    if(ExtIter % rampFreq == 0 &&  ExtIter <= finalRamp_Iter){
-      outPres = outPres_ini + ExtIter*(outPres_final - outPres_ini)/finalRamp_Iter;
-      if(rank == MASTER_NODE) config_container[ZONE_0]->SetMonitotOutletPressure(outPres);
-
-      for (iZone = 0; iZone < nZone; iZone++) {
-        for (iMarker = 0; iMarker < config_container[iZone]->GetnMarker_All(); iMarker++) {
-          KindBC = config_container[iZone]->GetMarker_All_KindBC(iMarker);
-          switch (KindBC) {
-          case RIEMANN_BOUNDARY:
-            Marker_Tag         = config_container[iZone]->GetMarker_All_TagBound(iMarker);
-            KindBCOption       = config_container[iZone]->GetKind_Data_Riemann(Marker_Tag);
-            if(KindBCOption == STATIC_PRESSURE || KindBCOption == RADIAL_EQUILIBRIUM ){
-              SU2_MPI::Error("Outlet pressure ramp only implemented for NRBC", CURRENT_FUNCTION);
-            }
-            break;
-          case GILES_BOUNDARY:
-            Marker_Tag         = config_container[iZone]->GetMarker_All_TagBound(iMarker);
-            KindBCOption       = config_container[iZone]->GetKind_Data_Giles(Marker_Tag);
-            if(KindBCOption == STATIC_PRESSURE || KindBCOption == STATIC_PRESSURE_1D || KindBCOption == RADIAL_EQUILIBRIUM ){
-              config_container[iZone]->SetGiles_Var1(outPres, Marker_Tag);
-            }
-            break;
-          }
-        }
-      }
-    }
-  }
-
-  /*--- Check whether the current simulation has reached the specified
-   convergence criteria, and set StopCalc to true, if so. ---*/
-
-  /// TODO: Get convergence from the output class
-
-  /*--- Set StopCalc to true if max. number of iterations has been reached ---*/
-
-  StopCalc = StopCalc || (ExtIter == Max_Iter - 1);
-
-  return StopCalc;
-
-}
-
 CHBDriver::CHBDriver(char* confFile,
     unsigned short val_nZone,
     SU2_Comm MPICommunicator) : CFluidDriver(confFile,
diff --git a/SU2_CFD/src/drivers/CMultizoneDriver.cpp b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
index 4bd72f6752f..0cdb774c9d9 100644
--- a/SU2_CFD/src/drivers/CMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
@@ -160,11 +160,11 @@ void CMultizoneDriver::StartSolver() {
   /*--- Main external loop of the solver. Runs for the number of time steps required. ---*/
 
   if (rank == MASTER_NODE){
-    cout << endl <<"------------------------------ Begin Solver -----------------------------" << endl;
+    cout << "\n------------------------------ Begin Solver -----------------------------" << endl;
   }
 
   if (rank == MASTER_NODE){
-    cout << endl <<"Simulation Run using the Multizone Driver" << endl;
+    cout << "\nSimulation Run using the Multizone Driver" << endl;
     if (driver_config->GetTime_Domain())
       cout << "The simulation will run until time step " << driver_config->GetnTime_Iter() - driver_config->GetRestart_Iter() << "." << endl;
   }
@@ -247,6 +247,11 @@ void CMultizoneDriver::Preprocess(unsigned long TimeIter) {
     }
   }
 
+  /*--- Ramp turbo values for unsteady problems here, otherwise do it over outer iterations. ---*/
+  if (config_container[ZONE_0]->GetTime_Domain()) {
+    RampTurbomachineryValues(TimeIter);
+  }
+
   SU2_MPI::Barrier(SU2_MPI::GetComm());
 
   /*--- Run a predictor step ---*/
@@ -283,10 +288,15 @@ void CMultizoneDriver::RunGaussSeidel() {
   }
 
   /*--- Loop over the number of outer iterations ---*/
-  for (auto iOuter_Iter = 0ul; iOuter_Iter < driver_config->GetnOuter_Iter(); iOuter_Iter++){
+  for (auto iOuter_Iter = 0ul; iOuter_Iter < driver_config->GetnOuter_Iter(); iOuter_Iter++) {
+
+    /*--- Ramp turbo values for steady problems here, otherwise do it over time steps. ---*/
+    if (!config_container[ZONE_0]->GetTime_Domain()) {
+      RampTurbomachineryValues(iOuter_Iter);
+    }
 
     /*--- Loop over the number of zones (IZONE) ---*/
-    for (iZone = 0; iZone < nZone; iZone++){
+    for (iZone = 0; iZone < nZone; iZone++) {
 
       /*--- In principle, the mesh does not need to be updated ---*/
       UpdateMesh = 0;
@@ -312,6 +322,8 @@ void CMultizoneDriver::RunGaussSeidel() {
                                                 solver_container, numerics_container, config_container,
                                                 surface_movement, grid_movement, FFDBox, iZone, INST_0);
 
+      if (mixingplane) SetMixingPlane(iZone);
+
       /*--- A corrector step can help preventing numerical instabilities ---*/
       Corrector(iZone);
 
@@ -335,6 +347,11 @@ void CMultizoneDriver::RunJacobi() {
   /*--- Loop over the number of outer iterations ---*/
   for (auto iOuter_Iter = 0ul; iOuter_Iter < driver_config->GetnOuter_Iter(); iOuter_Iter++){
 
+    /*--- Ramp turbo values for steady problems here, otherwise do it over time steps. ---*/
+    if (!config_container[ZONE_0]->GetTime_Domain()) {
+      RampTurbomachineryValues(iOuter_Iter);
+    }
+
     /*--- Transfer from all zones ---*/
     for (iZone = 0; iZone < nZone; iZone++){
 
@@ -356,10 +373,11 @@ void CMultizoneDriver::RunJacobi() {
       /*--- If a mesh update is required due to the transfer of data ---*/
       if (UpdateMesh > 0) DynamicMeshUpdate(iZone, TimeIter);
 
+      if (mixingplane) SetMixingPlane(iZone);
     }
 
       /*--- Loop over the number of zones (IZONE) ---*/
-    for (iZone = 0; iZone < nZone; iZone++){
+    for (iZone = 0; iZone < nZone; iZone++) {
 
       /*--- Set the OuterIter ---*/
       config_container[iZone]->SetOuterIter(iOuter_Iter);
@@ -577,6 +595,7 @@ bool CMultizoneDriver::TransferData(unsigned short donorZone, unsigned short tar
     case FLOW_TRACTION:
       BroadcastData(FLOW_SOL, FEA_SOL);
       break;
+    case MIXING_PLANE:
     case NO_TRANSFER:
     case ZONES_ARE_EQUAL:
     case NO_COMMON_INTERFACE:
@@ -591,6 +610,30 @@ bool CMultizoneDriver::TransferData(unsigned short donorZone, unsigned short tar
   return UpdateMesh;
 }
 
+void CMultizoneDriver::SetMixingPlane(unsigned short donorZone) {
+
+  const auto nMarkerInt = config_container[donorZone]->GetnMarker_MixingPlaneInterface() / 2;
+
+  /*--- Transfer the average value from the donor zones to the target zones ---*/
+  for (auto iMarkerInt = 1; iMarkerInt <= nMarkerInt; iMarkerInt++) {
+    for (auto targetZone = 0u; targetZone < nZone; targetZone++) {
+      if (targetZone == donorZone) continue;
+      interface_container[donorZone][targetZone]->AllgatherAverage(
+        solver_container[donorZone][INST_0][MESH_0][FLOW_SOL], solver_container[targetZone][INST_0][MESH_0][FLOW_SOL],
+        geometry_container[donorZone][INST_0][MESH_0], geometry_container[targetZone][INST_0][MESH_0],
+        config_container[donorZone], config_container[targetZone], iMarkerInt);
+    }
+  }
+}
+
+void CMultizoneDriver::SetTurboPerformance() {
+  for (auto donorZone = 1u; donorZone < nZone; donorZone++) {
+    interface_container[donorZone][ZONE_0]->GatherAverageValues(solver_container[donorZone][INST_0][MESH_0][FLOW_SOL],
+                                                                solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL],
+                                                                donorZone);
+  }
+}
+
 bool CMultizoneDriver::Monitor(unsigned long TimeIter){
 
   /*--- Check whether the inner solver has converged --- */
@@ -636,6 +679,8 @@ bool CMultizoneDriver::Monitor(unsigned long TimeIter){
     return (FinalTimeReached || MaxIterationsReached);
   }
 
+  if (rank == MASTER_NODE) SetTurboPerformance();
+
 }
 
 bool CMultizoneDriver::GetTimeConvergence() const{
diff --git a/SU2_CFD/src/drivers/CSinglezoneDriver.cpp b/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
index 73668884259..a7d030215b3 100644
--- a/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
@@ -125,6 +125,9 @@ void CSinglezoneDriver::Preprocess(unsigned long TimeIter) {
   else
     config_container[ZONE_0]->SetPhysicalTime(0.0);
 
+  /*--- Ramp turbo BCs for this time step. ---*/
+  RampTurbomachineryValues(TimeIter);
+
   /*--- Set the initial condition for EULER/N-S/RANS ---------------------------------------------*/
   if (config_container[ZONE_0]->GetFluidProblem()) {
     solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->SetInitialCondition(geometry_container[ZONE_0][INST_0],
diff --git a/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg b/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg
index 459e7763771..83f16b2d216 100644
--- a/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg
+++ b/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg
@@ -17,7 +17,7 @@ KIND_TURB_MODEL= SST
 MATH_PROBLEM= DISCRETE_ADJOINT
 RESTART_SOL= NO
 NZONES= 1
-SINGLEZONE_DRIVER=NO
+%SINGLEZONE_DRIVER=NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
diff --git a/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg b/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg
index 34f5e0d12a9..e1f7df0d26c 100644
--- a/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg
+++ b/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg
@@ -151,4 +151,4 @@ VOLUME_ADJ_FILENAME= adjoint
 GRAD_OBJFUNC_FILENAME= of_grad.dat
 SURFACE_FILENAME= surface_flow
 SURFACE_ADJ_FILENAME= surface_adjoint
-OUTPUT_WRT_FREQ= 500
\ No newline at end of file
+OUTPUT_WRT_FREQ= 500

From be1eaaaddf2f2be2edb81469e6296ec8c47c5476 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Tue, 4 Apr 2023 15:15:05 +0100
Subject: [PATCH 343/656] remove legacy output from HB driver

---
 SU2_CFD/include/drivers/CDriver.hpp       |  4 --
 SU2_CFD/src/drivers/CDriver.cpp           | 46 ++++-------------------
 SU2_CFD/src/iteration/CFluidIteration.cpp |  6 +--
 TestCases/harmonic_balance/HB.cfg         |  2 +-
 4 files changed, 11 insertions(+), 47 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index 54adf5c0d35..5ae9eb4ae34 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -65,9 +65,6 @@ class CDriver : public CDriverBase {
   su2double MDOFs;   /*!< \brief Total number of DOFs in millions in the calculation (including ghost points).*/
   su2double MDOFsDomain; /*!< \brief Total number of DOFs in millions in the calculation (excluding ghost points).*/
 
-  ofstream** ConvHist_file; /*!< \brief Convergence history file.*/
-  ofstream FSIHist_file;    /*!< \brief FSI convergence history file.*/
-
   bool StopCalc,   /*!< \brief Stop computation flag.*/
       mixingplane, /*!< \brief mixing-plane simulation flag.*/
       fsi,         /*!< \brief FSI simulation flag.*/
@@ -589,7 +586,6 @@ class CFluidDriver : public CDriver {
  */
 class CHBDriver : public CFluidDriver {
  private:
-  COutputLegacy* output_legacy;
   unsigned short nInstHB;
   su2double** D; /*!< \brief Harmonic Balance operator. */
 
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index 22590e18259..75deebaabc1 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -301,7 +301,6 @@ void CDriver::InitializeContainers(){
    hierarchy over all zones, multigrid levels, equation sets, and equation
    terms as described in the comments below. ---*/
 
-  ConvHist_file                  = nullptr;
   iteration_container            = nullptr;
   output_container               = nullptr;
   integration_container          = nullptr;
@@ -360,7 +359,7 @@ void CDriver::Finalize() {
   }
 
   if (rank == MASTER_NODE)
-    cout << endl <<"------------------------- Finalizing Solver -------------------------" << endl;
+    cout <<"\n--------------------------- Finalizing Solver ---------------------------" << endl;
 
   for (iZone = 0; iZone < nZone; iZone++) {
     for (iInst = 0; iInst < nInst[iZone]; iInst++){
@@ -3237,26 +3236,9 @@ CHBDriver::CHBDriver(char* confFile,
 
   nInstHB = nInst[ZONE_0];
 
-  D = nullptr;
   /*--- allocate dynamic memory for the Harmonic Balance operator ---*/
-  D = new su2double*[nInstHB]; for (kInst = 0; kInst < nInstHB; kInst++) D[kInst] = new su2double[nInstHB];
-
-  output_legacy = COutputFactory::CreateLegacyOutput(config_container[ZONE_0]);
-
-  /*--- Open the convergence history file ---*/
-  ConvHist_file = nullptr;
-  ConvHist_file = new ofstream*[nZone];
-  for (iZone = 0; iZone < nZone; iZone++) {
-    ConvHist_file[iZone] = nullptr;
-    if (rank == MASTER_NODE){
-      ConvHist_file[iZone] = new ofstream[nInst[iZone]];
-      for (iInst = 0; iInst < nInst[iZone]; iInst++) {
-        output_legacy->SetConvHistoryHeader(&ConvHist_file[iZone][iInst], config_container[iZone], iZone, iInst);
-      }
-    }
-  }
-
-
+  D = new su2double*[nInstHB];
+  for (kInst = 0; kInst < nInstHB; kInst++) D[kInst] = new su2double[nInstHB];
 }
 
 CHBDriver::~CHBDriver(void) {
@@ -3266,17 +3248,6 @@ CHBDriver::~CHBDriver(void) {
   /*--- delete dynamic memory for the Harmonic Balance operator ---*/
   for (kInst = 0; kInst < nInstHB; kInst++) delete [] D[kInst];
   delete [] D;
-
-  if (rank == MASTER_NODE){
-  /*--- Close the convergence history file. ---*/
-  for (iZone = 0; iZone < nZone; iZone++) {
-    for (iInst = 0; iInst < nInstHB; iInst++) {
-      ConvHist_file[iZone][iInst].close();
-    }
-    delete [] ConvHist_file[iZone];
-  }
-  delete [] ConvHist_file;
-  }
 }
 
 
@@ -3295,13 +3266,10 @@ void CHBDriver::Run() {
         solver_container, numerics_container, config_container,
         surface_movement, grid_movement, FFDBox, ZONE_0, iInst);
 
-  /*--- Update the convergence history file (serial and parallel computations). ---*/
-
-  for (iZone = 0; iZone < nZone; iZone++) {
-    for (iInst = 0; iInst < nInst[iZone]; iInst++)
-      output_legacy->SetConvHistoryBody(&ConvHist_file[iZone][iInst], geometry_container, solver_container,
-          config_container, integration_container, false, UsedTime, iZone, iInst);
-  }
+  for (iInst = 0; iInst < nInstHB; iInst++)
+    iteration_container[ZONE_0][iInst]->Monitor(output_container[ZONE_0], integration_container, geometry_container,
+        solver_container, numerics_container, config_container,
+        surface_movement, grid_movement, FFDBox, ZONE_0, iInst);
 
 }
 
diff --git a/SU2_CFD/src/iteration/CFluidIteration.cpp b/SU2_CFD/src/iteration/CFluidIteration.cpp
index 7d2fa63b74f..6fd247d3579 100644
--- a/SU2_CFD/src/iteration/CFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CFluidIteration.cpp
@@ -214,9 +214,9 @@ bool CFluidIteration::Monitor(COutput* output, CIntegration**** integration, CGe
   UsedTime = StopTime - StartTime;
 
   if (config[val_iZone]->GetMultizone_Problem() || config[val_iZone]->GetSinglezone_Driver()) {
-    output->SetHistoryOutput(geometry[val_iZone][INST_0][MESH_0], solver[val_iZone][INST_0][MESH_0], config[val_iZone],
-                              config[val_iZone]->GetTimeIter(), config[val_iZone]->GetOuterIter(),
-                              config[val_iZone]->GetInnerIter());
+    output->SetHistoryOutput(geometry[val_iZone][val_iInst][MESH_0], solver[val_iZone][val_iInst][MESH_0],
+                             config[val_iZone], config[val_iZone]->GetTimeIter(), config[val_iZone]->GetOuterIter(),
+                             config[val_iZone]->GetInnerIter());
   }
 
   /*--- If convergence was reached --*/
diff --git a/TestCases/harmonic_balance/HB.cfg b/TestCases/harmonic_balance/HB.cfg
index b34daa826e0..333d2aafc0c 100644
--- a/TestCases/harmonic_balance/HB.cfg
+++ b/TestCases/harmonic_balance/HB.cfg
@@ -55,7 +55,7 @@ CFL_NUMBER= 1.0
 CFL_ADAPT= NO
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-ITER= 70000
+ITER= 10
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %

From 670e5157e6c2590c4d87074e1db411317bba82ee Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Tue, 4 Apr 2023 15:19:20 +0100
Subject: [PATCH 344/656] remove legacy output

---
 SU2_CFD/include/drivers/CDriver.hpp           |    1 -
 SU2_CFD/include/output/COutputFactory.hpp     |    8 -
 SU2_CFD/include/output/COutputLegacy.hpp      |  284 -
 .../src/drivers/CDiscAdjMultizoneDriver.cpp   |    1 -
 .../src/drivers/CDiscAdjSinglezoneDriver.cpp  |    1 -
 SU2_CFD/src/drivers/CDriver.cpp               |    2 -
 SU2_CFD/src/meson.build                       |    2 -
 SU2_CFD/src/output/COutputFactory.cpp         |   10 -
 SU2_CFD/src/output/output_physics.cpp         |  296 -
 .../src/output/output_structure_legacy.cpp    | 7227 -----------------
 10 files changed, 7832 deletions(-)
 delete mode 100644 SU2_CFD/include/output/COutputLegacy.hpp
 delete mode 100644 SU2_CFD/src/output/output_physics.cpp
 delete mode 100644 SU2_CFD/src/output/output_structure_legacy.cpp

diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index 5ae9eb4ae34..32646fd6454 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -37,7 +37,6 @@
 
 using namespace std;
 
-class COutputLegacy;
 class CInterpolator;
 class CIteration;
 class COutput;
diff --git a/SU2_CFD/include/output/COutputFactory.hpp b/SU2_CFD/include/output/COutputFactory.hpp
index 88a9994013b..0bfbeaf60ad 100644
--- a/SU2_CFD/include/output/COutputFactory.hpp
+++ b/SU2_CFD/include/output/COutputFactory.hpp
@@ -29,7 +29,6 @@
 
 class COutput;
 class CConfig;
-class COutputLegacy;
 
 class COutputFactory{
 
@@ -57,11 +56,4 @@ class COutputFactory{
    * \return                    - Pointer to the allocated multizone output
    */
   static COutput* CreateMultizoneOutput(CConfig *driverConfig, CConfig** config_container, int nDim);
-
-  /*!
-   * \brief Create legacy output
-   * \param config          - Pointer to the config
-   * \return                - Pointer to the allocated legacy output
-   */
-  static COutputLegacy* CreateLegacyOutput(CConfig *config);
 };
diff --git a/SU2_CFD/include/output/COutputLegacy.hpp b/SU2_CFD/include/output/COutputLegacy.hpp
deleted file mode 100644
index a1b413a95ee..00000000000
--- a/SU2_CFD/include/output/COutputLegacy.hpp
+++ /dev/null
@@ -1,284 +0,0 @@
-/*!
- * \file COutputLegacy.hpp
- * \brief Headers of the main subroutines for generating the file outputs.
- *        The subroutines and functions are in the <i>output_structure_legacy.cpp</i> file.
- * \author F. Palacios, T. Economon, M. Colonno
- * \version 7.5.1 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-
-#pragma once
-
-#include "../../../Common/include/parallelization/mpi_structure.hpp"
-
-#ifdef HAVE_CGNS
-  #include "cgnslib.h"
-#endif
-#ifdef HAVE_TECIO
-  #include "TECIO.h"
-#endif
-#include <fstream>
-#include <cmath>
-#include <vector>
-
-#include "../../../Common/include/option_structure.hpp"
-class CGeometry;
-class CConfig;
-class CSolver;
-class CIntegration;
-
-using namespace std;
-
-/*!
- * \class COutputLegacy
- * \brief Class for writing the flow, adjoint and linearized solver
- *        solution (including the history solution, and parallel stuff).
- * \author F. Palacios, T. Economon, M. Colonno.
- */
-class COutputLegacy {
-
-  su2double Sum_Total_RadialDistortion, Sum_Total_CircumferentialDistortion; // Add all the distortion to compute a run average.
-  bool turbo;
-  unsigned short nSpanWiseSections, nMarkerTurboPerf;
-
-  su2double **TotalStaticEfficiency,
-        **TotalTotalEfficiency,
-        **KineticEnergyLoss,
-        **TRadius,
-        **TotalPressureLoss,
-        **MassFlowIn,
-        **MassFlowOut,
-        **FlowAngleIn,
-        **FlowAngleIn_BC,
-        **FlowAngleOut,
-        **EulerianWork,
-        **TotalEnthalpyIn,
-        **TotalEnthalpyIn_BC,
-        **EntropyIn,
-        **EntropyOut,
-        **EntropyIn_BC,
-        **PressureRatio,
-        **TotalTemperatureIn,
-        **EnthalpyOut,
-        ***MachIn,
-        ***MachOut,
-        **VelocityOutIs,
-        **DensityIn,
-        **PressureIn,
-        ***TurboVelocityIn,
-        **DensityOut,
-        **PressureOut,
-        ***TurboVelocityOut,
-        **EnthalpyOutIs,
-        **EntropyGen,
-        **AbsFlowAngleIn,
-        **TotalEnthalpyOut,
-        **RothalpyIn,
-        **RothalpyOut,
-        **TotalEnthalpyOutIs,
-        **AbsFlowAngleOut,
-        **PressureOut_BC,
-        **TemperatureIn,
-        **TemperatureOut,
-        **TotalPressureIn,
-        **TotalPressureOut,
-        **TotalTemperatureOut,
-        **EnthalpyIn,
-        **TurbIntensityIn,
-        **Turb2LamViscRatioIn,
-        **TurbIntensityOut,
-        **Turb2LamViscRatioOut,
-        **NuFactorIn,
-        **NuFactorOut;
-
-protected:
-
-  int rank,   /*!< \brief MPI Rank. */
-  size;         /*!< \brief MPI Size. */
-
-public:
-
-  /*!
-   * \brief Constructor of the class.
-   */
-  COutputLegacy(CConfig *config);
-
-  /*!
-   * \brief Destructor of the class.
-   */
-  ~COutputLegacy(void);
-
-  /*!
-   * \brief Writes inverse design.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] iExtIter - Current external (time) iteration.
-   */
-  void SetCpInverseDesign(CSolver *solver_container, CGeometry *geometry, CConfig *config,
-                         unsigned long iExtIter);
-
-  /*!
-   * \brief Writes inverse design.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] iExtIter - Current external (time) iteration.
-   */
-  void SetHeatFluxInverseDesign(CSolver *solver_container, CGeometry *geometry, CConfig *config,
-                        unsigned long iExtIter);
-
-  /*!
-   * \brief Writes forces at different sections.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] output - Create output files.
-   */
-  void SpecialOutputSpanLoad(CSolver *solver, CGeometry *geometry, CConfig *config, bool output) const;
-
-  /*!
-   * \brief Writes one dimensional output.
-   * \author H. Kline
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] output - Create output files.
-   */
-  void SpecialOutputAnalyzeSurface(CSolver *solver, CGeometry *geometry, CConfig *config, bool output) const;
-
-  /*!
-   * \brief Create and write the file with the flow coefficient on the surface.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] FlowSolution - Flow solution.
-   * \param[in] iExtIter - Current external (time) iteration.
-   * \param[in] val_iZone - Current zone number in the grid file.
-   * \param[in] output - Create output files.
-   */
-  void SpecialOutputDistortion(CSolver *solver, CGeometry *geometry, CConfig *config, bool output) const;
-
-  /*!
-   * \brief Write the header of the history file.
-   * \param[in] ConvHist_file - Pointer to the convergence history file (which is defined in the main subroutine).
-   * \param[in] config - Definition of the particular problem.
-   */
-  void SetConvHistoryHeader(ofstream *ConvHist_file, CConfig *config, unsigned short val_iZone, unsigned short val_iInst);
-
-  /*!
-   * \brief Write the history file and the convergence on the screen for serial computations.
-   * \param[in] ConvHist_file - Pointer to the convergence history file (which is defined in the main subroutine).
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] integration - Generic subroutines for space integration, time integration, and monitoring.
-   * \param[in] iExtIter - Current external (time) iteration.
-   * \param[in] timeused - Current number of clock tick in the computation (related with total time).
-   * \param[in] val_nZone - iZone index.
-   */
-  void SetConvHistoryBody(ofstream *ConvHist_file, CGeometry ****geometry, CSolver *****solver_container, CConfig **config,
-                              CIntegration ****integration, bool DualTime, su2double timeused, unsigned short val_iZone, unsigned short val_iInst);
-
-  /*!
-   * \brief Write the history file and the convergence on the screen for serial computations.
-   * \param[in] solver - Container vector with all the solutions.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] output - Create output files.
-   */
-  void SpecialOutputForcesBreakdown(CSolver *****solver, CGeometry ****geometry, CConfig **config, unsigned short val_iZone, bool output) const;
-
-  /*!
-   * \brief Compute .
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] iExtIter - Current external (time) iteration.
-   */
-  void ComputeTurboPerformance(CSolver *solver_container, CGeometry *geometry, CConfig *config);
-
-  /*!
-   * \brief Compute .
-   * \param[in] config - Definition of the particular problem.
-   */
-  void WriteTurboPerfConvHistory(CConfig *config);
-
-  /*!
-   * \brief Write the output file for spanwise turboperformance.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] val_nZone - iZone index.
-   * \param[in] output - Create output files.
-   */
-  void SpecialOutputTurbo(CSolver *****solver_container, CGeometry ****geometry, CConfig **config, unsigned short val_iZone, bool output);
-
-  /*!
-   * \brief Give the Entropy Generation performance parameters for turbomachinery.
-   * \param[in] iMarkerTP - Marker turbo-performance.
-   * \param[in] iSpan - span section.
-   */
-  su2double GetEntropyGen(unsigned short iMarkerTP, unsigned short iSpan);
-
-  /*!
-   * \brief Give the Entropy Generation performance parameters for turbomachinery.
-   * \param[in] iMarkerTP - Marker turbo-performance.
-   * \param[in] iSpan - span section.
-   */
-  su2double GetFlowAngleOut(unsigned short iMarkerTP, unsigned short iSpan);
-
-  /*!
-   * \brief Give the Entropy Generation performance parameters for turbomachinery.
-   * \param[in] iMarkerTP - Marker turbo-performance.
-   * \param[in] iSpan - span section.
-   */
-  su2double GetMassFlowIn(unsigned short iMarkerTP, unsigned short iSpan);
-
-  /*!
-   * \brief Write the output file for harmonic balance for each time-instance.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] val_nZone - Number of Zones.
-   * \param[in] val_iZone - Zone index.
-   * \param[in] output - Create output files.
-   */
-  void SpecialOutputHarmonicBalance(CSolver *****solver, CGeometry ****geometry, CConfig **config, unsigned short iZone, unsigned short val_nZone, bool output) const;
-
-  /*!
-   * \brief Writes the special output files.
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] iExtIter - Current external (time) iteration.
-   * \param[in] val_iZone - Total number of domains in the grid file.
-   * \param[in] val_nZone - Total number of domains in the grid file.
-   */
-  void SetSpecialOutput(CSolver *****solver_container, CGeometry ****geometry, CConfig **config,
-                         unsigned long iExtIter, unsigned short val_nZone);
-
-};
-
-inline su2double COutputLegacy::GetEntropyGen(unsigned short iMarkerTP, unsigned short iSpan) { return EntropyGen[iMarkerTP][iSpan]; }
-
-inline su2double COutputLegacy::GetFlowAngleOut(unsigned short iMarkerTP, unsigned short iSpan) { return FlowAngleOut[iMarkerTP][iSpan]*180.0/PI_NUMBER; }
-
-inline su2double COutputLegacy::GetMassFlowIn(unsigned short iMarkerTP, unsigned short iSpan) { return MassFlowIn[iMarkerTP][iSpan]; }
diff --git a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
index b27f08247ff..586c9cabfdc 100644
--- a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
@@ -28,7 +28,6 @@
 #include "../../include/drivers/CDiscAdjMultizoneDriver.hpp"
 #include "../../include/solvers/CFEASolver.hpp"
 #include "../../include/output/COutputFactory.hpp"
-#include "../../include/output/COutputLegacy.hpp"
 #include "../../include/output/COutput.hpp"
 #include "../../include/iteration/CIterationFactory.hpp"
 
diff --git a/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
index 5f64b68455a..dd710f0867e 100644
--- a/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
@@ -28,7 +28,6 @@
 #include "../../include/drivers/CDiscAdjSinglezoneDriver.hpp"
 #include "../../include/output/tools/CWindowingTools.hpp"
 #include "../../include/output/COutputFactory.hpp"
-#include "../../include/output/COutputLegacy.hpp"
 #include "../../include/output/COutput.hpp"
 #include "../../include/iteration/CIterationFactory.hpp"
 #include "../../include/iteration/CTurboIteration.hpp"
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index 75deebaabc1..4dc172499de 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -38,8 +38,6 @@
 #include "../../include/output/COutputFactory.hpp"
 #include "../../include/output/COutput.hpp"
 
-#include "../../include/output/COutputLegacy.hpp"
-
 #include "../../../Common/include/interface_interpolation/CInterpolator.hpp"
 #include "../../../Common/include/interface_interpolation/CInterpolatorFactory.hpp"
 
diff --git a/SU2_CFD/src/meson.build b/SU2_CFD/src/meson.build
index 23fbeee0627..9ca0188ffc0 100644
--- a/SU2_CFD/src/meson.build
+++ b/SU2_CFD/src/meson.build
@@ -30,9 +30,7 @@ su2_cfd_src += files(['output/COutputFactory.cpp',
                       'output/CHeatOutput.cpp',
                       'output/CMeshOutput.cpp',
                       'output/CNEMOCompOutput.cpp',
-                      'output/output_physics.cpp',
                       'output/COutput.cpp',
-                      'output/output_structure_legacy.cpp',
                       'output/filewriter/CParallelDataSorter.cpp',
                       'output/filewriter/CFVMDataSorter.cpp',
                       'output/filewriter/CFEMDataSorter.cpp',
diff --git a/SU2_CFD/src/output/COutputFactory.cpp b/SU2_CFD/src/output/COutputFactory.cpp
index fe0de7c9397..4f8892712b6 100644
--- a/SU2_CFD/src/output/COutputFactory.cpp
+++ b/SU2_CFD/src/output/COutputFactory.cpp
@@ -26,7 +26,6 @@
  */
 
 #include "../../include/output/COutputFactory.hpp"
-#include "../../include/output/COutputLegacy.hpp"
 #include "../../include/output/COutput.hpp"
 #include "../../include/output/CMultizoneOutput.hpp"
 #include "../../include/output/CElasticityOutput.hpp"
@@ -90,12 +89,3 @@ COutput* COutputFactory::CreateMultizoneOutput(CConfig *driverConfig, CConfig**
 
   return output;
 }
-
-COutputLegacy* COutputFactory::CreateLegacyOutput(CConfig *config){
-
-  COutputLegacy* output = new COutputLegacy(config);
-
-  return output;
-
-}
-
diff --git a/SU2_CFD/src/output/output_physics.cpp b/SU2_CFD/src/output/output_physics.cpp
deleted file mode 100644
index 47fc5203d35..00000000000
--- a/SU2_CFD/src/output/output_physics.cpp
+++ /dev/null
@@ -1,296 +0,0 @@
-/*!
- * \file output_physics.cpp
- * \brief Main subroutines to compute physical output quantities such as CL, CD, entropy generation, mass flow, ecc... .
- * \author S. Vitale
- * \version 7.5.1 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-
-
-#include "../../include/output/COutputLegacy.hpp"
-
-#include "../../../Common/include/geometry/CGeometry.hpp"
-#include "../../include/solvers/CSolver.hpp"
-
-void COutputLegacy::ComputeTurboPerformance(CSolver *solver_container, CGeometry *geometry, CConfig *config) {
-
-  CFluidModel *FluidModel;
-  unsigned short nDim = geometry->GetnDim();
-  unsigned short iMarkerTP, iSpan, iDim, iStage, iBlade;
-  unsigned short nMarkerTP = config->GetnMarker_Turbomachinery();
-  FluidModel = solver_container->GetFluidModel();
-  su2double area, absVel2, soundSpeed, mach, tangVel, tangVel2, *relVel, relVel2;
-  su2double relPressureIn, relPressureOut, enthalpyOutIs, relVelOutIs2;
-  relVel = new su2double[nDim];
-  su2double muLam, kine, omega, nu;
-  bool turbulent = ((config->GetKind_Solver() == MAIN_SOLVER::RANS) || (config->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_RANS));
-  bool menter_sst       = (config->GetKind_Turb_Model() == TURB_MODEL::SST);
-
-  unsigned short nBladesRow, nStages;
-
-  nBladesRow = config->GetnMarker_Turbomachinery();
-  nStages    = SU2_TYPE::Int(nBladesRow/2);
-
-
-  /*--- Compute BC imposed value for convergence monitoring ---*/
-  for(iMarkerTP = 0; iMarkerTP < nMarkerTP; iMarkerTP++ ){
-    for(iSpan = 0; iSpan < config->GetnSpan_iZones(iMarkerTP) + 1; iSpan++){
-      if(config->GetRampOutletPressure() && config->GetInnerIter() > 0){
-        PressureOut_BC[iMarkerTP][iSpan] = config->GetMonitorOutletPressure()/config->GetPressure_Ref();
-      }
-      FluidModel->SetTDState_PT(config->GetTotalPressureIn_BC(), config->GetTotalTemperatureIn_BC());
-      TotalEnthalpyIn_BC[iMarkerTP][iSpan] = FluidModel->GetStaticEnergy()+ FluidModel->GetPressure()/FluidModel->GetDensity();
-      EntropyIn_BC[iMarkerTP][iSpan]       = FluidModel->GetEntropy();
-    }
-  }
-
-  /*--- Compute performance for each blade ---*/
-  for(iMarkerTP = 0; iMarkerTP < nMarkerTP; iMarkerTP++ ){
-    for(iSpan = 0; iSpan < config->GetnSpan_iZones(iMarkerTP) + 1; iSpan++){
-
-
-      /*--- INFLOW ---*/
-      /*--- Retrieve Inflow primitive quantities ---*/
-      DensityIn[iMarkerTP][iSpan]          = solver_container->GetDensityIn(iMarkerTP, iSpan);
-      PressureIn[iMarkerTP][iSpan]         = solver_container->GetPressureIn(iMarkerTP, iSpan);
-
-      absVel2 = 0.0;
-
-      for (iDim = 0; iDim < nDim; iDim++){
-        TurboVelocityIn[iMarkerTP][iSpan][iDim]    = solver_container->GetTurboVelocityIn(iMarkerTP, iSpan)[iDim];
-        absVel2   += TurboVelocityIn[iMarkerTP][iSpan][iDim]*TurboVelocityIn[iMarkerTP][iSpan][iDim];
-      }
-      TurboVelocityIn[iMarkerTP][iSpan][nDim] = sqrt(absVel2);
-
-      TRadius[iMarkerTP][iSpan]  = geometry->GetTurboRadiusIn(iMarkerTP, iSpan);
-      area                       = geometry->GetSpanAreaIn(iMarkerTP, iSpan);
-
-      /*--- Compute static Inflow quantities ---*/
-      FluidModel->SetTDState_Prho(PressureIn[iMarkerTP][iSpan], DensityIn[iMarkerTP][iSpan]);
-      EntropyIn[iMarkerTP][iSpan]          = FluidModel->GetEntropy();
-      MassFlowIn[iMarkerTP][iSpan]         = config->GetnBlades(iMarkerTP)*DensityIn[iMarkerTP][iSpan]*TurboVelocityIn[iMarkerTP][iSpan][0]*area;
-      AbsFlowAngleIn[iMarkerTP][iSpan]     = atan(TurboVelocityIn[iMarkerTP][iSpan][1]/TurboVelocityIn[iMarkerTP][iSpan][0]);
-      EnthalpyIn[iMarkerTP][iSpan]         = FluidModel->GetStaticEnergy() + PressureIn[iMarkerTP][iSpan]/DensityIn[iMarkerTP][iSpan];
-      soundSpeed                           = FluidModel->GetSoundSpeed();
-
-
-      /*--- Compute Total Inflow quantities ---*/
-      TotalEnthalpyIn[iMarkerTP][iSpan]    = EnthalpyIn[iMarkerTP][iSpan] + 0.5*absVel2;
-      FluidModel->SetTDState_hs(TotalEnthalpyIn[iMarkerTP][iSpan], EntropyIn[iMarkerTP][iSpan]);
-      TotalPressureIn[iMarkerTP][iSpan]    = FluidModel->GetPressure();
-      TotalTemperatureIn[iMarkerTP][iSpan] = FluidModel->GetTemperature();
-
-      /*--- Retrieve Inflow relative quantities ---*/
-      tangVel = geometry->GetTangGridVelIn(iMarkerTP, iSpan);
-      tangVel2 = tangVel*tangVel;
-
-      for (iDim = 0; iDim < nDim; iDim++){
-        relVel[iDim] = TurboVelocityIn[iMarkerTP][iSpan][iDim];
-      }
-      relVel[1] -= tangVel;
-
-      relVel2 = 0.0;
-      for (iDim = 0; iDim < nDim; iDim++){
-        relVel2 += relVel[iDim]*relVel[iDim];
-      }
-
-      /*--- Compute Total relative Inflow quantities ---*/
-      RothalpyIn[iMarkerTP][iSpan]  = EnthalpyIn[iMarkerTP][iSpan] + 0.5*relVel2 - 0.5*tangVel2;
-      FluidModel->SetTDState_hs(RothalpyIn[iMarkerTP][iSpan], EntropyIn[iMarkerTP][iSpan]);
-      relPressureIn   = FluidModel->GetPressure();
-
-      /*--- Compute kinematic relative Inflow quantities ---*/
-      FlowAngleIn[iMarkerTP][iSpan]    = atan(relVel[1]/relVel[0]);
-      mach          = 0.0;
-      for (iDim = 0; iDim < nDim; iDim++){
-        MachIn[iMarkerTP][iSpan][iDim] = relVel[iDim]/soundSpeed;
-        mach = MachIn[iMarkerTP][iSpan][iDim]*MachIn[iMarkerTP][iSpan][iDim];
-      }
-      MachIn[iMarkerTP][iSpan][nDim]   = sqrt(mach);
-
-      /*--- Compute Turbulent Inflow quantities ---*/
-      if(turbulent){
-        FluidModel->SetTDState_Prho(PressureIn[iMarkerTP][iSpan], DensityIn[iMarkerTP][iSpan]);
-        muLam  = FluidModel->GetLaminarViscosity();
-        if(menter_sst){
-          kine   = solver_container->GetKineIn(iMarkerTP, iSpan);
-          omega  = solver_container->GetOmegaIn(iMarkerTP, iSpan);
-          TurbIntensityIn[iMarkerTP][iSpan]     =  sqrt(2.0/3.0*kine/absVel2);
-          Turb2LamViscRatioIn[iMarkerTP][iSpan] = DensityIn[iMarkerTP][iSpan]*kine/(muLam*omega);
-//          TurbIntensityIn[iMarkerTP][iSpan]     =  kine;
-//          Turb2LamViscRatioIn[iMarkerTP][iSpan] = omega;
-        }
-        else{
-          nu = solver_container->GetNuIn(iMarkerTP, iSpan);
-          NuFactorIn[iMarkerTP][iSpan]          = nu*DensityIn[iMarkerTP][iSpan]/muLam;
-          if (config->GetSAParsedOptions().bc) {
-            NuFactorIn[iMarkerTP][iSpan]        = nu*DensityIn[iMarkerTP][iSpan]/muLam/0.005;
-          }
-        }
-      }
-
-      /*--- OUTFLOW ---*/
-      /*--- Retrieve Outflow primitive quantities ---*/
-      DensityOut[iMarkerTP][iSpan]         = solver_container->GetDensityOut(iMarkerTP, iSpan);
-      PressureOut[iMarkerTP][iSpan]        = solver_container->GetPressureOut(iMarkerTP, iSpan);
-      absVel2 = 0.0;
-
-      for (iDim = 0; iDim < nDim; iDim++){
-        TurboVelocityOut[iMarkerTP][iSpan][iDim]    = solver_container->GetTurboVelocityOut(iMarkerTP, iSpan)[iDim];
-        absVel2   += TurboVelocityOut[iMarkerTP][iSpan][iDim]*TurboVelocityOut[iMarkerTP][iSpan][iDim];
-      }
-      TurboVelocityOut[iMarkerTP][iSpan][nDim] = sqrt(absVel2);
-
-
-      for (iDim = 0; iDim < 3; iDim++){
-      }
-      area   = geometry->GetSpanAreaOut(iMarkerTP, iSpan);
-
-
-      /*--- Compute all the Outflow quantities ---*/
-      FluidModel->SetTDState_Prho(PressureOut[iMarkerTP][iSpan], DensityOut[iMarkerTP][iSpan]);
-      EntropyOut[iMarkerTP][iSpan]          = FluidModel->GetEntropy();
-      MassFlowOut[iMarkerTP][iSpan]         = config->GetnBlades(iMarkerTP)*DensityOut[iMarkerTP][iSpan]*TurboVelocityOut[iMarkerTP][iSpan][0]*area;
-      AbsFlowAngleOut[iMarkerTP][iSpan]     = atan(TurboVelocityOut[iMarkerTP][iSpan][1]/TurboVelocityOut[iMarkerTP][iSpan][0]);
-      EnthalpyOut[iMarkerTP][iSpan]         = FluidModel->GetStaticEnergy() + PressureOut[iMarkerTP][iSpan]/DensityOut[iMarkerTP][iSpan];
-      soundSpeed                            = FluidModel->GetSoundSpeed();
-
-      /*--- Compute Total Outflow quantities ---*/
-      TotalEnthalpyOut[iMarkerTP][iSpan]    = EnthalpyOut[iMarkerTP][iSpan] + 0.5*absVel2;
-      FluidModel->SetTDState_hs(TotalEnthalpyOut[iMarkerTP][iSpan], EntropyOut[iMarkerTP][iSpan]);
-      TotalPressureOut[iMarkerTP][iSpan]    = FluidModel->GetPressure();
-      TotalTemperatureOut[iMarkerTP][iSpan] = FluidModel->GetTemperature();
-
-      /*--- Retrieve relative Outflow  quantities ---*/
-      tangVel  = geometry->GetTangGridVelOut(iMarkerTP, iSpan);
-      tangVel2 = tangVel*tangVel;
-
-      for (iDim = 0; iDim < nDim; iDim++){
-        relVel[iDim] = TurboVelocityOut[iMarkerTP][iSpan][iDim];
-      }
-      relVel[1] -= tangVel;
-
-      relVel2 = 0.0;
-      for (iDim = 0; iDim < nDim; iDim++){
-        relVel2 += relVel[iDim]*relVel[iDim];
-      }
-
-      /*--- Compute Total relative Outflow quantities ---*/
-      RothalpyOut[iMarkerTP][iSpan] = EnthalpyOut[iMarkerTP][iSpan] + 0.5*relVel2 - 0.5*tangVel2;
-      FluidModel->SetTDState_hs(RothalpyOut[iMarkerTP][iSpan], EntropyOut[iMarkerTP][iSpan]);
-      relPressureOut  = FluidModel->GetPressure();
-
-      /*--- Compute isentropic Outflow quantities ---*/
-      FluidModel->SetTDState_Ps(PressureOut[iMarkerTP][iSpan], EntropyIn[iMarkerTP][iSpan]);
-      enthalpyOutIs   = FluidModel->GetStaticEnergy() + PressureOut[iMarkerTP][iSpan]/FluidModel->GetDensity();
-      relVelOutIs2    = 2*(RothalpyOut[iMarkerTP][iSpan] - enthalpyOutIs) + tangVel2;
-
-
-      /*--- Compute kinematic relative Outflow quantities ---*/
-      FlowAngleOut[iMarkerTP][iSpan] = atan(relVel[1]/relVel[0]);
-      mach   = 0.0;
-      for (iDim = 0; iDim < nDim; iDim++){
-        MachOut[iMarkerTP][iSpan][iDim] = relVel[iDim]/soundSpeed;
-        mach = MachOut[iMarkerTP][iSpan][iDim]*MachOut[iMarkerTP][iSpan][iDim];
-      }
-      MachOut[iMarkerTP][iSpan][nDim]   = sqrt(mach);
-
-      /*--- Compute Turbulent Outflow quantities ---*/
-      if(turbulent){
-        FluidModel->SetTDState_Prho(PressureOut[iMarkerTP][iSpan], DensityOut[iMarkerTP][iSpan]);
-        muLam  = FluidModel->GetLaminarViscosity();
-        if(menter_sst){
-          kine   = solver_container->GetKineOut(iMarkerTP, iSpan);
-          omega  = solver_container->GetOmegaOut(iMarkerTP, iSpan);
-          TurbIntensityOut[iMarkerTP][iSpan]     =  sqrt(2.0/3.0*kine/absVel2);
-          Turb2LamViscRatioOut[iMarkerTP][iSpan] = DensityOut[iMarkerTP][iSpan]*kine/(muLam*omega);
-//          TurbIntensityOut[iMarkerTP][iSpan]     =  kine;
-//          Turb2LamViscRatioOut[iMarkerTP][iSpan] = omega;
-        }
-        else{
-          nu = solver_container->GetNuOut(iMarkerTP, iSpan);
-          NuFactorOut[iMarkerTP][iSpan]          = nu*DensityOut[iMarkerTP][iSpan]/muLam;
-          if (config->GetSAParsedOptions().bc) {
-            NuFactorOut[iMarkerTP][iSpan]        = nu*DensityOut[iMarkerTP][iSpan]/muLam/0.005;
-          }
-        }
-      }
-
-      /*--- TURBO-PERFORMANCE---*/
-      EntropyGen[iMarkerTP][iSpan]         = (EntropyOut[iMarkerTP][iSpan] - EntropyIn[iMarkerTP][iSpan])/abs(EntropyIn_BC[iMarkerTP][iSpan] + 1);
-      EulerianWork[iMarkerTP][iSpan]       = TotalEnthalpyIn[iMarkerTP][iSpan] - TotalEnthalpyOut[iMarkerTP][iSpan];
-      TotalPressureLoss[iMarkerTP][iSpan]  = (relPressureIn - relPressureOut)/(relPressureIn - PressureOut[iMarkerTP][iSpan]);
-      KineticEnergyLoss[iMarkerTP][iSpan]  = 2*(EnthalpyOut[iMarkerTP][iSpan] - enthalpyOutIs)/relVelOutIs2;
-      PressureRatio[iMarkerTP][iSpan]      = TotalPressureOut[iMarkerTP][iSpan]/TotalPressureIn[iMarkerTP][iSpan];
-      EnthalpyOutIs[iMarkerTP][iSpan]      = (pow(TotalPressureOut[iMarkerTP][iSpan]/TotalPressureIn[iMarkerTP][iSpan], 0.4/1.4) - 1.0)/(TotalTemperatureOut[iMarkerTP][iSpan]/TotalTemperatureIn[iMarkerTP][iSpan] -1.0);
-    }
-  }
-
-  if(nBladesRow > 1){
-    /*--- Compute performance for each stage ---*/
-
-    EulerianWork[nBladesRow + nStages][nSpanWiseSections]           = 0.0;
-    /*---Comnpute performance for each stage---*/
-    for(iStage = 0; iStage < nStages; iStage++ ){
-      FluidModel->SetTDState_Ps(PressureOut[iStage*2 +1][config->GetnSpan_iZones(iStage*2 +1)], EntropyIn[iStage*2][config->GetnSpan_iZones(iStage*2)]);
-      EnthalpyOutIs[nBladesRow + iStage][nSpanWiseSections]         = FluidModel->GetStaticEnergy() + PressureOut[iStage*2 +1][config->GetnSpan_iZones(iStage*2 +1)]/FluidModel->GetDensity();
-      FluidModel->SetTDState_Prho(PressureOut[iStage*2 +1][config->GetnSpan_iZones(iStage*2 +1)], DensityOut[iStage*2 +1][config->GetnSpan_iZones(iStage*2 +1)]);
-      absVel2 = 0.0;
-      for (iDim = 0; iDim<nDim; iDim++)
-        absVel2 += TurboVelocityOut[iStage*2 +1][config->GetnSpan_iZones(iStage*2 +1)][iDim]*TurboVelocityOut[iStage*2 +1][config->GetnSpan_iZones(iStage*2 +1)][iDim];
-      TotalEnthalpyOutIs[nBladesRow + iStage][nSpanWiseSections]    = EnthalpyOutIs[nBladesRow + iStage][nSpanWiseSections] + 0.5*absVel2;
-
-      TotalTotalEfficiency[nBladesRow + iStage][nSpanWiseSections]  = (TotalEnthalpyIn[iStage*2][config->GetnSpan_iZones(iStage*2)] - TotalEnthalpyOut[iStage*2 + 1][config->GetnSpan_iZones(iStage*2 +1)]);
-      TotalTotalEfficiency[nBladesRow + iStage][nSpanWiseSections]  /= (TotalEnthalpyIn[iStage*2][config->GetnSpan_iZones(iStage*2)] - TotalEnthalpyOutIs[nBladesRow + iStage][nSpanWiseSections]);
-      TotalStaticEfficiency[nBladesRow + iStage][nSpanWiseSections] = (TotalEnthalpyIn[iStage*2][config->GetnSpan_iZones(iStage*2)] - TotalEnthalpyOut[iStage*2 + 1][config->GetnSpan_iZones(iStage*2+1)]);
-      TotalStaticEfficiency[nBladesRow + iStage][nSpanWiseSections] /= (TotalEnthalpyIn[iStage*2][config->GetnSpan_iZones(iStage*2)] - EnthalpyOutIs[nBladesRow + iStage][nSpanWiseSections]);
-      PressureRatio[nBladesRow + iStage][nSpanWiseSections]         = (PressureRatio[iStage*2][config->GetnSpan_iZones(iStage*2)]*PressureOut[iStage*2][config->GetnSpan_iZones(iStage*2)]/PressureOut[iStage*2 + 1][config->GetnSpan_iZones(iStage*2+1)]);
-      MassFlowIn[nBladesRow + iStage][nSpanWiseSections]            = MassFlowIn[iStage*2][config->GetnSpan_iZones(iStage*2)];
-      MassFlowOut[nBladesRow + iStage][nSpanWiseSections]           = MassFlowOut[iStage*2 + 1][config->GetnSpan_iZones(iStage*2+1)];
-      EntropyGen[nBladesRow + iStage][nSpanWiseSections]            = EntropyGen[iStage*2 + 1][config->GetnSpan_iZones(iStage*2 +1)] + EntropyGen[iStage*2][config->GetnSpan_iZones(iStage*2)];
-
-    }
-
-    /*---Compute turbo performance for full machine---*/
-    FluidModel->SetTDState_Ps(PressureOut[nBladesRow-1][config->GetnSpan_iZones(nBladesRow-1)], EntropyIn[0][config->GetnSpan_iZones(0)]);
-    EnthalpyOutIs[nBladesRow + nStages][nSpanWiseSections]          = FluidModel->GetStaticEnergy() + PressureOut[nBladesRow-1][config->GetnSpan_iZones(nBladesRow-1)]/FluidModel->GetDensity();
-    FluidModel->SetTDState_Prho(PressureOut[nBladesRow-1][config->GetnSpan_iZones(nBladesRow-1)], DensityOut[nBladesRow-1][config->GetnSpan_iZones(nBladesRow-1)]);
-    absVel2 = 0.0;
-    for (iDim = 0; iDim<nDim;iDim++) absVel2 += TurboVelocityOut[nBladesRow-1][config->GetnSpan_iZones(nBladesRow-1)][iDim]*TurboVelocityOut[nBladesRow-1][config->GetnSpan_iZones(nBladesRow-1)][iDim];
-    TotalEnthalpyOutIs[nBladesRow + nStages][nSpanWiseSections]     = EnthalpyOutIs[nBladesRow + nStages][nSpanWiseSections] + 0.5*absVel2;
-
-    TotalTotalEfficiency[nBladesRow + nStages][nSpanWiseSections]   = (TotalEnthalpyIn[0][config->GetnSpan_iZones(0)] - TotalEnthalpyOut[nBladesRow-1][config->GetnSpan_iZones(nBladesRow-1)]);
-    TotalTotalEfficiency[nBladesRow + nStages][nSpanWiseSections]  /= (TotalEnthalpyIn[0][config->GetnSpan_iZones(0)] - TotalEnthalpyOutIs[nBladesRow + nStages][nSpanWiseSections]);
-    TotalStaticEfficiency[nBladesRow +nStages][nSpanWiseSections]   = (TotalEnthalpyIn[0][config->GetnSpan_iZones(0)] - TotalEnthalpyOut[nBladesRow-1][config->GetnSpan_iZones(nBladesRow-1)]);
-    TotalStaticEfficiency[nBladesRow +nStages][nSpanWiseSections]  /= (TotalEnthalpyIn[0][config->GetnSpan_iZones(0)] - EnthalpyOutIs[nBladesRow + nStages][nSpanWiseSections]);
-    PressureRatio[nBladesRow + nStages][nSpanWiseSections]          = PressureRatio[0][config->GetnSpan_iZones(0)]*PressureOut[0][config->GetnSpan_iZones(0)]/PressureOut[nBladesRow-1][config->GetnSpan_iZones(nBladesRow-1)];
-    MassFlowIn[nBladesRow + nStages][nSpanWiseSections]             = MassFlowIn[0][config->GetnSpan_iZones(0)];
-    MassFlowOut[nBladesRow + nStages][nSpanWiseSections]            = MassFlowOut[nBladesRow-1][config->GetnSpan_iZones(nBladesRow-1)];
-
-    EntropyGen[nBladesRow + nStages][nSpanWiseSections]             = 0.0;
-    for(iBlade = 0; iBlade < nBladesRow; iBlade++ ){
-      EntropyGen[nBladesRow + nStages][nSpanWiseSections]          += EntropyGen[iBlade][config->GetnSpan_iZones(iBlade)];
-    }
-  }
-
-  delete [] relVel;
-}
diff --git a/SU2_CFD/src/output/output_structure_legacy.cpp b/SU2_CFD/src/output/output_structure_legacy.cpp
deleted file mode 100644
index 40e495d6b66..00000000000
--- a/SU2_CFD/src/output/output_structure_legacy.cpp
+++ /dev/null
@@ -1,7227 +0,0 @@
-/*!
- * \file output_structure_legacy.cpp
- * \brief Main subroutines for output solver information
- * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
-
-
-#include "../../include/output/COutputLegacy.hpp"
-
-#include "../../../Common/include/geometry/CGeometry.hpp"
-#include "../../include/solvers/CBaselineSolver.hpp"
-#include "../../include/fluid/CCoolProp.hpp"
-
-COutputLegacy::COutputLegacy(CConfig *config) {
-
-  rank = SU2_MPI::GetRank();
-  size = SU2_MPI::GetSize();
-
-  unsigned short iDim, iSpan, iMarker;
-
-  /*--- Initialize point and connectivity counters to zero. ---*/
-
-  /*--- Initialize turbo flag ---*/
-  turbo = config->GetBoolTurbomachinery();
-
-  if(turbo){
-    /*--- Initializate quantities for turboperformace ---*/
-    nSpanWiseSections = config->GetnSpanMaxAllZones();
-    nMarkerTurboPerf  = config->GetnMarker_TurboPerformance();
-
-
-    TotalStaticEfficiency         = new su2double*[nMarkerTurboPerf];
-    TotalTotalEfficiency          = new su2double*[nMarkerTurboPerf];
-    KineticEnergyLoss             = new su2double*[nMarkerTurboPerf];
-    TRadius                       = new su2double*[nMarkerTurboPerf];
-    TotalPressureLoss             = new su2double*[nMarkerTurboPerf];
-    MassFlowIn                    = new su2double*[nMarkerTurboPerf];
-    MassFlowOut                   = new su2double*[nMarkerTurboPerf];
-    FlowAngleIn                   = new su2double*[nMarkerTurboPerf];
-    FlowAngleIn_BC                = new su2double*[nMarkerTurboPerf];
-    FlowAngleOut                  = new su2double*[nMarkerTurboPerf];
-    EulerianWork                  = new su2double*[nMarkerTurboPerf];
-    TotalEnthalpyIn               = new su2double*[nMarkerTurboPerf];
-    TotalEnthalpyIn_BC            = new su2double*[nMarkerTurboPerf];
-    EntropyIn                     = new su2double*[nMarkerTurboPerf];
-    EntropyOut                    = new su2double*[nMarkerTurboPerf];
-    EntropyIn_BC                  = new su2double*[nMarkerTurboPerf];
-    PressureRatio                 = new su2double*[nMarkerTurboPerf];
-    TotalTemperatureIn            = new su2double*[nMarkerTurboPerf];
-    EnthalpyOut                   = new su2double*[nMarkerTurboPerf];
-    MachIn                        = new su2double**[nMarkerTurboPerf];
-    MachOut                       = new su2double**[nMarkerTurboPerf];
-    VelocityOutIs                 = new su2double*[nMarkerTurboPerf];
-    DensityIn                     = new su2double*[nMarkerTurboPerf];
-    PressureIn                    = new su2double*[nMarkerTurboPerf];
-    TurboVelocityIn               = new su2double**[nMarkerTurboPerf];
-    DensityOut                    = new su2double*[nMarkerTurboPerf];
-    PressureOut                   = new su2double*[nMarkerTurboPerf];
-    TurboVelocityOut              = new su2double**[nMarkerTurboPerf];
-    EnthalpyOutIs                 = new su2double*[nMarkerTurboPerf];
-    EntropyGen                    = new su2double*[nMarkerTurboPerf];
-    AbsFlowAngleIn                = new su2double*[nMarkerTurboPerf];
-    TotalEnthalpyOut              = new su2double*[nMarkerTurboPerf];
-    TotalEnthalpyOutIs            = new su2double*[nMarkerTurboPerf];
-    RothalpyIn                    = new su2double*[nMarkerTurboPerf];
-    RothalpyOut                   = new su2double*[nMarkerTurboPerf];
-    AbsFlowAngleOut               = new su2double*[nMarkerTurboPerf];
-    PressureOut_BC                = new su2double*[nMarkerTurboPerf];
-    TemperatureIn                 = new su2double*[nMarkerTurboPerf];
-    TemperatureOut                = new su2double*[nMarkerTurboPerf];
-    TotalPressureIn               = new su2double*[nMarkerTurboPerf];
-    TotalPressureOut              = new su2double*[nMarkerTurboPerf];
-    TotalTemperatureOut           = new su2double*[nMarkerTurboPerf];
-    EnthalpyIn                    = new su2double*[nMarkerTurboPerf];
-    TurbIntensityIn               = new su2double*[nMarkerTurboPerf];
-    Turb2LamViscRatioIn           = new su2double*[nMarkerTurboPerf];
-    TurbIntensityOut              = new su2double*[nMarkerTurboPerf];
-    Turb2LamViscRatioOut          = new su2double*[nMarkerTurboPerf];
-    NuFactorIn                    = new su2double*[nMarkerTurboPerf];
-    NuFactorOut                   = new su2double*[nMarkerTurboPerf];
-
-    for (iMarker = 0; iMarker < nMarkerTurboPerf; iMarker++){
-      TotalStaticEfficiency   [iMarker] = new su2double [nSpanWiseSections + 1];
-      TotalTotalEfficiency    [iMarker] = new su2double [nSpanWiseSections + 1];
-      KineticEnergyLoss       [iMarker] = new su2double [nSpanWiseSections + 1];
-      TRadius                 [iMarker] = new su2double [nSpanWiseSections + 1];
-      TotalPressureLoss       [iMarker] = new su2double [nSpanWiseSections + 1];
-      MassFlowIn              [iMarker] = new su2double [nSpanWiseSections + 1];
-      MassFlowOut             [iMarker] = new su2double [nSpanWiseSections + 1];
-      FlowAngleIn             [iMarker] = new su2double [nSpanWiseSections + 1];
-      FlowAngleIn_BC          [iMarker] = new su2double [nSpanWiseSections + 1];
-      FlowAngleOut            [iMarker] = new su2double [nSpanWiseSections + 1];
-      EulerianWork            [iMarker] = new su2double [nSpanWiseSections + 1];
-      TotalEnthalpyIn         [iMarker] = new su2double [nSpanWiseSections + 1];
-      TotalEnthalpyIn_BC      [iMarker] = new su2double [nSpanWiseSections + 1];
-      EntropyIn               [iMarker] = new su2double [nSpanWiseSections + 1];
-      EntropyOut              [iMarker] = new su2double [nSpanWiseSections + 1];
-      EntropyIn_BC            [iMarker] = new su2double [nSpanWiseSections + 1];
-      PressureRatio           [iMarker] = new su2double [nSpanWiseSections + 1];
-      TotalTemperatureIn      [iMarker] = new su2double [nSpanWiseSections + 1];
-      EnthalpyOut             [iMarker] = new su2double [nSpanWiseSections + 1];
-      MachIn                  [iMarker] = new su2double*[nSpanWiseSections + 1];
-      MachOut                 [iMarker] = new su2double*[nSpanWiseSections + 1];
-      VelocityOutIs           [iMarker] = new su2double [nSpanWiseSections + 1];
-      DensityIn               [iMarker] = new su2double [nSpanWiseSections + 1];
-      PressureIn              [iMarker] = new su2double [nSpanWiseSections + 1];
-      TurboVelocityIn         [iMarker] = new su2double*[nSpanWiseSections + 1];
-      DensityOut              [iMarker] = new su2double [nSpanWiseSections + 1];
-      PressureOut             [iMarker] = new su2double [nSpanWiseSections + 1];
-      TurboVelocityOut        [iMarker] = new su2double*[nSpanWiseSections + 1];
-      EnthalpyOutIs           [iMarker] = new su2double [nSpanWiseSections + 1];
-      EntropyGen              [iMarker] = new su2double [nSpanWiseSections + 1];
-      AbsFlowAngleIn          [iMarker] = new su2double [nSpanWiseSections + 1];
-      TotalEnthalpyOut        [iMarker] = new su2double [nSpanWiseSections + 1];
-      TotalEnthalpyOutIs      [iMarker] = new su2double [nSpanWiseSections + 1];
-      RothalpyIn              [iMarker] = new su2double [nSpanWiseSections + 1];
-      RothalpyOut             [iMarker] = new su2double [nSpanWiseSections + 1];
-      AbsFlowAngleOut         [iMarker] = new su2double [nSpanWiseSections + 1];
-      PressureOut_BC          [iMarker] = new su2double [nSpanWiseSections + 1];
-      TemperatureIn           [iMarker] = new su2double [nSpanWiseSections + 1];
-      TemperatureOut          [iMarker] = new su2double [nSpanWiseSections + 1];
-      TotalPressureIn         [iMarker] = new su2double [nSpanWiseSections + 1];
-      TotalPressureOut        [iMarker] = new su2double [nSpanWiseSections + 1];
-      TotalTemperatureOut     [iMarker] = new su2double [nSpanWiseSections + 1];
-      EnthalpyIn              [iMarker] = new su2double [nSpanWiseSections + 1];
-      TurbIntensityIn         [iMarker] = new su2double [nSpanWiseSections + 1];
-      Turb2LamViscRatioIn     [iMarker] = new su2double [nSpanWiseSections + 1];
-      TurbIntensityOut        [iMarker] = new su2double [nSpanWiseSections + 1];
-      Turb2LamViscRatioOut    [iMarker] = new su2double [nSpanWiseSections + 1];
-      NuFactorIn              [iMarker] = new su2double [nSpanWiseSections + 1];
-      NuFactorOut             [iMarker] = new su2double [nSpanWiseSections + 1];
-
-
-      for (iSpan = 0; iSpan < nSpanWiseSections + 1; iSpan++){
-        TotalStaticEfficiency   [iMarker][iSpan] = 0.0;
-        TotalTotalEfficiency    [iMarker][iSpan] = 0.0;
-        KineticEnergyLoss       [iMarker][iSpan] = 0.0;
-        TRadius                 [iMarker][iSpan] = 0.0;
-        TotalPressureLoss       [iMarker][iSpan] = 0.0;
-        MassFlowIn              [iMarker][iSpan] = 0.0;
-        MassFlowOut             [iMarker][iSpan] = 0.0;
-        FlowAngleIn             [iMarker][iSpan] = 0.0;
-        FlowAngleIn_BC          [iMarker][iSpan] = config->GetFlowAngleIn_BC();
-        FlowAngleOut            [iMarker][iSpan] = 0.0;
-        EulerianWork            [iMarker][iSpan] = 0.0;
-        TotalEnthalpyIn         [iMarker][iSpan] = 0.0;
-        TotalEnthalpyIn_BC      [iMarker][iSpan] = 0.0;
-        EntropyIn               [iMarker][iSpan] = 0.0;
-        EntropyOut              [iMarker][iSpan] = 0.0;
-        EntropyIn_BC            [iMarker][iSpan] = 0.0;
-        PressureRatio           [iMarker][iSpan] = 0.0;
-        TotalTemperatureIn      [iMarker][iSpan] = 0.0;
-        EnthalpyOut             [iMarker][iSpan] = 0.0;
-
-
-        VelocityOutIs           [iMarker][iSpan] = 0.0;
-        DensityIn               [iMarker][iSpan] = 0.0;
-        PressureIn              [iMarker][iSpan] = 0.0;
-
-        DensityOut              [iMarker][iSpan] = 0.0;
-        PressureOut             [iMarker][iSpan] = 0.0;
-
-        EnthalpyOutIs           [iMarker][iSpan] = 0.0;
-        EntropyGen              [iMarker][iSpan] = 0.0;
-        AbsFlowAngleIn          [iMarker][iSpan] = 0.0;
-        TotalEnthalpyOut        [iMarker][iSpan] = 0.0;
-        TotalEnthalpyOutIs      [iMarker][iSpan] = 0.0;
-        RothalpyIn              [iMarker][iSpan] = 0.0;
-        RothalpyOut             [iMarker][iSpan] = 0.0;
-        AbsFlowAngleOut         [iMarker][iSpan] = 0.0;
-        PressureOut_BC          [iMarker][iSpan] = config->GetPressureOut_BC();
-
-        TemperatureIn           [iMarker][iSpan] = 0.0;
-        TemperatureOut          [iMarker][iSpan] = 0.0;
-        TotalPressureIn         [iMarker][iSpan] = 0.0;
-        TotalPressureOut        [iMarker][iSpan] = 0.0;
-        TotalTemperatureOut     [iMarker][iSpan] = 0.0;
-        EnthalpyIn              [iMarker][iSpan] = 0.0;
-        TurbIntensityIn         [iMarker][iSpan] = 0.0;
-        Turb2LamViscRatioIn     [iMarker][iSpan] = 0.0;
-        TurbIntensityOut        [iMarker][iSpan] = 0.0;
-        Turb2LamViscRatioOut    [iMarker][iSpan] = 0.0;
-        NuFactorIn              [iMarker][iSpan] = 0.0;
-        NuFactorOut             [iMarker][iSpan] = 0.0;
-        MachIn                  [iMarker][iSpan] = new su2double[4];
-        MachOut                 [iMarker][iSpan] = new su2double[4];
-        TurboVelocityIn         [iMarker][iSpan] = new su2double[4];
-        TurboVelocityOut        [iMarker][iSpan] = new su2double[4];
-
-        for (iDim = 0; iDim < 4; iDim++){
-          MachIn           [iMarker][iSpan][iDim]   = 0.0;
-          MachOut          [iMarker][iSpan][iDim]   = 0.0;
-          TurboVelocityIn  [iMarker][iSpan][iDim]   = 0.0;
-          TurboVelocityOut [iMarker][iSpan][iDim]   = 0.0;
-        }
-      }
-    }
-  }
-}
-
-COutputLegacy::~COutputLegacy(void) {
-  /* delete pointers initialized at construction*/
-  /* Coords and Conn_*(Connectivity) have their own dealloc functions */
-  /* Data is taken care of in DeallocateSolution function */
-
-  /*--- Delete turboperformance pointers initiliazed at constrction  ---*/
-  unsigned short iMarker, iSpan;
-  if(turbo){
-    for(iMarker = 0; iMarker< nMarkerTurboPerf; iMarker++){
-      for(iSpan=0; iSpan<nSpanWiseSections+1; iSpan++){
-        delete [] MachIn          [iMarker][iSpan];
-        delete [] MachOut         [iMarker][iSpan];
-        delete [] TurboVelocityIn [iMarker][iSpan];
-        delete [] TurboVelocityOut[iMarker][iSpan];
-      }
-    }
-    for(iMarker = 0; iMarker< nMarkerTurboPerf; iMarker++){
-      delete [] TotalStaticEfficiency[iMarker];
-      delete [] TotalTotalEfficiency [iMarker];
-      delete [] KineticEnergyLoss    [iMarker];
-      delete [] TRadius              [iMarker];
-      delete [] TotalPressureLoss    [iMarker];
-      delete [] MassFlowIn           [iMarker];
-      delete [] MassFlowOut          [iMarker];
-      delete [] FlowAngleIn          [iMarker];
-      delete [] FlowAngleOut         [iMarker];
-      delete [] EulerianWork         [iMarker];
-      delete [] TotalEnthalpyIn      [iMarker];
-      delete [] TotalEnthalpyOut     [iMarker];
-      delete [] TotalEnthalpyOutIs   [iMarker];
-      delete [] PressureRatio        [iMarker];
-      delete [] EnthalpyOut          [iMarker];
-      delete [] VelocityOutIs        [iMarker];
-      delete [] TotalTemperatureIn   [iMarker];
-      delete [] FlowAngleIn_BC       [iMarker];
-      delete [] EntropyIn            [iMarker];
-      delete [] EntropyIn_BC         [iMarker];
-      delete [] EntropyOut           [iMarker];
-      delete [] TotalEnthalpyIn_BC   [iMarker];
-      delete [] DensityIn            [iMarker];
-      delete [] PressureIn           [iMarker];
-      delete [] DensityOut           [iMarker];
-      delete [] PressureOut          [iMarker];
-      delete [] EnthalpyOutIs        [iMarker];
-      delete [] EntropyGen           [iMarker];
-      delete [] AbsFlowAngleIn       [iMarker];
-      delete [] RothalpyIn           [iMarker];
-      delete [] RothalpyOut          [iMarker];
-      delete [] AbsFlowAngleOut      [iMarker];
-      delete [] PressureOut_BC       [iMarker];
-      delete [] MachIn               [iMarker];
-      delete [] MachOut              [iMarker];
-      delete [] TurboVelocityIn      [iMarker];
-      delete [] TurboVelocityOut     [iMarker];
-      delete [] TemperatureIn        [iMarker];
-      delete [] TemperatureOut       [iMarker];
-      delete [] TotalPressureIn      [iMarker];
-      delete [] TotalPressureOut     [iMarker];
-      delete [] TotalTemperatureOut  [iMarker];
-      delete [] EnthalpyIn           [iMarker];
-      delete [] TurbIntensityIn      [iMarker];
-      delete [] Turb2LamViscRatioIn  [iMarker];
-      delete [] TurbIntensityOut     [iMarker];
-      delete [] Turb2LamViscRatioOut [iMarker];
-      delete [] NuFactorIn           [iMarker];
-      delete [] NuFactorOut          [iMarker];
-
-
-    }
-    delete [] TotalStaticEfficiency;
-    delete [] TotalTotalEfficiency;
-    delete [] KineticEnergyLoss;
-    delete [] TRadius;
-    delete [] TotalPressureLoss;
-    delete [] MassFlowIn;
-    delete [] MassFlowOut;
-    delete [] FlowAngleIn;
-    delete [] FlowAngleOut;
-    delete [] EulerianWork;
-    delete [] TotalEnthalpyIn;
-    delete [] TotalEnthalpyOut;
-    delete [] TotalEnthalpyOutIs;
-    delete [] PressureRatio;
-    delete [] EnthalpyOut;
-    delete [] VelocityOutIs;
-    delete [] TotalTemperatureIn;
-    delete [] FlowAngleIn_BC;
-    delete [] EntropyIn;
-    delete [] EntropyIn_BC;
-    delete [] EntropyOut;
-    delete [] TotalEnthalpyIn_BC;
-    delete [] DensityIn;
-    delete [] PressureIn;
-    delete [] DensityOut;
-    delete [] PressureOut;
-    delete [] EnthalpyOutIs;
-    delete [] EntropyGen;
-    delete [] AbsFlowAngleIn;
-    delete [] RothalpyIn;
-    delete [] RothalpyOut;
-    delete [] AbsFlowAngleOut;
-    delete [] PressureOut_BC;
-    delete [] MachIn;
-    delete [] MachOut;
-    delete [] TurboVelocityIn;
-    delete [] TurboVelocityOut;
-    delete [] TemperatureIn;
-    delete [] TemperatureOut;
-    delete [] TotalPressureIn;
-    delete [] TotalPressureOut;
-    delete [] TotalTemperatureOut;
-    delete [] EnthalpyIn;
-    delete [] TurbIntensityIn;
-    delete [] Turb2LamViscRatioIn;
-    delete [] TurbIntensityOut;
-    delete [] Turb2LamViscRatioOut;
-    delete [] NuFactorIn;
-    delete [] NuFactorOut;
-  }
-}
-
-void COutputLegacy::SetConvHistoryHeader(ofstream *ConvHist_file, CConfig *config, unsigned short val_iZone, unsigned short val_iInst) {
-  char cstr[200], turb_resid[1000], adj_turb_resid[1000];
-  unsigned short iMarker_Monitoring;
-  string Monitoring_Tag, monitoring_coeff, aeroelastic_coeff, turbo_coeff;
-
-  bool rotating_frame = config->GetRotating_Frame();
-  bool aeroelastic = config->GetAeroelastic_Simulation();
-  bool equiv_area = config->GetEquivArea();
-  bool buffet = (config->GetViscous() || config->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
-  bool engine        = ((config->GetnMarker_EngineInflow() != 0) || (config->GetnMarker_EngineExhaust() != 0));
-  bool actuator_disk = ((config->GetnMarker_ActDiskInlet() != 0) || (config->GetnMarker_ActDiskOutlet() != 0));
-  bool turbulent = ((config->GetKind_Solver() == MAIN_SOLVER::RANS) || (config->GetKind_Solver() == MAIN_SOLVER::ADJ_RANS) ||
-                    (config->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_RANS) || (config->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_INC_RANS) ||
-                    (config->GetKind_Solver() == MAIN_SOLVER::INC_RANS));
-  bool cont_adj = config->GetContinuous_Adjoint();
-  bool disc_adj = config->GetDiscrete_Adjoint();
-  bool frozen_visc = (cont_adj && config->GetFrozen_Visc_Cont()) ||( disc_adj && config->GetFrozen_Visc_Disc());
-  bool inv_design = (config->GetInvDesign_Cp() || config->GetInvDesign_HeatFlux());
-
-  bool output_surface = (config->GetnMarker_Analyze() != 0);
-  bool output_comboObj = (config->GetnObj() > 1);
-  bool output_per_surface = true;
-  bool turbo = config->GetBoolTurbomachinery();
-  unsigned short direct_diff = config->GetDirectDiff();
-
-  bool compressible = (config->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
-  bool incompressible = (config->GetKind_Regime() == ENUM_REGIME::INCOMPRESSIBLE);
-  bool incload = config->GetIncrementalLoad();
-
-  bool thermal = false; /* Flag for whether to print heat flux values */
-  bool weakly_coupled_heat = config->GetWeakly_Coupled_Heat();
-  bool radiation            = config->AddRadiation();
-
-  if (config->GetKind_Solver() == MAIN_SOLVER::RANS || config->GetKind_Solver()  == MAIN_SOLVER::NAVIER_STOKES ||
-      config->GetKind_Solver() == MAIN_SOLVER::INC_RANS || config->GetKind_Solver()  == MAIN_SOLVER::INC_NAVIER_STOKES) {
-    thermal = true;
-  }
-
-  /*--- Write file name with extension ---*/
-  string filename = config->GetConv_FileName();
-  string hist_ext = ".csv";
-  if (config->GetTabular_FileFormat() == TAB_OUTPUT::TAB_TECPLOT) hist_ext = ".dat";
-
-  if(config->GetnZone() > 1){
-    filename = config->GetMultizone_HistoryFileName(filename, val_iZone, hist_ext);
-  }
-  if(config->GetnTimeInstances() > 1){
-    filename = config->GetMultiInstance_HistoryFileName(filename, val_iInst);
-  }
-
-  if (config->GetTime_Domain() && config->GetRestart()) {
-    filename = config->GetUnsteady_FileName(filename, config->GetRestart_Iter(), hist_ext);
-  }
-
-  strcpy (cstr, filename.data());
-
-  ConvHist_file->open(cstr, ios::out);
-  ConvHist_file->precision(15);
-
-  /*--- Begin of the header ---*/
-
-  char begin[]= "\"Iteration\"";
-
-  /*--- Header for the coefficients ---*/
-
-  char flow_coeff[]= ",\"CL\",\"CD\",\"CSF\",\"CMx\",\"CMy\",\"CMz\",\"CFx\",\"CFy\",\"CFz\",\"CL/CD\",\"AoA\",\"Custom_ObjFunc\"";
-  char heat_coeff[]= ",\"HeatFlux_Total\",\"HeatFlux_Maximum\",\"Temperature_Total\"";
-  char equivalent_area_coeff[]= ",\"CEquivArea\",\"CNearFieldOF\"";
-  char buffet_coeff[]= ",\"Buffet_Metric\"";
-  char engine_coeff[]= ",\"NetThrust\",\"Power\",\"AeroCDrag\",\"SolidCDrag\",\"Radial_Distortion\",\"Circumferential_Distortion\"";
-  char rotating_frame_coeff[]= ",\"CMerit\",\"CT\",\"CQ\"";
-  char fem_coeff[]= ",\"VM_Stress\",\"Force_Coeff\"";
-  char fem_incload[]= ",\"IncLoad\"";
-  char adj_coeff[]= ",\"Sens_Geo\",\"Sens_Mach\",\"Sens_AoA\",\"Sens_Press\",\"Sens_Temp\",\"Sens_AoS\"";
-  char adj_inc_coeff[]=",\"Sens_Geo\",\"Sens_Vin\",\"Sens_Pout\",\"Sens_Temp\"";
-  char adj_turbo_coeff[]=",\"Sens_Geo\",\"Sens_PressOut\",\"Sens_TotTempIn\"";
-  char surface_outputs[]= ",\"Avg_MassFlow\",\"Avg_Mach\",\"Avg_Temp\",\"Avg_Press\",\"Avg_Density\",\"Avg_Enthalpy\",\"Avg_NormalVel\",\"Uniformity\",\"Secondary_Strength\",\"Momentum_Distortion\",\"Secondary_Over_Uniformity\",\"Avg_TotalTemp\",\"Avg_TotalPress\",\"Pressure_Drop\"";
-  char Cp_inverse_design[]= ",\"Cp_Diff\"";
-  char Heat_inverse_design[]= ",\"HeatFlux_Diff\"";
-  char d_flow_coeff[] = ",\"D(CL)\",\"D(CD)\",\"D(CSF)\",\"D(CMx)\",\"D(CMy)\",\"D(CMz)\",\"D(CFx)\",\"D(CFy)\",\"D(CFz)\",\"D(CL/CD)\",\"D(Custom_ObjFunc)\"";
-  char d_thermal_coeff[] = ",\"D(HeatFlux_Total)\",\"D(HeatFlux_Maximum)\"";
-  char d_engine[] = ",\"D(NetThrust)\",\"D(Power)\",\"D(AeroCDrag)\",\"D(SolidCDrag)\",\"D(Radial_Distortion)\",\"D(Circumferential_Distortion)\"";
-  char d_turbo_coeff[] = ",\"D(TotalPressureLoss_0)\",\"D(FlowAngleOut_0)\",\"D(TotalEfficency)\",\"D(TotalStaticEfficiency)\", \"D(EntropyGen)\"";
-  char d_surface_outputs[]= ",\"D(Uniformity)\",\"D(Secondary_Strength)\",\"D(Momentum_Distortion)\",\"D(Secondary_Over_Uniformity)\",\"D(Pressure_Drop)\"";
-
-  /*--- Find the markers being monitored and create a header for them ---*/
-
-  for (iMarker_Monitoring = 0; iMarker_Monitoring < config->GetnMarker_Monitoring(); iMarker_Monitoring++) {
-    Monitoring_Tag = config->GetMarker_Monitoring_TagBound(iMarker_Monitoring);
-    monitoring_coeff += ",\"CL_"  + Monitoring_Tag + "\"";
-    monitoring_coeff += ",\"CD_"  + Monitoring_Tag + "\"";
-    monitoring_coeff += ",\"CSF_" + Monitoring_Tag + "\"";
-    monitoring_coeff += ",\"CL/CD_" + Monitoring_Tag + "\"";
-    monitoring_coeff += ",\"CFx_"    + Monitoring_Tag + "\"";
-    monitoring_coeff += ",\"CFy_"    + Monitoring_Tag + "\"";
-    monitoring_coeff += ",\"CFz_"    + Monitoring_Tag + "\"";
-    monitoring_coeff += ",\"CMx_"    + Monitoring_Tag + "\"";
-    monitoring_coeff += ",\"CMy_"    + Monitoring_Tag + "\"";
-    monitoring_coeff += ",\"CMz_"    + Monitoring_Tag + "\"";
-    if(buffet) monitoring_coeff += ",\"Buffet_Metric_"    + Monitoring_Tag + "\"";
-    aeroelastic_coeff += ",\"plunge_" + Monitoring_Tag + "\"";
-    aeroelastic_coeff += ",\"pitch_"  + Monitoring_Tag + "\"";
-  }
-
-  if (turbo){
-    for (iMarker_Monitoring = 0; iMarker_Monitoring < config->GetnMarker_TurboPerformance(); iMarker_Monitoring++) {
-
-      stringstream tag;
-      tag << iMarker_Monitoring + 1;
-
-      turbo_coeff += ",\"TotalPressureLoss_" + tag.str() + "\"";
-      turbo_coeff += ",\"KineticEnergyLoss_" + tag.str() + "\"";
-      turbo_coeff += ",\"EntropyGen_" + tag.str() + "\"";
-      turbo_coeff += ",\"EulerianWork_" + tag.str() + "\"";
-      turbo_coeff += ",\"PressureRatio_" + tag.str() + "\"";
-      turbo_coeff += ",\"FlowAngleIn_" + tag.str() + "\"";
-      turbo_coeff += ",\"FlowAngleOut_" + tag.str() + "\"";
-      turbo_coeff += ",\"AbsFlowAngleIn_" + tag.str() + "\"";
-      turbo_coeff += ",\"AbsFlowAngleOut_" + tag.str() + "\"";
-      turbo_coeff += ",\"MassFlowIn_" + tag.str() + "\"";
-      turbo_coeff += ",\"MassFlowOut_" + tag.str() + "\"";
-      turbo_coeff += ",\"MachIn_" + tag.str() + "\"";
-      turbo_coeff += ",\"MachOut_" + tag.str() + "\"";
-      // different from zero only in multi-zone computation
-      turbo_coeff += ",\"TotalEfficiency_" + tag.str() + "\"";
-      turbo_coeff += ",\"TotalStaticEfficiency_" + tag.str() + "\"";
-
-    }
-  }
-
-  char combo_obj[] = ",\"ComboObj\"";
-
-  /*--- Header for the residuals ---*/
-
-  char flow_resid[]= ",\"Res_Flow[0]\",\"Res_Flow[1]\",\"Res_Flow[2]\",\"Res_Flow[3]\",\"Res_Flow[4]\"";
-  char adj_flow_resid[]= ",\"Res_AdjFlow[0]\",\"Res_AdjFlow[1]\",\"Res_AdjFlow[2]\",\"Res_AdjFlow[3]\",\"Res_AdjFlow[4]\"";
-  switch (config->GetKind_Turb_Model()) {
-    case TURB_MODEL::SA:
-      SPRINTF (turb_resid, ",\"Res_Turb[0]\"");
-      break;
-    case TURB_MODEL::SST:
-      SPRINTF (turb_resid, ",\"Res_Turb[0]\",\"Res_Turb[1]\"");
-      break;
-    default: break;
-  }
-  switch (config->GetKind_Turb_Model()) {
-    case TURB_MODEL::SA:
-      SPRINTF (adj_turb_resid, ",\"Res_AdjTurb[0]\"");
-      break;
-    case TURB_MODEL::SST:
-      SPRINTF (adj_turb_resid, ",\"Res_AdjTurb[0]\",\"Res_AdjTurb[1]\"");
-      break;
-    default: break;
-  }
-  char fem_resid[]= ",\"Res_FEM[0]\",\"Res_FEM[1]\",\"Res_FEM[2]\"";
-  char heat_resid[]= ",\"Res_Heat\"";
-  char rad_resid[]= ",\"Res_P1-rad\"";
-
-  /*--- End of the header ---*/
-
-  char end[]= ",\"Linear_Solver_Iterations\",\"CFL_Number\",\"Time(min)\"\n";
-  char endfea[]= ",\"Linear_Solver_Iterations\",\"Time(min)\"\n";
-
-  if ((config->GetTabular_FileFormat() == TAB_OUTPUT::TAB_TECPLOT)) {
-    ConvHist_file[0] << "TITLE = \"SU2 Simulation\"" << endl;
-    ConvHist_file[0] << "VARIABLES = ";
-  }
-
-  /*--- Write the header, case depending ---*/
-
-  switch (config->GetKind_Solver()) {
-
-    case MAIN_SOLVER::EULER : case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::RANS :
-    case MAIN_SOLVER::INC_EULER : case MAIN_SOLVER::INC_NAVIER_STOKES: case MAIN_SOLVER::INC_RANS :
-    case MAIN_SOLVER::FEM_EULER : case MAIN_SOLVER::FEM_NAVIER_STOKES: case MAIN_SOLVER::FEM_RANS : case MAIN_SOLVER::FEM_LES:
-      ConvHist_file[0] << begin;
-      if (!turbo) ConvHist_file[0] << flow_coeff;
-      if (buffet) ConvHist_file[0] << buffet_coeff;
-      if (turbo) ConvHist_file[0] << turbo_coeff;
-      if (thermal && !turbo) ConvHist_file[0] << heat_coeff;
-      if (equiv_area) ConvHist_file[0] << equivalent_area_coeff;
-      if (engine || actuator_disk) ConvHist_file[0] << engine_coeff;
-      if (inv_design) {
-        ConvHist_file[0] << Cp_inverse_design;
-        if (thermal && !turbo) ConvHist_file[0] << Heat_inverse_design;
-      }
-      if (rotating_frame && !turbo) ConvHist_file[0] << rotating_frame_coeff;
-
-      ConvHist_file[0] << flow_resid;
-      if (turbulent) ConvHist_file[0] << turb_resid;
-      if (weakly_coupled_heat) ConvHist_file[0] << heat_resid;
-      if (radiation) ConvHist_file[0] << rad_resid;
-      if (aeroelastic) ConvHist_file[0] << aeroelastic_coeff;
-      if (output_per_surface) ConvHist_file[0] << monitoring_coeff;
-      if (output_surface) ConvHist_file[0] << surface_outputs;
-      if (direct_diff != NO_DERIVATIVE) {
-        if (!turbo) ConvHist_file[0] << d_flow_coeff;
-        else        ConvHist_file[0] << d_turbo_coeff;
-        if (engine || actuator_disk) ConvHist_file[0] << d_engine;
-        if (thermal) ConvHist_file[0] << d_thermal_coeff;
-        if (output_surface) ConvHist_file[0] << d_surface_outputs;
-      }
-      if (output_comboObj) ConvHist_file[0] << combo_obj;
-      ConvHist_file[0] << end;
-
-      break;
-
-    case MAIN_SOLVER::ADJ_EULER      : case MAIN_SOLVER::ADJ_NAVIER_STOKES      : case MAIN_SOLVER::ADJ_RANS:
-    case MAIN_SOLVER::DISC_ADJ_EULER: case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_RANS:
-    case MAIN_SOLVER::DISC_ADJ_INC_EULER: case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_INC_RANS:
-      if (!turbo) {
-        if (compressible) {
-          ConvHist_file[0] << begin << adj_coeff << adj_flow_resid;
-        }
-        if (incompressible) {
-          ConvHist_file[0] << begin << adj_inc_coeff << adj_flow_resid;
-        }
-      }
-      else ConvHist_file[0] << begin << adj_turbo_coeff << adj_flow_resid;
-      if ((turbulent) && (!frozen_visc)) ConvHist_file[0] << adj_turb_resid;
-      ConvHist_file[0] << end;
-      break;
-
-    case MAIN_SOLVER::HEAT_EQUATION:
-      ConvHist_file[0] << begin << heat_coeff;
-      ConvHist_file[0] << heat_resid << end;
-      break;
-
-    case MAIN_SOLVER::FEM_ELASTICITY:
-      ConvHist_file[0] << begin << fem_coeff;
-      if (incload) ConvHist_file[0] << fem_incload;
-      ConvHist_file[0] << fem_resid << endfea;
-      break;
-
-    case MAIN_SOLVER::DISC_ADJ_FEM:
-      ConvHist_file[0] << begin << fem_coeff;
-      ConvHist_file[0] << fem_resid << endfea;
-      break;
-
-    default:
-      break;
-  }
-
-  if (config->GetTabular_FileFormat() == TAB_OUTPUT::TAB_TECPLOT) {
-    ConvHist_file[0] << "ZONE T= \"Convergence history\"" << endl;
-  }
-
-}
-
-
-void COutputLegacy::SetConvHistoryBody(ofstream *ConvHist_file,
-                                  CGeometry ****geometry,
-                                  CSolver *****solver_container,
-                                  CConfig **config,
-                                  CIntegration ****integration,
-                                  bool DualTime_Iteration,
-                                  su2double timeused,
-                                  unsigned short val_iZone,
-                                  unsigned short val_iInst) {
-
-  bool output_surface       = (config[val_iZone]->GetnMarker_Analyze() != 0);
-  bool output_comboObj      = (config[val_iZone]->GetnObj() > 1);
-  bool fluid_structure      = (config[val_iZone]->GetFSI_Simulation());
-  bool fea                  = ((config[val_iZone]->GetKind_Solver()== MAIN_SOLVER::FEM_ELASTICITY)||(config[val_iZone]->GetKind_Solver()== MAIN_SOLVER::DISC_ADJ_FEM));
-  unsigned long iIntIter    = config[val_iZone]->GetInnerIter();
-  unsigned long iExtIter    = config[val_iZone]->GetInnerIter();
-  unsigned short FinestMesh = config[val_iZone]->GetFinestMesh();
-  unsigned short nZone      = config[val_iZone]->GetnZone();
-  unsigned short nInst      = config[val_iZone]->GetnTimeInstances();
-  bool cont_adj             = config[val_iZone]->GetContinuous_Adjoint();
-  bool disc_adj             = config[val_iZone]->GetDiscrete_Adjoint();
-  bool energy               = config[val_iZone]->GetEnergy_Equation();
-  bool incload              = config[val_iZone]->GetIncrementalLoad();
-  bool fixed_cl             = config[val_iZone]->GetFixed_CL_Mode();
-  bool output_files         = true;
-
-  bool radiation            = config[val_iZone]->AddRadiation();
-
-  bool compressible = (config[val_iZone]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
-  bool incompressible = (config[val_iZone]->GetKind_Regime() == ENUM_REGIME::INCOMPRESSIBLE);
-
-  if (!disc_adj && !cont_adj && !DualTime_Iteration) {
-
-    if (fixed_cl &&
-        (solver_container[val_iZone][val_iInst][MESH_0][FLOW_SOL]->GetStart_AoA_FD()) &&
-        (iExtIter != solver_container[val_iZone][val_iInst][MESH_0][FLOW_SOL]->GetIter_Update_AoA())) {
-      output_files = false;
-    }
-
-    if (fea || fluid_structure) output_files = false;
-
-    /*--- We need to evaluate some of the objective functions to write the value on the history file ---*/
-
-    if (((iExtIter % (config[val_iZone]->GetVolumeOutputFrequency(0) )) == 0) ||
-        (!fixed_cl && (iExtIter == (config[val_iZone]->GetnInner_Iter()-1))) ||
-        /*--- If CL mode we need to compute the complete solution at two very particular iterations ---*/
-        (fixed_cl && (iExtIter == (config[val_iZone]->GetnInner_Iter()-2) ||
-          (solver_container[val_iZone][val_iInst][MESH_0][FLOW_SOL]->GetStart_AoA_FD() &&
-          iExtIter == solver_container[val_iZone][val_iInst][MESH_0][FLOW_SOL]->GetIter_Update_AoA())))) {
-
-
-      if ((rank == MASTER_NODE) && output_files) cout << endl << "------------------------ Evaluate Special Output ------------------------";
-
-      switch (config[val_iZone]->GetKind_Solver()) {
-
-        case MAIN_SOLVER::EULER: case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::RANS:
-        case MAIN_SOLVER::INC_EULER: case MAIN_SOLVER::INC_NAVIER_STOKES: case MAIN_SOLVER::INC_RANS:
-          /*--- For specific applications, evaluate and plot the surface. ---*/
-
-          if (config[val_iZone]->GetnMarker_Analyze() != 0) {
-            SpecialOutputAnalyzeSurface(solver_container[val_iZone][val_iInst][MESH_0][FLOW_SOL],
-                                         geometry[val_iZone][val_iInst][MESH_0], config[val_iZone], output_files);
-          }
-
-          /*--- For specific applications, evaluate and plot the surface. ---*/
-
-          if ((config[val_iZone]->GetnMarker_Analyze() != 0) && compressible) {
-            SpecialOutputDistortion(solver_container[val_iZone][val_iInst][MESH_0][FLOW_SOL],
-                                     geometry[val_iZone][val_iInst][MESH_0], config[val_iZone], output_files);
-          }
-
-          /*--- For specific applications, evaluate and plot the cp coefficent at different stations. ---*/
-
-          if (config[val_iZone]->GetPlot_Section_Forces()) {
-            SpecialOutputSpanLoad(solver_container[val_iZone][val_iInst][MESH_0][FLOW_SOL],
-                                   geometry[val_iZone][val_iInst][MESH_0], config[val_iZone], output_files);
-          }
-
-          break;
-
-        default:
-          break;
-      }
-
-      /*--- Output a file with the forces breakdown. ---*/
-
-      if (config[val_iZone]->GetTime_Marching() == TIME_MARCHING::HARMONIC_BALANCE) {
-        SpecialOutputHarmonicBalance(solver_container, geometry, config, val_iInst, nInst, output_files);
-      }
-
-      /*--- Compute span-wise values file for turbomachinery. ---*/
-
-      if (config[val_iZone]->GetBoolTurbomachinery()) {
-        SpecialOutputTurbo(solver_container, geometry, config, val_iZone, output_files);
-      }
-
-      /*--- Output a file with the forces breakdown. ---*/
-
-      SpecialOutputForcesBreakdown(solver_container, geometry, config, val_iZone, output_files);
-
-      if ((rank == MASTER_NODE) && output_files) cout << "-------------------------------------------------------------------------" << endl << endl;
-
-    }
-
-  }
-
-  /*--- Output using only the master node ---*/
-
-  if (rank == MASTER_NODE) {
-
-    /*-- Compute the total objective if a "combo" objective is used ---*/
-
-    if (output_comboObj) {
-      switch (config[val_iZone]->GetKind_Solver()) {
-      case MAIN_SOLVER::EULER:                   case MAIN_SOLVER::NAVIER_STOKES:                   case MAIN_SOLVER::RANS:
-      case MAIN_SOLVER::INC_EULER:               case MAIN_SOLVER::INC_NAVIER_STOKES:               case MAIN_SOLVER::INC_RANS:
-        solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->Evaluate_ObjFunc(config[val_iZone],
-                                                                                       solver_container[val_iZone][val_iInst][FinestMesh]);
-        break;
-      default:
-        break;
-      }
-    }
-
-    unsigned long ExtIter_OffSet = config[val_iZone]->GetExtIter_OffSet();
-    if (config[val_iZone]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST ||
-        config[val_iZone]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND)
-      ExtIter_OffSet = 0;
-
-    /*--- WARNING: These buffers have hard-coded lengths. Note that you
-     may have to adjust them to be larger if adding more entries. ---*/
-
-    char begin[1000], direct_coeff[1000], heat_coeff[1000], equivalent_area_coeff[1000], engine_coeff[1000], rotating_frame_coeff[1000], Cp_inverse_design[1000], Heat_inverse_design[1000], surface_coeff[1000], aeroelastic_coeff[1000], monitoring_coeff[10000], buffet_coeff[1000],
-    adjoint_coeff[1000], flow_resid[1000], adj_flow_resid[1000], turb_resid[1000], trans_resid[1000],
-    adj_turb_resid[1000], rad_resid[1000],
-    begin_fem[1000], fem_coeff[1000], heat_resid[1000], combo_obj[1000],
-    fem_resid[1000], end[1000], end_fem[1000], surface_outputs[1000], d_surface_outputs[1000], d_direct_coeff[1000], turbo_coeff[10000];
-
-
-    su2double dummy = 0.0;
-    const su2double *Coord = nullptr;
-    unsigned short iVar, iMarker_Monitoring;
-
-    unsigned long LinSolvIter = 0, iPointMaxResid;
-    su2double timeiter = timeused/su2double(iExtIter+1);
-
-    unsigned short nDim = geometry[val_iZone][val_iInst][FinestMesh]->GetnDim();
-
-
-    bool rotating_frame = config[val_iZone]->GetRotating_Frame();
-    bool aeroelastic = config[val_iZone]->GetAeroelastic_Simulation();
-    bool equiv_area = config[val_iZone]->GetEquivArea();
-    bool engine        = ((config[val_iZone]->GetnMarker_EngineInflow() != 0) || (config[val_iZone]->GetnMarker_EngineExhaust() != 0));
-    bool actuator_disk = ((config[val_iZone]->GetnMarker_ActDiskInlet() != 0) || (config[val_iZone]->GetnMarker_ActDiskOutlet() != 0));
-    bool inv_design = (config[val_iZone]->GetInvDesign_Cp() || config[val_iZone]->GetInvDesign_HeatFlux());
-    bool transition = (config[val_iZone]->GetKind_Trans_Model() == TURB_TRANS_MODEL::LM);
-    bool thermal = (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::RANS || config[val_iZone]->GetKind_Solver()  == MAIN_SOLVER::NAVIER_STOKES ||
-                    config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::INC_NAVIER_STOKES || config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::INC_RANS );
-    bool turbulent = ((config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::RANS) || (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::ADJ_RANS) ||
-                      (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_RANS) || config[val_iZone]->GetKind_Solver()  == MAIN_SOLVER::INC_RANS ||
-                      config[val_iZone]->GetKind_Solver()  == MAIN_SOLVER::DISC_ADJ_INC_RANS);
-    bool adjoint =  cont_adj || disc_adj;
-    bool frozen_visc = (cont_adj && config[val_iZone]->GetFrozen_Visc_Cont()) ||( disc_adj && config[val_iZone]->GetFrozen_Visc_Disc());
-    bool heat =  ((config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::HEAT_EQUATION) || (config[val_iZone]->GetWeakly_Coupled_Heat()));
-    bool weakly_coupled_heat = config[val_iZone]->GetWeakly_Coupled_Heat();
-    bool flow = (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::EULER) || (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::NAVIER_STOKES) ||
-                (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::RANS) || (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::FEM_EULER) ||
-                (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::FEM_NAVIER_STOKES) || (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::FEM_RANS) ||
-                (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::FEM_LES) || (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::ADJ_EULER) ||
-                (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::ADJ_NAVIER_STOKES) || (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::ADJ_RANS) ||
-                (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::INC_EULER) || (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::INC_NAVIER_STOKES) ||
-                (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::INC_RANS);
-    bool buffet = (config[val_iZone]->GetViscous() || config[val_iZone]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
-
-    bool fem = ((config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::FEM_ELASTICITY) ||          // FEM structural solver.
-                (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_FEM));
-    bool linear_analysis = (config[val_iZone]->GetGeometricConditions() == STRUCT_DEFORMATION::SMALL);
-    bool nonlinear_analysis = (config[val_iZone]->GetGeometricConditions() == STRUCT_DEFORMATION::LARGE);
-    bool fsi = (config[val_iZone]->GetFSI_Simulation());
-    bool discadj_fem = (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_FEM);
-
-    bool turbo = config[val_iZone]->GetBoolTurbomachinery();
-
-    unsigned short nTurboPerf  = config[val_iZone]->GetnMarker_TurboPerformance();
-
-    bool output_per_surface = true;
-
-    unsigned short direct_diff = config[val_iZone]->GetDirectDiff();
-
-    long ExtraHeatOutputZone = config[val_iZone]->GetExtraHeatOutputZone() - 1;
-    bool extra_heat_output = false;
-    su2double Extra_Total_Heat = 0.0;
-    //su2double Extra_Total_Temperature = 0.0;
-    su2double Extra_Heat_Residual = 0.0;
-
-    if (ExtraHeatOutputZone > -1) {
-      if (ExtraHeatOutputZone > nZone) {
-        SU2_MPI::Error("Error in output routine: Extra output zone number exceeds total number of zones.", CURRENT_FUNCTION);
-      }
-      else if ((config[ExtraHeatOutputZone]->GetKind_Solver() != MAIN_SOLVER::HEAT_EQUATION)) {
-        SU2_MPI::Error("Error in output routine: No heat solver in extra output zone.", CURRENT_FUNCTION);
-      }
-      else {
-        extra_heat_output = true;
-      }
-    }
-
-    /*--- Initialize variables to store information from all domains (direct solution) ---*/
-
-    su2double Total_CL = 0.0, Total_CD = 0.0, Total_CSF = 0.0, Total_CMx = 0.0, Total_CMy = 0.0, Total_CMz = 0.0, Total_CEff = 0.0,
-    Total_CEquivArea = 0.0, Total_CNearFieldOF = 0.0, Total_CFx = 0.0, Total_CFy = 0.0, Total_CFz = 0.0, Total_CMerit = 0.0,
-    Total_CT = 0.0, Total_CQ = 0.0,
-    Total_Heat = 0.0, Total_MaxHeat = 0.0, Total_Temperature = 0.0, Total_Custom_ObjFunc = 0.0,
-    Total_ComboObj = 0.0, Total_NetThrust = 0.0, Total_Power = 0.0, Total_AeroCD = 0.0, Total_SolidCD = 0.0, Total_IDR = 0.0, Total_IDC = 0.0,
-    Total_AoA = 0.0, Total_Buffet_Metric = 0.0;
-    su2double Surface_MassFlow = 0.0, Surface_Mach = 0.0, Surface_Temperature = 0.0, Surface_Pressure = 0.0, Surface_Density = 0.0, Surface_Enthalpy = 0.0, Surface_NormalVelocity = 0.0, Surface_TotalTemperature = 0.0, Surface_TotalPressure = 0.0, Surface_Uniformity = 0.0, Surface_SecondaryStrength = 0.0,Surface_MomentumDistortion = 0.0, Surface_SecondOverUniform = 0.0, Surface_PressureDrop = 0.0;
-
-    su2double Total_ForceCoeff = 0.0, Total_VMStress = 0.0, Total_IncLoad = 0.0;
-    su2double Total_SensE = 0.0, Total_SensNu = 0.0;
-
-    unsigned short iSpan;
-
-    /*--- Initialize variables to store information from all domains (adjoint solution) ---*/
-    su2double Total_Sens_Geo = 0.0, Total_Sens_Mach = 0.0, Total_Sens_AoA = 0.0;
-    su2double Total_Sens_Press = 0.0, Total_Sens_Temp = 0.0;
-
-    su2double Total_Sens_BPressure = 0.0;
-    su2double Total_Sens_ModVel = 0.0;
-
-    /*--- Initialize variables to store information from all domains (direct differentiation) ---*/
-    su2double D_Total_CL = 0.0, D_Total_CD = 0.0, D_Total_CSF = 0.0, D_Total_CMx = 0.0, D_Total_CMy = 0.0, D_Total_CMz = 0.0, D_Total_CEff = 0.0, D_Total_CFx = 0.0,
-        D_Total_CFy = 0.0, D_Total_CFz = 0.0, D_Total_NetThrust = 0.0, D_Total_Power = 0.0, D_Total_AeroCD = 0.0, D_Total_SolidCD = 0.0, D_Total_IDR = 0.0, D_Total_IDC = 0.0, D_Total_Custom_ObjFunc = 0.0, D_Total_Heat = 0.0, D_Total_MaxHeat = 0.0,
-        D_TotalPressure_Loss = 0.0, D_FlowAngle_Out = 0.0, D_TotalStaticEfficiency = 0.0,
-        D_TotalTotalEfficiency = 0.0, D_EntropyGen = 0.0,
-        D_Surface_Uniformity = 0.0, D_Surface_SecondaryStrength = 0.0, D_Surface_MomentumDistortion = 0.0, D_Surface_SecondOverUniform = 0.0, D_Surface_PressureDrop = 0.0;
-
-    /*--- Residual arrays ---*/
-    su2double *residual_flow         = nullptr,
-    *residual_turbulent    = nullptr,
-    *residual_transition   = nullptr;
-    su2double *residual_adjflow      = nullptr,
-    *residual_adjturbulent = nullptr,
-    *residual_adjheat = nullptr;
-    su2double *residual_fea          = nullptr;
-    su2double *residual_fem          = nullptr;
-    su2double *residual_heat         = nullptr;
-    su2double *residual_rad          = nullptr;
-
-    /*--- Coefficients Monitored arrays ---*/
-    su2double *aeroelastic_plunge = nullptr,
-    *aeroelastic_pitch     = nullptr,
-    *Surface_CL            = nullptr,
-    *Surface_CD            = nullptr,
-    *Surface_CSF           = nullptr,
-    *Surface_CEff          = nullptr,
-    *Surface_CFx           = nullptr,
-    *Surface_CFy           = nullptr,
-    *Surface_CFz           = nullptr,
-    *Surface_CMx           = nullptr,
-    *Surface_CMy           = nullptr,
-    *Surface_CMz           = nullptr,
-    *Surface_Buffet_Metric = nullptr;
-
-    /*--- Initialize number of variables ---*/
-    unsigned short nVar_Flow = 0, nVar_Turb = 0,
-    nVar_Trans = 0, nVar_Heat = 0,
-    nVar_AdjFlow = 0, nVar_AdjTurb = 0, nVar_AdjHeat = 0,
-    nVar_FEM = 0, nVar_Rad = 0;
-
-    /*--- Direct problem variables ---*/
-    if (compressible) nVar_Flow = nDim+2; else nVar_Flow = nDim+2;
-    if (turbulent) {
-      switch (config[val_iZone]->GetKind_Turb_Model()) {
-        case TURB_MODEL::SA: nVar_Turb = 1; break;
-        case TURB_MODEL::SST: nVar_Turb = 2; break;
-        default: break;
-      }
-    }
-    if (transition) nVar_Trans = 2;
-    if (heat) nVar_Heat = 1;
-
-    if (fem) {
-      if (linear_analysis) nVar_FEM = nDim;
-      if (nonlinear_analysis) nVar_FEM = 3;
-
-      if (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_FEM) nVar_FEM = nDim;
-
-    }
-
-    if (radiation) nVar_Rad = 1;
-
-    /*--- Adjoint problem variables ---*/
-    if (compressible) nVar_AdjFlow = nDim+2; else nVar_AdjFlow = nDim+2;
-    if (turbulent) {
-      switch (config[val_iZone]->GetKind_Turb_Model()) {
-        case TURB_MODEL::SA: nVar_AdjTurb = 1; break;
-        case TURB_MODEL::SST: nVar_AdjTurb = 2; break;
-        default: break;
-      }
-    }
-    if (weakly_coupled_heat) nVar_AdjHeat = 1;
-
-    /*--- Allocate memory for the residual ---*/
-    residual_flow       = new su2double[nVar_Flow];
-    residual_turbulent  = new su2double[nVar_Turb];
-    residual_transition = new su2double[nVar_Trans];
-    residual_heat       = new su2double[nVar_Heat];
-    residual_fem        = new su2double[nVar_FEM];
-    residual_rad        = new su2double[nVar_Rad];
-    residual_adjflow      = new su2double[nVar_AdjFlow];
-    residual_adjturbulent = new su2double[nVar_AdjTurb];
-    residual_adjheat      = new su2double[nVar_AdjHeat];
-
-    /*--- Allocate memory for the coefficients being monitored ---*/
-    aeroelastic_plunge = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    aeroelastic_pitch  = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CL      = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CD      = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CSF = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CEff       = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CFx        = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CFy        = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CFz        = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CMx        = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CMy        = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CMz        = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    if(buffet) Surface_Buffet_Metric = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-
-    /*--- Write information from nodes ---*/
-
-    switch (config[val_iZone]->GetKind_Solver()) {
-
-      case MAIN_SOLVER::EULER:                   case MAIN_SOLVER::NAVIER_STOKES:                   case MAIN_SOLVER::RANS:
-      case MAIN_SOLVER::INC_EULER:               case MAIN_SOLVER::INC_NAVIER_STOKES:               case MAIN_SOLVER::INC_RANS:
-      case MAIN_SOLVER::FEM_EULER:               case MAIN_SOLVER::FEM_NAVIER_STOKES:               case MAIN_SOLVER::FEM_RANS:      case MAIN_SOLVER::FEM_LES:
-      case MAIN_SOLVER::ADJ_EULER:               case MAIN_SOLVER::ADJ_NAVIER_STOKES:               case MAIN_SOLVER::ADJ_RANS:
-      case MAIN_SOLVER::DISC_ADJ_EULER:          case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES:          case MAIN_SOLVER::DISC_ADJ_RANS:
-      case MAIN_SOLVER::DISC_ADJ_INC_EULER:      case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES:      case MAIN_SOLVER::DISC_ADJ_INC_RANS:
-
-        /*--- Flow solution coefficients ---*/
-
-        Total_CL             = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_CL();
-        Total_CD             = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_CD();
-        Total_CSF            = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_CSF();
-        Total_CEff           = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_CEff();
-        Total_CMx            = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_CMx();
-        Total_CMy            = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_CMy();
-        Total_CMz            = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_CMz();
-        Total_CFx            = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_CFx();
-        Total_CFy            = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_CFy();
-        Total_CFz            = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_CFz();
-        Total_ComboObj       = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_ComboObj();
-        Total_AoA            = config[val_iZone]->GetAoA() - config[val_iZone]->GetAoA_Offset();
-
-        if (thermal) {
-          Total_Heat         = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_HeatFlux();
-          Total_MaxHeat      = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_MaxHeatFlux();
-          Total_Temperature  = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_AvgTemperature();
-
-          if(weakly_coupled_heat) {
-            Total_Heat         = solver_container[val_iZone][val_iInst][FinestMesh][HEAT_SOL]->GetTotal_HeatFlux();
-            Total_MaxHeat      = solver_container[val_iZone][val_iInst][FinestMesh][HEAT_SOL]->GetTotal_MaxHeatFlux();
-            Total_Temperature  = solver_container[val_iZone][val_iInst][FinestMesh][HEAT_SOL]->GetTotal_AvgTemperature();
-          }
-        }
-
-        if(buffet){
-          Total_Buffet_Metric = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_Buffet_Metric();
-        }
-
-        if (direct_diff != NO_DERIVATIVE) {
-          D_Total_CL             = SU2_TYPE::GetDerivative(Total_CL);
-          D_Total_CD             = SU2_TYPE::GetDerivative(Total_CD);
-          D_Total_CSF            = SU2_TYPE::GetDerivative(Total_CSF);
-          D_Total_CEff           = SU2_TYPE::GetDerivative(Total_CEff);
-          D_Total_CMx            = SU2_TYPE::GetDerivative(Total_CMx);
-          D_Total_CMy            = SU2_TYPE::GetDerivative(Total_CMy);
-          D_Total_CMz            = SU2_TYPE::GetDerivative(Total_CMz);
-          D_Total_CFx            = SU2_TYPE::GetDerivative(Total_CFx);
-          D_Total_CFy            = SU2_TYPE::GetDerivative(Total_CFy);
-          D_Total_CFz            = SU2_TYPE::GetDerivative(Total_CFz);
-          D_Total_Custom_ObjFunc = SU2_TYPE::GetDerivative(Total_Custom_ObjFunc);
-
-          if (thermal) {
-            D_Total_Heat    = SU2_TYPE::GetDerivative(Total_Heat);
-            D_Total_MaxHeat = SU2_TYPE::GetDerivative(Total_MaxHeat);
-            //Davg Temp
-          }
-
-          if (engine || actuator_disk) {
-            D_Total_NetThrust = SU2_TYPE::GetDerivative(Total_NetThrust);
-            D_Total_Power     = SU2_TYPE::GetDerivative(Total_Power);
-            D_Total_AeroCD    = SU2_TYPE::GetDerivative(Total_AeroCD);
-            D_Total_SolidCD   = SU2_TYPE::GetDerivative(Total_SolidCD);
-            D_Total_IDR       = SU2_TYPE::GetDerivative(Total_IDR);
-            D_Total_IDC       = SU2_TYPE::GetDerivative(Total_IDC);
-          }
-
-        }
-
-        if (equiv_area) {
-          Total_CEquivArea    = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_CEquivArea();
-          Total_CNearFieldOF  = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_CNearFieldOF();
-
-          Total_CEquivArea    = config[val_iZone]->GetWeightCd()*Total_CD + (1.0-config[val_iZone]->GetWeightCd())*Total_CEquivArea;
-          Total_CNearFieldOF  = config[val_iZone]->GetWeightCd()*Total_CD + (1.0-config[val_iZone]->GetWeightCd())*Total_CNearFieldOF;
-        }
-
-        if (engine || actuator_disk) {
-          Total_NetThrust = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_NetThrust();
-          Total_Power     = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_Power();
-          Total_AeroCD    = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_AeroCD();
-          Total_SolidCD   = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_SolidCD();
-          Total_IDR       = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_IDR();
-          Total_IDC       = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_IDC();
-        }
-
-        if (rotating_frame) {
-          Total_CT      = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_CT();
-          Total_CQ      = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_CQ();
-          Total_CMerit  = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_CMerit();
-        }
-
-        if (aeroelastic) {
-          /*--- Look over the markers being monitored and get the desired values ---*/
-          for (iMarker_Monitoring = 0; iMarker_Monitoring < config[ZONE_0]->GetnMarker_Monitoring(); iMarker_Monitoring++) {
-            aeroelastic_plunge[iMarker_Monitoring] = config[val_iZone]->GetAeroelastic_plunge(iMarker_Monitoring);
-            aeroelastic_pitch[iMarker_Monitoring]  = config[val_iZone]->GetAeroelastic_pitch(iMarker_Monitoring);
-          }
-        }
-
-        if (output_per_surface) {
-          /*--- Look over the markers being monitored and get the desired values ---*/
-          for (iMarker_Monitoring = 0; iMarker_Monitoring < config[ZONE_0]->GetnMarker_Monitoring(); iMarker_Monitoring++) {
-            Surface_CL[iMarker_Monitoring]      = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetSurface_CL(iMarker_Monitoring);
-            Surface_CD[iMarker_Monitoring]      = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetSurface_CD(iMarker_Monitoring);
-            Surface_CSF[iMarker_Monitoring] = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetSurface_CSF(iMarker_Monitoring);
-            Surface_CEff[iMarker_Monitoring]       = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetSurface_CEff(iMarker_Monitoring);
-            Surface_CFx[iMarker_Monitoring]        = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetSurface_CFx(iMarker_Monitoring);
-            Surface_CFy[iMarker_Monitoring]        = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetSurface_CFy(iMarker_Monitoring);
-            Surface_CFz[iMarker_Monitoring]        = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetSurface_CFz(iMarker_Monitoring);
-            Surface_CMx[iMarker_Monitoring]        = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetSurface_CMx(iMarker_Monitoring);
-            Surface_CMy[iMarker_Monitoring]        = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetSurface_CMy(iMarker_Monitoring);
-            Surface_CMz[iMarker_Monitoring]        = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetSurface_CMz(iMarker_Monitoring);
-
-            if(buffet) Surface_Buffet_Metric[iMarker_Monitoring] = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetSurface_Buffet_Metric(iMarker_Monitoring);
-          }
-        }
-
-        if (turbo) {
-          /*--- Loop over the nMarker of turboperformance and get the desired values ---*/
-          for (iMarker_Monitoring = 0; iMarker_Monitoring < nTurboPerf; iMarker_Monitoring++) {
-            for(iSpan=0; iSpan<nSpanWiseSections+1; iSpan++){
-              if ((iMarker_Monitoring == 0) && (direct_diff != NO_DERIVATIVE)){
-                D_TotalPressure_Loss = SU2_TYPE::GetDerivative(TotalPressureLoss[iMarker_Monitoring][iSpan]);
-                D_FlowAngle_Out      = 180.0/PI_NUMBER*SU2_TYPE::GetDerivative(FlowAngleOut[iMarker_Monitoring][iSpan]);
-              }
-            }
-          }
-          if (direct_diff != NO_DERIVATIVE){
-            D_TotalStaticEfficiency = SU2_TYPE::GetDerivative(TotalStaticEfficiency[nTurboPerf-1][nSpanWiseSections]);
-            D_TotalTotalEfficiency  = SU2_TYPE::GetDerivative(TotalTotalEfficiency[nTurboPerf-1][nSpanWiseSections]);
-            D_EntropyGen            = SU2_TYPE::GetDerivative(EntropyGen[nTurboPerf-1][nSpanWiseSections]);
-          }
-        }
-
-        /*--- Get flux-averaged values at the specified surface ---*/
-
-        if (output_surface) {
-
-          unsigned short iMarker_Analyze = 0;
-          Surface_MassFlow = config[ZONE_0]->GetSurface_MassFlow(iMarker_Analyze);
-          Surface_Mach = config[ZONE_0]->GetSurface_Mach(iMarker_Analyze);
-          Surface_Temperature = config[ZONE_0]->GetSurface_Temperature(iMarker_Analyze);
-          Surface_Pressure = config[ZONE_0]->GetSurface_Pressure(iMarker_Analyze);
-          Surface_Density = config[ZONE_0]->GetSurface_Density(iMarker_Analyze);
-          Surface_Enthalpy = config[ZONE_0]->GetSurface_Enthalpy(iMarker_Analyze);
-          Surface_NormalVelocity = config[ZONE_0]->GetSurface_NormalVelocity(iMarker_Analyze);
-          Surface_Uniformity = config[ZONE_0]->GetSurface_Uniformity(iMarker_Analyze);
-          Surface_SecondaryStrength = config[ZONE_0]->GetSurface_SecondaryStrength(iMarker_Analyze);
-          Surface_MomentumDistortion = config[ZONE_0]->GetSurface_MomentumDistortion(iMarker_Analyze);
-          Surface_SecondOverUniform = config[ZONE_0]->GetSurface_SecondOverUniform(iMarker_Analyze);
-          Surface_TotalTemperature = config[ZONE_0]->GetSurface_TotalTemperature(iMarker_Analyze);
-          Surface_TotalPressure = config[ZONE_0]->GetSurface_TotalPressure(iMarker_Analyze);
-          Surface_PressureDrop = config[ZONE_0]->GetSurface_PressureDrop(iMarker_Analyze);
-
-          if (direct_diff != NO_DERIVATIVE){
-            D_Surface_Uniformity = SU2_TYPE::GetDerivative(Surface_Uniformity);
-            D_Surface_SecondaryStrength = SU2_TYPE::GetDerivative(Surface_SecondaryStrength);
-            D_Surface_MomentumDistortion = SU2_TYPE::GetDerivative(Surface_MomentumDistortion);
-            D_Surface_SecondOverUniform = SU2_TYPE::GetDerivative(Surface_SecondOverUniform);
-            D_Surface_PressureDrop = SU2_TYPE::GetDerivative(Surface_PressureDrop);
-          }
-        }
-
-        /*--- Flow Residuals ---*/
-
-        for (iVar = 0; iVar < nVar_Flow; iVar++)
-          residual_flow[iVar] = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetRes_RMS(iVar);
-
-        /*--- Turbulent residual ---*/
-
-        if (turbulent) {
-          for (iVar = 0; iVar < nVar_Turb; iVar++)
-            residual_turbulent[iVar] = solver_container[val_iZone][val_iInst][FinestMesh][TURB_SOL]->GetRes_RMS(iVar);
-        }
-
-        if (weakly_coupled_heat) {
-          for (iVar = 0; iVar < nVar_Heat; iVar++) {
-            residual_heat[iVar] = solver_container[val_iZone][val_iInst][FinestMesh][HEAT_SOL]->GetRes_RMS(iVar);
-          }
-
-        }
-
-        /*--- Transition residual ---*/
-
-        if (transition) {
-          for (iVar = 0; iVar < nVar_Trans; iVar++)
-            residual_transition[iVar] = solver_container[val_iZone][val_iInst][FinestMesh][TRANS_SOL]->GetRes_RMS(iVar);
-        }
-
-
-        /*--- FEA residual ---*/
-        //        if (fluid_structure) {
-        //          for (iVar = 0; iVar < nVar_FEA; iVar++)
-        //            residual_fea[iVar] = solver_container[ZONE_0][FinestMesh][FEA_SOL]->GetRes_RMS(iVar);
-        //        }
-
-        /*--- Iterations of the linear solver ---*/
-
-        LinSolvIter = (unsigned long) solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetIterLinSolver();
-
-        /*--- Adjoint solver ---*/
-
-        if (adjoint) {
-
-          /*--- Adjoint solution coefficients ---*/
-
-          Total_Sens_Geo       = solver_container[val_iZone][val_iInst][FinestMesh][ADJFLOW_SOL]->GetTotal_Sens_Geo();
-          Total_Sens_Mach      = solver_container[val_iZone][val_iInst][FinestMesh][ADJFLOW_SOL]->GetTotal_Sens_Mach();
-          Total_Sens_AoA       = solver_container[val_iZone][val_iInst][FinestMesh][ADJFLOW_SOL]->GetTotal_Sens_AoA() * PI_NUMBER / 180.0;
-          Total_Sens_Press     = solver_container[val_iZone][val_iInst][FinestMesh][ADJFLOW_SOL]->GetTotal_Sens_Press();
-          Total_Sens_Temp      = solver_container[val_iZone][val_iInst][FinestMesh][ADJFLOW_SOL]->GetTotal_Sens_Temp();
-          Total_Sens_BPressure = solver_container[val_iZone][val_iInst][FinestMesh][ADJFLOW_SOL]->GetTotal_Sens_BPress();
-          Total_Sens_ModVel    = solver_container[val_iZone][val_iInst][FinestMesh][ADJFLOW_SOL]->GetTotal_Sens_ModVel();
-
-          if (radiation){
-            Total_Sens_Temp      += solver_container[val_iZone][val_iInst][FinestMesh][ADJRAD_SOL]->GetTotal_Sens_Temp();
-          }
-
-          /*--- Adjoint flow residuals ---*/
-
-          for (iVar = 0; iVar < nVar_AdjFlow; iVar++) {
-            residual_adjflow[iVar] = solver_container[val_iZone][val_iInst][FinestMesh][ADJFLOW_SOL]->GetRes_RMS(iVar);
-          }
-
-          /*--- Adjoint turbulent residuals ---*/
-
-          if (turbulent) {
-            if (!frozen_visc) {
-              for (iVar = 0; iVar < nVar_AdjTurb; iVar++)
-                residual_adjturbulent[iVar] = solver_container[val_iZone][val_iInst][FinestMesh][ADJTURB_SOL]->GetRes_RMS(iVar);
-            }
-          }
-
-          if (weakly_coupled_heat) {
-            for (iVar = 0; iVar < nVar_Heat; iVar++) {
-              residual_adjheat[iVar] = solver_container[val_iZone][val_iInst][FinestMesh][ADJHEAT_SOL]->GetRes_RMS(iVar);
-            }
-          }
-
-        }
-
-        break;
-
-
-      case MAIN_SOLVER::HEAT_EQUATION:
-
-        /*--- Heat coefficients  ---*/
-
-        Total_Heat         = solver_container[val_iZone][val_iInst][FinestMesh][HEAT_SOL]->GetTotal_HeatFlux();
-        Total_MaxHeat      = solver_container[val_iZone][val_iInst][FinestMesh][HEAT_SOL]->GetTotal_MaxHeatFlux();
-        Total_Temperature  = solver_container[val_iZone][val_iInst][FinestMesh][HEAT_SOL]->GetTotal_AvgTemperature();
-
-        /*--- Heat Residuals ---*/
-
-        for (iVar = 0; iVar < nVar_Heat; iVar++) {
-          residual_heat[iVar] = solver_container[val_iZone][val_iInst][FinestMesh][HEAT_SOL]->GetRes_RMS(iVar);
-        }
-
-        break;
-
-      case MAIN_SOLVER::FEM_ELASTICITY:
-
-        /*--- FEM coefficients -- As of now, this is the Von Mises Stress ---*/
-
-        Total_VMStress = solver_container[val_iZone][val_iInst][FinestMesh][FEA_SOL]->GetTotal_CFEA();
-
-        Total_ForceCoeff = solver_container[val_iZone][val_iInst][FinestMesh][FEA_SOL]->GetForceCoeff();
-
-        Total_IncLoad = solver_container[val_iZone][val_iInst][FinestMesh][FEA_SOL]->GetLoad_Increment();
-
-        LinSolvIter = (unsigned long) solver_container[val_iZone][val_iInst][FinestMesh][FEA_SOL]->GetIterLinSolver();
-
-        /*--- Residuals: ---*/
-        /*--- Linear analysis: RMS of the displacements in the nDim coordinates ---*/
-        /*--- Nonlinear analysis: UTOL, RTOL and DTOL (defined in the Postprocessing function) ---*/
-
-        if (linear_analysis) {
-          for (iVar = 0; iVar < nVar_FEM; iVar++) {
-            residual_fem[iVar] = solver_container[val_iZone][val_iInst][FinestMesh][FEA_SOL]->GetRes_RMS(iVar);
-          }
-        }
-        else if (nonlinear_analysis) {
-          for (iVar = 0; iVar < nVar_FEM; iVar++) {
-            residual_fem[iVar] = solver_container[val_iZone][val_iInst][FinestMesh][FEA_SOL]->GetRes_FEM(iVar);
-          }
-        }
-
-        break;
-
-      case MAIN_SOLVER::DISC_ADJ_FEM:
-
-        /*--- FEM coefficients -- As of now, this is the Von Mises Stress ---*/
-
-        Total_VMStress = solver_container[val_iZone][val_iInst][FinestMesh][FEA_SOL]->GetTotal_CFEA();
-
-        /*--- Residuals: ---*/
-        /*--- Linear analysis: RMS of the displacements in the nDim coordinates ---*/
-        /*--- Nonlinear analysis: UTOL, RTOL and DTOL (defined in the Postprocessing function) ---*/
-         for (iVar = 0; iVar < nVar_FEM; iVar++) {
-           residual_fem[iVar] = solver_container[val_iZone][val_iInst][FinestMesh][ADJFEA_SOL]->GetRes_RMS(iVar);
-         }
-
-        break;
-
-      default:
-        break;
-
-    }
-
-    if (extra_heat_output) {
-      Extra_Total_Heat      = solver_container[ExtraHeatOutputZone][val_iInst][FinestMesh][HEAT_SOL]->GetTotal_HeatFlux();
-      //Extra_Total_Temperature   = solver_container[ExtraHeatOutputZone][val_iInst][FinestMesh][HEAT_SOL]->GetTotal_Temperature();
-      Extra_Heat_Residual   = log10(solver_container[ExtraHeatOutputZone][val_iInst][FinestMesh][HEAT_SOL]->GetRes_RMS(0));
-    }
-
-    if (radiation){
-      if (disc_adj){
-        for (iVar = 0; iVar < nVar_Rad; iVar++) {
-          residual_rad[iVar] = solver_container[val_iZone][val_iInst][FinestMesh][ADJRAD_SOL]->GetRes_RMS(iVar);
-        }
-      }
-      else{
-        for (iVar = 0; iVar < nVar_Rad; iVar++) {
-          residual_rad[iVar] = solver_container[val_iZone][val_iInst][FinestMesh][RAD_SOL]->GetRes_RMS(iVar);
-        }
-      }
-    }
-
-    /*--- Header frequency ---*/
-
-    bool Unsteady = ((config[val_iZone]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
-                     (config[val_iZone]->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND));
-    bool In_NoDualTime = (!DualTime_Iteration && (iExtIter % config[val_iZone]->GetScreen_Wrt_Freq(2) == 0));
-    bool In_DualTime_0 = (DualTime_Iteration && (iIntIter % config[val_iZone]->GetScreen_Wrt_Freq(0) == 0));
-    bool In_DualTime_1 = (!DualTime_Iteration && Unsteady);
-    bool In_DualTime_2 = (Unsteady && DualTime_Iteration && (iExtIter % config[val_iZone]->GetScreen_Wrt_Freq(2) == 0));
-    bool In_DualTime_3 = (Unsteady && !DualTime_Iteration && (iExtIter % config[val_iZone]->GetScreen_Wrt_Freq(2) == 0));
-
-    /*--- Header frequency: analogy for dynamic structural analysis ---*/
-    /*--- DualTime_Iteration is a bool we receive, which is true if it comes from FEM_StructuralIteration and false from SU2_CFD ---*/
-    /*--- We maintain the name, as it is an input of the function ---*/
-    /*--- dynamic determines if the problem is, or not, time dependent ---*/
-    bool dynamic = (config[val_iZone]->GetTime_Domain());              // Dynamic simulations.
-    bool In_NoDynamic = (!DualTime_Iteration && (iExtIter % config[val_iZone]->GetScreen_Wrt_Freq(2) == 0));
-    bool In_Dynamic_0 = (DualTime_Iteration && (iIntIter % config[val_iZone]->GetScreen_Wrt_Freq(0) == 0));
-    bool In_Dynamic_1 = (!DualTime_Iteration && nonlinear_analysis);
-    bool In_Dynamic_2 = (nonlinear_analysis && DualTime_Iteration && (iExtIter % config[val_iZone]->GetScreen_Wrt_Freq(2) == 0));
-    bool In_Dynamic_3 = (nonlinear_analysis && !DualTime_Iteration && (iExtIter % config[val_iZone]->GetScreen_Wrt_Freq(2) == 0));
-
-    bool write_heads;
-    if (Unsteady) write_heads = (iIntIter == 0);
-    else write_heads = (((iExtIter % (config[val_iZone]->GetScreen_Wrt_Freq(2)*40)) == 0));
-
-    bool write_turbo = (((iExtIter % (config[val_iZone]->GetScreen_Wrt_Freq(2)*40)) == 0) || (iExtIter == (config[val_iZone]->GetnInner_Iter() -1)));
-
-    /*--- Analogous for dynamic problems (as of now I separate the problems, it may be worthy to do all together later on ---*/
-    bool write_heads_FEM;
-    if (nonlinear_analysis) write_heads_FEM = (iIntIter == 0);
-    else write_heads_FEM = (((iExtIter % (config[val_iZone]->GetScreen_Wrt_Freq(2)*40)) == 0));
-
-    if (  (!fem && ((In_NoDualTime || In_DualTime_0 || In_DualTime_1) && (In_NoDualTime || In_DualTime_2 || In_DualTime_3))) ||
-        (fem  && ( (In_NoDynamic || In_Dynamic_0 || In_Dynamic_1) && (In_NoDynamic || In_Dynamic_2 || In_Dynamic_3)))
-        ) {
-
-
-      /*--- Prepare the history file output, note that the dual
-       time output don't write to the history file ---*/
-      if (!DualTime_Iteration) {
-
-        /*--- Write the begining of the history file ---*/
-        SPRINTF(begin, "%12d", SU2_TYPE::Int(iExtIter+ExtIter_OffSet));
-
-        /*--- Write the end of the history file ---*/
-        SPRINTF (end, ", %12.10f, %12.10f, %12.10f\n", su2double(LinSolvIter), config[val_iZone]->GetCFL(MESH_0), timeused/60.0);
-
-        /*--- Write the solution and residual of the history file ---*/
-        switch (config[val_iZone]->GetKind_Solver()) {
-
-          case MAIN_SOLVER::EULER : case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::RANS:
-          case MAIN_SOLVER::INC_EULER : case MAIN_SOLVER::INC_NAVIER_STOKES: case MAIN_SOLVER::INC_RANS:
-          case MAIN_SOLVER::FEM_EULER : case MAIN_SOLVER::FEM_NAVIER_STOKES: case MAIN_SOLVER::FEM_RANS: case MAIN_SOLVER::FEM_LES:
-          case MAIN_SOLVER::ADJ_EULER: case MAIN_SOLVER::ADJ_NAVIER_STOKES: case MAIN_SOLVER::ADJ_RANS: case MAIN_SOLVER::DISC_ADJ_EULER:
-          case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_RANS:
-          case MAIN_SOLVER::DISC_ADJ_INC_EULER: case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_INC_RANS:
-
-            /*--- Direct coefficients ---*/
-            SPRINTF (direct_coeff, ", %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e",
-                     Total_CL, Total_CD, Total_CSF, Total_CMx, Total_CMy, Total_CMz, Total_CFx, Total_CFy,
-                     Total_CFz, Total_CEff, Total_AoA, Total_Custom_ObjFunc);
-            if (buffet) SPRINTF (buffet_coeff, ", %14.8e",  Total_Buffet_Metric);
-            if (thermal || heat) SPRINTF (heat_coeff, ", %14.8e, %14.8e, %14.8e",  Total_Heat, Total_MaxHeat, Total_Temperature);
-            if (equiv_area) SPRINTF (equivalent_area_coeff, ", %14.8e, %14.8e", Total_CEquivArea, Total_CNearFieldOF);
-            if (engine || actuator_disk) SPRINTF (engine_coeff, ", %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e", Total_NetThrust, Total_Power, Total_AeroCD, Total_SolidCD, Total_IDR, Total_IDC);
-            if (rotating_frame) SPRINTF (rotating_frame_coeff, ", %14.8e, %14.8e, %14.8e", Total_CMerit, Total_CT, Total_CQ);
-            if (inv_design) {
-              SPRINTF (Cp_inverse_design, ", %14.8e", solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_CpDiff());
-              if (thermal && !turbo) SPRINTF (Heat_inverse_design, ", %14.8e", solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetTotal_HeatFluxDiff());
-            }
-
-            if (direct_diff != NO_DERIVATIVE) {
-              if (!turbo)
-                SPRINTF (d_direct_coeff, ", %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e",
-                         D_Total_CL, D_Total_CD, D_Total_CSF, D_Total_CMx, D_Total_CMy, D_Total_CMz, D_Total_CFx, D_Total_CFy,
-                         D_Total_CFz, D_Total_CEff, D_Total_Custom_ObjFunc);
-              else
-                SPRINTF (d_direct_coeff, ", %12.10f, %12.10f, %12.10f, %12.10f, %12.10f", D_TotalPressure_Loss, D_FlowAngle_Out,
-                         D_TotalTotalEfficiency, D_TotalStaticEfficiency, D_EntropyGen);
-              if (engine || actuator_disk)
-              SPRINTF (d_direct_coeff, ", %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e",
-                       D_Total_CL, D_Total_CD, D_Total_CSF, D_Total_CMx, D_Total_CMy, D_Total_CMz, D_Total_CFx, D_Total_CFy,
-                       D_Total_CFz, D_Total_CEff, D_Total_Custom_ObjFunc, D_Total_NetThrust, D_Total_Power, D_Total_AeroCD, D_Total_SolidCD, D_Total_IDR, D_Total_IDC);
-              if (thermal)
-                SPRINTF (d_direct_coeff, ", %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e",
-                         D_Total_CL, D_Total_CD, D_Total_CSF, D_Total_CMx, D_Total_CMy, D_Total_CMz, D_Total_CFx, D_Total_CFy,
-                         D_Total_CFz, D_Total_CEff, D_Total_Custom_ObjFunc, D_Total_Heat, D_Total_MaxHeat);
-            }
-
-            if (aeroelastic) {
-              for (iMarker_Monitoring = 0; iMarker_Monitoring < config[ZONE_0]->GetnMarker_Monitoring(); iMarker_Monitoring++) {
-                //Append one by one the surface coeff to aeroelastic coeff. (Think better way do this, maybe use string)
-                if (iMarker_Monitoring == 0) {
-                  SPRINTF(aeroelastic_coeff, ", %12.10f", aeroelastic_plunge[iMarker_Monitoring]);
-                }
-                else {
-                  SPRINTF(surface_coeff, ", %12.10f", aeroelastic_plunge[iMarker_Monitoring]);
-                  strcat(aeroelastic_coeff, surface_coeff);
-                }
-                SPRINTF(surface_coeff, ", %12.10f", aeroelastic_pitch[iMarker_Monitoring]);
-                strcat(aeroelastic_coeff, surface_coeff);
-              }
-            }
-
-            if (output_per_surface) {
-              for (iMarker_Monitoring = 0; iMarker_Monitoring < config[ZONE_0]->GetnMarker_Monitoring(); iMarker_Monitoring++) {
-                //Append one by one the surface coeff to monitoring coeff. (Think better way do this, maybe use string)
-                if (iMarker_Monitoring == 0) {
-                  SPRINTF(monitoring_coeff, ", %12.10f", Surface_CL[iMarker_Monitoring]);
-                }
-                else {
-                  SPRINTF(surface_coeff, ", %12.10f", Surface_CL[iMarker_Monitoring]);
-                  strcat(monitoring_coeff, surface_coeff);
-                }
-                SPRINTF(surface_coeff, ", %12.10f", Surface_CD[iMarker_Monitoring]);
-                strcat(monitoring_coeff, surface_coeff);
-                SPRINTF(surface_coeff, ", %12.10f", Surface_CSF[iMarker_Monitoring]);
-                strcat(monitoring_coeff, surface_coeff);
-                SPRINTF(surface_coeff, ", %12.10f", Surface_CEff[iMarker_Monitoring]);
-                strcat(monitoring_coeff, surface_coeff);
-                SPRINTF(surface_coeff, ", %12.10f", Surface_CFx[iMarker_Monitoring]);
-                strcat(monitoring_coeff, surface_coeff);
-                SPRINTF(surface_coeff, ", %12.10f", Surface_CFy[iMarker_Monitoring]);
-                strcat(monitoring_coeff, surface_coeff);
-                SPRINTF(surface_coeff, ", %12.10f", Surface_CFz[iMarker_Monitoring]);
-                strcat(monitoring_coeff, surface_coeff);
-                SPRINTF(surface_coeff, ", %12.10f", Surface_CMx[iMarker_Monitoring]);
-                strcat(monitoring_coeff, surface_coeff);
-                SPRINTF(surface_coeff, ", %12.10f", Surface_CMy[iMarker_Monitoring]);
-                strcat(monitoring_coeff, surface_coeff);
-                SPRINTF(surface_coeff, ", %12.10f", Surface_CMz[iMarker_Monitoring]);
-                strcat(monitoring_coeff, surface_coeff);
-
-                if(buffet){
-                  SPRINTF(surface_coeff, ", %12.10f", Surface_Buffet_Metric[iMarker_Monitoring]);
-                  strcat(monitoring_coeff, surface_coeff);
-                }
-              }
-            }
-
-            if (turbo){
-              for (iMarker_Monitoring = 0; iMarker_Monitoring < config[ZONE_0]->GetnMarker_TurboPerformance(); iMarker_Monitoring++){
-                if (iMarker_Monitoring == 0){
-                  SPRINTF(turbo_coeff, ", %12.10f", TotalPressureLoss[iMarker_Monitoring][nSpanWiseSections]);
-                }else{
-                  SPRINTF(surface_coeff, ", %12.10f", TotalPressureLoss[iMarker_Monitoring][nSpanWiseSections]);
-                  strcat(turbo_coeff, surface_coeff);
-                }
-                SPRINTF(surface_coeff, ", %12.10f", KineticEnergyLoss[iMarker_Monitoring][nSpanWiseSections]);
-                strcat(turbo_coeff, surface_coeff);
-                SPRINTF(surface_coeff, ", %12.10f", EntropyGen[iMarker_Monitoring][nSpanWiseSections]);
-                strcat(turbo_coeff, surface_coeff);
-                SPRINTF(surface_coeff, ", %12.10f", EulerianWork[iMarker_Monitoring][nSpanWiseSections]);
-                strcat(turbo_coeff, surface_coeff);
-                SPRINTF(surface_coeff, ", %12.10f", PressureRatio[iMarker_Monitoring][nSpanWiseSections]);
-                strcat(turbo_coeff, surface_coeff);
-                SPRINTF(surface_coeff, ", %12.10f", 180.0/PI_NUMBER*FlowAngleIn[iMarker_Monitoring][nSpanWiseSections]);
-                strcat(turbo_coeff, surface_coeff);
-                SPRINTF(surface_coeff, ", %12.10f", 180.0/PI_NUMBER*FlowAngleOut[iMarker_Monitoring][nSpanWiseSections]);
-                strcat(turbo_coeff, surface_coeff);
-                SPRINTF(surface_coeff, ", %12.10f", 180.0/PI_NUMBER*AbsFlowAngleIn[iMarker_Monitoring][nSpanWiseSections]);
-                strcat(turbo_coeff, surface_coeff);
-                SPRINTF(surface_coeff, ", %12.10f", 180.0/PI_NUMBER*AbsFlowAngleOut[iMarker_Monitoring][nSpanWiseSections]);
-                strcat(turbo_coeff, surface_coeff);
-                SPRINTF(surface_coeff, ", %12.10f", MassFlowIn[iMarker_Monitoring][nSpanWiseSections]);
-                strcat(turbo_coeff, surface_coeff);
-                SPRINTF(surface_coeff, ", %12.10f", MassFlowOut[iMarker_Monitoring][nSpanWiseSections]);
-                strcat(turbo_coeff, surface_coeff);
-                SPRINTF(surface_coeff, ", %12.10f", sqrt(MachIn[iMarker_Monitoring][nSpanWiseSections][1]*MachIn[iMarker_Monitoring][nSpanWiseSections][1] + MachIn[iMarker_Monitoring][nSpanWiseSections][0]*MachIn[iMarker_Monitoring][nSpanWiseSections][0]));
-                strcat(turbo_coeff, surface_coeff);
-                SPRINTF(surface_coeff, ", %12.10f", sqrt(MachOut[iMarker_Monitoring][nSpanWiseSections][1]*MachOut[iMarker_Monitoring][nSpanWiseSections][1] + MachOut[iMarker_Monitoring][nSpanWiseSections][0]*MachOut[iMarker_Monitoring][nSpanWiseSections][0]));
-                strcat(turbo_coeff, surface_coeff);
-                SPRINTF(surface_coeff, ", %12.10f", TotalTotalEfficiency[iMarker_Monitoring][nSpanWiseSections]);
-                strcat(turbo_coeff, surface_coeff);
-                SPRINTF(surface_coeff, ", %12.10f", TotalStaticEfficiency[iMarker_Monitoring][nSpanWiseSections]);
-                strcat(turbo_coeff, surface_coeff);
-
-              }
-            }
-
-
-            /*--- Flow residual ---*/
-            if (nDim == 2) {
-              if (compressible) SPRINTF (flow_resid, ", %14.8e, %14.8e, %14.8e, %14.8e, %14.8e", log10 (residual_flow[0]), log10 (residual_flow[1]), log10 (residual_flow[2]), log10 (residual_flow[3]), dummy);
-              if (incompressible) SPRINTF (flow_resid, ", %14.8e, %14.8e, %14.8e, %14.8e, %14.8e", log10 (residual_flow[0]), log10 (residual_flow[1]), log10 (residual_flow[2]), log10 (residual_flow[3]), dummy);
-            }
-            else {
-              if (compressible) SPRINTF (flow_resid, ", %14.8e, %14.8e, %14.8e, %14.8e, %14.8e", log10 (residual_flow[0]), log10 (residual_flow[1]), log10 (residual_flow[2]), log10 (residual_flow[3]), log10 (residual_flow[4]) );
-              if (incompressible) SPRINTF (flow_resid, ", %14.8e, %14.8e, %14.8e, %14.8e, %14.8e", log10 (residual_flow[0]), log10 (residual_flow[1]), log10 (residual_flow[2]), log10 (residual_flow[3]), log10 (residual_flow[4]));
-            }
-
-            /*--- Turbulent residual ---*/
-            if (turbulent) {
-              switch(nVar_Turb) {
-                case 1: SPRINTF (turb_resid, ", %12.10f", log10 (residual_turbulent[0])); break;
-                case 2: SPRINTF (turb_resid, ", %12.10f, %12.10f", log10(residual_turbulent[0]), log10(residual_turbulent[1])); break;
-              }
-            }
-
-            /*---- Averaged stagnation pressure at an exit ----*/
-
-            if (output_surface) {
-              SPRINTF( surface_outputs, ", %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, %14.8e", Surface_MassFlow, Surface_Mach, Surface_Temperature, Surface_Pressure, Surface_Density, Surface_Enthalpy, Surface_NormalVelocity, Surface_Uniformity, Surface_SecondaryStrength, Surface_MomentumDistortion, Surface_SecondOverUniform, Surface_TotalTemperature, Surface_TotalPressure, Surface_PressureDrop);
-
-              if (direct_diff != NO_DERIVATIVE) {
-                SPRINTF( d_surface_outputs, ", %14.8e, %14.8e, %14.8e, %14.8e, %14.8e",
-                        D_Surface_Uniformity, D_Surface_SecondaryStrength, D_Surface_MomentumDistortion, D_Surface_SecondOverUniform, D_Surface_PressureDrop);
-              }
-            }
-
-            /*--- Transition residual ---*/
-            if (transition) {
-              SPRINTF (trans_resid, ", %12.10f, %12.10f", log10(residual_transition[0]), log10(residual_transition[1]));
-            }
-
-            /*--- Combo objective ---*/
-            if (output_comboObj) {
-              SPRINTF(combo_obj,", %12.10f", Total_ComboObj);
-            }
-
-            /*--- Fluid structure residual ---*/
-            //            if (fluid_structure) {
-            //              if (nDim == 2) SPRINTF (levelset_resid, ", %12.10f, %12.10f, 0.0", log10 (residual_fea[0]), log10 (residual_fea[1]));
-            //              else SPRINTF (levelset_resid, ", %12.10f, %12.10f, %12.10f", log10 (residual_fea[0]), log10 (residual_fea[1]), log10 (residual_fea[2]));
-            //            }
-
-            if (adjoint) {
-
-              /*--- Adjoint coefficients ---*/
-              if (!turbo) {
-                if (compressible) {
-                  SPRINTF (adjoint_coeff, ", %14.8e, %14.8e, %14.8e, %14.8e, %14.8e, 0.0", Total_Sens_Geo, Total_Sens_Mach, Total_Sens_AoA, Total_Sens_Press, Total_Sens_Temp);
-                }
-                if (incompressible) {
-                  SPRINTF (adjoint_coeff, ", %14.8e, %14.8e, %14.8e, %14.8e", Total_Sens_Geo, Total_Sens_ModVel, Total_Sens_BPressure, Total_Sens_Temp);
-                }
-              } else
-                SPRINTF (adjoint_coeff, ", %14.8e, %14.8e, %14.8e", Total_Sens_Geo, Total_Sens_BPressure, Total_Sens_Temp);
-
-              /*--- Adjoint flow residuals ---*/
-              if (nDim == 2) {
-                if (compressible) SPRINTF (adj_flow_resid, ", %14.8e, %14.8e, %14.8e, %14.8e, 0.0", log10 (residual_adjflow[0]), log10 (residual_adjflow[1]), log10 (residual_adjflow[2]), log10 (residual_adjflow[3]) );
-                if (incompressible) SPRINTF (adj_flow_resid, ", %14.8e, %14.8e, %14.8e, %14.8e, 0.0", log10 (residual_adjflow[0]), log10 (residual_adjflow[1]), log10 (residual_adjflow[2]), log10 (residual_adjflow[3]) );
-              }
-              else {
-                if (compressible) SPRINTF (adj_flow_resid, ", %14.8e, %14.8e, %14.8e, %14.8e, %14.8e", log10 (residual_adjflow[0]), log10 (residual_adjflow[1]), log10 (residual_adjflow[2]), log10 (residual_adjflow[3]), log10 (residual_adjflow[4]) );
-                if (incompressible) SPRINTF (adj_flow_resid, ", %14.8e, %14.8e, %14.8e, %14.8e, %14.8e", log10 (residual_adjflow[0]), log10 (residual_adjflow[1]), log10 (residual_adjflow[2]), log10 (residual_adjflow[3]), log10 (residual_adjflow[4]));
-              }
-
-              /*--- Adjoint turbulent residuals ---*/
-              if (turbulent)
-                if (!frozen_visc) {
-                  if (nVar_AdjTurb == 1) {
-                  SPRINTF (adj_turb_resid, ", %14.8e", log10 (residual_adjturbulent[0]));
-                  } else if (nVar_AdjTurb > 1) {
-                    SPRINTF (adj_turb_resid, ", %14.8e, %14.8e", log10 (residual_adjturbulent[0]), log10 (residual_adjturbulent[1]));
-                  }
-                }
-
-            }
-
-            if (weakly_coupled_heat) {
-              SPRINTF (heat_resid, ", %14.8e", log10 (residual_heat[0]));
-            }
-
-            if (radiation){
-              SPRINTF (rad_resid, ", %14.8e", log10 (residual_rad[0]));
-            }
-
-            break;
-
-          case MAIN_SOLVER::HEAT_EQUATION:
-
-            SPRINTF (direct_coeff, ", %14.8e, %14.8e, %14.8e", Total_Heat, Total_MaxHeat, Total_Temperature);
-            SPRINTF (heat_resid, ", %14.8e", log10 (residual_heat[0]));
-
-            break;
-
-          case MAIN_SOLVER::FEM_ELASTICITY:
-
-            SPRINTF (begin_fem, ", %14.8e", 0.0);
-
-            if (incload) SPRINTF (fem_coeff, ", %14.8e, %14.8e, %14.8e", Total_VMStress, Total_ForceCoeff, Total_IncLoad);
-            else SPRINTF (fem_coeff, ", %14.8e, %14.8e", Total_VMStress, Total_ForceCoeff);
-            /*--- FEM residual ---*/
-            if (nDim == 2) {
-              if (linear_analysis) SPRINTF (fem_resid, ", %14.8e, %14.8e, %14.8e", log10 (residual_fem[0]), log10 (residual_fem[1]), dummy);
-              if (nonlinear_analysis) SPRINTF (fem_resid, ", %14.8e, %14.8e, %14.8e", log10 (residual_fem[0]), log10 (residual_fem[1]), log10 (residual_fem[2]));
-            }
-            else {
-              SPRINTF (fem_resid, ", %14.8e, %14.8e, %14.8e", log10 (residual_fem[0]), log10 (residual_fem[1]), log10 (residual_fem[2]));
-            }
-            SPRINTF (end_fem, ", %lu, %12.10f\n", LinSolvIter, timeused/60.0);
-
-            break;
-
-          case MAIN_SOLVER::DISC_ADJ_FEM:
-
-            SPRINTF (direct_coeff, ", %12.10f", Total_VMStress);
-            if (nDim == 2) {
-              SPRINTF (fem_resid, ", %14.8e, %14.8e, %14.8e, %14.8e, %14.8e", log10 (residual_fem[0]), log10 (residual_fem[1]), dummy, dummy, dummy);
-            }
-            else {
-              SPRINTF (fem_resid, ", %14.8e, %14.8e, %14.8e, %14.8e, %14.8e", log10 (residual_fem[0]), log10 (residual_fem[1]), log10 (residual_fem[2]), dummy, dummy);
-            }
-
-            break;
-          default:
-            break;
-        }
-      }
-      if ((val_iZone == 0 && val_iInst == 0)|| fluid_structure){
-        /*--- Write the screen header---*/
-        if (  (!fem && ((write_heads) && !(!DualTime_Iteration && Unsteady))) ||
-            (fem && ((write_heads_FEM) && !(!DualTime_Iteration && nonlinear_analysis)))
-        ) {
-
-          if (!fem) {
-            if (!Unsteady && (config[val_iZone]->GetTime_Marching() != TIME_MARCHING::TIME_STEPPING)) {
-              switch (config[val_iZone]->GetKind_Solver()) {
-              case MAIN_SOLVER::EULER : case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::RANS:
-              case MAIN_SOLVER::INC_EULER : case MAIN_SOLVER::INC_NAVIER_STOKES: case MAIN_SOLVER::INC_RANS:
-              case MAIN_SOLVER::FEM_EULER : case MAIN_SOLVER::FEM_NAVIER_STOKES: case MAIN_SOLVER::FEM_RANS: case MAIN_SOLVER::FEM_LES:
-              case MAIN_SOLVER::ADJ_EULER : case MAIN_SOLVER::ADJ_NAVIER_STOKES: case MAIN_SOLVER::ADJ_RANS:
-
-                cout << endl << "---------------------- Local Time Stepping Summary ----------------------" << endl;
-
-                for (unsigned short iMesh = FinestMesh; iMesh <= config[val_iZone]->GetnMGLevels(); iMesh++)
-                  cout << "MG level: "<< iMesh << " -> Min. DT: " << solver_container[val_iZone][val_iInst][iMesh][FLOW_SOL]->GetMin_Delta_Time()<<
-                  ". Max. DT: " << solver_container[val_iZone][val_iInst][iMesh][FLOW_SOL]->GetMax_Delta_Time() <<
-                  ". CFL: " << config[val_iZone]->GetCFL(iMesh)  << "." << endl;
-
-                if (nZone > 1)
-                  cout << "CFL in zone 2: " << config[1]->GetCFL(MESH_0) << endl;
-
-                cout << "-------------------------------------------------------------------------" << endl;
-
-                if (direct_diff != NO_DERIVATIVE) {
-                  cout << endl << "---------------------- Direct Differentiation Summary -------------------" << endl;
-                  cout << "Coefficients are differentiated with respect to ";
-                  switch (direct_diff) {
-                  case D_MACH:
-                    cout << "Mach number." << endl;
-                    break;
-                  case D_AOA:
-                    cout << "AoA." << endl;
-                    break;
-                  case D_SIDESLIP:
-                    cout << "AoS." << endl;
-                    break;
-                  case D_REYNOLDS:
-                    cout << "Reynolds number." << endl;
-                    break;
-                  case D_TURB2LAM:
-                    cout << "Turb/Lam ratio." << endl;
-                    break;
-                  case D_PRESSURE:
-                    cout << "Freestream Pressure." << endl;
-                    break;
-                  case D_TEMPERATURE:
-                    cout << "Freestream Temperature." << endl;
-                    break;
-                  case D_DENSITY:
-                    cout << "Freestream Density." << endl;
-                    break;
-                  case D_VISCOSITY:
-                    cout << "Freestream Viscosity." << endl;
-                    break;
-                  case D_DESIGN:
-                    cout << "Design Variables." << endl;
-                    break;
-                  default:
-                    break;
-                  }
-
-                  cout << "    D_CLift(Total)" << "    D_CDrag(Total)" << "      D_CMz(Total)" <<"     D_CEff(Total)" << endl;
-                  cout.width(18); cout << D_Total_CL;
-                  cout.width(18); cout << D_Total_CD;
-                  cout.width(18); cout << D_Total_CMz;
-                  cout.width(18); cout << D_Total_CEff;
-                  cout << endl << "-------------------------------------------------------------------------" << endl;
-                  cout << endl;
-                }
-                if (turbo && write_turbo && val_iZone== 0){
-                  WriteTurboPerfConvHistory(config[val_iZone]);
-                }
-                break;
-
-              case MAIN_SOLVER::DISC_ADJ_EULER: case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_RANS:
-              case MAIN_SOLVER::DISC_ADJ_INC_EULER: case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES: case MAIN_SOLVER::DISC_ADJ_INC_RANS:
-
-                cout << endl;
-                cout << "------------------------ Discrete Adjoint Summary -----------------------" << endl;
-                cout << "Total Geometry Sensitivity (updated every "  << config[val_iZone]->GetVolumeOutputFrequency(0) << " iterations): ";
-                cout.precision(4);
-                cout.setf(ios::scientific, ios::floatfield);
-                cout << Total_Sens_Geo;
-                cout << endl << "-------------------------------------------------------------------------" << endl;
-                break;
-              default:
-                break;
-              }
-            }
-            else {
-              if (flow) {
-                if ((config[val_iZone]->GetTime_Marching() == TIME_MARCHING::TIME_STEPPING) && (config[val_iZone]->GetUnst_CFL()== 0.0))
-                {
-                  cout << endl << "Min DT: " << solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetMin_Delta_Time()<< ".Max DT: " << solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetMax_Delta_Time() << ".Time step: " << config[val_iZone]->GetDelta_UnstTimeND() << ".";
-                } else if ((config[val_iZone]->GetTime_Marching() == TIME_MARCHING::TIME_STEPPING) && (config[val_iZone]->GetUnst_CFL()!= 0.0)) {
-                  cout << endl << "Min DT: " << solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetMin_Delta_Time()<< ".Max DT: " << solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetMax_Delta_Time() << ". Time step: " << solver_container[val_iZone][val_iInst][config[val_iZone]->GetFinestMesh()][FLOW_SOL]->GetMin_Delta_Time() << ". CFL: " << config[val_iZone]->GetUnst_CFL()<<".";
-                } else {
-                  cout << endl << "Min DT: " << solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetMin_Delta_Time()<< ".Max DT: " << solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetMax_Delta_Time() << ".Dual Time step: " << config[val_iZone]->GetDelta_UnstTimeND() << ".";
-                }
-              } else {
-                cout << endl << "Dual Time step: " << config[val_iZone]->GetDelta_UnstTimeND() << ".";
-              }
-            }
-          }
-          else if (fem && !fsi) {
-            if (dynamic) {
-              cout << endl << "Simulation time: " << config[val_iZone]->GetCurrent_DynTime() << ". Time step: " << config[val_iZone]->GetDelta_DynTime() << ".";
-            }
-          }
-
-          switch (config[val_iZone]->GetKind_Solver()) {
-          case MAIN_SOLVER::EULER :                  case MAIN_SOLVER::NAVIER_STOKES:
-          case MAIN_SOLVER::INC_EULER :              case MAIN_SOLVER::INC_NAVIER_STOKES:
-          case MAIN_SOLVER::FEM_EULER : case MAIN_SOLVER::FEM_NAVIER_STOKES: case MAIN_SOLVER::FEM_LES:
-
-            /*--- Visualize the maximum residual ---*/
-            iPointMaxResid = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetPoint_Max(0);
-            Coord = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetPoint_Max_Coord(0);
-
-            cout << endl << "----------------------- Residual Evolution Summary ----------------------" << endl;
-
-            cout << "log10[Maximum residual]: " << log10(solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetRes_Max(0)) << "." << endl;
-
-            if (config[val_iZone]->GetSystemMeasurements() == SI) {
-              cout <<"Maximum residual point " << iPointMaxResid << ", located at (" << Coord[0] << ", " << Coord[1];
-              if (nDim == 3) cout << ", " << Coord[2];
-              cout <<   ")." << endl;
-            }
-            else {
-              cout <<"Maximum residual point " << iPointMaxResid << ", located at (" << Coord[0]*12.0 << ", " << Coord[1]*12.0;
-              if (nDim == 3) cout << ", " << Coord[2]*12.0;
-              cout <<   ")." << endl;
-            }
-
-            /*--- Print out the number of non-physical points and reconstructions ---*/
-
-            if (config[val_iZone]->GetNonphysical_Points() > 0)
-              cout << "There are " << config[val_iZone]->GetNonphysical_Points() << " non-physical points in the solution." << endl;
-            if (config[val_iZone]->GetNonphysical_Reconstr() > 0)
-              cout << "There are " << config[val_iZone]->GetNonphysical_Reconstr() << " non-physical states in the upwind reconstruction." << endl;
-
-            cout << "-------------------------------------------------------------------------" << endl;
-
-            if (!Unsteady) cout << endl << " Iter" << "    Time(s)";
-            else cout << endl << " IntIter" << " ExtIter";
-
-            //            if (!fluid_structure) {
-              if (incompressible && !weakly_coupled_heat) {
-              if (energy) {cout << "   Res[Press]" << "     Res[Temp]" << "   CLift(Total)" << "   CDrag(Total)" << endl;}
-              else {cout << "   Res[Press]" << "     Res[Velx]" << "   CLift(Total)" << "   CDrag(Total)" << endl;}
-              }
-              else if (incompressible && weakly_coupled_heat) cout << "   Res[Press]" << "     Res[Heat]" << "   HFlux(Total)";
-            else if (rotating_frame && nDim == 3 && !turbo) cout << "     Res[Rho]" << "     Res[RhoE]" << " CThrust(Total)" << " CTorque(Total)" << endl;
-            else if (aeroelastic) cout << "     Res[Rho]" << "     Res[RhoE]" << "   CLift(Total)" << "   CDrag(Total)" << "         plunge" << "          pitch" << endl;
-            else if (equiv_area) cout << "     Res[Rho]" << "   CLift(Total)" << "   CDrag(Total)" << "    CPress(N-F)" << endl;
-
-            else if (turbo){
-
-              if(nZone  < 2){
-                /*--- single zone output ---*/
-                cout << "     Res[Rho]" << "     Res[RhoE]"  << "  TotPresLoss(%)" << "  Entropy Gen.(%)";
-              }
-              else{
-                /* --- multi-zone output ---*/
-                cout << "     Res[Rho]" << "     Res[RhoE]"  << " TTEfficiency(%)" << " Entropy Gen.(%)";
-              }
-            }
-
-            else if (actuator_disk) cout << "     Res[Rho]" << "     Res[RhoE]" << "      CL(Total)" << "   CD-CT(Total)";
-            else if (engine) cout << "     Res[Rho]" << "     Res[RhoE]" << "      CL(Total)" << "   CD-CT(Total)";
-            else cout << "     Res[Rho]" << "     Res[RhoE]" << "      CL(Total)" << "      CD(Total)";
-
-            if(extra_heat_output) {
-              cout <<  "     Res[Heat]" << "   HFlux(Total)";
-            }
-
-            if (radiation){
-              cout << "     Res[P1-RAD]";
-            }
-
-            cout << endl;
-
-            break;
-
-          case MAIN_SOLVER::RANS : case MAIN_SOLVER::INC_RANS:
-
-            /*--- Visualize the maximum residual ---*/
-            iPointMaxResid = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetPoint_Max(0);
-            Coord = solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetPoint_Max_Coord(0);
-
-            cout << endl << "----------------------- Residual Evolution Summary ----------------------" << endl;
-
-            cout << "log10[Maximum residual]: " << log10(solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetRes_Max(0)) << "." << endl;
-            if (config[val_iZone]->GetSystemMeasurements() == SI) {
-              cout <<"Maximum residual point " << iPointMaxResid << ", located at (" << Coord[0] << ", " << Coord[1];
-              if (nDim == 3) cout << ", " << Coord[2];
-              cout <<   ")." << endl;
-            }
-            else {
-              cout <<"Maximum residual point " << iPointMaxResid << ", located at (" << Coord[0]*12.0 << ", " << Coord[1]*12.0;
-              if (nDim == 3) cout << ", " << Coord[2]*12.0;
-              cout <<   ")." << endl;
-            }
-            cout <<"Maximum Omega " << solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetOmega_Max() << ", maximum Strain Rate " << solver_container[val_iZone][val_iInst][FinestMesh][FLOW_SOL]->GetStrainMag_Max() << "." << endl;
-
-            /*--- Print out the number of non-physical points and reconstructions ---*/
-            if (config[val_iZone]->GetNonphysical_Points() > 0)
-              cout << "There are " << config[val_iZone]->GetNonphysical_Points() << " non-physical points in the solution." << endl;
-            if (config[val_iZone]->GetNonphysical_Reconstr() > 0)
-              cout << "There are " << config[val_iZone]->GetNonphysical_Reconstr() << " non-physical states in the upwind reconstruction." << endl;
-
-            cout << "-------------------------------------------------------------------------" << endl;
-
-            if (!Unsteady) cout << endl << " Iter" << "    Time(s)";
-            else cout << endl << " IntIter" << " ExtIter";
-            if (incompressible) cout << "   Res[Press]";
-            else cout << "      Res[Rho]";//, cout << "     Res[RhoE]";
-
-            switch (config[val_iZone]->GetKind_Turb_Model()) {
-              case TURB_MODEL::SA: cout << "       Res[nu]"; break;
-              case TURB_MODEL::SST: cout << "     Res[kine]" << "    Res[omega]"; break;
-              default: break;
-            }
-
-            if (weakly_coupled_heat) {
-              cout <<  "     Res[Heat]";
-            }
-
-            if (transition) { cout << "      Res[Int]" << "       Res[Re]"; }
-            else if (rotating_frame && nDim == 3 && !turbo ) cout << "   CThrust(Total)" << "   CTorque(Total)";
-            else if (aeroelastic) cout << "   CLift(Total)" << "   CDrag(Total)" << "         plunge" << "          pitch";
-            else if (equiv_area) cout << "   CLift(Total)" << "   CDrag(Total)" << "    CPress(N-F)";
-            else if (turbo){
-              if (nZone < 2){
-                /*--- single zone output ---*/
-                cout << "  TotPresLoss(%)" << "  Entropy Gen.(%)";
-              }
-              else{
-                /*--- multi zone output ---*/
-                cout << " TTEfficiency(%)" << " Entropy Gen.(%)";
-
-              }
-            }
-            else if (weakly_coupled_heat) {
-              cout << "   HFlux(Total)";
-            }
-            else cout << "   CLift(Total)"   << "   CDrag(Total)";
-
-            if(extra_heat_output) {
-              cout <<  "      Res[Heat]" << "   HFlux(Total)";
-            }
-
-            if (radiation){
-              cout << "     Res[P1-RAD]";
-            }
-
-            cout << endl;
-
-            break;
-
-            case MAIN_SOLVER::HEAT_EQUATION :
-              if (!Unsteady) cout << endl << " Iter" << "    Time(s)";
-              else cout << endl << " IntIter" << "  ExtIter";
-
-              cout <<  "      Res[Heat]" << "   HFlux(Total)";
-              break;
-
-            case MAIN_SOLVER::FEM_ELASTICITY :
-              if (!nonlinear_analysis) cout << endl << " Iter" << "    Time(s)";
-              else cout << endl << " IntIter" << " ExtIter";
-
-              if (linear_analysis) {
-                if (nDim == 2) cout << "    Res[Displx]" << "    Res[Disply]" << "      VMS(Max)"<<  endl;
-                if (nDim == 3) cout << "    Res[Displx]" << "    Res[Disply]" << "    Res[Displz]" << "      VMS(Max)"<<  endl;
-              }
-              else if (nonlinear_analysis) {
-                cout << "     Res[UTOL]" << "     Res[RTOL]" << "     Res[ETOL]"  << "      VMS(Max)"<<  endl;
-              }
-            break;
-
-            case MAIN_SOLVER::ADJ_EULER :              case MAIN_SOLVER::ADJ_NAVIER_STOKES :
-            case MAIN_SOLVER::DISC_ADJ_EULER:          case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES:
-            case MAIN_SOLVER::DISC_ADJ_INC_EULER:      case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES:
-
-              /*--- Visualize the maximum residual ---*/
-              iPointMaxResid = solver_container[val_iZone][val_iInst][FinestMesh][ADJFLOW_SOL]->GetPoint_Max(0);
-              Coord = solver_container[val_iZone][val_iInst][FinestMesh][ADJFLOW_SOL]->GetPoint_Max_Coord(0);
-              cout << endl << "log10[Maximum residual]: " << log10(solver_container[val_iZone][val_iInst][FinestMesh][ADJFLOW_SOL]->GetRes_Max(0)) << "." << endl;
-              if (config[val_iZone]->GetSystemMeasurements() == SI) {
-                cout <<"Maximum residual point " << iPointMaxResid << ", located at (" << Coord[0] << ", " << Coord[1];
-                if (nDim == 3) cout << ", " << Coord[2];
-                cout <<   ")." << endl;
-              }
-              else {
-                cout <<"Maximum residual point " << iPointMaxResid << ", located at (" << Coord[0]*12.0 << ", " << Coord[1]*12.0;
-                if (nDim == 3) cout << ", " << Coord[2]*12.0;
-                cout <<   ")." << endl;
-              }
-
-              /*--- Print out the number of non-physical points and reconstructions ---*/
-              if (config[val_iZone]->GetNonphysical_Points() > 0)
-                cout << "There are " << config[val_iZone]->GetNonphysical_Points() << " non-physical points in the solution." << endl;
-
-              if (!Unsteady) cout << endl << " Iter" << "    Time(s)";
-              else cout << endl << " IntIter" << "  ExtIter";
-
-              if (incompressible) {
-                if (energy) {cout << "   Res[Psi_Press]" << "   Res[Psi_Temp]";}
-                else {cout << "   Res[Psi_Press]" << "   Res[Psi_Velx]";}
-              }
-              else cout << "   Res[Psi_Rho]" << "     Res[Psi_E]";
-
-              if (radiation){
-                cout << "     Res[Psi_P1]";
-              }
-
-              if (disc_adj) {
-                if (!turbo){
-                  if (compressible) {
-                    cout << "    Sens_Press" << "      Sens_AoA" << endl;
-                  }
-                  if (incompressible) {
-                    if (energy) {
-                      cout << "      Sens_Vin" << "     Sens_Temp" << endl;
-                    } else {
-                      cout << "      Sens_Vin" << "     Sens_Pout" << endl;
-                    }
-                  }                } else {
-                  cout << " Sens_PressOut" << " Sens_TotTempIn" << endl;
-                }
-              } else {
-                cout << "      Sens_Geo" << "      Sens_AoA" << endl;
-              }
-              break;
-
-            case MAIN_SOLVER::ADJ_RANS : case MAIN_SOLVER::DISC_ADJ_RANS: case MAIN_SOLVER::DISC_ADJ_INC_RANS:
-
-              /*--- Visualize the maximum residual ---*/
-              iPointMaxResid = solver_container[val_iZone][val_iInst][FinestMesh][ADJFLOW_SOL]->GetPoint_Max(0);
-              Coord = solver_container[val_iZone][val_iInst][FinestMesh][ADJFLOW_SOL]->GetPoint_Max_Coord(0);
-              cout << endl << "log10[Maximum residual]: " << log10(solver_container[val_iZone][val_iInst][FinestMesh][ADJFLOW_SOL]->GetRes_Max(0)) << "." << endl;
-              if (config[val_iZone]->GetSystemMeasurements() == SI) {
-                cout <<"Maximum residual point " << iPointMaxResid << ", located at (" << Coord[0] << ", " << Coord[1];
-                if (nDim == 3) cout << ", " << Coord[2];
-                cout <<   ")." << endl;
-              }
-              else {
-                cout <<"Maximum residual point " << iPointMaxResid << ", located at (" << Coord[0]*12.0 << ", " << Coord[1]*12.0;
-                if (nDim == 3) cout << ", " << Coord[2]*12.0;
-                cout <<   ")." << endl;
-              }
-
-              /*--- Print out the number of non-physical points and reconstructions ---*/
-              if (config[val_iZone]->GetNonphysical_Points() > 0)
-                cout << "There are " << config[val_iZone]->GetNonphysical_Points() << " non-physical points in the solution." << endl;
-
-              if (!Unsteady) cout << endl << " Iter" << "    Time(s)";
-              else cout << endl << " IntIter" << "  ExtIter";
-
-              if (incompressible) cout << "     Res[Psi_Press]";
-              else cout << "     Res[Psi_Rho]";
-
-              if (!frozen_visc) {
-                cout << " Res[Psi_Turb[0]]";
-              }
-              else {
-                if (incompressible) {if (energy) {cout << "   Res[Psi_Temp]";}
-                  else {cout << "   Res[Psi_Velx]";}}
-                else cout << "     Res[Psi_E]";
-              }
-              if (weakly_coupled_heat) {
-                cout << "     Res[Psi_E]";
-              }
-              if (radiation){
-                cout << "    Res[Psi_P1]";
-              }
-              if (disc_adj) {
-                if (!turbo){
-                  if (compressible) {
-                  cout << "    Sens_Press" << "      Sens_AoA" << endl;
-                  }
-                  if (incompressible) {
-                    cout << "      Sens_Vin" << "     Sens_Pout" << endl;
-                  }
-                } else {
-                  cout << " Sens_PressOut" << " Sens_TotTempIn" << endl;                }
-              } else {
-                cout << "      Sens_Geo" << "      Sens_AoA" << endl;
-              }
-              break;
-
-            case MAIN_SOLVER::DISC_ADJ_FEM :
-              cout << endl << " IntIter" << " ExtIter";
-
-              if (nDim == 2) cout << "    Res[Ux_adj]" << "    Res[Uy_adj]" << "       Sens[E]" << "      Sens[Nu]"<<  endl;
-              if (nDim == 3) cout << "    Res[Ux_adj]" << "    Res[Uy_adj]" << "    Res[Uz_adj]" << "       Sens[E]" << "      Sens[Nu]"<<  endl;
-
-           break;
-
-          default:
-            break;
-          }
-        }
-      }
-
-      /*--- Write the solution on the screen ---*/
-
-      if ((val_iZone == 0 && val_iInst == 0)|| fluid_structure){
-        cout.precision(6);
-        cout.setf(ios::fixed, ios::floatfield);
-        if (!fem) {
-          if (!Unsteady) {
-            cout.width(5); cout << iExtIter + ExtIter_OffSet;
-            cout.width(11); cout << timeiter;
-
-          } else if (Unsteady && DualTime_Iteration) {
-            cout.width(8); cout << iIntIter;
-            cout.width(8); cout << iExtIter;
-          }
-        }
-        else if (fem) {
-          if (!DualTime_Iteration) {
-            if (!nonlinear_analysis) {
-              cout.width(5); cout << iExtIter;
-              cout.width(11); cout << timeiter;
-
-            } else {
-              cout.width(8); cout << iIntIter;
-              cout.width(8); cout << iExtIter;
-            }
-          }
-          else if (discadj_fem){
-              cout.width(8); cout << iIntIter;
-              cout.width(8); cout << iExtIter;
-          }
-        }
-      }
-
-      switch (config[val_iZone]->GetKind_Solver()) {
-        case MAIN_SOLVER::EULER : case MAIN_SOLVER::NAVIER_STOKES:
-        case MAIN_SOLVER::INC_EULER : case MAIN_SOLVER::INC_NAVIER_STOKES:
-        case MAIN_SOLVER::FEM_EULER : case MAIN_SOLVER::FEM_NAVIER_STOKES: case MAIN_SOLVER::FEM_LES:
-
-          /*--- Write history file ---*/
-
-          if ((!DualTime_Iteration) && (output_files)) {
-            if (!turbo) {
-              ConvHist_file[0] << begin << direct_coeff;
-              if (buffet) ConvHist_file[0] << buffet_coeff;
-              if (thermal) ConvHist_file[0] << heat_coeff;
-              if (equiv_area) ConvHist_file[0] << equivalent_area_coeff;
-              if (engine || actuator_disk) ConvHist_file[0] << engine_coeff;
-              if (inv_design) {
-                ConvHist_file[0] << Cp_inverse_design;
-                if (thermal) ConvHist_file[0] << Heat_inverse_design;
-              }
-              if (rotating_frame && !turbo) ConvHist_file[0] << rotating_frame_coeff;
-              ConvHist_file[0] << flow_resid;
-              if (weakly_coupled_heat) ConvHist_file[0] << heat_resid;
-              if (radiation) ConvHist_file[0] << rad_resid;
-            }
-            else {
-              ConvHist_file[0] << begin << turbo_coeff << flow_resid;
-            }
-
-            if (aeroelastic) ConvHist_file[0] << aeroelastic_coeff;
-            if (output_per_surface) ConvHist_file[0] << monitoring_coeff;
-            if (output_surface) ConvHist_file[0] << surface_outputs;
-            if (direct_diff != NO_DERIVATIVE) {
-              ConvHist_file[0] << d_direct_coeff;
-              if (output_surface) ConvHist_file[0] << d_surface_outputs;
-            }
-            if (output_comboObj) ConvHist_file[0] << combo_obj;
-            ConvHist_file[0] << end;
-            ConvHist_file[0].flush();
-          }
-
-          /*--- Write screen output ---*/
-          if ((val_iZone == 0 && val_iInst == 0)|| fluid_structure) {
-            if(DualTime_Iteration || !Unsteady) {
-              cout.precision(6);
-              cout.setf(ios::fixed, ios::floatfield);
-              cout.width(13); cout << log10(residual_flow[0]);
-              if (!equiv_area) {
-                if (compressible) {
-                  if (nDim == 2 ) { cout.width(14); cout << log10(residual_flow[3]); }
-                  else { cout.width(14); cout << log10(residual_flow[4]); }
-                }
-                if (incompressible && !weakly_coupled_heat) {
-                  if (energy) {cout.width(14); cout << log10(residual_flow[nDim+1]);}
-                  else {cout.width(14); cout << log10(residual_flow[1]);}
-                }
-                if (incompressible && weakly_coupled_heat)  { cout.width(14); cout << log10(residual_heat[0]);}
-
-              }
-
-              if (rotating_frame && nDim == 3 && !turbo ) {
-                cout.setf(ios::scientific, ios::floatfield);
-                cout.width(15); cout << Total_CT;
-                cout.width(15); cout << Total_CQ;
-                cout.unsetf(ios_base::floatfield);
-              }
-              else if (equiv_area) { cout.width(15); cout << min(10000.0, max(-10000.0, Total_CL)); cout.width(15); cout << min(10000.0, max(-10000.0, Total_CD)); cout.width(15);
-              cout.precision(4);
-              cout.setf(ios::scientific, ios::floatfield);
-              cout << Total_CNearFieldOF; }
-              else if (turbo) {
-                cout.setf(ios::scientific, ios::floatfield);
-
-                if (nZone < 2) {
-                  cout.width(15); cout << TotalPressureLoss[0][nSpanWiseSections]*100.0;
-                  cout.width(15); cout << EntropyGen[0][nSpanWiseSections]*100.0;
-                }
-                else {
-                  cout.width(15); cout << TotalTotalEfficiency[nTurboPerf -1][nSpanWiseSections]*100.0;
-                  cout.width(15); cout << EntropyGen[nTurboPerf -1][nSpanWiseSections]*100.0;
-                }
-
-                cout.unsetf(ios_base::floatfield);
-
-              }
-              else if (weakly_coupled_heat) { cout.width(14); cout << log10(Total_Heat); }
-              else { cout.width(15); cout << min(10000.0, max(-10000.0, Total_CL)); cout.width(15); cout << min(10000.0, max(-10000.0, Total_CD)); }
-              if (aeroelastic) {
-                cout.setf(ios::scientific, ios::floatfield);
-                cout.width(15); cout << aeroelastic_plunge[0]; //Only output the first marker being monitored to the console.
-                cout.width(15); cout << aeroelastic_pitch[0];
-                cout.unsetf(ios_base::floatfield);
-              }
-
-              if (extra_heat_output) { cout.width(15); cout << Extra_Heat_Residual; cout.width(15); cout << Extra_Total_Heat; }
-              if (radiation) { cout.width(15); cout << log10(residual_rad[0]); }
-            }
-            cout << endl;
-          }
-          break;
-
-        case MAIN_SOLVER::RANS : case MAIN_SOLVER::INC_RANS:
-
-          /*--- Write history file ---*/
-
-          if ((!DualTime_Iteration) && (output_files)) {
-
-            if (!turbo) {
-              ConvHist_file[0] << begin << direct_coeff;
-              if (buffet) ConvHist_file[0] << buffet_coeff;
-              if (thermal) ConvHist_file[0] << heat_coeff;
-              if (equiv_area) ConvHist_file[0] << equivalent_area_coeff;
-              if (engine || actuator_disk) ConvHist_file[0] << engine_coeff;
-              if (inv_design) {
-                ConvHist_file[0] << Cp_inverse_design;
-                if (thermal) ConvHist_file[0] << Heat_inverse_design;
-              }
-              if (rotating_frame && !turbo) ConvHist_file[0] << rotating_frame_coeff;
-              ConvHist_file[0] << flow_resid << turb_resid;
-              if (weakly_coupled_heat) ConvHist_file[0] << heat_resid;
-            }
-            else {
-              ConvHist_file[0] << begin << turbo_coeff << flow_resid << turb_resid;
-            }
-
-            if (aeroelastic) ConvHist_file[0] << aeroelastic_coeff;
-            if (output_per_surface) ConvHist_file[0] << monitoring_coeff;
-            if (output_surface) ConvHist_file[0] << surface_outputs;
-            if (direct_diff != NO_DERIVATIVE) {
-              ConvHist_file[0] << d_direct_coeff;
-              if (output_surface) ConvHist_file[0] << d_surface_outputs;
-            }
-            if (output_comboObj) ConvHist_file[0] << combo_obj;
-            ConvHist_file[0] << end;
-            ConvHist_file[0].flush();
-          }
-
-          /*--- Write screen output ---*/
-
-          if ((val_iZone == 0 && val_iInst == 0)|| fluid_structure){
-            if(DualTime_Iteration || !Unsteady) {
-              cout.precision(6);
-              cout.setf(ios::fixed, ios::floatfield);
-
-              if (incompressible) cout.width(13);
-              else  cout.width(14);
-              cout << log10(residual_flow[0]);
-              switch(nVar_Turb) {
-              case 1: cout.width(14); cout << log10(residual_turbulent[0]); break;
-              case 2: cout.width(14); cout << log10(residual_turbulent[0]);
-              cout.width(15); cout << log10(residual_turbulent[1]); break;
-              }
-
-              if (weakly_coupled_heat) {
-                cout.width(14); cout << log10(residual_heat[0]);
-              }
-
-              if (transition) { cout.width(14); cout << log10(residual_transition[0]); cout.width(14); cout << log10(residual_transition[1]); }
-
-              if (rotating_frame && nDim == 3 && !turbo ) {
-                cout.setf(ios::scientific, ios::floatfield);
-                cout.width(15); cout << Total_CT; cout.width(15);
-                cout << Total_CQ;
-                cout.unsetf(ios_base::floatfield);
-              }
-              else if (equiv_area) { cout.width(15); cout << min(10000.0, max(-10000.0, Total_CL)); cout.width(15); cout << min(10000.0, max(-10000.0, Total_CD)); cout.width(15);
-              cout.precision(4);
-              cout.setf(ios::scientific, ios::floatfield);
-              cout << Total_CNearFieldOF; }
-              else if (turbo) {
-                cout.setf(ios::scientific, ios::floatfield);
-                if (nZone < 2){
-                  /*--- single zone output ---*/
-                  cout.width(15); cout << TotalPressureLoss[0][nSpanWiseSections]*100.0;
-                  cout.width(15); cout << EntropyGen[0][nSpanWiseSections]*100.0;
-                }
-                else{
-                  /*--- multi zone output ---*/
-                  cout.width(15); cout << TotalTotalEfficiency[nTurboPerf - 1][nSpanWiseSections]*100.0;
-                  cout.width(15); cout << EntropyGen[nTurboPerf -1][nSpanWiseSections]*100.0;
-                  if (direct_diff){
-                    cout.width(15); cout << D_EntropyGen;
-                  }
-                }
-                cout.unsetf(ios_base::floatfield);
-              }
-              else if (weakly_coupled_heat) { cout.width(15); cout << Total_Heat; }
-              else { cout.width(15); cout << min(10000.0, max(-10000.0, Total_CL)); cout.width(15); cout << min(10000.0, max(-10000.0, Total_CD)); }
-
-              if (aeroelastic) {
-                cout.setf(ios::scientific, ios::floatfield);
-                cout.width(15); cout << aeroelastic_plunge[0]; //Only output the first marker being monitored to the console.
-                cout.width(15); cout << aeroelastic_pitch[0];
-                cout.unsetf(ios_base::floatfield);
-              }
-
-              if (extra_heat_output) { cout.width(15); cout << Extra_Heat_Residual; cout.width(15); cout << Extra_Total_Heat; }
-              cout << endl;
-            }
-          }
-          break;
-
-
-        case MAIN_SOLVER::HEAT_EQUATION:
-
-          if (!DualTime_Iteration) {
-            ConvHist_file[0] << begin << direct_coeff << heat_resid << end;
-            ConvHist_file[0].flush();
-          }
-          break;
-
-        case MAIN_SOLVER::FEM_ELASTICITY:
-
-          if (!DualTime_Iteration) {
-            ConvHist_file[0] << begin << fem_coeff << fem_resid << end_fem;
-            ConvHist_file[0].flush();
-
-          cout.precision(6);
-          cout.setf(ios::fixed, ios::floatfield);
-          if (linear_analysis) {
-            cout.width(14); cout << log10(residual_fem[0]);
-            cout.width(14); cout << log10(residual_fem[1]);
-            if (nDim == 3) { cout.width(14); cout << log10(residual_fem[2]); }
-          }
-          else if (nonlinear_analysis) {
-            cout.width(14); cout << log10(residual_fem[0]);
-            cout.width(14); cout << log10(residual_fem[1]);
-            cout.width(14); cout << log10(residual_fem[2]);
-          }
-
-          cout.precision(4);
-          cout.setf(ios::scientific, ios::floatfield);
-          cout.width(14); cout << Total_VMStress;
-          cout << endl;
-          }
-          break;
-
-        case MAIN_SOLVER::DISC_ADJ_FEM:
-
-          cout.precision(6);
-          cout.setf(ios::fixed, ios::floatfield);
-
-          cout.width(15); cout << log10(residual_fem[0]);
-          cout.width(15); cout << log10(residual_fem[1]);
-          if (nDim == 3) { cout.width(15); cout << log10(residual_fem[2]); }
-
-          cout.precision(4);
-          cout.setf(ios::scientific, ios::floatfield);
-
-
-          if (config[val_iZone]->GetnElasticityMod() == 1){
-            cout.width(14); cout << solver_container[val_iZone][val_iInst][FinestMesh][ADJFEA_SOL]->GetGlobal_Sens_E(0);
-            cout.width(14); cout << solver_container[val_iZone][val_iInst][FinestMesh][ADJFEA_SOL]->GetGlobal_Sens_Nu(0);
-          }
-          else{
-            Total_SensE = 0.0; Total_SensNu = 0.0;
-            for (unsigned short iVar = 0; iVar < config[val_iZone]->GetnElasticityMod(); iVar++){
-                Total_SensE += solver_container[val_iZone][val_iInst][FinestMesh][ADJFEA_SOL]->GetGlobal_Sens_E(0)
-                    *solver_container[val_iZone][val_iInst][FinestMesh][ADJFEA_SOL]->GetGlobal_Sens_E(0);
-                Total_SensNu += solver_container[val_iZone][val_iInst][FinestMesh][ADJFEA_SOL]->GetGlobal_Sens_Nu(0)
-                    *solver_container[val_iZone][val_iInst][FinestMesh][ADJFEA_SOL]->GetGlobal_Sens_Nu(0);
-            }
-            Total_SensE = sqrt(Total_SensE);
-            Total_SensNu = sqrt(Total_SensNu);
-            cout.width(14); cout << Total_SensE;
-            cout.width(14); cout << Total_SensNu;
-          }
-
-          cout << endl;
-          break;
-
-        case MAIN_SOLVER::ADJ_EULER :              case MAIN_SOLVER::ADJ_NAVIER_STOKES :
-        case MAIN_SOLVER::DISC_ADJ_EULER:          case MAIN_SOLVER::DISC_ADJ_NAVIER_STOKES:
-        case MAIN_SOLVER::DISC_ADJ_INC_EULER:      case MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES:
-
-          if (!DualTime_Iteration) {
-            ConvHist_file[0] << begin << adjoint_coeff << adj_flow_resid << end;
-            ConvHist_file[0].flush();
-          }
-          if ((val_iZone == 0 && val_iInst == 0)|| fluid_structure){
-            if (DualTime_Iteration || !Unsteady){
-              cout.precision(6);
-              cout.setf(ios::fixed, ios::floatfield);
-              if (compressible) {
-                cout.width(15); cout << log10(residual_adjflow[0]);
-                cout.width(15); cout << log10(residual_adjflow[nDim+1]);
-              }
-              if (incompressible) {
-                cout.width(17); cout << log10(residual_adjflow[0]);
-                if (energy) {cout.width(16); cout << log10(residual_adjflow[nDim+1]);}
-                else {cout.width(16); cout << log10(residual_adjflow[1]);}
-              }
-
-              if (radiation) { cout.width(15); cout << log10(residual_rad[0]); }
-
-              if (disc_adj) {
-                cout.precision(4);
-                cout.setf(ios::scientific, ios::floatfield);
-                if (!turbo){
-                  if (compressible) {
-                  cout.width(14); cout << Total_Sens_Press;
-                  cout.width(14); cout << Total_Sens_AoA;
-                  }
-                  if (incompressible) {
-                    cout.width(14); cout << Total_Sens_ModVel;
-                    if (energy) {
-                      cout.width(14); cout << Total_Sens_Temp;
-                    } else {
-                      cout.width(14); cout << Total_Sens_BPressure;
-                    }
-                  }
-                } else {
-                  cout.width(14); cout << Total_Sens_BPressure;
-                  cout.width(15); cout << Total_Sens_Temp;
-                }
-              }else {
-                cout.precision(4);
-                cout.setf(ios::scientific, ios::floatfield);
-                cout.width(14); cout << Total_Sens_Geo;
-                cout.width(14); cout << Total_Sens_AoA;
-              }
-              cout << endl;
-              cout.unsetf(ios_base::floatfield);
-            }
-          }
-          break;
-
-        case MAIN_SOLVER::ADJ_RANS : case MAIN_SOLVER::DISC_ADJ_RANS: case MAIN_SOLVER::DISC_ADJ_INC_RANS:
-
-          if (!DualTime_Iteration) {
-            ConvHist_file[0] << begin << adjoint_coeff << adj_flow_resid;
-            if (!frozen_visc)
-              ConvHist_file[0] << adj_turb_resid;
-            ConvHist_file[0] << end;
-            ConvHist_file[0].flush();
-          }
-          if ((val_iZone == 0 && val_iInst == 0)|| fluid_structure){
-            if (DualTime_Iteration || !Unsteady){
-              cout.precision(6);
-              cout.setf(ios::fixed, ios::floatfield);
-              cout.width(17); cout << log10(residual_adjflow[0]);
-            if (!frozen_visc) {
-                cout.width(17); cout << log10(residual_adjturbulent[0]);
-              }
-              else {
-                if (compressible) {
-                  if (geometry[val_iZone][val_iInst][FinestMesh]->GetnDim() == 2 ) { cout.width(15); cout << log10(residual_adjflow[3]); }
-                  else { cout.width(15); cout << log10(residual_adjflow[4]); }
-                }
-                if (incompressible) {
-                  if (energy) {cout.width(15); cout << log10(residual_adjflow[nDim+1]);}
-                  else {cout.width(15); cout << log10(residual_adjflow[1]);}
-                }
-              }
-            if (weakly_coupled_heat) {
-              cout.width(17); cout << log10(residual_adjheat[0]);
-            }
-
-            if (radiation) { cout.width(15); cout << log10(residual_rad[0]); }
-
-              if (disc_adj) {
-                if (!turbo){
-                  if (compressible) {
-                  cout.width(14); cout << Total_Sens_Press;
-                  cout.width(14); cout << Total_Sens_AoA;
-                  }
-                  if (incompressible) {
-                    cout.width(14); cout << Total_Sens_ModVel;
-                    if (energy) {
-                      cout.width(14); cout << Total_Sens_Temp;
-                    } else {
-                      cout.width(14); cout << Total_Sens_BPressure;
-                    }                  }
-                } else {
-                  cout.width(14); cout << Total_Sens_BPressure;
-                  cout.width(15); cout << Total_Sens_Temp;
-                }
-              }else {
-                cout.precision(4);
-                cout.setf(ios::scientific, ios::floatfield);
-                cout.width(14); cout << Total_Sens_Geo;
-                cout.width(14); cout << Total_Sens_AoA;
-              }
-              cout << endl;
-              cout.unsetf(ios_base::floatfield);
-            }
-          }
-          break;
-
-        default:
-          break;
-      }
-      cout.unsetf(ios::fixed);
-
-    }
-
-
-    delete [] residual_flow;
-    delete [] residual_turbulent;
-    delete [] residual_transition;
-    delete [] residual_fea;
-    delete [] residual_fem;
-    delete [] residual_heat;
-    delete [] residual_rad;
-
-    delete [] residual_adjflow;
-    delete [] residual_adjturbulent;
-
-    delete [] Surface_CL;
-    delete [] Surface_CD;
-    delete [] Surface_CSF;
-    delete [] Surface_CEff;
-    delete [] Surface_CFx;
-    delete [] Surface_CFy;
-    delete [] Surface_CFz;
-    delete [] Surface_CMx;
-    delete [] Surface_CMy;
-    delete [] Surface_CMz;
-    delete [] aeroelastic_pitch;
-    delete [] aeroelastic_plunge;
-
-  }
-}
-
-void COutputLegacy::SpecialOutputForcesBreakdown(CSolver *****solver, CGeometry ****geometry, CConfig **config, unsigned short val_iZone, bool output) const {
-
-  char cstr[200];
-  unsigned short iDim, iMarker_Monitoring;
-  ofstream Breakdown_file;
-
-  bool compressible       = (config[val_iZone]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
-  bool incompressible     = (config[val_iZone]->GetKind_Regime() == ENUM_REGIME::INCOMPRESSIBLE);
-  bool unsteady           = (config[val_iZone]->GetTime_Marching() != TIME_MARCHING::STEADY);
-  bool viscous            = config[val_iZone]->GetViscous();
-  bool dynamic_grid       = config[val_iZone]->GetDynamic_Grid();
-  bool gravity            = config[val_iZone]->GetGravityForce();
-  bool turbulent          = config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::RANS;
-  bool fixed_cl           = config[val_iZone]->GetFixed_CL_Mode();
-  MAIN_SOLVER Kind_Solver = config[val_iZone]->GetKind_Solver();
-  TURB_MODEL Kind_Turb_Model = config[val_iZone]->GetKind_Turb_Model();
-  unsigned short Ref_NonDim = config[val_iZone]->GetRef_NonDim();
-
-  unsigned short FinestMesh = config[val_iZone]->GetFinestMesh();
-  unsigned short nDim = geometry[val_iZone][INST_0][FinestMesh]->GetnDim();
-  bool flow = ((config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::EULER) ||
-               (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::NAVIER_STOKES) ||
-               (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::RANS) ||
-               (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::INC_EULER) ||
-               (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::INC_NAVIER_STOKES) ||
-               (config[val_iZone]->GetKind_Solver() == MAIN_SOLVER::INC_RANS));
-
-  /*--- Output the mean flow solution using only the master node ---*/
-
-  if ((rank == MASTER_NODE) && (flow) && (output)) {
-
-    cout << endl << "Writing the forces breakdown file ("<< config[val_iZone]->GetBreakdown_FileName() << ")." << endl;
-
-    /*--- Initialize variables to store information from all domains (direct solution) ---*/
-
-    su2double Total_CL = 0.0, Total_CD = 0.0, Total_CSF = 0.0,
-    Total_CMx = 0.0, Total_CMy = 0.0, Total_CMz = 0.0, Total_CEff = 0.0,
-    Total_CoPx = 0.0, Total_CoPy = 0.0, Total_CoPz = 0.0,
-    Total_CFx = 0.0, Total_CFy = 0.0, Total_CFz = 0.0, Inv_CL = 0.0,
-    Inv_CD = 0.0, Inv_CSF = 0.0, Inv_CMx = 0.0, Inv_CMy = 0.0,
-    Inv_CMz = 0.0, Inv_CEff = 0.0, Inv_CFx = 0.0, Inv_CFy = 0.0, Inv_CFz =
-    0.0,      Mnt_CL = 0.0,
-    Mnt_CD = 0.0, Mnt_CSF = 0.0, Mnt_CMx = 0.0, Mnt_CMy = 0.0,
-    Mnt_CMz = 0.0, Mnt_CEff = 0.0, Mnt_CFx = 0.0, Mnt_CFy = 0.0, Mnt_CFz =
-    0.0, Visc_CL = 0.0,
-    Visc_CD = 0.0, Visc_CSF = 0.0, Visc_CMx = 0.0, Visc_CMy = 0.0,
-    Visc_CMz = 0.0, Visc_CEff = 0.0, Visc_CFx = 0.0, Visc_CFy = 0.0, Visc_CFz =
-    0.0, *Surface_CL = nullptr, *Surface_CD = nullptr,
-    *Surface_CSF = nullptr, *Surface_CEff = nullptr, *Surface_CFx = nullptr,
-    *Surface_CFy = nullptr, *Surface_CFz = nullptr,
-    *Surface_CMx = nullptr, *Surface_CMy = nullptr, *Surface_CMz = nullptr,
-    *Surface_CL_Inv = nullptr,
-    *Surface_CD_Inv = nullptr, *Surface_CSF_Inv = nullptr,
-    *Surface_CEff_Inv = nullptr, *Surface_CFx_Inv = nullptr, *Surface_CFy_Inv =
-    nullptr, *Surface_CFz_Inv = nullptr, *Surface_CMx_Inv = nullptr,
-    *Surface_CMy_Inv = nullptr, *Surface_CMz_Inv = nullptr,
-    *Surface_CL_Visc = nullptr,
-    *Surface_CD_Visc = nullptr, *Surface_CSF_Visc = nullptr,
-    *Surface_CEff_Visc = nullptr, *Surface_CFx_Visc = nullptr, *Surface_CFy_Visc =
-    nullptr, *Surface_CFz_Visc = nullptr, *Surface_CMx_Visc = nullptr,
-    *Surface_CMy_Visc = nullptr, *Surface_CMz_Visc = nullptr,
-    *Surface_CL_Mnt = nullptr,
-    *Surface_CD_Mnt = nullptr, *Surface_CSF_Mnt = nullptr,
-    *Surface_CEff_Mnt = nullptr, *Surface_CFx_Mnt = nullptr, *Surface_CFy_Mnt =
-    nullptr, *Surface_CFz_Mnt = nullptr, *Surface_CMx_Mnt = nullptr,
-    *Surface_CMy_Mnt = nullptr, *Surface_CMz_Mnt = nullptr;
-
-    /*--- Allocate memory for the coefficients being monitored ---*/
-
-    Surface_CL      = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CD      = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CSF = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CEff       = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CFx        = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CFy        = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CFz        = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CMx        = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CMy        = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CMz        = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-
-    Surface_CL_Inv      = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CD_Inv      = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CSF_Inv = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CEff_Inv       = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CFx_Inv        = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CFy_Inv        = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CFz_Inv        = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CMx_Inv        = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CMy_Inv        = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CMz_Inv        = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-
-    Surface_CL_Visc = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CD_Visc = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CSF_Visc =
-    new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CEff_Visc = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CFx_Visc = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CFy_Visc = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CFz_Visc = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CMx_Visc = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CMy_Visc = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CMz_Visc = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-
-
-    Surface_CL_Mnt = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CD_Mnt = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CSF_Mnt =
-    new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CEff_Mnt = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CFx_Mnt = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CFy_Mnt = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CFz_Mnt = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CMx_Mnt = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CMy_Mnt = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-    Surface_CMz_Mnt = new su2double[config[ZONE_0]->GetnMarker_Monitoring()];
-
-    /*--- Flow solution coefficients ---*/
-
-    Total_CL       = solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CL();
-    Total_CD       = solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CD();
-    Total_CSF      = solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CSF();
-    Total_CEff        = solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CEff();
-    Total_CMx         = solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMx();
-    Total_CMy         = solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMy();
-    Total_CMz         = solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CMz();
-    Total_CFx         = solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CFx();
-    Total_CFy         = solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CFy();
-    Total_CFz         = solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CFz();
-
-    if (nDim == 2) {
-      Total_CoPx = solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CoPx() / solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CFy();
-      Total_CoPy = solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CoPy() / solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CFx();
-      Total_CoPz = 0.0;
-    }
-    if (nDim == 3) {
-      Total_CoPx = solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CoPx() / solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CFz();
-      Total_CoPy = 0.0;
-      Total_CoPz = solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CoPz() / solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CFx();
-    }
-
-    if (config[ZONE_0]->GetSystemMeasurements() == US) { Total_CoPx *= 12.0; Total_CoPy *= 12.0; Total_CoPz *= 12.0; }
-
-    /*--- Flow inviscid solution coefficients ---*/
-
-    Inv_CL =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CL_Inv();
-    Inv_CD =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CD_Inv();
-    Inv_CSF =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CSF_Inv();
-    Inv_CEff =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CEff_Inv();
-    Inv_CMx =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CMx_Inv();
-    Inv_CMy =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CMy_Inv();
-    Inv_CMz =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CMz_Inv();
-    Inv_CFx =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CFx_Inv();
-    Inv_CFy =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CFy_Inv();
-    Inv_CFz =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CFz_Inv();
-
-    /*--- Flow viscous solution coefficients ---*/
-
-    Visc_CL =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CL_Visc();
-    Visc_CD =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CD_Visc();
-    Visc_CSF =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CSF_Visc();
-    Visc_CEff =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CEff_Visc();
-    Visc_CMx =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CMx_Visc();
-    Visc_CMy =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CMy_Visc();
-    Visc_CMz =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CMz_Visc();
-    Visc_CFx =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CFx_Visc();
-    Visc_CFy =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CFy_Visc();
-    Visc_CFz =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CFz_Visc();
-
-    /*--- Flow momentum solution coefficients ---*/
-
-    Mnt_CL =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CL_Mnt();
-    Mnt_CD =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CD_Mnt();
-    Mnt_CSF =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CSF_Mnt();
-    Mnt_CEff =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CEff_Mnt();
-    Mnt_CMx =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CMx_Mnt();
-    Mnt_CMy =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CMy_Mnt();
-    Mnt_CMz =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CMz_Mnt();
-    Mnt_CFx =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CFx_Mnt();
-    Mnt_CFy =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CFy_Mnt();
-    Mnt_CFz =
-    solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetAllBound_CFz_Mnt();
-
-
-    /*--- Look over the markers being monitored and get the desired values ---*/
-
-    for (iMarker_Monitoring = 0;
-         iMarker_Monitoring < config[ZONE_0]->GetnMarker_Monitoring();
-         iMarker_Monitoring++) {
-      Surface_CL[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CL(
-                                                             iMarker_Monitoring);
-      Surface_CD[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CD(
-                                                             iMarker_Monitoring);
-      Surface_CSF[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CSF(
-                                                              iMarker_Monitoring);
-      Surface_CEff[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CEff(
-                                                               iMarker_Monitoring);
-      Surface_CMx[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CMx(
-                                                              iMarker_Monitoring);
-      Surface_CMy[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CMy(
-                                                              iMarker_Monitoring);
-      Surface_CMz[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CMz(
-                                                              iMarker_Monitoring);
-      Surface_CFx[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CFx(
-                                                              iMarker_Monitoring);
-      Surface_CFy[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CFy(
-                                                              iMarker_Monitoring);
-      Surface_CFz[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CFz(
-                                                              iMarker_Monitoring);
-
-      Surface_CL_Inv[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CL_Inv(
-                                                                 iMarker_Monitoring);
-      Surface_CD_Inv[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CD_Inv(
-                                                                 iMarker_Monitoring);
-      Surface_CSF_Inv[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CSF_Inv(
-                                                                  iMarker_Monitoring);
-      Surface_CEff_Inv[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CEff_Inv(
-                                                                   iMarker_Monitoring);
-      Surface_CMx_Inv[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CMx_Inv(
-                                                                  iMarker_Monitoring);
-      Surface_CMy_Inv[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CMy_Inv(
-                                                                  iMarker_Monitoring);
-      Surface_CMz_Inv[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CMz_Inv(
-                                                                  iMarker_Monitoring);
-      Surface_CFx_Inv[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CFx_Inv(
-                                                                  iMarker_Monitoring);
-      Surface_CFy_Inv[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CFy_Inv(
-                                                                  iMarker_Monitoring);
-      Surface_CFz_Inv[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CFz_Inv(
-                                                                  iMarker_Monitoring);
-      Surface_CL_Visc[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CL_Visc(
-                                                                  iMarker_Monitoring);
-      Surface_CD_Visc[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CD_Visc(
-                                                                  iMarker_Monitoring);
-      Surface_CSF_Visc[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CSF_Visc(
-                                                                   iMarker_Monitoring);
-      Surface_CEff_Visc[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CEff_Visc(
-                                                                    iMarker_Monitoring);
-      Surface_CMx_Visc[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CMx_Visc(
-                                                                   iMarker_Monitoring);
-      Surface_CMy_Visc[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CMy_Visc(
-                                                                   iMarker_Monitoring);
-      Surface_CMz_Visc[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CMz_Visc(
-                                                                   iMarker_Monitoring);
-      Surface_CFx_Visc[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CFx_Visc(
-                                                                   iMarker_Monitoring);
-      Surface_CFy_Visc[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CFy_Visc(
-                                                                   iMarker_Monitoring);
-      Surface_CFz_Visc[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CFz_Visc(
-                                                                   iMarker_Monitoring);
-
-      Surface_CL_Mnt[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CL_Mnt(
-                                                                 iMarker_Monitoring);
-      Surface_CD_Mnt[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CD_Mnt(
-                                                                 iMarker_Monitoring);
-      Surface_CSF_Mnt[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CSF_Mnt(
-                                                                  iMarker_Monitoring);
-      Surface_CEff_Mnt[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CEff_Mnt(
-                                                                   iMarker_Monitoring);
-      Surface_CMx_Mnt[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CMx_Mnt(
-                                                                  iMarker_Monitoring);
-      Surface_CMy_Mnt[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CMy_Mnt(
-                                                                  iMarker_Monitoring);
-      Surface_CMz_Mnt[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CMz_Mnt(
-                                                                  iMarker_Monitoring);
-      Surface_CFx_Mnt[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CFx_Mnt(
-                                                                  iMarker_Monitoring);
-      Surface_CFy_Mnt[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CFy_Mnt(
-                                                                  iMarker_Monitoring);
-      Surface_CFz_Mnt[iMarker_Monitoring] =
-      solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetSurface_CFz_Mnt(
-                                                                  iMarker_Monitoring);
-
-    }
-
-
-    /*--- Write file name with extension ---*/
-
-    string filename = config[val_iZone]->GetBreakdown_FileName();
-    strcpy (cstr, filename.data());
-
-    Breakdown_file.open(cstr, ios::out);
-
-    Breakdown_file << "\n" <<"-------------------------------------------------------------------------" << "\n";
-    Breakdown_file <<"|    ___ _   _ ___                                                      |" << "\n";
-    Breakdown_file <<"|   / __| | | |_  )   Release 7.5.0  \"Blackbird\"                        |" << "\n";
-    Breakdown_file <<"|   \\__ \\ |_| |/ /                                                      |" << "\n";
-    Breakdown_file <<"|   |___/\\___//___|   Suite (Computational Fluid Dynamics Code)         |" << "\n";
-    Breakdown_file << "|                                                                       |" << "\n";
-    Breakdown_file <<"-------------------------------------------------------------------------" << "\n";
-    Breakdown_file << "| SU2 Project Website: https://su2code.github.io                        |" << "\n";
-    Breakdown_file << "|                                                                       |" << "\n";
-    Breakdown_file << "| The SU2 Project is maintained by the SU2 Foundation                   |" << "\n";
-    Breakdown_file << "| (http://su2foundation.org)                                            |" << "\n";
-    Breakdown_file <<"-------------------------------------------------------------------------" << "\n";
-    Breakdown_file << "| Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)                |" << "\n";
-    Breakdown_file << "|                                                                       |" << "\n";
-    Breakdown_file << "| SU2 is free software; you can redistribute it and/or                  |" << "\n";
-    Breakdown_file << "| modify it under the terms of the GNU Lesser General Public            |" << "\n";
-    Breakdown_file << "| License as published by the Free Software Foundation; either          |" << "\n";
-    Breakdown_file << "| version 2.1 of the License, or (at your option) any later version.    |" << "\n";
-    Breakdown_file << "|                                                                       |" << "\n";
-    Breakdown_file << "| SU2 is distributed in the hope that it will be useful,                |" << "\n";
-    Breakdown_file << "| but WITHOUT ANY WARRANTY; without even the implied warranty of        |" << "\n";
-    Breakdown_file << "| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |" << "\n";
-    Breakdown_file << "| Lesser General Public License for more details.                       |" << "\n";
-    Breakdown_file << "|                                                                       |" << "\n";
-    Breakdown_file << "| You should have received a copy of the GNU Lesser General Public      |" << "\n";
-    Breakdown_file << "| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |" << "\n";
-    Breakdown_file <<"-------------------------------------------------------------------------" << "\n";
-
-    Breakdown_file.precision(6);
-
-    Breakdown_file << "\n" << "\n" << "Problem definition:" << "\n" << "\n";
-
-    switch (Kind_Solver) {
-      case MAIN_SOLVER::EULER: case MAIN_SOLVER::INC_EULER:
-        if (compressible) Breakdown_file << "Compressible Euler equations." << "\n";
-        if (incompressible) Breakdown_file << "Incompressible Euler equations." << "\n";
-        break;
-      case MAIN_SOLVER::NAVIER_STOKES: case MAIN_SOLVER::INC_NAVIER_STOKES:
-        if (compressible) Breakdown_file << "Compressible Laminar Navier-Stokes' equations." << "\n";
-        if (incompressible) Breakdown_file << "Incompressible Laminar Navier-Stokes' equations." << "\n";
-        break;
-      case MAIN_SOLVER::RANS: case MAIN_SOLVER::INC_RANS:
-        if (compressible) Breakdown_file << "Compressible RANS equations." << "\n";
-        if (incompressible) Breakdown_file << "Incompressible RANS equations." << "\n";
-        Breakdown_file << "Turbulence model: ";
-        switch (Kind_Turb_Model) {
-          case TURB_MODEL::SA:        Breakdown_file << "Spalart Allmaras" << "\n"; break;
-          case TURB_MODEL::SST:       Breakdown_file << "Menter's SST"     << "\n"; break;
-          default: break;
-        }
-        break;
-      default:
-        break;
-    }
-
-
-    /*--- Compressible version of console output ---*/
-
-    if (compressible) {
-
-
-    if ((compressible) && (Kind_Solver != MAIN_SOLVER::FEM_ELASTICITY)) {
-      Breakdown_file << "Mach number: " << config[val_iZone]->GetMach() <<"."<< "\n";
-      Breakdown_file << "Angle of attack (AoA): " << config[val_iZone]->GetAoA() <<" deg, and angle of sideslip (AoS): " << config[val_iZone]->GetAoS() <<" deg."<< "\n";
-      if ((Kind_Solver == MAIN_SOLVER::NAVIER_STOKES) || (Kind_Solver == MAIN_SOLVER::ADJ_NAVIER_STOKES) ||
-          (Kind_Solver == MAIN_SOLVER::RANS) || (Kind_Solver == MAIN_SOLVER::ADJ_RANS))
-        Breakdown_file << "Reynolds number: " << config[val_iZone]->GetReynolds() <<"."<< "\n";
-    }
-
-    if (fixed_cl) {
-      Breakdown_file << "Simulation at a cte. CL: " << config[val_iZone]->GetTarget_CL() << ".\n";
-      Breakdown_file << "Approx. Delta CL / Delta AoA: " << config[val_iZone]->GetdCL_dAlpha() << " (1/deg).\n";
-      Breakdown_file << "Approx. Delta CD / Delta CL: " << config[val_iZone]->GetdCD_dCL() << ".\n";
-      if (nDim == 3 ) {
-        Breakdown_file << "Approx. Delta CMx / Delta CL: " << config[val_iZone]->GetdCMx_dCL() << ".\n";
-        Breakdown_file << "Approx. Delta CMy / Delta CL: " << config[val_iZone]->GetdCMy_dCL() << ".\n";
-      }
-      Breakdown_file << "Approx. Delta CMz / Delta CL: " << config[val_iZone]->GetdCMz_dCL() << ".\n";
-    }
-
-    if (Ref_NonDim == DIMENSIONAL) { Breakdown_file << "Dimensional simulation." << "\n"; }
-    else if (Ref_NonDim == FREESTREAM_PRESS_EQ_ONE) { Breakdown_file << "Non-Dimensional simulation (P=1.0, Rho=1.0, T=1.0 at the farfield)." << "\n"; }
-    else if (Ref_NonDim == FREESTREAM_VEL_EQ_MACH) { Breakdown_file << "Non-Dimensional simulation (V=Mach, Rho=1.0, T=1.0 at the farfield)." << "\n"; }
-    else if (Ref_NonDim == FREESTREAM_VEL_EQ_ONE) { Breakdown_file << "Non-Dimensional simulation (V=1.0, Rho=1.0, T=1.0 at the farfield)." << "\n"; }
-
-    if (config[val_iZone]->GetSystemMeasurements() == SI) {
-      Breakdown_file << "The reference area is " << config[val_iZone]->GetRefArea() << " m^2." << "\n";
-      Breakdown_file << "The reference length is " << config[val_iZone]->GetRefLength() << " m." << "\n";
-    }
-
-    if (config[val_iZone]->GetSystemMeasurements() == US) {
-      Breakdown_file << "The reference area is " << config[val_iZone]->GetRefArea()*12.0*12.0 << " in^2." << "\n";
-      Breakdown_file << "The reference length is " << config[val_iZone]->GetRefLength()*12.0 << " in." << "\n";
-    }
-    Breakdown_file << "\n" << "\n" <<"Problem definition:" << "\n" << "\n";
-    if (compressible) {
-      if (viscous) {
-        Breakdown_file << "Viscous flow: Computing pressure using the ideal gas law" << "\n";
-        Breakdown_file << "based on the free-stream temperature and a density computed" << "\n";
-        Breakdown_file << "from the Reynolds number." << "\n";
-      } else {
-        Breakdown_file << "Inviscid flow: Computing density based on free-stream" << "\n";
-        Breakdown_file << "temperature and pressure using the ideal gas law." << "\n";
-      }
-    }
-
-    if (dynamic_grid) Breakdown_file << "Force coefficients computed using MACH_MOTION." << "\n";
-    else Breakdown_file << "Force coefficients computed using free-stream values." << "\n";
-
-    if (incompressible) {
-      Breakdown_file << "Viscous and Inviscid flow: rho_ref, and vel_ref" << "\n";
-      Breakdown_file << "are based on the free-stream values, p_ref = rho_ref*vel_ref^2." << "\n";
-      Breakdown_file << "The free-stream value of the pressure is 0." << "\n";
-      Breakdown_file << "Mach number: "<< config[val_iZone]->GetMach() << ", computed using the Bulk modulus." << "\n";
-      Breakdown_file << "Angle of attack (deg): "<< config[val_iZone]->GetAoA() << ", computed using the the free-stream velocity." << "\n";
-      Breakdown_file << "Side slip angle (deg): "<< config[val_iZone]->GetAoS() << ", computed using the the free-stream velocity." << "\n";
-      if (viscous) Breakdown_file << "Reynolds number: " << config[val_iZone]->GetReynolds() << ", computed using free-stream values."<< "\n";
-      Breakdown_file << "Only dimensional computation, the grid should be dimensional." << "\n";
-    }
-
-    Breakdown_file <<"-- Input conditions:"<< "\n";
-
-    if (compressible) {
-      switch (config[val_iZone]->GetKind_FluidModel()) {
-
-        case STANDARD_AIR:
-          Breakdown_file << "Fluid Model: STANDARD_AIR "<< "\n";
-          Breakdown_file << "Specific gas constant: " << config[val_iZone]->GetGas_Constant();
-          if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " N.m/kg.K." << "\n";
-          else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " lbf.ft/slug.R." << "\n";
-          Breakdown_file << "Specific gas constant (non-dim): " << config[val_iZone]->GetGas_ConstantND()<< "\n";
-          Breakdown_file << "Specific Heat Ratio: 1.4000 "<< "\n";
-          break;
-
-        case IDEAL_GAS:
-          Breakdown_file << "Fluid Model: IDEAL_GAS "<< "\n";
-          Breakdown_file << "Specific gas constant: " << config[val_iZone]->GetGas_Constant() << " N.m/kg.K." << "\n";
-          Breakdown_file << "Specific gas constant (non-dim): " << config[val_iZone]->GetGas_ConstantND()<< "\n";
-          Breakdown_file << "Specific Heat Ratio: "<< config[val_iZone]->GetGamma() << "\n";
-          break;
-
-        case VW_GAS:
-          Breakdown_file << "Fluid Model: Van der Waals "<< "\n";
-          Breakdown_file << "Specific gas constant: " << config[val_iZone]->GetGas_Constant() << " N.m/kg.K." << "\n";
-          Breakdown_file << "Specific gas constant (non-dim): " << config[val_iZone]->GetGas_ConstantND()<< "\n";
-          Breakdown_file << "Specific Heat Ratio: "<< config[val_iZone]->GetGamma() << "\n";
-          Breakdown_file << "Critical Pressure:   " << config[val_iZone]->GetPressure_Critical()  << " Pa." << "\n";
-          Breakdown_file << "Critical Temperature:  " << config[val_iZone]->GetTemperature_Critical() << " K." << "\n";
-          Breakdown_file << "Critical Pressure (non-dim):   " << config[val_iZone]->GetPressure_Critical() /config[val_iZone]->GetPressure_Ref() << "\n";
-          Breakdown_file << "Critical Temperature (non-dim) :  " << config[val_iZone]->GetTemperature_Critical() /config[val_iZone]->GetTemperature_Ref() << "\n";
-          break;
-
-        case PR_GAS:
-          Breakdown_file << "Fluid Model: Peng-Robinson "<< "\n";
-          Breakdown_file << "Specific gas constant: " << config[val_iZone]->GetGas_Constant() << " N.m/kg.K." << "\n";
-          Breakdown_file << "Specific gas constant(non-dim): " << config[val_iZone]->GetGas_ConstantND()<< "\n";
-          Breakdown_file << "Specific Heat Ratio: "<< config[val_iZone]->GetGamma() << "\n";
-          Breakdown_file << "Critical Pressure:   " << config[val_iZone]->GetPressure_Critical()  << " Pa." << "\n";
-          Breakdown_file << "Critical Temperature:  " << config[val_iZone]->GetTemperature_Critical() << " K." << "\n";
-          Breakdown_file << "Critical Pressure (non-dim):   " << config[val_iZone]->GetPressure_Critical() /config[val_iZone]->GetPressure_Ref() << "\n";
-          Breakdown_file << "Critical Temperature (non-dim) :  " << config[val_iZone]->GetTemperature_Critical() /config[val_iZone]->GetTemperature_Ref() << "\n";
-          break;
-        case COOLPROP: {
-          CCoolProp auxFluidModel(config[val_iZone]->GetFluid_Name());
-          Breakdown_file << "Fluid Model: CoolProp library \n";
-          Breakdown_file << "Specific gas constant: " << auxFluidModel.GetGas_Constant()<< " N.m/kg.K.\n";
-          Breakdown_file << "Specific gas constant(non-dim): " << config[val_iZone]->GetGas_ConstantND() << "\n";
-          Breakdown_file << "Specific Heat Ratio: " << auxFluidModel.GetGamma() << "\n";
-          Breakdown_file << "Critical Pressure:   " << auxFluidModel.GetPressure_Critical() << " Pa.\n";
-          Breakdown_file << "Critical Temperature:  " << auxFluidModel.GetTemperature_Critical()<< " K.\n";
-          Breakdown_file << "Critical Pressure (non-dim):   " << auxFluidModel.GetPressure_Critical()/ config[val_iZone]->GetPressure_Ref()<< "\n";
-          Breakdown_file << "Critical Temperature (non-dim) :  " << auxFluidModel.GetTemperature_Critical() / config[val_iZone]->GetTemperature_Ref() << "\n";
-        } break;
-      }
-
-      if (viscous) {
-
-        switch (config[val_iZone]->GetKind_ViscosityModel()) {
-
-          case VISCOSITYMODEL::CONSTANT:
-            Breakdown_file << "Viscosity Model: CONSTANT_VISCOSITY  "<< "\n";
-            Breakdown_file << "Laminar Viscosity: " << config[val_iZone]->GetMu_Constant();
-            if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " N.s/m^2." << "\n";
-            else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " lbf.s/ft^2." << "\n";
-            Breakdown_file << "Laminar Viscosity (non-dim): " << config[val_iZone]->GetMu_ConstantND()<< "\n";
-            break;
-
-          case VISCOSITYMODEL::SUTHERLAND:
-            Breakdown_file << "Viscosity Model: SUTHERLAND "<< "\n";
-            Breakdown_file << "Ref. Laminar Viscosity: " << config[val_iZone]->GetMu_Ref();
-            if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " N.s/m^2." << "\n";
-            else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " lbf.s/ft^2." << "\n";
-            Breakdown_file << "Ref. Temperature: " << config[val_iZone]->GetMu_Temperature_Ref();
-            if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " K." << "\n";
-            else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " R." << "\n";
-            Breakdown_file << "Sutherland Constant: "<< config[val_iZone]->GetMu_S();
-            if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " K." << "\n";
-            else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " R." << "\n";
-            Breakdown_file << "Laminar Viscosity (non-dim): " << config[val_iZone]->GetMu_ConstantND()<< "\n";
-            Breakdown_file << "Ref. Temperature (non-dim): " << config[val_iZone]->GetMu_Temperature_RefND()<< "\n";
-            Breakdown_file << "Sutherland constant (non-dim): "<< config[val_iZone]->GetMu_SND()<< "\n";
-            break;
-
-          case VISCOSITYMODEL::COOLPROP:
-            Breakdown_file << "Viscosity Model: CoolProp"<< "\n";
-            break;
-
-          default:
-            break;
-
-        }
-        switch (config[val_iZone]->GetKind_ConductivityModel()) {
-
-          case CONDUCTIVITYMODEL::CONSTANT_PRANDTL:
-            Breakdown_file << "Conductivity Model: CONSTANT_PRANDTL  "<< "\n";
-            Breakdown_file << "Prandtl: " << config[val_iZone]->GetPrandtl_Lam()<< "\n";
-            break;
-
-          case CONDUCTIVITYMODEL::CONSTANT:
-            Breakdown_file << "Conductivity Model: CONSTANT "<< "\n";
-            Breakdown_file << "Molecular Conductivity: " << config[val_iZone]->GetThermal_Conductivity_Constant()<< " W/m^2.K." << "\n";
-            Breakdown_file << "Molecular Conductivity (non-dim): " << config[val_iZone]->GetThermal_Conductivity_ConstantND()<< "\n";
-            break;
-
-          case CONDUCTIVITYMODEL::COOLPROP:
-            Breakdown_file << "Conductivity Model: COOLPROP "<< "\n";
-            break;
-
-          default:
-            break;
-
-        }
-
-        if ((Kind_Solver == MAIN_SOLVER::RANS) || (Kind_Solver == MAIN_SOLVER::ADJ_RANS) || (Kind_Solver == MAIN_SOLVER::DISC_ADJ_RANS)) {
-          switch (config[val_iZone]->GetKind_ConductivityModel_Turb()) {
-            case CONDUCTIVITYMODEL_TURB::CONSTANT_PRANDTL:
-              Breakdown_file << "Turbulent Conductivity Model: CONSTANT_PRANDTL  "<< "\n";
-              Breakdown_file << "Turbulent Prandtl: " << config[val_iZone]->GetPrandtl_Turb()<< "\n";
-              break;
-            case CONDUCTIVITYMODEL_TURB::NONE:
-              Breakdown_file << "Turbulent Conductivity Model: NONE "<< "\n";
-              Breakdown_file << "No turbulent component in effective thermal conductivity." << "\n";
-              break;
-          }
-        }
-
-      }
-    }
-
-    if (incompressible) {
-      Breakdown_file << "Bulk modulus: " << config[val_iZone]->GetBulk_Modulus();
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " Pa." << "\n";
-      else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " psf." << "\n";
-      Breakdown_file << "Epsilon^2 multiplier of Beta for incompressible preconditioner: " << config[val_iZone]->GetBeta_Factor();
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " Pa." << "\n";
-      else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " psf." << "\n";
-    }
-
-    Breakdown_file << "Free-stream static pressure: " << config[val_iZone]->GetPressure_FreeStream();
-    if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " Pa." << "\n";
-    else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " psf." << "\n";
-
-    Breakdown_file << "Free-stream total pressure: " << config[val_iZone]->GetPressure_FreeStream() * pow( 1.0+config[val_iZone]->GetMach()*config[val_iZone]->GetMach()*0.5*(config[val_iZone]->GetGamma()-1.0), config[val_iZone]->GetGamma()/(config[val_iZone]->GetGamma()-1.0) );
-    if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " Pa." << "\n";
-    else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " psf." << "\n";
-
-    if (compressible) {
-      Breakdown_file << "Free-stream temperature: " << config[val_iZone]->GetTemperature_FreeStream();
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " K." << "\n";
-      else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " R." << "\n";
-
-      Breakdown_file << "Free-stream total temperature: " << config[val_iZone]->GetTemperature_FreeStream() * (1.0 + config[val_iZone]->GetMach() * config[val_iZone]->GetMach() * 0.5 * (config[val_iZone]->GetGamma() - 1.0));
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " K." << "\n";
-      else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " R." << "\n";
-    }
-
-    Breakdown_file << "Free-stream density: " << config[val_iZone]->GetDensity_FreeStream();
-    if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " kg/m^3." << "\n";
-    else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " slug/ft^3." << "\n";
-
-    if (nDim == 2) {
-      Breakdown_file << "Free-stream velocity: (" << config[val_iZone]->GetVelocity_FreeStream()[0] << ", ";
-      Breakdown_file << config[val_iZone]->GetVelocity_FreeStream()[1] << ")";
-    }
-    if (nDim == 3) {
-      Breakdown_file << "Free-stream velocity: (" << config[val_iZone]->GetVelocity_FreeStream()[0] << ", ";
-      Breakdown_file << config[val_iZone]->GetVelocity_FreeStream()[1] << ", " << config[val_iZone]->GetVelocity_FreeStream()[2] << ")";
-    }
-    if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " m/s. ";
-    else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " ft/s. ";
-
-    Breakdown_file << "Magnitude: "  << config[val_iZone]->GetModVel_FreeStream();
-    if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " m/s." << "\n";
-    else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " ft/s." << "\n";
-
-    if (compressible) {
-      Breakdown_file << "Free-stream total energy per unit mass: " << config[val_iZone]->GetEnergy_FreeStream();
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " m^2/s^2." << "\n";
-      else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " ft^2/s^2." << "\n";
-    }
-
-    if (viscous) {
-      Breakdown_file << "Free-stream viscosity: " << config[val_iZone]->GetViscosity_FreeStream();
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " N.s/m^2." << "\n";
-      else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " lbf.s/ft^2." << "\n";
-      if (turbulent) {
-        Breakdown_file << "Free-stream turb. kinetic energy per unit mass: " << config[val_iZone]->GetTke_FreeStream();
-        if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " m^2/s^2." << "\n";
-        else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " ft^2/s^2." << "\n";
-        Breakdown_file << "Free-stream specific dissipation: " << config[val_iZone]->GetOmega_FreeStream();
-        if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " 1/s." << "\n";
-        else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " 1/s." << "\n";
-      }
-    }
-
-    if (unsteady) { Breakdown_file << "Total time: " << config[val_iZone]->GetTotal_UnstTime() << " s. Time step: " << config[val_iZone]->GetDelta_UnstTime() << " s." << "\n"; }
-
-    /*--- Print out reference values. ---*/
-
-    Breakdown_file <<"-- Reference values:"<< "\n";
-
-    if (compressible) {
-      Breakdown_file << "Reference specific gas constant: " << config[val_iZone]->GetGas_Constant_Ref();
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " N.m/kg.K." << "\n";
-      else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " lbf.ft/slug.R." << "\n";
-    }
-
-    Breakdown_file << "Reference pressure: " << config[val_iZone]->GetPressure_Ref();
-    if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " Pa." << "\n";
-    else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " psf." << "\n";
-
-    if (compressible) {
-      Breakdown_file << "Reference temperature: " << config[val_iZone]->GetTemperature_Ref();
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " K." << "\n";
-      else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " R." << "\n";
-    }
-
-    Breakdown_file << "Reference density: " << config[val_iZone]->GetDensity_Ref();
-    if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " kg/m^3." << "\n";
-    else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " slug/ft^3." << "\n";
-
-    Breakdown_file << "Reference velocity: " << config[val_iZone]->GetVelocity_Ref();
-    if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " m/s." << "\n";
-    else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " ft/s." << "\n";
-
-    if (compressible) {
-      Breakdown_file << "Reference energy per unit mass: " << config[val_iZone]->GetEnergy_Ref();
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " m^2/s^2." << "\n";
-      else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " ft^2/s^2." << "\n";
-    }
-
-    if (incompressible) {
-      Breakdown_file << "Reference length: " << config[val_iZone]->GetLength_Ref();
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " m." << "\n";
-      else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " in." << "\n";
-    }
-
-    if (viscous) {
-      Breakdown_file << "Reference viscosity: " << config[val_iZone]->GetViscosity_Ref();
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " N.s/m^2." << "\n";
-      else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " lbf.s/ft^2." << "\n";
-      if (compressible){
-        Breakdown_file << "Reference conductivity: " << config[val_iZone]->GetThermal_Conductivity_Ref();
-        if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " W/m^2.K." << "\n";
-        else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " lbf/ft.s.R." << "\n";
-      }
-    }
-
-
-    if (unsteady) Breakdown_file << "Reference time: " << config[val_iZone]->GetTime_Ref() <<" s." << "\n";
-
-    /*--- Print out resulting non-dim values here. ---*/
-
-    Breakdown_file << "-- Resulting non-dimensional state:" << "\n";
-    Breakdown_file << "Mach number (non-dim): " << config[val_iZone]->GetMach() << "\n";
-    if (viscous) {
-      Breakdown_file << "Reynolds number (non-dim): " << config[val_iZone]->GetReynolds() <<". Re length: " << config[val_iZone]->GetLength_Reynolds();
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " m." << "\n";
-      else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " ft." << "\n";
-    }
-    if (gravity) {
-      Breakdown_file << "Froude number (non-dim): " << config[val_iZone]->GetFroude() << "\n";
-      Breakdown_file << "Lenght of the baseline wave (non-dim): " << 2.0*PI_NUMBER*config[val_iZone]->GetFroude()*config[val_iZone]->GetFroude() << "\n";
-    }
-
-    if (compressible) {
-      Breakdown_file << "Specific gas constant (non-dim): " << config[val_iZone]->GetGas_ConstantND() << "\n";
-      Breakdown_file << "Free-stream temperature (non-dim): " << config[val_iZone]->GetTemperature_FreeStreamND() << "\n";
-    }
-
-    Breakdown_file << "Free-stream pressure (non-dim): " << config[val_iZone]->GetPressure_FreeStreamND() << "\n";
-
-    Breakdown_file << "Free-stream density (non-dim): " << config[val_iZone]->GetDensity_FreeStreamND() << "\n";
-
-    if (nDim == 2) {
-      Breakdown_file << "Free-stream velocity (non-dim): (" << config[val_iZone]->GetVelocity_FreeStreamND()[0] << ", ";
-      Breakdown_file << config[val_iZone]->GetVelocity_FreeStreamND()[1] << "). ";
-    } else {
-      Breakdown_file << "Free-stream velocity (non-dim): (" << config[val_iZone]->GetVelocity_FreeStreamND()[0] << ", ";
-      Breakdown_file << config[val_iZone]->GetVelocity_FreeStreamND()[1] << ", " << config[val_iZone]->GetVelocity_FreeStreamND()[2] << "). ";
-    }
-    Breakdown_file << "Magnitude: "   << config[val_iZone]->GetModVel_FreeStreamND() << "\n";
-
-    if (compressible)
-      Breakdown_file << "Free-stream total energy per unit mass (non-dim): " << config[val_iZone]->GetEnergy_FreeStreamND() << "\n";
-
-    if (viscous) {
-      Breakdown_file << "Free-stream viscosity (non-dim): " << config[val_iZone]->GetViscosity_FreeStreamND() << "\n";
-      if (turbulent) {
-        Breakdown_file << "Free-stream turb. kinetic energy (non-dim): " << config[val_iZone]->GetTke_FreeStreamND() << "\n";
-        Breakdown_file << "Free-stream specific dissipation (non-dim): " << config[val_iZone]->GetOmega_FreeStreamND() << "\n";
-      }
-    }
-
-    if (unsteady) {
-      Breakdown_file << "Total time (non-dim): " << config[val_iZone]->GetTotal_UnstTimeND() << "\n";
-      Breakdown_file << "Time step (non-dim): " << config[val_iZone]->GetDelta_UnstTimeND() << "\n";
-    }
-
-    } else {
-
-    /*--- Incompressible version of the console output ---*/
-
-      bool energy     = config[val_iZone]->GetEnergy_Equation();
-      bool boussinesq = (config[val_iZone]->GetKind_DensityModel() == INC_DENSITYMODEL::BOUSSINESQ);
-
-      if (config[val_iZone]->GetRef_Inc_NonDim() == DIMENSIONAL) {
-        Breakdown_file << "Viscous and Inviscid flow: rho_ref, vel_ref, temp_ref, p_ref" << "\n";
-        Breakdown_file << "are set to 1.0 in order to perform a dimensional calculation." << "\n";
-        if (dynamic_grid) Breakdown_file << "Force coefficients computed using MACH_MOTION." << "\n";
-        else Breakdown_file << "Force coefficients computed using initial values." << "\n";
-      }
-      else if (config[val_iZone]->GetRef_Inc_NonDim() == INITIAL_VALUES) {
-        Breakdown_file << "Viscous and Inviscid flow: rho_ref, vel_ref, and temp_ref" << "\n";
-        Breakdown_file << "are based on the initial values, p_ref = rho_ref*vel_ref^2." << "\n";
-        if (dynamic_grid) Breakdown_file << "Force coefficients computed using MACH_MOTION." << "\n";
-        else Breakdown_file << "Force coefficients computed using initial values." << "\n";
-      }
-      else if (config[val_iZone]->GetRef_Inc_NonDim() == REFERENCE_VALUES) {
-        Breakdown_file << "Viscous and Inviscid flow: rho_ref, vel_ref, and temp_ref" << "\n";
-        Breakdown_file << "are user-provided reference values, p_ref = rho_ref*vel_ref^2." << "\n";
-        if (dynamic_grid) Breakdown_file << "Force coefficients computed using MACH_MOTION." << "\n";
-        else Breakdown_file << "Force coefficients computed using reference values." << "\n";
-      }
-      Breakdown_file << "The reference area for force coeffs. is " << config[val_iZone]->GetRefArea() << " m^2." << "\n";
-      Breakdown_file << "The reference length for force coeffs. is " << config[val_iZone]->GetRefLength() << " m." << "\n";
-
-      Breakdown_file << "The pressure is decomposed into thermodynamic and dynamic components." << "\n";
-      Breakdown_file << "The initial value of the dynamic pressure is 0." << "\n";
-
-      Breakdown_file << "Mach number: "<< config[val_iZone]->GetMach();
-      if (config[val_iZone]->GetKind_FluidModel() == CONSTANT_DENSITY) {
-        Breakdown_file << ", computed using the Bulk modulus." << "\n";
-      } else {
-        Breakdown_file << ", computed using fluid speed of sound." << "\n";
-      }
-
-      Breakdown_file << "For external flows, the initial state is imposed at the far-field." << "\n";
-      Breakdown_file << "Angle of attack (deg): "<< config[val_iZone]->GetAoA() << ", computed using the initial velocity." << "\n";
-      Breakdown_file << "Side slip angle (deg): "<< config[val_iZone]->GetAoS() << ", computed using the initial velocity." << "\n";
-
-      if (viscous) {
-        Breakdown_file << "Reynolds number per meter: " << config[val_iZone]->GetReynolds() << ", computed using initial values."<< "\n";
-        Breakdown_file << "Reynolds number is a byproduct of inputs only (not used internally)." << "\n";
-      }
-      Breakdown_file << "SI units only. The grid should be dimensional (meters)." << "\n";
-
-      switch (config[val_iZone]->GetKind_DensityModel()) {
-
-        case INC_DENSITYMODEL::CONSTANT:
-          if (energy) Breakdown_file << "Energy equation is active and decoupled." << "\n";
-          else Breakdown_file << "No energy equation." << "\n";
-          break;
-
-        case INC_DENSITYMODEL::BOUSSINESQ:
-          if (energy) Breakdown_file << "Energy equation is active and coupled through Boussinesq approx." << "\n";
-          break;
-
-        case INC_DENSITYMODEL::VARIABLE:
-          if (energy) Breakdown_file << "Energy equation is active and coupled for variable density." << "\n";
-          break;
-
-      }
-
-      Breakdown_file <<"-- Input conditions:"<< "\n";
-
-      switch (config[val_iZone]->GetKind_FluidModel()) {
-
-        case CONSTANT_DENSITY:
-          Breakdown_file << "Fluid Model: CONSTANT_DENSITY "<< "\n";
-          if (energy) {
-            Breakdown_file << "Specific heat at constant pressure (Cp): " << config[val_iZone]->GetSpecific_Heat_Cp() << " N.m/kg.K." << "\n";
-          }
-          if (boussinesq) Breakdown_file << "Thermal expansion coefficient: " << config[val_iZone]->GetThermal_Expansion_Coeff() << " K^-1." << "\n";
-          Breakdown_file << "Thermodynamic pressure not required." << "\n";
-          break;
-
-        case INC_IDEAL_GAS:
-          Breakdown_file << "Fluid Model: INC_IDEAL_GAS "<< endl;
-          Breakdown_file << "Variable density incompressible flow using ideal gas law." << endl;
-          Breakdown_file << "Density is a function of temperature (constant thermodynamic pressure)." << endl;
-          Breakdown_file << "Specific heat at constant pressure (Cp): " << config[val_iZone]->GetSpecific_Heat_Cp() << " N.m/kg.K." << endl;
-          Breakdown_file << "Molecular weight : "<< config[val_iZone]->GetMolecular_Weight() << " g/mol" << endl;
-          Breakdown_file << "Specific gas constant: " << config[val_iZone]->GetGas_Constant() << " N.m/kg.K." << endl;
-          Breakdown_file << "Thermodynamic pressure: " << config[val_iZone]->GetPressure_Thermodynamic();
-          if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " Pa." << endl;
-          else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " psf." << endl;
-          break;
-
-        case INC_IDEAL_GAS_POLY:
-          Breakdown_file << "Fluid Model: INC_IDEAL_GAS_POLY "<< endl;
-          Breakdown_file << "Variable density incompressible flow using ideal gas law." << endl;
-          Breakdown_file << "Density is a function of temperature (constant thermodynamic pressure)." << endl;
-          Breakdown_file << "Molecular weight: " << config[val_iZone]->GetMolecular_Weight() << " g/mol." << endl;
-          Breakdown_file << "Specific gas constant: " << config[val_iZone]->GetGas_Constant() << " N.m/kg.K." << endl;
-          Breakdown_file << "Specific gas constant (non-dim): " << config[val_iZone]->GetGas_ConstantND() << endl;
-          Breakdown_file << "Thermodynamic pressure: " << config[val_iZone]->GetPressure_Thermodynamic();
-          if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " Pa." << endl;
-          else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " psf." << endl;
-          Breakdown_file << "Cp(T) polynomial coefficients: \n  (";
-          for (unsigned short iVar = 0; iVar < config[val_iZone]->GetnPolyCoeffs(); iVar++) {
-            Breakdown_file << config[val_iZone]->GetCp_PolyCoeff(iVar);
-            if (iVar < config[val_iZone]->GetnPolyCoeffs()-1) Breakdown_file << ", ";
-          }
-          Breakdown_file << ")." << endl;
-          Breakdown_file << "Cp(T) polynomial coefficients (non-dim.): \n  (";
-          for (unsigned short iVar = 0; iVar < config[val_iZone]->GetnPolyCoeffs(); iVar++) {
-            Breakdown_file << config[val_iZone]->GetCp_PolyCoeffND(iVar);
-            if (iVar < config[val_iZone]->GetnPolyCoeffs()-1) Breakdown_file << ", ";
-          }
-          Breakdown_file << ")." << endl;
-          break;
-
-      }
-      if (viscous) {
-        switch (config[val_iZone]->GetKind_ViscosityModel()) {
-
-          case VISCOSITYMODEL::CONSTANT:
-            Breakdown_file << "Viscosity Model: CONSTANT_VISCOSITY  "<< "\n";
-            Breakdown_file << "Constant Laminar Viscosity: " << config[val_iZone]->GetMu_Constant();
-            if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " N.s/m^2." << "\n";
-            else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " lbf.s/ft^2." << "\n";
-            Breakdown_file << "Laminar Viscosity (non-dim): " << config[val_iZone]->GetMu_ConstantND()<< "\n";
-            break;
-
-          case VISCOSITYMODEL::SUTHERLAND:
-            Breakdown_file << "Viscosity Model: SUTHERLAND "<< "\n";
-            Breakdown_file << "Ref. Laminar Viscosity: " << config[val_iZone]->GetMu_Ref();
-            if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " N.s/m^2." << "\n";
-            else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " lbf.s/ft^2." << "\n";
-            Breakdown_file << "Ref. Temperature: " << config[val_iZone]->GetMu_Temperature_Ref();
-            if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " K." << "\n";
-            else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " R." << "\n";
-            Breakdown_file << "Sutherland Constant: "<< config[val_iZone]->GetMu_S();
-            if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " K." << "\n";
-            else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " R." << "\n";
-            Breakdown_file << "Laminar Viscosity (non-dim): " << config[val_iZone]->GetMu_ConstantND()<< "\n";
-            Breakdown_file << "Ref. Temperature (non-dim): " << config[val_iZone]->GetMu_Temperature_RefND()<< "\n";
-            Breakdown_file << "Sutherland constant (non-dim): "<< config[val_iZone]->GetMu_SND()<< "\n";
-            break;
-
-          case VISCOSITYMODEL::POLYNOMIAL:
-            Breakdown_file << "Viscosity Model: POLYNOMIAL_VISCOSITY  "<< endl;
-            Breakdown_file << "Mu(T) polynomial coefficients: \n  (";
-            for (unsigned short iVar = 0; iVar < config[val_iZone]->GetnPolyCoeffs(); iVar++) {
-              Breakdown_file << config[val_iZone]->GetMu_PolyCoeff(iVar);
-              if (iVar < config[val_iZone]->GetnPolyCoeffs()-1) Breakdown_file << ", ";
-            }
-            Breakdown_file << ")." << endl;
-            Breakdown_file << "Mu(T) polynomial coefficients (non-dim.): \n  (";
-            for (unsigned short iVar = 0; iVar < config[val_iZone]->GetnPolyCoeffs(); iVar++) {
-              Breakdown_file << config[val_iZone]->GetMu_PolyCoeffND(iVar);
-              if (iVar < config[val_iZone]->GetnPolyCoeffs()-1) Breakdown_file << ", ";
-            }
-            Breakdown_file << ")." << endl;
-            break;
-
-          case VISCOSITYMODEL::COOLPROP:
-            Breakdown_file << "Viscosity Model: CoolProp"<< "\n";
-            break;
-
-        }
-
-        if (energy) {
-          switch (config[val_iZone]->GetKind_ConductivityModel()) {
-
-            case CONDUCTIVITYMODEL::CONSTANT_PRANDTL:
-              Breakdown_file << "Conductivity Model: CONSTANT_PRANDTL  "<< "\n";
-              Breakdown_file << "Prandtl (Laminar): " << config[val_iZone]->GetPrandtl_Lam()<< "\n";
-              break;
-
-            case CONDUCTIVITYMODEL::CONSTANT:
-              Breakdown_file << "Conductivity Model: CONSTANT "<< "\n";
-              Breakdown_file << "Molecular Conductivity: " << config[val_iZone]->GetThermal_Conductivity_Constant()<< " W/m^2.K." << "\n";
-              Breakdown_file << "Molecular Conductivity (non-dim): " << config[val_iZone]->GetThermal_Conductivity_ConstantND()<< "\n";
-              break;
-
-            case CONDUCTIVITYMODEL::COOLPROP:
-              Breakdown_file << "Conductivity Model: COOLPROP "<< "\n";
-              break;
-
-            case CONDUCTIVITYMODEL::POLYNOMIAL:
-              Breakdown_file << "Viscosity Model: POLYNOMIAL "<< endl;
-              Breakdown_file << "Kt(T) polynomial coefficients: \n  (";
-              for (unsigned short iVar = 0; iVar < config[val_iZone]->GetnPolyCoeffs(); iVar++) {
-                Breakdown_file << config[val_iZone]->GetKt_PolyCoeff(iVar);
-                if (iVar < config[val_iZone]->GetnPolyCoeffs()-1) Breakdown_file << ", ";
-              }
-              Breakdown_file << ")." << endl;
-              Breakdown_file << "Kt(T) polynomial coefficients (non-dim.): \n  (";
-              for (unsigned short iVar = 0; iVar < config[val_iZone]->GetnPolyCoeffs(); iVar++) {
-                Breakdown_file << config[val_iZone]->GetKt_PolyCoeffND(iVar);
-                if (iVar < config[val_iZone]->GetnPolyCoeffs()-1) Breakdown_file << ", ";
-              }
-              Breakdown_file << ")." << endl;
-              break;
-
-          }
-
-          if ((Kind_Solver == MAIN_SOLVER::RANS) || (Kind_Solver == MAIN_SOLVER::ADJ_RANS) || (Kind_Solver == MAIN_SOLVER::DISC_ADJ_RANS)) {
-            switch (config[val_iZone]->GetKind_ConductivityModel_Turb()) {
-              case CONDUCTIVITYMODEL_TURB::CONSTANT_PRANDTL:
-                Breakdown_file << "Turbulent Conductivity Model: CONSTANT_PRANDTL  "<< "\n";
-                Breakdown_file << "Turbulent Prandtl: " << config[val_iZone]->GetPrandtl_Turb()<< "\n";
-                break;
-              case CONDUCTIVITYMODEL_TURB::NONE:
-                Breakdown_file << "Turbulent Conductivity Model: NONE "<< "\n";
-                Breakdown_file << "No turbulent component in effective thermal conductivity." << "\n";
-                break;
-            }
-          }
-
-        }
-
-      }
-
-      if (config[val_iZone]->GetKind_FluidModel() == CONSTANT_DENSITY) {
-        Breakdown_file << "Bulk modulus: " << config[val_iZone]->GetBulk_Modulus();
-        if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " Pa." << "\n";
-        else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " psf." << "\n";
-      }
-
-      Breakdown_file << "Initial dynamic pressure: " << config[val_iZone]->GetPressure_FreeStream();
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " Pa." << "\n";
-      else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " psf." << "\n";
-
-      Breakdown_file << "Initial total pressure: " << config[val_iZone]->GetPressure_FreeStream() + 0.5*config[val_iZone]->GetDensity_FreeStream()*config[val_iZone]->GetModVel_FreeStream()*config[val_iZone]->GetModVel_FreeStream();
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " Pa." << "\n";
-      else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " psf." << "\n";
-
-      if (energy) {
-        Breakdown_file << "Initial temperature: " << config[val_iZone]->GetTemperature_FreeStream();
-        if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " K." << "\n";
-        else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " R." << "\n";
-      }
-
-      Breakdown_file << "Initial density: " << config[val_iZone]->GetDensity_FreeStream();
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " kg/m^3." << "\n";
-      else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " slug/ft^3." << "\n";
-
-      if (nDim == 2) {
-        Breakdown_file << "Initial velocity: (" << config[val_iZone]->GetVelocity_FreeStream()[0] << ", ";
-        Breakdown_file << config[val_iZone]->GetVelocity_FreeStream()[1] << ")";
-      }
-      if (nDim == 3) {
-        Breakdown_file << "Initial velocity: (" << config[val_iZone]->GetVelocity_FreeStream()[0] << ", ";
-        Breakdown_file << config[val_iZone]->GetVelocity_FreeStream()[1] << ", " << config[val_iZone]->GetVelocity_FreeStream()[2] << ")";
-      }
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " m/s. ";
-      else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " ft/s. ";
-
-      Breakdown_file << "Magnitude: "  << config[val_iZone]->GetModVel_FreeStream();
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " m/s." << "\n";
-      else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " ft/s." << "\n";
-
-      if (viscous) {
-        Breakdown_file << "Initial laminar viscosity: " << config[val_iZone]->GetViscosity_FreeStream();
-        if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " N.s/m^2." << "\n";
-        else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " lbf.s/ft^2." << "\n";
-        if (turbulent) {
-          Breakdown_file << "Initial turb. kinetic energy per unit mass: " << config[val_iZone]->GetTke_FreeStream();
-          if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " m^2/s^2." << "\n";
-          else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " ft^2/s^2." << "\n";
-          Breakdown_file << "Initial specific dissipation: " << config[val_iZone]->GetOmega_FreeStream();
-          if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " 1/s." << "\n";
-          else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " 1/s." << "\n";
-        }
-      }
-
-      if (unsteady) { Breakdown_file << "Total time: " << config[val_iZone]->GetTotal_UnstTime() << " s. Time step: " << config[val_iZone]->GetDelta_UnstTime() << " s." << "\n"; }
-
-      /*--- Print out reference values. ---*/
-
-      Breakdown_file <<"-- Reference values:"<< "\n";
-
-      if (config[val_iZone]->GetKind_FluidModel() != CONSTANT_DENSITY) {
-        Breakdown_file << "Reference specific gas constant: " << config[val_iZone]->GetGas_Constant_Ref();
-        if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " N.m/kg.K." << "\n";
-        else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " lbf.ft/slug.R." << "\n";
-      } else {
-        if (energy) {
-          Breakdown_file << "Reference specific heat: " << config[val_iZone]->GetGas_Constant_Ref();
-          if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " N.m/kg.K." << "\n";
-          else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " lbf.ft/slug.R." << "\n";
-        }
-      }
-
-      Breakdown_file << "Reference pressure: " << config[val_iZone]->GetPressure_Ref();
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " Pa." << "\n";
-      else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " psf." << "\n";
-
-      if (energy) {
-        Breakdown_file << "Reference temperature: " << config[val_iZone]->GetTemperature_Ref();
-        if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " K." << "\n";
-        else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " R." << "\n";
-      }
-
-      Breakdown_file << "Reference density: " << config[val_iZone]->GetDensity_Ref();
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " kg/m^3." << "\n";
-      else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " slug/ft^3." << "\n";
-
-      Breakdown_file << "Reference velocity: " << config[val_iZone]->GetVelocity_Ref();
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " m/s." << "\n";
-      else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " ft/s." << "\n";
-
-      Breakdown_file << "Reference length: " << config[val_iZone]->GetLength_Ref();
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " m." << "\n";
-      else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " in." << "\n";
-
-      if (viscous) {
-        Breakdown_file << "Reference viscosity: " << config[val_iZone]->GetViscosity_Ref();
-        if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " N.s/m^2." << "\n";
-        else if (config[val_iZone]->GetSystemMeasurements() == US) Breakdown_file << " lbf.s/ft^2." << "\n";
-      }
-
-      if (unsteady) Breakdown_file << "Reference time: " << config[val_iZone]->GetTime_Ref() <<" s." << "\n";
-
-      /*--- Print out resulting non-dim values here. ---*/
-
-      Breakdown_file << "-- Resulting non-dimensional state:" << "\n";
-      Breakdown_file << "Mach number (non-dim): " << config[val_iZone]->GetMach() << "\n";
-      if (viscous) {
-        Breakdown_file << "Reynolds number (per m): " << config[val_iZone]->GetReynolds() << "\n";
-      }
-
-      if (config[val_iZone]->GetKind_FluidModel() != CONSTANT_DENSITY) {
-        Breakdown_file << "Specific gas constant (non-dim): " << config[val_iZone]->GetGas_ConstantND() << "\n";
-        Breakdown_file << "Initial thermodynamic pressure (non-dim): " << config[val_iZone]->GetPressure_ThermodynamicND() << "\n";
-      } else {
-        if (energy) {
-          Breakdown_file << "Specific heat at constant pressure (non-dim): " << config[val_iZone]->GetSpecific_Heat_CpND() << "\n";
-          if (boussinesq) Breakdown_file << "Thermal expansion coefficient (non-dim.): " << config[val_iZone]->GetThermal_Expansion_CoeffND() << " K^-1." << "\n";
-        }
-      }
-
-      if (energy) Breakdown_file << "Initial temperature (non-dim): " << config[val_iZone]->GetTemperature_FreeStreamND() << "\n";
-      Breakdown_file << "Initial pressure (non-dim): " << config[val_iZone]->GetPressure_FreeStreamND() << "\n";
-      Breakdown_file << "Initial density (non-dim): " << config[val_iZone]->GetDensity_FreeStreamND() << "\n";
-
-      if (nDim == 2) {
-        Breakdown_file << "Initial velocity (non-dim): (" << config[val_iZone]->GetVelocity_FreeStreamND()[0] << ", ";
-        Breakdown_file << config[val_iZone]->GetVelocity_FreeStreamND()[1] << "). ";
-      } else {
-        Breakdown_file << "Initial velocity (non-dim): (" << config[val_iZone]->GetVelocity_FreeStreamND()[0] << ", ";
-        Breakdown_file << config[val_iZone]->GetVelocity_FreeStreamND()[1] << ", " << config[val_iZone]->GetVelocity_FreeStreamND()[2] << "). ";
-      }
-      Breakdown_file << "Magnitude: "   << config[val_iZone]->GetModVel_FreeStreamND() << "\n";
-
-      if (viscous) {
-        Breakdown_file << "Initial viscosity (non-dim): " << config[val_iZone]->GetViscosity_FreeStreamND() << "\n";
-        if (turbulent) {
-          Breakdown_file << "Initial turb. kinetic energy (non-dim): " << config[val_iZone]->GetTke_FreeStreamND() << "\n";
-          Breakdown_file << "Initial specific dissipation (non-dim): " << config[val_iZone]->GetOmega_FreeStreamND() << "\n";
-        }
-      }
-
-      if (unsteady) {
-        Breakdown_file << "Total time (non-dim): " << config[val_iZone]->GetTotal_UnstTimeND() << "\n";
-        Breakdown_file << "Time step (non-dim): " << config[val_iZone]->GetDelta_UnstTimeND() << "\n";
-      }
-
-    }
-
-    /*--- Begin forces breakdown info. ---*/
-
-    Breakdown_file << fixed;
-    Breakdown_file << "\n" << "\n" <<"Forces breakdown:" << "\n" << "\n";
-
-    if (nDim == 3) {
-      su2double m = solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CFz()/solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CFx();
-      su2double term = (Total_CoPz/m)-Total_CoPx;
-
-      if (term > 0) Breakdown_file << "Center of Pressure: X="  << 1/m <<"Z-"<< term << "." << "\n\n";
-      else Breakdown_file << "Center of Pressure: X="  << 1/m <<"Z+"<< fabs(term);
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " m." << "\n\n";
-      else Breakdown_file << " in." << "\n\n";
-    }
-    else {
-      su2double m = solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CFy()/solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetTotal_CFx();
-      su2double term = (Total_CoPy/m)-Total_CoPx;
-      if (term > 0) Breakdown_file << "Center of Pressure: X="  << 1/m <<"Y-"<< term << "." << "\n\n";
-      else Breakdown_file << "Center of Pressure: X="  << 1/m <<"Y+"<< fabs(term);
-      if (config[val_iZone]->GetSystemMeasurements() == SI) Breakdown_file << " m." << "\n\n";
-      else Breakdown_file << " in." << "\n\n";
-    }
-
-    /*--- Reference area and force factors. ---*/
-
-    su2double RefDensity, RefArea, RefVel, Factor, Ref;
-    RefArea     = config[val_iZone]->GetRefArea();
-    if (compressible) {
-      RefDensity  = solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetDensity_Inf();
-      RefVel = solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetModVelocity_Inf();
-    } else {
-      if ((config[val_iZone]->GetRef_Inc_NonDim() == DIMENSIONAL) ||
-          (config[val_iZone]->GetRef_Inc_NonDim() == INITIAL_VALUES)) {
-        RefDensity  = solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetDensity_Inf();
-        RefVel = 0.0;
-        for (iDim = 0; iDim < nDim; iDim++)
-          RefVel  += solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetVelocity_Inf(iDim)*solver[val_iZone][INST_0][FinestMesh][FLOW_SOL]->GetVelocity_Inf(iDim);
-        RefVel = sqrt(RefVel);
-      } else {
-        RefDensity = config[val_iZone]->GetInc_Density_Ref();
-        RefVel    = config[val_iZone]->GetInc_Velocity_Ref();
-      }
-    }
-    Factor = (0.5*RefDensity*RefArea*RefVel*RefVel);
-    Ref = config[val_iZone]->GetDensity_Ref() * config[val_iZone]->GetVelocity_Ref() * config[val_iZone]->GetVelocity_Ref() * 1.0 * 1.0;
-
-    Breakdown_file << "NOTE: Multiply forces by the non-dimensional factor: " << Factor << ", and the reference factor: " << Ref  << "\n";
-    Breakdown_file << "to obtain the dimensional force."  << "\n" << "\n";
-
-    Breakdown_file << "Total CL:    ";
-    Breakdown_file.width(11);
-    Breakdown_file << Total_CL;
-    Breakdown_file << " | Pressure (";
-    Breakdown_file.width(5);
-    Breakdown_file << SU2_TYPE::Int((Inv_CL * 100.0) / (Total_CL + EPS));
-    Breakdown_file << "%): ";
-    Breakdown_file.width(11);
-    Breakdown_file << Inv_CL;
-    Breakdown_file << " | Friction (";
-    Breakdown_file.width(5);
-    Breakdown_file << SU2_TYPE::Int((Visc_CL * 100.0) / (Total_CL + EPS));
-    Breakdown_file << "%): ";
-    Breakdown_file.width(11);
-    Breakdown_file << Visc_CL;
-    Breakdown_file << " | Momentum (";
-    Breakdown_file.width(5);
-    Breakdown_file << SU2_TYPE::Int((Mnt_CL * 100.0) / (Total_CL + EPS));
-    Breakdown_file << "%): ";
-    Breakdown_file.width(11);
-    Breakdown_file << Mnt_CL << "\n";
-
-    Breakdown_file << "Total CD:    ";
-    Breakdown_file.width(11);
-    Breakdown_file << Total_CD;
-    Breakdown_file << " | Pressure (";
-    Breakdown_file.width(5);
-    Breakdown_file << SU2_TYPE::Int((Inv_CD * 100.0) / (Total_CD + EPS)) << "%): ";
-    Breakdown_file.width(11);
-    Breakdown_file << Inv_CD;
-    Breakdown_file << " | Friction (";
-    Breakdown_file.width(5);
-    Breakdown_file << SU2_TYPE::Int((Visc_CD * 100.0) / (Total_CD + EPS)) << "%): ";
-    Breakdown_file.width(11);
-    Breakdown_file << Visc_CD;
-    Breakdown_file << " | Momentum (";
-    Breakdown_file.width(5);
-    Breakdown_file << SU2_TYPE::Int((Mnt_CD * 100.0) / (Total_CD + EPS)) << "%): ";
-    Breakdown_file.width(11);
-    Breakdown_file << Mnt_CD << "\n";
-
-    if (nDim == 3) {
-      Breakdown_file << "Total CSF:   ";
-      Breakdown_file.width(11);
-      Breakdown_file << Total_CSF;
-      Breakdown_file << " | Pressure (";
-      Breakdown_file.width(5);
-      Breakdown_file << SU2_TYPE::Int((Inv_CSF * 100.0) / (Total_CSF + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Inv_CSF;
-      Breakdown_file << " | Friction (";
-      Breakdown_file.width(5);
-      Breakdown_file <<  SU2_TYPE::Int((Visc_CSF * 100.0) / (Total_CSF + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Visc_CSF;
-      Breakdown_file << " | Momentum (";
-      Breakdown_file.width(5);
-      Breakdown_file << SU2_TYPE::Int((Mnt_CSF * 100.0) / (Total_CSF + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Mnt_CSF << "\n";
-    }
-
-    Breakdown_file << "Total CL/CD: ";
-    Breakdown_file.width(11);
-    Breakdown_file << Total_CEff;
-    Breakdown_file << " | Pressure (";
-    Breakdown_file.width(5);
-    Breakdown_file << SU2_TYPE::Int((Inv_CEff * 100.0) / (Total_CEff + EPS));
-    Breakdown_file << "%): ";
-    Breakdown_file.width(11);
-    Breakdown_file << Inv_CEff;
-    Breakdown_file << " | Friction (";
-    Breakdown_file.width(5);
-    Breakdown_file <<  SU2_TYPE::Int((Visc_CEff * 100.0) / (Total_CEff + EPS));
-    Breakdown_file << "%): ";
-    Breakdown_file.width(11);
-    Breakdown_file << Visc_CEff;
-    Breakdown_file << " | Momentum (";
-    Breakdown_file.width(5);
-    Breakdown_file << SU2_TYPE::Int((Mnt_CEff * 100.0) / (Total_CEff + EPS));
-    Breakdown_file << "%): ";
-    Breakdown_file.width(11);
-    Breakdown_file << Mnt_CEff << "\n";
-
-    if (nDim == 3) {
-      Breakdown_file << "Total CMx:   ";
-      Breakdown_file.width(11);
-      Breakdown_file << Total_CMx;
-      Breakdown_file << " | Pressure (";
-      Breakdown_file.width(5);
-      Breakdown_file << SU2_TYPE::Int((Inv_CMx * 100.0) / (Total_CMx + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Inv_CMx;
-      Breakdown_file << " | Friction (";
-      Breakdown_file.width(5);
-      Breakdown_file << SU2_TYPE::Int((Visc_CMx * 100.0) / (Total_CMx + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Visc_CMx;
-      Breakdown_file << " | Momentum (";
-      Breakdown_file.width(5);
-      Breakdown_file << SU2_TYPE::Int((Mnt_CMx * 100.0) / (Total_CMx + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Mnt_CMx << "\n";
-
-      Breakdown_file << "Total CMy:   ";
-      Breakdown_file.width(11);
-      Breakdown_file << Total_CMy;
-      Breakdown_file << " | Pressure (";
-      Breakdown_file.width(5);
-      Breakdown_file << SU2_TYPE::Int((Inv_CMy * 100.0) / (Total_CMy + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Inv_CMy;
-      Breakdown_file << " | Friction (";
-      Breakdown_file.width(5);
-      Breakdown_file << SU2_TYPE::Int((Visc_CMy * 100.0) / (Total_CMy + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Visc_CMy;
-      Breakdown_file << " | Momentum (";
-      Breakdown_file.width(5);
-      Breakdown_file << SU2_TYPE::Int((Mnt_CMz * 100.0) / (Total_CMz + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Mnt_CMy << "\n";
-    }
-
-    Breakdown_file << "Total CMz:   ";
-    Breakdown_file.width(11);
-    Breakdown_file << Total_CMz;
-    Breakdown_file << " | Pressure (";
-    Breakdown_file.width(5);
-    Breakdown_file << SU2_TYPE::Int((Inv_CMz * 100.0) / (Total_CMz + EPS));
-    Breakdown_file << "%): ";
-    Breakdown_file.width(11);
-    Breakdown_file << Inv_CMz;
-    Breakdown_file << " | Friction (";
-    Breakdown_file.width(5);
-    Breakdown_file << SU2_TYPE::Int((Visc_CMz * 100.0) / (Total_CMz + EPS));
-    Breakdown_file << "%): ";
-    Breakdown_file.width(11);
-    Breakdown_file << Visc_CMz;
-    Breakdown_file << " | Momentum (";
-    Breakdown_file.width(5);
-    Breakdown_file << SU2_TYPE::Int((Mnt_CMz * 100.0) / (Total_CMz + EPS));
-    Breakdown_file << "%): ";
-    Breakdown_file.width(11);
-    Breakdown_file << Mnt_CMz << "\n";
-
-    Breakdown_file << "Total CFx:   ";
-    Breakdown_file.width(11);
-    Breakdown_file << Total_CFx;
-    Breakdown_file << " | Pressure (";
-    Breakdown_file.width(5);
-    Breakdown_file << SU2_TYPE::Int((Inv_CFx * 100.0) / (Total_CFx + EPS));
-    Breakdown_file << "%): ";
-    Breakdown_file.width(11);
-    Breakdown_file << Inv_CFx;
-    Breakdown_file << " | Friction (";
-    Breakdown_file.width(5);
-    Breakdown_file << SU2_TYPE::Int((Visc_CFx * 100.0) / (Total_CFx + EPS));
-    Breakdown_file << "%): ";
-    Breakdown_file.width(11);
-    Breakdown_file << Visc_CFx;
-    Breakdown_file << " | Momentum (";
-    Breakdown_file.width(5);
-    Breakdown_file << SU2_TYPE::Int((Mnt_CFx * 100.0) / (Total_CFx + EPS));
-    Breakdown_file << "%): ";
-    Breakdown_file.width(11);
-    Breakdown_file << Mnt_CFx << "\n";
-
-    Breakdown_file << "Total CFy:   ";
-    Breakdown_file.width(11);
-    Breakdown_file << Total_CFy;
-    Breakdown_file << " | Pressure (";
-    Breakdown_file.width(5);
-    Breakdown_file << SU2_TYPE::Int((Inv_CFy * 100.0) / (Total_CFy + EPS));
-    Breakdown_file << "%): ";
-    Breakdown_file.width(11);
-    Breakdown_file << Inv_CFy;
-    Breakdown_file << " | Friction (";
-    Breakdown_file.width(5);
-    Breakdown_file << SU2_TYPE::Int((Visc_CFy * 100.0) / (Total_CFy + EPS));
-    Breakdown_file << "%): ";
-    Breakdown_file.width(11);
-    Breakdown_file << Visc_CFy;
-    Breakdown_file << " | Momentum (";
-    Breakdown_file.width(5);
-    Breakdown_file << SU2_TYPE::Int((Mnt_CFy * 100.0) / (Total_CFy + EPS));
-    Breakdown_file << "%): ";
-    Breakdown_file.width(11);
-    Breakdown_file << Mnt_CFy << "\n";
-
-    if (nDim == 3) {
-      Breakdown_file << "Total CFz:   ";
-      Breakdown_file.width(11);
-      Breakdown_file << Total_CFz;
-      Breakdown_file << " | Pressure (";
-      Breakdown_file.width(5);
-      Breakdown_file << SU2_TYPE::Int((Inv_CFz * 100.0) / (Total_CFz + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Inv_CFz;
-      Breakdown_file << " | Friction (";
-      Breakdown_file.width(5);
-      Breakdown_file << SU2_TYPE::Int((Visc_CFz * 100.0) / (Total_CFz + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Visc_CFz;
-      Breakdown_file << " | Momentum (";
-      Breakdown_file.width(5);
-      Breakdown_file << SU2_TYPE::Int((Mnt_CFz * 100.0) / (Total_CFz + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Mnt_CFz << "\n";
-    }
-
-    Breakdown_file << "\n" << "\n";
-
-    for (iMarker_Monitoring = 0;
-         iMarker_Monitoring < config[val_iZone]->GetnMarker_Monitoring();
-         iMarker_Monitoring++) {
-
-      Breakdown_file << "Surface name: "
-      << config[val_iZone]->GetMarker_Monitoring_TagBound(
-                                                          iMarker_Monitoring) << "\n" << "\n";
-
-      Breakdown_file << "Total CL    (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int(
-                       (Surface_CL[iMarker_Monitoring] * 100.0)
-                       / (Total_CL + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Surface_CL[iMarker_Monitoring];
-      Breakdown_file << " | Pressure (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int(
-                       (Surface_CL_Inv[iMarker_Monitoring] * 100.0)
-                       / (Surface_CL[iMarker_Monitoring] + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Surface_CL_Inv[iMarker_Monitoring];
-      Breakdown_file << " | Friction (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int(
-                       (Surface_CL_Visc[iMarker_Monitoring] * 100.0)
-                       / (Surface_CL[iMarker_Monitoring] + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Surface_CL_Visc[iMarker_Monitoring];
-      Breakdown_file << " | Momentum (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int(
-                       (Surface_CL_Mnt[iMarker_Monitoring] * 100.0)
-                       / (Surface_CL[iMarker_Monitoring] + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Surface_CL_Mnt[iMarker_Monitoring] << "\n";
-
-      Breakdown_file << "Total CD    (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int(
-                       (Surface_CD[iMarker_Monitoring] * 100.0)
-                       / (Total_CD + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Surface_CD[iMarker_Monitoring];
-      Breakdown_file << " | Pressure (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int(
-                       (Surface_CD_Inv[iMarker_Monitoring] * 100.0)
-                       / (Surface_CD[iMarker_Monitoring] + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Surface_CD_Inv[iMarker_Monitoring];
-      Breakdown_file << " | Friction (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int(
-                       (Surface_CD_Visc[iMarker_Monitoring] * 100.0)
-                       / (Surface_CD[iMarker_Monitoring] + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Surface_CD_Visc[iMarker_Monitoring];
-      Breakdown_file << " | Momentum (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int(
-                       (Surface_CD_Mnt[iMarker_Monitoring] * 100.0)
-                       / (Surface_CD[iMarker_Monitoring] + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Surface_CD_Mnt[iMarker_Monitoring] << "\n";
-
-      if (nDim == 3) {
-        Breakdown_file << "Total CSF   (";
-        Breakdown_file.width(5);
-        Breakdown_file
-        << SU2_TYPE::Int(
-                         (Surface_CSF[iMarker_Monitoring] * 100.0)
-                         / (Total_CSF + EPS));
-        Breakdown_file << "%): ";
-        Breakdown_file.width(11);
-        Breakdown_file << Surface_CSF[iMarker_Monitoring];
-        Breakdown_file << " | Pressure (";
-        Breakdown_file.width(5);
-        Breakdown_file
-        << SU2_TYPE::Int(
-                         (Surface_CSF_Inv[iMarker_Monitoring] * 100.0)
-                         / (Surface_CSF[iMarker_Monitoring] + EPS));
-        Breakdown_file << "%): ";
-        Breakdown_file.width(11);
-        Breakdown_file << Surface_CSF_Inv[iMarker_Monitoring];
-        Breakdown_file << " | Friction (";
-        Breakdown_file.width(5);
-        Breakdown_file
-        << SU2_TYPE::Int(
-                         (Surface_CSF_Visc[iMarker_Monitoring] * 100.0)
-                         / (Surface_CSF[iMarker_Monitoring] + EPS));
-        Breakdown_file << "%): ";
-        Breakdown_file.width(11);
-        Breakdown_file
-        << Surface_CSF_Visc[iMarker_Monitoring];
-        Breakdown_file << " | Momentum (";
-        Breakdown_file.width(5);
-        Breakdown_file
-        << SU2_TYPE::Int(
-                         (Surface_CSF_Mnt[iMarker_Monitoring] * 100.0)
-                         / (Surface_CSF[iMarker_Monitoring] + EPS));
-        Breakdown_file << "%): ";
-        Breakdown_file.width(11);
-        Breakdown_file
-        << Surface_CSF_Mnt[iMarker_Monitoring] << "\n";
-      }
-
-      Breakdown_file << "Total CL/CD (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int(
-                       (Surface_CEff[iMarker_Monitoring] * 100.0) / (Total_CEff + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Surface_CEff[iMarker_Monitoring];
-      Breakdown_file << " | Pressure (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int(
-                       (Surface_CEff_Inv[iMarker_Monitoring] * 100.0)
-                       / (Surface_CEff[iMarker_Monitoring] + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Surface_CEff_Inv[iMarker_Monitoring];
-      Breakdown_file << " | Friction (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int(
-                       (Surface_CEff_Visc[iMarker_Monitoring] * 100.0)
-                       / (Surface_CEff[iMarker_Monitoring] + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file
-      << Surface_CEff_Visc[iMarker_Monitoring];
-      Breakdown_file << " | Momentum (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int(
-                       (Surface_CEff_Mnt[iMarker_Monitoring] * 100.0)
-                       / (Surface_CEff[iMarker_Monitoring] + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file
-      << Surface_CEff_Mnt[iMarker_Monitoring] << "\n";
-
-      if (nDim == 3) {
-
-        Breakdown_file << "Total CMx   (";
-        Breakdown_file.width(5);
-        Breakdown_file
-        << SU2_TYPE::Int(
-                         (Surface_CMx[iMarker_Monitoring] * 100.0) / (Total_CMx + EPS));
-        Breakdown_file << "%): ";
-        Breakdown_file.width(11);
-        Breakdown_file << Surface_CMx[iMarker_Monitoring];
-        Breakdown_file << " | Pressure (";
-        Breakdown_file.width(5);
-        Breakdown_file
-        << SU2_TYPE::Int(
-                         (Surface_CMx_Inv[iMarker_Monitoring] * 100.0)
-                         / (Surface_CMx[iMarker_Monitoring] + EPS));
-        Breakdown_file << "%): ";
-        Breakdown_file.width(11);
-        Breakdown_file << Surface_CMx_Inv[iMarker_Monitoring];
-        Breakdown_file << " | Friction (";
-        Breakdown_file.width(5);
-        Breakdown_file
-        << SU2_TYPE::Int(
-                         (Surface_CMx_Visc[iMarker_Monitoring] * 100.0)
-                         / (Surface_CMx[iMarker_Monitoring] + EPS));
-        Breakdown_file << "%): ";
-        Breakdown_file.width(11);
-        Breakdown_file
-        << Surface_CMx_Visc[iMarker_Monitoring];
-        Breakdown_file << " | Momentum (";
-        Breakdown_file.width(5);
-        Breakdown_file
-        << SU2_TYPE::Int(
-                         (Surface_CMx_Mnt[iMarker_Monitoring] * 100.0)
-                         / (Surface_CMx[iMarker_Monitoring] + EPS));
-        Breakdown_file << "%): ";
-        Breakdown_file.width(11);
-        Breakdown_file
-        << Surface_CMx_Mnt[iMarker_Monitoring] << "\n";
-
-        Breakdown_file << "Total CMy   (";
-        Breakdown_file.width(5);
-        Breakdown_file
-        << SU2_TYPE::Int(
-                         (Surface_CMy[iMarker_Monitoring] * 100.0) / (Total_CMy + EPS));
-        Breakdown_file << "%): ";
-        Breakdown_file.width(11);
-        Breakdown_file << Surface_CMy[iMarker_Monitoring];
-        Breakdown_file << " | Pressure (";
-        Breakdown_file.width(5);
-        Breakdown_file
-        << SU2_TYPE::Int(
-                         (Surface_CMy_Inv[iMarker_Monitoring] * 100.0)
-                         / (Surface_CMy[iMarker_Monitoring] + EPS));
-        Breakdown_file << "%): ";
-        Breakdown_file.width(11);
-        Breakdown_file << Surface_CMy_Inv[iMarker_Monitoring];
-        Breakdown_file << " | Friction (";
-        Breakdown_file.width(5);
-        Breakdown_file
-        << SU2_TYPE::Int(
-                         (Surface_CMy_Visc[iMarker_Monitoring] * 100.0)
-                         / (Surface_CMy[iMarker_Monitoring] + EPS));
-        Breakdown_file << "%): ";
-        Breakdown_file.width(11);
-        Breakdown_file
-        << Surface_CMy_Visc[iMarker_Monitoring];
-        Breakdown_file << " | Momentum (";
-        Breakdown_file.width(5);
-        Breakdown_file
-        << SU2_TYPE::Int(
-                         (Surface_CMy_Mnt[iMarker_Monitoring] * 100.0)
-                         / (Surface_CMy[iMarker_Monitoring] + EPS));
-        Breakdown_file << "%): ";
-        Breakdown_file.width(11);
-        Breakdown_file
-        << Surface_CMy_Mnt[iMarker_Monitoring] << "\n";
-      }
-
-      Breakdown_file << "Total CMz   (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int((Surface_CMz[iMarker_Monitoring] * 100.0) / (Total_CMz + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Surface_CMz[iMarker_Monitoring];
-      Breakdown_file << " | Pressure (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int(
-                       (Surface_CMz_Inv[iMarker_Monitoring] * 100.0)
-                       / (Surface_CMz[iMarker_Monitoring] + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Surface_CMz_Inv[iMarker_Monitoring];
-      Breakdown_file << " | Friction (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int(
-                       (Surface_CMz_Visc[iMarker_Monitoring] * 100.0)
-                       / (Surface_CMz[iMarker_Monitoring] + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file
-      << Surface_CMz_Visc[iMarker_Monitoring];
-      Breakdown_file << " | Momentum (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int(
-                       (Surface_CMz_Mnt[iMarker_Monitoring] * 100.0)
-                       / (Surface_CMz[iMarker_Monitoring] + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file
-      << Surface_CMz_Mnt[iMarker_Monitoring] << "\n";
-
-      Breakdown_file << "Total CFx   (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int((Surface_CFx[iMarker_Monitoring] * 100.0) / (Total_CFx + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Surface_CFx[iMarker_Monitoring];
-      Breakdown_file << " | Pressure (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int(
-                       (Surface_CFx_Inv[iMarker_Monitoring] * 100.0)
-                       / (Surface_CFx[iMarker_Monitoring] + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Surface_CFx_Inv[iMarker_Monitoring];
-      Breakdown_file << " | Friction (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int(
-                       (Surface_CFx_Visc[iMarker_Monitoring] * 100.0)
-                       / (Surface_CFx[iMarker_Monitoring] + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file
-      << Surface_CFx_Visc[iMarker_Monitoring];
-      Breakdown_file << " | Momentum (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int(
-                       (Surface_CFx_Mnt[iMarker_Monitoring] * 100.0)
-                       / (Surface_CFx[iMarker_Monitoring] + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file
-      << Surface_CFx_Mnt[iMarker_Monitoring] << "\n";
-
-      Breakdown_file << "Total CFy   (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int((Surface_CFy[iMarker_Monitoring] * 100.0) / (Total_CFy + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Surface_CFy[iMarker_Monitoring];
-      Breakdown_file << " | Pressure (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int(
-                       (Surface_CFy_Inv[iMarker_Monitoring] * 100.0)
-                       / (Surface_CFy[iMarker_Monitoring] + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file << Surface_CFy_Inv[iMarker_Monitoring];
-      Breakdown_file << " | Friction (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int(
-                       (Surface_CFy_Visc[iMarker_Monitoring] * 100.0)
-                       / (Surface_CFy[iMarker_Monitoring] + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file
-      << Surface_CFy_Visc[iMarker_Monitoring];
-      Breakdown_file << " | Momentum (";
-      Breakdown_file.width(5);
-      Breakdown_file
-      << SU2_TYPE::Int(
-                       (Surface_CFy_Mnt[iMarker_Monitoring] * 100.0)
-                       / (Surface_CFy[iMarker_Monitoring] + EPS));
-      Breakdown_file << "%): ";
-      Breakdown_file.width(11);
-      Breakdown_file
-      << Surface_CFy_Mnt[iMarker_Monitoring] << "\n";
-
-      if (nDim == 3) {
-        Breakdown_file << "Total CFz   (";
-        Breakdown_file.width(5);
-        Breakdown_file
-        << SU2_TYPE::Int(
-                         (Surface_CFz[iMarker_Monitoring] * 100.0) / (Total_CFz + EPS));
-        Breakdown_file << "%): ";
-        Breakdown_file.width(11);
-        Breakdown_file << Surface_CFz[iMarker_Monitoring];
-        Breakdown_file << " | Pressure (";
-        Breakdown_file.width(5);
-        Breakdown_file
-        << SU2_TYPE::Int(
-                         (Surface_CFz_Inv[iMarker_Monitoring] * 100.0)
-                         / (Surface_CFz[iMarker_Monitoring] + EPS));
-        Breakdown_file << "%): ";
-        Breakdown_file.width(11);
-        Breakdown_file << Surface_CFz_Inv[iMarker_Monitoring];
-        Breakdown_file << " | Friction (";
-        Breakdown_file.width(5);
-        Breakdown_file
-        << SU2_TYPE::Int(
-                         (Surface_CFz_Visc[iMarker_Monitoring] * 100.0)
-                         / (Surface_CFz[iMarker_Monitoring] + EPS));
-        Breakdown_file << "%): ";
-        Breakdown_file.width(11);
-        Breakdown_file
-        << Surface_CFz_Visc[iMarker_Monitoring];
-        Breakdown_file << " | Momentum (";
-        Breakdown_file.width(5);
-        Breakdown_file
-        << SU2_TYPE::Int(
-                         (Surface_CFz_Mnt[iMarker_Monitoring] * 100.0)
-                         / (Surface_CFz[iMarker_Monitoring] + EPS));
-        Breakdown_file << "%): ";
-        Breakdown_file.width(11);
-        Breakdown_file
-        << Surface_CFz_Mnt[iMarker_Monitoring] << "\n";
-
-      }
-
-      Breakdown_file << "\n";
-
-
-    }
-
-    delete [] Surface_CL;
-    delete [] Surface_CD;
-    delete [] Surface_CSF;
-    delete [] Surface_CEff;
-    delete [] Surface_CFx;
-    delete [] Surface_CFy;
-    delete [] Surface_CFz;
-    delete [] Surface_CMx;
-    delete [] Surface_CMy;
-    delete [] Surface_CMz;
-
-    delete [] Surface_CL_Inv;
-    delete [] Surface_CD_Inv;
-    delete [] Surface_CSF_Inv;
-    delete [] Surface_CEff_Inv;
-    delete [] Surface_CFx_Inv;
-    delete [] Surface_CFy_Inv;
-    delete [] Surface_CFz_Inv;
-    delete [] Surface_CMx_Inv;
-    delete [] Surface_CMy_Inv;
-    delete [] Surface_CMz_Inv;
-
-    delete [] Surface_CL_Visc;
-    delete [] Surface_CD_Visc;
-    delete [] Surface_CSF_Visc;
-    delete [] Surface_CEff_Visc;
-    delete [] Surface_CFx_Visc;
-    delete [] Surface_CFy_Visc;
-    delete [] Surface_CFz_Visc;
-    delete [] Surface_CMx_Visc;
-    delete [] Surface_CMy_Visc;
-    delete [] Surface_CMz_Visc;
-
-    delete [] Surface_CL_Mnt;
-    delete [] Surface_CD_Mnt;
-    delete [] Surface_CSF_Mnt;
-    delete [] Surface_CEff_Mnt;
-    delete [] Surface_CFx_Mnt;
-    delete [] Surface_CFy_Mnt;
-    delete [] Surface_CFz_Mnt;
-    delete [] Surface_CMx_Mnt;
-    delete [] Surface_CMy_Mnt;
-    delete [] Surface_CMz_Mnt;
-
-    Breakdown_file.close();
-
-  }
-
-}
-
-void COutputLegacy::SpecialOutputSpanLoad(CSolver *solver, CGeometry *geometry, CConfig *config, bool output) const {
-
-  short iSection, nSection;
-  unsigned long iVertex, iPoint, Trailing_Point;
-  su2double *Plane_P0, *Plane_P0_, *Plane_Normal, *Plane_Normal_, *CPressure,
-  Force[3], ForceInviscid[3], MomentInviscid[3] =
-  { 0.0, 0.0, 0.0 }, MomentDist[3] = { 0.0, 0.0, 0.0 }, RefDensity,
-  RefPressure, RefArea, *Velocity_Inf, Gas_Constant, Mach2Vel,
-  Mach_Motion, Gamma, RefVel2 = 0.0, factor, NDPressure,
-  RefLength, Alpha, CL_Inv,
-  Xcoord_LeadingEdge = 0.0, Ycoord_LeadingEdge = 0.0, Zcoord_LeadingEdge = 0.0,
-  Xcoord_TrailingEdge = 0.0, Ycoord_TrailingEdge = 0.0, Zcoord_TrailingEdge = 0.0,
-  Xcoord_LeadingEdge_ = 0.0,
-  Xcoord_TrailingEdge_ = 0.0, Ycoord_TrailingEdge_ = 0.0, Zcoord_TrailingEdge_ = 0.0,
-  MaxDistance, Distance, Chord, Aux, Dihedral_Trailing;
-
-  su2double B, Y, C_L, C_L0, Elliptic_Spanload;
-
-  vector<su2double> Xcoord_Airfoil, Ycoord_Airfoil, Zcoord_Airfoil,
-  CPressure_Airfoil;
-  vector<su2double> Xcoord_Airfoil_, Ycoord_Airfoil_, Zcoord_Airfoil_,
-  CPressure_Airfoil_;
-  string Marker_Tag, Slice_Filename, Slice_Ext;
-  ofstream Cp_File;
-  unsigned short iDim;
-
-  bool dynamic_grid = config->GetDynamic_Grid();
-
-  Plane_P0 = new su2double[3];
-  Plane_P0_ = new su2double[3];
-  Plane_Normal = new su2double[3];
-  Plane_Normal_ = new su2double[3];
-  CPressure = new su2double[geometry->GetnPoint()];
-
-  if ((rank == MASTER_NODE) && (output)) {
-    cout << endl << "Writing the spanload file (load_distribution.dat).";
-  }
-
-  /*--- Compute some reference quantities and necessary values ---*/
-
-  RefDensity = solver->GetDensity_Inf();
-  RefPressure = solver->GetPressure_Inf();
-  RefArea = config->GetRefArea();
-  Velocity_Inf = solver->GetVelocity_Inf();
-  Gamma = config->GetGamma();
-  const auto Origin = config->GetRefOriginMoment(0);
-  RefLength = config->GetRefLength();
-  Alpha = config->GetAoA() * PI_NUMBER / 180.0;
-
-  if (dynamic_grid) {
-    Gas_Constant = config->GetGas_ConstantND();
-    Mach2Vel = sqrt(
-                    Gamma * Gas_Constant * config->GetTemperature_FreeStreamND());
-    Mach_Motion = config->GetMach_Motion();
-    RefVel2 = (Mach_Motion * Mach2Vel) * (Mach_Motion * Mach2Vel);
-  } else {
-    RefVel2 = 0.0;
-    for (iDim = 0; iDim < geometry->GetnDim(); iDim++)
-      RefVel2 += Velocity_Inf[iDim] * Velocity_Inf[iDim];
-  }
-  factor = 1.0 / (0.5 * RefDensity * RefArea * RefVel2);
-
-  if (geometry->GetnDim() == 3) {
-
-    /*--- Copy the pressure to an auxiliar structure ---*/
-
-    for (iPoint = 0; iPoint < geometry->GetnPoint(); iPoint++) {
-      CPressure[iPoint] = (solver->GetNodes()->GetPressure(iPoint)
-                           - RefPressure) * factor * RefArea;
-    }
-
-    nSection = config->GetnLocationStations();
-
-    for (iSection = 0; iSection < nSection; iSection++) {
-
-      /*--- Read the values from the config file ---*/
-
-      Plane_Normal[0] = 0.0; Plane_P0[0] = 0.0;
-      Plane_Normal[1] = 0.0; Plane_P0[1] = 0.0;
-      Plane_Normal[2] = 0.0; Plane_P0[2] = 0.0;
-
-      if (config->GetGeo_Description() == FUSELAGE) {
-        Plane_Normal[0] = 1.0;
-        Plane_P0[0] = config->GetLocationStations(iSection);
-      }
-      else if (config->GetGeo_Description() == NACELLE) {
-        Plane_Normal[0] = 0.0;
-        Plane_Normal[1] = -sin(config->GetLocationStations(iSection)*PI_NUMBER/180.0);
-        Plane_Normal[2] = cos(config->GetLocationStations(iSection)*PI_NUMBER/180.0);
-
-        /*--- Apply tilt angle to the plane ---*/
-
-        su2double Tilt_Angle = config->GetNacelleLocation(3)*PI_NUMBER/180;
-        su2double Plane_NormalX_Tilt = Plane_Normal[0]*cos(Tilt_Angle) + Plane_Normal[2]*sin(Tilt_Angle);
-        su2double Plane_NormalY_Tilt = Plane_Normal[1];
-        su2double Plane_NormalZ_Tilt = Plane_Normal[2]*cos(Tilt_Angle) - Plane_Normal[0]*sin(Tilt_Angle);
-
-        /*--- Apply toe angle to the plane ---*/
-
-        su2double Toe_Angle = config->GetNacelleLocation(4)*PI_NUMBER/180;
-        su2double Plane_NormalX_Tilt_Toe = Plane_NormalX_Tilt*cos(Toe_Angle) - Plane_NormalY_Tilt*sin(Toe_Angle);
-        su2double Plane_NormalY_Tilt_Toe = Plane_NormalX_Tilt*sin(Toe_Angle) + Plane_NormalY_Tilt*cos(Toe_Angle);
-        su2double Plane_NormalZ_Tilt_Toe = Plane_NormalZ_Tilt;
-
-        /*--- Update normal vector ---*/
-
-        Plane_Normal[0] = Plane_NormalX_Tilt_Toe;
-        Plane_Normal[1] = Plane_NormalY_Tilt_Toe;
-        Plane_Normal[2] = Plane_NormalZ_Tilt_Toe;
-
-      }
-      else {
-        Plane_Normal[1] = 1.0;
-        Plane_P0[1] = config->GetLocationStations(iSection);
-      }
-
-      /*--- Compute the airfoil sections (note that we feed in the Cp) ---*/
-
-      geometry->ComputeAirfoil_Section(Plane_P0, Plane_Normal, -1E6, 1E6, -1E6, 1E6, -1E6, 1E6,
-                                       CPressure, Xcoord_Airfoil, Ycoord_Airfoil, Zcoord_Airfoil,
-                                       CPressure_Airfoil, true, config);
-
-      if ((rank == MASTER_NODE) && (Xcoord_Airfoil.size() == 0)) {
-        if ((config->GetGeo_Description() == FUSELAGE) || (config->GetGeo_Description() == WING))
-          cout << endl << "Please check the config file, the section (" << Plane_P0[0] <<", " << Plane_P0[1] <<", " << Plane_P0[2] << ") has not been detected." << endl;
-        if (config->GetGeo_Description() == NACELLE)
-          cout << endl << "Please check the config file, the section (" << Plane_Normal[0] <<", " << Plane_Normal[1] <<", " << Plane_Normal[2] << ") has not been detected." << endl;
-      }
-
-
-      /*--- Compute dihedral using a step in the station value ---*/
-
-      Plane_P0_[0] = 0.0; Plane_Normal_[0] = 0.0;
-      Plane_P0_[1] = 0.0; Plane_Normal_[1] = 0.0;
-      Plane_P0_[2] = 0.0; Plane_Normal_[2] = 0.0;
-
-      if (config->GetGeo_Description() == FUSELAGE) {
-        Plane_Normal_[0] = 1.0;
-        if (iSection == 0) Plane_P0_[0] = config->GetLocationStations(iSection) + 0.01;
-        else Plane_P0_[0] = config->GetLocationStations(iSection) - 0.01;
-      }
-      else if (config->GetGeo_Description() == NACELLE) {
-        if (iSection == 0) {
-          Plane_Normal_[0] = 0.0;
-          Plane_Normal_[1] = -sin((config->GetLocationStations(iSection) + 0.01)*PI_NUMBER/180.0);
-          Plane_Normal_[2] = cos((config->GetLocationStations(iSection) + 0.01)*PI_NUMBER/180.0);
-
-          /*--- Apply tilt angle to the plane ---*/
-
-          su2double Tilt_Angle = config->GetNacelleLocation(3)*PI_NUMBER/180;
-          su2double Plane_NormalX_Tilt = Plane_Normal[0]*cos(Tilt_Angle) + Plane_Normal[2]*sin(Tilt_Angle);
-          su2double Plane_NormalY_Tilt = Plane_Normal[1];
-          su2double Plane_NormalZ_Tilt = Plane_Normal[2]*cos(Tilt_Angle) - Plane_Normal[0]*sin(Tilt_Angle);
-
-          /*--- Apply toe angle to the plane ---*/
-
-          su2double Toe_Angle = config->GetNacelleLocation(4)*PI_NUMBER/180;
-          su2double Plane_NormalX_Tilt_Toe = Plane_NormalX_Tilt*cos(Toe_Angle) - Plane_NormalY_Tilt*sin(Toe_Angle);
-          su2double Plane_NormalY_Tilt_Toe = Plane_NormalX_Tilt*sin(Toe_Angle) + Plane_NormalY_Tilt*cos(Toe_Angle);
-          su2double Plane_NormalZ_Tilt_Toe = Plane_NormalZ_Tilt;
-
-          /*--- Update normal vector ---*/
-
-          Plane_Normal[0] = Plane_NormalX_Tilt_Toe;
-          Plane_Normal[1] = Plane_NormalY_Tilt_Toe;
-          Plane_Normal[2] = Plane_NormalZ_Tilt_Toe;
-
-        }
-        else {
-          Plane_Normal_[0] = 0.0;
-          Plane_Normal_[1] = -sin((config->GetLocationStations(iSection) - 0.01)*PI_NUMBER/180.0);
-          Plane_Normal_[2] = cos((config->GetLocationStations(iSection) - 0.01)*PI_NUMBER/180.0);
-
-          /*--- Apply tilt angle to the plane ---*/
-
-          su2double Tilt_Angle = config->GetNacelleLocation(3)*PI_NUMBER/180;
-          su2double Plane_NormalX_Tilt = Plane_Normal[0]*cos(Tilt_Angle) + Plane_Normal[2]*sin(Tilt_Angle);
-          su2double Plane_NormalY_Tilt = Plane_Normal[1];
-          su2double Plane_NormalZ_Tilt = Plane_Normal[2]*cos(Tilt_Angle) - Plane_Normal[0]*sin(Tilt_Angle);
-
-          /*--- Apply toe angle to the plane ---*/
-
-          su2double Toe_Angle = config->GetNacelleLocation(4)*PI_NUMBER/180;
-          su2double Plane_NormalX_Tilt_Toe = Plane_NormalX_Tilt*cos(Toe_Angle) - Plane_NormalY_Tilt*sin(Toe_Angle);
-          su2double Plane_NormalY_Tilt_Toe = Plane_NormalX_Tilt*sin(Toe_Angle) + Plane_NormalY_Tilt*cos(Toe_Angle);
-          su2double Plane_NormalZ_Tilt_Toe = Plane_NormalZ_Tilt;
-
-          /*--- Update normal vector ---*/
-
-          Plane_Normal[0] = Plane_NormalX_Tilt_Toe;
-          Plane_Normal[1] = Plane_NormalY_Tilt_Toe;
-          Plane_Normal[2] = Plane_NormalZ_Tilt_Toe;
-
-        }
-      }
-      else {
-        Plane_Normal_[1] = 1.0;
-        if (iSection == 0) Plane_P0_[1] = config->GetLocationStations(iSection) + 0.01;
-        else Plane_P0_[1] = config->GetLocationStations(iSection) - 0.01;
-      }
-
-      geometry->ComputeAirfoil_Section(Plane_P0_, Plane_Normal_, -1E6, 1E6, -1E6, 1E6, -1E6, 1E6,
-                                       CPressure, Xcoord_Airfoil_, Ycoord_Airfoil_, Zcoord_Airfoil_,
-                                       CPressure_Airfoil_, true, config);
-
-      /*--- Output the pressure on each section (tecplot format) ---*/
-
-      if ((rank == MASTER_NODE) && (Xcoord_Airfoil.size() != 0)) {
-
-        /*--- Find leading and trailing edge ---*/
-
-        Xcoord_LeadingEdge = 1E6; Xcoord_TrailingEdge = -1E6;
-        for (iVertex = 0; iVertex < Xcoord_Airfoil.size(); iVertex++) {
-          if (Xcoord_Airfoil[iVertex] < Xcoord_LeadingEdge) {
-            Xcoord_LeadingEdge = Xcoord_Airfoil[iVertex];
-            Ycoord_LeadingEdge = Ycoord_Airfoil[iVertex];
-            Zcoord_LeadingEdge = Zcoord_Airfoil[iVertex];
-          }
-          if (Xcoord_Airfoil[iVertex] > Xcoord_TrailingEdge) {
-            Xcoord_TrailingEdge = Xcoord_Airfoil[iVertex];
-            Ycoord_TrailingEdge = Ycoord_Airfoil[iVertex];
-            Zcoord_TrailingEdge = Zcoord_Airfoil[iVertex];
-          }
-        }
-
-        Chord = (Xcoord_TrailingEdge-Xcoord_LeadingEdge);
-
-        /*--- Compute dihedral ---*/
-
-        Xcoord_LeadingEdge_ = 1E6; Xcoord_TrailingEdge_ = -1E6;
-        for (iVertex = 0; iVertex < Xcoord_Airfoil_.size(); iVertex++) {
-          if (Xcoord_Airfoil_[iVertex] < Xcoord_LeadingEdge_) {
-            Xcoord_LeadingEdge_ = Xcoord_Airfoil_[iVertex];
-          }
-          if (Xcoord_Airfoil_[iVertex] > Xcoord_TrailingEdge_) {
-            Xcoord_TrailingEdge_ = Xcoord_Airfoil_[iVertex];
-            Ycoord_TrailingEdge_ = Ycoord_Airfoil_[iVertex];
-            Zcoord_TrailingEdge_ = Zcoord_Airfoil_[iVertex];
-          }
-        }
-
-        if (iSection == 0) {
-          Dihedral_Trailing = atan((Zcoord_TrailingEdge_ - Zcoord_TrailingEdge) / (Ycoord_TrailingEdge_ - Ycoord_TrailingEdge))*180/PI_NUMBER;
-        }
-        else {
-          Dihedral_Trailing = atan((Zcoord_TrailingEdge - Zcoord_TrailingEdge_) / (Ycoord_TrailingEdge - Ycoord_TrailingEdge_))*180/PI_NUMBER;
-        }
-
-        /*--- Write Cp at each section (tecplot format) ---*/
-
-        if (output) {
-
-          ofstream Cp_File;
-
-          if (iSection == 0) {
-            Cp_File.open("cp_sections.dat", ios::out);
-            Cp_File << "TITLE = \"Airfoil sections\"" << endl;
-            Cp_File << "VARIABLES = \"x/c\",\"C<sub>p</sub>\",\"x\",\"y\",\"z\",\"y/c\",\"z/c\"" << endl;
-          } else
-            Cp_File.open("cp_sections.dat", ios::app);
-
-          if (config->GetGeo_Description() == NACELLE) {
-            su2double theta_deg = atan2(Plane_Normal[1], -Plane_Normal[2])/PI_NUMBER*180 + 180;
-            Cp_File << "ZONE T=\"Theta = " << theta_deg << " deg\", I= " << Xcoord_Airfoil.size() << ", F=POINT" << "\n";
-          }
-          else {
-            if (config->GetSystemMeasurements() == SI) Cp_File << "ZONE T=\"y = " << Plane_P0[1] << " m\", I= "
-              << Xcoord_Airfoil.size() << ", F=POINT" << "\n";
-
-            if (config->GetSystemMeasurements() == US) Cp_File << "ZONE T=\"y = " << Plane_P0[1]*12.0 << " in\", I= "
-              << Xcoord_Airfoil.size() << ", F=POINT" << "\n";
-          }
-
-
-
-          /*--- Coordinates and pressure value ---*/
-
-          for (iVertex = 0; iVertex < Xcoord_Airfoil.size(); iVertex++) {
-
-            su2double XCoord = Xcoord_Airfoil[iVertex];
-            su2double YCoord = Ycoord_Airfoil[iVertex];
-            su2double ZCoord = Zcoord_Airfoil[iVertex];
-
-            /*--- Undo the transformation based on the Theta angle ---*/
-
-            if (config->GetGeo_Description() == NACELLE) {
-              su2double theta_deg = atan2(Plane_Normal[1],-Plane_Normal[2])/PI_NUMBER*180 + 180;
-              su2double Angle = theta_deg*PI_NUMBER/180 - 0.5*PI_NUMBER;
-
-              XCoord = Xcoord_Airfoil[iVertex] + config->GetNacelleLocation(0);
-              YCoord = (Ycoord_Airfoil[iVertex]*cos(Angle) - Zcoord_Airfoil[iVertex]*sin(Angle)) + config->GetNacelleLocation(1);
-              ZCoord = (Zcoord_Airfoil[iVertex]*cos(Angle) + Ycoord_Airfoil[iVertex]*sin(Angle)) + config->GetNacelleLocation(2);
-
-            }
-
-            if (config->GetSystemMeasurements() == US) {
-              Cp_File <<  (Xcoord_Airfoil[iVertex] - Xcoord_LeadingEdge) / Chord  << " " << CPressure_Airfoil[iVertex]
-              << " " << XCoord * 12.0 << " " << YCoord * 12.0 << " " << ZCoord * 12.0
-              << " " << (Ycoord_Airfoil[iVertex] - Ycoord_LeadingEdge) / Chord << " " << (Zcoord_Airfoil[iVertex] - Zcoord_LeadingEdge)  / Chord << "\n";
-            }
-            else {
-              Cp_File << (Xcoord_Airfoil[iVertex] - Xcoord_LeadingEdge) / Chord << " " << CPressure_Airfoil[iVertex]
-              << " " << XCoord << " " << YCoord << " " << ZCoord
-              << " " << (Ycoord_Airfoil[iVertex] - Ycoord_LeadingEdge) / Chord << " " << (Zcoord_Airfoil[iVertex] - Zcoord_LeadingEdge)  / Chord << "\n";
-            }
-
-          }
-
-          Cp_File.close();
-
-        }
-
-        /*--- Compute load distribution ---*/
-
-        ForceInviscid[0] = 0.0; ForceInviscid[1] = 0.0; ForceInviscid[2] = 0.0; MomentInviscid[1] = 0.0;
-
-        for (iVertex = 0; iVertex < Xcoord_Airfoil.size() - 1; iVertex++) {
-
-          NDPressure = 0.5 * (CPressure_Airfoil[iVertex] + CPressure_Airfoil[iVertex + 1]);
-
-          Force[0] = -(Zcoord_Airfoil[iVertex + 1] - Zcoord_Airfoil[iVertex]) * NDPressure;
-          Force[1] = 0.0;
-          Force[2] = (Xcoord_Airfoil[iVertex + 1] - Xcoord_Airfoil[iVertex]) * NDPressure;
-
-          ForceInviscid[0] += Force[0];
-          ForceInviscid[1] += Force[1];
-          ForceInviscid[2] += Force[2];
-
-          MomentDist[0] = 0.5 * (Xcoord_Airfoil[iVertex] + Xcoord_Airfoil[iVertex + 1]) - Origin[0];
-          MomentDist[1] = 0.5 * (Ycoord_Airfoil[iVertex] + Ycoord_Airfoil[iVertex + 1]) - Origin[1];
-          MomentDist[2] = 0.5 * (Zcoord_Airfoil[iVertex] + Zcoord_Airfoil[iVertex + 1]) - Origin[3];
-
-          MomentInviscid[1] += (Force[0] * MomentDist[2] - Force[2] * MomentDist[0]) / RefLength;
-
-        }
-
-        /*--- Compute local chord, for the nondimensionalization  ---*/
-
-        MaxDistance = 0.0; Trailing_Point = 0;
-
-        for (iVertex = 1; iVertex < Xcoord_Airfoil.size(); iVertex++) {
-
-          Distance = sqrt(pow(Xcoord_Airfoil[iVertex] - Xcoord_Airfoil[Trailing_Point], 2.0) +
-                          pow(Ycoord_Airfoil[iVertex] - Ycoord_Airfoil[Trailing_Point], 2.0) +
-                          pow(Zcoord_Airfoil[iVertex] - Zcoord_Airfoil[Trailing_Point], 2.0));
-
-          if (MaxDistance < Distance) { MaxDistance = Distance; }
-
-        }
-
-        Chord = MaxDistance;
-
-        CL_Inv = cos(Dihedral_Trailing * PI_NUMBER / 180.0) * fabs( -ForceInviscid[0] * sin(Alpha) + ForceInviscid[2] * cos(Alpha) )/ Chord;
-
-        /*--- Compute sectional lift at the root ---*/
-
-        B                  = 2.0*config->GetSemiSpan();
-        RefArea            = config->GetRefArea();
-        C_L                = solver->GetTotal_CL();
-        C_L0               = 8.0*C_L*RefArea/(B*PI_NUMBER);
-        Y                  = Ycoord_Airfoil[0];
-        Aux                = Y/(0.5*B);
-        Elliptic_Spanload  = (C_L0 / RefLength) * sqrt(fabs(1.0-Aux*Aux));
-
-
-        /*--- Write load distribution ---*/
-
-        if (output) {
-
-          ofstream Load_File;
-          if (iSection == 0) {
-
-            if ((config->GetTabular_FileFormat() == TAB_OUTPUT::TAB_CSV)) {
-              Load_File.open("load_distribution.csv", ios::out);
-              Load_File << "\"Percent Semispan\",\"Sectional C_L\",\"Spanload (c C_L / c_ref) \",\"Elliptic Spanload\"" << endl;
-            }
-            else {
-              Load_File.open("load_distribution.dat", ios::out);
-              Load_File << "TITLE = \"Load distribution\"" << endl;
-              Load_File << "VARIABLES = \"Percent Semispan\",\"Sectional C<sub>L</sub>\",\"Spanload (c C<sub>L</sub> / c<sub>ref</sub>) \",\"Elliptic Spanload\"" << endl;
-              Load_File << "ZONE T=\"Wing load distribution\"" << endl;
-            }
-          } else {
-            if ((config->GetTabular_FileFormat() == TAB_OUTPUT::TAB_CSV)) Load_File.open("load_distribution.csv", ios::app);
-            else Load_File.open("load_distribution.dat", ios::app);
-          }
-
-
-          /*--- CL and spanload ---*/
-
-          if ((config->GetTabular_FileFormat() == TAB_OUTPUT::TAB_CSV))
-            Load_File << 100.0*Ycoord_Airfoil[0]/(0.5*B) << ", " << CL_Inv  << ", " << Chord*CL_Inv / RefLength <<", " << Elliptic_Spanload   << endl;
-          else
-            Load_File << 100.0*Ycoord_Airfoil[0]/(0.5*B) << " " << CL_Inv  << " " << Chord*CL_Inv / RefLength <<" " << Elliptic_Spanload   << endl;
-
-          Load_File.close();
-
-        }
-
-      }
-
-    }
-
-  }
-
-  /*--- Delete dynamically allocated memory ---*/
-
-  delete[] Plane_P0;
-  delete[] Plane_P0_;
-  delete[] Plane_Normal;
-  delete[] Plane_Normal_;
-  delete[] CPressure;
-
-}
-
-
-void COutputLegacy::SetCpInverseDesign(CSolver *solver_container, CGeometry *geometry, CConfig *config, unsigned long iExtIter) {
-
-  unsigned short iMarker, icommas, Boundary, iDim;
-  unsigned long iVertex, iPoint, (*Point2Vertex)[2], nPointLocal = 0, nPointGlobal = 0;
-  su2double XCoord, YCoord, ZCoord, Pressure, PressureCoeff = 0, Cp, CpTarget, *Normal = nullptr, Area, PressDiff;
-  bool *PointInDomain;
-  string text_line, surfCp_filename;
-  ifstream Surface_file;
-  char buffer[50], cstr[200];
-
-
-  nPointLocal = geometry->GetnPoint();
-#ifdef HAVE_MPI
-  SU2_MPI::Allreduce(&nPointLocal, &nPointGlobal, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
-#else
-  nPointGlobal = nPointLocal;
-#endif
-
-  Point2Vertex = new unsigned long[nPointGlobal][2];
-  PointInDomain = new bool[nPointGlobal];
-
-  for (iPoint = 0; iPoint < nPointGlobal; iPoint ++)
-    PointInDomain[iPoint] = false;
-
-  for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-    Boundary   = config->GetMarker_All_KindBC(iMarker);
-
-    if ((Boundary == EULER_WALL             ) ||
-        (Boundary == HEAT_FLUX              ) ||
-        (Boundary == ISOTHERMAL             ) ||
-        (Boundary == NEARFIELD_BOUNDARY)) {
-      for (iVertex = 0; iVertex < geometry->GetnVertex(iMarker); iVertex++) {
-
-        /*--- The Pressure file uses the global numbering ---*/
-
-#ifndef HAVE_MPI
-        iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
-#else
-        iPoint = geometry->nodes->GetGlobalIndex(geometry->vertex[iMarker][iVertex]->GetNode());
-#endif
-
-        if (geometry->vertex[iMarker][iVertex]->GetNode() < geometry->GetnPointDomain()) {
-          Point2Vertex[iPoint][0] = iMarker;
-          Point2Vertex[iPoint][1] = iVertex;
-          PointInDomain[iPoint] = true;
-          solver_container->SetCPressureTarget(iMarker, iVertex, 0.0);
-        }
-
-      }
-    }
-  }
-
-  /*--- Prepare to read the surface pressure files (CSV) ---*/
-
-  surfCp_filename = "TargetCp";
-  strcpy (cstr, surfCp_filename.c_str());
-
-  /*--- Write file name with extension if unsteady or steady ---*/
-
-  if (((config->GetTime_Marching() != TIME_MARCHING::STEADY) && config->GetTime_Domain()) ||
-       (config->GetTime_Marching() == TIME_MARCHING::HARMONIC_BALANCE)) {
-    if ((SU2_TYPE::Int(iExtIter) >= 0)    && (SU2_TYPE::Int(iExtIter) < 10))    SPRINTF (buffer, "_0000%d.dat", SU2_TYPE::Int(iExtIter));
-    if ((SU2_TYPE::Int(iExtIter) >= 10)   && (SU2_TYPE::Int(iExtIter) < 100))   SPRINTF (buffer, "_000%d.dat",  SU2_TYPE::Int(iExtIter));
-    if ((SU2_TYPE::Int(iExtIter) >= 100)  && (SU2_TYPE::Int(iExtIter) < 1000))  SPRINTF (buffer, "_00%d.dat",   SU2_TYPE::Int(iExtIter));
-    if ((SU2_TYPE::Int(iExtIter) >= 1000) && (SU2_TYPE::Int(iExtIter) < 10000)) SPRINTF (buffer, "_0%d.dat",    SU2_TYPE::Int(iExtIter));
-    if (SU2_TYPE::Int(iExtIter) >= 10000) SPRINTF (buffer, "_%d.dat", SU2_TYPE::Int(iExtIter));
-  }
-  else
-    SPRINTF (buffer, ".dat");
-
-  strcat (cstr, buffer);
-
-  /*--- Read the surface pressure file ---*/
-
-  string::size_type position;
-
-  Surface_file.open(cstr, ios::in);
-
-  if (!(Surface_file.fail())) {
-
-    getline(Surface_file, text_line);
-
-    while (getline(Surface_file, text_line)) {
-      for (icommas = 0; icommas < 50; icommas++) {
-        position = text_line.find( ",", 0 );
-        if (position!=string::npos) text_line.erase (position,1);
-      }
-      stringstream  point_line(text_line);
-
-      if (geometry->GetnDim() == 2) point_line >> iPoint >> XCoord >> YCoord >> Pressure >> PressureCoeff;
-      if (geometry->GetnDim() == 3) point_line >> iPoint >> XCoord >> YCoord >> ZCoord >> Pressure >> PressureCoeff;
-
-      if (PointInDomain[iPoint]) {
-
-        /*--- Find the vertex for the Point and Marker ---*/
-
-        iMarker = Point2Vertex[iPoint][0];
-        iVertex = Point2Vertex[iPoint][1];
-
-        solver_container->SetCPressureTarget(iMarker, iVertex, PressureCoeff);
-
-      }
-
-    }
-
-    Surface_file.close();
-
-  }
-
-  /*--- Compute the pressure difference ---*/
-
-  PressDiff = 0.0;
-  for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-    Boundary   = config->GetMarker_All_KindBC(iMarker);
-
-    if ((Boundary == EULER_WALL             ) ||
-        (Boundary == HEAT_FLUX              ) ||
-        (Boundary == ISOTHERMAL             ) ||
-        (Boundary == NEARFIELD_BOUNDARY)) {
-      for (iVertex = 0; iVertex < geometry->GetnVertex(iMarker); iVertex++) {
-
-        Normal = geometry->vertex[iMarker][iVertex]->GetNormal();
-
-        Cp = solver_container->GetCPressure(iMarker, iVertex);
-        CpTarget = solver_container->GetCPressureTarget(iMarker, iVertex);
-
-        Area = 0.0;
-        for (iDim = 0; iDim < geometry->GetnDim(); iDim++)
-          Area += Normal[iDim]*Normal[iDim];
-        Area = sqrt(Area);
-
-        PressDiff += Area * (CpTarget - Cp) * (CpTarget - Cp);
-      }
-
-    }
-  }
-
-#ifdef HAVE_MPI
-  su2double MyPressDiff = PressDiff;   PressDiff = 0.0;
-  SU2_MPI::Allreduce(&MyPressDiff, &PressDiff, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-#endif
-
-  /*--- Update the total Cp difference coeffient ---*/
-
-  solver_container->SetTotal_CpDiff(PressDiff);
-
-  delete [] Point2Vertex;
-  delete [] PointInDomain;
-
-}
-
-void COutputLegacy::SetHeatFluxInverseDesign(CSolver *solver_container, CGeometry *geometry, CConfig *config, unsigned long iExtIter) {
-
-  unsigned short iMarker, icommas, Boundary, iDim;
-  unsigned long iVertex, iPoint, (*Point2Vertex)[2], nPointLocal = 0, nPointGlobal = 0;
-  su2double XCoord, YCoord, ZCoord, PressureCoeff, HeatFlux = 0.0, HeatFluxDiff, HeatFluxTarget, *Normal = nullptr, Area,
-  Pressure, Cf;
-  bool *PointInDomain;
-  string text_line, surfHeatFlux_filename;
-  ifstream Surface_file;
-  char buffer[50], cstr[200];
-
-
-  nPointLocal = geometry->GetnPoint();
-#ifdef HAVE_MPI
-  SU2_MPI::Allreduce(&nPointLocal, &nPointGlobal, 1, MPI_UNSIGNED_LONG, MPI_SUM, SU2_MPI::GetComm());
-#else
-  nPointGlobal = nPointLocal;
-#endif
-
-  Point2Vertex = new unsigned long[nPointGlobal][2];
-  PointInDomain = new bool[nPointGlobal];
-
-  for (iPoint = 0; iPoint < nPointGlobal; iPoint ++)
-    PointInDomain[iPoint] = false;
-
-  for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-    Boundary   = config->GetMarker_All_KindBC(iMarker);
-
-    if ((Boundary == EULER_WALL             ) ||
-        (Boundary == HEAT_FLUX              ) ||
-        (Boundary == ISOTHERMAL             ) ||
-        (Boundary == NEARFIELD_BOUNDARY)) {
-      for (iVertex = 0; iVertex < geometry->GetnVertex(iMarker); iVertex++) {
-
-        /*--- The Pressure file uses the global numbering ---*/
-
-#ifndef HAVE_MPI
-        iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
-#else
-        iPoint = geometry->nodes->GetGlobalIndex(geometry->vertex[iMarker][iVertex]->GetNode());
-#endif
-
-        if (geometry->vertex[iMarker][iVertex]->GetNode() < geometry->GetnPointDomain()) {
-          Point2Vertex[iPoint][0] = iMarker;
-          Point2Vertex[iPoint][1] = iVertex;
-          PointInDomain[iPoint] = true;
-          solver_container->SetHeatFluxTarget(iMarker, iVertex, 0.0);
-        }
-      }
-    }
-  }
-
-  /*--- Prepare to read the surface pressure files (CSV) ---*/
-
-  surfHeatFlux_filename = "TargetHeatFlux";
-  strcpy (cstr, surfHeatFlux_filename.c_str());
-
-  /*--- Write file name with extension if unsteady or steady ---*/
-
-  if (((config->GetTime_Marching() != TIME_MARCHING::STEADY) && config->GetTime_Domain()) ||
-       (config->GetTime_Marching() == TIME_MARCHING::HARMONIC_BALANCE)) {
-    if ((SU2_TYPE::Int(iExtIter) >= 0)    && (SU2_TYPE::Int(iExtIter) < 10))    SPRINTF (buffer, "_0000%d.dat", SU2_TYPE::Int(iExtIter));
-    if ((SU2_TYPE::Int(iExtIter) >= 10)   && (SU2_TYPE::Int(iExtIter) < 100))   SPRINTF (buffer, "_000%d.dat",  SU2_TYPE::Int(iExtIter));
-    if ((SU2_TYPE::Int(iExtIter) >= 100)  && (SU2_TYPE::Int(iExtIter) < 1000))  SPRINTF (buffer, "_00%d.dat",   SU2_TYPE::Int(iExtIter));
-    if ((SU2_TYPE::Int(iExtIter) >= 1000) && (SU2_TYPE::Int(iExtIter) < 10000)) SPRINTF (buffer, "_0%d.dat",    SU2_TYPE::Int(iExtIter));
-    if (SU2_TYPE::Int(iExtIter) >= 10000) SPRINTF (buffer, "_%d.dat", SU2_TYPE::Int(iExtIter));
-  }
-  else
-    SPRINTF (buffer, ".dat");
-
-  strcat (cstr, buffer);
-
-  /*--- Read the surface pressure file ---*/
-
-  string::size_type position;
-
-  Surface_file.open(cstr, ios::in);
-
-  if (!(Surface_file.fail())) {
-
-    getline(Surface_file, text_line);
-
-    while (getline(Surface_file, text_line)) {
-      for (icommas = 0; icommas < 50; icommas++) {
-        position = text_line.find( ",", 0 );
-        if (position!=string::npos) text_line.erase (position,1);
-      }
-      stringstream  point_line(text_line);
-
-      if (geometry->GetnDim() == 2) point_line >> iPoint >> XCoord >> YCoord >> Pressure >> PressureCoeff >> Cf >> HeatFlux;
-      if (geometry->GetnDim() == 3) point_line >> iPoint >> XCoord >> YCoord >> ZCoord >> Pressure >> PressureCoeff >> Cf >> HeatFlux;
-
-      if (PointInDomain[iPoint]) {
-
-        /*--- Find the vertex for the Point and Marker ---*/
-
-        iMarker = Point2Vertex[iPoint][0];
-        iVertex = Point2Vertex[iPoint][1];
-
-        solver_container->SetHeatFluxTarget(iMarker, iVertex, HeatFlux);
-
-      }
-
-    }
-
-    Surface_file.close();
-  }
-
-  /*--- Compute the pressure difference ---*/
-
-  HeatFluxDiff = 0.0;
-  for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-    Boundary   = config->GetMarker_All_KindBC(iMarker);
-
-    if ((Boundary == EULER_WALL             ) ||
-        (Boundary == HEAT_FLUX              ) ||
-        (Boundary == ISOTHERMAL             ) ||
-        (Boundary == NEARFIELD_BOUNDARY)) {
-      for (iVertex = 0; iVertex < geometry->GetnVertex(iMarker); iVertex++) {
-
-        Normal = geometry->vertex[iMarker][iVertex]->GetNormal();
-
-        HeatFlux = solver_container->GetHeatFlux(iMarker, iVertex);
-        HeatFluxTarget = solver_container->GetHeatFluxTarget(iMarker, iVertex);
-
-        Area = 0.0;
-        for (iDim = 0; iDim < geometry->GetnDim(); iDim++)
-          Area += Normal[iDim]*Normal[iDim];
-        Area = sqrt(Area);
-
-        HeatFluxDiff += Area * (HeatFluxTarget - HeatFlux) * (HeatFluxTarget - HeatFlux);
-
-      }
-
-    }
-  }
-
-#ifdef HAVE_MPI
-  su2double MyHeatFluxDiff = HeatFluxDiff;   HeatFluxDiff = 0.0;
-  SU2_MPI::Allreduce(&MyHeatFluxDiff, &HeatFluxDiff, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-#endif
-
-  /*--- Update the total HeatFlux difference coeffient ---*/
-
-  solver_container->SetTotal_HeatFluxDiff(HeatFluxDiff);
-
-  delete [] Point2Vertex;
-  delete [] PointInDomain;
-
-}
-
-
-
-void COutputLegacy::SpecialOutputDistortion(CSolver *solver, CGeometry *geometry, CConfig *config, bool output) const {
-
-  unsigned short iMarker, iDim, iMarker_Analyze;
-  unsigned long iPoint, iVertex;
-  su2double xCoord = 0.0, yCoord = 0.0, zCoord = 0.0, Area = 0.0, *Vector, TotalArea = 0.0;
-  su2double xCoord_CG = 0.0, yCoord_CG = 0.0, zCoord_CG = 0.0, TipRadius, HubRadius, Distance = 0.0, Distance_Mirror = 0.0;
-  su2double *r, MinDistance, xCoord_ = 0.0, yCoord_ = 0.0, zCoord_ = 0;
-  unsigned short iStation, iAngle, nAngle;
-  char cstr[200];
-  su2double *** ProbeArray, dx = 0.0, dy = 0.0, dz = 0.0, dx_ = 0.0, dy_ = 0.0, dz_ = 0.0, UpVector[3], radians, RotatedVector[3];
-  su2double Pressure, SoundSpeed, Velocity2, Mach,  Gamma, TotalPressure, Mach_Inf, TotalPressure_Inf,
-  Temperature, TotalTemperature, Pressure_Inf, Temperature_Inf, TotalTemperature_Inf, Velocity_Inf, Density;
-  unsigned short nDim = geometry->GetnDim();
-  unsigned short Theta, nStation;
-  unsigned long nVertex_Surface, nLocalVertex_Surface, MaxLocalVertex_Surface;
-  unsigned long Buffer_Send_nVertex[1], *Buffer_Recv_nVertex = nullptr;
-  unsigned long Total_Index;
-  unsigned short Theta_DC60 = 60, nStation_DC60 = 5;
-  su2double PT_Mean, Mach_Mean, q_Mean, PT, q, *PT_Sector, PT_Sector_Min, DC60, *PT_Station, *PT_Station_Min, *Mach_Station, *Mach_Station_Min, IDR, IDC, IDC_Mach;
-
-
-  bool Engine_HalfModel = config->GetEngine_HalfModel();
-  su2double SignFlip = 1.0;
-  su2double Beta, Alpha;
-  su2double Mach_ij, Mach_ip1j, Mach_im1j, Mach_ijp1, Mach_ijm1, Filtered_Mach;
-  su2double Alpha_ij, Alpha_ip1j, Alpha_im1j, Alpha_ijp1, Alpha_ijm1, Filtered_Alpha;
-  su2double Beta_ij, Beta_ip1j, Beta_im1j, Beta_ijp1, Beta_ijm1, Filtered_Beta;
-  su2double a, b, c, d;
-
-  int iProcessor, nProcessor;
-  nProcessor = size;
-
-
-  if (rank == MASTER_NODE && !config->GetDiscrete_Adjoint()) cout << endl << "Writing Surface Analysis file (surface_analysis.dat).";
-
-  /*--- Open and rrite file name with extension if unsteady ---*/
-
-  ofstream SurfFlow_file;
-
-  if (output && (rank == MASTER_NODE)) {
-
-    if ((config->GetTabular_FileFormat() == TAB_OUTPUT::TAB_CSV)) strcpy (cstr, "surface_analysis.vtk");
-    else strcpy (cstr, "surface_analysis.dat");
-
-    SurfFlow_file.precision(15);
-
-    SurfFlow_file.open(cstr, ios::out);
-
-    if ((config->GetTabular_FileFormat() == TAB_OUTPUT::TAB_CSV)) {
-      SurfFlow_file << "# vtk DataFile Version 3.0" << endl;
-      SurfFlow_file << "vtk output" << endl;
-      SurfFlow_file << "ASCII" << endl;
-    }
-    else {
-      SurfFlow_file <<"TITLE = \"Surface Analysis\"" <<endl;
-      SurfFlow_file <<"VARIABLES = \"y(in)\", \"z(in)\", \"PT/PT<sub>inf</sub>\", \"TT/TT<sub>inf</sub>\", \"P/P<sub>inf</sub>\", \"T/T<sub>inf</sub>\", \"v<sub>x</sub>/v<sub>inf</sub>\", \"v<sub>y</sub>/v<sub>inf</sub>\", \"v<sub>z</sub>/v<sub>inf</sub>\", \"<greek>a</greek> (deg)\", \"<greek>b</greek> (deg)\", \"Mach\", \"Filtered <greek>a</greek> (deg)\", \"Filtered <greek>b</greek> (deg)\", \"Filtered Mach\"" << endl;
-    }
-
-  }
-
-  /*--- Loop over all the markers to analyze ---*/
-
-  for (iMarker_Analyze = 0; iMarker_Analyze < config->GetnMarker_Analyze(); iMarker_Analyze++) {
-
-    string Analyze_TagBound = config->GetMarker_Analyze_TagBound(iMarker_Analyze);
-
-    nVertex_Surface = 0; nLocalVertex_Surface = 0; MaxLocalVertex_Surface = 0;
-
-    /*--- Find the max number of surface vertices among all
-     partitions and set up buffers. The master node will handle the
-     writing of the CSV file after gathering all of the data. ---*/
-
-    nLocalVertex_Surface = 0;
-    for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-      string Marker_TagBound = config->GetMarker_All_TagBound(iMarker);
-      if (Marker_TagBound == Analyze_TagBound) {
-        for (iVertex = 0; iVertex < geometry->GetnVertex(iMarker); iVertex++) {
-          iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
-          if (geometry->nodes->GetDomain(iPoint)) nLocalVertex_Surface++;
-        }
-      }
-    }
-
-    /*--- Communicate the number of local vertices on each partition
-     to the master node ---*/
-
-    Buffer_Send_nVertex[0] = nLocalVertex_Surface;
-    if (rank == MASTER_NODE) Buffer_Recv_nVertex = new unsigned long [nProcessor];
-
-#ifdef HAVE_MPI
-    SU2_MPI::Allreduce(&nLocalVertex_Surface, &MaxLocalVertex_Surface, 1, MPI_UNSIGNED_LONG, MPI_MAX, SU2_MPI::GetComm());
-    SU2_MPI::Gather(&Buffer_Send_nVertex, 1, MPI_UNSIGNED_LONG, Buffer_Recv_nVertex, 1, MPI_UNSIGNED_LONG, MASTER_NODE, SU2_MPI::GetComm());
-#else
-    MaxLocalVertex_Surface = nLocalVertex_Surface;
-    Buffer_Recv_nVertex[MASTER_NODE] = Buffer_Send_nVertex[MASTER_NODE];
-#endif
-
-    /*--- Send and Recv buffers ---*/
-
-    su2double *Buffer_Send_Coord_x = nullptr, *Buffer_Recv_Coord_x = nullptr;
-    Buffer_Send_Coord_x = new su2double [MaxLocalVertex_Surface];
-
-    su2double *Buffer_Send_Coord_y = nullptr, *Buffer_Recv_Coord_y = nullptr;
-    Buffer_Send_Coord_y = new su2double [MaxLocalVertex_Surface];
-
-    su2double *Buffer_Send_Coord_z = nullptr, *Buffer_Recv_Coord_z = nullptr;
-    if (nDim == 3)  Buffer_Send_Coord_z = new su2double [MaxLocalVertex_Surface];
-
-    su2double *Buffer_Send_PT = nullptr, *Buffer_Recv_PT = nullptr;
-    Buffer_Send_PT = new su2double [MaxLocalVertex_Surface];
-
-    su2double *Buffer_Send_TT = nullptr, *Buffer_Recv_TT = nullptr;
-    Buffer_Send_TT = new su2double [MaxLocalVertex_Surface];
-
-    su2double *Buffer_Send_P = nullptr, *Buffer_Recv_P = nullptr;
-    Buffer_Send_P = new su2double [MaxLocalVertex_Surface];
-
-    su2double *Buffer_Send_T = nullptr, *Buffer_Recv_T = nullptr;
-    Buffer_Send_T = new su2double [MaxLocalVertex_Surface];
-
-    su2double *Buffer_Send_Mach = nullptr, *Buffer_Recv_Mach = nullptr;
-    Buffer_Send_Mach = new su2double [MaxLocalVertex_Surface];
-
-    su2double *Buffer_Send_Vel_x = nullptr, *Buffer_Recv_Vel_x = nullptr;
-    Buffer_Send_Vel_x = new su2double [MaxLocalVertex_Surface];
-
-    su2double *Buffer_Send_Vel_y = nullptr, *Buffer_Recv_Vel_y = nullptr;
-    Buffer_Send_Vel_y = new su2double [MaxLocalVertex_Surface];
-
-    su2double *Buffer_Send_Vel_z = nullptr, *Buffer_Recv_Vel_z = nullptr;
-    if (nDim == 3) Buffer_Send_Vel_z = new su2double [MaxLocalVertex_Surface];
-
-    su2double *Buffer_Send_q = nullptr, *Buffer_Recv_q = nullptr;
-    Buffer_Send_q = new su2double [MaxLocalVertex_Surface];
-
-    su2double *Buffer_Send_Area = nullptr, *Buffer_Recv_Area = nullptr;
-    Buffer_Send_Area = new su2double [MaxLocalVertex_Surface];
-
-    /*--- Prepare the receive buffers on the master node only. ---*/
-
-    if (rank == MASTER_NODE) {
-      Buffer_Recv_Coord_x = new su2double [nProcessor*MaxLocalVertex_Surface];
-      Buffer_Recv_Coord_y = new su2double [nProcessor*MaxLocalVertex_Surface];
-      if (nDim == 3) Buffer_Recv_Coord_z = new su2double [nProcessor*MaxLocalVertex_Surface];
-      Buffer_Recv_PT = new su2double [nProcessor*MaxLocalVertex_Surface];
-      Buffer_Recv_TT = new su2double [nProcessor*MaxLocalVertex_Surface];
-      Buffer_Recv_P = new su2double [nProcessor*MaxLocalVertex_Surface];
-      Buffer_Recv_T = new su2double [nProcessor*MaxLocalVertex_Surface];
-      Buffer_Recv_Mach = new su2double [nProcessor*MaxLocalVertex_Surface];
-      Buffer_Recv_Vel_x = new su2double [nProcessor*MaxLocalVertex_Surface];
-      Buffer_Recv_Vel_y = new su2double [nProcessor*MaxLocalVertex_Surface];
-      if (nDim == 3) {
-        Buffer_Recv_Vel_z = new su2double [nProcessor*MaxLocalVertex_Surface];
-      }
-      Buffer_Recv_q = new su2double [nProcessor*MaxLocalVertex_Surface];
-      Buffer_Recv_Area = new su2double [nProcessor*MaxLocalVertex_Surface];
-    }
-
-    /*--- Loop over all vertices in this partition and load the
-     data of the specified type into the buffer to be sent to
-     the master node. ---*/
-
-    nVertex_Surface = 0;
-    for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-      string Marker_TagBound = config->GetMarker_All_TagBound(iMarker);
-      if (Marker_TagBound == Analyze_TagBound) {
-
-        for (iVertex = 0; iVertex < geometry->GetnVertex(iMarker); iVertex++) {
-          iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
-
-          if (geometry->nodes->GetDomain(iPoint)) {
-
-            Buffer_Send_Coord_x[nVertex_Surface] = geometry->nodes->GetCoord(iPoint, 0);
-            Buffer_Send_Coord_y[nVertex_Surface] = geometry->nodes->GetCoord(iPoint, 1);
-            if (nDim == 3) { Buffer_Send_Coord_z[nVertex_Surface] = geometry->nodes->GetCoord(iPoint, 2); }
-
-            Pressure         = solver->GetNodes()->GetPressure(iPoint);
-            Density          = solver->GetNodes()->GetDensity(iPoint);
-            Temperature      = solver->GetNodes()->GetTemperature(iPoint);
-            SoundSpeed       = solver->GetNodes()->GetSoundSpeed(iPoint);
-            Velocity2        = solver->GetNodes()->GetVelocity2(iPoint);
-            Mach             = sqrt(Velocity2)/SoundSpeed;
-            Gamma            = config->GetGamma();
-
-            Mach_Inf         = config->GetMach();
-            Pressure_Inf     = config->GetPressure_FreeStreamND();
-            Temperature_Inf  = config->GetTemperature_FreeStreamND();
-            Velocity_Inf     = sqrt(config->GetVelocity_FreeStreamND()[0]*config->GetVelocity_FreeStreamND()[0]
-                                    + config->GetVelocity_FreeStreamND()[1]*config->GetVelocity_FreeStreamND()[1]
-                                    + config->GetVelocity_FreeStreamND()[2]*config->GetVelocity_FreeStreamND()[2]);
-
-            Buffer_Send_P[nVertex_Surface] = Pressure / Pressure_Inf;
-            Buffer_Send_T[nVertex_Surface]     = Temperature / Temperature_Inf;
-            Buffer_Send_Mach[nVertex_Surface] = Mach;
-
-            TotalPressure    = Pressure * pow( 1.0 + Mach * Mach * 0.5 * (Gamma - 1.0), Gamma / (Gamma - 1.0));
-            TotalPressure_Inf  = Pressure_Inf * pow( 1.0 + Mach_Inf * Mach_Inf * 0.5 * (Gamma - 1.0), Gamma / (Gamma - 1.0));
-            Buffer_Send_PT[nVertex_Surface] = TotalPressure / TotalPressure_Inf;
-
-            TotalTemperature = Temperature * (1.0 + Mach * Mach  * 0.5 * (Gamma - 1.0));
-            TotalTemperature_Inf  = Temperature_Inf * (1.0 + Mach * Mach  * 0.5 * (Gamma - 1.0));
-            Buffer_Send_TT[nVertex_Surface] = TotalTemperature / TotalTemperature_Inf;
-
-            Buffer_Send_Vel_x[nVertex_Surface] = solver->GetNodes()->GetVelocity(iPoint,0) / Velocity_Inf;
-            Buffer_Send_Vel_y[nVertex_Surface] = solver->GetNodes()->GetVelocity(iPoint,1) / Velocity_Inf;
-            if (nDim == 3) {
-              Buffer_Send_Vel_z[nVertex_Surface] = solver->GetNodes()->GetVelocity(iPoint,2) / Velocity_Inf;
-            }
-
-            Buffer_Send_q[nVertex_Surface] = 0.5*Density*Velocity2;
-
-            Vector = geometry->vertex[iMarker][iVertex]->GetNormal();
-            Area = 0.0; for (iDim = 0; iDim < nDim; iDim++) { Area += Vector[iDim]*Vector[iDim]; } Area = sqrt(Area);
-            Buffer_Send_Area[nVertex_Surface] = Area;
-
-            /*--- If US system, the output should be in inches ---*/
-
-            if (config->GetSystemMeasurements() == US) {
-
-              Buffer_Send_Coord_x[nVertex_Surface] *= 12.0;
-              Buffer_Send_Coord_y[nVertex_Surface] *= 12.0;
-              if (nDim == 3) Buffer_Send_Coord_z[nVertex_Surface] *= 12.0;
-              Buffer_Send_Area[nVertex_Surface] *= 144.0;
-
-            }
-
-            nVertex_Surface++;
-
-          }
-        }
-        break;
-      }
-    }
-
-    /*--- Send the information to the master node ---*/
-
-#ifdef HAVE_MPI
-
-    SU2_MPI::Gather(Buffer_Send_Coord_x, MaxLocalVertex_Surface, MPI_DOUBLE, Buffer_Recv_Coord_x, MaxLocalVertex_Surface, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Gather(Buffer_Send_Coord_y, MaxLocalVertex_Surface, MPI_DOUBLE, Buffer_Recv_Coord_y, MaxLocalVertex_Surface, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    if (nDim == 3) SU2_MPI::Gather(Buffer_Send_Coord_z, MaxLocalVertex_Surface, MPI_DOUBLE, Buffer_Recv_Coord_z, MaxLocalVertex_Surface, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Gather(Buffer_Send_PT, MaxLocalVertex_Surface, MPI_DOUBLE, Buffer_Recv_PT, MaxLocalVertex_Surface, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Gather(Buffer_Send_TT, MaxLocalVertex_Surface, MPI_DOUBLE, Buffer_Recv_TT, MaxLocalVertex_Surface, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Gather(Buffer_Send_P, MaxLocalVertex_Surface, MPI_DOUBLE, Buffer_Recv_P, MaxLocalVertex_Surface, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Gather(Buffer_Send_T, MaxLocalVertex_Surface, MPI_DOUBLE, Buffer_Recv_T, MaxLocalVertex_Surface, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Gather(Buffer_Send_Mach, MaxLocalVertex_Surface, MPI_DOUBLE, Buffer_Recv_Mach, MaxLocalVertex_Surface, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Gather(Buffer_Send_Vel_x, MaxLocalVertex_Surface, MPI_DOUBLE, Buffer_Recv_Vel_x, MaxLocalVertex_Surface, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Gather(Buffer_Send_Vel_y, MaxLocalVertex_Surface, MPI_DOUBLE, Buffer_Recv_Vel_y, MaxLocalVertex_Surface, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    if (nDim == 3) SU2_MPI::Gather(Buffer_Send_Vel_z, MaxLocalVertex_Surface, MPI_DOUBLE, Buffer_Recv_Vel_z, MaxLocalVertex_Surface, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Gather(Buffer_Send_q, MaxLocalVertex_Surface, MPI_DOUBLE, Buffer_Recv_q, MaxLocalVertex_Surface, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-    SU2_MPI::Gather(Buffer_Send_Area, MaxLocalVertex_Surface, MPI_DOUBLE, Buffer_Recv_Area, MaxLocalVertex_Surface, MPI_DOUBLE, MASTER_NODE, SU2_MPI::GetComm());
-
-#else
-
-    for (iVertex = 0; iVertex < MaxLocalVertex_Surface; iVertex++) {
-      Buffer_Recv_Coord_x[iVertex] = Buffer_Send_Coord_x[iVertex];
-      Buffer_Recv_Coord_y[iVertex] = Buffer_Send_Coord_y[iVertex];
-      if (nDim == 3) Buffer_Recv_Coord_z[iVertex] = Buffer_Send_Coord_z[iVertex];
-      Buffer_Recv_PT[iVertex] = Buffer_Send_PT[iVertex];
-      Buffer_Recv_TT[iVertex] = Buffer_Send_TT[iVertex];
-      Buffer_Recv_P[iVertex] = Buffer_Send_P[iVertex];
-      Buffer_Recv_T[iVertex] = Buffer_Send_T[iVertex];
-      Buffer_Recv_Mach[iVertex] = Buffer_Send_Mach[iVertex];
-      Buffer_Recv_Vel_x[iVertex] = Buffer_Send_Vel_x[iVertex];
-      Buffer_Recv_Vel_y[iVertex] = Buffer_Send_Vel_y[iVertex];
-      if (nDim == 3) Buffer_Recv_Vel_z[iVertex] = Buffer_Send_Vel_z[iVertex];
-      Buffer_Recv_q[iVertex] = Buffer_Send_q[iVertex];
-      Buffer_Recv_Area[iVertex] = Buffer_Send_Area[iVertex];
-    }
-
-#endif
-
-    if (rank == MASTER_NODE) {
-
-      /*--- Compute the location of the critical points of the distortion measure, and center of gravity ---*/
-
-      TotalArea = 0.0; xCoord_CG = 0.0; yCoord_CG = 0.0; zCoord_CG = 0.0; PT_Mean = 0.0; Mach_Mean = 0.0;  q_Mean = 0.0;
-
-      for (iProcessor = 0; iProcessor < nProcessor; iProcessor++) {
-        for (iVertex = 0; iVertex < Buffer_Recv_nVertex[iProcessor]; iVertex++) {
-
-          /*--- Current index position and global index ---*/
-
-          Total_Index = iProcessor*MaxLocalVertex_Surface+iVertex;
-
-          /*--- Retrieve the merged data for this node ---*/
-
-          xCoord = Buffer_Recv_Coord_x[Total_Index];
-          yCoord = Buffer_Recv_Coord_y[Total_Index];
-          if (nDim == 3) zCoord = Buffer_Recv_Coord_z[Total_Index];
-          PT   = Buffer_Recv_PT[Total_Index];
-          Mach = Buffer_Recv_Mach[Total_Index];
-          q    = Buffer_Recv_q[Total_Index];
-
-          Area       = Buffer_Recv_Area[Total_Index];
-          TotalArea += Area;
-          xCoord_CG += xCoord*Area;
-          yCoord_CG += yCoord*Area;
-          zCoord_CG += zCoord*Area;
-          PT_Mean   += PT*Area;
-          Mach_Mean += PT*Area;
-          q_Mean    += q*Area;
-
-        }
-      }
-
-      /*--- Evaluate the area averaged pressure and CG ---*/
-
-      xCoord_CG = xCoord_CG / TotalArea;
-      yCoord_CG = yCoord_CG / TotalArea;
-      zCoord_CG = zCoord_CG / TotalArea;
-      PT_Mean   /= TotalArea;
-      Mach_Mean /= TotalArea;
-      q_Mean    /=  TotalArea;
-
-      /*--- If it is a half model, CGy = 0 ---*/
-
-      if (Engine_HalfModel) { yCoord_CG = 0.0; }
-
-      /*--- Compute hub and tip radius ---*/
-
-      TipRadius = 1E-6; HubRadius = 1E6;
-      for (iProcessor = 0; iProcessor < nProcessor; iProcessor++) {
-        for (iVertex = 0; iVertex < Buffer_Recv_nVertex[iProcessor]; iVertex++) {
-
-          /*--- Current index position and global index ---*/
-
-          Total_Index = iProcessor*MaxLocalVertex_Surface+iVertex;
-
-          /*--- Retrieve the merged data for this node ---*/
-
-          xCoord = Buffer_Recv_Coord_x[Total_Index];
-          yCoord = Buffer_Recv_Coord_y[Total_Index];
-          if (nDim == 3) zCoord = Buffer_Recv_Coord_z[Total_Index];
-
-          if (nDim == 2)
-            Distance = sqrt((xCoord_CG-xCoord)*(xCoord_CG-xCoord) +
-                            (yCoord_CG-yCoord)*(yCoord_CG-yCoord));
-
-          if (nDim == 3)
-            Distance = sqrt((xCoord_CG-xCoord)*(xCoord_CG-xCoord) +
-                            (yCoord_CG-yCoord)*(yCoord_CG-yCoord) +
-                            (zCoord_CG-zCoord)*(zCoord_CG-zCoord));
-
-          if (Distance > TipRadius) TipRadius = Distance;
-          if (Distance < HubRadius) HubRadius = Distance;
-
-        }
-      }
-
-      if (HubRadius/TipRadius < 0.05) HubRadius = 0.0;
-
-      /*--- Evaluate the DC60 parameter ---*/
-
-      Theta = Theta_DC60;
-      nStation = nStation_DC60;
-
-      nAngle = SU2_TYPE::Int(360/float(Theta));
-      r = new su2double [nStation+1];
-
-      /*--- Allocate memory ---*/
-
-      PT_Sector = new su2double [nAngle];
-      ProbeArray = new su2double ** [nAngle];
-      for (iAngle = 0; iAngle < nAngle; iAngle++) {
-        ProbeArray[iAngle] = new su2double * [nStation];
-        for (iStation = 0; iStation < nStation; iStation++) {
-          ProbeArray[iAngle][iStation] = new su2double [5];
-        }
-      }
-
-      /*--- Define the radius for each probe ---*/
-
-      r[0] = HubRadius; r[nStation] = TipRadius;
-      for (iStation = 1; iStation < nStation; iStation++) {
-        r[iStation] = sqrt(  r[iStation-1]*r[iStation-1] + (r[nStation]*r[nStation] - r[0]*r[0])/float(nStation) );
-      }
-
-      /*--- Define the probe rack ---*/
-
-      UpVector[0] = 0.0; UpVector[1] = 0.0; UpVector[2] = 1.0;
-
-      for (iAngle = 0; iAngle < nAngle; iAngle++) {
-
-        radians = -iAngle*Theta*2.0*PI_NUMBER/360;
-        RotatedVector[0] =  UpVector[0];
-        RotatedVector[1] =  UpVector[1] * cos(radians) - UpVector[2] * sin(radians);
-        RotatedVector[2] =  UpVector[1] * sin(radians) + UpVector[2] * cos(radians);
-
-        for (iStation = 1; iStation <= nStation; iStation++) {
-          ProbeArray[iAngle][iStation-1][0] = xCoord_CG+RotatedVector[0]*sqrt(0.5*(r[iStation]*r[iStation]+r[iStation-1]*r[iStation-1]));
-          ProbeArray[iAngle][iStation-1][1] = yCoord_CG+RotatedVector[1]*sqrt(0.5*(r[iStation]*r[iStation]+r[iStation-1]*r[iStation-1]));
-          ProbeArray[iAngle][iStation-1][2] = zCoord_CG+RotatedVector[2]*sqrt(0.5*(r[iStation]*r[iStation]+r[iStation-1]*r[iStation-1]));
-        }
-
-      }
-
-      /*--- Compute the Total pressure at each probe, closes grid point to the location ---*/
-
-      for (iAngle = 0; iAngle < nAngle; iAngle++) {
-
-        for (iStation = 0; iStation < nStation; iStation++) {
-          xCoord_ = ProbeArray[iAngle][iStation][0];
-          yCoord_ = ProbeArray[iAngle][iStation][1];
-          zCoord_ = ProbeArray[iAngle][iStation][2];
-
-          MinDistance = 1E6;
-
-          for (iProcessor = 0; iProcessor < nProcessor; iProcessor++) {
-            for (iVertex = 0; iVertex < Buffer_Recv_nVertex[iProcessor]; iVertex++) {
-
-              Total_Index = iProcessor*MaxLocalVertex_Surface+iVertex;
-              xCoord = Buffer_Recv_Coord_x[Total_Index];
-              yCoord = Buffer_Recv_Coord_y[Total_Index];
-              if (nDim == 3) zCoord = Buffer_Recv_Coord_z[Total_Index];
-
-              dx = (xCoord_ - xCoord); dy = (yCoord_ - yCoord);
-              if (nDim == 3) dz = (zCoord_ - zCoord);
-
-              Distance = dx*dx + dy*dy; if (nDim == 3) Distance += dz*dz; Distance = sqrt(Distance);
-
-              if (Engine_HalfModel) {
-
-                yCoord = -yCoord;
-
-                dx_ = (xCoord_ - xCoord); dy_ = (yCoord_ - yCoord);
-                if (nDim == 3) dz_ = (zCoord_ - zCoord);
-
-                Distance_Mirror = dx_*dx_ + dy_*dy_;
-                if (nDim == 3) Distance_Mirror += dz_*dz_;
-                Distance_Mirror = sqrt(Distance_Mirror);
-
-                if (Distance_Mirror < Distance) {
-                  Distance = Distance_Mirror;
-                  dx = dx_; dy = dy_;
-                  if (nDim == 3) dz = dz_;
-                }
-
-              }
-
-              if (Distance <= MinDistance) {
-                MinDistance = Distance;
-                ProbeArray[iAngle][iStation][3] = Buffer_Recv_PT[Total_Index];
-                ProbeArray[iAngle][iStation][4] = Buffer_Recv_q[Total_Index];
-              }
-
-            }
-          }
-
-        }
-
-      }
-
-      /*--- Evaluate the average pressure at each sector, fan face and dynamic pressure ---*/
-
-      PT_Mean = 0.0; q_Mean = 0.0;
-      for (iAngle = 0; iAngle < nAngle; iAngle++) {
-        PT_Sector[iAngle] = 0.0;
-        for (iStation = 0; iStation < nStation; iStation++) {
-          PT_Sector[iAngle] += ProbeArray[iAngle][iStation][3]/float(nStation);
-          PT_Mean           += ProbeArray[iAngle][iStation][3]/float(nStation*nAngle);
-          q_Mean            += ProbeArray[iAngle][iStation][4]/float(nStation*nAngle);
-        }
-      }
-
-      /*--- Compute the min value of the averaged pressure at each sector ---*/
-
-      PT_Sector_Min = PT_Sector[0];
-      for (iAngle = 1; iAngle < nAngle; iAngle++) {
-        if (PT_Sector[iAngle] <= PT_Sector_Min) PT_Sector_Min = PT_Sector[iAngle];
-      }
-
-      /*--- Set the value of the distortion, it only works for one surface ---*/
-
-      Mach_Inf           = config->GetMach();
-      Gamma              = config->GetGamma();
-      TotalPressure_Inf  = config->GetPressure_FreeStreamND() * pow( 1.0 + Mach_Inf * Mach_Inf *
-                                                                    0.5 * (Gamma - 1.0), Gamma    / (Gamma - 1.0));
-
-      if (q_Mean != 0.0) DC60 = ((PT_Mean - PT_Sector_Min)*TotalPressure_Inf)/q_Mean;
-      else DC60 = 0.0;
-
-      config->SetSurface_DC60(iMarker_Analyze, DC60);
-
-      solver->SetTotal_DC60(DC60);
-
-      /*--- Deallocate the memory ---*/
-
-      delete[] r;
-
-      delete [] PT_Sector;
-
-      for (iAngle = 0; iAngle < nAngle; iAngle++) {
-        for (iStation = 0; iStation < nStation; iStation++) {
-          delete[] ProbeArray[iAngle][iStation];
-        }
-      }
-      delete[] ProbeArray;
-
-
-      /*--- Evaluate the IDC, and IDR parameters ---*/
-
-      nStation = SU2_TYPE::Int(config->GetDistortionRack()[0]);
-      Theta = SU2_TYPE::Int(config->GetDistortionRack()[1]);
-      nAngle = SU2_TYPE::Int(360/float(Theta));
-
-      /*--- Allocate memory ---*/
-
-      r = new su2double [nStation+1];
-      ProbeArray = new su2double ** [nAngle];
-      for (iAngle = 0; iAngle < nAngle; iAngle++) {
-        ProbeArray[iAngle] = new su2double * [nStation];
-        for (iStation = 0; iStation < nStation; iStation++) {
-          ProbeArray[iAngle][iStation] = new su2double [4];
-        }
-      }
-
-      /*--- Define the radius for each probe ---*/
-
-      r[0] = HubRadius; r[nStation] = TipRadius;
-      for (iStation = 1; iStation < nStation; iStation++) {
-        r[iStation] = sqrt(  r[iStation-1]*r[iStation-1] + (r[nStation]*r[nStation] - r[0]*r[0])/float(nStation) );
-      }
-
-      /*--- Define the probe rack ---*/
-
-      UpVector[0] = 0.0; UpVector[1] = 0.0; UpVector[2] = 1.0;
-
-      for (iAngle = 0; iAngle < nAngle; iAngle++) {
-
-        radians = -iAngle*Theta*2.0*PI_NUMBER/360;
-        RotatedVector[0] =  UpVector[0];
-        RotatedVector[1] =  UpVector[1] * cos(radians) - UpVector[2] * sin(radians);
-        RotatedVector[2] =  UpVector[1] * sin(radians) + UpVector[2] * cos(radians);
-
-        for (iStation = 1; iStation <= nStation; iStation++) {
-          ProbeArray[iAngle][iStation-1][0] = xCoord_CG+RotatedVector[0]*sqrt(0.5*(r[iStation]*r[iStation]+r[iStation-1]*r[iStation-1]));
-          ProbeArray[iAngle][iStation-1][1] = yCoord_CG+RotatedVector[1]*sqrt(0.5*(r[iStation]*r[iStation]+r[iStation-1]*r[iStation-1]));
-          ProbeArray[iAngle][iStation-1][2] = zCoord_CG+RotatedVector[2]*sqrt(0.5*(r[iStation]*r[iStation]+r[iStation-1]*r[iStation-1]));
-        }
-
-      }
-
-      /*--- Compute the Total pressure at each probe, closes grid point to the location ---*/
-
-      for (iAngle = 0; iAngle < nAngle; iAngle++) {
-        for (iStation = 0; iStation < nStation; iStation++) {
-          xCoord_ = ProbeArray[iAngle][iStation][0];
-          yCoord_ = ProbeArray[iAngle][iStation][1];
-          zCoord_ = ProbeArray[iAngle][iStation][2];
-
-          MinDistance = 1E6;
-
-          for (iProcessor = 0; iProcessor < nProcessor; iProcessor++) {
-            for (iVertex = 0; iVertex < Buffer_Recv_nVertex[iProcessor]; iVertex++) {
-
-              Total_Index = iProcessor*MaxLocalVertex_Surface+iVertex;
-              xCoord = Buffer_Recv_Coord_x[Total_Index];
-              yCoord = Buffer_Recv_Coord_y[Total_Index];
-              if (nDim == 3) zCoord = Buffer_Recv_Coord_z[Total_Index];
-
-              dx = (xCoord_ - xCoord); dy = (yCoord_ - yCoord);
-              if (nDim == 3) dz = (zCoord_ - zCoord);
-
-              Distance = dx*dx + dy*dy; if (nDim == 3) Distance += dz*dz; Distance = sqrt(Distance);
-
-              if (Engine_HalfModel) {
-
-                yCoord = -yCoord;
-
-                dx_ = (xCoord_ - xCoord); dy_ = (yCoord_ - yCoord);
-                if (nDim == 3) dz_ = (zCoord_ - zCoord);
-
-                Distance_Mirror = dx_*dx_ + dy_*dy_;
-                if (nDim == 3) Distance_Mirror += dz_*dz_;
-                Distance_Mirror = sqrt(Distance_Mirror);
-
-                if (Distance_Mirror < Distance) {
-                  Distance = Distance_Mirror;
-                  dx = dx_; dy = dy_;
-                  if (nDim == 3) dz = dz_;
-                }
-
-              }
-
-              if (Distance <= MinDistance) {
-                MinDistance = Distance;
-                ProbeArray[iAngle][iStation][3] = Buffer_Recv_PT[Total_Index];
-              }
-
-            }
-          }
-
-        }
-
-      }
-
-      /*--- Evaluate the average and min. pressure at each station/radius and fan  ---*/
-
-      PT_Station = new su2double [nStation];
-      PT_Station_Min = new su2double [nStation];
-
-      PT_Mean = 0.0;
-      for (iStation = 0; iStation < nStation; iStation++) {
-        PT_Station[iStation] = 0.0;
-        PT_Station_Min[iStation] = ProbeArray[0][iStation][3];
-        for (iAngle = 0; iAngle < nAngle; iAngle++) {
-          PT = ProbeArray[iAngle][iStation][3];
-          PT_Station[iStation] += PT / float(nAngle);
-          if (PT <= PT_Station_Min[iStation] ) PT_Station_Min[iStation] = PT;
-          PT_Mean += ProbeArray[iAngle][iStation][3]/float(nStation*nAngle);
-        }
-      }
-
-      /*--- Set the value of the distortion, it only works for one surface ---*/
-
-      IDC = 0.0;
-      for (iStation = 0; iStation < nStation-1; iStation++) {
-        IDC = max (IDC, 0.5*((PT_Station[iStation] - PT_Station_Min[iStation])/PT_Mean
-                             + (PT_Station[iStation+1] - PT_Station_Min[iStation+1])/PT_Mean) );
-
-      }
-
-      config->SetSurface_IDC(iMarker_Analyze, IDC);
-      solver->SetTotal_IDC(IDC);
-
-      IDR = 0.0;
-      for (iStation = 0; iStation < nStation; iStation++) {
-        IDR = max (IDR, (PT_Mean-PT_Station[iStation])/PT_Mean);
-      }
-
-      config->SetSurface_IDR(iMarker_Analyze, IDR);
-
-      solver->SetTotal_IDR(IDR);
-
-      /*--- Release IDX parameters ---*/
-
-      delete [] PT_Station_Min;
-      delete [] PT_Station;
-
-      /*--- Evaluate the IDC Mach parameter ---*/
-
-      /*--- Compute the Mach number at each probe, closes grid point to the location ---*/
-
-      for (iAngle = 0; iAngle < nAngle; iAngle++) {
-        for (iStation = 0; iStation < nStation; iStation++) {
-          xCoord_ = ProbeArray[iAngle][iStation][0];
-          yCoord_ = ProbeArray[iAngle][iStation][1];
-          zCoord_ = ProbeArray[iAngle][iStation][2];
-
-          MinDistance = 1E6;
-
-          for (iProcessor = 0; iProcessor < nProcessor; iProcessor++) {
-            for (iVertex = 0; iVertex < Buffer_Recv_nVertex[iProcessor]; iVertex++) {
-
-              Total_Index = iProcessor*MaxLocalVertex_Surface+iVertex;
-
-              xCoord = Buffer_Recv_Coord_x[Total_Index];
-              yCoord = Buffer_Recv_Coord_y[Total_Index];
-              if (nDim == 3) zCoord = Buffer_Recv_Coord_z[Total_Index];
-
-              dx = (xCoord_ - xCoord); dy = (yCoord_ - yCoord);
-              if (nDim == 3) dz = (zCoord_ - zCoord);
-
-              Distance = dx*dx + dy*dy;
-              if (nDim == 3) Distance += dz*dz;
-              Distance = sqrt(Distance);
-
-              if (Engine_HalfModel) {
-
-                yCoord = -yCoord;
-
-                dx_ = (xCoord_ - xCoord); dy_ = (yCoord_ - yCoord);
-                if (nDim == 3) dz_ = (zCoord_ - zCoord);
-
-                Distance_Mirror = dx_*dx_ + dy_*dy_;
-                if (nDim == 3) Distance_Mirror += dz_*dz_;
-                Distance_Mirror = sqrt(Distance_Mirror);
-
-                if (Distance_Mirror < Distance) {
-                  Distance = Distance_Mirror;
-                  dx = dx_; dy = dy_;
-                  if (nDim == 3) dz = dz_;
-                }
-
-              }
-
-              if (Distance <= MinDistance) {
-                MinDistance = Distance;
-                ProbeArray[iAngle][iStation][3] = Buffer_Recv_Mach[Total_Index];
-              }
-
-            }
-          }
-
-        }
-
-      }
-
-      /*--- Evaluate the average and min. pressure at each station/radius and fan face ---*/
-
-      Mach_Station = new su2double [nStation];
-      Mach_Station_Min = new su2double [nStation];
-
-      Mach_Mean = 0.0;
-      for (iStation = 0; iStation < nStation; iStation++) {
-        Mach_Station[iStation] = 0.0;
-        Mach_Station_Min[iStation] = ProbeArray[0][iStation][3];
-        for (iAngle = 0; iAngle < nAngle; iAngle++) {
-          Mach = ProbeArray[iAngle][iStation][3];
-          Mach_Station[iStation] += Mach / float(nAngle);
-          if (Mach <= Mach_Station_Min[iStation] ) Mach_Station_Min[iStation] = Mach;
-          Mach_Mean += ProbeArray[iAngle][iStation][3]/float(nStation*nAngle);
-        }
-      }
-
-      /*--- Set the value of the distortion, it only works for one surface ---*/
-
-      IDC_Mach = 0.0;
-      for (iStation = 0; iStation < nStation-1; iStation++) {
-        if (Mach_Mean != 0)
-          IDC_Mach = max (IDC_Mach, 0.5*((Mach_Station[iStation] - Mach_Station_Min[iStation])/Mach_Mean
-                                         + (Mach_Station[iStation+1] - Mach_Station_Min[iStation+1])/Mach_Mean)   );
-
-      }
-
-      config->SetSurface_IDC_Mach(iMarker_Analyze, IDC_Mach);
-
-      solver->SetTotal_IDC_Mach(IDC_Mach);
-
-      delete [] Mach_Station_Min;
-      delete [] Mach_Station;
-
-      /*--- Release distortion parameters ---*/
-
-      delete[] r;
-      for (iAngle = 0; iAngle < nAngle; iAngle++) {
-        for (iStation = 0; iStation < nStation; iStation++) {
-          delete[] ProbeArray[iAngle][iStation];
-        }
-      }
-      delete[] ProbeArray;
-
-      /*--- Create the distortion plot ---*/
-
-      Theta = 10; nStation = 20;
-
-      nAngle = SU2_TYPE::Int(360/float(Theta));
-      r = new su2double [nStation+1];
-
-      /*--- Allocate memory ---*/
-
-      ProbeArray = new su2double ** [nAngle];
-      for (iAngle = 0; iAngle < nAngle; iAngle++) {
-        ProbeArray[iAngle] = new su2double * [nStation];
-        for (iStation = 0; iStation < nStation; iStation++) {
-          ProbeArray[iAngle][iStation] = new su2double [11];
-        }
-      }
-
-      /*--- Define the radius for each probe ---*/
-
-      r[0] = HubRadius;
-      r[nStation] = TipRadius;
-
-      for (iStation = 1; iStation < nStation; iStation++) {
-        r[iStation] = sqrt(  r[iStation-1]*r[iStation-1] + (r[nStation]*r[nStation] - r[0]*r[0])/float(nStation) );
-      }
-
-      /*--- Define the probe rack ---*/
-
-      UpVector[0] = 0.0; UpVector[1] = 0.0; UpVector[2] = 1.0;
-
-      for (iAngle = 0; iAngle < nAngle; iAngle++) {
-
-        radians = -iAngle*Theta*2.0*PI_NUMBER/360;
-        RotatedVector[0] =  UpVector[0];
-        RotatedVector[1] =  UpVector[1] * cos(radians) - UpVector[2] * sin(radians);
-        RotatedVector[2] =  UpVector[1] * sin(radians) + UpVector[2] * cos(radians);
-
-        for (iStation = 1; iStation <= nStation; iStation++) {
-          ProbeArray[iAngle][iStation-1][0] = xCoord_CG+RotatedVector[0]*sqrt(0.5*(r[iStation]*r[iStation]+r[iStation-1]*r[iStation-1]));
-          ProbeArray[iAngle][iStation-1][1] = yCoord_CG+RotatedVector[1]*sqrt(0.5*(r[iStation]*r[iStation]+r[iStation-1]*r[iStation-1]));
-          ProbeArray[iAngle][iStation-1][2] = zCoord_CG+RotatedVector[2]*sqrt(0.5*(r[iStation]*r[iStation]+r[iStation-1]*r[iStation-1]));
-        }
-
-      }
-
-      /*--- Compute the primitieve variables, closest grid point to the location + gradient ---*/
-
-      for (iAngle = 0; iAngle < nAngle; iAngle++) {
-        for (iStation = 0; iStation < nStation; iStation++) {
-          xCoord_ = ProbeArray[iAngle][iStation][0];
-          yCoord_ = ProbeArray[iAngle][iStation][1];
-          zCoord_ = ProbeArray[iAngle][iStation][2];
-
-          MinDistance = 1E6;
-
-          for (iProcessor = 0; iProcessor < nProcessor; iProcessor++) {
-            for (iVertex = 0; iVertex < Buffer_Recv_nVertex[iProcessor]; iVertex++) {
-
-              Total_Index = iProcessor*MaxLocalVertex_Surface+iVertex;
-              xCoord = Buffer_Recv_Coord_x[Total_Index];
-              yCoord = Buffer_Recv_Coord_y[Total_Index];
-              if (nDim == 3) zCoord = Buffer_Recv_Coord_z[Total_Index];
-
-              dx = (xCoord_ - xCoord); dy = (yCoord_ - yCoord);
-              if (nDim == 3) dz = (zCoord_ - zCoord);
-
-              Distance = dx*dx + dy*dy; if (nDim == 3) Distance += dz*dz; Distance = sqrt(Distance);
-
-              SignFlip = 1.0;
-
-              if (Engine_HalfModel) {
-
-                yCoord = -yCoord;
-
-                dx_ = (xCoord_ - xCoord);
-                dy_ = (yCoord_ - yCoord);
-                if (nDim == 3) dz_ = (zCoord_ - zCoord);
-
-                Distance_Mirror = dx_*dx_ + dy_*dy_;
-                if (nDim == 3) Distance_Mirror += dz_*dz_;
-                Distance_Mirror = sqrt(Distance_Mirror);
-
-                if (Distance_Mirror < Distance) {
-                  SignFlip = -1.0;
-                  Distance = Distance_Mirror;
-                  dx = dx_; dy = dy_;
-                  if (nDim == 3) dz = dz_;
-                }
-
-              }
-
-
-              if (Distance <= MinDistance) {
-                MinDistance = Distance;
-                ProbeArray[iAngle][iStation][3] = Buffer_Recv_PT[Total_Index];
-                ProbeArray[iAngle][iStation][4] = Buffer_Recv_TT[Total_Index];
-                ProbeArray[iAngle][iStation][5] = Buffer_Recv_P[Total_Index];
-                ProbeArray[iAngle][iStation][6] = Buffer_Recv_T[Total_Index];
-                ProbeArray[iAngle][iStation][7] = Buffer_Recv_Mach[Total_Index];
-                ProbeArray[iAngle][iStation][8] = Buffer_Recv_Vel_x[Total_Index];
-                ProbeArray[iAngle][iStation][9] =  SignFlip * Buffer_Recv_Vel_y[Total_Index];
-                if (nDim == 3) ProbeArray[iAngle][iStation][10] = Buffer_Recv_Vel_z[Total_Index];
-              }
-
-            }
-          }
-
-        }
-
-      }
-
-      /*--- Reverse in the Y direction to move the solution from 3D to 2D ---*/
-
-      yCoord_CG = -yCoord_CG;
-      for (iAngle = 0; iAngle < nAngle; iAngle++) {
-        for (iStation = 0; iStation < nStation; iStation++) {
-          ProbeArray[iAngle][iStation][9] = -ProbeArray[iAngle][iStation][9];
-          ProbeArray[iAngle][iStation][1] = -ProbeArray[iAngle][iStation][1];
-        }
-      }
-
-      if (output) {
-
-        if (config->GetTabular_FileFormat() == TAB_OUTPUT::TAB_CSV) {
-
-          SurfFlow_file << "\nDATASET UNSTRUCTURED_GRID" << endl;
-          SurfFlow_file <<"POINTS " << nAngle*nStation << " float" << endl;
-          for (iAngle = 0; iAngle < nAngle; iAngle++) {
-            for (iStation = 0; iStation < nStation; iStation++) {
-              SurfFlow_file << ProbeArray[iAngle][iStation][1]-yCoord_CG << " " << ProbeArray[iAngle][iStation][2]-zCoord_CG << " 0.0 " <<" ";
-            }
-          }
-
-          SurfFlow_file <<"\nCELLS " << nAngle*(nStation-1) <<" "<< nAngle*(nStation-1)*5 << endl;
-          for (iAngle = 0; iAngle < nAngle; iAngle++) {
-            for (iStation = 0; iStation < nStation-1; iStation++) {
-              a = iAngle*nStation+iStation; b = a + nStation; c = b+1; d = a +1;
-              if (iAngle == nAngle-1) { b = iStation; c = b+1;   }
-              SurfFlow_file << "4 " << a  <<" "<< b <<" "<< c <<" "<< d <<" ";
-            }
-          }
-
-          SurfFlow_file <<"\nCELL_TYPES " << nAngle*(nStation-1) << endl;
-          for (iAngle = 0; iAngle < nAngle; iAngle++) {
-            for (iStation = 0; iStation < nStation-1; iStation++) {
-              SurfFlow_file << "9 " ;
-            }
-          }
-
-          SurfFlow_file <<"\nPOINT_DATA " << nAngle*nStation << endl;
-          SurfFlow_file <<"SCALARS PT/PT_inf float" << endl;
-          SurfFlow_file <<"LOOKUP_TABLE default" << endl;
-
-          for (iAngle = 0; iAngle < nAngle; iAngle++) {
-            for (iStation = 0; iStation < nStation; iStation++) {
-              SurfFlow_file << ProbeArray[iAngle][iStation][3] << " ";
-            }
-          }
-
-          SurfFlow_file <<"SCALARS TT/TT_inf float" << endl;
-          SurfFlow_file <<"LOOKUP_TABLE default" << endl;
-
-          for (iAngle = 0; iAngle < nAngle; iAngle++) {
-            for (iStation = 0; iStation < nStation; iStation++) {
-              SurfFlow_file << ProbeArray[iAngle][iStation][4] << " ";
-            }
-          }
-
-          SurfFlow_file <<"SCALARS Alpha float" << endl;
-          SurfFlow_file <<"LOOKUP_TABLE default" << endl;
-
-          for (iAngle = 0; iAngle < nAngle; iAngle++) {
-            for (iStation = 0; iStation < nStation; iStation++) {
-              Alpha = atan(ProbeArray[iAngle][iStation][10]/ProbeArray[iAngle][iStation][8])*360.0/(2.0*PI_NUMBER);
-              SurfFlow_file << Alpha << " ";
-            }
-          }
-
-          SurfFlow_file <<"SCALARS Beta float" << endl;
-          SurfFlow_file <<"LOOKUP_TABLE default" << endl;
-
-          for (iAngle = 0; iAngle < nAngle; iAngle++) {
-            for (iStation = 0; iStation < nStation; iStation++) {
-              Beta = atan(ProbeArray[iAngle][iStation][9]/ProbeArray[iAngle][iStation][8])*360.0/(2.0*PI_NUMBER);
-              SurfFlow_file << Beta << " ";
-            }
-          }
-
-          SurfFlow_file <<"SCALARS Mach float" << endl;
-          SurfFlow_file <<"LOOKUP_TABLE default" << endl;
-
-          for (iAngle = 0; iAngle < nAngle; iAngle++) {
-            for (iStation = 0; iStation < nStation; iStation++) {
-              SurfFlow_file << ProbeArray[iAngle][iStation][7] << " ";
-            }
-          }
-
-          SurfFlow_file <<"VECTORS Velocity float" << endl;
-
-          for (iAngle = 0; iAngle < nAngle; iAngle++) {
-            for (iStation = 0; iStation < nStation; iStation++) {
-              SurfFlow_file << ProbeArray[iAngle][iStation][8] << " " << ProbeArray[iAngle][iStation][9] << " " << ProbeArray[iAngle][iStation][10] << " ";
-            }
-          }
-
-        }
-        else {
-
-          SurfFlow_file <<"ZONE T= \"" << Analyze_TagBound <<"\", NODES=" << nAngle*nStation << " , ELEMENTS= " << nAngle*(nStation-1) <<", DATAPACKING=POINT, ZONETYPE=FEQUADRILATERAL" << endl;
-
-          for (iAngle = 0; iAngle < nAngle; iAngle++) {
-            for (iStation = 0; iStation < nStation; iStation++) {
-
-              Alpha = atan(ProbeArray[iAngle][iStation][10]/ProbeArray[iAngle][iStation][8])*360.0/(2.0*PI_NUMBER);
-              Beta = atan(ProbeArray[iAngle][iStation][9]/ProbeArray[iAngle][iStation][8])*360.0/(2.0*PI_NUMBER);
-
-              Mach_ij = ProbeArray[iAngle][iStation][7];
-              if (iAngle+1 != nAngle) Mach_ip1j = ProbeArray[iAngle+1][iStation][7];
-              else Mach_ip1j = ProbeArray[0][iStation][7];
-              if (iAngle-1 != -1) Mach_im1j = ProbeArray[iAngle-1][iStation][7];
-              else Mach_im1j = ProbeArray[nAngle-1][iStation][7];
-              if (iStation+1 != nStation) Mach_ijp1 = ProbeArray[iAngle][iStation+1][7];
-              else Mach_ijp1 = ProbeArray[iAngle][0][7];
-              if (iStation-1 != -1) Mach_ijm1 = ProbeArray[iAngle][iStation-1][7];
-              else Mach_ijm1 = ProbeArray[iAngle][nStation-1][7];
-              Filtered_Mach = (4.0*Mach_ij+Mach_ip1j+Mach_im1j+Mach_ijp1+Mach_ijm1)/8.0;
-
-              Alpha_ij = atan(ProbeArray[iAngle][iStation][10]/ProbeArray[iAngle][iStation][8])*360.0/(2.0*PI_NUMBER);
-              if (iAngle+1 != nAngle) Alpha_ip1j = atan(ProbeArray[iAngle+1][iStation][10]/ProbeArray[iAngle+1][iStation][8])*360.0/(2.0*PI_NUMBER);
-              else Alpha_ip1j = atan(ProbeArray[0][iStation][10]/ProbeArray[0][iStation][8])*360.0/(2.0*PI_NUMBER);
-              if (iAngle-1 != -1) Alpha_im1j = atan(ProbeArray[iAngle-1][iStation][10]/ProbeArray[iAngle-1][iStation][8])*360.0/(2.0*PI_NUMBER);
-              else Alpha_im1j = atan(ProbeArray[nAngle-1][iStation][10]/ProbeArray[nAngle-1][iStation][8])*360.0/(2.0*PI_NUMBER);
-              if (iStation+1 != nStation) Alpha_ijp1 = atan(ProbeArray[iAngle][iStation+1][10]/ProbeArray[iAngle][iStation+1][8])*360.0/(2.0*PI_NUMBER);
-              else Alpha_ijp1 = atan(ProbeArray[iAngle][0][10]/ProbeArray[iAngle][0][8])*360.0/(2.0*PI_NUMBER);
-              if (iStation-1 != -1) Alpha_ijm1 = atan(ProbeArray[iAngle][iStation-1][10]/ProbeArray[iAngle][iStation-1][8])*360.0/(2.0*PI_NUMBER);
-              else Alpha_ijm1 = atan(ProbeArray[iAngle][nStation-1][10]/ProbeArray[iAngle][nStation-1][8])*360.0/(2.0*PI_NUMBER);
-              Filtered_Alpha = (4.0*Alpha_ij+Alpha_ip1j+Alpha_im1j+Alpha_ijp1+Alpha_ijm1)/8.0;
-
-              Beta_ij = atan(ProbeArray[iAngle][iStation][9]/ProbeArray[iAngle][iStation][8])*360.0/(2.0*PI_NUMBER);
-              if (iAngle+1 != nAngle) Beta_ip1j = atan(ProbeArray[iAngle+1][iStation][9]/ProbeArray[iAngle+1][iStation][8])*360.0/(2.0*PI_NUMBER);
-              else Beta_ip1j = atan(ProbeArray[0][iStation][9]/ProbeArray[0][iStation][8])*360.0/(2.0*PI_NUMBER);
-              if (iAngle-1 != -1) Beta_im1j = atan(ProbeArray[iAngle-1][iStation][9]/ProbeArray[iAngle-1][iStation][8])*360.0/(2.0*PI_NUMBER);
-              else Beta_im1j = atan(ProbeArray[nAngle-1][iStation][9]/ProbeArray[nAngle-1][iStation][8])*360.0/(2.0*PI_NUMBER);
-              if (iStation+1 != nStation) Beta_ijp1 = atan(ProbeArray[iAngle][iStation+1][9]/ProbeArray[iAngle][iStation+1][8])*360.0/(2.0*PI_NUMBER);
-              else Beta_ijp1 = atan(ProbeArray[iAngle][0][9]/ProbeArray[iAngle][0][8])*360.0/(2.0*PI_NUMBER);
-              if (iStation-1 != -1) Beta_ijm1 = atan(ProbeArray[iAngle][iStation-1][9]/ProbeArray[iAngle][iStation-1][8])*360.0/(2.0*PI_NUMBER);
-              else Beta_ijm1 = atan(ProbeArray[iAngle][nStation-1][9]/ProbeArray[iAngle][nStation-1][8])*360.0/(2.0*PI_NUMBER);
-              Filtered_Beta = (4.0*Beta_ij+Beta_ip1j+Beta_im1j+Beta_ijp1+Beta_ijm1)/8.0;
-
-
-              SurfFlow_file
-              << " "  << ProbeArray[iAngle][iStation][1]-yCoord_CG
-              <<" " << ProbeArray[iAngle][iStation][2]-zCoord_CG
-              <<" " << ProbeArray[iAngle][iStation][3] <<" " << ProbeArray[iAngle][iStation][4]
-              <<" " << ProbeArray[iAngle][iStation][5] <<" " << ProbeArray[iAngle][iStation][6]
-              <<" " << ProbeArray[iAngle][iStation][8] <<" " << ProbeArray[iAngle][iStation][9]
-              <<" " << ProbeArray[iAngle][iStation][10]
-              <<" " << Alpha <<" " << Beta << " " << ProbeArray[iAngle][iStation][7]
-              <<" " << Filtered_Alpha <<" " << Filtered_Beta << " " << Filtered_Mach << endl;
-
-            }
-          }
-
-          for (iAngle = 0; iAngle < nAngle; iAngle++) {
-            for (iStation = 0; iStation < nStation-1; iStation++) {
-              a = iAngle*nStation+iStation; b = a + nStation; c = b+1; d = a +1;
-              if (iAngle == nAngle-1) { b = iStation; c = b+1;   }
-              SurfFlow_file << a+1  <<" "<< b+1  <<" "<< c+1 <<" "<< d+1 << endl;
-            }
-          }
-
-          /*--- Add extra info ---*/
-
-          SurfFlow_file << "TEXT X=14, Y=86, F=HELV-BOLD, C=BLUE, H=2.0, ";
-          unsigned short RackProbes = SU2_TYPE::Int(config->GetDistortionRack()[0]);
-          unsigned short RackAngle = SU2_TYPE::Int(config->GetDistortionRack()[1]);
-          SurfFlow_file << "T=\"Rack Size: " << RackProbes << " probes at "<< RackAngle << "deg." << "\\" << "\\n";
-          SurfFlow_file << "Mach " << config->GetMach() << ", Reynolds " << config->GetReynolds() << ", <greek>a</greek> "
-          << config->GetAoA() << "deg, <greek>b</greek> " << config->GetAoS() << "deg." << "\\" << "\\n";
-          SurfFlow_file.precision(1);
-          SurfFlow_file << fixed << "Net Thrust " << solver->GetTotal_NetThrust() << "lbs, Power " << solver->GetTotal_Power() <<  "HP";
-          SurfFlow_file.precision(4);
-          SurfFlow_file << ", MassFlow " << config->GetSurface_MassFlow(iMarker_Analyze) << ",\\" << "\\n";
-          SurfFlow_file << "IDC " << config->GetSurface_IDC(iMarker_Analyze)*100 << "%, IDCM " << config->GetSurface_IDC_Mach(iMarker_Analyze)*100 << "%, IDR " << config->GetSurface_IDR(iMarker_Analyze)*100 << "%,\\" << "\\n";
-          SurfFlow_file << "DC60 " << config->GetSurface_DC60(iMarker_Analyze) << ".\"" << endl;
-
-        }
-
-      }
-
-      /*--- Release the recv buffers on the master node ---*/
-
-      delete [] Buffer_Recv_Coord_x;
-      delete [] Buffer_Recv_Coord_y;
-      if (nDim == 3) delete [] Buffer_Recv_Coord_z;
-
-      delete [] Buffer_Recv_PT;
-      delete [] Buffer_Recv_TT;
-      delete [] Buffer_Recv_P;
-      delete [] Buffer_Recv_T;
-      delete [] Buffer_Recv_Mach;
-      delete [] Buffer_Recv_Vel_x;
-      delete [] Buffer_Recv_Vel_y;
-      if (nDim == 3) delete [] Buffer_Recv_Vel_z;
-      delete [] Buffer_Recv_q;
-
-      delete [] Buffer_Recv_Area;
-
-      delete [] Buffer_Recv_nVertex;
-
-      delete[] r;
-      for (iAngle = 0; iAngle < nAngle; iAngle++) {
-        for (iStation = 0; iStation < nStation; iStation++) {
-          delete[] ProbeArray[iAngle][iStation];
-        }
-      }
-      delete[] ProbeArray;
-
-    }
-
-//    if ((rank == MASTER_NODE) && !config->GetDiscrete_Adjoint()) {
-//
-//      cout << "Surface ("<< Analyze_TagBound << "): ";
-//      cout.precision(4);
-//      cout.setf(ios::fixed, ios::floatfield);
-//      cout << setprecision(1) << "IDC " << 100*config->GetSurface_IDC(iMarker_Analyze)
-//      << "%. IDC Mach " << 100*config->GetSurface_IDC_Mach(iMarker_Analyze)
-//      << "%. IDR " << 100*config->GetSurface_IDR(iMarker_Analyze)
-//      << "%. DC60 " << config->GetSurface_DC60(iMarker_Analyze) << "." << endl;
-//
-//    }
-
-    /*--- Release the memory for the remaining buffers and exit ---*/
-
-    delete [] Buffer_Send_Coord_x;
-    delete [] Buffer_Send_Coord_y;
-    if (nDim == 3) delete [] Buffer_Send_Coord_z;
-
-    delete [] Buffer_Send_PT;
-    delete [] Buffer_Send_TT;
-    delete [] Buffer_Send_P;
-    delete [] Buffer_Send_T;
-    delete [] Buffer_Send_Mach;
-    delete [] Buffer_Send_Vel_x;
-    delete [] Buffer_Send_Vel_y;
-    if (nDim == 3) delete [] Buffer_Send_Vel_z;
-    delete [] Buffer_Send_q;
-
-    delete [] Buffer_Send_Area;
-
-  }
-
-  /*--- Close the tecplot  file ---*/
-
-  if (output) {
-    SurfFlow_file.close();
-  }
-
-}
-
-void COutputLegacy::WriteTurboPerfConvHistory(CConfig *config){
-
-  unsigned short iMarker_Monitoring;
-  string inMarker_Tag, outMarker_Tag, inMarkerTag_Mix;
-  unsigned short nZone       = config->GetnZone();
-  bool turbulent = ((config->GetKind_Solver() == MAIN_SOLVER::RANS) || (config->GetKind_Solver() == MAIN_SOLVER::DISC_ADJ_RANS));
-  bool menter_sst = (config->GetKind_Turb_Model() == TURB_MODEL::SST);
-
-  unsigned short nBladesRow, nStages;
-  unsigned short iStage;
-  nBladesRow = config->GetnMarker_Turbomachinery();
-  nStages    = SU2_TYPE::Int(nBladesRow/2);
-
-  cout << endl << "------------------------- Turbomachinery Summary ------------------------" << endl;
-  cout << endl;
-  for (iMarker_Monitoring = 0; iMarker_Monitoring < config->GetnMarker_Turbomachinery(); iMarker_Monitoring++){
-    cout << endl << "----------------------------- Blade " << iMarker_Monitoring + 1 << " -----------------------------------" << endl;
-    inMarker_Tag = config->GetMarker_TurboPerf_BoundIn(iMarker_Monitoring);
-    outMarker_Tag = config->GetMarker_TurboPerf_BoundOut(iMarker_Monitoring);
-    if(iMarker_Monitoring == 0){
-      cout << "BC Inlet convergence monitoring marker " << inMarker_Tag << " : "<<endl;
-      cout << endl;
-      cout << "     Inlet Total Enthalpy" << "     Inlet Total Enthalpy BC" << "     err(%)" <<  endl;
-      cout.width(25); cout << TotalEnthalpyIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)]*config->GetEnergy_Ref();
-      cout.width(25); cout << TotalEnthalpyIn_BC[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)]*config->GetEnergy_Ref();
-      cout.width(25); cout << abs((TotalEnthalpyIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)] - TotalEnthalpyIn_BC[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)])/TotalEnthalpyIn_BC[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)])*100.0;
-      cout << endl;
-      cout << endl;
-      cout << "     Inlet Entropy" << "            Inlet Entropy BC" << "            err(%)" <<  endl;
-      cout.width(25); cout << EntropyIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)]*config->GetEnergy_Ref()/config->GetTemperature_Ref();
-      cout.width(25); cout << EntropyIn_BC[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)]*config->GetEnergy_Ref()/config->GetTemperature_Ref();
-      cout.width(25); cout << abs((EntropyIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)] - EntropyIn_BC[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)])/EntropyIn_BC[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)])*100.0;
-      cout << endl;
-      cout << endl;
-      cout << "     Inlet Absolute Angle" << "     Inlet Absolute Angle BC" << "     err(%)" <<  endl;
-      cout.width(25); cout << 180.0/PI_NUMBER*AbsFlowAngleIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)];
-      cout.width(25); cout << 180.0/PI_NUMBER*FlowAngleIn_BC[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)];
-      cout.width(25); cout << abs((AbsFlowAngleIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)] - FlowAngleIn_BC[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)])/FlowAngleIn_BC[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)])*100.0;
-      cout << endl;
-      cout << endl;
-      if(turbulent){
-        if(menter_sst){
-          cout << "     Inlet TurbIntensity" << "      Inlet TurbIntensity BC" << "      err(%)" <<  endl;
-          cout.width(25); cout << TurbIntensityIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)];
-          cout.width(25); cout << config->GetTurbulenceIntensity_FreeStream();
-          cout.width(25); cout << abs((TurbIntensityIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)] - config->GetTurbulenceIntensity_FreeStream())/config->GetTurbulenceIntensity_FreeStream())*100.0;
-          cout << endl;
-          cout << endl;
-          cout << "     Inlet Turb2LamRatio" << "      Inlet Turb2LamRatio BC" << "      err(%)" <<  endl;
-          cout.width(25); cout << Turb2LamViscRatioIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)];
-          cout.width(25); cout << config->GetTurb2LamViscRatio_FreeStream();
-          cout.width(25); cout << abs((Turb2LamViscRatioIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)] - config->GetTurb2LamViscRatio_FreeStream())/config->GetTurb2LamViscRatio_FreeStream())*100.0;
-          cout << endl;
-          cout << endl;
-        }
-        else{
-          cout << "     Inlet Nu Factor" << "          Inlet Nu Factor BC" << "          err(%)" <<  endl;
-          cout.width(25); cout << NuFactorIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)];
-          cout.width(25); cout << config->GetNuFactor_FreeStream();
-          cout.width(25); cout << abs((NuFactorIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)] - config->GetNuFactor_FreeStream())/config->GetNuFactor_FreeStream())*100.0;
-          cout << endl;
-          cout << endl;
-        }
-      }
-    }
-    if(iMarker_Monitoring == config->GetnMarker_Turbomachinery() -1 ){
-      // if BC outlet
-      cout << "BC outlet convergence monitoring  marker " << outMarker_Tag << " : "<<endl;
-      cout << endl;
-      cout << "     Outlet Pressure" << "          Outlet Pressure BC" << "          err(%)" <<  endl;
-      cout.width(25); cout << PressureOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)]*config->GetPressure_Ref();
-      cout.width(25); cout << PressureOut_BC[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)]*config->GetPressure_Ref();
-      cout.width(25); cout << abs((PressureOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)] - PressureOut_BC[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)])/PressureOut_BC[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)])*100.0;
-      cout << endl;
-      cout << endl;
-    }
-
-    cout << "Convergence monitoring for integral quantities between markers " << inMarker_Tag << " and "<< outMarker_Tag << " : "<<endl;
-    cout << endl;
-    cout << "     Inlet Mass Flow " << "         Outlet Mass Flow" << "            err(%)" <<  endl;
-    cout.width(25); cout << MassFlowIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)]*config->GetVelocity_Ref()*config->GetDensity_Ref();
-    cout.width(25); cout << MassFlowOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)]*config->GetVelocity_Ref()*config->GetDensity_Ref();
-    cout.width(25); cout << abs((MassFlowIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)] - MassFlowOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)])/MassFlowIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)])*100.0;
-    cout << endl;
-    cout << endl;
-    //if(stator)
-    //cout << "     Inlet Total Enthalpy " << "    Outlet Total Enthalpy" << "     err(%)" <<  endl;
-    //else
-    cout << "     Inlet Total Rothalpy " << "    Outlet Total Rothalpy" << "       err(%)" <<  endl;
-    cout.width(25); cout << RothalpyIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)]*config->GetEnergy_Ref();
-    cout.width(25); cout << RothalpyOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)]*config->GetEnergy_Ref();
-    cout.width(25); cout << abs((RothalpyIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)] - RothalpyOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)])/RothalpyIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)])*100.0;
-    cout << endl;
-    cout << endl;
-    cout << "Blade performance between boundaries " << inMarker_Tag << " and "<< outMarker_Tag << " : "<<endl;
-    cout << endl;
-    cout << "     Total Pressure Loss(%)" << "   Kinetic Energy Loss(%)" << "      Entropy Generation(%)" << endl;
-    cout.width(25); cout << TotalPressureLoss[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)]*100.0;
-    cout.width(25); cout << KineticEnergyLoss[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)]*100.0;
-    cout.width(25); cout << EntropyGen[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)]*100.0;
-    cout << endl;
-    cout << endl;
-    cout << "     Total Inlet Enthalpy" << "     Eulerian Work" << "               Pressure Ratio" <<  endl;
-    cout.width(25); cout << TotalEnthalpyIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)]*config->GetEnergy_Ref();
-    cout.width(25); cout << EulerianWork[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)]*config->GetEnergy_Ref();
-    cout.width(25); cout << PressureRatio[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)];
-    cout << endl;
-    cout << endl;
-    cout << "     Inlet Entropy" << "            Outlet Entropy" << "             Outlet Is. Enthalpy" <<  endl;
-    cout.width(25); cout << EntropyIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)]*config->GetEnergy_Ref()/config->GetTemperature_Ref();
-    cout.width(25); cout << EntropyOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)]*config->GetEnergy_Ref()/config->GetTemperature_Ref();
-    cout.width(25); cout << EnthalpyOutIs[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)]*config->GetEnergy_Ref();
-    cout << endl;
-    cout << endl;
-    cout << "Cinematic quantities between boundaries " << inMarker_Tag << " and "<< outMarker_Tag << " : "<<endl;
-    cout << endl;
-    cout << "     Inlet Mach"<< "               Inlet Normal Mach" << "            Inlet Tang. Mach" << endl;
-    cout.width(25); cout << sqrt(MachIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)][0]*MachIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)][0] +MachIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)][1]*MachIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)][1]);
-    cout.width(25); cout << MachIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)][0];
-    cout.width(25); cout << MachIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)][1];
-    cout << endl;
-    cout << endl;
-    cout << "     Outlet Mach"<< "              Outlet Normal Mach" << "           Outlet Tang. Mach" << endl;
-    cout.width(25); cout << sqrt(MachOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)][0]*MachOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)][0] +MachOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)][1]*MachOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)][1]);
-    cout.width(25); cout << MachOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)][0];
-    cout.width(25); cout << MachOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)][1];cout << endl;
-    cout << endl;
-    cout << "     Inlet Flow Angle" << "         Outlet flow Angle  " << endl;
-    cout.width(25); cout << 180.0/PI_NUMBER*FlowAngleIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)];
-    cout.width(25); cout << 180.0/PI_NUMBER*FlowAngleOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)];
-    cout << endl;
-    cout << endl;
-    // if gridmov
-    cout << "     Inlet Abs Flow Angle" << "     Outlet Abs Flow Angle  " << endl;
-    cout.width(25); cout << 180.0/PI_NUMBER*AbsFlowAngleIn[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)];
-    cout.width(25); cout << 180.0/PI_NUMBER*AbsFlowAngleOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)];
-    cout << endl;
-    cout << endl << "-------------------------------------------------------------------------" << endl;
-    cout << endl;
-    if(nZone > 0 && iMarker_Monitoring < config->GetnMarker_Turbomachinery() -1){
-      cout << endl << "---------- Mixing-Plane Interface between Blade " << iMarker_Monitoring + 1 << " and Blade " << iMarker_Monitoring + 2 << " -----------" << endl;
-      cout << endl;
-      inMarkerTag_Mix = config->GetMarker_TurboPerf_BoundIn(iMarker_Monitoring + 1);
-      cout << "Convergence monitoring for the outlet  " << outMarker_Tag << " and the inlet  "<< inMarkerTag_Mix << " : "<<endl;
-      cout << endl;
-      cout << "     Outlet Density " << "          Inlet Density" << "               err(%)" <<  endl;
-      cout.width(25); cout << DensityOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)]*config->GetDensity_Ref();
-      cout.width(25); cout << DensityIn[iMarker_Monitoring + 1][config->GetnSpan_iZones(iMarker_Monitoring + 1)]*config->GetDensity_Ref();
-      cout.width(25); cout << abs((DensityIn[iMarker_Monitoring + 1][config->GetnSpan_iZones(iMarker_Monitoring +1)] - DensityOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)])/DensityIn[iMarker_Monitoring + 1][config->GetnSpan_iZones(iMarker_Monitoring +1)])*100.0;
-      cout << endl;
-      cout << endl;
-      cout << "     Outlet Pressure " << "         Inlet Pressure" << "              err(%)" <<  endl;
-      cout.width(25); cout << PressureOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)]*config->GetPressure_Ref();
-      cout.width(25); cout << PressureIn[iMarker_Monitoring + 1][config->GetnSpan_iZones(iMarker_Monitoring +1)]*config->GetPressure_Ref();
-      cout.width(25); cout << abs((PressureIn[iMarker_Monitoring + 1][config->GetnSpan_iZones(iMarker_Monitoring +1)] - PressureOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)])/PressureIn[iMarker_Monitoring + 1][config->GetnSpan_iZones(iMarker_Monitoring +1)])*100.0;
-      cout << endl;
-      cout << endl;
-      cout << "     Outlet Normal Velocity " << "  Inlet Normal Velocity" << "       err(%)" <<  endl;
-      cout.width(25); cout << TurboVelocityOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)][0]*config->GetVelocity_Ref();
-      cout.width(25); cout << TurboVelocityIn[iMarker_Monitoring + 1][config->GetnSpan_iZones(iMarker_Monitoring +1)][0]*config->GetVelocity_Ref();
-      cout.width(25); cout << abs((TurboVelocityIn[iMarker_Monitoring + 1][config->GetnSpan_iZones(iMarker_Monitoring +1)][0] - TurboVelocityOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)][0])/TurboVelocityIn[iMarker_Monitoring+1][config->GetnSpan_iZones(iMarker_Monitoring +1)][0])*100.0;
-      cout << endl;
-      cout << endl;
-      cout << "     Outlet Tang. Velocity " << "   Inlet Tang. Velocity" << "        err(%)" <<  endl;
-      cout.width(25); cout << TurboVelocityOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)][1]*config->GetVelocity_Ref();
-      cout.width(25); cout << TurboVelocityIn[iMarker_Monitoring + 1][config->GetnSpan_iZones(iMarker_Monitoring +1)][1]*config->GetVelocity_Ref();
-      cout.width(25); cout << abs((TurboVelocityIn[iMarker_Monitoring + 1][config->GetnSpan_iZones(iMarker_Monitoring +1)][1] - TurboVelocityOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)][1])/TurboVelocityIn[iMarker_Monitoring+1][config->GetnSpan_iZones(iMarker_Monitoring +1)][1])*100.0;
-      cout << endl;
-      cout << endl;
-      cout << "     Outlet Entropy " << "          Inlet Entropy" << "               err(%)" <<  endl;
-      cout.width(25); cout << EntropyOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)]*config->GetEnergy_Ref()/config->GetTemperature_Ref();
-      cout.width(25); cout << EntropyIn[iMarker_Monitoring + 1][config->GetnSpan_iZones(iMarker_Monitoring +1)]*config->GetEnergy_Ref()/config->GetTemperature_Ref();
-      cout.width(25); cout << abs((EntropyIn[iMarker_Monitoring + 1][config->GetnSpan_iZones(iMarker_Monitoring+1)] - EntropyOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)])/EntropyIn[iMarker_Monitoring + 1][config->GetnSpan_iZones(iMarker_Monitoring+1)])*100.0;
-      if(turbulent){
-        cout << endl;
-        cout << endl;
-        if(menter_sst){
-          cout << "     Outlet TurbIntensity " << "    Inlet TurbIntensity" << "         err(%)" <<  endl;
-          cout.width(25); cout << TurbIntensityOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)];
-          cout.width(25); cout << TurbIntensityIn[iMarker_Monitoring + 1][config->GetnSpan_iZones(iMarker_Monitoring +1)];
-          cout.width(25); cout << abs((TurbIntensityIn[iMarker_Monitoring + 1][config->GetnSpan_iZones(iMarker_Monitoring+1)] - TurbIntensityOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)])/TurbIntensityIn[iMarker_Monitoring + 1][config->GetnSpan_iZones(iMarker_Monitoring+1)])*100.0;
-          cout << endl;
-          cout << endl;
-          cout << "     Outlet Turb2LamRatio " << "    Inlet Turb2LamRatio" << "         err(%)" <<  endl;
-          cout.width(25); cout << Turb2LamViscRatioOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)];
-          cout.width(25); cout << Turb2LamViscRatioIn[iMarker_Monitoring + 1][config->GetnSpan_iZones(iMarker_Monitoring +1)];
-          cout.width(25); cout << abs((Turb2LamViscRatioIn[iMarker_Monitoring + 1][config->GetnSpan_iZones(iMarker_Monitoring+1)] - Turb2LamViscRatioOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)])/Turb2LamViscRatioIn[iMarker_Monitoring + 1][config->GetnSpan_iZones(iMarker_Monitoring+1)])*100.0;
-        }
-        else{
-          cout << "     Outlet Nu Factor " << "        Inlet Nu Factor" << "             err(%)" <<  endl;
-          cout.width(25); cout << NuFactorOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)];
-          cout.width(25); cout << NuFactorIn[iMarker_Monitoring + 1][config->GetnSpan_iZones(iMarker_Monitoring +1)];
-          cout.width(25); cout << abs((NuFactorIn[iMarker_Monitoring + 1][config->GetnSpan_iZones(iMarker_Monitoring+1)] - NuFactorOut[iMarker_Monitoring][config->GetnSpan_iZones(iMarker_Monitoring)])/NuFactorIn[iMarker_Monitoring + 1][config->GetnSpan_iZones(iMarker_Monitoring+1)])*100.0;
-        }
-      }
-      cout << endl;
-      cout << endl << "-------------------------------------------------------------------------" << endl;
-      cout << endl;
-    }
-
-  }
-  if(nZone > 1){
-    /*--- Stage Performance ---*/
-    for(iStage = 0; iStage < nStages; iStage++ ){
-      cout << endl << "----------------------------- Stage " << iStage + 1 << " -----------------------------------" << endl;
-      inMarker_Tag = config->GetMarker_TurboPerf_BoundIn(iStage*2);
-      outMarker_Tag = config->GetMarker_TurboPerf_BoundOut(iStage*2+1);
-      cout << "Stage performance between boundaries " << inMarker_Tag << " and "<< outMarker_Tag << " : "<<endl;
-      cout << endl;
-      cout << "     Total-Total Eff.(%)" << "      Total-Static Eff.(%)" << "      Entropy Generation(%)" << endl;
-      cout.width(25); cout << TotalTotalEfficiency[nBladesRow + iStage][nSpanWiseSections]*100.0;
-      cout.width(25); cout << TotalStaticEfficiency[nBladesRow + iStage][nSpanWiseSections]*100.0;
-      cout.width(25); cout << EntropyGen[nBladesRow + iStage][nSpanWiseSections]*100.0;
-      cout << endl;
-      cout << endl;
-      cout << "     Pressure Ratio " << "          Outlet Is. Enthalpy" << "       In-Out MassFlow Diff (%)" <<  endl;
-      cout.width(25); cout << PressureRatio[nBladesRow + iStage][nSpanWiseSections];
-      cout.width(25); cout << EnthalpyOutIs[nBladesRow + iStage][nSpanWiseSections]*config->GetEnergy_Ref();
-      cout.width(25); cout << abs((MassFlowIn[nBladesRow + iStage][nSpanWiseSections] - MassFlowOut[nBladesRow + iStage][nSpanWiseSections])/MassFlowIn[nBladesRow + iStage][nSpanWiseSections])*100.0;
-    }
-    cout << endl;
-    cout << endl << "-------------------------------------------------------------------------" << endl;
-    cout << endl;
-
-    /*--- Full Machine Performance ---*/
-    // if(turbine)
-    cout << endl << "---------------------------- Turbine ------------------------------------" << endl;
-    inMarker_Tag = config->GetMarker_TurboPerf_BoundIn(0);
-    outMarker_Tag = config->GetMarker_TurboPerf_BoundOut(nBladesRow-1);
-    cout << "Turbine performance between boundaries " << inMarker_Tag << " and "<< outMarker_Tag << " : "<<endl;
-    cout << endl;
-    cout << "     Total-Total Eff.(%)" << "      Total-Static Eff.(%)" << "      Entropy Generation(%)" << endl;
-    cout.width(25); cout << TotalTotalEfficiency[nBladesRow + nStages][nSpanWiseSections]*100.0;
-    cout.width(25); cout << TotalStaticEfficiency[nBladesRow + nStages][nSpanWiseSections]*100.0;
-    cout.width(25); cout << EntropyGen[nBladesRow + nStages][nSpanWiseSections]*100.0;
-    cout << endl;
-    cout << endl;
-    cout << "     Pressure Ratio " << "          Outlet Is. Enthalpy" << "       In-Out MassFlow Diff (%)" <<  endl;
-    cout.width(25); cout << PressureRatio[nBladesRow + nStages][nSpanWiseSections];
-    cout.width(25); cout << EnthalpyOutIs[nBladesRow + nStages][nSpanWiseSections]*config->GetEnergy_Ref();;
-    cout.width(25); cout << abs((MassFlowIn[nBladesRow + nStages][nSpanWiseSections] - MassFlowOut[nBladesRow + nStages][nSpanWiseSections])/MassFlowIn[nBladesRow + nStages][nSpanWiseSections])*100.0;
-    cout << endl;
-    cout << endl << "-------------------------------------------------------------------------" << endl;
-    cout << endl;
-  }
-
-}
-
-void COutputLegacy::SpecialOutputTurbo(CSolver *****solver, CGeometry ****geometry, CConfig **config,
-                                       unsigned short val_iZone, bool output) {
-
-  string inMarker_Tag, outMarker_Tag, inMarkerTag_Mix;
-  unsigned short nZone       = config[val_iZone]->GetnZone();
-
-  unsigned short iDim, iSpan;
-
-  unsigned long iExtIter = config[val_iZone]->GetInnerIter();
-  const su2double* SpanWiseValuesIn, *SpanWiseValuesOut;
-  ofstream myfile;
-  string spanwise_performance_filename;
-
-
-  /*--- Start of write file turboperformance spanwise ---*/
-  if (rank == MASTER_NODE){
-    SpanWiseValuesIn = geometry[val_iZone][INST_0][MESH_0]->GetSpanWiseValue(1);
-    SpanWiseValuesOut = geometry[val_iZone][INST_0][MESH_0]->GetSpanWiseValue(2);
-
-
-
-    /*--- Writing Span wise inflow thermodynamic quantities. ---*/
-    spanwise_performance_filename = "TURBOMACHINERY/inflow_spanwise_thermodynamic_values.dat";
-    char buffer[50];
-    if (nZone > 1){
-      unsigned short lastindex      =  spanwise_performance_filename.find_last_of(".");
-      spanwise_performance_filename =  spanwise_performance_filename.substr(0, lastindex);
-      SPRINTF (buffer, "_%d.dat", SU2_TYPE::Int(val_iZone));
-      spanwise_performance_filename.append(string(buffer));
-    }
-
-
-    myfile.open (spanwise_performance_filename.data(), ios::out | ios::trunc);
-    myfile.setf(ios::scientific);
-    myfile.precision(12);
-
-    myfile << "TITLE = \"Inflow Spanwise Thermodynamic Values. iExtIter = " << iExtIter << " \"" << endl;
-    myfile << "VARIABLES =" << endl;
-
-    myfile.width(30); myfile << "\"SpanWise Value[m]\"";
-    myfile.width(15); myfile << "\"iSpan\"";
-    myfile.width(30); myfile << "\"Pressure[Pa]\"";
-    myfile.width(30); myfile << "\"TotalPressure[Pa]\"";
-    myfile.width(30); myfile << "\"Temperature[K]\"";
-    myfile.width(30); myfile << "\"TotalTemperature[K]\"";
-    myfile.width(30); myfile << "\"Enthalpy[J]\"";
-    myfile.width(30); myfile << "\"TotalEnthalpy[J]\"";
-    myfile.width(30); myfile << "\"Density[kg/m3]\"";
-    myfile.width(30); myfile << "\"Entropy[J/K]\"";
-    myfile.width(30); myfile << "\"TurbIntensity[-]\"";
-    myfile.width(30); myfile << "\"Turb2LamViscRatio[-]\"";
-    myfile.width(30); myfile << "\"NuFactor[-]\"";
-    myfile << endl;
-
-    for(iSpan = 0; iSpan < config[ZONE_0]->GetnSpan_iZones(val_iZone); iSpan++){
-
-      myfile.width(30); myfile << SpanWiseValuesIn[iSpan];
-      myfile.width(15); myfile << iSpan;
-      myfile.width(30); myfile << PressureIn           [val_iZone][iSpan]*config[ZONE_0]->GetPressure_Ref();
-      myfile.width(30); myfile << TotalPressureIn      [val_iZone][iSpan]*config[ZONE_0]->GetPressure_Ref();
-      myfile.width(30); myfile << TemperatureIn        [val_iZone][iSpan]*config[ZONE_0]->GetTemperature_Ref();
-      myfile.width(30); myfile << TotalTemperatureIn   [val_iZone][iSpan]*config[ZONE_0]->GetTemperature_Ref();
-      myfile.width(30); myfile << EnthalpyIn           [val_iZone][iSpan]*config[ZONE_0]->GetEnergy_Ref();
-      myfile.width(30); myfile << TotalEnthalpyIn      [val_iZone][iSpan]*config[ZONE_0]->GetEnergy_Ref();
-      myfile.width(30); myfile << DensityIn            [val_iZone][iSpan]*config[ZONE_0]->GetDensity_Ref();
-      myfile.width(30); myfile << EntropyIn            [val_iZone][iSpan]*config[ZONE_0]->GetEnergy_Ref()/config[ZONE_0]->GetTemperature_Ref();
-      if(TurbIntensityIn[val_iZone][iSpan] > 1.0){
-        myfile.width(30); myfile << TurbIntensityIn      [val_iZone][config[ZONE_0]->GetnSpan_iZones(val_iZone)/2];
-      }else{
-        myfile.width(30); myfile << TurbIntensityIn      [val_iZone][iSpan];
-      }
-      myfile.width(30); myfile << Turb2LamViscRatioIn  [val_iZone][iSpan];
-      myfile.width(30); myfile << NuFactorIn           [val_iZone][iSpan];
-      myfile << endl;
-    }
-
-    myfile.close();
-
-    /*--- Writing Span wise outflow thermodynamic quantities. ---*/
-    spanwise_performance_filename = "TURBOMACHINERY/outflow_spanwise_thermodynamic_values.dat";
-    if (nZone > 1){
-      unsigned short lastindex      =  spanwise_performance_filename.find_last_of(".");
-      spanwise_performance_filename =  spanwise_performance_filename.substr(0, lastindex);
-      SPRINTF (buffer, "_%d.dat", SU2_TYPE::Int(val_iZone));
-      spanwise_performance_filename.append(string(buffer));
-    }
-
-    myfile.open (spanwise_performance_filename.data(), ios::out | ios::trunc);
-    myfile.setf(ios::scientific);
-    myfile.precision(12);
-
-    myfile << "TITLE = \"Outflow Span-wise Thermodynamic Values. iExtIter = " << iExtIter << " \"" << endl;
-    myfile << "VARIABLES =" << endl;
-
-    myfile.width(30); myfile << "\"SpanWise Value[m]\"";
-    myfile.width(15); myfile << "\"iSpan\"";
-    myfile.width(30); myfile << "\"Pressure[Pa]\"";
-    myfile.width(30); myfile << "\"TotalPressure[Pa]\"";
-    myfile.width(30); myfile << "\"Temperature[K]\"";
-    myfile.width(30); myfile << "\"TotalTemperature[K]\"";
-    myfile.width(30); myfile << "\"Enthalpy[J]\"";
-    myfile.width(30); myfile << "\"TotalEnthalpy[J]\"";
-    myfile.width(30); myfile << "\"Density[kg/m3]\"";
-    myfile.width(30); myfile << "\"Entropy[J/K]\"";
-    myfile.width(30); myfile << "\"TurbIntensity[-]\"";
-    myfile.width(30); myfile << "\"Turb2LamViscRatio[-]\"";
-    myfile.width(30); myfile << "\"NuFactor[-]\"";
-    myfile << endl;
-
-
-    for(iSpan = 0; iSpan < config[ZONE_0]->GetnSpan_iZones(val_iZone); iSpan++){
-
-      myfile.width(30); myfile << SpanWiseValuesOut[iSpan];
-      myfile.width(15); myfile << iSpan;
-      myfile.width(30); myfile << PressureOut           [val_iZone][iSpan]*config[ZONE_0]->GetPressure_Ref();
-      myfile.width(30); myfile << TotalPressureOut      [val_iZone][iSpan]*config[ZONE_0]->GetPressure_Ref();
-      myfile.width(30); myfile << TemperatureOut        [val_iZone][iSpan]*config[ZONE_0]->GetTemperature_Ref();
-      myfile.width(30); myfile << TotalTemperatureOut   [val_iZone][iSpan]*config[ZONE_0]->GetTemperature_Ref();
-      myfile.width(30); myfile << EnthalpyOut           [val_iZone][iSpan]*config[ZONE_0]->GetEnergy_Ref();
-      myfile.width(30); myfile << TotalEnthalpyOut      [val_iZone][iSpan]*config[ZONE_0]->GetEnergy_Ref();
-      myfile.width(30); myfile << DensityOut            [val_iZone][iSpan]*config[ZONE_0]->GetDensity_Ref();
-      myfile.width(30); myfile << EntropyOut            [val_iZone][iSpan]*config[ZONE_0]->GetEnergy_Ref()/config[ZONE_0]->GetTemperature_Ref();
-      if(TurbIntensityOut[val_iZone][iSpan] > 1.0){
-        myfile.width(30); myfile << TurbIntensityOut      [val_iZone][config[ZONE_0]->GetnSpan_iZones(val_iZone)/2];
-      }else{
-        myfile.width(30); myfile << TurbIntensityOut      [val_iZone][iSpan];
-      }
-      myfile.width(30); myfile << Turb2LamViscRatioOut  [val_iZone][iSpan];
-      myfile.width(30); myfile << NuFactorOut           [val_iZone][iSpan];
-      myfile << endl;
-    }
-
-    myfile.close();
-
-    /*--- Writing Span wise inflow kinematic quantities. ---*/
-    spanwise_performance_filename = "TURBOMACHINERY/inflow_spanwise_kinematic_values.dat";
-    if (nZone > 1){
-      unsigned short lastindex      =  spanwise_performance_filename.find_last_of(".");
-      spanwise_performance_filename =  spanwise_performance_filename.substr(0, lastindex);
-      SPRINTF (buffer, "_%d.dat", SU2_TYPE::Int(val_iZone));
-      spanwise_performance_filename.append(string(buffer));
-    }
-
-    myfile.open (spanwise_performance_filename.data(), ios::out | ios::trunc);
-    myfile.setf(ios::scientific);
-    myfile.precision(12);
-
-    myfile << "TITLE = \"Inflow Span-wise Kinematic Values. iExtIter = " << iExtIter << " \"" << endl;
-    myfile << "VARIABLES =" << endl;
-
-    myfile.width(30); myfile << "\"SpanWise Value[m]\"";
-    myfile.width(15); myfile << "\"iSpan\"";
-    myfile.width(30); myfile << "\"Normal Mach[-]\"";
-    myfile.width(30); myfile << "\"Tangential Mach[-]\"";
-    myfile.width(30); myfile << "\"3rd Component Mach[-]\"";
-    myfile.width(30); myfile << "\"Mach Module[-]\"";
-    myfile.width(30); myfile << "\"Normal Velocity[m/s]\"";
-    myfile.width(30); myfile << "\"Tangential Velocity[m/s]\"";
-    myfile.width(30); myfile << "\"3rd Component Velocity[m/s]\"";
-    myfile.width(30); myfile << "\"Velocity Module[m/s]\"";
-    myfile.width(30); myfile << "\"Absolute Flow Angle[deg]\"";
-    myfile.width(30); myfile << "\"Relative Flow Angle[deg]\"";
-    myfile << endl;
-
-
-    for(iSpan = 0; iSpan < config[ZONE_0]->GetnSpan_iZones(val_iZone); iSpan++){
-
-      myfile.width(30); myfile << SpanWiseValuesIn[iSpan];
-      myfile.width(15); myfile << iSpan;
-      for (iDim = 0; iDim < 4; iDim++){
-        myfile.width(30); myfile << MachIn              [val_iZone][iSpan][iDim];
-      }
-      for (iDim = 0; iDim < 4; iDim++){
-        myfile.width(30); myfile << TurboVelocityIn     [val_iZone][iSpan][iDim]*config[ZONE_0]->GetVelocity_Ref();
-      }
-      if(AbsFlowAngleIn[val_iZone][iSpan] != AbsFlowAngleIn[val_iZone][iSpan]){
-        myfile.width(30); myfile << "0.0000";
-      }
-      else{
-        myfile.width(30); myfile << AbsFlowAngleIn     [val_iZone][iSpan]*180.0/PI_NUMBER;
-      }
-      if(FlowAngleIn[val_iZone][iSpan] != FlowAngleIn[val_iZone][iSpan]){
-        myfile.width(30); myfile << "0.0000";
-      }
-      else{
-        myfile.width(30); myfile << FlowAngleIn      [val_iZone][iSpan]*180.0/PI_NUMBER;
-      }
-      myfile << endl;
-    }
-
-    myfile.close();
-
-    /*--- Writing Span wise outflow thermodynamic quantities. ---*/
-    spanwise_performance_filename = "TURBOMACHINERY/outflow_spanwise_kinematic_values.dat";
-    if (nZone > 1){
-      unsigned short lastindex      =  spanwise_performance_filename.find_last_of(".");
-      spanwise_performance_filename =  spanwise_performance_filename.substr(0, lastindex);
-      SPRINTF (buffer, "_%d.dat", SU2_TYPE::Int(val_iZone));
-      spanwise_performance_filename.append(string(buffer));
-    }
-
-    myfile.open (spanwise_performance_filename.data(), ios::out | ios::trunc);
-    myfile.setf(ios::scientific);
-    myfile.precision(12);
-
-    myfile << "TITLE = \"Outflow Span-wise Kinematic Values. iExtIter = " << iExtIter << " \"" << endl;
-    myfile << "VARIABLES =" << endl;
-
-    myfile.width(30); myfile << "\"SpanWise Value[m]\"";
-    myfile.width(15); myfile << "\"iSpan\"";
-    myfile.width(30); myfile << "\"Normal Mach[-]\"";
-    myfile.width(30); myfile << "\"Tangential Mach[-]\"";
-    myfile.width(30); myfile << "\"3rd Component Mach[-]\"";
-    myfile.width(30); myfile << "\"Mach Module[-]\"";
-    myfile.width(30); myfile << "\"Normal Velocity[m/s]\"";
-    myfile.width(30); myfile << "\"Tangential Velocity[m/s]\"";
-    myfile.width(30); myfile << "\"3rd Component Velocity[m/s]\"";
-    myfile.width(30); myfile << "\"Velocity Module[m/s]\"";
-    myfile.width(30); myfile << "\"Absolute Flow Angle[deg]\"";
-    myfile.width(30); myfile << "\"Relative Flow Angle[deg]\"";
-    myfile << endl;
-
-
-    for(iSpan = 0; iSpan < config[ZONE_0]->GetnSpan_iZones(val_iZone); iSpan++){
-
-      myfile.width(30); myfile << SpanWiseValuesOut[iSpan];
-      myfile.width(15); myfile << iSpan;
-      for (iDim = 0; iDim < 4; iDim++){
-        myfile.width(30); myfile << MachOut              [val_iZone][iSpan][iDim];
-      }
-      for (iDim = 0; iDim < 4; iDim++){
-        myfile.width(30); myfile << TurboVelocityOut     [val_iZone][iSpan][iDim]*config[ZONE_0]->GetVelocity_Ref();
-      }
-      if(AbsFlowAngleOut[val_iZone][iSpan] != AbsFlowAngleOut[val_iZone][iSpan]){
-        myfile.width(30); myfile << "0.0000";
-      }
-      else{
-        myfile.width(30); myfile << AbsFlowAngleOut      [val_iZone][iSpan]*180.0/PI_NUMBER;
-      }
-      if(FlowAngleOut[val_iZone][iSpan] != FlowAngleOut[val_iZone][iSpan]){
-        myfile.width(30); myfile << "0.0000";
-      }
-      else{
-        myfile.width(30); myfile << FlowAngleOut      [val_iZone][iSpan]*180.0/PI_NUMBER;
-      }
-      myfile << endl;
-    }
-
-    myfile.close();
-
-  }
-}
-
-void COutputLegacy::SpecialOutputHarmonicBalance(CSolver *****solver, CGeometry ****geometry, CConfig **config, unsigned short iInst, unsigned short val_nInst, bool output) const {
-
-  /*--- Write file with flow quantities for harmonic balance HB ---*/
-  ofstream HB_output_file;
-  ofstream mean_HB_file;
-
-  /*--- MPI Send/Recv buffers ---*/
-  su2double *sbuf_var = nullptr,  *rbuf_var = nullptr;
-
-  /*--- Other variables ---*/
-  unsigned short iVar, kInst;
-  unsigned short nVar_output = 5;
-  unsigned long current_iter = config[ZONE_0]->GetInnerIter();
-
-  /*--- Allocate memory for send buffer ---*/
-  sbuf_var = new su2double[nVar_output];
-
-  su2double *averages = new su2double[nVar_output];
-  for (iVar = 0; iVar < nVar_output; iVar++)
-    averages[iVar] = 0;
-
-  /*--- Allocate memory for receive buffer ---*/
-  if (rank == MASTER_NODE) {
-    rbuf_var = new su2double[nVar_output];
-
-    HB_output_file.precision(15);
-    HB_output_file.open("HB_output.csv", ios::out);
-    HB_output_file <<  "\"time_instance\",\"CL\",\"CD\",\"CMx\",\"CMy\",\"CMz\"" << endl;
-
-    mean_HB_file.precision(15);
-    if (current_iter == 0 && iInst == 1) {
-      mean_HB_file.open("history_HB.plt", ios::trunc);
-      mean_HB_file << "TITLE = \"SU2 HARMONIC BALANCE SIMULATION\"" << endl;
-      mean_HB_file <<  "VARIABLES = \"Iteration\",\"CL\",\"CD\",\"CMx\",\"CMy\",\"CMz\",\"CT\",\"CQ\",\"CMerit\"" << endl;
-      mean_HB_file << "ZONE T= \"Average Convergence History\"" << endl;
-    }
-    else
-      mean_HB_file.open("history_HB.plt", ios::out | ios::app);
-  }
-
-  if (rank == MASTER_NODE) {
-
-    /*--- Run through the zones, collecting the output variables
-       N.B. Summing across processors within a given zone is being done
-       elsewhere. ---*/
-    for (kInst = 0; kInst < val_nInst; kInst++) {
-
-      /*--- Flow solution coefficients (parallel) ---*/
-      sbuf_var[0] = solver[ZONE_0][kInst][MESH_0][FLOW_SOL]->GetTotal_CL();
-      sbuf_var[1] = solver[ZONE_0][kInst][INST_0][FLOW_SOL]->GetTotal_CD();
-      sbuf_var[2] = solver[ZONE_0][kInst][INST_0][FLOW_SOL]->GetTotal_CMx();
-      sbuf_var[3] = solver[ZONE_0][kInst][INST_0][FLOW_SOL]->GetTotal_CMy();
-      sbuf_var[4] = solver[ZONE_0][kInst][INST_0][FLOW_SOL]->GetTotal_CMz();
-
-      for (iVar = 0; iVar < nVar_output; iVar++) {
-        rbuf_var[iVar] = sbuf_var[iVar];
-      }
-
-      HB_output_file << kInst << ", ";
-      for (iVar = 0; iVar < nVar_output; iVar++)
-        HB_output_file << rbuf_var[iVar] << ", ";
-      HB_output_file << endl;
-
-      /*--- Increment the total contributions from each zone, dividing by nZone as you go ---*/
-      for (iVar = 0; iVar < nVar_output; iVar++) {
-        averages[iVar] += (1.0/su2double(val_nInst))*rbuf_var[iVar];
-      }
-    }
-  }
-
-  if (rank == MASTER_NODE && iInst == INST_0) {
-
-    mean_HB_file << current_iter << ", ";
-    for (iVar = 0; iVar < nVar_output; iVar++) {
-      mean_HB_file << averages[iVar];
-      if (iVar < nVar_output-1)
-        mean_HB_file << ", ";
-    }
-    mean_HB_file << endl;
-  }
-
-  if (rank == MASTER_NODE) {
-    HB_output_file.close();
-    mean_HB_file.close();
-    delete [] rbuf_var;
-  }
-
-  delete [] sbuf_var;
-  delete [] averages;
-}
-
-void COutputLegacy::SetSpecialOutput(CSolver *****solver_container,
-                                       CGeometry ****geometry,
-                                       CConfig **config,
-                                       unsigned long iExtIter,
-                                       unsigned short val_nZone) {
-
-  bool special_output = false;
-  unsigned short iZone;
-
-  for (iZone = 0; iZone < val_nZone; iZone++){
-
-    special_output = config[iZone]->GetSpecial_Output();
-
-    /*--- Output a file with the forces breakdown. ---*/
-    if (config[iZone]->GetWrt_ForcesBreakdown())
-      SpecialOutputForcesBreakdown(solver_container, geometry, config, iZone, special_output);
-
-  }
-
-}
-
-void COutputLegacy::SpecialOutputAnalyzeSurface(CSolver *solver, CGeometry *geometry, CConfig *config, bool output) const {
-
-  unsigned short iDim, iMarker, iMarker_Analyze;
-  unsigned long iVertex, iPoint;
-  su2double Mach = 0.0, Pressure, Temperature = 0.0, TotalPressure = 0.0, TotalTemperature = 0.0,
-  Enthalpy, Velocity[3]= {0.0}, TangVel[3], Velocity2, MassFlow, Density, Area,
-  AxiFactor = 1.0, SoundSpeed, Vn, Vn2, Vtang2, Weight = 1.0;
-
-  su2double Gas_Constant      = config->GetGas_ConstantND();
-  su2double Gamma             = config->GetGamma();
-  unsigned short nMarker      = config->GetnMarker_All();
-  unsigned short nDim         = geometry->GetnDim();
-  unsigned short Kind_Average = config->GetKind_Average();
-
-  bool compressible   = config->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE;
-  bool incompressible = config->GetKind_Regime() == ENUM_REGIME::INCOMPRESSIBLE;
-  bool energy         = config->GetEnergy_Equation();
-
-
-  bool axisymmetric               = config->GetAxisymmetric();
-  unsigned short nMarker_Analyze  = config->GetnMarker_Analyze();
-
-  su2double  *Vector                    = new su2double[nDim];
-  su2double  *Surface_MassFlow          = new su2double[nMarker];
-  su2double  *Surface_Mach              = new su2double[nMarker];
-  su2double  *Surface_Temperature       = new su2double[nMarker];
-  su2double  *Surface_Density           = new su2double[nMarker];
-  su2double  *Surface_Enthalpy          = new su2double[nMarker];
-  su2double  *Surface_NormalVelocity    = new su2double[nMarker];
-  su2double  *Surface_StreamVelocity2   = new su2double[nMarker];
-  su2double  *Surface_TransvVelocity2   = new su2double[nMarker];
-  su2double  *Surface_Pressure          = new su2double[nMarker];
-  su2double  *Surface_TotalTemperature  = new su2double[nMarker];
-  su2double  *Surface_TotalPressure     = new su2double[nMarker];
-  su2double  *Surface_VelocityIdeal     = new su2double[nMarker];
-  su2double  *Surface_Area              = new su2double[nMarker];
-  su2double  *Surface_MassFlow_Abs      = new su2double[nMarker];
-
-  /*--- Compute the numerical fan face Mach number, and the total area of the inflow ---*/
-
-  for (iMarker = 0; iMarker < nMarker; iMarker++) {
-
-    Surface_MassFlow[iMarker]          = 0.0;
-    Surface_Mach[iMarker]              = 0.0;
-    Surface_Temperature[iMarker]       = 0.0;
-    Surface_Density[iMarker]           = 0.0;
-    Surface_Enthalpy[iMarker]          = 0.0;
-    Surface_NormalVelocity[iMarker]    = 0.0;
-    Surface_StreamVelocity2[iMarker]   = 0.0;
-    Surface_TransvVelocity2[iMarker]   = 0.0;
-    Surface_Pressure[iMarker]          = 0.0;
-    Surface_TotalTemperature[iMarker]  = 0.0;
-    Surface_TotalPressure[iMarker]     = 0.0;
-    Surface_VelocityIdeal[iMarker]     = 0.0;
-    Surface_Area[iMarker]              = 0.0;
-    Surface_MassFlow_Abs[iMarker]      = 0.0;
-
-    if (config->GetMarker_All_Analyze(iMarker) == YES) {
-
-      for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
-        iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
-
-        if (geometry->nodes->GetDomain(iPoint)) {
-
-          geometry->vertex[iMarker][iVertex]->GetNormal(Vector);
-
-          if (axisymmetric) {
-            if (geometry->nodes->GetCoord(iPoint, 1) != 0.0)
-              AxiFactor = 2.0*PI_NUMBER*geometry->nodes->GetCoord(iPoint, 1);
-            else
-              AxiFactor = 1.0;
-          } else {
-            AxiFactor = 1.0;
-          }
-
-          Density = solver->GetNodes()->GetDensity(iPoint);
-          Velocity2 = 0.0; Area = 0.0; MassFlow = 0.0; Vn = 0.0; Vtang2 = 0.0;
-
-          for (iDim = 0; iDim < nDim; iDim++) {
-            Area += (Vector[iDim] * AxiFactor) * (Vector[iDim] * AxiFactor);
-            Velocity[iDim] = solver->GetNodes()->GetVelocity(iPoint,iDim);
-            Velocity2 += Velocity[iDim] * Velocity[iDim];
-            Vn += Velocity[iDim] * Vector[iDim] * AxiFactor;
-            MassFlow += Vector[iDim] * AxiFactor * Density * Velocity[iDim];
-          }
-
-          Area       = sqrt (Area);
-          if (AxiFactor == 0.0) Vn = 0.0; else Vn /= Area;
-          Vn2        = Vn * Vn;
-          Pressure   = solver->GetNodes()->GetPressure(iPoint);
-          SoundSpeed = solver->GetNodes()->GetSoundSpeed(iPoint);
-
-          for (iDim = 0; iDim < nDim; iDim++) {
-            TangVel[iDim] = Velocity[iDim] - Vn*Vector[iDim]*AxiFactor/Area;
-            Vtang2       += TangVel[iDim]*TangVel[iDim];
-          }
-
-          if (incompressible){
-            if (config->GetKind_DensityModel() == INC_DENSITYMODEL::VARIABLE) {
-              Mach = sqrt(solver->GetNodes()->GetVelocity2(iPoint))/
-              sqrt(solver->GetNodes()->GetSpecificHeatCp(iPoint)*config->GetPressure_ThermodynamicND()/(solver->GetNodes()->GetSpecificHeatCv(iPoint)*solver->GetNodes()->GetDensity(iPoint)));
-            } else {
-              Mach = sqrt(solver->GetNodes()->GetVelocity2(iPoint))/
-              sqrt(config->GetBulk_Modulus()/(solver->GetNodes()->GetDensity(iPoint)));
-            }
-            Temperature       = solver->GetNodes()->GetTemperature(iPoint);
-            Enthalpy          = solver->GetNodes()->GetSpecificHeatCp(iPoint)*Temperature;
-            TotalTemperature  = Temperature + 0.5*Velocity2/solver->GetNodes()->GetSpecificHeatCp(iPoint);
-            TotalPressure     = Pressure + 0.5*Density*Velocity2;
-          }
-          else{
-            Mach              = sqrt(Velocity2)/SoundSpeed;
-            Temperature       = Pressure / (Gas_Constant * Density);
-            Enthalpy          = solver->GetNodes()->GetEnthalpy(iPoint);
-            TotalTemperature  = Temperature * (1.0 + Mach * Mach * 0.5 * (Gamma - 1.0));
-            TotalPressure     = Pressure * pow( 1.0 + Mach * Mach * 0.5 * (Gamma - 1.0), Gamma / (Gamma - 1.0));
-          }
-
-          /*--- Compute the mass Surface_MassFlow ---*/
-
-          Surface_Area[iMarker]             += Area;
-          Surface_MassFlow[iMarker]         += MassFlow;
-          Surface_MassFlow_Abs[iMarker]     += abs(MassFlow);
-
-          if (Kind_Average == AVERAGE_MASSFLUX) Weight = abs(MassFlow);
-          else if (Kind_Average == AVERAGE_AREA) Weight = abs(Area);
-          else Weight = 1.0;
-
-          Surface_Mach[iMarker]             += Mach*Weight;
-          Surface_Temperature[iMarker]      += Temperature*Weight;
-          Surface_Density[iMarker]          += Density*Weight;
-          Surface_Enthalpy[iMarker]         += Enthalpy*Weight;
-          Surface_NormalVelocity[iMarker]   += Vn*Weight;
-          Surface_Pressure[iMarker]         += Pressure*Weight;
-          Surface_TotalTemperature[iMarker] += TotalTemperature*Weight;
-          Surface_TotalPressure[iMarker]    += TotalPressure*Weight;
-
-          /*--- For now, always used the area to weight the uniformities. ---*/
-
-          Weight = abs(Area);
-
-          Surface_StreamVelocity2[iMarker]   += Vn2*Weight;
-          Surface_TransvVelocity2[iMarker]   += Vtang2*Weight;
-
-        }
-      }
-
-    }
-
-  }
-
-  /*--- Copy to the appropriate structure ---*/
-
-  su2double *Surface_MassFlow_Local          = new su2double [nMarker_Analyze];
-  su2double *Surface_Mach_Local              = new su2double [nMarker_Analyze];
-  su2double *Surface_Temperature_Local       = new su2double [nMarker_Analyze];
-  su2double *Surface_Density_Local           = new su2double [nMarker_Analyze];
-  su2double *Surface_Enthalpy_Local          = new su2double [nMarker_Analyze];
-  su2double *Surface_NormalVelocity_Local    = new su2double [nMarker_Analyze];
-  su2double *Surface_StreamVelocity2_Local   = new su2double [nMarker_Analyze];
-  su2double *Surface_TransvVelocity2_Local   = new su2double [nMarker_Analyze];
-  su2double *Surface_Pressure_Local          = new su2double [nMarker_Analyze];
-  su2double *Surface_TotalTemperature_Local  = new su2double [nMarker_Analyze];
-  su2double *Surface_TotalPressure_Local     = new su2double [nMarker_Analyze];
-  su2double *Surface_Area_Local              = new su2double [nMarker_Analyze];
-  su2double *Surface_MassFlow_Abs_Local      = new su2double [nMarker_Analyze];
-
-  su2double *Surface_MassFlow_Total          = new su2double [nMarker_Analyze];
-  su2double *Surface_Mach_Total              = new su2double [nMarker_Analyze];
-  su2double *Surface_Temperature_Total       = new su2double [nMarker_Analyze];
-  su2double *Surface_Density_Total           = new su2double [nMarker_Analyze];
-  su2double *Surface_Enthalpy_Total          = new su2double [nMarker_Analyze];
-  su2double *Surface_NormalVelocity_Total    = new su2double [nMarker_Analyze];
-  su2double *Surface_StreamVelocity2_Total   = new su2double [nMarker_Analyze];
-  su2double *Surface_TransvVelocity2_Total   = new su2double [nMarker_Analyze];
-  su2double *Surface_Pressure_Total          = new su2double [nMarker_Analyze];
-  su2double *Surface_TotalTemperature_Total  = new su2double [nMarker_Analyze];
-  su2double *Surface_TotalPressure_Total     = new su2double [nMarker_Analyze];
-  su2double *Surface_Area_Total              = new su2double [nMarker_Analyze];
-  su2double *Surface_MassFlow_Abs_Total      = new su2double [nMarker_Analyze];
-
-  su2double *Surface_MomentumDistortion_Total = new su2double [nMarker_Analyze];
-
-  for (iMarker_Analyze = 0; iMarker_Analyze < nMarker_Analyze; iMarker_Analyze++) {
-    Surface_MassFlow_Local[iMarker_Analyze]          = 0.0;
-    Surface_Mach_Local[iMarker_Analyze]              = 0.0;
-    Surface_Temperature_Local[iMarker_Analyze]       = 0.0;
-    Surface_Density_Local[iMarker_Analyze]           = 0.0;
-    Surface_Enthalpy_Local[iMarker_Analyze]          = 0.0;
-    Surface_NormalVelocity_Local[iMarker_Analyze]    = 0.0;
-    Surface_StreamVelocity2_Local[iMarker_Analyze]   = 0.0;
-    Surface_TransvVelocity2_Local[iMarker_Analyze]   = 0.0;
-    Surface_Pressure_Local[iMarker_Analyze]          = 0.0;
-    Surface_TotalTemperature_Local[iMarker_Analyze]  = 0.0;
-    Surface_TotalPressure_Local[iMarker_Analyze]     = 0.0;
-    Surface_Area_Local[iMarker_Analyze]              = 0.0;
-    Surface_MassFlow_Abs_Local[iMarker_Analyze]      = 0.0;
-
-    Surface_MassFlow_Total[iMarker_Analyze]          = 0.0;
-    Surface_Mach_Total[iMarker_Analyze]              = 0.0;
-    Surface_Temperature_Total[iMarker_Analyze]       = 0.0;
-    Surface_Density_Total[iMarker_Analyze]           = 0.0;
-    Surface_Enthalpy_Total[iMarker_Analyze]          = 0.0;
-    Surface_NormalVelocity_Total[iMarker_Analyze]    = 0.0;
-    Surface_StreamVelocity2_Total[iMarker_Analyze]   = 0.0;
-    Surface_TransvVelocity2_Total[iMarker_Analyze]   = 0.0;
-    Surface_Pressure_Total[iMarker_Analyze]          = 0.0;
-    Surface_TotalTemperature_Total[iMarker_Analyze]  = 0.0;
-    Surface_TotalPressure_Total[iMarker_Analyze]     = 0.0;
-    Surface_Area_Total[iMarker_Analyze]              = 0.0;
-    Surface_MassFlow_Abs_Total[iMarker_Analyze]      = 0.0;
-
-    Surface_MomentumDistortion_Total[iMarker_Analyze] = 0.0;
-
-  }
-
-  /*--- Compute the numerical fan face Mach number, mach number, temperature and the total area ---*/
-
-  for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
-
-    if (config->GetMarker_All_Analyze(iMarker) == YES)  {
-
-      for (iMarker_Analyze= 0; iMarker_Analyze < nMarker_Analyze; iMarker_Analyze++) {
-
-        /*--- Add the Surface_MassFlow, and Surface_Area to the particular boundary ---*/
-
-        if (config->GetMarker_All_TagBound(iMarker) == config->GetMarker_Analyze_TagBound(iMarker_Analyze)) {
-          Surface_MassFlow_Local[iMarker_Analyze]          += Surface_MassFlow[iMarker];
-          Surface_Mach_Local[iMarker_Analyze]              += Surface_Mach[iMarker];
-          Surface_Temperature_Local[iMarker_Analyze]       += Surface_Temperature[iMarker];
-          Surface_Density_Local[iMarker_Analyze]           += Surface_Density[iMarker];
-          Surface_Enthalpy_Local[iMarker_Analyze]          += Surface_Enthalpy[iMarker];
-          Surface_NormalVelocity_Local[iMarker_Analyze]    += Surface_NormalVelocity[iMarker];
-          Surface_StreamVelocity2_Local[iMarker_Analyze]   += Surface_StreamVelocity2[iMarker];
-          Surface_TransvVelocity2_Local[iMarker_Analyze]   += Surface_TransvVelocity2[iMarker];
-          Surface_Pressure_Local[iMarker_Analyze]          += Surface_Pressure[iMarker];
-          Surface_TotalTemperature_Local[iMarker_Analyze]  += Surface_TotalTemperature[iMarker];
-          Surface_TotalPressure_Local[iMarker_Analyze]     += Surface_TotalPressure[iMarker];
-          Surface_Area_Local[iMarker_Analyze]              += Surface_Area[iMarker];
-          Surface_MassFlow_Abs_Local[iMarker_Analyze]      += Surface_MassFlow_Abs[iMarker];
-        }
-
-      }
-
-    }
-
-  }
-
-#ifdef HAVE_MPI
-  if (config->GetComm_Level() == COMM_FULL) {
-    SU2_MPI::Allreduce(Surface_MassFlow_Local, Surface_MassFlow_Total, nMarker_Analyze, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-    SU2_MPI::Allreduce(Surface_Mach_Local, Surface_Mach_Total, nMarker_Analyze, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-    SU2_MPI::Allreduce(Surface_Temperature_Local, Surface_Temperature_Total, nMarker_Analyze, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-    SU2_MPI::Allreduce(Surface_Density_Local, Surface_Density_Total, nMarker_Analyze, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-    SU2_MPI::Allreduce(Surface_Enthalpy_Local, Surface_Enthalpy_Total, nMarker_Analyze, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-    SU2_MPI::Allreduce(Surface_NormalVelocity_Local, Surface_NormalVelocity_Total, nMarker_Analyze, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-    SU2_MPI::Allreduce(Surface_StreamVelocity2_Local, Surface_StreamVelocity2_Total, nMarker_Analyze, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-    SU2_MPI::Allreduce(Surface_TransvVelocity2_Local, Surface_TransvVelocity2_Total, nMarker_Analyze, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-    SU2_MPI::Allreduce(Surface_Pressure_Local, Surface_Pressure_Total, nMarker_Analyze, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-    SU2_MPI::Allreduce(Surface_TotalTemperature_Local, Surface_TotalTemperature_Total, nMarker_Analyze, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-    SU2_MPI::Allreduce(Surface_TotalPressure_Local, Surface_TotalPressure_Total, nMarker_Analyze, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-    SU2_MPI::Allreduce(Surface_Area_Local, Surface_Area_Total, nMarker_Analyze, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-    SU2_MPI::Allreduce(Surface_MassFlow_Abs_Local, Surface_MassFlow_Abs_Total, nMarker_Analyze, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
-  }
-#else
-
-  for (iMarker_Analyze = 0; iMarker_Analyze < nMarker_Analyze; iMarker_Analyze++) {
-    Surface_MassFlow_Total[iMarker_Analyze]          = Surface_MassFlow_Local[iMarker_Analyze];
-    Surface_Mach_Total[iMarker_Analyze]              = Surface_Mach_Local[iMarker_Analyze];
-    Surface_Temperature_Total[iMarker_Analyze]       = Surface_Temperature_Local[iMarker_Analyze];
-    Surface_Density_Total[iMarker_Analyze]           = Surface_Density_Local[iMarker_Analyze];
-    Surface_Enthalpy_Total[iMarker_Analyze]          = Surface_Enthalpy_Local[iMarker_Analyze];
-    Surface_NormalVelocity_Total[iMarker_Analyze]    = Surface_NormalVelocity_Local[iMarker_Analyze];
-    Surface_StreamVelocity2_Total[iMarker_Analyze]   = Surface_StreamVelocity2_Local[iMarker_Analyze];
-    Surface_TransvVelocity2_Total[iMarker_Analyze]   = Surface_TransvVelocity2_Local[iMarker_Analyze];
-    Surface_Pressure_Total[iMarker_Analyze]          = Surface_Pressure_Local[iMarker_Analyze];
-    Surface_TotalTemperature_Total[iMarker_Analyze]  = Surface_TotalTemperature_Local[iMarker_Analyze];
-    Surface_TotalPressure_Total[iMarker_Analyze]     = Surface_TotalPressure_Local[iMarker_Analyze];
-    Surface_Area_Total[iMarker_Analyze]              = Surface_Area_Local[iMarker_Analyze];
-    Surface_MassFlow_Abs_Total[iMarker_Analyze]      = Surface_MassFlow_Abs_Local[iMarker_Analyze];
-  }
-
-#endif
-
-  /*--- Compute the value of Surface_Area_Total, and Surface_Pressure_Total, and
-   set the value in the config structure for future use ---*/
-
-  for (iMarker_Analyze = 0; iMarker_Analyze < nMarker_Analyze; iMarker_Analyze++) {
-
-    if (Kind_Average == AVERAGE_MASSFLUX) Weight = Surface_MassFlow_Abs_Total[iMarker_Analyze];
-    else if (Kind_Average == AVERAGE_AREA) Weight = abs(Surface_Area_Total[iMarker_Analyze]);
-    else Weight = 1.0;
-
-    if (Weight != 0.0) {
-      Surface_Mach_Total[iMarker_Analyze]             /= Weight;
-      Surface_Temperature_Total[iMarker_Analyze]      /= Weight;
-      Surface_Density_Total[iMarker_Analyze]          /= Weight;
-      Surface_Enthalpy_Total[iMarker_Analyze]         /= Weight;
-      Surface_NormalVelocity_Total[iMarker_Analyze]   /= Weight;
-      Surface_Pressure_Total[iMarker_Analyze]         /= Weight;
-      Surface_TotalTemperature_Total[iMarker_Analyze] /= Weight;
-      Surface_TotalPressure_Total[iMarker_Analyze]    /= Weight;
-    }
-    else {
-      Surface_Mach_Total[iMarker_Analyze]             = 0.0;
-      Surface_Temperature_Total[iMarker_Analyze]      = 0.0;
-      Surface_Density_Total[iMarker_Analyze]          = 0.0;
-      Surface_Enthalpy_Total[iMarker_Analyze]         = 0.0;
-      Surface_NormalVelocity_Total[iMarker_Analyze]   = 0.0;
-      Surface_Pressure_Total[iMarker_Analyze]         = 0.0;
-      Surface_TotalTemperature_Total[iMarker_Analyze] = 0.0;
-      Surface_TotalPressure_Total[iMarker_Analyze]    = 0.0;
-    }
-
-    /*--- Compute flow uniformity parameters separately (always area for now). ---*/
-
-    Area = fabs(Surface_Area_Total[iMarker_Analyze]);
-
-    if (Area != 0.0) {
-      Surface_MomentumDistortion_Total[iMarker_Analyze] = Surface_StreamVelocity2_Total[iMarker_Analyze]/(Surface_NormalVelocity_Total[iMarker_Analyze]*Surface_NormalVelocity_Total[iMarker_Analyze]*Area) - 1.0;
-      Surface_StreamVelocity2_Total[iMarker_Analyze] /= Area;
-      Surface_TransvVelocity2_Total[iMarker_Analyze] /= Area;
-    }
-    else {
-      Surface_MomentumDistortion_Total[iMarker_Analyze] = 0.0;
-      Surface_StreamVelocity2_Total[iMarker_Analyze]    = 0.0;
-      Surface_TransvVelocity2_Total[iMarker_Analyze]    = 0.0;
-    }
-
-  }
-
-  for (iMarker_Analyze = 0; iMarker_Analyze < nMarker_Analyze; iMarker_Analyze++) {
-
-    su2double MassFlow = Surface_MassFlow_Total[iMarker_Analyze] * config->GetDensity_Ref() * config->GetVelocity_Ref();
-    if (config->GetSystemMeasurements() == US) MassFlow *= 32.174;
-    config->SetSurface_MassFlow(iMarker_Analyze, MassFlow);
-
-    su2double Mach = Surface_Mach_Total[iMarker_Analyze];
-    config->SetSurface_Mach(iMarker_Analyze, Mach);
-
-    su2double Temperature = Surface_Temperature_Total[iMarker_Analyze] * config->GetTemperature_Ref();
-    config->SetSurface_Temperature(iMarker_Analyze, Temperature);
-
-    su2double Pressure = Surface_Pressure_Total[iMarker_Analyze] * config->GetPressure_Ref();
-    config->SetSurface_Pressure(iMarker_Analyze, Pressure);
-
-    su2double Density = Surface_Density_Total[iMarker_Analyze] * config->GetDensity_Ref();
-    config->SetSurface_Density(iMarker_Analyze, Density);
-
-    su2double Enthalpy = Surface_Enthalpy_Total[iMarker_Analyze];
-    config->SetSurface_Enthalpy(iMarker_Analyze, Enthalpy);
-
-    su2double NormalVelocity = Surface_NormalVelocity_Total[iMarker_Analyze] * config->GetVelocity_Ref();
-    config->SetSurface_NormalVelocity(iMarker_Analyze, NormalVelocity);
-
-    su2double Uniformity = sqrt(Surface_StreamVelocity2_Total[iMarker_Analyze]) * config->GetVelocity_Ref();
-    config->SetSurface_Uniformity(iMarker_Analyze, Uniformity);
-
-    su2double SecondaryStrength = sqrt(Surface_TransvVelocity2_Total[iMarker_Analyze]) * config->GetVelocity_Ref();
-    config->SetSurface_SecondaryStrength(iMarker_Analyze, SecondaryStrength);
-
-    su2double MomentumDistortion = Surface_MomentumDistortion_Total[iMarker_Analyze];
-    config->SetSurface_MomentumDistortion(iMarker_Analyze, MomentumDistortion);
-
-    su2double SecondOverUniform = SecondaryStrength/Uniformity;
-    config->SetSurface_SecondOverUniform(iMarker_Analyze, SecondOverUniform);
-
-    su2double TotalTemperature = Surface_TotalTemperature_Total[iMarker_Analyze] * config->GetTemperature_Ref();
-    config->SetSurface_TotalTemperature(iMarker_Analyze, TotalTemperature);
-
-    su2double TotalPressure = Surface_TotalPressure_Total[iMarker_Analyze] * config->GetPressure_Ref();
-    config->SetSurface_TotalPressure(iMarker_Analyze, TotalPressure);
-
-  }
-
-  /*--- Compute the average static pressure drop between two surfaces. Note
-   that this assumes we have two surfaces being analyzed and that the outlet
-   is first followed by the inlet. This is because we may also want to choose
-   outlet values (temperature, uniformity, etc.) for our design problems,
-   which require the outlet to be listed first. This is a simple first version
-   that could be generalized to a different orders/lists/etc. ---*/
-
-  for (iMarker_Analyze = 0; iMarker_Analyze < nMarker_Analyze; iMarker_Analyze++) {
-    if (nMarker_Analyze == 2) {
-      su2double Pressure_Drop = (Surface_Pressure_Total[1]-Surface_Pressure_Total[0]) * config->GetPressure_Ref();
-      config->SetSurface_PressureDrop(iMarker_Analyze, Pressure_Drop);
-    } else {
-      config->SetSurface_PressureDrop(iMarker_Analyze, 0.0);
-    }
-  }
-
-  if ((rank == MASTER_NODE) && !config->GetDiscrete_Adjoint() && output) {
-
-    cout.precision(6);
-    cout.setf(ios::scientific, ios::floatfield);
-    cout << endl << "Computing surface mean values." << endl << endl;
-
-    for (iMarker_Analyze = 0; iMarker_Analyze < nMarker_Analyze; iMarker_Analyze++) {
-      cout << "Surface "<< config->GetMarker_Analyze_TagBound(iMarker_Analyze) << ":" << endl;
-
-      if (nDim == 3) { if (config->GetSystemMeasurements() == SI) cout << setw(20) << "Area (m^2): "; else cout << setw(20) << "Area (ft^2): "; }
-      else { if (config->GetSystemMeasurements() == SI) cout << setw(20) << "Area (m): "; else cout << setw(20) << "Area (ft): "; }
-
-      if (config->GetSystemMeasurements() == SI)      cout << setw(15) << fabs(Surface_Area_Total[iMarker_Analyze]);
-      else if (config->GetSystemMeasurements() == US) cout << setw(15) << fabs(Surface_Area_Total[iMarker_Analyze])*12.0*12.0;
-
-      cout << endl;
-
-      su2double MassFlow = config->GetSurface_MassFlow(iMarker_Analyze);
-      if (config->GetSystemMeasurements() == SI)      cout << setw(20) << "Mf (kg/s): " << setw(15) << MassFlow;
-      else if (config->GetSystemMeasurements() == US) cout << setw(20) << "Mf (lbs/s): " << setw(15) << MassFlow;
-
-      su2double NormalVelocity = config->GetSurface_NormalVelocity(iMarker_Analyze);
-      if (config->GetSystemMeasurements() == SI)      cout << setw(20) << "Vn (m/s): " << setw(15) << NormalVelocity;
-      else if (config->GetSystemMeasurements() == US) cout << setw(20) << "Vn (ft/s): " << setw(15) << NormalVelocity;
-
-      cout << endl;
-
-      su2double Uniformity = config->GetSurface_Uniformity(iMarker_Analyze);
-      if (config->GetSystemMeasurements() == SI)      cout << setw(20) << "Uniformity (m/s): " << setw(15) << Uniformity;
-      else if (config->GetSystemMeasurements() == US) cout << setw(20) << "Uniformity (ft/s): " << setw(15) << Uniformity;
-
-      su2double SecondaryStrength = config->GetSurface_SecondaryStrength(iMarker_Analyze);
-      if (config->GetSystemMeasurements() == SI)      cout << setw(20) << "Secondary (m/s): " << setw(15) << SecondaryStrength;
-      else if (config->GetSystemMeasurements() == US) cout << setw(20) << "Secondary (ft/s): " << setw(15) << SecondaryStrength;
-
-      cout << endl;
-
-      su2double MomentumDistortion = config->GetSurface_MomentumDistortion(iMarker_Analyze);
-      cout << setw(20) << "Mom. Distortion: " << setw(15) << MomentumDistortion;
-
-      su2double SecondOverUniform = config->GetSurface_SecondOverUniform(iMarker_Analyze);
-      cout << setw(20) << "Second/Uniform: " << setw(15) << SecondOverUniform;
-
-      cout << endl;
-
-      su2double Pressure = config->GetSurface_Pressure(iMarker_Analyze);
-      if (config->GetSystemMeasurements() == SI)      cout << setw(20) << "P (Pa): " << setw(15) << Pressure;
-      else if (config->GetSystemMeasurements() == US) cout << setw(20) << "P (psf): " << setw(15) << Pressure;
-
-      su2double TotalPressure = config->GetSurface_TotalPressure(iMarker_Analyze);
-      if (config->GetSystemMeasurements() == SI)      cout << setw(20) << "PT (Pa): " << setw(15) <<TotalPressure;
-      else if (config->GetSystemMeasurements() == US) cout << setw(20) << "PT (psf): " << setw(15) <<TotalPressure;
-
-      cout << endl;
-
-      su2double Mach = config->GetSurface_Mach(iMarker_Analyze);
-      cout << setw(20) << "Mach: " << setw(15) << Mach;
-
-      su2double Density = config->GetSurface_Density(iMarker_Analyze);
-      if (config->GetSystemMeasurements() == SI)      cout << setw(20) << "Rho (kg/m^3): " << setw(15) << Density;
-      else if (config->GetSystemMeasurements() == US) cout << setw(20) << "Rho (lb/ft^3): " << setw(15) << Density*32.174;
-
-      cout << endl;
-
-      if (compressible || energy) {
-        su2double Temperature = config->GetSurface_Temperature(iMarker_Analyze);
-        if (config->GetSystemMeasurements() == SI)      cout << setw(20) << "T (K): " << setw(15) << Temperature;
-        else if (config->GetSystemMeasurements() == US) cout << setw(20) << "T (R): " << setw(15) << Temperature;
-
-        su2double TotalTemperature = config->GetSurface_TotalTemperature(iMarker_Analyze);
-        if (config->GetSystemMeasurements() == SI)      cout << setw(20) << "TT (K): " << setw(15) << TotalTemperature;
-        else if (config->GetSystemMeasurements() == US) cout << setw(20) << "TT (R): " << setw(15) << TotalTemperature;
-
-        cout << endl;
-      }
-
-    }
-    cout.unsetf(ios_base::floatfield);
-
-  }
-
-  delete [] Surface_MassFlow_Local;
-  delete [] Surface_Mach_Local;
-  delete [] Surface_Temperature_Local;
-  delete [] Surface_Density_Local;
-  delete [] Surface_Enthalpy_Local;
-  delete [] Surface_NormalVelocity_Local;
-  delete [] Surface_Pressure_Local;
-  delete [] Surface_TotalTemperature_Local;
-  delete [] Surface_TotalPressure_Local;
-  delete [] Surface_Area_Local;
-  delete [] Surface_MassFlow_Abs_Local;
-
-  delete [] Surface_MassFlow_Total;
-  delete [] Surface_Mach_Total;
-  delete [] Surface_Temperature_Total;
-  delete [] Surface_Density_Total;
-  delete [] Surface_Enthalpy_Total;
-  delete [] Surface_NormalVelocity_Total;
-  delete [] Surface_Pressure_Total;
-  delete [] Surface_TotalTemperature_Total;
-  delete [] Surface_TotalPressure_Total;
-  delete [] Surface_Area_Total;
-  delete [] Surface_MassFlow_Abs_Total;
-
-  delete [] Surface_MassFlow;
-  delete [] Surface_Mach;
-  delete [] Surface_Temperature;
-  delete [] Surface_Density;
-  delete [] Surface_Enthalpy;
-  delete [] Surface_NormalVelocity;
-  delete [] Surface_Pressure;
-  delete [] Surface_TotalTemperature;
-  delete [] Surface_TotalPressure;
-  delete [] Surface_Area;
-  delete [] Vector;
-  delete [] Surface_VelocityIdeal;
-  delete [] Surface_MassFlow_Abs;
-
-}

From 26c5bf263e55f7e68e41b9bf78ca4d2d86fc3c07 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 4 Apr 2023 16:37:11 +0200
Subject: [PATCH 345/656] Pulled develop, updated MLPCpp version

---
 externals/codi         | 2 +-
 externals/meson        | 2 +-
 externals/ninja        | 2 +-
 meson_scripts/init.py  | 2 +-
 subprojects/CoolProp   | 2 +-
 subprojects/MLPCpp     | 2 +-
 subprojects/Mutationpp | 2 +-
 7 files changed, 7 insertions(+), 7 deletions(-)

diff --git a/externals/codi b/externals/codi
index 427c2dc754a..8cdb2a2e623 160000
--- a/externals/codi
+++ b/externals/codi
@@ -1 +1 @@
-Subproject commit 427c2dc754a628ad3c9310c766c988ac5ce21bc7
+Subproject commit 8cdb2a2e6231ede6343294ac9af748b3ea105ecd
diff --git a/externals/meson b/externals/meson
index 41c650a040d..3c655bca393 160000
--- a/externals/meson
+++ b/externals/meson
@@ -1 +1 @@
-Subproject commit 41c650a040d50e0912d268af7a903a9ce1456dfa
+Subproject commit 3c655bca39384c3be49204491d9a8e138484d719
diff --git a/externals/ninja b/externals/ninja
index 52649de2c56..2d9083b2608 160000
--- a/externals/ninja
+++ b/externals/ninja
@@ -1 +1 @@
-Subproject commit 52649de2c56b63f42bc59513d51286531c595b44
+Subproject commit 2d9083b2608bd60c31583193d321d13a81a75beb
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 59f9d711236..9f552ee934f 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -71,7 +71,7 @@ def init_submodules(
     github_repo_coolprop = "https://github.com/CoolProp/CoolProp"
     sha_version_mel = "2484cd3258ef800a10e361016cb341834ee7930b"
     github_repo_mel = "https://github.com/pcarruscag/MEL"
-    sha_version_mlpcpp = "a0fbc274934071331fc90b06bde6bef812cb2e42"
+    sha_version_mlpcpp = "1ff646b64de58142b5d6b9a1f15f27f08771354f"
     github_repo_mlpcpp = "https://github.com/EvertBunschoten/MLPCpp"
 
     medi_name = "MeDiPack"
diff --git a/subprojects/CoolProp b/subprojects/CoolProp
index 0ce42fcf3bb..3b510388279 160000
--- a/subprojects/CoolProp
+++ b/subprojects/CoolProp
@@ -1 +1 @@
-Subproject commit 0ce42fcf3bb2c373512bc825a4f0c1973a78f307
+Subproject commit 3b510388279d39fe63608736a00888327edc2aff
diff --git a/subprojects/MLPCpp b/subprojects/MLPCpp
index a0fbc274934..1ff646b64de 160000
--- a/subprojects/MLPCpp
+++ b/subprojects/MLPCpp
@@ -1 +1 @@
-Subproject commit a0fbc274934071331fc90b06bde6bef812cb2e42
+Subproject commit 1ff646b64de58142b5d6b9a1f15f27f08771354f
diff --git a/subprojects/Mutationpp b/subprojects/Mutationpp
index 5ff579f4378..4cb6e3a05c1 160000
--- a/subprojects/Mutationpp
+++ b/subprojects/Mutationpp
@@ -1 +1 @@
-Subproject commit 5ff579f43781cae07411e5ab46291c9971536be6
+Subproject commit 4cb6e3a05c15f49ffd346dc9f185ccc3459728b0

From 02b466c8ada5ec31e8e1456cea0a1119dce97303 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Tue, 4 Apr 2023 16:19:07 +0100
Subject: [PATCH 346/656] use the normal unsteady options for FEA problems
 instead of DYN_**

---
 Common/include/CConfig.hpp                    | 32 -------------------
 Common/include/option_structure.hpp           | 12 -------
 Common/src/CConfig.cpp                        | 21 +++++-------
 .../interfaces/fsi/CFlowTractionInterface.cpp |  2 +-
 .../src/output/output_structure_legacy.cpp    |  2 +-
 SU2_CFD/src/solvers/CFEASolver.cpp            | 15 +++++----
 .../fea_fsi/DynBeam_2d/configBeam_2d.cfg      | 19 +++++------
 7 files changed, 28 insertions(+), 75 deletions(-)

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index ba5190f4b24..d790a723604 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -150,7 +150,6 @@ class CConfig {
   su2double CL_Target;         /*!< \brief Fixed Cl mode Target Cl. */
   su2double Confinement_Param; /*!< \brief Confinement paramenter for Vorticity Confinement method. */
   TIME_MARCHING TimeMarching;        /*!< \brief Steady or unsteady (time stepping or dual time stepping) computation. */
-  unsigned short Dynamic_Analysis;   /*!< \brief Static or dynamic structural analysis. */
   su2double FixAzimuthalLine;        /*!< \brief Fix an azimuthal line due to misalignments of the nearfield. */
   su2double **DV_Value;              /*!< \brief Previous value of the design variable. */
   su2double Venkat_LimiterCoeff;     /*!< \brief Limiter coefficient */
@@ -168,9 +167,6 @@ class CConfig {
   su2double HarmonicBalance_Period;  /*!< \brief Period of oscillation to be used with harmonic balance computations. */
   su2double Delta_UnstTime,          /*!< \brief Time step for unsteady computations. */
   Delta_UnstTimeND;                  /*!< \brief Time step for unsteady computations (non dimensional). */
-  su2double Delta_DynTime,        /*!< \brief Time step for dynamic structural computations. */
-  Total_DynTime,                  /*!< \brief Total time for dynamic structural computations. */
-  Current_DynTime;                /*!< \brief Global time of the dynamic structural computations. */
   su2double Total_UnstTime,       /*!< \brief Total time for unsteady computations. */
   Total_UnstTimeND;               /*!< \brief Total time for unsteady computations (non dimensional). */
   su2double Current_UnstTime,     /*!< \brief Global time of the unsteady simulation. */
@@ -8723,34 +8719,6 @@ class CConfig {
    */
   bool GetSteadyRestart(void) const { return SteadyRestart; }
 
-  /*!
-   * \brief Provides information about the time integration of the structural analysis, and change the write in the output
-   *        files information about the iteration.
-   * \return The kind of time integration: Static or dynamic analysis
-   */
-  unsigned short GetDynamic_Analysis(void) const { return Dynamic_Analysis; }
-
-  /*!
-   * \brief If we are prforming an unsteady simulation, there is only
-   *        one value of the time step for the complete simulation.
-   * \return Value of the time step in an unsteady simulation (non dimensional).
-   */
-  su2double GetDelta_DynTime(void) const { return Delta_DynTime; }
-
-  /*!
-   * \brief If we are prforming an unsteady simulation, there is only
-   *        one value of the time step for the complete simulation.
-   * \return Value of the time step in an unsteady simulation (non dimensional).
-   */
-  su2double GetTotal_DynTime(void) const { return Total_DynTime; }
-
-  /*!
-   * \brief If we are prforming an unsteady simulation, there is only
-   *        one value of the time step for the complete simulation.
-   * \return Value of the time step in an unsteady simulation (non dimensional).
-   */
-  su2double GetCurrent_DynTime(void) const { return Current_DynTime; }
-
   /*!
    * \brief Get the current instance.
    * \return Current instance identifier.
diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index 4c934f0612b..57f89986b66 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -2368,18 +2368,6 @@ enum class RECORDING {
   SOLUTION_AND_MESH,
 };
 
-/*!
- * \brief Types of schemes for dynamic structural computations
- */
-enum ENUM_DYNAMIC {
-  STATIC = 0,     /*!< \brief A static structural computation. */
-  DYNAMIC = 1     /*!< \brief Use a time stepping strategy for dynamic computations. */
-};
-static const MapType<std::string, ENUM_DYNAMIC> Dynamic_Map = {
-  MakePair("NO", STATIC)
-  MakePair("YES", DYNAMIC)
-};
-
 /*!
  * \brief Types of input file formats
  */
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index ea45d2d0159..5b3eb0c10a0 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -2434,12 +2434,6 @@ void CConfig::SetConfig_Options() {
   /*  DESCRIPTION: Temporary: pseudo static analysis (no density in dynamic analysis)
   *  Options: NO, YES \ingroup Config */
   addBoolOption("PSEUDO_STATIC", PseudoStatic, false);
-  /* DESCRIPTION: Dynamic or static structural analysis */
-  addEnumOption("DYNAMIC_ANALYSIS", Dynamic_Analysis, Dynamic_Map, STATIC);
-  /* DESCRIPTION: Time Step for dynamic analysis (s) */
-  addDoubleOption("DYN_TIMESTEP", Delta_DynTime, 0.0);
-  /* DESCRIPTION: Total Physical Time for dual time stepping simulations (s) */
-  addDoubleOption("DYN_TIME", Total_DynTime, 1.0);
   /* DESCRIPTION: Parameter alpha for Newmark scheme (s) */
   addDoubleOption("NEWMARK_BETA", Newmark_beta, 0.25);
   /* DESCRIPTION: Parameter delta for Newmark scheme (s) */
@@ -3032,6 +3026,12 @@ void CConfig::SetConfig_Parsing(istream& config_buffer){
             newString.append("SOLID_TEMPERATURE_INIT is deprecated. Use FREESTREAM_TEMPERATURE instead.\n\n");
           else if (!option_name.compare("SA_QCR"))
             newString.append("SA_QCR is deprecated. Use SA_OPTIONS=QCR2000 instead.\n\n");
+          else if (!option_name.compare("DYN_TIMESTEP"))
+            newString.append("DYN_TIMESTEP is deprecated. Use TIME_STEP instead.\n\n");
+          else if (!option_name.compare("DYN_TIME"))
+            newString.append("DYN_TIME is deprecated. Use MAX_TIME instead.\n\n");
+          else if (!option_name.compare("DYNAMIC_ANALYSIS"))
+            newString.append("DYNAMIC_ANALYSIS is deprecated. Use TIME_DOMAIN instead.\n\n");
           else {
             /*--- Find the most likely candidate for the unrecognized option, based on the length
              of start and end character sequences shared by candidates and the option. ---*/
@@ -3707,7 +3707,6 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
 
   if (Time_Domain){
     Delta_UnstTime = Time_Step;
-    Delta_DynTime  = Time_Step;
 
     if (TimeMarching == TIME_MARCHING::TIME_STEPPING){ InnerIter = 1; }
 
@@ -6840,7 +6839,7 @@ void CConfig::SetOutput(SU2_COMPONENT val_software, unsigned short val_izone) {
   else {
     if (Time_Domain) {
       cout << "Dynamic structural analysis."<< endl;
-      cout << "Time step provided by the user for the dynamic analysis(s): "<< Delta_DynTime << "." << endl;
+      cout << "Time step provided by the user for the dynamic analysis(s): "<< Time_Step << "." << endl;
     } else {
       cout << "Static structural analysis." << endl;
     }
@@ -6915,7 +6914,7 @@ void CConfig::SetOutput(SU2_COMPONENT val_software, unsigned short val_izone) {
           cout << "Generalized-alpha method." << endl;
           break;
         case STRUCT_TIME_INT::NEWMARK_IMPLICIT:
-          if (Dynamic_Analysis) cout << "Newmark implicit method for the structural time integration." << endl;
+          if (Time_Domain) cout << "Newmark implicit method for the structural time integration." << endl;
           switch (Kind_Linear_Solver) {
             case BCGSTAB:
               cout << "BCGSTAB is used for solving the linear system." << endl;
@@ -8461,9 +8460,6 @@ void CConfig::SetGlobalParam(MAIN_SOLVER val_solver,
 
     case MAIN_SOLVER::FEM_ELASTICITY:
     case MAIN_SOLVER::DISC_ADJ_FEM:
-
-      Current_DynTime = static_cast<su2double>(TimeIter)*Delta_DynTime;
-
       if (val_system == RUNTIME_FEA_SYS) {
         SetKind_ConvNumScheme(NONE, CENTERED::NONE, UPWIND::NONE, LIMITER::NONE, NONE, NONE);
         SetKind_TimeIntScheme(NONE);
@@ -10040,7 +10036,6 @@ void CConfig::SetMultizone(const CConfig *driver_config, const CConfig* const* c
   /*--- Fix the Time Step for all subdomains, for the case of time-dependent problems ---*/
   if (driver_config->GetTime_Domain()){
     Delta_UnstTime = driver_config->GetTime_Step();
-    Delta_DynTime  = driver_config->GetTime_Step();
 
     Time_Domain = true;
   }
diff --git a/SU2_CFD/src/interfaces/fsi/CFlowTractionInterface.cpp b/SU2_CFD/src/interfaces/fsi/CFlowTractionInterface.cpp
index d95bb5a9841..1aaa0d422fe 100644
--- a/SU2_CFD/src/interfaces/fsi/CFlowTractionInterface.cpp
+++ b/SU2_CFD/src/interfaces/fsi/CFlowTractionInterface.cpp
@@ -132,7 +132,7 @@ void CFlowTractionInterface::GetPhysical_Constants(CSolver *flow_solution, CSolv
   /*--- Apply a ramp to the transfer of the fluid loads ---*/
 
   su2double ModAmpl = 0.0;
-  su2double CurrentTime = struct_config->GetCurrent_DynTime();
+  su2double CurrentTime = struct_config->GetCurrent_UnstTime();
 
   bool Ramp_Load = struct_config->GetRamp_Load();
   su2double Ramp_Time = struct_config->GetRamp_Time();
diff --git a/SU2_CFD/src/output/output_structure_legacy.cpp b/SU2_CFD/src/output/output_structure_legacy.cpp
index 40e495d6b66..896923965aa 100644
--- a/SU2_CFD/src/output/output_structure_legacy.cpp
+++ b/SU2_CFD/src/output/output_structure_legacy.cpp
@@ -1670,7 +1670,7 @@ void COutputLegacy::SetConvHistoryBody(ofstream *ConvHist_file,
           }
           else if (fem && !fsi) {
             if (dynamic) {
-              cout << endl << "Simulation time: " << config[val_iZone]->GetCurrent_DynTime() << ". Time step: " << config[val_iZone]->GetDelta_DynTime() << ".";
+              //cout << endl << "Simulation time: " << config[val_iZone]->GetCurrent_DynTime() << ". Time step: " << config[val_iZone]->GetDelta_DynTime() << ".";
             }
           }
 
diff --git a/SU2_CFD/src/solvers/CFEASolver.cpp b/SU2_CFD/src/solvers/CFEASolver.cpp
index 4f30cb91450..96d2c6e0a72 100644
--- a/SU2_CFD/src/solvers/CFEASolver.cpp
+++ b/SU2_CFD/src/solvers/CFEASolver.cpp
@@ -50,6 +50,7 @@ CFEASolver::CFEASolver(LINEAR_SOLVER_MODE mesh_deform_mode) : CFEASolverBase(mes
 CFEASolver::CFEASolver(CGeometry *geometry, CConfig *config) : CFEASolverBase(geometry, config) {
 
   bool dynamic = (config->GetTime_Domain());
+  config->SetDelta_UnstTimeND(config->GetDelta_UnstTime());
 
   /*--- Test whether we consider dielectric elastomers ---*/
   bool de_effects = config->GetDE_Effects();
@@ -1282,7 +1283,7 @@ void CFEASolver::Compute_NodalStress(CGeometry *geometry, CNumerics **numerics,
 
   if (outputReactions) {
 
-    bool dynamic = (config->GetDynamic_Analysis() == DYNAMIC);
+    const bool dynamic = config->GetTime_Domain();
 
     ofstream myfile;
     myfile.open ("Reactions.txt");
@@ -1481,7 +1482,7 @@ void CFEASolver::Compute_DeadLoad(CGeometry *geometry, CNumerics **numerics, con
 
 void CFEASolver::Compute_IntegrationConstants(const CConfig *config) {
 
-  su2double Delta_t= config->GetDelta_DynTime();
+  su2double Delta_t= config->GetDelta_UnstTime();
 
   su2double gamma = config->GetNewmark_gamma(), beta = config->GetNewmark_beta();
 
@@ -1652,7 +1653,7 @@ void CFEASolver::BC_DispDir(CGeometry *geometry, const CConfig *config, unsigned
   const su2double *DispDirLocal = config->GetDisp_Dir(TagBound);
   su2double DispDirMod = Norm(nDim, DispDirLocal);
 
-  su2double CurrentTime = config->GetCurrent_DynTime();
+  su2double CurrentTime = config->GetCurrent_UnstTime();
   su2double RampTime = config->GetRamp_Time();
   su2double ModAmpl = Compute_LoadCoefficient(CurrentTime, RampTime, config);
 
@@ -1818,7 +1819,7 @@ void CFEASolver::BC_Normal_Load(CGeometry *geometry, const CConfig *config, unsi
 
   /*--- Retrieve the normal pressure and the application conditions for the considered boundary. ---*/
 
-  su2double CurrentTime = config->GetCurrent_DynTime();
+  su2double CurrentTime = config->GetCurrent_UnstTime();
   su2double Ramp_Time = config->GetRamp_Time();
   su2double ModAmpl = Compute_LoadCoefficient(CurrentTime, Ramp_Time, config);
 
@@ -1914,7 +1915,7 @@ void CFEASolver::BC_Dir_Load(CGeometry *geometry, const CConfig *config, unsigne
   /*--- Compute the norm of the vector that was passed in the config file. ---*/
   su2double LoadNorm = Norm(nDim, Load_Dir_Local);
 
-  su2double CurrentTime=config->GetCurrent_DynTime();
+  su2double CurrentTime=config->GetCurrent_UnstTime();
   su2double Ramp_Time = config->GetRamp_Time();
   su2double ModAmpl = Compute_LoadCoefficient(CurrentTime, Ramp_Time, config);
 
@@ -2036,7 +2037,7 @@ su2double CFEASolver::Compute_LoadCoefficient(su2double CurrentTime, su2double R
 
   /*--- This offset introduces the ramp load in dynamic cases starting from the restart point. ---*/
   bool offset = (restart && fsi && (!stat_fsi));
-  su2double DeltaT = config->GetDelta_DynTime();
+  su2double DeltaT = config->GetDelta_UnstTime();
   su2double OffsetTime = offset? DeltaT * (config->GetRestart_Iter()-1) : su2double(0.0);
 
   /*--- Polynomial functions from https://en.wikipedia.org/wiki/Smoothstep ---*/
@@ -2507,7 +2508,7 @@ void CFEASolver::Solve_System(CGeometry *geometry, CConfig *config) {
 void CFEASolver::PredictStruct_Displacement(CGeometry *geometry, const CConfig *config) {
 
   const unsigned short predOrder = config->GetPredictorOrder();
-  const su2double Delta_t = config->GetDelta_DynTime();
+  const su2double Delta_t = config->GetDelta_UnstTime();
   const bool dynamic = config->GetTime_Domain();
 
   if(predOrder > 2 && rank == MASTER_NODE)
diff --git a/TestCases/fea_fsi/DynBeam_2d/configBeam_2d.cfg b/TestCases/fea_fsi/DynBeam_2d/configBeam_2d.cfg
index c4181d6339d..1df1677212b 100644
--- a/TestCases/fea_fsi/DynBeam_2d/configBeam_2d.cfg
+++ b/TestCases/fea_fsi/DynBeam_2d/configBeam_2d.cfg
@@ -18,7 +18,7 @@ RESTART_ITER= 1
 ELASTICITY_MODULUS=3E7
 POISSON_RATIO=0.3
 MATERIAL_DENSITY=7854
-FORMULATION_ELASTICITY_2D = PLANE_STRESS
+FORMULATION_ELASTICITY_2D= PLANE_STRESS
 TIME_DOMAIN=YES
 TIME_STEP=0.01
 MAX_TIME= 0.1
@@ -27,17 +27,18 @@ TIME_ITER=7
 TIME_DISCRE_FEA= NEWMARK_IMPLICIT
 NEWMARK_BETA=0.2601
 NEWMARK_GAMMA=0.52
-MARKER_CLAMPED = ( left , right )
-MARKER_PRESSURE= ( lower, 0)
-MARKER_LOAD= ( upper, 1, 1000, 0, -1, 0)
-LINEAR_SOLVER= FGMRES
-LINEAR_SOLVER_PREC= LU_SGS
-LINEAR_SOLVER_ERROR= 1E-8
-LINEAR_SOLVER_ITER= 1000
+MARKER_CLAMPED= ( left , right )
+MARKER_PRESSURE= ( lower, 0 )
+MARKER_LOAD= ( upper, 1, 1000, 0, -1, 0 )
+LINEAR_SOLVER= CONJUGATE_GRADIENT
+LINEAR_SOLVER_PREC= ILU
+LINEAR_SOLVER_ERROR= 1E-6
+LINEAR_SOLVER_ITER= 100
 MESH_FORMAT= SU2
 TABULAR_FORMAT= CSV
 VOLUME_FILENAME= beam
 RESTART_FILENAME= restart_beam.dat
 SOLUTION_FILENAME= solution_beam.dat
 OUTPUT_WRT_FREQ= 1
-OUTPUT_FILES= (RESTART_ASCII)
+OUTPUT_FILES= RESTART_ASCII, PARAVIEW
+SCREEN_OUTPUT= CUR_TIME, INNER_ITER, RMS_RES, LINSOL

From 815d3f074180bc4e3a259c53d9c874a9ce0ec65a Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Wed, 5 Apr 2023 04:30:38 -0700
Subject: [PATCH 347/656] remove "testcase".new_output = True because it is the
 default

---
 TestCases/hybrid_regression.py   | 11 -----
 TestCases/parallel_regression.py | 39 ----------------
 TestCases/serial_regression.py   | 80 --------------------------------
 TestCases/tutorials.py           |  5 --
 4 files changed, 135 deletions(-)

diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index e00948e9ff7..4a1719013fc 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -330,7 +330,6 @@ def main():
     harmonic_balance.cfg_file  = "HB.cfg"
     harmonic_balance.test_iter = 25
     harmonic_balance.test_vals = [-1.589740, 3.922578, 0.006703, 0.099632]
-    harmonic_balance.new_output = False
     test_list.append(harmonic_balance)
 
     # Turbulent pitching NACA 64a010 airfoil
@@ -339,7 +338,6 @@ def main():
     hb_rans_preconditioning.cfg_file  = "davis.cfg"
     hb_rans_preconditioning.test_iter = 25
     hb_rans_preconditioning.test_vals = [-1.902111, -5.949288, 0.007768, 0.128060]
-    hb_rans_preconditioning.new_output = False
     test_list.append(hb_rans_preconditioning)
 
     #############################
@@ -352,7 +350,6 @@ def main():
     inc_euler_naca0012.cfg_file  = "incomp_NACA0012.cfg"
     inc_euler_naca0012.test_iter = 20
     inc_euler_naca0012.test_vals = [-4.858287, -3.810487, 0.491850, 0.007002]
-    inc_euler_naca0012.new_output = True
     test_list.append(inc_euler_naca0012)
 
     # C-D nozzle with pressure inlet and mass flow outlet
@@ -362,7 +359,6 @@ def main():
     inc_nozzle.test_iter = 20
     inc_nozzle.test_vals         = [-5.971249, -4.910844, -0.000196, 0.121635]
     inc_nozzle.test_vals_aarch64 = [-5.971248, -4.910844, -0.000196, 0.121635]
-    inc_nozzle.new_output = True
     test_list.append(inc_nozzle)
 
     #############################
@@ -375,7 +371,6 @@ def main():
     inc_lam_cylinder.cfg_file  = "incomp_cylinder.cfg"
     inc_lam_cylinder.test_iter = 10
     inc_lam_cylinder.test_vals = [-4.004277, -3.227956, 0.003851, 7.626583]
-    inc_lam_cylinder.new_output  = True
     test_list.append(inc_lam_cylinder)
 
     # Buoyancy-driven cavity
@@ -384,7 +379,6 @@ def main():
     inc_buoyancy.cfg_file  = "lam_buoyancy_cavity.cfg"
     inc_buoyancy.test_iter = 20
     inc_buoyancy.test_vals = [-4.432484, 0.507522, 0.000000, 0.000000]
-    inc_buoyancy.new_output  = True
     test_list.append(inc_buoyancy)
 
     # Laminar heated cylinder with polynomial fluid model
@@ -394,7 +388,6 @@ def main():
     inc_poly_cylinder.test_iter = 20
     inc_poly_cylinder.test_vals         = [-7.851512, -2.093420, 0.029974, 1.921595, -175.300000]
     inc_poly_cylinder.test_vals_aarch64 = [-7.851510, -2.093419, 0.029974, 1.921595, -175.300000]
-    inc_poly_cylinder.new_output  = True
     test_list.append(inc_poly_cylinder)
 
     # X-coarse laminar bend as a mixed element CGNS test
@@ -416,7 +409,6 @@ def main():
     inc_turb_naca0012.cfg_file  = "naca0012.cfg"
     inc_turb_naca0012.test_iter = 20
     inc_turb_naca0012.test_vals = [-4.788405, -11.040493, 0.000008, 0.309506]
-    inc_turb_naca0012.new_output  = True
     test_list.append(inc_turb_naca0012)
 
     # NACA0012, SST_SUST
@@ -548,7 +540,6 @@ def main():
     Jones_tc_restart.cfg_file  = "Jones_restart.cfg"
     Jones_tc_restart.test_iter = 5
     Jones_tc_restart.test_vals = [-10.691521, -7.643723, 85.827890, 2.277151]
-    Jones_tc_restart.new_output = False
     test_list.append(Jones_tc_restart)
 
     # 2D axial stage
@@ -558,7 +549,6 @@ def main():
     axial_stage2D.test_iter = 20
     axial_stage2D.test_vals         = [-1.937003, 5.338805, 73.357170, 0.915734]
     axial_stage2D.test_vals_aarch64 = [-1.933115, 5.365583, 73.354510, 0.925902]
-    axial_stage2D.new_output = False
     test_list.append(axial_stage2D)
 
     # 2D transonic stator restart
@@ -568,7 +558,6 @@ def main():
     transonic_stator_restart.test_iter = 20
     transonic_stator_restart.test_vals         = [-6.796363, -0.743837, 5.003453, 0.002946]
     transonic_stator_restart.test_vals_aarch64 = [-6.619122, -0.615705, 5.002986, 0.002951]
-    transonic_stator_restart.new_output = False
     test_list.append(transonic_stator_restart)
 
     ######################################
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 1b359311076..98e7c000378 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -48,7 +48,6 @@ def main():
     thermalbath.cfg_file = "thermalbath.cfg"
     thermalbath.test_iter = 10
     thermalbath.test_vals = [0.945997, 0.945997, -12.039262, -12.171767, -32.000000, 10.013239]
-    thermalbath.new_output = True
     test_list.append(thermalbath)
 
     # Adiabatic thermal bath
@@ -58,7 +57,6 @@ def main():
     ionized.test_iter = 10
     ionized.test_vals = [-29.806157, -11.130797, -11.337264, -17.235059, -17.578729, -15.190274, -25.013626, -32.000000, -5.174887, 0.000000, 0.000000]
     ionized.test_vals_aarch64 = [-29.816386, -10.729986, -11.720016, -17.484469, -18.237891, -15.241605, -24.956918, -32.000000, -5.727244, 0.000000, 0.000000]
-    ionized.new_output = True
     test_list.append(ionized)
 
     # Adiabatic frozen thermal bath
@@ -67,7 +65,6 @@ def main():
     thermalbath_frozen.cfg_file = "thermalbath_frozen.cfg"
     thermalbath_frozen.test_iter = 10
     thermalbath_frozen.test_vals = [-32.000000, -32.000000, -11.962477, -11.962477, -32.000000, 10.013545]
-    thermalbath_frozen.new_output = True
     test_list.append(thermalbath_frozen)
 
     # Inviscid single wedge, ausm, implicit
@@ -77,7 +74,6 @@ def main():
     invwedge_a.test_iter = 10
     invwedge_a.test_vals = [-1.042842, -1.567605, -18.301264, -18.628631, -18.574668, 2.275192, 1.879772, 5.319421, 0.873699]
     invwedge_a.test_vals_aarch64 = [-1.042842, -1.567605, -18.301264, -18.628631, -18.574668, 2.275192, 1.879772, 5.319421, 0.873699]
-    invwedge_a.new_output = True
     test_list.append(invwedge_a)
 
     # Inviscid single wedge, ausm+-up2, implicit
@@ -87,7 +83,6 @@ def main():
     invwedge_ap2.test_iter = 10
     invwedge_ap2.test_vals = [-0.952589, -1.477352, -16.736014, -17.064021, -17.009120, 2.387086, 1.287286, 5.403046, 0.956402]
     invwedge_ap2.test_vals_aarch64 = [-0.952589, -1.477352, -16.736014, -17.064021, -17.009120, 2.387086, 1.287286, 5.403046, 0.956402]
-    invwedge_ap2.new_output = True
     test_list.append(invwedge_ap2)
 
     # Inviscid single wedge, msw, implicit
@@ -97,7 +92,6 @@ def main():
     invwedge_msw.test_iter = 10
     invwedge_msw.test_vals = [-1.165957, -1.690720, -18.298756, -18.626164, -18.572159, 2.151638, 1.721236, 5.193813, 0.751584]
     invwedge_msw.test_vals_aarch64 = [-1.165957, -1.690720, -18.298756, -18.626164, -18.572159, 2.151638, 1.721236, 5.193813, 0.751584]
-    invwedge_msw.new_output = True
     test_list.append(invwedge_msw)
 
     # Inviscid single wedge, roe, implicit
@@ -107,7 +101,6 @@ def main():
     invwedge_roe.test_iter = 10
     invwedge_roe.test_vals = [-1.038582, -1.563344, -18.300307, -18.627706, -18.573706, 2.278987, 1.861307, 5.323753, 0.874900]
     invwedge_roe.test_vals_aarch64 = [-1.038582, -1.563344, -18.300307, -18.627706, -18.573706, 2.278987, 1.861307, 5.323753, 0.874900]
-    invwedge_roe.new_output = True
     test_list.append(invwedge_roe)
 
     # Inviscid single wedge, lax, implicit
@@ -117,7 +110,6 @@ def main():
     invwedge_lax.test_iter = 10
     invwedge_lax.test_vals = [-1.075662, -1.600425, -32.000000, -32.000000, -24.972431, 2.252952, 1.725158, 5.282140, 0.848823]
     invwedge_lax.test_vals_aarch64 = [-1.075662, -1.600425, -32.000000, -32.000000, -24.972431, 2.252952, 1.725158, 5.282140, 0.848823]
-    invwedge_lax.new_output = True
     test_list.append(invwedge_lax)
 
     # Inviscid single wedge, implicit, AUSM+M scheme
@@ -127,7 +119,6 @@ def main():
     invwedge_ausm_m.test_iter = 10
     invwedge_ausm_m.test_vals = [-1.055083, -1.579845, -16.739725, -17.063618, -17.012831, 2.265430, 1.797602, 5.302740, 0.85654]
     invwedge_ausm_m.test_vals_aarch64 = [-1.055083, -1.579845, -16.739725, -17.063618, -17.012831, 2.265430, 1.797602, 5.302740, 0.85654]
-    invwedge_ausm_m.new_output = True
     test_list.append(invwedge_ausm_m)
 
     # Inviscid single wedge, implicit, NEMO supersonic inlet
@@ -137,7 +128,6 @@ def main():
     invwedge_ss_inlet.test_iter = 10
     invwedge_ss_inlet.test_vals = [-1.042718, -1.567481, -18.250175, -18.579516, -18.523248, 2.275305, 1.880068, 5.319548, 0.873821]
     invwedge_ss_inlet.test_vals_aarch64 = [-1.042718, -1.567481, -18.250175, -18.579516, -18.523248, 2.275305, 1.880068, 5.319548, 0.873821]
-    invwedge_ss_inlet.new_output = True
     test_list.append(invwedge_ss_inlet)
 
     # Viscous single cone - axisymmetric
@@ -147,7 +137,6 @@ def main():
     visc_cone.test_iter = 10
     visc_cone.test_vals = [-5.222212, -5.746462, -20.559802, -20.510196, -20.439814, 1.255865, -3.208363, -0.016006, 0.093455, 32633.000000]
     visc_cone.test_vals_aarch64 = [-5.222212, -5.746462, -20.559802, -20.510196, -20.439814, 1.255865, -3.208363, -0.016006, 0.093455, 32633.000000]
-    visc_cone.new_output = True
     test_list.append(visc_cone)
 
     # Viscous single wedge with Mutation++
@@ -156,7 +145,6 @@ def main():
     #viscwedge_mpp.cfg_file = "viscwedge_mpp.cfg"
     #viscwedge_mpp.test_iter = 10
     #viscwedge_mpp.test_vals = [-20.608474, -20.586446,-20.707524, -5.171304,-5.696067,-1.548350,-2.071211,2.231054,-2.545494]
-    #viscwedge_mpp.new_output = True
     #test_list.append(viscwedge_mpp)
 
     # Viscous single wedge - super catalytic walls
@@ -165,7 +153,6 @@ def main():
     super_cat.cfg_file = "super_cat.cfg"
     super_cat.test_iter = 10
     super_cat.test_vals = [-5.232590, -5.757884, -20.641547, -20.640244, -20.539243, 1.246889, -3.205235, -0.028406, 0.250857, 32459.000000]
-    super_cat.new_output = True
     test_list.append(super_cat)
 
     # Viscous single wedge - partially catalytic walls
@@ -174,7 +161,6 @@ def main():
     partial_cat.cfg_file = "partial_cat.cfg"
     partial_cat.test_iter = 10
     partial_cat.test_vals = [-5.210300, -5.735063, -20.880374, -20.825890, -23.475263, 1.806281, -2.813924, -0.078469, 0.496017, 2.9021e+04]
-    partial_cat.new_output = True
     test_list.append(partial_cat)
 
     # Viscous cylinder, ionization, Gupta-Yos
@@ -183,7 +169,6 @@ def main():
     ion_gy.cfg_file = "cyl_ion_gy.cfg"
     ion_gy.test_iter = 10
     ion_gy.test_vals = [-11.629873, -4.165563, -4.702662, -4.950351, -5.146155, -4.993878, -6.893332, 5.990109, 5.990004, -0.014849, 0.000000, 90090.000000]
-    ion_gy.new_output = True
     test_list.append(ion_gy)
 
     ##########################
@@ -653,7 +638,6 @@ def main():
     turbmod_sa_bsl_rae2822.cfg_file  = "turb_SA_BSL_RAE2822.cfg"
     turbmod_sa_bsl_rae2822.test_iter = 20
     turbmod_sa_bsl_rae2822.test_vals = [-2.004689, 0.742306, 0.497308, -5.265793, 0.809463, 0.062016]
-    turbmod_sa_bsl_rae2822.new_output = True
     test_list.append(turbmod_sa_bsl_rae2822)
 
     # SA Negative
@@ -663,7 +647,6 @@ def main():
     turbmod_sa_neg_rae2822.test_iter = 10
     turbmod_sa_neg_rae2822.test_vals         = [-1.374695, 1.976506, 1.898195, 4.831133, 1.187310, 0.426019, -86764]
     turbmod_sa_neg_rae2822.test_vals_aarch64 = [-1.347530, 1.439078, 1.306846, -1.928774, 1.480543, 0.571601, -91503]
-    turbmod_sa_neg_rae2822.new_output = True
     test_list.append(turbmod_sa_neg_rae2822)
 
     # SA Compressibility Correction
@@ -672,7 +655,6 @@ def main():
     turbmod_sa_comp_rae2822.cfg_file  = "turb_SA_COMP_RAE2822.cfg"
     turbmod_sa_comp_rae2822.test_iter = 20
     turbmod_sa_comp_rae2822.test_vals = [-2.004687, 0.742304, 0.497309, -5.266081, 0.809467, 0.062029]
-    turbmod_sa_comp_rae2822.new_output = True
     test_list.append(turbmod_sa_comp_rae2822)
 
     # SA Edwards
@@ -681,7 +663,6 @@ def main():
     turbmod_sa_edw_rae2822.cfg_file  = "turb_SA_EDW_RAE2822.cfg"
     turbmod_sa_edw_rae2822.test_iter = 20
     turbmod_sa_edw_rae2822.test_vals = [-2.004687, 0.742306, 0.497310, -5.290769, 0.809485, 0.062036]
-    turbmod_sa_edw_rae2822.new_output = True
     test_list.append(turbmod_sa_edw_rae2822)
 
     # SA Compressibility and Edwards
@@ -690,7 +671,6 @@ def main():
     turbmod_sa_comp_edw_rae2822.cfg_file  = "turb_SA_COMP_EDW_RAE2822.cfg"
     turbmod_sa_comp_edw_rae2822.test_iter = 20
     turbmod_sa_comp_edw_rae2822.test_vals = [-2.004685, 0.742307, 0.497311, -5.290750, 0.809487, 0.062045]
-    turbmod_sa_comp_edw_rae2822.new_output = True
     test_list.append(turbmod_sa_comp_edw_rae2822)
 
     # SA QCR
@@ -699,7 +679,6 @@ def main():
     turbmod_sa_qcr_rae2822.cfg_file  = "turb_SA_QCR_RAE2822.cfg"
     turbmod_sa_qcr_rae2822.test_iter = 20
     turbmod_sa_qcr_rae2822.test_vals = [-2.004793, 0.742353, 0.497315, -5.265974, 0.807841, 0.062027]
-    turbmod_sa_qcr_rae2822.new_output = True
     test_list.append(turbmod_sa_qcr_rae2822)
 
     ############################
@@ -864,7 +843,6 @@ def main():
     harmonic_balance.cfg_file  = "HB.cfg"
     harmonic_balance.test_iter = 25
     harmonic_balance.test_vals = [-1.589739, 3.922579, 0.006702, 0.099632]
-    harmonic_balance.new_output = False
     test_list.append(harmonic_balance)
 
     # Turbulent pitching NACA 64a010 airfoil
@@ -873,7 +851,6 @@ def main():
     hb_rans_preconditioning.cfg_file  = "davis.cfg"
     hb_rans_preconditioning.test_iter = 25
     hb_rans_preconditioning.test_vals = [-1.902098, -5.949275, 0.007768, 0.128061]
-    hb_rans_preconditioning.new_output = False
     test_list.append(hb_rans_preconditioning)
 
     ######################################
@@ -1008,7 +985,6 @@ def main():
     Jones_tc_restart.cfg_file  = "Jones_restart.cfg"
     Jones_tc_restart.test_iter = 5
     Jones_tc_restart.test_vals = [-10.691504, -7.643703, 85.827890, 2.277151]
-    Jones_tc_restart.new_output = False
     test_list.append(Jones_tc_restart)
 
     # 2D axial stage
@@ -1017,7 +993,6 @@ def main():
     axial_stage2D.cfg_file  = "Axial_stage2D.cfg"
     axial_stage2D.test_iter = 20
     axial_stage2D.test_vals = [-1.937007, 5.338943, 73.357200, 0.915725]
-    axial_stage2D.new_output = False
     test_list.append(axial_stage2D)
 
     # 2D transonic stator restart
@@ -1026,7 +1001,6 @@ def main():
     transonic_stator_restart.cfg_file  = "transonic_stator_restart.cfg"
     transonic_stator_restart.test_iter = 20
     transonic_stator_restart.test_vals = [-6.801911, -0.746307, 5.003453, 0.002946]
-    transonic_stator_restart.new_output = False
     test_list.append(transonic_stator_restart)
 
     ######################################
@@ -1197,7 +1171,6 @@ def main():
     p1rad           = TestCase('p1rad')
     p1rad.cfg_dir   = "radiation/p1model"
     p1rad.cfg_file  = "configp1.cfg"
-    p1rad.new_output= True
     p1rad.test_iter = 100
     p1rad.test_vals = [-7.743666, -7.921411, -2.111848, 0.098302, -45.023000]
     test_list.append(p1rad)
@@ -1319,7 +1292,6 @@ def main():
     pywrapper_unsteadyCHT.test_vals     = [-1.614167, 2.245725, -0.001241, 0.175713]
     pywrapper_unsteadyCHT.command       = TestCase.Command("mpirun -np 2", "python", "launch_unsteady_CHT_FlatPlate.py --parallel -f")
     pywrapper_unsteadyCHT.unsteady      = True
-    pywrapper_unsteadyCHT.new_output    = True
     test_list.append(pywrapper_unsteadyCHT)
 
     # Rigid motion
@@ -1410,7 +1382,6 @@ def main():
     species2_primitiveVenturi_mixingmodel.cfg_file  = "species2_primitiveVenturi_mixingmodel.cfg"
     species2_primitiveVenturi_mixingmodel.test_iter = 50
     species2_primitiveVenturi_mixingmodel.test_vals = [-5.447741, -4.578625, -4.560889, -5.671675, -0.069655, -5.630277, 5.000000, -1.714271, 5.000000, -4.878115, 5.000000, -1.254671, 0.000418, 0.000394, 0.000024, 0.000000]
-    species2_primitiveVenturi_mixingmodel.new_output = True
     test_list.append(species2_primitiveVenturi_mixingmodel)
 
     # 2 species (1 eq) primitive venturi mixing using mixing model and bounded scalar transport
@@ -1419,7 +1390,6 @@ def main():
     species2_primitiveVenturi_mixingmodel_boundedscalar.cfg_file  = "species2_primitiveVenturi_mixingmodel_boundedscalar.cfg"
     species2_primitiveVenturi_mixingmodel_boundedscalar.test_iter = 50
     species2_primitiveVenturi_mixingmodel_boundedscalar.test_vals = [-5.398649, -4.476373, -4.477258, -5.733271, -0.122667, -5.687136, 5.000000, -1.797791, 5.000000, -4.942913, 5.000000, -2.082842, 0.000295, 0.000295, 0.000000, 0.000000]
-    species2_primitiveVenturi_mixingmodel_boundedscalar.new_output = True
     test_list.append(species2_primitiveVenturi_mixingmodel_boundedscalar)
 
     # 2 species (1 eq) primitive venturi mixing using mixing model including viscosity, thermal conductivity and inlet markers for SA turbulence model
@@ -1428,7 +1398,6 @@ def main():
     species2_primitiveVenturi_mixingmodel_viscosity.cfg_file  = "species2_primitiveVenturi_mixingmodel_viscosity.cfg"
     species2_primitiveVenturi_mixingmodel_viscosity.test_iter = 50
     species2_primitiveVenturi_mixingmodel_viscosity.test_vals = [-4.843487, -3.585775, -3.486490, -7.560246, -5.094190, 5.000000, -1.898139, 5.000000, -3.329399, 5.000000, -2.113219, 2.482224, 0.974144, 0.607217, 0.900862]
-    species2_primitiveVenturi_mixingmodel_viscosity.new_output = True
     test_list.append(species2_primitiveVenturi_mixingmodel_viscosity)
 
     # 2 species (1 eq) primitive venturi mixing using mixing model including heat capacity and mass diffusivity
@@ -1437,7 +1406,6 @@ def main():
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg_file  = "species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg"
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.test_iter = 50
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.test_vals = [-6.113626, -4.989076, -4.880565, -7.351737, 2.452701, -5.627391, 30.000000, -5.721303, 11.000000, -8.001991, 10.000000, -8.813670, 2.084143, 1.000000, 0.600000, 0.484143]
-    species2_primitiveVenturi_mixingmodel_heatcapacity_H2.new_output = True
     test_list.append(species2_primitiveVenturi_mixingmodel_heatcapacity_H2)
 
     # 2 species (1 eq) primitive venturi mixing using mixing model including heat capacity and mass diffusivity NonDimensional case
@@ -1446,7 +1414,6 @@ def main():
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg_file  = "species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg"
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.test_iter = 50
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.test_vals = [-5.719472, -5.293846, -5.185419, -8.355307, 2.147874, -5.233215, 30.000000, -5.721396, 11.000000, -8.000062, 10.000000, -8.814100, 2.084145, 1.000000, 0.600000, 0.484145]
-    species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.new_output = True
     test_list.append(species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND)
 
     # 2 species (1 eq) primitive venturi mixing
@@ -1455,7 +1422,6 @@ def main():
     species2_primitiveVenturi.cfg_file  = "species2_primitiveVenturi.cfg"
     species2_primitiveVenturi.test_iter = 50
     species2_primitiveVenturi.test_vals = [-6.004340, -5.236017, -5.080329, -5.888785, -1.554476, -6.076144, 5.000000, -0.808416, 5.000000, -2.325030, 5.000000, -0.238222, 0.000089, 0.000088, 0.000001, 0.000000]
-    species2_primitiveVenturi.new_output = True
     test_list.append(species2_primitiveVenturi)
 
     # 2 species (1 eq) primitive venturi mixing with bounded scalar transport
@@ -1464,7 +1430,6 @@ def main():
     species_primitiveVenturi_boundedscalar.cfg_file    = "species2_primitiveVenturi_boundedscalar.cfg"
     species_primitiveVenturi_boundedscalar.test_iter   = 50
     species_primitiveVenturi_boundedscalar.test_vals   = [-5.297585, -4.397797, -4.377086, -5.593131, -1.011782, -5.623540, 5.000000, -1.775123, 5.000000, -4.086339, 5.000000, -2.080187, 0.000424, 0.000424, 0.000000, 0.000000]
-    species_primitiveVenturi_boundedscalar.new_output  = True
     test_list.append(species_primitiveVenturi_boundedscalar)
 
     # 2 species (1 eq) primitive venturi mixing using mixing model including inlet markers for turbulent intensity and viscosity ratios
@@ -1473,7 +1438,6 @@ def main():
     species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg_file  = "species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg"
     species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.test_iter = 50
     species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.test_vals = [-4.012157, -1.650191, -1.405134, -0.990205, 1.619918, -3.764227, 23.000000, -5.039466, 12.000000, -5.346201, 4.000000, -6.084514, 2.000000, 1.000000, 0.000000, 1.000000]
-    species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.new_output = True
     test_list.append(species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS)
 
     # 3 species (2 eq) primitive venturi mixing with inlet files.
@@ -1483,7 +1447,6 @@ def main():
     species3_primitiveVenturi_inletFile.cfg_file  = "species3_primitiveVenturi_inletFile.cfg"
     species3_primitiveVenturi_inletFile.test_iter = 50
     species3_primitiveVenturi_inletFile.test_vals = [-6.074971, -5.306648, -5.150960, -5.959416, -1.625107, -6.343704, -6.460033, 5.000000, -0.808413, 5.000000, -2.325029, 5.000000, -0.274923]
-    species3_primitiveVenturi_inletFile.new_output = True
     test_list.append(species3_primitiveVenturi_inletFile)
 
     # rectangle passive transport validation
@@ -1493,7 +1456,6 @@ def main():
     species_passive_val.test_iter = 50
     species_passive_val.test_vals =         [-16.559189, -16.315116, -16.908670, -4.257599, 10, -4.523292, 8, -5.19335, 0.18661, 0]
     species_passive_val.test_vals_aarch64 = [-16.538551, -16.312552, -16.882823, -4.257599, 10, -4.585464, 8, -5.19335, 0.18661, 0]
-    species_passive_val.new_output = True
     test_list.append(species_passive_val)
 
     # species transport, 3 species with multizone (2 fluid regions)
@@ -1502,7 +1464,6 @@ def main():
     species3_multizone_restart.cfg_file  = "configMaster.cfg"
     species3_multizone_restart.test_iter = 5
     species3_multizone_restart.test_vals = [-6.571720, -6.086110]
-    species3_multizone_restart.new_output = True
     species3_multizone_restart.multizone = True
     test_list.append(species3_multizone_restart)
 
diff --git a/TestCases/serial_regression.py b/TestCases/serial_regression.py
index 74068920570..c1d62447764 100644
--- a/TestCases/serial_regression.py
+++ b/TestCases/serial_regression.py
@@ -46,7 +46,6 @@ def main():
     thermalbath.cfg_file  = "thermalbath.cfg"
     thermalbath.test_iter = 10
     thermalbath.test_vals = [0.945997, 0.945997, -12.018025, -12.217291, -32.000000, 10.013239]
-    thermalbath.new_output = True
     test_list.append(thermalbath)
 
     # Adiabatic frozen thermal bath
@@ -55,7 +54,6 @@ def main():
     thermalbath_frozen.cfg_file  = "thermalbath_frozen.cfg"
     thermalbath_frozen.test_iter = 10
     thermalbath_frozen.test_vals = [-32.000000, -32.000000, -12.018022, -11.978730, -32.000000, 10.013545]
-    thermalbath_frozen.new_output = True
     test_list.append(thermalbath_frozen)
 
     # Inviscid single wedge, implicit
@@ -65,7 +63,6 @@ def main():
     invwedge.test_iter = 10
     invwedge.test_vals = [-1.046323, -1.571086, -18.301251, -18.628639, -18.574676, 2.271778, 1.875687, 5.315769, 0.870008]
     invwedge.test_vals_aarch64 = [-1.046323, -1.571086, -18.300667, -18.628064, -18.574092, 2.271778, 1.875687, 5.315769, 0.870008]
-    invwedge.new_output = True
     test_list.append(invwedge)
 
     # Viscous single cone - axisymmetric
@@ -75,7 +72,6 @@ def main():
     visc_cone.test_iter = 10
     visc_cone.test_vals = [-5.215236, -5.739371, -20.556662, -20.517023, -20.436970, 1.262783, -3.205463, -0.015695, 0.093205, 32656.000000]
     visc_cone.test_vals_aarch64 = [-5.215236, -5.739371, -20.556662, -20.517023, -20.436970, 1.262783, -3.205463, -0.015695, 0.093205, 32656.000000]
-    visc_cone.new_output = True
     test_list.append(visc_cone)
 
     #########################
@@ -95,7 +91,6 @@ def main():
     channel.cfg_file  = "inv_channel_RK.cfg"
     channel.test_iter = 10
     channel.test_vals = [-2.475872, 3.046370, -0.203974, 0.036018]
-    channel.new_output = True
     test_list.append(channel)
 
     # NACA0012
@@ -104,7 +99,6 @@ def main():
     naca0012.cfg_file  = "inv_NACA0012_Roe.cfg"
     naca0012.test_iter = 20
     naca0012.test_vals = [-4.023999, -3.515034, 0.339426, 0.022217] #last 4 columns
-    naca0012.new_output= True
     test_list.append(naca0012)
 
     # Supersonic wedge
@@ -113,7 +107,6 @@ def main():
     wedge.cfg_file  = "inv_wedge_HLLC.cfg"
     wedge.test_iter = 20
     wedge.test_vals = [-0.942862, 4.784581, -0.208106, 0.036665] #last 4 columns
-    wedge.new_output= True
     test_list.append(wedge)
 
     # ONERA M6 Wing
@@ -123,7 +116,6 @@ def main():
     oneram6.test_iter = 10
     oneram6.test_vals = [-9.279396, -8.697739, 0.281703, 0.011821]
     oneram6.timeout   = 9600
-    oneram6.new_output = True
     test_list.append(oneram6)
 
     # Fixed CL NACA0012
@@ -132,7 +124,6 @@ def main():
     fixedCL_naca0012.cfg_file  = "inv_NACA0012.cfg"
     fixedCL_naca0012.test_iter = 10
     fixedCL_naca0012.test_vals = [-7.382410, -1.879887, 0.300000, 0.019471]
-    fixedCL_naca0012.new_output = True
     test_list.append(fixedCL_naca0012)
 
     # Polar sweep of the inviscid NACA0012
@@ -140,7 +131,6 @@ def main():
     polar_naca0012.cfg_dir   = "polar/naca0012"
     polar_naca0012.cfg_file  = "inv_NACA0012.cfg"
     polar_naca0012.polar     = True
-    polar_naca0012.new_output= True
     polar_naca0012.test_iter = 10
     polar_naca0012.test_vals         = [-1.243326, 4.224483, 0.016432, 0.016145]
     polar_naca0012.test_vals_aarch64 = [-3.148445, 2.270143, 0.003666, 0.008682]
@@ -151,7 +141,6 @@ def main():
     bluntbody           = TestCase('bluntbody')
     bluntbody.cfg_dir   = "euler/bluntbody"
     bluntbody.cfg_file  = "blunt.cfg"
-    bluntbody.new_output = True
     bluntbody.test_iter = 20
     bluntbody.test_vals = [0.540009, 6.916653, -0.000000, 1.868975] #last 4 columns
     test_list.append(bluntbody)
@@ -173,7 +162,6 @@ def main():
     flatplate.cfg_file  = "lam_flatplate.cfg"
     flatplate.test_iter = 100
     flatplate.test_vals = [-9.856258, -4.371983, 0.001112, 0.036277, 2.361500, -2.325300, -2.279500, -2.279500]
-    flatplate.new_output = True
     test_list.append(flatplate)
 
     # Laminar cylinder (steady)
@@ -182,7 +170,6 @@ def main():
     cylinder.cfg_file  = "lam_cylinder.cfg"
     cylinder.test_iter = 25
     cylinder.test_vals = [-6.765430, -1.297426, 0.019508, 0.310015, 1.2325e-01]
-    cylinder.new_output = True
     test_list.append(cylinder)
 
     # Laminar cylinder (low Mach correction)
@@ -191,7 +178,6 @@ def main():
     cylinder_lowmach.cfg_file  = "cylinder_lowmach.cfg"
     cylinder_lowmach.test_iter = 25
     cylinder_lowmach.test_vals = [-6.850123, -1.388088, -0.056090, 108.140176, 0.007983]
-    cylinder_lowmach.new_output = True
     test_list.append(cylinder_lowmach)
 
     # 2D Poiseuille flow (body force driven with periodic inlet / outlet)
@@ -200,7 +186,6 @@ def main():
     poiseuille.cfg_file  = "lam_poiseuille.cfg"
     poiseuille.test_iter = 10
     poiseuille.test_vals = [-5.050732, 0.648355, 0.012273, 13.643219, -2.047100]
-    poiseuille.new_output = True
     test_list.append(poiseuille)
 
     # 2D Poiseuille flow (inlet profile file)
@@ -210,7 +195,6 @@ def main():
     poiseuille_profile.test_iter = 10
     poiseuille_profile.test_vals         = [-12.494681, -7.711642, -0.000000, 2.085796] #last 4 columns
     poiseuille_profile.test_vals_aarch64 = [-12.494705, -7.711332, -0.000000, 2.085796] #last 4 columns
-    poiseuille_profile.new_output = True
     test_list.append(poiseuille_profile)
 
     ##########################
@@ -230,7 +214,6 @@ def main():
     rae2822_sa.cfg_file  = "turb_SA_RAE2822.cfg"
     rae2822_sa.test_iter = 20
     rae2822_sa.test_vals = [-2.020123, -5.269330, 0.807147, 0.060499, -80603.000000]
-    rae2822_sa.new_output = True
     test_list.append(rae2822_sa)
 
     # RAE2822 SST
@@ -239,7 +222,6 @@ def main():
     rae2822_sst.cfg_file  = "turb_SST_RAE2822.cfg"
     rae2822_sst.test_iter = 20
     rae2822_sst.test_vals = [-0.510638, 4.870901, 0.812661, 0.061095, -80192.000000]
-    rae2822_sst.new_output = True
     test_list.append(rae2822_sst)
 
     # RAE2822 SST_SUST
@@ -256,7 +238,6 @@ def main():
     turb_flatplate.cfg_file  = "turb_SA_flatplate.cfg"
     turb_flatplate.test_iter = 20
     turb_flatplate.test_vals = [-4.157169, -6.736698, -0.176253, 0.057446] #last 4 columns
-    turb_flatplate.new_output  = True
     test_list.append(turb_flatplate)
 
     # FLAT PLATE, WALL FUNCTIONS, COMPRESSIBLE SST
@@ -281,7 +262,6 @@ def main():
     turb_oneram6.cfg_file  = "turb_ONERAM6.cfg"
     turb_oneram6.test_iter = 10
     turb_oneram6.test_vals = [-2.388841, -6.689414, 0.230321, 0.157640, -32539.000000]
-    turb_oneram6.new_output = True
     turb_oneram6.timeout   = 3200
     test_list.append(turb_oneram6)
 
@@ -291,7 +271,6 @@ def main():
     turb_naca0012_sa.cfg_file  = "turb_NACA0012_sa.cfg"
     turb_naca0012_sa.test_iter = 10
     turb_naca0012_sa.test_vals = [-8.629583, -10.377793, 1.064488, 0.019711, 20.000000, -2.173971, 20.000000, -5.213344, -46.50600]
-    turb_naca0012_sa.new_output = True
     turb_naca0012_sa.timeout   = 3200
     test_list.append(turb_naca0012_sa)
 
@@ -302,7 +281,6 @@ def main():
     turb_naca0012_sst.test_iter = 10
     turb_naca0012_sst.test_vals         = [-11.421948, -12.801962, -5.865325, 1.049990, 0.019163, -1.939735, -38.695000]
     turb_naca0012_sst.test_vals_aarch64 = [-11.451008, -12.798258, -5.863895, 1.049989, 0.019163, -1.925030, -38.694000]
-    turb_naca0012_sst.new_output  = True
     turb_naca0012_sst.timeout   = 3200
     test_list.append(turb_naca0012_sst)
 
@@ -312,7 +290,6 @@ def main():
     turb_naca0012_sst_2003m.cfg_file  = "turb_NACA0012_sst_2003m.cfg"
     turb_naca0012_sst_2003m.test_iter = 10
     turb_naca0012_sst_2003m.test_vals = [-7.698427, -10.060122, -3.421605, 1.049413, 0.019691, -2.193374, -45.178000]
-    turb_naca0012_sst_2003m.new_output  = True
     turb_naca0012_sst_2003m.timeout   = 3200
     test_list.append(turb_naca0012_sst_2003m)
 
@@ -340,7 +317,6 @@ def main():
     propeller.cfg_file  = "propeller.cfg"
     propeller.test_iter = 10
     propeller.test_vals = [-3.389575, -8.409529, 0.000048, 0.056329] #last 4 columns
-    propeller.new_output = True
     propeller.timeout   = 3200
     test_list.append(propeller)
 
@@ -368,7 +344,6 @@ def main():
     turb_naca0012_sst_restart_mg.test_iter = 50
     turb_naca0012_sst_restart_mg.ntest_vals = 5
     turb_naca0012_sst_restart_mg.test_vals = [-7.653236, -7.729549, -1.981855, -0.000015, 0.079062]
-    turb_naca0012_sst_restart_mg.new_output  = True
     turb_naca0012_sst_restart_mg.timeout   = 3200
     turb_naca0012_sst_restart_mg.tol       = 0.000001
     test_list.append(turb_naca0012_sst_restart_mg)
@@ -390,7 +365,6 @@ def main():
     inc_euler_naca0012.cfg_file  = "incomp_NACA0012.cfg"
     inc_euler_naca0012.test_iter = 20
     inc_euler_naca0012.test_vals = [-4.858287, -3.810487, 0.491850, 0.007002] #last 4 columns
-    inc_euler_naca0012.new_output = True
     test_list.append(inc_euler_naca0012)
 
     # C-D nozzle with pressure inlet and mass flow outlet
@@ -399,7 +373,6 @@ def main():
     inc_nozzle.cfg_file  = "inv_nozzle.cfg"
     inc_nozzle.test_iter = 20
     inc_nozzle.test_vals = [-5.971283, -4.911145, -0.000201, 0.121631] #last 4 columns
-    inc_nozzle.new_output = True
     test_list.append(inc_nozzle)
 
     #############################
@@ -419,7 +392,6 @@ def main():
     inc_lam_cylinder.cfg_file  = "incomp_cylinder.cfg"
     inc_lam_cylinder.test_iter = 10
     inc_lam_cylinder.test_vals = [-4.004277, -3.227956, 0.003852, 7.626578] #last 4 columns
-    inc_lam_cylinder.new_output  = True
     test_list.append(inc_lam_cylinder)
 
     # Buoyancy-driven cavity
@@ -428,7 +400,6 @@ def main():
     inc_buoyancy.cfg_file  = "lam_buoyancy_cavity.cfg"
     inc_buoyancy.test_iter = 20
     inc_buoyancy.test_vals = [-4.436657, 0.507847, 0.000000, 0.000000] #last 4 columns
-    inc_buoyancy.new_output  = True
     test_list.append(inc_buoyancy)
 
     # Laminar heated cylinder with polynomial fluid model
@@ -437,7 +408,6 @@ def main():
     inc_poly_cylinder.cfg_file  = "poly_cylinder.cfg"
     inc_poly_cylinder.test_iter = 20
     inc_poly_cylinder.test_vals = [-8.106741, -2.160042, 0.019225, 1.902421, -172.750000]
-    inc_poly_cylinder.new_output  = True
     test_list.append(inc_poly_cylinder)
 
     # X-coarse laminar bend as a mixed element CGNS test
@@ -465,7 +435,6 @@ def main():
     inc_turb_naca0012.cfg_file  = "naca0012.cfg"
     inc_turb_naca0012.test_iter = 20
     inc_turb_naca0012.test_vals = [-4.788495, -11.040511, 0.000023, 0.309503] #last 4 columns
-    inc_turb_naca0012.new_output  = True
     test_list.append(inc_turb_naca0012)
 
     # NACA0012, SST_SUST
@@ -509,7 +478,6 @@ def main():
     fem_euler_naca0012.cfg_file  = "fem_NACA0012_reg.cfg"
     fem_euler_naca0012.test_iter = 10
     fem_euler_naca0012.test_vals = [-6.519946,-5.976944,0.255551,0.000028] #last 4 columns
-    fem_euler_naca0012.new_output = True
     test_list.append(fem_euler_naca0012)
 
     ############################
@@ -529,7 +497,6 @@ def main():
     fem_ns_flatplate.cfg_file  = "lam_flatplate_reg.cfg"
     fem_ns_flatplate.test_iter = 25
     fem_ns_flatplate.test_vals = [1.383727,3.175247,0.058387,0.257951] #last 4 columns
-    fem_ns_flatplate.new_output = True
     test_list.append(fem_ns_flatplate)
 
     # Steady cylinder
@@ -538,7 +505,6 @@ def main():
     fem_ns_cylinder.cfg_file  = "fem_Cylinder_reg.cfg"
     fem_ns_cylinder.test_iter = 10
     fem_ns_cylinder.test_vals = [0.454960,0.979123,-0.000028,79.984799] #last 4 columns
-    fem_ns_cylinder.new_output  = True
     test_list.append(fem_ns_cylinder)
 
     # Steady sphere
@@ -547,7 +513,6 @@ def main():
     fem_ns_sphere.cfg_file  = "fem_Sphere_reg.cfg"
     fem_ns_sphere.test_iter = 10
     fem_ns_sphere.test_vals = [-0.288121,0.240324,0.000258,21.797363] #last 4 columns
-    fem_ns_sphere.new_output = True
     test_list.append(fem_ns_sphere)
 
     # Unsteady sphere ADER
@@ -556,7 +521,6 @@ def main():
     fem_ns_sphere_ader.cfg_file  = "fem_Sphere_reg_ADER.cfg"
     fem_ns_sphere_ader.test_iter = 10
     fem_ns_sphere_ader.test_vals = [-35.000000,-35.000000,0.000047,31.110911] #last 4 columns
-    fem_ns_sphere_ader.new_output = True
     fem_ns_sphere_ader.unsteady   = True
     test_list.append(fem_ns_sphere_ader)
 
@@ -566,7 +530,6 @@ def main():
     fem_ns_unsteady_cylinder.cfg_file  = "fem_unst_cylinder.cfg"
     fem_ns_unsteady_cylinder.test_iter = 11
     fem_ns_unsteady_cylinder.test_vals = [-3.558582,-3.014464,-0.038927,1.383983] #last 4 columns
-    fem_ns_unsteady_cylinder.new_output = True
     fem_ns_unsteady_cylinder.unsteady   = True
     test_list.append(fem_ns_unsteady_cylinder)
 
@@ -576,7 +539,6 @@ def main():
     fem_ns_unsteady_cylinder_ader.cfg_file  = "fem_unst_cylinder_ADER.cfg"
     fem_ns_unsteady_cylinder_ader.test_iter = 11
     fem_ns_unsteady_cylinder_ader.test_vals = [-35.000000,-35.000000,-0.041003,1.391339] #last 4 columns
-    fem_ns_unsteady_cylinder_ader.new_output = True
     fem_ns_unsteady_cylinder_ader.unsteady   = True
     test_list.append(fem_ns_unsteady_cylinder_ader)
 
@@ -589,7 +551,6 @@ def main():
     schubauer_klebanoff_transition.cfg_dir      = "transition/Schubauer_Klebanoff"
     schubauer_klebanoff_transition.cfg_file     = "transitional_BC_model_ConfigFile.cfg"
     schubauer_klebanoff_transition.test_iter    = 10
-    schubauer_klebanoff_transition.new_output   = True
     schubauer_klebanoff_transition.test_vals    = [-8.029786, -13.240213, 0.000053, 0.007986] #last 4 columns
     test_list.append(schubauer_klebanoff_transition)
 
@@ -610,7 +571,6 @@ def main():
     contadj_naca0012.cfg_file  = "inv_NACA0012.cfg"
     contadj_naca0012.test_iter = 5
     contadj_naca0012.test_vals = [-9.289565, -14.563861, 0.300920, 0.019552] #last 4 columns
-    contadj_naca0012.new_output = True
     contadj_naca0012.tol       = 0.001
     test_list.append(contadj_naca0012)
 
@@ -620,7 +580,6 @@ def main():
     contadj_oneram6.cfg_file  = "inv_ONERAM6.cfg"
     contadj_oneram6.test_iter = 10
     contadj_oneram6.test_vals = [-12.133160, -12.706697, 0.685900, 0.007594] #last 4 columns
-    contadj_oneram6.new_output = True
     test_list.append(contadj_oneram6)
 
     # Inviscid WEDGE: tests averaged outflow total pressure adjoint
@@ -629,7 +588,6 @@ def main():
     contadj_wedge.cfg_file  = "inv_wedge_ROE.cfg"
     contadj_wedge.test_iter = 10
     contadj_wedge.test_vals = [2.872691, -2.755572, 853000.000000, 0.000000] #last 4 columns
-    contadj_wedge.new_output = True
     test_list.append(contadj_wedge)
 
     # Inviscid fixed CL NACA0012
@@ -638,7 +596,6 @@ def main():
     contadj_fixedCL_naca0012.cfg_file  = "inv_NACA0012_ContAdj.cfg"
     contadj_fixedCL_naca0012.test_iter = 100
     contadj_fixedCL_naca0012.test_vals = [0.293213, -5.201710, 0.360590, -0.000022]
-    contadj_fixedCL_naca0012.new_output= True
     test_list.append(contadj_fixedCL_naca0012)
 
     ###################################
@@ -658,7 +615,6 @@ def main():
     contadj_ns_cylinder.cfg_file  = "lam_cylinder.cfg"
     contadj_ns_cylinder.test_iter = 20
     contadj_ns_cylinder.test_vals = [ -3.665848, -9.132055, 2.056700, -0.000000] #last 4 columns
-    contadj_ns_cylinder.new_output = True
     test_list.append(contadj_ns_cylinder)
 
     # Adjoint laminar naca0012 subsonic
@@ -667,7 +623,6 @@ def main():
     contadj_ns_naca0012_sub.cfg_file  = "lam_NACA0012.cfg"
     contadj_ns_naca0012_sub.test_iter = 20
     contadj_ns_naca0012_sub.test_vals = [-2.743268, -8.215193, 0.518810, 0.001210] #last 4 columns
-    contadj_ns_naca0012_sub.new_output =True
     test_list.append(contadj_ns_naca0012_sub)
 
     # Adjoint laminar naca0012 transonic
@@ -676,7 +631,6 @@ def main():
     contadj_ns_naca0012_trans.cfg_file  = "lam_NACA0012.cfg"
     contadj_ns_naca0012_trans.test_iter = 20
     contadj_ns_naca0012_trans.test_vals = [-1.039664, -6.575019, 1.772300, 0.012495] #last 4 columns
-    contadj_ns_naca0012_trans.new_output = True
     test_list.append(contadj_ns_naca0012_trans)
 
     #######################################################
@@ -689,7 +643,6 @@ def main():
     contadj_rans_naca0012.cfg_file  = "turb_nasa.cfg"
     contadj_rans_naca0012.test_iter = 20
     contadj_rans_naca0012.test_vals = [ -0.794162, -5.761722, 19.214000, -0.000000] #last 4 columns
-    contadj_rans_naca0012.new_output = True
     test_list.append(contadj_rans_naca0012)
 
     # Adjoint turbulent NACA0012 with binary restarts
@@ -698,7 +651,6 @@ def main():
     contadj_rans_naca0012_bin.cfg_file  = "turb_nasa_binary.cfg"
     contadj_rans_naca0012_bin.test_iter = 18
     contadj_rans_naca0012_bin.test_vals = [-0.794169, -5.761671, 19.214000, -0.000000] #last 4 columns
-    contadj_rans_naca0012_bin.new_output = True
     test_list.append(contadj_rans_naca0012_bin)
 
     # Adjoint turbulent RAE2822
@@ -707,7 +659,6 @@ def main():
     contadj_rans_rae2822.cfg_file  = "turb_SA_RAE2822.cfg"
     contadj_rans_rae2822.test_iter = 20
     contadj_rans_rae2822.test_vals = [-5.369688, -10.872211, -0.212470, 0.005448]
-    contadj_rans_rae2822.new_output = True
     test_list.append(contadj_rans_rae2822)
 
     #############################
@@ -721,7 +672,6 @@ def main():
     turb_naca0012_1c.test_iter = 10
     turb_naca0012_1c.test_vals         = [-4.985899, 1.137425, 0.375986, -0.078795]
     turb_naca0012_1c.test_vals_aarch64 = [-4.985900, 1.137455, 0.376000, -0.078781]
-    turb_naca0012_1c.new_output = True
     test_list.append(turb_naca0012_1c)
 
     # NACA0012 2c
@@ -731,7 +681,6 @@ def main():
     turb_naca0012_2c.test_iter = 10
     turb_naca0012_2c.test_vals         = [-5.483297, 0.968867, 0.255779, -0.109417] #last 4 columns
     turb_naca0012_2c.test_vals_aarch64 = [-5.483310, 0.968862, 0.255650, -0.109464] #last 4 columns
-    turb_naca0012_2c.new_output = True
     test_list.append(turb_naca0012_2c)
 
     # NACA0012 3c
@@ -740,7 +689,6 @@ def main():
     turb_naca0012_3c.cfg_file  = "turb_NACA0012_uq_3c.cfg"
     turb_naca0012_3c.test_iter = 10
     turb_naca0012_3c.test_vals = [-5.584300, 0.931352, 0.248990, -0.109405] #last 4 columns
-    turb_naca0012_3c.new_output = True
     test_list.append(turb_naca0012_3c)
 
     # NACA0012 p1c1
@@ -750,7 +698,6 @@ def main():
     turb_naca0012_p1c1.test_iter = 10
     turb_naca0012_p1c1.test_vals         = [-5.127470, 1.077450, 0.544081, -0.018573] #last 4 columns
     turb_naca0012_p1c1.test_vals_aarch64 = [-5.127512, 1.077345, 0.544130, -0.018555] #last 4 columns
-    turb_naca0012_p1c1.new_output = True
     test_list.append(turb_naca0012_p1c1)
 
     # NACA0012 p1c2
@@ -760,7 +707,6 @@ def main():
     turb_naca0012_p1c2.test_iter = 10
     turb_naca0012_p1c2.test_vals         = [-5.554427, 0.943668, 0.320426, -0.091140] #last 4 columns
     turb_naca0012_p1c2.test_vals_aarch64 = [-5.554391, 0.943687, 0.320285, -0.091188] #last 4 columns
-    turb_naca0012_p1c2.new_output = True
     test_list.append(turb_naca0012_p1c2)
 
     ######################################
@@ -773,7 +719,6 @@ def main():
     harmonic_balance.cfg_file  = "HB.cfg"
     harmonic_balance.test_iter = 25
     harmonic_balance.test_vals = [-1.589739, 3.922579, 0.006702, 0.099632]
-    harmonic_balance.new_output = False
     test_list.append(harmonic_balance)
 
     # Turbulent pitching NACA 64a010 airfoil
@@ -782,7 +727,6 @@ def main():
     hb_rans_preconditioning.cfg_file  = "davis.cfg"
     hb_rans_preconditioning.test_iter = 25
     hb_rans_preconditioning.test_vals = [-1.902098, -5.949277, 0.007768, 0.128061]
-    hb_rans_preconditioning.new_output= False
     test_list.append(hb_rans_preconditioning)
 
     ######################################
@@ -803,7 +747,6 @@ def main():
     cavity.cfg_file  = "lam_cavity.cfg"
     cavity.test_iter = 25
     cavity.test_vals = [-5.627934, -0.164470, 0.051972, 2.547039]
-    cavity.new_output = True
     test_list.append(cavity)
 
     # Spinning cylinder
@@ -812,7 +755,6 @@ def main():
     spinning_cylinder.cfg_file  = "spinning_cylinder.cfg"
     spinning_cylinder.test_iter = 25
     spinning_cylinder.test_vals = [-7.889994, -2.469385, 1.708162, 1.670039] #last 4 columns
-    spinning_cylinder.new_output = True
     test_list.append(spinning_cylinder)
 
     ######################################
@@ -826,7 +768,6 @@ def main():
     square_cylinder.test_iter = 3
     square_cylinder.test_vals = [-2.557820, -1.158056, 0.067984, 1.399788, 2.220411, 1.399743, 2.218612, -0.453170]
     square_cylinder.unsteady  = True
-    square_cylinder.new_output = True
     test_list.append(square_cylinder)
 
     # Gust
@@ -836,7 +777,6 @@ def main():
     sine_gust.test_iter = 5
     sine_gust.test_vals = [-1.977520, 3.481804, -0.012277, -0.007309]
     sine_gust.unsteady  = True
-    sine_gust.new_output = True
     test_list.append(sine_gust)
 
     # Aeroelastic
@@ -846,7 +786,6 @@ def main():
     aeroelastic.test_iter = 2
     aeroelastic.test_vals = [0.074836, 0.033102, -0.001650, -0.000127]
     aeroelastic.unsteady  = True
-    aeroelastic.new_output = True
     test_list.append(aeroelastic)
 
     # Delayed Detached Eddy Simulation
@@ -856,7 +795,6 @@ def main():
     ddes_flatplate.test_iter = 10
     ddes_flatplate.test_vals = [-2.714758, -5.882733, -0.215005, 0.023783, -618.160000]
     ddes_flatplate.unsteady  = True
-    ddes_flatplate.new_output = True
     test_list.append(ddes_flatplate)
 
     # unsteady pitching NACA0015, SA
@@ -887,7 +825,6 @@ def main():
     ls89_sa.cfg_file  = "turb_SA_PR.cfg"
     ls89_sa.test_iter = 20
     ls89_sa.test_vals = [-5.050483, -13.371788, 0.174939, 0.430757] #last 4 columns
-    ls89_sa.new_output= True
     test_list.append(ls89_sa)
 
     # Rarefaction shock wave edge_VW
@@ -896,7 +833,6 @@ def main():
     edge_VW.cfg_file  = "edge_VW.cfg"
     edge_VW.test_iter = 20
     edge_VW.test_vals = [-0.711552, 5.490479, -0.000975, 0.000000] #last 4 columns
-    edge_VW.new_output = True
     test_list.append(edge_VW)
 
     # Rarefaction shock wave edge_PPR
@@ -905,7 +841,6 @@ def main():
     edge_PPR.cfg_file  = "edge_PPR.cfg"
     edge_PPR.test_iter = 20
     edge_PPR.test_vals = [-1.670439, 4.522842, 0.001027, 0.000000] #last 4 columns
-    edge_PPR.new_output = True
     test_list.append(edge_PPR)
 
 
@@ -919,7 +854,6 @@ def main():
     Jones_tc_restart.cfg_file  = "Jones_restart.cfg"
     Jones_tc_restart.test_iter = 5
     Jones_tc_restart.test_vals = [-10.691501, -7.643699, 85.827890, 2.277151] #last 4 columns
-    Jones_tc_restart.new_output = False
     Jones_tc_restart.tol       = 0.0001
     test_list.append(Jones_tc_restart)
 
@@ -929,7 +863,6 @@ def main():
     axial_stage2D.cfg_file  = "Axial_stage2D.cfg"
     axial_stage2D.test_iter = 20
     axial_stage2D.test_vals = [-1.937012, 5.338671, 73.357200, 0.915728] #last 4 columns
-    axial_stage2D.new_output  = False
     test_list.append(axial_stage2D)
 
     # 2D transonic stator restart
@@ -938,7 +871,6 @@ def main():
     transonic_stator_restart.cfg_file  = "transonic_stator_restart.cfg"
     transonic_stator_restart.test_iter = 20
     transonic_stator_restart.test_vals = [-6.765890, -0.742094, 5.003454, 0.002946] #last 4 columns
-    transonic_stator_restart.new_output  = False
     test_list.append(transonic_stator_restart)
 
 
@@ -1062,7 +994,6 @@ def main():
     statbeam3d           = TestCase('statbeam3d')
     statbeam3d.cfg_dir   = "fea_fsi/StatBeam_3d"
     statbeam3d.cfg_file  = "configBeam_3d.cfg"
-    statbeam3d.new_output= True
     statbeam3d.test_iter = 0
     statbeam3d.test_vals         = [-8.498245, -8.230816, -8.123810, 64095.0] #last 4 columns
     statbeam3d.test_vals_aarch64 = [-8.498254, -8.230683, -8.123819, 64095.0] #last 4 columns
@@ -1083,7 +1014,6 @@ def main():
     dynbeam2d.cfg_dir   = "fea_fsi/DynBeam_2d"
     dynbeam2d.cfg_file  = "configBeam_2d.cfg"
     dynbeam2d.unsteady  = True
-    dynbeam2d.new_output= True
     dynbeam2d.test_iter = 6
     dynbeam2d.test_vals = [-3.240015, 2.895057, -0.353146, 6.6127e+04] #last 4 columns
     test_list.append(dynbeam2d)
@@ -1144,7 +1074,6 @@ def main():
     p1rad           = TestCase('p1rad')
     p1rad.cfg_dir   = "radiation/p1model"
     p1rad.cfg_file  = "configp1.cfg"
-    p1rad.new_output= True
     p1rad.test_iter = 100
     p1rad.test_vals = [-7.751309, -7.923059, -2.119084, 0.091733, -44.537000]
     test_list.append(p1rad)
@@ -1469,7 +1398,6 @@ def main():
     contadj_euler_py.timeout   = 1600
     contadj_euler_py.reference_file = "of_grad_cd.dat.ref"
     contadj_euler_py.test_file = "of_grad_cd.dat"
-    contadj_euler_py.new_output = True
     pass_list.append(contadj_euler_py.run_filediff())
     test_list.append(contadj_euler_py)
 
@@ -1481,7 +1409,6 @@ def main():
     shape_opt_euler_py.test_vals = [1, 1, 2.134974E-05, 0.003847] #last 4 columns
     shape_opt_euler_py.command   =  TestCase.Command(exec = "shape_optimization.py", param = "-g CONTINUOUS_ADJOINT -f")
     shape_opt_euler_py.timeout   = 1600
-    shape_opt_euler_py.new_output = True
     shape_opt_euler_py.tol       = 0.00001
     pass_list.append(shape_opt_euler_py.run_opt())
     test_list.append(shape_opt_euler_py)
@@ -1493,7 +1420,6 @@ def main():
     contadj_multi_py.test_iter  = 10
     contadj_multi_py.command    =  TestCase.Command(exec = "continuous_adjoint.py", param = "-f")
     contadj_multi_py.timeout    = 1600
-    contadj_multi_py.new_output = True
     contadj_multi_py.reference_file = "of_grad_combo.dat.ref"
     contadj_multi_py.test_file  = "of_grad_combo.dat"
     pass_list.append(contadj_multi_py.run_filediff())
@@ -1560,7 +1486,6 @@ def main():
     pywrapper_naca0012.test_iter = 20
     pywrapper_naca0012.test_vals = [-4.023999, -3.515034, 0.339426, 0.022217] #last 4 columns
     pywrapper_naca0012.command   =  TestCase.Command(exec = "SU2_CFD.py", param = "-f")
-    pywrapper_naca0012.new_output  = True
     pywrapper_naca0012.timeout   = 1600
     pywrapper_naca0012.tol       = 0.00001
     test_list.append(pywrapper_naca0012)
@@ -1574,7 +1499,6 @@ def main():
     pywrapper_turb_naca0012_sst.test_vals         = [-11.421948, -12.801962, -5.865325, 1.049990, 0.019163, -1.939735, -38.695000]
     pywrapper_turb_naca0012_sst.test_vals_aarch64 = [-11.451014, -12.798258, -5.863895, 1.049989, 0.019163, -1.925032, -38.694000]
     pywrapper_turb_naca0012_sst.command   =  TestCase.Command(exec = "SU2_CFD.py", param = "-f")
-    pywrapper_turb_naca0012_sst.new_output = True
     pywrapper_turb_naca0012_sst.timeout   = 3200
     pywrapper_turb_naca0012_sst.tol       = 0.00001
     test_list.append(pywrapper_turb_naca0012_sst)
@@ -1600,7 +1524,6 @@ def main():
     pywrapper_aeroelastic.test_iter = 2
     pywrapper_aeroelastic.test_vals = [0.074836, 0.033102, -0.001650, -0.000127]
     pywrapper_aeroelastic.command   =  TestCase.Command(exec = "SU2_CFD.py", param = "-f")
-    pywrapper_aeroelastic.new_output  = True
     pywrapper_aeroelastic.timeout   = 1600
     pywrapper_aeroelastic.tol       = 0.00001
     pywrapper_aeroelastic.unsteady  = True
@@ -1614,7 +1537,6 @@ def main():
     pywrapper_fsi2d.test_iter = 4
     pywrapper_fsi2d.test_vals = [4, 0, -3.743214, -4.133482] #last 4 columns
     pywrapper_fsi2d.command   =  TestCase.Command(exec = "SU2_CFD.py", param = "--nZone 2 --fsi True -f")
-    pywrapper_fsi2d.new_output  = True
     pywrapper_fsi2d.unsteady  = True
     pywrapper_fsi2d.multizone   = True
     pywrapper_fsi2d.timeout   = 1600
@@ -1630,7 +1552,6 @@ def main():
     pywrapper_unsteadyCHT.test_vals     = [-1.614167, 2.245716, 0.000766, 0.175719]
     pywrapper_unsteadyCHT.command       =  TestCase.Command(exec = "python", param = "launch_unsteady_CHT_FlatPlate.py -f")
     pywrapper_unsteadyCHT.timeout       = 1600
-    pywrapper_unsteadyCHT.new_output    = True
     pywrapper_unsteadyCHT.tol           = 0.00001
     pywrapper_unsteadyCHT.unsteady      = True
     test_list.append(pywrapper_unsteadyCHT)
@@ -1643,7 +1564,6 @@ def main():
     pywrapper_rigidMotion.test_iter     = 5
     pywrapper_rigidMotion.test_vals     = [-1.614170, 2.242953, 0.350050, 0.093116]
     pywrapper_rigidMotion.command       = TestCase.Command(exec = "python", param = "launch_flatPlate_rigidMotion.py -f")
-    pywrapper_rigidMotion.new_output      = True
     pywrapper_rigidMotion.timeout       = 1600
     pywrapper_rigidMotion.tol           = 0.00001
     pywrapper_rigidMotion.unsteady      = True
diff --git a/TestCases/tutorials.py b/TestCases/tutorials.py
index af0a0039b7b..0b730dcddda 100644
--- a/TestCases/tutorials.py
+++ b/TestCases/tutorials.py
@@ -90,7 +90,6 @@ def main():
     species3_primitiveVenturi.cfg_file  = "species3_primitiveVenturi.cfg"
     species3_primitiveVenturi.test_iter = 50
     species3_primitiveVenturi.test_vals = [-6.074971, -5.306648, -5.150960, -5.959416, -1.625107, -6.343704, -6.460033, 5.000000, -0.808413, 5.000000, -2.325029, 5.000000, -0.274923, 1.646091, 0.499028, 0.601019, 0.546044]
-    species3_primitiveVenturi.new_output = True
     test_list.append(species3_primitiveVenturi)
 
 
@@ -102,7 +101,6 @@ def main():
     DAspecies3_primitiveVenturi.test_vals         = [-8.528844, -7.799649, -7.783477, -7.482502, -12.140092, -12.250169, -11.455523]
     DAspecies3_primitiveVenturi.test_vals_aarch64 = [-8.528880, -7.799682, -7.783516, -7.482532, -12.140123, -12.250169, -11.455523]
     DAspecies3_primitiveVenturi.command   = TestCase.Command("mpirun -n 2", "SU2_CFD_AD")
-    DAspecies3_primitiveVenturi.new_output = True
     test_list.append(DAspecies3_primitiveVenturi)
 
     # 2 species (1 eq) kenics static mixer for composition-dependent model
@@ -112,7 +110,6 @@ def main():
     kenics_mixer_tutorial.test_iter = 10
     kenics_mixer_tutorial.test_vals = [-7.489828, -6.823474, -6.838069, -5.157396, -7.902254, -3.174210, -7.447809, 5.000000, -1.862023, 4.000000, -5.173815, 3.000000, -6.381121, 0.025490, 0.000000, 0.025490, 0.000000, 64.111000, 8.479500, 48.105000, 7.526700]
     kenics_mixer_tutorial.command   = TestCase.Command("mpirun -n 2", "SU2_CFD")
-    kenics_mixer_tutorial.new_output = True
     test_list.append(kenics_mixer_tutorial)
 
     # 90 degree pipe bend with wall functions from the experiments of Sudo et al.
@@ -122,7 +119,6 @@ def main():
     sudo_tutorial.test_iter = 10
     sudo_tutorial.test_vals = [-13.618610, -12.647974, -12.296537, -11.658760, -13.136523, -9.550829, 15.000000, -2.369703]
     sudo_tutorial.command   = TestCase.Command("mpirun -n 2", "SU2_CFD")
-    sudo_tutorial.new_output = True
     test_list.append(sudo_tutorial)
 
     ### Compressible Flow
@@ -133,7 +129,6 @@ def main():
     tutorial_inv_bump.cfg_file   = "inv_channel.cfg"
     tutorial_inv_bump.test_iter  = 0
     tutorial_inv_bump.test_vals  = [-1.437425, 4.075857, 0.005439, 0.012998]
-    tutorial_inv_bump.no_restart = True
     test_list.append(tutorial_inv_bump)
 
     # Inviscid Wedge

From 0e45e8bc54385e9cde32cd0f48120cc43fdcb9a0 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Wed, 5 Apr 2023 08:05:39 -0700
Subject: [PATCH 348/656] update turbo cases

---
 SU2_CFD/src/drivers/CMultizoneDriver.cpp           |  4 ++++
 TestCases/harmonic_balance/HB.cfg                  |  3 ++-
 .../hb_rans_preconditioning/davis.cfg              |  1 +
 TestCases/hybrid_regression.py                     | 14 +++++++-------
 TestCases/parallel_regression.py                   | 10 +++++-----
 TestCases/serial_regression.py                     | 10 +++++-----
 .../APU_turbocharger/Jones_restart.cfg             |  4 +++-
 .../axial_stage_2D/Axial_stage2D.cfg               |  2 ++
 .../transonic_stator_restart.cfg                   |  2 ++
 9 files changed, 31 insertions(+), 19 deletions(-)

diff --git a/SU2_CFD/src/drivers/CMultizoneDriver.cpp b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
index 0cdb774c9d9..b29da9b2161 100644
--- a/SU2_CFD/src/drivers/CMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
@@ -285,6 +285,9 @@ void CMultizoneDriver::RunGaussSeidel() {
 
   for (iZone = 0; iZone < nZone; iZone++) {
     config_container[iZone]->SetOuterIter(0ul);
+    /*--- This is required for correct restarts with mixing plane interfaces and GS iterations,
+    * for Jacobi we always do all the transfers before iterating all zones. ---*/
+    if (mixingplane) SetMixingPlane(iZone);
   }
 
   /*--- Loop over the number of outer iterations ---*/
@@ -314,6 +317,7 @@ void CMultizoneDriver::RunGaussSeidel() {
           if (DeformMesh) UpdateMesh+=1;
         }
       }
+
       /*--- If a mesh update is required due to the transfer of data ---*/
       if (UpdateMesh > 0) DynamicMeshUpdate(iZone, TimeIter);
 
diff --git a/TestCases/harmonic_balance/HB.cfg b/TestCases/harmonic_balance/HB.cfg
index 333d2aafc0c..b6d1ce04a81 100644
--- a/TestCases/harmonic_balance/HB.cfg
+++ b/TestCases/harmonic_balance/HB.cfg
@@ -55,7 +55,7 @@ CFL_NUMBER= 1.0
 CFL_ADAPT= NO
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-ITER= 10
+ITER= 30
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
@@ -105,6 +105,7 @@ CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
+SCREEN_OUTPUT= INNER_ITER, RMS_RES
 MESH_FILENAME= mesh_NACA64A010_inv.su2
 MESH_FORMAT= SU2
 MESH_OUT_FILENAME= mesh_out.su2
diff --git a/TestCases/harmonic_balance/hb_rans_preconditioning/davis.cfg b/TestCases/harmonic_balance/hb_rans_preconditioning/davis.cfg
index 07e6b6d0fab..af3a7142991 100644
--- a/TestCases/harmonic_balance/hb_rans_preconditioning/davis.cfg
+++ b/TestCases/harmonic_balance/hb_rans_preconditioning/davis.cfg
@@ -89,6 +89,7 @@ CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
+SCREEN_OUTPUT= INNER_ITER, RMS_RES
 MESH_FILENAME= n64a010_turb.su2
 MESH_FORMAT= SU2
 MESH_OUT_FILENAME= mesh_out.su2
diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index 4a1719013fc..665d8f2a5f0 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -329,7 +329,7 @@ def main():
     harmonic_balance.cfg_dir   = "harmonic_balance"
     harmonic_balance.cfg_file  = "HB.cfg"
     harmonic_balance.test_iter = 25
-    harmonic_balance.test_vals = [-1.589740, 3.922578, 0.006703, 0.099632]
+    harmonic_balance.test_vals = [-1.589739, 0.790169, 0.937053, 3.922579]
     test_list.append(harmonic_balance)
 
     # Turbulent pitching NACA 64a010 airfoil
@@ -337,7 +337,7 @@ def main():
     hb_rans_preconditioning.cfg_dir   = "harmonic_balance/hb_rans_preconditioning"
     hb_rans_preconditioning.cfg_file  = "davis.cfg"
     hb_rans_preconditioning.test_iter = 25
-    hb_rans_preconditioning.test_vals = [-1.902111, -5.949288, 0.007768, 0.128060]
+    hb_rans_preconditioning.test_vals = [-1.902097, 0.484069, 0.601483, 3.609005, -5.949274]
     test_list.append(hb_rans_preconditioning)
 
     #############################
@@ -539,7 +539,7 @@ def main():
     Jones_tc_restart.cfg_dir   = "turbomachinery/APU_turbocharger"
     Jones_tc_restart.cfg_file  = "Jones_restart.cfg"
     Jones_tc_restart.test_iter = 5
-    Jones_tc_restart.test_vals = [-10.691521, -7.643723, 85.827890, 2.277151]
+    Jones_tc_restart.test_vals = [-6.986563, -3.096834, -14.849532, -9.102914, -11.787851, -6.266208, 7.3266e+04, 7.3266e+04]
     test_list.append(Jones_tc_restart)
 
     # 2D axial stage
@@ -547,8 +547,8 @@ def main():
     axial_stage2D.cfg_dir   = "turbomachinery/axial_stage_2D"
     axial_stage2D.cfg_file  = "Axial_stage2D.cfg"
     axial_stage2D.test_iter = 20
-    axial_stage2D.test_vals         = [-1.937003, 5.338805, 73.357170, 0.915734]
-    axial_stage2D.test_vals_aarch64 = [-1.933115, 5.365583, 73.354510, 0.925902]
+    axial_stage2D.test_vals         = [1.047323, 1.661341, -2.913940, 2.588179, -2.486770, 3.050954, 1.0638e+05, 1.0638e+05]
+    axial_stage2D.test_vals_aarch64 = [1.047323, 1.661341, -2.913940, 2.588179, -2.486770, 3.050954, 1.0638e+05, 1.0638e+05]
     test_list.append(axial_stage2D)
 
     # 2D transonic stator restart
@@ -556,8 +556,8 @@ def main():
     transonic_stator_restart.cfg_dir   = "turbomachinery/transonic_stator_2D"
     transonic_stator_restart.cfg_file  = "transonic_stator_restart.cfg"
     transonic_stator_restart.test_iter = 20
-    transonic_stator_restart.test_vals         = [-6.796363, -0.743837, 5.003453, 0.002946]
-    transonic_stator_restart.test_vals_aarch64 = [-6.619122, -0.615705, 5.002986, 0.002951]
+    transonic_stator_restart.test_vals         = [-7.534574, -6.838075, -6.618228, -1.567726, -6.767343, -0.738638, -4.7165e+05]
+    transonic_stator_restart.test_vals_aarch64 = [-7.534574, -6.838075, -6.618228, -1.567726, -6.767343, -0.738638, -4.7165e+05]
     test_list.append(transonic_stator_restart)
 
     ######################################
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 98e7c000378..de4db10e99f 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -842,7 +842,7 @@ def main():
     harmonic_balance.cfg_dir   = "harmonic_balance"
     harmonic_balance.cfg_file  = "HB.cfg"
     harmonic_balance.test_iter = 25
-    harmonic_balance.test_vals = [-1.589739, 3.922579, 0.006702, 0.099632]
+    harmonic_balance.test_vals = [-1.589739, 0.790169, 0.937053, 3.922579]
     test_list.append(harmonic_balance)
 
     # Turbulent pitching NACA 64a010 airfoil
@@ -850,7 +850,7 @@ def main():
     hb_rans_preconditioning.cfg_dir   = "harmonic_balance/hb_rans_preconditioning"
     hb_rans_preconditioning.cfg_file  = "davis.cfg"
     hb_rans_preconditioning.test_iter = 25
-    hb_rans_preconditioning.test_vals = [-1.902098, -5.949275, 0.007768, 0.128061]
+    hb_rans_preconditioning.test_vals = [-1.902097, 0.484069, 0.601483, 3.609005, -5.949274]
     test_list.append(hb_rans_preconditioning)
 
     ######################################
@@ -984,7 +984,7 @@ def main():
     Jones_tc_restart.cfg_dir   = "turbomachinery/APU_turbocharger"
     Jones_tc_restart.cfg_file  = "Jones_restart.cfg"
     Jones_tc_restart.test_iter = 5
-    Jones_tc_restart.test_vals = [-10.691504, -7.643703, 85.827890, 2.277151]
+    Jones_tc_restart.test_vals = [-6.986563, -3.096834, -14.849532, -9.102914, -11.787851, -6.266208, 7.3266e+04, 7.3266e+04]
     test_list.append(Jones_tc_restart)
 
     # 2D axial stage
@@ -992,7 +992,7 @@ def main():
     axial_stage2D.cfg_dir   = "turbomachinery/axial_stage_2D"
     axial_stage2D.cfg_file  = "Axial_stage2D.cfg"
     axial_stage2D.test_iter = 20
-    axial_stage2D.test_vals = [-1.937007, 5.338943, 73.357200, 0.915725]
+    axial_stage2D.test_vals = [1.047323, 1.661341, -2.913940, 2.588179, -2.486770, 3.050954, 1.0638e+05, 1.0638e+05]
     test_list.append(axial_stage2D)
 
     # 2D transonic stator restart
@@ -1000,7 +1000,7 @@ def main():
     transonic_stator_restart.cfg_dir   = "turbomachinery/transonic_stator_2D"
     transonic_stator_restart.cfg_file  = "transonic_stator_restart.cfg"
     transonic_stator_restart.test_iter = 20
-    transonic_stator_restart.test_vals = [-6.801911, -0.746307, 5.003453, 0.002946]
+    transonic_stator_restart.test_vals = [-7.534574, -6.838075, -6.618228, -1.567726, -6.767343, -0.738638, -4.7165e+05]
     test_list.append(transonic_stator_restart)
 
     ######################################
diff --git a/TestCases/serial_regression.py b/TestCases/serial_regression.py
index c1d62447764..b7d00c3f3a0 100644
--- a/TestCases/serial_regression.py
+++ b/TestCases/serial_regression.py
@@ -718,7 +718,7 @@ def main():
     harmonic_balance.cfg_dir   = "harmonic_balance"
     harmonic_balance.cfg_file  = "HB.cfg"
     harmonic_balance.test_iter = 25
-    harmonic_balance.test_vals = [-1.589739, 3.922579, 0.006702, 0.099632]
+    harmonic_balance.test_vals = [-1.589739, 0.790169, 0.937053, 3.922579]
     test_list.append(harmonic_balance)
 
     # Turbulent pitching NACA 64a010 airfoil
@@ -726,7 +726,7 @@ def main():
     hb_rans_preconditioning.cfg_dir   = "harmonic_balance/hb_rans_preconditioning"
     hb_rans_preconditioning.cfg_file  = "davis.cfg"
     hb_rans_preconditioning.test_iter = 25
-    hb_rans_preconditioning.test_vals = [-1.902098, -5.949277, 0.007768, 0.128061]
+    hb_rans_preconditioning.test_vals = [-1.902097, 0.484069, 0.601483, 3.609005, -5.949274]
     test_list.append(hb_rans_preconditioning)
 
     ######################################
@@ -853,7 +853,7 @@ def main():
     Jones_tc_restart.cfg_dir   = "turbomachinery/APU_turbocharger"
     Jones_tc_restart.cfg_file  = "Jones_restart.cfg"
     Jones_tc_restart.test_iter = 5
-    Jones_tc_restart.test_vals = [-10.691501, -7.643699, 85.827890, 2.277151] #last 4 columns
+    Jones_tc_restart.test_vals = [-6.986563, -3.096834, -14.849532, -9.102914, -11.787851, -6.266208, 7.3266e+04, 7.3266e+04]
     Jones_tc_restart.tol       = 0.0001
     test_list.append(Jones_tc_restart)
 
@@ -862,7 +862,7 @@ def main():
     axial_stage2D.cfg_dir   = "turbomachinery/axial_stage_2D"
     axial_stage2D.cfg_file  = "Axial_stage2D.cfg"
     axial_stage2D.test_iter = 20
-    axial_stage2D.test_vals = [-1.937012, 5.338671, 73.357200, 0.915728] #last 4 columns
+    axial_stage2D.test_vals = [1.047323, 1.661341, -2.913940, 2.588179, -2.486770, 3.050954, 1.0638e+05, 1.0638e+05]
     test_list.append(axial_stage2D)
 
     # 2D transonic stator restart
@@ -870,7 +870,7 @@ def main():
     transonic_stator_restart.cfg_dir   = "turbomachinery/transonic_stator_2D"
     transonic_stator_restart.cfg_file  = "transonic_stator_restart.cfg"
     transonic_stator_restart.test_iter = 20
-    transonic_stator_restart.test_vals = [-6.765890, -0.742094, 5.003454, 0.002946] #last 4 columns
+    transonic_stator_restart.test_vals = [-7.534574, -6.838075, -6.618228, -1.567726, -6.767343, -0.738638, -4.7165e+05]
     test_list.append(transonic_stator_restart)
 
 
diff --git a/TestCases/turbomachinery/APU_turbocharger/Jones_restart.cfg b/TestCases/turbomachinery/APU_turbocharger/Jones_restart.cfg
index 8a4c24a0850..a766bc072b0 100755
--- a/TestCases/turbomachinery/APU_turbocharger/Jones_restart.cfg
+++ b/TestCases/turbomachinery/APU_turbocharger/Jones_restart.cfg
@@ -66,6 +66,7 @@ MARKER_PERIODIC= (PER1, PER2, 0.0, 0.0, 0.0, 0.0, 0.0, 18.947368421, 0.0, 0.0, 0
 %-------- INFLOW/OUTFLOW BOUNDARY CONDITION SPECIFIC FOR TURBOMACHINERY --------%
 %
 MARKER_TURBOMACHINERY= (INFLOW, OUTMIX, INMIX, OUTFLOW)
+MARKER_ANALYZE= (OUTFLOW)
 MARKER_MIXINGPLANE_INTERFACE= (OUTMIX, INMIX)
 MARKER_GILES= (INFLOW, TOTAL_CONDITIONS_PT, 413.6E+03, 477.6, 1.0, 0.0, 0.0, 1.0, 0.0, OUTMIX, MIXING_OUT, 0.0, 0.0, 0.0, 0.0, 0.0, 0.3, 0.0, INMIX, MIXING_IN, 0.0, 0.0, 0.0, 0.0, 0.0, 0.3, 0.0, OUTFLOW, STATIC_PRESSURE_1D, 67.46E+03, 0.0, 0.0, 0.0, 0.0 , 1.0, 0.0)
 GILES_EXTRA_RELAXFACTOR= (0.05, 0.05)
@@ -136,6 +137,7 @@ CONV_CAUCHY_EPS= 1E-6
 %
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
+SCREEN_OUTPUT= OUTER_ITER, AVG_BGS_RES[0], AVG_BGS_RES[1], RMS_DENSITY[0], RMS_ENERGY[0], RMS_DENSITY[1], RMS_ENERGY[1], SURFACE_TOTAL_PRESSURE[1]
 MESH_FILENAME= mesh_jones_turbine.su2
 MESH_FORMAT= SU2
 MESH_OUT_FILENAME= meshout.su2
@@ -150,4 +152,4 @@ VOLUME_ADJ_FILENAME= adjoint
 GRAD_OBJFUNC_FILENAME= of_grad.dat
 SURFACE_FILENAME= surface_flow
 SURFACE_ADJ_FILENAME= surface_adjoint
-OUTPUT_WRT_FREQ= 100
\ No newline at end of file
+OUTPUT_WRT_FREQ= 100
diff --git a/TestCases/turbomachinery/axial_stage_2D/Axial_stage2D.cfg b/TestCases/turbomachinery/axial_stage_2D/Axial_stage2D.cfg
index 38c0a560488..e1b98aee978 100755
--- a/TestCases/turbomachinery/axial_stage_2D/Axial_stage2D.cfg
+++ b/TestCases/turbomachinery/axial_stage_2D/Axial_stage2D.cfg
@@ -67,6 +67,7 @@ MARKER_PERIODIC= ( periodic1, periodic2, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.04
 %
 % Inflow and Outflow markers must be specified, for each blade (zone), following the natural groth of the machine (i.e, from the first blade to the last)
 MARKER_TURBOMACHINERY= (inflow, outmix, inmix, outflow)
+MARKER_ANALYZE= (outflow)
 %
 % Mixing-plane interface markers must be specified to activate the transfer of information between zones
 MARKER_MIXINGPLANE_INTERFACE= (outmix, inmix)
@@ -138,6 +139,7 @@ CONV_CAUCHY_EPS= 1E-6
 %
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
+SCREEN_OUTPUT= OUTER_ITER, AVG_BGS_RES[0], AVG_BGS_RES[1], RMS_DENSITY[0], RMS_ENERGY[0], RMS_DENSITY[1], RMS_ENERGY[1], SURFACE_TOTAL_PRESSURE[1]
 MESH_FILENAME= mesh_axial_stage_2d_turb.su2
 MESH_FORMAT= SU2
 MESH_OUT_FILENAME= meshout.su2
diff --git a/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg b/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg
index e1f7df0d26c..87c0f8abaa8 100644
--- a/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg
+++ b/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg
@@ -68,6 +68,7 @@ MARKER_PERIODIC= ( periodic_1, periodic_2, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.
 %-------- INFLOW/OUTFLOW BOUNDARY CONDITION SPECIFIC FOR TURBOMACHINERY --------%
 %
 MARKER_TURBOMACHINERY= (inflow, outflow)
+MARKER_ANALYZE= (inflow, outflow)
 MARKER_GILES= (inflow, TOTAL_CONDITIONS_PT, 13.8686E+05, 592.295, 1.0, 0.0, 0.0, 1.0, 1.0, outflow, STATIC_PRESSURE, 9.00E+05, 0.0, 0.0, 0.0, 0.0, 1.0, 1.0)
 SPATIAL_FOURIER= YES
 %
@@ -137,6 +138,7 @@ CONV_CAUCHY_EPS= 1E-6
 %
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
+SCREEN_OUTPUT= INNER_ITER, RMS_RES, SURFACE_PRESSURE_DROP
 MESH_FILENAME= mesh_stator_turb.su2
 MESH_FORMAT= SU2
 MESH_OUT_FILENAME= su2mesh_per.su2

From 3d8c1a6168d2c6bb52a7a9e49e644eef76e2ad17 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Wed, 5 Apr 2023 17:34:48 -0700
Subject: [PATCH 349/656] fix adjoint test, simplify SingleZoneDriver logic

---
 Common/include/CConfig.hpp                    |  7 ---
 Common/src/CConfig.cpp                        | 50 +------------------
 .../src/iteration/CDiscAdjFluidIteration.cpp  |  4 +-
 SU2_CFD/src/iteration/CFEAIteration.cpp       |  8 ++-
 SU2_CFD/src/iteration/CFluidIteration.cpp     | 10 ++--
 .../transonic_stator_2D/transonic_stator.cfg  |  6 +--
 TestCases/hybrid_regression.py                | 10 ++--
 TestCases/parallel_regression.py              |  4 +-
 8 files changed, 21 insertions(+), 78 deletions(-)

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index 228b71ee5ac..f10273fbfc8 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -1147,7 +1147,6 @@ class CConfig {
   unsigned long *VolumeOutputFrequencies; /*!< \brief list containing the writing frequencies */
 
   bool Multizone_Mesh;            /*!< \brief Determines if the mesh contains multiple zones. */
-  bool SinglezoneDriver = true;   /*!< \brief Determines if the single-zone driver is used. (TEMPORARY) */
   bool Wrt_ZoneConv;              /*!< \brief Write the convergence history of each individual zone to screen. */
   bool Wrt_ZoneHist;              /*!< \brief Write the convergence history of each individual zone to file. */
   bool SpecialOutput,             /*!< \brief Determines if the special output is written. */
@@ -9325,12 +9324,6 @@ class CConfig {
    */
   bool GetMultizone_Residual(void) const { return Multizone_Residual; }
 
-  /*!
-   * \brief Check if the (new) single-zone driver is to be used (temporary)
-   * \return YES if the (new) single-zone driver is to be used.
-   */
-  bool GetSinglezone_Driver(void) const { return SinglezoneDriver; }
-
   /*!
    * \brief Get the Kind of Radiation model applied.
    * \return Kind of radiation model used.
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index ffe963b7418..5f3a9d7535a 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -2984,52 +2984,8 @@ void CConfig::SetConfig_Parsing(istream& config_buffer){
           newString.append(": invalid option name");
           newString.append(". Check current SU2 options in config_template.cfg.");
           newString.append("\n");
-          if (!option_name.compare("RELAXATION_FACTOR_ADJFLOW"))
-            newString.append("Option RELAXATION_FACTOR_ADJFLOW is now RELAXATION_FACTOR_ADJOINT, "
-                             "and it also applies to discrete adjoint problems.\n\n");
-          else if (!option_name.compare("WRT_MESH_QUALITY"))
-            newString.append("WRT_MESH_QUALITY is deprecated. Use VOLUME_OUTPUT= (MESH_QUALITY, ...) instead.\n\n");
-          else if (!option_name.compare("VISUALIZE_SURFACE_DEF"))
-            newString.append("VISUALIZE_SURFACE_DEF is deprecated. Simply add a surface format to OUTPUT_FILES.\n\n");
-          else if (!option_name.compare("VISUALIZE_VOLUME_DEF"))
-            newString.append("VISUALIZE_VOLUME_DEF is deprecated. Simply add a volume format to OUTPUT_FILES.\n\n");
-          else if (!option_name.compare("WRT_BINARY_RESTART"))
-            newString.append("WRT_BINARY_RESTART is deprecated. The type of restart is determined from the OUTPUT_FILES list.\n\n");
-          else if (!option_name.compare("WRT_RESIDUALS"))
-            newString.append("WRT_RESIDUALS is deprecated. Use VOLUME_OUTPUT= ( RESIDUAL, ... ) instead.\n\n");
-          else if (!option_name.compare("WRT_LIMITERS"))
-            newString.append("WRT_LIMITERS is deprecated. Use VOLUME_OUTPUT= ( LIMITER, ... ) instead.\n\n");
-          else if (!option_name.compare("WRT_CON_FREQ"))
-            newString.append("WRT_CON_FREQ is deprecated. Use SCREEN_WRT_FREQ_INNER or SCREEN_WRT_FREQ_OUTER for multizone cases instead.\n\n");
-          else if (!option_name.compare("WRT_CON_FREQ_DUALTIME"))
-            newString.append("WRT_CON_FREQ_DUALTIME is deprecated. Use SCREEN_WRT_FREQ_TIME instead.\n\n");
-          else if (!option_name.compare("WRT_SRF_SOL"))
-            newString.append("WRT_SRF_SOL is deprecated. Simply add a surface format to OUTPUT_FILES.\n\n");
-          else if (!option_name.compare("WRT_CSV_SOL"))
-            newString.append("WRT_CSV_SOL is deprecated. Simply add a CSV format to OUTPUT_FILES.\n\n");
-          else if (!option_name.compare("WRT_SOL_FREQ"))
-            newString.append("WRT_SOL_FREQ is deprecated. Use OUTPUT_WRT_FREQ instead.\n\n");
-          else if (!option_name.compare("WRT_SOL_FREQ_DUALTIME"))
-            newString.append("WRT_SOL_FREQ_DUALTIME is deprecated. Use OUTPUT_WRT_FREQ instead.\n\n");
-          else if (!option_name.compare("UNST_RESTART_ITER"))
-            newString.append("UNST_RESTART_ITER is deprecated. Use RESTART_ITER instead.\n\n");
-          else if (!option_name.compare("DYN_RESTART_ITER"))
-            newString.append("DYN_RESTART_ITER is deprecated. Use RESTART_ITER instead.\n\n");
-          else if (!option_name.compare("CONV_CRITERIA"))
-            newString.append("CONV_CRITERIA is deprecated. SU2 will choose the criteria automatically based on the CONV_FIELD.\n"
-                             "RESIDUAL for any RMS_* BGS_* value. CAUCHY for coefficients like DRAG etc.\n\n");
-          else if (!option_name.compare("THERMAL_DIFFUSIVITY"))
-            newString.append("THERMAL_DIFFUSIVITY is deprecated. See the INC_ENERGY_EQUATION options instead.\n\n");
-          else if (!option_name.compare("THERMAL_DIFFUSIVITY_SOLID"))
-            newString.append("THERMAL_DIFFUSIVITY_SOLID is deprecated. Set THERMAL_CONDUCTIVITY_CONSTANT, MATERIAL_DENSITY and SPECIFIC_HEAT_CP instead.\n\n");
-          else if (!option_name.compare("SOLID_THERMAL_CONDUCTIVITY"))
-            newString.append("SOLID_THERMAL_CONDUCTIVITY is deprecated. Use THERMAL_CONDUCTIVITY_CONSTANT instead.\n\n");
-          else if (!option_name.compare("SOLID_DENSITY"))
-            newString.append("SOLID_DENSITY is deprecated. Use MATERIAL_DENSITY instead.\n\n");
-          else if (!option_name.compare("SOLID_TEMPERATURE_INIT"))
-            newString.append("SOLID_TEMPERATURE_INIT is deprecated. Use FREESTREAM_TEMPERATURE instead.\n\n");
-          else if (!option_name.compare("SA_QCR"))
-            newString.append("SA_QCR is deprecated. Use SA_OPTIONS=QCR2000 instead.\n\n");
+          if (!option_name.compare("SINGLEZONE_DRIVER"))
+            newString.append("Option SINGLEZONE_DRIVER is deprecated, it does not have a replacement.\n\n");
           else {
             /*--- Find the most likely candidate for the unrecognized option, based on the length
              of start and end character sequences shared by candidates and the option. ---*/
@@ -3296,8 +3252,6 @@ void CConfig::SetnZone(){
       SU2_MPI::Error("Number of markers in MARKER_ZONE_INTERFACE must be a multiple of 2", CURRENT_FUNCTION);
     }
 
-    SinglezoneDriver  = NO;
-
     if (Multizone_Mesh){
 
       /*--- Get the number of zones from the mesh file --- */
diff --git a/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
index 6e10e9df4fc..93e29ff3f30 100644
--- a/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
@@ -469,7 +469,7 @@ void CDiscAdjFluidIteration::InitializeAdjoint(CSolver***** solver, CGeometry***
     solver[iZone][iInst][MESH_0][ADJRAD_SOL]->SetAdjoint_Output(geometry[iZone][iInst][MESH_0], config[iZone]);
   }
 
-  if (config[iZone]->GetFluidProblem() && config[iZone]->GetSinglezone_Driver()) {
+  if (config[iZone]->GetFluidProblem() && !config[iZone]->GetMultizone_Problem()) {
     solver[iZone][iInst][MESH_0][FLOW_SOL]->SetVertexTractionsAdjoint(geometry[iZone][iInst][MESH_0], config[iZone]);
   }
 
@@ -601,7 +601,7 @@ void CDiscAdjFluidIteration::RegisterOutput(CSolver***** solver, CGeometry**** g
   if (config[iZone]->AddRadiation()) {
     solver[iZone][iInst][MESH_0][ADJRAD_SOL]->RegisterOutput(geometry[iZone][iInst][MESH_0], config[iZone]);
   }
-  if (config[iZone]->GetFluidProblem() && config[iZone]->GetSinglezone_Driver()) {
+  if (config[iZone]->GetFluidProblem() && !config[iZone]->GetMultizone_Problem()) {
     solver[iZone][iInst][MESH_0][FLOW_SOL]->RegisterVertexTractions(geometry[iZone][iInst][MESH_0], config[iZone]);
   }
 
diff --git a/SU2_CFD/src/iteration/CFEAIteration.cpp b/SU2_CFD/src/iteration/CFEAIteration.cpp
index c827f28467e..3c9dceba07e 100644
--- a/SU2_CFD/src/iteration/CFEAIteration.cpp
+++ b/SU2_CFD/src/iteration/CFEAIteration.cpp
@@ -240,11 +240,9 @@ bool CFEAIteration::Monitor(COutput* output, CIntegration**** integration, CGeom
 
   UsedTime = StopTime - StartTime;
 
-  if (config[val_iZone]->GetMultizone_Problem() || config[val_iZone]->GetSinglezone_Driver()) {
-    output->SetHistoryOutput(geometry[val_iZone][val_iInst][MESH_0], solver[val_iZone][val_iInst][MESH_0],
-                              config[val_iZone], config[val_iZone]->GetTimeIter(), config[val_iZone]->GetOuterIter(),
-                              config[val_iZone]->GetInnerIter());
-  }
+  output->SetHistoryOutput(geometry[val_iZone][val_iInst][MESH_0], solver[val_iZone][val_iInst][MESH_0],
+                           config[val_iZone], config[val_iZone]->GetTimeIter(), config[val_iZone]->GetOuterIter(),
+                           config[val_iZone]->GetInnerIter());
 
   return output->GetConvergence();
 }
diff --git a/SU2_CFD/src/iteration/CFluidIteration.cpp b/SU2_CFD/src/iteration/CFluidIteration.cpp
index 6fd247d3579..8a0dd350e88 100644
--- a/SU2_CFD/src/iteration/CFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CFluidIteration.cpp
@@ -213,11 +213,9 @@ bool CFluidIteration::Monitor(COutput* output, CIntegration**** integration, CGe
 
   UsedTime = StopTime - StartTime;
 
-  if (config[val_iZone]->GetMultizone_Problem() || config[val_iZone]->GetSinglezone_Driver()) {
-    output->SetHistoryOutput(geometry[val_iZone][val_iInst][MESH_0], solver[val_iZone][val_iInst][MESH_0],
-                             config[val_iZone], config[val_iZone]->GetTimeIter(), config[val_iZone]->GetOuterIter(),
-                             config[val_iZone]->GetInnerIter());
-  }
+  output->SetHistoryOutput(geometry[val_iZone][val_iInst][MESH_0], solver[val_iZone][val_iInst][MESH_0],
+                           config[val_iZone], config[val_iZone]->GetTimeIter(), config[val_iZone]->GetOuterIter(),
+                           config[val_iZone]->GetInnerIter());
 
   /*--- If convergence was reached --*/
   StopCalc = output->GetConvergence();
@@ -238,7 +236,7 @@ void CFluidIteration::Postprocess(COutput* output, CIntegration**** integration,
                                   CFreeFormDefBox*** FFDBox, unsigned short val_iZone, unsigned short val_iInst) {
 
   /*--- Temporary: enable only for single-zone driver. This should be removed eventually when generalized. ---*/
-  if (config[val_iZone]->GetSinglezone_Driver()) {
+  if (!config[val_iZone]->GetMultizone_Problem()) {
 
     /*--- Compute the tractions at the vertices ---*/
     solver[val_iZone][val_iInst][MESH_0][FLOW_SOL]->ComputeVertexTractions(geometry[val_iZone][val_iInst][MESH_0],
diff --git a/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg b/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg
index 83f16b2d216..66c520c0a09 100644
--- a/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg
+++ b/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg
@@ -17,7 +17,6 @@ KIND_TURB_MODEL= SST
 MATH_PROBLEM= DISCRETE_ADJOINT
 RESTART_SOL= NO
 NZONES= 1
-%SINGLEZONE_DRIVER=NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
@@ -87,6 +86,7 @@ AVERAGE_MACH_LIMIT= 0.03
 %
 MARKER_PLOTTING= (airfoil)
 MARKER_MONITORING= (airfoil)
+MARKER_ANALYZE= (outflow, inflow)
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
@@ -152,13 +152,13 @@ FFD_CONTINUITY= 2ND_DERIVATIVE
 %
 DEFINITION_DV= ( 19, 1.0 | airfoil | MAIN_BOX, 0, 0, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 1, 0, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 2, 0, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 3, 0, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 4, 0, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 0, 1, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 1, 1, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 2, 1, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 3, 1, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 4, 1, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 0, 2, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 1, 2, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 2, 2, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 3, 2, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 4, 2, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 0, 3, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 1, 3, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 2, 3, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 3, 3, 0.0, 0.0 ); ( 19, 1.0 | airfoil | MAIN_BOX, 4, 3, 0.0, 0.0 )
 OPT_CONSTRAINT= ( FLOW_ANGLE_OUT < -74.0 ) * 0.001
-OPT_OBJECTIVE= ENTROPY_GENERATION* 0.0001
+OPT_OBJECTIVE= SURFACE_PRESSURE_DROP* 0.0001
 OPT_ITERATIONS= 19
 OPT_ACCURACY= 1E-10
 
 % --------------------- OBJECTIVE FUNCTION DEFINITION -----------------------%
 %
-OBJECTIVE_FUNCTION= ENTROPY_GENERATION
+OBJECTIVE_FUNCTION= SURFACE_PRESSURE_DROP
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index 665d8f2a5f0..04997ff9ba8 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -539,7 +539,7 @@ def main():
     Jones_tc_restart.cfg_dir   = "turbomachinery/APU_turbocharger"
     Jones_tc_restart.cfg_file  = "Jones_restart.cfg"
     Jones_tc_restart.test_iter = 5
-    Jones_tc_restart.test_vals = [-6.986563, -3.096834, -14.849532, -9.102914, -11.787851, -6.266208, 7.3266e+04, 7.3266e+04]
+    Jones_tc_restart.test_vals = [-6.986581, -3.096834, -14.849548, -9.102930, -11.787851, -6.266207, 73266, 73266]
     test_list.append(Jones_tc_restart)
 
     # 2D axial stage
@@ -547,8 +547,8 @@ def main():
     axial_stage2D.cfg_dir   = "turbomachinery/axial_stage_2D"
     axial_stage2D.cfg_file  = "Axial_stage2D.cfg"
     axial_stage2D.test_iter = 20
-    axial_stage2D.test_vals         = [1.047323, 1.661341, -2.913940, 2.588179, -2.486770, 3.050954, 1.0638e+05, 1.0638e+05]
-    axial_stage2D.test_vals_aarch64 = [1.047323, 1.661341, -2.913940, 2.588179, -2.486770, 3.050954, 1.0638e+05, 1.0638e+05]
+    axial_stage2D.test_vals         = [1.047244, 1.661126, -2.914064, 2.588061, -2.486924, 3.050785, 106380, 106380]
+    axial_stage2D.test_vals_aarch64 = [1.047244, 1.661126, -2.914064, 2.588061, -2.486924, 3.050785, 106380, 106380]
     test_list.append(axial_stage2D)
 
     # 2D transonic stator restart
@@ -556,8 +556,8 @@ def main():
     transonic_stator_restart.cfg_dir   = "turbomachinery/transonic_stator_2D"
     transonic_stator_restart.cfg_file  = "transonic_stator_restart.cfg"
     transonic_stator_restart.test_iter = 20
-    transonic_stator_restart.test_vals         = [-7.534574, -6.838075, -6.618228, -1.567726, -6.767343, -0.738638, -4.7165e+05]
-    transonic_stator_restart.test_vals_aarch64 = [-7.534574, -6.838075, -6.618228, -1.567726, -6.767343, -0.738638, -4.7165e+05]
+    transonic_stator_restart.test_vals         = [-7.542642, -6.840866, -6.669194, -1.578593, -6.793009, -0.742574, -471650]
+    transonic_stator_restart.test_vals_aarch64 = [-7.542642, -6.840866, -6.669194, -1.578593, -6.793009, -0.742574, -471650]
     test_list.append(transonic_stator_restart)
 
     ######################################
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index de4db10e99f..32051bdf830 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -992,7 +992,7 @@ def main():
     axial_stage2D.cfg_dir   = "turbomachinery/axial_stage_2D"
     axial_stage2D.cfg_file  = "Axial_stage2D.cfg"
     axial_stage2D.test_iter = 20
-    axial_stage2D.test_vals = [1.047323, 1.661341, -2.913940, 2.588179, -2.486770, 3.050954, 1.0638e+05, 1.0638e+05]
+    axial_stage2D.test_vals = [1.047301, 1.661328, -2.913923, 2.588194, -2.486769, 3.050953, 106380, 106380]
     test_list.append(axial_stage2D)
 
     # 2D transonic stator restart
@@ -1000,7 +1000,7 @@ def main():
     transonic_stator_restart.cfg_dir   = "turbomachinery/transonic_stator_2D"
     transonic_stator_restart.cfg_file  = "transonic_stator_restart.cfg"
     transonic_stator_restart.test_iter = 20
-    transonic_stator_restart.test_vals = [-7.534574, -6.838075, -6.618228, -1.567726, -6.767343, -0.738638, -4.7165e+05]
+    transonic_stator_restart.test_vals = [-7.544516, -6.822541, -6.689799, -1.581068, -6.798361, -0.746758, -471650]
     test_list.append(transonic_stator_restart)
 
     ######################################

From 8292429b6d792a5c1acc4b1e5b9fbf9d7ddaa6dd Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Thu, 6 Apr 2023 10:48:06 +0200
Subject: [PATCH 350/656] Updated submodules

---
 externals/codi         | 2 +-
 subprojects/CoolProp   | 2 +-
 subprojects/Mutationpp | 2 +-
 3 files changed, 3 insertions(+), 3 deletions(-)

diff --git a/externals/codi b/externals/codi
index 8cdb2a2e623..427c2dc754a 160000
--- a/externals/codi
+++ b/externals/codi
@@ -1 +1 @@
-Subproject commit 8cdb2a2e6231ede6343294ac9af748b3ea105ecd
+Subproject commit 427c2dc754a628ad3c9310c766c988ac5ce21bc7
diff --git a/subprojects/CoolProp b/subprojects/CoolProp
index 3b510388279..0ce42fcf3bb 160000
--- a/subprojects/CoolProp
+++ b/subprojects/CoolProp
@@ -1 +1 @@
-Subproject commit 3b510388279d39fe63608736a00888327edc2aff
+Subproject commit 0ce42fcf3bb2c373512bc825a4f0c1973a78f307
diff --git a/subprojects/Mutationpp b/subprojects/Mutationpp
index 4cb6e3a05c1..5ff579f4378 160000
--- a/subprojects/Mutationpp
+++ b/subprojects/Mutationpp
@@ -1 +1 @@
-Subproject commit 4cb6e3a05c15f49ffd346dc9f185ccc3459728b0
+Subproject commit 5ff579f43781cae07411e5ab46291c9971536be6

From 22b45b793b8fd1ec6c2643316bb417852673f2c9 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Thu, 6 Apr 2023 05:33:59 -0700
Subject: [PATCH 351/656] update discadj case for new objective

---
 TestCases/hybrid_regression_AD.py   | 4 ++--
 TestCases/parallel_regression_AD.py | 2 +-
 2 files changed, 3 insertions(+), 3 deletions(-)

diff --git a/TestCases/hybrid_regression_AD.py b/TestCases/hybrid_regression_AD.py
index 1f1507c8874..2cb40a0d31d 100644
--- a/TestCases/hybrid_regression_AD.py
+++ b/TestCases/hybrid_regression_AD.py
@@ -193,8 +193,8 @@ def main():
     discadj_trans_stator.cfg_dir   = "disc_adj_turbomachinery/transonic_stator_2D"
     discadj_trans_stator.cfg_file  = "transonic_stator.cfg"
     discadj_trans_stator.test_iter = 79
-    discadj_trans_stator.test_vals         = [79.000000, -1.938803, -1.981888]
-    discadj_trans_stator.test_vals_aarch64 = [79.000000, -1.938809, -1.995540]
+    discadj_trans_stator.test_vals         = [79, 0.770158, 2.051501]
+    discadj_trans_stator.test_vals_aarch64 = [79, 0.770158, 2.051501]
     test_list.append(discadj_trans_stator)
 
     ###################################
diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index 74a991ec43b..a67de6139db 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -230,7 +230,7 @@ def main():
     discadj_trans_stator.cfg_dir   = "disc_adj_turbomachinery/transonic_stator_2D"
     discadj_trans_stator.cfg_file  = "transonic_stator.cfg"
     discadj_trans_stator.test_iter = 79
-    discadj_trans_stator.test_vals = [79.000000, -1.941681, -1.984570]
+    discadj_trans_stator.test_vals = [79, 0.770040, 2.052053]
     test_list.append(discadj_trans_stator)
 
     ###################################

From 9ae074889a02272b839f1b848b1832ed594de07f Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Thu, 6 Apr 2023 15:05:52 +0200
Subject: [PATCH 352/656] Implemented some of Pedros comments

---
 Common/include/CConfig.hpp                   |   6 +-
 Common/include/option_structure.hpp          |   8 +-
 Common/src/CConfig.cpp                       |   2 +-
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp   |  73 +++++++-------
 SU2_CFD/include/fluid/CFluidModel.hpp        |  24 ++---
 SU2_CFD/include/variables/CEulerVariable.hpp |  49 +++++++++
 SU2_CFD/include/variables/CVariable.hpp      |  19 ++--
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp       | 100 +++++++++----------
 SU2_CFD/src/solvers/CEulerSolver.cpp         |  16 +--
 SU2_CFD/src/solvers/CIncEulerSolver.cpp      |   2 +-
 SU2_CFD/src/variables/CNSVariable.cpp        |   7 --
 externals/meson                              |   2 +-
 externals/ninja                              |   2 +-
 meson_scripts/init.py                        |   2 +-
 subprojects/MLPCpp                           |   2 +-
 15 files changed, 172 insertions(+), 142 deletions(-)

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index c4b5ecd3174..83182e76a2b 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -524,8 +524,8 @@ class CConfig {
   Kind_TimeIntScheme_Species,   /*!< \brief Time integration for the species model. */
   Kind_TimeIntScheme_Heat,      /*!< \brief Time integration for the wave equations. */
   Kind_TimeStep_Heat,           /*!< \brief Time stepping method for the (fvm) heat equation. */
-  Kind_DataDriven_Method,       /*!< \brief Method used for datset regression in datadriven fluid models. */
   n_Datadriven_files;
+  ENUM_DATADRIVEN_METHOD Kind_DataDriven_Method;       /*!< \brief Method used for datset regression in datadriven fluid models. */
 
   su2double DataDriven_Relaxation_Factor, /*!< \brief Relaxation factor for Newton solvers in datadriven fluid models. */
             DataDriven_initial_density,   /*!< \brief Initial density value for Newton solvers in datadriven fluid models. */
@@ -3790,14 +3790,12 @@ class CConfig {
   /*!
    * \brief Datadriven method for EoS evaluation.
    */
-  unsigned short GetKind_DataDriven_Method(void) const { return Kind_DataDriven_Method; }
+  ENUM_DATADRIVEN_METHOD GetKind_DataDriven_Method(void) const { return Kind_DataDriven_Method; }
 
   /*!
    * \brief Get name of the input file for the data-driven fluid model interpolation method.
    * \return Name of the input file for the interpolation method.
    */
-  string GetDataDriven_Filename(unsigned short i_file=0) const { return DataDriven_Method_FileNames[i_file]; }
-
   string* GetDataDriven_FileNames(void) const { return DataDriven_Method_FileNames; }
 
   /*!
diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index 2cf4af81bd9..941afb31d58 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -595,16 +595,16 @@ MakePair("ONESPECIES", ONESPECIES)
 };
 
 /*!
-* \brief types of interpolation methods for data-driven fluid models.
+* \brief Types of interpolation methods for data-driven fluid models.
 */
-enum ENUM_DATADRIVEN_METHOD {
+enum class ENUM_DATADRIVEN_METHOD {
   LUT = 0,
   MLP = 1
 };
 
 static const MapType<std::string, ENUM_DATADRIVEN_METHOD> DataDrivenMethod_Map = {
-  MakePair("LUT", LUT)
-  MakePair("MLP", MLP)
+  MakePair("LUT", ENUM_DATADRIVEN_METHOD::LUT)
+  MakePair("MLP", ENUM_DATADRIVEN_METHOD::MLP)
 };
 
 /*!
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 509c49cb0f5..1ca4f57fb6d 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -1169,7 +1169,7 @@ void CConfig::SetConfig_Options() {
 
   /*!\par CONFIG_CATEGORY: Data-driven fluid model parameters \ingroup Config*/
   /*!\brief INTERPOLATION_METHOD \n DESCRIPTION: Interpolation method used to determine the thermodynamic state of the fluid. \n OPTIONS: See \link DataDrivenMethod_Map \endlink DEFAULT: MLP \ingroup Config*/
-  addEnumOption("INTERPOLATION_METHOD",Kind_DataDriven_Method, DataDrivenMethod_Map, MLP);
+  addEnumOption("INTERPOLATION_METHOD",Kind_DataDriven_Method, DataDrivenMethod_Map, ENUM_DATADRIVEN_METHOD::LUT);
   /*!\brief FILENAME_INTERPOLATOR \n DESCRIPTION: Input file for the interpolation method. \n \ingroup Config*/
   addStringListOption("FILENAMES_INTERPOLATOR", n_Datadriven_files, DataDriven_Method_FileNames);
   /*!\brief DATADRIVEN_NEWTON_RELAXATION \n DESCRIPTION: Relaxation factor for Newton solvers in data-driven fluid model. \n \ingroup Config*/
diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index bbbb0be7e4c..fff28602b67 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -42,48 +42,47 @@
  * fluid dynamic state definition.
  * \author: E.C.Bunschoten.
  */
-class CDataDrivenFluid : public CFluidModel {
+class CDataDrivenFluid final : public CFluidModel {
  protected:
-  int rank;
-  unsigned short Kind_DataDriven_Method = ENUM_DATADRIVEN_METHOD::LUT;  // Interpolation method for data set evaluation
+  int rank{MASTER_NODE}; /*!< \brief MPI Rank. */
+  ENUM_DATADRIVEN_METHOD Kind_DataDriven_Method = ENUM_DATADRIVEN_METHOD::LUT;  /*!< \brief Interpolation method for data set evaluation. */
 
-  size_t idx_rho,  // Interpolator index for density input
-      idx_e;       // Interpolator index for energy input
+  size_t idx_rho,  /*!< \brief Interpolator index for density input. */
+      idx_e;       /*!< \brief Interpolator index for energy input. */
 
-  su2double Newton_Relaxation,  // Relaxation factor for Newton solvers.
-      rho_start,                // Initial value for the density in Newton solver processes.
-      e_start,                  // Initial value for the energy in Newton solver processes.
-      Newton_Tolerance;         // Normalized tolerance for Newton solvers.
+  su2double Newton_Relaxation,  /*!< \brief Relaxation factor for Newton solvers. */
+      rho_start,                /*!< \brief Initial value for the density in Newton solver processes. */
+      e_start,                  /*!< \brief Initial value for the energy in Newton solver processes. */
+      Newton_Tolerance;         /*!< \brief Normalized tolerance for Newton solvers. */
 
-  unsigned long MaxIter_Newton;  // Maximum number of iterations for Newton solvers
+  unsigned long MaxIter_Newton;  /*!< \brief Maximum number of iterations for Newton solvers. */
 
-  su2double dsde_rho, /*!< \brief Entropy derivative w.r.t. density */
-      dsdrho_e,       /*!< \brief Entropy derivative w.r.t. static energy */
-      d2sde2,         /*!< \brief Entropy second derivative w.r.t. static energy */
-      d2sdedrho,      /*!< \brief Entropy second derivative w.r.t. density and static energy */
-      d2sdrho2;       /*!< \brief Entropy second derivative w.r.t. static density */
+  su2double dsde_rho, /*!< \brief Entropy derivative w.r.t. density. */
+      dsdrho_e,       /*!< \brief Entropy derivative w.r.t. static energy. */
+      d2sde2,         /*!< \brief Entropy second derivative w.r.t. static energy. */
+      d2sdedrho,      /*!< \brief Entropy second derivative w.r.t. density and static energy. */
+      d2sdrho2;       /*!< \brief Entropy second derivative w.r.t. static density. */
 
   vector<string>
-      input_names_rhoe,   // Data-driven method input variable names of the independent variables (density, energy).
-      output_names_rhoe;  // Output variable names listed in the data-driven method input file name.
+      input_names_rhoe,   /*!< \brief Data-driven method input variable names of the independent variables (density, energy). */
+      output_names_rhoe;  /*!< \brief Output variable names listed in the data-driven method input file name. */
 
-  vector<su2double*> outputs_rhoe;  // Pointers to output variables.
+  vector<su2double*> outputs_rhoe;  /*!< \brief Pointers to output variables. */
 
   /*--- Class variables for the multi-layer perceptron method ---*/
 #ifdef USE_MLPCPP
-  MLPToolbox::CLookUp_ANN* lookup_mlp;  // multi-layer perceptron collection.
-  MLPToolbox::CIOMap* iomap_rhoe;       // input-output map.
+  MLPToolbox::CLookUp_ANN* lookup_mlp;  /*!< \brief Multi-layer perceptron collection. */
+  MLPToolbox::CIOMap* iomap_rhoe;       /*!< \brief Input-output map. */
 #endif
-  vector<su2double> MLP_inputs;  // inputs for the multi-layer perceptron look-up operation.
+  vector<su2double> MLP_inputs;  /*!< \brief Inputs for the multi-layer perceptron look-up operation. */
 
-  /*--- Class variables for the look-up table method ---*/
-  CLookUpTable* lookup_table;
+  CLookUpTable* lookup_table; /*!< \brief Look-up table regression object. */
 
-  unsigned long outside_dataset,  // Density-energy combination lies outside data set.
-      nIter_Newton;               // Number of Newton solver iterations.
+  unsigned long outside_dataset,  /*!< \brief Density-energy combination lies outside data set. */
+      nIter_Newton;               /*!< \brief Number of Newton solver iterations. */
 
   /*!
-   * \brief Map dataset variables to specific look-up operations
+   * \brief Map dataset variables to specific look-up operations.
    */
   void MapInputs_to_Outputs();
 
@@ -114,71 +113,71 @@ class CDataDrivenFluid : public CFluidModel {
   /*!
    * \brief Constructor of the class.
    */
-  CDataDrivenFluid(const CConfig* config);
+  CDataDrivenFluid(const CConfig* config, bool display=true);
 
   ~CDataDrivenFluid();
   /*!
-   * \brief Set the Dimensionless State using Density and Internal Energy
+   * \brief Set the Dimensionless State using Density and Internal Energy.
    * \param[in] rho - first thermodynamic variable (density).
    * \param[in] e - second thermodynamic variable (static energy).
    */
   void SetTDState_rhoe(su2double rho, su2double e) override;
 
   /*!
-   * \brief Set the Dimensionless State using Pressure  and Temperature
+   * \brief Set the Dimensionless State using Pressure  and Temperature.
    * \param[in] P - first thermodynamic variable (pressure).
    * \param[in] T - second thermodynamic variable (temperature).
    */
   void SetTDState_PT(su2double P, su2double T) override;
 
   /*!
-   * \brief Set the Dimensionless State using Pressure and Density
+   * \brief Set the Dimensionless State using Pressure and Density.
    * \param[in] P - first thermodynamic variable (pressure).
    * \param[in] rho - second thermodynamic variable (density).
    */
   void SetTDState_Prho(su2double P, su2double rho) override;
 
   /*!
-   * \brief Set the Dimensionless Internal Energy using Pressure and Density
+   * \brief Set the Dimensionless Internal Energy using Pressure and Density.
    * \param[in] P - first thermodynamic variable (pressure).
    * \param[in] rho - second thermodynamic variable (density).
    */
   void SetEnergy_Prho(su2double P, su2double rho) override;
 
   /*!
-   * \brief Set the Dimensionless Internal Energy using Pressure and Density
+   * \brief Set the Dimensionless Internal Energy using Pressure and Density.
    * \param[in] rho - second thermodynamic variable (density).
    */
   void SetTDState_rhoT(su2double rho, su2double T) override;
 
   /*!
-   * \brief Set the Dimensionless State using Enthalpy and Entropy
+   * \brief Set the Dimensionless State using Enthalpy and Entropy.
    * \param[in] h - first thermodynamic variable (h).
    * \param[in] s - second thermodynamic variable (s).
    */
   void SetTDState_hs(su2double h, su2double s) override;
 
   /*!
-   * \brief Set the Dimensionless State using Pressure and Entropy
+   * \brief Set the Dimensionless State using Pressure and Entropy.
    * \param[in] P - first thermodynamic variable (P).
    * \param[in] s - second thermodynamic variable (s).
    */
   void SetTDState_Ps(su2double P, su2double s) override;
 
   /*!
-   * \brief Set the initial guess for the density in Newton solvers
+   * \brief Set the initial guess for the density in Newton solvers.
    * \param[in] rho - Initial value for density.
    */
   void SetInitialDensity(su2double rho) override { rho_start = rho; }
 
   /*!
-   * \brief Set the initial guess for the static energy in Newton solvers
+   * \brief Set the initial guess for the static energy in Newton solvers.
    * \param[in] e - Initial value for static energy.
    */
   void SetInitialEnergy(su2double e) override { e_start = e; }
 
   /*!
-   * \brief Get fluid model extrapolation instance
+   * \brief Get fluid model extrapolation instance.
    * \return Query point lies outside fluid model data range.
    */
   unsigned long GetExtrapolation() override { return outside_dataset; }
diff --git a/SU2_CFD/include/fluid/CFluidModel.hpp b/SU2_CFD/include/fluid/CFluidModel.hpp
index 0b2f71c4f0b..62a098fd1fe 100644
--- a/SU2_CFD/include/fluid/CFluidModel.hpp
+++ b/SU2_CFD/include/fluid/CFluidModel.hpp
@@ -327,26 +327,26 @@ class CFluidModel {
   void SetEddyViscosity(su2double val_Mu_Turb) { Mu_Turb = val_Mu_Turb; }
 
   /*!
-  * \brief Set the initial guess for the density in Newton solvers
-  * \param[in] rho - Initial value for density.
-  */
+   * \brief Set the initial guess for the density in Newton solvers
+   * \param[in] rho - Initial value for density.
+   */
   virtual void SetInitialDensity(su2double rho) {}
 
   /*!
-  * \brief Set the initial guess for the static energy in Newton solvers
-  * \param[in] e - Initial value for static energy.
-  */
+   * \brief Set the initial guess for the static energy in Newton solvers
+   * \param[in] e - Initial value for static energy.
+   */
   virtual void SetInitialEnergy(su2double e) {}
 
   /*!
-  * \brief Get fluid model extrapolation instance
-  * \return Query point lies outside fluid model data range.
-  */
+   * \brief Get fluid model extrapolation instance
+   * \return Query point lies outside fluid model data range.
+   */
   virtual unsigned long GetExtrapolation() { return 0; }
 
   /*!
-  * \brief Get number of Newton solver iterations.
-  * \return Newton solver iteration count at termination.
-  */
+   * \brief Get number of Newton solver iterations.
+   * \return Newton solver iteration count at termination.
+   */
   virtual unsigned long GetnIter_Newton() { return 0; }
 };
diff --git a/SU2_CFD/include/variables/CEulerVariable.hpp b/SU2_CFD/include/variables/CEulerVariable.hpp
index 44f07ffa0a2..ca3276817e1 100644
--- a/SU2_CFD/include/variables/CEulerVariable.hpp
+++ b/SU2_CFD/include/variables/CEulerVariable.hpp
@@ -74,6 +74,11 @@ class CEulerVariable : public CFlowVariable {
   MatrixType WindGust;      /*! < \brief Wind gust value */
   MatrixType WindGustDer;   /*! < \brief Wind gust derivatives value */
 
+  bool DataDrivenFluid = false; /*!< \brief Usage of data-driven fluid model. DatasetExtrapolation and FluidEntropy will not be sized if disabled. */
+  su2vector<unsigned short> DatasetExtrapolation; /*!< \brief Stores instances of dataset bounds violation when using datadriven fluid models. */
+  su2vector<unsigned long> NIterNewtonsolver;    /*!< \brief Stores number of Newton solver iterations when using datadriven fluid models. */
+  VectorType FluidEntropy;          /*!< \brief Stores the fluid entropy value as computed by the datadriven fluid model. */
+
  public:
   /*!
    * \brief Constructor of the class.
@@ -324,4 +329,48 @@ class CEulerVariable : public CFlowVariable {
     for (unsigned long iDim = 0; iDim < nDim; iDim++) Solution(iPoint, iDim+1) = GetDensity(iPoint) * val_vector[iDim];
   }
 
+  /*!
+   * \brief Set fluid entropy
+   * \param[in] iPoint - Node index
+   * \param[in] entropy - fluid entropy value.
+   */
+  inline void SetEntropy(unsigned long iPoint, su2double entropy) final { FluidEntropy[iPoint] = entropy; };
+
+  /*!
+   * \brief Get fluid entropy
+   * \param[in] iPoint - Node index
+   * \return Entropy - Fluid entropy value
+   */
+  inline su2double GetEntropy(unsigned long iPoint) const final { return FluidEntropy[iPoint]; }
+
+  /*!
+   * \brief Set dataset extrapolation instance
+   * \param[in] iPoint - Node index
+   * \param[in] extrapolation - Extrapolation instance (0 = within dataset, 1 = outside dataset)
+   */
+  inline void SetDataExtrapolation(unsigned long iPoint, unsigned short extrapolation) final {
+    DatasetExtrapolation[iPoint] = extrapolation;
+  };
+
+  /*!
+   * \brief Get dataset extrapolation instance
+   * \param[in] iPoint - Node index
+   * \return extrapolation - Extrapolation instance (0 = within dataset, 1 = outside dataset)
+   */
+  inline unsigned short GetDataExtrapolation(unsigned long iPoint) const final { return DatasetExtrapolation[iPoint]; }
+
+  /*!
+   * \brief Set the number of iterations required by a Newton solver used by the fluid model.
+   * \param[in] iPoint - Node index
+   * \param[in] nIter - Number of iterations evaluated by the Newton solver
+   */
+  inline void SetNewtonSolverIterations(unsigned long iPoint, unsigned long nIter) final { NIterNewtonsolver[iPoint] = nIter; }
+
+  /*!
+   * \brief Get the number of iterations required by a Newton solver used by the fluid model.
+   * \param[in] iPoint - Node index
+   * \return Number of iterations evaluated by the Newton solver
+   */
+  inline unsigned long GetNewtonSolverIterations(unsigned long iPoint) const final { return NIterNewtonsolver[iPoint]; }
+
 };
diff --git a/SU2_CFD/include/variables/CVariable.hpp b/SU2_CFD/include/variables/CVariable.hpp
index 446eeb4a1aa..9ca38e749f8 100644
--- a/SU2_CFD/include/variables/CVariable.hpp
+++ b/SU2_CFD/include/variables/CVariable.hpp
@@ -101,11 +101,6 @@ class CVariable {
 
   VectorType SolutionExtra_BGS_k; /*!< \brief Intermediate storage, enables cross term extraction as that is also pushed to Solution. */
 
-  bool DataDrivenFluid = false; /*!< \brief Usage of data-driven fluid model. DatasetExtrapolation and FluidEntropy will not be sized if disabled. */
-  su2vector<unsigned short> DatasetExtrapolation; /*!< \brief Stores instances of dataset bounds violation when using datadriven fluid models. */
-  su2vector<unsigned long> NIterNewtonsolver;    /*!< \brief Stores number of Newton solver iterations when using datadriven fluid models. */
-  VectorType FluidEntropy;          /*!< \brief Stores the fluid entropy value as computed by the datadriven fluid model. */
-
  protected:
   unsigned long nPoint = 0;  /*!< \brief Number of points in the domain. */
   unsigned long nDim = 0;      /*!< \brief Number of dimension of the problem. */
@@ -2320,43 +2315,41 @@ class CVariable {
    * \param[in] iPoint - Node index
    * \param[in] entropy - fluid entropy value.
    */
-  void SetEntropy(unsigned long iPoint, su2double entropy) { FluidEntropy[iPoint] = entropy; };
+  inline virtual void SetEntropy(unsigned long iPoint, su2double entropy) { };
 
   /*!
    * \brief Get fluid entropy
    * \param[in] iPoint - Node index
    * \return Entropy - Fluid entropy value
    */
-  su2double GetEntropy(unsigned long iPoint) const { return FluidEntropy[iPoint]; }
+  inline virtual su2double GetEntropy(unsigned long iPoint) const { return 0; }
 
   /*!
    * \brief Set dataset extrapolation instance
    * \param[in] iPoint - Node index
    * \param[in] extrapolation - Extrapolation instance (0 = within dataset, 1 = outside dataset)
    */
-  void SetDataExtrapolation(unsigned long iPoint, unsigned short extrapolation) {
-    DatasetExtrapolation[iPoint] = extrapolation;
-  };
+  inline virtual void SetDataExtrapolation(unsigned long iPoint, unsigned short extrapolation) { };
 
   /*!
    * \brief Get dataset extrapolation instance
    * \param[in] iPoint - Node index
    * \return extrapolation - Extrapolation instance (0 = within dataset, 1 = outside dataset)
    */
-  unsigned short GetDataExtrapolation(unsigned long iPoint) const { return DatasetExtrapolation[iPoint]; }
+  inline virtual unsigned short GetDataExtrapolation(unsigned long iPoint) const { return 0; }
 
   /*!
    * \brief Set the number of iterations required by a Newton solver used by the fluid model.
    * \param[in] iPoint - Node index
    * \param[in] nIter - Number of iterations evaluated by the Newton solver
    */
-  void SetNewtonSolverIterations(unsigned long iPoint, unsigned long nIter) { NIterNewtonsolver[iPoint] = nIter; }
+  inline virtual void SetNewtonSolverIterations(unsigned long iPoint, unsigned long nIter) { }
 
   /*!
    * \brief Get the number of iterations required by a Newton solver used by the fluid model.
    * \param[in] iPoint - Node index
    * \return Number of iterations evaluated by the Newton solver
    */
-  unsigned long GetNewtonSolverIterations(unsigned long iPoint) const { return NIterNewtonsolver[iPoint]; }
+  inline virtual unsigned long GetNewtonSolverIterations(unsigned long iPoint) const { return 0; }
 
 };
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 9ee38e22abb..64cf0b27409 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -31,10 +31,8 @@
 #define USE_MLPCPP
 #endif
 
-CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
-#ifdef HAVE_MPI
-  MPI_Comm_rank(MPI_COMM_WORLD, &rank);
-#endif
+CDataDrivenFluid::CDataDrivenFluid(const CConfig* config, bool display) : CFluidModel() {
+  rank = SU2_MPI::GetRank();
   Kind_DataDriven_Method = config->GetKind_DataDriven_Method();
 
   /*--- Set up interpolation algorithm according to data-driven method. Currently only MLP's are supported. ---*/
@@ -42,13 +40,13 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
     case ENUM_DATADRIVEN_METHOD::MLP:
 #ifdef USE_MLPCPP
       lookup_mlp = new MLPToolbox::CLookUp_ANN(config->GetNDataDriven_Files(), config->GetDataDriven_FileNames());
-      if (rank == MASTER_NODE) lookup_mlp->DisplayNetworkInfo();
+      if ((rank == MASTER_NODE) && display) lookup_mlp->DisplayNetworkInfo();
 #else
       SU2_MPI::Error("SU2 was not compiled with MLPCpp enabled (-Denable-mlpcpp=true).", CURRENT_FUNCTION);
 #endif
       break;
     case ENUM_DATADRIVEN_METHOD::LUT:
-      lookup_table = new CLookUpTable(config->GetDataDriven_Filename(), "Density", "Energy");
+      lookup_table = new CLookUpTable(config->GetDataDriven_FileNames()[0], "Density", "Energy");
       break;
     default:
       break;
@@ -62,7 +60,7 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config) : CFluidModel() {
   /*--- Preprocessing of inputs and outputs for the interpolation method. ---*/
   MapInputs_to_Outputs();
 
-  /*--- Set initial values for density and energy based on config options ---*/
+  /*--- Set initial values for density and energy based on config options. ---*/
   rho_start = config->GetDensity_Init_DataDriven();
   e_start = config->GetEnergy_Init_DataDriven();
 }
@@ -91,7 +89,7 @@ void CDataDrivenFluid::MapInputs_to_Outputs() {
   input_names_rhoe[idx_e] = "Energy";
 
   /*--- Required outputs for the interpolation method are entropy and its partial derivatives with respect to energy and
-   * density ---*/
+   * density. ---*/
   size_t n_outputs = 6;
   size_t idx_s = 0, idx_dsde_rho = 1, idx_dsdrho_e = 2, idx_d2sde2 = 3, idx_d2sdedrho = 4, idx_d2sdrho2 = 5;
 
@@ -110,9 +108,9 @@ void CDataDrivenFluid::MapInputs_to_Outputs() {
   output_names_rhoe[idx_d2sdrho2] = "d2sdrho2";
   outputs_rhoe[idx_d2sdrho2] = &d2sdrho2;
 
-  /*--- Further preprocessing of input and output variables ---*/
+  /*--- Further preprocessing of input and output variables. ---*/
   if (Kind_DataDriven_Method == ENUM_DATADRIVEN_METHOD::MLP) {
-/*--- Map MLP inputs to outputs ---*/
+/*--- Map MLP inputs to outputs. ---*/
 #ifdef USE_MLPCPP
     iomap_rhoe = new MLPToolbox::CIOMap(input_names_rhoe, output_names_rhoe);
     lookup_mlp->PairVariableswithMLPs(*iomap_rhoe);
@@ -122,20 +120,20 @@ void CDataDrivenFluid::MapInputs_to_Outputs() {
 }
 
 void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
-  /*--- Compute thermodynamic state based on density and energy ---*/
+  /*--- Compute thermodynamic state based on density and energy. ---*/
 
   Density = rho;
   StaticEnergy = e;
 
   Evaluate_Dataset(rho, e);
 
-  /*--- Compute speed of sound ---*/
+  /*--- Compute speed of sound. ---*/
   auto blue_term = (dsdrho_e * (2 - rho * pow(dsde_rho, -1) * d2sdedrho) + rho * d2sdrho2);
   auto green_term = (-pow(dsde_rho, -1) * d2sde2 * dsdrho_e + d2sdedrho);
 
   SoundSpeed2 = -rho * pow(dsde_rho, -1) * (blue_term - rho * green_term * (dsdrho_e / dsde_rho));
 
-  /*--- Compute primary flow variables ---*/
+  /*--- Compute primary flow variables. ---*/
   Temperature = 1.0 / dsde_rho;
   Pressure = -pow(rho, 2) * Temperature * dsdrho_e;
   Density = rho;
@@ -148,7 +146,7 @@ void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
   dPde_rho = -pow(rho, 2) * (dTde_rho * dsdrho_e + Temperature * d2sdedrho);
   dPdrho_e = -2 * rho * Temperature * dsdrho_e - pow(rho, 2) * (dTdrho_e * dsdrho_e + Temperature * d2sdrho2);
 
-  /*--- Compute enthalpy and entropy derivatives required for Giles boundary conditions ---*/
+  /*--- Compute enthalpy and entropy derivatives required for Giles boundary conditions. ---*/
   su2double dhdrho_e = -Pressure * pow(rho, -2) + dPdrho_e / rho;
   su2double dhde_rho = 1 + dPde_rho / rho;
 
@@ -159,10 +157,10 @@ void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
 }
 
 void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
-  /*--- Setting initial values for density and energy ---*/
+  /*--- Setting initial values for density and energy. ---*/
   su2double rho = rho_start, e = e_start;
 
-  bool converged = false;  // Convergence flag
+  bool converged = false;
   unsigned long Iter = 0;
 
   su2double delta_P,
@@ -172,17 +170,17 @@ void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
       determinant;
   /*--- Initiating Newton solver ---*/
   while (!converged && (Iter < MaxIter_Newton)) {
-    /*--- Determine thermodynamic state based on current density and energy*/
+    /*--- Determine thermodynamic state based on current density and energy. ---*/
     SetTDState_rhoe(rho, e);
 
-    /*--- Determine pressure and temperature residuals ---*/
+    /*--- Determine pressure and temperature residuals. ---*/
     delta_P = Pressure - P;
     delta_T = Temperature - T;
-    /*--- Continue iterative process if residuals are outside tolerances ---*/
+    /*--- Continue iterative process if residuals are outside tolerances. ---*/
     if ((abs(delta_P / P) < Newton_Tolerance) && (abs(delta_T / T) < Newton_Tolerance)) {
       converged = true;
     } else {
-      /*--- Compute step size for density and energy ---*/
+      /*--- Compute step size for density and energy. ---*/
       determinant = dPdrho_e * dTde_rho - dPde_rho * dTdrho_e;
 
       delta_rho = (dTde_rho * delta_P - dPde_rho * delta_T) / determinant;
@@ -195,22 +193,22 @@ void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
     Iter++;
   }
 
-  /*--- Calculate thermodynamic state based on converged values for density and energy ---*/
+  /*--- Calculate thermodynamic state based on converged values for density and energy. ---*/
   SetTDState_rhoe(rho, e);
 
   nIter_Newton = Iter;
 }
 
 void CDataDrivenFluid::SetTDState_Prho(su2double P, su2double rho) {
-  /*--- Computing static energy according to pressure and density ---*/
+  /*--- Computing static energy according to pressure and density. ---*/
   SetEnergy_Prho(P, rho);
 
-  /*--- Calculate thermodynamic state based on converged value for energy ---*/
+  /*--- Calculate thermodynamic state based on converged value for energy. ---*/
   SetTDState_rhoe(rho, StaticEnergy);
 }
 
 void CDataDrivenFluid::SetEnergy_Prho(su2double P, su2double rho) {
-  /*--- Setting initial values for energy ---*/
+  /*--- Setting initial values for energy. ---*/
   su2double e = e_start;
 
   bool converged = false;
@@ -220,33 +218,33 @@ void CDataDrivenFluid::SetEnergy_Prho(su2double P, su2double rho) {
       delta_e;
 
   while (!converged && (Iter < MaxIter_Newton)) {
-    /*--- Determine thermodynamic state based on current density and energy*/
+    /*--- Determine thermodynamic state based on current density and energy. ---*/
     SetTDState_rhoe(rho, e);
 
-    /*--- Determine pressure and temperature residuals ---*/
+    /*--- Determine pressure and temperature residuals. ---*/
     delta_P = Pressure - P;
 
-    /*--- Continue iterative process if residuals are outside tolerances ---*/
+    /*--- Continue iterative process if residuals are outside tolerances. ---*/
     if (abs(delta_P / P) < Newton_Tolerance) {
       converged = true;
     } else {
-      /*--- Compute step size for energy ---*/
+      /*--- Compute step size for energy. ---*/
       delta_e = delta_P / dPde_rho;
 
-      /*--- energy value ---*/
+      /*--- Update energy value. ---*/
       e -= Newton_Relaxation * delta_e;
     }
     Iter++;
   }
 
-  /*--- Setting static energy as the converged value ---*/
+  /*--- Setting static energy as the converged value. ---*/
   StaticEnergy = e;
 
   nIter_Newton = Iter;
 }
 
 void CDataDrivenFluid::SetTDState_rhoT(su2double rho, su2double T) {
-  /*--- Setting initial values for density and energy ---*/
+  /*--- Setting initial values for density and energy. ---*/
   su2double e = e_start;
 
   bool converged = false;
@@ -255,15 +253,15 @@ void CDataDrivenFluid::SetTDState_rhoT(su2double rho, su2double T) {
   su2double delta_T,
       delta_e;
 
-  /*--- Initiating Newton solver ---*/
+  /*--- Initiating Newton solver. ---*/
   while (!converged && (Iter < MaxIter_Newton)) {
-    /*--- Determine thermodynamic state based on current density and energy*/
+    /*--- Determine thermodynamic state based on current density and energy. ---*/
     SetTDState_rhoe(rho, e);
 
     /*--- Determine temperature residual ---*/
     delta_T = Temperature - T;
 
-    /*--- Continue iterative process if residuals are outside tolerances ---*/
+    /*--- Continue iterative process if residuals are outside tolerances. ---*/
     if (abs(delta_T / T) < Newton_Tolerance) {
       converged = true;
     } else {
@@ -275,14 +273,14 @@ void CDataDrivenFluid::SetTDState_rhoT(su2double rho, su2double T) {
     Iter++;
   }
 
-  /*--- Calculate thermodynamic state based on converged values for density and energy ---*/
+  /*--- Calculate thermodynamic state based on converged values for density and energy. ---*/
   SetTDState_rhoe(rho, e);
 
   nIter_Newton = Iter;
 }
 
 void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
-  /*--- Setting initial values for density and energy ---*/
+  /*--- Setting initial values for density and energy. ---*/
   su2double rho = rho_start, e = e_start;
 
   bool converged = false;
@@ -294,17 +292,17 @@ void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
       delta_e,
       determinant;
 
-  /*--- Initiating Newton solver ---*/
+  /*--- Initiating Newton solver. ---*/
   while (!converged && (Iter < MaxIter_Newton)) {
-    /*--- Determine thermodynamic state based on current density and energy*/
+    /*--- Determine thermodynamic state based on current density and energy. ---*/
     SetTDState_rhoe(rho, e);
 
     su2double Enthalpy = e + Pressure / rho;
-    /*--- Determine pressure and temperature residuals ---*/
+    /*--- Determine pressure and temperature residuals. ---*/
     delta_h = Enthalpy - h;
     delta_s = Entropy - s;
 
-    /*--- Continue iterative process if residuals are outside tolerances ---*/
+    /*--- Continue iterative process if residuals are outside tolerances. ---*/
     if ((abs(delta_h / h) < Newton_Tolerance) && (abs(delta_s / s) < Newton_Tolerance)) {
       converged = true;
     } else {
@@ -315,20 +313,20 @@ void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
       delta_rho = (dsde_rho * delta_h - dh_de * delta_s) / determinant;
       delta_e = (-dsdrho_e * delta_h + dh_drho * delta_s) / determinant;
 
-      /*--- Update density and energy values ---*/
+      /*--- Update density and energy values. ---*/
       rho -= Newton_Relaxation * delta_rho;
       e -= Newton_Relaxation * delta_e;
     }
     Iter++;
   }
-  /*--- Calculate thermodynamic state based on converged values for density and energy ---*/
+  /*--- Calculate thermodynamic state based on converged values for density and energy. ---*/
   SetTDState_rhoe(rho, e);
 
   nIter_Newton = Iter;
 }
 
 void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
-  /*--- Setting initial values for density and energy ---*/
+  /*--- Setting initial values for density and energy. ---*/
   su2double rho = rho_start, e = e_start;
 
   bool converged = false;
@@ -342,31 +340,31 @@ void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
 
   /*--- Initiating Newton solver ---*/
   while (!converged && (Iter < MaxIter_Newton)) {
-    /*--- Determine thermodynamic state based on current density and energy*/
+    /*--- Determine thermodynamic state based on current density and energy. ---*/
     SetTDState_rhoe(rho, e);
 
-    /*--- Determine pressure and temperature residuals ---*/
+    /*--- Determine pressure and temperature residuals. ---*/
     delta_P = Pressure - P;
     delta_s = Entropy - s;
 
-    /*--- Continue iterative process if residuals are outside tolerances ---*/
+    /*--- Continue iterative process if residuals are outside tolerances. ---*/
     if ((abs(delta_P / P) < Newton_Tolerance) && (abs(delta_s / s) < Newton_Tolerance)) {
       converged = true;
     } else {
-      /*--- Compute step size for density and energy ---*/
+      /*--- Compute step size for density and energy. ---*/
       determinant = dPdrho_e * dsde_rho - dPde_rho * dsdrho_e;
 
       delta_rho = (dsde_rho * delta_P - dPde_rho * delta_s) / determinant;
       delta_e = (-dsdrho_e * delta_P + dPdrho_e * delta_s) / determinant;
 
-      /*--- Update density and energy values ---*/
+      /*--- Update density and energy values. ---*/
       rho -= Newton_Relaxation * delta_rho;
       e -= Newton_Relaxation * delta_e;
     }
     Iter++;
   }
 
-  /*--- Calculate thermodynamic state based on converged values for density and energy ---*/
+  /*--- Calculate thermodynamic state based on converged values for density and energy. ---*/
   SetTDState_rhoe(rho, e);
 
   nIter_Newton = Iter;
@@ -374,7 +372,7 @@ void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
 
 unsigned long CDataDrivenFluid::Predict_MLP(su2double rho, su2double e) {
   unsigned long exit_code = 0;
-/* Evaluate MLP collection for the given values for density and energy */
+/*--- Evaluate MLP collection for the given values for density and energy. ---*/
 #ifdef USE_MLPCPP
   MLP_inputs[idx_rho] = rho;
   MLP_inputs[idx_e] = e;
@@ -402,7 +400,7 @@ unsigned long CDataDrivenFluid::Predict_LUT(su2double rho, su2double e) {
 }
 
 void CDataDrivenFluid::Evaluate_Dataset(su2double rho, su2double e) {
-  /*--- Evaluate dataset based on regression method ---*/
+  /*--- Evaluate dataset based on regression method. ---*/
   switch (Kind_DataDriven_Method) {
     case ENUM_DATADRIVEN_METHOD::LUT:
       outside_dataset = Predict_LUT(rho, e);
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index 7dbba2bdf5e..6889e6dcda8 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -791,7 +791,6 @@ void CEulerSolver::SetNondimensionalization(CConfig *config, unsigned short iMes
   bool free_stream_temp   = (config->GetKind_FreeStreamOption() == FREESTREAM_OPTION::TEMPERATURE_FS);
   bool reynolds_init      = (config->GetKind_InitOption() == REYNOLDS);
   bool aeroelastic        = config->GetAeroelastic_Simulation();
-  bool redefine_fluidmodel = true;
 
   /*--- Set temperature via the flutter speed index ---*/
   if (aeroelastic) {
@@ -858,7 +857,6 @@ void CEulerSolver::SetNondimensionalization(CConfig *config, unsigned short iMes
     case DATADRIVEN_FLUID:
 
       auxFluidModel = new CDataDrivenFluid(config);
-      redefine_fluidmodel = false;
 
       break;
     case COOLPROP:
@@ -1058,7 +1056,7 @@ void CEulerSolver::SetNondimensionalization(CConfig *config, unsigned short iMes
   /*--- Initialize the dimensionless Fluid Model that will be used to solve the dimensionless problem ---*/
 
   /*--- Auxilary (dimensional) FluidModel no longer needed. ---*/
-  if(redefine_fluidmodel) delete auxFluidModel;
+  delete auxFluidModel;
 
   /*--- Create one final fluid model object per OpenMP thread to be able to use them in parallel.
    *    GetFluidModel() should be used to automatically access the "right" object of each thread. ---*/
@@ -1094,7 +1092,7 @@ void CEulerSolver::SetNondimensionalization(CConfig *config, unsigned short iMes
         break;
 
       case DATADRIVEN_FLUID:
-        FluidModel[thread] = auxFluidModel;
+        FluidModel[thread] = new CDataDrivenFluid(config, false);
         break;
 
       case COOLPROP:
@@ -6150,10 +6148,12 @@ void CEulerSolver::BC_Giles(CGeometry *geometry, CSolver **solver_container, CNu
       Energy_i = nodes->GetEnergy(iPoint);
       StaticEnergy_i = Energy_i - 0.5*Velocity2_i;
 
-      /*--- Set initial values for density and energy for Newton solvers in fluid model ---*/
-      su2double relax_Newton = config->GetRelaxation_DataDriven();
-      GetFluidModel()->SetInitialDensity(relax_Newton*Density_i + (1 - relax_Newton)*config->GetDensity_Init_DataDriven());
-      GetFluidModel()->SetInitialEnergy(relax_Newton*StaticEnergy_i + (1 - relax_Newton)*config->GetEnergy_Init_DataDriven());
+      if (config->GetKind_FluidModel() == DATADRIVEN_FLUID) {
+        /*--- Set initial values for density and energy for Newton solvers in fluid model ---*/
+        su2double relax_Newton = config->GetRelaxation_DataDriven();
+        GetFluidModel()->SetInitialDensity(relax_Newton*Density_i + (1 - relax_Newton)*config->GetDensity_Init_DataDriven());
+        GetFluidModel()->SetInitialEnergy(relax_Newton*StaticEnergy_i + (1 - relax_Newton)*config->GetEnergy_Init_DataDriven());
+      }
 
       GetFluidModel()->SetTDState_rhoe(Density_i, StaticEnergy_i);
 
diff --git a/SU2_CFD/src/solvers/CIncEulerSolver.cpp b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
index f3f4f557756..2310e3f4fc8 100644
--- a/SU2_CFD/src/solvers/CIncEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
@@ -500,7 +500,7 @@ void CIncEulerSolver::SetNondimensionalization(CConfig *config, unsigned short i
         break;
 
       case DATADRIVEN_FLUID:
-        fluidModel = new CDataDrivenFluid(config);
+        fluidModel = new CDataDrivenFluid(config, false);
         fluidModel->SetTDState_T(Temperature_FreeStreamND);
         break;
 
diff --git a/SU2_CFD/src/variables/CNSVariable.cpp b/SU2_CFD/src/variables/CNSVariable.cpp
index 356ec48dac7..99b7de10741 100644
--- a/SU2_CFD/src/variables/CNSVariable.cpp
+++ b/SU2_CFD/src/variables/CNSVariable.cpp
@@ -43,13 +43,6 @@ CNSVariable::CNSVariable(su2double density, const su2double *velocity, su2double
   Vortex_Tilting.resize(nPoint) = su2double(0.0);
   Max_Lambda_Visc.resize(nPoint) = su2double(0.0);
 
-  if (config->GetKind_FluidModel() == ENUM_FLUIDMODEL::DATADRIVEN_FLUID){
-    DataDrivenFluid = true;
-    DatasetExtrapolation.resize(nPoint) = 0;
-    NIterNewtonsolver.resize(nPoint) = 0;
-    FluidEntropy.resize(nPoint) = su2double(0.0);
-  }
-
 }
 
 void CNSVariable::SetRoe_Dissipation_NTS(unsigned long iPoint,
diff --git a/externals/meson b/externals/meson
index 3c655bca393..41c650a040d 160000
--- a/externals/meson
+++ b/externals/meson
@@ -1 +1 @@
-Subproject commit 3c655bca39384c3be49204491d9a8e138484d719
+Subproject commit 41c650a040d50e0912d268af7a903a9ce1456dfa
diff --git a/externals/ninja b/externals/ninja
index 2d9083b2608..52649de2c56 160000
--- a/externals/ninja
+++ b/externals/ninja
@@ -1 +1 @@
-Subproject commit 2d9083b2608bd60c31583193d321d13a81a75beb
+Subproject commit 52649de2c56b63f42bc59513d51286531c595b44
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 9f552ee934f..053fdc065f5 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -71,7 +71,7 @@ def init_submodules(
     github_repo_coolprop = "https://github.com/CoolProp/CoolProp"
     sha_version_mel = "2484cd3258ef800a10e361016cb341834ee7930b"
     github_repo_mel = "https://github.com/pcarruscag/MEL"
-    sha_version_mlpcpp = "1ff646b64de58142b5d6b9a1f15f27f08771354f"
+    sha_version_mlpcpp = "84b616acc7b76905ea12a29e08eaf4e180f35854"
     github_repo_mlpcpp = "https://github.com/EvertBunschoten/MLPCpp"
 
     medi_name = "MeDiPack"
diff --git a/subprojects/MLPCpp b/subprojects/MLPCpp
index 1ff646b64de..84b616acc7b 160000
--- a/subprojects/MLPCpp
+++ b/subprojects/MLPCpp
@@ -1 +1 @@
-Subproject commit 1ff646b64de58142b5d6b9a1f15f27f08771354f
+Subproject commit 84b616acc7b76905ea12a29e08eaf4e180f35854

From 12ce662f670f99818a4184f588b7219d47d43925 Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Thu, 6 Apr 2023 21:51:54 +0530
Subject: [PATCH 353/656] Update CLimiterDetails.hpp

Nishikwa Rp Limiter implementation
---
 SU2_CFD/include/limiters/CLimiterDetails.hpp | 147 +++++++++++++++++++
 1 file changed, 147 insertions(+)

diff --git a/SU2_CFD/include/limiters/CLimiterDetails.hpp b/SU2_CFD/include/limiters/CLimiterDetails.hpp
index 09f8b34d21e..7c66badd7b5 100644
--- a/SU2_CFD/include/limiters/CLimiterDetails.hpp
+++ b/SU2_CFD/include/limiters/CLimiterDetails.hpp
@@ -87,6 +87,36 @@ struct LimiterHelpers
     Type factor = 0.5*(1.0+dist+sin(PI_NUMBER*dist)/PI_NUMBER);
     return max(0.0, min(factor, 1.0));
   }
+
+  FORCEINLINE static Type R3Function(const Type& proj, const Type& delta, const Type& epsp)
+  {
+    Type Dp = fabs(delta); Type Dm = fabs(proj);
+    if(Dp>(2.0*Dm)) {return 1.0;}
+    else {
+	Type y = Dp*Dp*Dp + epsp;
+	Type S3 = 4.0*Dm*Dm;	    
+ 	return ((y + Dp*S3) / (y + Dm*(delta*delta+S3)));}
+  }
+
+  FORCEINLINE static Type R4Function(const Type& proj, const Type& delta, const Type& epsp)
+  {
+    Type Dp = fabs(delta); Type Dm = fabs(proj);
+    if(Dp>(2.0*Dm)) {return 1.0;}
+    else {
+	Type y = Dp*Dp*Dp*Dp + epsp;
+        Type S4 = 2.0*Dm*(Dp*Dp-2.0*Dm*(Dp-2.0*Dm));	    
+        return ((y + Dp*S4) / (y + Dm*(delta*delta*delta+S4)));}
+  }
+
+  FORCEINLINE static Type R5Function(const Type& proj, const Type& delta, const Type& epsp)
+  {
+    Type Dp = fabs(delta); Type Dm = fabs(proj);
+    if(Dp>(2.0*Dm)) {return 1.0;}
+    else {
+	Type y = Dp*Dp*Dp*Dp*Dp + epsp;
+        Type S5 = 8.0*Dm*Dm*(Dp*Dp-2.0*Dm*(Dp-Dm));    
+        return ((y + Dp*S5) / (y + Dm*(delta*delta*delta*delta+S5)));}
+  }
 };
 
 
@@ -140,6 +170,7 @@ struct CLimiterDetails<LIMITER::VENKATAKRISHNAN>
     su2double L = config.GetRefElemLength();
     su2double K = config.GetVenkat_LimiterCoeff();
     su2double eps1 = fabs(L*K);
+
     eps2 = max(eps1*eps1*eps1, LimiterHelpers<>::epsilon());
   }
 
@@ -159,6 +190,122 @@ struct CLimiterDetails<LIMITER::VENKATAKRISHNAN>
 };
 
 
+/*!
+ * \brief Nishikawa R3 limiter specialization.
+ * \ingroup FvmAlgos
+ */
+template<>
+struct CLimiterDetails<LIMITER::NISHIKAWAR3>
+{
+  su2double epsp;
+
+  /*!
+   * \brief Store the reference lenght based eps^2 parameter,
+   *        limited to a small number to avoid divisions by 0.
+   */
+  template<class... Ts>
+  inline void preprocess(CGeometry&, const CConfig& config, Ts&...)
+  {
+    su2double L = config.GetRefElemLength();
+    su2double K = config.GetVenkat_LimiterCoeff();
+    su2double eps1 = fabs(L*K);
+    epsp = max(eps1*eps1*eps1*eps1, LimiterHelpers<>::epsilon());
+
+  }
+
+  /*!
+   * \brief No geometric modification for this kind of limiter.
+   */
+  template<class... Ts>
+  inline su2double geometricFactor(Ts&...) const {return 1.0;}
+
+  /*!
+   * \brief Smooth function that disables limiting in smooth regions.
+   */
+  inline su2double limiterFunction(size_t, su2double proj, su2double delta) const
+  {
+    return LimiterHelpers<>::R3Function(proj, delta, epsp);
+  }
+};
+
+
+/*!
+ * \brief Nishikawa R4 limiter specialization.
+ * \ingroup FvmAlgos
+ */
+template<>
+struct CLimiterDetails<LIMITER::NISHIKAWAR4>
+{
+  su2double epsp;
+
+  /*!
+   * \brief Store the reference lenght based eps^2 parameter,
+   *        limited to a small number to avoid divisions by 0.
+   */
+  template<class... Ts>
+  inline void preprocess(CGeometry&, const CConfig& config, Ts&...)
+  {
+    su2double L = config.GetRefElemLength();
+    su2double K = config.GetVenkat_LimiterCoeff();
+    su2double eps1 = fabs(L*K);
+    epsp = max(eps1*eps1*eps1*eps1*eps1, LimiterHelpers<>::epsilon());
+
+  }
+
+  /*!
+   * \brief No geometric modification for this kind of limiter.
+   */
+  template<class... Ts>
+  inline su2double geometricFactor(Ts&...) const {return 1.0;}
+
+  /*!
+   * \brief Smooth function that disables limiting in smooth regions.
+   */
+  inline su2double limiterFunction(size_t, su2double proj, su2double delta) const
+  {
+    return LimiterHelpers<>::R4Function(proj, delta, epsp);
+  }
+};
+
+
+/*!
+ * \brief Nishikawa R5 limiter specialization.
+ * \ingroup FvmAlgos
+ */
+template<>
+struct CLimiterDetails<LIMITER::NISHIKAWAR5>
+{
+  su2double epsp;
+
+  /*!
+   * \brief Store the reference lenght based eps^2 parameter,
+   *        limited to a small number to avoid divisions by 0.
+   */
+  template<class... Ts>
+  inline void preprocess(CGeometry&, const CConfig& config, Ts&...)
+  {
+    su2double L = config.GetRefElemLength();
+    su2double K = config.GetVenkat_LimiterCoeff();
+    su2double eps1 = fabs(L*K);
+    epsp = max(eps1*eps1*eps1*eps1*eps1*eps1, LimiterHelpers<>::epsilon());
+
+  }
+
+  /*!
+   * \brief No geometric modification for this kind of limiter.
+   */
+  template<class... Ts>
+  inline su2double geometricFactor(Ts&...) const {return 1.0;}
+
+  /*!
+   * \brief Smooth function that disables limiting in smooth regions.
+   */
+  inline su2double limiterFunction(size_t, su2double proj, su2double delta) const
+  {
+    return LimiterHelpers<>::R5Function(proj, delta, epsp);
+  }
+};
+
 /*!
  * \brief Venkatakrishnan-Wang specialization.
  * \ingroup FvmAlgos

From 29942c559ae281c33c66a192a0e097132c327e69 Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Thu, 6 Apr 2023 21:52:49 +0530
Subject: [PATCH 354/656] Update computeLimiters.hpp

---
 SU2_CFD/include/limiters/computeLimiters.hpp | 15 +++++++++++++++
 1 file changed, 15 insertions(+)

diff --git a/SU2_CFD/include/limiters/computeLimiters.hpp b/SU2_CFD/include/limiters/computeLimiters.hpp
index 3dab84c6c07..4c2bce4de21 100644
--- a/SU2_CFD/include/limiters/computeLimiters.hpp
+++ b/SU2_CFD/include/limiters/computeLimiters.hpp
@@ -82,6 +82,21 @@ if (geometry.GetnDim() == 2) {\
       INSTANTIATE(LIMITER::VENKATAKRISHNAN);
       break;
     }
+    case LIMITER::NISHIKAWAR3:
+    {
+      INSTANTIATE(LIMITER::NISHIKAWAR3);
+      break;
+    }
+    case LIMITER::NISHIKAWAR4:
+    {
+      INSTANTIATE(LIMITER::NISHIKAWAR4);
+      break;
+    }
+    case LIMITER::NISHIKAWAR5:
+    {
+      INSTANTIATE(LIMITER::NISHIKAWAR5);
+      break;
+    }
     case LIMITER::VENKATAKRISHNAN_WANG:
     {
       INSTANTIATE(LIMITER::VENKATAKRISHNAN_WANG);

From f08c7f165fd4681caaab1fb5dab60591d0159a72 Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Thu, 6 Apr 2023 21:57:26 +0530
Subject: [PATCH 355/656] Update option_structure.hpp

---
 Common/include/option_structure.hpp | 6 ++++++
 1 file changed, 6 insertions(+)

diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index cc5b578c011..5937d806eae 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -895,6 +895,9 @@ static const MapType<std::string, ENUM_MATRIX_COLORING> MatrixColoring_Map = {
 enum class LIMITER {
   NONE                 , /*!< \brief No limiter. */
   VENKATAKRISHNAN      , /*!< \brief Slope limiter using Venkatakrisnan method (stencil formulation). */
+  NISHIKAWAR3          , /*!< \brief Slope limiter using NISHIKAWAR3 method (stencil formulation). */
+  NISHIKAWAR4          , /*!< \brief Slope limiter using NISHIKAWAR4 method (stencil formulation). */
+  NISHIKAWAR5          , /*!< \brief Slope limiter using NISHIKAWAR5 method (stencil formulation). */
   VENKATAKRISHNAN_WANG , /*!< \brief Slope limiter using Venkatakrisnan method, eps based on solution (stencil formulation). */
   BARTH_JESPERSEN      , /*!< \brief Slope limiter using Barth-Jespersen method (stencil formulation). */
   VAN_ALBADA_EDGE      , /*!< \brief Slope limiter using Van Albada method (edge formulation). */
@@ -904,6 +907,9 @@ enum class LIMITER {
 static const MapType<std::string, LIMITER> Limiter_Map = {
   MakePair("NONE", LIMITER::NONE)
   MakePair("VENKATAKRISHNAN", LIMITER::VENKATAKRISHNAN)
+  MakePair("NISHIKAWAR3", LIMITER::NISHIKAWAR3)
+  MakePair("NISHIKAWAR4", LIMITER::NISHIKAWAR4)
+  MakePair("NISHIKAWAR5", LIMITER::NISHIKAWAR5)
   MakePair("VENKATAKRISHNAN_WANG", LIMITER::VENKATAKRISHNAN_WANG)
   MakePair("BARTH_JESPERSEN", LIMITER::BARTH_JESPERSEN)
   MakePair("VAN_ALBADA_EDGE", LIMITER::VAN_ALBADA_EDGE)

From e97c62c1a01279bff70cf0ee2e657c59af61ad62 Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Thu, 6 Apr 2023 22:02:33 +0530
Subject: [PATCH 356/656] Update CConfig.cpp

---
 Common/src/CConfig.cpp | 12 ++++++++++++
 1 file changed, 12 insertions(+)

diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index ea45d2d0159..0c3fa3eb305 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -6603,6 +6603,18 @@ void CConfig::SetOutput(SU2_COMPONENT val_software, unsigned short val_izone) {
           cout << "Venkatakrishnan slope-limiting method, with constant: " << Venkat_LimiterCoeff << ".\n";
           cout << "The reference element size is: " << RefElemLength << ". " << endl;
           break;
+        case LIMITER::NISHIKAWAR3:
+          cout << "NISHIKAWAR3 slope-limiting method, with constant: " << Venkat_LimiterCoeff << ".\n";
+          cout << "The reference element size is: " << RefElemLength << ". " << endl;
+          break;
+        case LIMITER::NISHIKAWAR4:
+          cout << "NISHIKAWAR4 slope-limiting method, with constant: " << Venkat_LimiterCoeff << ".\n";
+          cout << "The reference element size is: " << RefElemLength << ". " << endl;
+          break;
+        case LIMITER::NISHIKAWAR5:
+          cout << "NISHIKAWAR5 slope-limiting method, with constant: " << Venkat_LimiterCoeff << ".\n";
+          cout << "The reference element size is: " << RefElemLength << ". " << endl;
+          break;
         case LIMITER::VENKATAKRISHNAN_WANG:
           cout << "Venkatakrishnan-Wang slope-limiting method, with constant: " << Venkat_LimiterCoeff << "." << endl;
           break;

From 0ce3213b7b037d02d525977e620c9e60a81aaf3b Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Fri, 7 Apr 2023 01:04:30 +0530
Subject: [PATCH 357/656] Update config_template.cfg

---
 config_template.cfg | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/config_template.cfg b/config_template.cfg
index 7a30a6d6fc8..d9fd6e7e6f5 100644
--- a/config_template.cfg
+++ b/config_template.cfg
@@ -1112,7 +1112,7 @@ SLOPE_LIMITER_TURB= VENKATAKRISHNAN
 MUSCL_ADJFLOW= YES
 %
 % Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
+%                SHARP_EDGES, WALL_DISTANCE, NISHIKAWAR3, NISHIKAWAR4, NISHIKAWAR5)
 SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
 %
 % Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence adjoint equations.

From 906e2f7542cee919ae839c302d860d5f8f216c29 Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Fri, 7 Apr 2023 14:46:36 +0530
Subject: [PATCH 358/656] Update CLimiterDetails.hpp

---
 SU2_CFD/include/limiters/CLimiterDetails.hpp | 6 +++---
 1 file changed, 3 insertions(+), 3 deletions(-)

diff --git a/SU2_CFD/include/limiters/CLimiterDetails.hpp b/SU2_CFD/include/limiters/CLimiterDetails.hpp
index 7c66badd7b5..6f25d1e5726 100644
--- a/SU2_CFD/include/limiters/CLimiterDetails.hpp
+++ b/SU2_CFD/include/limiters/CLimiterDetails.hpp
@@ -200,7 +200,7 @@ struct CLimiterDetails<LIMITER::NISHIKAWAR3>
   su2double epsp;
 
   /*!
-   * \brief Store the reference lenght based eps^2 parameter,
+   * \brief Store the reference lenght based eps^3 parameter,
    *        limited to a small number to avoid divisions by 0.
    */
   template<class... Ts>
@@ -239,7 +239,7 @@ struct CLimiterDetails<LIMITER::NISHIKAWAR4>
   su2double epsp;
 
   /*!
-   * \brief Store the reference lenght based eps^2 parameter,
+   * \brief Store the reference lenght based eps^4 parameter,
    *        limited to a small number to avoid divisions by 0.
    */
   template<class... Ts>
@@ -278,7 +278,7 @@ struct CLimiterDetails<LIMITER::NISHIKAWAR5>
   su2double epsp;
 
   /*!
-   * \brief Store the reference lenght based eps^2 parameter,
+   * \brief Store the reference lenght based eps^5 parameter,
    *        limited to a small number to avoid divisions by 0.
    */
   template<class... Ts>

From 59c1faf8c635c89c8283570c9562c2208df31dcb Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Fri, 7 Apr 2023 16:56:27 +0530
Subject: [PATCH 359/656] Update CLimiterDetails.hpp

Space instead of Tab
---
 SU2_CFD/include/limiters/CLimiterDetails.hpp | 10 +++++-----
 1 file changed, 5 insertions(+), 5 deletions(-)

diff --git a/SU2_CFD/include/limiters/CLimiterDetails.hpp b/SU2_CFD/include/limiters/CLimiterDetails.hpp
index 6f25d1e5726..74bde0db26d 100644
--- a/SU2_CFD/include/limiters/CLimiterDetails.hpp
+++ b/SU2_CFD/include/limiters/CLimiterDetails.hpp
@@ -93,9 +93,9 @@ struct LimiterHelpers
     Type Dp = fabs(delta); Type Dm = fabs(proj);
     if(Dp>(2.0*Dm)) {return 1.0;}
     else {
-	Type y = Dp*Dp*Dp + epsp;
-	Type S3 = 4.0*Dm*Dm;	    
- 	return ((y + Dp*S3) / (y + Dm*(delta*delta+S3)));}
+    Type y = Dp*Dp*Dp + epsp;
+    Type S3 = 4.0*Dm*Dm;	    
+        return ((y + Dp*S3) / (y + Dm*(delta*delta+S3)));}
   }
 
   FORCEINLINE static Type R4Function(const Type& proj, const Type& delta, const Type& epsp)
@@ -103,7 +103,7 @@ struct LimiterHelpers
     Type Dp = fabs(delta); Type Dm = fabs(proj);
     if(Dp>(2.0*Dm)) {return 1.0;}
     else {
-	Type y = Dp*Dp*Dp*Dp + epsp;
+        Type y = Dp*Dp*Dp*Dp + epsp;
         Type S4 = 2.0*Dm*(Dp*Dp-2.0*Dm*(Dp-2.0*Dm));	    
         return ((y + Dp*S4) / (y + Dm*(delta*delta*delta+S4)));}
   }
@@ -113,7 +113,7 @@ struct LimiterHelpers
     Type Dp = fabs(delta); Type Dm = fabs(proj);
     if(Dp>(2.0*Dm)) {return 1.0;}
     else {
-	Type y = Dp*Dp*Dp*Dp*Dp + epsp;
+        Type y = Dp*Dp*Dp*Dp*Dp + epsp;
         Type S5 = 8.0*Dm*Dm*(Dp*Dp-2.0*Dm*(Dp-Dm));    
         return ((y + Dp*S5) / (y + Dm*(delta*delta*delta*delta+S5)));}
   }

From 6524d5cad1f35b035f4e900a65271b4feffff1de Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Fri, 7 Apr 2023 16:57:33 +0530
Subject: [PATCH 360/656] Update CLimiterDetails.hpp

---
 SU2_CFD/include/limiters/CLimiterDetails.hpp | 1 -
 1 file changed, 1 deletion(-)

diff --git a/SU2_CFD/include/limiters/CLimiterDetails.hpp b/SU2_CFD/include/limiters/CLimiterDetails.hpp
index 74bde0db26d..c6c5dfc6857 100644
--- a/SU2_CFD/include/limiters/CLimiterDetails.hpp
+++ b/SU2_CFD/include/limiters/CLimiterDetails.hpp
@@ -170,7 +170,6 @@ struct CLimiterDetails<LIMITER::VENKATAKRISHNAN>
     su2double L = config.GetRefElemLength();
     su2double K = config.GetVenkat_LimiterCoeff();
     su2double eps1 = fabs(L*K);
-
     eps2 = max(eps1*eps1*eps1, LimiterHelpers<>::epsilon());
   }
 

From ce3760f945b8e4b5d9dd3caefdde84256dfd6e49 Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Fri, 7 Apr 2023 18:17:13 +0530
Subject: [PATCH 361/656] Update CLimiterDetails.hpp

---
 SU2_CFD/include/limiters/CLimiterDetails.hpp | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/SU2_CFD/include/limiters/CLimiterDetails.hpp b/SU2_CFD/include/limiters/CLimiterDetails.hpp
index c6c5dfc6857..804f9b1d69e 100644
--- a/SU2_CFD/include/limiters/CLimiterDetails.hpp
+++ b/SU2_CFD/include/limiters/CLimiterDetails.hpp
@@ -93,8 +93,8 @@ struct LimiterHelpers
     Type Dp = fabs(delta); Type Dm = fabs(proj);
     if(Dp>(2.0*Dm)) {return 1.0;}
     else {
-    Type y = Dp*Dp*Dp + epsp;
-    Type S3 = 4.0*Dm*Dm;	    
+        Type y = Dp*Dp*Dp + epsp;
+        Type S3 = 4.0*Dm*Dm;	    
         return ((y + Dp*S3) / (y + Dm*(delta*delta+S3)));}
   }
 

From 3f2e74bffbd7cc41eb6481e284b5805b1c5c9984 Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Fri, 7 Apr 2023 18:20:02 +0530
Subject: [PATCH 362/656] Update CLimiterDetails.hpp

---
 SU2_CFD/include/limiters/CLimiterDetails.hpp | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/SU2_CFD/include/limiters/CLimiterDetails.hpp b/SU2_CFD/include/limiters/CLimiterDetails.hpp
index 804f9b1d69e..0bfaf402224 100644
--- a/SU2_CFD/include/limiters/CLimiterDetails.hpp
+++ b/SU2_CFD/include/limiters/CLimiterDetails.hpp
@@ -94,7 +94,7 @@ struct LimiterHelpers
     if(Dp>(2.0*Dm)) {return 1.0;}
     else {
         Type y = Dp*Dp*Dp + epsp;
-        Type S3 = 4.0*Dm*Dm;	    
+        Type S3 = 4.0*Dm*Dm;
         return ((y + Dp*S3) / (y + Dm*(delta*delta+S3)));}
   }
 
@@ -104,7 +104,7 @@ struct LimiterHelpers
     if(Dp>(2.0*Dm)) {return 1.0;}
     else {
         Type y = Dp*Dp*Dp*Dp + epsp;
-        Type S4 = 2.0*Dm*(Dp*Dp-2.0*Dm*(Dp-2.0*Dm));	    
+        Type S4 = 2.0*Dm*(Dp*Dp-2.0*Dm*(Dp-2.0*Dm));
         return ((y + Dp*S4) / (y + Dm*(delta*delta*delta+S4)));}
   }
 

From aed5f9b32200cecd82f38691aa3afc82bc23c553 Mon Sep 17 00:00:00 2001
From: Tommaso Bellosta <tommaso.bellosta@polimi.it>
Date: Fri, 7 Apr 2023 16:17:24 +0200
Subject: [PATCH 363/656] 2 spaces indentation

---
 SU2_CFD/include/limiters/CLimiterDetails.hpp | 18 +++++++++---------
 1 file changed, 9 insertions(+), 9 deletions(-)

diff --git a/SU2_CFD/include/limiters/CLimiterDetails.hpp b/SU2_CFD/include/limiters/CLimiterDetails.hpp
index 0bfaf402224..43703bddc74 100644
--- a/SU2_CFD/include/limiters/CLimiterDetails.hpp
+++ b/SU2_CFD/include/limiters/CLimiterDetails.hpp
@@ -93,9 +93,9 @@ struct LimiterHelpers
     Type Dp = fabs(delta); Type Dm = fabs(proj);
     if(Dp>(2.0*Dm)) {return 1.0;}
     else {
-        Type y = Dp*Dp*Dp + epsp;
-        Type S3 = 4.0*Dm*Dm;
-        return ((y + Dp*S3) / (y + Dm*(delta*delta+S3)));}
+      Type y = Dp*Dp*Dp + epsp;
+      Type S3 = 4.0*Dm*Dm;
+      return ((y + Dp*S3) / (y + Dm*(delta*delta+S3)));}
   }
 
   FORCEINLINE static Type R4Function(const Type& proj, const Type& delta, const Type& epsp)
@@ -103,9 +103,9 @@ struct LimiterHelpers
     Type Dp = fabs(delta); Type Dm = fabs(proj);
     if(Dp>(2.0*Dm)) {return 1.0;}
     else {
-        Type y = Dp*Dp*Dp*Dp + epsp;
-        Type S4 = 2.0*Dm*(Dp*Dp-2.0*Dm*(Dp-2.0*Dm));
-        return ((y + Dp*S4) / (y + Dm*(delta*delta*delta+S4)));}
+      Type y = Dp*Dp*Dp*Dp + epsp;
+      Type S4 = 2.0*Dm*(Dp*Dp-2.0*Dm*(Dp-2.0*Dm));
+      return ((y + Dp*S4) / (y + Dm*(delta*delta*delta+S4)));}
   }
 
   FORCEINLINE static Type R5Function(const Type& proj, const Type& delta, const Type& epsp)
@@ -113,9 +113,9 @@ struct LimiterHelpers
     Type Dp = fabs(delta); Type Dm = fabs(proj);
     if(Dp>(2.0*Dm)) {return 1.0;}
     else {
-        Type y = Dp*Dp*Dp*Dp*Dp + epsp;
-        Type S5 = 8.0*Dm*Dm*(Dp*Dp-2.0*Dm*(Dp-Dm));    
-        return ((y + Dp*S5) / (y + Dm*(delta*delta*delta*delta+S5)));}
+      Type y = Dp*Dp*Dp*Dp*Dp + epsp;
+      Type S5 = 8.0*Dm*Dm*(Dp*Dp-2.0*Dm*(Dp-Dm));    
+      return ((y + Dp*S5) / (y + Dm*(delta*delta*delta*delta+S5)));}
   }
 };
 

From ea443c76beb7b77eaada8186d82e893c6cddd7e9 Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Fri, 7 Apr 2023 20:17:32 +0530
Subject: [PATCH 364/656] Update option_structure.hpp

---
 Common/include/option_structure.hpp | 6 +++---
 1 file changed, 3 insertions(+), 3 deletions(-)

diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index 5937d806eae..36b3b9d49ac 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -895,9 +895,9 @@ static const MapType<std::string, ENUM_MATRIX_COLORING> MatrixColoring_Map = {
 enum class LIMITER {
   NONE                 , /*!< \brief No limiter. */
   VENKATAKRISHNAN      , /*!< \brief Slope limiter using Venkatakrisnan method (stencil formulation). */
-  NISHIKAWAR3          , /*!< \brief Slope limiter using NISHIKAWAR3 method (stencil formulation). */
-  NISHIKAWAR4          , /*!< \brief Slope limiter using NISHIKAWAR4 method (stencil formulation). */
-  NISHIKAWAR5          , /*!< \brief Slope limiter using NISHIKAWAR5 method (stencil formulation). */
+  NISHIKAWAR3          , /*!< \brief Slope limiter using Nishikawa's R3 method (stencil formulation). */
+  NISHIKAWAR4          , /*!< \brief Slope limiter using Nishikawa's R4 method (stencil formulation). */
+  NISHIKAWAR5          , /*!< \brief Slope limiter using Nishikawa's R5 method (stencil formulation). */
   VENKATAKRISHNAN_WANG , /*!< \brief Slope limiter using Venkatakrisnan method, eps based on solution (stencil formulation). */
   BARTH_JESPERSEN      , /*!< \brief Slope limiter using Barth-Jespersen method (stencil formulation). */
   VAN_ALBADA_EDGE      , /*!< \brief Slope limiter using Van Albada method (edge formulation). */

From 21fcae184130d81615e5e6e4ce37a24106017a15 Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Fri, 7 Apr 2023 20:20:05 +0530
Subject: [PATCH 365/656] Update CConfig.cpp

---
 Common/src/CConfig.cpp | 6 +++---
 1 file changed, 3 insertions(+), 3 deletions(-)

diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 0c3fa3eb305..903fca5be01 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -6604,15 +6604,15 @@ void CConfig::SetOutput(SU2_COMPONENT val_software, unsigned short val_izone) {
           cout << "The reference element size is: " << RefElemLength << ". " << endl;
           break;
         case LIMITER::NISHIKAWAR3:
-          cout << "NISHIKAWAR3 slope-limiting method, with constant: " << Venkat_LimiterCoeff << ".\n";
+          cout << "Nishikawa's R3 slope-limiting method, with constant: " << Venkat_LimiterCoeff << ".\n";
           cout << "The reference element size is: " << RefElemLength << ". " << endl;
           break;
         case LIMITER::NISHIKAWAR4:
-          cout << "NISHIKAWAR4 slope-limiting method, with constant: " << Venkat_LimiterCoeff << ".\n";
+          cout << "Nishikawa's R4 slope-limiting method, with constant: " << Venkat_LimiterCoeff << ".\n";
           cout << "The reference element size is: " << RefElemLength << ". " << endl;
           break;
         case LIMITER::NISHIKAWAR5:
-          cout << "NISHIKAWAR5 slope-limiting method, with constant: " << Venkat_LimiterCoeff << ".\n";
+          cout << "Nishikawa's R5 slope-limiting method, with constant: " << Venkat_LimiterCoeff << ".\n";
           cout << "The reference element size is: " << RefElemLength << ". " << endl;
           break;
         case LIMITER::VENKATAKRISHNAN_WANG:

From 11f6041b404d38ba2bf25e9d5b634cc25f04d839 Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Fri, 7 Apr 2023 20:25:41 +0530
Subject: [PATCH 366/656] Update option_structure.hpp

---
 Common/include/option_structure.hpp | 12 ++++++------
 1 file changed, 6 insertions(+), 6 deletions(-)

diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index 36b3b9d49ac..55d508bfdee 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -895,9 +895,9 @@ static const MapType<std::string, ENUM_MATRIX_COLORING> MatrixColoring_Map = {
 enum class LIMITER {
   NONE                 , /*!< \brief No limiter. */
   VENKATAKRISHNAN      , /*!< \brief Slope limiter using Venkatakrisnan method (stencil formulation). */
-  NISHIKAWAR3          , /*!< \brief Slope limiter using Nishikawa's R3 method (stencil formulation). */
-  NISHIKAWAR4          , /*!< \brief Slope limiter using Nishikawa's R4 method (stencil formulation). */
-  NISHIKAWAR5          , /*!< \brief Slope limiter using Nishikawa's R5 method (stencil formulation). */
+  NISHIKAWA_R3          , /*!< \brief Slope limiter using Nishikawa's R3 method (stencil formulation). */
+  NISHIKAWA_R4          , /*!< \brief Slope limiter using Nishikawa's R4 method (stencil formulation). */
+  NISHIKAWA_R5          , /*!< \brief Slope limiter using Nishikawa's R5 method (stencil formulation). */
   VENKATAKRISHNAN_WANG , /*!< \brief Slope limiter using Venkatakrisnan method, eps based on solution (stencil formulation). */
   BARTH_JESPERSEN      , /*!< \brief Slope limiter using Barth-Jespersen method (stencil formulation). */
   VAN_ALBADA_EDGE      , /*!< \brief Slope limiter using Van Albada method (edge formulation). */
@@ -907,9 +907,9 @@ enum class LIMITER {
 static const MapType<std::string, LIMITER> Limiter_Map = {
   MakePair("NONE", LIMITER::NONE)
   MakePair("VENKATAKRISHNAN", LIMITER::VENKATAKRISHNAN)
-  MakePair("NISHIKAWAR3", LIMITER::NISHIKAWAR3)
-  MakePair("NISHIKAWAR4", LIMITER::NISHIKAWAR4)
-  MakePair("NISHIKAWAR5", LIMITER::NISHIKAWAR5)
+  MakePair("NISHIKAWA_R3", LIMITER::NISHIKAWA_R3)
+  MakePair("NISHIKAWA_R4", LIMITER::NISHIKAWA_R4)
+  MakePair("NISHIKAWA_R5", LIMITER::NISHIKAWA_R5)
   MakePair("VENKATAKRISHNAN_WANG", LIMITER::VENKATAKRISHNAN_WANG)
   MakePair("BARTH_JESPERSEN", LIMITER::BARTH_JESPERSEN)
   MakePair("VAN_ALBADA_EDGE", LIMITER::VAN_ALBADA_EDGE)

From 06fe7521409301a09c631100f20ca58b4d5b17ce Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Fri, 7 Apr 2023 20:26:58 +0530
Subject: [PATCH 367/656] Update CConfig.cpp

---
 Common/src/CConfig.cpp | 6 +++---
 1 file changed, 3 insertions(+), 3 deletions(-)

diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 903fca5be01..6824af9a526 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -6603,15 +6603,15 @@ void CConfig::SetOutput(SU2_COMPONENT val_software, unsigned short val_izone) {
           cout << "Venkatakrishnan slope-limiting method, with constant: " << Venkat_LimiterCoeff << ".\n";
           cout << "The reference element size is: " << RefElemLength << ". " << endl;
           break;
-        case LIMITER::NISHIKAWAR3:
+        case LIMITER::NISHIKAWA_R3:
           cout << "Nishikawa's R3 slope-limiting method, with constant: " << Venkat_LimiterCoeff << ".\n";
           cout << "The reference element size is: " << RefElemLength << ". " << endl;
           break;
-        case LIMITER::NISHIKAWAR4:
+        case LIMITER::NISHIKAWA_R4:
           cout << "Nishikawa's R4 slope-limiting method, with constant: " << Venkat_LimiterCoeff << ".\n";
           cout << "The reference element size is: " << RefElemLength << ". " << endl;
           break;
-        case LIMITER::NISHIKAWAR5:
+        case LIMITER::NISHIKAWA_R5:
           cout << "Nishikawa's R5 slope-limiting method, with constant: " << Venkat_LimiterCoeff << ".\n";
           cout << "The reference element size is: " << RefElemLength << ". " << endl;
           break;

From 04ab2fdc7847009cb9ff7dc7c411c3c81a07f0d5 Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Fri, 7 Apr 2023 20:38:22 +0530
Subject: [PATCH 368/656] Update CLimiterDetails.hpp

---
 SU2_CFD/include/limiters/CLimiterDetails.hpp | 66 ++++++++++----------
 1 file changed, 33 insertions(+), 33 deletions(-)

diff --git a/SU2_CFD/include/limiters/CLimiterDetails.hpp b/SU2_CFD/include/limiters/CLimiterDetails.hpp
index 43703bddc74..bc94151300a 100644
--- a/SU2_CFD/include/limiters/CLimiterDetails.hpp
+++ b/SU2_CFD/include/limiters/CLimiterDetails.hpp
@@ -88,34 +88,34 @@ struct LimiterHelpers
     return max(0.0, min(factor, 1.0));
   }
 
-  FORCEINLINE static Type R3Function(const Type& proj, const Type& delta, const Type& epsp)
+  FORCEINLINE static Type r3Function(const Type& proj, const Type& delta, const Type& epsp)
   {
-    Type Dp = fabs(delta); Type Dm = fabs(proj);
-    if(Dp>(2.0*Dm)) {return 1.0;}
-    else {
-      Type y = Dp*Dp*Dp + epsp;
-      Type S3 = 4.0*Dm*Dm;
-      return ((y + Dp*S3) / (y + Dm*(delta*delta+S3)));}
+    Type Dp = fabs(delta);
+    Type Dm = fabs(proj);
+    if(Dp>(2.0*Dm)) return 1.0;
+    Type y = pow(Dp, 3) + epsp;
+    Type S3 = 4.0*Dm*Dm;
+    return (y + Dp*S3) / (y + Dm*(delta*delta+S3));
   }
 
-  FORCEINLINE static Type R4Function(const Type& proj, const Type& delta, const Type& epsp)
+  FORCEINLINE static Type r4Function(const Type& proj, const Type& delta, const Type& epsp)
   {
-    Type Dp = fabs(delta); Type Dm = fabs(proj);
-    if(Dp>(2.0*Dm)) {return 1.0;}
-    else {
-      Type y = Dp*Dp*Dp*Dp + epsp;
-      Type S4 = 2.0*Dm*(Dp*Dp-2.0*Dm*(Dp-2.0*Dm));
-      return ((y + Dp*S4) / (y + Dm*(delta*delta*delta+S4)));}
+    Type Dp = fabs(delta);
+    Type Dm = fabs(proj);
+    if(Dp>(2.0*Dm)) return 1.0;
+    Type y = pow(Dp, 4) + epsp;
+    Type S4 = 2.0*Dm*(Dp*Dp-2.0*Dm*(Dp-2.0*Dm));
+    return (y + Dp*S4) / (y + Dm*(pow(delta,3)+S4));
   }
 
-  FORCEINLINE static Type R5Function(const Type& proj, const Type& delta, const Type& epsp)
+  FORCEINLINE static Type r5Function(const Type& proj, const Type& delta, const Type& epsp)
   {
-    Type Dp = fabs(delta); Type Dm = fabs(proj);
-    if(Dp>(2.0*Dm)) {return 1.0;}
-    else {
-      Type y = Dp*Dp*Dp*Dp*Dp + epsp;
-      Type S5 = 8.0*Dm*Dm*(Dp*Dp-2.0*Dm*(Dp-Dm));    
-      return ((y + Dp*S5) / (y + Dm*(delta*delta*delta*delta+S5)));}
+    Type Dp = fabs(delta);
+    Type Dm = fabs(proj);
+    if(Dp>(2.0*Dm)) return 1.0;
+    Type y = pow(Dp, 5) + epsp;
+    Type S5 = 8.0*Dm*Dm*(Dp*Dp-2.0*Dm*(Dp-Dm));
+    return (y + Dp*S5) / (y + Dm*(pow(delta,4)+S5));
   }
 };
 
@@ -190,11 +190,11 @@ struct CLimiterDetails<LIMITER::VENKATAKRISHNAN>
 
 
 /*!
- * \brief Nishikawa R3 limiter specialization.
+ * \brief Nishikawa's R3 limiter specialization.
  * \ingroup FvmAlgos
  */
 template<>
-struct CLimiterDetails<LIMITER::NISHIKAWAR3>
+struct CLimiterDetails<LIMITER::NISHIKAWA_R3>
 {
   su2double epsp;
 
@@ -208,7 +208,7 @@ struct CLimiterDetails<LIMITER::NISHIKAWAR3>
     su2double L = config.GetRefElemLength();
     su2double K = config.GetVenkat_LimiterCoeff();
     su2double eps1 = fabs(L*K);
-    epsp = max(eps1*eps1*eps1*eps1, LimiterHelpers<>::epsilon());
+    epsp = max(pow(eps1, 4), LimiterHelpers<>::epsilon());
 
   }
 
@@ -223,17 +223,17 @@ struct CLimiterDetails<LIMITER::NISHIKAWAR3>
    */
   inline su2double limiterFunction(size_t, su2double proj, su2double delta) const
   {
-    return LimiterHelpers<>::R3Function(proj, delta, epsp);
+    return LimiterHelpers<>::r3Function(proj, delta, epsp);
   }
 };
 
 
 /*!
- * \brief Nishikawa R4 limiter specialization.
+ * \brief Nishikawa's R4 limiter specialization.
  * \ingroup FvmAlgos
  */
 template<>
-struct CLimiterDetails<LIMITER::NISHIKAWAR4>
+struct CLimiterDetails<LIMITER::NISHIKAWA_R4>
 {
   su2double epsp;
 
@@ -247,7 +247,7 @@ struct CLimiterDetails<LIMITER::NISHIKAWAR4>
     su2double L = config.GetRefElemLength();
     su2double K = config.GetVenkat_LimiterCoeff();
     su2double eps1 = fabs(L*K);
-    epsp = max(eps1*eps1*eps1*eps1*eps1, LimiterHelpers<>::epsilon());
+    epsp = max(pow(eps1, 5), LimiterHelpers<>::epsilon());
 
   }
 
@@ -262,17 +262,17 @@ struct CLimiterDetails<LIMITER::NISHIKAWAR4>
    */
   inline su2double limiterFunction(size_t, su2double proj, su2double delta) const
   {
-    return LimiterHelpers<>::R4Function(proj, delta, epsp);
+    return LimiterHelpers<>::r4Function(proj, delta, epsp);
   }
 };
 
 
 /*!
- * \brief Nishikawa R5 limiter specialization.
+ * \brief Nishikawa's R5 limiter specialization.
  * \ingroup FvmAlgos
  */
 template<>
-struct CLimiterDetails<LIMITER::NISHIKAWAR5>
+struct CLimiterDetails<LIMITER::NISHIKAWA_R5>
 {
   su2double epsp;
 
@@ -286,7 +286,7 @@ struct CLimiterDetails<LIMITER::NISHIKAWAR5>
     su2double L = config.GetRefElemLength();
     su2double K = config.GetVenkat_LimiterCoeff();
     su2double eps1 = fabs(L*K);
-    epsp = max(eps1*eps1*eps1*eps1*eps1*eps1, LimiterHelpers<>::epsilon());
+    epsp = max(pow(eps1, 6), LimiterHelpers<>::epsilon());
 
   }
 
@@ -301,7 +301,7 @@ struct CLimiterDetails<LIMITER::NISHIKAWAR5>
    */
   inline su2double limiterFunction(size_t, su2double proj, su2double delta) const
   {
-    return LimiterHelpers<>::R5Function(proj, delta, epsp);
+    return LimiterHelpers<>::r5Function(proj, delta, epsp);
   }
 };
 

From b4ba0ef040c8d2472cc0836919b011eafcaef20b Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Fri, 7 Apr 2023 20:42:52 +0530
Subject: [PATCH 369/656] Update computeLimiters.hpp

---
 SU2_CFD/include/limiters/computeLimiters.hpp | 12 ++++++------
 1 file changed, 6 insertions(+), 6 deletions(-)

diff --git a/SU2_CFD/include/limiters/computeLimiters.hpp b/SU2_CFD/include/limiters/computeLimiters.hpp
index 4c2bce4de21..75918e14702 100644
--- a/SU2_CFD/include/limiters/computeLimiters.hpp
+++ b/SU2_CFD/include/limiters/computeLimiters.hpp
@@ -82,19 +82,19 @@ if (geometry.GetnDim() == 2) {\
       INSTANTIATE(LIMITER::VENKATAKRISHNAN);
       break;
     }
-    case LIMITER::NISHIKAWAR3:
+    case LIMITER::NISHIKAWA_R3:
     {
-      INSTANTIATE(LIMITER::NISHIKAWAR3);
+      INSTANTIATE(LIMITER::NISHIKAWA_R3);
       break;
     }
-    case LIMITER::NISHIKAWAR4:
+    case LIMITER::NISHIKAWA_R4:
     {
-      INSTANTIATE(LIMITER::NISHIKAWAR4);
+      INSTANTIATE(LIMITER::NISHIKAWA_R4);
       break;
     }
-    case LIMITER::NISHIKAWAR5:
+    case LIMITER::NISHIKAWA_R5:
     {
-      INSTANTIATE(LIMITER::NISHIKAWAR5);
+      INSTANTIATE(LIMITER::NISHIKAWA_R5);
       break;
     }
     case LIMITER::VENKATAKRISHNAN_WANG:

From b47245172d9aab7785abffeff924f70ade7cc068 Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Fri, 7 Apr 2023 20:44:35 +0530
Subject: [PATCH 370/656] Update config_template.cfg

---
 config_template.cfg | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/config_template.cfg b/config_template.cfg
index d9fd6e7e6f5..de994a0ce60 100644
--- a/config_template.cfg
+++ b/config_template.cfg
@@ -1112,7 +1112,7 @@ SLOPE_LIMITER_TURB= VENKATAKRISHNAN
 MUSCL_ADJFLOW= YES
 %
 % Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE, NISHIKAWAR3, NISHIKAWAR4, NISHIKAWAR5)
+%                SHARP_EDGES, WALL_DISTANCE, NISHIKAWA_R3, NISHIKAWA_R4, NISHIKAWA_R5)
 SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
 %
 % Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence adjoint equations.

From deb3a7d3ea8d672a043c30bcd68c35bda36e2adb Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Fri, 7 Apr 2023 23:04:43 +0530
Subject: [PATCH 371/656] Update CLimiterDetails.hpp

---
 SU2_CFD/include/limiters/CLimiterDetails.hpp | 3 ---
 1 file changed, 3 deletions(-)

diff --git a/SU2_CFD/include/limiters/CLimiterDetails.hpp b/SU2_CFD/include/limiters/CLimiterDetails.hpp
index bc94151300a..370831eff27 100644
--- a/SU2_CFD/include/limiters/CLimiterDetails.hpp
+++ b/SU2_CFD/include/limiters/CLimiterDetails.hpp
@@ -209,7 +209,6 @@ struct CLimiterDetails<LIMITER::NISHIKAWA_R3>
     su2double K = config.GetVenkat_LimiterCoeff();
     su2double eps1 = fabs(L*K);
     epsp = max(pow(eps1, 4), LimiterHelpers<>::epsilon());
-
   }
 
   /*!
@@ -248,7 +247,6 @@ struct CLimiterDetails<LIMITER::NISHIKAWA_R4>
     su2double K = config.GetVenkat_LimiterCoeff();
     su2double eps1 = fabs(L*K);
     epsp = max(pow(eps1, 5), LimiterHelpers<>::epsilon());
-
   }
 
   /*!
@@ -287,7 +285,6 @@ struct CLimiterDetails<LIMITER::NISHIKAWA_R5>
     su2double K = config.GetVenkat_LimiterCoeff();
     su2double eps1 = fabs(L*K);
     epsp = max(pow(eps1, 6), LimiterHelpers<>::epsilon());
-
   }
 
   /*!

From 3430b3a39b7a39ce1aa0b1936f1667d058851027 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 8 Apr 2023 10:20:09 -0700
Subject: [PATCH 372/656] fix relaxation issue and add testcase

---
 SU2_CFD/src/iteration/CFEAIteration.cpp       | 17 ++---
 .../py_wrapper/custom_load_fea/config.cfg     | 32 +++++++++
 TestCases/py_wrapper/custom_load_fea/run.py   | 70 +++++++++++++++++++
 3 files changed, 108 insertions(+), 11 deletions(-)
 create mode 100644 TestCases/py_wrapper/custom_load_fea/config.cfg
 create mode 100755 TestCases/py_wrapper/custom_load_fea/run.py

diff --git a/SU2_CFD/src/iteration/CFEAIteration.cpp b/SU2_CFD/src/iteration/CFEAIteration.cpp
index c827f28467e..8390fdab76a 100644
--- a/SU2_CFD/src/iteration/CFEAIteration.cpp
+++ b/SU2_CFD/src/iteration/CFEAIteration.cpp
@@ -184,21 +184,16 @@ void CFEAIteration::Update(COutput* output, CIntegration**** integration, CGeome
                            CNumerics****** numerics, CConfig** config, CSurfaceMovement** surface_movement,
                            CVolumetricMovement*** grid_movement, CFreeFormDefBox*** FFDBox, unsigned short val_iZone,
                            unsigned short val_iInst) {
-  const bool dynamic = (config[val_iZone]->GetTime_Domain());
-  const bool fsi = config[val_iZone]->GetFSI_Simulation();
-
   CSolver* feaSolver = solver[val_iZone][val_iInst][MESH_0][FEA_SOL];
 
   /*----------------- Update structural solver ----------------------*/
 
-  if (dynamic) {
-    integration[val_iZone][val_iInst][FEA_SOL]->SetDualTime_Solver(
-        geometry[val_iZone][val_iInst][MESH_0], solver[val_iZone][val_iInst][MESH_0][FEA_SOL], config[val_iZone],
-        MESH_0);
-
-  } else if (fsi) {
-    /*--- For FSI problems, output the relaxed result, which is the one transferred into the fluid domain (for restart
-     * purposes) ---*/
+  if (config[val_iZone]->GetTime_Domain()) {
+    integration[val_iZone][val_iInst][FEA_SOL]->SetDualTime_Solver(geometry[val_iZone][val_iInst][MESH_0], feaSolver,
+                                                                   config[val_iZone], MESH_0);
+  } else if (config[val_iZone]->GetFSI_Simulation() && config[val_iZone]->GetRelaxation()) {
+    /*--- For FSI problems with relaxation, output the relaxed result, which is the one transferred into the fluid
+     * domain (for consistent restart purposes). ---*/
     if (config[val_iZone]->GetKind_TimeIntScheme_FEA() == STRUCT_TIME_INT::NEWMARK_IMPLICIT) {
       feaSolver->ImplicitNewmark_Relaxation(geometry[val_iZone][val_iInst][MESH_0], config[val_iZone]);
     }
diff --git a/TestCases/py_wrapper/custom_load_fea/config.cfg b/TestCases/py_wrapper/custom_load_fea/config.cfg
new file mode 100644
index 00000000000..c0352190d77
--- /dev/null
+++ b/TestCases/py_wrapper/custom_load_fea/config.cfg
@@ -0,0 +1,32 @@
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+% SU2 configuration file                                                       %
+% Case description: 2D Beam with custom load via Python wrapper                %
+% File Version 7.5.1 "Blackbird"                                               %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+SOLVER= ELASTICITY
+GEOMETRIC_CONDITIONS= LARGE_DEFORMATIONS
+FORMULATION_ELASTICITY_2D= PLANE_STRESS
+
+MATERIAL_MODEL= NEO_HOOKEAN
+ELASTICITY_MODULUS= 10000
+POISSON_RATIO= 0.3
+
+MARKER_CLAMPED= ( x_minus )
+MARKER_FLUID_LOAD= ( x_plus, y_minus, y_plus )
+
+LINEAR_SOLVER= CONJUGATE_GRADIENT
+LINEAR_SOLVER_PREC= ILU
+LINEAR_SOLVER_ERROR= 1E-6
+LINEAR_SOLVER_ITER= 100
+
+MESH_FORMAT= RECTANGLE
+MESH_BOX_SIZE= ( 17, 5, 0 )
+MESH_BOX_LENGTH= ( 0.5, 0.05, 0 )
+
+OUTPUT_FILES= RESTART_ASCII, PARAVIEW
+SCREEN_OUTPUT= INNER_ITER, RMS_RES, LINSOL, VMS
+
+INNER_ITER= 20
+CONV_FIELD= REL_RMS_RTOL
+CONV_RESIDUAL_MINVAL= -6
diff --git a/TestCases/py_wrapper/custom_load_fea/run.py b/TestCases/py_wrapper/custom_load_fea/run.py
new file mode 100755
index 00000000000..c1ac289b4de
--- /dev/null
+++ b/TestCases/py_wrapper/custom_load_fea/run.py
@@ -0,0 +1,70 @@
+#!/usr/bin/env python
+
+## \file run.py
+#  \brief FEA case with custom load.
+#  \version 7.5.1 "Blackbird"
+#
+# SU2 Project Website: https://su2code.github.io
+#
+# The SU2 Project is maintained by the SU2 Foundation
+# (http://su2foundation.org)
+#
+# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
+#
+# SU2 is free software; you can redistribute it and/or
+# modify it under the terms of the GNU Lesser General Public
+# License as published by the Free Software Foundation; either
+# version 2.1 of the License, or (at your option) any later version.
+#
+# SU2 is distributed in the hope that it will be useful,
+# but WITHOUT ANY WARRANTY; without even the implied warranty of
+# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+# Lesser General Public License for more details.
+#
+# You should have received a copy of the GNU Lesser General Public
+# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+
+import pysu2
+from mpi4py import MPI
+import numpy as np
+
+def main():
+  comm = MPI.COMM_WORLD
+  rank = comm.Get_rank()
+
+  # Initialize the corresponding driver of SU2, this includes solver preprocessing.
+  try:
+    SU2Driver = pysu2.CSinglezoneDriver('config.cfg', 1, comm)
+  except TypeError as exception:
+    print('A TypeError occured in pysu2.CDriver : ', exception)
+    raise
+
+  # Get the ID of the marker we want to deform.
+  AllMarkerIDs = SU2Driver.GetMarkerIndices()
+  MarkerName = 'y_minus'
+  MarkerID = AllMarkerIDs[MarkerName] if MarkerName in AllMarkerIDs else -1
+
+  # Number of vertices on the specified marker (per rank).
+  nVertex = SU2Driver.GetNumberMarkerNodes(MarkerID) if MarkerID >= 0 else 0
+
+  # Apply a load based on the coordinates.
+  MarkerCoords = SU2Driver.MarkerCoordinates(MarkerID)
+  L = 0.5
+  dx = L / 16 # known from mesh settings in this case.
+  for iVertex in range(nVertex):
+    x = MarkerCoords(iVertex, 0)
+    nodalForce = (2 * x / L) * dx
+    # Half load due to half dx on first and last node.
+    if abs(x) < 1e-6 or abs(x - L) < 1e-6:
+      nodalForce = nodalForce / 2
+    SU2Driver.SetMarkerCustomFEALoad(MarkerID, iVertex, (0, nodalForce))
+
+  # Solve.
+  SU2Driver.StartSolver()
+
+  # Finalize the solver and exit cleanly.
+  SU2Driver.Finalize()
+
+
+if __name__ == '__main__':
+  main()

From 51c13705138aa9776399d2352adfe071e1a5e432 Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Sat, 8 Apr 2023 23:01:11 +0530
Subject: [PATCH 373/656] Inviscid supersonic flow past a ramp

---
 TestCases/euler/ramp/inv_ramp.cfg | 100 ++++++++++++++++++++++++++++++
 1 file changed, 100 insertions(+)
 create mode 100644 TestCases/euler/ramp/inv_ramp.cfg

diff --git a/TestCases/euler/ramp/inv_ramp.cfg b/TestCases/euler/ramp/inv_ramp.cfg
new file mode 100644
index 00000000000..ccc36edbcc8
--- /dev/null
+++ b/TestCases/euler/ramp/inv_ramp.cfg
@@ -0,0 +1,100 @@
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+%                                                                              %
+% SU2 configuration file                                                       %
+% Case description: Supersonic flow over a ramp in a channel (regression)     %
+% Author: Thomas D. Economon, Amit Sachdeva                                                   %
+% Institution: Stanford University                                             %
+% Date: 2023.04.08                                                             %
+% File Version 7.5.1 "Blackbird"                                               %
+%                                                                              %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
+SOLVER= EULER
+MATH_PROBLEM= DIRECT
+RESTART_SOL= NO
+
+% ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
+%
+MACH_NUMBER= 2.0
+AOA= 0.0
+SIDESLIP_ANGLE= 0.0
+FREESTREAM_PRESSURE= 100000.0
+FREESTREAM_TEMPERATURE= 300.0
+
+% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
+%
+REF_ORIGIN_MOMENT_X = 0.25
+REF_ORIGIN_MOMENT_Y = 0.00
+REF_ORIGIN_MOMENT_Z = 0.00
+REF_LENGTH= 1.0
+REF_AREA= 1.0
+
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
+MARKER_EULER= ( upper, lower )
+MARKER_SUPERSONIC_INLET= ( inlet, 300.0, 100000.0, 695.4290761824674, 0.0, 0.0 )
+MARKER_OUTLET= ( outlet, 10000.0 )
+MARKER_PLOTTING= ( lower )
+MARKER_MONITORING= ( upper, lower )
+
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
+CFL_NUMBER= 1.0
+CFL_ADAPT= YES
+CFL_ADAPT_PARAM= ( 0.9, 1.1, 1.0, 100.0, 0.8)
+RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
+ITER= 500 
+LINEAR_SOLVER= FGMRES 
+LINEAR_SOLVER_ERROR= 1E-6
+LINEAR_SOLVER_ITER= 3
+NEWTON_KRYLOV= YES
+NEWTON_KRYLOV_IPARAM= (0, 1, 1) % n0, np, ft
+NEWTON_KRYLOV_DPARAM= (0.0, 1e-20, -2.0, 1e-5) % r0, tp, rf, e
+
+% -------------------------- MULTIGRID PARAMETERS -----------------------------%
+%
+MGLEVEL= 0
+MGCYCLE= V_CYCLE
+MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
+MG_POST_SMOOTH= ( 0, 0, 0, 0 )
+MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
+MG_DAMP_RESTRICTION= 0.8
+MG_DAMP_PROLONGATION= 0.8
+
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
+CONV_NUM_METHOD_FLOW= AUSMPLUSUP
+MUSCL_FLOW= YES
+SLOPE_LIMITER_FLOW= NISHIKAWA_R5 
+VENKAT_LIMITER_COEFF= 0.5   
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
+CONV_RESIDUAL_MINVAL= -13
+CONV_STARTITER= 10
+CONV_CAUCHY_ELEMS= 100
+CONV_CAUCHY_EPS= 1E-10
+
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+%
+MESH_FILENAME= ramp_unst.su2 
+MESH_FORMAT= SU2  
+MESH_OUT_FILENAME= mesh_out.su2
+SOLUTION_FILENAME= solution_flow.dat
+SOLUTION_ADJ_FILENAME= solution_adj.dat
+TABULAR_FORMAT= CSV
+CONV_FILENAME= history
+RESTART_FILENAME= restart_flow.dat
+RESTART_ADJ_FILENAME= restart_adj.dat
+VOLUME_FILENAME= flow
+VOLUME_ADJ_FILENAME= adjoint
+GRAD_OBJFUNC_FILENAME= of_grad.dat
+SURFACE_FILENAME= surface_flow
+SURFACE_ADJ_FILENAME= surface_adjoint
+OUTPUT_WRT_FREQ= 250
+SCREEN_OUTPUT = (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
+

From 6f2424d419c60dac0ac850ea7b6adfb9a65f9b0f Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 8 Apr 2023 10:50:48 -0700
Subject: [PATCH 374/656] parallel regression

---
 TestCases/parallel_regression.py            |  9 ++++++++
 TestCases/py_wrapper/custom_load_fea/run.py | 23 +++++++++++++++++++++
 2 files changed, 32 insertions(+)

diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 1b359311076..6973bdfb075 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -1300,6 +1300,15 @@ def main():
     pywrapper_aeroelastic.unsteady  = True
     test_list.append(pywrapper_aeroelastic)
 
+    # Custom FEA load
+    pywrapper_custom_fea_load = TestCase('pywrapper_custom_fea_load')
+    pywrapper_custom_fea_load.cfg_dir = "py_wrapper/custom_load_fea"
+    pywrapper_custom_fea_load.cfg_file = "config.cfg"
+    pywrapper_custom_fea_load.test_iter = 13
+    pywrapper_custom_fea_load.test_vals = [-7.263559, -4.946814, -14.165142, 34, -6.385218, 3.2058e+02]
+    pywrapper_custom_fea_load.command = TestCase.Command("mpirun -np 2", "python", "run.py")
+    test_list.append(pywrapper_custom_fea_load)
+
     # FSI, 2d
     pywrapper_fsi2d           = TestCase('pywrapper_fsi2d')
     pywrapper_fsi2d.cfg_dir   = "fea_fsi/WallChannel_2d"
diff --git a/TestCases/py_wrapper/custom_load_fea/run.py b/TestCases/py_wrapper/custom_load_fea/run.py
index c1ac289b4de..58733c9c504 100755
--- a/TestCases/py_wrapper/custom_load_fea/run.py
+++ b/TestCases/py_wrapper/custom_load_fea/run.py
@@ -62,6 +62,29 @@ def main():
   # Solve.
   SU2Driver.StartSolver()
 
+  # Find the tip displacement.
+  MarkerName = 'x_plus'
+  MarkerID = AllMarkerIDs[MarkerName] if MarkerName in AllMarkerIDs else -1
+  nVertex = SU2Driver.GetNumberMarkerNodes(MarkerID) if MarkerID >= 0 else 0
+  MarkerCoords = SU2Driver.MarkerCoordinates(MarkerID)
+
+  SolverID = SU2Driver.GetSolverIndices()["FEA"]
+  Solution = SU2Driver.MarkerSolution(SolverID, MarkerID)
+  DispID = SU2Driver.GetFEASolutionIndices()["DISPLACEMENT_Y"]
+
+  Disp = 0
+  NodeFound = False
+  for iVertex in range(nVertex):
+    y = MarkerCoords(iVertex, 1)
+    if abs(y - 0.025) < 1e-6:
+      Disp = Solution(iVertex, DispID)
+      NodeFound = True
+
+  if NodeFound:
+    print(f"Vertical displacement of tip: {Disp}")
+    # Test the value against expected.
+    assert abs(Disp / 0.095439 - 1) < 1e-5, "Test FAILED"
+
   # Finalize the solver and exit cleanly.
   SU2Driver.Finalize()
 

From 292d48bf514001d28ed55b2005aacdf010d6e5c9 Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Sat, 8 Apr 2023 23:40:30 +0530
Subject: [PATCH 375/656] Update parallel_regression.py

Added euler/ramp case details
---
 TestCases/parallel_regression.py | 8 ++++++++
 1 file changed, 8 insertions(+)

diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 1b359311076..5e443f5a9d7 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -257,6 +257,14 @@ def main():
     ea_naca64206.test_iter = 10
     ea_naca64206.test_vals = [-1.076215, -0.391987, -0.000701, 67775.0]
     test_list.append(ea_naca64206)
+    
+    # SUPERSONIC FLOW PAST A RAMP IN A CHANNEL
+    ramp           = TestCase('ramp')
+    ramp.cfg_dir   = "euler/ramp"
+    ramp.cfg_file  = "inv_ramp.cfg"
+    ramp.test_iter = 10
+    ramp.test_vals = [-0.777734, 4.952001, -0.188418, 0.049145] #last 4 columns
+    ramp.append(ramp)
 
     ##########################
     ###  Compressible N-S  ###

From 9c8e7adc656b73146191eeee56f2f43cfc3a4a3f Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Sat, 8 Apr 2023 23:44:14 +0530
Subject: [PATCH 376/656] Update parallel_regression.py

Removed space (CodeFactor pointed issue)
---
 TestCases/parallel_regression.py | 6 +++---
 1 file changed, 3 insertions(+), 3 deletions(-)

diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 5e443f5a9d7..ebee72b906d 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -259,9 +259,9 @@ def main():
     test_list.append(ea_naca64206)
     
     # SUPERSONIC FLOW PAST A RAMP IN A CHANNEL
-    ramp           = TestCase('ramp')
-    ramp.cfg_dir   = "euler/ramp"
-    ramp.cfg_file  = "inv_ramp.cfg"
+    ramp = TestCase('ramp')
+    ramp.cfg_dir = "euler/ramp"
+    ramp.cfg_file = "inv_ramp.cfg"
     ramp.test_iter = 10
     ramp.test_vals = [-0.777734, 4.952001, -0.188418, 0.049145] #last 4 columns
     ramp.append(ramp)

From 8d6c68a5633f178a543bcc1f330d28106c3041e7 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Sat, 8 Apr 2023 12:19:24 -0700
Subject: [PATCH 377/656] Apply suggestions from code review

---
 TestCases/euler/ramp/inv_ramp.cfg | 16 +++-------------
 1 file changed, 3 insertions(+), 13 deletions(-)

diff --git a/TestCases/euler/ramp/inv_ramp.cfg b/TestCases/euler/ramp/inv_ramp.cfg
index ccc36edbcc8..6b7cbc5554b 100644
--- a/TestCases/euler/ramp/inv_ramp.cfg
+++ b/TestCases/euler/ramp/inv_ramp.cfg
@@ -1,8 +1,8 @@
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %                                                                              %
 % SU2 configuration file                                                       %
-% Case description: Supersonic flow over a ramp in a channel (regression)     %
-% Author: Thomas D. Economon, Amit Sachdeva                                                   %
+% Case description: Supersonic flow over a ramp in a channel (regression)      %
+% Author: Thomas D. Economon, Amit Sachdeva                                    %
 % Institution: Stanford University                                             %
 % Date: 2023.04.08                                                             %
 % File Version 7.5.1 "Blackbird"                                               %
@@ -13,7 +13,7 @@
 %
 SOLVER= EULER
 MATH_PROBLEM= DIRECT
-RESTART_SOL= NO
+RESTART_SOL= YES
 
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 %
@@ -45,7 +45,6 @@ NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 CFL_NUMBER= 1.0
 CFL_ADAPT= YES
 CFL_ADAPT_PARAM= ( 0.9, 1.1, 1.0, 100.0, 0.8)
-RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 ITER= 500 
 LINEAR_SOLVER= FGMRES 
 LINEAR_SOLVER_ERROR= 1E-6
@@ -53,16 +52,7 @@ LINEAR_SOLVER_ITER= 3
 NEWTON_KRYLOV= YES
 NEWTON_KRYLOV_IPARAM= (0, 1, 1) % n0, np, ft
 NEWTON_KRYLOV_DPARAM= (0.0, 1e-20, -2.0, 1e-5) % r0, tp, rf, e
-
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
 MGLEVEL= 0
-MGCYCLE= V_CYCLE
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-MG_DAMP_RESTRICTION= 0.8
-MG_DAMP_PROLONGATION= 0.8
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %

From 73d111673c401c5dc341c0e8065de03773f2ea1d Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Sun, 9 Apr 2023 01:08:41 +0530
Subject: [PATCH 378/656] Update parallel_regression.py

Updated values after restart
---
 TestCases/parallel_regression.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index ebee72b906d..8e95379965f 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -263,7 +263,7 @@ def main():
     ramp.cfg_dir = "euler/ramp"
     ramp.cfg_file = "inv_ramp.cfg"
     ramp.test_iter = 10
-    ramp.test_vals = [-0.777734, 4.952001, -0.188418, 0.049145] #last 4 columns
+    ramp.test_vals = [-13.399623, -7.788893, -0.081064, 0.056474] #last 4 columns
     ramp.append(ramp)
 
     ##########################

From 30f6c1b2833b8302e9b15a97252963c0dbd79710 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 8 Apr 2023 13:26:39 -0700
Subject: [PATCH 379/656] cleanup configs

---
 TestCases/fea_fsi/MixElemsKnowles/config.cfg               | 1 -
 TestCases/fea_fsi/SquareCyl_Beam/config.cfg                | 2 +-
 TestCases/fea_fsi/StatBeam_3d/configBeam_3d.cfg            | 3 +--
 TestCases/fea_fsi/stat_fsi/configFEA.cfg                   | 2 +-
 TestCases/fea_topology/config.cfg                          | 1 -
 TestCases/fea_topology/quick_start/settings.cfg            | 1 -
 TestCases/fea_topology/quick_start/settings_compliance.cfg | 1 -
 TestCases/fea_topology/quick_start/settings_volfrac.cfg    | 1 -
 8 files changed, 3 insertions(+), 9 deletions(-)

diff --git a/TestCases/fea_fsi/MixElemsKnowles/config.cfg b/TestCases/fea_fsi/MixElemsKnowles/config.cfg
index 94e5328e4b9..ffa4573286a 100644
--- a/TestCases/fea_fsi/MixElemsKnowles/config.cfg
+++ b/TestCases/fea_fsi/MixElemsKnowles/config.cfg
@@ -11,7 +11,6 @@
 % Physics
 SOLVER= ELASTICITY
 MATH_PROBLEM= DIRECT
-DYNAMIC_ANALYSIS= NO
 %
 % Optimization
 OBJECTIVE_FUNCTION= REFERENCE_NODE
diff --git a/TestCases/fea_fsi/SquareCyl_Beam/config.cfg b/TestCases/fea_fsi/SquareCyl_Beam/config.cfg
index ab740fe4255..d4033e5f4b1 100644
--- a/TestCases/fea_fsi/SquareCyl_Beam/config.cfg
+++ b/TestCases/fea_fsi/SquareCyl_Beam/config.cfg
@@ -67,7 +67,7 @@ NONLINEAR_FEM_INT_ITER = 20
 
 % -------------------------- DYNAMIC SIMULATION -------------------------------%
 %
-DYNAMIC_ANALYSIS= YES
+TIME_DOMAIN= YES
 TIME_DISCRE_FEA= NEWMARK_IMPLICIT
 NEWMARK_BETA=0.2601
 NEWMARK_GAMMA=0.52
diff --git a/TestCases/fea_fsi/StatBeam_3d/configBeam_3d.cfg b/TestCases/fea_fsi/StatBeam_3d/configBeam_3d.cfg
index 1aee4275ed5..e3b82a9e601 100644
--- a/TestCases/fea_fsi/StatBeam_3d/configBeam_3d.cfg
+++ b/TestCases/fea_fsi/StatBeam_3d/configBeam_3d.cfg
@@ -6,7 +6,7 @@
 % Date: 2016.02.01                                                             %
 % File Version 7.5.1 "Blackbird"                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-                     
+
 SOLVER= ELASTICITY
 MATH_PROBLEM= DIRECT
 GEOMETRIC_CONDITIONS= SMALL_DEFORMATIONS
@@ -15,7 +15,6 @@ MESH_FILENAME= meshBeam_3d.su2
 ELASTICITY_MODULUS=3E7
 POISSON_RATIO=0.3
 MATERIAL_DENSITY=7854
-DYNAMIC_ANALYSIS= NO
 MARKER_CLAMPED = ( left , right )
 MARKER_PRESSURE= ( lower, 0 , symleft, 0, symright, 0)
 MARKER_LOAD= ( upper, 1, 1000, 0, -1, 0)
diff --git a/TestCases/fea_fsi/stat_fsi/configFEA.cfg b/TestCases/fea_fsi/stat_fsi/configFEA.cfg
index 3ce2b13322c..0f4e66ad1f7 100755
--- a/TestCases/fea_fsi/stat_fsi/configFEA.cfg
+++ b/TestCases/fea_fsi/stat_fsi/configFEA.cfg
@@ -59,7 +59,7 @@ FORMULATION_ELASTICITY_2D = PLANE_STRAIN
 POISSON_RATIO=0.4
 
 % -------------------------- DYNAMIC SIMULATION -------------------------------%
-DYNAMIC_ANALYSIS= NO
+TIME_DOMAIN= NO
 TIME_DISCRE_FEA= NEWMARK_IMPLICIT
 
 % -------------------------- STRUCTURAL SOLVER --------------------------------%
diff --git a/TestCases/fea_topology/config.cfg b/TestCases/fea_topology/config.cfg
index cf12a17353a..021e878895d 100644
--- a/TestCases/fea_topology/config.cfg
+++ b/TestCases/fea_topology/config.cfg
@@ -66,7 +66,6 @@ ITER=1
 % Physics
 SOLVER= ELASTICITY
 MATH_PROBLEM= DISCRETE_ADJOINT
-DYNAMIC_ANALYSIS= NO
 RESTART_SOL= NO
 %
 SOLUTION_FILENAME=solution_structure.dat
diff --git a/TestCases/fea_topology/quick_start/settings.cfg b/TestCases/fea_topology/quick_start/settings.cfg
index 44d8b3eafaf..8a0edb1041a 100644
--- a/TestCases/fea_topology/quick_start/settings.cfg
+++ b/TestCases/fea_topology/quick_start/settings.cfg
@@ -1,7 +1,6 @@
 % Physics
 SOLVER= ELASTICITY
 MATH_PROBLEM= DIRECT
-DYNAMIC_ANALYSIS= NO
 %
 ITER= 1
 %
diff --git a/TestCases/fea_topology/quick_start/settings_compliance.cfg b/TestCases/fea_topology/quick_start/settings_compliance.cfg
index d9cf275df75..57241e0615f 100644
--- a/TestCases/fea_topology/quick_start/settings_compliance.cfg
+++ b/TestCases/fea_topology/quick_start/settings_compliance.cfg
@@ -1,7 +1,6 @@
 % Physics
 SOLVER= ELASTICITY
 MATH_PROBLEM= DISCRETE_ADJOINT
-DYNAMIC_ANALYSIS= NO
 %
 ITER= 1
 %
diff --git a/TestCases/fea_topology/quick_start/settings_volfrac.cfg b/TestCases/fea_topology/quick_start/settings_volfrac.cfg
index a3ec2ebc3cb..c7da2fe14f5 100644
--- a/TestCases/fea_topology/quick_start/settings_volfrac.cfg
+++ b/TestCases/fea_topology/quick_start/settings_volfrac.cfg
@@ -1,7 +1,6 @@
 % Physics
 SOLVER= ELASTICITY
 MATH_PROBLEM= DISCRETE_ADJOINT
-DYNAMIC_ANALYSIS= NO
 %
 ITER= 1
 %

From 48f467908ff9be7798084f5709197b4b39dc71ba Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Sat, 8 Apr 2023 19:21:34 -0700
Subject: [PATCH 380/656] Update Common/src/CConfig.cpp

---
 Common/src/CConfig.cpp | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index bf936e6e8fc..ff9348ceede 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -8841,8 +8841,8 @@ const su2double* CConfig::GetInlet_TurbVal(const string& val_marker) const {
   }
   if (Kind_Turb_Model == TURB_MODEL::SST) {
     return TurbIntensityAndViscRatioFreeStream;
-  }     return &NuFactor_FreeStream;
-
+  }
+  return &NuFactor_FreeStream;
 }
 
 su2double CConfig::GetOutlet_Pressure(const string& val_marker) const {

From 390e46c8ad66cd3baaefa61c8ad96b9a9907b490 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Sat, 8 Apr 2023 19:24:22 -0700
Subject: [PATCH 381/656] Update TestCases/parallel_regression.py

---
 TestCases/parallel_regression.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 8e95379965f..f33d967e22a 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -264,7 +264,7 @@ def main():
     ramp.cfg_file = "inv_ramp.cfg"
     ramp.test_iter = 10
     ramp.test_vals = [-13.399623, -7.788893, -0.081064, 0.056474] #last 4 columns
-    ramp.append(ramp)
+    test_list.append(ramp)
 
     ##########################
     ###  Compressible N-S  ###

From 610fa17e7b2415dad7deb7078ac28beb272908db Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 8 Apr 2023 19:41:20 -0700
Subject: [PATCH 382/656] fix testcases

---
 .../fea_fsi/DynBeam_2d/configBeam_2d.cfg      |  3 +-
 TestCases/parallel_regression.py              |  2 +-
 TestCases/py_wrapper/custom_load_fea/run.py   | 46 +++++++++----------
 3 files changed, 25 insertions(+), 26 deletions(-)

diff --git a/TestCases/fea_fsi/DynBeam_2d/configBeam_2d.cfg b/TestCases/fea_fsi/DynBeam_2d/configBeam_2d.cfg
index 1df1677212b..1303f5457be 100644
--- a/TestCases/fea_fsi/DynBeam_2d/configBeam_2d.cfg
+++ b/TestCases/fea_fsi/DynBeam_2d/configBeam_2d.cfg
@@ -6,7 +6,7 @@
 % Date: 2016.02.01                                                             %
 % File Version 7.5.1 "Blackbird"                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-                    
+
 SOLVER= ELASTICITY
 MATH_PROBLEM= DIRECT
 GEOMETRIC_CONDITIONS= LARGE_DEFORMATIONS
@@ -41,4 +41,3 @@ RESTART_FILENAME= restart_beam.dat
 SOLUTION_FILENAME= solution_beam.dat
 OUTPUT_WRT_FREQ= 1
 OUTPUT_FILES= RESTART_ASCII, PARAVIEW
-SCREEN_OUTPUT= CUR_TIME, INNER_ITER, RMS_RES, LINSOL
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 6973bdfb075..4154ebc1a99 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -1305,7 +1305,7 @@ def main():
     pywrapper_custom_fea_load.cfg_dir = "py_wrapper/custom_load_fea"
     pywrapper_custom_fea_load.cfg_file = "config.cfg"
     pywrapper_custom_fea_load.test_iter = 13
-    pywrapper_custom_fea_load.test_vals = [-7.263559, -4.946814, -14.165142, 34, -6.385218, 3.2058e+02]
+    pywrapper_custom_fea_load.test_vals = [-7.263559, -4.946814, -14.165142, 34, -6.380144, 320.58]
     pywrapper_custom_fea_load.command = TestCase.Command("mpirun -np 2", "python", "run.py")
     test_list.append(pywrapper_custom_fea_load)
 
diff --git a/TestCases/py_wrapper/custom_load_fea/run.py b/TestCases/py_wrapper/custom_load_fea/run.py
index 58733c9c504..24881ef85df 100755
--- a/TestCases/py_wrapper/custom_load_fea/run.py
+++ b/TestCases/py_wrapper/custom_load_fea/run.py
@@ -26,11 +26,9 @@
 
 import pysu2
 from mpi4py import MPI
-import numpy as np
 
 def main():
   comm = MPI.COMM_WORLD
-  rank = comm.Get_rank()
 
   # Initialize the corresponding driver of SU2, this includes solver preprocessing.
   try:
@@ -48,16 +46,17 @@ def main():
   nVertex = SU2Driver.GetNumberMarkerNodes(MarkerID) if MarkerID >= 0 else 0
 
   # Apply a load based on the coordinates.
-  MarkerCoords = SU2Driver.MarkerCoordinates(MarkerID)
-  L = 0.5
-  dx = L / 16 # known from mesh settings in this case.
-  for iVertex in range(nVertex):
-    x = MarkerCoords(iVertex, 0)
-    nodalForce = (2 * x / L) * dx
-    # Half load due to half dx on first and last node.
-    if abs(x) < 1e-6 or abs(x - L) < 1e-6:
-      nodalForce = nodalForce / 2
-    SU2Driver.SetMarkerCustomFEALoad(MarkerID, iVertex, (0, nodalForce))
+  if nVertex > 0:
+    MarkerCoords = SU2Driver.MarkerCoordinates(MarkerID)
+    L = 0.5
+    dx = L / 16 # known from mesh settings in this case.
+    for iVertex in range(nVertex):
+      x = MarkerCoords(iVertex, 0)
+      nodalForce = (2 * x / L) * dx
+      # Half load due to half dx on first and last node.
+      if abs(x) < 1e-6 or abs(x - L) < 1e-6:
+        nodalForce = nodalForce / 2
+      SU2Driver.SetMarkerCustomFEALoad(MarkerID, iVertex, (0, nodalForce))
 
   # Solve.
   SU2Driver.StartSolver()
@@ -66,19 +65,20 @@ def main():
   MarkerName = 'x_plus'
   MarkerID = AllMarkerIDs[MarkerName] if MarkerName in AllMarkerIDs else -1
   nVertex = SU2Driver.GetNumberMarkerNodes(MarkerID) if MarkerID >= 0 else 0
-  MarkerCoords = SU2Driver.MarkerCoordinates(MarkerID)
-
-  SolverID = SU2Driver.GetSolverIndices()["FEA"]
-  Solution = SU2Driver.MarkerSolution(SolverID, MarkerID)
-  DispID = SU2Driver.GetFEASolutionIndices()["DISPLACEMENT_Y"]
-
   Disp = 0
   NodeFound = False
-  for iVertex in range(nVertex):
-    y = MarkerCoords(iVertex, 1)
-    if abs(y - 0.025) < 1e-6:
-      Disp = Solution(iVertex, DispID)
-      NodeFound = True
+
+  if nVertex > 0:
+    MarkerCoords = SU2Driver.MarkerCoordinates(MarkerID)
+    SolverID = SU2Driver.GetSolverIndices()["FEA"]
+    Solution = SU2Driver.MarkerSolution(SolverID, MarkerID)
+    DispID = SU2Driver.GetFEASolutionIndices()["DISPLACEMENT_Y"]
+
+    for iVertex in range(nVertex):
+      y = MarkerCoords(iVertex, 1)
+      if abs(y - 0.025) < 1e-6:
+        Disp = Solution(iVertex, DispID)
+        NodeFound = True
 
   if NodeFound:
     print(f"Vertical displacement of tip: {Disp}")

From b8bdc5fd55347385b0760bed97278b7c4bf4b8ee Mon Sep 17 00:00:00 2001
From: aeroamit <aero_amit@hotmail.com>
Date: Sun, 9 Apr 2023 09:35:22 +0530
Subject: [PATCH 383/656] Update inv_ramp.cfg

Changed SOLUTION_FILENAME= restart_flow.dat
---
 TestCases/euler/ramp/inv_ramp.cfg | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/TestCases/euler/ramp/inv_ramp.cfg b/TestCases/euler/ramp/inv_ramp.cfg
index 6b7cbc5554b..1ea26b65e2f 100644
--- a/TestCases/euler/ramp/inv_ramp.cfg
+++ b/TestCases/euler/ramp/inv_ramp.cfg
@@ -74,11 +74,11 @@ CONV_CAUCHY_EPS= 1E-10
 MESH_FILENAME= ramp_unst.su2 
 MESH_FORMAT= SU2  
 MESH_OUT_FILENAME= mesh_out.su2
-SOLUTION_FILENAME= solution_flow.dat
+SOLUTION_FILENAME= restart_flow.dat
 SOLUTION_ADJ_FILENAME= solution_adj.dat
 TABULAR_FORMAT= CSV
 CONV_FILENAME= history
-RESTART_FILENAME= restart_flow.dat
+RESTART_FILENAME= restart_flowrun.dat
 RESTART_ADJ_FILENAME= restart_adj.dat
 VOLUME_FILENAME= flow
 VOLUME_ADJ_FILENAME= adjoint

From 6b6fccb26f8ddf23af96a20ab5b9f28025d13011 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 9 Apr 2023 18:54:32 -0700
Subject: [PATCH 384/656] do not call Newmark relaxation also for transient
 when relaxation is off

---
 SU2_CFD/include/solvers/CFEASolver.hpp        | 23 ++-----------------
 SU2_CFD/include/solvers/CSolver.hpp           | 21 +----------------
 .../integration/CStructuralIntegration.cpp    | 13 +++--------
 SU2_CFD/src/solvers/CFEASolver.cpp            | 14 +++++------
 4 files changed, 13 insertions(+), 58 deletions(-)

diff --git a/SU2_CFD/include/solvers/CFEASolver.hpp b/SU2_CFD/include/solvers/CFEASolver.hpp
index ed0aee60236..86eb0813e6a 100644
--- a/SU2_CFD/include/solvers/CFEASolver.hpp
+++ b/SU2_CFD/include/solvers/CFEASolver.hpp
@@ -682,28 +682,9 @@ class CFEASolver : public CFEASolverBase {
   inline su2double GetFSI_ConvValue(unsigned short val_index) const final { return FSI_Conv[val_index]; }
 
   /*!
-   * \brief Retrieve the value of the dynamic Aitken relaxation factor.
-   * \return Value of the dynamic Aitken relaxation factor.
+   * \brief Store the value of the last Aitken relaxation factor in the current time step.
    */
-  inline su2double GetWAitken_Dyn(void) const final { return WAitken_Dyn; }
-
-  /*!
-   * \brief Retrieve the value of the last Aitken relaxation factor in the previous time step.
-   * \return Value of the last Aitken relaxation factor in the previous time step.
-   */
-  inline su2double GetWAitken_Dyn_tn1(void) const final { return WAitken_Dyn_tn1; }
-
-  /*!
-   * \brief Set the value of the dynamic Aitken relaxation factor
-   * \param[in] Value of the dynamic Aitken relaxation factor
-   */
-  inline void SetWAitken_Dyn(su2double waitk) final { WAitken_Dyn = waitk; }
-
-  /*!
-   * \brief Set the value of the last Aitken relaxation factor in the current time step.
-   * \param[in] Value of the last Aitken relaxation factor in the current time step.
-   */
-  inline void SetWAitken_Dyn_tn1(su2double waitk_tn1) final { WAitken_Dyn_tn1 = waitk_tn1; }
+  inline void SetWAitken_Dyn_tn1() final { WAitken_Dyn_tn1 = WAitken_Dyn; }
 
   /*!
    * \brief Set the value of the load increment for nonlinear structural analysis
diff --git a/SU2_CFD/include/solvers/CSolver.hpp b/SU2_CFD/include/solvers/CSolver.hpp
index cdfa1946151..892552859b0 100644
--- a/SU2_CFD/include/solvers/CSolver.hpp
+++ b/SU2_CFD/include/solvers/CSolver.hpp
@@ -3698,27 +3698,8 @@ class CSolver {
 
   /*!
    * \brief A virtual member.
-   * \return Value of the dynamic Aitken relaxation factor
    */
-  inline virtual su2double GetWAitken_Dyn(void) const { return 0; }
-
-  /*!
-   * \brief A virtual member.
-   * \return Value of the last Aitken relaxation factor in the previous time step.
-   */
-  inline virtual su2double GetWAitken_Dyn_tn1(void) const { return 0; }
-
-  /*!
-   * \brief A virtual member.
-   * \param[in] Value of the dynamic Aitken relaxation factor
-   */
-  inline virtual void SetWAitken_Dyn(su2double waitk) {  }
-
-  /*!
-   * \brief A virtual member.
-   * \param[in] Value of the last Aitken relaxation factor in the previous time step.
-   */
-  inline virtual void SetWAitken_Dyn_tn1(su2double waitk_tn1) {  }
+  inline virtual void SetWAitken_Dyn_tn1() {  }
 
   /*!
    * \brief A virtual member.
diff --git a/SU2_CFD/src/integration/CStructuralIntegration.cpp b/SU2_CFD/src/integration/CStructuralIntegration.cpp
index 1dd5573923c..04b207f6fa0 100644
--- a/SU2_CFD/src/integration/CStructuralIntegration.cpp
+++ b/SU2_CFD/src/integration/CStructuralIntegration.cpp
@@ -193,7 +193,7 @@ void CStructuralIntegration::Time_Integration_FEM(CGeometry *geometry, CSolver *
 
 void CStructuralIntegration::SetDualTime_Solver(const CGeometry *geometry, CSolver *solver, const CConfig *config, unsigned short iMesh) {
 
-  bool fsi = config->GetFSI_Simulation();
+  const bool fsi = config->GetFSI_Simulation();
 
   /*--- Update the solution according to the integration scheme used ---*/
 
@@ -201,7 +201,7 @@ void CStructuralIntegration::SetDualTime_Solver(const CGeometry *geometry, CSolv
     case (STRUCT_TIME_INT::CD_EXPLICIT):
       break;
     case (STRUCT_TIME_INT::NEWMARK_IMPLICIT):
-      if (fsi) solver->ImplicitNewmark_Relaxation(geometry, config);
+      if (fsi && config->GetRelaxation()) solver->ImplicitNewmark_Relaxation(geometry, config);
       break;
     case (STRUCT_TIME_INT::GENERALIZED_ALPHA):
       solver->GeneralizedAlpha_UpdateSolution(geometry, config);
@@ -215,12 +215,5 @@ void CStructuralIntegration::SetDualTime_Solver(const CGeometry *geometry, CSolv
 
   /*--- If FSI problem, save the last Aitken relaxation parameter of the previous time step ---*/
 
-  if (fsi) {
-
-    su2double WAitk=0.0;
-
-    WAitk = solver->GetWAitken_Dyn();
-    solver->SetWAitken_Dyn_tn1(WAitk);
-
-  }
+  if (fsi) solver->SetWAitken_Dyn_tn1();
 }
diff --git a/SU2_CFD/src/solvers/CFEASolver.cpp b/SU2_CFD/src/solvers/CFEASolver.cpp
index c7a1b4b08e4..74870622ea0 100644
--- a/SU2_CFD/src/solvers/CFEASolver.cpp
+++ b/SU2_CFD/src/solvers/CFEASolver.cpp
@@ -2576,26 +2576,26 @@ void CFEASolver::ComputeAitken_Coefficient(CGeometry *geometry, const CConfig *c
 
   if (RelaxMethod_FSI == BGS_RELAXATION::NONE) {
 
-    SetWAitken_Dyn(1.0);
+    WAitken_Dyn = 1.0;
 
   }
   else if (RelaxMethod_FSI == BGS_RELAXATION::FIXED) {
 
-    SetWAitken_Dyn(config->GetAitkenStatRelax());
+    WAitken_Dyn = config->GetAitkenStatRelax();
 
   }
   else if (RelaxMethod_FSI == BGS_RELAXATION::AITKEN) {
 
     if (iOuterIter == 0) {
 
-      WAitkDyn_tn1 = GetWAitken_Dyn_tn1();
+      WAitkDyn_tn1 = WAitken_Dyn_tn1;
       WAitkDyn_Max = config->GetAitkenDynMaxInit();
       WAitkDyn_Min = config->GetAitkenDynMinInit();
 
       WAitkDyn = min(WAitkDyn_tn1, WAitkDyn_Max);
       WAitkDyn = max(WAitkDyn, WAitkDyn_Min);
 
-      SetWAitken_Dyn(WAitkDyn);
+      WAitken_Dyn = WAitkDyn;
 
     }
     else {
@@ -2626,7 +2626,7 @@ void CFEASolver::ComputeAitken_Coefficient(CGeometry *geometry, const CConfig *c
       SU2_MPI::Allreduce(&sbuf_numAitk, &rbuf_numAitk, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
       SU2_MPI::Allreduce(&sbuf_denAitk, &rbuf_denAitk, 1, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
 
-      WAitkDyn = GetWAitken_Dyn();
+      WAitkDyn = WAitken_Dyn;
 
       if (rbuf_denAitk > EPS) {
         WAitkDyn = - 1.0 * WAitkDyn * rbuf_numAitk / rbuf_denAitk ;
@@ -2635,7 +2635,7 @@ void CFEASolver::ComputeAitken_Coefficient(CGeometry *geometry, const CConfig *c
       WAitkDyn = max(WAitkDyn, 0.1);
       WAitkDyn = min(WAitkDyn, 1.0);
 
-      SetWAitken_Dyn(WAitkDyn);
+      WAitken_Dyn = WAitkDyn;
 
     }
 
@@ -2648,7 +2648,7 @@ void CFEASolver::ComputeAitken_Coefficient(CGeometry *geometry, const CConfig *c
 
 void CFEASolver::SetAitken_Relaxation(CGeometry *geometry, const CConfig *config) {
 
-  const su2double WAitken = GetWAitken_Dyn();
+  const su2double WAitken = WAitken_Dyn;
   const bool dynamic = config->GetTime_Domain();
 
   /*--- To nPoint to avoid communication. ---*/

From 0acec215cdb9eb3248126020799c288daee8ab24 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Mon, 10 Apr 2023 09:15:02 -0700
Subject: [PATCH 385/656] cleanup limiter docs

---
 config_template.cfg | 31 ++++++++++++++++---------------
 1 file changed, 16 insertions(+), 15 deletions(-)

diff --git a/config_template.cfg b/config_template.cfg
index de994a0ce60..a99ec1a8922 100644
--- a/config_template.cfg
+++ b/config_template.cfg
@@ -733,7 +733,7 @@ CONV_NUM_METHOD_SPECIES= SCALAR_UPWIND
 % Required for 2nd order upwind schemes (NO, YES)
 MUSCL_SPECIES= NO
 %
-% Slope limiter for species equations (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG, BARTH_JESPERSEN, VAN_ALBADA_EDGE)
+% Slope limiter for species equations (same as SLOPE_LIMITER_TURB)
 SLOPE_LIMITER_SPECIES = NONE
 %
 % Time discretization for species equations (EULER_IMPLICIT, EULER_EXPLICIT)
@@ -1095,36 +1095,37 @@ CUSTOM_OBJFUNC= 'DRAG + 10 * pow(fmax(0.4-LIFT, 0), 2)'
 %           Required for 2nd order upwind schemes (NO, YES)
 MUSCL_FLOW= YES
 %
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG, BARTH_JESPERSEN, VAN_ALBADA_EDGE)
-%
+% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
+%                NISHIKAWA_R3, NISHIKAWA_R4, NISHIKAWA_R5)
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 %
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
+% Same as MUSCL_FLOW but for turbulence.
+%
 MUSCL_TURB= NO
 %
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG, BARTH_JESPERSEN)
+% Slope limiter (same as SLOPE_LIMITER_FLOW except VAN_ALBADA_EDGE)
 %
 SLOPE_LIMITER_TURB= VENKATAKRISHNAN
 %
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
+% Same as MUSCL_FLOW but for the continuous adjoint equations.
+%
 MUSCL_ADJFLOW= YES
 %
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE, NISHIKAWA_R3, NISHIKAWA_R4, NISHIKAWA_R5)
+% Slope limiter (same as SLOPE_LIMITER_FLOW plus SHARP_EDGES, WALL_DISTANCE)
+%
 SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
 %
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence adjoint equations.
-%           Required for 2nd order upwind schemes (NO, YES)
+% Same as MUSCL_FLOW but for continuous adjoint turbulence equations.
+%
 MUSCL_ADJTURB= NO
 %
 % Slope limiter (see SLOPE_LIMITER_ADJFLOW)
+%
 SLOPE_LIMITER_ADJTURB= VENKATAKRISHNAN
 %
-% Coefficient for the Venkat's limiter (upwind scheme). A larger values decrease
-%             the extent of limiting, values approaching zero cause
-%             lower-order approximation to the solution (0.05 by default)
+% Coefficient for Venkatakrishnan-type limiters (upwind scheme).
+% A larger value decreases the extent of limiting, values approaching zero
+% cause lower-order approximation to the solution (0.05 by default)
 VENKAT_LIMITER_COEFF= 0.05
 %
 % Reference coefficient for detecting sharp edges (3.0 by default).

From 96ca12fe124f47af4d2185f16d2de5d5150683e4 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 11 Apr 2023 10:31:30 +0200
Subject: [PATCH 386/656] Updated submodules, pulled develop, updated test case
 for datadriven nozzle

---
 .github/workflows/regression.yml              |   2 +-
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp    |   1 +
 TestCases/nicf/datadriven/MLP_air.mlp         | 138 ++++++++++++++++++
 .../nicf/datadriven/datadriven_nozzle.cfg     |   2 +-
 config_template.cfg                           |   1 +
 meson_scripts/init.py                         |   2 +-
 subprojects/MLPCpp                            |   2 +-
 7 files changed, 144 insertions(+), 4 deletions(-)
 create mode 100644 TestCases/nicf/datadriven/MLP_air.mlp

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index edce87f05e8..c1a9068a6b5 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t feature_multilayer_perceptron -c feature_multilayer_perceptron -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t feature_multilayer_perceptron -c develop -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index fff28602b67..e0faeb132d6 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -31,6 +31,7 @@
 #include <vector>
 #include "../../../Common/include/containers/CLookUpTable.hpp"
 #if defined(HAVE_MLPCPP)
+#define MLP_CUSTOM_TYPE su2double
 #include "../../../subprojects/MLPCpp/include/CLookUp_ANN.hpp"
 #define USE_MLPCPP
 #endif
diff --git a/TestCases/nicf/datadriven/MLP_air.mlp b/TestCases/nicf/datadriven/MLP_air.mlp
new file mode 100644
index 00000000000..e28657819cf
--- /dev/null
+++ b/TestCases/nicf/datadriven/MLP_air.mlp
@@ -0,0 +1,138 @@
+<header>
+
+[number of layers]
+4
+
+[neurons per layer]
+2
+50
+30
+6
+
+[activation function]
+linear
+swish
+swish
+linear
+
+[input names]
+Density
+Energy
+
+[input normalization]
++2.8103800000000001e-01	+2.7297899999999998e+01
++1.7995600000000000e+05	+4.4831800000000000e+05
+
+[output names]
+s
+dsde_rho
+dsdrho_e
+d2sde2
+d2sdedrho
+d2sdrho2
+
+[output normalization]
++5.7472900000000000e+03	+7.7785200000000004e+03
++1.6686100000000001e-03	+4.0000000000000001e-03
+-1.0563199999999999e+03	-1.0714800000000000e+01
+-2.1545900000000001e-08	-3.5737000000000002e-09
+-4.2049399999999996e-06	-4.9376699999999998e-07
++3.9691700000000002e-01	+3.7578600000000001e+03
+
+</header>
+
+[weights per layer]
+<layer>
+-8.7661929428577423e-03	-3.4266726970672607e+00	-1.1285322718322277e-02	-4.4609041213989258e+00	-6.2620453536510468e-03	-8.7659519910812378e-01	+8.1317527219653130e-03	+1.0037513971328735e+00	+5.1442968845367432e-01	-3.8515377044677734e+01	+3.0268053524196148e-03	-3.5439160466194153e-01	-5.6422060728073120e-01	-8.2498639822006226e-03	-1.1617618612945080e-02	+9.0869655832648277e-03	-9.9546900019049644e-03	+1.6827103495597839e-01	-2.7841054916381836e+01	-8.8479537516832352e-03	-3.9593321084976196e-01	+9.5181297510862350e-03	-2.3468191921710968e-01	-8.5755866020917892e-03	-9.0520847588777542e-03	+6.8784481287002563e-01	-3.5454284667968750e+01	-3.9844226837158203e+00	+4.1778454184532166e-01	-1.3072727015241981e-03	-1.0021785274147987e-02	-8.5394643247127533e-03	-2.2426181793212891e+01	-6.7269902229309082e+00	-2.2461936473846436e+00	+1.0424779728055000e-02	-2.1550936698913574e+00	+1.0762871503829956e+00	-5.4205872118473053e-02	+1.0137343406677246e+00	+1.0054445825517178e-02	+8.3967143297195435e-01	-3.2765858173370361e+00	-9.6592950820922852e-01	+7.5265145860612392e-03	+1.7908766865730286e-02	-1.0453859567642212e+00	+5.1517069339752197e-01	+1.0649362578988075e-02	-1.4490582466125488e+01	
+-3.2857151236385107e-03	+5.9187543392181396e-01	-2.7645176742225885e-03	-5.6996935606002808e-01	+2.6538472156971693e-03	-2.7195680141448975e+00	+3.0651132110506296e-03	+8.6517339944839478e-01	+4.3157178163528442e-01	+1.4268080890178680e-01	+3.5014057066291571e-03	+5.3483609110116959e-02	-6.2381106615066528e-01	-2.6864213868975639e-03	-3.6386675201356411e-03	+3.2822357024997473e-03	-6.2203389825299382e-04	+5.6492674350738525e-01	-4.0196239948272705e-02	-3.2206296455115080e-03	-1.3066108226776123e+00	+3.2423695083707571e-03	-4.7114229202270508e-01	-3.1998909544199705e-03	-3.4287294838577509e-03	-7.1377158164978027e-01	-3.3232133835554123e-02	+4.1278833150863647e-01	-6.1671531200408936e-01	+8.1366943195462227e-03	-2.5733003858476877e-03	-4.1674333624541759e-03	+2.6167348027229309e-01	+2.3013504222035408e-02	-3.9804546833038330e+00	+3.2503411639481783e-03	-4.1613835096359253e-01	+8.3258646726608276e-01	-4.6460423469543457e+00	-6.7755001783370972e-01	+2.0869453437626362e-03	-1.2752885818481445e+00	+3.7751388549804688e-01	+7.4102884531021118e-01	+2.5022702757269144e-03	-3.5920643806457520e+00	+4.4666483998298645e-01	+6.7768990993499756e-01	+3.8648282643407583e-03	-6.6180028021335602e-02	
+</layer>
+<layer>
++2.2392576560378075e-02	+7.9600289463996887e-03	+3.5748567897826433e-03	-9.0584503486752510e-03	+1.2166848406195641e-02	-2.5937089230865240e-03	-3.1598001718521118e-02	-1.0288016637787223e-03	+5.8472803793847561e-03	+9.6058771014213562e-03	+1.1490470496937633e-03	+1.1987331090494990e-03	-1.4139647595584393e-02	+5.7148635387420654e-03	-1.3746656477451324e-02	-1.1688595404848456e-03	-6.0691782273352146e-03	+1.2217802926898003e-02	+4.9242796376347542e-04	-3.5094288177788258e-03	-1.1753068974940106e-04	+1.0253794491291046e-02	-4.4527775608003139e-03	-9.4327889382839203e-03	+5.4327612742781639e-03	+1.4921743422746658e-02	-4.8628062941133976e-03	+2.6123812422156334e-03	-2.4538778234273195e-03	+1.0964288376271725e-03	
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++1.1766321258619428e-03	+7.2402417659759521e-02	+9.2022772878408432e-03	-1.8883422017097473e-01	-2.7701869606971741e-01	-2.8931684792041779e-03	
+-8.4980977699160576e-03	-1.5197299420833588e-01	-5.1791906356811523e-02	-5.4501686245203018e-02	-3.5542692989110947e-02	-3.5902922973036766e-03	
++6.3685655593872070e-01	+9.4508506357669830e-02	-2.7333220839500427e-01	-5.2644416689872742e-02	-5.5399943143129349e-02	-3.7951543927192688e-01	
+-2.9785081744194031e-01	-2.1770578622817993e-01	-2.7142554521560669e-01	-3.5189813375473022e-01	-2.1658948063850403e-01	-9.4562992453575134e-02	
+-3.8083154708147049e-02	-2.4195717647671700e-02	-2.1490247920155525e-02	-2.4765911698341370e-01	-6.1096609570086002e-03	+1.3527723029255867e-02	
+-5.6719094514846802e-01	-1.8840165436267853e-01	+7.2667652368545532e-01	+3.5026542842388153e-02	+5.1972195506095886e-03	-9.4628494977951050e-01	
+-2.2089238464832306e-01	-7.9360559582710266e-02	-4.5122358947992325e-02	-4.8103030771017075e-02	-1.0051660239696503e-01	+1.7232533544301987e-02	
++2.8489297628402710e-01	-2.5881674885749817e-01	-3.7712398171424866e-01	+3.2797567546367645e-02	-1.4035736024379730e-01	+3.1092634797096252e-01	
+</layer>
+
+[biases per layer]
++0.0000000000000000e+00	+0.0000000000000000e+00	+0.0000000000000000e+00
++5.7850396260619164e-03	-5.4800868034362793e-01	+7.0601208135485649e-03	+4.4343668222427368e-01	+9.5969978719949722e-03	-1.8918423652648926e+00	-5.9042316861450672e-03	-7.0072931051254272e-01	-3.7168869376182556e-01	+2.7316311374306679e-02	+9.8313717171549797e-03	-4.3344125151634216e-02	+3.4073707461357117e-01	+6.2903217040002346e-03	+6.4147775992751122e-03	-5.8323685079813004e-03	+6.0578244738280773e-03	-4.7514703869819641e-01	+1.3792721927165985e-01	+5.8732479810714722e-03	+4.2972606420516968e-01	-5.8087822981178761e-03	+6.9927662611007690e-02	+6.5745734609663486e-03	+5.7183597236871719e-03	-2.0756023004651070e-02	+8.2162462174892426e-02	-3.1270492076873779e-01	-4.9186524003744125e-02	+1.0777912102639675e-02	+7.7938484027981758e-03	+4.5307301916182041e-03	-2.4378831684589386e-01	-2.6500603184103966e-02	-3.5185754299163818e+00	-5.5729215964674950e-03	+2.8386363387107849e-01	-5.9977006912231445e-01	-3.2172240316867828e-02	+2.8363862633705139e-01	-7.1090161800384521e-03	+1.9982965663075447e-02	-2.2212673723697662e-01	-4.8118641972541809e-01	-6.8406895734369755e-03	+2.1139304339885712e-01	-3.5522702336311340e-01	-4.7585010528564453e-01	-6.0312664136290550e-03	+3.3170813322067261e-01	
+-3.7559503316879272e-01	+5.0203863531351089e-02	-6.7103123664855957e-01	-9.5661211013793945e-01	-3.7905260920524597e-02	-8.4884636104106903e-02	-1.4869323968887329e+00	-1.1877594888210297e-01	+9.2768125236034393e-02	-4.6068467199802399e-02	-4.6287722885608673e-02	+2.1052359044551849e-01	-1.0061993598937988e+00	-2.6615330949425697e-02	+2.9844671487808228e-02	-1.6860149800777435e-01	+4.1984126437455416e-04	-1.1137908697128296e+00	-3.0047450214624405e-02	-1.0990808010101318e+00	-9.0412914752960205e-01	-1.0024057626724243e+00	-5.0296580791473389e-01	-3.8795295357704163e-01	-1.4703199863433838e+00	-1.0035289525985718e+00	-6.4480721950531006e-01	-1.5599024295806885e+00	-1.0307478904724121e-01	+1.0781782865524292e-01	
++1.0000430047512054e-01	+1.5528109669685364e-01	+1.9897127151489258e-01	+1.2465928494930267e-01	+1.2603196501731873e-01	+1.1598975211381912e-01	
diff --git a/TestCases/nicf/datadriven/datadriven_nozzle.cfg b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
index 882f310d269..980f372091d 100644
--- a/TestCases/nicf/datadriven/datadriven_nozzle.cfg
+++ b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
@@ -98,7 +98,7 @@ CONV_STARTITER= 10
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
 % Mesh input file
-MESH_FILENAME= coolprop_nozzle.su2
+MESH_FILENAME= ../coolprop/coolprop_nozzle.su2
 %
 % Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
diff --git a/config_template.cfg b/config_template.cfg
index 4265a8098d5..ecd3b70284e 100644
--- a/config_template.cfg
+++ b/config_template.cfg
@@ -377,6 +377,7 @@ FROZEN_MIXTURE= NO
 INTERPOLATION_METHOD= MLP
 
 % Name of the input file containing the information required for the interpolator to function
+% See https://github.com/EvertBunschoten/MLPCpp for more information.
 FILENAME_INTERPOLATOR= MLP_collection.mlp
 
 % Relaxation factor for the Newton solvers in the data-driven fluid model
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 053fdc065f5..f4c32d30ca8 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -71,7 +71,7 @@ def init_submodules(
     github_repo_coolprop = "https://github.com/CoolProp/CoolProp"
     sha_version_mel = "2484cd3258ef800a10e361016cb341834ee7930b"
     github_repo_mel = "https://github.com/pcarruscag/MEL"
-    sha_version_mlpcpp = "84b616acc7b76905ea12a29e08eaf4e180f35854"
+    sha_version_mlpcpp = "b723a9c06694c52f9e392116436c41bbe8e17244"
     github_repo_mlpcpp = "https://github.com/EvertBunschoten/MLPCpp"
 
     medi_name = "MeDiPack"
diff --git a/subprojects/MLPCpp b/subprojects/MLPCpp
index 84b616acc7b..b723a9c0669 160000
--- a/subprojects/MLPCpp
+++ b/subprojects/MLPCpp
@@ -1 +1 @@
-Subproject commit 84b616acc7b76905ea12a29e08eaf4e180f35854
+Subproject commit b723a9c06694c52f9e392116436c41bbe8e17244

From 0ddf5d3dc202946f069d5d457e7ab81277dbe8b8 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Tue, 11 Apr 2023 12:03:38 +0200
Subject: [PATCH 387/656] CoDiPack update.

---
 externals/codi        | 2 +-
 meson_scripts/init.py | 2 +-
 2 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/externals/codi b/externals/codi
index 427c2dc754a..ca5573d50f9 160000
--- a/externals/codi
+++ b/externals/codi
@@ -1 +1 @@
-Subproject commit 427c2dc754a628ad3c9310c766c988ac5ce21bc7
+Subproject commit ca5573d50f9a54ba50d28a8639822a56d556240b
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 3f0b0646a6f..7b6ea828bd4 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -54,7 +54,7 @@ def init_submodules(
 
     # This information of the modules is used if projects was not cloned using git
     # The sha tag must be maintained manually to point to the correct commit
-    sha_version_codi = "427c2dc754a628ad3c9310c766c988ac5ce21bc7"
+    sha_version_codi = "ca5573d50f9a54ba50d28a8639822a56d556240b"
     github_repo_codi = "https://github.com/scicompkl/CoDiPack"
     sha_version_medi = "aafc2d1966ba1233640af737e71c77c1a86183fd"
     github_repo_medi = "https://github.com/SciCompKL/MeDiPack"

From af9ee8283d5f10b2c96ad0487ea4cb1cf6b59da8 Mon Sep 17 00:00:00 2001
From: voss_ar <voss_ar@escher.ae.go.dlr.de>
Date: Wed, 12 Apr 2023 11:03:40 +0200
Subject: [PATCH 388/656] - extending gust to 3D - fixing 1-cosing gust
 amplitude

---
 SU2_CFD/src/iteration/CFluidIteration.cpp | 32 ++++++++++++++---------
 1 file changed, 20 insertions(+), 12 deletions(-)

diff --git a/SU2_CFD/src/iteration/CFluidIteration.cpp b/SU2_CFD/src/iteration/CFluidIteration.cpp
index db7a7a18be4..c1130421f2c 100644
--- a/SU2_CFD/src/iteration/CFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CFluidIteration.cpp
@@ -318,13 +318,12 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
   // derivatives needed for the source term are calculated when applicable. If the gust derivatives are zero the source
   // term is also zero. The source term itself is implemented in the class CSourceWindGust
 
-  if (rank == MASTER_NODE) cout << endl << "Running simulation with a Wind Gust." << endl;
   unsigned short iDim, nDim = geometry[MESH_0]->GetnDim();  // We assume nDim = 2
-  if (nDim != 2) {
-    if (rank == MASTER_NODE) {
-      cout << endl << "WARNING - Wind Gust capability is only verified for 2 dimensional simulations." << endl;
-    }
-  }
+//  if (nDim != 2) {
+//    if (rank == MASTER_NODE) {
+//      cout << endl << "WARNING - Wind Gust capability is only verified for 2 dimensional simulations." << endl;
+//    }
+//  }
 
   /*--- Gust Parameters from config ---*/
   unsigned short Gust_Type = config->GetGust_Type();
@@ -340,7 +339,7 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
   unsigned long iPoint;
   unsigned short iMGlevel, nMGlevel = config->GetnMGLevels();
 
-  su2double x, y, x_gust, dgust_dx, dgust_dy, dgust_dt;
+  su2double x, y, x_gust, dgust_dx, dgust_dy, dgust_dz, dgust_dt;
   su2double *Gust, *GridVel, *NewGridVel, *GustDer;
 
   su2double Physical_dt = config->GetDelta_UnstTime();
@@ -358,8 +357,15 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
     NewGridVel[iDim] = 0.0;
   }
 
-  GustDer = new su2double[3];
-  for (unsigned short i = 0; i < 3; i++) {
+  // Print some information to check that we are doing the right thing. Not sure how to convert the index back to a string...
+  if (rank == MASTER_NODE) cout << endl << " Setting up a wind gust type " << Gust_Type << " with amplitude of " << gust_amp << " in direction " << GustDir << endl;
+  if (rank == MASTER_NODE) cout << " U_inf      = " << Uinf << endl;
+  if (rank == MASTER_NODE) cout << " Physical_t = " << Physical_t << endl;
+  su2double loc_x = (xbegin + L + Uinf * (Physical_t - tbegin));
+  if (rank == MASTER_NODE) cout << " Location_x = " << loc_x << endl;
+
+  GustDer = new su2double[4];
+  for (unsigned short i = 0; i < 4; i++) {
     GustDer[i] = 0.0;
   }
 
@@ -393,6 +399,7 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
       }
       dgust_dx = 0.0;
       dgust_dy = 0.0;
+      dgust_dz = 0.0;
       dgust_dt = 0.0;
 
       /*--- Begin applying the gust ---*/
@@ -429,7 +436,7 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
           case ONE_M_COSINE:
             // Check if we are in the region where the gust is active
             if (x_gust > 0 && x_gust < n) {
-              Gust[GustDir] = gust_amp * (1 - cos(2 * PI_NUMBER * x_gust));
+              Gust[GustDir] = gust_amp * 0.5 * (1 - cos(2 * PI_NUMBER * x_gust));
 
               // Gust derivatives
               // dgust_dx = gust_amp*2*PI_NUMBER*(sin(2*PI_NUMBER*x_gust))/L;
@@ -473,8 +480,9 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
 
       GustDer[0] = dgust_dx;
       GustDer[1] = dgust_dy;
-      GustDer[2] = dgust_dt;
-
+      GustDer[2] = dgust_dz;
+      GustDer[3] = dgust_dt;
+      // I think we don't need to set any source terms because they depend on the derivatives, which are zero in all cases from above.
       solver[iMGlevel][FLOW_SOL]->GetNodes()->SetWindGust(iPoint, Gust);
       solver[iMGlevel][FLOW_SOL]->GetNodes()->SetWindGustDer(iPoint, GustDer);
 

From 4ca52818bf28fa4ef1e88cd2556d8fa8e4ec0d75 Mon Sep 17 00:00:00 2001
From: voss_ar <voss_ar@escher.ae.go.dlr.de>
Date: Thu, 13 Apr 2023 10:16:00 +0200
Subject: [PATCH 389/656] Modifying the switch for resetting or keeping
 existing grid velocity to handle elastic mesh deformation.

---
 SU2_CFD/src/iteration/CFluidIteration.cpp | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/SU2_CFD/src/iteration/CFluidIteration.cpp b/SU2_CFD/src/iteration/CFluidIteration.cpp
index c1130421f2c..a5adf9e6256 100644
--- a/SU2_CFD/src/iteration/CFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CFluidIteration.cpp
@@ -358,7 +358,7 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
   }
 
   // Print some information to check that we are doing the right thing. Not sure how to convert the index back to a string...
-  if (rank == MASTER_NODE) cout << endl << " Setting up a wind gust type " << Gust_Type << " with amplitude of " << gust_amp << " in direction " << GustDir << endl;
+  if (rank == MASTER_NODE) cout << endl << "Setting up a wind gust type " << Gust_Type << " with amplitude of " << gust_amp << " in direction " << GustDir << endl;
   if (rank == MASTER_NODE) cout << " U_inf      = " << Uinf << endl;
   if (rank == MASTER_NODE) cout << " Physical_t = " << Physical_t << endl;
   su2double loc_x = (xbegin + L + Uinf * (Physical_t - tbegin));
@@ -388,7 +388,7 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
 
     for (iPoint = 0; iPoint < geometry[iMGlevel]->GetnPoint(); iPoint++) {
       /*--- Reset the Grid Velocity to zero if there is no grid movement ---*/
-      if (Kind_Grid_Movement == GUST && !(config->GetFSI_Simulation())) {
+      if (Kind_Grid_Movement == GUST && !(config->GetFSI_Simulation()) && !(config->GetDynamic_Grid())) {
         for (iDim = 0; iDim < nDim; iDim++) geometry[iMGlevel]->nodes->SetGridVel(iPoint, iDim, 0.0);
       }
 

From ae828e30eff2d9264f43a6ffe9a10f4dd2804368 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Vo=C3=9F=2C=20Arne?= <arne.voss@dlr.de>
Date: Mon, 27 Feb 2023 16:53:07 +0100
Subject: [PATCH 390/656] First try to implement a python wrapper for updating
 the dynamic mesh velovities

---
 SU2_CFD/include/drivers/CDriver.hpp      |  8 ++++++++
 SU2_CFD/src/python_wrapper_structure.cpp | 15 +++++++++++++++
 2 files changed, 23 insertions(+)

diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index 5481a8e9a97..08ab691af8e 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -617,6 +617,14 @@ class CDriver {
    */
   void SetMeshDisplacement(unsigned short iMarker, unsigned long iVertex, passivedouble DispX, passivedouble DispY, passivedouble DispZ);
 
+  /*!
+     * \brief Set the dynamic mesh rotation rates.
+     * \param[in] rot_x - Value of Angular velocity about x-axes.
+     * \param[in] rot_y - Value of Angular velocity about y-axes.
+     * \param[in] rot_z - Value of Angular velocity about z-axes.
+     */
+    void SetRotationRate(passivedouble rot_x, passivedouble rot_y, passivedouble rot_z);
+
   /*!
    * \brief Communicate the boundary mesh displacements in a python call
    */
diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index 32672e87eef..fbf8c6c5fcb 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -865,6 +865,21 @@ void CDriver::CommunicateMeshDisplacement(void) {
 
 }
 
+////////////////////////////////////////////////////////////////////////////////
+/* Functions related to dynamic mesh */
+////////////////////////////////////////////////////////////////////////////////
+
+void CDriver::SetRotationRate(passivedouble rot_x, passivedouble rot_y, passivedouble rot_z) {
+
+  config_container[iZone]->SetRotation_Rate(0, rot_x);
+  config_container[iZone]->SetRotation_Rate(1, rot_y);
+  config_container[iZone]->SetRotation_Rate(2, rot_z);
+  if (rank == MASTER_NODE) {
+	  cout << endl << " Set new angular velocity about x, y, z axes" << endl;
+  }
+
+}
+
 ////////////////////////////////////////////////////////////////////////////////
 /* Functions related to flow loads */
 ////////////////////////////////////////////////////////////////////////////////

From 1fcd7b20f006104e57f8c6c8400c6f4359ce9956 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Vo=C3=9F=2C=20Arne?= <arne.voss@dlr.de>
Date: Mon, 27 Feb 2023 18:35:17 +0100
Subject: [PATCH 391/656] Implementing the python wrapper for updating the
 translational mesh velocities, too.

---
 Common/include/CConfig.hpp               |  7 +++++++
 SU2_CFD/include/drivers/CDriver.hpp      | 20 ++++++++++++++------
 SU2_CFD/src/python_wrapper_structure.cpp | 23 +++++++++++++++++------
 3 files changed, 38 insertions(+), 12 deletions(-)

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index f3b1abd9876..d2f63d10403 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -5815,6 +5815,13 @@ class CConfig {
    */
   su2double GetTranslation_Rate(unsigned short iDim) const { return Translation_Rate[iDim];}
 
+  /*!
+   * \brief Set the translational velocity of the mesh.
+   * \param[in] iDim - spatial component
+   * \return Translational velocity of the mesh.
+   */
+  void SetTranslation_Rate(unsigned short iDim, su2double val) { Translation_Rate[iDim] = val;}
+
   /*!
    * \brief Get the translational velocity of the marker.
    * \param[in] iMarkerMoving -  Index of the moving marker (as specified in Marker_Moving)
diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index 08ab691af8e..a691eb2bd16 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -618,12 +618,20 @@ class CDriver {
   void SetMeshDisplacement(unsigned short iMarker, unsigned long iVertex, passivedouble DispX, passivedouble DispY, passivedouble DispZ);
 
   /*!
-     * \brief Set the dynamic mesh rotation rates.
-     * \param[in] rot_x - Value of Angular velocity about x-axes.
-     * \param[in] rot_y - Value of Angular velocity about y-axes.
-     * \param[in] rot_z - Value of Angular velocity about z-axes.
-     */
-    void SetRotationRate(passivedouble rot_x, passivedouble rot_y, passivedouble rot_z);
+   * \brief Set the dynamic mesh translation rates.
+   * \param[in] xDot - Value of translational velocity in x-direction.
+   * \param[in] yDot - Value of translational velocity in y-direction.
+   * \param[in] zDot - Value of translational velocity in z-direction.
+   */
+  void SetTranslationRate(passivedouble xDot, passivedouble yDot, passivedouble zDot);
+
+  /*!
+   * \brief Set the dynamic mesh rotation rates.
+   * \param[in] rot_x - Value of Angular velocity about x-axes.
+   * \param[in] rot_y - Value of Angular velocity about y-axes.
+   * \param[in] rot_z - Value of Angular velocity about z-axes.
+   */
+  void SetRotationRate(passivedouble rot_x, passivedouble rot_y, passivedouble rot_z);
 
   /*!
    * \brief Communicate the boundary mesh displacements in a python call
diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index fbf8c6c5fcb..d618dfd43e9 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -869,15 +869,26 @@ void CDriver::CommunicateMeshDisplacement(void) {
 /* Functions related to dynamic mesh */
 ////////////////////////////////////////////////////////////////////////////////
 
-void CDriver::SetRotationRate(passivedouble rot_x, passivedouble rot_y, passivedouble rot_z) {
-
-  config_container[iZone]->SetRotation_Rate(0, rot_x);
-  config_container[iZone]->SetRotation_Rate(1, rot_y);
-  config_container[iZone]->SetRotation_Rate(2, rot_z);
+void CDriver::SetTranslationRate(passivedouble xDot, passivedouble yDot, passivedouble zDot) {
   if (rank == MASTER_NODE) {
-	  cout << endl << " Set new angular velocity about x, y, z axes" << endl;
+    cout << endl << " Setting new translational velocity in x, y, z direction.";
   }
+  for (iZone = 0; iZone < nZone; iZone++) {
+    config_container[iZone]->SetTranslation_Rate(0, xDot);
+    config_container[iZone]->SetTranslation_Rate(1, yDot);
+    config_container[iZone]->SetTranslation_Rate(2, zDot);
+  }
+}
 
+void CDriver::SetRotationRate(passivedouble rot_x, passivedouble rot_y, passivedouble rot_z) {
+  if (rank == MASTER_NODE) {
+    cout << endl << " Setting new angular velocity about x, y, z axes.";
+  }
+  for (iZone = 0; iZone < nZone; iZone++) {
+    config_container[iZone]->SetRotation_Rate(0, rot_x);
+    config_container[iZone]->SetRotation_Rate(1, rot_y);
+    config_container[iZone]->SetRotation_Rate(2, rot_z);
+  }
 }
 
 ////////////////////////////////////////////////////////////////////////////////

From eb8a6ec3e12ff8e4c42bda1b89b3dc8cf3b9a906 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Fri, 14 Apr 2023 09:18:39 +0200
Subject: [PATCH 392/656] Restore 2D gusts

---
 SU2_CFD/src/iteration/CFluidIteration.cpp | 20 +++++++++++++-------
 1 file changed, 13 insertions(+), 7 deletions(-)

diff --git a/SU2_CFD/src/iteration/CFluidIteration.cpp b/SU2_CFD/src/iteration/CFluidIteration.cpp
index a5adf9e6256..49aeb6e1834 100644
--- a/SU2_CFD/src/iteration/CFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CFluidIteration.cpp
@@ -364,8 +364,8 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
   su2double loc_x = (xbegin + L + Uinf * (Physical_t - tbegin));
   if (rank == MASTER_NODE) cout << " Location_x = " << loc_x << endl;
 
-  GustDer = new su2double[4];
-  for (unsigned short i = 0; i < 4; i++) {
+  GustDer = new su2double[nDim+1];
+  for (unsigned short i = 0; i < nDim+1; i++) {
     GustDer[i] = 0.0;
   }
 
@@ -477,11 +477,17 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
       }
 
       /*--- Set the Wind Gust, Wind Gust Derivatives and the Grid Velocities ---*/
-
-      GustDer[0] = dgust_dx;
-      GustDer[1] = dgust_dy;
-      GustDer[2] = dgust_dz;
-      GustDer[3] = dgust_dt;
+      if (nDim = 2) {
+    	  GustDer[0] = dgust_dx;
+    	  GustDer[1] = dgust_dy;
+    	  GustDer[2] = dgust_dt;
+      }
+      else {
+    	  GustDer[0] = dgust_dx;
+    	  GustDer[1] = dgust_dy;
+    	  GustDer[2] = dgust_dz;
+    	  GustDer[3] = dgust_dt;
+      }
       // I think we don't need to set any source terms because they depend on the derivatives, which are zero in all cases from above.
       solver[iMGlevel][FLOW_SOL]->GetNodes()->SetWindGust(iPoint, Gust);
       solver[iMGlevel][FLOW_SOL]->GetNodes()->SetWindGustDer(iPoint, GustDer);

From 1c1cfffcde07d9f2efa1f1c8047b7f6fe1257860 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Fri, 14 Apr 2023 10:09:29 +0200
Subject: [PATCH 393/656] Refined cirterion on decision of keeping or
 overwriting existing grid velocities, should fix test case 'sine_gust'.

---
 SU2_CFD/src/iteration/CFluidIteration.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/SU2_CFD/src/iteration/CFluidIteration.cpp b/SU2_CFD/src/iteration/CFluidIteration.cpp
index 49aeb6e1834..d4fed319d19 100644
--- a/SU2_CFD/src/iteration/CFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CFluidIteration.cpp
@@ -388,7 +388,7 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
 
     for (iPoint = 0; iPoint < geometry[iMGlevel]->GetnPoint(); iPoint++) {
       /*--- Reset the Grid Velocity to zero if there is no grid movement ---*/
-      if (Kind_Grid_Movement == GUST && !(config->GetFSI_Simulation()) && !(config->GetDynamic_Grid())) {
+      if (Kind_Grid_Movement == GUST && !(config->GetFSI_Simulation()) && !(config->GetDeform_Mesh())) {
         for (iDim = 0; iDim < nDim; iDim++) geometry[iMGlevel]->nodes->SetGridVel(iPoint, iDim, 0.0);
       }
 

From 2259d67272a5f180714d19a77d2a4d1aaeaea232 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Fri, 14 Apr 2023 10:19:38 +0200
Subject: [PATCH 394/656] - Implemented style suggestions from CodeFactor, no
 functional change - Removed commented out code / warning messages w.r.t 2D
 gusts only

---
 SU2_CFD/src/iteration/CFluidIteration.cpp  | 23 +++++++++-------------
 SU2_CFD/src/numerics/flow/flow_sources.cpp | 16 +++++++--------
 2 files changed, 17 insertions(+), 22 deletions(-)

diff --git a/SU2_CFD/src/iteration/CFluidIteration.cpp b/SU2_CFD/src/iteration/CFluidIteration.cpp
index d4fed319d19..df256b876ec 100644
--- a/SU2_CFD/src/iteration/CFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CFluidIteration.cpp
@@ -318,12 +318,7 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
   // derivatives needed for the source term are calculated when applicable. If the gust derivatives are zero the source
   // term is also zero. The source term itself is implemented in the class CSourceWindGust
 
-  unsigned short iDim, nDim = geometry[MESH_0]->GetnDim();  // We assume nDim = 2
-//  if (nDim != 2) {
-//    if (rank == MASTER_NODE) {
-//      cout << endl << "WARNING - Wind Gust capability is only verified for 2 dimensional simulations." << endl;
-//    }
-//  }
+  unsigned short iDim, nDim = geometry[MESH_0]->GetnDim();
 
   /*--- Gust Parameters from config ---*/
   unsigned short Gust_Type = config->GetGust_Type();
@@ -477,16 +472,16 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
       }
 
       /*--- Set the Wind Gust, Wind Gust Derivatives and the Grid Velocities ---*/
-      if (nDim = 2) {
-    	  GustDer[0] = dgust_dx;
-    	  GustDer[1] = dgust_dy;
-    	  GustDer[2] = dgust_dt;
+      if (nDim == 2) {
+        GustDer[0] = dgust_dx;
+        GustDer[1] = dgust_dy;
+        GustDer[2] = dgust_dt;
       }
       else {
-    	  GustDer[0] = dgust_dx;
-    	  GustDer[1] = dgust_dy;
-    	  GustDer[2] = dgust_dz;
-    	  GustDer[3] = dgust_dt;
+        GustDer[0] = dgust_dx;
+        GustDer[1] = dgust_dy;
+        GustDer[2] = dgust_dz;
+        GustDer[3] = dgust_dt;
       }
       // I think we don't need to set any source terms because they depend on the derivatives, which are zero in all cases from above.
       solver[iMGlevel][FLOW_SOL]->GetNodes()->SetWindGust(iPoint, Gust);
diff --git a/SU2_CFD/src/numerics/flow/flow_sources.cpp b/SU2_CFD/src/numerics/flow/flow_sources.cpp
index 3d297157a51..a06cf7134f1 100644
--- a/SU2_CFD/src/numerics/flow/flow_sources.cpp
+++ b/SU2_CFD/src/numerics/flow/flow_sources.cpp
@@ -783,14 +783,14 @@ CNumerics::ResidualType<> CSourceWindGust::ComputeResidual(const CConfig* config
     residual[2] = smy*Volume;
     //residual[3] = smz*Volume;
     residual[3] = se*Volume;
-  } else {
-	  //    SU2_MPI::Error("You should only be in the gust source term in two dimensions", CURRENT_FUNCTION);
-	  	residual[0] = 0.0;
-	  	residual[1] = 0.0;
-	  	residual[2] = 0.0;
-	  	residual[3] = 0.0;
-	  	residual[4] = 0.0;
-	    }
+  }
+  else {
+    residual[0] = 0.0;
+    residual[1] = 0.0;
+    residual[2] = 0.0;
+    residual[3] = 0.0;
+    residual[4] = 0.0;
+    }
 
   /*--- For now the source term Jacobian is just set to zero ---*/
   //bool implicit = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);

From aa786d88c7ad2d3db15834b37e6a678564f271a4 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Thu, 13 Apr 2023 14:33:02 +0200
Subject: [PATCH 395/656] Make sure that the velocity field from a rotating
 frame is reset in every new iteration.

---
 SU2_CFD/src/iteration/CIteration.cpp | 11 +++++++++++
 1 file changed, 11 insertions(+)

diff --git a/SU2_CFD/src/iteration/CIteration.cpp b/SU2_CFD/src/iteration/CIteration.cpp
index 337e24edaea..2e81f90f7d3 100644
--- a/SU2_CFD/src/iteration/CIteration.cpp
+++ b/SU2_CFD/src/iteration/CIteration.cpp
@@ -63,6 +63,17 @@ void CIteration::SetGrid_Movement(CGeometry** geometry, CSurfaceMovement* surfac
       /*--- Already initialized in the static mesh movement routine at driver level. ---*/
     case STEADY_TRANSLATION:
     case ROTATING_FRAME:
+      if (rank == MASTER_NODE) cout << endl << " Setting rotating frame grid velocities" << endl;
+
+      /*--- Set the grid velocities on finest multigrid level for a rotating reference frame. ---*/
+
+      geometry[MESH_0]->SetRotationalVelocity(config, true);
+
+      /*--- Update the multigrid structure after moving the finest grid,
+            including computing the grid velocities on the coarser levels. ---*/
+
+      grid_movement->UpdateMultiGrid(geometry, config);
+
       break;
   }
 

From 9782af92b3e71921e3c6f9330d9a3c9c1839340c Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 15 Apr 2023 15:02:45 -0700
Subject: [PATCH 396/656] cleanup unsused code

---
 Common/include/CConfig.hpp                     |  6 ------
 SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp | 12 +++---------
 2 files changed, 3 insertions(+), 15 deletions(-)

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index b01d4d1c5ca..f7b57a2445b 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -9251,12 +9251,6 @@ class CConfig {
    */
   void SetnTime_Iter(unsigned long val_iter) { nTimeIter = val_iter; }
 
-  /*!
-   * \brief Get the number of pseudo-time iterations
-   * \return Number of pseudo-time steps run for the single-zone problem
-   */
-  unsigned long GetnIter(void) const { return nIter; }
-
   /*!
    * \brief Get the restart iteration
    * \return Iteration for the restart of multizone problems
diff --git a/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
index 4a6e61dfc2c..75ad91681f3 100644
--- a/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
@@ -34,7 +34,7 @@ CDiscAdjFEAIteration::CDiscAdjFEAIteration(const CConfig *config) : CIteration(c
   fem_iteration = new CFEAIteration(config);
 
   // TEMPORARY output only for standalone structural problems
-  if ((!config->GetFSI_Simulation()) && (rank == MASTER_NODE)) {
+  if (config->GetAdvanced_FEAElementBased() && (rank == MASTER_NODE)) {
     bool de_effects = config->GetDE_Effects();
     unsigned short iVar;
 
@@ -56,9 +56,7 @@ CDiscAdjFEAIteration::CDiscAdjFEAIteration(const CConfig *config) : CIteration(c
       for (iVar = 0; iVar < config->GetnElectric_Field(); iVar++) myfile_res << "Sens_EField_" << iVar << "\t";
     }
 
-    myfile_res << endl;
-
-    myfile_res.close();
+    myfile_res << '\n';
   }
 }
 
@@ -365,25 +363,21 @@ void CDiscAdjFEAIteration::Postprocess(COutput* output, CIntegration**** integra
   if (config[iZone]->GetAdvanced_FEAElementBased() && (rank == MASTER_NODE)) {
     /*--- Header of the temporary output file ---*/
     ofstream myfile_res;
-    bool outputDVFEA = false;
+    bool outputDVFEA = true;
 
     switch (config[iZone]->GetDV_FEA()) {
       case YOUNG_MODULUS:
         myfile_res.open("grad_young.opt");
-        outputDVFEA = true;
         break;
       case POISSON_RATIO:
         myfile_res.open("grad_poisson.opt");
-        outputDVFEA = true;
         break;
       case DENSITY_VAL:
       case DEAD_WEIGHT:
         myfile_res.open("grad_density.opt");
-        outputDVFEA = true;
         break;
       case ELECTRIC_FIELD:
         myfile_res.open("grad_efield.opt");
-        outputDVFEA = true;
         break;
       default:
         outputDVFEA = false;

From 45243a7cc48ca4f185f5bccadbcab855c7f29918 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 15 Apr 2023 18:47:11 -0700
Subject: [PATCH 397/656] fix structural unsteady adjoints

---
 .../src/drivers/CDiscAdjMultizoneDriver.cpp   | 14 ++--
 .../src/drivers/CDiscAdjSinglezoneDriver.cpp  | 18 +++--
 .../integration/CStructuralIntegration.cpp    |  6 +-
 .../src/iteration/CDiscAdjFEAIteration.cpp    | 65 ++++++-------------
 SU2_CFD/src/iteration/CFEAIteration.cpp       | 36 ++++------
 SU2_CFD/src/solvers/CFEASolver.cpp            | 18 +++--
 6 files changed, 63 insertions(+), 94 deletions(-)

diff --git a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
index 586c9cabfdc..0a2a77ae31f 100644
--- a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
@@ -763,15 +763,15 @@ void CDiscAdjMultizoneDriver::SetObjFunction(RECORDING kind_recording) {
 }
 
 void CDiscAdjMultizoneDriver::SetAdjObjFunction() {
-
-  const auto IterAvg_Obj = config_container[ZONE_0]->GetIter_Avg_Objective();
   su2double seeding = 1.0;
 
-  if (config_container[ZONE_0]->GetTime_Marching() != TIME_MARCHING::STEADY){
-    if (TimeIter < IterAvg_Obj){
-      // Default behavior (in case no specific window is chosen) is to use Square-Windowing, i.e. the numerator equals 1.0
+  if (config_container[ZONE_0]->GetTime_Domain()) {
+    const auto IterAvg_Obj = config_container[ZONE_0]->GetIter_Avg_Objective();
+    if (TimeIter < IterAvg_Obj) {
+      /*--- Default behavior when no window is chosen is to use Square-Windowing, i.e. the numerator equals 1.0 ---*/
       auto windowEvaluator = CWindowingTools();
-      su2double weight = windowEvaluator.GetWndWeight(config_container[ZONE_0]->GetKindWindow(), TimeIter, IterAvg_Obj-1);
+      const su2double weight =
+          windowEvaluator.GetWndWeight(config_container[ZONE_0]->GetKindWindow(), TimeIter, IterAvg_Obj - 1);
       seeding = weight / IterAvg_Obj;
     }
     else {
@@ -780,6 +780,8 @@ void CDiscAdjMultizoneDriver::SetAdjObjFunction() {
   }
   if (rank == MASTER_NODE) {
     AD::SetDerivative(ObjFunc_Index, SU2_TYPE::GetValue(seeding));
+  } else {
+    AD::SetDerivative(ObjFunc_Index, 0.0);
   }
 }
 
diff --git a/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
index 5a42be040d7..f9cfb269a8e 100644
--- a/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
@@ -319,23 +319,21 @@ void CDiscAdjSinglezoneDriver::SetRecording(RECORDING kind_recording){
 }
 
 void CDiscAdjSinglezoneDriver::SetAdjObjFunction(){
-
-  const auto IterAvg_Obj = config->GetIter_Avg_Objective();
   su2double seeding = 1.0;
 
-  CWindowingTools windowEvaluator = CWindowingTools();
-
-  if (config->GetTime_Marching() != TIME_MARCHING::STEADY){
-    if (TimeIter < IterAvg_Obj){
-      /*--- Default behavior (in case no specific window is chosen) is to use Square-Windowing, i.e. the numerator equals 1.0 ---*/
-      seeding = windowEvaluator.GetWndWeight(config->GetKindWindow(),TimeIter, IterAvg_Obj-1)/ (static_cast<su2double>(IterAvg_Obj));
+  if (config->GetTime_Domain()) {
+    const auto IterAvg_Obj = config->GetIter_Avg_Objective();
+    if (TimeIter < IterAvg_Obj) {
+      /*--- Default behavior when no window is chosen is to use Square-Windowing, i.e. the numerator equals 1.0 ---*/
+      auto windowEvaluator = CWindowingTools();
+      const su2double weight = windowEvaluator.GetWndWeight(config->GetKindWindow(), TimeIter, IterAvg_Obj - 1);
+      seeding = weight / IterAvg_Obj;
     }
     else {
       seeding = 0.0;
     }
   }
-
-  if (rank == MASTER_NODE){
+  if (rank == MASTER_NODE) {
     SU2_TYPE::SetDerivative(ObjFunc, SU2_TYPE::GetValue(seeding));
   } else {
     SU2_TYPE::SetDerivative(ObjFunc, 0.0);
diff --git a/SU2_CFD/src/integration/CStructuralIntegration.cpp b/SU2_CFD/src/integration/CStructuralIntegration.cpp
index 04b207f6fa0..276cf4a01bf 100644
--- a/SU2_CFD/src/integration/CStructuralIntegration.cpp
+++ b/SU2_CFD/src/integration/CStructuralIntegration.cpp
@@ -135,8 +135,6 @@ void CStructuralIntegration::Time_Integration_FEM(CGeometry *geometry, CSolver *
 
   switch (config->GetKind_TimeIntScheme_FEA()) {
     case (STRUCT_TIME_INT::CD_EXPLICIT):
-      solver_container[MainSolver]->ImplicitNewmark_Iteration(geometry, numerics, config);
-      break;
     case (STRUCT_TIME_INT::NEWMARK_IMPLICIT):
       solver_container[MainSolver]->ImplicitNewmark_Iteration(geometry, numerics, config);
       break;
@@ -161,7 +159,7 @@ void CStructuralIntegration::Time_Integration_FEM(CGeometry *geometry, CSolver *
     }
   }
 
-  /*--- Solver linear system ---*/
+  /*--- Solve linear system ---*/
 
   solver_container[MainSolver]->Solve_System(geometry, config);
 
@@ -169,8 +167,6 @@ void CStructuralIntegration::Time_Integration_FEM(CGeometry *geometry, CSolver *
 
   switch (config->GetKind_TimeIntScheme_FEA()) {
     case (STRUCT_TIME_INT::CD_EXPLICIT):
-      solver_container[MainSolver]->ImplicitNewmark_Update(geometry, config);
-      break;
     case (STRUCT_TIME_INT::NEWMARK_IMPLICIT):
       solver_container[MainSolver]->ImplicitNewmark_Update(geometry, config);
       break;
diff --git a/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
index 75ad91681f3..7decbd05b57 100644
--- a/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
@@ -56,7 +56,7 @@ CDiscAdjFEAIteration::CDiscAdjFEAIteration(const CConfig *config) : CIteration(c
       for (iVar = 0; iVar < config->GetnElectric_Field(); iVar++) myfile_res << "Sens_EField_" << iVar << "\t";
     }
 
-    myfile_res << '\n';
+    myfile_res << "\n";
   }
 }
 
@@ -66,7 +66,6 @@ void CDiscAdjFEAIteration::Preprocess(COutput* output, CIntegration**** integrat
                                       CSolver***** solver, CNumerics****** numerics, CConfig** config,
                                       CSurfaceMovement** surface_movement, CVolumetricMovement*** grid_movement,
                                       CFreeFormDefBox*** FFDBox, unsigned short iZone, unsigned short iInst) {
-  unsigned long iPoint;
   auto solvers0 = solver[iZone][iInst][MESH_0];
   auto geometry0 = geometry[iZone][iInst][MESH_0];
   auto dirNodes = solvers0[FEA_SOL]->GetNodes();
@@ -91,19 +90,12 @@ void CDiscAdjFEAIteration::Preprocess(COutput* output, CIntegration**** integrat
     /*--- Load solution timestep n ---*/
 
     LoadDynamic_Solution(geometry, solver, config, iZone, iInst, Direct_Iter);
+  }
 
-    /*--- Store FEA solution also in the adjoint solver in order to be able to reset it later ---*/
-
-    for (iPoint = 0; iPoint < geometry0->GetnPoint(); iPoint++) {
-      adjNodes->SetSolution_Direct(iPoint, dirNodes->GetSolution(iPoint));
-    }
+  /*--- Store FEA solution also in the adjoint solver in order to be able to reset it later. ---*/
 
-  } else {
-    /*--- Store FEA solution also in the adjoint solver in order to be able to reset it later ---*/
-
-    for (iPoint = 0; iPoint < geometry0->GetnPoint(); iPoint++) {
-      adjNodes->SetSolution_Direct(iPoint, dirNodes->GetSolution(iPoint));
-    }
+  for (auto iPoint = 0ul; iPoint < geometry0->GetnPoint(); iPoint++) {
+    adjNodes->SetSolution_Direct(iPoint, dirNodes->GetSolution(iPoint));
   }
 
   solvers0[ADJFEA_SOL]->Preprocessing(geometry0, solvers0, config[iZone], MESH_0, 0, RUNTIME_ADJFEA_SYS, false);
@@ -113,27 +105,19 @@ void CDiscAdjFEAIteration::Preprocess(COutput* output, CIntegration**** integrat
 void CDiscAdjFEAIteration::LoadDynamic_Solution(CGeometry**** geometry, CSolver***** solver, CConfig** config,
                                                 unsigned short iZone, unsigned short iInst,
                                                 int val_DirectIter) {
-  unsigned short iVar;
-  unsigned long iPoint;
-  bool update_geo = false;  // TODO: check
+  /*--- Set to false to prevent updating Solution_time_n when loading primal solutions of unsteady cases. ---*/
+  const bool update_geo = false;
+  auto*** solvers = solver[iZone][iInst];
 
   if (val_DirectIter >= 0) {
     if (rank == MASTER_NODE && iZone == ZONE_0)
-      cout << " Loading FEA solution from direct iteration " << val_DirectIter << "." << endl;
-    solver[iZone][iInst][MESH_0][FEA_SOL]->LoadRestart(
-        geometry[iZone][iInst], solver[iZone][iInst], config[iZone], val_DirectIter, update_geo);
+      cout << " Loading FEA solution from direct iteration " << val_DirectIter << ".\n";
+    solvers[MESH_0][FEA_SOL]->LoadRestart(geometry[iZone][iInst], solvers, config[iZone], val_DirectIter, update_geo);
   } else {
-    /*--- If there is no solution file we set the freestream condition ---*/
+    /*--- If there is no solution file we set the initial conditions. ---*/
     if (rank == MASTER_NODE && iZone == ZONE_0)
-      cout << " Setting static conditions at direct iteration " << val_DirectIter << "." << endl;
-    /*--- Push solution back to correct array ---*/
-    for (iPoint = 0; iPoint < geometry[iZone][iInst][MESH_0]->GetnPoint(); iPoint++) {
-      for (iVar = 0; iVar < solver[iZone][iInst][MESH_0][FEA_SOL]->GetnVar(); iVar++) {
-        solver[iZone][iInst][MESH_0][FEA_SOL]->GetNodes()->SetSolution(iPoint, iVar, 0.0);
-        solver[iZone][iInst][MESH_0][FEA_SOL]->GetNodes()->SetSolution_Accel(iPoint, iVar, 0.0);
-        solver[iZone][iInst][MESH_0][FEA_SOL]->GetNodes()->SetSolution_Vel(iPoint, iVar, 0.0);
-      }
-    }
+      cout << " Setting static conditions at direct iteration " << val_DirectIter << ".\n";
+    solvers[MESH_0][FEA_SOL]->SetInitialCondition(geometry[iZone][iInst], solvers, config[iZone], val_DirectIter);
   }
 }
 
@@ -354,9 +338,7 @@ void CDiscAdjFEAIteration::Postprocess(COutput* output, CIntegration**** integra
       myfile_res << scientific << solvers0[ADJFEA_SOL]->GetTotal_Sens_DVFEA(iVar) << "\t";
     }
 
-    myfile_res << endl;
-
-    myfile_res.close();
+    myfile_res << "\n";
   }
 
   // TEST: for implementation of python framework in standalone structural problems
@@ -385,23 +367,14 @@ void CDiscAdjFEAIteration::Postprocess(COutput* output, CIntegration**** integra
     }
 
     if (outputDVFEA) {
-      unsigned short iDV;
-      unsigned short nDV = solvers0[ADJFEA_SOL]->GetnDVFEA();
-
-      myfile_res << "INDEX"
-                 << "\t"
-                 << "GRAD" << endl;
-
+      const auto nDV = solvers0[ADJFEA_SOL]->GetnDVFEA();
+      myfile_res << "INDEX\tGRAD\n";
       myfile_res.precision(15);
 
-      for (iDV = 0; iDV < nDV; iDV++) {
-        myfile_res << iDV;
-        myfile_res << "\t";
-        myfile_res << scientific << solvers0[ADJFEA_SOL]->GetTotal_Sens_DVFEA(iDV);
-        myfile_res << endl;
+      for (auto iDV = 0u; iDV < nDV; iDV++) {
+        myfile_res << iDV << "\t";
+        myfile_res << scientific << solvers0[ADJFEA_SOL]->GetTotal_Sens_DVFEA(iDV) << "\n";
       }
-
-      myfile_res.close();
     }
   }
 }
diff --git a/SU2_CFD/src/iteration/CFEAIteration.cpp b/SU2_CFD/src/iteration/CFEAIteration.cpp
index 973f3600c6d..91b9e715681 100644
--- a/SU2_CFD/src/iteration/CFEAIteration.cpp
+++ b/SU2_CFD/src/iteration/CFEAIteration.cpp
@@ -69,8 +69,8 @@ void CFEAIteration::Iterate(COutput* output, CIntegration**** integration, CGeom
   } else if (nonlinear && !incremental_load) {
     /*--- THIS IS THE DIRECT APPROACH (NO INCREMENTAL LOAD APPLIED) ---*/
 
-    /*--- Keep the current inner iter, we need to restore it in discrete adjoint cases as file output depends on it
-     * ---*/
+    /*--- Keep the current inner iter, we need to restore it in discrete adjoint cases
+     * because file output depends on it. ---*/
     const auto CurIter = config[val_iZone]->GetInnerIter();
 
     /*--- Newton-Raphson subiterations ---*/
@@ -84,11 +84,11 @@ void CFEAIteration::Iterate(COutput* output, CIntegration**** integration, CGeom
       if (disc_adj_fem) {
         config[val_iZone]->SetInnerIter(CurIter);
         break;
-      }         StopCalc = Monitor(output, integration, geometry, solver, numerics, config, surface_movement, grid_movement,
-                           FFDBox, val_iZone, INST_0);
+      }
+      StopCalc = Monitor(output, integration, geometry, solver, numerics, config, surface_movement, grid_movement,
+                         FFDBox, val_iZone, INST_0);
 
-        if (StopCalc && (IntIter > 0)) break;
-     
+      if (StopCalc && (IntIter > 0)) break;
     }
 
   } else {
@@ -101,13 +101,16 @@ void CFEAIteration::Iterate(COutput* output, CIntegration**** integration, CGeom
 
     /*--- Run two nonlinear iterations to check if incremental loading can be skipped ---*/
 
-    for (IntIter = 0; IntIter < 2; ++IntIter) {
+    auto Iterate = [&](unsigned long IntIter) {
       config[val_iZone]->SetInnerIter(IntIter);
-
       feaIntegration->Structural_Iteration(geometry, solver, numerics, config, RUNTIME_FEA_SYS, val_iZone, val_iInst);
 
       StopCalc = Monitor(output, integration, geometry, solver, numerics, config, surface_movement, grid_movement,
                          FFDBox, val_iZone, INST_0);
+    };
+
+    for (IntIter = 0; IntIter < 2; ++IntIter) {
+      Iterate(IntIter);
     }
 
     /*--- Early return if we already meet the convergence criteria. ---*/
@@ -125,13 +128,7 @@ void CFEAIteration::Iterate(COutput* output, CIntegration**** integration, CGeom
       /*--- Newton-Raphson subiterations ---*/
 
       for (IntIter = 2; IntIter < config[val_iZone]->GetnInner_Iter(); IntIter++) {
-        config[val_iZone]->SetInnerIter(IntIter);
-
-        feaIntegration->Structural_Iteration(geometry, solver, numerics, config, RUNTIME_FEA_SYS, val_iZone, val_iInst);
-
-        StopCalc = Monitor(output, integration, geometry, solver, numerics, config, surface_movement, grid_movement,
-                           FFDBox, val_iZone, INST_0);
-
+        Iterate(IntIter);
         if (StopCalc) break;
       }
 
@@ -162,14 +159,7 @@ void CFEAIteration::Iterate(COutput* output, CIntegration**** integration, CGeom
         /*--- Newton-Raphson subiterations ---*/
 
         for (IntIter = 0; IntIter < config[val_iZone]->GetnInner_Iter(); IntIter++) {
-          config[val_iZone]->SetInnerIter(IntIter);
-
-          feaIntegration->Structural_Iteration(geometry, solver, numerics, config, RUNTIME_FEA_SYS, val_iZone,
-                                               val_iInst);
-
-          StopCalc = Monitor(output, integration, geometry, solver, numerics, config, surface_movement, grid_movement,
-                             FFDBox, val_iZone, INST_0);
-
+          Iterate(IntIter);
           if (StopCalc && (IntIter > 0)) break;
         }
       }
diff --git a/SU2_CFD/src/solvers/CFEASolver.cpp b/SU2_CFD/src/solvers/CFEASolver.cpp
index 74870622ea0..07018b95233 100644
--- a/SU2_CFD/src/solvers/CFEASolver.cpp
+++ b/SU2_CFD/src/solvers/CFEASolver.cpp
@@ -615,8 +615,8 @@ void CFEASolver::SetInitialCondition(CGeometry **geometry, CSolver ***solver_con
 
   SU2_OMP_PARALLEL
   {
+  su2double zeros[MAXNVAR] = {0.0};
   if (!config->GetPrestretch()) {
-    su2double zeros[MAXNVAR] = {0.0};
     SU2_OMP_FOR_STAT(omp_chunk_size)
     for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint)
       nodes->SetSolution(iPoint, zeros);
@@ -628,6 +628,14 @@ void CFEASolver::SetInitialCondition(CGeometry **geometry, CSolver ***solver_con
       nodes->SetSolution(iPoint, nodes->GetPrestretch(iPoint));
     END_SU2_OMP_FOR
   }
+  if (config->GetTime_Domain()) {
+    SU2_OMP_FOR_STAT(omp_chunk_size)
+    for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint) {
+      nodes->SetSolution_Vel(iPoint, zeros);
+      nodes->SetSolution_Accel(iPoint, zeros);
+    }
+    END_SU2_OMP_FOR
+  }
   }
   END_SU2_OMP_PARALLEL
 }
@@ -3108,8 +3116,8 @@ void CFEASolver::LoadRestart(CGeometry **geometry, CSolver ***solver, CConfig *c
   /*--- Detect a wrong solution file. ---*/
 
   if (counter != nPointDomain) {
-    SU2_MPI::Error(string("The solution file ") + filename + string(" doesn't match with the mesh file!\n") +
-                   string("It could be empty lines at the end of the file."), CURRENT_FUNCTION);
+    SU2_MPI::Error("The solution file " + filename + " doesn't match with the mesh file!\n"
+                   "It could be empty lines at the end of the file.", CURRENT_FUNCTION);
   }
 
   /*--- MPI. If dynamic, we also need to communicate the old solution. ---*/
@@ -3117,7 +3125,9 @@ void CFEASolver::LoadRestart(CGeometry **geometry, CSolver ***solver, CConfig *c
   InitiateComms(geometry[MESH_0], config, SOLUTION_FEA);
   CompleteComms(geometry[MESH_0], config, SOLUTION_FEA);
 
-  if (dynamic) nodes->Set_Solution_time_n();
+  /*--- It's important to not push back the solution when this function is used to load solutions for
+   * unsteady discrete adjoints, otherwise we overwrite one of the two solutions needed. ---*/
+  if (dynamic && val_update_geo) nodes->Set_Solution_time_n();
 
   if (fluid_structure) {
     for (auto iPoint = 0ul; iPoint < nPoint; ++iPoint) {

From 8d2b09697a3b39ae33a5ae04ae566be5fe33d275 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Sat, 15 Apr 2023 21:00:27 -0700
Subject: [PATCH 398/656] Update
 SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp

---
 SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp | 2 --
 1 file changed, 2 deletions(-)

diff --git a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
index 0a2a77ae31f..6277f409b8d 100644
--- a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
@@ -780,8 +780,6 @@ void CDiscAdjMultizoneDriver::SetAdjObjFunction() {
   }
   if (rank == MASTER_NODE) {
     AD::SetDerivative(ObjFunc_Index, SU2_TYPE::GetValue(seeding));
-  } else {
-    AD::SetDerivative(ObjFunc_Index, 0.0);
   }
 }
 

From 355d5e00d3a60e22e6efde8026469c49487d6506 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 16 Apr 2023 18:14:31 -0700
Subject: [PATCH 399/656] add unsteady FEA ad testcase

---
 .../py_wrapper/custom_load_fea/run_ad.py      | 221 ++++++++++++++++++
 TestCases/serial_regression_AD.py             |  13 ++
 2 files changed, 234 insertions(+)
 create mode 100644 TestCases/py_wrapper/custom_load_fea/run_ad.py

diff --git a/TestCases/py_wrapper/custom_load_fea/run_ad.py b/TestCases/py_wrapper/custom_load_fea/run_ad.py
new file mode 100644
index 00000000000..c39e05234d8
--- /dev/null
+++ b/TestCases/py_wrapper/custom_load_fea/run_ad.py
@@ -0,0 +1,221 @@
+#!/usr/bin/env python
+
+## \file run.py
+#  \brief Unsteady adjoint FEA case with custom load.
+#  \version 7.5.1 "Blackbird"
+#
+# SU2 Project Website: https://su2code.github.io
+#
+# The SU2 Project is maintained by the SU2 Foundation
+# (http://su2foundation.org)
+#
+# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
+#
+# SU2 is free software; you can redistribute it and/or
+# modify it under the terms of the GNU Lesser General Public
+# License as published by the Free Software Foundation; either
+# version 2.1 of the License, or (at your option) any later version.
+#
+# SU2 is distributed in the hope that it will be useful,
+# but WITHOUT ANY WARRANTY; without even the implied warranty of
+# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+# Lesser General Public License for more details.
+#
+# You should have received a copy of the GNU Lesser General Public
+# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+
+import pysu2ad
+from mpi4py import MPI
+
+common_settings = """
+SOLVER= ELASTICITY
+GEOMETRIC_CONDITIONS= LARGE_DEFORMATIONS
+FORMULATION_ELASTICITY_2D= PLANE_STRESS
+
+TIME_DOMAIN= YES
+TIME_STEP=0.01
+TIME_DISCRE_FEA= NEWMARK_IMPLICIT
+NEWMARK_GAMMA= 0.5
+NEWMARK_BETA= 0.25
+
+MATERIAL_MODEL= NEO_HOOKEAN
+ELASTICITY_MODULUS= 10000
+POISSON_RATIO= 0.3
+MATERIAL_DENSITY= __DENSITY__
+
+MARKER_CLAMPED= ( x_minus )
+MARKER_FLUID_LOAD= ( x_plus, y_minus, y_plus )
+
+LINEAR_SOLVER= CONJUGATE_GRADIENT
+DISCADJ_LIN_SOLVER= CONJUGATE_GRADIENT
+LINEAR_SOLVER_PREC= ILU
+DISCADJ_LIN_PREC= ILU
+LINEAR_SOLVER_ERROR= 1E-5
+LINEAR_SOLVER_ITER= 100
+
+MESH_FORMAT= RECTANGLE
+MESH_BOX_SIZE= ( 17, 5, 0 )
+MESH_BOX_LENGTH= ( 0.5, 0.05, 0 )
+
+OUTPUT_FILES= RESTART, PARAVIEW
+OUTPUT_WRT_FREQ= 1
+OBJECTIVE_FUNCTION= STRESS_PENALTY
+STRESS_PENALTY_PARAM= ( 500, 20 )
+
+INNER_ITER= 20
+CONV_RESIDUAL_MINVAL= -4
+CONV_STARTITER= 5
+MAX_TIME= 0.2
+TIME_ITER= 21
+"""
+
+primal_settings = """
+MATH_PROBLEM= DIRECT
+SCREEN_OUTPUT= TIME_ITER, CUR_TIME, INNER_ITER, RMS_RES, LINSOL, VMS, STRESS_PENALTY, TAVG_STRESS_PENALTY
+HISTORY_OUTPUT= ITER, RMS_RES, STRUCT_COEFF, TAVG_STRUCT_COEFF
+CONV_FIELD= REL_RMS_RTOL
+"""
+
+adjoint_settings = """
+MATH_PROBLEM= DISCRETE_ADJOINT
+SCREEN_OUTPUT= TIME_ITER, CUR_TIME, INNER_ITER, ADJOINT_DISP_X, ADJOINT_DISP_Y, LINSOL, SENSITIVITY
+CONV_FIELD= ADJOINT_DISP_X, ADJOINT_DISP_Y
+FEA_ADVANCED_MODE= YES
+UNST_ADJOINT_ITER= 21
+ITER_AVERAGE_OBJ= 0
+SOLUTION_FILENAME= restart.dat
+"""
+
+
+def ApplyLoad(driver, marker_id, peak_load):
+  """
+  Apply a load based on the coordinates and return the derivatives
+  of the nodal forces with respect to the peak load.
+  """
+  derivatives = []
+  if marker_id < 0: return
+
+  marker_coords = driver.MarkerCoordinates(marker_id)
+  l = 0.5
+  dx = l / 16 # known from mesh settings in this case.
+  for i_vertex in range(driver.GetNumberMarkerNodes(marker_id)):
+    x = marker_coords(i_vertex, 0)
+    nodal_force = (peak_load * x / l) * dx
+    # Half load due to half dx on first and last node.
+    if abs(x) < 1e-6 or abs(x - l) < 1e-6:
+      nodal_force = nodal_force / 2
+    driver.SetMarkerCustomFEALoad(marker_id, i_vertex, (0, nodal_force))
+    derivatives.append(nodal_force / peak_load)
+
+  return derivatives
+
+
+def RunPrimal(density, peak_load):
+  """Runs the primal solver for a given density and peak load and returns the time average objective function."""
+  comm = MPI.COMM_WORLD
+
+  with open('config_unsteady.cfg', 'w') as f:
+    f.write(common_settings.replace('__DENSITY__', str(density)) + primal_settings)
+
+  # Initialize the primal driver of SU2, this includes solver preprocessing.
+  try:
+    driver = pysu2ad.CSinglezoneDriver('config_unsteady.cfg', 1, comm)
+  except TypeError as exception:
+    print('A TypeError occured in pysu2ad.CSinglezoneDriver : ', exception)
+    raise
+
+  # Get the ID of the marker where the load is applied.
+  all_marker_ids = driver.GetMarkerIndices()
+  marker_name = 'y_minus'
+  marker_id = all_marker_ids[marker_name] if marker_name in all_marker_ids else -1
+
+  # Apply a load based on the coordinates.
+  ApplyLoad(driver, marker_id, peak_load)
+
+  # Solve.
+  driver.StartSolver()
+
+  # Get the time average
+  tavg_stress_penalty = driver.GetOutputValue('TAVG_STRESS_PENALTY')
+
+  # Finalize the solver and exit cleanly.
+  driver.Finalize()
+
+  return tavg_stress_penalty
+
+
+def RunAdjoint(density, peak_load):
+  """Runs the adjoint solver and returns the sensitivity of the objective function to the peak load."""
+  comm = MPI.COMM_WORLD
+
+  with open('config_unsteady_ad.cfg', 'w') as f:
+    f.write(common_settings.replace('__DENSITY__', str(density)) + adjoint_settings)
+
+  # Initialize the adjoint driver of SU2, this includes solver preprocessing.
+  try:
+    driver = pysu2ad.CDiscAdjSinglezoneDriver('config_unsteady_ad.cfg', 1, comm)
+  except TypeError as exception:
+    print('A TypeError occured in pysu2ad.CDiscAdjSinglezoneDriver : ', exception)
+    raise
+
+  # Get the ID of the marker where the load is applied.
+  all_marker_ids = driver.GetMarkerIndices()
+  marker_name = 'y_minus'
+  marker_id = all_marker_ids[marker_name] if marker_name in all_marker_ids else -1
+
+  # Apply the same load that was used in the primal problem.
+  derivatives = ApplyLoad(driver, marker_id, peak_load)
+
+  n_vertex = driver.GetNumberMarkerNodes(marker_id) if marker_id >= 0 else 0
+  load_sens = 0.0
+
+  # Run the time loop in python to extract sensitivities at each step.
+  for time_iter in range(driver.GetNumberTimeIter()):
+    # Preprocess adjoint iteration (AD recording).
+    driver.Preprocess(time_iter)
+
+    # Run one time iteration.
+    driver.Run()
+    driver.Postprocess()
+    driver.Update()
+
+    # Accumulate sensitivies.
+    for i_vertex in range(n_vertex):
+      load_sens += derivatives[i_vertex] * driver.GetMarkerFEALoadSensitivity(marker_id, i_vertex)[1]
+
+    # Monitor the solver and output solution to file if required.
+    driver.Monitor(time_iter)
+    driver.Output(time_iter)
+
+  # Finalize the solver and exit cleanly.
+  driver.Finalize()
+
+  return load_sens
+
+
+def main():
+  # Run the primal with 2 loads to compute the sensitivity via finite differences.
+  obj_pert_load = RunPrimal(1, 2.002)
+  obj_pert_rho = RunPrimal(1.0001, 2)
+  obj = RunPrimal(1, 2)
+  sens_load_fd = (obj_pert_load - obj) / 0.002
+  sens_rho_fd = (obj_pert_rho - obj) / 0.0001
+
+  sens_load = RunAdjoint(1, 2)
+  # Read the density sensitivity from the special output file.
+  with open('Results_Reverse_Adjoint.txt') as f:
+    sens_rho = float(f.readlines()[-1].strip().split('\t')[-1])
+
+  print("      Finite Differences\tDiscrete Adjoint")
+  print(f"Load  {sens_load_fd}\t{sens_load}")
+  print(f"Rho   {sens_rho_fd}\t{sens_rho}")
+
+  assert abs(sens_load / sens_load_fd - 1) < 1e-4, "Error in load derivative."
+  assert abs(sens_rho / sens_rho_fd - 1) < 1e-3, "Error in density derivative."
+
+  # Print results for the regression script to check.
+  print(100, 100, sens_load_fd, sens_load, sens_rho_fd, sens_rho)
+
+
+if __name__ == '__main__':
+  main()
diff --git a/TestCases/serial_regression_AD.py b/TestCases/serial_regression_AD.py
index d9885b1dcd1..dce2b58b25a 100644
--- a/TestCases/serial_regression_AD.py
+++ b/TestCases/serial_regression_AD.py
@@ -343,6 +343,19 @@ def main():
     test_list.append(pywrapper_FEA_AD_FlowLoad)
     pass_list.append(pywrapper_FEA_AD_FlowLoad.run_test())
 
+    # FEA unsteady AD Load Sensitivity
+    pywrapper_Unst_FEA_AD = TestCase('pywrapper_Unst_FEA_AD')
+    pywrapper_Unst_FEA_AD.cfg_dir = "py_wrapper/custom_load_fea"
+    pywrapper_Unst_FEA_AD.cfg_file = "config.cfg"
+    pywrapper_Unst_FEA_AD.test_iter = 100
+    pywrapper_Unst_FEA_AD.test_vals = [0.2569256889872473, 0.256926360722213, 0.03166391031539373, 0.0316910814265723]
+    pywrapper_Unst_FEA_AD.command = TestCase.Command(exec = "python", param = "run_ad.py")
+    pywrapper_Unst_FEA_AD.timeout = 1600
+    pywrapper_Unst_FEA_AD.tol = 0.00001
+    pywrapper_Unst_FEA_AD.new_output = False
+    test_list.append(pywrapper_Unst_FEA_AD)
+    pass_list.append(pywrapper_Unst_FEA_AD.run_test())
+
     # Flow AD Mesh Displacement Sensitivity
     pywrapper_CFD_AD_MeshDisp               = TestCase('pywrapper_CFD_AD_MeshDisp')
     pywrapper_CFD_AD_MeshDisp.cfg_dir       = "py_wrapper/disc_adj_flow/mesh_disp_sens"

From ee9ef29328909c55d589e18123c203b01fcbc274 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 16 Apr 2023 18:21:41 -0700
Subject: [PATCH 400/656] fix warning

---
 TestCases/py_wrapper/custom_load_fea/run_ad.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/py_wrapper/custom_load_fea/run_ad.py b/TestCases/py_wrapper/custom_load_fea/run_ad.py
index c39e05234d8..9e1f8e4a7b6 100644
--- a/TestCases/py_wrapper/custom_load_fea/run_ad.py
+++ b/TestCases/py_wrapper/custom_load_fea/run_ad.py
@@ -93,7 +93,7 @@ def ApplyLoad(driver, marker_id, peak_load):
   of the nodal forces with respect to the peak load.
   """
   derivatives = []
-  if marker_id < 0: return
+  if marker_id < 0: return derivatives
 
   marker_coords = driver.MarkerCoordinates(marker_id)
   l = 0.5

From b06ebdb2cc369b57af6ba363fb1bb9439af830fd Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 16 Apr 2023 18:30:17 -0700
Subject: [PATCH 401/656] remove CD explicit as it is not implemented

---
 Common/include/option_structure.hpp                | 2 --
 Common/src/CConfig.cpp                             | 3 ---
 SU2_CFD/src/integration/CStructuralIntegration.cpp | 4 ----
 SU2_CFD/src/solvers/CFEASolver.cpp                 | 6 ------
 4 files changed, 15 deletions(-)

diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index f08925fd40b..e661b451d1b 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -1434,12 +1434,10 @@ static const MapType<std::string, ENUM_HEAT_TIMESTEP> Heat_TimeStep_Map = {
  * \brief Type of time integration schemes
  */
 enum class STRUCT_TIME_INT {
-  CD_EXPLICIT,       /*!< \brief Support for implementing an explicit method. */
   NEWMARK_IMPLICIT,  /*!< \brief Implicit Newmark integration definition. */
   GENERALIZED_ALPHA, /*!< \brief Support for implementing another implicit method. */
 };
 static const MapType<std::string, STRUCT_TIME_INT> Time_Int_Map_FEA = {
-  MakePair("CD_EXPLICIT", STRUCT_TIME_INT::CD_EXPLICIT)
   MakePair("NEWMARK_IMPLICIT", STRUCT_TIME_INT::NEWMARK_IMPLICIT)
   MakePair("GENERALIZED_ALPHA", STRUCT_TIME_INT::GENERALIZED_ALPHA)
 };
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index e2d1e37cee0..4458e846616 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -6870,9 +6870,6 @@ void CConfig::SetOutput(SU2_COMPONENT val_software, unsigned short val_izone) {
 
     if (fea) {
       switch (Kind_TimeIntScheme_FEA) {
-        case STRUCT_TIME_INT::CD_EXPLICIT:
-          cout << "Explicit time integration (NOT IMPLEMENTED YET)." << endl;
-          break;
         case STRUCT_TIME_INT::GENERALIZED_ALPHA:
           cout << "Generalized-alpha method." << endl;
           break;
diff --git a/SU2_CFD/src/integration/CStructuralIntegration.cpp b/SU2_CFD/src/integration/CStructuralIntegration.cpp
index 276cf4a01bf..5fc18babb3f 100644
--- a/SU2_CFD/src/integration/CStructuralIntegration.cpp
+++ b/SU2_CFD/src/integration/CStructuralIntegration.cpp
@@ -134,7 +134,6 @@ void CStructuralIntegration::Time_Integration_FEM(CGeometry *geometry, CSolver *
   /*--- Set the Jacobian according to the different time integration methods ---*/
 
   switch (config->GetKind_TimeIntScheme_FEA()) {
-    case (STRUCT_TIME_INT::CD_EXPLICIT):
     case (STRUCT_TIME_INT::NEWMARK_IMPLICIT):
       solver_container[MainSolver]->ImplicitNewmark_Iteration(geometry, numerics, config);
       break;
@@ -166,7 +165,6 @@ void CStructuralIntegration::Time_Integration_FEM(CGeometry *geometry, CSolver *
   /*--- Update solution ---*/
 
   switch (config->GetKind_TimeIntScheme_FEA()) {
-    case (STRUCT_TIME_INT::CD_EXPLICIT):
     case (STRUCT_TIME_INT::NEWMARK_IMPLICIT):
       solver_container[MainSolver]->ImplicitNewmark_Update(geometry, config);
       break;
@@ -194,8 +192,6 @@ void CStructuralIntegration::SetDualTime_Solver(const CGeometry *geometry, CSolv
   /*--- Update the solution according to the integration scheme used ---*/
 
   switch (config->GetKind_TimeIntScheme_FEA()) {
-    case (STRUCT_TIME_INT::CD_EXPLICIT):
-      break;
     case (STRUCT_TIME_INT::NEWMARK_IMPLICIT):
       if (fsi && config->GetRelaxation()) solver->ImplicitNewmark_Relaxation(geometry, config);
       break;
diff --git a/SU2_CFD/src/solvers/CFEASolver.cpp b/SU2_CFD/src/solvers/CFEASolver.cpp
index 07018b95233..e4877179706 100644
--- a/SU2_CFD/src/solvers/CFEASolver.cpp
+++ b/SU2_CFD/src/solvers/CFEASolver.cpp
@@ -1340,9 +1340,6 @@ void CFEASolver::Compute_NodalStress(CGeometry *geometry, CNumerics **numerics,
     else if (dynamic) {
 
       switch (config->GetKind_TimeIntScheme_FEA()) {
-        case (STRUCT_TIME_INT::CD_EXPLICIT):
-          cout << "NOT IMPLEMENTED YET" << endl;
-          break;
         case (STRUCT_TIME_INT::NEWMARK_IMPLICIT):
 
           /*--- Loop over all points, and set aux vector TimeRes_Aux = a0*U+a2*U'+a3*U'' ---*/
@@ -1495,9 +1492,6 @@ void CFEASolver::Compute_IntegrationConstants(const CConfig *config) {
   su2double gamma = config->GetNewmark_gamma(), beta = config->GetNewmark_beta();
 
   switch (config->GetKind_TimeIntScheme_FEA()) {
-    case (STRUCT_TIME_INT::CD_EXPLICIT):
-      cout << "NOT IMPLEMENTED YET" << endl;
-      break;
     case (STRUCT_TIME_INT::NEWMARK_IMPLICIT):
 
       /*--- Integration constants for Newmark scheme ---*/

From bd95febb7e369379834efd7a87e175e121432b09 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Mon, 17 Apr 2023 11:58:07 -0700
Subject: [PATCH 402/656] parallel test instead of serial

---
 TestCases/parallel_regression_AD.py            | 13 +++++++++++++
 TestCases/py_wrapper/custom_load_fea/run_ad.py | 16 +++++++++++-----
 TestCases/serial_regression_AD.py              | 13 -------------
 3 files changed, 24 insertions(+), 18 deletions(-)

diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index a67de6139db..1ea499b38b6 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -408,6 +408,19 @@ def main():
     test_list.append(pywrapper_FEA_AD_FlowLoad)
     pass_list.append(pywrapper_FEA_AD_FlowLoad.run_test())
 
+    # FEA unsteady AD Load Sensitivity
+    pywrapper_Unst_FEA_AD = TestCase('pywrapper_Unst_FEA_AD')
+    pywrapper_Unst_FEA_AD.cfg_dir = "py_wrapper/custom_load_fea"
+    pywrapper_Unst_FEA_AD.cfg_file = "config.cfg"
+    pywrapper_Unst_FEA_AD.test_iter = 100
+    pywrapper_Unst_FEA_AD.test_vals = [0.2569257, 0.2569264, 0.03166391, 0.03169108]
+    pywrapper_Unst_FEA_AD.command = TestCase.Command("mpirun -n 2", "python", "run_ad.py")
+    pywrapper_Unst_FEA_AD.timeout = 1600
+    pywrapper_Unst_FEA_AD.tol = 0.00001
+    pywrapper_Unst_FEA_AD.new_output = False
+    test_list.append(pywrapper_Unst_FEA_AD)
+    pass_list.append(pywrapper_Unst_FEA_AD.run_test())
+
     # Flow AD Mesh Displacement Sensitivity
     pywrapper_CFD_AD_MeshDisp               = TestCase('pywrapper_CFD_AD_MeshDisp')
     pywrapper_CFD_AD_MeshDisp.cfg_dir       = "py_wrapper/disc_adj_flow/mesh_disp_sens"
diff --git a/TestCases/py_wrapper/custom_load_fea/run_ad.py b/TestCases/py_wrapper/custom_load_fea/run_ad.py
index 9e1f8e4a7b6..92e454083b3 100644
--- a/TestCases/py_wrapper/custom_load_fea/run_ad.py
+++ b/TestCases/py_wrapper/custom_load_fea/run_ad.py
@@ -190,10 +190,13 @@ def RunAdjoint(density, peak_load):
   # Finalize the solver and exit cleanly.
   driver.Finalize()
 
-  return load_sens
+  return comm.allreduce(load_sens)
 
 
 def main():
+  comm = MPI.COMM_WORLD
+  rank = comm.Get_rank()
+
   # Run the primal with 2 loads to compute the sensitivity via finite differences.
   obj_pert_load = RunPrimal(1, 2.002)
   obj_pert_rho = RunPrimal(1.0001, 2)
@@ -206,15 +209,18 @@ def main():
   with open('Results_Reverse_Adjoint.txt') as f:
     sens_rho = float(f.readlines()[-1].strip().split('\t')[-1])
 
-  print("      Finite Differences\tDiscrete Adjoint")
-  print(f"Load  {sens_load_fd}\t{sens_load}")
-  print(f"Rho   {sens_rho_fd}\t{sens_rho}")
+  if rank == 0:
+    print("      Finite Differences\tDiscrete Adjoint")
+    print(f"Load  {sens_load_fd}\t{sens_load}")
+    print(f"Rho   {sens_rho_fd}\t{sens_rho}")
 
   assert abs(sens_load / sens_load_fd - 1) < 1e-4, "Error in load derivative."
   assert abs(sens_rho / sens_rho_fd - 1) < 1e-3, "Error in density derivative."
 
   # Print results for the regression script to check.
-  print(100, 100, sens_load_fd, sens_load, sens_rho_fd, sens_rho)
+  if rank == 0:
+    print("\n")
+    print(100, 100, sens_load_fd, sens_load, sens_rho_fd, sens_rho)
 
 
 if __name__ == '__main__':
diff --git a/TestCases/serial_regression_AD.py b/TestCases/serial_regression_AD.py
index dce2b58b25a..d9885b1dcd1 100644
--- a/TestCases/serial_regression_AD.py
+++ b/TestCases/serial_regression_AD.py
@@ -343,19 +343,6 @@ def main():
     test_list.append(pywrapper_FEA_AD_FlowLoad)
     pass_list.append(pywrapper_FEA_AD_FlowLoad.run_test())
 
-    # FEA unsteady AD Load Sensitivity
-    pywrapper_Unst_FEA_AD = TestCase('pywrapper_Unst_FEA_AD')
-    pywrapper_Unst_FEA_AD.cfg_dir = "py_wrapper/custom_load_fea"
-    pywrapper_Unst_FEA_AD.cfg_file = "config.cfg"
-    pywrapper_Unst_FEA_AD.test_iter = 100
-    pywrapper_Unst_FEA_AD.test_vals = [0.2569256889872473, 0.256926360722213, 0.03166391031539373, 0.0316910814265723]
-    pywrapper_Unst_FEA_AD.command = TestCase.Command(exec = "python", param = "run_ad.py")
-    pywrapper_Unst_FEA_AD.timeout = 1600
-    pywrapper_Unst_FEA_AD.tol = 0.00001
-    pywrapper_Unst_FEA_AD.new_output = False
-    test_list.append(pywrapper_Unst_FEA_AD)
-    pass_list.append(pywrapper_Unst_FEA_AD.run_test())
-
     # Flow AD Mesh Displacement Sensitivity
     pywrapper_CFD_AD_MeshDisp               = TestCase('pywrapper_CFD_AD_MeshDisp')
     pywrapper_CFD_AD_MeshDisp.cfg_dir       = "py_wrapper/disc_adj_flow/mesh_disp_sens"

From 9cd53506214563d07731839081c53bad55f9165c Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Mon, 17 Apr 2023 12:37:35 -0700
Subject: [PATCH 403/656] update values

---
 TestCases/parallel_regression_AD.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index 1ea499b38b6..772b7012db7 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -413,7 +413,7 @@ def main():
     pywrapper_Unst_FEA_AD.cfg_dir = "py_wrapper/custom_load_fea"
     pywrapper_Unst_FEA_AD.cfg_file = "config.cfg"
     pywrapper_Unst_FEA_AD.test_iter = 100
-    pywrapper_Unst_FEA_AD.test_vals = [0.2569257, 0.2569264, 0.03166391, 0.03169108]
+    pywrapper_Unst_FEA_AD.test_vals = [0.256684, 0.256684, 0.031988, 0.032015]
     pywrapper_Unst_FEA_AD.command = TestCase.Command("mpirun -n 2", "python", "run_ad.py")
     pywrapper_Unst_FEA_AD.timeout = 1600
     pywrapper_Unst_FEA_AD.tol = 0.00001

From e2a406076412cbfda9f1b528d95cf9345c368fda Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 19 Apr 2023 16:09:46 +0200
Subject: [PATCH 404/656] CoDiPack update.

---
 externals/codi        | 2 +-
 meson_scripts/init.py | 2 +-
 2 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/externals/codi b/externals/codi
index ca5573d50f9..21e4f6e084d 160000
--- a/externals/codi
+++ b/externals/codi
@@ -1 +1 @@
-Subproject commit ca5573d50f9a54ba50d28a8639822a56d556240b
+Subproject commit 21e4f6e084d635e7834ca55dc9d83b667a5aca2b
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 7b6ea828bd4..47f5841a74a 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -54,7 +54,7 @@ def init_submodules(
 
     # This information of the modules is used if projects was not cloned using git
     # The sha tag must be maintained manually to point to the correct commit
-    sha_version_codi = "ca5573d50f9a54ba50d28a8639822a56d556240b"
+    sha_version_codi = "21e4f6e084d635e7834ca55dc9d83b667a5aca2b"
     github_repo_codi = "https://github.com/scicompkl/CoDiPack"
     sha_version_medi = "aafc2d1966ba1233640af737e71c77c1a86183fd"
     github_repo_medi = "https://github.com/SciCompKL/MeDiPack"

From 9b28e74216891cf914d5a5bb6a6a9f2efcdf8e9d Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Wed, 19 Apr 2023 18:55:30 -0700
Subject: [PATCH 405/656] cleanup the time integration of fea material
 sensitivities

---
 Common/include/CConfig.hpp                    |  30 +----
 Common/src/CConfig.cpp                        |   5 +
 SU2_CFD/include/solvers/CDiscAdjFEASolver.hpp |  52 +++------
 SU2_CFD/include/solvers/CSolver.hpp           |  36 ------
 .../src/iteration/CDiscAdjFEAIteration.cpp    | 109 +++++-------------
 .../numerics/elasticity/CFEAElasticity.cpp    |   8 +-
 SU2_CFD/src/output/CAdjElasticityOutput.cpp   |  75 +++++++-----
 SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp     |  11 +-
 SU2_CFD/src/solvers/CFEASolver.cpp            |   4 +-
 SU2_PY/SU2/io/historyMap.py                   |   8 +-
 TestCases/disc_adj_fsi/Airfoil_2d/config.cfg  |   2 +-
 TestCases/disc_adj_fsi/config.cfg             |   2 +-
 .../py_wrapper/custom_load_fea/run_ad.py      |  14 ++-
 13 files changed, 125 insertions(+), 231 deletions(-)

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index 14acb60ec69..626b8c30f9a 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -2108,17 +2108,11 @@ class CConfig {
   su2double GetElasticyMod(unsigned short id_val) const { return ElasticityMod[id_val]; }
 
   /*!
-    * \brief Decide whether to apply DE effects to the model.
-    * \return <code>TRUE</code> if the DE effects are to be applied, <code>FALSE</code> otherwise.
-    */
+   * \brief Decide whether to apply DE effects to the model.
+   * \return <code>TRUE</code> if the DE effects are to be applied, <code>FALSE</code> otherwise.
+   */
   bool GetDE_Effects(void) const { return DE_Effects; }
 
-  /*!
-    * \brief Decide whether to predict the DE effects for the next time step.
-    * \return <code>TRUE</code> if the DE effects are to be applied, <code>FALSE</code> otherwise.
-    */
-   bool GetDE_Predicted(void);
-
   /*!
    * \brief Get the number of different electric constants.
    * \return Value of the DE modulus.
@@ -8749,22 +8743,10 @@ class CConfig {
   unsigned short GetnIntCoeffs(void) const { return nIntCoeffs; }
 
   /*!
-   * \brief Get the number of different values for the elasticity modulus.
-   * \return Number of different values for the elasticity modulus.
-   */
-  unsigned short GetnElasticityMod(void) const { return nElasticityMod; }
-
-  /*!
-   * \brief Get the number of different values for the Poisson ratio.
-   * \return Number of different values for the Poisson ratio.
-   */
-  unsigned short GetnPoissonRatio(void) const { return nPoissonRatio; }
-
-  /*!
-   * \brief Get the number of different values for the Material density.
-   * \return Number of different values for the Material density.
+   * \brief Get the number of different materials for the elasticity solver.
+   * \return Number of different materials.
    */
-  unsigned short GetnMaterialDensity(void) const { return nMaterialDensity; }
+  unsigned short GetnElasticityMat(void) const { return nElasticityMod; }
 
   /*!
    * \brief Get the integration coefficients for the Generalized Alpha - Newmark integration integration scheme.
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 4458e846616..e705b7f38d4 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -4648,6 +4648,11 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
     MaterialDensity = new su2double[1]; MaterialDensity[0] = 7854;
   }
 
+  if (nElasticityMod != nPoissonRatio || nElasticityMod != nMaterialDensity) {
+    SU2_MPI::Error("ELASTICITY_MODULUS, POISSON_RATIO, and MATERIAL_DENSITY need to have the same number "
+                   "of entries (the number of materials).", CURRENT_FUNCTION);
+  }
+
   if (nElectric_Constant == 0) {
     nElectric_Constant = 1;
     Electric_Constant = new su2double[1]; Electric_Constant[0] = 0.0;
diff --git a/SU2_CFD/include/solvers/CDiscAdjFEASolver.hpp b/SU2_CFD/include/solvers/CDiscAdjFEASolver.hpp
index abd8fcddfb0..446306efdc3 100644
--- a/SU2_CFD/include/solvers/CDiscAdjFEASolver.hpp
+++ b/SU2_CFD/include/solvers/CDiscAdjFEASolver.hpp
@@ -50,7 +50,8 @@ class CDiscAdjFEASolver final : public CSolver {
     su2double* val = nullptr;         /*!< \brief Value of the variable. */
     su2double* LocalSens = nullptr;   /*!< \brief Local sensitivity (domain). */
     su2double* GlobalSens = nullptr;  /*!< \brief Global sensitivity (mpi). */
-    su2double* TotalSens = nullptr;   /*!< \brief Total sensitivity (time domain). */
+    su2double* OldSens = nullptr;     /*!< \brief Previous global sensitivity, used to update the total. */
+    su2double* TotalSens = nullptr;   /*!< \brief Total sensitivity (integrated over time). */
 
     su2double& operator[] (unsigned short i) { return val[i]; }
     const su2double& operator[] (unsigned short i) const { return val[i]; }
@@ -61,6 +62,7 @@ class CDiscAdjFEASolver final : public CSolver {
       val = new su2double[n]();
       LocalSens = new su2double[n]();
       GlobalSens = new su2double[n]();
+      OldSens = new su2double[n]();
       TotalSens = new su2double[n]();
     }
 
@@ -69,6 +71,7 @@ class CDiscAdjFEASolver final : public CSolver {
       delete [] val;
       delete [] LocalSens;
       delete [] GlobalSens;
+      delete [] OldSens;
       delete [] TotalSens;
     }
 
@@ -80,10 +83,19 @@ class CDiscAdjFEASolver final : public CSolver {
       for (auto i = 0u; i < size; ++i) LocalSens[i] = SU2_TYPE::GetDerivative(val[i]);
 
       SU2_MPI::Allreduce(LocalSens, GlobalSens, size, MPI_DOUBLE, MPI_SUM, SU2_MPI::GetComm());
+
+      for (auto i = 0u; i < size; ++i) {
+        /*--- Update the total by subtracting the old and adding the new value.
+         * Then update the old value for the next call to this function. ---*/
+        TotalSens[i] += GlobalSens[i] - OldSens[i];
+        OldSens[i] = GlobalSens[i];
+      }
     }
 
     void UpdateTotal() {
-      for (auto i = 0u; i < size; ++i) TotalSens[i] += GlobalSens[i];
+      /*--- Clears the old values such that on the next time step the total is
+       * incremented instead of updated. ---*/
+      for (auto i = 0u; i < size; ++i) OldSens[i] = 0.0;
     }
 
     ~SensData() { clear(); }
@@ -213,42 +225,6 @@ class CDiscAdjFEASolver final : public CSolver {
    */
   inline su2double GetTotal_Sens_DVFEA(unsigned short iDVFEA) const override { return DV.TotalSens[iDVFEA]; }
 
-  /*!
-   * \brief A virtual member.
-   * \return Value of the sensitivity coefficient for the Young Modulus E
-   */
-  inline su2double GetGlobal_Sens_E(unsigned short iVal) const override { return E.GlobalSens[iVal]; }
-
-  /*!
-   * \brief A virtual member.
-   * \return Value of the Mach sensitivity for the Poisson's ratio Nu
-   */
-  inline su2double GetGlobal_Sens_Nu(unsigned short iVal) const override { return Nu.GlobalSens[iVal]; }
-
-  /*!
-   * \brief A virtual member.
-   * \return Value of the sensitivity coefficient for the Electric Field in the region iEField
-   */
-  inline su2double GetGlobal_Sens_EField(unsigned short iEField) const override { return EField.GlobalSens[iEField]; }
-
-  /*!
-   * \brief A virtual member.
-   * \return Value of the sensitivity coefficient for the FEA DV in the region iDVFEA
-   */
-  inline su2double GetGlobal_Sens_DVFEA(unsigned short iDVFEA) const override { return DV.GlobalSens[iDVFEA]; }
-
-  /*!
-   * \brief Get the total sensitivity for the structural density
-   * \return Value of the structural density sensitivity
-   */
-  inline su2double GetGlobal_Sens_Rho(unsigned short iVal) const override { return Rho.GlobalSens[iVal]; }
-
-  /*!
-   * \brief Get the total sensitivity for the structural weight
-   * \return Value of the structural weight sensitivity
-   */
-  inline su2double GetGlobal_Sens_Rho_DL(unsigned short iVal) const override { return Rho_DL.GlobalSens[iVal]; }
-
   /*!
    * \brief Get the value of the Young modulus from the adjoint solver
    * \return Value of the Young modulus from the adjoint solver
diff --git a/SU2_CFD/include/solvers/CSolver.hpp b/SU2_CFD/include/solvers/CSolver.hpp
index 892552859b0..ba28bf8b193 100644
--- a/SU2_CFD/include/solvers/CSolver.hpp
+++ b/SU2_CFD/include/solvers/CSolver.hpp
@@ -3201,42 +3201,6 @@ class CSolver {
    */
   inline virtual su2double GetTotal_Sens_DVFEA(unsigned short iDVFEA) const { return 0.0; }
 
-  /*!
-   * \brief A virtual member.
-   * \return Value of the sensitivity coefficient for the Young Modulus E
-   */
-  inline virtual su2double GetGlobal_Sens_E(unsigned short iVal) const { return 0.0; }
-
-  /*!
-   * \brief A virtual member.
-   * \return Value of the sensitivity coefficient for the Poisson's ratio Nu
-   */
-  inline virtual su2double GetGlobal_Sens_Nu(unsigned short iVal) const { return 0.0; }
-
-  /*!
-   * \brief A virtual member.
-   * \return Value of the structural density sensitivity
-   */
-  inline virtual su2double GetGlobal_Sens_Rho(unsigned short iVal) const { return 0.0; }
-
-  /*!
-   * \brief A virtual member.
-   * \return Value of the structural weight sensitivity
-   */
-  inline virtual su2double GetGlobal_Sens_Rho_DL(unsigned short iVal) const { return 0.0; }
-
-  /*!
-   * \brief A virtual member.
-   * \return Value of the sensitivity coefficient for the Electric Field in the region iEField
-   */
-  inline virtual su2double GetGlobal_Sens_EField(unsigned short iEField) const { return 0.0; }
-
-  /*!
-   * \brief A virtual member.
-   * \return Value of the sensitivity coefficient for the FEA DV in the region iDVFEA
-   */
-  inline virtual su2double GetGlobal_Sens_DVFEA(unsigned short iDVFEA) const { return 0.0; }
-
   /*!
    * \brief A virtual member.
    * \return Value of the Young modulus from the adjoint solver
diff --git a/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
index 7decbd05b57..a37971f0aeb 100644
--- a/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
@@ -32,32 +32,6 @@
 
 CDiscAdjFEAIteration::CDiscAdjFEAIteration(const CConfig *config) : CIteration(config), CurrentRecording(NONE) {
   fem_iteration = new CFEAIteration(config);
-
-  // TEMPORARY output only for standalone structural problems
-  if (config->GetAdvanced_FEAElementBased() && (rank == MASTER_NODE)) {
-    bool de_effects = config->GetDE_Effects();
-    unsigned short iVar;
-
-    /*--- Header of the temporary output file ---*/
-    ofstream myfile_res;
-    myfile_res.open("Results_Reverse_Adjoint.txt");
-
-    myfile_res << "Obj_Func"
-               << " ";
-    for (iVar = 0; iVar < config->GetnElasticityMod(); iVar++) myfile_res << "Sens_E_" << iVar << "\t";
-
-    for (iVar = 0; iVar < config->GetnPoissonRatio(); iVar++) myfile_res << "Sens_Nu_" << iVar << "\t";
-
-    if (config->GetTime_Domain()) {
-      for (iVar = 0; iVar < config->GetnMaterialDensity(); iVar++) myfile_res << "Sens_Rho_" << iVar << "\t";
-    }
-
-    if (de_effects) {
-      for (iVar = 0; iVar < config->GetnElectric_Field(); iVar++) myfile_res << "Sens_EField_" << iVar << "\t";
-    }
-
-    myfile_res << "\n";
-  }
 }
 
 CDiscAdjFEAIteration::~CDiscAdjFEAIteration() = default;
@@ -71,31 +45,49 @@ void CDiscAdjFEAIteration::Preprocess(COutput* output, CIntegration**** integrat
   auto dirNodes = solvers0[FEA_SOL]->GetNodes();
   auto adjNodes = solvers0[ADJFEA_SOL]->GetNodes();
 
-  /*--- For the dynamic adjoint, load direct solutions from restart files. ---*/
+  auto StoreDirectSolution = [&]() {
+    for (auto iPoint = 0ul; iPoint < geometry0->GetnPoint(); iPoint++) {
+      adjNodes->SetSolution_Direct(iPoint, dirNodes->GetSolution(iPoint));
+    }
+  };
+
+  /*--- For the dynamic adjoint, load direct solutions from restart files.
+   * For steady, store the direct solution to be able to reset it later. ---*/
 
   if (config[iZone]->GetTime_Domain()) {
     const int TimeIter = config[iZone]->GetTimeIter();
     const int Direct_Iter = SU2_TYPE::Int(config[iZone]->GetUnst_AdjointIter()) - TimeIter - 1;
 
-    /*--- We want to load the already converged solution at timesteps n and n-1 ---*/
-
-    /*--- Load solution at timestep n-1 ---*/
+    /*--- We need the already converged solution at timesteps n and n-1. On the first
+     * adjoint time step we load both, then n-1 becomes "n" and we only load n-2. ---*/
 
-    LoadDynamic_Solution(geometry, solver, config, iZone, iInst, Direct_Iter - 1);
+    if (TimeIter > 0) {
+      /*--- Save n-1 to become n. ---*/
+      for (auto iPoint = 0ul; iPoint < geometry0->GetnPoint(); iPoint++) {
+        adjNodes->SetSolution_Direct(iPoint, dirNodes->GetSolution_time_n(iPoint));
+      }
+    }
 
-    /*--- Push solution back to correct array ---*/
+    /*--- Load solution at timestep n-1 and push back to correct array. ---*/
 
+    LoadDynamic_Solution(geometry, solver, config, iZone, iInst, Direct_Iter - 1);
     dirNodes->Set_Solution_time_n();
 
-    /*--- Load solution timestep n ---*/
+    /*--- Load or set solution at timestep n. ---*/
 
-    LoadDynamic_Solution(geometry, solver, config, iZone, iInst, Direct_Iter);
-  }
-
-  /*--- Store FEA solution also in the adjoint solver in order to be able to reset it later. ---*/
+    if (TimeIter == 0) {
+      LoadDynamic_Solution(geometry, solver, config, iZone, iInst, Direct_Iter);
+      StoreDirectSolution();
+    } else {
+      /*--- Set n-1 as n. ---*/
+      for (auto iPoint = 0ul; iPoint < geometry0->GetnPoint(); iPoint++)
+        for (auto iVar = 0u; iVar < solvers0[ADJFEA_SOL]->GetnVar(); iVar++)
+          dirNodes->SetSolution(iPoint, iVar, adjNodes->GetSolution_Direct(iPoint)[iVar]);
+    }
 
-  for (auto iPoint = 0ul; iPoint < geometry0->GetnPoint(); iPoint++) {
-    adjNodes->SetSolution_Direct(iPoint, dirNodes->GetSolution(iPoint));
+  } else {
+    /*--- Steady. ---*/
+    StoreDirectSolution();
   }
 
   solvers0[ADJFEA_SOL]->Preprocessing(geometry0, solvers0, config[iZone], MESH_0, 0, RUNTIME_ADJFEA_SYS, false);
@@ -178,7 +170,7 @@ void CDiscAdjFEAIteration::SetDependencies(CSolver***** solver, CGeometry**** ge
   const int mat_knowles = MAT_KNOWLES+offset;
   const int de_term = DE_TERM+offset;
 
-  for (unsigned short iProp = 0; iProp < config[iZone]->GetnElasticityMod(); iProp++) {
+  for (unsigned short iProp = 0; iProp < config[iZone]->GetnElasticityMat(); iProp++) {
     su2double E = adj_solver->GetVal_Young(iProp);
     su2double nu = adj_solver->GetVal_Poisson(iProp);
     su2double rho = adj_solver->GetVal_Rho(iProp);
@@ -302,45 +294,8 @@ void CDiscAdjFEAIteration::Postprocess(COutput* output, CIntegration**** integra
                                        CSolver***** solver, CNumerics****** numerics, CConfig** config,
                                        CSurfaceMovement** surface_movement, CVolumetricMovement*** grid_movement,
                                        CFreeFormDefBox*** FFDBox, unsigned short iZone, unsigned short iInst) {
-  const bool dynamic = (config[iZone]->GetTime_Domain());
   auto solvers0 = solver[iZone][iInst][MESH_0];
 
-  // TEMPORARY output only for standalone structural problems
-  if (config[iZone]->GetAdvanced_FEAElementBased() && (rank == MASTER_NODE)) {
-    unsigned short iVar;
-
-    const bool de_effects = config[iZone]->GetDE_Effects();
-
-    /*--- Header of the temporary output file ---*/
-    ofstream myfile_res;
-    myfile_res.open("Results_Reverse_Adjoint.txt", ios::app);
-
-    myfile_res.precision(15);
-
-    myfile_res << config[iZone]->GetTimeIter() << "\t";
-
-    solvers0[FEA_SOL]->Evaluate_ObjFunc(config[iZone], solvers0);
-    myfile_res << scientific << solvers0[FEA_SOL]->GetTotal_ComboObj() << "\t";
-
-    for (iVar = 0; iVar < config[iZone]->GetnElasticityMod(); iVar++)
-      myfile_res << scientific << solvers0[ADJFEA_SOL]->GetTotal_Sens_E(iVar) << "\t";
-    for (iVar = 0; iVar < config[iZone]->GetnPoissonRatio(); iVar++)
-      myfile_res << scientific << solvers0[ADJFEA_SOL]->GetTotal_Sens_Nu(iVar) << "\t";
-    if (dynamic) {
-      for (iVar = 0; iVar < config[iZone]->GetnMaterialDensity(); iVar++)
-        myfile_res << scientific << solvers0[ADJFEA_SOL]->GetTotal_Sens_Rho(iVar) << "\t";
-    }
-    if (de_effects) {
-      for (iVar = 0; iVar < config[iZone]->GetnElectric_Field(); iVar++)
-        myfile_res << scientific << solvers0[ADJFEA_SOL]->GetTotal_Sens_EField(iVar) << "\t";
-    }
-    for (iVar = 0; iVar < solvers0[ADJFEA_SOL]->GetnDVFEA(); iVar++) {
-      myfile_res << scientific << solvers0[ADJFEA_SOL]->GetTotal_Sens_DVFEA(iVar) << "\t";
-    }
-
-    myfile_res << "\n";
-  }
-
   // TEST: for implementation of python framework in standalone structural problems
   if (config[iZone]->GetAdvanced_FEAElementBased() && (rank == MASTER_NODE)) {
     /*--- Header of the temporary output file ---*/
diff --git a/SU2_CFD/src/numerics/elasticity/CFEAElasticity.cpp b/SU2_CFD/src/numerics/elasticity/CFEAElasticity.cpp
index 6fd3a35042c..fc87cbc19a5 100644
--- a/SU2_CFD/src/numerics/elasticity/CFEAElasticity.cpp
+++ b/SU2_CFD/src/numerics/elasticity/CFEAElasticity.cpp
@@ -38,23 +38,19 @@ CFEAElasticity::CFEAElasticity(unsigned short val_nDim, unsigned short val_nVar,
   bool body_forces = config->GetDeadLoad();  // Body forces (dead loads).
   bool pseudo_static = config->GetPseudoStatic();
 
-  unsigned short iVar, nProp;
+  unsigned short iVar;
 
   /*--- Initialize vector structures for multiple material definition ---*/
-  nProp = config->GetnElasticityMod();
+  const auto nProp = config->GetnElasticityMat();
 
   E_i = new su2double[nProp];
   for (iVar = 0; iVar < nProp; iVar++)
     E_i[iVar] = config->GetElasticyMod(iVar);
 
-  nProp = config->GetnPoissonRatio();
-
   Nu_i = new su2double[nProp];
   for (iVar = 0; iVar < nProp; iVar++)
     Nu_i[iVar] = config->GetPoissonRatio(iVar);
 
-  nProp = config->GetnMaterialDensity();
-
   Rho_s_i = new su2double[nProp];     // For inertial effects
   Rho_s_DL_i = new su2double[nProp];  // For dead loads
 
diff --git a/SU2_CFD/src/output/CAdjElasticityOutput.cpp b/SU2_CFD/src/output/CAdjElasticityOutput.cpp
index 8ed7017aba2..f55e441c2d6 100644
--- a/SU2_CFD/src/output/CAdjElasticityOutput.cpp
+++ b/SU2_CFD/src/output/CAdjElasticityOutput.cpp
@@ -27,6 +27,7 @@
 
 
 #include "../../include/output/CAdjElasticityOutput.hpp"
+#include <string>
 
 #include "../../../Common/include/geometry/CGeometry.hpp"
 #include "../../include/solvers/CSolver.hpp"
@@ -50,8 +51,8 @@ CAdjElasticityOutput::CAdjElasticityOutput(CConfig *config, unsigned short nDim)
     requestedScreenFields.emplace_back("INNER_ITER");
     requestedScreenFields.emplace_back("ADJOINT_DISP_X");
     requestedScreenFields.emplace_back("ADJOINT_DISP_Y");
-    requestedScreenFields.emplace_back("SENS_E");
-    requestedScreenFields.emplace_back("SENS_NU");
+    requestedScreenFields.emplace_back("SENS_E_0");
+    requestedScreenFields.emplace_back("SENS_NU_0");
     nRequestedScreenFields = requestedScreenFields.size();
   }
 
@@ -62,9 +63,9 @@ CAdjElasticityOutput::CAdjElasticityOutput(CConfig *config, unsigned short nDim)
     nRequestedVolumeFields = requestedVolumeFields.size();
   }
 
-  if (find(requestedVolumeFields.begin(), requestedVolumeFields.end(), string("SENSITIVITY")) == requestedVolumeFields.end()) {
+  if (find(requestedVolumeFields.begin(), requestedVolumeFields.end(), "SENSITIVITY") == requestedVolumeFields.end()) {
     requestedVolumeFields.emplace_back("SENSITIVITY");
-    nRequestedVolumeFields ++;
+    nRequestedVolumeFields++;
   }
 
   stringstream ss;
@@ -97,47 +98,69 @@ CAdjElasticityOutput::~CAdjElasticityOutput() = default;
 
 void CAdjElasticityOutput::SetHistoryOutputFields(CConfig *config){
 
-  // Residuals
+  /*--- Residuals ---*/
   AddHistoryOutput("ADJOINT_DISP_X", "rms[Ux_adj]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the adjoint of the X displacements.", HistoryFieldType::RESIDUAL);
   AddHistoryOutput("ADJOINT_DISP_Y", "rms[Uy_adj]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the adjoint of the Y displacements.", HistoryFieldType::RESIDUAL);
-  AddHistoryOutput("ADJOINT_DISP_Z", "rms[Uz_adj]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the adjoint of the Z displacements.", HistoryFieldType::RESIDUAL);
+  if (nVar_FEM == 3) {
+    AddHistoryOutput("ADJOINT_DISP_Z", "rms[Uz_adj]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the adjoint of the Z displacements.", HistoryFieldType::RESIDUAL);
+  }
 
-  //Sensitivities
-  AddHistoryOutput("SENS_E", "Sens[E]", ScreenOutputFormat::SCIENTIFIC, "SENSITIVITY", "d Objective / d Elasticity modulus");
-  AddHistoryOutput("SENS_NU", "Sens[Nu]", ScreenOutputFormat::SCIENTIFIC, "SENSITIVITY", "d Objective / d Poisson ratio");
+  /*--- Sensitivities ---*/
+  for (auto iVar = 0u; iVar < config->GetnElasticityMat(); iVar++) {
+    const auto iVarS = std::to_string(iVar);
+    AddHistoryOutput("SENS_E_" + iVarS, "Sens[E" + iVarS + ']', ScreenOutputFormat::SCIENTIFIC, "SENSITIVITY", "d Objective / d Elasticity modulus");
+    AddHistoryOutput("SENS_NU_" + iVarS, "Sens[Nu" + iVarS + ']', ScreenOutputFormat::SCIENTIFIC, "SENSITIVITY", "d Objective / d Poisson ratio");
+    if (config->GetTime_Domain() && !config->GetPseudoStatic()) {
+      AddHistoryOutput("SENS_RHO_" + iVarS, "Sens[Rho" + iVarS + ']', ScreenOutputFormat::SCIENTIFIC, "SENSITIVITY", "d Objective / d Material density");
+    }
+    if (config->GetDeadLoad()) {
+      AddHistoryOutput("SENS_RHO_DL_" + iVarS, "Sens[RhoDL" + iVarS + ']', ScreenOutputFormat::SCIENTIFIC, "SENSITIVITY", "d Objective / d Dead load density");
+    }
+  }
+  if (config->GetDE_Effects()) {
+    for (auto iVar = 0u; iVar < config->GetnElectric_Field(); iVar++) {
+      const auto iVarS = std::to_string(iVar);
+      AddHistoryOutput("SENS_EFIELD_" + iVarS, "Sens[EField" + iVarS + ']', ScreenOutputFormat::SCIENTIFIC, "SENSITIVITY", "d Objective / d Electric field");
+    }
+  }
 
   AddHistoryOutput("LINSOL_ITER", "LinSolIter", ScreenOutputFormat::INTEGER, "LINSOL", "Number of iterations of the linear solver.");
   AddHistoryOutput("LINSOL_RESIDUAL", "LinSolRes", ScreenOutputFormat::FIXED, "LINSOL", "Residual of the linear solver.");
 
-  AddHistoryOutput("BGS_ADJ_DISP_X", "bgs[A_Ux]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the adjoint X displacement.", HistoryFieldType::RESIDUAL);
-  AddHistoryOutput("BGS_ADJ_DISP_Y", "bgs[A_Uy]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the adjoint Y displacement.", HistoryFieldType::RESIDUAL);
-  AddHistoryOutput("BGS_ADJ_DISP_Z", "bgs[A_Uz]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the adjoint Z displacement.", HistoryFieldType::RESIDUAL);
-
+  if (multiZone) {
+    AddHistoryOutput("BGS_ADJ_DISP_X", "bgs[A_Ux]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the adjoint X displacement.", HistoryFieldType::RESIDUAL);
+    AddHistoryOutput("BGS_ADJ_DISP_Y", "bgs[A_Uy]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the adjoint Y displacement.", HistoryFieldType::RESIDUAL);
+    if (nVar_FEM == 3) {
+      AddHistoryOutput("BGS_ADJ_DISP_Z", "bgs[A_Uz]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the adjoint Z displacement.", HistoryFieldType::RESIDUAL);
+    }
+  }
 }
 
 inline void CAdjElasticityOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, CSolver **solver) {
 
   SetHistoryOutputValue("ADJOINT_DISP_X", log10(solver[ADJFEA_SOL]->GetRes_RMS(0)));
   SetHistoryOutputValue("ADJOINT_DISP_Y", log10(solver[ADJFEA_SOL]->GetRes_RMS(1)));
-  if (nVar_FEM == 3){
+  if (nVar_FEM == 3) {
     SetHistoryOutputValue("ADJOINT_DISP_Z", log10(solver[ADJFEA_SOL]->GetRes_RMS(2)));
   }
 
-  su2double Total_SensE = 0.0; su2double Total_SensNu = 0.0;
-  if (config->GetnElasticityMod() == 1) {
-    Total_SensE = solver[ADJFEA_SOL]->GetGlobal_Sens_E(0);
-    Total_SensNu = solver[ADJFEA_SOL]->GetGlobal_Sens_Nu(0);
+  for (unsigned short iVar = 0; iVar < config->GetnElasticityMat(); iVar++) {
+    const auto iVarS = std::to_string(iVar);
+    SetHistoryOutputValue("SENS_E_" + iVarS, solver[ADJFEA_SOL]->GetTotal_Sens_E(iVar));
+    SetHistoryOutputValue("SENS_NU_" + iVarS, solver[ADJFEA_SOL]->GetTotal_Sens_Nu(iVar));
+    if (config->GetTime_Domain() && !config->GetPseudoStatic()) {
+      SetHistoryOutputValue("SENS_RHO_" + iVarS, solver[ADJFEA_SOL]->GetTotal_Sens_Rho(iVar));
+    }
+    if (config->GetDeadLoad()) {
+      SetHistoryOutputValue("SENS_RHO_DL_" + iVarS, solver[ADJFEA_SOL]->GetTotal_Sens_Rho_DL(iVar));
+    }
   }
-  else {
-    for (unsigned short iVar = 0; iVar < config->GetnElasticityMod(); iVar++){
-      Total_SensE += pow(solver[ADJFEA_SOL]->GetGlobal_Sens_E(iVar),2);
-      Total_SensNu += pow(solver[ADJFEA_SOL]->GetGlobal_Sens_Nu(iVar),2);
+  if (config->GetDE_Effects()) {
+    for (auto iVar = 0u; iVar < config->GetnElectric_Field(); iVar++) {
+      const auto iVarS = std::to_string(iVar);
+      SetHistoryOutputValue("SENS_EFIELD_" + iVarS, solver[ADJFEA_SOL]->GetTotal_Sens_EField(iVar));
     }
-    Total_SensE = sqrt(Total_SensE);
-    Total_SensNu = sqrt(Total_SensNu);
   }
-  SetHistoryOutputValue("SENS_E", Total_SensE);
-  SetHistoryOutputValue("SENS_NU", Total_SensNu);
 
   SetHistoryOutputValue("LINSOL_ITER", solver[ADJFEA_SOL]->GetIterLinSolver());
   SetHistoryOutputValue("LINSOL_RESIDUAL", log10(solver[ADJFEA_SOL]->GetResLinSolver()));
diff --git a/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp b/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
index f11c9f580b6..34a19c89a3e 100644
--- a/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
+++ b/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
@@ -84,16 +84,7 @@ CDiscAdjFEASolver::CDiscAdjFEASolver(CGeometry *geometry, CConfig *config, CSolv
 
   /*--- Initialize vector structures for multiple material definition ---*/
 
-  nMPROP = config->GetnElasticityMod();
-
-  /*--- For a material to be fully defined, we need to have the same number for all three parameters ---*/
-  bool checkDef = ((config->GetnElasticityMod() == config->GetnPoissonRatio()) &&
-                   (config->GetnElasticityMod() == config->GetnMaterialDensity()) &&
-                   (config->GetnMaterialDensity() == config->GetnPoissonRatio()));
-
-  if (!checkDef){
-    SU2_MPI::Error("WARNING: For a material to be fully defined, E, Nu and Rho need to have the same dimensions.", CURRENT_FUNCTION);
-  }
+  nMPROP = config->GetnElasticityMat();
 
   E.resize(nMPROP);
   Nu.resize(nMPROP);
diff --git a/SU2_CFD/src/solvers/CFEASolver.cpp b/SU2_CFD/src/solvers/CFEASolver.cpp
index e4877179706..858257f094c 100644
--- a/SU2_CFD/src/solvers/CFEASolver.cpp
+++ b/SU2_CFD/src/solvers/CFEASolver.cpp
@@ -383,8 +383,8 @@ void CFEASolver::Set_ElementProperties(CGeometry *geometry, CConfig *config) {
     /*--- Detect a wrong solution file ---*/
 
     if (iElem_Global_Local != nElement) {
-      SU2_MPI::Error(string("The properties file ") + filename + string(" doesn't match with the mesh file!\n")  +
-                     string("It could be empty lines at the end of the file."), CURRENT_FUNCTION);
+      SU2_MPI::Error("The properties file " + filename + " doesn't match with the mesh file!\n"
+                     "It could be empty lines at the end of the file.", CURRENT_FUNCTION);
     }
 
   }
diff --git a/SU2_PY/SU2/io/historyMap.py b/SU2_PY/SU2/io/historyMap.py
index aca169155e2..a477478359c 100644
--- a/SU2_PY/SU2/io/historyMap.py
+++ b/SU2_PY/SU2/io/historyMap.py
@@ -1186,10 +1186,10 @@
         "HEADER": "Sens_AoA",
         "TYPE": "COEFFICIENT",
     },
-    "SENS_E": {
+    "SENS_E_0": {
         "DESCRIPTION": "d Objective / d Elasticity modulus",
         "GROUP": "SENSITIVITY",
-        "HEADER": "Sens[E]",
+        "HEADER": "Sens[E_0]",
         "TYPE": "DEFAULT",
     },
     "SENS_GEO": {
@@ -1207,10 +1207,10 @@
         "HEADER": "Sens_Mach",
         "TYPE": "COEFFICIENT",
     },
-    "SENS_NU": {
+    "SENS_NU_0": {
         "DESCRIPTION": "d Objective / d Poisson ratio",
         "GROUP": "SENSITIVITY",
-        "HEADER": "Sens[Nu]",
+        "HEADER": "Sens[Nu_0]",
         "TYPE": "DEFAULT",
     },
     "SENS_PRESS": {
diff --git a/TestCases/disc_adj_fsi/Airfoil_2d/config.cfg b/TestCases/disc_adj_fsi/Airfoil_2d/config.cfg
index 6b58ea8e026..a484a26c79b 100755
--- a/TestCases/disc_adj_fsi/Airfoil_2d/config.cfg
+++ b/TestCases/disc_adj_fsi/Airfoil_2d/config.cfg
@@ -13,6 +13,6 @@ MESH_FILENAME= mesh.su2
 
 OBJECTIVE_FUNCTION= CUSTOM_OBJFUNC
 
-SCREEN_OUTPUT= OUTER_ITER, AVG_BGS_RES[0], AVG_BGS_RES[1], LINSOL_RESIDUAL[0], SENS_E[1], SENS_NU[1]
+SCREEN_OUTPUT= OUTER_ITER, AVG_BGS_RES[0], AVG_BGS_RES[1], LINSOL_RESIDUAL[0], SENS_E_0[1], SENS_NU_0[1]
 
 %WRT_ZONE_CONV=YES
diff --git a/TestCases/disc_adj_fsi/config.cfg b/TestCases/disc_adj_fsi/config.cfg
index 35cf049125d..044f409302c 100644
--- a/TestCases/disc_adj_fsi/config.cfg
+++ b/TestCases/disc_adj_fsi/config.cfg
@@ -9,6 +9,6 @@ MESH_FILENAME= mesh.su2
 
 OBJECTIVE_FUNCTION = REFERENCE_GEOMETRY
 
-SCREEN_OUTPUT= OUTER_ITER, AVG_BGS_RES[0], RMS_ADJ_DENSITY[0], SENS_E[1], SENS_NU[1]
+SCREEN_OUTPUT= OUTER_ITER, AVG_BGS_RES[0], RMS_ADJ_DENSITY[0], SENS_E_0[1], SENS_NU_0[1]
 
 %WRT_ZONE_CONV= YES
diff --git a/TestCases/py_wrapper/custom_load_fea/run_ad.py b/TestCases/py_wrapper/custom_load_fea/run_ad.py
index 92e454083b3..cc85ca00239 100644
--- a/TestCases/py_wrapper/custom_load_fea/run_ad.py
+++ b/TestCases/py_wrapper/custom_load_fea/run_ad.py
@@ -145,7 +145,10 @@ def RunPrimal(density, peak_load):
 
 
 def RunAdjoint(density, peak_load):
-  """Runs the adjoint solver and returns the sensitivity of the objective function to the peak load."""
+  """
+  Runs the adjoint solver and returns the sensitivity of the objective function to the peak
+  load and to the material density.
+  """
   comm = MPI.COMM_WORLD
 
   with open('config_unsteady_ad.cfg', 'w') as f:
@@ -187,10 +190,12 @@ def RunAdjoint(density, peak_load):
     driver.Monitor(time_iter)
     driver.Output(time_iter)
 
+  rho_sens = driver.GetOutputValue('SENS_RHO_0')
+
   # Finalize the solver and exit cleanly.
   driver.Finalize()
 
-  return comm.allreduce(load_sens)
+  return comm.allreduce(load_sens), rho_sens
 
 
 def main():
@@ -204,10 +209,7 @@ def main():
   sens_load_fd = (obj_pert_load - obj) / 0.002
   sens_rho_fd = (obj_pert_rho - obj) / 0.0001
 
-  sens_load = RunAdjoint(1, 2)
-  # Read the density sensitivity from the special output file.
-  with open('Results_Reverse_Adjoint.txt') as f:
-    sens_rho = float(f.readlines()[-1].strip().split('\t')[-1])
+  sens_load, sens_rho = RunAdjoint(1, 2)
 
   if rank == 0:
     print("      Finite Differences\tDiscrete Adjoint")

From 7548083521ea76395488974afe2ffb0b2b958f68 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Wed, 19 Apr 2023 21:55:51 -0700
Subject: [PATCH 406/656] fixes and update ref file

---
 SU2_CFD/include/solvers/CDiscAdjFEASolver.hpp |  2 +-
 SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp     | 19 +++++++++++--------
 .../disc_adj_fsi/dyn_fsi/grad_dv.opt.ref      | 16 ++++++++--------
 3 files changed, 20 insertions(+), 17 deletions(-)

diff --git a/SU2_CFD/include/solvers/CDiscAdjFEASolver.hpp b/SU2_CFD/include/solvers/CDiscAdjFEASolver.hpp
index 446306efdc3..2755731f5a7 100644
--- a/SU2_CFD/include/solvers/CDiscAdjFEASolver.hpp
+++ b/SU2_CFD/include/solvers/CDiscAdjFEASolver.hpp
@@ -92,7 +92,7 @@ class CDiscAdjFEASolver final : public CSolver {
       }
     }
 
-    void UpdateTotal() {
+    void Store() {
       /*--- Clears the old values such that on the next time step the total is
        * incremented instead of updated. ---*/
       for (auto i = 0u; i < size; ++i) OldSens[i] = 0.0;
diff --git a/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp b/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
index 34a19c89a3e..5a03df9aff7 100644
--- a/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
+++ b/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
@@ -346,12 +346,17 @@ void CDiscAdjFEASolver::Preprocessing(CGeometry *geometry, CSolver **solver_cont
 
 void CDiscAdjFEASolver::SetSensitivity(CGeometry *geometry, CConfig *config, CSolver*){
 
-  E.UpdateTotal();
-  Nu.UpdateTotal();
-  Rho.UpdateTotal();
-  Rho_DL.UpdateTotal();
-  if (de_effects) EField.UpdateTotal();
-  if (fea_dv) DV.UpdateTotal();
+  const bool time_domain = config->GetTime_Domain();
+
+  /*--- Store the final material sensitivities for the time step to increment them on the next time step. ---*/
+  if (time_domain) {
+    E.Store();
+    Nu.Store();
+    Rho.Store();
+    Rho_DL.Store();
+    if (de_effects) EField.Store();
+    if (fea_dv) DV.Store();
+  }
 
   /*--- Extract the topology optimization density sensitivities. ---*/
 
@@ -359,8 +364,6 @@ void CDiscAdjFEASolver::SetSensitivity(CGeometry *geometry, CConfig *config, CSo
 
   /*--- Extract the geometric sensitivities ---*/
 
-  const bool time_domain = config->GetTime_Domain();
-
   for (unsigned long iPoint = 0; iPoint < nPoint; iPoint++) {
 
     auto Coord = geometry->nodes->GetCoord(iPoint);
diff --git a/TestCases/disc_adj_fsi/dyn_fsi/grad_dv.opt.ref b/TestCases/disc_adj_fsi/dyn_fsi/grad_dv.opt.ref
index e543b661a60..b2e428bed5a 100644
--- a/TestCases/disc_adj_fsi/dyn_fsi/grad_dv.opt.ref
+++ b/TestCases/disc_adj_fsi/dyn_fsi/grad_dv.opt.ref
@@ -1,9 +1,9 @@
 INDEX	GRAD
-0	-3.461460667601001e-03
-1	-1.841786311588662e-03
-2	-7.915536257748965e-04
-3	-2.739622082729719e-04
-4	-2.734869133461108e-04
-5	-7.881162428890194e-04
-6	-1.828978290516676e-03
-7	-3.427219398258311e-03
+0	-3.461460667601000e-03
+1	-1.841786311588663e-03
+2	-7.915536257748967e-04
+3	-2.739622082729717e-04
+4	-2.734869133461104e-04
+5	-7.881162428890206e-04
+6	-1.828978290516677e-03
+7	-3.427219398258316e-03

From 1549d45be67b7056745fda07034215fffe4d70e3 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 22 Apr 2023 17:22:11 -0700
Subject: [PATCH 407/656] checkpoint fixing AD index issues in the flow
 tractions

---
 Common/include/option_structure.hpp           |  2 +-
 SU2_CFD/include/drivers/CDriverBase.hpp       |  9 +++
 .../include/variables/CDiscAdjVariable.hpp    |  1 +
 .../include/variables/CFEABoundVariable.hpp   |  7 ++-
 SU2_CFD/include/variables/CVariable.hpp       |  8 ++-
 SU2_CFD/src/output/CAdjElasticityOutput.cpp   | 36 ++++++++++++
 SU2_CFD/src/output/CFlowOutput.cpp            |  4 +-
 SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp     | 16 ++++--
 SU2_CFD/src/variables/CFEABoundVariable.cpp   |  7 +++
 TestCases/parallel_regression_AD.py           |  4 +-
 .../py_wrapper/custom_load_fea/run_ad.py      | 57 +++++++++++++------
 11 files changed, 121 insertions(+), 30 deletions(-)

diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index e661b451d1b..69acd1c0c67 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -1439,7 +1439,7 @@ enum class STRUCT_TIME_INT {
 };
 static const MapType<std::string, STRUCT_TIME_INT> Time_Int_Map_FEA = {
   MakePair("NEWMARK_IMPLICIT", STRUCT_TIME_INT::NEWMARK_IMPLICIT)
-  MakePair("GENERALIZED_ALPHA", STRUCT_TIME_INT::GENERALIZED_ALPHA)
+  // MakePair("GENERALIZED_ALPHA", STRUCT_TIME_INT::GENERALIZED_ALPHA) Not fully implemented.
 };
 
 /*!
diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index 4e79537a829..d720246efb7 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -499,6 +499,15 @@ class CDriverBase {
         main_geometry->GetnVertex(iMarker), "MarkerPrimitives", false);
   }
 
+  /*!
+   * \brief Get a read-only view of the geometry sensitivity of a discrete adjoint solver.
+   */
+  inline CPyWrapperMatrixView Sensitivity(unsigned short iSolver) {
+    auto* solver = GetSolverAndCheckMarker(iSolver);
+    auto& sensitivity = const_cast<su2activematrix&>(solver->GetNodes()->GetSensitivity());
+    return CPyWrapperMatrixView(sensitivity, "Sensitivity", true);
+  }
+
   /*!
    * \brief Set the temperature of a vertex on a specified marker (MARKER_PYTHON_CUSTOM).
    * \note This can be the input of a heat or flow solver in a CHT setting.
diff --git a/SU2_CFD/include/variables/CDiscAdjVariable.hpp b/SU2_CFD/include/variables/CDiscAdjVariable.hpp
index 72ca67f9c24..bc72508de78 100644
--- a/SU2_CFD/include/variables/CDiscAdjVariable.hpp
+++ b/SU2_CFD/include/variables/CDiscAdjVariable.hpp
@@ -72,6 +72,7 @@ class CDiscAdjVariable : public CVariable {
   inline su2double GetSensitivity(unsigned long iPoint, unsigned long iDim) const final {
     return Sensitivity(iPoint,iDim);
   }
+  inline const MatrixType& GetSensitivity() const final { return Sensitivity; }
 
   /*!
    * \brief Set/store the dual time contributions to the adjoint variable.
diff --git a/SU2_CFD/include/variables/CFEABoundVariable.hpp b/SU2_CFD/include/variables/CFEABoundVariable.hpp
index e04d40467c1..950fef78ebe 100644
--- a/SU2_CFD/include/variables/CFEABoundVariable.hpp
+++ b/SU2_CFD/include/variables/CFEABoundVariable.hpp
@@ -159,10 +159,15 @@ class CFEABoundVariable final : public CFEAVariable {
    */
   void RegisterFlowTraction() override;
 
+  /*!
+   * \brief Resets the AD indices of the flow tractions.
+   */
+  void ResetInputFlowTraction() override;
+
   /*!
    * \brief Extract the flow traction derivatives.
    */
-  inline su2double ExtractFlowTraction_Sensitivity(unsigned long iPoint, unsigned long iDim) const override {
+  inline su2double ExtractFlowTractionSensitivity(unsigned long iPoint, unsigned long iDim) const override {
     if (!fsi_analysis) return 0.0;
     if (!VertexMap.GetVertexIndex(iPoint)) return 0.0;
     return SU2_TYPE::GetDerivative(FlowTraction(iPoint,iDim));
diff --git a/SU2_CFD/include/variables/CVariable.hpp b/SU2_CFD/include/variables/CVariable.hpp
index da68a28f051..efdbc25c9ce 100644
--- a/SU2_CFD/include/variables/CVariable.hpp
+++ b/SU2_CFD/include/variables/CVariable.hpp
@@ -2165,7 +2165,12 @@ class CVariable {
   /*!
    * \brief A virtual member.
    */
-  inline virtual su2double ExtractFlowTraction_Sensitivity(unsigned long iPoint, unsigned long iDim) const { return 0.0; }
+  inline virtual void ResetInputFlowTraction() { }
+
+  /*!
+   * \brief A virtual member.
+   */
+  inline virtual su2double ExtractFlowTractionSensitivity(unsigned long iPoint, unsigned long iDim) const { return 0.0; }
 
   /*!
    * \brief Register the variables in the solution array as input/output variable.
@@ -2224,6 +2229,7 @@ class CVariable {
    * \return value of the Sensitivity
    */
   inline virtual su2double GetSensitivity(unsigned long iPoint, unsigned long iDim) const { return 0.0; }
+  inline virtual const MatrixType& GetSensitivity() const { AssertOverride(); return Solution; }
 
   inline virtual void SetTau_Wall(unsigned long iPoint, su2double tau_wall) {}
 
diff --git a/SU2_CFD/src/output/CAdjElasticityOutput.cpp b/SU2_CFD/src/output/CAdjElasticityOutput.cpp
index f55e441c2d6..e30f2895f65 100644
--- a/SU2_CFD/src/output/CAdjElasticityOutput.cpp
+++ b/SU2_CFD/src/output/CAdjElasticityOutput.cpp
@@ -193,6 +193,23 @@ void CAdjElasticityOutput::LoadVolumeData(CConfig *config, CGeometry *geometry,
   SetVolumeOutputValue("SENSITIVITY-Y", iPoint, Node_Struc->GetSensitivity(iPoint, 1));
   if (nDim == 3)
     SetVolumeOutputValue("SENSITIVITY-Z", iPoint, Node_Struc->GetSensitivity(iPoint, 2));
+
+  if (!config->GetTime_Domain()) return;
+
+  SetVolumeOutputValue("SENS_DISP-X", iPoint, Node_Struc->GetSolution_time_n(iPoint, 0));
+  SetVolumeOutputValue("SENS_DISP-Y", iPoint, Node_Struc->GetSolution_time_n(iPoint, 1));
+  if (nDim == 3)
+    SetVolumeOutputValue("SENS_DISP-Z", iPoint, Node_Struc->GetSolution_time_n(iPoint, 2));
+
+  SetVolumeOutputValue("SENS_VEL-X", iPoint, Node_Struc->GetSolution_time_n(iPoint, nDim));
+  SetVolumeOutputValue("SENS_VEL-Y", iPoint, Node_Struc->GetSolution_time_n(iPoint, nDim + 1));
+  if (nDim == 3)
+    SetVolumeOutputValue("SENS_VEL-Z", iPoint, Node_Struc->GetSolution_time_n(iPoint, 5));
+
+  SetVolumeOutputValue("SENS_ACCEL-X", iPoint, Node_Struc->GetSolution_time_n(iPoint, 2 * nDim));
+  SetVolumeOutputValue("SENS_ACCEL-Y", iPoint, Node_Struc->GetSolution_time_n(iPoint, 2 * nDim + 1));
+  if (nDim == 3)
+    SetVolumeOutputValue("SENS_ACCEL-Z", iPoint, Node_Struc->GetSolution_time_n(iPoint, 8));
 }
 
 void CAdjElasticityOutput::SetVolumeOutputFields(CConfig *config){
@@ -223,4 +240,23 @@ void CAdjElasticityOutput::SetVolumeOutputFields(CConfig *config){
     AddVolumeOutput("SENSITIVITY-Z", "Sensitivity_z", "SENSITIVITY", "geometric sensitivity  in the z direction");
   /// END_GROUP
 
+  if (!config->GetTime_Domain()) return;
+
+  /*--- Sensitivities with respect to initial conditions. ---*/
+
+  AddVolumeOutput("SENS_DISP-X", "SensInitialDisp_x", "SENSITIVITY_T0", "sensitivity to the initial x displacement");
+  AddVolumeOutput("SENS_DISP-Y", "SensInitialDisp_y", "SENSITIVITY_T0", "sensitivity to the initial y displacement");
+  if (nDim == 3)
+    AddVolumeOutput("SENS_DISP-Z", "SensInitialDisp_z", "SENSITIVITY_T0", "sensitivity to the initial z displacement");
+
+  AddVolumeOutput("SENS_VEL-X", "SensInitialVel_x", "SENSITIVITY_T0", "sensitivity to the initial x velocity");
+  AddVolumeOutput("SENS_VEL-Y", "SensInitialVel_y", "SENSITIVITY_T0", "sensitivity to the initial y velocity");
+  if (nDim == 3)
+    AddVolumeOutput("SENS_VEL-Z", "SensInitialVel_z", "SENSITIVITY_T0", "sensitivity to the initial z velocity");
+
+  AddVolumeOutput("SENS_ACCEL-X", "SensInitialAccel_x", "SENSITIVITY_T0", "sensitivity to the initial x acceleration");
+  AddVolumeOutput("SENS_ACCEL-Y", "SensInitialAccel_y", "SENSITIVITY_T0", "sensitivity to the initial y acceleration");
+  if (nDim == 3)
+    AddVolumeOutput("SENS_ACCEL-Z", "SensInitialAccel_z", "SENSITIVITY_T0", "sensitivity to the initial z acceleration");
+
 }
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index 3fc02d126e7..bff61c408c9 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -873,8 +873,8 @@ void CFlowOutput::SetCustomOutputs(const CSolver* const* solver, const CGeometry
           const auto varIdx = i % CustomOutput::MAX_VARS_PER_SOLVER;
           if (solIdx == FLOW_SOL) {
             return flowNodes->GetPrimitive(iPoint, varIdx);
-          }             return solver[solIdx]->GetNodes()->GetSolution(iPoint, varIdx);
-         
+          }
+          return solver[solIdx]->GetNodes()->GetSolution(iPoint, varIdx);
         } else {
           return *output.otherOutputs[i - CustomOutput::NOT_A_VARIABLE];
         }
diff --git a/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp b/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
index 5a03df9aff7..5b38d271497 100644
--- a/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
+++ b/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
@@ -125,14 +125,18 @@ CDiscAdjFEASolver::~CDiscAdjFEASolver() { delete nodes; }
 void CDiscAdjFEASolver::SetRecording(CGeometry* geometry, CConfig *config){
 
   unsigned long iPoint;
-  unsigned short iVar;
+  unsigned short iDim, iVar;
 
   /*--- Reset the solution to the initial (converged) solution ---*/
 
-  for (iPoint = 0; iPoint < nPoint; iPoint++)
+  for (iPoint = 0; iPoint < nPoint; iPoint++) {
     for (iVar = 0; iVar < nVar; iVar++)
       direct_solver->GetNodes()->SetSolution(iPoint, iVar, nodes->GetSolution_Direct(iPoint)[iVar]);
 
+    auto Coord = geometry->nodes->GetCoord(iPoint);
+    for (iDim = 0; iDim < nDim; iDim++) AD::ResetInput(Coord[iDim]);
+  }
+
   /*--- Reset the input for time n ---*/
 
   if (config->GetTime_Domain()) {
@@ -198,6 +202,8 @@ void CDiscAdjFEASolver::RegisterVariables(CGeometry *geometry, CConfig *config,
       for (iVar = 0; iVar < nDV; iVar++) AD::ResetInput(DV[iVar]);
     }
 
+    direct_solver->GetNodes()->ResetInputFlowTraction();
+
     if (!reset) {
       E.Register();
       Nu.Register();
@@ -294,7 +300,7 @@ void CDiscAdjFEASolver::ExtractAdjoint_Variables(CGeometry *geometry, CConfig *c
   if (config->GetnMarker_Fluid_Load() > 0) {
     for (unsigned long iPoint = 0; iPoint < nPoint; iPoint++){
       for (unsigned short iDim = 0; iDim < nDim; iDim++){
-        su2double val_sens = direct_solver->GetNodes()->ExtractFlowTraction_Sensitivity(iPoint,iDim);
+        su2double val_sens = direct_solver->GetNodes()->ExtractFlowTractionSensitivity(iPoint,iDim);
         nodes->SetFlowTractionSensitivity(iPoint, iDim, val_sens);
       }
     }
@@ -366,12 +372,12 @@ void CDiscAdjFEASolver::SetSensitivity(CGeometry *geometry, CConfig *config, CSo
 
   for (unsigned long iPoint = 0; iPoint < nPoint; iPoint++) {
 
-    auto Coord = geometry->nodes->GetCoord(iPoint);
+    //auto Coord = geometry->nodes->GetCoord(iPoint);
 
     for (unsigned short iDim = 0; iDim < nDim; iDim++) {
 
       su2double Sensitivity = geometry->nodes->GetAdjointSolution(iPoint, iDim);
-      AD::ResetInput(Coord[iDim]);
+      //AD::ResetInput(Coord[iDim]);
 
       if (!time_domain) {
         nodes->SetSensitivity(iPoint, iDim, Sensitivity);
diff --git a/SU2_CFD/src/variables/CFEABoundVariable.cpp b/SU2_CFD/src/variables/CFEABoundVariable.cpp
index d61f6b2e524..3124f0d93ca 100644
--- a/SU2_CFD/src/variables/CFEABoundVariable.cpp
+++ b/SU2_CFD/src/variables/CFEABoundVariable.cpp
@@ -75,3 +75,10 @@ void CFEABoundVariable::RegisterFlowTraction() {
     for (unsigned long iVar = 0; iVar < nVar; iVar++)
       AD::RegisterInput(FlowTraction(iVertex,iVar));
 }
+
+void CFEABoundVariable::ResetInputFlowTraction() {
+  if (!fsi_analysis) return;
+  for (unsigned long iVertex = 0; iVertex < FlowTraction.rows(); iVertex++)
+    for (unsigned long iVar = 0; iVar < nVar; iVar++)
+      AD::ResetInput(FlowTraction(iVertex,iVar));
+}
\ No newline at end of file
diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index 772b7012db7..e88a480b52d 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -276,7 +276,7 @@ def main():
     discadj_fsi2.cfg_dir   = "disc_adj_fsi/Airfoil_2d"
     discadj_fsi2.cfg_file  = "config.cfg"
     discadj_fsi2.test_iter = 8
-    discadj_fsi2.test_vals         = [-4.349377, 0.128475, -1.303589, 7.5407e-09, 2.3244]
+    discadj_fsi2.test_vals         = [-4.349377, 0.189968, -1.303589, 7.5407e-09, 2.3244]
     discadj_fsi2.test_vals_aarch64 = [-3.479505, 0.127953, -1.303589, 7.5407e-09, 2.3244]
     discadj_fsi2.tol       = 0.00001
     test_list.append(discadj_fsi2)
@@ -413,7 +413,7 @@ def main():
     pywrapper_Unst_FEA_AD.cfg_dir = "py_wrapper/custom_load_fea"
     pywrapper_Unst_FEA_AD.cfg_file = "config.cfg"
     pywrapper_Unst_FEA_AD.test_iter = 100
-    pywrapper_Unst_FEA_AD.test_vals = [0.256684, 0.256684, 0.031988, 0.032015]
+    pywrapper_Unst_FEA_AD.test_vals = [0.256684, 0.256684, 0.031988, 0.032015, -18.44906, -18.45085]
     pywrapper_Unst_FEA_AD.command = TestCase.Command("mpirun -n 2", "python", "run_ad.py")
     pywrapper_Unst_FEA_AD.timeout = 1600
     pywrapper_Unst_FEA_AD.tol = 0.00001
diff --git a/TestCases/py_wrapper/custom_load_fea/run_ad.py b/TestCases/py_wrapper/custom_load_fea/run_ad.py
index cc85ca00239..76a020631c6 100644
--- a/TestCases/py_wrapper/custom_load_fea/run_ad.py
+++ b/TestCases/py_wrapper/custom_load_fea/run_ad.py
@@ -55,7 +55,7 @@
 
 MESH_FORMAT= RECTANGLE
 MESH_BOX_SIZE= ( 17, 5, 0 )
-MESH_BOX_LENGTH= ( 0.5, 0.05, 0 )
+MESH_BOX_LENGTH= ( 0.5, __HEIGHT__, 0 )
 
 OUTPUT_FILES= RESTART, PARAVIEW
 OUTPUT_WRT_FREQ= 1
@@ -84,6 +84,7 @@
 UNST_ADJOINT_ITER= 21
 ITER_AVERAGE_OBJ= 0
 SOLUTION_FILENAME= restart.dat
+VOLUME_OUTPUT= SENSITIVITY_T0
 """
 
 
@@ -110,12 +111,16 @@ def ApplyLoad(driver, marker_id, peak_load):
   return derivatives
 
 
-def RunPrimal(density, peak_load):
-  """Runs the primal solver for a given density and peak load and returns the time average objective function."""
+def RunPrimal(density, peak_load, height):
+  """
+  Runs the primal solver for a given density, peak load, and beam height.
+  Returns the time average objective function.
+  """
   comm = MPI.COMM_WORLD
 
   with open('config_unsteady.cfg', 'w') as f:
-    f.write(common_settings.replace('__DENSITY__', str(density)) + primal_settings)
+    f.write(common_settings.replace('__DENSITY__', str(density)).replace('__HEIGHT__', str(height)) +
+            primal_settings)
 
   # Initialize the primal driver of SU2, this includes solver preprocessing.
   try:
@@ -144,15 +149,16 @@ def RunPrimal(density, peak_load):
   return tavg_stress_penalty
 
 
-def RunAdjoint(density, peak_load):
+def RunAdjoint(density, peak_load, height):
   """
   Runs the adjoint solver and returns the sensitivity of the objective function to the peak
-  load and to the material density.
+  load, to the material density, and to the beam height.
   """
   comm = MPI.COMM_WORLD
 
   with open('config_unsteady_ad.cfg', 'w') as f:
-    f.write(common_settings.replace('__DENSITY__', str(density)) + adjoint_settings)
+    f.write(common_settings.replace('__DENSITY__', str(density)).replace('__HEIGHT__', str(height)) +
+            adjoint_settings)
 
   # Initialize the adjoint driver of SU2, this includes solver preprocessing.
   try:
@@ -182,7 +188,8 @@ def RunAdjoint(density, peak_load):
     driver.Postprocess()
     driver.Update()
 
-    # Accumulate sensitivies.
+    # Accumulate load sensitivies (the solver doesn't accumulate
+    # these for when they are used for FSI adjoints).
     for i_vertex in range(n_vertex):
       load_sens += derivatives[i_vertex] * driver.GetMarkerFEALoadSensitivity(marker_id, i_vertex)[1]
 
@@ -192,10 +199,19 @@ def RunAdjoint(density, peak_load):
 
   rho_sens = driver.GetOutputValue('SENS_RHO_0')
 
+  height_sens = 0.0
+  sensitivity = driver.Sensitivity(driver.GetSolverIndices()['ADJ.FEA'])
+  coords = driver.Coordinates()
+
+  for i_node in range(driver.GetNumberNodes() - driver.GetNumberHaloNodes()):
+    y = coords(i_node, 1)
+    dy_dh = y / height
+    height_sens += dy_dh * sensitivity(i_node, 1)
+
   # Finalize the solver and exit cleanly.
   driver.Finalize()
 
-  return comm.allreduce(load_sens), rho_sens
+  return comm.allreduce(load_sens), rho_sens, comm.allreduce(height_sens)
 
 
 def main():
@@ -203,26 +219,31 @@ def main():
   rank = comm.Get_rank()
 
   # Run the primal with 2 loads to compute the sensitivity via finite differences.
-  obj_pert_load = RunPrimal(1, 2.002)
-  obj_pert_rho = RunPrimal(1.0001, 2)
-  obj = RunPrimal(1, 2)
+  obj_pert_height = RunPrimal(1, 2, 0.05001)
+  obj_pert_load = RunPrimal(1, 2.002, 0.05)
+  obj_pert_rho = RunPrimal(1.0001, 2, 0.05)
+  # Run the un-perturbed last to use the restarts for the adjoint.
+  obj = RunPrimal(1, 2, 0.05)
+  sens_height_fd = (obj_pert_height - obj) / 0.00001
   sens_load_fd = (obj_pert_load - obj) / 0.002
   sens_rho_fd = (obj_pert_rho - obj) / 0.0001
 
-  sens_load, sens_rho = RunAdjoint(1, 2)
+  sens_load, sens_rho, sens_height = RunAdjoint(1, 2, 0.05)
 
   if rank == 0:
-    print("      Finite Differences\tDiscrete Adjoint")
-    print(f"Load  {sens_load_fd}\t{sens_load}")
-    print(f"Rho   {sens_rho_fd}\t{sens_rho}")
+    print("       Finite Differences\tDiscrete Adjoint")
+    print(f"Height {sens_height_fd}\t{sens_height}")
+    print(f"Load   {sens_load_fd}\t{sens_load}")
+    print(f"Rho    {sens_rho_fd}\t{sens_rho}")
 
+  assert abs(sens_height / sens_height_fd - 1) < 1e-4, "Error in geometric derivatives."
   assert abs(sens_load / sens_load_fd - 1) < 1e-4, "Error in load derivative."
-  assert abs(sens_rho / sens_rho_fd - 1) < 1e-3, "Error in density derivative."
+  assert abs(sens_rho / sens_rho_fd - 1) < 1e-3, "Error in material derivative."
 
   # Print results for the regression script to check.
   if rank == 0:
     print("\n")
-    print(100, 100, sens_load_fd, sens_load, sens_rho_fd, sens_rho)
+    print(100, 100, sens_load_fd, sens_load, sens_rho_fd, sens_rho, sens_height_fd, sens_height)
 
 
 if __name__ == '__main__':

From 51a9cb948043481dbf4500711bf35474eeec7f0e Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 22 Apr 2023 17:55:29 -0700
Subject: [PATCH 408/656] cleanup

---
 .../geometry/elements/CElementProperty.hpp    |  8 +++--
 .../include/variables/CFEABoundVariable.hpp   |  7 +---
 SU2_CFD/include/variables/CVariable.hpp       |  7 +---
 SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp     | 32 ++++++-------------
 SU2_CFD/src/solvers/CDiscAdjSolver.cpp        |  5 ---
 SU2_CFD/src/variables/CFEABoundVariable.cpp   | 12 ++-----
 TestCases/parallel_regression_AD.py           |  2 +-
 .../py_wrapper/custom_load_fea/run_ad.py      |  2 +-
 8 files changed, 23 insertions(+), 52 deletions(-)

diff --git a/Common/include/geometry/elements/CElementProperty.hpp b/Common/include/geometry/elements/CElementProperty.hpp
index fce7425694e..90efe7194b7 100644
--- a/Common/include/geometry/elements/CElementProperty.hpp
+++ b/Common/include/geometry/elements/CElementProperty.hpp
@@ -93,7 +93,7 @@ class CProperty {
   /*!
    * \brief Extract the derivative of the Design density.
    */
-  inline virtual su2double GetAdjointDensity(void) const { return 0.0; }
+  inline virtual su2double GetAdjointDensity(void) { return 0.0; }
 
   /*!
    * \brief Register the Design density as an AD input variable.
@@ -177,7 +177,11 @@ class CElementProperty final : public CProperty {
   /*!
    * \brief Extract the derivative of the Design density.
    */
-  inline su2double GetAdjointDensity(void) const override { return SU2_TYPE::GetDerivative(design_rho); }
+  inline su2double GetAdjointDensity(void) override {
+    su2double der = SU2_TYPE::GetDerivative(design_rho);
+    AD::ResetInput(design_rho);
+    return der;
+  }
 
   /*!
    * \brief Register the Design density as an AD input variable.
diff --git a/SU2_CFD/include/variables/CFEABoundVariable.hpp b/SU2_CFD/include/variables/CFEABoundVariable.hpp
index 950fef78ebe..e0f8c273cc1 100644
--- a/SU2_CFD/include/variables/CFEABoundVariable.hpp
+++ b/SU2_CFD/include/variables/CFEABoundVariable.hpp
@@ -157,12 +157,7 @@ class CFEABoundVariable final : public CFEAVariable {
   /*!
    * \brief Register the flow tractions as input variable.
    */
-  void RegisterFlowTraction() override;
-
-  /*!
-   * \brief Resets the AD indices of the flow tractions.
-   */
-  void ResetInputFlowTraction() override;
+  void RegisterFlowTraction(bool reset) override;
 
   /*!
    * \brief Extract the flow traction derivatives.
diff --git a/SU2_CFD/include/variables/CVariable.hpp b/SU2_CFD/include/variables/CVariable.hpp
index efdbc25c9ce..aa75d07596d 100644
--- a/SU2_CFD/include/variables/CVariable.hpp
+++ b/SU2_CFD/include/variables/CVariable.hpp
@@ -2160,12 +2160,7 @@ class CVariable {
   /*!
    * \brief A virtual member.
    */
-  inline virtual void RegisterFlowTraction() { }
-
-  /*!
-   * \brief A virtual member.
-   */
-  inline virtual void ResetInputFlowTraction() { }
+  inline virtual void RegisterFlowTraction(bool reset) { }
 
   /*!
    * \brief A virtual member.
diff --git a/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp b/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
index 5b38d271497..b64d409e5cc 100644
--- a/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
+++ b/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
@@ -124,32 +124,21 @@ CDiscAdjFEASolver::~CDiscAdjFEASolver() { delete nodes; }
 
 void CDiscAdjFEASolver::SetRecording(CGeometry* geometry, CConfig *config){
 
-  unsigned long iPoint;
-  unsigned short iDim, iVar;
-
   /*--- Reset the solution to the initial (converged) solution ---*/
 
-  for (iPoint = 0; iPoint < nPoint; iPoint++) {
-    for (iVar = 0; iVar < nVar; iVar++)
+  for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
+    for (auto iVar = 0u; iVar < nVar; iVar++)
       direct_solver->GetNodes()->SetSolution(iPoint, iVar, nodes->GetSolution_Direct(iPoint)[iVar]);
-
-    auto Coord = geometry->nodes->GetCoord(iPoint);
-    for (iDim = 0; iDim < nDim; iDim++) AD::ResetInput(Coord[iDim]);
   }
 
   /*--- Reset the input for time n ---*/
 
   if (config->GetTime_Domain()) {
-    for (iPoint = 0; iPoint < nPoint; iPoint++)
-      for (iVar = 0; iVar < nVar; iVar++)
+    for (auto iPoint = 0ul; iPoint < nPoint; iPoint++)
+      for (auto iVar = 0u; iVar < nVar; iVar++)
         AD::ResetInput(direct_solver->GetNodes()->GetSolution_time_n(iPoint)[iVar]);
   }
 
-  /*--- Set the Jacobian to zero since this is not done inside the meanflow iteration
-   * when running the discrete adjoint solver. ---*/
-
-  direct_solver->Jacobian.SetValZero();
-
   /*--- Set indices to zero ---*/
 
   RegisterVariables(geometry, config, true);
@@ -202,8 +191,6 @@ void CDiscAdjFEASolver::RegisterVariables(CGeometry *geometry, CConfig *config,
       for (iVar = 0; iVar < nDV; iVar++) AD::ResetInput(DV[iVar]);
     }
 
-    direct_solver->GetNodes()->ResetInputFlowTraction();
-
     if (!reset) {
       E.Register();
       Nu.Register();
@@ -211,10 +198,11 @@ void CDiscAdjFEASolver::RegisterVariables(CGeometry *geometry, CConfig *config,
       Rho_DL.Register();
       if (de_effects) EField.Register();
       if (fea_dv) DV.Register();
+    }
 
-      /*--- Register the flow tractions ---*/
-      if (config->GetnMarker_Fluid_Load() > 0)
-        direct_solver->GetNodes()->RegisterFlowTraction();
+    /*--- Register or reset the flow tractions ---*/
+    if (config->GetnMarker_Fluid_Load() > 0) {
+      direct_solver->GetNodes()->RegisterFlowTraction(reset);
     }
 
   }
@@ -372,12 +360,12 @@ void CDiscAdjFEASolver::SetSensitivity(CGeometry *geometry, CConfig *config, CSo
 
   for (unsigned long iPoint = 0; iPoint < nPoint; iPoint++) {
 
-    //auto Coord = geometry->nodes->GetCoord(iPoint);
+    auto Coord = geometry->nodes->GetCoord(iPoint);
 
     for (unsigned short iDim = 0; iDim < nDim; iDim++) {
 
       su2double Sensitivity = geometry->nodes->GetAdjointSolution(iPoint, iDim);
-      //AD::ResetInput(Coord[iDim]);
+      AD::ResetInput(Coord[iDim]);
 
       if (!time_domain) {
         nodes->SetSensitivity(iPoint, iDim, Sensitivity);
diff --git a/SU2_CFD/src/solvers/CDiscAdjSolver.cpp b/SU2_CFD/src/solvers/CDiscAdjSolver.cpp
index d6d94cf0d58..e236b19114d 100644
--- a/SU2_CFD/src/solvers/CDiscAdjSolver.cpp
+++ b/SU2_CFD/src/solvers/CDiscAdjSolver.cpp
@@ -146,11 +146,6 @@ void CDiscAdjSolver::SetRecording(CGeometry* geometry, CConfig *config){
     END_SU2_OMP_FOR
   }
 
-  /*--- Set the Jacobian to zero since this is not done inside the fluid iteration
-   * when running the discrete adjoint solver. ---*/
-
-  direct_solver->Jacobian.SetValZero();
-
   /*--- Set indices to zero ---*/
 
   RegisterVariables(geometry, config, true);
diff --git a/SU2_CFD/src/variables/CFEABoundVariable.cpp b/SU2_CFD/src/variables/CFEABoundVariable.cpp
index 3124f0d93ca..012498896ad 100644
--- a/SU2_CFD/src/variables/CFEABoundVariable.cpp
+++ b/SU2_CFD/src/variables/CFEABoundVariable.cpp
@@ -69,16 +69,10 @@ void CFEABoundVariable::Clear_FlowTraction() { FlowTraction.setConstant(0.0); }
 
 void CFEABoundVariable::Clear_SurfaceLoad_Res() { Residual_Ext_Surf.setConstant(0.0); }
 
-void CFEABoundVariable::RegisterFlowTraction() {
+void CFEABoundVariable::RegisterFlowTraction(bool reset) {
   if (!fsi_analysis) return;
   for (unsigned long iVertex = 0; iVertex < FlowTraction.rows(); iVertex++)
     for (unsigned long iVar = 0; iVar < nVar; iVar++)
-      AD::RegisterInput(FlowTraction(iVertex,iVar));
+      if (reset) AD::ResetInput(FlowTraction(iVertex,iVar));
+      else AD::RegisterInput(FlowTraction(iVertex,iVar));
 }
-
-void CFEABoundVariable::ResetInputFlowTraction() {
-  if (!fsi_analysis) return;
-  for (unsigned long iVertex = 0; iVertex < FlowTraction.rows(); iVertex++)
-    for (unsigned long iVar = 0; iVar < nVar; iVar++)
-      AD::ResetInput(FlowTraction(iVertex,iVar));
-}
\ No newline at end of file
diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index e88a480b52d..1f2d4297dd9 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -413,7 +413,7 @@ def main():
     pywrapper_Unst_FEA_AD.cfg_dir = "py_wrapper/custom_load_fea"
     pywrapper_Unst_FEA_AD.cfg_file = "config.cfg"
     pywrapper_Unst_FEA_AD.test_iter = 100
-    pywrapper_Unst_FEA_AD.test_vals = [0.256684, 0.256684, 0.031988, 0.032015, -18.44906, -18.45085]
+    pywrapper_Unst_FEA_AD.test_vals = [0.256684, 0.256684, 0.319877, 0.320149, -0.184491, -0.184509]
     pywrapper_Unst_FEA_AD.command = TestCase.Command("mpirun -n 2", "python", "run_ad.py")
     pywrapper_Unst_FEA_AD.timeout = 1600
     pywrapper_Unst_FEA_AD.tol = 0.00001
diff --git a/TestCases/py_wrapper/custom_load_fea/run_ad.py b/TestCases/py_wrapper/custom_load_fea/run_ad.py
index 76a020631c6..dd64982b51b 100644
--- a/TestCases/py_wrapper/custom_load_fea/run_ad.py
+++ b/TestCases/py_wrapper/custom_load_fea/run_ad.py
@@ -243,7 +243,7 @@ def main():
   # Print results for the regression script to check.
   if rank == 0:
     print("\n")
-    print(100, 100, sens_load_fd, sens_load, sens_rho_fd, sens_rho, sens_height_fd, sens_height)
+    print(100, 100, sens_load_fd, sens_load, sens_rho_fd * 10, sens_rho * 10, sens_height_fd / 100, sens_height / 100)
 
 
 if __name__ == '__main__':

From 2b7b16f456ea98b68cdd98dfd6819e0dd7294713 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 23 Apr 2023 10:53:45 -0700
Subject: [PATCH 409/656] update regression

---
 TestCases/parallel_regression_AD.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index 1f2d4297dd9..61c79202fb8 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -276,7 +276,7 @@ def main():
     discadj_fsi2.cfg_dir   = "disc_adj_fsi/Airfoil_2d"
     discadj_fsi2.cfg_file  = "config.cfg"
     discadj_fsi2.test_iter = 8
-    discadj_fsi2.test_vals         = [-4.349377, 0.189968, -1.303589, 7.5407e-09, 2.3244]
+    discadj_fsi2.test_vals         = [-4.349377, 0.192713, -1.303589, 7.5407e-09, 2.3244]
     discadj_fsi2.test_vals_aarch64 = [-3.479505, 0.127953, -1.303589, 7.5407e-09, 2.3244]
     discadj_fsi2.tol       = 0.00001
     test_list.append(discadj_fsi2)

From 2db8e75341a2a2250e45f5d6c4db88e9d18c4148 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Thu, 27 Apr 2023 08:26:07 -0700
Subject: [PATCH 410/656] py wrapper heat solver example, cleanup discadj fluid
 iteration, some fixes for unsteady adjoints

---
 SU2_CFD/include/drivers/CDriverBase.hpp       |  19 ++
 SU2_CFD/include/variables/CVariable.hpp       |   1 +
 .../src/drivers/CDiscAdjSinglezoneDriver.cpp  |   4 +
 SU2_CFD/src/drivers/CSinglezoneDriver.cpp     |   4 +-
 .../src/iteration/CDiscAdjFluidIteration.cpp  | 166 ++++++------
 .../src/iteration/CDiscAdjHeatIteration.cpp   |  86 +++---
 SU2_CFD/src/output/CAdjElasticityOutput.cpp   |  18 +-
 SU2_CFD/src/output/CAdjHeatOutput.cpp         |  15 ++
 TestCases/parallel_regression_AD.py           |  13 +
 .../py_wrapper/custom_heat_flux/run_ad.py     | 246 ++++++++++++++++++
 .../py_wrapper/custom_load_fea/run_ad.py      |   2 +-
 11 files changed, 431 insertions(+), 143 deletions(-)
 create mode 100644 TestCases/py_wrapper/custom_heat_flux/run_ad.py

diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index d720246efb7..c7123daff4b 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -473,6 +473,25 @@ class CDriverBase {
         "MarkerSolutionTimeN of " + solver->GetSolverName(), false);
   }
 
+  /*!
+   * \brief Get a read/write view of the solution at time N-1 on all mesh nodes of a solver.
+   */
+  inline CPyWrapperMatrixView SolutionTimeN1(unsigned short iSolver) {
+    auto* solver = GetSolverAndCheckMarker(iSolver);
+    return CPyWrapperMatrixView(
+        solver->GetNodes()->GetSolution_time_n1(), "SolutionTimeN1 of " + solver->GetSolverName(), false);
+  }
+
+  /*!
+   * \brief Get a read/write view of the solution at time N-1 on the mesh nodes of a marker.
+   */
+  inline CPyWrapperMarkerMatrixView MarkerSolutionTimeN1(unsigned short iSolver, unsigned short iMarker) {
+    auto* solver = GetSolverAndCheckMarker(iSolver, iMarker);
+    return CPyWrapperMarkerMatrixView(
+        solver->GetNodes()->GetSolution_time_n1(), main_geometry->vertex[iMarker], main_geometry->GetnVertex(iMarker),
+        "MarkerSolutionTimeN1 of " + solver->GetSolverName(), false);
+  }
+
   /*!
    * \brief Get the flow solver primitive variable names with their associated indices.
    * These correspond to the column indices in the matrix returned by Primitives.
diff --git a/SU2_CFD/include/variables/CVariable.hpp b/SU2_CFD/include/variables/CVariable.hpp
index aa75d07596d..a5beafd75e0 100644
--- a/SU2_CFD/include/variables/CVariable.hpp
+++ b/SU2_CFD/include/variables/CVariable.hpp
@@ -500,6 +500,7 @@ class CVariable {
    * \return Pointer to the solution (at time n-1) vector.
    */
   inline su2double *GetSolution_time_n1(unsigned long iPoint) { return Solution_time_n1[iPoint]; }
+  inline MatrixType& GetSolution_time_n1() { return Solution_time_n1; }
 
   /*!
    * \brief Set the value of the old residual.
diff --git a/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
index f9cfb269a8e..7731d8899bb 100644
--- a/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
@@ -129,6 +129,10 @@ CDiscAdjSinglezoneDriver::~CDiscAdjSinglezoneDriver() {
 
 void CDiscAdjSinglezoneDriver::Preprocess(unsigned long TimeIter) {
 
+  /*--- Set the current time iteration in the config and also in the driver
+   * because the python interface doesn't offer an explicit way of doing it. ---*/
+
+  this->TimeIter = TimeIter;
   config_container[ZONE_0]->SetTimeIter(TimeIter);
 
   /*--- Preprocess the adjoint iteration ---*/
diff --git a/SU2_CFD/src/drivers/CSinglezoneDriver.cpp b/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
index 3a3518d33ab..964888a83fb 100644
--- a/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
@@ -110,8 +110,10 @@ void CSinglezoneDriver::StartSolver() {
 
 void CSinglezoneDriver::Preprocess(unsigned long TimeIter) {
 
-  /*--- Set the current time iteration in the config ---*/
+  /*--- Set the current time iteration in the config and also in the driver
+   * because the python interface doesn't offer an explicit way of doing it. ---*/
 
+  this->TimeIter = TimeIter;
   config_container[ZONE_0]->SetTimeIter(TimeIter);
 
   /*--- Store the current physical time in the config container, as
diff --git a/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
index 93e29ff3f30..5a48a262390 100644
--- a/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
@@ -308,36 +308,28 @@ void CDiscAdjFluidIteration::Preprocess(COutput* output, CIntegration**** integr
   /*--- Store flow solution also in the adjoint solver in order to be able to reset it later ---*/
 
   if (TimeIter == 0 || dual_time) {
-    for (auto iMesh = 0u; iMesh <= config[iZone]->GetnMGLevels(); iMesh++) {
-      auto solvers = solver[iZone][iInst][iMesh];
+    auto SetSolutionDirect = [&](CSolver** solvers, int adj, int primal, unsigned long nPoint) {
       SU2_OMP_FOR_STAT(1024)
-      for (auto iPoint = 0ul; iPoint < geometries[iMesh]->GetnPoint(); iPoint++)
-        solvers[ADJFLOW_SOL]->GetNodes()->SetSolution_Direct(iPoint, solvers[FLOW_SOL]->GetNodes()->GetSolution(iPoint));
+      for (auto iPoint = 0ul; iPoint < nPoint; iPoint++)
+        solvers[adj]->GetNodes()->SetSolution_Direct(iPoint, solvers[primal]->GetNodes()->GetSolution(iPoint));
       END_SU2_OMP_FOR
+    };
+
+    for (auto iMesh = 0u; iMesh <= config[iZone]->GetnMGLevels(); iMesh++) {
+      auto solvers = solver[iZone][iInst][iMesh];
+      SetSolutionDirect(solvers, ADJFLOW_SOL, FLOW_SOL, geometries[iMesh]->GetnPoint());
     }
     if (turbulent && !config[iZone]->GetFrozen_Visc_Disc()) {
-      SU2_OMP_FOR_STAT(1024)
-      for (auto iPoint = 0ul; iPoint < geometries[MESH_0]->GetnPoint(); iPoint++)
-        solvers0[ADJTURB_SOL]->GetNodes()->SetSolution_Direct(iPoint, solvers0[TURB_SOL]->GetNodes()->GetSolution(iPoint));
-      END_SU2_OMP_FOR
+      SetSolutionDirect(solvers0, ADJTURB_SOL, TURB_SOL, geometries[MESH_0]->GetnPoint());
     }
     if (species) {
-      SU2_OMP_FOR_STAT(1024)
-      for (auto iPoint = 0ul; iPoint < geometries[MESH_0]->GetnPoint(); iPoint++)
-        solvers0[ADJSPECIES_SOL]->GetNodes()->SetSolution_Direct(iPoint, solvers0[SPECIES_SOL]->GetNodes()->GetSolution(iPoint));
-      END_SU2_OMP_FOR
+      SetSolutionDirect(solvers0, ADJSPECIES_SOL, SPECIES_SOL, geometries[MESH_0]->GetnPoint());
     }
     if (heat) {
-      SU2_OMP_FOR_STAT(1024)
-      for (auto iPoint = 0ul; iPoint < geometries[MESH_0]->GetnPoint(); iPoint++)
-        solvers0[ADJHEAT_SOL]->GetNodes()->SetSolution_Direct(iPoint, solvers0[HEAT_SOL]->GetNodes()->GetSolution(iPoint));
-      END_SU2_OMP_FOR
+      SetSolutionDirect(solvers0, ADJHEAT_SOL, HEAT_SOL, geometries[MESH_0]->GetnPoint());
     }
     if (config[iZone]->AddRadiation()) {
-      SU2_OMP_FOR_STAT(1024)
-      for (auto iPoint = 0ul; iPoint < geometries[MESH_0]->GetnPoint(); iPoint++)
-        solvers0[ADJRAD_SOL]->GetNodes()->SetSolution_Direct(iPoint, solvers0[RAD_SOL]->GetNodes()->GetSolution(iPoint));
-      END_SU2_OMP_FOR
+      SetSolutionDirect(solvers0, ADJRAD_SOL, RAD_SOL, geometries[MESH_0]->GetnPoint());
     }
   }
 
@@ -369,22 +361,23 @@ void CDiscAdjFluidIteration::LoadUnsteady_Solution(CGeometry**** geometry, CSolv
                                                    unsigned short iZone, unsigned short iInst, int DirectIter) {
 
   auto solvers = solver[iZone][iInst];
+  auto geometries = geometry[iZone][iInst];
   const bool species = config[iZone]->GetKind_Species_Model() != SPECIES_MODEL::NONE;
 
   if (DirectIter >= 0) {
     if (rank == MASTER_NODE)
       cout << " Loading flow solution from direct iteration " << DirectIter << " for zone " << iZone << "." << endl;
 
-    solvers[MESH_0][FLOW_SOL]->LoadRestart(geometry[iZone][iInst], solvers, config[iZone], DirectIter, true);
+    solvers[MESH_0][FLOW_SOL]->LoadRestart(geometries, solvers, config[iZone], DirectIter, true);
 
     if (turbulent) {
-      solvers[MESH_0][TURB_SOL]->LoadRestart(geometry[iZone][iInst], solvers, config[iZone], DirectIter, false);
+      solvers[MESH_0][TURB_SOL]->LoadRestart(geometries, solvers, config[iZone], DirectIter, false);
     }
     if (species) {
-      solvers[MESH_0][SPECIES_SOL]->LoadRestart(geometry[iZone][iInst], solvers, config[iZone], DirectIter, false);
+      solvers[MESH_0][SPECIES_SOL]->LoadRestart(geometries, solvers, config[iZone], DirectIter, false);
     }
     if (config[iZone]->GetWeakly_Coupled_Heat()) {
-      solvers[MESH_0][HEAT_SOL]->LoadRestart(geometry[iZone][iInst], solvers, config[iZone], DirectIter, false);
+      solvers[MESH_0][HEAT_SOL]->LoadRestart(geometries, solvers, config[iZone], DirectIter, false);
     }
   } else {
     /*--- If there is no solution file we set the freestream condition ---*/
@@ -393,19 +386,19 @@ void CDiscAdjFluidIteration::LoadUnsteady_Solution(CGeometry**** geometry, CSolv
 
     for (auto iMesh = 0u; iMesh <= config[iZone]->GetnMGLevels(); iMesh++) {
       solvers[iMesh][FLOW_SOL]->SetFreeStream_Solution(config[iZone]);
-      solvers[iMesh][FLOW_SOL]->Preprocessing(geometry[iZone][iInst][iMesh], solvers[iMesh], config[iZone], iMesh,
+      solvers[iMesh][FLOW_SOL]->Preprocessing(geometries[iMesh], solvers[iMesh], config[iZone], iMesh,
                                               DirectIter, RUNTIME_FLOW_SYS, false);
       if (turbulent) {
         solvers[iMesh][TURB_SOL]->SetFreeStream_Solution(config[iZone]);
-        solvers[iMesh][TURB_SOL]->Postprocessing(geometry[iZone][iInst][iMesh], solvers[iMesh], config[iZone], iMesh);
+        solvers[iMesh][TURB_SOL]->Postprocessing(geometries[iMesh], solvers[iMesh], config[iZone], iMesh);
       }
       if (species) {
         solvers[iMesh][SPECIES_SOL]->SetFreeStream_Solution(config[iZone]);
-        solvers[iMesh][SPECIES_SOL]->Postprocessing(geometry[iZone][iInst][iMesh], solvers[iMesh], config[iZone], iMesh);
+        solvers[iMesh][SPECIES_SOL]->Postprocessing(geometries[iMesh], solvers[iMesh], config[iZone], iMesh);
       }
       if (config[iZone]->GetWeakly_Coupled_Heat()) {
         solvers[iMesh][HEAT_SOL]->SetFreeStream_Solution(config[iZone]);
-        solvers[iMesh][HEAT_SOL]->Postprocessing(geometry[iZone][iInst][iMesh], solvers[iMesh], config[iZone], iMesh);
+        solvers[iMesh][HEAT_SOL]->Postprocessing(geometries[iMesh], solvers[iMesh], config[iZone], iMesh);
       }
     }
   }
@@ -413,29 +406,31 @@ void CDiscAdjFluidIteration::LoadUnsteady_Solution(CGeometry**** geometry, CSolv
 
 void CDiscAdjFluidIteration::IterateDiscAdj(CGeometry**** geometry, CSolver***** solver, CConfig** config,
                                             unsigned short iZone, unsigned short iInst, bool CrossTerm) {
+  auto solvers0 = solver[iZone][iInst][MESH_0];
+  auto geometry0 = geometry[iZone][iInst][MESH_0];
 
-  SU2_OMP_PARALLEL_(if(solver[iZone][iInst][MESH_0][ADJFLOW_SOL]->GetHasHybridParallel())) {
+  SU2_OMP_PARALLEL_(if(solvers0[ADJFLOW_SOL]->GetHasHybridParallel())) {
 
   /*--- Extract the adjoints of the conservative input variables and store them for the next iteration ---*/
 
   if (config[iZone]->GetFluidProblem()) {
-    solver[iZone][iInst][MESH_0][ADJFLOW_SOL]->ExtractAdjoint_Solution(geometry[iZone][iInst][MESH_0], config[iZone], CrossTerm);
+    solvers0[ADJFLOW_SOL]->ExtractAdjoint_Solution(geometry0, config[iZone], CrossTerm);
 
-    solver[iZone][iInst][MESH_0][ADJFLOW_SOL]->ExtractAdjoint_Variables(geometry[iZone][iInst][MESH_0], config[iZone]);
+    solvers0[ADJFLOW_SOL]->ExtractAdjoint_Variables(geometry0, config[iZone]);
   }
   if (turbulent && !config[iZone]->GetFrozen_Visc_Disc()) {
-    solver[iZone][iInst][MESH_0][ADJTURB_SOL]->ExtractAdjoint_Solution(geometry[iZone][iInst][MESH_0], config[iZone], CrossTerm);
+    solvers0[ADJTURB_SOL]->ExtractAdjoint_Solution(geometry0, config[iZone], CrossTerm);
   }
   if (config[iZone]->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
-    solver[iZone][iInst][MESH_0][ADJSPECIES_SOL]->ExtractAdjoint_Solution(geometry[iZone][iInst][MESH_0], config[iZone], CrossTerm);
+    solvers0[ADJSPECIES_SOL]->ExtractAdjoint_Solution(geometry0, config[iZone], CrossTerm);
   }
   if (config[iZone]->GetWeakly_Coupled_Heat()) {
-    solver[iZone][iInst][MESH_0][ADJHEAT_SOL]->ExtractAdjoint_Solution(geometry[iZone][iInst][MESH_0], config[iZone], CrossTerm);
+    solvers0[ADJHEAT_SOL]->ExtractAdjoint_Solution(geometry0, config[iZone], CrossTerm);
   }
   if (config[iZone]->AddRadiation()) {
-    solver[iZone][iInst][MESH_0][ADJRAD_SOL]->ExtractAdjoint_Solution(geometry[iZone][iInst][MESH_0], config[iZone], CrossTerm);
+    solvers0[ADJRAD_SOL]->ExtractAdjoint_Solution(geometry0, config[iZone], CrossTerm);
 
-    solver[iZone][iInst][MESH_0][ADJRAD_SOL]->ExtractAdjoint_Variables(geometry[iZone][iInst][MESH_0], config[iZone]);
+    solvers0[ADJRAD_SOL]->ExtractAdjoint_Variables(geometry0, config[iZone]);
   }
 
   }
@@ -444,33 +439,35 @@ void CDiscAdjFluidIteration::IterateDiscAdj(CGeometry**** geometry, CSolver*****
 
 void CDiscAdjFluidIteration::InitializeAdjoint(CSolver***** solver, CGeometry**** geometry, CConfig** config,
                                                unsigned short iZone, unsigned short iInst) {
+  auto solvers0 = solver[iZone][iInst][MESH_0];
+  auto geometry0 = geometry[iZone][iInst][MESH_0];
 
-  SU2_OMP_PARALLEL_(if(solver[iZone][iInst][MESH_0][ADJFLOW_SOL]->GetHasHybridParallel())) {
+  SU2_OMP_PARALLEL_(if(solvers0[ADJFLOW_SOL]->GetHasHybridParallel())) {
 
   /*--- Initialize the adjoints the conservative variables ---*/
 
   if (config[iZone]->GetFluidProblem()) {
-    solver[iZone][iInst][MESH_0][ADJFLOW_SOL]->SetAdjoint_Output(geometry[iZone][iInst][MESH_0], config[iZone]);
+    solvers0[ADJFLOW_SOL]->SetAdjoint_Output(geometry0, config[iZone]);
   }
 
   if (turbulent && !config[iZone]->GetFrozen_Visc_Disc()) {
-    solver[iZone][iInst][MESH_0][ADJTURB_SOL]->SetAdjoint_Output(geometry[iZone][iInst][MESH_0], config[iZone]);
+    solvers0[ADJTURB_SOL]->SetAdjoint_Output(geometry0, config[iZone]);
   }
 
   if (config[iZone]->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
-    solver[iZone][iInst][MESH_0][ADJSPECIES_SOL]->SetAdjoint_Output(geometry[iZone][iInst][MESH_0], config[iZone]);
+    solvers0[ADJSPECIES_SOL]->SetAdjoint_Output(geometry0, config[iZone]);
   }
 
   if (config[iZone]->GetWeakly_Coupled_Heat()) {
-    solver[iZone][iInst][MESH_0][ADJHEAT_SOL]->SetAdjoint_Output(geometry[iZone][iInst][MESH_0], config[iZone]);
+    solvers0[ADJHEAT_SOL]->SetAdjoint_Output(geometry0, config[iZone]);
   }
 
   if (config[iZone]->AddRadiation()) {
-    solver[iZone][iInst][MESH_0][ADJRAD_SOL]->SetAdjoint_Output(geometry[iZone][iInst][MESH_0], config[iZone]);
+    solvers0[ADJRAD_SOL]->SetAdjoint_Output(geometry0, config[iZone]);
   }
 
   if (config[iZone]->GetFluidProblem() && !config[iZone]->GetMultizone_Problem()) {
-    solver[iZone][iInst][MESH_0][FLOW_SOL]->SetVertexTractionsAdjoint(geometry[iZone][iInst][MESH_0], config[iZone]);
+    solvers0[FLOW_SOL]->SetVertexTractionsAdjoint(geometry0, config[iZone]);
   }
 
   }
@@ -479,46 +476,48 @@ void CDiscAdjFluidIteration::InitializeAdjoint(CSolver***** solver, CGeometry***
 
 void CDiscAdjFluidIteration::RegisterInput(CSolver***** solver, CGeometry**** geometry, CConfig** config,
                                            unsigned short iZone, unsigned short iInst, RECORDING kind_recording) {
+  auto solvers0 = solver[iZone][iInst][MESH_0];
+  auto geometry0 = geometry[iZone][iInst][MESH_0];
 
-  SU2_OMP_PARALLEL_(if(solver[iZone][iInst][MESH_0][ADJFLOW_SOL]->GetHasHybridParallel())) {
+  SU2_OMP_PARALLEL_(if(solvers0[ADJFLOW_SOL]->GetHasHybridParallel())) {
 
   if (kind_recording == RECORDING::SOLUTION_VARIABLES || kind_recording == RECORDING::SOLUTION_AND_MESH) {
     /*--- Register flow and turbulent variables as input ---*/
 
     if (config[iZone]->GetFluidProblem()) {
-      solver[iZone][iInst][MESH_0][ADJFLOW_SOL]->RegisterSolution(geometry[iZone][iInst][MESH_0], config[iZone]);
+      solvers0[ADJFLOW_SOL]->RegisterSolution(geometry0, config[iZone]);
 
-      solver[iZone][iInst][MESH_0][ADJFLOW_SOL]->RegisterVariables(geometry[iZone][iInst][MESH_0], config[iZone]);
+      solvers0[ADJFLOW_SOL]->RegisterVariables(geometry0, config[iZone]);
     }
 
     if (turbulent && !config[iZone]->GetFrozen_Visc_Disc()) {
-      solver[iZone][iInst][MESH_0][ADJTURB_SOL]->RegisterSolution(geometry[iZone][iInst][MESH_0], config[iZone]);
+      solvers0[ADJTURB_SOL]->RegisterSolution(geometry0, config[iZone]);
     }
     if (config[iZone]->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
-      solver[iZone][iInst][MESH_0][ADJSPECIES_SOL]->RegisterSolution(geometry[iZone][iInst][MESH_0], config[iZone]);
+      solvers0[ADJSPECIES_SOL]->RegisterSolution(geometry0, config[iZone]);
     }
     if (config[iZone]->GetWeakly_Coupled_Heat()) {
-      solver[iZone][iInst][MESH_0][ADJHEAT_SOL]->RegisterSolution(geometry[iZone][iInst][MESH_0], config[iZone]);
+      solvers0[ADJHEAT_SOL]->RegisterSolution(geometry0, config[iZone]);
     }
     if (config[iZone]->AddRadiation()) {
-      solver[iZone][iInst][MESH_0][ADJRAD_SOL]->RegisterSolution(geometry[iZone][iInst][MESH_0], config[iZone]);
+      solvers0[ADJRAD_SOL]->RegisterSolution(geometry0, config[iZone]);
 
-      solver[iZone][iInst][MESH_0][ADJRAD_SOL]->RegisterVariables(geometry[iZone][iInst][MESH_0], config[iZone]);
+      solvers0[ADJRAD_SOL]->RegisterVariables(geometry0, config[iZone]);
     }
   }
 
   if (kind_recording == RECORDING::MESH_COORDS || kind_recording == RECORDING::SOLUTION_AND_MESH) {
     /*--- Register node coordinates as input ---*/
 
-    geometry[iZone][iInst][MESH_0]->RegisterCoordinates();
+    geometry0->RegisterCoordinates();
   }
 
   if (kind_recording == RECORDING::MESH_DEFORM) {
     /*--- Undeformed mesh coordinates ---*/
-    solver[iZone][iInst][MESH_0][ADJMESH_SOL]->RegisterSolution(geometry[iZone][iInst][MESH_0], config[iZone]);
+    solvers0[ADJMESH_SOL]->RegisterSolution(geometry0, config[iZone]);
 
     /*--- Boundary displacements ---*/
-    solver[iZone][iInst][MESH_0][ADJMESH_SOL]->RegisterVariables(geometry[iZone][iInst][MESH_0], config[iZone]);
+    solvers0[ADJMESH_SOL]->RegisterVariables(geometry0, config[iZone]);
   }
   }
   END_SU2_OMP_PARALLEL
@@ -527,6 +526,8 @@ void CDiscAdjFluidIteration::RegisterInput(CSolver***** solver, CGeometry**** ge
 void CDiscAdjFluidIteration::SetDependencies(CSolver***** solver, CGeometry**** geometry, CNumerics****** numerics,
                                              CConfig** config, unsigned short iZone, unsigned short iInst,
                                              RECORDING kind_recording) {
+  auto solvers0 = solver[iZone][iInst][MESH_0];
+  auto geometry0 = geometry[iZone][iInst][MESH_0];
 
   if ((kind_recording == RECORDING::MESH_COORDS) ||
       (kind_recording == RECORDING::CLEAR_INDICES) ||
@@ -538,71 +539,68 @@ void CDiscAdjFluidIteration::SetDependencies(CSolver***** solver, CGeometry****
     CGeometry::ComputeWallDistance(config, geometry);
   }
 
-  SU2_OMP_PARALLEL_(if(solver[iZone][iInst][MESH_0][ADJFLOW_SOL]->GetHasHybridParallel())) {
+  SU2_OMP_PARALLEL_(if(solvers0[ADJFLOW_SOL]->GetHasHybridParallel())) {
 
   /*--- Compute coupling between flow, turbulent and species equations ---*/
-  solver[iZone][iInst][MESH_0][FLOW_SOL]->Preprocessing(geometry[iZone][iInst][MESH_0], solver[iZone][iInst][MESH_0],
-                                                        config[iZone], MESH_0, NO_RK_ITER, RUNTIME_FLOW_SYS, true);
-  solver[iZone][iInst][MESH_0][FLOW_SOL]->InitiateComms(geometry[iZone][iInst][MESH_0], config[iZone], SOLUTION);
-  solver[iZone][iInst][MESH_0][FLOW_SOL]->CompleteComms(geometry[iZone][iInst][MESH_0], config[iZone], SOLUTION);
+  solvers0[FLOW_SOL]->Preprocessing(geometry0, solvers0, config[iZone], MESH_0, NO_RK_ITER, RUNTIME_FLOW_SYS, true);
+  solvers0[FLOW_SOL]->InitiateComms(geometry0, config[iZone], SOLUTION);
+  solvers0[FLOW_SOL]->CompleteComms(geometry0, config[iZone], SOLUTION);
 
   if (turbulent && !config[iZone]->GetFrozen_Visc_Disc()) {
-    solver[iZone][iInst][MESH_0][TURB_SOL]->Postprocessing(geometry[iZone][iInst][MESH_0], solver[iZone][iInst][MESH_0],
+    solvers0[TURB_SOL]->Postprocessing(geometry0, solvers0,
                                                            config[iZone], MESH_0);
-    solver[iZone][iInst][MESH_0][TURB_SOL]->InitiateComms(geometry[iZone][iInst][MESH_0], config[iZone], SOLUTION);
-    solver[iZone][iInst][MESH_0][TURB_SOL]->CompleteComms(geometry[iZone][iInst][MESH_0], config[iZone], SOLUTION);
+    solvers0[TURB_SOL]->InitiateComms(geometry0, config[iZone], SOLUTION);
+    solvers0[TURB_SOL]->CompleteComms(geometry0, config[iZone], SOLUTION);
   }
   if (config[iZone]->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
-    solver[iZone][iInst][MESH_0][SPECIES_SOL]->Preprocessing(geometry[iZone][iInst][MESH_0], solver[iZone][iInst][MESH_0],
-                                                             config[iZone], MESH_0, NO_RK_ITER, RUNTIME_FLOW_SYS, true);
-    solver[iZone][iInst][MESH_0][SPECIES_SOL]->InitiateComms(geometry[iZone][iInst][MESH_0], config[iZone], SOLUTION);
-    solver[iZone][iInst][MESH_0][SPECIES_SOL]->CompleteComms(geometry[iZone][iInst][MESH_0], config[iZone], SOLUTION);
+    solvers0[SPECIES_SOL]->Preprocessing(geometry0, solvers0, config[iZone], MESH_0, NO_RK_ITER, RUNTIME_FLOW_SYS, true);
+    solvers0[SPECIES_SOL]->InitiateComms(geometry0, config[iZone], SOLUTION);
+    solvers0[SPECIES_SOL]->CompleteComms(geometry0, config[iZone], SOLUTION);
   }
 
   }
   END_SU2_OMP_PARALLEL
 
   if (config[iZone]->GetWeakly_Coupled_Heat()) {
-    solver[iZone][iInst][MESH_0][HEAT_SOL]->Set_Heatflux_Areas(geometry[iZone][iInst][MESH_0], config[iZone]);
-    solver[iZone][iInst][MESH_0][HEAT_SOL]->Preprocessing(geometry[iZone][iInst][MESH_0], solver[iZone][iInst][MESH_0],
-                                                          config[iZone], MESH_0, NO_RK_ITER, RUNTIME_HEAT_SYS, true);
-    solver[iZone][iInst][MESH_0][HEAT_SOL]->Postprocessing(geometry[iZone][iInst][MESH_0], solver[iZone][iInst][MESH_0],
-                                                           config[iZone], MESH_0);
-    solver[iZone][iInst][MESH_0][HEAT_SOL]->InitiateComms(geometry[iZone][iInst][MESH_0], config[iZone], SOLUTION);
-    solver[iZone][iInst][MESH_0][HEAT_SOL]->CompleteComms(geometry[iZone][iInst][MESH_0], config[iZone], SOLUTION);
+    solvers0[HEAT_SOL]->Set_Heatflux_Areas(geometry0, config[iZone]);
+    solvers0[HEAT_SOL]->Preprocessing(geometry0, solvers0, config[iZone], MESH_0, NO_RK_ITER, RUNTIME_HEAT_SYS, true);
+    solvers0[HEAT_SOL]->Postprocessing(geometry0, solvers0, config[iZone], MESH_0);
+    solvers0[HEAT_SOL]->InitiateComms(geometry0, config[iZone], SOLUTION);
+    solvers0[HEAT_SOL]->CompleteComms(geometry0, config[iZone], SOLUTION);
   }
   if (config[iZone]->AddRadiation()) {
-    solver[iZone][iInst][MESH_0][RAD_SOL]->Postprocessing(geometry[iZone][iInst][MESH_0], solver[iZone][iInst][MESH_0],
-                                                          config[iZone], MESH_0);
-    solver[iZone][iInst][MESH_0][RAD_SOL]->InitiateComms(geometry[iZone][iInst][MESH_0], config[iZone], SOLUTION);
-    solver[iZone][iInst][MESH_0][RAD_SOL]->CompleteComms(geometry[iZone][iInst][MESH_0], config[iZone], SOLUTION);
+    solvers0[RAD_SOL]->Postprocessing(geometry0, solvers0, config[iZone], MESH_0);
+    solvers0[RAD_SOL]->InitiateComms(geometry0, config[iZone], SOLUTION);
+    solvers0[RAD_SOL]->CompleteComms(geometry0, config[iZone], SOLUTION);
   }
 }
 
 void CDiscAdjFluidIteration::RegisterOutput(CSolver***** solver, CGeometry**** geometry, CConfig** config,
                                             unsigned short iZone, unsigned short iInst) {
+  auto solvers0 = solver[iZone][iInst][MESH_0];
+  auto geometry0 = geometry[iZone][iInst][MESH_0];
 
-  SU2_OMP_PARALLEL_(if(solver[iZone][iInst][MESH_0][ADJFLOW_SOL]->GetHasHybridParallel())) {
+  SU2_OMP_PARALLEL_(if(solvers0[ADJFLOW_SOL]->GetHasHybridParallel())) {
 
   /*--- Register conservative variables as output of the iteration ---*/
 
   if (config[iZone]->GetFluidProblem()) {
-    solver[iZone][iInst][MESH_0][ADJFLOW_SOL]->RegisterOutput(geometry[iZone][iInst][MESH_0], config[iZone]);
+    solvers0[ADJFLOW_SOL]->RegisterOutput(geometry0, config[iZone]);
   }
   if (turbulent && !config[iZone]->GetFrozen_Visc_Disc()) {
-    solver[iZone][iInst][MESH_0][ADJTURB_SOL]->RegisterOutput(geometry[iZone][iInst][MESH_0], config[iZone]);
+    solvers0[ADJTURB_SOL]->RegisterOutput(geometry0, config[iZone]);
   }
   if (config[iZone]->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
-    solver[iZone][iInst][MESH_0][ADJSPECIES_SOL]->RegisterOutput(geometry[iZone][iInst][MESH_0], config[iZone]);
+    solvers0[ADJSPECIES_SOL]->RegisterOutput(geometry0, config[iZone]);
   }
   if (config[iZone]->GetWeakly_Coupled_Heat()) {
-    solver[iZone][iInst][MESH_0][ADJHEAT_SOL]->RegisterOutput(geometry[iZone][iInst][MESH_0], config[iZone]);
+    solvers0[ADJHEAT_SOL]->RegisterOutput(geometry0, config[iZone]);
   }
   if (config[iZone]->AddRadiation()) {
-    solver[iZone][iInst][MESH_0][ADJRAD_SOL]->RegisterOutput(geometry[iZone][iInst][MESH_0], config[iZone]);
+    solvers0[ADJRAD_SOL]->RegisterOutput(geometry0, config[iZone]);
   }
   if (config[iZone]->GetFluidProblem() && !config[iZone]->GetMultizone_Problem()) {
-    solver[iZone][iInst][MESH_0][FLOW_SOL]->RegisterVertexTractions(geometry[iZone][iInst][MESH_0], config[iZone]);
+    solvers0[FLOW_SOL]->RegisterVertexTractions(geometry0, config[iZone]);
   }
 
   }
diff --git a/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
index a12cb43bdc0..7d8b841fd10 100644
--- a/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
@@ -45,78 +45,66 @@ void CDiscAdjHeatIteration::Preprocess(COutput* output, CIntegration**** integra
   if (config[val_iZone]->GetTime_Marching() != TIME_MARCHING::STEADY) {
     const int Direct_Iter = static_cast<int>(config[val_iZone]->GetUnst_AdjointIter()) - static_cast<int>(TimeIter) - 2 + dual_time;
 
-    /*--- For dual-time stepping we want to load the already converged solution at timestep n ---*/
+    /*--- For dual-time stepping we want to load the already converged solution at previous timesteps.
+     * In general we only load one file and shift the previously loaded solutions, on the first we
+     * load one or two more (depending on dual time order). ---*/
 
-    if (TimeIter == 0) {
-      if (dual_time_2nd) {
-        /*--- Load solution at timestep n-2 ---*/
-
-        LoadUnsteady_Solution(geometry, solver, config, val_iZone, val_iInst, Direct_Iter - 2);
-
-        /*--- Push solution back to correct array ---*/
+    if (dual_time_2nd) {
+      LoadUnsteady_Solution(geometry, solver, config, val_iZone, val_iInst, Direct_Iter - 2);
+    } else if (dual_time_1st) {
+      LoadUnsteady_Solution(geometry, solver, config, val_iZone, val_iInst, Direct_Iter - 1);
+    }
 
+    if (TimeIter == 0) {
+      /*--- Push solution back one or two levels, ---*/
+      if (dual_time) {
         for (auto iMesh = 0u; iMesh <= config[val_iZone]->GetnMGLevels(); iMesh++) {
           solvers[iMesh][HEAT_SOL]->GetNodes()->Set_Solution_time_n();
-          solvers[iMesh][HEAT_SOL]->GetNodes()->Set_Solution_time_n1();
+          if (dual_time_2nd) solvers[iMesh][HEAT_SOL]->GetNodes()->Set_Solution_time_n1();
         }
       }
-      if (dual_time) {
-        /*--- Load solution at timestep n-1 ---*/
 
+      /*--- If required load another time step. ---*/
+      if (dual_time_2nd) {
         LoadUnsteady_Solution(geometry, solver, config, val_iZone, val_iInst, Direct_Iter - 1);
 
-        /*--- Push solution back to correct array ---*/
-
         for (auto iMesh = 0u; iMesh <= config[val_iZone]->GetnMGLevels(); iMesh++) {
           solvers[iMesh][HEAT_SOL]->GetNodes()->Set_Solution_time_n();
         }
       }
 
-      /*--- Load solution timestep n ---*/
-
+      /*--- Load current solution. ---*/
       LoadUnsteady_Solution(geometry, solver, config, val_iZone, val_iInst, Direct_Iter);
     }
     if ((TimeIter > 0) && dual_time) {
-      /*--- Load solution timestep n - 2 ---*/
-
-      LoadUnsteady_Solution(geometry, solver, config, val_iZone, val_iInst, Direct_Iter - 2);
-
       /*--- Temporarily store the loaded solution in the Solution_Old array ---*/
-
       for (auto iMesh = 0u; iMesh <= config[val_iZone]->GetnMGLevels(); iMesh++)
         solvers[iMesh][HEAT_SOL]->Set_OldSolution();
 
-      /*--- Set Solution at timestep n to solution at n-1 ---*/
-
+      /*--- Move timestep n to current solution. ---*/
       for (auto iMesh = 0u; iMesh <= config[val_iZone]->GetnMGLevels(); iMesh++) {
         for (auto iPoint = 0ul; iPoint < geometry[val_iZone][val_iInst][iMesh]->GetnPoint(); iPoint++) {
           solvers[iMesh][HEAT_SOL]->GetNodes()->SetSolution(
               iPoint, solvers[iMesh][HEAT_SOL]->GetNodes()->GetSolution_time_n(iPoint));
         }
       }
-      if (dual_time_1st) {
-        /*--- Set Solution at timestep n-1 to the previously loaded solution ---*/
-        for (auto iMesh = 0u; iMesh <= config[val_iZone]->GetnMGLevels(); iMesh++) {
-          for (auto iPoint = 0ul; iPoint < geometry[val_iZone][val_iInst][iMesh]->GetnPoint(); iPoint++) {
-            solvers[iMesh][HEAT_SOL]->GetNodes()->Set_Solution_time_n(
-                iPoint, solvers[iMesh][HEAT_SOL]->GetNodes()->GetSolution_time_n1(iPoint));
-          }
-        }
-      }
+
+      /*--- If required also move timestep n-1 to timestep n. ---*/
       if (dual_time_2nd) {
-        /*--- Set Solution at timestep n-1 to solution at n-2 ---*/
         for (auto iMesh = 0u; iMesh <= config[val_iZone]->GetnMGLevels(); iMesh++) {
           for (auto iPoint = 0ul; iPoint < geometry[val_iZone][val_iInst][iMesh]->GetnPoint(); iPoint++) {
             solvers[iMesh][HEAT_SOL]->GetNodes()->Set_Solution_time_n(
                 iPoint, solvers[iMesh][HEAT_SOL]->GetNodes()->GetSolution_time_n1(iPoint));
           }
         }
-        /*--- Set Solution at timestep n-2 to the previously loaded solution ---*/
-        for (auto iMesh = 0u; iMesh <= config[val_iZone]->GetnMGLevels(); iMesh++) {
-          for (auto iPoint = 0ul; iPoint < geometry[val_iZone][val_iInst][iMesh]->GetnPoint(); iPoint++) {
-            solvers[iMesh][HEAT_SOL]->GetNodes()->Set_Solution_time_n1(
-                iPoint, solvers[iMesh][HEAT_SOL]->GetNodes()->GetSolution_Old(iPoint));
-          }
+      }
+
+      /*--- Finally, place the loaded solution in the correct place (n or n-1 depending on order). ---*/
+      for (auto iMesh = 0u; iMesh <= config[val_iZone]->GetnMGLevels(); iMesh++) {
+        for (auto iPoint = 0ul; iPoint < geometry[val_iZone][val_iInst][iMesh]->GetnPoint(); iPoint++) {
+          const auto sol = solvers[iMesh][HEAT_SOL]->GetNodes()->GetSolution_Old(iPoint);
+          if (dual_time_2nd) solvers[iMesh][HEAT_SOL]->GetNodes()->Set_Solution_time_n1(iPoint, sol);
+          else solvers[iMesh][HEAT_SOL]->GetNodes()->Set_Solution_time_n(iPoint, sol);
         }
       }
     }
@@ -140,13 +128,14 @@ void CDiscAdjHeatIteration::Preprocess(COutput* output, CIntegration**** integra
 void CDiscAdjHeatIteration::LoadUnsteady_Solution(CGeometry**** geometry, CSolver***** solver, CConfig** config,
                                                   unsigned short val_iZone, unsigned short val_iInst,
                                                   int val_DirectIter) {
+  auto solvers = solver[val_iZone][val_iInst];
+  auto geometries = geometry[val_iZone][val_iInst];
 
   if (val_DirectIter >= 0) {
     if (rank == MASTER_NODE)
       cout << " Loading heat solution from direct iteration " << val_DirectIter << " for zone " << val_iZone << "." << endl;
 
-    solver[val_iZone][val_iInst][MESH_0][HEAT_SOL]->LoadRestart(
-        geometry[val_iZone][val_iInst], solver[val_iZone][val_iInst], config[val_iZone], val_DirectIter, false);
+    solvers[MESH_0][HEAT_SOL]->LoadRestart(geometries, solvers, config[val_iZone], val_DirectIter, false);
   }
   else {
     /*--- If there is no solution file we set the freestream condition ---*/
@@ -154,9 +143,8 @@ void CDiscAdjHeatIteration::LoadUnsteady_Solution(CGeometry**** geometry, CSolve
       cout << " Setting freestream conditions at direct iteration " << val_DirectIter << " for zone " << val_iZone << "." << endl;
 
     for (auto iMesh = 0u; iMesh <= config[val_iZone]->GetnMGLevels(); iMesh++) {
-      solver[val_iZone][val_iInst][iMesh][HEAT_SOL]->SetFreeStream_Solution(config[val_iZone]);
-      solver[val_iZone][val_iInst][iMesh][HEAT_SOL]->Postprocessing(
-          geometry[val_iZone][val_iInst][iMesh], solver[val_iZone][val_iInst][iMesh], config[val_iZone], iMesh);
+      solvers[iMesh][HEAT_SOL]->SetFreeStream_Solution(config[val_iZone]);
+      solvers[iMesh][HEAT_SOL]->Postprocessing(geometries[iMesh], solvers[iMesh], config[val_iZone], iMesh);
     }
   }
 }
@@ -177,26 +165,28 @@ void CDiscAdjHeatIteration::InitializeAdjoint(CSolver***** solver, CGeometry****
 
 void CDiscAdjHeatIteration::RegisterInput(CSolver***** solver, CGeometry**** geometry, CConfig** config,
                                           unsigned short iZone, unsigned short iInst, RECORDING kind_recording) {
+  auto solvers0 = solver[iZone][iInst][MESH_0];
+  auto geometry0 = geometry[iZone][iInst][MESH_0];
 
   if (kind_recording == RECORDING::SOLUTION_VARIABLES || kind_recording == RECORDING::SOLUTION_AND_MESH) {
     /*--- Register flow and turbulent variables as input ---*/
 
-    solver[iZone][iInst][MESH_0][ADJHEAT_SOL]->RegisterSolution(geometry[iZone][iInst][MESH_0], config[iZone]);
+    solvers0[ADJHEAT_SOL]->RegisterSolution(geometry0, config[iZone]);
 
-    solver[iZone][iInst][MESH_0][ADJHEAT_SOL]->RegisterVariables(geometry[iZone][iInst][MESH_0], config[iZone]);
+    solvers0[ADJHEAT_SOL]->RegisterVariables(geometry0, config[iZone]);
   }
   else if (kind_recording == RECORDING::MESH_COORDS) {
     /*--- Register node coordinates as input ---*/
 
-    geometry[iZone][iInst][MESH_0]->RegisterCoordinates();
+    geometry0->RegisterCoordinates();
   }
   else if (kind_recording == RECORDING::MESH_DEFORM) {
     /*--- Register the variables of the mesh deformation ---*/
     /*--- Undeformed mesh coordinates ---*/
-    solver[iZone][iInst][MESH_0][ADJMESH_SOL]->RegisterSolution(geometry[iZone][iInst][MESH_0], config[iZone]);
+    solvers0[ADJMESH_SOL]->RegisterSolution(geometry0, config[iZone]);
 
     /*--- Boundary displacements ---*/
-    solver[iZone][iInst][MESH_0][ADJMESH_SOL]->RegisterVariables(geometry[iZone][iInst][MESH_0], config[iZone]);
+    solvers0[ADJMESH_SOL]->RegisterVariables(geometry0, config[iZone]);
   }
 }
 
diff --git a/SU2_CFD/src/output/CAdjElasticityOutput.cpp b/SU2_CFD/src/output/CAdjElasticityOutput.cpp
index e30f2895f65..d27b96c990c 100644
--- a/SU2_CFD/src/output/CAdjElasticityOutput.cpp
+++ b/SU2_CFD/src/output/CAdjElasticityOutput.cpp
@@ -244,19 +244,19 @@ void CAdjElasticityOutput::SetVolumeOutputFields(CConfig *config){
 
   /*--- Sensitivities with respect to initial conditions. ---*/
 
-  AddVolumeOutput("SENS_DISP-X", "SensInitialDisp_x", "SENSITIVITY_T0", "sensitivity to the initial x displacement");
-  AddVolumeOutput("SENS_DISP-Y", "SensInitialDisp_y", "SENSITIVITY_T0", "sensitivity to the initial y displacement");
+  AddVolumeOutput("SENS_DISP-X", "SensitivityDispN_x", "SENSITIVITY_N", "sensitivity to the previous x displacement");
+  AddVolumeOutput("SENS_DISP-Y", "SensitivityDispN_y", "SENSITIVITY_N", "sensitivity to the previous y displacement");
   if (nDim == 3)
-    AddVolumeOutput("SENS_DISP-Z", "SensInitialDisp_z", "SENSITIVITY_T0", "sensitivity to the initial z displacement");
+    AddVolumeOutput("SENS_DISP-Z", "SensitivityDispN_z", "SENSITIVITY_N", "sensitivity to the previous z displacement");
 
-  AddVolumeOutput("SENS_VEL-X", "SensInitialVel_x", "SENSITIVITY_T0", "sensitivity to the initial x velocity");
-  AddVolumeOutput("SENS_VEL-Y", "SensInitialVel_y", "SENSITIVITY_T0", "sensitivity to the initial y velocity");
+  AddVolumeOutput("SENS_VEL-X", "SensitivityVelN_x", "SENSITIVITY_N", "sensitivity to the previous x velocity");
+  AddVolumeOutput("SENS_VEL-Y", "SensitivityVelN_y", "SENSITIVITY_N", "sensitivity to the previous y velocity");
   if (nDim == 3)
-    AddVolumeOutput("SENS_VEL-Z", "SensInitialVel_z", "SENSITIVITY_T0", "sensitivity to the initial z velocity");
+    AddVolumeOutput("SENS_VEL-Z", "SensitivityVelN_z", "SENSITIVITY_N", "sensitivity to the previous z velocity");
 
-  AddVolumeOutput("SENS_ACCEL-X", "SensInitialAccel_x", "SENSITIVITY_T0", "sensitivity to the initial x acceleration");
-  AddVolumeOutput("SENS_ACCEL-Y", "SensInitialAccel_y", "SENSITIVITY_T0", "sensitivity to the initial y acceleration");
+  AddVolumeOutput("SENS_ACCEL-X", "SensitivityAccelN_x", "SENSITIVITY_N", "sensitivity to the previous x acceleration");
+  AddVolumeOutput("SENS_ACCEL-Y", "SensitivityAccelN_y", "SENSITIVITY_N", "sensitivity to the previous y acceleration");
   if (nDim == 3)
-    AddVolumeOutput("SENS_ACCEL-Z", "SensInitialAccel_z", "SENSITIVITY_T0", "sensitivity to the initial z acceleration");
+    AddVolumeOutput("SENS_ACCEL-Z", "SensitivityAccelN_z", "SENSITIVITY_N", "sensitivity to the previous z acceleration");
 
 }
diff --git a/SU2_CFD/src/output/CAdjHeatOutput.cpp b/SU2_CFD/src/output/CAdjHeatOutput.cpp
index 65d5679b8ca..889275f436b 100644
--- a/SU2_CFD/src/output/CAdjHeatOutput.cpp
+++ b/SU2_CFD/src/output/CAdjHeatOutput.cpp
@@ -176,6 +176,14 @@ void CAdjHeatOutput::SetVolumeOutputFields(CConfig *config){
   AddVolumeOutput("SENSITIVITY", "Surface_Sensitivity", "SENSITIVITY", "sensitivity in normal direction");
   /// END_GROUP
 
+  if (!config->GetTime_Domain()) return;
+
+  /*--- Sensitivities with respect to initial conditions. ---*/
+
+  AddVolumeOutput("SENS_TEMP_N", "SensitivityTempN", "SENSITIVITY_N", "sensitivity to the previous temperature");
+  if (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND) {
+    AddVolumeOutput("SENS_TEMP_N1", "SensitivityTempN1", "SENSITIVITY_N", "sensitivity to the previous-1 temperature");
+  }
 }
 
 void CAdjHeatOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolver **solver, unsigned long iPoint){
@@ -199,6 +207,13 @@ void CAdjHeatOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolve
   if (nDim == 3)
     SetVolumeOutputValue("SENSITIVITY-Z", iPoint, Node_AdjHeat->GetSensitivity(iPoint, 2));
 
+  if (!config->GetTime_Domain()) return;
+
+  SetVolumeOutputValue("SENS_TEMP_N", iPoint, Node_AdjHeat->GetSolution_time_n(iPoint, 0));
+  if (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND) {
+    SetVolumeOutputValue("SENS_TEMP_N1", iPoint, Node_AdjHeat->GetSolution_time_n1(iPoint, 0));
+  }
+
 }
 
 void CAdjHeatOutput::LoadSurfaceData(CConfig *config, CGeometry *geometry, CSolver **solver, unsigned long iPoint, unsigned short iMarker, unsigned long iVertex){
diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index 61c79202fb8..c440361c2f8 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -421,6 +421,19 @@ def main():
     test_list.append(pywrapper_Unst_FEA_AD)
     pass_list.append(pywrapper_Unst_FEA_AD.run_test())
 
+    # Heat solver unsteady AD
+    pywrapper_Unst_Heat_AD = TestCase('pywrapper_Unst_Heat_AD')
+    pywrapper_Unst_Heat_AD.cfg_dir = "py_wrapper/custom_heat_flux"
+    pywrapper_Unst_Heat_AD.cfg_file = "run_ad.cfg"
+    pywrapper_Unst_Heat_AD.test_iter = 100
+    pywrapper_Unst_Heat_AD.test_vals = [0.776365, 0.776430, 1.000003]
+    pywrapper_Unst_Heat_AD.command = TestCase.Command("mpirun -n 2", "python", "run_ad.py")
+    pywrapper_Unst_Heat_AD.timeout = 1600
+    pywrapper_Unst_Heat_AD.tol = 0.00001
+    pywrapper_Unst_Heat_AD.new_output = False
+    test_list.append(pywrapper_Unst_Heat_AD)
+    pass_list.append(pywrapper_Unst_Heat_AD.run_test())
+
     # Flow AD Mesh Displacement Sensitivity
     pywrapper_CFD_AD_MeshDisp               = TestCase('pywrapper_CFD_AD_MeshDisp')
     pywrapper_CFD_AD_MeshDisp.cfg_dir       = "py_wrapper/disc_adj_flow/mesh_disp_sens"
diff --git a/TestCases/py_wrapper/custom_heat_flux/run_ad.py b/TestCases/py_wrapper/custom_heat_flux/run_ad.py
new file mode 100644
index 00000000000..2b63af21d2d
--- /dev/null
+++ b/TestCases/py_wrapper/custom_heat_flux/run_ad.py
@@ -0,0 +1,246 @@
+#!/usr/bin/env python
+
+## \file run.py
+#  \brief Unsteady adjoint heat transfer case with custom heat flux.
+#  \version 7.5.1 "Blackbird"
+#
+# SU2 Project Website: https://su2code.github.io
+#
+# The SU2 Project is maintained by the SU2 Foundation
+# (http://su2foundation.org)
+#
+# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
+#
+# SU2 is free software; you can redistribute it and/or
+# modify it under the terms of the GNU Lesser General Public
+# License as published by the Free Software Foundation; either
+# version 2.1 of the License, or (at your option) any later version.
+#
+# SU2 is distributed in the hope that it will be useful,
+# but WITHOUT ANY WARRANTY; without even the implied warranty of
+# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+# Lesser General Public License for more details.
+#
+# You should have received a copy of the GNU Lesser General Public
+# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+
+import pysu2ad
+from mpi4py import MPI
+
+common_settings = """
+SOLVER= HEAT_EQUATION
+INC_NONDIM= DIMENSIONAL
+
+TIME_DOMAIN= YES
+TIME_STEP= 0.05
+TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
+
+FREESTREAM_TEMPERATURE= 345
+MATERIAL_DENSITY= 2700
+SPECIFIC_HEAT_CP = 870
+% Very high value to make the case more interesting.
+THERMAL_CONDUCTIVITY_CONSTANT= 1000
+
+MARKER_HEATFLUX= ( x_minus, 0, x_plus, 0, y_minus, 0, y_plus, 0 )
+MARKER_PYTHON_CUSTOM= ( x_minus, x_plus, y_minus, y_plus )
+MARKER_MONITORING= ( x_minus, x_plus, y_minus, y_plus )
+
+NUM_METHOD_GRAD= GREEN_GAUSS
+CFL_NUMBER= 1e8
+
+LINEAR_SOLVER= CONJUGATE_GRADIENT
+DISCADJ_LIN_SOLVER= CONJUGATE_GRADIENT
+LINEAR_SOLVER_PREC= ILU
+DISCADJ_LIN_PREC= ILU
+LINEAR_SOLVER_ERROR= 1E-5
+LINEAR_SOLVER_ITER= 100
+
+MESH_FORMAT= RECTANGLE
+MESH_BOX_SIZE= ( 33, 33, 0 )
+MESH_BOX_LENGTH= ( __SIZE__, __SIZE__, 0 )
+
+OUTPUT_FILES= RESTART, PARAVIEW
+OUTPUT_WRT_FREQ= 1
+OBJECTIVE_FUNCTION= AVG_TEMPERATURE
+
+INNER_ITER= 20
+CONV_RESIDUAL_MINVAL= -4
+CONV_STARTITER= 2
+MAX_TIME= 2.0
+TIME_ITER= 41
+"""
+
+primal_settings = """
+MATH_PROBLEM= DIRECT
+SCREEN_OUTPUT= TIME_ITER, CUR_TIME, INNER_ITER, RMS_RES, LINSOL, AVG_TEMPERATURE, TAVG_AVG_TEMPERATURE
+HISTORY_OUTPUT= ITER, RMS_RES, HEAT, TAVG_HEAT
+"""
+
+adjoint_settings = """
+MATH_PROBLEM= DISCRETE_ADJOINT
+SCREEN_OUTPUT= TIME_ITER, CUR_TIME, INNER_ITER, RMS_RES, LINSOL
+UNST_ADJOINT_ITER= 41
+% Only interested in the final value of the objective.
+ITER_AVERAGE_OBJ= 1
+SOLUTION_FILENAME= restart.dat
+VOLUME_OUTPUT= SOLUTION, SENSITIVITY, SENSITIVITY_N
+"""
+
+
+def ApplyHeatFlux(time, driver, marker_ids):
+  """Applies a heat flux on all boundaries for a period of time and then removes it."""
+  for marker_id in marker_ids:
+    if marker_id < 0:
+      continue
+    hf = (-1, 0)[time > 0.2]
+    for i_vertex in range(driver.GetNumberMarkerNodes(marker_id)):
+      driver.SetMarkerCustomNormalHeatFlux(marker_id, i_vertex, hf)
+
+
+def RunPrimal(size):
+  """
+  Run the heat solver with a custom heat (function of time) flux on all boundaries.
+  Returns the final average boundary temperature.
+  """
+  comm = MPI.COMM_WORLD
+
+  with open('config_unsteady.cfg', 'w') as f:
+    f.write(common_settings.replace('__SIZE__', str(size)) + primal_settings)
+
+  # Initialize the primal driver of SU2, this includes solver preprocessing.
+  try:
+    driver = pysu2ad.CSinglezoneDriver('config_unsteady.cfg', 1, comm)
+  except TypeError as exception:
+    print('A TypeError occured in pysu2ad.CSinglezoneDriver : ', exception)
+    raise
+
+  # Get the ID of the markers where the heat flux is applied.
+  all_marker_ids = driver.GetMarkerIndices()
+  marker_names = ['x_minus', 'x_plus', 'y_minus', 'y_plus']
+  marker_ids = []
+  for name in marker_names:
+    marker_ids.append(all_marker_ids[name] if name in all_marker_ids else -1)
+
+  # Run the time loop in python to vary the heat flux.
+  dt = driver.GetUnsteadyTimeStep()
+
+  for time_iter in range(driver.GetNumberTimeIter()):
+    # Custom heat flux.
+    ApplyHeatFlux(time_iter * dt, driver, marker_ids)
+
+    driver.Preprocess(time_iter)
+
+    # Run one time iteration.
+    driver.Run()
+    driver.Postprocess()
+    driver.Update()
+
+    # Monitor the solver and output solution to file if required.
+    driver.Monitor(time_iter)
+    driver.Output(time_iter)
+
+  # Get the final average temperature.
+  avg_temperature = driver.GetOutputValue('AVG_TEMPERATURE')
+
+  # Finalize the solver and exit cleanly.
+  driver.Finalize()
+
+  return avg_temperature
+
+
+def RunAdjoint(size):
+  """
+  Runs the adjoint heat solver and returns the sensitivity of the objective function to
+  size of the domain and to the initial temperature.
+  """
+  comm = MPI.COMM_WORLD
+
+  with open('config_unsteady_ad.cfg', 'w') as f:
+    f.write(common_settings.replace('__SIZE__', str(size)) + adjoint_settings)
+
+  # Initialize the adjoint driver of SU2, this includes solver preprocessing.
+  try:
+    driver = pysu2ad.CDiscAdjSinglezoneDriver('config_unsteady_ad.cfg', 1, comm)
+  except TypeError as exception:
+    print('A TypeError occured in pysu2ad.CDiscAdjSinglezoneDriver : ', exception)
+    raise
+
+  # Get the ID of the markers where the heat flux is applied.
+  all_marker_ids = driver.GetMarkerIndices()
+  marker_names = ['x_minus', 'x_plus', 'y_minus', 'y_plus']
+  marker_ids = []
+  for name in marker_names:
+    marker_ids.append(all_marker_ids[name] if name in all_marker_ids else -1)
+
+  # Run the time loop in python to vary the heat flux.
+  dt = driver.GetUnsteadyTimeStep()
+
+  # Run the time loop in python to extract sensitivities at each step.
+  for time_iter in range(driver.GetNumberTimeIter()):
+    # Note that time runs in reverse for the adjoint solver.
+    ApplyHeatFlux((driver.GetNumberTimeIter() - time_iter - 1) * dt, driver, marker_ids)
+
+    # Preprocess adjoint iteration (AD recording).
+    driver.Preprocess(time_iter)
+
+    # Run one time iteration.
+    driver.Run()
+    driver.Postprocess()
+    driver.Update()
+
+    # Monitor the solver and output solution to file if required.
+    driver.Monitor(time_iter)
+    driver.Output(time_iter)
+
+  size_sens = 0.0
+  temp_sens = 0.0
+  sensitivity = driver.Sensitivity(driver.GetSolverIndices()['ADJ.HEAT'])
+  sens_n = driver.SolutionTimeN(driver.GetSolverIndices()['ADJ.HEAT'])
+  sens_n1 = driver.SolutionTimeN1(driver.GetSolverIndices()['ADJ.HEAT'])
+  coords = driver.Coordinates()
+
+  for i_node in range(driver.GetNumberNodes() - driver.GetNumberHaloNodes()):
+    x, y = coords.Get(i_node)
+    dx_ds = x / size
+    dy_ds = y / size
+    size_sens += dx_ds * sensitivity(i_node, 0) + dy_ds * sensitivity(i_node, 1)
+    # For 2nd order BDF the initial conditions apply to time n and n-1,
+    # hence we combine the two sensitivities. n-1 is multiplied by 2 because
+    # the initial conditions are used as the n-1 solution twice (in the 1st and
+    # second iterations). However, note that this is an approximation, the
+    # correct value would be sens_n_t0 + sens_n1_t0 + sens_n1_t1 (we approximate
+    # sens_n1 at t1 as sens_n1 at t0).
+    temp_sens += sens_n(i_node, 0) + 2 * sens_n1(i_node, 0)
+
+  # Finalize the solver and exit cleanly.
+  driver.Finalize()
+
+  return comm.allreduce(size_sens), comm.allreduce(temp_sens)
+
+
+def main():
+  comm = MPI.COMM_WORLD
+  rank = comm.Get_rank()
+
+  obj_pert_size = RunPrimal(0.100005)
+  obj = RunPrimal(0.1)
+  sens_size_fd = (obj_pert_size - obj) / 0.000005
+
+  sens_size, sens_temp = RunAdjoint(0.1)
+
+  if rank == 0:
+    print("     Finite Differences\tDiscrete Adjoint")
+    print(f"Size {sens_size_fd}\t{sens_size}")
+
+  assert abs(sens_size / sens_size_fd - 1) < 1e-4, "Error in geometric derivatives."
+  # We expect the final average temperature to be directly proportional to the initial
+  # temperature since the applied heat flux is not a function of temperature.
+  assert abs(sens_temp - 1) < 1e-5, "Error in initial condition derivatives."
+
+  # Print results for the regression script to check.
+  if rank == 0:
+    print("\n")
+    print(100, 100, sens_size_fd / 100, sens_size / 100, sens_temp)
+
+if __name__ == '__main__':
+  main()
diff --git a/TestCases/py_wrapper/custom_load_fea/run_ad.py b/TestCases/py_wrapper/custom_load_fea/run_ad.py
index dd64982b51b..8a44b1e033f 100644
--- a/TestCases/py_wrapper/custom_load_fea/run_ad.py
+++ b/TestCases/py_wrapper/custom_load_fea/run_ad.py
@@ -84,7 +84,7 @@
 UNST_ADJOINT_ITER= 21
 ITER_AVERAGE_OBJ= 0
 SOLUTION_FILENAME= restart.dat
-VOLUME_OUTPUT= SENSITIVITY_T0
+VOLUME_OUTPUT= SOLUTION, SENSITIVITY, SENSITIVITY_N
 """
 
 

From 967f2f6b6741f24e1fe8f63b1a2f697a33cda507 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 28 Apr 2023 10:00:42 +0200
Subject: [PATCH 411/656] Updated regression.yml

---
 .github/workflows/regression.yml | 2 +-
 meson_scripts/init.py            | 2 +-
 subprojects/MLPCpp               | 2 +-
 3 files changed, 3 insertions(+), 3 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index c1a9068a6b5..0bb7110fd97 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t feature_multilayer_perceptron -c develop -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 809413dd382..0534c2a8d44 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -71,7 +71,7 @@ def init_submodules(
     github_repo_coolprop = "https://github.com/CoolProp/CoolProp"
     sha_version_mel = "2484cd3258ef800a10e361016cb341834ee7930b"
     github_repo_mel = "https://github.com/pcarruscag/MEL"
-    sha_version_mlpcpp = "b723a9c06694c52f9e392116436c41bbe8e17244"
+    sha_version_mlpcpp = "e82cd4354cd30d94e8664f2645834fed0bfefe82"
     github_repo_mlpcpp = "https://github.com/EvertBunschoten/MLPCpp"
 
     medi_name = "MeDiPack"
diff --git a/subprojects/MLPCpp b/subprojects/MLPCpp
index b723a9c0669..e82cd4354cd 160000
--- a/subprojects/MLPCpp
+++ b/subprojects/MLPCpp
@@ -1 +1 @@
-Subproject commit b723a9c06694c52f9e392116436c41bbe8e17244
+Subproject commit e82cd4354cd30d94e8664f2645834fed0bfefe82

From ce9b4abaf444d982c44143cc16ec68279e607a95 Mon Sep 17 00:00:00 2001
From: PENGYAN777 <peng.yan@mail.polimi.it>
Date: Fri, 28 Apr 2023 10:41:17 +0200
Subject: [PATCH 412/656] nothing

---
 SU2_CFD/include/fluid/CCoolProp.hpp |  87 ++++++++++------------
 SU2_CFD/src/fluid/CCoolProp.cpp     | 110 +++++++++++++++-------------
 2 files changed, 99 insertions(+), 98 deletions(-)

diff --git a/SU2_CFD/include/fluid/CCoolProp.hpp b/SU2_CFD/include/fluid/CCoolProp.hpp
index 9d241a4b000..67f2515d9df 100644
--- a/SU2_CFD/include/fluid/CCoolProp.hpp
+++ b/SU2_CFD/include/fluid/CCoolProp.hpp
@@ -30,46 +30,36 @@
 #if defined(HAVE_COOLPROP) && !defined(CODI_FORWARD_TYPE) && !defined(CODI_REVERSE_TYPE)
 #define USE_COOLPROP
 namespace CoolProp {
-class AbstractState;
+  class AbstractState;
 }
 #endif
 #include <memory>
 
+
 /*!
  * \class CCoolProp
  * \brief Child class for defining fluid model from CoolProp library.
  * \author: P.Yan
  */
 class CCoolProp final : public CFluidModel {
- private:
-  su2double Gamma{1.4};                /*!< \brief Ratio of Specific Heats. */
-  su2double Gas_Constant{297};         /*!< \brief specific Gas Constant. */
-  su2double Pressure_Critical{0.0};    /*!< \brief critical pressure */
-  su2double Temperature_Critical{0.0}; /*!< \brief critical temperature */
-  su2double acentric_factor{0.0};      /*!< \brief acentric factor */
-  const su2double dp{0.01};            /*!< threshold for pressure */
+private:
+    su2double Gamma{1.4};           /*!< \brief Ratio of Specific Heats. */
+    su2double Gas_Constant{297};    /*!< \brief specific Gas Constant. */
+    su2double Pressure_Critical{0.0};   /*!< \brief critical pressure */
+    su2double Temperature_Critical{0.0};    /*!< \brief critical temperature */
+    su2double acentric_factor{0.0};      /*!< \brief acentric factor */
 #ifdef USE_COOLPROP
-  std::unique_ptr<CoolProp::AbstractState> fluid_entity; /*!< \brief fluid entity */
+    std::unique_ptr<CoolProp::AbstractState> fluid_entity;   /*!< \brief fluid entity */
 #endif
-  /*!
-   * \brief Avoid critical pressure
-   * \param[in,out] Pressure: Modified so that it is not too close to critical pressure to avoid issues in CoolProp.
-   */
-  void CheckPressure(su2double& Pressure) const {
-    if (Pressure > Pressure_Critical)
-      Pressure = fmax(Pressure, (1 + dp) * Pressure_Critical);
-    else
-      Pressure = fmin(Pressure, (1 - dp) * Pressure_Critical);
-  }
-
- public:
-  /*!
-   * \brief Constructor of the class.
-   */
-  CCoolProp(string fluidname);
+
+public:
+    /*!
+     * \brief Constructor of the class.
+     */
+    CCoolProp(string fluidname);
 
 #ifdef USE_COOLPROP
-  /*!
+    /*!
    * \brief Destructor of the class.
    * \note Needs to be defined in the .cpp to allow using only a forward declaration of CoolProp::AbstractState.
    */
@@ -132,27 +122,28 @@ class CCoolProp final : public CFluidModel {
   void ComputeDerivativeNRBC_Prho(su2double P, su2double rho) override;
 #endif
 
-  /*!
-   * \brief Get the value of the critical pressure.
-   * \return Critical pressure.
-   */
-  su2double GetPressure_Critical(void) const { return Pressure_Critical; }
+    /*!
+     * \brief Get the value of the critical pressure.
+     * \return Critical pressure.
+     */
+    su2double GetPressure_Critical(void) const { return Pressure_Critical; }
+
+    /*!
+     * \brief Get the value of the critical temperature.
+     * \return Critical temperature.
+     */
+    su2double GetTemperature_Critical(void) const { return Temperature_Critical; }
+
+    /*!
+     * \brief Get the value of specific gas constant.
+     * \return Value of the constant: Gamma
+     */
+    su2double GetGas_Constant(void) const { return Gas_Constant; }
+
+    /*!
+     * \brief Get the value of specific gas constant.
+     * \return Value of the constant: Gamma
+     */
+    su2double GetGamma(void) const { return Gamma; }
 
-  /*!
-   * \brief Get the value of the critical temperature.
-   * \return Critical temperature.
-   */
-  su2double GetTemperature_Critical(void) const { return Temperature_Critical; }
-
-  /*!
-   * \brief Get the value of specific gas constant.
-   * \return Value of the constant: Gamma
-   */
-  su2double GetGas_Constant(void) const { return Gas_Constant; }
-
-  /*!
-   * \brief Get the value of specific gas constant.
-   * \return Value of the constant: Gamma
-   */
-  su2double GetGamma(void) const { return Gamma; }
 };
diff --git a/SU2_CFD/src/fluid/CCoolProp.cpp b/SU2_CFD/src/fluid/CCoolProp.cpp
index 4a3b443252b..c82745f6bc1 100644
--- a/SU2_CFD/src/fluid/CCoolProp.cpp
+++ b/SU2_CFD/src/fluid/CCoolProp.cpp
@@ -1,39 +1,39 @@
 /*!
- * \file CCoolProp.cpp
- * \brief Source of the fluid model from CoolProp.
- * \author P. Yan, G. Gori, A. Guardone
- * \version 7.5.1 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
+* \file CCoolProp.cpp
+* \brief Source of the fluid model from CoolProp.
+* \author P. Yan, G. Gori, A. Guardone
+* \version 7.4.0 "Blackbird"
+*
+* SU2 Project Website: https://su2code.github.io
+*
+* The SU2 Project is maintained by the SU2 Foundation
+* (http://su2foundation.org)
+*
+* Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+*
+* SU2 is free software; you can redistribute it and/or
+* modify it under the terms of the GNU Lesser General Public
+* License as published by the Free Software Foundation; either
+* version 2.1 of the License, or (at your option) any later version.
+*
+* SU2 is distributed in the hope that it will be useful,
+* but WITHOUT ANY WARRANTY; without even the implied warranty of
+* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+* Lesser General Public License for more details.
+*
+* You should have received a copy of the GNU Lesser General Public
+* License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+*/
 
 #include "../../include/fluid/CCoolProp.hpp"
 
 #ifdef USE_COOLPROP
-#include "AbstractState.h"
 #include "CoolProp.h"
+#include "AbstractState.h"
 
 CCoolProp::CCoolProp(string fluidname) : CFluidModel() {
-  fluid_entity = std::unique_ptr<CoolProp::AbstractState>(CoolProp::AbstractState::factory("HEOS", fluidname));
-  Gas_Constant = fluid_entity->gas_constant() / fluid_entity->molar_mass();
+  fluid_entity = std::unique_ptr<CoolProp::AbstractState>(CoolProp::AbstractState::factory("HEOS",fluidname));
+  Gas_Constant = fluid_entity->gas_constant()/fluid_entity->molar_mass();
   Pressure_Critical = fluid_entity->p_critical();
   Temperature_Critical = fluid_entity->T_critical();
   acentric_factor = fluid_entity->acentric_factor();
@@ -55,26 +55,33 @@ void CCoolProp::SetTDState_rhoe(su2double rho, su2double e) {
   dPde_rho = fluid_entity->first_partial_deriv(CoolProp::iP, CoolProp::iUmass, CoolProp::iDmass);
   dTdrho_e = fluid_entity->first_partial_deriv(CoolProp::iT, CoolProp::iDmass, CoolProp::iUmass);
   dTde_rho = fluid_entity->first_partial_deriv(CoolProp::iT, CoolProp::iUmass, CoolProp::iDmass);
-  if (fluid_entity->phase() == CoolProp::iphase_twophase) {
+  if (fluid_entity->phase() == 6) {
     // assume it is pure gas
     fluid_entity->specify_phase(CoolProp::iphase_gas);
-    CheckPressure(Pressure);
+    if(abs(Pressure/Pressure_Critical-1)<0.01){
+      // if P is very cloase to Pc, the CoolProp has issue
+      Pressure = Pressure_Critical*0.99;
+    }
     fluid_entity->update(CoolProp::PT_INPUTS, Pressure, Temperature);
-    if (abs(fluid_entity->rhomass() / Density - 1) < dp) {
+    if(abs(fluid_entity->rhomass()/Density-1)*100 < 1){
       // origial phase is near saturation gas, then just compute sound speed
       SoundSpeed2 = pow(fluid_entity->speed_sound(), 2);
-    } else {
+    }
+    else{
       // original phase is not near saturation gas, then specify the phase as gas phase
       fluid_entity->specify_phase(CoolProp::iphase_gas);
-      SetTDState_PT(Pressure, Temperature);
+      SetTDState_PT(Pressure,Temperature);
     }
-  } else {
+  }
+  else{
     SoundSpeed2 = pow(fluid_entity->speed_sound(), 2);
   }
 }
 
 void CCoolProp::SetTDState_PT(su2double P, su2double T) {
-  CheckPressure(P);
+  if(abs(P/Pressure_Critical-1)<0.01) {
+    P = Pressure_Critical * 0.99;
+  }
   fluid_entity->update(CoolProp::PT_INPUTS, P, T);
   su2double rho = fluid_entity->rhomass();
   su2double e = fluid_entity->umass();
@@ -82,14 +89,18 @@ void CCoolProp::SetTDState_PT(su2double P, su2double T) {
 }
 
 void CCoolProp::SetTDState_Prho(su2double P, su2double rho) {
-  CheckPressure(P);
+  if(abs(P/Pressure_Critical-1)<0.01){
+    P = Pressure_Critical*0.99;
+  }
   fluid_entity->update(CoolProp::DmassP_INPUTS, rho, P);
   su2double e = fluid_entity->umass();
   SetTDState_rhoe(rho, e);
 }
 
-void CCoolProp::SetEnergy_Prho(su2double P, su2double rho) {
-  CheckPressure(P);
+void CCoolProp::SetEnergy_Prho(su2double P, su2double rho){
+  if(abs(P/Pressure_Critical-1)<0.01){
+    P = Pressure_Critical*0.99;
+  }
   fluid_entity->update(CoolProp::DmassP_INPUTS, rho, P);
   StaticEnergy = fluid_entity->umass();
 }
@@ -101,8 +112,10 @@ void CCoolProp::SetTDState_hs(su2double h, su2double s) {
   SetTDState_rhoe(rho, e);
 }
 
-void CCoolProp::SetTDState_Ps(su2double P, su2double s) {
-  CheckPressure(P);
+void  CCoolProp::SetTDState_Ps(su2double P, su2double s) {
+  if(abs(P/Pressure_Critical-1)<0.01){
+    P = Pressure_Critical*0.99;
+  }
   fluid_entity->update(CoolProp::PSmass_INPUTS, P, s);
   su2double rho = fluid_entity->rhomass();
   su2double e = fluid_entity->umass();
@@ -115,19 +128,16 @@ void CCoolProp::SetTDState_rhoT(su2double rho, su2double T) {
   SetTDState_rhoe(rho, e);
 }
 
-void CCoolProp::ComputeDerivativeNRBC_Prho(su2double P, su2double rho) {
+void  CCoolProp::ComputeDerivativeNRBC_Prho(su2double P, su2double rho) {
   SetTDState_Prho(P, rho);
-  dhdrho_P = fluid_entity->first_partial_deriv(CoolProp::iHmass, CoolProp::iDmass, CoolProp::iP);
-  dhdP_rho = fluid_entity->first_partial_deriv(CoolProp::iHmass, CoolProp::iP, CoolProp::iDmass);
-  dsdP_rho = fluid_entity->first_partial_deriv(CoolProp::iSmass, CoolProp::iP, CoolProp::iDmass);
-  dsdrho_P = fluid_entity->first_partial_deriv(CoolProp::iSmass, CoolProp::iDmass, CoolProp::iP);
+  dhdrho_P = fluid_entity->first_partial_deriv(CoolProp::iHmass,CoolProp::iDmass,CoolProp::iP);
+  dhdP_rho = fluid_entity->first_partial_deriv(CoolProp::iHmass,CoolProp::iP,CoolProp::iDmass);
+  dsdP_rho = fluid_entity->first_partial_deriv(CoolProp::iSmass,CoolProp::iP,CoolProp::iDmass);
+  dsdrho_P = fluid_entity->first_partial_deriv(CoolProp::iSmass,CoolProp::iDmass,CoolProp::iP);
 }
 
 #else
 CCoolProp::CCoolProp(string fluidname) {
-  SU2_MPI::Error(
-      "SU2 was not compiled with CoolProp (-Denable-coolprop=true). Note that CoolProp cannot be used with directdiff "
-      "or autodiff",
-      CURRENT_FUNCTION);
+    SU2_MPI::Error("SU2 was not compiled with CoolProp (-Denable-coolprop=true). Note that CoolProp cannot be used with directdiff or autodiff", CURRENT_FUNCTION);
 }
-#endif
+#endif
\ No newline at end of file

From 32d7bb38596d4b1064e906aba4e77d5b9fb31b85 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Fri, 28 Apr 2023 17:52:34 -0700
Subject: [PATCH 413/656] Update Common/include/CConfig.hpp

---
 Common/include/CConfig.hpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index 591760c5e5d..13f1a8f6e9d 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -3785,7 +3785,7 @@ class CConfig {
    * \brief Get name of the input file for the data-driven fluid model interpolation method.
    * \return Name of the input file for the interpolation method.
    */
-  string* GetDataDriven_FileNames(void) const { return DataDriven_Method_FileNames; }
+  const string* GetDataDriven_FileNames(void) const { return DataDriven_Method_FileNames; }
 
   /*!
    * \brief Get number of listed look-up table or multi-layer perceptron input files.

From 36e7f6911b695ff1cb4740eb0255c134b41b3e1b Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Fri, 28 Apr 2023 20:40:57 -0700
Subject: [PATCH 414/656] allow simple custom outputs for all output classes
 and allow them to be used for primal and adjoint variables

---
 SU2_CFD/include/output/CFlowOutput.hpp        |  5 ++-
 SU2_CFD/include/output/COutput.hpp            | 12 ++++++
 SU2_CFD/src/output/CAdjElasticityOutput.cpp   |  2 +
 SU2_CFD/src/output/CAdjFlowCompOutput.cpp     |  2 +
 SU2_CFD/src/output/CAdjFlowIncOutput.cpp      |  2 +
 SU2_CFD/src/output/CAdjFlowOutput.cpp         |  2 +
 SU2_CFD/src/output/CAdjHeatOutput.cpp         |  1 +
 SU2_CFD/src/output/CElasticityOutput.cpp      |  3 ++
 SU2_CFD/src/output/CFlowCompFEMOutput.cpp     |  1 +
 SU2_CFD/src/output/CFlowOutput.cpp            | 23 +++++++++--
 SU2_CFD/src/output/CHeatOutput.cpp            |  2 +
 SU2_CFD/src/output/COutput.cpp                | 39 ++++++++++++++++++-
 TestCases/disc_adj_fsi/Airfoil_2d/config.cfg  |  2 +-
 .../disc_adj_fsi/Airfoil_2d/configFEA.cfg     |  7 +++-
 TestCases/parallel_regression_AD.py           |  4 +-
 15 files changed, 95 insertions(+), 12 deletions(-)

diff --git a/SU2_CFD/include/output/CFlowOutput.hpp b/SU2_CFD/include/output/CFlowOutput.hpp
index a3893cfb23c..dcab274bf02 100644
--- a/SU2_CFD/include/output/CFlowOutput.hpp
+++ b/SU2_CFD/include/output/CFlowOutput.hpp
@@ -215,7 +215,8 @@ class CFlowOutput : public CFVMOutput{
    * \brief Helper for custom outputs, converts variable names to indices and pointers which are then used
    * to evaluate the custom expressions.
    */
-  void ConvertVariableSymbolsToIndices(const CPrimitiveIndices<unsigned long>& idx, CustomOutput& output) const;
+  void ConvertVariableSymbolsToIndices(const CPrimitiveIndices<unsigned long>& idx, bool allowSkip,
+                                       CustomOutput& output) const;
 
   /*!
    * \brief Compute value of the Q criteration for vortex idenfitication
@@ -296,7 +297,7 @@ class CFlowOutput : public CFVMOutput{
    * \param[in] force_writing - boolean that forces writing of volume output
    * \param[in] iFile - index to the file that we need to consider for volume output
    */
-  bool WriteVolumeOutput(CConfig *config, unsigned long Iter, bool force_writing, unsigned short iFile) override; 
+  bool WriteVolumeOutput(CConfig *config, unsigned long Iter, bool force_writing, unsigned short iFile) override;
   /*!
    * \brief Write the forces breakdown file
    * \param[in] config - Definition of the particular problem per zone.
diff --git a/SU2_CFD/include/output/COutput.hpp b/SU2_CFD/include/output/COutput.hpp
index 2b2b093fbc9..bee30933850 100644
--- a/SU2_CFD/include/output/COutput.hpp
+++ b/SU2_CFD/include/output/COutput.hpp
@@ -223,6 +223,10 @@ class COutput {
      We store pointers to the required outputs to speed-up access. ---*/
     std::vector<const su2double*> otherOutputs;
 
+    /*--- For discrete adjoint we may need to skip some expressions because there is one output class
+     for the primal solver and one for the discrete adjoint (each with different variables). ---*/
+    bool skip = false;
+
     /*--- For evaluation, "vars" is a functor (i.e. has operator()) that returns the value of a variable at a given
      point. For example, it can be a wrapper to the primitives pointer, in which case varIndices needs to be setup
      with primitive indices. ---*/
@@ -807,6 +811,14 @@ class COutput {
    */
   void SetCustomOutputs(const CConfig *config);
 
+  /*!
+   * \brief Evaluates function-type custom outputs.
+   * Derived classes can use this to compute simple expressions of other outputs if they
+   * do not implement surface averages. This should be called just before evaluating the
+   * custom objective function.
+   */
+  void ComputeSimpleCustomOutputs(const CConfig *config);
+
   /*!
    * \brief Load values of the history fields common for all solvers.
    * \param[in] config - Definition of the particular problem.
diff --git a/SU2_CFD/src/output/CAdjElasticityOutput.cpp b/SU2_CFD/src/output/CAdjElasticityOutput.cpp
index e30f2895f65..5be89b6b2cb 100644
--- a/SU2_CFD/src/output/CAdjElasticityOutput.cpp
+++ b/SU2_CFD/src/output/CAdjElasticityOutput.cpp
@@ -172,6 +172,8 @@ inline void CAdjElasticityOutput::LoadHistoryData(CConfig *config, CGeometry *ge
       SetHistoryOutputValue("BGS_ADJ_DISP_Z", log10(solver[ADJFEA_SOL]->GetRes_BGS(2)));
     }
   }
+
+  ComputeSimpleCustomOutputs(config);
 }
 
 void CAdjElasticityOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolver **solver, unsigned long iPoint){
diff --git a/SU2_CFD/src/output/CAdjFlowCompOutput.cpp b/SU2_CFD/src/output/CAdjFlowCompOutput.cpp
index 7555b7ca6c3..8804f203b7f 100644
--- a/SU2_CFD/src/output/CAdjFlowCompOutput.cpp
+++ b/SU2_CFD/src/output/CAdjFlowCompOutput.cpp
@@ -225,6 +225,8 @@ void CAdjFlowCompOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, C
   }
 
   LoadHistoryDataAdjScalar(config, solver);
+
+  ComputeSimpleCustomOutputs(config);
 }
 
 void CAdjFlowCompOutput::SetVolumeOutputFields(CConfig *config) {
diff --git a/SU2_CFD/src/output/CAdjFlowIncOutput.cpp b/SU2_CFD/src/output/CAdjFlowIncOutput.cpp
index 6b58c2206b2..25ff3365250 100644
--- a/SU2_CFD/src/output/CAdjFlowIncOutput.cpp
+++ b/SU2_CFD/src/output/CAdjFlowIncOutput.cpp
@@ -275,6 +275,8 @@ void CAdjFlowIncOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, CS
   }
 
   LoadHistoryDataAdjScalar(config, solver);
+
+  ComputeSimpleCustomOutputs(config);
 }
 
 void CAdjFlowIncOutput::SetVolumeOutputFields(CConfig *config) {
diff --git a/SU2_CFD/src/output/CAdjFlowOutput.cpp b/SU2_CFD/src/output/CAdjFlowOutput.cpp
index bf80b6c807f..4ef01b6c16c 100644
--- a/SU2_CFD/src/output/CAdjFlowOutput.cpp
+++ b/SU2_CFD/src/output/CAdjFlowOutput.cpp
@@ -172,6 +172,8 @@ void CAdjFlowOutput::LoadHistoryDataAdjScalar(const CConfig* config, const CSolv
     SetHistoryOutputValue("LINSOL_ITER_SPECIES", adjspecies_solver->GetIterLinSolver());
     SetHistoryOutputValue("LINSOL_RESIDUAL_SPECIES", log10(adjspecies_solver->GetResLinSolver()));
   }
+
+  ComputeSimpleCustomOutputs(config);
 }
 
 void CAdjFlowOutput::SetVolumeOutputFieldsAdjScalarSolution(const CConfig* config) {
diff --git a/SU2_CFD/src/output/CAdjHeatOutput.cpp b/SU2_CFD/src/output/CAdjHeatOutput.cpp
index 65d5679b8ca..3e0cbcaf50c 100644
--- a/SU2_CFD/src/output/CAdjHeatOutput.cpp
+++ b/SU2_CFD/src/output/CAdjHeatOutput.cpp
@@ -142,6 +142,7 @@ void CAdjHeatOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, CSolv
     SetHistoryOutputValue("DEFORM_RESIDUAL", log10(solver[MESH_SOL]->System.GetResidual()));
   }
 
+  ComputeSimpleCustomOutputs(config);
 }
 
 void CAdjHeatOutput::SetVolumeOutputFields(CConfig *config){
diff --git a/SU2_CFD/src/output/CElasticityOutput.cpp b/SU2_CFD/src/output/CElasticityOutput.cpp
index 365901ba548..fe5efe5b390 100644
--- a/SU2_CFD/src/output/CElasticityOutput.cpp
+++ b/SU2_CFD/src/output/CElasticityOutput.cpp
@@ -146,6 +146,9 @@ void CElasticityOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, CS
     SetHistoryOutputValue("VOLUME_FRACTION", fea_solver->GetTotal_OFVolFrac());
     SetHistoryOutputValue("TOPOL_DISCRETENESS", fea_solver->GetTotal_OFDiscreteness());
   }
+
+  ComputeSimpleCustomOutputs(config);
+
   /*--- Keep this as last, since it uses the history values that were set. ---*/
   SetCustomAndComboObjectives(FEA_SOL, config, solver);
 
diff --git a/SU2_CFD/src/output/CFlowCompFEMOutput.cpp b/SU2_CFD/src/output/CFlowCompFEMOutput.cpp
index 91ce4393034..4a919c9278b 100644
--- a/SU2_CFD/src/output/CFlowCompFEMOutput.cpp
+++ b/SU2_CFD/src/output/CFlowCompFEMOutput.cpp
@@ -263,6 +263,7 @@ void CFlowCompFEMOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, C
 
   SetAerodynamicCoefficients(config, flow_solver);
 
+  ComputeSimpleCustomOutputs(config);
 }
 
 bool CFlowCompFEMOutput::SetInitResiduals(const CConfig *config){
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index bff61c408c9..25de58c53fa 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -745,7 +745,7 @@ void CFlowOutput::SetAnalyzeSurfaceSpeciesVariance(const CSolver* const*solver,
   SetHistoryOutputValue("SURFACE_SPECIES_VARIANCE", Tot_Surface_SpeciesVariance);
 }
 
-void CFlowOutput::ConvertVariableSymbolsToIndices(const CPrimitiveIndices<unsigned long>& idx,
+void CFlowOutput::ConvertVariableSymbolsToIndices(const CPrimitiveIndices<unsigned long>& idx, const bool allowSkip,
                                                   CustomOutput& output) const {
   const auto nameToIndex = PrimitiveNameToIndexMap(idx);
 
@@ -796,23 +796,38 @@ void CFlowOutput::ConvertVariableSymbolsToIndices(const CPrimitiveIndices<unsign
     output.varIndices.back() += output.otherOutputs.size();
     output.otherOutputs.push_back(GetPtrToHistoryOutput(var));
     if (output.otherOutputs.back() == nullptr) {
-      SU2_MPI::Error("Invalid history output or solver variable (" + var + ") used in function " + output.name +
-                     "\nValid solvers variables:\n" + knownVariables.str(), CURRENT_FUNCTION);
+      if (!allowSkip) {
+        SU2_MPI::Error("Invalid history output or solver variable (" + var + ") used in function " + output.name +
+                      "\nValid solvers variables:\n" + knownVariables.str(), CURRENT_FUNCTION);
+      } else {
+        if (rank == MASTER_NODE) {
+          std::cout << "Info: Ignoring function " + output.name + " because it may be used by the primal/adjoint "
+                        "solver.\n      If the function is ignored twice it is invalid." << std::endl;
+        }
+        output.skip = true;
+        break;
+      }
     }
   }
 }
 
 void CFlowOutput::SetCustomOutputs(const CSolver* const* solver, const CGeometry *geometry, const CConfig *config) {
 
+  const bool adjoint = config->GetDiscrete_Adjoint();
   const bool axisymmetric = config->GetAxisymmetric();
   const auto* flowNodes = su2staticcast_p<const CFlowVariable*>(solver[FLOW_SOL]->GetNodes());
 
   for (auto& output : customOutputs) {
+    if (output.skip) continue;
+
     if (output.varIndices.empty()) {
+      const bool allowSkip = adjoint && (output.type == OperationType::FUNCTION);
+
       /*--- Setup indices for the symbols in the expression. ---*/
       const auto primIdx = CPrimitiveIndices<unsigned long>(config->GetKind_Regime() == ENUM_REGIME::INCOMPRESSIBLE,
           config->GetNEMOProblem(), nDim, config->GetnSpecies());
-      ConvertVariableSymbolsToIndices(primIdx, output);
+      ConvertVariableSymbolsToIndices(primIdx, allowSkip, output);
+      if (output.skip) continue;
 
       /*--- Convert marker names to their index (if any) in this rank. Or probe locations to nearest points. ---*/
 
diff --git a/SU2_CFD/src/output/CHeatOutput.cpp b/SU2_CFD/src/output/CHeatOutput.cpp
index 6150f253480..eccba6e70e9 100644
--- a/SU2_CFD/src/output/CHeatOutput.cpp
+++ b/SU2_CFD/src/output/CHeatOutput.cpp
@@ -89,6 +89,8 @@ void CHeatOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, CSolver
   SetHistoryOutputValue("LINSOL_RESIDUAL", log10(heat_solver->GetResLinSolver()));
   SetHistoryOutputValue("CFL_NUMBER", config->GetCFL(MESH_0));
 
+  ComputeSimpleCustomOutputs(config);
+
   /*--- Keep this as last, since it uses the history values that were set. ---*/
   SetCustomAndComboObjectives(HEAT_SOL, config, solver);
 }
diff --git a/SU2_CFD/src/output/COutput.cpp b/SU2_CFD/src/output/COutput.cpp
index 7c76bbf50bc..db83dc1e322 100644
--- a/SU2_CFD/src/output/COutput.cpp
+++ b/SU2_CFD/src/output/COutput.cpp
@@ -2135,7 +2135,7 @@ bool COutput::WriteVolumeOutput(CConfig *config, unsigned long Iter, bool force_
     return ((Iter % config->GetVolumeOutputFrequency(iFile) == 0)) || force_writing;
   }
       return ((Iter > 0) && (Iter % config->GetVolumeOutputFrequency(iFile) == 0)) || force_writing;
- 
+
 }
 
 void COutput::SetCommonHistoryFields() {
@@ -2287,6 +2287,43 @@ void COutput::SetCustomOutputs(const CConfig* config) {
 
 }
 
+void COutput::ComputeSimpleCustomOutputs(const CConfig *config) {
+  const bool adjoint = config->GetDiscrete_Adjoint();
+
+  for (auto& output : customOutputs) {
+    if (output.type != OperationType::FUNCTION) continue;
+
+    if (output.varIndices.empty()) {
+      output.varIndices.reserve(output.varSymbols.size());
+      output.otherOutputs.reserve(output.varSymbols.size());
+
+      for (const auto& var : output.varSymbols) {
+        output.varIndices.push_back(output.varIndices.size());
+        output.otherOutputs.push_back(GetPtrToHistoryOutput(var));
+        if (output.otherOutputs.back() == nullptr) {
+          if (!adjoint) {
+            // In primal mode all functions must be valid.
+            SU2_MPI::Error("Invalid history output (" + var + ") used in function " + output.name, CURRENT_FUNCTION);
+          } else {
+            if (rank == MASTER_NODE) {
+              std::cout << "Info: Ignoring function " + output.name + " because it may be used by the primal/adjoint "
+                          "solver.\n      If the function is ignored twice it is invalid." << std::endl;
+            }
+            output.skip = true;
+            break;
+          }
+        }
+      }
+    }
+    if (output.skip) continue;
+
+    auto Functor = [&](unsigned long i) {
+      return *output.otherOutputs[i];
+    };
+    SetHistoryOutputValue(output.name, output.Eval(Functor));
+  }
+}
+
 void COutput::LoadCommonHistoryData(const CConfig *config) {
 
   SetHistoryOutputValue("TIME_STEP", config->GetDelta_UnstTimeND()*config->GetTime_Ref());
diff --git a/TestCases/disc_adj_fsi/Airfoil_2d/config.cfg b/TestCases/disc_adj_fsi/Airfoil_2d/config.cfg
index a484a26c79b..c35de2da263 100755
--- a/TestCases/disc_adj_fsi/Airfoil_2d/config.cfg
+++ b/TestCases/disc_adj_fsi/Airfoil_2d/config.cfg
@@ -13,6 +13,6 @@ MESH_FILENAME= mesh.su2
 
 OBJECTIVE_FUNCTION= CUSTOM_OBJFUNC
 
-SCREEN_OUTPUT= OUTER_ITER, AVG_BGS_RES[0], AVG_BGS_RES[1], LINSOL_RESIDUAL[0], SENS_E_0[1], SENS_NU_0[1]
+SCREEN_OUTPUT= OUTER_ITER, AVG_BGS_RES[0], AVG_BGS_RES[1], LINSOL_RESIDUAL[0], sens_e[1], SENS_NU_0[1]
 
 %WRT_ZONE_CONV=YES
diff --git a/TestCases/disc_adj_fsi/Airfoil_2d/configFEA.cfg b/TestCases/disc_adj_fsi/Airfoil_2d/configFEA.cfg
index 625809928eb..80502871ff2 100755
--- a/TestCases/disc_adj_fsi/Airfoil_2d/configFEA.cfg
+++ b/TestCases/disc_adj_fsi/Airfoil_2d/configFEA.cfg
@@ -7,7 +7,7 @@ REFERENCE_NODE= 234
 REFERENCE_NODE_DISPLACEMENT= (0.0, 0.0)
 REFERENCE_NODE_PENALTY= 1.0
 DESIGN_VARIABLE_FEA= YOUNG_MODULUS
-CUSTOM_OBJFUNC= '1e2 * (1e3 * REFERENCE_NODE + TOPOL_COMPLIANCE)'
+CUSTOM_OBJFUNC= '1e2 * (ref_node + TOPOL_COMPLIANCE)'
 
 % Solid properties ----------------------------------------------------- %
 MATERIAL_MODEL= NEO_HOOKEAN
@@ -41,7 +41,10 @@ INCREMENTAL_LOAD= YES
 % In\Out --------------------------------------------------------------- %
 MESH_FILENAME= mesh.su2
 MESH_FORMAT= SU2
-
+% Scale SENS_E_0 to avoid a very small value in the regression test.
+% Test using custom outputs for the adjoint and primal solver.
+CUSTOM_OUTPUTS= 'sens_e : Function{1e8 * SENS_E_0};\
+                 ref_node : Function{1e3 * REFERENCE_NODE}'
 RESTART_SOL= NO
 SOLUTION_FILENAME= solution_solid.dat
 SOLUTION_ADJ_FILENAME= adjoint_solid.dat
diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index 61c79202fb8..ebe91bf9337 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -276,8 +276,8 @@ def main():
     discadj_fsi2.cfg_dir   = "disc_adj_fsi/Airfoil_2d"
     discadj_fsi2.cfg_file  = "config.cfg"
     discadj_fsi2.test_iter = 8
-    discadj_fsi2.test_vals         = [-4.349377, 0.192713, -1.303589, 7.5407e-09, 2.3244]
-    discadj_fsi2.test_vals_aarch64 = [-3.479505, 0.127953, -1.303589, 7.5407e-09, 2.3244]
+    discadj_fsi2.test_vals         = [-4.349377, 0.192713, -1.303589, 0.75407, 2.3244]
+    discadj_fsi2.test_vals_aarch64 = [-3.479505, 0.127953, -1.303589, 0.75407, 2.3244]
     discadj_fsi2.tol       = 0.00001
     test_list.append(discadj_fsi2)
 

From f9fcdff892931b11d1ca1795b51ee7c44ac81a05 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Fri, 28 Apr 2023 20:45:00 -0700
Subject: [PATCH 415/656] check custom output type

---
 SU2_CFD/src/output/COutput.cpp | 5 ++++-
 1 file changed, 4 insertions(+), 1 deletion(-)

diff --git a/SU2_CFD/src/output/COutput.cpp b/SU2_CFD/src/output/COutput.cpp
index db83dc1e322..90d9f3ef925 100644
--- a/SU2_CFD/src/output/COutput.cpp
+++ b/SU2_CFD/src/output/COutput.cpp
@@ -2291,7 +2291,10 @@ void COutput::ComputeSimpleCustomOutputs(const CConfig *config) {
   const bool adjoint = config->GetDiscrete_Adjoint();
 
   for (auto& output : customOutputs) {
-    if (output.type != OperationType::FUNCTION) continue;
+    if (output.type != OperationType::FUNCTION) {
+      if (adjoint) continue;
+      SU2_MPI::Error("The current solver can only use 'Function' custom outputs.", CURRENT_FUNCTION);
+    }
 
     if (output.varIndices.empty()) {
       output.varIndices.reserve(output.varSymbols.size());

From df5838c335be8aa7d2ad6b5b09ddeec8d4e09b94 Mon Sep 17 00:00:00 2001
From: Afshawn Lotfi <me@afshawn.org>
Date: Thu, 27 Apr 2023 15:56:37 +0000
Subject: [PATCH 416/656] added compatibility for multizone driver selection

---
 SU2_CFD/include/drivers/CDriverBase.hpp       |  19 ++-
 .../src/drivers/CDiscAdjMultizoneDriver.cpp   |   8 +-
 SU2_CFD/src/drivers/CDriver.cpp               | 142 +++++++++---------
 SU2_CFD/src/drivers/CDriverBase.cpp           |  10 +-
 SU2_CFD/src/drivers/CMultizoneDriver.cpp      |  16 +-
 SU2_CFD/src/python_wrapper_structure.cpp      |  34 ++---
 6 files changed, 120 insertions(+), 109 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index d720246efb7..00ccb3d29b5 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -54,7 +54,7 @@ class CDriverBase {
       UsedTime;        /*!< \brief Elapsed time between Start and Stop point of the timer. */
 
   unsigned long TimeIter;
-
+  unsigned long selected_iZone = ZONE_0; /*!< \brief Selected zone for the driver. Defaults to ZONE_0 */
   unsigned short iMesh,  /*!< \brief Iterator on mesh levels. */
       iZone,             /*!< \brief Iterator on zones. */
       nZone,             /*!< \brief Total number of zones in the problem. */
@@ -227,7 +227,7 @@ class CDriverBase {
       SU2_MPI::Error("Initial coordinates are only available with DEFORM_MESH= YES", CURRENT_FUNCTION);
     }
     auto* coords =
-        const_cast<su2activematrix*>(solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord());
+        const_cast<su2activematrix*>(solver_container[selected_iZone][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord());
     return CPyWrapperMatrixView(*coords, "InitialCoordinates", true);
   }
 
@@ -241,7 +241,7 @@ class CDriverBase {
     if (iMarker >= GetNumberMarkers()) SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
 
     auto* coords =
-        const_cast<su2activematrix*>(solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord());
+        const_cast<su2activematrix*>(solver_container[selected_iZone][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord());
     return CPyWrapperMarkerMatrixView(*coords, main_geometry->vertex[iMarker], main_geometry->GetnVertex(iMarker),
                                       "MarkerInitialCoordinates", true);
   }
@@ -530,6 +530,17 @@ class CDriverBase {
     main_geometry->SetCustomBoundaryHeatFlux(iMarker, iVertex, WallHeatFlux);
   }
 
+
+  /*!
+   * \brief Selects zone to be used for Driver operation
+   * \param[in] iZone - Zone identifier.
+   */
+  inline void SelectZone(unsigned long iZone) {
+    selected_iZone = iZone;
+    main_geometry = geometry_container[selected_iZone][INST_0][MESH_0];
+    main_config = config_container[selected_iZone];
+  }
+
   /*!
    * \brief Get the wall normal heat flux at a vertex on a specified marker of the flow or heat solver.
    * \note This can be the output of a heat or flow solver in a CHT setting.
@@ -677,7 +688,7 @@ class CDriverBase {
     if (iMarker < std::numeric_limits<unsigned short>::max() && iMarker > GetNumberMarkers()) {
       SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
     }
-    auto* solver = solver_container[ZONE_0][INST_0][MESH_0][iSolver];
+    auto* solver = solver_container[selected_iZone][INST_0][MESH_0][iSolver];
     if (solver == nullptr) SU2_MPI::Error("The selected solver does not exist.", CURRENT_FUNCTION);
     return solver;
   }
diff --git a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
index 6277f409b8d..13319167fc6 100644
--- a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
@@ -440,7 +440,7 @@ void CDiscAdjMultizoneDriver::Run() {
     /*--- Check for convergence. ---*/
 
     StopCalc = driver_output->GetConvergence() || (iOuterIter == nOuterIter-1) ||
-               ((nZone==1) && output_container[ZONE_0]->GetConvergence());
+               ((nZone==1) && output_container[selected_iZone]->GetConvergence());
 
     /*--- Clear the stored adjoint information to be ready for a new evaluation. ---*/
 
@@ -765,13 +765,13 @@ void CDiscAdjMultizoneDriver::SetObjFunction(RECORDING kind_recording) {
 void CDiscAdjMultizoneDriver::SetAdjObjFunction() {
   su2double seeding = 1.0;
 
-  if (config_container[ZONE_0]->GetTime_Domain()) {
-    const auto IterAvg_Obj = config_container[ZONE_0]->GetIter_Avg_Objective();
+  if (config_container[selected_iZone]->GetTime_Domain()) {
+    const auto IterAvg_Obj = config_container[selected_iZone]->GetIter_Avg_Objective();
     if (TimeIter < IterAvg_Obj) {
       /*--- Default behavior when no window is chosen is to use Square-Windowing, i.e. the numerator equals 1.0 ---*/
       auto windowEvaluator = CWindowingTools();
       const su2double weight =
-          windowEvaluator.GetWndWeight(config_container[ZONE_0]->GetKindWindow(), TimeIter, IterAvg_Obj - 1);
+          windowEvaluator.GetWndWeight(config_container[selected_iZone]->GetKindWindow(), TimeIter, IterAvg_Obj - 1);
       seeding = weight / IterAvg_Obj;
     }
     else {
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index 07fc5ca3697..c60a7ba9b0c 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -120,8 +120,8 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
 
   /*--- Retrieve dimension from mesh file ---*/
 
-  nDim = CConfig::GetnDim(config_container[ZONE_0]->GetMesh_FileName(),
-                          config_container[ZONE_0]->GetMesh_FileFormat());
+  nDim = CConfig::GetnDim(config_container[selected_iZone]->GetMesh_FileName(),
+                          config_container[selected_iZone]->GetMesh_FileFormat());
 
   /*--- Output preprocessing ---*/
 
@@ -243,7 +243,7 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
     }
   }
 
-  if (config_container[ZONE_0]->GetBoolTurbomachinery()){
+  if (config_container[selected_iZone]->GetBoolTurbomachinery()){
     if (rank == MASTER_NODE)
       cout << endl <<"---------------------- Turbomachinery Preprocessing ---------------------" << endl;
 
@@ -342,7 +342,7 @@ void CDriver::InitializeContainers(){
 
 void CDriver::Finalize() {
 
-  const bool wrt_perf = config_container[ZONE_0]->GetWrt_Performance();
+  const bool wrt_perf = config_container[selected_iZone]->GetWrt_Performance();
 
     /*--- Output some information to the console. ---*/
 
@@ -350,10 +350,10 @@ void CDriver::Finalize() {
 
     /*--- Print out the number of non-physical points and reconstructions ---*/
 
-    if (config_container[ZONE_0]->GetNonphysical_Points() > 0)
-      cout << "Warning: there are " << config_container[ZONE_0]->GetNonphysical_Points() << " non-physical points in the solution." << endl;
-    if (config_container[ZONE_0]->GetNonphysical_Reconstr() > 0)
-      cout << "Warning: " << config_container[ZONE_0]->GetNonphysical_Reconstr() << " reconstructed states for upwinding are non-physical." << endl;
+    if (config_container[selected_iZone]->GetNonphysical_Points() > 0)
+      cout << "Warning: there are " << config_container[selected_iZone]->GetNonphysical_Points() << " non-physical points in the solution." << endl;
+    if (config_container[selected_iZone]->GetNonphysical_Reconstr() > 0)
+      cout << "Warning: " << config_container[selected_iZone]->GetNonphysical_Reconstr() << " reconstructed states for upwinding are non-physical." << endl;
   }
 
   if (rank == MASTER_NODE)
@@ -456,8 +456,8 @@ void CDriver::Finalize() {
   // Note that for now this is called only by a single thread, but all
   // necessary variables have been made thread private for safety (tick/tock)!!
 
-  config_container[ZONE_0]->SetProfilingCSV();
-  config_container[ZONE_0]->GEMMProfilingCSV();
+  config_container[selected_iZone]->SetProfilingCSV();
+  config_container[selected_iZone]->GEMMProfilingCSV();
 
   /*--- Deallocate config container ---*/
   if (config_container!= nullptr) {
@@ -585,14 +585,14 @@ void CDriver::PreprocessInput(CConfig **&config, CConfig *&driver_config) {
 
   /*--- Keep a reference to the main (ZONE 0) config. ---*/
 
-  main_config = config_container[ZONE_0];
+  main_config = config_container[selected_iZone];
 
   /*--- Determine whether or not the FEM solver is used, which decides the type of
    *    geometry classes that are instantiated. Only adapted for single-zone problems ---*/
 
-  fem_solver = config_container[ZONE_0]->GetFEMSolver();
+  fem_solver = config_container[selected_iZone]->GetFEMSolver();
 
-  fsi = config_container[ZONE_0]->GetFSI_Simulation();
+  fsi = config_container[selected_iZone]->GetFSI_Simulation();
 }
 
 void CDriver::InitializeGeometry(CConfig* config, CGeometry **&geometry, bool dummy){
@@ -693,7 +693,7 @@ void CDriver::InitializeGeometry(CConfig* config, CGeometry **&geometry, bool du
 
   /*--- Keep a reference to the main (ZONE_0, INST_0, MESH_0) geometry. ---*/
 
-  main_geometry = geometry_container[ZONE_0][INST_0][MESH_0];
+  main_geometry = geometry_container[selected_iZone][INST_0][MESH_0];
 }
 
 void CDriver::InitializeGeometryFVM(CConfig *config, CGeometry **&geometry) {
@@ -2470,7 +2470,7 @@ void CDriver::InitializeInterface(CConfig **config, CSolver***** solver, CGeomet
           interface_type = FLOW_TRACTION;
           auto nConst = 2;
           bool conservative = config[target]->GetConservativeInterpolation();
-          if(!config[ZONE_0]->GetDiscrete_Adjoint()) {
+          if(!config[selected_iZone]->GetDiscrete_Adjoint()) {
             interface[donor][target] = new CFlowTractionInterface(nDim, nConst, config[donor], conservative);
           } else {
             interface[donor][target] = new CDiscAdjFlowTractionInterface(nDim, nConst, config[donor], conservative);
@@ -2570,7 +2570,7 @@ void CDriver::PreprocessStaticMesh(const CConfig *config, CGeometry** geometry){
         /*--- Set the grid velocities on all multigrid levels for a steadily
            rotating reference frame. ---*/
 
-        for (iMGlevel = 0; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++){
+        for (iMGlevel = 0; iMGlevel <= config_container[selected_iZone]->GetnMGLevels(); iMGlevel++){
           geometry[iMGlevel]->SetRotationalVelocity(config, true);
           geometry[iMGlevel]->SetShroudVelocity(config);
         }
@@ -2588,7 +2588,7 @@ void CDriver::PreprocessStaticMesh(const CConfig *config, CGeometry** geometry){
 
         /*--- Set the translational velocity on all grid levels. ---*/
 
-        for (iMGlevel = 0; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++)
+        for (iMGlevel = 0; iMGlevel <= config_container[selected_iZone]->GetnMGLevels(); iMGlevel++)
           geometry_container[iZone][INST_0][iMGlevel]->SetTranslationalVelocity(config, true);
 
         break;
@@ -2667,8 +2667,8 @@ void CDriver::PreprocessOutput(CConfig **config, CConfig *driver_config, COutput
   }
 
   /*--- Check for an unsteady restart. Update ExtIter if necessary. ---*/
-  if (config_container[ZONE_0]->GetTime_Domain() && config_container[ZONE_0]->GetRestart())
-    TimeIter = config_container[ZONE_0]->GetRestart_Iter();
+  if (config_container[selected_iZone]->GetTime_Domain() && config_container[selected_iZone]->GetRestart())
+    TimeIter = config_container[selected_iZone]->GetRestart_Iter();
 
 }
 
@@ -2678,9 +2678,9 @@ void CDriver::PreprocessTurbomachinery(CConfig** config, CGeometry**** geometry,
 
   unsigned short donorZone,targetZone, nMarkerInt, iMarkerInt;
   unsigned short nSpanMax = 0;
-  bool restart   = (config[ZONE_0]->GetRestart() || config[ZONE_0]->GetRestart_Flow());
-  mixingplane = config[ZONE_0]->GetBoolMixingPlaneInterface();
-  bool discrete_adjoint = config[ZONE_0]->GetDiscrete_Adjoint();
+  bool restart   = (config[selected_iZone]->GetRestart() || config[selected_iZone]->GetRestart_Flow());
+  mixingplane = config[selected_iZone]->GetBoolMixingPlaneInterface();
+  bool discrete_adjoint = config[selected_iZone]->GetDiscrete_Adjoint();
   su2double areaIn, areaOut, nBlades, flowAngleIn, flowAngleOut;
 
   /*--- Create turbovertex structure ---*/
@@ -2694,7 +2694,7 @@ void CDriver::PreprocessTurbomachinery(CConfig** config, CGeometry**** geometry,
         nSpanMax = config[iZone]->GetnSpanWiseSections();
       }
 
-      config[ZONE_0]->SetnSpan_iZones(config[iZone]->GetnSpanWiseSections(), iZone);
+      config[selected_iZone]->SetnSpan_iZones(config[iZone]->GetnSpanWiseSections(), iZone);
 
       geometry[iZone][INST_0][MESH_0]->SetTurboVertex(config[iZone], iZone, INFLOW, true);
       geometry[iZone][INST_0][MESH_0]->SetTurboVertex(config[iZone], iZone, OUTFLOW, true);
@@ -2737,13 +2737,13 @@ void CDriver::PreprocessTurbomachinery(CConfig** config, CGeometry**** geometry,
 
   if (rank == MASTER_NODE) cout << "Transfer average geometric quantities to zone 0." << endl;
   for (iZone = 1; iZone < nZone; iZone++) {
-    interface[iZone][ZONE_0]->GatherAverageTurboGeoValues(geometry[iZone][INST_0][MESH_0],geometry[ZONE_0][INST_0][MESH_0], iZone);
+    interface[iZone][selected_iZone]->GatherAverageTurboGeoValues(geometry[iZone][INST_0][MESH_0],geometry[selected_iZone][INST_0][MESH_0], iZone);
   }
 
   /*--- Transfer number of blade to ZONE_0 to correctly compute turbo performance---*/
   for (iZone = 1; iZone < nZone; iZone++) {
     nBlades = config[iZone]->GetnBlades(iZone);
-    config[ZONE_0]->SetnBlades(iZone, nBlades);
+    config[selected_iZone]->SetnBlades(iZone, nBlades);
   }
 
   if (rank == MASTER_NODE){
@@ -2809,7 +2809,7 @@ void CDriver::PrintDirectResidual(RECORDING kind_recording) {
 
   if (rank != MASTER_NODE || kind_recording != RECORDING::SOLUTION_VARIABLES) return;
 
-  const bool multizone = config_container[ZONE_0]->GetMultizone_Problem();
+  const bool multizone = config_container[selected_iZone]->GetMultizone_Problem();
 
   /*--- Helper lambda func to return lenghty [iVar][iZone] string.  ---*/
   auto iVar_iZone2string = [&](unsigned short ivar, unsigned short izone) {
@@ -2822,7 +2822,7 @@ void CDriver::PrintDirectResidual(RECORDING kind_recording) {
 
   const unsigned short fieldWidth = 15;
   PrintingToolbox::CTablePrinter RMSTable(&std::cout);
-  RMSTable.SetPrecision(config_container[ZONE_0]->GetOutput_Precision());
+  RMSTable.SetPrecision(config_container[selected_iZone]->GetOutput_Precision());
 
   /*--- The CTablePrinter requires two sweeps:
     *--- 0. Add the colum names (addVals=0=false) plus CTablePrinter.PrintHeader()
@@ -2920,7 +2920,7 @@ void CDriver::PrintDirectResidual(RECORDING kind_recording) {
 }
 
 void CDriver::RampTurbomachineryValues(unsigned long iter) {
-  auto* config = config_container[ZONE_0];
+  auto* config = config_container[selected_iZone];
 
   /*--- ROTATING FRAME Ramp: Compute the updated rotational velocity. ---*/
   if (config->GetGrid_Movement() && config->GetRampRotatingFrame()) {
@@ -2952,8 +2952,8 @@ void CDriver::RampTurbomachineryValues(unsigned long iter) {
       }
 
       for (auto iZone = 1u; iZone < nZone; iZone++) {
-        interface_container[iZone][ZONE_0]->GatherAverageTurboGeoValues(
-            geometry_container[iZone][INST_0][MESH_0], geometry_container[ZONE_0][INST_0][MESH_0], iZone);
+        interface_container[iZone][selected_iZone]->GatherAverageTurboGeoValues(
+            geometry_container[iZone][INST_0][MESH_0], geometry_container[selected_iZone][INST_0][MESH_0], iZone);
       }
     }
   }
@@ -2996,7 +2996,7 @@ void CDriver::RampTurbomachineryValues(unsigned long iter) {
 }
 
 CFluidDriver::CFluidDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator) : CDriver(confFile, val_nZone, MPICommunicator, false) {
-  Max_Iter = config_container[ZONE_0]->GetnInner_Iter();
+  Max_Iter = config_container[selected_iZone]->GetnInner_Iter();
 }
 
 CFluidDriver::~CFluidDriver() = default;
@@ -3024,7 +3024,7 @@ void CFluidDriver::StartSolver(){
     /*--- For the Disc.Adj. of a case with (rigidly) moving grid, the appropriate
           mesh cordinates are read from the restart files. ---*/
     if (!fem_solver &&
-        !(config_container[ZONE_0]->GetGrid_Movement() && config_container[ZONE_0]->GetDiscrete_Adjoint())) {
+        !(config_container[selected_iZone]->GetGrid_Movement() && config_container[selected_iZone]->GetDiscrete_Adjoint())) {
       DynamicMeshUpdate(Iter);
     }
 
@@ -3037,7 +3037,7 @@ void CFluidDriver::StartSolver(){
     Update();
 
     /*--- Terminate the simulation if only the Jacobian must be computed. ---*/
-    if (config_container[ZONE_0]->GetJacobian_Spatial_Discretization_Only()) break;
+    if (config_container[selected_iZone]->GetJacobian_Spatial_Discretization_Only()) break;
 
     /*--- Monitor the computations after each iteration. ---*/
 
@@ -3231,7 +3231,7 @@ CHBDriver::CHBDriver(char* confFile,
         MPICommunicator) {
   unsigned short kInst;
 
-  nInstHB = nInst[ZONE_0];
+  nInstHB = nInst[selected_iZone];
 
   /*--- allocate dynamic memory for the Harmonic Balance operator ---*/
   D = new su2double*[nInstHB];
@@ -3254,17 +3254,17 @@ void CHBDriver::Run() {
    all zones before beginning the iteration. ---*/
 
   for (iInst = 0; iInst < nInstHB; iInst++)
-    iteration_container[ZONE_0][iInst]->Preprocess(output_container[ZONE_0], integration_container, geometry_container,
+    iteration_container[selected_iZone][iInst]->Preprocess(output_container[selected_iZone], integration_container, geometry_container,
         solver_container, numerics_container, config_container,
         surface_movement, grid_movement, FFDBox, ZONE_0, iInst);
 
   for (iInst = 0; iInst < nInstHB; iInst++)
-    iteration_container[ZONE_0][iInst]->Iterate(output_container[ZONE_0], integration_container, geometry_container,
+    iteration_container[selected_iZone][iInst]->Iterate(output_container[selected_iZone], integration_container, geometry_container,
         solver_container, numerics_container, config_container,
         surface_movement, grid_movement, FFDBox, ZONE_0, iInst);
 
   for (iInst = 0; iInst < nInstHB; iInst++)
-    iteration_container[ZONE_0][iInst]->Monitor(output_container[ZONE_0], integration_container, geometry_container,
+    iteration_container[selected_iZone][iInst]->Monitor(output_container[selected_iZone], integration_container, geometry_container,
         solver_container, numerics_container, config_container,
         surface_movement, grid_movement, FFDBox, ZONE_0, iInst);
 
@@ -3279,7 +3279,7 @@ void CHBDriver::Update() {
   }
 
   /*--- Precondition the harmonic balance source terms ---*/
-  if (config_container[ZONE_0]->GetHB_Precondition() == YES) {
+  if (config_container[selected_iZone]->GetHB_Precondition() == YES) {
     StabilizeHarmonicBalance();
 
   }
@@ -3287,7 +3287,7 @@ void CHBDriver::Update() {
   for (iInst = 0; iInst < nInstHB; iInst++) {
 
     /*--- Update the harmonic balance terms across all zones ---*/
-    iteration_container[ZONE_0][iInst]->Update(output_container[ZONE_0], integration_container, geometry_container,
+    iteration_container[selected_iZone][iInst]->Update(output_container[selected_iZone], integration_container, geometry_container,
         solver_container, numerics_container, config_container,
         surface_movement, grid_movement, FFDBox, ZONE_0, iInst);
 
@@ -3298,15 +3298,15 @@ void CHBDriver::Update() {
 void CHBDriver::SetHarmonicBalance(unsigned short iInst) {
 
   unsigned short iVar, jInst, iMGlevel;
-  unsigned short nVar = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetnVar();
+  unsigned short nVar = solver_container[selected_iZone][INST_0][MESH_0][FLOW_SOL]->GetnVar();
   unsigned long iPoint;
-  bool implicit = (config_container[ZONE_0]->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
-  bool adjoint = (config_container[ZONE_0]->GetContinuous_Adjoint());
+  bool implicit = (config_container[selected_iZone]->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
+  bool adjoint = (config_container[selected_iZone]->GetContinuous_Adjoint());
   if (adjoint) {
-    implicit = (config_container[ZONE_0]->GetKind_TimeIntScheme_AdjFlow() == EULER_IMPLICIT);
+    implicit = (config_container[selected_iZone]->GetKind_TimeIntScheme_AdjFlow() == EULER_IMPLICIT);
   }
 
-  unsigned long InnerIter = config_container[ZONE_0]->GetInnerIter();
+  unsigned long InnerIter = config_container[selected_iZone]->GetInnerIter();
 
   /*--- Retrieve values from the config file ---*/
   auto *U = new su2double[nVar];
@@ -3317,20 +3317,20 @@ void CHBDriver::SetHarmonicBalance(unsigned short iInst) {
   su2double deltaU, deltaPsi;
 
   /*--- Compute period of oscillation ---*/
-  su2double period = config_container[ZONE_0]->GetHarmonicBalance_Period();
+  su2double period = config_container[selected_iZone]->GetHarmonicBalance_Period();
 
   /*--- Non-dimensionalize the input period, if necessary.  */
-  period /= config_container[ZONE_0]->GetTime_Ref();
+  period /= config_container[selected_iZone]->GetTime_Ref();
 
   if (InnerIter == 0)
     ComputeHBOperator();
 
   /*--- Compute various source terms for explicit direct, implicit direct, and adjoint problems ---*/
   /*--- Loop over all grid levels ---*/
-  for (iMGlevel = 0; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++) {
+  for (iMGlevel = 0; iMGlevel <= config_container[selected_iZone]->GetnMGLevels(); iMGlevel++) {
 
     /*--- Loop over each node in the volume mesh ---*/
-    for (iPoint = 0; iPoint < geometry_container[ZONE_0][iInst][iMGlevel]->GetnPoint(); iPoint++) {
+    for (iPoint = 0; iPoint < geometry_container[selected_iZone][iInst][iMGlevel]->GetnPoint(); iPoint++) {
 
       for (iVar = 0; iVar < nVar; iVar++) {
         Source[iVar] = 0.0;
@@ -3343,11 +3343,11 @@ void CHBDriver::SetHarmonicBalance(unsigned short iInst) {
         for (iVar = 0; iVar < nVar; iVar++) {
 
           if (!adjoint) {
-            U[iVar] = solver_container[ZONE_0][jInst][iMGlevel][FLOW_SOL]->GetNodes()->GetSolution(iPoint, iVar);
+            U[iVar] = solver_container[selected_iZone][jInst][iMGlevel][FLOW_SOL]->GetNodes()->GetSolution(iPoint, iVar);
             Source[iVar] += U[iVar]*D[iInst][jInst];
 
             if (implicit) {
-              U_old[iVar] = solver_container[ZONE_0][jInst][iMGlevel][FLOW_SOL]->GetNodes()->GetSolution_Old(iPoint, iVar);
+              U_old[iVar] = solver_container[selected_iZone][jInst][iMGlevel][FLOW_SOL]->GetNodes()->GetSolution_Old(iPoint, iVar);
               deltaU = U[iVar] - U_old[iVar];
               Source[iVar] += deltaU*D[iInst][jInst];
             }
@@ -3355,11 +3355,11 @@ void CHBDriver::SetHarmonicBalance(unsigned short iInst) {
           }
 
           else {
-            Psi[iVar] = solver_container[ZONE_0][jInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->GetSolution(iPoint, iVar);
+            Psi[iVar] = solver_container[selected_iZone][jInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->GetSolution(iPoint, iVar);
             Source[iVar] += Psi[iVar]*D[jInst][iInst];
 
             if (implicit) {
-              Psi_old[iVar] = solver_container[ZONE_0][jInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->GetSolution_Old(iPoint, iVar);
+              Psi_old[iVar] = solver_container[selected_iZone][jInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->GetSolution_Old(iPoint, iVar);
               deltaPsi = Psi[iVar] - Psi_old[iVar];
               Source[iVar] += deltaPsi*D[jInst][iInst];
             }
@@ -3369,10 +3369,10 @@ void CHBDriver::SetHarmonicBalance(unsigned short iInst) {
         /*--- Store sources for current row ---*/
         for (iVar = 0; iVar < nVar; iVar++) {
           if (!adjoint) {
-            solver_container[ZONE_0][iInst][iMGlevel][FLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iVar]);
+            solver_container[selected_iZone][iInst][iMGlevel][FLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iVar]);
           }
           else {
-            solver_container[ZONE_0][iInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iVar]);
+            solver_container[selected_iZone][iInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iVar]);
           }
         }
 
@@ -3381,29 +3381,29 @@ void CHBDriver::SetHarmonicBalance(unsigned short iInst) {
   }
 
   /*--- Source term for a turbulence model ---*/
-  if (config_container[ZONE_0]->GetKind_Solver() == MAIN_SOLVER::RANS) {
+  if (config_container[selected_iZone]->GetKind_Solver() == MAIN_SOLVER::RANS) {
 
     /*--- Extra variables needed if we have a turbulence model. ---*/
-    unsigned short nVar_Turb = solver_container[ZONE_0][INST_0][MESH_0][TURB_SOL]->GetnVar();
+    unsigned short nVar_Turb = solver_container[selected_iZone][INST_0][MESH_0][TURB_SOL]->GetnVar();
     auto *U_Turb = new su2double[nVar_Turb];
     auto *Source_Turb = new su2double[nVar_Turb];
 
     /*--- Loop over only the finest mesh level (turbulence is always solved
      on the original grid only). ---*/
-    for (iPoint = 0; iPoint < geometry_container[ZONE_0][INST_0][MESH_0]->GetnPoint(); iPoint++) {
+    for (iPoint = 0; iPoint < geometry_container[selected_iZone][INST_0][MESH_0]->GetnPoint(); iPoint++) {
       for (iVar = 0; iVar < nVar_Turb; iVar++) Source_Turb[iVar] = 0.0;
       for (jInst = 0; jInst < nInstHB; jInst++) {
 
         /*--- Retrieve solution at this node in current zone ---*/
         for (iVar = 0; iVar < nVar_Turb; iVar++) {
-          U_Turb[iVar] = solver_container[ZONE_0][jInst][MESH_0][TURB_SOL]->GetNodes()->GetSolution(iPoint, iVar);
+          U_Turb[iVar] = solver_container[selected_iZone][jInst][MESH_0][TURB_SOL]->GetNodes()->GetSolution(iPoint, iVar);
           Source_Turb[iVar] += U_Turb[iVar]*D[iInst][jInst];
         }
       }
 
       /*--- Store sources for current iZone ---*/
       for (iVar = 0; iVar < nVar_Turb; iVar++)
-        solver_container[ZONE_0][iInst][MESH_0][TURB_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source_Turb[iVar]);
+        solver_container[selected_iZone][iInst][MESH_0][TURB_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source_Turb[iVar]);
     }
 
     delete [] U_Turb;
@@ -3421,9 +3421,9 @@ void CHBDriver::SetHarmonicBalance(unsigned short iInst) {
 void CHBDriver::StabilizeHarmonicBalance() {
 
   unsigned short i, j, k, iVar, iInst, jInst, iMGlevel;
-  unsigned short nVar = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetnVar();
+  unsigned short nVar = solver_container[selected_iZone][INST_0][MESH_0][FLOW_SOL]->GetnVar();
   unsigned long iPoint;
-  bool adjoint = (config_container[ZONE_0]->GetContinuous_Adjoint());
+  bool adjoint = (config_container[selected_iZone]->GetContinuous_Adjoint());
 
   /*--- Retrieve values from the config file ---*/
   auto *Source     = new su2double[nInstHB];
@@ -3438,13 +3438,13 @@ void CHBDriver::StabilizeHarmonicBalance() {
   }
 
   /*--- Loop over all grid levels ---*/
-  for (iMGlevel = 0; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++) {
+  for (iMGlevel = 0; iMGlevel <= config_container[selected_iZone]->GetnMGLevels(); iMGlevel++) {
 
     /*--- Loop over each node in the volume mesh ---*/
-    for (iPoint = 0; iPoint < geometry_container[ZONE_0][INST_0][iMGlevel]->GetnPoint(); iPoint++) {
+    for (iPoint = 0; iPoint < geometry_container[selected_iZone][INST_0][iMGlevel]->GetnPoint(); iPoint++) {
 
       /*--- Get time step for current node ---*/
-      Delta = solver_container[ZONE_0][INST_0][iMGlevel][FLOW_SOL]->GetNodes()->GetDelta_Time(iPoint);
+      Delta = solver_container[selected_iZone][INST_0][iMGlevel][FLOW_SOL]->GetNodes()->GetDelta_Time(iPoint);
 
       /*--- Setup stabilization matrix for this node ---*/
       for (iInst = 0; iInst < nInstHB; iInst++) {
@@ -3543,7 +3543,7 @@ void CHBDriver::StabilizeHarmonicBalance() {
 
         /*--- Get current source terms (not yet preconditioned) and zero source array to prepare preconditioning ---*/
         for (iInst = 0; iInst < nInstHB; iInst++) {
-          Source_old[iInst] = solver_container[ZONE_0][iInst][iMGlevel][FLOW_SOL]->GetNodes()->GetHarmonicBalance_Source(iPoint, iVar);
+          Source_old[iInst] = solver_container[selected_iZone][iInst][iMGlevel][FLOW_SOL]->GetNodes()->GetHarmonicBalance_Source(iPoint, iVar);
           Source[iInst] = 0;
         }
 
@@ -3555,10 +3555,10 @@ void CHBDriver::StabilizeHarmonicBalance() {
 
           /*--- Store updated source terms for current node ---*/
           if (!adjoint) {
-            solver_container[ZONE_0][iInst][iMGlevel][FLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iInst]);
+            solver_container[selected_iZone][iInst][iMGlevel][FLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iInst]);
           }
           else {
-            solver_container[ZONE_0][iInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iInst]);
+            solver_container[selected_iZone][iInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iInst]);
           }
         }
 
@@ -3594,15 +3594,15 @@ void CHBDriver::ComputeHBOperator() {
   }
 
   /*--- Get simualation period from config file ---*/
-  su2double Period = config_container[ZONE_0]->GetHarmonicBalance_Period();
+  su2double Period = config_container[selected_iZone]->GetHarmonicBalance_Period();
 
   /*--- Non-dimensionalize the input period, if necessary.      */
-  Period /= config_container[ZONE_0]->GetTime_Ref();
+  Period /= config_container[selected_iZone]->GetTime_Ref();
 
   /*--- Build the array containing the selected frequencies to solve ---*/
   for (iInst = 0; iInst < nInstHB; iInst++) {
-    Omega_HB[iInst]  = config_container[ZONE_0]->GetOmega_HB()[iInst];
-    Omega_HB[iInst] /= config_container[ZONE_0]->GetOmega_Ref(); //TODO: check
+    Omega_HB[iInst]  = config_container[selected_iZone]->GetOmega_HB()[iInst];
+    Omega_HB[iInst] /= config_container[selected_iZone]->GetOmega_Ref(); //TODO: check
   }
 
   /*--- Build the diagonal matrix of the frequencies DD ---*/
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index ff07e7d1e48..603e2f734f8 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -391,14 +391,14 @@ vector<passivedouble> CDriverBase::GetMarkerVertexNormals(unsigned short iMarker
 }
 
 void CDriverBase::CommunicateMeshDisplacements() {
-  solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->InitiateComms(main_geometry, main_config, MESH_DISPLACEMENTS);
-  solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->CompleteComms(main_geometry, main_config, MESH_DISPLACEMENTS);
+  solver_container[selected_iZone][INST_0][MESH_0][MESH_SOL]->InitiateComms(main_geometry, main_config, MESH_DISPLACEMENTS);
+  solver_container[selected_iZone][INST_0][MESH_0][MESH_SOL]->CompleteComms(main_geometry, main_config, MESH_DISPLACEMENTS);
 }
 
 map<string, unsigned short> CDriverBase::GetSolverIndices() const {
   map<string, unsigned short> indexMap;
   for (auto iSol = 0u; iSol < MAX_SOLS; iSol++) {
-    const auto* solver = solver_container[ZONE_0][INST_0][MESH_0][iSol];
+    const auto* solver = solver_container[selected_iZone][INST_0][MESH_0][iSol];
     if (solver != nullptr) {
       if (solver->GetSolverName().empty()) SU2_MPI::Error("Solver name was not defined.", CURRENT_FUNCTION);
       indexMap[solver->GetSolverName()] = iSol;
@@ -408,7 +408,7 @@ map<string, unsigned short> CDriverBase::GetSolverIndices() const {
 }
 
 std::map<string, unsigned short> CDriverBase::GetFEASolutionIndices() const {
-  if (solver_container[ZONE_0][INST_0][MESH_0][FEA_SOL] == nullptr) {
+  if (solver_container[selected_iZone][INST_0][MESH_0][FEA_SOL] == nullptr) {
     SU2_MPI::Error("The FEA solver does not exist.", CURRENT_FUNCTION);
   }
   const auto nDim = main_geometry->GetnDim();
@@ -429,7 +429,7 @@ std::map<string, unsigned short> CDriverBase::GetFEASolutionIndices() const {
 }
 
 map<string, unsigned short> CDriverBase::GetPrimitiveIndices() const {
-  if (solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL] == nullptr) {
+  if (solver_container[selected_iZone][INST_0][MESH_0][FLOW_SOL] == nullptr) {
     SU2_MPI::Error("The flow solver does not exist.", CURRENT_FUNCTION);
   }
   return PrimitiveNameToIndexMap(CPrimitiveIndices<unsigned short>(
diff --git a/SU2_CFD/src/drivers/CMultizoneDriver.cpp b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
index 61f59223fcf..9c8039db782 100644
--- a/SU2_CFD/src/drivers/CMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
@@ -248,7 +248,7 @@ void CMultizoneDriver::Preprocess(unsigned long TimeIter) {
   }
 
   /*--- Ramp turbo values for unsteady problems here, otherwise do it over outer iterations. ---*/
-  if (config_container[ZONE_0]->GetTime_Domain()) {
+  if (config_container[selected_iZone]->GetTime_Domain()) {
     RampTurbomachineryValues(TimeIter);
   }
 
@@ -294,7 +294,7 @@ void CMultizoneDriver::RunGaussSeidel() {
   for (auto iOuter_Iter = 0ul; iOuter_Iter < driver_config->GetnOuter_Iter(); iOuter_Iter++) {
 
     /*--- Ramp turbo values for steady problems here, otherwise do it over time steps. ---*/
-    if (!config_container[ZONE_0]->GetTime_Domain()) {
+    if (!config_container[selected_iZone]->GetTime_Domain()) {
       RampTurbomachineryValues(iOuter_Iter);
     }
 
@@ -352,7 +352,7 @@ void CMultizoneDriver::RunJacobi() {
   for (auto iOuter_Iter = 0ul; iOuter_Iter < driver_config->GetnOuter_Iter(); iOuter_Iter++){
 
     /*--- Ramp turbo values for steady problems here, otherwise do it over time steps. ---*/
-    if (!config_container[ZONE_0]->GetTime_Domain()) {
+    if (!config_container[selected_iZone]->GetTime_Domain()) {
       RampTurbomachineryValues(iOuter_Iter);
     }
 
@@ -407,7 +407,7 @@ void CMultizoneDriver::RunJacobi() {
 void CMultizoneDriver::Corrector(unsigned short val_iZone) {
 
   if (config_container[val_iZone]->GetRelaxation())
-    iteration_container[val_iZone][INST_0]->Relaxation(output_container[ZONE_0], integration_container,
+    iteration_container[val_iZone][INST_0]->Relaxation(output_container[selected_iZone], integration_container,
                                             geometry_container, solver_container, numerics_container, config_container,
                                             surface_movement, grid_movement, FFDBox, val_iZone, INST_0);
 }
@@ -493,7 +493,7 @@ void CMultizoneDriver::Output(unsigned long TimeIter) {
 
     UsedTimeOutput += StopTime-StartTime;
     OutputCount++;
-    BandwidthSum = config_container[ZONE_0]->GetRestart_Bandwidth_Agg();
+    BandwidthSum = config_container[selected_iZone]->GetRestart_Bandwidth_Agg();
 
     StartTime = SU2_MPI::Wtime();
 
@@ -632,8 +632,8 @@ void CMultizoneDriver::SetMixingPlane(unsigned short donorZone) {
 
 void CMultizoneDriver::SetTurboPerformance() {
   for (auto donorZone = 1u; donorZone < nZone; donorZone++) {
-    interface_container[donorZone][ZONE_0]->GatherAverageValues(solver_container[donorZone][INST_0][MESH_0][FLOW_SOL],
-                                                                solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL],
+    interface_container[donorZone][selected_iZone]->GatherAverageValues(solver_container[donorZone][INST_0][MESH_0][FLOW_SOL],
+                                                                solver_container[selected_iZone][INST_0][MESH_0][FLOW_SOL],
                                                                 donorZone);
   }
 }
@@ -688,5 +688,5 @@ bool CMultizoneDriver::Monitor(unsigned long TimeIter){
 }
 
 bool CMultizoneDriver::GetTimeConvergence() const{
-  return output_container[ZONE_0]->GetCauchyCorrectedTimeConvergence(config_container[ZONE_0]);
+  return output_container[selected_iZone]->GetCauchyCorrectedTimeConvergence(config_container[selected_iZone]);
 }
diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index 3626baaae5a..b5b8c80d581 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -62,15 +62,15 @@ void CDriver::PreprocessPythonInterface(CConfig** config, CGeometry**** geometry
 /* Functions to obtain global parameters from SU2 (time steps, delta t, etc.)   */
 //////////////////////////////////////////////////////////////////////////////////
 
-unsigned long CDriver::GetNumberTimeIter() const { return config_container[ZONE_0]->GetnTime_Iter(); }
+unsigned long CDriver::GetNumberTimeIter() const { return config_container[selected_iZone]->GetnTime_Iter(); }
 
 unsigned long CDriver::GetTimeIter() const { return TimeIter; }
 
 passivedouble CDriver::GetUnsteadyTimeStep() const {
-  return SU2_TYPE::GetValue(config_container[ZONE_0]->GetTime_Step());
+  return SU2_TYPE::GetValue(config_container[selected_iZone]->GetTime_Step());
 }
 
-string CDriver::GetSurfaceFileName() const { return config_container[ZONE_0]->GetSurfCoeff_FileName(); }
+string CDriver::GetSurfaceFileName() const { return config_container[selected_iZone]->GetSurfCoeff_FileName(); }
 
 ////////////////////////////////////////////////////////////////////////////////
 /* Functions related to the management of markers                             */
@@ -78,12 +78,12 @@ string CDriver::GetSurfaceFileName() const { return config_container[ZONE_0]->Ge
 
 void CDriver::SetHeatSourcePosition(passivedouble alpha, passivedouble pos_x, passivedouble pos_y,
                                      passivedouble pos_z) {
-  CSolver* solver = solver_container[ZONE_0][INST_0][MESH_0][RAD_SOL];
+  CSolver* solver = solver_container[selected_iZone][INST_0][MESH_0][RAD_SOL];
 
-  config_container[ZONE_0]->SetHeatSource_Rot_Z(alpha);
-  config_container[ZONE_0]->SetHeatSource_Center(pos_x, pos_y, pos_z);
+  config_container[selected_iZone]->SetHeatSource_Rot_Z(alpha);
+  config_container[selected_iZone]->SetHeatSource_Center(pos_x, pos_y, pos_z);
 
-  solver->SetVolumetricHeatSource(geometry_container[ZONE_0][INST_0][MESH_0], config_container[ZONE_0]);
+  solver->SetVolumetricHeatSource(geometry_container[selected_iZone][INST_0][MESH_0], config_container[selected_iZone]);
 }
 
 void CDriver::SetInletAngle(unsigned short iMarker, passivedouble alpha) {
@@ -91,9 +91,9 @@ void CDriver::SetInletAngle(unsigned short iMarker, passivedouble alpha) {
 
   unsigned long iVertex;
 
-  for (iVertex = 0; iVertex < geometry_container[ZONE_0][INST_0][MESH_0]->nVertex[iMarker]; iVertex++) {
-    solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->SetInlet_FlowDir(iMarker, iVertex, 0, cos(alpha_rad));
-    solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->SetInlet_FlowDir(iMarker, iVertex, 1, sin(alpha_rad));
+  for (iVertex = 0; iVertex < geometry_container[selected_iZone][INST_0][MESH_0]->nVertex[iMarker]; iVertex++) {
+    solver_container[selected_iZone][INST_0][MESH_0][FLOW_SOL]->SetInlet_FlowDir(iMarker, iVertex, 0, cos(alpha_rad));
+    solver_container[selected_iZone][INST_0][MESH_0][FLOW_SOL]->SetInlet_FlowDir(iMarker, iVertex, 1, sin(alpha_rad));
   }
 }
 
@@ -106,22 +106,22 @@ void CSinglezoneDriver::SetInitialMesh() {
 
   SU2_OMP_PARALLEL {
     for (iMesh = 0u; iMesh <= main_config->GetnMGLevels(); iMesh++) {
-      SU2_OMP_FOR_STAT(roundUpDiv(geometry_container[ZONE_0][INST_0][iMesh]->GetnPoint(), omp_get_max_threads()))
-      for (auto iPoint = 0ul; iPoint < geometry_container[ZONE_0][INST_0][iMesh]->GetnPoint(); iPoint++) {
+      SU2_OMP_FOR_STAT(roundUpDiv(geometry_container[selected_iZone][INST_0][iMesh]->GetnPoint(), omp_get_max_threads()))
+      for (auto iPoint = 0ul; iPoint < geometry_container[selected_iZone][INST_0][iMesh]->GetnPoint(); iPoint++) {
         /*--- Overwrite fictitious velocities. ---*/
         su2double Grid_Vel[3] = {0.0, 0.0, 0.0};
 
         /*--- Set the grid velocity for this coarse node. ---*/
-        geometry_container[ZONE_0][INST_0][iMesh]->nodes->SetGridVel(iPoint, Grid_Vel);
+        geometry_container[selected_iZone][INST_0][iMesh]->nodes->SetGridVel(iPoint, Grid_Vel);
       }
       END_SU2_OMP_FOR
       /*--- Push back the volume. ---*/
-      geometry_container[ZONE_0][INST_0][iMesh]->nodes->SetVolume_n();
-      geometry_container[ZONE_0][INST_0][iMesh]->nodes->SetVolume_nM1();
+      geometry_container[selected_iZone][INST_0][iMesh]->nodes->SetVolume_n();
+      geometry_container[selected_iZone][INST_0][iMesh]->nodes->SetVolume_nM1();
     }
     /*--- Push back the solution so that there is no fictitious velocity at the next step. ---*/
-    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->Set_Solution_time_n();
-    solver_container[ZONE_0][INST_0][MESH_0][MESH_SOL]->GetNodes()->Set_Solution_time_n1();
+    solver_container[selected_iZone][INST_0][MESH_0][MESH_SOL]->GetNodes()->Set_Solution_time_n();
+    solver_container[selected_iZone][INST_0][MESH_0][MESH_SOL]->GetNodes()->Set_Solution_time_n1();
   }
   END_SU2_OMP_PARALLEL
 }

From 930a25e35c17097d3a1e04ee3cf5f73f39e04554 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 29 Apr 2023 14:45:22 -0700
Subject: [PATCH 417/656] using the surface averages in a discrete adjoint case

---
 Common/include/CConfig.hpp                                   | 1 -
 SU2_CFD/src/output/CFlowOutput.cpp                           | 2 +-
 .../DAspecies3_primitiveVenturi.cfg                          | 5 +++++
 TestCases/tutorials.py                                       | 1 -
 4 files changed, 6 insertions(+), 3 deletions(-)

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index 626b8c30f9a..f8f7d01e73e 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -8658,7 +8658,6 @@ class CConfig {
   unsigned short GetKind_Average(void) const { return Kind_Average; }
 
   /*!
-   *
    * \brief Get the direct differentation method.
    * \return direct differentiation method.
    */
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index 25de58c53fa..5a3664a0264 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -739,8 +739,8 @@ void CFlowOutput::SetAnalyzeSurfaceSpeciesVariance(const CSolver* const*solver,
   for (unsigned short iMarker_Analyze = 0; iMarker_Analyze < nMarker_Analyze; iMarker_Analyze++) {
     su2double SpeciesVariance = Surface_SpeciesVariance_Total[iMarker_Analyze];
     SetHistoryOutputPerSurfaceValue("SURFACE_SPECIES_VARIANCE", SpeciesVariance, iMarker_Analyze);
+    config->SetSurface_Species_Variance(iMarker_Analyze, SpeciesVariance);
     Tot_Surface_SpeciesVariance += SpeciesVariance;
-    config->SetSurface_Species_Variance(iMarker_Analyze, Tot_Surface_SpeciesVariance);
   }
   SetHistoryOutputValue("SURFACE_SPECIES_VARIANCE", Tot_Surface_SpeciesVariance);
 }
diff --git a/TestCases/species_transport/venturi_primitive_3species/DAspecies3_primitiveVenturi.cfg b/TestCases/species_transport/venturi_primitive_3species/DAspecies3_primitiveVenturi.cfg
index f7c31afcc12..f58be145625 100644
--- a/TestCases/species_transport/venturi_primitive_3species/DAspecies3_primitiveVenturi.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/DAspecies3_primitiveVenturi.cfg
@@ -14,6 +14,11 @@
 SOLVER= INC_RANS
 KIND_TURB_MODEL= SST
 %
+CUSTOM_OUTPUTS= 'avg_species_0 : AreaAvg{SPECIES[0]}[outlet];\
+                 avg_species_1 : AreaAvg{SPECIES[1]}[outlet];\
+                 var_species : AreaAvg{pow(SPECIES[0] - avg_species_0, 2) +\
+                                       pow(SPECIES[1] - avg_species_1, 2)}[outlet]'
+CUSTOM_OBJFUNC= 'var_species'
 OBJECTIVE_FUNCTION= SURFACE_SPECIES_VARIANCE
 OBJECTIVE_WEIGHT= 1.0
 %
diff --git a/TestCases/tutorials.py b/TestCases/tutorials.py
index 0b730dcddda..3759a48e782 100644
--- a/TestCases/tutorials.py
+++ b/TestCases/tutorials.py
@@ -92,7 +92,6 @@ def main():
     species3_primitiveVenturi.test_vals = [-6.074971, -5.306648, -5.150960, -5.959416, -1.625107, -6.343704, -6.460033, 5.000000, -0.808413, 5.000000, -2.325029, 5.000000, -0.274923, 1.646091, 0.499028, 0.601019, 0.546044]
     test_list.append(species3_primitiveVenturi)
 
-
     # 3 species (2 eq) primitive venturi mixing
     DAspecies3_primitiveVenturi           = TestCase('DAspecies3_primitiveVenturi')
     DAspecies3_primitiveVenturi.cfg_dir   = "../Tutorials/incompressible_flow/Inc_Species_Transport"

From c9d656cda9315a605367b7b11cf295ac6718dec9 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Sat, 29 Apr 2023 15:01:49 -0700
Subject: [PATCH 418/656] Apply suggestions from code review

---
 SU2_CFD/src/output/CFlowOutput.cpp                            | 4 ++--
 SU2_CFD/src/output/COutput.cpp                                | 2 +-
 .../DAspecies3_primitiveVenturi.cfg                           | 2 +-
 3 files changed, 4 insertions(+), 4 deletions(-)

diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index 5a3664a0264..d297ca6fb99 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -798,11 +798,11 @@ void CFlowOutput::ConvertVariableSymbolsToIndices(const CPrimitiveIndices<unsign
     if (output.otherOutputs.back() == nullptr) {
       if (!allowSkip) {
         SU2_MPI::Error("Invalid history output or solver variable (" + var + ") used in function " + output.name +
-                      "\nValid solvers variables:\n" + knownVariables.str(), CURRENT_FUNCTION);
+                       "\nValid solvers variables:\n" + knownVariables.str(), CURRENT_FUNCTION);
       } else {
         if (rank == MASTER_NODE) {
           std::cout << "Info: Ignoring function " + output.name + " because it may be used by the primal/adjoint "
-                        "solver.\n      If the function is ignored twice it is invalid." << std::endl;
+                       "solver.\n      If the function is ignored twice it is invalid." << std::endl;
         }
         output.skip = true;
         break;
diff --git a/SU2_CFD/src/output/COutput.cpp b/SU2_CFD/src/output/COutput.cpp
index 90d9f3ef925..cb689a0d48a 100644
--- a/SU2_CFD/src/output/COutput.cpp
+++ b/SU2_CFD/src/output/COutput.cpp
@@ -2310,7 +2310,7 @@ void COutput::ComputeSimpleCustomOutputs(const CConfig *config) {
           } else {
             if (rank == MASTER_NODE) {
               std::cout << "Info: Ignoring function " + output.name + " because it may be used by the primal/adjoint "
-                          "solver.\n      If the function is ignored twice it is invalid." << std::endl;
+                           "solver.\n      If the function is ignored twice it is invalid." << std::endl;
             }
             output.skip = true;
             break;
diff --git a/TestCases/species_transport/venturi_primitive_3species/DAspecies3_primitiveVenturi.cfg b/TestCases/species_transport/venturi_primitive_3species/DAspecies3_primitiveVenturi.cfg
index f58be145625..6ab9176cd75 100644
--- a/TestCases/species_transport/venturi_primitive_3species/DAspecies3_primitiveVenturi.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/DAspecies3_primitiveVenturi.cfg
@@ -19,7 +19,7 @@ CUSTOM_OUTPUTS= 'avg_species_0 : AreaAvg{SPECIES[0]}[outlet];\
                  var_species : AreaAvg{pow(SPECIES[0] - avg_species_0, 2) +\
                                        pow(SPECIES[1] - avg_species_1, 2)}[outlet]'
 CUSTOM_OBJFUNC= 'var_species'
-OBJECTIVE_FUNCTION= SURFACE_SPECIES_VARIANCE
+OBJECTIVE_FUNCTION= CUSTOM_OBJFUNC
 OBJECTIVE_WEIGHT= 1.0
 %
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%

From f2697737a2a7b1f8839fc0ec9fc16ebb7d83a06e Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 29 Apr 2023 17:12:40 -0700
Subject: [PATCH 419/656] fix file name

---
 TestCases/parallel_regression_AD.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index c440361c2f8..8efd8f7a6d7 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -424,7 +424,7 @@ def main():
     # Heat solver unsteady AD
     pywrapper_Unst_Heat_AD = TestCase('pywrapper_Unst_Heat_AD')
     pywrapper_Unst_Heat_AD.cfg_dir = "py_wrapper/custom_heat_flux"
-    pywrapper_Unst_Heat_AD.cfg_file = "run_ad.cfg"
+    pywrapper_Unst_Heat_AD.cfg_file = "run_ad.py"
     pywrapper_Unst_Heat_AD.test_iter = 100
     pywrapper_Unst_Heat_AD.test_vals = [0.776365, 0.776430, 1.000003]
     pywrapper_Unst_Heat_AD.command = TestCase.Command("mpirun -n 2", "python", "run_ad.py")

From fdc15e04abe456d4d2e0dcb7bf8a0aa49745ae0d Mon Sep 17 00:00:00 2001
From: Afshawn Lotfi <me@afshawn.org>
Date: Sun, 30 Apr 2023 01:25:40 +0000
Subject: [PATCH 420/656] Removed changes for non pysu2 functions

---
 .../src/drivers/CDiscAdjMultizoneDriver.cpp   |   8 +-
 SU2_CFD/src/drivers/CDriver.cpp               | 142 +++++++++---------
 SU2_CFD/src/drivers/CMultizoneDriver.cpp      |  16 +-
 3 files changed, 83 insertions(+), 83 deletions(-)

diff --git a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
index 13319167fc6..6277f409b8d 100644
--- a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
@@ -440,7 +440,7 @@ void CDiscAdjMultizoneDriver::Run() {
     /*--- Check for convergence. ---*/
 
     StopCalc = driver_output->GetConvergence() || (iOuterIter == nOuterIter-1) ||
-               ((nZone==1) && output_container[selected_iZone]->GetConvergence());
+               ((nZone==1) && output_container[ZONE_0]->GetConvergence());
 
     /*--- Clear the stored adjoint information to be ready for a new evaluation. ---*/
 
@@ -765,13 +765,13 @@ void CDiscAdjMultizoneDriver::SetObjFunction(RECORDING kind_recording) {
 void CDiscAdjMultizoneDriver::SetAdjObjFunction() {
   su2double seeding = 1.0;
 
-  if (config_container[selected_iZone]->GetTime_Domain()) {
-    const auto IterAvg_Obj = config_container[selected_iZone]->GetIter_Avg_Objective();
+  if (config_container[ZONE_0]->GetTime_Domain()) {
+    const auto IterAvg_Obj = config_container[ZONE_0]->GetIter_Avg_Objective();
     if (TimeIter < IterAvg_Obj) {
       /*--- Default behavior when no window is chosen is to use Square-Windowing, i.e. the numerator equals 1.0 ---*/
       auto windowEvaluator = CWindowingTools();
       const su2double weight =
-          windowEvaluator.GetWndWeight(config_container[selected_iZone]->GetKindWindow(), TimeIter, IterAvg_Obj - 1);
+          windowEvaluator.GetWndWeight(config_container[ZONE_0]->GetKindWindow(), TimeIter, IterAvg_Obj - 1);
       seeding = weight / IterAvg_Obj;
     }
     else {
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index c60a7ba9b0c..07fc5ca3697 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -120,8 +120,8 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
 
   /*--- Retrieve dimension from mesh file ---*/
 
-  nDim = CConfig::GetnDim(config_container[selected_iZone]->GetMesh_FileName(),
-                          config_container[selected_iZone]->GetMesh_FileFormat());
+  nDim = CConfig::GetnDim(config_container[ZONE_0]->GetMesh_FileName(),
+                          config_container[ZONE_0]->GetMesh_FileFormat());
 
   /*--- Output preprocessing ---*/
 
@@ -243,7 +243,7 @@ CDriverBase(confFile, val_nZone, MPICommunicator), StopCalc(false), fsi(false),
     }
   }
 
-  if (config_container[selected_iZone]->GetBoolTurbomachinery()){
+  if (config_container[ZONE_0]->GetBoolTurbomachinery()){
     if (rank == MASTER_NODE)
       cout << endl <<"---------------------- Turbomachinery Preprocessing ---------------------" << endl;
 
@@ -342,7 +342,7 @@ void CDriver::InitializeContainers(){
 
 void CDriver::Finalize() {
 
-  const bool wrt_perf = config_container[selected_iZone]->GetWrt_Performance();
+  const bool wrt_perf = config_container[ZONE_0]->GetWrt_Performance();
 
     /*--- Output some information to the console. ---*/
 
@@ -350,10 +350,10 @@ void CDriver::Finalize() {
 
     /*--- Print out the number of non-physical points and reconstructions ---*/
 
-    if (config_container[selected_iZone]->GetNonphysical_Points() > 0)
-      cout << "Warning: there are " << config_container[selected_iZone]->GetNonphysical_Points() << " non-physical points in the solution." << endl;
-    if (config_container[selected_iZone]->GetNonphysical_Reconstr() > 0)
-      cout << "Warning: " << config_container[selected_iZone]->GetNonphysical_Reconstr() << " reconstructed states for upwinding are non-physical." << endl;
+    if (config_container[ZONE_0]->GetNonphysical_Points() > 0)
+      cout << "Warning: there are " << config_container[ZONE_0]->GetNonphysical_Points() << " non-physical points in the solution." << endl;
+    if (config_container[ZONE_0]->GetNonphysical_Reconstr() > 0)
+      cout << "Warning: " << config_container[ZONE_0]->GetNonphysical_Reconstr() << " reconstructed states for upwinding are non-physical." << endl;
   }
 
   if (rank == MASTER_NODE)
@@ -456,8 +456,8 @@ void CDriver::Finalize() {
   // Note that for now this is called only by a single thread, but all
   // necessary variables have been made thread private for safety (tick/tock)!!
 
-  config_container[selected_iZone]->SetProfilingCSV();
-  config_container[selected_iZone]->GEMMProfilingCSV();
+  config_container[ZONE_0]->SetProfilingCSV();
+  config_container[ZONE_0]->GEMMProfilingCSV();
 
   /*--- Deallocate config container ---*/
   if (config_container!= nullptr) {
@@ -585,14 +585,14 @@ void CDriver::PreprocessInput(CConfig **&config, CConfig *&driver_config) {
 
   /*--- Keep a reference to the main (ZONE 0) config. ---*/
 
-  main_config = config_container[selected_iZone];
+  main_config = config_container[ZONE_0];
 
   /*--- Determine whether or not the FEM solver is used, which decides the type of
    *    geometry classes that are instantiated. Only adapted for single-zone problems ---*/
 
-  fem_solver = config_container[selected_iZone]->GetFEMSolver();
+  fem_solver = config_container[ZONE_0]->GetFEMSolver();
 
-  fsi = config_container[selected_iZone]->GetFSI_Simulation();
+  fsi = config_container[ZONE_0]->GetFSI_Simulation();
 }
 
 void CDriver::InitializeGeometry(CConfig* config, CGeometry **&geometry, bool dummy){
@@ -693,7 +693,7 @@ void CDriver::InitializeGeometry(CConfig* config, CGeometry **&geometry, bool du
 
   /*--- Keep a reference to the main (ZONE_0, INST_0, MESH_0) geometry. ---*/
 
-  main_geometry = geometry_container[selected_iZone][INST_0][MESH_0];
+  main_geometry = geometry_container[ZONE_0][INST_0][MESH_0];
 }
 
 void CDriver::InitializeGeometryFVM(CConfig *config, CGeometry **&geometry) {
@@ -2470,7 +2470,7 @@ void CDriver::InitializeInterface(CConfig **config, CSolver***** solver, CGeomet
           interface_type = FLOW_TRACTION;
           auto nConst = 2;
           bool conservative = config[target]->GetConservativeInterpolation();
-          if(!config[selected_iZone]->GetDiscrete_Adjoint()) {
+          if(!config[ZONE_0]->GetDiscrete_Adjoint()) {
             interface[donor][target] = new CFlowTractionInterface(nDim, nConst, config[donor], conservative);
           } else {
             interface[donor][target] = new CDiscAdjFlowTractionInterface(nDim, nConst, config[donor], conservative);
@@ -2570,7 +2570,7 @@ void CDriver::PreprocessStaticMesh(const CConfig *config, CGeometry** geometry){
         /*--- Set the grid velocities on all multigrid levels for a steadily
            rotating reference frame. ---*/
 
-        for (iMGlevel = 0; iMGlevel <= config_container[selected_iZone]->GetnMGLevels(); iMGlevel++){
+        for (iMGlevel = 0; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++){
           geometry[iMGlevel]->SetRotationalVelocity(config, true);
           geometry[iMGlevel]->SetShroudVelocity(config);
         }
@@ -2588,7 +2588,7 @@ void CDriver::PreprocessStaticMesh(const CConfig *config, CGeometry** geometry){
 
         /*--- Set the translational velocity on all grid levels. ---*/
 
-        for (iMGlevel = 0; iMGlevel <= config_container[selected_iZone]->GetnMGLevels(); iMGlevel++)
+        for (iMGlevel = 0; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++)
           geometry_container[iZone][INST_0][iMGlevel]->SetTranslationalVelocity(config, true);
 
         break;
@@ -2667,8 +2667,8 @@ void CDriver::PreprocessOutput(CConfig **config, CConfig *driver_config, COutput
   }
 
   /*--- Check for an unsteady restart. Update ExtIter if necessary. ---*/
-  if (config_container[selected_iZone]->GetTime_Domain() && config_container[selected_iZone]->GetRestart())
-    TimeIter = config_container[selected_iZone]->GetRestart_Iter();
+  if (config_container[ZONE_0]->GetTime_Domain() && config_container[ZONE_0]->GetRestart())
+    TimeIter = config_container[ZONE_0]->GetRestart_Iter();
 
 }
 
@@ -2678,9 +2678,9 @@ void CDriver::PreprocessTurbomachinery(CConfig** config, CGeometry**** geometry,
 
   unsigned short donorZone,targetZone, nMarkerInt, iMarkerInt;
   unsigned short nSpanMax = 0;
-  bool restart   = (config[selected_iZone]->GetRestart() || config[selected_iZone]->GetRestart_Flow());
-  mixingplane = config[selected_iZone]->GetBoolMixingPlaneInterface();
-  bool discrete_adjoint = config[selected_iZone]->GetDiscrete_Adjoint();
+  bool restart   = (config[ZONE_0]->GetRestart() || config[ZONE_0]->GetRestart_Flow());
+  mixingplane = config[ZONE_0]->GetBoolMixingPlaneInterface();
+  bool discrete_adjoint = config[ZONE_0]->GetDiscrete_Adjoint();
   su2double areaIn, areaOut, nBlades, flowAngleIn, flowAngleOut;
 
   /*--- Create turbovertex structure ---*/
@@ -2694,7 +2694,7 @@ void CDriver::PreprocessTurbomachinery(CConfig** config, CGeometry**** geometry,
         nSpanMax = config[iZone]->GetnSpanWiseSections();
       }
 
-      config[selected_iZone]->SetnSpan_iZones(config[iZone]->GetnSpanWiseSections(), iZone);
+      config[ZONE_0]->SetnSpan_iZones(config[iZone]->GetnSpanWiseSections(), iZone);
 
       geometry[iZone][INST_0][MESH_0]->SetTurboVertex(config[iZone], iZone, INFLOW, true);
       geometry[iZone][INST_0][MESH_0]->SetTurboVertex(config[iZone], iZone, OUTFLOW, true);
@@ -2737,13 +2737,13 @@ void CDriver::PreprocessTurbomachinery(CConfig** config, CGeometry**** geometry,
 
   if (rank == MASTER_NODE) cout << "Transfer average geometric quantities to zone 0." << endl;
   for (iZone = 1; iZone < nZone; iZone++) {
-    interface[iZone][selected_iZone]->GatherAverageTurboGeoValues(geometry[iZone][INST_0][MESH_0],geometry[selected_iZone][INST_0][MESH_0], iZone);
+    interface[iZone][ZONE_0]->GatherAverageTurboGeoValues(geometry[iZone][INST_0][MESH_0],geometry[ZONE_0][INST_0][MESH_0], iZone);
   }
 
   /*--- Transfer number of blade to ZONE_0 to correctly compute turbo performance---*/
   for (iZone = 1; iZone < nZone; iZone++) {
     nBlades = config[iZone]->GetnBlades(iZone);
-    config[selected_iZone]->SetnBlades(iZone, nBlades);
+    config[ZONE_0]->SetnBlades(iZone, nBlades);
   }
 
   if (rank == MASTER_NODE){
@@ -2809,7 +2809,7 @@ void CDriver::PrintDirectResidual(RECORDING kind_recording) {
 
   if (rank != MASTER_NODE || kind_recording != RECORDING::SOLUTION_VARIABLES) return;
 
-  const bool multizone = config_container[selected_iZone]->GetMultizone_Problem();
+  const bool multizone = config_container[ZONE_0]->GetMultizone_Problem();
 
   /*--- Helper lambda func to return lenghty [iVar][iZone] string.  ---*/
   auto iVar_iZone2string = [&](unsigned short ivar, unsigned short izone) {
@@ -2822,7 +2822,7 @@ void CDriver::PrintDirectResidual(RECORDING kind_recording) {
 
   const unsigned short fieldWidth = 15;
   PrintingToolbox::CTablePrinter RMSTable(&std::cout);
-  RMSTable.SetPrecision(config_container[selected_iZone]->GetOutput_Precision());
+  RMSTable.SetPrecision(config_container[ZONE_0]->GetOutput_Precision());
 
   /*--- The CTablePrinter requires two sweeps:
     *--- 0. Add the colum names (addVals=0=false) plus CTablePrinter.PrintHeader()
@@ -2920,7 +2920,7 @@ void CDriver::PrintDirectResidual(RECORDING kind_recording) {
 }
 
 void CDriver::RampTurbomachineryValues(unsigned long iter) {
-  auto* config = config_container[selected_iZone];
+  auto* config = config_container[ZONE_0];
 
   /*--- ROTATING FRAME Ramp: Compute the updated rotational velocity. ---*/
   if (config->GetGrid_Movement() && config->GetRampRotatingFrame()) {
@@ -2952,8 +2952,8 @@ void CDriver::RampTurbomachineryValues(unsigned long iter) {
       }
 
       for (auto iZone = 1u; iZone < nZone; iZone++) {
-        interface_container[iZone][selected_iZone]->GatherAverageTurboGeoValues(
-            geometry_container[iZone][INST_0][MESH_0], geometry_container[selected_iZone][INST_0][MESH_0], iZone);
+        interface_container[iZone][ZONE_0]->GatherAverageTurboGeoValues(
+            geometry_container[iZone][INST_0][MESH_0], geometry_container[ZONE_0][INST_0][MESH_0], iZone);
       }
     }
   }
@@ -2996,7 +2996,7 @@ void CDriver::RampTurbomachineryValues(unsigned long iter) {
 }
 
 CFluidDriver::CFluidDriver(char* confFile, unsigned short val_nZone, SU2_Comm MPICommunicator) : CDriver(confFile, val_nZone, MPICommunicator, false) {
-  Max_Iter = config_container[selected_iZone]->GetnInner_Iter();
+  Max_Iter = config_container[ZONE_0]->GetnInner_Iter();
 }
 
 CFluidDriver::~CFluidDriver() = default;
@@ -3024,7 +3024,7 @@ void CFluidDriver::StartSolver(){
     /*--- For the Disc.Adj. of a case with (rigidly) moving grid, the appropriate
           mesh cordinates are read from the restart files. ---*/
     if (!fem_solver &&
-        !(config_container[selected_iZone]->GetGrid_Movement() && config_container[selected_iZone]->GetDiscrete_Adjoint())) {
+        !(config_container[ZONE_0]->GetGrid_Movement() && config_container[ZONE_0]->GetDiscrete_Adjoint())) {
       DynamicMeshUpdate(Iter);
     }
 
@@ -3037,7 +3037,7 @@ void CFluidDriver::StartSolver(){
     Update();
 
     /*--- Terminate the simulation if only the Jacobian must be computed. ---*/
-    if (config_container[selected_iZone]->GetJacobian_Spatial_Discretization_Only()) break;
+    if (config_container[ZONE_0]->GetJacobian_Spatial_Discretization_Only()) break;
 
     /*--- Monitor the computations after each iteration. ---*/
 
@@ -3231,7 +3231,7 @@ CHBDriver::CHBDriver(char* confFile,
         MPICommunicator) {
   unsigned short kInst;
 
-  nInstHB = nInst[selected_iZone];
+  nInstHB = nInst[ZONE_0];
 
   /*--- allocate dynamic memory for the Harmonic Balance operator ---*/
   D = new su2double*[nInstHB];
@@ -3254,17 +3254,17 @@ void CHBDriver::Run() {
    all zones before beginning the iteration. ---*/
 
   for (iInst = 0; iInst < nInstHB; iInst++)
-    iteration_container[selected_iZone][iInst]->Preprocess(output_container[selected_iZone], integration_container, geometry_container,
+    iteration_container[ZONE_0][iInst]->Preprocess(output_container[ZONE_0], integration_container, geometry_container,
         solver_container, numerics_container, config_container,
         surface_movement, grid_movement, FFDBox, ZONE_0, iInst);
 
   for (iInst = 0; iInst < nInstHB; iInst++)
-    iteration_container[selected_iZone][iInst]->Iterate(output_container[selected_iZone], integration_container, geometry_container,
+    iteration_container[ZONE_0][iInst]->Iterate(output_container[ZONE_0], integration_container, geometry_container,
         solver_container, numerics_container, config_container,
         surface_movement, grid_movement, FFDBox, ZONE_0, iInst);
 
   for (iInst = 0; iInst < nInstHB; iInst++)
-    iteration_container[selected_iZone][iInst]->Monitor(output_container[selected_iZone], integration_container, geometry_container,
+    iteration_container[ZONE_0][iInst]->Monitor(output_container[ZONE_0], integration_container, geometry_container,
         solver_container, numerics_container, config_container,
         surface_movement, grid_movement, FFDBox, ZONE_0, iInst);
 
@@ -3279,7 +3279,7 @@ void CHBDriver::Update() {
   }
 
   /*--- Precondition the harmonic balance source terms ---*/
-  if (config_container[selected_iZone]->GetHB_Precondition() == YES) {
+  if (config_container[ZONE_0]->GetHB_Precondition() == YES) {
     StabilizeHarmonicBalance();
 
   }
@@ -3287,7 +3287,7 @@ void CHBDriver::Update() {
   for (iInst = 0; iInst < nInstHB; iInst++) {
 
     /*--- Update the harmonic balance terms across all zones ---*/
-    iteration_container[selected_iZone][iInst]->Update(output_container[selected_iZone], integration_container, geometry_container,
+    iteration_container[ZONE_0][iInst]->Update(output_container[ZONE_0], integration_container, geometry_container,
         solver_container, numerics_container, config_container,
         surface_movement, grid_movement, FFDBox, ZONE_0, iInst);
 
@@ -3298,15 +3298,15 @@ void CHBDriver::Update() {
 void CHBDriver::SetHarmonicBalance(unsigned short iInst) {
 
   unsigned short iVar, jInst, iMGlevel;
-  unsigned short nVar = solver_container[selected_iZone][INST_0][MESH_0][FLOW_SOL]->GetnVar();
+  unsigned short nVar = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetnVar();
   unsigned long iPoint;
-  bool implicit = (config_container[selected_iZone]->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
-  bool adjoint = (config_container[selected_iZone]->GetContinuous_Adjoint());
+  bool implicit = (config_container[ZONE_0]->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
+  bool adjoint = (config_container[ZONE_0]->GetContinuous_Adjoint());
   if (adjoint) {
-    implicit = (config_container[selected_iZone]->GetKind_TimeIntScheme_AdjFlow() == EULER_IMPLICIT);
+    implicit = (config_container[ZONE_0]->GetKind_TimeIntScheme_AdjFlow() == EULER_IMPLICIT);
   }
 
-  unsigned long InnerIter = config_container[selected_iZone]->GetInnerIter();
+  unsigned long InnerIter = config_container[ZONE_0]->GetInnerIter();
 
   /*--- Retrieve values from the config file ---*/
   auto *U = new su2double[nVar];
@@ -3317,20 +3317,20 @@ void CHBDriver::SetHarmonicBalance(unsigned short iInst) {
   su2double deltaU, deltaPsi;
 
   /*--- Compute period of oscillation ---*/
-  su2double period = config_container[selected_iZone]->GetHarmonicBalance_Period();
+  su2double period = config_container[ZONE_0]->GetHarmonicBalance_Period();
 
   /*--- Non-dimensionalize the input period, if necessary.  */
-  period /= config_container[selected_iZone]->GetTime_Ref();
+  period /= config_container[ZONE_0]->GetTime_Ref();
 
   if (InnerIter == 0)
     ComputeHBOperator();
 
   /*--- Compute various source terms for explicit direct, implicit direct, and adjoint problems ---*/
   /*--- Loop over all grid levels ---*/
-  for (iMGlevel = 0; iMGlevel <= config_container[selected_iZone]->GetnMGLevels(); iMGlevel++) {
+  for (iMGlevel = 0; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++) {
 
     /*--- Loop over each node in the volume mesh ---*/
-    for (iPoint = 0; iPoint < geometry_container[selected_iZone][iInst][iMGlevel]->GetnPoint(); iPoint++) {
+    for (iPoint = 0; iPoint < geometry_container[ZONE_0][iInst][iMGlevel]->GetnPoint(); iPoint++) {
 
       for (iVar = 0; iVar < nVar; iVar++) {
         Source[iVar] = 0.0;
@@ -3343,11 +3343,11 @@ void CHBDriver::SetHarmonicBalance(unsigned short iInst) {
         for (iVar = 0; iVar < nVar; iVar++) {
 
           if (!adjoint) {
-            U[iVar] = solver_container[selected_iZone][jInst][iMGlevel][FLOW_SOL]->GetNodes()->GetSolution(iPoint, iVar);
+            U[iVar] = solver_container[ZONE_0][jInst][iMGlevel][FLOW_SOL]->GetNodes()->GetSolution(iPoint, iVar);
             Source[iVar] += U[iVar]*D[iInst][jInst];
 
             if (implicit) {
-              U_old[iVar] = solver_container[selected_iZone][jInst][iMGlevel][FLOW_SOL]->GetNodes()->GetSolution_Old(iPoint, iVar);
+              U_old[iVar] = solver_container[ZONE_0][jInst][iMGlevel][FLOW_SOL]->GetNodes()->GetSolution_Old(iPoint, iVar);
               deltaU = U[iVar] - U_old[iVar];
               Source[iVar] += deltaU*D[iInst][jInst];
             }
@@ -3355,11 +3355,11 @@ void CHBDriver::SetHarmonicBalance(unsigned short iInst) {
           }
 
           else {
-            Psi[iVar] = solver_container[selected_iZone][jInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->GetSolution(iPoint, iVar);
+            Psi[iVar] = solver_container[ZONE_0][jInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->GetSolution(iPoint, iVar);
             Source[iVar] += Psi[iVar]*D[jInst][iInst];
 
             if (implicit) {
-              Psi_old[iVar] = solver_container[selected_iZone][jInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->GetSolution_Old(iPoint, iVar);
+              Psi_old[iVar] = solver_container[ZONE_0][jInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->GetSolution_Old(iPoint, iVar);
               deltaPsi = Psi[iVar] - Psi_old[iVar];
               Source[iVar] += deltaPsi*D[jInst][iInst];
             }
@@ -3369,10 +3369,10 @@ void CHBDriver::SetHarmonicBalance(unsigned short iInst) {
         /*--- Store sources for current row ---*/
         for (iVar = 0; iVar < nVar; iVar++) {
           if (!adjoint) {
-            solver_container[selected_iZone][iInst][iMGlevel][FLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iVar]);
+            solver_container[ZONE_0][iInst][iMGlevel][FLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iVar]);
           }
           else {
-            solver_container[selected_iZone][iInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iVar]);
+            solver_container[ZONE_0][iInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iVar]);
           }
         }
 
@@ -3381,29 +3381,29 @@ void CHBDriver::SetHarmonicBalance(unsigned short iInst) {
   }
 
   /*--- Source term for a turbulence model ---*/
-  if (config_container[selected_iZone]->GetKind_Solver() == MAIN_SOLVER::RANS) {
+  if (config_container[ZONE_0]->GetKind_Solver() == MAIN_SOLVER::RANS) {
 
     /*--- Extra variables needed if we have a turbulence model. ---*/
-    unsigned short nVar_Turb = solver_container[selected_iZone][INST_0][MESH_0][TURB_SOL]->GetnVar();
+    unsigned short nVar_Turb = solver_container[ZONE_0][INST_0][MESH_0][TURB_SOL]->GetnVar();
     auto *U_Turb = new su2double[nVar_Turb];
     auto *Source_Turb = new su2double[nVar_Turb];
 
     /*--- Loop over only the finest mesh level (turbulence is always solved
      on the original grid only). ---*/
-    for (iPoint = 0; iPoint < geometry_container[selected_iZone][INST_0][MESH_0]->GetnPoint(); iPoint++) {
+    for (iPoint = 0; iPoint < geometry_container[ZONE_0][INST_0][MESH_0]->GetnPoint(); iPoint++) {
       for (iVar = 0; iVar < nVar_Turb; iVar++) Source_Turb[iVar] = 0.0;
       for (jInst = 0; jInst < nInstHB; jInst++) {
 
         /*--- Retrieve solution at this node in current zone ---*/
         for (iVar = 0; iVar < nVar_Turb; iVar++) {
-          U_Turb[iVar] = solver_container[selected_iZone][jInst][MESH_0][TURB_SOL]->GetNodes()->GetSolution(iPoint, iVar);
+          U_Turb[iVar] = solver_container[ZONE_0][jInst][MESH_0][TURB_SOL]->GetNodes()->GetSolution(iPoint, iVar);
           Source_Turb[iVar] += U_Turb[iVar]*D[iInst][jInst];
         }
       }
 
       /*--- Store sources for current iZone ---*/
       for (iVar = 0; iVar < nVar_Turb; iVar++)
-        solver_container[selected_iZone][iInst][MESH_0][TURB_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source_Turb[iVar]);
+        solver_container[ZONE_0][iInst][MESH_0][TURB_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source_Turb[iVar]);
     }
 
     delete [] U_Turb;
@@ -3421,9 +3421,9 @@ void CHBDriver::SetHarmonicBalance(unsigned short iInst) {
 void CHBDriver::StabilizeHarmonicBalance() {
 
   unsigned short i, j, k, iVar, iInst, jInst, iMGlevel;
-  unsigned short nVar = solver_container[selected_iZone][INST_0][MESH_0][FLOW_SOL]->GetnVar();
+  unsigned short nVar = solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->GetnVar();
   unsigned long iPoint;
-  bool adjoint = (config_container[selected_iZone]->GetContinuous_Adjoint());
+  bool adjoint = (config_container[ZONE_0]->GetContinuous_Adjoint());
 
   /*--- Retrieve values from the config file ---*/
   auto *Source     = new su2double[nInstHB];
@@ -3438,13 +3438,13 @@ void CHBDriver::StabilizeHarmonicBalance() {
   }
 
   /*--- Loop over all grid levels ---*/
-  for (iMGlevel = 0; iMGlevel <= config_container[selected_iZone]->GetnMGLevels(); iMGlevel++) {
+  for (iMGlevel = 0; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++) {
 
     /*--- Loop over each node in the volume mesh ---*/
-    for (iPoint = 0; iPoint < geometry_container[selected_iZone][INST_0][iMGlevel]->GetnPoint(); iPoint++) {
+    for (iPoint = 0; iPoint < geometry_container[ZONE_0][INST_0][iMGlevel]->GetnPoint(); iPoint++) {
 
       /*--- Get time step for current node ---*/
-      Delta = solver_container[selected_iZone][INST_0][iMGlevel][FLOW_SOL]->GetNodes()->GetDelta_Time(iPoint);
+      Delta = solver_container[ZONE_0][INST_0][iMGlevel][FLOW_SOL]->GetNodes()->GetDelta_Time(iPoint);
 
       /*--- Setup stabilization matrix for this node ---*/
       for (iInst = 0; iInst < nInstHB; iInst++) {
@@ -3543,7 +3543,7 @@ void CHBDriver::StabilizeHarmonicBalance() {
 
         /*--- Get current source terms (not yet preconditioned) and zero source array to prepare preconditioning ---*/
         for (iInst = 0; iInst < nInstHB; iInst++) {
-          Source_old[iInst] = solver_container[selected_iZone][iInst][iMGlevel][FLOW_SOL]->GetNodes()->GetHarmonicBalance_Source(iPoint, iVar);
+          Source_old[iInst] = solver_container[ZONE_0][iInst][iMGlevel][FLOW_SOL]->GetNodes()->GetHarmonicBalance_Source(iPoint, iVar);
           Source[iInst] = 0;
         }
 
@@ -3555,10 +3555,10 @@ void CHBDriver::StabilizeHarmonicBalance() {
 
           /*--- Store updated source terms for current node ---*/
           if (!adjoint) {
-            solver_container[selected_iZone][iInst][iMGlevel][FLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iInst]);
+            solver_container[ZONE_0][iInst][iMGlevel][FLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iInst]);
           }
           else {
-            solver_container[selected_iZone][iInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iInst]);
+            solver_container[ZONE_0][iInst][iMGlevel][ADJFLOW_SOL]->GetNodes()->SetHarmonicBalance_Source(iPoint, iVar, Source[iInst]);
           }
         }
 
@@ -3594,15 +3594,15 @@ void CHBDriver::ComputeHBOperator() {
   }
 
   /*--- Get simualation period from config file ---*/
-  su2double Period = config_container[selected_iZone]->GetHarmonicBalance_Period();
+  su2double Period = config_container[ZONE_0]->GetHarmonicBalance_Period();
 
   /*--- Non-dimensionalize the input period, if necessary.      */
-  Period /= config_container[selected_iZone]->GetTime_Ref();
+  Period /= config_container[ZONE_0]->GetTime_Ref();
 
   /*--- Build the array containing the selected frequencies to solve ---*/
   for (iInst = 0; iInst < nInstHB; iInst++) {
-    Omega_HB[iInst]  = config_container[selected_iZone]->GetOmega_HB()[iInst];
-    Omega_HB[iInst] /= config_container[selected_iZone]->GetOmega_Ref(); //TODO: check
+    Omega_HB[iInst]  = config_container[ZONE_0]->GetOmega_HB()[iInst];
+    Omega_HB[iInst] /= config_container[ZONE_0]->GetOmega_Ref(); //TODO: check
   }
 
   /*--- Build the diagonal matrix of the frequencies DD ---*/
diff --git a/SU2_CFD/src/drivers/CMultizoneDriver.cpp b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
index 9c8039db782..61f59223fcf 100644
--- a/SU2_CFD/src/drivers/CMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
@@ -248,7 +248,7 @@ void CMultizoneDriver::Preprocess(unsigned long TimeIter) {
   }
 
   /*--- Ramp turbo values for unsteady problems here, otherwise do it over outer iterations. ---*/
-  if (config_container[selected_iZone]->GetTime_Domain()) {
+  if (config_container[ZONE_0]->GetTime_Domain()) {
     RampTurbomachineryValues(TimeIter);
   }
 
@@ -294,7 +294,7 @@ void CMultizoneDriver::RunGaussSeidel() {
   for (auto iOuter_Iter = 0ul; iOuter_Iter < driver_config->GetnOuter_Iter(); iOuter_Iter++) {
 
     /*--- Ramp turbo values for steady problems here, otherwise do it over time steps. ---*/
-    if (!config_container[selected_iZone]->GetTime_Domain()) {
+    if (!config_container[ZONE_0]->GetTime_Domain()) {
       RampTurbomachineryValues(iOuter_Iter);
     }
 
@@ -352,7 +352,7 @@ void CMultizoneDriver::RunJacobi() {
   for (auto iOuter_Iter = 0ul; iOuter_Iter < driver_config->GetnOuter_Iter(); iOuter_Iter++){
 
     /*--- Ramp turbo values for steady problems here, otherwise do it over time steps. ---*/
-    if (!config_container[selected_iZone]->GetTime_Domain()) {
+    if (!config_container[ZONE_0]->GetTime_Domain()) {
       RampTurbomachineryValues(iOuter_Iter);
     }
 
@@ -407,7 +407,7 @@ void CMultizoneDriver::RunJacobi() {
 void CMultizoneDriver::Corrector(unsigned short val_iZone) {
 
   if (config_container[val_iZone]->GetRelaxation())
-    iteration_container[val_iZone][INST_0]->Relaxation(output_container[selected_iZone], integration_container,
+    iteration_container[val_iZone][INST_0]->Relaxation(output_container[ZONE_0], integration_container,
                                             geometry_container, solver_container, numerics_container, config_container,
                                             surface_movement, grid_movement, FFDBox, val_iZone, INST_0);
 }
@@ -493,7 +493,7 @@ void CMultizoneDriver::Output(unsigned long TimeIter) {
 
     UsedTimeOutput += StopTime-StartTime;
     OutputCount++;
-    BandwidthSum = config_container[selected_iZone]->GetRestart_Bandwidth_Agg();
+    BandwidthSum = config_container[ZONE_0]->GetRestart_Bandwidth_Agg();
 
     StartTime = SU2_MPI::Wtime();
 
@@ -632,8 +632,8 @@ void CMultizoneDriver::SetMixingPlane(unsigned short donorZone) {
 
 void CMultizoneDriver::SetTurboPerformance() {
   for (auto donorZone = 1u; donorZone < nZone; donorZone++) {
-    interface_container[donorZone][selected_iZone]->GatherAverageValues(solver_container[donorZone][INST_0][MESH_0][FLOW_SOL],
-                                                                solver_container[selected_iZone][INST_0][MESH_0][FLOW_SOL],
+    interface_container[donorZone][ZONE_0]->GatherAverageValues(solver_container[donorZone][INST_0][MESH_0][FLOW_SOL],
+                                                                solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL],
                                                                 donorZone);
   }
 }
@@ -688,5 +688,5 @@ bool CMultizoneDriver::Monitor(unsigned long TimeIter){
 }
 
 bool CMultizoneDriver::GetTimeConvergence() const{
-  return output_container[selected_iZone]->GetCauchyCorrectedTimeConvergence(config_container[selected_iZone]);
+  return output_container[ZONE_0]->GetCauchyCorrectedTimeConvergence(config_container[ZONE_0]);
 }

From 52e42ecadd52dadf1e4ccb7da758f648d809e2ae Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 29 Apr 2023 18:46:51 -0700
Subject: [PATCH 421/656] cleanup the discadj fluid iteration

---
 .../src/iteration/CDiscAdjFluidIteration.cpp  | 266 +++++++-----------
 .../src/iteration/CDiscAdjHeatIteration.cpp   |  26 +-
 2 files changed, 110 insertions(+), 182 deletions(-)

diff --git a/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
index 5a48a262390..34c163a400f 100644
--- a/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
@@ -41,69 +41,77 @@ void CDiscAdjFluidIteration::Preprocess(COutput* output, CIntegration**** integr
   const bool grid_IsMoving = config[iZone]->GetGrid_Movement();
   const bool species = config[iZone]->GetKind_Species_Model() != SPECIES_MODEL::NONE;
   const bool heat = config[iZone]->GetWeakly_Coupled_Heat();
+  const bool radiation = config[iZone]->AddRadiation();
 
   auto solvers0 = solver[iZone][iInst][MESH_0];
   auto geometries = geometry[iZone][iInst];
 
+  unsigned long nSolvers = 1;
+  std::array<int, 5> solversToProcess{{FLOW_SOL}};
+  if (turbulent) {
+    solversToProcess[nSolvers] = TURB_SOL;
+    ++nSolvers;
+  }
+  if (species) {
+    solversToProcess[nSolvers] = SPECIES_SOL;
+    ++nSolvers;
+  }
+  if (heat) {
+    solversToProcess[nSolvers] = HEAT_SOL;
+    ++nSolvers;
+  }
+  if (radiation) {
+    solversToProcess[nSolvers] = RAD_SOL;
+    ++nSolvers;
+  }
+
   /*--- For the unsteady adjoint, load direct solutions from restart files. ---*/
 
   if (config[iZone]->GetTime_Marching() != TIME_MARCHING::STEADY) {
-    const int Direct_Iter = static_cast<int>(config[iZone]->GetUnst_AdjointIter()) - static_cast<int>(TimeIter) - 2 + dual_time;
+    const int Direct_Iter = static_cast<int>(config[iZone]->GetUnst_AdjointIter()) -
+                            static_cast<int>(TimeIter) - 2 + dual_time;
 
-    /*--- For dual-time stepping we want to load the already converged solution at timestep n ---*/
+    /*--- For dual-time stepping we want to load the already converged solution at previous timesteps.
+     * In general we only load one file and shift the previously loaded solutions, on the first we
+     * load one or two more (depending on dual time order). ---*/
 
-    if (TimeIter == 0) {
-      if (dual_time_2nd) {
-        /*--- Load solution at timestep n-2 ---*/
-        LoadUnsteady_Solution(geometry, solver, config, iZone, iInst, Direct_Iter - 2);
+    if (dual_time_2nd) {
+      LoadUnsteady_Solution(geometry, solver, config, iZone, iInst, Direct_Iter - 2);
+    } else if (dual_time_1st) {
+      LoadUnsteady_Solution(geometry, solver, config, iZone, iInst, Direct_Iter - 1);
+    }
 
-        /*--- Push solution back to correct array ---*/
+    if (TimeIter == 0) {
+      /*--- Push solution back one or two levels. ---*/
 
+      if (dual_time) {
         for (auto iMesh = 0u; iMesh <= config[iZone]->GetnMGLevels(); iMesh++) {
-          auto solvers = solver[iZone][iInst][iMesh];
-
-          solvers[FLOW_SOL]->GetNodes()->Set_Solution_time_n();
-          solvers[FLOW_SOL]->GetNodes()->Set_Solution_time_n1();
-          if (turbulent) {
-            solvers[TURB_SOL]->GetNodes()->Set_Solution_time_n();
-            solvers[TURB_SOL]->GetNodes()->Set_Solution_time_n1();
-          }
-          if (species) {
-            solvers[SPECIES_SOL]->GetNodes()->Set_Solution_time_n();
-            solvers[SPECIES_SOL]->GetNodes()->Set_Solution_time_n1();
-          }
-          if (heat) {
-            solvers[HEAT_SOL]->GetNodes()->Set_Solution_time_n();
-            solvers[HEAT_SOL]->GetNodes()->Set_Solution_time_n1();
+          for (auto iSol = 0ul; iSol < nSolvers; ++iSol) {
+            solver[iZone][iInst][iMesh][solversToProcess[iSol]]->GetNodes()->Set_Solution_time_n();
+            if (dual_time_2nd)
+              solver[iZone][iInst][iMesh][solversToProcess[iSol]]->GetNodes()->Set_Solution_time_n1();
           }
           if (grid_IsMoving) {
             geometries[iMesh]->nodes->SetCoord_n();
-            geometries[iMesh]->nodes->SetCoord_n1();
+            if (dual_time_2nd)
+              geometries[iMesh]->nodes->SetCoord_n1();
           }
           if (config[iZone]->GetDynamic_Grid()) {
             geometries[iMesh]->nodes->SetVolume_n();
-            geometries[iMesh]->nodes->SetVolume_nM1();
+            if (dual_time_2nd)
+              geometries[iMesh]->nodes->SetVolume_nM1();
           }
         }
       }
-      if (dual_time) {
-        /*--- Load solution at timestep n-1 ---*/
-        LoadUnsteady_Solution(geometry, solver, config, iZone, iInst, Direct_Iter - 1);
 
-        /*--- Push solution back to correct array ---*/
+      /*--- If required load another time step. ---*/
 
-        for (auto iMesh = 0u; iMesh <= config[iZone]->GetnMGLevels(); iMesh++) {
-          auto solvers = solver[iZone][iInst][iMesh];
+      if (dual_time_2nd) {
+        LoadUnsteady_Solution(geometry, solver, config, iZone, iInst, Direct_Iter - 1);
 
-          solvers[FLOW_SOL]->GetNodes()->Set_Solution_time_n();
-          if (turbulent) {
-            solvers[TURB_SOL]->GetNodes()->Set_Solution_time_n();
-          }
-          if (species) {
-            solvers[SPECIES_SOL]->GetNodes()->Set_Solution_time_n();
-          }
-          if (heat) {
-            solvers[HEAT_SOL]->GetNodes()->Set_Solution_time_n();
+        for (auto iMesh = 0u; iMesh <= config[iZone]->GetnMGLevels(); iMesh++) {
+          for (auto iSol = 0ul; iSol < nSolvers; ++iSol) {
+            solver[iZone][iInst][iMesh][solversToProcess[iSol]]->GetNodes()->Set_Solution_time_n();
           }
           if (grid_IsMoving) {
             geometries[iMesh]->nodes->SetCoord_n();
@@ -123,15 +131,13 @@ void CDiscAdjFluidIteration::Preprocess(COutput* output, CIntegration**** integr
       }
 
     }
-    else if ((TimeIter > 0) && dual_time) {
-      /*---
-      Here the primal solutions (only working variables) are loaded and put in the correct order
-      into containers. For ALE the mesh coordinates have to be put into the
-      correct containers as well, i.e. follow the same logic for the solution.
-      Afterwards the GridVelocity is computed based on the Coordinates.
-      ---*/
-
-      /*--- Temporarily store the loaded volumes into old containers ---*/
+    if ((TimeIter > 0) && dual_time) {
+      /*--- Here the primal solutions (only working variables) are loaded and put in the correct order
+       into containers. For ALE the mesh coordinates have to be put into the correct containers as well,
+       i.e. follow the same logic for the solution. Afterwards the GridVelocity is computed based on
+       the Coordinates. ---*/
+
+      /*--- Temporarily store the loaded volumes into old containers. ---*/
       if (config[iZone]->GetDynamic_Grid()) {
         for (auto iMesh=0; iMesh<=config[iZone]->GetnMGLevels();iMesh++) {
           geometries[iMesh]->nodes->SetVolume_Old();
@@ -140,155 +146,80 @@ void CDiscAdjFluidIteration::Preprocess(COutput* output, CIntegration**** integr
         }
       }
 
-      /*-- Load mesh solver ---*/
+      /*--- Load mesh solver. ---*/
       if (config[iZone]->GetDeform_Mesh()) {
         solvers0[MESH_SOL]->LoadRestart(geometries, solver[iZone][iInst], config[iZone], Direct_Iter, true);
       }
 
-      /*--- Load solution timestep n-1 | n-2 for DualTimestepping 1st | 2nd order ---*/
-      if (dual_time_1st) {
-        LoadUnsteady_Solution(geometry, solver, config, iZone, iInst, Direct_Iter - 1);
-      } else {
-        LoadUnsteady_Solution(geometry, solver, config, iZone, iInst, Direct_Iter - 2);
-
-        /*--- Set volumes into correct containers ---*/
-        if (config[iZone]->GetDynamic_Grid()) {
-          for (auto iMesh=0; iMesh<=config[iZone]->GetnMGLevels();iMesh++) {
-            /*--- If negative iteration number, set default ---*/
-            if (Direct_Iter - 2 < 0) {
-              for(auto iPoint=0ul; iPoint<geometries[iMesh]->GetnPoint();iPoint++) {
-                geometries[iMesh]->nodes->SetVolume(iPoint,0.0);
-              }
+      /*--- Set volumes into correct containers ---*/
+      if (config[iZone]->GetDynamic_Grid()) {
+        for (auto iMesh = 0; iMesh <= config[iZone]->GetnMGLevels(); iMesh++) {
+          /*--- If negative iteration number, set default. ---*/
+          if (Direct_Iter - 1 - dual_time_2nd < 0) {
+            for(auto iPoint = 0ul; iPoint < geometries[iMesh]->GetnPoint(); iPoint++) {
+              geometries[iMesh]->nodes->SetVolume(iPoint, 0.0);
             }
+          }
 
-            /*--- Set currently loaded volume to Volume_nM1 ---*/
-            geometries[iMesh]->nodes->SetVolume_n();
-            geometries[iMesh]->nodes->SetVolume_nM1();
+          /*--- Set currently loaded volume to Volume_nM1 ---*/
+          geometries[iMesh]->nodes->SetVolume_n();
+          geometries[iMesh]->nodes->SetVolume_nM1();
 
-            /*--- Set Volume_n and Volume from old containers ---*/
-            geometries[iMesh]->nodes->SetVolume_n_from_OldnM1();
-            geometries[iMesh]->nodes->SetVolume_from_Oldn();
-          }
+          /*--- Set Volume_n and Volume from old containers ---*/
+          geometries[iMesh]->nodes->SetVolume_n_from_OldnM1();
+          geometries[iMesh]->nodes->SetVolume_from_Oldn();
         }
       }
 
-      /*--- Temporarily store the loaded solution in the Solution_Old array ---*/
+      /*--- Temporarily store the loaded solution and coordinates in the "Old" arrays. ---*/
 
       for (auto iMesh = 0u; iMesh <= config[iZone]->GetnMGLevels(); iMesh++) {
-        auto solvers = solver[iZone][iInst][iMesh];
-
-        solvers[FLOW_SOL]->Set_OldSolution();
-        if (turbulent) {
-          solvers[TURB_SOL]->Set_OldSolution();
-        }
-        if (species) {
-          solvers[SPECIES_SOL]->Set_OldSolution();
-        }
-        if (heat) {
-          solvers[HEAT_SOL]->Set_OldSolution();
+        for (auto iSol = 0ul; iSol < nSolvers; ++iSol) {
+          solver[iZone][iInst][iMesh][solversToProcess[iSol]]->Set_OldSolution();
         }
         if (grid_IsMoving) {
           geometries[iMesh]->nodes->SetCoord_Old();
         }
       }
 
-      /*--- Set Solution at timestep n to solution at n-1 ---*/
+      /*--- Move timestep n to current solution. ---*/
 
       for (auto iMesh = 0u; iMesh <= config[iZone]->GetnMGLevels(); iMesh++) {
-        auto solvers = solver[iZone][iInst][iMesh];
-
-        for (auto iPoint = 0ul; iPoint < geometries[iMesh]->GetnPoint(); iPoint++) {
-          solvers[FLOW_SOL]->GetNodes()->SetSolution(iPoint, solvers[FLOW_SOL]->GetNodes()->GetSolution_time_n(iPoint));
-
-          if (grid_IsMoving) {
-            geometries[iMesh]->nodes->SetCoord(iPoint, geometries[iMesh]->nodes->GetCoord_n(iPoint));
-          }
-          if (turbulent) {
-            solvers[TURB_SOL]->GetNodes()->SetSolution(iPoint, solvers[TURB_SOL]->GetNodes()->GetSolution_time_n(iPoint));
-          }
-          if (species) {
-            solvers[SPECIES_SOL]->GetNodes()->SetSolution(iPoint, solvers[SPECIES_SOL]->GetNodes()->GetSolution_time_n(iPoint));
-          }
-          if (heat) {
-            solvers[HEAT_SOL]->GetNodes()->SetSolution(iPoint, solvers[HEAT_SOL]->GetNodes()->GetSolution_time_n(iPoint));
+        for (auto iSol = 0ul; iSol < nSolvers; ++iSol) {
+          auto* s = solver[iZone][iInst][iMesh][solversToProcess[iSol]];
+          for (auto iPoint = 0ul; iPoint < geometries[iMesh]->GetnPoint(); iPoint++) {
+            s->GetNodes()->SetSolution(iPoint, s->GetNodes()->GetSolution_time_n(iPoint));
           }
         }
-      }
-      if (dual_time_1st) {
-        /*--- Set Solution at timestep n-1 to the previously loaded solution ---*/
-        for (auto iMesh = 0u; iMesh <= config[iZone]->GetnMGLevels(); iMesh++) {
-          auto solvers = solver[iZone][iInst][iMesh];
-
+        if (grid_IsMoving) {
           for (auto iPoint = 0ul; iPoint < geometries[iMesh]->GetnPoint(); iPoint++) {
-            solvers[FLOW_SOL]->GetNodes()->Set_Solution_time_n(
-                iPoint, solvers[FLOW_SOL]->GetNodes()->GetSolution_Old(iPoint));
-
-            if (grid_IsMoving) {
-              geometries[iMesh]->nodes->SetCoord_n(iPoint, geometries[iMesh]->nodes->GetCoord_Old(iPoint));
-            }
-            if (turbulent) {
-              solvers[TURB_SOL]->GetNodes()->Set_Solution_time_n(
-                  iPoint, solvers[TURB_SOL]->GetNodes()->GetSolution_Old(iPoint));
-            }
-            if (species) {
-              solvers[SPECIES_SOL]->GetNodes()->Set_Solution_time_n(
-                  iPoint, solvers[SPECIES_SOL]->GetNodes()->GetSolution_Old(iPoint));
-            }
-            if (heat) {
-              solvers[HEAT_SOL]->GetNodes()->Set_Solution_time_n(
-                  iPoint, solvers[HEAT_SOL]->GetNodes()->GetSolution_Old(iPoint));
-            }
+            geometries[iMesh]->nodes->SetCoord(iPoint, geometries[iMesh]->nodes->GetCoord_n(iPoint));
           }
         }
       }
-      if (dual_time_2nd) {
-        /*--- Set Solution at timestep n-1 to solution at n-2 ---*/
-        for (auto iMesh = 0u; iMesh <= config[iZone]->GetnMGLevels(); iMesh++) {
-          auto solvers = solver[iZone][iInst][iMesh];
 
-          for (auto iPoint = 0ul; iPoint < geometries[iMesh]->GetnPoint(); iPoint++) {
-            solvers[FLOW_SOL]->GetNodes()->Set_Solution_time_n(
-                iPoint, solvers[FLOW_SOL]->GetNodes()->GetSolution_time_n1(iPoint));
+      /*--- Finally, place the loaded solution in the correct place (n or n-1 depending on order). ---*/
 
-            if (grid_IsMoving) {
-              geometries[iMesh]->nodes->SetCoord_n(iPoint, geometries[iMesh]->nodes->GetCoord_n1(iPoint));
-            }
-            if (turbulent) {
-              solvers[TURB_SOL]->GetNodes()->Set_Solution_time_n(
-                  iPoint, solvers[TURB_SOL]->GetNodes()->GetSolution_time_n1(iPoint));
-            }
-            if (species) {
-              solvers[SPECIES_SOL]->GetNodes()->Set_Solution_time_n(
-                  iPoint, solvers[SPECIES_SOL]->GetNodes()->GetSolution_time_n1(iPoint));
-            }
-            if (heat) {
-              solvers[HEAT_SOL]->GetNodes()->Set_Solution_time_n(
-                  iPoint, solvers[HEAT_SOL]->GetNodes()->GetSolution_time_n1(iPoint));
+      for (auto iMesh = 0u; iMesh <= config[iZone]->GetnMGLevels(); iMesh++) {
+        for (auto iSol = 0ul; iSol < nSolvers; ++iSol) {
+          auto* s = solver[iZone][iInst][iMesh][solversToProcess[iSol]];
+          for (auto iPoint = 0ul; iPoint < geometries[iMesh]->GetnPoint(); iPoint++) {
+            if (dual_time_2nd) {
+              /*--- If required also move timestep n-1 to timestep n. ---*/
+              s->GetNodes()->Set_Solution_time_n(iPoint, s->GetNodes()->GetSolution_time_n1(iPoint));
+              s->GetNodes()->Set_Solution_time_n1(iPoint, s->GetNodes()->GetSolution_Old(iPoint));
+            } else {
+              s->GetNodes()->Set_Solution_time_n(iPoint, s->GetNodes()->GetSolution_Old(iPoint));
             }
           }
         }
-        /*--- Set Solution at timestep n-2 to the previously loaded solution ---*/
-        for (auto iMesh = 0u; iMesh <= config[iZone]->GetnMGLevels(); iMesh++) {
-          auto solvers = solver[iZone][iInst][iMesh];
-
+        if (grid_IsMoving) {
           for (auto iPoint = 0ul; iPoint < geometries[iMesh]->GetnPoint(); iPoint++) {
-            solvers[FLOW_SOL]->GetNodes()->Set_Solution_time_n1(
-                iPoint, solvers[FLOW_SOL]->GetNodes()->GetSolution_Old(iPoint));
-
-            if (grid_IsMoving) {
+            if (dual_time_2nd) {
+              geometries[iMesh]->nodes->SetCoord_n(iPoint, geometries[iMesh]->nodes->GetCoord_n1(iPoint));
               geometries[iMesh]->nodes->SetCoord_n1(iPoint, geometries[iMesh]->nodes->GetCoord_Old(iPoint));
-            }
-            if (turbulent) {
-              solvers[TURB_SOL]->GetNodes()->Set_Solution_time_n1(
-                  iPoint, solvers[TURB_SOL]->GetNodes()->GetSolution_Old(iPoint));
-            }
-            if (species) {
-              solvers[SPECIES_SOL]->GetNodes()->Set_Solution_time_n1(
-                  iPoint, solvers[SPECIES_SOL]->GetNodes()->GetSolution_Old(iPoint));
-            }
-            if (heat) {
-              solvers[HEAT_SOL]->GetNodes()->Set_Solution_time_n1(
-                  iPoint, solvers[HEAT_SOL]->GetNodes()->GetSolution_Old(iPoint));
+            } else {
+              geometries[iMesh]->nodes->SetCoord_n(iPoint, geometries[iMesh]->nodes->GetCoord_Old(iPoint));
             }
           }
         }
@@ -297,9 +228,10 @@ void CDiscAdjFluidIteration::Preprocess(COutput* output, CIntegration**** integr
     }  // else if TimeIter > 0
 
     /*--- Compute & set Grid Velocity via finite differences of the Coordinates. ---*/
-    if (grid_IsMoving)
+    if (grid_IsMoving) {
       for (auto iMesh = 0u; iMesh <= config[iZone]->GetnMGLevels(); iMesh++)
         geometries[iMesh]->SetGridVelocity(config[iZone]);
+    }
 
   }  // if unsteady
 
@@ -328,7 +260,7 @@ void CDiscAdjFluidIteration::Preprocess(COutput* output, CIntegration**** integr
     if (heat) {
       SetSolutionDirect(solvers0, ADJHEAT_SOL, HEAT_SOL, geometries[MESH_0]->GetnPoint());
     }
-    if (config[iZone]->AddRadiation()) {
+    if (radiation) {
       SetSolutionDirect(solvers0, ADJRAD_SOL, RAD_SOL, geometries[MESH_0]->GetnPoint());
     }
   }
@@ -348,7 +280,7 @@ void CDiscAdjFluidIteration::Preprocess(COutput* output, CIntegration**** integr
     solvers0[ADJHEAT_SOL]->Preprocessing(geometries[MESH_0], solvers0, config[iZone],
                                          MESH_0, 0, RUNTIME_ADJHEAT_SYS, false);
   }
-  if (config[iZone]->AddRadiation()) {
+  if (radiation) {
     solvers0[ADJRAD_SOL]->Preprocessing(geometries[MESH_0], solvers0, config[iZone],
                                         MESH_0, 0, RUNTIME_ADJRAD_SYS, false);
   }
diff --git a/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
index 7d8b841fd10..54172d5f8d6 100644
--- a/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
@@ -43,7 +43,8 @@ void CDiscAdjHeatIteration::Preprocess(COutput* output, CIntegration**** integra
   /*--- For the unsteady adjoint, load direct solutions from restart files. ---*/
 
   if (config[val_iZone]->GetTime_Marching() != TIME_MARCHING::STEADY) {
-    const int Direct_Iter = static_cast<int>(config[val_iZone]->GetUnst_AdjointIter()) - static_cast<int>(TimeIter) - 2 + dual_time;
+    const int Direct_Iter = static_cast<int>(config[val_iZone]->GetUnst_AdjointIter()) -
+                            static_cast<int>(TimeIter) - 2 + dual_time;
 
     /*--- For dual-time stepping we want to load the already converged solution at previous timesteps.
      * In general we only load one file and shift the previously loaded solutions, on the first we
@@ -56,7 +57,7 @@ void CDiscAdjHeatIteration::Preprocess(COutput* output, CIntegration**** integra
     }
 
     if (TimeIter == 0) {
-      /*--- Push solution back one or two levels, ---*/
+      /*--- Push solution back one or two levels. ---*/
       if (dual_time) {
         for (auto iMesh = 0u; iMesh <= config[val_iZone]->GetnMGLevels(); iMesh++) {
           solvers[iMesh][HEAT_SOL]->GetNodes()->Set_Solution_time_n();
@@ -89,22 +90,17 @@ void CDiscAdjHeatIteration::Preprocess(COutput* output, CIntegration**** integra
         }
       }
 
-      /*--- If required also move timestep n-1 to timestep n. ---*/
-      if (dual_time_2nd) {
-        for (auto iMesh = 0u; iMesh <= config[val_iZone]->GetnMGLevels(); iMesh++) {
-          for (auto iPoint = 0ul; iPoint < geometry[val_iZone][val_iInst][iMesh]->GetnPoint(); iPoint++) {
-            solvers[iMesh][HEAT_SOL]->GetNodes()->Set_Solution_time_n(
-                iPoint, solvers[iMesh][HEAT_SOL]->GetNodes()->GetSolution_time_n1(iPoint));
-          }
-        }
-      }
-
       /*--- Finally, place the loaded solution in the correct place (n or n-1 depending on order). ---*/
       for (auto iMesh = 0u; iMesh <= config[val_iZone]->GetnMGLevels(); iMesh++) {
+        auto* heatSol = solvers[iMesh][HEAT_SOL];
         for (auto iPoint = 0ul; iPoint < geometry[val_iZone][val_iInst][iMesh]->GetnPoint(); iPoint++) {
-          const auto sol = solvers[iMesh][HEAT_SOL]->GetNodes()->GetSolution_Old(iPoint);
-          if (dual_time_2nd) solvers[iMesh][HEAT_SOL]->GetNodes()->Set_Solution_time_n1(iPoint, sol);
-          else solvers[iMesh][HEAT_SOL]->GetNodes()->Set_Solution_time_n(iPoint, sol);
+          if (dual_time_2nd) {
+            /*--- If required also move timestep n-1 to timestep n. ---*/
+            heatSol->GetNodes()->Set_Solution_time_n(iPoint, heatSol->GetNodes()->GetSolution_time_n1(iPoint));
+            heatSol->GetNodes()->Set_Solution_time_n1(iPoint, heatSol->GetNodes()->GetSolution_Old(iPoint));
+          } else {
+            heatSol->GetNodes()->Set_Solution_time_n(iPoint, heatSol->GetNodes()->GetSolution_Old(iPoint));
+          }
         }
       }
     }

From 74b174fc24c0be75fe987b4a3a8b1dfb8ec9f956 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 29 Apr 2023 18:51:15 -0700
Subject: [PATCH 422/656] small cleanup

---
 .../src/iteration/CDiscAdjFluidIteration.cpp  | 20 ++++---------------
 1 file changed, 4 insertions(+), 16 deletions(-)

diff --git a/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
index 34c163a400f..0efe6285707 100644
--- a/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
@@ -48,22 +48,10 @@ void CDiscAdjFluidIteration::Preprocess(COutput* output, CIntegration**** integr
 
   unsigned long nSolvers = 1;
   std::array<int, 5> solversToProcess{{FLOW_SOL}};
-  if (turbulent) {
-    solversToProcess[nSolvers] = TURB_SOL;
-    ++nSolvers;
-  }
-  if (species) {
-    solversToProcess[nSolvers] = SPECIES_SOL;
-    ++nSolvers;
-  }
-  if (heat) {
-    solversToProcess[nSolvers] = HEAT_SOL;
-    ++nSolvers;
-  }
-  if (radiation) {
-    solversToProcess[nSolvers] = RAD_SOL;
-    ++nSolvers;
-  }
+  if (turbulent) solversToProcess[nSolvers++] = TURB_SOL;
+  if (species) solversToProcess[nSolvers++] = SPECIES_SOL;
+  if (heat) solversToProcess[nSolvers++] = HEAT_SOL;
+  if (radiation) solversToProcess[nSolvers++] = RAD_SOL;
 
   /*--- For the unsteady adjoint, load direct solutions from restart files. ---*/
 

From 2eceeda9ae60a5571d5ed3d70cdb2ec9e3102aa7 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 29 Apr 2023 18:57:15 -0700
Subject: [PATCH 423/656] simplify more

---
 SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp | 14 ++++++--------
 SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp  |  7 ++++---
 2 files changed, 10 insertions(+), 11 deletions(-)

diff --git a/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
index 0efe6285707..5b451907865 100644
--- a/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
@@ -70,41 +70,39 @@ void CDiscAdjFluidIteration::Preprocess(COutput* output, CIntegration**** integr
     }
 
     if (TimeIter == 0) {
-      /*--- Push solution back one or two levels. ---*/
+      /*--- Push solution back one level. ---*/
 
       if (dual_time) {
         for (auto iMesh = 0u; iMesh <= config[iZone]->GetnMGLevels(); iMesh++) {
           for (auto iSol = 0ul; iSol < nSolvers; ++iSol) {
             solver[iZone][iInst][iMesh][solversToProcess[iSol]]->GetNodes()->Set_Solution_time_n();
-            if (dual_time_2nd)
-              solver[iZone][iInst][iMesh][solversToProcess[iSol]]->GetNodes()->Set_Solution_time_n1();
           }
           if (grid_IsMoving) {
             geometries[iMesh]->nodes->SetCoord_n();
-            if (dual_time_2nd)
-              geometries[iMesh]->nodes->SetCoord_n1();
           }
           if (config[iZone]->GetDynamic_Grid()) {
             geometries[iMesh]->nodes->SetVolume_n();
-            if (dual_time_2nd)
-              geometries[iMesh]->nodes->SetVolume_nM1();
           }
         }
       }
 
-      /*--- If required load another time step. ---*/
+      /*--- If required load another time step. Push the previous time step to n-1 and the
+       loaded time step to n. ---*/
 
       if (dual_time_2nd) {
         LoadUnsteady_Solution(geometry, solver, config, iZone, iInst, Direct_Iter - 1);
 
         for (auto iMesh = 0u; iMesh <= config[iZone]->GetnMGLevels(); iMesh++) {
           for (auto iSol = 0ul; iSol < nSolvers; ++iSol) {
+            solver[iZone][iInst][iMesh][solversToProcess[iSol]]->GetNodes()->Set_Solution_time_n1();
             solver[iZone][iInst][iMesh][solversToProcess[iSol]]->GetNodes()->Set_Solution_time_n();
           }
           if (grid_IsMoving) {
+            geometries[iMesh]->nodes->SetCoord_n1();
             geometries[iMesh]->nodes->SetCoord_n();
           }
           if (config[iZone]->GetDynamic_Grid()) {
+            geometries[iMesh]->nodes->SetVolume_nM1();
             geometries[iMesh]->nodes->SetVolume_n();
           }
         }
diff --git a/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
index 54172d5f8d6..a7935c92b19 100644
--- a/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
@@ -57,19 +57,20 @@ void CDiscAdjHeatIteration::Preprocess(COutput* output, CIntegration**** integra
     }
 
     if (TimeIter == 0) {
-      /*--- Push solution back one or two levels. ---*/
+      /*--- Push solution back one level. ---*/
       if (dual_time) {
         for (auto iMesh = 0u; iMesh <= config[val_iZone]->GetnMGLevels(); iMesh++) {
           solvers[iMesh][HEAT_SOL]->GetNodes()->Set_Solution_time_n();
-          if (dual_time_2nd) solvers[iMesh][HEAT_SOL]->GetNodes()->Set_Solution_time_n1();
         }
       }
 
-      /*--- If required load another time step. ---*/
+      /*--- If required load another time step. Push the previous time step to n-1 and the
+       loaded time step to n. ---*/
       if (dual_time_2nd) {
         LoadUnsteady_Solution(geometry, solver, config, val_iZone, val_iInst, Direct_Iter - 1);
 
         for (auto iMesh = 0u; iMesh <= config[val_iZone]->GetnMGLevels(); iMesh++) {
+          solvers[iMesh][HEAT_SOL]->GetNodes()->Set_Solution_time_n1();
           solvers[iMesh][HEAT_SOL]->GetNodes()->Set_Solution_time_n();
         }
       }

From 69a7bfe19fd78d84c508490e034f543741a6e79d Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 30 Apr 2023 15:01:47 -0700
Subject: [PATCH 424/656] remove configs that are in tutorials

---
 .../DAspecies3_primitiveVenturi.cfg           | 146 ------------------
 .../species3_primitiveVenturi.cfg             | 138 -----------------
 2 files changed, 284 deletions(-)
 delete mode 100644 TestCases/species_transport/venturi_primitive_3species/DAspecies3_primitiveVenturi.cfg
 delete mode 100644 TestCases/species_transport/venturi_primitive_3species/species3_primitiveVenturi.cfg

diff --git a/TestCases/species_transport/venturi_primitive_3species/DAspecies3_primitiveVenturi.cfg b/TestCases/species_transport/venturi_primitive_3species/DAspecies3_primitiveVenturi.cfg
deleted file mode 100644
index 6ab9176cd75..00000000000
--- a/TestCases/species_transport/venturi_primitive_3species/DAspecies3_primitiveVenturi.cfg
+++ /dev/null
@@ -1,146 +0,0 @@
-%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-%                                                                              %
-% SU2 configuration file                                                       %
-% Case description: Discrete Adjiont Species mixing with 3 species             %
-% Author: T. Kattmann                                                          %
-% Institution: Bosch Thermotechniek B.V.                                       %
-% Date: 2021/10/14                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
-%                                                                              %
-%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
-% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
-%
-SOLVER= INC_RANS
-KIND_TURB_MODEL= SST
-%
-CUSTOM_OUTPUTS= 'avg_species_0 : AreaAvg{SPECIES[0]}[outlet];\
-                 avg_species_1 : AreaAvg{SPECIES[1]}[outlet];\
-                 var_species : AreaAvg{pow(SPECIES[0] - avg_species_0, 2) +\
-                                       pow(SPECIES[1] - avg_species_1, 2)}[outlet]'
-CUSTOM_OBJFUNC= 'var_species'
-OBJECTIVE_FUNCTION= CUSTOM_OBJFUNC
-OBJECTIVE_WEIGHT= 1.0
-%
-% ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
-%
-INC_DENSITY_MODEL= CONSTANT
-INC_DENSITY_INIT= 1.1766
-%
-INC_VELOCITY_INIT= ( 1.00, 0.0, 0.0 )
-%
-INC_ENERGY_EQUATION= YES
-INC_TEMPERATURE_INIT= 300.0
-%
-INC_NONDIM= INITIAL_VALUES
-%
-% -------------------- FLUID PROPERTIES ------------------------------------- %
-%
-FLUID_MODEL= CONSTANT_DENSITY
-%
-CONDUCTIVITY_MODEL= CONSTANT_CONDUCTIVITY
-THERMAL_CONDUCTIVITY_CONSTANT= 0.0357
-%
-PRANDTL_LAM= 0.72
-TURBULENT_CONDUCTIVITY_MODEL= NONE
-PRANDTL_TURB= 0.90
-%
-VISCOSITY_MODEL= CONSTANT_VISCOSITY
-MU_CONSTANT=  1.716E-5
-%
-% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
-%
-MARKER_HEATFLUX= ( wall, 0.0 )
-MARKER_SYM= ( axis )
-%
-SPECIFIED_INLET_PROFILE= NO
-INLET_FILENAME= inlet_venturi.dat
-INC_INLET_TYPE=  VELOCITY_INLET VELOCITY_INLET
-MARKER_INLET= ( gas_inlet,       300, 1.0, 1.0,  0.0, 0.0,\
-                air_axial_inlet, 300, 1.0, 0.0, -1.0, 0.0 )
-SPECIES_USE_STRONG_BC= YES
-MARKER_INLET_SPECIES= (gas_inlet,       0.5, 0.5,\
-                       air_axial_inlet, 0.6, 0.0 )
-%
-INC_OUTLET_TYPE= PRESSURE_OUTLET
-MARKER_OUTLET= ( outlet, 0.0 )
-%
-% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
-%
-NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Note that the CFL-Number was dramatically reduced compared to the primal.
-% This was necessary to ensure proper convergence. It is not necessary to do
-% this for a reasonably accurate gradient validation though.
-CFL_NUMBER= 500
-CFL_REDUCTION_SPECIES= 1.0
-CFL_REDUCTION_TURB= 1.0
-%
-% Run commented Iter for good results
-ITER= 50
-%
-% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
-%
-LINEAR_SOLVER= FGMRES
-LINEAR_SOLVER_PREC= ILU
-LINEAR_SOLVER_ERROR= 1E-8
-LINEAR_SOLVER_ITER= 20
-%
-% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
-%
-CONV_NUM_METHOD_FLOW= FDS
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW = NONE
-TIME_DISCRE_FLOW= EULER_IMPLICIT
-%
-% -------------------- SCALAR TRANSPORT ---------------------------------------%
-%
-KIND_SCALAR_MODEL= SPECIES_TRANSPORT
-DIFFUSIVITY_MODEL= CONSTANT_DIFFUSIVITY
-DIFFUSIVITY_CONSTANT= 0.001
-%
-CONV_NUM_METHOD_SPECIES= SCALAR_UPWIND
-MUSCL_SPECIES= NO
-SLOPE_LIMITER_SPECIES = NONE
-%
-TIME_DISCRE_SPECIES= EULER_IMPLICIT
-%
-SPECIES_INIT= 1.0, 0.0
-SPECIES_CLIPPING= YES
-SPECIES_CLIPPING_MIN= 0.0, 0.0
-SPECIES_CLIPPING_MAX= 1.0, 1.0
-%
-% -------------------- TURBULENT TRANSPORT ---------------------------------------%
-%
-CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-MUSCL_TURB= NO
-%
-% --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-CONV_FIELD= RMS_PRESSURE, RMS_VELOCITY-X, RMS_VELOCITY-Y, RMS_TKE, RMS_SPECIES
-CONV_RESIDUAL_MINVAL= -18
-CONV_STARTITER= 10
-%
-% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-%
-MESH_FILENAME= primitiveVenturi.su2
-SCREEN_OUTPUT= INNER_ITER WALL_TIME RMS_ADJ_PRESSURE RMS_ADJ_VELOCITY-X RMS_ADJ_VELOCITY-Y RMS_ADJ_TKE RMS_ADJ_DISSIPATION RMS_ADJ_SPECIES_0 RMS_ADJ_SPECIES_1
-SCREEN_WRT_FREQ_INNER= 10
-%
-HISTORY_OUTPUT= ITER RMS_RES LINSOL
-CONV_FILENAME= history
-MARKER_ANALYZE= outlet
-MARKER_ANALYZE_AVERAGE= MASSFLUX
-%
-OUTPUT_FILES= RESTART_ASCII, PARAVIEW
-VOLUME_OUTPUT= RESIDUAL, PRIMITIVE
-OUTPUT_WRT_FREQ= 1000
-%
-GRAD_OBJFUNC_FILENAME= of_grad.csv
-%
-RESTART_SOL= NO
-READ_BINARY_RESTART= NO
-RESTART_FILENAME= restart
-SOLUTION_FILENAME= solution
-%
-WRT_PERFORMANCE= YES
diff --git a/TestCases/species_transport/venturi_primitive_3species/species3_primitiveVenturi.cfg b/TestCases/species_transport/venturi_primitive_3species/species3_primitiveVenturi.cfg
deleted file mode 100644
index 7237f760404..00000000000
--- a/TestCases/species_transport/venturi_primitive_3species/species3_primitiveVenturi.cfg
+++ /dev/null
@@ -1,138 +0,0 @@
-%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-%                                                                              %
-% SU2 configuration file                                                       %
-% Case description: Species mixing with 3 species, i.e. 2 transport equations  %
-% Author: T. Kattmann                                                          %
-% Institution: Bosch Thermotechniek B.V.                                       %
-% Date: 2021/10/14                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
-%                                                                              %
-%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
-% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
-%
-SOLVER= INC_RANS
-KIND_TURB_MODEL= SST
-%
-% ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
-%
-INC_DENSITY_MODEL= CONSTANT
-INC_DENSITY_INIT= 1.1766
-%
-INC_VELOCITY_INIT= ( 1.00, 0.0, 0.0 )
-%
-INC_ENERGY_EQUATION= YES
-INC_TEMPERATURE_INIT= 300.0
-%
-INC_NONDIM= INITIAL_VALUES
-%
-% -------------------- FLUID PROPERTIES ------------------------------------- %
-%
-FLUID_MODEL= CONSTANT_DENSITY
-%
-CONDUCTIVITY_MODEL= CONSTANT_CONDUCTIVITY
-THERMAL_CONDUCTIVITY_CONSTANT= 0.0357
-%
-PRANDTL_LAM= 0.72
-TURBULENT_CONDUCTIVITY_MODEL= NONE
-PRANDTL_TURB= 0.90
-%
-VISCOSITY_MODEL= CONSTANT_VISCOSITY
-MU_CONSTANT=  1.716E-5
-%
-% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
-%
-MARKER_HEATFLUX= ( wall, 0.0 )
-MARKER_SYM= ( axis )
-%
-SPECIFIED_INLET_PROFILE= NO
-INLET_FILENAME= inlet_venturi.dat
-INC_INLET_TYPE=  VELOCITY_INLET VELOCITY_INLET
-MARKER_INLET= ( gas_inlet,       300, 1.0, 1.0,  0.0, 0.0,\
-                air_axial_inlet, 300, 1.0, 0.0, -1.0, 0.0 )
-SPECIES_USE_STRONG_BC= NO
-MARKER_INLET_SPECIES= (gas_inlet,       0.5, 0.5,\
-                       air_axial_inlet, 0.6, 0.0 )
-%
-INC_OUTLET_TYPE= PRESSURE_OUTLET
-MARKER_OUTLET= ( outlet, 0.0 )
-%
-% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
-%
-NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-CFL_NUMBER= 2000
-CFL_REDUCTION_SPECIES= 1.0
-CFL_REDUCTION_TURB= 1.0
-%
-% Run commented Iter for good results
-ITER= 1000
-%
-% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
-%
-LINEAR_SOLVER= FGMRES
-LINEAR_SOLVER_PREC= ILU
-LINEAR_SOLVER_ERROR= 1E-8
-LINEAR_SOLVER_ITER= 5
-%
-% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
-%
-CONV_NUM_METHOD_FLOW= FDS
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW = NONE
-TIME_DISCRE_FLOW= EULER_IMPLICIT
-%
-% -------------------- SCALAR TRANSPORT ---------------------------------------%
-%
-KIND_SCALAR_MODEL= SPECIES_TRANSPORT
-DIFFUSIVITY_MODEL= CONSTANT_DIFFUSIVITY
-DIFFUSIVITY_CONSTANT= 0.001
-%
-CONV_NUM_METHOD_SPECIES= SCALAR_UPWIND
-MUSCL_SPECIES= NO
-SLOPE_LIMITER_SPECIES = NONE
-%
-TIME_DISCRE_SPECIES= EULER_IMPLICIT
-%
-SPECIES_INIT= 1.0, 0.0
-SPECIES_CLIPPING= YES
-SPECIES_CLIPPING_MIN= 0.0, 0.0
-SPECIES_CLIPPING_MAX= 1.0, 1.0
-%
-% -------------------- TURBULENT TRANSPORT ---------------------------------------%
-%
-CONV_NUM_METHOD_TURB= SCALAR_UPWIND
-MUSCL_TURB= NO
-%
-% --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-CONV_FIELD= RMS_PRESSURE, RMS_VELOCITY-X, RMS_VELOCITY-Y, RMS_TKE, RMS_SPECIES
-CONV_RESIDUAL_MINVAL= -18
-CONV_STARTITER= 10
-%
-% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-%
-MESH_FILENAME= primitiveVenturi.su2
-SCREEN_OUTPUT= INNER_ITER WALL_TIME \
-               RMS_PRESSURE RMS_VELOCITY-X RMS_VELOCITY-Y RMS_TKE RMS_DISSIPATION RMS_SPECIES_0 RMS_SPECIES_1 \
-               LINSOL_ITER LINSOL_RESIDUAL \
-               LINSOL_ITER_TURB LINSOL_RESIDUAL_TURB \
-               LINSOL_ITER_SPECIES LINSOL_RESIDUAL_SPECIES \
-               SURFACE_SPECIES_0
-SCREEN_WRT_FREQ_INNER= 10
-%
-HISTORY_OUTPUT= ITER RMS_RES LINSOL SPECIES_COEFF SPECIES_COEFF_SURF
-CONV_FILENAME= history
-MARKER_ANALYZE= gas_inlet, air_axial_inlet, outlet
-MARKER_ANALYZE_AVERAGE= AREA
-%
-OUTPUT_FILES= RESTART_ASCII, PARAVIEW_MULTIBLOCK
-VOLUME_OUTPUT= RESIDUAL, PRIMITIVE
-OUTPUT_WRT_FREQ= 1000
-%
-RESTART_SOL= NO
-READ_BINARY_RESTART= NO
-RESTART_FILENAME= restart
-SOLUTION_FILENAME= solution
-%
-WRT_PERFORMANCE= YES

From 84e44a38ee8e11dabec55ebc985b2ee2c5e54cd1 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 30 Apr 2023 15:04:07 -0700
Subject: [PATCH 425/656] change branch

---
 .github/workflows/regression.yml | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 76545cdb274..13f883fcc3c 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t avoid_duplicated_config -c develop -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:

From e219c058f3ba5980a8f458bc98500e67c3eb7db6 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 30 Apr 2023 16:08:50 -0700
Subject: [PATCH 426/656] update residuals

---
 .github/workflows/regression.yml | 2 +-
 TestCases/tutorials.py           | 4 ++--
 2 files changed, 3 insertions(+), 3 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 13f883fcc3c..76545cdb274 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t avoid_duplicated_config -c develop -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
diff --git a/TestCases/tutorials.py b/TestCases/tutorials.py
index 3759a48e782..b2bb04b6e88 100644
--- a/TestCases/tutorials.py
+++ b/TestCases/tutorials.py
@@ -97,8 +97,8 @@ def main():
     DAspecies3_primitiveVenturi.cfg_dir   = "../Tutorials/incompressible_flow/Inc_Species_Transport"
     DAspecies3_primitiveVenturi.cfg_file  = "DAspecies3_primitiveVenturi.cfg"
     DAspecies3_primitiveVenturi.test_iter = 50
-    DAspecies3_primitiveVenturi.test_vals         = [-8.528844, -7.799649, -7.783477, -7.482502, -12.140092, -12.250169, -11.455523]
-    DAspecies3_primitiveVenturi.test_vals_aarch64 = [-8.528880, -7.799682, -7.783516, -7.482532, -12.140123, -12.250169, -11.455523]
+    DAspecies3_primitiveVenturi.test_vals         = [-8.422882, -7.699257, -7.683269, -7.411648, -12.064694, -12.205189, -11.368995]
+    DAspecies3_primitiveVenturi.test_vals_aarch64 = [-8.422882, -7.699257, -7.683269, -7.411648, -12.064694, -12.205189, -11.368995]
     DAspecies3_primitiveVenturi.command   = TestCase.Command("mpirun -n 2", "SU2_CFD_AD")
     test_list.append(DAspecies3_primitiveVenturi)
 

From da66ed308dc48bf20d8c86ad827d239f0d7b3418 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 30 Apr 2023 16:28:17 -0700
Subject: [PATCH 427/656] add a "Begin Solver" to make the tests happy

---
 TestCases/py_wrapper/custom_heat_flux/run_ad.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/py_wrapper/custom_heat_flux/run_ad.py b/TestCases/py_wrapper/custom_heat_flux/run_ad.py
index 2b63af21d2d..15d2ed8d845 100644
--- a/TestCases/py_wrapper/custom_heat_flux/run_ad.py
+++ b/TestCases/py_wrapper/custom_heat_flux/run_ad.py
@@ -239,7 +239,7 @@ def main():
 
   # Print results for the regression script to check.
   if rank == 0:
-    print("\n")
+    print("\n------------------------------ Begin Solver -----------------------------")
     print(100, 100, sens_size_fd / 100, sens_size / 100, sens_temp)
 
 if __name__ == '__main__':

From c02a79c17ec5beb1de586b438702a4fe0b7ebd92 Mon Sep 17 00:00:00 2001
From: PENGYAN777 <peng.yan@mail.polimi.it>
Date: Tue, 2 May 2023 14:05:15 +0200
Subject: [PATCH 428/656] check T

---
 SU2_CFD/include/fluid/CCoolProp.hpp | 275 +++++++++++++++-------------
 SU2_CFD/src/fluid/CCoolProp.cpp     | 151 +++++++--------
 2 files changed, 216 insertions(+), 210 deletions(-)

diff --git a/SU2_CFD/include/fluid/CCoolProp.hpp b/SU2_CFD/include/fluid/CCoolProp.hpp
index 67f2515d9df..fce51f8d5c1 100644
--- a/SU2_CFD/include/fluid/CCoolProp.hpp
+++ b/SU2_CFD/include/fluid/CCoolProp.hpp
@@ -1,149 +1,170 @@
 /*!
- * \file CCoolProp.hpp
- * \brief Defines the state-of-the-art fluid model from CoolProp library.
- * \author P. Yan, G. Gori, A. Guardone
- * \version 7.5.1 "Blackbird"
- *
- * SU2 Project Website: https://su2code.github.io
- *
- * The SU2 Project is maintained by the SU2 Foundation
- * (http://su2foundation.org)
- *
- * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
- *
- * SU2 is free software; you can redistribute it and/or
- * modify it under the terms of the GNU Lesser General Public
- * License as published by the Free Software Foundation; either
- * version 2.1 of the License, or (at your option) any later version.
- *
- * SU2 is distributed in the hope that it will be useful,
- * but WITHOUT ANY WARRANTY; without even the implied warranty of
- * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
- * Lesser General Public License for more details.
- *
- * You should have received a copy of the GNU Lesser General Public
- * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
- */
+* \file CCoolProp.hpp
+* \brief Defines the state-of-the-art fluid model from CoolProp library.
+* \author P. Yan, G. Gori, A. Guardone
+* \version 7.5.1 "Blackbird"
+*
+* SU2 Project Website: https://su2code.github.io
+*
+* The SU2 Project is maintained by the SU2 Foundation
+* (http://su2foundation.org)
+*
+* Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
+*
+* SU2 is free software; you can redistribute it and/or
+* modify it under the terms of the GNU Lesser General Public
+* License as published by the Free Software Foundation; either
+* version 2.1 of the License, or (at your option) any later version.
+*
+* SU2 is distributed in the hope that it will be useful,
+* but WITHOUT ANY WARRANTY; without even the implied warranty of
+* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+* Lesser General Public License for more details.
+*
+* You should have received a copy of the GNU Lesser General Public
+* License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+*/
 
 #pragma once
 #include "CFluidModel.hpp"
 #if defined(HAVE_COOLPROP) && !defined(CODI_FORWARD_TYPE) && !defined(CODI_REVERSE_TYPE)
 #define USE_COOLPROP
 namespace CoolProp {
-  class AbstractState;
+class AbstractState;
 }
 #endif
 #include <memory>
 
-
 /*!
- * \class CCoolProp
- * \brief Child class for defining fluid model from CoolProp library.
- * \author: P.Yan
- */
+* \class CCoolProp
+* \brief Child class for defining fluid model from CoolProp library.
+* \author: P.Yan
+*/
 class CCoolProp final : public CFluidModel {
 private:
-    su2double Gamma{1.4};           /*!< \brief Ratio of Specific Heats. */
-    su2double Gas_Constant{297};    /*!< \brief specific Gas Constant. */
-    su2double Pressure_Critical{0.0};   /*!< \brief critical pressure */
-    su2double Temperature_Critical{0.0};    /*!< \brief critical temperature */
-    su2double acentric_factor{0.0};      /*!< \brief acentric factor */
+ su2double Gamma{1.4};                /*!< \brief Ratio of Specific Heats. */
+ su2double Gas_Constant{297};         /*!< \brief specific Gas Constant. */
+ su2double Pressure_Critical{0.0};    /*!< \brief critical pressure */
+ su2double Temperature_Critical{0.0}; /*!< \brief critical temperature */
+ su2double acentric_factor{0.0};      /*!< \brief acentric factor */
+ const su2double dp{0.01};            /*!< threshold for pressure */
+ const su2double dt{0.01};            /*!< threshold for temperature */
 #ifdef USE_COOLPROP
-    std::unique_ptr<CoolProp::AbstractState> fluid_entity;   /*!< \brief fluid entity */
+ std::unique_ptr<CoolProp::AbstractState> fluid_entity; /*!< \brief fluid entity */
 #endif
+ /*!
+  * \brief Avoid critical pressure
+  * \param[in,out] Pressure: Modified so that it is not too close to critical pressure to avoid issues in CoolProp.
+  */
+ void CheckPressure(su2double& Pressure) const {
+   if (Pressure > Pressure_Critical)
+     Pressure = fmax(Pressure, (1 + dp) * Pressure_Critical);
+   else
+     Pressure = fmin(Pressure, (1 - dp) * Pressure_Critical);
+ }
+
+ /*!
+  * \brief Avoid critical temperature
+  * \param[in,out] Temperature: Modified so that it is not too close to critical temperature to avoid issues in CoolProp.
+  */
+ void CheckTemperature(su2double& Temperature) const {
+   if (Temperature > Temperature_Critical)
+     Temperature = fmax(Temperature, (1 + dt) * Temperature_Critical);
+   else
+     Temperature = fmin(Temperature, (1 + dt) * Temperature_Critical);
+ }
 
 public:
-    /*!
-     * \brief Constructor of the class.
-     */
-    CCoolProp(string fluidname);
+ /*!
+  * \brief Constructor of the class.
+  */
+ CCoolProp(string fluidname);
 
 #ifdef USE_COOLPROP
-    /*!
-   * \brief Destructor of the class.
-   * \note Needs to be defined in the .cpp to allow using only a forward declaration of CoolProp::AbstractState.
-   */
-  ~CCoolProp();
-
-  /*!
-   * \brief Set the Dimensionless State using Density and Internal Energy
-   * \param[in] rho - first thermodynamic variable.
-   * \param[in] e - second thermodynamic variable.
-   */
-  void SetTDState_rhoe(su2double rho, su2double e) override;
-
-  /*!
-   * \brief Set the Dimensionless State using Pressure  and Temperature
-   * \param[in] P - first thermodynamic variable.
-   * \param[in] T - second thermodynamic variable.
-   */
-  void SetTDState_PT(su2double P, su2double T) override;
-
-  /*!
-   * \brief Set the Dimensionless State using Pressure and Density
-   * \param[in] P - first thermodynamic variable.
-   * \param[in] rho - second thermodynamic variable.
-   */
-  void SetTDState_Prho(su2double P, su2double rho) override;
-
-  /*!
-   * \brief Set the Dimensionless Internal Energy using Pressure and Density
-   * \param[in] P - first thermodynamic variable.
-   * \param[in] rho - second thermodynamic variable.
-   */
-  void SetEnergy_Prho(su2double P, su2double rho) override;
-
-  /*!
-   * \brief Set the Dimensionless State using Enthalpy and Entropy
-   * \param[in] th1 - first thermodynamic variable (h).
-   * \param[in] th2 - second thermodynamic variable (s).
-   */
-  void SetTDState_hs(su2double h, su2double s) override;
-
-  /*!
-   * \brief Set the Dimensionless State using Density and Temperature
-   * \param[in] th1 - first thermodynamic variable (rho).
-   * \param[in] th2 - second thermodynamic variable (T).
-   */
-  void SetTDState_rhoT(su2double rho, su2double T) override;
-
-  /*!
-   * \brief Set the Dimensionless State using Pressure and Entropy
-   * \param[in] th1 - first thermodynamic variable (P).
-   * \param[in] th2 - second thermodynamic variable (s).
-   */
-  void SetTDState_Ps(su2double P, su2double s) override;
-
-  /*!
-   * \brief compute some derivatives of enthalpy and entropy needed for subsonic inflow BC
-   * \param[in] th1 - first thermodynamic variable (P).
-   * \param[in] th2 - second thermodynamic variable (rho).
-   */
-  void ComputeDerivativeNRBC_Prho(su2double P, su2double rho) override;
+ /*!
+  * \brief Destructor of the class.
+  * \note Needs to be defined in the .cpp to allow using only a forward declaration of CoolProp::AbstractState.
+  */
+ ~CCoolProp();
+
+ /*!
+  * \brief Set the Dimensionless State using Density and Internal Energy
+  * \param[in] rho - first thermodynamic variable.
+  * \param[in] e - second thermodynamic variable.
+  */
+ void SetTDState_rhoe(su2double rho, su2double e) override;
+
+ /*!
+  * \brief Set the Dimensionless State using Pressure  and Temperature
+  * \param[in] P - first thermodynamic variable.
+  * \param[in] T - second thermodynamic variable.
+  */
+ void SetTDState_PT(su2double P, su2double T) override;
+
+ /*!
+  * \brief Set the Dimensionless State using Pressure and Density
+  * \param[in] P - first thermodynamic variable.
+  * \param[in] rho - second thermodynamic variable.
+  */
+ void SetTDState_Prho(su2double P, su2double rho) override;
+
+ /*!
+  * \brief Set the Dimensionless Internal Energy using Pressure and Density
+  * \param[in] P - first thermodynamic variable.
+  * \param[in] rho - second thermodynamic variable.
+  */
+ void SetEnergy_Prho(su2double P, su2double rho) override;
+
+ /*!
+  * \brief Set the Dimensionless State using Enthalpy and Entropy
+  * \param[in] th1 - first thermodynamic variable (h).
+  * \param[in] th2 - second thermodynamic variable (s).
+  */
+ void SetTDState_hs(su2double h, su2double s) override;
+
+ /*!
+  * \brief Set the Dimensionless State using Density and Temperature
+  * \param[in] th1 - first thermodynamic variable (rho).
+  * \param[in] th2 - second thermodynamic variable (T).
+  */
+ void SetTDState_rhoT(su2double rho, su2double T) override;
+
+ /*!
+  * \brief Set the Dimensionless State using Pressure and Entropy
+  * \param[in] th1 - first thermodynamic variable (P).
+  * \param[in] th2 - second thermodynamic variable (s).
+  */
+ void SetTDState_Ps(su2double P, su2double s) override;
+
+ /*!
+  * \brief compute some derivatives of enthalpy and entropy needed for subsonic inflow BC
+  * \param[in] th1 - first thermodynamic variable (P).
+  * \param[in] th2 - second thermodynamic variable (rho).
+  */
+ void ComputeDerivativeNRBC_Prho(su2double P, su2double rho) override;
 #endif
 
-    /*!
-     * \brief Get the value of the critical pressure.
-     * \return Critical pressure.
-     */
-    su2double GetPressure_Critical(void) const { return Pressure_Critical; }
-
-    /*!
-     * \brief Get the value of the critical temperature.
-     * \return Critical temperature.
-     */
-    su2double GetTemperature_Critical(void) const { return Temperature_Critical; }
-
-    /*!
-     * \brief Get the value of specific gas constant.
-     * \return Value of the constant: Gamma
-     */
-    su2double GetGas_Constant(void) const { return Gas_Constant; }
-
-    /*!
-     * \brief Get the value of specific gas constant.
-     * \return Value of the constant: Gamma
-     */
-    su2double GetGamma(void) const { return Gamma; }
-
-};
+ /*!
+  * \brief Get the value of the critical pressure.
+  * \return Critical pressure.
+  */
+ su2double GetPressure_Critical(void) const { return Pressure_Critical; }
+
+ /*!
+  * \brief Get the value of the critical temperature.
+  * \return Critical temperature.
+  */
+ su2double GetTemperature_Critical(void) const { return Temperature_Critical; }
+
+ /*!
+  * \brief Get the value of specific gas constant.
+  * \return Value of the constant: Gamma
+  */
+ su2double GetGas_Constant(void) const { return Gas_Constant; }
+
+ /*!
+  * \brief Get the value of specific gas constant.
+  * \return Value of the constant: Gamma
+  */
+ su2double GetGamma(void) const { return Gamma; }
+};
\ No newline at end of file
diff --git a/SU2_CFD/src/fluid/CCoolProp.cpp b/SU2_CFD/src/fluid/CCoolProp.cpp
index c82745f6bc1..ab7150ab1f5 100644
--- a/SU2_CFD/src/fluid/CCoolProp.cpp
+++ b/SU2_CFD/src/fluid/CCoolProp.cpp
@@ -2,14 +2,14 @@
 * \file CCoolProp.cpp
 * \brief Source of the fluid model from CoolProp.
 * \author P. Yan, G. Gori, A. Guardone
-* \version 7.4.0 "Blackbird"
+* \version 7.5.1 "Blackbird"
 *
 * SU2 Project Website: https://su2code.github.io
 *
 * The SU2 Project is maintained by the SU2 Foundation
 * (http://su2foundation.org)
 *
-* Copyright 2012-2022, SU2 Contributors (cf. AUTHORS.md)
+* Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
 *
 * SU2 is free software; you can redistribute it and/or
 * modify it under the terms of the GNU Lesser General Public
@@ -28,116 +28,101 @@
 #include "../../include/fluid/CCoolProp.hpp"
 
 #ifdef USE_COOLPROP
-#include "CoolProp.h"
 #include "AbstractState.h"
+#include "CoolProp.h"
 
 CCoolProp::CCoolProp(string fluidname) : CFluidModel() {
-  fluid_entity = std::unique_ptr<CoolProp::AbstractState>(CoolProp::AbstractState::factory("HEOS",fluidname));
-  Gas_Constant = fluid_entity->gas_constant()/fluid_entity->molar_mass();
-  Pressure_Critical = fluid_entity->p_critical();
-  Temperature_Critical = fluid_entity->T_critical();
-  acentric_factor = fluid_entity->acentric_factor();
+ fluid_entity = std::unique_ptr<CoolProp::AbstractState>(CoolProp::AbstractState::factory("HEOS", fluidname));
+ Gas_Constant = fluid_entity->gas_constant() / fluid_entity->molar_mass();
+ Pressure_Critical = fluid_entity->p_critical();
+ Temperature_Critical = fluid_entity->T_critical();
+ acentric_factor = fluid_entity->acentric_factor();
 }
 
 CCoolProp::~CCoolProp() {}
 
 void CCoolProp::SetTDState_rhoe(su2double rho, su2double e) {
-  Density = rho;
-  StaticEnergy = e;
-  fluid_entity->update(CoolProp::DmassUmass_INPUTS, Density, StaticEnergy);
-  Cp = fluid_entity->cpmass();
-  Cv = fluid_entity->cvmass();
-  Gamma = Cp / Cv;
-  Pressure = fluid_entity->p();
-  Temperature = fluid_entity->T();
-  Entropy = fluid_entity->smass();
-  dPdrho_e = fluid_entity->first_partial_deriv(CoolProp::iP, CoolProp::iDmass, CoolProp::iUmass);
-  dPde_rho = fluid_entity->first_partial_deriv(CoolProp::iP, CoolProp::iUmass, CoolProp::iDmass);
-  dTdrho_e = fluid_entity->first_partial_deriv(CoolProp::iT, CoolProp::iDmass, CoolProp::iUmass);
-  dTde_rho = fluid_entity->first_partial_deriv(CoolProp::iT, CoolProp::iUmass, CoolProp::iDmass);
-  if (fluid_entity->phase() == 6) {
-    // assume it is pure gas
-    fluid_entity->specify_phase(CoolProp::iphase_gas);
-    if(abs(Pressure/Pressure_Critical-1)<0.01){
-      // if P is very cloase to Pc, the CoolProp has issue
-      Pressure = Pressure_Critical*0.99;
-    }
-    fluid_entity->update(CoolProp::PT_INPUTS, Pressure, Temperature);
-    if(abs(fluid_entity->rhomass()/Density-1)*100 < 1){
-      // origial phase is near saturation gas, then just compute sound speed
-      SoundSpeed2 = pow(fluid_entity->speed_sound(), 2);
-    }
-    else{
-      // original phase is not near saturation gas, then specify the phase as gas phase
-      fluid_entity->specify_phase(CoolProp::iphase_gas);
-      SetTDState_PT(Pressure,Temperature);
-    }
-  }
-  else{
-    SoundSpeed2 = pow(fluid_entity->speed_sound(), 2);
-  }
+ Density = rho;
+ StaticEnergy = e;
+ fluid_entity->update(CoolProp::DmassUmass_INPUTS, Density, StaticEnergy);
+ Cp = fluid_entity->cpmass();
+ Cv = fluid_entity->cvmass();
+ Gamma = Cp / Cv;
+ Pressure = fluid_entity->p();
+ Temperature = fluid_entity->T();
+ Entropy = fluid_entity->smass();
+ dPdrho_e = fluid_entity->first_partial_deriv(CoolProp::iP, CoolProp::iDmass, CoolProp::iUmass);
+ dPde_rho = fluid_entity->first_partial_deriv(CoolProp::iP, CoolProp::iUmass, CoolProp::iDmass);
+ dTdrho_e = fluid_entity->first_partial_deriv(CoolProp::iT, CoolProp::iDmass, CoolProp::iUmass);
+ dTde_rho = fluid_entity->first_partial_deriv(CoolProp::iT, CoolProp::iUmass, CoolProp::iDmass);
+ if (fluid_entity->phase() == CoolProp::iphase_twophase) {
+   // impose gas phase
+   Temperature = Temperature + 0.1;
+   CheckPressure(Pressure);
+   CheckTemperature(Temperature);
+   fluid_entity->update(CoolProp::PT_INPUTS, Pressure, Temperature);
+   SoundSpeed2 = pow(fluid_entity->speed_sound(), 2);
+ } else {
+   SoundSpeed2 = pow(fluid_entity->speed_sound(), 2);
+ }
 }
 
 void CCoolProp::SetTDState_PT(su2double P, su2double T) {
-  if(abs(P/Pressure_Critical-1)<0.01) {
-    P = Pressure_Critical * 0.99;
-  }
-  fluid_entity->update(CoolProp::PT_INPUTS, P, T);
-  su2double rho = fluid_entity->rhomass();
-  su2double e = fluid_entity->umass();
-  SetTDState_rhoe(rho, e);
+ CheckPressure(P);
+ CheckTemperature(T);
+ fluid_entity->update(CoolProp::PT_INPUTS, P, T);
+ su2double rho = fluid_entity->rhomass();
+ su2double e = fluid_entity->umass();
+ SetTDState_rhoe(rho, e);
 }
 
 void CCoolProp::SetTDState_Prho(su2double P, su2double rho) {
-  if(abs(P/Pressure_Critical-1)<0.01){
-    P = Pressure_Critical*0.99;
-  }
-  fluid_entity->update(CoolProp::DmassP_INPUTS, rho, P);
-  su2double e = fluid_entity->umass();
-  SetTDState_rhoe(rho, e);
+ CheckPressure(P);
+ fluid_entity->update(CoolProp::DmassP_INPUTS, rho, P);
+ su2double e = fluid_entity->umass();
+ SetTDState_rhoe(rho, e);
 }
 
-void CCoolProp::SetEnergy_Prho(su2double P, su2double rho){
-  if(abs(P/Pressure_Critical-1)<0.01){
-    P = Pressure_Critical*0.99;
-  }
-  fluid_entity->update(CoolProp::DmassP_INPUTS, rho, P);
-  StaticEnergy = fluid_entity->umass();
+void CCoolProp::SetEnergy_Prho(su2double P, su2double rho) {
+ CheckPressure(P);
+ fluid_entity->update(CoolProp::DmassP_INPUTS, rho, P);
+ StaticEnergy = fluid_entity->umass();
 }
 
 void CCoolProp::SetTDState_hs(su2double h, su2double s) {
-  fluid_entity->update(CoolProp::HmassSmass_INPUTS, h, s);
-  su2double rho = fluid_entity->rhomass();
-  su2double e = fluid_entity->umass();
-  SetTDState_rhoe(rho, e);
+ fluid_entity->update(CoolProp::HmassSmass_INPUTS, h, s);
+ su2double rho = fluid_entity->rhomass();
+ su2double e = fluid_entity->umass();
+ SetTDState_rhoe(rho, e);
 }
 
-void  CCoolProp::SetTDState_Ps(su2double P, su2double s) {
-  if(abs(P/Pressure_Critical-1)<0.01){
-    P = Pressure_Critical*0.99;
-  }
-  fluid_entity->update(CoolProp::PSmass_INPUTS, P, s);
-  su2double rho = fluid_entity->rhomass();
-  su2double e = fluid_entity->umass();
-  SetTDState_rhoe(rho, e);
+void CCoolProp::SetTDState_Ps(su2double P, su2double s) {
+ CheckPressure(P);
+ fluid_entity->update(CoolProp::PSmass_INPUTS, P, s);
+ su2double rho = fluid_entity->rhomass();
+ su2double e = fluid_entity->umass();
+ SetTDState_rhoe(rho, e);
 }
 
 void CCoolProp::SetTDState_rhoT(su2double rho, su2double T) {
-  fluid_entity->update(CoolProp::DmassT_INPUTS, rho, T);
-  su2double e = fluid_entity->umass();
-  SetTDState_rhoe(rho, e);
+ fluid_entity->update(CoolProp::DmassT_INPUTS, rho, T);
+ su2double e = fluid_entity->umass();
+ SetTDState_rhoe(rho, e);
 }
 
-void  CCoolProp::ComputeDerivativeNRBC_Prho(su2double P, su2double rho) {
-  SetTDState_Prho(P, rho);
-  dhdrho_P = fluid_entity->first_partial_deriv(CoolProp::iHmass,CoolProp::iDmass,CoolProp::iP);
-  dhdP_rho = fluid_entity->first_partial_deriv(CoolProp::iHmass,CoolProp::iP,CoolProp::iDmass);
-  dsdP_rho = fluid_entity->first_partial_deriv(CoolProp::iSmass,CoolProp::iP,CoolProp::iDmass);
-  dsdrho_P = fluid_entity->first_partial_deriv(CoolProp::iSmass,CoolProp::iDmass,CoolProp::iP);
+void CCoolProp::ComputeDerivativeNRBC_Prho(su2double P, su2double rho) {
+ SetTDState_Prho(P, rho);
+ dhdrho_P = fluid_entity->first_partial_deriv(CoolProp::iHmass, CoolProp::iDmass, CoolProp::iP);
+ dhdP_rho = fluid_entity->first_partial_deriv(CoolProp::iHmass, CoolProp::iP, CoolProp::iDmass);
+ dsdP_rho = fluid_entity->first_partial_deriv(CoolProp::iSmass, CoolProp::iP, CoolProp::iDmass);
+ dsdrho_P = fluid_entity->first_partial_deriv(CoolProp::iSmass, CoolProp::iDmass, CoolProp::iP);
 }
 
 #else
 CCoolProp::CCoolProp(string fluidname) {
-    SU2_MPI::Error("SU2 was not compiled with CoolProp (-Denable-coolprop=true). Note that CoolProp cannot be used with directdiff or autodiff", CURRENT_FUNCTION);
+ SU2_MPI::Error(
+     "SU2 was not compiled with CoolProp (-Denable-coolprop=true). Note that CoolProp cannot be used with directdiff "
+     "or autodiff",
+     CURRENT_FUNCTION);
 }
 #endif
\ No newline at end of file

From c153f6a2e58380ebc90bed5ca4cd656e6cd9f1e1 Mon Sep 17 00:00:00 2001
From: PENGYAN777 <peng.yan@mail.polimi.it>
Date: Tue, 2 May 2023 14:09:56 +0200
Subject: [PATCH 429/656] clang format

---
 SU2_CFD/include/fluid/CCoolProp.hpp | 299 ++++++++++++++--------------
 SU2_CFD/src/fluid/CCoolProp.cpp     | 174 ++++++++--------
 2 files changed, 237 insertions(+), 236 deletions(-)

diff --git a/SU2_CFD/include/fluid/CCoolProp.hpp b/SU2_CFD/include/fluid/CCoolProp.hpp
index fce51f8d5c1..8423cd7d554 100644
--- a/SU2_CFD/include/fluid/CCoolProp.hpp
+++ b/SU2_CFD/include/fluid/CCoolProp.hpp
@@ -1,29 +1,29 @@
 /*!
-* \file CCoolProp.hpp
-* \brief Defines the state-of-the-art fluid model from CoolProp library.
-* \author P. Yan, G. Gori, A. Guardone
-* \version 7.5.1 "Blackbird"
-*
-* SU2 Project Website: https://su2code.github.io
-*
-* The SU2 Project is maintained by the SU2 Foundation
-* (http://su2foundation.org)
-*
-* Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
-*
-* SU2 is free software; you can redistribute it and/or
-* modify it under the terms of the GNU Lesser General Public
-* License as published by the Free Software Foundation; either
-* version 2.1 of the License, or (at your option) any later version.
-*
-* SU2 is distributed in the hope that it will be useful,
-* but WITHOUT ANY WARRANTY; without even the implied warranty of
-* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
-* Lesser General Public License for more details.
-*
-* You should have received a copy of the GNU Lesser General Public
-* License along with SU2. If not, see <http://www.gnu.org/licenses/>.
-*/
+ * \file CCoolProp.hpp
+ * \brief Defines the state-of-the-art fluid model from CoolProp library.
+ * \author P. Yan, G. Gori, A. Guardone
+ * \version 7.5.1 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
 
 #pragma once
 #include "CFluidModel.hpp"
@@ -36,135 +36,136 @@ class AbstractState;
 #include <memory>
 
 /*!
-* \class CCoolProp
-* \brief Child class for defining fluid model from CoolProp library.
-* \author: P.Yan
-*/
+ * \class CCoolProp
+ * \brief Child class for defining fluid model from CoolProp library.
+ * \author: P.Yan
+ */
 class CCoolProp final : public CFluidModel {
-private:
- su2double Gamma{1.4};                /*!< \brief Ratio of Specific Heats. */
- su2double Gas_Constant{297};         /*!< \brief specific Gas Constant. */
- su2double Pressure_Critical{0.0};    /*!< \brief critical pressure */
- su2double Temperature_Critical{0.0}; /*!< \brief critical temperature */
- su2double acentric_factor{0.0};      /*!< \brief acentric factor */
- const su2double dp{0.01};            /*!< threshold for pressure */
- const su2double dt{0.01};            /*!< threshold for temperature */
+ private:
+  su2double Gamma{1.4};                /*!< \brief Ratio of Specific Heats. */
+  su2double Gas_Constant{297};         /*!< \brief specific Gas Constant. */
+  su2double Pressure_Critical{0.0};    /*!< \brief critical pressure */
+  su2double Temperature_Critical{0.0}; /*!< \brief critical temperature */
+  su2double acentric_factor{0.0};      /*!< \brief acentric factor */
+  const su2double dp{0.01};            /*!< threshold for pressure */
+  const su2double dt{0.01};            /*!< threshold for temperature */
 #ifdef USE_COOLPROP
- std::unique_ptr<CoolProp::AbstractState> fluid_entity; /*!< \brief fluid entity */
+  std::unique_ptr<CoolProp::AbstractState> fluid_entity; /*!< \brief fluid entity */
 #endif
- /*!
-  * \brief Avoid critical pressure
-  * \param[in,out] Pressure: Modified so that it is not too close to critical pressure to avoid issues in CoolProp.
-  */
- void CheckPressure(su2double& Pressure) const {
-   if (Pressure > Pressure_Critical)
-     Pressure = fmax(Pressure, (1 + dp) * Pressure_Critical);
-   else
-     Pressure = fmin(Pressure, (1 - dp) * Pressure_Critical);
- }
-
- /*!
-  * \brief Avoid critical temperature
-  * \param[in,out] Temperature: Modified so that it is not too close to critical temperature to avoid issues in CoolProp.
-  */
- void CheckTemperature(su2double& Temperature) const {
-   if (Temperature > Temperature_Critical)
-     Temperature = fmax(Temperature, (1 + dt) * Temperature_Critical);
-   else
-     Temperature = fmin(Temperature, (1 + dt) * Temperature_Critical);
- }
-
-public:
- /*!
-  * \brief Constructor of the class.
-  */
- CCoolProp(string fluidname);
+  /*!
+   * \brief Avoid critical pressure
+   * \param[in,out] Pressure: Modified so that it is not too close to critical pressure to avoid issues in CoolProp.
+   */
+  void CheckPressure(su2double& Pressure) const {
+    if (Pressure > Pressure_Critical)
+      Pressure = fmax(Pressure, (1 + dp) * Pressure_Critical);
+    else
+      Pressure = fmin(Pressure, (1 - dp) * Pressure_Critical);
+  }
+
+  /*!
+   * \brief Avoid critical temperature
+   * \param[in,out] Temperature: Modified so that it is not too close to critical temperature to avoid issues in
+   * CoolProp.
+   */
+  void CheckTemperature(su2double& Temperature) const {
+    if (Temperature > Temperature_Critical)
+      Temperature = fmax(Temperature, (1 + dt) * Temperature_Critical);
+    else
+      Temperature = fmin(Temperature, (1 + dt) * Temperature_Critical);
+  }
+
+ public:
+  /*!
+   * \brief Constructor of the class.
+   */
+  CCoolProp(string fluidname);
 
 #ifdef USE_COOLPROP
- /*!
-  * \brief Destructor of the class.
-  * \note Needs to be defined in the .cpp to allow using only a forward declaration of CoolProp::AbstractState.
-  */
- ~CCoolProp();
-
- /*!
-  * \brief Set the Dimensionless State using Density and Internal Energy
-  * \param[in] rho - first thermodynamic variable.
-  * \param[in] e - second thermodynamic variable.
-  */
- void SetTDState_rhoe(su2double rho, su2double e) override;
-
- /*!
-  * \brief Set the Dimensionless State using Pressure  and Temperature
-  * \param[in] P - first thermodynamic variable.
-  * \param[in] T - second thermodynamic variable.
-  */
- void SetTDState_PT(su2double P, su2double T) override;
-
- /*!
-  * \brief Set the Dimensionless State using Pressure and Density
-  * \param[in] P - first thermodynamic variable.
-  * \param[in] rho - second thermodynamic variable.
-  */
- void SetTDState_Prho(su2double P, su2double rho) override;
-
- /*!
-  * \brief Set the Dimensionless Internal Energy using Pressure and Density
-  * \param[in] P - first thermodynamic variable.
-  * \param[in] rho - second thermodynamic variable.
-  */
- void SetEnergy_Prho(su2double P, su2double rho) override;
-
- /*!
-  * \brief Set the Dimensionless State using Enthalpy and Entropy
-  * \param[in] th1 - first thermodynamic variable (h).
-  * \param[in] th2 - second thermodynamic variable (s).
-  */
- void SetTDState_hs(su2double h, su2double s) override;
-
- /*!
-  * \brief Set the Dimensionless State using Density and Temperature
-  * \param[in] th1 - first thermodynamic variable (rho).
-  * \param[in] th2 - second thermodynamic variable (T).
-  */
- void SetTDState_rhoT(su2double rho, su2double T) override;
-
- /*!
-  * \brief Set the Dimensionless State using Pressure and Entropy
-  * \param[in] th1 - first thermodynamic variable (P).
-  * \param[in] th2 - second thermodynamic variable (s).
-  */
- void SetTDState_Ps(su2double P, su2double s) override;
-
- /*!
-  * \brief compute some derivatives of enthalpy and entropy needed for subsonic inflow BC
-  * \param[in] th1 - first thermodynamic variable (P).
-  * \param[in] th2 - second thermodynamic variable (rho).
-  */
- void ComputeDerivativeNRBC_Prho(su2double P, su2double rho) override;
+  /*!
+   * \brief Destructor of the class.
+   * \note Needs to be defined in the .cpp to allow using only a forward declaration of CoolProp::AbstractState.
+   */
+  ~CCoolProp();
+
+  /*!
+   * \brief Set the Dimensionless State using Density and Internal Energy
+   * \param[in] rho - first thermodynamic variable.
+   * \param[in] e - second thermodynamic variable.
+   */
+  void SetTDState_rhoe(su2double rho, su2double e) override;
+
+  /*!
+   * \brief Set the Dimensionless State using Pressure  and Temperature
+   * \param[in] P - first thermodynamic variable.
+   * \param[in] T - second thermodynamic variable.
+   */
+  void SetTDState_PT(su2double P, su2double T) override;
+
+  /*!
+   * \brief Set the Dimensionless State using Pressure and Density
+   * \param[in] P - first thermodynamic variable.
+   * \param[in] rho - second thermodynamic variable.
+   */
+  void SetTDState_Prho(su2double P, su2double rho) override;
+
+  /*!
+   * \brief Set the Dimensionless Internal Energy using Pressure and Density
+   * \param[in] P - first thermodynamic variable.
+   * \param[in] rho - second thermodynamic variable.
+   */
+  void SetEnergy_Prho(su2double P, su2double rho) override;
+
+  /*!
+   * \brief Set the Dimensionless State using Enthalpy and Entropy
+   * \param[in] th1 - first thermodynamic variable (h).
+   * \param[in] th2 - second thermodynamic variable (s).
+   */
+  void SetTDState_hs(su2double h, su2double s) override;
+
+  /*!
+   * \brief Set the Dimensionless State using Density and Temperature
+   * \param[in] th1 - first thermodynamic variable (rho).
+   * \param[in] th2 - second thermodynamic variable (T).
+   */
+  void SetTDState_rhoT(su2double rho, su2double T) override;
+
+  /*!
+   * \brief Set the Dimensionless State using Pressure and Entropy
+   * \param[in] th1 - first thermodynamic variable (P).
+   * \param[in] th2 - second thermodynamic variable (s).
+   */
+  void SetTDState_Ps(su2double P, su2double s) override;
+
+  /*!
+   * \brief compute some derivatives of enthalpy and entropy needed for subsonic inflow BC
+   * \param[in] th1 - first thermodynamic variable (P).
+   * \param[in] th2 - second thermodynamic variable (rho).
+   */
+  void ComputeDerivativeNRBC_Prho(su2double P, su2double rho) override;
 #endif
 
- /*!
-  * \brief Get the value of the critical pressure.
-  * \return Critical pressure.
-  */
- su2double GetPressure_Critical(void) const { return Pressure_Critical; }
-
- /*!
-  * \brief Get the value of the critical temperature.
-  * \return Critical temperature.
-  */
- su2double GetTemperature_Critical(void) const { return Temperature_Critical; }
-
- /*!
-  * \brief Get the value of specific gas constant.
-  * \return Value of the constant: Gamma
-  */
- su2double GetGas_Constant(void) const { return Gas_Constant; }
-
- /*!
-  * \brief Get the value of specific gas constant.
-  * \return Value of the constant: Gamma
-  */
- su2double GetGamma(void) const { return Gamma; }
+  /*!
+   * \brief Get the value of the critical pressure.
+   * \return Critical pressure.
+   */
+  su2double GetPressure_Critical(void) const { return Pressure_Critical; }
+
+  /*!
+   * \brief Get the value of the critical temperature.
+   * \return Critical temperature.
+   */
+  su2double GetTemperature_Critical(void) const { return Temperature_Critical; }
+
+  /*!
+   * \brief Get the value of specific gas constant.
+   * \return Value of the constant: Gamma
+   */
+  su2double GetGas_Constant(void) const { return Gas_Constant; }
+
+  /*!
+   * \brief Get the value of specific gas constant.
+   * \return Value of the constant: Gamma
+   */
+  su2double GetGamma(void) const { return Gamma; }
 };
\ No newline at end of file
diff --git a/SU2_CFD/src/fluid/CCoolProp.cpp b/SU2_CFD/src/fluid/CCoolProp.cpp
index ab7150ab1f5..96ab44f6e82 100644
--- a/SU2_CFD/src/fluid/CCoolProp.cpp
+++ b/SU2_CFD/src/fluid/CCoolProp.cpp
@@ -1,29 +1,29 @@
 /*!
-* \file CCoolProp.cpp
-* \brief Source of the fluid model from CoolProp.
-* \author P. Yan, G. Gori, A. Guardone
-* \version 7.5.1 "Blackbird"
-*
-* SU2 Project Website: https://su2code.github.io
-*
-* The SU2 Project is maintained by the SU2 Foundation
-* (http://su2foundation.org)
-*
-* Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
-*
-* SU2 is free software; you can redistribute it and/or
-* modify it under the terms of the GNU Lesser General Public
-* License as published by the Free Software Foundation; either
-* version 2.1 of the License, or (at your option) any later version.
-*
-* SU2 is distributed in the hope that it will be useful,
-* but WITHOUT ANY WARRANTY; without even the implied warranty of
-* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
-* Lesser General Public License for more details.
-*
-* You should have received a copy of the GNU Lesser General Public
-* License along with SU2. If not, see <http://www.gnu.org/licenses/>.
-*/
+ * \file CCoolProp.cpp
+ * \brief Source of the fluid model from CoolProp.
+ * \author P. Yan, G. Gori, A. Guardone
+ * \version 7.5.1 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
 
 #include "../../include/fluid/CCoolProp.hpp"
 
@@ -32,97 +32,97 @@
 #include "CoolProp.h"
 
 CCoolProp::CCoolProp(string fluidname) : CFluidModel() {
- fluid_entity = std::unique_ptr<CoolProp::AbstractState>(CoolProp::AbstractState::factory("HEOS", fluidname));
- Gas_Constant = fluid_entity->gas_constant() / fluid_entity->molar_mass();
- Pressure_Critical = fluid_entity->p_critical();
- Temperature_Critical = fluid_entity->T_critical();
- acentric_factor = fluid_entity->acentric_factor();
+  fluid_entity = std::unique_ptr<CoolProp::AbstractState>(CoolProp::AbstractState::factory("HEOS", fluidname));
+  Gas_Constant = fluid_entity->gas_constant() / fluid_entity->molar_mass();
+  Pressure_Critical = fluid_entity->p_critical();
+  Temperature_Critical = fluid_entity->T_critical();
+  acentric_factor = fluid_entity->acentric_factor();
 }
 
 CCoolProp::~CCoolProp() {}
 
 void CCoolProp::SetTDState_rhoe(su2double rho, su2double e) {
- Density = rho;
- StaticEnergy = e;
- fluid_entity->update(CoolProp::DmassUmass_INPUTS, Density, StaticEnergy);
- Cp = fluid_entity->cpmass();
- Cv = fluid_entity->cvmass();
- Gamma = Cp / Cv;
- Pressure = fluid_entity->p();
- Temperature = fluid_entity->T();
- Entropy = fluid_entity->smass();
- dPdrho_e = fluid_entity->first_partial_deriv(CoolProp::iP, CoolProp::iDmass, CoolProp::iUmass);
- dPde_rho = fluid_entity->first_partial_deriv(CoolProp::iP, CoolProp::iUmass, CoolProp::iDmass);
- dTdrho_e = fluid_entity->first_partial_deriv(CoolProp::iT, CoolProp::iDmass, CoolProp::iUmass);
- dTde_rho = fluid_entity->first_partial_deriv(CoolProp::iT, CoolProp::iUmass, CoolProp::iDmass);
- if (fluid_entity->phase() == CoolProp::iphase_twophase) {
-   // impose gas phase
-   Temperature = Temperature + 0.1;
-   CheckPressure(Pressure);
-   CheckTemperature(Temperature);
-   fluid_entity->update(CoolProp::PT_INPUTS, Pressure, Temperature);
-   SoundSpeed2 = pow(fluid_entity->speed_sound(), 2);
- } else {
-   SoundSpeed2 = pow(fluid_entity->speed_sound(), 2);
- }
+  Density = rho;
+  StaticEnergy = e;
+  fluid_entity->update(CoolProp::DmassUmass_INPUTS, Density, StaticEnergy);
+  Cp = fluid_entity->cpmass();
+  Cv = fluid_entity->cvmass();
+  Gamma = Cp / Cv;
+  Pressure = fluid_entity->p();
+  Temperature = fluid_entity->T();
+  Entropy = fluid_entity->smass();
+  dPdrho_e = fluid_entity->first_partial_deriv(CoolProp::iP, CoolProp::iDmass, CoolProp::iUmass);
+  dPde_rho = fluid_entity->first_partial_deriv(CoolProp::iP, CoolProp::iUmass, CoolProp::iDmass);
+  dTdrho_e = fluid_entity->first_partial_deriv(CoolProp::iT, CoolProp::iDmass, CoolProp::iUmass);
+  dTde_rho = fluid_entity->first_partial_deriv(CoolProp::iT, CoolProp::iUmass, CoolProp::iDmass);
+  if (fluid_entity->phase() == CoolProp::iphase_twophase) {
+    // impose gas phase
+    Temperature = Temperature + 0.1;
+    CheckPressure(Pressure);
+    CheckTemperature(Temperature);
+    fluid_entity->update(CoolProp::PT_INPUTS, Pressure, Temperature);
+    SoundSpeed2 = pow(fluid_entity->speed_sound(), 2);
+  } else {
+    SoundSpeed2 = pow(fluid_entity->speed_sound(), 2);
+  }
 }
 
 void CCoolProp::SetTDState_PT(su2double P, su2double T) {
- CheckPressure(P);
- CheckTemperature(T);
- fluid_entity->update(CoolProp::PT_INPUTS, P, T);
- su2double rho = fluid_entity->rhomass();
- su2double e = fluid_entity->umass();
- SetTDState_rhoe(rho, e);
+  CheckPressure(P);
+  CheckTemperature(T);
+  fluid_entity->update(CoolProp::PT_INPUTS, P, T);
+  su2double rho = fluid_entity->rhomass();
+  su2double e = fluid_entity->umass();
+  SetTDState_rhoe(rho, e);
 }
 
 void CCoolProp::SetTDState_Prho(su2double P, su2double rho) {
- CheckPressure(P);
- fluid_entity->update(CoolProp::DmassP_INPUTS, rho, P);
- su2double e = fluid_entity->umass();
- SetTDState_rhoe(rho, e);
+  CheckPressure(P);
+  fluid_entity->update(CoolProp::DmassP_INPUTS, rho, P);
+  su2double e = fluid_entity->umass();
+  SetTDState_rhoe(rho, e);
 }
 
 void CCoolProp::SetEnergy_Prho(su2double P, su2double rho) {
- CheckPressure(P);
- fluid_entity->update(CoolProp::DmassP_INPUTS, rho, P);
- StaticEnergy = fluid_entity->umass();
+  CheckPressure(P);
+  fluid_entity->update(CoolProp::DmassP_INPUTS, rho, P);
+  StaticEnergy = fluid_entity->umass();
 }
 
 void CCoolProp::SetTDState_hs(su2double h, su2double s) {
- fluid_entity->update(CoolProp::HmassSmass_INPUTS, h, s);
- su2double rho = fluid_entity->rhomass();
- su2double e = fluid_entity->umass();
- SetTDState_rhoe(rho, e);
+  fluid_entity->update(CoolProp::HmassSmass_INPUTS, h, s);
+  su2double rho = fluid_entity->rhomass();
+  su2double e = fluid_entity->umass();
+  SetTDState_rhoe(rho, e);
 }
 
 void CCoolProp::SetTDState_Ps(su2double P, su2double s) {
- CheckPressure(P);
- fluid_entity->update(CoolProp::PSmass_INPUTS, P, s);
- su2double rho = fluid_entity->rhomass();
- su2double e = fluid_entity->umass();
- SetTDState_rhoe(rho, e);
+  CheckPressure(P);
+  fluid_entity->update(CoolProp::PSmass_INPUTS, P, s);
+  su2double rho = fluid_entity->rhomass();
+  su2double e = fluid_entity->umass();
+  SetTDState_rhoe(rho, e);
 }
 
 void CCoolProp::SetTDState_rhoT(su2double rho, su2double T) {
- fluid_entity->update(CoolProp::DmassT_INPUTS, rho, T);
- su2double e = fluid_entity->umass();
- SetTDState_rhoe(rho, e);
+  fluid_entity->update(CoolProp::DmassT_INPUTS, rho, T);
+  su2double e = fluid_entity->umass();
+  SetTDState_rhoe(rho, e);
 }
 
 void CCoolProp::ComputeDerivativeNRBC_Prho(su2double P, su2double rho) {
- SetTDState_Prho(P, rho);
- dhdrho_P = fluid_entity->first_partial_deriv(CoolProp::iHmass, CoolProp::iDmass, CoolProp::iP);
- dhdP_rho = fluid_entity->first_partial_deriv(CoolProp::iHmass, CoolProp::iP, CoolProp::iDmass);
- dsdP_rho = fluid_entity->first_partial_deriv(CoolProp::iSmass, CoolProp::iP, CoolProp::iDmass);
- dsdrho_P = fluid_entity->first_partial_deriv(CoolProp::iSmass, CoolProp::iDmass, CoolProp::iP);
+  SetTDState_Prho(P, rho);
+  dhdrho_P = fluid_entity->first_partial_deriv(CoolProp::iHmass, CoolProp::iDmass, CoolProp::iP);
+  dhdP_rho = fluid_entity->first_partial_deriv(CoolProp::iHmass, CoolProp::iP, CoolProp::iDmass);
+  dsdP_rho = fluid_entity->first_partial_deriv(CoolProp::iSmass, CoolProp::iP, CoolProp::iDmass);
+  dsdrho_P = fluid_entity->first_partial_deriv(CoolProp::iSmass, CoolProp::iDmass, CoolProp::iP);
 }
 
 #else
 CCoolProp::CCoolProp(string fluidname) {
- SU2_MPI::Error(
-     "SU2 was not compiled with CoolProp (-Denable-coolprop=true). Note that CoolProp cannot be used with directdiff "
-     "or autodiff",
-     CURRENT_FUNCTION);
+  SU2_MPI::Error(
+      "SU2 was not compiled with CoolProp (-Denable-coolprop=true). Note that CoolProp cannot be used with directdiff "
+      "or autodiff",
+      CURRENT_FUNCTION);
 }
 #endif
\ No newline at end of file

From 75777c7868ad81bd4d5f52a55f3cfc9715ae3769 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Mon, 8 May 2023 16:47:23 +0200
Subject: [PATCH 430/656] Make comment more clear as suggested in code review

---
 SU2_CFD/src/iteration/CIteration.cpp | 8 +++++---
 1 file changed, 5 insertions(+), 3 deletions(-)

diff --git a/SU2_CFD/src/iteration/CIteration.cpp b/SU2_CFD/src/iteration/CIteration.cpp
index 3fef70d4837..9d0c1c650bc 100644
--- a/SU2_CFD/src/iteration/CIteration.cpp
+++ b/SU2_CFD/src/iteration/CIteration.cpp
@@ -60,18 +60,20 @@ void CIteration::SetGrid_Movement(CGeometry** geometry, CSurfaceMovement* surfac
 
       break;
 
-      /*--- Already initialized in the static mesh movement routine at driver level. ---*/
     case STEADY_TRANSLATION:
+      /*--- Pure translation is initialized in the static mesh movement routine at driver level. ---*/
+
     case ROTATING_FRAME:
+      /*--- Set or update the rotating frame mesh movement with the current translation and rotation
+       * rates, which might be altered via the python interface. ---*/
+
       if (rank == MASTER_NODE) cout << endl << " Setting rotating frame grid velocities" << endl;
 
       /*--- Set the grid velocities on finest multigrid level for a rotating reference frame. ---*/
-
       geometry[MESH_0]->SetRotationalVelocity(config, true);
 
       /*--- Update the multigrid structure after moving the finest grid,
             including computing the grid velocities on the coarser levels. ---*/
-
       grid_movement->UpdateMultiGrid(geometry, config);
 
       break;

From d7e3e6c5450adfc1520a91423470266dd120aba8 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Tue, 9 May 2023 09:07:02 +0200
Subject: [PATCH 431/656] Add a test case that updates the translation and
 rotation rates given in the config file via the python wrapper

---
 .../updated_moving_frame_NACA12/config.cfg    |  75 +++++++
 .../forces_0.csv.ref                          | 200 ++++++++++++++++++
 .../updated_moving_frame_NACA12/run_su2.py    |  81 +++++++
 3 files changed, 356 insertions(+)
 create mode 100644 TestCases/py_wrapper/updated_moving_frame_NACA12/config.cfg
 create mode 100644 TestCases/py_wrapper/updated_moving_frame_NACA12/forces_0.csv.ref
 create mode 100644 TestCases/py_wrapper/updated_moving_frame_NACA12/run_su2.py

diff --git a/TestCases/py_wrapper/updated_moving_frame_NACA12/config.cfg b/TestCases/py_wrapper/updated_moving_frame_NACA12/config.cfg
new file mode 100644
index 00000000000..449248bf169
--- /dev/null
+++ b/TestCases/py_wrapper/updated_moving_frame_NACA12/config.cfg
@@ -0,0 +1,75 @@
+% PROBLEM DEFINITION
+%
+SOLVER= EULER
+REF_DIMENSIONALIZATION= FREESTREAM_VEL_EQ_MACH
+MATH_PROBLEM= DIRECT
+RESTART_SOL= NO
+
+% FREE-STREAM DEFINITION
+%
+% We are translating the domain instead of having farfield velocity.
+% Note: The rotating frame is intended for 3D cases. To use the feature in a 2D case,
+% care must be taken with respect to the axes, e.g. to obtain a pitching motion, a 
+% rotation about the z-axis can be used.
+GRID_MOVEMENT= ROTATING_FRAME
+MOTION_ORIGIN= 0.0, 0.0, 0.0
+ROTATION_RATE=  0.0, 0.0, 0.0
+TRANSLATION_RATE= -265.05707641411146, 0.0, 0.0
+MACH_NUMBER= 0.0
+FREESTREAM_PRESSURE= 101325.0
+FREESTREAM_TEMPERATURE= 273.15
+
+% REFERENCE VALUES
+%
+% The AOA is only needed to compute CD and CL, it should match the translation rate.
+AOA= 0.0
+% Same for the Mach number of the motion.
+MACH_MOTION= 0.8
+REF_ORIGIN_MOMENT_X= 0.00
+REF_ORIGIN_MOMENT_Y= 0.00
+REF_ORIGIN_MOMENT_Z= 0.00
+REF_LENGTH= 1.0
+REF_AREA= 1.0
+
+% BOUNDARY CONDITIONS
+%
+MARKER_EULER= ( airfoil )
+MARKER_FAR= ( farfield )
+MARKER_PLOTTING= ( airfoil )
+MARKER_MONITORING= ( airfoil )
+% We are specifying this marker to have an easy way to access it in python.
+MARKER_DEFORM_MESH= ( airfoil )
+
+% DISCRETIZATION METHODS
+%
+CONV_NUM_METHOD_FLOW= ROE
+MUSCL_FLOW= YES
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
+SLOPE_LIMITER_FLOW= VENKATAKRISHNAN_WANG
+VENKAT_LIMITER_COEFF= 0.1
+
+% SOLUTION ACCELERATION
+%
+CFL_NUMBER= 1e3
+CFL_ADAPT= NO
+%
+MGLEVEL= 3
+MGCYCLE= W_CYCLE
+%
+LINEAR_SOLVER= FGMRES
+LINEAR_SOLVER_PREC= ILU
+LINEAR_SOLVER_ERROR= 0.1
+LINEAR_SOLVER_ITER= 10
+
+% CONVERGENCE PARAMETERS
+%
+ITER= 250
+CONV_FIELD= RMS_DENSITY
+CONV_RESIDUAL_MINVAL= -9
+
+% INPUT/OUTPUT
+%
+MESH_FILENAME= ../../euler/naca0012/mesh_NACA0012_inv.su2
+MESH_FORMAT= SU2
+SCREEN_OUTPUT= (INNER_ITER, RMS_RES, FORCE_X, FORCE_Y, FORCE_Z, MOMENT_X, MOMENT_Y, MOMENT_Z)
+HISTORY_OUTPUT= (INNER_ITER, RMS_RES, AERO_COEFF)
diff --git a/TestCases/py_wrapper/updated_moving_frame_NACA12/forces_0.csv.ref b/TestCases/py_wrapper/updated_moving_frame_NACA12/forces_0.csv.ref
new file mode 100644
index 00000000000..eae8cf091e5
--- /dev/null
+++ b/TestCases/py_wrapper/updated_moving_frame_NACA12/forces_0.csv.ref
@@ -0,0 +1,200 @@
+199, -1.02, -0.00, 0.00
+0, -2.05, 14.11, 0.00
+1, -3.63, 25.02, 0.00
+2, -4.85, 33.50, 0.00
+3, -5.88, 40.69, 0.00
+4, -6.73, 46.67, 0.00
+5, -7.41, 51.56, 0.00
+6, -7.97, 55.71, 0.00
+7, -8.40, 58.99, 0.00
+8, -8.71, 61.49, 0.00
+9, -8.90, 63.22, 0.00
+10, -8.98, 64.25, 0.00
+11, -8.98, 64.66, 0.00
+12, -8.87, 64.38, 0.00
+13, -8.68, 63.48, 0.00
+14, -8.39, 61.96, 0.00
+15, -8.03, 59.85, 0.00
+16, -7.61, 57.27, 0.00
+17, -7.12, 54.13, 0.00
+18, -6.57, 50.50, 0.00
+19, -5.97, 46.39, 0.00
+20, -5.32, 41.81, 0.00
+21, -4.63, 36.81, 0.00
+22, -3.90, 31.39, 0.00
+23, -3.13, 25.55, 0.00
+24, -2.34, 19.36, 0.00
+25, -1.53, 12.80, 0.00
+26, -0.69, 5.88, 0.00
+27, 0.16, -1.35, 0.00
+28, 1.02, -8.91, 0.00
+29, 1.88, -16.75, 0.00
+30, 2.74, -24.86, 0.00
+31, 3.61, -33.24, 0.00
+32, 4.46, -41.90, 0.00
+33, 5.31, -50.77, 0.00
+34, 6.14, -59.83, 0.00
+35, 6.95, -69.11, 0.00
+36, 7.73, -78.57, 0.00
+37, 8.48, -88.14, 0.00
+38, 9.19, -97.82, 0.00
+39, 9.86, -107.57, 0.00
+40, 10.47, -117.28, 0.00
+41, 11.01, -126.92, 0.00
+42, 11.49, -136.43, 0.00
+43, 11.87, -145.62, 0.00
+44, 12.15, -154.31, 0.00
+45, 12.30, -162.22, 0.00
+46, 12.31, -169.04, 0.00
+47, 12.11, -173.89, 0.00
+48, 11.66, -175.88, 0.00
+49, 11.13, -177.08, 0.00
+50, 10.20, -172.29, 0.00
+51, 6.86, -123.94, 0.00
+52, 5.97, -116.29, 0.00
+53, 21.77, -461.42, 0.00
+54, 26.12, -610.78, 0.00
+55, 21.89, -573.85, 0.00
+56, 18.71, -561.76, 0.00
+57, 15.72, -557.10, 0.00
+58, 12.57, -549.52, 0.00
+59, 9.33, -540.36, 0.00
+60, 6.04, -530.05, 0.00
+61, 2.71, -518.89, 0.00
+62, -0.62, -506.43, 0.00
+63, -3.95, -492.74, 0.00
+64, -7.24, -478.42, 0.00
+65, -10.47, -463.16, 0.00
+66, -13.60, -446.83, 0.00
+67, -16.63, -429.81, 0.00
+68, -19.50, -411.99, 0.00
+69, -22.22, -393.60, 0.00
+70, -24.75, -374.77, 0.00
+71, -27.06, -355.42, 0.00
+72, -29.14, -335.60, 0.00
+73, -30.94, -315.27, 0.00
+74, -32.45, -294.65, 0.00
+75, -33.65, -273.85, 0.00
+76, -34.49, -252.64, 0.00
+77, -34.95, -231.28, 0.00
+78, -35.02, -209.98, 0.00
+79, -34.64, -188.53, 0.00
+80, -33.79, -167.17, 0.00
+81, -32.42, -145.88, 0.00
+82, -30.48, -124.69, 0.00
+83, -27.91, -103.76, 0.00
+84, -24.63, -83.06, 0.00
+85, -20.55, -62.73, 0.00
+86, -15.56, -42.84, 0.00
+87, -9.50, -23.48, 0.00
+88, -2.17, -4.79, 0.00
+89, 6.62, 12.94, 0.00
+90, 17.16, 29.44, 0.00
+91, 29.73, 44.19, 0.00
+92, 44.58, 56.46, 0.00
+93, 61.71, 65.06, 0.00
+94, 81.10, 68.89, 0.00
+95, 101.88, 66.36, 0.00
+96, 122.09, 55.96, 0.00
+97, 139.13, 37.65, 0.00
+98, 108.84, 14.60, 0.00
+99, 71.28, -0.00, 0.00
+100, 106.29, -14.26, 0.00
+101, 130.33, -35.27, 0.00
+102, 108.14, -49.57, 0.00
+103, 84.37, -54.95, 0.00
+104, 61.43, -52.19, 0.00
+105, 40.94, -43.16, 0.00
+106, 23.22, -29.41, 0.00
+107, 8.42, -12.52, 0.00
+108, -3.78, 6.48, 0.00
+109, -13.76, 26.90, 0.00
+110, -21.85, 48.23, 0.00
+111, -28.39, 70.19, 0.00
+112, -33.65, 92.65, 0.00
+113, -37.82, 115.44, 0.00
+114, -41.08, 138.55, 0.00
+115, -43.55, 161.90, 0.00
+116, -45.31, 185.37, 0.00
+117, -46.46, 209.03, 0.00
+118, -47.03, 232.69, 0.00
+119, -47.10, 256.34, 0.00
+120, -46.71, 280.06, 0.00
+121, -45.86, 303.51, 0.00
+122, -44.63, 326.98, 0.00
+123, -43.04, 350.21, 0.00
+124, -41.06, 372.86, 0.00
+125, -38.81, 395.46, 0.00
+126, -36.30, 418.02, 0.00
+127, -33.51, 440.10, 0.00
+128, -30.48, 461.60, 0.00
+129, -27.23, 482.42, 0.00
+130, -23.80, 502.74, 0.00
+131, -20.21, 522.54, 0.00
+132, -16.49, 541.62, 0.00
+133, -12.66, 560.14, 0.00
+134, -8.74, 577.66, 0.00
+135, -4.77, 594.37, 0.00
+136, -0.75, 610.64, 0.00
+137, 3.27, 625.80, 0.00
+138, 7.29, 639.80, 0.00
+139, 11.28, 653.28, 0.00
+140, 15.23, 665.78, 0.00
+141, 19.09, 676.85, 0.00
+142, 22.88, 687.16, 0.00
+143, 26.58, 696.67, 0.00
+144, 30.15, 704.91, 0.00
+145, 33.58, 711.87, 0.00
+146, 36.88, 717.99, 0.00
+147, 40.04, 723.07, 0.00
+148, 43.03, 726.92, 0.00
+149, 45.86, 729.95, 0.00
+150, 48.47, 730.99, 0.00
+151, 50.57, 726.34, 0.00
+152, 54.71, 751.52, 0.00
+153, 52.81, 696.43, 0.00
+154, 5.64, 71.68, 0.00
+155, -0.65, -7.95, 0.00
+156, 3.46, 41.08, 0.00
+157, 3.63, 41.77, 0.00
+158, 4.01, 44.95, 0.00
+159, 4.28, 46.74, 0.00
+160, 4.32, 46.00, 0.00
+161, 4.21, 43.77, 0.00
+162, 3.98, 40.43, 0.00
+163, 3.64, 36.21, 0.00
+164, 3.22, 31.35, 0.00
+165, 2.72, 26.01, 0.00
+166, 2.16, 20.31, 0.00
+167, 1.56, 14.37, 0.00
+168, 0.92, 8.30, 0.00
+169, 0.24, 2.16, 0.00
+170, -0.45, -3.98, 0.00
+171, -1.16, -10.05, 0.00
+172, -1.88, -15.99, 0.00
+173, -2.60, -21.79, 0.00
+174, -3.31, -27.37, 0.00
+175, -4.00, -32.68, 0.00
+176, -4.69, -37.76, 0.00
+177, -5.34, -42.49, 0.00
+178, -5.96, -46.87, 0.00
+179, -6.55, -50.90, 0.00
+180, -7.09, -54.49, 0.00
+181, -7.59, -57.67, 0.00
+182, -8.03, -60.38, 0.00
+183, -8.40, -62.58, 0.00
+184, -8.72, -64.34, 0.00
+185, -8.96, -65.53, 0.00
+186, -9.11, -66.13, 0.00
+187, -9.18, -66.13, 0.00
+188, -9.15, -65.46, 0.00
+189, -9.04, -64.19, 0.00
+190, -8.81, -62.24, 0.00
+191, -8.48, -59.55, 0.00
+192, -8.02, -56.09, 0.00
+193, -7.44, -51.78, 0.00
+194, -6.74, -46.74, 0.00
+195, -5.87, -40.64, 0.00
+196, -4.83, -33.31, 0.00
+197, -3.59, -24.74, 0.00
+198, -1.96, -13.51, 0.00
diff --git a/TestCases/py_wrapper/updated_moving_frame_NACA12/run_su2.py b/TestCases/py_wrapper/updated_moving_frame_NACA12/run_su2.py
new file mode 100644
index 00000000000..7a63380137d
--- /dev/null
+++ b/TestCases/py_wrapper/updated_moving_frame_NACA12/run_su2.py
@@ -0,0 +1,81 @@
+import sys
+import numpy as np
+from mpi4py import MPI
+import SU2, pysu2
+
+"""
+This test case updates the translation and rotation rates given in the config file via the python wrapper
+using the python functions SetTranslationRate() and SetRotationRate(). 
+Expected results:
+            |  Inner_Iter|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|         CFx|         CFy|         CFz|         CMx|         CMy|         CMz|
+A0A=0.0 deg: no lift and moments for the symmetrical airfoil (for reference)
+             |          51|   -9.205443|   -9.406638|   -9.542742|   -8.868505|    0.008431|   -0.000001|    0.000000|    0.000000|    0.000000|   -0.000037|
+AoA=0.5 deg: increase in lift (CFy), small pitching moment (CMz) because origin at the leading edge
+             |          65|   -9.016705|   -9.182525|   -9.424299|   -8.656815|    0.009455|    0.133624|    0.000000|    0.000000|    0.000000|    0.045316|
+AoA=0.5 deg and rot_z=-30 deg/s: small increase in pitching moment (CMz) and with the origin at the leading edge, the pitch rate adds a little lift (CFy)
+             |          50|   -9.031666|   -9.303253|   -9.288828|   -8.652367|    0.009733|    0.153685|    0.000000|    0.000000|    0.000000|    0.053223|
+Thus, a check of the final surface forces is an indicator that the update of the moving frame worked properly.
+"""
+
+def setup_mpi():
+    if 'mpi4py.MPI' in sys.modules:
+        have_mpi = True
+        comm = MPI.COMM_WORLD
+        status = MPI.Status()
+        myid = comm.Get_rank()
+    else:
+        have_mpi = False
+        comm = None
+        status = None
+        myid = 0
+    return have_mpi, comm, status, myid
+
+
+class SU2Interface:
+    def __init__(self, config_filename):
+        self.have_mpi, self.comm, self.status, self.myid = setup_mpi()
+        self.FluidSolver = pysu2.CSinglezoneDriver(config_filename, 1, self.comm)
+
+    def run_solver(self):
+        self.comm.barrier()
+        # run solver
+        self.FluidSolver.Preprocess(0)
+        self.FluidSolver.Run()
+        self.FluidSolver.Postprocess()
+        # write outputs
+        self.FluidSolver.Monitor(0)
+        self.FluidSolver.Output(0)
+        self.comm.barrier()
+        
+    def update_moving_frame(self):
+        # Reduce AoA from 0.0 to 0.5 deg
+        self.FluidSolver.SetTranslationRate(xDot=-265.0469838528219, yDot=-2.3130299864229564, zDot=0.0)
+        # Add a pitch rate (in the 2D case, nose up pitch is a negative rotation about the z-axis)
+        self.FluidSolver.SetRotationRate(rot_x=0.0, rot_y=0.0, rot_z=-30.0/180.0*np.pi)
+
+    def save_forces(self):
+        solver_all_moving_markers = np.array(self.FluidSolver.GetDeformableMarkerTags())
+        solver_markers = self.FluidSolver.GetMarkerTags()
+        solver_marker_ids = self.FluidSolver.GetMarkerIndices()
+        # The surface marker and the partitioning of the solver usually don't agree.
+        # Thus, it is necessary to figure out if the partition of the current mpi process has
+        # a node that belongs to a moving surface marker.
+        has_moving_marker = [marker in solver_markers for marker in solver_all_moving_markers]
+
+        f = open('forces_'+str(self.myid)+'.csv','w')
+
+        for marker in solver_all_moving_markers[has_moving_marker]:
+            solver_marker_id = solver_marker_ids[marker]
+            n_vertices = self.FluidSolver.GetNumberMarkerNodes(solver_marker_id)
+            for i_vertex in range(n_vertices):
+                fxyz = self.FluidSolver.GetMarkerFlowLoad(solver_marker_id, i_vertex)
+                iPoint = self.FluidSolver.GetMarkerNode(solver_marker_id, i_vertex)
+                GlobalIndex = self.FluidSolver.GetNodeGlobalIndex(iPoint)
+                f.write('{}, {:.2f}, {:.2f}, {:.2f}\n'.format(GlobalIndex, fxyz[0], fxyz[1], 0.0))
+        f.close()
+
+cfd_interface = SU2Interface('config.cfg')
+cfd_interface.update_moving_frame()
+cfd_interface.run_solver()
+cfd_interface.save_forces()
+

From 28f4133ecfa4640d3e529ece0fe17e1440dba11f Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Tue, 9 May 2023 09:42:47 +0200
Subject: [PATCH 432/656] Removed units from screen output as the values can be
 non-dimensional, too.

---
 Common/src/geometry/CGeometry.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/Common/src/geometry/CGeometry.cpp b/Common/src/geometry/CGeometry.cpp
index cc5c84e54f3..ef0ff2cf0de 100644
--- a/Common/src/geometry/CGeometry.cpp
+++ b/Common/src/geometry/CGeometry.cpp
@@ -3443,7 +3443,7 @@ void CGeometry::SetRotationalVelocity(const CConfig* config, bool print) {
     cout << " Rotational origin (x, y, z): ( " << Center[0] << ", " << Center[1];
     cout << ", " << Center[2] << " )\n";
     cout << " Angular velocity about x, y, z axes: ( " << Omega[0] << ", ";
-    cout << Omega[1] << ", " << Omega[2] << " ) rad/s" << endl;
+    cout << Omega[1] << ", " << Omega[2] << " )" << endl;
     cout << " Translational velocity in x, y, z direction: (" << xDot[0] << ", " << xDot[1] << ", " << xDot[2] << ")."
          << endl;
   }

From cf4fc61a9a0d1ced27b3a412327f5966fd471530 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Tue, 9 May 2023 09:46:42 +0200
Subject: [PATCH 433/656] Removed calculation of moving frame grid velocities
 due to Roating frame from preprocessing.

---
 SU2_CFD/src/drivers/CDriver.cpp | 19 ++-----------------
 1 file changed, 2 insertions(+), 17 deletions(-)

diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index 07fc5ca3697..6a8d18de96d 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -2558,23 +2558,8 @@ void CDriver::PreprocessStaticMesh(const CConfig *config, CGeometry** geometry){
     switch (Kind_Grid_Movement) {
 
       case ROTATING_FRAME:
-
-        /*--- Steadily rotating frame: set the grid velocities just once
-         before the first iteration flow solver. ---*/
-
-        if (rank == MASTER_NODE) {
-          cout << endl << " Setting rotating frame grid velocities";
-          cout << " for zone " << iZone << "." << endl;
-        }
-
-        /*--- Set the grid velocities on all multigrid levels for a steadily
-           rotating reference frame. ---*/
-
-        for (iMGlevel = 0; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++){
-          geometry[iMGlevel]->SetRotationalVelocity(config, true);
-          geometry[iMGlevel]->SetShroudVelocity(config);
-        }
-
+        /*--- Do nothing here, the steady rotating frame will be handled in the first iteration
+         * of the flow solver, see CIteration::SetGrid_Movement(). ---*/
         break;
 
       case STEADY_TRANSLATION:

From faf2d2c290b7660c98e8e01cc6de5453b740aaa5 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Tue, 9 May 2023 09:57:41 +0200
Subject: [PATCH 434/656] Added new testcase from previous commit to the
 regression tests.

---
 TestCases/hybrid_regression.py                |  12 ++
 .../forces_0_aarch64.csv.ref                  | 200 ++++++++++++++++++
 2 files changed, 212 insertions(+)
 create mode 100644 TestCases/py_wrapper/updated_moving_frame_NACA12/forces_0_aarch64.csv.ref

diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index 04997ff9ba8..bb748388ec9 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -751,6 +751,18 @@ def main():
     pywrapper_translating_naca0012.test_file = "forces_0.csv"
     pywrapper_translating_naca0012.enabled_on_cpu_arch = ["x86_64"]
     file_diff_list.append(pywrapper_translating_naca0012)
+    
+    # NACA0012 with updated moving frame
+    pywrapper_updated_moving_frame_naca0012 = TestCase('pywrapper_updated_moving_frame_naca0012')
+    pywrapper_updated_moving_frame_naca0012.cfg_dir = "py_wrapper/updated_moving_frame_NACA12"
+    pywrapper_updated_moving_frame_naca0012.cfg_file = "config.cfg"
+    pywrapper_updated_moving_frame_naca0012.command = TestCase.Command(exec = "python", param = "run_su2.py")
+    pywrapper_updated_moving_frame_naca0012.timeout = 60
+    pywrapper_updated_moving_frame_naca0012.reference_file = "forces_0.csv.ref"
+    pywrapper_updated_moving_frame_naca0012.reference_file_aarch64 = "forces_0_aarch64.csv.ref"
+    pywrapper_updated_moving_frame_naca0012.test_file = "forces_0.csv"
+    pywrapper_updated_moving_frame_naca0012.enabled_on_cpu_arch = ["x86_64"]
+    file_diff_list.append(pywrapper_updated_moving_frame_naca0012)
 
     ######################################
     ### RUN TESTS                      ###
diff --git a/TestCases/py_wrapper/updated_moving_frame_NACA12/forces_0_aarch64.csv.ref b/TestCases/py_wrapper/updated_moving_frame_NACA12/forces_0_aarch64.csv.ref
new file mode 100644
index 00000000000..eae8cf091e5
--- /dev/null
+++ b/TestCases/py_wrapper/updated_moving_frame_NACA12/forces_0_aarch64.csv.ref
@@ -0,0 +1,200 @@
+199, -1.02, -0.00, 0.00
+0, -2.05, 14.11, 0.00
+1, -3.63, 25.02, 0.00
+2, -4.85, 33.50, 0.00
+3, -5.88, 40.69, 0.00
+4, -6.73, 46.67, 0.00
+5, -7.41, 51.56, 0.00
+6, -7.97, 55.71, 0.00
+7, -8.40, 58.99, 0.00
+8, -8.71, 61.49, 0.00
+9, -8.90, 63.22, 0.00
+10, -8.98, 64.25, 0.00
+11, -8.98, 64.66, 0.00
+12, -8.87, 64.38, 0.00
+13, -8.68, 63.48, 0.00
+14, -8.39, 61.96, 0.00
+15, -8.03, 59.85, 0.00
+16, -7.61, 57.27, 0.00
+17, -7.12, 54.13, 0.00
+18, -6.57, 50.50, 0.00
+19, -5.97, 46.39, 0.00
+20, -5.32, 41.81, 0.00
+21, -4.63, 36.81, 0.00
+22, -3.90, 31.39, 0.00
+23, -3.13, 25.55, 0.00
+24, -2.34, 19.36, 0.00
+25, -1.53, 12.80, 0.00
+26, -0.69, 5.88, 0.00
+27, 0.16, -1.35, 0.00
+28, 1.02, -8.91, 0.00
+29, 1.88, -16.75, 0.00
+30, 2.74, -24.86, 0.00
+31, 3.61, -33.24, 0.00
+32, 4.46, -41.90, 0.00
+33, 5.31, -50.77, 0.00
+34, 6.14, -59.83, 0.00
+35, 6.95, -69.11, 0.00
+36, 7.73, -78.57, 0.00
+37, 8.48, -88.14, 0.00
+38, 9.19, -97.82, 0.00
+39, 9.86, -107.57, 0.00
+40, 10.47, -117.28, 0.00
+41, 11.01, -126.92, 0.00
+42, 11.49, -136.43, 0.00
+43, 11.87, -145.62, 0.00
+44, 12.15, -154.31, 0.00
+45, 12.30, -162.22, 0.00
+46, 12.31, -169.04, 0.00
+47, 12.11, -173.89, 0.00
+48, 11.66, -175.88, 0.00
+49, 11.13, -177.08, 0.00
+50, 10.20, -172.29, 0.00
+51, 6.86, -123.94, 0.00
+52, 5.97, -116.29, 0.00
+53, 21.77, -461.42, 0.00
+54, 26.12, -610.78, 0.00
+55, 21.89, -573.85, 0.00
+56, 18.71, -561.76, 0.00
+57, 15.72, -557.10, 0.00
+58, 12.57, -549.52, 0.00
+59, 9.33, -540.36, 0.00
+60, 6.04, -530.05, 0.00
+61, 2.71, -518.89, 0.00
+62, -0.62, -506.43, 0.00
+63, -3.95, -492.74, 0.00
+64, -7.24, -478.42, 0.00
+65, -10.47, -463.16, 0.00
+66, -13.60, -446.83, 0.00
+67, -16.63, -429.81, 0.00
+68, -19.50, -411.99, 0.00
+69, -22.22, -393.60, 0.00
+70, -24.75, -374.77, 0.00
+71, -27.06, -355.42, 0.00
+72, -29.14, -335.60, 0.00
+73, -30.94, -315.27, 0.00
+74, -32.45, -294.65, 0.00
+75, -33.65, -273.85, 0.00
+76, -34.49, -252.64, 0.00
+77, -34.95, -231.28, 0.00
+78, -35.02, -209.98, 0.00
+79, -34.64, -188.53, 0.00
+80, -33.79, -167.17, 0.00
+81, -32.42, -145.88, 0.00
+82, -30.48, -124.69, 0.00
+83, -27.91, -103.76, 0.00
+84, -24.63, -83.06, 0.00
+85, -20.55, -62.73, 0.00
+86, -15.56, -42.84, 0.00
+87, -9.50, -23.48, 0.00
+88, -2.17, -4.79, 0.00
+89, 6.62, 12.94, 0.00
+90, 17.16, 29.44, 0.00
+91, 29.73, 44.19, 0.00
+92, 44.58, 56.46, 0.00
+93, 61.71, 65.06, 0.00
+94, 81.10, 68.89, 0.00
+95, 101.88, 66.36, 0.00
+96, 122.09, 55.96, 0.00
+97, 139.13, 37.65, 0.00
+98, 108.84, 14.60, 0.00
+99, 71.28, -0.00, 0.00
+100, 106.29, -14.26, 0.00
+101, 130.33, -35.27, 0.00
+102, 108.14, -49.57, 0.00
+103, 84.37, -54.95, 0.00
+104, 61.43, -52.19, 0.00
+105, 40.94, -43.16, 0.00
+106, 23.22, -29.41, 0.00
+107, 8.42, -12.52, 0.00
+108, -3.78, 6.48, 0.00
+109, -13.76, 26.90, 0.00
+110, -21.85, 48.23, 0.00
+111, -28.39, 70.19, 0.00
+112, -33.65, 92.65, 0.00
+113, -37.82, 115.44, 0.00
+114, -41.08, 138.55, 0.00
+115, -43.55, 161.90, 0.00
+116, -45.31, 185.37, 0.00
+117, -46.46, 209.03, 0.00
+118, -47.03, 232.69, 0.00
+119, -47.10, 256.34, 0.00
+120, -46.71, 280.06, 0.00
+121, -45.86, 303.51, 0.00
+122, -44.63, 326.98, 0.00
+123, -43.04, 350.21, 0.00
+124, -41.06, 372.86, 0.00
+125, -38.81, 395.46, 0.00
+126, -36.30, 418.02, 0.00
+127, -33.51, 440.10, 0.00
+128, -30.48, 461.60, 0.00
+129, -27.23, 482.42, 0.00
+130, -23.80, 502.74, 0.00
+131, -20.21, 522.54, 0.00
+132, -16.49, 541.62, 0.00
+133, -12.66, 560.14, 0.00
+134, -8.74, 577.66, 0.00
+135, -4.77, 594.37, 0.00
+136, -0.75, 610.64, 0.00
+137, 3.27, 625.80, 0.00
+138, 7.29, 639.80, 0.00
+139, 11.28, 653.28, 0.00
+140, 15.23, 665.78, 0.00
+141, 19.09, 676.85, 0.00
+142, 22.88, 687.16, 0.00
+143, 26.58, 696.67, 0.00
+144, 30.15, 704.91, 0.00
+145, 33.58, 711.87, 0.00
+146, 36.88, 717.99, 0.00
+147, 40.04, 723.07, 0.00
+148, 43.03, 726.92, 0.00
+149, 45.86, 729.95, 0.00
+150, 48.47, 730.99, 0.00
+151, 50.57, 726.34, 0.00
+152, 54.71, 751.52, 0.00
+153, 52.81, 696.43, 0.00
+154, 5.64, 71.68, 0.00
+155, -0.65, -7.95, 0.00
+156, 3.46, 41.08, 0.00
+157, 3.63, 41.77, 0.00
+158, 4.01, 44.95, 0.00
+159, 4.28, 46.74, 0.00
+160, 4.32, 46.00, 0.00
+161, 4.21, 43.77, 0.00
+162, 3.98, 40.43, 0.00
+163, 3.64, 36.21, 0.00
+164, 3.22, 31.35, 0.00
+165, 2.72, 26.01, 0.00
+166, 2.16, 20.31, 0.00
+167, 1.56, 14.37, 0.00
+168, 0.92, 8.30, 0.00
+169, 0.24, 2.16, 0.00
+170, -0.45, -3.98, 0.00
+171, -1.16, -10.05, 0.00
+172, -1.88, -15.99, 0.00
+173, -2.60, -21.79, 0.00
+174, -3.31, -27.37, 0.00
+175, -4.00, -32.68, 0.00
+176, -4.69, -37.76, 0.00
+177, -5.34, -42.49, 0.00
+178, -5.96, -46.87, 0.00
+179, -6.55, -50.90, 0.00
+180, -7.09, -54.49, 0.00
+181, -7.59, -57.67, 0.00
+182, -8.03, -60.38, 0.00
+183, -8.40, -62.58, 0.00
+184, -8.72, -64.34, 0.00
+185, -8.96, -65.53, 0.00
+186, -9.11, -66.13, 0.00
+187, -9.18, -66.13, 0.00
+188, -9.15, -65.46, 0.00
+189, -9.04, -64.19, 0.00
+190, -8.81, -62.24, 0.00
+191, -8.48, -59.55, 0.00
+192, -8.02, -56.09, 0.00
+193, -7.44, -51.78, 0.00
+194, -6.74, -46.74, 0.00
+195, -5.87, -40.64, 0.00
+196, -4.83, -33.31, 0.00
+197, -3.59, -24.74, 0.00
+198, -1.96, -13.51, 0.00

From 4a5d80a6d28d90181e49a0c4f58537daa45bf462 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Tue, 9 May 2023 10:03:07 +0200
Subject: [PATCH 435/656] Aplly sugestion form Code scanning / CodeQL

---
 TestCases/py_wrapper/updated_moving_frame_NACA12/run_su2.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/py_wrapper/updated_moving_frame_NACA12/run_su2.py b/TestCases/py_wrapper/updated_moving_frame_NACA12/run_su2.py
index 7a63380137d..c3f73a190fe 100644
--- a/TestCases/py_wrapper/updated_moving_frame_NACA12/run_su2.py
+++ b/TestCases/py_wrapper/updated_moving_frame_NACA12/run_su2.py
@@ -1,7 +1,7 @@
 import sys
 import numpy as np
 from mpi4py import MPI
-import SU2, pysu2
+import pysu2
 
 """
 This test case updates the translation and rotation rates given in the config file via the python wrapper

From 04f5e1abde63a87e0b46846a3f3ee1dd23604030 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Thu, 11 May 2023 15:49:02 +0200
Subject: [PATCH 436/656] Simplified Newton solver process in data-driven fluid
 model

---
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp  |  68 +++--
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp      | 295 +++++++-------------
 SU2_CFD/src/solvers/CEulerSolver.cpp        |  29 +-
 SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp |  20 ++
 4 files changed, 188 insertions(+), 224 deletions(-)

diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index e0faeb132d6..0d6cdb78d4a 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -46,17 +46,20 @@
 class CDataDrivenFluid final : public CFluidModel {
  protected:
   int rank{MASTER_NODE}; /*!< \brief MPI Rank. */
-  ENUM_DATADRIVEN_METHOD Kind_DataDriven_Method = ENUM_DATADRIVEN_METHOD::LUT;  /*!< \brief Interpolation method for data set evaluation. */
+  ENUM_DATADRIVEN_METHOD Kind_DataDriven_Method =
+      ENUM_DATADRIVEN_METHOD::LUT; /*!< \brief Interpolation method for data set evaluation. */
 
-  size_t idx_rho,  /*!< \brief Interpolator index for density input. */
-      idx_e;       /*!< \brief Interpolator index for energy input. */
+  size_t idx_rho, /*!< \brief Interpolator index for density input. */
+      idx_e;      /*!< \brief Interpolator index for energy input. */
 
-  su2double Newton_Relaxation,  /*!< \brief Relaxation factor for Newton solvers. */
-      rho_start,                /*!< \brief Initial value for the density in Newton solver processes. */
-      e_start,                  /*!< \brief Initial value for the energy in Newton solver processes. */
-      Newton_Tolerance;         /*!< \brief Normalized tolerance for Newton solvers. */
+  su2double Newton_Relaxation, /*!< \brief Relaxation factor for Newton solvers. */
+      rho_start,               /*!< \brief Starting value for the density in Newton solver processes. */
+      e_start,                 /*!< \brief Starting value for the energy in Newton solver processes. */
+      rho_init,                /*!< \brief Initial value for the density from config. */
+      e_init,                  /*!< \brief Initial value for the energy from config. */
+      Newton_Tolerance;        /*!< \brief Normalized tolerance for Newton solvers. */
 
-  unsigned long MaxIter_Newton;  /*!< \brief Maximum number of iterations for Newton solvers. */
+  unsigned long MaxIter_Newton; /*!< \brief Maximum number of iterations for Newton solvers. */
 
   su2double dsde_rho, /*!< \brief Entropy derivative w.r.t. density. */
       dsdrho_e,       /*!< \brief Entropy derivative w.r.t. static energy. */
@@ -64,23 +67,29 @@ class CDataDrivenFluid final : public CFluidModel {
       d2sdedrho,      /*!< \brief Entropy second derivative w.r.t. density and static energy. */
       d2sdrho2;       /*!< \brief Entropy second derivative w.r.t. static density. */
 
-  vector<string>
-      input_names_rhoe,   /*!< \brief Data-driven method input variable names of the independent variables (density, energy). */
-      output_names_rhoe;  /*!< \brief Output variable names listed in the data-driven method input file name. */
+  su2double Enthalpy, /*!< \brief Fluid enthalpy value [J kg^-1] */
+      dhdrho_e,       /*!< \brief Enthalpy derivative w.r.t. density. */
+      dhde_rho;       /*!< \brief Enthalpy derivative w.r.t. static energy. */
 
-  vector<su2double*> outputs_rhoe;  /*!< \brief Pointers to output variables. */
+  vector<string> input_names_rhoe, /*!< \brief Data-driven method input variable names of the independent variables
+                                      (density, energy). */
+      output_names_rhoe; /*!< \brief Output variable names listed in the data-driven method input file name. */
+
+  vector<su2double*> outputs_rhoe; /*!< \brief Pointers to output variables. */
+
+  bool set_local_rhoe = false;
 
   /*--- Class variables for the multi-layer perceptron method ---*/
 #ifdef USE_MLPCPP
-  MLPToolbox::CLookUp_ANN* lookup_mlp;  /*!< \brief Multi-layer perceptron collection. */
-  MLPToolbox::CIOMap* iomap_rhoe;       /*!< \brief Input-output map. */
+  MLPToolbox::CLookUp_ANN* lookup_mlp; /*!< \brief Multi-layer perceptron collection. */
+  MLPToolbox::CIOMap* iomap_rhoe;      /*!< \brief Input-output map. */
 #endif
-  vector<su2double> MLP_inputs;  /*!< \brief Inputs for the multi-layer perceptron look-up operation. */
+  vector<su2double> MLP_inputs; /*!< \brief Inputs for the multi-layer perceptron look-up operation. */
 
   CLookUpTable* lookup_table; /*!< \brief Look-up table regression object. */
 
-  unsigned long outside_dataset,  /*!< \brief Density-energy combination lies outside data set. */
-      nIter_Newton;               /*!< \brief Number of Newton solver iterations. */
+  unsigned long outside_dataset, /*!< \brief Density-energy combination lies outside data set. */
+      nIter_Newton;              /*!< \brief Number of Newton solver iterations. */
 
   /*!
    * \brief Map dataset variables to specific look-up operations.
@@ -110,11 +119,34 @@ class CDataDrivenFluid final : public CFluidModel {
    */
   void Evaluate_Dataset(su2double rho, su2double e);
 
+  /*!
+   * \brief 2D Newton solver for computing the density and energy corresponding to Y1_target and Y2_target.
+   * \param[in] Y1_target - Target value for output quantity 1.
+   * \param[in] Y2_target - Target value for output quantity 2.
+   * \param[in] Y1 - Pointer to output quantity 1.
+   * \param[in] Y2 - Pointer to output quantity 2.
+   * \param[in] dY1drho - Pointer to the partial derivative of quantity 1 w.r.t. density at constant energy.
+   * \param[in] dY1de - Pointer to the partial derivative of quantity 1 w.r.t. energy at constant density.
+   * \param[in] dY2drho - Pointer to the partial derivative of quantity 2 w.r.t. density at constant energy.
+   * \param[in] dY2de - Pointer to the partial derivative of quantity 2 w.r.t. energy at constant density.
+   */
+  void Run_Newton_Solver(su2double Y1_target, su2double Y2_target, su2double* Y1, su2double* Y2, su2double* dY1drho,
+                         su2double* dY1de, su2double* dY2drho, su2double* dY2de);
+
+  /*!
+   * \brief 1D Newton solver for computing the density or energy corresponding to Y_target.
+   * \param[in] Y_target - Target quantity value.
+   * \param[in] Y - Pointer to output quantity.
+   * \param[in] X - Pointer to controlling variable (density or energy).
+   * \param[in] dYdX - Pointer to the partial derivative of target quantity w.r.t. controlling variable.
+   */
+  void Run_Newton_Solver(su2double Y_target, su2double* Y, su2double* X, su2double* dYdX);
+
  public:
   /*!
    * \brief Constructor of the class.
    */
-  CDataDrivenFluid(const CConfig* config, bool display=true);
+  CDataDrivenFluid(const CConfig* config, bool display = true);
 
   ~CDataDrivenFluid();
   /*!
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 64cf0b27409..9e79ab69a0e 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -61,8 +61,12 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config, bool display) : CFluid
   MapInputs_to_Outputs();
 
   /*--- Set initial values for density and energy based on config options. ---*/
-  rho_start = config->GetDensity_Init_DataDriven();
-  e_start = config->GetEnergy_Init_DataDriven();
+  rho_init = config->GetDensity_Init_DataDriven();
+  e_init = config->GetEnergy_Init_DataDriven();
+
+  /*--- Set default Newton solver density and energy values. ---*/
+  rho_start = rho_init;
+  e_start = e_init;
 }
 
 CDataDrivenFluid::~CDataDrivenFluid() {
@@ -121,7 +125,6 @@ void CDataDrivenFluid::MapInputs_to_Outputs() {
 
 void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
   /*--- Compute thermodynamic state based on density and energy. ---*/
-
   Density = rho;
   StaticEnergy = e;
 
@@ -138,6 +141,7 @@ void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
   Pressure = -pow(rho, 2) * Temperature * dsdrho_e;
   Density = rho;
   StaticEnergy = e;
+  Enthalpy = e + Pressure / rho;
 
   /*--- Compute secondary flow variables ---*/
   dTde_rho = -pow(dsde_rho, -2) * d2sde2;
@@ -147,171 +151,129 @@ void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
   dPdrho_e = -2 * rho * Temperature * dsdrho_e - pow(rho, 2) * (dTdrho_e * dsdrho_e + Temperature * d2sdrho2);
 
   /*--- Compute enthalpy and entropy derivatives required for Giles boundary conditions. ---*/
-  su2double dhdrho_e = -Pressure * pow(rho, -2) + dPdrho_e / rho;
-  su2double dhde_rho = 1 + dPde_rho / rho;
+  dhdrho_e = -Pressure * pow(rho, -2) + dPdrho_e / rho;
+  dhde_rho = 1 + dPde_rho / rho;
 
   dhdrho_P = dhdrho_e - dhde_rho * (1 / dPde_rho) * dPdrho_e;
   dhdP_rho = dhde_rho * (1 / dPde_rho);
   dsdrho_P = dsdrho_e - dPdrho_e * (1 / dPde_rho) * dsde_rho;
   dsdP_rho = dsde_rho / dPde_rho;
-}
-
-void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
-  /*--- Setting initial values for density and energy. ---*/
-  su2double rho = rho_start, e = e_start;
-
-  bool converged = false;
-  unsigned long Iter = 0;
 
-  su2double delta_P,
-      delta_T,    
-      delta_rho,
-      delta_e,
-      determinant;
-  /*--- Initiating Newton solver ---*/
-  while (!converged && (Iter < MaxIter_Newton)) {
-    /*--- Determine thermodynamic state based on current density and energy. ---*/
-    SetTDState_rhoe(rho, e);
-
-    /*--- Determine pressure and temperature residuals. ---*/
-    delta_P = Pressure - P;
-    delta_T = Temperature - T;
-    /*--- Continue iterative process if residuals are outside tolerances. ---*/
-    if ((abs(delta_P / P) < Newton_Tolerance) && (abs(delta_T / T) < Newton_Tolerance)) {
-      converged = true;
-    } else {
-      /*--- Compute step size for density and energy. ---*/
-      determinant = dPdrho_e * dTde_rho - dPde_rho * dTdrho_e;
-
-      delta_rho = (dTde_rho * delta_P - dPde_rho * delta_T) / determinant;
-      delta_e = (-dTdrho_e * delta_P + dPdrho_e * delta_T) / determinant;
-
-      /*--- Update density and energy values ---*/
-      rho -= Newton_Relaxation * delta_rho;
-      e -= Newton_Relaxation * delta_e;
-    }
-    Iter++;
+  if (set_local_rhoe) {
+    rho_start = Newton_Relaxation * Density + (1 - Newton_Relaxation) * rho_init;
+    e_start = Newton_Relaxation * StaticEnergy + (1 - Newton_Relaxation) * e_init;
   }
+}
 
-  /*--- Calculate thermodynamic state based on converged values for density and energy. ---*/
-  SetTDState_rhoe(rho, e);
-
-  nIter_Newton = Iter;
+void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
+  /*--- Run 2D Newton solver for pressure and temperature ---*/
+  Run_Newton_Solver(P, T, &Pressure, &Temperature, &dPdrho_e, &dPde_rho, &dTdrho_e, &dTde_rho);
 }
 
 void CDataDrivenFluid::SetTDState_Prho(su2double P, su2double rho) {
   /*--- Computing static energy according to pressure and density. ---*/
   SetEnergy_Prho(P, rho);
-
-  /*--- Calculate thermodynamic state based on converged value for energy. ---*/
-  SetTDState_rhoe(rho, StaticEnergy);
 }
 
 void CDataDrivenFluid::SetEnergy_Prho(su2double P, su2double rho) {
-  /*--- Setting initial values for energy. ---*/
-  su2double e = e_start;
-
-  bool converged = false;
-  unsigned long Iter = 0;
-
-  su2double delta_P,
-      delta_e;
-
-  while (!converged && (Iter < MaxIter_Newton)) {
-    /*--- Determine thermodynamic state based on current density and energy. ---*/
-    SetTDState_rhoe(rho, e);
-
-    /*--- Determine pressure and temperature residuals. ---*/
-    delta_P = Pressure - P;
-
-    /*--- Continue iterative process if residuals are outside tolerances. ---*/
-    if (abs(delta_P / P) < Newton_Tolerance) {
-      converged = true;
-    } else {
-      /*--- Compute step size for energy. ---*/
-      delta_e = delta_P / dPde_rho;
-
-      /*--- Update energy value. ---*/
-      e -= Newton_Relaxation * delta_e;
-    }
-    Iter++;
-  }
-
-  /*--- Setting static energy as the converged value. ---*/
-  StaticEnergy = e;
-
-  nIter_Newton = Iter;
+  /*--- Run 1D Newton solver for pressure at constant density. ---*/
+  Density = rho;
+  StaticEnergy = e_start;
+  Run_Newton_Solver(P, &Pressure, &StaticEnergy, &dPde_rho);
 }
 
 void CDataDrivenFluid::SetTDState_rhoT(su2double rho, su2double T) {
-  /*--- Setting initial values for density and energy. ---*/
-  su2double e = e_start;
-
-  bool converged = false;
-  unsigned long Iter = 0;
+  /*--- Run 1D Newton solver for temperature at constant density. ---*/
+  Density = rho;
+  StaticEnergy = e_start;
+  Run_Newton_Solver(T, &Temperature, &StaticEnergy, &dTde_rho);
+}
 
-  su2double delta_T,
-      delta_e;
+void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
+  /*--- Run 2D Newton solver for enthalpy and entropy. ---*/
+  Run_Newton_Solver(h, s, &Enthalpy, &Entropy, &dhdrho_e, &dhde_rho, &dsdrho_e, &dsde_rho);
+}
 
-  /*--- Initiating Newton solver. ---*/
-  while (!converged && (Iter < MaxIter_Newton)) {
-    /*--- Determine thermodynamic state based on current density and energy. ---*/
-    SetTDState_rhoe(rho, e);
+void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
+  /*--- Run 2D Newton solver for pressure and entropy ---*/
+  Run_Newton_Solver(P, s, &Pressure, &Entropy, &dPdrho_e, &dPde_rho, &dsdrho_e, &dsde_rho);
+}
 
-    /*--- Determine temperature residual ---*/
-    delta_T = Temperature - T;
+unsigned long CDataDrivenFluid::Predict_MLP(su2double rho, su2double e) {
+  unsigned long exit_code = 0;
+/*--- Evaluate MLP collection for the given values for density and energy. ---*/
+#ifdef USE_MLPCPP
+  MLP_inputs[idx_rho] = rho;
+  MLP_inputs[idx_e] = e;
+  exit_code = lookup_mlp->PredictANN(iomap_rhoe, MLP_inputs, outputs_rhoe);
+#endif
+  return exit_code;
+}
 
-    /*--- Continue iterative process if residuals are outside tolerances. ---*/
-    if (abs(delta_T / T) < Newton_Tolerance) {
-      converged = true;
-    } else {
-      delta_e = delta_T / dTde_rho;
+unsigned long CDataDrivenFluid::Predict_LUT(su2double rho, su2double e) {
+  unsigned long exit_code;
+  std::vector<std::string> output_names_rhoe_LUT;
+  std::vector<su2double*> outputs_LUT;
+  output_names_rhoe_LUT.resize(output_names_rhoe.size());
+  for (auto iOutput = 0u; iOutput < output_names_rhoe.size(); iOutput++) {
+    output_names_rhoe_LUT[iOutput] = output_names_rhoe[iOutput];
+  }
 
-      /*--- Update energy value ---*/
-      e -= Newton_Relaxation * delta_e;
-    }
-    Iter++;
+  outputs_LUT.resize(outputs_rhoe.size());
+  for (auto iOutput = 0u; iOutput < outputs_rhoe.size(); iOutput++) {
+    outputs_LUT[iOutput] = outputs_rhoe[iOutput];
   }
 
-  /*--- Calculate thermodynamic state based on converged values for density and energy. ---*/
-  SetTDState_rhoe(rho, e);
+  exit_code = lookup_table->LookUp_XY(output_names_rhoe_LUT, outputs_LUT, rho, e);
+  return exit_code;
+}
 
-  nIter_Newton = Iter;
+void CDataDrivenFluid::Evaluate_Dataset(su2double rho, su2double e) {
+  /*--- Evaluate dataset based on regression method. ---*/
+  switch (Kind_DataDriven_Method) {
+    case ENUM_DATADRIVEN_METHOD::LUT:
+      outside_dataset = Predict_LUT(rho, e);
+      break;
+    case ENUM_DATADRIVEN_METHOD::MLP:
+      outside_dataset = Predict_MLP(rho, e);
+      break;
+    default:
+      break;
+  }
 }
 
-void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
+void CDataDrivenFluid::Run_Newton_Solver(su2double Y1_target, su2double Y2_target, su2double* Y1, su2double* Y2,
+                                         su2double* dY1drho, su2double* dY1de, su2double* dY2drho, su2double* dY2de) {
+  /*--- 2D Newton solver, computing the density and internal energy values corresponding to Y1_target and Y2_target.
+   * ---*/
+
   /*--- Setting initial values for density and energy. ---*/
   su2double rho = rho_start, e = e_start;
 
   bool converged = false;
   unsigned long Iter = 0;
 
-  su2double delta_h,
-      delta_s,
-      delta_rho,
-      delta_e,
-      determinant;
+  su2double delta_Y1, delta_Y2, delta_rho, delta_e, determinant;
 
-  /*--- Initiating Newton solver. ---*/
+  set_local_rhoe = false;
+  /*--- Initiating Newton solver ---*/
   while (!converged && (Iter < MaxIter_Newton)) {
     /*--- Determine thermodynamic state based on current density and energy. ---*/
     SetTDState_rhoe(rho, e);
 
-    su2double Enthalpy = e + Pressure / rho;
-    /*--- Determine pressure and temperature residuals. ---*/
-    delta_h = Enthalpy - h;
-    delta_s = Entropy - s;
+    /*--- Determine residuals. ---*/
+    delta_Y1 = *Y1 - Y1_target;
+    delta_Y2 = *Y2 - Y2_target;
 
     /*--- Continue iterative process if residuals are outside tolerances. ---*/
-    if ((abs(delta_h / h) < Newton_Tolerance) && (abs(delta_s / s) < Newton_Tolerance)) {
+    if ((abs(delta_Y1 / *Y1) < Newton_Tolerance) && (abs(delta_Y2 / *Y2) < Newton_Tolerance)) {
       converged = true;
     } else {
-      su2double dh_de = 1 + dPde_rho / rho;
-      su2double dh_drho = -Pressure * pow(rho, -2) + dPdrho_e / rho;
+      /*--- Compute step size for density and energy. ---*/
+      determinant = (*dY1drho) * (*dY2de) - (*dY1de) * (*dY2drho);
 
-      determinant = dh_drho * dsde_rho - dh_de * dsdrho_e;
-      delta_rho = (dsde_rho * delta_h - dh_de * delta_s) / determinant;
-      delta_e = (-dsdrho_e * delta_h + dh_drho * delta_s) / determinant;
+      delta_rho = (*dY2de * delta_Y1 - *dY1de * delta_Y2) / determinant;
+      delta_e = (-*dY2drho * delta_Y1 + *dY1drho * delta_Y2) / determinant;
 
       /*--- Update density and energy values. ---*/
       rho -= Newton_Relaxation * delta_rho;
@@ -319,96 +281,45 @@ void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
     }
     Iter++;
   }
-  /*--- Calculate thermodynamic state based on converged values for density and energy. ---*/
-  SetTDState_rhoe(rho, e);
-
   nIter_Newton = Iter;
+
+  /*--- Evaluation of final state. ---*/
+  Density = rho;
+  StaticEnergy = e;
+  SetTDState_rhoe(Density, StaticEnergy);
+  set_local_rhoe = true;
 }
 
-void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
-  /*--- Setting initial values for density and energy. ---*/
-  su2double rho = rho_start, e = e_start;
+void CDataDrivenFluid::Run_Newton_Solver(su2double Y_target, su2double* Y, su2double* X, su2double* dYdX) {
+  /*--- 1D Newton solver, computing the density or internal energy value corresponding to Y_target. ---*/
 
   bool converged = false;
   unsigned long Iter = 0;
 
-  su2double delta_P,
-      delta_s,
-      delta_rho,
-      delta_e,
-      determinant;
+  su2double delta_Y, delta_X;
 
-  /*--- Initiating Newton solver ---*/
+  /*--- Initiating Newton solver. ---*/
   while (!converged && (Iter < MaxIter_Newton)) {
     /*--- Determine thermodynamic state based on current density and energy. ---*/
-    SetTDState_rhoe(rho, e);
+    SetTDState_rhoe(Density, StaticEnergy);
 
-    /*--- Determine pressure and temperature residuals. ---*/
-    delta_P = Pressure - P;
-    delta_s = Entropy - s;
+    /*--- Determine residual ---*/
+    delta_Y = Y_target - *Y;
 
     /*--- Continue iterative process if residuals are outside tolerances. ---*/
-    if ((abs(delta_P / P) < Newton_Tolerance) && (abs(delta_s / s) < Newton_Tolerance)) {
+    if (abs(delta_Y / *Y) < Newton_Tolerance) {
       converged = true;
     } else {
-      /*--- Compute step size for density and energy. ---*/
-      determinant = dPdrho_e * dsde_rho - dPde_rho * dsdrho_e;
-
-      delta_rho = (dsde_rho * delta_P - dPde_rho * delta_s) / determinant;
-      delta_e = (-dsdrho_e * delta_P + dPdrho_e * delta_s) / determinant;
+      delta_X = delta_Y / *dYdX;
 
-      /*--- Update density and energy values. ---*/
-      rho -= Newton_Relaxation * delta_rho;
-      e -= Newton_Relaxation * delta_e;
+      /*--- Update energy value ---*/
+      *X += Newton_Relaxation * delta_X;
     }
     Iter++;
   }
 
   /*--- Calculate thermodynamic state based on converged values for density and energy. ---*/
-  SetTDState_rhoe(rho, e);
+  SetTDState_rhoe(Density, StaticEnergy);
 
   nIter_Newton = Iter;
 }
-
-unsigned long CDataDrivenFluid::Predict_MLP(su2double rho, su2double e) {
-  unsigned long exit_code = 0;
-/*--- Evaluate MLP collection for the given values for density and energy. ---*/
-#ifdef USE_MLPCPP
-  MLP_inputs[idx_rho] = rho;
-  MLP_inputs[idx_e] = e;
-  exit_code = lookup_mlp->PredictANN(iomap_rhoe, MLP_inputs, outputs_rhoe);
-#endif
-  return exit_code;
-}
-
-unsigned long CDataDrivenFluid::Predict_LUT(su2double rho, su2double e) {
-  unsigned long exit_code;
-  std::vector<std::string> output_names_rhoe_LUT;
-  std::vector<su2double*> outputs_LUT;
-  output_names_rhoe_LUT.resize(output_names_rhoe.size());
-  for (auto iOutput = 0u; iOutput < output_names_rhoe.size(); iOutput++) {
-    output_names_rhoe_LUT[iOutput] = output_names_rhoe[iOutput];
-  }
-
-  outputs_LUT.resize(outputs_rhoe.size());
-  for (auto iOutput = 0u; iOutput < outputs_rhoe.size(); iOutput++) {
-    outputs_LUT[iOutput] = outputs_rhoe[iOutput];
-  }
-
-  exit_code = lookup_table->LookUp_XY(output_names_rhoe_LUT, outputs_LUT, rho, e);
-  return exit_code;
-}
-
-void CDataDrivenFluid::Evaluate_Dataset(su2double rho, su2double e) {
-  /*--- Evaluate dataset based on regression method. ---*/
-  switch (Kind_DataDriven_Method) {
-    case ENUM_DATADRIVEN_METHOD::LUT:
-      outside_dataset = Predict_LUT(rho, e);
-      break;
-    case ENUM_DATADRIVEN_METHOD::MLP:
-      outside_dataset = Predict_MLP(rho, e);
-      break;
-    default:
-      break;
-  }
-}
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index 209125a96ad..5183e83dd7b 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -4677,13 +4677,6 @@ void CEulerSolver::BC_Riemann(CGeometry *geometry, CSolver **solver_container,
       StaticEnergy_i = Energy_i - 0.5*Velocity2_i;
 
       GetFluidModel()->SetTDState_rhoe(Density_i, StaticEnergy_i);
-
-      /*--- Set initial values for density and energy for Newton solvers in fluid model ---*/
-      if(config->GetKind_FluidModel() == DATADRIVEN_FLUID){
-        su2double relax_Newton = config->GetRelaxation_DataDriven();
-        GetFluidModel()->SetInitialDensity(relax_Newton*Density_i + (1 - relax_Newton)*config->GetDensity_Init_DataDriven());
-        GetFluidModel()->SetInitialEnergy(relax_Newton*StaticEnergy_i + (1 - relax_Newton)*config->GetEnergy_Init_DataDriven());
-      }
       
       Pressure_i = GetFluidModel()->GetPressure();
       Enthalpy_i = Energy_i + Pressure_i/Density_i;
@@ -5673,6 +5666,15 @@ void CEulerSolver::PreprocessBC_Giles(CGeometry *geometry, CConfig *config, CNum
                 {
                   Velocity_i[iDim] = nodes->GetVelocity(iPoint,iDim);
                 }
+
+                /*--- Set Newton solver starting point in case of data-driven fluid model. ---*/
+                if (config->GetKind_FluidModel() == DATADRIVEN_FLUID){
+                  su2double Velocity2_i = GeometryToolbox::SquaredNorm(nDim, Velocity_i);
+                  su2double Energy_i = nodes->GetEnergy(iPoint);
+                  su2double StaticEnergy_i = Energy_i - 0.5*Velocity2_i;
+                  GetFluidModel()->SetTDState_rhoe(AverageDensity[iMarker][iSpan], StaticEnergy_i);
+                }
+                
                 ComputeTurboVelocity(Velocity_i, turboNormal, turboVelocity, marker_flag, config->GetKind_TurboMachinery(iZone));
 
                 if(nDim ==2){
@@ -5890,6 +5892,12 @@ void CEulerSolver::BC_Giles(CGeometry *geometry, CSolver **solver_container, CNu
       }
     }
 
+    /*--- Set Newton solver starting point in case of data-driven fluid model. ---*/
+    if (config->GetKind_FluidModel() == DATADRIVEN_FLUID){
+      GetFluidModel()->SetInitialDensity(AverageDensity[val_marker][iSpan]);
+      GetFluidModel()->SetInitialEnergy(config->GetEnergy_Init_DataDriven());
+    }
+
     GetFluidModel()->SetTDState_Prho(AveragePressure[val_marker][iSpan], AverageDensity[val_marker][iSpan]);
     AverageSoundSpeed = GetFluidModel()->GetSoundSpeed();
     AverageTurboMach[0] = AverageTurboVelocity[val_marker][iSpan][0]/AverageSoundSpeed;
@@ -6147,13 +6155,6 @@ void CEulerSolver::BC_Giles(CGeometry *geometry, CSolver **solver_container, CNu
       Energy_i = nodes->GetEnergy(iPoint);
       StaticEnergy_i = Energy_i - 0.5*Velocity2_i;
 
-      if (config->GetKind_FluidModel() == DATADRIVEN_FLUID) {
-        /*--- Set initial values for density and energy for Newton solvers in fluid model ---*/
-        su2double relax_Newton = config->GetRelaxation_DataDriven();
-        GetFluidModel()->SetInitialDensity(relax_Newton*Density_i + (1 - relax_Newton)*config->GetDensity_Init_DataDriven());
-        GetFluidModel()->SetInitialEnergy(relax_Newton*StaticEnergy_i + (1 - relax_Newton)*config->GetEnergy_Init_DataDriven());
-      }
-
       GetFluidModel()->SetTDState_rhoe(Density_i, StaticEnergy_i);
 
       Pressure_i = GetFluidModel()->GetPressure();
diff --git a/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp b/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
index 877611c3787..fc4a7a92e36 100644
--- a/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
@@ -32,6 +32,7 @@
 #include "../../include/fluid/CVanDerWaalsGas.hpp"
 #include "../../include/fluid/CPengRobinson.hpp"
 #include "../../include/fluid/CCoolProp.hpp"
+#include "../../include/fluid/CDataDrivenFluid.hpp"
 
 enum {
 SIZE_ARR_NORM = 8
@@ -897,6 +898,20 @@ void CFEM_DG_EulerSolver::SetNondimensionalization(CConfig        *config,
       }
       break;
 
+    case DATADRIVEN_FLUID:
+      FluidModel = new CDataDrivenFluid(config, false);
+      if (free_stream_temp) {
+        FluidModel->SetTDState_PT(Pressure_FreeStream, Temperature_FreeStream);
+        Density_FreeStream = FluidModel->GetDensity();
+        config->SetDensity_FreeStream(Density_FreeStream);
+      }
+      else {
+        FluidModel->SetTDState_Prho(Pressure_FreeStream, Density_FreeStream );
+        Temperature_FreeStream = FluidModel->GetTemperature();
+        config->SetTemperature_FreeStream(Temperature_FreeStream);
+      }
+
+      break;
   }
 
   Mach2Vel_FreeStream = FluidModel->GetSoundSpeed();
@@ -1085,6 +1100,11 @@ void CFEM_DG_EulerSolver::SetNondimensionalization(CConfig        *config,
       FluidModel = new CCoolProp(config->GetFluid_Name());
       FluidModel->SetEnergy_Prho(Pressure_FreeStreamND, Density_FreeStreamND);
       break;
+
+    case DATADRIVEN_FLUID:
+      FluidModel = new CDataDrivenFluid(config);
+      FluidModel->SetEnergy_Prho(Pressure_FreeStreamND, Density_FreeStreamND);
+      break;
   }
 
   Energy_FreeStreamND = FluidModel->GetStaticEnergy() + 0.5*ModVel_FreeStreamND*ModVel_FreeStreamND;

From c8c7931bfe58c725362297b762c307ea2d058d67 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?=
 <96138805+ArneVoss@users.noreply.github.com>
Date: Fri, 12 May 2023 10:43:16 +0200
Subject: [PATCH 437/656] Undoing 28f4133 as rotations are always in rad/s

Co-authored-by: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
---
 Common/src/geometry/CGeometry.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/Common/src/geometry/CGeometry.cpp b/Common/src/geometry/CGeometry.cpp
index ef0ff2cf0de..cc5c84e54f3 100644
--- a/Common/src/geometry/CGeometry.cpp
+++ b/Common/src/geometry/CGeometry.cpp
@@ -3443,7 +3443,7 @@ void CGeometry::SetRotationalVelocity(const CConfig* config, bool print) {
     cout << " Rotational origin (x, y, z): ( " << Center[0] << ", " << Center[1];
     cout << ", " << Center[2] << " )\n";
     cout << " Angular velocity about x, y, z axes: ( " << Omega[0] << ", ";
-    cout << Omega[1] << ", " << Omega[2] << " )" << endl;
+    cout << Omega[1] << ", " << Omega[2] << " ) rad/s" << endl;
     cout << " Translational velocity in x, y, z direction: (" << xDot[0] << ", " << xDot[1] << ", " << xDot[2] << ")."
          << endl;
   }

From 4f00bcce1bf5b7eb42c6aafcb9f5dff9ead4dbd6 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Fri, 12 May 2023 11:05:00 +0200
Subject: [PATCH 438/656] Removing print messages from python interface.

---
 SU2_CFD/src/python_wrapper_structure.cpp | 6 ------
 1 file changed, 6 deletions(-)

diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index a70311d0318..f470bc03564 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -142,9 +142,6 @@ void CDriver::BoundaryConditionsUpdate() {
 ////////////////////////////////////////////////////////////////////////////////
 
 void CDriver::SetTranslationRate(passivedouble xDot, passivedouble yDot, passivedouble zDot) {
-  if (rank == MASTER_NODE) {
-    cout << endl << " Setting new translational velocity in x, y, z direction.";
-  }
   for (iZone = 0; iZone < nZone; iZone++) {
     config_container[iZone]->SetTranslation_Rate(0, xDot);
     config_container[iZone]->SetTranslation_Rate(1, yDot);
@@ -153,9 +150,6 @@ void CDriver::SetTranslationRate(passivedouble xDot, passivedouble yDot, passive
 }
 
 void CDriver::SetRotationRate(passivedouble rot_x, passivedouble rot_y, passivedouble rot_z) {
-  if (rank == MASTER_NODE) {
-    cout << endl << " Setting new angular velocity about x, y, z axes.";
-  }
   for (iZone = 0; iZone < nZone; iZone++) {
     config_container[iZone]->SetRotation_Rate(0, rot_x);
     config_container[iZone]->SetRotation_Rate(1, rot_y);

From cdd2e610ff64c07201aef474a072072c5b5903d4 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Fri, 12 May 2023 11:06:51 +0200
Subject: [PATCH 439/656] Removing reference results file for ARM64

---
 .../forces_0_aarch64.csv.ref                  | 200 ------------------
 1 file changed, 200 deletions(-)
 delete mode 100644 TestCases/py_wrapper/translating_NACA0012/forces_0_aarch64.csv.ref

diff --git a/TestCases/py_wrapper/translating_NACA0012/forces_0_aarch64.csv.ref b/TestCases/py_wrapper/translating_NACA0012/forces_0_aarch64.csv.ref
deleted file mode 100644
index ba1b413acde..00000000000
--- a/TestCases/py_wrapper/translating_NACA0012/forces_0_aarch64.csv.ref
+++ /dev/null
@@ -1,200 +0,0 @@
-199, -1.01, -0.00, 0.00
-0, -2.07, 14.25, 0.00
-1, -3.62, 24.97, 0.00
-2, -4.84, 33.38, 0.00
-3, -5.85, 40.49, 0.00
-4, -6.69, 46.42, 0.00
-5, -7.36, 51.26, 0.00
-6, -7.92, 55.36, 0.00
-7, -8.34, 58.59, 0.00
-8, -8.64, 61.04, 0.00
-9, -8.83, 62.73, 0.00
-10, -8.91, 63.73, 0.00
-11, -8.90, 64.10, 0.00
-12, -8.79, 63.80, 0.00
-13, -8.59, 62.88, 0.00
-14, -8.31, 61.35, 0.00
-15, -7.95, 59.25, 0.00
-16, -7.53, 56.67, 0.00
-17, -7.05, 53.55, 0.00
-18, -6.50, 49.94, 0.00
-19, -5.90, 45.87, 0.00
-20, -5.26, 41.32, 0.00
-21, -4.57, 36.38, 0.00
-22, -3.85, 31.01, 0.00
-23, -3.09, 25.23, 0.00
-24, -2.31, 19.12, 0.00
-25, -1.51, 12.63, 0.00
-26, -0.68, 5.79, 0.00
-27, 0.16, -1.36, 0.00
-28, 1.01, -8.84, 0.00
-29, 1.86, -16.61, 0.00
-30, 2.72, -24.66, 0.00
-31, 3.58, -32.98, 0.00
-32, 4.43, -41.60, 0.00
-33, 5.28, -50.47, 0.00
-34, 6.11, -59.56, 0.00
-35, 6.93, -68.92, 0.00
-36, 7.73, -78.52, 0.00
-37, 8.50, -88.30, 0.00
-38, 9.24, -98.33, 0.00
-39, 9.95, -108.57, 0.00
-40, 10.62, -118.95, 0.00
-41, 11.24, -129.51, 0.00
-42, 11.81, -140.28, 0.00
-43, 12.33, -151.22, 0.00
-44, 12.78, -162.28, 0.00
-45, 13.15, -173.40, 0.00
-46, 13.44, -184.61, 0.00
-47, 13.64, -195.87, 0.00
-48, 13.73, -207.12, 0.00
-49, 13.72, -218.38, 0.00
-50, 13.58, -229.47, 0.00
-51, 13.30, -240.11, 0.00
-52, 12.85, -250.14, 0.00
-53, 12.31, -261.02, 0.00
-54, 11.62, -271.62, 0.00
-55, 10.32, -270.49, 0.00
-56, 8.26, -248.20, 0.00
-57, 6.94, -245.94, 0.00
-58, 7.97, -348.30, 0.00
-59, 7.61, -440.57, 0.00
-60, 5.11, -448.31, 0.00
-61, 2.28, -436.77, 0.00
-62, -0.53, -428.04, 0.00
-63, -3.36, -418.60, 0.00
-64, -6.17, -407.62, 0.00
-65, -8.93, -395.29, 0.00
-66, -11.62, -381.67, 0.00
-67, -14.20, -367.12, 0.00
-68, -16.64, -351.56, 0.00
-69, -18.92, -335.22, 0.00
-70, -21.01, -318.22, 0.00
-71, -22.89, -300.56, 0.00
-72, -24.52, -282.37, 0.00
-73, -25.88, -263.71, 0.00
-74, -26.96, -244.77, 0.00
-75, -27.72, -225.59, 0.00
-76, -28.12, -205.99, 0.00
-77, -28.13, -186.20, 0.00
-78, -27.76, -166.42, 0.00
-79, -26.92, -146.54, 0.00
-80, -25.62, -126.74, 0.00
-81, -23.79, -107.06, 0.00
-82, -21.39, -87.53, 0.00
-83, -18.36, -68.27, 0.00
-84, -14.63, -49.34, 0.00
-85, -10.10, -30.83, 0.00
-86, -4.66, -12.84, 0.00
-87, 1.82, 4.49, 0.00
-88, 9.54, 21.04, 0.00
-89, 18.64, 36.46, 0.00
-90, 29.42, 50.48, 0.00
-91, 42.11, 62.60, 0.00
-92, 56.77, 71.89, 0.00
-93, 73.41, 77.41, 0.00
-94, 91.92, 78.09, 0.00
-95, 111.10, 72.36, 0.00
-96, 128.91, 59.09, 0.00
-97, 142.62, 38.60, 0.00
-98, 108.87, 14.61, 0.00
-99, 70.25, -0.00, 0.00
-100, 103.25, -13.86, 0.00
-101, 123.24, -33.35, 0.00
-102, 98.16, -44.99, 0.00
-103, 72.48, -47.21, 0.00
-104, 48.60, -41.28, 0.00
-105, 27.56, -29.06, 0.00
-106, 9.78, -12.38, 0.00
-107, -4.77, 7.09, 0.00
-108, -16.59, 28.46, 0.00
-109, -26.11, 51.06, 0.00
-110, -33.64, 74.25, 0.00
-111, -39.61, 97.94, 0.00
-112, -44.31, 122.01, 0.00
-113, -47.92, 146.26, 0.00
-114, -50.63, 170.78, 0.00
-115, -52.57, 195.45, 0.00
-116, -53.80, 220.12, 0.00
-117, -54.43, 244.90, 0.00
-118, -54.50, 269.61, 0.00
-119, -54.06, 294.24, 0.00
-120, -53.18, 318.89, 0.00
-121, -51.86, 343.20, 0.00
-122, -50.17, 367.52, 0.00
-123, -48.12, 391.59, 0.00
-124, -45.70, 414.97, 0.00
-125, -43.01, 438.21, 0.00
-126, -40.06, 461.35, 0.00
-127, -36.86, 484.02, 0.00
-128, -33.42, 506.10, 0.00
-129, -29.77, 527.50, 0.00
-130, -25.96, 548.39, 0.00
-131, -22.00, 568.76, 0.00
-132, -17.91, 588.36, 0.00
-133, -13.73, 607.39, 0.00
-134, -9.47, 625.38, 0.00
-135, -5.15, 642.54, 0.00
-136, -0.81, 659.27, 0.00
-137, 3.53, 674.87, 0.00
-138, 7.85, 689.30, 0.00
-139, 12.15, 703.23, 0.00
-140, 16.38, 716.18, 0.00
-141, 20.53, 727.67, 0.00
-142, 24.59, 738.40, 0.00
-143, 28.55, 748.36, 0.00
-144, 32.38, 757.04, 0.00
-145, 36.06, 764.43, 0.00
-146, 39.61, 771.02, 0.00
-147, 43.00, 776.59, 0.00
-148, 46.22, 780.89, 0.00
-149, 49.29, 784.46, 0.00
-150, 52.17, 786.78, 0.00
-151, 54.87, 788.13, 0.00
-152, 57.40, 788.54, 0.00
-153, 59.77, 788.13, 0.00
-154, 61.95, 786.74, 0.00
-155, 63.49, 778.73, 0.00
-156, 67.16, 797.62, 0.00
-157, 62.16, 716.24, 0.00
-158, 1.28, 14.33, 0.00
-159, -2.99, -32.64, 0.00
-160, 0.35, 3.75, 0.00
-161, -0.04, -0.41, 0.00
-162, 0.11, 1.11, 0.00
-163, 0.13, 1.27, 0.00
-164, 0.00, 0.00, 0.00
-165, -0.22, -2.15, 0.00
-166, -0.53, -5.01, 0.00
-167, -0.91, -8.41, 0.00
-168, -1.35, -12.19, 0.00
-169, -1.83, -16.27, 0.00
-170, -2.34, -20.53, 0.00
-171, -2.88, -24.89, 0.00
-172, -3.44, -29.28, 0.00
-173, -4.01, -33.68, 0.00
-174, -4.59, -37.96, 0.00
-175, -5.16, -42.10, 0.00
-176, -5.72, -46.12, 0.00
-177, -6.27, -49.88, 0.00
-178, -6.79, -53.37, 0.00
-179, -7.28, -56.59, 0.00
-180, -7.74, -59.45, 0.00
-181, -8.15, -61.97, 0.00
-182, -8.52, -64.08, 0.00
-183, -8.82, -65.74, 0.00
-184, -9.08, -67.01, 0.00
-185, -9.26, -67.76, 0.00
-186, -9.37, -67.96, 0.00
-187, -9.39, -67.62, 0.00
-188, -9.32, -66.63, 0.00
-189, -9.16, -65.08, 0.00
-190, -8.90, -62.89, 0.00
-191, -8.54, -59.98, 0.00
-192, -8.06, -56.33, 0.00
-193, -7.45, -51.85, 0.00
-194, -6.73, -46.69, 0.00
-195, -5.85, -40.49, 0.00
-196, -4.79, -33.08, 0.00
-197, -3.55, -24.47, 0.00
-198, -1.91, -13.14, 0.00

From 1d8e956e558c5a69867bf58780299bf9e534e866 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Fri, 12 May 2023 11:12:11 +0200
Subject: [PATCH 440/656] Move the translating frame as well so that it can be
 updated from the python interface, too.

---
 SU2_CFD/src/drivers/CDriver.cpp      | 27 ---------------------------
 SU2_CFD/src/iteration/CIteration.cpp | 14 ++++++++++++--
 2 files changed, 12 insertions(+), 29 deletions(-)

diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index 6a8d18de96d..61bd22cb87f 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -2555,33 +2555,6 @@ void CDriver::PreprocessStaticMesh(const CConfig *config, CGeometry** geometry){
 
   if (!fem_solver) {
 
-    switch (Kind_Grid_Movement) {
-
-      case ROTATING_FRAME:
-        /*--- Do nothing here, the steady rotating frame will be handled in the first iteration
-         * of the flow solver, see CIteration::SetGrid_Movement(). ---*/
-        break;
-
-      case STEADY_TRANSLATION:
-
-        /*--- Set the translational velocity and hold the grid fixed during
-         the calculation (similar to rotating frame, but there is no extra
-         source term for translation). ---*/
-
-        if (rank == MASTER_NODE)
-          cout << endl << " Setting translational grid velocities." << endl;
-
-        /*--- Set the translational velocity on all grid levels. ---*/
-
-        for (iMGlevel = 0; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++)
-          geometry_container[iZone][INST_0][iMGlevel]->SetTranslationalVelocity(config, true);
-
-        break;
-
-      default:
-        break;
-    }
-
     if (config->GetnMarker_Moving() > 0) {
 
       /*--- Fixed wall velocities: set the grid velocities only one time
diff --git a/SU2_CFD/src/iteration/CIteration.cpp b/SU2_CFD/src/iteration/CIteration.cpp
index 9d0c1c650bc..660968c70c3 100644
--- a/SU2_CFD/src/iteration/CIteration.cpp
+++ b/SU2_CFD/src/iteration/CIteration.cpp
@@ -61,13 +61,23 @@ void CIteration::SetGrid_Movement(CGeometry** geometry, CSurfaceMovement* surfac
       break;
 
     case STEADY_TRANSLATION:
-      /*--- Pure translation is initialized in the static mesh movement routine at driver level. ---*/
+      /*--- Set or update the translating frame mesh movement with the current translation rates,
+       * which might be altered via the python interface. ---*/
+
+      if (rank == MASTER_NODE) cout << endl << " Setting translational grid velocities." << endl;
+
+      /*--- Set the grid velocities on finest multigrid level for a translating reference frame. ---*/
+      geometry[MESH_0]->SetTranslationalVelocity(config, true);
+
+      /*--- Update the multigrid structure after moving the finest grid,
+       * including computing the grid velocities on the coarser levels. ---*/
+      grid_movement->UpdateMultiGrid(geometry, config);
 
     case ROTATING_FRAME:
       /*--- Set or update the rotating frame mesh movement with the current translation and rotation
        * rates, which might be altered via the python interface. ---*/
 
-      if (rank == MASTER_NODE) cout << endl << " Setting rotating frame grid velocities" << endl;
+      if (rank == MASTER_NODE) cout << endl << " Setting rotating frame grid velocities." << endl;
 
       /*--- Set the grid velocities on finest multigrid level for a rotating reference frame. ---*/
       geometry[MESH_0]->SetRotationalVelocity(config, true);

From e3a44fbb63a146bab11899e81261a01fc9071a29 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Fri, 12 May 2023 11:22:32 +0200
Subject: [PATCH 441/656] Apply sugestion form Code scanning / CodeQL

---
 .../updated_moving_frame_NACA12/run_su2.py    | 20 +++++++++----------
 1 file changed, 9 insertions(+), 11 deletions(-)

diff --git a/TestCases/py_wrapper/updated_moving_frame_NACA12/run_su2.py b/TestCases/py_wrapper/updated_moving_frame_NACA12/run_su2.py
index c3f73a190fe..bb0e5379830 100644
--- a/TestCases/py_wrapper/updated_moving_frame_NACA12/run_su2.py
+++ b/TestCases/py_wrapper/updated_moving_frame_NACA12/run_su2.py
@@ -62,17 +62,15 @@ def save_forces(self):
         # a node that belongs to a moving surface marker.
         has_moving_marker = [marker in solver_markers for marker in solver_all_moving_markers]
 
-        f = open('forces_'+str(self.myid)+'.csv','w')
-
-        for marker in solver_all_moving_markers[has_moving_marker]:
-            solver_marker_id = solver_marker_ids[marker]
-            n_vertices = self.FluidSolver.GetNumberMarkerNodes(solver_marker_id)
-            for i_vertex in range(n_vertices):
-                fxyz = self.FluidSolver.GetMarkerFlowLoad(solver_marker_id, i_vertex)
-                iPoint = self.FluidSolver.GetMarkerNode(solver_marker_id, i_vertex)
-                GlobalIndex = self.FluidSolver.GetNodeGlobalIndex(iPoint)
-                f.write('{}, {:.2f}, {:.2f}, {:.2f}\n'.format(GlobalIndex, fxyz[0], fxyz[1], 0.0))
-        f.close()
+        with open('forces_'+str(self.myid)+'.csv','w') as f:
+            for marker in solver_all_moving_markers[has_moving_marker]:
+                solver_marker_id = solver_marker_ids[marker]
+                n_vertices = self.FluidSolver.GetNumberMarkerNodes(solver_marker_id)
+                for i_vertex in range(n_vertices):
+                    fxyz = self.FluidSolver.GetMarkerFlowLoad(solver_marker_id, i_vertex)
+                    iPoint = self.FluidSolver.GetMarkerNode(solver_marker_id, i_vertex)
+                    GlobalIndex = self.FluidSolver.GetNodeGlobalIndex(iPoint)
+                    f.write('{}, {:.2f}, {:.2f}, {:.2f}\n'.format(GlobalIndex, fxyz[0], fxyz[1], 0.0))
 
 cfd_interface = SU2Interface('config.cfg')
 cfd_interface.update_moving_frame()

From 67f6e931d204e2a67c0f074b94ac3a8de00c3360 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Fri, 12 May 2023 11:26:48 +0200
Subject: [PATCH 442/656] Revert "Removing reference results file for ARM64"

This reverts commit cdd2e610ff64c07201aef474a072072c5b5903d4.
---
 .../forces_0_aarch64.csv.ref                  | 200 ++++++++++++++++++
 1 file changed, 200 insertions(+)
 create mode 100644 TestCases/py_wrapper/translating_NACA0012/forces_0_aarch64.csv.ref

diff --git a/TestCases/py_wrapper/translating_NACA0012/forces_0_aarch64.csv.ref b/TestCases/py_wrapper/translating_NACA0012/forces_0_aarch64.csv.ref
new file mode 100644
index 00000000000..ba1b413acde
--- /dev/null
+++ b/TestCases/py_wrapper/translating_NACA0012/forces_0_aarch64.csv.ref
@@ -0,0 +1,200 @@
+199, -1.01, -0.00, 0.00
+0, -2.07, 14.25, 0.00
+1, -3.62, 24.97, 0.00
+2, -4.84, 33.38, 0.00
+3, -5.85, 40.49, 0.00
+4, -6.69, 46.42, 0.00
+5, -7.36, 51.26, 0.00
+6, -7.92, 55.36, 0.00
+7, -8.34, 58.59, 0.00
+8, -8.64, 61.04, 0.00
+9, -8.83, 62.73, 0.00
+10, -8.91, 63.73, 0.00
+11, -8.90, 64.10, 0.00
+12, -8.79, 63.80, 0.00
+13, -8.59, 62.88, 0.00
+14, -8.31, 61.35, 0.00
+15, -7.95, 59.25, 0.00
+16, -7.53, 56.67, 0.00
+17, -7.05, 53.55, 0.00
+18, -6.50, 49.94, 0.00
+19, -5.90, 45.87, 0.00
+20, -5.26, 41.32, 0.00
+21, -4.57, 36.38, 0.00
+22, -3.85, 31.01, 0.00
+23, -3.09, 25.23, 0.00
+24, -2.31, 19.12, 0.00
+25, -1.51, 12.63, 0.00
+26, -0.68, 5.79, 0.00
+27, 0.16, -1.36, 0.00
+28, 1.01, -8.84, 0.00
+29, 1.86, -16.61, 0.00
+30, 2.72, -24.66, 0.00
+31, 3.58, -32.98, 0.00
+32, 4.43, -41.60, 0.00
+33, 5.28, -50.47, 0.00
+34, 6.11, -59.56, 0.00
+35, 6.93, -68.92, 0.00
+36, 7.73, -78.52, 0.00
+37, 8.50, -88.30, 0.00
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+175, -5.16, -42.10, 0.00
+176, -5.72, -46.12, 0.00
+177, -6.27, -49.88, 0.00
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+180, -7.74, -59.45, 0.00
+181, -8.15, -61.97, 0.00
+182, -8.52, -64.08, 0.00
+183, -8.82, -65.74, 0.00
+184, -9.08, -67.01, 0.00
+185, -9.26, -67.76, 0.00
+186, -9.37, -67.96, 0.00
+187, -9.39, -67.62, 0.00
+188, -9.32, -66.63, 0.00
+189, -9.16, -65.08, 0.00
+190, -8.90, -62.89, 0.00
+191, -8.54, -59.98, 0.00
+192, -8.06, -56.33, 0.00
+193, -7.45, -51.85, 0.00
+194, -6.73, -46.69, 0.00
+195, -5.85, -40.49, 0.00
+196, -4.79, -33.08, 0.00
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+198, -1.91, -13.14, 0.00

From 9dd3ecb8d28a39d1812cdaf01c0807344b782a38 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Fri, 12 May 2023 11:27:55 +0200
Subject: [PATCH 443/656] Removing reference results file in the right folder

---
 .../forces_0_aarch64.csv.ref                  | 200 ------------------
 1 file changed, 200 deletions(-)
 delete mode 100644 TestCases/py_wrapper/updated_moving_frame_NACA12/forces_0_aarch64.csv.ref

diff --git a/TestCases/py_wrapper/updated_moving_frame_NACA12/forces_0_aarch64.csv.ref b/TestCases/py_wrapper/updated_moving_frame_NACA12/forces_0_aarch64.csv.ref
deleted file mode 100644
index eae8cf091e5..00000000000
--- a/TestCases/py_wrapper/updated_moving_frame_NACA12/forces_0_aarch64.csv.ref
+++ /dev/null
@@ -1,200 +0,0 @@
-199, -1.02, -0.00, 0.00
-0, -2.05, 14.11, 0.00
-1, -3.63, 25.02, 0.00
-2, -4.85, 33.50, 0.00
-3, -5.88, 40.69, 0.00
-4, -6.73, 46.67, 0.00
-5, -7.41, 51.56, 0.00
-6, -7.97, 55.71, 0.00
-7, -8.40, 58.99, 0.00
-8, -8.71, 61.49, 0.00
-9, -8.90, 63.22, 0.00
-10, -8.98, 64.25, 0.00
-11, -8.98, 64.66, 0.00
-12, -8.87, 64.38, 0.00
-13, -8.68, 63.48, 0.00
-14, -8.39, 61.96, 0.00
-15, -8.03, 59.85, 0.00
-16, -7.61, 57.27, 0.00
-17, -7.12, 54.13, 0.00
-18, -6.57, 50.50, 0.00
-19, -5.97, 46.39, 0.00
-20, -5.32, 41.81, 0.00
-21, -4.63, 36.81, 0.00
-22, -3.90, 31.39, 0.00
-23, -3.13, 25.55, 0.00
-24, -2.34, 19.36, 0.00
-25, -1.53, 12.80, 0.00
-26, -0.69, 5.88, 0.00
-27, 0.16, -1.35, 0.00
-28, 1.02, -8.91, 0.00
-29, 1.88, -16.75, 0.00
-30, 2.74, -24.86, 0.00
-31, 3.61, -33.24, 0.00
-32, 4.46, -41.90, 0.00
-33, 5.31, -50.77, 0.00
-34, 6.14, -59.83, 0.00
-35, 6.95, -69.11, 0.00
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-37, 8.48, -88.14, 0.00
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-166, 2.16, 20.31, 0.00
-167, 1.56, 14.37, 0.00
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-169, 0.24, 2.16, 0.00
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-182, -8.03, -60.38, 0.00
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-188, -9.15, -65.46, 0.00
-189, -9.04, -64.19, 0.00
-190, -8.81, -62.24, 0.00
-191, -8.48, -59.55, 0.00
-192, -8.02, -56.09, 0.00
-193, -7.44, -51.78, 0.00
-194, -6.74, -46.74, 0.00
-195, -5.87, -40.64, 0.00
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-198, -1.96, -13.51, 0.00

From 3b601130eb1fd5efc9d3122e97aedd3312e99246 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Fri, 12 May 2023 11:31:08 +0200
Subject: [PATCH 444/656] Use reference results calculated by GitHub runner

---
 .../updated_moving_frame_NACA12/forces_0.csv.ref       | 10 +++++-----
 1 file changed, 5 insertions(+), 5 deletions(-)

diff --git a/TestCases/py_wrapper/updated_moving_frame_NACA12/forces_0.csv.ref b/TestCases/py_wrapper/updated_moving_frame_NACA12/forces_0.csv.ref
index eae8cf091e5..de783b9af84 100644
--- a/TestCases/py_wrapper/updated_moving_frame_NACA12/forces_0.csv.ref
+++ b/TestCases/py_wrapper/updated_moving_frame_NACA12/forces_0.csv.ref
@@ -31,17 +31,17 @@
 29, 1.88, -16.75, 0.00
 30, 2.74, -24.86, 0.00
 31, 3.61, -33.24, 0.00
-32, 4.46, -41.90, 0.00
+32, 4.46, -41.89, 0.00
 33, 5.31, -50.77, 0.00
 34, 6.14, -59.83, 0.00
 35, 6.95, -69.11, 0.00
-36, 7.73, -78.57, 0.00
-37, 8.48, -88.14, 0.00
+36, 7.73, -78.56, 0.00
+37, 8.48, -88.13, 0.00
 38, 9.19, -97.82, 0.00
 39, 9.86, -107.57, 0.00
 40, 10.47, -117.28, 0.00
 41, 11.01, -126.92, 0.00
-42, 11.49, -136.43, 0.00
+42, 11.49, -136.42, 0.00
 43, 11.87, -145.62, 0.00
 44, 12.15, -154.31, 0.00
 45, 12.30, -162.22, 0.00
@@ -173,7 +173,7 @@
 171, -1.16, -10.05, 0.00
 172, -1.88, -15.99, 0.00
 173, -2.60, -21.79, 0.00
-174, -3.31, -27.37, 0.00
+174, -3.31, -27.36, 0.00
 175, -4.00, -32.68, 0.00
 176, -4.69, -37.76, 0.00
 177, -5.34, -42.49, 0.00

From 95628ce6398982b68fab55553c31fa687f3283ca Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Fri, 12 May 2023 14:06:14 +0200
Subject: [PATCH 445/656] Remove unused variable Kind_Grid_Movement

---
 SU2_CFD/src/drivers/CDriver.cpp | 3 ---
 1 file changed, 3 deletions(-)

diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index 61bd22cb87f..639e34c4304 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -2547,12 +2547,9 @@ void CDriver::InitializeInterface(CConfig **config, CSolver***** solver, CGeomet
 void CDriver::PreprocessStaticMesh(const CConfig *config, CGeometry** geometry){
 
   unsigned short iMGlevel, iMGfine;
-  unsigned short Kind_Grid_Movement;
 
   unsigned short iZone = config->GetiZone();
 
-  Kind_Grid_Movement = config->GetKind_GridMovement();
-
   if (!fem_solver) {
 
     if (config->GetnMarker_Moving() > 0) {

From e93f258eae0e2acd09de1546b80d08c6dbf82256 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Fri, 12 May 2023 14:55:15 +0200
Subject: [PATCH 446/656] C++ seems to require a break statement when using
 switch/case...

---
 SU2_CFD/src/iteration/CIteration.cpp | 2 ++
 1 file changed, 2 insertions(+)

diff --git a/SU2_CFD/src/iteration/CIteration.cpp b/SU2_CFD/src/iteration/CIteration.cpp
index 660968c70c3..e79ff1ec395 100644
--- a/SU2_CFD/src/iteration/CIteration.cpp
+++ b/SU2_CFD/src/iteration/CIteration.cpp
@@ -73,6 +73,8 @@ void CIteration::SetGrid_Movement(CGeometry** geometry, CSurfaceMovement* surfac
        * including computing the grid velocities on the coarser levels. ---*/
       grid_movement->UpdateMultiGrid(geometry, config);
 
+      break;
+
     case ROTATING_FRAME:
       /*--- Set or update the rotating frame mesh movement with the current translation and rotation
        * rates, which might be altered via the python interface. ---*/

From 02f5388bb197fce307c1fcea383ab46245c23508 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Fri, 12 May 2023 16:41:51 +0200
Subject: [PATCH 447/656] Proposal for a test case for cosine gusts in
 z-direction on a 3D mesh. Test duration: 0.83 min Not sure where the mesh and
 the restart files should go, so this will break the testing until I commit
 the missing files.

---
 TestCases/gust/cosine_gust_zdir.cfg | 172 ++++++++++++++++++++++++++++
 TestCases/hybrid_regression.py      |   9 ++
 2 files changed, 181 insertions(+)
 create mode 100644 TestCases/gust/cosine_gust_zdir.cfg

diff --git a/TestCases/gust/cosine_gust_zdir.cfg b/TestCases/gust/cosine_gust_zdir.cfg
new file mode 100644
index 00000000000..0c523862f40
--- /dev/null
+++ b/TestCases/gust/cosine_gust_zdir.cfg
@@ -0,0 +1,172 @@
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
+% Solver type (EULER, NAVIER_STOKES, RANS,
+%              INC_EULER, INC_NAVIER_STOKES, INC_RANS,
+%              NEMO_EULER, NEMO_NAVIER_STOKES,
+%              FEM_EULER, FEM_NAVIER_STOKES, FEM_RANS, FEM_LES,
+%              HEAT_EQUATION_FVM, ELASTICITY)
+SOLVER= EULER
+%
+% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
+MATH_PROBLEM= DIRECT
+%
+% Restart solution (NO, YES)
+RESTART_SOL= YES
+%
+% Iteration number to begin unsteady restarts
+RESTART_ITER= 72
+%
+% ------------------------------- SOLVER CONTROL ------------------------------%
+%
+% Maximum number of inner iterations
+INNER_ITER= 30
+%
+% Min value of the residual (log10 of the residual)
+CONV_RESIDUAL_MINVAL= -6
+%
+% Start convergence criteria at iteration number
+CONV_STARTITER= 0
+%
+% ------------------------- UNSTEADY SIMULATION -------------------------------%
+%
+TIME_DOMAIN=YES
+TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
+TIME_STEP= 0.001
+TIME_ITER= 80
+%
+% --------------------------- GUST SIMULATION ---------------------------------%
+%
+% The gust simulation requires the GRID_MOVEMENT flag to be set to YES.
+% and the GRID_MOVEMENT_KIND to be set to GUST or any of the other options.
+% Apply a wind gust (NO, YES)
+GRID_MOVEMENT=GUST
+WIND_GUST= YES
+GUST_TYPE= ONE_M_COSINE
+GUST_DIR= Z_DIR
+GUST_WAVELENGTH= 5.0
+GUST_PERIODS= 1.0
+% Gust amplitude corresponds to ~2.0 deg AoA
+GUST_AMPL= 2.37
+%
+GUST_BEGIN_TIME= 0.0
+GUST_BEGIN_LOC=-10.0
+% -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
+%
+% Mach number (non-dimensional, based on the free-stream values)
+MACH_NUMBER= 0.2
+%
+% Angle of attack (degrees, only for compressible flows)
+AOA= 0.0
+%
+% Side-slip angle (degrees, only for compressible flows)
+SIDESLIP_ANGLE= 0.0
+%
+% Free-stream option to choose between density and temperature (default) for
+% initializing the solution (TEMPERATURE_FS, DENSITY_FS)
+FREESTREAM_OPTION= DENSITY_FS
+%
+% Free-stream pressure (101325.0 N/m^2, 2116.216 psf by default)
+FREESTREAM_PRESSURE= 101325.0
+%
+% Free-stream density (1.2886 Kg/m^3, 0.0025 slug/ft^3 by default)
+FREESTREAM_DENSITY= 1.225
+%
+% Free-stream temperature (288.15 K, 518.67 R by default)
+FREESTREAM_TEMPERATURE= 288.15
+%
+% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
+%
+% Reference origin for moment computation (m or in)
+REF_ORIGIN_MOMENT_X = 0.25
+REF_ORIGIN_MOMENT_Y = 0.00
+REF_ORIGIN_MOMENT_Z = 0.00
+%
+% Reference length for moment non-dimensional coefficients (m or in)
+REF_LENGTH= 1.0
+%
+% Reference area for non-dimensional force coefficients (0 implies automatic
+% calculation) (m^2 or in^2)
+REF_AREA= 3.0
+%
+% Aircraft semi-span (0 implies automatic calculation) (m or in)
+SEMI_SPAN= 1.5
+%
+% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
+%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
+REF_DIMENSIONALIZATION= DIMENSIONAL
+
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
+% Euler wall boundary marker(s) (NONE = no marker)
+% Implementation identical to MARKER_SYM.
+MARKER_EULER= ( wing, tip)
+%
+% Far-field boundary marker(s) (NONE = no marker)
+MARKER_FAR= ( far_away )
+
+% ------------------------ SURFACES IDENTIFICATION ----------------------------%
+%
+% Marker(s) of the surface in the surface flow solution file
+MARKER_PLOTTING = ( wing, tip )
+%
+% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
+MARKER_MONITORING = ( wing, tip )
+
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
+% CFL number (initial value for the adaptive CFL number)
+CFL_NUMBER= 1000.0
+%
+% Adaptive CFL number (NO, YES)
+CFL_ADAPT= YES
+%
+% -------------------------- MULTIGRID PARAMETERS -----------------------------%
+%
+% Multi-grid levels (0 = no multi-grid)
+MGLEVEL= 3
+%
+% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
+MGCYCLE= W_CYCLE
+
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
+% Convective numerical method (JST, JST_KE, JST_MAT, LAX-FRIEDRICH, CUSP, ROE, AUSM,
+%                              AUSMPLUSUP, AUSMPLUSUP2, AUSMPWPLUS, HLLC, TURKEL_PREC,
+%                              SW, MSW, FDS, SLAU, SLAU2, L2ROE, LMROE)
+CONV_NUM_METHOD_FLOW= JST
+%
+% Max number of iterations of the linear solver for the implicit formulation
+LINEAR_SOLVER_ITER= 20
+%
+% ------------------------- SCREEN/HISTORY VOLUME OUTPUT --------------------------%
+%
+% Screen output fields (use 'SU2_CFD -d <config_file>' to view list of available fields)
+SCREEN_OUTPUT= (TIME_ITER, INNER_ITER, RMS_DENSITY, LIFT, MOMENT_X, MOMENT_Y, MOMENT_Z)
+%
+% History output groups (use 'SU2_CFD -d <config_file>' to view list of available fields)
+HISTORY_OUTPUT= (ITER, RMS_RES, AERO_COEFF, CAUCHY, WALL_TIME)
+%
+% ------------------------- INPUT/OUTPUT FILE INFORMATION --------------------------%
+%
+% Mesh input file
+MESH_FILENAME= mesh_rectangular_wing.su2
+%
+% Mesh input file format (SU2, CGNS)
+MESH_FORMAT= SU2
+%
+% Restart flow input file
+SOLUTION_FILENAME= restart_gust.dat
+RESTART_FILENAME= restart_gust.dat
+SURFACE_FILENAME= surface_gust
+VOLUME_FILENAME= volume_gust
+CONV_FILENAME= history_gust
+%
+% Output tabular file format (TECPLOT, CSV)
+TABULAR_FORMAT= CSV
+%
+% Files to output
+% Possible formats : (TECPLOT, TECPLOT_BINARY, SURFACE_TECPLOT,
+%  SURFACE_TECPLOT_BINARY, CSV, SURFACE_CSV, PARAVIEW, PARAVIEW_BINARY, SURFACE_PARAVIEW,
+%  SURFACE_PARAVIEW_BINARY, MESH, RESTART_BINARY, RESTART_ASCII, CGNS, SURFACE_CGNS, STL)
+OUTPUT_FILES= (RESTART, RESTART_ASCII, TECPLOT, SURFACE_TECPLOT)
+
diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index 4e2094b56f6..211294d2fd2 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -478,6 +478,15 @@ def main():
     sine_gust.test_vals = [-1.977520, 3.481804, -0.012402, -0.007454]
     sine_gust.unsteady  = True
     test_list.append(sine_gust)
+    
+    # Cosine gust in z-direction
+    cosine_gust           = TestCase('cosine_gust_zdir')
+    cosine_gust.cfg_dir   = "gust"
+    cosine_gust.cfg_file  = "cosine_gust_zdir.cfg"
+    cosine_gust.test_iter = 79
+    cosine_gust.test_vals = [-2.418813, 0.004650, -0.001878, -0.000637, -0.000271]
+    cosine_gust.unsteady  = True
+    test_list.append(cosine_gust)
 
     # Aeroelastic
     aeroelastic           = TestCase('aeroelastic')

From 83310459b1f600498dfefbbf9e60c32c411e942e Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Fri, 12 May 2023 08:29:32 -0700
Subject: [PATCH 448/656] Apply suggestions from code review

---
 SU2_CFD/src/iteration/CIteration.cpp | 23 +++++++++++------------
 1 file changed, 11 insertions(+), 12 deletions(-)

diff --git a/SU2_CFD/src/iteration/CIteration.cpp b/SU2_CFD/src/iteration/CIteration.cpp
index e79ff1ec395..53124b45e3f 100644
--- a/SU2_CFD/src/iteration/CIteration.cpp
+++ b/SU2_CFD/src/iteration/CIteration.cpp
@@ -64,14 +64,12 @@ void CIteration::SetGrid_Movement(CGeometry** geometry, CSurfaceMovement* surfac
       /*--- Set or update the translating frame mesh movement with the current translation rates,
        * which might be altered via the python interface. ---*/
 
-      if (rank == MASTER_NODE) cout << endl << " Setting translational grid velocities." << endl;
+      if (rank == MASTER_NODE) cout << "\n Setting translational grid velocities." << endl;
 
-      /*--- Set the grid velocities on finest multigrid level for a translating reference frame. ---*/
-      geometry[MESH_0]->SetTranslationalVelocity(config, true);
+        /*--- Set the translational velocity on all grid levels. ---*/
 
-      /*--- Update the multigrid structure after moving the finest grid,
-       * including computing the grid velocities on the coarser levels. ---*/
-      grid_movement->UpdateMultiGrid(geometry, config);
+        for (auto iMGlevel = 0u; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++)
+          geometry_container[iZone][INST_0][iMGlevel]->SetTranslationalVelocity(config, true);
 
       break;
 
@@ -79,14 +77,15 @@ void CIteration::SetGrid_Movement(CGeometry** geometry, CSurfaceMovement* surfac
       /*--- Set or update the rotating frame mesh movement with the current translation and rotation
        * rates, which might be altered via the python interface. ---*/
 
-      if (rank == MASTER_NODE) cout << endl << " Setting rotating frame grid velocities." << endl;
+      if (rank == MASTER_NODE) cout << "\n Setting rotating frame grid velocities." << endl;
 
-      /*--- Set the grid velocities on finest multigrid level for a rotating reference frame. ---*/
-      geometry[MESH_0]->SetRotationalVelocity(config, true);
+        /*--- Set the grid velocities on all multigrid levels for a steadily
+           rotating reference frame. ---*/
 
-      /*--- Update the multigrid structure after moving the finest grid,
-            including computing the grid velocities on the coarser levels. ---*/
-      grid_movement->UpdateMultiGrid(geometry, config);
+        for (auto iMGlevel = 0u; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++){
+          geometry[iMGlevel]->SetRotationalVelocity(config, true);
+          geometry[iMGlevel]->SetShroudVelocity(config);
+        }
 
       break;
   }

From c14d7839cd4dcf3faad31c1ec13e34e1af1026c2 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Fri, 12 May 2023 08:31:04 -0700
Subject: [PATCH 449/656] Apply suggestions from code review

---
 SU2_CFD/src/iteration/CIteration.cpp | 18 +++++++++---------
 1 file changed, 9 insertions(+), 9 deletions(-)

diff --git a/SU2_CFD/src/iteration/CIteration.cpp b/SU2_CFD/src/iteration/CIteration.cpp
index 53124b45e3f..d95217232d2 100644
--- a/SU2_CFD/src/iteration/CIteration.cpp
+++ b/SU2_CFD/src/iteration/CIteration.cpp
@@ -66,10 +66,10 @@ void CIteration::SetGrid_Movement(CGeometry** geometry, CSurfaceMovement* surfac
 
       if (rank == MASTER_NODE) cout << "\n Setting translational grid velocities." << endl;
 
-        /*--- Set the translational velocity on all grid levels. ---*/
+      /*--- Set the translational velocity on all grid levels. ---*/
 
-        for (auto iMGlevel = 0u; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++)
-          geometry_container[iZone][INST_0][iMGlevel]->SetTranslationalVelocity(config, true);
+      for (auto iMGlevel = 0u; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++)
+        geometry_container[iZone][INST_0][iMGlevel]->SetTranslationalVelocity(config, true);
 
       break;
 
@@ -79,13 +79,13 @@ void CIteration::SetGrid_Movement(CGeometry** geometry, CSurfaceMovement* surfac
 
       if (rank == MASTER_NODE) cout << "\n Setting rotating frame grid velocities." << endl;
 
-        /*--- Set the grid velocities on all multigrid levels for a steadily
-           rotating reference frame. ---*/
+      /*--- Set the grid velocities on all multigrid levels for a steadily
+         rotating reference frame. ---*/
 
-        for (auto iMGlevel = 0u; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++){
-          geometry[iMGlevel]->SetRotationalVelocity(config, true);
-          geometry[iMGlevel]->SetShroudVelocity(config);
-        }
+      for (auto iMGlevel = 0u; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++){
+        geometry[iMGlevel]->SetRotationalVelocity(config, true);
+        geometry[iMGlevel]->SetShroudVelocity(config);
+      }
 
       break;
   }

From 254fe213658ef66cbb315dbf707d305ff8fd830f Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Fri, 12 May 2023 09:33:23 -0700
Subject: [PATCH 450/656] Update SU2_CFD/src/iteration/CIteration.cpp

---
 SU2_CFD/src/iteration/CIteration.cpp | 6 +++---
 1 file changed, 3 insertions(+), 3 deletions(-)

diff --git a/SU2_CFD/src/iteration/CIteration.cpp b/SU2_CFD/src/iteration/CIteration.cpp
index d95217232d2..a08efb85367 100644
--- a/SU2_CFD/src/iteration/CIteration.cpp
+++ b/SU2_CFD/src/iteration/CIteration.cpp
@@ -68,8 +68,8 @@ void CIteration::SetGrid_Movement(CGeometry** geometry, CSurfaceMovement* surfac
 
       /*--- Set the translational velocity on all grid levels. ---*/
 
-      for (auto iMGlevel = 0u; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++)
-        geometry_container[iZone][INST_0][iMGlevel]->SetTranslationalVelocity(config, true);
+      for (auto iMGlevel = 0u; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
+        geometry[iMGlevel]->SetTranslationalVelocity(config, true);
 
       break;
 
@@ -82,7 +82,7 @@ void CIteration::SetGrid_Movement(CGeometry** geometry, CSurfaceMovement* surfac
       /*--- Set the grid velocities on all multigrid levels for a steadily
          rotating reference frame. ---*/
 
-      for (auto iMGlevel = 0u; iMGlevel <= config_container[ZONE_0]->GetnMGLevels(); iMGlevel++){
+      for (auto iMGlevel = 0u; iMGlevel <= config->GetnMGLevels(); iMGlevel++){
         geometry[iMGlevel]->SetRotationalVelocity(config, true);
         geometry[iMGlevel]->SetShroudVelocity(config);
       }

From bb6742776744f392cb48c57a77fe7cd25ec484d3 Mon Sep 17 00:00:00 2001
From: Daniel Mayer <daniel.mayer4@us.bosch.com>
Date: Fri, 12 May 2023 16:49:07 -0700
Subject: [PATCH 451/656] Add word-by-word comparison with tolerance and
 threshold to file diff.

---
 TestCases/TestCase.py | 115 +++++++++++++++++++++++++++++++++++++++---
 1 file changed, 108 insertions(+), 7 deletions(-)

diff --git a/TestCases/TestCase.py b/TestCases/TestCase.py
index e1b8f70cacb..132f28bbfc4 100644
--- a/TestCases/TestCase.py
+++ b/TestCases/TestCase.py
@@ -34,6 +34,12 @@ def print_vals(vals, name="Values"):
     """Print an array of floats."""
     print(name + ': ' + ', '.join('{:f}'.format(v) for v in vals))
 
+def is_float(test_string):
+    try:
+        float(test_string)
+        return True
+    except ValueError:
+        return False
 
 class TestCase:
 
@@ -104,6 +110,8 @@ def __init__(self,tag_in):
         self.command = self.Command()
         self.timeout = 0
         self.tol = 0.0
+        self.tol_file_percent = 0.0
+        self.comp_threshold = 0.0
 
         # Options for file-comparison tests
         self.reference_file = "of_grad.dat.ref"
@@ -313,6 +321,7 @@ def run_filediff(self):
             print("Output from the failed case:")
             subprocess.call(["cat", logfilename])
 
+        diff_time_start = datetime.datetime.now()
         if not timed_out and passed:
             # Compare files
             fromfile = self.reference_file
@@ -325,7 +334,90 @@ def run_filediff(self):
                 try:
                     todate = time.ctime(os.stat(tofile).st_mtime)
                     tolines = open(tofile, 'U').readlines()
-                    diff = list(difflib.unified_diff(fromlines, tolines, fromfile, tofile, fromdate, todate))
+
+                    # If file tolerance is set to 0, make regular diff
+                    if self.tol_file_percent == 0.0:
+                        diff = list(difflib.unified_diff(fromlines, tolines, fromfile, tofile, fromdate, todate))
+
+                    # Else test word by word with given tolerance
+                    else:
+
+                        diff            = [];
+                        max_delta       = 0
+                        compare_counter = 0
+                        ignore_counter  = 0
+
+                        # Assert that both files have the same number of lines
+                        if len(fromlines) != len(tolines):
+                            diff   = ["ERROR: Number of lines in " + fromfile + " and " + tofile + " differ."]
+                            passed = False
+                        
+                        # Loop through all lines
+                        for i_line in range(0, len(fromlines)):
+
+                            if passed == False: break
+
+                            # Extract next line and split it
+                            from_line = fromlines[i_line].split()
+                            to_line   = tolines[i_line].split()
+
+                            # Assert that both lines have the same number of words
+                            if len(from_line) != len(to_line):
+                                diff   = ["ERROR: Number of words in line " + str(i_line+1) + " differ."]
+                                passed = False
+                                break
+                            
+                            # Loop through all words of one line
+                            for i_word in range(0, len(from_line)):
+
+                                # Extract next word and strip whitespace and commas
+                                from_word = from_line[i_word].strip().strip(',')
+                                to_word   = to_line[i_word].strip().strip(',')
+
+                                # Assert that words are either both numeric or both non-numeric
+                                from_isfloat = is_float(from_word)
+                                to_isfloat   = is_float(to_word)
+                                if from_isfloat != to_isfloat:
+                                    diff      = ["ERROR: File entries '" + from_word + "' and '" + to_word + "' in line " + str(i_line+1) + ", word " + str(i_word+1) + " differ."]
+                                    passed    = False
+                                    delta     = 0.0
+                                    max_delta = "Not applicable"
+                                    break
+
+                                # Make actual comparison
+                                # Compare floats
+                                if from_isfloat:
+                                    try:
+                                        # Only do a relative comparison when the threshold is met.
+                                        # This is to prevent large relative differences for very small numbers.
+                                        if (abs(float(from_word)) > self.comp_threshold):
+                                            delta = abs( (float(from_word) - float(to_word)) / float(from_word) ) * 100
+                                            compare_counter += 1
+                                        else:
+                                            delta = 0.0
+                                            ignore_counter += 1
+
+                                        max_delta = max(max_delta, delta)
+
+                                    except ZeroDivisionError:
+                                        ignore_counter += 1
+                                        continue
+
+                                # Compare non-floats
+                                else:
+                                    delta  = 0.0
+                                    compare_counter += 1
+                                    if from_word != to_word:
+                                        diff      = ["ERROR: File entries '" + from_word + "' and '" + to_word + "' in line " + str(i_line+1) + ", word " + str(i_word+1) + " differ."]
+                                        passed    = False
+                                        max_delta = "Not applicable"
+                                        break
+
+                                if delta > self.tol_file_percent:
+                                    diff   = ["ERROR: File entries '" + from_word + "' and '" + to_word + "' in line " + str(i_line+1) + ", word " + str(i_word+1) + " differ."]
+                                    passed = False
+                                    break
+
                 except OSError:
                     print("OS error, most likely from missing reference file:", fromfile)
                     print("Current working directory contents:")
@@ -335,10 +427,6 @@ def run_filediff(self):
                 print("Current working directory contents:")
                 print(os.listdir("."))
 
-
-
-
-
             if (diff==[]):
                 passed=True
             else:
@@ -349,8 +437,21 @@ def run_filediff(self):
         else:
             passed = False
 
-        print('CPU architecture=%s'%self.cpu_arch)
-        print('test duration: %.2f min'%(running_time/60.0))
+        # Report results
+        diff_time_stop = datetime.datetime.now()
+        diff_time      = (diff_time_stop - diff_time_start).microseconds
+
+        print('CPU architecture:    %s'%self.cpu_arch)
+        print('Test duration:       %.2f min'%(running_time/60.0))
+        print('Diff duration:       %.2f sec'%(diff_time/1e6))
+        print('Specified tolerance: ' + str(self.tol_file_percent) + '%')
+        print('Specified threshold: ' + str(self.comp_threshold)) 
+
+        if self.tol_file_percent != 0.0:
+            print('Compared entries:    ' + str(compare_counter))
+            print('Ignored entries:     ' + str(ignore_counter))
+            print('Maximum difference:  ' + str(max_delta) + '%')
+
         print('==================== End Test: %s ====================\n'%self.tag)
 
         sys.stdout.flush()

From 8ec4d0e85b9d82fbc7c6318b0b2a1440abf1ca29 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 13 May 2023 20:03:37 -0700
Subject: [PATCH 452/656] improve FFD setting feedback

---
 Common/include/geometry/CGeometry.hpp         |  11 -
 .../include/grid_movement/CFreeFormDefBox.hpp |   8 +-
 Common/include/toolboxes/geometry_toolbox.hpp |   9 +
 Common/src/geometry/CGeometry.cpp             |  24 ---
 Common/src/grid_movement/CFreeFormDefBox.cpp  |  86 ++------
 Common/src/grid_movement/CSurfaceMovement.cpp | 197 +++++++++---------
 6 files changed, 130 insertions(+), 205 deletions(-)

diff --git a/Common/include/geometry/CGeometry.hpp b/Common/include/geometry/CGeometry.hpp
index 22280ddf04f..2eb464c7dcd 100644
--- a/Common/include/geometry/CGeometry.hpp
+++ b/Common/include/geometry/CGeometry.hpp
@@ -595,17 +595,6 @@ class CGeometry {
     return FindEdge(first_point, second_point, false) >= 0;
   }
 
-  /*!
-   * \brief Get the distance between a plane (defined by three point) and a point.
-   * \param[in] Coord - Coordinates of the point.
-   * \param[in] iCoord - Coordinates of the first point that defines the plane.
-   * \param[in] jCoord - Coordinates of the second point that defines the plane.
-   * \param[in] kCoord - Coordinates of the third point that defines the plane.
-   * \return Signed distance.
-   */
-  su2double Point2Plane_Distance(const su2double* Coord, const su2double* iCoord, const su2double* jCoord,
-                                 const su2double* kCoord);
-
   /*!
    * \brief Create a file for testing the geometry.
    */
diff --git a/Common/include/grid_movement/CFreeFormDefBox.hpp b/Common/include/grid_movement/CFreeFormDefBox.hpp
index 87ff31993a6..aca98e7a2ba 100644
--- a/Common/include/grid_movement/CFreeFormDefBox.hpp
+++ b/Common/include/grid_movement/CFreeFormDefBox.hpp
@@ -642,12 +642,10 @@ class CFreeFormDefBox : public CGridMovement {
   }
 
   /*!
-   * \brief Set, at each vertex, the index of the free form FFDBox that contains the vertex.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] iFFDBox - Index of the FFDBox.
+   * \brief Returns true if the point is inside the FFD.
+   * \param[in] coord - Coordinate of the point to check.
    */
-  bool GetPointFFD(CGeometry* geometry, CConfig* config, unsigned long iPoint) const;
+  bool CheckPointInsideFFD(const su2double* coord) const;
 
   /*!
    * \brief Set the zone of the computational domain that is going to be deformed.
diff --git a/Common/include/toolboxes/geometry_toolbox.hpp b/Common/include/toolboxes/geometry_toolbox.hpp
index 8cb1d988df3..c61ba413af0 100644
--- a/Common/include/toolboxes/geometry_toolbox.hpp
+++ b/Common/include/toolboxes/geometry_toolbox.hpp
@@ -150,6 +150,15 @@ inline void QuadrilateralNormal(const T& coords, U* normal) {
   normal[2] *= 0.5;
 }
 
+/*! \brief Signed distance from a point to a plane defined by 3 coordinates. */
+template <class T, class U>
+inline U PointToPlaneDistance(const T& coords, const U* point) {
+  U normal[3], distance[3];
+  TriangleNormal(coords, normal);
+  Distance(3, point, coords[0], distance);
+  return DotProduct(3, distance, normal) / Norm(3, normal);
+}
+
 /*!
  * \brief Compute a 3D rotation matrix.
  * \note The implicit ordering is rotation about the x, y, and then z axis.
diff --git a/Common/src/geometry/CGeometry.cpp b/Common/src/geometry/CGeometry.cpp
index cc5c84e54f3..9d526f45ebd 100644
--- a/Common/src/geometry/CGeometry.cpp
+++ b/Common/src/geometry/CGeometry.cpp
@@ -1246,30 +1246,6 @@ void CGeometry::PostPeriodicSends(CGeometry* geometry, const CConfig* config, un
 #endif
 }
 
-su2double CGeometry::Point2Plane_Distance(const su2double* Coord, const su2double* iCoord, const su2double* jCoord,
-                                          const su2double* kCoord) {
-  su2double CrossProduct[3], iVector[3], jVector[3], distance, modulus;
-  unsigned short iDim;
-
-  for (iDim = 0; iDim < 3; iDim++) {
-    iVector[iDim] = jCoord[iDim] - iCoord[iDim];
-    jVector[iDim] = kCoord[iDim] - iCoord[iDim];
-  }
-
-  CrossProduct[0] = iVector[1] * jVector[2] - iVector[2] * jVector[1];
-  CrossProduct[1] = iVector[2] * jVector[0] - iVector[0] * jVector[2];
-  CrossProduct[2] = iVector[0] * jVector[1] - iVector[1] * jVector[0];
-
-  modulus =
-      sqrt(CrossProduct[0] * CrossProduct[0] + CrossProduct[1] * CrossProduct[1] + CrossProduct[2] * CrossProduct[2]);
-
-  distance = 0.0;
-  for (iDim = 0; iDim < 3; iDim++) distance += CrossProduct[iDim] * (Coord[iDim] - iCoord[iDim]);
-  distance /= modulus;
-
-  return distance;
-}
-
 void CGeometry::SetEdges() {
   nEdge = 0;
   for (auto iPoint = 0ul; iPoint < nPoint; iPoint++) {
diff --git a/Common/src/grid_movement/CFreeFormDefBox.cpp b/Common/src/grid_movement/CFreeFormDefBox.cpp
index 2872b22aebd..3757225b133 100644
--- a/Common/src/grid_movement/CFreeFormDefBox.cpp
+++ b/Common/src/grid_movement/CFreeFormDefBox.cpp
@@ -28,6 +28,7 @@
 #include "../../include/grid_movement/CFreeFormDefBox.hpp"
 #include "../../include/grid_movement/CBezierBlending.hpp"
 #include "../../include/grid_movement/CBSplineBlending.hpp"
+#include "../../include/toolboxes/geometry_toolbox.hpp"
 
 CFreeFormDefBox::CFreeFormDefBox() : CGridMovement() {}
 
@@ -1014,13 +1015,8 @@ su2double* CFreeFormDefBox::GetParametricCoord_Iterative(unsigned long iPoint, s
   return ParamCoord;
 }
 
-bool CFreeFormDefBox::GetPointFFD(CGeometry* geometry, CConfig* config, unsigned long iPoint) const {
-  bool Inside = true;
-  bool cylindrical = (config->GetFFD_CoordSystem() == CYLINDRICAL);
-  bool spherical = (config->GetFFD_CoordSystem() == SPHERICAL);
-  bool polar = (config->GetFFD_CoordSystem() == POLAR);
-
-  /*--- indices of the FFD box. Note that the front face is labelled 0,1,2,3 and the back face is 4,5,6,7 ---*/
+bool CFreeFormDefBox::CheckPointInsideFFD(const su2double* coord) const {
+  /*--- Indices of the FFD box. Note that the front face is labelled 0,1,2,3 and the back face is 4,5,6,7 ---*/
 
   unsigned short Index[6][5] = {{0, 1, 2, 3, 0},   // front side
                                 {1, 5, 6, 2, 1},   // right side
@@ -1029,76 +1025,34 @@ bool CFreeFormDefBox::GetPointFFD(CGeometry* geometry, CConfig* config, unsigned
                                 {4, 5, 1, 0, 4},   // bottom side
                                 {4, 7, 6, 5, 4}};  // back side
 
-  /*--- The current approach is to subdivide each of the 6 faces of the hexahedral FFD box into 4 triangles
-      by defining a supporting middle point. This allows nonplanar FFD boxes.
-      Note that the definition of the FFD box is as follows: the FFD box is a 6-sided die and we are looking at the side
-     "1". The opposite side is side "6". If we are looking at side "1", we define the nodes counterclockwise. If we are
-     looking at side "6", we define the face clockwise  ---*/
-
-  unsigned short nDim = geometry->GetnDim();
-
-  su2double Coord[3] = {0.0, 0.0, 0.0};
-  for (unsigned short iDim = 0; iDim < nDim; iDim++) Coord[iDim] = geometry->nodes->GetCoord(iPoint, iDim);
-
-  su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
-
-  if (cylindrical) {
-    X_0 = config->GetFFD_Axis(0);
-    Y_0 = config->GetFFD_Axis(1);
-    Z_0 = config->GetFFD_Axis(2);
-
-    Xbar = Coord[0] - X_0;
-    Ybar = Coord[1] - Y_0;
-    Zbar = Coord[2] - Z_0;
-
-    Coord[0] = sqrt(Ybar * Ybar + Zbar * Zbar);
-    Coord[1] = atan2(Zbar, Ybar);
-    if (Coord[1] > PI_NUMBER / 2.0) Coord[1] -= 2.0 * PI_NUMBER;
-    Coord[2] = Xbar;
+  /*--- The current approach is to subdivide each of the 6 faces of the hexahedral FFD box into 4 triangles by defining
+   a supporting middle point. This allows nonplanar FFD boxes. Note that the definition of the FFD box is as follows:
+   the FFD box is a 6-sided die and we are looking at the side "1". The opposite side is side "6". If we are looking at
+   side "1", we define the nodes counterclockwise. If we are looking at side "6", we define the face clockwise. ---*/
 
-  }
-
-  else if (spherical || polar) {
-    X_0 = config->GetFFD_Axis(0);
-    Y_0 = config->GetFFD_Axis(1);
-    Z_0 = config->GetFFD_Axis(2);
-
-    Xbar = Coord[0] - X_0;
-    Ybar = Coord[1] - Y_0;
-    Zbar = Coord[2] - Z_0;
-
-    Coord[0] = sqrt(Xbar * Xbar + Ybar * Ybar + Zbar * Zbar);
-    Coord[1] = atan2(Zbar, Ybar);
-    if (Coord[1] > PI_NUMBER / 2.0) Coord[1] -= 2.0 * PI_NUMBER;
-    Coord[2] = acos(Xbar / Coord[0]);
-  }
+  /*--- Loop over the faces of the FFD box. ---*/
 
-  /*--- loop over the faces of the FFD box  ---*/
+  for (unsigned short iFace = 0; iFace < 6; iFace++) {
+    /*--- Every face needs an interpolated middle point for the triangles. ---*/
 
-  for (unsigned short iVar = 0; iVar < 6; iVar++) {
     su2double P[3] = {0.0, 0.0, 0.0};
-
-    /*--- every face needs an interpolated middle point for the triangles ---*/
-
     for (int p = 0; p < 4; p++) {
-      P[0] += 0.25 * Coord_Corner_Points[Index[iVar][p]][0];
-      P[1] += 0.25 * Coord_Corner_Points[Index[iVar][p]][1];
-      P[2] += 0.25 * Coord_Corner_Points[Index[iVar][p]][2];
+      P[0] += 0.25 * Coord_Corner_Points[Index[iFace][p]][0];
+      P[1] += 0.25 * Coord_Corner_Points[Index[iFace][p]][1];
+      P[2] += 0.25 * Coord_Corner_Points[Index[iFace][p]][2];
     }
 
-    /*--- loop over the 4 triangles making up the FFD box. The sign is equal for all distances ---*/
+    /*--- Loop over the 4 triangles making up the FFD box. The sign should be equal for all distances. ---*/
 
-    for (unsigned short jVar = 0; jVar < 4; jVar++) {
-      su2double Distance_Point = geometry->Point2Plane_Distance(Coord, Coord_Corner_Points[Index[iVar][jVar]],
-                                                                Coord_Corner_Points[Index[iVar][jVar + 1]], P);
-      if (Distance_Point < 0) {
-        Inside = false;
-        return Inside;
+    for (int iNode = 0; iNode < 4; iNode++) {
+      const su2double* plane[] = {P, Coord_Corner_Points[Index[iFace][iNode]],
+                                  Coord_Corner_Points[Index[iFace][iNode + 1]]};
+      if (GeometryToolbox::PointToPlaneDistance(plane, coord) < 0) {
+        return false;
       }
     }
   }
-
-  return Inside;
+  return true;
 }
 
 su2double CFreeFormDefBox::GetDerivative1(su2double* uvw, unsigned short val_diff, unsigned short* ijk,
diff --git a/Common/src/grid_movement/CSurfaceMovement.cpp b/Common/src/grid_movement/CSurfaceMovement.cpp
index 1c3b49a8b96..2fc644001b4 100644
--- a/Common/src/grid_movement/CSurfaceMovement.cpp
+++ b/Common/src/grid_movement/CSurfaceMovement.cpp
@@ -27,6 +27,7 @@
 
 #include "../../include/grid_movement/CSurfaceMovement.hpp"
 #include "../../include/toolboxes/C1DInterpolation.hpp"
+#include "../../include/toolboxes/geometry_toolbox.hpp"
 
 CSurfaceMovement::CSurfaceMovement() : CGridMovement() {
   size = SU2_MPI::GetSize();
@@ -709,28 +710,23 @@ void CSurfaceMovement::CopyBoundary(CGeometry* geometry, CConfig* config) {
 
 void CSurfaceMovement::SetParametricCoord(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox,
                                           unsigned short iFFDBox) {
-  unsigned short iMarker, iDim, iOrder, jOrder, kOrder, lOrder, mOrder, nOrder;
-  unsigned long iVertex, iPoint, TotalVertex = 0;
-  su2double *CartCoordNew, *ParamCoord, CartCoord[3], ParamCoordGuess[3], MaxDiff, my_MaxDiff = 0.0, Diff, *Coord;
-  unsigned short nDim = geometry->GetnDim();
-  su2double X_0, Y_0, Z_0, Xbar, Ybar, Zbar;
-
-  unsigned short BoxFFD = true;
-  bool cylindrical = (config->GetFFD_CoordSystem() == CYLINDRICAL);
-  bool spherical = (config->GetFFD_CoordSystem() == SPHERICAL);
-  bool polar = (config->GetFFD_CoordSystem() == POLAR);
+  const auto nDim = geometry->GetnDim();
+  const bool cartesian = (config->GetFFD_CoordSystem() == CARTESIAN);
+  const bool cylindrical = (config->GetFFD_CoordSystem() == CYLINDRICAL);
+  const bool spherical = (config->GetFFD_CoordSystem() == SPHERICAL);
+  const bool polar = (config->GetFFD_CoordSystem() == POLAR);
 
-  /*--- Change order and control points reduce the
-   complexity of the point inversion (this only works with boxes,
- in case of Bezier curves, and we maintain an internal copy)---*/
+  /*--- Change order and control points reduce the complexity of the point inversion
+   (this only works with boxes, in case of Bezier curves, and we maintain an internal copy). ---*/
 
+  const bool BoxFFD = true;
   if (BoxFFD && (config->GetFFD_Blending() == BEZIER)) {
-    for (iOrder = 0; iOrder < 2; iOrder++) {
-      for (jOrder = 0; jOrder < 2; jOrder++) {
-        for (kOrder = 0; kOrder < 2; kOrder++) {
-          lOrder = 0;
-          mOrder = 0;
-          nOrder = 0;
+    for (int iOrder = 0; iOrder < 2; iOrder++) {
+      for (int jOrder = 0; jOrder < 2; jOrder++) {
+        for (int kOrder = 0; kOrder < 2; kOrder++) {
+          unsigned short lOrder = 0;
+          unsigned short mOrder = 0;
+          unsigned short nOrder = 0;
           if (iOrder == 1) {
             lOrder = FFDBox->GetlOrder() - 1;
           }
@@ -740,8 +736,7 @@ void CSurfaceMovement::SetParametricCoord(CGeometry* geometry, CConfig* config,
           if (kOrder == 1) {
             nOrder = FFDBox->GetnOrder() - 1;
           }
-
-          Coord = FFDBox->GetCoordControlPoints(lOrder, mOrder, nOrder);
+          const auto* Coord = FFDBox->GetCoordControlPoints(lOrder, mOrder, nOrder);
 
           FFDBox->SetCoordControlPoints(Coord, iOrder, jOrder, kOrder);
         }
@@ -756,101 +751,108 @@ void CSurfaceMovement::SetParametricCoord(CGeometry* geometry, CConfig* config,
     FFDBox->BlendingFunction[1]->SetOrder(2, 2);
     FFDBox->BlendingFunction[2]->SetOrder(2, 2);
   }
-  /*--- Point inversion algorithm with a basic box ---*/
-
-  ParamCoordGuess[0] = 0.5;
-  ParamCoordGuess[1] = 0.5;
-  ParamCoordGuess[2] = 0.5;
-  CartCoord[0] = 0.0;
-  CartCoord[1] = 0.0;
-  CartCoord[2] = 0.0;
 
-  /*--- Count the number of vertices ---*/
+  /*--- Point inversion algorithm with a basic box ---*/
 
-  for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++)
-    if (config->GetMarker_All_DV(iMarker) == YES)
-      for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) TotalVertex++;
+  su2double my_MaxDiff = 0.0;
+  unsigned long TotalVertex = 0;
+  unsigned long VisitedVertex = 0;
+  unsigned long MappedVertex = 0;
+  su2double ParamCoordGuess[3] = {0.5, 0.5, 0.5};
+
+  /*--- Check that the box is defined correctly for the preliminary point containment check,
+   * by checking that the midpoint of the box is considered to be inside it. ---*/
+
+  su2double BoxMidPoint[3] = {};
+  for (int iOrder = 0; iOrder < 2; iOrder++) {
+    for (int jOrder = 0; jOrder < 2; jOrder++) {
+      for (int kOrder = 0; kOrder < 2; kOrder++) {
+        const auto* Coord = FFDBox->GetCoordControlPoints(iOrder, jOrder, kOrder);
+        BoxMidPoint[0] += 0.125 * Coord[0];
+        BoxMidPoint[1] += 0.125 * Coord[1];
+        BoxMidPoint[2] += 0.125 * Coord[2];
+      }
+    }
+  }
+  if (!FFDBox->CheckPointInsideFFD(BoxMidPoint)) {
+    SU2_MPI::Error("The FFD box '" + FFDBox->GetTag() +
+                       "' is not properly defined. The first 4 points must be listed counter\n"
+                       "clockwise, such that applying the right-hand rule results in a vector into the box.\n"
+                       "This is according to the VTK hexahedron ordering.",
+                   CURRENT_FUNCTION);
+  }
 
-  for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
+  for (auto iMarker = 0u; iMarker < config->GetnMarker_All(); iMarker++) {
     if (config->GetMarker_All_DV(iMarker) == YES) {
-      for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
+      TotalVertex += geometry->nVertex[iMarker];
+
+      for (auto iVertex = 0ul; iVertex < geometry->nVertex[iMarker]; iVertex++) {
         /*--- Get the cartesian coordinates ---*/
 
-        for (iDim = 0; iDim < nDim; iDim++) CartCoord[iDim] = geometry->vertex[iMarker][iVertex]->GetCoord(iDim);
+        su2double CartCoord[3] = {};
+        for (auto iDim = 0u; iDim < nDim; iDim++) CartCoord[iDim] = geometry->vertex[iMarker][iVertex]->GetCoord(iDim);
 
         /*--- Transform the cartesian into polar ---*/
 
-        if (cylindrical) {
-          X_0 = config->GetFFD_Axis(0);
-          Y_0 = config->GetFFD_Axis(1);
-          Z_0 = config->GetFFD_Axis(2);
+        if (!cartesian) {
+          const su2double X_0 = config->GetFFD_Axis(0);
+          const su2double Y_0 = config->GetFFD_Axis(1);
+          const su2double Z_0 = config->GetFFD_Axis(2);
 
-          Xbar = CartCoord[0] - X_0;
-          Ybar = CartCoord[1] - Y_0;
-          Zbar = CartCoord[2] - Z_0;
+          const su2double Xbar = CartCoord[0] - X_0;
+          const su2double Ybar = CartCoord[1] - Y_0;
+          const su2double Zbar = CartCoord[2] - Z_0;
 
-          CartCoord[0] = sqrt(Ybar * Ybar + Zbar * Zbar);
           CartCoord[1] = atan2(Zbar, Ybar);
           if (CartCoord[1] > PI_NUMBER / 2.0) CartCoord[1] -= 2.0 * PI_NUMBER;
-          CartCoord[2] = Xbar;
-        } else if (spherical || polar) {
-          X_0 = config->GetFFD_Axis(0);
-          Y_0 = config->GetFFD_Axis(1);
-          Z_0 = config->GetFFD_Axis(2);
-
-          Xbar = CartCoord[0] - X_0;
-          Ybar = CartCoord[1] - Y_0;
-          Zbar = CartCoord[2] - Z_0;
 
-          CartCoord[0] = sqrt(Xbar * Xbar + Ybar * Ybar + Zbar * Zbar);
-          CartCoord[1] = atan2(Zbar, Ybar);
-          if (CartCoord[1] > PI_NUMBER / 2.0) CartCoord[1] -= 2.0 * PI_NUMBER;
-          CartCoord[2] = acos(Xbar / CartCoord[0]);
+          if (cylindrical) {
+            CartCoord[0] = sqrt(Ybar * Ybar + Zbar * Zbar);
+            CartCoord[2] = Xbar;
+          } else if (spherical || polar) {
+            CartCoord[0] = sqrt(Xbar * Xbar + Ybar * Ybar + Zbar * Zbar);
+            CartCoord[2] = acos(Xbar / CartCoord[0]);
+          }
         }
 
-        iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
+        const auto iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
 
-        /*--- If the point is inside the FFD, compute the value of the parametric coordinate ---*/
+        /*--- If the point is inside the FFD, compute the value of the parametric coordinate. ---*/
 
-        if (FFDBox->GetPointFFD(geometry, config, iPoint)) {
+        if (FFDBox->CheckPointInsideFFD(CartCoord)) {
           /*--- Find the parametric coordinate ---*/
 
-          ParamCoord = FFDBox->GetParametricCoord_Iterative(iPoint, CartCoord, ParamCoordGuess, config);
+          ++VisitedVertex;
+          auto* ParamCoord = FFDBox->GetParametricCoord_Iterative(iPoint, CartCoord, ParamCoordGuess, config);
 
           /*--- Compute the cartesian coordinates using the parametric coordinates
            to check that everything is correct ---*/
 
-          CartCoordNew = FFDBox->EvalCartesianCoord(ParamCoord);
+          const auto* CartCoordNew = FFDBox->EvalCartesianCoord(ParamCoord);
 
           /*--- Compute max difference between original value and the recomputed value ---*/
 
-          Diff = 0.0;
-          for (iDim = 0; iDim < nDim; iDim++)
-            Diff += (CartCoordNew[iDim] - CartCoord[iDim]) * (CartCoordNew[iDim] - CartCoord[iDim]);
-          Diff = sqrt(Diff);
+          const su2double Diff = GeometryToolbox::Distance(nDim, CartCoordNew, CartCoord);
           my_MaxDiff = max(my_MaxDiff, Diff);
 
-          /*--- If the parametric coordinates are in (0,1) the point belongs to the FFDBox, using the input tolerance
-           * ---*/
+          /*--- If the parametric coordinates are in (-tol, 1+tol) the point belongs to the FFDBox ---*/
 
           if (((ParamCoord[0] >= -config->GetFFD_Tol()) && (ParamCoord[0] <= 1.0 + config->GetFFD_Tol())) &&
               ((ParamCoord[1] >= -config->GetFFD_Tol()) && (ParamCoord[1] <= 1.0 + config->GetFFD_Tol())) &&
               ((ParamCoord[2] >= -config->GetFFD_Tol()) && (ParamCoord[2] <= 1.0 + config->GetFFD_Tol()))) {
             /*--- Rectification of the initial tolerance (we have detected situations
-             where 0.0 and 1.0 doesn't work properly ---*/
+             where 0.0 and 1.0 do not work properly. ---*/
 
-            su2double lower_limit = config->GetFFD_Tol();
-            su2double upper_limit = 1.0 - config->GetFFD_Tol();
+            const su2double lower_limit = config->GetFFD_Tol();
+            const su2double upper_limit = 1.0 - config->GetFFD_Tol();
 
-            if (ParamCoord[0] < lower_limit) ParamCoord[0] = lower_limit;
-            if (ParamCoord[1] < lower_limit) ParamCoord[1] = lower_limit;
-            if (ParamCoord[2] < lower_limit) ParamCoord[2] = lower_limit;
-            if (ParamCoord[0] > upper_limit) ParamCoord[0] = upper_limit;
-            if (ParamCoord[1] > upper_limit) ParamCoord[1] = upper_limit;
-            if (ParamCoord[2] > upper_limit) ParamCoord[2] = upper_limit;
+            ParamCoord[0] = fmin(fmax(lower_limit, ParamCoord[0]), upper_limit);
+            ParamCoord[1] = fmin(fmax(lower_limit, ParamCoord[1]), upper_limit);
+            ParamCoord[2] = fmin(fmax(lower_limit, ParamCoord[2]), upper_limit);
 
             /*--- Set the value of the parametric coordinate ---*/
 
+            ++MappedVertex;
             FFDBox->Set_MarkerIndex(iMarker);
             FFDBox->Set_VertexIndex(iVertex);
             FFDBox->Set_PointIndex(iPoint);
@@ -860,37 +862,34 @@ void CSurfaceMovement::SetParametricCoord(CGeometry* geometry, CConfig* config,
             ParamCoordGuess[0] = ParamCoord[0];
             ParamCoordGuess[1] = ParamCoord[1];
             ParamCoordGuess[2] = ParamCoord[2];
+          }
 
-            if (Diff >= config->GetFFD_Tol()) {
-              cout << "Please check this point: Local (" << ParamCoord[0] << " " << ParamCoord[1] << " "
-                   << ParamCoord[2] << ") <-> Global (" << CartCoord[0] << " " << CartCoord[1] << " " << CartCoord[2]
-                   << ") <-> Error " << Diff << " vs " << config->GetFFD_Tol() << "." << endl;
-            }
-
-          } else {
-            if (Diff >= config->GetFFD_Tol()) {
-              cout << "Please check this point: Local (" << ParamCoord[0] << " " << ParamCoord[1] << " "
-                   << ParamCoord[2] << ") <-> Global (" << CartCoord[0] << " " << CartCoord[1] << " " << CartCoord[2]
-                   << ") <-> Error " << Diff << " vs " << config->GetFFD_Tol() << "." << endl;
-            }
+          if (Diff >= config->GetFFD_Tol()) {
+            cout << "Please check this point: Local (" << ParamCoord[0] << " " << ParamCoord[1] << " " << ParamCoord[2]
+                 << ") <-> Global (" << CartCoord[0] << " " << CartCoord[1] << " " << CartCoord[2] << ") <-> Error "
+                 << Diff << " vs " << config->GetFFD_Tol() << "." << endl;
           }
         }
       }
     }
   }
 
-#ifdef HAVE_MPI
-  SU2_MPI::Allreduce(&my_MaxDiff, &MaxDiff, 1, MPI_DOUBLE, MPI_MAX, SU2_MPI::GetComm());
-#else
-  MaxDiff = my_MaxDiff;
-#endif
+  su2double MaxDiff = 0.0;
+  SU2_MPI::Reduce(&my_MaxDiff, &MaxDiff, 1, MPI_DOUBLE, MPI_MAX, MASTER_NODE, SU2_MPI::GetComm());
 
-  if (rank == MASTER_NODE)
-    cout << "Compute parametric coord      | FFD box: " << FFDBox->GetTag() << ". Max Diff: " << MaxDiff << "." << endl;
+  unsigned long GlobalVertex = 0, GlobalVisited = 0, GlobalMapped = 0;
+  SU2_MPI::Reduce(&TotalVertex, &GlobalVertex, 1, MPI_UNSIGNED_LONG, MPI_SUM, MASTER_NODE, SU2_MPI::GetComm());
+  SU2_MPI::Reduce(&VisitedVertex, &GlobalVisited, 1, MPI_UNSIGNED_LONG, MPI_SUM, MASTER_NODE, SU2_MPI::GetComm());
+  SU2_MPI::Reduce(&MappedVertex, &GlobalMapped, 1, MPI_UNSIGNED_LONG, MPI_SUM, MASTER_NODE, SU2_MPI::GetComm());
+
+  if (rank == MASTER_NODE) {
+    cout << "Computed parametric coord for FFD box '" << FFDBox->GetTag() << "'\n";
+    cout << "  Number of vertices (Total, Inside FFD, Mapped to FFD): " << GlobalVertex;
+    cout << ", " << GlobalVisited << ", " << GlobalMapped << "\n";
+    cout << "  Max coord differece: " << MaxDiff << "\n";
+  }
 
-  /*--- After the point inversion, copy the original
-   information back (this only works with boxes,
-   and we maintain an internal copy) ---*/
+  /*--- After the point inversion, copy the original information back. ---*/
 
   if (BoxFFD) {
     FFDBox->SetOriginalControlPoints();

From 5167ec10fbc4d1a5fa52878e36d0a70314f0f3fa Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 13 May 2023 20:06:48 -0700
Subject: [PATCH 453/656] 2D info

---
 Common/src/grid_movement/CSurfaceMovement.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/Common/src/grid_movement/CSurfaceMovement.cpp b/Common/src/grid_movement/CSurfaceMovement.cpp
index 2fc644001b4..37f8760ed97 100644
--- a/Common/src/grid_movement/CSurfaceMovement.cpp
+++ b/Common/src/grid_movement/CSurfaceMovement.cpp
@@ -778,7 +778,7 @@ void CSurfaceMovement::SetParametricCoord(CGeometry* geometry, CConfig* config,
     SU2_MPI::Error("The FFD box '" + FFDBox->GetTag() +
                        "' is not properly defined. The first 4 points must be listed counter\n"
                        "clockwise, such that applying the right-hand rule results in a vector into the box.\n"
-                       "This is according to the VTK hexahedron ordering.",
+                       "This is according to the VTK hexahedron ordering. The CCW convention also applies in 2D.",
                    CURRENT_FUNCTION);
   }
 

From 7622b7fed91270e0c74c1ee47b8930c7f0165264 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 14 May 2023 18:17:21 -0700
Subject: [PATCH 454/656] fix mpi race conditions, add the VTK hex to the
 message

---
 Common/src/grid_movement/CSurfaceMovement.cpp  |  9 ++++++++-
 .../py_wrapper/custom_heat_flux/run_ad.py      | 14 ++++++++++----
 TestCases/py_wrapper/custom_load_fea/run_ad.py | 18 ++++++++++++------
 3 files changed, 30 insertions(+), 11 deletions(-)

diff --git a/Common/src/grid_movement/CSurfaceMovement.cpp b/Common/src/grid_movement/CSurfaceMovement.cpp
index 37f8760ed97..2147af42f9f 100644
--- a/Common/src/grid_movement/CSurfaceMovement.cpp
+++ b/Common/src/grid_movement/CSurfaceMovement.cpp
@@ -778,7 +778,14 @@ void CSurfaceMovement::SetParametricCoord(CGeometry* geometry, CConfig* config,
     SU2_MPI::Error("The FFD box '" + FFDBox->GetTag() +
                        "' is not properly defined. The first 4 points must be listed counter\n"
                        "clockwise, such that applying the right-hand rule results in a vector into the box.\n"
-                       "This is according to the VTK hexahedron ordering. The CCW convention also applies in 2D.",
+                       "This is according to the VTK hexahedron ordering:\n"
+                       "    7 +----+ 6 \n"
+                       "     /|   /|   \n"
+                       "  4 +----+5|   \n"
+                       "    |3+--|-+ 2 \n"
+                       "    |/   |/    \n"
+                       "  0 +----+ 1   \n"
+                       "The CCW convention also applies in 2D, where only the bottom face is specified.",
                    CURRENT_FUNCTION);
   }
 
diff --git a/TestCases/py_wrapper/custom_heat_flux/run_ad.py b/TestCases/py_wrapper/custom_heat_flux/run_ad.py
index 15d2ed8d845..91695b4e6b2 100644
--- a/TestCases/py_wrapper/custom_heat_flux/run_ad.py
+++ b/TestCases/py_wrapper/custom_heat_flux/run_ad.py
@@ -103,9 +103,12 @@ def RunPrimal(size):
   Returns the final average boundary temperature.
   """
   comm = MPI.COMM_WORLD
+  rank = comm.Get_rank()
 
-  with open('config_unsteady.cfg', 'w') as f:
-    f.write(common_settings.replace('__SIZE__', str(size)) + primal_settings)
+  if rank == 0:
+    with open('config_unsteady.cfg', 'w') as f:
+      f.write(common_settings.replace('__SIZE__', str(size)) + primal_settings)
+  comm.Barrier()
 
   # Initialize the primal driver of SU2, this includes solver preprocessing.
   try:
@@ -154,9 +157,12 @@ def RunAdjoint(size):
   size of the domain and to the initial temperature.
   """
   comm = MPI.COMM_WORLD
+  rank = comm.Get_rank()
 
-  with open('config_unsteady_ad.cfg', 'w') as f:
-    f.write(common_settings.replace('__SIZE__', str(size)) + adjoint_settings)
+  if rank == 0:
+    with open('config_unsteady_ad.cfg', 'w') as f:
+      f.write(common_settings.replace('__SIZE__', str(size)) + adjoint_settings)
+  comm.Barrier()
 
   # Initialize the adjoint driver of SU2, this includes solver preprocessing.
   try:
diff --git a/TestCases/py_wrapper/custom_load_fea/run_ad.py b/TestCases/py_wrapper/custom_load_fea/run_ad.py
index 8a44b1e033f..c7b7ebbc48f 100644
--- a/TestCases/py_wrapper/custom_load_fea/run_ad.py
+++ b/TestCases/py_wrapper/custom_load_fea/run_ad.py
@@ -117,10 +117,13 @@ def RunPrimal(density, peak_load, height):
   Returns the time average objective function.
   """
   comm = MPI.COMM_WORLD
+  rank = comm.Get_rank()
 
-  with open('config_unsteady.cfg', 'w') as f:
-    f.write(common_settings.replace('__DENSITY__', str(density)).replace('__HEIGHT__', str(height)) +
-            primal_settings)
+  if rank == 0:
+    with open('config_unsteady.cfg', 'w') as f:
+      f.write(common_settings.replace('__DENSITY__', str(density)).replace('__HEIGHT__', str(height)) +
+              primal_settings)
+  comm.Barrier()
 
   # Initialize the primal driver of SU2, this includes solver preprocessing.
   try:
@@ -155,10 +158,13 @@ def RunAdjoint(density, peak_load, height):
   load, to the material density, and to the beam height.
   """
   comm = MPI.COMM_WORLD
+  rank = comm.Get_rank()
 
-  with open('config_unsteady_ad.cfg', 'w') as f:
-    f.write(common_settings.replace('__DENSITY__', str(density)).replace('__HEIGHT__', str(height)) +
-            adjoint_settings)
+  if rank == 0:
+    with open('config_unsteady_ad.cfg', 'w') as f:
+      f.write(common_settings.replace('__DENSITY__', str(density)).replace('__HEIGHT__', str(height)) +
+              adjoint_settings)
+  comm.Barrier()
 
   # Initialize the adjoint driver of SU2, this includes solver preprocessing.
   try:

From b83b4bb487a8ee8a7dcdf9e4c23177b3281e8537 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Sun, 14 May 2023 18:26:42 -0700
Subject: [PATCH 455/656] Apply suggestions from code review

---
 SU2_CFD/include/drivers/CDriverBase.hpp | 6 +++---
 1 file changed, 3 insertions(+), 3 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index 00ccb3d29b5..9625c83d74d 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -54,7 +54,7 @@ class CDriverBase {
       UsedTime;        /*!< \brief Elapsed time between Start and Stop point of the timer. */
 
   unsigned long TimeIter;
-  unsigned long selected_iZone = ZONE_0; /*!< \brief Selected zone for the driver. Defaults to ZONE_0 */
+  unsigned short selected_iZone = ZONE_0; /*!< \brief Selected zone for the driver. Defaults to ZONE_0 */
   unsigned short iMesh,  /*!< \brief Iterator on mesh levels. */
       iZone,             /*!< \brief Iterator on zones. */
       nZone,             /*!< \brief Total number of zones in the problem. */
@@ -530,12 +530,12 @@ class CDriverBase {
     main_geometry->SetCustomBoundaryHeatFlux(iMarker, iVertex, WallHeatFlux);
   }
 
-
   /*!
    * \brief Selects zone to be used for Driver operation
    * \param[in] iZone - Zone identifier.
    */
-  inline void SelectZone(unsigned long iZone) {
+  inline void SelectZone(unsigned short iZone) {
+    if (iZone >= nZone) SU2_MPI::Error("Zone index out of range", CURRENT_FUNCTION);
     selected_iZone = iZone;
     main_geometry = geometry_container[selected_iZone][INST_0][MESH_0];
     main_config = config_container[selected_iZone];

From 9ccb1b71c3a5f107dded2a97416accb1dca455c8 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 15 May 2023 13:41:03 +0200
Subject: [PATCH 456/656] Prefer master constructs over tests against thread
 num.

---
 Common/src/linear_algebra/CSysSolve.cpp | 125 ++++++++++++++++++------
 1 file changed, 94 insertions(+), 31 deletions(-)

diff --git a/Common/src/linear_algebra/CSysSolve.cpp b/Common/src/linear_algebra/CSysSolve.cpp
index fbaf2fd1def..24ffeee49fb 100644
--- a/Common/src/linear_algebra/CSysSolve.cpp
+++ b/Common/src/linear_algebra/CSysSolve.cpp
@@ -192,7 +192,7 @@ unsigned long CSysSolve<ScalarType>::CG_LinSolver(const CSysVector<ScalarType>&
                                                   const CPreconditioner<ScalarType>& precond, ScalarType tol,
                                                   unsigned long m, ScalarType& residual, bool monitoring,
                                                   const CConfig* config) const {
-  const bool master = (SU2_MPI::GetRank() == MASTER_NODE) && (omp_get_thread_num() == 0);
+  const bool masterRank = (SU2_MPI::GetRank() == MASTER_NODE);
   ScalarType norm_r = 0.0, norm0 = 0.0;
   unsigned long i = 0;
 
@@ -241,16 +241,22 @@ unsigned long CSysSolve<ScalarType>::CG_LinSolver(const CSysVector<ScalarType>&
     if (tol_type == LinearToleranceType::RELATIVE) norm0 = norm_r;
 
     if ((norm_r < tol * norm0) || (norm_r < eps)) {
-      if (master && (lin_sol_mode != LINEAR_SOLVER_MODE::MESH_DEFORM))
+      if (masterRank && (lin_sol_mode != LINEAR_SOLVER_MODE::MESH_DEFORM)) {
+        SU2_OMP_MASTER
         cout << "CSysSolve::ConjugateGradient(): system solved by initial guess." << endl;
+        END_SU2_OMP_MASTER
+      }
       return 0;
     }
 
     /*--- Output header information including initial residual ---*/
 
-    if (monitoring && master) {
-      WriteHeader("CG", tol, norm_r);
-      WriteHistory(i, norm_r / norm0);
+    if (monitoring && masterRank) {
+      SU2_OMP_MASTER {
+        WriteHeader("CG", tol, norm_r);
+        WriteHistory(i, norm_r / norm0);
+      }
+      END_SU2_OMP_MASTER
     }
   }
 
@@ -281,7 +287,11 @@ unsigned long CSysSolve<ScalarType>::CG_LinSolver(const CSysVector<ScalarType>&
 
       norm_r = r.norm();
       if (norm_r < tol * norm0) break;
-      if (((monitoring) && (master)) && ((i + 1) % monitorFreq == 0)) WriteHistory(i + 1, norm_r / norm0);
+      if (((monitoring) && (masterRank)) && ((i + 1) % monitorFreq == 0)) {
+        SU2_OMP_MASTER
+        WriteHistory(i + 1, norm_r / norm0);
+        END_SU2_OMP_MASTER
+      }
     }
 
     precond(r, z);
@@ -300,7 +310,11 @@ unsigned long CSysSolve<ScalarType>::CG_LinSolver(const CSysVector<ScalarType>&
   /*--- Recalculate final residual (this should be optional) ---*/
 
   if ((monitoring) && (config->GetComm_Level() == COMM_FULL)) {
-    if (master) WriteFinalResidual("CG", i, norm_r / norm0);
+    if (masterRank) {
+      SU2_OMP_MASTER
+      WriteFinalResidual("CG", i, norm_r / norm0);
+      END_SU2_OMP_MASTER
+    }
 
     if (recomputeRes) {
       mat_vec(x, A_x);
@@ -308,8 +322,10 @@ unsigned long CSysSolve<ScalarType>::CG_LinSolver(const CSysVector<ScalarType>&
       ScalarType true_res = r.norm();
 
       if (fabs(true_res - norm_r) > tol * 10.0) {
-        if (master) {
+        if (masterRank) {
+          SU2_OMP_MASTER
           WriteWarning(norm_r, true_res, tol);
+          END_SU2_OMP_MASTER
         }
       }
     }
@@ -325,7 +341,7 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
                                                       const CPreconditioner<ScalarType>& precond, ScalarType tol,
                                                       unsigned long m, ScalarType& residual, bool monitoring,
                                                       const CConfig* config) const {
-  const bool master = (SU2_MPI::GetRank() == MASTER_NODE) && (omp_get_thread_num() == 0);
+  const bool masterRank = (SU2_MPI::GetRank() == MASTER_NODE);
   const bool flexible = !precond.IsIdentity();
 
   /*---  Check the subspace size ---*/
@@ -386,7 +402,11 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
   if ((beta < tol * norm0) || (beta < eps)) {
     /*--- System is already solved ---*/
 
-    if (master) cout << "CSysSolve::FGMRES(): system solved by initial guess." << endl;
+    if (masterRank) {
+      SU2_OMP_MASTER
+      cout << "CSysSolve::FGMRES(): system solved by initial guess." << endl;
+      END_SU2_OMP_MASTER
+    }
     residual = beta;
     return 0;
   }
@@ -403,9 +423,12 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
   /*--- Output header information including initial residual ---*/
 
   unsigned long i = 0;
-  if ((monitoring) && (master)) {
-    WriteHeader("FGMRES", tol, beta);
-    WriteHistory(i, beta / norm0);
+  if ((monitoring) && (masterRank)) {
+    SU2_OMP_MASTER {
+      WriteHeader("FGMRES", tol, beta);
+      WriteHistory(i, beta / norm0);
+    }
+    END_SU2_OMP_MASTER
   }
 
   /*---  Loop over all search directions ---*/
@@ -444,7 +467,11 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
 
     /*---  Output the relative residual if necessary ---*/
 
-    if ((((monitoring) && (master)) && ((i + 1) % monitorFreq == 0)) && (master)) WriteHistory(i + 1, beta / norm0);
+    if ((((monitoring) && (masterRank)) && ((i + 1) % monitorFreq == 0)) && (masterRank)) {
+      SU2_OMP_MASTER
+      WriteHistory(i + 1, beta / norm0);
+      END_SU2_OMP_MASTER
+    }
   }
 
   /*---  Solve the least-squares system and update solution ---*/
@@ -460,7 +487,11 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
   /*---  Recalculate final (neg.) residual (this should be optional) ---*/
 
   if ((monitoring) && (config->GetComm_Level() == COMM_FULL)) {
-    if (master) WriteFinalResidual("FGMRES", i, beta / norm0);
+    if (masterRank) {
+      SU2_OMP_MASTER
+      WriteFinalResidual("FGMRES", i, beta / norm0);
+      END_SU2_OMP_MASTER
+    }
 
     if (recomputeRes) {
       mat_vec(x, W[0]);
@@ -468,8 +499,10 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
       ScalarType res = W[0].norm();
 
       if (fabs(res - beta) > tol * 10) {
-        if (master) {
+        if (masterRank) {
+          SU2_OMP_MASTER
           WriteWarning(beta, res, tol);
+          END_SU2_OMP_MASTER
         }
       }
     }
@@ -511,7 +544,7 @@ unsigned long CSysSolve<ScalarType>::BCGSTAB_LinSolver(const CSysVector<ScalarTy
                                                        const CPreconditioner<ScalarType>& precond, ScalarType tol,
                                                        unsigned long m, ScalarType& residual, bool monitoring,
                                                        const CConfig* config) const {
-  const bool master = (SU2_MPI::GetRank() == MASTER_NODE) && (omp_get_thread_num() == 0);
+  const bool masterRank = (SU2_MPI::GetRank() == MASTER_NODE);
   ScalarType norm_r = 0.0, norm0 = 0.0;
   unsigned long i = 0;
 
@@ -561,15 +594,22 @@ unsigned long CSysSolve<ScalarType>::BCGSTAB_LinSolver(const CSysVector<ScalarTy
     if (tol_type == LinearToleranceType::RELATIVE) norm0 = norm_r;
 
     if ((norm_r < tol * norm0) || (norm_r < eps)) {
-      if (master) cout << "CSysSolve::BCGSTAB(): system solved by initial guess." << endl;
+      if (masterRank) {
+        SU2_OMP_MASTER
+        cout << "CSysSolve::BCGSTAB(): system solved by initial guess." << endl;
+        END_SU2_OMP_MASTER
+      }
       return 0;
     }
 
     /*--- Output header information including initial residual ---*/
 
-    if ((monitoring) && (master)) {
-      WriteHeader("BCGSTAB", tol, norm_r);
-      WriteHistory(i, norm_r / norm0);
+    if ((monitoring) && (masterRank)) {
+      SU2_OMP_MASTER {
+        WriteHeader("BCGSTAB", tol, norm_r);
+        WriteHistory(i, norm_r / norm0);
+      }
+      END_SU2_OMP_MASTER
     }
   }
 
@@ -637,22 +677,32 @@ unsigned long CSysSolve<ScalarType>::BCGSTAB_LinSolver(const CSysVector<ScalarTy
 
       norm_r = r.norm();
       if (norm_r < tol * norm0) break;
-      if (((monitoring) && (master)) && ((i + 1) % monitorFreq == 0) && (master)) WriteHistory(i + 1, norm_r / norm0);
+      if (((monitoring) && (masterRank)) && ((i + 1) % monitorFreq == 0) && (masterRank)) {
+        SU2_OMP_MASTER
+        WriteHistory(i + 1, norm_r / norm0);
+        END_SU2_OMP_MASTER
+      }
     }
   }
 
   /*--- Recalculate final residual (this should be optional) ---*/
 
   if ((monitoring) && (config->GetComm_Level() == COMM_FULL)) {
-    if (master) WriteFinalResidual("BCGSTAB", i, norm_r / norm0);
+    if (masterRank) {
+      SU2_OMP_MASTER
+      WriteFinalResidual("BCGSTAB", i, norm_r / norm0);
+      END_SU2_OMP_MASTER
+    }
 
     if (recomputeRes) {
       mat_vec(x, A_x);
       r = b - A_x;
       ScalarType true_res = r.norm();
 
-      if ((fabs(true_res - norm_r) > tol * 10.0) && (master)) {
+      if ((fabs(true_res - norm_r) > tol * 10.0) && (masterRank)) {
+        SU2_OMP_MASTER
         WriteWarning(norm_r, true_res, tol);
+        END_SU2_OMP_MASTER
       }
     }
   }
@@ -667,7 +717,7 @@ unsigned long CSysSolve<ScalarType>::Smoother_LinSolver(const CSysVector<ScalarT
                                                         const CPreconditioner<ScalarType>& precond, ScalarType tol,
                                                         unsigned long m, ScalarType& residual, bool monitoring,
                                                         const CConfig* config) const {
-  const bool master = (SU2_MPI::GetRank() == MASTER_NODE) && (omp_get_thread_num() == 0);
+  const bool masterRank = (SU2_MPI::GetRank() == MASTER_NODE);
   const bool fix_iter_mode = tol < eps;
   ScalarType norm_r = 0.0, norm0 = 0.0;
   unsigned long i = 0;
@@ -717,15 +767,22 @@ unsigned long CSysSolve<ScalarType>::Smoother_LinSolver(const CSysVector<ScalarT
     if (tol_type == LinearToleranceType::RELATIVE) norm0 = norm_r;
 
     if ((norm_r < tol * norm0) || (norm_r < eps)) {
-      if (master) cout << "CSysSolve::Smoother_LinSolver(): system solved by initial guess." << endl;
+      if (masterRank) {
+        SU2_OMP_MASTER
+        cout << "CSysSolve::Smoother_LinSolver(): system solved by initial guess." << endl;
+        END_SU2_OMP_MASTER
+      }
       return 0;
     }
 
     /*--- Output header information including initial residual. ---*/
 
-    if ((monitoring) && (master)) {
-      WriteHeader("Smoother", tol, norm_r);
-      WriteHistory(i, norm_r / norm0);
+    if ((monitoring) && (masterRank)) {
+      SU2_OMP_MASTER {
+        WriteHeader("Smoother", tol, norm_r);
+        WriteHistory(i, norm_r / norm0);
+      }
+      END_SU2_OMP_MASTER
     }
   }
 
@@ -759,14 +816,20 @@ unsigned long CSysSolve<ScalarType>::Smoother_LinSolver(const CSysVector<ScalarT
     if (!fix_iter_mode && config->GetComm_Level() == COMM_FULL) {
       norm_r = r.norm();
       if (norm_r < tol * norm0) break;
-      if (((monitoring) && (master)) && ((i + 1) % monitorFreq == 0)) WriteHistory(i + 1, norm_r / norm0);
+      if (((monitoring) && (masterRank)) && ((i + 1) % monitorFreq == 0)) {
+        SU2_OMP_MASTER
+        WriteHistory(i + 1, norm_r / norm0);
+        END_SU2_OMP_MASTER
+      }
     }
   }
 
   if (fix_iter_mode) norm_r = r.norm();
 
-  if ((monitoring) && (master) && (config->GetComm_Level() == COMM_FULL)) {
+  if ((monitoring) && (masterRank) && (config->GetComm_Level() == COMM_FULL)) {
+    SU2_OMP_MASTER
     WriteFinalResidual("Smoother", i, norm_r / norm0);
+    END_SU2_OMP_MASTER
   }
 
   residual = norm_r / norm0;

From 1c65172c729ce32033abcbf888d6b3e6005d33f9 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 15 May 2023 20:10:02 +0200
Subject: [PATCH 457/656] Remove redundant checks for master rank.

---
 Common/src/linear_algebra/CSysSolve.cpp | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/Common/src/linear_algebra/CSysSolve.cpp b/Common/src/linear_algebra/CSysSolve.cpp
index 24ffeee49fb..f561618b6ad 100644
--- a/Common/src/linear_algebra/CSysSolve.cpp
+++ b/Common/src/linear_algebra/CSysSolve.cpp
@@ -467,7 +467,7 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
 
     /*---  Output the relative residual if necessary ---*/
 
-    if ((((monitoring) && (masterRank)) && ((i + 1) % monitorFreq == 0)) && (masterRank)) {
+    if ((((monitoring) && (masterRank)) && ((i + 1) % monitorFreq == 0))) {
       SU2_OMP_MASTER
       WriteHistory(i + 1, beta / norm0);
       END_SU2_OMP_MASTER
@@ -677,7 +677,7 @@ unsigned long CSysSolve<ScalarType>::BCGSTAB_LinSolver(const CSysVector<ScalarTy
 
       norm_r = r.norm();
       if (norm_r < tol * norm0) break;
-      if (((monitoring) && (masterRank)) && ((i + 1) % monitorFreq == 0) && (masterRank)) {
+      if (((monitoring) && (masterRank)) && ((i + 1) % monitorFreq == 0)) {
         SU2_OMP_MASTER
         WriteHistory(i + 1, norm_r / norm0);
         END_SU2_OMP_MASTER

From 6ef89debc0fcc15b0b93c5ee4d9cc9b6cb04c20f Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 15 May 2023 20:28:37 +0200
Subject: [PATCH 458/656] Do not treat passive parts as interruptions of the
 recording.

---
 Common/include/basic_types/ad_structure.hpp | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/Common/include/basic_types/ad_structure.hpp b/Common/include/basic_types/ad_structure.hpp
index c3ba75d9204..623dde2d314 100644
--- a/Common/include/basic_types/ad_structure.hpp
+++ b/Common/include/basic_types/ad_structure.hpp
@@ -523,14 +523,14 @@ FORCEINLINE void delete_handler(void* handler) {
 
 FORCEINLINE bool BeginPassive() {
   if (AD::getTape().isActive()) {
-    StopRecording();
+    AD::getTape().setPassive();
     return true;
   }
   return false;
 }
 
 FORCEINLINE void EndPassive(bool wasActive) {
-  if (wasActive) StartRecording();
+  if (wasActive) AD::getTape().setActive();
 }
 
 FORCEINLINE bool PausePreaccumulation() {

From eaf0389ab09a3f0ed5e7223ac791d0793021ec3d Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 15 May 2023 20:29:27 +0200
Subject: [PATCH 459/656] Drop bounds checking in AD::SetDerivative().

Introduce AD::ResizeAdjoints().
Add AD::ResizeAdjoints() calls.
---
 Common/include/basic_types/ad_structure.hpp      | 9 ++++++++-
 SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp   | 1 +
 SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp | 2 ++
 SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp  | 2 ++
 4 files changed, 13 insertions(+), 1 deletion(-)

diff --git a/Common/include/basic_types/ad_structure.hpp b/Common/include/basic_types/ad_structure.hpp
index 623dde2d314..57413d87287 100644
--- a/Common/include/basic_types/ad_structure.hpp
+++ b/Common/include/basic_types/ad_structure.hpp
@@ -369,9 +369,16 @@ FORCEINLINE void Reset() {
   }
 }
 
+FORCEINLINE void ResizeAdjoints() { AD::getTape().resizeAdjointVector(); }
+
 FORCEINLINE void SetIndex(int& index, const su2double& data) { index = data.getIdentifier(); }
 
-FORCEINLINE void SetDerivative(int index, const double val) { AD::getTape().setGradient(index, val); }
+// WARNING: For performance reasons, this method does not perform bounds checking.
+// When using it, please ensure sufficient adjoint vector size by a call to AD::ResizeAdjoints().
+FORCEINLINE void SetDerivative(int index, const double val) {
+  using ResizingPolicy = codi::GradientAccessTapeInterface<su2double::Gradient, su2double::Identifier>::ResizingPolicy;
+  AD::getTape().setGradient(index, val, ResizingPolicy::NoBoundsChecking);
+}
 
 FORCEINLINE double GetDerivative(int index) { return AD::getTape().getGradient(index); }
 
diff --git a/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
index a37971f0aeb..0ecf23e17fc 100644
--- a/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
@@ -274,6 +274,7 @@ void CDiscAdjFEAIteration::InitializeAdjoint(CSolver***** solver, CGeometry****
                                              unsigned short iZone, unsigned short iInst) {
   /*--- Initialize the adjoints the conservative variables ---*/
 
+  AD::ResizeAdjoints();
   solver[iZone][iInst][MESH_0][ADJFEA_SOL]->SetAdjoint_Output(geometry[iZone][iInst][MESH_0], config[iZone]);
 }
 
diff --git a/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
index 5b451907865..004d9cabfa4 100644
--- a/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
@@ -360,6 +360,8 @@ void CDiscAdjFluidIteration::InitializeAdjoint(CSolver***** solver, CGeometry***
   auto solvers0 = solver[iZone][iInst][MESH_0];
   auto geometry0 = geometry[iZone][iInst][MESH_0];
 
+  AD::ResizeAdjoints();
+
   SU2_OMP_PARALLEL_(if(solvers0[ADJFLOW_SOL]->GetHasHybridParallel())) {
 
   /*--- Initialize the adjoints the conservative variables ---*/
diff --git a/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
index a7935c92b19..0d220db739e 100644
--- a/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
@@ -157,6 +157,8 @@ void CDiscAdjHeatIteration::InitializeAdjoint(CSolver***** solver, CGeometry****
                                               unsigned short iZone, unsigned short iInst) {
 
   /*--- Initialize the adjoints the solution variables ---*/
+
+  AD::ResizeAdjoints();
   solver[iZone][iInst][MESH_0][ADJHEAT_SOL]->SetAdjoint_Output(geometry[iZone][iInst][MESH_0], config[iZone]);
 }
 

From 5462786a7491caa3443764dbeecaba85d96f01ac Mon Sep 17 00:00:00 2001
From: Daniel Mayer <daniel.mayer4@us.bosch.com>
Date: Mon, 15 May 2023 13:56:14 -0700
Subject: [PATCH 460/656] Remove some white-space to make CodeFactor happy.

---
 TestCases/TestCase.py | 36 ++++++++++++++++++------------------
 1 file changed, 18 insertions(+), 18 deletions(-)

diff --git a/TestCases/TestCase.py b/TestCases/TestCase.py
index 132f28bbfc4..473851451e0 100644
--- a/TestCases/TestCase.py
+++ b/TestCases/TestCase.py
@@ -342,14 +342,14 @@ def run_filediff(self):
                     # Else test word by word with given tolerance
                     else:
 
-                        diff            = [];
-                        max_delta       = 0
+                        diff = []
+                        max_delta = 0
                         compare_counter = 0
-                        ignore_counter  = 0
+                        ignore_counter = 0
 
                         # Assert that both files have the same number of lines
                         if len(fromlines) != len(tolines):
-                            diff   = ["ERROR: Number of lines in " + fromfile + " and " + tofile + " differ."]
+                            diff = ["ERROR: Number of lines in " + fromfile + " and " + tofile + " differ."]
                             passed = False
                         
                         # Loop through all lines
@@ -359,11 +359,11 @@ def run_filediff(self):
 
                             # Extract next line and split it
                             from_line = fromlines[i_line].split()
-                            to_line   = tolines[i_line].split()
+                            to_line = tolines[i_line].split()
 
                             # Assert that both lines have the same number of words
                             if len(from_line) != len(to_line):
-                                diff   = ["ERROR: Number of words in line " + str(i_line+1) + " differ."]
+                                diff = ["ERROR: Number of words in line " + str(i_line+1) + " differ."]
                                 passed = False
                                 break
                             
@@ -372,15 +372,15 @@ def run_filediff(self):
 
                                 # Extract next word and strip whitespace and commas
                                 from_word = from_line[i_word].strip().strip(',')
-                                to_word   = to_line[i_word].strip().strip(',')
+                                to_word = to_line[i_word].strip().strip(',')
 
                                 # Assert that words are either both numeric or both non-numeric
                                 from_isfloat = is_float(from_word)
-                                to_isfloat   = is_float(to_word)
+                                to_isfloat = is_float(to_word)
                                 if from_isfloat != to_isfloat:
-                                    diff      = ["ERROR: File entries '" + from_word + "' and '" + to_word + "' in line " + str(i_line+1) + ", word " + str(i_word+1) + " differ."]
-                                    passed    = False
-                                    delta     = 0.0
+                                    diff = ["ERROR: File entries '" + from_word + "' and '" + to_word + "' in line " + str(i_line+1) + ", word " + str(i_word+1) + " differ."]
+                                    passed = False
+                                    delta = 0.0
                                     max_delta = "Not applicable"
                                     break
 
@@ -405,16 +405,16 @@ def run_filediff(self):
 
                                 # Compare non-floats
                                 else:
-                                    delta  = 0.0
+                                    delta = 0.0
                                     compare_counter += 1
                                     if from_word != to_word:
-                                        diff      = ["ERROR: File entries '" + from_word + "' and '" + to_word + "' in line " + str(i_line+1) + ", word " + str(i_word+1) + " differ."]
-                                        passed    = False
+                                        diff = ["ERROR: File entries '" + from_word + "' and '" + to_word + "' in line " + str(i_line+1) + ", word " + str(i_word+1) + " differ."]
+                                        passed = False
                                         max_delta = "Not applicable"
                                         break
 
                                 if delta > self.tol_file_percent:
-                                    diff   = ["ERROR: File entries '" + from_word + "' and '" + to_word + "' in line " + str(i_line+1) + ", word " + str(i_word+1) + " differ."]
+                                    diff = ["ERROR: File entries '" + from_word + "' and '" + to_word + "' in line " + str(i_line+1) + ", word " + str(i_word+1) + " differ."]
                                     passed = False
                                     break
 
@@ -439,7 +439,7 @@ def run_filediff(self):
 
         # Report results
         diff_time_stop = datetime.datetime.now()
-        diff_time      = (diff_time_stop - diff_time_start).microseconds
+        diff_time = (diff_time_stop - diff_time_start).microseconds
 
         print('CPU architecture:    %s'%self.cpu_arch)
         print('Test duration:       %.2f min'%(running_time/60.0))
@@ -755,7 +755,7 @@ def run_def(self):
                 except AttributeError: # popen.kill apparently fails on some versions of subprocess... the killall command should take care of things!
                     pass
                 timed_out = True
-                passed    = False
+                passed = False
 
         # Examine the output
         f = open(logfilename,'r')
@@ -789,7 +789,7 @@ def run_def(self):
                             delta_vals.append( abs(float(data[j])-self.test_vals[j]) )
                             if delta_vals[j] > self.tol:
                                 exceed_tol = True
-                                passed     = False
+                                passed = False
                         break
                     else:
                         iter_missing = True

From dd579c7d0be1f028f65fb126a4763a49d2a9092f Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 17 May 2023 14:48:31 +0200
Subject: [PATCH 461/656] CoDiPack update.

---
 externals/codi        | 2 +-
 meson_scripts/init.py | 2 +-
 2 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/externals/codi b/externals/codi
index 21e4f6e084d..13874231e23 160000
--- a/externals/codi
+++ b/externals/codi
@@ -1 +1 @@
-Subproject commit 21e4f6e084d635e7834ca55dc9d83b667a5aca2b
+Subproject commit 13874231e23186f18622f116cb0cc049cb90c778
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 47f5841a74a..a19d5f7d836 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -54,7 +54,7 @@ def init_submodules(
 
     # This information of the modules is used if projects was not cloned using git
     # The sha tag must be maintained manually to point to the correct commit
-    sha_version_codi = "21e4f6e084d635e7834ca55dc9d83b667a5aca2b"
+    sha_version_codi = "13874231e23186f18622f116cb0cc049cb90c778"
     github_repo_codi = "https://github.com/scicompkl/CoDiPack"
     sha_version_medi = "aafc2d1966ba1233640af737e71c77c1a86183fd"
     github_repo_medi = "https://github.com/SciCompKL/MeDiPack"

From a52d22f5735a04a39c8c20fdc2f9227bbef6e7e7 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 17 May 2023 14:49:25 +0200
Subject: [PATCH 462/656] OpDiLib update.

---
 externals/opdi        | 2 +-
 meson_scripts/init.py | 2 +-
 2 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/externals/opdi b/externals/opdi
index f33b507c24f..3ff7bb16bd7 160000
--- a/externals/opdi
+++ b/externals/opdi
@@ -1 +1 @@
-Subproject commit f33b507c24f7448d4cf4df16ab5c53ea254b8774
+Subproject commit 3ff7bb16bd70aa8f74277704b5feccaaaf6838bd
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index a19d5f7d836..18ec2ece2af 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -58,7 +58,7 @@ def init_submodules(
     github_repo_codi = "https://github.com/scicompkl/CoDiPack"
     sha_version_medi = "aafc2d1966ba1233640af737e71c77c1a86183fd"
     github_repo_medi = "https://github.com/SciCompKL/MeDiPack"
-    sha_version_opdi = "f33b507c24f7448d4cf4df16ab5c53ea254b8774"
+    sha_version_opdi = "3ff7bb16bd70aa8f74277704b5feccaaaf6838bd"
     github_repo_opdi = "https://github.com/SciCompKL/OpDiLib"
     sha_version_meson = "41c650a040d50e0912d268af7a903a9ce1456dfa"
     github_repo_meson = "https://github.com/mesonbuild/meson"

From 2531972cc40ef04c09270a57f08ff2cd7aea1b1a Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 17 May 2023 14:50:29 +0200
Subject: [PATCH 463/656] Refactor ResizingPolicy -> BoundsChecking.

---
 Common/include/basic_types/ad_structure.hpp | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/Common/include/basic_types/ad_structure.hpp b/Common/include/basic_types/ad_structure.hpp
index 57413d87287..4ff1849853b 100644
--- a/Common/include/basic_types/ad_structure.hpp
+++ b/Common/include/basic_types/ad_structure.hpp
@@ -376,8 +376,8 @@ FORCEINLINE void SetIndex(int& index, const su2double& data) { index = data.getI
 // WARNING: For performance reasons, this method does not perform bounds checking.
 // When using it, please ensure sufficient adjoint vector size by a call to AD::ResizeAdjoints().
 FORCEINLINE void SetDerivative(int index, const double val) {
-  using ResizingPolicy = codi::GradientAccessTapeInterface<su2double::Gradient, su2double::Identifier>::ResizingPolicy;
-  AD::getTape().setGradient(index, val, ResizingPolicy::NoBoundsChecking);
+  using BoundsChecking = codi::GradientAccessTapeInterface<su2double::Gradient, su2double::Identifier>::BoundsChecking;
+  AD::getTape().setGradient(index, val, BoundsChecking::False);
 }
 
 FORCEINLINE double GetDerivative(int index) { return AD::getTape().getGradient(index); }

From 9a73f673f1a2f1d18b799d0a196e0aa832a35f8e Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 17 May 2023 15:01:14 +0200
Subject: [PATCH 464/656] Drop bounds checking in AD::GetDerivative().

---
 Common/include/basic_types/ad_structure.hpp | 8 +++++++-
 1 file changed, 7 insertions(+), 1 deletion(-)

diff --git a/Common/include/basic_types/ad_structure.hpp b/Common/include/basic_types/ad_structure.hpp
index 4ff1849853b..7b5ee4e35ca 100644
--- a/Common/include/basic_types/ad_structure.hpp
+++ b/Common/include/basic_types/ad_structure.hpp
@@ -380,7 +380,13 @@ FORCEINLINE void SetDerivative(int index, const double val) {
   AD::getTape().setGradient(index, val, BoundsChecking::False);
 }
 
-FORCEINLINE double GetDerivative(int index) { return AD::getTape().getGradient(index); }
+// WARNING: For performance reasons, this method does not perform bounds checking.
+// If called after tape evaluations, the adjoints should exist.
+// Otherwise, please ensure sufficient adjoint vector size by a call to AD::ResizeAdjoints().
+FORCEINLINE double GetDerivative(int index) {
+  using BoundsChecking = codi::GradientAccessTapeInterface<su2double::Gradient, su2double::Identifier>::BoundsChecking;
+  return AD::getTape().getGradient(index, BoundsChecking::False);
+}
 
 FORCEINLINE bool IsIdentifierActive(su2double const& value) {
   return getTape().isIdentifierActive(value.getIdentifier());

From 7478e133e5ec0040f3ff9fd666ec3620f1ab8bcc Mon Sep 17 00:00:00 2001
From: Daniel Mayer <daniel.mayer4@us.bosch.com>
Date: Wed, 17 May 2023 10:10:16 -0700
Subject: [PATCH 465/656] Fix functionality of 'WRT_*_OVERWRITE' flags.

---
 SU2_CFD/src/output/COutput.cpp | 140 ++++++++++++++++++++++++++++-----
 1 file changed, 120 insertions(+), 20 deletions(-)

diff --git a/SU2_CFD/src/output/COutput.cpp b/SU2_CFD/src/output/COutput.cpp
index cb689a0d48a..ff476a5c71c 100644
--- a/SU2_CFD/src/output/COutput.cpp
+++ b/SU2_CFD/src/output/COutput.cpp
@@ -337,6 +337,7 @@ void COutput::LoadData(CGeometry *geometry, CConfig *config, CSolver** solver_co
 void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE format, string fileName){
 
   CFileWriter *fileWriter = nullptr;
+  bool do_write_iter_file = false;
 
   /*--- if it is still present, strip the extension (suffix) from the filename ---*/
   unsigned short lastindex = fileName.find_last_of('.');
@@ -361,6 +362,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       surfaceDataSorter->SortConnectivity(config, geometry);
       surfaceDataSorter->SortOutputData();
 
+      /*--- Write output information to screen ---*/
       if (rank == MASTER_NODE) {
         (*fileWritingTable) << "CSV file" << fileName + extension;
 
@@ -368,8 +370,14 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
           (*fileWritingTable) << "CSV file + iter" << filename_iter + extension;
       }
 
+      /*--- Create file writer that will later be used to write the file to disk ---*/
       fileWriter = new CSU2FileWriter(surfaceDataSorter);
 
+      /*--- If file overwrite is turned off, switch on additional file output
+       *    with the value of 'filename_iter' as file name ---*/
+      if (!config->GetWrt_Surface_Overwrite())
+        do_write_iter_file = true;
+
       break;
 
     case OUTPUT_TYPE::RESTART_ASCII: case OUTPUT_TYPE::CSV:
@@ -382,7 +390,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       if (!config->GetWrt_Restart_Overwrite())
         filename_iter = config->GetFilename_Iter(fileName,curInnerIter, curOuterIter);
 
-
+      /*--- Write output information to screen ---*/
       if (rank == MASTER_NODE) {
         (*fileWritingTable) << "SU2 ASCII restart" << fileName + extension;
 
@@ -390,8 +398,14 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
           (*fileWritingTable) << "SU2 ASCII restart + iter" << filename_iter + extension;
       }
 
+      /*--- Create file writer that will later be used to write the file to disk ---*/
       fileWriter = new CSU2FileWriter(volumeDataSorter);
 
+      /*--- If file overwrite is turned off, switch on additional file output
+       *    with the value of 'filename_iter' as file name ---*/
+      if (!config->GetWrt_Restart_Overwrite())
+        do_write_iter_file = true;
+
       break;
 
     case OUTPUT_TYPE::RESTART_BINARY:
@@ -404,7 +418,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       if (!config->GetWrt_Restart_Overwrite())
         filename_iter = config->GetFilename_Iter(fileName,curInnerIter, curOuterIter);
 
-
+      /*--- Write output information to screen ---*/
       if (rank == MASTER_NODE) {
         (*fileWritingTable) << "SU2 binary restart" << fileName + extension;
 
@@ -413,8 +427,13 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
 
       }
 
+      /*--- Create file writer that will later be used to write the file to disk ---*/
       fileWriter = new CSU2BinaryFileWriter(volumeDataSorter);
 
+      /*--- If file overwrite is turned off, switch on additional file output
+       *    with the value of 'filename_iter' as file name ---*/
+      if (!config->GetWrt_Restart_Overwrite())
+        do_write_iter_file = true;
 
       break;
 
@@ -432,7 +451,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
 
       volumeDataSorter->SortConnectivity(config, geometry, true);
 
-      /*--- Set the mesh ASCII format ---*/
+      /*--- Write output information to screen ---*/
       if (rank == MASTER_NODE) {
         (*fileWritingTable) << "SU2 mesh" << fileName + extension;
 
@@ -440,9 +459,14 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
           (*fileWritingTable) << "SU2 mesh + iter" << filename_iter + extension;
       }
 
+      /*--- Create file writer that will later be used to write the file to disk ---*/
       fileWriter = new CSU2MeshFileWriter(volumeDataSorter,
                                           config->GetiZone(), config->GetnZone());
 
+      /*--- If file overwrite is turned off, switch on additional file output
+       *    with the value of 'filename_iter' as file name ---*/
+      if (!config->GetWrt_Volume_Overwrite())
+        do_write_iter_file = true;
 
       break;
 
@@ -460,7 +484,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
 
       volumeDataSorter->SortConnectivity(config, geometry, false);
 
-      /*--- Write tecplot binary ---*/
+      /*--- Write output information to screen ---*/
       if (rank == MASTER_NODE) {
         (*fileWritingTable) << "Tecplot binary" << fileName + extension;
 
@@ -468,9 +492,15 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
           (*fileWritingTable) << "Tecplot binary + iter" << filename_iter + extension;
       }
 
+      /*--- Create file writer that will later be used to write the file to disk ---*/
       fileWriter = new CTecplotBinaryFileWriter(volumeDataSorter,
                                                 curTimeIter, GetHistoryFieldValue("TIME_STEP"));
 
+      /*--- If file overwrite is turned off, switch on additional file output
+       *    with the value of 'filename_iter' as file name ---*/
+      if (!config->GetWrt_Volume_Overwrite())
+        do_write_iter_file = true;
+
       break;
 
     case OUTPUT_TYPE::TECPLOT_ASCII:
@@ -487,7 +517,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
 
       volumeDataSorter->SortConnectivity(config, geometry, true);
 
-      /*--- Write tecplot ascii ---*/
+      /*--- Write output information to screen ---*/
       if (rank == MASTER_NODE) {
         (*fileWritingTable) << "Tecplot ASCII" << fileName + extension;
 
@@ -495,9 +525,15 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
           (*fileWritingTable) << "Tecplot ASCII + iter" << filename_iter + extension;
       }
 
+      /*--- Create file writer that will later be used to write the file to disk ---*/
       fileWriter = new CTecplotFileWriter(volumeDataSorter,
                                           curTimeIter, GetHistoryFieldValue("TIME_STEP"));
 
+      /*--- If file overwrite is turned off, switch on additional file output
+       *    with the value of 'filename_iter' as file name ---*/
+      if (!config->GetWrt_Volume_Overwrite())
+        do_write_iter_file = true;
+
       break;
 
     case OUTPUT_TYPE::PARAVIEW_XML:
@@ -514,7 +550,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
 
       volumeDataSorter->SortConnectivity(config, geometry, true);
 
-      /*--- Write paraview binary ---*/
+      /*--- Write output information to screen ---*/
       if (rank == MASTER_NODE) {
         (*fileWritingTable) << "Paraview" << fileName + extension;
 
@@ -522,8 +558,14 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
           (*fileWritingTable) << "Paraview + iter" << filename_iter + extension;
       }
 
+      /*--- Create file writer that will later be used to write the file to disk ---*/
       fileWriter = new CParaviewXMLFileWriter(volumeDataSorter);
 
+      /*--- If file overwrite is turned off, switch on additional file output
+       *    with the value of 'filename_iter' as file name ---*/
+      if (!config->GetWrt_Volume_Overwrite())
+        do_write_iter_file = true;
+
       break;
 
     case OUTPUT_TYPE::PARAVIEW_LEGACY_BINARY:
@@ -540,7 +582,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
 
       volumeDataSorter->SortConnectivity(config, geometry, true);
 
-      /*--- Write paraview binary ---*/
+      /*--- Write output information to screen ---*/
       if (rank == MASTER_NODE) {
         (*fileWritingTable) << "Paraview binary (legacy)" << fileName + extension;
 
@@ -548,8 +590,14 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
           (*fileWritingTable) << "Paraview binary + iter" << filename_iter + extension;
       }
 
+      /*--- Create file writer that will later be used to write the file to disk ---*/
       fileWriter = new CParaviewBinaryFileWriter(volumeDataSorter);
 
+      /*--- If file overwrite is turned off, switch on additional file output
+       *    with the value of 'filename_iter' as file name ---*/
+      if (!config->GetWrt_Volume_Overwrite())
+        do_write_iter_file = true;
+
       break;
 
     case OUTPUT_TYPE::PARAVIEW_MULTIBLOCK:
@@ -567,6 +615,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
 
         volumeDataSorter->SortConnectivity(config, geometry, true);
 
+        /*--- Write output information to screen ---*/
         if (rank == MASTER_NODE) {
           (*fileWritingTable) << "Paraview Multiblock" << fileName + extension;
 
@@ -575,12 +624,10 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
         }
 
         /*--- Allocate the vtm file writer (using fileName as the folder name) ---*/
-
         fileWriter = new CParaviewVTMFileWriter(GetHistoryFieldValue("CUR_TIME"),
                                                 config->GetiZone(), config->GetnZone());
 
         /*--- We cast the pointer to its true type, to avoid virtual functions ---*/
-
         auto* vtmWriter = dynamic_cast<CParaviewVTMFileWriter*>(fileWriter);
 
         /*--- then we write the data into the folder---*/
@@ -609,7 +656,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
 
       volumeDataSorter->SortConnectivity(config, geometry, true);
 
-      /*--- Write paraview ascii ---*/
+      /*--- Write output information to screen ---*/
       if (rank == MASTER_NODE) {
         (*fileWritingTable) << "Paraview ASCII" << fileName + extension;
 
@@ -617,8 +664,14 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
           (*fileWritingTable) << "Paraview ASCII + iter" << filename_iter + extension;
       }
 
+      /*--- Create file writer that will later be used to write the file to disk ---*/
       fileWriter = new CParaviewFileWriter(volumeDataSorter);
 
+      /*--- If file overwrite is turned off, switch on additional file output
+       *    with the value of 'filename_iter' as file name ---*/
+      if (!config->GetWrt_Volume_Overwrite())
+        do_write_iter_file = true;
+
       break;
 
     case OUTPUT_TYPE::SURFACE_PARAVIEW_ASCII:
@@ -637,7 +690,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       surfaceDataSorter->SortConnectivity(config, geometry);
       surfaceDataSorter->SortOutputData();
 
-      /*--- Write surface paraview ascii ---*/
+      /*--- Write output information to screen ---*/
       if (rank == MASTER_NODE) {
         (*fileWritingTable) << "Paraview ASCII surface" << fileName + extension;
 
@@ -645,8 +698,14 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
           (*fileWritingTable) << "Paraview ASCII + iter" << filename_iter + extension;
       }
 
+      /*--- Create file writer that will later be used to write the file to disk ---*/
       fileWriter = new CParaviewFileWriter(surfaceDataSorter);
 
+      /*--- If file overwrite is turned off, switch on additional file output
+       *    with the value of 'filename_iter' as file name ---*/
+      if (!config->GetWrt_Surface_Overwrite())
+        do_write_iter_file = true;
+
       break;
 
     case OUTPUT_TYPE::SURFACE_PARAVIEW_LEGACY_BINARY:
@@ -665,7 +724,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       surfaceDataSorter->SortConnectivity(config, geometry);
       surfaceDataSorter->SortOutputData();
 
-      /*--- Write surface paraview binary ---*/
+      /*--- Write output information to screen ---*/
       if (rank == MASTER_NODE) {
         (*fileWritingTable) << "Paraview binary surface (legacy)" << fileName + extension;
 
@@ -673,8 +732,14 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
           (*fileWritingTable) << "Paraview binary surface + iter" << filename_iter + extension;
       }
 
+      /*--- Create file writer that will later be used to write the file to disk ---*/
       fileWriter = new CParaviewBinaryFileWriter(surfaceDataSorter);
 
+      /*--- If file overwrite is turned off, switch on additional file output
+       *    with the value of 'filename_iter' as file name ---*/
+      if (!config->GetWrt_Surface_Overwrite())
+        do_write_iter_file = true;
+
       break;
 
     case OUTPUT_TYPE::SURFACE_PARAVIEW_XML:
@@ -693,7 +758,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       surfaceDataSorter->SortConnectivity(config, geometry);
       surfaceDataSorter->SortOutputData();
 
-      /*--- Write paraview binary ---*/
+      /*--- Write output information to screen ---*/
       if (rank == MASTER_NODE) {
         (*fileWritingTable) << "Paraview surface" << fileName + extension;
 
@@ -701,8 +766,14 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
           (*fileWritingTable) << "Paraview surface + iter" << filename_iter + extension;
       }
 
+      /*--- Create file writer that will later be used to write the file to disk ---*/
       fileWriter = new CParaviewXMLFileWriter(surfaceDataSorter);
 
+      /*--- If file overwrite is turned off, switch on additional file output
+       *    with the value of 'filename_iter' as file name ---*/
+      if (!config->GetWrt_Surface_Overwrite())
+        do_write_iter_file = true;
+
       break;
 
     case OUTPUT_TYPE::SURFACE_TECPLOT_ASCII:
@@ -721,7 +792,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       surfaceDataSorter->SortConnectivity(config, geometry);
       surfaceDataSorter->SortOutputData();
 
-      /*--- Write surface tecplot ascii ---*/
+      /*--- Write output information to screen ---*/
       if (rank == MASTER_NODE) {
         (*fileWritingTable) << "Tecplot ASCII surface" << fileName + extension;
 
@@ -730,9 +801,15 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
 
       }
 
+      /*--- Create file writer that will later be used to write the file to disk ---*/
       fileWriter = new CTecplotFileWriter(surfaceDataSorter,
                                           curTimeIter, GetHistoryFieldValue("TIME_STEP"));
 
+      /*--- If file overwrite is turned off, switch on additional file output
+       *    with the value of 'filename_iter' as file name ---*/
+      if (!config->GetWrt_Surface_Overwrite())
+        do_write_iter_file = true;
+
       break;
 
     case OUTPUT_TYPE::SURFACE_TECPLOT_BINARY:
@@ -751,7 +828,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       surfaceDataSorter->SortConnectivity(config, geometry);
       surfaceDataSorter->SortOutputData();
 
-      /*--- Write surface tecplot binary ---*/
+      /*--- Write output information to screen ---*/
       if (rank == MASTER_NODE) {
         (*fileWritingTable) << "Tecplot binary surface" << fileName + extension;
 
@@ -760,9 +837,15 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
 
       }
 
+      /*--- Create file writer that will later be used to write the file to disk ---*/
       fileWriter = new CTecplotBinaryFileWriter(surfaceDataSorter,
                                                 curTimeIter, GetHistoryFieldValue("TIME_STEP"));
 
+      /*--- If file overwrite is turned off, switch on additional file output
+       *    with the value of 'filename_iter' as file name ---*/
+      if (!config->GetWrt_Surface_Overwrite())
+        do_write_iter_file = true;
+
       break;
 
     case OUTPUT_TYPE::STL_ASCII:
@@ -777,11 +860,10 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
 
 
       /*--- Load and sort the output data and connectivity. ---*/
-
       surfaceDataSorter->SortConnectivity(config, geometry);
       surfaceDataSorter->SortOutputData();
 
-      /*--- Write ASCII STL ---*/
+      /*--- Write output information to screen ---*/
       if (rank == MASTER_NODE) {
         (*fileWritingTable) << "STL ASCII" << fileName + extension;
 
@@ -790,8 +872,14 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
 
       }
 
+      /*--- Create file writer that will later be used to write the file to disk ---*/
       fileWriter = new CSTLFileWriter(surfaceDataSorter);
 
+      /*--- If file overwrite is turned off, switch on additional file output
+       *    with the value of 'filename_iter' as file name ---*/
+      if (!config->GetWrt_Surface_Overwrite())
+        do_write_iter_file = true;
+
       break;
 
     case OUTPUT_TYPE::CGNS:
@@ -808,7 +896,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       /*--- Load and sort the output data and connectivity. ---*/
       volumeDataSorter->SortConnectivity(config, geometry, true);
 
-      /*--- Write CGNS ---*/
+      /*--- Write output information to screen ---*/
       if (rank == MASTER_NODE) {
         (*fileWritingTable) << "CGNS" << fileName + extension;
 
@@ -817,8 +905,14 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
 
       }
 
+      /*--- Create file writer that will later be used to write the file to disk ---*/
       fileWriter = new CCGNSFileWriter(volumeDataSorter);
 
+      /*--- If file overwrite is turned off, switch on additional file output
+       *    with the value of 'filename_iter' as file name ---*/
+      if (!config->GetWrt_Volume_Overwrite())
+        do_write_iter_file = true;
+
       break;
 
     case OUTPUT_TYPE::SURFACE_CGNS:
@@ -836,7 +930,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       surfaceDataSorter->SortConnectivity(config, geometry);
       surfaceDataSorter->SortOutputData();
 
-      /*--- Write SURFACE_CGNS ---*/
+      /*--- Write output information to screen ---*/
       if (rank == MASTER_NODE) {
         (*fileWritingTable) << "CGNS surface" << fileName + extension;
 
@@ -845,8 +939,14 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
 
       }
 
+      /*--- Create file writer that will later be used to write the file to disk ---*/
       fileWriter = new CCGNSFileWriter(surfaceDataSorter, true);
 
+      /*--- If file overwrite is turned off, switch on additional file output
+       *    with the value of 'filename_iter' as file name ---*/
+      if (!config->GetWrt_Surface_Overwrite())
+        do_write_iter_file = true;
+
       break;
 
     default:
@@ -863,7 +963,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
 
     /*--- Write data with iteration number to file ---*/
 
-    if (!filename_iter.empty() && !config->GetWrt_Restart_Overwrite()){
+    if (!filename_iter.empty() && do_write_iter_file){
       fileWriter->WriteData(filename_iter);
 
       /*--- overwrite bandwidth ---*/

From 7b48ec8472566f808ad9cd4e0c1a65031e776545 Mon Sep 17 00:00:00 2001
From: Daniel Mayer <daniel.mayer4@us.bosch.com>
Date: Wed, 17 May 2023 13:31:14 -0700
Subject: [PATCH 466/656] Switch variable name from snake_case to
 lowerCamelCase.

---
 SU2_CFD/src/output/COutput.cpp | 38 +++++++++++++++++-----------------
 1 file changed, 19 insertions(+), 19 deletions(-)

diff --git a/SU2_CFD/src/output/COutput.cpp b/SU2_CFD/src/output/COutput.cpp
index ff476a5c71c..b79b42985e4 100644
--- a/SU2_CFD/src/output/COutput.cpp
+++ b/SU2_CFD/src/output/COutput.cpp
@@ -337,7 +337,7 @@ void COutput::LoadData(CGeometry *geometry, CConfig *config, CSolver** solver_co
 void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE format, string fileName){
 
   CFileWriter *fileWriter = nullptr;
-  bool do_write_iter_file = false;
+  bool doWriteIterFile = false;
 
   /*--- if it is still present, strip the extension (suffix) from the filename ---*/
   unsigned short lastindex = fileName.find_last_of('.');
@@ -376,7 +376,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       /*--- If file overwrite is turned off, switch on additional file output
        *    with the value of 'filename_iter' as file name ---*/
       if (!config->GetWrt_Surface_Overwrite())
-        do_write_iter_file = true;
+        doWriteIterFile = true;
 
       break;
 
@@ -404,7 +404,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       /*--- If file overwrite is turned off, switch on additional file output
        *    with the value of 'filename_iter' as file name ---*/
       if (!config->GetWrt_Restart_Overwrite())
-        do_write_iter_file = true;
+        doWriteIterFile = true;
 
       break;
 
@@ -433,7 +433,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       /*--- If file overwrite is turned off, switch on additional file output
        *    with the value of 'filename_iter' as file name ---*/
       if (!config->GetWrt_Restart_Overwrite())
-        do_write_iter_file = true;
+        doWriteIterFile = true;
 
       break;
 
@@ -466,7 +466,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       /*--- If file overwrite is turned off, switch on additional file output
        *    with the value of 'filename_iter' as file name ---*/
       if (!config->GetWrt_Volume_Overwrite())
-        do_write_iter_file = true;
+        doWriteIterFile = true;
 
       break;
 
@@ -499,7 +499,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       /*--- If file overwrite is turned off, switch on additional file output
        *    with the value of 'filename_iter' as file name ---*/
       if (!config->GetWrt_Volume_Overwrite())
-        do_write_iter_file = true;
+        doWriteIterFile = true;
 
       break;
 
@@ -532,7 +532,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       /*--- If file overwrite is turned off, switch on additional file output
        *    with the value of 'filename_iter' as file name ---*/
       if (!config->GetWrt_Volume_Overwrite())
-        do_write_iter_file = true;
+        doWriteIterFile = true;
 
       break;
 
@@ -564,7 +564,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       /*--- If file overwrite is turned off, switch on additional file output
        *    with the value of 'filename_iter' as file name ---*/
       if (!config->GetWrt_Volume_Overwrite())
-        do_write_iter_file = true;
+        doWriteIterFile = true;
 
       break;
 
@@ -596,7 +596,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       /*--- If file overwrite is turned off, switch on additional file output
        *    with the value of 'filename_iter' as file name ---*/
       if (!config->GetWrt_Volume_Overwrite())
-        do_write_iter_file = true;
+        doWriteIterFile = true;
 
       break;
 
@@ -670,7 +670,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       /*--- If file overwrite is turned off, switch on additional file output
        *    with the value of 'filename_iter' as file name ---*/
       if (!config->GetWrt_Volume_Overwrite())
-        do_write_iter_file = true;
+        doWriteIterFile = true;
 
       break;
 
@@ -704,7 +704,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       /*--- If file overwrite is turned off, switch on additional file output
        *    with the value of 'filename_iter' as file name ---*/
       if (!config->GetWrt_Surface_Overwrite())
-        do_write_iter_file = true;
+        doWriteIterFile = true;
 
       break;
 
@@ -738,7 +738,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       /*--- If file overwrite is turned off, switch on additional file output
        *    with the value of 'filename_iter' as file name ---*/
       if (!config->GetWrt_Surface_Overwrite())
-        do_write_iter_file = true;
+        doWriteIterFile = true;
 
       break;
 
@@ -772,7 +772,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       /*--- If file overwrite is turned off, switch on additional file output
        *    with the value of 'filename_iter' as file name ---*/
       if (!config->GetWrt_Surface_Overwrite())
-        do_write_iter_file = true;
+        doWriteIterFile = true;
 
       break;
 
@@ -808,7 +808,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       /*--- If file overwrite is turned off, switch on additional file output
        *    with the value of 'filename_iter' as file name ---*/
       if (!config->GetWrt_Surface_Overwrite())
-        do_write_iter_file = true;
+        doWriteIterFile = true;
 
       break;
 
@@ -844,7 +844,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       /*--- If file overwrite is turned off, switch on additional file output
        *    with the value of 'filename_iter' as file name ---*/
       if (!config->GetWrt_Surface_Overwrite())
-        do_write_iter_file = true;
+        doWriteIterFile = true;
 
       break;
 
@@ -878,7 +878,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       /*--- If file overwrite is turned off, switch on additional file output
        *    with the value of 'filename_iter' as file name ---*/
       if (!config->GetWrt_Surface_Overwrite())
-        do_write_iter_file = true;
+        doWriteIterFile = true;
 
       break;
 
@@ -911,7 +911,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       /*--- If file overwrite is turned off, switch on additional file output
        *    with the value of 'filename_iter' as file name ---*/
       if (!config->GetWrt_Volume_Overwrite())
-        do_write_iter_file = true;
+        doWriteIterFile = true;
 
       break;
 
@@ -945,7 +945,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
       /*--- If file overwrite is turned off, switch on additional file output
        *    with the value of 'filename_iter' as file name ---*/
       if (!config->GetWrt_Surface_Overwrite())
-        do_write_iter_file = true;
+        doWriteIterFile = true;
 
       break;
 
@@ -963,7 +963,7 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
 
     /*--- Write data with iteration number to file ---*/
 
-    if (!filename_iter.empty() && do_write_iter_file){
+    if (!filename_iter.empty() && doWriteIterFile){
       fileWriter->WriteData(filename_iter);
 
       /*--- overwrite bandwidth ---*/

From dea5d41400104946f000b8c2fdafa296eb076437 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Sat, 20 May 2023 17:39:13 -0700
Subject: [PATCH 467/656] Apply suggestions from code review

---
 SU2_CFD/src/iteration/CIteration.cpp | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/SU2_CFD/src/iteration/CIteration.cpp b/SU2_CFD/src/iteration/CIteration.cpp
index a08efb85367..517f3bff2c4 100644
--- a/SU2_CFD/src/iteration/CIteration.cpp
+++ b/SU2_CFD/src/iteration/CIteration.cpp
@@ -69,7 +69,7 @@ void CIteration::SetGrid_Movement(CGeometry** geometry, CSurfaceMovement* surfac
       /*--- Set the translational velocity on all grid levels. ---*/
 
       for (auto iMGlevel = 0u; iMGlevel <= config->GetnMGLevels(); iMGlevel++)
-        geometry[iMGlevel]->SetTranslationalVelocity(config, true);
+        geometry[iMGlevel]->SetTranslationalVelocity(config, iMGlevel == 0);
 
       break;
 
@@ -83,7 +83,7 @@ void CIteration::SetGrid_Movement(CGeometry** geometry, CSurfaceMovement* surfac
          rotating reference frame. ---*/
 
       for (auto iMGlevel = 0u; iMGlevel <= config->GetnMGLevels(); iMGlevel++){
-        geometry[iMGlevel]->SetRotationalVelocity(config, true);
+        geometry[iMGlevel]->SetRotationalVelocity(config, iMGlevel == 0);
         geometry[iMGlevel]->SetShroudVelocity(config);
       }
 

From 2f070485cb8f586b4a498ecb39fcef436da32888 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 20 May 2023 18:05:58 -0700
Subject: [PATCH 468/656] fix the cylindrical FFD to work with the FFD
 containment check

---
 .../cylindrical_ffd/def_cylindrical.cfg       | 57 ++++++++++++-------
 1 file changed, 37 insertions(+), 20 deletions(-)

diff --git a/TestCases/deformation/cylindrical_ffd/def_cylindrical.cfg b/TestCases/deformation/cylindrical_ffd/def_cylindrical.cfg
index 26f700d59e4..a22c4745843 100644
--- a/TestCases/deformation/cylindrical_ffd/def_cylindrical.cfg
+++ b/TestCases/deformation/cylindrical_ffd/def_cylindrical.cfg
@@ -9,9 +9,43 @@
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
+% -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
+%
+FFD_TOLERANCE= 1E-10
+FFD_ITERATIONS= 1000
+% The definition of the box is in cartesian coordinates, the first face
+% (first 4 points) is extruded along the x axis to connect it with the
+% second face. The x-y plane marks theta = 0 and x-z marks theta = pi/2.
+% Angles above pi/2 (negative y coord) are subtracted 2*pi which allows
+% creating a ~360 degree box as shown here.
+FFD_DEFINITION= (CYLINDER_BOX,\
+  0.6, -0.1, 1.5,\
+  0.6, -0.1, 0.5,\
+  0.6, 0.1, 0.5,\
+  0.6, 0.1, 1.5,\
+ -0.6, -0.1, 1.5,\
+ -0.6, -0.1, 0.5,\
+ -0.6, 0.1, 0.5,\
+ -0.6, 0.1, 1.5)
+% Abovew We start by changing Z, which changes the radius and thus the cylindrical
+% "i" is the radius, then we change Y, which changes the angle and thus "j" is for
+% theta. Finally we change X and thus "k" is for the axial coordinate.
+FFD_DEGREE= (1, 9, 4)
+FFD_CONTINUITY= 1ST_DERIVATIVE
+FFD_COORD_SYSTEM= CYLINDRICAL
+% This is the origin of axis, the direction is always x.
+FFD_AXIS= (0.0, 0.0, 0.0)
+
+% ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
+%
+DV_KIND= FFD_CONTROL_POINT
+DV_MARKER= ( CYLINDER )
+DV_PARAM= ( CYLINDER_BOX, 0, 3, 2, 1.0, 0.0, 0.0 )
+DV_VALUE= 1.0
+
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-SOLVER= EULER 
+SOLVER= EULER
 MATH_PROBLEM= DIRECT
 RESTART_SOL= NO
 SYSTEM_MEASUREMENTS= US
@@ -22,7 +56,7 @@ MACH_NUMBER= 0.8
 AOA= 0.0
 SIDESLIP_ANGLE= 0.0
 FREESTREAM_TEMPERATURE= 518.67
-FREESTREAM_PRESSURE= 2116.216 
+FREESTREAM_PRESSURE= 2116.216
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
@@ -46,7 +80,7 @@ MARKER_DESIGNING = ( CYLINDER )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-NUM_METHOD_GRAD= GREEN_GAUSS 
+NUM_METHOD_GRAD= GREEN_GAUSS
 CFL_NUMBER= 1.0
 CFL_ADAPT= NO
 CFL_ADAPT_PARAM= ( 1.0, 1.0, 1.0, 10.0 )
@@ -72,13 +106,6 @@ MUSCL_FLOW= YES
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
-% ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
-%
-DV_KIND= FFD_CONTROL_POINT 
-DV_MARKER= ( CYLINDER )
-DV_PARAM= ( CYLINDER_BOX, 0, 3, 2, 1.0, 0.0, 0.0 )
-DV_VALUE= 1.0 
-
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
 DEFORM_LINEAR_SOLVER= FGMRES
@@ -88,16 +115,6 @@ DEFORM_CONSOLE_OUTPUT= YES
 DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 DEFORM_LINEAR_SOLVER_ERROR= 1E-14
 
-% -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
-%
-FFD_TOLERANCE= 1E-10
-FFD_ITERATIONS= 1000
-FFD_DEFINITION= (CYLINDER_BOX, -0.6, -0.1, 1.5, -0.6, -0.1, 0.5, -0.6, 0.1, 0.5, -0.6, 0.1, 1.5, 0.6, -0.1, 1.5, 0.6, -0.1, 0.5, 0.6, 0.1, 0.5, 0.6, 0.1, 1.5)
-FFD_DEGREE= (1, 9, 4)
-FFD_CONTINUITY= 1ST_DERIVATIVE
-FFD_COORD_SYSTEM= CYLINDRICAL
-FFD_AXIS= (0.0, 0.0, 0.0)
-
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
 ITER= 5

From 47333554927536527a6439c24f46cf9fc44f50e7 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 20 May 2023 19:37:30 -0700
Subject: [PATCH 469/656] simpler fix

---
 SU2_CFD/src/output/COutput.cpp | 380 ++++++---------------------------
 1 file changed, 68 insertions(+), 312 deletions(-)

diff --git a/SU2_CFD/src/output/COutput.cpp b/SU2_CFD/src/output/COutput.cpp
index b79b42985e4..2a8dce49058 100644
--- a/SU2_CFD/src/output/COutput.cpp
+++ b/SU2_CFD/src/output/COutput.cpp
@@ -336,15 +336,26 @@ void COutput::LoadData(CGeometry *geometry, CConfig *config, CSolver** solver_co
 
 void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE format, string fileName){
 
+  /*--- File writer that will later be used to write the file to disk. Created below in the "switch" ---*/
   CFileWriter *fileWriter = nullptr;
-  bool doWriteIterFile = false;
 
-  /*--- if it is still present, strip the extension (suffix) from the filename ---*/
-  unsigned short lastindex = fileName.find_last_of('.');
+  /*--- If it is still present, strip the extension (suffix) from the filename ---*/
+  const auto lastindex = fileName.find_last_of('.');
   fileName = fileName.substr(0, lastindex);
 
+  /*--- If the filename with appended iteration is set (depending on the WRT_*_OVERWRITE options)
+   *    two files are writen, the normal one and a copy to avoid overwriting previous outputs. ---*/
   string filename_iter, extension;
 
+  /*--- Write output information to screen ---*/
+
+  auto LogOutputFiles = [&](const std::string& message) {
+    if (rank == MASTER_NODE) {
+      (*fileWritingTable) << message << fileName + extension;
+      if (!filename_iter.empty()) (*fileWritingTable) << message + " + iter" << filename_iter + extension;
+    }
+  };
+
   /*--- Write files depending on the format --- */
 
   switch (format) {
@@ -357,27 +368,14 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
         fileName = config->GetFilename(surfaceFilename, "", curTimeIter);
 
       if (!config->GetWrt_Surface_Overwrite())
-        filename_iter = config->GetFilename_Iter(fileName,curInnerIter, curOuterIter);
+        filename_iter = config->GetFilename_Iter(fileName, curInnerIter, curOuterIter);
 
       surfaceDataSorter->SortConnectivity(config, geometry);
       surfaceDataSorter->SortOutputData();
 
-      /*--- Write output information to screen ---*/
-      if (rank == MASTER_NODE) {
-        (*fileWritingTable) << "CSV file" << fileName + extension;
-
-        if (!config->GetWrt_Surface_Overwrite())
-          (*fileWritingTable) << "CSV file + iter" << filename_iter + extension;
-      }
-
-      /*--- Create file writer that will later be used to write the file to disk ---*/
+      LogOutputFiles("CSV file");
       fileWriter = new CSU2FileWriter(surfaceDataSorter);
 
-      /*--- If file overwrite is turned off, switch on additional file output
-       *    with the value of 'filename_iter' as file name ---*/
-      if (!config->GetWrt_Surface_Overwrite())
-        doWriteIterFile = true;
-
       break;
 
     case OUTPUT_TYPE::RESTART_ASCII: case OUTPUT_TYPE::CSV:
@@ -388,24 +386,11 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
         fileName = config->GetFilename(restartFilename, "", curTimeIter);
 
       if (!config->GetWrt_Restart_Overwrite())
-        filename_iter = config->GetFilename_Iter(fileName,curInnerIter, curOuterIter);
-
-      /*--- Write output information to screen ---*/
-      if (rank == MASTER_NODE) {
-        (*fileWritingTable) << "SU2 ASCII restart" << fileName + extension;
-
-        if (!config->GetWrt_Restart_Overwrite())
-          (*fileWritingTable) << "SU2 ASCII restart + iter" << filename_iter + extension;
-      }
+        filename_iter = config->GetFilename_Iter(fileName, curInnerIter, curOuterIter);
 
-      /*--- Create file writer that will later be used to write the file to disk ---*/
+      LogOutputFiles("SU2 ASCII restart");
       fileWriter = new CSU2FileWriter(volumeDataSorter);
 
-      /*--- If file overwrite is turned off, switch on additional file output
-       *    with the value of 'filename_iter' as file name ---*/
-      if (!config->GetWrt_Restart_Overwrite())
-        doWriteIterFile = true;
-
       break;
 
     case OUTPUT_TYPE::RESTART_BINARY:
@@ -416,25 +401,11 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
         fileName = config->GetFilename(restartFilename, "", curTimeIter);
 
       if (!config->GetWrt_Restart_Overwrite())
-        filename_iter = config->GetFilename_Iter(fileName,curInnerIter, curOuterIter);
-
-      /*--- Write output information to screen ---*/
-      if (rank == MASTER_NODE) {
-        (*fileWritingTable) << "SU2 binary restart" << fileName + extension;
+        filename_iter = config->GetFilename_Iter(fileName, curInnerIter, curOuterIter);
 
-        if (!config->GetWrt_Restart_Overwrite())
-          (*fileWritingTable) << "SU2 binary restart + iter" << filename_iter + extension;
-
-      }
-
-      /*--- Create file writer that will later be used to write the file to disk ---*/
+      LogOutputFiles("SU2 binary restart");
       fileWriter = new CSU2BinaryFileWriter(volumeDataSorter);
 
-      /*--- If file overwrite is turned off, switch on additional file output
-       *    with the value of 'filename_iter' as file name ---*/
-      if (!config->GetWrt_Restart_Overwrite())
-        doWriteIterFile = true;
-
       break;
 
     case OUTPUT_TYPE::MESH:
@@ -445,28 +416,14 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
         fileName = volumeFilename;
 
       if (!config->GetWrt_Volume_Overwrite())
-        filename_iter = config->GetFilename_Iter(fileName,curInnerIter, curOuterIter);
+        filename_iter = config->GetFilename_Iter(fileName, curInnerIter, curOuterIter);
 
       /*--- Load and sort the output data and connectivity. ---*/
 
       volumeDataSorter->SortConnectivity(config, geometry, true);
 
-      /*--- Write output information to screen ---*/
-      if (rank == MASTER_NODE) {
-        (*fileWritingTable) << "SU2 mesh" << fileName + extension;
-
-        if (!config->GetWrt_Volume_Overwrite())
-          (*fileWritingTable) << "SU2 mesh + iter" << filename_iter + extension;
-      }
-
-      /*--- Create file writer that will later be used to write the file to disk ---*/
-      fileWriter = new CSU2MeshFileWriter(volumeDataSorter,
-                                          config->GetiZone(), config->GetnZone());
-
-      /*--- If file overwrite is turned off, switch on additional file output
-       *    with the value of 'filename_iter' as file name ---*/
-      if (!config->GetWrt_Volume_Overwrite())
-        doWriteIterFile = true;
+      LogOutputFiles("SU2 mesh");
+      fileWriter = new CSU2MeshFileWriter(volumeDataSorter, config->GetiZone(), config->GetnZone());
 
       break;
 
@@ -478,28 +435,14 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
         fileName = config->GetFilename(volumeFilename, "", curTimeIter);
 
       if (!config->GetWrt_Volume_Overwrite())
-        filename_iter = config->GetFilename_Iter(fileName,curInnerIter, curOuterIter);
+        filename_iter = config->GetFilename_Iter(fileName, curInnerIter, curOuterIter);
 
       /*--- Load and sort the output data and connectivity. ---*/
 
       volumeDataSorter->SortConnectivity(config, geometry, false);
 
-      /*--- Write output information to screen ---*/
-      if (rank == MASTER_NODE) {
-        (*fileWritingTable) << "Tecplot binary" << fileName + extension;
-
-        if (!config->GetWrt_Volume_Overwrite())
-          (*fileWritingTable) << "Tecplot binary + iter" << filename_iter + extension;
-      }
-
-      /*--- Create file writer that will later be used to write the file to disk ---*/
-      fileWriter = new CTecplotBinaryFileWriter(volumeDataSorter,
-                                                curTimeIter, GetHistoryFieldValue("TIME_STEP"));
-
-      /*--- If file overwrite is turned off, switch on additional file output
-       *    with the value of 'filename_iter' as file name ---*/
-      if (!config->GetWrt_Volume_Overwrite())
-        doWriteIterFile = true;
+      LogOutputFiles("Tecplot binary");
+      fileWriter = new CTecplotBinaryFileWriter(volumeDataSorter, curTimeIter, GetHistoryFieldValue("TIME_STEP"));
 
       break;
 
@@ -511,28 +454,14 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
         fileName = config->GetFilename(volumeFilename, "", curTimeIter);
 
       if (!config->GetWrt_Volume_Overwrite())
-        filename_iter = config->GetFilename_Iter(fileName,curInnerIter, curOuterIter);
+        filename_iter = config->GetFilename_Iter(fileName, curInnerIter, curOuterIter);
 
       /*--- Load and sort the output data and connectivity. ---*/
 
       volumeDataSorter->SortConnectivity(config, geometry, true);
 
-      /*--- Write output information to screen ---*/
-      if (rank == MASTER_NODE) {
-        (*fileWritingTable) << "Tecplot ASCII" << fileName + extension;
-
-        if (!config->GetWrt_Volume_Overwrite())
-          (*fileWritingTable) << "Tecplot ASCII + iter" << filename_iter + extension;
-      }
-
-      /*--- Create file writer that will later be used to write the file to disk ---*/
-      fileWriter = new CTecplotFileWriter(volumeDataSorter,
-                                          curTimeIter, GetHistoryFieldValue("TIME_STEP"));
-
-      /*--- If file overwrite is turned off, switch on additional file output
-       *    with the value of 'filename_iter' as file name ---*/
-      if (!config->GetWrt_Volume_Overwrite())
-        doWriteIterFile = true;
+      LogOutputFiles("Tecplot ASCII");
+      fileWriter = new CTecplotFileWriter(volumeDataSorter, curTimeIter, GetHistoryFieldValue("TIME_STEP"));
 
       break;
 
@@ -544,28 +473,15 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
         fileName = config->GetFilename(volumeFilename, "", curTimeIter);
 
       if (!config->GetWrt_Volume_Overwrite())
-        filename_iter = config->GetFilename_Iter(fileName,curInnerIter, curOuterIter);
+        filename_iter = config->GetFilename_Iter(fileName, curInnerIter, curOuterIter);
 
       /*--- Load and sort the output data and connectivity. ---*/
 
       volumeDataSorter->SortConnectivity(config, geometry, true);
 
-      /*--- Write output information to screen ---*/
-      if (rank == MASTER_NODE) {
-        (*fileWritingTable) << "Paraview" << fileName + extension;
-
-        if (!config->GetWrt_Volume_Overwrite())
-          (*fileWritingTable) << "Paraview + iter" << filename_iter + extension;
-      }
-
-      /*--- Create file writer that will later be used to write the file to disk ---*/
+      LogOutputFiles("Paraview");
       fileWriter = new CParaviewXMLFileWriter(volumeDataSorter);
 
-      /*--- If file overwrite is turned off, switch on additional file output
-       *    with the value of 'filename_iter' as file name ---*/
-      if (!config->GetWrt_Volume_Overwrite())
-        doWriteIterFile = true;
-
       break;
 
     case OUTPUT_TYPE::PARAVIEW_LEGACY_BINARY:
@@ -576,69 +492,44 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
         fileName = config->GetFilename(volumeFilename, "", curTimeIter);
 
       if (!config->GetWrt_Volume_Overwrite())
-        filename_iter = config->GetFilename_Iter(fileName,curInnerIter, curOuterIter);
+        filename_iter = config->GetFilename_Iter(fileName, curInnerIter, curOuterIter);
 
       /*--- Load and sort the output data and connectivity. ---*/
 
       volumeDataSorter->SortConnectivity(config, geometry, true);
 
-      /*--- Write output information to screen ---*/
-      if (rank == MASTER_NODE) {
-        (*fileWritingTable) << "Paraview binary (legacy)" << fileName + extension;
-
-        if (!config->GetWrt_Volume_Overwrite())
-          (*fileWritingTable) << "Paraview binary + iter" << filename_iter + extension;
-      }
-
-      /*--- Create file writer that will later be used to write the file to disk ---*/
+      LogOutputFiles("Paraview binary (legacy)");
       fileWriter = new CParaviewBinaryFileWriter(volumeDataSorter);
 
-      /*--- If file overwrite is turned off, switch on additional file output
-       *    with the value of 'filename_iter' as file name ---*/
-      if (!config->GetWrt_Volume_Overwrite())
-        doWriteIterFile = true;
-
       break;
 
     case OUTPUT_TYPE::PARAVIEW_MULTIBLOCK:
       {
-
         extension = CParaviewVTMFileWriter::fileExt;
 
         if (fileName.empty())
           fileName = config->GetUnsteady_FileName(volumeFilename, curTimeIter, "");
 
         if (!config->GetWrt_Volume_Overwrite())
-          filename_iter = config->GetFilename_Iter(fileName,curInnerIter, curOuterIter);
+          filename_iter = config->GetFilename_Iter(fileName, curInnerIter, curOuterIter);
 
         /*--- Sort volume connectivity ---*/
 
         volumeDataSorter->SortConnectivity(config, geometry, true);
 
-        /*--- Write output information to screen ---*/
-        if (rank == MASTER_NODE) {
-          (*fileWritingTable) << "Paraview Multiblock" << fileName + extension;
-
-          if (!config->GetWrt_Volume_Overwrite())
-            (*fileWritingTable) << "Paraview Multiblock + iter" << filename_iter + extension;
-        }
-
-        /*--- Allocate the vtm file writer (using fileName as the folder name) ---*/
-        fileWriter = new CParaviewVTMFileWriter(GetHistoryFieldValue("CUR_TIME"),
-                                                config->GetiZone(), config->GetnZone());
+        LogOutputFiles("Paraview Multiblock");
+        fileWriter = new CParaviewVTMFileWriter(GetHistoryFieldValue("CUR_TIME"), config->GetiZone(), config->GetnZone());
 
         /*--- We cast the pointer to its true type, to avoid virtual functions ---*/
         auto* vtmWriter = dynamic_cast<CParaviewVTMFileWriter*>(fileWriter);
 
         /*--- then we write the data into the folder---*/
-        vtmWriter->WriteFolderData(fileName, config, multiZoneHeaderString, volumeDataSorter,surfaceDataSorter, geometry);
+        vtmWriter->WriteFolderData(fileName, config, multiZoneHeaderString, volumeDataSorter, surfaceDataSorter, geometry);
 
         /*--- and we write the data into the folder with the iteration number ---*/
         if (!config->GetWrt_Volume_Overwrite())
-          vtmWriter->WriteFolderData(filename_iter, config, multiZoneHeaderString, volumeDataSorter,surfaceDataSorter, geometry);
-
+          vtmWriter->WriteFolderData(filename_iter, config, multiZoneHeaderString, volumeDataSorter, surfaceDataSorter, geometry);
       }
-
       break;
 
     case OUTPUT_TYPE::PARAVIEW_ASCII:
@@ -649,29 +540,15 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
         fileName = config->GetFilename(volumeFilename, "", curTimeIter);
 
       if (!config->GetWrt_Volume_Overwrite())
-        filename_iter = config->GetFilename_Iter(fileName,curInnerIter, curOuterIter);
-
+        filename_iter = config->GetFilename_Iter(fileName, curInnerIter, curOuterIter);
 
       /*--- Load and sort the output data and connectivity. ---*/
 
       volumeDataSorter->SortConnectivity(config, geometry, true);
 
-      /*--- Write output information to screen ---*/
-      if (rank == MASTER_NODE) {
-        (*fileWritingTable) << "Paraview ASCII" << fileName + extension;
-
-        if (!config->GetWrt_Volume_Overwrite())
-          (*fileWritingTable) << "Paraview ASCII + iter" << filename_iter + extension;
-      }
-
-      /*--- Create file writer that will later be used to write the file to disk ---*/
+      LogOutputFiles("Paraview ASCII");
       fileWriter = new CParaviewFileWriter(volumeDataSorter);
 
-      /*--- If file overwrite is turned off, switch on additional file output
-       *    with the value of 'filename_iter' as file name ---*/
-      if (!config->GetWrt_Volume_Overwrite())
-        doWriteIterFile = true;
-
       break;
 
     case OUTPUT_TYPE::SURFACE_PARAVIEW_ASCII:
@@ -682,64 +559,36 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
         fileName = config->GetFilename(surfaceFilename, "", curTimeIter);
 
       if (!config->GetWrt_Surface_Overwrite())
-        filename_iter = config->GetFilename_Iter(fileName,curInnerIter, curOuterIter);
-
+        filename_iter = config->GetFilename_Iter(fileName, curInnerIter, curOuterIter);
 
       /*--- Load and sort the output data and connectivity. ---*/
 
       surfaceDataSorter->SortConnectivity(config, geometry);
       surfaceDataSorter->SortOutputData();
 
-      /*--- Write output information to screen ---*/
-      if (rank == MASTER_NODE) {
-        (*fileWritingTable) << "Paraview ASCII surface" << fileName + extension;
-
-        if (!config->GetWrt_Surface_Overwrite())
-          (*fileWritingTable) << "Paraview ASCII + iter" << filename_iter + extension;
-      }
-
-      /*--- Create file writer that will later be used to write the file to disk ---*/
+      LogOutputFiles("Paraview ASCII surface");
       fileWriter = new CParaviewFileWriter(surfaceDataSorter);
 
-      /*--- If file overwrite is turned off, switch on additional file output
-       *    with the value of 'filename_iter' as file name ---*/
-      if (!config->GetWrt_Surface_Overwrite())
-        doWriteIterFile = true;
-
       break;
 
     case OUTPUT_TYPE::SURFACE_PARAVIEW_LEGACY_BINARY:
 
-        extension = CParaviewBinaryFileWriter::fileExt;
+      extension = CParaviewBinaryFileWriter::fileExt;
 
       if (fileName.empty())
         fileName = config->GetFilename(surfaceFilename, "", curTimeIter);
 
       if (!config->GetWrt_Surface_Overwrite())
-        filename_iter = config->GetFilename_Iter(fileName,curInnerIter, curOuterIter);
-
+        filename_iter = config->GetFilename_Iter(fileName, curInnerIter, curOuterIter);
 
       /*--- Load and sort the output data and connectivity. ---*/
 
       surfaceDataSorter->SortConnectivity(config, geometry);
       surfaceDataSorter->SortOutputData();
 
-      /*--- Write output information to screen ---*/
-      if (rank == MASTER_NODE) {
-        (*fileWritingTable) << "Paraview binary surface (legacy)" << fileName + extension;
-
-        if (!config->GetWrt_Surface_Overwrite())
-          (*fileWritingTable) << "Paraview binary surface + iter" << filename_iter + extension;
-      }
-
-      /*--- Create file writer that will later be used to write the file to disk ---*/
+      LogOutputFiles("Paraview binary surface (legacy)");
       fileWriter = new CParaviewBinaryFileWriter(surfaceDataSorter);
 
-      /*--- If file overwrite is turned off, switch on additional file output
-       *    with the value of 'filename_iter' as file name ---*/
-      if (!config->GetWrt_Surface_Overwrite())
-        doWriteIterFile = true;
-
       break;
 
     case OUTPUT_TYPE::SURFACE_PARAVIEW_XML:
@@ -750,65 +599,35 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
         fileName = config->GetFilename(surfaceFilename, "", curTimeIter);
 
       if (!config->GetWrt_Surface_Overwrite())
-        filename_iter = config->GetFilename_Iter(fileName,curInnerIter, curOuterIter);
-
+        filename_iter = config->GetFilename_Iter(fileName, curInnerIter, curOuterIter);
 
       /*--- Load and sort the output data and connectivity. ---*/
 
       surfaceDataSorter->SortConnectivity(config, geometry);
       surfaceDataSorter->SortOutputData();
 
-      /*--- Write output information to screen ---*/
-      if (rank == MASTER_NODE) {
-        (*fileWritingTable) << "Paraview surface" << fileName + extension;
-
-        if (!config->GetWrt_Surface_Overwrite())
-          (*fileWritingTable) << "Paraview surface + iter" << filename_iter + extension;
-      }
-
-      /*--- Create file writer that will later be used to write the file to disk ---*/
+      LogOutputFiles("Paraview surface");
       fileWriter = new CParaviewXMLFileWriter(surfaceDataSorter);
 
-      /*--- If file overwrite is turned off, switch on additional file output
-       *    with the value of 'filename_iter' as file name ---*/
-      if (!config->GetWrt_Surface_Overwrite())
-        doWriteIterFile = true;
-
       break;
 
     case OUTPUT_TYPE::SURFACE_TECPLOT_ASCII:
 
-        extension = CTecplotFileWriter::fileExt;
+      extension = CTecplotFileWriter::fileExt;
 
       if (fileName.empty())
         fileName = config->GetFilename(surfaceFilename, "", curTimeIter);
 
       if (!config->GetWrt_Surface_Overwrite())
-        filename_iter = config->GetFilename_Iter(fileName,curInnerIter, curOuterIter);
-
+        filename_iter = config->GetFilename_Iter(fileName, curInnerIter, curOuterIter);
 
       /*--- Load and sort the output data and connectivity. ---*/
 
       surfaceDataSorter->SortConnectivity(config, geometry);
       surfaceDataSorter->SortOutputData();
 
-      /*--- Write output information to screen ---*/
-      if (rank == MASTER_NODE) {
-        (*fileWritingTable) << "Tecplot ASCII surface" << fileName + extension;
-
-        if (!config->GetWrt_Surface_Overwrite())
-          (*fileWritingTable) << "Tecplot ASCII surface + iter" << filename_iter + extension;
-
-      }
-
-      /*--- Create file writer that will later be used to write the file to disk ---*/
-      fileWriter = new CTecplotFileWriter(surfaceDataSorter,
-                                          curTimeIter, GetHistoryFieldValue("TIME_STEP"));
-
-      /*--- If file overwrite is turned off, switch on additional file output
-       *    with the value of 'filename_iter' as file name ---*/
-      if (!config->GetWrt_Surface_Overwrite())
-        doWriteIterFile = true;
+      LogOutputFiles("Tecplot ASCII surface");
+      fileWriter = new CTecplotFileWriter(surfaceDataSorter, curTimeIter, GetHistoryFieldValue("TIME_STEP"));
 
       break;
 
@@ -820,31 +639,15 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
         fileName = config->GetFilename(surfaceFilename, "", curTimeIter);
 
       if (!config->GetWrt_Surface_Overwrite())
-        filename_iter = config->GetFilename_Iter(fileName,curInnerIter, curOuterIter);
-
+        filename_iter = config->GetFilename_Iter(fileName, curInnerIter, curOuterIter);
 
       /*--- Load and sort the output data and connectivity. ---*/
 
       surfaceDataSorter->SortConnectivity(config, geometry);
       surfaceDataSorter->SortOutputData();
 
-      /*--- Write output information to screen ---*/
-      if (rank == MASTER_NODE) {
-        (*fileWritingTable) << "Tecplot binary surface" << fileName + extension;
-
-        if (!config->GetWrt_Surface_Overwrite())
-          (*fileWritingTable) << "Tecplot binary surface + iter" << filename_iter + extension;
-
-      }
-
-      /*--- Create file writer that will later be used to write the file to disk ---*/
-      fileWriter = new CTecplotBinaryFileWriter(surfaceDataSorter,
-                                                curTimeIter, GetHistoryFieldValue("TIME_STEP"));
-
-      /*--- If file overwrite is turned off, switch on additional file output
-       *    with the value of 'filename_iter' as file name ---*/
-      if (!config->GetWrt_Surface_Overwrite())
-        doWriteIterFile = true;
+      LogOutputFiles("Tecplot binary surface");
+      fileWriter = new CTecplotBinaryFileWriter(surfaceDataSorter, curTimeIter, GetHistoryFieldValue("TIME_STEP"));
 
       break;
 
@@ -856,30 +659,15 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
         fileName = config->GetFilename(surfaceFilename, "", curTimeIter);
 
       if (!config->GetWrt_Surface_Overwrite())
-        filename_iter = config->GetFilename_Iter(fileName,curInnerIter, curOuterIter);
-
+        filename_iter = config->GetFilename_Iter(fileName, curInnerIter, curOuterIter);
 
       /*--- Load and sort the output data and connectivity. ---*/
       surfaceDataSorter->SortConnectivity(config, geometry);
       surfaceDataSorter->SortOutputData();
 
-      /*--- Write output information to screen ---*/
-      if (rank == MASTER_NODE) {
-        (*fileWritingTable) << "STL ASCII" << fileName + extension;
-
-        if (!config->GetWrt_Surface_Overwrite())
-          (*fileWritingTable) << "STL ASCII + iter" << filename_iter + extension;
-
-      }
-
-      /*--- Create file writer that will later be used to write the file to disk ---*/
+      LogOutputFiles("STL ASCII");
       fileWriter = new CSTLFileWriter(surfaceDataSorter);
 
-      /*--- If file overwrite is turned off, switch on additional file output
-       *    with the value of 'filename_iter' as file name ---*/
-      if (!config->GetWrt_Surface_Overwrite())
-        doWriteIterFile = true;
-
       break;
 
     case OUTPUT_TYPE::CGNS:
@@ -890,29 +678,14 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
         fileName = config->GetFilename(volumeFilename, "", curTimeIter);
 
       if (!config->GetWrt_Volume_Overwrite())
-        filename_iter = config->GetFilename_Iter(fileName,curInnerIter, curOuterIter);
-
+        filename_iter = config->GetFilename_Iter(fileName, curInnerIter, curOuterIter);
 
       /*--- Load and sort the output data and connectivity. ---*/
       volumeDataSorter->SortConnectivity(config, geometry, true);
 
-      /*--- Write output information to screen ---*/
-      if (rank == MASTER_NODE) {
-        (*fileWritingTable) << "CGNS" << fileName + extension;
-
-        if (!config->GetWrt_Volume_Overwrite())
-          (*fileWritingTable) << "CGNS + iter" << filename_iter + extension;
-
-      }
-
-      /*--- Create file writer that will later be used to write the file to disk ---*/
+      LogOutputFiles("CGNS");
       fileWriter = new CCGNSFileWriter(volumeDataSorter);
 
-      /*--- If file overwrite is turned off, switch on additional file output
-       *    with the value of 'filename_iter' as file name ---*/
-      if (!config->GetWrt_Volume_Overwrite())
-        doWriteIterFile = true;
-
       break;
 
     case OUTPUT_TYPE::SURFACE_CGNS:
@@ -923,37 +696,22 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
         fileName = config->GetFilename(surfaceFilename, "", curTimeIter);
 
       if (!config->GetWrt_Surface_Overwrite())
-        filename_iter = config->GetFilename_Iter(fileName,curInnerIter, curOuterIter);
-
+        filename_iter = config->GetFilename_Iter(fileName, curInnerIter, curOuterIter);
 
       /*--- Load and sort the output data and connectivity. ---*/
       surfaceDataSorter->SortConnectivity(config, geometry);
       surfaceDataSorter->SortOutputData();
 
-      /*--- Write output information to screen ---*/
-      if (rank == MASTER_NODE) {
-        (*fileWritingTable) << "CGNS surface" << fileName + extension;
-
-        if (!config->GetWrt_Surface_Overwrite())
-          (*fileWritingTable) << "CGNS surface + iter" << filename_iter + extension;
-
-      }
-
-      /*--- Create file writer that will later be used to write the file to disk ---*/
+      LogOutputFiles("CGNS surface");
       fileWriter = new CCGNSFileWriter(surfaceDataSorter, true);
 
-      /*--- If file overwrite is turned off, switch on additional file output
-       *    with the value of 'filename_iter' as file name ---*/
-      if (!config->GetWrt_Surface_Overwrite())
-        doWriteIterFile = true;
-
       break;
 
     default:
       break;
   }
 
-  if (fileWriter != nullptr){
+  if (fileWriter != nullptr) {
 
     /*--- Write data to file ---*/
 
@@ -961,21 +719,19 @@ void COutput::WriteToFile(CConfig *config, CGeometry *geometry, OUTPUT_TYPE form
 
     su2double BandWidth = fileWriter->GetBandwidth();
 
-    /*--- Write data with iteration number to file ---*/
+    /*--- Write data with iteration number to file if required ---*/
 
-    if (!filename_iter.empty() && doWriteIterFile){
+    if (!filename_iter.empty()) {
       fileWriter->WriteData(filename_iter);
 
-      /*--- overwrite bandwidth ---*/
-      BandWidth = fileWriter->GetBandwidth();
-
+      /*--- Average bandwidth ---*/
+      BandWidth = (BandWidth + fileWriter->GetBandwidth()) / 2;
     }
 
+    /*--- Compute and store the bandwidth ---*/
 
-  /*--- Compute and store the bandwidth ---*/
-
-    if (format == OUTPUT_TYPE::RESTART_BINARY){
-      config->SetRestart_Bandwidth_Agg(config->GetRestart_Bandwidth_Agg()+BandWidth);
+    if (format == OUTPUT_TYPE::RESTART_BINARY) {
+      config->SetRestart_Bandwidth_Agg(config->GetRestart_Bandwidth_Agg() + BandWidth);
     }
 
     if (config->GetWrt_Performance() && (rank == MASTER_NODE)){

From cb9701e07ec5e682222fa748e196616c17496dc3 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Mon, 22 May 2023 10:38:18 +0200
Subject: [PATCH 470/656] Removed Tecplot outputs from testcase.

---
 TestCases/gust/cosine_gust_zdir.cfg | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/gust/cosine_gust_zdir.cfg b/TestCases/gust/cosine_gust_zdir.cfg
index 0c523862f40..be0e38a8fd0 100644
--- a/TestCases/gust/cosine_gust_zdir.cfg
+++ b/TestCases/gust/cosine_gust_zdir.cfg
@@ -168,5 +168,5 @@ TABULAR_FORMAT= CSV
 % Possible formats : (TECPLOT, TECPLOT_BINARY, SURFACE_TECPLOT,
 %  SURFACE_TECPLOT_BINARY, CSV, SURFACE_CSV, PARAVIEW, PARAVIEW_BINARY, SURFACE_PARAVIEW,
 %  SURFACE_PARAVIEW_BINARY, MESH, RESTART_BINARY, RESTART_ASCII, CGNS, SURFACE_CGNS, STL)
-OUTPUT_FILES= (RESTART, RESTART_ASCII, TECPLOT, SURFACE_TECPLOT)
+OUTPUT_FILES= (RESTART, RESTART_ASCII)
 

From dc7fb834856f7e7a9d10d3366290b9fdca2ea44e Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Mon, 22 May 2023 14:51:22 +0200
Subject: [PATCH 471/656] Adding testcase for gust in combination with mesh
 deformation by using the SU2-internal option SURFACE_MOVEMENT= DEFORMING

---
 TestCases/gust/gust_with_mesh_deformation.cfg | 182 ++++++++++++++++++
 TestCases/hybrid_regression.py                |   9 +
 2 files changed, 191 insertions(+)
 create mode 100644 TestCases/gust/gust_with_mesh_deformation.cfg

diff --git a/TestCases/gust/gust_with_mesh_deformation.cfg b/TestCases/gust/gust_with_mesh_deformation.cfg
new file mode 100644
index 00000000000..460340af08e
--- /dev/null
+++ b/TestCases/gust/gust_with_mesh_deformation.cfg
@@ -0,0 +1,182 @@
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
+% Solver type (EULER, NAVIER_STOKES, RANS,
+%              INC_EULER, INC_NAVIER_STOKES, INC_RANS,
+%              NEMO_EULER, NEMO_NAVIER_STOKES,
+%              FEM_EULER, FEM_NAVIER_STOKES, FEM_RANS, FEM_LES,
+%              HEAT_EQUATION_FVM, ELASTICITY)
+SOLVER= EULER
+%
+% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
+MATH_PROBLEM= DIRECT
+%
+% ------------------------------- SOLVER CONTROL ------------------------------%
+%
+% Maximum number of inner iterations
+INNER_ITER= 100
+%
+% Min value of the residual (log10 of the residual)
+CONV_RESIDUAL_MINVAL= -6
+%
+% Start convergence criteria at iteration number
+CONV_STARTITER= 0
+%
+% ------------------------- UNSTEADY SIMULATION -------------------------------%
+%
+TIME_DOMAIN=YES
+TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
+TIME_STEP= 0.001
+TIME_ITER= 26
+%
+% --------------------------- GUST SIMULATION ---------------------------------%
+%
+% The gust simulation requires the GRID_MOVEMENT flag to be set to YES.
+% and the GRID_MOVEMENT_KIND to be set to GUST or any of the other options.
+% Apply a wind gust (NO, YES)
+GRID_MOVEMENT=GUST
+WIND_GUST= YES
+GUST_TYPE= ONE_M_COSINE
+GUST_DIR= Y_DIR
+GUST_WAVELENGTH= 10.0
+GUST_PERIODS= 1.0
+% Gust amplitude corresponds to ~2.0 deg AoA
+GUST_AMPL= 1.0
+%
+GUST_BEGIN_TIME= 0.0
+GUST_BEGIN_LOC=-10.0
+% --------------------------- MESH DEFORMATION--------------------------------%
+% Type of dynamic surface movement (NONE, DEFORMING, MOVING_WALL,
+% AEROELASTIC, AEROELASTIC_RIGID_MOTION EXTERNAL, EXTERNAL_ROTATION)
+SURFACE_MOVEMENT= DEFORMING
+%
+% Moving wall boundary marker(s) (NONE = no marker, ignored for RIGID_MOTION)
+MARKER_MOVING= ( airfoil )
+%
+% Plunging angular freq. (rad/s) in x, y, & z directions
+SURFACE_PLUNGING_OMEGA= 0.0 125.6 0.0
+%
+% Plunging amplitude (m or ft) in x, y, & z directions
+SURFACE_PLUNGING_AMPL= 0.0 0.001 0.0
+%
+% Move Motion Origin for marker moving (1 or 0)
+MOVE_MOTION_ORIGIN = 0
+% -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
+%
+% Mach number (non-dimensional, based on the free-stream values)
+MACH_NUMBER= 0.2
+%
+% Angle of attack (degrees, only for compressible flows)
+AOA= 0.0
+%
+% Side-slip angle (degrees, only for compressible flows)
+SIDESLIP_ANGLE= 0.0
+%
+% Free-stream option to choose between density and temperature (default) for
+% initializing the solution (TEMPERATURE_FS, DENSITY_FS)
+FREESTREAM_OPTION= DENSITY_FS
+%
+% Free-stream pressure (101325.0 N/m^2, 2116.216 psf by default)
+FREESTREAM_PRESSURE= 101325.0
+%
+% Free-stream density (1.2886 Kg/m^3, 0.0025 slug/ft^3 by default)
+FREESTREAM_DENSITY= 1.225
+%
+% Free-stream temperature (288.15 K, 518.67 R by default)
+FREESTREAM_TEMPERATURE= 288.15
+%
+% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
+%
+% Reference origin for moment computation (m or in)
+REF_ORIGIN_MOMENT_X = 0.25
+REF_ORIGIN_MOMENT_Y = 0.00
+REF_ORIGIN_MOMENT_Z = 0.00
+%
+% Reference length for moment non-dimensional coefficients (m or in)
+REF_LENGTH= 1.0
+%
+% Reference area for non-dimensional force coefficients (0 implies automatic
+% calculation) (m^2 or in^2)
+REF_AREA= 1.0
+%
+% Aircraft semi-span (0 implies automatic calculation) (m or in)
+SEMI_SPAN= 1.0
+%
+% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
+%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
+REF_DIMENSIONALIZATION= DIMENSIONAL
+
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
+% Euler wall boundary marker(s) (NONE = no marker)
+% Implementation identical to MARKER_SYM.
+MARKER_EULER= ( airfoil )
+%
+% Far-field boundary marker(s) (NONE = no marker)
+MARKER_FAR= ( farfield )
+
+% ------------------------ SURFACES IDENTIFICATION ----------------------------%
+%
+% Marker(s) of the surface in the surface flow solution file
+MARKER_PLOTTING = ( airfoil )
+%
+% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
+MARKER_MONITORING = ( airfoil )
+
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
+% CFL number (initial value for the adaptive CFL number)
+CFL_NUMBER= 100.0
+%
+% Adaptive CFL number (NO, YES)
+CFL_ADAPT= YES
+%
+% -------------------------- MULTIGRID PARAMETERS -----------------------------%
+%
+% Multi-grid levels (0 = no multi-grid)
+MGLEVEL= 3
+%
+% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
+MGCYCLE= W_CYCLE
+
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
+% Convective numerical method (JST, JST_KE, JST_MAT, LAX-FRIEDRICH, CUSP, ROE, AUSM,
+%                              AUSMPLUSUP, AUSMPLUSUP2, AUSMPWPLUS, HLLC, TURKEL_PREC,
+%                              SW, MSW, FDS, SLAU, SLAU2, L2ROE, LMROE)
+CONV_NUM_METHOD_FLOW= JST
+%
+% Max number of iterations of the linear solver for the implicit formulation
+LINEAR_SOLVER_ITER= 20
+%
+% ------------------------- SCREEN/HISTORY VOLUME OUTPUT --------------------------%
+%
+% Screen output fields (use 'SU2_CFD -d <config_file>' to view list of available fields)
+SCREEN_OUTPUT= (TIME_ITER, INNER_ITER, RMS_DENSITY, LIFT, MOMENT_Z)
+%
+% History output groups (use 'SU2_CFD -d <config_file>' to view list of available fields)
+HISTORY_OUTPUT= (ITER, RMS_RES, AERO_COEFF, CAUCHY, WALL_TIME)
+%
+% ------------------------- INPUT/OUTPUT FILE INFORMATION --------------------------%
+%
+% Mesh input file
+MESH_FILENAME= mesh_NACA0012_inv.su2
+%
+% Mesh input file format (SU2, CGNS)
+MESH_FORMAT= SU2
+%
+% Restart flow input file
+SOLUTION_FILENAME= restart_gust.dat
+RESTART_FILENAME= restart_gust.dat
+SURFACE_FILENAME= surface_gust
+VOLUME_FILENAME= volume_gust
+CONV_FILENAME= history_gust
+%
+% Output tabular file format (TECPLOT, CSV)
+TABULAR_FORMAT= CSV
+%
+% Files to output
+% Possible formats : (TECPLOT, TECPLOT_BINARY, SURFACE_TECPLOT,
+%  SURFACE_TECPLOT_BINARY, CSV, SURFACE_CSV, PARAVIEW, PARAVIEW_BINARY, SURFACE_PARAVIEW,
+%  SURFACE_PARAVIEW_BINARY, MESH, RESTART_BINARY, RESTART_ASCII, CGNS, SURFACE_CGNS, STL)
+OUTPUT_FILES= (TECPLOT, SURFACE_TECPLOT)
+
diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index 564df0f4a1d..e0febfcfb2e 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -479,6 +479,15 @@ def main():
     cosine_gust.test_vals = [-2.418813, 0.004650, -0.001878, -0.000637, -0.000271]
     cosine_gust.unsteady  = True
     test_list.append(cosine_gust)
+    
+    # Gust with mesh deformation
+    gust_mesh_defo           = TestCase('gust_with_mesh_deformation')
+    gust_mesh_defo.cfg_dir   = "gust"
+    gust_mesh_defo.cfg_file  = "gust_with_mesh_deformation.cfg"
+    gust_mesh_defo.test_iter = 25
+    gust_mesh_defo.test_vals = [-1.585670, 0.004771, 0.000413]
+    gust_mesh_defo.unsteady  = True
+    test_list.append(gust_mesh_defo)
 
     # Aeroelastic
     aeroelastic           = TestCase('aeroelastic')

From 8897fe1a5219c42eac7a5c77e9ae4daf02d76ff2 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Mon, 22 May 2023 15:52:31 +0200
Subject: [PATCH 472/656] Remove Tecplot outputs

---
 TestCases/gust/gust_with_mesh_deformation.cfg | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/gust/gust_with_mesh_deformation.cfg b/TestCases/gust/gust_with_mesh_deformation.cfg
index 460340af08e..9cf09168951 100644
--- a/TestCases/gust/gust_with_mesh_deformation.cfg
+++ b/TestCases/gust/gust_with_mesh_deformation.cfg
@@ -178,5 +178,5 @@ TABULAR_FORMAT= CSV
 % Possible formats : (TECPLOT, TECPLOT_BINARY, SURFACE_TECPLOT,
 %  SURFACE_TECPLOT_BINARY, CSV, SURFACE_CSV, PARAVIEW, PARAVIEW_BINARY, SURFACE_PARAVIEW,
 %  SURFACE_PARAVIEW_BINARY, MESH, RESTART_BINARY, RESTART_ASCII, CGNS, SURFACE_CGNS, STL)
-OUTPUT_FILES= (TECPLOT, SURFACE_TECPLOT)
+OUTPUT_FILES= (NONE)
 

From d051de810d091fc7cf148386e80c37298563d693 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 22 May 2023 16:23:45 +0200
Subject: [PATCH 473/656] CoDiPack update.

---
 externals/codi        | 2 +-
 meson_scripts/init.py | 2 +-
 2 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/externals/codi b/externals/codi
index 13874231e23..4237fe38c90 160000
--- a/externals/codi
+++ b/externals/codi
@@ -1 +1 @@
-Subproject commit 13874231e23186f18622f116cb0cc049cb90c778
+Subproject commit 4237fe38c90b83541f699bd84e00c656099b7d18
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 18ec2ece2af..f1e298a9cbb 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -54,7 +54,7 @@ def init_submodules(
 
     # This information of the modules is used if projects was not cloned using git
     # The sha tag must be maintained manually to point to the correct commit
-    sha_version_codi = "13874231e23186f18622f116cb0cc049cb90c778"
+    sha_version_codi = "4237fe38c90b83541f699bd84e00c656099b7d18"
     github_repo_codi = "https://github.com/scicompkl/CoDiPack"
     sha_version_medi = "aafc2d1966ba1233640af737e71c77c1a86183fd"
     github_repo_medi = "https://github.com/SciCompKL/MeDiPack"

From 0ad658cf2043ca06b2094b2417f72f1d00eb3be3 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 22 May 2023 16:49:48 +0200
Subject: [PATCH 474/656] Shared reading optimization for safe global access
 macros.

---
 Common/include/basic_types/ad_structure.hpp   | 25 ++++++++++---------
 .../include/parallelization/omp_structure.hpp | 12 ++++++---
 2 files changed, 21 insertions(+), 16 deletions(-)

diff --git a/Common/include/basic_types/ad_structure.hpp b/Common/include/basic_types/ad_structure.hpp
index 7b5ee4e35ca..99a29debd6a 100644
--- a/Common/include/basic_types/ad_structure.hpp
+++ b/Common/include/basic_types/ad_structure.hpp
@@ -546,18 +546,6 @@ FORCEINLINE void EndPassive(bool wasActive) {
   if (wasActive) AD::getTape().setActive();
 }
 
-FORCEINLINE bool PausePreaccumulation() {
-  const auto current = PreaccEnabled;
-  if (!current) return false;
-  SU2_OMP_SAFE_GLOBAL_ACCESS(PreaccEnabled = false;)
-  return true;
-}
-
-FORCEINLINE void ResumePreaccumulation(bool wasActive) {
-  if (!wasActive) return;
-  SU2_OMP_SAFE_GLOBAL_ACCESS(PreaccEnabled = true;)
-}
-
 FORCEINLINE void StartNoSharedReading() {
 #ifdef HAVE_OPDI
   opdi::logic->setAdjointAccessMode(opdi::LogicInterface::AdjointAccessMode::Classical);
@@ -571,6 +559,19 @@ FORCEINLINE void EndNoSharedReading() {
   opdi::logic->addReverseBarrier();
 #endif
 }
+
+FORCEINLINE bool PausePreaccumulation() {
+  const auto current = PreaccEnabled;
+  if (!current) return false;
+  SU2_OMP_SAFE_GLOBAL_ACCESS(PreaccEnabled = false;)
+  return true;
+}
+
+FORCEINLINE void ResumePreaccumulation(bool wasActive) {
+  if (!wasActive) return;
+  SU2_OMP_SAFE_GLOBAL_ACCESS(PreaccEnabled = true;)
+}
+
 #endif  // CODI_REVERSE_TYPE
 
 void Initialize();
diff --git a/Common/include/parallelization/omp_structure.hpp b/Common/include/parallelization/omp_structure.hpp
index de19ec1e544..6f49c3012f4 100644
--- a/Common/include/parallelization/omp_structure.hpp
+++ b/Common/include/parallelization/omp_structure.hpp
@@ -188,12 +188,16 @@ void omp_finalize();
  * thread, with all threads and memory views synchronized both beforehand and afterwards.
  */
 
-#define BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS \
-  SU2_OMP_BARRIER                        \
+#define BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS  \
+  SU2_OMP_BARRIER                         \
+  if (omp_in_parallel())                  \
+    AD::StartNoSharedReading();           \
   SU2_OMP_MASTER
 
-#define END_SU2_OMP_SAFE_GLOBAL_ACCESS \
-  END_SU2_OMP_MASTER                   \
+#define END_SU2_OMP_SAFE_GLOBAL_ACCESS  \
+  END_SU2_OMP_MASTER                    \
+  if (omp_in_parallel())                \
+    AD::EndNoSharedReading();           \
   SU2_OMP_BARRIER
 
 #define SU2_OMP_SAFE_GLOBAL_ACCESS(...) BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS{__VA_ARGS__} END_SU2_OMP_SAFE_GLOBAL_ACCESS

From 8a35370b364be38f2f855fd0ae2543a50ca7e6b8 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 22 May 2023 17:01:14 +0200
Subject: [PATCH 475/656] Evaluate serial parts of the tape without atomics.

---
 Common/include/code_config.hpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/Common/include/code_config.hpp b/Common/include/code_config.hpp
index bbc5eebb76e..958a82f0e38 100644
--- a/Common/include/code_config.hpp
+++ b/Common/include/code_config.hpp
@@ -96,7 +96,7 @@ FORCEINLINE Out su2staticcast_p(In ptr) {
 #include "codi/tools/data/externalFunctionUserData.hpp"
 
 #if defined(HAVE_OMP)
-using su2double = codi::RealReverseIndexOpenMP;
+using su2double = codi::RealReverseIndexOpenMPGen<double, double>;
 #else
 #if defined(CODI_INDEX_TAPE)
 using su2double = codi::RealReverseIndex;

From 59a142b6f85c3398f3129b44edbe1e5dd64ca0ec Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Mon, 22 May 2023 17:22:04 +0200
Subject: [PATCH 476/656] Modified config to make testcase faster. New test
 duration: 0.42 min.

---
 TestCases/gust/gust_with_mesh_deformation.cfg | 8 ++++----
 TestCases/hybrid_regression.py                | 4 ++--
 2 files changed, 6 insertions(+), 6 deletions(-)

diff --git a/TestCases/gust/gust_with_mesh_deformation.cfg b/TestCases/gust/gust_with_mesh_deformation.cfg
index 9cf09168951..7c0117fc685 100644
--- a/TestCases/gust/gust_with_mesh_deformation.cfg
+++ b/TestCases/gust/gust_with_mesh_deformation.cfg
@@ -26,7 +26,7 @@ CONV_STARTITER= 0
 TIME_DOMAIN=YES
 TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
 TIME_STEP= 0.001
-TIME_ITER= 26
+TIME_ITER= 7
 %
 % --------------------------- GUST SIMULATION ---------------------------------%
 %
@@ -37,13 +37,13 @@ GRID_MOVEMENT=GUST
 WIND_GUST= YES
 GUST_TYPE= ONE_M_COSINE
 GUST_DIR= Y_DIR
-GUST_WAVELENGTH= 10.0
+GUST_WAVELENGTH= 5.0
 GUST_PERIODS= 1.0
 % Gust amplitude corresponds to ~2.0 deg AoA
 GUST_AMPL= 1.0
 %
 GUST_BEGIN_TIME= 0.0
-GUST_BEGIN_LOC=-10.0
+GUST_BEGIN_LOC=-5.0
 % --------------------------- MESH DEFORMATION--------------------------------%
 % Type of dynamic surface movement (NONE, DEFORMING, MOVING_WALL,
 % AEROELASTIC, AEROELASTIC_RIGID_MOTION EXTERNAL, EXTERNAL_ROTATION)
@@ -56,7 +56,7 @@ MARKER_MOVING= ( airfoil )
 SURFACE_PLUNGING_OMEGA= 0.0 125.6 0.0
 %
 % Plunging amplitude (m or ft) in x, y, & z directions
-SURFACE_PLUNGING_AMPL= 0.0 0.001 0.0
+SURFACE_PLUNGING_AMPL= 0.0 0.0001 0.0
 %
 % Move Motion Origin for marker moving (1 or 0)
 MOVE_MOTION_ORIGIN = 0
diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index e0febfcfb2e..12b81ba0870 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -484,8 +484,8 @@ def main():
     gust_mesh_defo           = TestCase('gust_with_mesh_deformation')
     gust_mesh_defo.cfg_dir   = "gust"
     gust_mesh_defo.cfg_file  = "gust_with_mesh_deformation.cfg"
-    gust_mesh_defo.test_iter = 25
-    gust_mesh_defo.test_vals = [-1.585670, 0.004771, 0.000413]
+    gust_mesh_defo.test_iter = 6
+    gust_mesh_defo.test_vals = [-1.844778, 0.000846, -0.000408]
     gust_mesh_defo.unsteady  = True
     test_list.append(gust_mesh_defo)
 

From 8d7f881dbfb67ffb7121e9a00d7b19f1772eca5b Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 22 May 2023 18:34:11 +0200
Subject: [PATCH 477/656] Code formatting.

---
 Common/include/parallelization/omp_structure.hpp | 14 ++++++--------
 1 file changed, 6 insertions(+), 8 deletions(-)

diff --git a/Common/include/parallelization/omp_structure.hpp b/Common/include/parallelization/omp_structure.hpp
index 6f49c3012f4..60baa3e44dd 100644
--- a/Common/include/parallelization/omp_structure.hpp
+++ b/Common/include/parallelization/omp_structure.hpp
@@ -188,16 +188,14 @@ void omp_finalize();
  * thread, with all threads and memory views synchronized both beforehand and afterwards.
  */
 
-#define BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS  \
-  SU2_OMP_BARRIER                         \
-  if (omp_in_parallel())                  \
-    AD::StartNoSharedReading();           \
+#define BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS             \
+  SU2_OMP_BARRIER                                    \
+  if (omp_in_parallel()) AD::StartNoSharedReading(); \
   SU2_OMP_MASTER
 
-#define END_SU2_OMP_SAFE_GLOBAL_ACCESS  \
-  END_SU2_OMP_MASTER                    \
-  if (omp_in_parallel())                \
-    AD::EndNoSharedReading();           \
+#define END_SU2_OMP_SAFE_GLOBAL_ACCESS             \
+  END_SU2_OMP_MASTER                               \
+  if (omp_in_parallel()) AD::EndNoSharedReading(); \
   SU2_OMP_BARRIER
 
 #define SU2_OMP_SAFE_GLOBAL_ACCESS(...) BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS{__VA_ARGS__} END_SU2_OMP_SAFE_GLOBAL_ACCESS

From e593fb61fac5fb1f6e2413f1497f4acde265d933 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 22 May 2023 19:00:46 +0200
Subject: [PATCH 478/656] Non-AD variant of ResizeAdjoints.

---
 Common/include/basic_types/ad_structure.hpp | 5 +++++
 1 file changed, 5 insertions(+)

diff --git a/Common/include/basic_types/ad_structure.hpp b/Common/include/basic_types/ad_structure.hpp
index 99a29debd6a..b12d0068c50 100644
--- a/Common/include/basic_types/ad_structure.hpp
+++ b/Common/include/basic_types/ad_structure.hpp
@@ -74,6 +74,11 @@ inline void RegisterInput(su2double& data, bool push_index = true) {}
  */
 inline void RegisterOutput(su2double& data) {}
 
+/*!
+ * \brief Resize the adjoint vector, for subsequent access without bounds checking.
+ */
+inline void ResizeAdjoints() {}
+
 /*!
  * \brief Sets the adjoint value at index to val
  * \param[in] index - Position in the adjoint vector.

From be6e95fd51be2c8897bf24a0d536fa8e9372a663 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 23 May 2023 15:03:35 +0200
Subject: [PATCH 479/656] Made sure initial density and energy are set for all
 relevant boundary conditions in the compressible flow solvers

---
 Common/include/CConfig.hpp                   | 12 ++++-----
 Common/src/CConfig.cpp                       |  5 ++++
 SU2_CFD/include/variables/CEulerVariable.hpp |  6 ++---
 SU2_CFD/src/solvers/CEulerSolver.cpp         | 23 ++++++++++++++++-
 SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp  | 27 ++++++++++++++++++++
 SU2_CFD/src/solvers/CIncEulerSolver.cpp      | 14 ----------
 6 files changed, 63 insertions(+), 24 deletions(-)

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index 07dcf810e43..5bb5031016c 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -521,11 +521,11 @@ class CConfig {
   Kind_TimeIntScheme_Heat,      /*!< \brief Time integration for the wave equations. */
   Kind_TimeStep_Heat,           /*!< \brief Time stepping method for the (fvm) heat equation. */
   n_Datadriven_files;
-  ENUM_DATADRIVEN_METHOD Kind_DataDriven_Method;       /*!< \brief Method used for datset regression in datadriven fluid models. */
+  ENUM_DATADRIVEN_METHOD Kind_DataDriven_Method;       /*!< \brief Method used for datset regression in data-driven fluid models. */
 
-  su2double DataDriven_Relaxation_Factor, /*!< \brief Relaxation factor for Newton solvers in datadriven fluid models. */
-            DataDriven_initial_density,   /*!< \brief Initial density value for Newton solvers in datadriven fluid models. */
-            DataDriven_initial_energy;    /*!< \brief Initial static energy value for Newton solvers in datadriven fluid models. */
+  su2double DataDriven_Relaxation_Factor, /*!< \brief Relaxation factor for Newton solvers in data-driven fluid models. */
+            DataDriven_initial_density,   /*!< \brief Initial density value for Newton solvers in data-driven fluid models. */
+            DataDriven_initial_energy;    /*!< \brief Initial static energy value for Newton solvers in data-driven fluid models. */
 
   STRUCT_TIME_INT Kind_TimeIntScheme_FEA;    /*!< \brief Time integration for the FEA equations. */
   STRUCT_SPACE_ITE Kind_SpaceIteScheme_FEA;  /*!< \brief Iterative scheme for nonlinear structural analysis. */
@@ -806,7 +806,7 @@ class CConfig {
   SurfSens_FileName,             /*!< \brief Output file for the sensitivity on the surface (discrete adjoint). */
   VolSens_FileName,              /*!< \brief Output file for the sensitivity in the volume (discrete adjoint). */
   ObjFunc_Hess_FileName,         /*!< \brief Hessian approximation obtained by the Sobolev smoothing solver. */
-  *DataDriven_Method_FileNames;    /*!< \brief Dataset information for datadriven fluid models. */
+  *DataDriven_Method_FileNames;    /*!< \brief Dataset information for data-driven fluid models. */
 
   bool
   Wrt_Performance,           /*!< \brief Write the performance summary at the end of a calculation.  */
@@ -3789,7 +3789,7 @@ class CConfig {
 
   /*!
    * \brief Get number of listed look-up table or multi-layer perceptron input files.
-   * \return Number of listed datadriven method input files.
+   * \return Number of listed data-driven method input files.
    */
   unsigned short GetNDataDriven_Files(void) const { return n_Datadriven_files; }
 
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 8588a7d6568..65bf99d958b 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -4922,6 +4922,11 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
     }
   }
 
+  /*--- Data-driven fluid model is currently only supported for compressible flow problems. ---*/
+  if ((Kind_Solver == MAIN_SOLVER::INC_EULER || Kind_Solver == MAIN_SOLVER::INC_NAVIER_STOKES || Kind_Solver == MAIN_SOLVER::INC_RANS) && (Kind_FluidModel == DATADRIVEN_FLUID)) {
+    SU2_MPI::Error("Data-driven fluid model can only be used for compressible flows.", CURRENT_FUNCTION);
+  }
+
   if ((Kind_Solver == MAIN_SOLVER::INC_EULER || Kind_Solver == MAIN_SOLVER::INC_NAVIER_STOKES || Kind_Solver == MAIN_SOLVER::INC_RANS) && (Kind_FluidModel == INC_IDEAL_GAS_POLY)) {
     su2double sum = 0.0;
     for (unsigned short iVar = 0; iVar < N_POLY_COEFFS; iVar++) {
diff --git a/SU2_CFD/include/variables/CEulerVariable.hpp b/SU2_CFD/include/variables/CEulerVariable.hpp
index ca3276817e1..d9a1d809f95 100644
--- a/SU2_CFD/include/variables/CEulerVariable.hpp
+++ b/SU2_CFD/include/variables/CEulerVariable.hpp
@@ -75,9 +75,9 @@ class CEulerVariable : public CFlowVariable {
   MatrixType WindGustDer;   /*! < \brief Wind gust derivatives value */
 
   bool DataDrivenFluid = false; /*!< \brief Usage of data-driven fluid model. DatasetExtrapolation and FluidEntropy will not be sized if disabled. */
-  su2vector<unsigned short> DatasetExtrapolation; /*!< \brief Stores instances of dataset bounds violation when using datadriven fluid models. */
-  su2vector<unsigned long> NIterNewtonsolver;    /*!< \brief Stores number of Newton solver iterations when using datadriven fluid models. */
-  VectorType FluidEntropy;          /*!< \brief Stores the fluid entropy value as computed by the datadriven fluid model. */
+  su2vector<unsigned short> DatasetExtrapolation; /*!< \brief Stores instances of dataset bounds violation when using data-driven fluid models. */
+  su2vector<unsigned long> NIterNewtonsolver;    /*!< \brief Stores number of Newton solver iterations when using data-driven fluid models. */
+  VectorType FluidEntropy;          /*!< \brief Stores the fluid entropy value as computed by the data-driven fluid model. */
 
  public:
   /*!
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index 5183e83dd7b..58b688de933 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -5672,7 +5672,8 @@ void CEulerSolver::PreprocessBC_Giles(CGeometry *geometry, CConfig *config, CNum
                   su2double Velocity2_i = GeometryToolbox::SquaredNorm(nDim, Velocity_i);
                   su2double Energy_i = nodes->GetEnergy(iPoint);
                   su2double StaticEnergy_i = Energy_i - 0.5*Velocity2_i;
-                  GetFluidModel()->SetTDState_rhoe(AverageDensity[iMarker][iSpan], StaticEnergy_i);
+                  GetFluidModel()->SetInitialDensity(AverageDensity[iMarker][iSpan]);
+                  GetFluidModel()->SetInitialEnergy(StaticEnergy_i);
                 }
                 
                 ComputeTurboVelocity(Velocity_i, turboNormal, turboVelocity, marker_flag, config->GetKind_TurboMachinery(iZone));
@@ -7910,6 +7911,11 @@ void CEulerSolver::BC_ActDisk(CGeometry *geometry, CSolver **solver_container, C
       /*--- Subsonic outlet ---*/
 
       else {
+        /* Set initial guesses for density and static energy in case of data-driven fluid model. */
+        if (config->GetKind_FluidModel() == DATADRIVEN_FLUID) {
+          GetFluidModel()->SetInitialDensity(config->GetDensity_Init_DataDriven());
+          GetFluidModel()->SetInitialEnergy(config->GetEnergy_Init_DataDriven());
+        }
 
         GetFluidModel()->SetTDState_PT(P_static, T_static);
         SoS_outlet = GetFluidModel()->GetSoundSpeed();
@@ -8440,6 +8446,11 @@ void CEulerSolver::SetFreeStream_TurboSolution(CConfig *config) {
 
   auto turboNormal = config->GetFreeStreamTurboNormal();
 
+  /* Set initial guess for static energy in case of data-driven fluid model. */
+  if (config->GetKind_FluidModel() == DATADRIVEN_FLUID) {
+    GetFluidModel()->SetInitialEnergy(config->GetEnergy_Init_DataDriven());
+  }
+
   GetFluidModel()->SetTDState_Prho(Pressure_Inf, Density_Inf);
   SoundSpeed = GetFluidModel()->GetSoundSpeed();
 
@@ -8925,6 +8936,11 @@ void CEulerSolver::TurboAverageProcess(CSolver **solver, CGeometry *geometry, CC
             AverageTurboNormal  = geometry->GetAverageTurboNormal(iMarker,iSpan);
             nVert               = geometry->GetnTotVertexSpan(iMarker,iSpan);
 
+            /* Set initial guess for static energy in case of data-driven fluid model. */
+            if (config->GetKind_FluidModel() == DATADRIVEN_FLUID) {
+              GetFluidModel()->SetInitialEnergy(config->GetEnergy_Init_DataDriven());
+            }
+
             /*--- compute normal Mach number as a check for massflow average and mixedout average ---*/
             GetFluidModel()->SetTDState_Prho(TotalAreaPressure/TotalArea, TotalAreaDensity / TotalArea);
             soundSpeed = GetFluidModel()->GetSoundSpeed();
@@ -9244,6 +9260,11 @@ void CEulerSolver::MixedOut_Average (CConfig *config, su2double val_init_pressur
 
   pressure_mix = val_init_pressure;
 
+  /* Set initial guess for static energy in case of data-driven fluid model. */
+  if (config->GetKind_FluidModel() == DATADRIVEN_FLUID) {
+    GetFluidModel()->SetInitialEnergy(config->GetEnergy_Init_DataDriven());
+  }
+
   /*--- Newton-Raphson's method with central difference formula ---*/
 
   while ( iter <= maxiter ) {
diff --git a/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp b/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
index fc4a7a92e36..022225089d7 100644
--- a/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
@@ -7789,8 +7789,16 @@ void CFEM_DG_EulerSolver::BoundaryStates_Riemann(CConfig                  *confi
       P_Total /= config->GetPressure_Ref();
       T_Total /= config->GetTemperature_Ref();
 
+      /* Set initial guesses for density and static energy in case of 
+         data-driven fluid model. */
+      if (config->GetKind_FluidModel() == DATADRIVEN_FLUID) {
+        FluidModel->SetInitialDensity(config->GetDensity_Init_DataDriven());
+        FluidModel->SetInitialEnergy(config->GetEnergy_Init_DataDriven());
+      }
+      
       /* Compute the total enthalpy and entropy from these values. */
       FluidModel->SetTDState_PT(P_Total, T_Total);
+
       const su2double Enthalpy_e = FluidModel->GetStaticEnergy()
                                  + FluidModel->GetPressure()/FluidModel->GetDensity();
       const su2double Entropy_e  = FluidModel->GetEntropy();
@@ -7850,6 +7858,13 @@ void CFEM_DG_EulerSolver::BoundaryStates_Riemann(CConfig                  *confi
       P_static /= config->GetPressure_Ref();
       T_static /= config->GetTemperature_Ref();
 
+      /* Set initial guesses for density and static energy in case of 
+         data-driven fluid model. */
+      if (config->GetKind_FluidModel() == DATADRIVEN_FLUID) {
+        FluidModel->SetInitialDensity(config->GetDensity_Init_DataDriven());
+        FluidModel->SetInitialEnergy(config->GetEnergy_Init_DataDriven());
+      }
+
       /* Compute the prescribed density, static energy per unit mass
          and speed of sound. */
       FluidModel->SetTDState_PT(P_static, T_static);
@@ -7901,6 +7916,12 @@ void CFEM_DG_EulerSolver::BoundaryStates_Riemann(CConfig                  *confi
       P_static /= config->GetPressure_Ref();
       Rho_static /= config->GetDensity_Ref();
 
+      /* Set initial guess for static energy in case of 
+         data-driven fluid model. */
+      if (config->GetKind_FluidModel() == DATADRIVEN_FLUID) {
+        FluidModel->SetInitialEnergy(config->GetEnergy_Init_DataDriven());
+      }
+
       /* Compute the prescribed pressure, static energy per unit mass
          and speed of sound. */
       FluidModel->SetTDState_Prho(P_static, Rho_static);
@@ -7986,6 +8007,12 @@ void CFEM_DG_EulerSolver::BoundaryStates_Riemann(CConfig                  *confi
       const su2double Pressure_e = config->GetRiemann_Var1(Marker_Tag)
                                  / config->GetPressure_Ref();
 
+      /* Set initial guesses for density and static energy in case of 
+         data-driven fluid model. */             
+      if (config->GetKind_FluidModel() == DATADRIVEN_FLUID) {
+        FluidModel->SetInitialDensity(config->GetDensity_Init_DataDriven());
+        FluidModel->SetInitialEnergy(config->GetEnergy_Init_DataDriven());
+      }
       /* Loop over the faces that are treated simultaneously. */
       for(unsigned short l=0; l<nFaceSimul; ++l) {
         const unsigned short llNVar = l*nVar;
diff --git a/SU2_CFD/src/solvers/CIncEulerSolver.cpp b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
index c3ba5e93e2e..e148eb731d3 100644
--- a/SU2_CFD/src/solvers/CIncEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
@@ -30,7 +30,6 @@
 #include "../../include/fluid/CConstantDensity.hpp"
 #include "../../include/fluid/CIncIdealGas.hpp"
 #include "../../include/fluid/CIncIdealGasPolynomial.hpp"
-#include "../../include/fluid/CDataDrivenFluid.hpp"
 #include "../../include/variables/CIncNSVariable.hpp"
 #include "../../include/limiters/CLimiterDetails.hpp"
 #include "../../../Common/include/toolboxes/geometry_toolbox.hpp"
@@ -329,14 +328,6 @@ void CIncEulerSolver::SetNondimensionalization(CConfig *config, unsigned short i
       auxFluidModel->SetTDState_T(Temperature_FreeStream, config->GetSpecies_Init());
       break;
 
-    case DATADRIVEN_FLUID:
-    
-      auxFluidModel = new CDataDrivenFluid(config);
-      auxFluidModel->SetTDState_T(Temperature_FreeStream);
-      Pressure_Thermodynamic = auxFluidModel->GetPressure();
-      config->SetPressure_Thermodynamic(Pressure_Thermodynamic);
-      break;
-
     default:
 
       SU2_MPI::Error("Fluid model not implemented for incompressible solver.", CURRENT_FUNCTION);
@@ -499,11 +490,6 @@ void CIncEulerSolver::SetNondimensionalization(CConfig *config, unsigned short i
         fluidModel->SetTDState_T(Temperature_FreeStreamND);
         break;
 
-      case DATADRIVEN_FLUID:
-        fluidModel = new CDataDrivenFluid(config, false);
-        fluidModel->SetTDState_T(Temperature_FreeStreamND);
-        break;
-
     }
 
     if (viscous) {

From 605839acb6d902cfd58c82faf2b04ed6c6ea999c Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Thu, 25 May 2023 08:56:30 +0200
Subject: [PATCH 480/656] Apply suggestions from Code Review

---
 SU2_CFD/src/iteration/CFluidIteration.cpp     | 24 ++---
 SU2_CFD/src/numerics/flow/flow_sources.cpp    |  2 +-
 TestCases/gust/cosine_gust_zdir.cfg           | 87 +++--------------
 TestCases/gust/gust_with_mesh_deformation.cfg | 96 ++++---------------
 4 files changed, 41 insertions(+), 168 deletions(-)

diff --git a/SU2_CFD/src/iteration/CFluidIteration.cpp b/SU2_CFD/src/iteration/CFluidIteration.cpp
index 59d3d386838..298ee40d56c 100644
--- a/SU2_CFD/src/iteration/CFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CFluidIteration.cpp
@@ -329,23 +329,17 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
 
   su2double Uinf = solver[MESH_0][FLOW_SOL]->GetVelocity_Inf(0);  // Assumption gust moves at infinity velocity
 
-  Gust = new su2double[nDim];
-  NewGridVel = new su2double[nDim];
-  for (iDim = 0; iDim < nDim; iDim++) {
-    Gust[iDim] = 0.0;
-    NewGridVel[iDim] = 0.0;
-  }
+  Gust       = new su2double[nDim]();
+  NewGridVel = new su2double[nDim]();
+  GustDer    = new su2double[nDim+1]();
 
   // Print some information to check that we are doing the right thing. Not sure how to convert the index back to a string...
-  if (rank == MASTER_NODE) cout << endl << "Setting up a wind gust type " << Gust_Type << " with amplitude of " << gust_amp << " in direction " << GustDir << endl;
-  if (rank == MASTER_NODE) cout << " U_inf      = " << Uinf << endl;
-  if (rank == MASTER_NODE) cout << " Physical_t = " << Physical_t << endl;
-  su2double loc_x = (xbegin + L + Uinf * (Physical_t - tbegin));
-  if (rank == MASTER_NODE) cout << " Location_x = " << loc_x << endl;
-
-  GustDer = new su2double[nDim+1];
-  for (unsigned short i = 0; i < nDim+1; i++) {
-    GustDer[i] = 0.0;
+  if (rank == MASTER_NODE) {
+	  cout << endl << "Setting up a wind gust type " << Gust_Type << " with amplitude of " << gust_amp << " in direction " << GustDir << endl;
+	  cout << " U_inf      = " << Uinf << endl;
+	  cout << " Physical_t = " << Physical_t << endl;
+	  su2double loc_x = (xbegin + L + Uinf * (Physical_t - tbegin));
+	  cout << " Location_x = " << loc_x << endl;
   }
 
   // Vortex variables
diff --git a/SU2_CFD/src/numerics/flow/flow_sources.cpp b/SU2_CFD/src/numerics/flow/flow_sources.cpp
index a06cf7134f1..cd8e8d1d4ad 100644
--- a/SU2_CFD/src/numerics/flow/flow_sources.cpp
+++ b/SU2_CFD/src/numerics/flow/flow_sources.cpp
@@ -790,7 +790,7 @@ CNumerics::ResidualType<> CSourceWindGust::ComputeResidual(const CConfig* config
     residual[2] = 0.0;
     residual[3] = 0.0;
     residual[4] = 0.0;
-    }
+  }
 
   /*--- For now the source term Jacobian is just set to zero ---*/
   //bool implicit = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
diff --git a/TestCases/gust/cosine_gust_zdir.cfg b/TestCases/gust/cosine_gust_zdir.cfg
index be0e38a8fd0..515a8d44c49 100644
--- a/TestCases/gust/cosine_gust_zdir.cfg
+++ b/TestCases/gust/cosine_gust_zdir.cfg
@@ -1,30 +1,26 @@
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+%                                                                              %
+% SU2 configuration file                                                       %
+% Case description: Cosine gust in z-direction of a 3D mesh                    %
+% Author: Arne Voß                                                             %
+% Institution: DLR                                                             %
+% Date: 25.05.2023                                                             %
+% File Version 7.5.1 "Blackbird"                                               %
+%                                                                              %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Solver type (EULER, NAVIER_STOKES, RANS,
-%              INC_EULER, INC_NAVIER_STOKES, INC_RANS,
-%              NEMO_EULER, NEMO_NAVIER_STOKES,
-%              FEM_EULER, FEM_NAVIER_STOKES, FEM_RANS, FEM_LES,
-%              HEAT_EQUATION_FVM, ELASTICITY)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
 %
-% Restart solution (NO, YES)
 RESTART_SOL= YES
-%
-% Iteration number to begin unsteady restarts
 RESTART_ITER= 72
 %
 % ------------------------------- SOLVER CONTROL ------------------------------%
 %
-% Maximum number of inner iterations
 INNER_ITER= 30
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -6
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 0
 %
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
@@ -49,124 +45,67 @@ GUST_PERIODS= 1.0
 GUST_AMPL= 2.37
 %
 GUST_BEGIN_TIME= 0.0
+% Gust is placed 5m ahead of the wing
 GUST_BEGIN_LOC=-10.0
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.2
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Side-slip angle (degrees, only for compressible flows)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream option to choose between density and temperature (default) for
-% initializing the solution (TEMPERATURE_FS, DENSITY_FS)
 FREESTREAM_OPTION= DENSITY_FS
-%
-% Free-stream pressure (101325.0 N/m^2, 2116.216 psf by default)
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream density (1.2886 Kg/m^3, 0.0025 slug/ft^3 by default)
 FREESTREAM_DENSITY= 1.225
-%
-% Free-stream temperature (288.15 K, 518.67 R by default)
 FREESTREAM_TEMPERATURE= 288.15
 %
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation (m or in)
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for moment non-dimensional coefficients (m or in)
 REF_LENGTH= 1.0
-%
-% Reference area for non-dimensional force coefficients (0 implies automatic
-% calculation) (m^2 or in^2)
 REF_AREA= 3.0
-%
-% Aircraft semi-span (0 implies automatic calculation) (m or in)
 SEMI_SPAN= 1.5
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= DIMENSIONAL
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
-% Implementation identical to MARKER_SYM.
 MARKER_EULER= ( wing, tip)
-%
-% Far-field boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( far_away )
 
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( wing, tip )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( wing, tip )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% CFL number (initial value for the adaptive CFL number)
 CFL_NUMBER= 1000.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= YES
 %
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-grid levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, JST_KE, JST_MAT, LAX-FRIEDRICH, CUSP, ROE, AUSM,
-%                              AUSMPLUSUP, AUSMPLUSUP2, AUSMPWPLUS, HLLC, TURKEL_PREC,
-%                              SW, MSW, FDS, SLAU, SLAU2, L2ROE, LMROE)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 %
 % ------------------------- SCREEN/HISTORY VOLUME OUTPUT --------------------------%
 %
-% Screen output fields (use 'SU2_CFD -d <config_file>' to view list of available fields)
 SCREEN_OUTPUT= (TIME_ITER, INNER_ITER, RMS_DENSITY, LIFT, MOMENT_X, MOMENT_Y, MOMENT_Z)
-%
-% History output groups (use 'SU2_CFD -d <config_file>' to view list of available fields)
 HISTORY_OUTPUT= (ITER, RMS_RES, AERO_COEFF, CAUCHY, WALL_TIME)
 %
 % ------------------------- INPUT/OUTPUT FILE INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_rectangular_wing.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_gust.dat
 RESTART_FILENAME= restart_gust.dat
 SURFACE_FILENAME= surface_gust
 VOLUME_FILENAME= volume_gust
 CONV_FILENAME= history_gust
-%
-% Output tabular file format (TECPLOT, CSV)
 TABULAR_FORMAT= CSV
-%
-% Files to output
-% Possible formats : (TECPLOT, TECPLOT_BINARY, SURFACE_TECPLOT,
-%  SURFACE_TECPLOT_BINARY, CSV, SURFACE_CSV, PARAVIEW, PARAVIEW_BINARY, SURFACE_PARAVIEW,
-%  SURFACE_PARAVIEW_BINARY, MESH, RESTART_BINARY, RESTART_ASCII, CGNS, SURFACE_CGNS, STL)
 OUTPUT_FILES= (RESTART, RESTART_ASCII)
-
+%
\ No newline at end of file
diff --git a/TestCases/gust/gust_with_mesh_deformation.cfg b/TestCases/gust/gust_with_mesh_deformation.cfg
index 7c0117fc685..6f208952ac9 100644
--- a/TestCases/gust/gust_with_mesh_deformation.cfg
+++ b/TestCases/gust/gust_with_mesh_deformation.cfg
@@ -1,24 +1,22 @@
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+%                                                                              %
+% SU2 configuration file                                                       %
+% Case description: Cosine gust combined with mesh deformation                 %
+% Author: Arne Voß                                                             %
+% Institution: DLR                                                             %
+% Date: 25.05.2023                                                             %
+% File Version 7.5.1 "Blackbird"                                               %
+%                                                                              %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-% Solver type (EULER, NAVIER_STOKES, RANS,
-%              INC_EULER, INC_NAVIER_STOKES, INC_RANS,
-%              NEMO_EULER, NEMO_NAVIER_STOKES,
-%              FEM_EULER, FEM_NAVIER_STOKES, FEM_RANS, FEM_LES,
-%              HEAT_EQUATION_FVM, ELASTICITY)
 SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
-%
 % ------------------------------- SOLVER CONTROL ------------------------------%
 %
-% Maximum number of inner iterations
 INNER_ITER= 100
-%
-% Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -6
-%
-% Start convergence criteria at iteration number
 CONV_STARTITER= 0
 %
 % ------------------------- UNSTEADY SIMULATION -------------------------------%
@@ -39,11 +37,10 @@ GUST_TYPE= ONE_M_COSINE
 GUST_DIR= Y_DIR
 GUST_WAVELENGTH= 5.0
 GUST_PERIODS= 1.0
-% Gust amplitude corresponds to ~2.0 deg AoA
 GUST_AMPL= 1.0
-%
 GUST_BEGIN_TIME= 0.0
 GUST_BEGIN_LOC=-5.0
+%
 % --------------------------- MESH DEFORMATION--------------------------------%
 % Type of dynamic surface movement (NONE, DEFORMING, MOVING_WALL,
 % AEROELASTIC, AEROELASTIC_RIGID_MOTION EXTERNAL, EXTERNAL_ROTATION)
@@ -60,123 +57,66 @@ SURFACE_PLUNGING_AMPL= 0.0 0.0001 0.0
 %
 % Move Motion Origin for marker moving (1 or 0)
 MOVE_MOTION_ORIGIN = 0
+%
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
-% Mach number (non-dimensional, based on the free-stream values)
 MACH_NUMBER= 0.2
-%
-% Angle of attack (degrees, only for compressible flows)
 AOA= 0.0
-%
-% Side-slip angle (degrees, only for compressible flows)
 SIDESLIP_ANGLE= 0.0
-%
-% Free-stream option to choose between density and temperature (default) for
-% initializing the solution (TEMPERATURE_FS, DENSITY_FS)
 FREESTREAM_OPTION= DENSITY_FS
-%
-% Free-stream pressure (101325.0 N/m^2, 2116.216 psf by default)
 FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream density (1.2886 Kg/m^3, 0.0025 slug/ft^3 by default)
 FREESTREAM_DENSITY= 1.225
-%
-% Free-stream temperature (288.15 K, 518.67 R by default)
 FREESTREAM_TEMPERATURE= 288.15
 %
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
-% Reference origin for moment computation (m or in)
 REF_ORIGIN_MOMENT_X = 0.25
 REF_ORIGIN_MOMENT_Y = 0.00
 REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for moment non-dimensional coefficients (m or in)
 REF_LENGTH= 1.0
-%
-% Reference area for non-dimensional force coefficients (0 implies automatic
-% calculation) (m^2 or in^2)
 REF_AREA= 1.0
-%
-% Aircraft semi-span (0 implies automatic calculation) (m or in)
 SEMI_SPAN= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
 REF_DIMENSIONALIZATION= DIMENSIONAL
-
+%
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-% Euler wall boundary marker(s) (NONE = no marker)
-% Implementation identical to MARKER_SYM.
 MARKER_EULER= ( airfoil )
-%
-% Far-field boundary marker(s) (NONE = no marker)
 MARKER_FAR= ( farfield )
-
+%
 % ------------------------ SURFACES IDENTIFICATION ----------------------------%
 %
-% Marker(s) of the surface in the surface flow solution file
 MARKER_PLOTTING = ( airfoil )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
 MARKER_MONITORING = ( airfoil )
-
+%
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-% CFL number (initial value for the adaptive CFL number)
 CFL_NUMBER= 100.0
-%
-% Adaptive CFL number (NO, YES)
 CFL_ADAPT= YES
 %
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %
-% Multi-grid levels (0 = no multi-grid)
 MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
 MGCYCLE= W_CYCLE
-
+%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
-% Convective numerical method (JST, JST_KE, JST_MAT, LAX-FRIEDRICH, CUSP, ROE, AUSM,
-%                              AUSMPLUSUP, AUSMPLUSUP2, AUSMPWPLUS, HLLC, TURKEL_PREC,
-%                              SW, MSW, FDS, SLAU, SLAU2, L2ROE, LMROE)
 CONV_NUM_METHOD_FLOW= JST
-%
-% Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 20
 %
 % ------------------------- SCREEN/HISTORY VOLUME OUTPUT --------------------------%
 %
-% Screen output fields (use 'SU2_CFD -d <config_file>' to view list of available fields)
 SCREEN_OUTPUT= (TIME_ITER, INNER_ITER, RMS_DENSITY, LIFT, MOMENT_Z)
-%
-% History output groups (use 'SU2_CFD -d <config_file>' to view list of available fields)
 HISTORY_OUTPUT= (ITER, RMS_RES, AERO_COEFF, CAUCHY, WALL_TIME)
 %
 % ------------------------- INPUT/OUTPUT FILE INFORMATION --------------------------%
 %
-% Mesh input file
 MESH_FILENAME= mesh_NACA0012_inv.su2
-%
-% Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
-%
-% Restart flow input file
 SOLUTION_FILENAME= restart_gust.dat
 RESTART_FILENAME= restart_gust.dat
 SURFACE_FILENAME= surface_gust
 VOLUME_FILENAME= volume_gust
 CONV_FILENAME= history_gust
-%
-% Output tabular file format (TECPLOT, CSV)
 TABULAR_FORMAT= CSV
-%
-% Files to output
-% Possible formats : (TECPLOT, TECPLOT_BINARY, SURFACE_TECPLOT,
-%  SURFACE_TECPLOT_BINARY, CSV, SURFACE_CSV, PARAVIEW, PARAVIEW_BINARY, SURFACE_PARAVIEW,
-%  SURFACE_PARAVIEW_BINARY, MESH, RESTART_BINARY, RESTART_ASCII, CGNS, SURFACE_CGNS, STL)
 OUTPUT_FILES= (NONE)
-
+%
\ No newline at end of file

From aaea293cf8a8c80bccbdbb357cbb75eed41277be Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Fri, 26 May 2023 18:03:33 +0200
Subject: [PATCH 481/656] Skip bounds checking in SetVertexTractionsAdjoint().

---
 SU2_CFD/src/solvers/CSolver.cpp | 5 +++--
 1 file changed, 3 insertions(+), 2 deletions(-)

diff --git a/SU2_CFD/src/solvers/CSolver.cpp b/SU2_CFD/src/solvers/CSolver.cpp
index 6223385e808..4bd4c0616ee 100644
--- a/SU2_CFD/src/solvers/CSolver.cpp
+++ b/SU2_CFD/src/solvers/CSolver.cpp
@@ -4045,6 +4045,7 @@ void CSolver::SetVertexTractionsAdjoint(CGeometry *geometry, const CConfig *conf
 
   unsigned short iMarker, iDim;
   unsigned long iVertex, iPoint;
+  int index;
 
   /*--- Loop over all the markers ---*/
   for (iMarker = 0; iMarker < config->GetnMarker_All(); iMarker++) {
@@ -4064,8 +4065,8 @@ void CSolver::SetVertexTractionsAdjoint(CGeometry *geometry, const CConfig *conf
 
       /*--- Set the adjoint of the vertex traction from the value received ---*/
       for (iDim = 0; iDim < nDim; iDim++) {
-        SU2_TYPE::SetDerivative(VertexTraction[iMarker][iVertex][iDim],
-                                SU2_TYPE::GetValue(VertexTractionAdjoint[iMarker][iVertex][iDim]));
+        AD::SetIndex(index, VertexTraction[iMarker][iVertex][iDim]);
+        AD::SetDerivative(index, SU2_TYPE::GetValue(VertexTractionAdjoint[iMarker][iVertex][iDim]));
       }
     }
     END_SU2_OMP_FOR

From 9dba7eb5bec67ab061824b361cda853e9d5676a0 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Fri, 26 May 2023 18:04:31 +0200
Subject: [PATCH 482/656] Fix data race.

---
 Common/include/basic_types/ad_structure.hpp | 3 +++
 1 file changed, 3 insertions(+)

diff --git a/Common/include/basic_types/ad_structure.hpp b/Common/include/basic_types/ad_structure.hpp
index b12d0068c50..adb9b94e71a 100644
--- a/Common/include/basic_types/ad_structure.hpp
+++ b/Common/include/basic_types/ad_structure.hpp
@@ -381,6 +381,9 @@ FORCEINLINE void SetIndex(int& index, const su2double& data) { index = data.getI
 // WARNING: For performance reasons, this method does not perform bounds checking.
 // When using it, please ensure sufficient adjoint vector size by a call to AD::ResizeAdjoints().
 FORCEINLINE void SetDerivative(int index, const double val) {
+  if (index == 0)  // Allow multiple threads to "set the derivative" of passive variables without causing data races.
+    return;
+
   using BoundsChecking = codi::GradientAccessTapeInterface<su2double::Gradient, su2double::Identifier>::BoundsChecking;
   AD::getTape().setGradient(index, val, BoundsChecking::False);
 }

From 3113d70e0c07a0873572dae8e36285d3bb9157c5 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 31 May 2023 10:50:22 +0200
Subject: [PATCH 483/656] OpDiLib update.

---
 externals/opdi        | 2 +-
 meson_scripts/init.py | 2 +-
 2 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/externals/opdi b/externals/opdi
index 3ff7bb16bd7..913535c4909 160000
--- a/externals/opdi
+++ b/externals/opdi
@@ -1 +1 @@
-Subproject commit 3ff7bb16bd70aa8f74277704b5feccaaaf6838bd
+Subproject commit 913535c490989ea9aa654e8c7df41c7e3718a5a2
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index f1e298a9cbb..231c091cbb6 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -58,7 +58,7 @@ def init_submodules(
     github_repo_codi = "https://github.com/scicompkl/CoDiPack"
     sha_version_medi = "aafc2d1966ba1233640af737e71c77c1a86183fd"
     github_repo_medi = "https://github.com/SciCompKL/MeDiPack"
-    sha_version_opdi = "3ff7bb16bd70aa8f74277704b5feccaaaf6838bd"
+    sha_version_opdi = "913535c490989ea9aa654e8c7df41c7e3718a5a2"
     github_repo_opdi = "https://github.com/SciCompKL/OpDiLib"
     sha_version_meson = "41c650a040d50e0912d268af7a903a9ce1456dfa"
     github_repo_meson = "https://github.com/mesonbuild/meson"

From 818c39ba3a8ccaf30c7e7669481034a56e7678d2 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 3 Jun 2023 21:27:24 +0100
Subject: [PATCH 484/656] only "coefficient" type outputs are averaged
 automatically

---
 SU2_CFD/include/output/COutput.hpp | 2 +-
 SU2_CFD/src/output/COutput.cpp     | 4 ++--
 2 files changed, 3 insertions(+), 3 deletions(-)

diff --git a/SU2_CFD/include/output/COutput.hpp b/SU2_CFD/include/output/COutput.hpp
index bee30933850..2b41909f254 100644
--- a/SU2_CFD/include/output/COutput.hpp
+++ b/SU2_CFD/include/output/COutput.hpp
@@ -629,7 +629,7 @@ class COutput {
    */
   inline void AddHistoryOutput(string name, string field_name, ScreenOutputFormat format,
                                string groupname, string description,
-                               HistoryFieldType field_type = HistoryFieldType::DEFAULT ){
+                               HistoryFieldType field_type = HistoryFieldType::DEFAULT) {
     historyOutput_Map[name] = HistoryOutputField(field_name, format, groupname, field_type, description);
     historyOutput_List.push_back(name);
   }
diff --git a/SU2_CFD/src/output/COutput.cpp b/SU2_CFD/src/output/COutput.cpp
index 2a8dce49058..ec61f9754e2 100644
--- a/SU2_CFD/src/output/COutput.cpp
+++ b/SU2_CFD/src/output/COutput.cpp
@@ -2120,7 +2120,7 @@ void COutput::SetCustomOutputs(const CConfig* config) {
 #endif
 
       if (type == OperationType::FUNCTION) {
-        AddHistoryOutput(output.name, output.name, ScreenOutputFormat::SCIENTIFIC, "CUSTOM", "Custom output");
+        AddHistoryOutput(output.name, output.name, ScreenOutputFormat::SCIENTIFIC, "CUSTOM", "Custom output", HistoryFieldType::COEFFICIENT);
         break;
       }
 
@@ -2137,7 +2137,7 @@ void COutput::SetCustomOutputs(const CConfig* config) {
       /*--- Skip the terminating "]". ---*/
       if (it != last) ++it;
 
-      AddHistoryOutput(output.name, output.name, ScreenOutputFormat::SCIENTIFIC, "CUSTOM", "Custom output");
+      AddHistoryOutput(output.name, output.name, ScreenOutputFormat::SCIENTIFIC, "CUSTOM", "Custom output", HistoryFieldType::COEFFICIENT);
     }
   }
 

From f4adad0131f3c17c0ce4d29eed63470556de00fa Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 3 Jun 2023 21:35:57 +0100
Subject: [PATCH 485/656] add time averages to incomp solver

---
 SU2_CFD/src/output/CFlowCompOutput.cpp |  4 ++--
 SU2_CFD/src/output/CFlowIncOutput.cpp  | 10 +++++++++-
 SU2_CFD/src/output/CFlowOutput.cpp     |  2 +-
 SU2_CFD/src/output/CNEMOCompOutput.cpp |  2 +-
 4 files changed, 13 insertions(+), 5 deletions(-)

diff --git a/SU2_CFD/src/output/CFlowCompOutput.cpp b/SU2_CFD/src/output/CFlowCompOutput.cpp
index 0e8e6b78613..a943f4dfb98 100644
--- a/SU2_CFD/src/output/CFlowCompOutput.cpp
+++ b/SU2_CFD/src/output/CFlowCompOutput.cpp
@@ -280,7 +280,7 @@ void CFlowCompOutput::SetVolumeOutputFields(CConfig *config){
 
   AddCommonFVMOutputs(config);
 
-  if (config->GetTime_Domain()){
+  if (config->GetTime_Domain()) {
     SetTimeAveragedFields();
   }
 }
@@ -349,7 +349,7 @@ void CFlowCompOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolv
 
   LoadCommonFVMOutputs(config, geometry, iPoint);
 
-  if (config->GetTime_Domain()){
+  if (config->GetTime_Domain()) {
     LoadTimeAveragedData(iPoint, Node_Flow);
   }
 }
diff --git a/SU2_CFD/src/output/CFlowIncOutput.cpp b/SU2_CFD/src/output/CFlowIncOutput.cpp
index 122ebb26a34..dbf63568bd7 100644
--- a/SU2_CFD/src/output/CFlowIncOutput.cpp
+++ b/SU2_CFD/src/output/CFlowIncOutput.cpp
@@ -366,6 +366,10 @@ void CFlowIncOutput::SetVolumeOutputFields(CConfig *config){
   }
 
   AddCommonFVMOutputs(config);
+
+  if (config->GetTime_Domain()) {
+    SetTimeAveragedFields();
+  }
 }
 
 void CFlowIncOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolver **solver, unsigned long iPoint){
@@ -435,13 +439,17 @@ void CFlowIncOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolve
   LoadVolumeDataScalar(config, solver, geometry, iPoint);
 
   // Streamwise Periodicity
-  if(streamwisePeriodic) {
+  if (streamwisePeriodic) {
     SetVolumeOutputValue("RECOVERED_PRESSURE", iPoint, Node_Flow->GetStreamwise_Periodic_RecoveredPressure(iPoint));
     if (heat && streamwisePeriodic_temperature)
       SetVolumeOutputValue("RECOVERED_TEMPERATURE", iPoint, Node_Flow->GetStreamwise_Periodic_RecoveredTemperature(iPoint));
   }
 
   LoadCommonFVMOutputs(config, geometry, iPoint);
+
+  if (config->GetTime_Domain()) {
+    LoadTimeAveragedData(iPoint, Node_Flow);
+  }
 }
 
 bool CFlowIncOutput::SetInitResiduals(const CConfig *config){
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index d297ca6fb99..12189f04d69 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -3653,7 +3653,7 @@ bool CFlowOutput::WriteVolumeOutput(CConfig *config, unsigned long Iter, bool fo
   return force_writing;
 }
 
-void CFlowOutput::SetTimeAveragedFields(){
+void CFlowOutput::SetTimeAveragedFields() {
   AddVolumeOutput("MEAN_DENSITY", "MeanDensity", "TIME_AVERAGE", "Mean density");
   AddVolumeOutput("MEAN_VELOCITY-X", "MeanVelocity_x", "TIME_AVERAGE", "Mean velocity x-component");
   AddVolumeOutput("MEAN_VELOCITY-Y", "MeanVelocity_y", "TIME_AVERAGE", "Mean velocity y-component");
diff --git a/SU2_CFD/src/output/CNEMOCompOutput.cpp b/SU2_CFD/src/output/CNEMOCompOutput.cpp
index a4eba6ff6da..d02a2d0c437 100644
--- a/SU2_CFD/src/output/CNEMOCompOutput.cpp
+++ b/SU2_CFD/src/output/CNEMOCompOutput.cpp
@@ -287,7 +287,7 @@ void CNEMOCompOutput::SetVolumeOutputFields(CConfig *config){
 
   AddCommonFVMOutputs(config);
 
-  if (config->GetTime_Domain()){
+  if (config->GetTime_Domain()) {
     SetTimeAveragedFields();
   }
 }

From bdd22c742e7593878d18a13808fe52dbca696cc7 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 3 Jun 2023 21:35:57 +0100
Subject: [PATCH 486/656] add time averages to incomp solver

---
 SU2_CFD/src/output/CFlowCompOutput.cpp |  4 ++--
 SU2_CFD/src/output/CFlowIncOutput.cpp  | 10 +++++++++-
 SU2_CFD/src/output/CFlowOutput.cpp     |  2 +-
 SU2_CFD/src/output/CNEMOCompOutput.cpp |  2 +-
 4 files changed, 13 insertions(+), 5 deletions(-)

diff --git a/SU2_CFD/src/output/CFlowCompOutput.cpp b/SU2_CFD/src/output/CFlowCompOutput.cpp
index 0e8e6b78613..a943f4dfb98 100644
--- a/SU2_CFD/src/output/CFlowCompOutput.cpp
+++ b/SU2_CFD/src/output/CFlowCompOutput.cpp
@@ -280,7 +280,7 @@ void CFlowCompOutput::SetVolumeOutputFields(CConfig *config){
 
   AddCommonFVMOutputs(config);
 
-  if (config->GetTime_Domain()){
+  if (config->GetTime_Domain()) {
     SetTimeAveragedFields();
   }
 }
@@ -349,7 +349,7 @@ void CFlowCompOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolv
 
   LoadCommonFVMOutputs(config, geometry, iPoint);
 
-  if (config->GetTime_Domain()){
+  if (config->GetTime_Domain()) {
     LoadTimeAveragedData(iPoint, Node_Flow);
   }
 }
diff --git a/SU2_CFD/src/output/CFlowIncOutput.cpp b/SU2_CFD/src/output/CFlowIncOutput.cpp
index 122ebb26a34..dbf63568bd7 100644
--- a/SU2_CFD/src/output/CFlowIncOutput.cpp
+++ b/SU2_CFD/src/output/CFlowIncOutput.cpp
@@ -366,6 +366,10 @@ void CFlowIncOutput::SetVolumeOutputFields(CConfig *config){
   }
 
   AddCommonFVMOutputs(config);
+
+  if (config->GetTime_Domain()) {
+    SetTimeAveragedFields();
+  }
 }
 
 void CFlowIncOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolver **solver, unsigned long iPoint){
@@ -435,13 +439,17 @@ void CFlowIncOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolve
   LoadVolumeDataScalar(config, solver, geometry, iPoint);
 
   // Streamwise Periodicity
-  if(streamwisePeriodic) {
+  if (streamwisePeriodic) {
     SetVolumeOutputValue("RECOVERED_PRESSURE", iPoint, Node_Flow->GetStreamwise_Periodic_RecoveredPressure(iPoint));
     if (heat && streamwisePeriodic_temperature)
       SetVolumeOutputValue("RECOVERED_TEMPERATURE", iPoint, Node_Flow->GetStreamwise_Periodic_RecoveredTemperature(iPoint));
   }
 
   LoadCommonFVMOutputs(config, geometry, iPoint);
+
+  if (config->GetTime_Domain()) {
+    LoadTimeAveragedData(iPoint, Node_Flow);
+  }
 }
 
 bool CFlowIncOutput::SetInitResiduals(const CConfig *config){
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index d297ca6fb99..12189f04d69 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -3653,7 +3653,7 @@ bool CFlowOutput::WriteVolumeOutput(CConfig *config, unsigned long Iter, bool fo
   return force_writing;
 }
 
-void CFlowOutput::SetTimeAveragedFields(){
+void CFlowOutput::SetTimeAveragedFields() {
   AddVolumeOutput("MEAN_DENSITY", "MeanDensity", "TIME_AVERAGE", "Mean density");
   AddVolumeOutput("MEAN_VELOCITY-X", "MeanVelocity_x", "TIME_AVERAGE", "Mean velocity x-component");
   AddVolumeOutput("MEAN_VELOCITY-Y", "MeanVelocity_y", "TIME_AVERAGE", "Mean velocity y-component");
diff --git a/SU2_CFD/src/output/CNEMOCompOutput.cpp b/SU2_CFD/src/output/CNEMOCompOutput.cpp
index a4eba6ff6da..d02a2d0c437 100644
--- a/SU2_CFD/src/output/CNEMOCompOutput.cpp
+++ b/SU2_CFD/src/output/CNEMOCompOutput.cpp
@@ -287,7 +287,7 @@ void CNEMOCompOutput::SetVolumeOutputFields(CConfig *config){
 
   AddCommonFVMOutputs(config);
 
-  if (config->GetTime_Domain()){
+  if (config->GetTime_Domain()) {
     SetTimeAveragedFields();
   }
 }

From 8c151f32a3833129b1f11b43fe91dc92cd2080aa Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 3 Jun 2023 21:39:04 +0100
Subject: [PATCH 487/656] Revert "add time averages to incomp solver"

This reverts commit f4adad0131f3c17c0ce4d29eed63470556de00fa.
---
 SU2_CFD/src/output/CFlowCompOutput.cpp |  4 ++--
 SU2_CFD/src/output/CFlowIncOutput.cpp  | 10 +---------
 SU2_CFD/src/output/CFlowOutput.cpp     |  2 +-
 SU2_CFD/src/output/CNEMOCompOutput.cpp |  2 +-
 4 files changed, 5 insertions(+), 13 deletions(-)

diff --git a/SU2_CFD/src/output/CFlowCompOutput.cpp b/SU2_CFD/src/output/CFlowCompOutput.cpp
index a943f4dfb98..0e8e6b78613 100644
--- a/SU2_CFD/src/output/CFlowCompOutput.cpp
+++ b/SU2_CFD/src/output/CFlowCompOutput.cpp
@@ -280,7 +280,7 @@ void CFlowCompOutput::SetVolumeOutputFields(CConfig *config){
 
   AddCommonFVMOutputs(config);
 
-  if (config->GetTime_Domain()) {
+  if (config->GetTime_Domain()){
     SetTimeAveragedFields();
   }
 }
@@ -349,7 +349,7 @@ void CFlowCompOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolv
 
   LoadCommonFVMOutputs(config, geometry, iPoint);
 
-  if (config->GetTime_Domain()) {
+  if (config->GetTime_Domain()){
     LoadTimeAveragedData(iPoint, Node_Flow);
   }
 }
diff --git a/SU2_CFD/src/output/CFlowIncOutput.cpp b/SU2_CFD/src/output/CFlowIncOutput.cpp
index dbf63568bd7..122ebb26a34 100644
--- a/SU2_CFD/src/output/CFlowIncOutput.cpp
+++ b/SU2_CFD/src/output/CFlowIncOutput.cpp
@@ -366,10 +366,6 @@ void CFlowIncOutput::SetVolumeOutputFields(CConfig *config){
   }
 
   AddCommonFVMOutputs(config);
-
-  if (config->GetTime_Domain()) {
-    SetTimeAveragedFields();
-  }
 }
 
 void CFlowIncOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolver **solver, unsigned long iPoint){
@@ -439,17 +435,13 @@ void CFlowIncOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolve
   LoadVolumeDataScalar(config, solver, geometry, iPoint);
 
   // Streamwise Periodicity
-  if (streamwisePeriodic) {
+  if(streamwisePeriodic) {
     SetVolumeOutputValue("RECOVERED_PRESSURE", iPoint, Node_Flow->GetStreamwise_Periodic_RecoveredPressure(iPoint));
     if (heat && streamwisePeriodic_temperature)
       SetVolumeOutputValue("RECOVERED_TEMPERATURE", iPoint, Node_Flow->GetStreamwise_Periodic_RecoveredTemperature(iPoint));
   }
 
   LoadCommonFVMOutputs(config, geometry, iPoint);
-
-  if (config->GetTime_Domain()) {
-    LoadTimeAveragedData(iPoint, Node_Flow);
-  }
 }
 
 bool CFlowIncOutput::SetInitResiduals(const CConfig *config){
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index 12189f04d69..d297ca6fb99 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -3653,7 +3653,7 @@ bool CFlowOutput::WriteVolumeOutput(CConfig *config, unsigned long Iter, bool fo
   return force_writing;
 }
 
-void CFlowOutput::SetTimeAveragedFields() {
+void CFlowOutput::SetTimeAveragedFields(){
   AddVolumeOutput("MEAN_DENSITY", "MeanDensity", "TIME_AVERAGE", "Mean density");
   AddVolumeOutput("MEAN_VELOCITY-X", "MeanVelocity_x", "TIME_AVERAGE", "Mean velocity x-component");
   AddVolumeOutput("MEAN_VELOCITY-Y", "MeanVelocity_y", "TIME_AVERAGE", "Mean velocity y-component");
diff --git a/SU2_CFD/src/output/CNEMOCompOutput.cpp b/SU2_CFD/src/output/CNEMOCompOutput.cpp
index d02a2d0c437..a4eba6ff6da 100644
--- a/SU2_CFD/src/output/CNEMOCompOutput.cpp
+++ b/SU2_CFD/src/output/CNEMOCompOutput.cpp
@@ -287,7 +287,7 @@ void CNEMOCompOutput::SetVolumeOutputFields(CConfig *config){
 
   AddCommonFVMOutputs(config);
 
-  if (config->GetTime_Domain()) {
+  if (config->GetTime_Domain()){
     SetTimeAveragedFields();
   }
 }

From 35389df1651b8b3ddaf22e030f4e501697aa7570 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?K=C3=BCr=C5=9Fat=20Yurt?=
 <57598663+kursatyurt@users.noreply.github.com>
Date: Wed, 7 Jun 2023 09:49:56 +0200
Subject: [PATCH 488/656] Add python interface for setting AoA and AoS (#2045)

* Add python methods for setting AoA and AoS

---------

Co-authored-by: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
---
 SU2_CFD/include/drivers/CDriver.hpp           | 12 ++++++++++
 .../include/solvers/CFVMFlowSolverBase.hpp    | 23 +++++++++++++++++++
 SU2_CFD/include/solvers/CSolver.hpp           |  5 ++++
 SU2_CFD/src/python_wrapper_structure.cpp      | 11 +++++++++
 SU2_CFD/src/solvers/CEulerSolver.cpp          | 21 +----------------
 5 files changed, 52 insertions(+), 20 deletions(-)

diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index 694c66ec6bf..236c932b630 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -508,6 +508,18 @@ class CDriver : public CDriverBase {
    */
   void SetInletAngle(unsigned short iMarker, passivedouble alpha);
 
+  /*!
+   * \brief Set the angle of attack of the farfield.
+   * \param[in] alpha - Angle (degree).
+   */
+  void SetFarFieldAoA(passivedouble alpha);
+
+  /*!
+   * \brief Set the angle of sideslip of the farfield.
+   * \param[in] beta - Angle (degree).
+   */
+  void SetFarFieldAoS(passivedouble beta);
+
   /*!
    * \brief Set the dynamic mesh translation rates.
    * \param[in] xDot - Value of translational velocity in x-direction.
diff --git a/SU2_CFD/include/solvers/CFVMFlowSolverBase.hpp b/SU2_CFD/include/solvers/CFVMFlowSolverBase.hpp
index 1fa8f1fb8b0..b1dc8b8a308 100644
--- a/SU2_CFD/include/solvers/CFVMFlowSolverBase.hpp
+++ b/SU2_CFD/include/solvers/CFVMFlowSolverBase.hpp
@@ -2198,6 +2198,29 @@ class CFVMFlowSolverBase : public CSolver {
       Inlet_FlowDir[val_marker][val_vertex][val_dim] = val_flowdir;
   }
 
+  /*!
+   * \brief Updates the components of the farfield velocity vector.
+   */
+  inline void UpdateFarfieldVelocity(const CConfig* config) final {
+    /*--- Retrieve the AoA and AoS (degrees) ---*/
+    const su2double AoA = config->GetAoA() * PI_NUMBER / 180.0;
+    const su2double AoS = config->GetAoS() * PI_NUMBER / 180.0;
+    /*--- Update the freestream velocity vector at the farfield
+     * Compute the new freestream velocity with the updated AoA,
+     * "Velocity_Inf" is shared with config. ---*/
+
+    const su2double Vel_Infty_Mag = GeometryToolbox::Norm(nDim, Velocity_Inf);
+
+    if (nDim == 2) {
+      Velocity_Inf[0] = cos(AoA) * Vel_Infty_Mag;
+      Velocity_Inf[1] = sin(AoA) * Vel_Infty_Mag;
+    } else {
+      Velocity_Inf[0] = cos(AoA) * cos(AoS) * Vel_Infty_Mag;
+      Velocity_Inf[1] = sin(AoS) * Vel_Infty_Mag;
+      Velocity_Inf[2] = sin(AoA) * cos(AoS) * Vel_Infty_Mag;
+    }
+  }
+
   /*!
    * \brief Compute the global error measures (L2, Linf) for verification cases.
    * \param[in] geometry - Geometrical definition.
diff --git a/SU2_CFD/include/solvers/CSolver.hpp b/SU2_CFD/include/solvers/CSolver.hpp
index ba28bf8b193..06cd950aa13 100644
--- a/SU2_CFD/include/solvers/CSolver.hpp
+++ b/SU2_CFD/include/solvers/CSolver.hpp
@@ -2871,6 +2871,11 @@ class CSolver {
                                        unsigned short val_dim,
                                        su2double val_flowdir) { }
 
+  /*!
+   * \brief Updates the components of the farfield velocity vector.
+   */
+  inline virtual void UpdateFarfieldVelocity(const CConfig* config) {}
+
   /*!
    * \brief A virtual member
    * \param[in] iMarker - Marker identifier.
diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index f470bc03564..ffcc36d2f54 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -97,6 +97,16 @@ void CDriver::SetInletAngle(unsigned short iMarker, passivedouble alpha) {
   }
 }
 
+void CDriver::SetFarFieldAoA(const passivedouble AoA) {
+  config_container[ZONE_0]->SetAoA(AoA);
+  solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->UpdateFarfieldVelocity(config_container[ZONE_0]);
+}
+
+void CDriver::SetFarFieldAoS(const passivedouble AoS) {
+  config_container[ZONE_0]->SetAoS(AoS);
+  solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->UpdateFarfieldVelocity(config_container[ZONE_0]);
+}
+
 /////////////////////////////////////////////////////////////////////////////////////////////////////////////////
 /* Functions related to simulation control, high level functions (reset convergence, set initial mesh, etc.)   */
 /////////////////////////////////////////////////////////////////////////////////////////////////////////////////
@@ -156,3 +166,4 @@ void CDriver::SetRotationRate(passivedouble rot_x, passivedouble rot_y, passived
     config_container[iZone]->SetRotation_Rate(2, rot_z);
   }
 }
+
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index 547cc8c307c..6fe92b813d3 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -4061,8 +4061,6 @@ void CEulerSolver::SetFarfield_AoA(CGeometry *geometry, CSolver **solver_contain
                                    CConfig *config, unsigned short iMesh, bool Output) {
 
   const auto InnerIter = config->GetInnerIter();
-  const su2double AoS = config->GetAoS()*PI_NUMBER/180.0;
-
   /* --- Initialize values at first iteration --- */
 
   if (InnerIter == 0) {
@@ -4101,24 +4099,7 @@ void CEulerSolver::SetFarfield_AoA(CGeometry *geometry, CSolver **solver_contain
       AoA = AoA + AoA_inc;
       config->SetAoA(AoA);
     }
-
-    AoA *= PI_NUMBER/180.0;
-
-    /*--- Update the freestream velocity vector at the farfield
-     * Compute the new freestream velocity with the updated AoA,
-     * "Velocity_Inf" is shared with config. ---*/
-
-    const su2double Vel_Infty_Mag = GeometryToolbox::Norm(nDim, Velocity_Inf);
-
-    if (nDim == 2) {
-      Velocity_Inf[0] = cos(AoA)*Vel_Infty_Mag;
-      Velocity_Inf[1] = sin(AoA)*Vel_Infty_Mag;
-    }
-    else {
-      Velocity_Inf[0] = cos(AoA)*cos(AoS)*Vel_Infty_Mag;
-      Velocity_Inf[1] = sin(AoS)*Vel_Infty_Mag;
-      Velocity_Inf[2] = sin(AoA)*cos(AoS)*Vel_Infty_Mag;
-    }
+    UpdateFarfieldVelocity(config);
   }
 }
 

From 979feffd7d9b3a69e2f901b05442939580be0329 Mon Sep 17 00:00:00 2001
From: Nijso <bigfootedrockmidget@hotmail.com>
Date: Wed, 7 Jun 2023 16:33:09 +0200
Subject: [PATCH 489/656] Flamelet approach for premixed flames (#1917)

* Add capabilities for progress variable - flamelet approach for laminar premixed flames
---------

Co-authored-by: Daniel Mayer <daniel.mayer4@us.bosch.com>
Co-authored-by: EvertBunschoten <evertbun@xs4all.nl>
Co-authored-by: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Co-authored-by: danielmayer <the.mayer@icloud.com>
Co-authored-by: Cristopher Morales <98025159+Cristopher-Morales@users.noreply.github.com>
---
 Common/include/CConfig.hpp                    |  85 ++-
 Common/include/containers/CLookUpTable.hpp    | 195 ++++---
 Common/include/option_structure.hpp           |  68 ++-
 Common/src/CConfig.cpp                        | 132 ++++-
 Common/src/containers/CFileReaderLUT.cpp      |   2 +-
 Common/src/containers/CLookUpTable.cpp        |  22 +-
 Common/src/containers/CTrapezoidalMap.cpp     |  63 ++-
 Common/src/grid_movement/CSurfaceMovement.cpp |   2 +-
 SU2_CFD/include/fluid/CFluidFlamelet.hpp      | 114 ++++
 SU2_CFD/include/fluid/CFluidModel.hpp         |  21 +-
 .../numerics/species/species_diffusion.hpp    |   2 +-
 .../numerics/species/species_sources.hpp      |   1 +
 SU2_CFD/include/output/CFlowIncOutput.hpp     |   1 +
 SU2_CFD/include/output/CFlowOutput.hpp        |  26 +-
 .../solvers/CSpeciesFlameletSolver.hpp        | 171 ++++++
 SU2_CFD/include/solvers/CSpeciesSolver.hpp    |   6 +-
 .../variables/CSpeciesFlameletVariable.hpp    |  90 +++
 .../include/variables/CSpeciesVariable.hpp    |   2 +-
 SU2_CFD/include/variables/CVariable.hpp       |  13 +
 SU2_CFD/src/drivers/CDriver.cpp               |   3 +
 SU2_CFD/src/drivers/CMultizoneDriver.cpp      |   8 +
 SU2_CFD/src/drivers/CSinglezoneDriver.cpp     |   5 +
 SU2_CFD/src/fluid/CFluidFlamelet.cpp          | 138 +++++
 SU2_CFD/src/fluid/CFluidModel.cpp             |  12 +-
 SU2_CFD/src/integration/CIntegration.cpp      |   7 +-
 .../cht/CConjugateHeatInterface.cpp           |   1 +
 SU2_CFD/src/iteration/CFluidIteration.cpp     |   2 +-
 SU2_CFD/src/meson.build                       |   3 +
 .../src/numerics/species/species_sources.cpp  |   3 +-
 SU2_CFD/src/output/CAdjFlowOutput.cpp         | 115 +++-
 SU2_CFD/src/output/CFlowCompOutput.cpp        |   8 +
 SU2_CFD/src/output/CFlowIncOutput.cpp         |  15 +-
 SU2_CFD/src/output/CFlowOutput.cpp            | 349 ++++++++++--
 SU2_CFD/src/output/CMultizoneOutput.cpp       |   2 +-
 SU2_CFD/src/output/CNEMOCompOutput.cpp        |   8 +
 SU2_CFD/src/output/COutput.cpp                |   1 -
 SU2_CFD/src/solvers/CEulerSolver.cpp          |   1 +
 SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp   |   1 +
 SU2_CFD/src/solvers/CIncEulerSolver.cpp       |  66 ++-
 SU2_CFD/src/solvers/CSolver.cpp               |  10 +
 SU2_CFD/src/solvers/CSolverFactory.cpp        |  22 +-
 .../src/solvers/CSpeciesFlameletSolver.cpp    | 511 ++++++++++++++++++
 SU2_CFD/src/solvers/CSpeciesSolver.cpp        | 127 +++--
 SU2_CFD/src/solvers/CTurbSolver.cpp           |   3 +-
 SU2_CFD/src/variables/CIncNSVariable.cpp      |  12 +-
 .../variables/CSpeciesFlameletVariable.cpp    |  56 ++
 TestCases/.gitignore                          |   3 +
 .../lam_prem_ch4_cfd.cfg                      | 135 +++++
 .../lam_prem_ch4_hx_ad.cfg                    | 141 +++++
 .../lam_prem_ch4_hx_dot.cfg                   | 251 +++++++++
 .../lam_prem_ch4_cht_cfd_fluid.cfg            | 109 ++++
 .../lam_prem_ch4_cht_cfd_master.cfg           |  55 ++
 .../lam_prem_ch4_cht_cfd_solid.cfg            |  57 ++
 .../lam_prem_ch4_cht_ad_fluid.cfg             | 110 ++++
 .../lam_prem_ch4_cht_ad_master.cfg            |  97 ++++
 .../lam_prem_ch4_cht_ad_solid.cfg             |  57 ++
 .../lam_prem_ch4_cht_dot_master.cfg           |  97 ++++
 .../lam_prem_ch4_cfd_axi.cfg                  | 136 +++++
 TestCases/flamelet/README.md                  |   8 +
 TestCases/parallel_regression.py              |  41 ++
 TestCases/parallel_regression_AD.py           |  71 +++
 .../species_transport/multizone/zone1.cfg     |   1 -
 .../species_transport/multizone/zone2.cfg     |   1 -
 .../passive_transport.cfg                     |   2 +-
 .../species2_primitiveVenturi.cfg             |   1 -
 ...pecies2_primitiveVenturi_boundedscalar.cfg |   1 -
 .../species2_primitiveVenturi_mixingmodel.cfg |   1 -
 ...eVenturi_mixingmodel_TURBULENT_MARKERS.cfg |   2 +-
 ...itiveVenturi_mixingmodel_boundedscalar.cfg |   1 -
 ...iveVenturi_mixingmodel_heatcapacity_H2.cfg |   2 +-
 ...Venturi_mixingmodel_heatcapacity_H2_ND.cfg |   2 +-
 ...primitiveVenturi_mixingmodel_viscosity.cfg |   1 -
 .../species3_primitiveVenturi_inletFile.cfg   |   1 -
 .../user_defined_functions/lam_flatplate.cfg  |   2 +-
 config_template.cfg                           |  45 +-
 75 files changed, 3602 insertions(+), 334 deletions(-)
 create mode 100644 SU2_CFD/include/fluid/CFluidFlamelet.hpp
 create mode 100644 SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp
 create mode 100644 SU2_CFD/include/variables/CSpeciesFlameletVariable.hpp
 create mode 100644 SU2_CFD/src/fluid/CFluidFlamelet.cpp
 create mode 100644 SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
 create mode 100644 SU2_CFD/src/variables/CSpeciesFlameletVariable.cpp
 create mode 100644 TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg
 create mode 100644 TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg
 create mode 100644 TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg
 create mode 100644 TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg
 create mode 100644 TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_master.cfg
 create mode 100644 TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_solid.cfg
 create mode 100644 TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg
 create mode 100644 TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_master.cfg
 create mode 100644 TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_solid.cfg
 create mode 100644 TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_dot_master.cfg
 create mode 100644 TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg
 create mode 100644 TestCases/flamelet/README.md

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index d1ac360a4bb..54e00341482 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -697,6 +697,7 @@ class CConfig {
   nMarker_PyCustom,                   /*!< \brief Number of markers that are customizable in Python. */
   nMarker_DV,                         /*!< \brief Number of markers affected by the design variables. */
   nMarker_WallFunctions,              /*!< \brief Number of markers for which wall functions must be applied. */
+  nMarker_StrongBC,                   /*!< \brief Number of markers for which a strong BC must be applied. */
   nMarker_SobolevBC;                  /*!< \brief Number of markers treaded in the gradient problem. */
   string *Marker_Monitoring,          /*!< \brief Markers to monitor. */
   *Marker_Designing,                  /*!< \brief Markers to design. */
@@ -708,6 +709,7 @@ class CConfig {
   *Marker_PyCustom,                   /*!< \brief Markers that are customizable in Python. */
   *Marker_DV,                         /*!< \brief Markers affected by the design variables. */
   *Marker_WallFunctions,              /*!< \brief Markers for which wall functions must be applied. */
+  *Marker_StrongBC,                   /*!< \brief Markers for which a strong BC must be applied. */
   *Marker_SobolevBC;                  /*!< \brief Markers in the gradient solver */
 
   unsigned short nConfig_Files;       /*!< \brief Number of config files for multiphysics problems. */
@@ -1179,7 +1181,7 @@ class CConfig {
   unsigned short maxBasisDim,               /*!< \brief Maximum number of POD basis dimensions. */
   rom_save_freq;                            /*!< \brief Frequency of unsteady time steps to save. */
 
-  unsigned short nSpecies;                  /*!< \brief Number of transported species equations (for NEMO and species transport)*/
+  unsigned short nSpecies = 0;              /*!< \brief Number of transported species equations (for NEMO and species transport)*/
 
   /* other NEMO configure options*/
   unsigned short nSpecies_Cat_Wall,         /*!< \brief No. of species for a catalytic wall. */
@@ -1210,6 +1212,23 @@ class CConfig {
   su2double* Species_Init;         /*!< \brief Initial uniform value for scalar transport. */
   unsigned short nSpecies_Init;    /*!< \brief Number of entries of SPECIES_INIT */
 
+  /*--- Additional flamelet solver options ---*/
+  su2double flame_init[8];       /*!< \brief Initial solution parameters for flamelet solver.*/
+
+  /*--- lookup table ---*/
+  unsigned short n_scalars = 0;       /*!< \brief Number of transported scalars for flamelet LUT approach. */
+  unsigned short n_lookups = 0;       /*!< \brief Number of lookup variables, for visualization only. */
+  unsigned short n_table_sources = 0; /*!< \brief Number of transported scalar source terms for LUT. */
+  unsigned short n_user_scalars = 0;  /*!< \brief Number of user defined (auxiliary) scalar transport equations. */
+  unsigned short n_user_sources = 0;  /*!< \brief Number of source terms for user defined (auxiliary) scalar transport equations. */
+  unsigned short n_control_vars = 0;  /*!< \brief Number of controlling variables (independent variables) for the LUT. */
+
+  vector<string> table_scalar_names;  /*!< \brief Names of transported scalar variables. */
+  string* table_lookup_names;         /*!< \brief Names of LUT variables. */
+  string file_name_lut;               /*!< \brief Filename of the LUT. */
+  string* user_scalar_names;          /*!< \brief Names of the user defined (auxiliary) transported scalars .*/
+  string* user_source_names;          /*!< \brief Names of the source terms for the user defined transported scalars. */
+
   /*!
    * \brief Set the default values of config options not set in the config file using another config object.
    * \param config - Config object to use the default values from.
@@ -2101,6 +2120,63 @@ class CConfig {
    */
   bool GetSpecies_StrongBC() const { return Species_StrongBC; }
 
+  /*!
+   * \brief Get the flame initialization.
+   *        (x1,x2,x3) = flame offset.
+   *        (x4,x5,x6) = flame normal, separating unburnt from burnt.
+   *        (x7) = flame thickness, the length from unburnt to burnt conditions.
+   *        (x8) = flame burnt thickness, the length to stay at burnt conditions.
+   * \return Flame initialization for the flamelet model.
+   */
+  const su2double* GetFlameInit() const { return flame_init; }
+
+  /*!
+   * \brief Get the number of control variables for flamelet model.
+   */
+  unsigned short GetNControlVars() const { return n_control_vars; }
+
+  /*!
+   * \brief Get the number of total transported scalars for flamelet model.
+   */
+  unsigned short GetNScalars() const { return n_scalars; }
+
+  /*!
+   * \brief Get the number of user scalars for flamelet model.
+   */
+  unsigned short GetNUserScalars() const { return n_user_scalars; }
+
+  /*!
+   * \brief Get the name of the user scalar.
+   */
+  const string& GetUserScalarName(unsigned short i_user_scalar) const {
+    static const std::string none = "NONE";
+    if (n_user_scalars > 0) return user_scalar_names[i_user_scalar]; else return none;
+  }
+
+  /*!
+   * \brief Get the name of the user scalar source term.
+   */
+  const string& GetUserSourceName(unsigned short i_user_source) const {
+    static const std::string none = "NONE";
+    if (n_user_sources > 0) return user_source_names[i_user_source]; else return none;
+  }
+
+  /*!
+   * \brief Get the number of transported scalars for combustion.
+   */
+  unsigned short GetNLookups() const { return n_lookups; }
+
+  /*!
+   * \brief Get the name of the variable that we want to retrieve from the lookup table.
+   */
+  const string& GetLUTLookupName(unsigned short i_lookup) const { return table_lookup_names[i_lookup]; }
+
+  /*!
+   * \brief Get the file name of the look up table.
+   * \return File name of the look up table.
+   */
+  const string& GetFileNameLUT() const { return file_name_lut; }
+
   /*!
    * \brief Get the Young's modulus of elasticity.
    * \return Value of the Young's modulus of elasticity.
@@ -9305,6 +9381,13 @@ class CConfig {
    */
   su2double GetWall_Emissivity(const string& val_index) const;
 
+  /*!
+   * \brief Get if boundary is strong or weak.
+   * \param[in] val_index - Index corresponding to the boundary.
+   * \return true if strong BC.
+   */
+  bool GetMarker_StrongBC(const string& val_index) const;
+
   /*!
    * \brief Get the value of the CFL condition for radiation solvers.
    * \return Value of the CFL condition for radiation solvers.
diff --git a/Common/include/containers/CLookUpTable.hpp b/Common/include/containers/CLookUpTable.hpp
index f6cd4c91bb8..0effac26d4d 100644
--- a/Common/include/containers/CLookUpTable.hpp
+++ b/Common/include/containers/CLookUpTable.hpp
@@ -60,13 +60,13 @@ class CLookUpTable {
 
   unsigned short table_dim = 2; /*!< \brief Table dimension.*/
   /*!
-   * \brief the lower and upper limits of the z, y and x variable for each table level.
+   * \brief The lower and upper limits of the z, y and x variable for each table level.
    */
   std::pair<su2double*, su2double*> limits_table_z;
   su2vector<std::pair<su2double*, su2double*>> limits_table_y, limits_table_x;
 
   /*! \brief Holds the variable names stored in the table file.
-   * Order is in sync with data
+   * Order is in sync with data.
    */
   su2vector<std::string> names_var;
 
@@ -99,12 +99,12 @@ class CLookUpTable {
   su2vector<CTrapezoidalMap> trap_map_x_y;
 
   /*! \brief
-   * vector of all the weight factors for the interpolation.
+   * Vector of all the weight factors for the interpolation.
    */
   su2vector<su2vector<su2activematrix>> interp_mat_inv_x_y;
 
   /*! \brief
-   * returns the index to the variable in the lookup table.
+   * Returns the index to the variable in the lookup table.
    */
   inline unsigned int GetIndexOfVar(const std::string& nameVar) const {
     int index = find(names_var.begin(), names_var.end(), nameVar) - names_var.begin();
@@ -118,72 +118,84 @@ class CLookUpTable {
     return index;
   }
 
+  /*! \brief
+   * Returns true if the string is null or zero (ignores case).
+   */
+  inline bool noSource(const std::string& name_var) const {
+    if (name_var.compare("NULL") == 0 || name_var.compare("Null") == 0 || name_var.compare("null") == 0 ||
+        name_var.compare("ZERO") == 0 || name_var.compare("Zero") == 0 || name_var.compare("zero") == 0) {
+      return true;
+    } else {
+      return false;
+    }
+  }
+
   /*!
    * \brief Get the pointer to the column data of the table (density, temperature, source terms, ...).
-   * \returns pointer to the column data.
+   * \returns Pointer to the column data.
    */
   inline const su2double* GetDataP(const std::string& name_var, unsigned long i_level = 0) const {
     return table_data[i_level][GetIndexOfVar(name_var)];
   }
 
   /*!
-   * \brief find the table limits, i.e. the minimum and maximum values of the 2 independent.
+   * \brief Find the table limits, i.e. the minimum and maximum values of the 2 independent
    * controlling variables. We put the values in the variables.
    * limits_table_x[2] and limit_table_y[2].
-   * \param[in] name_CV1 - the string name for the first controlling variable.
-   * \param[in] name_CV2 - the string name of the second controlling variable.
+   * \param[in] name_CV1 - The string name for the first controlling variable.
+   * \param[in] name_CV2 - The string name of the second controlling variable.
    */
   void FindTableLimits(const std::string& name_CV1, const std::string& name_CV2);
 
   /*!
-   * \brief construct a list of all the edges and a list of the pair of elements left and right of the edge.
+   * \brief Construct a list of all the edges and a list of the pair of elements left and right of the edge.
    */
   void IdentifyUniqueEdges();
 
   /*!
-   * \brief read the lookup table from file and store the data.
+   * \brief Read the lookup table from file and store the data.
    * \param[in] file_name_lut - the filename of the lookup table.
    */
   void LoadTableRaw(const std::string& file_name_lut);
 
   /*!
-   * \brief compute vector of all (inverse) interpolation coefficients "interp_mat_inv_x_y" of all triangles.
+   * \brief Compute vector of all (inverse) interpolation coefficients "interp_mat_inv_x_y" of all triangles.
    */
   void ComputeInterpCoeffs();
 
   /*!
-   * \brief compute the inverse matrix for interpolation.
-   * \param[in] vec_CV1 - pointer to first coordinate (progress variable).
-   * \param[in] vec_CV2 - pointer to second coordinate (enthalpy).
-   * \param[in] point_ids - single triangle data.
-   * \param[out] interp_mat_inv - inverse matrix for interpolation.
+   * \brief Compute the inverse matrix for interpolation.
+   * \param[in] vec_CV1 - Pointer to first coordinate (progress variable).
+   * \param[in] vec_CV2 - Pointer to second coordinate (enthalpy).
+   * \param[in] point_ids - Single triangle data.
+   * \param[out] interp_mat_inv - Inverse matrix for interpolation.
    */
   void GetInterpMatInv(const su2double* vec_CV1, const su2double* vec_CV2, std::array<unsigned long, 3>& point_ids,
                        su2activematrix& interp_mat_inv);
 
   /*!
-   * \brief compute the interpolation coefficients for the triangular interpolation.
-   * \param[in] val_CV1 - value of first coordinate (progress variable).
-   * \param[in] val_CV2 - value of second coordinate (enthalpy).
-   * \param[in] interp_mat_inv - inverse matrix for interpolation.
-   * \param[out] interp_coeffs - interpolation coefficients.
+   * \brief Compute the interpolation coefficients for the triangular interpolation.
+   * \param[in] val_CV1 - Value of first coordinate (progress variable).
+   * \param[in] val_CV2 - Value of second coordinate (enthalpy).
+   * \param[in] interp_mat_inv - Inverse matrix for interpolation.
+   * \param[out] interp_coeffs - Interpolation coefficients.
    */
   void GetInterpCoeffs(su2double val_CV1, su2double val_CV2, su2activematrix& interp_mat_inv,
                        std::array<su2double, 3>& interp_coeffs);
 
   /*!
-   * \brief compute interpolated value of a point P in the triangle.
-   * \param[in] val_samples - pointer to the variable data.
+   * \brief Compute interpolated value of a point P in the triangle.
+   * \param[in] val_samples - Pointer to the variable data.
    * \param[in] val_triangle - ID to the triangle.
-   * \param[in] val_interp_coeffs - interpolation coefficients using the point data in P.
-   * \returns resulting value of the interpolation.
+   * \param[in] val_interp_coeffs - Interpolation coefficients using the point data in P.
+   * \returns Resulting value of the interpolation.
    */
   su2double Interpolate(const su2double* val_samples, std::array<unsigned long, 3>& val_triangle,
                         std::array<su2double, 3>& val_interp_coeffs);
 
   /*!
    * \brief Perform linear interpolation between two table levels for a single variable.
-   * \param[in] val_CV3 - value of the third controlling variable at the query point.
+   * \param[in] val_CV3 - Value of the third controlling variable at the query point.
    * \param[in] lower_level - Table level index of the table level directly below the query point.
    * \param[in] upper_level - Table level index of the table level directly above the query point.
    * \param[in] lower_value - Result from x-y interpolation on the lower table level.
@@ -195,7 +207,7 @@ class CLookUpTable {
 
   /*!
    * \brief Perform linear interpolation between two table levels for a vector of variables.
-   * \param[in] val_CV3 - value of the third controlling variable at the query point.
+   * \param[in] val_CV3 - Value of the third controlling variable at the query point.
    * \param[in] lower_level - Table level index of the table level directly below the query point.
    * \param[in] upper_level - Table level index of the table level directly above the query point.
    * \param[in] lower_values - Results from x-y interpolation on the lower table level.
@@ -207,52 +219,52 @@ class CLookUpTable {
                             std::vector<su2double*>& var_vals) const;
 
   /*!
-   * \brief find the point on the hull (boundary of the table) that is closest to the point P(val_CV1,val_CV2).
-   * \param[in] val_CV1 - first coordinate of point P(val_CV1,val_CV2) to check.
-   * \param[in] val_CV2 - second coordinate of point P(val_CV1,val_CV2) to check.
-   * \returns point id of the nearest neighbor on the hull.
+   * \brief Find the point on the hull (boundary of the table) that is closest to the point P(val_CV1,val_CV2).
+   * \param[in] val_CV1 - First coordinate of point P(val_CV1,val_CV2) to check.
+   * \param[in] val_CV2 - Second coordinate of point P(val_CV1,val_CV2) to check.
+   * \returns Point id of the nearest neighbor on the hull.
    */
   unsigned long FindNearestNeighborOnHull(su2double val_CV1, su2double val_CV2, unsigned long i_level = 0);
 
   /*!
    * \brief Interpolate data based on distance-weighted averaging on the nearest two table nodes.
-   * \param[in] val_CV1 - - first coordinate of point P(val_CV1,val_CV2) to check.
-   * \param[in] val_CV2 - second coordinate of point P(val_CV1,val_CV2) to check.
-   * \param[in] val_names_var - vector of string names of the variables to look up.
-   * \param[out] val_vars - pointer to the vector of stored values of the variables to look up.
+   * \param[in] val_CV1 - First coordinate of point P(val_CV1,val_CV2) to check.
+   * \param[in] val_CV2 - Second coordinate of point P(val_CV1,val_CV2) to check.
+   * \param[in] val_names_var - Vector of string names of the variables to look up.
+   * \param[out] val_vars - Pointer to the vector of stored values of the variables to look up.
    */
   void InterpolateToNearestNeighbors(const su2double val_CV1, const su2double val_CV2,
                                      const std::vector<std::string>& names_var, std::vector<su2double*>& var_vals,
                                      const unsigned long i_level = 0);
 
   /*!
-   * \brief Interpolate data based on distance-weighted averaging on the nearest two table nodes for a single variable
-   * \param[in] val_CV1 - - first coordinate of point P(val_CV1,val_CV2) to check.
-   * \param[in] val_CV2 - second coordinate of point P(val_CV1,val_CV2) to check.
-   * \param[in] name_var - variable name to look up.
-   * \param[out] var_val - pointer to the to be interpolated variable.
+   * \brief Interpolate data based on distance-weighted averaging on the nearest two table nodes for a single variable.
+   * \param[in] val_CV1 - First coordinate of point P(val_CV1,val_CV2) to check.
+   * \param[in] val_CV2 - Second coordinate of point P(val_CV1,val_CV2) to check.
+   * \param[in] name_var - Variable name to look up.
+   * \param[out] var_val - Pointer to the to be interpolated variable.
    */
   void InterpolateToNearestNeighbors(const su2double val_CV1, const su2double val_CV2, const std::string& name_var,
                                      su2double* var_val, const unsigned long i_level = 0);
 
   /*!
-   * \brief determine if a point P(val_CV1,val_CV2) is inside the triangle val_id_triangle.
-   * \param[in] val_CV1 - first coordinate of point P(val_CV1,val_CV2) to check.
-   * \param[in] val_CV2 - second coordinate of point P(val_CV1,val_CV2) to check.
+   * \brief Determine if a point P(val_CV1,val_CV2) is inside the triangle val_id_triangle.
+   * \param[in] val_CV1 - First coordinate of point P(val_CV1,val_CV2) to check.
+   * \param[in] val_CV2 - Second coordinate of point P(val_CV1,val_CV2) to check.
    * \param[in] val_id_triangle - ID of the triangle to check.
-   * \returns true if the point is in the triangle, false if it is outside.
+   * \returns True if the point is in the triangle, false if it is outside.
    */
   bool IsInTriangle(su2double val_CV1, su2double val_CV2, unsigned long val_id_triangle, unsigned long i_level = 0);
 
   /*!
-   * \brief compute the area of a triangle given the 3 points of the triangle.
-   * \param[in] x1 - the coordinates of the points P1(x1,y1), P2(x2,y2) and P3(x3,y3).
-   * \param[in] y1 - the coordinates of the points P1(x1,y1), P2(x2,y2) and P3(x3,y3).
-   * \param[in] x2 - the coordinates of the points P1(x1,y1), P2(x2,y2) and P3(x3,y3).
-   * \param[in] y2 - the coordinates of the points P1(x1,y1), P2(x2,y2) and P3(x3,y3).
-   * \param[in] x3 - the coordinates of the points P1(x1,y1), P2(x2,y2) and P3(x3,y3).
-   * \param[in] y3 - the coordinates of the points P1(x1,y1), P2(x2,y2) and P3(x3,y3).
-   * \returns the absolute value of the area of the triangle.
+   * \brief Compute the area of a triangle given the 3 points of the triangle.
+   * \param[in] x1 - The coordinates of the points P1(x1,y1), P2(x2,y2) and P3(x3,y3).
+   * \param[in] y1 - The coordinates of the points P1(x1,y1), P2(x2,y2) and P3(x3,y3).
+   * \param[in] x2 - The coordinates of the points P1(x1,y1), P2(x2,y2) and P3(x3,y3).
+   * \param[in] y2 - The coordinates of the points P1(x1,y1), P2(x2,y2) and P3(x3,y3).
+   * \param[in] x3 - The coordinates of the points P1(x1,y1), P2(x2,y2) and P3(x3,y3).
+   * \param[in] y3 - The coordinates of the points P1(x1,y1), P2(x2,y2) and P3(x3,y3).
+   * \returns The absolute value of the area of the triangle.
    */
   inline su2double TriArea(su2double x1, su2double y1, su2double x2, su2double y2, su2double x3, su2double y3) {
     return abs((x1 * (y2 - y3) + x2 * (y3 - y1) + x3 * (y1 - y2)) * 0.5);
@@ -261,10 +273,10 @@ class CLookUpTable {
   /*!
    * \brief Compute the values of the first and second controlling variable based on normalized query coordinates
    * \param[in] inclusion_levels - Pair containing lower(first) and upper(second) table inclusion level indices.
-   * \param[in] val_CV1 - first controlling variable value.
-   * \param[in] val_CV2 - second controlling variable value.
-   * \param[in] val_CV3 - third controlling variable value.
-   * \returns array with first and second controlling variable values for the upper and lower table inclusion levels.
+   * \param[in] val_CV1 - First controlling variable value.
+   * \param[in] val_CV2 - Second controlling variable value.
+   * \param[in] val_CV3 - Third controlling variable value.
+   * \returns Array with first and second controlling variable values for the upper and lower table inclusion levels.
    */
   std::array<std::array<su2double, 2>, 2> ComputeNormalizedXY(std::pair<unsigned long, unsigned long>& inclusion_levels,
                                                               const su2double val_CV1, const su2double val_CV2,
@@ -274,60 +286,63 @@ class CLookUpTable {
   CLookUpTable(const std::string& file_name_lut, std::string name_CV1_in, std::string name_CV2_in);
 
   /*!
-   * \brief print information to screen.
+   * \brief Print information to screen.
    */
   void PrintTableInfo();
 
   /*!
-   * \brief lookup 1 value of the single variable "val_name_var" using controlling variable values(val_CV1,val_CV2).
-   * \param[in] val_name_var - string name of the variable to look up.
-   * \param[out] val_var - the stored value of the variable to look up.
-   * \param[in] val_CV1 - value of controlling variable 1.
-   * \param[in] val_CV2 - value of controlling variable 2.
+   * \brief Lookup 1 value of the single variable "val_name_var" using controlling variable values(val_CV1,val_CV2).
+   * \param[in] val_name_var - String name of the variable to look up.
+   * \param[out] val_var - The stored value of the variable to look up.
+   * \param[in] val_CV1 - Value of controlling variable 1.
+   * \param[in] val_CV2 - Value of controlling variable 2.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
   unsigned long LookUp_XY(const std::string& val_name_var, su2double* val_var, su2double val_CV1, su2double val_CV2,
                           unsigned long i_level = 0);
 
   /*!
-   * \brief lookup 1 value for each of the variables in "val_name_var" using controlling variable
-   * values(val_CV1,val_CV2). \param[in] val_names_var - vector of string names of the variables to look up. \param[out]
-   * val_vars - pointer to the vector of stored values of the variables to look up. \param[in] val_CV1 - value of
-   * controlling variable 1. \param[in] val_CV2 - value of controlling variable 2. \returns 1 if the lookup and
-   * subsequent interpolation was a success, 0 if not.
+   * \brief Lookup 1 value for each of the variables in "val_name_var" using controlling variable
+   * values(val_CV1,val_CV2).
+   * \param[in] val_names_var - vector of string names of the variables to look up.
+   * \param[out] val_vars - pointer to the vector of stored values of the variables to look up.
+   * \param[in] val_CV1 - value of controlling variable 1.
+   * \param[in] val_CV2 - value of controlling variable 2.
+   * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
   unsigned long LookUp_XY(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars,
                           su2double val_CV1, su2double val_CV2, unsigned long i_level = 0);
 
   /*!
-   * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_CV1,val_CV2).
-   * \param[in] val_name_var - string name of the variable to look up.
-   * \param[out] val_var - the stored value of the variable to look up.
-   * \param[in] val_CV1 - value of controlling variable 1.
-   * \param[in] val_CV2 - value of controlling variable 2.
+   * \brief Lookup the value of the variable "val_name_var" using controlling variable values(val_CV1,val_CV2).
+   * \param[in] val_name_var - String name of the variable to look up.
+   * \param[out] val_var - The stored value of the variable to look up.
+   * \param[in] val_CV1 - Value of controlling variable 1.
+   * \param[in] val_CV2 - Value of controlling variable 2.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
   unsigned long LookUp_XY(const std::vector<std::string>& val_names_var, std::vector<su2double>& val_vars,
                           su2double val_CV1, su2double val_CV2, unsigned long i_level = 0);
+
   /*!
-   * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_CV1,val_CV2,val_z).
-   * \param[in] val_name_var - string name of the variable to look up.
-   * \param[out] val_var - the stored value of the variable to look up.
-   * \param[in] val_CV1 - value of controlling variable 1.
-   * \param[in] val_CV2 - value of controlling variable 2.
-   * \param[in] val_CV3 - value of controlling variable 3.
+   * \brief Lookup the value of the variable "val_name_var" using controlling variable values(val_CV1,val_CV2,val_z).
+   * \param[in] val_name_var - String name of the variable to look up.
+   * \param[out] val_var - The stored value of the variable to look up.
+   * \param[in] val_CV1 - Value of controlling variable 1.
+   * \param[in] val_CV2 - Value of controlling variable 2.
+   * \param[in] val_CV3 - Value of controlling variable 3.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
   unsigned long LookUp_XYZ(const std::string& val_name_var, su2double* val_var, su2double val_CV1, su2double val_CV2,
                            su2double val_CV3);
 
   /*!
-   * \brief lookup the value of the variable "val_name_var" using controlling variable values(val_CV1,val_CV2,val_z).
-   * \param[in] val_name_var - string name of the variable to look up.
-   * \param[out] val_var - the stored value of the variable to look up.
-   * \param[in] val_CV1 - value of controlling variable 1.
-   * \param[in] val_CV2 - value of controlling variable 2.
-   * \param[in] val_CV3 - value of controlling variable 3.
+   * \brief Lookup the value of the variable "val_name_var" using controlling variable values(val_CV1,val_CV2,val_z).
+   * \param[in] val_name_var - String name of the variable to look up.
+   * \param[out] val_var - The stored value of the variable to look up.
+   * \param[in] val_CV1 - Value of controlling variable 1.
+   * \param[in] val_CV2 - Value of controlling variable 2.
+   * \param[in] val_CV3 - Value of controlling variable 3.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
   unsigned long LookUp_XYZ(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars,
@@ -335,23 +350,23 @@ class CLookUpTable {
 
   /*!
    * \brief Find the table levels with constant z-values directly above and below query val_z.
-   * \param[in] val_CV3 - value of controlling variable 3.
+   * \param[in] val_CV3 - Value of controlling variable 3.
    * \param[in] within_limits - Whether query point lies within table bounds.
-   * \returns pair of inclusion level indices (first = lower level index, second = upper level index)
+   * \returns Pair of inclusion level indices (first = lower level index, second = upper level index).
    */
   std::pair<unsigned long, unsigned long> FindInclusionLevels(const su2double val_CV3);
 
   /*!
-   * \brief determine the minimum and maximum value of the second controlling variable.
-   * \returns pair of minimum and maximum value of controlling variable 2.
+   * \brief Determine the minimum and maximum value of the second controlling variable.
+   * \returns Pair of minimum and maximum value of controlling variable 2.
    */
   inline std::pair<su2double*, su2double*> GetTableLimitsY(unsigned long i_level = 0) const {
     return limits_table_y[i_level];
   }
 
   /*!
-   * \brief determine the minimum and maximum value of the first controlling variable.
-   * \returns pair of minimum and maximum value of controlling variable 1.
+   * \brief Determine the minimum and maximum value of the first controlling variable.
+   * \returns Pair of minimum and maximum value of controlling variable 1.
    */
   inline std::pair<su2double*, su2double*> GetTableLimitsX(unsigned long i_level = 0) const {
     return limits_table_x[i_level];
diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index d8a6e4dd69e..ea657b43afd 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -472,28 +472,24 @@ enum RUNTIME_TYPE {
   RUNTIME_ADJSPECIES_SYS = 26,/*!< \brief One-physics case, the code is solving the adjoint species model. */
 };
 
-const int FLOW_SOL = 0;     /*!< \brief Position of the mean flow solution in the solver container array. */
-const int ADJFLOW_SOL = 1;  /*!< \brief Position of the continuous adjoint flow solution in the solver container array. */
-
-const int TURB_SOL = 2;     /*!< \brief Position of the turbulence model solution in the solver container array. */
-const int ADJTURB_SOL = 3;  /*!< \brief Position of the continuous adjoint turbulence solution in the solver container array. */
-
-const int TRANS_SOL = 4;    /*!< \brief Position of the transition model solution in the solver container array. */
-const int HEAT_SOL = 5;     /*!< \brief Position of the heat equation in the solution solver array. */
-const int ADJHEAT_SOL = 6;  /*!< \brief Position of the adjoint heat equation in the solution solver array. */
-const int RAD_SOL = 7;      /*!< \brief Position of the radiation equation in the solution solver array. */
-const int ADJRAD_SOL = 8;   /*!< \brief Position of the continuous adjoint turbulence solution in the solver container array. */
-
-const int MESH_SOL = 9;      /*!< \brief Position of the mesh solver. */
-const int ADJMESH_SOL = 10;   /*!< \brief Position of the adjoint of the mesh solver. */
-
-const int SPECIES_SOL = 11;    /*!< \brief Position of the species solver. */
-const int ADJSPECIES_SOL = 12; /*!< \brief Position of the adjoint of the species solver. */
-
-const int FEA_SOL = 0;      /*!< \brief Position of the FEA equation in the solution solver array. */
-const int ADJFEA_SOL = 1;   /*!< \brief Position of the FEA adjoint equation in the solution solver array. */
-
-const int TEMPLATE_SOL = 0; /*!< \brief Position of the template solution. */
+ enum SOLVER_TYPE : const int {
+   FLOW_SOL=0,       /*!< \brief Position of the mean flow solution in the solver container array. */
+   ADJFLOW_SOL=1,    /*!< \brief Position of the continuous adjoint flow solution in the solver container array. */
+   TURB_SOL=2,       /*!< \brief Position of the turbulence model solution in the solver container array. */
+   ADJTURB_SOL=3,    /*!< \brief Position of the continuous adjoint turbulence solution in the solver container array. */
+   TRANS_SOL=4,      /*!< \brief Position of the transition model solution in the solver container array. */
+   HEAT_SOL=5,       /*!< \brief Position of the heat equation in the solution solver array. */
+   ADJHEAT_SOL=6,    /*!< \brief Position of the adjoint heat equation in the solution solver array. */
+   RAD_SOL=7,        /*!< \brief Position of the radiation equation in the solution solver array. */
+   ADJRAD_SOL=8,     /*!< \brief Position of the continuous adjoint turbulence solution in the solver container array. */
+   MESH_SOL=9,       /*!< \brief Position of the mesh solver. */
+   ADJMESH_SOL=10,    /*!< \brief Position of the adjoint of the mesh solver. */
+   SPECIES_SOL=11,    /*!< \brief Position of the species solver. */
+   ADJSPECIES_SOL=12, /*!< \brief Position of the adjoint of the species solver. */
+   FEA_SOL=0,        /*!< \brief Position of the Finite Element flow solution in the solver container array. */
+   ADJFEA_SOL=1,     /*!< \brief Position of the continuous adjoint Finite Element flow solution in the solver container array. */
+   TEMPLATE_SOL=0,   /*!< \brief Position of the template solution. */
+ };
 
 const int CONV_TERM = 0;           /*!< \brief Position of the convective terms in the numerics container array. */
 const int VISC_TERM = 1;           /*!< \brief Position of the viscous terms in the numerics container array. */
@@ -551,6 +547,7 @@ enum ENUM_FLUIDMODEL {
   SU2_NONEQ = 8,          /*!< \brief User defined gas model for nonequilibrium flow. */
   FLUID_MIXTURE = 9,      /*!< \brief Species mixture model. */
   COOLPROP = 10,          /*!< \brief Thermodynamics library. */
+  FLUID_FLAMELET = 11,    /*!< \brief lookup table (LUT) method for premixed flamelets. */
 };
 static const MapType<std::string, ENUM_FLUIDMODEL> FluidModel_Map = {
   MakePair("STANDARD_AIR", STANDARD_AIR)
@@ -564,6 +561,7 @@ static const MapType<std::string, ENUM_FLUIDMODEL> FluidModel_Map = {
   MakePair("SU2_NONEQ", SU2_NONEQ)
   MakePair("FLUID_MIXTURE", FLUID_MIXTURE)
   MakePair("COOLPROP", COOLPROP)
+  MakePair("FLUID_FLAMELET", FLUID_FLAMELET)
 };
 
 /*!
@@ -653,12 +651,14 @@ enum class VISCOSITYMODEL {
   CONSTANT, /*!< \brief Constant viscosity. */
   SUTHERLAND, /*!< \brief Sutherlands Law viscosity. */
   POLYNOMIAL, /*!< \brief Polynomial viscosity. */
+  FLAMELET, /*!< \brief LUT method for flamelets */
   COOLPROP, /*!< \brief CoolProp viscosity. */
 };
 static const MapType<std::string, VISCOSITYMODEL> ViscosityModel_Map = {
   MakePair("CONSTANT_VISCOSITY", VISCOSITYMODEL::CONSTANT)
   MakePair("SUTHERLAND", VISCOSITYMODEL::SUTHERLAND)
   MakePair("POLYNOMIAL_VISCOSITY", VISCOSITYMODEL::POLYNOMIAL)
+  MakePair("FLAMELET", VISCOSITYMODEL::FLAMELET)
   MakePair("COOLPROP", VISCOSITYMODEL::COOLPROP)
 };
 
@@ -681,12 +681,14 @@ enum class CONDUCTIVITYMODEL {
   CONSTANT, /*!< \brief Constant thermal conductivity. */
   CONSTANT_PRANDTL, /*!< \brief Constant Prandtl number. */
   POLYNOMIAL, /*!< \brief Polynomial thermal conductivity. */
+  FLAMELET, /*!< \brief LUT method for flamelets */
   COOLPROP, /*!< \brief COOLPROP thermal conductivity. */
 };
 static const MapType<std::string, CONDUCTIVITYMODEL> ConductivityModel_Map = {
   MakePair("CONSTANT_CONDUCTIVITY", CONDUCTIVITYMODEL::CONSTANT)
   MakePair("CONSTANT_PRANDTL", CONDUCTIVITYMODEL::CONSTANT_PRANDTL)
   MakePair("POLYNOMIAL_CONDUCTIVITY", CONDUCTIVITYMODEL::POLYNOMIAL)
+  MakePair("FLAMELET", CONDUCTIVITYMODEL::FLAMELET)
   MakePair("COOLPROP", CONDUCTIVITYMODEL::COOLPROP)
 };
 
@@ -710,6 +712,7 @@ enum class DIFFUSIVITYMODEL {
   CONSTANT_SCHMIDT,     /*!< \brief Constant Schmidt number for mass diffusion in scalar transport. */
   UNITY_LEWIS,          /*!< \brief Unity Lewis model for mass diffusion in scalar transport. */
   CONSTANT_LEWIS,      /*!< \brief Different Lewis number model for mass diffusion in scalar transport. */
+  FLAMELET,            /*!< \brief flamelet model for tabulated chemistry, diffusivity from lookup table */
 };
 
 static const MapType<std::string, DIFFUSIVITYMODEL> Diffusivity_Model_Map = {
@@ -717,6 +720,7 @@ static const MapType<std::string, DIFFUSIVITYMODEL> Diffusivity_Model_Map = {
   MakePair("CONSTANT_SCHMIDT", DIFFUSIVITYMODEL::CONSTANT_SCHMIDT)
   MakePair("UNITY_LEWIS", DIFFUSIVITYMODEL::UNITY_LEWIS)
   MakePair("CONSTANT_LEWIS", DIFFUSIVITYMODEL::CONSTANT_LEWIS)
+  MakePair("FLAMELET", DIFFUSIVITYMODEL::FLAMELET)
 };
 
 /*!
@@ -1287,11 +1291,29 @@ inline LM_ParsedOptions ParseLMOptions(const LM_OPTIONS *LM_Options, unsigned sh
  */
 enum class SPECIES_MODEL {
   NONE,              /*!< \brief No scalar transport model. */
-  SPECIES_TRANSPORT,    /*!< \brief Passive scalar transport model. */
+  SPECIES_TRANSPORT,    /*!< \brief species transport model. */
+  FLAMELET,          /*!< \brief flamelet model. */
 };
 static const MapType<std::string, SPECIES_MODEL> Species_Model_Map = {
   MakePair("NONE", SPECIES_MODEL::NONE)
   MakePair("SPECIES_TRANSPORT", SPECIES_MODEL::SPECIES_TRANSPORT)
+  MakePair("FLAMELET", SPECIES_MODEL::FLAMELET)
+};
+
+/*!
+ * \brief Progress variable and enthalpy are the first and second entries in the lookup table.
+ * \note The order matters.
+ */
+enum FLAMELET_SCALAR_VARIABLES {
+  I_PROGVAR,
+  I_ENTH,
+};
+
+/*!
+ * \brief the source terms for the flamelet method. At the moment only progress variable
+ */
+enum FLAMELET_SCALAR_SOURCES {
+  I_SRC_TOT_PROGVAR
 };
 
 /*!
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index e705b7f38d4..ace96e28cbb 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -837,6 +837,7 @@ void CConfig::SetPointersNull() {
   Marker_Designing            = nullptr;   Marker_GeoEval           = nullptr;    Marker_Plotting   = nullptr;
   Marker_Analyze              = nullptr;   Marker_PyCustom          = nullptr;    Marker_WallFunctions        = nullptr;
   Marker_CfgFile_KindBC       = nullptr;   Marker_All_KindBC        = nullptr;    Marker_SobolevBC  = nullptr;
+  Marker_StrongBC             = nullptr;
 
   Kind_WallFunctions       = nullptr;
   IntInfo_WallFunctions    = nullptr;
@@ -1351,8 +1352,15 @@ void CConfig::SetConfig_Options() {
   addDoubleListOption("SPECIES_CLIPPING_MAX", nSpecies_Clipping_Max, Species_Clipping_Max);
   /*!\brief SPECIES_CLIPPING_MIN \n DESCRIPTION: Minimum values for scalar clipping \ingroup Config*/
   addDoubleListOption("SPECIES_CLIPPING_MIN", nSpecies_Clipping_Min, Species_Clipping_Min);
-  /*!\brief SPECIES_CLIPPING \n DESCRIPTION: Use strong inlet and outlet BC in the species solver \n DEFAULT: false \ingroup Config*/
-  addBoolOption("SPECIES_USE_STRONG_BC", Species_StrongBC, false);
+
+  /*!\brief FLAME_INIT \n DESCRIPTION: flame initialization using the flamelet model \ingroup Config*/
+  /*--- flame offset (x,y,z) ---*/
+  flame_init[0] = 0.0; flame_init[1] = 0.0; flame_init[2] = 0.0;
+  /*--- flame normal (nx, ny, nz) ---*/
+  flame_init[3] = 1.0; flame_init[4] = 0.0; flame_init[5] = 0.0;
+  /*--- flame thickness (x) and flame burnt thickness (after this thickness, we have unburnt conditions again)  ---*/
+  flame_init[6] = 0.5e-3; flame_init[7] = 1.0;
+  addDoubleArrayOption("FLAME_INIT", 8,flame_init);
 
   /*--- Options related to mass diffusivity and thereby the species solver. ---*/
 
@@ -1496,6 +1504,9 @@ void CConfig::SetConfig_Options() {
   addWallFunctionOption("MARKER_WALL_FUNCTIONS", nMarker_WallFunctions, Marker_WallFunctions,
                         Kind_WallFunctions, IntInfo_WallFunctions, DoubleInfo_WallFunctions);
 
+  /*!\brief MARKER_STRONG_BC\n DESCRIPTION: Markers where a strong BC must be applied.*/
+  addStringListOption("MARKER_SPECIES_STRONG_BC", nMarker_StrongBC, Marker_StrongBC);
+
   /*!\brief ACTDISK_TYPE  \n DESCRIPTION: Actuator Disk boundary type \n OPTIONS: see \link ActDisk_Map \endlink \n Default: VARIABLES_JUMP \ingroup Config*/
   addEnumOption("ACTDISK_TYPE", Kind_ActDisk, ActDisk_Map, VARIABLES_JUMP);
 
@@ -2082,6 +2093,18 @@ void CConfig::SetConfig_Options() {
   /* DESCRIPTION: Determine if we need to allocate memory to store the multizone residual. \n DEFAULT: true (temporarily) */
   addBoolOption("MULTIZONE_RESIDUAL", Multizone_Residual, false);
 
+  /*!\brief File name of the flamelet look up table.*/
+  addStringOption("FILENAME_LUT", file_name_lut, string("LUT"));
+
+  /* DESCRIPTION: Names of the passive lookup variables for flamelet LUT */
+  addStringListOption("LOOKUP_NAMES", n_lookups, table_lookup_names);
+
+  /* DESCRIPTION: Names of the user transport equations solved in the flamelet problem. */
+  addStringListOption("USER_SCALAR_NAMES", n_user_scalars, user_scalar_names);
+
+  /* DESCRIPTION: Names of the user scalar source terms. */
+  addStringListOption("USER_SOURCE_NAMES", n_user_sources, user_source_names);
+
   /*!\brief CONV_FILENAME \n DESCRIPTION: Output file convergence history (w/o extension) \n DEFAULT: history \ingroup Config*/
   addStringOption("CONV_FILENAME", Conv_FileName, string("history"));
   /*!\brief BREAKDOWN_FILENAME \n DESCRIPTION: Output file forces breakdown \ingroup Config*/
@@ -2987,6 +3010,8 @@ void CConfig::SetConfig_Parsing(istream& config_buffer){
             newString.append("DYN_TIME is deprecated. Use MAX_TIME instead.\n\n");
           else if (!option_name.compare("DYNAMIC_ANALYSIS"))
             newString.append("DYNAMIC_ANALYSIS is deprecated. Use TIME_DOMAIN instead.\n\n");
+          else if (!option_name.compare("SPECIES_USE_STRONG_BC"))
+            newString.append("SPECIES_USE_STRONG_BC is deprecated. Use MARKER_SPECIES_STRONG_BC= (marker1, ...) instead.\n\n");
           else {
             /*--- Find the most likely candidate for the unrecognized option, based on the length
              of start and end character sequences shared by candidates and the option. ---*/
@@ -3297,6 +3322,7 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
                     (Kind_FluidModel == IDEAL_GAS) ||
                     (Kind_FluidModel == INC_IDEAL_GAS) ||
                     (Kind_FluidModel == FLUID_MIXTURE) ||
+                    (Kind_FluidModel == FLUID_FLAMELET) ||
                     (Kind_FluidModel == INC_IDEAL_GAS_POLY) ||
                     (Kind_FluidModel == CONSTANT_DENSITY));
   bool noneq_gas = ((Kind_FluidModel == MUTATIONPP) ||
@@ -3644,9 +3670,11 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
     }
   }
 
-  if (Kind_ObjFunc[0] == CUSTOM_OBJFUNC && CustomObjFunc.empty() && !Multizone_Problem) {
-    SU2_MPI::Error("The expression for the custom objective function was not set.\n"
-                   "For example, CUSTOM_OBJFUNC= LIFT/DRAG", CURRENT_FUNCTION);
+  if (nObj > 0){
+    if (Kind_ObjFunc[0] == CUSTOM_OBJFUNC && CustomObjFunc.empty() && !Multizone_Problem) {
+      SU2_MPI::Error("The expression for the custom objective function was not set.\n"
+                    "For example, CUSTOM_OBJFUNC= LIFT/DRAG", CURRENT_FUNCTION);
+    }
   }
 
   /*--- Check for unsteady problem ---*/
@@ -3845,7 +3873,7 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
           }
           break;
         default:
-          if (nSpecies_Init + 1 != 1) SU2_MPI::Error("Viscosity model not available.", CURRENT_FUNCTION);
+          if (nSpecies_Init + 1 != 1) SU2_MPI::Error("Fluid mixture: viscosity model not available.", CURRENT_FUNCTION);
           break;
       }
 
@@ -3892,6 +3920,35 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
       }
     }
 
+
+    if (Kind_Species_Model == SPECIES_MODEL::FLAMELET) {
+
+      if (Kind_FluidModel != FLUID_FLAMELET) {
+        SU2_MPI::Error("The use of SCALAR_MODEL= FLAMELET requires the FLUID_MODEL option to be FLUID_FLAMELET",
+                       CURRENT_FUNCTION);
+      }
+
+      if (Kind_DensityModel != INC_DENSITYMODEL::VARIABLE) {
+        SU2_MPI::Error("The use of FLUID_FLAMELET requires the INC_DENSITY_MODEL option to be VARIABLE",
+                       CURRENT_FUNCTION);
+      }
+
+      if (Kind_ConductivityModel != CONDUCTIVITYMODEL::FLAMELET) {
+        SU2_MPI::Error("The use of FLUID_FLAMELET requires the CONDUCTIVITY_MODEL option to be FLAMELET",
+                       CURRENT_FUNCTION);
+      }
+
+      if (Kind_Diffusivity_Model != DIFFUSIVITYMODEL::FLAMELET) {
+        SU2_MPI::Error("The use of FLUID_FLAMELET requires the DIFFUSIVITY_MODEL option to be FLAMELET",
+                       CURRENT_FUNCTION);
+      }
+
+      if (Kind_ViscosityModel != VISCOSITYMODEL::FLAMELET) {
+        SU2_MPI::Error("The use of FLUID_FLAMELET requires the VISCOSITY_MODEL option to be FLAMELET",
+                       CURRENT_FUNCTION);
+      }
+    }
+
     /*--- Check for Measurement System ---*/
 
     if (SystemMeasurements == US && !standard_air) {
@@ -4859,9 +4916,9 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
       Kind_FluidModel = CONSTANT_DENSITY;
   }
 
-  /*--- Energy equation must be active for any fluid models other than constant density. ---*/
-
   if ((Kind_DensityModel != INC_DENSITYMODEL::CONSTANT) && (Kind_Species_Model==SPECIES_MODEL::NONE)) Energy_Equation = true;
+  /*--- For the flamelet combustion model, energy equation is a passive field, we lookup T and write it to the field ---*/
+  if (Kind_Species_Model == SPECIES_MODEL::FLAMELET ) Energy_Equation = false;
 
   if (Kind_DensityModel == INC_DENSITYMODEL::BOUSSINESQ) {
     Energy_Equation = true;
@@ -4871,7 +4928,7 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
   }
 
   if (Kind_DensityModel == INC_DENSITYMODEL::VARIABLE) {
-    if (Kind_FluidModel != INC_IDEAL_GAS && Kind_FluidModel != INC_IDEAL_GAS_POLY && Kind_FluidModel != FLUID_MIXTURE) {
+    if (Kind_FluidModel != INC_IDEAL_GAS && Kind_FluidModel != INC_IDEAL_GAS_POLY && Kind_FluidModel != FLUID_MIXTURE && Kind_FluidModel != FLUID_FLAMELET) {
       SU2_MPI::Error("Variable density incompressible solver limited to ideal gases.\n Check the fluid model options (use INC_IDEAL_GAS, INC_IDEAL_GAS_POLY).", CURRENT_FUNCTION);
     }
   }
@@ -5313,7 +5370,7 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
         CURRENT_FUNCTION);
 
   /*--- Checks for additional species transport. ---*/
-  if (Kind_Species_Model == SPECIES_MODEL::SPECIES_TRANSPORT) {
+  if ((Kind_Species_Model == SPECIES_MODEL::SPECIES_TRANSPORT) || (Kind_Species_Model == SPECIES_MODEL::FLAMELET)) {
     if (Kind_Solver != MAIN_SOLVER::INC_NAVIER_STOKES &&
         Kind_Solver != MAIN_SOLVER::INC_RANS &&
         Kind_Solver != MAIN_SOLVER::DISC_ADJ_INC_NAVIER_STOKES &&
@@ -5383,24 +5440,35 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
     nSpecies = nSpecies_Init;
 
     /*--- Check whether some variables (or their sums) are in physical bounds. [0,1] for species related quantities. ---*/
-    su2double Species_Init_Sum = 0.0;
-    for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
-      checkScalarBounds(Species_Init[iSpecies], "SPECIES_INIT individual", 0.0, 1.0);
-      Species_Init_Sum += Species_Init[iSpecies];
-    }
-    checkScalarBounds(Species_Init_Sum, "SPECIES_INIT sum", 0.0, 1.0);
-
-    for (unsigned short iMarker = 0; iMarker < nMarker_Inlet_Species; iMarker++) {
-      su2double Inlet_SpeciesVal_Sum = 0.0;
+    /*--- Note, only for species transport, not for flamelet model ---*/
+    if (Kind_Species_Model == SPECIES_MODEL::SPECIES_TRANSPORT) {
+      su2double Species_Init_Sum = 0.0;
       for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
-        checkScalarBounds(Inlet_SpeciesVal[iMarker][iSpecies], "MARKER_INLET_SPECIES individual", 0.0, 1.0);
-        Inlet_SpeciesVal_Sum += Inlet_SpeciesVal[iMarker][iSpecies];
+        checkScalarBounds(Species_Init[iSpecies], "SPECIES_INIT individual", 0.0, 1.0);
+        Species_Init_Sum += Species_Init[iSpecies];
+      }
+      checkScalarBounds(Species_Init_Sum, "SPECIES_INIT sum", 0.0, 1.0);
+
+      for (iMarker = 0; iMarker < nMarker_Inlet_Species; iMarker++) {
+        su2double Inlet_SpeciesVal_Sum = 0.0;
+        for (unsigned short iSpecies = 0; iSpecies < nSpecies; iSpecies++) {
+          checkScalarBounds(Inlet_SpeciesVal[iMarker][iSpecies], "MARKER_INLET_SPECIES individual", 0.0, 1.0);
+          Inlet_SpeciesVal_Sum += Inlet_SpeciesVal[iMarker][iSpecies];
+        }
+        checkScalarBounds(Inlet_SpeciesVal_Sum, "MARKER_INLET_SPECIES sum", 0.0, 1.0);
       }
-      checkScalarBounds(Inlet_SpeciesVal_Sum, "MARKER_INLET_SPECIES sum", 0.0, 1.0);
     }
 
   } // species transport checks
 
+  /*--- Define some variables for flamelet model. ---*/
+  if (Kind_Species_Model == SPECIES_MODEL::FLAMELET) {
+    /*--- The controlling variables are progress variable and total enthalpy ---*/
+    n_control_vars = 2;
+    /*--- We can have additional user defined transported scalars ---*/
+    n_scalars = n_control_vars + n_user_scalars;
+  }
+
   if (Kind_Regime == ENUM_REGIME::COMPRESSIBLE && GetBounded_Scalar()) {
     SU2_MPI::Error("BOUNDED_SCALAR discretization can only be used for incompressible problems.", CURRENT_FUNCTION);
   }
@@ -5946,7 +6014,7 @@ void CConfig::SetOutput(SU2_COMPONENT val_software, unsigned short val_izone) {
   iMarker_Designing, iMarker_GeoEval, iMarker_Plotting, iMarker_Analyze, iMarker_DV, iDV_Value,
   iMarker_ZoneInterface, iMarker_PyCustom, iMarker_Load_Dir, iMarker_Disp_Dir, iMarker_Load_Sine, iMarker_Clamped,
   iMarker_Moving, iMarker_Supersonic_Inlet, iMarker_Supersonic_Outlet, iMarker_ActDiskInlet,
-  iMarker_Emissivity,
+  iMarker_Emissivity, iMarker_StrongBC,
   iMarker_ActDiskOutlet, iMarker_MixingPlaneInterface,
   iMarker_SobolevBC;
 
@@ -7458,6 +7526,15 @@ void CConfig::SetOutput(SU2_COMPONENT val_software, unsigned short val_izone) {
     BoundaryTable.PrintFooter();
   }
 
+  if (nMarker_StrongBC != 0) {
+    BoundaryTable << "Strong boundary";
+    for (iMarker_StrongBC = 0; iMarker_StrongBC < nMarker_StrongBC; iMarker_StrongBC++) {
+      BoundaryTable << Marker_StrongBC[iMarker_StrongBC];
+      if (iMarker_StrongBC < nMarker_StrongBC-1)  BoundaryTable << " ";
+    }
+    BoundaryTable.PrintFooter();
+  }
+
   if (nMarker_Custom != 0) {
     BoundaryTable << "Custom boundary";
     for (iMarker_Custom = 0; iMarker_Custom < nMarker_Custom; iMarker_Custom++) {
@@ -9493,6 +9570,15 @@ su2double CConfig::GetWall_Emissivity(const string& val_marker) const {
   return Wall_Emissivity[iMarker_Emissivity];
 }
 
+bool CConfig::GetMarker_StrongBC(const string& val_marker) const {
+
+  unsigned short iMarker_StrongBC = 0;
+
+  for (iMarker_StrongBC = 0; iMarker_StrongBC < nMarker_StrongBC; iMarker_StrongBC++)
+    if (Marker_StrongBC[iMarker_StrongBC] == val_marker) return true;
+
+  return false;
+}
 su2double CConfig::GetFlowLoad_Value(const string& val_marker) const {
   unsigned short iMarker_FlowLoad;
   for (iMarker_FlowLoad = 0; iMarker_FlowLoad < nMarker_FlowLoad; iMarker_FlowLoad++)
diff --git a/Common/src/containers/CFileReaderLUT.cpp b/Common/src/containers/CFileReaderLUT.cpp
index d71f4e9ee3a..31bb8de3338 100644
--- a/Common/src/containers/CFileReaderLUT.cpp
+++ b/Common/src/containers/CFileReaderLUT.cpp
@@ -1,5 +1,5 @@
 /*!
- * \file CFileReaderLUT.hpp
+ * \file CFileReaderLUT.cpp
  * \brief reading lookup table for tabulated fluid properties
  * \author D. Mayer, T. Economon
  * \version 7.5.1 "Blackbird"
diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index 130f53bfc18..d13feb6b82c 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -92,15 +92,14 @@ CLookUpTable::CLookUpTable(const string& var_file_name_lut, string name_CV1_in,
   if (rank == MASTER_NODE) {
     switch (table_dim) {
       case 2:
-        cout << "Construction of trapezoidal map took " << stopTime - startTime << " seconds\n" << endl;
+        cout << "\nConstruction of trapezoidal map took " << stopTime - startTime << " seconds\n" << endl;
         break;
       case 3:
-        cout << "Construction of trapezoidal map stack took " << stopTime - startTime << " seconds\n" << endl;
+        cout << "\nConstruction of trapezoidal map stack took " << stopTime - startTime << " seconds\n" << endl;
         break;
       default:
         break;
     }
-    cout << "Precomputing interpolation coefficients..." << endl;
   }
 
   ComputeInterpCoeffs();
@@ -576,7 +575,7 @@ unsigned long CLookUpTable::LookUp_XY(const string& val_name_var, su2double* val
                                       su2double val_CV2, unsigned long i_level) {
   unsigned long exit_code = 1;
 
-  if (val_name_var.compare("NULL") == 0) {
+  if (noSource(val_name_var)) {
     *val_var = 0.0;
     exit_code = 0;
     return exit_code;
@@ -645,18 +644,19 @@ unsigned long CLookUpTable::LookUp_XY(const vector<string>& val_names_var, vecto
   }
 
   /* loop over variable names and interpolate / get values */
-  if (exit_code == 0) {
-    for (long unsigned int i_var = 0; i_var < val_names_var.size(); ++i_var) {
-      if (val_names_var[i_var].compare("NULL") == 0) {
-        *val_vars[i_var] = 0.0;
-      } else {
+  for (long unsigned int i_var = 0; i_var < val_names_var.size(); ++i_var) {
+    if (noSource(val_names_var[i_var])) {
+      *val_vars[i_var] = 0.0;
+      exit_code = 0;
+    } else {
+      if (exit_code == 0) {
         /* first, copy the single triangle from the large triangle list*/
         for (int p = 0; p < 3; p++) triangle[p] = triangles[i_level][id_triangle][p];
         *val_vars[i_var] = Interpolate(GetDataP(val_names_var[i_var], i_level), triangle, interp_coeffs);
+      } else {
+        InterpolateToNearestNeighbors(val_CV1, val_CV2, val_names_var[i_var], val_vars[i_var], i_level);
       }
     }
-  } else {
-    InterpolateToNearestNeighbors(val_CV1, val_CV2, val_names_var, val_vars, i_level);
   }
 
   return exit_code;
diff --git a/Common/src/containers/CTrapezoidalMap.cpp b/Common/src/containers/CTrapezoidalMap.cpp
index 22f45868a8f..c0f71e98eb0 100644
--- a/Common/src/containers/CTrapezoidalMap.cpp
+++ b/Common/src/containers/CTrapezoidalMap.cpp
@@ -26,6 +26,7 @@
  */
 
 #include <array>
+#include <iomanip>
 
 #include "../../Common/include/option_structure.hpp"
 #include "../../Common/include/containers/CTrapezoidalMap.hpp"
@@ -40,6 +41,9 @@ using namespace std;
 CTrapezoidalMap::CTrapezoidalMap(const su2double* samples_x, const su2double* samples_y, const unsigned long size,
                                  vector<std::array<unsigned long, 2> > const& edges,
                                  su2vector<vector<unsigned long> > const& val_edge_to_triangle) {
+  int rank = SU2_MPI::GetRank();
+  su2double startTime = SU2_MPI::Wtime();
+
   edge_to_triangle = su2vector<vector<unsigned long> >(val_edge_to_triangle);
 
   unique_bands_x.assign(samples_x, samples_x + size);
@@ -71,6 +75,7 @@ CTrapezoidalMap::CTrapezoidalMap(const su2double* samples_x, const su2double* sa
   unsigned long n_edges = edges.size();
   /* edge index */
   unsigned long i_edge = 0;
+  unsigned long j_edge = 0;
   /* counter for edges intersects */
   unsigned long n_intersects = 0;
   /* lower and upper x value of each band */
@@ -125,6 +130,52 @@ CTrapezoidalMap::CTrapezoidalMap(const su2double* samples_x, const su2double* sa
 
     i_band++;
   }
+
+  su2double stopTime = SU2_MPI::Wtime();
+
+  /* calculate size of trapezoidal map components */
+  double size_unique_bands = sizeof(su2double) * unique_bands_x.size() / 1e6;
+  double size_edge_limits_x = sizeof(su2double) * edge_limits_x.size() * 2 / 1e6;
+  double size_edge_limits_y = sizeof(su2double) * edge_limits_y.size() * 2 / 1e6;
+
+  double size_edge_to_triangle = 0;
+  for (i_edge = 0; i_edge < edge_to_triangle.size(); i_edge++)
+    for (j_edge = 0; j_edge < edge_to_triangle[i_edge].size(); j_edge++)
+      size_edge_to_triangle += sizeof(unsigned long) / 1e6;
+
+  double size_y_edge_at_band_mid = 0;
+  for (unsigned long i_y = 0; i_y < y_edge_at_band_mid.size(); i_y++)
+    for (unsigned long j_y = 0; j_y < y_edge_at_band_mid[i_y].size(); j_y++)
+      size_y_edge_at_band_mid += sizeof(su2double) / 1e6 + sizeof(unsigned long) / 1e6;
+
+  double size_total =
+      size_unique_bands + size_edge_limits_x + size_edge_limits_y + size_edge_to_triangle + size_y_edge_at_band_mid;
+
+  /* print size of trapezoidal map components to screen */
+  if (rank == MASTER_NODE) {
+    cout << setfill(' ');
+    cout << "\n" << endl;
+    cout << "+------------------------------------------------------------------+\n";
+    cout << "|                       Trapezoidal map info                       |\n";
+    cout << "+------------------------------------------------------------------+" << endl;
+
+    cout << "| Time to construct trapezoidal map:    " << setw(22) << right << stopTime - startTime << " sec"
+         << " |" << endl;
+    cout << "| Size of unique_bands in memory:       " << setw(22) << size_unique_bands << " MB "
+         << " |" << endl;
+    cout << "| Size of edge_limits_x in memory:      " << setw(22) << size_edge_limits_x << " MB "
+         << " |" << endl;
+    cout << "| Size of edge_limits_y in memory:      " << setw(22) << size_edge_limits_y << " MB "
+         << " |" << endl;
+    cout << "| Size of edge_to_triangle in memory:   " << setw(22) << size_edge_to_triangle << " MB "
+         << " |" << endl;
+    cout << "| Size of y_edge_at_band_mid in memory: " << setw(22) << size_y_edge_at_band_mid << " MB "
+         << " |" << endl;
+    cout << "| Total:                                " << setw(22) << size_total << " MB "
+         << " |" << endl;
+    cout << "+------------------------------------------------------------------+" << endl;
+    cout << "\n" << endl;
+  }
 }
 
 unsigned long CTrapezoidalMap::GetTriangle(su2double val_x, su2double val_y) {
@@ -134,19 +185,19 @@ unsigned long CTrapezoidalMap::GetTriangle(su2double val_x, su2double val_y) {
   /* within that band, find edges which enclose the (val_x, val_y) point */
   pair<unsigned long, unsigned long> edges = GetEdges(band, val_x, val_y);
 
-  /* identify the triangle using the two edges */
+  /* identify the adjacent triangles using the two edges */
   std::array<unsigned long, 2> triangles_edge_low;
-
-  for (int i = 0; i < 2; i++) triangles_edge_low[i] = edge_to_triangle[edges.first][i];
+  for (unsigned long i = 0; i < edge_to_triangle[edges.first].size(); i++)
+    triangles_edge_low[i] = edge_to_triangle[edges.first][i];
 
   std::array<unsigned long, 2> triangles_edge_up;
-  for (int i = 0; i < 2; i++) triangles_edge_up[i] = edge_to_triangle[edges.second][i];
+  for (unsigned long i = 0; i < edge_to_triangle[edges.second].size(); i++)
+    triangles_edge_up[i] = edge_to_triangle[edges.second][i];
 
   sort(triangles_edge_low.begin(), triangles_edge_low.end());
   sort(triangles_edge_up.begin(), triangles_edge_up.end());
 
-  // The intersection of the faces to which upper or lower belongs is
-  // the face that both belong to.
+  /* The intersection of the faces to which upper or lower belongs is the face that both belong to. */
   vector<unsigned long> triangle(1);
   set_intersection(triangles_edge_up.begin(), triangles_edge_up.end(), triangles_edge_low.begin(),
                    triangles_edge_low.end(), triangle.begin());
diff --git a/Common/src/grid_movement/CSurfaceMovement.cpp b/Common/src/grid_movement/CSurfaceMovement.cpp
index 2147af42f9f..1905b57deaa 100644
--- a/Common/src/grid_movement/CSurfaceMovement.cpp
+++ b/Common/src/grid_movement/CSurfaceMovement.cpp
@@ -893,7 +893,7 @@ void CSurfaceMovement::SetParametricCoord(CGeometry* geometry, CConfig* config,
     cout << "Computed parametric coord for FFD box '" << FFDBox->GetTag() << "'\n";
     cout << "  Number of vertices (Total, Inside FFD, Mapped to FFD): " << GlobalVertex;
     cout << ", " << GlobalVisited << ", " << GlobalMapped << "\n";
-    cout << "  Max coord differece: " << MaxDiff << "\n";
+    cout << "  Max coord difference: " << MaxDiff << "\n";
   }
 
   /*--- After the point inversion, copy the original information back. ---*/
diff --git a/SU2_CFD/include/fluid/CFluidFlamelet.hpp b/SU2_CFD/include/fluid/CFluidFlamelet.hpp
new file mode 100644
index 00000000000..1d0bf91986d
--- /dev/null
+++ b/SU2_CFD/include/fluid/CFluidFlamelet.hpp
@@ -0,0 +1,114 @@
+/*!
+ * \file CFluidFlamelet.hpp
+ * \brief  Defines the flamelet fluid model
+ * \author D. Mayer, T. Economon, N. Beishuizen
+ * \version 7.5.1 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+
+#pragma once
+
+#include "../../Common/include/containers/CLookUpTable.hpp"
+#include "CFluidModel.hpp"
+
+class CFluidFlamelet final : public CFluidModel {
+ private:
+  enum LOOKUP_TD {
+    TEMPERATURE,
+    DENSITY,
+    HEATCAPACITY,
+    VISCOSITY,
+    CONDUCTIVITY,
+    DIFFUSIONCOEFFICIENT,
+    MOLARWEIGHT,
+    SIZE
+  };
+
+  int rank;
+
+  unsigned short n_scalars;
+  unsigned short n_lookups;
+  unsigned short n_user_scalars; /*!< \brief number of passive reactant species. */
+  unsigned short n_control_vars; /*!< \brief number of controlling variables. */
+
+  vector<string> table_scalar_names; /*!< \brief vector to store names of scalar variables.   */
+  vector<string> table_lookup_names; /*!< \brief vector to store names of look up variables.   */
+
+  su2double mass_diffusivity; /*!< \brief local mass diffusivity of the mixture */
+  su2double molar_weight;     /*!< \brief local molar weight of the mixture */
+
+  CLookUpTable* look_up_table;
+
+  vector<string> varnames_TD;    /*!< \brief Lookup names for thermodynamic state variables. */
+  vector<su2double> val_vars_TD; /*!< \brief References to thermodynamic state variables. */
+
+ public:
+  CFluidFlamelet(CConfig* config, su2double value_pressure_operating);
+
+  ~CFluidFlamelet();
+
+  /*!
+   * \brief Set the thermodynamic state.
+   * \param[in] val_temperature - temperature
+   * \param[in] val_scalars - pointer to species mass fractions
+   */
+  void SetTDState_T(su2double val_temperature, const su2double* val_scalars = nullptr) override;
+
+  /*!
+   * \brief Get the total enthalpy from the tabulated temperature and species (inverse lookup).
+   * \param[in/out] enthalpy - total enthalpy
+   * \param[in] val_prog - progress variable
+   * \param[in] val_temp - temperature
+   * \param[in] initial_value - initial value for the iterative lookup procedure.
+   * \param[out] exit_code = error code
+   */
+  unsigned long GetEnthFromTemp(su2double& enthalpy, const su2double val_prog, const su2double val_temp,
+                                su2double initial_value = 0) override;
+
+  /*!
+   * \brief Return a pointer to the lookup table.
+   * \param[out] look_up_table - pointer to lookup table
+   */
+  inline CLookUpTable* GetLookUpTable() override { return look_up_table; }
+
+  /*!
+   * \brief Get the mass diffusivity of the species.
+   * \param[in] iVar - index to the species
+   * \param[out] mass_diffusivity - value of the mass diffusivity
+   */
+  inline su2double GetMassDiffusivity(int iVar) override { return mass_diffusivity; }
+
+  /*!
+   * \brief Get the thermal conductivity of the species.
+   * \param[in] iVar - index to the species
+   * \param[out] Kt - value of the thermal conductivity
+   */
+  inline su2double GetThermalConductivity() override { return Kt; }
+
+  /*!
+   * \brief Get the laminar viscosity of the species.
+   * \param[in] iVar - index to the species
+   * \param[out] Mu - value of the laminar viscosity
+   */
+  inline su2double GetLaminarViscosity() override { return Mu; }
+
+};
diff --git a/SU2_CFD/include/fluid/CFluidModel.hpp b/SU2_CFD/include/fluid/CFluidModel.hpp
index bd8b8b4952e..5e3785bcda1 100644
--- a/SU2_CFD/include/fluid/CFluidModel.hpp
+++ b/SU2_CFD/include/fluid/CFluidModel.hpp
@@ -38,6 +38,7 @@
 
 using namespace std;
 
+class CLookUpTable;
 /*!
  * \class CFluidModel
  * \brief Main class for defining the Thermo-Physical Model
@@ -137,6 +138,24 @@ class CFluidModel {
    */
   su2double GetCv() const { return Cv; }
 
+  /*!
+   * \brief Flamelet LUT - Get the number of transported scalars.
+   */
+  virtual inline unsigned short GetNScalars() const { return 0; }
+
+  /*!
+   * \brief Flamelet LUT - Get the lookup table.
+   */
+  virtual CLookUpTable* GetLookUpTable() { return nullptr; }
+
+  /*!
+   * \brief Flamelet LUT - Get the total enthalpy from the temperature (reverse lookup).
+   */
+  virtual inline unsigned long GetEnthFromTemp(su2double& enthalpy,
+                                               const su2double val_prog,
+                                               const su2double val_temp,
+                                               su2double initial_value) { return 0; }
+
   /*!
    * \brief Get fluid dynamic viscosity.
    */
@@ -319,7 +338,7 @@ class CFluidModel {
    * \brief Virtual member.
    * \param[in] T - Temperature value at the point.
    */
-  virtual void SetTDState_T(su2double val_Temperature, const su2double* val_scalars = nullptr) {}
+  virtual void SetTDState_T(su2double val_Temperature, const su2double* val_scalars = nullptr) { }
 
   /*!
    * \brief Set fluid eddy viscosity provided by a turbulence model needed for computing effective thermal conductivity.
diff --git a/SU2_CFD/include/numerics/species/species_diffusion.hpp b/SU2_CFD/include/numerics/species/species_diffusion.hpp
index e100496b135..7db4d407cd7 100644
--- a/SU2_CFD/include/numerics/species/species_diffusion.hpp
+++ b/SU2_CFD/include/numerics/species/species_diffusion.hpp
@@ -71,8 +71,8 @@ class CAvgGrad_Species final : public CAvgGrad_Scalar<FlowIndices> {
   void FinishResidualCalc(const CConfig* config) override {
     for (auto iVar = 0u; iVar < nVar; iVar++) {
 
-      /* --- in case of species transport, Diffusion_Coeff is the binary diffusion coefficient --- */
       const su2double Diffusivity_Lam = 0.5 * (Density_i * Diffusion_Coeff_i[iVar] + Density_j * Diffusion_Coeff_j[iVar]);
+
       su2double Diffusivity_Turb = 0.0;
 
       if (turbulence) {
diff --git a/SU2_CFD/include/numerics/species/species_sources.hpp b/SU2_CFD/include/numerics/species/species_sources.hpp
index 7dd564720ef..87910f37d37 100644
--- a/SU2_CFD/include/numerics/species/species_sources.hpp
+++ b/SU2_CFD/include/numerics/species/species_sources.hpp
@@ -89,4 +89,5 @@ class CSourceAxisymmetric_Species : public CSourceBase_Species {
    * \return Lightweight const-view of residual and Jacobian.
    */
   ResidualType<> ComputeResidual(const CConfig* config) override;
+
 };
diff --git a/SU2_CFD/include/output/CFlowIncOutput.hpp b/SU2_CFD/include/output/CFlowIncOutput.hpp
index bdb7a23c5cb..7a8621f25db 100644
--- a/SU2_CFD/include/output/CFlowIncOutput.hpp
+++ b/SU2_CFD/include/output/CFlowIncOutput.hpp
@@ -41,6 +41,7 @@ class CFlowIncOutput final: public CFlowOutput {
   TURB_MODEL turb_model;     /*!< \brief The kind of turbulence model*/
   bool heat;                 /*!< \brief Boolean indicating whether have a heat problem*/
   bool weakly_coupled_heat;  /*!< \brief Boolean indicating whether have a weakly coupled heat equation*/
+  bool flamelet;  /*!< \brief Boolean indicating whether we solve the flamelet equations */
   unsigned short streamwisePeriodic;   /*!< \brief Boolean indicating whether it is a streamwise periodic simulation. */
   bool streamwisePeriodic_temperature; /*!< \brief Boolean indicating streamwise periodic temperature is used. */
 
diff --git a/SU2_CFD/include/output/CFlowOutput.hpp b/SU2_CFD/include/output/CFlowOutput.hpp
index dcab274bf02..a47cae8de2b 100644
--- a/SU2_CFD/include/output/CFlowOutput.hpp
+++ b/SU2_CFD/include/output/CFlowOutput.hpp
@@ -125,7 +125,31 @@ class CFlowOutput : public CFVMOutput{
   void SetVolumeOutputFieldsScalarResidual(const CConfig* config);
 
   /*!
-   * \brief Add scalar (turbulence/species) volume limiter fields (and more) for a point (FVMComp, FVMInc, FVMNEMO).
+   * \brief Add scalar (turbulence/species) volume primitive fields for a point (FVMComp, FVMInc, FVMNEMO).
+   * \param[in] config - Definition of the particular problem.
+   */
+  void SetVolumeOutputFieldsScalarPrimitive(const CConfig* config);
+
+  /*!
+   * \brief Add scalar (turbulence/species) volume limiter fields for a point (FVMComp, FVMInc, FVMNEMO).
+   * \param[in] config - Definition of the particular problem.
+   */
+  void SetVolumeOutputFieldsScalarLimiter(const CConfig* config);
+
+  /*!
+   * \brief Add flamelet volume source term fields for a point (FVMComp, FVMInc, FVMNEMO).
+   * \param[in] config - Definition of the particular problem.
+   */
+  void SetVolumeOutputFieldsScalarSource(const CConfig* config);
+
+  /*!
+   * \brief Add flamelet volume lookup value fields for a point (FVMComp, FVMInc, FVMNEMO).
+   * \param[in] config - Definition of the particular problem.
+   */
+  void SetVolumeOutputFieldsScalarLookup(const CConfig* config);
+
+  /*!
+   * \brief Add miscellaneous scalar volume fields for a point (FVMComp, FVMInc, FVMNEMO).
    * \param[in] config - Definition of the particular problem.
    */
   void SetVolumeOutputFieldsScalarMisc(const CConfig* config);
diff --git a/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp b/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp
new file mode 100644
index 00000000000..95b4afe7311
--- /dev/null
+++ b/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp
@@ -0,0 +1,171 @@
+/*!
+ * \file CSpeciesFlameletSolver.hpp
+ * \brief Headers of the CSpeciesFlameletSolver class
+ * \author D. Mayer, N. Beishuizen, T. Economon
+ * \version 7.5.1 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+
+#pragma once
+
+#include "CSpeciesSolver.hpp"
+
+/*!
+ * \class CSpeciesFlameletSolver
+ * \brief Main class for defining the flamelet model solver.
+ * \author N. Beishuizen
+ * \ingroup Scalar_Transport
+ */
+class CSpeciesFlameletSolver final : public CSpeciesSolver {
+ private:
+  vector<su2activematrix> conjugate_var; /*!< \brief CHT variables for each boundary and vertex. */
+
+  /*!
+   * \brief Compute the preconditioner for low-Mach flows.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] config - Definition of the particular problem.
+   */
+  void SetPreconditioner(CGeometry* geometry, CSolver** solver_container, CConfig* config);
+
+  /*!
+   * \brief Compute the primitive variables (diffusivities).
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] Output - Boolean to determine whether to print output.
+   * \return - The number of non-physical points.
+   */
+  unsigned long SetPrimitive_Variables(CSolver** solver_container, CConfig* config, bool Output);
+
+  /*!
+   * \brief Generic implementation of the isothermal wall also covering CHT cases,
+   * for which the wall temperature is given by GetConjugateHeatVariable.
+   */
+  void BC_Isothermal_Wall_Generic(CGeometry* geometry, CSolver** solver_container, CNumerics* conv_numerics,
+                                  CNumerics* visc_numerics, CConfig* config, unsigned short val_marker,
+                                  bool cht_mode = false);
+
+ public:
+  /*!
+   * \brief Constructor.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] iMesh - Index of the mesh in multigrid computations.
+   * \param[in] FluidModel
+   */
+  CSpeciesFlameletSolver(CGeometry* geometry, CConfig* config, unsigned short iMesh);
+
+  /*!
+   * \brief Restart residual and compute gradients.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] iMesh - Index of the mesh in multigrid computations.
+   * \param[in] iRKStep - Current step of the Runge-Kutta iteration.
+   * \param[in] RunTime_EqSystem - System of equations which is going to be solved.
+   * \param[in] Output - Boolean to determine whether to print output.
+   */
+  void Preprocessing(CGeometry* geometry, CSolver** solver_container, CConfig* config, unsigned short iMesh,
+                     unsigned short iRKStep, unsigned short RunTime_EqSystem, bool Output) override;
+
+  /*!
+   * \brief Set the initial condition for the scalar transport problem.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver_container - Container with all the solutions.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] ExtIter - External iteration.
+   */
+  void SetInitialCondition(CGeometry** geometry, CSolver*** solver_container, CConfig* config,
+                           unsigned long ExtIter) override;
+
+  /*!
+   * \brief Source term computation.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] numerics - Description of the numerical method.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] iMesh - Index of the mesh in multigrid computations.
+   */
+  void Source_Residual(CGeometry* geometry, CSolver** solver_container, CNumerics** numerics_container, CConfig* config,
+                       unsigned short iMesh) override;
+
+  /*!
+   * \brief Impose the Navier-Stokes wall boundary condition.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] conv_numerics - Description of the numerical method.
+   * \param[in] visc_numerics - Description of the numerical method.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] val_marker - Surface marker where the boundary condition is applied.
+   */
+  void BC_Isothermal_Wall(CGeometry* geometry, CSolver** solver_container, CNumerics* conv_numerics,
+                          CNumerics* visc_numerics, CConfig* config, unsigned short val_marker) override;
+
+  /*!
+   * \brief Impose the inlet boundary condition.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] conv_numerics - Description of the numerical method.
+   * \param[in] visc_numerics - Description of the numerical method.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] val_marker - Surface marker where the boundary condition is applied.
+   */
+  void BC_Inlet(CGeometry* geometry, CSolver** solver_container, CNumerics* conv_numerics, CNumerics* visc_numerics,
+                CConfig* config, unsigned short val_marker) override;
+
+  /*!
+   * \brief Impose the (received) conjugate heat variables.
+   * \param[in] geometry - Geometrical definition of the problem.
+   * \param[in] solver_container - Container vector with all the solutions.
+   * \param[in] numerics - Description of the numerical method.
+   * \param[in] config - Definition of the particular problem.
+   * \param[in] val_marker - Surface marker where the boundary condition is applied.
+   */
+  void BC_ConjugateHeat_Interface(CGeometry* geometry, CSolver** solver_container, CNumerics* numerics, CConfig* config,
+                                  unsigned short val_marker) override;
+
+  /*!
+   * \brief Get the conjugate heat variables.
+   * \param[in] val_marker - The marker index.
+   * \param[in] val_vertex - The vertex index.
+   * \param[in] pos_var - The variable position (in vector of all conjugate heat variables).
+   */
+  inline su2double GetConjugateHeatVariable(unsigned short val_marker, unsigned long val_vertex,
+                                            unsigned short pos_var) const override {
+    return conjugate_var[val_marker][val_vertex][pos_var];
+  }
+
+  /*!
+   * \brief Set the conjugate heat variables.
+   * \param[in] val_marker - The marker index.
+   * \param[in] val_vertex - The vertex index.
+   * \param[in] pos_var - The variable position (in vector of all conjugate heat variables).
+   * \param[in] relaxation_factor - The relaxation factor for the change of the variables.
+   * \param[in] val_var - The value of the variable.
+   */
+  inline void SetConjugateHeatVariable(unsigned short val_marker, unsigned long val_vertex, unsigned short pos_var,
+                                       su2double relaxation_factor, su2double val_var) override {
+    conjugate_var[val_marker][val_vertex][pos_var] =
+        relaxation_factor * val_var + (1.0 - relaxation_factor) * conjugate_var[val_marker][val_vertex][pos_var];
+  }
+
+};
diff --git a/SU2_CFD/include/solvers/CSpeciesSolver.hpp b/SU2_CFD/include/solvers/CSpeciesSolver.hpp
index d4d751e3ff5..1d4eef366de 100644
--- a/SU2_CFD/include/solvers/CSpeciesSolver.hpp
+++ b/SU2_CFD/include/solvers/CSpeciesSolver.hpp
@@ -65,6 +65,8 @@ class CSpeciesSolver : public CScalarSolver<CSpeciesVariable> {
    */
   void LoadRestart(CGeometry** geometry, CSolver*** solver, CConfig* config, int val_iter, bool val_update_geo) final;
 
+  void Initialize(CGeometry* geometry, CConfig* config, unsigned short iMesh, unsigned short nVar);
+
   /*!
    * \brief Restart residual and compute gradients.
    * \param[in] geometry - Geometrical definition of the problem.
@@ -76,7 +78,7 @@ class CSpeciesSolver : public CScalarSolver<CSpeciesVariable> {
    * \param[in] Output - boolean to determine whether to print output.
    */
   void Preprocessing(CGeometry* geometry, CSolver** solver_container, CConfig* config, unsigned short iMesh,
-                     unsigned short iRKStep, unsigned short RunTime_EqSystem, bool Output) final;
+                     unsigned short iRKStep, unsigned short RunTime_EqSystem, bool Output) override;
 
   /*!
    * \brief Compute the viscous flux for the turbulent equation at a particular edge.
@@ -100,7 +102,7 @@ class CSpeciesSolver : public CScalarSolver<CSpeciesVariable> {
    * \param[in] val_marker - Surface marker where the boundary condition is applied.
    */
   void BC_Inlet(CGeometry* geometry, CSolver** solver_container, CNumerics* conv_numerics, CNumerics* visc_numerics,
-                CConfig* config, unsigned short val_marker) final;
+                CConfig* config, unsigned short val_marker) override;
 
   /*!
    * \brief Store of a set of provided inlet profile values at a vertex.
diff --git a/SU2_CFD/include/variables/CSpeciesFlameletVariable.hpp b/SU2_CFD/include/variables/CSpeciesFlameletVariable.hpp
new file mode 100644
index 00000000000..6f2eb6fe42b
--- /dev/null
+++ b/SU2_CFD/include/variables/CSpeciesFlameletVariable.hpp
@@ -0,0 +1,90 @@
+/*!
+ * \file CSpeciesFlameletVariable.hpp
+ * \brief Base class for defining the variables of the flamelet transport model.
+ * \author D. Mayer, T. Economon, N. Beishuizen
+ * \version 7.5.1 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+
+#pragma once
+
+#include "CSpeciesVariable.hpp"
+
+/*!
+ * \class CSpeciesFlameletVariable
+ * \brief Base class for defining the variables of the flamelet model.
+ */
+class CSpeciesFlameletVariable final : public CSpeciesVariable {
+ protected:
+  MatrixType source_scalar; /*!< \brief Vector of the source terms from the lookup table for each scalar equation */
+  MatrixType lookup_scalar; /*!< \brief Vector of the source terms from the lookup table for each scalar equation */
+  su2vector<unsigned short> table_misses; /*!< \brief Vector of lookup table misses. */
+
+ public:
+  /*!
+   * \brief Constructor of the class.
+   * \param[in] species_inf - species variable values (initialization value).
+   * \param[in] npoint - Number of points/nodes/vertices in the domain.
+   * \param[in] ndim - Number of dimensions of the problem.
+   * \param[in] nvar - Number of variables of the problem.
+   * \param[in] config - Definition of the particular problem.
+   */
+  CSpeciesFlameletVariable(const su2double* species_inf, unsigned long npoint, unsigned long ndim, unsigned long nvar,
+                           const CConfig* config);
+
+  /*!
+   * \brief Set the value of the transported scalar source term.
+   * \param[in] iPoint - the location where the value has to be set.
+   * \param[in] val_lookup_scalar - the value of the scalar to set.
+   * \param[in] val_ivar - Eqn. index to the transport equation.
+   */
+  inline void SetLookupScalar(unsigned long iPoint, su2double val_lookup_scalar, unsigned short val_ivar) override {
+    lookup_scalar(iPoint, val_ivar) = val_lookup_scalar;
+  }
+
+  /*!
+
+   * \brief Set a source term for the specie transport equation.
+   * \param[in] iPoint - Node index.
+   * \param[in] val_ivar - Species index.
+   * \param[in] val_source - Source term value.
+  */
+  inline void SetScalarSource(unsigned long iPoint, unsigned short val_ivar, su2double val_source) override {
+    source_scalar(iPoint, val_ivar) = val_source;
+  }
+
+  /*!
+   * \brief Get the value of the transported scalars source term.
+   * \return Pointer to the transported scalars source term.
+   */
+  inline const su2double* GetScalarSources(unsigned long iPoint) const override { return source_scalar[iPoint]; }
+
+  /*!
+   * \brief Get the value of the looked up table based on the transported scalar.
+   * \return Pointer to the transported scalars source term.
+   */
+  inline const su2double* GetScalarLookups(unsigned long iPoint) const override { return lookup_scalar[iPoint]; }
+
+  inline void SetTableMisses(unsigned long iPoint, unsigned short misses) override { table_misses[iPoint] = misses; }
+
+  inline unsigned short GetTableMisses(unsigned long iPoint) const override { return table_misses[iPoint]; }
+};
diff --git a/SU2_CFD/include/variables/CSpeciesVariable.hpp b/SU2_CFD/include/variables/CSpeciesVariable.hpp
index d668e006db2..a3d254ec30b 100644
--- a/SU2_CFD/include/variables/CSpeciesVariable.hpp
+++ b/SU2_CFD/include/variables/CSpeciesVariable.hpp
@@ -38,7 +38,7 @@ class CSpeciesVariable : public CScalarVariable {
   MatrixType Diffusivity; /*!< \brief Matrix (nPoint,nVar) of mass diffusivities for scalar transport. */
 
  public:
-  static constexpr size_t MAXNVAR = 4; /*!< \brief Max number of variables for static arrays. Increase, if necessary. */
+  static constexpr size_t MAXNVAR = 20; /*!< \brief Max number of variables for static arrays. Increase, if necessary. */
 
   /*!
    * \brief Constructor of the class.
diff --git a/SU2_CFD/include/variables/CVariable.hpp b/SU2_CFD/include/variables/CVariable.hpp
index a5beafd75e0..5167ef953f6 100644
--- a/SU2_CFD/include/variables/CVariable.hpp
+++ b/SU2_CFD/include/variables/CVariable.hpp
@@ -2312,4 +2312,17 @@ class CVariable {
   virtual su2double GetSourceTerm_DispAdjoint(unsigned long iPoint, unsigned long iDim) const { return 0.0; }
   virtual su2double GetSourceTerm_VelAdjoint(unsigned long iPoint, unsigned long iDim) const { return 0.0; }
 
+  /*!
+   * \brief LUT premixed flamelet: virtual functions for the speciesflameletvariable LUT
+   */
+  inline virtual void SetLookupScalar(unsigned long iPoint, su2double val_lookup_scalar, unsigned short val_ivar) { }
+
+  inline virtual void SetScalarSource(unsigned long iPoint, unsigned short val_ivar, su2double val_source) { }
+
+  inline virtual void SetTableMisses(unsigned long iPoint, unsigned short misses) { }
+
+  inline virtual unsigned short GetTableMisses(unsigned long iPoint) const { return 0; }
+
+  inline virtual const su2double *GetScalarSources(unsigned long iPoint) const { return nullptr; }
+  inline virtual const su2double *GetScalarLookups(unsigned long iPoint) const { return nullptr; }
 };
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index 639e34c4304..1eee1af5e85 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -1430,6 +1430,7 @@ void CDriver::InstantiateSpeciesNumerics(unsigned short nVar_Species, int offset
     numerics[iMGlevel][SPECIES_SOL][source_second_term] = new CSourceNothing(nDim, nVar_Species, config);
   }
 }
+
 /*--- Explicit instantiation of the template above, needed because it is defined in a cpp file, instead of hpp. ---*/
 template void CDriver::InstantiateSpeciesNumerics<CEulerVariable::CIndices<unsigned short>>(
     unsigned short, int, const CConfig*, const CSolver*, CNumerics****&) const;
@@ -3034,6 +3035,8 @@ void CFluidDriver::Preprocess(unsigned long Iter) {
       if (config_container[iZone]->GetFluidProblem()) {
         for (iInst = 0; iInst < nInst[iZone]; iInst++) {
           solver_container[iZone][iInst][MESH_0][FLOW_SOL]->SetInitialCondition(geometry_container[iZone][INST_0], solver_container[iZone][iInst], config_container[iZone], Iter);
+          if (config_container[iZone]->GetKind_Species_Model() != SPECIES_MODEL::NONE)
+            solver_container[iZone][iInst][MESH_0][SPECIES_SOL]->SetInitialCondition(geometry_container[iZone][INST_0], solver_container[iZone][iInst], config_container[iZone], Iter);
         }
       }
     }
diff --git a/SU2_CFD/src/drivers/CMultizoneDriver.cpp b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
index 61f59223fcf..b3a7af5e369 100644
--- a/SU2_CFD/src/drivers/CMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
@@ -245,6 +245,14 @@ void CMultizoneDriver::Preprocess(unsigned long TimeIter) {
                                                                               solver_container[iZone][INST_0],
                                                                               config_container[iZone], TimeIter);
     }
+    if (!fsi && (config_container[iZone]->GetKind_Species_Model() != SPECIES_MODEL::NONE)) {
+      /*--- Set the initial condition for SPECIES solver (species or flamelet) ----------------------*/
+      solver_container[iZone][INST_0][MESH_0][SPECIES_SOL]->SetInitialCondition(geometry_container[ZONE_0][INST_0],
+                                                                                solver_container[ZONE_0][INST_0],
+                                                                                config_container[ZONE_0], TimeIter);
+    }
+
+
   }
 
   /*--- Ramp turbo values for unsteady problems here, otherwise do it over outer iterations. ---*/
diff --git a/SU2_CFD/src/drivers/CSinglezoneDriver.cpp b/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
index 964888a83fb..c1f2c2519c8 100644
--- a/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
@@ -134,6 +134,11 @@ void CSinglezoneDriver::Preprocess(unsigned long TimeIter) {
                                                                             solver_container[ZONE_0][INST_0],
                                                                             config_container[ZONE_0], TimeIter);
   }
+  if (config_container[ZONE_0]->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
+    solver_container[ZONE_0][INST_0][MESH_0][SPECIES_SOL]->SetInitialCondition(geometry_container[ZONE_0][INST_0],
+                                                                                solver_container[ZONE_0][INST_0],
+                                                                                config_container[ZONE_0], TimeIter);
+  }
   else if (config_container[ZONE_0]->GetHeatProblem()) {
     /*--- Set the initial condition for HEAT equation ---------------------------------------------*/
     solver_container[ZONE_0][INST_0][MESH_0][HEAT_SOL]->SetInitialCondition(geometry_container[ZONE_0][INST_0],
diff --git a/SU2_CFD/src/fluid/CFluidFlamelet.cpp b/SU2_CFD/src/fluid/CFluidFlamelet.cpp
new file mode 100644
index 00000000000..34051288559
--- /dev/null
+++ b/SU2_CFD/src/fluid/CFluidFlamelet.cpp
@@ -0,0 +1,138 @@
+/*!
+ * \file CfluidFlamelet.cpp
+ * \brief Main subroutines of CFluidFlamelet class
+ * \author D. Mayer, T. Economon, N. Beishuizen
+ * \version 7.5.1 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+
+#include "../include/fluid/CFluidFlamelet.hpp"
+#include "../../../Common/include/containers/CLookUpTable.hpp"
+
+CFluidFlamelet::CFluidFlamelet(CConfig* config, su2double value_pressure_operating) : CFluidModel() {
+  rank = SU2_MPI::GetRank();
+
+  /* -- number of auxiliary species transport equations, e.g. 1=CO, 2=NOx  --- */
+  n_user_scalars = config->GetNUserScalars();
+  n_control_vars = config->GetNControlVars();
+  n_scalars = config->GetNScalars();
+
+  if (rank == MASTER_NODE) {
+    cout << "Number of scalars:           " << n_scalars << endl;
+    cout << "Number of user scalars:      " << n_user_scalars << endl;
+    cout << "Number of control variables: " << n_control_vars << endl;
+  }
+
+  if (rank == MASTER_NODE) {
+    cout << "*****************************************" << endl;
+    cout << "***   initializing the lookup table   ***" << endl;
+    cout << "*****************************************" << endl;
+  }
+
+  table_scalar_names.resize(n_scalars);
+  table_scalar_names[I_ENTH] = "EnthalpyTot";
+  table_scalar_names[I_PROGVAR] = "ProgressVariable";
+  /*--- auxiliary species transport equations---*/
+  for (size_t i_aux = 0; i_aux < n_user_scalars; i_aux++) {
+    table_scalar_names[n_control_vars + i_aux] = config->GetUserScalarName(i_aux);
+  }
+
+  look_up_table = new CLookUpTable(config->GetFileNameLUT(), table_scalar_names[I_PROGVAR], table_scalar_names[I_ENTH]);
+
+  n_lookups = config->GetNLookups();
+  table_lookup_names.resize(n_lookups);
+  for (int i_lookup = 0; i_lookup < n_lookups; ++i_lookup) {
+    table_lookup_names[i_lookup] = config->GetLUTLookupName(i_lookup);
+  }
+
+  Pressure = value_pressure_operating;
+
+  /*--- Thermodynamic state variables and names. ---*/
+  varnames_TD.resize(LOOKUP_TD::SIZE);
+  val_vars_TD.resize(LOOKUP_TD::SIZE);
+
+  /*--- The string in varnames_TD as it appears in the LUT file. ---*/
+  varnames_TD[LOOKUP_TD::TEMPERATURE] =  "Temperature";
+  varnames_TD[LOOKUP_TD::DENSITY] = "Density";
+  varnames_TD[LOOKUP_TD::HEATCAPACITY] = "Cp";
+  varnames_TD[LOOKUP_TD::VISCOSITY] = "ViscosityDyn";
+  varnames_TD[LOOKUP_TD::CONDUCTIVITY] = "Conductivity";
+  varnames_TD[LOOKUP_TD::DIFFUSIONCOEFFICIENT] = "DiffusionCoefficient";
+  varnames_TD[LOOKUP_TD::MOLARWEIGHT] = "MolarWeightMix";
+
+}
+
+CFluidFlamelet::~CFluidFlamelet() { delete look_up_table; }
+
+void CFluidFlamelet::SetTDState_T(su2double val_temperature, const su2double* val_scalars) {
+  su2double val_enth = val_scalars[I_ENTH];
+  su2double val_prog = val_scalars[I_PROGVAR];
+
+  /*--- Add all quantities and their names to the look up vectors. ---*/
+  look_up_table->LookUp_XY(varnames_TD, val_vars_TD, val_prog, val_enth);
+
+  Temperature = val_vars_TD[LOOKUP_TD::TEMPERATURE];
+  Density = val_vars_TD[LOOKUP_TD::DENSITY];
+  Cp = val_vars_TD[LOOKUP_TD::HEATCAPACITY];
+  Mu = val_vars_TD[LOOKUP_TD::VISCOSITY];
+  Kt = val_vars_TD[LOOKUP_TD::CONDUCTIVITY];
+  mass_diffusivity = val_vars_TD[LOOKUP_TD::DIFFUSIONCOEFFICIENT];
+  molar_weight = val_vars_TD[LOOKUP_TD::MOLARWEIGHT];
+
+  /*--- Compute Cv from Cp and molar weight of the mixture (ideal gas). ---*/
+  Cv = Cp - UNIVERSAL_GAS_CONSTANT / molar_weight;
+}
+
+/* --- Total enthalpy is the transported variable, but we usually have temperature as a boundary condition,
+       so we do a reverse lookup */
+unsigned long CFluidFlamelet::GetEnthFromTemp(su2double& val_enth, const su2double val_prog, const su2double val_temp,
+                                              const su2double initial_value) {
+  /*--- convergence criterion for temperature in [K], high accuracy needed for restarts. ---*/
+  su2double delta_temp_final = 0.001;
+  su2double enth_iter = initial_value;
+  su2double delta_enth;
+  su2double delta_temp_iter = 1e10;
+  unsigned long exit_code = 0;
+  const int counter_limit = 1000;
+
+  int counter = 0;
+  while ((abs(delta_temp_iter) > delta_temp_final) && (counter++ < counter_limit)) {
+    /*--- Add all quantities and their names to the look up vectors. ---*/
+    look_up_table->LookUp_XY(varnames_TD, val_vars_TD, val_prog, enth_iter);
+    Temperature = val_vars_TD[LOOKUP_TD::TEMPERATURE];
+    Cp = val_vars_TD[LOOKUP_TD::HEATCAPACITY];
+
+    delta_temp_iter = val_temp - Temperature;
+
+    delta_enth = Cp * delta_temp_iter;
+
+    enth_iter += delta_enth;
+  }
+
+  val_enth = enth_iter;
+
+  if (counter >= counter_limit) {
+    exit_code = 1;
+  }
+
+  return exit_code;
+}
diff --git a/SU2_CFD/src/fluid/CFluidModel.cpp b/SU2_CFD/src/fluid/CFluidModel.cpp
index 15ab39b24e2..5aca9e783da 100644
--- a/SU2_CFD/src/fluid/CFluidModel.cpp
+++ b/SU2_CFD/src/fluid/CFluidModel.cpp
@@ -41,6 +41,7 @@
 #include "../../include/fluid/CPolynomialConductivityRANS.hpp"
 #include "../../include/fluid/CPolynomialViscosity.hpp"
 #include "../../include/fluid/CSutherland.hpp"
+#include "../../include/fluid/CFluidFlamelet.hpp"
 #include "../../include/fluid/CCoolPropViscosity.hpp"
 #include "../../include/fluid/CConstantLewisDiffusivity.hpp"
 #include "../../include/fluid/CCoolPropConductivity.hpp"
@@ -58,6 +59,9 @@ unique_ptr<CViscosityModel> CFluidModel::MakeLaminarViscosityModel(const CConfig
     case VISCOSITYMODEL::POLYNOMIAL:
       return unique_ptr<CPolynomialViscosity<N_POLY_COEFFS>>(
           new CPolynomialViscosity<N_POLY_COEFFS>(config->GetMu_PolyCoeffND()));
+    case VISCOSITYMODEL::FLAMELET:
+      /*--- Viscosity is obtained from the LUT ---*/
+      return nullptr;
     default:
       SU2_MPI::Error("Viscosity model not available.", CURRENT_FUNCTION);
       return nullptr;
@@ -108,10 +112,12 @@ unique_ptr<CConductivityModel> CFluidModel::MakeThermalConductivityModel(const C
             new CPolynomialConductivity<N_POLY_COEFFS>(config->GetKt_PolyCoeffND()));
       }
       break;
+    case CONDUCTIVITYMODEL::FLAMELET:
+      /*--- Conductivity is obtained from the LUT ---*/
+      return nullptr;
     default:
       SU2_MPI::Error("Conductivity model not available.", CURRENT_FUNCTION);
       return nullptr;
-      break;
   }
 }
 
@@ -134,6 +140,10 @@ unique_ptr<CDiffusivityModel> CFluidModel::MakeMassDiffusivityModel(const CConfi
       return unique_ptr<CConstantLewisDiffusivity>(
           new CConstantLewisDiffusivity(config->GetConstant_Lewis_Number(iSpecies)));
       break;
+    case DIFFUSIVITYMODEL::FLAMELET:
+      /*--- Diffusivity is obtained from the LUT ---*/
+      return nullptr;
+      break;
     default:
       SU2_MPI::Error("Diffusivity model not available.", CURRENT_FUNCTION);
       return nullptr;
diff --git a/SU2_CFD/src/integration/CIntegration.cpp b/SU2_CFD/src/integration/CIntegration.cpp
index 1da64f36a32..d27be847c53 100644
--- a/SU2_CFD/src/integration/CIntegration.cpp
+++ b/SU2_CFD/src/integration/CIntegration.cpp
@@ -161,7 +161,12 @@ void CIntegration::Space_Integration(CGeometry *geometry,
         solver_container[MainSolver]->BC_Custom(geometry, solver_container, conv_bound_numerics, visc_bound_numerics, config, iMarker);
         break;
       case CHT_WALL_INTERFACE:
-        if ((MainSolver == HEAT_SOL) || ((MainSolver == FLOW_SOL) && ((config->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE) || config->GetEnergy_Equation()))) {
+
+        if ( MainSolver == FLOW_SOL && (config->GetKind_FluidModel() == FLUID_FLAMELET) ){
+          solver_container[MainSolver]->BC_Isothermal_Wall(geometry, solver_container, conv_bound_numerics, visc_bound_numerics, config, iMarker);
+          break;
+        }
+        if ((MainSolver == SPECIES_SOL) || (MainSolver == HEAT_SOL) || ((MainSolver == FLOW_SOL) && ((config->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE) || config->GetEnergy_Equation()))) {
           solver_container[MainSolver]->BC_ConjugateHeat_Interface(geometry, solver_container, conv_bound_numerics, config, iMarker);
         }
         else {
diff --git a/SU2_CFD/src/interfaces/cht/CConjugateHeatInterface.cpp b/SU2_CFD/src/interfaces/cht/CConjugateHeatInterface.cpp
index 56fcea263e2..594863bb9a1 100644
--- a/SU2_CFD/src/interfaces/cht/CConjugateHeatInterface.cpp
+++ b/SU2_CFD/src/interfaces/cht/CConjugateHeatInterface.cpp
@@ -104,6 +104,7 @@ void CConjugateHeatInterface::GetDonor_Variable(CSolver *donor_solution, CGeomet
       switch (donor_config->GetKind_ConductivityModel()) {
 
         case CONDUCTIVITYMODEL::CONSTANT:
+        case CONDUCTIVITYMODEL::FLAMELET:
         case CONDUCTIVITYMODEL::COOLPROP:
           thermal_conductivity = thermal_conductivityND*donor_config->GetThermal_Conductivity_Ref();
           break;
diff --git a/SU2_CFD/src/iteration/CFluidIteration.cpp b/SU2_CFD/src/iteration/CFluidIteration.cpp
index 298ee40d56c..da63e7812a5 100644
--- a/SU2_CFD/src/iteration/CFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CFluidIteration.cpp
@@ -98,7 +98,7 @@ void CFluidIteration::Iterate(COutput* output, CIntegration**** integration, CGe
                                                                       RUNTIME_TURB_SYS, val_iZone, val_iInst);
   }
 
-  if (config[val_iZone]->GetKind_Species_Model() != SPECIES_MODEL::NONE){
+  if (config[val_iZone]->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
     config[val_iZone]->SetGlobalParam(main_solver, RUNTIME_SPECIES_SYS);
     integration[val_iZone][val_iInst][SPECIES_SOL]->SingleGrid_Iteration(geometry, solver, numerics, config,
                                                                          RUNTIME_SPECIES_SYS, val_iZone, val_iInst);
diff --git a/SU2_CFD/src/meson.build b/SU2_CFD/src/meson.build
index 9ca0188ffc0..98f71f9fd45 100644
--- a/SU2_CFD/src/meson.build
+++ b/SU2_CFD/src/meson.build
@@ -6,6 +6,7 @@ su2_cfd_src = files(['definition_structure.cpp',
 su2_cfd_src += files(['fluid/CFluidModel.cpp',
                       'fluid/CIdealGas.cpp',
                       'fluid/CFluidScalar.cpp',
+                      'fluid/CFluidFlamelet.cpp',
                       'fluid/CPengRobinson.cpp',
                       'fluid/CVanDerWaalsGas.cpp',
                       'fluid/CCoolProp.cpp',
@@ -58,6 +59,7 @@ su2_cfd_src += files(['variables/CIncNSVariable.cpp',
                       'variables/CTurbVariable.cpp',
                       'variables/CScalarVariable.cpp',
                       'variables/CSpeciesVariable.cpp',
+                      'variables/CSpeciesFlameletVariable.cpp',
                       'variables/CAdjNSVariable.cpp',
                       'variables/CBaselineVariable.cpp',
                       'variables/CDiscAdjFEABoundVariable.cpp',
@@ -107,6 +109,7 @@ su2_cfd_src += files(['solvers/CSolverFactory.cpp',
                       'solvers/CSolver.cpp',
                       'solvers/CTemplateSolver.cpp',
                       'solvers/CSpeciesSolver.cpp',
+                      'solvers/CSpeciesFlameletSolver.cpp',
                       'solvers/CTransLMSolver.cpp',
                       'solvers/CTurbSolver.cpp',
                       'solvers/CTurbSASolver.cpp',
diff --git a/SU2_CFD/src/numerics/species/species_sources.cpp b/SU2_CFD/src/numerics/species/species_sources.cpp
index 06a26902b8a..ab51d4b15e7 100644
--- a/SU2_CFD/src/numerics/species/species_sources.cpp
+++ b/SU2_CFD/src/numerics/species/species_sources.cpp
@@ -90,7 +90,6 @@ CNumerics::ResidualType<> CSourceAxisymmetric_Species<T>::ComputeResidual(const
 
   /*--- Contribution due to 2D axisymmetric formulation ---*/
   if (Coord_i[1] > EPS) {
-
     AD::SetPreaccIn(Coord_i[1]);
     AD::SetPreaccIn(Diffusion_Coeff_i, nVar);
     AD::SetPreaccIn(ScalarVar_Grad_i, nVar, nDim);
@@ -123,7 +122,7 @@ CNumerics::ResidualType<> CSourceAxisymmetric_Species<T>::ComputeResidual(const
       if (turbulence)
         Mass_Diffusivity_Tur = V_i[idx.EddyViscosity()] / Sc_t;
 
-      for (auto iVar=0u; iVar < nVar; iVar++){
+      for (auto iVar = 0u; iVar < nVar; iVar++) {
         residual[iVar] += yinv * Volume * (Density_i * Diffusion_Coeff_i[iVar] + Mass_Diffusivity_Tur) * ScalarVar_Grad_i[iVar][1];
       }
     }
diff --git a/SU2_CFD/src/output/CAdjFlowOutput.cpp b/SU2_CFD/src/output/CAdjFlowOutput.cpp
index 4ef01b6c16c..9489926a537 100644
--- a/SU2_CFD/src/output/CAdjFlowOutput.cpp
+++ b/SU2_CFD/src/output/CAdjFlowOutput.cpp
@@ -55,11 +55,22 @@ void CAdjFlowOutput::AddHistoryOutputFields_AdjScalarRMS_RES(const CConfig* conf
     }
   }
 
-  if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
+  if (config->GetKind_Species_Model() == SPECIES_MODEL::SPECIES_TRANSPORT) {
     for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
       AddHistoryOutput("RMS_ADJ_SPECIES_" + std::to_string(iVar), "rms[A_rho*Y_" + std::to_string(iVar) + "]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the adjoint transported species.", HistoryFieldType::RESIDUAL);
     }
   }
+
+  if (config->GetKind_Species_Model() == SPECIES_MODEL::FLAMELET) {
+
+    AddHistoryOutput("RMS_ADJ_PROGRESS_VARIABLE", "rms[PV]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the adjoint progress variable.", HistoryFieldType::RESIDUAL);
+    AddHistoryOutput("RMS_ADJ_TOTAL_ENTHALPY", "rms[Enth]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the adjoint total enthalpy.", HistoryFieldType::RESIDUAL);
+    
+    for (unsigned short i_scalar = 0; i_scalar < config->GetNUserScalars(); i_scalar++) {
+      const auto& scalar_name = config->GetUserScalarName(i_scalar);
+      AddHistoryOutput("RMS_ADJ_" + scalar_name, "rms[" + scalar_name + "]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the adjoint of " + scalar_name + " .", HistoryFieldType::RESIDUAL);
+    }
+  }
 }
 
 void CAdjFlowOutput::AddHistoryOutputFields_AdjScalarMAX_RES(const CConfig* config) {
@@ -80,11 +91,22 @@ void CAdjFlowOutput::AddHistoryOutputFields_AdjScalarMAX_RES(const CConfig* conf
     }
   }
 
-  if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
+  if (config->GetKind_Species_Model() == SPECIES_MODEL::SPECIES_TRANSPORT) {
     for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
       AddHistoryOutput("MAX_ADJ_SPECIES_" + std::to_string(iVar), "max[A_rho*Y_" + std::to_string(iVar) + "]",ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the adjoint transported species.", HistoryFieldType::RESIDUAL);
     }
   }
+
+  if (config->GetKind_Species_Model() == SPECIES_MODEL::FLAMELET) {
+
+    AddHistoryOutput("MAX_ADJ_PROGRESS_VARIABLE", "max[PV]",ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the adjoint progress variable.", HistoryFieldType::RESIDUAL);
+    AddHistoryOutput("MAX_ADJ_TOTAL_ENTHALPY", "max[Enth]",ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the adjoint total enthalpy.", HistoryFieldType::RESIDUAL);
+    
+    for (unsigned short i_scalar = 0; i_scalar < config->GetNUserScalars(); i_scalar++) {
+      const auto& scalar_name = config->GetUserScalarName(i_scalar);
+      AddHistoryOutput("MAX_ADJ_" + scalar_name, "max[scalar_" + scalar_name + "]",ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the adjoint of " + scalar_name + " .", HistoryFieldType::RESIDUAL);
+    }
+  }
 }
 
 void CAdjFlowOutput::AddHistoryOutputFields_AdjScalarBGS_RES(const CConfig* config) {
@@ -107,11 +129,22 @@ void CAdjFlowOutput::AddHistoryOutputFields_AdjScalarBGS_RES(const CConfig* conf
     }
   }
 
-  if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
+  if (config->GetKind_Species_Model() == SPECIES_MODEL::SPECIES_TRANSPORT) {
     for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
       AddHistoryOutput("BGS_ADJ_SPECIES_" + std::to_string(iVar), "bgs[A_rho*Y_" + std::to_string(iVar) + "]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the adjoint transported species.", HistoryFieldType::RESIDUAL);
     }
   }
+
+  if (config->GetKind_Species_Model() == SPECIES_MODEL::FLAMELET) {
+
+    AddHistoryOutput("BGS_ADJ_PROGRESS_VARIABLE", "bgs[PV]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the adjoint progress variable.", HistoryFieldType::RESIDUAL);
+    AddHistoryOutput("BGS_ADJ_TOTAL_ENTHALPY", "bgs[Enth]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the adjoint total enthalpy.", HistoryFieldType::RESIDUAL);
+
+    for (unsigned short i_scalar = 0; i_scalar < config->GetNUserScalars(); i_scalar++) {
+      const auto& scalar_name = config->GetUserScalarName(i_scalar);
+      AddHistoryOutput("BGS_ADJ_" + scalar_name, "bgs[" + scalar_name + "]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the adjoint of " + scalar_name + " .", HistoryFieldType::RESIDUAL);
+    }
+  }
 }
 
 void CAdjFlowOutput::AddHistoryOutputFieldsAdjScalarLinsol(const CConfig* config) {
@@ -120,10 +153,15 @@ void CAdjFlowOutput::AddHistoryOutputFieldsAdjScalarLinsol(const CConfig* config
     AddHistoryOutput("LINSOL_RESIDUAL_TURB", "LinSolResTurb", ScreenOutputFormat::FIXED, "LINSOL", "Residual of the linear solver for turbulence.");
   }
 
-  if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
+  if (config->GetKind_Species_Model() == SPECIES_MODEL::SPECIES_TRANSPORT) {
     AddHistoryOutput("LINSOL_ITER_SPECIES", "LinSolIterSpecies", ScreenOutputFormat::INTEGER, "LINSOL", "Number of iterations of the linear solver for species solver.");
     AddHistoryOutput("LINSOL_RESIDUAL_SPECIES", "LinSolResSpecies", ScreenOutputFormat::FIXED, "LINSOL", "Residual of the linear solver for species solver.");
   }
+  
+  if (config->GetKind_Species_Model() == SPECIES_MODEL::FLAMELET) {
+    AddHistoryOutput("LINSOL_ITER_FLAMELET", "LinSolIterScalar", ScreenOutputFormat::INTEGER, "LINSOL", "Number of iterations of the linear solver for scalar solver.");
+    AddHistoryOutput("LINSOL_RESIDUAL_FLAMELET", "LinSolResScalar", ScreenOutputFormat::FIXED, "LINSOL", "Residual of the linear solver for scalar solver.");
+  }
 }
 // clang-format on
 
@@ -160,7 +198,7 @@ void CAdjFlowOutput::LoadHistoryDataAdjScalar(const CConfig* config, const CSolv
     }
   }
 
-  if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
+  if (config->GetKind_Species_Model() == SPECIES_MODEL::SPECIES_TRANSPORT) {
     for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
       SetHistoryOutputValue("RMS_ADJ_SPECIES_" + std::to_string(iVar), log10(adjspecies_solver->GetRes_RMS(iVar)));
       SetHistoryOutputValue("MAX_ADJ_SPECIES_" + std::to_string(iVar), log10(adjspecies_solver->GetRes_Max(iVar)));
@@ -173,6 +211,30 @@ void CAdjFlowOutput::LoadHistoryDataAdjScalar(const CConfig* config, const CSolv
     SetHistoryOutputValue("LINSOL_RESIDUAL_SPECIES", log10(adjspecies_solver->GetResLinSolver()));
   }
 
+  if (config->GetKind_Species_Model() == SPECIES_MODEL::FLAMELET) {
+
+      SetHistoryOutputValue("RMS_ADJ_PROGRESS_VARIABLE", log10(adjspecies_solver->GetRes_RMS(I_PROGVAR)));
+      SetHistoryOutputValue("MAX_ADJ_PROGRESS_VARIABLE", log10(adjspecies_solver->GetRes_Max(I_PROGVAR)));
+      SetHistoryOutputValue("RMS_ADJ_TOTAL_ENTHALPY", log10(adjspecies_solver->GetRes_RMS(I_ENTH)));
+      SetHistoryOutputValue("MAX_ADJ_TOTAL_ENTHALPY", log10(adjspecies_solver->GetRes_Max(I_ENTH)));
+      if (multiZone) {
+        SetHistoryOutputValue("BGS_ADJ_PROGRESS_VARIABLE", log10(adjspecies_solver->GetRes_BGS(I_PROGVAR)));
+        SetHistoryOutputValue("BGS_ADJ_TOTAL_ENTHALPY", log10(adjspecies_solver->GetRes_BGS(I_ENTH)));
+      }
+
+    for (unsigned short i_scalar = 0; i_scalar < config->GetNUserScalars(); i_scalar++) {
+      const auto& scalar_name = config->GetUserScalarName(i_scalar);
+      SetHistoryOutputValue("RMS_ADJ_" + scalar_name, log10(adjspecies_solver->GetRes_RMS(2 + i_scalar)));
+      SetHistoryOutputValue("MAX_ADJ_" + scalar_name, log10(adjspecies_solver->GetRes_Max(2 + i_scalar)));
+      if (multiZone) {
+        SetHistoryOutputValue("BGS_ADJ_" + scalar_name, log10(adjspecies_solver->GetRes_BGS(2 + i_scalar)));
+      }
+    }
+
+    SetHistoryOutputValue("LINSOL_ITER_FLAMELET", adjspecies_solver->GetIterLinSolver());
+    SetHistoryOutputValue("LINSOL_RESIDUAL_FLAMELET", log10(adjspecies_solver->GetResLinSolver()));
+  }
+
   ComputeSimpleCustomOutputs(config);
 }
 
@@ -194,12 +256,23 @@ void CAdjFlowOutput::SetVolumeOutputFieldsAdjScalarSolution(const CConfig* confi
     }
   }
 
-  if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
+  if (config->GetKind_Species_Model() == SPECIES_MODEL::SPECIES_TRANSPORT) {
     for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
       AddVolumeOutput("ADJ_SPECIES_" + std::to_string(iVar), "Adjoint_Species_" + std::to_string(iVar), "SOLUTION",
                       "Adjoint Species variable");
     }
   }
+
+  if (config->GetKind_Species_Model() == SPECIES_MODEL::FLAMELET) {
+
+    AddVolumeOutput("ADJ_PROGRESS_VARIABLE", "Adjoint_Progress_Variable", "SOLUTION", "Adjoint of the progress variable.");
+    AddVolumeOutput("ADJ_TOTAL_ENTHALPY", "Adjoint_Total_Enthalpy", "SOLUTION", "Adjoint of the total enthalphy.");
+
+    for (unsigned short i_scalar = 0; i_scalar < config->GetNUserScalars(); i_scalar++) {
+      const auto& scalar_name = config->GetUserScalarName(i_scalar);
+      AddVolumeOutput("ADJ_" + scalar_name, "Adjoint_" + scalar_name, "SOLUTION", "Adjoint of " + scalar_name);
+    }
+  }
 }
 
 void CAdjFlowOutput::SetVolumeOutputFieldsAdjScalarResidual(const CConfig* config) {
@@ -223,12 +296,23 @@ void CAdjFlowOutput::SetVolumeOutputFieldsAdjScalarResidual(const CConfig* confi
     }
   }
 
-  if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
+  if (config->GetKind_Species_Model() == SPECIES_MODEL::SPECIES_TRANSPORT) {
     for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
       AddVolumeOutput("RES_ADJ_SPECIES_" + std::to_string(iVar), "Residual_Adjoint_Species_" + std::to_string(iVar),
                       "RESIDUAL", "Residual of the adjoint Species variable");
     }
   }
+
+  if (config->GetKind_Species_Model() == SPECIES_MODEL::FLAMELET) {
+
+    AddVolumeOutput("RES_ADJ_PROGRESS_VARIABLE", "Residual_Adjoint_Progress_Variable", "RESIDUAL", "Residual of the adjoint of the progress variable");
+    AddVolumeOutput("RES_ADJ_TOTAL_ENTHALPY", "Residual_Adjoint_Total_Enthalpy", "RESIDUAL", "Residual of the adjoint of the total enthalpy");
+
+    for (unsigned short i_scalar = 0; i_scalar < config->GetNUserScalars(); i_scalar++) {
+      const auto& scalar_name = config->GetUserScalarName(i_scalar);
+      AddVolumeOutput("RES_ADJ_" + scalar_name, "Residual_Adjoint_" + scalar_name, "RESIDUAL", "Residual of the adjoint of " + scalar_name);
+    }
+  }
 }
 
 void CAdjFlowOutput::LoadVolumeDataAdjScalar(const CConfig* config, const CSolver* const* solver,
@@ -258,11 +342,26 @@ void CAdjFlowOutput::LoadVolumeDataAdjScalar(const CConfig* config, const CSolve
     }
   }
 
-  if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
+  if (config->GetKind_Species_Model() == SPECIES_MODEL::SPECIES_TRANSPORT) {
     for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
       SetVolumeOutputValue("ADJ_SPECIES_" + std::to_string(iVar), iPoint, Node_AdjSpecies->GetSolution(iPoint, iVar));
       SetVolumeOutputValue("RES_ADJ_SPECIES_" + std::to_string(iVar), iPoint,
                            Node_AdjSpecies->GetSolution(iPoint, iVar) - Node_AdjSpecies->GetSolution_Old(iPoint, iVar));
     }
   }
+
+  if (config->GetKind_Species_Model() == SPECIES_MODEL::FLAMELET) {
+
+      SetVolumeOutputValue("ADJ_PROGRESS_VARIABLE", iPoint, Node_AdjSpecies->GetSolution(iPoint, I_PROGVAR));
+      SetVolumeOutputValue("RES_ADJ_PROGRESS_VARIABLE", iPoint, Node_AdjSpecies->GetSolution(iPoint, I_PROGVAR) - Node_AdjSpecies->GetSolution_Old(iPoint, I_PROGVAR));
+      SetVolumeOutputValue("ADJ_TOTAL_ENTHALPY", iPoint, Node_AdjSpecies->GetSolution(iPoint, I_ENTH));
+      SetVolumeOutputValue("RES_ADJ_TOTAL_ENTHALPY", iPoint, Node_AdjSpecies->GetSolution(iPoint, I_ENTH) - Node_AdjSpecies->GetSolution_Old(iPoint, I_ENTH));
+
+    for (unsigned short i_scalar = 0; i_scalar < config->GetNUserScalars(); i_scalar++) {
+      const auto& scalar_name = config->GetUserScalarName(i_scalar);
+      SetVolumeOutputValue("ADJ_" + scalar_name, iPoint, Node_AdjSpecies->GetSolution(iPoint, 2 + i_scalar));
+      SetVolumeOutputValue("RES_ADJ_" + scalar_name, iPoint, Node_AdjSpecies->GetSolution(iPoint, 2 + i_scalar) - Node_AdjSpecies->GetSolution_Old(iPoint, 2 + i_scalar));
+    }
+  }
+
 }
diff --git a/SU2_CFD/src/output/CFlowCompOutput.cpp b/SU2_CFD/src/output/CFlowCompOutput.cpp
index a943f4dfb98..4cfe8b9f64c 100644
--- a/SU2_CFD/src/output/CFlowCompOutput.cpp
+++ b/SU2_CFD/src/output/CFlowCompOutput.cpp
@@ -250,6 +250,8 @@ void CFlowCompOutput::SetVolumeOutputFields(CConfig *config){
     AddVolumeOutput("Y_PLUS", "Y_Plus", "PRIMITIVE", "Non-dim. wall distance (Y-Plus)");
   }
 
+  SetVolumeOutputFieldsScalarPrimitive(config);
+
   //Residuals
   AddVolumeOutput("RES_DENSITY", "Residual_Density", "RESIDUAL", "Residual of the density");
   AddVolumeOutput("RES_MOMENTUM-X", "Residual_Momentum_x", "RESIDUAL", "Residual of the x-momentum component");
@@ -271,6 +273,12 @@ void CFlowCompOutput::SetVolumeOutputFields(CConfig *config){
     AddVolumeOutput("LIMITER_ENTHALPY", "Limiter_Enthalpy", "LIMITER", "Limiter value of the enthalpy");
   }
 
+  SetVolumeOutputFieldsScalarLimiter(config);
+
+  SetVolumeOutputFieldsScalarSource(config);
+
+  SetVolumeOutputFieldsScalarLookup(config);
+
   SetVolumeOutputFieldsScalarMisc(config);
 
   // Roe Low Dissipation
diff --git a/SU2_CFD/src/output/CFlowIncOutput.cpp b/SU2_CFD/src/output/CFlowIncOutput.cpp
index dbf63568bd7..0a500f187ba 100644
--- a/SU2_CFD/src/output/CFlowIncOutput.cpp
+++ b/SU2_CFD/src/output/CFlowIncOutput.cpp
@@ -38,6 +38,7 @@ CFlowIncOutput::CFlowIncOutput(CConfig *config, unsigned short nDim) : CFlowOutp
   heat = config->GetEnergy_Equation();
 
   weakly_coupled_heat = config->GetWeakly_Coupled_Heat();
+  flamelet = (config->GetKind_Species_Model() == SPECIES_MODEL::FLAMELET);
 
   streamwisePeriodic = (config->GetKind_Streamwise_Periodic() != ENUM_STREAMWISE_PERIODIC::NONE);
   streamwisePeriodic_temperature = config->GetStreamwise_Periodic_Temperature();
@@ -295,7 +296,7 @@ void CFlowIncOutput::SetVolumeOutputFields(CConfig *config){
   AddVolumeOutput("VELOCITY-Y", "Velocity_y", "SOLUTION", "y-component of the velocity vector");
   if (nDim == 3)
     AddVolumeOutput("VELOCITY-Z", "Velocity_z", "SOLUTION", "z-component of the velocity vector");
-  if (heat || weakly_coupled_heat)
+  if (heat || weakly_coupled_heat || flamelet)
     AddVolumeOutput("TEMPERATURE",  "Temperature","SOLUTION", "Temperature");
 
   SetVolumeOutputFieldsScalarSolution(config);
@@ -331,6 +332,8 @@ void CFlowIncOutput::SetVolumeOutputFields(CConfig *config){
 
   }
 
+  SetVolumeOutputFieldsScalarPrimitive(config);
+
   if (config->GetSAParsedOptions().bc) {
     AddVolumeOutput("INTERMITTENCY", "gamma_BC", "INTERMITTENCY", "Intermittency");
   }
@@ -352,10 +355,16 @@ void CFlowIncOutput::SetVolumeOutputFields(CConfig *config){
     AddVolumeOutput("LIMITER_VELOCITY-Y", "Limiter_Velocity_y", "LIMITER", "Limiter value of the y-velocity");
     if (nDim == 3)
       AddVolumeOutput("LIMITER_VELOCITY-Z", "Limiter_Velocity_z", "LIMITER", "Limiter value of the z-velocity");
-    if (heat || weakly_coupled_heat)
+    if (heat || weakly_coupled_heat || flamelet)
       AddVolumeOutput("LIMITER_TEMPERATURE", "Limiter_Temperature", "LIMITER", "Limiter value of the temperature");
   }
 
+  SetVolumeOutputFieldsScalarLimiter(config);
+
+  SetVolumeOutputFieldsScalarSource(config);
+
+  SetVolumeOutputFieldsScalarLookup(config);
+
   SetVolumeOutputFieldsScalarMisc(config);
 
   // Streamwise Periodicity
@@ -391,7 +400,7 @@ void CFlowIncOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolve
   if (nDim == 3)
     SetVolumeOutputValue("VELOCITY-Z", iPoint, Node_Flow->GetSolution(iPoint, 3));
 
-  if (heat) SetVolumeOutputValue("TEMPERATURE", iPoint, Node_Flow->GetSolution(iPoint, nDim+1));
+  if (heat || flamelet) SetVolumeOutputValue("TEMPERATURE", iPoint, Node_Flow->GetSolution(iPoint, nDim+1));
   if (weakly_coupled_heat) SetVolumeOutputValue("TEMPERATURE", iPoint, Node_Heat->GetSolution(iPoint, 0));
 
   // Radiation solver
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index 12189f04d69..4f7f94f0d02 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -27,6 +27,8 @@
 
 #include <sstream>
 #include <string>
+#include <sstream>
+#include <iomanip>
 
 #include "../../include/output/CFlowOutput.hpp"
 
@@ -77,7 +79,7 @@ void CFlowOutput::AddAnalyzeSurfaceOutput(const CConfig *config){
   } else if (rank == MASTER_NODE) {
     cout << "\nWARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)\n" << endl;
   }
-  if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
+  if (config->GetKind_Species_Model() == SPECIES_MODEL::SPECIES_TRANSPORT) {
     /// DESCRIPTION: Average Species
     for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
       AddHistoryOutput("SURFACE_SPECIES_" + std::to_string(iVar), "Avg_Species_" + std::to_string(iVar), ScreenOutputFormat::FIXED, "SPECIES_COEFF", "Total average species " + std::to_string(iVar) + " on all markers set in MARKER_ANALYZE", HistoryFieldType::COEFFICIENT);
@@ -119,7 +121,7 @@ void CFlowOutput::AddAnalyzeSurfaceOutput(const CConfig *config){
   AddHistoryOutputPerSurface("SURFACE_TOTAL_TEMPERATURE","Avg_TotalTemp",             ScreenOutputFormat::SCIENTIFIC, "FLOW_COEFF_SURF", Marker_Analyze, HistoryFieldType::COEFFICIENT);
   /// DESCRIPTION: Average total pressure
   AddHistoryOutputPerSurface("SURFACE_TOTAL_PRESSURE",   "Avg_TotalPress",            ScreenOutputFormat::SCIENTIFIC, "FLOW_COEFF_SURF", Marker_Analyze, HistoryFieldType::COEFFICIENT);
-  if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
+  if (config->GetKind_Species_Model() == SPECIES_MODEL::SPECIES_TRANSPORT) {
     /// DESCRIPTION: Average Species
     for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
       AddHistoryOutputPerSurface("SURFACE_SPECIES_" + std::to_string(iVar), "Avg_Species_" + std::to_string(iVar), ScreenOutputFormat::FIXED, "SPECIES_COEFF_SURF", Marker_Analyze, HistoryFieldType::COEFFICIENT);
@@ -127,7 +129,6 @@ void CFlowOutput::AddAnalyzeSurfaceOutput(const CConfig *config){
     /// DESCRIPTION: Species Variance
     AddHistoryOutputPerSurface("SURFACE_SPECIES_VARIANCE", "Species_Variance", ScreenOutputFormat::SCIENTIFIC, "SPECIES_COEFF_SURF", Marker_Analyze, HistoryFieldType::COEFFICIENT);
   }
-  /// END_GROUP
 }
 // clang-format on
 
@@ -149,7 +150,7 @@ void CFlowOutput::SetAnalyzeSurface(const CSolver* const*solver, const CGeometry
   const bool incompressible = config->GetKind_Regime() == ENUM_REGIME::INCOMPRESSIBLE;
   const bool energy         = config->GetEnergy_Equation();
   const bool streamwisePeriodic = (config->GetKind_Streamwise_Periodic() != ENUM_STREAMWISE_PERIODIC::NONE);
-  const bool species        = config->GetKind_Species_Model() != SPECIES_MODEL::NONE;
+  const bool species        = config->GetKind_Species_Model() == SPECIES_MODEL::SPECIES_TRANSPORT;
   const auto nSpecies       = config->GetnSpecies();
 
   const bool axisymmetric               = config->GetAxisymmetric();
@@ -378,7 +379,6 @@ void CFlowOutput::SetAnalyzeSurface(const CSolver* const*solver, const CGeometry
   Allreduce(Surface_MassFlow_Abs_Local, Surface_MassFlow_Abs_Total);
   Allreduce_su2activematrix(Surface_Species_Local, Surface_Species_Total);
 
-
   /*--- Compute the value of Surface_Area_Total, and Surface_Pressure_Total, and
    set the value in the config structure for future use ---*/
 
@@ -639,7 +639,7 @@ void CFlowOutput::SetAnalyzeSurfaceSpeciesVariance(const CSolver* const*solver,
   const unsigned short nMarker      = config->GetnMarker_All();
   const unsigned short Kind_Average = config->GetKind_Average();
 
-  const bool species        = config->GetKind_Species_Model() != SPECIES_MODEL::NONE;
+  const bool species        = config->GetKind_Species_Model() == SPECIES_MODEL::SPECIES_TRANSPORT;
   const auto nSpecies       = config->GetnSpecies();
 
   const bool axisymmetric               = config->GetAxisymmetric();
@@ -753,7 +753,7 @@ void CFlowOutput::ConvertVariableSymbolsToIndices(const CPrimitiveIndices<unsign
   for (const auto& items : nameToIndex) {
     knownVariables << items.first + '\n';
   }
-  knownVariables << "TURB[0,1,...]\nRAD[0,1,...]\nSPECIES[0,1,...]\n";
+  knownVariables << "TURB[0,1,...]\nRAD[0,1,...]\nSPECIES[0,1,...]\nSCALAR[0,1,...]\n";
 
   auto IndexOfVariable = [](const map<std::string, unsigned long>& nameToIndex, const std::string& var) {
     /*--- Primitives of the flow solver. ---*/
@@ -766,10 +766,11 @@ void CFlowOutput::ConvertVariableSymbolsToIndices(const CPrimitiveIndices<unsign
       /*--- Extract an int from "name[int]", nameLen is the length of "name". ---*/
       return std::stoi(std::string(s.begin() + nameLen + 1, s.end() - 1));
     };
+
     if (var.rfind("SPECIES", 0) == 0) return SPECIES_SOL * CustomOutput::MAX_VARS_PER_SOLVER + GetIndex(var, 7);
+    if (var.rfind("SCALAR", 0) == 0) return SPECIES_SOL * CustomOutput::MAX_VARS_PER_SOLVER + GetIndex(var, 6);
     if (var.rfind("TURB", 0) == 0) return TURB_SOL * CustomOutput::MAX_VARS_PER_SOLVER + GetIndex(var, 4);
     if (var.rfind("RAD", 0) == 0) return RAD_SOL * CustomOutput::MAX_VARS_PER_SOLVER + GetIndex(var, 3);
-
     return CustomOutput::NOT_A_VARIABLE;
   };
 
@@ -984,10 +985,24 @@ void CFlowOutput::AddHistoryOutputFields_ScalarRMS_RES(const CConfig* config) {
     case TURB_TRANS_MODEL::NONE: break;
   }
 
-   if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
-    for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
-      AddHistoryOutput("RMS_SPECIES_" + std::to_string(iVar), "rms[rho*Y_" + std::to_string(iVar)+"]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of transported species.", HistoryFieldType::RESIDUAL);
+  switch (config->GetKind_Species_Model()) {
+    case SPECIES_MODEL::SPECIES_TRANSPORT: {
+      for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
+        AddHistoryOutput("RMS_SPECIES_" + std::to_string(iVar), "rms[rho*Y_" + std::to_string(iVar)+"]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of transported species.", HistoryFieldType::RESIDUAL);
+      }
+      break;
     }
+    case SPECIES_MODEL::FLAMELET: {
+      AddHistoryOutput("RMS_PROGRESS_VARIABLE", "rms[PV]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the progress variable equation.", HistoryFieldType::RESIDUAL);
+      AddHistoryOutput("RMS_TOTAL_ENTHALPY", "rms[Enth]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the total enthalpy equation.", HistoryFieldType::RESIDUAL);
+      /*--- auxiliary species transport ---*/
+      for (auto i_scalar = 0u; i_scalar < config->GetNUserScalars(); i_scalar++){
+        const auto& scalar_name = config->GetUserScalarName(i_scalar);
+        AddHistoryOutput("RMS_"+scalar_name, "rms["+scalar_name+"]", ScreenOutputFormat::FIXED  , "RMS_RES", "Root-mean squared residual of the "+scalar_name+" mass fraction equation." , HistoryFieldType::RESIDUAL);
+      }
+      break;
+    }
+    case SPECIES_MODEL::NONE: break;
   }
 }
 
@@ -1022,10 +1037,24 @@ void CFlowOutput::AddHistoryOutputFields_ScalarMAX_RES(const CConfig* config) {
       break;
   }
 
-  if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
-    for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
-      AddHistoryOutput("MAX_SPECIES_" + std::to_string(iVar), "max[rho*Y_" + std::to_string(iVar)+"]", ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of transported species.", HistoryFieldType::RESIDUAL);
+  switch (config->GetKind_Species_Model()) {
+    case SPECIES_MODEL::SPECIES_TRANSPORT: {
+      for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
+        AddHistoryOutput("MAX_SPECIES_" + std::to_string(iVar), "max[rho*Y_" + std::to_string(iVar)+"]", ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of transported species.", HistoryFieldType::RESIDUAL);
+      }
+      break;
     }
+    case SPECIES_MODEL::FLAMELET: {
+      AddHistoryOutput("MAX_PROGRESS_VARIABLE", "max[PV]", ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the progress variable equation.", HistoryFieldType::RESIDUAL);
+      AddHistoryOutput("MAX_TOTAL_ENTHALPY", "max[Enth]", ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the total enthalpy equation.", HistoryFieldType::RESIDUAL);
+      /*--- auxiliary species transport ---*/
+      for (auto i_scalar = 0u; i_scalar < config->GetNUserScalars(); i_scalar++){
+        const auto& scalar_name = config->GetUserScalarName(i_scalar);
+        AddHistoryOutput("MAX_" + scalar_name, "max[" + scalar_name + "]", ScreenOutputFormat::FIXED  , "MAX_RES", "Maximum residual of the " + scalar_name + " mass fraction equation." , HistoryFieldType::RESIDUAL);
+      }
+      break;
+    }
+    case SPECIES_MODEL::NONE: break;
   }
 }
 
@@ -1059,10 +1088,24 @@ void CFlowOutput::AddHistoryOutputFields_ScalarBGS_RES(const CConfig* config) {
     case TURB_TRANS_MODEL::NONE: break;
   }
 
-  if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
-    for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
-      AddHistoryOutput("BGS_SPECIES_" + std::to_string(iVar), "bgs[rho*Y_" + std::to_string(iVar)+"]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of transported species.", HistoryFieldType::RESIDUAL);
+  switch (config->GetKind_Species_Model()) {
+    case SPECIES_MODEL::SPECIES_TRANSPORT: {
+      for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
+        AddHistoryOutput("BGS_SPECIES_" + std::to_string(iVar), "bgs[rho*Y_" + std::to_string(iVar)+"]", ScreenOutputFormat::FIXED, "BGS_RES", "Maximum residual of transported species.", HistoryFieldType::RESIDUAL);
+      }
+      break;
     }
+    case SPECIES_MODEL::FLAMELET: {
+      AddHistoryOutput("BGS_PROGRESS_VARIABLE", "bgs[PV]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the progress variable equation.", HistoryFieldType::RESIDUAL);
+      AddHistoryOutput("BGS_TOTAL_ENTHALPY", "bgs[Enth]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the total enthalpy equation.", HistoryFieldType::RESIDUAL);
+      /*--- auxiliary species transport ---*/
+      for (auto i_scalar = 0u; i_scalar < config->GetNUserScalars(); i_scalar++){
+        const auto& scalar_name = config->GetUserScalarName(i_scalar);
+        AddHistoryOutput("BGS_"+scalar_name, "bgs["+scalar_name+"]", ScreenOutputFormat::FIXED  , "BGS_RES", "BGS residual of the "+scalar_name+" mass fraction equation." , HistoryFieldType::RESIDUAL);
+      }
+      break;
+    }
+    case SPECIES_MODEL::NONE: break;
   }
 }
 
@@ -1077,9 +1120,18 @@ void CFlowOutput::AddHistoryOutputFieldsScalarLinsol(const CConfig* config) {
     AddHistoryOutput("LINSOL_RESIDUAL_TRANS", "LinSolResTrans", ScreenOutputFormat::FIXED, "LINSOL", "Residual of the linear solver for transition solver.");
   }
 
-  if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
-    AddHistoryOutput("LINSOL_ITER_SPECIES", "LinSolIterSpecies", ScreenOutputFormat::INTEGER, "LINSOL", "Number of iterations of the linear solver for species solver.");
-    AddHistoryOutput("LINSOL_RESIDUAL_SPECIES", "LinSolResSpecies", ScreenOutputFormat::FIXED, "LINSOL", "Residual of the linear solver for species solver.");
+  switch (config->GetKind_Species_Model()) {
+    case SPECIES_MODEL::SPECIES_TRANSPORT: {
+      AddHistoryOutput("LINSOL_ITER_SPECIES", "LinSolIterSpecies", ScreenOutputFormat::INTEGER, "LINSOL", "Number of iterations of the linear solver for species solver.");
+      AddHistoryOutput("LINSOL_RESIDUAL_SPECIES", "LinSolResSpecies", ScreenOutputFormat::FIXED, "LINSOL", "Residual of the linear solver for species solver.");
+      break;
+    }
+    case SPECIES_MODEL::FLAMELET: {
+      AddHistoryOutput("LINSOL_ITER_FLAMELET", "LinSolIterSpecies", ScreenOutputFormat::INTEGER, "LINSOL", "Number of iterations of the linear solver for flamelet solver.");
+      AddHistoryOutput("LINSOL_RESIDUAL_FLAMELET", "LinSolResSpecies", ScreenOutputFormat::FIXED, "LINSOL", "Residual of the linear solver for flamelet solver.");
+      break;
+    }
+    case SPECIES_MODEL::NONE: break;
   }
 }
 // clang-format on
@@ -1130,17 +1182,41 @@ void CFlowOutput::LoadHistoryDataScalar(const CConfig* config, const CSolver* co
     case TURB_TRANS_MODEL::NONE: break;
   }
 
-  if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
-    for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
-      SetHistoryOutputValue("RMS_SPECIES_" + std::to_string(iVar), log10(solver[SPECIES_SOL]->GetRes_RMS(iVar)));
-      SetHistoryOutputValue("MAX_SPECIES_" + std::to_string(iVar), log10(solver[SPECIES_SOL]->GetRes_Max(iVar)));
-      if (multiZone) {
-        SetHistoryOutputValue("BGS_SPECIES_" + std::to_string(iVar), log10(solver[SPECIES_SOL]->GetRes_BGS(iVar)));
+  switch(config->GetKind_Species_Model()) {
+    case SPECIES_MODEL::SPECIES_TRANSPORT: {
+      for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
+        SetHistoryOutputValue("RMS_SPECIES_" + std::to_string(iVar), log10(solver[SPECIES_SOL]->GetRes_RMS(iVar)));
+        SetHistoryOutputValue("MAX_SPECIES_" + std::to_string(iVar), log10(solver[SPECIES_SOL]->GetRes_Max(iVar)));
+        if (multiZone) {
+          SetHistoryOutputValue("BGS_SPECIES_" + std::to_string(iVar), log10(solver[SPECIES_SOL]->GetRes_BGS(iVar)));
+        }
       }
+      SetHistoryOutputValue("LINSOL_ITER_SPECIES", solver[SPECIES_SOL]->GetIterLinSolver());
+      SetHistoryOutputValue("LINSOL_RESIDUAL_SPECIES", log10(solver[SPECIES_SOL]->GetResLinSolver()));
+      break;
     }
 
-    SetHistoryOutputValue("LINSOL_ITER_SPECIES", solver[SPECIES_SOL]->GetIterLinSolver());
-    SetHistoryOutputValue("LINSOL_RESIDUAL_SPECIES", log10(solver[SPECIES_SOL]->GetResLinSolver()));
+    case SPECIES_MODEL::FLAMELET: {
+      SetHistoryOutputValue("RMS_PROGRESS_VARIABLE", log10(solver[SPECIES_SOL]->GetRes_RMS(I_PROGVAR)));
+      SetHistoryOutputValue("MAX_PROGRESS_VARIABLE", log10(solver[SPECIES_SOL]->GetRes_Max(I_PROGVAR)));
+      SetHistoryOutputValue("RMS_TOTAL_ENTHALPY", log10(solver[SPECIES_SOL]->GetRes_RMS(I_ENTH)));
+      SetHistoryOutputValue("MAX_TOTAL_ENTHALPY", log10(solver[SPECIES_SOL]->GetRes_Max(I_ENTH)));
+      /*--- auxiliary species transport ---*/
+      for (unsigned short iReactant=0; iReactant<config->GetNUserScalars(); iReactant++){
+        const auto& species_name = config->GetUserScalarName(iReactant);
+        SetHistoryOutputValue("RMS_" + species_name, log10(solver[SPECIES_SOL]->GetRes_RMS(config->GetNControlVars() + iReactant)));
+        SetHistoryOutputValue("MAX_" + species_name, log10(solver[SPECIES_SOL]->GetRes_Max(config->GetNControlVars() + iReactant)));
+        if (multiZone) {
+          SetHistoryOutputValue("BGS_" + species_name, log10(solver[SPECIES_SOL]->GetRes_BGS(config->GetNControlVars() + iReactant)));
+        }
+      }
+
+      SetHistoryOutputValue("LINSOL_ITER_FLAMELET", solver[SPECIES_SOL]->GetIterLinSolver());
+      SetHistoryOutputValue("LINSOL_RESIDUAL_FLAMELET", log10(solver[SPECIES_SOL]->GetResLinSolver()));
+      break;
+    }
+
+    case SPECIES_MODEL::NONE: break;
   }
 }
 
@@ -1171,10 +1247,24 @@ void CFlowOutput::SetVolumeOutputFieldsScalarSolution(const CConfig* config){
       break;
   }
 
-  if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
-    for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
-      AddVolumeOutput("SPECIES_" + std::to_string(iVar), "Species_" + std::to_string(iVar), "SOLUTION", "Species_" + std::to_string(iVar) + " mass fraction");
-    }
+  switch (config->GetKind_Species_Model()) {
+    case SPECIES_MODEL::SPECIES_TRANSPORT:
+      for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++){
+        AddVolumeOutput("SPECIES_" + std::to_string(iVar), "Species_" + std::to_string(iVar), "SOLUTION", "Species_" + std::to_string(iVar) + " mass fraction");
+      }
+      break;
+    case SPECIES_MODEL::FLAMELET:
+      AddVolumeOutput("PROGVAR", "Progress_Variable", "SOLUTION", "Progress variable");
+      AddVolumeOutput("ENTHALPY", "Total_Enthalpy", "SOLUTION", "Total enthalpy");
+      /*--- auxiliary species ---*/
+      for (unsigned short iReactant=0; iReactant<config->GetNUserScalars(); iReactant++) {
+        const auto& species_name = config->GetUserScalarName(iReactant);
+        AddVolumeOutput(species_name, species_name, "SOLUTION", species_name + "Mass fraction solution");
+      }
+
+      break;
+    case SPECIES_MODEL::NONE:
+      break;
   }
 }
 
@@ -1195,6 +1285,25 @@ void CFlowOutput::SetVolumeOutputFieldsScalarResidual(const CConfig* config) {
       break;
   }
 
+  switch (config->GetKind_Species_Model()) {
+    case SPECIES_MODEL::SPECIES_TRANSPORT:
+      for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++){
+        AddVolumeOutput("RES_SPECIES_" + std::to_string(iVar), "Residual_Species_" + std::to_string(iVar), "RESIDUAL", "Residual of the transported species " + std::to_string(iVar));
+      }
+      break;
+    case SPECIES_MODEL::FLAMELET:
+      AddVolumeOutput("RES_PROGVAR", "Residual_Progress_Variable", "RESIDUAL", "Residual of progress variable");
+      AddVolumeOutput("RES_ENTHALPY", "Residual_Total_Enthalpy", "RESIDUAL", "Residual of total enthalpy");
+      /*--- residuals for auxiliary species transport equations ---*/
+      for (unsigned short iReactant=0; iReactant<config->GetNUserScalars(); iReactant++){
+        const auto& species_name = config->GetUserScalarName(iReactant);
+        AddVolumeOutput("RES_" + species_name, "Residual_" + species_name, "RESIDUAL", "Residual of the " + species_name + " equation");
+      }
+      break;
+    case SPECIES_MODEL::NONE:
+      break;
+  }
+
   switch (config->GetKind_Trans_Model()) {
     case TURB_TRANS_MODEL::LM:
       AddVolumeOutput("RES_INTERMITTENCY", "Residual_LM_intermittency", "RESIDUAL", "Residual of LM intermittency");
@@ -1204,16 +1313,11 @@ void CFlowOutput::SetVolumeOutputFieldsScalarResidual(const CConfig* config) {
     case TURB_TRANS_MODEL::NONE:
       break;
   }
-
-  if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
-    for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++){
-      AddVolumeOutput("RES_SPECIES_" + std::to_string(iVar), "Residual_Species_" + std::to_string(iVar), "RESIDUAL", "Residual of the transported species " + std::to_string(iVar));
-    }
-  }
 }
 
-void CFlowOutput::SetVolumeOutputFieldsScalarMisc(const CConfig* config) {
-  /*--- Place "PRIMITIVE", "LIMITER", and other groups here. ---*/
+
+void CFlowOutput::SetVolumeOutputFieldsScalarLimiter(const CConfig* config) {
+  /*--- Only place outputs of the "SOLUTION" group for species transport here. ---*/
 
   if (config->GetKind_SlopeLimit_Turb() != LIMITER::NONE) {
     switch (TurbModelFamily(config->GetKind_Turb_Model())) {
@@ -1231,15 +1335,41 @@ void CFlowOutput::SetVolumeOutputFieldsScalarMisc(const CConfig* config) {
     }
   }
 
-  if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
-    if (config->GetKind_SlopeLimit_Species() != LIMITER::NONE) {
-      for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++)
-        AddVolumeOutput("LIMITER_SPECIES_" + std::to_string(iVar), "Limiter_Species_" + std::to_string(iVar), "LIMITER", "Limiter value of the transported species " + std::to_string(iVar));
-    }
-    for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
-      AddVolumeOutput("DIFFUSIVITY_" + std::to_string(iVar), "Diffusivity_" + std::to_string(iVar), "PRIMITIVE", "Diffusivity of the transported species " + std::to_string(iVar));
+  if (config->GetKind_SlopeLimit_Species() != LIMITER::NONE) {
+    switch (config->GetKind_Species_Model()) {
+      case SPECIES_MODEL::SPECIES_TRANSPORT:
+        for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++)
+          AddVolumeOutput("LIMITER_SPECIES_" + std::to_string(iVar), "Limiter_Species_" + std::to_string(iVar), "LIMITER", "Limiter value of the transported species " + std::to_string(iVar));
+      break;
+      case SPECIES_MODEL::FLAMELET:
+        AddVolumeOutput("LIMITER_PROGVAR", "Limiter_Progress_Variable", "LIMITER", "Limiter of progress variable");
+        AddVolumeOutput("LIMITER_ENTHALPY", "Limiter_Total_Enthalpy", "LIMITER", "Limiter of total enthalpy");
+        /*--- limiter for auxiliary species transport ---*/
+        for (unsigned short iReactant=0; iReactant < config->GetNUserScalars(); iReactant++) {
+          const auto& species_name = config->GetUserScalarName(iReactant);
+          AddVolumeOutput("LIMITER_" + species_name, "LIMITER_" + species_name, "LIMITER", "Limiter value for the " + species_name + " equation");
+        }
+      break;
+      case SPECIES_MODEL::NONE:
+        break;
     }
   }
+}
+
+void CFlowOutput::SetVolumeOutputFieldsScalarPrimitive(const CConfig* config) {
+  /*--- Only place outputs of the "PRIMITIVE" group for scalar transport here. ---*/
+
+  switch (config->GetKind_Species_Model()) {
+    case SPECIES_MODEL::SPECIES_TRANSPORT:
+      for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++){
+        AddVolumeOutput("DIFFUSIVITY_" + std::to_string(iVar), "Diffusivity_" + std::to_string(iVar), "PRIMITIVE", "Diffusivity of the transported species " + std::to_string(iVar));
+      }
+      break;
+    case SPECIES_MODEL::FLAMELET:
+      break;
+    case SPECIES_MODEL::NONE:
+      break;
+  }
 
   switch (config->GetKind_Trans_Model()) {
     case TURB_TRANS_MODEL::LM:
@@ -1256,6 +1386,51 @@ void CFlowOutput::SetVolumeOutputFieldsScalarMisc(const CConfig* config) {
     AddVolumeOutput("EDDY_VISCOSITY", "Eddy_Viscosity", "PRIMITIVE", "Turbulent eddy viscosity");
   }
 
+}
+
+void CFlowOutput::SetVolumeOutputFieldsScalarSource(const CConfig* config) {
+  /*--- Only place outputs of the "SOURCE" group for scalar transport here. ---*/
+
+  switch (config->GetKind_Species_Model()) {
+    case SPECIES_MODEL::SPECIES_TRANSPORT:
+      break;
+    case SPECIES_MODEL::FLAMELET:
+      AddVolumeOutput("SOURCE_PROGVAR", "Source_Progress_Variable", "SOURCE", "Source Progress Variable");
+      /*--- no source term for enthalpy ---*/
+      /*--- auxiliary species source terms ---*/
+      for (unsigned short iReactant=0; iReactant<config->GetNUserScalars(); iReactant++) {
+        const auto& species_name = config->GetUserScalarName(iReactant);
+        AddVolumeOutput("SOURCE_" + species_name, "Source_" + species_name, "SOURCE", "Source " + species_name);
+      }
+      break;
+    case SPECIES_MODEL::NONE:
+      break;
+  }
+}
+
+
+void CFlowOutput::SetVolumeOutputFieldsScalarLookup(const CConfig* config) {
+  /*--- Only place outputs of the "LOOKUP" group for scalar transport here. ---*/
+
+  switch (config->GetKind_Species_Model()) {
+    case SPECIES_MODEL::SPECIES_TRANSPORT:
+      break;
+    case SPECIES_MODEL::FLAMELET:
+      for (int i_lookup = 0; i_lookup < config->GetNLookups(); ++i_lookup) {
+        string strname1 = "lookup_" + config->GetLUTLookupName(i_lookup);
+        AddVolumeOutput(config->GetLUTLookupName(i_lookup), strname1,"LOOKUP", config->GetLUTLookupName(i_lookup));
+      }
+
+      AddVolumeOutput("TABLE_MISSES"       , "Table_misses"       , "LOOKUP", "Lookup table misses");
+      break;
+    case SPECIES_MODEL::NONE:
+      break;
+  }
+}
+
+void CFlowOutput::SetVolumeOutputFieldsScalarMisc(const CConfig* config) {
+  /*--- Only place outputs of the group for scalar transport here that do not fit in other categories. ---*/
+
   if (config->GetSAParsedOptions().bc) {
     AddVolumeOutput("INTERMITTENCY", "gamma_BC", "INTERMITTENCY", "Intermittency");
   }
@@ -1351,16 +1526,57 @@ void CFlowOutput::LoadVolumeDataScalar(const CConfig* config, const CSolver* con
     SetVolumeOutputValue("WALL_DISTANCE", iPoint, Node_Geo->GetWall_Distance(iPoint));
   }
 
-  if (config->GetKind_Species_Model() != SPECIES_MODEL::NONE) {
-    const auto Node_Species = solver[SPECIES_SOL]->GetNodes();
+  switch (config->GetKind_Species_Model()) {
 
-    for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
-      SetVolumeOutputValue("SPECIES_" + std::to_string(iVar), iPoint, Node_Species->GetSolution(iPoint, iVar));
-      SetVolumeOutputValue("RES_SPECIES_" + std::to_string(iVar), iPoint, solver[SPECIES_SOL]->LinSysRes(iPoint, iVar));
-      SetVolumeOutputValue("DIFFUSIVITY_"+ std::to_string(iVar), iPoint, Node_Species->GetDiffusivity(iPoint,iVar));
-      if (config->GetKind_SlopeLimit_Species() != LIMITER::NONE)
-        SetVolumeOutputValue("LIMITER_SPECIES_" + std::to_string(iVar), iPoint, Node_Species->GetLimiter(iPoint, iVar));
+    case SPECIES_MODEL::SPECIES_TRANSPORT: {
+      const auto Node_Species = solver[SPECIES_SOL]->GetNodes();
+      for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) {
+        SetVolumeOutputValue("SPECIES_" + std::to_string(iVar), iPoint, Node_Species->GetSolution(iPoint, iVar));
+        SetVolumeOutputValue("RES_SPECIES_" + std::to_string(iVar), iPoint, solver[SPECIES_SOL]->LinSysRes(iPoint, iVar));
+        SetVolumeOutputValue("DIFFUSIVITY_"+ std::to_string(iVar), iPoint, Node_Species->GetDiffusivity(iPoint,iVar));
+        if (config->GetKind_SlopeLimit_Species() != LIMITER::NONE)
+          SetVolumeOutputValue("LIMITER_SPECIES_" + std::to_string(iVar), iPoint, Node_Species->GetLimiter(iPoint, iVar));
+      }
+      break;
+    }
+
+    case SPECIES_MODEL::FLAMELET: {
+      const auto Node_Species = solver[SPECIES_SOL]->GetNodes();
+
+      SetVolumeOutputValue("PROGVAR", iPoint, Node_Species->GetSolution(iPoint, I_PROGVAR));
+      SetVolumeOutputValue("ENTHALPY", iPoint, Node_Species->GetSolution(iPoint, I_ENTH));
+      SetVolumeOutputValue("SOURCE_PROGVAR", iPoint, Node_Species->GetScalarSources(iPoint)[I_PROGVAR]);
+      SetVolumeOutputValue("RES_PROGVAR", iPoint, solver[SPECIES_SOL]->LinSysRes(iPoint, I_PROGVAR));
+      SetVolumeOutputValue("RES_ENTHALPY", iPoint, solver[SPECIES_SOL]->LinSysRes(iPoint, I_ENTH));
+      SetVolumeOutputValue("TABLE_MISSES", iPoint, su2double(Node_Species->GetTableMisses(iPoint)));
+
+      /*--- auxiliary species transport equations ---*/
+      for (unsigned short i_scalar=0; i_scalar<config->GetNUserScalars(); i_scalar++) {
+        const auto& scalar_name = config->GetUserScalarName(i_scalar);
+        SetVolumeOutputValue(scalar_name, iPoint, Node_Species->GetSolution(iPoint, config->GetNControlVars() + i_scalar));
+        SetVolumeOutputValue("SOURCE_" + scalar_name, iPoint, Node_Species->GetScalarSources(iPoint)[config->GetNControlVars() + i_scalar]);
+        SetVolumeOutputValue("RES_" + scalar_name, iPoint, solver[SPECIES_SOL]->LinSysRes(iPoint, config->GetNControlVars() + i_scalar));
+      }
+
+      if (config->GetKind_SlopeLimit_Species() != LIMITER::NONE) {
+        SetVolumeOutputValue("LIMITER_PROGVAR", iPoint, Node_Species->GetLimiter(iPoint, I_PROGVAR));
+        SetVolumeOutputValue("LIMITER_ENTHALPY", iPoint, Node_Species->GetLimiter(iPoint, I_ENTH));
+        /*--- limiter for auxiliary species transport equations ---*/
+        for (unsigned short i_scalar=0; i_scalar<config->GetNUserScalars(); i_scalar++) {
+          const auto& scalar_name = config->GetUserScalarName(i_scalar);
+          SetVolumeOutputValue("LIMITER_" + scalar_name, iPoint, Node_Species->GetLimiter(iPoint, config->GetNControlVars() + i_scalar));
+        }
+      }
+
+      /*--- variables that we look up from the LUT ---*/
+      for (int i_lookup = 0; i_lookup < config->GetNLookups(); ++i_lookup) {
+        if (config->GetLUTLookupName(i_lookup)!="NULL")
+          SetVolumeOutputValue(config->GetLUTLookupName(i_lookup), iPoint, Node_Species->GetScalarLookups(iPoint)[i_lookup]);
+      }
+
+      break;
     }
+    case SPECIES_MODEL::NONE: break;
   }
 }
 
@@ -2514,6 +2730,10 @@ void CFlowOutput::WriteForcesBreakdown(const CConfig* config, const CSolver* flo
              << config->GetTemperature_Critical() / config->GetTemperature_Ref() << "\n";
         break;
 
+     case FLUID_FLAMELET:
+        file << "Fluid Model: FLAMELET \n";
+        break;
+
       case COOLPROP: {
         CCoolProp auxFluidModel(config->GetFluid_Name());
         file << "Fluid Model: CoolProp library \n";
@@ -2833,6 +3053,12 @@ void CFlowOutput::WriteForcesBreakdown(const CConfig* config, const CSolver* flo
         else file << " psf.\n";
         break;
 
+      case FLUID_FLAMELET:
+        file << "Fluid model: FLUID_FLAMELET \n";
+        if (si_units) file << " Pa.\n";
+        else file << " psf.\n";
+        break;
+
       case INC_IDEAL_GAS_POLY:
         file << "Fluid Model: INC_IDEAL_GAS_POLY \n";
         file << "Variable density incompressible flow using ideal gas law.\n";
@@ -2867,6 +3093,13 @@ void CFlowOutput::WriteForcesBreakdown(const CConfig* config, const CSolver* flo
           file << "Laminar Viscosity (non-dim): " << config->GetMu_ConstantND() << "\n";
           break;
 
+        case VISCOSITYMODEL::FLAMELET:
+          file << "Viscosity Model: FLAMELET  \n";
+          if (si_units) file << " N.s/m^2.\n";
+          else file << " lbf.s/ft^2.\n";
+          file << "Laminar Viscosity (non-dim): " << config->GetMu_ConstantND() << "\n";
+          break;
+
         case VISCOSITYMODEL::COOLPROP:
           file << "Viscosity Model: CoolProp \n";
           break;
@@ -2920,6 +3153,12 @@ void CFlowOutput::WriteForcesBreakdown(const CConfig* config, const CSolver* flo
             file << "Conductivity Model: COOLPROP \n";
             break;
 
+          case CONDUCTIVITYMODEL::FLAMELET:
+            file << "Conductivity Model: FLAMELET \n";
+            file << "Molecular Conductivity units: "  << " W/m^2.K.\n";
+            file << "Molecular Conductivity (non-dim): " << config->GetThermal_Conductivity_ConstantND() << "\n";
+            break;
+
           case CONDUCTIVITYMODEL::POLYNOMIAL:
             file << "Viscosity Model: POLYNOMIAL \n";
             file << "Kt(T) polynomial coefficients: \n  (";
diff --git a/SU2_CFD/src/output/CMultizoneOutput.cpp b/SU2_CFD/src/output/CMultizoneOutput.cpp
index a9e0833c422..2c63c04ed2b 100644
--- a/SU2_CFD/src/output/CMultizoneOutput.cpp
+++ b/SU2_CFD/src/output/CMultizoneOutput.cpp
@@ -173,7 +173,7 @@ void CMultizoneOutput::SetMultizoneHistoryOutputFields(const COutput* const* out
 
       /*--- Determine whether Maker_Analyze/Monitoring has to be used. ---*/
       auto* Marker = &Marker_Monitoring;
-      if ((group == "FLOW_COEFF_SURF") || (group == "SPECIES_COEFF_SURF"))
+      if ((group == "FLOW_COEFF_SURF") || (group == "SPECIES_COEFF_SURF") )
         Marker = &Marker_Analyze;
       else if (group != "AERO_COEFF_SURF" && group != "HEAT_SURF")
         SU2_MPI::Error("Per Surface output group unknown: " + group, CURRENT_FUNCTION);
diff --git a/SU2_CFD/src/output/CNEMOCompOutput.cpp b/SU2_CFD/src/output/CNEMOCompOutput.cpp
index d02a2d0c437..f639e3e2d1b 100644
--- a/SU2_CFD/src/output/CNEMOCompOutput.cpp
+++ b/SU2_CFD/src/output/CNEMOCompOutput.cpp
@@ -261,6 +261,8 @@ void CNEMOCompOutput::SetVolumeOutputFields(CConfig *config){
 
   }
 
+  SetVolumeOutputFieldsScalarPrimitive(config);
+
   //Residuals
   for(iSpecies = 0; iSpecies < nSpecies; iSpecies++)
     AddVolumeOutput("RES_DENSITY_" + std::to_string(iSpecies), "Residual_Density_" + std::to_string(iSpecies), "RESIDUAL", "Residual of species density " + std::to_string(iSpecies));
@@ -283,6 +285,12 @@ void CNEMOCompOutput::SetVolumeOutputFields(CConfig *config){
     AddVolumeOutput("LIMITER_ENERGY", "Limiter_Energy", "LIMITER", "Limiter value of the energy");
   }
 
+  SetVolumeOutputFieldsScalarLimiter(config);
+
+  SetVolumeOutputFieldsScalarSource(config);
+
+  SetVolumeOutputFieldsScalarLookup(config);
+
   SetVolumeOutputFieldsScalarMisc(config);
 
   AddCommonFVMOutputs(config);
diff --git a/SU2_CFD/src/output/COutput.cpp b/SU2_CFD/src/output/COutput.cpp
index ec61f9754e2..94d7c0a3cb3 100644
--- a/SU2_CFD/src/output/COutput.cpp
+++ b/SU2_CFD/src/output/COutput.cpp
@@ -263,7 +263,6 @@ void COutput::OutputScreenAndHistory(CConfig *config) {
 }
 
 void COutput::SetupCustomHistoryOutput(const std::string& expression, CustomHistoryOutput& output) const {
-
   std::vector<std::string> symbols;
   output.expression = mel::Parse<passivedouble>(expression, symbols);
 
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index 6fe92b813d3..5db213329f9 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -1093,6 +1093,7 @@ void CEulerSolver::SetNondimensionalization(CConfig *config, unsigned short iMes
     if (viscous) {
       GetFluidModel()->SetLaminarViscosityModel(config);
       GetFluidModel()->SetThermalConductivityModel(config);
+      GetFluidModel()->SetMassDiffusivityModel(config);
     }
 
   }
diff --git a/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp b/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
index 877611c3787..7beeb095bbe 100644
--- a/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
@@ -1092,6 +1092,7 @@ void CFEM_DG_EulerSolver::SetNondimensionalization(CConfig        *config,
   if (viscous) {
     FluidModel->SetLaminarViscosityModel(config);
     FluidModel->SetThermalConductivityModel(config);
+    FluidModel->SetMassDiffusivityModel(config); // nijso: TODO, needs to be tested
   }
 
   if (tkeNeeded) { Energy_FreeStreamND += Tke_FreeStreamND; };  config->SetEnergy_FreeStreamND(Energy_FreeStreamND);
diff --git a/SU2_CFD/src/solvers/CIncEulerSolver.cpp b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
index e148eb731d3..355b480eb53 100644
--- a/SU2_CFD/src/solvers/CIncEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
@@ -34,6 +34,7 @@
 #include "../../include/limiters/CLimiterDetails.hpp"
 #include "../../../Common/include/toolboxes/geometry_toolbox.hpp"
 #include "../../include/fluid/CFluidScalar.hpp"
+#include "../../include/fluid/CFluidFlamelet.hpp"
 #include "../../include/fluid/CFluidModel.hpp"
 
 
@@ -328,6 +329,16 @@ void CIncEulerSolver::SetNondimensionalization(CConfig *config, unsigned short i
       auxFluidModel->SetTDState_T(Temperature_FreeStream, config->GetSpecies_Init());
       break;
 
+    case FLUID_FLAMELET:
+
+      config->SetGas_Constant(UNIVERSAL_GAS_CONSTANT / (config->GetMolecular_Weight() / 1000.0));
+      Pressure_Thermodynamic = Density_FreeStream * Temperature_FreeStream * config->GetGas_Constant();
+      auxFluidModel = new CFluidFlamelet(config, Pressure_Thermodynamic);
+      auxFluidModel->SetTDState_T(Temperature_FreeStream, config->GetSpecies_Init());
+      config->SetPressure_Thermodynamic(Pressure_Thermodynamic);
+
+      break;
+
     default:
 
       SU2_MPI::Error("Fluid model not implemented for incompressible solver.", CURRENT_FUNCTION);
@@ -403,6 +414,9 @@ void CIncEulerSolver::SetNondimensionalization(CConfig *config, unsigned short i
   if (tkeNeeded) { Energy_FreeStream += Tke_FreeStream; };
   config->SetEnergy_FreeStream(Energy_FreeStream);
 
+  /*--- Auxilary (dimensional) FluidModel no longer needed. ---*/
+  delete auxFluidModel;
+
   /*--- Compute Mach number ---*/
 
   if (config->GetKind_FluidModel() == CONSTANT_DENSITY) {
@@ -449,11 +463,6 @@ void CIncEulerSolver::SetNondimensionalization(CConfig *config, unsigned short i
   const su2double MassDiffusivityND = config->GetDiffusivity_Constant() / (Velocity_Ref * Length_Ref);
   config->SetDiffusivity_ConstantND(MassDiffusivityND);
 
-
-  /*--- Delete the original (dimensional) FluidModel object. No fluid is used for inscompressible cases. ---*/
-
-  delete auxFluidModel;
-
   /*--- Create one final fluid model object per OpenMP thread to be able to use them in parallel.
    *    GetFluidModel() should be used to automatically access the "right" object of each thread. ---*/
 
@@ -478,6 +487,11 @@ void CIncEulerSolver::SetNondimensionalization(CConfig *config, unsigned short i
         fluidModel->SetTDState_T(Temperature_FreeStreamND, config->GetSpecies_Init());
         break;
 
+      case FLUID_FLAMELET:
+        fluidModel = new CFluidFlamelet(config, Pressure_Thermodynamic);
+        fluidModel->SetTDState_T(Temperature_FreeStreamND, config->GetSpecies_Init());
+        break;
+
       case INC_IDEAL_GAS_POLY:
         fluidModel = new CIncIdealGasPolynomial<N_POLY_COEFFS>(Gas_ConstantND, Pressure_ThermodynamicND);
         if (viscous) {
@@ -510,7 +524,7 @@ void CIncEulerSolver::SetNondimensionalization(CConfig *config, unsigned short i
 
       fluidModel->SetLaminarViscosityModel(config);
       fluidModel->SetThermalConductivityModel(config);
-
+      fluidModel->SetMassDiffusivityModel(config);
     }
 
   }
@@ -625,6 +639,15 @@ void CIncEulerSolver::SetNondimensionalization(CConfig *config, unsigned short i
         NonDimTable.PrintFooter();
         break;
 
+      case VISCOSITYMODEL::FLAMELET:
+        ModelTable << "FLAMELET";
+        if      (config->GetSystemMeasurements() == SI) Unit << "N.s/m^2";
+        else if (config->GetSystemMeasurements() == US) Unit << "lbf.s/ft^2";
+        NonDimTable << "Viscosity" << "--" << "--" << Unit.str() << config->GetMu_ConstantND();
+        Unit.str("");
+        NonDimTable.PrintFooter();
+        break;
+
       case VISCOSITYMODEL::COOLPROP:
         ModelTable << "COOLPROP_VISCOSITY";
         if      (config->GetSystemMeasurements() == SI) Unit << "N.s/m^2";
@@ -682,6 +705,13 @@ void CIncEulerSolver::SetNondimensionalization(CConfig *config, unsigned short i
         NonDimTable.PrintFooter();
         break;
 
+      case CONDUCTIVITYMODEL::FLAMELET:
+        ModelTable << "FLAMELET";
+        Unit << "W/m^2.K";
+        NonDimTable << "Molecular Cond." << "--" << "--" << Unit.str() << config->GetThermal_Conductivity_ConstantND();
+        Unit.str("");
+        break;
+
       case CONDUCTIVITYMODEL::COOLPROP:
         ModelTable << "COOLPROP";
         Unit << "W/m^2.K";
@@ -759,6 +789,23 @@ void CIncEulerSolver::SetNondimensionalization(CConfig *config, unsigned short i
       NonDimTable.PrintFooter();
       break;
 
+    case FLUID_FLAMELET:
+      ModelTable << "FLAMELET";
+      Unit << "N.m/kg.K";
+      NonDimTable << "Spec. Heat (Cp)" << "--" << "--" << Unit.str() << config->GetSpecific_Heat_CpND();
+      Unit.str("");
+      Unit << "g/mol";
+      NonDimTable << "Molecular weight" << "--" << "--" << Unit.str() << config->GetMolecular_Weight();
+      Unit.str("");
+      Unit << "N.m/kg.K";
+      NonDimTable << "Gas Constant" << "--" << config->GetGas_Constant_Ref() << Unit.str() << config->GetGas_ConstantND();
+      Unit.str("");
+      Unit << "Pa";
+      NonDimTable << "Therm. Pressure" << config->GetPressure_Thermodynamic() << config->GetPressure_Ref() << Unit.str() << config->GetPressure_ThermodynamicND();
+      Unit.str("");
+      NonDimTable.PrintFooter();
+      break;
+
     case INC_IDEAL_GAS_POLY:
       ModelTable << "INC_IDEAL_GAS_POLY";
       Unit.str("");
@@ -2904,8 +2951,6 @@ void CIncEulerSolver::GetOutlet_Properties(CGeometry *geometry, CConfig *config,
 
           if (geometry->nodes->GetDomain(iPoint)) {
 
-            V_outlet = nodes->GetPrimitive(iPoint);
-
             geometry->vertex[iMarker][iVertex]->GetNormal(Vector);
 
             su2double AxiFactor = 1.0;
@@ -2921,7 +2966,9 @@ void CIncEulerSolver::GetOutlet_Properties(CGeometry *geometry, CConfig *config,
               }
             }
 
-            Density      = V_outlet[prim_idx.Density()];
+            V_outlet = nodes->GetPrimitive(iPoint);
+
+            Density = V_outlet[prim_idx.Density()];
 
             Velocity2 = 0.0; Area = 0.0; MassFlow = 0.0;
 
@@ -2931,6 +2978,7 @@ void CIncEulerSolver::GetOutlet_Properties(CGeometry *geometry, CConfig *config,
               Velocity2 += Velocity[iDim] * Velocity[iDim];
               MassFlow += Vector[iDim] * AxiFactor * Density * Velocity[iDim];
             }
+
             Area = sqrt (Area);
 
             Outlet_MassFlow[iMarker] += MassFlow;
diff --git a/SU2_CFD/src/solvers/CSolver.cpp b/SU2_CFD/src/solvers/CSolver.cpp
index 4bd4c0616ee..a7d985811ff 100644
--- a/SU2_CFD/src/solvers/CSolver.cpp
+++ b/SU2_CFD/src/solvers/CSolver.cpp
@@ -3659,6 +3659,16 @@ void CSolver::LoadInletProfile(CGeometry **geometry,
           columnValue << config->GetInlet_SpeciesVal(Marker_Tag)[iVar] << "\t";
         }
         break;
+      case SPECIES_MODEL::FLAMELET:
+        /*--- 2-equation flamelet model ---*/
+        columnName << "PROGRESSVAR" << setw(24) << "ENTHALPYTOT" << setw(24);
+        columnValue << config->GetInlet_SpeciesVal(Marker_Tag)[0] << "\t" <<  config->GetInlet_SpeciesVal(Marker_Tag)[1]<<"\t";
+        /*--- auxiliary species transport equations ---*/
+        for (unsigned short iReactant = 0; iReactant < config->GetNUserScalars(); iReactant++) {
+          columnName << config->GetUserScalarName(iReactant) << setw(24);
+          columnValue << config->GetInlet_SpeciesVal(Marker_Tag)[config->GetNControlVars() + iReactant] << "\t";
+        }
+        break;
     }
 
     columnNames.push_back(columnName.str());
diff --git a/SU2_CFD/src/solvers/CSolverFactory.cpp b/SU2_CFD/src/solvers/CSolverFactory.cpp
index 02843124a4f..af9669fa392 100644
--- a/SU2_CFD/src/solvers/CSolverFactory.cpp
+++ b/SU2_CFD/src/solvers/CSolverFactory.cpp
@@ -52,6 +52,7 @@
 #include "../../include/solvers/CBaselineSolver_FEM.hpp"
 #include "../../include/solvers/CRadP1Solver.hpp"
 #include "../../include/solvers/CSpeciesSolver.hpp"
+#include "../../include/solvers/CSpeciesFlameletSolver.hpp"
 
 map<const CSolver*, SolverMetaData> CSolverFactory::allocatedSolvers;
 
@@ -398,7 +399,10 @@ CSolver* CSolverFactory::CreateSpeciesSolver(CSolver **solver, CGeometry *geomet
     if (adjoint){
       speciesSolver = new CDiscAdjSolver(geometry, config, solver[SPECIES_SOL], RUNTIME_SPECIES_SYS, iMGLevel);
     } else {
-      speciesSolver = new CSpeciesSolver(geometry, config, iMGLevel);
+      if (config->GetKind_Species_Model() == SPECIES_MODEL::SPECIES_TRANSPORT)
+        speciesSolver = new CSpeciesSolver(geometry, config, iMGLevel);
+      else if (config->GetKind_Species_Model() == SPECIES_MODEL::FLAMELET)
+        speciesSolver = new CSpeciesFlameletSolver(geometry, config, iMGLevel);
     }
   }
   return speciesSolver;
@@ -411,9 +415,9 @@ CSolver* CSolverFactory::CreateHeatSolver(CSolver **solver, CGeometry *geometry,
   /*--- Only allocate a heat solver if it should run standalone
    * or if the weakly coupled heat solver is enabled and no energy equation is included ---*/
 
-  if ((config->GetWeakly_Coupled_Heat() && !config->GetEnergy_Equation()) || config->GetHeatProblem()){
-    if (adjoint){
-      if (config->GetDiscrete_Adjoint()){
+  if ((config->GetWeakly_Coupled_Heat() && !config->GetEnergy_Equation()) || config->GetHeatProblem()) {
+    if (adjoint) {
+      if (config->GetDiscrete_Adjoint()) {
         heatSolver = new CDiscAdjSolver(geometry, config, solver[HEAT_SOL], RUNTIME_HEAT_SYS, iMGLevel);
       }
       else {
@@ -424,24 +428,24 @@ CSolver* CSolverFactory::CreateHeatSolver(CSolver **solver, CGeometry *geometry,
       heatSolver = new CHeatSolver(geometry, config, iMGLevel);
     }
   }
-  return heatSolver;
 
+  return heatSolver;
 }
 
 CSolver* CSolverFactory::CreateMeshSolver(CSolver **solver, CGeometry *geometry, CConfig *config, int iMGLevel, bool adjoint){
 
   CSolver *meshSolver = nullptr;
 
-  if (config->GetDeform_Mesh() && iMGLevel == MESH_0){
-    if (!adjoint){
+  if (config->GetDeform_Mesh() && iMGLevel == MESH_0) {
+    if (!adjoint) {
       meshSolver = new CMeshSolver(geometry, config);
     }
-    if (adjoint && config->GetDiscrete_Adjoint()){
+    if (adjoint && config->GetDiscrete_Adjoint()) {
       meshSolver = new CDiscAdjMeshSolver(geometry, config, solver[MESH_SOL]);
     }
   }
-  return meshSolver;
 
+  return meshSolver;
 }
 
 CSolver* CSolverFactory::CreateDGSolver(SUB_SOLVER_TYPE kindDGSolver, CGeometry *geometry, CConfig *config, int iMGLevel){
diff --git a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
new file mode 100644
index 00000000000..f79b12b232f
--- /dev/null
+++ b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
@@ -0,0 +1,511 @@
+/*!
+ * \file CSpeciesFlameletSolver.cpp
+ * \brief Main subroutines of CSpeciesFlameletSolver class
+ * \author D. Mayer, T. Economon, N. Beishuizen
+ * \version 7.5.1 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+
+#include "../../include/solvers/CSpeciesFlameletSolver.hpp"
+
+#include "../../../Common/include/parallelization/omp_structure.hpp"
+#include "../../../Common/include/toolboxes/geometry_toolbox.hpp"
+#include "../../include/fluid/CFluidFlamelet.hpp"
+#include "../../include/solvers/CSpeciesSolver.hpp"
+#include "../../include/variables/CFlowVariable.hpp"
+#include "../../include/variables/CSpeciesFlameletVariable.hpp"
+
+CSpeciesFlameletSolver::CSpeciesFlameletSolver(CGeometry* geometry, CConfig* config, unsigned short iMesh)
+    : CSpeciesSolver(geometry, config, true) {
+  /*--- Dimension of the problem. ---*/
+  nVar = config->GetNScalars();
+
+  Initialize(geometry, config, iMesh, nVar);
+
+  /*--- Initialize the solution to the far-field state everywhere. ---*/
+
+  nodes = new CSpeciesFlameletVariable(Solution_Inf, nPoint, nDim, nVar, config);
+  SetBaseClassPointerToNodes();
+
+  /*--- Store the initial CFL number for all grid points. ---*/
+
+  const su2double CFL = config->GetCFL(MGLevel) * config->GetCFLRedCoeff_Species();
+  SU2_OMP_FOR_STAT(omp_chunk_size)
+  for (auto iPoint = 0u; iPoint < nPoint; iPoint++) {
+    nodes->SetLocalCFL(iPoint, CFL);
+  }
+  END_SU2_OMP_FOR
+  Min_CFL_Local = CFL;
+  Max_CFL_Local = CFL;
+  Avg_CFL_Local = CFL;
+
+  /*--- Allocates a 3D array with variable "middle" sizes and init to 0. ---*/
+
+  auto Alloc3D = [](unsigned long M, const vector<unsigned long>& N, unsigned long P, vector<su2activematrix>& X) {
+    X.resize(M);
+    for (unsigned long i = 0; i < M; ++i) X[i].resize(N[i], P) = su2double(0.0);
+  };
+
+  /*--- Store the values of the temperature and the heat flux density at the boundaries,
+   used for coupling with a solid donor cell. ---*/
+  constexpr auto n_conjugate_var = 4u;
+
+  Alloc3D(nMarker, nVertex, n_conjugate_var, conjugate_var);
+  for (auto& x : conjugate_var) x = config->GetTemperature_FreeStreamND();
+
+  /*--- Add the solver name. ---*/
+  SolverName = "FLAMELET";
+}
+
+void CSpeciesFlameletSolver::Preprocessing(CGeometry* geometry, CSolver** solver_container, CConfig* config,
+                                           unsigned short iMesh, unsigned short iRKStep,
+                                           unsigned short RunTime_EqSystem, bool Output) {
+  const auto n_user_scalars = config->GetNUserScalars();
+  const auto n_control_vars = config->GetNControlVars();
+
+  vector<string> table_scalar_names(config->GetNScalars());
+  table_scalar_names[I_ENTH] = "EnthalpyTot";
+  table_scalar_names[I_PROGVAR] = "ProgressVariable";
+
+  /*--- auxiliary species transport equations---*/
+  for (size_t i_aux = 0; i_aux < n_user_scalars; i_aux++) {
+    table_scalar_names[n_control_vars + i_aux] = config->GetUserScalarName(i_aux);
+  }
+
+  /*--- we currently only need 1 source term from the LUT for the progress variable
+        and each auxiliary equations needs 2 source terms ---*/
+  unsigned short n_table_sources = 1 + 2 * n_user_scalars;
+
+  vector<string> table_source_names(n_table_sources);
+  table_source_names[I_SRC_TOT_PROGVAR] = "ProdRateTot_PV";
+  /*--- No source term for enthalpy ---*/
+
+  /*--- For the auxiliary equations, we use a positive (production) and a negative (consumption) term:
+        S_tot = S_PROD + S_CONS * Y ---*/
+
+  for (size_t i_aux = 0; i_aux < n_user_scalars; i_aux++) {
+    /*--- Order of the source terms: S_prod_1, S_cons_1, S_prod_2, S_cons_2, ...---*/
+    table_source_names[1 + 2 * i_aux] = config->GetUserSourceName(2 * i_aux);
+    table_source_names[1 + 2 * i_aux + 1] = config->GetUserSourceName(2 * i_aux + 1);
+  }
+
+  auto* flowNodes = su2staticcast_p<CFlowVariable*>(solver_container[FLOW_SOL]->GetNodes());
+
+  SU2_OMP_SAFE_GLOBAL_ACCESS(config->SetGlobalParam(config->GetKind_Solver(), RunTime_EqSystem);)
+
+  vector<string> table_lookup_names(config->GetNLookups());
+  for (int i_lookup = 0; i_lookup < config->GetNLookups(); ++i_lookup) {
+    table_lookup_names[i_lookup] = config->GetLUTLookupName(i_lookup);
+  }
+
+  SU2_OMP_FOR_STAT(omp_chunk_size)
+  for (auto i_point = 0u; i_point < nPoint; i_point++) {
+    CFluidModel* fluid_model_local = solver_container[FLOW_SOL]->GetFluidModel();
+    su2double* scalars = nodes->GetSolution(i_point);
+
+    /*--- Compute total source terms from the production and consumption. ---*/
+
+    vector<su2double> table_sources(n_table_sources);
+    unsigned long misses = fluid_model_local->GetLookUpTable()->LookUp_XY(table_source_names, table_sources,
+                                                                          scalars[I_PROGVAR], scalars[I_ENTH]);
+    nodes->SetTableMisses(i_point, misses);
+
+    /*--- The source term for progress variable is always positive, we clip from below to makes sure. --- */
+
+    vector<su2double> source_scalar(config->GetNScalars());
+    source_scalar[I_PROGVAR] = fmax(EPS, table_sources[I_SRC_TOT_PROGVAR]);
+    source_scalar[I_ENTH] = 0.0;
+
+    /*--- Source term for the auxiliary species transport equations. ---*/
+    for (size_t i_aux = 0; i_aux < config->GetNUserScalars(); i_aux++) {
+      /*--- The source term for the auxiliary equations consists of a production term and a consumption term:
+            S_TOT = S_PROD + S_CONS * Y ---*/
+      su2double y_aux = scalars[n_control_vars + i_aux];
+      su2double source_prod = table_sources[1 + 2 * i_aux];
+      su2double source_cons = table_sources[1 + 2 * i_aux + 1];
+      source_scalar[n_control_vars + i_aux] = source_prod + source_cons * y_aux;
+    }
+    for (auto i_scalar = 0u; i_scalar < nVar; i_scalar++)
+      nodes->SetScalarSource(i_point, i_scalar, source_scalar[i_scalar]);
+
+    vector<su2double> lookup_scalar(config->GetNLookups());
+    misses = fluid_model_local->GetLookUpTable()->LookUp_XY(table_lookup_names, lookup_scalar, scalars[I_PROGVAR],
+                                                            scalars[I_ENTH]);
+
+    for (auto i_lookup = 0u; i_lookup < config->GetNLookups(); i_lookup++) {
+      nodes->SetLookupScalar(i_point, lookup_scalar[i_lookup], i_lookup);
+    }
+
+    su2double T = flowNodes->GetTemperature(i_point);
+    fluid_model_local->SetTDState_T(T, scalars);
+    /*--- set the diffusivity in the fluid model to the diffusivity obtained from the lookup table ---*/
+    for (auto i_scalar = 0u; i_scalar < nVar; ++i_scalar) {
+      nodes->SetDiffusivity(i_point, fluid_model_local->GetMassDiffusivity(i_scalar), i_scalar);
+    }
+
+    if (!Output) LinSysRes.SetBlock_Zero(i_point);
+  }
+  END_SU2_OMP_FOR
+
+  /*--- Clear Residual and Jacobian. Upwind second order reconstruction and gradients ---*/
+  CommonPreprocessing(geometry, config, Output);
+}
+
+void CSpeciesFlameletSolver::SetInitialCondition(CGeometry** geometry, CSolver*** solver_container, CConfig* config,
+                                                 unsigned long ExtIter) {
+  const bool Restart = (config->GetRestart() || config->GetRestart_Flow());
+
+  if ((!Restart) && ExtIter == 0) {
+    if (rank == MASTER_NODE) {
+      cout << "Initializing progress variable and total enthalpy (using temperature)" << endl;
+    }
+
+    vector<su2double> scalar_init(nVar, 0.0);
+    const su2double* flame_init = config->GetFlameInit();
+    const su2double flame_offset[3] = {flame_init[0], flame_init[1], flame_init[2]};
+    const su2double flame_normal[3] = {flame_init[3], flame_init[4], flame_init[5]};
+    const su2double flame_thickness = flame_init[6];
+    const su2double flame_burnt_thickness = flame_init[7];
+
+    const su2double flamenorm = GeometryToolbox::Norm(nDim, flame_normal);
+    const su2double temp_inlet = config->GetInc_Temperature_Init();
+    su2double prog_inlet = config->GetSpecies_Init()[I_PROGVAR];
+    su2double enth_inlet = config->GetSpecies_Init()[I_ENTH];
+
+    su2double prog_burnt;
+    su2double prog_unburnt = 0.0;
+
+    if (rank == MASTER_NODE) {
+      cout << "initial condition: T = " << temp_inlet << endl;
+      cout << "initial condition: c = " << prog_inlet << endl;
+      cout << "initial condition: h = " << enth_inlet << endl;
+    }
+
+    su2double point_loc;
+
+    CFluidModel* fluid_model_local;
+
+    vector<string> look_up_tags;
+    vector<su2double*> look_up_data;
+
+    unsigned long n_not_iterated_local = 0;
+    unsigned long n_not_in_domain_local = 0;
+    unsigned long n_points_unburnt_local = 0;
+    unsigned long n_points_burnt_local = 0;
+    unsigned long n_points_flame_local = 0;
+    unsigned long n_not_iterated_global;
+    unsigned long n_not_in_domain_global;
+    unsigned long n_points_burnt_global;
+    unsigned long n_points_flame_global;
+    unsigned long n_points_unburnt_global;
+
+    for (unsigned long i_mesh = 0; i_mesh <= config->GetnMGLevels(); i_mesh++) {
+      fluid_model_local = solver_container[i_mesh][FLOW_SOL]->GetFluidModel();
+
+      prog_burnt = *fluid_model_local->GetLookUpTable()->GetTableLimitsX().second;
+      for (unsigned long i_point = 0; i_point < nPointDomain; i_point++) {
+        auto coords = geometry[i_mesh]->nodes->GetCoord(i_point);
+
+        /*--- Determine if point is above or below the plane, assuming the normal
+           is pointing towards the burned region. ---*/
+        point_loc = 0.0;
+        for (unsigned short i_dim = 0; i_dim < geometry[i_mesh]->GetnDim(); i_dim++) {
+          point_loc += flame_normal[i_dim] * (coords[i_dim] - flame_offset[i_dim]);
+        }
+
+        /*--- Compute the exact distance from point to plane. ---*/
+        point_loc = point_loc / flamenorm;
+
+        /* --- Unburnt region upstream of the flame. --- */
+        if (point_loc <= 0) {
+          scalar_init[I_PROGVAR] = prog_unburnt;
+          n_points_unburnt_local++;
+
+          /* --- Flame zone where we lineary increase from unburnt to burnt conditions. --- */
+        } else if ((point_loc > 0) && (point_loc <= flame_thickness)) {
+          scalar_init[I_PROGVAR] = prog_unburnt + point_loc * (prog_burnt - prog_unburnt) / flame_thickness;
+          n_points_flame_local++;
+
+          /* --- Burnt region behind the flame zone. --- */
+        } else if ((point_loc > flame_thickness) && (point_loc <= flame_thickness + flame_burnt_thickness)) {
+          scalar_init[I_PROGVAR] = prog_burnt;
+          n_points_burnt_local++;
+
+          /* --- Unburnt region downstream of the flame and burnt region. --- */
+        } else {
+          scalar_init[I_PROGVAR] = prog_unburnt;
+          n_points_unburnt_local++;
+        }
+
+        n_not_iterated_local += fluid_model_local->GetEnthFromTemp(enth_inlet, prog_inlet, temp_inlet, enth_inlet);
+        scalar_init[I_ENTH] = enth_inlet;
+
+        n_not_in_domain_local += fluid_model_local->GetLookUpTable()->LookUp_XY(
+            look_up_tags, look_up_data, scalar_init[I_PROGVAR], scalar_init[I_ENTH]);
+
+        /* --- Initialize the auxiliary transported scalars  (not controlling variables). --- */
+        for (int i_scalar = config->GetNControlVars(); i_scalar < config->GetNScalars(); ++i_scalar) {
+          scalar_init[i_scalar] = config->GetSpecies_Init()[i_scalar];
+        }
+
+        solver_container[i_mesh][SPECIES_SOL]->GetNodes()->SetSolution(i_point, scalar_init.data());
+      }
+
+      solver_container[i_mesh][SPECIES_SOL]->InitiateComms(geometry[i_mesh], config, SOLUTION);
+      solver_container[i_mesh][SPECIES_SOL]->CompleteComms(geometry[i_mesh], config, SOLUTION);
+
+      solver_container[i_mesh][FLOW_SOL]->InitiateComms(geometry[i_mesh], config, SOLUTION);
+      solver_container[i_mesh][FLOW_SOL]->CompleteComms(geometry[i_mesh], config, SOLUTION);
+
+      solver_container[i_mesh][FLOW_SOL]->Preprocessing(geometry[i_mesh], solver_container[i_mesh], config, i_mesh,
+                                                        NO_RK_ITER, RUNTIME_FLOW_SYS, false);
+    }
+
+    /* --- Sum up some global counters over processes. --- */
+    SU2_MPI::Reduce(&n_not_in_domain_local, &n_not_in_domain_global, 1, MPI_UNSIGNED_LONG, MPI_SUM, MASTER_NODE,
+                    SU2_MPI::GetComm());
+    SU2_MPI::Reduce(&n_not_iterated_local, &n_not_iterated_global, 1, MPI_UNSIGNED_LONG, MPI_SUM, MASTER_NODE,
+                    SU2_MPI::GetComm());
+    SU2_MPI::Reduce(&n_points_unburnt_local, &n_points_unburnt_global, 1, MPI_UNSIGNED_LONG, MPI_SUM, MASTER_NODE,
+                    SU2_MPI::GetComm());
+    SU2_MPI::Reduce(&n_points_burnt_local, &n_points_burnt_global, 1, MPI_UNSIGNED_LONG, MPI_SUM, MASTER_NODE,
+                    SU2_MPI::GetComm());
+    SU2_MPI::Reduce(&n_points_flame_local, &n_points_flame_global, 1, MPI_UNSIGNED_LONG, MPI_SUM, MASTER_NODE,
+                    SU2_MPI::GetComm());
+
+    if (rank == MASTER_NODE) {
+      cout << endl;
+      cout << " Number of points in unburnt region: " << n_points_unburnt_global << "." << endl;
+      cout << " Number of points in burnt region  : " << n_points_burnt_global << "." << endl;
+      cout << " Number of points in flame zone    : " << n_points_flame_global << "." << endl;
+
+      if (n_not_in_domain_global > 0)
+        cout << " Initial condition: Number of points outside of table domain: " << n_not_in_domain_global << " !!!"
+             << endl;
+
+      if (n_not_iterated_global > 0)
+        cout << " Initial condition: Number of points in which enthalpy could not be iterated: " << n_not_iterated_global
+             << " !!!" << endl;
+    }
+  }
+}
+
+void CSpeciesFlameletSolver::SetPreconditioner(CGeometry* geometry, CSolver** solver_container, CConfig* config) {
+  const bool variable_density = (config->GetKind_DensityModel() == INC_DENSITYMODEL::VARIABLE);
+  const bool implicit = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
+
+  SU2_OMP_FOR_STAT(omp_chunk_size)
+  for (auto iPoint = 0u; iPoint < nPointDomain; iPoint++) {
+    /*--- Access the primitive variables at this node. ---*/
+
+    su2double Density = solver_container[FLOW_SOL]->GetNodes()->GetDensity(iPoint);
+    su2double BetaInc2 = solver_container[FLOW_SOL]->GetNodes()->GetBetaInc2(iPoint);
+    su2double Temperature = solver_container[FLOW_SOL]->GetNodes()->GetTemperature(iPoint);
+
+    su2double SolP = solver_container[FLOW_SOL]->LinSysSol(iPoint, prim_idx.Pressure());
+    su2double SolT = solver_container[FLOW_SOL]->LinSysSol(iPoint, prim_idx.Temperature());
+
+    /*--- We need the derivative of the equation of state to build the
+     preconditioning matrix. For now, the only option is the ideal gas
+     law, but in the future, dRhodT should be in the fluid model. ---*/
+
+    su2double dRhodT = 0.0;
+    if (variable_density) {
+      dRhodT = -Density / Temperature;
+    }
+
+    /*--- Passive scalars have no impact on the density. ---*/
+
+    su2double dRhodC = 0.0;
+
+    /*--- Modify matrix diagonal with term including volume and time step. ---*/
+
+    su2double Vol = geometry->nodes->GetVolume(iPoint);
+    su2double Delta =
+        Vol / (config->GetCFLRedCoeff_Species() * solver_container[FLOW_SOL]->GetNodes()->GetDelta_Time(iPoint));
+
+    /*--- Calculating the inverse of the preconditioning matrix
+     that multiplies the time derivative during time integration. ---*/
+
+    if (implicit) {
+      for (unsigned short iVar = 0; iVar < nVar; iVar++) {
+        su2double scalar = nodes->GetSolution(iPoint, iVar);
+
+        /*--- Compute the lag terms for the decoupled linear system from
+         the mean flow equations and add to the residual for the scalar.
+         In short, we are effectively making these terms explicit. ---*/
+
+        su2double artcompc1 = SolP * scalar / (Density * BetaInc2);
+        su2double artcompc2 = SolT * dRhodT * scalar / (Density);
+
+        LinSysRes(iPoint, iVar) += artcompc1 + artcompc2;
+
+        /*--- Add the extra Jacobian term to the scalar system. ---*/
+
+        su2double Jaccomp = scalar * dRhodC + Density;
+        su2double JacTerm = Jaccomp * Delta;
+
+        Jacobian.AddVal2Diag(iPoint, iVar, JacTerm);
+      }
+    }
+  }
+  END_SU2_OMP_FOR
+}
+
+void CSpeciesFlameletSolver::Source_Residual(CGeometry* geometry, CSolver** solver_container,
+                                             CNumerics** numerics_container, CConfig* config, unsigned short iMesh) {
+  SU2_OMP_FOR_STAT(omp_chunk_size)
+  for (auto i_point = 0u; i_point < nPointDomain; i_point++) {
+
+    /*--- Add source terms from the lookup table directly to the residual. ---*/
+
+    for (auto i_var = 0; i_var < nVar; i_var++) {
+      LinSysRes(i_point, i_var) -= nodes->GetScalarSources(i_point)[i_var] * geometry->nodes->GetVolume(i_point);
+    }
+  }
+  END_SU2_OMP_FOR
+
+  /*--- call the species solver for the shared sources (axisymmetric) ---*/
+  CSpeciesSolver::Source_Residual(geometry, solver_container, numerics_container, config, iMesh);
+}
+
+void CSpeciesFlameletSolver::BC_Inlet(CGeometry* geometry, CSolver** solver_container, CNumerics* conv_numerics,
+                                      CNumerics* visc_numerics, CConfig* config, unsigned short val_marker) {
+  string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
+
+  su2double temp_inlet = config->GetInlet_Ttotal(Marker_Tag);
+  const su2double* scalar_inlet = config->GetInlet_SpeciesVal(Marker_Tag);
+
+  /*--- We compute inlet enthalpy from the temperature and progress variable. ---*/
+  su2double enth_inlet = scalar_inlet[I_ENTH];
+  solver_container[FLOW_SOL]->GetFluidModel()->GetEnthFromTemp(enth_inlet, scalar_inlet[I_PROGVAR], temp_inlet,
+                                                               scalar_inlet[I_ENTH]);
+
+  SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
+  for (auto iVertex = 0u; iVertex < geometry->nVertex[val_marker]; iVertex++) {
+    Inlet_SpeciesVars[val_marker][iVertex][I_ENTH] = enth_inlet;
+  END_SU2_OMP_FOR
+
+  }
+
+  /*--- Call the general inlet boundary condition implementation. ---*/
+  CSpeciesSolver::BC_Inlet(geometry, solver_container, conv_numerics, visc_numerics, config, val_marker);
+}
+
+void CSpeciesFlameletSolver::BC_Isothermal_Wall_Generic(CGeometry* geometry, CSolver** solver_container,
+                                                        CNumerics* conv_numerics, CNumerics* visc_numerics,
+                                                        CConfig* config, unsigned short val_marker, bool cht_mode) {
+  const bool implicit = config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT;
+  const string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
+  su2double temp_wall = config->GetIsothermal_Temperature(Marker_Tag);
+  CFluidModel* fluid_model_local = solver_container[FLOW_SOL]->GetFluidModel();
+  auto* flowNodes = su2staticcast_p<CFlowVariable*>(solver_container[FLOW_SOL]->GetNodes());
+  su2double enth_init, enth_wall, prog_wall;
+  unsigned long n_not_iterated = 0;
+
+  /*--- Loop over all the vertices on this boundary marker. ---*/
+  SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
+  for (unsigned long iVertex = 0; iVertex < geometry->nVertex[val_marker]; iVertex++) {
+    unsigned long iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
+
+    if (cht_mode) temp_wall = GetConjugateHeatVariable(val_marker, iVertex, 0);
+
+    /*--- Check if the node belongs to the domain (i.e., not a halo node). ---*/
+
+    if (geometry->nodes->GetDomain(iPoint)) {
+      if (config->GetMarker_StrongBC(Marker_Tag) == true) {
+        /*--- Initial guess for enthalpy value. ---*/
+
+        enth_init = nodes->GetSolution(iPoint, I_ENTH);
+        enth_wall = enth_init;
+
+        /*--- Set enthalpy on the wall. ---*/
+
+        prog_wall = solver_container[SPECIES_SOL]->GetNodes()->GetSolution(iPoint)[I_PROGVAR];
+        n_not_iterated += fluid_model_local->GetEnthFromTemp(enth_wall, prog_wall, temp_wall, enth_init);
+
+        /*--- Impose the value of the enthalpy as a strong boundary
+        condition (Dirichlet) and remove any
+        contribution to the residual at this node. ---*/
+
+        nodes->SetSolution(iPoint, I_ENTH, enth_wall);
+        nodes->SetSolution_Old(iPoint, I_ENTH, enth_wall);
+
+        LinSysRes(iPoint, I_ENTH) = 0.0;
+
+        nodes->SetVal_ResTruncError_Zero(iPoint, I_ENTH);
+
+        if (implicit) {
+          unsigned long total_index = iPoint * nVar + I_ENTH;
+          Jacobian.DeleteValsRowi(total_index);
+        }
+      } else {
+        /*--- Weak BC formulation. ---*/
+        const auto Normal = geometry->vertex[val_marker][iVertex]->GetNormal();
+
+        const su2double Area = GeometryToolbox::Norm(nDim, Normal);
+
+        const auto Point_Normal = geometry->vertex[val_marker][iVertex]->GetNormal_Neighbor();
+
+        /*--- Get coordinates of i & nearest normal and compute distance. ---*/
+
+        const auto Coord_i = geometry->nodes->GetCoord(iPoint);
+        const auto Coord_j = geometry->nodes->GetCoord(Point_Normal);
+        su2double Edge_Vector[MAXNDIM];
+        GeometryToolbox::Distance(nDim, Coord_j, Coord_i, Edge_Vector);
+        su2double dist_ij_2 = GeometryToolbox::SquaredNorm(nDim, Edge_Vector);
+        su2double dist_ij = sqrt(dist_ij_2);
+
+        /*--- Compute the normal gradient in temperature using Twall. ---*/
+
+        su2double dTdn = -(flowNodes->GetTemperature(Point_Normal) - temp_wall) / dist_ij;
+
+        /*--- Get thermal conductivity. ---*/
+
+        su2double thermal_conductivity = flowNodes->GetThermalConductivity(iPoint);
+
+        /*--- Apply a weak boundary condition for the energy equation.
+        Compute the residual due to the prescribed heat flux. ---*/
+
+        LinSysRes(iPoint, I_ENTH) -= thermal_conductivity * dTdn * Area;
+      }
+    }
+  }
+  END_SU2_OMP_FOR
+
+  if (rank == MASTER_NODE && n_not_iterated > 0) {
+    cout << " !!! Wall bc (" << Marker_Tag
+         << "): Number of points in which enthalpy could not be iterated: " << n_not_iterated << " !!!" << endl;
+  }
+}
+
+void CSpeciesFlameletSolver::BC_Isothermal_Wall(CGeometry* geometry, CSolver** solver_container,
+                                                CNumerics* conv_numerics, CNumerics* visc_numerics, CConfig* config,
+                                                unsigned short val_marker) {
+  BC_Isothermal_Wall_Generic(geometry, solver_container, conv_numerics, visc_numerics, config, val_marker);
+}
+
+void CSpeciesFlameletSolver::BC_ConjugateHeat_Interface(CGeometry* geometry, CSolver** solver_container,
+                                                        CNumerics* conv_numerics, CConfig* config,
+                                                        unsigned short val_marker) {
+  BC_Isothermal_Wall_Generic(geometry, solver_container, conv_numerics, nullptr, config, val_marker, true);
+}
diff --git a/SU2_CFD/src/solvers/CSpeciesSolver.cpp b/SU2_CFD/src/solvers/CSpeciesSolver.cpp
index 43a88edf3ea..5acebd6164a 100644
--- a/SU2_CFD/src/solvers/CSpeciesSolver.cpp
+++ b/SU2_CFD/src/solvers/CSpeciesSolver.cpp
@@ -36,12 +36,64 @@ template class CScalarSolver<CSpeciesVariable>;
 
 CSpeciesSolver::CSpeciesSolver(CGeometry* geometry, CConfig* config, unsigned short iMesh)
     : CScalarSolver<CSpeciesVariable>(geometry, config, true) {
-  /*--- Store if an implicit scheme is used, for use during periodic boundary conditions. ---*/
-  SetImplicitPeriodic(config->GetKind_TimeIntScheme_Species() == EULER_IMPLICIT);
 
   /*--- Dimension of the problem. ---*/
 
   nVar = config->GetnSpecies();
+
+  Initialize(geometry, config, iMesh, nVar);
+
+  /*--- Initialize the solution to the far-field state everywhere. ---*/
+
+  nodes = new CSpeciesVariable(Solution_Inf, nPoint, nDim, nVar, config);
+  SetBaseClassPointerToNodes();
+
+  /*--- Initialize the mass diffusivity. Nondimensionalization done in the flow solver. ---*/
+  SU2_OMP_FOR_STAT(omp_chunk_size)
+  for (unsigned long iPoint = 0; iPoint < nPoint; iPoint++) {
+    for (auto iVar = 0u; iVar <= nVar; iVar++) {
+      const auto MassDiffusivity = config->GetDiffusivity_ConstantND();
+      nodes->SetDiffusivity(iPoint, MassDiffusivity, iVar);
+    }
+  }
+  END_SU2_OMP_FOR
+
+  /*--- MPI solution ---*/
+
+  InitiateComms(geometry, config, SOLUTION);
+  CompleteComms(geometry, config, SOLUTION);
+
+  SlidingState.resize(nMarker);
+  SlidingStateNodes.resize(nMarker);
+
+  for (unsigned long iMarker = 0; iMarker < nMarker; iMarker++) {
+    if (config->GetMarker_All_KindBC(iMarker) == FLUID_INTERFACE) {
+      SlidingState[iMarker].resize(nVertex[iMarker], nPrimVar+1) = nullptr;
+      SlidingStateNodes[iMarker].resize(nVertex[iMarker],0);
+    }
+  }
+
+  /*--- Store the initial CFL number for all grid points. ---*/
+
+  const su2double CFL = config->GetCFL(MGLevel) * config->GetCFLRedCoeff_Species();
+  SU2_OMP_FOR_STAT(omp_chunk_size)
+  for (auto iPoint = 0u; iPoint < nPoint; iPoint++) {
+    nodes->SetLocalCFL(iPoint, CFL);
+  }
+  END_SU2_OMP_FOR
+  Min_CFL_Local = CFL;
+  Max_CFL_Local = CFL;
+  Avg_CFL_Local = CFL;
+
+  /*--- Add the solver name. ---*/
+  SolverName = "SPECIES";
+}
+
+
+void CSpeciesSolver::Initialize(CGeometry* geometry, CConfig* config, unsigned short iMesh, unsigned short nVar) {
+  /*--- Store if an implicit scheme is used, for use during periodic boundary conditions. ---*/
+  SetImplicitPeriodic(config->GetKind_TimeIntScheme_Species() == EULER_IMPLICIT);
+
   nPrimVar = nVar;
 
   if (nVar > MAXNVAR)
@@ -58,9 +110,8 @@ CSpeciesSolver::CSpeciesSolver(CGeometry* geometry, CConfig* config, unsigned sh
 
   nDim = geometry->GetnDim();
 
-  /*--- Single grid simulation ---*/
 
-  if (iMesh == MESH_0 || config->GetMGCycle() == FULLMG_CYCLE) {
+if (iMesh == MESH_0 || config->GetMGCycle() == FULLMG_CYCLE) {
 
     /*--- Define some auxiliary vector related with the residual ---*/
 
@@ -108,41 +159,11 @@ CSpeciesSolver::CSpeciesSolver(CGeometry* geometry, CConfig* config, unsigned sh
     Solution_Inf[iVar] = config->GetSpecies_Init()[iVar];
   }
 
-  /*--- Initialize the solution to the far-field state everywhere. ---*/
-
-  nodes = new CSpeciesVariable(Solution_Inf, nPoint, nDim, nVar, config);
-  SetBaseClassPointerToNodes();
-
-  /*--- Initialize the mass diffusivity. Nondimensionalization done in the flow solver. ---*/
-  SU2_OMP_FOR_STAT(omp_chunk_size)
-  for (unsigned long iPoint = 0; iPoint < nPoint; iPoint++) {
-    for (auto iVar = 0u; iVar <= nVar; iVar++) {
-      const auto MassDiffusivity = config->GetDiffusivity_ConstantND();
-      nodes->SetDiffusivity(iPoint, MassDiffusivity, iVar);
-    }
-  }
-  END_SU2_OMP_FOR
-
-  /*--- MPI solution ---*/
-
-  InitiateComms(geometry, config, SOLUTION);
-  CompleteComms(geometry, config, SOLUTION);
-
-  SlidingState.resize(nMarker);
-  SlidingStateNodes.resize(nMarker);
-
-  for (unsigned long iMarker = 0; iMarker < nMarker; iMarker++) {
-    if (config->GetMarker_All_KindBC(iMarker) == FLUID_INTERFACE) {
-      SlidingState[iMarker].resize(nVertex[iMarker], nPrimVar+1) = nullptr;
-      SlidingStateNodes[iMarker].resize(nVertex[iMarker],0);
-    }
-  }
-
   /*--- Set the column number for species in inlet-files.
    * e.g. Coords(nDim), Temp(1), VelMag(1), Normal(nDim), Turb(1 or 2), Species(arbitrary) ---*/
   Inlet_Position = nDim + 2 + nDim + config->GetnTurbVar();
 
-  /*-- Allocation of inlet-values. Will be filled either by an inlet files,
+  /*-- Allocation of inlet-values. Will be filled either by an inlet file,
    * or uniformly by a uniform boundary condition. ---*/
 
   Inlet_SpeciesVars.resize(nMarker);
@@ -154,23 +175,9 @@ CSpeciesSolver::CSpeciesSolver(CGeometry* geometry, CConfig* config, unsigned sh
       }
     }
   }
-
-  /*--- Store the initial CFL number for all grid points. ---*/
-
-  const su2double CFL = config->GetCFL(MGLevel) * config->GetCFLRedCoeff_Species();
-  SU2_OMP_FOR_STAT(omp_chunk_size)
-  for (auto iPoint = 0u; iPoint < nPoint; iPoint++) {
-    nodes->SetLocalCFL(iPoint, CFL);
-  }
-  END_SU2_OMP_FOR
-  Min_CFL_Local = CFL;
-  Max_CFL_Local = CFL;
-  Avg_CFL_Local = CFL;
-
-  /*--- Add the solver name. ---*/
-  SolverName = "SPECIES";
 }
 
+
 void CSpeciesSolver::LoadRestart(CGeometry** geometry, CSolver*** solver, CConfig* config, int val_iter,
                                  bool val_update_geo) {
   /*--- Restart the solution from file information ---*/
@@ -199,9 +206,12 @@ void CSpeciesSolver::LoadRestart(CGeometry** geometry, CSolver*** solver, CConfi
 
     const bool incompressible = (config->GetKind_Regime() == ENUM_REGIME::INCOMPRESSIBLE);
     const bool energy = config->GetEnergy_Equation();
+    const bool flamelet = (config->GetKind_FluidModel() == FLUID_FLAMELET);
     const bool weakly_coupled_heat = config->GetWeakly_Coupled_Heat();
 
-    if (incompressible && ((!energy) && (!weakly_coupled_heat))) skipVars--;
+    /*--- for the flamelet model, the temperature is saved to file, but the energy equation is off ---*/
+
+   if (incompressible && ((!energy) && (!weakly_coupled_heat) && (!flamelet))) skipVars--;
 
     /*--- Load data from the restart into correct containers. ---*/
 
@@ -322,7 +332,6 @@ void CSpeciesSolver::Viscous_Residual(unsigned long iEdge, CGeometry* geometry,
 
 void CSpeciesSolver::BC_Inlet(CGeometry* geometry, CSolver** solver_container, CNumerics* conv_numerics,
                               CNumerics* visc_numerics, CConfig* config, unsigned short val_marker) {
-  string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
 
   const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
 
@@ -336,7 +345,10 @@ void CSpeciesSolver::BC_Inlet(CGeometry* geometry, CSolver** solver_container, C
 
     if (!geometry->nodes->GetDomain(iPoint)) continue;
 
-    if (config->GetSpecies_StrongBC()) {
+    /*--- Identify the boundary by string name ---*/
+    string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
+   
+    if (config->GetMarker_StrongBC(Marker_Tag)==true) {
       nodes->SetSolution_Old(iPoint, Inlet_SpeciesVars[val_marker][iVertex]);
 
       LinSysRes.SetBlock_Zero(iPoint);
@@ -426,7 +438,7 @@ su2double CSpeciesSolver::GetInletAtVertex(su2double *val_inlet,
       if ((config->GetMarker_All_KindBC(iMarker) == INLET_FLOW) &&
           (config->GetMarker_All_TagBound(iMarker) == val_marker)) {
 
-        for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++){
+        for (iVertex = 0; iVertex < nVertex[iMarker]; iVertex++) {
 
           iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
 
@@ -481,14 +493,17 @@ void CSpeciesSolver::BC_Outlet(CGeometry* geometry, CSolver** solver_container,
 
   SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
   for (auto iVertex = 0u; iVertex < geometry->nVertex[val_marker]; iVertex++) {
-    /* strong zero flux Neumann boundary condition at the outlet */
+    /*--- Strong zero flux Neumann boundary condition at the outlet ---*/
     const auto iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
     /*--- Check if the node belongs to the domain (i.e., not a halo node) ---*/
 
     if (!geometry->nodes->GetDomain(iPoint)) continue;
 
-    if (config->GetSpecies_StrongBC()) {
+    /*--- Identify the boundary by string name ---*/
+    string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
+
+    if (config->GetMarker_StrongBC(Marker_Tag)==true) {
       /*--- Allocate the value at the outlet ---*/
       auto Point_Normal = geometry->vertex[val_marker][iVertex]->GetNormal_Neighbor();
 
diff --git a/SU2_CFD/src/solvers/CTurbSolver.cpp b/SU2_CFD/src/solvers/CTurbSolver.cpp
index d68c550d185..ffd7152346b 100644
--- a/SU2_CFD/src/solvers/CTurbSolver.cpp
+++ b/SU2_CFD/src/solvers/CTurbSolver.cpp
@@ -129,8 +129,9 @@ void CTurbSolver::LoadRestart(CGeometry** geometry, CSolver*** solver, CConfig*
     const bool incompressible = (config->GetKind_Regime() == ENUM_REGIME::INCOMPRESSIBLE);
     const bool energy = config->GetEnergy_Equation();
     const bool weakly_coupled_heat = config->GetWeakly_Coupled_Heat();
+    const bool flamelet = (config->GetKind_FluidModel() == FLUID_FLAMELET);
 
-    if (incompressible && ((!energy) && (!weakly_coupled_heat))) skipVars--;
+    if (incompressible && ((!energy) && (!weakly_coupled_heat) && (!flamelet))) skipVars--;
 
     /*--- Load data from the restart into correct containers. ---*/
 
diff --git a/SU2_CFD/src/variables/CIncNSVariable.cpp b/SU2_CFD/src/variables/CIncNSVariable.cpp
index c000575c218..c132cb20efd 100644
--- a/SU2_CFD/src/variables/CIncNSVariable.cpp
+++ b/SU2_CFD/src/variables/CIncNSVariable.cpp
@@ -58,8 +58,8 @@ bool CIncNSVariable::SetPrimVar(unsigned long iPoint, su2double eddy_visc, su2do
 
   /*--- Set the value of the temperature directly ---*/
 
-  su2double Temperature = Solution(iPoint, nDim+1);
-  const auto check_temp = SetTemperature(iPoint,Temperature);
+  su2double Temperature = Solution(iPoint, indices.Temperature());
+  auto check_temp = SetTemperature(iPoint, Temperature);
 
   /*--- Use the fluid model to compute the new value of density.
   Note that the thermodynamic pressure is constant and decoupled
@@ -69,6 +69,12 @@ bool CIncNSVariable::SetPrimVar(unsigned long iPoint, su2double eddy_visc, su2do
 
   FluidModel->SetTDState_T(Temperature, scalar);
 
+  /*--- for FLAMELET: copy the LUT temperature into the solution ---*/
+  Solution(iPoint,nDim+1) = FluidModel->GetTemperature();
+  /*--- for FLAMELET: update the local temperature using LUT variables ---*/
+  Temperature = Solution(iPoint,indices.Temperature());
+  check_temp = SetTemperature(iPoint, Temperature);
+
   /*--- Set the value of the density ---*/
 
   const auto check_dens = SetDensity(iPoint, FluidModel->GetDensity());
@@ -84,7 +90,7 @@ bool CIncNSVariable::SetPrimVar(unsigned long iPoint, su2double eddy_visc, su2do
 
     /*--- Recompute the primitive variables ---*/
 
-    Temperature = Solution(iPoint, nDim+1);
+    Temperature = Solution(iPoint, indices.Temperature());
     SetTemperature(iPoint, Temperature);
     FluidModel->SetTDState_T(Temperature, scalar);
     SetDensity(iPoint, FluidModel->GetDensity());
diff --git a/SU2_CFD/src/variables/CSpeciesFlameletVariable.cpp b/SU2_CFD/src/variables/CSpeciesFlameletVariable.cpp
new file mode 100644
index 00000000000..16536909bee
--- /dev/null
+++ b/SU2_CFD/src/variables/CSpeciesFlameletVariable.cpp
@@ -0,0 +1,56 @@
+/*!
+ * \file CSpeciesFlameletVariable.cpp
+ * \brief Definition of the variable fields for the flamelet class.
+ * \author D. Mayer, T. Economon, N. Beishuizen
+ * \version 7.5.1 "Blackbird"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+ */
+
+#include "../../include/variables/CSpeciesFlameletVariable.hpp"
+
+CSpeciesFlameletVariable::CSpeciesFlameletVariable(const su2double* species_inf, unsigned long npoint,
+                                                   unsigned long ndim, unsigned long nvar, const CConfig* config)
+    : CSpeciesVariable(species_inf, npoint, ndim, nvar, config) {
+  for (unsigned long iPoint = 0; iPoint < nPoint; iPoint++)
+    for (unsigned long iVar = 0; iVar < nVar; iVar++) Solution(iPoint, iVar) = species_inf[iVar];
+
+  Solution_Old = Solution;
+
+  /*--- Allocate and initialize solution for the dual time strategy ---*/
+  bool dual_time = ((config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_1ST) ||
+                    (config->GetTime_Marching() == TIME_MARCHING::DT_STEPPING_2ND));
+
+  if (dual_time) {
+    Solution_time_n = Solution;
+    Solution_time_n1 = Solution;
+  }
+
+  /*--- Allocate residual structures ---*/
+
+  Res_TruncError.resize(nPoint, nVar) = su2double(0.0);
+
+  /* Allocate space for the source and scalars for visualization */
+
+  source_scalar.resize(nPoint, config->GetNScalars()) = su2double(0.0);
+  lookup_scalar.resize(nPoint, config->GetNLookups()) = su2double(0.0);
+  table_misses.resize(nPoint) = 0;
+}
diff --git a/TestCases/.gitignore b/TestCases/.gitignore
index 315ff14f09e..a63f2d78d23 100644
--- a/TestCases/.gitignore
+++ b/TestCases/.gitignore
@@ -29,3 +29,6 @@ config_*.cfg
 *.tgz
 COPYING
 *.eqn
+
+# dragon files for flamelet models
+*.drg
diff --git a/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg b/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg
new file mode 100644
index 00000000000..55ef51919de
--- /dev/null
+++ b/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg
@@ -0,0 +1,135 @@
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+% SU2 configuration file                                                       %
+% Case description: Laminar premixed flame stabilized on isothermal burner     %
+% Author: Nijso Beishuizen                                                     %
+% Institution: Bosch Thermotechnology                                          %
+% Date: 08/09/2021                                                             %
+% File Version 7.5.1 "Blackbird"                                               %
+%                                                                              %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+%
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
+SOLVER = INC_NAVIER_STOKES
+KIND_TURB_MODEL= NONE
+MATH_PROBLEM= DIRECT
+RESTART_SOL = YES
+%
+% ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
+%
+INC_DENSITY_MODEL= VARIABLE 
+INC_ENERGY_EQUATION = YES
+INC_DENSITY_INIT= 1.00
+INC_VELOCITY_INIT= (0.5, 0.0, 0.0 )
+INC_TEMPERATURE_INIT= 300.0
+INC_NONDIM= DIMENSIONAL
+%
+% -------------------- FLUID MODEL --------------------------------------- %
+%
+FLUID_MODEL= FLUID_FLAMELET
+FILENAME_LUT= fgm_ch4.drg
+%
+% -------------------- SCALAR TRANSPORT ---------------------------------------%
+%
+KIND_SCALAR_MODEL= FLAMELET      
+DIFFUSIVITY_MODEL= FLAMELET
+VISCOSITY_MODEL= FLAMELET
+CONDUCTIVITY_MODEL= FLAMELET
+FLAME_INIT= (0.0032, 0.00, 0.00, 1.0, 0.1, 0.0, 1.0e-3, 0.1)
+% # progvar, enthalpy
+SPECIES_INIT = (0.0, -210000, 0.0, 0.0)
+CONV_NUM_METHOD_SPECIES= SCALAR_UPWIND
+MUSCL_SPECIES= YES
+SLOPE_LIMITER_SPECIES= NONE
+TIME_DISCRE_SPECIES= EULER_IMPLICIT
+% SCALAR CLIPPING
+SPECIES_CLIPPING= YES
+SPECIES_CLIPPING_MIN= 0 -2e6 0 0
+SPECIES_CLIPPING_MAX= 1 2e6 1 1
+%
+MARKER_INLET_SPECIES = (inlet, 0, -193600.0, 0.0, 0.0)
+CFL_REDUCTION_SPECIES= 1.0
+MARKER_SPECIES_STRONG_BC= (inlet, outlet, wall)
+LOOKUP_NAMES = (MolarWeightMix, Conductivity, Cp, HeatRelease, Diffusivity)
+USER_SCALAR_NAMES= (CO, NOx)
+USER_SOURCE_NAMES = ( \
+    ProdRatePos_Y-CO,  ProdRateNegScaled_Y-CO  ,\
+    ProdRateTot_Y-NOx, NULL
+)
+%
+% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
+%
+REF_ORIGIN_MOMENT_X = 0.25
+REF_ORIGIN_MOMENT_Y = 0.00
+REF_ORIGIN_MOMENT_Z = 0.00
+REF_LENGTH= 1.0
+REF_AREA= 1.0
+%
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
+MARKER_ISOTHERMAL= (wall, 450)
+MARKER_SYM= (symmetry, symmetry_2-part-fluid)
+INC_INLET_TYPE= VELOCITY_INLET
+MARKER_INLET = (inlet, 300.0, 0.20, 1.0, 0.0, 0.0)
+INC_OUTLET_TYPE= PRESSURE_OUTLET
+%INC_INLET_DAMPING = 0.05
+%INC_OUTLET_DAMPING = 0.05
+MARKER_OUTLET= (outlet, 0.0)
+MARKER_PLOTTING= ( wall )
+MARKER_MONITORING= ( wall )
+MARKER_ANALYZE= ( inlet,outlet )
+MARKER_ANALYZE_AVERAGE = AREA
+%
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
+CFL_NUMBER= 350
+CFL_ADAPT= NO
+ITER= 100
+OUTPUT_WRT_FREQ= 100
+%
+% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
+%
+LINEAR_SOLVER= FGMRES
+LINEAR_SOLVER_PREC= ILU
+LINEAR_SOLVER_ERROR= 1E-03
+LINEAR_SOLVER_ITER= 10
+%
+% -------------------------- MULTIGRID PARAMETERS -----------------------------%
+%
+MGLEVEL= 0
+%
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
+CONV_NUM_METHOD_FLOW= FDS
+MUSCL_FLOW= YES
+SLOPE_LIMITER_FLOW = NONE
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+%
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
+CONV_RESIDUAL_MINVAL= -15
+CONV_STARTITER= 10
+CONV_CAUCHY_ELEMS= 100
+CONV_CAUCHY_EPS= 1E-6
+SCREEN_OUTPUT = INNER_ITER RMS_VELOCITY-X RMS_VELOCITY-Y RMS_PRESSURE RMS_PROGRESS_VARIABLE RMS_TOTAL_ENTHALPY RMS_CO RMS_NOx
+HISTORY_OUTPUT = RMS_RES AERO_COEFF FLOW_COEFF FLOW_COEFF_SURF
+VOLUME_OUTPUT = SOLUTION PRIMITIVE SOURCE RESIDUAL SENSITIVITY LOOKUP TIMESTEP
+CONV_FIELD = RMS_PRESSURE
+%
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+%
+MESH_FORMAT= CGNS
+MESH_FILENAME = mesh_structured.cgns
+MESH_OUT_FILENAME= mesh_out.su2
+SOLUTION_FILENAME= solution
+RESTART_FILENAME= restart
+%OUTPUT_FILES = (RESTART,PARAVIEW,PARAVIEW_MULTIBLOCK) 
+OUTPUT_FILES = (RESTART) 
+TABULAR_FORMAT = CSV
+CONV_FILENAME= history
+VOLUME_FILENAME= ch4_flame_cfd
+SURFACE_FILENAME= surface_flow
+WRT_PERFORMANCE = NO 
+SCREEN_WRT_FREQ_INNER = 1
+SCREEN_WRT_FREQ_OUTER = 1
diff --git a/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg
new file mode 100644
index 00000000000..884dd859268
--- /dev/null
+++ b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg
@@ -0,0 +1,141 @@
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+%                                                                              %
+% SU2 configuration file                                                       %
+% Case description: Laminar premixed flame stabilized on isothermal burner     %
+%                   with cold wall (hx) downstream of the flame (adjoint run)  %
+%                                                                              %
+% Author a: Daniel Mayer                                                       %
+% Institution a: Robert Bosch LLC                                              %
+%                                                                              %
+% Author b: Nijso Beishuizen                                                   %
+% Institution b: Bosch Thermotechnology                                        %
+%                                                                              %
+% Date: 02/21/2023                                                             %
+% File Version 7.5.1 "Blackbird"                                               %
+%                                                                              %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
+SOLVER= INC_NAVIER_STOKES
+KIND_TURB_MODEL= NONE
+%
+OBJECTIVE_FUNCTION= CUSTOM_OBJFUNC
+OBJECTIVE_WEIGHT= 1.0
+CUSTOM_OBJFUNC= avg_NOx
+CUSTOM_OUTPUTS= 'avg_NOx : MassFlowAvg{SPECIES[3]}[outlet]'
+%
+% ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
+%
+INC_DENSITY_MODEL= VARIABLE
+INC_DENSITY_INIT= 1.1766
+INC_VELOCITY_INIT= ( 0.2, 0, 0 )
+INC_ENERGY_EQUATION= YES
+INC_TEMPERATURE_INIT= 300.0
+INC_NONDIM= DIMENSIONAL
+%
+% -------------------- FLUID PROPERTIES ------------------------------------- %
+%
+FLUID_MODEL= FLUID_FLAMELET
+FILENAME_LUT= fgm_ch4.drg
+CONDUCTIVITY_MODEL= FLAMELET
+DIFFUSIVITY_MODEL= FLAMELET
+KIND_SCALAR_MODEL= FLAMELET
+VISCOSITY_MODEL= FLAMELET
+%
+FLAME_INIT= (0.0035, 0, 0, 3.0, 2.0, 0.0, 5.0e-4, 1.0)
+%
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
+MARKER_ISOTHERMAL= ( wall_burner, 450, wall_hx, 900 )
+MARKER_SYM= ( axis, symmetry_xm, symmetry_xp )
+%
+INC_INLET_TYPE=  VELOCITY_INLET
+MARKER_INLET= (inlet, 300.0, 0.20,    1.0, 0.0, 0.0)
+MARKER_INLET_SPECIES= (inlet, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
+MARKER_SPECIES_STRONG_BC= (inlet, wall_burner, wall_hx)
+
+%
+INC_OUTLET_TYPE= PRESSURE_OUTLET
+MARKER_OUTLET= ( outlet, 0.0 )
+%
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
+CFL_NUMBER= 50
+CFL_REDUCTION_SPECIES= 1.0
+ITER= 11
+%
+% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
+%
+LINEAR_SOLVER= FGMRES
+LINEAR_SOLVER_PREC= ILU
+LINEAR_SOLVER_ERROR= 1E-03
+LINEAR_SOLVER_ITER= 10
+%
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
+CONV_NUM_METHOD_FLOW= FDS
+MUSCL_FLOW= NO
+SLOPE_LIMITER_FLOW= NONE
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+%
+% -------------------- SCALAR TRANSPORT ---------------------------------------%
+%
+USER_SCALAR_NAMES= (Y-CO, Y-NOx_tot)
+
+USER_SOURCE_NAMES= ( \
+    ProdRatePos_Y-CO, ProdRateNegScaled_Y-CO ,\
+    ProdRateTot_Y-NOx, zero)
+
+DIFFUSIVITY_CONSTANT= 0.00001
+%
+CONV_NUM_METHOD_SPECIES= BOUNDED_SCALAR
+MUSCL_SPECIES= NO
+SLOPE_LIMITER_SPECIES= NONE
+%
+TIME_DISCRE_SPECIES= EULER_IMPLICIT
+%
+SPECIES_INIT= (0, 0, 0, 0, 0, 0, 0)
+SPECIES_CLIPPING= NO
+LOOKUP_NAMES= (MolarWeightMix, Conductivity, HeatRelease, Diffusivity, \
+    ProdRatePos_Y-CO, ProdRateNegScaled_Y-CO ,\
+    ProdRateTot_Y-NOx)
+
+%
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
+CONV_FIELD= RMS_PRESSURE, RMS_VELOCITY-X, RMS_VELOCITY-Y
+CONV_RESIDUAL_MINVAL= -18
+CONV_STARTITER= 10
+%
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+%
+MESH_FILENAME= mesh_unstructured_hx.su2
+%
+SCREEN_OUTPUT= INNER_ITER WALL_TIME RMS_ADJ_PRESSURE RMS_ADJ_VELOCITY-X RMS_ADJ_VELOCITY-Y RMS_ADJ_SPECIES_0 RMS_ADJ_SPECIES_1 RMS_ADJ_SPECIES_2 RMS_ADJ_SPECIES_3
+SCREEN_WRT_FREQ_INNER= 1
+%
+HISTORY_OUTPUT= ITER RMS_RES LINSOL FLOW_COEFF_SURF CUSTOM COMBO
+CONV_FILENAME= history
+MARKER_ANALYZE= outlet
+MARKER_ANALYZE_AVERAGE= MASSFLUX
+%
+%OUTPUT_FILES= RESTART, PARAVIEW, PARAVIEW_MULTIBLOCK
+OUTPUT_FILES= RESTART, RESTART_ASCII
+VOLUME_OUTPUT= RESIDUAL, PRIMITIVE
+VOLUME_ADJ_FILENAME= ch4_flame_hx_ad
+
+OUTPUT_WRT_FREQ= 100
+%
+GRAD_OBJFUNC_FILENAME= of_grad.csv
+%
+RESTART_SOL= YES
+READ_BINARY_RESTART= NO
+RESTART_FILENAME= restart
+RESTART_ADJ_FILENAME= restart_adj
+SOLUTION_FILENAME= solution
+SOLUTION_ADJ_FILENAME= solution_adj
+%
+WRT_PERFORMANCE= YES
+OUTPUT_PRECISION= 16
diff --git a/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg
new file mode 100644
index 00000000000..14266a33b58
--- /dev/null
+++ b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg
@@ -0,0 +1,251 @@
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+%                                                                              %
+% SU2 configuration file                                                       %
+% Case description: Laminar premixed flame stabilized on isothermal burner     %
+%                   with cold wall (hx) downstream of the flame (adjoint run)  %
+%                                                                              %
+% Author a: Daniel Mayer                                                       %
+% Institution a: Robert Bosch LLC                                              %
+%                                                                              %
+% Author b: Nijso Beishuizen                                                   %
+% Institution b: Bosch Thermotechnology                                        %
+%                                                                              %
+% Date: 02/21/2023                                                             %
+% File Version 7.5.1 "Blackbird"                                               %
+%                                                                              %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
+SOLVER= INC_NAVIER_STOKES
+KIND_TURB_MODEL= NONE
+%
+OBJECTIVE_FUNCTION= CUSTOM_OBJFUNC
+OBJECTIVE_WEIGHT= 1.0
+CUSTOM_OBJFUNC= avg_NOx
+CUSTOM_OUTPUTS= 'avg_NOx : MassFlowAvg{SPECIES[3]}[outlet]'
+
+%
+% ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
+%
+INC_DENSITY_MODEL= VARIABLE
+INC_DENSITY_INIT= 1.1766
+INC_VELOCITY_INIT= ( 0.2, 0, 0 )
+INC_ENERGY_EQUATION= YES
+INC_TEMPERATURE_INIT= 300.0
+INC_NONDIM= DIMENSIONAL
+%
+% -------------------- FLUID PROPERTIES ------------------------------------- %
+%
+FLUID_MODEL= FLUID_FLAMELET
+FILENAME_LUT= fgm_ch4.drg
+CONDUCTIVITY_MODEL= FLAMELET
+DIFFUSIVITY_MODEL= FLAMELET
+KIND_SCALAR_MODEL= FLAMELET
+VISCOSITY_MODEL= FLAMELET
+%
+FLAME_INIT= (0.0035, 0, 0, 3, 2, 0, 5.0e-4, 1.0)
+%
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
+MARKER_ISOTHERMAL= ( wall_burner, 450, wall_hx, 900 )
+MARKER_SYM= ( axis, symmetry_xm, symmetry_xp, outlet )
+%
+INC_INLET_TYPE=  VELOCITY_INLET
+MARKER_INLET= (inlet, 300.0, 0.20, 1.0, 0.0, 0.0)
+MARKER_INLET_SPECIES= (inlet, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
+MARKER_SPECIES_STRONG_BC= (inlet, wall_burner, wall_hx)
+%
+% INC_OUTLET_TYPE= PRESSURE_OUTLET
+% MARKER_OUTLET= ( outlet, 0.0 )
+%
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
+CFL_NUMBER= 100
+CFL_REDUCTION_SPECIES= 1.0
+ITER= 11
+%
+% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
+%
+LINEAR_SOLVER= FGMRES
+LINEAR_SOLVER_PREC= ILU
+LINEAR_SOLVER_ERROR= 1E-03
+LINEAR_SOLVER_ITER= 10
+%
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
+CONV_NUM_METHOD_FLOW= FDS
+MUSCL_FLOW= NO
+SLOPE_LIMITER_FLOW= NONE
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+%
+% -------------------- SCALAR TRANSPORT ---------------------------------------%
+%
+USER_SCALAR_NAMES= (Y-CO, Y-NOx_tot)
+
+USER_SOURCE_NAMES= ( \
+    ProdRatePos_Y-CO,  ProdRateNegScaled_Y-CO  ,\
+    ProdRateTot_Y-NOx, zero)
+
+DIFFUSIVITY_CONSTANT= 0.00001
+%
+CONV_NUM_METHOD_SPECIES= BOUNDED_SCALAR
+MUSCL_SPECIES= NO
+SLOPE_LIMITER_SPECIES= NONE
+%
+TIME_DISCRE_SPECIES= EULER_IMPLICIT
+%
+SPECIES_INIT= (0, 0, 0, 0, 0, 0, 0)
+SPECIES_CLIPPING= NO
+LOOKUP_NAMES= (MolarWeightMix, Conductivity, HeatRelease, Diffusivity, \
+    ProdRatePos_Y-CO,  ProdRateNegScaled_Y-CO  ,\
+    ProdRateTot_Y-NOx)
+
+%
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
+CONV_FIELD= RMS_PRESSURE, RMS_VELOCITY-X, RMS_VELOCITY-Y
+CONV_RESIDUAL_MINVAL= -18
+CONV_STARTITER= 10
+%
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+%
+MESH_FILENAME= mesh_unstructured_hx.su2
+%
+SCREEN_OUTPUT= INNER_ITER WALL_TIME RMS_ADJ_PRESSURE RMS_ADJ_VELOCITY-X RMS_ADJ_VELOCITY-Y RMS_ADJ_SPECIES_0 RMS_ADJ_SPECIES_1 RMS_ADJ_SPECIES_2 RMS_ADJ_SPECIES_3
+SCREEN_WRT_FREQ_INNER= 1
+%
+HISTORY_OUTPUT= ITER RMS_RES LINSOL FLOW_COEFF_SURF
+CONV_FILENAME= history
+MARKER_ANALYZE= outlet
+MARKER_ANALYZE_AVERAGE= MASSFLUX
+%
+%OUTPUT_FILES= RESTART, PARAVIEW, PARAVIEW_MULTIBLOCK
+OUTPUT_FILES= RESTART
+VOLUME_OUTPUT= RESIDUAL, PRIMITIVE
+VOLUME_ADJ_FILENAME= ch4_flame_hx_ad
+
+OUTPUT_WRT_FREQ= 100
+%
+GRAD_OBJFUNC_FILENAME= of_grad.csv
+%
+RESTART_SOL= YES
+READ_BINARY_RESTART= NO
+RESTART_FILENAME= restart
+RESTART_ADJ_FILENAME= restart_adj
+SOLUTION_FILENAME= solution
+SOLUTION_ADJ_FILENAME= restart_adj
+%
+WRT_PERFORMANCE= YES
+OUTPUT_PRECISION= 16
+%
+% -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
+%
+% Tolerance of the Free-Form Deformation point inversion
+FFD_TOLERANCE= 1E-10
+%
+% Maximum number of iterations in the Free-Form Deformation point inversion
+FFD_ITERATIONS= 500
+%
+% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
+%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
+%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
+%                              0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
+% Start at the lowest leftest corner and turn counter-clockwise
+FFD_DEFINITION= (BOX, \
+0.065, 0.01, 0.0, \
+0.15, 0.01, 0.0 \
+0.15, 0.02, 0.0, \
+0.065, 0.02, 0.0, \
+0.0, 0.0 ,0.0, \
+0.0 ,0.0, 0.0, \
+0.0, 0.0, 0.0, \
+0.0, 0.0, 0.0 )
+%
+% FFD box degree: 3D case (i_degree, j_degree, k_degree)
+%                 2D case (i_degree, j_degree, 0)
+FFD_DEGREE= (6, 1, 0)
+%
+% Surface grid continuity at the intersection with the faces of the FFD boxes.
+% To keep a particular level of surface continuity, SU2 automatically freezes the right
+% number of control point planes (NO_DERIVATIVE, 1ST_DERIVATIVE, 2ND_DERIVATIVE, USER_INPUT)
+FFD_CONTINUITY= USER_INPUT
+%
+% Definition of the FFD planes to be frozen in the FFD (x,y,z).
+% Value from 0 FFD degree in that direction. Pick a value larger than degree if you do not want to fix any plane.
+%FFD_FIX_I= (0,2,3)
+%FFD_FIX_J= (0,2,3)
+%FFD_FIX_K= (0,2,3)
+
+% ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
+%
+
+DV_KIND= \
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D
+
+%
+% Marker of the surface in which we are going apply the shape deformation
+% NOTE: for deformation the outlet should be a MARKER_SYM to hinder the mesh being ripped apart.
+DV_MARKER= ( wall_hx )
+%
+% Parameters of the shape deformation
+% - FFD_SETTING ( 1.0 )
+% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
+
+DV_PARAM= (BOX, 1, 0, 0, 1.0);  \
+(BOX, 2, 0, 0, 1.0);  \
+(BOX, 3, 0, 0, 1.0);  \
+(BOX, 4, 0, 0, 1.0);  \
+(BOX, 5, 0, 0, 1.0);  \
+(BOX, 1, 1, 0, 1.0);  \
+(BOX, 2, 1, 0, 1.0);  \
+(BOX, 3, 1, 0, 1.0);  \
+(BOX, 4, 1, 0, 1.0);  \
+(BOX, 5, 1, 0, 1.0)
+
+DEFINITION_DV= ( 19, 1.0 | wall_hx | BOX, 0, 0, 1.0, 0.0 )
+
+DV_VALUE= 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0 
+
+%
+% ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
+%
+% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
+DEFORM_LINEAR_SOLVER= FGMRES
+%
+% Preconditioner of the Krylov linear solver (ILU, LU_SGS, JACOBI)
+DEFORM_LINEAR_SOLVER_PREC= ILU
+%
+% Number of smoothing iterations for mesh deformation
+DEFORM_LINEAR_SOLVER_ITER= 1000
+%
+% Number of nonlinear deformation iterations (surface deformation increments)
+DEFORM_NONLINEAR_ITER= 1
+%
+% Minimum residual criteria for the linear solver convergence of grid deformation
+DEFORM_LINEAR_SOLVER_ERROR= 1E-14
+%
+% Print the residuals during mesh deformation to the console (YES, NO)
+DEFORM_CONSOLE_OUTPUT= YES
+%
+% Deformation coefficient (linear elasticity limits from -1.0 to 0.5, a larger
+% value is also possible)
+DEFORM_COEFF = 0.0
+%
+% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
+%                                           WALL_DISTANCE, CONSTANT_STIFFNESS)
+DEFORM_STIFFNESS_TYPE= WALL_DISTANCE
+%
+% Deform the grid only close to the surface. It is possible to specify how much
+% of the volumetric grid is going to be deformed in meters or inches (1E6 by default)
+DEFORM_LIMIT = 1E6
diff --git a/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg b/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg
new file mode 100644
index 00000000000..aff2d5561a8
--- /dev/null
+++ b/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg
@@ -0,0 +1,109 @@
+
+
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+
+SOLVER= INC_NAVIER_STOKES
+KIND_TURB_MODEL= NONE
+
+MARKER_ANALYZE= (outlet)
+MARKER_ANALYZE_AVERAGE= AREA
+
+MARKER_MONITORING= ( NONE )
+MARKER_PLOTTING= ( NONE )
+
+WRT_ZONE_HIST= YES
+
+SCREEN_OUTPUT= INNER_ITER WALL_TIME RMS_PRESSURE RMS_PROGRESS_VARIABLE
+
+HISTORY_OUTPUT= RMS_RES AERO_COEFF FLOW_COEFF FLOW_COEFF_SURF
+
+VOLUME_OUTPUT= SOLUTION PRIMITIVE SOURCE RESIDUAL LOOKUP
+
+OUTPUT_FILES= (RESTART_ASCII)
+
+INNER_ITER= 1
+
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+
+MARKER_SYM= ( symmetry_ym, symmetry_yp )
+
+MARKER_ISOTHERMAL= ( wall_burner, 450.0 )
+
+INLET_MATCHING_TOLERANCE= 1e-5
+
+INC_INLET_TYPE= VELOCITY_INLET
+
+MARKER_INLET= (inlet, 300.0, 0.4, 1.0, 0.0, 0.0)
+MARKER_INLET_SPECIES= (inlet, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
+
+INC_OUTLET_TYPE= PRESSURE_OUTLET
+MARKER_OUTLET= (outlet, 0.0)
+MARKER_SPECIES_STRONG_BC= (inlet, outlet, wall_burner)
+
+% ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
+
+INC_DENSITY_MODEL= VARIABLE
+INC_DENSITY_INIT= 1.1766
+INC_VELOCITY_INIT= ( 0.2, 0, 0 )
+INC_ENERGY_EQUATION= YES
+INC_TEMPERATURE_INIT= 300.0
+INC_NONDIM= DIMENSIONAL
+
+% -------------------- FLUID MODEL --------------------------------------- %
+
+FLUID_MODEL= FLUID_FLAMELET
+FILENAME_LUT= fgm_ch4.drg
+FLAME_INIT= (0.004, 0.0, 0.0, 1.0, 0.0, 0.0, 0.2e-3, 1.0)
+
+% -------------------- SPECIES TRANSPORT ---------------------------------------%
+
+USER_SCALAR_NAMES= (Y-CO, Y-NOx_tot)
+
+USER_SOURCE_NAMES= ( \
+    ProdRatePos_Y-CO,  ProdRateNegScaled_Y-CO  ,\
+    ProdRateTot_Y-NOx, zero)
+
+DIFFUSIVITY_CONSTANT= 0.00001
+
+CONV_NUM_METHOD_SPECIES= BOUNDED_SCALAR
+MUSCL_SPECIES= NO
+SLOPE_LIMITER_SPECIES= NONE
+
+TIME_DISCRE_SPECIES= EULER_IMPLICIT
+
+SPECIES_INIT= (0, 0, 0, 0, 0, 0, 0)
+SPECIES_CLIPPING= NO
+LOOKUP_NAMES= (MolarWeightMix, Conductivity, HeatRelease, Diffusivity, \
+    ProdRatePos_Y-CO,  ProdRateNegScaled_Y-CO  ,\
+    ProdRateTot_Y-NOx)
+
+% --------------------------- VISCOSITY MODEL ---------------------------------%
+
+CONDUCTIVITY_MODEL= FLAMELET
+DIFFUSIVITY_MODEL= FLAMELET
+KIND_SCALAR_MODEL= FLAMELET
+VISCOSITY_MODEL= FLAMELET
+
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+
+%NUM_METHOD_GRAD= GREEN_GAUSS
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
+
+CFL_NUMBER= 25
+CFL_ADAPT= NO
+
+% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
+
+LINEAR_SOLVER= BCGSTAB
+LINEAR_SOLVER_PREC= ILU
+LINEAR_SOLVER_ERROR= 1E-10
+LINEAR_SOLVER_ITER= 20
+
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+
+CONV_NUM_METHOD_FLOW= FDS
+MUSCL_FLOW= NO
+SLOPE_LIMITER_FLOW= NONE
+VENKAT_LIMITER_COEFF= 10.0
+JST_SENSOR_COEFF= ( 0.5, 0.02 )
+TIME_DISCRE_FLOW= EULER_IMPLICIT
diff --git a/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_master.cfg b/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_master.cfg
new file mode 100644
index 00000000000..1ca70ab9d79
--- /dev/null
+++ b/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_master.cfg
@@ -0,0 +1,55 @@
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+%                                                                              %
+% SU2 configuration file                                                       %
+% Case description: flow through a heat exchanger, CHT setup                   %
+% Author: Nijso Beishuizen, Ole Burghardt                                      %
+% Institution: Bosch Thermotechniek BV, Technical University of Kaiserslautern %
+% Date: 24/11/2020                                                             %
+%                                                                              %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+SOLVER= MULTIPHYSICS
+
+CONFIG_LIST= ( lam_prem_ch4_cht_cfd_fluid.cfg, lam_prem_ch4_cht_cfd_solid.cfg )
+
+%%%%%%%%%%%%%%%%%%
+%   Mesh stuff   %
+%%%%%%%%%%%%%%%%%%
+
+MESH_FORMAT= SU2
+MULTIZONE_MESH= YES
+
+% Restart flow input file
+SOLUTION_FILENAME= solution
+
+% define the interface between the zones
+MARKER_ZONE_INTERFACE= ( cht_interface_fluid, cht_interface_solid )
+MARKER_CHT_INTERFACE=  ( cht_interface_fluid, cht_interface_solid )
+
+CHT_COUPLING_METHOD= DIRECT_TEMPERATURE_ROBIN_HEATFLUX
+
+READ_BINARY_RESTART= NO
+RESTART_SOL= YES
+
+RESTART_FILENAME= restart
+RESTART_ADJ_FILENAME= restart_adj
+
+TIME_DOMAIN= NO
+OUTER_ITER= 10
+
+OUTPUT_WRT_FREQ= 500
+SCREEN_WRT_FREQ_INNER= 1
+SCREEN_WRT_FREQ_OUTER= 1
+
+WRT_VOLUME_OVERWRITE= YES
+
+WRT_ZONE_CONV= YES
+CONV_RESIDUAL_MINVAL= -20
+
+VOLUME_FILENAME= fluid
+
+CONV_FILENAME= history
+
+% --------------------------- Optimization Parameters --------------------------%
+
+MESH_FILENAME= mesh_unstructured_cht.su2
diff --git a/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_solid.cfg b/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_solid.cfg
new file mode 100644
index 00000000000..197980c4899
--- /dev/null
+++ b/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_solid.cfg
@@ -0,0 +1,57 @@
+
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+
+SOLVER= HEAT_EQUATION
+
+MARKER_PLOTTING= ( NONE )
+MARKER_MONITORING= ( NONE )
+
+WRT_ZONE_HIST= YES
+OUTPUT_FILES= ( RESTART_ASCII )
+
+INC_NONDIM= DIMENSIONAL
+
+INNER_ITER= 1
+
+% ---------------- (SOLIDS) CONDUCTION CONDITION DEFINITION -------------------%
+
+FREESTREAM_TEMPERATURE= 450.0
+
+MATERIAL_DENSITY= 2700
+
+THERMAL_CONDUCTIVITY_CONSTANT=200
+
+SPECIFIC_HEAT_CP= 900
+
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+
+MARKER_ISOTHERMAL= ( wall_water, 350.0 )
+
+% -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
+
+TIME_DISCRE_HEAT= EULER_IMPLICIT
+
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
+CFL_NUMBER= 250
+CFL_ADAPT= NO
+
+% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
+
+LINEAR_SOLVER= BCGSTAB
+LINEAR_SOLVER_PREC= ILU
+LINEAR_SOLVER_ERROR= 1e-16
+LINEAR_SOLVER_ITER= 100
+
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+
+TABULAR_FORMAT= CSV
+CONV_FILENAME= history
+VOLUME_FILENAME= solid
+VOLUME_ADJ_FILENAME= adjoint
+VALUE_OBJFUNC_FILENAME= of_eval.dat
+SURFACE_FILENAME= surface_solid
+SURFACE_ADJ_FILENAME= surface_adjoint
+
+
diff --git a/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg b/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg
new file mode 100644
index 00000000000..b100aa3fcb3
--- /dev/null
+++ b/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg
@@ -0,0 +1,110 @@
+
+
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+
+SOLVER= INC_NAVIER_STOKES
+KIND_TURB_MODEL= NONE
+
+MARKER_ANALYZE= (outlet)
+MARKER_ANALYZE_AVERAGE= AREA
+
+MARKER_MONITORING= ( NONE )
+MARKER_PLOTTING= ( NONE )
+
+WRT_ZONE_HIST= YES
+
+%SCREEN_OUTPUT= INNER_ITER WALL_TIME RMS_PRESSURE RMS_VELOCITY-X RMS_VELOCITY-Y RMS_TKE RMS_DISSIPATION LINSOL_ITER LINSOL_RESIDUAL RMS_ADJ_PRESSURE RMS_ADJ_VELOCITY-X RMS_ADJ_VELOCITY-Y
+
+SCREEN_OUTPUT= INNER_ITER WALL_TIME RMS_ADJ_PRESSURE RMS_ADJ_VELOCITY-X RMS_ADJ_VELOCITY-Y RMS_ADJ_PROGRESS_VARIABLE RMS_ADJ_TOTAL_ENTHALPY RMS_ADJ_Y-CO RMS_ADJ_Y-NOx_tot
+
+HISTORY_OUTPUT= RMS_RES AERO_COEFF FLOW_COEFF FLOW_COEFF_SURF
+
+VOLUME_OUTPUT= SOLUTION PRIMITIVE SOURCE RESIDUAL LOOKUP
+
+OUTPUT_FILES= ( RESTART_ASCII)
+
+INNER_ITER= 1
+
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+
+MARKER_SYM= ( symmetry_ym, symmetry_yp )
+
+MARKER_ISOTHERMAL= ( wall_burner, 450.0 )
+
+INLET_MATCHING_TOLERANCE= 1e-5
+
+INC_INLET_TYPE= VELOCITY_INLET
+
+MARKER_INLET= (inlet, 300.0, 0.4, 1.0, 0.0, 0.0)
+MARKER_INLET_SPECIES= (inlet, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
+
+INC_OUTLET_TYPE= PRESSURE_OUTLET
+MARKER_OUTLET= (outlet, 0.0)
+MARKER_SPECIES_STRONG_BC= (inlet, wall_burner)
+
+% ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
+
+INC_DENSITY_MODEL= VARIABLE
+INC_DENSITY_INIT= 1.1766
+INC_VELOCITY_INIT= ( 0.2, 0, 0 )
+INC_ENERGY_EQUATION= YES
+INC_TEMPERATURE_INIT= 300.0
+INC_NONDIM= DIMENSIONAL
+
+% -------------------- FLUID MODEL --------------------------------------- %
+
+FLUID_MODEL= FLUID_FLAMELET
+FILENAME_LUT= fgm_ch4.drg
+FLAME_INIT= (0.004, 0.0, 0.0, 1, 0, 0, 0.2e-3, 1)
+
+% -------------------- SPECIES TRANSPORT ---------------------------------------%
+
+USER_SCALAR_NAMES= (Y-CO, Y-NOx_tot)
+
+USER_SOURCE_NAMES= ( \
+    ProdRatePos_Y-CO,  ProdRateNegScaled_Y-CO  ,\
+    ProdRateTot_Y-NOx, zero)
+
+DIFFUSIVITY_CONSTANT= 0.00001
+
+CONV_NUM_METHOD_SPECIES= BOUNDED_SCALAR
+MUSCL_SPECIES= NO
+SLOPE_LIMITER_SPECIES= NONE
+
+TIME_DISCRE_SPECIES= EULER_IMPLICIT
+
+SPECIES_INIT= (0, 0, 0, 0, 0, 0, 0)
+SPECIES_CLIPPING= NO
+LOOKUP_NAMES= (MolarWeightMix, Conductivity, HeatRelease, Diffusivity, \
+    ProdRatePos_Y-CO,  ProdRateNegScaled_Y-CO  ,\
+    ProdRateTot_Y-NOx)
+
+% --------------------------- VISCOSITY MODEL ---------------------------------%
+
+CONDUCTIVITY_MODEL= FLAMELET
+DIFFUSIVITY_MODEL= FLAMELET
+KIND_SCALAR_MODEL= FLAMELET
+VISCOSITY_MODEL= FLAMELET
+
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+
+%NUM_METHOD_GRAD= GREEN_GAUSS
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
+CFL_NUMBER= 25
+CFL_ADAPT= NO
+
+% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
+
+LINEAR_SOLVER= BCGSTAB
+LINEAR_SOLVER_PREC= ILU
+LINEAR_SOLVER_ERROR= 1E-10
+LINEAR_SOLVER_ITER= 20
+
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+
+CONV_NUM_METHOD_FLOW= FDS
+MUSCL_FLOW= NO
+SLOPE_LIMITER_FLOW= NONE
+VENKAT_LIMITER_COEFF= 10.0
+JST_SENSOR_COEFF= ( 0.5, 0.02 )
+TIME_DISCRE_FLOW= EULER_IMPLICIT
diff --git a/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_master.cfg b/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_master.cfg
new file mode 100644
index 00000000000..e3e9a0597c1
--- /dev/null
+++ b/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_master.cfg
@@ -0,0 +1,97 @@
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+%                                                                              %
+% SU2 configuration file                                                       %
+% Case description: flow through a heat exchanger, CHT setup                   %
+% Author: Nijso Beishuizen, Ole Burghardt                                      %
+% Institution: Bosch Thermotechniek BV, Technical University of Kaiserslautern %
+% Date: 24/11/2020                                                             %
+%                                                                              %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+SOLVER= MULTIPHYSICS
+
+CONFIG_LIST= ( lam_prem_ch4_cht_ad_fluid.cfg, lam_prem_ch4_cht_ad_solid.cfg )
+
+
+%%%%%%%%%%%%%%%%%%
+%   Mesh stuff   %
+%%%%%%%%%%%%%%%%%%
+
+
+MESH_FILENAME= mesh_unstructured_cht.su2
+% MESH_OUT_FILENAME= mesh_def.su2
+
+MESH_FORMAT= SU2
+MULTIZONE_MESH= YES
+
+% Restart flow input file
+SOLUTION_FILENAME= solution
+READ_BINARY_RESTART= NO
+RESTART_SOL= YES
+RESTART_FILENAME= restart
+RESTART_ADJ_FILENAME= restart_adj
+SOLUTION_ADJ_FILENAME= solution_adj
+
+% define the interface between the zones
+MARKER_ZONE_INTERFACE= ( cht_interface_fluid, cht_interface_solid )
+MARKER_CHT_INTERFACE=  ( cht_interface_fluid, cht_interface_solid )
+
+CHT_COUPLING_METHOD= DIRECT_TEMPERATURE_ROBIN_HEATFLUX
+
+TIME_DOMAIN= NO
+OUTER_ITER = 1100
+
+OUTPUT_WRT_FREQ= 50
+SCREEN_WRT_FREQ_INNER= 1
+SCREEN_WRT_FREQ_OUTER= 1
+
+WRT_VOLUME_OVERWRITE= YES
+
+WRT_ZONE_CONV= YES
+CONV_RESIDUAL_MINVAL= -20
+
+VOLUME_FILENAME= fluid
+
+CONV_FILENAME= history
+
+% --------------------------- Optimization Parameters --------------------------%
+
+GRAD_OBJFUNC_FILENAME= of_grad.csv
+
+OBJECTIVE_FUNCTION= SURFACE_STATIC_TEMPERATURE
+OBJECTIVE_WEIGHT= 1.0
+
+DV_KIND= \
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D
+
+DV_MARKER= ( cht_interface_fluid, cht_interface_solid )
+
+DV_PARAM= \
+ (BOX, 0, 0, 1.0, 1.0);  \
+ (BOX, 2, 0, 1.0, 1.0);  \
+ (BOX, 2, 2, 1.0, 1.0);  \
+ (BOX, 0, 2, 1.0, 1.0);  \
+%
+ (BOX, 1, 0, 0.0, 1.0);  \
+ (BOX, 2, 1, 1.0, 0.0);  \
+ (BOX, 1, 2, 0.0, 1.0);  \
+ (BOX, 0, 1, 1.0, 0.0)
+
+FFD_DEFINITION= (BOX, 0.0089, 0.0006, 0.0,   0.018, 0.0006, 0.0,   0.018, 0.0018, 0.0,   0.0089, 0.0018, 0.0,   0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
+FFD_DEGREE= ( 2, 1, 0)
+FFD_CONTINUITY= 1ST_DERIVATIVE
+FFD_FIX_I= (100)
+FFD_FIX_J= (100)
+FFD_ITERATIONS= 1000
+FFD_TOLERANCE= 1E-10
+
+DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
+
+DV_VALUE=0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0
diff --git a/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_solid.cfg b/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_solid.cfg
new file mode 100644
index 00000000000..197980c4899
--- /dev/null
+++ b/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_solid.cfg
@@ -0,0 +1,57 @@
+
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+
+SOLVER= HEAT_EQUATION
+
+MARKER_PLOTTING= ( NONE )
+MARKER_MONITORING= ( NONE )
+
+WRT_ZONE_HIST= YES
+OUTPUT_FILES= ( RESTART_ASCII )
+
+INC_NONDIM= DIMENSIONAL
+
+INNER_ITER= 1
+
+% ---------------- (SOLIDS) CONDUCTION CONDITION DEFINITION -------------------%
+
+FREESTREAM_TEMPERATURE= 450.0
+
+MATERIAL_DENSITY= 2700
+
+THERMAL_CONDUCTIVITY_CONSTANT=200
+
+SPECIFIC_HEAT_CP= 900
+
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+
+MARKER_ISOTHERMAL= ( wall_water, 350.0 )
+
+% -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
+
+TIME_DISCRE_HEAT= EULER_IMPLICIT
+
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
+CFL_NUMBER= 250
+CFL_ADAPT= NO
+
+% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
+
+LINEAR_SOLVER= BCGSTAB
+LINEAR_SOLVER_PREC= ILU
+LINEAR_SOLVER_ERROR= 1e-16
+LINEAR_SOLVER_ITER= 100
+
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+
+TABULAR_FORMAT= CSV
+CONV_FILENAME= history
+VOLUME_FILENAME= solid
+VOLUME_ADJ_FILENAME= adjoint
+VALUE_OBJFUNC_FILENAME= of_eval.dat
+SURFACE_FILENAME= surface_solid
+SURFACE_ADJ_FILENAME= surface_adjoint
+
+
diff --git a/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_dot_master.cfg b/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_dot_master.cfg
new file mode 100644
index 00000000000..4a3e831b6c6
--- /dev/null
+++ b/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_dot_master.cfg
@@ -0,0 +1,97 @@
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+%                                                                              %
+% SU2 configuration file                                                       %
+% Case description: flow through a heat exchanger, CHT setup                   %
+% Author: Nijso Beishuizen, Ole Burghardt                                      %
+% Institution: Bosch Thermotechniek BV, Technical University of Kaiserslautern %
+% Date: 24/11/2020                                                             %
+%                                                                              %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+SOLVER= MULTIPHYSICS
+
+CONFIG_LIST= ( lam_prem_ch4_cht_ad_fluid.cfg, lam_prem_ch4_cht_ad_solid.cfg )
+
+
+%%%%%%%%%%%%%%%%%%
+%   Mesh stuff   %
+%%%%%%%%%%%%%%%%%%
+
+
+MESH_FILENAME= mesh_unstructured_cht.su2
+% MESH_OUT_FILENAME= mesh_def.su2
+
+MESH_FORMAT= SU2
+MULTIZONE_MESH= YES
+
+% Restart flow input file
+SOLUTION_FILENAME= solution
+READ_BINARY_RESTART= NO
+RESTART_SOL= YES
+RESTART_FILENAME= restart
+RESTART_ADJ_FILENAME= restart_adj
+SOLUTION_ADJ_FILENAME= restart_adj
+
+% define the interface between the zones
+MARKER_ZONE_INTERFACE= ( cht_interface_fluid, cht_interface_solid )
+MARKER_CHT_INTERFACE=  ( cht_interface_fluid, cht_interface_solid )
+
+CHT_COUPLING_METHOD= DIRECT_TEMPERATURE_ROBIN_HEATFLUX
+
+TIME_DOMAIN= NO
+OUTER_ITER = 11
+
+OUTPUT_WRT_FREQ= 500
+SCREEN_WRT_FREQ_INNER= 1
+SCREEN_WRT_FREQ_OUTER= 1
+
+WRT_VOLUME_OVERWRITE= YES
+
+WRT_ZONE_CONV= YES
+CONV_RESIDUAL_MINVAL= -20
+
+VOLUME_FILENAME= fluid
+
+CONV_FILENAME= history
+
+% --------------------------- Optimization Parameters --------------------------%
+
+GRAD_OBJFUNC_FILENAME= of_grad.csv
+
+OBJECTIVE_FUNCTION= SURFACE_STATIC_TEMPERATURE
+OBJECTIVE_WEIGHT= 1.0
+
+DV_KIND= \
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D,\
+FFD_CONTROL_POINT_2D
+
+DV_MARKER= ( cht_interface_fluid, cht_interface_solid )
+
+DV_PARAM= \
+ (BOX, 0, 0, 1.0, 1.0);  \
+ (BOX, 2, 0, 1.0, 1.0);  \
+ (BOX, 2, 2, 1.0, 1.0);  \
+ (BOX, 0, 2, 1.0, 1.0);  \
+%
+ (BOX, 1, 0, 0.0, 1.0);  \
+ (BOX, 2, 1, 1.0, 0.0);  \
+ (BOX, 1, 2, 0.0, 1.0);  \
+ (BOX, 0, 1, 1.0, 0.0)
+
+FFD_DEFINITION= (BOX, 0.0089, 0.0006, 0.0,   0.018, 0.0006, 0.0,   0.018, 0.0018, 0.0,   0.0089, 0.0018, 0.0,   0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
+FFD_DEGREE= ( 2, 1, 0)
+FFD_CONTINUITY= 1ST_DERIVATIVE
+FFD_FIX_I= (100)
+FFD_FIX_J= (100)
+FFD_ITERATIONS= 1000
+FFD_TOLERANCE= 1E-10
+
+DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
+
+DV_VALUE=0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0
diff --git a/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg b/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg
new file mode 100644
index 00000000000..6fa6662e253
--- /dev/null
+++ b/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg
@@ -0,0 +1,136 @@
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+% SU2 configuration file                                                       %
+% Case description: Laminar premixed flame stabilized on isothermal burner     %
+%                   axisymmetric setup
+% Author: Nijso Beishuizen                                                     %
+% Institution: Bosch Thermotechnology                                          %
+% Date: 08/09/2021                                                             %
+% File Version 7.5.0 "Falcon", branch: feature_new_flamelet                    %
+%                                                                              %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+%
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
+SOLVER= INC_NAVIER_STOKES
+KIND_TURB_MODEL= NONE
+MATH_PROBLEM= DIRECT
+RESTART_SOL= YES
+%
+% ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
+%
+INC_DENSITY_MODEL= VARIABLE 
+INC_ENERGY_EQUATION= YES
+INC_DENSITY_INIT= 1.00
+INC_VELOCITY_INIT= (0.5, 0.0, 0.0 )
+INC_TEMPERATURE_INIT= 300.0
+INC_NONDIM= DIMENSIONAL
+%
+% 
+AXISYMMETRIC= YES
+% -------------------- FLUID MODEL --------------------------------------- %
+%
+FLUID_MODEL= FLUID_FLAMELET
+FILENAME_LUT= fgm_ch4.drg
+%
+% -------------------- SCALAR TRANSPORT ---------------------------------------%
+%
+KIND_SCALAR_MODEL= FLAMELET      
+DIFFUSIVITY_MODEL= FLAMELET
+VISCOSITY_MODEL= FLAMELET
+CONDUCTIVITY_MODEL= FLAMELET
+FLAME_INIT= (0.0032, 0.0, 0.0, 1, 0.1, 0, 1e-3, 0.1)
+% # progvar, enthalpy
+SPECIES_INIT= (0.0, -210000, 0.0, 0.0)
+CONV_NUM_METHOD_SPECIES= BOUNDED_SCALAR
+%CONV_NUM_METHOD_SPECIES= SCALAR_UPWIND
+MUSCL_SPECIES= YES
+SLOPE_LIMITER_SPECIES= NONE
+TIME_DISCRE_SPECIES= EULER_IMPLICIT
+% SCALAR CLIPPING
+SPECIES_CLIPPING= YES
+SPECIES_CLIPPING_MIN= 0 -2e6 0 0
+SPECIES_CLIPPING_MAX= 1 2e6 1 1
+%
+MARKER_INLET_SPECIES= (inlet, 0, -193600.0, 0.0, 0.0)
+CFL_REDUCTION_SPECIES= 1.0
+MARKER_SPECIES_STRONG_BC= (inlet, outlet, wall)
+LOOKUP_NAMES= (MolarWeightMix, Conductivity, Cp, HeatRelease, Diffusivity)
+USER_SCALAR_NAMES= (CO, NOx)
+USER_SOURCE_NAMES= ( \
+    ProdRatePos_Y-CO,  ProdRateNegScaled_Y-CO  ,\
+    ProdRateTot_Y-NOx, NULL )
+%
+% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
+%
+REF_ORIGIN_MOMENT_X= 0.25
+REF_ORIGIN_MOMENT_Y= 0.00
+REF_ORIGIN_MOMENT_Z= 0.00
+REF_LENGTH= 1.0
+REF_AREA= 1.0
+%
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
+MARKER_ISOTHERMAL= (wall, 450)
+MARKER_SYM= (symmetry, symmetry_2-part-fluid)
+INC_INLET_TYPE= VELOCITY_INLET
+MARKER_INLET= (inlet, 300.0, 0.20, 1.0, 0.0, 0.0)
+INC_OUTLET_TYPE= PRESSURE_OUTLET
+MARKER_OUTLET= (outlet, 0.0)
+MARKER_PLOTTING= ( wall )
+MARKER_MONITORING= ( wall )
+MARKER_ANALYZE= ( inlet,outlet )
+MARKER_ANALYZE_AVERAGE= AREA
+%
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
+CFL_NUMBER= 20
+CFL_ADAPT= NO
+ITER= 10000
+OUTPUT_WRT_FREQ= 100
+%
+% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
+%
+LINEAR_SOLVER= FGMRES
+LINEAR_SOLVER_PREC= ILU
+LINEAR_SOLVER_ERROR= 1E-10
+LINEAR_SOLVER_ITER= 25
+%
+% -------------------------- MULTIGRID PARAMETERS -----------------------------%
+%
+MGLEVEL= 0
+%
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
+CONV_NUM_METHOD_FLOW= FDS
+MUSCL_FLOW= YES
+SLOPE_LIMITER_FLOW= NONE
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+%
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
+CONV_RESIDUAL_MINVAL= -15
+CONV_STARTITER= 10
+CONV_CAUCHY_ELEMS= 100
+CONV_CAUCHY_EPS= 1E-6
+SCREEN_OUTPUT= INNER_ITER WALL_TIME RMS_VELOCITY-X RMS_VELOCITY-Y RMS_PRESSURE RMS_PROGRESS_VARIABLE RMS_TOTAL_ENTHALPY
+HISTORY_OUTPUT= RMS_RES AERO_COEFF FLOW_COEFF FLOW_COEFF_SURF
+VOLUME_OUTPUT= SOLUTION PRIMITIVE SOURCE RESIDUAL SENSITIVITY LOOKUP TIMESTEP
+CONV_FIELD= RMS_PRESSURE
+%
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+%
+MESH_FORMAT= SU2
+MESH_FILENAME= mesh_axi.su2
+MESH_OUT_FILENAME= mesh_out.su2
+SOLUTION_FILENAME= solution
+RESTART_FILENAME= restart
+%OUTPUT_FILES= (RESTART,PARAVIEW,PARAVIEW_MULTIBLOCK) 
+OUTPUT_FILES= (RESTART) 
+TABULAR_FORMAT= CSV
+CONV_FILENAME= history
+VOLUME_FILENAME= flow
+SURFACE_FILENAME= surface_flow
+WRT_PERFORMANCE= NO 
+SCREEN_WRT_FREQ_INNER= 1
+SCREEN_WRT_FREQ_OUTER= 1
diff --git a/TestCases/flamelet/README.md b/TestCases/flamelet/README.md
new file mode 100644
index 00000000000..8608d466f0d
--- /dev/null
+++ b/TestCases/flamelet/README.md
@@ -0,0 +1,8 @@
+# Flamelet regression cases
+
+## laminar_premixed_flame
+1. A laminar premixed flame stabilized on an isothermal burner with a fixed wall temperature using a low resolution look-up table for all thermo-chemical quantities.
+2. A laminar premixed flame including a heat exchanger, AD test.
+3. A laminar premixed flame including a heat exchanger (Conjugate Heat Transfer).
+4. A laminar premixed flame including a heat exchanger (Conjugate Heat Transfer), AD test.
+5. An axisymmetric laminar premixed flame.
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 95c486de561..50dd5b013ce 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -38,6 +38,28 @@ def main():
 
     test_list = []
 
+    #######################
+    ### Flamelet solver ###
+    #######################
+
+    # 2D planar laminar premixed methane flame on isothermal burner (restart)
+    cfd_flamelet_ch4 = TestCase('cfd_flamelet_ch4')
+    cfd_flamelet_ch4.cfg_dir = "flamelet/01_laminar_premixed_ch4_flame_cfd"
+    cfd_flamelet_ch4.cfg_file = "lam_prem_ch4_cfd.cfg"
+    cfd_flamelet_ch4.test_iter = 10
+    cfd_flamelet_ch4.test_vals = [-15.313265, -15.180884, -15.291808, -8.488238, -15.010141, -15.920950]
+    cfd_flamelet_ch4.new_output = True
+    test_list.append(cfd_flamelet_ch4)
+
+   # axisymmetric 2D planar laminar premixed methane flame on isothermal burner (restart)
+    cfd_flamelet_ch4_axi = TestCase('cfd_flamelet_ch4_axi')
+    cfd_flamelet_ch4_axi.cfg_dir = "flamelet/05_laminar_premixed_ch4_flame_cfd_axi"
+    cfd_flamelet_ch4_axi.cfg_file = "lam_prem_ch4_cfd_axi.cfg"
+    cfd_flamelet_ch4_axi.test_iter = 10
+    cfd_flamelet_ch4_axi.test_vals = [-11.054149, -12.276393, -11.299388, -13.877670, -6.291548]
+    cfd_flamelet_ch4_axi.new_output = True
+    test_list.append(cfd_flamelet_ch4_axi)
+
     #########################
     ## NEMO solver ###
     #########################
@@ -1502,6 +1524,25 @@ def main():
 
     pass_list = [ test.run_test() for test in test_list ]
 
+    ######################################
+    ### RUN CHT TEST WITH FILEDIFF     ###
+    ######################################
+
+    # 2D planar laminar premixed methane flame on isothermal burner with conjugate heat transfer in cooling fin (restart)
+    cfd_flamelet_ch4_cht                  = TestCase('cfd_flamelet_ch4_cht')
+    cfd_flamelet_ch4_cht.cfg_dir          = "flamelet/03_laminar_premixed_ch4_flame_cht_cfd"
+    cfd_flamelet_ch4_cht.cfg_file         = "lam_prem_ch4_cht_cfd_master.cfg"
+    cfd_flamelet_ch4_cht.test_iter        = 10
+    cfd_flamelet_ch4_cht.command          = TestCase.Command("mpirun -n 2", "SU2_CFD")
+    cfd_flamelet_ch4_cht.timeout          = 1600
+    cfd_flamelet_ch4_cht.reference_file   = "restart_0.csv.ref"
+    cfd_flamelet_ch4_cht.test_file        = "restart_0.csv"
+    cfd_flamelet_ch4_cht.multizone        = True
+    cfd_flamelet_ch4_cht.comp_threshold   = 1e-6
+    cfd_flamelet_ch4_cht.tol_file_percent = 0.1
+    pass_list.append(cfd_flamelet_ch4_cht.run_filediff())
+    test_list.append(cfd_flamelet_ch4_cht)
+
     ######################################
     ### RUN SU2_SOL TESTS              ###
     ######################################
diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index 436715d9866..d7415431119 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -340,6 +340,77 @@ def main():
 
     pass_list = [ test.run_test() for test in test_list ]
 
+    ##################################
+    ### Disc. adj. flamelet solver ###
+    ##################################
+
+    # 2D planar laminar premixed flame on isothermal burner (restart)
+    discadj_flamelet_ch4_hx                  = TestCase('discadj_flamelet_ch4_hx')
+    discadj_flamelet_ch4_hx.command          = TestCase.Command("mpirun -n 2", "SU2_CFD_AD")
+    discadj_flamelet_ch4_hx.cfg_dir          = "flamelet/02_laminar_premixed_ch4_flame_hx_ad"
+    discadj_flamelet_ch4_hx.cfg_file         = "lam_prem_ch4_hx_ad.cfg"
+    discadj_flamelet_ch4_hx.multizone        = True
+    discadj_flamelet_ch4_hx.test_iter        = 10
+    discadj_flamelet_ch4_hx.timeout          = 20000
+    discadj_flamelet_ch4_hx.reference_file   = "restart_adj_custom.csv.ref"
+    discadj_flamelet_ch4_hx.test_file        = "restart_adj_custom.csv"
+    discadj_flamelet_ch4_hx.comp_threshold   = 1e-6
+    discadj_flamelet_ch4_hx.tol_file_percent = 0.1
+    pass_list.append(discadj_flamelet_ch4_hx.run_filediff())
+    test_list.append(discadj_flamelet_ch4_hx)
+
+    # 2D planar laminar premixed flame on isothermal burner with conjugate heat transfer (restart)
+    discadj_flamelet_ch4_cht                  = TestCase('discadj_flamelet_ch4_cht')
+    discadj_flamelet_ch4_cht.command          = TestCase.Command("mpirun -n 2", "SU2_CFD_AD")
+    discadj_flamelet_ch4_cht.cfg_dir          = "flamelet/04_laminar_premixed_ch4_flame_cht_ad"
+    discadj_flamelet_ch4_cht.cfg_file         = "lam_prem_ch4_cht_ad_master.cfg"
+    discadj_flamelet_ch4_cht.multizone        = True
+    discadj_flamelet_ch4_cht.test_iter        = 5
+    discadj_flamelet_ch4_cht.reference_file   = "restart_adj_T_0.csv.ref"
+    discadj_flamelet_ch4_cht.test_file        = "restart_adj_T_0.csv"
+    discadj_flamelet_ch4_cht.comp_threshold   = 1e-6
+    discadj_flamelet_ch4_cht.tol_file_percent = 0.1
+    discadj_flamelet_ch4_cht.timeout          = 20000
+    pass_list.append(discadj_flamelet_ch4_cht.run_filediff())
+    test_list.append(discadj_flamelet_ch4_cht)
+
+    ################################################
+    ### Gradient check (dot) for flamelet solver ###
+    ################################################
+    
+    # 2D planar laminar premixed flame on isothermal burner (restart)
+    # This test restarts on the output of test discadj_flamelet_ch4_hx and 
+    # will only pass if test discadj_flamelet_ch4_hx passes.
+    dot_flamelet_ch4_hx                  = TestCase('dot_flamelet_ch4_hx')
+    dot_flamelet_ch4_hx.cfg_dir          = "flamelet/02_laminar_premixed_ch4_flame_hx_ad"
+    dot_flamelet_ch4_hx.cfg_file         = "lam_prem_ch4_hx_dot.cfg"
+    dot_flamelet_ch4_hx.test_iter        = 10
+    dot_flamelet_ch4_hx.command          = TestCase.Command("mpirun -n 2", "SU2_DOT_AD")
+    dot_flamelet_ch4_hx.timeout          = 20000
+    dot_flamelet_ch4_hx.reference_file   = "of_grad.csv.ref"
+    dot_flamelet_ch4_hx.test_file        = "of_grad.csv"
+    dot_flamelet_ch4_hx.comp_threshold   = 1e-6
+    dot_flamelet_ch4_hx.tol_file_percent = 0.1
+    pass_list.append(dot_flamelet_ch4_hx.run_filediff())
+    test_list.append(dot_flamelet_ch4_hx)
+
+    # 2D planar laminar premixed flame on isothermal burner with conjugate heat transfer (restart)
+    # This test restarts on the output of test discadj_flamelet_ch4_cht and 
+    # will only pass if test discadj_flamelet_ch4_cht passes.
+    dot_flamelet_ch4_cht                  = TestCase('dot_flamelet_ch4_cht')
+    dot_flamelet_ch4_cht.cfg_dir          = "flamelet/04_laminar_premixed_ch4_flame_cht_ad"
+    dot_flamelet_ch4_cht.cfg_file         = "lam_prem_ch4_cht_dot_master.cfg"
+    dot_flamelet_ch4_cht.multizone        = True
+    dot_flamelet_ch4_cht.test_iter        = 10
+    dot_flamelet_ch4_cht.command          = TestCase.Command("mpirun -n 2", "SU2_DOT_AD")
+    dot_flamelet_ch4_cht.timeout          = 20000
+    dot_flamelet_ch4_cht.reference_file   = "of_grad.csv.ref"
+    dot_flamelet_ch4_cht.test_file        = "of_grad.csv"
+    dot_flamelet_ch4_cht.comp_threshold   = 1e-6
+    dot_flamelet_ch4_cht.tol_file_percent = 0.1
+    pass_list.append(dot_flamelet_ch4_cht.run_filediff())
+    test_list.append(dot_flamelet_ch4_cht)
+
     ##################################################
     ### Structural Adjoint - Topology Optimization ###
     ##################################################
diff --git a/TestCases/species_transport/multizone/zone1.cfg b/TestCases/species_transport/multizone/zone1.cfg
index 50c6e455e4c..c18f0565b1e 100644
--- a/TestCases/species_transport/multizone/zone1.cfg
+++ b/TestCases/species_transport/multizone/zone1.cfg
@@ -19,7 +19,6 @@ INLET_FILENAME= inlet_venturi.dat
 INC_INLET_TYPE=  VELOCITY_INLET VELOCITY_INLET
 MARKER_INLET= ( gas_inlet1,       300.0, 1.0, 1.0,  0.0, 0.0,\
                 air_axial_inlet1, 305.0, 1.0, 0.0  -1.0, 0.0 )
-SPECIES_USE_STRONG_BC= NO
 MARKER_INLET_SPECIES= (gas_inlet1,       0.5, 0.5,\
                        air_axial_inlet1, 0.6, 0.0 )	
 MARKER_PLOTTING= (NONE)
diff --git a/TestCases/species_transport/multizone/zone2.cfg b/TestCases/species_transport/multizone/zone2.cfg
index 622685ab51f..2ad80c3dd58 100644
--- a/TestCases/species_transport/multizone/zone2.cfg
+++ b/TestCases/species_transport/multizone/zone2.cfg
@@ -18,7 +18,6 @@ SPECIFIED_INLET_PROFILE= NO
 INLET_FILENAME= inlet_venturi.dat
 INC_INLET_TYPE=  VELOCITY_INLET
 MARKER_INLET= ( air_axial_inlet2, 310.0, 1.2, 0.0  -1.0, 0.0 )
-SPECIES_USE_STRONG_BC= NO
 MARKER_INLET_SPECIES= (air_axial_inlet2, 0.6, 0.0 )	
 INC_OUTLET_TYPE= PRESSURE_OUTLET
 MARKER_OUTLET= ( outlet2, 0.0 )
diff --git a/TestCases/species_transport/passive_transport_validation/passive_transport.cfg b/TestCases/species_transport/passive_transport_validation/passive_transport.cfg
index 09c870157d6..a618a1e4e1c 100644
--- a/TestCases/species_transport/passive_transport_validation/passive_transport.cfg
+++ b/TestCases/species_transport/passive_transport_validation/passive_transport.cfg
@@ -52,7 +52,7 @@ MARKER_SYM= ( top, bottom )
 INC_INLET_TYPE= VELOCITY_INLET, VELOCITY_INLET
 MARKER_INLET= ( gas_inlet, 300, 1, 1.0, 0.0, 0.0, air_inlet, 300, 1, 1.0, 0.0, 0.0 )
 %
-SPECIES_USE_STRONG_BC= YES
+MARKER_SPECIES_STRONG_BC= (gas_inlet, air_inlet, outlet)
 MARKER_INLET_SPECIES = (gas_inlet, 1.0, air_inlet, 0.0 )
 %
 INC_OUTLET_TYPE= PRESSURE_OUTLET
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi.cfg
index 6a223174a54..d39ae5957ac 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi.cfg
@@ -48,7 +48,6 @@ MARKER_SYM= ( axis )
 INC_INLET_TYPE=  VELOCITY_INLET VELOCITY_INLET
 MARKER_INLET= ( gas_inlet,       300, 1.0, 1.0,  0.0, 0.0,\
                 air_axial_inlet, 300, 1.0, 0.0, -1.0, 0.0 )
-SPECIES_USE_STRONG_BC= NO
 MARKER_INLET_SPECIES= (gas_inlet,       1.0,\
                        air_axial_inlet, 0.6 )
 %
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_boundedscalar.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_boundedscalar.cfg
index b38b3390754..4f5a9a62460 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_boundedscalar.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_boundedscalar.cfg
@@ -48,7 +48,6 @@ MARKER_SYM= ( axis )
 INC_INLET_TYPE=  VELOCITY_INLET VELOCITY_INLET
 MARKER_INLET= ( gas_inlet,       300, 1.0, 1.0,  0.0, 0.0,\
                 air_axial_inlet, 300, 1.0, 0.0, -1.0, 0.0 )
-SPECIES_USE_STRONG_BC= NO
 MARKER_INLET_SPECIES= (gas_inlet,       1.0,\
                        air_axial_inlet, 0.6 )
 %
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel.cfg
index 7b022511d86..5ad7433c102 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel.cfg
@@ -60,7 +60,6 @@ INLET_FILENAME= inlet_venturi.dat
 INC_INLET_TYPE=  VELOCITY_INLET VELOCITY_INLET
 MARKER_INLET= ( gas_inlet,       300, 1.0, 1.0,  0.0, 0.0,\
                 air_axial_inlet, 300, 1.0, 0.0, -1.0, 0.0 )
-SPECIES_USE_STRONG_BC= NO
 MARKER_INLET_SPECIES= (gas_inlet, 1.0,\          
                        air_axial_inlet, 0.6)           
 %
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg
index 662646b3134..f49ea42aa8e 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg
@@ -64,7 +64,7 @@ INLET_FILENAME= inlet_venturi.dat
 INC_INLET_TYPE=  VELOCITY_INLET VELOCITY_INLET
 MARKER_INLET= ( gas_inlet,       300, 15.0, 1.0,  0.0, 0.0,\
                 air_axial_inlet, 300, 10.0, 0.0, -1.0, 0.0 )
-SPECIES_USE_STRONG_BC= YES
+MARKER_SPECIES_STRONG_BC= (gas-inlet, air_axial_inlet, wall, outlet)
 MARKER_INLET_SPECIES= (gas_inlet, 1.0, \          
                        air_axial_inlet, 0.0)           
 %
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_boundedscalar.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_boundedscalar.cfg
index 8a4c8d6a40d..319ab8e778e 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_boundedscalar.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_boundedscalar.cfg
@@ -60,7 +60,6 @@ INLET_FILENAME= inlet_venturi.dat
 INC_INLET_TYPE=  VELOCITY_INLET VELOCITY_INLET
 MARKER_INLET= ( gas_inlet,       300, 1.0, 1.0,  0.0, 0.0,\
                 air_axial_inlet, 300, 1.0, 0.0, -1.0, 0.0 )
-SPECIES_USE_STRONG_BC= NO
 MARKER_INLET_SPECIES= (gas_inlet, 1.0,\          
                        air_axial_inlet, 0.6)           
 %
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg
index e208b15fa59..93ad887d155 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg
@@ -70,7 +70,7 @@ INLET_FILENAME= inlet_venturi.dat
 INC_INLET_TYPE=  VELOCITY_INLET VELOCITY_INLET
 MARKER_INLET= ( gas_inlet,       400, 5.0, 1.0,  0.0, 0.0,\
                 air_axial_inlet, 300, 5.0, 0.0, -1.0, 0.0 )
-SPECIES_USE_STRONG_BC= YES
+MARKER_SPECIES_STRONG_BC= (gas_inlet, air_axial_inlet, wall, outlet)
 MARKER_INLET_SPECIES= (gas_inlet, 1.0, \          
                        air_axial_inlet, 0.6)           
 %
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg
index d941f96705f..2cd26d57e2d 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg
@@ -71,7 +71,7 @@ INLET_FILENAME= inlet_venturi.dat
 INC_INLET_TYPE=  VELOCITY_INLET VELOCITY_INLET
 MARKER_INLET= ( gas_inlet,       400, 5.0, 1.0,  0.0, 0.0,\
                 air_axial_inlet, 300, 5.0, 0.0, -1.0, 0.0 )
-SPECIES_USE_STRONG_BC= YES
+MARKER_SPECIES_STRONG_BC= (gas_inlet, air_axial_inlet, wall, outlet)
 MARKER_INLET_SPECIES= (gas_inlet, 1.0, \          
                        air_axial_inlet, 0.6)           
 %
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_viscosity.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_viscosity.cfg
index dd8017ec2a6..7df939a97d6 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_viscosity.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_viscosity.cfg
@@ -65,7 +65,6 @@ INLET_FILENAME= inlet_venturi.dat
 INC_INLET_TYPE=  VELOCITY_INLET VELOCITY_INLET
 MARKER_INLET= ( gas_inlet,       300, 5.0, 1.0,  0.0, 0.0,\
                 air_axial_inlet, 300, 3.0, 0.0, -1.0, 0.0 )
-SPECIES_USE_STRONG_BC= NO
 MARKER_INLET_SPECIES= (gas_inlet, 1.0, \          
                        air_axial_inlet, 0.6)
 %
diff --git a/TestCases/species_transport/venturi_primitive_3species/species3_primitiveVenturi_inletFile.cfg b/TestCases/species_transport/venturi_primitive_3species/species3_primitiveVenturi_inletFile.cfg
index 6de6854f3ee..06b085e6fdf 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species3_primitiveVenturi_inletFile.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species3_primitiveVenturi_inletFile.cfg
@@ -51,7 +51,6 @@ INLET_FILENAME= inlet_venturi.dat
 INC_INLET_TYPE=  VELOCITY_INLET VELOCITY_INLET
 MARKER_INLET= ( gas_inlet,       300, 1.0, 1.0,  0.0, 0.0,\
                 air_axial_inlet, 300, 1.0, 0.0, -1.0, 0.0 )
-SPECIES_USE_STRONG_BC= NO
 MARKER_INLET_SPECIES= (gas_inlet,       0.5, 0.5,\
                        air_axial_inlet, 0.6, 0.0 )
 %
diff --git a/TestCases/user_defined_functions/lam_flatplate.cfg b/TestCases/user_defined_functions/lam_flatplate.cfg
index c2544a6851e..457ef91fc10 100644
--- a/TestCases/user_defined_functions/lam_flatplate.cfg
+++ b/TestCases/user_defined_functions/lam_flatplate.cfg
@@ -37,7 +37,7 @@ CUSTOM_OUTPUTS= 'velocity : Macro{sqrt(pow(VELOCITY_X, 2) + pow(VELOCITY_Y, 2) +
                  probe1 : Probe{$velocity}[0.005, 0.005, 0.05]'
 %
 % "COMBO" is the name and group of the output for the objective function
-% (regardless of definition). "CUSTOM" is the group for all custom outpus.
+% (regardless of definition). "CUSTOM" is the group for all custom outputs.
 SCREEN_OUTPUT= INNER_ITER, RMS_DENSITY, RMS_ENERGY, LINSOL_RESIDUAL, FORCE_Z,\
                SURFACE_MASSFLOW, SURFACE_TOTAL_TEMPERATURE, avg_vel, dev_vel, probe1, COMBO
 HISTORY_OUTPUT = ITER, AERO_COEFF, FLOW_COEFF, FLOW_COEFF_SURF, CUSTOM, COMBO
diff --git a/config_template.cfg b/config_template.cfg
index a494d47eea7..e36c6d9cfc3 100644
--- a/config_template.cfg
+++ b/config_template.cfg
@@ -317,7 +317,7 @@ SEMI_SPAN= 0.0
 % ---- NONEQUILIBRIUM GAS, IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS, CoolProp library -------%
 %
 % Fluid model (STANDARD_AIR, IDEAL_GAS, VW_GAS, PR_GAS,
-%              CONSTANT_DENSITY, INC_IDEAL_GAS, INC_IDEAL_GAS_POLY, MUTATIONPP, SU2_NONEQ, FLUID_MIXTURE, COOLPROP)
+%              CONSTANT_DENSITY, INC_IDEAL_GAS, INC_IDEAL_GAS_POLY, MUTATIONPP, SU2_NONEQ, FLUID_MIXTURE, COOLPROP, FLUID_FLAMELET)
 FLUID_MODEL= STANDARD_AIR
 % To find all available fluid name for CoolProp library, clikc the following link:
 % http://www.coolprop.org/fluid_properties/PurePseudoPure.html#list-of-fluids
@@ -375,7 +375,7 @@ INLET_GAS_COMPOSITION = (0.77, 0.23, 0.0, 0.0, 0.0)
 %
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 %
-% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY, POLYNOMIAL_VISCOSITY).
+% Viscosity model (SUTHERLAND, CONSTANT_VISCOSITY, POLYNOMIAL_VISCOSITY, FLAMELET).
 VISCOSITY_MODEL= SUTHERLAND
 %
 % Molecular Viscosity that would be constant (1.716E-5 by default)
@@ -397,7 +397,7 @@ MU_POLYCOEFFS= (0.0, 0.0, 0.0, 0.0, 0.0)
 % --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
 %
 % Laminar Conductivity model (CONSTANT_CONDUCTIVITY, CONSTANT_PRANDTL,
-% POLYNOMIAL_CONDUCTIVITY).
+% POLYNOMIAL_CONDUCTIVITY, FLAMELET).
 CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
 %
 % Molecular Thermal Conductivity that would be constant (0.0257 by default)
@@ -707,10 +707,10 @@ TIME_DISCRE_RADIATION = EULER_IMPLICIT
 
 % --------------------- SPECIES TRANSPORT SIMULATION --------------------------%
 %
-% Specify scalar transport model (NONE, SPECIES_TRANSPORT)
+% Specify scalar transport model (NONE, SPECIES_TRANSPORT, FLAMELET)
 KIND_SCALAR_MODEL= NONE
 %
-% Mass diffusivity model (CONSTANT_DIFFUSIVITY)
+% Mass diffusivity model (CONSTANT_DIFFUSIVITY, FLAMELET)
 DIFFUSIVITY_MODEL= CONSTANT_DIFFUSIVITY
 %
 % Mass diffusivity if DIFFUSIVITY_MODEL= CONSTANT_DIFFUSIVITY is chosen. D_air ~= 0.001
@@ -724,9 +724,6 @@ SCHMIDT_NUMBER_TURBULENT= 0.7
 % For N species, N-1 transport equations are solved, the last one Y_N is solved algebraically as 1-(sum of the species 1 to (N-1))
 MARKER_INLET_SPECIES= (inlet, 0.5, ..., inlet2, 0.6, ...)
 %
-% Use strong inlet and outlet BC in the species solver
-SPECIES_USE_STRONG_BC= NO
-%
 % Convective numerical method for species transport (SCALAR_UPWIND, BOUNDED_SCALAR)
 CONV_NUM_METHOD_SPECIES= SCALAR_UPWIND
 %
@@ -755,6 +752,35 @@ SPECIES_CLIPPING_MAX= 1.0, ...
 % Minimum values for scalar clipping
 SPECIES_CLIPPING_MIN= 0.0, ...
 
+% --------------------- FLAMELET MODEL -----------------------------%
+%
+% Names of the user defined (auxiliary) transport equations.
+USER_SCALAR_NAMES= (Y-CO)
+%
+% Names of the source terms for the user defined transport equations. The source term
+% has the form
+%  S = S_production + S_consumption * Y, with Y the mass fraction of the user scalar
+%  S = S_production + S_consumption * X, with X the mole fraction of the user scalar
+% The second term can have the name "zero" or "null" to indicate that only a total source
+% will be used.
+USER_SOURCE_NAMES= ( ProdRateTot_Y-CO,  zero)
+%
+% Names of variables from the LUT that will be looked up for visualization
+LOOKUP_NAMES= (MolarWeightMix, Conductivity, HeatRelease, Diffusivity)
+%
+% filename of the lookup table
+FILENAME_LUT= fgm_ch4.drg
+%
+% flamelet initialization
+% the flame is initialized using a plane, defined by a point and a normal. On one side, the solution is initialized
+% using 'burnt' conditions and on the other side 'unburnt' conditions. The normal points in the direction of the 'burnt'
+% condition.
+% (x1,x2,x3) = point on the plane.
+% (x4,x5,x6) = normal of the plane.
+% (x7) = thickness of the reaction zone, this is the transition from unburnt to burnt conditions.
+% (x8) = Thickness of the 'burnt' zone, after this length, the conditions will be 'unburnt' again.
+FLAME_INIT= (0.004, 0.0, 0.0, 1.0, 0.0, 0.0, 0.2e-3, 1.0)
+%
 % --------------------- INVERSE DESIGN SIMULATION -----------------------------%
 %
 % Evaluate an inverse design problem using Cp (NO, YES)
@@ -991,6 +1017,9 @@ CATALYTIC_WALL= ( NONE )
 % SA Model: (inlet_marker1, NuFactor1, inlet_marker2, NuFactor2, ...)
 % SST Model: (inlet_marker1, TurbIntensity1, RatioTurbLamViscosity1, inlet_marker2, TurbIntensity2, RatioTurbLamViscosity2, ...)
 MARKER_INLET_TURBULENT= (inlet1, 0.05, 15, inlet2, 0.02, ...)
+%
+% list of markers species transport and flamelet model where strong boundary conditions should be used
+MARKER_SPECIES_STRONG_BC= (inlet, wall)
 
 % ------------------------ WALL ROUGHNESS DEFINITION --------------------------%
 % The equivalent sand grain roughness height (k_s) on each of the wall. This must be in m.

From 0a0dc9e5dc4bcf99aa1356010991fcfcc7fed476 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Arne=20Vo=C3=9F?= <arne.voss@dlr.de>
Date: Fri, 9 Jun 2023 15:36:30 +0200
Subject: [PATCH 490/656] First step in removing the unused code of the Split
 Velocity Method.

---
 SU2_CFD/include/numerics/CNumerics.hpp       | 24 +-----
 SU2_CFD/include/variables/CEulerVariable.hpp | 31 --------
 SU2_CFD/include/variables/CVariable.hpp      | 28 -------
 SU2_CFD/src/drivers/CDriver.cpp              |  3 -
 SU2_CFD/src/iteration/CFluidIteration.cpp    | 41 +---------
 SU2_CFD/src/numerics/flow/flow_sources.cpp   | 84 --------------------
 SU2_CFD/src/solvers/CEulerSolver.cpp         | 32 --------
 SU2_CFD/src/variables/CEulerVariable.cpp     |  1 -
 8 files changed, 3 insertions(+), 241 deletions(-)

diff --git a/SU2_CFD/include/numerics/CNumerics.hpp b/SU2_CFD/include/numerics/CNumerics.hpp
index e8682cc8da5..c2068ef311b 100644
--- a/SU2_CFD/include/numerics/CNumerics.hpp
+++ b/SU2_CFD/include/numerics/CNumerics.hpp
@@ -171,9 +171,7 @@ class CNumerics {
   su2double vel2_inf;     /*!< \brief value of the square of freestream speed. */
   const su2double
   *WindGust_i,  /*!< \brief Wind gust at point i. */
-  *WindGust_j,  /*!< \brief Wind gust at point j. */
-  *WindGustDer_i,  /*!< \brief Wind gust derivatives at point i. */
-  *WindGustDer_j;  /*!< \brief Wind gust derivatives at point j. */
+  *WindGust_j;  /*!< \brief Wind gust at point j. */
   const su2double *Vorticity_i, *Vorticity_j;    /*!< \brief Vorticity. */
   su2double StrainMag_i, StrainMag_j;      /*!< \brief Strain rate magnitude. */
   su2double Dissipation_i, Dissipation_j;  /*!< \brief Dissipation. */
@@ -860,26 +858,6 @@ class CNumerics {
     GridVel_j = val_gridvel_j;
   }
 
-  /*!
-   * \brief Set the wind gust value.
-   * \param[in] val_windgust_i - Wind gust of the point i.
-   * \param[in] val_windgust_j - Wind gust of the point j.
-   */
-  inline void SetWindGust(const su2double *val_windgust_i, const su2double *val_windgust_j) {
-    WindGust_i = val_windgust_i;
-    WindGust_j = val_windgust_j;
-  }
-
-  /*!
-   * \brief Set the wind gust derivatives values.
-   * \param[in] val_windgust_i - Wind gust derivatives of the point i.
-   * \param[in] val_windgust_j - Wind gust derivatives of the point j.
-   */
-  inline void SetWindGustDer(const su2double *val_windgustder_i, const su2double *val_windgustder_j) {
-    WindGustDer_i = val_windgustder_i;
-    WindGustDer_j = val_windgustder_j;
-  }
-
   /*!
    * \brief Set the value of the pressure.
    * \param[in] val_pressure_i - Value of the pressure at point i.
diff --git a/SU2_CFD/include/variables/CEulerVariable.hpp b/SU2_CFD/include/variables/CEulerVariable.hpp
index 44f07ffa0a2..43641a27199 100644
--- a/SU2_CFD/include/variables/CEulerVariable.hpp
+++ b/SU2_CFD/include/variables/CEulerVariable.hpp
@@ -72,7 +72,6 @@ class CEulerVariable : public CFlowVariable {
   MatrixType Secondary;
 
   MatrixType WindGust;      /*! < \brief Wind gust value */
-  MatrixType WindGustDer;   /*! < \brief Wind gust derivatives value */
 
  public:
   /*!
@@ -285,36 +284,6 @@ class CEulerVariable : public CFlowVariable {
     for (unsigned long iDim = 0; iDim < nDim; iDim++) Res_TruncError(iPoint,iDim+1) = 0.0;
   }
 
-  /*!
-   * \brief Get the value of the wind gust
-   * \return Value of the wind gust
-   */
-  inline su2double* GetWindGust(unsigned long iPoint) final { return WindGust[iPoint]; }
-
-  /*!
-   * \brief Set the value of the wind gust
-   * \param[in] Value of the wind gust
-   */
-  inline void SetWindGust(unsigned long iPoint, const su2double* val_WindGust) final {
-    for (unsigned long iDim = 0; iDim < nDim; iDim++)
-      WindGust(iPoint,iDim) = val_WindGust[iDim];
-  }
-
-  /*!
-   * \brief Get the value of the derivatives of the wind gust
-   * \return Value of the derivatives of the wind gust
-   */
-  inline su2double* GetWindGustDer(unsigned long iPoint) final { return WindGustDer[iPoint]; }
-
-  /*!
-   * \brief Set the value of the derivatives of the wind gust
-   * \param[in] Value of the derivatives of the wind gust
-   */
-  inline void SetWindGustDer(unsigned long iPoint, const su2double* val_WindGustDer) final {
-    for (unsigned long iDim = 0; iDim < nDim+1; iDim++)
-      WindGustDer(iPoint,iDim) = val_WindGustDer[iDim];
-  }
-
   /*!
    * \brief Specify a vector to set the velocity components of the solution. Multiplied by density for compressible cases.
    * \param[in] iPoint - Point index.
diff --git a/SU2_CFD/include/variables/CVariable.hpp b/SU2_CFD/include/variables/CVariable.hpp
index 5167ef953f6..a1c89d5a414 100644
--- a/SU2_CFD/include/variables/CVariable.hpp
+++ b/SU2_CFD/include/variables/CVariable.hpp
@@ -794,34 +794,6 @@ class CVariable {
   inline MatrixType& GetSolution_Min() { return Solution_Min; }
   inline const MatrixType& GetSolution_Min() const { return Solution_Min; }
 
-  /*!
-   * \brief Get the value of the wind gust
-   * \param[in] iPoint - Point index.
-   * \return Value of the wind gust
-   */
-  inline virtual su2double* GetWindGust(unsigned long iPoint) { return nullptr; }
-
-  /*!
-   * \brief Set the value of the wind gust
-   * \param[in] iPoint - Point index.
-   * \param[in] val_WindGust - Value of the wind gust
-   */
-  inline virtual void SetWindGust(unsigned long iPoint, const su2double* val_WindGust) {}
-
-  /*!
-   * \brief Get the value of the derivatives of the wind gust
-   * \param[in] iPoint - Point index.
-   * \return Value of the derivatives of the wind gust
-   */
-  inline virtual su2double* GetWindGustDer(unsigned long iPoint) { return nullptr;}
-
-  /*!
-   * \brief Set the value of the derivatives of the wind gust
-   * \param[in] iPoint - Point index.
-   * \param[in] val_WindGust - Value of the derivatives of the wind gust
-   */
-  inline virtual void SetWindGustDer(unsigned long iPoint, const su2double* val_WindGust) {}
-
   /*!
    * \brief Set the value of the time step.
    * \param[in] iPoint - Point index.
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index 1eee1af5e85..5b85ead935e 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -1873,9 +1873,6 @@ void CDriver::InitializeNumerics(CConfig *config, CGeometry **geometry, CSolver
       else if (config->GetGravityForce() == YES) {
         numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceGravity(nDim, nVar_Flow, config);
       }
-      else if (config->GetWind_Gust() == YES) {
-        numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceWindGust(nDim, nVar_Flow, config);
-      }
       else {
         numerics[iMGlevel][FLOW_SOL][source_first_term] = new CSourceNothing(nDim, nVar_Flow, config);
       }
diff --git a/SU2_CFD/src/iteration/CFluidIteration.cpp b/SU2_CFD/src/iteration/CFluidIteration.cpp
index da63e7812a5..a5948656b55 100644
--- a/SU2_CFD/src/iteration/CFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CFluidIteration.cpp
@@ -297,11 +297,6 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
   // described in the NASA TM–2012-217771 - Development, Verification and Use of Gust Modeling in the NASA Computational
   // Fluid Dynamics Code FUN3D the desired gust is prescribed as the negative of the grid velocity.
 
-  // If a source term is included to account for the gust field, the method is described by Jones et al. as the Split
-  // Velocity Method in Simulation of Airfoil Gust Responses Using Prescribed Velocities. In this routine the gust
-  // derivatives needed for the source term are calculated when applicable. If the gust derivatives are zero the source
-  // term is also zero. The source term itself is implemented in the class CSourceWindGust
-
   unsigned short iDim, nDim = geometry[MESH_0]->GetnDim();
 
   /*--- Gust Parameters from config ---*/
@@ -318,8 +313,8 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
   unsigned long iPoint;
   unsigned short iMGlevel, nMGlevel = config->GetnMGLevels();
 
-  su2double x, y, x_gust, dgust_dx, dgust_dy, dgust_dz, dgust_dt;
-  su2double *Gust, *GridVel, *NewGridVel, *GustDer;
+  su2double x, y, x_gust;
+  su2double *Gust, *GridVel, *NewGridVel;
 
   su2double Physical_dt = config->GetDelta_UnstTime();
   unsigned long TimeIter = config->GetTimeIter();
@@ -331,7 +326,6 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
 
   Gust       = new su2double[nDim]();
   NewGridVel = new su2double[nDim]();
-  GustDer    = new su2double[nDim+1]();
 
   // Print some information to check that we are doing the right thing. Not sure how to convert the index back to a string...
   if (rank == MASTER_NODE) {
@@ -370,10 +364,6 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
       for (iDim = 0; iDim < nDim; iDim++) {
         Gust[iDim] = 0.0;
       }
-      dgust_dx = 0.0;
-      dgust_dy = 0.0;
-      dgust_dz = 0.0;
-      dgust_dt = 0.0;
 
       /*--- Begin applying the gust ---*/
 
@@ -398,11 +388,6 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
             // Check if we are in the region where the gust is active
             if (x_gust > 0 && x_gust < n) {
               Gust[GustDir] = gust_amp * (sin(2 * PI_NUMBER * x_gust));
-
-              // Gust derivatives
-              // dgust_dx = gust_amp*2*PI_NUMBER*(cos(2*PI_NUMBER*x_gust))/L;
-              // dgust_dy = 0;
-              // dgust_dt = gust_amp*2*PI_NUMBER*(cos(2*PI_NUMBER*x_gust))*(-Uinf)/L;
             }
             break;
 
@@ -410,11 +395,6 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
             // Check if we are in the region where the gust is active
             if (x_gust > 0 && x_gust < n) {
               Gust[GustDir] = gust_amp * 0.5 * (1 - cos(2 * PI_NUMBER * x_gust));
-
-              // Gust derivatives
-              // dgust_dx = gust_amp*2*PI_NUMBER*(sin(2*PI_NUMBER*x_gust))/L;
-              // dgust_dy = 0;
-              // dgust_dt = gust_amp*2*PI_NUMBER*(sin(2*PI_NUMBER*x_gust))*(-Uinf)/L;
             }
             break;
 
@@ -449,22 +429,6 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
         }
       }
 
-      /*--- Set the Wind Gust, Wind Gust Derivatives and the Grid Velocities ---*/
-      if (nDim == 2) {
-        GustDer[0] = dgust_dx;
-        GustDer[1] = dgust_dy;
-        GustDer[2] = dgust_dt;
-      }
-      else {
-        GustDer[0] = dgust_dx;
-        GustDer[1] = dgust_dy;
-        GustDer[2] = dgust_dz;
-        GustDer[3] = dgust_dt;
-      }
-      // I think we don't need to set any source terms because they depend on the derivatives, which are zero in all cases from above.
-      solver[iMGlevel][FLOW_SOL]->GetNodes()->SetWindGust(iPoint, Gust);
-      solver[iMGlevel][FLOW_SOL]->GetNodes()->SetWindGustDer(iPoint, GustDer);
-
       GridVel = geometry[iMGlevel]->nodes->GetGridVel(iPoint);
 
       /*--- Store new grid velocity ---*/
@@ -477,7 +441,6 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
   }
 
   delete[] Gust;
-  delete[] GustDer;
   delete[] NewGridVel;
 }
 
diff --git a/SU2_CFD/src/numerics/flow/flow_sources.cpp b/SU2_CFD/src/numerics/flow/flow_sources.cpp
index cd8e8d1d4ad..64f8145cf15 100644
--- a/SU2_CFD/src/numerics/flow/flow_sources.cpp
+++ b/SU2_CFD/src/numerics/flow/flow_sources.cpp
@@ -715,90 +715,6 @@ CNumerics::ResidualType<> CSourceVorticityConfinement::ComputeResidual(const CCo
   return ResidualType<>(residual, jacobian, nullptr);
 }
 
-CSourceWindGust::CSourceWindGust(unsigned short val_nDim, unsigned short val_nVar, const CConfig* config) :
-                 CSourceBase_Flow(val_nDim, val_nVar, config) { }
-
-CNumerics::ResidualType<> CSourceWindGust::ComputeResidual(const CConfig* config) {
-
-  su2double u_gust, v_gust, du_gust_dx, du_gust_dy, du_gust_dt, dv_gust_dx, dv_gust_dy, dv_gust_dt;
-  su2double smx, smy, se, rho, u, v, p;
-  unsigned short GustDir = config->GetGust_Dir(); //Gust direction
-
-  u_gust = WindGust_i[0];
-  v_gust = WindGust_i[1];
-// w_gust = WindGust_i[2];
-
-  if (GustDir == X_DIR) {
-    du_gust_dx = WindGustDer_i[0];
-    du_gust_dy = WindGustDer_i[1];
-    //du_gust_dz = WindGustDer_i[2];
-    du_gust_dt = WindGustDer_i[2];
-
-    dv_gust_dx = 0.0;
-    dv_gust_dy = 0.0;
-    //dv_gust_dz = 0.0;
-    dv_gust_dt = 0.0;
-
-    //dw_gust_dx = 0.0;
-    //dw_gust_dy = 0.0;
-    //dw_gust_dz = 0.0;
-    //dw_gust_dt = 0.0;
-  } else {
-    du_gust_dx = 0.0;
-    du_gust_dy = 0.0;
-    //du_gust_dz = 0.0;
-    du_gust_dt = 0.0;
-    dv_gust_dx = WindGustDer_i[0];
-    dv_gust_dy = WindGustDer_i[1];
-    //dv_gust_dz = WindGustDer_i[2]
-    dv_gust_dt = WindGustDer_i[2];
-
-    //dw_gust_dx = 0.0;
-    //dw_gust_dy = 0.0;
-    //dw_gust_dz = 0.0;
-    //dw_gust_dt = 0.0;
-    //
-
-  }
-
-  /*--- Primitive variables at point i ---*/
-  u = V_i[1];
-  v = V_i[2];
-  // w = V_i[3]
-
-  p = V_i[nDim+1];
-  rho = V_i[nDim+2];
-
-  /*--- Source terms ---*/
-  smx = rho*(du_gust_dt + (u+u_gust)*du_gust_dx + (v+v_gust)*du_gust_dy);
-  smy = rho*(dv_gust_dt + (u+u_gust)*dv_gust_dx + (v+v_gust)*dv_gust_dy);
-  //smz = rho*(dw_gust_dt + (u+u_gust)*dw_gust_dx + (v+v_gust)*dw_gust_dy) + (w+w_gust)*dw_gust_dz;
-
-  se = u*smx + v*smy + p*(du_gust_dx + dv_gust_dy);
-  //se = u*smx + v*smy + w*smz + p*(du_gust_dx + dv_gust_dy + dw_gust_dz);
-
-  if (nDim == 2) {
-    residual[0] = 0.0;
-    residual[1] = smx*Volume;
-    residual[2] = smy*Volume;
-    //residual[3] = smz*Volume;
-    residual[3] = se*Volume;
-  }
-  else {
-    residual[0] = 0.0;
-    residual[1] = 0.0;
-    residual[2] = 0.0;
-    residual[3] = 0.0;
-    residual[4] = 0.0;
-  }
-
-  /*--- For now the source term Jacobian is just set to zero ---*/
-  //bool implicit = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
-
-  return ResidualType<>(residual, jacobian, nullptr);
-}
-
-
 CSourceIncStreamwise_Periodic::CSourceIncStreamwise_Periodic(unsigned short val_nDim,
                                                              unsigned short val_nVar,
                                                              CConfig        *config) :
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index 5db213329f9..a8dedcba6d7 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -2010,7 +2010,6 @@ void CEulerSolver::Source_Residual(CGeometry *geometry, CSolver **solver_contain
   const bool axisymmetric     = config->GetAxisymmetric();
   const bool gravity          = (config->GetGravityForce() == YES);
   const bool harmonic_balance = (config->GetTime_Marching() == TIME_MARCHING::HARMONIC_BALANCE);
-  const bool windgust         = config->GetWind_Gust();
   const bool body_force       = config->GetBody_Force();
   const bool vorticity_confinement = config->GetVorticityConfinement();
   const bool ideal_gas        = (config->GetKind_FluidModel() == STANDARD_AIR) ||
@@ -2180,37 +2179,6 @@ void CEulerSolver::Source_Residual(CGeometry *geometry, CSolver **solver_contain
     END_SU2_OMP_FOR
   }
 
-  if (windgust) {
-
-    /*--- Loop over all points ---*/
-    SU2_OMP_FOR_DYN(omp_chunk_size)
-    for (iPoint = 0; iPoint < nPointDomain; iPoint++) {
-
-      /*--- Load the wind gust ---*/
-      numerics->SetWindGust(nodes->GetWindGust(iPoint), nodes->GetWindGust(iPoint));
-
-      /*--- Load the wind gust derivatives ---*/
-      numerics->SetWindGustDer(nodes->GetWindGustDer(iPoint), nodes->GetWindGustDer(iPoint));
-
-      /*--- Load the primitive variables ---*/
-      numerics->SetPrimitive(nodes->GetPrimitive(iPoint), nodes->GetPrimitive(iPoint));
-
-      /*--- Load the volume of the dual mesh cell ---*/
-      numerics->SetVolume(geometry->nodes->GetVolume(iPoint));
-
-      /*--- Compute the rotating frame source residual ---*/
-      auto residual = numerics->ComputeResidual(config);
-
-      /*--- Add the source residual to the total ---*/
-      LinSysRes.AddBlock(iPoint, residual);
-
-      /*--- Add the implicit Jacobian contribution ---*/
-      if (implicit) Jacobian.AddBlock2Diag(iPoint, residual.jacobian_i);
-
-    }
-    END_SU2_OMP_FOR
-  }
-
   if (vorticity_confinement) {
 
     CNumerics* second_numerics = numerics_container[SOURCE_SECOND_TERM + omp_get_thread_num()*MAX_TERMS];
diff --git a/SU2_CFD/src/variables/CEulerVariable.cpp b/SU2_CFD/src/variables/CEulerVariable.cpp
index 4a666042c96..cf3432ebd07 100644
--- a/SU2_CFD/src/variables/CEulerVariable.cpp
+++ b/SU2_CFD/src/variables/CEulerVariable.cpp
@@ -70,7 +70,6 @@ CEulerVariable::CEulerVariable(su2double density, const su2double *velocity, su2
 
   if (config->GetWind_Gust()) {
     WindGust.resize(nPoint,nDim);
-    WindGustDer.resize(nPoint,nDim+1);
   }
 
   if (config->GetVorticityConfinement()) {

From 536def1cc939a423aa7deaf63c46fd61cef1183c Mon Sep 17 00:00:00 2001
From: rois1995 <43813346+rois1995@users.noreply.github.com>
Date: Sun, 11 Jun 2023 00:11:11 +0200
Subject: [PATCH 491/656] Corrections to SA-NEG-R and SA model (#2014)

* Added changes for HLPW5

---------

Co-authored-by: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Co-authored-by: Nijso <bigfootedrockmidget@hotmail.com>
---
 .../numerics/turbulent/turb_sources.hpp       | 22 ++++++++++---
 SU2_CFD/src/solvers/CTurbSASolver.cpp         |  2 +-
 TestCases/hybrid_regression.py                | 16 ++++-----
 TestCases/hybrid_regression_AD.py             |  2 +-
 TestCases/parallel_regression.py              | 33 ++++++++++---------
 TestCases/parallel_regression_AD.py           |  6 ++--
 TestCases/rans/naca0012/turb_NACA0012_sa.cfg  |  1 -
 TestCases/serial_regression.py                | 22 ++++++-------
 TestCases/serial_regression_AD.py             |  4 +--
 TestCases/tutorials.py                        | 16 ++++-----
 TestCases/vandv.py                            |  8 +++--
 11 files changed, 74 insertions(+), 58 deletions(-)

diff --git a/SU2_CFD/include/numerics/turbulent/turb_sources.hpp b/SU2_CFD/include/numerics/turbulent/turb_sources.hpp
index 704403746fc..00d685baa67 100644
--- a/SU2_CFD/include/numerics/turbulent/turb_sources.hpp
+++ b/SU2_CFD/include/numerics/turbulent/turb_sources.hpp
@@ -48,6 +48,8 @@ struct CSAVariables {
   const su2double cb2_sigma = cb2 / sigma;
   const su2double cw1 = cb1 / k2 + (1 + cb2) / sigma;
   const su2double cr1 = 0.5;
+  const su2double CRot = 1.0;
+  const su2double c2 = 0.7, c3 = 0.9; 
 
   /*--- List of auxiliary functions ---*/
   su2double ft2, d_ft2, r, d_r, g, d_g, glim, fw, d_fw, Ji, d_Ji, S, Shat, d_Shat, fv1, d_fv1, fv2, d_fv2;
@@ -122,7 +124,9 @@ class CSourceBase_TurbSA : public CNumerics {
 
     /*--- Dacles-Mariani et. al. rotation correction ("-R"). ---*/
     if (options.rot) {
-      var.Omega += 2.0 * min(0.0, StrainMag_i - var.Omega);
+      var.Omega += var.CRot * min(0.0, StrainMag_i - var.Omega);
+      /*--- Do not allow negative production for SA-neg. ---*/
+      if (ScalarVar_i[0] < 0) var.Omega = abs(var.Omega);
     }
 
     if (dist_i > 1e-10) {
@@ -303,9 +307,19 @@ struct ModVort {
 struct Bsl {
   static void get(const su2double& nue, const su2double& nu, CSAVariables& var) {
     const su2double Sbar = nue * var.fv2 * var.inv_k2_d2;
-    var.Shat = var.S + Sbar;
-    var.Shat = max(var.Shat, 1.0e-10);
-    if (var.Shat <= 1.0e-10) {
+    const su2double c2 = 0.7, c3 = 0.9;
+
+    /*--- Limiting of \hat{S} based on "Modifications and Clarifications for the Implementation of the Spalart-Allmaras Turbulence Model"
+     * Note 1 option c in https://turbmodels.larc.nasa.gov/spalart.html ---*/
+    if (Sbar >= - c2 * var.S) {
+      var.Shat = var.S + Sbar;
+    } else {
+      const su2double Num = var.S * (c2 * c2 * var.S + c3 * Sbar);
+      const su2double Den = (c3 - 2 * c2) * var.S - Sbar;
+      var.Shat = var.S + Num / Den;
+    }
+    if (var.Shat <= 1e-10) {
+      var.Shat = 1e-10;
       var.d_Shat = 0.0;
     } else {
       var.d_Shat = (var.fv2 + nue * var.d_fv2) * var.inv_k2_d2;
diff --git a/SU2_CFD/src/solvers/CTurbSASolver.cpp b/SU2_CFD/src/solvers/CTurbSASolver.cpp
index fb18d50b551..e1f60cebbb1 100644
--- a/SU2_CFD/src/solvers/CTurbSASolver.cpp
+++ b/SU2_CFD/src/solvers/CTurbSASolver.cpp
@@ -235,7 +235,7 @@ void CTurbSASolver::Postprocessing(CGeometry *geometry, CSolver **solver_contain
 
     su2double muT = rho*fv1*nu_hat;
 
-    if (neg_spalart_allmaras) muT = max(muT,0.0);
+    if (neg_spalart_allmaras && nu_hat < 0) muT = 0.0;
 
     nodes->SetmuT(iPoint,muT);
 
diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index a77ce5648b3..612b7669a56 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -158,7 +158,7 @@ def main():
     rae2822_sa.cfg_dir   = "rans/rae2822"
     rae2822_sa.cfg_file  = "turb_SA_RAE2822.cfg"
     rae2822_sa.test_iter = 20
-    rae2822_sa.test_vals = [-2.020123, -5.269330, 0.807147, 0.060499, -80603.000000]
+    rae2822_sa.test_vals = [-2.020123, -5.269324, 0.807147, 0.060499, -80602.000000]
     test_list.append(rae2822_sa)
 
     # RAE2822 SST
@@ -182,7 +182,7 @@ def main():
     turb_flatplate.cfg_dir   = "rans/flatplate"
     turb_flatplate.cfg_file  = "turb_SA_flatplate.cfg"
     turb_flatplate.test_iter = 20
-    turb_flatplate.test_vals = [-4.157169, -6.736698, -0.176253, 0.057446]
+    turb_flatplate.test_vals = [-4.157358, -6.736289, -0.176258, 0.057431]
     test_list.append(turb_flatplate)
 
     # ONERA M6 Wing
@@ -197,8 +197,8 @@ def main():
     turb_naca0012_sa           = TestCase('turb_naca0012_sa')
     turb_naca0012_sa.cfg_dir   = "rans/naca0012"
     turb_naca0012_sa.cfg_file  = "turb_NACA0012_sa.cfg"
-    turb_naca0012_sa.test_iter = 10
-    turb_naca0012_sa.test_vals         = [-8.627052, -10.377936, 1.064491, 0.019710, 20.000000, -1.763092, 20.000000, -4.794204, -46.506000]
+    turb_naca0012_sa.test_iter = 5
+    turb_naca0012_sa.test_vals         = [-10.451625, -13.859808, 1.057622, 0.022916, 20.000000, -1.358306, 20.000000, -2.512316, -44.540000]
     turb_naca0012_sa.test_vals_aarch64 = [-8.627052, -10.377936, 1.064491, 0.019710, 20.000000, -1.763093, 20.000000, -4.794073, -46.506000]
     test_list.append(turb_naca0012_sa)
 
@@ -242,7 +242,7 @@ def main():
     propeller.cfg_dir   = "rans/propeller"
     propeller.cfg_file  = "propeller.cfg"
     propeller.test_iter = 10
-    propeller.test_vals = [-3.389575, -8.409529, 0.000048, 0.056329]
+    propeller.test_vals = [-3.389575, -8.409251, 0.000048, 0.056329]
     test_list.append(propeller)
 
     #######################################
@@ -408,7 +408,7 @@ def main():
     inc_turb_naca0012.cfg_dir   = "incomp_rans/naca0012"
     inc_turb_naca0012.cfg_file  = "naca0012.cfg"
     inc_turb_naca0012.test_iter = 20
-    inc_turb_naca0012.test_vals = [-4.788405, -11.040493, 0.000008, 0.309506]
+    inc_turb_naca0012.test_vals = [-4.788405, -11.039465, 0.000008, 0.309490]
     test_list.append(inc_turb_naca0012)
 
     # NACA0012, SST_SUST
@@ -424,7 +424,7 @@ def main():
     inc_weakly_coupled.cfg_dir = "disc_adj_heat"
     inc_weakly_coupled.cfg_file = "primal.cfg"
     inc_weakly_coupled.test_iter = 10
-    inc_weakly_coupled.test_vals = [-17.240436, -16.184455, -16.069131, -17.230730, -18.350601, -13.768070, 5.545700]
+    inc_weakly_coupled.test_vals = [-16.498562, -15.335587, -15.570565, -12.867787, -18.185331, -13.071436, 5.545800]
     test_list.append(inc_weakly_coupled)
 
     ######################################
@@ -505,7 +505,7 @@ def main():
     ddes_flatplate.cfg_dir   = "ddes/flatplate"
     ddes_flatplate.cfg_file  = "ddes_flatplate.cfg"
     ddes_flatplate.test_iter = 10
-    ddes_flatplate.test_vals = [-2.714758, -5.882733, -0.215005, 0.023783, -618.160000]
+    ddes_flatplate.test_vals = [-2.714757, -5.882779, -0.215005, 0.023783, -618.130000]
     ddes_flatplate.unsteady  = True
     test_list.append(ddes_flatplate)
 
diff --git a/TestCases/hybrid_regression_AD.py b/TestCases/hybrid_regression_AD.py
index 2cb40a0d31d..438b2fa731f 100644
--- a/TestCases/hybrid_regression_AD.py
+++ b/TestCases/hybrid_regression_AD.py
@@ -75,7 +75,7 @@ def main():
     discadj_rans_naca0012_sa.cfg_dir   = "disc_adj_rans/naca0012"
     discadj_rans_naca0012_sa.cfg_file  = "turb_NACA0012_sa.cfg"
     discadj_rans_naca0012_sa.test_iter = 10
-    discadj_rans_naca0012_sa.test_vals         = [-2.230631, 0.644953, 0.177890, -0.000016, 5.000000, -3.007652, 5.000000, -7.631910]
+    discadj_rans_naca0012_sa.test_vals         = [-2.230621, 0.644162, 0.177890, -0.000016, 5.000000, -3.007652, 5.000000, -7.728093]
     discadj_rans_naca0012_sa.test_vals_aarch64 = [-2.230631, 0.644954, 0.177890, -0.000016, 5.000000, -3.007651, 5.000000, -7.631909]
     test_list.append(discadj_rans_naca0012_sa)
 
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 50dd5b013ce..35f1f890050 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -336,7 +336,7 @@ def main():
     rae2822_sa.cfg_dir   = "rans/rae2822"
     rae2822_sa.cfg_file  = "turb_SA_RAE2822.cfg"
     rae2822_sa.test_iter = 20
-    rae2822_sa.test_vals = [-2.004689, -5.265793, 0.809463, 0.062016, -80577.000000]
+    rae2822_sa.test_vals = [-2.004689, -5.265782, 0.809463, 0.062016, -80576.000000]
     test_list.append(rae2822_sa)
 
     # RAE2822 SST
@@ -360,7 +360,7 @@ def main():
     turb_flatplate.cfg_dir   = "rans/flatplate"
     turb_flatplate.cfg_file  = "turb_SA_flatplate.cfg"
     turb_flatplate.test_iter = 20
-    turb_flatplate.test_vals = [-4.147548, -6.728790, -0.176227, 0.057731]
+    turb_flatplate.test_vals = [-4.147727, -6.728308, -0.176232, 0.057717]
     test_list.append(turb_flatplate)
 
     # Flat plate (compressible) with species inlet
@@ -368,7 +368,7 @@ def main():
     turb_flatplate_species.cfg_dir   = "rans/flatplate"
     turb_flatplate_species.cfg_file  = "turb_SA_flatplate_species.cfg"
     turb_flatplate_species.test_iter = 20
-    turb_flatplate_species.test_vals = [-4.147548, -0.634735, -1.770801, 1.335176, -3.250308, 9, -6.700992, 5, -6.999234, 10, -6.033847, 0.996033, 0.996033]
+    turb_flatplate_species.test_vals = [-4.147727, -0.634899, -1.770894, 1.334987, -3.250340, 9.000000, -6.700853, 5.000000, -6.991055, 10.000000, -6.033829, 0.996033, 0.996033]
     test_list.append(turb_flatplate_species)
 
     # ONERA M6 Wing
@@ -376,7 +376,7 @@ def main():
     turb_oneram6.cfg_dir   = "rans/oneram6"
     turb_oneram6.cfg_file  = "turb_ONERAM6.cfg"
     turb_oneram6.test_iter = 10
-    turb_oneram6.test_vals = [-2.388839, -6.689413, 0.230321, 0.157640, -32539.000000]
+    turb_oneram6.test_vals = [-2.388839, -6.689426, 0.230321, 0.157640, -32539.000000]
     turb_oneram6.timeout   = 3200
     test_list.append(turb_oneram6)
 
@@ -385,7 +385,7 @@ def main():
     turb_oneram6_vc.cfg_dir = "rans/oneram6"
     turb_oneram6_vc.cfg_file = "turb_ONERAM6_vc.cfg"
     turb_oneram6_vc.test_iter = 15
-    turb_oneram6_vc.test_vals = [-2.262387, -6.626467, 0.228393, 0.140799, -2.7107e+04]
+    turb_oneram6_vc.test_vals = [-2.262387, -6.626454, 0.228392, 0.140799, -27107.000000]
     turb_oneram6_vc.timeout = 3200
     test_list.append(turb_oneram6_vc)
 
@@ -403,8 +403,8 @@ def main():
     turb_naca0012_sa           = TestCase('turb_naca0012_sa')
     turb_naca0012_sa.cfg_dir   = "rans/naca0012"
     turb_naca0012_sa.cfg_file  = "turb_NACA0012_sa.cfg"
-    turb_naca0012_sa.test_iter = 10
-    turb_naca0012_sa.test_vals = [-8.621456, -10.378269, 1.064502, 0.019710, 20.000000, -1.811700, 20.000000, -5.171326, -46.506000]
+    turb_naca0012_sa.test_iter = 5
+    turb_naca0012_sa.test_vals = [-10.453509, -13.866376, 1.057622, 0.022916, 20.000000, -1.867547, 20.000000, -3.632893, -44.540000]
     turb_naca0012_sa.timeout   = 3200
     test_list.append(turb_naca0012_sa)
 
@@ -468,7 +468,7 @@ def main():
     propeller.cfg_dir   = "rans/propeller"
     propeller.cfg_file  = "propeller.cfg"
     propeller.test_iter = 10
-    propeller.test_vals = [-3.389575, -8.409529, 0.000048, 0.056329] #last 4 columns
+    propeller.test_vals = [-3.389575, -8.409251, 0.000048, 0.056329]
     propeller.timeout   = 3200
     test_list.append(propeller)
 
@@ -581,7 +581,7 @@ def main():
     inc_turb_naca0012.cfg_dir   = "incomp_rans/naca0012"
     inc_turb_naca0012.cfg_file  = "naca0012.cfg"
     inc_turb_naca0012.test_iter = 20
-    inc_turb_naca0012.test_vals = [-4.788595, -11.040557, -0.000002, 0.309519]
+    inc_turb_naca0012.test_vals = [-4.788596, -11.039529, -0.000002, 0.309504]
     test_list.append(inc_turb_naca0012)
 
     # NACA0012, SST_SUST
@@ -667,7 +667,7 @@ def main():
     turbmod_sa_bsl_rae2822.cfg_dir   = "turbulence_models/sa/rae2822"
     turbmod_sa_bsl_rae2822.cfg_file  = "turb_SA_BSL_RAE2822.cfg"
     turbmod_sa_bsl_rae2822.test_iter = 20
-    turbmod_sa_bsl_rae2822.test_vals = [-2.004689, 0.742306, 0.497308, -5.265793, 0.809463, 0.062016]
+    turbmod_sa_bsl_rae2822.test_vals = [-2.004689, 0.742306, 0.497308, -5.265782, 0.809463, 0.062016]
     test_list.append(turbmod_sa_bsl_rae2822)
 
     # SA Negative
@@ -675,7 +675,7 @@ def main():
     turbmod_sa_neg_rae2822.cfg_dir   = "turbulence_models/sa/rae2822"
     turbmod_sa_neg_rae2822.cfg_file  = "turb_SA_NEG_RAE2822.cfg"
     turbmod_sa_neg_rae2822.test_iter = 10
-    turbmod_sa_neg_rae2822.test_vals         = [-1.374695, 1.976506, 1.898195, 4.831133, 1.187310, 0.426019, -86764]
+    turbmod_sa_neg_rae2822.test_vals         = [-1.466238, 3.169232, 2.756518, 4.722767, 1.120253, 0.378675, -83444.000000]
     turbmod_sa_neg_rae2822.test_vals_aarch64 = [-1.347530, 1.439078, 1.306846, -1.928774, 1.480543, 0.571601, -91503]
     test_list.append(turbmod_sa_neg_rae2822)
 
@@ -684,7 +684,7 @@ def main():
     turbmod_sa_comp_rae2822.cfg_dir   = "turbulence_models/sa/rae2822"
     turbmod_sa_comp_rae2822.cfg_file  = "turb_SA_COMP_RAE2822.cfg"
     turbmod_sa_comp_rae2822.test_iter = 20
-    turbmod_sa_comp_rae2822.test_vals = [-2.004687, 0.742304, 0.497309, -5.266081, 0.809467, 0.062029]
+    turbmod_sa_comp_rae2822.test_vals = [-2.004687, 0.742304, 0.497309, -5.266067, 0.809467, 0.062029]
     test_list.append(turbmod_sa_comp_rae2822)
 
     # SA Edwards
@@ -708,7 +708,7 @@ def main():
     turbmod_sa_qcr_rae2822.cfg_dir   = "turbulence_models/sa/rae2822"
     turbmod_sa_qcr_rae2822.cfg_file  = "turb_SA_QCR_RAE2822.cfg"
     turbmod_sa_qcr_rae2822.test_iter = 20
-    turbmod_sa_qcr_rae2822.test_vals = [-2.004793, 0.742353, 0.497315, -5.265974, 0.807841, 0.062027]
+    turbmod_sa_qcr_rae2822.test_vals = [-2.004793, 0.742353, 0.497315, -5.265962, 0.807841, 0.062027]
     test_list.append(turbmod_sa_qcr_rae2822)
 
     ############################
@@ -880,7 +880,8 @@ def main():
     hb_rans_preconditioning.cfg_dir   = "harmonic_balance/hb_rans_preconditioning"
     hb_rans_preconditioning.cfg_file  = "davis.cfg"
     hb_rans_preconditioning.test_iter = 25
-    hb_rans_preconditioning.test_vals = [-1.902097, 0.484069, 0.601483, 3.609005, -5.949274]
+    hb_rans_preconditioning.tol       = 0.00001
+    hb_rans_preconditioning.test_vals = [-1.902098, 0.484070, 0.601481, 3.609002, -5.949360]
     test_list.append(hb_rans_preconditioning)
 
     ######################################
@@ -947,7 +948,7 @@ def main():
     ddes_flatplate.cfg_dir   = "ddes/flatplate"
     ddes_flatplate.cfg_file  = "ddes_flatplate.cfg"
     ddes_flatplate.test_iter = 10
-    ddes_flatplate.test_vals = [-2.714758, -5.882733, -0.215005, 0.023783, -618.160000]
+    ddes_flatplate.test_vals = [-2.714757, -5.882779, -0.215005, 0.023783, -618.130000]
     ddes_flatplate.unsteady  = True
     test_list.append(ddes_flatplate)
 
@@ -1436,7 +1437,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_viscosity.cfg_dir   = "species_transport/venturi_primitive_3species"
     species2_primitiveVenturi_mixingmodel_viscosity.cfg_file  = "species2_primitiveVenturi_mixingmodel_viscosity.cfg"
     species2_primitiveVenturi_mixingmodel_viscosity.test_iter = 50
-    species2_primitiveVenturi_mixingmodel_viscosity.test_vals = [-4.843487, -3.585775, -3.486490, -7.560246, -5.094190, 5.000000, -1.898139, 5.000000, -3.329399, 5.000000, -2.113219, 2.482224, 0.974144, 0.607217, 0.900862]
+    species2_primitiveVenturi_mixingmodel_viscosity.test_vals = [-4.843481, -3.585988, -3.486593, -7.560545, -5.094245, 5.000000, -1.898097, 5.000000, -3.328995, 5.000000, -2.113241, 2.482221, 0.974142, 0.607219, 0.900860]
     test_list.append(species2_primitiveVenturi_mixingmodel_viscosity)
 
     # 2 species (1 eq) primitive venturi mixing using mixing model including heat capacity and mass diffusivity
diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index d7415431119..2e0d70f516a 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -83,7 +83,7 @@ def main():
     discadj_rans_naca0012_sa.cfg_dir   = "disc_adj_rans/naca0012"
     discadj_rans_naca0012_sa.cfg_file  = "turb_NACA0012_sa.cfg"
     discadj_rans_naca0012_sa.test_iter = 10
-    discadj_rans_naca0012_sa.test_vals = [-2.230578, 0.645001, 0.181590, -0.000018, 5.000000, -3.421214, 5.000000, -6.769609]
+    discadj_rans_naca0012_sa.test_vals = [-2.230568, 0.644202, 0.181590, -0.000018, 5.000000, -3.421717, 5.000000, -6.769530]
     test_list.append(discadj_rans_naca0012_sa)
 
     # Adjoint turbulent NACA0012 SST
@@ -255,8 +255,8 @@ def main():
     discadj_heat.cfg_dir   = "disc_adj_heat"
     discadj_heat.cfg_file  = "disc_adj_heat.cfg"
     discadj_heat.test_iter = 10
-    discadj_heat.test_vals         = [-2.226525, 0.603989, 0.000000, -6.256200]
-    discadj_heat.test_vals_aarch64 = [-2.226525, 0.603989, 0.000000, -6.256200]
+    discadj_heat.test_vals         = [-2.226539, 0.605868, 0.000000, -6.256400]
+    discadj_heat.test_vals_aarch64 = [-2.226539, 0.605868, 0.000000, -6.256400]
     test_list.append(discadj_heat)
 
     ###################################
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sa.cfg b/TestCases/rans/naca0012/turb_NACA0012_sa.cfg
index aceafbc305c..c80150a03b6 100644
--- a/TestCases/rans/naca0012/turb_NACA0012_sa.cfg
+++ b/TestCases/rans/naca0012/turb_NACA0012_sa.cfg
@@ -67,7 +67,6 @@ LINEAR_SOLVER_ITER= 20
 %
 CONV_NUM_METHOD_FLOW= ROE
 MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= NONE
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
diff --git a/TestCases/serial_regression.py b/TestCases/serial_regression.py
index b7d00c3f3a0..a17d5737b52 100644
--- a/TestCases/serial_regression.py
+++ b/TestCases/serial_regression.py
@@ -213,7 +213,7 @@ def main():
     rae2822_sa.cfg_dir   = "rans/rae2822"
     rae2822_sa.cfg_file  = "turb_SA_RAE2822.cfg"
     rae2822_sa.test_iter = 20
-    rae2822_sa.test_vals = [-2.020123, -5.269330, 0.807147, 0.060499, -80603.000000]
+    rae2822_sa.test_vals = [-2.020123, -5.269324, 0.807147, 0.060499, -80602.000000]
     test_list.append(rae2822_sa)
 
     # RAE2822 SST
@@ -237,7 +237,7 @@ def main():
     turb_flatplate.cfg_dir   = "rans/flatplate"
     turb_flatplate.cfg_file  = "turb_SA_flatplate.cfg"
     turb_flatplate.test_iter = 20
-    turb_flatplate.test_vals = [-4.157169, -6.736698, -0.176253, 0.057446] #last 4 columns
+    turb_flatplate.test_vals = [-4.157358, -6.736289, -0.176258, 0.057431]
     test_list.append(turb_flatplate)
 
     # FLAT PLATE, WALL FUNCTIONS, COMPRESSIBLE SST
@@ -253,7 +253,7 @@ def main():
     turb_wallfunction_flatplate_sa.cfg_dir   = "wallfunctions/flatplate/compressible_SA"
     turb_wallfunction_flatplate_sa.cfg_file  = "turb_SA_flatplate.cfg"
     turb_wallfunction_flatplate_sa.test_iter = 10
-    turb_wallfunction_flatplate_sa.test_vals = [-4.436048, -2.044706, -2.114644, 0.979771, -5.393729, 10, -1.589465, 0.069744, 0.002686] #last 9 columns
+    turb_wallfunction_flatplate_sa.test_vals = [-4.435719, -2.044696, -2.114266, 0.980115, -5.393813, 10.000000, -1.589802, 0.069744, 0.002686]
     test_list.append(turb_wallfunction_flatplate_sa)
 
     # ONERA M6 Wing
@@ -261,7 +261,7 @@ def main():
     turb_oneram6.cfg_dir   = "rans/oneram6"
     turb_oneram6.cfg_file  = "turb_ONERAM6.cfg"
     turb_oneram6.test_iter = 10
-    turb_oneram6.test_vals = [-2.388841, -6.689414, 0.230321, 0.157640, -32539.000000]
+    turb_oneram6.test_vals = [-2.388841, -6.689427, 0.230321, 0.157640, -32539.000000]
     turb_oneram6.timeout   = 3200
     test_list.append(turb_oneram6)
 
@@ -269,8 +269,8 @@ def main():
     turb_naca0012_sa           = TestCase('turb_naca0012_sa')
     turb_naca0012_sa.cfg_dir   = "rans/naca0012"
     turb_naca0012_sa.cfg_file  = "turb_NACA0012_sa.cfg"
-    turb_naca0012_sa.test_iter = 10
-    turb_naca0012_sa.test_vals = [-8.629583, -10.377793, 1.064488, 0.019711, 20.000000, -2.173971, 20.000000, -5.213344, -46.50600]
+    turb_naca0012_sa.test_iter = 5
+    turb_naca0012_sa.test_vals = [-10.451742, -13.864841, 1.057622, 0.022916, 20.000000, -1.588482, 20.000000, -2.963093, -44.540000]
     turb_naca0012_sa.timeout   = 3200
     test_list.append(turb_naca0012_sa)
 
@@ -316,7 +316,7 @@ def main():
     propeller.cfg_dir   = "rans/propeller"
     propeller.cfg_file  = "propeller.cfg"
     propeller.test_iter = 10
-    propeller.test_vals = [-3.389575, -8.409529, 0.000048, 0.056329] #last 4 columns
+    propeller.test_vals = [-3.389575, -8.409251, 0.000048, 0.056329]
     propeller.timeout   = 3200
     test_list.append(propeller)
 
@@ -434,7 +434,7 @@ def main():
     inc_turb_naca0012.cfg_dir   = "incomp_rans/naca0012"
     inc_turb_naca0012.cfg_file  = "naca0012.cfg"
     inc_turb_naca0012.test_iter = 20
-    inc_turb_naca0012.test_vals = [-4.788495, -11.040511, 0.000023, 0.309503] #last 4 columns
+    inc_turb_naca0012.test_vals = [-4.788496, -11.039482, 0.000023, 0.309488]
     test_list.append(inc_turb_naca0012)
 
     # NACA0012, SST_SUST
@@ -726,7 +726,7 @@ def main():
     hb_rans_preconditioning.cfg_dir   = "harmonic_balance/hb_rans_preconditioning"
     hb_rans_preconditioning.cfg_file  = "davis.cfg"
     hb_rans_preconditioning.test_iter = 25
-    hb_rans_preconditioning.test_vals = [-1.902097, 0.484069, 0.601483, 3.609005, -5.949274]
+    hb_rans_preconditioning.test_vals = [-1.902097, 0.484069, 0.601483, 3.609005, -5.949359]
     test_list.append(hb_rans_preconditioning)
 
     ######################################
@@ -793,7 +793,7 @@ def main():
     ddes_flatplate.cfg_dir   = "ddes/flatplate"
     ddes_flatplate.cfg_file  = "ddes_flatplate.cfg"
     ddes_flatplate.test_iter = 10
-    ddes_flatplate.test_vals = [-2.714758, -5.882733, -0.215005, 0.023783, -618.160000]
+    ddes_flatplate.test_vals = [-2.714757, -5.882779, -0.215005, 0.023783, -618.130000]
     ddes_flatplate.unsteady  = True
     test_list.append(ddes_flatplate)
 
@@ -802,7 +802,7 @@ def main():
     unst_inc_turb_naca0015_sa.cfg_dir   = "unsteady/pitching_naca0015_rans_inc"
     unst_inc_turb_naca0015_sa.cfg_file  = "config_incomp_turb_sa.cfg"
     unst_inc_turb_naca0015_sa.test_iter = 1
-    unst_inc_turb_naca0015_sa.test_vals = [-3.007635, -6.879789, 1.445300, 0.419281] #last 4 columns
+    unst_inc_turb_naca0015_sa.test_vals = [-3.007635, -6.879778, 1.445293, 0.419274]
     unst_inc_turb_naca0015_sa.unsteady  = True
     test_list.append(unst_inc_turb_naca0015_sa)
 
diff --git a/TestCases/serial_regression_AD.py b/TestCases/serial_regression_AD.py
index d9885b1dcd1..c4e7157149e 100644
--- a/TestCases/serial_regression_AD.py
+++ b/TestCases/serial_regression_AD.py
@@ -75,7 +75,7 @@ def main():
     discadj_rans_naca0012_sa.cfg_dir   = "disc_adj_rans/naca0012"
     discadj_rans_naca0012_sa.cfg_file  = "turb_NACA0012_sa.cfg"
     discadj_rans_naca0012_sa.test_iter = 10
-    discadj_rans_naca0012_sa.test_vals = [-2.230555, 0.645023, 0.180740, -0.000018, 5.000000, -4.275184, 5.000000, -8.892454] #last 8 columns
+    discadj_rans_naca0012_sa.test_vals = [-2.230545, 0.644224, 0.180740, -0.000018, 5.000000, -4.275182, 5.000000, -10.051224]
     test_list.append(discadj_rans_naca0012_sa)
 
     # Adjoint turbulent NACA0012 SST
@@ -200,7 +200,7 @@ def main():
     discadj_heat.cfg_dir   = "disc_adj_heat"
     discadj_heat.cfg_file  = "disc_adj_heat.cfg"
     discadj_heat.test_iter = 10
-    discadj_heat.test_vals = [-2.227518, 0.576043, 0.000000, -7.753900] #last 4 columns
+    discadj_heat.test_vals = [-2.227530, 0.577932, 0.000000, -7.754000]
     test_list.append(discadj_heat)
 
     ###################################
diff --git a/TestCases/tutorials.py b/TestCases/tutorials.py
index b2bb04b6e88..621a7ffc9c8 100644
--- a/TestCases/tutorials.py
+++ b/TestCases/tutorials.py
@@ -98,7 +98,7 @@ def main():
     DAspecies3_primitiveVenturi.cfg_file  = "DAspecies3_primitiveVenturi.cfg"
     DAspecies3_primitiveVenturi.test_iter = 50
     DAspecies3_primitiveVenturi.test_vals         = [-8.422882, -7.699257, -7.683269, -7.411648, -12.064694, -12.205189, -11.368995]
-    DAspecies3_primitiveVenturi.test_vals_aarch64 = [-8.422882, -7.699257, -7.683269, -7.411648, -12.064694, -12.205189, -11.368995]
+    DAspecies3_primitiveVenturi.test_vals_aarch64 = [-8.528843, -7.799649, -7.783477, -7.482502, -12.140092, -12.250169, -11.455523]
     DAspecies3_primitiveVenturi.command   = TestCase.Command("mpirun -n 2", "SU2_CFD_AD")
     test_list.append(DAspecies3_primitiveVenturi)
 
@@ -171,7 +171,7 @@ def main():
     tutorial_turb_flatplate.cfg_dir    = "../Tutorials/compressible_flow/Turbulent_Flat_Plate"
     tutorial_turb_flatplate.cfg_file   = "turb_SA_flatplate.cfg"
     tutorial_turb_flatplate.test_iter  = 0
-    tutorial_turb_flatplate.test_vals  = [-2.258584, -4.899502, -0.429375, 0.201236]
+    tutorial_turb_flatplate.test_vals  = [-2.258584, -4.901015, -0.429375, 0.201236]
     tutorial_turb_flatplate.no_restart = True
     test_list.append(tutorial_turb_flatplate)
 
@@ -207,7 +207,7 @@ def main():
     tutorial_trans_e387_sa.cfg_dir    = "../Tutorials/compressible_flow/Transitional_Airfoil/Langtry_and_Menter/E387"
     tutorial_trans_e387_sa.cfg_file   = "transitional_SA_LM_model_ConfigFile.cfg"
     tutorial_trans_e387_sa.test_iter  = 20
-    tutorial_trans_e387_sa.test_vals  = [-6.527027, -5.081543, -0.795267, 1.022557, 0.150240, 2, -9.580670]
+    tutorial_trans_e387_sa.test_vals  = [-6.527027, -5.081560, -0.795267, 1.022556, 0.150189, 2.000000, -9.580669]
     tutorial_trans_e387_sa.no_restart = True
     test_list.append(tutorial_trans_e387_sa)
 
@@ -216,7 +216,7 @@ def main():
     tutorial_trans_e387_sst.cfg_dir    = "../Tutorials/compressible_flow/Transitional_Airfoil/Langtry_and_Menter/E387"
     tutorial_trans_e387_sst.cfg_file   = "transitional_SST_LM_model_ConfigFile.cfg"
     tutorial_trans_e387_sst.test_iter  = 20
-    tutorial_trans_e387_sst.test_vals  = [-6.532421, -5.085785, -0.789723, 1.078391, 0.188263, 2, -9.567014]
+    tutorial_trans_e387_sst.test_vals  = [-6.532421, -5.085785, -0.789723, 1.078391, 0.188263, 2.000000, -9.567014]
     tutorial_trans_e387_sst.no_restart = True
     test_list.append(tutorial_trans_e387_sst)
 
@@ -225,7 +225,7 @@ def main():
     tutorial_turb_oneram6.cfg_dir    = "../Tutorials/compressible_flow/Turbulent_ONERAM6"
     tutorial_turb_oneram6.cfg_file   = "turb_ONERAM6.cfg"
     tutorial_turb_oneram6.test_iter  = 0
-    tutorial_turb_oneram6.test_vals  = [-4.564441, -11.524277, 0.327954, 0.097349]
+    tutorial_turb_oneram6.test_vals  = [-4.564441, -11.524476, 0.327954, 0.097349]
     test_list.append(tutorial_turb_oneram6)
 
     # NICD Nozzle
@@ -242,7 +242,7 @@ def main():
     tutorial_unst_naca0012.cfg_dir       = "../Tutorials/compressible_flow/Unsteady_NACA0012"
     tutorial_unst_naca0012.cfg_file      = "unsteady_naca0012.cfg"
     tutorial_unst_naca0012.test_iter     = 520
-    tutorial_unst_naca0012.test_vals         = [520, 0, -5.297585, 0, 0.297416, 0.770060, 0.003308, 0.014647]
+    tutorial_unst_naca0012.test_vals         = [520.000000, 0.000000, -5.291711, 0.000000, 0.305248, 0.810326, 0.001814, 0.006573]
     tutorial_unst_naca0012.test_vals_aarch64 = [520, 0, -5.296968, 0, 0.312131, 0.801193, 0.002868, 0.014303]
     tutorial_unst_naca0012.unsteady      = True
     test_list.append(tutorial_unst_naca0012)
@@ -252,7 +252,7 @@ def main():
     propeller_var_load.cfg_dir   = "../Tutorials/compressible_flow/ActuatorDisk_VariableLoad"
     propeller_var_load.cfg_file  = "propeller_variable_load.cfg"
     propeller_var_load.test_iter = 20
-    propeller_var_load.test_vals = [-1.830252, -4.535038, -0.000323, 0.171648]
+    propeller_var_load.test_vals = [-1.830276, -4.535127, -0.000323, 0.171623]
     propeller_var_load.timeout   = 3200
     test_list.append(propeller_var_load)
 
@@ -272,7 +272,7 @@ def main():
     tutorial_design_turb_rae2822.cfg_dir    = "../Tutorials/design/Turbulent_2D_Constrained_RAE2822"
     tutorial_design_turb_rae2822.cfg_file   = "turb_SA_RAE2822.cfg"
     tutorial_design_turb_rae2822.test_iter  = 0
-    tutorial_design_turb_rae2822.test_vals  = [-1.700114, -4.941305, 0.218348, 0.190357]
+    tutorial_design_turb_rae2822.test_vals  = [-1.700114, -4.941834, 0.218348, 0.190357]
     tutorial_design_turb_rae2822.no_restart = True
     test_list.append(tutorial_design_turb_rae2822)
 
diff --git a/TestCases/vandv.py b/TestCases/vandv.py
index 15056dd64e3..a1cad128cdf 100644
--- a/TestCases/vandv.py
+++ b/TestCases/vandv.py
@@ -45,7 +45,7 @@ def main():
     p30n30.cfg_dir   = "vandv/rans/30p30n"
     p30n30.cfg_file  = "config.cfg"
     p30n30.test_iter = 20
-    p30n30.test_vals         = [-10.639125, -10.302345, -10.493880, -10.249452, -13.517221, 0.050962, 2.828563, 1.317849, -0.217586]
+    p30n30.test_vals         = [-10.806343, -10.326374, -10.559106, -10.432754, -13.517105, 0.050962, 2.828563, 1.317849, -0.228843]
     p30n30.test_vals_aarch64 = [-10.636663, -10.298256, -10.479415, -10.246700, -13.517161, 0.050962, 2.828563, 1.317849, -0.209200]
     test_list.append(p30n30)
 
@@ -71,10 +71,12 @@ def main():
     swbli_sa           = TestCase('swbli_sa')
     swbli_sa.cfg_dir   = "vandv/rans/swbli"
     swbli_sa.cfg_file  = "config_sa.cfg"
-    swbli_sa.test_iter = 20
-    swbli_sa.test_vals         = [-11.029255, -10.511982, -11.400926, -10.128471, -14.536798, 0.002233, -2.608466, 2.786]
+    swbli_sa.test_iter = 5
+    swbli_sa.test_vals         = [-11.530796, -10.915564, -12.034495, -10.538719, -15.922522, 0.002233, -3.359164, 1.340100]
+    swbli_sa.test_vals_aarch64 = [-11.014738, -9.936534, -11.120020, -10.050397, -13.203736, 0.002233, -3.222675, 1.340100]
     test_list.append(swbli_sa)
 
+
     # SWBLI - sst-v2003m
     swbli_sst           = TestCase('swbli_sst')
     swbli_sst.cfg_dir   = "vandv/rans/swbli"

From 33ba4183870633562beda47a950514a88540a475 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Sun, 11 Jun 2023 22:12:02 +0100
Subject: [PATCH 492/656] Apply suggestions from code review

---
 SU2_CFD/src/iteration/CFluidIteration.cpp | 10 ++--------
 1 file changed, 2 insertions(+), 8 deletions(-)

diff --git a/SU2_CFD/src/iteration/CFluidIteration.cpp b/SU2_CFD/src/iteration/CFluidIteration.cpp
index a5948656b55..cde93a085bb 100644
--- a/SU2_CFD/src/iteration/CFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CFluidIteration.cpp
@@ -313,8 +313,8 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
   unsigned long iPoint;
   unsigned short iMGlevel, nMGlevel = config->GetnMGLevels();
 
-  su2double x, y, x_gust;
-  su2double *Gust, *GridVel, *NewGridVel;
+  su2double x, y, x_gust, Gust[3] = {0.0}, NewGridVel[3] = {0.0};
+  const su2double* GridVel = nullptr;
 
   su2double Physical_dt = config->GetDelta_UnstTime();
   unsigned long TimeIter = config->GetTimeIter();
@@ -324,9 +324,6 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
 
   su2double Uinf = solver[MESH_0][FLOW_SOL]->GetVelocity_Inf(0);  // Assumption gust moves at infinity velocity
 
-  Gust       = new su2double[nDim]();
-  NewGridVel = new su2double[nDim]();
-
   // Print some information to check that we are doing the right thing. Not sure how to convert the index back to a string...
   if (rank == MASTER_NODE) {
 	  cout << endl << "Setting up a wind gust type " << Gust_Type << " with amplitude of " << gust_amp << " in direction " << GustDir << endl;
@@ -439,9 +436,6 @@ void CFluidIteration::SetWind_GustField(CConfig* config, CGeometry** geometry, C
       }
     }
   }
-
-  delete[] Gust;
-  delete[] NewGridVel;
 }
 
 void CFluidIteration::InitializeVortexDistribution(unsigned long& nVortex, vector<su2double>& x0, vector<su2double>& y0,

From c2b7d29a4f66de8403c63434f5c822a563b66b9b Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 13 Jun 2023 16:10:59 +0200
Subject: [PATCH 493/656] Pulled develop and updated submodules

---
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp | 2 --
 1 file changed, 2 deletions(-)

diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index b3827116ac0..9e79ab69a0e 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -207,8 +207,6 @@ unsigned long CDataDrivenFluid::Predict_MLP(su2double rho, su2double e) {
   MLP_inputs[idx_e] = e;
   exit_code = lookup_mlp->PredictANN(iomap_rhoe, MLP_inputs, outputs_rhoe);
 #endif
-  dsdrho_e = -exp(dsdrho_e);
-  d2sdrho2 = exp(d2sdrho2);
   return exit_code;
 }
 

From b4320bc940893fe26cd16061a306a3b91339095d Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 13 Jun 2023 16:47:19 +0200
Subject: [PATCH 494/656] Fixed build error

---
 meson_scripts/init.py | 2 +-
 subprojects/MLPCpp    | 2 +-
 2 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 4cc430a8516..616afd31a21 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -71,7 +71,7 @@ def init_submodules(
     github_repo_coolprop = "https://github.com/CoolProp/CoolProp"
     sha_version_mel = "2484cd3258ef800a10e361016cb341834ee7930b"
     github_repo_mel = "https://github.com/pcarruscag/MEL"
-    sha_version_mlpcpp = "d9f49565e9f4241156c4ef5c2926157439845665"
+    sha_version_mlpcpp = "596ed4c69c284304d8eb59e4f103ffab8afbfb1b"
     github_repo_mlpcpp = "https://github.com/EvertBunschoten/MLPCpp"
 
     medi_name = "MeDiPack"
diff --git a/subprojects/MLPCpp b/subprojects/MLPCpp
index d9f49565e9f..596ed4c69c2 160000
--- a/subprojects/MLPCpp
+++ b/subprojects/MLPCpp
@@ -1 +1 @@
-Subproject commit d9f49565e9f4241156c4ef5c2926157439845665
+Subproject commit 596ed4c69c284304d8eb59e4f103ffab8afbfb1b

From ddc918e27f94a476f4acc80dc4c8416f49dbbf51 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 19 Jun 2023 17:14:59 +0200
Subject: [PATCH 495/656] Implemented flexible look-up function for flamelet
 fluid model

---
 Common/include/containers/CLookUpTable.hpp    |   6 +-
 Common/include/containers/CTrapezoidalMap.hpp |  10 +-
 Common/include/option_structure.hpp           |   7 +
 Common/src/CConfig.cpp                        |   4 +-
 Common/src/containers/CLookUpTable.cpp        |  18 +-
 Common/src/containers/CTrapezoidalMap.cpp     |  10 +-
 SU2_CFD/include/fluid/CFluidFlamelet.hpp      |  65 +++--
 SU2_CFD/include/fluid/CFluidModel.hpp         |  13 +-
 .../solvers/CSpeciesFlameletSolver.hpp        |  43 +++-
 SU2_CFD/src/fluid/CFluidFlamelet.cpp          | 137 ++++++-----
 SU2_CFD/src/output/CFlowOutput.cpp            |  44 +++-
 SU2_CFD/src/solvers/CIncEulerSolver.cpp       |   5 +-
 .../src/solvers/CSpeciesFlameletSolver.cpp    | 231 ++++++++++--------
 .../lam_partial_premixed_ch4_cfd.cfg          | 138 +++++++++++
 TestCases/flamelet/README.md                  |   1 +
 15 files changed, 510 insertions(+), 222 deletions(-)
 create mode 100644 TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_premixed_ch4_cfd.cfg

diff --git a/Common/include/containers/CLookUpTable.hpp b/Common/include/containers/CLookUpTable.hpp
index 0effac26d4d..be60704ebfa 100644
--- a/Common/include/containers/CLookUpTable.hpp
+++ b/Common/include/containers/CLookUpTable.hpp
@@ -76,6 +76,8 @@ class CLookUpTable {
    */
   su2vector<su2activematrix> table_data;
 
+  double memory_footprint_data = 0; /*!< \brief Memory footprint of the loaded table data. */
+
   /*! \brief
    * Holds all connectivity data stored in the table for each level. First index
    * addresses the variable while second index addresses the point.
@@ -216,7 +218,7 @@ class CLookUpTable {
    */
   void Linear_Interpolation(const su2double val_CV3, const unsigned long lower_level, const unsigned long upper_level,
                             std::vector<su2double>& lower_values, std::vector<su2double>& upper_values,
-                            std::vector<su2double*>& var_vals) const;
+                            std::vector<su2double>& var_vals) const;
 
   /*!
    * \brief Find the point on the hull (boundary of the table) that is closest to the point P(val_CV1,val_CV2).
@@ -345,7 +347,7 @@ class CLookUpTable {
    * \param[in] val_CV3 - Value of controlling variable 3.
    * \returns 1 if the lookup and subsequent interpolation was a success, 0 if not.
    */
-  unsigned long LookUp_XYZ(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars,
+  unsigned long LookUp_XYZ(const std::vector<std::string>& val_names_var, std::vector<su2double>& val_vars,
                            su2double val_CV1, su2double val_CV2, su2double val_CV3 = 0);
 
   /*!
diff --git a/Common/include/containers/CTrapezoidalMap.hpp b/Common/include/containers/CTrapezoidalMap.hpp
index 982f9430992..cbb77b4a70f 100644
--- a/Common/include/containers/CTrapezoidalMap.hpp
+++ b/Common/include/containers/CTrapezoidalMap.hpp
@@ -54,12 +54,14 @@ class CTrapezoidalMap {
    * same band. Used to sort the edges */
   su2vector<std::vector<std::pair<su2double, unsigned long> > > y_edge_at_band_mid;
 
+  double memory_footprint = 0;
  public:
   CTrapezoidalMap() = default;
 
   CTrapezoidalMap(const su2double* samples_x, const su2double* samples_y, const unsigned long size,
                   const std::vector<std::array<unsigned long, 2> >& edges,
-                  const su2vector<std::vector<unsigned long> >& edge_to_triangle);
+                  const su2vector<std::vector<unsigned long> >& edge_to_triangle,
+                  bool display = false);
 
   /*!
    * \brief return the index to the triangle that contains the coordinates (val_x,val_y)
@@ -97,4 +99,10 @@ class CTrapezoidalMap {
   inline bool IsInsideHullX(su2double val_x) {
     return (val_x >= unique_bands_x.front()) && (val_x <= unique_bands_x.back());
   }
+
+  /*!
+   * \brief get memory footprint of trapezoidal map.
+   * \return - memory footprint in mega bytes.
+   */
+  double GetMemoryFootprint() { return memory_footprint; }
 };
diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index ea657b43afd..7836da64ffb 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -1307,6 +1307,7 @@ static const MapType<std::string, SPECIES_MODEL> Species_Model_Map = {
 enum FLAMELET_SCALAR_VARIABLES {
   I_PROGVAR,
   I_ENTH,
+  I_MIXFRAC,
 };
 
 /*!
@@ -1316,6 +1317,12 @@ enum FLAMELET_SCALAR_SOURCES {
   I_SRC_TOT_PROGVAR
 };
 
+enum FLAMELET_LOOKUP_OPS {
+  TD,
+  SOURCES,
+  LOOKUP,
+};
+
 /*!
  * \brief Types of subgrid scale models
  */
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index ace96e28cbb..39421d82965 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -5463,8 +5463,8 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
 
   /*--- Define some variables for flamelet model. ---*/
   if (Kind_Species_Model == SPECIES_MODEL::FLAMELET) {
-    /*--- The controlling variables are progress variable and total enthalpy ---*/
-    n_control_vars = 2;
+    /*--- The controlling variables are progress variable, total enthalpy, and optionally mixture fraction ---*/
+    n_control_vars = nSpecies - n_user_scalars;
     /*--- We can have additional user defined transported scalars ---*/
     n_scalars = n_control_vars + n_user_scalars;
   }
diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index d13feb6b82c..e4b084df3a3 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -73,9 +73,13 @@ CLookUpTable::CLookUpTable(const string& var_file_name_lut, string name_CV1_in,
   trap_map_x_y.resize(n_table_levels);
   su2double startTime = SU2_MPI::Wtime();
   unsigned short barwidth = 65;
+  bool display_map_info = (n_table_levels < 2); 
+  double tmap_memory_footprint = 0;
   for (auto i_level = 0ul; i_level < n_table_levels; i_level++) {
     trap_map_x_y[i_level] = CTrapezoidalMap(GetDataP(name_CV1, i_level), GetDataP(name_CV2, i_level),
-                                            table_data[i_level].cols(), edges[i_level], edge_to_triangle[i_level]);
+                                            table_data[i_level].cols(), edges[i_level], edge_to_triangle[i_level],
+                                            display_map_info);
+    tmap_memory_footprint += trap_map_x_y[i_level].GetMemoryFootprint();
     /* Display a progress bar to monitor table generation process */
     if (rank == MASTER_NODE) {
       su2double progress = su2double(i_level) / n_table_levels;
@@ -100,6 +104,8 @@ CLookUpTable::CLookUpTable(const string& var_file_name_lut, string name_CV1_in,
       default:
         break;
     }
+    cout << "Trapezoidal map memory footprint: " << tmap_memory_footprint << " MB\n";
+    cout << "Table data memory footprint: " << memory_footprint_data << " MB\n" << endl;
   }
 
   ComputeInterpCoeffs();
@@ -133,7 +139,9 @@ void CLookUpTable::LoadTableRaw(const string& var_file_name_lut) {
     table_data[i_level] = file_reader.GetTableData(i_level);
     triangles[i_level] = file_reader.GetTriangles(i_level);
     hull[i_level] = file_reader.GetHull(i_level);
+    memory_footprint_data += n_points[i_level] * sizeof(su2double);
   }
+  memory_footprint_data /= 1e6;
 
   n_variables = file_reader.GetNVariables();
   version_lut = file_reader.GetVersionLUT();
@@ -164,7 +172,7 @@ void CLookUpTable::FindTableLimits(const string& name_cv1, const string& name_cv
   }
 
   if (table_dim == 3) {
-    limits_table_z = minmax_element(z_values_levels.data(), z_values_levels.data() + z_values_levels.cols());
+    limits_table_z = minmax_element(&z_values_levels[0], &z_values_levels[0] + z_values_levels.size());
   }
 }
 
@@ -451,7 +459,7 @@ unsigned long CLookUpTable::LookUp_XYZ(const std::string& val_name_var, su2doubl
     return 1;
   }
 }
-unsigned long CLookUpTable::LookUp_XYZ(const std::vector<std::string>& val_names_var, std::vector<su2double*>& val_vars,
+unsigned long CLookUpTable::LookUp_XYZ(const std::vector<std::string>& val_names_var, std::vector<su2double>& val_vars,
                                        su2double val_CV1, su2double val_CV2, su2double val_CV3) {
   /*--- Perform quasi-3D interpolation for a vector of variables with names val_names_var
         on a query point with coordinates val_CV1, val_CV2, and val_CV3 ---*/
@@ -509,7 +517,7 @@ void CLookUpTable::Linear_Interpolation(const su2double val_CV3, const unsigned
 
 void CLookUpTable::Linear_Interpolation(const su2double val_CV3, const unsigned long lower_level,
                                         const unsigned long upper_level, std::vector<su2double>& lower_values,
-                                        std::vector<su2double>& upper_values, std::vector<su2double*>& var_vals) const {
+                                        std::vector<su2double>& upper_values, std::vector<su2double>& var_vals) const {
   /* Perform linear interpolation along the z-direction of the table for multiple variables */
 
   /* Retrieve constant z-values of inclusion levels */
@@ -522,7 +530,7 @@ void CLookUpTable::Linear_Interpolation(const su2double val_CV3, const unsigned
 
   /* Perform linear interpolation */
   for (size_t iVar = 0; iVar < var_vals.size(); iVar++) {
-    *var_vals[iVar] = lower_values[iVar] * factor_lower + upper_values[iVar] * factor_upper;
+    var_vals[iVar] = lower_values[iVar] * factor_lower + upper_values[iVar] * factor_upper;
   }
 }
 
diff --git a/Common/src/containers/CTrapezoidalMap.cpp b/Common/src/containers/CTrapezoidalMap.cpp
index c0f71e98eb0..804c27e8eb6 100644
--- a/Common/src/containers/CTrapezoidalMap.cpp
+++ b/Common/src/containers/CTrapezoidalMap.cpp
@@ -40,7 +40,8 @@ using namespace std;
  */
 CTrapezoidalMap::CTrapezoidalMap(const su2double* samples_x, const su2double* samples_y, const unsigned long size,
                                  vector<std::array<unsigned long, 2> > const& edges,
-                                 su2vector<vector<unsigned long> > const& val_edge_to_triangle) {
+                                 su2vector<vector<unsigned long> > const& val_edge_to_triangle,
+                                 bool display) {
   int rank = SU2_MPI::GetRank();
   su2double startTime = SU2_MPI::Wtime();
 
@@ -148,11 +149,10 @@ CTrapezoidalMap::CTrapezoidalMap(const su2double* samples_x, const su2double* sa
     for (unsigned long j_y = 0; j_y < y_edge_at_band_mid[i_y].size(); j_y++)
       size_y_edge_at_band_mid += sizeof(su2double) / 1e6 + sizeof(unsigned long) / 1e6;
 
-  double size_total =
-      size_unique_bands + size_edge_limits_x + size_edge_limits_y + size_edge_to_triangle + size_y_edge_at_band_mid;
+  memory_footprint = size_unique_bands + size_edge_limits_x + size_edge_limits_y + size_edge_to_triangle + size_y_edge_at_band_mid;
 
   /* print size of trapezoidal map components to screen */
-  if (rank == MASTER_NODE) {
+  if ((rank == MASTER_NODE) && display) {
     cout << setfill(' ');
     cout << "\n" << endl;
     cout << "+------------------------------------------------------------------+\n";
@@ -171,7 +171,7 @@ CTrapezoidalMap::CTrapezoidalMap(const su2double* samples_x, const su2double* sa
          << " |" << endl;
     cout << "| Size of y_edge_at_band_mid in memory: " << setw(22) << size_y_edge_at_band_mid << " MB "
          << " |" << endl;
-    cout << "| Total:                                " << setw(22) << size_total << " MB "
+    cout << "| Total:                                " << setw(22) << memory_footprint << " MB "
          << " |" << endl;
     cout << "+------------------------------------------------------------------+" << endl;
     cout << "\n" << endl;
diff --git a/SU2_CFD/include/fluid/CFluidFlamelet.hpp b/SU2_CFD/include/fluid/CFluidFlamelet.hpp
index 1d0bf91986d..5e2e7d7a455 100644
--- a/SU2_CFD/include/fluid/CFluidFlamelet.hpp
+++ b/SU2_CFD/include/fluid/CFluidFlamelet.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file CFluidFlamelet.hpp
  * \brief  Defines the flamelet fluid model
- * \author D. Mayer, T. Economon, N. Beishuizen
+ * \author D. Mayer, T. Economon, N. Beishuizen, E. Bunschoten
  * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
@@ -32,37 +32,39 @@
 
 class CFluidFlamelet final : public CFluidModel {
  private:
-  enum LOOKUP_TD {
-    TEMPERATURE,
-    DENSITY,
-    HEATCAPACITY,
-    VISCOSITY,
-    CONDUCTIVITY,
-    DIFFUSIONCOEFFICIENT,
-    MOLARWEIGHT,
-    SIZE
-  };
+  enum LOOKUP_TD { TEMPERATURE, HEATCAPACITY, VISCOSITY, CONDUCTIVITY, DIFFUSIONCOEFFICIENT, MOLARWEIGHT, SIZE };
 
   int rank;
 
-  unsigned short n_scalars;
-  unsigned short n_lookups;
-  unsigned short n_user_scalars; /*!< \brief number of passive reactant species. */
-  unsigned short n_control_vars; /*!< \brief number of controlling variables. */
+  bool include_mixture_fraction = false, /*!< \brief include mixture fraction in controlling variables. */ 
+       generate_manifold = false;
+
+  unsigned short n_scalars, n_lookups, n_user_scalars, /*!< \brief number of passive reactant species. */
+      n_control_vars;                                  /*!< \brief number of controlling variables. */
+
+  unsigned long extrapolation;
 
   vector<string> table_scalar_names; /*!< \brief vector to store names of scalar variables.   */
-  vector<string> table_lookup_names; /*!< \brief vector to store names of look up variables.   */
 
-  su2double mass_diffusivity; /*!< \brief local mass diffusivity of the mixture */
-  su2double molar_weight;     /*!< \brief local molar weight of the mixture */
+  su2double mass_diffusivity, /*!< \brief local mass diffusivity of the mixture */
+      molar_weight;           /*!< \brief local molar weight of the mixture */
 
   CLookUpTable* look_up_table;
 
-  vector<string> varnames_TD;    /*!< \brief Lookup names for thermodynamic state variables. */
-  vector<su2double> val_vars_TD; /*!< \brief References to thermodynamic state variables. */
+  vector<su2double> scalars_vector;
+
+  vector<string> varnames_TD, /*!< \brief Lookup names for thermodynamic state variables. */
+                 varnames_Sources,
+                 varnames_LookUp;
+
+  vector<su2double> val_vars_TD, /*!< \brief References to thermodynamic state variables. */
+                    val_vars_Sources,
+                    val_vars_LookUp;
+  
+  void PreprocessLookUp(CConfig* config);
 
  public:
-  CFluidFlamelet(CConfig* config, su2double value_pressure_operating);
+  CFluidFlamelet(CConfig* config, su2double value_pressure_operating, bool load_manifold = false);
 
   ~CFluidFlamelet();
 
@@ -74,21 +76,19 @@ class CFluidFlamelet final : public CFluidModel {
   void SetTDState_T(su2double val_temperature, const su2double* val_scalars = nullptr) override;
 
   /*!
-   * \brief Get the total enthalpy from the tabulated temperature and species (inverse lookup).
-   * \param[in/out] enthalpy - total enthalpy
-   * \param[in] val_prog - progress variable
-   * \param[in] val_temp - temperature
-   * \param[in] initial_value - initial value for the iterative lookup procedure.
-   * \param[out] exit_code = error code
+   * \brief Evaluate the flamelet manifold.
+   * \param[in] input_scalar - scalar solution.
+   * \param[in] input_varnames - names of variables to evaluate.
+   * \param[in] output_refs - output data.
+   * \param[out] Extrapolation - scalar solution is within bounds (0) or out of bounds (1).
    */
-  unsigned long GetEnthFromTemp(su2double& enthalpy, const su2double val_prog, const su2double val_temp,
-                                su2double initial_value = 0) override;
+  inline unsigned long EvaluateDataSet(vector<su2double> &input_scalar, FLAMELET_LOOKUP_OPS lookup_type, vector<su2double> &output_refs) override;
 
   /*!
-   * \brief Return a pointer to the lookup table.
-   * \param[out] look_up_table - pointer to lookup table
+   * \brief Check for out-of-bounds condition for data set interpolation.
+   * \return - within bounds (0) or out of bounds (1).
    */
-  inline CLookUpTable* GetLookUpTable() override { return look_up_table; }
+  inline unsigned long GetExtrapolation() override { return extrapolation; }
 
   /*!
    * \brief Get the mass diffusivity of the species.
@@ -110,5 +110,4 @@ class CFluidFlamelet final : public CFluidModel {
    * \param[out] Mu - value of the laminar viscosity
    */
   inline su2double GetLaminarViscosity() override { return Mu; }
-
 };
diff --git a/SU2_CFD/include/fluid/CFluidModel.hpp b/SU2_CFD/include/fluid/CFluidModel.hpp
index 5e3785bcda1..d757a1d7830 100644
--- a/SU2_CFD/include/fluid/CFluidModel.hpp
+++ b/SU2_CFD/include/fluid/CFluidModel.hpp
@@ -144,17 +144,12 @@ class CFluidModel {
   virtual inline unsigned short GetNScalars() const { return 0; }
 
   /*!
-   * \brief Flamelet LUT - Get the lookup table.
+   * \brief Evaluate data manifold for flamelet or data-driven fluid problems.
+   * \param[in] input - input data for manifold regression.
    */
-  virtual CLookUpTable* GetLookUpTable() { return nullptr; }
+  virtual unsigned long EvaluateDataSet(vector<su2double> &input_scalar, FLAMELET_LOOKUP_OPS lookup_type, vector<su2double> &output_refs) { return 0; }
 
-  /*!
-   * \brief Flamelet LUT - Get the total enthalpy from the temperature (reverse lookup).
-   */
-  virtual inline unsigned long GetEnthFromTemp(su2double& enthalpy,
-                                               const su2double val_prog,
-                                               const su2double val_temp,
-                                               su2double initial_value) { return 0; }
+  virtual unsigned long GetExtrapolation() { return 0; }
 
   /*!
    * \brief Get fluid dynamic viscosity.
diff --git a/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp b/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp
index 95b4afe7311..b0727e4e242 100644
--- a/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp
+++ b/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp
@@ -38,7 +38,7 @@
 class CSpeciesFlameletSolver final : public CSpeciesSolver {
  private:
   vector<su2activematrix> conjugate_var; /*!< \brief CHT variables for each boundary and vertex. */
-
+  bool include_mixture_fraction = false; /*!< \brief include mixture fraction as a controlling variable. */
   /*!
    * \brief Compute the preconditioner for low-Mach flows.
    * \param[in] geometry - Geometrical definition of the problem.
@@ -64,6 +64,46 @@ class CSpeciesFlameletSolver final : public CSpeciesSolver {
                                   CNumerics* visc_numerics, CConfig* config, unsigned short val_marker,
                                   bool cht_mode = false);
 
+  /*!
+   * \brief Reverse look-up to retrieve enthalpy value based on temperature and other controlling variables.
+   * \param[in] fluid_model - pointer to flamelet fluid model.
+   * \param[in] val_temp - temperature value used for reverse look-up.
+   * \param[in] val_enth - pointer to enthalpy value to be retrieved.
+   * \param[in] scalar_solution - local scalar solution.
+   * \param[out] Converged - 0 if Newton solver converged, 1 if not.
+   */
+  unsigned long GetEnthFromTemp(CFluidModel * fluid_model, su2double const val_temp, su2double * val_enth, const su2double * scalar_solution);
+
+  /*!
+   * \brief Find maximum progress variable value within the manifold for the current solution.
+   * \param[in] fluid_model - pointer to flamelet fluid model.
+   * \param[in] scalars - local scalar solution.
+   * \return - maximum progress variable value within manifold bounds.
+   */
+  su2double GetBurntProgressVariable(CFluidModel * fluid_model, const su2double * scalars);
+
+  /*!
+   * \brief Retrieve scalar source terms from manifold.
+   * \param[in] config - definition of particular problem.
+   * \param[in] fluid_model_local - pointer to flamelet fluid model.
+   * \param[in] iPoint - node ID.
+   * \param[in] scalars - local scalar solution.
+   * \param[in] table_source_names - variable names of scalar source terms.
+   * \return - within manifold bounds (0) or outside manifold bounds (1).
+   */
+  unsigned long SetScalarSources(CConfig *config, CFluidModel *fluid_model_local, unsigned long iPoint, vector<su2double> &scalars);
+
+  /*!
+   * \brief Retrieve passive look-up data from manifold.
+   * \param[in] config - definition of particular problem.
+   * \param[in] fluid_model_local - pointer to flamelet fluid model.
+   * \param[in] iPoint - node ID.
+   * \param[in] scalars - local scalar solution.
+   * \param[in] table_lookup_names - variable names of scalar source terms.
+   * \return - within manifold bounds (0) or outside manifold bounds (1).
+   */
+  unsigned long SetScalarLookUps(CConfig *config, CFluidModel *fluid_model_local, unsigned long iPoint, vector<su2double> &scalars);
+
  public:
   /*!
    * \brief Constructor.
@@ -167,5 +207,4 @@ class CSpeciesFlameletSolver final : public CSpeciesSolver {
     conjugate_var[val_marker][val_vertex][pos_var] =
         relaxation_factor * val_var + (1.0 - relaxation_factor) * conjugate_var[val_marker][val_vertex][pos_var];
   }
-
 };
diff --git a/SU2_CFD/src/fluid/CFluidFlamelet.cpp b/SU2_CFD/src/fluid/CFluidFlamelet.cpp
index 34051288559..c5bf7cc3c1c 100644
--- a/SU2_CFD/src/fluid/CFluidFlamelet.cpp
+++ b/SU2_CFD/src/fluid/CFluidFlamelet.cpp
@@ -1,7 +1,7 @@
 /*!
  * \file CfluidFlamelet.cpp
  * \brief Main subroutines of CFluidFlamelet class
- * \author D. Mayer, T. Economon, N. Beishuizen
+ * \author D. Mayer, T. Economon, N. Beishuizen, E. Bunschoten
  * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
@@ -28,12 +28,13 @@
 #include "../include/fluid/CFluidFlamelet.hpp"
 #include "../../../Common/include/containers/CLookUpTable.hpp"
 
-CFluidFlamelet::CFluidFlamelet(CConfig* config, su2double value_pressure_operating) : CFluidModel() {
+CFluidFlamelet::CFluidFlamelet(CConfig* config, su2double value_pressure_operating, bool load_manifold) : CFluidModel(), generate_manifold(load_manifold) {
   rank = SU2_MPI::GetRank();
 
   /* -- number of auxiliary species transport equations, e.g. 1=CO, 2=NOx  --- */
   n_user_scalars = config->GetNUserScalars();
   n_control_vars = config->GetNControlVars();
+  include_mixture_fraction = (n_control_vars == 3);
   n_scalars = config->GetNScalars();
 
   if (rank == MASTER_NODE) {
@@ -48,91 +49,115 @@ CFluidFlamelet::CFluidFlamelet(CConfig* config, su2double value_pressure_operati
     cout << "*****************************************" << endl;
   }
 
+  scalars_vector.resize(n_scalars);
+
   table_scalar_names.resize(n_scalars);
   table_scalar_names[I_ENTH] = "EnthalpyTot";
   table_scalar_names[I_PROGVAR] = "ProgressVariable";
+  if (include_mixture_fraction) table_scalar_names[I_MIXFRAC] = "MixtureFraction";
+
   /*--- auxiliary species transport equations---*/
   for (size_t i_aux = 0; i_aux < n_user_scalars; i_aux++) {
     table_scalar_names[n_control_vars + i_aux] = config->GetUserScalarName(i_aux);
   }
-
-  look_up_table = new CLookUpTable(config->GetFileNameLUT(), table_scalar_names[I_PROGVAR], table_scalar_names[I_ENTH]);
-
-  n_lookups = config->GetNLookups();
-  table_lookup_names.resize(n_lookups);
-  for (int i_lookup = 0; i_lookup < n_lookups; ++i_lookup) {
-    table_lookup_names[i_lookup] = config->GetLUTLookupName(i_lookup);
-  }
+  
+  if (generate_manifold)
+    look_up_table = new CLookUpTable(config->GetFileNameLUT(), table_scalar_names[I_PROGVAR], table_scalar_names[I_ENTH]);
 
   Pressure = value_pressure_operating;
 
-  /*--- Thermodynamic state variables and names. ---*/
-  varnames_TD.resize(LOOKUP_TD::SIZE);
-  val_vars_TD.resize(LOOKUP_TD::SIZE);
-
-  /*--- The string in varnames_TD as it appears in the LUT file. ---*/
-  varnames_TD[LOOKUP_TD::TEMPERATURE] =  "Temperature";
-  varnames_TD[LOOKUP_TD::DENSITY] = "Density";
-  varnames_TD[LOOKUP_TD::HEATCAPACITY] = "Cp";
-  varnames_TD[LOOKUP_TD::VISCOSITY] = "ViscosityDyn";
-  varnames_TD[LOOKUP_TD::CONDUCTIVITY] = "Conductivity";
-  varnames_TD[LOOKUP_TD::DIFFUSIONCOEFFICIENT] = "DiffusionCoefficient";
-  varnames_TD[LOOKUP_TD::MOLARWEIGHT] = "MolarWeightMix";
-
+  PreprocessLookUp(config);
+ 
 }
 
-CFluidFlamelet::~CFluidFlamelet() { delete look_up_table; }
+CFluidFlamelet::~CFluidFlamelet() { if(generate_manifold) delete look_up_table; }
 
 void CFluidFlamelet::SetTDState_T(su2double val_temperature, const su2double* val_scalars) {
-  su2double val_enth = val_scalars[I_ENTH];
-  su2double val_prog = val_scalars[I_PROGVAR];
+  for (auto iVar = 0u; iVar < n_scalars; iVar++) scalars_vector[iVar] = val_scalars[iVar];
 
   /*--- Add all quantities and their names to the look up vectors. ---*/
-  look_up_table->LookUp_XY(varnames_TD, val_vars_TD, val_prog, val_enth);
+  EvaluateDataSet(scalars_vector, FLAMELET_LOOKUP_OPS::TD, val_vars_TD);
 
   Temperature = val_vars_TD[LOOKUP_TD::TEMPERATURE];
-  Density = val_vars_TD[LOOKUP_TD::DENSITY];
   Cp = val_vars_TD[LOOKUP_TD::HEATCAPACITY];
   Mu = val_vars_TD[LOOKUP_TD::VISCOSITY];
   Kt = val_vars_TD[LOOKUP_TD::CONDUCTIVITY];
   mass_diffusivity = val_vars_TD[LOOKUP_TD::DIFFUSIONCOEFFICIENT];
   molar_weight = val_vars_TD[LOOKUP_TD::MOLARWEIGHT];
+  Density = Pressure / (molar_weight * UNIVERSAL_GAS_CONSTANT * Temperature);
 
   /*--- Compute Cv from Cp and molar weight of the mixture (ideal gas). ---*/
   Cv = Cp - UNIVERSAL_GAS_CONSTANT / molar_weight;
 }
 
-/* --- Total enthalpy is the transported variable, but we usually have temperature as a boundary condition,
-       so we do a reverse lookup */
-unsigned long CFluidFlamelet::GetEnthFromTemp(su2double& val_enth, const su2double val_prog, const su2double val_temp,
-                                              const su2double initial_value) {
-  /*--- convergence criterion for temperature in [K], high accuracy needed for restarts. ---*/
-  su2double delta_temp_final = 0.001;
-  su2double enth_iter = initial_value;
-  su2double delta_enth;
-  su2double delta_temp_iter = 1e10;
-  unsigned long exit_code = 0;
-  const int counter_limit = 1000;
-
-  int counter = 0;
-  while ((abs(delta_temp_iter) > delta_temp_final) && (counter++ < counter_limit)) {
-    /*--- Add all quantities and their names to the look up vectors. ---*/
-    look_up_table->LookUp_XY(varnames_TD, val_vars_TD, val_prog, enth_iter);
-    Temperature = val_vars_TD[LOOKUP_TD::TEMPERATURE];
-    Cp = val_vars_TD[LOOKUP_TD::HEATCAPACITY];
-
-    delta_temp_iter = val_temp - Temperature;
-
-    delta_enth = Cp * delta_temp_iter;
-
-    enth_iter += delta_enth;
+void CFluidFlamelet::PreprocessLookUp(CConfig* config) {
+   /*--- Thermodynamic state variables and names. ---*/
+  varnames_TD.resize(LOOKUP_TD::SIZE);
+  val_vars_TD.resize(LOOKUP_TD::SIZE);
+
+  /*--- The string in varnames_TD as it appears in the LUT file. ---*/
+  varnames_TD[LOOKUP_TD::TEMPERATURE] = "Temperature";
+  varnames_TD[LOOKUP_TD::HEATCAPACITY] = "Cp";
+  varnames_TD[LOOKUP_TD::VISCOSITY] = "ViscosityDyn";
+  varnames_TD[LOOKUP_TD::CONDUCTIVITY] = "Conductivity";
+  varnames_TD[LOOKUP_TD::DIFFUSIONCOEFFICIENT] = "DiffusionCoefficient";
+  varnames_TD[LOOKUP_TD::MOLARWEIGHT] = "MolarWeightMix";
+
+  /*--- Scalar source term variables and names. ---*/
+  size_t n_sources = 1 + 2*n_user_scalars;
+  varnames_Sources.resize(n_sources);
+  val_vars_Sources.resize(n_sources);
+  varnames_Sources[I_SRC_TOT_PROGVAR] = "ProdRateTot_PV";
+  /*--- No source term for enthalpy ---*/
+
+  /*--- For the auxiliary equations, we use a positive (production) and a negative (consumption) term:
+        S_tot = S_PROD + S_CONS * Y ---*/
+
+  for (size_t i_aux = 0; i_aux < n_user_scalars; i_aux++) {
+    /*--- Order of the source terms: S_prod_1, S_cons_1, S_prod_2, S_cons_2, ...---*/
+    varnames_Sources[1 + 2 * i_aux] = config->GetUserSourceName(2 * i_aux);
+    varnames_Sources[1 + 2 * i_aux + 1] = config->GetUserSourceName(2 * i_aux + 1);
   }
 
-  val_enth = enth_iter;
+  /*--- Passive look-up terms ---*/
+  size_t n_lookups = config->GetNLookups();
+  varnames_LookUp.resize(n_lookups);
+  val_vars_LookUp.resize(n_lookups);
+  for (auto iLookup=0u; iLookup < n_lookups; iLookup++)
+    varnames_LookUp[iLookup] = config->GetLUTLookupName(iLookup);
+
+}
+
+unsigned long CFluidFlamelet::EvaluateDataSet(vector<su2double> &input_scalar, FLAMELET_LOOKUP_OPS lookup_type, vector<su2double> &output_refs) {
+  su2double val_enth = input_scalar[I_ENTH];
+  su2double val_prog = input_scalar[I_PROGVAR];
+  su2double val_mixfrac = include_mixture_fraction ? input_scalar[I_MIXFRAC] : 0.0;
+  vector<string> varnames;
+  vector<su2double> val_vars;
+  switch (lookup_type)
+  {
+  case FLAMELET_LOOKUP_OPS::TD:
+    varnames = varnames_TD;
+    break;
+  case FLAMELET_LOOKUP_OPS::SOURCES:
+    varnames = varnames_Sources;
+    break;
+  case FLAMELET_LOOKUP_OPS::LOOKUP:
+    varnames = varnames_LookUp;
+    break;
+  
+  default:
+    break;
+  }
+  if (output_refs.size() != varnames.size())
+    SU2_MPI::Error(string("Output vector size incompatible with manifold lookup operation."), CURRENT_FUNCTION);
 
-  if (counter >= counter_limit) {
-    exit_code = 1;
+  /*--- Add all quantities and their names to the look up vectors. ---*/
+  if (include_mixture_fraction) {
+    extrapolation = look_up_table->LookUp_XYZ(varnames, output_refs, val_prog, val_enth, val_mixfrac);
+  } else {
+    extrapolation = look_up_table->LookUp_XY(varnames, output_refs, val_prog, val_enth);
   }
 
-  return exit_code;
+  return extrapolation;
 }
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index 4f7f94f0d02..56461b534a3 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -958,6 +958,8 @@ void CFlowOutput::SetCustomOutputs(const CSolver* const* solver, const CGeometry
 // The "AddHistoryOutput(" must not be split over multiple lines to ensure proper python parsing
 // clang-format off
 void CFlowOutput::AddHistoryOutputFields_ScalarRMS_RES(const CConfig* config) {
+  const auto include_mixfrac = (config->GetNControlVars() == 3);
+
   switch (TurbModelFamily(config->GetKind_Turb_Model())) {
     case TURB_FAMILY::SA:
       /// DESCRIPTION: Root-mean square residual of nu tilde (SA model).
@@ -995,6 +997,9 @@ void CFlowOutput::AddHistoryOutputFields_ScalarRMS_RES(const CConfig* config) {
     case SPECIES_MODEL::FLAMELET: {
       AddHistoryOutput("RMS_PROGRESS_VARIABLE", "rms[PV]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the progress variable equation.", HistoryFieldType::RESIDUAL);
       AddHistoryOutput("RMS_TOTAL_ENTHALPY", "rms[Enth]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the total enthalpy equation.", HistoryFieldType::RESIDUAL);
+      if (include_mixfrac)
+        AddHistoryOutput("RMS_MIXTURE_FRACTION", "rms[Mixfrac]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the mixture fraction equation.", HistoryFieldType::RESIDUAL);
+      
       /*--- auxiliary species transport ---*/
       for (auto i_scalar = 0u; i_scalar < config->GetNUserScalars(); i_scalar++){
         const auto& scalar_name = config->GetUserScalarName(i_scalar);
@@ -1007,6 +1012,8 @@ void CFlowOutput::AddHistoryOutputFields_ScalarRMS_RES(const CConfig* config) {
 }
 
 void CFlowOutput::AddHistoryOutputFields_ScalarMAX_RES(const CConfig* config) {
+  const auto include_mixfrac = (config->GetNControlVars() == 3);
+
   switch (TurbModelFamily(config->GetKind_Turb_Model())) {
     case TURB_FAMILY::SA:
       /// DESCRIPTION: Maximum residual of nu tilde (SA model).
@@ -1047,6 +1054,9 @@ void CFlowOutput::AddHistoryOutputFields_ScalarMAX_RES(const CConfig* config) {
     case SPECIES_MODEL::FLAMELET: {
       AddHistoryOutput("MAX_PROGRESS_VARIABLE", "max[PV]", ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the progress variable equation.", HistoryFieldType::RESIDUAL);
       AddHistoryOutput("MAX_TOTAL_ENTHALPY", "max[Enth]", ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the total enthalpy equation.", HistoryFieldType::RESIDUAL);
+      if (include_mixfrac) 
+        AddHistoryOutput("MAX_MIXTURE_FRACTION", "max[Mixfrac]", ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the mixture fraction equation.", HistoryFieldType::RESIDUAL);
+      
       /*--- auxiliary species transport ---*/
       for (auto i_scalar = 0u; i_scalar < config->GetNUserScalars(); i_scalar++){
         const auto& scalar_name = config->GetUserScalarName(i_scalar);
@@ -1060,6 +1070,7 @@ void CFlowOutput::AddHistoryOutputFields_ScalarMAX_RES(const CConfig* config) {
 
 void CFlowOutput::AddHistoryOutputFields_ScalarBGS_RES(const CConfig* config) {
   if (!multiZone) return;
+  const auto include_mixfrac = (config->GetNControlVars() == 3);
 
   switch (TurbModelFamily(config->GetKind_Turb_Model())) {
     case TURB_FAMILY::SA:
@@ -1098,6 +1109,9 @@ void CFlowOutput::AddHistoryOutputFields_ScalarBGS_RES(const CConfig* config) {
     case SPECIES_MODEL::FLAMELET: {
       AddHistoryOutput("BGS_PROGRESS_VARIABLE", "bgs[PV]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the progress variable equation.", HistoryFieldType::RESIDUAL);
       AddHistoryOutput("BGS_TOTAL_ENTHALPY", "bgs[Enth]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the total enthalpy equation.", HistoryFieldType::RESIDUAL);
+      if (include_mixfrac)
+        AddHistoryOutput("BGS_MIXTURE_FRACTION", "bgs[Mixfrac]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the mixture fraction equation.", HistoryFieldType::RESIDUAL);
+      
       /*--- auxiliary species transport ---*/
       for (auto i_scalar = 0u; i_scalar < config->GetNUserScalars(); i_scalar++){
         const auto& scalar_name = config->GetUserScalarName(i_scalar);
@@ -1137,6 +1151,8 @@ void CFlowOutput::AddHistoryOutputFieldsScalarLinsol(const CConfig* config) {
 // clang-format on
 
 void CFlowOutput::LoadHistoryDataScalar(const CConfig* config, const CSolver* const* solver) {
+  const auto include_mixfrac = (config->GetNControlVars() == 3);
+
   switch (TurbModelFamily(config->GetKind_Turb_Model())) {
     case TURB_FAMILY::SA:
       SetHistoryOutputValue("RMS_NU_TILDE", log10(solver[TURB_SOL]->GetRes_RMS(0)));
@@ -1201,6 +1217,10 @@ void CFlowOutput::LoadHistoryDataScalar(const CConfig* config, const CSolver* co
       SetHistoryOutputValue("MAX_PROGRESS_VARIABLE", log10(solver[SPECIES_SOL]->GetRes_Max(I_PROGVAR)));
       SetHistoryOutputValue("RMS_TOTAL_ENTHALPY", log10(solver[SPECIES_SOL]->GetRes_RMS(I_ENTH)));
       SetHistoryOutputValue("MAX_TOTAL_ENTHALPY", log10(solver[SPECIES_SOL]->GetRes_Max(I_ENTH)));
+      if (include_mixfrac) {
+        SetHistoryOutputValue("RMS_MIXTURE_FRACTION", log10(solver[SPECIES_SOL]->GetRes_RMS(I_MIXFRAC)));
+        SetHistoryOutputValue("MAX_MIXTURE_FRACTION", log10(solver[SPECIES_SOL]->GetRes_Max(I_MIXFRAC)));
+      }
       /*--- auxiliary species transport ---*/
       for (unsigned short iReactant=0; iReactant<config->GetNUserScalars(); iReactant++){
         const auto& species_name = config->GetUserScalarName(iReactant);
@@ -1223,6 +1243,8 @@ void CFlowOutput::LoadHistoryDataScalar(const CConfig* config, const CSolver* co
 void CFlowOutput::SetVolumeOutputFieldsScalarSolution(const CConfig* config){
   /*--- Only place outputs of the "SOLUTION" group here. ---*/
 
+  const auto include_mixfrac = (config->GetNControlVars() == 3);
+  
   switch (TurbModelFamily(config->GetKind_Turb_Model())) {
     case TURB_FAMILY::SA:
       AddVolumeOutput("NU_TILDE", "Nu_Tilde", "SOLUTION", "Spalart-Allmaras variable");
@@ -1256,6 +1278,8 @@ void CFlowOutput::SetVolumeOutputFieldsScalarSolution(const CConfig* config){
     case SPECIES_MODEL::FLAMELET:
       AddVolumeOutput("PROGVAR", "Progress_Variable", "SOLUTION", "Progress variable");
       AddVolumeOutput("ENTHALPY", "Total_Enthalpy", "SOLUTION", "Total enthalpy");
+      if (include_mixfrac)
+        AddVolumeOutput("MIXTURE_FRACTION", "Mixture_Fraction", "SOLUTION", "Mixture fraction");
       /*--- auxiliary species ---*/
       for (unsigned short iReactant=0; iReactant<config->GetNUserScalars(); iReactant++) {
         const auto& species_name = config->GetUserScalarName(iReactant);
@@ -1271,6 +1295,7 @@ void CFlowOutput::SetVolumeOutputFieldsScalarSolution(const CConfig* config){
 void CFlowOutput::SetVolumeOutputFieldsScalarResidual(const CConfig* config) {
   /*--- Only place outputs of the "RESIDUAL" group here. ---*/
 
+  const auto include_mixfrac = (config->GetNControlVars() == 3);
   switch (TurbModelFamily(config->GetKind_Turb_Model())){
     case TURB_FAMILY::SA:
       AddVolumeOutput("RES_NU_TILDE", "Residual_Nu_Tilde", "RESIDUAL", "Residual of the Spalart-Allmaras variable");
@@ -1294,6 +1319,9 @@ void CFlowOutput::SetVolumeOutputFieldsScalarResidual(const CConfig* config) {
     case SPECIES_MODEL::FLAMELET:
       AddVolumeOutput("RES_PROGVAR", "Residual_Progress_Variable", "RESIDUAL", "Residual of progress variable");
       AddVolumeOutput("RES_ENTHALPY", "Residual_Total_Enthalpy", "RESIDUAL", "Residual of total enthalpy");
+      if (include_mixfrac) 
+        AddVolumeOutput("RES_MIXFRAC", "Residual_Mixture_Fraction", "RESIDUAL", "Residual of mixture fraction");
+
       /*--- residuals for auxiliary species transport equations ---*/
       for (unsigned short iReactant=0; iReactant<config->GetNUserScalars(); iReactant++){
         const auto& species_name = config->GetUserScalarName(iReactant);
@@ -1319,6 +1347,8 @@ void CFlowOutput::SetVolumeOutputFieldsScalarResidual(const CConfig* config) {
 void CFlowOutput::SetVolumeOutputFieldsScalarLimiter(const CConfig* config) {
   /*--- Only place outputs of the "SOLUTION" group for species transport here. ---*/
 
+  const auto include_mixfrac = (config->GetNControlVars() == 3);
+
   if (config->GetKind_SlopeLimit_Turb() != LIMITER::NONE) {
     switch (TurbModelFamily(config->GetKind_Turb_Model())) {
       case TURB_FAMILY::SA:
@@ -1344,6 +1374,9 @@ void CFlowOutput::SetVolumeOutputFieldsScalarLimiter(const CConfig* config) {
       case SPECIES_MODEL::FLAMELET:
         AddVolumeOutput("LIMITER_PROGVAR", "Limiter_Progress_Variable", "LIMITER", "Limiter of progress variable");
         AddVolumeOutput("LIMITER_ENTHALPY", "Limiter_Total_Enthalpy", "LIMITER", "Limiter of total enthalpy");
+        if (include_mixfrac)
+          AddVolumeOutput("LIMITER_MIXFRAC", "Limiter_Mixture_Fraction", "LIMITER", "Limiter of mixture fraction");
+
         /*--- limiter for auxiliary species transport ---*/
         for (unsigned short iReactant=0; iReactant < config->GetNUserScalars(); iReactant++) {
           const auto& species_name = config->GetUserScalarName(iReactant);
@@ -1461,7 +1494,8 @@ void CFlowOutput::LoadVolumeDataScalar(const CConfig* config, const CSolver* con
   const auto* Node_Turb = (config->GetKind_Turb_Model() != TURB_MODEL::NONE) ? turb_solver->GetNodes() : nullptr;
   const auto* Node_Trans = (config->GetKind_Trans_Model() != TURB_TRANS_MODEL::NONE) ? trans_solver->GetNodes() : nullptr;
   const auto* Node_Geo = geometry->nodes;
-
+  const auto include_mixfrac = (config->GetNControlVars() == 3);
+  
   if (config->GetViscous()) {
     if (nDim == 3){
       SetVolumeOutputValue("VORTICITY_X", iPoint, Node_Flow->GetVorticity(iPoint)[0]);
@@ -1549,7 +1583,10 @@ void CFlowOutput::LoadVolumeDataScalar(const CConfig* config, const CSolver* con
       SetVolumeOutputValue("RES_PROGVAR", iPoint, solver[SPECIES_SOL]->LinSysRes(iPoint, I_PROGVAR));
       SetVolumeOutputValue("RES_ENTHALPY", iPoint, solver[SPECIES_SOL]->LinSysRes(iPoint, I_ENTH));
       SetVolumeOutputValue("TABLE_MISSES", iPoint, su2double(Node_Species->GetTableMisses(iPoint)));
-
+      if (include_mixfrac) {
+        SetVolumeOutputValue("MIXTURE_FRACTION", iPoint, Node_Species->GetSolution(iPoint, I_MIXFRAC));
+        SetVolumeOutputValue("RES_MIXFRAC", iPoint, solver[SPECIES_SOL]->LinSysRes(iPoint, I_MIXFRAC));
+      }
       /*--- auxiliary species transport equations ---*/
       for (unsigned short i_scalar=0; i_scalar<config->GetNUserScalars(); i_scalar++) {
         const auto& scalar_name = config->GetUserScalarName(i_scalar);
@@ -1561,6 +1598,9 @@ void CFlowOutput::LoadVolumeDataScalar(const CConfig* config, const CSolver* con
       if (config->GetKind_SlopeLimit_Species() != LIMITER::NONE) {
         SetVolumeOutputValue("LIMITER_PROGVAR", iPoint, Node_Species->GetLimiter(iPoint, I_PROGVAR));
         SetVolumeOutputValue("LIMITER_ENTHALPY", iPoint, Node_Species->GetLimiter(iPoint, I_ENTH));
+        if (include_mixfrac) 
+          SetVolumeOutputValue("LIMITER_MIXFRAC", iPoint, Node_Species->GetLimiter(iPoint, I_MIXFRAC));
+          
         /*--- limiter for auxiliary species transport equations ---*/
         for (unsigned short i_scalar=0; i_scalar<config->GetNUserScalars(); i_scalar++) {
           const auto& scalar_name = config->GetUserScalarName(i_scalar);
diff --git a/SU2_CFD/src/solvers/CIncEulerSolver.cpp b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
index 355b480eb53..a4f57d4420e 100644
--- a/SU2_CFD/src/solvers/CIncEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
@@ -332,9 +332,8 @@ void CIncEulerSolver::SetNondimensionalization(CConfig *config, unsigned short i
     case FLUID_FLAMELET:
 
       config->SetGas_Constant(UNIVERSAL_GAS_CONSTANT / (config->GetMolecular_Weight() / 1000.0));
-      Pressure_Thermodynamic = Density_FreeStream * Temperature_FreeStream * config->GetGas_Constant();
+      Pressure_Thermodynamic = config->GetPressure_Thermodynamic();
       auxFluidModel = new CFluidFlamelet(config, Pressure_Thermodynamic);
-      auxFluidModel->SetTDState_T(Temperature_FreeStream, config->GetSpecies_Init());
       config->SetPressure_Thermodynamic(Pressure_Thermodynamic);
 
       break;
@@ -488,7 +487,7 @@ void CIncEulerSolver::SetNondimensionalization(CConfig *config, unsigned short i
         break;
 
       case FLUID_FLAMELET:
-        fluidModel = new CFluidFlamelet(config, Pressure_Thermodynamic);
+        fluidModel = new CFluidFlamelet(config, Pressure_Thermodynamic, true);
         fluidModel->SetTDState_T(Temperature_FreeStreamND, config->GetSpecies_Init());
         break;
 
diff --git a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
index f79b12b232f..8d2e8e1d626 100644
--- a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
+++ b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
@@ -38,6 +38,7 @@ CSpeciesFlameletSolver::CSpeciesFlameletSolver(CGeometry* geometry, CConfig* con
     : CSpeciesSolver(geometry, config, true) {
   /*--- Dimension of the problem. ---*/
   nVar = config->GetNScalars();
+  include_mixture_fraction = (config->GetNControlVars() == 3);
 
   Initialize(geometry, config, iMesh, nVar);
 
@@ -82,79 +83,25 @@ void CSpeciesFlameletSolver::Preprocessing(CGeometry* geometry, CSolver** solver
   const auto n_user_scalars = config->GetNUserScalars();
   const auto n_control_vars = config->GetNControlVars();
 
-  vector<string> table_scalar_names(config->GetNScalars());
-  table_scalar_names[I_ENTH] = "EnthalpyTot";
-  table_scalar_names[I_PROGVAR] = "ProgressVariable";
-
-  /*--- auxiliary species transport equations---*/
-  for (size_t i_aux = 0; i_aux < n_user_scalars; i_aux++) {
-    table_scalar_names[n_control_vars + i_aux] = config->GetUserScalarName(i_aux);
-  }
-
-  /*--- we currently only need 1 source term from the LUT for the progress variable
-        and each auxiliary equations needs 2 source terms ---*/
-  unsigned short n_table_sources = 1 + 2 * n_user_scalars;
-
-  vector<string> table_source_names(n_table_sources);
-  table_source_names[I_SRC_TOT_PROGVAR] = "ProdRateTot_PV";
-  /*--- No source term for enthalpy ---*/
-
-  /*--- For the auxiliary equations, we use a positive (production) and a negative (consumption) term:
-        S_tot = S_PROD + S_CONS * Y ---*/
-
-  for (size_t i_aux = 0; i_aux < n_user_scalars; i_aux++) {
-    /*--- Order of the source terms: S_prod_1, S_cons_1, S_prod_2, S_cons_2, ...---*/
-    table_source_names[1 + 2 * i_aux] = config->GetUserSourceName(2 * i_aux);
-    table_source_names[1 + 2 * i_aux + 1] = config->GetUserSourceName(2 * i_aux + 1);
-  }
+  vector<su2double> scalars_vector(nVar);
 
   auto* flowNodes = su2staticcast_p<CFlowVariable*>(solver_container[FLOW_SOL]->GetNodes());
 
   SU2_OMP_SAFE_GLOBAL_ACCESS(config->SetGlobalParam(config->GetKind_Solver(), RunTime_EqSystem);)
 
-  vector<string> table_lookup_names(config->GetNLookups());
-  for (int i_lookup = 0; i_lookup < config->GetNLookups(); ++i_lookup) {
-    table_lookup_names[i_lookup] = config->GetLUTLookupName(i_lookup);
-  }
-
   SU2_OMP_FOR_STAT(omp_chunk_size)
   for (auto i_point = 0u; i_point < nPoint; i_point++) {
     CFluidModel* fluid_model_local = solver_container[FLOW_SOL]->GetFluidModel();
     su2double* scalars = nodes->GetSolution(i_point);
+    for (auto iVar = 0u; iVar < nVar; iVar++) scalars_vector[iVar] = scalars[iVar];
 
     /*--- Compute total source terms from the production and consumption. ---*/
+    unsigned long misses = SetScalarSources(config, fluid_model_local, i_point, scalars_vector);
 
-    vector<su2double> table_sources(n_table_sources);
-    unsigned long misses = fluid_model_local->GetLookUpTable()->LookUp_XY(table_source_names, table_sources,
-                                                                          scalars[I_PROGVAR], scalars[I_ENTH]);
-    nodes->SetTableMisses(i_point, misses);
-
-    /*--- The source term for progress variable is always positive, we clip from below to makes sure. --- */
-
-    vector<su2double> source_scalar(config->GetNScalars());
-    source_scalar[I_PROGVAR] = fmax(EPS, table_sources[I_SRC_TOT_PROGVAR]);
-    source_scalar[I_ENTH] = 0.0;
-
-    /*--- Source term for the auxiliary species transport equations. ---*/
-    for (size_t i_aux = 0; i_aux < config->GetNUserScalars(); i_aux++) {
-      /*--- The source term for the auxiliary equations consists of a production term and a consumption term:
-            S_TOT = S_PROD + S_CONS * Y ---*/
-      su2double y_aux = scalars[n_control_vars + i_aux];
-      su2double source_prod = table_sources[1 + 2 * i_aux];
-      su2double source_cons = table_sources[1 + 2 * i_aux + 1];
-      source_scalar[n_control_vars + i_aux] = source_prod + source_cons * y_aux;
-    }
-    for (auto i_scalar = 0u; i_scalar < nVar; i_scalar++)
-      nodes->SetScalarSource(i_point, i_scalar, source_scalar[i_scalar]);
-
-    vector<su2double> lookup_scalar(config->GetNLookups());
-    misses = fluid_model_local->GetLookUpTable()->LookUp_XY(table_lookup_names, lookup_scalar, scalars[I_PROGVAR],
-                                                            scalars[I_ENTH]);
-
-    for (auto i_lookup = 0u; i_lookup < config->GetNLookups(); i_lookup++) {
-      nodes->SetLookupScalar(i_point, lookup_scalar[i_lookup], i_lookup);
-    }
+    /*--- Obtain passive look-up scalars. ---*/
+    SetScalarLookUps(config, fluid_model_local, i_point, scalars_vector);
 
+    /*--- Set mass diffusivity based on thermodynamic state. ---*/
     su2double T = flowNodes->GetTemperature(i_point);
     fluid_model_local->SetTDState_T(T, scalars);
     /*--- set the diffusivity in the fluid model to the diffusivity obtained from the lookup table ---*/
@@ -179,7 +126,6 @@ void CSpeciesFlameletSolver::SetInitialCondition(CGeometry** geometry, CSolver**
       cout << "Initializing progress variable and total enthalpy (using temperature)" << endl;
     }
 
-    vector<su2double> scalar_init(nVar, 0.0);
     const su2double* flame_init = config->GetFlameInit();
     const su2double flame_offset[3] = {flame_init[0], flame_init[1], flame_init[2]};
     const su2double flame_normal[3] = {flame_init[3], flame_init[4], flame_init[5]};
@@ -190,38 +136,34 @@ void CSpeciesFlameletSolver::SetInitialCondition(CGeometry** geometry, CSolver**
     const su2double temp_inlet = config->GetInc_Temperature_Init();
     su2double prog_inlet = config->GetSpecies_Init()[I_PROGVAR];
     su2double enth_inlet = config->GetSpecies_Init()[I_ENTH];
+    su2double mixfrac_inlet = include_mixture_fraction ? config->GetSpecies_Init()[I_MIXFRAC] : 0.0;
 
-    su2double prog_burnt;
-    su2double prog_unburnt = 0.0;
+    su2double prog_burnt, prog_unburnt, point_loc, scalar_init[nVar];
 
     if (rank == MASTER_NODE) {
       cout << "initial condition: T = " << temp_inlet << endl;
       cout << "initial condition: c = " << prog_inlet << endl;
       cout << "initial condition: h = " << enth_inlet << endl;
+      if (include_mixture_fraction) cout << "initial condition: Z = " << mixfrac_inlet << endl;
     }
 
-    su2double point_loc;
-
     CFluidModel* fluid_model_local;
 
-    vector<string> look_up_tags;
-    vector<su2double*> look_up_data;
-
-    unsigned long n_not_iterated_local = 0;
-    unsigned long n_not_in_domain_local = 0;
-    unsigned long n_points_unburnt_local = 0;
-    unsigned long n_points_burnt_local = 0;
-    unsigned long n_points_flame_local = 0;
-    unsigned long n_not_iterated_global;
-    unsigned long n_not_in_domain_global;
-    unsigned long n_points_burnt_global;
-    unsigned long n_points_flame_global;
-    unsigned long n_points_unburnt_global;
+    unsigned long n_not_iterated_local = 0, n_not_in_domain_local = 0, n_points_unburnt_local = 0,
+                  n_points_burnt_local = 0, n_points_flame_local = 0, n_not_iterated_global, n_not_in_domain_global,
+                  n_points_burnt_global, n_points_flame_global, n_points_unburnt_global;
 
     for (unsigned long i_mesh = 0; i_mesh <= config->GetnMGLevels(); i_mesh++) {
       fluid_model_local = solver_container[i_mesh][FLOW_SOL]->GetFluidModel();
 
-      prog_burnt = *fluid_model_local->GetLookUpTable()->GetTableLimitsX().second;
+      for (auto iVar = 0u; iVar < nVar; iVar++)
+        scalar_init[iVar] = config->GetSpecies_Init()[iVar];
+
+      /*--- Set enthalpy based on initial temperature and scalars. ---*/
+      n_not_iterated_local += GetEnthFromTemp(fluid_model_local, temp_inlet, &enth_inlet, config->GetSpecies_Init());
+      scalar_init[I_ENTH] = enth_inlet;
+
+      prog_burnt = GetBurntProgressVariable(fluid_model_local, scalar_init);
       for (unsigned long i_point = 0; i_point < nPointDomain; i_point++) {
         auto coords = geometry[i_mesh]->nodes->GetCoord(i_point);
 
@@ -256,18 +198,16 @@ void CSpeciesFlameletSolver::SetInitialCondition(CGeometry** geometry, CSolver**
           n_points_unburnt_local++;
         }
 
-        n_not_iterated_local += fluid_model_local->GetEnthFromTemp(enth_inlet, prog_inlet, temp_inlet, enth_inlet);
-        scalar_init[I_ENTH] = enth_inlet;
-
-        n_not_in_domain_local += fluid_model_local->GetLookUpTable()->LookUp_XY(
-            look_up_tags, look_up_data, scalar_init[I_PROGVAR], scalar_init[I_ENTH]);
+        /* --- Perform manifold evaluation to check whether initial scalar is out-of-bounds. --- */
+        fluid_model_local->SetTDState_T(temp_inlet, scalar_init);
+        n_not_in_domain_local += fluid_model_local->GetExtrapolation();
 
         /* --- Initialize the auxiliary transported scalars  (not controlling variables). --- */
         for (int i_scalar = config->GetNControlVars(); i_scalar < config->GetNScalars(); ++i_scalar) {
           scalar_init[i_scalar] = config->GetSpecies_Init()[i_scalar];
         }
 
-        solver_container[i_mesh][SPECIES_SOL]->GetNodes()->SetSolution(i_point, scalar_init.data());
+        solver_container[i_mesh][SPECIES_SOL]->GetNodes()->SetSolution(i_point, scalar_init);
       }
 
       solver_container[i_mesh][SPECIES_SOL]->InitiateComms(geometry[i_mesh], config, SOLUTION);
@@ -303,8 +243,8 @@ void CSpeciesFlameletSolver::SetInitialCondition(CGeometry** geometry, CSolver**
              << endl;
 
       if (n_not_iterated_global > 0)
-        cout << " Initial condition: Number of points in which enthalpy could not be iterated: " << n_not_iterated_global
-             << " !!!" << endl;
+        cout << " Initial condition: Number of points in which enthalpy could not be iterated: "
+             << n_not_iterated_global << " !!!" << endl;
     }
   }
 }
@@ -375,9 +315,7 @@ void CSpeciesFlameletSolver::Source_Residual(CGeometry* geometry, CSolver** solv
                                              CNumerics** numerics_container, CConfig* config, unsigned short iMesh) {
   SU2_OMP_FOR_STAT(omp_chunk_size)
   for (auto i_point = 0u; i_point < nPointDomain; i_point++) {
-
     /*--- Add source terms from the lookup table directly to the residual. ---*/
-
     for (auto i_var = 0; i_var < nVar; i_var++) {
       LinSysRes(i_point, i_var) -= nodes->GetScalarSources(i_point)[i_var] * geometry->nodes->GetVolume(i_point);
     }
@@ -393,18 +331,16 @@ void CSpeciesFlameletSolver::BC_Inlet(CGeometry* geometry, CSolver** solver_cont
   string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
 
   su2double temp_inlet = config->GetInlet_Ttotal(Marker_Tag);
-  const su2double* scalar_inlet = config->GetInlet_SpeciesVal(Marker_Tag);
 
   /*--- We compute inlet enthalpy from the temperature and progress variable. ---*/
-  su2double enth_inlet = scalar_inlet[I_ENTH];
-  solver_container[FLOW_SOL]->GetFluidModel()->GetEnthFromTemp(enth_inlet, scalar_inlet[I_PROGVAR], temp_inlet,
-                                                               scalar_inlet[I_ENTH]);
+  su2double enth_inlet;
+  GetEnthFromTemp(solver_container[FLOW_SOL]->GetFluidModel(), temp_inlet, &enth_inlet,
+                  config->GetInlet_SpeciesVal(Marker_Tag));
 
   SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
   for (auto iVertex = 0u; iVertex < geometry->nVertex[val_marker]; iVertex++) {
     Inlet_SpeciesVars[val_marker][iVertex][I_ENTH] = enth_inlet;
-  END_SU2_OMP_FOR
-
+    END_SU2_OMP_FOR
   }
 
   /*--- Call the general inlet boundary condition implementation. ---*/
@@ -419,7 +355,7 @@ void CSpeciesFlameletSolver::BC_Isothermal_Wall_Generic(CGeometry* geometry, CSo
   su2double temp_wall = config->GetIsothermal_Temperature(Marker_Tag);
   CFluidModel* fluid_model_local = solver_container[FLOW_SOL]->GetFluidModel();
   auto* flowNodes = su2staticcast_p<CFlowVariable*>(solver_container[FLOW_SOL]->GetNodes());
-  su2double enth_init, enth_wall, prog_wall;
+  su2double enth_wall;
   unsigned long n_not_iterated = 0;
 
   /*--- Loop over all the vertices on this boundary marker. ---*/
@@ -434,14 +370,11 @@ void CSpeciesFlameletSolver::BC_Isothermal_Wall_Generic(CGeometry* geometry, CSo
     if (geometry->nodes->GetDomain(iPoint)) {
       if (config->GetMarker_StrongBC(Marker_Tag) == true) {
         /*--- Initial guess for enthalpy value. ---*/
-
-        enth_init = nodes->GetSolution(iPoint, I_ENTH);
-        enth_wall = enth_init;
+        enth_wall = nodes->GetSolution(iPoint, I_ENTH);
 
         /*--- Set enthalpy on the wall. ---*/
-
-        prog_wall = solver_container[SPECIES_SOL]->GetNodes()->GetSolution(iPoint)[I_PROGVAR];
-        n_not_iterated += fluid_model_local->GetEnthFromTemp(enth_wall, prog_wall, temp_wall, enth_init);
+        n_not_iterated += GetEnthFromTemp(fluid_model_local, temp_wall, &enth_wall,
+                                          solver_container[SPECIES_SOL]->GetNodes()->GetSolution(iPoint));
 
         /*--- Impose the value of the enthalpy as a strong boundary
         condition (Dirichlet) and remove any
@@ -509,3 +442,97 @@ void CSpeciesFlameletSolver::BC_ConjugateHeat_Interface(CGeometry* geometry, CSo
                                                         unsigned short val_marker) {
   BC_Isothermal_Wall_Generic(geometry, solver_container, conv_numerics, nullptr, config, val_marker, true);
 }
+
+unsigned long CSpeciesFlameletSolver::SetScalarSources(CConfig* config, CFluidModel* fluid_model_local,
+                                                       unsigned long iPoint, vector<su2double>& scalars) {
+  /*--- Compute total source terms from the production and consumption. ---*/
+
+  vector<su2double> table_sources(1 + 2*config->GetNUserScalars());
+  unsigned long misses = fluid_model_local->EvaluateDataSet(scalars, FLAMELET_LOOKUP_OPS::SOURCES, table_sources);
+  nodes->SetTableMisses(iPoint, misses);
+
+  /*--- The source term for progress variable is always positive, we clip from below to makes sure. --- */
+
+  vector<su2double> source_scalar(config->GetNScalars());
+  source_scalar[I_PROGVAR] = fmax(EPS, table_sources[I_SRC_TOT_PROGVAR]);
+  source_scalar[I_ENTH] = 0.0;
+  if (include_mixture_fraction) source_scalar[I_MIXFRAC] = 0.0;
+
+  /*--- Source term for the auxiliary species transport equations. ---*/
+  for (size_t i_aux = 0; i_aux < config->GetNUserScalars(); i_aux++) {
+    /*--- The source term for the auxiliary equations consists of a production term and a consumption term:
+          S_TOT = S_PROD + S_CONS * Y ---*/
+    su2double y_aux = scalars[config->GetNControlVars() + i_aux];
+    su2double source_prod = table_sources[1 + 2 * i_aux];
+    su2double source_cons = table_sources[1 + 2 * i_aux + 1];
+    source_scalar[config->GetNControlVars() + i_aux] = source_prod + source_cons * y_aux;
+  }
+  for (auto i_scalar = 0u; i_scalar < nVar; i_scalar++)
+    nodes->SetScalarSource(iPoint, i_scalar, source_scalar[i_scalar]);
+  return misses;
+}
+
+unsigned long CSpeciesFlameletSolver::SetScalarLookUps(CConfig* config, CFluidModel* fluid_model_local,
+                                                       unsigned long iPoint, vector<su2double>& scalars) {
+  /*--- Compute total source terms from the production and consumption. ---*/
+
+  vector<su2double> lookup_scalar(config->GetNLookups());
+  unsigned long misses = fluid_model_local->EvaluateDataSet(scalars, FLAMELET_LOOKUP_OPS::LOOKUP, lookup_scalar);
+
+  for (auto i_lookup = 0u; i_lookup < config->GetNLookups(); i_lookup++) {
+    nodes->SetLookupScalar(iPoint, lookup_scalar[i_lookup], i_lookup);
+  }
+  return misses;
+}
+
+unsigned long CSpeciesFlameletSolver::GetEnthFromTemp(CFluidModel* fluid_model, su2double const val_temp,
+                                                      su2double* val_enth, const su2double* scalar_solution) {
+  /*--- convergence criterion for temperature in [K], high accuracy needed for restarts. ---*/
+  su2double delta_temp_final = 0.001;
+  su2double enth_iter = scalar_solution[I_ENTH];
+  su2double delta_enth;
+  su2double delta_temp_iter = 1e10;
+  unsigned long exit_code = 0;
+  const int counter_limit = 1000;
+
+  int counter = 0;
+
+  su2double val_scalars[nVar];
+  for (auto iVar = 0u; iVar < nVar; iVar++) val_scalars[iVar] = scalar_solution[iVar];
+
+  while ((abs(delta_temp_iter) > delta_temp_final) && (counter++ < counter_limit)) {
+    /*--- Add all quantities and their names to the look up vectors. ---*/
+    val_scalars[I_ENTH] = enth_iter;
+    fluid_model->SetTDState_T(val_temp, val_scalars);
+
+    su2double Temperature = fluid_model->GetTemperature();
+    su2double Cp = fluid_model->GetCp();
+
+    delta_temp_iter = val_temp - Temperature;
+
+    delta_enth = Cp * delta_temp_iter;
+
+    enth_iter += delta_enth;
+  }
+
+  *val_enth = enth_iter;
+
+  if (counter >= counter_limit) {
+    exit_code = 1;
+  }
+
+  return exit_code;
+}
+
+su2double CSpeciesFlameletSolver::GetBurntProgressVariable(CFluidModel* fluid_model, const su2double* scalar_solution) {
+  su2double scalars[nVar];
+  for (auto iVar = 0u; iVar < nVar; iVar++) scalars[iVar] = scalar_solution[iVar];
+
+  bool outside = false;
+  while (!outside) {
+    fluid_model->SetTDState_T(300, scalars);
+    if (fluid_model->GetExtrapolation() == 1) outside = true;
+    scalars[I_PROGVAR] += 1e-3;
+  }
+  return scalars[I_PROGVAR] - 1e-3;
+}
diff --git a/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_premixed_ch4_cfd.cfg b/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_premixed_ch4_cfd.cfg
new file mode 100644
index 00000000000..7856575d99f
--- /dev/null
+++ b/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_premixed_ch4_cfd.cfg
@@ -0,0 +1,138 @@
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+% SU2 configuration file                                                       %
+% Case description: Laminar premixed flame stabilized on isothermal burner     %
+% Author: Nijso Beishuizen                                                     %
+% Institution: Bosch Thermotechnology                                          %
+% Date: 16/06/2023                                                             %
+% File Version 7.5.1 "Blackbird"                                               %
+%                                                                              %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+%
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
+SOLVER = INC_NAVIER_STOKES
+KIND_TURB_MODEL= NONE
+MATH_PROBLEM= DIRECT
+RESTART_SOL= NO
+%
+% ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
+%
+INC_DENSITY_MODEL= VARIABLE 
+INC_ENERGY_EQUATION = YES
+INC_DENSITY_INIT= 1.00
+INC_VELOCITY_INIT= (0.7, 0.0, 0.0 )
+INC_TEMPERATURE_INIT= 300.0
+INC_NONDIM= DIMENSIONAL
+%
+% -------------------- FLUID MODEL --------------------------------------- %
+%
+FLUID_MODEL= FLUID_FLAMELET
+FILENAME_LUT= LUT_methane_PD.drg
+
+OBJECTIVE_FUNCTION= CUSTOM_OBJFUNC
+OBJECTIVE_WEIGHT= 1.0
+% -------------------- SCALAR TRANSPORT ---------------------------------------%
+%
+KIND_SCALAR_MODEL= FLAMELET      
+DIFFUSIVITY_MODEL= FLAMELET
+VISCOSITY_MODEL= FLAMELET
+CONDUCTIVITY_MODEL= FLAMELET
+FLAME_INIT= (0.003, 0.00, 0.00, 1.0, 0.0, 0.0, 1e-4, 1.0)
+% # progvar, enthalpy, mixture fraction, Y-CO, Y-CO2
+SPECIES_INIT = (0.0,	-253498.718914723, 0.05, 0.0, 0.0)
+CONV_NUM_METHOD_SPECIES= BOUNDED_SCALAR
+MUSCL_SPECIES= YES
+SLOPE_LIMITER_SPECIES= NONE
+TIME_DISCRE_SPECIES= EULER_IMPLICIT
+% SCALAR CLIPPING
+SPECIES_CLIPPING= YES
+SPECIES_CLIPPING_MIN= 0 -2.0e6 0 0 0
+SPECIES_CLIPPING_MAX= 0.3 2e6 1 1 1
+%
+MARKER_INLET_SPECIES = (inlet_upper, 0.0,	-253498.718914723, 0.09, 0.0, 0.0,\
+                        inlet_lower, 0.0,	-253498.718914723, 0.01, 0.0, 0.0) 
+CFL_REDUCTION_SPECIES= 1.0
+MARKER_SPECIES_STRONG_BC= (inlet, outlet,cht_interface_burner_fluid, outlet,cht_interface_hex_fluid)
+LOOKUP_NAMES = (MolarWeightMix, Conductivity, Cp, ProdRateTot_PV)
+USER_SCALAR_NAMES= (CO, CO2)
+USER_SOURCE_NAMES = ( \
+    ProdRateTot_Y-CO,  NULL  ,\
+    ProdRateTot_Y-CO2, NULL
+)
+%
+% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
+%
+REF_ORIGIN_MOMENT_X = 0.25
+REF_ORIGIN_MOMENT_Y = 0.00
+REF_ORIGIN_MOMENT_Z = 0.00
+REF_LENGTH= 1.0
+REF_AREA= 1.0
+%
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
+MARKER_ISOTHERMAL= (cht_interface_burner_fluid, 400, cht_interface_hex_fluid, 400)
+MARKER_SYM= (sides)
+INC_INLET_TYPE= VELOCITY_INLET,VELOCITY_INLET
+MARKER_INLET = (inlet_upper, 300.000, 0.3, 1.0, 0.0, 0.0,\
+                inlet_lower, 300.000, 0.25, 1.0, 0.0, 0.0)
+INC_OUTLET_TYPE= PRESSURE_OUTLET
+INC_INLET_DAMPING = 0.05
+INC_OUTLET_DAMPING = 0.05
+MARKER_OUTLET= (outlet, 0.0)
+%
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
+CFL_NUMBER= 20
+CFL_ADAPT= NO
+ITER= 20000
+OUTPUT_WRT_FREQ= 20
+%
+% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
+%
+LINEAR_SOLVER= FGMRES
+LINEAR_SOLVER_PREC= ILU
+LINEAR_SOLVER_ERROR= 1E-03
+LINEAR_SOLVER_ITER= 10
+%
+% -------------------------- MULTIGRID PARAMETERS -----------------------------%
+%
+MGLEVEL= 0
+%
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
+CONV_NUM_METHOD_FLOW= FDS
+MUSCL_FLOW= YES
+SLOPE_LIMITER_FLOW = NONE
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+%
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
+CONV_RESIDUAL_MINVAL= -15
+CONV_STARTITER= 10
+CONV_CAUCHY_ELEMS= 100
+CONV_CAUCHY_EPS= 1E-6
+SCREEN_OUTPUT = INNER_ITER RMS_VELOCITY-X RMS_VELOCITY-Y RMS_PRESSURE RMS_PROGRESS_VARIABLE RMS_TOTAL_ENTHALPY RMS_MIXTURE_FRACTION RMS_CO2
+HISTORY_OUTPUT = RMS_RES AERO_COEFF FLOW_COEFF FLOW_COEFF_SURF
+VOLUME_OUTPUT = SOLUTION PRIMITIVE SOURCE RESIDUAL SENSITIVITY LOOKUP TIMESTEP
+CONV_FIELD = RMS_PRESSURE
+%
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+%
+OUTPUT_PRECISION= 16
+MESH_FORMAT= SU2
+MESH_FILENAME= fluid.su2
+MESH_OUT_FILENAME= mesh_out.su2
+SOLUTION_FILENAME= solution
+RESTART_FILENAME= restart
+%OUTPUT_FILES = (RESTART,PARAVIEW,PARAVIEW_MULTIBLOCK) 
+OUTPUT_FILES = (RESTART,PARAVIEW) 
+TABULAR_FORMAT = CSV
+CONV_FILENAME= history
+VOLUME_FILENAME= ch4_flame_cfd
+SURFACE_FILENAME= surface_flow
+WRT_PERFORMANCE = NO 
+SCREEN_WRT_FREQ_INNER = 1
+SCREEN_WRT_FREQ_OUTER = 1
+
+
diff --git a/TestCases/flamelet/README.md b/TestCases/flamelet/README.md
index 8608d466f0d..5ae4def7851 100644
--- a/TestCases/flamelet/README.md
+++ b/TestCases/flamelet/README.md
@@ -6,3 +6,4 @@
 3. A laminar premixed flame including a heat exchanger (Conjugate Heat Transfer).
 4. A laminar premixed flame including a heat exchanger (Conjugate Heat Transfer), AD test.
 5. An axisymmetric laminar premixed flame.
+6. A laminar, partially premixed flame including a heat exchanger.
\ No newline at end of file

From 883ddf34ee9d730d4b58ba5a9decbfbb96848a16 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 20 Jun 2023 20:48:30 +0200
Subject: [PATCH 496/656] Added config option on controlling variable and their
 sources names and generalized the flamelet output options accordingly

---
 Common/include/CConfig.hpp                    |   9 ++
 Common/include/option_structure.hpp           |   2 +
 Common/src/CConfig.cpp                        |  11 +-
 SU2_CFD/include/fluid/CFluidFlamelet.hpp      |   5 +-
 SU2_CFD/include/fluid/CFluidModel.hpp         |   2 +-
 SU2_CFD/src/fluid/CFluidFlamelet.cpp          |  50 +++++--
 SU2_CFD/src/output/CAdjFlowOutput.cpp         |  66 ++++-----
 SU2_CFD/src/output/CFlowOutput.cpp            | 130 +++++++++---------
 .../src/solvers/CSpeciesFlameletSolver.cpp    |  15 +-
 .../lam_prem_ch4_cfd.cfg                      |   2 +
 .../lam_prem_ch4_hx_ad.cfg                    |   3 +
 .../lam_prem_ch4_hx_dot.cfg                   |   2 +
 .../lam_prem_ch4_cht_cfd_fluid.cfg            |   2 +
 .../lam_prem_ch4_cht_ad_fluid.cfg             |   2 +
 .../lam_prem_ch4_cfd_axi.cfg                  |   2 +
 .../lam_partial_premixed_ch4_cfd.cfg          |   2 +
 16 files changed, 182 insertions(+), 123 deletions(-)

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index 54e00341482..fe6e42176be 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -1223,6 +1223,8 @@ class CConfig {
   unsigned short n_user_sources = 0;  /*!< \brief Number of source terms for user defined (auxiliary) scalar transport equations. */
   unsigned short n_control_vars = 0;  /*!< \brief Number of controlling variables (independent variables) for the LUT. */
 
+  string* controlling_variable_names;
+  string* cv_source_names;
   vector<string> table_scalar_names;  /*!< \brief Names of transported scalar variables. */
   string* table_lookup_names;         /*!< \brief Names of LUT variables. */
   string file_name_lut;               /*!< \brief Filename of the LUT. */
@@ -2145,6 +2147,13 @@ class CConfig {
    */
   unsigned short GetNUserScalars() const { return n_user_scalars; }
 
+  const string& GetControllingVariableName(unsigned short i_cv) const {
+    return controlling_variable_names[i_cv];
+  }
+
+  const string& GetControllingVariableSourceName(unsigned short i_cv) const {
+    return cv_source_names[i_cv];
+  }
   /*!
    * \brief Get the name of the user scalar.
    */
diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index 7836da64ffb..1d69c1eef98 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -613,11 +613,13 @@ enum class INC_DENSITYMODEL {
   CONSTANT,   /*!< \brief Constant density. */
   BOUSSINESQ, /*!< \brief Boussinesq density model. */
   VARIABLE,   /*!< \brief Variable density model. */
+  FLAMELET,   /*!< \brief Density according to flamelet manifold. */
 };
 static const MapType<std::string, INC_DENSITYMODEL> DensityModel_Map = {
   MakePair("CONSTANT", INC_DENSITYMODEL::CONSTANT)
   MakePair("BOUSSINESQ", INC_DENSITYMODEL::BOUSSINESQ)
   MakePair("VARIABLE", INC_DENSITYMODEL::VARIABLE)
+  MakePair("FLAMELET", INC_DENSITYMODEL::FLAMELET)
 };
 
 /*!
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 39421d82965..08b1ace33e7 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -2096,6 +2096,9 @@ void CConfig::SetConfig_Options() {
   /*!\brief File name of the flamelet look up table.*/
   addStringOption("FILENAME_LUT", file_name_lut, string("LUT"));
 
+  addStringListOption("CONTROLLING_VARIABLE_NAMES", n_control_vars, controlling_variable_names);
+  addStringListOption("CONTROLLING_VARIABLE_SOURCE_NAMES", n_control_vars, cv_source_names);
+
   /* DESCRIPTION: Names of the passive lookup variables for flamelet LUT */
   addStringListOption("LOOKUP_NAMES", n_lookups, table_lookup_names);
 
@@ -3928,8 +3931,8 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
                        CURRENT_FUNCTION);
       }
 
-      if (Kind_DensityModel != INC_DENSITYMODEL::VARIABLE) {
-        SU2_MPI::Error("The use of FLUID_FLAMELET requires the INC_DENSITY_MODEL option to be VARIABLE",
+      if ((Kind_DensityModel != INC_DENSITYMODEL::VARIABLE) && (Kind_DensityModel != INC_DENSITYMODEL::FLAMELET)) {
+        SU2_MPI::Error("The use of FLUID_FLAMELET requires the INC_DENSITY_MODEL option to be VARIABLE or FLAMELET",
                        CURRENT_FUNCTION);
       }
 
@@ -5464,7 +5467,9 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
   /*--- Define some variables for flamelet model. ---*/
   if (Kind_Species_Model == SPECIES_MODEL::FLAMELET) {
     /*--- The controlling variables are progress variable, total enthalpy, and optionally mixture fraction ---*/
-    n_control_vars = nSpecies - n_user_scalars;
+    //n_control_vars = nSpecies - n_user_scalars;
+    if (n_control_vars != (nSpecies - n_user_scalars))
+      SU2_MPI::Error("Number of initial species incompatbile with number of controlling variables and user scalars.", CURRENT_FUNCTION);
     /*--- We can have additional user defined transported scalars ---*/
     n_scalars = n_control_vars + n_user_scalars;
   }
diff --git a/SU2_CFD/include/fluid/CFluidFlamelet.hpp b/SU2_CFD/include/fluid/CFluidFlamelet.hpp
index 5e2e7d7a455..1eb69d4beff 100644
--- a/SU2_CFD/include/fluid/CFluidFlamelet.hpp
+++ b/SU2_CFD/include/fluid/CFluidFlamelet.hpp
@@ -43,7 +43,8 @@ class CFluidFlamelet final : public CFluidModel {
       n_control_vars;                                  /*!< \brief number of controlling variables. */
 
   unsigned long extrapolation;
-
+  
+  INC_DENSITYMODEL density_model;
   vector<string> table_scalar_names; /*!< \brief vector to store names of scalar variables.   */
 
   su2double mass_diffusivity, /*!< \brief local mass diffusivity of the mixture */
@@ -82,7 +83,7 @@ class CFluidFlamelet final : public CFluidModel {
    * \param[in] output_refs - output data.
    * \param[out] Extrapolation - scalar solution is within bounds (0) or out of bounds (1).
    */
-  inline unsigned long EvaluateDataSet(vector<su2double> &input_scalar, FLAMELET_LOOKUP_OPS lookup_type, vector<su2double> &output_refs) override;
+  inline unsigned long EvaluateDataSet(vector<su2double> &input_scalar, unsigned short lookup_type, vector<su2double> &output_refs) override;
 
   /*!
    * \brief Check for out-of-bounds condition for data set interpolation.
diff --git a/SU2_CFD/include/fluid/CFluidModel.hpp b/SU2_CFD/include/fluid/CFluidModel.hpp
index d757a1d7830..006dfade11d 100644
--- a/SU2_CFD/include/fluid/CFluidModel.hpp
+++ b/SU2_CFD/include/fluid/CFluidModel.hpp
@@ -147,7 +147,7 @@ class CFluidModel {
    * \brief Evaluate data manifold for flamelet or data-driven fluid problems.
    * \param[in] input - input data for manifold regression.
    */
-  virtual unsigned long EvaluateDataSet(vector<su2double> &input_scalar, FLAMELET_LOOKUP_OPS lookup_type, vector<su2double> &output_refs) { return 0; }
+  virtual unsigned long EvaluateDataSet(vector<su2double> &input_scalar, unsigned short lookup_type, vector<su2double> &output_refs) { return 0; }
 
   virtual unsigned long GetExtrapolation() { return 0; }
 
diff --git a/SU2_CFD/src/fluid/CFluidFlamelet.cpp b/SU2_CFD/src/fluid/CFluidFlamelet.cpp
index c5bf7cc3c1c..5a1f7d7301e 100644
--- a/SU2_CFD/src/fluid/CFluidFlamelet.cpp
+++ b/SU2_CFD/src/fluid/CFluidFlamelet.cpp
@@ -52,9 +52,12 @@ CFluidFlamelet::CFluidFlamelet(CConfig* config, su2double value_pressure_operati
   scalars_vector.resize(n_scalars);
 
   table_scalar_names.resize(n_scalars);
-  table_scalar_names[I_ENTH] = "EnthalpyTot";
-  table_scalar_names[I_PROGVAR] = "ProgressVariable";
-  if (include_mixture_fraction) table_scalar_names[I_MIXFRAC] = "MixtureFraction";
+  for (auto iCV=0u; iCV<n_control_vars; iCV++)
+    table_scalar_names[iCV] = config->GetControllingVariableName(iCV);
+  
+  // table_scalar_names[I_ENTH] = "EnthalpyTot";
+  // table_scalar_names[I_PROGVAR] = "ProgressVariable";
+  // if (include_mixture_fraction) table_scalar_names[I_MIXFRAC] = "MixtureFraction";
 
   /*--- auxiliary species transport equations---*/
   for (size_t i_aux = 0; i_aux < n_user_scalars; i_aux++) {
@@ -83,14 +86,26 @@ void CFluidFlamelet::SetTDState_T(su2double val_temperature, const su2double* va
   Mu = val_vars_TD[LOOKUP_TD::VISCOSITY];
   Kt = val_vars_TD[LOOKUP_TD::CONDUCTIVITY];
   mass_diffusivity = val_vars_TD[LOOKUP_TD::DIFFUSIONCOEFFICIENT];
-  molar_weight = val_vars_TD[LOOKUP_TD::MOLARWEIGHT];
-  Density = Pressure / (molar_weight * UNIVERSAL_GAS_CONSTANT * Temperature);
+  switch (density_model)
+  {
+  case INC_DENSITYMODEL::FLAMELET:
+    Density = val_vars_TD[LOOKUP_TD::MOLARWEIGHT];
+    molar_weight = Pressure / (Density * UNIVERSAL_GAS_CONSTANT * Temperature);
+    break;
+  case INC_DENSITYMODEL::VARIABLE:
+    molar_weight = val_vars_TD[LOOKUP_TD::MOLARWEIGHT];
+    Density = Pressure / (molar_weight * UNIVERSAL_GAS_CONSTANT * Temperature);
+  default:
+    break;
+  }
 
   /*--- Compute Cv from Cp and molar weight of the mixture (ideal gas). ---*/
   Cv = Cp - UNIVERSAL_GAS_CONSTANT / molar_weight;
 }
 
 void CFluidFlamelet::PreprocessLookUp(CConfig* config) {
+
+  density_model = config->GetKind_DensityModel();
    /*--- Thermodynamic state variables and names. ---*/
   varnames_TD.resize(LOOKUP_TD::SIZE);
   val_vars_TD.resize(LOOKUP_TD::SIZE);
@@ -101,13 +116,25 @@ void CFluidFlamelet::PreprocessLookUp(CConfig* config) {
   varnames_TD[LOOKUP_TD::VISCOSITY] = "ViscosityDyn";
   varnames_TD[LOOKUP_TD::CONDUCTIVITY] = "Conductivity";
   varnames_TD[LOOKUP_TD::DIFFUSIONCOEFFICIENT] = "DiffusionCoefficient";
-  varnames_TD[LOOKUP_TD::MOLARWEIGHT] = "MolarWeightMix";
 
+  /*--- In case of FLAMELET density model, the density is directly interpolated from the manifold.---*/
+  switch (density_model)
+  {
+  case INC_DENSITYMODEL::FLAMELET:
+    varnames_TD[LOOKUP_TD::MOLARWEIGHT] = "Density";
+    break;
+  case INC_DENSITYMODEL::VARIABLE:
+    varnames_TD[LOOKUP_TD::MOLARWEIGHT] = "MolarWeightMix";
+    break;
+  default:
+    break;
+  }
   /*--- Scalar source term variables and names. ---*/
-  size_t n_sources = 1 + 2*n_user_scalars;
+  size_t n_sources = n_control_vars + 2*n_user_scalars;
   varnames_Sources.resize(n_sources);
   val_vars_Sources.resize(n_sources);
-  varnames_Sources[I_SRC_TOT_PROGVAR] = "ProdRateTot_PV";
+  for (auto iCV=0u; iCV<n_control_vars; iCV++)
+    varnames_Sources[iCV] = config->GetControllingVariableSourceName(iCV);
   /*--- No source term for enthalpy ---*/
 
   /*--- For the auxiliary equations, we use a positive (production) and a negative (consumption) term:
@@ -115,8 +142,8 @@ void CFluidFlamelet::PreprocessLookUp(CConfig* config) {
 
   for (size_t i_aux = 0; i_aux < n_user_scalars; i_aux++) {
     /*--- Order of the source terms: S_prod_1, S_cons_1, S_prod_2, S_cons_2, ...---*/
-    varnames_Sources[1 + 2 * i_aux] = config->GetUserSourceName(2 * i_aux);
-    varnames_Sources[1 + 2 * i_aux + 1] = config->GetUserSourceName(2 * i_aux + 1);
+    varnames_Sources[n_control_vars + 2 * i_aux] = config->GetUserSourceName(2 * i_aux);
+    varnames_Sources[n_control_vars + 2 * i_aux + 1] = config->GetUserSourceName(2 * i_aux + 1);
   }
 
   /*--- Passive look-up terms ---*/
@@ -128,7 +155,7 @@ void CFluidFlamelet::PreprocessLookUp(CConfig* config) {
 
 }
 
-unsigned long CFluidFlamelet::EvaluateDataSet(vector<su2double> &input_scalar, FLAMELET_LOOKUP_OPS lookup_type, vector<su2double> &output_refs) {
+unsigned long CFluidFlamelet::EvaluateDataSet(vector<su2double> &input_scalar, unsigned short lookup_type, vector<su2double> &output_refs) {
   su2double val_enth = input_scalar[I_ENTH];
   su2double val_prog = input_scalar[I_PROGVAR];
   su2double val_mixfrac = include_mixture_fraction ? input_scalar[I_MIXFRAC] : 0.0;
@@ -145,7 +172,6 @@ unsigned long CFluidFlamelet::EvaluateDataSet(vector<su2double> &input_scalar, F
   case FLAMELET_LOOKUP_OPS::LOOKUP:
     varnames = varnames_LookUp;
     break;
-  
   default:
     break;
   }
diff --git a/SU2_CFD/src/output/CAdjFlowOutput.cpp b/SU2_CFD/src/output/CAdjFlowOutput.cpp
index 9489926a537..ce9719001f0 100644
--- a/SU2_CFD/src/output/CAdjFlowOutput.cpp
+++ b/SU2_CFD/src/output/CAdjFlowOutput.cpp
@@ -62,10 +62,10 @@ void CAdjFlowOutput::AddHistoryOutputFields_AdjScalarRMS_RES(const CConfig* conf
   }
 
   if (config->GetKind_Species_Model() == SPECIES_MODEL::FLAMELET) {
-
-    AddHistoryOutput("RMS_ADJ_PROGRESS_VARIABLE", "rms[PV]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the adjoint progress variable.", HistoryFieldType::RESIDUAL);
-    AddHistoryOutput("RMS_ADJ_TOTAL_ENTHALPY", "rms[Enth]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the adjoint total enthalpy.", HistoryFieldType::RESIDUAL);
-    
+    for (auto iCV=0u; iCV < config->GetNControlVars(); iCV++) {
+      const auto& cv_name = config->GetControllingVariableName(iCV);
+      AddHistoryOutput("RMS_ADJ_"+cv_name, "rms[" + cv_name + "]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the adjoint " + cv_name, HistoryFieldType::RESIDUAL);
+    }
     for (unsigned short i_scalar = 0; i_scalar < config->GetNUserScalars(); i_scalar++) {
       const auto& scalar_name = config->GetUserScalarName(i_scalar);
       AddHistoryOutput("RMS_ADJ_" + scalar_name, "rms[" + scalar_name + "]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the adjoint of " + scalar_name + " .", HistoryFieldType::RESIDUAL);
@@ -98,10 +98,10 @@ void CAdjFlowOutput::AddHistoryOutputFields_AdjScalarMAX_RES(const CConfig* conf
   }
 
   if (config->GetKind_Species_Model() == SPECIES_MODEL::FLAMELET) {
-
-    AddHistoryOutput("MAX_ADJ_PROGRESS_VARIABLE", "max[PV]",ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the adjoint progress variable.", HistoryFieldType::RESIDUAL);
-    AddHistoryOutput("MAX_ADJ_TOTAL_ENTHALPY", "max[Enth]",ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the adjoint total enthalpy.", HistoryFieldType::RESIDUAL);
-    
+    for (auto iCV=0u; iCV < config->GetNControlVars(); iCV++) {
+      const auto& cv_name = config->GetControllingVariableName(iCV);
+      AddHistoryOutput("MAX_ADJ_" + cv_name, "max["+cv_name +"]", ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the adjoint " + cv_name, HistoryFieldType::RESIDUAL);
+    }
     for (unsigned short i_scalar = 0; i_scalar < config->GetNUserScalars(); i_scalar++) {
       const auto& scalar_name = config->GetUserScalarName(i_scalar);
       AddHistoryOutput("MAX_ADJ_" + scalar_name, "max[scalar_" + scalar_name + "]",ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the adjoint of " + scalar_name + " .", HistoryFieldType::RESIDUAL);
@@ -136,9 +136,10 @@ void CAdjFlowOutput::AddHistoryOutputFields_AdjScalarBGS_RES(const CConfig* conf
   }
 
   if (config->GetKind_Species_Model() == SPECIES_MODEL::FLAMELET) {
-
-    AddHistoryOutput("BGS_ADJ_PROGRESS_VARIABLE", "bgs[PV]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the adjoint progress variable.", HistoryFieldType::RESIDUAL);
-    AddHistoryOutput("BGS_ADJ_TOTAL_ENTHALPY", "bgs[Enth]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the adjoint total enthalpy.", HistoryFieldType::RESIDUAL);
+    for (auto iCV=0u; iCV < config->GetNControlVars(); iCV++) {
+      const auto& cv_name = config->GetControllingVariableName(iCV);
+      AddHistoryOutput("BGS_ADJ_" + cv_name, "bgs[" + cv_name + "]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the adjoint " + cv_name, HistoryFieldType::RESIDUAL);
+    }
 
     for (unsigned short i_scalar = 0; i_scalar < config->GetNUserScalars(); i_scalar++) {
       const auto& scalar_name = config->GetUserScalarName(i_scalar);
@@ -212,14 +213,12 @@ void CAdjFlowOutput::LoadHistoryDataAdjScalar(const CConfig* config, const CSolv
   }
 
   if (config->GetKind_Species_Model() == SPECIES_MODEL::FLAMELET) {
-
-      SetHistoryOutputValue("RMS_ADJ_PROGRESS_VARIABLE", log10(adjspecies_solver->GetRes_RMS(I_PROGVAR)));
-      SetHistoryOutputValue("MAX_ADJ_PROGRESS_VARIABLE", log10(adjspecies_solver->GetRes_Max(I_PROGVAR)));
-      SetHistoryOutputValue("RMS_ADJ_TOTAL_ENTHALPY", log10(adjspecies_solver->GetRes_RMS(I_ENTH)));
-      SetHistoryOutputValue("MAX_ADJ_TOTAL_ENTHALPY", log10(adjspecies_solver->GetRes_Max(I_ENTH)));
-      if (multiZone) {
-        SetHistoryOutputValue("BGS_ADJ_PROGRESS_VARIABLE", log10(adjspecies_solver->GetRes_BGS(I_PROGVAR)));
-        SetHistoryOutputValue("BGS_ADJ_TOTAL_ENTHALPY", log10(adjspecies_solver->GetRes_BGS(I_ENTH)));
+      for (auto iCV=0u; iCV < config->GetNControlVars(); iCV++) {
+        const auto& cv_name = config->GetControllingVariableName(iCV);
+        SetHistoryOutputValue("RMS_ADJ_"+cv_name, log10(adjspecies_solver->GetRes_RMS(iCV)));
+        SetHistoryOutputValue("MAX_ADJ_"+cv_name, log10(adjspecies_solver->GetRes_Max(iCV)));
+        if (multiZone)
+          SetHistoryOutputValue("BGS_ADJ_" + cv_name, log10(adjspecies_solver->GetRes_BGS(iCV)));
       }
 
     for (unsigned short i_scalar = 0; i_scalar < config->GetNUserScalars(); i_scalar++) {
@@ -264,9 +263,10 @@ void CAdjFlowOutput::SetVolumeOutputFieldsAdjScalarSolution(const CConfig* confi
   }
 
   if (config->GetKind_Species_Model() == SPECIES_MODEL::FLAMELET) {
-
-    AddVolumeOutput("ADJ_PROGRESS_VARIABLE", "Adjoint_Progress_Variable", "SOLUTION", "Adjoint of the progress variable.");
-    AddVolumeOutput("ADJ_TOTAL_ENTHALPY", "Adjoint_Total_Enthalpy", "SOLUTION", "Adjoint of the total enthalphy.");
+    for (auto iCV=0u; iCV < config->GetNControlVars(); iCV++) {
+      const auto& cv_name = config->GetControllingVariableName(iCV);
+      AddVolumeOutput("ADJ_" + cv_name, "Adjoint_" + cv_name, "SOLUTION", "Adjoint of the " + cv_name + " controlling variable.");
+    }
 
     for (unsigned short i_scalar = 0; i_scalar < config->GetNUserScalars(); i_scalar++) {
       const auto& scalar_name = config->GetUserScalarName(i_scalar);
@@ -304,10 +304,10 @@ void CAdjFlowOutput::SetVolumeOutputFieldsAdjScalarResidual(const CConfig* confi
   }
 
   if (config->GetKind_Species_Model() == SPECIES_MODEL::FLAMELET) {
-
-    AddVolumeOutput("RES_ADJ_PROGRESS_VARIABLE", "Residual_Adjoint_Progress_Variable", "RESIDUAL", "Residual of the adjoint of the progress variable");
-    AddVolumeOutput("RES_ADJ_TOTAL_ENTHALPY", "Residual_Adjoint_Total_Enthalpy", "RESIDUAL", "Residual of the adjoint of the total enthalpy");
-
+    for(auto iCV=0u; iCV < config->GetNControlVars(); iCV) {
+      const auto& cv_name = config->GetControllingVariableName(iCV);
+      AddVolumeOutput("RES_ADJ_" + cv_name, "Residual_Adjoint_" + cv_name, "RESIDUAL", "Residual of the adjoint of the " + cv_name + " controlling variable.");
+    }
     for (unsigned short i_scalar = 0; i_scalar < config->GetNUserScalars(); i_scalar++) {
       const auto& scalar_name = config->GetUserScalarName(i_scalar);
       AddVolumeOutput("RES_ADJ_" + scalar_name, "Residual_Adjoint_" + scalar_name, "RESIDUAL", "Residual of the adjoint of " + scalar_name);
@@ -352,15 +352,15 @@ void CAdjFlowOutput::LoadVolumeDataAdjScalar(const CConfig* config, const CSolve
 
   if (config->GetKind_Species_Model() == SPECIES_MODEL::FLAMELET) {
 
-      SetVolumeOutputValue("ADJ_PROGRESS_VARIABLE", iPoint, Node_AdjSpecies->GetSolution(iPoint, I_PROGVAR));
-      SetVolumeOutputValue("RES_ADJ_PROGRESS_VARIABLE", iPoint, Node_AdjSpecies->GetSolution(iPoint, I_PROGVAR) - Node_AdjSpecies->GetSolution_Old(iPoint, I_PROGVAR));
-      SetVolumeOutputValue("ADJ_TOTAL_ENTHALPY", iPoint, Node_AdjSpecies->GetSolution(iPoint, I_ENTH));
-      SetVolumeOutputValue("RES_ADJ_TOTAL_ENTHALPY", iPoint, Node_AdjSpecies->GetSolution(iPoint, I_ENTH) - Node_AdjSpecies->GetSolution_Old(iPoint, I_ENTH));
-
+    for (auto iCV=0u; iCV < config->GetNControlVars(); iCV++) {
+      const auto& cv_name = config->GetControllingVariableName(iCV);
+      SetVolumeOutputValue("ADJ_" + cv_name, iPoint, Node_AdjSpecies->GetSolution(iPoint, iCV));
+      SetVolumeOutputValue("RES_ADJ_" + cv_name, iPoint, Node_AdjSpecies->GetSolution(iPoint, iCV) - Node_AdjSpecies->GetSolution_Old(iPoint, iCV))
+    }
     for (unsigned short i_scalar = 0; i_scalar < config->GetNUserScalars(); i_scalar++) {
       const auto& scalar_name = config->GetUserScalarName(i_scalar);
-      SetVolumeOutputValue("ADJ_" + scalar_name, iPoint, Node_AdjSpecies->GetSolution(iPoint, 2 + i_scalar));
-      SetVolumeOutputValue("RES_ADJ_" + scalar_name, iPoint, Node_AdjSpecies->GetSolution(iPoint, 2 + i_scalar) - Node_AdjSpecies->GetSolution_Old(iPoint, 2 + i_scalar));
+      SetVolumeOutputValue("ADJ_" + scalar_name, iPoint, Node_AdjSpecies->GetSolution(iPoint, config->GetNControlVars() + i_scalar));
+      SetVolumeOutputValue("RES_ADJ_" + scalar_name, iPoint, Node_AdjSpecies->GetSolution(iPoint, config->GetNControlVars() + i_scalar) - Node_AdjSpecies->GetSolution_Old(iPoint, config->GetNControlVars() + i_scalar));
     }
   }
 
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index 56461b534a3..18cace9294c 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -995,11 +995,12 @@ void CFlowOutput::AddHistoryOutputFields_ScalarRMS_RES(const CConfig* config) {
       break;
     }
     case SPECIES_MODEL::FLAMELET: {
-      AddHistoryOutput("RMS_PROGRESS_VARIABLE", "rms[PV]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the progress variable equation.", HistoryFieldType::RESIDUAL);
-      AddHistoryOutput("RMS_TOTAL_ENTHALPY", "rms[Enth]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the total enthalpy equation.", HistoryFieldType::RESIDUAL);
-      if (include_mixfrac)
-        AddHistoryOutput("RMS_MIXTURE_FRACTION", "rms[Mixfrac]", ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean square residual of the mixture fraction equation.", HistoryFieldType::RESIDUAL);
-      
+      /*--- Controlling variable transport. ---*/
+      for (auto iCV = 0u; iCV < config->GetNControlVars(); iCV++){
+        const auto& CV_name = config->GetControllingVariableName(iCV);
+        AddHistoryOutput("RMS_"+CV_name, "rms["+CV_name+"]",ScreenOutputFormat::FIXED, "RMS_RES", "Root-mean squared residual of " + CV_name + " controlling variable equation.", HistoryFieldType::RESIDUAL);
+      }
+
       /*--- auxiliary species transport ---*/
       for (auto i_scalar = 0u; i_scalar < config->GetNUserScalars(); i_scalar++){
         const auto& scalar_name = config->GetUserScalarName(i_scalar);
@@ -1052,11 +1053,12 @@ void CFlowOutput::AddHistoryOutputFields_ScalarMAX_RES(const CConfig* config) {
       break;
     }
     case SPECIES_MODEL::FLAMELET: {
-      AddHistoryOutput("MAX_PROGRESS_VARIABLE", "max[PV]", ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the progress variable equation.", HistoryFieldType::RESIDUAL);
-      AddHistoryOutput("MAX_TOTAL_ENTHALPY", "max[Enth]", ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the total enthalpy equation.", HistoryFieldType::RESIDUAL);
-      if (include_mixfrac) 
-        AddHistoryOutput("MAX_MIXTURE_FRACTION", "max[Mixfrac]", ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the mixture fraction equation.", HistoryFieldType::RESIDUAL);
-      
+      /*--- Controlling variable transport. ---*/
+      for (auto iCV=0u; iCV < config->GetNControlVars(); iCV++){
+        const auto& cv_name = config->GetControllingVariableName(iCV);
+        AddHistoryOutput("MAX_" + cv_name, "max[" + cv_name + "]", ScreenOutputFormat::FIXED, "MAX_RES", "Maximum residual of the " + cv_name + " equation.", HistoryFieldType::RESIDUAL);
+      }
+
       /*--- auxiliary species transport ---*/
       for (auto i_scalar = 0u; i_scalar < config->GetNUserScalars(); i_scalar++){
         const auto& scalar_name = config->GetUserScalarName(i_scalar);
@@ -1107,11 +1109,12 @@ void CFlowOutput::AddHistoryOutputFields_ScalarBGS_RES(const CConfig* config) {
       break;
     }
     case SPECIES_MODEL::FLAMELET: {
-      AddHistoryOutput("BGS_PROGRESS_VARIABLE", "bgs[PV]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the progress variable equation.", HistoryFieldType::RESIDUAL);
-      AddHistoryOutput("BGS_TOTAL_ENTHALPY", "bgs[Enth]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the total enthalpy equation.", HistoryFieldType::RESIDUAL);
-      if (include_mixfrac)
-        AddHistoryOutput("BGS_MIXTURE_FRACTION", "bgs[Mixfrac]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the mixture fraction equation.", HistoryFieldType::RESIDUAL);
-      
+      /*--- Controlling variable transport. ---*/
+      for (auto iCV=0u; iCV < config->GetNControlVars(); iCV++){
+        const auto& cv_name = config->GetControllingVariableName(iCV);
+        AddHistoryOutput("BGS_" + cv_name, "bgs[" + cv_name + "]", ScreenOutputFormat::FIXED, "BGS_RES", "BGS residual of the " + cv_name + " controlling variable equation.", HistoryFieldType::RESIDUAL);
+      }
+
       /*--- auxiliary species transport ---*/
       for (auto i_scalar = 0u; i_scalar < config->GetNUserScalars(); i_scalar++){
         const auto& scalar_name = config->GetUserScalarName(i_scalar);
@@ -1213,13 +1216,11 @@ void CFlowOutput::LoadHistoryDataScalar(const CConfig* config, const CSolver* co
     }
 
     case SPECIES_MODEL::FLAMELET: {
-      SetHistoryOutputValue("RMS_PROGRESS_VARIABLE", log10(solver[SPECIES_SOL]->GetRes_RMS(I_PROGVAR)));
-      SetHistoryOutputValue("MAX_PROGRESS_VARIABLE", log10(solver[SPECIES_SOL]->GetRes_Max(I_PROGVAR)));
-      SetHistoryOutputValue("RMS_TOTAL_ENTHALPY", log10(solver[SPECIES_SOL]->GetRes_RMS(I_ENTH)));
-      SetHistoryOutputValue("MAX_TOTAL_ENTHALPY", log10(solver[SPECIES_SOL]->GetRes_Max(I_ENTH)));
-      if (include_mixfrac) {
-        SetHistoryOutputValue("RMS_MIXTURE_FRACTION", log10(solver[SPECIES_SOL]->GetRes_RMS(I_MIXFRAC)));
-        SetHistoryOutputValue("MAX_MIXTURE_FRACTION", log10(solver[SPECIES_SOL]->GetRes_Max(I_MIXFRAC)));
+      /*--- Controlling variable transport. ---*/
+      for (auto iCV=0u; iCV < config->GetNControlVars(); iCV++){
+        const auto& cv_name = config->GetControllingVariableName(iCV);
+        SetHistoryOutputValue("RMS_" + cv_name, log10(solver[SPECIES_SOL]->GetRes_RMS(iCV)));
+        SetHistoryOutputValue("MAX_" + cv_name, log10(solver[SPECIES_SOL]->GetRes_Max(iCV)));
       }
       /*--- auxiliary species transport ---*/
       for (unsigned short iReactant=0; iReactant<config->GetNUserScalars(); iReactant++){
@@ -1276,12 +1277,13 @@ void CFlowOutput::SetVolumeOutputFieldsScalarSolution(const CConfig* config){
       }
       break;
     case SPECIES_MODEL::FLAMELET:
-      AddVolumeOutput("PROGVAR", "Progress_Variable", "SOLUTION", "Progress variable");
-      AddVolumeOutput("ENTHALPY", "Total_Enthalpy", "SOLUTION", "Total enthalpy");
-      if (include_mixfrac)
-        AddVolumeOutput("MIXTURE_FRACTION", "Mixture_Fraction", "SOLUTION", "Mixture fraction");
+      /*--- Controlling variables. ---*/
+      for (auto iCV=0u; iCV<config->GetNControlVars(); iCV++) {
+        const auto& cv_name = config->GetControllingVariableName(iCV);
+        AddVolumeOutput(cv_name, cv_name, "SOLUTION", cv_name + " solution.");
+      }
       /*--- auxiliary species ---*/
-      for (unsigned short iReactant=0; iReactant<config->GetNUserScalars(); iReactant++) {
+      for (auto iReactant=0u; iReactant<config->GetNUserScalars(); iReactant++) {
         const auto& species_name = config->GetUserScalarName(iReactant);
         AddVolumeOutput(species_name, species_name, "SOLUTION", species_name + "Mass fraction solution");
       }
@@ -1317,11 +1319,11 @@ void CFlowOutput::SetVolumeOutputFieldsScalarResidual(const CConfig* config) {
       }
       break;
     case SPECIES_MODEL::FLAMELET:
-      AddVolumeOutput("RES_PROGVAR", "Residual_Progress_Variable", "RESIDUAL", "Residual of progress variable");
-      AddVolumeOutput("RES_ENTHALPY", "Residual_Total_Enthalpy", "RESIDUAL", "Residual of total enthalpy");
-      if (include_mixfrac) 
-        AddVolumeOutput("RES_MIXFRAC", "Residual_Mixture_Fraction", "RESIDUAL", "Residual of mixture fraction");
-
+      /*--- Residuals for controlling variable transport equations. ---*/
+      for (auto iCV=0u; iCV<config->GetNControlVars(); iCV++) {
+        const auto& cv_name = config->GetControllingVariableName(iCV);
+        AddVolumeOutput("RES_"+cv_name, "Residual_"+cv_name, "RESIDUAL", "Residual of " + cv_name + " controlling variable.");
+      }
       /*--- residuals for auxiliary species transport equations ---*/
       for (unsigned short iReactant=0; iReactant<config->GetNUserScalars(); iReactant++){
         const auto& species_name = config->GetUserScalarName(iReactant);
@@ -1372,18 +1374,18 @@ void CFlowOutput::SetVolumeOutputFieldsScalarLimiter(const CConfig* config) {
           AddVolumeOutput("LIMITER_SPECIES_" + std::to_string(iVar), "Limiter_Species_" + std::to_string(iVar), "LIMITER", "Limiter value of the transported species " + std::to_string(iVar));
       break;
       case SPECIES_MODEL::FLAMELET:
-        AddVolumeOutput("LIMITER_PROGVAR", "Limiter_Progress_Variable", "LIMITER", "Limiter of progress variable");
-        AddVolumeOutput("LIMITER_ENTHALPY", "Limiter_Total_Enthalpy", "LIMITER", "Limiter of total enthalpy");
-        if (include_mixfrac)
-          AddVolumeOutput("LIMITER_MIXFRAC", "Limiter_Mixture_Fraction", "LIMITER", "Limiter of mixture fraction");
-
+        /*--- Limiter for controlling variables transport. ---*/
+        for (auto iCV=0u; iCV < config->GetNControlVars(); iCV++) {
+          const auto& cv_name = config->GetControllingVariableName(iCV);
+          AddVolumeOutput("LIMITER_" + cv_name, "Limiter_" + cv_name, "LIMITER", "Limiter of " + cv_name + " controlling variable.");
+        }
         /*--- limiter for auxiliary species transport ---*/
         for (unsigned short iReactant=0; iReactant < config->GetNUserScalars(); iReactant++) {
           const auto& species_name = config->GetUserScalarName(iReactant);
           AddVolumeOutput("LIMITER_" + species_name, "LIMITER_" + species_name, "LIMITER", "Limiter value for the " + species_name + " equation");
         }
       break;
-      case SPECIES_MODEL::NONE:
+      default:
         break;
     }
   }
@@ -1398,9 +1400,7 @@ void CFlowOutput::SetVolumeOutputFieldsScalarPrimitive(const CConfig* config) {
         AddVolumeOutput("DIFFUSIVITY_" + std::to_string(iVar), "Diffusivity_" + std::to_string(iVar), "PRIMITIVE", "Diffusivity of the transported species " + std::to_string(iVar));
       }
       break;
-    case SPECIES_MODEL::FLAMELET:
-      break;
-    case SPECIES_MODEL::NONE:
+    default:
       break;
   }
 
@@ -1425,18 +1425,20 @@ void CFlowOutput::SetVolumeOutputFieldsScalarSource(const CConfig* config) {
   /*--- Only place outputs of the "SOURCE" group for scalar transport here. ---*/
 
   switch (config->GetKind_Species_Model()) {
-    case SPECIES_MODEL::SPECIES_TRANSPORT:
-      break;
     case SPECIES_MODEL::FLAMELET:
-      AddVolumeOutput("SOURCE_PROGVAR", "Source_Progress_Variable", "SOURCE", "Source Progress Variable");
+      for (auto iCV=0u; iCV < config->GetNControlVars(); iCV++) {
+        const auto& cv_name = config->GetControllingVariableName(iCV);
+        if (cv_name.compare("NULL") != 0)
+          AddVolumeOutput("SOURCE_"+cv_name, "Source_" + cv_name, "SOURCE", "Source " + cv_name);
+      }
       /*--- no source term for enthalpy ---*/
       /*--- auxiliary species source terms ---*/
-      for (unsigned short iReactant=0; iReactant<config->GetNUserScalars(); iReactant++) {
+      for (auto iReactant=0u; iReactant<config->GetNUserScalars(); iReactant++) {
         const auto& species_name = config->GetUserScalarName(iReactant);
         AddVolumeOutput("SOURCE_" + species_name, "Source_" + species_name, "SOURCE", "Source " + species_name);
       }
       break;
-    case SPECIES_MODEL::NONE:
+    default:
       break;
   }
 }
@@ -1446,17 +1448,14 @@ void CFlowOutput::SetVolumeOutputFieldsScalarLookup(const CConfig* config) {
   /*--- Only place outputs of the "LOOKUP" group for scalar transport here. ---*/
 
   switch (config->GetKind_Species_Model()) {
-    case SPECIES_MODEL::SPECIES_TRANSPORT:
-      break;
     case SPECIES_MODEL::FLAMELET:
-      for (int i_lookup = 0; i_lookup < config->GetNLookups(); ++i_lookup) {
+      for (auto i_lookup = 0u; i_lookup < config->GetNLookups(); ++i_lookup) {
         string strname1 = "lookup_" + config->GetLUTLookupName(i_lookup);
         AddVolumeOutput(config->GetLUTLookupName(i_lookup), strname1,"LOOKUP", config->GetLUTLookupName(i_lookup));
       }
-
       AddVolumeOutput("TABLE_MISSES"       , "Table_misses"       , "LOOKUP", "Lookup table misses");
       break;
-    case SPECIES_MODEL::NONE:
+    default:
       break;
   }
 }
@@ -1577,15 +1576,14 @@ void CFlowOutput::LoadVolumeDataScalar(const CConfig* config, const CSolver* con
     case SPECIES_MODEL::FLAMELET: {
       const auto Node_Species = solver[SPECIES_SOL]->GetNodes();
 
-      SetVolumeOutputValue("PROGVAR", iPoint, Node_Species->GetSolution(iPoint, I_PROGVAR));
-      SetVolumeOutputValue("ENTHALPY", iPoint, Node_Species->GetSolution(iPoint, I_ENTH));
-      SetVolumeOutputValue("SOURCE_PROGVAR", iPoint, Node_Species->GetScalarSources(iPoint)[I_PROGVAR]);
-      SetVolumeOutputValue("RES_PROGVAR", iPoint, solver[SPECIES_SOL]->LinSysRes(iPoint, I_PROGVAR));
-      SetVolumeOutputValue("RES_ENTHALPY", iPoint, solver[SPECIES_SOL]->LinSysRes(iPoint, I_ENTH));
-      SetVolumeOutputValue("TABLE_MISSES", iPoint, su2double(Node_Species->GetTableMisses(iPoint)));
-      if (include_mixfrac) {
-        SetVolumeOutputValue("MIXTURE_FRACTION", iPoint, Node_Species->GetSolution(iPoint, I_MIXFRAC));
-        SetVolumeOutputValue("RES_MIXFRAC", iPoint, solver[SPECIES_SOL]->LinSysRes(iPoint, I_MIXFRAC));
+      /*--- Controlling variables transport equations. ---*/
+      for (auto iCV=0u; iCV < config->GetNControlVars(); iCV++) {
+        const auto& cv_name = config->GetControllingVariableName(iCV);
+        SetVolumeOutputValue(cv_name, iPoint, Node_Species->GetSolution(iPoint, iCV));
+        SetVolumeOutputValue("RES_" + cv_name, iPoint, solver[SPECIES_SOL]->LinSysRes(iPoint, iCV));
+        const auto& source_name = config->GetControllingVariableSourceName(iCV);
+        if (source_name.compare("NULL") != 0)
+          SetVolumeOutputValue("SOURCE_" + cv_name, iPoint, Node_Species->GetScalarSources(iPoint)[iCV]);
       }
       /*--- auxiliary species transport equations ---*/
       for (unsigned short i_scalar=0; i_scalar<config->GetNUserScalars(); i_scalar++) {
@@ -1596,11 +1594,11 @@ void CFlowOutput::LoadVolumeDataScalar(const CConfig* config, const CSolver* con
       }
 
       if (config->GetKind_SlopeLimit_Species() != LIMITER::NONE) {
-        SetVolumeOutputValue("LIMITER_PROGVAR", iPoint, Node_Species->GetLimiter(iPoint, I_PROGVAR));
-        SetVolumeOutputValue("LIMITER_ENTHALPY", iPoint, Node_Species->GetLimiter(iPoint, I_ENTH));
-        if (include_mixfrac) 
-          SetVolumeOutputValue("LIMITER_MIXFRAC", iPoint, Node_Species->GetLimiter(iPoint, I_MIXFRAC));
-          
+        /*--- Limiter for controlling variable transport equations. ---*/
+        for (auto iCV=0u; iCV<config->GetNControlVars(); iCV++) {
+          const auto& cv_name = config->GetControllingVariableName(iCV);
+          SetVolumeOutputValue("LIMITER_" + cv_name, iPoint, Node_Species->GetLimiter(iPoint, iCV));
+        }
         /*--- limiter for auxiliary species transport equations ---*/
         for (unsigned short i_scalar=0; i_scalar<config->GetNUserScalars(); i_scalar++) {
           const auto& scalar_name = config->GetUserScalarName(i_scalar);
@@ -1614,6 +1612,8 @@ void CFlowOutput::LoadVolumeDataScalar(const CConfig* config, const CSolver* con
           SetVolumeOutputValue(config->GetLUTLookupName(i_lookup), iPoint, Node_Species->GetScalarLookups(iPoint)[i_lookup]);
       }
 
+      SetVolumeOutputValue("TABLE_MISSES", iPoint, Node_Species->GetTableMisses(iPoint));
+
       break;
     }
     case SPECIES_MODEL::NONE: break;
diff --git a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
index 8d2e8e1d626..6b3e5bdc418 100644
--- a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
+++ b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
@@ -97,6 +97,7 @@ void CSpeciesFlameletSolver::Preprocessing(CGeometry* geometry, CSolver** solver
 
     /*--- Compute total source terms from the production and consumption. ---*/
     unsigned long misses = SetScalarSources(config, fluid_model_local, i_point, scalars_vector);
+    nodes->SetTableMisses(i_point, misses);
 
     /*--- Obtain passive look-up scalars. ---*/
     SetScalarLookUps(config, fluid_model_local, i_point, scalars_vector);
@@ -142,9 +143,10 @@ void CSpeciesFlameletSolver::SetInitialCondition(CGeometry** geometry, CSolver**
 
     if (rank == MASTER_NODE) {
       cout << "initial condition: T = " << temp_inlet << endl;
-      cout << "initial condition: c = " << prog_inlet << endl;
-      cout << "initial condition: h = " << enth_inlet << endl;
-      if (include_mixture_fraction) cout << "initial condition: Z = " << mixfrac_inlet << endl;
+      for (auto iCV=0u; iCV < config->GetNControlVars(); iCV++) {
+        const auto& cv_name = config->GetControllingVariableName(iCV);
+        cout << "initial condition: " << cv_name << " = " << config->GetSpecies_Init()[iCV] << endl;
+      }
     }
 
     CFluidModel* fluid_model_local;
@@ -447,16 +449,15 @@ unsigned long CSpeciesFlameletSolver::SetScalarSources(CConfig* config, CFluidMo
                                                        unsigned long iPoint, vector<su2double>& scalars) {
   /*--- Compute total source terms from the production and consumption. ---*/
 
-  vector<su2double> table_sources(1 + 2*config->GetNUserScalars());
+  vector<su2double> table_sources(config->GetNControlVars() + 2*config->GetNUserScalars());
   unsigned long misses = fluid_model_local->EvaluateDataSet(scalars, FLAMELET_LOOKUP_OPS::SOURCES, table_sources);
   nodes->SetTableMisses(iPoint, misses);
 
   /*--- The source term for progress variable is always positive, we clip from below to makes sure. --- */
 
   vector<su2double> source_scalar(config->GetNScalars());
-  source_scalar[I_PROGVAR] = fmax(EPS, table_sources[I_SRC_TOT_PROGVAR]);
-  source_scalar[I_ENTH] = 0.0;
-  if (include_mixture_fraction) source_scalar[I_MIXFRAC] = 0.0;
+  for (auto iCV=0u; iCV<config->GetNControlVars(); iCV++)
+    source_scalar[iCV] = table_sources[iCV];
 
   /*--- Source term for the auxiliary species transport equations. ---*/
   for (size_t i_aux = 0; i_aux < config->GetNUserScalars(); i_aux++) {
diff --git a/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg b/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg
index 55ef51919de..f6f9beccf39 100644
--- a/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg
+++ b/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg
@@ -28,6 +28,8 @@ INC_NONDIM= DIMENSIONAL
 %
 FLUID_MODEL= FLUID_FLAMELET
 FILENAME_LUT= fgm_ch4.drg
+CONTROLLING_VARIABLE_NAMES= ("ProgressVariable", "EnthalpyTot")
+CONTROLLING_VARIABLE_SOURCE_NAMES = ("ProdRateTot_PV", "NULL")
 %
 % -------------------- SCALAR TRANSPORT ---------------------------------------%
 %
diff --git a/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg
index 884dd859268..e2201f1c20e 100644
--- a/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg
+++ b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg
@@ -38,6 +38,9 @@ INC_NONDIM= DIMENSIONAL
 %
 FLUID_MODEL= FLUID_FLAMELET
 FILENAME_LUT= fgm_ch4.drg
+CONTROLLING_VARIABLE_NAMES= ("ProgressVariable", "EnthalpyTot")
+CONTROLLING_VARIABLE_SOURCE_NAMES= ("ProdRateTot_PV", "NULL")
+
 CONDUCTIVITY_MODEL= FLAMELET
 DIFFUSIVITY_MODEL= FLAMELET
 KIND_SCALAR_MODEL= FLAMELET
diff --git a/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg
index 14266a33b58..1a36d71128d 100644
--- a/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg
+++ b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg
@@ -39,6 +39,8 @@ INC_NONDIM= DIMENSIONAL
 %
 FLUID_MODEL= FLUID_FLAMELET
 FILENAME_LUT= fgm_ch4.drg
+CONTROLLING_VARIABLE_NAMES= ("ProgressVariable", "EnthalpyTot")
+CONTROLLING_VARIABLE_SOURCE_NAMES= ("ProdRateTot_PV", "NULL")
 CONDUCTIVITY_MODEL= FLAMELET
 DIFFUSIVITY_MODEL= FLAMELET
 KIND_SCALAR_MODEL= FLAMELET
diff --git a/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg b/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg
index aff2d5561a8..c1e0ef8bd8b 100644
--- a/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg
+++ b/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg
@@ -53,6 +53,8 @@ INC_NONDIM= DIMENSIONAL
 
 FLUID_MODEL= FLUID_FLAMELET
 FILENAME_LUT= fgm_ch4.drg
+CONTROLLING_VARIABLE_NAMES= ("ProgressVariable", "EnthalpyTot")
+CONTROLLING_VARIABLE_SOURCE_NAMES= ("ProdRateTot_PV", "NULL")
 FLAME_INIT= (0.004, 0.0, 0.0, 1.0, 0.0, 0.0, 0.2e-3, 1.0)
 
 % -------------------- SPECIES TRANSPORT ---------------------------------------%
diff --git a/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg b/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg
index b100aa3fcb3..73988c0df47 100644
--- a/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg
+++ b/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg
@@ -55,6 +55,8 @@ INC_NONDIM= DIMENSIONAL
 
 FLUID_MODEL= FLUID_FLAMELET
 FILENAME_LUT= fgm_ch4.drg
+CONTROLLING_VARIABLE_NAMES= ("ProgressVariable", "EnthalpyTot")
+CONTROLLING_VARIABLE_SOURCE_NAMES= ("ProdRateTot_PV", "NULL")
 FLAME_INIT= (0.004, 0.0, 0.0, 1, 0, 0, 0.2e-3, 1)
 
 % -------------------- SPECIES TRANSPORT ---------------------------------------%
diff --git a/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg b/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg
index 6fa6662e253..2fe94fc0f2c 100644
--- a/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg
+++ b/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg
@@ -31,6 +31,8 @@ AXISYMMETRIC= YES
 %
 FLUID_MODEL= FLUID_FLAMELET
 FILENAME_LUT= fgm_ch4.drg
+CONTROLLING_VARIABLE_NAMES= ("ProgressVariable", "EnthalpyTot")
+CONTROLLING_VARIABLE_SOURCE_NAMES= ("ProdRateTot_PV", "NULL")
 %
 % -------------------- SCALAR TRANSPORT ---------------------------------------%
 %
diff --git a/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_premixed_ch4_cfd.cfg b/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_premixed_ch4_cfd.cfg
index 7856575d99f..8a40f4eda09 100644
--- a/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_premixed_ch4_cfd.cfg
+++ b/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_premixed_ch4_cfd.cfg
@@ -28,6 +28,8 @@ INC_NONDIM= DIMENSIONAL
 %
 FLUID_MODEL= FLUID_FLAMELET
 FILENAME_LUT= LUT_methane_PD.drg
+CONTROLLING_VARIABLE_NAMES= ("ProgressVariable", "EnthalpyTot","MixtureFraction")
+CONTROLLING_VARIABLE_SOURCE_NAMES= ("ProdRateTot_PV", "NULL", "NULL")
 
 OBJECTIVE_FUNCTION= CUSTOM_OBJFUNC
 OBJECTIVE_WEIGHT= 1.0

From 96c64ceda94fbf44b8f1e4715d23abbe4e45de92 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 20 Jun 2023 21:16:08 +0200
Subject: [PATCH 497/656] Bug fixes

---
 SU2_CFD/src/output/CAdjFlowOutput.cpp          | 2 +-
 SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp | 4 ++--
 2 files changed, 3 insertions(+), 3 deletions(-)

diff --git a/SU2_CFD/src/output/CAdjFlowOutput.cpp b/SU2_CFD/src/output/CAdjFlowOutput.cpp
index ce9719001f0..f47995baee4 100644
--- a/SU2_CFD/src/output/CAdjFlowOutput.cpp
+++ b/SU2_CFD/src/output/CAdjFlowOutput.cpp
@@ -355,7 +355,7 @@ void CAdjFlowOutput::LoadVolumeDataAdjScalar(const CConfig* config, const CSolve
     for (auto iCV=0u; iCV < config->GetNControlVars(); iCV++) {
       const auto& cv_name = config->GetControllingVariableName(iCV);
       SetVolumeOutputValue("ADJ_" + cv_name, iPoint, Node_AdjSpecies->GetSolution(iPoint, iCV));
-      SetVolumeOutputValue("RES_ADJ_" + cv_name, iPoint, Node_AdjSpecies->GetSolution(iPoint, iCV) - Node_AdjSpecies->GetSolution_Old(iPoint, iCV))
+      SetVolumeOutputValue("RES_ADJ_" + cv_name, iPoint, Node_AdjSpecies->GetSolution(iPoint, iCV) - Node_AdjSpecies->GetSolution_Old(iPoint, iCV));
     }
     for (unsigned short i_scalar = 0; i_scalar < config->GetNUserScalars(); i_scalar++) {
       const auto& scalar_name = config->GetUserScalarName(i_scalar);
diff --git a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
index 6b3e5bdc418..33bcf5d7818 100644
--- a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
+++ b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
@@ -464,8 +464,8 @@ unsigned long CSpeciesFlameletSolver::SetScalarSources(CConfig* config, CFluidMo
     /*--- The source term for the auxiliary equations consists of a production term and a consumption term:
           S_TOT = S_PROD + S_CONS * Y ---*/
     su2double y_aux = scalars[config->GetNControlVars() + i_aux];
-    su2double source_prod = table_sources[1 + 2 * i_aux];
-    su2double source_cons = table_sources[1 + 2 * i_aux + 1];
+    su2double source_prod = table_sources[config->GetNControlVars() + 2 * i_aux];
+    su2double source_cons = table_sources[config->GetNControlVars() + 2 * i_aux + 1];
     source_scalar[config->GetNControlVars() + i_aux] = source_prod + source_cons * y_aux;
   }
   for (auto i_scalar = 0u; i_scalar < nVar; i_scalar++)

From 6e57517f448e2c9d226f9e0f0ba88d25b41a0c4e Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 23 Jun 2023 14:31:31 +0200
Subject: [PATCH 498/656] Generalized output for flamelet solver depending on
 controlling variable names

---
 .github/workflows/regression.yml              |  2 +-
 Common/include/containers/CTrapezoidalMap.hpp |  4 +--
 Common/src/containers/CLookUpTable.cpp        |  8 ++---
 Common/src/containers/CTrapezoidalMap.cpp     |  6 ++--
 SU2_CFD/include/fluid/CFluidFlamelet.hpp      |  5 ++-
 SU2_CFD/src/fluid/CFluidFlamelet.cpp          | 13 +++----
 SU2_CFD/src/output/CAdjFlowOutput.cpp         |  4 +--
 SU2_CFD/src/output/CFlowOutput.cpp            | 16 ++++-----
 SU2_CFD/src/solvers/CIncEulerSolver.cpp       |  7 ++--
 .../src/solvers/CSpeciesFlameletSolver.cpp    | 36 ++++++++++++-------
 .../lam_prem_ch4_cfd.cfg                      |  6 ++--
 .../lam_prem_ch4_hx_ad.cfg                    | 14 ++++----
 .../lam_prem_ch4_hx_dot.cfg                   | 10 +++---
 .../lam_prem_ch4_cht_cfd_fluid.cfg            |  6 ++--
 .../lam_prem_ch4_cht_ad_fluid.cfg             |  6 ++--
 .../lam_prem_ch4_cfd_axi.cfg                  |  6 ++--
 ...4_cfd.cfg => lam_partial_prem_ch4_cfd.cfg} | 31 ++++++++--------
 config_template.cfg                           | 10 ++++++
 18 files changed, 102 insertions(+), 88 deletions(-)
 rename TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/{lam_partial_premixed_ch4_cfd.cfg => lam_partial_prem_ch4_cfd.cfg} (82%)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 76545cdb274..126461f884f 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c feature_new_flamelet -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
diff --git a/Common/include/containers/CTrapezoidalMap.hpp b/Common/include/containers/CTrapezoidalMap.hpp
index cbb77b4a70f..c53a09168ce 100644
--- a/Common/include/containers/CTrapezoidalMap.hpp
+++ b/Common/include/containers/CTrapezoidalMap.hpp
@@ -55,13 +55,13 @@ class CTrapezoidalMap {
   su2vector<std::vector<std::pair<su2double, unsigned long> > > y_edge_at_band_mid;
 
   double memory_footprint = 0;
+
  public:
   CTrapezoidalMap() = default;
 
   CTrapezoidalMap(const su2double* samples_x, const su2double* samples_y, const unsigned long size,
                   const std::vector<std::array<unsigned long, 2> >& edges,
-                  const su2vector<std::vector<unsigned long> >& edge_to_triangle,
-                  bool display = false);
+                  const su2vector<std::vector<unsigned long> >& edge_to_triangle, bool display = false);
 
   /*!
    * \brief return the index to the triangle that contains the coordinates (val_x,val_y)
diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index e4b084df3a3..0b3ebb0213d 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -73,12 +73,12 @@ CLookUpTable::CLookUpTable(const string& var_file_name_lut, string name_CV1_in,
   trap_map_x_y.resize(n_table_levels);
   su2double startTime = SU2_MPI::Wtime();
   unsigned short barwidth = 65;
-  bool display_map_info = (n_table_levels < 2); 
+  bool display_map_info = (n_table_levels < 2);
   double tmap_memory_footprint = 0;
   for (auto i_level = 0ul; i_level < n_table_levels; i_level++) {
-    trap_map_x_y[i_level] = CTrapezoidalMap(GetDataP(name_CV1, i_level), GetDataP(name_CV2, i_level),
-                                            table_data[i_level].cols(), edges[i_level], edge_to_triangle[i_level],
-                                            display_map_info);
+    trap_map_x_y[i_level] =
+        CTrapezoidalMap(GetDataP(name_CV1, i_level), GetDataP(name_CV2, i_level), table_data[i_level].cols(),
+                        edges[i_level], edge_to_triangle[i_level], display_map_info);
     tmap_memory_footprint += trap_map_x_y[i_level].GetMemoryFootprint();
     /* Display a progress bar to monitor table generation process */
     if (rank == MASTER_NODE) {
diff --git a/Common/src/containers/CTrapezoidalMap.cpp b/Common/src/containers/CTrapezoidalMap.cpp
index 804c27e8eb6..af3ff86a7e7 100644
--- a/Common/src/containers/CTrapezoidalMap.cpp
+++ b/Common/src/containers/CTrapezoidalMap.cpp
@@ -40,8 +40,7 @@ using namespace std;
  */
 CTrapezoidalMap::CTrapezoidalMap(const su2double* samples_x, const su2double* samples_y, const unsigned long size,
                                  vector<std::array<unsigned long, 2> > const& edges,
-                                 su2vector<vector<unsigned long> > const& val_edge_to_triangle,
-                                 bool display) {
+                                 su2vector<vector<unsigned long> > const& val_edge_to_triangle, bool display) {
   int rank = SU2_MPI::GetRank();
   su2double startTime = SU2_MPI::Wtime();
 
@@ -149,7 +148,8 @@ CTrapezoidalMap::CTrapezoidalMap(const su2double* samples_x, const su2double* sa
     for (unsigned long j_y = 0; j_y < y_edge_at_band_mid[i_y].size(); j_y++)
       size_y_edge_at_band_mid += sizeof(su2double) / 1e6 + sizeof(unsigned long) / 1e6;
 
-  memory_footprint = size_unique_bands + size_edge_limits_x + size_edge_limits_y + size_edge_to_triangle + size_y_edge_at_band_mid;
+  memory_footprint =
+      size_unique_bands + size_edge_limits_x + size_edge_limits_y + size_edge_to_triangle + size_y_edge_at_band_mid;
 
   /* print size of trapezoidal map components to screen */
   if ((rank == MASTER_NODE) && display) {
diff --git a/SU2_CFD/include/fluid/CFluidFlamelet.hpp b/SU2_CFD/include/fluid/CFluidFlamelet.hpp
index 1eb69d4beff..cc402ea0520 100644
--- a/SU2_CFD/include/fluid/CFluidFlamelet.hpp
+++ b/SU2_CFD/include/fluid/CFluidFlamelet.hpp
@@ -36,8 +36,7 @@ class CFluidFlamelet final : public CFluidModel {
 
   int rank;
 
-  bool include_mixture_fraction = false, /*!< \brief include mixture fraction in controlling variables. */ 
-       generate_manifold = false;
+  bool include_mixture_fraction = false; /*!< \brief include mixture fraction in controlling variables. */ 
 
   unsigned short n_scalars, n_lookups, n_user_scalars, /*!< \brief number of passive reactant species. */
       n_control_vars;                                  /*!< \brief number of controlling variables. */
@@ -65,7 +64,7 @@ class CFluidFlamelet final : public CFluidModel {
   void PreprocessLookUp(CConfig* config);
 
  public:
-  CFluidFlamelet(CConfig* config, su2double value_pressure_operating, bool load_manifold = false);
+  CFluidFlamelet(CConfig* config, su2double value_pressure_operating);
 
   ~CFluidFlamelet();
 
diff --git a/SU2_CFD/src/fluid/CFluidFlamelet.cpp b/SU2_CFD/src/fluid/CFluidFlamelet.cpp
index 5a1f7d7301e..feb0244826c 100644
--- a/SU2_CFD/src/fluid/CFluidFlamelet.cpp
+++ b/SU2_CFD/src/fluid/CFluidFlamelet.cpp
@@ -28,7 +28,7 @@
 #include "../include/fluid/CFluidFlamelet.hpp"
 #include "../../../Common/include/containers/CLookUpTable.hpp"
 
-CFluidFlamelet::CFluidFlamelet(CConfig* config, su2double value_pressure_operating, bool load_manifold) : CFluidModel(), generate_manifold(load_manifold) {
+CFluidFlamelet::CFluidFlamelet(CConfig* config, su2double value_pressure_operating) : CFluidModel() {
   rank = SU2_MPI::GetRank();
 
   /* -- number of auxiliary species transport equations, e.g. 1=CO, 2=NOx  --- */
@@ -55,17 +55,12 @@ CFluidFlamelet::CFluidFlamelet(CConfig* config, su2double value_pressure_operati
   for (auto iCV=0u; iCV<n_control_vars; iCV++)
     table_scalar_names[iCV] = config->GetControllingVariableName(iCV);
   
-  // table_scalar_names[I_ENTH] = "EnthalpyTot";
-  // table_scalar_names[I_PROGVAR] = "ProgressVariable";
-  // if (include_mixture_fraction) table_scalar_names[I_MIXFRAC] = "MixtureFraction";
-
   /*--- auxiliary species transport equations---*/
   for (size_t i_aux = 0; i_aux < n_user_scalars; i_aux++) {
     table_scalar_names[n_control_vars + i_aux] = config->GetUserScalarName(i_aux);
   }
-  
-  if (generate_manifold)
-    look_up_table = new CLookUpTable(config->GetFileNameLUT(), table_scalar_names[I_PROGVAR], table_scalar_names[I_ENTH]);
+
+  look_up_table = new CLookUpTable(config->GetFileNameLUT(), table_scalar_names[I_PROGVAR], table_scalar_names[I_ENTH]);
 
   Pressure = value_pressure_operating;
 
@@ -73,7 +68,7 @@ CFluidFlamelet::CFluidFlamelet(CConfig* config, su2double value_pressure_operati
  
 }
 
-CFluidFlamelet::~CFluidFlamelet() { if(generate_manifold) delete look_up_table; }
+CFluidFlamelet::~CFluidFlamelet() { delete look_up_table; }
 
 void CFluidFlamelet::SetTDState_T(su2double val_temperature, const su2double* val_scalars) {
   for (auto iVar = 0u; iVar < n_scalars; iVar++) scalars_vector[iVar] = val_scalars[iVar];
diff --git a/SU2_CFD/src/output/CAdjFlowOutput.cpp b/SU2_CFD/src/output/CAdjFlowOutput.cpp
index f47995baee4..7d61021a8d0 100644
--- a/SU2_CFD/src/output/CAdjFlowOutput.cpp
+++ b/SU2_CFD/src/output/CAdjFlowOutput.cpp
@@ -304,9 +304,9 @@ void CAdjFlowOutput::SetVolumeOutputFieldsAdjScalarResidual(const CConfig* confi
   }
 
   if (config->GetKind_Species_Model() == SPECIES_MODEL::FLAMELET) {
-    for(auto iCV=0u; iCV < config->GetNControlVars(); iCV) {
+    for(auto iCV=0u; iCV < config->GetNControlVars(); iCV++) {
       const auto& cv_name = config->GetControllingVariableName(iCV);
-      AddVolumeOutput("RES_ADJ_" + cv_name, "Residual_Adjoint_" + cv_name, "RESIDUAL", "Residual of the adjoint of the " + cv_name + " controlling variable.");
+      AddVolumeOutput("RES_ADJ_" + cv_name, "Residual_Adjoint_" + cv_name, "RESIDUAL", "Residual of the adjoint of " + cv_name);
     }
     for (unsigned short i_scalar = 0; i_scalar < config->GetNUserScalars(); i_scalar++) {
       const auto& scalar_name = config->GetUserScalarName(i_scalar);
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index 18cace9294c..836262c3fe9 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -958,7 +958,6 @@ void CFlowOutput::SetCustomOutputs(const CSolver* const* solver, const CGeometry
 // The "AddHistoryOutput(" must not be split over multiple lines to ensure proper python parsing
 // clang-format off
 void CFlowOutput::AddHistoryOutputFields_ScalarRMS_RES(const CConfig* config) {
-  const auto include_mixfrac = (config->GetNControlVars() == 3);
 
   switch (TurbModelFamily(config->GetKind_Turb_Model())) {
     case TURB_FAMILY::SA:
@@ -1013,7 +1012,6 @@ void CFlowOutput::AddHistoryOutputFields_ScalarRMS_RES(const CConfig* config) {
 }
 
 void CFlowOutput::AddHistoryOutputFields_ScalarMAX_RES(const CConfig* config) {
-  const auto include_mixfrac = (config->GetNControlVars() == 3);
 
   switch (TurbModelFamily(config->GetKind_Turb_Model())) {
     case TURB_FAMILY::SA:
@@ -1072,7 +1070,6 @@ void CFlowOutput::AddHistoryOutputFields_ScalarMAX_RES(const CConfig* config) {
 
 void CFlowOutput::AddHistoryOutputFields_ScalarBGS_RES(const CConfig* config) {
   if (!multiZone) return;
-  const auto include_mixfrac = (config->GetNControlVars() == 3);
 
   switch (TurbModelFamily(config->GetKind_Turb_Model())) {
     case TURB_FAMILY::SA:
@@ -1154,7 +1151,6 @@ void CFlowOutput::AddHistoryOutputFieldsScalarLinsol(const CConfig* config) {
 // clang-format on
 
 void CFlowOutput::LoadHistoryDataScalar(const CConfig* config, const CSolver* const* solver) {
-  const auto include_mixfrac = (config->GetNControlVars() == 3);
 
   switch (TurbModelFamily(config->GetKind_Turb_Model())) {
     case TURB_FAMILY::SA:
@@ -1243,8 +1239,6 @@ void CFlowOutput::LoadHistoryDataScalar(const CConfig* config, const CSolver* co
 
 void CFlowOutput::SetVolumeOutputFieldsScalarSolution(const CConfig* config){
   /*--- Only place outputs of the "SOLUTION" group here. ---*/
-
-  const auto include_mixfrac = (config->GetNControlVars() == 3);
   
   switch (TurbModelFamily(config->GetKind_Turb_Model())) {
     case TURB_FAMILY::SA:
@@ -1297,7 +1291,6 @@ void CFlowOutput::SetVolumeOutputFieldsScalarSolution(const CConfig* config){
 void CFlowOutput::SetVolumeOutputFieldsScalarResidual(const CConfig* config) {
   /*--- Only place outputs of the "RESIDUAL" group here. ---*/
 
-  const auto include_mixfrac = (config->GetNControlVars() == 3);
   switch (TurbModelFamily(config->GetKind_Turb_Model())){
     case TURB_FAMILY::SA:
       AddVolumeOutput("RES_NU_TILDE", "Residual_Nu_Tilde", "RESIDUAL", "Residual of the Spalart-Allmaras variable");
@@ -1349,7 +1342,6 @@ void CFlowOutput::SetVolumeOutputFieldsScalarResidual(const CConfig* config) {
 void CFlowOutput::SetVolumeOutputFieldsScalarLimiter(const CConfig* config) {
   /*--- Only place outputs of the "SOLUTION" group for species transport here. ---*/
 
-  const auto include_mixfrac = (config->GetNControlVars() == 3);
 
   if (config->GetKind_SlopeLimit_Turb() != LIMITER::NONE) {
     switch (TurbModelFamily(config->GetKind_Turb_Model())) {
@@ -1427,8 +1419,9 @@ void CFlowOutput::SetVolumeOutputFieldsScalarSource(const CConfig* config) {
   switch (config->GetKind_Species_Model()) {
     case SPECIES_MODEL::FLAMELET:
       for (auto iCV=0u; iCV < config->GetNControlVars(); iCV++) {
+        const auto& cv_source_name = config->GetControllingVariableSourceName(iCV);
         const auto& cv_name = config->GetControllingVariableName(iCV);
-        if (cv_name.compare("NULL") != 0)
+        if (cv_source_name.compare("NULL") != 0)
           AddVolumeOutput("SOURCE_"+cv_name, "Source_" + cv_name, "SOURCE", "Source " + cv_name);
       }
       /*--- no source term for enthalpy ---*/
@@ -1493,7 +1486,6 @@ void CFlowOutput::LoadVolumeDataScalar(const CConfig* config, const CSolver* con
   const auto* Node_Turb = (config->GetKind_Turb_Model() != TURB_MODEL::NONE) ? turb_solver->GetNodes() : nullptr;
   const auto* Node_Trans = (config->GetKind_Trans_Model() != TURB_TRANS_MODEL::NONE) ? trans_solver->GetNodes() : nullptr;
   const auto* Node_Geo = geometry->nodes;
-  const auto include_mixfrac = (config->GetNControlVars() == 3);
   
   if (config->GetViscous()) {
     if (nDim == 3){
@@ -3055,6 +3047,10 @@ void CFlowOutput::WriteForcesBreakdown(const CConfig* config, const CSolver* flo
       case INC_DENSITYMODEL::VARIABLE:
         if (energy) file << "Energy equation is active and coupled for variable density.\n";
         break;
+
+      case INC_DENSITYMODEL::FLAMELET:
+        file << "Density is obtained through flamelet manifold.\n";
+        break;
     }
 
     file << "-- Input conditions:\n";
diff --git a/SU2_CFD/src/solvers/CIncEulerSolver.cpp b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
index a4f57d4420e..70a7f909ef5 100644
--- a/SU2_CFD/src/solvers/CIncEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
@@ -335,7 +335,7 @@ void CIncEulerSolver::SetNondimensionalization(CConfig *config, unsigned short i
       Pressure_Thermodynamic = config->GetPressure_Thermodynamic();
       auxFluidModel = new CFluidFlamelet(config, Pressure_Thermodynamic);
       config->SetPressure_Thermodynamic(Pressure_Thermodynamic);
-
+      auxFluidModel->SetTDState_T(Temperature_FreeStream, config->GetSpecies_Init());
       break;
 
     default:
@@ -487,7 +487,7 @@ void CIncEulerSolver::SetNondimensionalization(CConfig *config, unsigned short i
         break;
 
       case FLUID_FLAMELET:
-        fluidModel = new CFluidFlamelet(config, Pressure_Thermodynamic, true);
+        fluidModel = new CFluidFlamelet(config, Pressure_Thermodynamic);
         fluidModel->SetTDState_T(Temperature_FreeStreamND, config->GetSpecies_Init());
         break;
 
@@ -599,6 +599,9 @@ void CIncEulerSolver::SetNondimensionalization(CConfig *config, unsigned short i
         if (energy) cout << "Energy equation is active and coupled for variable density." << endl;
         break;
 
+      case INC_DENSITYMODEL::FLAMELET:
+        cout << "Energy equation is disabled and density is obtained through flamelet manifold." << endl;
+        break;
     }
 
     stringstream NonDimTableOut, ModelTableOut;
diff --git a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
index 33bcf5d7818..23f172279e0 100644
--- a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
+++ b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
@@ -80,9 +80,7 @@ CSpeciesFlameletSolver::CSpeciesFlameletSolver(CGeometry* geometry, CConfig* con
 void CSpeciesFlameletSolver::Preprocessing(CGeometry* geometry, CSolver** solver_container, CConfig* config,
                                            unsigned short iMesh, unsigned short iRKStep,
                                            unsigned short RunTime_EqSystem, bool Output) {
-  const auto n_user_scalars = config->GetNUserScalars();
-  const auto n_control_vars = config->GetNControlVars();
-
+  unsigned long n_not_in_domain_local = 0, n_not_in_domain_global=0;
   vector<su2double> scalars_vector(nVar);
 
   auto* flowNodes = su2staticcast_p<CFlowVariable*>(solver_container[FLOW_SOL]->GetNodes());
@@ -98,7 +96,7 @@ void CSpeciesFlameletSolver::Preprocessing(CGeometry* geometry, CSolver** solver
     /*--- Compute total source terms from the production and consumption. ---*/
     unsigned long misses = SetScalarSources(config, fluid_model_local, i_point, scalars_vector);
     nodes->SetTableMisses(i_point, misses);
-
+    n_not_in_domain_local += misses;
     /*--- Obtain passive look-up scalars. ---*/
     SetScalarLookUps(config, fluid_model_local, i_point, scalars_vector);
 
@@ -113,7 +111,11 @@ void CSpeciesFlameletSolver::Preprocessing(CGeometry* geometry, CSolver** solver
     if (!Output) LinSysRes.SetBlock_Zero(i_point);
   }
   END_SU2_OMP_FOR
-
+  /* --- Sum up some global counters over processes. --- */
+  SU2_MPI::Reduce(&n_not_in_domain_local, &n_not_in_domain_global, 1, MPI_UNSIGNED_LONG, MPI_SUM, MASTER_NODE,
+                  SU2_MPI::GetComm());
+  if ((rank == MASTER_NODE) && (n_not_in_domain_global > 0))
+    cout << "Number of points outside manifold domain: " << n_not_in_domain_global << endl;
   /*--- Clear Residual and Jacobian. Upwind second order reconstruction and gradients ---*/
   CommonPreprocessing(geometry, config, Output);
 }
@@ -135,11 +137,10 @@ void CSpeciesFlameletSolver::SetInitialCondition(CGeometry** geometry, CSolver**
 
     const su2double flamenorm = GeometryToolbox::Norm(nDim, flame_normal);
     const su2double temp_inlet = config->GetInc_Temperature_Init();
-    su2double prog_inlet = config->GetSpecies_Init()[I_PROGVAR];
     su2double enth_inlet = config->GetSpecies_Init()[I_ENTH];
-    su2double mixfrac_inlet = include_mixture_fraction ? config->GetSpecies_Init()[I_MIXFRAC] : 0.0;
 
-    su2double prog_burnt, prog_unburnt, point_loc, scalar_init[nVar];
+    su2double prog_burnt = 0, prog_unburnt, point_loc;
+    su2double *scalar_init = new su2double[nVar];
 
     if (rank == MASTER_NODE) {
       cout << "initial condition: T = " << temp_inlet << endl;
@@ -165,8 +166,10 @@ void CSpeciesFlameletSolver::SetInitialCondition(CGeometry** geometry, CSolver**
       n_not_iterated_local += GetEnthFromTemp(fluid_model_local, temp_inlet, &enth_inlet, config->GetSpecies_Init());
       scalar_init[I_ENTH] = enth_inlet;
 
+      prog_unburnt = config->GetSpecies_Init()[I_PROGVAR];
       prog_burnt = GetBurntProgressVariable(fluid_model_local, scalar_init);
-      for (unsigned long i_point = 0; i_point < nPointDomain; i_point++) {
+      SU2_OMP_FOR_STAT(omp_chunk_size)
+      for (unsigned long i_point = 0; i_point < nPoint; i_point++) {
         auto coords = geometry[i_mesh]->nodes->GetCoord(i_point);
 
         /*--- Determine if point is above or below the plane, assuming the normal
@@ -220,6 +223,7 @@ void CSpeciesFlameletSolver::SetInitialCondition(CGeometry** geometry, CSolver**
 
       solver_container[i_mesh][FLOW_SOL]->Preprocessing(geometry[i_mesh], solver_container[i_mesh], config, i_mesh,
                                                         NO_RK_ITER, RUNTIME_FLOW_SYS, false);
+      END_SU2_OMP_FOR
     }
 
     /* --- Sum up some global counters over processes. --- */
@@ -248,6 +252,8 @@ void CSpeciesFlameletSolver::SetInitialCondition(CGeometry** geometry, CSolver**
         cout << " Initial condition: Number of points in which enthalpy could not be iterated: "
              << n_not_iterated_global << " !!!" << endl;
     }
+
+    delete [] scalar_init;
   }
 }
 
@@ -498,7 +504,7 @@ unsigned long CSpeciesFlameletSolver::GetEnthFromTemp(CFluidModel* fluid_model,
 
   int counter = 0;
 
-  su2double val_scalars[nVar];
+  su2double *val_scalars = new su2double[nVar];
   for (auto iVar = 0u; iVar < nVar; iVar++) val_scalars[iVar] = scalar_solution[iVar];
 
   while ((abs(delta_temp_iter) > delta_temp_final) && (counter++ < counter_limit)) {
@@ -515,6 +521,7 @@ unsigned long CSpeciesFlameletSolver::GetEnthFromTemp(CFluidModel* fluid_model,
 
     enth_iter += delta_enth;
   }
+  delete [] val_scalars;
 
   *val_enth = enth_iter;
 
@@ -526,14 +533,17 @@ unsigned long CSpeciesFlameletSolver::GetEnthFromTemp(CFluidModel* fluid_model,
 }
 
 su2double CSpeciesFlameletSolver::GetBurntProgressVariable(CFluidModel* fluid_model, const su2double* scalar_solution) {
-  su2double scalars[nVar];
+  su2double *scalars = new su2double[nVar],
+            delta = 1e-3;
   for (auto iVar = 0u; iVar < nVar; iVar++) scalars[iVar] = scalar_solution[iVar];
 
   bool outside = false;
   while (!outside) {
     fluid_model->SetTDState_T(300, scalars);
     if (fluid_model->GetExtrapolation() == 1) outside = true;
-    scalars[I_PROGVAR] += 1e-3;
+    scalars[I_PROGVAR] += delta;
   }
-  return scalars[I_PROGVAR] - 1e-3;
+  su2double pv_burnt = scalars[I_PROGVAR] - delta;
+  delete [] scalars;
+  return pv_burnt;
 }
diff --git a/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg b/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg
index f6f9beccf39..8cb22a0406f 100644
--- a/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg
+++ b/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg
@@ -28,8 +28,8 @@ INC_NONDIM= DIMENSIONAL
 %
 FLUID_MODEL= FLUID_FLAMELET
 FILENAME_LUT= fgm_ch4.drg
-CONTROLLING_VARIABLE_NAMES= ("ProgressVariable", "EnthalpyTot")
-CONTROLLING_VARIABLE_SOURCE_NAMES = ("ProdRateTot_PV", "NULL")
+CONTROLLING_VARIABLE_NAMES= (ProgressVariable, EnthalpyTot)
+CONTROLLING_VARIABLE_SOURCE_NAMES = (ProdRateTot_PV, NULL)
 %
 % -------------------- SCALAR TRANSPORT ---------------------------------------%
 %
@@ -114,7 +114,7 @@ CONV_RESIDUAL_MINVAL= -15
 CONV_STARTITER= 10
 CONV_CAUCHY_ELEMS= 100
 CONV_CAUCHY_EPS= 1E-6
-SCREEN_OUTPUT = INNER_ITER RMS_VELOCITY-X RMS_VELOCITY-Y RMS_PRESSURE RMS_PROGRESS_VARIABLE RMS_TOTAL_ENTHALPY RMS_CO RMS_NOx
+SCREEN_OUTPUT = INNER_ITER RMS_VELOCITY-X RMS_VELOCITY-Y RMS_PRESSURE RMS_ProgressVariable RMS_EnthalpyTot RMS_CO RMS_NOx
 HISTORY_OUTPUT = RMS_RES AERO_COEFF FLOW_COEFF FLOW_COEFF_SURF
 VOLUME_OUTPUT = SOLUTION PRIMITIVE SOURCE RESIDUAL SENSITIVITY LOOKUP TIMESTEP
 CONV_FIELD = RMS_PRESSURE
diff --git a/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg
index e2201f1c20e..fdad7b11f80 100644
--- a/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg
+++ b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg
@@ -38,8 +38,8 @@ INC_NONDIM= DIMENSIONAL
 %
 FLUID_MODEL= FLUID_FLAMELET
 FILENAME_LUT= fgm_ch4.drg
-CONTROLLING_VARIABLE_NAMES= ("ProgressVariable", "EnthalpyTot")
-CONTROLLING_VARIABLE_SOURCE_NAMES= ("ProdRateTot_PV", "NULL")
+CONTROLLING_VARIABLE_NAMES= (ProgressVariable, EnthalpyTot)
+CONTROLLING_VARIABLE_SOURCE_NAMES= (ProdRateTot_PV, NULL)
 
 CONDUCTIVITY_MODEL= FLAMELET
 DIFFUSIVITY_MODEL= FLAMELET
@@ -55,7 +55,7 @@ MARKER_SYM= ( axis, symmetry_xm, symmetry_xp )
 %
 INC_INLET_TYPE=  VELOCITY_INLET
 MARKER_INLET= (inlet, 300.0, 0.20,    1.0, 0.0, 0.0)
-MARKER_INLET_SPECIES= (inlet, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
+MARKER_INLET_SPECIES= (inlet, 0.0, 0.0, 0.0, 0.0)
 MARKER_SPECIES_STRONG_BC= (inlet, wall_burner, wall_hx)
 
 %
@@ -67,7 +67,7 @@ MARKER_OUTLET= ( outlet, 0.0 )
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 CFL_NUMBER= 50
 CFL_REDUCTION_SPECIES= 1.0
-ITER= 11
+ITER= 7000
 %
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
@@ -99,7 +99,7 @@ SLOPE_LIMITER_SPECIES= NONE
 %
 TIME_DISCRE_SPECIES= EULER_IMPLICIT
 %
-SPECIES_INIT= (0, 0, 0, 0, 0, 0, 0)
+SPECIES_INIT= (0, 0, 0, 0)
 SPECIES_CLIPPING= NO
 LOOKUP_NAMES= (MolarWeightMix, Conductivity, HeatRelease, Diffusivity, \
     ProdRatePos_Y-CO, ProdRateNegScaled_Y-CO ,\
@@ -116,7 +116,7 @@ CONV_STARTITER= 10
 %
 MESH_FILENAME= mesh_unstructured_hx.su2
 %
-SCREEN_OUTPUT= INNER_ITER WALL_TIME RMS_ADJ_PRESSURE RMS_ADJ_VELOCITY-X RMS_ADJ_VELOCITY-Y RMS_ADJ_SPECIES_0 RMS_ADJ_SPECIES_1 RMS_ADJ_SPECIES_2 RMS_ADJ_SPECIES_3
+SCREEN_OUTPUT= INNER_ITER WALL_TIME RMS_ADJ_PRESSURE RMS_ADJ_VELOCITY-X RMS_ADJ_VELOCITY-Y RMS_ADJ_ProgressVariable RMS_ADJ_EnthalpyTot RMS_ADJ_Y-NOx_tot RMS_ADJ_Y-CO
 SCREEN_WRT_FREQ_INNER= 1
 %
 HISTORY_OUTPUT= ITER RMS_RES LINSOL FLOW_COEFF_SURF CUSTOM COMBO
@@ -125,7 +125,7 @@ MARKER_ANALYZE= outlet
 MARKER_ANALYZE_AVERAGE= MASSFLUX
 %
 %OUTPUT_FILES= RESTART, PARAVIEW, PARAVIEW_MULTIBLOCK
-OUTPUT_FILES= RESTART, RESTART_ASCII
+OUTPUT_FILES= RESTART, RESTART_ASCII, PARAVIEW
 VOLUME_OUTPUT= RESIDUAL, PRIMITIVE
 VOLUME_ADJ_FILENAME= ch4_flame_hx_ad
 
diff --git a/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg
index 1a36d71128d..64988b994dc 100644
--- a/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg
+++ b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg
@@ -39,8 +39,8 @@ INC_NONDIM= DIMENSIONAL
 %
 FLUID_MODEL= FLUID_FLAMELET
 FILENAME_LUT= fgm_ch4.drg
-CONTROLLING_VARIABLE_NAMES= ("ProgressVariable", "EnthalpyTot")
-CONTROLLING_VARIABLE_SOURCE_NAMES= ("ProdRateTot_PV", "NULL")
+CONTROLLING_VARIABLE_NAMES= (ProgressVariable, EnthalpyTot)
+CONTROLLING_VARIABLE_SOURCE_NAMES= (ProdRateTot_PV, NULL)
 CONDUCTIVITY_MODEL= FLAMELET
 DIFFUSIVITY_MODEL= FLAMELET
 KIND_SCALAR_MODEL= FLAMELET
@@ -55,7 +55,7 @@ MARKER_SYM= ( axis, symmetry_xm, symmetry_xp, outlet )
 %
 INC_INLET_TYPE=  VELOCITY_INLET
 MARKER_INLET= (inlet, 300.0, 0.20, 1.0, 0.0, 0.0)
-MARKER_INLET_SPECIES= (inlet, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
+MARKER_INLET_SPECIES= (inlet, 0.0, 0.0, 0.0, 0.0)
 MARKER_SPECIES_STRONG_BC= (inlet, wall_burner, wall_hx)
 %
 % INC_OUTLET_TYPE= PRESSURE_OUTLET
@@ -98,7 +98,7 @@ SLOPE_LIMITER_SPECIES= NONE
 %
 TIME_DISCRE_SPECIES= EULER_IMPLICIT
 %
-SPECIES_INIT= (0, 0, 0, 0, 0, 0, 0)
+SPECIES_INIT= (0, 0, 0, 0)
 SPECIES_CLIPPING= NO
 LOOKUP_NAMES= (MolarWeightMix, Conductivity, HeatRelease, Diffusivity, \
     ProdRatePos_Y-CO,  ProdRateNegScaled_Y-CO  ,\
@@ -115,7 +115,7 @@ CONV_STARTITER= 10
 %
 MESH_FILENAME= mesh_unstructured_hx.su2
 %
-SCREEN_OUTPUT= INNER_ITER WALL_TIME RMS_ADJ_PRESSURE RMS_ADJ_VELOCITY-X RMS_ADJ_VELOCITY-Y RMS_ADJ_SPECIES_0 RMS_ADJ_SPECIES_1 RMS_ADJ_SPECIES_2 RMS_ADJ_SPECIES_3
+SCREEN_OUTPUT= INNER_ITER WALL_TIME RMS_ADJ_PRESSURE RMS_ADJ_VELOCITY-X RMS_ADJ_VELOCITY-Y RMS_ADJ_ProgressVariable RMS_ADJ_EnthalpyTot RMS_ADJ_Y-NOx_tot RMS_ADJ_Y-CO
 SCREEN_WRT_FREQ_INNER= 1
 %
 HISTORY_OUTPUT= ITER RMS_RES LINSOL FLOW_COEFF_SURF
diff --git a/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg b/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg
index c1e0ef8bd8b..808236c6df5 100644
--- a/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg
+++ b/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg
@@ -13,7 +13,7 @@ MARKER_PLOTTING= ( NONE )
 
 WRT_ZONE_HIST= YES
 
-SCREEN_OUTPUT= INNER_ITER WALL_TIME RMS_PRESSURE RMS_PROGRESS_VARIABLE
+SCREEN_OUTPUT= INNER_ITER WALL_TIME RMS_PRESSURE RMS_ProgressVariable
 
 HISTORY_OUTPUT= RMS_RES AERO_COEFF FLOW_COEFF FLOW_COEFF_SURF
 
@@ -53,8 +53,8 @@ INC_NONDIM= DIMENSIONAL
 
 FLUID_MODEL= FLUID_FLAMELET
 FILENAME_LUT= fgm_ch4.drg
-CONTROLLING_VARIABLE_NAMES= ("ProgressVariable", "EnthalpyTot")
-CONTROLLING_VARIABLE_SOURCE_NAMES= ("ProdRateTot_PV", "NULL")
+CONTROLLING_VARIABLE_NAMES= (ProgressVariable, EnthalpyTot)
+CONTROLLING_VARIABLE_SOURCE_NAMES= (ProdRateTot_PV, NULL)
 FLAME_INIT= (0.004, 0.0, 0.0, 1.0, 0.0, 0.0, 0.2e-3, 1.0)
 
 % -------------------- SPECIES TRANSPORT ---------------------------------------%
diff --git a/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg b/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg
index 73988c0df47..927ef5f7b31 100644
--- a/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg
+++ b/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg
@@ -15,7 +15,7 @@ WRT_ZONE_HIST= YES
 
 %SCREEN_OUTPUT= INNER_ITER WALL_TIME RMS_PRESSURE RMS_VELOCITY-X RMS_VELOCITY-Y RMS_TKE RMS_DISSIPATION LINSOL_ITER LINSOL_RESIDUAL RMS_ADJ_PRESSURE RMS_ADJ_VELOCITY-X RMS_ADJ_VELOCITY-Y
 
-SCREEN_OUTPUT= INNER_ITER WALL_TIME RMS_ADJ_PRESSURE RMS_ADJ_VELOCITY-X RMS_ADJ_VELOCITY-Y RMS_ADJ_PROGRESS_VARIABLE RMS_ADJ_TOTAL_ENTHALPY RMS_ADJ_Y-CO RMS_ADJ_Y-NOx_tot
+SCREEN_OUTPUT= INNER_ITER WALL_TIME RMS_ADJ_PRESSURE RMS_ADJ_VELOCITY-X RMS_ADJ_VELOCITY-Y RMS_ADJ_ProgressVariable RMS_ADJ_EnthalpyTot RMS_ADJ_Y-CO RMS_ADJ_Y-NOx_tot
 
 HISTORY_OUTPUT= RMS_RES AERO_COEFF FLOW_COEFF FLOW_COEFF_SURF
 
@@ -55,8 +55,8 @@ INC_NONDIM= DIMENSIONAL
 
 FLUID_MODEL= FLUID_FLAMELET
 FILENAME_LUT= fgm_ch4.drg
-CONTROLLING_VARIABLE_NAMES= ("ProgressVariable", "EnthalpyTot")
-CONTROLLING_VARIABLE_SOURCE_NAMES= ("ProdRateTot_PV", "NULL")
+CONTROLLING_VARIABLE_NAMES= (ProgressVariable, EnthalpyTot)
+CONTROLLING_VARIABLE_SOURCE_NAMES= (ProdRateTot_PV, NULL)
 FLAME_INIT= (0.004, 0.0, 0.0, 1, 0, 0, 0.2e-3, 1)
 
 % -------------------- SPECIES TRANSPORT ---------------------------------------%
diff --git a/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg b/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg
index 2fe94fc0f2c..859cd446323 100644
--- a/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg
+++ b/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg
@@ -31,8 +31,8 @@ AXISYMMETRIC= YES
 %
 FLUID_MODEL= FLUID_FLAMELET
 FILENAME_LUT= fgm_ch4.drg
-CONTROLLING_VARIABLE_NAMES= ("ProgressVariable", "EnthalpyTot")
-CONTROLLING_VARIABLE_SOURCE_NAMES= ("ProdRateTot_PV", "NULL")
+CONTROLLING_VARIABLE_NAMES= (ProgressVariable, EnthalpyTot)
+CONTROLLING_VARIABLE_SOURCE_NAMES= (ProdRateTot_PV, NULL)
 %
 % -------------------- SCALAR TRANSPORT ---------------------------------------%
 %
@@ -115,7 +115,7 @@ CONV_RESIDUAL_MINVAL= -15
 CONV_STARTITER= 10
 CONV_CAUCHY_ELEMS= 100
 CONV_CAUCHY_EPS= 1E-6
-SCREEN_OUTPUT= INNER_ITER WALL_TIME RMS_VELOCITY-X RMS_VELOCITY-Y RMS_PRESSURE RMS_PROGRESS_VARIABLE RMS_TOTAL_ENTHALPY
+SCREEN_OUTPUT= INNER_ITER WALL_TIME RMS_VELOCITY-X RMS_VELOCITY-Y RMS_PRESSURE RMS_ProgressVariable RMS_EnthalpyTot
 HISTORY_OUTPUT= RMS_RES AERO_COEFF FLOW_COEFF FLOW_COEFF_SURF
 VOLUME_OUTPUT= SOLUTION PRIMITIVE SOURCE RESIDUAL SENSITIVITY LOOKUP TIMESTEP
 CONV_FIELD= RMS_PRESSURE
diff --git a/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_premixed_ch4_cfd.cfg b/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_prem_ch4_cfd.cfg
similarity index 82%
rename from TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_premixed_ch4_cfd.cfg
rename to TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_prem_ch4_cfd.cfg
index 8a40f4eda09..bd0d9af93db 100644
--- a/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_premixed_ch4_cfd.cfg
+++ b/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_prem_ch4_cfd.cfg
@@ -17,7 +17,7 @@ RESTART_SOL= NO
 %
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
-INC_DENSITY_MODEL= VARIABLE 
+INC_DENSITY_MODEL= VARIABLE
 INC_ENERGY_EQUATION = YES
 INC_DENSITY_INIT= 1.00
 INC_VELOCITY_INIT= (0.7, 0.0, 0.0 )
@@ -27,12 +27,12 @@ INC_NONDIM= DIMENSIONAL
 % -------------------- FLUID MODEL --------------------------------------- %
 %
 FLUID_MODEL= FLUID_FLAMELET
-FILENAME_LUT= LUT_methane_PD.drg
-CONTROLLING_VARIABLE_NAMES= ("ProgressVariable", "EnthalpyTot","MixtureFraction")
-CONTROLLING_VARIABLE_SOURCE_NAMES= ("ProdRateTot_PV", "NULL", "NULL")
+FILENAME_LUT= LUT_methane_3D.drg
+% FGM controlling variable names (must include mixture fraction for partial 
+% premixed cases)
+CONTROLLING_VARIABLE_NAMES=(ProgressVariable,EnthalpyTot,MixtureFraction)
 
-OBJECTIVE_FUNCTION= CUSTOM_OBJFUNC
-OBJECTIVE_WEIGHT= 1.0
+CONTROLLING_VARIABLE_SOURCE_NAMES=(ProdRateTot_PV,NULL,NULL)
 % -------------------- SCALAR TRANSPORT ---------------------------------------%
 %
 KIND_SCALAR_MODEL= FLAMELET      
@@ -51,10 +51,10 @@ SPECIES_CLIPPING= YES
 SPECIES_CLIPPING_MIN= 0 -2.0e6 0 0 0
 SPECIES_CLIPPING_MAX= 0.3 2e6 1 1 1
 %
-MARKER_INLET_SPECIES = (inlet_upper, 0.0,	-253498.718914723, 0.09, 0.0, 0.0,\
-                        inlet_lower, 0.0,	-253498.718914723, 0.01, 0.0, 0.0) 
+MARKER_INLET_SPECIES = (inlet_rich, 0.0,	-253498.718914723, 0.06, 0.0, 0.0,\
+                        inlet_lean, 0.0,	-253498.718914723, 0.04, 0.0, 0.0) 
 CFL_REDUCTION_SPECIES= 1.0
-MARKER_SPECIES_STRONG_BC= (inlet, outlet,cht_interface_burner_fluid, outlet,cht_interface_hex_fluid)
+MARKER_SPECIES_STRONG_BC= (inlet_rich,inlet_lean, burner_wall,outlet)
 LOOKUP_NAMES = (MolarWeightMix, Conductivity, Cp, ProdRateTot_PV)
 USER_SCALAR_NAMES= (CO, CO2)
 USER_SOURCE_NAMES = ( \
@@ -72,11 +72,12 @@ REF_AREA= 1.0
 %
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-MARKER_ISOTHERMAL= (cht_interface_burner_fluid, 400, cht_interface_hex_fluid, 400)
+MARKER_ISOTHERMAL= (burner_wall, 400, hex_wall, 400)
+MARKER_HEATFLUX= (mixing_edge, 0.0)
 MARKER_SYM= (sides)
 INC_INLET_TYPE= VELOCITY_INLET,VELOCITY_INLET
-MARKER_INLET = (inlet_upper, 300.000, 0.3, 1.0, 0.0, 0.0,\
-                inlet_lower, 300.000, 0.25, 1.0, 0.0, 0.0)
+MARKER_INLET = (inlet_rich, 300.000, 0.3, 1.0, 0.0, 0.0,\
+                inlet_lean, 300.000, 0.25, 1.0, 0.0, 0.0)
 INC_OUTLET_TYPE= PRESSURE_OUTLET
 INC_INLET_DAMPING = 0.05
 INC_OUTLET_DAMPING = 0.05
@@ -87,7 +88,7 @@ MARKER_OUTLET= (outlet, 0.0)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 CFL_NUMBER= 20
 CFL_ADAPT= NO
-ITER= 20000
+ITER= 10000
 OUTPUT_WRT_FREQ= 20
 %
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
@@ -114,7 +115,7 @@ CONV_RESIDUAL_MINVAL= -15
 CONV_STARTITER= 10
 CONV_CAUCHY_ELEMS= 100
 CONV_CAUCHY_EPS= 1E-6
-SCREEN_OUTPUT = INNER_ITER RMS_VELOCITY-X RMS_VELOCITY-Y RMS_PRESSURE RMS_PROGRESS_VARIABLE RMS_TOTAL_ENTHALPY RMS_MIXTURE_FRACTION RMS_CO2
+SCREEN_OUTPUT = INNER_ITER RMS_VELOCITY-X RMS_VELOCITY-Y RMS_PRESSURE RMS_ProgressVariable RMS_EnthalpyTot RMS_MixtureFraction RMS_CO2
 HISTORY_OUTPUT = RMS_RES AERO_COEFF FLOW_COEFF FLOW_COEFF_SURF
 VOLUME_OUTPUT = SOLUTION PRIMITIVE SOURCE RESIDUAL SENSITIVITY LOOKUP TIMESTEP
 CONV_FIELD = RMS_PRESSURE
@@ -123,7 +124,7 @@ CONV_FIELD = RMS_PRESSURE
 %
 OUTPUT_PRECISION= 16
 MESH_FORMAT= SU2
-MESH_FILENAME= fluid.su2
+MESH_FILENAME= mesh_unstructured.su2
 MESH_OUT_FILENAME= mesh_out.su2
 SOLUTION_FILENAME= solution
 RESTART_FILENAME= restart
diff --git a/config_template.cfg b/config_template.cfg
index e36c6d9cfc3..47d9996df7a 100644
--- a/config_template.cfg
+++ b/config_template.cfg
@@ -770,6 +770,16 @@ LOOKUP_NAMES= (MolarWeightMix, Conductivity, HeatRelease, Diffusivity)
 %
 % filename of the lookup table
 FILENAME_LUT= fgm_ch4.drg
+
+% Names of the controlling variables used to evaluate the look-up table and for which
+% transported scalar variables are generated. These names should coincide with those
+% listed in the look-up table.
+CONTROLLING_VARIABLE_NAMES= (ProgressVariable, EnthalpyTot)
+
+% Names of the source term variables as they are present in the look-up table. For
+% controlling variables without source terms, use "zero" or "null", similar to the
+% option USER_SOURCE_NAMES.
+CONTROLLING_VARIABLE_SOURCE_NAMES= (ProdRateTot_PV, NULL)
 %
 % flamelet initialization
 % the flame is initialized using a plane, defined by a point and a normal. On one side, the solution is initialized

From c2f2a34e054f779f62b8eb0271014ed07c4280f2 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 23 Jun 2023 15:28:51 +0200
Subject: [PATCH 499/656] Removed extra zeros from initial species arrays

---
 .../lam_prem_ch4_cht_cfd_fluid.cfg                            | 4 ++--
 .../lam_prem_ch4_cht_ad_fluid.cfg                             | 4 ++--
 .../lam_partial_prem_ch4_cfd.cfg                              | 2 +-
 3 files changed, 5 insertions(+), 5 deletions(-)

diff --git a/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg b/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg
index 808236c6df5..8eab5644d61 100644
--- a/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg
+++ b/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg
@@ -34,7 +34,7 @@ INLET_MATCHING_TOLERANCE= 1e-5
 INC_INLET_TYPE= VELOCITY_INLET
 
 MARKER_INLET= (inlet, 300.0, 0.4, 1.0, 0.0, 0.0)
-MARKER_INLET_SPECIES= (inlet, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
+MARKER_INLET_SPECIES= (inlet, 0.0, 0.0, 0.0, 0.0)
 
 INC_OUTLET_TYPE= PRESSURE_OUTLET
 MARKER_OUTLET= (outlet, 0.0)
@@ -73,7 +73,7 @@ SLOPE_LIMITER_SPECIES= NONE
 
 TIME_DISCRE_SPECIES= EULER_IMPLICIT
 
-SPECIES_INIT= (0, 0, 0, 0, 0, 0, 0)
+SPECIES_INIT= (0, 0, 0, 0)
 SPECIES_CLIPPING= NO
 LOOKUP_NAMES= (MolarWeightMix, Conductivity, HeatRelease, Diffusivity, \
     ProdRatePos_Y-CO,  ProdRateNegScaled_Y-CO  ,\
diff --git a/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg b/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg
index 927ef5f7b31..4bf950c936a 100644
--- a/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg
+++ b/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg
@@ -36,7 +36,7 @@ INLET_MATCHING_TOLERANCE= 1e-5
 INC_INLET_TYPE= VELOCITY_INLET
 
 MARKER_INLET= (inlet, 300.0, 0.4, 1.0, 0.0, 0.0)
-MARKER_INLET_SPECIES= (inlet, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
+MARKER_INLET_SPECIES= (inlet, 0.0, 0.0, 0.0, 0.0)
 
 INC_OUTLET_TYPE= PRESSURE_OUTLET
 MARKER_OUTLET= (outlet, 0.0)
@@ -75,7 +75,7 @@ SLOPE_LIMITER_SPECIES= NONE
 
 TIME_DISCRE_SPECIES= EULER_IMPLICIT
 
-SPECIES_INIT= (0, 0, 0, 0, 0, 0, 0)
+SPECIES_INIT= (0, 0, 0, 0)
 SPECIES_CLIPPING= NO
 LOOKUP_NAMES= (MolarWeightMix, Conductivity, HeatRelease, Diffusivity, \
     ProdRatePos_Y-CO,  ProdRateNegScaled_Y-CO  ,\
diff --git a/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_prem_ch4_cfd.cfg b/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_prem_ch4_cfd.cfg
index bd0d9af93db..bb157368398 100644
--- a/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_prem_ch4_cfd.cfg
+++ b/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_prem_ch4_cfd.cfg
@@ -13,7 +13,7 @@
 SOLVER = INC_NAVIER_STOKES
 KIND_TURB_MODEL= NONE
 MATH_PROBLEM= DIRECT
-RESTART_SOL= NO
+RESTART_SOL= YES
 %
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %

From 187c9865cf9f531dcdb1da5eea42f2535c5251c3 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 23 Jun 2023 15:46:43 +0200
Subject: [PATCH 500/656] Added partially premixed methane test case files

---
 .../lam_partial_prem_ch4_cfd.cfg                         | 8 ++++----
 TestCases/parallel_regression.py                         | 9 +++++++++
 2 files changed, 13 insertions(+), 4 deletions(-)

diff --git a/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_prem_ch4_cfd.cfg b/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_prem_ch4_cfd.cfg
index bb157368398..cd22b4147ec 100644
--- a/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_prem_ch4_cfd.cfg
+++ b/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_prem_ch4_cfd.cfg
@@ -48,13 +48,13 @@ SLOPE_LIMITER_SPECIES= NONE
 TIME_DISCRE_SPECIES= EULER_IMPLICIT
 % SCALAR CLIPPING
 SPECIES_CLIPPING= YES
-SPECIES_CLIPPING_MIN= 0 -2.0e6 0 0 0
+SPECIES_CLIPPING_MIN= 0 -3.0e6 0 0 0
 SPECIES_CLIPPING_MAX= 0.3 2e6 1 1 1
 %
 MARKER_INLET_SPECIES = (inlet_rich, 0.0,	-253498.718914723, 0.06, 0.0, 0.0,\
                         inlet_lean, 0.0,	-253498.718914723, 0.04, 0.0, 0.0) 
 CFL_REDUCTION_SPECIES= 1.0
-MARKER_SPECIES_STRONG_BC= (inlet_rich,inlet_lean, burner_wall,outlet)
+MARKER_SPECIES_STRONG_BC= (inlet_rich,inlet_lean, burner_wall, hex_wall)
 LOOKUP_NAMES = (MolarWeightMix, Conductivity, Cp, ProdRateTot_PV)
 USER_SCALAR_NAMES= (CO, CO2)
 USER_SOURCE_NAMES = ( \
@@ -72,7 +72,7 @@ REF_AREA= 1.0
 %
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
-MARKER_ISOTHERMAL= (burner_wall, 400, hex_wall, 400)
+MARKER_ISOTHERMAL= (burner_wall, 400, hex_wall, 500)
 MARKER_HEATFLUX= (mixing_edge, 0.0)
 MARKER_SYM= (sides)
 INC_INLET_TYPE= VELOCITY_INLET,VELOCITY_INLET
@@ -88,7 +88,7 @@ MARKER_OUTLET= (outlet, 0.0)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 CFL_NUMBER= 20
 CFL_ADAPT= NO
-ITER= 10000
+ITER= 10
 OUTPUT_WRT_FREQ= 20
 %
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 35f1f890050..57cb607670c 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -60,6 +60,15 @@ def main():
     cfd_flamelet_ch4_axi.new_output = True
     test_list.append(cfd_flamelet_ch4_axi)
 
+    # 2D planar laminar partially premixed flame on isothermal burner and heat exchanger (restart)
+    cfd_flamelet_ch4_partial_premix = TestCase('cfd_flamelet_ch4_partial_premix')
+    cfd_flamelet_ch4_partial_premix.cfg_dir = "flamelet/06_laminar_partial_premixed_ch4_flame_cfd"
+    cfd_flamelet_ch4_partial_premix.cfg_file = "lam_partial_prem_ch4_cfd.cfg"
+    cfd_flamelet_ch4_partial_premix.test_iter = 10
+    cfd_flamelet_ch4_partial_premix.test_vals = [-8.557377, -9.715636, -9.436786, -9.813844, -2.684793]
+    cfd_flamelet_ch4_partial_premix.new_output = True
+    test_list.append(cfd_flamelet_ch4_partial_premix)
+
     #########################
     ## NEMO solver ###
     #########################

From bba0c8a858377f7587bb6890551182fecd75903f Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Fri, 23 Jun 2023 21:41:01 +0100
Subject: [PATCH 501/656] add new example, fix #2058

---
 .github/workflows/regression.yml             |   2 +-
 TestCases/parallel_regression_AD.py          |  19 +-
 TestCases/py_wrapper/wavy_wall/run_steady.py | 317 +++++++++++++++++++
 externals/cgns/hdf5/meson.build              | 117 +++----
 externals/cgns/meson.build                   |   4 +-
 5 files changed, 395 insertions(+), 64 deletions(-)
 create mode 100644 TestCases/py_wrapper/wavy_wall/run_steady.py

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 76545cdb274..9c85ced8e11 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c py_wrapper_example -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index 2e0d70f516a..a54f7dfdeb7 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -377,9 +377,9 @@ def main():
     ################################################
     ### Gradient check (dot) for flamelet solver ###
     ################################################
-    
+
     # 2D planar laminar premixed flame on isothermal burner (restart)
-    # This test restarts on the output of test discadj_flamelet_ch4_hx and 
+    # This test restarts on the output of test discadj_flamelet_ch4_hx and
     # will only pass if test discadj_flamelet_ch4_hx passes.
     dot_flamelet_ch4_hx                  = TestCase('dot_flamelet_ch4_hx')
     dot_flamelet_ch4_hx.cfg_dir          = "flamelet/02_laminar_premixed_ch4_flame_hx_ad"
@@ -395,7 +395,7 @@ def main():
     test_list.append(dot_flamelet_ch4_hx)
 
     # 2D planar laminar premixed flame on isothermal burner with conjugate heat transfer (restart)
-    # This test restarts on the output of test discadj_flamelet_ch4_cht and 
+    # This test restarts on the output of test discadj_flamelet_ch4_cht and
     # will only pass if test discadj_flamelet_ch4_cht passes.
     dot_flamelet_ch4_cht                  = TestCase('dot_flamelet_ch4_cht')
     dot_flamelet_ch4_cht.cfg_dir          = "flamelet/04_laminar_premixed_ch4_flame_cht_ad"
@@ -518,6 +518,19 @@ def main():
     test_list.append(pywrapper_CFD_AD_MeshDisp)
     pass_list.append(pywrapper_CFD_AD_MeshDisp.run_test())
 
+    # Flow AD Mesh Displacement and Initial Coordinates Sensitivity
+    pywrapper_wavy_wall_steady = TestCase('pywrapper_wavy_wall_steady')
+    pywrapper_wavy_wall_steady.cfg_dir = "py_wrapper/disc_adj_flow/mesh_disp_sens"
+    pywrapper_wavy_wall_steady.cfg_file = "run_steady.py"
+    pywrapper_wavy_wall_steady.test_iter = 100
+    pywrapper_wavy_wall_steady.test_vals = [-1.360044, 2.580709, -2.892473]
+    pywrapper_wavy_wall_steady.command = TestCase.Command("mpirun -n 2", "python", "run_steady.py")
+    pywrapper_wavy_wall_steady.timeout = 1600
+    pywrapper_wavy_wall_steady.tol = 0.00001
+    pywrapper_wavy_wall_steady.new_output = False
+    test_list.append(pywrapper_wavy_wall_steady)
+    pass_list.append(pywrapper_wavy_wall_steady.run_test())
+
     ####################################################################
     ###  Unsteady Disc. adj. compressible RANS restart optimization  ###
     ####################################################################
diff --git a/TestCases/py_wrapper/wavy_wall/run_steady.py b/TestCases/py_wrapper/wavy_wall/run_steady.py
new file mode 100644
index 00000000000..93361a1458f
--- /dev/null
+++ b/TestCases/py_wrapper/wavy_wall/run_steady.py
@@ -0,0 +1,317 @@
+#!/usr/bin/env python
+
+## \file run.py
+#  \brief Channel with wave-like motion on walls (steady state version).
+#  \version 7.5.1 "Blackbird"
+#
+# SU2 Project Website: https://su2code.github.io
+#
+# The SU2 Project is maintained by the SU2 Foundation
+# (http://su2foundation.org)
+#
+# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
+#
+# SU2 is free software; you can redistribute it and/or
+# modify it under the terms of the GNU Lesser General Public
+# License as published by the Free Software Foundation; either
+# version 2.1 of the License, or (at your option) any later version.
+#
+# SU2 is distributed in the hope that it will be useful,
+# but WITHOUT ANY WARRANTY; without even the implied warranty of
+# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+# Lesser General Public License for more details.
+#
+# You should have received a copy of the GNU Lesser General Public
+# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+
+import pysu2ad as pysu2
+from mpi4py import MPI
+import numpy as np
+
+common_settings = """
+SOLVER= NAVIER_STOKES
+
+FLUID_MODEL= IDEAL_GAS
+GAMMA_VALUE= 1.4
+GAS_CONSTANT= 287.87
+
+MACH_NUMBER= 0.034
+INIT_OPTION= TD_CONDITIONS
+FREESTREAM_OPTION= TEMPERATURE_FS
+FREESTREAM_TEMPERATURE= 299.99
+FREESTREAM_PRESSURE= 98750
+REYNOLDS_NUMBER= 2000
+REYNOLDS_LENGTH= 0.055
+
+VISCOSITY_MODEL= CONSTANT_VISCOSITY
+MU_CONSTANT= 0.0005
+
+MARKER_HEATFLUX= ( y_minus, 0, y_plus, 0 )
+MARKER_INLET= ( x_minus, 300, 100000, 1, 0, 0 )
+MARKER_FAR= ( x_plus )
+
+MARKER_MONITORING= ( y_minus, y_plus )
+MARKER_PLOTTING= ( x_minus, x_plus, y_minus, y_plus )
+
+DEFORM_MESH= YES
+MARKER_DEFORM_MESH= ( y_minus, y_plus )
+DEFORM_CONSOLE_OUTPUT= YES
+DEFORM_LINEAR_SOLVER= CONJUGATE_GRADIENT
+DEFORM_LINEAR_SOLVER_PREC= ILU
+DEFORM_LINEAR_SOLVER_ERROR= 1e-12
+DEFORM_LINEAR_SOLVER_ITER= 1000
+DEFORM_STIFFNESS_TYPE= CONSTANT_STIFFNESS
+DEFORM_POISSONS_RATIO= 0.35
+
+CONV_NUM_METHOD_FLOW= ROE
+ENTROPY_FIX_COEFF= 1e-5
+MUSCL_FLOW= YES
+SLOPE_LIMITER_FLOW= NONE
+NUM_METHOD_GRAD= GREEN_GAUSS
+
+MESH_FORMAT= RECTANGLE
+MESH_BOX_SIZE= ( 193, 33, 0 )
+MESH_BOX_LENGTH= ( 0.75, __WIDTH__, 0 )
+
+CUSTOM_OUTPUTS= 'p_tot : Macro{PRESSURE + 0.5 * DENSITY * (pow(VELOCITY_X, 2) + pow(VELOCITY_Y, 2))};\
+                 p_in : MassFlowAvg{$p_tot}[x_minus];\
+                 p_out : MassFlowAvg{$p_tot}[x_plus];\
+                 p_drop : Function{p_out - p_in}'
+
+CUSTOM_OBJFUNC= 'p_drop'
+OBJECTIVE_FUNCTION= CUSTOM_OBJFUNC
+
+SOLUTION_FILENAME= restart.dat
+OUTPUT_FILES= RESTART, PARAVIEW_MULTIBLOCK
+OUTPUT_WRT_FREQ= 9999
+SCREEN_WRT_FREQ_INNER= 10
+
+INNER_ITER= 3000
+CONV_STARTITER= 10
+"""
+
+primal_settings = """
+MATH_PROBLEM= DIRECT
+RESTART_SOL= YES
+
+CFL_NUMBER= 1000
+LINEAR_SOLVER= FGMRES
+LINEAR_SOLVER_PREC= ILU
+LINEAR_SOLVER_ERROR= 0.1
+LINEAR_SOLVER_ITER= 20
+
+SCREEN_OUTPUT= INNER_ITER, RMS_RES, LINSOL, p_drop
+HISTORY_OUTPUT= ITER, RMS_RES, CUSTOM
+VOLUME_OUTPUT= PRIMITIVE, VORTEX_IDENTIFICATION
+
+CONV_RESIDUAL_MINVAL= -13
+CONV_FIELD= RMS_DENSITY
+"""
+
+adjoint_settings = """
+MATH_PROBLEM= DISCRETE_ADJOINT
+
+CFL_NUMBER= 1000
+DISCADJ_LIN_SOLVER= FGMRES
+DISCADJ_LIN_PREC= ILU
+LINEAR_SOLVER_ERROR= 0.001
+LINEAR_SOLVER_ITER= 20
+
+SCREEN_OUTPUT= INNER_ITER, RMS_RES, LINSOL
+HISTORY_OUTPUT= ITER, RMS_RES, SENSITIVITY
+
+QUASI_NEWTON_NUM_SAMPLES= 20
+
+CONV_RESIDUAL_MINVAL= -8
+CONV_FIELD= REL_RMS_ADJ_DENSITY
+"""
+
+
+def GetMarkerIds(driver):
+    """Get the ID of the markers where the deformation is applied."""
+    all_marker_ids = driver.GetMarkerIndices()
+    marker_names = ['y_minus', 'y_plus']
+    marker_ids = []
+    for name in marker_names:
+        marker_ids.append(all_marker_ids[name] if name in all_marker_ids else -1)
+    return marker_ids
+
+
+def RunPrimal(channel_width, deform_amplitude):
+    """
+    Runs the primal solver for a given amplitude of the deformation.
+    Returns the objective function.
+    """
+    comm = MPI.COMM_WORLD
+    rank = comm.Get_rank()
+
+    with open('config.cfg', 'w') as f:
+        f.write(common_settings.replace('__WIDTH__', str(channel_width)) + primal_settings)
+
+    # Initialize the corresponding driver of SU2, this includes solver preprocessing.
+    try:
+        driver = pysu2.CSinglezoneDriver('config.cfg', 1, comm)
+    except TypeError as exception:
+        print('A TypeError occured in pysu2.CSinglezoneDriver : ', exception)
+        raise
+
+    marker_ids = GetMarkerIds(driver)
+
+    for marker_id in marker_ids:
+        Deformation(0, deform_amplitude, marker_id, driver)
+
+    driver.StartSolver()
+    avg_p_drop = driver.GetOutputValue('p_drop')
+
+    # Finalize the solver and exit cleanly
+    driver.Finalize()
+
+    return avg_p_drop
+
+
+def RunAdjoint(channel_width, deform_amplitude):
+    """
+    Runs the adjoint solver for a given amplitude of the deformation, and channel width.
+    Returns the sensitivity of the objective function to the amplitude and width.
+    """
+    comm = MPI.COMM_WORLD
+    rank = comm.Get_rank()
+
+    with open('config_ad.cfg', 'w') as f:
+        f.write(common_settings.replace('__WIDTH__', str(channel_width)) + adjoint_settings)
+
+    # Initialize the corresponding driver of SU2, this includes solver preprocessing.
+    try:
+        driver = pysu2.CDiscAdjSinglezoneDriver('config_ad.cfg', 1, comm)
+    except TypeError as exception:
+        print('A TypeError occured in pysu2.CDiscAdjSinglezoneDriver : ', exception)
+        raise
+
+    marker_ids = GetMarkerIds(driver)
+
+    # Preprocess adjoint to load the primal solution.
+    driver.Preprocess(0)
+
+    # Check the surface deformation is the expected from loading the primal results.
+    for marker_id in marker_ids:
+        Deformation(0, deform_amplitude, marker_id, driver, True)
+
+    driver.Run()
+    driver.Postprocess()
+    driver.Update()
+
+    # Accumulate the sensitivity to the deformation amplitude.
+    sens = 0
+    for marker_id in marker_ids:
+        sens += SumSensitivity(0, marker_id, driver)
+
+    driver.Monitor(0)
+    driver.Output(0)
+
+    size_sens = 0.0
+    sensitivity = driver.Sensitivity(driver.GetSolverIndices()['ADJ.FLOW'])
+    coords = driver.InitialCoordinates()
+
+    for i_node in range(driver.GetNumberNodes() - driver.GetNumberHaloNodes()):
+        y = coords.Get(i_node, 1)
+        dy_dw = y / channel_width
+        size_sens += dy_dw * sensitivity(i_node, 1)
+
+    # Finalize the solver and exit cleanly
+    driver.Finalize()
+
+    return comm.allreduce(size_sens), comm.allreduce(sens)
+
+
+def Phase(t):
+    # 10 cycles per second
+    return 10 * 2 * np.pi * t
+
+
+def DeformationBottom(x, phase):
+    # Deformation between 0.1 and 0.4.
+    if x < 0.1 or x > 0.4:
+        return 0
+    t = (x - 0.1) / 0.3 * 2 * np.pi
+    ampl = (1 - np.cos(t)) / 2
+
+    # Shape parameter, makes the peaks narrower or wider.
+    N = 1
+
+    p = N * (t - phase)
+    denom = N * 2 * np.pi
+    n = round(p / denom)
+    p -= n * denom
+    wave = (1 - np.cos(min(max(0, p + np.pi), 2 * np.pi))) / 2
+
+    return ampl * wave
+
+
+def DeformationTop(x, phase):
+    # Top deforms downward with a phase shift.
+    return -DeformationBottom(x, phase + np.pi)
+
+
+def Deformation(t, amplitude, marker_id, driver, check = False):
+    """
+    Applies the deformation to the marker or checks that the current mesh
+    coordinates (loaded by the adjoint solver) match the expected for the time.
+    """
+    if marker_id < 0:
+        return
+    ini_coords = driver.MarkerInitialCoordinates(marker_id)
+    coords = driver.MarkerCoordinates(marker_id)
+    phase = Phase(t)
+
+    for i_vertex in range(ini_coords.Shape()[0]):
+        x, y = ini_coords.Get(i_vertex)
+        if (y > 1e-3):
+            dy = DeformationTop(x, phase)
+        else:
+            dy = DeformationBottom(x, phase)
+        if not check:
+            driver.SetMarkerCustomDisplacement(marker_id, i_vertex, (0.0, amplitude * dy))
+        else:
+            assert abs((coords(i_vertex, 1) - y) / amplitude - dy) < 1e-9
+
+
+def SumSensitivity(t, marker_id, driver):
+    """Integrates the sensitivity with respect to the amplitude of the deformation."""
+    if marker_id < 0:
+        return
+    ini_coords = driver.MarkerInitialCoordinates(marker_id)
+    phase = Phase(t)
+    sens = 0
+
+    for i_vertex in range(ini_coords.Shape()[0]):
+        i_point = driver.GetMarkerNode(marker_id, i_vertex)
+        if not driver.GetNodeDomain(i_point):
+            continue
+
+        x, y = ini_coords.Get(i_vertex)
+        if (y > 1e-3):
+            dy = DeformationTop(x, phase)
+        else:
+            dy = DeformationBottom(x, phase)
+        sens_x, sens_y = driver.GetMarkerDisplacementSensitivity(marker_id, i_vertex)
+        sens += sens_y * dy
+
+    return sens
+
+
+def main():
+    comm = MPI.COMM_WORLD
+    rank = comm.Get_rank()
+
+    p_drop = RunPrimal(0.055, 0.045)
+    w_sens, a_sens = RunAdjoint(0.055, 0.045)
+
+    # Print results for the regression script to check.
+    # The derivates were verified with finite difference steps of 5e-5.
+    if rank == 0:
+        print("\n------------------------------ Begin Solver -----------------------------\n")
+        print(100, 100, p_drop / 1000, w_sens / 100000, a_sens / 100000, '\n')
+
+
+if __name__ == '__main__':
+  main()
diff --git a/externals/cgns/hdf5/meson.build b/externals/cgns/hdf5/meson.build
index 89cdbaaa2c7..782e1771a28 100644
--- a/externals/cgns/hdf5/meson.build
+++ b/externals/cgns/hdf5/meson.build
@@ -1,6 +1,8 @@
 hdf5_default_warnings = []
 
-if target_machine.system() != 'windows' and meson.get_compiler('c').get_id() != 'intel'
+cc = meson.get_compiler('c')
+
+if target_machine.system() != 'windows' and cc.get_id() != 'intel'
   desired_warnings = ['-Wno-unused-result',
                       '-Wno-unused-parameter',
                       '-Wno-unused-variable',
@@ -16,14 +18,13 @@ if target_machine.system() != 'windows' and meson.get_compiler('c').get_id() !=
                       '-Wno-error=cast-function-type',
                       '-Wno-stringop-truncation']
   foreach flag : desired_warnings
-    if meson.get_compiler('cpp').has_argument(flag)
+    if cc.has_argument(flag)
       hdf5_default_warnings += flag
     endif
   endforeach
 endif
 
-cc = meson.get_compiler('c')
-# Check if can run tests
+# Check if we can run tests
 cc_can_run = not meson.is_cross_build() or meson.has_exe_wrapper()
 
 
@@ -331,33 +332,33 @@ endif
 hdf5_conf_data.set('H5_SIZEOF_FLOAT',            cc.sizeof('float'))
 hdf5_conf_data.set('H5_SIZEOF_DOUBLE',           cc.sizeof('double'))
 hdf5_conf_data.set('H5_SIZEOF_LONG_DOUBLE',      cc.sizeof('long double'))
-                                                 
+
 hdf5_conf_data.set('H5_SIZEOF_INT8_T',           cc.sizeof ('int8_t', prefix:'#include <stdint.h>'))
 hdf5_conf_data.set('H5_SIZEOF_UINT8_T',          cc.sizeof ('uint8_t', prefix:'#include <stdint.h>'))
-hdf5_conf_data.set('H5_SIZEOF_INT_LEAST8_T',     cc.sizeof ('int_least8_t', prefix:'#include <stdint.h>')) 
-hdf5_conf_data.set('H5_SIZEOF_UINT_LEAST8_T',    cc.sizeof ('uint_least8_t', prefix:'#include <stdint.h>')) 
-hdf5_conf_data.set('H5_SIZEOF_INT_FAST8_T',      cc.sizeof ('int_fast8_t', prefix:'#include <stdint.h>'))   
+hdf5_conf_data.set('H5_SIZEOF_INT_LEAST8_T',     cc.sizeof ('int_least8_t', prefix:'#include <stdint.h>'))
+hdf5_conf_data.set('H5_SIZEOF_UINT_LEAST8_T',    cc.sizeof ('uint_least8_t', prefix:'#include <stdint.h>'))
+hdf5_conf_data.set('H5_SIZEOF_INT_FAST8_T',      cc.sizeof ('int_fast8_t', prefix:'#include <stdint.h>'))
 hdf5_conf_data.set('H5_SIZEOF_UINT_FAST8_T',     cc.sizeof ('uint_fast8_t', prefix:'#include <stdint.h>'))
 
-hdf5_conf_data.set('H5_SIZEOF_INT16_T',          cc.sizeof ('int16_t', prefix:'#include <stdint.h>')) 
-hdf5_conf_data.set('H5_SIZEOF_UINT16_T',         cc.sizeof ('uint16_t', prefix:'#include <stdint.h>')) 
+hdf5_conf_data.set('H5_SIZEOF_INT16_T',          cc.sizeof ('int16_t', prefix:'#include <stdint.h>'))
+hdf5_conf_data.set('H5_SIZEOF_UINT16_T',         cc.sizeof ('uint16_t', prefix:'#include <stdint.h>'))
 hdf5_conf_data.set('H5_SIZEOF_INT_LEAST16_T',    cc.sizeof ('int_least16_t', prefix:'#include <stdint.h>'))
 hdf5_conf_data.set('H5_SIZEOF_UINT_LEAST16_T',   cc.sizeof ('uint_least16_t', prefix:'#include <stdint.h>'))
-hdf5_conf_data.set('H5_SIZEOF_INT_FAST16_T',     cc.sizeof ('int_fast16_t', prefix:'#include <stdint.h>')) 
-hdf5_conf_data.set('H5_SIZEOF_UINT_FAST16_T',    cc.sizeof ('uint_fast16_t', prefix:'#include <stdint.h>')) 
+hdf5_conf_data.set('H5_SIZEOF_INT_FAST16_T',     cc.sizeof ('int_fast16_t', prefix:'#include <stdint.h>'))
+hdf5_conf_data.set('H5_SIZEOF_UINT_FAST16_T',    cc.sizeof ('uint_fast16_t', prefix:'#include <stdint.h>'))
 
-hdf5_conf_data.set('H5_SIZEOF_INT32_T',          cc.sizeof ('int32_t', prefix:'#include <stdint.h>')) 
-hdf5_conf_data.set('H5_SIZEOF_UINT32_T',         cc.sizeof ('uint32_t', prefix:'#include <stdint.h>'))      
+hdf5_conf_data.set('H5_SIZEOF_INT32_T',          cc.sizeof ('int32_t', prefix:'#include <stdint.h>'))
+hdf5_conf_data.set('H5_SIZEOF_UINT32_T',         cc.sizeof ('uint32_t', prefix:'#include <stdint.h>'))
 hdf5_conf_data.set('H5_SIZEOF_INT_LEAST32_T',    cc.sizeof ('int_least32_t', prefix:'#include <stdint.h>'))
 hdf5_conf_data.set('H5_SIZEOF_UINT_LEAST32_T',   cc.sizeof ('uint_least32_t', prefix:'#include <stdint.h>'))
-hdf5_conf_data.set('H5_SIZEOF_INT_FAST32_T',     cc.sizeof ('int_fast32_t', prefix:'#include <stdint.h>'))  
-hdf5_conf_data.set('H5_SIZEOF_UINT_FAST32_T',    cc.sizeof ('uint_fast32_t', prefix:'#include <stdint.h>')) 
-                                                
-hdf5_conf_data.set('H5_SIZEOF_INT64_T',          cc.sizeof ('int64_t', prefix:'#include <stdint.h>'))   
-hdf5_conf_data.set('H5_SIZEOF_UINT64_T',         cc.sizeof ('uint64_t', prefix:'#include <stdint.h>')) 
-hdf5_conf_data.set('H5_SIZEOF_INT_LEAST64_T',    cc.sizeof ('int_least64_t', prefix:'#include <stdint.h>')) 
+hdf5_conf_data.set('H5_SIZEOF_INT_FAST32_T',     cc.sizeof ('int_fast32_t', prefix:'#include <stdint.h>'))
+hdf5_conf_data.set('H5_SIZEOF_UINT_FAST32_T',    cc.sizeof ('uint_fast32_t', prefix:'#include <stdint.h>'))
+
+hdf5_conf_data.set('H5_SIZEOF_INT64_T',          cc.sizeof ('int64_t', prefix:'#include <stdint.h>'))
+hdf5_conf_data.set('H5_SIZEOF_UINT64_T',         cc.sizeof ('uint64_t', prefix:'#include <stdint.h>'))
+hdf5_conf_data.set('H5_SIZEOF_INT_LEAST64_T',    cc.sizeof ('int_least64_t', prefix:'#include <stdint.h>'))
 hdf5_conf_data.set('H5_SIZEOF_UINT_LEAST64_T',   cc.sizeof ('uint_least64_t', prefix:'#include <stdint.h>'))
-hdf5_conf_data.set('H5_SIZEOF_INT_FAST64_T',     cc.sizeof ('int_fast64_t', prefix:'#include <stdint.h>'))  
+hdf5_conf_data.set('H5_SIZEOF_INT_FAST64_T',     cc.sizeof ('int_fast64_t', prefix:'#include <stdint.h>'))
 hdf5_conf_data.set('H5_SIZEOF_UINT_FAST64_T',    cc.sizeof ('uint_fast64_t', prefix:'#include <stdint.h>'))
 if target_machine.system() != 'darwin'
   hdf5_conf_data.set('H5_SIZEOF_SIZE_T', cc.sizeof('size_t'))
@@ -376,7 +377,7 @@ endif
 
 hdf5_conf_data.set('H5_SIZEOF_TIME_T', cc.sizeof('time_t', prefix: '#include <sys/time.h>'))
 
-if hdf5_conf_data.get('H5_HAVE_STDBOOL_H') == 1 
+if hdf5_conf_data.get('H5_HAVE_STDBOOL_H') == 1
   hdf5_conf_data.set('H5_SIZEOF_BOOL', cc.sizeof('bool', prefix: '#include <stdbool.h>'))
 else
   hdf5_conf_data.set('H5_SIZEOF_BOOL', cc.sizeof('_Bool'))
@@ -507,49 +508,49 @@ endif
 #-----------------------------------------------------------------------------
 # Check for some functions that are used
 #
-hdf5_conf_data.set('H5_HAVE_ALARM',           cc.has_function ('alarm') )   
-hdf5_conf_data.set('H5_HAVE_FCNTL',           cc.has_function ('fcntl')          )  
-hdf5_conf_data.set('H5_HAVE_FLOCK',           cc.has_function ('flock')         )   
-hdf5_conf_data.set('H5_HAVE_FORK',            cc.has_function ('fork')            )   
-hdf5_conf_data.set('H5_HAVE_FREXPF',          cc.has_function ('frexpf')        )   
-hdf5_conf_data.set('H5_HAVE_FREXPL',          cc.has_function ('frexpl')        )   
-                                             
+hdf5_conf_data.set('H5_HAVE_ALARM',           cc.has_function ('alarm') )
+hdf5_conf_data.set('H5_HAVE_FCNTL',           cc.has_function ('fcntl')          )
+hdf5_conf_data.set('H5_HAVE_FLOCK',           cc.has_function ('flock')         )
+hdf5_conf_data.set('H5_HAVE_FORK',            cc.has_function ('fork')            )
+hdf5_conf_data.set('H5_HAVE_FREXPF',          cc.has_function ('frexpf')        )
+hdf5_conf_data.set('H5_HAVE_FREXPL',          cc.has_function ('frexpl')        )
+
 hdf5_conf_data.set('H5_HAVE_GETHOSTNAME',     cc.has_function ('gethostname') )
-hdf5_conf_data.set('H5_HAVE_GETRUSAGE',       cc.has_function ('getrusage') )   
-hdf5_conf_data.set('H5_HAVE_LLROUND',         cc.has_function ('llround') )   
-hdf5_conf_data.set('H5_HAVE_LLROUNDF',        cc.has_function ('llroundf') )   
-hdf5_conf_data.set('H5_HAVE_LROUND',          cc.has_function ('lround') )   
+hdf5_conf_data.set('H5_HAVE_GETRUSAGE',       cc.has_function ('getrusage') )
+hdf5_conf_data.set('H5_HAVE_LLROUND',         cc.has_function ('llround') )
+hdf5_conf_data.set('H5_HAVE_LLROUNDF',        cc.has_function ('llroundf') )
+hdf5_conf_data.set('H5_HAVE_LROUND',          cc.has_function ('lround') )
 hdf5_conf_data.set('H5_HAVE_LROUNDF',         cc.has_function ('lroundf'))
-hdf5_conf_data.set('H5_HAVE_LSTAT',           cc.has_function ('lstat'))   
-                                             
-hdf5_conf_data.set('H5_HAVE_PREAD',           cc.has_function ('pread') )   
-hdf5_conf_data.set('H5_HAVE_PWRITE',          cc.has_function ('pwrite'))   
-hdf5_conf_data.set('H5_HAVE_RAND_R',          cc.has_function ('rand_r'))  
+hdf5_conf_data.set('H5_HAVE_LSTAT',           cc.has_function ('lstat'))
+
+hdf5_conf_data.set('H5_HAVE_PREAD',           cc.has_function ('pread') )
+hdf5_conf_data.set('H5_HAVE_PWRITE',          cc.has_function ('pwrite'))
+hdf5_conf_data.set('H5_HAVE_RAND_R',          cc.has_function ('rand_r'))
 hdf5_conf_data.set('H5_HAVE_RANDOM',          cc.has_function ('random'))
-hdf5_conf_data.set('H5_HAVE_ROUND',           cc.has_function ('round') )  
-hdf5_conf_data.set('H5_HAVE_ROUNDF',          cc.has_function ('roundf'))   
+hdf5_conf_data.set('H5_HAVE_ROUND',           cc.has_function ('round') )
+hdf5_conf_data.set('H5_HAVE_ROUNDF',          cc.has_function ('roundf'))
 hdf5_conf_data.set('H5_HAVE_SETSYSINFO',      cc.has_function ('setsysinfo'))
-                                             
+
 hdf5_conf_data.set('H5_HAVE_SIGNAL',          cc.has_function ('signal')         )
-hdf5_conf_data.set('H5_HAVE_LONGJMP',         cc.has_function ('longjmp')        )   
-hdf5_conf_data.set('H5_HAVE_SETJMP',          cc.has_function ('setjmp')         ) 
+hdf5_conf_data.set('H5_HAVE_LONGJMP',         cc.has_function ('longjmp')        )
+hdf5_conf_data.set('H5_HAVE_SETJMP',          cc.has_function ('setjmp')         )
 hdf5_conf_data.set('H5_HAVE_SIGLONGJMP',      cc.has_function ('siglongjmp')     )
-hdf5_conf_data.set('H5_HAVE_SIGSETJMP',       cc.has_function ('sigsetjmp')      ) 
+hdf5_conf_data.set('H5_HAVE_SIGSETJMP',       cc.has_function ('sigsetjmp')      )
 hdf5_conf_data.set('H5_HAVE_SIGPROCMASK',     cc.has_function ('sigprocmask')    )
-                                             
-hdf5_conf_data.set('H5_HAVE_SNPRINTF',        cc.has_function ('snprintf')       )  
-hdf5_conf_data.set('H5_HAVE_SRANDOM',         cc.has_function ('srandom')        ) 
-hdf5_conf_data.set('H5_HAVE_STRDUP',          cc.has_function ('strdup')         ) 
+
+hdf5_conf_data.set('H5_HAVE_SNPRINTF',        cc.has_function ('snprintf')       )
+hdf5_conf_data.set('H5_HAVE_SRANDOM',         cc.has_function ('srandom')        )
+hdf5_conf_data.set('H5_HAVE_STRDUP',          cc.has_function ('strdup')         )
 hdf5_conf_data.set('H5_HAVE_STRTOLL',         cc.has_function ('strtoll')        )
-hdf5_conf_data.set('H5_HAVE_STRTOULL',        cc.has_function ('strtoull')      )   
-hdf5_conf_data.set('H5_HAVE_SYMLINK',         cc.has_function ('symlink')        ) 
-hdf5_conf_data.set('H5_HAVE_SYSTEM',          cc.has_function ('system')         ) 
-                                             
+hdf5_conf_data.set('H5_HAVE_STRTOULL',        cc.has_function ('strtoull')      )
+hdf5_conf_data.set('H5_HAVE_SYMLINK',         cc.has_function ('symlink')        )
+hdf5_conf_data.set('H5_HAVE_SYSTEM',          cc.has_function ('system')         )
+
 hdf5_conf_data.set('H5_HAVE_TMPFILE',         cc.has_function ('tmpfile')        )
-hdf5_conf_data.set('H5_HAVE_ASPRINTF',        cc.has_function ('asprintf')       )   
-hdf5_conf_data.set('H5_HAVE_VASPRINTF',       cc.has_function ('vasprintf')      )   
+hdf5_conf_data.set('H5_HAVE_ASPRINTF',        cc.has_function ('asprintf')       )
+hdf5_conf_data.set('H5_HAVE_VASPRINTF',       cc.has_function ('vasprintf')      )
 hdf5_conf_data.set('H5_HAVE_WAITPID',         cc.has_function ('waitpid')        )
-                                             
+
 hdf5_conf_data.set('H5_HAVE_VSNPRINTF',       cc.has_function ('vsnprintf')      )
 
 if cc.has_header_symbol('setjmp.h', 'sigsetjmp')
@@ -870,7 +871,7 @@ H5G_SOURCES =[
     'H5Gtraverse.c']
 
 H5HF_SOURCES = [
-    'H5HF.c', 
+    'H5HF.c',
     'H5HFbtree2.c',
     'H5HFcache.c',
     'H5HFdbg.c',
@@ -1150,7 +1151,7 @@ H5_GENERATED_HEADERS = [
    'H5overflow.h',
     ]
 
-    
+
 # Generate 'H5detect to generate H5Tinit.c
 if cc_can_run
   H5detect = executable('H5detect', 'H5detect.c',
@@ -1189,6 +1190,6 @@ lib_hdf5_embedded = static_library('su2hdf5',
                           c_args: hdf5_default_warnings + defs,
                           dependencies : ext_deps)
 
-hdf5_dep = declare_dependency(link_with: lib_hdf5_embedded, 
+hdf5_dep = declare_dependency(link_with: lib_hdf5_embedded,
                               dependencies: ext_deps,
                               include_directories: hdf5_include)
diff --git a/externals/cgns/meson.build b/externals/cgns/meson.build
index 233f76554a0..95edcb12e40 100644
--- a/externals/cgns/meson.build
+++ b/externals/cgns/meson.build
@@ -1,6 +1,6 @@
 cgns_default_warnings = []
 
-if build_machine.system() != 'windows' and meson.get_compiler('cpp').get_id() != 'intel'
+if build_machine.system() != 'windows' and meson.get_compiler('c').get_id() != 'intel'
   desired_warnings = ['-Wno-unused-result',
                       '-Wno-unused-parameter',
                       '-Wno-unused-variable',
@@ -13,7 +13,7 @@ if build_machine.system() != 'windows' and meson.get_compiler('cpp').get_id() !=
                       '-Wno-error=absolute-value',
                       '-Wno-error=class-memaccess']
   foreach flag : desired_warnings
-    if meson.get_compiler('cpp').has_argument(flag)
+    if meson.get_compiler('c').has_argument(flag)
       cgns_default_warnings += flag
     endif
   endforeach

From 27821b162e0179adda212745b647bc16c58d9641 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Fri, 23 Jun 2023 22:42:58 +0100
Subject: [PATCH 502/656] Update TestCases/parallel_regression_AD.py

---
 TestCases/parallel_regression_AD.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index a54f7dfdeb7..814d2102d36 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -520,7 +520,7 @@ def main():
 
     # Flow AD Mesh Displacement and Initial Coordinates Sensitivity
     pywrapper_wavy_wall_steady = TestCase('pywrapper_wavy_wall_steady')
-    pywrapper_wavy_wall_steady.cfg_dir = "py_wrapper/disc_adj_flow/mesh_disp_sens"
+    pywrapper_wavy_wall_steady.cfg_dir = "py_wrapper/wavy_wall"
     pywrapper_wavy_wall_steady.cfg_file = "run_steady.py"
     pywrapper_wavy_wall_steady.test_iter = 100
     pywrapper_wavy_wall_steady.test_vals = [-1.360044, 2.580709, -2.892473]

From 0911ef2776b8e42af89b4c7587481c920a598482 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Sat, 24 Jun 2023 08:35:27 +0100
Subject: [PATCH 503/656] fix warnings

---
 .github/workflows/regression.yml             | 2 +-
 TestCases/py_wrapper/wavy_wall/run_steady.py | 4 +---
 2 files changed, 2 insertions(+), 4 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 9c85ced8e11..76545cdb274 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c py_wrapper_example -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
diff --git a/TestCases/py_wrapper/wavy_wall/run_steady.py b/TestCases/py_wrapper/wavy_wall/run_steady.py
index 93361a1458f..e65ff6408e9 100644
--- a/TestCases/py_wrapper/wavy_wall/run_steady.py
+++ b/TestCases/py_wrapper/wavy_wall/run_steady.py
@@ -143,7 +143,6 @@ def RunPrimal(channel_width, deform_amplitude):
     Returns the objective function.
     """
     comm = MPI.COMM_WORLD
-    rank = comm.Get_rank()
 
     with open('config.cfg', 'w') as f:
         f.write(common_settings.replace('__WIDTH__', str(channel_width)) + primal_settings)
@@ -175,7 +174,6 @@ def RunAdjoint(channel_width, deform_amplitude):
     Returns the sensitivity of the objective function to the amplitude and width.
     """
     comm = MPI.COMM_WORLD
-    rank = comm.Get_rank()
 
     with open('config_ad.cfg', 'w') as f:
         f.write(common_settings.replace('__WIDTH__', str(channel_width)) + adjoint_settings)
@@ -278,7 +276,7 @@ def Deformation(t, amplitude, marker_id, driver, check = False):
 def SumSensitivity(t, marker_id, driver):
     """Integrates the sensitivity with respect to the amplitude of the deformation."""
     if marker_id < 0:
-        return
+        return 0.0
     ini_coords = driver.MarkerInitialCoordinates(marker_id)
     phase = Phase(t)
     sens = 0

From e7bc2d9ade396866a9c06a1e54aa9731ff006fc2 Mon Sep 17 00:00:00 2001
From: Joseph Signorelli <jms26@illinois.edu>
Date: Sat, 24 Jun 2023 09:59:09 -0500
Subject: [PATCH 504/656] Add local timestep + CFL as volume output

---
 SU2_CFD/src/output/CFlowOutput.cpp | 14 ++++++++++++++
 1 file changed, 14 insertions(+)

diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index 4f7f94f0d02..20b41e7fc79 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -1451,6 +1451,15 @@ void CFlowOutput::SetVolumeOutputFieldsScalarMisc(const CConfig* config) {
     }
     AddVolumeOutput("Q_CRITERION", "Q_Criterion", "VORTEX_IDENTIFICATION", "Value of the Q-Criterion");
   }
+
+  // Timestep info
+  AddVolumeOutput("DELTA_TIME", "Delta_Time", "TIMESTEP", "Value of the local timestep for the flow variables");
+  AddVolumeOutput("CFL", "CFL", "TIMESTEP", "Value of the local CFL for the flow variables");
+  if (config->GetKind_Turb_Model() != TURB_MODEL::NONE)
+  {
+    AddVolumeOutput("TURB_DELTA_TIME", "Turb_Delta_Time", "TIMESTEP", "Value of the local timestep for the turbulence variables");
+    AddVolumeOutput("TURB_CFL", "Turb_CFL", "TIMESTEP", "Value of the local CFL for the turbulence variables");
+  }
 }
 
 void CFlowOutput::LoadVolumeDataScalar(const CConfig* config, const CSolver* const* solver, const CGeometry* geometry,
@@ -1462,6 +1471,9 @@ void CFlowOutput::LoadVolumeDataScalar(const CConfig* config, const CSolver* con
   const auto* Node_Trans = (config->GetKind_Trans_Model() != TURB_TRANS_MODEL::NONE) ? trans_solver->GetNodes() : nullptr;
   const auto* Node_Geo = geometry->nodes;
 
+  SetVolumeOutputValue("DELTA_TIME", iPoint, Node_Flow->GetDelta_Time(iPoint));
+  SetVolumeOutputValue("CFL", iPoint, Node_Flow->GetLocalCFL(iPoint));
+
   if (config->GetViscous()) {
     if (nDim == 3){
       SetVolumeOutputValue("VORTICITY_X", iPoint, Node_Flow->GetVorticity(iPoint)[0]);
@@ -1501,6 +1513,8 @@ void CFlowOutput::LoadVolumeDataScalar(const CConfig* config, const CSolver* con
   /*--- If we got here a turbulence model is being used, therefore there is eddy viscosity. ---*/
   if (config->GetKind_Turb_Model() != TURB_MODEL::NONE) {
     SetVolumeOutputValue("EDDY_VISCOSITY", iPoint, Node_Flow->GetEddyViscosity(iPoint));
+    SetVolumeOutputValue("TURB_DELTA_TIME", iPoint, Node_Turb->GetDelta_Time(iPoint));
+    SetVolumeOutputValue("TURB_CFL", iPoint, Node_Turb->GetLocalCFL(iPoint));
   }
 
   if (config->GetSAParsedOptions().bc) {

From 5b1bc07b17361d85c093d98c203e1cf9a7a1416b Mon Sep 17 00:00:00 2001
From: Joseph Signorelli <jms26@illinois.edu>
Date: Sat, 24 Jun 2023 10:48:31 -0500
Subject: [PATCH 505/656] Added name to AUTHORS.md

---
 AUTHORS.md | 1 +
 1 file changed, 1 insertion(+)

diff --git a/AUTHORS.md b/AUTHORS.md
index 2c2c9d7982e..7ff280cf5e9 100644
--- a/AUTHORS.md
+++ b/AUTHORS.md
@@ -92,6 +92,7 @@ Jessie Lauzon
 João Loureiro
 Johannes Blühdorn
 JonathanSmith1936
+Joseph Signorelli
 Josy P. Pullockara
 Kedar Naik
 Kürşat Yurt

From df7432dfc2f19755ccf3522d589bd7e5a325f0bc Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 25 Jun 2023 15:55:11 +0100
Subject: [PATCH 506/656] fix inconsistency of 1994m and make 2003m the default

---
 Common/include/option_structure.hpp                 | 13 ++++---------
 SU2_CFD/include/numerics/turbulent/turb_sources.hpp | 10 ++--------
 SU2_CFD/src/solvers/CAdjNSSolver.cpp                |  8 ++------
 3 files changed, 8 insertions(+), 23 deletions(-)

diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index ea657b43afd..7f6db2cd81f 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -1033,16 +1033,11 @@ inline SST_ParsedOptions ParseSSTOptions(const SST_OPTIONS *SST_Options, unsigne
 
   if (sst_1994 && sst_2003) {
     SU2_MPI::Error("Two versions (1994 and 2003) selected for SST_OPTIONS. Please choose only one.", CURRENT_FUNCTION);
-  } else if (sst_2003) {
-    SSTParsedOptions.version = SST_OPTIONS::V2003;
-  } else {
+  } else if (sst_1994) {
     SSTParsedOptions.version = SST_OPTIONS::V1994;
-
-    if (rank==MASTER_NODE) {
-      std::cout <<
-        "WARNING: The current SST-1994m model is inconsistent with literature. We recommend using the SST-2003m model.\n"
-        "In SU2 v8 the 2003m model will become default, and the inconsistency will be fixed." << std::endl;
-    }
+  } else {
+    /*--- Default version since v8. ---*/
+    SSTParsedOptions.version = SST_OPTIONS::V2003;
   }
 
   // Parse production modifications
diff --git a/SU2_CFD/include/numerics/turbulent/turb_sources.hpp b/SU2_CFD/include/numerics/turbulent/turb_sources.hpp
index 00d685baa67..541383e6dbd 100644
--- a/SU2_CFD/include/numerics/turbulent/turb_sources.hpp
+++ b/SU2_CFD/include/numerics/turbulent/turb_sources.hpp
@@ -49,7 +49,7 @@ struct CSAVariables {
   const su2double cw1 = cb1 / k2 + (1 + cb2) / sigma;
   const su2double cr1 = 0.5;
   const su2double CRot = 1.0;
-  const su2double c2 = 0.7, c3 = 0.9; 
+  const su2double c2 = 0.7, c3 = 0.9;
 
   /*--- List of auxiliary functions ---*/
   su2double ft2, d_ft2, r, d_r, g, d_g, glim, fw, d_fw, Ji, d_Ji, S, Shat, d_Shat, fv1, d_fv1, fv2, d_fv2;
@@ -805,11 +805,6 @@ class CSourcePieceWise_TurbSST final : public CNumerics {
       const su2double prod_limit = prod_lim_const * beta_star * Density_i * ScalarVar_i[1] * ScalarVar_i[0];
 
       su2double P = Eddy_Viscosity_i * pow(P_Base, 2);
-
-      if (sstParsedOptions.version == SST_OPTIONS::V1994) {
-        /*--- INTRODUCE THE SST-V1994m BUG WHERE DIVERGENCE TERM WILL BE REMOVED ---*/
-        P -= 2.0 / 3.0 * Density_i * ScalarVar_i[0] * diverg;
-      }
       su2double pk = max(0.0, min(P, prod_limit));
 
       const auto& eddy_visc_var = sstParsedOptions.version == SST_OPTIONS::V1994 ? VorticityMag : StrainMag_i;
@@ -818,8 +813,7 @@ class CSourcePieceWise_TurbSST final : public CNumerics {
       /*--- Production limiter only for V2003, recompute for V1994. ---*/
       su2double pw;
       if (sstParsedOptions.version == SST_OPTIONS::V1994) {
-        /*--- INTRODUCE THE SST-V1994m BUG WHERE DIVERGENCE TERM WILL BE REMOVED ---*/
-        pw = alfa_blended * Density_i * max(pow(P_Base, 2) - 2.0 / 3.0 * zeta * diverg, 0.0);
+        pw = alfa_blended * Density_i * pow(P_Base, 2);
       } else {
         pw = (alfa_blended * Density_i / Eddy_Viscosity_i) * pk;
       }
diff --git a/SU2_CFD/src/solvers/CAdjNSSolver.cpp b/SU2_CFD/src/solvers/CAdjNSSolver.cpp
index 75e5e65558b..42dbce29cdf 100644
--- a/SU2_CFD/src/solvers/CAdjNSSolver.cpp
+++ b/SU2_CFD/src/solvers/CAdjNSSolver.cpp
@@ -766,12 +766,8 @@ void CAdjNSSolver::Viscous_Sensitivity(CGeometry *geometry, CSolver **solver_con
             Enthalpy = solver_container[FLOW_SOL]->GetNodes()->GetEnthalpy(iPoint);
 
             /*--- Turbulent kinetic energy ---*/
-            /// TODO: This does not seem to be consistent with the primal treatment.
-            if (config->GetKind_Turb_Model() == TURB_MODEL::SST)
-              val_turb_ke = solver_container[TURB_SOL]->GetNodes()->GetSolution(iPoint,0);
-            else
-              val_turb_ke = 0.0;
-
+            // turb_ke is not considered in the stress tensor, see #797
+            val_turb_ke = 0.0;
             CNumerics::ComputeStressTensor(nDim, tau, PrimVar_Grad+1, Laminar_Viscosity, Density, val_turb_ke);
 
             /*--- Form normal_grad_gridvel = \partial_n (u_omega) ---*/

From 72ea846d4b57a051523ce00c9bda915d82be53c7 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 25 Jun 2023 16:05:19 +0100
Subject: [PATCH 507/656] remove old scripts

---
 SU2_PY/compute_multipoint.py |  68 -------
 SU2_PY/compute_stability.py  |  83 --------
 SU2_PY/config_gui.py         | 365 -----------------------------------
 SU2_PY/convert_to_csv.py     |  64 ------
 SU2_PY/meson.build           |   2 -
 SU2_PY/package_tests.py      | 334 --------------------------------
 6 files changed, 916 deletions(-)
 delete mode 100755 SU2_PY/compute_multipoint.py
 delete mode 100755 SU2_PY/compute_stability.py
 delete mode 100755 SU2_PY/config_gui.py
 delete mode 100755 SU2_PY/convert_to_csv.py
 delete mode 100755 SU2_PY/package_tests.py

diff --git a/SU2_PY/compute_multipoint.py b/SU2_PY/compute_multipoint.py
deleted file mode 100755
index e4641791028..00000000000
--- a/SU2_PY/compute_multipoint.py
+++ /dev/null
@@ -1,68 +0,0 @@
-#!/usr/bin/env python
-
-## \file Compute_multipoint.py
-#  \brief Python script for performing a multipoint design.
-#  \author Indiana Stokes
-#  \version 7.5.1 "Blackbird"
-#
-# SU2 Project Website: https://su2code.github.io
-#
-# The SU2 Project is maintained by the SU2 Foundation
-# (http://su2foundation.org)
-#
-# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
-#
-# SU2 is free software; you can redistribute it and/or
-# modify it under the terms of the GNU Lesser General Public
-# License as published by the Free Software Foundation; either
-# version 2.1 of the License, or (at your option) any later version.
-#
-# SU2 is distributed in the hope that it will be useful,
-# but WITHOUT ANY WARRANTY; without even the implied warranty of
-# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
-# Lesser General Public License for more details.
-#
-# You should have received a copy of the GNU Lesser General Public
-# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
-
-# imports
-import numpy as np
-from optparse import OptionParser
-import os, sys, shutil, copy
-import SU2
-
-# Command Line Options
-parser = OptionParser()
-parser.add_option(
-    "-f", "--file", dest="filename", help="read config from FILE", metavar="FILE"
-)
-parser.add_option(
-    "-n",
-    "--partitions",
-    dest="partitions",
-    default=2,
-    help="number of PARTITIONS",
-    metavar="PARTITIONS",
-)
-
-(options, args) = parser.parse_args()
-options.partitions = int(options.partitions)
-
-# load config, start state
-config = SU2.io.Config(options.filename)
-state = SU2.io.State()
-
-# prepare config
-config.NUMBER_PART = options.partitions
-
-# find solution files if they exist
-state.find_files(config)
-
-# run su2
-multipoint_drag = SU2.eval.func("MULTIPOINT_DRAG", config, state)
-grad_multipoint_drag = SU2.eval.grad(
-    "MULTIPOINT_DRAG", "CONTINUOUS_ADJOINT", config, state
-)
-
-print("MULTIPOINT_DRAG     =", multipoint_drag)
-print("GRADIENT MULTIPOINT_DRAG =", grad_multipoint_drag)
diff --git a/SU2_PY/compute_stability.py b/SU2_PY/compute_stability.py
deleted file mode 100755
index b727782d7de..00000000000
--- a/SU2_PY/compute_stability.py
+++ /dev/null
@@ -1,83 +0,0 @@
-#!/usr/bin/env python
-
-## \file compute_stability.py
-#  \brief Python script for performing the shape optimization.
-#  \author T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
-#
-# SU2 Project Website: https://su2code.github.io
-#
-# The SU2 Project is maintained by the SU2 Foundation
-# (http://su2foundation.org)
-#
-# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
-#
-# SU2 is free software; you can redistribute it and/or
-# modify it under the terms of the GNU Lesser General Public
-# License as published by the Free Software Foundation; either
-# version 2.1 of the License, or (at your option) any later version.
-#
-# SU2 is distributed in the hope that it will be useful,
-# but WITHOUT ANY WARRANTY; without even the implied warranty of
-# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
-# Lesser General Public License for more details.
-#
-# You should have received a copy of the GNU Lesser General Public
-# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
-
-# make print(*args) function available in PY2.6+, does'nt work on PY < 2.6
-from __future__ import print_function
-
-# imports
-from optparse import OptionParser
-import SU2
-
-# Command Line Options
-parser = OptionParser()
-parser.add_option(
-    "-f", "--file", dest="filename", help="read config from FILE", metavar="FILE"
-)
-parser.add_option(
-    "-n",
-    "--partitions",
-    dest="partitions",
-    default=2,
-    help="number of PARTITIONS",
-    metavar="PARTITIONS",
-)
-parser.add_option(
-    "-i",
-    "--iterations",
-    dest="iterations",
-    default=99999,
-    help="number of ITERATIONS",
-    metavar="ITERATIONS",
-)
-
-(options, args) = parser.parse_args()
-options.partitions = int(options.partitions)
-options.iterations = int(options.iterations)
-
-# load config, start state
-config = SU2.io.Config(options.filename)
-state = SU2.io.State()
-
-# prepare config
-config.NUMBER_PART = options.partitions
-config.EXT_ITER = options.iterations
-
-# find solution files if they exist
-state.find_files(config)
-
-# run su2
-drag_alpha = SU2.eval.func("D_DRAG_D_ALPHA", config, state)
-moment_y_alpha = SU2.eval.func("D_MOMENT_Z_D_ALPHA", config, state)
-
-grad_moment_y_alpha = SU2.eval.grad(
-    "D_MOMENT_Z_D_ALPHA", "CONTINUOUS_ADJOINT", config, state
-)
-
-print("D_DRAG_D_ALPHA     =", drag_alpha)
-print("D_MOMENT_Y_D_ALPHA =", moment_y_alpha)
-
-print("DD_MOMENT_Y_D_ALPHA_D_X =", grad_moment_y_alpha)
diff --git a/SU2_PY/config_gui.py b/SU2_PY/config_gui.py
deleted file mode 100755
index 293a6c92c9f..00000000000
--- a/SU2_PY/config_gui.py
+++ /dev/null
@@ -1,365 +0,0 @@
-#!/usr/bin/env python
-
-## \file config_gui.py
-#  \brief _____________.
-#  \author A. Aranake
-#  \version 7.5.1 "Blackbird"
-#
-# SU2 Project Website: https://su2code.github.io
-#
-# The SU2 Project is maintained by the SU2 Foundation
-# (http://su2foundation.org)
-#
-# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
-#
-# SU2 is free software; you can redistribute it and/or
-# modify it under the terms of the GNU Lesser General Public
-# License as published by the Free Software Foundation; either
-# version 2.1 of the License, or (at your option) any later version.
-#
-# SU2 is distributed in the hope that it will be useful,
-# but WITHOUT ANY WARRANTY; without even the implied warranty of
-# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
-# Lesser General Public License for more details.
-#
-# You should have received a copy of the GNU Lesser General Public
-# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
-
-# make print(*args) function available in PY2.6+, does'nt work on PY < 2.6
-from __future__ import print_function
-
-from parse_config import *
-import wx, sys
-import wx.lib.scrolledpanel as sp
-
-
-# ctrldict is a dictionary
-# keys of ctrldict are option categories
-# Values of ctrldict are lists (optlist) of lists (option_data)
-# option_data takes the form [option_name, option_value, StaticText,Control]
-
-
-class YesNoBox(wx.CheckBox):
-    """The regular checkbox returns True or False, this one returns YES or NO to match the SU2 config format."""
-
-    def __init__(self, parent, *args, **kwargs):
-        wx.CheckBox.__init__(self, parent, *args, **kwargs)
-
-    def GetValue(self):
-        if self.Value:
-            return "YES"
-        else:
-            return "NO"
-
-    def SetValue(self, stringval):
-        if stringval == "YES":
-            self.Value = True
-        else:
-            self.Value = False
-
-
-class LabeledComboBox:
-    """Wrap a StaticText and TextCtrl into a single object"""
-
-    def __init__(
-        self,
-        parent,
-        option_name,
-        txtlabel,
-        option_default,
-        option_values,
-        option_type,
-        option_description,
-    ):
-        self.label = wx.StaticText(parent, label=txtlabel + ", " + option_type)
-        self.option_name = option_name
-        self.control = wx.ComboBox(parent, value=option_default, choices=option_values)
-        self.control.SetSize((400, 20))
-        self.sizer = wx.BoxSizer(wx.HORIZONTAL)
-        self.sizer.Add(self.label, wx.EXPAND)
-        self.sizer.AddSpacer(20)
-        self.sizer.Add(self.control, wx.EXPAND)
-        self.sizer.SetMinSize((400, 20))
-
-        self.option_default = option_default
-        self.option_type = option_type
-        self.option_description = option_description
-
-    def GetSizer(self):
-        return self.sizer
-
-    def GetValue(self):
-        return self.control.GetValue()
-
-    def SetValue(self, val):
-        self.control.SetValue(val)
-
-    def SetDefaultValue(self):
-        self.control.SetValue(self.option_default)
-
-    def GetCtrl(self):
-        return self.control
-
-
-class LabeledTextCtrl:
-    """Wrap a StaticText and TextCtrl into a single object"""
-
-    def __init__(self, parent, option_name, txtlabel, option_default, option_type):
-        self.label = wx.StaticText(parent, label=txtlabel + ", " + option_type)
-        self.option_name = option_name
-        self.control = wx.TextCtrl(parent, value=option_default)
-        self.control.SetSize((400, 20))
-        self.sizer = wx.BoxSizer(wx.HORIZONTAL)
-        self.sizer.Add(self.label, wx.EXPAND)
-        self.sizer.AddSpacer(20)
-        self.sizer.Add(self.control, wx.EXPAND)
-        self.sizer.SetMinSize((400, 20))
-
-        self.option_default = option_default
-        self.option_type = option_type
-
-    def GetSizer(self):
-        return self.sizer
-
-    def GetValue(self):
-        return self.control.GetValue()
-
-    def SetValue(self, val):
-        self.control.SetValue(val)
-
-    def SetDefaultValue(self):
-        self.control.SetValue(self.option_default)
-
-    def GetCtrl(self):
-        return self.control
-
-
-class config_gui(wx.Frame):
-    def __init__(self, option_data):
-
-        # wx Initialization
-        wx.Frame.__init__(self, None, title="SU2 config file editor")
-
-        # Define the main sizers
-        self.frame_sizer = wx.BoxSizer(wx.HORIZONTAL)
-        self.main_sizer = wx.BoxSizer(wx.HORIZONTAL)
-        self.left_sizer = wx.BoxSizer(wx.VERTICAL)
-        self.right_sizer = wx.BoxSizer(wx.VERTICAL)
-
-        # Use a scrolled panel on the right side
-        self.main_panel = wx.Panel(self)
-        self.scroll_sizer = wx.BoxSizer(wx.VERTICAL)
-        self.right_panel = sp.ScrolledPanel(self.main_panel, size=(500, 500))
-        self.right_panel.SetupScrolling()
-
-        # Left side - list of option categories
-        self.list_ctrl = wx.ListCtrl(
-            self.main_panel, style=wx.LC_REPORT | wx.BORDER_SUNKEN, size=(300, 600)
-        )
-        self.list_ctrl.InsertColumn(0, "Option Category")
-
-        bigfont = wx.Font(20, wx.MODERN, wx.NORMAL, wx.BOLD)
-
-        # Read the option_data and build controls
-        self.ctrldict = {}
-        self.optlabels = {}
-        for j, category in enumerate(option_data):
-
-            self.list_ctrl.InsertStringItem(
-                j, category
-            )  # Add category to left size list
-
-            self.optlabels[category] = wx.StaticText(self.right_panel, label=category)
-            self.optlabels[category].SetFont(bigfont)
-
-            if j > 0:
-                self.scroll_sizer.AddSpacer(20)
-            self.scroll_sizer.Add(self.optlabels[category], wx.EXPAND)
-
-            self.ctrldict[category] = []
-            yctr = 0
-            for j, opt in enumerate(option_data[category]):
-                if opt.option_type in [
-                    "EnumOption",
-                    "MathProblem",
-                    "SpecialOption",
-                    "ConvectOption",
-                ]:
-                    self.ctrldict[category].append(
-                        LabeledComboBox(
-                            self.right_panel,
-                            opt.option_name,
-                            opt.option_name,
-                            opt.option_default,
-                            opt.option_values,
-                            opt.option_type,
-                            opt.option_description,
-                        )
-                    )
-                else:
-                    self.ctrldict[category].append(
-                        LabeledTextCtrl(
-                            self.right_panel,
-                            opt.option_name,
-                            opt.option_name,
-                            opt.option_default,
-                            opt.option_type,
-                        )
-                    )
-
-            for control in self.ctrldict[category]:
-                self.scroll_sizer.Add(
-                    control.GetSizer(), wx.EXPAND
-                )  # Add each control to the sizer
-                self.lastctrl = control.GetCtrl()
-
-        # Set right_panel to scroll vertically
-        self.right_panel.SetSizer(self.scroll_sizer)
-
-        # Set up menu
-        menuBar = wx.MenuBar()
-        m_file = wx.Menu()
-        m_save = m_file.Append(wx.ID_SAVE, "&Save", "Save an SU2 .cfg file")
-        m_open = m_file.Append(wx.ID_OPEN, "&Open", "Load an SU2 .cfg file")
-        m_exit = m_file.Append(wx.ID_EXIT, "E&xit", "Close window and exit program.")
-
-        menuBar.Append(m_file, "&File")
-        self.SetMenuBar(menuBar)
-        self.CreateStatusBar()
-
-        # Specify which functions to call when stuff is changed
-        self.Bind(wx.EVT_LIST_ITEM_SELECTED, self.list_click, self.list_ctrl)
-        self.Bind(wx.EVT_MENU, self.OnSave, m_save)
-        self.Bind(wx.EVT_MENU, self.OnOpen, m_open)
-        self.Bind(wx.EVT_SIZE, self.OnResize)
-        self.right_panel.SetAutoLayout(1)
-
-        # Add it all to the panel and draw
-        self.left_sizer.SetMinSize((300, 600))
-        self.right_sizer.SetMinSize((300, 600))
-        self.list_ctrl.SetColumnWidth(0, 500)
-
-        self.left_sizer.Add(self.list_ctrl, 0, wx.EXPAND)
-        self.right_sizer.Add(self.right_panel, 0, wx.EXPAND)
-        self.main_sizer.Add(self.left_sizer, 0, wx.EXPAND)
-        self.main_sizer.Add(self.right_sizer, 0, wx.EXPAND)
-        self.frame_sizer.Add(self.main_sizer, 0, wx.EXPAND)
-
-        self.main_panel.SetSizer(self.main_sizer)
-        self.SetSizer(self.frame_sizer)
-        self.SetInitialSize()
-
-    def OnCheck(self, event):
-        print(event)
-        print(dir(event))
-        print(event.GetEventObject())
-        print(event.GetEventObject().GetValue())
-
-    def OnResize(self, event):
-        # There is surely a better way to do this....
-        framesize = self.GetSize()
-        self.main_panel.SetSize(framesize)
-        self.list_ctrl.SetSize((300, framesize[1] - 50))
-        self.right_panel.SetSize((framesize[0] - 300, framesize[1] - 50))
-
-    def OnSave(self, event):
-
-        # Dialog to set output filename
-        SaveDialog = wx.FileDialog(self, style=wx.FD_SAVE, wildcard="*.cfg")
-        SaveDialog.ShowModal()
-        outfile = SaveDialog.GetPath()
-
-        f = open(outfile, "w")
-
-        for category, optlist in self.ctrldict.items():
-            f.write("%% %s \n" % category)
-            for option in optlist:
-                value = option.GetValue()
-                if not value == "":
-                    f.write("%s=%s\n" % (option.option_name, option.GetValue()))
-        f.close()
-
-    def OnOpen(self, event):
-
-        # Dialog to select file
-        OpenDialog = wx.FileDialog(self, wildcard="*.cfg")
-        OpenDialog.ShowModal()
-        infile = OpenDialog.GetPath()
-
-        # Open file, Load values into a dictionary
-        cfgfile = open(infile, "r")
-        infiledict = {}
-        lines = cfgfile.readlines()
-        for line in lines:
-            if line[0] == "%" or line.find("=") == -1:  # Skip lines w/o = sign
-                continue
-            else:  # Get value
-                key, val = [text.strip() for text in line.split("=")]
-                key = key.upper()  # AoA should work as well as AOA
-                infiledict[key] = val
-
-        # Loop through controls and set them to the new values
-        for category, optlist in self.ctrldict.items():
-            for option in optlist:
-                if option.option_name in infiledict:
-                    option.SetValue(infiledict[option.option_name])
-                else:
-                    option.SetValue("")
-
-    def OnClose(self, event):
-        sys.exit(1)
-
-    def OnAbout(self, event):
-        print("OnAbout")
-
-    def list_click(self, event):
-
-        category = event.GetText()
-
-        self.right_panel.ScrollChildIntoView(self.lastctrl)
-        self.right_panel.ScrollChildIntoView(self.optlabels[category])
-
-
-def prepare_data():
-    """Method to get configuration data from source files.
-    Outputs a dictionary of categories as keys and lists of config_options as values
-    """
-
-    # These variables should point to the configuration files
-    su2_basedir = os.environ["SU2_HOME"]
-    config_cpp = os.path.join(su2_basedir, "Common/src/config_structure.cpp")
-    config_hpp = os.path.join(su2_basedir, "Common/include/option_structure.hpp")
-
-    # Check that files exist
-    if not os.path.isfile(config_cpp):
-        sys.exit(
-            "Could not find cpp file, please check that su2_basedir is set correctly in config_gui.py"
-        )
-    if not os.path.isfile(config_hpp):
-        sys.exit(
-            "Could not find hpp file, please check that su2_basedir is set correctly in config_gui.py"
-        )
-
-    # Run the parser
-    option_list = parse_config(config_cpp, config_hpp)
-
-    # Organize data into dictionary with categories as keys
-    option_data = {}
-    for opt in option_list:
-        if not opt.option_category in option_data:
-            option_data[opt.option_category] = []
-        option_data[opt.option_category].append(opt)
-
-    return option_data
-
-
-if __name__ == "__main__":
-
-    # Read source files, get option data
-    option_data = prepare_data()
-
-    # Launch GUI
-    app = wx.App(None)
-    frame = config_gui(option_data)
-    frame.Show()
-    app.MainLoop()
diff --git a/SU2_PY/convert_to_csv.py b/SU2_PY/convert_to_csv.py
deleted file mode 100755
index 32b13cace83..00000000000
--- a/SU2_PY/convert_to_csv.py
+++ /dev/null
@@ -1,64 +0,0 @@
-#!/usr/bin/env python
-
-## \file convert_to_csv.py
-#  \brief This script converts SU2 ASCII restart files generated with a version prior v7 to the CSV format
-#  \author T. Albring
-#  \version 7.5.1 "Blackbird"
-#
-# SU2 Project Website: https://su2code.github.io
-#
-# The SU2 Project is maintained by the SU2 Foundation
-# (http://su2foundation.org)
-#
-# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
-#
-# SU2 is free software; you can redistribute it and/or
-# modify it under the terms of the GNU Lesser General Public
-# License as published by the Free Software Foundation; either
-# version 2.1 of the License, or (at your option) any later version.
-#
-# SU2 is distributed in the hope that it will be useful,
-# but WITHOUT ANY WARRANTY; without even the implied warranty of
-# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
-# Lesser General Public License for more details.
-#
-# You should have received a copy of the GNU Lesser General Public
-# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
-
-from optparse import OptionParser
-import os
-
-parser = OptionParser(
-    usage="%prog -i INPUT_FILE",
-    description="This script converts SU2 ASCII restart files generated with a version prior v7 to the CSV format",
-)
-parser.add_option(
-    "-i",
-    "--inputfile",
-    dest="infile",
-    help="ASCII restart file (*.dat)",
-    metavar="INPUT_FILE",
-)
-(options, args) = parser.parse_args()
-
-
-infile = open(options.infile, "r")
-out_name = options.infile.split(".")[0] + ".csv"
-if os.path.isfile(out_name):
-    print("File " + out_name + " already exists.")
-    exit(1)
-outfile = open(out_name, "w")
-
-while 1:
-    line = infile.readline()
-    if not line:
-        break
-
-    line = line.split()
-    for i, val in enumerate(line):
-        outfile.write(val.strip())
-        if i != len(line) - 1:
-            outfile.write(", ")
-    outfile.write("\n")
-
-print("Converted " + options.infile + " to " + out_name)
diff --git a/SU2_PY/meson.build b/SU2_PY/meson.build
index 38136b25db9..85ae325f3f0 100644
--- a/SU2_PY/meson.build
+++ b/SU2_PY/meson.build
@@ -4,12 +4,10 @@ install_data(['continuous_adjoint.py',
 	     'mesh_deformation.py',
 	     'parallel_computation.py',
 	     'parallel_computation_fsi.py',
-	     'package_tests.py',
 	     'shape_optimization.py',
 	     'merge_solution.py',
 	     'set_ffd_design_var.py',
 	     'compute_polar.py',
-	     'compute_multipoint.py',
 	     'discrete_adjoint.py',
 	     'direct_differentiation.py',
 	     'fsi_computation.py',
diff --git a/SU2_PY/package_tests.py b/SU2_PY/package_tests.py
deleted file mode 100755
index 186f86e4ec5..00000000000
--- a/SU2_PY/package_tests.py
+++ /dev/null
@@ -1,334 +0,0 @@
-#!/usr/bin/env python
-
-## \file package_tests.py
-#  \brief _____________.
-#  \author T. Lukaczyk
-#  \version 7.5.1 "Blackbird"
-#
-# SU2 Project Website: https://su2code.github.io
-#
-# The SU2 Project is maintained by the SU2 Foundation
-# (http://su2foundation.org)
-#
-# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
-#
-# SU2 is free software; you can redistribute it and/or
-# modify it under the terms of the GNU Lesser General Public
-# License as published by the Free Software Foundation; either
-# version 2.1 of the License, or (at your option) any later version.
-#
-# SU2 is distributed in the hope that it will be useful,
-# but WITHOUT ANY WARRANTY; without even the implied warranty of
-# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
-# Lesser General Public License for more details.
-#
-# You should have received a copy of the GNU Lesser General Public
-# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
-
-# make print(*args) function available in PY2.6+, does'nt work on PY < 2.6
-from __future__ import print_function
-
-import os, sys, copy
-
-sys.path.append(os.environ["SU2_RUN"])
-import SU2
-
-from collections import OrderedDict
-
-# todo:
-# verify command line interface
-# commenting
-# verify optimization, gradients, flow solutions
-# verbosity
-# plotting
-# verbose redirection
-# pyopt optimizers
-
-
-# needed config options
-# OPT_CONSTRAINT
-# OPT_OBJECTIVE
-# CONSOLE
-
-# OUTPUT_WEIGHT
-# FINDIFF_STEP
-# DOT_FINDIFF_STEP
-# GRADIENT_METHOD= FINITE_DIFFERENCING, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT
-# ADAPTATION= DIRECT, ADJOINT
-
-
-def main():
-
-    # io0()       # working
-    # io1()
-    # level0()    # working
-    # level1()    # working
-    # level2()    # working
-    # level3()    # working
-    # level4()    # working
-    # level5()    # working
-
-    print("DONE!")
-
-
-def io0():
-    folder = "test_io0"
-    pull = "config_NACA0012.cfg"
-    link = "mesh_NACA0012.su2"
-    with SU2.io.redirect_folder(folder, pull, link):
-
-        config_name = "config_NACA0012.cfg"
-        config = SU2.io.Config(filename=config_name)
-
-        print(config)
-
-        config.ADAPT_CYCLES
-        config["ADAPT_CYCLES"]
-
-        config.dump("out.cfg")
-
-        konfig = copy.deepcopy(config)
-        konfig["TASKS"] = ["TEST"]
-        konfig["NUMBER_PART"] = 0
-
-        config_diff = config.diff(konfig)
-
-        print(config_diff)
-
-    wait = 0
-
-
-def io1():
-
-    option = SU2.io.config.MathProblem()
-
-    option = "DIRECT"
-
-    wait = 0
-
-
-def level0():
-    folder = "test_level0"
-    pull = "config_NACA0012.cfg"
-    link = "mesh_NACA0012.su2"
-    with SU2.io.redirect_folder(folder, pull, link):
-
-        # Setup
-        config_name = "config_NACA0012.cfg"
-        config = SU2.io.Config(config_name)
-        config.EXT_ITER = 9
-        config.NUMBER_PART = 2
-
-        SU2.run.CFD(config)
-
-
-def level1():
-    folder = "test_level1"
-    pull = "config_NACA0012.cfg"
-    link = "mesh_NACA0012.su2"
-    with SU2.io.redirect_folder(folder, pull, link):
-
-        # Setup
-        config_name = "config_NACA0012.cfg"
-        config = SU2.io.Config(config_name)
-        config["NUMBER_PART"] = 2
-        config["EXT_ITER"] = 9
-
-        state = SU2.io.State()
-
-        # Deformation
-        dv_new = [0.002] * 38
-        info = SU2.run.deform(config, dv_new)
-        state.update(info)
-
-        # Direct Solution
-        info = SU2.run.direct(config)
-        state.update(info)
-        SU2.io.restart2solution(config, state)
-
-        # Adjoint Solution
-        info = SU2.run.adjoint(config)
-        state.update(info)
-        SU2.io.restart2solution(config, state)
-
-        # Gradient Projection
-        info = SU2.run.projection(config)
-        state.update(info)
-
-        print(state)
-
-        SU2.io.save_data("state.pkl", state)
-        data = SU2.io.load_data("state.pkl")
-
-        SU2.io.save_data("config.pkl", config)
-        data = SU2.io.load_data("config.pkl")
-
-    wait = 0
-
-
-def level2():
-    folder = "test_level2"
-    pull = "config_NACA0012.cfg"
-    link = "mesh_NACA0012.su2"
-    with SU2.io.redirect_folder(folder, pull, link):
-
-        # Setup
-        config_name = "config_NACA0012.cfg"
-        config = SU2.io.Config(config_name)
-        config["NUMBER_PART"] = 2
-        config["EXT_ITER"] = 9
-        dv_new = [0.0] * 38
-        # dv_new[10] = 0.05
-        config.unpack_dvs(dv_new)
-
-        state = SU2.io.State()
-
-        # with SU2.io.redirect.folder(folder='JOB_001',link='mesh_NACA0012.su2'):
-        #    grad = SU2.eval.grad( 'DRAG', 'FINDIFF', config, state )
-
-        with SU2.io.redirect_folder(folder="JOB_001", link="mesh_NACA0012.su2"):
-            func = SU2.eval.func("LIFT", config, state)
-            grads = SU2.eval.grad("LIFT", "CONTINUOUS_ADJOINT", config, state)
-
-        with SU2.io.redirect_folder(folder="JOB_001", link="mesh_NACA0012.su2"):
-            func = SU2.eval.func("DRAG", config, state)  # will not run direct
-            grads = SU2.eval.grad(
-                "LIFT", "CONTINUOUS_ADJOINT", config, state
-            )  # will not run adjoint
-            grads = SU2.eval.grad(
-                "DRAG", "CONTINUOUS_ADJOINT", config, state
-            )  # will run adjoint
-
-    wait = 0
-
-
-def level3():
-    folder = "test_level3"
-    pull = "config_NACA0012.cfg"
-    link = "mesh_NACA0012.su2"
-    with SU2.io.redirect_folder(folder, pull, link):
-
-        # Setup
-        config_name = "config_NACA0012.cfg"
-        config = SU2.io.Config(config_name)
-        config["NUMBER_PART"] = 2
-        config["EXT_ITER"] = 9
-
-        # initialize design state
-        state = SU2.io.State()
-        state.find_files(config)
-
-        # start design
-        design = SU2.eval.Design(config, state)
-
-        # run design with dv change
-        dv_new = [0.0] * 38
-        vals = design.obj_f(dv_new)
-        vals = design.obj_df(dv_new)
-        vals = design.con_ceq(dv_new)
-        vals = design.con_dceq(dv_new)
-        vals = design.con_cieq(dv_new)
-        vals = design.con_dcieq(dv_new)
-        vals = design.func("LIFT")
-        vals = design.grad("LIFT", "CONTINUOUS_ADJOINT")
-
-        SU2.io.save_data("design.pkl", design)
-        data = SU2.io.load_data("design.pkl")
-
-    wait = 0
-
-
-def level4():
-    folder = "test_level4"
-    pull = "config_NACA0012.cfg"
-    link = "mesh_NACA0012.su2"
-    with SU2.io.redirect_folder(folder, pull, link):
-
-        # Setup
-        config_name = "config_NACA0012.cfg"
-        config = SU2.io.Config(config_name)
-        config["NUMBER_PART"] = 2
-        config["EXT_ITER"] = 9
-        config.CONSOLE = "QUIET"
-
-        # initialize design state
-        state = SU2.io.State()
-        state.find_files(config)
-
-        # initialize project
-        project = SU2.opt.Project(config, state)
-
-        # run project with dv changes
-        dv_new = [0.0] * 38
-        vals = project.obj_f(dv_new)
-        vals = project.obj_df(dv_new)
-
-        dv_new = [-0.005] * 38
-        vals = project.obj_f(dv_new)
-
-        dv_new = [0.0] * 38
-        dv_new[9] = -0.02
-        vals = project.obj_f(dv_new)
-
-        dv_new = [0.005] * 38
-        vals = project.obj_f(dv_new)  # will not rerun solutions
-
-        SU2.io.save_data("project.pkl", project)
-        data = SU2.io.load_data("project.pkl")
-
-        data = project.data
-
-    wait = 0
-    print("Done!")
-
-
-def level5():
-    folder = "test_level5"
-    pull = "config_NACA0012.cfg"
-    link = "mesh_NACA0012.su2"
-    with SU2.io.redirect_folder(folder, pull, link):
-
-        # Setup
-        config_name = "config_NACA0012.cfg"
-        config = SU2.io.Config(config_name)
-        config["NUMBER_PART"] = 2
-        config["EXT_ITER"] = 9
-        config["CONSOLE"] = "CONCISE"
-
-        # set optimization problem
-        obj = {}
-        obj["DRAG"] = {"SCALE": 1.0e-2}
-
-        cons = {}
-        cons["EQUALITY"] = {}
-        cons["INEQUALITY"] = {}
-        cons["INEQUALITY"]["LIFT"] = {"SIGN": ">", "VALUE": 0.328188, "SCALE": 1e-1}
-        cons["INEQUALITY"]["MOMENT_Z"] = {"SIGN": ">", "VALUE": 0.034068, "SCALE": 1e-2}
-
-        def_dv = config.DEFINITION_DV
-        n_dv = sum(def_dv["KIND"])
-        def_dv["SCALE"] = [1.0e0] * n_dv
-
-        config.OPT_OBJECTIVE = obj
-        config.OPT_CONSTRAINT = cons
-
-        # initialize design state
-        state = SU2.io.State()
-        state.find_files(config)
-
-        # initialize project
-        project = SU2.opt.Project(config, state)
-
-        # optimization setup
-        x0 = [0.0] * n_dv
-        xb = []  # [[-0.02,0.02]]*n_dv
-        its = 20
-
-        # optimize
-        SU2.opt.SLSQP(project, x0, xb, its)
-
-    wait = 0
-
-
-if __name__ == "__main__":
-    main()

From b9fc5456c32490ebf45c58f8ea26516511a5f132 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 26 Jun 2023 12:02:38 +0200
Subject: [PATCH 508/656] Fixed density model implementation for flamelet fluid
 model

---
 Common/include/CConfig.hpp                    |  7 ++++++
 Common/src/CConfig.cpp                        |  4 +++-
 SU2_CFD/src/fluid/CFluidFlamelet.cpp          | 22 +++++++++----------
 .../src/numerics/flow/convection/centered.cpp |  4 ++--
 SU2_CFD/src/numerics/flow/convection/fds.cpp  |  2 +-
 SU2_CFD/src/numerics/flow/flow_sources.cpp    |  2 +-
 SU2_CFD/src/output/CFlowOutput.cpp            |  2 +-
 SU2_CFD/src/solvers/CIncEulerSolver.cpp       |  2 +-
 .../src/solvers/CSpeciesFlameletSolver.cpp    |  3 ++-
 .../lam_prem_ch4_cfd.cfg                      |  2 +-
 .../lam_prem_ch4_hx_ad.cfg                    |  2 +-
 .../lam_prem_ch4_hx_dot.cfg                   |  2 +-
 .../lam_prem_ch4_cht_cfd_fluid.cfg            |  2 +-
 .../lam_prem_ch4_cht_ad_fluid.cfg             |  2 +-
 .../lam_prem_ch4_cfd_axi.cfg                  |  2 +-
 config_template.cfg                           |  5 +++--
 16 files changed, 38 insertions(+), 27 deletions(-)

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index fe6e42176be..cec6e4cd140 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -903,6 +903,7 @@ class CConfig {
   Tke_FreeStreamND,           /*!< \brief Farfield kinetic energy (external flow). */
   Omega_FreeStreamND,         /*!< \brief Specific dissipation (external flow). */
   Omega_FreeStream;           /*!< \brief Specific dissipation (external flow). */
+  bool Variable_Density;      /*!< \brief Variable density for incompressible flow. */
   unsigned short nElectric_Constant;    /*!< \brief Number of different electric constants. */
   su2double *Electric_Constant;         /*!< \brief Dielectric constant modulus. */
   su2double Knowles_B,                  /*!< \brief Knowles material model constant B. */
@@ -3864,6 +3865,12 @@ class CConfig {
    */
   INC_DENSITYMODEL GetKind_DensityModel() const { return Kind_DensityModel; }
 
+  /*!
+   * \brief Selection of variable density option for incompressible flows.
+   * \return Flag for variable density for incompressible flows.
+   */
+  bool GetVariable_Density_Model() const { return Variable_Density; }
+
   /*!
    * \brief Flag for whether to solve the energy equation for incompressible flows.
    * \return Flag for energy equation
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 08b1ace33e7..d268651dcfe 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -3836,6 +3836,8 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
   SetDefaultIfEmpty(Prandtl_Turb, nPrandtl_Turb, Prandtl_Turb_Default);
   SetDefaultIfEmpty(Constant_Lewis_Number, nConstant_Lewis_Number, Lewis_Number_Default);
 
+  Variable_Density = ((Kind_DensityModel == INC_DENSITYMODEL::VARIABLE) || (Kind_DensityModel == INC_DENSITYMODEL::FLAMELET));
+
   /*--- Check whether inputs for FLUID_MIXTURE are correctly specified. ---*/
 
     if (Kind_FluidModel == FLUID_MIXTURE) {
@@ -3931,7 +3933,7 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
                        CURRENT_FUNCTION);
       }
 
-      if ((Kind_DensityModel != INC_DENSITYMODEL::VARIABLE) && (Kind_DensityModel != INC_DENSITYMODEL::FLAMELET)) {
+      if (!Variable_Density) {
         SU2_MPI::Error("The use of FLUID_FLAMELET requires the INC_DENSITY_MODEL option to be VARIABLE or FLAMELET",
                        CURRENT_FUNCTION);
       }
diff --git a/SU2_CFD/src/fluid/CFluidFlamelet.cpp b/SU2_CFD/src/fluid/CFluidFlamelet.cpp
index feb0244826c..770604bdc64 100644
--- a/SU2_CFD/src/fluid/CFluidFlamelet.cpp
+++ b/SU2_CFD/src/fluid/CFluidFlamelet.cpp
@@ -83,18 +83,18 @@ void CFluidFlamelet::SetTDState_T(su2double val_temperature, const su2double* va
   mass_diffusivity = val_vars_TD[LOOKUP_TD::DIFFUSIONCOEFFICIENT];
   switch (density_model)
   {
-  case INC_DENSITYMODEL::FLAMELET:
-    Density = val_vars_TD[LOOKUP_TD::MOLARWEIGHT];
-    molar_weight = Pressure / (Density * UNIVERSAL_GAS_CONSTANT * Temperature);
-    break;
-  case INC_DENSITYMODEL::VARIABLE:
-    molar_weight = val_vars_TD[LOOKUP_TD::MOLARWEIGHT];
-    Density = Pressure / (molar_weight * UNIVERSAL_GAS_CONSTANT * Temperature);
-  default:
-    break;
+    case INC_DENSITYMODEL::FLAMELET:
+      Density = val_vars_TD[LOOKUP_TD::MOLARWEIGHT];
+      molar_weight = Pressure / (Density * UNIVERSAL_GAS_CONSTANT * Temperature);
+      break;
+    case INC_DENSITYMODEL::VARIABLE:
+      molar_weight = val_vars_TD[LOOKUP_TD::MOLARWEIGHT];
+      Density = Pressure / (molar_weight * UNIVERSAL_GAS_CONSTANT * Temperature);
+      break;
+    default:
+      break;
   }
-
-  /*--- Compute Cv from Cp and molar weight of the mixture (ideal gas). ---*/
+    /*--- Compute Cv from Cp and molar weight of the mixture (ideal gas). ---*/
   Cv = Cp - UNIVERSAL_GAS_CONSTANT / molar_weight;
 }
 
diff --git a/SU2_CFD/src/numerics/flow/convection/centered.cpp b/SU2_CFD/src/numerics/flow/convection/centered.cpp
index 88ba161f45d..89a5ec243db 100644
--- a/SU2_CFD/src/numerics/flow/convection/centered.cpp
+++ b/SU2_CFD/src/numerics/flow/convection/centered.cpp
@@ -31,7 +31,7 @@
 CCentLaxInc_Flow::CCentLaxInc_Flow(unsigned short val_nDim, unsigned short val_nVar, const CConfig* config) : CNumerics(val_nDim, val_nVar, config) {
 
   implicit         = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
-  variable_density = (config->GetKind_DensityModel() == INC_DENSITYMODEL::VARIABLE);
+  variable_density = ((config->GetKind_DensityModel() == INC_DENSITYMODEL::VARIABLE) || (config->GetKind_DensityModel() == INC_DENSITYMODEL::FLAMELET));
   /* A grid is defined as dynamic if there's rigid grid movement or grid deformation AND the problem is time domain */
   dynamic_grid = config->GetDynamic_Grid();
   fix_factor = config->GetCent_Inc_Jac_Fix_Factor();
@@ -251,7 +251,7 @@ CNumerics::ResidualType<> CCentLaxInc_Flow::ComputeResidual(const CConfig* confi
 CCentJSTInc_Flow::CCentJSTInc_Flow(unsigned short val_nDim, unsigned short val_nVar, const CConfig* config) : CNumerics(val_nDim, val_nVar, config) {
 
   implicit         = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
-  variable_density = (config->GetKind_DensityModel() == INC_DENSITYMODEL::VARIABLE);
+  variable_density = (config->GetVariable_Density_Model());
   energy           = config->GetEnergy_Equation();
   /* A grid is defined as dynamic if there's rigid grid movement or grid deformation AND the problem is time domain */
   dynamic_grid = config->GetDynamic_Grid();
diff --git a/SU2_CFD/src/numerics/flow/convection/fds.cpp b/SU2_CFD/src/numerics/flow/convection/fds.cpp
index 1df4b04f35f..1fae70b6d9b 100644
--- a/SU2_CFD/src/numerics/flow/convection/fds.cpp
+++ b/SU2_CFD/src/numerics/flow/convection/fds.cpp
@@ -31,7 +31,7 @@
 CUpwFDSInc_Flow::CUpwFDSInc_Flow(unsigned short val_nDim, unsigned short val_nVar, const CConfig *config) : CNumerics(val_nDim, val_nVar, config) {
 
   implicit         = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
-  variable_density = (config->GetKind_DensityModel() == INC_DENSITYMODEL::VARIABLE);
+  variable_density = (config->GetVariable_Density_Model());
   energy           = config->GetEnergy_Equation();
   /* A grid is defined as dynamic if there's rigid grid movement or grid deformation AND the problem is time domain */
   dynamic_grid = config->GetDynamic_Grid();
diff --git a/SU2_CFD/src/numerics/flow/flow_sources.cpp b/SU2_CFD/src/numerics/flow/flow_sources.cpp
index 64f8145cf15..95bd3f09e5b 100644
--- a/SU2_CFD/src/numerics/flow/flow_sources.cpp
+++ b/SU2_CFD/src/numerics/flow/flow_sources.cpp
@@ -405,7 +405,7 @@ CNumerics::ResidualType<> CSourceIncBodyForce::ComputeResidual(const CConfig* co
   unsigned short iDim;
   su2double DensityInc_0 = 0.0;
   su2double Force_Ref    = config->GetForce_Ref();
-  bool variable_density  = (config->GetKind_DensityModel() == INC_DENSITYMODEL::VARIABLE);
+  bool variable_density  = (config->GetVariable_Density_Model());
 
   /*--- Check for variable density. If we have a variable density
    problem, we should subtract out the hydrostatic pressure component. ---*/
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index 836262c3fe9..7e2b4c67881 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -232,7 +232,7 @@ void CFlowOutput::SetAnalyzeSurface(const CSolver* const*solver, const CGeometry
           }
 
           if (incompressible){
-            if (config->GetKind_DensityModel() == INC_DENSITYMODEL::VARIABLE) {
+            if (config->GetVariable_Density_Model()) {
               Mach = sqrt(flow_nodes->GetVelocity2(iPoint))/
               sqrt(flow_nodes->GetSpecificHeatCp(iPoint)*config->GetPressure_ThermodynamicND()/(flow_nodes->GetSpecificHeatCv(iPoint)*flow_nodes->GetDensity(iPoint)));
             } else {
diff --git a/SU2_CFD/src/solvers/CIncEulerSolver.cpp b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
index 70a7f909ef5..9c8b67f410e 100644
--- a/SU2_CFD/src/solvers/CIncEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
@@ -1976,7 +1976,7 @@ void CIncEulerSolver::SetPreconditioner(const CConfig *config, unsigned long iPo
   su2double  BetaInc2, Density, dRhodT, Temperature, oneOverCp, Cp;
   su2double  Velocity[MAXNDIM] = {0.0};
 
-  bool variable_density = (config->GetKind_DensityModel() == INC_DENSITYMODEL::VARIABLE);
+  bool variable_density = (config->GetVariable_Density_Model());
   bool implicit         = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
   bool energy           = config->GetEnergy_Equation();
 
diff --git a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
index 23f172279e0..d0b94709071 100644
--- a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
+++ b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
@@ -258,7 +258,7 @@ void CSpeciesFlameletSolver::SetInitialCondition(CGeometry** geometry, CSolver**
 }
 
 void CSpeciesFlameletSolver::SetPreconditioner(CGeometry* geometry, CSolver** solver_container, CConfig* config) {
-  const bool variable_density = (config->GetKind_DensityModel() == INC_DENSITYMODEL::VARIABLE);
+  const bool variable_density = (config->GetVariable_Density_Model());
   const bool implicit = (config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT);
 
   SU2_OMP_FOR_STAT(omp_chunk_size)
@@ -464,6 +464,7 @@ unsigned long CSpeciesFlameletSolver::SetScalarSources(CConfig* config, CFluidMo
   vector<su2double> source_scalar(config->GetNScalars());
   for (auto iCV=0u; iCV<config->GetNControlVars(); iCV++)
     source_scalar[iCV] = table_sources[iCV];
+  source_scalar[I_PROGVAR] = fmax(EPS, source_scalar[I_PROGVAR]);
 
   /*--- Source term for the auxiliary species transport equations. ---*/
   for (size_t i_aux = 0; i_aux < config->GetNUserScalars(); i_aux++) {
diff --git a/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg b/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg
index 8cb22a0406f..8cdbcca8a3f 100644
--- a/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg
+++ b/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg
@@ -17,7 +17,7 @@ RESTART_SOL = YES
 %
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
-INC_DENSITY_MODEL= VARIABLE 
+INC_DENSITY_MODEL= FLAMELET
 INC_ENERGY_EQUATION = YES
 INC_DENSITY_INIT= 1.00
 INC_VELOCITY_INIT= (0.5, 0.0, 0.0 )
diff --git a/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg
index fdad7b11f80..c0108c0e298 100644
--- a/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg
+++ b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg
@@ -27,7 +27,7 @@ CUSTOM_OUTPUTS= 'avg_NOx : MassFlowAvg{SPECIES[3]}[outlet]'
 %
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
-INC_DENSITY_MODEL= VARIABLE
+INC_DENSITY_MODEL= FLAMELET
 INC_DENSITY_INIT= 1.1766
 INC_VELOCITY_INIT= ( 0.2, 0, 0 )
 INC_ENERGY_EQUATION= YES
diff --git a/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg
index 64988b994dc..f0d0191ff05 100644
--- a/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg
+++ b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg
@@ -28,7 +28,7 @@ CUSTOM_OUTPUTS= 'avg_NOx : MassFlowAvg{SPECIES[3]}[outlet]'
 %
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
-INC_DENSITY_MODEL= VARIABLE
+INC_DENSITY_MODEL= FLAMELET
 INC_DENSITY_INIT= 1.1766
 INC_VELOCITY_INIT= ( 0.2, 0, 0 )
 INC_ENERGY_EQUATION= YES
diff --git a/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg b/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg
index 8eab5644d61..c91c5b4ae67 100644
--- a/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg
+++ b/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg
@@ -42,7 +42,7 @@ MARKER_SPECIES_STRONG_BC= (inlet, outlet, wall_burner)
 
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 
-INC_DENSITY_MODEL= VARIABLE
+INC_DENSITY_MODEL= FLAMELET
 INC_DENSITY_INIT= 1.1766
 INC_VELOCITY_INIT= ( 0.2, 0, 0 )
 INC_ENERGY_EQUATION= YES
diff --git a/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg b/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg
index 4bf950c936a..6f22997846a 100644
--- a/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg
+++ b/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg
@@ -44,7 +44,7 @@ MARKER_SPECIES_STRONG_BC= (inlet, wall_burner)
 
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 
-INC_DENSITY_MODEL= VARIABLE
+INC_DENSITY_MODEL= FLAMELET
 INC_DENSITY_INIT= 1.1766
 INC_VELOCITY_INIT= ( 0.2, 0, 0 )
 INC_ENERGY_EQUATION= YES
diff --git a/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg b/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg
index 859cd446323..484240977cc 100644
--- a/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg
+++ b/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg
@@ -18,7 +18,7 @@ RESTART_SOL= YES
 %
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
-INC_DENSITY_MODEL= VARIABLE 
+INC_DENSITY_MODEL= FLAMELET
 INC_ENERGY_EQUATION= YES
 INC_DENSITY_INIT= 1.00
 INC_VELOCITY_INIT= (0.5, 0.0, 0.0 )
diff --git a/config_template.cfg b/config_template.cfg
index 47d9996df7a..6fdbc33696d 100644
--- a/config_template.cfg
+++ b/config_template.cfg
@@ -218,8 +218,9 @@ REF_DIMENSIONALIZATION= DIMENSIONAL
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
 % Density model within the incompressible flow solver.
-% Options are CONSTANT (default), BOUSSINESQ, or VARIABLE. If VARIABLE,
-% an appropriate fluid model must be selected.
+% Options are CONSTANT (default), BOUSSINESQ, VARIABLE, or FLAMELET. If VARIABLE,
+% an appropriate fluid model must be selected. For FLAMELET, the density is
+% retrieved directly from the flamelet manifold.
 INC_DENSITY_MODEL= CONSTANT
 %
 % Solve the energy equation in the incompressible flow solver

From 45a28cc00d07ebadac3b2d52a66ab9e9133609cb Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 26 Jun 2023 13:37:51 +0200
Subject: [PATCH 509/656] Updated regression values for partially premixed
 flamelet test case

---
 TestCases/parallel_regression.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 57cb607670c..c6e7ec4bd80 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -65,7 +65,7 @@ def main():
     cfd_flamelet_ch4_partial_premix.cfg_dir = "flamelet/06_laminar_partial_premixed_ch4_flame_cfd"
     cfd_flamelet_ch4_partial_premix.cfg_file = "lam_partial_prem_ch4_cfd.cfg"
     cfd_flamelet_ch4_partial_premix.test_iter = 10
-    cfd_flamelet_ch4_partial_premix.test_vals = [-8.557377, -9.715636, -9.436786, -9.813844, -2.684793]
+    cfd_flamelet_ch4_partial_premix.test_vals = [-9.408381, -9.414935, -2.684728, -11.330306, -9.310217]
     cfd_flamelet_ch4_partial_premix.new_output = True
     test_list.append(cfd_flamelet_ch4_partial_premix)
 

From c6f2c46033be408fe869792c03cdea16a5510469 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 27 Jun 2023 10:18:35 +0200
Subject: [PATCH 510/656] Implemented ideal gas approximation for data-driven
 fluid model, such that initial values for density and energy no longer need
 to be provided by the user

---
 Common/include/CConfig.hpp                    |  15 +--
 Common/src/CConfig.cpp                        |   4 -
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp    |  31 +++--
 SU2_CFD/include/fluid/CFluidModel.hpp         |  12 --
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        | 108 ++++++++++++++----
 SU2_CFD/src/solvers/CEulerSolver.cpp          |  38 +-----
 SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp   |  28 +----
 .../nicf/datadriven/datadriven_nozzle.cfg     |   2 -
 config_template.cfg                           |  11 +-
 9 files changed, 106 insertions(+), 143 deletions(-)

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index 2b2888f4091..39ebcf28c01 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -523,9 +523,7 @@ class CConfig {
   n_Datadriven_files;
   ENUM_DATADRIVEN_METHOD Kind_DataDriven_Method;       /*!< \brief Method used for datset regression in data-driven fluid models. */
 
-  su2double DataDriven_Relaxation_Factor, /*!< \brief Relaxation factor for Newton solvers in data-driven fluid models. */
-            DataDriven_initial_density,   /*!< \brief Initial density value for Newton solvers in data-driven fluid models. */
-            DataDriven_initial_energy;    /*!< \brief Initial static energy value for Newton solvers in data-driven fluid models. */
+  su2double DataDriven_Relaxation_Factor; /*!< \brief Relaxation factor for Newton solvers in data-driven fluid models. */
 
   STRUCT_TIME_INT Kind_TimeIntScheme_FEA;    /*!< \brief Time integration for the FEA equations. */
   STRUCT_SPACE_ITE Kind_SpaceIteScheme_FEA;  /*!< \brief Iterative scheme for nonlinear structural analysis. */
@@ -3875,17 +3873,6 @@ class CConfig {
    */
   su2double GetRelaxation_DataDriven(void) const { return DataDriven_Relaxation_Factor; }
 
-  /*!
-   * \brief Get initial value for the density in the Newton solvers in the data-driven fluid model.
-   * \return Initial density value.
-   */
-  su2double GetDensity_Init_DataDriven(void) const { return DataDriven_initial_density; }
-  /*!
-   * \brief Get initial value for the static energy in the Newton solvers in the data-driven fluid model.
-   * \return Initial dstatic energy value.
-   */
-  su2double GetEnergy_Init_DataDriven(void) const { return DataDriven_initial_energy; }
-
   /*!
    * \brief Returns the name of the fluid we are using in CoolProp.
    */
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index ab4a85ae645..b5cd0ba2fa9 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -1176,10 +1176,6 @@ void CConfig::SetConfig_Options() {
   addStringListOption("FILENAMES_INTERPOLATOR", n_Datadriven_files, DataDriven_Method_FileNames);
   /*!\brief DATADRIVEN_NEWTON_RELAXATION \n DESCRIPTION: Relaxation factor for Newton solvers in data-driven fluid model. \n \ingroup Config*/
   addDoubleOption("DATADRIVEN_NEWTON_RELAXATION", DataDriven_Relaxation_Factor, 0.05);
-  /*!\brief DATADRIVEN_FLUID_INITIAL_DENSITY \n DESCRIPTION: Initial value for the density in the Newton solvers in the data-driven fluid model. \n \ingroup Config*/
-  addDoubleOption("DATADRIVEN_FLUID_INITIAL_DENSITY", DataDriven_initial_density, 1.225);
-  /*!\brief DATADRIVEN_FLUID_INITIAL_ENERGY \n DESCRIPTION: Initial value for the static energy in the Newton solvers in the data-driven fluid model. \n \ingroup Config*/
-  addDoubleOption("DATADRIVEN_FLUID_INITIAL_ENERGY", DataDriven_initial_energy, 1e5);
 
   /*!\brief CONFINEMENT_PARAM \n DESCRIPTION: Input Confinement Parameter for Vorticity Confinement*/
   addDoubleOption("CONFINEMENT_PARAM", Confinement_Param, 0.0);
diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index 0d6cdb78d4a..ddf33ba9641 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -49,15 +49,18 @@ class CDataDrivenFluid final : public CFluidModel {
   ENUM_DATADRIVEN_METHOD Kind_DataDriven_Method =
       ENUM_DATADRIVEN_METHOD::LUT; /*!< \brief Interpolation method for data set evaluation. */
 
+  string varname_rho,  /*!< \brief Controlling variable name for density. */
+         varname_e;    /*!< \brief Controlling variable name for static energy. */
+         
   size_t idx_rho, /*!< \brief Interpolator index for density input. */
       idx_e;      /*!< \brief Interpolator index for energy input. */
 
   su2double Newton_Relaxation, /*!< \brief Relaxation factor for Newton solvers. */
       rho_start,               /*!< \brief Starting value for the density in Newton solver processes. */
       e_start,                 /*!< \brief Starting value for the energy in Newton solver processes. */
-      rho_init,                /*!< \brief Initial value for the density from config. */
-      e_init,                  /*!< \brief Initial value for the energy from config. */
-      Newton_Tolerance;        /*!< \brief Normalized tolerance for Newton solvers. */
+      Newton_Tolerance,        /*!< \brief Normalized tolerance for Newton solvers. */
+      rho_min, rho_max,        /*!< \brief Minimum and maximum density values in data set. */
+      e_min, e_max;            /*!< \brief Minimum and maximum energy values in data set. */
 
   unsigned long MaxIter_Newton; /*!< \brief Maximum number of iterations for Newton solvers. */
 
@@ -67,6 +70,13 @@ class CDataDrivenFluid final : public CFluidModel {
       d2sdedrho,      /*!< \brief Entropy second derivative w.r.t. density and static energy. */
       d2sdrho2;       /*!< \brief Entropy second derivative w.r.t. static density. */
 
+  su2double R_idealgas,     /*!< \brief Approximated ideal gas constant. */
+            Cp_idealgas,    /*!< \brief Approximated ideal gas specific heat at constant pressure. */
+            gamma_idealgas, /*!< \brief Approximated ideal gas specific heat ratio. */
+            Cv_idealgas,    /*!< \brief Approximated ideal gas specific heat at constant volume. */
+            P_middle,       /*!< \brief Pressure computed from the centre of the data set. */
+            T_middle;       /*!< \brief Temperature computed from the centre of the data set. */
+
   su2double Enthalpy, /*!< \brief Fluid enthalpy value [J kg^-1] */
       dhdrho_e,       /*!< \brief Enthalpy derivative w.r.t. density. */
       dhde_rho;       /*!< \brief Enthalpy derivative w.r.t. static energy. */
@@ -77,8 +87,6 @@ class CDataDrivenFluid final : public CFluidModel {
 
   vector<su2double*> outputs_rhoe; /*!< \brief Pointers to output variables. */
 
-  bool set_local_rhoe = false;
-
   /*--- Class variables for the multi-layer perceptron method ---*/
 #ifdef USE_MLPCPP
   MLPToolbox::CLookUp_ANN* lookup_mlp; /*!< \brief Multi-layer perceptron collection. */
@@ -142,6 +150,7 @@ class CDataDrivenFluid final : public CFluidModel {
    */
   void Run_Newton_Solver(su2double Y_target, su2double* Y, su2double* X, su2double* dYdX);
 
+  void ComputeIdealGasQuantities();
  public:
   /*!
    * \brief Constructor of the class.
@@ -197,18 +206,6 @@ class CDataDrivenFluid final : public CFluidModel {
    */
   void SetTDState_Ps(su2double P, su2double s) override;
 
-  /*!
-   * \brief Set the initial guess for the density in Newton solvers.
-   * \param[in] rho - Initial value for density.
-   */
-  void SetInitialDensity(su2double rho) override { rho_start = rho; }
-
-  /*!
-   * \brief Set the initial guess for the static energy in Newton solvers.
-   * \param[in] e - Initial value for static energy.
-   */
-  void SetInitialEnergy(su2double e) override { e_start = e; }
-
   /*!
    * \brief Get fluid model extrapolation instance.
    * \return Query point lies outside fluid model data range.
diff --git a/SU2_CFD/include/fluid/CFluidModel.hpp b/SU2_CFD/include/fluid/CFluidModel.hpp
index e9bbf88a145..fae2d900347 100644
--- a/SU2_CFD/include/fluid/CFluidModel.hpp
+++ b/SU2_CFD/include/fluid/CFluidModel.hpp
@@ -345,18 +345,6 @@ class CFluidModel {
    */
   void SetEddyViscosity(su2double val_Mu_Turb) { Mu_Turb = val_Mu_Turb; }
 
-  /*!
-   * \brief Set the initial guess for the density in Newton solvers
-   * \param[in] rho - Initial value for density.
-   */
-  virtual void SetInitialDensity(su2double rho) {}
-
-  /*!
-   * \brief Set the initial guess for the static energy in Newton solvers
-   * \param[in] e - Initial value for static energy.
-   */
-  virtual void SetInitialEnergy(su2double e) {}
-
   /*!
    * \brief Get fluid model extrapolation instance
    * \return Query point lies outside fluid model data range.
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 9e79ab69a0e..3d7b05b7172 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -35,6 +35,9 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config, bool display) : CFluid
   rank = SU2_MPI::GetRank();
   Kind_DataDriven_Method = config->GetKind_DataDriven_Method();
 
+  varname_rho = "Density";
+  varname_e = "Energy";
+
   /*--- Set up interpolation algorithm according to data-driven method. Currently only MLP's are supported. ---*/
   switch (Kind_DataDriven_Method) {
     case ENUM_DATADRIVEN_METHOD::MLP:
@@ -46,7 +49,7 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config, bool display) : CFluid
 #endif
       break;
     case ENUM_DATADRIVEN_METHOD::LUT:
-      lookup_table = new CLookUpTable(config->GetDataDriven_FileNames()[0], "Density", "Energy");
+      lookup_table = new CLookUpTable(config->GetDataDriven_FileNames()[0], varname_rho, varname_e);
       break;
     default:
       break;
@@ -60,13 +63,8 @@ CDataDrivenFluid::CDataDrivenFluid(const CConfig* config, bool display) : CFluid
   /*--- Preprocessing of inputs and outputs for the interpolation method. ---*/
   MapInputs_to_Outputs();
 
-  /*--- Set initial values for density and energy based on config options. ---*/
-  rho_init = config->GetDensity_Init_DataDriven();
-  e_init = config->GetEnergy_Init_DataDriven();
-
-  /*--- Set default Newton solver density and energy values. ---*/
-  rho_start = rho_init;
-  e_start = e_init;
+  /*--- Compute approximate ideal gas properties ---*/
+  ComputeIdealGasQuantities();
 }
 
 CDataDrivenFluid::~CDataDrivenFluid() {
@@ -89,8 +87,8 @@ void CDataDrivenFluid::MapInputs_to_Outputs() {
   input_names_rhoe.resize(2);
   idx_rho = 0;
   idx_e = 1;
-  input_names_rhoe[idx_rho] = "Density";
-  input_names_rhoe[idx_e] = "Energy";
+  input_names_rhoe[idx_rho] = varname_rho;
+  input_names_rhoe[idx_e] = varname_e;
 
   /*--- Required outputs for the interpolation method are entropy and its partial derivatives with respect to energy and
    * density. ---*/
@@ -128,7 +126,11 @@ void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
   Density = rho;
   StaticEnergy = e;
 
-  Evaluate_Dataset(rho, e);
+  /*--- Clip density and energy values to prevent extrapolation. ---*/
+  Density = min(rho_max, max(rho_min, Density));
+  StaticEnergy = min(e_max, max(e_min, StaticEnergy));
+
+  Evaluate_Dataset(Density, StaticEnergy);
 
   /*--- Compute speed of sound. ---*/
   auto blue_term = (dsdrho_e * (2 - rho * pow(dsde_rho, -1) * d2sdedrho) + rho * d2sdrho2);
@@ -158,14 +160,14 @@ void CDataDrivenFluid::SetTDState_rhoe(su2double rho, su2double e) {
   dhdP_rho = dhde_rho * (1 / dPde_rho);
   dsdrho_P = dsdrho_e - dPdrho_e * (1 / dPde_rho) * dsde_rho;
   dsdP_rho = dsde_rho / dPde_rho;
-
-  if (set_local_rhoe) {
-    rho_start = Newton_Relaxation * Density + (1 - Newton_Relaxation) * rho_init;
-    e_start = Newton_Relaxation * StaticEnergy + (1 - Newton_Relaxation) * e_init;
-  }
 }
 
 void CDataDrivenFluid::SetTDState_PT(su2double P, su2double T) {
+
+  /*--- Approximate density and static energy with ideal gas law. ---*/
+  rho_start = P / (R_idealgas * T);
+  e_start = Cv_idealgas * T;
+  
   /*--- Run 2D Newton solver for pressure and temperature ---*/
   Run_Newton_Solver(P, T, &Pressure, &Temperature, &dPdrho_e, &dPde_rho, &dTdrho_e, &dTde_rho);
 }
@@ -178,24 +180,44 @@ void CDataDrivenFluid::SetTDState_Prho(su2double P, su2double rho) {
 void CDataDrivenFluid::SetEnergy_Prho(su2double P, su2double rho) {
   /*--- Run 1D Newton solver for pressure at constant density. ---*/
   Density = rho;
-  StaticEnergy = e_start;
+
+  /*--- Approximate static energy through ideal gas law. ---*/
+  su2double e_idealgas = Cv_idealgas * (P / (R_idealgas * rho));
+  StaticEnergy = min(e_max, max(e_idealgas, e_min));
+
   Run_Newton_Solver(P, &Pressure, &StaticEnergy, &dPde_rho);
 }
 
 void CDataDrivenFluid::SetTDState_rhoT(su2double rho, su2double T) {
   /*--- Run 1D Newton solver for temperature at constant density. ---*/
   Density = rho;
-  StaticEnergy = e_start;
+
+  /*--- Approximate static energy through ideal gas law. ---*/
+  StaticEnergy = Cv_idealgas * T;
+
   Run_Newton_Solver(T, &Temperature, &StaticEnergy, &dTde_rho);
 }
 
 void CDataDrivenFluid::SetTDState_hs(su2double h, su2double s) {
   /*--- Run 2D Newton solver for enthalpy and entropy. ---*/
+
+  /*--- Approximate density and static energy through ideal gas law under isentropic assumption. ---*/
+  su2double T_init = h / Cp_idealgas;
+  su2double P_init = P_middle * pow(T_init / T_middle, gamma_idealgas/(gamma_idealgas - 1));
+
+  e_start = h * Cv_idealgas / Cp_idealgas; 
+  rho_start = P_init / (R_idealgas * T_init);
   Run_Newton_Solver(h, s, &Enthalpy, &Entropy, &dhdrho_e, &dhde_rho, &dsdrho_e, &dsde_rho);
 }
 
 void CDataDrivenFluid::SetTDState_Ps(su2double P, su2double s) {
   /*--- Run 2D Newton solver for pressure and entropy ---*/
+
+  /*--- Approximate initial state through isentropic assumption and ideal gas law. ---*/
+  su2double T_init = T_middle * pow(P / P_middle, (gamma_idealgas - 1)/gamma_idealgas);
+  e_start = Cv_idealgas * T_init;
+  rho_start = P / (R_idealgas * T_init);
+
   Run_Newton_Solver(P, s, &Pressure, &Entropy, &dPdrho_e, &dPde_rho, &dsdrho_e, &dsde_rho);
 }
 
@@ -255,7 +277,6 @@ void CDataDrivenFluid::Run_Newton_Solver(su2double Y1_target, su2double Y2_targe
 
   su2double delta_Y1, delta_Y2, delta_rho, delta_e, determinant;
 
-  set_local_rhoe = false;
   /*--- Initiating Newton solver ---*/
   while (!converged && (Iter < MaxIter_Newton)) {
     /*--- Determine thermodynamic state based on current density and energy. ---*/
@@ -284,10 +305,7 @@ void CDataDrivenFluid::Run_Newton_Solver(su2double Y1_target, su2double Y2_targe
   nIter_Newton = Iter;
 
   /*--- Evaluation of final state. ---*/
-  Density = rho;
-  StaticEnergy = e;
-  SetTDState_rhoe(Density, StaticEnergy);
-  set_local_rhoe = true;
+  SetTDState_rhoe(rho, e);
 }
 
 void CDataDrivenFluid::Run_Newton_Solver(su2double Y_target, su2double* Y, su2double* X, su2double* dYdX) {
@@ -323,3 +341,47 @@ void CDataDrivenFluid::Run_Newton_Solver(su2double Y_target, su2double* Y, su2do
 
   nIter_Newton = Iter;
 }
+
+void CDataDrivenFluid::ComputeIdealGasQuantities() {
+  /*--- Compute approximate ideal gas properties from the middle of the reference data set. These properties are used to approximate the initial condition of the Newton solvers using the ideal gas law. ---*/
+  su2double rho_average, e_average;
+
+  /*--- Obtain minimum and maximum density and static energy from data set. ---*/
+  switch (Kind_DataDriven_Method)
+  {
+  case ENUM_DATADRIVEN_METHOD::LUT:
+    rho_min = *lookup_table->GetTableLimitsX().first;
+    e_min = *lookup_table->GetTableLimitsY().first;
+    rho_max = *lookup_table->GetTableLimitsX().second;
+    e_max = *lookup_table->GetTableLimitsY().second;
+    rho_average = 0.5*(*lookup_table->GetTableLimitsX().first + *lookup_table->GetTableLimitsX().second);
+    e_average = 0.5*(*lookup_table->GetTableLimitsY().first + *lookup_table->GetTableLimitsY().second);
+    break;
+  case ENUM_DATADRIVEN_METHOD::MLP:
+#ifdef USE_MLPCPP
+    rho_min = lookup_mlp->GetInputNorm(iomap_rhoe, idx_rho).first;
+    e_min = lookup_mlp->GetInputNorm(iomap_rhoe, idx_e).first;
+    rho_max = lookup_mlp->GetInputNorm(iomap_rhoe, idx_rho).second;
+    e_max = lookup_mlp->GetInputNorm(iomap_rhoe, idx_e).second;
+    rho_average = 0.5*(lookup_mlp->GetInputNorm(iomap_rhoe, idx_rho).first + lookup_mlp->GetInputNorm(iomap_rhoe, idx_rho).second);
+    e_average = 0.5*(lookup_mlp->GetInputNorm(iomap_rhoe, idx_e).first + lookup_mlp->GetInputNorm(iomap_rhoe, idx_e).second);
+#endif
+    break;
+  default:
+    rho_average = 1.0;
+    e_average = 1.0;
+    rho_min = 1.0;
+    e_min = 1.0;
+    break;
+  }
+
+  /*--- Compute thermodynamic state from middle of data set. ---*/
+  SetTDState_rhoe(rho_average, e_average);
+  P_middle = Pressure;
+  T_middle = Temperature;
+
+  R_idealgas = P_middle / (rho_average * T_middle);
+  Cv_idealgas = e_average / T_middle;
+  Cp_idealgas = Enthalpy / T_middle;
+  gamma_idealgas = (R_idealgas / Cv_idealgas) + 1;
+}
\ No newline at end of file
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index 431ad077c28..5b20e11ce09 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -5018,6 +5018,9 @@ void CEulerSolver::BC_Riemann(CGeometry *geometry, CSolver **solver_container,
           Jacobian.SubtractBlock2Diag(iPoint, residual.jacobian_i);
 
       }
+      /*--- Store number of Newton iterations at BC ---*/
+      if(config->GetKind_FluidModel() == DATADRIVEN_FLUID)
+        nodes->SetNewtonSolverIterations(iPoint, GetFluidModel()->GetnIter_Newton());
 
     }
   }
@@ -5616,15 +5619,6 @@ void CEulerSolver::PreprocessBC_Giles(CGeometry *geometry, CConfig *config, CNum
                 {
                   Velocity_i[iDim] = nodes->GetVelocity(iPoint,iDim);
                 }
-
-                /*--- Set Newton solver starting point in case of data-driven fluid model. ---*/
-                if (config->GetKind_FluidModel() == DATADRIVEN_FLUID){
-                  su2double Velocity2_i = GeometryToolbox::SquaredNorm(nDim, Velocity_i);
-                  su2double Energy_i = nodes->GetEnergy(iPoint);
-                  su2double StaticEnergy_i = Energy_i - 0.5*Velocity2_i;
-                  GetFluidModel()->SetInitialDensity(AverageDensity[iMarker][iSpan]);
-                  GetFluidModel()->SetInitialEnergy(StaticEnergy_i);
-                }
                 
                 ComputeTurboVelocity(Velocity_i, turboNormal, turboVelocity, marker_flag, config->GetKind_TurboMachinery(iZone));
 
@@ -5843,12 +5837,6 @@ void CEulerSolver::BC_Giles(CGeometry *geometry, CSolver **solver_container, CNu
       }
     }
 
-    /*--- Set Newton solver starting point in case of data-driven fluid model. ---*/
-    if (config->GetKind_FluidModel() == DATADRIVEN_FLUID){
-      GetFluidModel()->SetInitialDensity(AverageDensity[val_marker][iSpan]);
-      GetFluidModel()->SetInitialEnergy(config->GetEnergy_Init_DataDriven());
-    }
-
     GetFluidModel()->SetTDState_Prho(AveragePressure[val_marker][iSpan], AverageDensity[val_marker][iSpan]);
     AverageSoundSpeed = GetFluidModel()->GetSoundSpeed();
     AverageTurboMach[0] = AverageTurboVelocity[val_marker][iSpan][0]/AverageSoundSpeed;
@@ -7861,11 +7849,6 @@ void CEulerSolver::BC_ActDisk(CGeometry *geometry, CSolver **solver_container, C
       /*--- Subsonic outlet ---*/
 
       else {
-        /* Set initial guesses for density and static energy in case of data-driven fluid model. */
-        if (config->GetKind_FluidModel() == DATADRIVEN_FLUID) {
-          GetFluidModel()->SetInitialDensity(config->GetDensity_Init_DataDriven());
-          GetFluidModel()->SetInitialEnergy(config->GetEnergy_Init_DataDriven());
-        }
 
         GetFluidModel()->SetTDState_PT(P_static, T_static);
         SoS_outlet = GetFluidModel()->GetSoundSpeed();
@@ -8396,11 +8379,6 @@ void CEulerSolver::SetFreeStream_TurboSolution(CConfig *config) {
 
   auto turboNormal = config->GetFreeStreamTurboNormal();
 
-  /* Set initial guess for static energy in case of data-driven fluid model. */
-  if (config->GetKind_FluidModel() == DATADRIVEN_FLUID) {
-    GetFluidModel()->SetInitialEnergy(config->GetEnergy_Init_DataDriven());
-  }
-
   GetFluidModel()->SetTDState_Prho(Pressure_Inf, Density_Inf);
   SoundSpeed = GetFluidModel()->GetSoundSpeed();
 
@@ -8886,11 +8864,6 @@ void CEulerSolver::TurboAverageProcess(CSolver **solver, CGeometry *geometry, CC
             AverageTurboNormal  = geometry->GetAverageTurboNormal(iMarker,iSpan);
             nVert               = geometry->GetnTotVertexSpan(iMarker,iSpan);
 
-            /* Set initial guess for static energy in case of data-driven fluid model. */
-            if (config->GetKind_FluidModel() == DATADRIVEN_FLUID) {
-              GetFluidModel()->SetInitialEnergy(config->GetEnergy_Init_DataDriven());
-            }
-
             /*--- compute normal Mach number as a check for massflow average and mixedout average ---*/
             GetFluidModel()->SetTDState_Prho(TotalAreaPressure/TotalArea, TotalAreaDensity / TotalArea);
             soundSpeed = GetFluidModel()->GetSoundSpeed();
@@ -9210,11 +9183,6 @@ void CEulerSolver::MixedOut_Average (CConfig *config, su2double val_init_pressur
 
   pressure_mix = val_init_pressure;
 
-  /* Set initial guess for static energy in case of data-driven fluid model. */
-  if (config->GetKind_FluidModel() == DATADRIVEN_FLUID) {
-    GetFluidModel()->SetInitialEnergy(config->GetEnergy_Init_DataDriven());
-  }
-
   /*--- Newton-Raphson's method with central difference formula ---*/
 
   while ( iter <= maxiter ) {
diff --git a/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp b/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
index 70ca34ebc9a..2c702832f40 100644
--- a/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
@@ -7790,13 +7790,6 @@ void CFEM_DG_EulerSolver::BoundaryStates_Riemann(CConfig                  *confi
       P_Total /= config->GetPressure_Ref();
       T_Total /= config->GetTemperature_Ref();
 
-      /* Set initial guesses for density and static energy in case of 
-         data-driven fluid model. */
-      if (config->GetKind_FluidModel() == DATADRIVEN_FLUID) {
-        FluidModel->SetInitialDensity(config->GetDensity_Init_DataDriven());
-        FluidModel->SetInitialEnergy(config->GetEnergy_Init_DataDriven());
-      }
-      
       /* Compute the total enthalpy and entropy from these values. */
       FluidModel->SetTDState_PT(P_Total, T_Total);
 
@@ -7859,13 +7852,6 @@ void CFEM_DG_EulerSolver::BoundaryStates_Riemann(CConfig                  *confi
       P_static /= config->GetPressure_Ref();
       T_static /= config->GetTemperature_Ref();
 
-      /* Set initial guesses for density and static energy in case of 
-         data-driven fluid model. */
-      if (config->GetKind_FluidModel() == DATADRIVEN_FLUID) {
-        FluidModel->SetInitialDensity(config->GetDensity_Init_DataDriven());
-        FluidModel->SetInitialEnergy(config->GetEnergy_Init_DataDriven());
-      }
-
       /* Compute the prescribed density, static energy per unit mass
          and speed of sound. */
       FluidModel->SetTDState_PT(P_static, T_static);
@@ -7916,13 +7902,7 @@ void CFEM_DG_EulerSolver::BoundaryStates_Riemann(CConfig                  *confi
 
       P_static /= config->GetPressure_Ref();
       Rho_static /= config->GetDensity_Ref();
-
-      /* Set initial guess for static energy in case of 
-         data-driven fluid model. */
-      if (config->GetKind_FluidModel() == DATADRIVEN_FLUID) {
-        FluidModel->SetInitialEnergy(config->GetEnergy_Init_DataDriven());
-      }
-
+      
       /* Compute the prescribed pressure, static energy per unit mass
          and speed of sound. */
       FluidModel->SetTDState_Prho(P_static, Rho_static);
@@ -8008,12 +7988,6 @@ void CFEM_DG_EulerSolver::BoundaryStates_Riemann(CConfig                  *confi
       const su2double Pressure_e = config->GetRiemann_Var1(Marker_Tag)
                                  / config->GetPressure_Ref();
 
-      /* Set initial guesses for density and static energy in case of 
-         data-driven fluid model. */             
-      if (config->GetKind_FluidModel() == DATADRIVEN_FLUID) {
-        FluidModel->SetInitialDensity(config->GetDensity_Init_DataDriven());
-        FluidModel->SetInitialEnergy(config->GetEnergy_Init_DataDriven());
-      }
       /* Loop over the faces that are treated simultaneously. */
       for(unsigned short l=0; l<nFaceSimul; ++l) {
         const unsigned short llNVar = l*nVar;
diff --git a/TestCases/nicf/datadriven/datadriven_nozzle.cfg b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
index 980f372091d..e8b133da4ff 100644
--- a/TestCases/nicf/datadriven/datadriven_nozzle.cfg
+++ b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
@@ -39,8 +39,6 @@ FLUID_MODEL = DATADRIVEN_FLUID
 INTERPOLATION_METHOD = MLP 
 FILENAMES_INTERPOLATOR = (MLP_air.mlp)
 DATADRIVEN_NEWTON_RELAXATION = 0.8
-DATADRIVEN_FLUID_INITIAL_DENSITY = 5.54548
-DATADRIVEN_FLUID_INITIAL_ENERGY = 1.8e+05
 
 % --------------------------- VISCOSITY MODEL ---------------------------------%
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
diff --git a/config_template.cfg b/config_template.cfg
index fa42705d828..45f33fede27 100644
--- a/config_template.cfg
+++ b/config_template.cfg
@@ -373,7 +373,7 @@ FROZEN_MIXTURE= NO
 % Datadriven fluid model
 % For data-driven fluid models, an interpolation algorithm is used to retrieve the thermodynamic state for a given density and internal energy
 
-% Interpolation method for thermodynamic state calculation (only MLP is supported for now)
+% Interpolation method for thermodynamic state calculation (MLP for multi-layer perceptron, LUT for 2D, unstructured look-up table)
 INTERPOLATION_METHOD= MLP
 
 % Name of the input file containing the information required for the interpolator to function
@@ -381,14 +381,7 @@ INTERPOLATION_METHOD= MLP
 FILENAME_INTERPOLATOR= MLP_collection.mlp
 
 % Relaxation factor for the Newton solvers in the data-driven fluid model
-DATADRIVEN_NEWTON_RELAXATION= 0.05
-
-% Initial value for the density used by the Newton solvers in the data-driven fluid model
-DATADRIVEN_FLUID_INITIAL_DENSITY= 1.225
-
-% Initial value for the static energy used by the Newton solvers in the data-driven fluid model
-DATADRIVEN_FLUID_INITIAL_ENERGY= 1e5
-
+DATADRIVEN_NEWTON_RELAXATION= 0.8
 
 %
 % NEMO Inlet Options

From 51143a69742050b723ae953741f14ab363ebef3b Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 27 Jun 2023 11:37:41 +0200
Subject: [PATCH 511/656] Fixed build error and updated submodule

---
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp | 6 +-----
 meson_scripts/init.py                  | 2 +-
 subprojects/MLPCpp                     | 2 +-
 3 files changed, 3 insertions(+), 7 deletions(-)

diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index 3d7b05b7172..a53601b7f5c 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -344,7 +344,7 @@ void CDataDrivenFluid::Run_Newton_Solver(su2double Y_target, su2double* Y, su2do
 
 void CDataDrivenFluid::ComputeIdealGasQuantities() {
   /*--- Compute approximate ideal gas properties from the middle of the reference data set. These properties are used to approximate the initial condition of the Newton solvers using the ideal gas law. ---*/
-  su2double rho_average, e_average;
+  su2double rho_average = 1.0, e_average = 1.0;
 
   /*--- Obtain minimum and maximum density and static energy from data set. ---*/
   switch (Kind_DataDriven_Method)
@@ -368,10 +368,6 @@ void CDataDrivenFluid::ComputeIdealGasQuantities() {
 #endif
     break;
   default:
-    rho_average = 1.0;
-    e_average = 1.0;
-    rho_min = 1.0;
-    e_min = 1.0;
     break;
   }
 
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 616afd31a21..372e77bc228 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -71,7 +71,7 @@ def init_submodules(
     github_repo_coolprop = "https://github.com/CoolProp/CoolProp"
     sha_version_mel = "2484cd3258ef800a10e361016cb341834ee7930b"
     github_repo_mel = "https://github.com/pcarruscag/MEL"
-    sha_version_mlpcpp = "596ed4c69c284304d8eb59e4f103ffab8afbfb1b"
+    sha_version_mlpcpp = "a80115c6f4779cc168d1464cf32aead61559c9ea"
     github_repo_mlpcpp = "https://github.com/EvertBunschoten/MLPCpp"
 
     medi_name = "MeDiPack"
diff --git a/subprojects/MLPCpp b/subprojects/MLPCpp
index 596ed4c69c2..a80115c6f47 160000
--- a/subprojects/MLPCpp
+++ b/subprojects/MLPCpp
@@ -1 +1 @@
-Subproject commit 596ed4c69c284304d8eb59e4f103ffab8afbfb1b
+Subproject commit a80115c6f4779cc168d1464cf32aead61559c9ea

From ecb9e85449664575419c1edd3d26546b1b2c67dd Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 1 Jul 2023 10:29:05 -0700
Subject: [PATCH 512/656] update v&v, fix logic for default

---
 .github/workflows/regression.yml                     |  2 +-
 Common/include/option_structure.hpp                  | 12 ++++++------
 TestCases/tutorials.py                               |  2 +-
 TestCases/vandv.py                                   |  8 ++++----
 .../vandv/rans/bump_in_channel/turb_bump_sst.cfg     |  2 +-
 .../vandv/rans/flatplate/turb_flatplate_sst.cfg      |  4 ++--
 6 files changed, 15 insertions(+), 15 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 76545cdb274..088412f17c8 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c sst_consistency -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index 7f6db2cd81f..8baa2e31901 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -1020,8 +1020,9 @@ inline SST_ParsedOptions ParseSSTOptions(const SST_OPTIONS *SST_Options, unsigne
 
   const bool default_version = !found_1994 && !found_1994m && !found_2003 && !found_2003m;
 
-  const bool sst_1994 = found_1994 || found_1994m || default_version;
-  const bool sst_2003 = found_2003 || found_2003m;
+  const bool sst_1994 = found_1994 || found_1994m;
+  /*--- Default version since v8. ---*/
+  const bool sst_2003 = found_2003 || found_2003m || default_version;
 
   /*--- When V2003m or V1994m is selected, we automatically select sst_m. ---*/
   const bool sst_m = found_1994m || found_2003m || default_version;
@@ -1033,11 +1034,10 @@ inline SST_ParsedOptions ParseSSTOptions(const SST_OPTIONS *SST_Options, unsigne
 
   if (sst_1994 && sst_2003) {
     SU2_MPI::Error("Two versions (1994 and 2003) selected for SST_OPTIONS. Please choose only one.", CURRENT_FUNCTION);
-  } else if (sst_1994) {
-    SSTParsedOptions.version = SST_OPTIONS::V1994;
-  } else {
-    /*--- Default version since v8. ---*/
+  } else if (sst_2003) {
     SSTParsedOptions.version = SST_OPTIONS::V2003;
+  } else {
+    SSTParsedOptions.version = SST_OPTIONS::V1994;
   }
 
   // Parse production modifications
diff --git a/TestCases/tutorials.py b/TestCases/tutorials.py
index 621a7ffc9c8..82aca1afc75 100644
--- a/TestCases/tutorials.py
+++ b/TestCases/tutorials.py
@@ -71,7 +71,7 @@ def main():
     sp_pinArray_2d_mf_hf.cfg_dir   = "../Tutorials/incompressible_flow/Inc_Streamwise_Periodic"
     sp_pinArray_2d_mf_hf.cfg_file  = "sp_pinArray_2d_mf_hf.cfg"
     sp_pinArray_2d_mf_hf.test_iter = 25
-    sp_pinArray_2d_mf_hf.test_vals = [-4.626243, 1.444608, -0.750995, 241.756998] #last 4 lines
+    sp_pinArray_2d_mf_hf.test_vals = [-4.625757, 1.445108, -0.750969, 241.762883]
     test_list.append(sp_pinArray_2d_mf_hf)
 
     # 2D pin case pressure drop periodic with heatflux BC and temperature periodicity
diff --git a/TestCases/vandv.py b/TestCases/vandv.py
index a1cad128cdf..0716d12069e 100644
--- a/TestCases/vandv.py
+++ b/TestCases/vandv.py
@@ -54,8 +54,8 @@ def main():
     flatplate_sst1994m.cfg_dir   = "vandv/rans/flatplate"
     flatplate_sst1994m.cfg_file  = "turb_flatplate_sst.cfg"
     flatplate_sst1994m.test_iter = 5
-    flatplate_sst1994m.test_vals         = [-13.022266, -9.782360, -10.951053, -7.775218, -10.035041, -5.141447, 0.002809]
-    flatplate_sst1994m.test_vals_aarch64 = [-13.044282, -9.682503, -10.712657, -7.519027, -9.742878, -5.374663, 0.002809]
+    flatplate_sst1994m.test_vals         = [-13.001873, -9.928107, -11.077909, -7.915809, -10.178822, -5.110162, 0.002808]
+    flatplate_sst1994m.test_vals_aarch64 = [-13.001873, -9.928107, -11.077909, -7.915809, -10.178822, -5.110162, 0.002808]
     test_list.append(flatplate_sst1994m)
 
     # bump in channel - sst-v1994m
@@ -63,8 +63,8 @@ def main():
     bump_sst1994m.cfg_dir   = "vandv/rans/bump_in_channel"
     bump_sst1994m.cfg_file  = "turb_bump_sst.cfg"
     bump_sst1994m.test_iter = 5
-    bump_sst1994m.test_vals         = [-13.048445, -9.929559, -10.602530, -7.593266, -10.323567, -5.548893, 0.004967]
-    bump_sst1994m.test_vals_aarch64 = [-13.005103, -9.889383, -10.555402, -7.584122, -10.312935, -5.470352, 0.004967]
+    bump_sst1994m.test_vals         = [-13.005815, -10.677095, -10.604787, -7.647741, -10.720450, -5.556079, 0.004972]
+    bump_sst1994m.test_vals_aarch64 = [-13.005815, -10.677095, -10.604787, -7.647741, -10.720450, -5.556079, 0.004972]
     test_list.append(bump_sst1994m)
 
     # SWBLI SA
diff --git a/TestCases/vandv/rans/bump_in_channel/turb_bump_sst.cfg b/TestCases/vandv/rans/bump_in_channel/turb_bump_sst.cfg
index e556bf970cb..b30ea280f10 100644
--- a/TestCases/vandv/rans/bump_in_channel/turb_bump_sst.cfg
+++ b/TestCases/vandv/rans/bump_in_channel/turb_bump_sst.cfg
@@ -1,7 +1,7 @@
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 SOLVER= RANS
 KIND_TURB_MODEL= SST
-%SST_OPTIONS= V2003m
+SST_OPTIONS= V1994m
 RESTART_SOL= YES
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 MACH_NUMBER= 0.2
diff --git a/TestCases/vandv/rans/flatplate/turb_flatplate_sst.cfg b/TestCases/vandv/rans/flatplate/turb_flatplate_sst.cfg
index d7e0813a0b5..2b53ee86d71 100644
--- a/TestCases/vandv/rans/flatplate/turb_flatplate_sst.cfg
+++ b/TestCases/vandv/rans/flatplate/turb_flatplate_sst.cfg
@@ -1,7 +1,7 @@
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 SOLVER= RANS
 KIND_TURB_MODEL= SST
-%SST_OPTIONS= V2003m
+SST_OPTIONS= V1994m
 RESTART_SOL= YES
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
 MACH_NUMBER= 0.2
@@ -55,7 +55,7 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
 CONV_FIELD= RMS_DENSITY
 CONV_RESIDUAL_MINVAL= -13
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-MESH_FILENAME= mesh_flatplate_turb_035x025.su2 
+MESH_FILENAME= mesh_flatplate_turb_035x025.su2
 MESH_FORMAT= SU2
 MESH_OUT_FILENAME= mesh_out.su2
 SOLUTION_FILENAME= solution_flow.dat

From 301a6df6903573d219e2479ad38ea5facb217a01 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 1 Jul 2023 11:28:29 -0700
Subject: [PATCH 513/656] update tutorials

---
 .github/workflows/regression.yml |  2 +-
 TestCases/tutorials.py           | 18 +++++++++---------
 TestCases/vandv.py               |  8 ++++----
 3 files changed, 14 insertions(+), 14 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 088412f17c8..c04724d24de 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c sst_consistency -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t sst_consistency -c sst_consistency -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
diff --git a/TestCases/tutorials.py b/TestCases/tutorials.py
index 82aca1afc75..424374bc743 100644
--- a/TestCases/tutorials.py
+++ b/TestCases/tutorials.py
@@ -79,7 +79,7 @@ def main():
     sp_pinArray_2d_dp_hf_tp.cfg_dir   = "../Tutorials/incompressible_flow/Inc_Streamwise_Periodic"
     sp_pinArray_2d_dp_hf_tp.cfg_file  = "sp_pinArray_2d_dp_hf_tp.cfg"
     sp_pinArray_2d_dp_hf_tp.test_iter = 25
-    sp_pinArray_2d_dp_hf_tp.test_vals = [-4.666992, 1.395929, -0.709333, 208.023676] #last 4 lines
+    sp_pinArray_2d_dp_hf_tp.test_vals = [-4.666547, 1.396426, -0.709267, 208.023676]
     test_list.append(sp_pinArray_2d_dp_hf_tp)
 
     ### Species Transport
@@ -89,7 +89,7 @@ def main():
     species3_primitiveVenturi.cfg_dir   = "../Tutorials/incompressible_flow/Inc_Species_Transport"
     species3_primitiveVenturi.cfg_file  = "species3_primitiveVenturi.cfg"
     species3_primitiveVenturi.test_iter = 50
-    species3_primitiveVenturi.test_vals = [-6.074971, -5.306648, -5.150960, -5.959416, -1.625107, -6.343704, -6.460033, 5.000000, -0.808413, 5.000000, -2.325029, 5.000000, -0.274923, 1.646091, 0.499028, 0.601019, 0.546044]
+    species3_primitiveVenturi.test_vals = [-6.082040, -5.293756, -5.131970, -5.933415, -1.606563, -6.274241, -6.408477, 5.000000, -0.811535, 5.000000, -2.344697, 5.000000, -0.388358, 1.647440, 0.499101, 0.600978, 0.547361]
     test_list.append(species3_primitiveVenturi)
 
     # 3 species (2 eq) primitive venturi mixing
@@ -97,8 +97,8 @@ def main():
     DAspecies3_primitiveVenturi.cfg_dir   = "../Tutorials/incompressible_flow/Inc_Species_Transport"
     DAspecies3_primitiveVenturi.cfg_file  = "DAspecies3_primitiveVenturi.cfg"
     DAspecies3_primitiveVenturi.test_iter = 50
-    DAspecies3_primitiveVenturi.test_vals         = [-8.422882, -7.699257, -7.683269, -7.411648, -12.064694, -12.205189, -11.368995]
-    DAspecies3_primitiveVenturi.test_vals_aarch64 = [-8.528843, -7.799649, -7.783477, -7.482502, -12.140092, -12.250169, -11.455523]
+    DAspecies3_primitiveVenturi.test_vals         = [-8.443103, -7.715615, -7.706589, -7.428740, -12.067471, -12.205189, -11.368995]
+    DAspecies3_primitiveVenturi.test_vals_aarch64 = [-8.443103, -7.715615, -7.706589, -7.428740, -12.067471, -12.205189, -11.368995]
     DAspecies3_primitiveVenturi.command   = TestCase.Command("mpirun -n 2", "SU2_CFD_AD")
     test_list.append(DAspecies3_primitiveVenturi)
 
@@ -107,7 +107,7 @@ def main():
     kenics_mixer_tutorial.cfg_dir   = "../Tutorials/incompressible_flow/Inc_Species_Transport_Composition_Dependent_Model"
     kenics_mixer_tutorial.cfg_file  = "kenics_mixer_tutorial.cfg"
     kenics_mixer_tutorial.test_iter = 10
-    kenics_mixer_tutorial.test_vals = [-7.489828, -6.823474, -6.838069, -5.157396, -7.902254, -3.174210, -7.447809, 5.000000, -1.862023, 4.000000, -5.173815, 3.000000, -6.381121, 0.025490, 0.000000, 0.025490, 0.000000, 64.111000, 8.479500, 48.105000, 7.526700]
+    kenics_mixer_tutorial.test_vals = [-7.489796, -6.823473, -6.838032, -5.157793, -7.911512, -3.166212, -7.447901, 5.000000, -1.862212, 4.000000, -5.131048, 3.000000, -6.380193, 0.025472, 0.000000, 0.025472, 0.000000, 64.105000, 8.479200, 48.099000, 7.526700]
     kenics_mixer_tutorial.command   = TestCase.Command("mpirun -n 2", "SU2_CFD")
     test_list.append(kenics_mixer_tutorial)
 
@@ -189,7 +189,7 @@ def main():
     tutorial_trans_flatplate_T3A.cfg_dir    = "../Tutorials/compressible_flow/Transitional_Flat_Plate/Langtry_and_Menter/T3A"
     tutorial_trans_flatplate_T3A.cfg_file   = "transitional_LM_model_ConfigFile.cfg"
     tutorial_trans_flatplate_T3A.test_iter  = 20
-    tutorial_trans_flatplate_T3A.test_vals  = [-5.837191, -2.092249, -3.982626, -0.302018, -1.916974, 1.668678, -3.496294, 0.391531]
+    tutorial_trans_flatplate_T3A.test_vals  = [-5.837186, -2.092246, -3.982633, -0.302219, -1.921235, 1.667190, -3.496277, 0.391605]
     tutorial_trans_flatplate_T3A.no_restart = True
     test_list.append(tutorial_trans_flatplate_T3A)
 
@@ -198,7 +198,7 @@ def main():
     tutorial_trans_flatplate_T3Am.cfg_dir    = "../Tutorials/compressible_flow/Transitional_Flat_Plate/Langtry_and_Menter/T3A-"
     tutorial_trans_flatplate_T3Am.cfg_file   = "transitional_LM_model_ConfigFile.cfg"
     tutorial_trans_flatplate_T3Am.test_iter  = 20
-    tutorial_trans_flatplate_T3Am.test_vals  = [-6.063550, -1.945057, -3.946359, -0.549026, -3.863798, 2.664577, -2.517606, 1.112977]
+    tutorial_trans_flatplate_T3Am.test_vals  = [-6.063600, -1.945057, -3.946760, -0.549063, -3.863792, 2.664453, -2.517606, 1.112979]
     tutorial_trans_flatplate_T3Am.no_restart = True
     test_list.append(tutorial_trans_flatplate_T3Am)
 
@@ -216,7 +216,7 @@ def main():
     tutorial_trans_e387_sst.cfg_dir    = "../Tutorials/compressible_flow/Transitional_Airfoil/Langtry_and_Menter/E387"
     tutorial_trans_e387_sst.cfg_file   = "transitional_SST_LM_model_ConfigFile.cfg"
     tutorial_trans_e387_sst.test_iter  = 20
-    tutorial_trans_e387_sst.test_vals  = [-6.532421, -5.085785, -0.789723, 1.078391, 0.188263, 2.000000, -9.567014]
+    tutorial_trans_e387_sst.test_vals  = [-6.532424, -5.085816, -0.789725, 1.078014, 0.188274, 2.000000, -9.567012]
     tutorial_trans_e387_sst.no_restart = True
     test_list.append(tutorial_trans_e387_sst)
 
@@ -233,7 +233,7 @@ def main():
     tutorial_nicfd_nozzle.cfg_dir   = "../Tutorials/compressible_flow/NICFD_nozzle"
     tutorial_nicfd_nozzle.cfg_file  = "NICFD_nozzle.cfg"
     tutorial_nicfd_nozzle.test_iter = 20
-    tutorial_nicfd_nozzle.test_vals = [-2.187397, -2.338536, 3.613629, 0.000000, 0.000000]
+    tutorial_nicfd_nozzle.test_vals = [-2.187397, -2.338457, 3.617301, 0.000000, 0.000000]
     tutorial_nicfd_nozzle.no_restart = True
     test_list.append(tutorial_nicfd_nozzle)
 
diff --git a/TestCases/vandv.py b/TestCases/vandv.py
index 0716d12069e..3f3f1267a80 100644
--- a/TestCases/vandv.py
+++ b/TestCases/vandv.py
@@ -54,8 +54,8 @@ def main():
     flatplate_sst1994m.cfg_dir   = "vandv/rans/flatplate"
     flatplate_sst1994m.cfg_file  = "turb_flatplate_sst.cfg"
     flatplate_sst1994m.test_iter = 5
-    flatplate_sst1994m.test_vals         = [-13.001873, -9.928107, -11.077909, -7.915809, -10.178822, -5.110162, 0.002808]
-    flatplate_sst1994m.test_vals_aarch64 = [-13.001873, -9.928107, -11.077909, -7.915809, -10.178822, -5.110162, 0.002808]
+    flatplate_sst1994m.test_vals         = [-13.023358, -9.956752, -11.099910, -7.933220, -10.206577, -5.132343, 0.002808]
+    flatplate_sst1994m.test_vals_aarch64 = [-13.023358, -9.956752, -11.099910, -7.933220, -10.206577, -5.132343, 0.002808]
     test_list.append(flatplate_sst1994m)
 
     # bump in channel - sst-v1994m
@@ -63,8 +63,8 @@ def main():
     bump_sst1994m.cfg_dir   = "vandv/rans/bump_in_channel"
     bump_sst1994m.cfg_file  = "turb_bump_sst.cfg"
     bump_sst1994m.test_iter = 5
-    bump_sst1994m.test_vals         = [-13.005815, -10.677095, -10.604787, -7.647741, -10.720450, -5.556079, 0.004972]
-    bump_sst1994m.test_vals_aarch64 = [-13.005815, -10.677095, -10.604787, -7.647741, -10.720450, -5.556079, 0.004972]
+    bump_sst1994m.test_vals         = [-12.986182, -10.719941, -10.556276, -7.606531, -10.774915, -5.605156, 0.004972]
+    bump_sst1994m.test_vals_aarch64 = [-12.986182, -10.719941, -10.556276, -7.606531, -10.774915, -5.605156, 0.004972]
     test_list.append(bump_sst1994m)
 
     # SWBLI SA

From 4ddc47f8ef2191058bdae8f6a03bae2a9c41332a Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 1 Jul 2023 11:54:39 -0700
Subject: [PATCH 514/656] parallel regression wo restarts

---
 TestCases/parallel_regression.py | 140 +++++++++++++++----------------
 1 file changed, 70 insertions(+), 70 deletions(-)

diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 35f1f890050..b2610bd9823 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -139,7 +139,7 @@ def main():
     invwedge_ausm_m.cfg_dir = "nonequilibrium/invwedge"
     invwedge_ausm_m.cfg_file = "invwedge_am.cfg"
     invwedge_ausm_m.test_iter = 10
-    invwedge_ausm_m.test_vals = [-1.055083, -1.579845, -16.739725, -17.063618, -17.012831, 2.265430, 1.797602, 5.302740, 0.85654]
+    invwedge_ausm_m.test_vals = [-1.055083, -1.579845, -16.739725, -17.063618, -17.012831, 2.265430, 1.797602, 5.302740, 0.856548]
     invwedge_ausm_m.test_vals_aarch64 = [-1.055083, -1.579845, -16.739725, -17.063618, -17.012831, 2.265430, 1.797602, 5.302740, 0.85654]
     test_list.append(invwedge_ausm_m)
 
@@ -182,7 +182,7 @@ def main():
     partial_cat.cfg_dir = "nonequilibrium/visc_wedge"
     partial_cat.cfg_file = "partial_cat.cfg"
     partial_cat.test_iter = 10
-    partial_cat.test_vals = [-5.210300, -5.735063, -20.880374, -20.825890, -23.475263, 1.806281, -2.813924, -0.078469, 0.496017, 2.9021e+04]
+    partial_cat.test_vals = [-5.210300, -5.735063, -20.880374, -20.825890, -23.475263, 1.806281, -2.813924, -0.078469, 0.496017, 29021.000000]
     test_list.append(partial_cat)
 
     # Viscous cylinder, ionization, Gupta-Yos
@@ -254,7 +254,7 @@ def main():
     bluntbody.cfg_dir   = "euler/bluntbody"
     bluntbody.cfg_file  = "blunt.cfg"
     bluntbody.test_iter = 20
-    bluntbody.test_vals = [0.540009, 6.916653, 0.000000, 1.868976] #last 4 columns
+    bluntbody.test_vals = [0.540009, 6.916653, 0.000000, 1.868976]
     test_list.append(bluntbody)
 
     # Equivalent area NACA64-206
@@ -262,7 +262,7 @@ def main():
     ea_naca64206.cfg_dir   = "optimization_euler/equivalentarea_naca64206"
     ea_naca64206.cfg_file  = "NACA64206.cfg"
     ea_naca64206.test_iter = 10
-    ea_naca64206.test_vals = [-1.076215, -0.391987, -0.000701, 67775.0]
+    ea_naca64206.test_vals = [-1.076215, -0.391987, -0.000701, 67775.000000]
     test_list.append(ea_naca64206)
     
     # SUPERSONIC FLOW PAST A RAMP IN A CHANNEL
@@ -270,7 +270,7 @@ def main():
     ramp.cfg_dir = "euler/ramp"
     ramp.cfg_file = "inv_ramp.cfg"
     ramp.test_iter = 10
-    ramp.test_vals = [-13.399623, -7.788893, -0.081064, 0.056474] #last 4 columns
+    ramp.test_vals = [-13.399623, -7.788893, -0.081064, 0.056474]
     test_list.append(ramp)
 
     ##########################
@@ -290,7 +290,7 @@ def main():
     flatplate_udobj.cfg_dir   = "user_defined_functions"
     flatplate_udobj.cfg_file  = "lam_flatplate.cfg"
     flatplate_udobj.test_iter = 20
-    flatplate_udobj.test_vals = [-6.653802, -1.181430, -0.794887, 0.000611, -0.000369, 0.000736, -0.001104, 596.690000, 299.800000, 296.890000, 21.492000, 0.563990, 37.148, 2.278700]
+    flatplate_udobj.test_vals = [-6.653802, -1.181430, -0.794887, 0.000611, -0.000369, 0.000736, -0.001104, 596.690000, 299.800000, 296.890000, 21.492000, 0.563990, 37.148000, 2.278700]
     test_list.append(flatplate_udobj)
 
     # Laminar cylinder (steady)
@@ -344,7 +344,7 @@ def main():
     rae2822_sst.cfg_dir   = "rans/rae2822"
     rae2822_sst.cfg_file  = "turb_SST_RAE2822.cfg"
     rae2822_sst.test_iter = 20
-    rae2822_sst.test_vals = [-0.510640, 4.868654, 0.813724, 0.062439, -80115.000000]
+    rae2822_sst.test_vals = [-0.510369, 4.870643, 0.816647, 0.061833, -71779.000000]
     test_list.append(rae2822_sst)
 
     # RAE2822 SST_SUST
@@ -352,7 +352,7 @@ def main():
     rae2822_sst_sust.cfg_dir   = "rans/rae2822"
     rae2822_sst_sust.cfg_file  = "turb_SST_SUST_RAE2822.cfg"
     rae2822_sst_sust.test_iter = 20
-    rae2822_sst_sust.test_vals = [-2.425725, 4.868653, 0.813724, 0.062438]
+    rae2822_sst_sust.test_vals = [-2.537339, 4.870643, 0.816647, 0.061833]
     test_list.append(rae2822_sst_sust)
 
     # Flat plate
@@ -394,7 +394,7 @@ def main():
     turb_oneram6_nk.cfg_dir   = "rans/oneram6"
     turb_oneram6_nk.cfg_file  = "turb_ONERAM6_nk.cfg"
     turb_oneram6_nk.test_iter = 20
-    turb_oneram6_nk.test_vals = [-4.892253, -4.514006, -11.432312, 0.221026, 0.045570, 2.000000, -0.899460, 31.384000]
+    turb_oneram6_nk.test_vals = [-4.892252, -4.514006, -11.432306, 0.221025, 0.045570, 2.000000, -0.899460, 31.384000]
     turb_oneram6_nk.timeout   = 600
     turb_oneram6_nk.tol       = 0.0001
     test_list.append(turb_oneram6_nk)
@@ -440,7 +440,7 @@ def main():
     turb_naca0012_sst_1994_KLm.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst_1994_KLm.cfg_file  = "turb_NACA0012_sst_1994-KLm.cfg"
     turb_naca0012_sst_1994_KLm.test_iter = 10
-    turb_naca0012_sst_1994_KLm.test_vals = [-8.567222, -10.798741, -3.990574, 1.049274, 0.019199, -1.809143]
+    turb_naca0012_sst_1994_KLm.test_vals = [-8.616539, -10.868753, -4.060879, 1.049473, 0.019192, -1.867965]
     turb_naca0012_sst_1994_KLm.timeout   = 3200
     test_list.append(turb_naca0012_sst_1994_KLm)
 
@@ -450,7 +450,7 @@ def main():
     turb_naca0012_sst_fixedvalues.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst_fixedvalues.cfg_file  = "turb_NACA0012_sst_fixedvalues.cfg"
     turb_naca0012_sst_fixedvalues.test_iter = 10
-    turb_naca0012_sst_fixedvalues.test_vals = [-5.216685, -9.561914, -1.565777, 1.022393, 0.040542, -3.729635]
+    turb_naca0012_sst_fixedvalues.test_vals = [-5.216737, -10.025507, -1.615166, 1.021891, 0.040213, -3.731060]
     turb_naca0012_sst_fixedvalues.timeout   = 3200
     test_list.append(turb_naca0012_sst_fixedvalues)
 
@@ -459,7 +459,7 @@ def main():
     turb_naca0012_sst_expliciteuler.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst_expliciteuler.cfg_file  = "turb_NACA0012_sst_expliciteuler.cfg"
     turb_naca0012_sst_expliciteuler.test_iter = 10
-    turb_naca0012_sst_expliciteuler.test_vals = [-3.532228, -3.157766, 3.364025, 1.124824, 0.501717, -float("inf")]
+    turb_naca0012_sst_expliciteuler.test_vals = [-3.532289, -3.157766, 3.364024, 1.122901, 0.500798, -inf]
     turb_naca0012_sst_expliciteuler.timeout   = 3200
     test_list.append(turb_naca0012_sst_expliciteuler)
 
@@ -495,7 +495,7 @@ def main():
     turb_naca0012_sst_restart_mg.cfg_file  = "turb_NACA0012_sst_multigrid_restart.cfg"
     turb_naca0012_sst_restart_mg.test_iter = 20
     turb_naca0012_sst_restart_mg.ntest_vals = 5
-    turb_naca0012_sst_restart_mg.test_vals = [-7.619889, -7.729499, -1.981039, -0.000016, 0.079062]
+    turb_naca0012_sst_restart_mg.test_vals = [-7.612353, -7.432347, -1.918249, -0.000013, 0.079110]
     turb_naca0012_sst_restart_mg.timeout   = 3200
     turb_naca0012_sst_restart_mg.tol       = 0.000001
     test_list.append(turb_naca0012_sst_restart_mg)
@@ -561,7 +561,7 @@ def main():
     sp_pipeSlice_3d_dp_hf_tp.cfg_dir   = "incomp_navierstokes/streamwise_periodic/pipeSlice_3d"
     sp_pipeSlice_3d_dp_hf_tp.cfg_file  = "sp_pipeSlice_3d_dp_hf_tp.cfg"
     sp_pipeSlice_3d_dp_hf_tp.test_iter = 10
-    sp_pipeSlice_3d_dp_hf_tp.test_vals = [-11.119796, -11.234737, -8.694310, -0.000023] #last 4 lines
+    sp_pipeSlice_3d_dp_hf_tp.test_vals = [-11.119796, -11.234737, -8.694310, -0.000023]
     test_list.append(sp_pipeSlice_3d_dp_hf_tp)
 
     # 2D pin array with heat transfer BC on pin surfaces
@@ -569,7 +569,7 @@ def main():
     inc_heatTransfer_BC.cfg_dir   = "incomp_navierstokes/streamwise_periodic/chtPinArray_2d"
     inc_heatTransfer_BC.cfg_file  = "BC_HeatTransfer.cfg"
     inc_heatTransfer_BC.test_iter = 50
-    inc_heatTransfer_BC.test_vals = [-8.242651, -7.341179, -7.407346, -0.152603, -1667.300000] #last 5 lines
+    inc_heatTransfer_BC.test_vals = [-8.242651, -7.341179, -7.407346, -0.152603, -1667.300000]
     test_list.append(inc_heatTransfer_BC)
 
     ############################
@@ -589,7 +589,7 @@ def main():
     inc_turb_naca0012_sst_sust.cfg_dir   = "incomp_rans/naca0012"
     inc_turb_naca0012_sst_sust.cfg_file  = "naca0012_SST_SUST.cfg"
     inc_turb_naca0012_sst_sust.test_iter = 20
-    inc_turb_naca0012_sst_sust.test_vals = [-7.274050, 0.145887, -0.000001, 0.312023]
+    inc_turb_naca0012_sst_sust.test_vals = [-7.270578, 0.018403, -0.000001, 0.307688]
     test_list.append(inc_turb_naca0012_sst_sust)
 
     ####################
@@ -601,7 +601,7 @@ def main():
     fem_euler_naca0012.cfg_dir   = "hom_euler/NACA0012_5thOrder"
     fem_euler_naca0012.cfg_file  = "fem_NACA0012_reg.cfg"
     fem_euler_naca0012.test_iter = 10
-    fem_euler_naca0012.test_vals = [-6.519946,-5.976944,0.255551,0.000028] #last 4 columns
+    fem_euler_naca0012.test_vals = [-6.519946, -5.976944, 0.255551, 0.000028]
     test_list.append(fem_euler_naca0012)
 
     ############################
@@ -613,7 +613,7 @@ def main():
     fem_ns_flatplate.cfg_dir   = "hom_navierstokes/FlatPlate/nPoly4"
     fem_ns_flatplate.cfg_file  = "lam_flatplate_reg.cfg"
     fem_ns_flatplate.test_iter = 25
-    fem_ns_flatplate.test_vals = [1.383727,3.175247,0.058387,0.257951] #last 4 columns
+    fem_ns_flatplate.test_vals = [1.383727, 3.175247, 0.058387, 0.257951]
     test_list.append(fem_ns_flatplate)
 
     # Steady cylinder
@@ -621,7 +621,7 @@ def main():
     fem_ns_cylinder.cfg_dir   = "hom_navierstokes/CylinderViscous/nPoly3"
     fem_ns_cylinder.cfg_file  = "fem_Cylinder_reg.cfg"
     fem_ns_cylinder.test_iter = 10
-    fem_ns_cylinder.test_vals = [0.454960,0.979123,-0.000028,79.984799] #last 4 columns
+    fem_ns_cylinder.test_vals = [0.454960, 0.979123, -0.000028, 79.984799]
     test_list.append(fem_ns_cylinder)
 
     # Steady sphere
@@ -629,7 +629,7 @@ def main():
     fem_ns_sphere.cfg_dir   = "hom_navierstokes/SphereViscous/nPoly3_QuadDominant"
     fem_ns_sphere.cfg_file  = "fem_Sphere_reg.cfg"
     fem_ns_sphere.test_iter = 10
-    fem_ns_sphere.test_vals = [-0.288121,0.240324,0.000258,21.797363] #last 4 columns
+    fem_ns_sphere.test_vals = [-0.288121, 0.240324, 0.000258, 21.797363]
     test_list.append(fem_ns_sphere)
 
     # Unsteady sphere ADER
@@ -637,7 +637,7 @@ def main():
     fem_ns_sphere_ader.cfg_dir   = "hom_navierstokes/SphereViscous/nPoly3_QuadDominant"
     fem_ns_sphere_ader.cfg_file  = "fem_Sphere_reg_ADER.cfg"
     fem_ns_sphere_ader.test_iter = 10
-    fem_ns_sphere_ader.test_vals = [-35.000000,-35.000000,0.000047,31.110911] #last 4 columns
+    fem_ns_sphere_ader.test_vals = [-35.000000, -35.000000, 0.000047, 31.110911]
     test_list.append(fem_ns_sphere_ader)
 
     # Unsteady cylinder
@@ -645,7 +645,7 @@ def main():
     fem_ns_unsteady_cylinder.cfg_dir   = "hom_navierstokes/UnsteadyCylinder/nPoly4"
     fem_ns_unsteady_cylinder.cfg_file  = "fem_unst_cylinder.cfg"
     fem_ns_unsteady_cylinder.test_iter = 11
-    fem_ns_unsteady_cylinder.test_vals = [-3.558582,-3.014464,-0.038927,1.383983] #last 4 columns
+    fem_ns_unsteady_cylinder.test_vals = [-3.558582, -3.014464, -0.038927, 1.383983]
     fem_ns_unsteady_cylinder.unsteady  = True
     test_list.append(fem_ns_unsteady_cylinder)
 
@@ -654,7 +654,7 @@ def main():
     fem_ns_unsteady_cylinder_ader.cfg_dir   = "hom_navierstokes/UnsteadyCylinder/nPoly4"
     fem_ns_unsteady_cylinder_ader.cfg_file  = "fem_unst_cylinder_ADER.cfg"
     fem_ns_unsteady_cylinder_ader.test_iter = 11
-    fem_ns_unsteady_cylinder_ader.test_vals = [-35.000000,-35.000000,-0.041003,1.391339] #last 4 columns
+    fem_ns_unsteady_cylinder_ader.test_vals = [-35.000000, -35.000000, -0.041003, 1.391339]
     fem_ns_unsteady_cylinder_ader.unsteady  = True
     test_list.append(fem_ns_unsteady_cylinder_ader)
 
@@ -732,7 +732,7 @@ def main():
     contadj_naca0012.cfg_dir   = "cont_adj_euler/naca0012"
     contadj_naca0012.cfg_file  = "inv_NACA0012.cfg"
     contadj_naca0012.test_iter = 5
-    contadj_naca0012.test_vals = [-9.300815, -14.587362, 0.300920, 0.019552]
+    contadj_naca0012.test_vals = [-9.300816, -14.587365, 0.300920, 0.019552]
     test_list.append(contadj_naca0012)
 
     # Inviscid ONERA M6
@@ -748,7 +748,7 @@ def main():
     contadj_wedge.cfg_dir   = "cont_adj_euler/wedge"
     contadj_wedge.cfg_file  = "inv_wedge_ROE.cfg"
     contadj_wedge.test_iter = 10
-    contadj_wedge.test_vals = [2.872691, -2.755572, 853010.000000, 0.000000] #last 4 columns
+    contadj_wedge.test_vals = [2.872691, -2.755572, 853010.000000, -0.000000]
     test_list.append(contadj_wedge)
 
     # Inviscid fixed CL NACA0012
@@ -776,7 +776,7 @@ def main():
     contadj_ns_naca0012_sub.cfg_dir   = "cont_adj_navierstokes/naca0012_sub"
     contadj_ns_naca0012_sub.cfg_file  = "lam_NACA0012.cfg"
     contadj_ns_naca0012_sub.test_iter = 20
-    contadj_ns_naca0012_sub.test_vals = [-2.743268, -8.215193, 0.518810, 0.001210] #last 4 columns
+    contadj_ns_naca0012_sub.test_vals = [-2.743268, -8.215193, 0.518810, 0.001210]
     test_list.append(contadj_ns_naca0012_sub)
 
     # Adjoint laminar naca0012 transonic
@@ -784,7 +784,7 @@ def main():
     contadj_ns_naca0012_trans.cfg_dir   = "cont_adj_navierstokes/naca0012_trans"
     contadj_ns_naca0012_trans.cfg_file  = "lam_NACA0012.cfg"
     contadj_ns_naca0012_trans.test_iter = 20
-    contadj_ns_naca0012_trans.test_vals = [ -1.039664, -6.575019, 1.772300, 0.012495] #last 4 columns
+    contadj_ns_naca0012_trans.test_vals = [-1.039664, -6.575019, 1.772300, 0.012495]
     test_list.append(contadj_ns_naca0012_trans)
 
     #######################################################
@@ -796,7 +796,7 @@ def main():
     contadj_rans_naca0012.cfg_dir   = "cont_adj_rans/naca0012"
     contadj_rans_naca0012.cfg_file  = "turb_nasa.cfg"
     contadj_rans_naca0012.test_iter = 20
-    contadj_rans_naca0012.test_vals = [-0.794162, -5.761722, 19.214000, -0.000000] #last 4 columns
+    contadj_rans_naca0012.test_vals = [-0.794162, -5.761722, 19.214000, -0.000000]
     test_list.append(contadj_rans_naca0012)
 
     # Adjoint turbulent NACA0012 with binary restarts
@@ -804,7 +804,7 @@ def main():
     contadj_rans_naca0012_bin.cfg_dir   = "cont_adj_rans/naca0012"
     contadj_rans_naca0012_bin.cfg_file  = "turb_nasa_binary.cfg"
     contadj_rans_naca0012_bin.test_iter = 18
-    contadj_rans_naca0012_bin.test_vals = [-0.794169, -5.761671, 19.214000, -0.000000] #last 4 columns
+    contadj_rans_naca0012_bin.test_vals = [-0.794169, -5.761671, 19.214000, -0.000000]
     test_list.append(contadj_rans_naca0012_bin)
 
     # Adjoint turbulent RAE2822
@@ -824,7 +824,7 @@ def main():
     turb_naca0012_1c.cfg_dir   = "rans_uq/naca0012"
     turb_naca0012_1c.cfg_file  = "turb_NACA0012_uq_1c.cfg"
     turb_naca0012_1c.test_iter = 10
-    turb_naca0012_1c.test_vals         = [-4.976246, 1.141479, 0.459999, -0.078853]
+    turb_naca0012_1c.test_vals         = [-4.976284, 1.141136, 0.463115, -0.083307]
     turb_naca0012_1c.test_vals_aarch64 = [-4.983548, 1.138789, 0.456805, -0.079667]
     test_list.append(turb_naca0012_1c)
 
@@ -833,7 +833,7 @@ def main():
     turb_naca0012_2c.cfg_dir   = "rans_uq/naca0012"
     turb_naca0012_2c.cfg_file  = "turb_NACA0012_uq_2c.cfg"
     turb_naca0012_2c.test_iter = 10
-    turb_naca0012_2c.test_vals         = [-5.483323, 0.968820, 0.304757, -0.113468]
+    turb_naca0012_2c.test_vals         = [-5.483317, 0.968654, 0.307611, -0.118062]
     turb_naca0012_2c.test_vals_aarch64 = [-5.483345, 0.968812, 0.305213, -0.113317]
     test_list.append(turb_naca0012_2c)
 
@@ -842,7 +842,7 @@ def main():
     turb_naca0012_3c.cfg_dir   = "rans_uq/naca0012"
     turb_naca0012_3c.cfg_file  = "turb_NACA0012_uq_3c.cfg"
     turb_naca0012_3c.test_iter = 10
-    turb_naca0012_3c.test_vals = [-5.584310, 0.931348, 0.279056, -0.113209]
+    turb_naca0012_3c.test_vals = [-5.584309, 0.931259, 0.281831, -0.117821]
     test_list.append(turb_naca0012_3c)
 
     # NACA0012 p1c1
@@ -850,7 +850,7 @@ def main():
     turb_naca0012_p1c1.cfg_dir   = "rans_uq/naca0012"
     turb_naca0012_p1c1.cfg_file  = "turb_NACA0012_uq_p1c1.cfg"
     turb_naca0012_p1c1.test_iter = 10
-    turb_naca0012_p1c1.test_vals         = [-5.128867, 1.077141, 0.586532, -0.047632]
+    turb_naca0012_p1c1.test_vals         = [-5.128887, 1.076846, 0.589839, -0.051939]
     turb_naca0012_p1c1.test_vals_aarch64 = [-5.130279, 1.076643, 0.587076, -0.047445]
     test_list.append(turb_naca0012_p1c1)
 
@@ -859,7 +859,7 @@ def main():
     turb_naca0012_p1c2.cfg_dir   = "rans_uq/naca0012"
     turb_naca0012_p1c2.cfg_file  = "turb_NACA0012_uq_p1c2.cfg"
     turb_naca0012_p1c2.test_iter = 10
-    turb_naca0012_p1c2.test_vals         = [-5.554659, 0.943705, 0.399234, -0.095799]
+    turb_naca0012_p1c2.test_vals         = [-5.554633, 0.943626, 0.402263, -0.100275]
     turb_naca0012_p1c2.test_vals_aarch64 = [-5.554645, 0.943709, 0.398620, -0.096021]
     test_list.append(turb_naca0012_p1c2)
 
@@ -921,7 +921,7 @@ def main():
     square_cylinder.cfg_dir   = "unsteady/square_cylinder"
     square_cylinder.cfg_file  = "turb_square.cfg"
     square_cylinder.test_iter = 3
-    square_cylinder.test_vals = [-1.158117, 0.067945, 1.399789, 2.220404, 1.399743, 2.218605, -0.453170]
+    square_cylinder.test_vals = [-1.173603, 0.058045, 1.399795, 2.220404, 1.399749, 2.218605, -0.453330]
     square_cylinder.unsteady  = True
     test_list.append(square_cylinder)
 
@@ -957,7 +957,7 @@ def main():
     unst_inc_turb_naca0015_sa.cfg_dir   = "unsteady/pitching_naca0015_rans_inc"
     unst_inc_turb_naca0015_sa.cfg_file  = "config_incomp_turb_sa.cfg"
     unst_inc_turb_naca0015_sa.test_iter = 1
-    unst_inc_turb_naca0015_sa.test_vals = [-3.004011, -6.876230, 1.487888, 0.421869]
+    unst_inc_turb_naca0015_sa.test_vals = [-3.004012, -6.876220, 1.487882, 0.421861]
     unst_inc_turb_naca0015_sa.unsteady  = True
     test_list.append(unst_inc_turb_naca0015_sa)
 
@@ -995,7 +995,7 @@ def main():
     coolprop_fluidModel.cfg_dir   = "nicf/coolprop"
     coolprop_fluidModel.cfg_file  = "fluidModel.cfg"
     coolprop_fluidModel.test_iter = 5
-    coolprop_fluidModel.test_vals = [-4.525458, -1.578441, 3.439057, 0.000000, 0.000000]
+    coolprop_fluidModel.test_vals = [-4.525459, -1.578697, 3.443116, 0.000000, 0.000000]
     test_list.append(coolprop_fluidModel)
 
     # Rarefaction Q1D nozzle, include CoolProp transport model
@@ -1003,7 +1003,7 @@ def main():
     coolprop_transportModel.cfg_dir   = "nicf/coolprop"
     coolprop_transportModel.cfg_file  = "transportModel.cfg"
     coolprop_transportModel.test_iter = 5
-    coolprop_transportModel.test_vals = [-4.527922, -1.308741, 4.630469, 0.000000, 0.000000]
+    coolprop_transportModel.test_vals = [-4.527922, -1.308648, 4.630717, 0.000000, 0.000000]
     test_list.append(coolprop_transportModel)
 
     ######################################
@@ -1023,7 +1023,7 @@ def main():
     axial_stage2D.cfg_dir   = "turbomachinery/axial_stage_2D"
     axial_stage2D.cfg_file  = "Axial_stage2D.cfg"
     axial_stage2D.test_iter = 20
-    axial_stage2D.test_vals = [1.047301, 1.661328, -2.913923, 2.588194, -2.486769, 3.050953, 106380, 106380]
+    axial_stage2D.test_vals = [0.974805, 1.534447, -2.897694, 2.599376, -2.418379, 3.087219, 106380.000000, 106380.000000]
     test_list.append(axial_stage2D)
 
     # 2D transonic stator restart
@@ -1106,7 +1106,7 @@ def main():
     bars_SST_2D.cfg_dir   = "sliding_interface/bars_SST_2D"
     bars_SST_2D.cfg_file  = "bars.cfg"
     bars_SST_2D.test_iter = 13
-    bars_SST_2D.test_vals = [13.000000, -0.604409, -1.523885]
+    bars_SST_2D.test_vals = [13.000000, -0.773513, -1.700012]
     bars_SST_2D.multizone = True
     test_list.append(bars_SST_2D)
 
@@ -1115,7 +1115,7 @@ def main():
     slinc_steady.cfg_dir   = "sliding_interface/incompressible_steady"
     slinc_steady.cfg_file  = "config.cfg"
     slinc_steady.test_iter = 19
-    slinc_steady.test_vals = [19.000000, -1.778863, -2.040209] #last 3 columns
+    slinc_steady.test_vals = [19.000000, -1.778863, -2.040209]
     slinc_steady.timeout   = 100
     slinc_steady.tol       = 0.00002
     slinc_steady.multizone = True
@@ -1141,7 +1141,7 @@ def main():
     statbeam3d.cfg_dir   = "fea_fsi/StatBeam_3d"
     statbeam3d.cfg_file  = "configBeam_3d.cfg"
     statbeam3d.test_iter = 0
-    statbeam3d.test_vals         = [-8.396797, -8.162206, -8.156102, 64095.0] #last 4 columns
+    statbeam3d.test_vals         = [-8.396797, -8.162206, -8.156102, 64095.000000]
     statbeam3d.test_vals_aarch64 = [-8.396793, -8.162255, -8.156118, 64095.0] #last 4 columns
     statbeam3d.command   = TestCase.Command(exec = "parallel_computation_fsi.py", param = "-f")
     test_list.append(statbeam3d)
@@ -1151,7 +1151,7 @@ def main():
     dynbeam2d.cfg_dir   = "fea_fsi/DynBeam_2d"
     dynbeam2d.cfg_file  = "configBeam_2d.cfg"
     dynbeam2d.test_iter = 6
-    dynbeam2d.test_vals = [-3.240015, 2.895057, -0.353146, 6.6127e+04] #last 4 columns
+    dynbeam2d.test_vals = [-3.240015, 2.895057, -0.353146, 66127.000000]
     dynbeam2d.unsteady  = True
     test_list.append(dynbeam2d)
 
@@ -1160,7 +1160,7 @@ def main():
     fsi2d.cfg_dir   = "fea_fsi/WallChannel_2d"
     fsi2d.cfg_file  = "configFSI.cfg"
     fsi2d.test_iter = 4
-    fsi2d.test_vals = [4, 0, -3.743210, -4.133483] #last 4 columns
+    fsi2d.test_vals = [4.000000, 0.000000, -3.743210, -4.133483]
     fsi2d.command   = TestCase.Command(exec = "parallel_computation_fsi.py", param = "-f")
     fsi2d.multizone= True
     fsi2d.unsteady = True
@@ -1171,7 +1171,7 @@ def main():
     stat_fsi.cfg_dir   = "fea_fsi/stat_fsi"
     stat_fsi.cfg_file  = "config.cfg"
     stat_fsi.test_iter = 7
-    stat_fsi.test_vals = [-3.296605, -4.934646, 0.000000, 7.000000] #last 4 columns
+    stat_fsi.test_vals = [-3.296605, -4.934646, 0.000000, 7.000000]
     stat_fsi.multizone = True
     test_list.append(stat_fsi)
 
@@ -1190,7 +1190,7 @@ def main():
     stat_fsi_restart.cfg_dir   = "fea_fsi/stat_fsi"
     stat_fsi_restart.cfg_file  = "config_restart.cfg"
     stat_fsi_restart.test_iter = 1
-    stat_fsi_restart.test_vals = [-3.435926, -4.264912, 0.000000, 28.000000] #last 4 columns
+    stat_fsi_restart.test_vals = [-3.435926, -4.264912, 0.000000, 28.000000]
     stat_fsi_restart.multizone = True
     test_list.append(stat_fsi_restart)
 
@@ -1216,7 +1216,7 @@ def main():
     solid_periodic_pins.cfg_dir   = "solid_heat_conduction/periodic_pins"
     solid_periodic_pins.cfg_file  = "configSolid.cfg"
     solid_periodic_pins.test_iter = 750
-    solid_periodic_pins.test_vals = [-15.878977, -14.569206, 300.900000, 425.320000, 0.000000, 5.000000, -1.672737] #last 7 lines
+    solid_periodic_pins.test_vals = [-15.878977, -14.569206, 300.900000, 425.320000, 0.000000, 5.000000, -1.672737]
     solid_periodic_pins.test_vals_aarch64 = [-15.879010, -14.569206, 300.900000, 425.320000, 0.000000, 5.000000, -1.672630] #last 7 lines
     test_list.append(solid_periodic_pins)
 
@@ -1229,7 +1229,7 @@ def main():
     cht_incompressible.cfg_dir   = "coupled_cht/incomp_2d"
     cht_incompressible.cfg_file  = "cht_2d_3cylinders.cfg"
     cht_incompressible.test_iter = 10
-    cht_incompressible.test_vals = [-2.128826, -0.588813, -0.588813, -0.588813] #last 4 columns
+    cht_incompressible.test_vals = [-2.128827, -0.588812, -0.588812, -0.588812]
     cht_incompressible.multizone = True
     test_list.append(cht_incompressible)
 
@@ -1247,7 +1247,7 @@ def main():
     sp_pinArray_cht_2d_dp_hf.cfg_dir   = "incomp_navierstokes/streamwise_periodic/chtPinArray_2d"
     sp_pinArray_cht_2d_dp_hf.cfg_file  = "configMaster.cfg"
     sp_pinArray_cht_2d_dp_hf.test_iter = 100
-    sp_pinArray_cht_2d_dp_hf.test_vals = [0.255546, -0.778969, -0.964351, -0.752492, 208.023676, 351.010000, -0.000000, -0.752490, 0.752490]
+    sp_pinArray_cht_2d_dp_hf.test_vals = [0.104306, -1.005859, -1.028870, -0.753282, 208.023676, 353.490000, -0.000000, -0.753280, 0.753280]
     sp_pinArray_cht_2d_dp_hf.multizone = True
     test_list.append(sp_pinArray_cht_2d_dp_hf)
 
@@ -1270,7 +1270,7 @@ def main():
     pywrapper_naca0012.cfg_dir   = "euler/naca0012"
     pywrapper_naca0012.cfg_file  = "inv_NACA0012_Roe.cfg"
     pywrapper_naca0012.test_iter = 100
-    pywrapper_naca0012.test_vals = [-6.747210, -6.149915, 0.333445, 0.021241] #last 4 columns
+    pywrapper_naca0012.test_vals = [-6.747210, -6.149915, 0.333445, 0.021241]
     pywrapper_naca0012.command   = TestCase.Command("mpirun -np 2", "SU2_CFD.py", "--parallel -f")
     test_list.append(pywrapper_naca0012)
 
@@ -1289,7 +1289,7 @@ def main():
     pywrapper_square_cylinder.cfg_dir   = "unsteady/square_cylinder"
     pywrapper_square_cylinder.cfg_file  = "turb_square.cfg"
     pywrapper_square_cylinder.test_iter = 10
-    pywrapper_square_cylinder.test_vals = [-1.136553, -0.347305, 1.407915, 2.358881, 1.404192, 2.301559, -0.348120]
+    pywrapper_square_cylinder.test_vals = [-1.175619, -0.352238, 1.408450, 2.360729, 1.404693, 2.302284, -0.347980]
     pywrapper_square_cylinder.command   = TestCase.Command("mpirun -np 2", "SU2_CFD.py", "--parallel -f")
     pywrapper_square_cylinder.unsteady  = True
     test_list.append(pywrapper_square_cylinder)
@@ -1309,7 +1309,7 @@ def main():
     pywrapper_custom_fea_load.cfg_dir = "py_wrapper/custom_load_fea"
     pywrapper_custom_fea_load.cfg_file = "config.cfg"
     pywrapper_custom_fea_load.test_iter = 13
-    pywrapper_custom_fea_load.test_vals = [-7.263559, -4.946814, -14.165142, 34, -6.380144, 320.58]
+    pywrapper_custom_fea_load.test_vals = [-7.263559, -4.946814, -14.165142, 34.000000, -6.380144, 320.580000]
     pywrapper_custom_fea_load.command = TestCase.Command("mpirun -np 2", "python", "run.py")
     test_list.append(pywrapper_custom_fea_load)
 
@@ -1318,7 +1318,7 @@ def main():
     pywrapper_fsi2d.cfg_dir   = "fea_fsi/WallChannel_2d"
     pywrapper_fsi2d.cfg_file  = "configFSI.cfg"
     pywrapper_fsi2d.test_iter = 4
-    pywrapper_fsi2d.test_vals = [4, 0, -3.743210, -4.133483] #last 4 columns
+    pywrapper_fsi2d.test_vals = [4.000000, 0.000000, -3.743210, -4.133483]
     pywrapper_fsi2d.command   = TestCase.Command("mpirun -np 2", "SU2_CFD.py", "--nZone 2 --fsi True --parallel -f")
     pywrapper_fsi2d.unsteady  = True
     pywrapper_fsi2d.multizone = True
@@ -1329,7 +1329,7 @@ def main():
     pywrapper_unsteadyCHT.cfg_dir       = "py_wrapper/flatPlate_unsteady_CHT"
     pywrapper_unsteadyCHT.cfg_file      = "unsteady_CHT_FlatPlate_Conf.cfg"
     pywrapper_unsteadyCHT.test_iter     = 5
-    pywrapper_unsteadyCHT.test_vals     = [-1.614167, 2.245725, -0.001241, 0.175713]
+    pywrapper_unsteadyCHT.test_vals     = [-1.614167, 2.240663, -0.001316, 0.177491]
     pywrapper_unsteadyCHT.command       = TestCase.Command("mpirun -np 2", "python", "launch_unsteady_CHT_FlatPlate.py --parallel -f")
     pywrapper_unsteadyCHT.unsteady      = True
     test_list.append(pywrapper_unsteadyCHT)
@@ -1339,7 +1339,7 @@ def main():
     pywrapper_rigidMotion.cfg_dir       = "py_wrapper/flatPlate_rigidMotion"
     pywrapper_rigidMotion.cfg_file      = "flatPlate_rigidMotion_Conf.cfg"
     pywrapper_rigidMotion.test_iter     = 5
-    pywrapper_rigidMotion.test_vals     = [-1.614170, 2.242953, 0.350037, 0.093116]
+    pywrapper_rigidMotion.test_vals     = [-1.614165, 2.238591, 0.349970, 0.095593]
     pywrapper_rigidMotion.command       = TestCase.Command("mpirun -np 2", "python", "launch_flatPlate_rigidMotion.py --parallel -f")
     pywrapper_rigidMotion.unsteady      = True
     test_list.append(pywrapper_rigidMotion)
@@ -1349,7 +1349,7 @@ def main():
     pywrapper_deformingBump.cfg_dir = "py_wrapper/deforming_bump_in_channel"
     pywrapper_deformingBump.cfg_file = "config.cfg"
     pywrapper_deformingBump.test_iter = 1
-    pywrapper_deformingBump.test_vals = [0.5, 0, -2.55436, -1.084594, -0.024882, 2.907803, 8.785498, -0.363585]
+    pywrapper_deformingBump.test_vals = [0.500000, 0.000000, -2.554360, -1.084594, -0.024882, 2.907803, 8.785498, -0.363585]
     pywrapper_deformingBump.command = TestCase.Command("mpirun -np 2", "python", "run.py")
     pywrapper_deformingBump.unsteady = True
     test_list.append(pywrapper_deformingBump)
@@ -1363,7 +1363,7 @@ def main():
     mms_fvm_ns.cfg_dir   = "mms/fvm_navierstokes"
     mms_fvm_ns.cfg_file  = "lam_mms_roe.cfg"
     mms_fvm_ns.test_iter = 20
-    mms_fvm_ns.test_vals = [-2.851428, 2.192348, 0.000000, 0.000000] #last 4 columns
+    mms_fvm_ns.test_vals = [-2.851428, 2.192348, 0.000000, 0.000000]
     mms_fvm_ns.tol       = 0.0001
     test_list.append(mms_fvm_ns)
 
@@ -1372,7 +1372,7 @@ def main():
     mms_fvm_inc_euler.cfg_dir   = "mms/fvm_incomp_euler"
     mms_fvm_inc_euler.cfg_file  = "inv_mms_jst.cfg"
     mms_fvm_inc_euler.test_iter = 20
-    mms_fvm_inc_euler.test_vals = [-9.128660, -9.441806, 0.000000, 0.000000] #last 4 columns
+    mms_fvm_inc_euler.test_vals = [-9.128660, -9.441806, 0.000000, 0.000000]
     mms_fvm_inc_euler.tol       = 0.0001
     test_list.append(mms_fvm_inc_euler)
 
@@ -1381,7 +1381,7 @@ def main():
     mms_fvm_inc_ns.cfg_dir   = "mms/fvm_incomp_navierstokes"
     mms_fvm_inc_ns.cfg_file  = "lam_mms_fds.cfg"
     mms_fvm_inc_ns.test_iter = 20
-    mms_fvm_inc_ns.test_vals = [-7.414944, -7.631546, 0.000000, 0.000000] #last 4 columns
+    mms_fvm_inc_ns.test_vals = [-7.414944, -7.631546, 0.000000, 0.000000]
     mms_fvm_inc_ns.tol       = 0.0001
     test_list.append(mms_fvm_inc_ns)
 
@@ -1390,7 +1390,7 @@ def main():
     ringleb_dg_euler.cfg_dir   = "mms/dg_ringleb"
     ringleb_dg_euler.cfg_file  = "ringleb_dg.cfg"
     ringleb_dg_euler.test_iter = 100
-    ringleb_dg_euler.test_vals = [-5.136652, -4.724941, 0.000000, 0.000000] #last 4 columns
+    ringleb_dg_euler.test_vals = [-5.136652, -4.724941, 0.000000, 0.000000]
     ringleb_dg_euler.tol       = 0.0001
     test_list.append(ringleb_dg_euler)
 
@@ -1399,7 +1399,7 @@ def main():
     mms_dg_ns.cfg_dir   = "mms/dg_navierstokes"
     mms_dg_ns.cfg_file  = "lam_mms_dg.cfg"
     mms_dg_ns.test_iter = 100
-    mms_dg_ns.test_vals = [-1.845393, 3.520699, 0.000000, 0.000000] #last 4 columns
+    mms_dg_ns.test_vals = [-1.845393, 3.520699, 0.000000, 0.000000]
     mms_dg_ns.tol       = 0.0001
     test_list.append(mms_dg_ns)
 
@@ -1408,7 +1408,7 @@ def main():
     mms_dg_ns_3d.cfg_dir   = "mms/dg_navierstokes_3d"
     mms_dg_ns_3d.cfg_file  = "lam_mms_dg_3d.cfg"
     mms_dg_ns_3d.test_iter = 100
-    mms_dg_ns_3d.test_vals = [-0.146826, 5.356413, 0.000000, 0.000000] #last 4 columns
+    mms_dg_ns_3d.test_vals = [-0.146826, 5.356413, 0.000000, 0.000000]
     mms_dg_ns_3d.tol       = 0.0001
     test_list.append(mms_dg_ns_3d)
 
@@ -1421,7 +1421,7 @@ def main():
     species2_primitiveVenturi_mixingmodel.cfg_dir   = "species_transport/venturi_primitive_3species"
     species2_primitiveVenturi_mixingmodel.cfg_file  = "species2_primitiveVenturi_mixingmodel.cfg"
     species2_primitiveVenturi_mixingmodel.test_iter = 50
-    species2_primitiveVenturi_mixingmodel.test_vals = [-5.447741, -4.578625, -4.560889, -5.671675, -0.069655, -5.630277, 5.000000, -1.714271, 5.000000, -4.878115, 5.000000, -1.254671, 0.000418, 0.000394, 0.000024, 0.000000]
+    species2_primitiveVenturi_mixingmodel.test_vals = [-5.359429, -4.504612, -4.480004, -5.629196, -0.059934, -5.596051, 5.000000, -1.870943, 5.000000, -4.915279, 5.000000, -1.183531, 0.000429, 0.000393, 0.000036, 0.000000]
     test_list.append(species2_primitiveVenturi_mixingmodel)
 
     # 2 species (1 eq) primitive venturi mixing using mixing model and bounded scalar transport
@@ -1429,7 +1429,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_boundedscalar.cfg_dir   = "species_transport/venturi_primitive_3species"
     species2_primitiveVenturi_mixingmodel_boundedscalar.cfg_file  = "species2_primitiveVenturi_mixingmodel_boundedscalar.cfg"
     species2_primitiveVenturi_mixingmodel_boundedscalar.test_iter = 50
-    species2_primitiveVenturi_mixingmodel_boundedscalar.test_vals = [-5.398649, -4.476373, -4.477258, -5.733271, -0.122667, -5.687136, 5.000000, -1.797791, 5.000000, -4.942913, 5.000000, -2.082842, 0.000295, 0.000295, 0.000000, 0.000000]
+    species2_primitiveVenturi_mixingmodel_boundedscalar.test_vals = [-5.336209, -4.445047, -4.432074, -5.785385, -0.127631, -5.672217, 5.000000, -1.944369, 5.000000, -4.878272, 5.000000, -1.806657, 0.000272, 0.000272, 0.000000, 0.000000]
     test_list.append(species2_primitiveVenturi_mixingmodel_boundedscalar)
 
     # 2 species (1 eq) primitive venturi mixing using mixing model including viscosity, thermal conductivity and inlet markers for SA turbulence model
@@ -1445,7 +1445,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg_dir   = "species_transport/venturi_primitive_3species"
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg_file  = "species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg"
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2.test_iter = 50
-    species2_primitiveVenturi_mixingmodel_heatcapacity_H2.test_vals = [-6.113626, -4.989076, -4.880565, -7.351737, 2.452701, -5.627391, 30.000000, -5.721303, 11.000000, -8.001991, 10.000000, -8.813670, 2.084143, 1.000000, 0.600000, 0.484143]
+    species2_primitiveVenturi_mixingmodel_heatcapacity_H2.test_vals = [-6.118333, -4.985699, -4.918326, -7.249080, 2.445213, -5.624080, 30.000000, -5.681895, 12.000000, -8.186475, 10.000000, -8.853067, 2.083524, 1.000000, 0.600000, 0.483524]
     test_list.append(species2_primitiveVenturi_mixingmodel_heatcapacity_H2)
 
     # 2 species (1 eq) primitive venturi mixing using mixing model including heat capacity and mass diffusivity NonDimensional case
@@ -1453,7 +1453,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg_dir   = "species_transport/venturi_primitive_3species"
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg_file  = "species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg"
     species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.test_iter = 50
-    species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.test_vals = [-5.719472, -5.293846, -5.185419, -8.355307, 2.147874, -5.233215, 30.000000, -5.721396, 11.000000, -8.000062, 10.000000, -8.814100, 2.084145, 1.000000, 0.600000, 0.484145]
+    species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.test_vals = [-5.724191, -5.290524, -5.223195, -8.252900, 2.140394, -5.229908, 30.000000, -5.681850, 12.000000, -8.186296, 10.000000, -8.852858, 2.083526, 1.000000, 0.600000, 0.483526]
     test_list.append(species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND)
 
     # 2 species (1 eq) primitive venturi mixing
@@ -1461,7 +1461,7 @@ def main():
     species2_primitiveVenturi.cfg_dir   = "species_transport/venturi_primitive_3species"
     species2_primitiveVenturi.cfg_file  = "species2_primitiveVenturi.cfg"
     species2_primitiveVenturi.test_iter = 50
-    species2_primitiveVenturi.test_vals = [-6.004340, -5.236017, -5.080329, -5.888785, -1.554476, -6.076144, 5.000000, -0.808416, 5.000000, -2.325030, 5.000000, -0.238222, 0.000089, 0.000088, 0.000001, 0.000000]
+    species2_primitiveVenturi.test_vals = [-5.641112, -4.724266, -4.677148, -5.470711, -1.121455, -5.713132, 5.000000, -0.830412, 5.000000, -2.668654, 5.000000, -0.454161, 0.000092, 0.000091, 0.000001, 0.000000]
     test_list.append(species2_primitiveVenturi)
 
     # 2 species (1 eq) primitive venturi mixing with bounded scalar transport
@@ -1469,7 +1469,7 @@ def main():
     species_primitiveVenturi_boundedscalar.cfg_dir     = "species_transport/venturi_primitive_3species"
     species_primitiveVenturi_boundedscalar.cfg_file    = "species2_primitiveVenturi_boundedscalar.cfg"
     species_primitiveVenturi_boundedscalar.test_iter   = 50
-    species_primitiveVenturi_boundedscalar.test_vals   = [-5.297585, -4.397797, -4.377086, -5.593131, -1.011782, -5.623540, 5.000000, -1.775123, 5.000000, -4.086339, 5.000000, -2.080187, 0.000424, 0.000424, 0.000000, 0.000000]
+    species_primitiveVenturi_boundedscalar.test_vals   = [-5.278467, -4.368236, -4.350556, -5.693359, -0.978845, -5.618393, 5.000000, -1.804015, 5.000000, -4.057089, 5.000000, -2.003816, 0.000415, 0.000415, 0.000000, 0.000000]
     test_list.append(species_primitiveVenturi_boundedscalar)
 
     # 2 species (1 eq) primitive venturi mixing using mixing model including inlet markers for turbulent intensity and viscosity ratios
@@ -1477,7 +1477,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg_dir   = "species_transport/venturi_primitive_3species"
     species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg_file  = "species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg"
     species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.test_iter = 50
-    species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.test_vals = [-4.012157, -1.650191, -1.405134, -0.990205, 1.619918, -3.764227, 23.000000, -5.039466, 12.000000, -5.346201, 4.000000, -6.084514, 2.000000, 1.000000, 0.000000, 1.000000]
+    species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.test_vals = [-4.026294, -1.649804, -1.404882, -0.746005, 1.609256, -3.767237, 23.000000, -5.082019, 10.000000, -5.056739, 4.000000, -6.480965, 2.000000, 1.000000, 0.000000, 1.000000]
     test_list.append(species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS)
 
     # 3 species (2 eq) primitive venturi mixing with inlet files.
@@ -1486,7 +1486,7 @@ def main():
     species3_primitiveVenturi_inletFile.cfg_dir   = "species_transport/venturi_primitive_3species"
     species3_primitiveVenturi_inletFile.cfg_file  = "species3_primitiveVenturi_inletFile.cfg"
     species3_primitiveVenturi_inletFile.test_iter = 50
-    species3_primitiveVenturi_inletFile.test_vals = [-6.074971, -5.306648, -5.150960, -5.959416, -1.625107, -6.343704, -6.460033, 5.000000, -0.808413, 5.000000, -2.325029, 5.000000, -0.274923]
+    species3_primitiveVenturi_inletFile.test_vals = [-5.711734, -4.794814, -4.747694, -5.541323, -1.192017, -5.951964, -6.096677, 5.000000, -0.830172, 5.000000, -2.668819, 5.000000, -0.516308]
     test_list.append(species3_primitiveVenturi_inletFile)
 
     # rectangle passive transport validation

From 28785b520f43b3a1471c44c19382c70152a17c2c Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 1 Jul 2023 12:17:04 -0700
Subject: [PATCH 515/656] serial regression without restarts

---
 TestCases/serial_regression.py | 150 ++++++++++++++++-----------------
 1 file changed, 75 insertions(+), 75 deletions(-)

diff --git a/TestCases/serial_regression.py b/TestCases/serial_regression.py
index a17d5737b52..586cb5ba0b0 100644
--- a/TestCases/serial_regression.py
+++ b/TestCases/serial_regression.py
@@ -98,7 +98,7 @@ def main():
     naca0012.cfg_dir   = "euler/naca0012"
     naca0012.cfg_file  = "inv_NACA0012_Roe.cfg"
     naca0012.test_iter = 20
-    naca0012.test_vals = [-4.023999, -3.515034, 0.339426, 0.022217] #last 4 columns
+    naca0012.test_vals = [-4.023999, -3.515034, 0.339426, 0.022217]
     test_list.append(naca0012)
 
     # Supersonic wedge
@@ -106,7 +106,7 @@ def main():
     wedge.cfg_dir   = "euler/wedge"
     wedge.cfg_file  = "inv_wedge_HLLC.cfg"
     wedge.test_iter = 20
-    wedge.test_vals = [-0.942862, 4.784581, -0.208106, 0.036665] #last 4 columns
+    wedge.test_vals = [-0.942862, 4.784581, -0.208106, 0.036665]
     test_list.append(wedge)
 
     # ONERA M6 Wing
@@ -142,7 +142,7 @@ def main():
     bluntbody.cfg_dir   = "euler/bluntbody"
     bluntbody.cfg_file  = "blunt.cfg"
     bluntbody.test_iter = 20
-    bluntbody.test_vals = [0.540009, 6.916653, -0.000000, 1.868975] #last 4 columns
+    bluntbody.test_vals = [0.540009, 6.916653, -0.000000, 1.868975]
     test_list.append(bluntbody)
 
     ##########################
@@ -169,7 +169,7 @@ def main():
     cylinder.cfg_dir   = "navierstokes/cylinder"
     cylinder.cfg_file  = "lam_cylinder.cfg"
     cylinder.test_iter = 25
-    cylinder.test_vals = [-6.765430, -1.297426, 0.019508, 0.310015, 1.2325e-01]
+    cylinder.test_vals = [-6.765430, -1.297426, 0.019508, 0.310015, 0.123250]
     test_list.append(cylinder)
 
     # Laminar cylinder (low Mach correction)
@@ -193,7 +193,7 @@ def main():
     poiseuille_profile.cfg_dir   = "navierstokes/poiseuille"
     poiseuille_profile.cfg_file  = "profile_poiseuille.cfg"
     poiseuille_profile.test_iter = 10
-    poiseuille_profile.test_vals         = [-12.494681, -7.711642, -0.000000, 2.085796] #last 4 columns
+    poiseuille_profile.test_vals         = [-12.494681, -7.711642, -0.000000, 2.085796]
     poiseuille_profile.test_vals_aarch64 = [-12.494705, -7.711332, -0.000000, 2.085796] #last 4 columns
     test_list.append(poiseuille_profile)
 
@@ -221,7 +221,7 @@ def main():
     rae2822_sst.cfg_dir   = "rans/rae2822"
     rae2822_sst.cfg_file  = "turb_SST_RAE2822.cfg"
     rae2822_sst.test_iter = 20
-    rae2822_sst.test_vals = [-0.510638, 4.870901, 0.812661, 0.061095, -80192.000000]
+    rae2822_sst.test_vals = [-0.510376, 4.873617, 0.816197, 0.060504, -71886.000000]
     test_list.append(rae2822_sst)
 
     # RAE2822 SST_SUST
@@ -229,7 +229,7 @@ def main():
     rae2822_sst_sust.cfg_dir   = "rans/rae2822"
     rae2822_sst_sust.cfg_file  = "turb_SST_SUST_RAE2822.cfg"
     rae2822_sst_sust.test_iter = 20
-    rae2822_sst_sust.test_vals = [-2.422024, 4.870900, 0.812660, 0.061095]
+    rae2822_sst_sust.test_vals = [-2.536121, 4.873617, 0.816197, 0.060504]
     test_list.append(rae2822_sst_sust)
 
     # Flat plate
@@ -245,7 +245,7 @@ def main():
     turb_wallfunction_flatplate_sst.cfg_dir   = "wallfunctions/flatplate/compressible_SST"
     turb_wallfunction_flatplate_sst.cfg_file  = "turb_SST_flatplate.cfg"
     turb_wallfunction_flatplate_sst.test_iter = 10
-    turb_wallfunction_flatplate_sst.test_vals = [-4.229999, -1.930714, -1.998514, 1.250334, -1.635256, 1.474343, 10.000000, -2.152260, 0.072873, 0.002514] #last 10 columns
+    turb_wallfunction_flatplate_sst.test_vals = [-4.181412, -1.864638, -1.966031, 1.259921, -1.487159, 1.544166, 10.000000, -2.130777, 0.073950, 0.002971]
     test_list.append(turb_wallfunction_flatplate_sst)
 
     # FLAT PLATE, WALL FUNCTIONS, COMPRESSIBLE SA
@@ -307,7 +307,7 @@ def main():
     turb_naca0012_sst_fixedvalues.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst_fixedvalues.cfg_file  = "turb_NACA0012_sst_fixedvalues.cfg"
     turb_naca0012_sst_fixedvalues.test_iter = 10
-    turb_naca0012_sst_fixedvalues.test_vals = [-5.206744, -9.561900, -1.566602, 1.022029, 0.040549, -3.483578]
+    turb_naca0012_sst_fixedvalues.test_vals = [-5.206797, -10.023481, -1.616002, 1.021528, 0.040220, -3.480532]
     turb_naca0012_sst_fixedvalues.timeout   = 3200
     test_list.append(turb_naca0012_sst_fixedvalues)
 
@@ -343,7 +343,7 @@ def main():
     turb_naca0012_sst_restart_mg.cfg_file  = "turb_NACA0012_sst_multigrid_restart.cfg"
     turb_naca0012_sst_restart_mg.test_iter = 50
     turb_naca0012_sst_restart_mg.ntest_vals = 5
-    turb_naca0012_sst_restart_mg.test_vals = [-7.653236, -7.729549, -1.981855, -0.000015, 0.079062]
+    turb_naca0012_sst_restart_mg.test_vals = [-7.639702, -7.441853, -1.895004, 0.000001, 0.079178]
     turb_naca0012_sst_restart_mg.timeout   = 3200
     turb_naca0012_sst_restart_mg.tol       = 0.000001
     test_list.append(turb_naca0012_sst_restart_mg)
@@ -364,7 +364,7 @@ def main():
     inc_euler_naca0012.cfg_dir   = "incomp_euler/naca0012"
     inc_euler_naca0012.cfg_file  = "incomp_NACA0012.cfg"
     inc_euler_naca0012.test_iter = 20
-    inc_euler_naca0012.test_vals = [-4.858287, -3.810487, 0.491850, 0.007002] #last 4 columns
+    inc_euler_naca0012.test_vals = [-4.858287, -3.810487, 0.491850, 0.007002]
     test_list.append(inc_euler_naca0012)
 
     # C-D nozzle with pressure inlet and mass flow outlet
@@ -372,7 +372,7 @@ def main():
     inc_nozzle.cfg_dir   = "incomp_euler/nozzle"
     inc_nozzle.cfg_file  = "inv_nozzle.cfg"
     inc_nozzle.test_iter = 20
-    inc_nozzle.test_vals = [-5.971283, -4.911145, -0.000201, 0.121631] #last 4 columns
+    inc_nozzle.test_vals = [-5.971283, -4.911145, -0.000201, 0.121631]
     test_list.append(inc_nozzle)
 
     #############################
@@ -391,7 +391,7 @@ def main():
     inc_lam_cylinder.cfg_dir   = "incomp_navierstokes/cylinder"
     inc_lam_cylinder.cfg_file  = "incomp_cylinder.cfg"
     inc_lam_cylinder.test_iter = 10
-    inc_lam_cylinder.test_vals = [-4.004277, -3.227956, 0.003852, 7.626578] #last 4 columns
+    inc_lam_cylinder.test_vals = [-4.004277, -3.227956, 0.003852, 7.626578]
     test_list.append(inc_lam_cylinder)
 
     # Buoyancy-driven cavity
@@ -399,7 +399,7 @@ def main():
     inc_buoyancy.cfg_dir   = "incomp_navierstokes/buoyancy_cavity"
     inc_buoyancy.cfg_file  = "lam_buoyancy_cavity.cfg"
     inc_buoyancy.test_iter = 20
-    inc_buoyancy.test_vals = [-4.436657, 0.507847, 0.000000, 0.000000] #last 4 columns
+    inc_buoyancy.test_vals = [-4.436657, 0.507847, 0.000000, 0.000000]
     test_list.append(inc_buoyancy)
 
     # Laminar heated cylinder with polynomial fluid model
@@ -415,7 +415,7 @@ def main():
     inc_lam_bend.cfg_dir   = "incomp_navierstokes/bend"
     inc_lam_bend.cfg_file  = "lam_bend.cfg"
     inc_lam_bend.test_iter = 10
-    inc_lam_bend.test_vals = [-3.455147, -3.082194, -0.018579, 1.169947] #last 4 columns
+    inc_lam_bend.test_vals = [-3.455147, -3.082194, -0.018579, 1.169947]
     test_list.append(inc_lam_bend)
 
     ############################
@@ -442,7 +442,7 @@ def main():
     inc_turb_naca0012_sst_sust.cfg_dir   = "incomp_rans/naca0012"
     inc_turb_naca0012_sst_sust.cfg_file  = "naca0012_SST_SUST.cfg"
     inc_turb_naca0012_sst_sust.test_iter = 20
-    inc_turb_naca0012_sst_sust.test_vals = [-7.273895, 0.145922, 0.000021, 0.312007] #last 4 columns
+    inc_turb_naca0012_sst_sust.test_vals = [-7.270375, 0.018431, 0.000021, 0.307673]
     test_list.append(inc_turb_naca0012_sst_sust)
 
     # FLAT PLATE, WALL FUNCTIONS, INCOMPRESSIBLE SST
@@ -450,7 +450,7 @@ def main():
     inc_turb_wallfunction_flatplate_sst.cfg_dir   = "wallfunctions/flatplate/incompressible_SST"
     inc_turb_wallfunction_flatplate_sst.cfg_file  = "turb_SST_flatplate.cfg"
     inc_turb_wallfunction_flatplate_sst.test_iter = 10
-    inc_turb_wallfunction_flatplate_sst.test_vals = [-6.561451, -5.730262, -6.306047, -4.230307, -7.164384, -2.047277, 10.000000, -2.941826, 0.000974, 0.003195, 0.206290]
+    inc_turb_wallfunction_flatplate_sst.test_vals = [-6.560775, -5.700721, -6.304284, -4.230488, -7.179831, -1.956057, 10.000000, -2.918240, 0.000887, 0.003680, 0.518450]
     test_list.append(inc_turb_wallfunction_flatplate_sst)
 
     # FLAT PLATE, WALL FUNCTIONS, INCOMPRESSIBLE SA
@@ -458,7 +458,7 @@ def main():
     inc_turb_wallfunction_flatplate_sa.cfg_dir   = "wallfunctions/flatplate/incompressible_SA"
     inc_turb_wallfunction_flatplate_sa.cfg_file  = "turb_SA_flatplate.cfg"
     inc_turb_wallfunction_flatplate_sa.test_iter = 10
-    inc_turb_wallfunction_flatplate_sa.test_vals = [-6.561303, -5.718581, -6.306403, -4.230225, -9.586904, 10, -2.927392, 0.000858, 0.003792 ] #last 9 columns
+    inc_turb_wallfunction_flatplate_sa.test_vals = [-6.561303, -5.718581, -6.306403, -4.230225, -9.586904, 10.000000, -2.927392, 0.000858, 0.003792]
     test_list.append(inc_turb_wallfunction_flatplate_sa)
 
     ####################
@@ -477,7 +477,7 @@ def main():
     fem_euler_naca0012.cfg_dir   = "hom_euler/NACA0012_5thOrder"
     fem_euler_naca0012.cfg_file  = "fem_NACA0012_reg.cfg"
     fem_euler_naca0012.test_iter = 10
-    fem_euler_naca0012.test_vals = [-6.519946,-5.976944,0.255551,0.000028] #last 4 columns
+    fem_euler_naca0012.test_vals = [-6.519946, -5.976944, 0.255551, 0.000028]
     test_list.append(fem_euler_naca0012)
 
     ############################
@@ -496,7 +496,7 @@ def main():
     fem_ns_flatplate.cfg_dir   = "hom_navierstokes/FlatPlate/nPoly4"
     fem_ns_flatplate.cfg_file  = "lam_flatplate_reg.cfg"
     fem_ns_flatplate.test_iter = 25
-    fem_ns_flatplate.test_vals = [1.383727,3.175247,0.058387,0.257951] #last 4 columns
+    fem_ns_flatplate.test_vals = [1.383727, 3.175247, 0.058387, 0.257951]
     test_list.append(fem_ns_flatplate)
 
     # Steady cylinder
@@ -504,7 +504,7 @@ def main():
     fem_ns_cylinder.cfg_dir   = "hom_navierstokes/CylinderViscous/nPoly3"
     fem_ns_cylinder.cfg_file  = "fem_Cylinder_reg.cfg"
     fem_ns_cylinder.test_iter = 10
-    fem_ns_cylinder.test_vals = [0.454960,0.979123,-0.000028,79.984799] #last 4 columns
+    fem_ns_cylinder.test_vals = [0.454960, 0.979123, -0.000028, 79.984799]
     test_list.append(fem_ns_cylinder)
 
     # Steady sphere
@@ -512,7 +512,7 @@ def main():
     fem_ns_sphere.cfg_dir   = "hom_navierstokes/SphereViscous/nPoly3_QuadDominant"
     fem_ns_sphere.cfg_file  = "fem_Sphere_reg.cfg"
     fem_ns_sphere.test_iter = 10
-    fem_ns_sphere.test_vals = [-0.288121,0.240324,0.000258,21.797363] #last 4 columns
+    fem_ns_sphere.test_vals = [-0.288121, 0.240324, 0.000258, 21.797363]
     test_list.append(fem_ns_sphere)
 
     # Unsteady sphere ADER
@@ -520,7 +520,7 @@ def main():
     fem_ns_sphere_ader.cfg_dir   = "hom_navierstokes/SphereViscous/nPoly3_QuadDominant"
     fem_ns_sphere_ader.cfg_file  = "fem_Sphere_reg_ADER.cfg"
     fem_ns_sphere_ader.test_iter = 10
-    fem_ns_sphere_ader.test_vals = [-35.000000,-35.000000,0.000047,31.110911] #last 4 columns
+    fem_ns_sphere_ader.test_vals = [-35.000000, -35.000000, 0.000047, 31.110911]
     fem_ns_sphere_ader.unsteady   = True
     test_list.append(fem_ns_sphere_ader)
 
@@ -529,7 +529,7 @@ def main():
     fem_ns_unsteady_cylinder.cfg_dir   = "hom_navierstokes/UnsteadyCylinder/nPoly4"
     fem_ns_unsteady_cylinder.cfg_file  = "fem_unst_cylinder.cfg"
     fem_ns_unsteady_cylinder.test_iter = 11
-    fem_ns_unsteady_cylinder.test_vals = [-3.558582,-3.014464,-0.038927,1.383983] #last 4 columns
+    fem_ns_unsteady_cylinder.test_vals = [-3.558582, -3.014464, -0.038927, 1.383983]
     fem_ns_unsteady_cylinder.unsteady   = True
     test_list.append(fem_ns_unsteady_cylinder)
 
@@ -538,7 +538,7 @@ def main():
     fem_ns_unsteady_cylinder_ader.cfg_dir   = "hom_navierstokes/UnsteadyCylinder/nPoly4"
     fem_ns_unsteady_cylinder_ader.cfg_file  = "fem_unst_cylinder_ADER.cfg"
     fem_ns_unsteady_cylinder_ader.test_iter = 11
-    fem_ns_unsteady_cylinder_ader.test_vals = [-35.000000,-35.000000,-0.041003,1.391339] #last 4 columns
+    fem_ns_unsteady_cylinder_ader.test_vals = [-35.000000, -35.000000, -0.041003, 1.391339]
     fem_ns_unsteady_cylinder_ader.unsteady   = True
     test_list.append(fem_ns_unsteady_cylinder_ader)
 
@@ -551,7 +551,7 @@ def main():
     schubauer_klebanoff_transition.cfg_dir      = "transition/Schubauer_Klebanoff"
     schubauer_klebanoff_transition.cfg_file     = "transitional_BC_model_ConfigFile.cfg"
     schubauer_klebanoff_transition.test_iter    = 10
-    schubauer_klebanoff_transition.test_vals    = [-8.029786, -13.240213, 0.000053, 0.007986] #last 4 columns
+    schubauer_klebanoff_transition.test_vals    = [-8.029786, -13.240213, 0.000053, 0.007986]
     test_list.append(schubauer_klebanoff_transition)
 
     #####################################
@@ -570,7 +570,7 @@ def main():
     contadj_naca0012.cfg_dir   = "cont_adj_euler/naca0012"
     contadj_naca0012.cfg_file  = "inv_NACA0012.cfg"
     contadj_naca0012.test_iter = 5
-    contadj_naca0012.test_vals = [-9.289565, -14.563861, 0.300920, 0.019552] #last 4 columns
+    contadj_naca0012.test_vals = [-9.289565, -14.563859, 0.300920, 0.019552]
     contadj_naca0012.tol       = 0.001
     test_list.append(contadj_naca0012)
 
@@ -579,7 +579,7 @@ def main():
     contadj_oneram6.cfg_dir   = "cont_adj_euler/oneram6"
     contadj_oneram6.cfg_file  = "inv_ONERAM6.cfg"
     contadj_oneram6.test_iter = 10
-    contadj_oneram6.test_vals = [-12.133160, -12.706697, 0.685900, 0.007594] #last 4 columns
+    contadj_oneram6.test_vals = [-12.133160, -12.706697, 0.685900, 0.007594]
     test_list.append(contadj_oneram6)
 
     # Inviscid WEDGE: tests averaged outflow total pressure adjoint
@@ -587,7 +587,7 @@ def main():
     contadj_wedge.cfg_dir   = "cont_adj_euler/wedge"
     contadj_wedge.cfg_file  = "inv_wedge_ROE.cfg"
     contadj_wedge.test_iter = 10
-    contadj_wedge.test_vals = [2.872691, -2.755572, 853000.000000, 0.000000] #last 4 columns
+    contadj_wedge.test_vals = [2.872691, -2.755572, 853000.000000, 0.000000]
     test_list.append(contadj_wedge)
 
     # Inviscid fixed CL NACA0012
@@ -614,7 +614,7 @@ def main():
     contadj_ns_cylinder.cfg_dir   = "cont_adj_navierstokes/cylinder"
     contadj_ns_cylinder.cfg_file  = "lam_cylinder.cfg"
     contadj_ns_cylinder.test_iter = 20
-    contadj_ns_cylinder.test_vals = [ -3.665848, -9.132055, 2.056700, -0.000000] #last 4 columns
+    contadj_ns_cylinder.test_vals = [-3.665842, -9.132048, 2.056700, -0.000000]
     test_list.append(contadj_ns_cylinder)
 
     # Adjoint laminar naca0012 subsonic
@@ -622,7 +622,7 @@ def main():
     contadj_ns_naca0012_sub.cfg_dir   = "cont_adj_navierstokes/naca0012_sub"
     contadj_ns_naca0012_sub.cfg_file  = "lam_NACA0012.cfg"
     contadj_ns_naca0012_sub.test_iter = 20
-    contadj_ns_naca0012_sub.test_vals = [-2.743268, -8.215193, 0.518810, 0.001210] #last 4 columns
+    contadj_ns_naca0012_sub.test_vals = [-2.743268, -8.215193, 0.518810, 0.001210]
     test_list.append(contadj_ns_naca0012_sub)
 
     # Adjoint laminar naca0012 transonic
@@ -630,7 +630,7 @@ def main():
     contadj_ns_naca0012_trans.cfg_dir   = "cont_adj_navierstokes/naca0012_trans"
     contadj_ns_naca0012_trans.cfg_file  = "lam_NACA0012.cfg"
     contadj_ns_naca0012_trans.test_iter = 20
-    contadj_ns_naca0012_trans.test_vals = [-1.039664, -6.575019, 1.772300, 0.012495] #last 4 columns
+    contadj_ns_naca0012_trans.test_vals = [-1.039664, -6.575019, 1.772300, 0.012495]
     test_list.append(contadj_ns_naca0012_trans)
 
     #######################################################
@@ -642,7 +642,7 @@ def main():
     contadj_rans_naca0012.cfg_dir   = "cont_adj_rans/naca0012"
     contadj_rans_naca0012.cfg_file  = "turb_nasa.cfg"
     contadj_rans_naca0012.test_iter = 20
-    contadj_rans_naca0012.test_vals = [ -0.794162, -5.761722, 19.214000, -0.000000] #last 4 columns
+    contadj_rans_naca0012.test_vals = [-0.794162, -5.761722, 19.214000, -0.000000]
     test_list.append(contadj_rans_naca0012)
 
     # Adjoint turbulent NACA0012 with binary restarts
@@ -650,7 +650,7 @@ def main():
     contadj_rans_naca0012_bin.cfg_dir   = "cont_adj_rans/naca0012"
     contadj_rans_naca0012_bin.cfg_file  = "turb_nasa_binary.cfg"
     contadj_rans_naca0012_bin.test_iter = 18
-    contadj_rans_naca0012_bin.test_vals = [-0.794169, -5.761671, 19.214000, -0.000000] #last 4 columns
+    contadj_rans_naca0012_bin.test_vals = [-0.794169, -5.761671, 19.214000, -0.000000]
     test_list.append(contadj_rans_naca0012_bin)
 
     # Adjoint turbulent RAE2822
@@ -670,7 +670,7 @@ def main():
     turb_naca0012_1c.cfg_dir   = "rans_uq/naca0012"
     turb_naca0012_1c.cfg_file  = "turb_NACA0012_uq_1c.cfg"
     turb_naca0012_1c.test_iter = 10
-    turb_naca0012_1c.test_vals         = [-4.985899, 1.137425, 0.375986, -0.078795]
+    turb_naca0012_1c.test_vals         = [-4.986094, 1.137009, 0.378604, -0.083526]
     turb_naca0012_1c.test_vals_aarch64 = [-4.985900, 1.137455, 0.376000, -0.078781]
     test_list.append(turb_naca0012_1c)
 
@@ -679,7 +679,7 @@ def main():
     turb_naca0012_2c.cfg_dir   = "rans_uq/naca0012"
     turb_naca0012_2c.cfg_file  = "turb_NACA0012_uq_2c.cfg"
     turb_naca0012_2c.test_iter = 10
-    turb_naca0012_2c.test_vals         = [-5.483297, 0.968867, 0.255779, -0.109417] #last 4 columns
+    turb_naca0012_2c.test_vals         = [-5.483291, 0.968701, 0.258168, -0.114217]
     turb_naca0012_2c.test_vals_aarch64 = [-5.483310, 0.968862, 0.255650, -0.109464] #last 4 columns
     test_list.append(turb_naca0012_2c)
 
@@ -688,7 +688,7 @@ def main():
     turb_naca0012_3c.cfg_dir   = "rans_uq/naca0012"
     turb_naca0012_3c.cfg_file  = "turb_NACA0012_uq_3c.cfg"
     turb_naca0012_3c.test_iter = 10
-    turb_naca0012_3c.test_vals = [-5.584300, 0.931352, 0.248990, -0.109405] #last 4 columns
+    turb_naca0012_3c.test_vals = [-5.584299, 0.931258, 0.251298, -0.114232]
     test_list.append(turb_naca0012_3c)
 
     # NACA0012 p1c1
@@ -696,7 +696,7 @@ def main():
     turb_naca0012_p1c1.cfg_dir   = "rans_uq/naca0012"
     turb_naca0012_p1c1.cfg_file  = "turb_NACA0012_uq_p1c1.cfg"
     turb_naca0012_p1c1.test_iter = 10
-    turb_naca0012_p1c1.test_vals         = [-5.127470, 1.077450, 0.544081, -0.018573] #last 4 columns
+    turb_naca0012_p1c1.test_vals         = [-5.127497, 1.077175, 0.546823, -0.023191]
     turb_naca0012_p1c1.test_vals_aarch64 = [-5.127512, 1.077345, 0.544130, -0.018555] #last 4 columns
     test_list.append(turb_naca0012_p1c1)
 
@@ -705,7 +705,7 @@ def main():
     turb_naca0012_p1c2.cfg_dir   = "rans_uq/naca0012"
     turb_naca0012_p1c2.cfg_file  = "turb_NACA0012_uq_p1c2.cfg"
     turb_naca0012_p1c2.test_iter = 10
-    turb_naca0012_p1c2.test_vals         = [-5.554427, 0.943668, 0.320426, -0.091140] #last 4 columns
+    turb_naca0012_p1c2.test_vals         = [-5.554412, 0.943562, 0.322803, -0.095946]
     turb_naca0012_p1c2.test_vals_aarch64 = [-5.554391, 0.943687, 0.320285, -0.091188] #last 4 columns
     test_list.append(turb_naca0012_p1c2)
 
@@ -754,7 +754,7 @@ def main():
     spinning_cylinder.cfg_dir   = "moving_wall/spinning_cylinder"
     spinning_cylinder.cfg_file  = "spinning_cylinder.cfg"
     spinning_cylinder.test_iter = 25
-    spinning_cylinder.test_vals = [-7.889994, -2.469385, 1.708162, 1.670039] #last 4 columns
+    spinning_cylinder.test_vals = [-7.889994, -2.469385, 1.708162, 1.670039]
     test_list.append(spinning_cylinder)
 
     ######################################
@@ -766,7 +766,7 @@ def main():
     square_cylinder.cfg_dir   = "unsteady/square_cylinder"
     square_cylinder.cfg_file  = "turb_square.cfg"
     square_cylinder.test_iter = 3
-    square_cylinder.test_vals = [-2.557820, -1.158056, 0.067984, 1.399788, 2.220411, 1.399743, 2.218612, -0.453170]
+    square_cylinder.test_vals = [-2.557884, -1.173573, 0.058052, 1.399794, 2.220411, 1.399748, 2.218612, -0.453340]
     square_cylinder.unsteady  = True
     test_list.append(square_cylinder)
 
@@ -811,7 +811,7 @@ def main():
     unst_deforming_naca0012.cfg_dir   = "disc_adj_euler/naca0012_pitching_def"
     unst_deforming_naca0012.cfg_file  = "inv_NACA0012_pitching_deform.cfg"
     unst_deforming_naca0012.test_iter = 5
-    unst_deforming_naca0012.test_vals = [-3.665128, -3.793593, -3.716506, -3.148308] #last 4 columns
+    unst_deforming_naca0012.test_vals = [-3.665129, -3.793590, -3.716505, -3.148308]
     unst_deforming_naca0012.unsteady  = True
     test_list.append(unst_deforming_naca0012)
 
@@ -824,7 +824,7 @@ def main():
     ls89_sa.cfg_dir   = "nicf/LS89"
     ls89_sa.cfg_file  = "turb_SA_PR.cfg"
     ls89_sa.test_iter = 20
-    ls89_sa.test_vals = [-5.050483, -13.371788, 0.174939, 0.430757] #last 4 columns
+    ls89_sa.test_vals = [-5.050483, -13.371791, 0.174939, 0.430757]
     test_list.append(ls89_sa)
 
     # Rarefaction shock wave edge_VW
@@ -832,7 +832,7 @@ def main():
     edge_VW.cfg_dir   = "nicf/edge"
     edge_VW.cfg_file  = "edge_VW.cfg"
     edge_VW.test_iter = 20
-    edge_VW.test_vals = [-0.711552, 5.490479, -0.000975, 0.000000] #last 4 columns
+    edge_VW.test_vals = [-0.711552, 5.490479, -0.000975, 0.000000]
     test_list.append(edge_VW)
 
     # Rarefaction shock wave edge_PPR
@@ -840,7 +840,7 @@ def main():
     edge_PPR.cfg_dir   = "nicf/edge"
     edge_PPR.cfg_file  = "edge_PPR.cfg"
     edge_PPR.test_iter = 20
-    edge_PPR.test_vals = [-1.670439, 4.522842, 0.001027, 0.000000] #last 4 columns
+    edge_PPR.test_vals = [-1.670439, 4.522842, 0.001027, 0.000000]
     test_list.append(edge_PPR)
 
 
@@ -862,7 +862,7 @@ def main():
     axial_stage2D.cfg_dir   = "turbomachinery/axial_stage_2D"
     axial_stage2D.cfg_file  = "Axial_stage2D.cfg"
     axial_stage2D.test_iter = 20
-    axial_stage2D.test_vals = [1.047323, 1.661341, -2.913940, 2.588179, -2.486770, 3.050954, 1.0638e+05, 1.0638e+05]
+    axial_stage2D.test_vals = [0.974801, 1.534472, -2.897692, 2.599377, -2.418396, 3.087203, 106380.000000, 106380.000000]
     test_list.append(axial_stage2D)
 
     # 2D transonic stator restart
@@ -890,7 +890,7 @@ def main():
     uniform_flow.cfg_dir   = "sliding_interface/uniform_flow"
     uniform_flow.cfg_file  = "uniform_NN.cfg"
     uniform_flow.test_iter = 2
-    uniform_flow.test_vals         = [2.000000, 0.000000, -0.205134, -13.251542] #last 4 columns
+    uniform_flow.test_vals         = [2.000000, 0.000000, -0.205134, -13.251542]
     uniform_flow.test_vals_aarch64 = [2.000000, 0.000000, -0.205134, -13.250720] #last 4 columns
     uniform_flow.tol       = 0.000001
     uniform_flow.unsteady  = True
@@ -902,7 +902,7 @@ def main():
     channel_2D.cfg_dir   = "sliding_interface/channel_2D"
     channel_2D.cfg_file  = "channel_2D_WA.cfg"
     channel_2D.test_iter = 2
-    channel_2D.test_vals         = [2.000000, 0.000000, 0.397995, 0.352789, 0.405474] #last 5 columns
+    channel_2D.test_vals         = [2.000000, 0.000000, 0.397995, 0.352789, 0.405474]
     channel_2D.test_vals_aarch64 = [2.000000, 0.000000, 0.398053, 0.352788, 0.405474] #last 5 columns
     channel_2D.timeout   = 100
     channel_2D.unsteady  = True
@@ -914,7 +914,7 @@ def main():
     channel_3D.cfg_dir   = "sliding_interface/channel_3D"
     channel_3D.cfg_file  = "channel_3D_WA.cfg"
     channel_3D.test_iter = 1
-    channel_3D.test_vals         = [1.000000, 0.000000, 0.661408, 0.769988, 0.696033] #last 5 columns
+    channel_3D.test_vals         = [1.000000, 0.000000, 0.661408, 0.769988, 0.696033]
     channel_3D.test_vals_aarch64 = [1.000000, 0.000000, 0.661408, 0.769902, 0.695663] #last 5 columns
     channel_3D.unsteady  = True
     channel_3D.multizone = True
@@ -925,7 +925,7 @@ def main():
     pipe.cfg_dir   = "sliding_interface/pipe"
     pipe.cfg_file  = "pipe_NN.cfg"
     pipe.test_iter = 2
-    pipe.test_vals = [0.491954, 0.677756, 0.963981, 1.006936] #last 4 columns
+    pipe.test_vals = [0.491954, 0.677756, 0.963981, 1.006936]
     pipe.unsteady  = True
     pipe.multizone = True
     test_list.append(pipe)
@@ -935,7 +935,7 @@ def main():
     rotating_cylinders.cfg_dir   = "sliding_interface/rotating_cylinders"
     rotating_cylinders.cfg_file  = "rot_cylinders_WA.cfg"
     rotating_cylinders.test_iter = 3
-    rotating_cylinders.test_vals = [3.000000, 0.000000, 0.777574, 1.134794, 1.224127] #last 4 columns
+    rotating_cylinders.test_vals = [3.000000, 0.000000, 0.777574, 1.134794, 1.224127]
     rotating_cylinders.unsteady  = True
     rotating_cylinders.multizone = True
     test_list.append(rotating_cylinders)
@@ -945,7 +945,7 @@ def main():
     supersonic_vortex_shedding.cfg_dir   = "sliding_interface/supersonic_vortex_shedding"
     supersonic_vortex_shedding.cfg_file  = "sup_vor_shed_WA.cfg"
     supersonic_vortex_shedding.test_iter = 5
-    supersonic_vortex_shedding.test_vals = [5.000000, 0.000000, 1.214364, 1.663910] #last 4 columns
+    supersonic_vortex_shedding.test_vals = [5.000000, 0.000000, 1.214359, 1.663910]
     supersonic_vortex_shedding.unsteady  = True
     supersonic_vortex_shedding.multizone = True
     test_list.append(supersonic_vortex_shedding)
@@ -955,7 +955,7 @@ def main():
     bars_SST_2D.cfg_dir   = "sliding_interface/bars_SST_2D"
     bars_SST_2D.cfg_file  = "bars.cfg"
     bars_SST_2D.test_iter = 13
-    bars_SST_2D.test_vals = [13.000000, -0.604409, -1.523885]
+    bars_SST_2D.test_vals = [13.000000, -0.773513, -1.700012]
     bars_SST_2D.multizone = True
     test_list.append(bars_SST_2D)
 
@@ -964,7 +964,7 @@ def main():
     slinc_steady.cfg_dir   = "sliding_interface/incompressible_steady"
     slinc_steady.cfg_file  = "config.cfg"
     slinc_steady.test_iter = 19
-    slinc_steady.test_vals = [19.000000, -1.803732, -2.108492] #last 3 columns
+    slinc_steady.test_vals = [19.000000, -1.803732, -2.108492]
     slinc_steady.timeout   = 100
     slinc_steady.multizone = True
     test_list.append(slinc_steady)
@@ -995,7 +995,7 @@ def main():
     statbeam3d.cfg_dir   = "fea_fsi/StatBeam_3d"
     statbeam3d.cfg_file  = "configBeam_3d.cfg"
     statbeam3d.test_iter = 0
-    statbeam3d.test_vals         = [-8.498245, -8.230816, -8.123810, 64095.0] #last 4 columns
+    statbeam3d.test_vals         = [-8.498245, -8.230816, -8.123810, 64095.000000]
     statbeam3d.test_vals_aarch64 = [-8.498254, -8.230683, -8.123819, 64095.0] #last 4 columns
     test_list.append(statbeam3d)
 
@@ -1004,7 +1004,7 @@ def main():
     knowlesbeam.cfg_dir   = "fea_fsi/MixElemsKnowles"
     knowlesbeam.cfg_file  = "config.cfg"
     knowlesbeam.test_iter = 0
-    knowlesbeam.test_vals         = [-14.513600, -13.57735, -28.126420, 0.44503, 9.7306] #last 5 columns
+    knowlesbeam.test_vals         = [-14.513598, -13.577350, -28.126416, 0.445030, 9.730600]
     knowlesbeam.test_vals_aarch64 = [-14.475326, -13.54641, -28.057487, 0.44503, 9.7306] #last 5 columns
     knowlesbeam.tol       = 0.0001
     test_list.append(knowlesbeam)
@@ -1015,7 +1015,7 @@ def main():
     dynbeam2d.cfg_file  = "configBeam_2d.cfg"
     dynbeam2d.unsteady  = True
     dynbeam2d.test_iter = 6
-    dynbeam2d.test_vals = [-3.240015, 2.895057, -0.353146, 6.6127e+04] #last 4 columns
+    dynbeam2d.test_vals = [-3.240015, 2.895057, -0.353146, 66127.000000]
     test_list.append(dynbeam2d)
 
     # # FSI, 2d
@@ -1023,7 +1023,7 @@ def main():
     fsi2d.cfg_dir   = "fea_fsi/WallChannel_2d"
     fsi2d.cfg_file  = "configFSI.cfg"
     fsi2d.test_iter = 4
-    fsi2d.test_vals = [4, 0, -3.743214, -4.133482] #last 4 columns
+    fsi2d.test_vals = [4.000000, 0.000000, -3.743214, -4.133482]
     fsi2d.multizone = True
     fsi2d.unsteady  = True
     test_list.append(fsi2d)
@@ -1033,7 +1033,7 @@ def main():
     stat_fsi.cfg_dir   = "fea_fsi/stat_fsi"
     stat_fsi.cfg_file  = "config.cfg"
     stat_fsi.test_iter = 7
-    stat_fsi.test_vals = [-3.326934, -4.981505, 0.000000, 7.000000] #last 5 columns
+    stat_fsi.test_vals = [-3.326934, -4.981505, 0.000000, 7.000000]
     stat_fsi.multizone = True
     test_list.append(stat_fsi)
 
@@ -1042,7 +1042,7 @@ def main():
     stat_fsi_restart.cfg_dir   = "fea_fsi/stat_fsi"
     stat_fsi_restart.cfg_file  = "config_restart.cfg"
     stat_fsi_restart.test_iter = 1
-    stat_fsi_restart.test_vals = [-3.407486, -4.339837, 0.000000, 27.000000] #last 5 columns
+    stat_fsi_restart.test_vals = [-3.407486, -4.339837, 0.000000, 27.000000]
     stat_fsi_restart.multizone = True
     test_list.append(stat_fsi_restart)
 
@@ -1051,7 +1051,7 @@ def main():
     dyn_fsi.cfg_dir   = "fea_fsi/dyn_fsi"
     dyn_fsi.cfg_file  = "config.cfg"
     dyn_fsi.test_iter = 4
-    dyn_fsi.test_vals         = [-4.355809, -4.060588, 0.000000, 87.000000] #last 4 columns
+    dyn_fsi.test_vals         = [-4.355809, -4.060588, 0.000000, 87.000000]
     dyn_fsi.test_vals_aarch64 = [-4.355809, -4.060588, 0.000000, 86.000000] #last 4 columns
     dyn_fsi.multizone = True
     dyn_fsi.unsteady  = True
@@ -1094,7 +1094,7 @@ def main():
     cht_incompressible.cfg_dir   = "coupled_cht/incomp_2d"
     cht_incompressible.cfg_file  = "cht_2d_3cylinders.cfg"
     cht_incompressible.test_iter = 10
-    cht_incompressible.test_vals = [-2.128826, -0.588813, -0.588813, -0.588813] #last 4 columns
+    cht_incompressible.test_vals = [-2.128826, -0.588813, -0.588813, -0.588813]
     cht_incompressible.multizone = True
     test_list.append(cht_incompressible)
 
@@ -1116,7 +1116,7 @@ def main():
     mms_fvm_ns.cfg_dir   = "mms/fvm_navierstokes"
     mms_fvm_ns.cfg_file  = "lam_mms_roe.cfg"
     mms_fvm_ns.test_iter = 20
-    mms_fvm_ns.test_vals = [-2.851428, 2.192348, 0.000000, 0.000000] #last 4 columns
+    mms_fvm_ns.test_vals = [-2.851428, 2.192348, 0.000000, 0.000000]
     mms_fvm_ns.tol       = 0.0001
     test_list.append(mms_fvm_ns)
 
@@ -1125,7 +1125,7 @@ def main():
     mms_fvm_inc_euler.cfg_dir   = "mms/fvm_incomp_euler"
     mms_fvm_inc_euler.cfg_file  = "inv_mms_jst.cfg"
     mms_fvm_inc_euler.test_iter = 20
-    mms_fvm_inc_euler.test_vals = [-9.128345, -9.441741, 0.000000, 0.000000] #last 4 columns
+    mms_fvm_inc_euler.test_vals = [-9.128345, -9.441741, 0.000000, 0.000000]
     mms_fvm_inc_euler.tol       = 0.0001
     test_list.append(mms_fvm_inc_euler)
 
@@ -1134,7 +1134,7 @@ def main():
     mms_fvm_inc_ns.cfg_dir   = "mms/fvm_incomp_navierstokes"
     mms_fvm_inc_ns.cfg_file  = "lam_mms_fds.cfg"
     mms_fvm_inc_ns.test_iter = 20
-    mms_fvm_inc_ns.test_vals = [-7.414944, -7.631546, 0.000000, 0.000000] #last 4 columns
+    mms_fvm_inc_ns.test_vals = [-7.414944, -7.631546, 0.000000, 0.000000]
     mms_fvm_inc_ns.tol       = 0.0001
     test_list.append(mms_fvm_inc_ns)
 
@@ -1143,7 +1143,7 @@ def main():
     ringleb_dg_euler.cfg_dir   = "mms/dg_ringleb"
     ringleb_dg_euler.cfg_file  = "ringleb_dg.cfg"
     ringleb_dg_euler.test_iter = 100
-    ringleb_dg_euler.test_vals = [-5.136652, -4.724941, 0.000000, 0.000000] #last 4 columns
+    ringleb_dg_euler.test_vals = [-5.136652, -4.724941, 0.000000, 0.000000]
     ringleb_dg_euler.tol       = 0.0001
     test_list.append(ringleb_dg_euler)
 
@@ -1152,7 +1152,7 @@ def main():
     mms_dg_ns.cfg_dir   = "mms/dg_navierstokes"
     mms_dg_ns.cfg_file  = "lam_mms_dg.cfg"
     mms_dg_ns.test_iter = 100
-    mms_dg_ns.test_vals = [-1.845393, 3.520699, 0.000000, 0.000000] #last 4 columns
+    mms_dg_ns.test_vals = [-1.845393, 3.520699, 0.000000, 0.000000]
     mms_dg_ns.tol       = 0.0001
     test_list.append(mms_dg_ns)
 
@@ -1161,7 +1161,7 @@ def main():
     mms_dg_ns_3d.cfg_dir   = "mms/dg_navierstokes_3d"
     mms_dg_ns_3d.cfg_file  = "lam_mms_dg_3d.cfg"
     mms_dg_ns_3d.test_iter = 100
-    mms_dg_ns_3d.test_vals = [-0.146826, 5.356413, 0.000000, 0.000000] #last 4 columns
+    mms_dg_ns_3d.test_vals = [-0.146826, 5.356413, 0.000000, 0.000000]
     mms_dg_ns_3d.tol       = 0.0001
     test_list.append(mms_dg_ns_3d)
 
@@ -1456,7 +1456,7 @@ def main():
     opt_multiobj1surf_py.cfg_dir    = "optimization_euler/multiobjective_wedge"
     opt_multiobj1surf_py.cfg_file   = "inv_wedge_ROE_multiobj_1surf.cfg"
     opt_multiobj1surf_py.test_iter  = 1
-    opt_multiobj1surf_py.test_vals = [1.000000, 1.000000, 30.428280, 2.039416] #last 4 columns
+    opt_multiobj1surf_py.test_vals = [1.000000, 1.000000, 30.428280, 2.039416]
     opt_multiobj1surf_py.command    =  TestCase.Command(exec = "shape_optimization.py", param = "-g CONTINUOUS_ADJOINT -f")
     opt_multiobj1surf_py.timeout    = 1600
     opt_multiobj1surf_py.tol       = 0.00001
@@ -1468,7 +1468,7 @@ def main():
     opt_2surf1obj_py.cfg_dir    = "optimization_euler/multiobjective_wedge"
     opt_2surf1obj_py.cfg_file   = "inv_wedge_ROE_2surf_1obj.cfg"
     opt_2surf1obj_py.test_iter  = 1
-    opt_2surf1obj_py.test_vals = [1.000000, 1.000000, 2.005694, 0.000185] #last 4 columns
+    opt_2surf1obj_py.test_vals = [1.000000, 1.000000, 2.005694, 0.000185]
     opt_2surf1obj_py.command    =  TestCase.Command(exec = "shape_optimization.py", param = "-g CONTINUOUS_ADJOINT -f")
     opt_2surf1obj_py.timeout    = 1600
     opt_2surf1obj_py.tol       = 0.00001
@@ -1484,7 +1484,7 @@ def main():
     pywrapper_naca0012.cfg_dir   = "euler/naca0012"
     pywrapper_naca0012.cfg_file  = "inv_NACA0012_Roe.cfg"
     pywrapper_naca0012.test_iter = 20
-    pywrapper_naca0012.test_vals = [-4.023999, -3.515034, 0.339426, 0.022217] #last 4 columns
+    pywrapper_naca0012.test_vals = [-4.023999, -3.515034, 0.339426, 0.022217]
     pywrapper_naca0012.command   =  TestCase.Command(exec = "SU2_CFD.py", param = "-f")
     pywrapper_naca0012.timeout   = 1600
     pywrapper_naca0012.tol       = 0.00001
@@ -1509,7 +1509,7 @@ def main():
     pywrapper_square_cylinder.cfg_dir   = "unsteady/square_cylinder"
     pywrapper_square_cylinder.cfg_file  = "turb_square.cfg"
     pywrapper_square_cylinder.test_iter = 3
-    pywrapper_square_cylinder.test_vals = [-2.557820, -1.158056, 0.067984, 1.399788, 2.220411, 1.399743, 2.218612, -0.453170]
+    pywrapper_square_cylinder.test_vals = [-2.557884, -1.173573, 0.058052, 1.399794, 2.220411, 1.399748, 2.218612, -0.453340]
     pywrapper_square_cylinder.command   =  TestCase.Command(exec = "SU2_CFD.py", param = "-f")
     pywrapper_square_cylinder.timeout   = 1600
     pywrapper_square_cylinder.tol       = 0.00001
@@ -1535,7 +1535,7 @@ def main():
     pywrapper_fsi2d.cfg_dir   = "fea_fsi/WallChannel_2d"
     pywrapper_fsi2d.cfg_file  = "configFSI.cfg"
     pywrapper_fsi2d.test_iter = 4
-    pywrapper_fsi2d.test_vals = [4, 0, -3.743214, -4.133482] #last 4 columns
+    pywrapper_fsi2d.test_vals = [4.000000, 0.000000, -3.743214, -4.133482]
     pywrapper_fsi2d.command   =  TestCase.Command(exec = "SU2_CFD.py", param = "--nZone 2 --fsi True -f")
     pywrapper_fsi2d.unsteady  = True
     pywrapper_fsi2d.multizone   = True
@@ -1549,7 +1549,7 @@ def main():
     pywrapper_unsteadyCHT.cfg_dir       = "py_wrapper/flatPlate_unsteady_CHT"
     pywrapper_unsteadyCHT.cfg_file      = "unsteady_CHT_FlatPlate_Conf.cfg"
     pywrapper_unsteadyCHT.test_iter     = 5
-    pywrapper_unsteadyCHT.test_vals     = [-1.614167, 2.245716, 0.000766, 0.175719]
+    pywrapper_unsteadyCHT.test_vals     = [-1.614167, 2.240658, 0.000772, 0.177467]
     pywrapper_unsteadyCHT.command       =  TestCase.Command(exec = "python", param = "launch_unsteady_CHT_FlatPlate.py -f")
     pywrapper_unsteadyCHT.timeout       = 1600
     pywrapper_unsteadyCHT.tol           = 0.00001
@@ -1562,7 +1562,7 @@ def main():
     pywrapper_rigidMotion.cfg_dir       = "py_wrapper/flatPlate_rigidMotion"
     pywrapper_rigidMotion.cfg_file      = "flatPlate_rigidMotion_Conf.cfg"
     pywrapper_rigidMotion.test_iter     = 5
-    pywrapper_rigidMotion.test_vals     = [-1.614170, 2.242953, 0.350050, 0.093116]
+    pywrapper_rigidMotion.test_vals     = [-1.614165, 2.238592, 0.349984, 0.095593]
     pywrapper_rigidMotion.command       = TestCase.Command(exec = "python", param = "launch_flatPlate_rigidMotion.py -f")
     pywrapper_rigidMotion.timeout       = 1600
     pywrapper_rigidMotion.tol           = 0.00001

From 44c931289c56329c505a216dfa18ffaab0d3cc58 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 1 Jul 2023 13:33:51 -0700
Subject: [PATCH 516/656] hybrid

---
 TestCases/hybrid_regression.py | 54 +++++++++++++++++-----------------
 1 file changed, 27 insertions(+), 27 deletions(-)

diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index 612b7669a56..d5a79faac09 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -100,7 +100,7 @@ def main():
     flatplate.cfg_dir   = "navierstokes/flatplate"
     flatplate.cfg_file  = "lam_flatplate.cfg"
     flatplate.test_iter = 100
-    flatplate.test_vals         = [-9.154121, -3.663180, 0.001112, 0.036277, 2.361500, -2.325300, -2.278800, -2.278800]
+    flatplate.test_vals         = [-9.154123, -3.663185, 0.001112, 0.036277, 2.361500, -2.325300, -2.278800, -2.278800]
     flatplate.test_vals_aarch64 = [-9.154130, -3.663197, 0.001112, 0.036277, 2.361500, -2.325300, -2.278800, -2.278800]
     test_list.append(flatplate)
 
@@ -109,7 +109,7 @@ def main():
     cylinder.cfg_dir   = "navierstokes/cylinder"
     cylinder.cfg_file  = "lam_cylinder.cfg"
     cylinder.test_iter = 25
-    cylinder.test_vals         = [-6.765429, -1.297425, 0.019571, 0.310230, 0.123270]
+    cylinder.test_vals         = [-6.765429, -1.297425, 0.019571, 0.310233, 0.123270]
     cylinder.test_vals_aarch64 = [-6.765429, -1.297425, 0.019571, 0.310231, 0.123270]
     test_list.append(cylinder)
 
@@ -118,7 +118,7 @@ def main():
     cylinder_lowmach.cfg_dir   = "navierstokes/cylinder"
     cylinder_lowmach.cfg_file  = "cylinder_lowmach.cfg"
     cylinder_lowmach.test_iter = 25
-    cylinder_lowmach.test_vals         = [-6.850130, -1.388096, -0.056036, 108.140806, 0.007988]
+    cylinder_lowmach.test_vals         = [-6.850130, -1.388096, -0.056036, 108.140809, 0.007988]
     cylinder_lowmach.test_vals_aarch64 = [-6.850130, -1.388096, -0.056036, 108.140813, 0.007988]
     test_list.append(cylinder_lowmach)
 
@@ -166,7 +166,7 @@ def main():
     rae2822_sst.cfg_dir   = "rans/rae2822"
     rae2822_sst.cfg_file  = "turb_SST_RAE2822.cfg"
     rae2822_sst.test_iter = 20
-    rae2822_sst.test_vals = [-0.510634, 4.869669, 0.811906, 0.061614, -82395.000000]
+    rae2822_sst.test_vals = [-0.510363, 4.872736, 0.815617, 0.060920, -73391.000000]
     test_list.append(rae2822_sst)
 
     # RAE2822 SST_SUST
@@ -174,7 +174,7 @@ def main():
     rae2822_sst_sust.cfg_dir   = "rans/rae2822"
     rae2822_sst_sust.cfg_file  = "turb_SST_SUST_RAE2822.cfg"
     rae2822_sst_sust.test_iter = 20
-    rae2822_sst_sust.test_vals = [-2.420843, 4.869669, 0.811906, 0.061614]
+    rae2822_sst_sust.test_vals = [-2.535141, 4.872736, 0.815617, 0.060920]
     test_list.append(rae2822_sst_sust)
 
     # Flat plate
@@ -190,7 +190,7 @@ def main():
     turb_oneram6.cfg_dir   = "rans/oneram6"
     turb_oneram6.cfg_file  = "turb_ONERAM6.cfg"
     turb_oneram6.test_iter = 10
-    turb_oneram6.test_vals = [-2.388836, -6.689414, 0.230320, 0.157640, -32539.000000]
+    turb_oneram6.test_vals = [-2.388836, -6.689426, 0.230320, 0.157640, -32539.000000]
     test_list.append(turb_oneram6)
 
     # NACA0012 (SA, FUN3D finest grid results: CL=1.0983, CD=0.01242)
@@ -225,7 +225,7 @@ def main():
     turb_naca0012_sst_fixedvalues.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst_fixedvalues.cfg_file  = "turb_NACA0012_sst_fixedvalues.cfg"
     turb_naca0012_sst_fixedvalues.test_iter = 10
-    turb_naca0012_sst_fixedvalues.test_vals         = [-5.192502, -9.575351, -1.568269, 1.022571, 0.040527, -2.384334]
+    turb_naca0012_sst_fixedvalues.test_vals         = [-5.192598, -10.042489, -1.617721, 1.022073, 0.040198, -2.381138]
     turb_naca0012_sst_fixedvalues.test_vals_aarch64 = [-5.192501, -9.575897, -1.568269, 1.022571, 0.040527, -2.384327]
     test_list.append(turb_naca0012_sst_fixedvalues)
 
@@ -234,7 +234,7 @@ def main():
     turb_naca0012_sst_expliciteuler.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst_expliciteuler.cfg_file  = "turb_NACA0012_sst_expliciteuler.cfg"
     turb_naca0012_sst_expliciteuler.test_iter = 10
-    turb_naca0012_sst_expliciteuler.test_vals = [-3.532228, -3.157766, 3.364025, 1.124824, 0.501717, -float("inf")]
+    turb_naca0012_sst_expliciteuler.test_vals = [-3.532289, -3.157766, 3.364024, 1.122901, 0.500798, -inf]
     test_list.append(turb_naca0012_sst_expliciteuler)
 
     # PROPELLER
@@ -268,7 +268,7 @@ def main():
     turb_naca0012_sst_restart_mg.cfg_file  = "turb_NACA0012_sst_multigrid_restart.cfg"
     turb_naca0012_sst_restart_mg.test_iter = 20
     turb_naca0012_sst_restart_mg.ntest_vals = 5
-    turb_naca0012_sst_restart_mg.test_vals = [-7.652987, -7.729472, -1.981061, -0.000015, 0.079061]
+    turb_naca0012_sst_restart_mg.test_vals = [-7.644702, -7.433663, -1.918163, -0.000003, 0.079111]
     test_list.append(turb_naca0012_sst_restart_mg)
 
     #############################
@@ -280,7 +280,7 @@ def main():
     turb_naca0012_1c.cfg_dir   = "rans_uq/naca0012"
     turb_naca0012_1c.cfg_file  = "turb_NACA0012_uq_1c.cfg"
     turb_naca0012_1c.test_iter = 10
-    turb_naca0012_1c.test_vals         = [-4.980749, 1.139261, 0.244644, -0.112857]
+    turb_naca0012_1c.test_vals         = [-4.980878, 1.138865, 0.247731, -0.117335]
     turb_naca0012_1c.test_vals_aarch64 = [-4.981149, 1.139192, 0.244886, -0.112789]
     test_list.append(turb_naca0012_1c)
 
@@ -289,7 +289,7 @@ def main():
     turb_naca0012_2c.cfg_dir   = "rans_uq/naca0012"
     turb_naca0012_2c.cfg_file  = "turb_NACA0012_uq_2c.cfg"
     turb_naca0012_2c.test_iter = 10
-    turb_naca0012_2c.test_vals         = [-5.483318, 0.968892, 0.212994, -0.120007]
+    turb_naca0012_2c.test_vals         = [-5.483313, 0.968731, 0.215420, -0.124767]
     turb_naca0012_2c.test_vals_aarch64 = [-5.483350, 0.968882, 0.212493, -0.120171]
     test_list.append(turb_naca0012_2c)
 
@@ -298,7 +298,7 @@ def main():
     turb_naca0012_3c.cfg_dir   = "rans_uq/naca0012"
     turb_naca0012_3c.cfg_file  = "turb_NACA0012_uq_3c.cfg"
     turb_naca0012_3c.test_iter = 10
-    turb_naca0012_3c.test_vals         = [-5.584300, 0.931383, 0.205114, -0.120892]
+    turb_naca0012_3c.test_vals         = [-5.584300, 0.931293, 0.207446, -0.125692]
     turb_naca0012_3c.test_vals_aarch64 = [-5.584300, 0.931383, 0.205116, -0.120891]
     test_list.append(turb_naca0012_3c)
 
@@ -307,7 +307,7 @@ def main():
     turb_naca0012_p1c1.cfg_dir   = "rans_uq/naca0012"
     turb_naca0012_p1c1.cfg_file  = "turb_NACA0012_uq_p1c1.cfg"
     turb_naca0012_p1c1.test_iter = 10
-    turb_naca0012_p1c1.test_vals         = [-5.132760, 1.075858, 0.333412, -0.078553]
+    turb_naca0012_p1c1.test_vals         = [-5.132363, 1.075634, 0.337251, -0.082829]
     turb_naca0012_p1c1.test_vals_aarch64 = [-5.132731, 1.075863, 0.333419, -0.078553]
     test_list.append(turb_naca0012_p1c1)
 
@@ -316,7 +316,7 @@ def main():
     turb_naca0012_p1c2.cfg_dir   = "rans_uq/naca0012"
     turb_naca0012_p1c2.cfg_file  = "turb_NACA0012_uq_p1c2.cfg"
     turb_naca0012_p1c2.test_iter = 10
-    turb_naca0012_p1c2.test_vals         = [-5.554392, 0.943810, 0.226719, -0.116439]
+    turb_naca0012_p1c2.test_vals         = [-5.554392, 0.943703, 0.229483, -0.121058]
     turb_naca0012_p1c2.test_vals_aarch64 = [-5.554433, 0.943787, 0.226530, -0.116503]
     test_list.append(turb_naca0012_p1c2)
 
@@ -329,7 +329,7 @@ def main():
     harmonic_balance.cfg_dir   = "harmonic_balance"
     harmonic_balance.cfg_file  = "HB.cfg"
     harmonic_balance.test_iter = 25
-    harmonic_balance.test_vals = [-1.589739, 0.790169, 0.937053, 3.922579]
+    harmonic_balance.test_vals = [-1.589740, 0.790168, 0.937052, 3.922578]
     test_list.append(harmonic_balance)
 
     # Turbulent pitching NACA 64a010 airfoil
@@ -337,7 +337,7 @@ def main():
     hb_rans_preconditioning.cfg_dir   = "harmonic_balance/hb_rans_preconditioning"
     hb_rans_preconditioning.cfg_file  = "davis.cfg"
     hb_rans_preconditioning.test_iter = 25
-    hb_rans_preconditioning.test_vals = [-1.902097, 0.484069, 0.601483, 3.609005, -5.949274]
+    hb_rans_preconditioning.test_vals = [-1.902111, 0.484080, 0.601469, 3.608991, -5.949373]
     test_list.append(hb_rans_preconditioning)
 
     #############################
@@ -416,7 +416,7 @@ def main():
     inc_turb_naca0012_sst_sust.cfg_dir   = "incomp_rans/naca0012"
     inc_turb_naca0012_sst_sust.cfg_file  = "naca0012_SST_SUST.cfg"
     inc_turb_naca0012_sst_sust.test_iter = 20
-    inc_turb_naca0012_sst_sust.test_vals = [-7.274028, 0.145888, 0.000002, 0.312014]
+    inc_turb_naca0012_sst_sust.test_vals = [-7.270637, 0.018416, 0.000004, 0.307678]
     test_list.append(inc_turb_naca0012_sst_sust)
 
     # Weakly coupled heat equation
@@ -436,7 +436,7 @@ def main():
     cavity.cfg_dir   = "moving_wall/cavity"
     cavity.cfg_file  = "lam_cavity.cfg"
     cavity.test_iter = 25
-    cavity.test_vals = [-5.627934, -0.164469, 0.052000, 2.547062]
+    cavity.test_vals = [-5.627934, -0.164469, 0.052000, 2.547063]
     test_list.append(cavity)
 
     # Spinning cylinder
@@ -444,7 +444,7 @@ def main():
     spinning_cylinder.cfg_dir   = "moving_wall/spinning_cylinder"
     spinning_cylinder.cfg_file  = "spinning_cylinder.cfg"
     spinning_cylinder.test_iter = 25
-    spinning_cylinder.test_vals         = [-8.001290, -2.607958, 1.501321, 1.488559]
+    spinning_cylinder.test_vals         = [-8.001291, -2.607959, 1.501321, 1.488559]
     spinning_cylinder.test_vals_aarch64 = [-8.001291, -2.607959, 1.501321, 1.488559]
     test_list.append(spinning_cylinder)
 
@@ -457,7 +457,7 @@ def main():
     square_cylinder.cfg_dir   = "unsteady/square_cylinder"
     square_cylinder.cfg_file  = "turb_square.cfg"
     square_cylinder.test_iter = 3
-    square_cylinder.test_vals = [-2.558128, -1.158062, 0.067932, 1.399788, 2.220402, 1.399743, 2.218603, -0.453110]
+    square_cylinder.test_vals = [-2.557949, -1.173575, 0.058030, 1.399794, 2.220402, 1.399748, 2.218603, -0.453270]
     square_cylinder.test_vals_aarch64 = [-2.558106, -1.162563, 0.066386, 1.399788, 2.220402, 1.399743, 2.218603, -0.453110]
     square_cylinder.unsteady  = True
     test_list.append(square_cylinder)
@@ -494,7 +494,7 @@ def main():
     aeroelastic.cfg_dir   = "aeroelastic"
     aeroelastic.cfg_file  = "aeroelastic_NACA64A010.cfg"
     aeroelastic.test_iter = 2
-    aeroelastic.test_vals         = [0.074433, 0.033108, -0.001650, -0.000127]
+    aeroelastic.test_vals         = [0.074432, 0.033108, -0.001650, -0.000127]
     aeroelastic.test_vals_aarch64 = [0.074836, 0.033102, -0.001650, -0.000127]
     aeroelastic.unsteady  = True
     aeroelastic.enabled_on_cpu_arch = ["x86_64"] # Requires AVX-capable architecture
@@ -514,7 +514,7 @@ def main():
     unst_inc_turb_naca0015_sa.cfg_dir   = "unsteady/pitching_naca0015_rans_inc"
     unst_inc_turb_naca0015_sa.cfg_file  = "config_incomp_turb_sa.cfg"
     unst_inc_turb_naca0015_sa.test_iter = 1
-    unst_inc_turb_naca0015_sa.test_vals = [-3.008629, -6.888974, 1.435193, 0.433537]
+    unst_inc_turb_naca0015_sa.test_vals = [-3.008629, -6.888963, 1.435186, 0.433529]
     unst_inc_turb_naca0015_sa.unsteady  = True
     test_list.append(unst_inc_turb_naca0015_sa)
 
@@ -536,7 +536,7 @@ def main():
     edge_VW.cfg_dir   = "nicf/edge"
     edge_VW.cfg_file  = "edge_VW.cfg"
     edge_VW.test_iter = 100
-    edge_VW.test_vals = [-5.040287, 1.124488, -0.000009, 0.000000]
+    edge_VW.test_vals = [-5.040246, 1.124521, -0.000009, 0.000000]
     test_list.append(edge_VW)
 
     # Rarefaction shock wave edge_PPR
@@ -544,7 +544,7 @@ def main():
     edge_PPR.cfg_dir   = "nicf/edge"
     edge_PPR.cfg_file  = "edge_PPR.cfg"
     edge_PPR.test_iter = 100
-    edge_PPR.test_vals         = [-5.401597, 0.738210, -0.000035, 0.000000]
+    edge_PPR.test_vals         = [-5.401604, 0.738202, -0.000035, 0.000000]
     edge_PPR.test_vals_aarch64 = [-5.401642, 0.738164, -0.000035, 0.000000]
     test_list.append(edge_PPR)
 
@@ -565,7 +565,7 @@ def main():
     axial_stage2D.cfg_dir   = "turbomachinery/axial_stage_2D"
     axial_stage2D.cfg_file  = "Axial_stage2D.cfg"
     axial_stage2D.test_iter = 20
-    axial_stage2D.test_vals         = [1.047244, 1.661126, -2.914064, 2.588061, -2.486924, 3.050785, 106380, 106380]
+    axial_stage2D.test_vals         = [0.974788, 1.534326, -2.897693, 2.599374, -2.418314, 3.087291, 106380.000000, 106380.000000]
     axial_stage2D.test_vals_aarch64 = [1.047244, 1.661126, -2.914064, 2.588061, -2.486924, 3.050785, 106380, 106380]
     test_list.append(axial_stage2D)
 
@@ -648,7 +648,7 @@ def main():
     bars_SST_2D.cfg_dir   = "sliding_interface/bars_SST_2D"
     bars_SST_2D.cfg_file  = "bars.cfg"
     bars_SST_2D.test_iter = 13
-    bars_SST_2D.test_vals = [13.000000, -0.604409, -1.523885]
+    bars_SST_2D.test_vals = [13.000000, -0.773513, -1.700012]
     bars_SST_2D.multizone = True
     test_list.append(bars_SST_2D)
 
@@ -680,7 +680,7 @@ def main():
     dynbeam2d.cfg_dir   = "fea_fsi/DynBeam_2d"
     dynbeam2d.cfg_file  = "configBeam_2d.cfg"
     dynbeam2d.test_iter = 6
-    dynbeam2d.test_vals = [-3.240015, 2.895057, -0.353146, 66127.000000]
+    dynbeam2d.test_vals = [-3.240016, 2.895057, -0.353147, 66127.000000]
     dynbeam2d.unsteady  = True
     test_list.append(dynbeam2d)
 

From d50035800ed097672eb9887bb58c7867f5cdf90a Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Sat, 1 Jul 2023 14:29:43 -0700
Subject: [PATCH 517/656] Update TestCases/hybrid_regression.py

---
 TestCases/hybrid_regression.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index d5a79faac09..25811d49a7f 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -234,7 +234,7 @@ def main():
     turb_naca0012_sst_expliciteuler.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst_expliciteuler.cfg_file  = "turb_NACA0012_sst_expliciteuler.cfg"
     turb_naca0012_sst_expliciteuler.test_iter = 10
-    turb_naca0012_sst_expliciteuler.test_vals = [-3.532289, -3.157766, 3.364024, 1.122901, 0.500798, -inf]
+    turb_naca0012_sst_expliciteuler.test_vals = [-3.532289, -3.157766, 3.364024, 1.122901, 0.500798, -float("inf")]
     test_list.append(turb_naca0012_sst_expliciteuler)
 
     # PROPELLER

From 2756e05780bd267543c1442a79032ac8edff6882 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 1 Jul 2023 19:15:52 -0700
Subject: [PATCH 518/656] update parallel restarts

---
 TestCases/parallel_regression.py              |  4 ++--
 TestCases/rans/naca0012/turb_NACA0012_sst.cfg |  1 +
 TestCases/serial_regression.py                | 16 ++++++++--------
 3 files changed, 11 insertions(+), 10 deletions(-)

diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index b2610bd9823..43a38a042fb 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -264,7 +264,7 @@ def main():
     ea_naca64206.test_iter = 10
     ea_naca64206.test_vals = [-1.076215, -0.391987, -0.000701, 67775.000000]
     test_list.append(ea_naca64206)
-    
+
     # SUPERSONIC FLOW PAST A RAMP IN A CHANNEL
     ramp = TestCase('ramp')
     ramp.cfg_dir = "euler/ramp"
@@ -459,7 +459,7 @@ def main():
     turb_naca0012_sst_expliciteuler.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst_expliciteuler.cfg_file  = "turb_NACA0012_sst_expliciteuler.cfg"
     turb_naca0012_sst_expliciteuler.test_iter = 10
-    turb_naca0012_sst_expliciteuler.test_vals = [-3.532289, -3.157766, 3.364024, 1.122901, 0.500798, -inf]
+    turb_naca0012_sst_expliciteuler.test_vals = [-3.532289, -3.157766, 3.364024, 1.122901, 0.500798, -float("inf")]
     turb_naca0012_sst_expliciteuler.timeout   = 3200
     test_list.append(turb_naca0012_sst_expliciteuler)
 
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst.cfg
index 5bf963e82aa..caa8b1bad5b 100644
--- a/TestCases/rans/naca0012/turb_NACA0012_sst.cfg
+++ b/TestCases/rans/naca0012/turb_NACA0012_sst.cfg
@@ -14,6 +14,7 @@
 %
 SOLVER= RANS
 KIND_TURB_MODEL= SST
+SST_OPTIONS= V1994m
 MATH_PROBLEM= DIRECT
 RESTART_SOL= YES
 READ_BINARY_RESTART= NO
diff --git a/TestCases/serial_regression.py b/TestCases/serial_regression.py
index 586cb5ba0b0..6efa0e033cf 100644
--- a/TestCases/serial_regression.py
+++ b/TestCases/serial_regression.py
@@ -279,8 +279,8 @@ def main():
     turb_naca0012_sst.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     turb_naca0012_sst.test_iter = 10
-    turb_naca0012_sst.test_vals         = [-11.421948, -12.801962, -5.865325, 1.049990, 0.019163, -1.939735, -38.695000]
-    turb_naca0012_sst.test_vals_aarch64 = [-11.451008, -12.798258, -5.863895, 1.049989, 0.019163, -1.925030, -38.694000]
+    turb_naca0012_sst.test_vals         = [-12.007177, -14.272504, -6.994514, 1.050109, 0.019148, -1.455402, -3.8510e+01]
+    turb_naca0012_sst.test_vals_aarch64 = [-12.007177, -14.272504, -6.994514, 1.050109, 0.019148, -1.455402, -3.8510e+01]
     turb_naca0012_sst.timeout   = 3200
     test_list.append(turb_naca0012_sst)
 
@@ -298,7 +298,7 @@ def main():
     turb_naca0012_sst_sust_restart.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst_sust_restart.cfg_file  = "turb_NACA0012_sst_sust.cfg"
     turb_naca0012_sst_sust_restart.test_iter = 10
-    turb_naca0012_sst_sust_restart.test_vals = [-11.364741, -12.642741, -5.748040, 1.005234, 0.019017, -1.895891]
+    turb_naca0012_sst_sust_restart.test_vals = [-12.006877, -14.685697, -6.270559, 1.001189, 0.019384, -1.435246]
     turb_naca0012_sst_sust_restart.timeout   = 3200
     test_list.append(turb_naca0012_sst_sust_restart)
 
@@ -329,7 +329,7 @@ def main():
     axi_rans_air_nozzle_restart.cfg_dir   = "axisymmetric_rans/air_nozzle"
     axi_rans_air_nozzle_restart.cfg_file  = "air_nozzle_restart.cfg"
     axi_rans_air_nozzle_restart.test_iter = 10
-    axi_rans_air_nozzle_restart.test_vals = [-12.088204, -7.497812, -8.714688, -4.019578, -1924.800000]
+    axi_rans_air_nozzle_restart.test_vals = [-12.003752, -6.926896, -8.627670, -4.003588, -2.0198e+03]
     axi_rans_air_nozzle_restart.tol       = 0.0001
     test_list.append(axi_rans_air_nozzle_restart)
 
@@ -853,7 +853,7 @@ def main():
     Jones_tc_restart.cfg_dir   = "turbomachinery/APU_turbocharger"
     Jones_tc_restart.cfg_file  = "Jones_restart.cfg"
     Jones_tc_restart.test_iter = 5
-    Jones_tc_restart.test_vals = [-6.986563, -3.096834, -14.849532, -9.102914, -11.787851, -6.266208, 7.3266e+04, 7.3266e+04]
+    Jones_tc_restart.test_vals = [-6.341673, -4.347529, -14.317871, -8.739672, -11.333584, -5.762934, 7.3273e+04, 7.3273e+04]
     Jones_tc_restart.tol       = 0.0001
     test_list.append(Jones_tc_restart)
 
@@ -870,7 +870,7 @@ def main():
     transonic_stator_restart.cfg_dir   = "turbomachinery/transonic_stator_2D"
     transonic_stator_restart.cfg_file  = "transonic_stator_restart.cfg"
     transonic_stator_restart.test_iter = 20
-    transonic_stator_restart.test_vals = [-7.534574, -6.838075, -6.618228, -1.567726, -6.767343, -0.738638, -4.7165e+05]
+    transonic_stator_restart.test_vals = [-7.853522, -6.815458, -6.565073, -1.880583, -6.316205, -1.017773, -4.7182e+05]
     test_list.append(transonic_stator_restart)
 
 
@@ -1496,8 +1496,8 @@ def main():
     pywrapper_turb_naca0012_sst.cfg_dir   = "rans/naca0012"
     pywrapper_turb_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     pywrapper_turb_naca0012_sst.test_iter = 10
-    pywrapper_turb_naca0012_sst.test_vals         = [-11.421948, -12.801962, -5.865325, 1.049990, 0.019163, -1.939735, -38.695000]
-    pywrapper_turb_naca0012_sst.test_vals_aarch64 = [-11.451014, -12.798258, -5.863895, 1.049989, 0.019163, -1.925032, -38.694000]
+    pywrapper_turb_naca0012_sst.test_vals         = [-12.007177, -14.272504, -6.994514, 1.050109, 0.019148, -1.455402, -3.8510e+01]
+    pywrapper_turb_naca0012_sst.test_vals_aarch64 = [-12.007177, -14.272504, -6.994514, 1.050109, 0.019148, -1.455402, -3.8510e+01]
     pywrapper_turb_naca0012_sst.command   =  TestCase.Command(exec = "SU2_CFD.py", param = "-f")
     pywrapper_turb_naca0012_sst.timeout   = 3200
     pywrapper_turb_naca0012_sst.tol       = 0.00001

From 46b42e313cd9aa8f769a1c9fbf038b91937225df Mon Sep 17 00:00:00 2001
From: "Francesco Poli (wintermute)" <invernomuto@paranoici.org>
Date: Sun, 2 Jul 2023 18:37:13 +0200
Subject: [PATCH 519/656] drop QuickStart subdirectory

It has been moved to the Tutorials repository.
---
 QuickStart/.gitignore            |    12 -
 QuickStart/inv_NACA0012.cfg      |   324 -
 QuickStart/mesh_NACA0012_inv.su2 | 15707 -----------------------------
 externals/utils/release_su2.sh   |     3 -
 4 files changed, 16046 deletions(-)
 delete mode 100644 QuickStart/.gitignore
 delete mode 100644 QuickStart/inv_NACA0012.cfg
 delete mode 100644 QuickStart/mesh_NACA0012_inv.su2

diff --git a/QuickStart/.gitignore b/QuickStart/.gitignore
deleted file mode 100644
index 3fc9c7e5f80..00000000000
--- a/QuickStart/.gitignore
+++ /dev/null
@@ -1,12 +0,0 @@
-# In the QuickStart/ directory, we would like to
-# ignore any of the data needed to run the case
-# or their output data, i.e., meshes, solution
-# files, restart files, CSVs, etc.
-
-# Things appearing in QuickStart/ to ignore:
-*.dat
-*.csv
-*.plt
-*.szplt
-*.vtk
-config_*.cfg
diff --git a/QuickStart/inv_NACA0012.cfg b/QuickStart/inv_NACA0012.cfg
deleted file mode 100644
index 7f30c73c42a..00000000000
--- a/QuickStart/inv_NACA0012.cfg
+++ /dev/null
@@ -1,324 +0,0 @@
-%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-%                                                                              %
-% SU2 configuration file                                                       %
-% Case description: Transonic inviscid flow around a NACA0012 airfoil          %
-% Author: Thomas D. Economon                                                   %
-% Institution: Stanford University                                             %
-% Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                                  %
-%                                                                              %
-%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
-% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
-%
-% Physical governing equations (EULER, NAVIER_STOKES,
-%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
-%                               POISSON_EQUATION)
-SOLVER= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
-MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
-RESTART_SOL= NO
-
-% ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
-%
-% Mach number (non-dimensional, based on the free-stream values)
-MACH_NUMBER= 0.8
-%
-% Angle of attack (degrees)
-AOA= 1.25
-%
-% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)
-FREESTREAM_PRESSURE= 101325.0
-%
-% Free-stream temperature (273.15 K by default)
-FREESTREAM_TEMPERATURE= 273.15
-
-% -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
-%
-% Ratio of specific heats (1.4 (air), only for compressible flows)
-GAMMA_VALUE= 1.4
-%
-% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
-GAS_CONSTANT= 287.87
-
-% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
-%
-% Reference origin for moment computation
-REF_ORIGIN_MOMENT_X = 0.25
-REF_ORIGIN_MOMENT_Y = 0.00
-REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
-REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
-REF_AREA= 1.0
-%
-% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
-%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
-REF_DIMENSIONALIZATION= DIMENSIONAL
-
-% ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
-%
-% Marker of the Euler boundary (NONE = no marker)
-MARKER_EULER= ( airfoil )
-%
-% Marker of the far field (NONE = no marker)
-MARKER_FAR= ( farfield )
-
-% ------------------------ SURFACES IDENTIFICATION ----------------------------%
-%
-% Marker(s) of the surface in the surface flow solution file
-MARKER_PLOTTING = ( airfoil )
-%
-% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
-MARKER_MONITORING = ( airfoil )
-%
-% Marker(s) of the surface where obj. func. (design problem) will be evaluated
-MARKER_DESIGNING = ( airfoil )
-
-% ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
-%
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
-NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-%
-% Objective function in optimization problem (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX)
-OBJECTIVE_FUNCTION= DRAG
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
-CFL_NUMBER= 1e3
-%
-% Adaptive CFL number (NO, YES)
-CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
-CFL_ADAPT_PARAM= ( 0.1, 2.0, 10.0, 1e10 )
-%
-% Number of total iterations
-ITER= 250
-
-% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
-%
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
-LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
-LINEAR_SOLVER_PREC= ILU
-%
-% Minimum error of the linear solver for implicit formulations
-LINEAR_SOLVER_ERROR= 1E-10
-%
-% Max number of iterations of the linear solver for the implicit formulation
-LINEAR_SOLVER_ITER= 10
-
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= W_CYCLE
-%
-% Multi-Grid PreSmoothing Level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-Grid PostSmoothing Level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 1.0
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 1.0
-
-% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
-%
-% Convective numerical method
-%
-CONV_NUM_METHOD_FLOW= JST
-%
-% 2nd and 4th order artificial dissipation coefficients
-JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
-TIME_DISCRE_FLOW= EULER_IMPLICIT
-
-% ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
-%
-% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
-CONV_NUM_METHOD_ADJFLOW= JST
-%
-% Reduction factor of the CFL coefficient in the adjoint problem
-CFL_REDUCTION_ADJFLOW= 0.01
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
-TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
-
-% ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
-%
-% Kind of deformation (NO_DEFORMATION, TRANSLATION, ROTATION, SCALE,
-%                      FFD_SETTING, FFD_NACELLE
-%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS, FFD_TWIST
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D, FFD_TWIST_2D,
-%                      HICKS_HENNE, SURFACE_BUMP)
-DV_KIND= HICKS_HENNE
-%
-% Marker of the surface in which we are going apply the shape deformation
-DV_MARKER= ( airfoil )
-%
-% Parameters of the shape deformation
-% - NO_DEFORMATION ( 1.0 )
-% - TRANSLATION ( x_Disp, y_Disp, z_Disp ), as a unit vector
-% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - SCALE ( 1.0 )
-% - ANGLE_OF_ATTACK ( 1.0 )
-% - FFD_SETTING ( 1.0 )
-% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
-% - FFD_NACELLE ( FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Disp, phi_Disp )
-% - FFD_GULL ( FFD_BoxTag, j_Ind )
-% - FFD_ANGLE_OF_ATTACK ( FFD_BoxTag, 1.0 )
-% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
-% - FFD_TWIST ( FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
-% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
-% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - FFD_TWIST_2D ( FFD_BoxTag, x_Orig, y_Orig )
-% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
-% - SURFACE_BUMP ( x_Start, x_End, x_Loc )
-DV_PARAM= ( 1, 0.5 )
-%
-% Value of the shape deformation
-DV_VALUE= 0.01
-
-% ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
-%
-% Number of smoothing iterations for FEA mesh deformation
-DEFORM_LINEAR_SOLVER_ITER= 500
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
-DEFORM_NONLINEAR_ITER= 1
-%
-% Minimum residual criteria for the linear solver convergence of grid deformation
-DEFORM_LINEAR_SOLVER_ERROR= 1E-14
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
-DEFORM_CONSOLE_OUTPUT= YES
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
-DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-
-% --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-CONV_FIELD= RMS_DENSITY
-%
-% Min value of the residual (log10 of the residual)
-CONV_RESIDUAL_MINVAL= -8
-%
-% Start Cauchy criteria at iteration number
-CONV_STARTITER= 10
-%
-% Number of elements to apply the criteria
-CONV_CAUCHY_ELEMS= 100
-%
-% Epsilon to control the series convergence
-CONV_CAUCHY_EPS= 1E-6
-%
-SCREEN_OUTPUT=(INNER_ITER, WALL_TIME, RMS_RES, LIFT, DRAG, CAUCHY_SENS_PRESS, CAUCHY_DRAG RMS_ADJ_DENSITY RMS_ADJ_ENERGY)
-
-% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-% Mesh input file
-MESH_FILENAME= mesh_NACA0012_inv.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
-MESH_FORMAT= SU2
-%
-% Mesh output file
-MESH_OUT_FILENAME= mesh_out.su2
-%
-% Restart flow input file
-SOLUTION_FILENAME= solution_flow.dat
-%
-% Restart adjoint input file
-SOLUTION_ADJ_FILENAME= solution_adj.dat
-%
-% Output file format (TECPLOT, CSV)
-TABULAR_FORMAT= CSV
-%
-% Output file convergence history (w/o extension)
-CONV_FILENAME= history
-%
-% Output file restart flow
-RESTART_FILENAME= restart_flow.dat
-%
-% Output file restart adjoint
-RESTART_ADJ_FILENAME= restart_adj.dat
-%
-% Output file flow (w/o extension) variables
-VOLUME_FILENAME= flow
-%
-% Output file adjoint (w/o extension) variables
-VOLUME_ADJ_FILENAME= adjoint
-%
-% Output Objective function gradient (using continuous adjoint)
-GRAD_OBJFUNC_FILENAME= of_grad.dat
-%
-% Output file surface flow coefficient (w/o extension)
-SURFACE_FILENAME= surface_flow
-%
-% Output file surface adjoint coefficient (w/o extension)
-SURFACE_ADJ_FILENAME= surface_adjoint
-%
-% Writing solution file frequency
-OUTPUT_WRT_FREQ= 250
-
-% --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
-% Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY,
-%    FORCE_X, FORCE_Y, FORCE_Z,
-%    MOMENT_X, MOMENT_Y, MOMENT_Z,
-%    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
-%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%
-% Available geometrical based objective functions or constraint functions
-%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
-%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
-%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
-%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
-%
-% Available design variables
-%    HICKS_HENNE 	(  1, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    NACA_4DIGITS	(  4, Scale | Mark. List | 1st digit, 2nd digit, 3rd and 4th digit )
-%    TRANSLATION	(  5, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION		(  6, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_CONTROL_POINT_2D (  15, Scale | Mark. List | FFD_Box_ID, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D 	( 16, Scale | Mark. List | FFD_Box_ID, i_Ind )
-%    FFD_THICKNESS_2D 	( 17, Scale | Mark. List | FFD_Box_ID, i_Ind )
-%
-% Optimization objective function with scaling factor
-% ex= Objective * Scale
-OPT_OBJECTIVE= DRAG * 0.001
-%
-% Optimization constraint functions with scaling factors, separated by semicolons
-% ex= (Objective = Value ) * Scale, use '>','<','='
-OPT_CONSTRAINT= ( LIFT > 0.328188 ) * 0.001; ( MOMENT_Z > 0.034068 ) * 0.001; ( AIRFOIL_THICKNESS > 0.11 ) * 0.001
-%
-
-% Optimization design variables, separated by semicolons
-DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 ); ( 30, 1.0 | airfoil | 0, 0.20 ); ( 30, 1.0 | airfoil | 0, 0.25 ); ( 30, 1.0 | airfoil | 0, 0.30 ); ( 30, 1.0 | airfoil | 0, 0.35 ); ( 30, 1.0 | airfoil | 0, 0.40 ); ( 30, 1.0 | airfoil | 0, 0.45 ); ( 30, 1.0 | airfoil | 0, 0.50 ); ( 30, 1.0 | airfoil | 0, 0.55 ); ( 30, 1.0 | airfoil | 0, 0.60 ); ( 30, 1.0 | airfoil | 0, 0.65 ); ( 30, 1.0 | airfoil | 0, 0.70 ); ( 30, 1.0 | airfoil | 0, 0.75 ); ( 30, 1.0 | airfoil | 0, 0.80 ); ( 30, 1.0 | airfoil | 0, 0.85 ); ( 30, 1.0 | airfoil | 0, 0.90 ); ( 30, 1.0 | airfoil | 0, 0.95 ); ( 30, 1.0 | airfoil | 1, 0.05 ); ( 30, 1.0 | airfoil | 1, 0.10 ); ( 30, 1.0 | airfoil | 1, 0.15 ); ( 30, 1.0 | airfoil | 1, 0.20 ); ( 30, 1.0 | airfoil | 1, 0.25 ); ( 30, 1.0 | airfoil | 1, 0.30 ); ( 30, 1.0 | airfoil | 1, 0.35 ); ( 30, 1.0 | airfoil | 1, 0.40 ); ( 30, 1.0 | airfoil | 1, 0.45 ); ( 30, 1.0 | airfoil | 1, 0.50 ); ( 30, 1.0 | airfoil | 1, 0.55 ); ( 30, 1.0 | airfoil | 1, 0.60 ); ( 30, 1.0 | airfoil | 1, 0.65 ); ( 30, 1.0 | airfoil | 1, 0.70 ); ( 30, 1.0 | airfoil | 1, 0.75 ); ( 30, 1.0 | airfoil | 1, 0.80 ); ( 30, 1.0 | airfoil | 1, 0.85 ); ( 30, 1.0 | airfoil | 1, 0.90 ); ( 30, 1.0 | airfoil | 1, 0.95 )
diff --git a/QuickStart/mesh_NACA0012_inv.su2 b/QuickStart/mesh_NACA0012_inv.su2
deleted file mode 100644
index 0c809e5807e..00000000000
--- a/QuickStart/mesh_NACA0012_inv.su2
+++ /dev/null
@@ -1,15707 +0,0 @@
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-5	1508	720	886	1774
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-5	932	679	896	1778
-5	932	746	679	1779
-5	917	729	743	1780
-5	942	758	889	1781
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-5	890	662	673	1783
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-5	892	669	723	1787
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-5	895	890	673	1792
-5	895	673	680	1793
-5	932	888	746	1794
-5	896	679	666	1795
-5	897	895	680	1796
-5	897	680	675	1797
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-5	905	900	710	1812
-5	905	710	688	1813
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-5	909	678	715	1818
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-5	969	655	784	1823
-5	1335	1163	1313	1824
-5	912	866	656	1825
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-5	913	892	723	1828
-5	913	723	671	1829
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-5	1269	1140	1086	1832
-5	1151	961	1150	1833
-5	916	889	728	1834
-5	916	728	696	1835
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-5	918	877	667	1838
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-5	926	740	739	1845
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-5	1195	919	1016	1847
-5	924	873	697	1848
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-5	927	740	926	1855
-5	1129	937	1065	1856
-5	1085	855	854	1857
-5	929	696	742	1858
-5	928	742	741	1859
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-5	945	761	944	1862
-5	931	745	930	1863
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-5	934	747	933	1869
-5	1194	1016	1015	1870
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-5	936	731	750	1872
-5	936	874	731	1873
-5	1125	933	874	1874
-5	1139	949	941	1875
-5	938	741	753	1876
-5	937	753	752	1877
-5	1130	1121	928	1878
-5	1227	888	1061	1879
-5	940	699	755	1880
-5	940	870	699	1881
-5	1131	940	939	1882
-5	1052	959	870	1883
-5	949	765	757	1884
-5	1034	842	766	1885
-5	943	743	759	1886
-5	942	759	758	1887
-5	1368	1227	1061	1888
-5	1124	932	896	1889
-5	945	744	761	1890
-5	944	761	760	1891
-5	1117	925	922	1892
-5	1123	945	1135	1893
-5	947	764	763	1894
-5	948	764	947	1895
-5	1297	1136	1244	1896
-5	1106	908	1037	1897
-5	1095	964	965	1898
-5	1304	1144	1240	1899
-5	1149	960	959	1900
-5	950	765	949	1901
-5	1320	1176	1175	1902
-5	1034	766	950	1903
-5	952	768	767	1904
-5	953	768	952	1905
-5	1089	892	1050	1906
-5	1282	1094	1236	1907
-5	1430	1280	1373	1908
-5	954	769	953	1909
-5	1137	947	1136	1910
-5	1151	962	961	1911
-5	1146	956	1145	1912
-5	1212	950	1139	1913
-5	1152	962	1151	1914
-5	957	771	956	1915
-5	1197	1017	1196	1916
-5	958	772	957	1917
-5	1340	1126	1290	1918
-5	1196	1017	934	1919
-5	960	775	774	1920
-5	962	776	716	1921
-5	1110	1051	915	1922
-5	963	776	962	1923
-5	1094	871	890	1924
-5	966	780	777	1925
-5	1140	951	1086	1926
-5	1425	1282	1370	1927
-5	1079	1047	848	1928
-5	966	777	963	1929
-5	964	955	676	1930
-5	964	676	779	1931
-5	965	964	779	1932
-5	965	779	778	1933
-5	1298	1293	1131	1934
-5	1038	780	966	1935
-5	970	785	783	1936
-5	972	787	786	1937
-5	1169	983	1069	1938
-5	969	784	968	1939
-5	1173	987	986	1940
-5	1090	878	862	1941
-5	1182	1003	1002	1942
-5	971	785	970	1943
-5	1183	918	1005	1944
-5	972	786	971	1945
-5	1259	1087	1229	1946
-5	973	787	972	1947
-5	1179	995	994	1948
-5	974	732	973	1949
-5	1074	880	1178	1950
-5	1027	788	974	1951
-5	1185	1007	1006	1952
-5	1013	824	823	1953
-5	1347	1201	1346	1954
-5	1343	1199	1198	1955
-5	1172	986	904	1956
-5	1007	818	1006	1957
-5	1160	973	972	1958
-5	1008	819	1007	1959
-5	980	795	794	1960
-5	982	713	796	1961
-5	1168	981	1167	1962
-5	1023	832	713	1963
-5	1191	1012	976	1964
-5	1205	1162	884	1965
-5	1332	1188	1331	1966
-5	1023	713	982	1967
-5	984	799	798	1968
-5	985	708	799	1969
-5	1310	1226	1156	1970
-5	985	799	984	1971
-5	1318	1173	1172	1972
-5	1176	989	1175	1973
-5	1169	984	983	1974
-5	987	800	986	1975
-5	1178	991	1177	1976
-5	988	801	987	1977
-5	1177	991	990	1978
-5	989	802	988	1979
-5	1174	988	987	1980
-5	1310	1156	1155	1981
-5	1181	1073	903	1982
-5	991	804	990	1983
-5	1175	989	988	1984
-5	992	805	991	1985
-5	1170	984	1169	1986
-5	1157	970	967	1987
-5	994	808	807	1988
-5	999	705	811	1989
-5	1172	904	1171	1990
-5	997	810	809	1991
-5	1161	974	973	1992
-5	1207	1028	1027	1993
-5	1075	967	858	1994
-5	997	809	996	1995
-5	1101	1046	893	1996
-5	998	810	997	1997
-5	1584	1430	1509	1998
-5	999	811	998	1999
-5	1073	865	903	2000
-5	1183	1098	918	2001
-5	1000	899	682	2002
-5	1000	682	814	2003
-5	1001	1000	814	2004
-5	1001	814	813	2005
-5	1003	816	815	2006
-5	1005	730	817	2007
-5	1181	903	999	2008
-5	1004	816	1003	2009
-5	1178	880	992	2010
-5	1005	817	1004	2011
-5	1073	1002	865	2012
-5	1183	1004	1182	2013
-5	1189	1011	1010	2014
-5	1009	821	820	2015
-5	1104	906	1103	2016
-5	1334	1250	1053	2017
-5	1166	980	979	2018
-5	1009	820	1008	2019
-5	1203	1025	1024	2020
-5	1010	821	1009	2021
-5	1191	976	1163	2022
-5	1011	822	1010	2023
-5	1166	979	1053	2024
-5	1168	982	981	2025
-5	1192	1013	1012	2026
-5	1021	830	1020	2027
-5	1201	982	1168	2028
-5	1022	831	1021	2029
-5	1015	827	826	2030
-5	1016	733	827	2031
-5	1046	894	893	2032
-5	1016	827	1015	2033
-5	1212	1034	950	2034
-5	1128	936	1127	2035
-5	1135	944	1046	2036
-5	1018	828	1017	2037
-5	1106	1101	909	2038
-5	1019	851	651	2039
-5	1076	941	851	2040
-5	1212	1035	1034	2041
-5	1415	1056	1253	2042
-5	1163	975	1162	2043
-5	1349	1203	1348	2044
-5	1022	860	694	2045
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-5	1055	866	912	2047
-5	1192	1012	1191	2048
-5	1024	832	1023	2049
-5	1164	977	882	2050
-5	1026	690	834	2051
-5	1184	1006	978	2052
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-5	1179	996	995	2054
-5	1105	882	907	2055
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-5	1028	836	1027	2057
-5	1180	998	997	2058
-5	1029	837	1028	2059
-5	1105	907	1104	2060
-5	1030	838	1029	2061
-5	1103	906	900	2062
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-5	1031	983	789	2064
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-5	1033	841	840	2066
-5	1033	1031	841	2067
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-5	1517	1470	1397	2069
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-5	1066	869	931	2074
-5	1037	844	1036	2075
-5	1085	1065	855	2076
-5	1122	929	1121	2077
-5	1136	947	946	2078
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-5	1149	959	1052	2082
-5	1216	1040	1039	2083
-5	1050	892	913	2084
-5	1422	1270	1246	2085
-5	1042	863	849	2086
-5	1044	659	867	2087
-5	1436	1289	1260	2088
-5	1122	916	929	2089
-5	1256	691	1044	2090
-5	1080	658	691	2091
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-5	1045	895	897	2093
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-5	1273	1051	1110	2097
-5	1048	1045	897	2098
-5	1048	897	861	2099
-5	1049	910	850	2100
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-5	1089	861	892	2102
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-5	1079	848	873	2105
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-5	1053	979	881	2108
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-5	1054	902	860	2110
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-5	1102	864	1091	2114
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-5	1058	724	698	2117
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-5	1356	1243	1212	2124
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-5	1179	994	1074	2206
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-5	1439	1416	1288	2242
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-5	1130	938	1129	2244
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-5	1123	931	930	2248
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-5	1126	934	933	2252
-5	1197	1076	1019	2253
-5	1295	1123	1135	2254
-5	1196	934	1126	2255
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-5	1128	1125	874	2257
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-5	1130	928	938	2260
-5	1129	938	937	2261
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-5	1435	1386	1241	2263
-5	1132	870	940	2264
-5	1132	1052	870	2265
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-5	1134	1100	917	2268
-5	1133	943	942	2269
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-5	1285	1248	1115	2272
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-5	1137	948	947	2274
-5	1138	939	948	2275
-5	1293	1132	1131	2276
-5	1138	948	1137	2277
-5	1307	1152	1151	2278
-5	1298	1131	1138	2279
-5	1299	1076	1238	2280
-5	1213	1037	1036	2281
-5	1143	954	1142	2282
-5	1142	953	1141	2283
-5	1300	1141	1140	2284
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-5	1557	1381	1552	2286
-5	1297	1138	1137	2287
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-5	1147	958	957	2291
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-5	1304	1145	1144	2294
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-5	1305	1146	1304	2302
-5	1153	963	1152	2303
-5	1305	1148	1147	2304
-5	1214	966	1153	2305
-5	1359	1216	1215	2306
-5	1215	1039	1038	2307
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-5	1307	1151	1150	2309
-5	1155	969	968	2310
-5	1156	1090	862	2311
-5	1515	1080	1256	2312
-5	1156	969	1155	2313
-5	1899	1755	1754	2314
-5	1274	1090	1226	2315
-5	1158	971	970	2316
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-5	1453	1376	1309	2831
-5	1571	1253	1374	2832
-5	1576	1221	1415	2833
-5	1416	1404	1255	2834
-5	1416	1255	1288	2835
-5	1556	1389	1555	2836
-5	1521	1393	1233	2837
-5	1586	1380	1433	2838
-5	1767	1591	1658	2839
-5	1802	1663	1571	2840
-5	1702	1509	1541	2841
-5	1668	1578	1362	2842
-5	1669	1528	1364	2843
-5	1421	1400	1285	2844
-5	1421	1285	1303	2845
-5	1531	1384	1369	2846
-5	1581	1369	1423	2847
-5	1579	1422	1411	2848
-5	1670	1566	1531	2849
-5	1582	1427	1532	2850
-5	1538	1428	1378	2851
-5	1425	1381	1273	2852
-5	1425	1273	1282	2853
-5	1536	1457	1496	2854
-5	1642	1536	1496	2855
-5	1427	1424	1276	2856
-5	1427	1276	1272	2857
-5	1428	1397	1277	2858
-5	1428	1277	1232	2859
-5	1429	1398	1329	2860
-5	1429	1329	1328	2861
-5	1431	1235	1281	2862
-5	1430	1281	1280	2863
-5	1580	1422	1579	2864
-5	1548	1408	1507	2865
-5	1433	1286	1284	2866
-5	1432	1284	1283	2867
-5	1768	1623	1767	2868
-5	1770	1625	1672	2869
-5	1435	1241	1242	2870
-5	1434	1242	1287	2871
-5	1555	1389	1404	2872
-5	1565	1407	1390	2873
-5	1542	1394	1395	2874
-5	1565	1390	1556	2875
-5	1480	1340	1290	2876
-5	1481	1341	1340	2877
-5	1439	1288	1292	2878
-5	1438	1292	1291	2879
-5	1803	1709	1739	2880
-5	1738	1589	1673	2881
-5	1445	1297	1444	2882
-5	1500	1359	1308	2883
-5	1442	1339	1338	2884
-5	1479	1283	1339	2885
-5	1591	1442	1441	2886
-5	1479	1339	1442	2887
-5	1478	1337	1296	2888
-5	1598	1449	1597	2889
-5	1445	1298	1297	2890
-5	1501	1360	1359	2891
-5	1646	1451	1599	2892
-5	1499	1307	1451	2893
-5	1599	1451	1450	2894
-5	1500	1308	1499	2895
-5	1580	1423	1422	2896
-5	1577	1229	1419	2897
-5	1451	1245	1450	2898
-5	1499	1308	1307	2899
-5	1794	1647	1793	2900
-5	1804	1716	1791	2901
-5	1451	1307	1245	2902
-5	1501	1359	1500	2903
-5	1599	1450	1523	2904
-5	1543	1410	1540	2905
-5	1452	1399	1358	2906
-5	1452	1358	1357	2907
-5	1676	1516	1656	2908
-5	1608	1464	1463	2909
-5	1562	1517	1397	2910
-5	1455	1263	1454	2911
-5	1607	1463	1459	2912
-5	1492	1311	1455	2913
-5	1471	1314	1470	2914
-5	1471	1330	1314	2915
-5	1495	1354	1275	2916
-5	1496	1252	1355	2917
-5	1561	1396	1405	2918
-5	1604	1460	1537	2919
-5	1461	1319	1460	2920
-5	1465	1324	1323	2921
-5	1461	1320	1319	2922
-5	1462	1321	1320	2923
-5	1609	1465	1464	2924
-5	1462	1320	1461	2925
-5	1607	1459	1606	2926
-5	1676	1561	1516	2927
-5	1611	1467	1466	2928
-5	1613	1469	1468	2929
-5	1612	1467	1611	2930
-5	1465	1323	1464	2931
-5	1610	1466	1465	2932
-5	1466	1324	1465	2933
-5	1606	1462	1605	2934
-5	1469	1327	1468	2935
-5	1605	1461	1604	2936
-5	1469	1328	1327	2937
-5	1537	1460	1458	2938
-5	1750	1537	1699	2939
-5	1640	1493	1639	2940
-5	1757	1611	1610	2941
-5	1473	1331	1472	2942
-5	1472	1331	1330	2943
-5	1615	1470	1517	2944
-5	1617	1474	1616	2945
-5	1636	1490	1635	2946
-5	1474	1332	1473	2947
-5	1762	1617	1616	2948
-5	1582	1424	1427	2949
-5	1475	1334	1474	2950
-5	1475	1250	1334	2951
-5	1606	1459	1462	2952
-5	1605	1462	1461	2953
-5	1477	1336	1335	2954
-5	1486	1345	1485	2955
-5	1751	1605	1604	2956
-5	1621	1476	1539	2957
-5	2080	1934	2079	2958
-5	1585	1433	1432	2959
-5	1588	1386	1435	2960
-5	1650	1448	1502	2961
-5	1481	1410	1341	2962
-5	1481	1340	1480	2963
-5	1543	1388	1410	2964
-5	1648	1501	1500	2965
-5	1484	1343	1483	2966
-5	1485	1344	1484	2967
-5	1629	1483	1628	2968
-5	1631	1486	1485	2969
-5	1628	1483	1482	2970
-5	1486	1254	1345	2971
-5	1774	1629	1628	2972
-5	1486	1383	1254	2973
-5	1780	1636	1635	2974
-5	1634	1489	1488	2975
-5	1562	1397	1428	2976
-5	1490	1348	1489	2977
-5	1633	1488	1487	2978
-5	1491	1350	1349	2979
-5	1633	1487	1632	2980
-5	1615	1471	1470	2981
-5	1752	1606	1605	2982
-5	1491	1349	1490	2983
-5	1773	1627	1772	2984
-5	1621	1477	1476	2985
-5	1760	1614	1613	2986
-5	1493	1312	1492	2987
-5	1601	1424	1582	2988
-5	1494	1378	1353	2989
-5	1860	1714	1700	2990
-5	1616	1474	1473	2991
-5	1570	1414	1394	2992
-5	1496	1355	1495	2993
-5	1807	1570	1653	2994
-5	1786	1583	1731	2995
-5	1533	1452	1387	2996
-5	1498	1356	1497	2997
-5	1645	1533	1387	2998
-5	1643	1388	1543	2999
-5	1649	1502	1501	3000
-5	1502	1240	1360	3001
-5	1648	1500	1647	3002
-5	1569	1413	1568	3003
-5	1558	1392	1391	3004
-5	1502	1360	1501	3005
-5	1524	1421	1365	3006
-5	1564	1421	1524	3007
-5	1814	1551	1696	3008
-5	1515	1256	1393	3009
-5	1519	1371	1227	3010
-5	1849	1706	1687	3011
-5	1505	1504	660	3012
-5	1505	660	746	3013
-5	1506	1068	863	3014
-5	1506	1042	1379	3015
-5	1584	1507	1431	3016
-5	1541	1509	1373	3017
-5	1809	1508	1662	3018
-5	1546	1366	1545	3019
-5	1584	1431	1430	3020
-5	1509	1430	1373	3021
-5	1510	1438	1386	3022
-5	1588	1510	1386	3023
-5	1685	1379	1529	3024
-5	1556	1390	1389	3025
-5	1810	1504	1505	3026
-5	1687	1372	1512	3027
-5	1513	1512	1436	3028
-5	2136	1943	1816	3029
-5	1590	1439	1589	3030
-5	1735	1587	1525	3031
-5	1559	1080	1515	3032
-5	1689	1402	1559	3033
-5	1516	1405	1376	3034
-5	1867	1688	1723	3035
-5	1997	1852	1669	3036
-5	1506	1361	1068	3037
-5	1695	1521	1367	3038
-5	1691	1515	1393	3039
-5	1956	1695	1853	3040
-5	1951	1693	1848	3041
-5	1520	1425	1370	3042
-5	1812	1713	1743	3043
-5	1948	1817	1818	3044
-5	1578	1530	1084	3045
-5	1541	1373	1383	3046
-5	1522	1383	1486	3047
-5	1523	1450	1446	3048
-5	1594	1523	1446	3049
-5	1593	1444	1569	3050
-5	1564	1412	1400	3051
-5	1587	1435	1434	3052
-5	1588	1435	1587	3053
-5	1526	1443	1377	3054
-5	1575	1526	1377	3055
-5	1527	932	1124	3056
-5	1547	1362	1363	3057
-5	1529	1266	1528	3058
-5	1529	1379	1266	3059
-5	1941	1692	1940	3060
-5	1690	1361	1506	3061
-5	1698	1420	1530	3062
-5	1530	1420	1268	3063
-5	1553	1370	1409	3064
-5	1566	1384	1531	3065
-5	1532	1427	1398	3066
-5	1614	1535	1429	3067
-5	1563	1399	1452	3068
-5	1574	1418	1399	3069
-5	1626	1540	1481	3070
-5	1643	1497	1388	3071
-5	1535	1532	1398	3072
-5	1535	1398	1429	3073
-5	1583	1396	1561	3074
-5	1642	1496	1495	3075
-5	1751	1604	1750	3076
-5	1901	1756	1900	3077
-5	1700	1538	1549	3078
-5	1639	1493	1492	3079
-5	1539	1476	1382	3080
-5	1637	1382	1491	3081
-5	1626	1480	1625	3082
-5	1644	1498	1497	3083
-5	1774	1628	1773	3084
-5	1909	1765	1908	3085
-5	1560	1376	1453	3086
-5	1570	1394	1542	3087
-5	1703	1543	1540	3088
-5	1788	1643	1543	3089
-5	1809	1364	1544	3090
-5	1544	1364	849	3091
-5	1858	1710	1709	3092
-5	1545	1366	1264	3093
-5	1817	1704	1705	3094
-5	1818	1366	1546	3095
-5	1527	1124	1372	3096
-5	1819	1521	1695	3097
-5	1567	1411	1375	3098
-5	1579	1411	1567	3099
-5	1549	1538	1378	3100
-5	1549	1378	1494	3101
-5	1853	1550	1697	3102
-5	1691	1393	1521	3103
-5	1551	1550	1265	3104
-5	1551	1265	1406	3105
-5	1557	1391	1381	3106
-5	1596	1447	1595	3107
-5	1741	1594	1593	3108
-5	1659	1552	1520	3109
-5	1554	1534	1385	3110
-5	1554	1385	1440	3111
-5	1735	1525	1680	3112
-5	1910	1820	1734	3113
-5	1944	1910	1912	3114
-5	1799	1573	1722	3115
-5	2023	1875	1874	3116
-5	1850	1694	1708	3117
-5	1712	1557	1711	3118
-5	1711	1557	1552	3119
-5	1660	1559	1515	3120
-5	1691	1660	1515	3121
-5	1600	1414	1570	3122
-5	1656	1516	1560	3123
-5	1583	1426	1396	3124
-5	1641	1495	1426	3125
-5	1824	1766	1782	3126
-5	1900	1755	1899	3127
-5	1770	1626	1625	3128
-5	1574	1399	1563	3129
-5	1822	1567	1721	3130
-5	1729	1580	1579	3131
-5	1680	1525	1586	3132
-5	1736	1588	1587	3133
-5	1566	1553	1409	3134
-5	1566	1409	1384	3135
-5	1720	1569	1568	3136
-5	1718	1564	1524	3137
-5	1719	1564	1718	3138
-5	1594	1446	1445	3139
-5	1742	1523	1594	3140
-5	1712	1558	1557	3141
-5	1600	1453	1414	3142
-5	1600	1560	1453	3143
-5	1577	1375	1229	3144
-5	1701	1522	1681	3145
-5	1822	1728	1567	3146
-5	1576	1419	1572	3147
-5	1688	1436	1417	3148
-5	1826	1436	1688	3149
-5	1797	1744	1597	3150
-5	1575	1418	1574	3151
-5	1675	1672	1534	3152
-5	1882	1737	1736	3153
-5	1576	1572	1403	3154
-5	1576	1403	1221	3155
-5	1727	1419	1576	3156
-5	1667	1571	1374	3157
-5	1945	1668	1547	3158
-5	1668	1362	1547	3159
-5	1775	1630	1629	3160
-5	1720	1568	1719	3161
-5	1887	1712	1711	3162
-5	1581	1531	1369	3163
-5	1713	1524	1596	3164
-5	1670	1531	1654	3165
-5	1601	1454	1424	3166
-5	1638	1492	1455	3167
-5	1807	1746	1570	3168
-5	2072	1927	1876	3169
-5	1727	1576	1663	3170
-5	1729	1579	1728	3171
-5	1623	1442	1591	3172
-5	1624	1585	1432	3173
-5	1820	1680	1734	3174
-5	1930	1790	1789	3175
-5	1829	1674	1742	3176
-5	1716	1563	1533	3177
-5	1830	1722	1565	3178
-5	1717	1556	1710	3179
-5	1590	1416	1439	3180
-5	1589	1439	1438	3181
-5	1709	1555	1514	3182
-5	1880	1735	1680	3183
-5	1623	1479	1442	3184
-5	1624	1479	1623	3185
-5	1592	1591	1441	3186
-5	1592	1441	1478	3187
-5	1932	1792	1839	3188
-5	1594	1445	1593	3189
-5	1793	1646	1792	3190
-5	1745	1675	1554	3191
-5	2012	1863	1958	3192
-5	1596	1524	1365	3193
-5	1741	1593	1740	3194
-5	2078	1933	1932	3195
-5	1598	1440	1449	3196
-5	1597	1449	1448	3197
-5	1890	1675	1745	3198
-5	1724	1563	1716	3199
-5	1646	1499	1451	3200
-5	1649	1501	1648	3201
-5	1876	1676	1800	3202
-5	1891	1833	1747	3203
-5	1748	1582	1678	3204
-5	1602	1454	1601	3205
-5	1784	1639	1638	3206
-5	1638	1455	1602	3207
-5	1603	1537	1458	3208
-5	1603	1458	1457	3209
-5	1677	1536	1661	3210
-5	1612	1468	1467	3211
-5	1759	1613	1612	3212
-5	1753	1606	1752	3213
-5	1758	1612	1611	3214
-5	1609	1464	1608	3215
-5	1677	1603	1536	3216
-5	1610	1465	1609	3217
-5	1755	1608	1754	3218
-5	1613	1468	1612	3219
-5	1785	1639	1784	3220
-5	1749	1602	1601	3221
-5	1761	1683	1535	3222
-5	1611	1466	1610	3223
-5	1759	1612	1758	3224
-5	1614	1469	1613	3225
-5	1755	1609	1608	3226
-5	1614	1429	1469	3227
-5	1699	1537	1603	3228
-5	1841	1657	1785	3229
-5	1904	1760	1759	3230
-5	1678	1582	1532	3231
-5	1619	1616	1473	3232
-5	1620	1475	1617	3233
-5	1619	1472	1618	3234
-5	1632	1456	1620	3235
-5	1781	1637	1636	3236
-5	1632	1487	1456	3237
-5	1619	1473	1472	3238
-5	1618	1472	1471	3239
-5	1753	1607	1606	3240
-5	1715	1517	1562	3241
-5	1777	1620	1765	3242
-5	1682	1615	1679	3243
-5	1775	1629	1774	3244
-5	1631	1522	1486	3245
-5	1622	1592	1478	3246
-5	1622	1478	1443	3247
-5	1767	1623	1591	3248
-5	1769	1585	1624	3249
-5	1768	1624	1623	3250
-5	1989	1723	1799	3251
-5	1626	1481	1480	3252
-5	1625	1480	1437	3253
-5	1937	1889	1744	3254
-5	1725	1574	1724	3255
-5	1702	1541	1701	3256
-5	1629	1484	1483	3257
-5	1681	1522	1631	3258
-5	1921	1781	1780	3259
-5	1776	1631	1630	3260
-5	1778	1632	1777	3261
-5	1772	1621	1766	3262
-5	1631	1485	1630	3263
-5	1879	1651	1733	3264
-5	1732	1509	1702	3265
-5	1773	1628	1627	3266
-5	1635	1489	1634	3267
-5	1682	1618	1615	3268
-5	1765	1620	1617	3269
-5	2099	1995	1957	3270
-5	1637	1491	1636	3271
-5	1772	1627	1621	3272
-5	1637	1539	1382	3273
-5	1779	1635	1634	3274
-5	1781	1636	1780	3275
-5	1765	1617	1762	3276
-5	1777	1632	1620	3277
-5	1908	1765	1762	3278
-5	1639	1492	1638	3279
-5	1679	1615	1517	3280
-5	1640	1549	1494	3281
-5	1763	1618	1682	3282
-5	1700	1549	1657	3283
-5	1661	1536	1642	3284
-5	1642	1495	1641	3285
-5	1699	1603	1677	3286
-5	1787	1661	1642	3287
-5	1934	1794	1933	3288
-5	1644	1497	1643	3289
-5	1724	1574	1563	3290
-5	1645	1498	1644	3291
-5	1832	1771	1770	3292
-5	1726	1575	1725	3293
-5	1792	1599	1674	3294
-5	1796	1649	1795	3295
-5	1797	1650	1796	3296
-5	1650	1502	1649	3297
-5	1931	1791	1790	3298
-5	1650	1597	1448	3299
-5	1675	1534	1554	3300
-5	1711	1552	1659	3301
-5	1719	1568	1564	3302
-5	1796	1650	1649	3303
-5	1651	1548	1507	3304
-5	1733	1651	1507	3305
-5	1665	1547	1363	3306
-5	1652	1363	853	3307
-5	1653	1570	1542	3308
-5	2093	1857	1983	3309
-5	1730	1581	1580	3310
-5	1728	1579	1567	3311
-5	1655	1546	1545	3312
-5	1655	1545	1361	3313
-5	1747	1600	1746	3314
-5	1747	1560	1600	3315
-5	1860	1700	1806	3316
-5	1785	1640	1639	3317
-5	1726	1671	1526	3318
-5	1725	1575	1574	3319
-5	1855	1701	1681	3320
-5	1694	1520	1553	3321
-5	1684	1401	1503	3322
-5	2127	1997	1977	3323
-5	1731	1561	1676	3324
-5	1787	1642	1641	3325
-5	1662	1508	886	3326
-5	1662	886	1401	3327
-5	1802	1571	1667	3328
-5	1663	1576	1415	3329
-5	1811	1696	1511	3330
-5	1707	1529	1528	3331
-5	1810	1505	1371	3332
-5	1810	1371	1686	3333
-5	1666	1658	1592	3334
-5	1666	1592	1622	3335
-5	1845	1727	1663	3336
-5	1721	1567	1375	3337
-5	1808	1519	1692	3338
-5	1693	1530	1578	3339
-5	1690	1655	1361	3340
-5	1950	1687	1513	3341
-5	1694	1659	1520	3342
-5	1708	1566	1670	3343
-5	1671	1666	1622	3344
-5	1671	1622	1526	3345
-5	1672	1625	1534	3346
-5	1836	1788	1703	3347
-5	1673	1589	1510	3348
-5	1737	1673	1510	3349
-5	1674	1599	1523	3350
-5	1742	1674	1523	3351
-5	1745	1598	1744	3352
-5	1795	1649	1648	3353
-5	1731	1583	1561	3354
-5	1786	1641	1583	3355
-5	1897	1752	1896	3356
-5	1899	1754	1898	3357
-5	1748	1601	1582	3358
-5	1783	1638	1602	3359
-5	1714	1538	1700	3360
-5	1715	1679	1517	3361
-5	1737	1588	1736	3362
-5	1736	1587	1735	3363
-5	1701	1541	1522	3364
-5	1733	1584	1732	3365
-5	1903	1759	1758	3366
-5	1897	1753	1752	3367
-5	1683	1678	1532	3368
-5	1683	1532	1535	3369
-5	2152	1977	1809	3370
-5	1809	1544	1508	3371
-5	1692	1519	1518	3372
-5	1951	1854	1693	3373
-5	1798	1692	1518	3374
-5	1945	1848	1668	3375
-5	1706	1664	1368	3376
-5	2157	1867	1989	3377
-5	1717	1565	1556	3378
-5	1710	1556	1555	3379
-5	2003	1844	1660	3380
-5	1689	1503	1402	3381
-5	1690	1506	1379	3382
-5	1690	1379	1685	3383
-5	1698	1511	1420	3384
-5	1695	1367	1550	3385
-5	1808	1686	1519	3386
-5	1954	1685	1813	3387
-5	1696	1551	1406	3388
-5	1696	1406	1511	3389
-5	1955	1842	1873	3390
-5	2026	1651	1879	3391
-5	1819	1691	1521	3392
-5	1851	1691	1819	3393
-5	1811	1511	1698	3394
-5	1852	1528	1669	3395
-5	2004	1697	1814	3396
-5	1697	1550	1551	3397
-5	1698	1530	1693	3398
-5	1814	1697	1551	3399
-5	1750	1604	1537	3400
-5	1752	1605	1751	3401
-5	1714	1562	1538	3402
-5	1715	1562	1714	3403
-5	1733	1507	1584	3404
-5	1732	1584	1509	3405
-5	1856	1701	1855	3406
-5	1917	1774	1916	3407
-5	1771	1626	1770	3408
-5	1871	1671	1726	3409
-5	1857	1653	1542	3410
-5	1704	1542	1395	3411
-5	1705	1704	1395	3412
-5	1705	1395	1366	3413
-5	1706	1527	1372	3414
-5	1706	1372	1687	3415
-5	1798	1518	1664	3416
-5	1813	1685	1529	3417
-5	1708	1694	1553	3418
-5	1708	1553	1566	3419
-5	1739	1590	1738	3420
-5	1739	1514	1590	3421
-5	1866	1717	1710	3422
-5	2087	1799	1991	3423
-5	1743	1595	1712	3424
-5	1718	1524	1713	3425
-5	1932	1793	1792	3426
-5	1712	1595	1558	3427
-5	1743	1596	1595	3428
-5	1865	1719	1864	3429
-5	2056	1909	1908	3430
-5	1908	1762	1838	3431
-5	1861	1714	1860	3432
-5	2053	1906	1905	3433
-5	1789	1643	1788	3434
-5	1790	1645	1644	3435
-5	1799	1723	1573	3436
-5	1723	1417	1573	3437
-5	2034	1865	2013	3438
-5	1740	1593	1569	3439
-5	1913	1703	1771	3440
-5	1740	1569	1720	3441
-5	2196	2050	2195	3442
-5	1885	1720	1865	3443
-5	1801	1548	1651	3444
-5	2007	1855	2006	3445
-5	2015	1858	2014	3446
-5	1813	1529	1707	3447
-5	2088	1513	2016	3448
-5	1867	1826	1688	3449
-5	1868	1724	1716	3450
-5	1726	1526	1575	3451
-5	2032	1884	1835	3452
-5	2030	1882	2029	3453
-5	1870	1726	1725	3454
-5	1871	1828	1671	3455
-5	1998	1802	1972	3456
-5	1727	1577	1419	3457
-5	1873	1842	1654	3458
-5	1730	1580	1729	3459
-5	1823	1659	1694	3460
-5	1730	1654	1581	3461
-5	2002	1843	2001	3462
-5	2160	2001	2089	3463
-5	1902	1757	1901	3464
-5	1846	1677	1661	3465
-5	1877	1732	1702	3466
-5	2025	1878	1877	3467
-5	1855	1681	1837	3468
-5	1845	1663	1802	3469
-5	1734	1680	1586	3470
-5	1734	1586	1585	3471
-5	2028	1880	1964	3472
-5	1737	1510	1588	3473
-5	1884	1739	1738	3474
-5	1883	1835	1673	3475
-5	1880	1680	1820	3476
-5	1821	1767	1658	3477
-5	1739	1709	1514	3478
-5	1738	1590	1589	3479
-5	1858	1709	1803	3480
-5	1830	1565	1717	3481
-5	1831	1711	1659	3482
-5	1831	1659	1823	3483
-5	1874	1729	1728	3484
-5	1742	1594	1741	3485
-5	1839	1674	1829	3486
-5	1743	1713	1596	3487
-5	1935	1795	1934	3488
-5	1863	1713	1812	3489
-5	1745	1554	1598	3490
-5	1744	1598	1597	3491
-5	1839	1792	1674	3492
-5	1933	1793	1932	3493
-5	1747	1656	1560	3494
-5	1896	1751	1895	3495
-5	2016	1513	1826	3496
-5	1928	1827	1787	3497
-5	1896	1752	1751	3498
-5	1749	1601	1748	3499
-5	2071	1926	1925	3500
-5	1783	1602	1749	3501
-5	1895	1750	1894	3502
-5	1898	1754	1753	3503
-5	1894	1699	1815	3504
-5	1754	1608	1607	3505
-5	1895	1751	1750	3506
-5	1756	1610	1609	3507
-5	2240	1866	2100	3508
-5	1846	1661	1827	3509
-5	1927	1731	1876	3510
-5	1757	1610	1756	3511
-5	1928	1787	1786	3512
-5	1760	1613	1759	3513
-5	1892	1748	1678	3514
-5	1924	1783	1749	3515
-5	1834	1678	1683	3516
-5	1758	1611	1757	3517
-5	1905	1761	1760	3518
-5	1761	1614	1760	3519
-5	1902	1758	1757	3520
-5	1761	1535	1614	3521
-5	1898	1753	1897	3522
-5	1894	1750	1699	3523
-5	2090	2040	1962	3524
-5	1841	1806	1657	3525
-5	1764	1619	1763	3526
-5	1764	1616	1619	3527
-5	1764	1762	1616	3528
-5	1763	1619	1618	3529
-5	1906	1834	1683	3530
-5	2009	1860	1963	3531
-5	1838	1762	1764	3532
-5	1779	1634	1633	3533
-5	1766	1621	1539	3534
-5	1782	1637	1781	3535
-5	1964	1880	1820	3536
-5	1769	1624	1768	3537
-5	2170	2020	2169	3538
-5	1769	1734	1585	3539
-5	1805	1658	1666	3540
-5	1821	1658	1805	3541
-5	1771	1540	1626	3542
-5	1771	1703	1540	3543
-5	1966	1840	1890	3544
-5	1937	1797	1936	3545
-5	1918	1775	1917	3546
-5	1914	1766	1824	3547
-5	1856	1702	1701	3548
-5	1776	1630	1775	3549
-5	2063	1918	2062	3550
-5	2059	1915	1914	3551
-5	2197	2052	2051	3552
-5	1776	1681	1631	3553
-5	2064	1968	1919	3554
-5	1919	1777	1909	3555
-5	1778	1633	1632	3556
-5	1779	1633	1778	3557
-5	1922	1778	1919	3558
-5	1837	1681	1776	3559
-5	1782	1766	1539	3560
-5	1780	1635	1779	3561
-5	1918	1837	1776	3562
-5	1782	1539	1637	3563
-5	1907	1763	1825	3564
-5	2059	1914	1967	3565
-5	1878	1732	1877	3566
-5	1914	1772	1766	3567
-5	1926	1785	1784	3568
-5	1784	1638	1783	3569
-5	1825	1763	1682	3570
-5	1785	1657	1640	3571
-5	1862	1847	1679	3572
-5	1920	1780	1779	3573
-5	2072	1876	1946	3574
-5	1787	1641	1786	3575
-5	2093	2008	1857	3576
-5	2133	1983	1817	3577
-5	1789	1644	1643	3578
-5	1791	1533	1645	3579
-5	1869	1724	1868	3580
-5	1790	1644	1789	3581
-5	1911	1767	1821	3582
-5	1791	1716	1533	3583
-5	1884	1738	1835	3584
-5	1868	1716	1804	3585
-5	1793	1647	1646	3586
-5	1794	1648	1647	3587
-5	1929	1788	1836	3588
-5	1832	1672	1840	3589
-5	1864	1718	1863	3590
-5	1795	1648	1794	3591
-5	2082	1937	1936	3592
-5	1797	1597	1650	3593
-5	2081	1936	1935	3594
-5	1865	1720	1719	3595
-5	1863	1718	1713	3596
-5	1840	1672	1675	3597
-5	1954	1690	1685	3598
-5	1816	1655	1690	3599
-5	1866	1710	1858	3600
-5	1835	1738	1673	3601
-5	1800	1676	1656	3602
-5	2193	2047	2192	3603
-5	1873	1654	1730	3604
-5	2174	2027	2025	3605
-5	1972	1802	1667	3606
-5	2095	1969	2036	3607
-5	1884	1803	1739	3608
-5	2033	2014	1803	3609
-5	2228	2101	2110	3610
-5	1929	1789	1788	3611
-5	1985	1821	1960	3612
-5	2096	1944	1959	3613
-5	1806	1700	1657	3614
-5	1988	1957	1825	3615
-5	1891	1747	1746	3616
-5	2074	1827	1928	3617
-5	1854	1698	1693	3618
-5	1854	1811	1698	3619
-5	1977	1669	1809	3620
-5	1809	1669	1364	3621
-5	1978	1810	1686	3622
-5	2147	1810	1978	3623
-5	1942	1811	1854	3624
-5	1979	1696	1811	3625
-5	1888	1743	1712	3626
-5	1842	1670	1654	3627
-5	2128	1814	1979	3628
-5	1853	1695	1550	3629
-5	2416	2244	2415	3630
-5	1982	1547	1665	3631
-5	1815	1699	1677	3632
-5	1827	1661	1787	3633
-5	1952	1686	1808	3634
-5	1984	1503	1939	3635
-5	2084	1717	1866	3636
-5	1857	1542	1704	3637
-5	1818	1817	1705	3638
-5	1818	1705	1366	3639
-5	1939	1689	1844	3640
-5	1844	1559	1660	3641
-5	2316	2175	2121	3642
-5	1911	1768	1767	3643
-5	1910	1734	1769	3644
-5	2169	2019	2168	3645
-5	1879	1733	1878	3646
-5	1998	1845	1802	3647
-5	1888	1712	1887	3648
-5	1887	1711	1831	3649
-5	1923	1782	1781	3650
-5	1923	1781	1921	3651
-5	1995	1907	1957	3652
-5	2345	2207	2206	3653
-5	1989	1867	1723	3654
-5	1826	1513	1436	3655
-5	1846	1815	1677	3656
-5	1990	1815	1846	3657
-5	1828	1805	1666	3658
-5	1828	1666	1671	3659
-5	1886	1741	1740	3660
-5	1885	1740	1720	3661
-5	2084	1830	1717	3662
-5	1991	1722	1830	3663
-5	2301	2155	2173	3664
-5	2026	1801	1651	3665
-5	2168	2018	2091	3666
-5	1931	1790	1930	3667
-5	1833	1800	1656	3668
-5	1833	1656	1747	3669
-5	2050	1902	2049	3670
-5	1892	1678	1834	3671
-5	1881	1735	1880	3672
-5	1881	1736	1735	3673
-5	1832	1770	1672	3674
-5	1974	1965	1804	3675
-5	1915	1772	1914	3676
-5	1916	1774	1773	3677
-5	2068	1921	2065	3678
-5	1909	1777	1765	3679
-5	1936	1797	1796	3680
-5	2078	1932	1938	3681
-5	1890	1745	1889	3682
-5	1935	1796	1795	3683
-5	1893	1748	1892	3684
-5	1925	1784	1783	3685
-5	1843	1708	1670	3686
-5	1850	1823	1694	3687
-5	2037	1887	1831	3688
-5	1850	1708	1843	3689
-5	2131	1854	1951	3690
-5	1939	1503	1689	3691
-5	1987	1874	1728	3692
-5	1872	1577	1727	3693
-5	2044	1897	1896	3694
-5	2047	1900	1899	3695
-5	1847	1825	1682	3696
-5	1847	1682	1679	3697
-5	1848	1693	1578	3698
-5	1848	1578	1668	3699
-5	2041	1815	1990	3700
-5	2295	2148	1980	3701
-5	2182	2035	2181	3702
-5	2001	1842	1955	3703
-5	2305	2127	2152	3704
-5	1851	1660	1691	3705
-5	1979	1811	1942	3706
-5	1979	1814	1696	3707
-5	2104	1956	1853	3708
-5	2105	1851	2005	3709
-5	1941	1808	1692	3710
-5	1943	1655	1816	3711
-5	1972	1667	1801	3712
-5	1877	1702	1856	3713
-5	2371	2265	2425	3714
-5	2025	1877	1961	3715
-5	2151	1746	1807	3716
-5	2106	1971	1891	3717
-5	1940	1692	1798	3718
-5	2270	1989	2087	3719
-5	1859	1829	1742	3720
-5	1859	1742	1741	3721
-5	1861	1715	1714	3722
-5	1862	1679	1715	3723
-5	2069	1893	2040	3724
-5	1862	1715	1861	3725
-5	2165	2163	2011	3726
-5	2349	2123	2236	3727
-5	1864	1719	1718	3728
-5	1886	1740	1885	3729
-5	2287	2160	2286	3730
-5	1969	1829	1859	3731
-5	2114	2078	1938	3732
-5	1886	1859	1741	3733
-5	2031	1835	1883	3734
-5	2015	1866	1858	3735
-5	2135	1953	2086	3736
-5	1950	1849	1687	3737
-5	1869	1725	1724	3738
-5	1870	1725	1869	3739
-5	2225	2080	2224	3740
-5	2020	1871	1870	3741
-5	2175	2028	2121	3742
-5	1871	1726	1870	3743
-5	1975	1960	1805	3744
-5	2058	1993	1913	3745
-5	2022	1872	1999	3746
-5	1872	1721	1577	3747
-5	1875	1729	1874	3748
-5	2116	2012	1958	3749
-5	1875	1730	1729	3750
-5	1875	1873	1730	3751
-5	1992	1831	1823	3752
-5	2001	1843	1842	3753
-5	1927	1786	1731	3754
-5	1928	1786	1927	3755
-5	1878	1733	1732	3756
-5	1999	1872	1845	3757
-5	2006	1855	1837	3758
-5	2234	1987	2145	3759
-5	2055	1838	1995	3760
-5	1987	1728	1822	3761
-5	1883	1737	1882	3762
-5	1882	1736	1881	3763
-5	1974	1804	1931	3764
-5	1883	1673	1737	3765
-5	2299	2154	2153	3766
-5	2360	2223	2282	3767
-5	1975	1805	1828	3768
-5	1986	1910	1944	3769
-5	2141	1986	2098	3770
-5	2029	1882	1881	3771
-5	2108	1958	1973	3772
-5	2012	1864	1863	3773
-5	2204	2058	2203	3774
-5	2222	2077	2076	3775
-5	1995	1838	1907	3776
-5	1888	1812	1743	3777
-5	2160	2002	2001	3778
-5	2116	1958	2108	3779
-5	1890	1840	1675	3780
-5	1889	1745	1744	3781
-5	2076	1929	2075	3782
-5	1993	1836	1913	3783
-5	2179	2033	2113	3784
-5	2245	2151	2008	3785
-5	1893	1749	1748	3786
-5	1926	1784	1925	3787
-5	1988	1825	1847	3788
-5	1924	1749	1893	3789
-5	2043	1895	2042	3790
-5	2042	1894	2041	3791
-5	2049	1901	2048	3792
-5	1900	1756	1755	3793
-5	2047	1899	2046	3794
-5	2073	1927	2072	3795
-5	2119	1990	2000	3796
-5	1901	1757	1756	3797
-5	2073	1928	1927	3798
-5	1905	1760	1904	3799
-5	2041	1894	1815	3800
-5	2043	1896	1895	3801
-5	2042	1895	1894	3802
-5	1903	1758	1902	3803
-5	2052	1905	1904	3804
-5	1904	1759	1903	3805
-5	2048	1900	2047	3806
-5	2045	1897	2044	3807
-5	2045	1898	1897	3808
-5	1906	1761	1905	3809
-5	2215	2124	2071	3810
-5	1906	1683	1761	3811
-5	2192	2047	2046	3812
-5	2009	1861	1860	3813
-5	2194	2049	2048	3814
-5	2040	1892	1962	3815
-5	1907	1838	1764	3816
-5	1907	1764	1763	3817
-5	1921	1780	1920	3818
-5	1919	1778	1777	3819
-5	2011	1847	1862	3820
-5	2342	2201	2260	3821
-5	1912	1768	1911	3822
-5	2280	2015	2178	3823
-5	1912	1769	1768	3824
-5	1912	1910	1769	3825
-5	1913	1836	1703	3826
-5	1913	1771	1832	3827
-5	2018	1869	1868	3828
-5	1965	1868	1804	3829
-5	1915	1773	1772	3830
-5	1917	1775	1774	3831
-5	2122	2059	1967	3832
-5	1916	1773	1915	3833
-5	2208	2063	2062	3834
-5	1918	1776	1775	3835
-5	2007	1961	1856	3836
-5	2007	1856	1855	3837
-5	2064	1919	1909	3838
-5	2062	1917	2061	3839
-5	2050	1903	1902	3840
-5	1963	1860	1806	3841
-5	1968	1922	1919	3842
-5	2063	2006	1837	3843
-5	2211	2107	2065	3844
-5	1923	1824	1782	3845
-5	1922	1920	1779	3846
-5	1922	1779	1778	3847
-5	2066	1922	1968	3848
-5	2207	2061	2206	3849
-5	2040	1893	1892	3850
-5	1925	1783	1924	3851
-5	2213	2069	2040	3852
-5	1926	1841	1785	3853
-5	2051	1904	1903	3854
-5	2044	1896	2043	3855
-5	2046	1899	1898	3856
-5	2049	1902	1901	3857
-5	2117	1946	1970	3858
-5	2028	1881	1880	3859
-5	2079	1933	2078	3860
-5	1930	1789	1929	3861
-5	2058	1832	2057	3862
-5	1931	1804	1791	3863
-5	2057	1840	1966	3864
-5	2283	2115	2142	3865
-5	1933	1794	1793	3866
-5	1934	1795	1794	3867
-5	2238	2114	2125	3868
-5	1936	1796	1935	3869
-5	2077	1930	2076	3870
-5	2081	1935	2080	3871
-5	2035	1885	2034	3872
-5	1937	1744	1797	3873
-5	2111	2057	1966	3874
-5	2037	1831	1992	3875
-5	2036	1859	1886	3876
-5	1969	1947	1829	3877
-5	1938	1932	1839	3878
-5	2126	1969	2095	3879
-5	2146	1852	1997	3880
-5	2152	1662	1684	3881
-5	1943	1546	1655	3882
-5	2239	2085	2129	3883
-5	2245	2008	2093	3884
-5	2128	2004	1814	3885
-5	1956	1819	1695	3886
-5	2104	2005	1956	3887
-5	2129	1546	1943	3888
-5	1991	1799	1722	3889
-5	1985	1959	1911	3890
-5	2224	2079	2223	3891
-5	2131	1942	1854	3892
-5	2132	1848	1945	3893
-5	1946	1876	1800	3894
-5	1983	1857	1704	3895
-5	1947	1938	1839	3896
-5	1947	1839	1829	3897
-5	2241	2093	1983	3898
-5	1983	1704	1817	3899
-5	1949	1948	1818	3900
-5	1949	1818	1546	3901
-5	2086	1849	1950	3902
-5	1953	1706	1849	3903
-5	2293	2097	1940	3904
-5	2134	1808	1941	3905
-5	2149	1978	1952	3906
-5	1978	1686	1952	3907
-5	2135	1940	1798	3908
-5	1953	1798	1664	3909
-5	2550	2304	2380	3910
-5	1954	1816	1690	3911
-5	2024	1875	2023	3912
-5	2024	1873	1875	3913
-5	2103	1844	2003	3914
-5	2097	1941	1940	3915
-5	1957	1907	1825	3916
-5	2243	2138	2163	3917
-5	1958	1863	1812	3918
-5	2038	1888	1887	3919
-5	1959	1944	1912	3920
-5	1959	1912	1911	3921
-5	1985	1911	1821	3922
-5	1960	1821	1805	3923
-5	1961	1877	1856	3924
-5	2144	2026	1879	3925
-5	1962	1892	1834	3926
-5	2054	1962	1834	3927
-5	2199	2053	2198	3928
-5	2070	1925	1924	3929
-5	2177	2030	2176	3930
-5	2112	2032	2031	3931
-5	2021	1975	1828	3932
-5	2018	1868	1965	3933
-5	2220	1993	2204	3934
-5	2083	1937	2082	3935
-5	1967	1914	1824	3936
-5	2208	2062	2207	3937
-5	2065	1921	1920	3938
-5	2067	1824	1923	3939
-5	2013	1864	2012	3940
-5	2035	1886	1885	3941
-5	1970	1946	1800	3942
-5	1970	1800	1833	3943
-5	1971	1970	1833	3944
-5	1971	1833	1891	3945
-5	2144	1879	2027	3946
-5	2145	1987	1822	3947
-5	1973	1958	1812	3948
-5	1973	1812	1888	3949
-5	2075	1836	1993	3950
-5	2076	1930	1929	3951
-5	2019	1869	2018	3952
-5	2019	1870	1869	3953
-5	1976	1963	1806	3954
-5	1976	1806	1841	3955
-5	1997	1669	1977	3956
-5	2244	2127	2229	3957
-5	1982	1945	1547	3958
-5	2150	1945	1982	3959
-5	2005	1851	1819	3960
-5	2004	1853	1697	3961
-5	2148	2136	1954	3962
-5	1980	1813	1707	3963
-5	1981	1980	1707	3964
-5	1981	1707	1852	3965
-5	2296	2289	2149	3966
-5	2134	1952	1808	3967
-5	2379	2167	2233	3968
-5	2008	1653	1857	3969
-5	2152	1684	1984	3970
-5	1984	1684	1503	3971
-5	2220	2075	1993	3972
-5	2221	2076	2075	3973
-5	1986	1964	1820	3974
-5	1986	1820	1910	3975
-5	2185	2108	1973	3976
-5	2375	2370	2262	3977
-5	2010	1861	2009	3978
-5	2010	1862	1861	3979
-5	2217	2072	1946	3980
-5	2157	2017	1867	3981
-5	2074	1928	2073	3982
-5	2217	1946	2117	3983
-5	2113	2032	2112	3984
-5	2008	1807	1653	3985
-5	2038	1973	1888	3986
-5	2038	1887	2037	3987
-5	2075	1929	1836	3988
-5	2077	1931	1930	3989
-5	1994	1976	1841	3990
-5	1994	1841	1926	3991
-5	2055	1908	1838	3992
-5	2064	1909	2056	3993
-5	1996	1992	1823	3994
-5	1996	1823	1850	3995
-5	2103	1939	1844	3996
-5	2003	1660	1851	3997
-5	2022	1822	1721	3998
-5	1999	1845	1998	3999
-5	2172	1999	2159	4000
-5	2022	1721	1872	4001
-5	2000	1990	1846	4002
-5	2000	1846	1827	4003
-5	2002	1850	1843	4004
-5	2002	1996	1850	4005
-5	2320	2166	2310	4006
-5	2161	2102	1996	4007
-5	2128	1979	1942	4008
-5	2005	1819	1956	4009
-5	2369	1941	2097	4010
-5	2147	1652	1810	4011
-5	2105	2003	1851	4012
-5	2684	2517	2518	4013
-5	2060	1915	2059	4014
-5	2061	1917	1916	4015
-5	2212	2068	2107	4016
-5	2422	2260	2276	4017
-5	2249	2087	1991	4018
-5	2084	1991	1830	4019
-5	2202	2055	2201	4020
-5	2011	1862	2010	4021
-5	2213	2040	2090	4022
-5	2011	1988	1847	4023
-5	2092	2009	1963	4024
-5	2371	2308	2250	4025
-5	2013	1865	1864	4026
-5	2034	1885	1865	4027
-5	2185	1973	2038	4028
-5	2036	1886	2035	4029
-5	2100	1866	2015	4030
-5	2014	1858	1803	4031
-5	2033	1884	2032	4032
-5	2240	2084	1866	4033
-5	2136	1816	1954	4034
-5	2135	1798	1953	4035
-5	2017	2016	1826	4036
-5	2017	1826	1867	4037
-5	2021	1871	2020	4038
-5	2020	1870	2019	4039
-5	2154	1959	1985	4040
-5	2021	1828	1871	4041
-5	2098	1944	2096	4042
-5	2121	2028	1964	4043
-5	2450	2311	2372	4044
-5	2203	2057	2111	4045
-5	2109	1801	2026	4046
-5	2109	1972	1801	4047
-5	2027	1878	2025	4048
-5	2024	1955	1873	4049
-5	2102	1992	1996	4050
-5	2324	2184	2183	4051
-5	2314	2246	2172	4052
-5	2253	1972	2109	4053
-5	2159	1999	1998	4054
-5	2027	1879	1878	4055
-5	2166	2012	2116	4056
-5	2183	2037	1992	4057
-5	2031	1883	2030	4058
-5	2030	1883	1882	4059
-5	2153	1960	2130	4060
-5	2171	1975	2021	4061
-5	2168	2019	2018	4062
-5	2032	1835	2031	4063
-5	2098	1986	1944	4064
-5	2255	2113	2254	4065
-5	2033	1803	1884	4066
-5	2268	2141	2098	4067
-5	2176	2029	2175	4068
-5	2176	2030	2029	4069
-5	2373	2256	2283	4070
-5	2363	2226	2362	4071
-5	2273	2228	2110	4072
-5	2036	1969	1859	4073
-5	2362	2225	2361	4074
-5	2223	2078	2114	4075
-5	2156	2023	1874	4076
-5	2205	2060	2059	4077
-5	2374	2263	2350	4078
-5	2856	2731	2765	4079
-5	2039	1966	1890	4080
-5	2039	1890	1889	4081
-5	2069	1924	1893	4082
-5	2071	1925	2070	4083
-5	2188	2042	2187	4084
-5	2189	2043	2188	4085
-5	2186	1990	2119	4086
-5	2046	1898	2045	4087
-5	2190	2045	2044	4088
-5	2336	2195	2194	4089
-5	2218	2072	2217	4090
-5	2048	1901	1900	4091
-5	2186	2041	1990	4092
-5	2195	2049	2194	4093
-5	2187	2041	2186	4094
-5	2053	1905	2052	4095
-5	2187	2042	2041	4096
-5	2188	2043	2042	4097
-5	2190	2044	2189	4098
-5	2051	1903	2050	4099
-5	2199	2054	2053	4100
-5	2052	1904	2051	4101
-5	2198	2052	2197	4102
-5	2192	2046	2191	4103
-5	2189	2044	2043	4104
-5	2054	1906	2053	4105
-5	2196	2051	2050	4106
-5	2054	1834	1906	4107
-5	2140	2092	1963	4108
-5	2352	2213	2351	4109
-5	2164	2009	2092	4110
-5	2164	2010	2009	4111
-5	2210	2064	2056	4112
-5	2056	1908	2055	4113
-5	2236	2123	2200	4114
-5	2165	2010	2164	4115
-5	2058	1913	1832	4116
-5	2057	1832	1840	4117
-5	2115	1966	2039	4118
-5	2223	2079	2078	4119
-5	2060	1916	1915	4120
-5	2063	1837	1918	4121
-5	2062	1918	1917	4122
-5	2061	1916	2060	4123
-5	2303	2094	2262	4124
-5	2346	2207	2345	4125
-5	2285	2143	2261	4126
-5	2139	1961	2007	4127
-5	2139	2094	1961	4128
-5	2205	2059	2122	4129
-5	2201	1995	2099	4130
-5	2206	2060	2205	4131
-5	2285	2122	2143	4132
-5	2067	1967	1824	4133
-5	2066	2065	1920	4134
-5	2066	1920	1922	4135
-5	2107	2068	2065	4136
-5	2201	2055	1995	4137
-5	2068	2067	1923	4138
-5	2068	1923	1921	4139
-5	2090	2054	2199	4140
-5	2070	1924	2069	4141
-5	2419	2144	2315	4142
-5	2071	1994	1926	4143
-5	2448	2308	2371	4144
-5	2475	2336	2474	4145
-5	2191	2045	2190	4146
-5	2074	2000	1827	4147
-5	2219	2073	2218	4148
-5	2266	1971	2106	4149
-5	2331	2189	2330	4150
-5	2194	2048	2193	4151
-5	2299	2153	2298	4152
-5	2627	2494	2502	4153
-5	2171	2130	1975	4154
-5	2077	1974	1931	4155
-5	2377	2274	2300	4156
-5	2298	2153	2130	4157
-5	2079	1934	1933	4158
-5	2080	1935	1934	4159
-5	2180	2034	2013	4160
-5	2083	1889	1937	4161
-5	2183	1992	2102	4162
-5	2166	2013	2012	4163
-5	2115	2111	1966	4164
-5	2082	1936	2081	4165
-5	2227	2142	2083	4166
-5	2083	2039	1889	4167
-5	2343	2203	2111	4168
-5	2226	2081	2225	4169
-5	2085	1948	1949	4170
-5	2086	1953	1849	4171
-5	2270	2157	1989	4172
-5	2087	1989	1799	4173
-5	2167	2088	2016	4174
-5	2369	2134	1941	4175
-5	2151	1807	2008	4176
-5	2133	1817	1948	4177
-5	2386	2135	2086	4178
-5	2088	1950	1513	4179
-5	2089	2001	1955	4180
-5	2155	2089	1955	4181
-5	2330	2188	2329	4182
-5	2337	2196	2195	4183
-5	2091	2018	1965	4184
-5	2237	2130	2171	4185
-5	2140	1976	2120	4186
-5	2215	2071	2070	4187
-5	2271	2086	1950	4188
-5	2429	2271	2304	4189
-5	2094	2025	1961	4190
-5	2478	2272	2339	4191
-5	2182	2036	2035	4192
-5	2181	2035	2034	4193
-5	2154	2096	1959	4194
-5	2130	1960	1975	4195
-5	2167	2016	2017	4196
-5	2148	1813	1980	4197
-5	2275	2141	2268	4198
-5	2496	2361	2360	4199
-5	2696	2564	2520	4200
-5	2341	2200	2210	4201
-5	2178	2015	2014	4202
-5	2555	2432	2280	4203
-5	2101	2091	1965	4204
-5	2101	1965	1974	4205
-5	2161	2002	2160	4206
-5	2324	2183	2251	4207
-5	2388	2148	2295	4208
-5	2278	2003	2105	4209
-5	2384	2105	2277	4210
-5	2104	1853	2004	4211
-5	2152	1809	1662	4212
-5	2158	1939	2103	4213
-5	2113	2033	2032	4214
-5	2279	2119	2216	4215
-5	2211	2066	2123	4216
-5	2202	2056	2055	4217
-5	2184	2037	2183	4218
-5	2306	2102	2161	4219
-5	2314	2159	2253	4220
-5	2145	1822	2022	4221
-5	2110	2101	1974	4222
-5	2110	1974	2077	4223
-5	2203	2058	2057	4224
-5	2204	1993	2058	4225
-5	2280	2100	2015	4226
-5	2318	2254	2112	4227
-5	2255	2179	2113	4228
-5	2266	2118	1971	4229
-5	2226	2082	2081	4230
-5	2282	2114	2238	4231
-5	2273	2110	2222	4232
-5	2256	2111	2115	4233
-5	2180	2013	2166	4234
-5	2181	2034	2180	4235
-5	2317	2175	2316	4236
-5	2457	2319	2385	4237
-5	2118	2117	1970	4238
-5	2118	1970	1971	4239
-5	2219	2074	2073	4240
-5	2334	2193	2192	4241
-5	2140	1963	1976	4242
-5	2120	1976	1994	4243
-5	2175	2029	2028	4244
-5	2177	2031	2030	4245
-5	2462	2324	2398	4246
-5	2345	2205	2230	4247
-5	2211	2065	2066	4248
-5	2123	2066	1968	4249
-5	2124	2120	1994	4250
-5	2124	1994	2071	4251
-5	2125	2114	1938	4252
-5	2125	1938	1947	4253
-5	2126	2125	1947	4254
-5	2126	1947	1969	4255
-5	2303	2174	2094	4256
-5	2383	2277	2104	4257
-5	2296	2149	2290	4258
-5	2277	2005	2104	4259
-5	2129	2085	1949	4260
-5	2129	1949	1546	4261
-5	2153	1985	1960	4262
-5	2154	1985	2153	4263
-5	2289	2147	2149	4264
-5	2290	2149	1952	4265
-5	2291	2131	1951	4266
-5	2132	1951	1848	4267
-5	2292	2133	1948	4268
-5	2249	1991	2084	4269
-5	2150	2132	1945	4270
-5	2149	2147	1978	4271
-5	2386	2086	2378	4272
-5	2417	2383	2247	4273
-5	2518	2388	2295	4274
-5	2504	2408	2409	4275
-5	2148	1954	1813	4276
-5	2137	1980	1981	4277
-5	2138	2099	1957	4278
-5	2138	1957	1988	4279
-5	2209	2006	2063	4280
-5	2207	2062	2061	4281
-5	2338	2197	2196	4282
-5	2340	2199	2272	4283
-5	2141	2121	1964	4284
-5	2141	1964	1986	4285
-5	2142	2115	2039	4286
-5	2142	2039	2083	4287
-5	2143	2122	1967	4288
-5	2143	1967	2067	4289
-5	2174	2025	2094	4290
-5	2155	1955	2024	4291
-5	2156	1874	1987	4292
-5	2172	2022	1999	4293
-5	2416	2137	1981	4294
-5	2146	1981	1852	4295
-5	2147	1982	1665	4296
-5	2147	1665	1652	4297
-5	2295	1980	2137	4298
-5	2652	2544	2387	4299
-5	2417	2248	2391	4300
-5	2247	2104	2004	4301
-5	2391	2248	2128	4302
-5	2291	1951	2132	4303
-5	2297	1891	2151	4304
-5	2151	1891	1746	4305
-5	2158	1984	1939	4306
-5	2152	2127	1977	4307
-5	2267	2101	2228	4308
-5	2317	2176	2175	4309
-5	2298	2130	2237	4310
-5	2311	2169	2168	4311
-5	2368	2258	2156	4312
-5	2262	2094	2139	4313
-5	2345	2206	2205	4314
-5	2234	2156	1987	4315
-5	2242	1943	2136	4316
-5	2271	1950	2088	4317
-5	2305	1984	2158	4318
-5	2305	2152	1984	4319
-5	2172	2145	2022	4320
-5	2723	2453	2540	4321
-5	2161	1996	2002	4322
-5	2320	2180	2166	4323
-5	2277	2105	2005	4324
-5	2288	2128	1942	4325
-5	2162	2139	2007	4326
-5	2162	2007	2006	4327
-5	2163	2138	1988	4328
-5	2163	1988	2011	4329
-5	2165	2011	2010	4330
-5	2422	2276	2394	4331
-5	2335	2193	2334	4332
-5	2307	2163	2165	4333
-5	2310	2116	2309	4334
-5	2449	2322	2320	4335
-5	2438	2241	2133	4336
-5	2292	1948	2085	4337
-5	2169	2020	2019	4338
-5	2170	2021	2020	4339
-5	2644	2585	2511	4340
-5	2316	2121	2275	4341
-5	2358	2221	2220	4342
-5	2171	2021	2170	4343
-5	2358	2220	2357	4344
-5	2360	2224	2223	4345
-5	2314	2172	2159	4346
-5	2252	2026	2144	4347
-5	2173	2155	2024	4348
-5	2173	2024	2023	4349
-5	2258	2023	2156	4350
-5	2433	2261	2423	4351
-5	2411	2228	2273	4352
-5	2443	2298	2396	4353
-5	2318	2112	2177	4354
-5	2275	2121	2141	4355
-5	2319	2176	2317	4356
-5	2177	2112	2031	4357
-5	2284	2179	2255	4358
-5	2505	2266	2397	4359
-5	2179	2178	2014	4360
-5	2179	2014	2033	4361
-5	2326	2108	2185	4362
-5	2364	2283	2142	4363
-5	2418	2398	2251	4364
-5	2182	2095	2036	4365
-5	2322	2180	2320	4366
-5	2325	2184	2324	4367
-5	2184	2038	2037	4368
-5	2185	2038	2184	4369
-5	2462	2325	2324	4370
-5	2309	2116	2108	4371
-5	2326	2309	2108	4372
-5	2446	2286	2435	4373
-5	2330	2189	2188	4374
-5	2329	2187	2328	4375
-5	2475	2337	2336	4376
-5	2193	2048	2047	4377
-5	2430	2275	2268	4378
-5	2441	2397	2106	4379
-5	2327	2186	2119	4380
-5	2191	2046	2045	4381
-5	2336	2194	2335	4382
-5	2334	2192	2333	4383
-5	2328	2187	2186	4384
-5	2329	2188	2187	4385
-5	2331	2190	2189	4386
-5	2197	2051	2196	4387
-5	2351	2090	2340	4388
-5	2195	2050	2049	4389
-5	2272	2199	2198	4390
-5	2339	2198	2197	4391
-5	2339	2197	2338	4392
-5	2198	2053	2052	4393
-5	2337	2195	2336	4394
-5	2332	2191	2190	4395
-5	2352	2214	2213	4396
-5	2090	1962	2054	4397
-5	2404	2259	2376	4398
-5	2214	2070	2069	4399
-5	2484	2403	2341	4400
-5	2250	2164	2092	4401
-5	2200	2123	1968	4402
-5	2200	1968	2064	4403
-5	2260	2201	2099	4404
-5	2210	2056	2202	4405
-5	2341	2236	2200	4406
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-5	2221	2075	2220	4409
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-5	2216	2119	2000	4434
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-5	2359	2222	2221	4458
-5	2555	2178	2284	4459
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-5	2232	2162	2209	4467
-5	2233	2167	2017	4468
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-5	2585	2450	2511	4472
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-5	2432	2366	2100	4544
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-5	2276	2099	2138	4555
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-5	2431	2103	2278	4559
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-	1.141681957531808e+01	1.405512047239916e+01	5231
-	1.719315911158019e+01	7.913059239332790e+00	5232
-NMARK= 2
-MARKER_TAG= airfoil
-MARKER_ELEMS= 200
-3	199	0
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-3	3	4
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-MARKER_ELEMS= 50
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diff --git a/externals/utils/release_su2.sh b/externals/utils/release_su2.sh
index a5e224d4728..dc8555aff25 100755
--- a/externals/utils/release_su2.sh
+++ b/externals/utils/release_su2.sh
@@ -47,11 +47,8 @@ if [ ! -d ${RELEASEDIR} ]
 then
  mkdir ${RELEASEDIR}
  mkdir ${RELEASEDIR}/bin
- mkdir ${RELEASEDIR}/QuickStart
 fi
 cp -R ${SU2DIR}/bin/* ${RELEASEDIR}/bin/
-cp ${SU2DIR}/QuickStart/inv_NACA0012.cfg ${RELEASEDIR}/QuickStart/
-cp ${SU2DIR}/QuickStart/mesh_NACA0012_inv.su2 ${RELEASEDIR}/QuickStart/
 rm -fr ${SU2DIR}
 
 # Tar up the finished build directory and clean up

From fbeabbc3dc2db5b3ed97b8666ac66b3346943ac4 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 2 Jul 2023 14:26:50 -0700
Subject: [PATCH 520/656] more updates

---
 TestCases/hybrid_regression.py                | 20 +++++++++----------
 .../chtPinArray_2d/of_grad_findiff.csv.ref    |  2 +-
 TestCases/parallel_regression.py              | 18 ++++++++---------
 TestCases/serial_regression.py                | 14 ++++++-------
 .../transonic_stator_restart.cfg              |  1 +
 5 files changed, 28 insertions(+), 27 deletions(-)

diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index 25811d49a7f..facf401921a 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -207,8 +207,8 @@ def main():
     turb_naca0012_sst.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     turb_naca0012_sst.test_iter = 10
-    turb_naca0012_sst.test_vals         = [-11.418415, -12.801780, -5.864804, 1.049990, 0.019163, -1.669899, -38.695000]
-    turb_naca0012_sst.test_vals_aarch64 = [-11.450473, -12.797872, -5.863655, 1.049989, 0.019163, -1.856266, -38.694000]
+    turb_naca0012_sst.test_vals         = [-12.216989, -14.439370, -7.108639, 1.050109, 0.019148, -1.483537, -38.510000]
+    turb_naca0012_sst.test_vals_aarch64 = [-12.216989, -14.439370, -7.108639, 1.050109, 0.019148, -1.483537, -38.510000]
     test_list.append(turb_naca0012_sst)
 
     # NACA0012 (SST_SUST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
@@ -216,8 +216,8 @@ def main():
     turb_naca0012_sst_sust.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst_sust.cfg_file  = "turb_NACA0012_sst_sust.cfg"
     turb_naca0012_sst_sust.test_iter = 10
-    turb_naca0012_sst_sust.test_vals         = [-11.361657, -12.642245, -5.747099, 1.005234, 0.019017, -1.573783]
-    turb_naca0012_sst_sust.test_vals_aarch64 = [-11.367052, -12.640670, -5.746919, 1.005233, 0.019017, -1.913907]
+    turb_naca0012_sst_sust.test_vals         = [-12.148204, -14.755890, -6.342986, 1.001189, 0.019384, -1.432333]
+    turb_naca0012_sst_sust.test_vals_aarch64 = [-12.148204, -14.755890, -6.342986, 1.001189, 0.019384, -1.432333]
     test_list.append(turb_naca0012_sst_sust)
 
     # NACA0012 (SST, fixed values for turbulence quantities)
@@ -254,8 +254,8 @@ def main():
     axi_rans_air_nozzle_restart.cfg_dir   = "axisymmetric_rans/air_nozzle"
     axi_rans_air_nozzle_restart.cfg_file  = "air_nozzle_restart.cfg"
     axi_rans_air_nozzle_restart.test_iter = 10
-    axi_rans_air_nozzle_restart.test_vals         = [-12.085749, -7.439410, -8.772091, -4.045091, -1924.800000]
-    axi_rans_air_nozzle_restart.test_vals_aarch64 = [-12.093539, -6.630357, -8.798732, -2.399130, -1938.200000]
+    axi_rans_air_nozzle_restart.test_vals         = [-12.060634, -6.992273, -8.808757, -4.097753, -2019.800000]
+    axi_rans_air_nozzle_restart.test_vals_aarch64 = [-12.060634, -6.992273, -8.808757, -4.097753, -2019.800000]
     test_list.append(axi_rans_air_nozzle_restart)
 
     #################################
@@ -470,7 +470,7 @@ def main():
     sine_gust.test_vals = [-1.977520, 3.481804, -0.012402, -0.007454]
     sine_gust.unsteady  = True
     test_list.append(sine_gust)
-    
+
     # Cosine gust in z-direction
     cosine_gust           = TestCase('cosine_gust_zdir')
     cosine_gust.cfg_dir   = "gust"
@@ -479,7 +479,7 @@ def main():
     cosine_gust.test_vals = [-2.418813, 0.004650, -0.001878, -0.000637, -0.000271]
     cosine_gust.unsteady  = True
     test_list.append(cosine_gust)
-    
+
     # Gust with mesh deformation
     gust_mesh_defo           = TestCase('gust_with_mesh_deformation')
     gust_mesh_defo.cfg_dir   = "gust"
@@ -557,7 +557,7 @@ def main():
     Jones_tc_restart.cfg_dir   = "turbomachinery/APU_turbocharger"
     Jones_tc_restart.cfg_file  = "Jones_restart.cfg"
     Jones_tc_restart.test_iter = 5
-    Jones_tc_restart.test_vals = [-6.986581, -3.096834, -14.849548, -9.102930, -11.787851, -6.266207, 73266, 73266]
+    Jones_tc_restart.test_vals = [-6.604542, -2.792279, -14.328530, -8.769313, -11.371439, -5.845633, 73273.000000, 73273.000000]
     test_list.append(Jones_tc_restart)
 
     # 2D axial stage
@@ -769,7 +769,7 @@ def main():
     pywrapper_translating_naca0012.test_file = "forces_0.csv"
     pywrapper_translating_naca0012.enabled_on_cpu_arch = ["x86_64"]
     file_diff_list.append(pywrapper_translating_naca0012)
-    
+
     # NACA0012 with updated moving frame
     pywrapper_updated_moving_frame_naca0012 = TestCase('pywrapper_updated_moving_frame_naca0012')
     pywrapper_updated_moving_frame_naca0012.cfg_dir = "py_wrapper/updated_moving_frame_NACA12"
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/of_grad_findiff.csv.ref b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/of_grad_findiff.csv.ref
index 82730a5fe1e..f959a481490 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/of_grad_findiff.csv.ref
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/of_grad_findiff.csv.ref
@@ -1,2 +1,2 @@
 "VARIABLE"      , "AVG_DENSITY[0]", "AVG_ENTHALPY[0]", "AVG_NORMALVEL[0]", "DRAG[0]"       , "EFFICIENCY[0]" , "FORCE_X[0]"    , "FORCE_Y[0]"    , "FORCE_Z[0]"    , "LIFT[0]"       , "MOMENT_X[0]"   , "MOMENT_Y[0]"   , "MOMENT_Z[0]"   , "SIDEFORCE[0]"  , "SURFACE_MACH[0]", "SURFACE_MASSFLOW[0]", "SURFACE_MOM_DISTORTION[0]", "SURFACE_PRESSURE_DROP[0]", "SURFACE_SECONDARY[0]", "SURFACE_SECOND_OVER_UNIFORM[0]", "SURFACE_STATIC_PRESSURE[0]", "SURFACE_STATIC_TEMPERATURE[0]", "SURFACE_TOTAL_PRESSURE[0]", "SURFACE_TOTAL_TEMPERATURE[0]", "SURFACE_UNIFORMITY[0]", "AVG_TEMPERATURE[1]", "MAXIMUM_HEATFLUX[1]", "TOTAL_HEATFLUX[1]", "FINDIFF_STEP"  
-0               , 0.0             , -100000.01639127731, -1.1103000000496327e-08, 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , -0.0399999991462785, 3.3309999998872306e-08, -2.1099999997220564      , 0.0                     , 2.1799999999627673  , 3.8000000007754053            , 319.9999980552093         , -39.999997625272954          , 318.0000007318995        , -39.999997625272954         , -1.400000004814217   , -139.99999737279722, 0.0                , -540.0000077315781, 1e-08           
+0               , 0.0             , -199999.9862164259, -5.551100000002363e-08, 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , -0.02000000026702864, 5.550999999230055e-08, -0.6560000001543109      , 0.0                     , 0.6520000012111282  , 1.1399999999550658            , 319.9999980552093         , -39.999997625272954          , 260.999999568412         , -39.999997625272954         , -0.4999999969612645  , -269.99999818144715, 0.0                , -560.0000008598727, 1e-08           
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 43a38a042fb..040a59dd7d7 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -413,7 +413,7 @@ def main():
     turb_naca0012_sst.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     turb_naca0012_sst.test_iter = 10
-    turb_naca0012_sst.test_vals = [-11.422619, -12.803419, -5.867375, 1.049989, 0.019163, -1.827695, -38.695000]
+    turb_naca0012_sst.test_vals = [-12.219694, -14.440925, -7.107551, 1.050109, 0.019148, -1.601287, -38.510000]
     turb_naca0012_sst.timeout   = 3200
     test_list.append(turb_naca0012_sst)
 
@@ -422,7 +422,7 @@ def main():
     turb_naca0012_sst_sust.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst_sust.cfg_file  = "turb_NACA0012_sst_sust.cfg"
     turb_naca0012_sst_sust.test_iter = 10
-    turb_naca0012_sst_sust.test_vals = [-11.366100, -12.643576, -5.749377, 1.005234, 0.019017, -1.818746]
+    turb_naca0012_sst_sust.test_vals = [-12.148637, -14.756583, -6.342201, 1.001189, 0.019384, -1.579100]
     turb_naca0012_sst_sust.timeout   = 3200
     test_list.append(turb_naca0012_sst_sust)
 
@@ -431,7 +431,7 @@ def main():
     turb_naca0012_sst_2003_Vm.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst_2003_Vm.cfg_file  = "turb_NACA0012_sst_2003-Vm.cfg"
     turb_naca0012_sst_2003_Vm.test_iter = 10
-    turb_naca0012_sst_2003_Vm.test_vals = [-7.672926, -10.025010, -3.365892, 1.048735, 0.019723, -2.052543]
+    turb_naca0012_sst_2003_Vm.test_vals = [-7.664806, -10.014760, -3.358584, 1.048643, 0.019718, -2.067883]
     turb_naca0012_sst_2003_Vm.timeout   = 3200
     test_list.append(turb_naca0012_sst_2003_Vm)
 
@@ -440,7 +440,7 @@ def main():
     turb_naca0012_sst_1994_KLm.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst_1994_KLm.cfg_file  = "turb_NACA0012_sst_1994-KLm.cfg"
     turb_naca0012_sst_1994_KLm.test_iter = 10
-    turb_naca0012_sst_1994_KLm.test_vals = [-8.616539, -10.868753, -4.060879, 1.049473, 0.019192, -1.867965]
+    turb_naca0012_sst_1994_KLm.test_vals = [-8.570837, -10.805211, -3.997146, 1.049397, 0.019183, -1.805750]
     turb_naca0012_sst_1994_KLm.timeout   = 3200
     test_list.append(turb_naca0012_sst_1994_KLm)
 
@@ -481,7 +481,7 @@ def main():
     axi_rans_air_nozzle_restart.cfg_dir   = "axisymmetric_rans/air_nozzle"
     axi_rans_air_nozzle_restart.cfg_file  = "air_nozzle_restart.cfg"
     axi_rans_air_nozzle_restart.test_iter = 10
-    axi_rans_air_nozzle_restart.test_vals = [-12.089268, -7.493381, -8.716391, -4.021218, -1924.800000]
+    axi_rans_air_nozzle_restart.test_vals = [-12.063597, -7.006585, -8.702557, -4.039824, -2019.0]
     axi_rans_air_nozzle_restart.tol       = 0.0001
     test_list.append(axi_rans_air_nozzle_restart)
 
@@ -1015,7 +1015,7 @@ def main():
     Jones_tc_restart.cfg_dir   = "turbomachinery/APU_turbocharger"
     Jones_tc_restart.cfg_file  = "Jones_restart.cfg"
     Jones_tc_restart.test_iter = 5
-    Jones_tc_restart.test_vals = [-6.986563, -3.096834, -14.849532, -9.102914, -11.787851, -6.266208, 7.3266e+04, 7.3266e+04]
+    Jones_tc_restart.test_vals = [-6.604542, -2.792281, -14.328530, -8.769313, -11.371439, -5.845632, 73273, 73273]
     test_list.append(Jones_tc_restart)
 
     # 2D axial stage
@@ -1256,8 +1256,8 @@ def main():
     sp_pinArray_3d_cht_mf_hf_tp.cfg_dir   = "incomp_navierstokes/streamwise_periodic/chtPinArray_3d"
     sp_pinArray_3d_cht_mf_hf_tp.cfg_file  = "configMaster.cfg"
     sp_pinArray_3d_cht_mf_hf_tp.test_iter = 30
-    sp_pinArray_3d_cht_mf_hf_tp.test_vals         = [-3.773085, -4.220555, -4.811282, -0.009675, 99.879858, 419.200000, 0.000000]
-    sp_pinArray_3d_cht_mf_hf_tp.test_vals_aarch64 = [-13.400623, -7.476945, -7.025285, -0.009675, 99.879812, 419.200000, 0.0]
+    sp_pinArray_3d_cht_mf_hf_tp.test_vals         = [-5.109072, -5.409931, -6.807748, -0.009675, 104.655093, 4.1921e+02, 0.0]
+    sp_pinArray_3d_cht_mf_hf_tp.test_vals_aarch64 = [-5.109072, -5.409931, -6.807748, -0.009675, 104.655093, 4.1921e+02, 0.0]
     sp_pinArray_3d_cht_mf_hf_tp.multizone = True
     test_list.append(sp_pinArray_3d_cht_mf_hf_tp)
 
@@ -1279,7 +1279,7 @@ def main():
     pywrapper_turb_naca0012_sst.cfg_dir   = "rans/naca0012"
     pywrapper_turb_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     pywrapper_turb_naca0012_sst.test_iter = 10
-    pywrapper_turb_naca0012_sst.test_vals = [-11.422619, -12.803419, -5.867375, 1.049989, 0.019163, -1.827695, -38.695000]
+    pywrapper_turb_naca0012_sst.test_vals = [-12.219694, -14.440925, -7.107551, 1.050109, 0.019148, -1.601287, -38.510000]
     pywrapper_turb_naca0012_sst.command   = TestCase.Command("mpirun -np 2", "SU2_CFD.py", "--parallel -f")
     pywrapper_turb_naca0012_sst.timeout   = 3200
     test_list.append(pywrapper_turb_naca0012_sst)
diff --git a/TestCases/serial_regression.py b/TestCases/serial_regression.py
index 6efa0e033cf..433da5063af 100644
--- a/TestCases/serial_regression.py
+++ b/TestCases/serial_regression.py
@@ -279,8 +279,8 @@ def main():
     turb_naca0012_sst.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     turb_naca0012_sst.test_iter = 10
-    turb_naca0012_sst.test_vals         = [-12.007177, -14.272504, -6.994514, 1.050109, 0.019148, -1.455402, -3.8510e+01]
-    turb_naca0012_sst.test_vals_aarch64 = [-12.007177, -14.272504, -6.994514, 1.050109, 0.019148, -1.455402, -3.8510e+01]
+    turb_naca0012_sst.test_vals         = [-12.213755, -14.439873, -7.108062, 1.050109, 0.019148, -1.875539, -38.510000]
+    turb_naca0012_sst.test_vals_aarch64 = [-12.213755, -14.439873, -7.108062, 1.050109, 0.019148, -1.875539, -38.510000]
     turb_naca0012_sst.timeout   = 3200
     test_list.append(turb_naca0012_sst)
 
@@ -289,7 +289,7 @@ def main():
     turb_naca0012_sst_2003m.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst_2003m.cfg_file  = "turb_NACA0012_sst_2003m.cfg"
     turb_naca0012_sst_2003m.test_iter = 10
-    turb_naca0012_sst_2003m.test_vals = [-7.698427, -10.060122, -3.421605, 1.049413, 0.019691, -2.193374, -45.178000]
+    turb_naca0012_sst_2003m.test_vals = [-7.690803, -10.049843, -3.414020, 1.049314, 0.019686, -2.207421, -45.199000]
     turb_naca0012_sst_2003m.timeout   = 3200
     test_list.append(turb_naca0012_sst_2003m)
 
@@ -298,7 +298,7 @@ def main():
     turb_naca0012_sst_sust_restart.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst_sust_restart.cfg_file  = "turb_NACA0012_sst_sust.cfg"
     turb_naca0012_sst_sust_restart.test_iter = 10
-    turb_naca0012_sst_sust_restart.test_vals = [-12.006877, -14.685697, -6.270559, 1.001189, 0.019384, -1.435246]
+    turb_naca0012_sst_sust_restart.test_vals = [-12.153015, -14.756601, -6.342509, 1.001189, 0.019384, -1.820009]
     turb_naca0012_sst_sust_restart.timeout   = 3200
     test_list.append(turb_naca0012_sst_sust_restart)
 
@@ -329,7 +329,7 @@ def main():
     axi_rans_air_nozzle_restart.cfg_dir   = "axisymmetric_rans/air_nozzle"
     axi_rans_air_nozzle_restart.cfg_file  = "air_nozzle_restart.cfg"
     axi_rans_air_nozzle_restart.test_iter = 10
-    axi_rans_air_nozzle_restart.test_vals = [-12.003752, -6.926896, -8.627670, -4.003588, -2.0198e+03]
+    axi_rans_air_nozzle_restart.test_vals = [-12.063377, -7.005051, -8.705733, -4.036815, -2019.8]
     axi_rans_air_nozzle_restart.tol       = 0.0001
     test_list.append(axi_rans_air_nozzle_restart)
 
@@ -1496,8 +1496,8 @@ def main():
     pywrapper_turb_naca0012_sst.cfg_dir   = "rans/naca0012"
     pywrapper_turb_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     pywrapper_turb_naca0012_sst.test_iter = 10
-    pywrapper_turb_naca0012_sst.test_vals         = [-12.007177, -14.272504, -6.994514, 1.050109, 0.019148, -1.455402, -3.8510e+01]
-    pywrapper_turb_naca0012_sst.test_vals_aarch64 = [-12.007177, -14.272504, -6.994514, 1.050109, 0.019148, -1.455402, -3.8510e+01]
+    pywrapper_turb_naca0012_sst.test_vals         = [-12.213755, -14.439873, -7.108062, 1.050109, 0.019148, -1.875539, -38.510000]
+    pywrapper_turb_naca0012_sst.test_vals_aarch64 = [-12.213755, -14.439873, -7.108062, 1.050109, 0.019148, -1.875539, -38.510000]
     pywrapper_turb_naca0012_sst.command   =  TestCase.Command(exec = "SU2_CFD.py", param = "-f")
     pywrapper_turb_naca0012_sst.timeout   = 3200
     pywrapper_turb_naca0012_sst.tol       = 0.00001
diff --git a/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg b/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg
index 87c0f8abaa8..635a73af161 100644
--- a/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg
+++ b/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg
@@ -13,6 +13,7 @@
 %
 SOLVER= RANS
 KIND_TURB_MODEL= SST
+SST_OPTIONS= V1994m
 MATH_PROBLEM= DIRECT
 RESTART_SOL= YES
 DISCARD_INFILES= NO

From c5e23e3880f7e122f4401b4922290dcff32eb0ae Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 2 Jul 2023 16:00:04 -0700
Subject: [PATCH 521/656] begin disc adj updates

---
 .../air_nozzle/air_nozzle_restart.cfg                |  2 +-
 .../transonic_stator_2D/transonic_stator.cfg         |  4 ++--
 TestCases/hybrid_regression.py                       |  4 ++--
 TestCases/parallel_regression.py                     | 10 +++++-----
 TestCases/parallel_regression_AD.py                  | 12 ++++++------
 TestCases/serial_regression.py                       |  4 ++--
 .../transonic_stator_2D/transonic_stator_restart.cfg |  1 -
 7 files changed, 18 insertions(+), 19 deletions(-)

diff --git a/TestCases/axisymmetric_rans/air_nozzle/air_nozzle_restart.cfg b/TestCases/axisymmetric_rans/air_nozzle/air_nozzle_restart.cfg
index 0ba7296c7ef..effd129b9df 100644
--- a/TestCases/axisymmetric_rans/air_nozzle/air_nozzle_restart.cfg
+++ b/TestCases/axisymmetric_rans/air_nozzle/air_nozzle_restart.cfg
@@ -93,4 +93,4 @@ SOLUTION_FILENAME= solution_flow.dat
 RESTART_FILENAME= restart_flow.dat
 OUTPUT_WRT_FREQ= 1000
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, RMS_TKE, RMS_DISSIPATION, TOTAL_HEATFLUX, \
-                RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, RMS_ADJ_TKE, RMS_ADJ_DISSIPATION, SENS_AOA, SENS_MACH)
+                RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, RMS_ADJ_TKE, RMS_ADJ_DISSIPATION)
diff --git a/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg b/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg
index 66c520c0a09..1177b441780 100644
--- a/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg
+++ b/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg
@@ -14,7 +14,7 @@
 %
 SOLVER= RANS
 KIND_TURB_MODEL= SST
-MATH_PROBLEM= DISCRETE_ADJOINT
+SST_OPTIONS= V1994m
 RESTART_SOL= NO
 NZONES= 1
 
@@ -185,4 +185,4 @@ GRAD_OBJFUNC_FILENAME= of_grad.dat
 SURFACE_FILENAME= surface_flow
 SURFACE_ADJ_FILENAME= surface_adjoint
 OUTPUT_WRT_FREQ= 500
-SCREEN_OUTPUT=(INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_TKE)
+SCREEN_OUTPUT=(INNER_ITER, RMS_RES)
diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index facf401921a..3df7f73d9ca 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -574,8 +574,8 @@ def main():
     transonic_stator_restart.cfg_dir   = "turbomachinery/transonic_stator_2D"
     transonic_stator_restart.cfg_file  = "transonic_stator_restart.cfg"
     transonic_stator_restart.test_iter = 20
-    transonic_stator_restart.test_vals         = [-7.542642, -6.840866, -6.669194, -1.578593, -6.793009, -0.742574, -471650]
-    transonic_stator_restart.test_vals_aarch64 = [-7.542642, -6.840866, -6.669194, -1.578593, -6.793009, -0.742574, -471650]
+    transonic_stator_restart.test_vals         = [-5.346503, -3.510597, -3.156830, 0.752511, -3.834382, 1.816610, -471690]
+    transonic_stator_restart.test_vals_aarch64 = [-5.346503, -3.510597, -3.156830, 0.752511, -3.834382, 1.816610, -471690]
     test_list.append(transonic_stator_restart)
 
     ######################################
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 040a59dd7d7..0a27b9fa7d2 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -481,7 +481,7 @@ def main():
     axi_rans_air_nozzle_restart.cfg_dir   = "axisymmetric_rans/air_nozzle"
     axi_rans_air_nozzle_restart.cfg_file  = "air_nozzle_restart.cfg"
     axi_rans_air_nozzle_restart.test_iter = 10
-    axi_rans_air_nozzle_restart.test_vals = [-12.063597, -7.006585, -8.702557, -4.039824, -2019.0]
+    axi_rans_air_nozzle_restart.test_vals = [-12.063597, -7.006585, -8.702557, -4.039824, -2019.8]
     axi_rans_air_nozzle_restart.tol       = 0.0001
     test_list.append(axi_rans_air_nozzle_restart)
 
@@ -1031,7 +1031,7 @@ def main():
     transonic_stator_restart.cfg_dir   = "turbomachinery/transonic_stator_2D"
     transonic_stator_restart.cfg_file  = "transonic_stator_restart.cfg"
     transonic_stator_restart.test_iter = 20
-    transonic_stator_restart.test_vals = [-7.544516, -6.822541, -6.689799, -1.581068, -6.798361, -0.746758, -471650]
+    transonic_stator_restart.test_vals = [-5.354418, -3.509964, -3.163206, 0.744733, -3.846691, 1.805587, -471690]
     test_list.append(transonic_stator_restart)
 
     ######################################
@@ -1256,8 +1256,8 @@ def main():
     sp_pinArray_3d_cht_mf_hf_tp.cfg_dir   = "incomp_navierstokes/streamwise_periodic/chtPinArray_3d"
     sp_pinArray_3d_cht_mf_hf_tp.cfg_file  = "configMaster.cfg"
     sp_pinArray_3d_cht_mf_hf_tp.test_iter = 30
-    sp_pinArray_3d_cht_mf_hf_tp.test_vals         = [-5.109072, -5.409931, -6.807748, -0.009675, 104.655093, 4.1921e+02, 0.0]
-    sp_pinArray_3d_cht_mf_hf_tp.test_vals_aarch64 = [-5.109072, -5.409931, -6.807748, -0.009675, 104.655093, 4.1921e+02, 0.0]
+    sp_pinArray_3d_cht_mf_hf_tp.test_vals         = [-5.128577, -5.425081, -6.788413, -0.009675, 104.655438, 419.210000, 0.0]
+    sp_pinArray_3d_cht_mf_hf_tp.test_vals_aarch64 = [-5.128577, -5.425081, -6.788413, -0.009675, 104.655438, 419.210000, 0.0]
     sp_pinArray_3d_cht_mf_hf_tp.multizone = True
     test_list.append(sp_pinArray_3d_cht_mf_hf_tp)
 
@@ -1503,7 +1503,7 @@ def main():
     species3_multizone_restart.cfg_dir   = "species_transport/multizone"
     species3_multizone_restart.cfg_file  = "configMaster.cfg"
     species3_multizone_restart.test_iter = 5
-    species3_multizone_restart.test_vals = [-6.571720, -6.086110]
+    species3_multizone_restart.test_vals = [-6.175178, -5.763030]
     species3_multizone_restart.multizone = True
     test_list.append(species3_multizone_restart)
 
diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index 814d2102d36..70c05d08bc7 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -91,8 +91,8 @@ def main():
     discadj_rans_naca0012_sst.cfg_dir   = "disc_adj_rans/naca0012"
     discadj_rans_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     discadj_rans_naca0012_sst.test_iter = 10
-    discadj_rans_naca0012_sst.test_vals         = [-2.221792, -0.491538, 0.182010, -0.000018]
-    discadj_rans_naca0012_sst.test_vals_aarch64 = [-2.221795, -0.491538, 0.182010, -0.000018]
+    discadj_rans_naca0012_sst.test_vals         = [-2.221848, -0.502430, 0.182000, -0.000018]
+    discadj_rans_naca0012_sst.test_vals_aarch64 = [-2.221848, -0.502430, 0.182000, -0.000018]
     test_list.append(discadj_rans_naca0012_sst)
 
     #######################################
@@ -137,8 +137,8 @@ def main():
     discadj_incomp_turb_NACA0012_sst.cfg_dir   = "disc_adj_incomp_rans/naca0012"
     discadj_incomp_turb_NACA0012_sst.cfg_file  = "turb_naca0012_sst.cfg"
     discadj_incomp_turb_NACA0012_sst.test_iter = 10
-    discadj_incomp_turb_NACA0012_sst.test_vals         = [-3.845593, -2.413098, -8.419991, 0.000000]
-    discadj_incomp_turb_NACA0012_sst.test_vals_aarch64 = [-3.845595, -2.413099, -8.419992, 0.000000]
+    discadj_incomp_turb_NACA0012_sst.test_vals         = [-3.845596, -2.432265, -8.351920, 0.000000]
+    discadj_incomp_turb_NACA0012_sst.test_vals_aarch64 = [-3.845596, -2.432265, -8.351920, 0.000000]
     test_list.append(discadj_incomp_turb_NACA0012_sst)
 
     ####################################################################
@@ -150,7 +150,7 @@ def main():
     discadj_axisymmetric_rans_nozzle.cfg_dir    = "axisymmetric_rans/air_nozzle"
     discadj_axisymmetric_rans_nozzle.cfg_file   = "air_nozzle_restart.cfg"
     discadj_axisymmetric_rans_nozzle.test_iter  = 10
-    discadj_axisymmetric_rans_nozzle.test_vals  = [9.523445, 5.023948, 7.509000, 2.841876, 0.000000, -246139999999999992659968.000000]
+    discadj_axisymmetric_rans_nozzle.test_vals  = [9.516464, 5.022130, 7.370705, 2.744551]
     discadj_axisymmetric_rans_nozzle.no_restart = True
     test_list.append(discadj_axisymmetric_rans_nozzle)
 
@@ -230,7 +230,7 @@ def main():
     discadj_trans_stator.cfg_dir   = "disc_adj_turbomachinery/transonic_stator_2D"
     discadj_trans_stator.cfg_file  = "transonic_stator.cfg"
     discadj_trans_stator.test_iter = 79
-    discadj_trans_stator.test_vals = [79, 0.770040, 2.052053]
+    discadj_trans_stator.test_vals = [79, 0.765040, 0.375492, 0.467751, -0.999841, 2.154003, -4.445648]
     test_list.append(discadj_trans_stator)
 
     ###################################
diff --git a/TestCases/serial_regression.py b/TestCases/serial_regression.py
index 433da5063af..cd9d7409f59 100644
--- a/TestCases/serial_regression.py
+++ b/TestCases/serial_regression.py
@@ -853,7 +853,7 @@ def main():
     Jones_tc_restart.cfg_dir   = "turbomachinery/APU_turbocharger"
     Jones_tc_restart.cfg_file  = "Jones_restart.cfg"
     Jones_tc_restart.test_iter = 5
-    Jones_tc_restart.test_vals = [-6.341673, -4.347529, -14.317871, -8.739672, -11.333584, -5.762934, 7.3273e+04, 7.3273e+04]
+    Jones_tc_restart.test_vals = [-6.604538, -2.792279, -14.328534, -8.769317, -11.371438, -5.845632, 73273.000000, 73273.000000]
     Jones_tc_restart.tol       = 0.0001
     test_list.append(Jones_tc_restart)
 
@@ -870,7 +870,7 @@ def main():
     transonic_stator_restart.cfg_dir   = "turbomachinery/transonic_stator_2D"
     transonic_stator_restart.cfg_file  = "transonic_stator_restart.cfg"
     transonic_stator_restart.test_iter = 20
-    transonic_stator_restart.test_vals = [-7.853522, -6.815458, -6.565073, -1.880583, -6.316205, -1.017773, -4.7182e+05]
+    transonic_stator_restart.test_vals = [-5.345491, -3.512311, -3.153972, 0.753530, -3.835478, 1.808296, -471690]
     test_list.append(transonic_stator_restart)
 
 
diff --git a/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg b/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg
index 635a73af161..87c0f8abaa8 100644
--- a/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg
+++ b/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg
@@ -13,7 +13,6 @@
 %
 SOLVER= RANS
 KIND_TURB_MODEL= SST
-SST_OPTIONS= V1994m
 MATH_PROBLEM= DIRECT
 RESTART_SOL= YES
 DISCARD_INFILES= NO

From a64499bc44d54e7ef74b8d4954ce54eff4a72abe Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 2 Jul 2023 18:07:02 -0700
Subject: [PATCH 522/656] more updates

---
 .../naca0012/turb_naca0012_sst.cfg                    | 11 ++++-------
 TestCases/hybrid_regression_AD.py                     |  8 ++++----
 TestCases/parallel_regression_AD.py                   |  6 +++---
 TestCases/serial_regression_AD.py                     |  4 ++--
 4 files changed, 13 insertions(+), 16 deletions(-)

diff --git a/TestCases/disc_adj_incomp_rans/naca0012/turb_naca0012_sst.cfg b/TestCases/disc_adj_incomp_rans/naca0012/turb_naca0012_sst.cfg
index cca9e34bef1..bde0ff08ebd 100755
--- a/TestCases/disc_adj_incomp_rans/naca0012/turb_naca0012_sst.cfg
+++ b/TestCases/disc_adj_incomp_rans/naca0012/turb_naca0012_sst.cfg
@@ -13,7 +13,6 @@
 %
 SOLVER= INC_RANS
 KIND_TURB_MODEL= SST
-MATH_PROBLEM= DISCRETE_ADJOINT
 RESTART_SOL= NO
 
 % -------------------- INCOMPRESSIBLE FREE-STREAM DEFINITION ------------------%
@@ -45,11 +44,9 @@ MARKER_MONITORING= ( airfoil )
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
 NUM_METHOD_GRAD= GREEN_GAUSS
-CFL_NUMBER= 25.0
+CFL_NUMBER= 1500.0
 CFL_ADAPT= NO
-CFL_ADAPT_PARAM= ( 1.5, 0.5, 25.0, 10000.0 )
-MAX_DELTA_TIME= 1E6
-RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
+QUASI_NEWTON_NUM_SAMPLES= 30
 ITER= 99999
 OBJECTIVE_FUNCTION= DRAG
 OBJECTIVE_WEIGHT = 1.0
@@ -67,7 +64,7 @@ LINEAR_SOLVER= FGMRES
 LINEAR_SOLVER_PREC= ILU
 LINEAR_SOLVER_ILU_FILL_IN= 0
 LINEAR_SOLVER_ERROR= 1E-10
-LINEAR_SOLVER_ITER= 10
+LINEAR_SOLVER_ITER= 15
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
@@ -115,7 +112,7 @@ GRAD_OBJFUNC_FILENAME= of_grad.dat
 SURFACE_FILENAME= surface_flow
 SURFACE_ADJ_FILENAME= surface_adjoint
 OUTPUT_WRT_FREQ= 250
-SCREEN_OUTPUT= (INNER_ITER, RMS_ADJ_PRESSURE, RMS_ADJ_TKE, RMS_ADJ_DISSIPATION, SENS_PRESS, SENS_AOA)
+SCREEN_OUTPUT= (INNER_ITER, RMS_ADJ_PRESSURE, RMS_ADJ_TKE, RMS_ADJ_DISSIPATION, SENS_PRESS, SENS_AOA, LINSOL_RESIDUAL)
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
diff --git a/TestCases/hybrid_regression_AD.py b/TestCases/hybrid_regression_AD.py
index 438b2fa731f..a5ae3786037 100644
--- a/TestCases/hybrid_regression_AD.py
+++ b/TestCases/hybrid_regression_AD.py
@@ -84,7 +84,7 @@ def main():
     discadj_rans_naca0012_sst.cfg_dir   = "disc_adj_rans/naca0012"
     discadj_rans_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     discadj_rans_naca0012_sst.test_iter = 10
-    discadj_rans_naca0012_sst.test_vals = [-2.221793, -0.491367, 0.182000, -0.000018]
+    discadj_rans_naca0012_sst.test_vals = [-2.221846, -0.491928, 0.182000, -0.000018]
     test_list.append(discadj_rans_naca0012_sst)
 
     #######################################
@@ -129,7 +129,7 @@ def main():
     discadj_incomp_turb_NACA0012_sst.cfg_dir   = "disc_adj_incomp_rans/naca0012"
     discadj_incomp_turb_NACA0012_sst.cfg_file  = "turb_naca0012_sst.cfg"
     discadj_incomp_turb_NACA0012_sst.test_iter = 10
-    discadj_incomp_turb_NACA0012_sst.test_vals = [-3.845593, -2.414026, -8.420194, 0.000000]
+    discadj_incomp_turb_NACA0012_sst.test_vals = [-4.148134, -2.442830, -7.875040, 0, -1.076773]
     test_list.append(discadj_incomp_turb_NACA0012_sst)
 
     #######################################################
@@ -193,8 +193,8 @@ def main():
     discadj_trans_stator.cfg_dir   = "disc_adj_turbomachinery/transonic_stator_2D"
     discadj_trans_stator.cfg_file  = "transonic_stator.cfg"
     discadj_trans_stator.test_iter = 79
-    discadj_trans_stator.test_vals         = [79, 0.770158, 2.051501]
-    discadj_trans_stator.test_vals_aarch64 = [79, 0.770158, 2.051501]
+    discadj_trans_stator.test_vals         = [79, 0.770065, 0.383137, 0.472153, -0.996484, 2.153296, -4.444301]
+    discadj_trans_stator.test_vals_aarch64 = [79, 0.770065, 0.383137, 0.472153, -0.996484, 2.153296, -4.444301]
     test_list.append(discadj_trans_stator)
 
     ###################################
diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index 70c05d08bc7..282ec14a9a1 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -230,7 +230,7 @@ def main():
     discadj_trans_stator.cfg_dir   = "disc_adj_turbomachinery/transonic_stator_2D"
     discadj_trans_stator.cfg_file  = "transonic_stator.cfg"
     discadj_trans_stator.test_iter = 79
-    discadj_trans_stator.test_vals = [79, 0.765040, 0.375492, 0.467751, -0.999841, 2.154003, -4.445648]
+    discadj_trans_stator.test_vals = [79, 0.769972, 0.374328, 0.474458, -0.996522, 2.154079, -4.446062]
     test_list.append(discadj_trans_stator)
 
     ###################################
@@ -298,7 +298,7 @@ def main():
     da_sp_pinArray_cht_2d_dp_hf.cfg_dir   = "incomp_navierstokes/streamwise_periodic/chtPinArray_2d"
     da_sp_pinArray_cht_2d_dp_hf.cfg_file  = "DA_configMaster.cfg"
     da_sp_pinArray_cht_2d_dp_hf.test_iter = 100
-    da_sp_pinArray_cht_2d_dp_hf.test_vals = [-4.800597, -4.065541, -4.137339]
+    da_sp_pinArray_cht_2d_dp_hf.test_vals = [-4.739373, -4.060562, -3.867056]
     da_sp_pinArray_cht_2d_dp_hf.multizone = True
     test_list.append(da_sp_pinArray_cht_2d_dp_hf)
 
@@ -307,7 +307,7 @@ def main():
     da_sp_pinArray_cht_2d_mf.cfg_dir   = "incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d"
     da_sp_pinArray_cht_2d_mf.cfg_file  = "configMaster.cfg"
     da_sp_pinArray_cht_2d_mf.test_iter = 100
-    da_sp_pinArray_cht_2d_mf.test_vals = [-4.609362, -1.273845, -1.502739, -18.503852, -0.834361, -5.813325, -19.074376, -48.287501]
+    da_sp_pinArray_cht_2d_mf.test_vals = [-6.124936, -2.661408, -2.981673, -18.926294, -2.862099, -7.673088, -18.810904, -23.849963]
     da_sp_pinArray_cht_2d_mf.multizone = True
     test_list.append(da_sp_pinArray_cht_2d_mf)
 
diff --git a/TestCases/serial_regression_AD.py b/TestCases/serial_regression_AD.py
index c4e7157149e..e3a3e0b2cd5 100644
--- a/TestCases/serial_regression_AD.py
+++ b/TestCases/serial_regression_AD.py
@@ -83,7 +83,7 @@ def main():
     discadj_rans_naca0012_sst.cfg_dir   = "disc_adj_rans/naca0012"
     discadj_rans_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     discadj_rans_naca0012_sst.test_iter = 10
-    discadj_rans_naca0012_sst.test_vals = [-2.221792, -0.491367, 0.182010, -0.000018]
+    discadj_rans_naca0012_sst.test_vals = [-2.221845, -0.491927, 0.182000, -0.000018]
     test_list.append(discadj_rans_naca0012_sst)
 
     #######################################
@@ -127,7 +127,7 @@ def main():
     discadj_incomp_turb_NACA0012_sst.cfg_dir   = "disc_adj_incomp_rans/naca0012"
     discadj_incomp_turb_NACA0012_sst.cfg_file  = "turb_naca0012_sst.cfg"
     discadj_incomp_turb_NACA0012_sst.test_iter = 10
-    discadj_incomp_turb_NACA0012_sst.test_vals = [-3.845577, -2.414021, -8.420183, 0.000000] #last 4 columns
+    discadj_incomp_turb_NACA0012_sst.test_vals = [-4.148134, -2.442830, -7.875040, 0, -1.076773]
     test_list.append(discadj_incomp_turb_NACA0012_sst)
 
     #######################################################

From c75a3aaa063ed88b8cc33ffc46c0f818c2ff1bac Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 2 Jul 2023 19:00:53 -0700
Subject: [PATCH 523/656] final update

---
 .github/workflows/regression.yml    |  2 +-
 TestCases/hybrid_regression_AD.py   |  2 +-
 TestCases/parallel_regression_AD.py |  8 ++++----
 TestCases/serial_regression_AD.py   | 20 --------------------
 4 files changed, 6 insertions(+), 26 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index c04724d24de..76545cdb274 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t sst_consistency -c sst_consistency -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
diff --git a/TestCases/hybrid_regression_AD.py b/TestCases/hybrid_regression_AD.py
index a5ae3786037..ed6dae1a519 100644
--- a/TestCases/hybrid_regression_AD.py
+++ b/TestCases/hybrid_regression_AD.py
@@ -129,7 +129,7 @@ def main():
     discadj_incomp_turb_NACA0012_sst.cfg_dir   = "disc_adj_incomp_rans/naca0012"
     discadj_incomp_turb_NACA0012_sst.cfg_file  = "turb_naca0012_sst.cfg"
     discadj_incomp_turb_NACA0012_sst.test_iter = 10
-    discadj_incomp_turb_NACA0012_sst.test_vals = [-4.148134, -2.442830, -7.875040, 0, -1.076773]
+    discadj_incomp_turb_NACA0012_sst.test_vals = [-4.029282, -2.181911, -7.734686, 0.000000, -0.939944]
     test_list.append(discadj_incomp_turb_NACA0012_sst)
 
     #######################################################
diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index 282ec14a9a1..93c4cabf278 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -137,8 +137,8 @@ def main():
     discadj_incomp_turb_NACA0012_sst.cfg_dir   = "disc_adj_incomp_rans/naca0012"
     discadj_incomp_turb_NACA0012_sst.cfg_file  = "turb_naca0012_sst.cfg"
     discadj_incomp_turb_NACA0012_sst.test_iter = 10
-    discadj_incomp_turb_NACA0012_sst.test_vals         = [-3.845596, -2.432265, -8.351920, 0.000000]
-    discadj_incomp_turb_NACA0012_sst.test_vals_aarch64 = [-3.845596, -2.432265, -8.351920, 0.000000]
+    discadj_incomp_turb_NACA0012_sst.test_vals         = [-4.183391, -2.287284, -7.892044, 0, -1.230919]
+    discadj_incomp_turb_NACA0012_sst.test_vals_aarch64 = [-4.183391, -2.287284, -7.892044, 0, -1.230919]
     test_list.append(discadj_incomp_turb_NACA0012_sst)
 
     ####################################################################
@@ -298,7 +298,7 @@ def main():
     da_sp_pinArray_cht_2d_dp_hf.cfg_dir   = "incomp_navierstokes/streamwise_periodic/chtPinArray_2d"
     da_sp_pinArray_cht_2d_dp_hf.cfg_file  = "DA_configMaster.cfg"
     da_sp_pinArray_cht_2d_dp_hf.test_iter = 100
-    da_sp_pinArray_cht_2d_dp_hf.test_vals = [-4.739373, -4.060562, -3.867056]
+    da_sp_pinArray_cht_2d_dp_hf.test_vals = [-4.743218, -4.059800, -4.138231]
     da_sp_pinArray_cht_2d_dp_hf.multizone = True
     test_list.append(da_sp_pinArray_cht_2d_dp_hf)
 
@@ -307,7 +307,7 @@ def main():
     da_sp_pinArray_cht_2d_mf.cfg_dir   = "incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d"
     da_sp_pinArray_cht_2d_mf.cfg_file  = "configMaster.cfg"
     da_sp_pinArray_cht_2d_mf.test_iter = 100
-    da_sp_pinArray_cht_2d_mf.test_vals = [-6.124936, -2.661408, -2.981673, -18.926294, -2.862099, -7.673088, -18.810904, -23.849963]
+    da_sp_pinArray_cht_2d_mf.test_vals = [-4.611237, -1.290668, -1.453678, -18.507826, -0.859013, -5.755971, -19.067984, -47.993931]
     da_sp_pinArray_cht_2d_mf.multizone = True
     test_list.append(da_sp_pinArray_cht_2d_mf)
 
diff --git a/TestCases/serial_regression_AD.py b/TestCases/serial_regression_AD.py
index e3a3e0b2cd5..9317f318046 100644
--- a/TestCases/serial_regression_AD.py
+++ b/TestCases/serial_regression_AD.py
@@ -110,26 +110,6 @@ def main():
     discadj_incomp_cylinder.test_vals = [20.000000, -2.373367, -2.368305, 0.000000] #last 4 columns
     test_list.append(discadj_incomp_cylinder)
 
-    ######################################
-    ### Disc. adj. incompressible RANS ###
-    ######################################
-
-    # Adjoint Incompressible Turbulent NACA 0012 SA
-    discadj_incomp_turb_NACA0012_sa           = TestCase('discadj_incomp_turb_NACA0012_sa')
-    discadj_incomp_turb_NACA0012_sa.cfg_dir   = "disc_adj_incomp_rans/naca0012"
-    discadj_incomp_turb_NACA0012_sa.cfg_file  = "turb_naca0012_sa.cfg"
-    discadj_incomp_turb_NACA0012_sa.test_iter = 10
-    discadj_incomp_turb_NACA0012_sa.test_vals = [10.000000, -3.845979, -1.031095, 0.000000] #last 4 columns
-    test_list.append(discadj_incomp_turb_NACA0012_sa)
-
-    # Adjoint Incompressible Turbulent NACA 0012 SST
-    discadj_incomp_turb_NACA0012_sst           = TestCase('discadj_incomp_turb_NACA0012_sst')
-    discadj_incomp_turb_NACA0012_sst.cfg_dir   = "disc_adj_incomp_rans/naca0012"
-    discadj_incomp_turb_NACA0012_sst.cfg_file  = "turb_naca0012_sst.cfg"
-    discadj_incomp_turb_NACA0012_sst.test_iter = 10
-    discadj_incomp_turb_NACA0012_sst.test_vals = [-4.148134, -2.442830, -7.875040, 0, -1.076773]
-    test_list.append(discadj_incomp_turb_NACA0012_sst)
-
     #######################################################
     ### Unsteady Disc. adj. compressible RANS           ###
     #######################################################

From b860fd19559712db7a541668a245e4c185da228b Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 3 Jul 2023 12:28:09 +0200
Subject: [PATCH 524/656] Fixed communication between species and heat solver
 for CHT simulations

---
 SU2_CFD/src/drivers/CDriver.cpp                        | 3 ++-
 SU2_CFD/src/interfaces/cht/CConjugateHeatInterface.cpp | 3 ++-
 SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp         | 2 +-
 3 files changed, 5 insertions(+), 3 deletions(-)

diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index 5b85ead935e..c8ead183730 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -2497,7 +2497,8 @@ void CDriver::InitializeInterface(CConfig **config, CSolver***** solver, CGeomet
 
           const auto fluidZone = heat_target? donor : target;
 
-          if (config[fluidZone]->GetEnergy_Equation() || (config[fluidZone]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE))
+          if (config[fluidZone]->GetEnergy_Equation() || (config[fluidZone]->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE) 
+              || (config[fluidZone]->GetKind_FluidModel() == ENUM_FLUIDMODEL::FLUID_FLAMELET))
             interface_type = heat_target? CONJUGATE_HEAT_FS : CONJUGATE_HEAT_SF;
           else if (config[fluidZone]->GetWeakly_Coupled_Heat())
             interface_type = heat_target? CONJUGATE_HEAT_WEAKLY_FS : CONJUGATE_HEAT_WEAKLY_SF;
diff --git a/SU2_CFD/src/interfaces/cht/CConjugateHeatInterface.cpp b/SU2_CFD/src/interfaces/cht/CConjugateHeatInterface.cpp
index 594863bb9a1..a1400ad0799 100644
--- a/SU2_CFD/src/interfaces/cht/CConjugateHeatInterface.cpp
+++ b/SU2_CFD/src/interfaces/cht/CConjugateHeatInterface.cpp
@@ -70,7 +70,8 @@ void CConjugateHeatInterface::GetDonor_Variable(CSolver *donor_solution, CGeomet
   su2double conductivity_over_dist = 0.0;
 
   const bool compressible_flow = (donor_config->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
-  const bool incompressible_flow = (donor_config->GetKind_Regime() == ENUM_REGIME::INCOMPRESSIBLE) && donor_config->GetEnergy_Equation();
+  const bool incompressible_flow = (donor_config->GetKind_Regime() == ENUM_REGIME::INCOMPRESSIBLE) && 
+                                   (donor_config->GetEnergy_Equation() || (donor_config->GetKind_FluidModel() == ENUM_FLUIDMODEL::FLUID_FLAMELET));
 
   if (compressible_flow) {
 
diff --git a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
index f79b12b232f..9c3ce1e5e1f 100644
--- a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
+++ b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
@@ -427,7 +427,7 @@ void CSpeciesFlameletSolver::BC_Isothermal_Wall_Generic(CGeometry* geometry, CSo
   for (unsigned long iVertex = 0; iVertex < geometry->nVertex[val_marker]; iVertex++) {
     unsigned long iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
-    if (cht_mode) temp_wall = GetConjugateHeatVariable(val_marker, iVertex, 0);
+    if (cht_mode) temp_wall = solver_container[FLOW_SOL]->GetConjugateHeatVariable(val_marker, iVertex, 0);
 
     /*--- Check if the node belongs to the domain (i.e., not a halo node). ---*/
 

From 13a3b311e9db675d4bea67c8dcf9b10e92d2bc6d Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 3 Jul 2023 12:50:42 +0200
Subject: [PATCH 525/656] Update container image versions.

---
 .github/workflows/regression.yml | 18 +++++++++---------
 1 file changed, 9 insertions(+), 9 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 76545cdb274..dfef77cc05d 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -52,12 +52,12 @@ jobs:
           key: ${{ matrix.config_set }}-${{ github.sha }}
           restore-keys: ${{ matrix.config_set }}
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/build-su2:230225-2136
+        uses: docker://ghcr.io/su2code/su2/build-su2:230629-0917
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
       - name: Build
-        uses: docker://ghcr.io/su2code/su2/build-su2:230225-2136
+        uses: docker://ghcr.io/su2code/su2/build-su2:230629-0917
         with:
           args: -b ${{github.ref}} -f "${{matrix.flags}}"
       - name: Compress binaries
@@ -68,7 +68,7 @@ jobs:
           name: ${{ matrix.config_set }}
           path: install_bin.tgz
       - name: Post Cleanup
-        uses: docker://ghcr.io/su2code/su2/build-su2:230225-2136
+        uses: docker://ghcr.io/su2code/su2/build-su2:230629-0917
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -99,7 +99,7 @@ jobs:
             tag: OMP
     steps:
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
+        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -125,12 +125,12 @@ jobs:
           chmod a+x $BIN_FOLDER/*
           ls -lahR $BIN_FOLDER
       - name: Run Tests in Container
-        uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
+        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
           args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
       - name: Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
+        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -151,7 +151,7 @@ jobs:
             tag: MPI
     steps:
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
+        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -212,11 +212,11 @@ jobs:
           echo $PWD
           ls -lahR
       - name: Run Unit Tests
-        uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
+        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
         with:
           entrypoint: install/bin/${{matrix.testdriver}}
       - name: Post Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
+        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}

From 73ce89b5397b15e8d7d2eb2b09a4c69173196fde Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 3 Jul 2023 15:14:53 +0200
Subject: [PATCH 526/656] Updated data-driven fluid test case

---
 TestCases/nicf/datadriven/datadriven_nozzle.cfg | 6 +++---
 TestCases/parallel_regression.py                | 4 ++--
 2 files changed, 5 insertions(+), 5 deletions(-)

diff --git a/TestCases/nicf/datadriven/datadriven_nozzle.cfg b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
index e8b133da4ff..45fc486e696 100644
--- a/TestCases/nicf/datadriven/datadriven_nozzle.cfg
+++ b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
@@ -15,7 +15,7 @@
 SOLVER= RANS
 KIND_TURB_MODEL= SST
 MATH_PROBLEM= DIRECT
-RESTART_SOL= NO
+RESTART_SOL= YES
 SYSTEM_MEASUREMENTS= SI
 %
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
@@ -89,7 +89,7 @@ CFL_REDUCTION_TURB= 1.0
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
 % Number of total iterations
-ITER= 51
+ITER= 10
 CONV_RESIDUAL_MINVAL= -24
 CONV_STARTITER= 10
 
@@ -121,7 +121,7 @@ VOLUME_FILENAME= flow
 SURFACE_FILENAME= surface_flow
 %
 % Writing solution file frequency
-OUTPUT_WRT_FREQ= 10
+OUTPUT_WRT_FREQ= 500
 %
 % Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG)
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index e31dbdf14f5..47d6bd54ff3 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -1002,8 +1002,8 @@ def main():
     datadriven_fluidModel           = TestCase('datadriven_fluidModel')
     datadriven_fluidModel.cfg_dir   = "nicf/datadriven"
     datadriven_fluidModel.cfg_file  = "datadriven_nozzle.cfg"
-    datadriven_fluidModel.test_iter = 20
-    datadriven_fluidModel.test_vals = [-1.873575, 0.964932, 5.467181, 0.000000, 0.000000]
+    datadriven_fluidModel.test_iter = 10
+    datadriven_fluidModel.test_vals = [-14.397040, -9.904042, -5.038828, 0.000000, 0.000000]
     test_list.append(datadriven_fluidModel)
 
     # Rarefaction Q1D nozzle, include CoolProp transport model

From b27849f2a0ad1554fdd479ffa17a8614a9b99548 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 3 Jul 2023 16:52:58 +0200
Subject: [PATCH 527/656] Updated data-driven fluid regression test

---
 SU2_CFD/src/solvers/CEulerSolver.cpp            | 2 +-
 SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp     | 2 +-
 TestCases/nicf/datadriven/datadriven_nozzle.cfg | 2 +-
 TestCases/parallel_regression.py                | 4 ++--
 4 files changed, 5 insertions(+), 5 deletions(-)

diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index 5b20e11ce09..1ce06058b5e 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -4627,7 +4627,7 @@ void CEulerSolver::BC_Riemann(CGeometry *geometry, CSolver **solver_container,
       StaticEnergy_i = Energy_i - 0.5*Velocity2_i;
 
       GetFluidModel()->SetTDState_rhoe(Density_i, StaticEnergy_i);
-      
+
       Pressure_i = GetFluidModel()->GetPressure();
       Enthalpy_i = Energy_i + Pressure_i/Density_i;
 
diff --git a/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp b/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
index 2c702832f40..ae9da1c7350 100644
--- a/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
@@ -7902,7 +7902,7 @@ void CFEM_DG_EulerSolver::BoundaryStates_Riemann(CConfig                  *confi
 
       P_static /= config->GetPressure_Ref();
       Rho_static /= config->GetDensity_Ref();
-      
+
       /* Compute the prescribed pressure, static energy per unit mass
          and speed of sound. */
       FluidModel->SetTDState_Prho(P_static, Rho_static);
diff --git a/TestCases/nicf/datadriven/datadriven_nozzle.cfg b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
index 45fc486e696..700f1c38865 100644
--- a/TestCases/nicf/datadriven/datadriven_nozzle.cfg
+++ b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
@@ -15,7 +15,7 @@
 SOLVER= RANS
 KIND_TURB_MODEL= SST
 MATH_PROBLEM= DIRECT
-RESTART_SOL= YES
+RESTART_SOL= NO
 SYSTEM_MEASUREMENTS= SI
 %
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 47d6bd54ff3..82597e17abe 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -1002,8 +1002,8 @@ def main():
     datadriven_fluidModel           = TestCase('datadriven_fluidModel')
     datadriven_fluidModel.cfg_dir   = "nicf/datadriven"
     datadriven_fluidModel.cfg_file  = "datadriven_nozzle.cfg"
-    datadriven_fluidModel.test_iter = 10
-    datadriven_fluidModel.test_vals = [-14.397040, -9.904042, -5.038828, 0.000000, 0.000000]
+    datadriven_fluidModel.test_iter = 50
+    datadriven_fluidModel.test_vals = [-2.623753, 0.145100, 4.688298, 0.000000, 0.000000]
     test_list.append(datadriven_fluidModel)
 
     # Rarefaction Q1D nozzle, include CoolProp transport model

From f946c26a52dffe919154c9e159fb0dc23f3292ed Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 3 Jul 2023 19:23:34 +0200
Subject: [PATCH 528/656] Specify container images as part of the job matrix.

---
 .github/workflows/regression.yml | 21 ++++++++++++---------
 1 file changed, 12 insertions(+), 9 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index dfef77cc05d..98c9432cbf7 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -25,6 +25,7 @@ jobs:
       matrix:
         config_set: [BaseMPI, ReverseMPI, ForwardMPI, BaseNoMPI, ReverseNoMPI, ForwardNoMPI, BaseOMP, ReverseOMP, ForwardOMP]
         include:
+          - container_image: docker://ghcr.io/su2code/su2/build-su2:230629-0917
           - config_set: BaseMPI
             flags: '-Denable-pywrapper=true -Denable-coolprop=true -Denable-tests=true --warnlevel=2 --werror'
           - config_set: ReverseMPI
@@ -52,12 +53,12 @@ jobs:
           key: ${{ matrix.config_set }}-${{ github.sha }}
           restore-keys: ${{ matrix.config_set }}
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/build-su2:230629-0917
+        uses: ${{ matrix.container_image }}
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
       - name: Build
-        uses: docker://ghcr.io/su2code/su2/build-su2:230629-0917
+        uses: ${{ matrix.container_image }}
         with:
           args: -b ${{github.ref}} -f "${{matrix.flags}}"
       - name: Compress binaries
@@ -68,7 +69,7 @@ jobs:
           name: ${{ matrix.config_set }}
           path: install_bin.tgz
       - name: Post Cleanup
-        uses: docker://ghcr.io/su2code/su2/build-su2:230629-0917
+        uses: ${{ matrix.container_image }}
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -81,6 +82,7 @@ jobs:
       matrix:
         testscript: ['vandv.py', 'tutorials.py', 'parallel_regression.py', 'parallel_regression_AD.py', 'serial_regression.py', 'serial_regression_AD.py', 'hybrid_regression.py', 'hybrid_regression_AD.py']
         include:
+          - container_image: docker://ghcr.io/su2code/su2/test-su2:230629-0917
           - testscript: 'vandv.py'
             tag: MPI
           - testscript: 'tutorials.py'
@@ -99,7 +101,7 @@ jobs:
             tag: OMP
     steps:
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
+        uses: ${{ matrix.container_image }}
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -125,12 +127,12 @@ jobs:
           chmod a+x $BIN_FOLDER/*
           ls -lahR $BIN_FOLDER
       - name: Run Tests in Container
-        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
+        uses: ${{ matrix.container_image }}
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
           args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
       - name: Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
+        uses: ${{ matrix.container_image }}
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -143,6 +145,7 @@ jobs:
       matrix:
         testdriver: ['test_driver', 'test_driver_AD', 'test_driver_DD']
         include:
+          - container_image: docker://ghcr.io/su2code/su2/test-su2:230629-0917
           - testdriver: 'test_driver'
             tag: MPI
           - testdriver: 'test_driver_AD'
@@ -151,7 +154,7 @@ jobs:
             tag: MPI
     steps:
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
+        uses: ${{ matrix.container_image }}
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -212,11 +215,11 @@ jobs:
           echo $PWD
           ls -lahR
       - name: Run Unit Tests
-        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
+        uses: ${{ matrix.container_image }}
         with:
           entrypoint: install/bin/${{matrix.testdriver}}
       - name: Post Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
+        uses: ${{ matrix.container_image }}
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}

From f578d93f77b9f8eb34cabd5baadec4b76d43ee80 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 3 Jul 2023 20:14:42 +0200
Subject: [PATCH 529/656] Revert "Specify container images as part of the job
 matrix."

This reverts commit f946c26a52dffe919154c9e159fb0dc23f3292ed.
---
 .github/workflows/regression.yml | 21 +++++++++------------
 1 file changed, 9 insertions(+), 12 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 98c9432cbf7..dfef77cc05d 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -25,7 +25,6 @@ jobs:
       matrix:
         config_set: [BaseMPI, ReverseMPI, ForwardMPI, BaseNoMPI, ReverseNoMPI, ForwardNoMPI, BaseOMP, ReverseOMP, ForwardOMP]
         include:
-          - container_image: docker://ghcr.io/su2code/su2/build-su2:230629-0917
           - config_set: BaseMPI
             flags: '-Denable-pywrapper=true -Denable-coolprop=true -Denable-tests=true --warnlevel=2 --werror'
           - config_set: ReverseMPI
@@ -53,12 +52,12 @@ jobs:
           key: ${{ matrix.config_set }}-${{ github.sha }}
           restore-keys: ${{ matrix.config_set }}
       - name: Pre Cleanup
-        uses: ${{ matrix.container_image }}
+        uses: docker://ghcr.io/su2code/su2/build-su2:230629-0917
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
       - name: Build
-        uses: ${{ matrix.container_image }}
+        uses: docker://ghcr.io/su2code/su2/build-su2:230629-0917
         with:
           args: -b ${{github.ref}} -f "${{matrix.flags}}"
       - name: Compress binaries
@@ -69,7 +68,7 @@ jobs:
           name: ${{ matrix.config_set }}
           path: install_bin.tgz
       - name: Post Cleanup
-        uses: ${{ matrix.container_image }}
+        uses: docker://ghcr.io/su2code/su2/build-su2:230629-0917
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -82,7 +81,6 @@ jobs:
       matrix:
         testscript: ['vandv.py', 'tutorials.py', 'parallel_regression.py', 'parallel_regression_AD.py', 'serial_regression.py', 'serial_regression_AD.py', 'hybrid_regression.py', 'hybrid_regression_AD.py']
         include:
-          - container_image: docker://ghcr.io/su2code/su2/test-su2:230629-0917
           - testscript: 'vandv.py'
             tag: MPI
           - testscript: 'tutorials.py'
@@ -101,7 +99,7 @@ jobs:
             tag: OMP
     steps:
       - name: Pre Cleanup
-        uses: ${{ matrix.container_image }}
+        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -127,12 +125,12 @@ jobs:
           chmod a+x $BIN_FOLDER/*
           ls -lahR $BIN_FOLDER
       - name: Run Tests in Container
-        uses: ${{ matrix.container_image }}
+        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
           args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
       - name: Cleanup
-        uses: ${{ matrix.container_image }}
+        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -145,7 +143,6 @@ jobs:
       matrix:
         testdriver: ['test_driver', 'test_driver_AD', 'test_driver_DD']
         include:
-          - container_image: docker://ghcr.io/su2code/su2/test-su2:230629-0917
           - testdriver: 'test_driver'
             tag: MPI
           - testdriver: 'test_driver_AD'
@@ -154,7 +151,7 @@ jobs:
             tag: MPI
     steps:
       - name: Pre Cleanup
-        uses: ${{ matrix.container_image }}
+        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -215,11 +212,11 @@ jobs:
           echo $PWD
           ls -lahR
       - name: Run Unit Tests
-        uses: ${{ matrix.container_image }}
+        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
         with:
           entrypoint: install/bin/${{matrix.testdriver}}
       - name: Post Cleanup
-        uses: ${{ matrix.container_image }}
+        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}

From 5da06cc0adc7c5e4fa6e918c1ca6fe413424d225 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 3 Jul 2023 20:21:36 +0200
Subject: [PATCH 530/656] Add separate job for tsan builds.

---
 .github/workflows/regression.yml | 42 ++++++++++++++++++++++++++++++++
 1 file changed, 42 insertions(+)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index dfef77cc05d..16de9571026 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -72,6 +72,48 @@ jobs:
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
+  build_tsan:
+    name: Build SU2 (tsan)
+    strategy:
+      fail-fast: false
+      matrix:
+        config_set: [BaseOMP, ReverseOMP, ForwardOMP]
+        include:
+          - config_set: BaseOMP
+            flags: '-Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
+          - config_set: ReverseOMP
+            flags: '-Denable-autodiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
+          - config_set: ForwardOMP
+            flags: '-Denable-directdiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
+    runs-on: ${{ inputs.runner || 'ubuntu-latest' }}
+    steps:
+      - name: Cache Object Files
+        uses: actions/cache@v3
+        with:
+          path: ccache
+          key: ${{ matrix.config_set }}-${{ github.sha }}
+          restore-keys: ${{ matrix.config_set }}
+      - name: Pre Cleanup
+        uses: docker://ghcr.io/su2code/su2/build-su2-tsan:230629-0917
+        with:
+          entrypoint: /bin/rm
+          args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
+      - name: Build
+        uses: docker://ghcr.io/su2code/su2/build-su2-tsan:230629-0917
+        with:
+          args: -b ${{github.ref}} -f "${{matrix.flags}}"
+      - name: Compress binaries
+        run: tar -zcvf install_bin.tgz install/bin
+      - name: Upload Binaries
+        uses: actions/upload-artifact@v3
+        with:
+          name: ${{ matrix.config_set }}
+          path: install_bin.tgz
+      - name: Post Cleanup
+        uses: docker://ghcr.io/su2code/su2/build-su2-tsan:230629-0917
+        with:
+          entrypoint: /bin/rm
+          args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
   regression_tests:
     runs-on: ${{ inputs.runner || 'ubuntu-latest' }}
     name: Regression Tests

From 43b10354764541f989c27fe49f836f31d941496b Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 3 Jul 2023 20:27:58 +0200
Subject: [PATCH 531/656] No tsan builds on ARM64 for now.

---
 .github/workflows/regression.yml | 1 +
 1 file changed, 1 insertion(+)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 16de9571026..e4d84c4d449 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -74,6 +74,7 @@ jobs:
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
   build_tsan:
     name: Build SU2 (tsan)
+    if: inputs.runner != 'ARM64'
     strategy:
       fail-fast: false
       matrix:

From f936984995ae12ed809c9b993c3187cf9b2efac9 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 3 Jul 2023 20:55:56 +0200
Subject: [PATCH 532/656] Use non-ambiguous names.

---
 .github/workflows/regression.yml | 8 ++++----
 1 file changed, 4 insertions(+), 4 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index e4d84c4d449..4956c96fba1 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -78,13 +78,13 @@ jobs:
     strategy:
       fail-fast: false
       matrix:
-        config_set: [BaseOMP, ReverseOMP, ForwardOMP]
+        config_set: [BaseOMP-tsan, ReverseOMP-tsan, ForwardOMP-tsan]
         include:
-          - config_set: BaseOMP
+          - config_set: BaseOMP-tsan
             flags: '-Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
-          - config_set: ReverseOMP
+          - config_set: ReverseOMP-tsan
             flags: '-Denable-autodiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
-          - config_set: ForwardOMP
+          - config_set: ForwardOMP-tsan
             flags: '-Denable-directdiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
     runs-on: ${{ inputs.runner || 'ubuntu-latest' }}
     steps:

From bd44854fbbdb36a20f24da9fb743ecc4b38cd287 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 4 Jul 2023 09:53:53 +0200
Subject: [PATCH 533/656] Removed conjugate heat variables from
 speciesFlameletSolver as they're not necessary

---
 SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp | 7 -------
 1 file changed, 7 deletions(-)

diff --git a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
index 9c3ce1e5e1f..6b1a77e281d 100644
--- a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
+++ b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
@@ -65,13 +65,6 @@ CSpeciesFlameletSolver::CSpeciesFlameletSolver(CGeometry* geometry, CConfig* con
     for (unsigned long i = 0; i < M; ++i) X[i].resize(N[i], P) = su2double(0.0);
   };
 
-  /*--- Store the values of the temperature and the heat flux density at the boundaries,
-   used for coupling with a solid donor cell. ---*/
-  constexpr auto n_conjugate_var = 4u;
-
-  Alloc3D(nMarker, nVertex, n_conjugate_var, conjugate_var);
-  for (auto& x : conjugate_var) x = config->GetTemperature_FreeStreamND();
-
   /*--- Add the solver name. ---*/
   SolverName = "FLAMELET";
 }

From 15ebb3b92ea4266ef68463a63162da4ca0e91eff Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Tue, 4 Jul 2023 11:34:18 +0200
Subject: [PATCH 534/656] Introduce --tsan argument for hybrid regression
 tests.

---
 TestCases/TestCase.py             | 6 ++++++
 TestCases/hybrid_regression.py    | 3 +++
 TestCases/hybrid_regression_AD.py | 3 +++
 3 files changed, 12 insertions(+)

diff --git a/TestCases/TestCase.py b/TestCases/TestCase.py
index 473851451e0..7a736d5ebce 100644
--- a/TestCases/TestCase.py
+++ b/TestCases/TestCase.py
@@ -28,6 +28,7 @@
 import time, os, subprocess, datetime, sys
 import difflib
 import platform
+import argparse
 
 
 def print_vals(vals, name="Values"):
@@ -41,6 +42,11 @@ def is_float(test_string):
     except ValueError:
         return False
 
+def parse_args(description: str):
+    parser = argparse.ArgumentParser(description=description)
+    parser.add_argument('--tsan', action='store_true', help='Run thread sanitizer tests. Requires a tsan-enabled SU2 build.')
+    return parser.parse_args()
+
 class TestCase:
 
     class Command:
diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index 3df7f73d9ca..64ea0ce90f6 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -30,12 +30,15 @@
 
 import sys
 from TestCase import TestCase
+from TestCase import parse_args
 
 def main():
     '''This program runs SU2 and ensures that the output matches specified values.
        This will be used to do checks when code is pushed to github
        to make sure nothing is broken. '''
 
+    args = parse_args('Hybrid Regression Tests')
+
     test_list = []
     file_diff_list = []
 
diff --git a/TestCases/hybrid_regression_AD.py b/TestCases/hybrid_regression_AD.py
index ed6dae1a519..dcbc1234dca 100644
--- a/TestCases/hybrid_regression_AD.py
+++ b/TestCases/hybrid_regression_AD.py
@@ -30,12 +30,15 @@
 
 import sys
 from TestCase import TestCase
+from TestCase import parse_args
 
 def main():
     '''This program runs SU2 and ensures that the output matches specified values.
        This will be used to do checks when code is pushed to github
        to make sure nothing is broken. '''
 
+    args = parse_args('Hybrid Regression AD Tests')
+
     test_list = []
 
     #####################################

From 3fc49d530d5fcf0e2b5b7ce2389889741889ace8 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Tue, 4 Jul 2023 13:22:22 +0200
Subject: [PATCH 535/656] Prepare python scripts for thread-sanitzer tests.

---
 TestCases/TestCase.py             | 320 +++++++++++++++---------------
 TestCases/hybrid_regression.py    |   4 +-
 TestCases/hybrid_regression_AD.py |   6 +-
 3 files changed, 169 insertions(+), 161 deletions(-)

diff --git a/TestCases/TestCase.py b/TestCases/TestCase.py
index 7a736d5ebce..af78fb93edd 100644
--- a/TestCases/TestCase.py
+++ b/TestCases/TestCase.py
@@ -113,6 +113,7 @@ def __init__(self,tag_in):
         self.test_vals_aarch64 = []
         self.cpu_arch = platform.processor()
         self.enabled_on_cpu_arch = ["x86_64", "aarch64"]
+        self.enabled_with_tsan = True
         self.command = self.Command()
         self.timeout = 0
         self.tol = 0.0
@@ -124,9 +125,9 @@ def __init__(self,tag_in):
         self.reference_file_aarch64 = ""
         self.test_file      = "of_grad.dat"
 
-    def run_test(self):
+    def run_test(self, running_with_tsan=False):
 
-        if not self.is_enabled():
+        if not self.is_enabled(running_with_tsan):
             return True
 
         print('==================== Start Test: %s ===================='%self.tag)
@@ -182,54 +183,55 @@ def run_test(self):
                 timed_out = True
                 passed    = False
 
-        # Examine the output
-        f = open(logfilename,'r')
-        output = f.readlines()
-        delta_vals = []
-        sim_vals = []
-        if not timed_out and len(self.test_vals) != 0:
-            start_solver = False
-            for line in output:
-                if not start_solver: # Don't bother parsing anything before --Start solver ---
-                    if line.find('Begin Solver') > -1:
-                        start_solver=True
-                else:   # Found the --Begin solver --- line; parse the input
-                    if self.new_output or self.multizone:
-                        raw_data = line.strip() # Strip removes whitespaces head-tail
-                        raw_data = raw_data[1:-1].split('|') # Remove heat-tail bars before splitting
-                    else:
-                        raw_data = line.split()
-                    try:
-                        iter_number = int(raw_data[0])
-                        if self.unsteady and not self.multizone and not self.new_output:
-                            iter_number = int(raw_data[1])
-                        data = raw_data[len(raw_data) - len(self.test_vals):]
-                    except ValueError:
-                        continue
-                    except IndexError:
-                        continue
-
-                    if iter_number == self.test_iter:  # Found the iteration number we're checking for
-                        iter_missing = False
-                        if not len(self.test_vals)==len(data):   # something went wrong... probably bad input
-                            print("Error in test_vals!")
-                            passed = False
+        if not running_with_tsan: # tsan findings result in non-zero return code, no need to examine the output
+            # Examine the output
+            f = open(logfilename,'r')
+            output = f.readlines()
+            delta_vals = []
+            sim_vals = []
+            if not timed_out and len(self.test_vals) != 0:
+                start_solver = False
+                for line in output:
+                    if not start_solver: # Don't bother parsing anything before --Start solver ---
+                        if line.find('Begin Solver') > -1:
+                            start_solver=True
+                    else:   # Found the --Begin solver --- line; parse the input
+                        if self.new_output or self.multizone:
+                            raw_data = line.strip() # Strip removes whitespaces head-tail
+                            raw_data = raw_data[1:-1].split('|') # Remove heat-tail bars before splitting
+                        else:
+                            raw_data = line.split()
+                        try:
+                            iter_number = int(raw_data[0])
+                            if self.unsteady and not self.multizone and not self.new_output:
+                                iter_number = int(raw_data[1])
+                            data = raw_data[len(raw_data) - len(self.test_vals):]
+                        except ValueError:
+                            continue
+                        except IndexError:
+                            continue
+
+                        if iter_number == self.test_iter:  # Found the iteration number we're checking for
+                            iter_missing = False
+                            if not len(self.test_vals)==len(data):   # something went wrong... probably bad input
+                                print("Error in test_vals!")
+                                passed = False
+                                break
+                            for j in range(len(data)):
+                                sim_vals.append( float(data[j]) )
+                                delta_vals.append( abs(float(data[j])-self.test_vals[j]) )
+                                if delta_vals[j] > self.tol:
+                                    exceed_tol = True
+                                    passed     = False
                             break
-                        for j in range(len(data)):
-                            sim_vals.append( float(data[j]) )
-                            delta_vals.append( abs(float(data[j])-self.test_vals[j]) )
-                            if delta_vals[j] > self.tol:
-                                exceed_tol = True
-                                passed     = False
-                        break
-                    else:
-                        iter_missing = True
+                        else:
+                            iter_missing = True
 
-            if not start_solver:
-                passed = False
+                if not start_solver:
+                    passed = False
 
-            if iter_missing:
-                passed = False
+                if iter_missing:
+                    passed = False
 
         # Write the test results
         #for j in output:
@@ -257,7 +259,7 @@ def run_test(self):
         if not start_solver:
             print('ERROR: The code was not able to get to the "Begin solver" section.')
 
-        if iter_missing:
+        if not running_with_tsan and iter_missing:
             print('ERROR: The iteration number %d could not be found.'%self.test_iter)
 
         print('CPU architecture=%s' % self.cpu_arch)
@@ -278,9 +280,9 @@ def run_test(self):
         os.chdir(workdir)
         return passed
 
-    def run_filediff(self):
+    def run_filediff(self, running_with_tsan=False):
 
-        if not self.is_enabled():
+        if not self.is_enabled(running_with_tsan):
             return True
 
         print('==================== Start Test: %s ===================='%self.tag)
@@ -327,136 +329,137 @@ def run_filediff(self):
             print("Output from the failed case:")
             subprocess.call(["cat", logfilename])
 
-        diff_time_start = datetime.datetime.now()
-        if not timed_out and passed:
-            # Compare files
-            fromfile = self.reference_file
-            tofile = self.test_file
-            # Initial value s.t. will fail if it does not get to diff step
-            diff = ''
-            try:
-                fromdate = time.ctime(os.stat(fromfile).st_mtime)
-                fromlines = open(fromfile, 'U').readlines()
+        if not running_with_tsan: # thread sanitizer tests only check the return code, no need to compare outputs
+            diff_time_start = datetime.datetime.now()
+            if not timed_out and passed:
+                # Compare files
+                fromfile = self.reference_file
+                tofile = self.test_file
+                # Initial value s.t. will fail if it does not get to diff step
+                diff = ''
                 try:
-                    todate = time.ctime(os.stat(tofile).st_mtime)
-                    tolines = open(tofile, 'U').readlines()
+                    fromdate = time.ctime(os.stat(fromfile).st_mtime)
+                    fromlines = open(fromfile, 'U').readlines()
+                    try:
+                        todate = time.ctime(os.stat(tofile).st_mtime)
+                        tolines = open(tofile, 'U').readlines()
 
-                    # If file tolerance is set to 0, make regular diff
-                    if self.tol_file_percent == 0.0:
-                        diff = list(difflib.unified_diff(fromlines, tolines, fromfile, tofile, fromdate, todate))
+                        # If file tolerance is set to 0, make regular diff
+                        if self.tol_file_percent == 0.0:
+                            diff = list(difflib.unified_diff(fromlines, tolines, fromfile, tofile, fromdate, todate))
 
-                    # Else test word by word with given tolerance
-                    else:
+                        # Else test word by word with given tolerance
+                        else:
 
-                        diff = []
-                        max_delta = 0
-                        compare_counter = 0
-                        ignore_counter = 0
+                            diff = []
+                            max_delta = 0
+                            compare_counter = 0
+                            ignore_counter = 0
 
-                        # Assert that both files have the same number of lines
-                        if len(fromlines) != len(tolines):
-                            diff = ["ERROR: Number of lines in " + fromfile + " and " + tofile + " differ."]
-                            passed = False
-                        
-                        # Loop through all lines
-                        for i_line in range(0, len(fromlines)):
+                            # Assert that both files have the same number of lines
+                            if len(fromlines) != len(tolines):
+                                diff = ["ERROR: Number of lines in " + fromfile + " and " + tofile + " differ."]
+                                passed = False
+                            
+                            # Loop through all lines
+                            for i_line in range(0, len(fromlines)):
 
-                            if passed == False: break
+                                if passed == False: break
 
-                            # Extract next line and split it
-                            from_line = fromlines[i_line].split()
-                            to_line = tolines[i_line].split()
+                                # Extract next line and split it
+                                from_line = fromlines[i_line].split()
+                                to_line = tolines[i_line].split()
 
-                            # Assert that both lines have the same number of words
-                            if len(from_line) != len(to_line):
-                                diff = ["ERROR: Number of words in line " + str(i_line+1) + " differ."]
-                                passed = False
-                                break
-                            
-                            # Loop through all words of one line
-                            for i_word in range(0, len(from_line)):
-
-                                # Extract next word and strip whitespace and commas
-                                from_word = from_line[i_word].strip().strip(',')
-                                to_word = to_line[i_word].strip().strip(',')
-
-                                # Assert that words are either both numeric or both non-numeric
-                                from_isfloat = is_float(from_word)
-                                to_isfloat = is_float(to_word)
-                                if from_isfloat != to_isfloat:
-                                    diff = ["ERROR: File entries '" + from_word + "' and '" + to_word + "' in line " + str(i_line+1) + ", word " + str(i_word+1) + " differ."]
+                                # Assert that both lines have the same number of words
+                                if len(from_line) != len(to_line):
+                                    diff = ["ERROR: Number of words in line " + str(i_line+1) + " differ."]
                                     passed = False
-                                    delta = 0.0
-                                    max_delta = "Not applicable"
                                     break
 
-                                # Make actual comparison
-                                # Compare floats
-                                if from_isfloat:
-                                    try:
-                                        # Only do a relative comparison when the threshold is met.
-                                        # This is to prevent large relative differences for very small numbers.
-                                        if (abs(float(from_word)) > self.comp_threshold):
-                                            delta = abs( (float(from_word) - float(to_word)) / float(from_word) ) * 100
-                                            compare_counter += 1
-                                        else:
-                                            delta = 0.0
-                                            ignore_counter += 1
-
-                                        max_delta = max(max_delta, delta)
+                                # Loop through all words of one line
+                                for i_word in range(0, len(from_line)):
 
-                                    except ZeroDivisionError:
-                                        ignore_counter += 1
-                                        continue
+                                    # Extract next word and strip whitespace and commas
+                                    from_word = from_line[i_word].strip().strip(',')
+                                    to_word = to_line[i_word].strip().strip(',')
 
-                                # Compare non-floats
-                                else:
-                                    delta = 0.0
-                                    compare_counter += 1
-                                    if from_word != to_word:
+                                    # Assert that words are either both numeric or both non-numeric
+                                    from_isfloat = is_float(from_word)
+                                    to_isfloat = is_float(to_word)
+                                    if from_isfloat != to_isfloat:
                                         diff = ["ERROR: File entries '" + from_word + "' and '" + to_word + "' in line " + str(i_line+1) + ", word " + str(i_word+1) + " differ."]
                                         passed = False
+                                        delta = 0.0
                                         max_delta = "Not applicable"
                                         break
 
-                                if delta > self.tol_file_percent:
-                                    diff = ["ERROR: File entries '" + from_word + "' and '" + to_word + "' in line " + str(i_line+1) + ", word " + str(i_word+1) + " differ."]
-                                    passed = False
-                                    break
+                                    # Make actual comparison
+                                    # Compare floats
+                                    if from_isfloat:
+                                        try:
+                                            # Only do a relative comparison when the threshold is met.
+                                            # This is to prevent large relative differences for very small numbers.
+                                            if (abs(float(from_word)) > self.comp_threshold):
+                                                delta = abs( (float(from_word) - float(to_word)) / float(from_word) ) * 100
+                                                compare_counter += 1
+                                            else:
+                                                delta = 0.0
+                                                ignore_counter += 1
+
+                                            max_delta = max(max_delta, delta)
+
+                                        except ZeroDivisionError:
+                                            ignore_counter += 1
+                                            continue
+
+                                    # Compare non-floats
+                                    else:
+                                        delta = 0.0
+                                        compare_counter += 1
+                                        if from_word != to_word:
+                                            diff = ["ERROR: File entries '" + from_word + "' and '" + to_word + "' in line " + str(i_line+1) + ", word " + str(i_word+1) + " differ."]
+                                            passed = False
+                                            max_delta = "Not applicable"
+                                            break
+
+                                    if delta > self.tol_file_percent:
+                                        diff = ["ERROR: File entries '" + from_word + "' and '" + to_word + "' in line " + str(i_line+1) + ", word " + str(i_word+1) + " differ."]
+                                        passed = False
+                                        break
 
+                    except OSError:
+                        print("OS error, most likely from missing reference file:", fromfile)
+                        print("Current working directory contents:")
+                        print(os.listdir("."))
                 except OSError:
                     print("OS error, most likely from missing reference file:", fromfile)
                     print("Current working directory contents:")
                     print(os.listdir("."))
-            except OSError:
-                print("OS error, most likely from missing reference file:", fromfile)
-                print("Current working directory contents:")
-                print(os.listdir("."))
 
-            if (diff==[]):
-                passed=True
-            else:
-                for line in diff:
-                    print(line[:-1])
-                passed=False
+                if (diff==[]):
+                    passed=True
+                else:
+                    for line in diff:
+                        print(line[:-1])
+                    passed=False
 
-        else:
-            passed = False
+            else:
+                passed = False
 
-        # Report results
-        diff_time_stop = datetime.datetime.now()
-        diff_time = (diff_time_stop - diff_time_start).microseconds
+            # Report results
+            diff_time_stop = datetime.datetime.now()
+            diff_time = (diff_time_stop - diff_time_start).microseconds
 
-        print('CPU architecture:    %s'%self.cpu_arch)
-        print('Test duration:       %.2f min'%(running_time/60.0))
-        print('Diff duration:       %.2f sec'%(diff_time/1e6))
-        print('Specified tolerance: ' + str(self.tol_file_percent) + '%')
-        print('Specified threshold: ' + str(self.comp_threshold)) 
+            print('CPU architecture:    %s'%self.cpu_arch)
+            print('Test duration:       %.2f min'%(running_time/60.0))
+            print('Diff duration:       %.2f sec'%(diff_time/1e6))
+            print('Specified tolerance: ' + str(self.tol_file_percent) + '%')
+            print('Specified threshold: ' + str(self.comp_threshold))
 
-        if self.tol_file_percent != 0.0:
-            print('Compared entries:    ' + str(compare_counter))
-            print('Ignored entries:     ' + str(ignore_counter))
-            print('Maximum difference:  ' + str(max_delta) + '%')
+            if self.tol_file_percent != 0.0:
+                print('Compared entries:    ' + str(compare_counter))
+                print('Ignored entries:     ' + str(ignore_counter))
+                print('Maximum difference:  ' + str(max_delta) + '%')
 
         print('==================== End Test: %s ====================\n'%self.tag)
 
@@ -924,13 +927,18 @@ def disable_restart(self):
 
         return
 
-    def is_enabled(self):
-        is_enabled = self.cpu_arch in self.enabled_on_cpu_arch
+    def is_enabled(self, running_with_tsan=False):
+        is_enabled_on_arch = self.cpu_arch in self.enabled_on_cpu_arch
 
-        if not is_enabled:
+        if not is_enabled_on_arch:
             print('Ignoring test "%s" because it is not enabled for the current CPU architecture: %s' % (self.tag, self.cpu_arch))
 
-        return is_enabled
+        tsan_compatible = not running_with_tsan or self.enabled_with_tsan
+
+        if not tsan_compatible:
+            print('Ignoring test "%s" because it is not enabled to run with the thread sanitizer.' % self.tag)
+
+        return is_enabled_on_arch and tsan_compatible
 
     def adjust_test_data(self):
 
diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index 64ea0ce90f6..0927c4c21a4 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -795,8 +795,8 @@ def main():
         test.tol = 1e-4
     #end
 
-    pass_list = [ test.run_test() for test in test_list ]
-    pass_list += [ test.run_filediff() for test in file_diff_list ]
+    pass_list = [ test.run_test(args.tsan) for test in test_list ]
+    pass_list += [ test.run_filediff(args.tsan) for test in file_diff_list ]
 
     # Tests summary
     print('==================================================================')
diff --git a/TestCases/hybrid_regression_AD.py b/TestCases/hybrid_regression_AD.py
index dcbc1234dca..481abbbe483 100644
--- a/TestCases/hybrid_regression_AD.py
+++ b/TestCases/hybrid_regression_AD.py
@@ -223,7 +223,7 @@ def main():
         test.tol = 1e-4
     #end
 
-    pass_list = [ test.run_test() for test in test_list ]
+    pass_list = [ test.run_test(args.tsan) for test in test_list ]
 
     ###################################
     ### Python Wrapper              ###
@@ -240,7 +240,7 @@ def main():
     pywrapper_FEA_AD_FlowLoad.tol           = 1e-4
     pywrapper_FEA_AD_FlowLoad.new_output    = False
     test_list.append(pywrapper_FEA_AD_FlowLoad)
-    pass_list.append(pywrapper_FEA_AD_FlowLoad.run_test())
+    pass_list.append(pywrapper_FEA_AD_FlowLoad.run_test(args.tsan))
 
     # Flow AD Mesh Displacement Sensitivity
     pywrapper_CFD_AD_MeshDisp               = TestCase('pywrapper_CFD_AD_MeshDisp')
@@ -253,7 +253,7 @@ def main():
     pywrapper_CFD_AD_MeshDisp.tol           = 1e-4
     pywrapper_CFD_AD_MeshDisp.new_output    = False
     test_list.append(pywrapper_CFD_AD_MeshDisp)
-    pass_list.append(pywrapper_CFD_AD_MeshDisp.run_test())
+    pass_list.append(pywrapper_CFD_AD_MeshDisp.run_test(args.tsan))
 
 
     # Tests summary

From 48b094afae24bbb92a7bf05662036f5b7f87869b Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 4 Jul 2023 13:53:58 +0200
Subject: [PATCH 536/656] Implemented compatibility check for flamelet + weakly
 coupled heat

---
 .github/workflows/regression.yml               | 2 +-
 Common/src/CConfig.cpp                         | 5 +++++
 SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp | 7 -------
 3 files changed, 6 insertions(+), 8 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 76545cdb274..5b533bfd4e0 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c bug_fix_cht_flamelet -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index ace96e28cbb..3a28e257e5e 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -3947,6 +3947,11 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
         SU2_MPI::Error("The use of FLUID_FLAMELET requires the VISCOSITY_MODEL option to be FLAMELET",
                        CURRENT_FUNCTION);
       }
+
+      if (Weakly_Coupled_Heat) {
+        SU2_MPI::Error("The use of FLUID_FLAMELET is incompatible with WEAKLY_COUPLED_HEAT in the same zone.",
+                       CURRENT_FUNCTION);
+      }
     }
 
     /*--- Check for Measurement System ---*/
diff --git a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
index 6b1a77e281d..d6dc98a9323 100644
--- a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
+++ b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
@@ -58,13 +58,6 @@ CSpeciesFlameletSolver::CSpeciesFlameletSolver(CGeometry* geometry, CConfig* con
   Max_CFL_Local = CFL;
   Avg_CFL_Local = CFL;
 
-  /*--- Allocates a 3D array with variable "middle" sizes and init to 0. ---*/
-
-  auto Alloc3D = [](unsigned long M, const vector<unsigned long>& N, unsigned long P, vector<su2activematrix>& X) {
-    X.resize(M);
-    for (unsigned long i = 0; i < M; ++i) X[i].resize(N[i], P) = su2double(0.0);
-  };
-
   /*--- Add the solver name. ---*/
   SolverName = "FLAMELET";
 }

From 2a0fd69a8f9ad02d20aa16e385b7c2bcf28c137b Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Tue, 4 Jul 2023 14:03:41 +0200
Subject: [PATCH 537/656] Updated regression values for data-driven fluid test
 case

---
 TestCases/parallel_regression.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index b6944c7b033..94deb08de2f 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -1003,7 +1003,7 @@ def main():
     datadriven_fluidModel.cfg_dir   = "nicf/datadriven"
     datadriven_fluidModel.cfg_file  = "datadriven_nozzle.cfg"
     datadriven_fluidModel.test_iter = 50
-    datadriven_fluidModel.test_vals = [-2.623753, 0.145100, 4.688298, 0.000000, 0.000000]
+    datadriven_fluidModel.test_vals = [-2.623890, 0.145236, 4.688439, 0.000000, 0.000000]
     test_list.append(datadriven_fluidModel)
 
     # Rarefaction Q1D nozzle, include CoolProp transport model

From 780fb2d4135e1261ed961631b68de14191579a83 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Tue, 4 Jul 2023 18:09:23 +0200
Subject: [PATCH 538/656] Update container image versions.

---
 .github/workflows/regression.yml | 24 ++++++++++++------------
 1 file changed, 12 insertions(+), 12 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 4956c96fba1..965f19c31f2 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -52,12 +52,12 @@ jobs:
           key: ${{ matrix.config_set }}-${{ github.sha }}
           restore-keys: ${{ matrix.config_set }}
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/build-su2:230629-0917
+        uses: docker://ghcr.io/su2code/su2/build-su2:230704-1323
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
       - name: Build
-        uses: docker://ghcr.io/su2code/su2/build-su2:230629-0917
+        uses: docker://ghcr.io/su2code/su2/build-su2:230704-1323
         with:
           args: -b ${{github.ref}} -f "${{matrix.flags}}"
       - name: Compress binaries
@@ -68,7 +68,7 @@ jobs:
           name: ${{ matrix.config_set }}
           path: install_bin.tgz
       - name: Post Cleanup
-        uses: docker://ghcr.io/su2code/su2/build-su2:230629-0917
+        uses: docker://ghcr.io/su2code/su2/build-su2:230704-1323
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -95,12 +95,12 @@ jobs:
           key: ${{ matrix.config_set }}-${{ github.sha }}
           restore-keys: ${{ matrix.config_set }}
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/build-su2-tsan:230629-0917
+        uses: docker://ghcr.io/su2code/su2/build-su2-tsan:230704-1323
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
       - name: Build
-        uses: docker://ghcr.io/su2code/su2/build-su2-tsan:230629-0917
+        uses: docker://ghcr.io/su2code/su2/build-su2-tsan:230704-1323
         with:
           args: -b ${{github.ref}} -f "${{matrix.flags}}"
       - name: Compress binaries
@@ -111,7 +111,7 @@ jobs:
           name: ${{ matrix.config_set }}
           path: install_bin.tgz
       - name: Post Cleanup
-        uses: docker://ghcr.io/su2code/su2/build-su2-tsan:230629-0917
+        uses: docker://ghcr.io/su2code/su2/build-su2-tsan:230704-1323
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -142,7 +142,7 @@ jobs:
             tag: OMP
     steps:
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
+        uses: docker://ghcr.io/su2code/su2/test-su2:230704-1323
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -168,12 +168,12 @@ jobs:
           chmod a+x $BIN_FOLDER/*
           ls -lahR $BIN_FOLDER
       - name: Run Tests in Container
-        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
+        uses: docker://ghcr.io/su2code/su2/test-su2:230704-1323
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
           args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
       - name: Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
+        uses: docker://ghcr.io/su2code/su2/test-su2:230704-1323
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -194,7 +194,7 @@ jobs:
             tag: MPI
     steps:
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
+        uses: docker://ghcr.io/su2code/su2/test-su2:230704-1323
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -255,11 +255,11 @@ jobs:
           echo $PWD
           ls -lahR
       - name: Run Unit Tests
-        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
+        uses: docker://ghcr.io/su2code/su2/test-su2:230704-1323
         with:
           entrypoint: install/bin/${{matrix.testdriver}}
       - name: Post Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:230629-0917
+        uses: docker://ghcr.io/su2code/su2/test-su2:230704-1323
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}

From ae3d799c64da55651967cf39d671fc3cce56bf78 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Tue, 4 Jul 2023 18:10:01 +0200
Subject: [PATCH 539/656] Define variables outside the if block.

---
 TestCases/TestCase.py | 5 +++--
 1 file changed, 3 insertions(+), 2 deletions(-)

diff --git a/TestCases/TestCase.py b/TestCases/TestCase.py
index af78fb93edd..757c0520a50 100644
--- a/TestCases/TestCase.py
+++ b/TestCases/TestCase.py
@@ -183,12 +183,13 @@ def run_test(self, running_with_tsan=False):
                 timed_out = True
                 passed    = False
 
+        delta_vals = []
+        sim_vals = []
+
         if not running_with_tsan: # tsan findings result in non-zero return code, no need to examine the output
             # Examine the output
             f = open(logfilename,'r')
             output = f.readlines()
-            delta_vals = []
-            sim_vals = []
             if not timed_out and len(self.test_vals) != 0:
                 start_solver = False
                 for line in output:

From f192be1c23881b682ad74203f4d5a4a7de913668 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 5 Jul 2023 12:42:53 +0200
Subject: [PATCH 540/656] Add thread sanitizer tests to the workflow.

---
 .github/workflows/regression.yml | 45 ++++++++++++++++++++++++++++++++
 1 file changed, 45 insertions(+)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 965f19c31f2..867b022a0ca 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -177,6 +177,51 @@ jobs:
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
+  thread_sanitizer_tests:
+    runs-on: ${{ inputs.runner || 'ubuntu-latest' }}
+    name: Thread Sanitizer Tests
+    needs: build
+    strategy:
+      fail-fast: false
+      matrix:
+        testscript: ['hybrid_regression.py', 'hybrid_regression_AD.py']
+    steps:
+      - name: Pre Cleanup
+        uses: docker://ghcr.io/su2code/su2/test-su2-tsan:230704-1323
+        with:
+          entrypoint: /bin/rm
+          args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
+      - name: Download All artifacts
+        uses: actions/download-artifact@v3
+      - name: Uncompress and Move Binaries
+        run: |
+          BIN_FOLDER="$PWD/install/bin"
+          mkdir -p $BIN_FOLDER
+          ls -lah $BIN_FOLDER
+          for type in Base Reverse Forward; do
+            TYPE_FOLDER="${type}OMP-tsan"
+            echo "Processing '$TYPE_FOLDER' ..."
+            if [ -d $TYPE_FOLDER ]; then
+              pushd $TYPE_FOLDER
+              ls -lah
+              tar -zxvf install_bin.tgz
+              ls -lah install/bin/
+              cp -r install/bin/* $BIN_FOLDER;
+              popd;
+            fi
+          done
+          chmod a+x $BIN_FOLDER/*
+          ls -lahR $BIN_FOLDER
+      - name: Run Tests in Container
+        uses: docker://ghcr.io/su2code/su2/test-su2-tsan:230704-1323
+        with:
+          # -t <Tutorials-branch> -c <Testcases-branch>
+          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
+      - name: Cleanup
+        uses: docker://ghcr.io/su2code/su2/test-su2-tsan:230704-1323
+        with:
+          entrypoint: /bin/rm
+          args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
   unit_tests:
     runs-on: ${{ inputs.runner || 'ubuntu-latest' }}
     name: Unit Tests

From 1a519ccd948e4858b056e82e4a6abb7d2efef720 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 5 Jul 2023 12:44:42 +0200
Subject: [PATCH 541/656] Fix dependency.

---
 .github/workflows/regression.yml | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 867b022a0ca..bec3fa8e66d 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -180,7 +180,7 @@ jobs:
   thread_sanitizer_tests:
     runs-on: ${{ inputs.runner || 'ubuntu-latest' }}
     name: Thread Sanitizer Tests
-    needs: build
+    needs: build_tsan
     strategy:
       fail-fast: false
       matrix:

From 955be02557a075f4e5e2c70f7d6fb929035af1f9 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 5 Jul 2023 12:46:50 +0200
Subject: [PATCH 542/656] Skip thread sanitizer tests on ARM64 for now.

---
 .github/workflows/regression.yml | 1 +
 1 file changed, 1 insertion(+)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index bec3fa8e66d..dc2e956a85b 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -178,6 +178,7 @@ jobs:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
   thread_sanitizer_tests:
+    if: inputs.runner != 'ARM64'
     runs-on: ${{ inputs.runner || 'ubuntu-latest' }}
     name: Thread Sanitizer Tests
     needs: build_tsan

From 177e889afa8d46d4c792e8164bfc8833aa6376bd Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 5 Jul 2023 12:47:04 +0200
Subject: [PATCH 543/656] Add --tsan parameter.

---
 .github/workflows/regression.yml | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index dc2e956a85b..bcb01918b1f 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -217,7 +217,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2-tsan:230704-1323
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}} -a "--tsan"
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2-tsan:230704-1323
         with:

From e0a63519a0d717b53386d1b1ceb69a924352f0ff Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 5 Jul 2023 14:34:42 +0200
Subject: [PATCH 544/656] Exclude pywrapper tests from tsan testing.

---
 TestCases/hybrid_regression_AD.py | 2 ++
 1 file changed, 2 insertions(+)

diff --git a/TestCases/hybrid_regression_AD.py b/TestCases/hybrid_regression_AD.py
index 481abbbe483..0bcfc971a95 100644
--- a/TestCases/hybrid_regression_AD.py
+++ b/TestCases/hybrid_regression_AD.py
@@ -239,6 +239,7 @@ def main():
     pywrapper_FEA_AD_FlowLoad.timeout       = 1600
     pywrapper_FEA_AD_FlowLoad.tol           = 1e-4
     pywrapper_FEA_AD_FlowLoad.new_output    = False
+    pywrapper_FEA_AD_FlowLoad.enabled_with_tsan = False
     test_list.append(pywrapper_FEA_AD_FlowLoad)
     pass_list.append(pywrapper_FEA_AD_FlowLoad.run_test(args.tsan))
 
@@ -252,6 +253,7 @@ def main():
     pywrapper_CFD_AD_MeshDisp.timeout       = 1600
     pywrapper_CFD_AD_MeshDisp.tol           = 1e-4
     pywrapper_CFD_AD_MeshDisp.new_output    = False
+    pywrapper_CFD_AD_MeshDisp.enabled_with_tsan = False
     test_list.append(pywrapper_CFD_AD_MeshDisp)
     pass_list.append(pywrapper_CFD_AD_MeshDisp.run_test(args.tsan))
 

From 1e6e9d4a18f78a9e335dbf722a75a92fd0ad2520 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 5 Jul 2023 14:45:03 +0200
Subject: [PATCH 545/656] Disable hybrid AD tsan tests that take too long.

---
 TestCases/hybrid_regression_AD.py | 4 ++++
 1 file changed, 4 insertions(+)

diff --git a/TestCases/hybrid_regression_AD.py b/TestCases/hybrid_regression_AD.py
index 0bcfc971a95..2d939abd8a4 100644
--- a/TestCases/hybrid_regression_AD.py
+++ b/TestCases/hybrid_regression_AD.py
@@ -146,6 +146,7 @@ def main():
     discadj_cylinder.test_iter = 9
     discadj_cylinder.test_vals = [3.746907, -1.544882, -0.008321, 0.000014]
     discadj_cylinder.unsteady  = True
+    discadj_cylinder.enabled_with_tsan = False
     test_list.append(discadj_cylinder)
 
     ##############################################################
@@ -159,6 +160,7 @@ def main():
     discadj_cylinder.test_iter = 9
     discadj_cylinder.test_vals = [3.004402]
     discadj_cylinder.unsteady  = True
+    discadj_cylinder.enabled_with_tsan = False
     test_list.append(discadj_cylinder)
 
     ##########################################################################
@@ -172,6 +174,7 @@ def main():
     discadj_DT_1ST_cylinder.test_iter = 9
     discadj_DT_1ST_cylinder.test_vals = [3.698167, -1.607051, -0.002159, 0.000028]
     discadj_DT_1ST_cylinder.unsteady  = True
+    discadj_DT_1ST_cylinder.enabled_with_tsan = False
     test_list.append(discadj_DT_1ST_cylinder)
 
     ######################################################
@@ -185,6 +188,7 @@ def main():
     discadj_pitchingNACA0012.test_iter = 4
     discadj_pitchingNACA0012.test_vals = [-1.219713, -1.645717, -0.007513, 0.000013]
     discadj_pitchingNACA0012.unsteady  = True
+    discadj_pitchingNACA0012.enabled_with_tsan = False
     test_list.append(discadj_pitchingNACA0012)
 
     #######################################################

From f95fadd23e064a607d3388dfb8bc2892aaa6cca8 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 5 Jul 2023 15:05:18 +0200
Subject: [PATCH 546/656] Exclude further pywrapper tests.

---
 TestCases/hybrid_regression.py | 2 ++
 1 file changed, 2 insertions(+)

diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index 0927c4c21a4..1579251d565 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -771,6 +771,7 @@ def main():
     pywrapper_translating_naca0012.reference_file_aarch64 = "forces_0_aarch64.csv.ref"
     pywrapper_translating_naca0012.test_file = "forces_0.csv"
     pywrapper_translating_naca0012.enabled_on_cpu_arch = ["x86_64"]
+    pywrapper_translating_naca0012.enabled_with_tsan = False
     file_diff_list.append(pywrapper_translating_naca0012)
 
     # NACA0012 with updated moving frame
@@ -783,6 +784,7 @@ def main():
     pywrapper_updated_moving_frame_naca0012.reference_file_aarch64 = "forces_0_aarch64.csv.ref"
     pywrapper_updated_moving_frame_naca0012.test_file = "forces_0.csv"
     pywrapper_updated_moving_frame_naca0012.enabled_on_cpu_arch = ["x86_64"]
+    pywrapper_updated_moving_frame_naca0012.enabled_with_tsan = False
     file_diff_list.append(pywrapper_updated_moving_frame_naca0012)
 
     ######################################

From a981cacc7141e10610fd7ad41c6af3ef6d95b9c6 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 5 Jul 2023 15:47:43 +0200
Subject: [PATCH 547/656] Disable hybrid tsan tests that take too long.

---
 TestCases/hybrid_regression.py | 6 ++++++
 1 file changed, 6 insertions(+)

diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index 1579251d565..2fbc6cf5c4e 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -481,6 +481,7 @@ def main():
     cosine_gust.test_iter = 79
     cosine_gust.test_vals = [-2.418813, 0.004650, -0.001878, -0.000637, -0.000271]
     cosine_gust.unsteady  = True
+    cosine_gust.enabled_with_tsan = False
     test_list.append(cosine_gust)
 
     # Gust with mesh deformation
@@ -490,6 +491,7 @@ def main():
     gust_mesh_defo.test_iter = 6
     gust_mesh_defo.test_vals = [-1.844778, 0.000846, -0.000408]
     gust_mesh_defo.unsteady  = True
+    gust_mesh_defo.enabled_with_tsan = False
     test_list.append(gust_mesh_defo)
 
     # Aeroelastic
@@ -501,6 +503,7 @@ def main():
     aeroelastic.test_vals_aarch64 = [0.074836, 0.033102, -0.001650, -0.000127]
     aeroelastic.unsteady  = True
     aeroelastic.enabled_on_cpu_arch = ["x86_64"] # Requires AVX-capable architecture
+    aeroelastic.enabled_with_tsan = False
     test_list.append(aeroelastic)
 
     # Delayed Detached Eddy Simulation
@@ -528,6 +531,7 @@ def main():
     unst_deforming_naca0012.test_iter = 5
     unst_deforming_naca0012.test_vals = [-3.665120, -3.793643, -3.716518, -3.148310]
     unst_deforming_naca0012.unsteady  = True
+    unst_deforming_naca0012.enabled_with_tsan = False
     test_list.append(unst_deforming_naca0012)
 
     ######################################
@@ -614,6 +618,7 @@ def main():
     channel_3D.test_vals_aarch64 = [2.000000, 0.000000, 0.620189, 0.505311, 0.415246]
     channel_3D.unsteady  = True
     channel_3D.multizone = True
+    channel_3D.enabled_with_tsan = False
     test_list.append(channel_3D)
 
     # Pipe
@@ -695,6 +700,7 @@ def main():
     fsi2d.test_vals = [4.000000, 0.000000, -3.743227, -4.133479]
     fsi2d.multizone= True
     fsi2d.unsteady = True
+    fsi2d.enabled_with_tsan = False
     test_list.append(fsi2d)
 
     # FSI, Static, 2D, new mesh solver

From 13307f07cf35e4a2416dc592a466add43daddace Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Thu, 6 Jul 2023 10:50:06 +0200
Subject: [PATCH 548/656] Disable transonic_stator as well.

---
 TestCases/hybrid_regression_AD.py | 1 +
 1 file changed, 1 insertion(+)

diff --git a/TestCases/hybrid_regression_AD.py b/TestCases/hybrid_regression_AD.py
index 2d939abd8a4..db5191ddbe6 100644
--- a/TestCases/hybrid_regression_AD.py
+++ b/TestCases/hybrid_regression_AD.py
@@ -202,6 +202,7 @@ def main():
     discadj_trans_stator.test_iter = 79
     discadj_trans_stator.test_vals         = [79, 0.770065, 0.383137, 0.472153, -0.996484, 2.153296, -4.444301]
     discadj_trans_stator.test_vals_aarch64 = [79, 0.770065, 0.383137, 0.472153, -0.996484, 2.153296, -4.444301]
+    discadj_trans_stator.enabled_with_tsan = False
     test_list.append(discadj_trans_stator)
 
     ###################################

From 4b60792df20dabcf7b101d808a97665cdce8160b Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Thu, 6 Jul 2023 11:51:09 +0200
Subject: [PATCH 549/656] Pulled develop and implemented changes according to
 the introduction of CDataDrivenFluid

---
 Common/include/CConfig.hpp                    | 11 ++--------
 Common/src/CConfig.cpp                        |  5 +----
 SU2_CFD/include/fluid/CFluidFlamelet.hpp      |  5 ++++-
 SU2_CFD/include/fluid/CFluidModel.hpp         |  2 --
 SU2_CFD/src/fluid/CFluidFlamelet.cpp          | 21 +++++++++++++------
 SU2_CFD/src/output/CFlowOutput.cpp            |  8 +++----
 .../src/solvers/CSpeciesFlameletSolver.cpp    |  3 +--
 .../lam_prem_ch4_cfd.cfg                      |  2 +-
 .../lam_prem_ch4_hx_ad.cfg                    |  2 +-
 .../lam_prem_ch4_hx_dot.cfg                   |  2 +-
 .../lam_prem_ch4_cht_cfd_fluid.cfg            |  2 +-
 .../lam_prem_ch4_cht_ad_fluid.cfg             |  2 +-
 .../lam_prem_ch4_cfd_axi.cfg                  |  2 +-
 .../lam_partial_prem_ch4_cfd.cfg              |  2 +-
 config_template.cfg                           | 13 ++++++------
 15 files changed, 41 insertions(+), 41 deletions(-)

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index 507c40e4781..0835b5040d0 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -1233,8 +1233,7 @@ class CConfig {
   string* controlling_variable_names;
   string* cv_source_names;
   vector<string> table_scalar_names;  /*!< \brief Names of transported scalar variables. */
-  string* table_lookup_names;         /*!< \brief Names of LUT variables. */
-  string file_name_lut;               /*!< \brief Filename of the LUT. */
+  string* lookup_names;         /*!< \brief Names of passive look-up variables. */
   string* user_scalar_names;          /*!< \brief Names of the user defined (auxiliary) transported scalars .*/
   string* user_source_names;          /*!< \brief Names of the source terms for the user defined transported scalars. */
 
@@ -2185,13 +2184,7 @@ class CConfig {
   /*!
    * \brief Get the name of the variable that we want to retrieve from the lookup table.
    */
-  const string& GetLUTLookupName(unsigned short i_lookup) const { return table_lookup_names[i_lookup]; }
-
-  /*!
-   * \brief Get the file name of the look up table.
-   * \return File name of the look up table.
-   */
-  const string& GetFileNameLUT() const { return file_name_lut; }
+  const string& GetLookupName(unsigned short i_lookup) const { return lookup_names[i_lookup]; }
 
   /*!
    * \brief Get the Young's modulus of elasticity.
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 3335b70b8a6..cf4c7b41cc9 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -2101,14 +2101,11 @@ void CConfig::SetConfig_Options() {
   /* DESCRIPTION: Determine if we need to allocate memory to store the multizone residual. \n DEFAULT: true (temporarily) */
   addBoolOption("MULTIZONE_RESIDUAL", Multizone_Residual, false);
 
-  /*!\brief File name of the flamelet look up table.*/
-  addStringOption("FILENAME_LUT", file_name_lut, string("LUT"));
-
   addStringListOption("CONTROLLING_VARIABLE_NAMES", n_control_vars, controlling_variable_names);
   addStringListOption("CONTROLLING_VARIABLE_SOURCE_NAMES", n_control_vars, cv_source_names);
 
   /* DESCRIPTION: Names of the passive lookup variables for flamelet LUT */
-  addStringListOption("LOOKUP_NAMES", n_lookups, table_lookup_names);
+  addStringListOption("LOOKUP_NAMES", n_lookups, lookup_names);
 
   /* DESCRIPTION: Names of the user transport equations solved in the flamelet problem. */
   addStringListOption("USER_SCALAR_NAMES", n_user_scalars, user_scalar_names);
diff --git a/SU2_CFD/include/fluid/CFluidFlamelet.hpp b/SU2_CFD/include/fluid/CFluidFlamelet.hpp
index cc402ea0520..4d4906be6a7 100644
--- a/SU2_CFD/include/fluid/CFluidFlamelet.hpp
+++ b/SU2_CFD/include/fluid/CFluidFlamelet.hpp
@@ -32,6 +32,9 @@
 
 class CFluidFlamelet final : public CFluidModel {
  private:
+  ENUM_DATADRIVEN_METHOD Kind_DataDriven_Method =
+      ENUM_DATADRIVEN_METHOD::LUT; /*!< \brief Interpolation method for data set evaluation. */
+
   enum LOOKUP_TD { TEMPERATURE, HEATCAPACITY, VISCOSITY, CONDUCTIVITY, DIFFUSIONCOEFFICIENT, MOLARWEIGHT, SIZE };
 
   int rank;
@@ -88,7 +91,7 @@ class CFluidFlamelet final : public CFluidModel {
    * \brief Check for out-of-bounds condition for data set interpolation.
    * \return - within bounds (0) or out of bounds (1).
    */
-  inline unsigned long GetExtrapolation() override { return extrapolation; }
+  unsigned long GetExtrapolation() override { return extrapolation; }
 
   /*!
    * \brief Get the mass diffusivity of the species.
diff --git a/SU2_CFD/include/fluid/CFluidModel.hpp b/SU2_CFD/include/fluid/CFluidModel.hpp
index 33b2339244f..77d7c314e37 100644
--- a/SU2_CFD/include/fluid/CFluidModel.hpp
+++ b/SU2_CFD/include/fluid/CFluidModel.hpp
@@ -149,8 +149,6 @@ class CFluidModel {
    */
   virtual unsigned long EvaluateDataSet(vector<su2double> &input_scalar, unsigned short lookup_type, vector<su2double> &output_refs) { return 0; }
 
-  virtual unsigned long GetExtrapolation() { return 0; }
-
   /*!
    * \brief Get fluid dynamic viscosity.
    */
diff --git a/SU2_CFD/src/fluid/CFluidFlamelet.cpp b/SU2_CFD/src/fluid/CFluidFlamelet.cpp
index 770604bdc64..a871e548a48 100644
--- a/SU2_CFD/src/fluid/CFluidFlamelet.cpp
+++ b/SU2_CFD/src/fluid/CFluidFlamelet.cpp
@@ -30,6 +30,7 @@
 
 CFluidFlamelet::CFluidFlamelet(CConfig* config, su2double value_pressure_operating) : CFluidModel() {
   rank = SU2_MPI::GetRank();
+  Kind_DataDriven_Method = config->GetKind_DataDriven_Method();
 
   /* -- number of auxiliary species transport equations, e.g. 1=CO, 2=NOx  --- */
   n_user_scalars = config->GetNUserScalars();
@@ -43,10 +44,18 @@ CFluidFlamelet::CFluidFlamelet(CConfig* config, su2double value_pressure_operati
     cout << "Number of control variables: " << n_control_vars << endl;
   }
 
-  if (rank == MASTER_NODE) {
-    cout << "*****************************************" << endl;
-    cout << "***   initializing the lookup table   ***" << endl;
-    cout << "*****************************************" << endl;
+  switch (Kind_DataDriven_Method)
+  {
+  case ENUM_DATADRIVEN_METHOD::LUT:
+    if (rank == MASTER_NODE) {
+      cout << "*****************************************" << endl;
+      cout << "***   initializing the lookup table   ***" << endl;
+      cout << "*****************************************" << endl;
+    }
+    break;
+  default:
+    SU2_MPI::Error("Interpolation method not implemented for flamelet solver.", CURRENT_FUNCTION);
+    break;
   }
 
   scalars_vector.resize(n_scalars);
@@ -60,7 +69,7 @@ CFluidFlamelet::CFluidFlamelet(CConfig* config, su2double value_pressure_operati
     table_scalar_names[n_control_vars + i_aux] = config->GetUserScalarName(i_aux);
   }
 
-  look_up_table = new CLookUpTable(config->GetFileNameLUT(), table_scalar_names[I_PROGVAR], table_scalar_names[I_ENTH]);
+  look_up_table = new CLookUpTable(config->GetDataDriven_FileNames()[0], table_scalar_names[I_PROGVAR], table_scalar_names[I_ENTH]);
 
   Pressure = value_pressure_operating;
 
@@ -146,7 +155,7 @@ void CFluidFlamelet::PreprocessLookUp(CConfig* config) {
   varnames_LookUp.resize(n_lookups);
   val_vars_LookUp.resize(n_lookups);
   for (auto iLookup=0u; iLookup < n_lookups; iLookup++)
-    varnames_LookUp[iLookup] = config->GetLUTLookupName(iLookup);
+    varnames_LookUp[iLookup] = config->GetLookupName(iLookup);
 
 }
 
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index 216e0264a97..ab66b34b4c8 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -1443,8 +1443,8 @@ void CFlowOutput::SetVolumeOutputFieldsScalarLookup(const CConfig* config) {
   switch (config->GetKind_Species_Model()) {
     case SPECIES_MODEL::FLAMELET:
       for (auto i_lookup = 0u; i_lookup < config->GetNLookups(); ++i_lookup) {
-        string strname1 = "lookup_" + config->GetLUTLookupName(i_lookup);
-        AddVolumeOutput(config->GetLUTLookupName(i_lookup), strname1,"LOOKUP", config->GetLUTLookupName(i_lookup));
+        string strname1 = "lookup_" + config->GetLookupName(i_lookup);
+        AddVolumeOutput(config->GetLookupName(i_lookup), strname1,"LOOKUP", config->GetLookupName(i_lookup));
       }
       AddVolumeOutput("TABLE_MISSES"       , "Table_misses"       , "LOOKUP", "Lookup table misses");
       break;
@@ -1614,8 +1614,8 @@ void CFlowOutput::LoadVolumeDataScalar(const CConfig* config, const CSolver* con
 
       /*--- variables that we look up from the LUT ---*/
       for (int i_lookup = 0; i_lookup < config->GetNLookups(); ++i_lookup) {
-        if (config->GetLUTLookupName(i_lookup)!="NULL")
-          SetVolumeOutputValue(config->GetLUTLookupName(i_lookup), iPoint, Node_Species->GetScalarLookups(iPoint)[i_lookup]);
+        if (config->GetLookupName(i_lookup)!="NULL")
+          SetVolumeOutputValue(config->GetLookupName(i_lookup), iPoint, Node_Species->GetScalarLookups(iPoint)[i_lookup]);
       }
 
       SetVolumeOutputValue("TABLE_MISSES", iPoint, Node_Species->GetTableMisses(iPoint));
diff --git a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
index d0b94709071..37dda9f3c56 100644
--- a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
+++ b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
@@ -381,8 +381,7 @@ void CSpeciesFlameletSolver::BC_Isothermal_Wall_Generic(CGeometry* geometry, CSo
         enth_wall = nodes->GetSolution(iPoint, I_ENTH);
 
         /*--- Set enthalpy on the wall. ---*/
-        n_not_iterated += GetEnthFromTemp(fluid_model_local, temp_wall, &enth_wall,
-                                          solver_container[SPECIES_SOL]->GetNodes()->GetSolution(iPoint));
+        n_not_iterated += GetEnthFromTemp(fluid_model_local, temp_wall, &enth_wall, nodes->GetSolution(iPoint));
 
         /*--- Impose the value of the enthalpy as a strong boundary
         condition (Dirichlet) and remove any
diff --git a/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg b/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg
index 8cdbcca8a3f..9193f0820ee 100644
--- a/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg
+++ b/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg
@@ -27,7 +27,7 @@ INC_NONDIM= DIMENSIONAL
 % -------------------- FLUID MODEL --------------------------------------- %
 %
 FLUID_MODEL= FLUID_FLAMELET
-FILENAME_LUT= fgm_ch4.drg
+FILENAMES_INTERPOLATOR= (fgm_ch4.drg)
 CONTROLLING_VARIABLE_NAMES= (ProgressVariable, EnthalpyTot)
 CONTROLLING_VARIABLE_SOURCE_NAMES = (ProdRateTot_PV, NULL)
 %
diff --git a/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg
index c0108c0e298..452bc271b5a 100644
--- a/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg
+++ b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg
@@ -37,7 +37,7 @@ INC_NONDIM= DIMENSIONAL
 % -------------------- FLUID PROPERTIES ------------------------------------- %
 %
 FLUID_MODEL= FLUID_FLAMELET
-FILENAME_LUT= fgm_ch4.drg
+FILENAMES_INTERPOLATOR= (fgm_ch4.drg)
 CONTROLLING_VARIABLE_NAMES= (ProgressVariable, EnthalpyTot)
 CONTROLLING_VARIABLE_SOURCE_NAMES= (ProdRateTot_PV, NULL)
 
diff --git a/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg
index f0d0191ff05..acd766cbe84 100644
--- a/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg
+++ b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg
@@ -38,7 +38,7 @@ INC_NONDIM= DIMENSIONAL
 % -------------------- FLUID PROPERTIES ------------------------------------- %
 %
 FLUID_MODEL= FLUID_FLAMELET
-FILENAME_LUT= fgm_ch4.drg
+FILENAMES_INTERPOLATOR= (fgm_ch4.drg)
 CONTROLLING_VARIABLE_NAMES= (ProgressVariable, EnthalpyTot)
 CONTROLLING_VARIABLE_SOURCE_NAMES= (ProdRateTot_PV, NULL)
 CONDUCTIVITY_MODEL= FLAMELET
diff --git a/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg b/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg
index c91c5b4ae67..e0828cc4d44 100644
--- a/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg
+++ b/TestCases/flamelet/03_laminar_premixed_ch4_flame_cht_cfd/lam_prem_ch4_cht_cfd_fluid.cfg
@@ -52,7 +52,7 @@ INC_NONDIM= DIMENSIONAL
 % -------------------- FLUID MODEL --------------------------------------- %
 
 FLUID_MODEL= FLUID_FLAMELET
-FILENAME_LUT= fgm_ch4.drg
+FILENAMES_INTERPOLATOR= (fgm_ch4.drg)
 CONTROLLING_VARIABLE_NAMES= (ProgressVariable, EnthalpyTot)
 CONTROLLING_VARIABLE_SOURCE_NAMES= (ProdRateTot_PV, NULL)
 FLAME_INIT= (0.004, 0.0, 0.0, 1.0, 0.0, 0.0, 0.2e-3, 1.0)
diff --git a/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg b/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg
index 6f22997846a..7824d6780fd 100644
--- a/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg
+++ b/TestCases/flamelet/04_laminar_premixed_ch4_flame_cht_ad/lam_prem_ch4_cht_ad_fluid.cfg
@@ -54,7 +54,7 @@ INC_NONDIM= DIMENSIONAL
 % -------------------- FLUID MODEL --------------------------------------- %
 
 FLUID_MODEL= FLUID_FLAMELET
-FILENAME_LUT= fgm_ch4.drg
+FILENAMES_INTERPOLATOR= (fgm_ch4.drg)
 CONTROLLING_VARIABLE_NAMES= (ProgressVariable, EnthalpyTot)
 CONTROLLING_VARIABLE_SOURCE_NAMES= (ProdRateTot_PV, NULL)
 FLAME_INIT= (0.004, 0.0, 0.0, 1, 0, 0, 0.2e-3, 1)
diff --git a/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg b/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg
index 484240977cc..62957216e01 100644
--- a/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg
+++ b/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg
@@ -30,7 +30,7 @@ AXISYMMETRIC= YES
 % -------------------- FLUID MODEL --------------------------------------- %
 %
 FLUID_MODEL= FLUID_FLAMELET
-FILENAME_LUT= fgm_ch4.drg
+FILENAMES_INTERPOLATOR= (fgm_ch4.drg)
 CONTROLLING_VARIABLE_NAMES= (ProgressVariable, EnthalpyTot)
 CONTROLLING_VARIABLE_SOURCE_NAMES= (ProdRateTot_PV, NULL)
 %
diff --git a/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_prem_ch4_cfd.cfg b/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_prem_ch4_cfd.cfg
index cd22b4147ec..9092a1ff39d 100644
--- a/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_prem_ch4_cfd.cfg
+++ b/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_prem_ch4_cfd.cfg
@@ -27,7 +27,7 @@ INC_NONDIM= DIMENSIONAL
 % -------------------- FLUID MODEL --------------------------------------- %
 %
 FLUID_MODEL= FLUID_FLAMELET
-FILENAME_LUT= LUT_methane_3D.drg
+FILENAMES_INTERPOLATOR= (LUT_methane_3D.drg)
 % FGM controlling variable names (must include mixture fraction for partial 
 % premixed cases)
 CONTROLLING_VARIABLE_NAMES=(ProgressVariable,EnthalpyTot,MixtureFraction)
diff --git a/config_template.cfg b/config_template.cfg
index cbffe2fc3e3..34de9b4aeab 100644
--- a/config_template.cfg
+++ b/config_template.cfg
@@ -374,12 +374,15 @@ FROZEN_MIXTURE= NO
 % Datadriven fluid model
 % For data-driven fluid models, an interpolation algorithm is used to retrieve the thermodynamic state for a given density and internal energy
 
-% Interpolation method for thermodynamic state calculation (MLP for multi-layer perceptron, LUT for 2D, unstructured look-up table)
+% Interpolation method for thermodynamic state calculation for data-driven fluid model or flamelet fluid model.
+% (MLP for multi-layer perceptron, LUT for 2D or 3D, unstructured look-up table)
 INTERPOLATION_METHOD= MLP
 
-% Name of the input file containing the information required for the interpolator to function
-% See https://github.com/EvertBunschoten/MLPCpp for more information.
-FILENAME_INTERPOLATOR= MLP_collection.mlp
+% Name of the input file containing the information required for the interpolator to function.
+% Provide list of .mlp files (See https://github.com/EvertBunschoten/MLPCpp for more information.)
+% when using the MLP option for INTERPOLATION_METHOD
+% or a single .drg file for the LUT INTERPOLATION_METHOD option.
+FILENAMES_INTERPOLATOR= (MLP_1.mlp, MLP_2.mlp, MLP_3.mlp)
 
 % Relaxation factor for the Newton solvers in the data-driven fluid model
 DATADRIVEN_NEWTON_RELAXATION= 0.8
@@ -784,8 +787,6 @@ USER_SOURCE_NAMES= ( ProdRateTot_Y-CO,  zero)
 % Names of variables from the LUT that will be looked up for visualization
 LOOKUP_NAMES= (MolarWeightMix, Conductivity, HeatRelease, Diffusivity)
 %
-% filename of the lookup table
-FILENAME_LUT= fgm_ch4.drg
 
 % Names of the controlling variables used to evaluate the look-up table and for which
 % transported scalar variables are generated. These names should coincide with those

From cd79110bc4eded14077c4c16c79906a8451b1df9 Mon Sep 17 00:00:00 2001
From: Judah Milgram <milgram@cgpp.com>
Date: Thu, 6 Jul 2023 07:16:16 -0400
Subject: [PATCH 550/656] chmod +x SU2_PY/fsi_computation.py

---
 SU2_PY/fsi_computation.py | 0
 1 file changed, 0 insertions(+), 0 deletions(-)
 mode change 100644 => 100755 SU2_PY/fsi_computation.py

diff --git a/SU2_PY/fsi_computation.py b/SU2_PY/fsi_computation.py
old mode 100644
new mode 100755

From 85b5e1aa7b879e4a20f0e989bcbef29e000a336a Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Thu, 6 Jul 2023 15:30:47 +0200
Subject: [PATCH 551/656] Disabled multizone flag for adjoint flamelet test
 case 02

---
 TestCases/parallel_regression_AD.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index 93c4cabf278..5a08b59123f 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -349,7 +349,7 @@ def main():
     discadj_flamelet_ch4_hx.command          = TestCase.Command("mpirun -n 2", "SU2_CFD_AD")
     discadj_flamelet_ch4_hx.cfg_dir          = "flamelet/02_laminar_premixed_ch4_flame_hx_ad"
     discadj_flamelet_ch4_hx.cfg_file         = "lam_prem_ch4_hx_ad.cfg"
-    discadj_flamelet_ch4_hx.multizone        = True
+    discadj_flamelet_ch4_hx.multizone        = False
     discadj_flamelet_ch4_hx.test_iter        = 10
     discadj_flamelet_ch4_hx.timeout          = 20000
     discadj_flamelet_ch4_hx.reference_file   = "restart_adj_custom.csv.ref"

From acf37bb78914ec8ddb9fe604c04abf99b5eb7cc9 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Thu, 6 Jul 2023 17:21:28 +0200
Subject: [PATCH 552/656] Deliberately introduce a data race for testing.

---
 SU2_CFD/src/SU2_CFD.cpp | 6 ++++++
 1 file changed, 6 insertions(+)

diff --git a/SU2_CFD/src/SU2_CFD.cpp b/SU2_CFD/src/SU2_CFD.cpp
index fce69de5fd0..b712b143caa 100644
--- a/SU2_CFD/src/SU2_CFD.cpp
+++ b/SU2_CFD/src/SU2_CFD.cpp
@@ -82,6 +82,12 @@ int main(int argc, char *argv[]) {
   libxsmm_init();
 #endif
 
+  int i = 0;
+  #pragma omp parallel
+  {
+    i = omp_get_thread_num();
+  }
+
   /*--- Create a pointer to the main SU2 Driver ---*/
 
   CDriver* driver = nullptr;

From 85104176439742b8e7104bb8ee0077996bd98cdb Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Thu, 6 Jul 2023 17:38:42 +0200
Subject: [PATCH 553/656] Silence warning.

---
 SU2_CFD/src/SU2_CFD.cpp | 1 +
 1 file changed, 1 insertion(+)

diff --git a/SU2_CFD/src/SU2_CFD.cpp b/SU2_CFD/src/SU2_CFD.cpp
index b712b143caa..8c27f8f7191 100644
--- a/SU2_CFD/src/SU2_CFD.cpp
+++ b/SU2_CFD/src/SU2_CFD.cpp
@@ -87,6 +87,7 @@ int main(int argc, char *argv[]) {
   {
     i = omp_get_thread_num();
   }
+  std::cout << i << std::endl;
 
   /*--- Create a pointer to the main SU2 Driver ---*/
 

From 37e6bc19e1967535e600a8e95e559da121f4ae31 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Thu, 6 Jul 2023 18:04:14 +0200
Subject: [PATCH 554/656] Silence more warnings.

---
 SU2_CFD/src/SU2_CFD.cpp | 3 ++-
 1 file changed, 2 insertions(+), 1 deletion(-)

diff --git a/SU2_CFD/src/SU2_CFD.cpp b/SU2_CFD/src/SU2_CFD.cpp
index 8c27f8f7191..40f631c239f 100644
--- a/SU2_CFD/src/SU2_CFD.cpp
+++ b/SU2_CFD/src/SU2_CFD.cpp
@@ -83,10 +83,11 @@ int main(int argc, char *argv[]) {
 #endif
 
   int i = 0;
-  #pragma omp parallel
+  SU2_OMP_PARALLEL
   {
     i = omp_get_thread_num();
   }
+  END_SU2_OMP_PARALLEL
   std::cout << i << std::endl;
 
   /*--- Create a pointer to the main SU2 Driver ---*/

From 96baee23262bff43f0c162079aa587247a7a1eef Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Thu, 6 Jul 2023 10:58:48 -0700
Subject: [PATCH 555/656] Update .github/workflows/regression.yml

---
 .github/workflows/regression.yml | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index b7ea7b00800..0bb7110fd97 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -128,7 +128,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c bug_fix_cht_flamelet -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:230225-2136
         with:

From 96ad0bb8e6056a72606bac6e6fb63440df5e7bb4 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Fri, 7 Jul 2023 09:38:28 +0200
Subject: [PATCH 556/656] Use tsan with debug builds.

---
 .github/workflows/regression.yml | 6 +++---
 1 file changed, 3 insertions(+), 3 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index ea6e2754f19..d63faae2263 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -81,11 +81,11 @@ jobs:
         config_set: [BaseOMP-tsan, ReverseOMP-tsan, ForwardOMP-tsan]
         include:
           - config_set: BaseOMP-tsan
-            flags: '-Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
+            flags: '--buildtype=debug -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
           - config_set: ReverseOMP-tsan
-            flags: '-Denable-autodiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
+            flags: '--buildtype=debug -Denable-autodiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
           - config_set: ForwardOMP-tsan
-            flags: '-Denable-directdiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
+            flags: '--buildtype=debug -Denable-directdiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
     runs-on: ${{ inputs.runner || 'ubuntu-latest' }}
     steps:
       - name: Cache Object Files

From dcaa3b6fa780e99e0ad7e3c7501614894398ec62 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Fri, 7 Jul 2023 09:39:56 +0200
Subject: [PATCH 557/656] Disable ForwardOMP-tsan since it is not used right
 now.

---
 .github/workflows/regression.yml | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index d63faae2263..780d373ef6e 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -84,8 +84,8 @@ jobs:
             flags: '--buildtype=debug -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
           - config_set: ReverseOMP-tsan
             flags: '--buildtype=debug -Denable-autodiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
-          - config_set: ForwardOMP-tsan
-            flags: '--buildtype=debug -Denable-directdiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
+          #- config_set: ForwardOMP-tsan
+          #  flags: '--buildtype=debug -Denable-directdiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
     runs-on: ${{ inputs.runner || 'ubuntu-latest' }}
     steps:
       - name: Cache Object Files

From 7eea7694dd312a2fa7424e32add590417e52915b Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Fri, 7 Jul 2023 11:39:05 +0200
Subject: [PATCH 558/656] Work around segfault.

---
 SU2_CFD/src/SU2_CFD.cpp | 18 ++++++++++--------
 1 file changed, 10 insertions(+), 8 deletions(-)

diff --git a/SU2_CFD/src/SU2_CFD.cpp b/SU2_CFD/src/SU2_CFD.cpp
index 40f631c239f..0a8dd062092 100644
--- a/SU2_CFD/src/SU2_CFD.cpp
+++ b/SU2_CFD/src/SU2_CFD.cpp
@@ -82,14 +82,6 @@ int main(int argc, char *argv[]) {
   libxsmm_init();
 #endif
 
-  int i = 0;
-  SU2_OMP_PARALLEL
-  {
-    i = omp_get_thread_num();
-  }
-  END_SU2_OMP_PARALLEL
-  std::cout << i << std::endl;
-
   /*--- Create a pointer to the main SU2 Driver ---*/
 
   CDriver* driver = nullptr;
@@ -152,6 +144,16 @@ int main(int argc, char *argv[]) {
 
   }
 
+  {
+    int i = 0;
+    SU2_OMP_PARALLEL
+    {
+      i = omp_get_thread_num();
+    }
+    END_SU2_OMP_PARALLEL
+    std::cout << i << std::endl;
+  }
+
   /*--- Launch the main external loop of the solver. ---*/
 
   driver->StartSolver();

From bfce8b59078e2e3a4bf0ef712b9e3ea385643d51 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Fri, 7 Jul 2023 11:42:08 +0200
Subject: [PATCH 559/656] Fix.

---
 .github/workflows/regression.yml | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 780d373ef6e..33fc2e8af43 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -78,7 +78,7 @@ jobs:
     strategy:
       fail-fast: false
       matrix:
-        config_set: [BaseOMP-tsan, ReverseOMP-tsan, ForwardOMP-tsan]
+        config_set: [BaseOMP-tsan, ReverseOMP-tsan] #ForwardOMP-tsan
         include:
           - config_set: BaseOMP-tsan
             flags: '--buildtype=debug -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'

From d41a860ad6f65b042ec2b10c2468ed80fcec6ed3 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Fri, 7 Jul 2023 12:10:40 +0200
Subject: [PATCH 560/656] Don't treat warnings as errors for now.

---
 .github/workflows/regression.yml | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 33fc2e8af43..a044eb78fc7 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -81,9 +81,9 @@ jobs:
         config_set: [BaseOMP-tsan, ReverseOMP-tsan] #ForwardOMP-tsan
         include:
           - config_set: BaseOMP-tsan
-            flags: '--buildtype=debug -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
+            flags: '--buildtype=debug -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3'
           - config_set: ReverseOMP-tsan
-            flags: '--buildtype=debug -Denable-autodiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
+            flags: '--buildtype=debug -Denable-autodiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3'
           #- config_set: ForwardOMP-tsan
           #  flags: '--buildtype=debug -Denable-directdiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
     runs-on: ${{ inputs.runner || 'ubuntu-latest' }}

From 8dba8a60277314b32808bd25b3876239dd7f7dce Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Fri, 7 Jul 2023 13:07:52 +0200
Subject: [PATCH 561/656] Remove deliberate data race.

---
 SU2_CFD/src/SU2_CFD.cpp | 10 ----------
 1 file changed, 10 deletions(-)

diff --git a/SU2_CFD/src/SU2_CFD.cpp b/SU2_CFD/src/SU2_CFD.cpp
index 0a8dd062092..fce69de5fd0 100644
--- a/SU2_CFD/src/SU2_CFD.cpp
+++ b/SU2_CFD/src/SU2_CFD.cpp
@@ -144,16 +144,6 @@ int main(int argc, char *argv[]) {
 
   }
 
-  {
-    int i = 0;
-    SU2_OMP_PARALLEL
-    {
-      i = omp_get_thread_num();
-    }
-    END_SU2_OMP_PARALLEL
-    std::cout << i << std::endl;
-  }
-
   /*--- Launch the main external loop of the solver. ---*/
 
   driver->StartSolver();

From 8163706781a1a95d002102a0bb24aec45e82dc4f Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Fri, 7 Jul 2023 17:44:49 +0200
Subject: [PATCH 562/656] Use optimized debug builds.

---
 .github/workflows/regression.yml | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index a044eb78fc7..219e44b8c47 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -81,9 +81,9 @@ jobs:
         config_set: [BaseOMP-tsan, ReverseOMP-tsan] #ForwardOMP-tsan
         include:
           - config_set: BaseOMP-tsan
-            flags: '--buildtype=debug -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3'
+            flags: '--buildtype=debugoptimized -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3'
           - config_set: ReverseOMP-tsan
-            flags: '--buildtype=debug -Denable-autodiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3'
+            flags: '--buildtype=debugoptimized -Denable-autodiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3'
           #- config_set: ForwardOMP-tsan
           #  flags: '--buildtype=debug -Denable-directdiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
     runs-on: ${{ inputs.runner || 'ubuntu-latest' }}

From f649eb999c03282d4e75a34b0fd016cde3dda657 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 8 Jul 2023 15:32:59 -0700
Subject: [PATCH 563/656] update v&v

---
 TestCases/vandv.py | 9 +++++----
 1 file changed, 5 insertions(+), 4 deletions(-)

diff --git a/TestCases/vandv.py b/TestCases/vandv.py
index 3f3f1267a80..4770c6088c3 100644
--- a/TestCases/vandv.py
+++ b/TestCases/vandv.py
@@ -46,7 +46,7 @@ def main():
     p30n30.cfg_file  = "config.cfg"
     p30n30.test_iter = 20
     p30n30.test_vals         = [-10.806343, -10.326374, -10.559106, -10.432754, -13.517105, 0.050962, 2.828563, 1.317849, -0.228843]
-    p30n30.test_vals_aarch64 = [-10.636663, -10.298256, -10.479415, -10.246700, -13.517161, 0.050962, 2.828563, 1.317849, -0.209200]
+    p30n30.test_vals_aarch64 = [-10.801521, -10.325747, -10.557163, -10.427274, -13.517118, 0.050962, 2.828563, 1.317849, -0.207763]
     test_list.append(p30n30)
 
     # flat plate - sst-v1994m
@@ -55,7 +55,7 @@ def main():
     flatplate_sst1994m.cfg_file  = "turb_flatplate_sst.cfg"
     flatplate_sst1994m.test_iter = 5
     flatplate_sst1994m.test_vals         = [-13.023358, -9.956752, -11.099910, -7.933220, -10.206577, -5.132343, 0.002808]
-    flatplate_sst1994m.test_vals_aarch64 = [-13.023358, -9.956752, -11.099910, -7.933220, -10.206577, -5.132343, 0.002808]
+    flatplate_sst1994m.test_vals_aarch64 = [-13.022835, -9.956652, -11.102384, -7.928197, -10.206580, -5.132317, 0.002808]
     test_list.append(flatplate_sst1994m)
 
     # bump in channel - sst-v1994m
@@ -64,7 +64,7 @@ def main():
     bump_sst1994m.cfg_file  = "turb_bump_sst.cfg"
     bump_sst1994m.test_iter = 5
     bump_sst1994m.test_vals         = [-12.986182, -10.719941, -10.556276, -7.606531, -10.774915, -5.605156, 0.004972]
-    bump_sst1994m.test_vals_aarch64 = [-12.986182, -10.719941, -10.556276, -7.606531, -10.774915, -5.605156, 0.004972]
+    bump_sst1994m.test_vals_aarch64 = [-13.039365, -10.729085, -10.609923, -7.682911, -10.774915, -5.605087, 0.004972]
     test_list.append(bump_sst1994m)
 
     # SWBLI SA
@@ -73,7 +73,7 @@ def main():
     swbli_sa.cfg_file  = "config_sa.cfg"
     swbli_sa.test_iter = 5
     swbli_sa.test_vals         = [-11.530796, -10.915564, -12.034495, -10.538719, -15.922522, 0.002233, -3.359164, 1.340100]
-    swbli_sa.test_vals_aarch64 = [-11.014738, -9.936534, -11.120020, -10.050397, -13.203736, 0.002233, -3.222675, 1.340100]
+    swbli_sa.test_vals_aarch64 = [-11.530796, -10.915564, -12.034495, -10.538719, -15.922522, 0.002233, -3.359164, 1.340100]
     test_list.append(swbli_sa)
 
 
@@ -115,3 +115,4 @@ def main():
 
 if __name__ == '__main__':
     main()
+= [-11.527743, -11.150388, -11.944924, -10.750834, -11.116769, -4.030059, 0.002339, -2.730392, -4.067274, 1.276300]

From 33303ebf17f4c18c6d613e1dd8489eaab0b60c4a Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 8 Jul 2023 15:41:47 -0700
Subject: [PATCH 564/656] tutorials

---
 TestCases/tutorials.py | 4 +++-
 1 file changed, 3 insertions(+), 1 deletion(-)

diff --git a/TestCases/tutorials.py b/TestCases/tutorials.py
index 424374bc743..d7ea51572bd 100644
--- a/TestCases/tutorials.py
+++ b/TestCases/tutorials.py
@@ -190,6 +190,7 @@ def main():
     tutorial_trans_flatplate_T3A.cfg_file   = "transitional_LM_model_ConfigFile.cfg"
     tutorial_trans_flatplate_T3A.test_iter  = 20
     tutorial_trans_flatplate_T3A.test_vals  = [-5.837186, -2.092246, -3.982633, -0.302219, -1.921235, 1.667190, -3.496277, 0.391605]
+    tutorial_trans_flatplate_T3A.test_vals_aarch64 = [-5.837191, -2.092246, -3.982640, -0.302224, -1.922554, 1.667190, -3.496277, 0.391605]
     tutorial_trans_flatplate_T3A.no_restart = True
     test_list.append(tutorial_trans_flatplate_T3A)
 
@@ -199,6 +200,7 @@ def main():
     tutorial_trans_flatplate_T3Am.cfg_file   = "transitional_LM_model_ConfigFile.cfg"
     tutorial_trans_flatplate_T3Am.test_iter  = 20
     tutorial_trans_flatplate_T3Am.test_vals  = [-6.063600, -1.945057, -3.946760, -0.549063, -3.863792, 2.664453, -2.517606, 1.112979]
+    tutorial_trans_flatplate_T3Am.test_vals_aarch64 = [-6.063598, -1.945057, -3.946744, -0.549062, -3.863792, 2.664453, -2.517606, 1.112979]
     tutorial_trans_flatplate_T3Am.no_restart = True
     test_list.append(tutorial_trans_flatplate_T3Am)
 
@@ -243,7 +245,7 @@ def main():
     tutorial_unst_naca0012.cfg_file      = "unsteady_naca0012.cfg"
     tutorial_unst_naca0012.test_iter     = 520
     tutorial_unst_naca0012.test_vals         = [520.000000, 0.000000, -5.291711, 0.000000, 0.305248, 0.810326, 0.001814, 0.006573]
-    tutorial_unst_naca0012.test_vals_aarch64 = [520, 0, -5.296968, 0, 0.312131, 0.801193, 0.002868, 0.014303]
+    tutorial_unst_naca0012.test_vals_aarch64 = [520.000000, 0.000000, -5.298777, 0.000000, 0.288956, 0.736706, 0.002419, 0.007134]
     tutorial_unst_naca0012.unsteady      = True
     test_list.append(tutorial_unst_naca0012)
 

From 7a5cff4ff2e7e48ba72e392e380e6544cccc995c Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 8 Jul 2023 16:15:46 -0700
Subject: [PATCH 565/656] parallel

---
 TestCases/parallel_regression.py | 27 +++++++++++++++------------
 1 file changed, 15 insertions(+), 12 deletions(-)

diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 94deb08de2f..a401724958a 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -95,7 +95,7 @@ def main():
     invwedge_a.cfg_file = "invwedge_ausm.cfg"
     invwedge_a.test_iter = 10
     invwedge_a.test_vals = [-1.042842, -1.567605, -18.301264, -18.628631, -18.574668, 2.275192, 1.879772, 5.319421, 0.873699]
-    invwedge_a.test_vals_aarch64 = [-1.042842, -1.567605, -18.301264, -18.628631, -18.574668, 2.275192, 1.879772, 5.319421, 0.873699]
+    invwedge_a.test_vals_aarch64 = [-1.042842, -1.567605, -18.301374, -18.628734, -18.574780, 2.275192, 1.879772, 5.319421, 0.873699]
     test_list.append(invwedge_a)
 
     # Inviscid single wedge, ausm+-up2, implicit
@@ -113,7 +113,7 @@ def main():
     invwedge_msw.cfg_file = "invwedge_msw.cfg"
     invwedge_msw.test_iter = 10
     invwedge_msw.test_vals = [-1.165957, -1.690720, -18.298756, -18.626164, -18.572159, 2.151638, 1.721236, 5.193813, 0.751584]
-    invwedge_msw.test_vals_aarch64 = [-1.165957, -1.690720, -18.298756, -18.626164, -18.572159, 2.151638, 1.721236, 5.193813, 0.751584]
+    invwedge_msw.test_vals_aarch64 = [-1.165957, -1.690720, -18.301301, -18.628685, -18.574704, 2.151638, 1.721236, 5.193813, 0.751584]
     test_list.append(invwedge_msw)
 
     # Inviscid single wedge, roe, implicit
@@ -122,7 +122,7 @@ def main():
     invwedge_roe.cfg_file = "invwedge_roe.cfg"
     invwedge_roe.test_iter = 10
     invwedge_roe.test_vals = [-1.038582, -1.563344, -18.300307, -18.627706, -18.573706, 2.278987, 1.861307, 5.323753, 0.874900]
-    invwedge_roe.test_vals_aarch64 = [-1.038582, -1.563344, -18.300307, -18.627706, -18.573706, 2.278987, 1.861307, 5.323753, 0.874900]
+    invwedge_roe.test_vals_aarch64 = [-1.038582, -1.563344, -18.299879, -18.627263, -18.573276, 2.278987, 1.861307, 5.323753, 0.874900]
     test_list.append(invwedge_roe)
 
     # Inviscid single wedge, lax, implicit
@@ -140,7 +140,7 @@ def main():
     invwedge_ausm_m.cfg_file = "invwedge_am.cfg"
     invwedge_ausm_m.test_iter = 10
     invwedge_ausm_m.test_vals = [-1.055083, -1.579845, -16.739725, -17.063618, -17.012831, 2.265430, 1.797602, 5.302740, 0.856548]
-    invwedge_ausm_m.test_vals_aarch64 = [-1.055083, -1.579845, -16.739725, -17.063618, -17.012831, 2.265430, 1.797602, 5.302740, 0.85654]
+    invwedge_ausm_m.test_vals_aarch64 = [-1.055079, -1.579842, -16.739725, -17.063618, -17.012831, 2.265433, 1.797600, 5.302743, 0.856551]
     test_list.append(invwedge_ausm_m)
 
     # Inviscid single wedge, implicit, NEMO supersonic inlet
@@ -158,7 +158,7 @@ def main():
     visc_cone.cfg_file = "axi_visccone.cfg"
     visc_cone.test_iter = 10
     visc_cone.test_vals = [-5.222212, -5.746462, -20.559802, -20.510196, -20.439814, 1.255865, -3.208363, -0.016006, 0.093455, 32633.000000]
-    visc_cone.test_vals_aarch64 = [-5.222212, -5.746462, -20.559802, -20.510196, -20.439814, 1.255865, -3.208363, -0.016006, 0.093455, 32633.000000]
+    visc_cone.test_vals_aarch64 = [-5.222267, -5.746522, -20.559799, -20.510195, -20.440311, 1.255761, -3.208360, -0.016014, 0.093462, 32634.000000]
     test_list.append(visc_cone)
 
     # Viscous single wedge with Mutation++
@@ -245,7 +245,7 @@ def main():
     polar_naca0012.polar     = True
     polar_naca0012.test_iter = 10
     polar_naca0012.test_vals         = [-1.217981, 4.256386, 0.009084, 0.016823]
-    polar_naca0012.test_vals_aarch64 = [-2.936433, 2.478784, 0.005113, 0.008684]
+    polar_naca0012.test_vals_aarch64 = [-6.491535, -1.076111, 0.001168, 0.008666]
     polar_naca0012.command   = TestCase.Command(exec = "compute_polar.py", param = "-i 11")
     test_list.append(polar_naca0012)
 
@@ -271,6 +271,7 @@ def main():
     ramp.cfg_file = "inv_ramp.cfg"
     ramp.test_iter = 10
     ramp.test_vals = [-13.399623, -7.788893, -0.081064, 0.056474]
+    ramp.test_vals_aarch64 = [-13.398422, -7.786461, -0.081064, 0.056474]
     test_list.append(ramp)
 
     ##########################
@@ -324,7 +325,7 @@ def main():
     poiseuille_profile.cfg_file  = "profile_poiseuille.cfg"
     poiseuille_profile.test_iter = 10
     poiseuille_profile.test_vals         = [-12.492939, -7.672950, -0.000000, 2.085796]
-    poiseuille_profile.test_vals_aarch64 = [-12.492842, -7.672800, -0.000000, 2.085796]
+    poiseuille_profile.test_vals_aarch64 = [-12.492864, -7.671632, -0.000000, 2.085796]
     test_list.append(poiseuille_profile)
 
     ##########################
@@ -414,6 +415,7 @@ def main():
     turb_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     turb_naca0012_sst.test_iter = 10
     turb_naca0012_sst.test_vals = [-12.219694, -14.440925, -7.107551, 1.050109, 0.019148, -1.601287, -38.510000]
+    turb_naca0012_sst.test_vals_aarch64 = [-12.219735, -14.440925, -7.107550, 1.050109, 0.019148, -1.601262, -38.510000]
     turb_naca0012_sst.timeout   = 3200
     test_list.append(turb_naca0012_sst)
 
@@ -423,6 +425,7 @@ def main():
     turb_naca0012_sst_sust.cfg_file  = "turb_NACA0012_sst_sust.cfg"
     turb_naca0012_sst_sust.test_iter = 10
     turb_naca0012_sst_sust.test_vals = [-12.148637, -14.756583, -6.342201, 1.001189, 0.019384, -1.579100]
+    turb_naca0012_sst_sust.test_vals_aarch64 = [-12.148716, -14.756582, -6.342200, 1.001189, 0.019384, -1.579104]
     turb_naca0012_sst_sust.timeout   = 3200
     test_list.append(turb_naca0012_sst_sust)
 
@@ -676,7 +679,7 @@ def main():
     turbmod_sa_neg_rae2822.cfg_file  = "turb_SA_NEG_RAE2822.cfg"
     turbmod_sa_neg_rae2822.test_iter = 10
     turbmod_sa_neg_rae2822.test_vals         = [-1.466238, 3.169232, 2.756518, 4.722767, 1.120253, 0.378675, -83444.000000]
-    turbmod_sa_neg_rae2822.test_vals_aarch64 = [-1.347530, 1.439078, 1.306846, -1.928774, 1.480543, 0.571601, -91503]
+    turbmod_sa_neg_rae2822.test_vals_aarch64 = [-1.359612, 1.493629, 1.218367, -1.441703, 1.248499, 0.457987, -86467.000000]
     test_list.append(turbmod_sa_neg_rae2822)
 
     # SA Compressibility Correction
@@ -825,7 +828,7 @@ def main():
     turb_naca0012_1c.cfg_file  = "turb_NACA0012_uq_1c.cfg"
     turb_naca0012_1c.test_iter = 10
     turb_naca0012_1c.test_vals         = [-4.976284, 1.141136, 0.463115, -0.083307]
-    turb_naca0012_1c.test_vals_aarch64 = [-4.983548, 1.138789, 0.456805, -0.079667]
+    turb_naca0012_1c.test_vals_aarch64 = [-4.983453, 1.138491, 0.459947, -0.084114]
     test_list.append(turb_naca0012_1c)
 
     # NACA0012 2c
@@ -834,7 +837,7 @@ def main():
     turb_naca0012_2c.cfg_file  = "turb_NACA0012_uq_2c.cfg"
     turb_naca0012_2c.test_iter = 10
     turb_naca0012_2c.test_vals         = [-5.483317, 0.968654, 0.307611, -0.118062]
-    turb_naca0012_2c.test_vals_aarch64 = [-5.483345, 0.968812, 0.305213, -0.113317]
+    turb_naca0012_2c.test_vals_aarch64 = [-5.483338, 0.968646, 0.308055, -0.117915]
     test_list.append(turb_naca0012_2c)
 
     # NACA0012 3c
@@ -851,7 +854,7 @@ def main():
     turb_naca0012_p1c1.cfg_file  = "turb_NACA0012_uq_p1c1.cfg"
     turb_naca0012_p1c1.test_iter = 10
     turb_naca0012_p1c1.test_vals         = [-5.128887, 1.076846, 0.589839, -0.051939]
-    turb_naca0012_p1c1.test_vals_aarch64 = [-5.130279, 1.076643, 0.587076, -0.047445]
+    turb_naca0012_p1c1.test_vals_aarch64 = [-5.128883, 1.076873, 0.590376, -0.051754]
     test_list.append(turb_naca0012_p1c1)
 
     # NACA0012 p1c2
@@ -860,7 +863,7 @@ def main():
     turb_naca0012_p1c2.cfg_file  = "turb_NACA0012_uq_p1c2.cfg"
     turb_naca0012_p1c2.test_iter = 10
     turb_naca0012_p1c2.test_vals         = [-5.554633, 0.943626, 0.402263, -0.100275]
-    turb_naca0012_p1c2.test_vals_aarch64 = [-5.554645, 0.943709, 0.398620, -0.096021]
+    turb_naca0012_p1c2.test_vals_aarch64 = [-5.554636, 0.943621, 0.401650, -0.100495]
     test_list.append(turb_naca0012_p1c2)
 
     ######################################

From 1e2445071786c680bc260c5b8f3f34fb04e367e1 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 8 Jul 2023 16:22:07 -0700
Subject: [PATCH 566/656] parallel AD

---
 .../disc_adj_fsi/dyn_fsi/grad_dv_aarch64.opt.ref | 16 ++++++++--------
 TestCases/parallel_regression_AD.py              |  5 +++--
 2 files changed, 11 insertions(+), 10 deletions(-)

diff --git a/TestCases/disc_adj_fsi/dyn_fsi/grad_dv_aarch64.opt.ref b/TestCases/disc_adj_fsi/dyn_fsi/grad_dv_aarch64.opt.ref
index 7b1a574aae0..28353aa54bd 100644
--- a/TestCases/disc_adj_fsi/dyn_fsi/grad_dv_aarch64.opt.ref
+++ b/TestCases/disc_adj_fsi/dyn_fsi/grad_dv_aarch64.opt.ref
@@ -1,9 +1,9 @@
 INDEX	GRAD
-0	-3.461461010189737e-03
-1	-1.841786479954763e-03
-2	-7.915536887423713e-04
-3	-2.739622314151781e-04
-4	-2.734869609160976e-04
-5	-7.881163788847894e-04
-6	-1.828978579462100e-03
-7	-3.427219908218581e-03
+0	-3.461460506635121e-03
+1	-1.841786208967458e-03
+2	-7.915535677936552e-04
+3	-2.739621839525785e-04
+4	-2.734869125125620e-04
+5	-7.881162552527191e-04
+6	-1.828978304797359e-03
+7	-3.427219401431795e-03
diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index 93c4cabf278..4b77ca9a6c6 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -231,6 +231,7 @@ def main():
     discadj_trans_stator.cfg_file  = "transonic_stator.cfg"
     discadj_trans_stator.test_iter = 79
     discadj_trans_stator.test_vals = [79, 0.769972, 0.374328, 0.474458, -0.996522, 2.154079, -4.446062]
+    discadj_trans_stator.test_vals_aarch64 = [79.000000, 0.769908, 0.374328, 0.474687, -0.996522, 2.154079, -4.446062]
     test_list.append(discadj_trans_stator)
 
     ###################################
@@ -243,7 +244,7 @@ def main():
     discadj_fea.cfg_file  = "configAD_fem.cfg"
     discadj_fea.test_iter = 4
     discadj_fea.test_vals         = [-2.849453, -3.238429, -0.000364, -8.708700] #last 4 columns
-    discadj_fea.test_vals_aarch64 = [-2.849726, -3.238594, -0.000364, -8.708700] #last 4 columns
+    discadj_fea.test_vals_aarch64 = [-2.849573, -3.238516, -0.000364, -8.708700] #last 4 columns
     test_list.append(discadj_fea)
 
     ###################################
@@ -277,7 +278,7 @@ def main():
     discadj_fsi2.cfg_file  = "config.cfg"
     discadj_fsi2.test_iter = 8
     discadj_fsi2.test_vals         = [-4.349377, 0.192713, -1.303589, 0.75407, 2.3244]
-    discadj_fsi2.test_vals_aarch64 = [-3.479505, 0.127953, -1.303589, 0.75407, 2.3244]
+    discadj_fsi2.test_vals_aarch64 = [-4.349372, 0.190601, -1.303589, 0.754070, 2.324400]
     discadj_fsi2.tol       = 0.00001
     test_list.append(discadj_fsi2)
 

From 883052a817d4ce2634e0bdb2c4061565eac6b18d Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 8 Jul 2023 16:33:35 -0700
Subject: [PATCH 567/656] serial

---
 TestCases/serial_regression.py | 24 +++++++++++++-----------
 1 file changed, 13 insertions(+), 11 deletions(-)

diff --git a/TestCases/serial_regression.py b/TestCases/serial_regression.py
index cd9d7409f59..81d09be9aa1 100644
--- a/TestCases/serial_regression.py
+++ b/TestCases/serial_regression.py
@@ -62,7 +62,7 @@ def main():
     invwedge.cfg_file = "invwedge_ausm.cfg"
     invwedge.test_iter = 10
     invwedge.test_vals = [-1.046323, -1.571086, -18.301251, -18.628639, -18.574676, 2.271778, 1.875687, 5.315769, 0.870008]
-    invwedge.test_vals_aarch64 = [-1.046323, -1.571086, -18.300667, -18.628064, -18.574092, 2.271778, 1.875687, 5.315769, 0.870008]
+    invwedge.test_vals_aarch64 = [-1.046323, -1.571086, -18.301361, -18.628744, -18.574788, 2.271778, 1.875687, 5.315769, 0.870008]
     test_list.append(invwedge)
 
     # Viscous single cone - axisymmetric
@@ -71,7 +71,7 @@ def main():
     visc_cone.cfg_file = "axi_visccone.cfg"
     visc_cone.test_iter = 10
     visc_cone.test_vals = [-5.215236, -5.739371, -20.556662, -20.517023, -20.436970, 1.262783, -3.205463, -0.015695, 0.093205, 32656.000000]
-    visc_cone.test_vals_aarch64 = [-5.215236, -5.739371, -20.556662, -20.517023, -20.436970, 1.262783, -3.205463, -0.015695, 0.093205, 32656.000000]
+    visc_cone.test_vals_aarch64 = [-5.215229, -5.739368, -20.556662, -20.517022, -20.437459, 1.262784, -3.205455, -0.015696, 0.093207, 32656.000000]
     test_list.append(visc_cone)
 
     #########################
@@ -133,7 +133,7 @@ def main():
     polar_naca0012.polar     = True
     polar_naca0012.test_iter = 10
     polar_naca0012.test_vals         = [-1.243326, 4.224483, 0.016432, 0.016145]
-    polar_naca0012.test_vals_aarch64 = [-3.148445, 2.270143, 0.003666, 0.008682]
+    polar_naca0012.test_vals_aarch64 = [-3.538211, 1.882519, 0.002450, 0.008663]
     polar_naca0012.command   = TestCase.Command(exec = "compute_polar.py", param = "-n 1 -i 11")
     test_list.append(polar_naca0012)
 
@@ -194,7 +194,7 @@ def main():
     poiseuille_profile.cfg_file  = "profile_poiseuille.cfg"
     poiseuille_profile.test_iter = 10
     poiseuille_profile.test_vals         = [-12.494681, -7.711642, -0.000000, 2.085796]
-    poiseuille_profile.test_vals_aarch64 = [-12.494705, -7.711332, -0.000000, 2.085796] #last 4 columns
+    poiseuille_profile.test_vals_aarch64 = [-12.494684, -7.711379, -0.000000, 2.085796] #last 4 columns
     test_list.append(poiseuille_profile)
 
     ##########################
@@ -280,7 +280,7 @@ def main():
     turb_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     turb_naca0012_sst.test_iter = 10
     turb_naca0012_sst.test_vals         = [-12.213755, -14.439873, -7.108062, 1.050109, 0.019148, -1.875539, -38.510000]
-    turb_naca0012_sst.test_vals_aarch64 = [-12.213755, -14.439873, -7.108062, 1.050109, 0.019148, -1.875539, -38.510000]
+    turb_naca0012_sst.test_vals_aarch64 = [-12.213728, -14.439873, -7.108062, 1.050109, 0.019148, -1.875538, -38.510000]
     turb_naca0012_sst.timeout   = 3200
     test_list.append(turb_naca0012_sst)
 
@@ -299,6 +299,7 @@ def main():
     turb_naca0012_sst_sust_restart.cfg_file  = "turb_NACA0012_sst_sust.cfg"
     turb_naca0012_sst_sust_restart.test_iter = 10
     turb_naca0012_sst_sust_restart.test_vals = [-12.153015, -14.756601, -6.342509, 1.001189, 0.019384, -1.820009]
+    turb_naca0012_sst_sust_restart.test_vals_aarch64 = [-12.153059, -14.756601, -6.342509, 1.001189, 0.019384, -1.819999]
     turb_naca0012_sst_sust_restart.timeout   = 3200
     test_list.append(turb_naca0012_sst_sust_restart)
 
@@ -330,6 +331,7 @@ def main():
     axi_rans_air_nozzle_restart.cfg_file  = "air_nozzle_restart.cfg"
     axi_rans_air_nozzle_restart.test_iter = 10
     axi_rans_air_nozzle_restart.test_vals = [-12.063377, -7.005051, -8.705733, -4.036815, -2019.8]
+    axi_rans_air_nozzle_restart.test_vals_aarch64 = [-12.063354, -7.004772, -8.705740, -4.036824, -2019.800000]
     axi_rans_air_nozzle_restart.tol       = 0.0001
     test_list.append(axi_rans_air_nozzle_restart)
 
@@ -671,7 +673,7 @@ def main():
     turb_naca0012_1c.cfg_file  = "turb_NACA0012_uq_1c.cfg"
     turb_naca0012_1c.test_iter = 10
     turb_naca0012_1c.test_vals         = [-4.986094, 1.137009, 0.378604, -0.083526]
-    turb_naca0012_1c.test_vals_aarch64 = [-4.985900, 1.137455, 0.376000, -0.078781]
+    turb_naca0012_1c.test_vals_aarch64 = [-4.986054, 1.137073, 0.378618, -0.083513]
     test_list.append(turb_naca0012_1c)
 
     # NACA0012 2c
@@ -680,7 +682,7 @@ def main():
     turb_naca0012_2c.cfg_file  = "turb_NACA0012_uq_2c.cfg"
     turb_naca0012_2c.test_iter = 10
     turb_naca0012_2c.test_vals         = [-5.483291, 0.968701, 0.258168, -0.114217]
-    turb_naca0012_2c.test_vals_aarch64 = [-5.483310, 0.968862, 0.255650, -0.109464] #last 4 columns
+    turb_naca0012_2c.test_vals_aarch64 = [-5.483307, 0.968694, 0.258049, -0.114260] #last 4 columns
     test_list.append(turb_naca0012_2c)
 
     # NACA0012 3c
@@ -697,7 +699,7 @@ def main():
     turb_naca0012_p1c1.cfg_file  = "turb_NACA0012_uq_p1c1.cfg"
     turb_naca0012_p1c1.test_iter = 10
     turb_naca0012_p1c1.test_vals         = [-5.127497, 1.077175, 0.546823, -0.023191]
-    turb_naca0012_p1c1.test_vals_aarch64 = [-5.127512, 1.077345, 0.544130, -0.018555] #last 4 columns
+    turb_naca0012_p1c1.test_vals_aarch64 = [-5.127510, 1.077107, 0.546893, -0.023166] #last 4 columns
     test_list.append(turb_naca0012_p1c1)
 
     # NACA0012 p1c2
@@ -706,7 +708,7 @@ def main():
     turb_naca0012_p1c2.cfg_file  = "turb_NACA0012_uq_p1c2.cfg"
     turb_naca0012_p1c2.test_iter = 10
     turb_naca0012_p1c2.test_vals         = [-5.554412, 0.943562, 0.322803, -0.095946]
-    turb_naca0012_p1c2.test_vals_aarch64 = [-5.554391, 0.943687, 0.320285, -0.091188] #last 4 columns
+    turb_naca0012_p1c2.test_vals_aarch64 = [-5.554381, 0.943577, 0.322676, -0.095989] #last 4 columns
     test_list.append(turb_naca0012_p1c2)
 
     ######################################
@@ -914,7 +916,7 @@ def main():
     channel_3D.cfg_dir   = "sliding_interface/channel_3D"
     channel_3D.cfg_file  = "channel_3D_WA.cfg"
     channel_3D.test_iter = 1
-    channel_3D.test_vals         = [1.000000, 0.000000, 0.661408, 0.769988, 0.696033]
+    channel_3D.test_vals         = [1.000000, 0.000000, 0.661408, 0.769902, 0.695663]
     channel_3D.test_vals_aarch64 = [1.000000, 0.000000, 0.661408, 0.769902, 0.695663] #last 5 columns
     channel_3D.unsteady  = True
     channel_3D.multizone = True
@@ -1497,7 +1499,7 @@ def main():
     pywrapper_turb_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     pywrapper_turb_naca0012_sst.test_iter = 10
     pywrapper_turb_naca0012_sst.test_vals         = [-12.213755, -14.439873, -7.108062, 1.050109, 0.019148, -1.875539, -38.510000]
-    pywrapper_turb_naca0012_sst.test_vals_aarch64 = [-12.213755, -14.439873, -7.108062, 1.050109, 0.019148, -1.875539, -38.510000]
+    pywrapper_turb_naca0012_sst.test_vals_aarch64 = [-12.213728, -14.439873, -7.108062, 1.050109, 0.019148, -1.875538, -38.510000]
     pywrapper_turb_naca0012_sst.command   =  TestCase.Command(exec = "SU2_CFD.py", param = "-f")
     pywrapper_turb_naca0012_sst.timeout   = 3200
     pywrapper_turb_naca0012_sst.tol       = 0.00001

From f67138db9c7e292b9575533fbe92f139f1aed811 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 8 Jul 2023 16:38:59 -0700
Subject: [PATCH 568/656] serial AD

---
 TestCases/serial_regression_AD.py | 3 +--
 1 file changed, 1 insertion(+), 2 deletions(-)

diff --git a/TestCases/serial_regression_AD.py b/TestCases/serial_regression_AD.py
index 9317f318046..39bee1ffb4b 100644
--- a/TestCases/serial_regression_AD.py
+++ b/TestCases/serial_regression_AD.py
@@ -167,8 +167,7 @@ def main():
     discadj_fea.cfg_dir   = "disc_adj_fea"
     discadj_fea.cfg_file  = "configAD_fem.cfg"
     discadj_fea.test_iter = 4
-    discadj_fea.test_vals         = [-2.849844, -3.238713, -3.6413e-04, -8.7087] #last 4 columns
-    discadj_fea.test_vals_aarch64 = [-2.849570, -3.238519, -3.6413e-04, -8.7087] #last 4 columns
+    discadj_fea.test_vals         = [-2.849781, -3.238667, -0.000364, -8.708700]
     test_list.append(discadj_fea)
 
     ###################################

From 959338ec4e7253b1354905995040e97a295eb1d0 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 8 Jul 2023 16:48:43 -0700
Subject: [PATCH 569/656] hybrid

---
 TestCases/hybrid_regression.py | 23 +++++++++--------------
 1 file changed, 9 insertions(+), 14 deletions(-)

diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index 3df7f73d9ca..8a168208577 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -137,7 +137,7 @@ def main():
     poiseuille_profile.cfg_file  = "profile_poiseuille.cfg"
     poiseuille_profile.test_iter = 10
     poiseuille_profile.test_vals         = [-12.494728, -7.712546, -0.000000, 2.085796]
-    poiseuille_profile.test_vals_aarch64 = [-12.494692, -7.710648, -0.000000, 2.085796]
+    poiseuille_profile.test_vals_aarch64 = [-12.494717, -7.711274, -0.000000, 2.085796]
     test_list.append(poiseuille_profile)
 
     # 2D Rotational Periodic
@@ -199,7 +199,7 @@ def main():
     turb_naca0012_sa.cfg_file  = "turb_NACA0012_sa.cfg"
     turb_naca0012_sa.test_iter = 5
     turb_naca0012_sa.test_vals         = [-10.451625, -13.859808, 1.057622, 0.022916, 20.000000, -1.358306, 20.000000, -2.512316, -44.540000]
-    turb_naca0012_sa.test_vals_aarch64 = [-8.627052, -10.377936, 1.064491, 0.019710, 20.000000, -1.763093, 20.000000, -4.794073, -46.506000]
+    turb_naca0012_sa.test_vals_aarch64 = [-10.451625, -13.859809, 1.057622, 0.022916, 20.000000, -1.358307, 20.000000, -2.512316, -44.540000]
     test_list.append(turb_naca0012_sa)
 
     # NACA0012 (SST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
@@ -208,7 +208,6 @@ def main():
     turb_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     turb_naca0012_sst.test_iter = 10
     turb_naca0012_sst.test_vals         = [-12.216989, -14.439370, -7.108639, 1.050109, 0.019148, -1.483537, -38.510000]
-    turb_naca0012_sst.test_vals_aarch64 = [-12.216989, -14.439370, -7.108639, 1.050109, 0.019148, -1.483537, -38.510000]
     test_list.append(turb_naca0012_sst)
 
     # NACA0012 (SST_SUST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
@@ -217,7 +216,6 @@ def main():
     turb_naca0012_sst_sust.cfg_file  = "turb_NACA0012_sst_sust.cfg"
     turb_naca0012_sst_sust.test_iter = 10
     turb_naca0012_sst_sust.test_vals         = [-12.148204, -14.755890, -6.342986, 1.001189, 0.019384, -1.432333]
-    turb_naca0012_sst_sust.test_vals_aarch64 = [-12.148204, -14.755890, -6.342986, 1.001189, 0.019384, -1.432333]
     test_list.append(turb_naca0012_sst_sust)
 
     # NACA0012 (SST, fixed values for turbulence quantities)
@@ -226,7 +224,7 @@ def main():
     turb_naca0012_sst_fixedvalues.cfg_file  = "turb_NACA0012_sst_fixedvalues.cfg"
     turb_naca0012_sst_fixedvalues.test_iter = 10
     turb_naca0012_sst_fixedvalues.test_vals         = [-5.192598, -10.042489, -1.617721, 1.022073, 0.040198, -2.381138]
-    turb_naca0012_sst_fixedvalues.test_vals_aarch64 = [-5.192501, -9.575897, -1.568269, 1.022571, 0.040527, -2.384327]
+    turb_naca0012_sst_fixedvalues.test_vals_aarch64 = [-5.192599, -10.042490, -1.617720, 1.022073, 0.040198, -2.381138]
     test_list.append(turb_naca0012_sst_fixedvalues)
 
     # NACA0012 (SST, explicit Euler for flow and turbulence equations)
@@ -255,7 +253,6 @@ def main():
     axi_rans_air_nozzle_restart.cfg_file  = "air_nozzle_restart.cfg"
     axi_rans_air_nozzle_restart.test_iter = 10
     axi_rans_air_nozzle_restart.test_vals         = [-12.060634, -6.992273, -8.808757, -4.097753, -2019.800000]
-    axi_rans_air_nozzle_restart.test_vals_aarch64 = [-12.060634, -6.992273, -8.808757, -4.097753, -2019.800000]
     test_list.append(axi_rans_air_nozzle_restart)
 
     #################################
@@ -281,7 +278,7 @@ def main():
     turb_naca0012_1c.cfg_file  = "turb_NACA0012_uq_1c.cfg"
     turb_naca0012_1c.test_iter = 10
     turb_naca0012_1c.test_vals         = [-4.980878, 1.138865, 0.247731, -0.117335]
-    turb_naca0012_1c.test_vals_aarch64 = [-4.981149, 1.139192, 0.244886, -0.112789]
+    turb_naca0012_1c.test_vals_aarch64 = [-4.981105, 1.138873, 0.248013, -0.117248]
     test_list.append(turb_naca0012_1c)
 
     # NACA0012 2c
@@ -290,7 +287,7 @@ def main():
     turb_naca0012_2c.cfg_file  = "turb_NACA0012_uq_2c.cfg"
     turb_naca0012_2c.test_iter = 10
     turb_naca0012_2c.test_vals         = [-5.483313, 0.968731, 0.215420, -0.124767]
-    turb_naca0012_2c.test_vals_aarch64 = [-5.483350, 0.968882, 0.212493, -0.120171]
+    turb_naca0012_2c.test_vals_aarch64 = [-5.483345, 0.968720, 0.214914, -0.124932]
     test_list.append(turb_naca0012_2c)
 
     # NACA0012 3c
@@ -299,7 +296,7 @@ def main():
     turb_naca0012_3c.cfg_file  = "turb_NACA0012_uq_3c.cfg"
     turb_naca0012_3c.test_iter = 10
     turb_naca0012_3c.test_vals         = [-5.584300, 0.931293, 0.207446, -0.125692]
-    turb_naca0012_3c.test_vals_aarch64 = [-5.584300, 0.931383, 0.205116, -0.120891]
+    turb_naca0012_3c.test_vals_aarch64 = [-5.584300, 0.931293, 0.207447, -0.125691]
     test_list.append(turb_naca0012_3c)
 
     # NACA0012 p1c1
@@ -308,7 +305,7 @@ def main():
     turb_naca0012_p1c1.cfg_file  = "turb_NACA0012_uq_p1c1.cfg"
     turb_naca0012_p1c1.test_iter = 10
     turb_naca0012_p1c1.test_vals         = [-5.132363, 1.075634, 0.337251, -0.082829]
-    turb_naca0012_p1c1.test_vals_aarch64 = [-5.132731, 1.075863, 0.333419, -0.078553]
+    turb_naca0012_p1c1.test_vals_aarch64 = [-5.132358, 1.075658, 0.337268, -0.082827]
     test_list.append(turb_naca0012_p1c1)
 
     # NACA0012 p1c2
@@ -317,7 +314,7 @@ def main():
     turb_naca0012_p1c2.cfg_file  = "turb_NACA0012_uq_p1c2.cfg"
     turb_naca0012_p1c2.test_iter = 10
     turb_naca0012_p1c2.test_vals         = [-5.554392, 0.943703, 0.229483, -0.121058]
-    turb_naca0012_p1c2.test_vals_aarch64 = [-5.554433, 0.943787, 0.226530, -0.116503]
+    turb_naca0012_p1c2.test_vals_aarch64 = [-5.554425, 0.943683, 0.229293, -0.121125]
     test_list.append(turb_naca0012_p1c2)
 
     ######################################
@@ -458,7 +455,7 @@ def main():
     square_cylinder.cfg_file  = "turb_square.cfg"
     square_cylinder.test_iter = 3
     square_cylinder.test_vals = [-2.557949, -1.173575, 0.058030, 1.399794, 2.220402, 1.399748, 2.218603, -0.453270]
-    square_cylinder.test_vals_aarch64 = [-2.558106, -1.162563, 0.066386, 1.399788, 2.220402, 1.399743, 2.218603, -0.453110]
+    square_cylinder.test_vals_aarch64 = [-2.557902, -1.173574, 0.058050, 1.399794, 2.220402, 1.399748, 2.218604, -0.453270]
     square_cylinder.unsteady  = True
     test_list.append(square_cylinder)
 
@@ -566,7 +563,6 @@ def main():
     axial_stage2D.cfg_file  = "Axial_stage2D.cfg"
     axial_stage2D.test_iter = 20
     axial_stage2D.test_vals         = [0.974788, 1.534326, -2.897693, 2.599374, -2.418314, 3.087291, 106380.000000, 106380.000000]
-    axial_stage2D.test_vals_aarch64 = [1.047244, 1.661126, -2.914064, 2.588061, -2.486924, 3.050785, 106380, 106380]
     test_list.append(axial_stage2D)
 
     # 2D transonic stator restart
@@ -575,7 +571,6 @@ def main():
     transonic_stator_restart.cfg_file  = "transonic_stator_restart.cfg"
     transonic_stator_restart.test_iter = 20
     transonic_stator_restart.test_vals         = [-5.346503, -3.510597, -3.156830, 0.752511, -3.834382, 1.816610, -471690]
-    transonic_stator_restart.test_vals_aarch64 = [-5.346503, -3.510597, -3.156830, 0.752511, -3.834382, 1.816610, -471690]
     test_list.append(transonic_stator_restart)
 
     ######################################

From 2c0e77c97c2aa5ffc04b8c8cb09cf69f7d019db7 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 8 Jul 2023 17:01:15 -0700
Subject: [PATCH 570/656] hybrid AD

---
 TestCases/hybrid_regression_AD.py | 9 +++++----
 1 file changed, 5 insertions(+), 4 deletions(-)

diff --git a/TestCases/hybrid_regression_AD.py b/TestCases/hybrid_regression_AD.py
index ed6dae1a519..ceaec1f9a0e 100644
--- a/TestCases/hybrid_regression_AD.py
+++ b/TestCases/hybrid_regression_AD.py
@@ -75,8 +75,7 @@ def main():
     discadj_rans_naca0012_sa.cfg_dir   = "disc_adj_rans/naca0012"
     discadj_rans_naca0012_sa.cfg_file  = "turb_NACA0012_sa.cfg"
     discadj_rans_naca0012_sa.test_iter = 10
-    discadj_rans_naca0012_sa.test_vals         = [-2.230621, 0.644162, 0.177890, -0.000016, 5.000000, -3.007652, 5.000000, -7.728093]
-    discadj_rans_naca0012_sa.test_vals_aarch64 = [-2.230631, 0.644954, 0.177890, -0.000016, 5.000000, -3.007651, 5.000000, -7.631909]
+    discadj_rans_naca0012_sa.test_vals = [-2.230621, 0.644162, 0.177890, -0.000016, 5.000000, -3.007652, 5.000000, -7.728093]
     test_list.append(discadj_rans_naca0012_sa)
 
     # Adjoint turbulent NACA0012 SST
@@ -194,7 +193,7 @@ def main():
     discadj_trans_stator.cfg_file  = "transonic_stator.cfg"
     discadj_trans_stator.test_iter = 79
     discadj_trans_stator.test_vals         = [79, 0.770065, 0.383137, 0.472153, -0.996484, 2.153296, -4.444301]
-    discadj_trans_stator.test_vals_aarch64 = [79, 0.770065, 0.383137, 0.472153, -0.996484, 2.153296, -4.444301]
+    discadj_trans_stator.test_vals_aarch64 = [79, 0.769987, 0.383135, 0.472391, -0.996504, 2.153296, -4.444301]
     test_list.append(discadj_trans_stator)
 
     ###################################
@@ -207,7 +206,7 @@ def main():
     discadj_fea.cfg_file  = "configAD_fem.cfg"
     discadj_fea.test_iter = 4
     discadj_fea.test_vals         = [1.774569, 1.928023, -0.000364, -8.690300]
-    discadj_fea.test_vals_aarch64 = [2.216938, 2.129429, -0.000365, -8.782500]
+    discadj_fea.test_vals_aarch64 = [1.939275, 1.989717, -0.000364, -8.708200]
     test_list.append(discadj_fea)
 
     ######################################
@@ -232,6 +231,7 @@ def main():
     pywrapper_FEA_AD_FlowLoad.cfg_file      = "configAD_fem.cfg"
     pywrapper_FEA_AD_FlowLoad.test_iter     = 100
     pywrapper_FEA_AD_FlowLoad.test_vals     = [-0.131742, -0.553318, -0.000364, -0.003101] #last 4 columns
+    pywrapper_FEA_AD_FlowLoad.test_vals_aarch64 = [-0.132166, -0.554904, -0.000364, -0.003101]
     pywrapper_FEA_AD_FlowLoad.command       = TestCase.Command(exec = "python", param = "run_adjoint.py --parallel -f")
     pywrapper_FEA_AD_FlowLoad.timeout       = 1600
     pywrapper_FEA_AD_FlowLoad.tol           = 1e-4
@@ -245,6 +245,7 @@ def main():
     pywrapper_CFD_AD_MeshDisp.cfg_file      = "configAD_flow.cfg"
     pywrapper_CFD_AD_MeshDisp.test_iter     = 1000
     pywrapper_CFD_AD_MeshDisp.test_vals     = [30.000000, -2.520967, 1.375188, 0.000000] #last 4 columns
+    pywrapper_CFD_AD_MeshDisp.test_vals_aarch64 = [30.000000, -2.516536, 1.386443, 0.000000]
     pywrapper_CFD_AD_MeshDisp.command       = TestCase.Command(exec = "python", param = "run_adjoint.py --parallel -f")
     pywrapper_CFD_AD_MeshDisp.timeout       = 1600
     pywrapper_CFD_AD_MeshDisp.tol           = 1e-4

From aa086b0704153ed71e5b8ead46073ebd127cdb84 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Sat, 8 Jul 2023 18:17:26 -0700
Subject: [PATCH 571/656] Apply suggestions from code review

---
 TestCases/serial_regression.py    | 2 +-
 TestCases/serial_regression_AD.py | 1 +
 TestCases/vandv.py                | 1 -
 3 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/TestCases/serial_regression.py b/TestCases/serial_regression.py
index 81d09be9aa1..3317106160d 100644
--- a/TestCases/serial_regression.py
+++ b/TestCases/serial_regression.py
@@ -916,7 +916,7 @@ def main():
     channel_3D.cfg_dir   = "sliding_interface/channel_3D"
     channel_3D.cfg_file  = "channel_3D_WA.cfg"
     channel_3D.test_iter = 1
-    channel_3D.test_vals         = [1.000000, 0.000000, 0.661408, 0.769902, 0.695663]
+    channel_3D.test_vals         = [1.000000, 0.000000, 0.661408, 0.769988, 0.696033]
     channel_3D.test_vals_aarch64 = [1.000000, 0.000000, 0.661408, 0.769902, 0.695663] #last 5 columns
     channel_3D.unsteady  = True
     channel_3D.multizone = True
diff --git a/TestCases/serial_regression_AD.py b/TestCases/serial_regression_AD.py
index 39bee1ffb4b..6d0a32046f2 100644
--- a/TestCases/serial_regression_AD.py
+++ b/TestCases/serial_regression_AD.py
@@ -168,6 +168,7 @@ def main():
     discadj_fea.cfg_file  = "configAD_fem.cfg"
     discadj_fea.test_iter = 4
     discadj_fea.test_vals         = [-2.849781, -3.238667, -0.000364, -8.708700]
+    discadj_fea.tol               = 0.00007
     test_list.append(discadj_fea)
 
     ###################################
diff --git a/TestCases/vandv.py b/TestCases/vandv.py
index 4770c6088c3..4c798598bc2 100644
--- a/TestCases/vandv.py
+++ b/TestCases/vandv.py
@@ -115,4 +115,3 @@ def main():
 
 if __name__ == '__main__':
     main()
-= [-11.527743, -11.150388, -11.944924, -10.750834, -11.116769, -4.030059, 0.002339, -2.730392, -4.067274, 1.276300]

From 137db955696f27106b6f71d311ef88e02633d508 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 9 Jul 2023 14:23:20 -0700
Subject: [PATCH 572/656] more updates and fix a race condition

---
 TestCases/hybrid_regression_AD.py            |  2 +-
 TestCases/parallel_regression.py             | 25 ++++++++++++--------
 TestCases/py_wrapper/wavy_wall/run_steady.py | 14 +++++++----
 TestCases/serial_regression.py               |  2 +-
 4 files changed, 27 insertions(+), 16 deletions(-)

diff --git a/TestCases/hybrid_regression_AD.py b/TestCases/hybrid_regression_AD.py
index ceaec1f9a0e..5b6d6894315 100644
--- a/TestCases/hybrid_regression_AD.py
+++ b/TestCases/hybrid_regression_AD.py
@@ -231,7 +231,7 @@ def main():
     pywrapper_FEA_AD_FlowLoad.cfg_file      = "configAD_fem.cfg"
     pywrapper_FEA_AD_FlowLoad.test_iter     = 100
     pywrapper_FEA_AD_FlowLoad.test_vals     = [-0.131742, -0.553318, -0.000364, -0.003101] #last 4 columns
-    pywrapper_FEA_AD_FlowLoad.test_vals_aarch64 = [-0.132166, -0.554904, -0.000364, -0.003101]
+    pywrapper_FEA_AD_FlowLoad.test_vals_aarch64 = [-0.131745, -0.553214, -0.000364, -0.003101]
     pywrapper_FEA_AD_FlowLoad.command       = TestCase.Command(exec = "python", param = "run_adjoint.py --parallel -f")
     pywrapper_FEA_AD_FlowLoad.timeout       = 1600
     pywrapper_FEA_AD_FlowLoad.tol           = 1e-4
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index a401724958a..cf9922edb4e 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -245,7 +245,7 @@ def main():
     polar_naca0012.polar     = True
     polar_naca0012.test_iter = 10
     polar_naca0012.test_vals         = [-1.217981, 4.256386, 0.009084, 0.016823]
-    polar_naca0012.test_vals_aarch64 = [-6.491535, -1.076111, 0.001168, 0.008666]
+    polar_naca0012.test_vals_aarch64 = [-1.718925, 3.711429, 0.009217, 0.007784]
     polar_naca0012.command   = TestCase.Command(exec = "compute_polar.py", param = "-i 11")
     test_list.append(polar_naca0012)
 
@@ -999,24 +999,26 @@ def main():
     coolprop_fluidModel.cfg_file  = "fluidModel.cfg"
     coolprop_fluidModel.test_iter = 5
     coolprop_fluidModel.test_vals = [-4.525459, -1.578697, 3.443116, 0.000000, 0.000000]
+    coolprop_fluidModel.enabled_on_cpu_arch = ["x86_64"]
     test_list.append(coolprop_fluidModel)
 
-    # Rarefaction Q1D nozzle, include CoolProp fluid model
-    datadriven_fluidModel           = TestCase('datadriven_fluidModel')
-    datadriven_fluidModel.cfg_dir   = "nicf/datadriven"
-    datadriven_fluidModel.cfg_file  = "datadriven_nozzle.cfg"
-    datadriven_fluidModel.test_iter = 50
-    datadriven_fluidModel.test_vals = [-2.623890, 0.145236, 4.688439, 0.000000, 0.000000]
-    test_list.append(datadriven_fluidModel)
-
     # Rarefaction Q1D nozzle, include CoolProp transport model
     coolprop_transportModel           = TestCase('coolprop_transportModel')
     coolprop_transportModel.cfg_dir   = "nicf/coolprop"
     coolprop_transportModel.cfg_file  = "transportModel.cfg"
     coolprop_transportModel.test_iter = 5
     coolprop_transportModel.test_vals = [-4.527922, -1.308648, 4.630717, 0.000000, 0.000000]
+    coolprop_transportModel.enabled_on_cpu_arch = ["x86_64"]
     test_list.append(coolprop_transportModel)
 
+    # Rarefaction Q1D nozzle, include data-driven fluid model
+    datadriven_fluidModel           = TestCase('datadriven_fluidModel')
+    datadriven_fluidModel.cfg_dir   = "nicf/datadriven"
+    datadriven_fluidModel.cfg_file  = "datadriven_nozzle.cfg"
+    datadriven_fluidModel.test_iter = 50
+    datadriven_fluidModel.test_vals = [-2.623890, 0.145236, 4.688439, 0.000000, 0.000000]
+    test_list.append(datadriven_fluidModel)
+
     ######################################
     ### Turbomachinery                 ###
     ######################################
@@ -1228,7 +1230,7 @@ def main():
     solid_periodic_pins.cfg_file  = "configSolid.cfg"
     solid_periodic_pins.test_iter = 750
     solid_periodic_pins.test_vals = [-15.878977, -14.569206, 300.900000, 425.320000, 0.000000, 5.000000, -1.672737]
-    solid_periodic_pins.test_vals_aarch64 = [-15.879010, -14.569206, 300.900000, 425.320000, 0.000000, 5.000000, -1.672630] #last 7 lines
+    solid_periodic_pins.test_vals_aarch64 = [-15.879016, -14.569206, 300.900000, 425.320000, 0.000000, 5.000000, -1.672666]
     test_list.append(solid_periodic_pins)
 
     # ###############################
@@ -1291,6 +1293,7 @@ def main():
     pywrapper_turb_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     pywrapper_turb_naca0012_sst.test_iter = 10
     pywrapper_turb_naca0012_sst.test_vals = [-12.219694, -14.440925, -7.107551, 1.050109, 0.019148, -1.601287, -38.510000]
+    pywrapper_turb_naca0012_sst.test_vals_aarch64 = [-12.219735, -14.440925, -7.107550, 1.050109, 0.019148, -1.601262, -38.510000]
     pywrapper_turb_naca0012_sst.command   = TestCase.Command("mpirun -np 2", "SU2_CFD.py", "--parallel -f")
     pywrapper_turb_naca0012_sst.timeout   = 3200
     test_list.append(pywrapper_turb_naca0012_sst)
@@ -1301,6 +1304,7 @@ def main():
     pywrapper_square_cylinder.cfg_file  = "turb_square.cfg"
     pywrapper_square_cylinder.test_iter = 10
     pywrapper_square_cylinder.test_vals = [-1.175619, -0.352238, 1.408450, 2.360729, 1.404693, 2.302284, -0.347980]
+    pywrapper_square_cylinder.test_vals_aarch64 = [-1.175617, -0.352079, 1.408450, 2.360729, 1.404693, 2.302284, -0.347980]
     pywrapper_square_cylinder.command   = TestCase.Command("mpirun -np 2", "SU2_CFD.py", "--parallel -f")
     pywrapper_square_cylinder.unsteady  = True
     test_list.append(pywrapper_square_cylinder)
@@ -1321,6 +1325,7 @@ def main():
     pywrapper_custom_fea_load.cfg_file = "config.cfg"
     pywrapper_custom_fea_load.test_iter = 13
     pywrapper_custom_fea_load.test_vals = [-7.263559, -4.946814, -14.165142, 34.000000, -6.380144, 320.580000]
+    pywrapper_custom_fea_load.test_vals_aarch64 = [-7.263558, -4.946814, -14.165142, 35.000000, -6.802790, 320.580000]
     pywrapper_custom_fea_load.command = TestCase.Command("mpirun -np 2", "python", "run.py")
     test_list.append(pywrapper_custom_fea_load)
 
diff --git a/TestCases/py_wrapper/wavy_wall/run_steady.py b/TestCases/py_wrapper/wavy_wall/run_steady.py
index e65ff6408e9..3f0372cf646 100644
--- a/TestCases/py_wrapper/wavy_wall/run_steady.py
+++ b/TestCases/py_wrapper/wavy_wall/run_steady.py
@@ -143,9 +143,12 @@ def RunPrimal(channel_width, deform_amplitude):
     Returns the objective function.
     """
     comm = MPI.COMM_WORLD
+    rank = comm.Get_rank()
 
-    with open('config.cfg', 'w') as f:
-        f.write(common_settings.replace('__WIDTH__', str(channel_width)) + primal_settings)
+    if rank == 0:
+        with open('config.cfg', 'w') as f:
+            f.write(common_settings.replace('__WIDTH__', str(channel_width)) + primal_settings)
+    comm.Barrier()
 
     # Initialize the corresponding driver of SU2, this includes solver preprocessing.
     try:
@@ -174,9 +177,12 @@ def RunAdjoint(channel_width, deform_amplitude):
     Returns the sensitivity of the objective function to the amplitude and width.
     """
     comm = MPI.COMM_WORLD
+    rank = comm.Get_rank()
 
-    with open('config_ad.cfg', 'w') as f:
-        f.write(common_settings.replace('__WIDTH__', str(channel_width)) + adjoint_settings)
+    if rank == 0:
+        with open('config_ad.cfg', 'w') as f:
+            f.write(common_settings.replace('__WIDTH__', str(channel_width)) + adjoint_settings)
+    comm.Barrier()
 
     # Initialize the corresponding driver of SU2, this includes solver preprocessing.
     try:
diff --git a/TestCases/serial_regression.py b/TestCases/serial_regression.py
index 3317106160d..d6512b98c8b 100644
--- a/TestCases/serial_regression.py
+++ b/TestCases/serial_regression.py
@@ -133,7 +133,7 @@ def main():
     polar_naca0012.polar     = True
     polar_naca0012.test_iter = 10
     polar_naca0012.test_vals         = [-1.243326, 4.224483, 0.016432, 0.016145]
-    polar_naca0012.test_vals_aarch64 = [-3.538211, 1.882519, 0.002450, 0.008663]
+    polar_naca0012.test_vals_aarch64 = [-1.811046, 3.612379, 0.012330, 0.009194]
     polar_naca0012.command   = TestCase.Command(exec = "compute_polar.py", param = "-n 1 -i 11")
     test_list.append(polar_naca0012)
 

From f06a8807d09c9115fe0d2d13cd75e1d9a0fefee1 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 10 Jul 2023 11:25:17 +0200
Subject: [PATCH 573/656] Added MLP interpolation option for flamelet fluid
 model

---
 SU2_CFD/include/fluid/CFluidFlamelet.hpp |  16 ++++
 SU2_CFD/src/fluid/CFluidFlamelet.cpp     | 112 +++++++++++++++++++----
 2 files changed, 109 insertions(+), 19 deletions(-)

diff --git a/SU2_CFD/include/fluid/CFluidFlamelet.hpp b/SU2_CFD/include/fluid/CFluidFlamelet.hpp
index 4d4906be6a7..c758887a35b 100644
--- a/SU2_CFD/include/fluid/CFluidFlamelet.hpp
+++ b/SU2_CFD/include/fluid/CFluidFlamelet.hpp
@@ -28,6 +28,11 @@
 #pragma once
 
 #include "../../Common/include/containers/CLookUpTable.hpp"
+#if defined(HAVE_MLPCPP)
+#define MLP_CUSTOM_TYPE su2double
+#include "../../../subprojects/MLPCpp/include/CLookUp_ANN.hpp"
+#define USE_MLPCPP
+#endif
 #include "CFluidModel.hpp"
 
 class CFluidFlamelet final : public CFluidModel {
@@ -47,6 +52,8 @@ class CFluidFlamelet final : public CFluidModel {
   unsigned long extrapolation;
   
   INC_DENSITYMODEL density_model;
+  vector<string> controlling_variable_names,
+                 passive_specie_names;
   vector<string> table_scalar_names; /*!< \brief vector to store names of scalar variables.   */
 
   su2double mass_diffusivity, /*!< \brief local mass diffusivity of the mixture */
@@ -54,6 +61,15 @@ class CFluidFlamelet final : public CFluidModel {
 
   CLookUpTable* look_up_table;
 
+  /*--- Class variables for the multi-layer perceptron method ---*/
+#ifdef USE_MLPCPP
+  MLPToolbox::CLookUp_ANN* lookup_mlp; /*!< \brief Multi-layer perceptron collection. */
+  MLPToolbox::CIOMap* iomap_TD;      /*!< \brief Input-output map for thermochemical properties. */
+  MLPToolbox::CIOMap* iomap_Sources; /*!< \brief Input-output map for species source terms. */
+  MLPToolbox::CIOMap* iomap_LookUp;  /*!< \brief Input-output map for passive look-up terms. */
+  MLPToolbox::CIOMap* iomap_Current;
+#endif
+
   vector<su2double> scalars_vector;
 
   vector<string> varnames_TD, /*!< \brief Lookup names for thermodynamic state variables. */
diff --git a/SU2_CFD/src/fluid/CFluidFlamelet.cpp b/SU2_CFD/src/fluid/CFluidFlamelet.cpp
index a871e548a48..f4e22cead73 100644
--- a/SU2_CFD/src/fluid/CFluidFlamelet.cpp
+++ b/SU2_CFD/src/fluid/CFluidFlamelet.cpp
@@ -27,6 +27,10 @@
 
 #include "../include/fluid/CFluidFlamelet.hpp"
 #include "../../../Common/include/containers/CLookUpTable.hpp"
+#if defined(HAVE_MLPCPP)
+#include "../../../subprojects/MLPCpp/include/CLookUp_ANN.hpp"
+#define USE_MLPCPP
+#endif
 
 CFluidFlamelet::CFluidFlamelet(CConfig* config, su2double value_pressure_operating) : CFluidModel() {
   rank = SU2_MPI::GetRank();
@@ -44,6 +48,25 @@ CFluidFlamelet::CFluidFlamelet(CConfig* config, su2double value_pressure_operati
     cout << "Number of control variables: " << n_control_vars << endl;
   }
 
+  scalars_vector.resize(n_scalars);
+
+  table_scalar_names.resize(n_scalars);
+  for (auto iCV=0u; iCV<n_control_vars; iCV++)
+    table_scalar_names[iCV] = config->GetControllingVariableName(iCV);
+  
+  /*--- auxiliary species transport equations---*/
+  for (size_t i_aux = 0; i_aux < n_user_scalars; i_aux++) {
+    table_scalar_names[n_control_vars + i_aux] = config->GetUserScalarName(i_aux);
+  }
+
+  controlling_variable_names.resize(n_control_vars);
+  for (auto iCV=0u; iCV<n_control_vars; iCV++)
+    controlling_variable_names[iCV] = config->GetControllingVariableName(iCV);
+  
+  passive_specie_names.resize(n_user_scalars);
+  for (auto i_aux=0u; i_aux < n_user_scalars; i_aux++) 
+    passive_specie_names[i_aux] = config->GetUserScalarName(i_aux);
+  
   switch (Kind_DataDriven_Method)
   {
   case ENUM_DATADRIVEN_METHOD::LUT:
@@ -52,32 +75,47 @@ CFluidFlamelet::CFluidFlamelet(CConfig* config, su2double value_pressure_operati
       cout << "***   initializing the lookup table   ***" << endl;
       cout << "*****************************************" << endl;
     }
+    look_up_table = new CLookUpTable(config->GetDataDriven_FileNames()[0], table_scalar_names[I_PROGVAR], table_scalar_names[I_ENTH]);
     break;
   default:
-    SU2_MPI::Error("Interpolation method not implemented for flamelet solver.", CURRENT_FUNCTION);
+    if (rank == MASTER_NODE) {
+      cout << "***********************************************" << endl;
+      cout << "*** initializing the multi-layer perceptron ***" << endl;
+      cout << "***********************************************" << endl;
+    }
+#ifdef USE_MLPCPP
+      lookup_mlp = new MLPToolbox::CLookUp_ANN(config->GetNDataDriven_Files(), config->GetDataDriven_FileNames());
+      if ((rank == MASTER_NODE)) lookup_mlp->DisplayNetworkInfo();
+#else
+      SU2_MPI::Error("SU2 was not compiled with MLPCpp enabled (-Denable-mlpcpp=true).", CURRENT_FUNCTION);
+#endif
     break;
   }
-
-  scalars_vector.resize(n_scalars);
-
-  table_scalar_names.resize(n_scalars);
-  for (auto iCV=0u; iCV<n_control_vars; iCV++)
-    table_scalar_names[iCV] = config->GetControllingVariableName(iCV);
   
-  /*--- auxiliary species transport equations---*/
-  for (size_t i_aux = 0; i_aux < n_user_scalars; i_aux++) {
-    table_scalar_names[n_control_vars + i_aux] = config->GetUserScalarName(i_aux);
-  }
-
-  look_up_table = new CLookUpTable(config->GetDataDriven_FileNames()[0], table_scalar_names[I_PROGVAR], table_scalar_names[I_ENTH]);
-
   Pressure = value_pressure_operating;
 
   PreprocessLookUp(config);
  
 }
 
-CFluidFlamelet::~CFluidFlamelet() { delete look_up_table; }
+CFluidFlamelet::~CFluidFlamelet() { 
+  switch (Kind_DataDriven_Method)
+  {
+  case ENUM_DATADRIVEN_METHOD::LUT:
+    delete look_up_table; 
+    break;
+  case ENUM_DATADRIVEN_METHOD::MLP:
+#ifdef USE_MLPCPP
+    delete iomap_TD;
+    delete iomap_Sources;
+    delete iomap_LookUp;
+    delete lookup_mlp;
+#endif
+    break;
+  default:
+    break;
+  }
+}
 
 void CFluidFlamelet::SetTDState_T(su2double val_temperature, const su2double* val_scalars) {
   for (auto iVar = 0u; iVar < n_scalars; iVar++) scalars_vector[iVar] = val_scalars[iVar];
@@ -157,6 +195,16 @@ void CFluidFlamelet::PreprocessLookUp(CConfig* config) {
   for (auto iLookup=0u; iLookup < n_lookups; iLookup++)
     varnames_LookUp[iLookup] = config->GetLookupName(iLookup);
 
+  if (Kind_DataDriven_Method == ENUM_DATADRIVEN_METHOD::MLP) {
+#ifdef USE_MLPCPP
+    iomap_TD = new MLPToolbox::CIOMap(controlling_variable_names, varnames_TD);
+    iomap_Sources = new MLPToolbox::CIOMap(controlling_variable_names, varnames_Sources);
+    iomap_LookUp = new MLPToolbox::CIOMap(controlling_variable_names, varnames_LookUp);
+    lookup_mlp->PairVariableswithMLPs(*iomap_TD);
+    lookup_mlp->PairVariableswithMLPs(*iomap_Sources);
+    lookup_mlp->PairVariableswithMLPs(*iomap_LookUp);
+#endif
+  }
 }
 
 unsigned long CFluidFlamelet::EvaluateDataSet(vector<su2double> &input_scalar, unsigned short lookup_type, vector<su2double> &output_refs) {
@@ -165,16 +213,26 @@ unsigned long CFluidFlamelet::EvaluateDataSet(vector<su2double> &input_scalar, u
   su2double val_mixfrac = include_mixture_fraction ? input_scalar[I_MIXFRAC] : 0.0;
   vector<string> varnames;
   vector<su2double> val_vars;
+  vector<su2double*> refs_vars;
   switch (lookup_type)
   {
   case FLAMELET_LOOKUP_OPS::TD:
     varnames = varnames_TD;
+  #ifdef USE_MLPCPP
+    iomap_Current = iomap_TD;
+  #endif
     break;
   case FLAMELET_LOOKUP_OPS::SOURCES:
     varnames = varnames_Sources;
+  #ifdef USE_MLPCPP
+    iomap_Current = iomap_Sources;
+  #endif
     break;
   case FLAMELET_LOOKUP_OPS::LOOKUP:
     varnames = varnames_LookUp;
+  #ifdef USE_MLPCPP
+    iomap_Current = iomap_LookUp;
+  #endif
     break;
   default:
     break;
@@ -183,11 +241,27 @@ unsigned long CFluidFlamelet::EvaluateDataSet(vector<su2double> &input_scalar, u
     SU2_MPI::Error(string("Output vector size incompatible with manifold lookup operation."), CURRENT_FUNCTION);
 
   /*--- Add all quantities and their names to the look up vectors. ---*/
-  if (include_mixture_fraction) {
-    extrapolation = look_up_table->LookUp_XYZ(varnames, output_refs, val_prog, val_enth, val_mixfrac);
-  } else {
-    extrapolation = look_up_table->LookUp_XY(varnames, output_refs, val_prog, val_enth);
+  switch (Kind_DataDriven_Method)
+  {
+  case ENUM_DATADRIVEN_METHOD::LUT:
+    if (include_mixture_fraction) {
+      extrapolation = look_up_table->LookUp_XYZ(varnames, output_refs, val_prog, val_enth, val_mixfrac);
+    } else {
+      extrapolation = look_up_table->LookUp_XY(varnames, output_refs, val_prog, val_enth);
+    }
+    break;
+  case ENUM_DATADRIVEN_METHOD::MLP:
+    refs_vars.resize(output_refs.size());
+    for (auto iVar=0u; iVar<output_refs.size(); iVar++)
+      refs_vars[iVar] = &output_refs[iVar];
+#ifdef USE_MLPCPP
+    extrapolation = lookup_mlp->PredictANN(iomap_Current, input_scalar, refs_vars);
+#endif
+    break;
+  default:
+    break;
   }
+  
 
   return extrapolation;
 }

From 7dfc9c23ea98a6d3a421267e3b058c8725a01a90 Mon Sep 17 00:00:00 2001
From: MastermindScope <81287997+MastermindScope@users.noreply.github.com>
Date: Mon, 10 Jul 2023 11:33:01 +0200
Subject: [PATCH 574/656] Add Velocity Output To CFlowCompOutput.cpp

Added Velocity output, since I am interested in that and adding it only in the config just gets ignored and no output happens
---
 SU2_CFD/src/output/CFlowCompOutput.cpp | 3 +++
 1 file changed, 3 insertions(+)

diff --git a/SU2_CFD/src/output/CFlowCompOutput.cpp b/SU2_CFD/src/output/CFlowCompOutput.cpp
index 953c1d9015f..d57e59997a9 100644
--- a/SU2_CFD/src/output/CFlowCompOutput.cpp
+++ b/SU2_CFD/src/output/CFlowCompOutput.cpp
@@ -218,8 +218,11 @@ void CFlowCompOutput::SetVolumeOutputFields(CConfig *config){
   AddVolumeOutput("DENSITY",    "Density",    "SOLUTION", "Density");
   AddVolumeOutput("MOMENTUM-X", "Momentum_x", "SOLUTION", "x-component of the momentum vector");
   AddVolumeOutput("MOMENTUM-Y", "Momentum_y", "SOLUTION", "y-component of the momentum vector");
+  AddVolumeOutput("VELOCITY-X", "Veocity_x", "SOLUTION", "x-component of the velocity vector");
+  AddVolumeOutput("VELOCITY-Y", "Velocity_y", "SOLUTION", "y-component of the velocity vector");
   if (nDim == 3)
     AddVolumeOutput("MOMENTUM-Z", "Momentum_z", "SOLUTION", "z-component of the momentum vector");
+    AddVolumeOutput("VELOCITY-Z", "Velocity_z", "SOLUTION", "z-component of the velocity vector");
   AddVolumeOutput("ENERGY",     "Energy",     "SOLUTION", "Energy");
 
   SetVolumeOutputFields_ScalarSolution(config);

From 6241f6988d9d7ee2c4bdbf1ba86d4ae632f725cf Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 10 Jul 2023 18:21:09 +0200
Subject: [PATCH 575/656] Thread sanitizer builds don't need the python
 wrapper.

---
 .github/workflows/regression.yml | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 219e44b8c47..bb4b8f06082 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -81,9 +81,9 @@ jobs:
         config_set: [BaseOMP-tsan, ReverseOMP-tsan] #ForwardOMP-tsan
         include:
           - config_set: BaseOMP-tsan
-            flags: '--buildtype=debugoptimized -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3'
+            flags: '--buildtype=debugoptimized -Dwith-omp=true -Denable-mixedprec=true -Denable-tecio=false --warnlevel=3'
           - config_set: ReverseOMP-tsan
-            flags: '--buildtype=debugoptimized -Denable-autodiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3'
+            flags: '--buildtype=debugoptimized -Denable-autodiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-tecio=false --warnlevel=3'
           #- config_set: ForwardOMP-tsan
           #  flags: '--buildtype=debug -Denable-directdiff=true -Denable-normal=false -Dwith-omp=true -Denable-mixedprec=true -Denable-pywrapper=true -Denable-tecio=false --warnlevel=3 --werror'
     runs-on: ${{ inputs.runner || 'ubuntu-latest' }}

From 961518967ce98d7f2c7330d7eab80a0bffafe847 Mon Sep 17 00:00:00 2001
From: MastermindScope <81287997+MastermindScope@users.noreply.github.com>
Date: Tue, 11 Jul 2023 07:30:35 +0200
Subject: [PATCH 576/656] Add Velocity Volume Output To CFlowCompOutput.cpp

Added Velocity Volume Output
---
 SU2_CFD/src/output/CFlowCompOutput.cpp | 9 ++++++---
 1 file changed, 6 insertions(+), 3 deletions(-)

diff --git a/SU2_CFD/src/output/CFlowCompOutput.cpp b/SU2_CFD/src/output/CFlowCompOutput.cpp
index d57e59997a9..87b9d0e47fe 100644
--- a/SU2_CFD/src/output/CFlowCompOutput.cpp
+++ b/SU2_CFD/src/output/CFlowCompOutput.cpp
@@ -218,11 +218,9 @@ void CFlowCompOutput::SetVolumeOutputFields(CConfig *config){
   AddVolumeOutput("DENSITY",    "Density",    "SOLUTION", "Density");
   AddVolumeOutput("MOMENTUM-X", "Momentum_x", "SOLUTION", "x-component of the momentum vector");
   AddVolumeOutput("MOMENTUM-Y", "Momentum_y", "SOLUTION", "y-component of the momentum vector");
-  AddVolumeOutput("VELOCITY-X", "Veocity_x", "SOLUTION", "x-component of the velocity vector");
-  AddVolumeOutput("VELOCITY-Y", "Velocity_y", "SOLUTION", "y-component of the velocity vector");
+  
   if (nDim == 3)
     AddVolumeOutput("MOMENTUM-Z", "Momentum_z", "SOLUTION", "z-component of the momentum vector");
-    AddVolumeOutput("VELOCITY-Z", "Velocity_z", "SOLUTION", "z-component of the velocity vector");
   AddVolumeOutput("ENERGY",     "Energy",     "SOLUTION", "Energy");
 
   SetVolumeOutputFields_ScalarSolution(config);
@@ -240,6 +238,11 @@ void CFlowCompOutput::SetVolumeOutputFields(CConfig *config){
   AddVolumeOutput("TEMPERATURE", "Temperature",             "PRIMITIVE", "Temperature");
   AddVolumeOutput("MACH",        "Mach",                    "PRIMITIVE", "Mach number");
   AddVolumeOutput("PRESSURE_COEFF", "Pressure_Coefficient", "PRIMITIVE", "Pressure coefficient");
+  AddVolumeOutput("VELOCITY-X", "Veocity_x", "PRIMITIVE", "x-component of the velocity vector");
+  AddVolumeOutput("VELOCITY-Y", "Velocity_y", "PRIMITIVE", "y-component of the velocity vector");
+  
+  if (nDim == 3)
+    AddVolumeOutput("VELOCITY-Z", "Velocity_z", "PRIMITIVE", "z-component of the velocity vector");
 
   if (config->GetViscous()) {
     AddVolumeOutput("LAMINAR_VISCOSITY", "Laminar_Viscosity", "PRIMITIVE", "Laminar viscosity");

From b5636c48e85438af9b8945add87b347456be9825 Mon Sep 17 00:00:00 2001
From: MastermindScope <81287997+MastermindScope@users.noreply.github.com>
Date: Tue, 11 Jul 2023 07:33:04 +0200
Subject: [PATCH 577/656] Added Velocity Output To CNEMOCompOutput.cpp

Added Velocity Output
---
 SU2_CFD/src/output/CNEMOCompOutput.cpp | 5 +++++
 1 file changed, 5 insertions(+)

diff --git a/SU2_CFD/src/output/CNEMOCompOutput.cpp b/SU2_CFD/src/output/CNEMOCompOutput.cpp
index e2c799e269f..29b77197e1c 100644
--- a/SU2_CFD/src/output/CNEMOCompOutput.cpp
+++ b/SU2_CFD/src/output/CNEMOCompOutput.cpp
@@ -242,10 +242,15 @@ void CNEMOCompOutput::SetVolumeOutputFields(CConfig *config){
   AddVolumeOutput("PRESSURE",       "Pressure",       "PRIMITIVE", "Pressure");
   AddVolumeOutput("TEMPERATURE_TR", "Temperature_tr", "PRIMITIVE", "Temperature_tr");
   AddVolumeOutput("TEMPERATURE_VE", "Temperature_ve", "PRIMITIVE", "Temperature_ve");
+  AddVolumeOutput("VELOCITY-X", "Velocity_x", "PRIMITIVE", "x-component of the velocity vector");
+  AddVolumeOutput("VELOCITY-Y", "Velocity_y", "PRIMITIVE", "y-component of the velocity vector");
 
   AddVolumeOutput("MACH",        "Mach",                    "PRIMITIVE", "Mach number");
   AddVolumeOutput("PRESSURE_COEFF", "Pressure_Coefficient", "PRIMITIVE", "Pressure coefficient");
 
+  if (nDim == 3)
+    AddVolumeOutput("VELOCITY-Z", "Velocity_z", "PRIMITIVE", "z-component of the velocity vector");
+
   if (config->GetViscous()) {
     AddVolumeOutput("LAMINAR_VISCOSITY", "Laminar_Viscosity", "PRIMITIVE", "Laminar viscosity");
 

From cd58b68806f6d59bbbe1665824fb45a0580f3d1c Mon Sep 17 00:00:00 2001
From: MastermindScope <81287997+MastermindScope@users.noreply.github.com>
Date: Tue, 11 Jul 2023 07:34:21 +0200
Subject: [PATCH 578/656] Fixed spelling in description

---
 SU2_CFD/src/output/CFlowCompOutput.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/SU2_CFD/src/output/CFlowCompOutput.cpp b/SU2_CFD/src/output/CFlowCompOutput.cpp
index 87b9d0e47fe..3fdec807392 100644
--- a/SU2_CFD/src/output/CFlowCompOutput.cpp
+++ b/SU2_CFD/src/output/CFlowCompOutput.cpp
@@ -238,7 +238,7 @@ void CFlowCompOutput::SetVolumeOutputFields(CConfig *config){
   AddVolumeOutput("TEMPERATURE", "Temperature",             "PRIMITIVE", "Temperature");
   AddVolumeOutput("MACH",        "Mach",                    "PRIMITIVE", "Mach number");
   AddVolumeOutput("PRESSURE_COEFF", "Pressure_Coefficient", "PRIMITIVE", "Pressure coefficient");
-  AddVolumeOutput("VELOCITY-X", "Veocity_x", "PRIMITIVE", "x-component of the velocity vector");
+  AddVolumeOutput("VELOCITY-X", "Velocity_x", "PRIMITIVE", "x-component of the velocity vector");
   AddVolumeOutput("VELOCITY-Y", "Velocity_y", "PRIMITIVE", "y-component of the velocity vector");
   
   if (nDim == 3)

From ced15ae7f7df38a1f5ac3c562cd3e107bbf5eaed Mon Sep 17 00:00:00 2001
From: MastermindScope <81287997+MastermindScope@users.noreply.github.com>
Date: Tue, 11 Jul 2023 07:35:53 +0200
Subject: [PATCH 579/656] Added my name to AUTHORS.md

---
 AUTHORS.md | 1 +
 1 file changed, 1 insertion(+)

diff --git a/AUTHORS.md b/AUTHORS.md
index 49ce6d21fe8..0a2231ec0d7 100644
--- a/AUTHORS.md
+++ b/AUTHORS.md
@@ -129,6 +129,7 @@ Thomas D. Economon
 Tim Albring
 TobiKattmann
 Trent Lukaczyk
+Vinzenz Götz
 VivaanKhatri
 Wally Maier
 Y. Chandukrishna

From 37d095460deeccad04229a3ce99bd44655818cbc Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Tue, 11 Jul 2023 07:57:56 -0700
Subject: [PATCH 580/656] Update SU2_CFD/src/output/CNEMOCompOutput.cpp

---
 SU2_CFD/src/output/CNEMOCompOutput.cpp | 5 ++---
 1 file changed, 2 insertions(+), 3 deletions(-)

diff --git a/SU2_CFD/src/output/CNEMOCompOutput.cpp b/SU2_CFD/src/output/CNEMOCompOutput.cpp
index 29b77197e1c..c21d655f57e 100644
--- a/SU2_CFD/src/output/CNEMOCompOutput.cpp
+++ b/SU2_CFD/src/output/CNEMOCompOutput.cpp
@@ -244,13 +244,12 @@ void CNEMOCompOutput::SetVolumeOutputFields(CConfig *config){
   AddVolumeOutput("TEMPERATURE_VE", "Temperature_ve", "PRIMITIVE", "Temperature_ve");
   AddVolumeOutput("VELOCITY-X", "Velocity_x", "PRIMITIVE", "x-component of the velocity vector");
   AddVolumeOutput("VELOCITY-Y", "Velocity_y", "PRIMITIVE", "y-component of the velocity vector");
+  if (nDim == 3)
+    AddVolumeOutput("VELOCITY-Z", "Velocity_z", "PRIMITIVE", "z-component of the velocity vector");
 
   AddVolumeOutput("MACH",        "Mach",                    "PRIMITIVE", "Mach number");
   AddVolumeOutput("PRESSURE_COEFF", "Pressure_Coefficient", "PRIMITIVE", "Pressure coefficient");
 
-  if (nDim == 3)
-    AddVolumeOutput("VELOCITY-Z", "Velocity_z", "PRIMITIVE", "z-component of the velocity vector");
-
   if (config->GetViscous()) {
     AddVolumeOutput("LAMINAR_VISCOSITY", "Laminar_Viscosity", "PRIMITIVE", "Laminar viscosity");
 

From 03623bb17d234d94bf9a0641b55ef73dfa1c5258 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Vinzenz=20G=C3=B6tz?=
 <81287997+MastermindScope@users.noreply.github.com>
Date: Tue, 11 Jul 2023 18:57:16 +0200
Subject: [PATCH 581/656] Added SetVolumeOutputValue for Velocity to
 CFlowCompOutput.cpp

---
 SU2_CFD/src/output/CFlowCompOutput.cpp | 9 ++++++---
 1 file changed, 6 insertions(+), 3 deletions(-)

diff --git a/SU2_CFD/src/output/CFlowCompOutput.cpp b/SU2_CFD/src/output/CFlowCompOutput.cpp
index 3b5fc841d09..6e39ea53df4 100644
--- a/SU2_CFD/src/output/CFlowCompOutput.cpp
+++ b/SU2_CFD/src/output/CFlowCompOutput.cpp
@@ -316,11 +316,14 @@ void CFlowCompOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolv
   SetVolumeOutputValue("DENSITY",    iPoint, Node_Flow->GetSolution(iPoint, 0));
   SetVolumeOutputValue("MOMENTUM-X", iPoint, Node_Flow->GetSolution(iPoint, 1));
   SetVolumeOutputValue("MOMENTUM-Y", iPoint, Node_Flow->GetSolution(iPoint, 2));
+  SetVolumeOutputValue("VELOCITY-X", iPoint, Node_Flow->GetSolution(iPoint, 3));
+  SetVolumeOutputValue("VELOCITY-Y", iPoint, Node_Flow->GetSolution(iPoint, 4));
   if (nDim == 3){
-    SetVolumeOutputValue("MOMENTUM-Z", iPoint, Node_Flow->GetSolution(iPoint, 3));
-    SetVolumeOutputValue("ENERGY",     iPoint, Node_Flow->GetSolution(iPoint, 4));
+    SetVolumeOutputValue("MOMENTUM-Z", iPoint, Node_Flow->GetSolution(iPoint, 5));
+    SetVolumeOutputValue("ENERGY",     iPoint, Node_Flow->GetSolution(iPoint, 6));
+    SetVolumeOutputValue("VELOCITY-Z", iPoint, Node_Flow->GetSolution(iPoint, 7));
   } else {
-    SetVolumeOutputValue("ENERGY",     iPoint, Node_Flow->GetSolution(iPoint, 3));
+    SetVolumeOutputValue("ENERGY",     iPoint, Node_Flow->GetSolution(iPoint, 5));
   }
 
   if (gridMovement){

From d0b7922033a68c1730fb9ad09ea6391fddf504d5 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Vinzenz=20G=C3=B6tz?=
 <81287997+MastermindScope@users.noreply.github.com>
Date: Tue, 11 Jul 2023 19:00:01 +0200
Subject: [PATCH 582/656] Add SetVolumeOutputValue for velocity to
 CNEMOCompOutput.cpp

---
 SU2_CFD/src/output/CNEMOCompOutput.cpp | 13 ++++++++-----
 1 file changed, 8 insertions(+), 5 deletions(-)

diff --git a/SU2_CFD/src/output/CNEMOCompOutput.cpp b/SU2_CFD/src/output/CNEMOCompOutput.cpp
index 06f51f29224..8afbd1448a0 100644
--- a/SU2_CFD/src/output/CNEMOCompOutput.cpp
+++ b/SU2_CFD/src/output/CNEMOCompOutput.cpp
@@ -317,13 +317,16 @@ void CNEMOCompOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolv
 
   SetVolumeOutputValue("MOMENTUM-X", iPoint, Node_Flow->GetSolution(iPoint, nSpecies));
   SetVolumeOutputValue("MOMENTUM-Y", iPoint, Node_Flow->GetSolution(iPoint, nSpecies+1));
+  SetVolumeOutputValue("VELOCITY-X", iPoint, Node_Flow->GetSolution(iPoint, nSpecies+2));
+  SetVolumeOutputValue("VELOCITY-Y", iPoint, Node_Flow->GetSolution(iPoint, nSpecies+3));
   if (nDim == 3){
-    SetVolumeOutputValue("MOMENTUM-Z", iPoint, Node_Flow->GetSolution(iPoint, nSpecies+2));
-    SetVolumeOutputValue("ENERGY",     iPoint, Node_Flow->GetSolution(iPoint, nSpecies+3));
-    SetVolumeOutputValue("ENERGY_VE",  iPoint, Node_Flow->GetSolution(iPoint, nSpecies+4));
+    SetVolumeOutputValue("MOMENTUM-Z", iPoint, Node_Flow->GetSolution(iPoint, nSpecies+4));
+    SetVolumeOutputValue("ENERGY",     iPoint, Node_Flow->GetSolution(iPoint, nSpecies+5));
+    SetVolumeOutputValue("ENERGY_VE",  iPoint, Node_Flow->GetSolution(iPoint, nSpecies+6));
+    SetVolumeOutputValue("VELOCITY-Z", iPoint, Node_Flow->GetSolution(iPoint, nSpecies+7));
   } else {
-    SetVolumeOutputValue("ENERGY",     iPoint, Node_Flow->GetSolution(iPoint, nSpecies+2));
-    SetVolumeOutputValue("ENERGY_VE",  iPoint, Node_Flow->GetSolution(iPoint, nSpecies+3));
+    SetVolumeOutputValue("ENERGY",     iPoint, Node_Flow->GetSolution(iPoint, nSpecies+4));
+    SetVolumeOutputValue("ENERGY_VE",  iPoint, Node_Flow->GetSolution(iPoint, nSpecies+5));
   }
 
   for(iSpecies = 0; iSpecies < nSpecies; iSpecies++)

From 0b0150037b46716c84ea9a56ebc7a521af8c7027 Mon Sep 17 00:00:00 2001
From: "Francesco Poli (wintermute)" <invernomuto@paranoici.org>
Date: Tue, 11 Jul 2023 23:08:07 +0200
Subject: [PATCH 583/656] restore QuickStart subdirectory

...with the mesh and config file.
---
 QuickStart/.gitignore            |    17 +
 QuickStart/inv_NACA0012.cfg      |   327 +
 QuickStart/mesh_NACA0012_inv.su2 | 15707 +++++++++++++++++++++++++++++
 externals/utils/release_su2.sh   |     3 +
 4 files changed, 16054 insertions(+)
 create mode 100644 QuickStart/.gitignore
 create mode 100644 QuickStart/inv_NACA0012.cfg
 create mode 100644 QuickStart/mesh_NACA0012_inv.su2

diff --git a/QuickStart/.gitignore b/QuickStart/.gitignore
new file mode 100644
index 00000000000..78e9921b732
--- /dev/null
+++ b/QuickStart/.gitignore
@@ -0,0 +1,17 @@
+# In the QuickStart/ directory, we would like to
+# ignore any of the data needed to run the case
+# or their output data, i.e., meshes, solution
+# files, restart files, CSVs, etc.
+
+# Things appearing in QuickStart/ to ignore:
+*.dat
+*.csv
+*.plt
+*.szplt
+*.vtu
+*.log
+*.out
+*.aux
+*.pdf
+*.png
+config_*.cfg
diff --git a/QuickStart/inv_NACA0012.cfg b/QuickStart/inv_NACA0012.cfg
new file mode 100644
index 00000000000..9287d90d60a
--- /dev/null
+++ b/QuickStart/inv_NACA0012.cfg
@@ -0,0 +1,327 @@
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+%                                                                              %
+% SU2 configuration file                                                       %
+% Case description: Transonic inviscid flow around a NACA0012 airfoil          %
+% Author: Thomas D. Economon                                                   %
+% Institution: Stanford University                                             %
+% Date: 2014.06.11                                                             %
+% File Version 7.5.1 "Blackbird"                                                  %
+%                                                                              %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
+% Physical governing equations (EULER, NAVIER_STOKES,
+%                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
+%                               POISSON_EQUATION)
+SOLVER= EULER
+%
+% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
+MATH_PROBLEM= DIRECT
+%
+% Restart solution (NO, YES)
+RESTART_SOL= NO
+
+% ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
+%
+% Mach number (non-dimensional, based on the free-stream values)
+MACH_NUMBER= 0.8
+%
+% Angle of attack (degrees)
+AOA= 1.25
+%
+% Free-stream pressure (101325.0 N/m^2 by default, only Euler flows)
+FREESTREAM_PRESSURE= 101325.0
+%
+% Free-stream temperature (273.15 K by default)
+FREESTREAM_TEMPERATURE= 273.15
+
+% -------------- COMPRESSIBLE AND INCOMPRESSIBLE FLUID CONSTANTS --------------%
+%
+% Ratio of specific heats (1.4 (air), only for compressible flows)
+GAMMA_VALUE= 1.4
+%
+% Specific gas constant (287.87 J/kg*K (air), only for compressible flows)
+GAS_CONSTANT= 287.87
+
+% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
+%
+% Reference origin for moment computation
+REF_ORIGIN_MOMENT_X = 0.25
+REF_ORIGIN_MOMENT_Y = 0.00
+REF_ORIGIN_MOMENT_Z = 0.00
+%
+% Reference length for pitching, rolling, and yawing non-dimensional moment
+REF_LENGTH= 1.0
+%
+% Reference area for force coefficients (0 implies automatic calculation)
+REF_AREA= 1.0
+%
+% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
+%                              FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
+REF_DIMENSIONALIZATION= DIMENSIONAL
+
+% ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
+%
+% Marker of the Euler boundary (NONE = no marker)
+MARKER_EULER= ( airfoil )
+%
+% Marker of the far field (NONE = no marker)
+MARKER_FAR= ( farfield )
+
+% ------------------------ SURFACES IDENTIFICATION ----------------------------%
+%
+% Marker(s) of the surface in the surface flow solution file
+MARKER_PLOTTING = ( airfoil )
+%
+% Marker(s) of the surface where the non-dimensional coefficients are evaluated.
+MARKER_MONITORING = ( airfoil )
+%
+% Marker(s) of the surface where obj. func. (design problem) will be evaluated
+MARKER_DESIGNING = ( airfoil )
+
+% ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
+%
+% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
+%
+% Objective function in optimization problem (DRAG, LIFT, SIDEFORCE, MOMENT_X,
+%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
+%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
+%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
+%                                             TORQUE, FREE_SURFACE, TOTAL_HEATFLUX,
+%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
+%                                             INVERSE_DESIGN_HEATFLUX)
+OBJECTIVE_FUNCTION= DRAG
+%
+% Courant-Friedrichs-Lewy condition of the finest grid
+CFL_NUMBER= 1e3
+%
+% Adaptive CFL number (NO, YES)
+CFL_ADAPT= NO
+%
+% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
+%                                        CFL max value )
+CFL_ADAPT_PARAM= ( 0.1, 2.0, 10.0, 1e10 )
+%
+% Number of total iterations
+ITER= 250
+
+% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
+%
+% Linear solver for implicit formulations (BCGSTAB, FGMRES)
+LINEAR_SOLVER= FGMRES
+%
+% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
+LINEAR_SOLVER_PREC= ILU
+%
+% Minimum error of the linear solver for implicit formulations
+LINEAR_SOLVER_ERROR= 1E-10
+%
+% Max number of iterations of the linear solver for the implicit formulation
+LINEAR_SOLVER_ITER= 10
+
+% -------------------------- MULTIGRID PARAMETERS -----------------------------%
+%
+% Multi-Grid Levels (0 = no multi-grid)
+MGLEVEL= 3
+%
+% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
+MGCYCLE= W_CYCLE
+%
+% Multi-Grid PreSmoothing Level
+MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
+%
+% Multi-Grid PostSmoothing Level
+MG_POST_SMOOTH= ( 0, 0, 0, 0 )
+%
+% Jacobi implicit smoothing of the correction
+MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
+%
+% Damping factor for the residual restriction
+MG_DAMP_RESTRICTION= 1.0
+%
+% Damping factor for the correction prolongation
+MG_DAMP_PROLONGATION= 1.0
+
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
+% Convective numerical method
+%
+CONV_NUM_METHOD_FLOW= JST
+%
+% 2nd and 4th order artificial dissipation coefficients
+JST_SENSOR_COEFF= ( 0.5, 0.02 )
+%
+% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+
+% ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
+%
+% Convective numerical method (JST, LAX-FRIEDRICH, ROE)
+CONV_NUM_METHOD_ADJFLOW= JST
+%
+% Reduction factor of the CFL coefficient in the adjoint problem
+CFL_REDUCTION_ADJFLOW= 0.01
+%
+% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT)
+TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
+
+% ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
+%
+% Kind of deformation (NO_DEFORMATION, TRANSLATION, ROTATION, SCALE,
+%                      FFD_SETTING, FFD_NACELLE
+%                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS, FFD_TWIST
+%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D, FFD_TWIST_2D,
+%                      HICKS_HENNE, SURFACE_BUMP)
+DV_KIND= HICKS_HENNE
+%
+% Marker of the surface in which we are going apply the shape deformation
+DV_MARKER= ( airfoil )
+%
+% Parameters of the shape deformation
+% - NO_DEFORMATION ( 1.0 )
+% - TRANSLATION ( x_Disp, y_Disp, z_Disp ), as a unit vector
+% - ROTATION ( x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
+% - SCALE ( 1.0 )
+% - ANGLE_OF_ATTACK ( 1.0 )
+% - FFD_SETTING ( 1.0 )
+% - FFD_CONTROL_POINT ( FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
+% - FFD_NACELLE ( FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Disp, phi_Disp )
+% - FFD_GULL ( FFD_BoxTag, j_Ind )
+% - FFD_ANGLE_OF_ATTACK ( FFD_BoxTag, 1.0 )
+% - FFD_CAMBER ( FFD_BoxTag, i_Ind, j_Ind )
+% - FFD_THICKNESS ( FFD_BoxTag, i_Ind, j_Ind )
+% - FFD_TWIST ( FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
+% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
+% - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
+% - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
+% - FFD_TWIST_2D ( FFD_BoxTag, x_Orig, y_Orig )
+% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
+% - SURFACE_BUMP ( x_Start, x_End, x_Loc )
+DV_PARAM= ( 1, 0.5 )
+%
+% Value of the shape deformation
+DV_VALUE= 0.01
+
+% ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
+%
+% Number of smoothing iterations for FEA mesh deformation
+DEFORM_LINEAR_SOLVER_ITER= 500
+%
+% Number of nonlinear deformation iterations (surface deformation increments)
+DEFORM_NONLINEAR_ITER= 1
+%
+% Minimum residual criteria for the linear solver convergence of grid deformation
+DEFORM_LINEAR_SOLVER_ERROR= 1E-14
+%
+% Print the residuals during mesh deformation to the console (YES, NO)
+DEFORM_CONSOLE_OUTPUT= YES
+%
+% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
+%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
+DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
+
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
+CONV_FIELD= RMS_DENSITY
+%
+% Min value of the residual (log10 of the residual)
+CONV_RESIDUAL_MINVAL= -8
+%
+% Start Cauchy criteria at iteration number
+CONV_STARTITER= 10
+%
+% Number of elements to apply the criteria
+CONV_CAUCHY_ELEMS= 100
+%
+% Epsilon to control the series convergence
+CONV_CAUCHY_EPS= 1E-6
+%
+SCREEN_OUTPUT=(INNER_ITER, WALL_TIME, RMS_RES, LIFT, DRAG, CAUCHY_SENS_PRESS, CAUCHY_DRAG RMS_ADJ_DENSITY RMS_ADJ_ENERGY)
+
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+% Mesh input file
+MESH_FILENAME= mesh_NACA0012_inv.su2
+%
+% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
+MESH_FORMAT= SU2
+%
+% Mesh output file
+MESH_OUT_FILENAME= mesh_out.su2
+%
+% Restart flow input file
+SOLUTION_FILENAME= solution_flow.dat
+%
+% Restart adjoint input file
+SOLUTION_ADJ_FILENAME= solution_adj.dat
+%
+% Output file format (TECPLOT, CSV)
+TABULAR_FORMAT= CSV
+%
+% Output file convergence history (w/o extension)
+CONV_FILENAME= history
+%
+% Output file restart flow
+RESTART_FILENAME= restart_flow.dat
+%
+% Output file restart adjoint
+RESTART_ADJ_FILENAME= restart_adj.dat
+%
+% Output file flow (w/o extension) variables
+VOLUME_FILENAME= flow
+%
+% Output file adjoint (w/o extension) variables
+VOLUME_ADJ_FILENAME= adjoint
+%
+% Output Objective function gradient (using continuous adjoint)
+GRAD_OBJFUNC_FILENAME= of_grad.dat
+%
+% Output file surface flow coefficient (w/o extension)
+SURFACE_FILENAME= surface_flow
+%
+% Output file surface adjoint coefficient (w/o extension)
+SURFACE_ADJ_FILENAME= surface_adjoint
+%
+% Writing solution file frequency
+OUTPUT_WRT_FREQ= 250
+%
+% Output file format
+OUTPUT_FILES= (RESTART, PARAVIEW, SURFACE_CSV)
+
+% --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
+% Available flow based objective functions or constraint functions
+%    DRAG, LIFT, SIDEFORCE, EFFICIENCY,
+%    FORCE_X, FORCE_Y, FORCE_Z,
+%    MOMENT_X, MOMENT_Y, MOMENT_Z,
+%    THRUST, TORQUE, FIGURE_OF_MERIT,
+%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
+%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
+%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
+%
+% Available geometrical based objective functions or constraint functions
+%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
+%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
+%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
+%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
+%
+% Available design variables
+%    HICKS_HENNE 	(  1, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
+%    NACA_4DIGITS	(  4, Scale | Mark. List | 1st digit, 2nd digit, 3rd and 4th digit )
+%    TRANSLATION	(  5, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
+%    ROTATION		(  6, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
+%    FFD_CONTROL_POINT_2D (  15, Scale | Mark. List | FFD_Box_ID, i_Ind, j_Ind, x_Mov, y_Mov )
+%    FFD_CAMBER_2D 	( 16, Scale | Mark. List | FFD_Box_ID, i_Ind )
+%    FFD_THICKNESS_2D 	( 17, Scale | Mark. List | FFD_Box_ID, i_Ind )
+%
+% Optimization objective function with scaling factor
+% ex= Objective * Scale
+OPT_OBJECTIVE= DRAG * 0.001
+%
+% Optimization constraint functions with scaling factors, separated by semicolons
+% ex= (Objective = Value ) * Scale, use '>','<','='
+OPT_CONSTRAINT= ( LIFT > 0.328188 ) * 0.001; ( MOMENT_Z > 0.034068 ) * 0.001; ( AIRFOIL_THICKNESS > 0.11 ) * 0.001
+%
+
+% Optimization design variables, separated by semicolons
+DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 ); ( 30, 1.0 | airfoil | 0, 0.20 ); ( 30, 1.0 | airfoil | 0, 0.25 ); ( 30, 1.0 | airfoil | 0, 0.30 ); ( 30, 1.0 | airfoil | 0, 0.35 ); ( 30, 1.0 | airfoil | 0, 0.40 ); ( 30, 1.0 | airfoil | 0, 0.45 ); ( 30, 1.0 | airfoil | 0, 0.50 ); ( 30, 1.0 | airfoil | 0, 0.55 ); ( 30, 1.0 | airfoil | 0, 0.60 ); ( 30, 1.0 | airfoil | 0, 0.65 ); ( 30, 1.0 | airfoil | 0, 0.70 ); ( 30, 1.0 | airfoil | 0, 0.75 ); ( 30, 1.0 | airfoil | 0, 0.80 ); ( 30, 1.0 | airfoil | 0, 0.85 ); ( 30, 1.0 | airfoil | 0, 0.90 ); ( 30, 1.0 | airfoil | 0, 0.95 ); ( 30, 1.0 | airfoil | 1, 0.05 ); ( 30, 1.0 | airfoil | 1, 0.10 ); ( 30, 1.0 | airfoil | 1, 0.15 ); ( 30, 1.0 | airfoil | 1, 0.20 ); ( 30, 1.0 | airfoil | 1, 0.25 ); ( 30, 1.0 | airfoil | 1, 0.30 ); ( 30, 1.0 | airfoil | 1, 0.35 ); ( 30, 1.0 | airfoil | 1, 0.40 ); ( 30, 1.0 | airfoil | 1, 0.45 ); ( 30, 1.0 | airfoil | 1, 0.50 ); ( 30, 1.0 | airfoil | 1, 0.55 ); ( 30, 1.0 | airfoil | 1, 0.60 ); ( 30, 1.0 | airfoil | 1, 0.65 ); ( 30, 1.0 | airfoil | 1, 0.70 ); ( 30, 1.0 | airfoil | 1, 0.75 ); ( 30, 1.0 | airfoil | 1, 0.80 ); ( 30, 1.0 | airfoil | 1, 0.85 ); ( 30, 1.0 | airfoil | 1, 0.90 ); ( 30, 1.0 | airfoil | 1, 0.95 )
diff --git a/QuickStart/mesh_NACA0012_inv.su2 b/QuickStart/mesh_NACA0012_inv.su2
new file mode 100644
index 00000000000..0c809e5807e
--- /dev/null
+++ b/QuickStart/mesh_NACA0012_inv.su2
@@ -0,0 +1,15707 @@
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+5	1859	1742	1741	3721
+5	1861	1715	1714	3722
+5	1862	1679	1715	3723
+5	2069	1893	2040	3724
+5	1862	1715	1861	3725
+5	2165	2163	2011	3726
+5	2349	2123	2236	3727
+5	1864	1719	1718	3728
+5	1886	1740	1885	3729
+5	2287	2160	2286	3730
+5	1969	1829	1859	3731
+5	2114	2078	1938	3732
+5	1886	1859	1741	3733
+5	2031	1835	1883	3734
+5	2015	1866	1858	3735
+5	2135	1953	2086	3736
+5	1950	1849	1687	3737
+5	1869	1725	1724	3738
+5	1870	1725	1869	3739
+5	2225	2080	2224	3740
+5	2020	1871	1870	3741
+5	2175	2028	2121	3742
+5	1871	1726	1870	3743
+5	1975	1960	1805	3744
+5	2058	1993	1913	3745
+5	2022	1872	1999	3746
+5	1872	1721	1577	3747
+5	1875	1729	1874	3748
+5	2116	2012	1958	3749
+5	1875	1730	1729	3750
+5	1875	1873	1730	3751
+5	1992	1831	1823	3752
+5	2001	1843	1842	3753
+5	1927	1786	1731	3754
+5	1928	1786	1927	3755
+5	1878	1733	1732	3756
+5	1999	1872	1845	3757
+5	2006	1855	1837	3758
+5	2234	1987	2145	3759
+5	2055	1838	1995	3760
+5	1987	1728	1822	3761
+5	1883	1737	1882	3762
+5	1882	1736	1881	3763
+5	1974	1804	1931	3764
+5	1883	1673	1737	3765
+5	2299	2154	2153	3766
+5	2360	2223	2282	3767
+5	1975	1805	1828	3768
+5	1986	1910	1944	3769
+5	2141	1986	2098	3770
+5	2029	1882	1881	3771
+5	2108	1958	1973	3772
+5	2012	1864	1863	3773
+5	2204	2058	2203	3774
+5	2222	2077	2076	3775
+5	1995	1838	1907	3776
+5	1888	1812	1743	3777
+5	2160	2002	2001	3778
+5	2116	1958	2108	3779
+5	1890	1840	1675	3780
+5	1889	1745	1744	3781
+5	2076	1929	2075	3782
+5	1993	1836	1913	3783
+5	2179	2033	2113	3784
+5	2245	2151	2008	3785
+5	1893	1749	1748	3786
+5	1926	1784	1925	3787
+5	1988	1825	1847	3788
+5	1924	1749	1893	3789
+5	2043	1895	2042	3790
+5	2042	1894	2041	3791
+5	2049	1901	2048	3792
+5	1900	1756	1755	3793
+5	2047	1899	2046	3794
+5	2073	1927	2072	3795
+5	2119	1990	2000	3796
+5	1901	1757	1756	3797
+5	2073	1928	1927	3798
+5	1905	1760	1904	3799
+5	2041	1894	1815	3800
+5	2043	1896	1895	3801
+5	2042	1895	1894	3802
+5	1903	1758	1902	3803
+5	2052	1905	1904	3804
+5	1904	1759	1903	3805
+5	2048	1900	2047	3806
+5	2045	1897	2044	3807
+5	2045	1898	1897	3808
+5	1906	1761	1905	3809
+5	2215	2124	2071	3810
+5	1906	1683	1761	3811
+5	2192	2047	2046	3812
+5	2009	1861	1860	3813
+5	2194	2049	2048	3814
+5	2040	1892	1962	3815
+5	1907	1838	1764	3816
+5	1907	1764	1763	3817
+5	1921	1780	1920	3818
+5	1919	1778	1777	3819
+5	2011	1847	1862	3820
+5	2342	2201	2260	3821
+5	1912	1768	1911	3822
+5	2280	2015	2178	3823
+5	1912	1769	1768	3824
+5	1912	1910	1769	3825
+5	1913	1836	1703	3826
+5	1913	1771	1832	3827
+5	2018	1869	1868	3828
+5	1965	1868	1804	3829
+5	1915	1773	1772	3830
+5	1917	1775	1774	3831
+5	2122	2059	1967	3832
+5	1916	1773	1915	3833
+5	2208	2063	2062	3834
+5	1918	1776	1775	3835
+5	2007	1961	1856	3836
+5	2007	1856	1855	3837
+5	2064	1919	1909	3838
+5	2062	1917	2061	3839
+5	2050	1903	1902	3840
+5	1963	1860	1806	3841
+5	1968	1922	1919	3842
+5	2063	2006	1837	3843
+5	2211	2107	2065	3844
+5	1923	1824	1782	3845
+5	1922	1920	1779	3846
+5	1922	1779	1778	3847
+5	2066	1922	1968	3848
+5	2207	2061	2206	3849
+5	2040	1893	1892	3850
+5	1925	1783	1924	3851
+5	2213	2069	2040	3852
+5	1926	1841	1785	3853
+5	2051	1904	1903	3854
+5	2044	1896	2043	3855
+5	2046	1899	1898	3856
+5	2049	1902	1901	3857
+5	2117	1946	1970	3858
+5	2028	1881	1880	3859
+5	2079	1933	2078	3860
+5	1930	1789	1929	3861
+5	2058	1832	2057	3862
+5	1931	1804	1791	3863
+5	2057	1840	1966	3864
+5	2283	2115	2142	3865
+5	1933	1794	1793	3866
+5	1934	1795	1794	3867
+5	2238	2114	2125	3868
+5	1936	1796	1935	3869
+5	2077	1930	2076	3870
+5	2081	1935	2080	3871
+5	2035	1885	2034	3872
+5	1937	1744	1797	3873
+5	2111	2057	1966	3874
+5	2037	1831	1992	3875
+5	2036	1859	1886	3876
+5	1969	1947	1829	3877
+5	1938	1932	1839	3878
+5	2126	1969	2095	3879
+5	2146	1852	1997	3880
+5	2152	1662	1684	3881
+5	1943	1546	1655	3882
+5	2239	2085	2129	3883
+5	2245	2008	2093	3884
+5	2128	2004	1814	3885
+5	1956	1819	1695	3886
+5	2104	2005	1956	3887
+5	2129	1546	1943	3888
+5	1991	1799	1722	3889
+5	1985	1959	1911	3890
+5	2224	2079	2223	3891
+5	2131	1942	1854	3892
+5	2132	1848	1945	3893
+5	1946	1876	1800	3894
+5	1983	1857	1704	3895
+5	1947	1938	1839	3896
+5	1947	1839	1829	3897
+5	2241	2093	1983	3898
+5	1983	1704	1817	3899
+5	1949	1948	1818	3900
+5	1949	1818	1546	3901
+5	2086	1849	1950	3902
+5	1953	1706	1849	3903
+5	2293	2097	1940	3904
+5	2134	1808	1941	3905
+5	2149	1978	1952	3906
+5	1978	1686	1952	3907
+5	2135	1940	1798	3908
+5	1953	1798	1664	3909
+5	2550	2304	2380	3910
+5	1954	1816	1690	3911
+5	2024	1875	2023	3912
+5	2024	1873	1875	3913
+5	2103	1844	2003	3914
+5	2097	1941	1940	3915
+5	1957	1907	1825	3916
+5	2243	2138	2163	3917
+5	1958	1863	1812	3918
+5	2038	1888	1887	3919
+5	1959	1944	1912	3920
+5	1959	1912	1911	3921
+5	1985	1911	1821	3922
+5	1960	1821	1805	3923
+5	1961	1877	1856	3924
+5	2144	2026	1879	3925
+5	1962	1892	1834	3926
+5	2054	1962	1834	3927
+5	2199	2053	2198	3928
+5	2070	1925	1924	3929
+5	2177	2030	2176	3930
+5	2112	2032	2031	3931
+5	2021	1975	1828	3932
+5	2018	1868	1965	3933
+5	2220	1993	2204	3934
+5	2083	1937	2082	3935
+5	1967	1914	1824	3936
+5	2208	2062	2207	3937
+5	2065	1921	1920	3938
+5	2067	1824	1923	3939
+5	2013	1864	2012	3940
+5	2035	1886	1885	3941
+5	1970	1946	1800	3942
+5	1970	1800	1833	3943
+5	1971	1970	1833	3944
+5	1971	1833	1891	3945
+5	2144	1879	2027	3946
+5	2145	1987	1822	3947
+5	1973	1958	1812	3948
+5	1973	1812	1888	3949
+5	2075	1836	1993	3950
+5	2076	1930	1929	3951
+5	2019	1869	2018	3952
+5	2019	1870	1869	3953
+5	1976	1963	1806	3954
+5	1976	1806	1841	3955
+5	1997	1669	1977	3956
+5	2244	2127	2229	3957
+5	1982	1945	1547	3958
+5	2150	1945	1982	3959
+5	2005	1851	1819	3960
+5	2004	1853	1697	3961
+5	2148	2136	1954	3962
+5	1980	1813	1707	3963
+5	1981	1980	1707	3964
+5	1981	1707	1852	3965
+5	2296	2289	2149	3966
+5	2134	1952	1808	3967
+5	2379	2167	2233	3968
+5	2008	1653	1857	3969
+5	2152	1684	1984	3970
+5	1984	1684	1503	3971
+5	2220	2075	1993	3972
+5	2221	2076	2075	3973
+5	1986	1964	1820	3974
+5	1986	1820	1910	3975
+5	2185	2108	1973	3976
+5	2375	2370	2262	3977
+5	2010	1861	2009	3978
+5	2010	1862	1861	3979
+5	2217	2072	1946	3980
+5	2157	2017	1867	3981
+5	2074	1928	2073	3982
+5	2217	1946	2117	3983
+5	2113	2032	2112	3984
+5	2008	1807	1653	3985
+5	2038	1973	1888	3986
+5	2038	1887	2037	3987
+5	2075	1929	1836	3988
+5	2077	1931	1930	3989
+5	1994	1976	1841	3990
+5	1994	1841	1926	3991
+5	2055	1908	1838	3992
+5	2064	1909	2056	3993
+5	1996	1992	1823	3994
+5	1996	1823	1850	3995
+5	2103	1939	1844	3996
+5	2003	1660	1851	3997
+5	2022	1822	1721	3998
+5	1999	1845	1998	3999
+5	2172	1999	2159	4000
+5	2022	1721	1872	4001
+5	2000	1990	1846	4002
+5	2000	1846	1827	4003
+5	2002	1850	1843	4004
+5	2002	1996	1850	4005
+5	2320	2166	2310	4006
+5	2161	2102	1996	4007
+5	2128	1979	1942	4008
+5	2005	1819	1956	4009
+5	2369	1941	2097	4010
+5	2147	1652	1810	4011
+5	2105	2003	1851	4012
+5	2684	2517	2518	4013
+5	2060	1915	2059	4014
+5	2061	1917	1916	4015
+5	2212	2068	2107	4016
+5	2422	2260	2276	4017
+5	2249	2087	1991	4018
+5	2084	1991	1830	4019
+5	2202	2055	2201	4020
+5	2011	1862	2010	4021
+5	2213	2040	2090	4022
+5	2011	1988	1847	4023
+5	2092	2009	1963	4024
+5	2371	2308	2250	4025
+5	2013	1865	1864	4026
+5	2034	1885	1865	4027
+5	2185	1973	2038	4028
+5	2036	1886	2035	4029
+5	2100	1866	2015	4030
+5	2014	1858	1803	4031
+5	2033	1884	2032	4032
+5	2240	2084	1866	4033
+5	2136	1816	1954	4034
+5	2135	1798	1953	4035
+5	2017	2016	1826	4036
+5	2017	1826	1867	4037
+5	2021	1871	2020	4038
+5	2020	1870	2019	4039
+5	2154	1959	1985	4040
+5	2021	1828	1871	4041
+5	2098	1944	2096	4042
+5	2121	2028	1964	4043
+5	2450	2311	2372	4044
+5	2203	2057	2111	4045
+5	2109	1801	2026	4046
+5	2109	1972	1801	4047
+5	2027	1878	2025	4048
+5	2024	1955	1873	4049
+5	2102	1992	1996	4050
+5	2324	2184	2183	4051
+5	2314	2246	2172	4052
+5	2253	1972	2109	4053
+5	2159	1999	1998	4054
+5	2027	1879	1878	4055
+5	2166	2012	2116	4056
+5	2183	2037	1992	4057
+5	2031	1883	2030	4058
+5	2030	1883	1882	4059
+5	2153	1960	2130	4060
+5	2171	1975	2021	4061
+5	2168	2019	2018	4062
+5	2032	1835	2031	4063
+5	2098	1986	1944	4064
+5	2255	2113	2254	4065
+5	2033	1803	1884	4066
+5	2268	2141	2098	4067
+5	2176	2029	2175	4068
+5	2176	2030	2029	4069
+5	2373	2256	2283	4070
+5	2363	2226	2362	4071
+5	2273	2228	2110	4072
+5	2036	1969	1859	4073
+5	2362	2225	2361	4074
+5	2223	2078	2114	4075
+5	2156	2023	1874	4076
+5	2205	2060	2059	4077
+5	2374	2263	2350	4078
+5	2856	2731	2765	4079
+5	2039	1966	1890	4080
+5	2039	1890	1889	4081
+5	2069	1924	1893	4082
+5	2071	1925	2070	4083
+5	2188	2042	2187	4084
+5	2189	2043	2188	4085
+5	2186	1990	2119	4086
+5	2046	1898	2045	4087
+5	2190	2045	2044	4088
+5	2336	2195	2194	4089
+5	2218	2072	2217	4090
+5	2048	1901	1900	4091
+5	2186	2041	1990	4092
+5	2195	2049	2194	4093
+5	2187	2041	2186	4094
+5	2053	1905	2052	4095
+5	2187	2042	2041	4096
+5	2188	2043	2042	4097
+5	2190	2044	2189	4098
+5	2051	1903	2050	4099
+5	2199	2054	2053	4100
+5	2052	1904	2051	4101
+5	2198	2052	2197	4102
+5	2192	2046	2191	4103
+5	2189	2044	2043	4104
+5	2054	1906	2053	4105
+5	2196	2051	2050	4106
+5	2054	1834	1906	4107
+5	2140	2092	1963	4108
+5	2352	2213	2351	4109
+5	2164	2009	2092	4110
+5	2164	2010	2009	4111
+5	2210	2064	2056	4112
+5	2056	1908	2055	4113
+5	2236	2123	2200	4114
+5	2165	2010	2164	4115
+5	2058	1913	1832	4116
+5	2057	1832	1840	4117
+5	2115	1966	2039	4118
+5	2223	2079	2078	4119
+5	2060	1916	1915	4120
+5	2063	1837	1918	4121
+5	2062	1918	1917	4122
+5	2061	1916	2060	4123
+5	2303	2094	2262	4124
+5	2346	2207	2345	4125
+5	2285	2143	2261	4126
+5	2139	1961	2007	4127
+5	2139	2094	1961	4128
+5	2205	2059	2122	4129
+5	2201	1995	2099	4130
+5	2206	2060	2205	4131
+5	2285	2122	2143	4132
+5	2067	1967	1824	4133
+5	2066	2065	1920	4134
+5	2066	1920	1922	4135
+5	2107	2068	2065	4136
+5	2201	2055	1995	4137
+5	2068	2067	1923	4138
+5	2068	1923	1921	4139
+5	2090	2054	2199	4140
+5	2070	1924	2069	4141
+5	2419	2144	2315	4142
+5	2071	1994	1926	4143
+5	2448	2308	2371	4144
+5	2475	2336	2474	4145
+5	2191	2045	2190	4146
+5	2074	2000	1827	4147
+5	2219	2073	2218	4148
+5	2266	1971	2106	4149
+5	2331	2189	2330	4150
+5	2194	2048	2193	4151
+5	2299	2153	2298	4152
+5	2627	2494	2502	4153
+5	2171	2130	1975	4154
+5	2077	1974	1931	4155
+5	2377	2274	2300	4156
+5	2298	2153	2130	4157
+5	2079	1934	1933	4158
+5	2080	1935	1934	4159
+5	2180	2034	2013	4160
+5	2083	1889	1937	4161
+5	2183	1992	2102	4162
+5	2166	2013	2012	4163
+5	2115	2111	1966	4164
+5	2082	1936	2081	4165
+5	2227	2142	2083	4166
+5	2083	2039	1889	4167
+5	2343	2203	2111	4168
+5	2226	2081	2225	4169
+5	2085	1948	1949	4170
+5	2086	1953	1849	4171
+5	2270	2157	1989	4172
+5	2087	1989	1799	4173
+5	2167	2088	2016	4174
+5	2369	2134	1941	4175
+5	2151	1807	2008	4176
+5	2133	1817	1948	4177
+5	2386	2135	2086	4178
+5	2088	1950	1513	4179
+5	2089	2001	1955	4180
+5	2155	2089	1955	4181
+5	2330	2188	2329	4182
+5	2337	2196	2195	4183
+5	2091	2018	1965	4184
+5	2237	2130	2171	4185
+5	2140	1976	2120	4186
+5	2215	2071	2070	4187
+5	2271	2086	1950	4188
+5	2429	2271	2304	4189
+5	2094	2025	1961	4190
+5	2478	2272	2339	4191
+5	2182	2036	2035	4192
+5	2181	2035	2034	4193
+5	2154	2096	1959	4194
+5	2130	1960	1975	4195
+5	2167	2016	2017	4196
+5	2148	1813	1980	4197
+5	2275	2141	2268	4198
+5	2496	2361	2360	4199
+5	2696	2564	2520	4200
+5	2341	2200	2210	4201
+5	2178	2015	2014	4202
+5	2555	2432	2280	4203
+5	2101	2091	1965	4204
+5	2101	1965	1974	4205
+5	2161	2002	2160	4206
+5	2324	2183	2251	4207
+5	2388	2148	2295	4208
+5	2278	2003	2105	4209
+5	2384	2105	2277	4210
+5	2104	1853	2004	4211
+5	2152	1809	1662	4212
+5	2158	1939	2103	4213
+5	2113	2033	2032	4214
+5	2279	2119	2216	4215
+5	2211	2066	2123	4216
+5	2202	2056	2055	4217
+5	2184	2037	2183	4218
+5	2306	2102	2161	4219
+5	2314	2159	2253	4220
+5	2145	1822	2022	4221
+5	2110	2101	1974	4222
+5	2110	1974	2077	4223
+5	2203	2058	2057	4224
+5	2204	1993	2058	4225
+5	2280	2100	2015	4226
+5	2318	2254	2112	4227
+5	2255	2179	2113	4228
+5	2266	2118	1971	4229
+5	2226	2082	2081	4230
+5	2282	2114	2238	4231
+5	2273	2110	2222	4232
+5	2256	2111	2115	4233
+5	2180	2013	2166	4234
+5	2181	2034	2180	4235
+5	2317	2175	2316	4236
+5	2457	2319	2385	4237
+5	2118	2117	1970	4238
+5	2118	1970	1971	4239
+5	2219	2074	2073	4240
+5	2334	2193	2192	4241
+5	2140	1963	1976	4242
+5	2120	1976	1994	4243
+5	2175	2029	2028	4244
+5	2177	2031	2030	4245
+5	2462	2324	2398	4246
+5	2345	2205	2230	4247
+5	2211	2065	2066	4248
+5	2123	2066	1968	4249
+5	2124	2120	1994	4250
+5	2124	1994	2071	4251
+5	2125	2114	1938	4252
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+3	92	93
+3	93	94
+3	94	95
+3	95	96
+3	96	97
+3	97	98
+3	98	99
+3	99	100
+3	100	101
+3	101	102
+3	102	103
+3	103	104
+3	104	105
+3	105	106
+3	106	107
+3	107	108
+3	108	109
+3	109	110
+3	110	111
+3	111	112
+3	112	113
+3	113	114
+3	114	115
+3	115	116
+3	116	117
+3	117	118
+3	118	119
+3	119	120
+3	120	121
+3	121	122
+3	122	123
+3	123	124
+3	124	125
+3	125	126
+3	126	127
+3	127	128
+3	128	129
+3	129	130
+3	130	131
+3	131	132
+3	132	133
+3	133	134
+3	134	135
+3	135	136
+3	136	137
+3	137	138
+3	138	139
+3	139	140
+3	140	141
+3	141	142
+3	142	143
+3	143	144
+3	144	145
+3	145	146
+3	146	147
+3	147	148
+3	148	149
+3	149	150
+3	150	151
+3	151	152
+3	152	153
+3	153	154
+3	154	155
+3	155	156
+3	156	157
+3	157	158
+3	158	159
+3	159	160
+3	160	161
+3	161	162
+3	162	163
+3	163	164
+3	164	165
+3	165	166
+3	166	167
+3	167	168
+3	168	169
+3	169	170
+3	170	171
+3	171	172
+3	172	173
+3	173	174
+3	174	175
+3	175	176
+3	176	177
+3	177	178
+3	178	179
+3	179	180
+3	180	181
+3	181	182
+3	182	183
+3	183	184
+3	184	185
+3	185	186
+3	186	187
+3	187	188
+3	188	189
+3	189	190
+3	190	191
+3	191	192
+3	192	193
+3	193	194
+3	194	195
+3	195	196
+3	196	197
+3	197	198
+3	198	199
+MARKER_TAG= farfield
+MARKER_ELEMS= 50
+3	200	201
+3	201	202
+3	202	203
+3	203	204
+3	204	205
+3	205	206
+3	206	207
+3	207	208
+3	208	209
+3	209	210
+3	210	211
+3	211	212
+3	212	213
+3	213	214
+3	214	215
+3	215	216
+3	216	217
+3	217	218
+3	218	219
+3	219	220
+3	220	221
+3	221	222
+3	222	223
+3	223	224
+3	224	225
+3	225	226
+3	226	227
+3	227	228
+3	228	229
+3	229	230
+3	230	231
+3	231	232
+3	232	233
+3	233	234
+3	234	235
+3	235	236
+3	236	237
+3	237	238
+3	238	239
+3	239	240
+3	240	241
+3	241	242
+3	242	243
+3	243	244
+3	244	245
+3	245	246
+3	246	247
+3	247	248
+3	248	249
+3	249	200
diff --git a/externals/utils/release_su2.sh b/externals/utils/release_su2.sh
index dc8555aff25..a5e224d4728 100755
--- a/externals/utils/release_su2.sh
+++ b/externals/utils/release_su2.sh
@@ -47,8 +47,11 @@ if [ ! -d ${RELEASEDIR} ]
 then
  mkdir ${RELEASEDIR}
  mkdir ${RELEASEDIR}/bin
+ mkdir ${RELEASEDIR}/QuickStart
 fi
 cp -R ${SU2DIR}/bin/* ${RELEASEDIR}/bin/
+cp ${SU2DIR}/QuickStart/inv_NACA0012.cfg ${RELEASEDIR}/QuickStart/
+cp ${SU2DIR}/QuickStart/mesh_NACA0012_inv.su2 ${RELEASEDIR}/QuickStart/
 rm -fr ${SU2DIR}
 
 # Tar up the finished build directory and clean up

From aeafb37700a65184ddaed6469b23477fa63d9601 Mon Sep 17 00:00:00 2001
From: Joseph Signorelli <jms26@illinois.edu>
Date: Tue, 11 Jul 2023 19:06:03 -0500
Subject: [PATCH 584/656] Nondimensionalize Python custom HFs correctly

---
 SU2_CFD/src/solvers/CHeatSolver.cpp | 2 +-
 SU2_CFD/src/solvers/CNSSolver.cpp   | 2 +-
 2 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/SU2_CFD/src/solvers/CHeatSolver.cpp b/SU2_CFD/src/solvers/CHeatSolver.cpp
index aeefcfd75f0..c5047666d6a 100644
--- a/SU2_CFD/src/solvers/CHeatSolver.cpp
+++ b/SU2_CFD/src/solvers/CHeatSolver.cpp
@@ -400,7 +400,7 @@ void CHeatSolver::BC_HeatFlux_Wall(CGeometry* geometry, CSolver** solver_contain
     if (!geometry->nodes->GetDomain(iPoint)) continue;
 
     if (IsPyCustom) {
-      Wall_HeatFlux = geometry->GetCustomBoundaryHeatFlux(val_marker, iVertex);
+      Wall_HeatFlux = geometry->GetCustomBoundaryHeatFlux(val_marker, iVertex) / config->GetHeat_Flux_Ref();
     }
     /*--- Viscous contribution to the residual at the wall. ---*/
     const auto* Normal = geometry->vertex[val_marker][iVertex]->GetNormal();
diff --git a/SU2_CFD/src/solvers/CNSSolver.cpp b/SU2_CFD/src/solvers/CNSSolver.cpp
index dcbedda2907..638eb16ee6a 100644
--- a/SU2_CFD/src/solvers/CNSSolver.cpp
+++ b/SU2_CFD/src/solvers/CNSSolver.cpp
@@ -472,7 +472,7 @@ void CNSSolver::BC_HeatFlux_Wall_Generic(const CGeometry* geometry, const CConfi
     /*--- If it is a customizable patch, retrieve the specified wall heat flux. ---*/
 
     if (config->GetMarker_All_PyCustom(val_marker))
-      Wall_HeatFlux = geometry->GetCustomBoundaryHeatFlux(val_marker, iVertex);
+      Wall_HeatFlux = geometry->GetCustomBoundaryHeatFlux(val_marker, iVertex) / config->GetHeat_Flux_Ref();
     else if (kind_boundary == HEAT_TRANSFER) {
       const su2double Twall = nodes->GetTemperature(iPoint);
       Wall_HeatFlux = Transfer_Coefficient * (Tinfinity - Twall);

From 84f9227ea92c182315816f9cce40d872886fbac8 Mon Sep 17 00:00:00 2001
From: Joseph Signorelli <jms26@illinois.edu>
Date: Tue, 11 Jul 2023 19:06:58 -0500
Subject: [PATCH 585/656] Nondimensionalize Python custom temperatures
 correctly

---
 SU2_CFD/src/solvers/CHeatSolver.cpp | 2 +-
 SU2_CFD/src/solvers/CNSSolver.cpp   | 2 +-
 2 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/SU2_CFD/src/solvers/CHeatSolver.cpp b/SU2_CFD/src/solvers/CHeatSolver.cpp
index c5047666d6a..407fa0455cc 100644
--- a/SU2_CFD/src/solvers/CHeatSolver.cpp
+++ b/SU2_CFD/src/solvers/CHeatSolver.cpp
@@ -377,7 +377,7 @@ void CHeatSolver::BC_Isothermal_Wall(CGeometry *geometry, CSolver **solver_conta
   SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
   for (auto iVertex = 0ul; iVertex < geometry->nVertex[val_marker]; iVertex++) {
     if (IsPyCustom) {
-      Twall = geometry->GetCustomBoundaryTemperature(val_marker, iVertex);
+      Twall = geometry->GetCustomBoundaryTemperature(val_marker, iVertex) / config->GetTemperature_Ref();
     }
     IsothermalBoundaryCondition(geometry, solver_container[FLOW_SOL], config, val_marker, iVertex, Twall);
   }
diff --git a/SU2_CFD/src/solvers/CNSSolver.cpp b/SU2_CFD/src/solvers/CNSSolver.cpp
index 638eb16ee6a..b9b9b698823 100644
--- a/SU2_CFD/src/solvers/CNSSolver.cpp
+++ b/SU2_CFD/src/solvers/CNSSolver.cpp
@@ -710,7 +710,7 @@ void CNSSolver::BC_Isothermal_Wall_Generic(CGeometry *geometry, CSolver **solver
                                     thermal_conductivity, There, Temperature_Ref);
     }
     else if (config->GetMarker_All_PyCustom(val_marker)) {
-      Twall = geometry->GetCustomBoundaryTemperature(val_marker, iVertex);
+      Twall = geometry->GetCustomBoundaryTemperature(val_marker, iVertex) / Temperature_Ref;
     }
 
     /*--- Compute the normal gradient in temperature using Twall ---*/

From 3fa5caa63077981b54aa7c97ec8c194646d3ee26 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Thu, 13 Jul 2023 16:30:40 +0200
Subject: [PATCH 586/656] Move if out of parallel region.

---
 Common/src/geometry/CPhysicalGeometry.cpp | 26 ++++++++++++-----------
 1 file changed, 14 insertions(+), 12 deletions(-)

diff --git a/Common/src/geometry/CPhysicalGeometry.cpp b/Common/src/geometry/CPhysicalGeometry.cpp
index 6ecfb42c140..4c5fdd47d9f 100644
--- a/Common/src/geometry/CPhysicalGeometry.cpp
+++ b/Common/src/geometry/CPhysicalGeometry.cpp
@@ -10571,25 +10571,27 @@ void CPhysicalGeometry::SetWallDistance(CADTElemClass* WallADT, const CConfig* c
   /*---        distance to a solid wall element                           ---*/
   /*--------------------------------------------------------------------------*/
 
-  SU2_OMP_PARALLEL
   if (!WallADT->IsEmpty()) {
     /*--- Solid wall boundary nodes are present. Compute the wall
      distance for all nodes. ---*/
 
-    SU2_OMP_FOR_DYN(roundUpDiv(nPoint, 2 * omp_get_max_threads()))
-    for (unsigned long iPoint = 0; iPoint < GetnPoint(); ++iPoint) {
-      unsigned short markerID;
-      unsigned long elemID;
-      int rankID;
-      su2double dist;
+    SU2_OMP_PARALLEL
+    {
+      SU2_OMP_FOR_DYN(roundUpDiv(nPoint, 2 * omp_get_max_threads()))
+      for (unsigned long iPoint = 0; iPoint < GetnPoint(); ++iPoint) {
+        unsigned short markerID;
+        unsigned long elemID;
+        int rankID;
+        su2double dist;
 
-      WallADT->DetermineNearestElement(nodes->GetCoord(iPoint), dist, markerID, elemID, rankID);
+        WallADT->DetermineNearestElement(nodes->GetCoord(iPoint), dist, markerID, elemID, rankID);
 
-      if (dist < nodes->GetWall_Distance(iPoint)) {
-        nodes->SetWall_Distance(iPoint, dist, rankID, iZone, markerID, elemID);
+        if (dist < nodes->GetWall_Distance(iPoint)) {
+          nodes->SetWall_Distance(iPoint, dist, rankID, iZone, markerID, elemID);
+        }
       }
+      END_SU2_OMP_FOR
     }
-    END_SU2_OMP_FOR
+    END_SU2_OMP_PARALLEL
   }
-  END_SU2_OMP_PARALLEL
 }

From 8802c668601b7e96ddcdedbb865b7abba5c9e84a Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Thu, 13 Jul 2023 18:04:16 +0200
Subject: [PATCH 587/656] Different loop schedule to fix suspected false
 positives.

---
 Common/src/geometry/CPhysicalGeometry.cpp | 4 ++++
 1 file changed, 4 insertions(+)

diff --git a/Common/src/geometry/CPhysicalGeometry.cpp b/Common/src/geometry/CPhysicalGeometry.cpp
index 4c5fdd47d9f..8f9d7beb51f 100644
--- a/Common/src/geometry/CPhysicalGeometry.cpp
+++ b/Common/src/geometry/CPhysicalGeometry.cpp
@@ -10577,7 +10577,11 @@ void CPhysicalGeometry::SetWallDistance(CADTElemClass* WallADT, const CConfig* c
 
     SU2_OMP_PARALLEL
     {
+      #ifdef __SANITIZE_THREAD__
+      SU2_OMP_FOR_()
+      #else
       SU2_OMP_FOR_DYN(roundUpDiv(nPoint, 2 * omp_get_max_threads()))
+      #endif
       for (unsigned long iPoint = 0; iPoint < GetnPoint(); ++iPoint) {
         unsigned short markerID;
         unsigned long elemID;

From 4366d5c91bce7e424f3780f414cecbe817772817 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Thu, 13 Jul 2023 18:11:50 +0200
Subject: [PATCH 588/656] Formatting.

---
 Common/src/geometry/CPhysicalGeometry.cpp | 9 ++++-----
 1 file changed, 4 insertions(+), 5 deletions(-)

diff --git a/Common/src/geometry/CPhysicalGeometry.cpp b/Common/src/geometry/CPhysicalGeometry.cpp
index 8f9d7beb51f..222db44b624 100644
--- a/Common/src/geometry/CPhysicalGeometry.cpp
+++ b/Common/src/geometry/CPhysicalGeometry.cpp
@@ -10575,13 +10575,12 @@ void CPhysicalGeometry::SetWallDistance(CADTElemClass* WallADT, const CConfig* c
     /*--- Solid wall boundary nodes are present. Compute the wall
      distance for all nodes. ---*/
 
-    SU2_OMP_PARALLEL
-    {
-      #ifdef __SANITIZE_THREAD__
+    SU2_OMP_PARALLEL {
+#ifdef __SANITIZE_THREAD__
       SU2_OMP_FOR_()
-      #else
+#else
       SU2_OMP_FOR_DYN(roundUpDiv(nPoint, 2 * omp_get_max_threads()))
-      #endif
+#endif
       for (unsigned long iPoint = 0; iPoint < GetnPoint(); ++iPoint) {
         unsigned short markerID;
         unsigned long elemID;

From 1df0ea1b95df0a4ae5731f5e1f04452e387bca46 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Thu, 13 Jul 2023 18:42:30 +0200
Subject: [PATCH 589/656] Work around syntax check.

---
 Common/src/geometry/CPhysicalGeometry.cpp | 8 ++++----
 1 file changed, 4 insertions(+), 4 deletions(-)

diff --git a/Common/src/geometry/CPhysicalGeometry.cpp b/Common/src/geometry/CPhysicalGeometry.cpp
index 222db44b624..7ceaa0d0457 100644
--- a/Common/src/geometry/CPhysicalGeometry.cpp
+++ b/Common/src/geometry/CPhysicalGeometry.cpp
@@ -10576,11 +10576,11 @@ void CPhysicalGeometry::SetWallDistance(CADTElemClass* WallADT, const CConfig* c
      distance for all nodes. ---*/
 
     SU2_OMP_PARALLEL {
-#ifdef __SANITIZE_THREAD__
-      SU2_OMP_FOR_()
-#else
-      SU2_OMP_FOR_DYN(roundUpDiv(nPoint, 2 * omp_get_max_threads()))
+      SU2_OMP_FOR_(
+#ifndef __SANITIZE_THREAD__
+        schedule(dynamic, roundUpDiv(nPoint, 2 * omp_get_max_threads()))
 #endif
+      )
       for (unsigned long iPoint = 0; iPoint < GetnPoint(); ++iPoint) {
         unsigned short markerID;
         unsigned long elemID;

From 1835a8408c4590b03c55aeca211e2efdafd03814 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Thu, 13 Jul 2023 18:44:43 +0200
Subject: [PATCH 590/656] Formatting.

---
 Common/src/geometry/CPhysicalGeometry.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/Common/src/geometry/CPhysicalGeometry.cpp b/Common/src/geometry/CPhysicalGeometry.cpp
index 7ceaa0d0457..8e2cc4d7bcb 100644
--- a/Common/src/geometry/CPhysicalGeometry.cpp
+++ b/Common/src/geometry/CPhysicalGeometry.cpp
@@ -10578,7 +10578,7 @@ void CPhysicalGeometry::SetWallDistance(CADTElemClass* WallADT, const CConfig* c
     SU2_OMP_PARALLEL {
       SU2_OMP_FOR_(
 #ifndef __SANITIZE_THREAD__
-        schedule(dynamic, roundUpDiv(nPoint, 2 * omp_get_max_threads()))
+          schedule(dynamic, roundUpDiv(nPoint, 2 * omp_get_max_threads()))
 #endif
       )
       for (unsigned long iPoint = 0; iPoint < GetnPoint(); ++iPoint) {

From 194c249c6208341c2e766cebcea391a4ec81335a Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 14 Jul 2023 16:02:33 +0200
Subject: [PATCH 591/656] Fixed bug for density calculation when using ideal
 gas approximation in flamelet fluid model

---
 SU2_CFD/src/fluid/CFluidFlamelet.cpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/SU2_CFD/src/fluid/CFluidFlamelet.cpp b/SU2_CFD/src/fluid/CFluidFlamelet.cpp
index f4e22cead73..471c22fe1a4 100644
--- a/SU2_CFD/src/fluid/CFluidFlamelet.cpp
+++ b/SU2_CFD/src/fluid/CFluidFlamelet.cpp
@@ -136,7 +136,7 @@ void CFluidFlamelet::SetTDState_T(su2double val_temperature, const su2double* va
       break;
     case INC_DENSITYMODEL::VARIABLE:
       molar_weight = val_vars_TD[LOOKUP_TD::MOLARWEIGHT];
-      Density = Pressure / (molar_weight * UNIVERSAL_GAS_CONSTANT * Temperature);
+      Density = (molar_weight / 1000) *  Pressure / ( UNIVERSAL_GAS_CONSTANT * Temperature);
       break;
     default:
       break;

From 614d076326aa0d9355099f8d3751b04401d609a7 Mon Sep 17 00:00:00 2001
From: bigfooted <bigfootedrockmidget@hotmail.com>
Date: Sat, 15 Jul 2023 21:54:22 +0200
Subject: [PATCH 592/656] fix table lookup bug

---
 Common/src/containers/CTrapezoidalMap.cpp | 9 +++++++--
 1 file changed, 7 insertions(+), 2 deletions(-)

diff --git a/Common/src/containers/CTrapezoidalMap.cpp b/Common/src/containers/CTrapezoidalMap.cpp
index af3ff86a7e7..4bb943768fd 100644
--- a/Common/src/containers/CTrapezoidalMap.cpp
+++ b/Common/src/containers/CTrapezoidalMap.cpp
@@ -198,9 +198,14 @@ unsigned long CTrapezoidalMap::GetTriangle(su2double val_x, su2double val_y) {
   sort(triangles_edge_up.begin(), triangles_edge_up.end());
 
   /* The intersection of the faces to which upper or lower belongs is the face that both belong to. */
-  vector<unsigned long> triangle(1);
+  vector<unsigned long> triangle;
   set_intersection(triangles_edge_up.begin(), triangles_edge_up.end(), triangles_edge_low.begin(),
-                   triangles_edge_low.end(), triangle.begin());
+                   triangles_edge_low.end(), std::back_inserter(triangle));
+
+  /*--- We failed to find an intersection, so take the lower triangle inside the band enclosing the point---*/
+  if (triangle.size() < 1) {
+    triangle.resize(1, triangles_edge_low[0]);
+  }
 
   return triangle[0];
 }

From e200d8d9da8ca6d1b78778a02ece59600d91b130 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 15 Jul 2023 15:47:17 -0700
Subject: [PATCH 593/656] remove unimplemented TWIST_2D

---
 .../grid_movement/CSurfaceMovement.hpp        | 11 -----------
 Common/include/option_structure.hpp           |  2 --
 Common/include/option_structure.inl           | 13 +++++--------
 Common/src/CConfig.cpp                        |  4 ----
 Common/src/grid_movement/CSurfaceMovement.cpp | 19 +++++--------------
 QuickStart/inv_NACA0012.cfg                   |  3 +--
 .../src/drivers/CDiscAdjDeformationDriver.cpp | 11 ++++-------
 SU2_GEO/src/SU2_GEO.cpp                       |  5 -----
 SU2_PY/SU2/io/config.py                       |  3 ---
 SU2_PY/SU2/io/config_options.py               |  2 --
 SU2_PY/SU2/io/tools.py                        |  1 -
 config_template.cfg                           |  4 +---
 12 files changed, 16 insertions(+), 62 deletions(-)

diff --git a/Common/include/grid_movement/CSurfaceMovement.hpp b/Common/include/grid_movement/CSurfaceMovement.hpp
index 6a8382d1571..bcee11a7ec2 100644
--- a/Common/include/grid_movement/CSurfaceMovement.hpp
+++ b/Common/include/grid_movement/CSurfaceMovement.hpp
@@ -336,17 +336,6 @@ class CSurfaceMovement : public CGridMovement {
   bool SetFFDCamber_2D(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox, CFreeFormDefBox** ResetFFDBox,
                        unsigned short iDV, bool ResetDef) const;
 
-  /*!
-   * \brief Set a camber deformation of the Free From box using the control point position.
-   * \param[in] geometry - Geometrical definition of the problem.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] FFDBox - Array with all the free forms FFDBoxes of the computation.
-   * \param[in] iDV - Index of the design variable.
-   * \param[in] ResetDef - Reset the deformation before starting a new one.
-   */
-  bool SetFFDTwist_2D(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox, CFreeFormDefBox** ResetFFDBox,
-                      unsigned short iDV, bool ResetDef);
-
   /*!
    * \brief Set a thickness deformation of the Free From box using the control point position.
    * \param[in] geometry - Geometrical definition of the problem.
diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index 7e5aa1727de..e2ce38ed724 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -2124,7 +2124,6 @@ enum ENUM_PARAM {
   FFD_CONTROL_POINT_2D = 19,  /*!< \brief Free form deformation for 2D design (change a control point). */
   FFD_CAMBER_2D = 20,         /*!< \brief Free form deformation for 3D design (camber change). */
   FFD_THICKNESS_2D = 21,      /*!< \brief Free form deformation for 3D design (thickness change). */
-  FFD_TWIST_2D = 22,          /*!< \brief Free form deformation for 3D design (camber change). */
   FFD_CONTROL_SURFACE = 23,   /*!< \brief Free form deformation for 3D design (control surface). */
   FFD_ANGLE_OF_ATTACK = 24,   /*!< \brief Angle of attack for FFD problem. */
   HICKS_HENNE = 30,           /*!< \brief Hicks-Henne bump function for airfoil deformation. */
@@ -2147,7 +2146,6 @@ enum ENUM_PARAM {
 static const MapType<std::string, ENUM_PARAM> Param_Map = {
   MakePair("FFD_SETTING", FFD_SETTING)
   MakePair("FFD_CONTROL_POINT_2D", FFD_CONTROL_POINT_2D)
-  MakePair("FFD_TWIST_2D", FFD_TWIST_2D)
   MakePair("FFD_ANGLE_OF_ATTACK", FFD_ANGLE_OF_ATTACK)
   MakePair("FFD_CAMBER_2D", FFD_CAMBER_2D)
   MakePair("FFD_THICKNESS_2D", FFD_THICKNESS_2D)
diff --git a/Common/include/option_structure.inl b/Common/include/option_structure.inl
index f017aa65e2c..6cdc29d9656 100644
--- a/Common/include/option_structure.inl
+++ b/Common/include/option_structure.inl
@@ -567,9 +567,6 @@ class COptionDVParam : public COptionBase {
         case FFD_THICKNESS_2D:
           nParamDV[iDV] = 2;
           break;
-        case FFD_TWIST_2D:
-          nParamDV[iDV] = 3;
-          break;
         case HICKS_HENNE:
           nParamDV[iDV] = 2;
           break;
@@ -676,11 +673,11 @@ class COptionDVParam : public COptionBase {
             ((this->design_variable[iDV] == NO_DEFORMATION) || (this->design_variable[iDV] == FFD_SETTING) ||
              (this->design_variable[iDV] == FFD_ANGLE_OF_ATTACK) ||
              (this->design_variable[iDV] == FFD_CONTROL_POINT_2D) || (this->design_variable[iDV] == FFD_CAMBER_2D) ||
-             (this->design_variable[iDV] == FFD_TWIST_2D) || (this->design_variable[iDV] == FFD_THICKNESS_2D) ||
-             (this->design_variable[iDV] == FFD_CONTROL_POINT) || (this->design_variable[iDV] == FFD_NACELLE) ||
-             (this->design_variable[iDV] == FFD_GULL) || (this->design_variable[iDV] == FFD_TWIST) ||
-             (this->design_variable[iDV] == FFD_ROTATION) || (this->design_variable[iDV] == FFD_CONTROL_SURFACE) ||
-             (this->design_variable[iDV] == FFD_CAMBER) || (this->design_variable[iDV] == FFD_THICKNESS))) {
+             (this->design_variable[iDV] == FFD_THICKNESS_2D) || (this->design_variable[iDV] == FFD_CONTROL_POINT) ||
+             (this->design_variable[iDV] == FFD_NACELLE) || (this->design_variable[iDV] == FFD_GULL) ||
+             (this->design_variable[iDV] == FFD_TWIST) || (this->design_variable[iDV] == FFD_ROTATION) ||
+             (this->design_variable[iDV] == FFD_CONTROL_SURFACE) || (this->design_variable[iDV] == FFD_CAMBER) ||
+             (this->design_variable[iDV] == FFD_THICKNESS))) {
           ss >> this->FFDTag[iDV];
           this->paramDV[iDV][iParamDV] = 0;
         } else
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 33ef724f162..beed960dea1 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -2302,7 +2302,6 @@ void CConfig::SetConfig_Options() {
    - SPHERICAL ( ControlPoint_Index, Theta_Disp, R_Disp )
    - FFD_CONTROL_POINT ( FFDBox ID, i_Ind, j_Ind, k_Ind, x_Disp, y_Disp, z_Disp )
    - FFD_TWIST ( FFDBox ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-   - FFD_TWIST_2D ( FFDBox ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
    - FFD_ROTATION ( FFDBox ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
    - FFD_CONTROL_SURFACE ( FFDBox ID, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
    - FFD_CAMBER ( FFDBox ID, i_Ind, j_Ind )
@@ -6434,7 +6433,6 @@ void CConfig::SetOutput(SU2_COMPONENT val_software, unsigned short val_izone) {
           case FFD_CONTROL_POINT_2D:  cout << "FFD 2D (control point) <-> "; break;
           case FFD_CAMBER_2D:         cout << "FFD 2D (camber) <-> "; break;
           case FFD_THICKNESS_2D:      cout << "FFD 2D (thickness) <-> "; break;
-          case FFD_TWIST_2D:          cout << "FFD 2D (twist) <-> "; break;
           case HICKS_HENNE:           cout << "Hicks Henne <-> " ; break;
           case SURFACE_BUMP:          cout << "Surface bump <-> " ; break;
           case ANGLE_OF_ATTACK:       cout << "Angle of attack <-> " ; break;
@@ -6484,7 +6482,6 @@ void CConfig::SetOutput(SU2_COMPONENT val_software, unsigned short val_izone) {
             (Design_Variable[iDV] ==  CST) ||
             (Design_Variable[iDV] ==  SURFACE_BUMP) ||
             (Design_Variable[iDV] ==  FFD_CAMBER) ||
-            (Design_Variable[iDV] ==  FFD_TWIST_2D) ||
             (Design_Variable[iDV] ==  FFD_THICKNESS) ) nParamDV = 3;
         if (Design_Variable[iDV] == FFD_CONTROL_POINT_2D) nParamDV = 5;
         if (Design_Variable[iDV] == ROTATION) nParamDV = 6;
@@ -6504,7 +6501,6 @@ void CConfig::SetOutput(SU2_COMPONENT val_software, unsigned short val_izone) {
                (Design_Variable[iDV] == FFD_CONTROL_POINT_2D) ||
                (Design_Variable[iDV] == FFD_CAMBER_2D) ||
                (Design_Variable[iDV] == FFD_THICKNESS_2D) ||
-               (Design_Variable[iDV] == FFD_TWIST_2D) ||
                (Design_Variable[iDV] == FFD_CONTROL_POINT) ||
                (Design_Variable[iDV] == FFD_NACELLE) ||
                (Design_Variable[iDV] == FFD_GULL) ||
diff --git a/Common/src/grid_movement/CSurfaceMovement.cpp b/Common/src/grid_movement/CSurfaceMovement.cpp
index 1905b57deaa..b09631f9836 100644
--- a/Common/src/grid_movement/CSurfaceMovement.cpp
+++ b/Common/src/grid_movement/CSurfaceMovement.cpp
@@ -160,12 +160,11 @@ vector<vector<su2double> > CSurfaceMovement::SetSurface_Deformation(CGeometry* g
   /*--- Free Form deformation based ---*/
 
   if ((config->GetDesign_Variable(0) == FFD_CONTROL_POINT_2D) || (config->GetDesign_Variable(0) == FFD_CAMBER_2D) ||
-      (config->GetDesign_Variable(0) == FFD_THICKNESS_2D) || (config->GetDesign_Variable(0) == FFD_TWIST_2D) ||
-      (config->GetDesign_Variable(0) == FFD_CONTROL_POINT) || (config->GetDesign_Variable(0) == FFD_NACELLE) ||
-      (config->GetDesign_Variable(0) == FFD_GULL) || (config->GetDesign_Variable(0) == FFD_TWIST) ||
-      (config->GetDesign_Variable(0) == FFD_ROTATION) || (config->GetDesign_Variable(0) == FFD_CONTROL_SURFACE) ||
-      (config->GetDesign_Variable(0) == FFD_CAMBER) || (config->GetDesign_Variable(0) == FFD_THICKNESS) ||
-      (config->GetDesign_Variable(0) == FFD_ANGLE_OF_ATTACK)) {
+      (config->GetDesign_Variable(0) == FFD_THICKNESS_2D) || (config->GetDesign_Variable(0) == FFD_CONTROL_POINT) ||
+      (config->GetDesign_Variable(0) == FFD_NACELLE) || (config->GetDesign_Variable(0) == FFD_GULL) ||
+      (config->GetDesign_Variable(0) == FFD_TWIST) || (config->GetDesign_Variable(0) == FFD_ROTATION) ||
+      (config->GetDesign_Variable(0) == FFD_CONTROL_SURFACE) || (config->GetDesign_Variable(0) == FFD_CAMBER) ||
+      (config->GetDesign_Variable(0) == FFD_THICKNESS) || (config->GetDesign_Variable(0) == FFD_ANGLE_OF_ATTACK)) {
     /*--- Definition of the FFD deformation class ---*/
 
     FFDBox = new CFreeFormDefBox*[MAX_NUMBER_FFD];
@@ -1558,9 +1557,6 @@ void CSurfaceMovement::ApplyDesignVariables(CGeometry* geometry, CConfig* config
       case FFD_THICKNESS_2D:
         SetFFDThickness_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false);
         break;
-      case FFD_TWIST_2D:
-        SetFFDTwist_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false);
-        break;
       case FFD_CONTROL_POINT:
         SetFFDCPChange(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, false);
         break;
@@ -2247,11 +2243,6 @@ bool CSurfaceMovement::SetFFDThickness_2D(CGeometry* geometry, CConfig* config,
   return true;
 }
 
-bool CSurfaceMovement::SetFFDTwist_2D(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox,
-                                      CFreeFormDefBox** ResetFFDBox, unsigned short iDV, bool ResetDef) {
-  return true;
-}
-
 bool CSurfaceMovement::SetFFDCamber(CGeometry* geometry, CConfig* config, CFreeFormDefBox* FFDBox,
                                     CFreeFormDefBox** ResetFFDBox, unsigned short iDV, bool ResetDef) const {
   su2double Ampl, movement[3] = {0.0, 0.0, 0.0};
diff --git a/QuickStart/inv_NACA0012.cfg b/QuickStart/inv_NACA0012.cfg
index 7f30c73c42a..9c25bbd1094 100644
--- a/QuickStart/inv_NACA0012.cfg
+++ b/QuickStart/inv_NACA0012.cfg
@@ -172,7 +172,7 @@ TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 % Kind of deformation (NO_DEFORMATION, TRANSLATION, ROTATION, SCALE,
 %                      FFD_SETTING, FFD_NACELLE
 %                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS, FFD_TWIST
-%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D, FFD_TWIST_2D,
+%                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
 %                      HICKS_HENNE, SURFACE_BUMP)
 DV_KIND= HICKS_HENNE
 %
@@ -196,7 +196,6 @@ DV_MARKER= ( airfoil )
 % - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
 % - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
 % - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - FFD_TWIST_2D ( FFD_BoxTag, x_Orig, y_Orig )
 % - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
 % - SURFACE_BUMP ( x_Start, x_End, x_Loc )
 DV_PARAM= ( 1, 0.5 )
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index 5645b8b7bdc..e37b1bb0c00 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -426,10 +426,10 @@ void CDiscAdjDeformationDriver::SetProjection_FD(CGeometry* geometry, CConfig* c
 
     if ((config->GetDesign_Variable(iDV) == FFD_CONTROL_POINT_2D) ||
         (config->GetDesign_Variable(iDV) == FFD_CAMBER_2D) || (config->GetDesign_Variable(iDV) == FFD_THICKNESS_2D) ||
-        (config->GetDesign_Variable(iDV) == FFD_TWIST_2D) || (config->GetDesign_Variable(iDV) == FFD_CONTROL_POINT) ||
-        (config->GetDesign_Variable(iDV) == FFD_NACELLE) || (config->GetDesign_Variable(iDV) == FFD_GULL) ||
-        (config->GetDesign_Variable(iDV) == FFD_TWIST) || (config->GetDesign_Variable(iDV) == FFD_ROTATION) ||
-        (config->GetDesign_Variable(iDV) == FFD_CAMBER) || (config->GetDesign_Variable(iDV) == FFD_THICKNESS) ||
+        (config->GetDesign_Variable(iDV) == FFD_CONTROL_POINT) || (config->GetDesign_Variable(iDV) == FFD_NACELLE) ||
+        (config->GetDesign_Variable(iDV) == FFD_GULL) || (config->GetDesign_Variable(iDV) == FFD_TWIST) ||
+        (config->GetDesign_Variable(iDV) == FFD_ROTATION) || (config->GetDesign_Variable(iDV) == FFD_CAMBER) ||
+        (config->GetDesign_Variable(iDV) == FFD_THICKNESS) ||
         (config->GetDesign_Variable(iDV) == FFD_ANGLE_OF_ATTACK)) {
       /*--- Read the FFD information in the first iteration. ---*/
 
@@ -482,9 +482,6 @@ void CDiscAdjDeformationDriver::SetProjection_FD(CGeometry* geometry, CConfig* c
             Local_MoveSurface =
                 surface_movement->SetFFDThickness_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true);
             break;
-          case FFD_TWIST_2D:
-            Local_MoveSurface = surface_movement->SetFFDTwist_2D(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true);
-            break;
           case FFD_CONTROL_POINT:
             Local_MoveSurface = surface_movement->SetFFDCPChange(geometry, config, FFDBox[iFFDBox], FFDBox, iDV, true);
             break;
diff --git a/SU2_GEO/src/SU2_GEO.cpp b/SU2_GEO/src/SU2_GEO.cpp
index eb0cb5c151e..585fa7aec7f 100644
--- a/SU2_GEO/src/SU2_GEO.cpp
+++ b/SU2_GEO/src/SU2_GEO.cpp
@@ -745,7 +745,6 @@ int main(int argc, char* argv[]) {
       if ((config_container[ZONE_0]->GetDesign_Variable(iDV) == FFD_CONTROL_POINT_2D) ||
           (config_container[ZONE_0]->GetDesign_Variable(iDV) == FFD_CAMBER_2D) ||
           (config_container[ZONE_0]->GetDesign_Variable(iDV) == FFD_THICKNESS_2D) ||
-          (config_container[ZONE_0]->GetDesign_Variable(iDV) == FFD_TWIST_2D) ||
           (config_container[ZONE_0]->GetDesign_Variable(iDV) == FFD_CONTROL_POINT) ||
           (config_container[ZONE_0]->GetDesign_Variable(iDV) == FFD_NACELLE) ||
           (config_container[ZONE_0]->GetDesign_Variable(iDV) == FFD_GULL) ||
@@ -824,10 +823,6 @@ int main(int argc, char* argv[]) {
               Local_MoveSurface = surface_movement->SetFFDThickness_2D(
                   geometry_container[ZONE_0], config_container[ZONE_0], FFDBox[iFFDBox], FFDBox, iDV, true);
               break;
-            case FFD_TWIST_2D:
-              Local_MoveSurface = surface_movement->SetFFDTwist_2D(geometry_container[ZONE_0], config_container[ZONE_0],
-                                                                   FFDBox[iFFDBox], FFDBox, iDV, true);
-              break;
             case FFD_CONTROL_POINT:
               Local_MoveSurface = surface_movement->SetFFDCPChange(geometry_container[ZONE_0], config_container[ZONE_0],
                                                                    FFDBox[iFFDBox], FFDBox, iDV, true);
diff --git a/SU2_PY/SU2/io/config.py b/SU2_PY/SU2/io/config.py
index e80e61ff900..41cac49d5db 100755
--- a/SU2_PY/SU2/io/config.py
+++ b/SU2_PY/SU2/io/config.py
@@ -413,7 +413,6 @@ def read_config(filename):
                         "FFD_CONTROL_POINT",
                         "FFD_NACELLE",
                         "FFD_GULL",
-                        "FFD_TWIST_2D",
                         "FFD_TWIST",
                         "FFD_ROTATION",
                         "FFD_CAMBER",
@@ -546,7 +545,6 @@ def read_config(filename):
                             "FFD_NACELLE",
                             "FFD_GULL",
                             "FFD_TWIST",
-                            "FFD_TWIST_2D",
                             "FFD_TWIST_ANGLE",
                             "FFD_ROTATION",
                             "FFD_CAMBER",
@@ -1117,7 +1115,6 @@ def write_config(filename, param_dict):
                             "FFD_GULL",
                             "FFD_TWIST_ANGLE",
                             "FFD_TWIST",
-                            "FFD_TWIST_2D",
                             "FFD_ROTATION",
                             "FFD_CAMBER",
                             "FFD_THICKNESS",
diff --git a/SU2_PY/SU2/io/config_options.py b/SU2_PY/SU2/io/config_options.py
index 1fda9691abd..512aa9d1f89 100644
--- a/SU2_PY/SU2/io/config_options.py
+++ b/SU2_PY/SU2/io/config_options.py
@@ -72,7 +72,6 @@ class DEFINITION_DV(ordered_bunch):
        -FFD_CONTROL_POINT_2D (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
        -FFD_CAMBER_2D 	 (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
        -FFD_THICKNESS_2D 	 (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-       -FFD_TWIST_2D    	 (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
        -HICKS_HENNE 	 (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
        -ANGLE_OF_ATTACK	 ( 101, Scale | Mark. List | 1.0 )
 
@@ -128,7 +127,6 @@ class DV_KIND(ordered_bunch):
        -FFD_CONTROL_POINT_2D (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
        -FFD_CAMBER_2D 	 (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
        -FFD_THICKNESS_2D 	 (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-       -FFD_TWIST_2D    	 (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
        -HICKS_HENNE 	 (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
        -ANGLE_OF_ATTACK	 ( 101, Scale | Mark. List | 1.0 )
 
diff --git a/SU2_PY/SU2/io/tools.py b/SU2_PY/SU2/io/tools.py
index 52b51d9ae54..0bf58603942 100755
--- a/SU2_PY/SU2/io/tools.py
+++ b/SU2_PY/SU2/io/tools.py
@@ -591,7 +591,6 @@ def get_dvMap():
         19: "FFD_CONTROL_POINT_2D",
         20: "FFD_CAMBER_2D",
         21: "FFD_THICKNESS_2D",
-        22: "FFD_TWIST_2D",
         23: "FFD_CONTROL_SURFACE",
         24: "FFD_ANGLE_OF_ATTACK",
         30: "HICKS_HENNE",
diff --git a/config_template.cfg b/config_template.cfg
index 45f33fede27..a5812c78d0a 100644
--- a/config_template.cfg
+++ b/config_template.cfg
@@ -1466,7 +1466,7 @@ ADAPT_BOUNDARY= YES
 %                      FFD_SETTING, FFD_NACELLE,
 %                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS, FFD_TWIST
 %                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D,
-%                      FFD_TWIST_2D, HICKS_HENNE, SURFACE_BUMP, SURFACE_FILE)
+%                      HICKS_HENNE, SURFACE_BUMP, SURFACE_FILE)
 DV_KIND= FFD_SETTING
 %
 % Marker of the surface in which we are going apply the shape deformation
@@ -1489,7 +1489,6 @@ DV_MARKER= ( airfoil )
 % - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
 % - FFD_CAMBER_2D ( FFD_BoxTag, i_Ind )
 % - FFD_THICKNESS_2D ( FFD_BoxTag, i_Ind )
-% - FFD_TWIST_2D ( FFD_BoxTag, x_Orig, y_Orig )
 % - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
 % - SURFACE_BUMP ( x_Start, x_End, x_Loc )
 DV_PARAM= ( 1, 0.5 )
@@ -1842,7 +1841,6 @@ REORIENT_ELEMENTS= YES
 %    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
 %    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
 %    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
 %    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
 %    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
 %

From 81e10b8fe338c8b9aa269a64a9dd0a946a4a7d99 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 16 Jul 2023 18:42:28 -0700
Subject: [PATCH 594/656] fix time output and some formating

---
 .../linear_algebra/vector_expressions.hpp     | 44 +++++++++----------
 Common/src/linear_algebra/CSysSolve.cpp       |  4 ++
 .../src/drivers/CDiscAdjMultizoneDriver.cpp   |  1 +
 3 files changed, 27 insertions(+), 22 deletions(-)

diff --git a/Common/include/linear_algebra/vector_expressions.hpp b/Common/include/linear_algebra/vector_expressions.hpp
index 000ce3cb2d0..b958411b0ba 100644
--- a/Common/include/linear_algebra/vector_expressions.hpp
+++ b/Common/include/linear_algebra/vector_expressions.hpp
@@ -146,28 +146,28 @@ MAKE_UNARY_FUN(sign, sign_, sign_impl)
 
 /*--- Macro to create expressions and overloads for binary functions. ---*/
 
-#define MAKE_BINARY_FUN(FUN, EXPR, IMPL)                                                                             \
-  /*!--- Expression class. ---*/                                                                                     \
-  template <class U, class V, class Scalar>                                                                          \
-  class EXPR : public CVecExpr<EXPR<U, V, Scalar>, Scalar> {                                                         \
-    store_t<const U> u;                                                                                              \
-    store_t<const V> v;                                                                                              \
-                                                                                                                     \
-   public:                                                                                                           \
-    static constexpr bool StoreAsRef = false;                                                                        \
-    FORCEINLINE EXPR(const U& u_, const V& v_) : u(u_), v(v_) {}                                                     \
-    FORCEINLINE auto operator[](size_t i) const RETURNS(IMPL(u[i], v[i]))                                            \
-  };                                                                                                                 \
-  /*!--- Vector with vector function overload. ---*/                                                                 \
-  template <class U, class V, class S>                                                                               \
-  FORCEINLINE auto FUN(const CVecExpr<U, S>& u, const CVecExpr<V, S>& v)                                             \
-      RETURNS(EXPR<U, V, S>(u.derived(), v.derived())) /*!--- Vector with scalar function overload. ---*/            \
-      template <class U, class S>                                                                                    \
-      FORCEINLINE auto FUN(const CVecExpr<U, S>& u, decay_t<S> v)                                                    \
-          RETURNS(EXPR<U, Bcast<S>, S>(u.derived(), Bcast<S>(v))) /*!--- Scalar with vector function overload. ---*/ \
-      template <class S, class V>                                                                                    \
-      FORCEINLINE auto FUN(decay_t<S> u, const CVecExpr<V, S>& v)                                                    \
-          RETURNS(EXPR<Bcast<S>, V, S>(Bcast<S>(u), v.derived()))
+#define MAKE_BINARY_FUN(FUN, EXPR, IMPL)                                                                               \
+  /*!--- Expression class. ---*/                                                                                       \
+  template <class U, class V, class Scalar>                                                                            \
+  class EXPR : public CVecExpr<EXPR<U, V, Scalar>, Scalar> {                                                           \
+    store_t<const U> u;                                                                                                \
+    store_t<const V> v;                                                                                                \
+                                                                                                                       \
+   public:                                                                                                             \
+    static constexpr bool StoreAsRef = false;                                                                          \
+    FORCEINLINE EXPR(const U& u_, const V& v_) : u(u_), v(v_) {}                                                       \
+    FORCEINLINE auto operator[](size_t i) const RETURNS(IMPL(u[i], v[i]))                                              \
+  };                                                                                                                   \
+  /*!--- Vector with vector function overload. ---*/                                                                   \
+  template <class U, class V, class S>                                                                                 \
+  FORCEINLINE auto FUN(const CVecExpr<U, S>& u, const CVecExpr<V, S>& v)                                               \
+      RETURNS(EXPR<U, V, S>(u.derived(), v.derived()));                                                                \
+  /*!--- Vector with scalar function overload. ---*/                                                                   \
+  template <class U, class S>                                                                                          \
+  FORCEINLINE auto FUN(const CVecExpr<U, S>& u, decay_t<S> v) RETURNS(EXPR<U, Bcast<S>, S>(u.derived(), Bcast<S>(v))); \
+  /*!--- Scalar with vector function overload. ---*/                                                                   \
+  template <class S, class V>                                                                                          \
+  FORCEINLINE auto FUN(decay_t<S> u, const CVecExpr<V, S>& v) RETURNS(EXPR<Bcast<S>, V, S>(Bcast<S>(u), v.derived()));
 
 /*--- std::max/min have issues (because they return by reference).
  * fmin and fmax return by value and thus are fine, but they would force
diff --git a/Common/src/linear_algebra/CSysSolve.cpp b/Common/src/linear_algebra/CSysSolve.cpp
index f561618b6ad..85ab1705942 100644
--- a/Common/src/linear_algebra/CSysSolve.cpp
+++ b/Common/src/linear_algebra/CSysSolve.cpp
@@ -452,7 +452,9 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
 
     /*---  Modified Gram-Schmidt orthogonalization ---*/
 
+    SU2_OMP_PARALLEL_(if (!omp_in_parallel()))
     ModGramSchmidt(i, H, W);
+    END_SU2_OMP_PARALLEL
 
     /*---  Apply old Givens rotations to new column of the Hessenberg matrix then generate the
      new Givens rotation matrix and apply it to the last two elements of H[:][i] and g ---*/
@@ -480,9 +482,11 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
 
   const auto& basis = flexible ? Z : W;
 
+  SU2_OMP_PARALLEL_(if (!omp_in_parallel()))
   for (unsigned long k = 0; k < i; k++) {
     x += y[k] * basis[k];
   }
+  END_SU2_OMP_PARALLEL
 
   /*---  Recalculate final (neg.) residual (this should be optional) ---*/
 
diff --git a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
index 6277f409b8d..615980dd728 100644
--- a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
@@ -308,6 +308,7 @@ void CDiscAdjMultizoneDriver::Run() {
 
   const unsigned long nOuterIter = driver_config->GetnOuter_Iter();
   const bool time_domain = driver_config->GetTime_Domain();
+  driver_config->Set_StartTime(SU2_MPI::Wtime());
 
   /*--- If the gradient of the objective function is 0 so are the adjoint variables.
    * Unless in unsteady problems where there are other contributions to the RHS. ---*/

From a31b8004a02507ce547c9eb2d142de77ebaeffa9 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Vinzenz=20G=C3=B6tz?=
 <81287997+MastermindScope@users.noreply.github.com>
Date: Mon, 17 Jul 2023 09:50:02 +0200
Subject: [PATCH 595/656] Update CFlowCompOutput.cpp with suggestions from 
 EvertBunschoten

---
 SU2_CFD/src/output/CFlowCompOutput.cpp | 12 ++++++------
 1 file changed, 6 insertions(+), 6 deletions(-)

diff --git a/SU2_CFD/src/output/CFlowCompOutput.cpp b/SU2_CFD/src/output/CFlowCompOutput.cpp
index 6e39ea53df4..92c933c52df 100644
--- a/SU2_CFD/src/output/CFlowCompOutput.cpp
+++ b/SU2_CFD/src/output/CFlowCompOutput.cpp
@@ -316,14 +316,14 @@ void CFlowCompOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolv
   SetVolumeOutputValue("DENSITY",    iPoint, Node_Flow->GetSolution(iPoint, 0));
   SetVolumeOutputValue("MOMENTUM-X", iPoint, Node_Flow->GetSolution(iPoint, 1));
   SetVolumeOutputValue("MOMENTUM-Y", iPoint, Node_Flow->GetSolution(iPoint, 2));
-  SetVolumeOutputValue("VELOCITY-X", iPoint, Node_Flow->GetSolution(iPoint, 3));
-  SetVolumeOutputValue("VELOCITY-Y", iPoint, Node_Flow->GetSolution(iPoint, 4));
+  SetVolumeOutputValue("VELOCITY-X", iPoint, Node_Flow->GetPrimitive(iPoint, 1));
+  SetVolumeOutputValue("VELOCITY-Y", iPoint, Node_Flow->GetPrimitive(iPoint, 2));
   if (nDim == 3){
-    SetVolumeOutputValue("MOMENTUM-Z", iPoint, Node_Flow->GetSolution(iPoint, 5));
-    SetVolumeOutputValue("ENERGY",     iPoint, Node_Flow->GetSolution(iPoint, 6));
-    SetVolumeOutputValue("VELOCITY-Z", iPoint, Node_Flow->GetSolution(iPoint, 7));
+    SetVolumeOutputValue("MOMENTUM-Z", iPoint, Node_Flow->GetSolution(iPoint, 3));
+    SetVolumeOutputValue("ENERGY",     iPoint, Node_Flow->GetSolution(iPoint, 4));
+    SetVolumeOutputValue("VELOCITY-Z", iPoint, Node_Flow->GetPrimitive(iPoint, 3));
   } else {
-    SetVolumeOutputValue("ENERGY",     iPoint, Node_Flow->GetSolution(iPoint, 5));
+    SetVolumeOutputValue("ENERGY",     iPoint, Node_Flow->GetSolution(iPoint, 3));
   }
 
   if (gridMovement){

From 6c156e2b7806f08e5da37f02250c0d55cc61a206 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Vinzenz=20G=C3=B6tz?=
 <81287997+MastermindScope@users.noreply.github.com>
Date: Mon, 17 Jul 2023 09:53:05 +0200
Subject: [PATCH 596/656] Update CNEMOCompOutput.cpp with suggestions from
 EvertBunschoten and  WallyMaier

---
 SU2_CFD/src/output/CNEMOCompOutput.cpp | 16 ++++++++--------
 1 file changed, 8 insertions(+), 8 deletions(-)

diff --git a/SU2_CFD/src/output/CNEMOCompOutput.cpp b/SU2_CFD/src/output/CNEMOCompOutput.cpp
index 8afbd1448a0..9902192bbc9 100644
--- a/SU2_CFD/src/output/CNEMOCompOutput.cpp
+++ b/SU2_CFD/src/output/CNEMOCompOutput.cpp
@@ -317,16 +317,16 @@ void CNEMOCompOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolv
 
   SetVolumeOutputValue("MOMENTUM-X", iPoint, Node_Flow->GetSolution(iPoint, nSpecies));
   SetVolumeOutputValue("MOMENTUM-Y", iPoint, Node_Flow->GetSolution(iPoint, nSpecies+1));
-  SetVolumeOutputValue("VELOCITY-X", iPoint, Node_Flow->GetSolution(iPoint, nSpecies+2));
-  SetVolumeOutputValue("VELOCITY-Y", iPoint, Node_Flow->GetSolution(iPoint, nSpecies+3));
+  SetVolumeOutputValue("VELOCITY-X", iPoint, Node_Flow->GetPrimitive(iPoint, nSpecies));
+  SetVolumeOutputValue("VELOCITY-Y", iPoint, Node_Flow->GetPrimitive(iPoint, nSpecies+1));
   if (nDim == 3){
-    SetVolumeOutputValue("MOMENTUM-Z", iPoint, Node_Flow->GetSolution(iPoint, nSpecies+4));
-    SetVolumeOutputValue("ENERGY",     iPoint, Node_Flow->GetSolution(iPoint, nSpecies+5));
-    SetVolumeOutputValue("ENERGY_VE",  iPoint, Node_Flow->GetSolution(iPoint, nSpecies+6));
-    SetVolumeOutputValue("VELOCITY-Z", iPoint, Node_Flow->GetSolution(iPoint, nSpecies+7));
+    SetVolumeOutputValue("MOMENTUM-Z", iPoint, Node_Flow->GetSolution(iPoint, nSpecies+2));
+    SetVolumeOutputValue("ENERGY",     iPoint, Node_Flow->GetSolution(iPoint, nSpecies+3));
+    SetVolumeOutputValue("ENERGY_VE",  iPoint, Node_Flow->GetSolution(iPoint, nSpecies+4));
+    SetVolumeOutputValue("VELOCITY-Z", iPoint, Node_Flow->GetPrimitive(iPoint, nSpecies+2));
   } else {
-    SetVolumeOutputValue("ENERGY",     iPoint, Node_Flow->GetSolution(iPoint, nSpecies+4));
-    SetVolumeOutputValue("ENERGY_VE",  iPoint, Node_Flow->GetSolution(iPoint, nSpecies+5));
+    SetVolumeOutputValue("ENERGY",     iPoint, Node_Flow->GetSolution(iPoint, nSpecies+2));
+    SetVolumeOutputValue("ENERGY_VE",  iPoint, Node_Flow->GetSolution(iPoint, nSpecies+3));
   }
 
   for(iSpecies = 0; iSpecies < nSpecies; iSpecies++)

From 9ef63ef2df1f41babc54e9ef9708da3abfcd5e68 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 17 Jul 2023 12:10:43 +0200
Subject: [PATCH 597/656] Address compiler warning.

---
 Common/src/geometry/CPhysicalGeometry.cpp | 10 +++++++---
 1 file changed, 7 insertions(+), 3 deletions(-)

diff --git a/Common/src/geometry/CPhysicalGeometry.cpp b/Common/src/geometry/CPhysicalGeometry.cpp
index 8e2cc4d7bcb..36f257b238a 100644
--- a/Common/src/geometry/CPhysicalGeometry.cpp
+++ b/Common/src/geometry/CPhysicalGeometry.cpp
@@ -10576,11 +10576,11 @@ void CPhysicalGeometry::SetWallDistance(CADTElemClass* WallADT, const CConfig* c
      distance for all nodes. ---*/
 
     SU2_OMP_PARALLEL {
-      SU2_OMP_FOR_(
 #ifndef __SANITIZE_THREAD__
-          schedule(dynamic, roundUpDiv(nPoint, 2 * omp_get_max_threads()))
+      SU2_OMP_FOR_DYN(roundUpDiv(nPoint, 2 * omp_get_max_threads()))
+#else
+      SU2_OMP_FOR_()
 #endif
-      )
       for (unsigned long iPoint = 0; iPoint < GetnPoint(); ++iPoint) {
         unsigned short markerID;
         unsigned long elemID;
@@ -10593,7 +10593,11 @@ void CPhysicalGeometry::SetWallDistance(CADTElemClass* WallADT, const CConfig* c
           nodes->SetWall_Distance(iPoint, dist, rankID, iZone, markerID, elemID);
         }
       }
+#ifndef __SANITIZE_THREAD__
       END_SU2_OMP_FOR
+#else
+      END_SU2_OMP_FOR
+#endif
     }
     END_SU2_OMP_PARALLEL
   }

From 212ffdcfcb7fe9c4814c78e1fd70d821f814e398 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 17 Jul 2023 14:31:13 +0200
Subject: [PATCH 598/656] Implemented reviewer comments

---
 Common/include/CConfig.hpp                    |   6 +
 Common/include/containers/CTrapezoidalMap.hpp |   2 +-
 Common/include/option_structure.hpp           |   9 +-
 Common/src/CConfig.cpp                        |   3 +
 Common/src/containers/CLookUpTable.cpp        |   2 +-
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp    |   2 +-
 SU2_CFD/include/fluid/CFluidFlamelet.hpp      |  26 ++-
 SU2_CFD/include/fluid/CFluidModel.hpp         |   2 +-
 .../solvers/CSpeciesFlameletSolver.hpp        |  12 +-
 SU2_CFD/src/fluid/CFluidFlamelet.cpp          | 193 +++++++++---------
 .../src/solvers/CSpeciesFlameletSolver.cpp    |  27 +--
 TestCases/parallel_regression.py              |   2 +-
 12 files changed, 140 insertions(+), 146 deletions(-)

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index 0835b5040d0..dd5bde0606c 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -2153,10 +2153,16 @@ class CConfig {
    */
   unsigned short GetNUserScalars() const { return n_user_scalars; }
 
+  /*!
+   * \brief Get the name of a specific controlling variable.
+   */
   const string& GetControllingVariableName(unsigned short i_cv) const {
     return controlling_variable_names[i_cv];
   }
 
+  /*!
+   * \brief Get the name of the source term variable for a specific controlling variable.
+   */
   const string& GetControllingVariableSourceName(unsigned short i_cv) const {
     return cv_source_names[i_cv];
   }
diff --git a/Common/include/containers/CTrapezoidalMap.hpp b/Common/include/containers/CTrapezoidalMap.hpp
index c53a09168ce..207b010d31e 100644
--- a/Common/include/containers/CTrapezoidalMap.hpp
+++ b/Common/include/containers/CTrapezoidalMap.hpp
@@ -104,5 +104,5 @@ class CTrapezoidalMap {
    * \brief get memory footprint of trapezoidal map.
    * \return - memory footprint in mega bytes.
    */
-  double GetMemoryFootprint() { return memory_footprint; }
+  double GetMemoryFootprint() const { return memory_footprint; }
 };
diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index 26b8083634f..bbbc976715c 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -1329,10 +1329,13 @@ enum FLAMELET_SCALAR_SOURCES {
   I_SRC_TOT_PROGVAR
 };
 
+/*!
+ * \brief Look-up operations for the flamelet scalar solver.
+ */
 enum FLAMELET_LOOKUP_OPS {
-  TD,
-  SOURCES,
-  LOOKUP,
+  TD,       /*!< \brief Thermochemical properties (temperature, density, diffusivity, etc.). */
+  SOURCES,  /*!< \brief Scalar source terms (controlling variables, passive species).*/
+  LOOKUP,   /*!< \brief Passive look-up variables specified in config. */
 };
 
 /*!
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index aebf9cccd0d..7c1431fa3d8 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -2101,7 +2101,10 @@ void CConfig::SetConfig_Options() {
   /* DESCRIPTION: Determine if we need to allocate memory to store the multizone residual. \n DEFAULT: true (temporarily) */
   addBoolOption("MULTIZONE_RESIDUAL", Multizone_Residual, false);
 
+  /* !\brief CONTROLLING_VARIABLE_NAMES \n DESCRIPTION: Names of the variables used as inputs for the data regression method in flamelet or data-driven fluid models. */
   addStringListOption("CONTROLLING_VARIABLE_NAMES", n_control_vars, controlling_variable_names);
+
+  /* !\brief CONTROLLING_VARIABLE_SOURCE_NAMES \n DESCRIPTION: Names of the variables in the flamelet manifold corresponding to the source terms of the controlling variables. */
   addStringListOption("CONTROLLING_VARIABLE_SOURCE_NAMES", n_control_vars, cv_source_names);
 
   /* DESCRIPTION: Names of the passive lookup variables for flamelet LUT */
diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index 0b3ebb0213d..bff408de8d0 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -172,7 +172,7 @@ void CLookUpTable::FindTableLimits(const string& name_cv1, const string& name_cv
   }
 
   if (table_dim == 3) {
-    limits_table_z = minmax_element(&z_values_levels[0], &z_values_levels[0] + z_values_levels.size());
+    limits_table_z = minmax_element(z_values_levels.data(), z_values_levels.data() + z_values_levels.size());
   }
 }
 
diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index ddf33ba9641..b888a104307 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -210,7 +210,7 @@ class CDataDrivenFluid final : public CFluidModel {
    * \brief Get fluid model extrapolation instance.
    * \return Query point lies outside fluid model data range.
    */
-  unsigned long GetExtrapolation() override { return outside_dataset; }
+  unsigned long GetExtrapolation() const override { return outside_dataset; }
 
   /*!
    * \brief Get number of Newton solver iterations.
diff --git a/SU2_CFD/include/fluid/CFluidFlamelet.hpp b/SU2_CFD/include/fluid/CFluidFlamelet.hpp
index c758887a35b..c9e15e5ed4b 100644
--- a/SU2_CFD/include/fluid/CFluidFlamelet.hpp
+++ b/SU2_CFD/include/fluid/CFluidFlamelet.hpp
@@ -44,16 +44,15 @@ class CFluidFlamelet final : public CFluidModel {
 
   int rank;
 
-  bool include_mixture_fraction = false; /*!< \brief include mixture fraction in controlling variables. */ 
+  bool include_mixture_fraction = false; /*!< \brief include mixture fraction in controlling variables. */
 
   unsigned short n_scalars, n_lookups, n_user_scalars, /*!< \brief number of passive reactant species. */
       n_control_vars;                                  /*!< \brief number of controlling variables. */
 
   unsigned long extrapolation;
-  
+
   INC_DENSITYMODEL density_model;
-  vector<string> controlling_variable_names,
-                 passive_specie_names;
+  vector<string> controlling_variable_names, passive_specie_names;
   vector<string> table_scalar_names; /*!< \brief vector to store names of scalar variables.   */
 
   su2double mass_diffusivity, /*!< \brief local mass diffusivity of the mixture */
@@ -64,22 +63,20 @@ class CFluidFlamelet final : public CFluidModel {
   /*--- Class variables for the multi-layer perceptron method ---*/
 #ifdef USE_MLPCPP
   MLPToolbox::CLookUp_ANN* lookup_mlp; /*!< \brief Multi-layer perceptron collection. */
-  MLPToolbox::CIOMap* iomap_TD;      /*!< \brief Input-output map for thermochemical properties. */
-  MLPToolbox::CIOMap* iomap_Sources; /*!< \brief Input-output map for species source terms. */
-  MLPToolbox::CIOMap* iomap_LookUp;  /*!< \brief Input-output map for passive look-up terms. */
+  MLPToolbox::CIOMap* iomap_TD;        /*!< \brief Input-output map for thermochemical properties. */
+  MLPToolbox::CIOMap* iomap_Sources;   /*!< \brief Input-output map for species source terms. */
+  MLPToolbox::CIOMap* iomap_LookUp;    /*!< \brief Input-output map for passive look-up terms. */
   MLPToolbox::CIOMap* iomap_Current;
 #endif
 
   vector<su2double> scalars_vector;
 
   vector<string> varnames_TD, /*!< \brief Lookup names for thermodynamic state variables. */
-                 varnames_Sources,
-                 varnames_LookUp;
+      varnames_Sources, varnames_LookUp;
 
   vector<su2double> val_vars_TD, /*!< \brief References to thermodynamic state variables. */
-                    val_vars_Sources,
-                    val_vars_LookUp;
-  
+      val_vars_Sources, val_vars_LookUp;
+
   void PreprocessLookUp(CConfig* config);
 
  public:
@@ -101,13 +98,14 @@ class CFluidFlamelet final : public CFluidModel {
    * \param[in] output_refs - output data.
    * \param[out] Extrapolation - scalar solution is within bounds (0) or out of bounds (1).
    */
-  inline unsigned long EvaluateDataSet(vector<su2double> &input_scalar, unsigned short lookup_type, vector<su2double> &output_refs) override;
+  inline unsigned long EvaluateDataSet(vector<su2double>& input_scalar, unsigned short lookup_type,
+                                       vector<su2double>& output_refs) override;
 
   /*!
    * \brief Check for out-of-bounds condition for data set interpolation.
    * \return - within bounds (0) or out of bounds (1).
    */
-  unsigned long GetExtrapolation() override { return extrapolation; }
+  unsigned long GetExtrapolation() const override { return extrapolation; }
 
   /*!
    * \brief Get the mass diffusivity of the species.
diff --git a/SU2_CFD/include/fluid/CFluidModel.hpp b/SU2_CFD/include/fluid/CFluidModel.hpp
index 77d7c314e37..b18f55c6a51 100644
--- a/SU2_CFD/include/fluid/CFluidModel.hpp
+++ b/SU2_CFD/include/fluid/CFluidModel.hpp
@@ -342,7 +342,7 @@ class CFluidModel {
    * \brief Get fluid model extrapolation instance
    * \return Query point lies outside fluid model data range.
    */
-  virtual unsigned long GetExtrapolation() { return 0; }
+  virtual unsigned long GetExtrapolation() const { return 0; }
 
   /*!
    * \brief Get number of Newton solver iterations.
diff --git a/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp b/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp
index b0727e4e242..62f379cafe6 100644
--- a/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp
+++ b/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp
@@ -72,7 +72,8 @@ class CSpeciesFlameletSolver final : public CSpeciesSolver {
    * \param[in] scalar_solution - local scalar solution.
    * \param[out] Converged - 0 if Newton solver converged, 1 if not.
    */
-  unsigned long GetEnthFromTemp(CFluidModel * fluid_model, su2double const val_temp, su2double * val_enth, const su2double * scalar_solution);
+  unsigned long GetEnthFromTemp(CFluidModel* fluid_model, su2double const val_temp, su2double* val_enth,
+                                const su2double* scalar_solution);
 
   /*!
    * \brief Find maximum progress variable value within the manifold for the current solution.
@@ -80,7 +81,7 @@ class CSpeciesFlameletSolver final : public CSpeciesSolver {
    * \param[in] scalars - local scalar solution.
    * \return - maximum progress variable value within manifold bounds.
    */
-  su2double GetBurntProgressVariable(CFluidModel * fluid_model, const su2double * scalars);
+  su2double GetBurntProgressVariable(CFluidModel* fluid_model, const su2double* scalars);
 
   /*!
    * \brief Retrieve scalar source terms from manifold.
@@ -91,7 +92,8 @@ class CSpeciesFlameletSolver final : public CSpeciesSolver {
    * \param[in] table_source_names - variable names of scalar source terms.
    * \return - within manifold bounds (0) or outside manifold bounds (1).
    */
-  unsigned long SetScalarSources(CConfig *config, CFluidModel *fluid_model_local, unsigned long iPoint, vector<su2double> &scalars);
+  unsigned long SetScalarSources(const CConfig* config, CFluidModel* fluid_model_local, unsigned long iPoint,
+                                 vector<su2double>& scalars);
 
   /*!
    * \brief Retrieve passive look-up data from manifold.
@@ -99,10 +101,10 @@ class CSpeciesFlameletSolver final : public CSpeciesSolver {
    * \param[in] fluid_model_local - pointer to flamelet fluid model.
    * \param[in] iPoint - node ID.
    * \param[in] scalars - local scalar solution.
-   * \param[in] table_lookup_names - variable names of scalar source terms.
    * \return - within manifold bounds (0) or outside manifold bounds (1).
    */
-  unsigned long SetScalarLookUps(CConfig *config, CFluidModel *fluid_model_local, unsigned long iPoint, vector<su2double> &scalars);
+  unsigned long SetScalarLookUps(const CConfig* config, CFluidModel* fluid_model_local, unsigned long iPoint,
+                                 vector<su2double>& scalars);
 
  public:
   /*!
diff --git a/SU2_CFD/src/fluid/CFluidFlamelet.cpp b/SU2_CFD/src/fluid/CFluidFlamelet.cpp
index 471c22fe1a4..a3806d7867d 100644
--- a/SU2_CFD/src/fluid/CFluidFlamelet.cpp
+++ b/SU2_CFD/src/fluid/CFluidFlamelet.cpp
@@ -51,69 +51,65 @@ CFluidFlamelet::CFluidFlamelet(CConfig* config, su2double value_pressure_operati
   scalars_vector.resize(n_scalars);
 
   table_scalar_names.resize(n_scalars);
-  for (auto iCV=0u; iCV<n_control_vars; iCV++)
-    table_scalar_names[iCV] = config->GetControllingVariableName(iCV);
-  
+  for (auto iCV = 0u; iCV < n_control_vars; iCV++) table_scalar_names[iCV] = config->GetControllingVariableName(iCV);
+
   /*--- auxiliary species transport equations---*/
   for (size_t i_aux = 0; i_aux < n_user_scalars; i_aux++) {
     table_scalar_names[n_control_vars + i_aux] = config->GetUserScalarName(i_aux);
   }
 
   controlling_variable_names.resize(n_control_vars);
-  for (auto iCV=0u; iCV<n_control_vars; iCV++)
+  for (auto iCV = 0u; iCV < n_control_vars; iCV++)
     controlling_variable_names[iCV] = config->GetControllingVariableName(iCV);
-  
+
   passive_specie_names.resize(n_user_scalars);
-  for (auto i_aux=0u; i_aux < n_user_scalars; i_aux++) 
-    passive_specie_names[i_aux] = config->GetUserScalarName(i_aux);
-  
-  switch (Kind_DataDriven_Method)
-  {
-  case ENUM_DATADRIVEN_METHOD::LUT:
-    if (rank == MASTER_NODE) {
-      cout << "*****************************************" << endl;
-      cout << "***   initializing the lookup table   ***" << endl;
-      cout << "*****************************************" << endl;
-    }
-    look_up_table = new CLookUpTable(config->GetDataDriven_FileNames()[0], table_scalar_names[I_PROGVAR], table_scalar_names[I_ENTH]);
-    break;
-  default:
-    if (rank == MASTER_NODE) {
-      cout << "***********************************************" << endl;
-      cout << "*** initializing the multi-layer perceptron ***" << endl;
-      cout << "***********************************************" << endl;
-    }
+  for (auto i_aux = 0u; i_aux < n_user_scalars; i_aux++) passive_specie_names[i_aux] = config->GetUserScalarName(i_aux);
+
+  switch (Kind_DataDriven_Method) {
+    case ENUM_DATADRIVEN_METHOD::LUT:
+      if (rank == MASTER_NODE) {
+        cout << "*****************************************" << endl;
+        cout << "***   initializing the lookup table   ***" << endl;
+        cout << "*****************************************" << endl;
+      }
+      look_up_table = new CLookUpTable(config->GetDataDriven_FileNames()[0], table_scalar_names[I_PROGVAR],
+                                       table_scalar_names[I_ENTH]);
+      break;
+    default:
+      if (rank == MASTER_NODE) {
+        cout << "***********************************************" << endl;
+        cout << "*** initializing the multi-layer perceptron ***" << endl;
+        cout << "***********************************************" << endl;
+      }
 #ifdef USE_MLPCPP
       lookup_mlp = new MLPToolbox::CLookUp_ANN(config->GetNDataDriven_Files(), config->GetDataDriven_FileNames());
       if ((rank == MASTER_NODE)) lookup_mlp->DisplayNetworkInfo();
 #else
       SU2_MPI::Error("SU2 was not compiled with MLPCpp enabled (-Denable-mlpcpp=true).", CURRENT_FUNCTION);
 #endif
-    break;
+      break;
   }
-  
+
   Pressure = value_pressure_operating;
 
   PreprocessLookUp(config);
- 
 }
 
-CFluidFlamelet::~CFluidFlamelet() { 
-  switch (Kind_DataDriven_Method)
-  {
-  case ENUM_DATADRIVEN_METHOD::LUT:
-    delete look_up_table; 
-    break;
-  case ENUM_DATADRIVEN_METHOD::MLP:
+CFluidFlamelet::~CFluidFlamelet() {
+  switch (Kind_DataDriven_Method) {
+    case ENUM_DATADRIVEN_METHOD::LUT:
+      delete look_up_table;
+      break;
+    case ENUM_DATADRIVEN_METHOD::MLP:
 #ifdef USE_MLPCPP
-    delete iomap_TD;
-    delete iomap_Sources;
-    delete iomap_LookUp;
-    delete lookup_mlp;
+      delete iomap_TD;
+      delete iomap_Sources;
+      delete iomap_LookUp;
+      delete lookup_mlp;
 #endif
-    break;
-  default:
-    break;
+      break;
+    default:
+      break;
   }
 }
 
@@ -128,27 +124,25 @@ void CFluidFlamelet::SetTDState_T(su2double val_temperature, const su2double* va
   Mu = val_vars_TD[LOOKUP_TD::VISCOSITY];
   Kt = val_vars_TD[LOOKUP_TD::CONDUCTIVITY];
   mass_diffusivity = val_vars_TD[LOOKUP_TD::DIFFUSIONCOEFFICIENT];
-  switch (density_model)
-  {
+  switch (density_model) {
     case INC_DENSITYMODEL::FLAMELET:
       Density = val_vars_TD[LOOKUP_TD::MOLARWEIGHT];
       molar_weight = Pressure / (Density * UNIVERSAL_GAS_CONSTANT * Temperature);
       break;
     case INC_DENSITYMODEL::VARIABLE:
       molar_weight = val_vars_TD[LOOKUP_TD::MOLARWEIGHT];
-      Density = (molar_weight / 1000) *  Pressure / ( UNIVERSAL_GAS_CONSTANT * Temperature);
+      Density = (molar_weight / 1000) * Pressure / (UNIVERSAL_GAS_CONSTANT * Temperature);
       break;
     default:
       break;
   }
-    /*--- Compute Cv from Cp and molar weight of the mixture (ideal gas). ---*/
+  /*--- Compute Cv from Cp and molar weight of the mixture (ideal gas). ---*/
   Cv = Cp - UNIVERSAL_GAS_CONSTANT / molar_weight;
 }
 
 void CFluidFlamelet::PreprocessLookUp(CConfig* config) {
-
   density_model = config->GetKind_DensityModel();
-   /*--- Thermodynamic state variables and names. ---*/
+  /*--- Thermodynamic state variables and names. ---*/
   varnames_TD.resize(LOOKUP_TD::SIZE);
   val_vars_TD.resize(LOOKUP_TD::SIZE);
 
@@ -160,22 +154,21 @@ void CFluidFlamelet::PreprocessLookUp(CConfig* config) {
   varnames_TD[LOOKUP_TD::DIFFUSIONCOEFFICIENT] = "DiffusionCoefficient";
 
   /*--- In case of FLAMELET density model, the density is directly interpolated from the manifold.---*/
-  switch (density_model)
-  {
-  case INC_DENSITYMODEL::FLAMELET:
-    varnames_TD[LOOKUP_TD::MOLARWEIGHT] = "Density";
-    break;
-  case INC_DENSITYMODEL::VARIABLE:
-    varnames_TD[LOOKUP_TD::MOLARWEIGHT] = "MolarWeightMix";
-    break;
-  default:
-    break;
+  switch (density_model) {
+    case INC_DENSITYMODEL::FLAMELET:
+      varnames_TD[LOOKUP_TD::MOLARWEIGHT] = "Density";
+      break;
+    case INC_DENSITYMODEL::VARIABLE:
+      varnames_TD[LOOKUP_TD::MOLARWEIGHT] = "MolarWeightMix";
+      break;
+    default:
+      break;
   }
   /*--- Scalar source term variables and names. ---*/
-  size_t n_sources = n_control_vars + 2*n_user_scalars;
+  size_t n_sources = n_control_vars + 2 * n_user_scalars;
   varnames_Sources.resize(n_sources);
   val_vars_Sources.resize(n_sources);
-  for (auto iCV=0u; iCV<n_control_vars; iCV++)
+  for (auto iCV = 0u; iCV < n_control_vars; iCV++)
     varnames_Sources[iCV] = config->GetControllingVariableSourceName(iCV);
   /*--- No source term for enthalpy ---*/
 
@@ -192,8 +185,7 @@ void CFluidFlamelet::PreprocessLookUp(CConfig* config) {
   size_t n_lookups = config->GetNLookups();
   varnames_LookUp.resize(n_lookups);
   val_vars_LookUp.resize(n_lookups);
-  for (auto iLookup=0u; iLookup < n_lookups; iLookup++)
-    varnames_LookUp[iLookup] = config->GetLookupName(iLookup);
+  for (auto iLookup = 0u; iLookup < n_lookups; iLookup++) varnames_LookUp[iLookup] = config->GetLookupName(iLookup);
 
   if (Kind_DataDriven_Method == ENUM_DATADRIVEN_METHOD::MLP) {
 #ifdef USE_MLPCPP
@@ -207,61 +199,58 @@ void CFluidFlamelet::PreprocessLookUp(CConfig* config) {
   }
 }
 
-unsigned long CFluidFlamelet::EvaluateDataSet(vector<su2double> &input_scalar, unsigned short lookup_type, vector<su2double> &output_refs) {
+unsigned long CFluidFlamelet::EvaluateDataSet(vector<su2double>& input_scalar, unsigned short lookup_type,
+                                              vector<su2double>& output_refs) {
   su2double val_enth = input_scalar[I_ENTH];
   su2double val_prog = input_scalar[I_PROGVAR];
   su2double val_mixfrac = include_mixture_fraction ? input_scalar[I_MIXFRAC] : 0.0;
   vector<string> varnames;
   vector<su2double> val_vars;
   vector<su2double*> refs_vars;
-  switch (lookup_type)
-  {
-  case FLAMELET_LOOKUP_OPS::TD:
-    varnames = varnames_TD;
-  #ifdef USE_MLPCPP
-    iomap_Current = iomap_TD;
-  #endif
-    break;
-  case FLAMELET_LOOKUP_OPS::SOURCES:
-    varnames = varnames_Sources;
-  #ifdef USE_MLPCPP
-    iomap_Current = iomap_Sources;
-  #endif
-    break;
-  case FLAMELET_LOOKUP_OPS::LOOKUP:
-    varnames = varnames_LookUp;
-  #ifdef USE_MLPCPP
-    iomap_Current = iomap_LookUp;
-  #endif
-    break;
-  default:
-    break;
+  switch (lookup_type) {
+    case FLAMELET_LOOKUP_OPS::TD:
+      varnames = varnames_TD;
+#ifdef USE_MLPCPP
+      iomap_Current = iomap_TD;
+#endif
+      break;
+    case FLAMELET_LOOKUP_OPS::SOURCES:
+      varnames = varnames_Sources;
+#ifdef USE_MLPCPP
+      iomap_Current = iomap_Sources;
+#endif
+      break;
+    case FLAMELET_LOOKUP_OPS::LOOKUP:
+      varnames = varnames_LookUp;
+#ifdef USE_MLPCPP
+      iomap_Current = iomap_LookUp;
+#endif
+      break;
+    default:
+      break;
   }
   if (output_refs.size() != varnames.size())
     SU2_MPI::Error(string("Output vector size incompatible with manifold lookup operation."), CURRENT_FUNCTION);
 
   /*--- Add all quantities and their names to the look up vectors. ---*/
-  switch (Kind_DataDriven_Method)
-  {
-  case ENUM_DATADRIVEN_METHOD::LUT:
-    if (include_mixture_fraction) {
-      extrapolation = look_up_table->LookUp_XYZ(varnames, output_refs, val_prog, val_enth, val_mixfrac);
-    } else {
-      extrapolation = look_up_table->LookUp_XY(varnames, output_refs, val_prog, val_enth);
-    }
-    break;
-  case ENUM_DATADRIVEN_METHOD::MLP:
-    refs_vars.resize(output_refs.size());
-    for (auto iVar=0u; iVar<output_refs.size(); iVar++)
-      refs_vars[iVar] = &output_refs[iVar];
+  switch (Kind_DataDriven_Method) {
+    case ENUM_DATADRIVEN_METHOD::LUT:
+      if (include_mixture_fraction) {
+        extrapolation = look_up_table->LookUp_XYZ(varnames, output_refs, val_prog, val_enth, val_mixfrac);
+      } else {
+        extrapolation = look_up_table->LookUp_XY(varnames, output_refs, val_prog, val_enth);
+      }
+      break;
+    case ENUM_DATADRIVEN_METHOD::MLP:
+      refs_vars.resize(output_refs.size());
+      for (auto iVar = 0u; iVar < output_refs.size(); iVar++) refs_vars[iVar] = &output_refs[iVar];
 #ifdef USE_MLPCPP
-    extrapolation = lookup_mlp->PredictANN(iomap_Current, input_scalar, refs_vars);
+      extrapolation = lookup_mlp->PredictANN(iomap_Current, input_scalar, refs_vars);
 #endif
-    break;
-  default:
-    break;
+      break;
+    default:
+      break;
   }
-  
 
   return extrapolation;
 }
diff --git a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
index 8324eca6695..f48ac84a7e5 100644
--- a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
+++ b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
@@ -66,7 +66,7 @@ CSpeciesFlameletSolver::CSpeciesFlameletSolver(CGeometry* geometry, CConfig* con
 void CSpeciesFlameletSolver::Preprocessing(CGeometry* geometry, CSolver** solver_container, CConfig* config,
                                            unsigned short iMesh, unsigned short iRKStep,
                                            unsigned short RunTime_EqSystem, bool Output) {
-  unsigned long n_not_in_domain_local = 0, n_not_in_domain_global=0;
+  unsigned long n_not_in_domain_local = 0, n_not_in_domain_global = 0;
   vector<su2double> scalars_vector(nVar);
 
   auto* flowNodes = su2staticcast_p<CFlowVariable*>(solver_container[FLOW_SOL]->GetNodes());
@@ -126,11 +126,11 @@ void CSpeciesFlameletSolver::SetInitialCondition(CGeometry** geometry, CSolver**
     su2double enth_inlet = config->GetSpecies_Init()[I_ENTH];
 
     su2double prog_burnt = 0, prog_unburnt, point_loc;
-    su2double *scalar_init = new su2double[nVar];
+    su2double scalar_init[MAXNVAR];
 
     if (rank == MASTER_NODE) {
       cout << "initial condition: T = " << temp_inlet << endl;
-      for (auto iCV=0u; iCV < config->GetNControlVars(); iCV++) {
+      for (auto iCV = 0u; iCV < config->GetNControlVars(); iCV++) {
         const auto& cv_name = config->GetControllingVariableName(iCV);
         cout << "initial condition: " << cv_name << " = " << config->GetSpecies_Init()[iCV] << endl;
       }
@@ -145,8 +145,7 @@ void CSpeciesFlameletSolver::SetInitialCondition(CGeometry** geometry, CSolver**
     for (unsigned long i_mesh = 0; i_mesh <= config->GetnMGLevels(); i_mesh++) {
       fluid_model_local = solver_container[i_mesh][FLOW_SOL]->GetFluidModel();
 
-      for (auto iVar = 0u; iVar < nVar; iVar++)
-        scalar_init[iVar] = config->GetSpecies_Init()[iVar];
+      for (auto iVar = 0u; iVar < nVar; iVar++) scalar_init[iVar] = config->GetSpecies_Init()[iVar];
 
       /*--- Set enthalpy based on initial temperature and scalars. ---*/
       n_not_iterated_local += GetEnthFromTemp(fluid_model_local, temp_inlet, &enth_inlet, config->GetSpecies_Init());
@@ -238,8 +237,6 @@ void CSpeciesFlameletSolver::SetInitialCondition(CGeometry** geometry, CSolver**
         cout << " Initial condition: Number of points in which enthalpy could not be iterated: "
              << n_not_iterated_global << " !!!" << endl;
     }
-
-    delete [] scalar_init;
   }
 }
 
@@ -436,19 +433,18 @@ void CSpeciesFlameletSolver::BC_ConjugateHeat_Interface(CGeometry* geometry, CSo
   BC_Isothermal_Wall_Generic(geometry, solver_container, conv_numerics, nullptr, config, val_marker, true);
 }
 
-unsigned long CSpeciesFlameletSolver::SetScalarSources(CConfig* config, CFluidModel* fluid_model_local,
+unsigned long CSpeciesFlameletSolver::SetScalarSources(const CConfig* config, CFluidModel* fluid_model_local,
                                                        unsigned long iPoint, vector<su2double>& scalars) {
   /*--- Compute total source terms from the production and consumption. ---*/
 
-  vector<su2double> table_sources(config->GetNControlVars() + 2*config->GetNUserScalars());
+  vector<su2double> table_sources(config->GetNControlVars() + 2 * config->GetNUserScalars());
   unsigned long misses = fluid_model_local->EvaluateDataSet(scalars, FLAMELET_LOOKUP_OPS::SOURCES, table_sources);
   nodes->SetTableMisses(iPoint, misses);
 
   /*--- The source term for progress variable is always positive, we clip from below to makes sure. --- */
 
   vector<su2double> source_scalar(config->GetNScalars());
-  for (auto iCV=0u; iCV<config->GetNControlVars(); iCV++)
-    source_scalar[iCV] = table_sources[iCV];
+  for (auto iCV = 0u; iCV < config->GetNControlVars(); iCV++) source_scalar[iCV] = table_sources[iCV];
   source_scalar[I_PROGVAR] = fmax(EPS, source_scalar[I_PROGVAR]);
 
   /*--- Source term for the auxiliary species transport equations. ---*/
@@ -465,7 +461,7 @@ unsigned long CSpeciesFlameletSolver::SetScalarSources(CConfig* config, CFluidMo
   return misses;
 }
 
-unsigned long CSpeciesFlameletSolver::SetScalarLookUps(CConfig* config, CFluidModel* fluid_model_local,
+unsigned long CSpeciesFlameletSolver::SetScalarLookUps(const CConfig* config, CFluidModel* fluid_model_local,
                                                        unsigned long iPoint, vector<su2double>& scalars) {
   /*--- Compute total source terms from the production and consumption. ---*/
 
@@ -490,7 +486,7 @@ unsigned long CSpeciesFlameletSolver::GetEnthFromTemp(CFluidModel* fluid_model,
 
   int counter = 0;
 
-  su2double *val_scalars = new su2double[nVar];
+  su2double val_scalars[MAXNVAR];
   for (auto iVar = 0u; iVar < nVar; iVar++) val_scalars[iVar] = scalar_solution[iVar];
 
   while ((abs(delta_temp_iter) > delta_temp_final) && (counter++ < counter_limit)) {
@@ -507,7 +503,6 @@ unsigned long CSpeciesFlameletSolver::GetEnthFromTemp(CFluidModel* fluid_model,
 
     enth_iter += delta_enth;
   }
-  delete [] val_scalars;
 
   *val_enth = enth_iter;
 
@@ -519,8 +514,7 @@ unsigned long CSpeciesFlameletSolver::GetEnthFromTemp(CFluidModel* fluid_model,
 }
 
 su2double CSpeciesFlameletSolver::GetBurntProgressVariable(CFluidModel* fluid_model, const su2double* scalar_solution) {
-  su2double *scalars = new su2double[nVar],
-            delta = 1e-3;
+  su2double scalars[MAXNVAR], delta = 1e-3;
   for (auto iVar = 0u; iVar < nVar; iVar++) scalars[iVar] = scalar_solution[iVar];
 
   bool outside = false;
@@ -530,6 +524,5 @@ su2double CSpeciesFlameletSolver::GetBurntProgressVariable(CFluidModel* fluid_mo
     scalars[I_PROGVAR] += delta;
   }
   su2double pv_burnt = scalars[I_PROGVAR] - delta;
-  delete [] scalars;
   return pv_burnt;
 }
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 90618d8cebb..a5309e5fb86 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -65,7 +65,7 @@ def main():
     cfd_flamelet_ch4_partial_premix.cfg_dir = "flamelet/06_laminar_partial_premixed_ch4_flame_cfd"
     cfd_flamelet_ch4_partial_premix.cfg_file = "lam_partial_prem_ch4_cfd.cfg"
     cfd_flamelet_ch4_partial_premix.test_iter = 10
-    cfd_flamelet_ch4_partial_premix.test_vals = [-9.408381, -9.414935, -2.684728, -11.330306, -9.310217]
+    cfd_flamelet_ch4_partial_premix.test_vals = [-10.070242, -11.294887, -4.651523, -13.155604, -11.083940]
     cfd_flamelet_ch4_partial_premix.new_output = True
     test_list.append(cfd_flamelet_ch4_partial_premix)
 

From dffa192d4b9080072e6e40362d3321eccad4dc0e Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Mon, 17 Jul 2023 15:46:12 +0200
Subject: [PATCH 599/656] Implemented comments from reviewers

---
 SU2_CFD/include/fluid/CFluidFlamelet.hpp      |  2 +-
 SU2_CFD/include/fluid/CFluidModel.hpp         |  2 +-
 .../solvers/CSpeciesFlameletSolver.hpp        | 40 ++-----------------
 SU2_CFD/src/fluid/CFluidFlamelet.cpp          |  2 +-
 .../src/solvers/CSpeciesFlameletSolver.cpp    | 13 +++---
 meson_scripts/init.py                         |  2 +-
 subprojects/MLPCpp                            |  2 +-
 7 files changed, 16 insertions(+), 47 deletions(-)

diff --git a/SU2_CFD/include/fluid/CFluidFlamelet.hpp b/SU2_CFD/include/fluid/CFluidFlamelet.hpp
index c9e15e5ed4b..929146baa30 100644
--- a/SU2_CFD/include/fluid/CFluidFlamelet.hpp
+++ b/SU2_CFD/include/fluid/CFluidFlamelet.hpp
@@ -98,7 +98,7 @@ class CFluidFlamelet final : public CFluidModel {
    * \param[in] output_refs - output data.
    * \param[out] Extrapolation - scalar solution is within bounds (0) or out of bounds (1).
    */
-  inline unsigned long EvaluateDataSet(vector<su2double>& input_scalar, unsigned short lookup_type,
+  inline unsigned long EvaluateDataSet(const vector<su2double>& input_scalar, unsigned short lookup_type,
                                        vector<su2double>& output_refs) override;
 
   /*!
diff --git a/SU2_CFD/include/fluid/CFluidModel.hpp b/SU2_CFD/include/fluid/CFluidModel.hpp
index b18f55c6a51..aa7131f468e 100644
--- a/SU2_CFD/include/fluid/CFluidModel.hpp
+++ b/SU2_CFD/include/fluid/CFluidModel.hpp
@@ -147,7 +147,7 @@ class CFluidModel {
    * \brief Evaluate data manifold for flamelet or data-driven fluid problems.
    * \param[in] input - input data for manifold regression.
    */
-  virtual unsigned long EvaluateDataSet(vector<su2double> &input_scalar, unsigned short lookup_type, vector<su2double> &output_refs) { return 0; }
+  virtual unsigned long EvaluateDataSet(const vector<su2double> &input_scalar, unsigned short lookup_type, vector<su2double> &output_refs) { return 0; }
 
   /*!
    * \brief Get fluid dynamic viscosity.
diff --git a/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp b/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp
index 62f379cafe6..ba1661191cd 100644
--- a/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp
+++ b/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file CSpeciesFlameletSolver.hpp
  * \brief Headers of the CSpeciesFlameletSolver class
- * \author D. Mayer, N. Beishuizen, T. Economon
+ * \author D. Mayer, N. Beishuizen, T. Economon, E. Bunschoten
  * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
@@ -47,15 +47,6 @@ class CSpeciesFlameletSolver final : public CSpeciesSolver {
    */
   void SetPreconditioner(CGeometry* geometry, CSolver** solver_container, CConfig* config);
 
-  /*!
-   * \brief Compute the primitive variables (diffusivities).
-   * \param[in] solver_container - Container vector with all the solutions.
-   * \param[in] config - Definition of the particular problem.
-   * \param[in] Output - Boolean to determine whether to print output.
-   * \return - The number of non-physical points.
-   */
-  unsigned long SetPrimitive_Variables(CSolver** solver_container, CConfig* config, bool Output);
-
   /*!
    * \brief Generic implementation of the isothermal wall also covering CHT cases,
    * for which the wall temperature is given by GetConjugateHeatVariable.
@@ -93,7 +84,7 @@ class CSpeciesFlameletSolver final : public CSpeciesSolver {
    * \return - within manifold bounds (0) or outside manifold bounds (1).
    */
   unsigned long SetScalarSources(const CConfig* config, CFluidModel* fluid_model_local, unsigned long iPoint,
-                                 vector<su2double>& scalars);
+                                 const vector<su2double>& scalars);
 
   /*!
    * \brief Retrieve passive look-up data from manifold.
@@ -104,7 +95,7 @@ class CSpeciesFlameletSolver final : public CSpeciesSolver {
    * \return - within manifold bounds (0) or outside manifold bounds (1).
    */
   unsigned long SetScalarLookUps(const CConfig* config, CFluidModel* fluid_model_local, unsigned long iPoint,
-                                 vector<su2double>& scalars);
+                                 const vector<su2double>& scalars);
 
  public:
   /*!
@@ -184,29 +175,4 @@ class CSpeciesFlameletSolver final : public CSpeciesSolver {
    */
   void BC_ConjugateHeat_Interface(CGeometry* geometry, CSolver** solver_container, CNumerics* numerics, CConfig* config,
                                   unsigned short val_marker) override;
-
-  /*!
-   * \brief Get the conjugate heat variables.
-   * \param[in] val_marker - The marker index.
-   * \param[in] val_vertex - The vertex index.
-   * \param[in] pos_var - The variable position (in vector of all conjugate heat variables).
-   */
-  inline su2double GetConjugateHeatVariable(unsigned short val_marker, unsigned long val_vertex,
-                                            unsigned short pos_var) const override {
-    return conjugate_var[val_marker][val_vertex][pos_var];
-  }
-
-  /*!
-   * \brief Set the conjugate heat variables.
-   * \param[in] val_marker - The marker index.
-   * \param[in] val_vertex - The vertex index.
-   * \param[in] pos_var - The variable position (in vector of all conjugate heat variables).
-   * \param[in] relaxation_factor - The relaxation factor for the change of the variables.
-   * \param[in] val_var - The value of the variable.
-   */
-  inline void SetConjugateHeatVariable(unsigned short val_marker, unsigned long val_vertex, unsigned short pos_var,
-                                       su2double relaxation_factor, su2double val_var) override {
-    conjugate_var[val_marker][val_vertex][pos_var] =
-        relaxation_factor * val_var + (1.0 - relaxation_factor) * conjugate_var[val_marker][val_vertex][pos_var];
-  }
 };
diff --git a/SU2_CFD/src/fluid/CFluidFlamelet.cpp b/SU2_CFD/src/fluid/CFluidFlamelet.cpp
index a3806d7867d..f75a68700a5 100644
--- a/SU2_CFD/src/fluid/CFluidFlamelet.cpp
+++ b/SU2_CFD/src/fluid/CFluidFlamelet.cpp
@@ -199,7 +199,7 @@ void CFluidFlamelet::PreprocessLookUp(CConfig* config) {
   }
 }
 
-unsigned long CFluidFlamelet::EvaluateDataSet(vector<su2double>& input_scalar, unsigned short lookup_type,
+unsigned long CFluidFlamelet::EvaluateDataSet(const vector<su2double>& input_scalar, unsigned short lookup_type,
                                               vector<su2double>& output_refs) {
   su2double val_enth = input_scalar[I_ENTH];
   su2double val_prog = input_scalar[I_PROGVAR];
diff --git a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
index f48ac84a7e5..6e99e4eb568 100644
--- a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
+++ b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
@@ -1,7 +1,7 @@
 /*!
  * \file CSpeciesFlameletSolver.cpp
  * \brief Main subroutines of CSpeciesFlameletSolver class
- * \author D. Mayer, T. Economon, N. Beishuizen
+ * \author D. Mayer, T. Economon, N. Beishuizen, E. Bunschoten
  * \version 7.5.1 "Blackbird"
  *
  * SU2 Project Website: https://su2code.github.io
@@ -343,7 +343,7 @@ void CSpeciesFlameletSolver::BC_Isothermal_Wall_Generic(CGeometry* geometry, CSo
                                                         CConfig* config, unsigned short val_marker, bool cht_mode) {
   const bool implicit = config->GetKind_TimeIntScheme_Flow() == EULER_IMPLICIT;
   const string Marker_Tag = config->GetMarker_All_TagBound(val_marker);
-  su2double temp_wall = config->GetIsothermal_Temperature(Marker_Tag);
+  su2double temp_wall;
   CFluidModel* fluid_model_local = solver_container[FLOW_SOL]->GetFluidModel();
   auto* flowNodes = su2staticcast_p<CFlowVariable*>(solver_container[FLOW_SOL]->GetNodes());
   su2double enth_wall;
@@ -354,7 +354,10 @@ void CSpeciesFlameletSolver::BC_Isothermal_Wall_Generic(CGeometry* geometry, CSo
   for (unsigned long iVertex = 0; iVertex < geometry->nVertex[val_marker]; iVertex++) {
     unsigned long iPoint = geometry->vertex[val_marker][iVertex]->GetNode();
 
-    if (cht_mode) temp_wall = solver_container[FLOW_SOL]->GetConjugateHeatVariable(val_marker, iVertex, 0);
+    if (cht_mode)
+      temp_wall = solver_container[FLOW_SOL]->GetConjugateHeatVariable(val_marker, iVertex, 0);
+    else 
+      temp_wall = config->GetIsothermal_Temperature(Marker_Tag);
 
     /*--- Check if the node belongs to the domain (i.e., not a halo node). ---*/
 
@@ -434,7 +437,7 @@ void CSpeciesFlameletSolver::BC_ConjugateHeat_Interface(CGeometry* geometry, CSo
 }
 
 unsigned long CSpeciesFlameletSolver::SetScalarSources(const CConfig* config, CFluidModel* fluid_model_local,
-                                                       unsigned long iPoint, vector<su2double>& scalars) {
+                                                       unsigned long iPoint, const vector<su2double>& scalars) {
   /*--- Compute total source terms from the production and consumption. ---*/
 
   vector<su2double> table_sources(config->GetNControlVars() + 2 * config->GetNUserScalars());
@@ -462,7 +465,7 @@ unsigned long CSpeciesFlameletSolver::SetScalarSources(const CConfig* config, CF
 }
 
 unsigned long CSpeciesFlameletSolver::SetScalarLookUps(const CConfig* config, CFluidModel* fluid_model_local,
-                                                       unsigned long iPoint, vector<su2double>& scalars) {
+                                                       unsigned long iPoint, const vector<su2double>& scalars) {
   /*--- Compute total source terms from the production and consumption. ---*/
 
   vector<su2double> lookup_scalar(config->GetNLookups());
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 372e77bc228..7bf69d1afd6 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -71,7 +71,7 @@ def init_submodules(
     github_repo_coolprop = "https://github.com/CoolProp/CoolProp"
     sha_version_mel = "2484cd3258ef800a10e361016cb341834ee7930b"
     github_repo_mel = "https://github.com/pcarruscag/MEL"
-    sha_version_mlpcpp = "a80115c6f4779cc168d1464cf32aead61559c9ea"
+    sha_version_mlpcpp = "665c45b7d3533c977eb1f637918d5b8b75c07d3b"
     github_repo_mlpcpp = "https://github.com/EvertBunschoten/MLPCpp"
 
     medi_name = "MeDiPack"
diff --git a/subprojects/MLPCpp b/subprojects/MLPCpp
index a80115c6f47..665c45b7d35 160000
--- a/subprojects/MLPCpp
+++ b/subprojects/MLPCpp
@@ -1 +1 @@
-Subproject commit a80115c6f4779cc168d1464cf32aead61559c9ea
+Subproject commit 665c45b7d3533c977eb1f637918d5b8b75c07d3b

From 6d965b9dbae0607a72e6156edaebb44452c228d6 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 17 Jul 2023 16:17:06 +0200
Subject: [PATCH 600/656] Introduce a thread-sanitizer dependent loop macro.

---
 Common/src/geometry/CPhysicalGeometry.cpp | 24 +++++++++++++----------
 su2omp.syntax.json                        |  3 ++-
 2 files changed, 16 insertions(+), 11 deletions(-)

diff --git a/Common/src/geometry/CPhysicalGeometry.cpp b/Common/src/geometry/CPhysicalGeometry.cpp
index 36f257b238a..917894f4bf3 100644
--- a/Common/src/geometry/CPhysicalGeometry.cpp
+++ b/Common/src/geometry/CPhysicalGeometry.cpp
@@ -10565,6 +10565,15 @@ std::unique_ptr<CADTElemClass> CPhysicalGeometry::ComputeViscousWallADT(const CC
   return WallADT;
 }
 
+/*--- Use a thread-sanitizer dependent loop schedule to work around suspected false positives ---*/
+#ifndef __SANITIZE_THREAD__
+#define CPHYSGEO_PARFOR SU2_OMP_FOR_DYN(roundUpDiv(nPoint, 2 * omp_get_max_threads()))
+#else
+#define CPHYSGEO_PARFOR SU2_OMP_FOR_()
+#endif
+
+#define END_CPHYSGEO_PARFOR END_SU2_OMP_FOR
+
 void CPhysicalGeometry::SetWallDistance(CADTElemClass* WallADT, const CConfig* config, unsigned short iZone) {
   /*--------------------------------------------------------------------------*/
   /*--- Step 3: Loop over all interior mesh nodes and compute minimum      ---*/
@@ -10576,11 +10585,7 @@ void CPhysicalGeometry::SetWallDistance(CADTElemClass* WallADT, const CConfig* c
      distance for all nodes. ---*/
 
     SU2_OMP_PARALLEL {
-#ifndef __SANITIZE_THREAD__
-      SU2_OMP_FOR_DYN(roundUpDiv(nPoint, 2 * omp_get_max_threads()))
-#else
-      SU2_OMP_FOR_()
-#endif
+      CPHYSGEO_PARFOR
       for (unsigned long iPoint = 0; iPoint < GetnPoint(); ++iPoint) {
         unsigned short markerID;
         unsigned long elemID;
@@ -10593,12 +10598,11 @@ void CPhysicalGeometry::SetWallDistance(CADTElemClass* WallADT, const CConfig* c
           nodes->SetWall_Distance(iPoint, dist, rankID, iZone, markerID, elemID);
         }
       }
-#ifndef __SANITIZE_THREAD__
-      END_SU2_OMP_FOR
-#else
-      END_SU2_OMP_FOR
-#endif
+      END_CPHYSGEO_PARFOR
     }
     END_SU2_OMP_PARALLEL
   }
 }
+
+#undef CPHYSGEO_PARFOR
+#undef END_CPHYSGEO_PARFOR
diff --git a/su2omp.syntax.json b/su2omp.syntax.json
index dc853982da1..28e22388ccc 100644
--- a/su2omp.syntax.json
+++ b/su2omp.syntax.json
@@ -38,6 +38,7 @@
     "SU2_OMP_FOR_STAT": "END_SU2_OMP_FOR",
     "CSYSVEC_PARFOR": "END_CSYSVEC_PARFOR",
     "CNEWTON_PARFOR": "END_CNEWTON_PARFOR",
-    "BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS": "END_SU2_OMP_SAFE_GLOBAL_ACCESS"
+    "BEGIN_SU2_OMP_SAFE_GLOBAL_ACCESS": "END_SU2_OMP_SAFE_GLOBAL_ACCESS",
+    "CPHYSGEO_PARFOR": "END_CPHYSGEO_PARFOR"
   }
 }

From 9facc2623bbcc29a81daa56962b1314952000fd1 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 17 Jul 2023 16:31:14 +0200
Subject: [PATCH 601/656] Default to two iterations with the thread sanitizer.

---
 TestCases/TestCase.py | 15 ++++++++++-----
 1 file changed, 10 insertions(+), 5 deletions(-)

diff --git a/TestCases/TestCase.py b/TestCases/TestCase.py
index 757c0520a50..90f2de2e926 100644
--- a/TestCases/TestCase.py
+++ b/TestCases/TestCase.py
@@ -142,7 +142,7 @@ def run_test(self, running_with_tsan=False):
 
         # Adjust the number of iterations in the config file
         if len(self.test_vals) != 0:
-            self.adjust_iter()
+            self.adjust_iter(running_with_tsan)
 
         # Check for disabling the restart
         if self.no_restart:
@@ -291,7 +291,7 @@ def run_filediff(self, running_with_tsan=False):
         timed_out    = False
 
         # Adjust the number of iterations in the config file
-        self.adjust_iter()
+        self.adjust_iter(running_with_tsan)
 
         self.adjust_test_data()
 
@@ -850,7 +850,12 @@ def run_def(self):
         os.chdir(workdir)
         return passed
 
-    def adjust_iter(self):
+    def adjust_iter(self, running_with_tsan=False):
+
+        if not running_with_tsan:
+          new_iter = self.test_iter + 1
+        else:
+          new_iter = 2
 
         # Read the cfg file
         workdir = os.getcwd()
@@ -863,7 +868,7 @@ def adjust_iter(self):
         self.cfg_file = "%s.autotest"%self.cfg_file
         file_out = open(self.cfg_file,'w')
         file_out.write('% This file automatically generated by the regression script\n')
-        file_out.write('%% Number of iterations changed to %d\n'%(self.test_iter+1))
+        file_out.write('%% Number of iterations changed to %d\n'%(new_iter))
         if (self.multizone or self.new_output) and self.unsteady:
             adjust_string = "TIME_ITER"
         elif self.multizone:
@@ -874,7 +879,7 @@ def adjust_iter(self):
             if not line.strip().split("=")[0].strip() == adjust_string:
                 file_out.write(line)
             else:
-                file_out.write(adjust_string+"=%d\n"%(self.test_iter+1))
+                file_out.write(adjust_string+"=%d\n"%(new_iter))
         file_out.close()
         os.chdir(workdir)
 

From 063ddf2dc859795dabc277fd9bbf58c7510fa538 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 17 Jul 2023 16:49:57 +0200
Subject: [PATCH 602/656] Ensure that the number of iterations does not
 increase.

---
 TestCases/TestCase.py | 5 ++---
 1 file changed, 2 insertions(+), 3 deletions(-)

diff --git a/TestCases/TestCase.py b/TestCases/TestCase.py
index 90f2de2e926..51f588838c2 100644
--- a/TestCases/TestCase.py
+++ b/TestCases/TestCase.py
@@ -852,9 +852,8 @@ def run_def(self):
 
     def adjust_iter(self, running_with_tsan=False):
 
-        if not running_with_tsan:
-          new_iter = self.test_iter + 1
-        else:
+        new_iter = self.test_iter + 1
+        if running_with_tsan and new_iter > 2:
           new_iter = 2
 
         # Read the cfg file

From abc6ea3e266cdeca6086406a1070bf0af966e709 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Mon, 17 Jul 2023 08:08:39 -0700
Subject: [PATCH 603/656] cannot have extra ; so disable clang-format in
 section

---
 .../linear_algebra/vector_expressions.hpp     | 46 ++++++++++---------
 1 file changed, 24 insertions(+), 22 deletions(-)

diff --git a/Common/include/linear_algebra/vector_expressions.hpp b/Common/include/linear_algebra/vector_expressions.hpp
index b958411b0ba..e7883c4b5c7 100644
--- a/Common/include/linear_algebra/vector_expressions.hpp
+++ b/Common/include/linear_algebra/vector_expressions.hpp
@@ -146,28 +146,30 @@ MAKE_UNARY_FUN(sign, sign_, sign_impl)
 
 /*--- Macro to create expressions and overloads for binary functions. ---*/
 
-#define MAKE_BINARY_FUN(FUN, EXPR, IMPL)                                                                               \
-  /*!--- Expression class. ---*/                                                                                       \
-  template <class U, class V, class Scalar>                                                                            \
-  class EXPR : public CVecExpr<EXPR<U, V, Scalar>, Scalar> {                                                           \
-    store_t<const U> u;                                                                                                \
-    store_t<const V> v;                                                                                                \
-                                                                                                                       \
-   public:                                                                                                             \
-    static constexpr bool StoreAsRef = false;                                                                          \
-    FORCEINLINE EXPR(const U& u_, const V& v_) : u(u_), v(v_) {}                                                       \
-    FORCEINLINE auto operator[](size_t i) const RETURNS(IMPL(u[i], v[i]))                                              \
-  };                                                                                                                   \
-  /*!--- Vector with vector function overload. ---*/                                                                   \
-  template <class U, class V, class S>                                                                                 \
-  FORCEINLINE auto FUN(const CVecExpr<U, S>& u, const CVecExpr<V, S>& v)                                               \
-      RETURNS(EXPR<U, V, S>(u.derived(), v.derived()));                                                                \
-  /*!--- Vector with scalar function overload. ---*/                                                                   \
-  template <class U, class S>                                                                                          \
-  FORCEINLINE auto FUN(const CVecExpr<U, S>& u, decay_t<S> v) RETURNS(EXPR<U, Bcast<S>, S>(u.derived(), Bcast<S>(v))); \
-  /*!--- Scalar with vector function overload. ---*/                                                                   \
-  template <class S, class V>                                                                                          \
-  FORCEINLINE auto FUN(decay_t<S> u, const CVecExpr<V, S>& v) RETURNS(EXPR<Bcast<S>, V, S>(Bcast<S>(u), v.derived()));
+// clang-format off
+#define MAKE_BINARY_FUN(FUN, EXPR, IMPL)                                                                              \
+  /*!--- Expression class. ---*/                                                                                      \
+  template <class U, class V, class Scalar>                                                                           \
+  class EXPR : public CVecExpr<EXPR<U, V, Scalar>, Scalar> {                                                          \
+    store_t<const U> u;                                                                                               \
+    store_t<const V> v;                                                                                               \
+                                                                                                                      \
+   public:                                                                                                            \
+    static constexpr bool StoreAsRef = false;                                                                         \
+    FORCEINLINE EXPR(const U& u_, const V& v_) : u(u_), v(v_) {}                                                      \
+    FORCEINLINE auto operator[](size_t i) const RETURNS(IMPL(u[i], v[i]))                                             \
+  };                                                                                                                  \
+  /*!--- Vector with vector function overload. ---*/                                                                  \
+  template <class U, class V, class S>                                                                                \
+  FORCEINLINE auto FUN(const CVecExpr<U, S>& u, const CVecExpr<V, S>& v)                                              \
+      RETURNS(EXPR<U, V, S>(u.derived(), v.derived()))                                                                \
+  /*!--- Vector with scalar function overload. ---*/                                                                  \
+  template <class U, class S>                                                                                         \
+  FORCEINLINE auto FUN(const CVecExpr<U, S>& u, decay_t<S> v) RETURNS(EXPR<U, Bcast<S>, S>(u.derived(), Bcast<S>(v))) \
+  /*!--- Scalar with vector function overload. ---*/                                                                  \
+  template <class S, class V>                                                                                         \
+  FORCEINLINE auto FUN(decay_t<S> u, const CVecExpr<V, S>& v) RETURNS(EXPR<Bcast<S>, V, S>(Bcast<S>(u), v.derived()))
+// clang-format on
 
 /*--- std::max/min have issues (because they return by reference).
  * fmin and fmax return by value and thus are fine, but they would force

From b3e4bddc5a626db5ad602cfa9b269a011ca7a56c Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Vinzenz=20G=C3=B6tz?=
 <81287997+MastermindScope@users.noreply.github.com>
Date: Mon, 17 Jul 2023 18:12:28 +0200
Subject: [PATCH 604/656] Update CFlowCompOutput.cpp to reflect pcarruscag's
 suggestions

---
 SU2_CFD/src/output/CFlowCompOutput.cpp | 8 +++++---
 1 file changed, 5 insertions(+), 3 deletions(-)

diff --git a/SU2_CFD/src/output/CFlowCompOutput.cpp b/SU2_CFD/src/output/CFlowCompOutput.cpp
index 92c933c52df..30f93e70ea2 100644
--- a/SU2_CFD/src/output/CFlowCompOutput.cpp
+++ b/SU2_CFD/src/output/CFlowCompOutput.cpp
@@ -316,12 +316,9 @@ void CFlowCompOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolv
   SetVolumeOutputValue("DENSITY",    iPoint, Node_Flow->GetSolution(iPoint, 0));
   SetVolumeOutputValue("MOMENTUM-X", iPoint, Node_Flow->GetSolution(iPoint, 1));
   SetVolumeOutputValue("MOMENTUM-Y", iPoint, Node_Flow->GetSolution(iPoint, 2));
-  SetVolumeOutputValue("VELOCITY-X", iPoint, Node_Flow->GetPrimitive(iPoint, 1));
-  SetVolumeOutputValue("VELOCITY-Y", iPoint, Node_Flow->GetPrimitive(iPoint, 2));
   if (nDim == 3){
     SetVolumeOutputValue("MOMENTUM-Z", iPoint, Node_Flow->GetSolution(iPoint, 3));
     SetVolumeOutputValue("ENERGY",     iPoint, Node_Flow->GetSolution(iPoint, 4));
-    SetVolumeOutputValue("VELOCITY-Z", iPoint, Node_Flow->GetPrimitive(iPoint, 3));
   } else {
     SetVolumeOutputValue("ENERGY",     iPoint, Node_Flow->GetSolution(iPoint, 3));
   }
@@ -339,6 +336,11 @@ void CFlowCompOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolv
 
   const su2double factor = solver[FLOW_SOL]->GetReferenceDynamicPressure();
   SetVolumeOutputValue("PRESSURE_COEFF", iPoint, (Node_Flow->GetPressure(iPoint) - solver[FLOW_SOL]->GetPressure_Inf())/factor);
+  SetVolumeOutputValue("VELOCITY-X", iPoint, Node_Flow->GetVelocity(iPoint, 0));
+  SetVolumeOutputValue("VELOCITY-Y", iPoint, Node_Flow->GetVelocity(iPoint, 1));
+  if (nDim == 3){
+    SetVolumeOutputValue("VELOCITY-Z", iPoint, Node_Flow->GetVelocity(iPoint, 2));
+  }
 
   if(config->GetKind_FluidModel() == DATADRIVEN_FLUID){
     SetVolumeOutputValue("EXTRAPOLATION", iPoint, Node_Flow->GetDataExtrapolation(iPoint));

From 88f474fcaa6922ee3a76750417b0e09c8a9b0b8d Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 17 Jul 2023 18:51:49 +0200
Subject: [PATCH 605/656] Regard restart iter.

---
 TestCases/TestCase.py | 18 ++++++++++++++----
 1 file changed, 14 insertions(+), 4 deletions(-)

diff --git a/TestCases/TestCase.py b/TestCases/TestCase.py
index 51f588838c2..0d0b39d735a 100644
--- a/TestCases/TestCase.py
+++ b/TestCases/TestCase.py
@@ -852,10 +852,6 @@ def run_def(self):
 
     def adjust_iter(self, running_with_tsan=False):
 
-        new_iter = self.test_iter + 1
-        if running_with_tsan and new_iter > 2:
-          new_iter = 2
-
         # Read the cfg file
         workdir = os.getcwd()
         os.chdir(self.cfg_dir)
@@ -863,6 +859,20 @@ def adjust_iter(self, running_with_tsan=False):
         lines   = file_in.readlines()
         file_in.close()
 
+        new_iter = self.test_iter + 1
+
+        if running_with_tsan:
+
+          # detect restart
+          restart_iter = 0
+          for line in lines:
+              if line.strip().split("=")[0].strip() == "RESTART_ITER":
+                  restart_iter = int(line.strip().split("=")[1].strip())
+                  break
+
+          if  new_iter > restart_iter + 2:
+            new_iter = restart_iter + 2
+
         # Rewrite the file with a .autotest extension
         self.cfg_file = "%s.autotest"%self.cfg_file
         file_out = open(self.cfg_file,'w')

From eca634b0e8224833fa123de6217b7e3aa02a5cf0 Mon Sep 17 00:00:00 2001
From: Liang <106984354+lcheng9@users.noreply.github.com>
Date: Mon, 17 Jul 2023 20:36:24 -0400
Subject: [PATCH 606/656] Revise the header file path

---
 SU2_GEO/include/SU2_GEO.hpp | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/SU2_GEO/include/SU2_GEO.hpp b/SU2_GEO/include/SU2_GEO.hpp
index 9752149364e..4e5b8354f59 100644
--- a/SU2_GEO/include/SU2_GEO.hpp
+++ b/SU2_GEO/include/SU2_GEO.hpp
@@ -38,7 +38,7 @@
 
 #include "../../Common/include/geometry/CPhysicalGeometry.hpp"
 #include "../../Common/include/CConfig.hpp"
-#include "../../../Common/include/grid_movement/CSurfaceMovement.hpp"
-#include "../../../Common/include/grid_movement/CFreeFormDefBox.hpp"
+#include "../../Common/include/grid_movement/CSurfaceMovement.hpp"
+#include "../../Common/include/grid_movement/CFreeFormDefBox.hpp"
 
 using namespace std;

From c6931d7714f2b51dc699ce4bb0b53ef83e8674c7 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Tue, 18 Jul 2023 17:20:02 +0200
Subject: [PATCH 607/656] Update container image in release action.

---
 .github/workflows/release-management.yml | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/.github/workflows/release-management.yml b/.github/workflows/release-management.yml
index 46a618f9a6c..45bb698198f 100644
--- a/.github/workflows/release-management.yml
+++ b/.github/workflows/release-management.yml
@@ -35,7 +35,7 @@ jobs:
           key: ${{ matrix.os_bin }}-${{ github.sha }}
           restore-keys: ${{ matrix.os_bin }}
       - name: Build
-        uses: docker://ghcr.io/su2code/su2/build-su2-cross:230225-2136
+        uses: docker://ghcr.io/su2code/su2/build-su2-cross:230704-1323
         with:
           args: -b ${{ github.sha }} -f "${{matrix.flags}}"
       - name: Create Archive

From 3ddd27ad8c4cfe3170ff1648f86842bfa4bedb1d Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 19 Jul 2023 18:10:28 +0200
Subject: [PATCH 608/656] OpDiLib update.

---
 externals/opdi        | 2 +-
 meson_scripts/init.py | 2 +-
 2 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/externals/opdi b/externals/opdi
index 913535c4909..c42cca71a3d 160000
--- a/externals/opdi
+++ b/externals/opdi
@@ -1 +1 @@
-Subproject commit 913535c490989ea9aa654e8c7df41c7e3718a5a2
+Subproject commit c42cca71a3d0b44fb482e268ecd40b623e71776b
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 372e77bc228..be044f16c53 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -59,7 +59,7 @@ def init_submodules(
     github_repo_codi = "https://github.com/scicompkl/CoDiPack"
     sha_version_medi = "aafc2d1966ba1233640af737e71c77c1a86183fd"
     github_repo_medi = "https://github.com/SciCompKL/MeDiPack"
-    sha_version_opdi = "913535c490989ea9aa654e8c7df41c7e3718a5a2"
+    sha_version_opdi = "c42cca71a3d0b44fb482e268ecd40b623e71776b"
     github_repo_opdi = "https://github.com/SciCompKL/OpDiLib"
     sha_version_meson = "41c650a040d50e0912d268af7a903a9ce1456dfa"
     github_repo_meson = "https://github.com/mesonbuild/meson"

From d2f81f4adead96249a8314d14fedd3cddf37723e Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Thu, 20 Jul 2023 13:40:54 +0200
Subject: [PATCH 609/656] Update bounds checking parameters.

---
 Common/include/basic_types/ad_structure.hpp | 6 ++----
 1 file changed, 2 insertions(+), 4 deletions(-)

diff --git a/Common/include/basic_types/ad_structure.hpp b/Common/include/basic_types/ad_structure.hpp
index adb9b94e71a..6721808119f 100644
--- a/Common/include/basic_types/ad_structure.hpp
+++ b/Common/include/basic_types/ad_structure.hpp
@@ -384,16 +384,14 @@ FORCEINLINE void SetDerivative(int index, const double val) {
   if (index == 0)  // Allow multiple threads to "set the derivative" of passive variables without causing data races.
     return;
 
-  using BoundsChecking = codi::GradientAccessTapeInterface<su2double::Gradient, su2double::Identifier>::BoundsChecking;
-  AD::getTape().setGradient(index, val, BoundsChecking::False);
+  AD::getTape().setGradient(index, val, codi::AdjointsBoundsChecking::False);
 }
 
 // WARNING: For performance reasons, this method does not perform bounds checking.
 // If called after tape evaluations, the adjoints should exist.
 // Otherwise, please ensure sufficient adjoint vector size by a call to AD::ResizeAdjoints().
 FORCEINLINE double GetDerivative(int index) {
-  using BoundsChecking = codi::GradientAccessTapeInterface<su2double::Gradient, su2double::Identifier>::BoundsChecking;
-  return AD::getTape().getGradient(index, BoundsChecking::False);
+  return AD::getTape().getGradient(index, codi::AdjointsBoundsChecking::False);
 }
 
 FORCEINLINE bool IsIdentifierActive(su2double const& value) {

From 5f8887f2005b5160d39d63c34fadf2ae969624c2 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 21 Jul 2023 09:41:02 +0200
Subject: [PATCH 610/656] Moved enthalpy pointer in GetEnthFromTemp function

---
 SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp |  6 +++---
 SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp     | 12 ++++++------
 2 files changed, 9 insertions(+), 9 deletions(-)

diff --git a/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp b/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp
index ba1661191cd..514a3c9a863 100644
--- a/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp
+++ b/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp
@@ -59,12 +59,12 @@ class CSpeciesFlameletSolver final : public CSpeciesSolver {
    * \brief Reverse look-up to retrieve enthalpy value based on temperature and other controlling variables.
    * \param[in] fluid_model - pointer to flamelet fluid model.
    * \param[in] val_temp - temperature value used for reverse look-up.
-   * \param[in] val_enth - pointer to enthalpy value to be retrieved.
    * \param[in] scalar_solution - local scalar solution.
+   * \param[in] val_enth_out - pointer to output enthalpy variable.
    * \param[out] Converged - 0 if Newton solver converged, 1 if not.
    */
-  unsigned long GetEnthFromTemp(CFluidModel* fluid_model, su2double const val_temp, su2double* val_enth,
-                                const su2double* scalar_solution);
+  unsigned long GetEnthFromTemp(CFluidModel* fluid_model, su2double const val_temp,
+                                const su2double* scalar_solution, su2double* val_enth_out);
 
   /*!
    * \brief Find maximum progress variable value within the manifold for the current solution.
diff --git a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
index 6e99e4eb568..2f8297a91a0 100644
--- a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
+++ b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
@@ -148,7 +148,7 @@ void CSpeciesFlameletSolver::SetInitialCondition(CGeometry** geometry, CSolver**
       for (auto iVar = 0u; iVar < nVar; iVar++) scalar_init[iVar] = config->GetSpecies_Init()[iVar];
 
       /*--- Set enthalpy based on initial temperature and scalars. ---*/
-      n_not_iterated_local += GetEnthFromTemp(fluid_model_local, temp_inlet, &enth_inlet, config->GetSpecies_Init());
+      n_not_iterated_local += GetEnthFromTemp(fluid_model_local, temp_inlet, config->GetSpecies_Init(), &enth_inlet);
       scalar_init[I_ENTH] = enth_inlet;
 
       prog_unburnt = config->GetSpecies_Init()[I_PROGVAR];
@@ -325,8 +325,8 @@ void CSpeciesFlameletSolver::BC_Inlet(CGeometry* geometry, CSolver** solver_cont
 
   /*--- We compute inlet enthalpy from the temperature and progress variable. ---*/
   su2double enth_inlet;
-  GetEnthFromTemp(solver_container[FLOW_SOL]->GetFluidModel(), temp_inlet, &enth_inlet,
-                  config->GetInlet_SpeciesVal(Marker_Tag));
+  GetEnthFromTemp(solver_container[FLOW_SOL]->GetFluidModel(), temp_inlet, config->GetInlet_SpeciesVal(Marker_Tag),
+                  &enth_inlet);
 
   SU2_OMP_FOR_STAT(OMP_MIN_SIZE)
   for (auto iVertex = 0u; iVertex < geometry->nVertex[val_marker]; iVertex++) {
@@ -356,7 +356,7 @@ void CSpeciesFlameletSolver::BC_Isothermal_Wall_Generic(CGeometry* geometry, CSo
 
     if (cht_mode)
       temp_wall = solver_container[FLOW_SOL]->GetConjugateHeatVariable(val_marker, iVertex, 0);
-    else 
+    else
       temp_wall = config->GetIsothermal_Temperature(Marker_Tag);
 
     /*--- Check if the node belongs to the domain (i.e., not a halo node). ---*/
@@ -367,7 +367,7 @@ void CSpeciesFlameletSolver::BC_Isothermal_Wall_Generic(CGeometry* geometry, CSo
         enth_wall = nodes->GetSolution(iPoint, I_ENTH);
 
         /*--- Set enthalpy on the wall. ---*/
-        n_not_iterated += GetEnthFromTemp(fluid_model_local, temp_wall, &enth_wall, nodes->GetSolution(iPoint));
+        n_not_iterated += GetEnthFromTemp(fluid_model_local, temp_wall, nodes->GetSolution(iPoint), &enth_wall);
 
         /*--- Impose the value of the enthalpy as a strong boundary
         condition (Dirichlet) and remove any
@@ -478,7 +478,7 @@ unsigned long CSpeciesFlameletSolver::SetScalarLookUps(const CConfig* config, CF
 }
 
 unsigned long CSpeciesFlameletSolver::GetEnthFromTemp(CFluidModel* fluid_model, su2double const val_temp,
-                                                      su2double* val_enth, const su2double* scalar_solution) {
+                                                      const su2double* scalar_solution, su2double* val_enth) {
   /*--- convergence criterion for temperature in [K], high accuracy needed for restarts. ---*/
   su2double delta_temp_final = 0.001;
   su2double enth_iter = scalar_solution[I_ENTH];

From 0bb922dd19e28f69796257f405d179c1216634d6 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 21 Jul 2023 10:05:04 +0200
Subject: [PATCH 611/656] Updated regression values for partially premixed
 flamelet test case due to update of the solution file in test cases
 repository

---
 TestCases/parallel_regression.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index a5309e5fb86..81ed8e4f1c5 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -65,7 +65,7 @@ def main():
     cfd_flamelet_ch4_partial_premix.cfg_dir = "flamelet/06_laminar_partial_premixed_ch4_flame_cfd"
     cfd_flamelet_ch4_partial_premix.cfg_file = "lam_partial_prem_ch4_cfd.cfg"
     cfd_flamelet_ch4_partial_premix.test_iter = 10
-    cfd_flamelet_ch4_partial_premix.test_vals = [-10.070242, -11.294887, -4.651523, -13.155604, -11.083940]
+    cfd_flamelet_ch4_partial_premix.test_vals = [-10.072805, -11.301138, -4.658971, -13.158224, -11.087511]
     cfd_flamelet_ch4_partial_premix.new_output = True
     test_list.append(cfd_flamelet_ch4_partial_premix)
 

From 74b893ac7a986f44aab765fc5252598b81c3d6c0 Mon Sep 17 00:00:00 2001
From: EvertBunschoten <evertbun@xs4all.nl>
Date: Fri, 21 Jul 2023 19:50:52 +0200
Subject: [PATCH 612/656] Updated test case branch for regression tests

---
 .github/workflows/regression.yml | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index feecd995252..bb4b8f06082 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -171,7 +171,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:230704-1323
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c feature_new_flamelet -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:230704-1323
         with:

From f3de6e55a53db85af7124e1eecf1379c35244164 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 23 Jul 2023 16:20:14 -0700
Subject: [PATCH 613/656] fix race condition to access Hsbg

---
 Common/include/linear_algebra/CSysSolve.hpp |  3 +-
 Common/src/linear_algebra/CSysSolve.cpp     | 31 +++++++++++++++------
 2 files changed, 25 insertions(+), 9 deletions(-)

diff --git a/Common/include/linear_algebra/CSysSolve.hpp b/Common/include/linear_algebra/CSysSolve.hpp
index 02569f8b396..c38f1bfd9ca 100644
--- a/Common/include/linear_algebra/CSysSolve.hpp
+++ b/Common/include/linear_algebra/CSysSolve.hpp
@@ -168,6 +168,7 @@ class CSysSolve {
    * \brief Modified Gram-Schmidt orthogonalization
    * \author Based on Kesheng John Wu's mgsro subroutine in Saad's SPARSKIT
    *
+   * \param[in] shared_hsbg - if the Hessenberg matrix is shared by multiple threads
    * \param[in] i - index indicating which vector in w is being orthogonalized
    * \param[in,out] Hsbg - the upper Hessenberg begin updated
    * \param[in,out] w - the (i+1)th vector of w is orthogonalized against the
@@ -181,7 +182,7 @@ class CSysSolve {
    * vector is kept in nrm0 and updated after operating with each vector
    *
    */
-  void ModGramSchmidt(int i, su2matrix<ScalarType>& Hsbg, std::vector<VectorType>& w) const;
+  void ModGramSchmidt(bool shared_hsbg, int i, su2matrix<ScalarType>& Hsbg, std::vector<VectorType>& w) const;
 
   /*!
    * \brief writes header information for a CSysSolve residual history
diff --git a/Common/src/linear_algebra/CSysSolve.cpp b/Common/src/linear_algebra/CSysSolve.cpp
index 85ab1705942..174d64b34f1 100644
--- a/Common/src/linear_algebra/CSysSolve.cpp
+++ b/Common/src/linear_algebra/CSysSolve.cpp
@@ -109,8 +109,19 @@ void CSysSolve<ScalarType>::SolveReduced(int n, const su2matrix<ScalarType>& Hsb
 }
 
 template <class ScalarType>
-void CSysSolve<ScalarType>::ModGramSchmidt(int i, su2matrix<ScalarType>& Hsbg,
+void CSysSolve<ScalarType>::ModGramSchmidt(bool shared_hsbg, int i, su2matrix<ScalarType>& Hsbg,
                                            vector<CSysVector<ScalarType> >& w) const {
+  const auto thread = omp_get_thread_num();
+
+  /*--- If Hsbg is shared by multiple threads calling this function, only one
+   * thread can write into it. If Hsbg is private, all threads need to write. ---*/
+
+  auto SetHsbg = [&](int row, int col, const ScalarType& value) {
+    if (!shared_hsbg || thread == 0) {
+      Hsbg(row, col) = value;
+    }
+  };
+
   /*--- Parameter for reorthonormalization ---*/
 
   const ScalarType reorth = 0.98;
@@ -132,20 +143,21 @@ void CSysSolve<ScalarType>::ModGramSchmidt(int i, su2matrix<ScalarType>& Hsbg,
 
   for (int k = 0; k < i + 1; k++) {
     ScalarType prod = w[i + 1].dot(w[k]);
-    Hsbg(k, i) = prod;
+    ScalarType h_ki = prod;
     w[i + 1] -= prod * w[k];
 
     /*--- Check if reorthogonalization is necessary ---*/
 
     if (prod * prod > thr) {
       prod = w[i + 1].dot(w[k]);
-      Hsbg(k, i) += prod;
+      h_ki += prod;
       w[i + 1] -= prod * w[k];
     }
+    SetHsbg(k, i, h_ki);
 
     /*--- Update the norm and check its size ---*/
 
-    nrm -= pow(Hsbg(k, i), 2);
+    nrm -= pow(h_ki, 2);
     nrm = max<ScalarType>(nrm, 0.0);
     thr = nrm * reorth;
   }
@@ -153,7 +165,7 @@ void CSysSolve<ScalarType>::ModGramSchmidt(int i, su2matrix<ScalarType>& Hsbg,
   /*--- Test the resulting vector ---*/
 
   nrm = w[i + 1].norm();
-  Hsbg(i + 1, i) = nrm;
+  SetHsbg(i + 1, i, nrm);
 
   /*--- Scale the resulting vector ---*/
 
@@ -343,6 +355,9 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
                                                       const CConfig* config) const {
   const bool masterRank = (SU2_MPI::GetRank() == MASTER_NODE);
   const bool flexible = !precond.IsIdentity();
+  /*--- If we call the solver outside of a parallel region, but the number of threads allows,
+   * we still want to parallelize some of the expensive operations. ---*/
+  const bool nestedParallel = !omp_in_parallel() && omp_get_max_threads() > 1;
 
   /*---  Check the subspace size ---*/
 
@@ -452,8 +467,8 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
 
     /*---  Modified Gram-Schmidt orthogonalization ---*/
 
-    SU2_OMP_PARALLEL_(if (!omp_in_parallel()))
-    ModGramSchmidt(i, H, W);
+    SU2_OMP_PARALLEL_(if (nestedParallel))
+    ModGramSchmidt(nestedParallel, i, H, W);
     END_SU2_OMP_PARALLEL
 
     /*---  Apply old Givens rotations to new column of the Hessenberg matrix then generate the
@@ -482,7 +497,7 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
 
   const auto& basis = flexible ? Z : W;
 
-  SU2_OMP_PARALLEL_(if (!omp_in_parallel()))
+  SU2_OMP_PARALLEL_(if (nestedParallel))
   for (unsigned long k = 0; k < i; k++) {
     x += y[k] * basis[k];
   }

From 19e200ec2b5cdd3bb2c2cf1eaa706a95a32e5d5f Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 23 Jul 2023 19:08:18 -0700
Subject: [PATCH 614/656] avoid some weirdness with "parallel if"

---
 Common/src/linear_algebra/CSysSolve.cpp | 21 ++++++++++++++-------
 1 file changed, 14 insertions(+), 7 deletions(-)

diff --git a/Common/src/linear_algebra/CSysSolve.cpp b/Common/src/linear_algebra/CSysSolve.cpp
index 174d64b34f1..0d50e561ae9 100644
--- a/Common/src/linear_algebra/CSysSolve.cpp
+++ b/Common/src/linear_algebra/CSysSolve.cpp
@@ -467,9 +467,14 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
 
     /*---  Modified Gram-Schmidt orthogonalization ---*/
 
-    SU2_OMP_PARALLEL_(if (nestedParallel))
-    ModGramSchmidt(nestedParallel, i, H, W);
-    END_SU2_OMP_PARALLEL
+    if (nestedParallel) {
+      /*--- "omp parallel if" does not work well here ---*/
+      SU2_OMP_PARALLEL
+      ModGramSchmidt(true, i, H, W);
+      END_SU2_OMP_PARALLEL
+    } else {
+      ModGramSchmidt(false, i, H, W);
+    }
 
     /*---  Apply old Givens rotations to new column of the Hessenberg matrix then generate the
      new Givens rotation matrix and apply it to the last two elements of H[:][i] and g ---*/
@@ -497,11 +502,13 @@ unsigned long CSysSolve<ScalarType>::FGMRES_LinSolver(const CSysVector<ScalarTyp
 
   const auto& basis = flexible ? Z : W;
 
-  SU2_OMP_PARALLEL_(if (nestedParallel))
-  for (unsigned long k = 0; k < i; k++) {
-    x += y[k] * basis[k];
+  if (nestedParallel) {
+    SU2_OMP_PARALLEL
+    for (unsigned long k = 0; k < i; k++) x += y[k] * basis[k];
+    END_SU2_OMP_PARALLEL
+  } else {
+    for (unsigned long k = 0; k < i; k++) x += y[k] * basis[k];
   }
-  END_SU2_OMP_PARALLEL
 
   /*---  Recalculate final (neg.) residual (this should be optional) ---*/
 

From f4feba9c2a7ae3c2fdb68f20fcbe998fe02f9388 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Tue, 25 Jul 2023 12:43:16 +0200
Subject: [PATCH 615/656] Update bounds checking parameters.

---
 Common/include/basic_types/ad_structure.hpp | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/Common/include/basic_types/ad_structure.hpp b/Common/include/basic_types/ad_structure.hpp
index 6721808119f..8a46096a58e 100644
--- a/Common/include/basic_types/ad_structure.hpp
+++ b/Common/include/basic_types/ad_structure.hpp
@@ -384,14 +384,14 @@ FORCEINLINE void SetDerivative(int index, const double val) {
   if (index == 0)  // Allow multiple threads to "set the derivative" of passive variables without causing data races.
     return;
 
-  AD::getTape().setGradient(index, val, codi::AdjointsBoundsChecking::False);
+  AD::getTape().setGradient(index, val, codi::AdjointsManagement::Manual);
 }
 
 // WARNING: For performance reasons, this method does not perform bounds checking.
 // If called after tape evaluations, the adjoints should exist.
 // Otherwise, please ensure sufficient adjoint vector size by a call to AD::ResizeAdjoints().
 FORCEINLINE double GetDerivative(int index) {
-  return AD::getTape().getGradient(index, codi::AdjointsBoundsChecking::False);
+  return AD::getTape().getGradient(index, codi::AdjointsManagement::Manual);
 }
 
 FORCEINLINE bool IsIdentifierActive(su2double const& value) {

From dfd656eccdd50277f913f0dc66fe243590dfe94b Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Tue, 25 Jul 2023 10:56:06 -0700
Subject: [PATCH 616/656] use the "real" current coordinates to compute surface
 rotations

---
 SU2_CFD/src/solvers/CMeshSolver.cpp | 18 ++++++++++++------
 1 file changed, 12 insertions(+), 6 deletions(-)

diff --git a/SU2_CFD/src/solvers/CMeshSolver.cpp b/SU2_CFD/src/solvers/CMeshSolver.cpp
index 3da0b843e6b..474112d3c73 100644
--- a/SU2_CFD/src/solvers/CMeshSolver.cpp
+++ b/SU2_CFD/src/solvers/CMeshSolver.cpp
@@ -969,7 +969,6 @@ void CMeshSolver::RestartOldGeometry(CGeometry *geometry, const CConfig *config)
 void CMeshSolver::Surface_Pitching(CGeometry *geometry, CConfig *config, unsigned long iter) {
 
   su2double deltaT, time_new, time_old, Lref;
-  const su2double* Coord = nullptr;
   su2double Center[3] = {0.0}, VarCoord[3] = {0.0}, Omega[3] = {0.0}, Ampl[3] = {0.0}, Phase[3] = {0.0};
   su2double VarCoordAbs[3] = {0.0};
   su2double rotCoord[3] = {0.0}, r[3] = {0.0};
@@ -1052,10 +1051,14 @@ void CMeshSolver::Surface_Pitching(CGeometry *geometry, CConfig *config, unsigne
 
       for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
 
-        /*--- Index and coordinates of the current point ---*/
+        /*--- Index and coordinates of the current point accounting for other
+         * motions that may be applied, e.g. plunging. ---*/
 
         iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
-        Coord  = geometry->nodes->GetCoord(iPoint);
+        su2double Coord[3] = {0.0};
+        for (iDim = 0; iDim < nDim; ++iDim) {
+          Coord[iDim] = nodes->GetMesh_Coord(iPoint, iDim) + nodes->GetBound_Disp(iPoint, iDim);
+        }
 
         /*--- Calculate non-dim. position from rotation center ---*/
 
@@ -1086,7 +1089,6 @@ void CMeshSolver::Surface_Pitching(CGeometry *geometry, CConfig *config, unsigne
 void CMeshSolver::Surface_Rotating(CGeometry *geometry, CConfig *config, unsigned long iter) {
 
   su2double deltaT, time_new, time_old, Lref;
-  const su2double* Coord = nullptr;
   su2double VarCoordAbs[3] = {0.0};
   su2double Center[3] = {0.0}, VarCoord[3] = {0.0}, Omega[3] = {0.0},
   rotCoord[3] = {0.0}, r[3] = {0.0}, Center_Aux[3] = {0.0};
@@ -1158,10 +1160,14 @@ void CMeshSolver::Surface_Rotating(CGeometry *geometry, CConfig *config, unsigne
 
       for (iVertex = 0; iVertex < geometry->nVertex[iMarker]; iVertex++) {
 
-        /*--- Index and coordinates of the current point ---*/
+        /*--- Index and coordinates of the current point accounting for other
+         * motions that may be applied, e.g. plunging. ---*/
 
         iPoint = geometry->vertex[iMarker][iVertex]->GetNode();
-        Coord  = geometry->nodes->GetCoord(iPoint);
+        su2double Coord[3] = {0.0};
+        for (iDim = 0; iDim < nDim; ++iDim) {
+          Coord[iDim] = nodes->GetMesh_Coord(iPoint, iDim) + nodes->GetBound_Disp(iPoint, iDim);
+        }
 
         /*--- Calculate non-dim. position from rotation center ---*/
 

From 542bf076a60a34a2f12d07d5512b02fd5887bf11 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Tue, 25 Jul 2023 16:22:15 -0700
Subject: [PATCH 617/656] update test

---
 TestCases/hybrid_regression.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index da01743218f..af97193431f 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -526,7 +526,7 @@ def main():
     unst_deforming_naca0012.cfg_dir   = "disc_adj_euler/naca0012_pitching_def"
     unst_deforming_naca0012.cfg_file  = "inv_NACA0012_pitching_deform.cfg"
     unst_deforming_naca0012.test_iter = 5
-    unst_deforming_naca0012.test_vals = [-3.665120, -3.793643, -3.716518, -3.148310]
+    unst_deforming_naca0012.test_vals = [-3.665126, -3.793497, -3.716496, -3.148290]
     unst_deforming_naca0012.unsteady  = True
     unst_deforming_naca0012.enabled_with_tsan = False
     test_list.append(unst_deforming_naca0012)

From a9a7ad82c6b65fd170b48797eb11228f9d32b290 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 26 Jul 2023 14:03:55 +0200
Subject: [PATCH 618/656] Update CoDiPack version.

---
 externals/codi        | 2 +-
 meson_scripts/init.py | 2 +-
 2 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/externals/codi b/externals/codi
index 4237fe38c90..17232fed052 160000
--- a/externals/codi
+++ b/externals/codi
@@ -1 +1 @@
-Subproject commit 4237fe38c90b83541f699bd84e00c656099b7d18
+Subproject commit 17232fed05245dbb8f04a31e274a02d53458c75c
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 1e70f41296f..eb69728e2a0 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -55,7 +55,7 @@ def init_submodules(
 
     # This information of the modules is used if projects was not cloned using git
     # The sha tag must be maintained manually to point to the correct commit
-    sha_version_codi = "4237fe38c90b83541f699bd84e00c656099b7d18"
+    sha_version_codi = "17232fed05245dbb8f04a31e274a02d53458c75c"
     github_repo_codi = "https://github.com/scicompkl/CoDiPack"
     sha_version_medi = "aafc2d1966ba1233640af737e71c77c1a86183fd"
     github_repo_medi = "https://github.com/SciCompKL/MeDiPack"

From 0fccdc117e9cc6d3c46ebb11d4965f88aaf9fc7c Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Thu, 27 Jul 2023 16:31:00 +0200
Subject: [PATCH 619/656] Address meson deprecation warnings.

---
 meson.build | 6 +++---
 1 file changed, 3 insertions(+), 3 deletions(-)

diff --git a/meson.build b/meson.build
index cbfdacc0e12..d4a290d54a1 100644
--- a/meson.build
+++ b/meson.build
@@ -46,7 +46,7 @@ if build_machine.system() != 'windows'
 endif
 
 # meson script path
-script_path = meson.source_root() / 'meson_scripts'
+script_path = meson.project_source_root() / 'meson_scripts'
 
 # mpi flag
 mpi = false
@@ -325,10 +325,10 @@ message('''---------------------------------------------------------------------
          export PYTHONPATH=$PYTHONPATH:$SU2_RUN
 
          Use './ninja -C @13@ install' to compile and install SU2
-'''.format(get_option('prefix')+'/bin', meson.source_root(), get_option('enable-tecio'), get_option('enable-cgns'),
+'''.format(get_option('prefix')+'/bin', meson.project_source_root(), get_option('enable-tecio'), get_option('enable-cgns'),
            get_option('enable-autodiff'), get_option('enable-directdiff'), get_option('enable-pywrapper'), get_option('enable-mkl'),
            get_option('enable-openblas'), get_option('enable-pastix'), get_option('enable-mixedprec'), get_option('enable-librom'), get_option('enable-coolprop'),
-           get_option('enable-mlpcpp'), meson.build_root().startswith(meson.source_root()) ? meson.build_root().split('/')[-1] : meson.build_root()))
+           get_option('enable-mlpcpp'), meson.project_build_root().startswith(meson.project_source_root()) ? meson.project_build_root().split('/')[-1] : meson.project_build_root()))
 
 if get_option('enable-mpp')
   message(''' To run SU2 with Mutation++ library, add these lines to your .bashrc file:

From d343c40a6fd828349f96d5377bfe4a56de5445cd Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Thu, 27 Jul 2023 16:35:32 +0200
Subject: [PATCH 620/656] Fix MLPCpp output and ninja path.

---
 meson.build | 3 ++-
 1 file changed, 2 insertions(+), 1 deletion(-)

diff --git a/meson.build b/meson.build
index d4a290d54a1..bc862b6572f 100644
--- a/meson.build
+++ b/meson.build
@@ -313,6 +313,7 @@ message('''---------------------------------------------------------------------
          Mixed Float:    @10@
          libROM:         @11@
          CoolProp:       @12@
+         MLPCpp:         @13@
 
          Please be sure to add the $SU2_HOME and $SU2_RUN environment variables,
          and update your $PATH (and $PYTHONPATH if applicable) with $SU2_RUN
@@ -324,7 +325,7 @@ message('''---------------------------------------------------------------------
          export PATH=$PATH:$SU2_RUN
          export PYTHONPATH=$PYTHONPATH:$SU2_RUN
 
-         Use './ninja -C @13@ install' to compile and install SU2
+         Use './ninja -C @14@ install' to compile and install SU2
 '''.format(get_option('prefix')+'/bin', meson.project_source_root(), get_option('enable-tecio'), get_option('enable-cgns'),
            get_option('enable-autodiff'), get_option('enable-directdiff'), get_option('enable-pywrapper'), get_option('enable-mkl'),
            get_option('enable-openblas'), get_option('enable-pastix'), get_option('enable-mixedprec'), get_option('enable-librom'), get_option('enable-coolprop'),

From fa70e1a1ded232a10eefbd794ba477697b54bc8d Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 29 Jul 2023 18:09:31 -0700
Subject: [PATCH 621/656] add custom temp and hf to inc ns solver and fix
 failing test

---
 SU2_CFD/src/solvers/CIncNSSolver.cpp            | 9 +++++++--
 TestCases/py_wrapper/custom_heat_flux/run_ad.py | 6 +++---
 2 files changed, 10 insertions(+), 5 deletions(-)

diff --git a/SU2_CFD/src/solvers/CIncNSSolver.cpp b/SU2_CFD/src/solvers/CIncNSSolver.cpp
index ea9fc7a1bdb..ce1c28fe364 100644
--- a/SU2_CFD/src/solvers/CIncNSSolver.cpp
+++ b/SU2_CFD/src/solvers/CIncNSSolver.cpp
@@ -336,13 +336,13 @@ void CIncNSSolver::BC_Wall_Generic(const CGeometry *geometry, const CConfig *con
 
   const bool implicit = (config->GetKind_TimeIntScheme() == EULER_IMPLICIT);
   const bool energy = config->GetEnergy_Equation();
+  const bool py_custom = config->GetMarker_All_PyCustom(val_marker);
 
   /*--- Variables for streamwise periodicity ---*/
   const bool streamwise_periodic = (config->GetKind_Streamwise_Periodic() != ENUM_STREAMWISE_PERIODIC::NONE);
   const bool streamwise_periodic_temperature = config->GetStreamwise_Periodic_Temperature();
   su2double Cp, thermal_conductivity, dot_product, scalar_factor;
 
-
   /*--- Identify the boundary by string name ---*/
 
   const auto Marker_Tag = config->GetMarker_All_TagBound(val_marker);
@@ -426,6 +426,9 @@ void CIncNSSolver::BC_Wall_Generic(const CGeometry *geometry, const CConfig *con
       /*--- Apply a weak boundary condition for the energy equation.
       Compute the residual due to the prescribed heat flux. ---*/
 
+      if (py_custom) {
+        Wall_HeatFlux = geometry->GetCustomBoundaryHeatFlux(val_marker, iVertex) / config->GetHeat_Flux_Ref();
+      }
       LinSysRes(iPoint, nDim+1) -= Wall_HeatFlux*Area;
 
       /*--- With streamwise periodic flow and heatflux walls an additional term is introduced in the boundary formulation ---*/
@@ -460,7 +463,9 @@ void CIncNSSolver::BC_Wall_Generic(const CGeometry *geometry, const CConfig *con
       break;
 
     case ISOTHERMAL:
-
+      if (py_custom) {
+        Twall = geometry->GetCustomBoundaryTemperature(val_marker, iVertex) / config->GetTemperature_Ref();
+      }
       const auto Point_Normal = geometry->vertex[val_marker][iVertex]->GetNormal_Neighbor();
 
       /*--- Get coordinates of i & nearest normal and compute distance ---*/
diff --git a/TestCases/py_wrapper/custom_heat_flux/run_ad.py b/TestCases/py_wrapper/custom_heat_flux/run_ad.py
index 91695b4e6b2..8a13e067a56 100644
--- a/TestCases/py_wrapper/custom_heat_flux/run_ad.py
+++ b/TestCases/py_wrapper/custom_heat_flux/run_ad.py
@@ -228,9 +228,9 @@ def main():
   comm = MPI.COMM_WORLD
   rank = comm.Get_rank()
 
-  obj_pert_size = RunPrimal(0.100005)
+  obj_pert_size = RunPrimal(0.10002)
   obj = RunPrimal(0.1)
-  sens_size_fd = (obj_pert_size - obj) / 0.000005
+  sens_size_fd = (obj_pert_size - obj) / 0.00002
 
   sens_size, sens_temp = RunAdjoint(0.1)
 
@@ -238,7 +238,7 @@ def main():
     print("     Finite Differences\tDiscrete Adjoint")
     print(f"Size {sens_size_fd}\t{sens_size}")
 
-  assert abs(sens_size / sens_size_fd - 1) < 1e-4, "Error in geometric derivatives."
+  assert abs(sens_size / sens_size_fd - 1) < 1e-3, "Error in geometric derivatives."
   # We expect the final average temperature to be directly proportional to the initial
   # temperature since the applied heat flux is not a function of temperature.
   assert abs(sens_temp - 1) < 1e-5, "Error in initial condition derivatives."

From f679db17223395c6224bcf20af4e010168840474 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 29 Jul 2023 19:33:33 -0700
Subject: [PATCH 622/656] fix the python case

---
 SU2_CFD/src/interfaces/cht/CConjugateHeatInterface.cpp | 2 +-
 SU2_CFD/src/solvers/CIncNSSolver.cpp                   | 2 +-
 TestCases/py_wrapper/custom_heat_flux/run_ad.py        | 8 ++++----
 3 files changed, 6 insertions(+), 6 deletions(-)

diff --git a/SU2_CFD/src/interfaces/cht/CConjugateHeatInterface.cpp b/SU2_CFD/src/interfaces/cht/CConjugateHeatInterface.cpp
index a1400ad0799..ea9dd7134f7 100644
--- a/SU2_CFD/src/interfaces/cht/CConjugateHeatInterface.cpp
+++ b/SU2_CFD/src/interfaces/cht/CConjugateHeatInterface.cpp
@@ -70,7 +70,7 @@ void CConjugateHeatInterface::GetDonor_Variable(CSolver *donor_solution, CGeomet
   su2double conductivity_over_dist = 0.0;
 
   const bool compressible_flow = (donor_config->GetKind_Regime() == ENUM_REGIME::COMPRESSIBLE);
-  const bool incompressible_flow = (donor_config->GetKind_Regime() == ENUM_REGIME::INCOMPRESSIBLE) && 
+  const bool incompressible_flow = (donor_config->GetKind_Regime() == ENUM_REGIME::INCOMPRESSIBLE) &&
                                    (donor_config->GetEnergy_Equation() || (donor_config->GetKind_FluidModel() == ENUM_FLUIDMODEL::FLUID_FLAMELET));
 
   if (compressible_flow) {
diff --git a/SU2_CFD/src/solvers/CIncNSSolver.cpp b/SU2_CFD/src/solvers/CIncNSSolver.cpp
index ce1c28fe364..061c8ee02ec 100644
--- a/SU2_CFD/src/solvers/CIncNSSolver.cpp
+++ b/SU2_CFD/src/solvers/CIncNSSolver.cpp
@@ -219,7 +219,7 @@ void CIncNSSolver::GetStreamwise_Periodic_Properties(const CGeometry *geometry,
 
           const su2double FaceArea = GeometryToolbox::Norm(nDim, AreaNormal);
 
-          HeatFlow_Local += FaceArea * (-1.0) * Wall_HeatFlux/config->GetHeat_Flux_Ref();;
+          HeatFlow_Local += FaceArea * (-1.0) * Wall_HeatFlux/config->GetHeat_Flux_Ref();
         } // loop Vertices
       } // loop Heatflux marker
     } // loop AllMarker
diff --git a/TestCases/py_wrapper/custom_heat_flux/run_ad.py b/TestCases/py_wrapper/custom_heat_flux/run_ad.py
index 8a13e067a56..8fa54a0a891 100644
--- a/TestCases/py_wrapper/custom_heat_flux/run_ad.py
+++ b/TestCases/py_wrapper/custom_heat_flux/run_ad.py
@@ -92,7 +92,7 @@ def ApplyHeatFlux(time, driver, marker_ids):
   for marker_id in marker_ids:
     if marker_id < 0:
       continue
-    hf = (-1, 0)[time > 0.2]
+    hf = (-1 * 2700 * 870, 0)[time > 0.2]
     for i_vertex in range(driver.GetNumberMarkerNodes(marker_id)):
       driver.SetMarkerCustomNormalHeatFlux(marker_id, i_vertex, hf)
 
@@ -228,9 +228,9 @@ def main():
   comm = MPI.COMM_WORLD
   rank = comm.Get_rank()
 
-  obj_pert_size = RunPrimal(0.10002)
+  obj_pert_size = RunPrimal(0.100005)
   obj = RunPrimal(0.1)
-  sens_size_fd = (obj_pert_size - obj) / 0.00002
+  sens_size_fd = (obj_pert_size - obj) / 0.000005
 
   sens_size, sens_temp = RunAdjoint(0.1)
 
@@ -238,7 +238,7 @@ def main():
     print("     Finite Differences\tDiscrete Adjoint")
     print(f"Size {sens_size_fd}\t{sens_size}")
 
-  assert abs(sens_size / sens_size_fd - 1) < 1e-3, "Error in geometric derivatives."
+  assert abs(sens_size / sens_size_fd - 1) < 1e-4, "Error in geometric derivatives."
   # We expect the final average temperature to be directly proportional to the initial
   # temperature since the applied heat flux is not a function of temperature.
   assert abs(sens_temp - 1) < 1e-5, "Error in initial condition derivatives."

From e53937c6b739922ea814f88ad76ff0043498957b Mon Sep 17 00:00:00 2001
From: Jan Rottmayer <jan.rottmayer@web.de>
Date: Tue, 1 Aug 2023 13:09:58 +0200
Subject: [PATCH 623/656] added cstdint header to printing_toolbox.hpp

---
 Common/include/toolboxes/printing_toolbox.hpp | 1 +
 1 file changed, 1 insertion(+)

diff --git a/Common/include/toolboxes/printing_toolbox.hpp b/Common/include/toolboxes/printing_toolbox.hpp
index 7461f0465de..d70271a5539 100644
--- a/Common/include/toolboxes/printing_toolbox.hpp
+++ b/Common/include/toolboxes/printing_toolbox.hpp
@@ -27,6 +27,7 @@
 
 #include <iostream>
 #include <iomanip>
+#include <cstdint>
 #include <vector>
 #include <string>
 #include <sstream>

From 374a385421261a0dc818b47cae7f6abb88a13425 Mon Sep 17 00:00:00 2001
From: sjhbosmans <sjhbosmans@Ubuntu-22.10.myguest.virtualbox.org>
Date: Thu, 3 Aug 2023 14:48:52 +0200
Subject: [PATCH 624/656] Added files for vandv case sandia jet for test cases

---
 .github/workflows/regression.yml              |   2 +-
 TestCases/vandv.py                            |  12 ++
 .../sandia_jet/VALIDATION.cfg                 | 151 ++++++++++++++++++
 3 files changed, 164 insertions(+), 1 deletion(-)
 create mode 100644 TestCases/vandv/species_transport/sandia_jet/VALIDATION.cfg

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index bb4b8f06082..2b2ab240c26 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -171,7 +171,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:230704-1323
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c feature_validation_sandia_jet -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:230704-1323
         with:
diff --git a/TestCases/vandv.py b/TestCases/vandv.py
index 4c798598bc2..4a91efa1b95 100644
--- a/TestCases/vandv.py
+++ b/TestCases/vandv.py
@@ -85,6 +85,18 @@ def main():
     swbli_sst.test_vals = [-11.527743, -11.150388, -11.944923, -10.750834, -11.116769, -4.030059, 0.002339, -2.730391, -4.067274, 1.276300]
     test_list.append(swbli_sst)
 
+    ##########################
+    ### Incompressible RANS ###
+    ##########################
+
+    # Sandia jet - sst-v2003m
+    sandiajet_sst           = TestCase('sandiajet_sst')
+    sandiajet_sst.cfg_dir   = "vandv/species_transport/sandia_jet"
+    sandiajet_sst.cfg_file  = "VALIDATION.cfg"
+    sandiajet_sst.test_iter = 5
+    sandiajet_sst.test_vals = [-11.527743, -11.150388, -11.944923, -10.750834, -11.116769, -4.030059]
+    test_list.append(sandiajet_sst)
+
     #################
     ### RUN TESTS ###
     #################
diff --git a/TestCases/vandv/species_transport/sandia_jet/VALIDATION.cfg b/TestCases/vandv/species_transport/sandia_jet/VALIDATION.cfg
new file mode 100644
index 00000000000..2fd45926aaa
--- /dev/null
+++ b/TestCases/vandv/species_transport/sandia_jet/VALIDATION.cfg
@@ -0,0 +1,151 @@
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+%                                                                                   %
+% SU2 configuration file                                                            %
+% Case description: V&V Composition-dependent model Sandia's turbulent jet    	    %
+% Author: S.J.H. Bosmans                                                            %
+% Institution: TU Eindhoven (TU/e)                                                  %
+% Date: 2023/05/04                                                                  %
+% File Version 7.5.0 "Blackbird"                                                    %
+%                                                                                   %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
+SOLVER= INC_RANS
+KIND_TURB_MODEL= SST
+SST_OPTIONS= V2003m
+RESTART_SOL= YES
+%
+% ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
+%
+INC_DENSITY_MODEL= VARIABLE
+INC_DENSITY_INIT= 1.828
+%
+INC_VELOCITY_INIT= ( 53.0, 0.0, 0.0 )
+%
+INC_ENERGY_EQUATION= NO
+INC_TEMPERATURE_INIT= 294.0
+%
+INC_NONDIM= DIMENSIONAL
+%
+% -------------------- FLUID PROPERTIES ------------------------------------- %
+%
+FLUID_MODEL= FLUID_MIXTURE
+%
+MOLECULAR_WEIGHT= 44.097, 28.960
+THERMODYNAMIC_PRESSURE = 101325.0
+%
+SPECIFIC_HEAT_CP = 1680.0, 1009.39
+%
+CONDUCTIVITY_MODEL= CONSTANT_CONDUCTIVITY
+THERMAL_CONDUCTIVITY_CONSTANT= 0.0179, 0.0258
+%
+PRANDTL_LAM= 0.72, 0.72
+TURBULENT_CONDUCTIVITY_MODEL= CONSTANT_PRANDTL_TURB
+PRANDTL_TURB= 0.90, 0.90
+%
+% --------------------------- VISCOSITY MODEL ---------------------------------%
+%
+VISCOSITY_MODEL= CONSTANT_VISCOSITY
+%
+MU_CONSTANT= 8.04E-06, 1.8551E-05 
+% 
+MIXING_VISCOSITY_MODEL = WILKE
+%
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
+MARKER_HEATFLUX= ( wall, 0.0 )
+AXISYMMETRIC= YES
+MARKER_SYM= ( symmetry )
+MARKER_EULER= ( top_wall )
+MARKER_INLET_TURBULENT= ( inlet_gas, 0.04, 5, inlet_air, 0.004, 1 )
+%
+INC_INLET_TYPE=  VELOCITY_INLET VELOCITY_INLET
+SPECIFIED_INLET_PROFILE= NO
+%INLET_FILENAME= inlet_jet.dat
+%INLET_MATCHING_TOLERANCE= 1.2E-06
+%
+MARKER_INLET= ( inlet_gas, 294, 53.0, 1.0, 0.0 0.0, inlet_air, 294, 9.2, 1.0, 0.0, 0.0 )
+MARKER_INLET_SPECIES= ( inlet_gas, 1.0, inlet_air, 0.0 )
+%
+INC_OUTLET_TYPE= PRESSURE_OUTLET
+MARKER_OUTLET= ( outlet, 0.0 )
+%
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
+%
+CFL_NUMBER= 200.0
+CFL_ADAPT= NO
+CFL_REDUCTION_SPECIES= 1.0
+CFL_REDUCTION_TURB= 0.5
+%
+ITER= 9999
+%
+% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
+%
+LINEAR_SOLVER= FGMRES
+LINEAR_SOLVER_PREC= ILU
+LINEAR_SOLVER_ERROR= 1E-5
+LINEAR_SOLVER_ITER= 5
+%
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
+CONV_NUM_METHOD_FLOW= FDS
+MUSCL_FLOW= NO
+SLOPE_LIMITER_FLOW = NONE
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+%
+% -------------------- SCALAR TRANSPORT ---------------------------------------%
+%
+KIND_SCALAR_MODEL= SPECIES_TRANSPORT
+%
+DIFFUSIVITY_MODEL= UNITY_LEWIS
+%
+SCHMIDT_NUMBER_TURBULENT= 0.7
+%
+CONV_NUM_METHOD_SPECIES= BOUNDED_SCALAR
+MUSCL_SPECIES= NO
+SLOPE_LIMITER_SPECIES = NONE
+%
+TIME_DISCRE_SPECIES= EULER_IMPLICIT
+%
+SPECIES_INIT= 0.05
+SPECIES_CLIPPING= NO
+SPECIES_CLIPPING_MIN= 0.0
+SPECIES_CLIPPING_MAX= 1.0
+%
+% -------------------- TURBULENT TRANSPORT ---------------------------------------%
+%
+CONV_NUM_METHOD_TURB= BOUNDED_SCALAR
+MUSCL_TURB= NO
+%
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
+CONV_FIELD= RMS_PRESSURE, RMS_VELOCITY-X, RMS_VELOCITY-Y, RMS_TKE, RMS_SPECIES
+CONV_RESIDUAL_MINVAL= -14.0
+CONV_CAUCHY_ELEMS= 100
+CONV_CAUCHY_EPS= 1E-6
+%
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+%
+MESH_FILENAME= MESH_validation.su2
+%
+SCREEN_OUTPUT= INNER_ITER WALL_TIME RMS_RES LINSOL_ITER LINSOL_RESIDUAL LINSOL_ITER_TURB LINSOL_RESIDUAL_TURB LINSOL_ITER_SPECIES LINSOL_RESIDUAL_SPECIES SURFACE_SPECIES_VARIANCE SURFACE_TOTAL_PRESSURE
+SCREEN_WRT_FREQ_INNER= 10
+%
+HISTORY_OUTPUT= ITER RMS_RES LINSOL SPECIES_COEFF SPECIES_COEFF_SURF SURFACE_TOTAL_PRESSURE
+CONV_FILENAME= history
+MARKER_ANALYZE= inlet_gas,inlet_air, outlet
+MARKER_ANALYZE_AVERAGE= AREA
+%
+OUTPUT_FILES= RESTART_ASCII, PARAVIEW_MULTIBLOCK
+VOLUME_OUTPUT= RESIDUAL, PRIMITIVE
+OUTPUT_WRT_FREQ= 100
+%
+READ_BINARY_RESTART= NO
+RESTART_FILENAME= restart.csv
+SOLUTION_FILENAME= solution.csv
+%
+WRT_PERFORMANCE= YES
+OUTPUT_PRECISION= 16

From 6e0db0db68b3e89edcb080a80bd30f0e15428747 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Fri, 4 Aug 2023 07:41:17 -0700
Subject: [PATCH 625/656] Update .github/workflows/regression.yml

---
 .github/workflows/regression.yml | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 2b2ab240c26..bb4b8f06082 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -171,7 +171,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:230704-1323
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c feature_validation_sandia_jet -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:230704-1323
         with:

From 72230f96c9d2023e2e9be749eec1d02f04747257 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Fri, 4 Aug 2023 09:55:27 -0700
Subject: [PATCH 626/656] Update TestCases/vandv.py

---
 TestCases/vandv.py | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/vandv.py b/TestCases/vandv.py
index 4a91efa1b95..536abf61f2e 100644
--- a/TestCases/vandv.py
+++ b/TestCases/vandv.py
@@ -94,7 +94,7 @@ def main():
     sandiajet_sst.cfg_dir   = "vandv/species_transport/sandia_jet"
     sandiajet_sst.cfg_file  = "VALIDATION.cfg"
     sandiajet_sst.test_iter = 5
-    sandiajet_sst.test_vals = [-11.527743, -11.150388, -11.944923, -10.750834, -11.116769, -4.030059]
+    sandiajet_sst.test_vals = [-16.249917, -13.835991, -14.303372, -13.276035, -10.074262, -14.027223, 5, -1.672359, 5, -4.938477, 5, -3.462217, 2.5859e-04, 2.8215e-32, 4.5010e-68, 2.5859e-04, 4.0474e+03, 3.9468e+03, 4.9170e+01, 5.1441e+01]
     test_list.append(sandiajet_sst)
 
     #################

From f26b292adb1e0939775444495c4e8825a4c12b66 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 5 Aug 2023 19:31:11 -0700
Subject: [PATCH 627/656] rename testcase config

---
 TestCases/vandv.py                                              | 2 +-
 .../sandia_jet/{VALIDATION.cfg => validation.cfg}               | 0
 2 files changed, 1 insertion(+), 1 deletion(-)
 rename TestCases/vandv/species_transport/sandia_jet/{VALIDATION.cfg => validation.cfg} (100%)

diff --git a/TestCases/vandv.py b/TestCases/vandv.py
index 536abf61f2e..baba0b84169 100644
--- a/TestCases/vandv.py
+++ b/TestCases/vandv.py
@@ -92,7 +92,7 @@ def main():
     # Sandia jet - sst-v2003m
     sandiajet_sst           = TestCase('sandiajet_sst')
     sandiajet_sst.cfg_dir   = "vandv/species_transport/sandia_jet"
-    sandiajet_sst.cfg_file  = "VALIDATION.cfg"
+    sandiajet_sst.cfg_file  = "validation.cfg"
     sandiajet_sst.test_iter = 5
     sandiajet_sst.test_vals = [-16.249917, -13.835991, -14.303372, -13.276035, -10.074262, -14.027223, 5, -1.672359, 5, -4.938477, 5, -3.462217, 2.5859e-04, 2.8215e-32, 4.5010e-68, 2.5859e-04, 4.0474e+03, 3.9468e+03, 4.9170e+01, 5.1441e+01]
     test_list.append(sandiajet_sst)
diff --git a/TestCases/vandv/species_transport/sandia_jet/VALIDATION.cfg b/TestCases/vandv/species_transport/sandia_jet/validation.cfg
similarity index 100%
rename from TestCases/vandv/species_transport/sandia_jet/VALIDATION.cfg
rename to TestCases/vandv/species_transport/sandia_jet/validation.cfg

From f75045c2f55d9835e433fba516424ef5178f6a4c Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 5 Aug 2023 19:46:11 -0700
Subject: [PATCH 628/656] fix some version numbers

---
 .github/workflows/change-version.yml               |  2 +-
 .../lam_prem_ch4_cfd_axi.cfg                       | 14 +++++++-------
 TestCases/nicf/datadriven/datadriven_nozzle.cfg    |  4 ++--
 .../species_transport/sandia_jet/validation.cfg    |  6 +++---
 4 files changed, 13 insertions(+), 13 deletions(-)

diff --git a/.github/workflows/change-version.yml b/.github/workflows/change-version.yml
index 58752ea921c..012217a248f 100644
--- a/.github/workflows/change-version.yml
+++ b/.github/workflows/change-version.yml
@@ -16,7 +16,7 @@ jobs:
       id: extract_branch
     - name: Change the version number
       run: |
-        SU2_PY/change_version_number.py -v ${GITHUB_REF##*/release_v} -r Blackbird -y
+        SU2_PY/change_version_number.py -v ${GITHUB_REF##*/release_v} -r Harrier -y
     - name: Commit files
       run: |
         git config --local user.email "action@github.com"
diff --git a/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg b/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg
index 62957216e01..391b49a5d07 100644
--- a/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg
+++ b/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg
@@ -1,11 +1,11 @@
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 % SU2 configuration file                                                       %
 % Case description: Laminar premixed flame stabilized on isothermal burner     %
-%                   axisymmetric setup
+%                   axisymmetric setup                                         %
 % Author: Nijso Beishuizen                                                     %
 % Institution: Bosch Thermotechnology                                          %
 % Date: 08/09/2021                                                             %
-% File Version 7.5.0 "Falcon", branch: feature_new_flamelet                    %
+% File Version 7.5.1 "Blackbird",                                              %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
@@ -25,7 +25,7 @@ INC_VELOCITY_INIT= (0.5, 0.0, 0.0 )
 INC_TEMPERATURE_INIT= 300.0
 INC_NONDIM= DIMENSIONAL
 %
-% 
+%
 AXISYMMETRIC= YES
 % -------------------- FLUID MODEL --------------------------------------- %
 %
@@ -36,7 +36,7 @@ CONTROLLING_VARIABLE_SOURCE_NAMES= (ProdRateTot_PV, NULL)
 %
 % -------------------- SCALAR TRANSPORT ---------------------------------------%
 %
-KIND_SCALAR_MODEL= FLAMELET      
+KIND_SCALAR_MODEL= FLAMELET
 DIFFUSIVITY_MODEL= FLAMELET
 VISCOSITY_MODEL= FLAMELET
 CONDUCTIVITY_MODEL= FLAMELET
@@ -127,12 +127,12 @@ MESH_FILENAME= mesh_axi.su2
 MESH_OUT_FILENAME= mesh_out.su2
 SOLUTION_FILENAME= solution
 RESTART_FILENAME= restart
-%OUTPUT_FILES= (RESTART,PARAVIEW,PARAVIEW_MULTIBLOCK) 
-OUTPUT_FILES= (RESTART) 
+%OUTPUT_FILES= (RESTART,PARAVIEW,PARAVIEW_MULTIBLOCK)
+OUTPUT_FILES= (RESTART)
 TABULAR_FORMAT= CSV
 CONV_FILENAME= history
 VOLUME_FILENAME= flow
 SURFACE_FILENAME= surface_flow
-WRT_PERFORMANCE= NO 
+WRT_PERFORMANCE= NO
 SCREEN_WRT_FREQ_INNER= 1
 SCREEN_WRT_FREQ_OUTER= 1
diff --git a/TestCases/nicf/datadriven/datadriven_nozzle.cfg b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
index 700f1c38865..32f16319c5f 100644
--- a/TestCases/nicf/datadriven/datadriven_nozzle.cfg
+++ b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
@@ -7,7 +7,7 @@
 % Author: Evert Bunschoten                                                     %
 % Institution: Delft University of Technology                                  %
 % Date: 2022.10.8                                                              %
-% File Version  7.4.0 Blackbird                                                %
+% File Version  7.5.1 Blackbird                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -36,7 +36,7 @@ REF_DIMENSIONALIZATION= DIMENSIONAL
 % ---- DATADRIVEN FLUID MODEL DEFINITION -------%
 %
 FLUID_MODEL = DATADRIVEN_FLUID
-INTERPOLATION_METHOD = MLP 
+INTERPOLATION_METHOD = MLP
 FILENAMES_INTERPOLATOR = (MLP_air.mlp)
 DATADRIVEN_NEWTON_RELAXATION = 0.8
 
diff --git a/TestCases/vandv/species_transport/sandia_jet/validation.cfg b/TestCases/vandv/species_transport/sandia_jet/validation.cfg
index 2fd45926aaa..f72e90167ce 100644
--- a/TestCases/vandv/species_transport/sandia_jet/validation.cfg
+++ b/TestCases/vandv/species_transport/sandia_jet/validation.cfg
@@ -5,7 +5,7 @@
 % Author: S.J.H. Bosmans                                                            %
 % Institution: TU Eindhoven (TU/e)                                                  %
 % Date: 2023/05/04                                                                  %
-% File Version 7.5.0 "Blackbird"                                                    %
+% File Version 7.5.1 "Blackbird"                                                    %
 %                                                                                   %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -48,8 +48,8 @@ PRANDTL_TURB= 0.90, 0.90
 %
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
 %
-MU_CONSTANT= 8.04E-06, 1.8551E-05 
-% 
+MU_CONSTANT= 8.04E-06, 1.8551E-05
+%
 MIXING_VISCOSITY_MODEL = WILKE
 %
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%

From edccf5c6cfdef50567e772bfcf62e413f9dd757e Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 6 Aug 2023 14:33:04 -0700
Subject: [PATCH 629/656] update change_version_number to not break config
 headers

---
 SU2_PY/change_version_number.py | 17 +++++++++++++----
 1 file changed, 13 insertions(+), 4 deletions(-)

diff --git a/SU2_PY/change_version_number.py b/SU2_PY/change_version_number.py
index 4786a9eedd3..43371c94d78 100755
--- a/SU2_PY/change_version_number.py
+++ b/SU2_PY/change_version_number.py
@@ -110,11 +110,20 @@
 
 # Loop through and correct all files
 for fname in filelist:
-    s = open(fname, "r").read()
-    s_new = s.replace(oldvers, newvers)
-    s_new = s_new.replace(oldvers_q, newvers_q)
+    lines = open(fname, "r").readlines()
+    for i, line in enumerate(lines):
+        if oldvers in line:
+            # Avoid breaking the formating of some testcase headers
+            if line.endswith("%\n"):
+                n = len(newvers) - len(oldvers)
+                lines[i] = line.replace(
+                    oldvers + " " * max(0, n), newvers + " " * max(0, -n)
+                )
+            else:
+                lines[i] = line.replace(oldvers, newvers)
+        lines[i] = line.replace(oldvers_q, newvers_q)
     f = open(fname, "w")
-    f.write(s_new)
+    f.writelines(lines)
     f.close()
 
 os.system("rm -rf version.txt")

From 77a972e0aa02ee248f0e8a043236d673e8430540 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 6 Aug 2023 15:15:25 -0700
Subject: [PATCH 630/656] cleanup some SU2 header priting code

---
 Common/src/CConfig.cpp             | 68 +++++++++++++++---------------
 SU2_CFD/src/output/CFlowOutput.cpp |  6 +--
 SU2_PY/change_version_number.py    | 17 +++-----
 3 files changed, 44 insertions(+), 47 deletions(-)

diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 23b84730103..be3aa73a744 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -3226,41 +3226,41 @@ bool CConfig::SetRunTime_Parsing(char case_filename[MAX_STRING_SIZE]) {
 
 void CConfig::SetHeader(SU2_COMPONENT val_software) const{
 
-  if ((iZone == 0) && (rank == MASTER_NODE)){
-    cout << endl << "-------------------------------------------------------------------------" << endl;
-    cout << "|    ___ _   _ ___                                                      |" << endl;
-    cout << "|   / __| | | |_  )   Release 7.5.1 \"Blackbird\"                         |" << endl;
-    cout << "|   \\__ \\ |_| |/ /                                                      |" << endl;
+  if ((iZone == 0) && (rank == MASTER_NODE)) {
+    cout << "\n";
+    cout << "-------------------------------------------------------------------------\n";
+    cout << "|    ___ _   _ ___                                                      |\n";
+    cout << "|   / __| | | |_  )   Release 7.5.1 \"Blackbird\"                         |\n";
+    cout << "|   \\__ \\ |_| |/ /                                                      |\n";
     switch (val_software) {
-    case SU2_COMPONENT::SU2_CFD: cout << "|   |___/\\___//___|   Suite (Computational Fluid Dynamics Code)         |" << endl; break;
-    case SU2_COMPONENT::SU2_DEF: cout << "|   |___/\\___//___|   Suite (Mesh Deformation Code)                     |" << endl; break;
-    case SU2_COMPONENT::SU2_DOT: cout << "|   |___/\\___//___|   Suite (Gradient Projection Code)                  |" << endl; break;
-    case SU2_COMPONENT::SU2_GEO: cout << "|   |___/\\___//___|   Suite (Geometry Definition Code)                  |" << endl; break;
-    case SU2_COMPONENT::SU2_SOL: cout << "|   |___/\\___//___|   Suite (Solution Exporting Code)                   |" << endl; break;
-    }
-
-    cout << "|                                                                       |" << endl;
-    cout <<"-------------------------------------------------------------------------" << endl;
-    cout << "| SU2 Project Website: https://su2code.github.io                        |" << endl;
-    cout << "|                                                                       |" << endl;
-    cout << "| The SU2 Project is maintained by the SU2 Foundation                   |" << endl;
-    cout << "| (http://su2foundation.org)                                            |" << endl;
-    cout <<"-------------------------------------------------------------------------" << endl;
-    cout << "| Copyright 2012-2023, SU2 Contributors                                 |" << endl;
-    cout << "|                                                                       |" << endl;
-    cout << "| SU2 is free software; you can redistribute it and/or                  |" << endl;
-    cout << "| modify it under the terms of the GNU Lesser General Public            |" << endl;
-    cout << "| License as published by the Free Software Foundation; either          |" << endl;
-    cout << "| version 2.1 of the License, or (at your option) any later version.    |" << endl;
-    cout << "|                                                                       |" << endl;
-    cout << "| SU2 is distributed in the hope that it will be useful,                |" << endl;
-    cout << "| but WITHOUT ANY WARRANTY; without even the implied warranty of        |" << endl;
-    cout << "| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |" << endl;
-    cout << "| Lesser General Public License for more details.                       |" << endl;
-    cout << "|                                                                       |" << endl;
-    cout << "| You should have received a copy of the GNU Lesser General Public      |" << endl;
-    cout << "| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |" << endl;
-    cout <<"-------------------------------------------------------------------------" << endl;
+    case SU2_COMPONENT::SU2_CFD: cout << "|   |___/\\___//___|   Suite (Computational Fluid Dynamics Code)         |\n"; break;
+    case SU2_COMPONENT::SU2_DEF: cout << "|   |___/\\___//___|   Suite (Mesh Deformation Code)                     |\n"; break;
+    case SU2_COMPONENT::SU2_DOT: cout << "|   |___/\\___//___|   Suite (Gradient Projection Code)                  |\n"; break;
+    case SU2_COMPONENT::SU2_GEO: cout << "|   |___/\\___//___|   Suite (Geometry Definition Code)                  |\n"; break;
+    case SU2_COMPONENT::SU2_SOL: cout << "|   |___/\\___//___|   Suite (Solution Exporting Code)                   |\n"; break;
+    }
+    cout << "|                                                                       |\n";
+    cout << "-------------------------------------------------------------------------\n";
+    cout << "| SU2 Project Website: https://su2code.github.io                        |\n";
+    cout << "|                                                                       |\n";
+    cout << "| The SU2 Project is maintained by the SU2 Foundation                   |\n";
+    cout << "| (http://su2foundation.org)                                            |\n";
+    cout << "-------------------------------------------------------------------------\n";
+    cout << "| Copyright 2012-2023, SU2 Contributors                                 |\n";
+    cout << "|                                                                       |\n";
+    cout << "| SU2 is free software; you can redistribute it and/or                  |\n";
+    cout << "| modify it under the terms of the GNU Lesser General Public            |\n";
+    cout << "| License as published by the Free Software Foundation; either          |\n";
+    cout << "| version 2.1 of the License, or (at your option) any later version.    |\n";
+    cout << "|                                                                       |\n";
+    cout << "| SU2 is distributed in the hope that it will be useful,                |\n";
+    cout << "| but WITHOUT ANY WARRANTY; without even the implied warranty of        |\n";
+    cout << "| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |\n";
+    cout << "| Lesser General Public License for more details.                       |\n";
+    cout << "|                                                                       |\n";
+    cout << "| You should have received a copy of the GNU Lesser General Public      |\n";
+    cout << "| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |\n";
+    cout << "-------------------------------------------------------------------------" << endl;
   }
 
 }
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index ab66b34b4c8..bb3f5c8cd07 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -1239,7 +1239,7 @@ void CFlowOutput::LoadHistoryDataScalar(const CConfig* config, const CSolver* co
 
 void CFlowOutput::SetVolumeOutputFieldsScalarSolution(const CConfig* config){
   /*--- Only place outputs of the "SOLUTION" group here. ---*/
-  
+
   switch (TurbModelFamily(config->GetKind_Turb_Model())) {
     case TURB_FAMILY::SA:
       AddVolumeOutput("NU_TILDE", "Nu_Tilde", "SOLUTION", "Spalart-Allmaras variable");
@@ -2594,13 +2594,13 @@ void CFlowOutput::WriteForcesBreakdown(const CConfig* config, const CSolver* flo
   ofstream file;
   file.open(fileName);
 
-  file << "\n-------------------------------------------------------------------------\n";
+  file << "\n";
+  file << "-------------------------------------------------------------------------\n";
   file << "|    ___ _   _ ___                                                      |\n";
   file << "|   / __| | | |_  )   Release 7.5.1 \"Blackbird\"                         |\n";
   file << "|   \\__ \\ |_| |/ /                                                      |\n";
   file << "|   |___/\\___//___|   Suite (Computational Fluid Dynamics Code)         |\n";
   file << "|                                                                       |\n";
-  // file << "|   Local date and time: " << dt << "                      |\n";
   file << "-------------------------------------------------------------------------\n";
   file << "| SU2 Project Website: https://su2code.github.io                        |\n";
   file << "|                                                                       |\n";
diff --git a/SU2_PY/change_version_number.py b/SU2_PY/change_version_number.py
index 43371c94d78..53e920bbf1d 100755
--- a/SU2_PY/change_version_number.py
+++ b/SU2_PY/change_version_number.py
@@ -112,16 +112,13 @@
 for fname in filelist:
     lines = open(fname, "r").readlines()
     for i, line in enumerate(lines):
-        if oldvers in line:
-            # Avoid breaking the formating of some testcase headers
-            if line.endswith("%\n"):
-                n = len(newvers) - len(oldvers)
-                lines[i] = line.replace(
-                    oldvers + " " * max(0, n), newvers + " " * max(0, -n)
-                )
-            else:
-                lines[i] = line.replace(oldvers, newvers)
-        lines[i] = line.replace(oldvers_q, newvers_q)
+        for old, new in zip((oldvers, oldvers_q), (newvers, newvers_q)):
+            # Avoid breaking the formating of some headers
+            if old + "  " in line:
+                n = len(new) - len(old)
+                lines[i] = line.replace(old + " " * max(0, n), new + " " * max(0, -n))
+            if old in line:
+                lines[i] = line.replace(old, new)
     f = open(fname, "w")
     f.writelines(lines)
     f.close()

From 241acfed8b1b61f35ea771c9ccf86cc66d628322 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 6 Aug 2023 15:21:32 -0700
Subject: [PATCH 631/656] fix some headers

---
 SU2_PY/change_version_number.py                    |  2 +-
 TestCases/aeroelastic/aeroelastic_NACA64A010.cfg   |  2 +-
 TestCases/cont_adj_euler/naca0012/inv_NACA0012.cfg |  2 +-
 .../cont_adj_euler/naca0012/inv_NACA0012_FD.cfg    |  2 +-
 .../naca0012/inv_NACA0012_discadj.cfg              |  2 +-
 TestCases/cont_adj_euler/wedge/inv_wedge_ROE.cfg   |  4 ++--
 .../wedge/inv_wedge_ROE_multiobj.cfg               |  2 +-
 .../cylinder/lam_cylinder.cfg                      |  2 +-
 .../naca0012_sub/lam_NACA0012.cfg                  |  2 +-
 .../naca0012_trans/lam_NACA0012.cfg                |  2 +-
 TestCases/cont_adj_rans/naca0012/turb_nasa.cfg     |  2 +-
 .../cont_adj_rans/naca0012/turb_nasa_binary.cfg    |  2 +-
 TestCases/cont_adj_rans/oneram6/turb_ONERAM6.cfg   |  2 +-
 .../cont_adj_rans/rae2822/turb_SA_RAE2822.cfg      |  2 +-
 TestCases/control_surface/inv_ONERAM6_moving.cfg   |  2 +-
 TestCases/control_surface/inv_ONERAM6_setting.cfg  |  2 +-
 .../coupled_cht/comp_2d/cht_2d_3cylinders.cfg      |  2 +-
 .../disc_adj_incomp_2d/cht_2d_3cylinders.cfg       |  2 +-
 .../coupled_cht/incomp_2d/cht_2d_3cylinders.cfg    |  2 +-
 .../incomp_2d_unsteady/cht_2d_3cylinders.cfg       |  2 +-
 .../cylindrical_ffd/def_cylindrical.cfg            |  2 +-
 TestCases/deformation/naca0012/def_NACA0012.cfg    |  2 +-
 .../deformation/naca0012/surface_file_NACA0012.cfg |  2 +-
 TestCases/deformation/rae2822/def_RAE2822.cfg      |  2 +-
 .../deformation/spherical_ffd/def_spherical.cfg    | 14 +++++++-------
 TestCases/disc_adj_heat/disc_adj_heat.cfg          |  2 +-
 TestCases/disc_adj_heat/primal.cfg                 |  2 +-
 .../nPoly4/fem_unst_cylinder_ADER.cfg              |  2 +-
 .../chtPinArray_2d/DA_configMaster.cfg             |  2 +-
 .../chtPinArray_2d/FD_configMaster.cfg             |  2 +-
 .../chtPinArray_2d/configMaster.cfg                |  2 +-
 .../chtPinArray_3d/configMaster.cfg                |  2 +-
 .../dp-adjoint_chtPinArray_2d/configMaster.cfg     |  2 +-
 .../inv_wedge_ROE_multiobj_combo.cfg               |  6 +++---
 .../steady_naca0012/inv_NACA0012_basic.cfg         |  2 +-
 .../pitching_naca64a010/turb_NACA64A010.cfg        |  2 +-
 .../pitching_oneram6/turb_ONERAM6.cfg              |  2 +-
 .../steady_rae2822/turb_SA_RAE2822.cfg             |  2 +-
 TestCases/polar/naca0012/inv_NACA0012.cfg          |  2 +-
 TestCases/rans/flatplate/turb_SA_flatplate.cfg     |  2 +-
 TestCases/rans/oneram6/turb_ONERAM6.cfg            |  2 +-
 TestCases/rans/oneram6/turb_ONERAM6_vc.cfg         |  2 +-
 TestCases/rans/rae2822/turb_SA_RAE2822.cfg         |  2 +-
 TestCases/rans/rae2822/turb_SST_RAE2822.cfg        |  2 +-
 TestCases/rans/rae2822/turb_SST_SUST_RAE2822.cfg   |  2 +-
 TestCases/rans/s809/trans_s809.cfg                 |  2 +-
 TestCases/rans/s809/turb_S809.cfg                  |  2 +-
 TestCases/rans/vki_turbine/turb_vki.cfg            |  2 +-
 .../incompressible_steady/config.cfg               |  2 +-
 .../incompressible_steady/configCircle.cfg         |  2 +-
 .../incompressible_steady/configOut.cfg            |  2 +-
 .../incompressible_unsteady/config.cfg             |  2 +-
 .../incompressible_unsteady/configCircle.cfg       |  2 +-
 .../incompressible_unsteady/configOut.cfg          |  2 +-
 .../species_transport/multizone/configMaster.cfg   |  2 +-
 .../pitching_NACA64A010.cfg                        |  2 +-
 .../plunging_naca0012/plunging_NACA0012.cfg        |  2 +-
 57 files changed, 66 insertions(+), 66 deletions(-)

diff --git a/SU2_PY/change_version_number.py b/SU2_PY/change_version_number.py
index 53e920bbf1d..49dda8e54fe 100755
--- a/SU2_PY/change_version_number.py
+++ b/SU2_PY/change_version_number.py
@@ -117,7 +117,7 @@
             if old + "  " in line:
                 n = len(new) - len(old)
                 lines[i] = line.replace(old + " " * max(0, n), new + " " * max(0, -n))
-            if old in line:
+            elif old in line:
                 lines[i] = line.replace(old, new)
     f = open(fname, "w")
     f.writelines(lines)
diff --git a/TestCases/aeroelastic/aeroelastic_NACA64A010.cfg b/TestCases/aeroelastic/aeroelastic_NACA64A010.cfg
index 8f7fdb4048d..cbb53e213ef 100644
--- a/TestCases/aeroelastic/aeroelastic_NACA64A010.cfg
+++ b/TestCases/aeroelastic/aeroelastic_NACA64A010.cfg
@@ -5,7 +5,7 @@
 % Author: Santiago Padron                                                      %
 % Institution: Stanford University                                             %
 % Date: 07-09-15                                                               %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_euler/naca0012/inv_NACA0012.cfg b/TestCases/cont_adj_euler/naca0012/inv_NACA0012.cfg
index 292545e17be..f8ba55367fc 100644
--- a/TestCases/cont_adj_euler/naca0012/inv_NACA0012.cfg
+++ b/TestCases/cont_adj_euler/naca0012/inv_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_euler/naca0012/inv_NACA0012_FD.cfg b/TestCases/cont_adj_euler/naca0012/inv_NACA0012_FD.cfg
index fca45524600..32c74d5c1eb 100644
--- a/TestCases/cont_adj_euler/naca0012/inv_NACA0012_FD.cfg
+++ b/TestCases/cont_adj_euler/naca0012/inv_NACA0012_FD.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg b/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg
index 824e6c15caa..172fdb8dc6b 100644
--- a/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg
+++ b/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_euler/wedge/inv_wedge_ROE.cfg b/TestCases/cont_adj_euler/wedge/inv_wedge_ROE.cfg
index a3f3e9e2ecb..b659a44e6d2 100644
--- a/TestCases/cont_adj_euler/wedge/inv_wedge_ROE.cfg
+++ b/TestCases/cont_adj_euler/wedge/inv_wedge_ROE.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2012.10.07                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -107,7 +107,7 @@ GRAD_OBJFUNC_FILENAME= of_grad.dat
 SURFACE_FILENAME= surface_flow
 SURFACE_ADJ_FILENAME= surface_adjoint
 OUTPUT_WRT_FREQ= 250
-SCREEN_OUTPUT = (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_GEO, SENS_AOA) 
+SCREEN_OUTPUT = (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_GEO, SENS_AOA)
 OUTPUT_FILES=(RESTART_ASCII)
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
diff --git a/TestCases/cont_adj_euler/wedge/inv_wedge_ROE_multiobj.cfg b/TestCases/cont_adj_euler/wedge/inv_wedge_ROE_multiobj.cfg
index 40c8ba5ccee..89e84be2421 100644
--- a/TestCases/cont_adj_euler/wedge/inv_wedge_ROE_multiobj.cfg
+++ b/TestCases/cont_adj_euler/wedge/inv_wedge_ROE_multiobj.cfg
@@ -6,7 +6,7 @@
 % Author: H.L. Kline, modified from inviscid wedge by Thomas D. Economon       %
 % Institution: Stanford University                                             %
 % Date: 2018.01.07                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_navierstokes/cylinder/lam_cylinder.cfg b/TestCases/cont_adj_navierstokes/cylinder/lam_cylinder.cfg
index 067f9fd25bc..a77f8c0fcaf 100644
--- a/TestCases/cont_adj_navierstokes/cylinder/lam_cylinder.cfg
+++ b/TestCases/cont_adj_navierstokes/cylinder/lam_cylinder.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.03.01                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_navierstokes/naca0012_sub/lam_NACA0012.cfg b/TestCases/cont_adj_navierstokes/naca0012_sub/lam_NACA0012.cfg
index 7c0ac2cf859..53e3202e8ea 100644
--- a/TestCases/cont_adj_navierstokes/naca0012_sub/lam_NACA0012.cfg
+++ b/TestCases/cont_adj_navierstokes/naca0012_sub/lam_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: Jul 18th, 2014                                                         %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_navierstokes/naca0012_trans/lam_NACA0012.cfg b/TestCases/cont_adj_navierstokes/naca0012_trans/lam_NACA0012.cfg
index 919e841ad46..7cb5eee3de7 100644
--- a/TestCases/cont_adj_navierstokes/naca0012_trans/lam_NACA0012.cfg
+++ b/TestCases/cont_adj_navierstokes/naca0012_trans/lam_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: Jul 18th, 2014                                                         %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_rans/naca0012/turb_nasa.cfg b/TestCases/cont_adj_rans/naca0012/turb_nasa.cfg
index ca0506980a6..628a4db8a5d 100644
--- a/TestCases/cont_adj_rans/naca0012/turb_nasa.cfg
+++ b/TestCases/cont_adj_rans/naca0012/turb_nasa.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.03.01                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_rans/naca0012/turb_nasa_binary.cfg b/TestCases/cont_adj_rans/naca0012/turb_nasa_binary.cfg
index df636cd5fcd..0ce12b1f16f 100644
--- a/TestCases/cont_adj_rans/naca0012/turb_nasa_binary.cfg
+++ b/TestCases/cont_adj_rans/naca0012/turb_nasa_binary.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.03.01                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_rans/oneram6/turb_ONERAM6.cfg b/TestCases/cont_adj_rans/oneram6/turb_ONERAM6.cfg
index 2e52829fc48..7a99624cf9e 100644
--- a/TestCases/cont_adj_rans/oneram6/turb_ONERAM6.cfg
+++ b/TestCases/cont_adj_rans/oneram6/turb_ONERAM6.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.03.01                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_rans/rae2822/turb_SA_RAE2822.cfg b/TestCases/cont_adj_rans/rae2822/turb_SA_RAE2822.cfg
index acb177feb6d..fb2ea6d9e65 100644
--- a/TestCases/cont_adj_rans/rae2822/turb_SA_RAE2822.cfg
+++ b/TestCases/cont_adj_rans/rae2822/turb_SA_RAE2822.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/control_surface/inv_ONERAM6_moving.cfg b/TestCases/control_surface/inv_ONERAM6_moving.cfg
index d9db83c262d..1119269cce6 100644
--- a/TestCases/control_surface/inv_ONERAM6_moving.cfg
+++ b/TestCases/control_surface/inv_ONERAM6_moving.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 09.07.2011                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/control_surface/inv_ONERAM6_setting.cfg b/TestCases/control_surface/inv_ONERAM6_setting.cfg
index d29f8702234..19e10e6bfef 100644
--- a/TestCases/control_surface/inv_ONERAM6_setting.cfg
+++ b/TestCases/control_surface/inv_ONERAM6_setting.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 09.07.2011                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/coupled_cht/comp_2d/cht_2d_3cylinders.cfg b/TestCases/coupled_cht/comp_2d/cht_2d_3cylinders.cfg
index 01bdcc333fa..c202ce7924e 100644
--- a/TestCases/coupled_cht/comp_2d/cht_2d_3cylinders.cfg
+++ b/TestCases/coupled_cht/comp_2d/cht_2d_3cylinders.cfg
@@ -5,7 +5,7 @@
 % Author: O. Burghardt                                                          %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 6, 2020                                                         %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/coupled_cht/disc_adj_incomp_2d/cht_2d_3cylinders.cfg b/TestCases/coupled_cht/disc_adj_incomp_2d/cht_2d_3cylinders.cfg
index 38eb52af3e8..9db2e157dc7 100644
--- a/TestCases/coupled_cht/disc_adj_incomp_2d/cht_2d_3cylinders.cfg
+++ b/TestCases/coupled_cht/disc_adj_incomp_2d/cht_2d_3cylinders.cfg
@@ -5,7 +5,7 @@
 % Author: O. Burghardt, T. Economon                                             %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: August 8, 2019                                                          %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/coupled_cht/incomp_2d/cht_2d_3cylinders.cfg b/TestCases/coupled_cht/incomp_2d/cht_2d_3cylinders.cfg
index 0db56062790..99173751b46 100644
--- a/TestCases/coupled_cht/incomp_2d/cht_2d_3cylinders.cfg
+++ b/TestCases/coupled_cht/incomp_2d/cht_2d_3cylinders.cfg
@@ -5,7 +5,7 @@
 % Author: O. Burghardt, T. Economon                                             %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: August 8, 2019                                                          %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/coupled_cht/incomp_2d_unsteady/cht_2d_3cylinders.cfg b/TestCases/coupled_cht/incomp_2d_unsteady/cht_2d_3cylinders.cfg
index bb06f67b7ee..5e889b88a6d 100644
--- a/TestCases/coupled_cht/incomp_2d_unsteady/cht_2d_3cylinders.cfg
+++ b/TestCases/coupled_cht/incomp_2d_unsteady/cht_2d_3cylinders.cfg
@@ -5,7 +5,7 @@
 % Author: O. Burghardt, T. Economon                                             %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: August 8, 2019                                                          %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/deformation/cylindrical_ffd/def_cylindrical.cfg b/TestCases/deformation/cylindrical_ffd/def_cylindrical.cfg
index a22c4745843..8677ee14b99 100644
--- a/TestCases/deformation/cylindrical_ffd/def_cylindrical.cfg
+++ b/TestCases/deformation/cylindrical_ffd/def_cylindrical.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/deformation/naca0012/def_NACA0012.cfg b/TestCases/deformation/naca0012/def_NACA0012.cfg
index 9f5d4a7a883..a44a8f6aabf 100644
--- a/TestCases/deformation/naca0012/def_NACA0012.cfg
+++ b/TestCases/deformation/naca0012/def_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/deformation/naca0012/surface_file_NACA0012.cfg b/TestCases/deformation/naca0012/surface_file_NACA0012.cfg
index 8896ecd9454..09d7aefa518 100644
--- a/TestCases/deformation/naca0012/surface_file_NACA0012.cfg
+++ b/TestCases/deformation/naca0012/surface_file_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/deformation/rae2822/def_RAE2822.cfg b/TestCases/deformation/rae2822/def_RAE2822.cfg
index 831a14a2ee6..a2bffdaac0d 100644
--- a/TestCases/deformation/rae2822/def_RAE2822.cfg
+++ b/TestCases/deformation/rae2822/def_RAE2822.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/deformation/spherical_ffd/def_spherical.cfg b/TestCases/deformation/spherical_ffd/def_spherical.cfg
index d8ee5fdb74d..aef3ede987d 100644
--- a/TestCases/deformation/spherical_ffd/def_spherical.cfg
+++ b/TestCases/deformation/spherical_ffd/def_spherical.cfg
@@ -5,13 +5,13 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
-SOLVER= EULER 
+SOLVER= EULER
 MATH_PROBLEM= DIRECT
 RESTART_SOL= NO
 SYSTEM_MEASUREMENTS= US
@@ -22,7 +22,7 @@ MACH_NUMBER= 0.8
 AOA= 0.0
 SIDESLIP_ANGLE= 0.0
 FREESTREAM_TEMPERATURE= 518.67
-FREESTREAM_PRESSURE= 2116.216 
+FREESTREAM_PRESSURE= 2116.216
 
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
@@ -46,7 +46,7 @@ MARKER_DESIGNING = ( SPHERE )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
-NUM_METHOD_GRAD= GREEN_GAUSS 
+NUM_METHOD_GRAD= GREEN_GAUSS
 CFL_NUMBER= 1.0
 CFL_ADAPT= NO
 CFL_ADAPT_PARAM= ( 1.0, 1.0, 1.0, 10.0 )
@@ -74,10 +74,10 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
-DV_KIND= FFD_CONTROL_POINT 
+DV_KIND= FFD_CONTROL_POINT
 DV_MARKER= ( SPHERE )
 DV_PARAM= ( SPHERE_BOX, 0, 3, 2, 1.0, 0.0, 0.0 )
-DV_VALUE= 0.1 
+DV_VALUE= 0.1
 
 % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
 %
@@ -108,7 +108,7 @@ CONV_STARTITER= 10
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
 MESH_FILENAME= spherical.su2
-MESH_FORMAT= SU2 
+MESH_FORMAT= SU2
 MESH_OUT_FILENAME= mesh_out.su2
 SOLUTION_FILENAME= solution_flow.dat
 SOLUTION_ADJ_FILENAME= solution_adj.dat
diff --git a/TestCases/disc_adj_heat/disc_adj_heat.cfg b/TestCases/disc_adj_heat/disc_adj_heat.cfg
index 2b3ad200e75..4d40da5daaa 100644
--- a/TestCases/disc_adj_heat/disc_adj_heat.cfg
+++ b/TestCases/disc_adj_heat/disc_adj_heat.cfg
@@ -6,7 +6,7 @@
 % Author: Ole Burghardt                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: November 26th, 2018                                                     %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/disc_adj_heat/primal.cfg b/TestCases/disc_adj_heat/primal.cfg
index 4fb1d63fbd4..8237cdbd8df 100644
--- a/TestCases/disc_adj_heat/primal.cfg
+++ b/TestCases/disc_adj_heat/primal.cfg
@@ -5,7 +5,7 @@
 % Author: Ole Burghardt                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: November 26th, 2018                                                     %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/hom_navierstokes/UnsteadyCylinder/nPoly4/fem_unst_cylinder_ADER.cfg b/TestCases/hom_navierstokes/UnsteadyCylinder/nPoly4/fem_unst_cylinder_ADER.cfg
index 19c4b24d69a..6724df7250c 100644
--- a/TestCases/hom_navierstokes/UnsteadyCylinder/nPoly4/fem_unst_cylinder_ADER.cfg
+++ b/TestCases/hom_navierstokes/UnsteadyCylinder/nPoly4/fem_unst_cylinder_ADER.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/DA_configMaster.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/DA_configMaster.cfg
index fb41015dfb7..e67bf89d2a2 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/DA_configMaster.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/DA_configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                           %
 % Institution: Robert Bosch GmbH                                                %
 % Date: 2020.12.15                                                              %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/FD_configMaster.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/FD_configMaster.cfg
index 42aea7ba914..0afccda64c3 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/FD_configMaster.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/FD_configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                           %
 % Institution: Robert Bosch GmbH                                                %
 % Date: 2020.12.15                                                              %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configMaster.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configMaster.cfg
index 8e66cb0ab71..91ea8aee874 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configMaster.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                           %
 % Institution: Robert Bosch GmbH                                                %
 % Date: 2020.12.15                                                              %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configMaster.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configMaster.cfg
index 6fcbc300a41..db62020b22f 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configMaster.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                           %
 % Institution: Robert Bosch GmbH                                                %
 % Date: 2020.12.15                                                              %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configMaster.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configMaster.cfg
index 71fb7a2d777..508a000466c 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configMaster.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                           %
 % Institution: None                                                             %
 % Date: 2022.02.10                                                              %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj_combo.cfg b/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj_combo.cfg
index 462d3935872..77e758b4b99 100644
--- a/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj_combo.cfg
+++ b/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj_combo.cfg
@@ -2,15 +2,15 @@
 %                                                                              %
 % SU2 configuration file                                                       %
 % Case description: Multi-objective optimization for outflow averaged pressure %
-%   and a quadratic penalty function on a surface drag constraint, using       % 
-%   combined evaluation of the gradient rather than separate gradient          % 
+%   and a quadratic penalty function on a surface drag constraint, using       %
+%   combined evaluation of the gradient rather than separate gradient          %
 %   evaluations for each function.				               %
 %   For the definition of the penalty function see 'obj_p' method defined in   %
 %   SU2/SU2_PY/SU2/eval/designs.py                                             %
 % Author: H.L. Kline, modified from inviscid wedge by Thomas D. Economon       %
 % Institution: Stanford University                                             %
 % Date: 2018.01.07                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_euler/steady_naca0012/inv_NACA0012_basic.cfg b/TestCases/optimization_euler/steady_naca0012/inv_NACA0012_basic.cfg
index 933786afaa1..e0abfe78057 100644
--- a/TestCases/optimization_euler/steady_naca0012/inv_NACA0012_basic.cfg
+++ b/TestCases/optimization_euler/steady_naca0012/inv_NACA0012_basic.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.09.29                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_rans/pitching_naca64a010/turb_NACA64A010.cfg b/TestCases/optimization_rans/pitching_naca64a010/turb_NACA64A010.cfg
index 0d327d0e90f..9f42badaa70 100644
--- a/TestCases/optimization_rans/pitching_naca64a010/turb_NACA64A010.cfg
+++ b/TestCases/optimization_rans/pitching_naca64a010/turb_NACA64A010.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_rans/pitching_oneram6/turb_ONERAM6.cfg b/TestCases/optimization_rans/pitching_oneram6/turb_ONERAM6.cfg
index ce6db99717a..b8dfed828bf 100644
--- a/TestCases/optimization_rans/pitching_oneram6/turb_ONERAM6.cfg
+++ b/TestCases/optimization_rans/pitching_oneram6/turb_ONERAM6.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_rans/steady_rae2822/turb_SA_RAE2822.cfg b/TestCases/optimization_rans/steady_rae2822/turb_SA_RAE2822.cfg
index 3e3baaa6fc9..bcf9093b451 100644
--- a/TestCases/optimization_rans/steady_rae2822/turb_SA_RAE2822.cfg
+++ b/TestCases/optimization_rans/steady_rae2822/turb_SA_RAE2822.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/polar/naca0012/inv_NACA0012.cfg b/TestCases/polar/naca0012/inv_NACA0012.cfg
index b083add885f..edf3775394c 100644
--- a/TestCases/polar/naca0012/inv_NACA0012.cfg
+++ b/TestCases/polar/naca0012/inv_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/flatplate/turb_SA_flatplate.cfg b/TestCases/rans/flatplate/turb_SA_flatplate.cfg
index eed7ca2f152..d62701dd5c4 100644
--- a/TestCases/rans/flatplate/turb_SA_flatplate.cfg
+++ b/TestCases/rans/flatplate/turb_SA_flatplate.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.10                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/oneram6/turb_ONERAM6.cfg b/TestCases/rans/oneram6/turb_ONERAM6.cfg
index ebf2c93d89a..4dc93e48803 100644
--- a/TestCases/rans/oneram6/turb_ONERAM6.cfg
+++ b/TestCases/rans/oneram6/turb_ONERAM6.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.14                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/oneram6/turb_ONERAM6_vc.cfg b/TestCases/rans/oneram6/turb_ONERAM6_vc.cfg
index bb084427e36..16ba7484c52 100644
--- a/TestCases/rans/oneram6/turb_ONERAM6_vc.cfg
+++ b/TestCases/rans/oneram6/turb_ONERAM6_vc.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.14                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/rae2822/turb_SA_RAE2822.cfg b/TestCases/rans/rae2822/turb_SA_RAE2822.cfg
index a2e55937a88..73397fe91a1 100644
--- a/TestCases/rans/rae2822/turb_SA_RAE2822.cfg
+++ b/TestCases/rans/rae2822/turb_SA_RAE2822.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/rae2822/turb_SST_RAE2822.cfg b/TestCases/rans/rae2822/turb_SST_RAE2822.cfg
index e867e993ec2..f28e58a14ad 100644
--- a/TestCases/rans/rae2822/turb_SST_RAE2822.cfg
+++ b/TestCases/rans/rae2822/turb_SST_RAE2822.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/rae2822/turb_SST_SUST_RAE2822.cfg b/TestCases/rans/rae2822/turb_SST_SUST_RAE2822.cfg
index 42f3ec6079e..3d95d9c82b3 100644
--- a/TestCases/rans/rae2822/turb_SST_SUST_RAE2822.cfg
+++ b/TestCases/rans/rae2822/turb_SST_SUST_RAE2822.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/s809/trans_s809.cfg b/TestCases/rans/s809/trans_s809.cfg
index 733d2729700..d807bd0f496 100644
--- a/TestCases/rans/s809/trans_s809.cfg
+++ b/TestCases/rans/s809/trans_s809.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/s809/turb_S809.cfg b/TestCases/rans/s809/turb_S809.cfg
index cef80f37f0d..6691fa178a0 100644
--- a/TestCases/rans/s809/turb_S809.cfg
+++ b/TestCases/rans/s809/turb_S809.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/vki_turbine/turb_vki.cfg b/TestCases/rans/vki_turbine/turb_vki.cfg
index 94a68ccacd1..c808a08bdce 100644
--- a/TestCases/rans/vki_turbine/turb_vki.cfg
+++ b/TestCases/rans/vki_turbine/turb_vki.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios, Thomas D. Economon	                           %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/incompressible_steady/config.cfg b/TestCases/sliding_interface/incompressible_steady/config.cfg
index 0abe97efa10..a886c9fea2f 100644
--- a/TestCases/sliding_interface/incompressible_steady/config.cfg
+++ b/TestCases/sliding_interface/incompressible_steady/config.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/incompressible_steady/configCircle.cfg b/TestCases/sliding_interface/incompressible_steady/configCircle.cfg
index 82943af7b81..c9a3d5205e4 100644
--- a/TestCases/sliding_interface/incompressible_steady/configCircle.cfg
+++ b/TestCases/sliding_interface/incompressible_steady/configCircle.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/incompressible_steady/configOut.cfg b/TestCases/sliding_interface/incompressible_steady/configOut.cfg
index d19fb2e702c..9608668cbd4 100644
--- a/TestCases/sliding_interface/incompressible_steady/configOut.cfg
+++ b/TestCases/sliding_interface/incompressible_steady/configOut.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/incompressible_unsteady/config.cfg b/TestCases/sliding_interface/incompressible_unsteady/config.cfg
index 4c3221eff70..7dee6aaf3a5 100644
--- a/TestCases/sliding_interface/incompressible_unsteady/config.cfg
+++ b/TestCases/sliding_interface/incompressible_unsteady/config.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg b/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg
index 9bc21717854..b6185490368 100644
--- a/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg
+++ b/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg b/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg
index 29941635096..a9a3d03511c 100644
--- a/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg
+++ b/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/species_transport/multizone/configMaster.cfg b/TestCases/species_transport/multizone/configMaster.cfg
index 4f4f1ca2cae..37918d3923b 100644
--- a/TestCases/species_transport/multizone/configMaster.cfg
+++ b/TestCases/species_transport/multizone/configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: N. Beishuizen                                                         %
 % Institution: Technische Universiteit Eindhoven                                %
 % Date: November 1, 2022                                                        %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/unsteady/pitching_naca64a010_euler/pitching_NACA64A010.cfg b/TestCases/unsteady/pitching_naca64a010_euler/pitching_NACA64A010.cfg
index bd7083dd7b1..f7aefbf144f 100644
--- a/TestCases/unsteady/pitching_naca64a010_euler/pitching_NACA64A010.cfg
+++ b/TestCases/unsteady/pitching_naca64a010_euler/pitching_NACA64A010.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/unsteady/plunging_naca0012/plunging_NACA0012.cfg b/TestCases/unsteady/plunging_naca0012/plunging_NACA0012.cfg
index c43c14882e5..dcc907f5bca 100644
--- a/TestCases/unsteady/plunging_naca0012/plunging_NACA0012.cfg
+++ b/TestCases/unsteady/plunging_naca0012/plunging_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: Jun 12, 2014                                                           %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 7.5.1 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 

From e29988c750639dbc562964cab0d2a91dee4e5fb5 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 6 Aug 2023 15:23:45 -0700
Subject: [PATCH 632/656] one more fix

---
 TestCases/nicf/datadriven/datadriven_nozzle.cfg | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/TestCases/nicf/datadriven/datadriven_nozzle.cfg b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
index 32f16319c5f..46e3346ea60 100644
--- a/TestCases/nicf/datadriven/datadriven_nozzle.cfg
+++ b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
@@ -7,7 +7,7 @@
 % Author: Evert Bunschoten                                                     %
 % Institution: Delft University of Technology                                  %
 % Date: 2022.10.8                                                              %
-% File Version  7.5.1 Blackbird                                                %
+% File Version  7.5.1 "Blackbird"                                              %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 

From bd56f5bfcba6eb658f17f4a26eada9946a14a710 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Sun, 6 Aug 2023 15:40:43 -0700
Subject: [PATCH 633/656] Apply suggestions from code review

---
 TestCases/coupled_cht/comp_2d/cht_2d_3cylinders.cfg             | 2 +-
 TestCases/coupled_cht/disc_adj_incomp_2d/cht_2d_3cylinders.cfg  | 2 +-
 TestCases/coupled_cht/incomp_2d/cht_2d_3cylinders.cfg           | 2 +-
 TestCases/coupled_cht/incomp_2d_unsteady/cht_2d_3cylinders.cfg  | 2 +-
 TestCases/disc_adj_heat/disc_adj_heat.cfg                       | 2 +-
 TestCases/disc_adj_heat/primal.cfg                              | 2 +-
 .../streamwise_periodic/chtPinArray_2d/DA_configMaster.cfg      | 2 +-
 .../streamwise_periodic/chtPinArray_2d/FD_configMaster.cfg      | 2 +-
 .../streamwise_periodic/chtPinArray_2d/configMaster.cfg         | 2 +-
 .../streamwise_periodic/chtPinArray_3d/configMaster.cfg         | 2 +-
 .../dp-adjoint_chtPinArray_2d/configMaster.cfg                  | 2 +-
 TestCases/sliding_interface/incompressible_steady/config.cfg    | 2 +-
 .../sliding_interface/incompressible_steady/configCircle.cfg    | 2 +-
 TestCases/sliding_interface/incompressible_steady/configOut.cfg | 2 +-
 TestCases/sliding_interface/incompressible_unsteady/config.cfg  | 2 +-
 .../sliding_interface/incompressible_unsteady/configCircle.cfg  | 2 +-
 .../sliding_interface/incompressible_unsteady/configOut.cfg     | 2 +-
 TestCases/species_transport/multizone/configMaster.cfg          | 2 +-
 18 files changed, 18 insertions(+), 18 deletions(-)

diff --git a/TestCases/coupled_cht/comp_2d/cht_2d_3cylinders.cfg b/TestCases/coupled_cht/comp_2d/cht_2d_3cylinders.cfg
index c202ce7924e..01bdcc333fa 100644
--- a/TestCases/coupled_cht/comp_2d/cht_2d_3cylinders.cfg
+++ b/TestCases/coupled_cht/comp_2d/cht_2d_3cylinders.cfg
@@ -5,7 +5,7 @@
 % Author: O. Burghardt                                                          %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 6, 2020                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 7.5.1 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/coupled_cht/disc_adj_incomp_2d/cht_2d_3cylinders.cfg b/TestCases/coupled_cht/disc_adj_incomp_2d/cht_2d_3cylinders.cfg
index 9db2e157dc7..38eb52af3e8 100644
--- a/TestCases/coupled_cht/disc_adj_incomp_2d/cht_2d_3cylinders.cfg
+++ b/TestCases/coupled_cht/disc_adj_incomp_2d/cht_2d_3cylinders.cfg
@@ -5,7 +5,7 @@
 % Author: O. Burghardt, T. Economon                                             %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: August 8, 2019                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 7.5.1 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/coupled_cht/incomp_2d/cht_2d_3cylinders.cfg b/TestCases/coupled_cht/incomp_2d/cht_2d_3cylinders.cfg
index 99173751b46..0db56062790 100644
--- a/TestCases/coupled_cht/incomp_2d/cht_2d_3cylinders.cfg
+++ b/TestCases/coupled_cht/incomp_2d/cht_2d_3cylinders.cfg
@@ -5,7 +5,7 @@
 % Author: O. Burghardt, T. Economon                                             %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: August 8, 2019                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 7.5.1 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/coupled_cht/incomp_2d_unsteady/cht_2d_3cylinders.cfg b/TestCases/coupled_cht/incomp_2d_unsteady/cht_2d_3cylinders.cfg
index 5e889b88a6d..bb06f67b7ee 100644
--- a/TestCases/coupled_cht/incomp_2d_unsteady/cht_2d_3cylinders.cfg
+++ b/TestCases/coupled_cht/incomp_2d_unsteady/cht_2d_3cylinders.cfg
@@ -5,7 +5,7 @@
 % Author: O. Burghardt, T. Economon                                             %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: August 8, 2019                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 7.5.1 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/disc_adj_heat/disc_adj_heat.cfg b/TestCases/disc_adj_heat/disc_adj_heat.cfg
index 4d40da5daaa..2b3ad200e75 100644
--- a/TestCases/disc_adj_heat/disc_adj_heat.cfg
+++ b/TestCases/disc_adj_heat/disc_adj_heat.cfg
@@ -6,7 +6,7 @@
 % Author: Ole Burghardt                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: November 26th, 2018                                                     %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 7.5.1 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/disc_adj_heat/primal.cfg b/TestCases/disc_adj_heat/primal.cfg
index 8237cdbd8df..4fb1d63fbd4 100644
--- a/TestCases/disc_adj_heat/primal.cfg
+++ b/TestCases/disc_adj_heat/primal.cfg
@@ -5,7 +5,7 @@
 % Author: Ole Burghardt                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: November 26th, 2018                                                     %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 7.5.1 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/DA_configMaster.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/DA_configMaster.cfg
index e67bf89d2a2..fb41015dfb7 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/DA_configMaster.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/DA_configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                           %
 % Institution: Robert Bosch GmbH                                                %
 % Date: 2020.12.15                                                              %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 7.5.1 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/FD_configMaster.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/FD_configMaster.cfg
index 0afccda64c3..42aea7ba914 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/FD_configMaster.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/FD_configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                           %
 % Institution: Robert Bosch GmbH                                                %
 % Date: 2020.12.15                                                              %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 7.5.1 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configMaster.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configMaster.cfg
index 91ea8aee874..8e66cb0ab71 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configMaster.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                           %
 % Institution: Robert Bosch GmbH                                                %
 % Date: 2020.12.15                                                              %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 7.5.1 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configMaster.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configMaster.cfg
index db62020b22f..6fcbc300a41 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configMaster.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                           %
 % Institution: Robert Bosch GmbH                                                %
 % Date: 2020.12.15                                                              %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 7.5.1 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configMaster.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configMaster.cfg
index 508a000466c..71fb7a2d777 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configMaster.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                           %
 % Institution: None                                                             %
 % Date: 2022.02.10                                                              %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 7.5.1 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/incompressible_steady/config.cfg b/TestCases/sliding_interface/incompressible_steady/config.cfg
index a886c9fea2f..0abe97efa10 100644
--- a/TestCases/sliding_interface/incompressible_steady/config.cfg
+++ b/TestCases/sliding_interface/incompressible_steady/config.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 7.5.1 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/incompressible_steady/configCircle.cfg b/TestCases/sliding_interface/incompressible_steady/configCircle.cfg
index c9a3d5205e4..82943af7b81 100644
--- a/TestCases/sliding_interface/incompressible_steady/configCircle.cfg
+++ b/TestCases/sliding_interface/incompressible_steady/configCircle.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 7.5.1 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/incompressible_steady/configOut.cfg b/TestCases/sliding_interface/incompressible_steady/configOut.cfg
index 9608668cbd4..d19fb2e702c 100644
--- a/TestCases/sliding_interface/incompressible_steady/configOut.cfg
+++ b/TestCases/sliding_interface/incompressible_steady/configOut.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 7.5.1 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/incompressible_unsteady/config.cfg b/TestCases/sliding_interface/incompressible_unsteady/config.cfg
index 7dee6aaf3a5..4c3221eff70 100644
--- a/TestCases/sliding_interface/incompressible_unsteady/config.cfg
+++ b/TestCases/sliding_interface/incompressible_unsteady/config.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 7.5.1 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg b/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg
index b6185490368..9bc21717854 100644
--- a/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg
+++ b/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 7.5.1 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg b/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg
index a9a3d03511c..29941635096 100644
--- a/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg
+++ b/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 7.5.1 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/species_transport/multizone/configMaster.cfg b/TestCases/species_transport/multizone/configMaster.cfg
index 37918d3923b..4f4f1ca2cae 100644
--- a/TestCases/species_transport/multizone/configMaster.cfg
+++ b/TestCases/species_transport/multizone/configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: N. Beishuizen                                                         %
 % Institution: Technische Universiteit Eindhoven                                %
 % Date: November 1, 2022                                                        %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 7.5.1 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %

From 0758281aaae6956513fe927951931ba87f4a2131 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 6 Aug 2023 15:44:51 -0700
Subject: [PATCH 634/656] fix warning

---
 SU2_PY/change_version_number.py | 8 ++++----
 1 file changed, 4 insertions(+), 4 deletions(-)

diff --git a/SU2_PY/change_version_number.py b/SU2_PY/change_version_number.py
index 49dda8e54fe..db448d73173 100755
--- a/SU2_PY/change_version_number.py
+++ b/SU2_PY/change_version_number.py
@@ -110,7 +110,8 @@
 
 # Loop through and correct all files
 for fname in filelist:
-    lines = open(fname, "r").readlines()
+    with open(fname, "r") as f:
+        lines = f.readlines()
     for i, line in enumerate(lines):
         for old, new in zip((oldvers, oldvers_q), (newvers, newvers_q)):
             # Avoid breaking the formating of some headers
@@ -119,8 +120,7 @@
                 lines[i] = line.replace(old + " " * max(0, n), new + " " * max(0, -n))
             elif old in line:
                 lines[i] = line.replace(old, new)
-    f = open(fname, "w")
-    f.writelines(lines)
-    f.close()
+    with open(fname, "w") as f:
+        f.writelines(lines)
 
 os.system("rm -rf version.txt")

From 3278ea98b19f9376ac20f152cbda7e1ff93b3aa2 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 6 Aug 2023 17:59:42 -0700
Subject: [PATCH 635/656] PR comments

---
 SU2_CFD/src/output/CNEMOCompOutput.cpp | 8 +++++---
 1 file changed, 5 insertions(+), 3 deletions(-)

diff --git a/SU2_CFD/src/output/CNEMOCompOutput.cpp b/SU2_CFD/src/output/CNEMOCompOutput.cpp
index 9902192bbc9..d5bb669ec8b 100644
--- a/SU2_CFD/src/output/CNEMOCompOutput.cpp
+++ b/SU2_CFD/src/output/CNEMOCompOutput.cpp
@@ -317,13 +317,10 @@ void CNEMOCompOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolv
 
   SetVolumeOutputValue("MOMENTUM-X", iPoint, Node_Flow->GetSolution(iPoint, nSpecies));
   SetVolumeOutputValue("MOMENTUM-Y", iPoint, Node_Flow->GetSolution(iPoint, nSpecies+1));
-  SetVolumeOutputValue("VELOCITY-X", iPoint, Node_Flow->GetPrimitive(iPoint, nSpecies));
-  SetVolumeOutputValue("VELOCITY-Y", iPoint, Node_Flow->GetPrimitive(iPoint, nSpecies+1));
   if (nDim == 3){
     SetVolumeOutputValue("MOMENTUM-Z", iPoint, Node_Flow->GetSolution(iPoint, nSpecies+2));
     SetVolumeOutputValue("ENERGY",     iPoint, Node_Flow->GetSolution(iPoint, nSpecies+3));
     SetVolumeOutputValue("ENERGY_VE",  iPoint, Node_Flow->GetSolution(iPoint, nSpecies+4));
-    SetVolumeOutputValue("VELOCITY-Z", iPoint, Node_Flow->GetPrimitive(iPoint, nSpecies+2));
   } else {
     SetVolumeOutputValue("ENERGY",     iPoint, Node_Flow->GetSolution(iPoint, nSpecies+2));
     SetVolumeOutputValue("ENERGY_VE",  iPoint, Node_Flow->GetSolution(iPoint, nSpecies+3));
@@ -342,6 +339,11 @@ void CNEMOCompOutput::LoadVolumeData(CConfig *config, CGeometry *geometry, CSolv
   SetVolumeOutputValue("PRESSURE", iPoint, Node_Flow->GetPressure(iPoint));
   SetVolumeOutputValue("TEMPERATURE_TR", iPoint, Node_Flow->GetTemperature(iPoint));
   SetVolumeOutputValue("TEMPERATURE_VE", iPoint, Node_Flow->GetTemperature_ve(iPoint));
+  SetVolumeOutputValue("VELOCITY-X", iPoint, Node_Flow->GetVelocity(iPoint, 0));
+  SetVolumeOutputValue("VELOCITY-Y", iPoint, Node_Flow->GetVelocity(iPoint, 1));
+  if (nDim == 3)
+    SetVolumeOutputValue("VELOCITY-Z", iPoint, Node_Flow->GetVelocity(iPoint, 2));
+
   SetVolumeOutputValue("MACH", iPoint, sqrt(Node_Flow->GetVelocity2(iPoint))/Node_Flow->GetSoundSpeed(iPoint));
 
   const su2double factor = solver[FLOW_SOL]->GetReferenceDynamicPressure();

From be559bc3a9863c63f5ccc94c74027346c21661d6 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Mon, 7 Aug 2023 08:26:20 -0700
Subject: [PATCH 636/656] Update .github/workflows/regression.yml

---
 .github/workflows/regression.yml | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 1b49b9a4e14..61b61dd42a0 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -26,7 +26,7 @@ jobs:
         config_set: [BaseMPI, ReverseMPI, ForwardMPI, BaseNoMPI, ReverseNoMPI, ForwardNoMPI, BaseOMP, ReverseOMP, ForwardOMP]
         include:
           - config_set: BaseMPI
-            flags: '-Denable-pywrapper=true -Denable-coolprop=true -Denable-mpp=true -Denable-mlpcpp=true -Denable-tests=true --warnlevel=2 --werror'
+            flags: '-Denable-pywrapper=true -Denable-coolprop=true -Denable-mpp=true -Denable-mlpcpp=true -Denable-tests=true --warnlevel=2'
           - config_set: ReverseMPI
             flags: '-Denable-autodiff=true -Denable-normal=false -Denable-pywrapper=true -Denable-tests=true --warnlevel=3 --werror'
           - config_set: ForwardMPI

From 3e30b1ca2bd103729fd312c12047e47d06b5b4d4 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Mon, 7 Aug 2023 18:58:08 -0700
Subject: [PATCH 637/656] try to make mutation accesible in test scripts

---
 .github/workflows/regression.yml |  2 +-
 TestCases/parallel_regression.py |  4 ++++
 meson.build                      | 27 +++++++++++++++++++++------
 meson_options.txt                |  1 +
 4 files changed, 27 insertions(+), 7 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 61b61dd42a0..81b8750d8ea 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -26,7 +26,7 @@ jobs:
         config_set: [BaseMPI, ReverseMPI, ForwardMPI, BaseNoMPI, ReverseNoMPI, ForwardNoMPI, BaseOMP, ReverseOMP, ForwardOMP]
         include:
           - config_set: BaseMPI
-            flags: '-Denable-pywrapper=true -Denable-coolprop=true -Denable-mpp=true -Denable-mlpcpp=true -Denable-tests=true --warnlevel=2'
+            flags: '-Denable-pywrapper=true -Denable-coolprop=true -Denable-mpp=true -Dinstall-mpp=true -Denable-mlpcpp=true -Denable-tests=true --warnlevel=2'
           - config_set: ReverseMPI
             flags: '-Denable-autodiff=true -Denable-normal=false -Denable-pywrapper=true -Denable-tests=true --warnlevel=3 --werror'
           - config_set: ForwardMPI
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 81ed8e4f1c5..658eee5fe53 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -29,9 +29,13 @@
 from __future__ import print_function
 
 import sys
+import os
 from TestCase import TestCase
 
 def main():
+    os.environ['MPP_DATA_DIRECTORY'] = os.environ['SU2_RUN'] + "../mpp-data"
+    os.environ['LD_LIBRARY_PATH'] = os.environ['LD_LIBRARY_PATH'] + ":" + os.environ['SU2_RUN'] + "../lib"
+
     '''This program runs SU2 and ensures that the output matches specified values.
        This will be used to do checks when code is pushed to github
        to make sure nothing is broken. '''
diff --git a/meson.build b/meson.build
index 974d166faf4..d42e96818fa 100644
--- a/meson.build
+++ b/meson.build
@@ -238,14 +238,20 @@ if get_option('enable-mpp')
     cmake_opts = cmake.subproject_options()
     cmake_opts.set_override_option('warning_level', '0')
     cmake_opts.add_cmake_defines({
-    'CMAKE_MAKE_PROGRAM': meson.source_root() + '/ninja',
-    'CMAKE_POSITION_INDEPENDENT_CODE': 'ON'
+      'CMAKE_MAKE_PROGRAM': meson.source_root() + '/ninja',
+      'CMAKE_POSITION_INDEPENDENT_CODE': 'ON'
     })
+    cmake_opts.set_install(get_option('install-mpp'))
   endif
   mpp_subproj = cmake.subproject('Mutationpp', options: cmake_opts)
   mpp_dep = mpp_subproj.dependency('mutation++')
   su2_deps     += mpp_dep
   su2_cpp_args += '-DHAVE_MPP'
+
+  if get_option('install-mpp')
+    run_command('cp', '-r', join_paths(meson.source_root(), '/subprojects/Mutationpp/data'),
+        join_paths(get_option('prefix'), '/mpp-data'), check: true)
+  endif
 endif
 
 if get_option('enable-coolprop')
@@ -340,12 +346,21 @@ message('''---------------------------------------------------------------------
            get_option('enable-mlpcpp'), meson.project_build_root().startswith(meson.project_source_root()) ? meson.project_build_root().split('/')[-1] : meson.project_build_root()))
 
 if get_option('enable-mpp')
-  message(''' To run SU2 with Mutation++ library, add these lines to your .bashrc file:
+  if get_option('install-mpp')
+    message(''' To run SU2 with Mutation++ library, add these lines to your .bashrc file:
 
-          export MPP_DATA_DIRECTORY=$SU2_HOME/subprojects/Mutationpp/data
-          export LD_LIBRARY_PATH=$SU2_HOME/<build_dir>/subprojects/Mutationpp
+            export MPP_DATA_DIRECTORY=$SU2_RUN/../mpp-data
+            export LD_LIBRARY_PATH=$LD_LIBRARY_PATH:$SU2_RUN/../lib
 
-          ''')
+            ''')
+  else
+    message(''' To run SU2 with Mutation++ library, add these lines to your .bashrc file:
+
+            export MPP_DATA_DIRECTORY=$SU2_HOME/subprojects/Mutationpp/data
+            export LD_LIBRARY_PATH=$LD_LIBRARY_PATH:$SU2_HOME/<build_dir>/subprojects/Mutationpp
+
+            ''')
+  endif
 endif
 
 if get_option('enable-librom')
diff --git a/meson_options.txt b/meson_options.txt
index f31f9a0fc57..c3886bd037e 100644
--- a/meson_options.txt
+++ b/meson_options.txt
@@ -18,6 +18,7 @@ option('enable-tests',  type : 'boolean', value : false, description: 'compile U
 option('enable-mixedprec', type : 'boolean', value : false, description: 'use single precision floating point arithmetic for sparse algebra')
 option('extra-deps', type : 'string', value : '', description: 'comma-separated list of extra (custom) dependencies to add for compilation')
 option('enable-mpp',  type : 'boolean', value : false, description: 'enable Mutation++ support')
+option('install-mpp', type : 'boolean', value : false, description: 'install Mutation++ in the directory defined with --prefix')
 option('enable-coolprop',  type : 'boolean', value : false, description: 'enable CoolProp support')
 option('enable-mlpcpp', type : 'boolean', value : false, description: 'enable MLPCpp support')
 option('opdi-backend', type : 'combo', choices : ['auto', 'macro', 'ompt'], value : 'auto', description: 'OpDiLib backend choice')

From dc55d1ed2cc02935ee751758524d5c6b2b2d12ae Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 12 Aug 2023 16:08:01 -0700
Subject: [PATCH 638/656] use python to copy mutation data

---
 SU2_PY/copy_directory.py | 11 +++++++++++
 meson.build              | 11 +++++++----
 2 files changed, 18 insertions(+), 4 deletions(-)
 create mode 100755 SU2_PY/copy_directory.py

diff --git a/SU2_PY/copy_directory.py b/SU2_PY/copy_directory.py
new file mode 100755
index 00000000000..aa42e27cc61
--- /dev/null
+++ b/SU2_PY/copy_directory.py
@@ -0,0 +1,11 @@
+#!/usr/bin/env python
+# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
+
+import sys
+import os
+import shutil
+
+if __name__ == "__main__":
+    src = os.path.abspath(sys.argv[1])
+    dst = os.path.abspath(sys.argv[2])
+    shutil.copytree(src, dst)
diff --git a/meson.build b/meson.build
index d42e96818fa..d8501b42db9 100644
--- a/meson.build
+++ b/meson.build
@@ -238,7 +238,7 @@ if get_option('enable-mpp')
     cmake_opts = cmake.subproject_options()
     cmake_opts.set_override_option('warning_level', '0')
     cmake_opts.add_cmake_defines({
-      'CMAKE_MAKE_PROGRAM': meson.source_root() + '/ninja',
+      'CMAKE_MAKE_PROGRAM': join_paths(meson.project_source_root(), 'ninja'),
       'CMAKE_POSITION_INDEPENDENT_CODE': 'ON'
     })
     cmake_opts.set_install(get_option('install-mpp'))
@@ -249,8 +249,11 @@ if get_option('enable-mpp')
   su2_cpp_args += '-DHAVE_MPP'
 
   if get_option('install-mpp')
-    run_command('cp', '-r', join_paths(meson.source_root(), '/subprojects/Mutationpp/data'),
-        join_paths(get_option('prefix'), '/mpp-data'), check: true)
+    py = find_program('python3', 'python')
+    p = run_command(py, 'SU2_PY/copy_directory.py', 'subprojects/Mutationpp/data', join_paths(get_option('prefix'), 'mpp-data'))
+    if p.returncode() != 0
+      error(p.stderr())
+    endif
   endif
 endif
 
@@ -261,7 +264,7 @@ if get_option('enable-coolprop')
     cmake_opts.set_override_option('warning_level', '0')
     cmake_opts.add_cmake_defines({
       'COOLPROP_STATIC_LIBRARY': true,
-      'CMAKE_MAKE_PROGRAM': meson.source_root() + '/ninja',
+      'CMAKE_MAKE_PROGRAM': join_paths(meson.project_source_root(), 'ninja'),
       'CMAKE_POSITION_INDEPENDENT_CODE': 'ON'
     })
     coolprop_subproj = cmake.subproject('CoolProp', options: cmake_opts)

From d111f40af3dd7fcec4cdaf60084d77bf4f02d3d1 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 12 Aug 2023 19:13:46 -0700
Subject: [PATCH 639/656] remove env vars set in regression script

---
 TestCases/parallel_regression.py | 3 ---
 1 file changed, 3 deletions(-)

diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 658eee5fe53..8e3efe7c917 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -33,9 +33,6 @@
 from TestCase import TestCase
 
 def main():
-    os.environ['MPP_DATA_DIRECTORY'] = os.environ['SU2_RUN'] + "../mpp-data"
-    os.environ['LD_LIBRARY_PATH'] = os.environ['LD_LIBRARY_PATH'] + ":" + os.environ['SU2_RUN'] + "../lib"
-
     '''This program runs SU2 and ensures that the output matches specified values.
        This will be used to do checks when code is pushed to github
        to make sure nothing is broken. '''

From c2c208bedd37e9d7806c511b0558f879ffee0d85 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 13 Aug 2023 13:55:29 -0700
Subject: [PATCH 640/656] update docker images

---
 .github/workflows/regression.yml         | 30 ++++++++++++------------
 .github/workflows/release-management.yml |  2 +-
 2 files changed, 16 insertions(+), 16 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 81b8750d8ea..1a46bec332b 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -52,12 +52,12 @@ jobs:
           key: ${{ matrix.config_set }}-${{ github.sha }}
           restore-keys: ${{ matrix.config_set }}
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/build-su2:230704-1323
+        uses: docker://ghcr.io/su2code/su2/build-su2:230813-0103
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
       - name: Build
-        uses: docker://ghcr.io/su2code/su2/build-su2:230704-1323
+        uses: docker://ghcr.io/su2code/su2/build-su2:230813-0103
         with:
           args: -b ${{github.ref}} -f "${{matrix.flags}}"
       - name: Compress binaries
@@ -68,7 +68,7 @@ jobs:
           name: ${{ matrix.config_set }}
           path: install_bin.tgz
       - name: Post Cleanup
-        uses: docker://ghcr.io/su2code/su2/build-su2:230704-1323
+        uses: docker://ghcr.io/su2code/su2/build-su2:230813-0103
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -95,12 +95,12 @@ jobs:
           key: ${{ matrix.config_set }}-${{ github.sha }}
           restore-keys: ${{ matrix.config_set }}
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/build-su2-tsan:230704-1323
+        uses: docker://ghcr.io/su2code/su2/build-su2-tsan:230813-0103
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
       - name: Build
-        uses: docker://ghcr.io/su2code/su2/build-su2-tsan:230704-1323
+        uses: docker://ghcr.io/su2code/su2/build-su2-tsan:230813-0103
         with:
           args: -b ${{github.ref}} -f "${{matrix.flags}}"
       - name: Compress binaries
@@ -111,7 +111,7 @@ jobs:
           name: ${{ matrix.config_set }}
           path: install_bin.tgz
       - name: Post Cleanup
-        uses: docker://ghcr.io/su2code/su2/build-su2-tsan:230704-1323
+        uses: docker://ghcr.io/su2code/su2/build-su2-tsan:230813-0103
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -142,7 +142,7 @@ jobs:
             tag: OMP
     steps:
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:230704-1323
+        uses: docker://ghcr.io/su2code/su2/test-su2:230813-0103
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -168,12 +168,12 @@ jobs:
           chmod a+x $BIN_FOLDER/*
           ls -lahR $BIN_FOLDER
       - name: Run Tests in Container
-        uses: docker://ghcr.io/su2code/su2/test-su2:230704-1323
+        uses: docker://ghcr.io/su2code/su2/test-su2:230813-0103
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
           args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
       - name: Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:230704-1323
+        uses: docker://ghcr.io/su2code/su2/test-su2:230813-0103
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -188,7 +188,7 @@ jobs:
         testscript: ['hybrid_regression.py', 'hybrid_regression_AD.py']
     steps:
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2-tsan:230704-1323
+        uses: docker://ghcr.io/su2code/su2/test-su2-tsan:230813-0103
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -214,12 +214,12 @@ jobs:
           chmod a+x $BIN_FOLDER/*
           ls -lahR $BIN_FOLDER
       - name: Run Tests in Container
-        uses: docker://ghcr.io/su2code/su2/test-su2-tsan:230704-1323
+        uses: docker://ghcr.io/su2code/su2/test-su2-tsan:230813-0103
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
           args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}} -a "--tsan"
       - name: Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2-tsan:230704-1323
+        uses: docker://ghcr.io/su2code/su2/test-su2-tsan:230813-0103
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -240,7 +240,7 @@ jobs:
             tag: MPI
     steps:
       - name: Pre Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:230704-1323
+        uses: docker://ghcr.io/su2code/su2/test-su2:230813-0103
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
@@ -301,11 +301,11 @@ jobs:
           echo $PWD
           ls -lahR
       - name: Run Unit Tests
-        uses: docker://ghcr.io/su2code/su2/test-su2:230704-1323
+        uses: docker://ghcr.io/su2code/su2/test-su2:230813-0103
         with:
           entrypoint: install/bin/${{matrix.testdriver}}
       - name: Post Cleanup
-        uses: docker://ghcr.io/su2code/su2/test-su2:230704-1323
+        uses: docker://ghcr.io/su2code/su2/test-su2:230813-0103
         with:
           entrypoint: /bin/rm
           args: -rf install install_bin.tgz src ccache ${{ matrix.config_set }}
diff --git a/.github/workflows/release-management.yml b/.github/workflows/release-management.yml
index 45bb698198f..f0b680a6485 100644
--- a/.github/workflows/release-management.yml
+++ b/.github/workflows/release-management.yml
@@ -35,7 +35,7 @@ jobs:
           key: ${{ matrix.os_bin }}-${{ github.sha }}
           restore-keys: ${{ matrix.os_bin }}
       - name: Build
-        uses: docker://ghcr.io/su2code/su2/build-su2-cross:230704-1323
+        uses: docker://ghcr.io/su2code/su2/build-su2-cross:230813-0103
         with:
           args: -b ${{ github.sha }} -f "${{matrix.flags}}"
       - name: Create Archive

From 510ded23e54fcc30b11d4e4949a6b8d647803c5b Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 13 Aug 2023 14:54:18 -0700
Subject: [PATCH 641/656] capture mpp files

---
 .github/workflows/regression.yml | 10 +++++-----
 1 file changed, 5 insertions(+), 5 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index 1a46bec332b..e0e2e3cefba 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -61,7 +61,7 @@ jobs:
         with:
           args: -b ${{github.ref}} -f "${{matrix.flags}}"
       - name: Compress binaries
-        run: tar -zcvf install_bin.tgz install/bin
+        run: tar -zcvf install_bin.tgz install/bin install/lib install/mpp-data
       - name: Upload Binaries
         uses: actions/upload-artifact@v3
         with:
@@ -104,7 +104,7 @@ jobs:
         with:
           args: -b ${{github.ref}} -f "${{matrix.flags}}"
       - name: Compress binaries
-        run: tar -zcvf install_bin.tgz install/bin
+        run: tar -zcvf install_bin.tgz install/bin install/lib install/mpp-data
       - name: Upload Binaries
         uses: actions/upload-artifact@v3
         with:
@@ -161,7 +161,7 @@ jobs:
               ls -lah
               tar -zxvf install_bin.tgz
               ls -lah install/bin/
-              cp -r install/bin/* $BIN_FOLDER;
+              cp -r install/* $BIN_FOLDER/../
               popd;
             fi
           done
@@ -207,7 +207,7 @@ jobs:
               ls -lah
               tar -zxvf install_bin.tgz
               ls -lah install/bin/
-              cp -r install/bin/* $BIN_FOLDER;
+              cp -r install/* $BIN_FOLDER/../
               popd;
             fi
           done
@@ -273,7 +273,7 @@ jobs:
               ls -lah
               tar -zxvf install_bin.tgz
               ls -laH install/bin/
-              cp -r install/bin/* $BIN_FOLDER;
+              cp -r install/* $BIN_FOLDER/../
               popd;
             else
               echo "$TYPE_FOLDER does not exist!"

From c9500152c18d238c4201a3a032f959809f8f1f2e Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sun, 13 Aug 2023 15:10:58 -0700
Subject: [PATCH 642/656] fix

---
 .github/workflows/regression.yml | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/.github/workflows/regression.yml b/.github/workflows/regression.yml
index e0e2e3cefba..129913c82cf 100644
--- a/.github/workflows/regression.yml
+++ b/.github/workflows/regression.yml
@@ -61,7 +61,7 @@ jobs:
         with:
           args: -b ${{github.ref}} -f "${{matrix.flags}}"
       - name: Compress binaries
-        run: tar -zcvf install_bin.tgz install/bin install/lib install/mpp-data
+        run: tar -zcvf install_bin.tgz install/*
       - name: Upload Binaries
         uses: actions/upload-artifact@v3
         with:
@@ -104,7 +104,7 @@ jobs:
         with:
           args: -b ${{github.ref}} -f "${{matrix.flags}}"
       - name: Compress binaries
-        run: tar -zcvf install_bin.tgz install/bin install/lib install/mpp-data
+        run: tar -zcvf install_bin.tgz install/*
       - name: Upload Binaries
         uses: actions/upload-artifact@v3
         with:

From a0b41853b7b17ae73f848b8a5b911fa1f06f2c27 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Mon, 14 Aug 2023 16:36:56 +0200
Subject: [PATCH 643/656] Clarify and extend tape choices.

---
 Common/include/code_config.hpp                | 24 +++++++++++++------
 .../src/drivers/CDiscAdjMultizoneDriver.cpp   |  4 ++--
 meson.build                                   | 20 +++++++++++-----
 meson_options.txt                             |  2 +-
 4 files changed, 34 insertions(+), 16 deletions(-)

diff --git a/Common/include/code_config.hpp b/Common/include/code_config.hpp
index 958a82f0e38..3ab5b3070fc 100644
--- a/Common/include/code_config.hpp
+++ b/Common/include/code_config.hpp
@@ -98,20 +98,30 @@ FORCEINLINE Out su2staticcast_p(In ptr) {
 #if defined(HAVE_OMP)
 using su2double = codi::RealReverseIndexOpenMPGen<double, double>;
 #else
-#if defined(CODI_INDEX_TAPE)
+#if defined(CODI_JACOBIAN_LINEAR_TAPE)
+using su2double = codi::RealReverse;
+#elif defined(CODI_JACOBIAN_REUSE_TAPE)
+using su2double = codi::RealReverseIndexGen<double, double, codi::ReuseIndexManager<int> >;
+#elif defined(CODI_JACOBIAN_MULTIUSE_TAPE)
 using su2double = codi::RealReverseIndex;
-// #elif defined(CODI_PRIMAL_TAPE)
-// using su2double = codi::RealReversePrimal;
-// #elif defined(CODI_PRIMAL_INDEX_TAPE)
-// using su2double = codi::RealReversePrimalIndex;
+#elif defined(CODI_PRIMAL_LINEAR_TAPE)
+using su2double = codi::RealReversePrimal;
+#elif defined(CODI_PRIMAL_REUSE_TAPE)
+using su2double = codi::RealReversePrimalIndexGen<double, double, codi::ReuseIndexManager<int> >;
+#elif defined(CODI_PRIMAL_MULTIUSE_TAPE)
+using su2double = codi::RealReversePrimalIndex;
 #else
-using su2double = codi::RealReverse;
+#error "Please define a CoDiPack tape."
 #endif
 #endif
+
+#if defined(HAVE_OMP) || defined(CODI_JACOBIAN_REUSE_TAPE) || defined(CODI_JACOBIAN_MULTIUSE_TAPE) || \
+    defined(CODI_PRIMAL_REUSE_TAPE) || defined(CODI_PRIMAL_MULTIUSE_TAPE)
+#define CODI_INDEX_REUSE
+#endif
 #elif defined(CODI_FORWARD_TYPE)  // forward mode AD
 #include "codi.hpp"
 using su2double = codi::RealForward;
-
 #else  // primal / direct / no AD
 using su2double = double;
 #endif
diff --git a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
index 615980dd728..ef2d2ee56c8 100644
--- a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
@@ -786,9 +786,9 @@ void CDiscAdjMultizoneDriver::SetAdjObjFunction() {
 
 void CDiscAdjMultizoneDriver::ComputeAdjoints(unsigned short iZone, bool eval_transfer) {
 
-#if defined(CODI_INDEX_TAPE) || defined(HAVE_OPDI)
+#if defined(CODI_INDEX_REUSE)
   if (nZone > 1 && rank == MASTER_NODE) {
-    std::cout << "WARNING: Index AD types do not support multiple zones." << std::endl;
+    std::cout << "WARNING: AD types that reuse indices do not support multiple zones." << std::endl;
   }
 #endif
 
diff --git a/meson.build b/meson.build
index bc862b6572f..5d98a6ac729 100644
--- a/meson.build
+++ b/meson.build
@@ -78,12 +78,20 @@ if get_option('enable-autodiff') or get_option('enable-directdiff')
 endif
 
 if get_option('enable-autodiff')
-  if get_option('codi-tape') == 'JacobianIndex'
-    codi_rev_args += '-DCODI_INDEX_TAPE'
-  #elif get_option('codi-tape') == 'PrimalLinear'
-  #  codi_rev_args += '-DCODI_PRIMAL_TAPE'
-  #elif get_option('codi-tape') == 'PrimalIndex'
-  #  codi_rev_args += '-DCODI_PRIMAL_INDEX_TAPE'
+  if get_option('codi-tape') == 'JacobianLinear'
+    codi_rev_args += '-DCODI_JACOBIAN_LINEAR_TAPE'
+  elif get_option('codi-tape') == 'JacobianReuse'
+    codi_rev_args += '-DCODI_JACOBIAN_REUSE_TAPE'
+  elif get_option('codi-tape') == 'JacobianMultiUse'
+    codi_rev_args += '-DCODI_JACOBIAN_MULTIUSE_TAPE'
+  elif get_option('codi-tape') == 'PrimalLinear'
+    codi_rev_args += '-DCODI_PRIMAL_LINEAR_TAPE'
+  elif get_option('codi-tape') == 'PrimalReuse'
+    codi_rev_args += '-DCODI_PRIMAL_REUSE_TAPE'
+  elif get_option('codi-tape') == 'PrimalMultiUse'
+    codi_rev_args += '-DCODI_PRIMAL_MULTIUSE_TAPE'
+  else
+    message('Invalid CoDiPack tape choice @1@'.format(get_option('codi-tape')))
   endif
 endif
 
diff --git a/meson_options.txt b/meson_options.txt
index f31f9a0fc57..4fbc35b82d7 100644
--- a/meson_options.txt
+++ b/meson_options.txt
@@ -21,7 +21,7 @@ option('enable-mpp',  type : 'boolean', value : false, description: 'enable Muta
 option('enable-coolprop',  type : 'boolean', value : false, description: 'enable CoolProp support')
 option('enable-mlpcpp', type : 'boolean', value : false, description: 'enable MLPCpp support')
 option('opdi-backend', type : 'combo', choices : ['auto', 'macro', 'ompt'], value : 'auto', description: 'OpDiLib backend choice')
-option('codi-tape', type : 'combo', choices : ['JacobianLinear', 'JacobianIndex'], value : 'JacobianLinear', description: 'CoDiPack tape choice')
+option('codi-tape', type : 'combo', choices : ['JacobianLinear', 'JacobianReuse', 'JacobianMultiUse', 'PrimalLinear', 'PrimalReuse', 'PrimalMultiUse'], value : 'JacobianLinear', description: 'CoDiPack tape choice')
 option('opdi-shared-read-opt', type : 'boolean', value : true, description : 'OpDiLib shared reading optimization')
 option('librom_root', type : 'string', value : '', description: 'libROM base directory')
 option('enable-librom', type : 'boolean', value : false, description: 'enable LLNL libROM support')

From 785a362a974b1f19e96367f3692a2b5268c45aba Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Tue, 15 Aug 2023 15:33:58 +0200
Subject: [PATCH 644/656] CoDiPack update.

---
 externals/codi        | 2 +-
 meson_scripts/init.py | 2 +-
 2 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/externals/codi b/externals/codi
index 17232fed052..c30f195eb9d 160000
--- a/externals/codi
+++ b/externals/codi
@@ -1 +1 @@
-Subproject commit 17232fed05245dbb8f04a31e274a02d53458c75c
+Subproject commit c30f195eb9d772cadc75e9dbf4c88cb351ee34bb
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index eb69728e2a0..bde2da386ee 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -55,7 +55,7 @@ def init_submodules(
 
     # This information of the modules is used if projects was not cloned using git
     # The sha tag must be maintained manually to point to the correct commit
-    sha_version_codi = "17232fed05245dbb8f04a31e274a02d53458c75c"
+    sha_version_codi = "c30f195eb9d772cadc75e9dbf4c88cb351ee34bb"
     github_repo_codi = "https://github.com/scicompkl/CoDiPack"
     sha_version_medi = "aafc2d1966ba1233640af737e71c77c1a86183fd"
     github_repo_medi = "https://github.com/SciCompKL/MeDiPack"

From fb02214cecb75bb9c1e706652e5d885c1eb017f2 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 16 Aug 2023 11:21:05 +0200
Subject: [PATCH 645/656] Add warning.

---
 meson.build | 6 +++++-
 1 file changed, 5 insertions(+), 1 deletion(-)

diff --git a/meson.build b/meson.build
index 5d98a6ac729..d1a5b3b91fb 100644
--- a/meson.build
+++ b/meson.build
@@ -77,7 +77,7 @@ if get_option('enable-autodiff') or get_option('enable-directdiff')
   codi_for_args = ['-DCODI_FORWARD_TYPE']
 endif
 
-if get_option('enable-autodiff')
+if get_option('enable-autodiff') and not omp
   if get_option('codi-tape') == 'JacobianLinear'
     codi_rev_args += '-DCODI_JACOBIAN_LINEAR_TAPE'
   elif get_option('codi-tape') == 'JacobianReuse'
@@ -93,6 +93,10 @@ if get_option('enable-autodiff')
   else
     message('Invalid CoDiPack tape choice @1@'.format(get_option('codi-tape')))
   endif
+
+  if get_option('codi-tape') != 'JacobianLinear'
+    warning('The tape choice @1@ is not tested regularly in SU2'.format(get_option('codi-tape')))
+  endif
 endif
 
 # add cgns library

From f5160b2351f0addc9337d6500824c66eb00b6189 Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Sat, 19 Aug 2023 19:39:23 -0700
Subject: [PATCH 646/656] go back to current version of mpp for now

---
 TestCases/parallel_regression.py | 1 -
 meson_scripts/init.py            | 2 +-
 subprojects/Mutationpp           | 2 +-
 3 files changed, 2 insertions(+), 3 deletions(-)

diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 8e3efe7c917..81ed8e4f1c5 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -29,7 +29,6 @@
 from __future__ import print_function
 
 import sys
-import os
 from TestCase import TestCase
 
 def main():
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 214d4a9a599..eb69728e2a0 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -65,7 +65,7 @@ def init_submodules(
     github_repo_meson = "https://github.com/mesonbuild/meson"
     sha_version_ninja = "52649de2c56b63f42bc59513d51286531c595b44"
     github_repo_ninja = "https://github.com/ninja-build/ninja"
-    sha_version_mpp = "4cb6e3a05c15f49ffd346dc9f185ccc3459728b0"
+    sha_version_mpp = "5ff579f43781cae07411e5ab46291c9971536be6"
     github_repo_mpp = "https://github.com/mutationpp/Mutationpp"
     sha_version_coolprop = "0ce42fcf3bb2c373512bc825a4f0c1973a78f307"
     github_repo_coolprop = "https://github.com/CoolProp/CoolProp"
diff --git a/subprojects/Mutationpp b/subprojects/Mutationpp
index 4cb6e3a05c1..5ff579f4378 160000
--- a/subprojects/Mutationpp
+++ b/subprojects/Mutationpp
@@ -1 +1 @@
-Subproject commit 4cb6e3a05c15f49ffd346dc9f185ccc3459728b0
+Subproject commit 5ff579f43781cae07411e5ab46291c9971536be6

From deb7027a7491399c4a8e95b3a543b2ecfa33fc32 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Tue, 22 Aug 2023 12:51:39 +0200
Subject: [PATCH 647/656] Explicit adjoint vector resizing.

---
 SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp | 1 +
 1 file changed, 1 insertion(+)

diff --git a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
index ef2d2ee56c8..b1eafa89ef3 100644
--- a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
@@ -780,6 +780,7 @@ void CDiscAdjMultizoneDriver::SetAdjObjFunction() {
     }
   }
   if (rank == MASTER_NODE) {
+    AD::ResizeAdjoints();
     AD::SetDerivative(ObjFunc_Index, SU2_TYPE::GetValue(seeding));
   }
 }

From d3184c379323040ddbbfdabdcf274a92700d7b11 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Tue, 22 Aug 2023 13:09:43 +0200
Subject: [PATCH 648/656] Update non-AD version of AD::RegisterInput.

---
 Common/include/basic_types/ad_structure.hpp | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/Common/include/basic_types/ad_structure.hpp b/Common/include/basic_types/ad_structure.hpp
index 8a46096a58e..1eb925bec1f 100644
--- a/Common/include/basic_types/ad_structure.hpp
+++ b/Common/include/basic_types/ad_structure.hpp
@@ -66,7 +66,7 @@ inline void PrintStatistics() {}
  * graph. \param[in] data - The variable to be registered as input. \param[in] push_index - boolean whether we also want
  * to push the index.
  */
-inline void RegisterInput(su2double& data, bool push_index = true) {}
+inline void RegisterInput(su2double& data) {}
 
 /*!
  * \brief Registers the variable as an output. I.e. as the root of the computational graph.

From 894770ef5a57d5fdadc613290ac86dced081aa4e Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Tue, 22 Aug 2023 15:16:25 +0200
Subject: [PATCH 649/656] Fix format range.

---
 meson.build | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/meson.build b/meson.build
index 2a45b4838de..455c598ed2f 100644
--- a/meson.build
+++ b/meson.build
@@ -95,7 +95,7 @@ if get_option('enable-autodiff') and not omp
   endif
 
   if get_option('codi-tape') != 'JacobianLinear'
-    warning('The tape choice @1@ is not tested regularly in SU2'.format(get_option('codi-tape')))
+    warning('The tape choice @0@ is not tested regularly in SU2'.format(get_option('codi-tape')))
   endif
 endif
 

From 682664a3b23134b83a81c8dee54bcbbbc26ea742 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Tue, 22 Aug 2023 17:43:36 +0200
Subject: [PATCH 650/656] Update comment.

---
 Common/include/basic_types/ad_structure.hpp | 5 ++---
 1 file changed, 2 insertions(+), 3 deletions(-)

diff --git a/Common/include/basic_types/ad_structure.hpp b/Common/include/basic_types/ad_structure.hpp
index 1eb925bec1f..2373163a215 100644
--- a/Common/include/basic_types/ad_structure.hpp
+++ b/Common/include/basic_types/ad_structure.hpp
@@ -62,9 +62,8 @@ inline bool TapeActive() { return false; }
 inline void PrintStatistics() {}
 
 /*!
- * \brief Registers the variable as an input and saves internal data (indices). I.e. as a leaf of the computational
- * graph. \param[in] data - The variable to be registered as input. \param[in] push_index - boolean whether we also want
- * to push the index.
+ * \brief Registers the variable as an input. I.e. as a leaf of the computational graph.
+ * \param[in] data - The variable to be registered as input.
  */
 inline void RegisterInput(su2double& data) {}
 

From 784f703178d58652ea4b389e7b59f5d40f36359d Mon Sep 17 00:00:00 2001
From: Pedro Gomes <pcarruscag@gmail.com>
Date: Tue, 22 Aug 2023 11:57:26 -0700
Subject: [PATCH 651/656] fix build with mutation++ on Arm architectures

---
 meson.build | 18 ++++++++----------
 1 file changed, 8 insertions(+), 10 deletions(-)

diff --git a/meson.build b/meson.build
index 2a45b4838de..a90407aaeee 100644
--- a/meson.build
+++ b/meson.build
@@ -245,16 +245,14 @@ endforeach
 catch2_dep = declare_dependency(include_directories: 'externals/catch2/')
 
 if get_option('enable-mpp')
-  if build_machine.cpu_family() == 'x86' or build_machine.cpu_family() == 'x86_64'
-    cmake = import('cmake')
-    cmake_opts = cmake.subproject_options()
-    cmake_opts.set_override_option('warning_level', '0')
-    cmake_opts.add_cmake_defines({
-      'CMAKE_MAKE_PROGRAM': join_paths(meson.project_source_root(), 'ninja'),
-      'CMAKE_POSITION_INDEPENDENT_CODE': 'ON'
-    })
-    cmake_opts.set_install(get_option('install-mpp'))
-  endif
+  cmake = import('cmake')
+  cmake_opts = cmake.subproject_options()
+  cmake_opts.set_override_option('warning_level', '0')
+  cmake_opts.add_cmake_defines({
+    'CMAKE_MAKE_PROGRAM': join_paths(meson.project_source_root(), 'ninja'),
+    'CMAKE_POSITION_INDEPENDENT_CODE': 'ON'
+  })
+  cmake_opts.set_install(get_option('install-mpp'))
   mpp_subproj = cmake.subproject('Mutationpp', options: cmake_opts)
   mpp_dep = mpp_subproj.dependency('mutation++')
   su2_deps     += mpp_dep

From 9c7034f15ddac6f405c4d5f3b249cc6deea90a05 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 23 Aug 2023 11:31:55 +0200
Subject: [PATCH 652/656] Enable CoDiPack assertions in debug builds.

---
 meson.build | 5 +++++
 1 file changed, 5 insertions(+)

diff --git a/meson.build b/meson.build
index 620918783d8..d9e5dd84f3e 100644
--- a/meson.build
+++ b/meson.build
@@ -75,6 +75,11 @@ if get_option('enable-autodiff') or get_option('enable-directdiff')
   codi_dep = [declare_dependency(include_directories: 'externals/codi/include')]
   codi_rev_args = ['-DCODI_REVERSE_TYPE']
   codi_for_args = ['-DCODI_FORWARD_TYPE']
+
+  if get_option('debug')
+    codi_rev_args += '-DCODI_EnableAssert'
+    codi_for_args += '-DCODI_EnableAssert'
+  endif
 endif
 
 if get_option('enable-autodiff') and not omp

From 510b4bb498d2bc32dbe74156ea9273d71af31e58 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 23 Aug 2023 11:36:17 +0200
Subject: [PATCH 653/656] Fix format range, error instead of message.

---
 meson.build | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/meson.build b/meson.build
index d9e5dd84f3e..d0c0e4e10e8 100644
--- a/meson.build
+++ b/meson.build
@@ -96,7 +96,7 @@ if get_option('enable-autodiff') and not omp
   elif get_option('codi-tape') == 'PrimalMultiUse'
     codi_rev_args += '-DCODI_PRIMAL_MULTIUSE_TAPE'
   else
-    message('Invalid CoDiPack tape choice @1@'.format(get_option('codi-tape')))
+    error('Invalid CoDiPack tape choice @0@'.format(get_option('codi-tape')))
   endif
 
   if get_option('codi-tape') != 'JacobianLinear'

From 1d2dcb26bdb3d5ebd2b7257fd75c4fabc3d728f5 Mon Sep 17 00:00:00 2001
From: =?UTF-8?q?Johannes=20Bl=C3=BChdorn?=
 <johannes.bluehdorn@scicomp.uni-kl.de>
Date: Wed, 23 Aug 2023 13:20:47 +0200
Subject: [PATCH 654/656] CoDiPack update.

---
 externals/codi        | 2 +-
 meson_scripts/init.py | 2 +-
 2 files changed, 2 insertions(+), 2 deletions(-)

diff --git a/externals/codi b/externals/codi
index c30f195eb9d..8ee822a9b0b 160000
--- a/externals/codi
+++ b/externals/codi
@@ -1 +1 @@
-Subproject commit c30f195eb9d772cadc75e9dbf4c88cb351ee34bb
+Subproject commit 8ee822a9b0bb8235a2494467b774e27fb64ff14f
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index bde2da386ee..948636d3856 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -55,7 +55,7 @@ def init_submodules(
 
     # This information of the modules is used if projects was not cloned using git
     # The sha tag must be maintained manually to point to the correct commit
-    sha_version_codi = "c30f195eb9d772cadc75e9dbf4c88cb351ee34bb"
+    sha_version_codi = "8ee822a9b0bb8235a2494467b774e27fb64ff14f"
     github_repo_codi = "https://github.com/scicompkl/CoDiPack"
     sha_version_medi = "aafc2d1966ba1233640af737e71c77c1a86183fd"
     github_repo_medi = "https://github.com/SciCompKL/MeDiPack"

From c5e97f862bb0bdd93fd48f9f666ab2993724866f Mon Sep 17 00:00:00 2001
From: Pedro Gomes <38071223+pcarruscag@users.noreply.github.com>
Date: Thu, 24 Aug 2023 08:50:19 -0700
Subject: [PATCH 655/656] Multizone py wrapper example (FSI) (#2111)

* checkpoint naming and update some functions

* add FSI example with additional custom load via the python wrapper

* remove mesh files

* fix segfault

* add some arm64 values

* disable polar naca on arm64
---
 SU2_CFD/include/drivers/CDriverBase.hpp       | 21 +++--
 SU2_CFD/include/drivers/CMultizoneDriver.hpp  | 20 ++++-
 .../interfaces/fsi/CFlowTractionInterface.hpp |  5 +-
 .../include/variables/CFEABoundVariable.hpp   |  5 --
 SU2_CFD/include/variables/CVariable.hpp       |  5 --
 SU2_CFD/src/drivers/CDriverBase.cpp           | 10 +--
 SU2_CFD/src/drivers/CMultizoneDriver.cpp      | 43 +++++-----
 SU2_CFD/src/drivers/CSinglezoneDriver.cpp     | 15 ++--
 .../fsi/CDiscAdjFlowTractionInterface.cpp     |  6 +-
 .../interfaces/fsi/CFlowTractionInterface.cpp | 28 +++++--
 SU2_CFD/src/output/CElasticityOutput.cpp      |  6 +-
 SU2_CFD/src/python_wrapper_structure.cpp      | 60 +++++++-------
 SU2_CFD/src/variables/CFEABoundVariable.cpp   |  2 -
 TestCases/parallel_regression.py              | 13 +++
 TestCases/py_wrapper/dyn_fsi/config.cfg       | 31 +++++++
 TestCases/py_wrapper/dyn_fsi/configFEA.cfg    | 54 ++++++++++++
 TestCases/py_wrapper/dyn_fsi/configFlow.cfg   | 80 ++++++++++++++++++
 TestCases/py_wrapper/dyn_fsi/run.py           | 83 +++++++++++++++++++
 TestCases/serial_regression.py                |  2 +
 TestCases/vandv.py                            |  1 +
 20 files changed, 386 insertions(+), 104 deletions(-)
 create mode 100644 TestCases/py_wrapper/dyn_fsi/config.cfg
 create mode 100644 TestCases/py_wrapper/dyn_fsi/configFEA.cfg
 create mode 100644 TestCases/py_wrapper/dyn_fsi/configFlow.cfg
 create mode 100644 TestCases/py_wrapper/dyn_fsi/run.py

diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index 6ee8a860ca5..01c3ae7a58d 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -54,7 +54,7 @@ class CDriverBase {
       UsedTime;        /*!< \brief Elapsed time between Start and Stop point of the timer. */
 
   unsigned long TimeIter;
-  unsigned short selected_iZone = ZONE_0; /*!< \brief Selected zone for the driver. Defaults to ZONE_0 */
+  unsigned short selected_zone = ZONE_0; /*!< \brief Selected zone for the driver. Defaults to ZONE_0 */
   unsigned short iMesh,  /*!< \brief Iterator on mesh levels. */
       iZone,             /*!< \brief Iterator on zones. */
       nZone,             /*!< \brief Total number of zones in the problem. */
@@ -227,7 +227,7 @@ class CDriverBase {
       SU2_MPI::Error("Initial coordinates are only available with DEFORM_MESH= YES", CURRENT_FUNCTION);
     }
     auto* coords =
-        const_cast<su2activematrix*>(solver_container[selected_iZone][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord());
+        const_cast<su2activematrix*>(solver_container[selected_zone][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord());
     return CPyWrapperMatrixView(*coords, "InitialCoordinates", true);
   }
 
@@ -241,7 +241,7 @@ class CDriverBase {
     if (iMarker >= GetNumberMarkers()) SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
 
     auto* coords =
-        const_cast<su2activematrix*>(solver_container[selected_iZone][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord());
+        const_cast<su2activematrix*>(solver_container[selected_zone][INST_0][MESH_0][MESH_SOL]->GetNodes()->GetMesh_Coord());
     return CPyWrapperMarkerMatrixView(*coords, main_geometry->vertex[iMarker], main_geometry->GetnVertex(iMarker),
                                       "MarkerInitialCoordinates", true);
   }
@@ -550,16 +550,21 @@ class CDriverBase {
   }
 
   /*!
-   * \brief Selects zone to be used for Driver operation
+   * \brief Selects zone to be used for python driver operations.
    * \param[in] iZone - Zone identifier.
    */
   inline void SelectZone(unsigned short iZone) {
     if (iZone >= nZone) SU2_MPI::Error("Zone index out of range", CURRENT_FUNCTION);
-    selected_iZone = iZone;
-    main_geometry = geometry_container[selected_iZone][INST_0][MESH_0];
-    main_config = config_container[selected_iZone];
+    selected_zone = iZone;
+    main_geometry = geometry_container[selected_zone][INST_0][MESH_0];
+    main_config = config_container[selected_zone];
   }
 
+  /*!
+   * \brief Returns the index of the zone selected for python driver operations.
+   */
+  inline unsigned short SelectedZone() const { return selected_zone; }
+
   /*!
    * \brief Get the wall normal heat flux at a vertex on a specified marker of the flow or heat solver.
    * \note This can be the output of a heat or flow solver in a CHT setting.
@@ -707,7 +712,7 @@ class CDriverBase {
     if (iMarker < std::numeric_limits<unsigned short>::max() && iMarker > GetNumberMarkers()) {
       SU2_MPI::Error("Marker index exceeds size.", CURRENT_FUNCTION);
     }
-    auto* solver = solver_container[selected_iZone][INST_0][MESH_0][iSolver];
+    auto* solver = solver_container[selected_zone][INST_0][MESH_0][iSolver];
     if (solver == nullptr) SU2_MPI::Error("The selected solver does not exist.", CURRENT_FUNCTION);
     return solver;
   }
diff --git a/SU2_CFD/include/drivers/CMultizoneDriver.hpp b/SU2_CFD/include/drivers/CMultizoneDriver.hpp
index afff04b8eac..adf9bf9d617 100644
--- a/SU2_CFD/include/drivers/CMultizoneDriver.hpp
+++ b/SU2_CFD/include/drivers/CMultizoneDriver.hpp
@@ -122,7 +122,7 @@ class CMultizoneDriver : public CDriver {
   /*!
    * \brief Destructor of the class.
    */
-  ~CMultizoneDriver(void) override;
+  ~CMultizoneDriver() override;
 
   /*!
    * \brief [Overload] Launch the computation for multizone problems.
@@ -130,10 +130,26 @@ class CMultizoneDriver : public CDriver {
   void StartSolver() override;
 
   /*!
-   * \brief Preprocess the multizone iteration
+   * \brief Preprocess the multizone iteration.
    */
   void Preprocess(unsigned long TimeIter) override;
 
+  /*!
+   * \brief Solves one time iteration.
+   */
+  void Run() override {
+    switch (driver_config->GetKind_MZSolver()){
+      case ENUM_MULTIZONE::MZ_BLOCK_GAUSS_SEIDEL: RunGaussSeidel(); break;  // Block Gauss-Seidel iteration
+      case ENUM_MULTIZONE::MZ_BLOCK_JACOBI: RunJacobi(); break;             // Block-Jacobi iteration
+    }
+  }
+
+  /*!
+   * \brief Placeholder for post processing operations to make the interface
+   * of this driver identical to CSinglezoneDriver.
+   */
+  void Postprocess() {}
+
   /*!
    * \brief Update the dual-time solution within multiple zones.
    */
diff --git a/SU2_CFD/include/interfaces/fsi/CFlowTractionInterface.hpp b/SU2_CFD/include/interfaces/fsi/CFlowTractionInterface.hpp
index 2074319c110..d3ea4a6a59d 100644
--- a/SU2_CFD/include/interfaces/fsi/CFlowTractionInterface.hpp
+++ b/SU2_CFD/include/interfaces/fsi/CFlowTractionInterface.hpp
@@ -43,8 +43,11 @@ class CFlowTractionInterface : public CInterface {
   /*!
    * \brief Sets the dimensional factor for pressure and the consistent_interpolation flag.
    * \param[in] flow_config - Definition of the fluid (donor) problem.
+   * \param[in] struct_config - Definition of the structural (target) problem.
+   * \param[in] geometry - FEA geometry.
+   * \param[in] solution - FEA solver.
    */
-  void Preprocess(const CConfig *flow_config);
+  void Preprocess(const CConfig *flow_config, const CConfig *struct_config, CGeometry *geometry, CSolver *solution);
 
   /*!
    * \brief Computes vertex areas (FEA side) for when tractions need to be integrated.
diff --git a/SU2_CFD/include/variables/CFEABoundVariable.hpp b/SU2_CFD/include/variables/CFEABoundVariable.hpp
index e0f8c273cc1..cdac1cdd476 100644
--- a/SU2_CFD/include/variables/CFEABoundVariable.hpp
+++ b/SU2_CFD/include/variables/CFEABoundVariable.hpp
@@ -149,11 +149,6 @@ class CFEABoundVariable final : public CFEAVariable {
     return FlowTraction_n(iPoint,iVar);
   }
 
-  /*!
-   * \brief Clear the flow traction residual
-   */
-  void Clear_FlowTraction() override;
-
   /*!
    * \brief Register the flow tractions as input variable.
    */
diff --git a/SU2_CFD/include/variables/CVariable.hpp b/SU2_CFD/include/variables/CVariable.hpp
index ec2557c8088..af0d70f2673 100644
--- a/SU2_CFD/include/variables/CVariable.hpp
+++ b/SU2_CFD/include/variables/CVariable.hpp
@@ -1508,11 +1508,6 @@ class CVariable {
    */
   inline virtual su2double Get_FlowTraction_n(unsigned long iPoint, unsigned long iVar) const { return 0.0; }
 
-  /*!
-   * \brief A virtual member.
-   */
-  inline virtual void Clear_FlowTraction() {}
-
   /*!
    * \brief A virtual member.
    */
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index 603e2f734f8..82bb3c3a477 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -391,14 +391,14 @@ vector<passivedouble> CDriverBase::GetMarkerVertexNormals(unsigned short iMarker
 }
 
 void CDriverBase::CommunicateMeshDisplacements() {
-  solver_container[selected_iZone][INST_0][MESH_0][MESH_SOL]->InitiateComms(main_geometry, main_config, MESH_DISPLACEMENTS);
-  solver_container[selected_iZone][INST_0][MESH_0][MESH_SOL]->CompleteComms(main_geometry, main_config, MESH_DISPLACEMENTS);
+  solver_container[selected_zone][INST_0][MESH_0][MESH_SOL]->InitiateComms(main_geometry, main_config, MESH_DISPLACEMENTS);
+  solver_container[selected_zone][INST_0][MESH_0][MESH_SOL]->CompleteComms(main_geometry, main_config, MESH_DISPLACEMENTS);
 }
 
 map<string, unsigned short> CDriverBase::GetSolverIndices() const {
   map<string, unsigned short> indexMap;
   for (auto iSol = 0u; iSol < MAX_SOLS; iSol++) {
-    const auto* solver = solver_container[selected_iZone][INST_0][MESH_0][iSol];
+    const auto* solver = solver_container[selected_zone][INST_0][MESH_0][iSol];
     if (solver != nullptr) {
       if (solver->GetSolverName().empty()) SU2_MPI::Error("Solver name was not defined.", CURRENT_FUNCTION);
       indexMap[solver->GetSolverName()] = iSol;
@@ -408,7 +408,7 @@ map<string, unsigned short> CDriverBase::GetSolverIndices() const {
 }
 
 std::map<string, unsigned short> CDriverBase::GetFEASolutionIndices() const {
-  if (solver_container[selected_iZone][INST_0][MESH_0][FEA_SOL] == nullptr) {
+  if (solver_container[selected_zone][INST_0][MESH_0][FEA_SOL] == nullptr) {
     SU2_MPI::Error("The FEA solver does not exist.", CURRENT_FUNCTION);
   }
   const auto nDim = main_geometry->GetnDim();
@@ -429,7 +429,7 @@ std::map<string, unsigned short> CDriverBase::GetFEASolutionIndices() const {
 }
 
 map<string, unsigned short> CDriverBase::GetPrimitiveIndices() const {
-  if (solver_container[selected_iZone][INST_0][MESH_0][FLOW_SOL] == nullptr) {
+  if (solver_container[selected_zone][INST_0][MESH_0][FLOW_SOL] == nullptr) {
     SU2_MPI::Error("The flow solver does not exist.", CURRENT_FUNCTION);
   }
   return PrimitiveNameToIndexMap(CPrimitiveIndices<unsigned short>(
diff --git a/SU2_CFD/src/drivers/CMultizoneDriver.cpp b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
index b3a7af5e369..14c31aa9ea3 100644
--- a/SU2_CFD/src/drivers/CMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
@@ -182,10 +182,7 @@ void CMultizoneDriver::StartSolver() {
 
     /*--- Run a block iteration of the multizone problem. ---*/
 
-    switch (driver_config->GetKind_MZSolver()){
-      case ENUM_MULTIZONE::MZ_BLOCK_GAUSS_SEIDEL: RunGaussSeidel(); break;  // Block Gauss-Seidel iteration
-      case ENUM_MULTIZONE::MZ_BLOCK_JACOBI: RunJacobi(); break;             // Block-Jacobi iteration
-    }
+    Run();
 
     /*--- Update the solution for dual time stepping strategy ---*/
 
@@ -646,11 +643,11 @@ void CMultizoneDriver::SetTurboPerformance() {
   }
 }
 
-bool CMultizoneDriver::Monitor(unsigned long TimeIter){
+bool CMultizoneDriver::Monitor(unsigned long TimeIter) {
 
   /*--- Check whether the inner solver has converged --- */
 
-  if (driver_config->GetTime_Domain() == NO){
+  if (driver_config->GetTime_Domain() == NO) {
 
     const auto OuterIter  = driver_config->GetOuterIter();
     const auto nOuterIter = driver_config->GetnOuter_Iter();
@@ -670,29 +667,27 @@ bool CMultizoneDriver::Monitor(unsigned long TimeIter){
   }
   // i.e. unsteady simulation
 
-    /*--- Check whether the outer time integration has reached the final time ---*/
-    const auto TimeConvergence = GetTimeConvergence();
+  /*--- Check whether the outer time integration has reached the final time. ---*/
+  const auto TimeConvergence = GetTimeConvergence();
 
-    const auto nTimeIter = driver_config->GetnTime_Iter();
-    const auto MaxTime   = driver_config->GetMax_Time();
-    const auto CurTime   = driver_output->GetHistoryFieldValue("CUR_TIME");
+  const auto nTimeIter = driver_config->GetnTime_Iter();
+  const auto MaxTime   = driver_config->GetMax_Time();
+  const auto CurTime   = driver_output->GetHistoryFieldValue("CUR_TIME");
 
-    const bool FinalTimeReached = (CurTime >= MaxTime);
-    const bool MaxIterationsReached = (TimeIter+1 >= nTimeIter);
+  const bool FinalTimeReached = (CurTime >= MaxTime);
+  const bool MaxIterationsReached = (TimeIter+1 >= nTimeIter);
 
-    if ((TimeConvergence || FinalTimeReached || MaxIterationsReached) && (rank == MASTER_NODE)){
-      cout << "\n----------------------------- Solver Exit -------------------------------";
-      if (TimeConvergence)  cout << "\nAll windowed time-averaged convergence criteria are fullfilled." << endl;
-      if (FinalTimeReached) cout << "\nMaximum time reached (MAX_TIME = " << MaxTime << "s)." << endl;
-      else cout << "\nMaximum number of time iterations reached (TIME_ITER = " << nTimeIter << ")." << endl;
-      cout << "-------------------------------------------------------------------------" << endl;
-    }
-
-    return (FinalTimeReached || MaxIterationsReached);
- 
+  if ((TimeConvergence || FinalTimeReached || MaxIterationsReached) && (rank == MASTER_NODE)){
+    cout << "\n----------------------------- Solver Exit -------------------------------";
+    if (TimeConvergence)  cout << "\nAll windowed time-averaged convergence criteria are fullfilled." << endl;
+    if (FinalTimeReached) cout << "\nMaximum time reached (MAX_TIME = " << MaxTime << "s)." << endl;
+    else cout << "\nMaximum number of time iterations reached (TIME_ITER = " << nTimeIter << ")." << endl;
+    cout << "-------------------------------------------------------------------------" << endl;
+  }
 
-  if (rank == MASTER_NODE) SetTurboPerformance();
+  if (rank == MASTER_NODE && driver_config->GetBoolTurbomachinery()) SetTurboPerformance();
 
+  return (FinalTimeReached || MaxIterationsReached);
 }
 
 bool CMultizoneDriver::GetTimeConvergence() const{
diff --git a/SU2_CFD/src/drivers/CSinglezoneDriver.cpp b/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
index c1f2c2519c8..f9fa11e87d6 100644
--- a/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
@@ -92,12 +92,6 @@ void CSinglezoneDriver::StartSolver() {
 
     Output(TimeIter);
 
-    /*--- Save iteration solution for libROM ---*/
-    if (config_container[MESH_0]->GetSave_libROM()) {
-      solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->SavelibROM(geometry_container[ZONE_0][INST_0][MESH_0],
-                                                                     config_container[ZONE_0], StopCalc);
-    }
-
     /*--- If the convergence criteria has been met, terminate the simulation. ---*/
 
     if (StopCalc) break;
@@ -208,7 +202,14 @@ void CSinglezoneDriver::Output(unsigned long TimeIter) {
                                                                solver_container[ZONE_0][INST_0][MESH_0],
                                                                TimeIter, StopCalc);
 
-  if (wrote_files){
+  /*--- Save iteration solution for libROM ---*/
+  if (config_container[MESH_0]->GetSave_libROM()) {
+    solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->SavelibROM(geometry_container[ZONE_0][INST_0][MESH_0],
+                                                                   config_container[ZONE_0], StopCalc);
+    wrote_files = true;
+  }
+
+  if (wrote_files) {
 
     StopTime = SU2_MPI::Wtime();
 
diff --git a/SU2_CFD/src/interfaces/fsi/CDiscAdjFlowTractionInterface.cpp b/SU2_CFD/src/interfaces/fsi/CDiscAdjFlowTractionInterface.cpp
index b8a48ae8fc4..2db45dd5825 100644
--- a/SU2_CFD/src/interfaces/fsi/CDiscAdjFlowTractionInterface.cpp
+++ b/SU2_CFD/src/interfaces/fsi/CDiscAdjFlowTractionInterface.cpp
@@ -40,11 +40,7 @@ void CDiscAdjFlowTractionInterface::GetPhysical_Constants(CSolver *flow_solution
                                                           CGeometry *flow_geometry, CGeometry *struct_geometry,
                                                           const CConfig *flow_config, const CConfig *struct_config){
 
-  /*--- We have to clear the traction before applying it, because we are "adding" to node and not "setting" ---*/
-
-  struct_solution->GetNodes()->Clear_FlowTraction();
-
-  Preprocess(flow_config);
+  Preprocess(flow_config, struct_config, struct_geometry, struct_solution);
 
   if (!conservative) ComputeVertexAreas(struct_config, struct_geometry, struct_solution);
 
diff --git a/SU2_CFD/src/interfaces/fsi/CFlowTractionInterface.cpp b/SU2_CFD/src/interfaces/fsi/CFlowTractionInterface.cpp
index 1aaa0d422fe..88ee4a5e41f 100644
--- a/SU2_CFD/src/interfaces/fsi/CFlowTractionInterface.cpp
+++ b/SU2_CFD/src/interfaces/fsi/CFlowTractionInterface.cpp
@@ -31,6 +31,7 @@
 #include "../../../../Common/include/geometry/CGeometry.hpp"
 #include "../../../include/solvers/CSolver.hpp"
 #include "../../../../Common/include/toolboxes/geometry_toolbox.hpp"
+#include "../../../Common/include/interface_interpolation/CInterpolator.hpp"
 #include <unordered_set>
 
 CFlowTractionInterface::CFlowTractionInterface(unsigned short val_nVar, unsigned short val_nConst,
@@ -39,7 +40,26 @@ CFlowTractionInterface::CFlowTractionInterface(unsigned short val_nVar, unsigned
   conservative(conservative_) {
 }
 
-void CFlowTractionInterface::Preprocess(const CConfig *flow_config) {
+void CFlowTractionInterface::Preprocess(const CConfig *flow_config, const CConfig *struct_config,
+                                        CGeometry *struct_geometry, CSolver *struct_solution) {
+
+  /*--- Clear the tractions only on the markers involved in interface, fluid tractions
+   * on other markers can be specified via e.g. the python wrapper. ---*/
+
+  for (auto iMarkerInt = 0u; iMarkerInt < struct_config->GetMarker_n_ZoneInterface()/2; iMarkerInt++) {
+    const auto markDonor = flow_config->FindInterfaceMarker(iMarkerInt);
+    const auto markTarget = struct_config->FindInterfaceMarker(iMarkerInt);
+
+    if(!CInterpolator::CheckInterfaceBoundary(markDonor, markTarget)) continue;
+    if (markTarget < 0) continue;
+
+    for (auto iVertex = 0ul; iVertex < struct_geometry->GetnVertex(markTarget); iVertex++) {
+      const auto iPoint = struct_geometry->vertex[markTarget][iVertex]->GetNode();
+      if (!struct_geometry->nodes->GetDomain(iPoint)) continue;
+      su2double zeros[3] = {};
+      struct_solution->GetNodes()->Set_FlowTraction(iPoint, zeros);
+    }
+  }
 
   /*--- Compute the constant factor to dimensionalize pressure and shear stress. ---*/
   const su2double *Velocity_ND, *Velocity_Real;
@@ -121,11 +141,7 @@ void CFlowTractionInterface::GetPhysical_Constants(CSolver *flow_solution, CSolv
                                                    CGeometry *flow_geometry, CGeometry *struct_geometry,
                                                    const CConfig *flow_config, const CConfig *struct_config) {
 
-  /*--- We have to clear the traction before applying it, because we are "adding" to node and not "setting" ---*/
-
-  struct_solution->GetNodes()->Clear_FlowTraction();
-
-  Preprocess(flow_config);
+  Preprocess(flow_config, struct_config, struct_geometry, struct_solution);
 
   if (!conservative) ComputeVertexAreas(struct_config, struct_geometry, struct_solution);
 
diff --git a/SU2_CFD/src/output/CElasticityOutput.cpp b/SU2_CFD/src/output/CElasticityOutput.cpp
index fe5efe5b390..71726c6ebb3 100644
--- a/SU2_CFD/src/output/CElasticityOutput.cpp
+++ b/SU2_CFD/src/output/CElasticityOutput.cpp
@@ -98,8 +98,10 @@ CElasticityOutput::CElasticityOutput(CConfig *config, unsigned short nDim) : COu
 
   /*--- Set the default convergence field --- */
 
-  if (convFields.empty() ) convFields.emplace_back("RMS_DISP_X");
-
+  if (convFields.empty()) {
+    if (linear_analysis) convFields.emplace_back("RMS_DISP_X");
+    if (nonlinear_analysis) convFields.emplace_back("RMS_UTOL");
+  }
 }
 
 void CElasticityOutput::LoadHistoryData(CConfig *config, CGeometry *geometry, CSolver **solver)  {
diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index a189217aa63..ac1b774e808 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -62,15 +62,15 @@ void CDriver::PreprocessPythonInterface(CConfig** config, CGeometry**** geometry
 /* Functions to obtain global parameters from SU2 (time steps, delta t, etc.)   */
 //////////////////////////////////////////////////////////////////////////////////
 
-unsigned long CDriver::GetNumberTimeIter() const { return config_container[selected_iZone]->GetnTime_Iter(); }
+unsigned long CDriver::GetNumberTimeIter() const { return config_container[selected_zone]->GetnTime_Iter(); }
 
 unsigned long CDriver::GetTimeIter() const { return TimeIter; }
 
 passivedouble CDriver::GetUnsteadyTimeStep() const {
-  return SU2_TYPE::GetValue(config_container[selected_iZone]->GetTime_Step());
+  return SU2_TYPE::GetValue(config_container[selected_zone]->GetTime_Step());
 }
 
-string CDriver::GetSurfaceFileName() const { return config_container[selected_iZone]->GetSurfCoeff_FileName(); }
+string CDriver::GetSurfaceFileName() const { return config_container[selected_zone]->GetSurfCoeff_FileName(); }
 
 ////////////////////////////////////////////////////////////////////////////////
 /* Functions related to the management of markers                             */
@@ -78,12 +78,12 @@ string CDriver::GetSurfaceFileName() const { return config_container[selected_iZ
 
 void CDriver::SetHeatSourcePosition(passivedouble alpha, passivedouble pos_x, passivedouble pos_y,
                                      passivedouble pos_z) {
-  CSolver* solver = solver_container[selected_iZone][INST_0][MESH_0][RAD_SOL];
+  CSolver* solver = solver_container[selected_zone][INST_0][MESH_0][RAD_SOL];
 
-  config_container[selected_iZone]->SetHeatSource_Rot_Z(alpha);
-  config_container[selected_iZone]->SetHeatSource_Center(pos_x, pos_y, pos_z);
+  config_container[selected_zone]->SetHeatSource_Rot_Z(alpha);
+  config_container[selected_zone]->SetHeatSource_Center(pos_x, pos_y, pos_z);
 
-  solver->SetVolumetricHeatSource(geometry_container[selected_iZone][INST_0][MESH_0], config_container[selected_iZone]);
+  solver->SetVolumetricHeatSource(geometry_container[selected_zone][INST_0][MESH_0], config_container[selected_zone]);
 }
 
 void CDriver::SetInletAngle(unsigned short iMarker, passivedouble alpha) {
@@ -91,20 +91,20 @@ void CDriver::SetInletAngle(unsigned short iMarker, passivedouble alpha) {
 
   unsigned long iVertex;
 
-  for (iVertex = 0; iVertex < geometry_container[selected_iZone][INST_0][MESH_0]->nVertex[iMarker]; iVertex++) {
-    solver_container[selected_iZone][INST_0][MESH_0][FLOW_SOL]->SetInlet_FlowDir(iMarker, iVertex, 0, cos(alpha_rad));
-    solver_container[selected_iZone][INST_0][MESH_0][FLOW_SOL]->SetInlet_FlowDir(iMarker, iVertex, 1, sin(alpha_rad));
+  for (iVertex = 0; iVertex < geometry_container[selected_zone][INST_0][MESH_0]->nVertex[iMarker]; iVertex++) {
+    solver_container[selected_zone][INST_0][MESH_0][FLOW_SOL]->SetInlet_FlowDir(iMarker, iVertex, 0, cos(alpha_rad));
+    solver_container[selected_zone][INST_0][MESH_0][FLOW_SOL]->SetInlet_FlowDir(iMarker, iVertex, 1, sin(alpha_rad));
   }
 }
 
 void CDriver::SetFarFieldAoA(const passivedouble AoA) {
-  config_container[ZONE_0]->SetAoA(AoA);
-  solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->UpdateFarfieldVelocity(config_container[ZONE_0]);
+  config_container[selected_zone]->SetAoA(AoA);
+  solver_container[selected_zone][INST_0][MESH_0][FLOW_SOL]->UpdateFarfieldVelocity(config_container[selected_zone]);
 }
 
 void CDriver::SetFarFieldAoS(const passivedouble AoS) {
-  config_container[ZONE_0]->SetAoS(AoS);
-  solver_container[ZONE_0][INST_0][MESH_0][FLOW_SOL]->UpdateFarfieldVelocity(config_container[ZONE_0]);
+  config_container[selected_zone]->SetAoS(AoS);
+  solver_container[selected_zone][INST_0][MESH_0][FLOW_SOL]->UpdateFarfieldVelocity(config_container[selected_zone]);
 }
 
 /////////////////////////////////////////////////////////////////////////////////////////////////////////////////
@@ -116,22 +116,22 @@ void CSinglezoneDriver::SetInitialMesh() {
 
   SU2_OMP_PARALLEL {
     for (iMesh = 0u; iMesh <= main_config->GetnMGLevels(); iMesh++) {
-      SU2_OMP_FOR_STAT(roundUpDiv(geometry_container[selected_iZone][INST_0][iMesh]->GetnPoint(), omp_get_max_threads()))
-      for (auto iPoint = 0ul; iPoint < geometry_container[selected_iZone][INST_0][iMesh]->GetnPoint(); iPoint++) {
+      SU2_OMP_FOR_STAT(roundUpDiv(geometry_container[selected_zone][INST_0][iMesh]->GetnPoint(), omp_get_max_threads()))
+      for (auto iPoint = 0ul; iPoint < geometry_container[selected_zone][INST_0][iMesh]->GetnPoint(); iPoint++) {
         /*--- Overwrite fictitious velocities. ---*/
         su2double Grid_Vel[3] = {0.0, 0.0, 0.0};
 
         /*--- Set the grid velocity for this coarse node. ---*/
-        geometry_container[selected_iZone][INST_0][iMesh]->nodes->SetGridVel(iPoint, Grid_Vel);
+        geometry_container[selected_zone][INST_0][iMesh]->nodes->SetGridVel(iPoint, Grid_Vel);
       }
       END_SU2_OMP_FOR
       /*--- Push back the volume. ---*/
-      geometry_container[selected_iZone][INST_0][iMesh]->nodes->SetVolume_n();
-      geometry_container[selected_iZone][INST_0][iMesh]->nodes->SetVolume_nM1();
+      geometry_container[selected_zone][INST_0][iMesh]->nodes->SetVolume_n();
+      geometry_container[selected_zone][INST_0][iMesh]->nodes->SetVolume_nM1();
     }
     /*--- Push back the solution so that there is no fictitious velocity at the next step. ---*/
-    solver_container[selected_iZone][INST_0][MESH_0][MESH_SOL]->GetNodes()->Set_Solution_time_n();
-    solver_container[selected_iZone][INST_0][MESH_0][MESH_SOL]->GetNodes()->Set_Solution_time_n1();
+    solver_container[selected_zone][INST_0][MESH_0][MESH_SOL]->GetNodes()->Set_Solution_time_n();
+    solver_container[selected_zone][INST_0][MESH_0][MESH_SOL]->GetNodes()->Set_Solution_time_n1();
   }
   END_SU2_OMP_PARALLEL
 }
@@ -143,7 +143,7 @@ void CDriver::BoundaryConditionsUpdate() {
 
   if (rank == MASTER_NODE) cout << "Updating boundary conditions." << endl;
   for (auto iZone = 0u; iZone < nZone; iZone++) {
-    geometry_container[iZone][INST_0][MESH_0]->UpdateCustomBoundaryConditions(geometry_container[iZone][INST_0],config_container[iZone]);
+    geometry_container[iZone][INST_0][MESH_0]->UpdateCustomBoundaryConditions(geometry_container[iZone][INST_0], config_container[iZone]);
   }
 }
 
@@ -152,18 +152,14 @@ void CDriver::BoundaryConditionsUpdate() {
 ////////////////////////////////////////////////////////////////////////////////
 
 void CDriver::SetTranslationRate(passivedouble xDot, passivedouble yDot, passivedouble zDot) {
-  for (iZone = 0; iZone < nZone; iZone++) {
-    config_container[iZone]->SetTranslation_Rate(0, xDot);
-    config_container[iZone]->SetTranslation_Rate(1, yDot);
-    config_container[iZone]->SetTranslation_Rate(2, zDot);
-  }
+  main_config->SetTranslation_Rate(0, xDot);
+  main_config->SetTranslation_Rate(1, yDot);
+  main_config->SetTranslation_Rate(2, zDot);
 }
 
 void CDriver::SetRotationRate(passivedouble rot_x, passivedouble rot_y, passivedouble rot_z) {
-  for (iZone = 0; iZone < nZone; iZone++) {
-    config_container[iZone]->SetRotation_Rate(0, rot_x);
-    config_container[iZone]->SetRotation_Rate(1, rot_y);
-    config_container[iZone]->SetRotation_Rate(2, rot_z);
-  }
+  main_config->SetRotation_Rate(0, rot_x);
+  main_config->SetRotation_Rate(1, rot_y);
+  main_config->SetRotation_Rate(2, rot_z);
 }
 
diff --git a/SU2_CFD/src/variables/CFEABoundVariable.cpp b/SU2_CFD/src/variables/CFEABoundVariable.cpp
index 012498896ad..04d1e676260 100644
--- a/SU2_CFD/src/variables/CFEABoundVariable.cpp
+++ b/SU2_CFD/src/variables/CFEABoundVariable.cpp
@@ -65,8 +65,6 @@ void CFEABoundVariable::Set_FlowTraction_n() { FlowTraction_n = FlowTraction; }
 
 void CFEABoundVariable::Set_SurfaceLoad_Res_n() { Residual_Ext_Surf_n = Residual_Ext_Surf; }
 
-void CFEABoundVariable::Clear_FlowTraction() { FlowTraction.setConstant(0.0); }
-
 void CFEABoundVariable::Clear_SurfaceLoad_Res() { Residual_Ext_Surf.setConstant(0.0); }
 
 void CFEABoundVariable::RegisterFlowTraction(bool reset) {
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index 81ed8e4f1c5..e86bf444a5f 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -256,6 +256,8 @@ def main():
     polar_naca0012.test_vals         = [-1.217981, 4.256386, 0.009084, 0.016823]
     polar_naca0012.test_vals_aarch64 = [-1.718925, 3.711429, 0.009217, 0.007784]
     polar_naca0012.command   = TestCase.Command(exec = "compute_polar.py", param = "-i 11")
+    # flaky test on arm64
+    polar_naca0012.enabled_on_cpu_arch = ["x86_64"]
     test_list.append(polar_naca0012)
 
     # HYPERSONIC FLOW PAST BLUNT BODY
@@ -1349,6 +1351,17 @@ def main():
     pywrapper_fsi2d.multizone = True
     test_list.append(pywrapper_fsi2d)
 
+    # Unsteady FSI with custom load
+    pywrapper_unsteadyFSI = TestCase('pywrapper_unsteadyFSI')
+    pywrapper_unsteadyFSI.cfg_dir = "py_wrapper/dyn_fsi"
+    pywrapper_unsteadyFSI.cfg_file = "config.cfg"
+    pywrapper_unsteadyFSI.test_iter = 4
+    pywrapper_unsteadyFSI.test_vals = [0, 31, 5, 58, -1.756780, -2.828276, -7.652558, -6.863929, 1.5618e-04]
+    pywrapper_unsteadyFSI.command = TestCase.Command("mpirun -np 2", "python", "run.py")
+    pywrapper_unsteadyFSI.unsteady  = True
+    pywrapper_unsteadyFSI.multizone = True
+    test_list.append(pywrapper_unsteadyFSI)
+
     # Unsteady CHT
     pywrapper_unsteadyCHT               = TestCase('pywrapper_unsteadyCHT')
     pywrapper_unsteadyCHT.cfg_dir       = "py_wrapper/flatPlate_unsteady_CHT"
diff --git a/TestCases/py_wrapper/dyn_fsi/config.cfg b/TestCases/py_wrapper/dyn_fsi/config.cfg
new file mode 100644
index 00000000000..28bafc8fccc
--- /dev/null
+++ b/TestCases/py_wrapper/dyn_fsi/config.cfg
@@ -0,0 +1,31 @@
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+% SU2 configuration file                                                       %
+% Case description: Fluid Structure Interaction - Wall in channel              %
+% Author: R.Sanchez                                                            %
+% Institution: Imperial College London                                         %
+% Date: 2016.02.01                                                             %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+SOLVER= MULTIPHYSICS
+
+CONFIG_LIST= (configFlow.cfg, configFEA.cfg)
+
+MARKER_ZONE_INTERFACE= (wallUpperF, wallUpperS, wallUpwF, wallUpwS, wallDownF, wallDownS)
+
+MULTIZONE_MESH= NO
+
+TIME_DOMAIN= YES
+TIME_ITER= 5
+TIME_STEP= 0.002
+SCREEN_OUTPUT= (TIME_ITER, OUTER_ITER, INNER_ITER[0], INNER_ITER[1], DEFORM_ITER[0],\
+                BGS_DENSITY[0], AVG_BGS_RES[1], RMS_DENSITY[0], RMS_UTOL[1], REFERENCE_NODE[1])
+RESTART_SOL= NO
+RESTART_ITER= 2
+
+OUTER_ITER= 10
+CONV_FIELD= BGS_DENSITY[0], AVG_BGS_RES[1]
+CONV_RESIDUAL_MINVAL= -5
+
+OUTPUT_FILES= RESTART, PARAVIEW
+OUTPUT_WRT_FREQ= 1
+WRT_ZONE_HIST= YES
diff --git a/TestCases/py_wrapper/dyn_fsi/configFEA.cfg b/TestCases/py_wrapper/dyn_fsi/configFEA.cfg
new file mode 100644
index 00000000000..d782e3a1003
--- /dev/null
+++ b/TestCases/py_wrapper/dyn_fsi/configFEA.cfg
@@ -0,0 +1,54 @@
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+% SU2 configuration file                                                       %
+% Case description: Fluid Structure Interaction - Wall in channel              %
+% Author: R.Sanchez                                                            %
+% Institution: Imperial College London                                         %
+% Date: 2016.02.01                                                             %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+SOLVER= ELASTICITY
+
+OBJECTIVE_FUNCTION= REFERENCE_NODE
+REFERENCE_NODE= 3
+REFERENCE_NODE_DISPLACEMENT= (0.0, 0.0)
+REFERENCE_NODE_PENALTY= 1.0
+
+GEOMETRIC_CONDITIONS= LARGE_DEFORMATIONS
+MATERIAL_MODEL= NEO_HOOKEAN
+ELASTICITY_MODULUS= 1.5E5
+MATERIAL_DENSITY= 50
+FORMULATION_ELASTICITY_2D= PLANE_STRESS
+POISSON_RATIO= 0.3
+
+MARKER_CLAMPED= ( clamped )
+MARKER_FLUID_LOAD= ( wallDownS, wallUpperS, wallUpwS, internal )
+
+BGS_RELAXATION= FIXED_PARAMETER
+STAT_RELAX_PARAMETER= 0.5
+
+LINEAR_SOLVER= CONJUGATE_GRADIENT
+LINEAR_SOLVER_PREC= ILU
+LINEAR_SOLVER_ERROR= 1E-6
+LINEAR_SOLVER_ITER= 1000
+
+TIME_DISCRE_FEA= NEWMARK_IMPLICIT
+NEWMARK_BETA= 0.25
+NEWMARK_GAMMA= 0.5
+
+PREDICTOR= YES
+RELAXATION= YES
+
+INNER_ITER= 10
+CONV_FIELD= REL_RMS_UTOL
+CONV_RESIDUAL_MINVAL= -5
+
+SCREEN_WRT_FREQ_INNER= 100
+
+MESH_FORMAT= SU2
+MESH_FILENAME= meshFEA.su2
+
+VOLUME_FILENAME= results_wall
+RESTART_FILENAME= restart_wall.dat
+SOLUTION_FILENAME= solution_wall.dat
+
+HISTORY_OUTPUT= ITER, RMS_RES, STRUCT_COEFF, TAVG_STRUCT_COEFF
diff --git a/TestCases/py_wrapper/dyn_fsi/configFlow.cfg b/TestCases/py_wrapper/dyn_fsi/configFlow.cfg
new file mode 100644
index 00000000000..6b1df89cc7f
--- /dev/null
+++ b/TestCases/py_wrapper/dyn_fsi/configFlow.cfg
@@ -0,0 +1,80 @@
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+% SU2 configuration file                                                       %
+% Case description: Fluid Structure Interaction - Wall in channel              %
+% Author: R.Sanchez                                                            %
+% Institution: Imperial College London                                         %
+% Date: 2016.02.01                                                             %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+SOLVER= NAVIER_STOKES
+KIND_TURB_MODEL= NONE
+DEFORM_MESH= YES
+
+MATH_PROBLEM= DIRECT
+
+AOA= 0.0
+REYNOLDS_NUMBER= 100
+REYNOLDS_LENGTH= 0.016
+MACH_NUMBER= 0.05
+MACH_MOTION= 0.2
+
+INIT_OPTION= TD_CONDITIONS
+FREESTREAM_OPTION= DENSITY_FS
+FREESTREAM_DENSITY= 1.0
+FREESTREAM_PRESSURE= 17.85714286
+FREESTREAM_TEMPERATURE= 0.062207438
+
+VISCOSITY_MODEL= CONSTANT_VISCOSITY
+MU_CONSTANT= 1.6E-2
+
+REF_ORIGIN_MOMENT_X= 0
+REF_ORIGIN_MOMENT_Y= 0
+REF_ORIGIN_MOMENT_Z= 0
+REF_LENGTH= 0.016
+REF_AREA= 0.016
+
+MARKER_INLET= ( inlet, 0.062207438, 23.36216288, 1.0, 0.0, 0.0 )
+MARKER_OUTLET= ( outlet, 17.85714286)
+MARKER_EULER= ( upper, lower )
+
+MARKER_HEATFLUX= ( wallUpwF, 0.0, wallDownF, 0.0, wallUpperF, 0.0 )
+MARKER_DEFORM_MESH= ( wallUpwF, wallDownF, wallUpperF )
+MARKER_DEFORM_MESH_SYM_PLANE= ( upper )
+
+MARKER_PLOTTING= ( wallUpwF, wallDownF, wallUpperF )
+MARKER_MONITORING= ( wallUpwF, wallDownF, wallUpperF )
+
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+CFL_NUMBER= 1000
+LINEAR_SOLVER= FGMRES
+LINEAR_SOLVER_PREC= ILU
+LINEAR_SOLVER_ERROR= 0.05
+LINEAR_SOLVER_ITER= 6
+
+TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
+CONV_NUM_METHOD_FLOW= ROE
+MUSCL_FLOW= YES
+NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
+SLOPE_LIMITER_FLOW= NONE
+
+DEFORM_LINEAR_SOLVER= CONJUGATE_GRADIENT
+DEFORM_LINEAR_SOLVER_PREC= ILU
+DEFORM_LINEAR_SOLVER_ERROR= 1E-9
+DEFORM_LINEAR_SOLVER_ITER= 100
+DEFORM_STIFFNESS_TYPE= WALL_DISTANCE
+
+INNER_ITER= 50
+CONV_FIELD= REL_RMS_DENSITY
+CONV_RESIDUAL_MINVAL= -3
+CONV_STARTITER= 5
+
+SCREEN_WRT_FREQ_INNER= 100
+
+MESH_FORMAT= SU2
+MESH_FILENAME= meshFlow.su2
+
+VOLUME_FILENAME= results_flow
+RESTART_FILENAME= restart_flow.dat
+SOLUTION_FILENAME= solution_flow.dat
+
+HISTORY_OUTPUT= ITER, RMS_RES, AERO_COEFF, TAVG_AERO_COEFF
diff --git a/TestCases/py_wrapper/dyn_fsi/run.py b/TestCases/py_wrapper/dyn_fsi/run.py
new file mode 100644
index 00000000000..ba6253db6b8
--- /dev/null
+++ b/TestCases/py_wrapper/dyn_fsi/run.py
@@ -0,0 +1,83 @@
+#!/usr/bin/env python
+
+## \file run.py
+#  \brief Unsteady FSI case with custom load.
+#  \version 7.5.1 "Blackbird"
+#
+# SU2 Project Website: https://su2code.github.io
+#
+# The SU2 Project is maintained by the SU2 Foundation
+# (http://su2foundation.org)
+#
+# Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md)
+#
+# SU2 is free software; you can redistribute it and/or
+# modify it under the terms of the GNU Lesser General Public
+# License as published by the Free Software Foundation; either
+# version 2.1 of the License, or (at your option) any later version.
+#
+# SU2 is distributed in the hope that it will be useful,
+# but WITHOUT ANY WARRANTY; without even the implied warranty of
+# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+# Lesser General Public License for more details.
+#
+# You should have received a copy of the GNU Lesser General Public
+# License along with SU2. If not, see <http://www.gnu.org/licenses/>.
+
+import sys
+import pysu2
+import math
+from mpi4py import MPI
+
+def main():
+  comm = MPI.COMM_WORLD
+  rank = comm.Get_rank()
+
+  # Initialize the corresponding driver of SU2, this includes solver preprocessing.
+  try:
+    driver = pysu2.CMultizoneDriver('config.cfg', 2, comm)
+  except TypeError as exception:
+    print('A TypeError occured in pysu2.CDriver : ', exception)
+    raise
+
+  # By default the first zone is selected (flow in the case).
+  # Select the structural zone (second zone) to work with the FEA solver.
+  driver.SelectZone(1)
+
+  # Get the ID of the marker where we will apply a force.
+  # This marker cannot be used by the fluid-solid interface otherwise the imposed
+  # load will be cleared when interpolating forces.
+  all_marker_ids = driver.GetMarkerIndices()
+  ctrl_id = all_marker_ids['internal'] if 'internal' in all_marker_ids else -1
+
+  # Number of vertices on the specified markers (per rank).
+  n_vertex_ctrl = driver.GetNumberMarkerNodes(ctrl_id) if ctrl_id >= 0 else 0
+
+  if rank == 0:
+    print("\n------------------------------ Begin Solver -----------------------------")
+    sys.stdout.flush()
+
+  for time_iter in range(driver.GetNumberTimeIter()):
+    # Apply a custom load and then solve the time step.
+    time = time_iter * driver.GetUnsteadyTimeStep()
+    for i_vertex in range(n_vertex_ctrl):
+      i_point = driver.GetMarkerNode(ctrl_id, i_vertex)
+      if driver.GetNodeDomain(i_point):
+        driver.SetMarkerCustomFEALoad(ctrl_id, i_vertex, (-0.002 + 0.002 * math.cos(2 * math.pi * time / 0.02), 0))
+
+    driver.Preprocess(time_iter)
+
+    driver.Run()
+    driver.Postprocess()
+    driver.Update()
+
+    stop = driver.Monitor(time_iter)
+    driver.Output(time_iter)
+    if stop: break
+
+  # Finalize the solver and exit cleanly.
+  driver.Finalize()
+
+
+if __name__ == '__main__':
+  main()
diff --git a/TestCases/serial_regression.py b/TestCases/serial_regression.py
index d6512b98c8b..0ca25c6f3c4 100644
--- a/TestCases/serial_regression.py
+++ b/TestCases/serial_regression.py
@@ -135,6 +135,8 @@ def main():
     polar_naca0012.test_vals         = [-1.243326, 4.224483, 0.016432, 0.016145]
     polar_naca0012.test_vals_aarch64 = [-1.811046, 3.612379, 0.012330, 0.009194]
     polar_naca0012.command   = TestCase.Command(exec = "compute_polar.py", param = "-n 1 -i 11")
+    # flaky test on arm64
+    polar_naca0012.enabled_on_cpu_arch = ["x86_64"]
     test_list.append(polar_naca0012)
 
     # HYPERSONIC FLOW PAST BLUNT BODY
diff --git a/TestCases/vandv.py b/TestCases/vandv.py
index baba0b84169..a5757cd7043 100644
--- a/TestCases/vandv.py
+++ b/TestCases/vandv.py
@@ -95,6 +95,7 @@ def main():
     sandiajet_sst.cfg_file  = "validation.cfg"
     sandiajet_sst.test_iter = 5
     sandiajet_sst.test_vals = [-16.249917, -13.835991, -14.303372, -13.276035, -10.074262, -14.027223, 5, -1.672359, 5, -4.938477, 5, -3.462217, 2.5859e-04, 2.8215e-32, 4.5010e-68, 2.5859e-04, 4.0474e+03, 3.9468e+03, 4.9170e+01, 5.1441e+01]
+    sandiajet_sst.test_vals_aarch64 = [-16.249289, -13.833785, -14.303058, -13.276559, -10.267928, -14.027240, 5, -1.676412, 5, -4.815216, 5, -3.462247, 0.000259, 0, 0, 0.000259, 4047.4, 3946.8, 49.17, 51.441]
     test_list.append(sandiajet_sst)
 
     #################

From e7d88da1c5461200e33e6897393f0583d56d8b6d Mon Sep 17 00:00:00 2001
From: GitHub Action <action@github.com>
Date: Tue, 29 Aug 2023 01:11:00 +0000
Subject: [PATCH 656/656] Changing version number to 8.0.0

---
 Common/include/CConfig.hpp                    |  2 +-
 Common/include/adt/CADTBaseClass.hpp          |  2 +-
 Common/include/adt/CADTComparePointClass.hpp  |  2 +-
 Common/include/adt/CADTElemClass.hpp          |  4 ++--
 Common/include/adt/CADTNodeClass.hpp          |  2 +-
 Common/include/adt/CADTPointsOnlyClass.hpp    |  2 +-
 Common/include/adt/CBBoxTargetClass.hpp       |  4 ++--
 Common/include/basic_types/ad_structure.hpp   |  2 +-
 .../basic_types/datatype_structure.hpp        |  2 +-
 Common/include/code_config.hpp                |  2 +-
 Common/include/containers/C2DContainer.hpp    |  2 +-
 .../containers/CFastFindAndEraseQueue.hpp     |  2 +-
 Common/include/containers/CFileReaderLUT.hpp  |  2 +-
 Common/include/containers/CLookUpTable.hpp    |  2 +-
 .../containers/CPyWrapperMatrixView.hpp       |  2 +-
 Common/include/containers/CTrapezoidalMap.hpp |  4 ++--
 Common/include/containers/CVertexMap.hpp      |  2 +-
 .../containers/container_decorators.hpp       |  2 +-
 Common/include/fem/fem_cgns_elements.hpp      |  2 +-
 .../fem/fem_gauss_jacobi_quadrature.hpp       |  4 ++--
 Common/include/fem/fem_geometry_structure.hpp | 24 +++++++++----------
 Common/include/fem/fem_standard_element.hpp   | 10 ++++----
 .../fem/geometry_structure_fem_part.hpp       |  2 +-
 Common/include/geometry/CDummyGeometry.hpp    |  2 +-
 Common/include/geometry/CGeometry.hpp         |  2 +-
 .../include/geometry/CMultiGridGeometry.hpp   |  2 +-
 Common/include/geometry/CMultiGridQueue.hpp   |  2 +-
 Common/include/geometry/CPhysicalGeometry.hpp |  2 +-
 .../include/geometry/dual_grid/CDualGrid.hpp  |  2 +-
 Common/include/geometry/dual_grid/CEdge.hpp   |  2 +-
 Common/include/geometry/dual_grid/CPoint.hpp  |  2 +-
 .../geometry/dual_grid/CTurboVertex.hpp       |  2 +-
 Common/include/geometry/dual_grid/CVertex.hpp |  2 +-
 Common/include/geometry/elements/CElement.hpp |  4 ++--
 .../geometry/elements/CElementProperty.hpp    |  6 ++---
 .../geometry/elements/CGaussVariable.hpp      |  4 ++--
 .../geometry/meshreader/CBoxMeshReaderFVM.hpp |  2 +-
 .../meshreader/CCGNSMeshReaderFVM.hpp         |  2 +-
 .../geometry/meshreader/CMeshReaderFVM.hpp    |  2 +-
 .../meshreader/CRectangularMeshReaderFVM.hpp  |  2 +-
 .../meshreader/CSU2ASCIIMeshReaderFVM.hpp     |  2 +-
 .../geometry/primal_grid/CHexahedron.hpp      |  2 +-
 Common/include/geometry/primal_grid/CLine.hpp |  2 +-
 .../geometry/primal_grid/CPrimalGrid.hpp      |  2 +-
 .../primal_grid/CPrimalGridBoundFEM.hpp       |  4 ++--
 .../geometry/primal_grid/CPrimalGridFEM.hpp   |  4 ++--
 .../include/geometry/primal_grid/CPrism.hpp   |  2 +-
 .../include/geometry/primal_grid/CPyramid.hpp |  2 +-
 .../geometry/primal_grid/CQuadrilateral.hpp   |  2 +-
 .../geometry/primal_grid/CTetrahedron.hpp     |  2 +-
 .../geometry/primal_grid/CTriangle.hpp        |  2 +-
 .../geometry/primal_grid/CVertexMPI.hpp       |  2 +-
 Common/include/graph_coloring_structure.hpp   |  4 ++--
 .../grid_movement/CBSplineBlending.hpp        |  2 +-
 .../include/grid_movement/CBezierBlending.hpp |  2 +-
 .../grid_movement/CFreeFormBlending.hpp       |  2 +-
 .../include/grid_movement/CFreeFormDefBox.hpp |  2 +-
 .../include/grid_movement/CGridMovement.hpp   |  2 +-
 .../grid_movement/CSurfaceMovement.hpp        |  2 +-
 .../grid_movement/CVolumetricMovement.hpp     |  2 +-
 .../interface_interpolation/CInterpolator.hpp |  2 +-
 .../CInterpolatorFactory.hpp                  |  2 +-
 .../CIsoparametric.hpp                        |  2 +-
 .../interface_interpolation/CMirror.hpp       |  2 +-
 .../CNearestNeighbor.hpp                      |  2 +-
 .../CRadialBasisFunction.hpp                  |  2 +-
 .../interface_interpolation/CSlidingMesh.hpp  |  2 +-
 .../linear_algebra/CMatrixVectorProduct.hpp   |  2 +-
 .../include/linear_algebra/CPastixWrapper.hpp |  2 +-
 .../linear_algebra/CPreconditioner.hpp        |  2 +-
 Common/include/linear_algebra/CSysMatrix.hpp  |  2 +-
 Common/include/linear_algebra/CSysMatrix.inl  |  2 +-
 Common/include/linear_algebra/CSysSolve.hpp   |  2 +-
 Common/include/linear_algebra/CSysSolve_b.hpp |  2 +-
 Common/include/linear_algebra/CSysVector.hpp  |  2 +-
 .../include/linear_algebra/blas_structure.hpp |  4 ++--
 .../linear_algebra/vector_expressions.hpp     |  2 +-
 Common/include/option_structure.hpp           |  2 +-
 Common/include/option_structure.inl           |  2 +-
 .../include/parallelization/mpi_structure.cpp |  2 +-
 .../include/parallelization/mpi_structure.hpp |  2 +-
 .../include/parallelization/omp_structure.cpp |  2 +-
 .../include/parallelization/omp_structure.hpp |  2 +-
 .../parallelization/special_vectorization.hpp |  2 +-
 .../include/parallelization/vectorization.hpp |  2 +-
 Common/include/toolboxes/C1DInterpolation.hpp |  2 +-
 .../include/toolboxes/CLinearPartitioner.hpp  |  2 +-
 .../toolboxes/CQuasiNewtonInvLeastSquares.hpp |  2 +-
 Common/include/toolboxes/CSquareMatrixCM.hpp  |  2 +-
 Common/include/toolboxes/CSymmetricMatrix.hpp |  2 +-
 .../include/toolboxes/MMS/CIncTGVSolution.hpp |  2 +-
 .../toolboxes/MMS/CInviscidVortexSolution.hpp |  2 +-
 .../toolboxes/MMS/CMMSIncEulerSolution.hpp    |  2 +-
 .../toolboxes/MMS/CMMSIncNSSolution.hpp       |  2 +-
 .../MMS/CMMSNSTwoHalfCirclesSolution.hpp      |  2 +-
 .../MMS/CMMSNSTwoHalfSpheresSolution.hpp      |  2 +-
 .../toolboxes/MMS/CMMSNSUnitQuadSolution.hpp  |  2 +-
 .../MMS/CMMSNSUnitQuadSolutionWallBC.hpp      |  2 +-
 .../toolboxes/MMS/CNSUnitQuadSolution.hpp     |  2 +-
 .../toolboxes/MMS/CRinglebSolution.hpp        |  2 +-
 Common/include/toolboxes/MMS/CTGVSolution.hpp |  2 +-
 .../toolboxes/MMS/CUserDefinedSolution.hpp    |  2 +-
 .../toolboxes/MMS/CVerificationSolution.hpp   |  2 +-
 .../include/toolboxes/allocation_toolbox.hpp  |  2 +-
 Common/include/toolboxes/geometry_toolbox.hpp |  2 +-
 Common/include/toolboxes/graph_toolbox.hpp    |  2 +-
 Common/include/toolboxes/ndflattener.hpp      |  2 +-
 Common/include/toolboxes/printing_toolbox.hpp |  2 +-
 Common/include/wall_model.hpp                 |  4 ++--
 Common/src/CConfig.cpp                        |  4 ++--
 Common/src/adt/CADTBaseClass.cpp              |  2 +-
 Common/src/adt/CADTElemClass.cpp              |  2 +-
 Common/src/adt/CADTPointsOnlyClass.cpp        |  2 +-
 Common/src/basic_types/ad_structure.cpp       |  2 +-
 Common/src/containers/CFileReaderLUT.cpp      |  2 +-
 Common/src/containers/CLookUpTable.cpp        |  2 +-
 Common/src/containers/CTrapezoidalMap.cpp     |  2 +-
 Common/src/fem/fem_cgns_elements.cpp          |  2 +-
 .../src/fem/fem_gauss_jacobi_quadrature.cpp   |  2 +-
 Common/src/fem/fem_geometry_structure.cpp     |  2 +-
 Common/src/fem/fem_integration_rules.cpp      |  2 +-
 Common/src/fem/fem_standard_element.cpp       |  2 +-
 Common/src/fem/fem_wall_distance.cpp          |  2 +-
 Common/src/fem/fem_work_estimate_metis.cpp    |  2 +-
 .../src/fem/geometry_structure_fem_part.cpp   |  2 +-
 Common/src/geometry/CDummyGeometry.cpp        |  2 +-
 Common/src/geometry/CGeometry.cpp             |  2 +-
 Common/src/geometry/CMultiGridGeometry.cpp    |  2 +-
 Common/src/geometry/CMultiGridQueue.cpp       |  2 +-
 Common/src/geometry/CPhysicalGeometry.cpp     |  2 +-
 Common/src/geometry/dual_grid/CDualGrid.cpp   |  2 +-
 Common/src/geometry/dual_grid/CEdge.cpp       |  2 +-
 Common/src/geometry/dual_grid/CPoint.cpp      |  2 +-
 .../src/geometry/dual_grid/CTurboVertex.cpp   |  2 +-
 Common/src/geometry/dual_grid/CVertex.cpp     |  2 +-
 Common/src/geometry/elements/CElement.cpp     |  2 +-
 Common/src/geometry/elements/CHEXA8.cpp       |  2 +-
 Common/src/geometry/elements/CLINE.cpp        |  2 +-
 Common/src/geometry/elements/CPRISM6.cpp      |  2 +-
 Common/src/geometry/elements/CPYRAM5.cpp      |  2 +-
 Common/src/geometry/elements/CPYRAM6.cpp      |  2 +-
 Common/src/geometry/elements/CQUAD4.cpp       |  2 +-
 Common/src/geometry/elements/CTETRA1.cpp      |  2 +-
 Common/src/geometry/elements/CTETRA4.cpp      |  2 +-
 Common/src/geometry/elements/CTRIA1.cpp       |  2 +-
 Common/src/geometry/elements/CTRIA3.cpp       |  2 +-
 .../geometry/meshreader/CBoxMeshReaderFVM.cpp |  2 +-
 .../meshreader/CCGNSMeshReaderFVM.cpp         |  2 +-
 .../geometry/meshreader/CMeshReaderFVM.cpp    |  2 +-
 .../meshreader/CRectangularMeshReaderFVM.cpp  |  2 +-
 .../meshreader/CSU2ASCIIMeshReaderFVM.cpp     |  2 +-
 .../src/geometry/primal_grid/CHexahedron.cpp  |  2 +-
 Common/src/geometry/primal_grid/CLine.cpp     |  2 +-
 .../src/geometry/primal_grid/CPrimalGrid.cpp  |  2 +-
 .../primal_grid/CPrimalGridBoundFEM.cpp       |  2 +-
 .../geometry/primal_grid/CPrimalGridFEM.cpp   |  2 +-
 Common/src/geometry/primal_grid/CPrism.cpp    |  2 +-
 Common/src/geometry/primal_grid/CPyramid.cpp  |  2 +-
 .../geometry/primal_grid/CQuadrilateral.cpp   |  2 +-
 .../src/geometry/primal_grid/CTetrahedron.cpp |  2 +-
 Common/src/geometry/primal_grid/CTriangle.cpp |  2 +-
 .../src/geometry/primal_grid/CVertexMPI.cpp   |  2 +-
 Common/src/graph_coloring_structure.cpp       |  2 +-
 Common/src/grid_movement/CBSplineBlending.cpp |  2 +-
 Common/src/grid_movement/CBezierBlending.cpp  |  2 +-
 .../src/grid_movement/CFreeFormBlending.cpp   |  2 +-
 Common/src/grid_movement/CFreeFormDefBox.cpp  |  2 +-
 Common/src/grid_movement/CGridMovement.cpp    |  2 +-
 Common/src/grid_movement/CSurfaceMovement.cpp |  2 +-
 .../src/grid_movement/CVolumetricMovement.cpp |  2 +-
 .../interface_interpolation/CInterpolator.cpp |  2 +-
 .../CInterpolatorFactory.cpp                  |  2 +-
 .../CIsoparametric.cpp                        |  2 +-
 .../src/interface_interpolation/CMirror.cpp   |  2 +-
 .../CNearestNeighbor.cpp                      |  2 +-
 .../CRadialBasisFunction.cpp                  |  2 +-
 .../interface_interpolation/CSlidingMesh.cpp  |  2 +-
 Common/src/linear_algebra/CPastixWrapper.cpp  |  2 +-
 Common/src/linear_algebra/CSysMatrix.cpp      |  2 +-
 Common/src/linear_algebra/CSysSolve.cpp       |  2 +-
 Common/src/linear_algebra/CSysSolve_b.cpp     |  2 +-
 Common/src/linear_algebra/CSysVector.cpp      |  2 +-
 Common/src/linear_algebra/blas_structure.cpp  |  2 +-
 Common/src/toolboxes/C1DInterpolation.cpp     |  2 +-
 Common/src/toolboxes/CLinearPartitioner.cpp   |  2 +-
 Common/src/toolboxes/CSquareMatrixCM.cpp      |  2 +-
 Common/src/toolboxes/CSymmetricMatrix.cpp     |  2 +-
 Common/src/toolboxes/MMS/CIncTGVSolution.cpp  |  2 +-
 .../toolboxes/MMS/CInviscidVortexSolution.cpp |  2 +-
 .../toolboxes/MMS/CMMSIncEulerSolution.cpp    |  2 +-
 .../src/toolboxes/MMS/CMMSIncNSSolution.cpp   |  2 +-
 .../MMS/CMMSNSTwoHalfCirclesSolution.cpp      |  2 +-
 .../MMS/CMMSNSTwoHalfSpheresSolution.cpp      |  2 +-
 .../toolboxes/MMS/CMMSNSUnitQuadSolution.cpp  |  2 +-
 .../MMS/CMMSNSUnitQuadSolutionWallBC.cpp      |  2 +-
 .../src/toolboxes/MMS/CNSUnitQuadSolution.cpp |  2 +-
 Common/src/toolboxes/MMS/CRinglebSolution.cpp |  2 +-
 Common/src/toolboxes/MMS/CTGVSolution.cpp     |  2 +-
 .../toolboxes/MMS/CUserDefinedSolution.cpp    |  2 +-
 .../toolboxes/MMS/CVerificationSolution.cpp   |  2 +-
 .../CMMSIncEulerSolution.py                   |  2 +-
 .../CreateMMSSourceTerms/CMMSIncNSSolution.py |  2 +-
 Common/src/toolboxes/printing_toolbox.cpp     |  2 +-
 Common/src/wall_model.cpp                     |  2 +-
 Docs/docmain.hpp                              |  4 ++--
 QuickStart/inv_NACA0012.cfg                   |  2 +-
 README.md                                     |  2 +-
 SU2_CFD/include/CMarkerProfileReaderFVM.hpp   |  2 +-
 SU2_CFD/include/SU2_CFD.hpp                   |  2 +-
 SU2_CFD/include/definition_structure.hpp      |  2 +-
 .../drivers/CDiscAdjMultizoneDriver.hpp       |  2 +-
 .../drivers/CDiscAdjSinglezoneDriver.hpp      |  4 ++--
 SU2_CFD/include/drivers/CDriver.hpp           |  2 +-
 SU2_CFD/include/drivers/CDriverBase.hpp       |  2 +-
 SU2_CFD/include/drivers/CDummyDriver.hpp      |  2 +-
 SU2_CFD/include/drivers/CMultizoneDriver.hpp  |  4 ++--
 SU2_CFD/include/drivers/CSinglezoneDriver.hpp |  4 ++--
 SU2_CFD/include/fluid/CConductivityModel.hpp  |  2 +-
 .../include/fluid/CConstantConductivity.hpp   |  2 +-
 .../fluid/CConstantConductivityRANS.hpp       |  2 +-
 SU2_CFD/include/fluid/CConstantDensity.hpp    |  2 +-
 .../include/fluid/CConstantDiffusivity.hpp    |  2 +-
 .../fluid/CConstantLewisDiffusivity.hpp       |  2 +-
 SU2_CFD/include/fluid/CConstantPrandtl.hpp    |  2 +-
 .../include/fluid/CConstantPrandtlRANS.hpp    |  2 +-
 SU2_CFD/include/fluid/CConstantSchmidt.hpp    |  2 +-
 SU2_CFD/include/fluid/CConstantViscosity.hpp  |  2 +-
 SU2_CFD/include/fluid/CCoolProp.hpp           |  2 +-
 .../include/fluid/CCoolPropConductivity.hpp   |  2 +-
 SU2_CFD/include/fluid/CCoolPropViscosity.hpp  |  2 +-
 SU2_CFD/include/fluid/CDataDrivenFluid.hpp    |  2 +-
 SU2_CFD/include/fluid/CDiffusivityModel.hpp   |  2 +-
 SU2_CFD/include/fluid/CFluidFlamelet.hpp      |  2 +-
 SU2_CFD/include/fluid/CFluidModel.hpp         |  2 +-
 SU2_CFD/include/fluid/CFluidScalar.hpp        |  2 +-
 SU2_CFD/include/fluid/CIdealGas.hpp           |  2 +-
 SU2_CFD/include/fluid/CIncIdealGas.hpp        |  2 +-
 .../include/fluid/CIncIdealGasPolynomial.hpp  |  2 +-
 SU2_CFD/include/fluid/CMutationTCLib.hpp      |  2 +-
 SU2_CFD/include/fluid/CNEMOGas.hpp            |  2 +-
 SU2_CFD/include/fluid/CPengRobinson.hpp       |  2 +-
 .../include/fluid/CPolynomialConductivity.hpp |  2 +-
 .../fluid/CPolynomialConductivityRANS.hpp     |  2 +-
 .../include/fluid/CPolynomialViscosity.hpp    |  2 +-
 SU2_CFD/include/fluid/CSU2TCLib.hpp           |  2 +-
 SU2_CFD/include/fluid/CSutherland.hpp         |  2 +-
 SU2_CFD/include/fluid/CVanDerWaalsGas.hpp     |  2 +-
 SU2_CFD/include/fluid/CViscosityModel.hpp     |  2 +-
 .../gradients/computeGradientsGreenGauss.hpp  |  2 +-
 .../computeGradientsLeastSquares.hpp          |  2 +-
 .../integration/CFEM_DG_Integration.hpp       |  4 ++--
 SU2_CFD/include/integration/CIntegration.hpp  |  2 +-
 .../integration/CIntegrationFactory.hpp       |  2 +-
 .../integration/CMultiGridIntegration.hpp     |  2 +-
 .../integration/CNewtonIntegration.hpp        |  2 +-
 .../integration/CSingleGridIntegration.hpp    |  2 +-
 .../integration/CStructuralIntegration.hpp    |  2 +-
 SU2_CFD/include/interfaces/CInterface.hpp     |  4 ++--
 .../cfd/CConservativeVarsInterface.hpp        |  2 +-
 .../interfaces/cfd/CMixingPlaneInterface.hpp  |  2 +-
 .../interfaces/cfd/CSlidingInterface.hpp      |  2 +-
 .../cht/CConjugateHeatInterface.hpp           |  2 +-
 .../fsi/CDiscAdjFlowTractionInterface.hpp     |  2 +-
 .../fsi/CDisplacementsInterface.hpp           |  2 +-
 .../interfaces/fsi/CFlowTractionInterface.hpp |  2 +-
 .../include/iteration/CAdjFluidIteration.hpp  |  2 +-
 .../iteration/CDiscAdjFEAIteration.hpp        |  2 +-
 .../iteration/CDiscAdjFluidIteration.hpp      |  2 +-
 .../iteration/CDiscAdjHeatIteration.hpp       |  2 +-
 SU2_CFD/include/iteration/CFEAIteration.hpp   |  4 ++--
 .../include/iteration/CFEMFluidIteration.hpp  |  4 ++--
 SU2_CFD/include/iteration/CFluidIteration.hpp |  2 +-
 SU2_CFD/include/iteration/CHeatIteration.hpp  |  2 +-
 SU2_CFD/include/iteration/CIteration.hpp      |  2 +-
 .../include/iteration/CIterationFactory.hpp   |  2 +-
 SU2_CFD/include/iteration/CTurboIteration.hpp |  2 +-
 SU2_CFD/include/limiters/CLimiterDetails.hpp  |  2 +-
 SU2_CFD/include/limiters/computeLimiters.hpp  |  2 +-
 .../include/limiters/computeLimiters_impl.hpp |  2 +-
 SU2_CFD/include/numerics/CGradSmoothing.hpp   |  2 +-
 SU2_CFD/include/numerics/CNumerics.hpp        |  2 +-
 .../include/numerics/NEMO/CNEMONumerics.hpp   |  2 +-
 .../include/numerics/NEMO/NEMO_diffusion.hpp  |  6 ++---
 .../include/numerics/NEMO/NEMO_sources.hpp    |  4 ++--
 .../numerics/NEMO/convection/ausm_slau.hpp    |  2 +-
 .../include/numerics/NEMO/convection/lax.hpp  |  2 +-
 .../include/numerics/NEMO/convection/msw.hpp  |  4 ++--
 .../include/numerics/NEMO/convection/roe.hpp  |  4 ++--
 .../continuous_adjoint/adj_convection.hpp     |  2 +-
 .../continuous_adjoint/adj_diffusion.hpp      |  2 +-
 .../continuous_adjoint/adj_sources.hpp        |  2 +-
 .../numerics/elasticity/CFEAElasticity.hpp    |  4 ++--
 .../elasticity/CFEALinearElasticity.hpp       |  6 ++---
 .../elasticity/CFEANonlinearElasticity.hpp    |  4 ++--
 .../numerics/elasticity/nonlinear_models.hpp  | 10 ++++----
 .../numerics/flow/convection/ausm_slau.hpp    |  2 +-
 .../numerics/flow/convection/centered.hpp     |  2 +-
 .../include/numerics/flow/convection/fds.hpp  |  2 +-
 .../include/numerics/flow/convection/fvs.hpp  |  2 +-
 .../include/numerics/flow/convection/hllc.hpp |  6 ++---
 .../include/numerics/flow/convection/roe.hpp  |  6 ++---
 .../include/numerics/flow/flow_diffusion.hpp  |  2 +-
 .../include/numerics/flow/flow_sources.hpp    |  6 ++---
 SU2_CFD/include/numerics/heat.hpp             |  6 ++---
 SU2_CFD/include/numerics/radiation.hpp        |  2 +-
 .../numerics/scalar/scalar_convection.hpp     |  2 +-
 .../numerics/scalar/scalar_diffusion.hpp      |  2 +-
 .../numerics/scalar/scalar_sources.hpp        |  2 +-
 .../numerics/species/species_convection.hpp   |  2 +-
 .../numerics/species/species_diffusion.hpp    |  2 +-
 .../numerics/species/species_sources.hpp      |  2 +-
 SU2_CFD/include/numerics/template.hpp         |  2 +-
 .../turbulent/transition/trans_convection.hpp |  2 +-
 .../transition/trans_correlations.hpp         |  2 +-
 .../turbulent/transition/trans_diffusion.hpp  |  2 +-
 .../turbulent/transition/trans_sources.hpp    |  2 +-
 .../numerics/turbulent/turb_convection.hpp    |  2 +-
 .../numerics/turbulent/turb_diffusion.hpp     |  2 +-
 .../numerics/turbulent/turb_sources.hpp       |  2 +-
 .../include/numerics_simd/CNumericsSIMD.cpp   |  2 +-
 .../include/numerics_simd/CNumericsSIMD.hpp   |  2 +-
 .../flow/convection/centered.hpp              |  2 +-
 .../numerics_simd/flow/convection/common.hpp  |  2 +-
 .../numerics_simd/flow/convection/roe.hpp     |  2 +-
 .../numerics_simd/flow/diffusion/common.hpp   |  2 +-
 .../flow/diffusion/viscous_fluxes.hpp         |  2 +-
 .../include/numerics_simd/flow/variables.hpp  |  2 +-
 SU2_CFD/include/numerics_simd/util.hpp        |  2 +-
 .../include/output/CAdjElasticityOutput.hpp   |  2 +-
 SU2_CFD/include/output/CAdjFlowCompOutput.hpp |  2 +-
 SU2_CFD/include/output/CAdjFlowIncOutput.hpp  |  2 +-
 SU2_CFD/include/output/CAdjFlowOutput.hpp     |  2 +-
 SU2_CFD/include/output/CAdjHeatOutput.hpp     |  2 +-
 SU2_CFD/include/output/CBaselineOutput.hpp    |  2 +-
 SU2_CFD/include/output/CElasticityOutput.hpp  |  2 +-
 SU2_CFD/include/output/CFVMOutput.hpp         |  2 +-
 SU2_CFD/include/output/CFlowCompFEMOutput.hpp |  2 +-
 SU2_CFD/include/output/CFlowCompOutput.hpp    |  2 +-
 SU2_CFD/include/output/CFlowIncOutput.hpp     |  2 +-
 SU2_CFD/include/output/CFlowOutput.hpp        |  2 +-
 SU2_CFD/include/output/CHeatOutput.hpp        |  2 +-
 SU2_CFD/include/output/CMeshOutput.hpp        |  2 +-
 SU2_CFD/include/output/CMultizoneOutput.hpp   |  2 +-
 SU2_CFD/include/output/CNEMOCompOutput.hpp    |  2 +-
 SU2_CFD/include/output/COutput.hpp            |  2 +-
 SU2_CFD/include/output/COutputFactory.hpp     |  2 +-
 .../output/filewriter/CCGNSFileWriter.hpp     |  2 +-
 .../output/filewriter/CCSVFileWriter.hpp      |  2 +-
 .../output/filewriter/CFEMDataSorter.hpp      |  2 +-
 .../output/filewriter/CFVMDataSorter.hpp      |  2 +-
 .../include/output/filewriter/CFileWriter.hpp |  2 +-
 .../output/filewriter/CParallelDataSorter.hpp |  2 +-
 .../filewriter/CParaviewBinaryFileWriter.hpp  |  2 +-
 .../output/filewriter/CParaviewFileWriter.hpp |  2 +-
 .../filewriter/CParaviewVTMFileWriter.hpp     |  2 +-
 .../filewriter/CParaviewXMLFileWriter.hpp     |  2 +-
 .../output/filewriter/CSTLFileWriter.hpp      |  4 ++--
 .../filewriter/CSU2BinaryFileWriter.hpp       |  2 +-
 .../output/filewriter/CSU2FileWriter.hpp      |  2 +-
 .../output/filewriter/CSU2MeshFileWriter.hpp  |  2 +-
 .../filewriter/CSurfaceFEMDataSorter.hpp      |  2 +-
 .../filewriter/CSurfaceFVMDataSorter.hpp      |  2 +-
 .../filewriter/CTecplotBinaryFileWriter.hpp   |  2 +-
 .../output/filewriter/CTecplotFileWriter.hpp  |  2 +-
 .../include/output/tools/CWindowingTools.hpp  |  2 +-
 SU2_CFD/include/sgs_model.hpp                 | 10 ++++----
 SU2_CFD/include/sgs_model.inl                 |  2 +-
 SU2_CFD/include/solvers/CAdjEulerSolver.hpp   |  2 +-
 SU2_CFD/include/solvers/CAdjNSSolver.hpp      |  2 +-
 SU2_CFD/include/solvers/CAdjTurbSolver.hpp    |  2 +-
 SU2_CFD/include/solvers/CBaselineSolver.hpp   |  2 +-
 .../include/solvers/CBaselineSolver_FEM.hpp   |  4 ++--
 SU2_CFD/include/solvers/CDiscAdjFEASolver.hpp |  2 +-
 .../include/solvers/CDiscAdjMeshSolver.hpp    |  2 +-
 SU2_CFD/include/solvers/CDiscAdjSolver.hpp    |  2 +-
 SU2_CFD/include/solvers/CEulerSolver.hpp      |  2 +-
 SU2_CFD/include/solvers/CFEASolver.hpp        |  2 +-
 SU2_CFD/include/solvers/CFEASolverBase.hpp    |  2 +-
 .../include/solvers/CFEM_DG_EulerSolver.hpp   |  4 ++--
 SU2_CFD/include/solvers/CFEM_DG_NSSolver.hpp  |  4 ++--
 .../include/solvers/CFVMFlowSolverBase.hpp    |  2 +-
 .../include/solvers/CFVMFlowSolverBase.inl    |  2 +-
 .../solvers/CGradientSmoothingSolver.hpp      |  2 +-
 SU2_CFD/include/solvers/CHeatSolver.hpp       |  4 ++--
 SU2_CFD/include/solvers/CIncEulerSolver.hpp   |  2 +-
 SU2_CFD/include/solvers/CIncNSSolver.hpp      |  2 +-
 SU2_CFD/include/solvers/CMeshSolver.hpp       |  2 +-
 SU2_CFD/include/solvers/CNEMOEulerSolver.hpp  |  4 ++--
 SU2_CFD/include/solvers/CNEMONSSolver.hpp     |  2 +-
 SU2_CFD/include/solvers/CNSSolver.hpp         |  2 +-
 SU2_CFD/include/solvers/CRadP1Solver.hpp      |  2 +-
 SU2_CFD/include/solvers/CRadSolver.hpp        |  2 +-
 SU2_CFD/include/solvers/CScalarSolver.hpp     |  2 +-
 SU2_CFD/include/solvers/CScalarSolver.inl     |  2 +-
 SU2_CFD/include/solvers/CSolver.hpp           |  2 +-
 SU2_CFD/include/solvers/CSolverFactory.hpp    |  2 +-
 .../solvers/CSpeciesFlameletSolver.hpp        |  2 +-
 SU2_CFD/include/solvers/CSpeciesSolver.hpp    |  2 +-
 SU2_CFD/include/solvers/CTemplateSolver.hpp   |  2 +-
 SU2_CFD/include/solvers/CTransLMSolver.hpp    |  2 +-
 SU2_CFD/include/solvers/CTurbSASolver.hpp     |  2 +-
 SU2_CFD/include/solvers/CTurbSSTSolver.hpp    |  2 +-
 SU2_CFD/include/solvers/CTurbSolver.hpp       |  2 +-
 SU2_CFD/include/task_definition.hpp           |  4 ++--
 SU2_CFD/include/task_definition.inl           |  2 +-
 .../include/variables/CAdjEulerVariable.hpp   |  2 +-
 SU2_CFD/include/variables/CAdjNSVariable.hpp  |  2 +-
 .../include/variables/CAdjTurbVariable.hpp    |  2 +-
 .../include/variables/CBaselineVariable.hpp   |  2 +-
 .../variables/CDiscAdjFEABoundVariable.hpp    |  4 ++--
 .../variables/CDiscAdjMeshBoundVariable.hpp   |  2 +-
 .../include/variables/CDiscAdjVariable.hpp    |  2 +-
 SU2_CFD/include/variables/CEulerVariable.hpp  |  2 +-
 .../include/variables/CFEABoundVariable.hpp   |  4 ++--
 SU2_CFD/include/variables/CFEAVariable.hpp    |  4 ++--
 SU2_CFD/include/variables/CFlowVariable.hpp   |  2 +-
 SU2_CFD/include/variables/CHeatVariable.hpp   |  4 ++--
 .../include/variables/CIncEulerVariable.hpp   |  2 +-
 SU2_CFD/include/variables/CIncNSVariable.hpp  |  2 +-
 .../include/variables/CMeshBoundVariable.hpp  |  2 +-
 SU2_CFD/include/variables/CMeshElement.hpp    |  2 +-
 SU2_CFD/include/variables/CMeshVariable.hpp   |  2 +-
 .../include/variables/CNEMOEulerVariable.hpp  |  2 +-
 SU2_CFD/include/variables/CNEMONSVariable.hpp |  2 +-
 SU2_CFD/include/variables/CNSVariable.hpp     |  2 +-
 .../include/variables/CPrimitiveIndices.hpp   |  2 +-
 SU2_CFD/include/variables/CRadP1Variable.hpp  |  2 +-
 SU2_CFD/include/variables/CRadVariable.hpp    |  2 +-
 SU2_CFD/include/variables/CScalarVariable.hpp |  2 +-
 .../variables/CSobolevSmoothingVariable.hpp   |  2 +-
 .../variables/CSpeciesFlameletVariable.hpp    |  2 +-
 .../include/variables/CSpeciesVariable.hpp    |  2 +-
 .../include/variables/CTransLMVariable.hpp    |  2 +-
 SU2_CFD/include/variables/CTurbSAVariable.hpp |  2 +-
 .../include/variables/CTurbSSTVariable.hpp    |  2 +-
 SU2_CFD/include/variables/CTurbVariable.hpp   |  2 +-
 SU2_CFD/include/variables/CVariable.hpp       |  2 +-
 SU2_CFD/src/CMarkerProfileReaderFVM.cpp       |  2 +-
 SU2_CFD/src/SU2_CFD.cpp                       |  4 ++--
 SU2_CFD/src/definition_structure.cpp          |  2 +-
 .../src/drivers/CDiscAdjMultizoneDriver.cpp   |  2 +-
 .../src/drivers/CDiscAdjSinglezoneDriver.cpp  |  2 +-
 SU2_CFD/src/drivers/CDriver.cpp               |  2 +-
 SU2_CFD/src/drivers/CDriverBase.cpp           |  2 +-
 SU2_CFD/src/drivers/CDummyDriver.cpp          |  2 +-
 SU2_CFD/src/drivers/CMultizoneDriver.cpp      |  2 +-
 SU2_CFD/src/drivers/CSinglezoneDriver.cpp     |  2 +-
 SU2_CFD/src/fluid/CCoolProp.cpp               |  2 +-
 SU2_CFD/src/fluid/CDataDrivenFluid.cpp        |  2 +-
 SU2_CFD/src/fluid/CFluidFlamelet.cpp          |  2 +-
 SU2_CFD/src/fluid/CFluidModel.cpp             |  2 +-
 SU2_CFD/src/fluid/CFluidScalar.cpp            |  2 +-
 SU2_CFD/src/fluid/CIdealGas.cpp               |  2 +-
 SU2_CFD/src/fluid/CMutationTCLib.cpp          |  2 +-
 SU2_CFD/src/fluid/CNEMOGas.cpp                |  2 +-
 SU2_CFD/src/fluid/CPengRobinson.cpp           |  2 +-
 SU2_CFD/src/fluid/CSU2TCLib.cpp               |  2 +-
 SU2_CFD/src/fluid/CVanDerWaalsGas.cpp         |  2 +-
 .../src/integration/CFEM_DG_Integration.cpp   |  2 +-
 SU2_CFD/src/integration/CIntegration.cpp      |  2 +-
 .../src/integration/CIntegrationFactory.cpp   |  2 +-
 .../src/integration/CMultiGridIntegration.cpp |  2 +-
 .../src/integration/CNewtonIntegration.cpp    |  2 +-
 .../integration/CSingleGridIntegration.cpp    |  2 +-
 .../integration/CStructuralIntegration.cpp    |  2 +-
 SU2_CFD/src/interfaces/CInterface.cpp         |  2 +-
 .../cfd/CConservativeVarsInterface.cpp        |  2 +-
 .../interfaces/cfd/CMixingPlaneInterface.cpp  |  2 +-
 .../src/interfaces/cfd/CSlidingInterface.cpp  |  2 +-
 .../cht/CConjugateHeatInterface.cpp           |  2 +-
 .../fsi/CDiscAdjFlowTractionInterface.cpp     |  2 +-
 .../fsi/CDisplacementsInterface.cpp           |  2 +-
 .../interfaces/fsi/CFlowTractionInterface.cpp |  2 +-
 SU2_CFD/src/iteration/CAdjFluidIteration.cpp  |  2 +-
 .../src/iteration/CDiscAdjFEAIteration.cpp    |  2 +-
 .../src/iteration/CDiscAdjFluidIteration.cpp  |  2 +-
 .../src/iteration/CDiscAdjHeatIteration.cpp   |  2 +-
 SU2_CFD/src/iteration/CFEAIteration.cpp       |  2 +-
 SU2_CFD/src/iteration/CFEMFluidIteration.cpp  |  2 +-
 SU2_CFD/src/iteration/CFluidIteration.cpp     |  2 +-
 SU2_CFD/src/iteration/CHeatIteration.cpp      |  2 +-
 SU2_CFD/src/iteration/CIteration.cpp          |  2 +-
 SU2_CFD/src/iteration/CIterationFactory.cpp   |  2 +-
 SU2_CFD/src/iteration/CTurboIteration.cpp     |  2 +-
 SU2_CFD/src/limiters/CLimiterDetails.cpp      |  2 +-
 SU2_CFD/src/numerics/CGradSmoothing.cpp       |  2 +-
 SU2_CFD/src/numerics/CNumerics.cpp            |  2 +-
 SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp   |  2 +-
 SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp  |  2 +-
 SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp    |  2 +-
 .../numerics/NEMO/convection/ausm_slau.cpp    |  2 +-
 SU2_CFD/src/numerics/NEMO/convection/lax.cpp  |  2 +-
 SU2_CFD/src/numerics/NEMO/convection/msw.cpp  |  2 +-
 SU2_CFD/src/numerics/NEMO/convection/roe.cpp  |  2 +-
 .../continuous_adjoint/adj_convection.cpp     |  2 +-
 .../continuous_adjoint/adj_diffusion.cpp      |  2 +-
 .../continuous_adjoint/adj_sources.cpp        |  2 +-
 .../numerics/elasticity/CFEAElasticity.cpp    |  2 +-
 .../elasticity/CFEALinearElasticity.cpp       |  2 +-
 .../elasticity/CFEANonlinearElasticity.cpp    |  2 +-
 .../numerics/elasticity/nonlinear_models.cpp  |  2 +-
 .../numerics/flow/convection/ausm_slau.cpp    |  2 +-
 .../src/numerics/flow/convection/centered.cpp |  2 +-
 SU2_CFD/src/numerics/flow/convection/fds.cpp  |  2 +-
 SU2_CFD/src/numerics/flow/convection/fvs.cpp  |  2 +-
 SU2_CFD/src/numerics/flow/convection/hllc.cpp |  2 +-
 SU2_CFD/src/numerics/flow/convection/roe.cpp  |  2 +-
 SU2_CFD/src/numerics/flow/flow_diffusion.cpp  |  2 +-
 SU2_CFD/src/numerics/flow/flow_sources.cpp    |  2 +-
 SU2_CFD/src/numerics/radiation.cpp            |  2 +-
 .../src/numerics/scalar/scalar_sources.cpp    |  2 +-
 .../src/numerics/species/species_sources.cpp  |  2 +-
 SU2_CFD/src/numerics/template.cpp             |  2 +-
 SU2_CFD/src/output/CAdjElasticityOutput.cpp   |  2 +-
 SU2_CFD/src/output/CAdjFlowCompOutput.cpp     |  2 +-
 SU2_CFD/src/output/CAdjFlowIncOutput.cpp      |  2 +-
 SU2_CFD/src/output/CAdjFlowOutput.cpp         |  2 +-
 SU2_CFD/src/output/CAdjHeatOutput.cpp         |  2 +-
 SU2_CFD/src/output/CBaselineOutput.cpp        |  2 +-
 SU2_CFD/src/output/CElasticityOutput.cpp      |  2 +-
 SU2_CFD/src/output/CFVMOutput.cpp             |  2 +-
 SU2_CFD/src/output/CFlowCompFEMOutput.cpp     |  2 +-
 SU2_CFD/src/output/CFlowCompOutput.cpp        |  2 +-
 SU2_CFD/src/output/CFlowIncOutput.cpp         |  2 +-
 SU2_CFD/src/output/CFlowOutput.cpp            |  4 ++--
 SU2_CFD/src/output/CHeatOutput.cpp            |  2 +-
 SU2_CFD/src/output/CMeshOutput.cpp            |  2 +-
 SU2_CFD/src/output/CMultizoneOutput.cpp       |  2 +-
 SU2_CFD/src/output/CNEMOCompOutput.cpp        |  2 +-
 SU2_CFD/src/output/COutput.cpp                |  2 +-
 SU2_CFD/src/output/COutputFactory.cpp         |  2 +-
 .../src/output/filewriter/CCGNSFileWriter.cpp |  2 +-
 .../src/output/filewriter/CCSVFileWriter.cpp  |  2 +-
 .../src/output/filewriter/CFEMDataSorter.cpp  |  2 +-
 .../src/output/filewriter/CFVMDataSorter.cpp  |  2 +-
 .../output/filewriter/CParallelDataSorter.cpp |  2 +-
 .../output/filewriter/CParallelFileWriter.cpp |  2 +-
 .../filewriter/CParaviewBinaryFileWriter.cpp  |  2 +-
 .../output/filewriter/CParaviewFileWriter.cpp |  2 +-
 .../filewriter/CParaviewVTMFileWriter.cpp     |  2 +-
 .../filewriter/CParaviewXMLFileWriter.cpp     |  2 +-
 .../src/output/filewriter/CSTLFileWriter.cpp  |  2 +-
 .../filewriter/CSU2BinaryFileWriter.cpp       |  2 +-
 .../src/output/filewriter/CSU2FileWriter.cpp  |  2 +-
 .../output/filewriter/CSU2MeshFileWriter.cpp  |  2 +-
 .../filewriter/CSurfaceFEMDataSorter.cpp      |  2 +-
 .../filewriter/CSurfaceFVMDataSorter.cpp      |  2 +-
 .../filewriter/CTecplotBinaryFileWriter.cpp   |  2 +-
 .../output/filewriter/CTecplotFileWriter.cpp  |  2 +-
 SU2_CFD/src/output/tools/CWindowingTools.cpp  |  2 +-
 SU2_CFD/src/python_wrapper_structure.cpp      |  2 +-
 SU2_CFD/src/solvers/CAdjEulerSolver.cpp       |  2 +-
 SU2_CFD/src/solvers/CAdjNSSolver.cpp          |  2 +-
 SU2_CFD/src/solvers/CAdjTurbSolver.cpp        |  2 +-
 SU2_CFD/src/solvers/CBaselineSolver.cpp       |  2 +-
 SU2_CFD/src/solvers/CBaselineSolver_FEM.cpp   |  2 +-
 SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp     |  2 +-
 SU2_CFD/src/solvers/CDiscAdjMeshSolver.cpp    |  2 +-
 SU2_CFD/src/solvers/CDiscAdjSolver.cpp        |  2 +-
 SU2_CFD/src/solvers/CEulerSolver.cpp          |  2 +-
 SU2_CFD/src/solvers/CFEASolver.cpp            |  2 +-
 SU2_CFD/src/solvers/CFEASolverBase.cpp        |  2 +-
 SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp   |  2 +-
 SU2_CFD/src/solvers/CFEM_DG_NSSolver.cpp      |  2 +-
 .../src/solvers/CGradientSmoothingSolver.cpp  |  2 +-
 SU2_CFD/src/solvers/CHeatSolver.cpp           |  2 +-
 SU2_CFD/src/solvers/CIncEulerSolver.cpp       |  2 +-
 SU2_CFD/src/solvers/CIncNSSolver.cpp          |  2 +-
 SU2_CFD/src/solvers/CMeshSolver.cpp           |  2 +-
 SU2_CFD/src/solvers/CNEMOEulerSolver.cpp      |  2 +-
 SU2_CFD/src/solvers/CNEMONSSolver.cpp         |  2 +-
 SU2_CFD/src/solvers/CNSSolver.cpp             |  2 +-
 SU2_CFD/src/solvers/CRadP1Solver.cpp          |  2 +-
 SU2_CFD/src/solvers/CRadSolver.cpp            |  2 +-
 SU2_CFD/src/solvers/CSolver.cpp               |  2 +-
 SU2_CFD/src/solvers/CSolverFactory.cpp        |  2 +-
 .../src/solvers/CSpeciesFlameletSolver.cpp    |  2 +-
 SU2_CFD/src/solvers/CSpeciesSolver.cpp        |  2 +-
 SU2_CFD/src/solvers/CTemplateSolver.cpp       |  2 +-
 SU2_CFD/src/solvers/CTransLMSolver.cpp        |  2 +-
 SU2_CFD/src/solvers/CTurbSASolver.cpp         |  2 +-
 SU2_CFD/src/solvers/CTurbSSTSolver.cpp        |  2 +-
 SU2_CFD/src/solvers/CTurbSolver.cpp           |  2 +-
 SU2_CFD/src/variables/CAdjEulerVariable.cpp   |  2 +-
 SU2_CFD/src/variables/CAdjNSVariable.cpp      |  2 +-
 SU2_CFD/src/variables/CAdjTurbVariable.cpp    |  2 +-
 SU2_CFD/src/variables/CBaselineVariable.cpp   |  2 +-
 .../variables/CDiscAdjFEABoundVariable.cpp    |  2 +-
 .../variables/CDiscAdjMeshBoundVariable.cpp   |  2 +-
 SU2_CFD/src/variables/CDiscAdjVariable.cpp    |  2 +-
 SU2_CFD/src/variables/CEulerVariable.cpp      |  2 +-
 SU2_CFD/src/variables/CFEABoundVariable.cpp   |  2 +-
 SU2_CFD/src/variables/CFEAVariable.cpp        |  2 +-
 SU2_CFD/src/variables/CFlowVariable.cpp       |  2 +-
 SU2_CFD/src/variables/CHeatVariable.cpp       |  2 +-
 SU2_CFD/src/variables/CIncEulerVariable.cpp   |  2 +-
 SU2_CFD/src/variables/CIncNSVariable.cpp      |  2 +-
 SU2_CFD/src/variables/CMeshBoundVariable.cpp  |  2 +-
 SU2_CFD/src/variables/CMeshElement.cpp        |  2 +-
 SU2_CFD/src/variables/CMeshVariable.cpp       |  2 +-
 SU2_CFD/src/variables/CNEMOEulerVariable.cpp  |  2 +-
 SU2_CFD/src/variables/CNEMONSVariable.cpp     |  2 +-
 SU2_CFD/src/variables/CNSVariable.cpp         |  2 +-
 SU2_CFD/src/variables/CRadP1Variable.cpp      |  2 +-
 SU2_CFD/src/variables/CRadVariable.cpp        |  2 +-
 SU2_CFD/src/variables/CScalarVariable.cpp     |  2 +-
 .../variables/CSobolevSmoothingVariable.cpp   |  2 +-
 .../variables/CSpeciesFlameletVariable.cpp    |  2 +-
 SU2_CFD/src/variables/CSpeciesVariable.cpp    |  2 +-
 SU2_CFD/src/variables/CTransLMVariable.cpp    |  2 +-
 SU2_CFD/src/variables/CTurbSAVariable.cpp     |  2 +-
 SU2_CFD/src/variables/CTurbSSTVariable.cpp    |  2 +-
 SU2_CFD/src/variables/CTurbVariable.cpp       |  2 +-
 SU2_CFD/src/variables/CVariable.cpp           |  2 +-
 .../include/drivers/CDeformationDriver.hpp    |  2 +-
 .../drivers/CDiscAdjDeformationDriver.hpp     |  2 +-
 SU2_DEF/src/SU2_DEF.cpp                       |  2 +-
 SU2_DEF/src/drivers/CDeformationDriver.cpp    |  2 +-
 .../src/drivers/CDiscAdjDeformationDriver.cpp |  2 +-
 SU2_DOT/src/SU2_DOT.cpp                       |  2 +-
 SU2_GEO/include/SU2_GEO.hpp                   |  2 +-
 SU2_GEO/src/SU2_GEO.cpp                       |  2 +-
 SU2_PY/FSI_tools/FSIInterface.py              |  2 +-
 SU2_PY/FSI_tools/FSI_config.py                |  2 +-
 SU2_PY/OptimalPropeller.py                    |  2 +-
 SU2_PY/SU2/eval/design.py                     |  2 +-
 SU2_PY/SU2/eval/functions.py                  |  2 +-
 SU2_PY/SU2/eval/gradients.py                  |  2 +-
 SU2_PY/SU2/io/config.py                       |  2 +-
 SU2_PY/SU2/io/config_options.py               |  2 +-
 SU2_PY/SU2/io/data.py                         |  2 +-
 SU2_PY/SU2/io/filelock.py                     |  2 +-
 SU2_PY/SU2/io/redirect.py                     |  2 +-
 SU2_PY/SU2/io/state.py                        |  2 +-
 SU2_PY/SU2/io/tools.py                        |  2 +-
 SU2_PY/SU2/opt/project.py                     |  2 +-
 SU2_PY/SU2/opt/scipy_tools.py                 |  2 +-
 SU2_PY/SU2/run/adjoint.py                     |  2 +-
 SU2_PY/SU2/run/deform.py                      |  2 +-
 SU2_PY/SU2/run/direct.py                      |  2 +-
 SU2_PY/SU2/run/geometry.py                    |  2 +-
 SU2_PY/SU2/run/interface.py                   |  2 +-
 SU2_PY/SU2/run/merge.py                       |  2 +-
 SU2_PY/SU2/run/projection.py                  |  2 +-
 SU2_PY/SU2/util/filter_adjoint.py             |  2 +-
 SU2_PY/SU2/util/plot.py                       |  2 +-
 SU2_PY/SU2/util/polarSweepLib.py              |  2 +-
 SU2_PY/SU2/util/which.py                      |  2 +-
 SU2_PY/SU2_CFD.py                             |  2 +-
 SU2_PY/SU2_Nastran/pysu2_nastran.py           |  2 +-
 SU2_PY/change_version_number.py               |  6 ++---
 SU2_PY/compute_polar.py                       |  2 +-
 SU2_PY/compute_uncertainty.py                 |  2 +-
 SU2_PY/continuous_adjoint.py                  |  2 +-
 SU2_PY/direct_differentiation.py              |  2 +-
 SU2_PY/discrete_adjoint.py                    |  2 +-
 SU2_PY/finite_differences.py                  |  2 +-
 SU2_PY/fsi_computation.py                     |  2 +-
 SU2_PY/merge_solution.py                      |  2 +-
 SU2_PY/mesh_deformation.py                    |  2 +-
 SU2_PY/parallel_computation.py                |  2 +-
 SU2_PY/parallel_computation_fsi.py            |  2 +-
 SU2_PY/parse_config.py                        |  2 +-
 SU2_PY/profiling.py                           |  2 +-
 SU2_PY/pySU2/pySU2.i                          |  2 +-
 SU2_PY/pySU2/pySU2ad.i                        |  2 +-
 SU2_PY/set_ffd_design_var.py                  |  2 +-
 SU2_PY/shape_optimization.py                  |  4 ++--
 SU2_PY/topology_optimization.py               |  2 +-
 SU2_PY/updateHistoryMap.py                    |  2 +-
 SU2_SOL/include/SU2_SOL.hpp                   |  2 +-
 SU2_SOL/src/SU2_SOL.cpp                       |  2 +-
 TestCases/TestCase.py                         |  2 +-
 .../aeroelastic/aeroelastic_NACA64A010.cfg    |  2 +-
 .../air_nozzle/air_nozzle_restart.cfg         |  2 +-
 .../cont_adj_euler/naca0012/inv_NACA0012.cfg  |  2 +-
 .../naca0012/inv_NACA0012_FD.cfg              |  2 +-
 .../naca0012/inv_NACA0012_discadj.cfg         |  2 +-
 .../cont_adj_euler/oneram6/inv_ONERAM6.cfg    |  2 +-
 .../cont_adj_euler/wedge/inv_wedge_ROE.cfg    |  2 +-
 .../wedge/inv_wedge_ROE_multiobj.cfg          |  2 +-
 .../cylinder/lam_cylinder.cfg                 |  2 +-
 .../naca0012_sub/lam_NACA0012.cfg             |  2 +-
 .../naca0012_trans/lam_NACA0012.cfg           |  2 +-
 .../cont_adj_rans/naca0012/turb_nasa.cfg      |  2 +-
 .../naca0012/turb_nasa_binary.cfg             |  2 +-
 .../cont_adj_rans/oneram6/turb_ONERAM6.cfg    |  2 +-
 .../cont_adj_rans/rae2822/turb_SA_RAE2822.cfg |  2 +-
 .../control_surface/inv_ONERAM6_moving.cfg    |  2 +-
 .../control_surface/inv_ONERAM6_setting.cfg   |  2 +-
 .../coupled_cht/comp_2d/cht_2d_3cylinders.cfg |  2 +-
 .../disc_adj_incomp_2d/cht_2d_3cylinders.cfg  |  2 +-
 .../incomp_2d/cht_2d_3cylinders.cfg           |  2 +-
 .../incomp_2d_unsteady/cht_2d_3cylinders.cfg  |  2 +-
 TestCases/ddes/flatplate/ddes_flatplate.cfg   |  2 +-
 .../deformation/brick_hex/def_brick_hex.cfg   |  2 +-
 .../brick_hex_rans/def_brick_hex_rans.cfg     |  2 +-
 .../brick_prism/def_brick_prism.cfg           |  2 +-
 .../brick_prism_rans/def_brick_prism_rans.cfg |  2 +-
 .../deformation/brick_pyra/def_brick_pyra.cfg |  2 +-
 .../deformation/brick_tets/def_brick_tets.cfg |  2 +-
 .../cylindrical_ffd/def_cylindrical.cfg       |  2 +-
 .../intersection_prevention/def_intersect.cfg |  2 +-
 .../deformation/naca0012/def_NACA0012.cfg     |  2 +-
 .../naca0012/surface_file_NACA0012.cfg        |  2 +-
 .../deformation/naca4412/def_NACA4412.cfg     |  2 +-
 TestCases/deformation/rae2822/def_RAE2822.cfg |  2 +-
 .../spherical_ffd/def_spherical.cfg           |  2 +-
 .../spherical_ffd/def_spherical_bspline.cfg   |  2 +-
 .../disc_adj_euler/arina2k/Arina2KRS.cfg      |  2 +-
 .../cylinder3D/inv_cylinder3D.cfg             |  2 +-
 .../disc_adj_euler/oneram6/inv_ONERAM6.cfg    |  2 +-
 TestCases/disc_adj_fea/configAD_fem.cfg       |  2 +-
 TestCases/disc_adj_fsi/configFEA.cfg          |  2 +-
 TestCases/disc_adj_fsi/configFlow.cfg         |  2 +-
 TestCases/disc_adj_heat/disc_adj_heat.cfg     |  2 +-
 TestCases/disc_adj_heat/primal.cfg            |  2 +-
 .../naca0012/incomp_NACA0012_disc.cfg         |  2 +-
 .../cylinder/heated_cylinder.cfg              |  2 +-
 .../naca0012/turb_naca0012_sa.cfg             |  2 +-
 .../naca0012/turb_naca0012_sst.cfg            |  2 +-
 TestCases/disc_adj_rans/cylinder/cylinder.cfg |  2 +-
 .../cylinder/cylinder_Windowing.cfg           |  2 +-
 .../cylinder/cylinder_Windowing_AD.cfg        |  2 +-
 .../cylinder_DT_1ST/cylinder.cfg              |  2 +-
 TestCases/disc_adj_rans/naca0012/naca0012.cfg |  2 +-
 .../naca0012/turb_NACA0012_sa.cfg             |  2 +-
 .../naca0012/turb_NACA0012_sst.cfg            |  2 +-
 .../transonic_stator_2D/transonic_stator.cfg  |  2 +-
 TestCases/euler/CRM/inv_CRM_JST.cfg           |  2 +-
 TestCases/euler/biparabolic/BIPARABOLIC.cfg   |  2 +-
 TestCases/euler/bluntbody/blunt.cfg           |  2 +-
 TestCases/euler/channel/inv_channel.cfg       |  2 +-
 TestCases/euler/channel/inv_channel_RK.cfg    |  2 +-
 TestCases/euler/naca0012/inv_NACA0012.cfg     |  2 +-
 TestCases/euler/naca0012/inv_NACA0012_Roe.cfg |  2 +-
 TestCases/euler/oneram6/inv_ONERAM6.cfg       |  2 +-
 TestCases/euler/ramp/inv_ramp.cfg             |  2 +-
 TestCases/euler/wedge/inv_wedge_HLLC.cfg      |  2 +-
 TestCases/fea_fsi/Airfoil_RBF/config.cfg      |  2 +-
 TestCases/fea_fsi/Airfoil_RBF/configFEA.cfg   |  2 +-
 TestCases/fea_fsi/Airfoil_RBF/configFlow.cfg  |  2 +-
 .../fea_fsi/DynBeam_2d/configBeam_2d.cfg      |  2 +-
 TestCases/fea_fsi/MixElemsKnowles/config.cfg  |  2 +-
 TestCases/fea_fsi/SquareCyl_Beam/config.cfg   |  2 +-
 .../fea_fsi/StatBeam_3d/configBeam_3d.cfg     |  2 +-
 TestCases/fea_topology/config.cfg             |  2 +-
 TestCases/fixed_cl/naca0012/inv_NACA0012.cfg  |  2 +-
 .../naca0012/inv_NACA0012_ContAdj.cfg         |  2 +-
 .../lam_prem_ch4_cfd.cfg                      |  2 +-
 .../lam_prem_ch4_hx_ad.cfg                    |  2 +-
 .../lam_prem_ch4_hx_dot.cfg                   |  2 +-
 .../lam_prem_ch4_cfd_axi.cfg                  |  2 +-
 .../lam_partial_prem_ch4_cfd.cfg              |  2 +-
 .../naca0012/inv_NACA0012_gradsmooth.cfg      |  2 +-
 .../oneram6/ONERAM6_gradsmooth.cfg            |  2 +-
 TestCases/gust/cosine_gust_zdir.cfg           |  2 +-
 TestCases/gust/gust_with_mesh_deformation.cfg |  2 +-
 TestCases/gust/inv_gust_NACA0012.cfg          |  2 +-
 TestCases/harmonic_balance/HB.cfg             |  2 +-
 .../hb_rans_preconditioning/davis.cfg         |  2 +-
 .../fem_NACA0012.cfg                          |  2 +-
 .../NACA0012_5thOrder/fem_NACA0012.cfg        |  2 +-
 .../NACA0012_5thOrder/fem_NACA0012_reg.cfg    |  2 +-
 .../Sphere_4thOrder_Hexa/fem_Sphere.cfg       |  2 +-
 .../Sphere_4thOrder_Tet/fem_Sphere.cfg        |  2 +-
 .../nPoly1/fem_SubsonicChannel.cfg            |  2 +-
 .../nPoly1/fem_SubsonicChannel_Farfield.cfg   |  2 +-
 .../nPoly2/fem_SubsonicChannel.cfg            |  2 +-
 .../nPoly2/fem_SubsonicChannel_Farfield.cfg   |  2 +-
 .../nPoly4/fem_SubsonicChannel.cfg            |  2 +-
 .../nPoly4/fem_SubsonicChannel_Farfield.cfg   |  2 +-
 .../nPoly3/fem_Cylinder_reg.cfg               |  2 +-
 .../FlatPlate/nPoly4/lam_flatplate_reg.cfg    |  2 +-
 .../nPoly3_QuadDominant/fem_Sphere_reg.cfg    |  2 +-
 .../fem_Sphere_reg_ADER.cfg                   |  2 +-
 .../nPoly4/fem_unst_cylinder.cfg              |  2 +-
 .../nPoly4/fem_unst_cylinder_ADER.cfg         |  2 +-
 TestCases/hybrid_regression.py                |  2 +-
 TestCases/hybrid_regression_AD.py             |  2 +-
 .../incomp_euler/naca0012/incomp_NACA0012.cfg |  2 +-
 TestCases/incomp_euler/nozzle/inv_nozzle.cfg  |  2 +-
 .../buoyancy_cavity/lam_buoyancy_cavity.cfg   |  2 +-
 .../cylinder/incomp_cylinder.cfg              |  2 +-
 .../cylinder/poly_cylinder.cfg                |  2 +-
 .../chtPinArray_2d/BC_HeatTransfer.cfg        |  2 +-
 .../chtPinArray_2d/DA_configMaster.cfg        |  2 +-
 .../chtPinArray_2d/FD_configMaster.cfg        |  2 +-
 .../chtPinArray_2d/configFluid.cfg            |  2 +-
 .../chtPinArray_2d/configMaster.cfg           |  2 +-
 .../chtPinArray_2d/configSolid.cfg            |  2 +-
 .../chtPinArray_3d/configFluid.cfg            |  2 +-
 .../chtPinArray_3d/configMaster.cfg           |  2 +-
 .../chtPinArray_3d/configSolid.cfg            |  2 +-
 .../dp-adjoint_chtPinArray_2d/configFluid.cfg |  2 +-
 .../configMaster.cfg                          |  2 +-
 .../dp-adjoint_chtPinArray_2d/configSolid.cfg |  2 +-
 .../pipeSlice_3d/sp_pipeSlice_3d_dp_hf_tp.cfg |  2 +-
 TestCases/incomp_rans/naca0012/naca0012.cfg   |  2 +-
 .../naca0012/naca0012_SST_SUST.cfg            |  2 +-
 .../rough_flatplate_incomp.cfg                |  2 +-
 TestCases/mms/dg_ringleb/ringleb_dg.cfg       |  2 +-
 .../mms/fvm_incomp_euler/inv_mms_jst.cfg      |  2 +-
 .../fvm_incomp_navierstokes/lam_mms_fds.cfg   |  2 +-
 .../mms/fvm_navierstokes/lam_mms_roe.cfg      |  2 +-
 TestCases/moving_wall/cavity/lam_cavity.cfg   |  2 +-
 .../spinning_cylinder/spinning_cylinder.cfg   |  2 +-
 .../naca0012/inv_NACA0012_ffd.cfg             |  2 +-
 .../cylinder/cylinder_lowmach.cfg             |  2 +-
 .../navierstokes/cylinder/lam_cylinder.cfg    |  2 +-
 .../navierstokes/flatplate/lam_flatplate.cfg  |  2 +-
 .../flatplate/lam_flatplate_unst.cfg          |  2 +-
 .../navierstokes/naca0012/lam_NACA0012.cfg    |  2 +-
 .../poiseuille/lam_poiseuille.cfg             |  2 +-
 .../poiseuille/profile_poiseuille.cfg         |  2 +-
 TestCases/nicf/LS89/turb_SA_PR.cfg            |  2 +-
 TestCases/nicf/LS89/turb_SST_PR.cfg           |  2 +-
 TestCases/nicf/coolprop/fluidModel.cfg        |  2 +-
 TestCases/nicf/coolprop/transportModel.cfg    |  2 +-
 .../nicf/datadriven/datadriven_nozzle.cfg     |  2 +-
 TestCases/nicf/edge/edge_PPR.cfg              |  2 +-
 TestCases/nicf/edge/edge_VW.cfg               |  2 +-
 .../nonequilibrium/invwedge/invwedge_ausm.cfg |  2 +-
 .../invwedge/invwedge_ausmplusup2.cfg         |  2 +-
 .../nonequilibrium/invwedge/invwedge_lax.cfg  |  2 +-
 .../nonequilibrium/invwedge/invwedge_msw.cfg  |  2 +-
 .../nonequilibrium/invwedge/invwedge_roe.cfg  |  2 +-
 .../invwedge/invwedge_ss_inlet.cfg            |  2 +-
 .../finitechemistry/thermalbath.cfg           |  2 +-
 .../thermalbath/frozen/thermalbath_frozen.cfg |  2 +-
 .../visc_wedge/axi_visccone.cfg               |  2 +-
 .../nonequilibrium/visc_wedge/partial_cat.cfg |  2 +-
 .../nonequilibrium/visc_wedge/super_cat.cfg   |  2 +-
 .../viscwedge_mpp/viscwedge_mpp.cfg           |  2 +-
 .../equivalentarea_naca64206/NACA64206.cfg    |  2 +-
 .../inv_wedge_ROE_2surf_1obj.cfg              |  2 +-
 .../inv_wedge_ROE_multiobj.cfg                |  2 +-
 .../inv_wedge_ROE_multiobj_1surf.cfg          |  2 +-
 .../inv_wedge_ROE_multiobj_combo.cfg          |  2 +-
 .../inv_NACA0012_multipoint.cfg               |  2 +-
 .../pitching_NACA64A010.cfg                   |  2 +-
 .../pitching_oneram6/pitching_ONERAM6.cfg     |  2 +-
 .../rotating_naca0012/rotating_NACA0012.cfg   |  2 +-
 .../steady_inverse_design/inv_NACA0012.cfg    |  2 +-
 .../steady_naca0012/inv_NACA0012_adv.cfg      |  2 +-
 .../steady_naca0012/inv_NACA0012_basic.cfg    |  2 +-
 .../steady_oneram6/inv_ONERAM6_adv.cfg        |  2 +-
 .../steady_oneram6/inv_ONERAM6_basic.cfg      |  2 +-
 .../optimization_rans/naca0012/naca0012.cfg   |  2 +-
 .../pitching_naca64a010/turb_NACA64A010.cfg   |  2 +-
 .../pitching_oneram6/turb_ONERAM6.cfg         |  2 +-
 .../steady_oneram6/turb_ONERAM6.cfg           |  2 +-
 .../steady_rae2822/turb_SA_RAE2822.cfg        |  2 +-
 TestCases/parallel_regression.py              |  2 +-
 TestCases/parallel_regression_AD.py           |  2 +-
 TestCases/pastix_support/config.cfg           |  2 +-
 TestCases/pastix_support/readme.txt           |  2 +-
 TestCases/polar/naca0012/inv_NACA0012.cfg     |  2 +-
 .../py_wrapper/custom_heat_flux/run_ad.py     |  2 +-
 .../py_wrapper/custom_load_fea/config.cfg     |  2 +-
 TestCases/py_wrapper/custom_load_fea/run.py   |  2 +-
 .../py_wrapper/custom_load_fea/run_ad.py      |  2 +-
 .../deforming_bump_in_channel/run.py          |  2 +-
 .../flow_load_sens/run_adjoint.py             |  2 +-
 .../mesh_disp_sens/run_adjoint.py             |  2 +-
 TestCases/py_wrapper/dyn_fsi/run.py           |  2 +-
 .../flatPlate_rigidMotion_Conf.cfg            |  2 +-
 .../launch_flatPlate_rigidMotion.py           |  2 +-
 .../launch_unsteady_CHT_FlatPlate.py          |  2 +-
 .../unsteady_CHT_FlatPlate_Conf.cfg           |  2 +-
 TestCases/py_wrapper/wavy_wall/run_steady.py  |  2 +-
 .../radiation/p1adjoint/configp1adjoint.cfg   |  2 +-
 TestCases/radiation/p1model/configp1.cfg      |  2 +-
 .../propeller_variable_load.cfg               |  2 +-
 .../rans/flatplate/turb_SA_flatplate.cfg      |  2 +-
 .../flatplate/turb_SA_flatplate_species.cfg   |  2 +-
 .../rans/flatplate/turb_SST_flatplate.cfg     |  2 +-
 TestCases/rans/naca0012/turb_NACA0012_sa.cfg  |  2 +-
 TestCases/rans/naca0012/turb_NACA0012_sst.cfg |  2 +-
 .../naca0012/turb_NACA0012_sst_1994-KLm.cfg   |  2 +-
 .../naca0012/turb_NACA0012_sst_2003-Vm.cfg    |  2 +-
 .../rans/naca0012/turb_NACA0012_sst_2003m.cfg |  2 +-
 .../turb_NACA0012_sst_expliciteuler.cfg       |  2 +-
 .../turb_NACA0012_sst_fixedvalues.cfg         |  2 +-
 .../turb_NACA0012_sst_multigrid_restart.cfg   |  2 +-
 .../rans/naca0012/turb_NACA0012_sst_sust.cfg  |  2 +-
 TestCases/rans/oneram6/turb_ONERAM6.cfg       |  2 +-
 TestCases/rans/oneram6/turb_ONERAM6_nk.cfg    |  2 +-
 TestCases/rans/oneram6/turb_ONERAM6_vc.cfg    |  2 +-
 TestCases/rans/propeller/propeller.cfg        |  2 +-
 TestCases/rans/rae2822/turb_SA_RAE2822.cfg    |  2 +-
 TestCases/rans/rae2822/turb_SST_RAE2822.cfg   |  2 +-
 .../rans/rae2822/turb_SST_SUST_RAE2822.cfg    |  2 +-
 .../rans/restart_directdiff_naca/naca0012.cfg |  2 +-
 TestCases/rans/s809/trans_s809.cfg            |  2 +-
 TestCases/rans/s809/turb_S809.cfg             |  2 +-
 TestCases/rans/vki_turbine/turb_vki.cfg       |  2 +-
 .../rans_uq/naca0012/turb_NACA0012_uq.cfg     |  2 +-
 .../rans_uq/naca0012/turb_NACA0012_uq_1c.cfg  |  2 +-
 .../rans_uq/naca0012/turb_NACA0012_uq_2c.cfg  |  2 +-
 .../rans_uq/naca0012/turb_NACA0012_uq_3c.cfg  |  2 +-
 .../naca0012/turb_NACA0012_uq_p1c1.cfg        |  2 +-
 .../naca0012/turb_NACA0012_uq_p1c2.cfg        |  2 +-
 .../caradonna_tung/rot_caradonna_tung.cfg     |  2 +-
 TestCases/rotating/naca0012/rot_NACA0012.cfg  |  2 +-
 TestCases/serial_regression.py                |  2 +-
 TestCases/serial_regression_AD.py             |  2 +-
 .../sliding_interface/bars_SST_2D/bars.cfg    |  2 +-
 .../sliding_interface/bars_SST_2D/zone_1.cfg  |  2 +-
 .../sliding_interface/bars_SST_2D/zone_2.cfg  |  2 +-
 .../sliding_interface/bars_SST_2D/zone_3.cfg  |  2 +-
 .../channel_2D/channel_2D_NN.cfg              |  2 +-
 .../channel_2D/channel_2D_WA.cfg              |  2 +-
 .../sliding_interface/channel_2D/zone_2.cfg   |  2 +-
 .../sliding_interface/channel_2D/zone_3.cfg   |  2 +-
 .../channel_3D/channel_3D_NN.cfg              |  2 +-
 .../channel_3D/channel_3D_WA.cfg              |  2 +-
 .../sliding_interface/channel_3D/zone_1.cfg   |  2 +-
 .../sliding_interface/channel_3D/zone_2.cfg   |  2 +-
 .../sliding_interface/channel_3D/zone_3.cfg   |  2 +-
 .../incompressible_steady/config.cfg          |  2 +-
 .../incompressible_steady/configCircle.cfg    |  2 +-
 .../incompressible_steady/configOut.cfg       |  2 +-
 .../incompressible_unsteady/config.cfg        |  2 +-
 .../incompressible_unsteady/configCircle.cfg  |  2 +-
 .../incompressible_unsteady/configOut.cfg     |  2 +-
 TestCases/sliding_interface/pipe/pipe_NN.cfg  |  2 +-
 TestCases/sliding_interface/pipe/pipe_WA.cfg  |  2 +-
 TestCases/sliding_interface/pipe/zone_1.cfg   |  2 +-
 TestCases/sliding_interface/pipe/zone_2.cfg   |  2 +-
 TestCases/sliding_interface/pipe/zone_3.cfg   |  2 +-
 TestCases/sliding_interface/pipe/zone_4.cfg   |  2 +-
 TestCases/sliding_interface/pipe/zone_5.cfg   |  2 +-
 .../rotating_cylinders/rot_cylinders_NN.cfg   |  2 +-
 .../rotating_cylinders/rot_cylinders_WA.cfg   |  2 +-
 .../single_stage/single_stage_NN.cfg          |  2 +-
 .../single_stage/single_stage_WA.cfg          |  2 +-
 .../sliding_interface/single_stage/zone_1.cfg |  2 +-
 .../sliding_interface/single_stage/zone_2.cfg |  2 +-
 .../sup_vor_shed_NN.cfg                       |  2 +-
 .../sup_vor_shed_WA.cfg                       |  2 +-
 .../supersonic_vortex_shedding/zone_1.cfg     |  2 +-
 .../supersonic_vortex_shedding/zone_2.cfg     |  2 +-
 .../uniform_flow/uniform_NN.cfg               |  2 +-
 .../uniform_flow/uniform_WA.cfg               |  2 +-
 .../sliding_interface/uniform_flow/zone_1.cfg |  2 +-
 .../sliding_interface/uniform_flow/zone_2.cfg |  2 +-
 .../periodic_pins/configSolid.cfg             |  2 +-
 .../multizone/configMaster.cfg                |  2 +-
 .../passive_transport.cfg                     |  2 +-
 .../species2_primitiveVenturi.cfg             |  2 +-
 ...pecies2_primitiveVenturi_boundedscalar.cfg |  2 +-
 .../species2_primitiveVenturi_mixingmodel.cfg |  2 +-
 ...eVenturi_mixingmodel_TURBULENT_MARKERS.cfg |  2 +-
 ...itiveVenturi_mixingmodel_boundedscalar.cfg |  2 +-
 ...iveVenturi_mixingmodel_heatcapacity_H2.cfg |  2 +-
 ...Venturi_mixingmodel_heatcapacity_H2_ND.cfg |  2 +-
 ...primitiveVenturi_mixingmodel_viscosity.cfg |  2 +-
 .../species3_primitiveVenturi_inletFile.cfg   |  2 +-
 .../transitional_BC_model_ConfigFile.cfg      |  2 +-
 .../transitional_BC_model_ConfigFile.cfg      |  2 +-
 .../transitional_BC_model_ConfigFile.cfg      |  2 +-
 .../APU_turbocharger/Jones_restart.cfg        |  2 +-
 .../axial_stage_2D/Axial_stage2D.cfg          |  2 +-
 .../turbomachinery/axial_stage_2D/zone_1.cfg  |  2 +-
 .../turbomachinery/axial_stage_2D/zone_2.cfg  |  2 +-
 .../centrifugal_blade/centrifugal_blade.cfg   |  2 +-
 .../centrifugal_stage/centrifugal_stage.cfg   |  2 +-
 .../transonic_stator_restart.cfg              |  2 +-
 TestCases/tutorials.py                        |  2 +-
 .../pitching_NACA64A010.cfg                   |  2 +-
 .../turb_NACA64A010.cfg                       |  2 +-
 .../plunging_naca0012/plunging_NACA0012.cfg   |  2 +-
 .../unsteady/square_cylinder/turb_square.cfg  |  2 +-
 .../user_defined_functions/lam_flatplate.cfg  |  2 +-
 TestCases/vandv.py                            |  2 +-
 .../sandia_jet/validation.cfg                 |  2 +-
 .../compressible_SA/turb_SA_flatplate.cfg     |  2 +-
 .../compressible_SST/turb_SST_flatplate.cfg   |  2 +-
 .../incompressible_SA/turb_SA_flatplate.cfg   |  2 +-
 .../incompressible_SST/turb_SST_flatplate.cfg |  2 +-
 .../Common/containers/CLookupTable_tests.cpp  |  2 +-
 UnitTests/Common/geometry/CGeometry_test.cpp  |  2 +-
 .../geometry/dual_grid/CDualGrid_tests.cpp    |  2 +-
 .../primal_grid/CPrimalGrid_tests.cpp         |  2 +-
 UnitTests/Common/simple_ad_test.cpp           |  2 +-
 UnitTests/Common/simple_directdiff_test.cpp   |  2 +-
 .../toolboxes/C1DInterpolation_tests.cpp      |  2 +-
 .../CQuasiNewtonInvLeastSquares_tests.cpp     |  2 +-
 .../CLookUp_ANN_tests.cpp                     |  2 +-
 .../Common/toolboxes/ndflattener_tests.cpp    |  2 +-
 UnitTests/Common/vectorization.cpp            |  2 +-
 UnitTests/SU2_CFD/gradients.cpp               |  2 +-
 .../SU2_CFD/numerics/CNumerics_tests.cpp      |  2 +-
 UnitTests/SU2_CFD/windowing.cpp               |  2 +-
 UnitTests/UnitQuadTestCase.hpp                |  2 +-
 UnitTests/test_driver.cpp                     |  2 +-
 config_template.cfg                           |  2 +-
 meson.build                                   |  4 ++--
 meson.py                                      |  2 +-
 meson_scripts/init.py                         |  2 +-
 preconfigure.py                               |  2 +-
 su2omp.syntax.json                            |  2 +-
 1003 files changed, 1082 insertions(+), 1082 deletions(-)

diff --git a/Common/include/CConfig.hpp b/Common/include/CConfig.hpp
index dd5bde0606c..563d477a696 100644
--- a/Common/include/CConfig.hpp
+++ b/Common/include/CConfig.hpp
@@ -3,7 +3,7 @@
  * \brief All the information about the definition of the physical problem.
  *        The subroutines and functions are in the <i>CConfig.cpp</i> file.
  * \author F. Palacios, T. Economon, B. Tracey
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/adt/CADTBaseClass.hpp b/Common/include/adt/CADTBaseClass.hpp
index 9a10f9fce54..996a11a8edf 100644
--- a/Common/include/adt/CADTBaseClass.hpp
+++ b/Common/include/adt/CADTBaseClass.hpp
@@ -2,7 +2,7 @@
  * \file CADTBaseClass.hpp
  * \brief Base class for storing an ADT in an arbitrary number of dimensions.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/adt/CADTComparePointClass.hpp b/Common/include/adt/CADTComparePointClass.hpp
index 5457241b839..ca6655f40f5 100644
--- a/Common/include/adt/CADTComparePointClass.hpp
+++ b/Common/include/adt/CADTComparePointClass.hpp
@@ -2,7 +2,7 @@
  * \file CADTComparePointClass.hpp
  * \brief subroutines for comparing two points in an alternating digital tree (ADT).
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/adt/CADTElemClass.hpp b/Common/include/adt/CADTElemClass.hpp
index dd0b862be60..2f8855aeb68 100644
--- a/Common/include/adt/CADTElemClass.hpp
+++ b/Common/include/adt/CADTElemClass.hpp
@@ -2,7 +2,7 @@
  * \file CADTElemClass.hpp
  * \brief Class for storing an ADT of (linear) elements in an arbitrary number of dimensions.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -36,7 +36,7 @@
  * \ingroup ADT
  * \brief  Class for storing an ADT of (linear) elements in an arbitrary number of dimensions.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CADTElemClass : public CADTBaseClass {
  private:
diff --git a/Common/include/adt/CADTNodeClass.hpp b/Common/include/adt/CADTNodeClass.hpp
index 28ac30696c6..c09dda7799d 100644
--- a/Common/include/adt/CADTNodeClass.hpp
+++ b/Common/include/adt/CADTNodeClass.hpp
@@ -2,7 +2,7 @@
  * \file CADTNodeClass.hpp
  * \brief Class for storing the information needed in a node of an ADT.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/adt/CADTPointsOnlyClass.hpp b/Common/include/adt/CADTPointsOnlyClass.hpp
index ba5f38adc49..721c09398b1 100644
--- a/Common/include/adt/CADTPointsOnlyClass.hpp
+++ b/Common/include/adt/CADTPointsOnlyClass.hpp
@@ -2,7 +2,7 @@
  * \file CADTPointsOnlyClass.hpp
  * \brief Class for storing an ADT of only points in an arbitrary number of dimensions.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/adt/CBBoxTargetClass.hpp b/Common/include/adt/CBBoxTargetClass.hpp
index 405a9956e98..3ff32c169a2 100644
--- a/Common/include/adt/CBBoxTargetClass.hpp
+++ b/Common/include/adt/CBBoxTargetClass.hpp
@@ -3,7 +3,7 @@
  * \brief Class for storing the information of a possible bounding box candidate
            during a minimum distance search.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -35,7 +35,7 @@
  * \brief  Class for storing the information of a possible bounding box candidate
            during a minimum distance search.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 struct CBBoxTargetClass {
   unsigned long boundingBoxID;  /*!< \brief Corresponding bounding box ID. */
diff --git a/Common/include/basic_types/ad_structure.hpp b/Common/include/basic_types/ad_structure.hpp
index 2373163a215..8cf72344258 100644
--- a/Common/include/basic_types/ad_structure.hpp
+++ b/Common/include/basic_types/ad_structure.hpp
@@ -2,7 +2,7 @@
  * \file ad_structure.hpp
  * \brief Main routines for the algorithmic differentiation (AD) structure.
  * \author T. Albring, J. Blühdorn
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/basic_types/datatype_structure.hpp b/Common/include/basic_types/datatype_structure.hpp
index b4bfbd47b1b..54d8d5fbd64 100644
--- a/Common/include/basic_types/datatype_structure.hpp
+++ b/Common/include/basic_types/datatype_structure.hpp
@@ -2,7 +2,7 @@
  * \file datatype_structure.hpp
  * \brief Headers for generalized datatypes, defines an interface for AD types.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/code_config.hpp b/Common/include/code_config.hpp
index 3ab5b3070fc..447c1a5fb5f 100644
--- a/Common/include/code_config.hpp
+++ b/Common/include/code_config.hpp
@@ -2,7 +2,7 @@
  * \file code_config.hpp
  * \brief Header file for collecting common macros, definitions and type configurations.
  * \author T. Albring, P. Gomes, J. Blühdorn
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/containers/C2DContainer.hpp b/Common/include/containers/C2DContainer.hpp
index 8e726ee4ef9..d53be8ddcd8 100644
--- a/Common/include/containers/C2DContainer.hpp
+++ b/Common/include/containers/C2DContainer.hpp
@@ -2,7 +2,7 @@
  * \file C2DContainer.hpp
  * \brief A templated vector/matrix object.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/containers/CFastFindAndEraseQueue.hpp b/Common/include/containers/CFastFindAndEraseQueue.hpp
index 004500dcc86..cd4a528d883 100644
--- a/Common/include/containers/CFastFindAndEraseQueue.hpp
+++ b/Common/include/containers/CFastFindAndEraseQueue.hpp
@@ -3,7 +3,7 @@
  * \brief A queue-type container (push back, pop front), but with
  *        fast deletion of arbitrary items (possibly in the middle).
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/containers/CFileReaderLUT.hpp b/Common/include/containers/CFileReaderLUT.hpp
index 69d3c4c0286..bd1c64d2844 100644
--- a/Common/include/containers/CFileReaderLUT.hpp
+++ b/Common/include/containers/CFileReaderLUT.hpp
@@ -2,7 +2,7 @@
  * \file CFileReaderLUT.hpp
  * \brief reading lookup table for tabulated fluid properties
  * \author D. Mayer, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/containers/CLookUpTable.hpp b/Common/include/containers/CLookUpTable.hpp
index be60704ebfa..102f69d1db1 100644
--- a/Common/include/containers/CLookUpTable.hpp
+++ b/Common/include/containers/CLookUpTable.hpp
@@ -2,7 +2,7 @@
  * \file CLookupTable.hpp
  * \brief tabulation of fluid properties
  * \author D. Mayer, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/containers/CPyWrapperMatrixView.hpp b/Common/include/containers/CPyWrapperMatrixView.hpp
index 321f062738d..67562065978 100644
--- a/Common/include/containers/CPyWrapperMatrixView.hpp
+++ b/Common/include/containers/CPyWrapperMatrixView.hpp
@@ -2,7 +2,7 @@
  * \file CPyWrapperMatrixView.hpp
  * \brief Simple matrix views to use with the python wrapper.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/containers/CTrapezoidalMap.hpp b/Common/include/containers/CTrapezoidalMap.hpp
index 207b010d31e..c5f99f1bb3f 100644
--- a/Common/include/containers/CTrapezoidalMap.hpp
+++ b/Common/include/containers/CTrapezoidalMap.hpp
@@ -2,7 +2,7 @@
  * \file CTrapezoidalMap.hpp
  * \brief Implementation of the trapezoidal map for tabulation and lookup of fluid properties
  * \author D. Mayer, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -38,7 +38,7 @@
  * \ingroup LookUpInterp
  * \brief Construction of trapezoidal map for tabulated lookup
  * \author: D. Mayer, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CTrapezoidalMap {
  protected:
diff --git a/Common/include/containers/CVertexMap.hpp b/Common/include/containers/CVertexMap.hpp
index 54e5ee85da0..e02bf7a4a25 100644
--- a/Common/include/containers/CVertexMap.hpp
+++ b/Common/include/containers/CVertexMap.hpp
@@ -2,7 +2,7 @@
  * \file CVertexMap.hpp
  * \brief An index to index lookup vector.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/containers/container_decorators.hpp b/Common/include/containers/container_decorators.hpp
index c6c0f3f1201..3bcbf705217 100644
--- a/Common/include/containers/container_decorators.hpp
+++ b/Common/include/containers/container_decorators.hpp
@@ -3,7 +3,7 @@
  * \brief Collection of small classes that decorate C2DContainer to
  * augment its functionality, e.g. give it extra dimensions.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/fem/fem_cgns_elements.hpp b/Common/include/fem/fem_cgns_elements.hpp
index 8e9458d8d06..43bcfb0b6fb 100644
--- a/Common/include/fem/fem_cgns_elements.hpp
+++ b/Common/include/fem/fem_cgns_elements.hpp
@@ -4,7 +4,7 @@
  *        with high order elements.
  *        The functions are in the <i>cgns_elements.cpp</i> file.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/fem/fem_gauss_jacobi_quadrature.hpp b/Common/include/fem/fem_gauss_jacobi_quadrature.hpp
index 04a450d8cce..03ed52eab78 100644
--- a/Common/include/fem/fem_gauss_jacobi_quadrature.hpp
+++ b/Common/include/fem/fem_gauss_jacobi_quadrature.hpp
@@ -6,7 +6,7 @@
           All the functions in this class are based on the program JACOBI_RULE
           of John Burkardt.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -95,7 +95,7 @@ using namespace std;
  * \brief Class used to determine the quadrature points of the Gauss Jacobi
           integration rules.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CGaussJacobiQuadrature {
  public:
diff --git a/Common/include/fem/fem_geometry_structure.hpp b/Common/include/fem/fem_geometry_structure.hpp
index a6b79f276cc..3ea11dedb01 100644
--- a/Common/include/fem/fem_geometry_structure.hpp
+++ b/Common/include/fem/fem_geometry_structure.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for creating the geometrical structure for the FEM solver.
  *        The subroutines and functions are in the <i>fem_geometry_structure.cpp</i> file.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -41,7 +41,7 @@ using namespace std;
 /*!
  * \class CLong3T
  * \brief Help class used to store three longs as one entity.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 struct CLong3T {
   long long0 = 0; /*!< \brief First long to store in this class. */
@@ -63,7 +63,7 @@ struct CLong3T {
  * \class CReorderElements
  * \brief Class, used to reorder the owned elements after the partitioning.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CReorderElements {
  private:
@@ -131,7 +131,7 @@ class CReorderElements {
  * \brief Functor, used for a different sorting of the faces than the < operator
  *        of CFaceOfElement.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CVolumeElementFEM;  // Forward declaration to avoid problems.
 class CSortFaces {
@@ -169,7 +169,7 @@ class CSortFaces {
  * \brief Functor, used for a different sorting of the faces than the < operator
  *        of CSurfaceElementFEM.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 struct CSurfaceElementFEM;  // Forward declaration to avoid problems.
 struct CSortBoundaryFaces {
@@ -185,7 +185,7 @@ struct CSortBoundaryFaces {
  * \class CVolumeElementFEM
  * \brief Class to store a volume element for the FEM solver.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CVolumeElementFEM {
  public:
@@ -276,7 +276,7 @@ class CVolumeElementFEM {
  * \class CPointFEM
  * \brief Class to a point for the FEM solver.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 struct CPointFEM {
   unsigned long globalID;    /*!< \brief The global ID of this point in the grid. */
@@ -300,7 +300,7 @@ struct CPointFEM {
  * \class CInternalFaceElementFEM
  * \brief Class to store an internal face for the FEM solver.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 struct CInternalFaceElementFEM {
   unsigned short VTK_Type; /*!< \brief Element type using the VTK convention. */
@@ -344,7 +344,7 @@ struct CInternalFaceElementFEM {
  * \class CSurfaceElementFEM
  * \brief Class to store a surface element for the FEM solver.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 struct CSurfaceElementFEM {
   unsigned short VTK_Type;  /*!< \brief Element type using the VTK convention. */
@@ -405,7 +405,7 @@ struct CSurfaceElementFEM {
  * \class CBoundaryFEM
  * \brief Class to store a boundary for the FEM solver.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 struct CBoundaryFEM {
   string markerTag; /*!< \brief Marker tag of this boundary. */
@@ -428,7 +428,7 @@ struct CBoundaryFEM {
  * \class CMeshFEM
  * \brief Base class for the FEM solver.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CMeshFEM : public CGeometry {
  protected:
@@ -693,7 +693,7 @@ class CMeshFEM : public CGeometry {
  * \class CMeshFEM_DG
  * \brief Class which contains all the variables for the DG FEM solver.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CMeshFEM_DG : public CMeshFEM {
  protected:
diff --git a/Common/include/fem/fem_standard_element.hpp b/Common/include/fem/fem_standard_element.hpp
index 63869d7fff7..7457fe715cf 100644
--- a/Common/include/fem/fem_standard_element.hpp
+++ b/Common/include/fem/fem_standard_element.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main functions for the FEM standard elements.
  *        The functions are in the <i>fem_standard_element.cpp</i> file.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -40,7 +40,7 @@ using namespace std;
  * \class CFEMStandardElementBase
  * \brief Base class for a FEM standard element.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CFEMStandardElementBase {
  protected:
@@ -668,7 +668,7 @@ class CFEMStandardElementBase {
  * \class CFEMStandardElement
  * \brief Class to define a FEM standard element.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CFEMStandardElement : public CFEMStandardElementBase {
  private:
@@ -1101,7 +1101,7 @@ class CFEMStandardElement : public CFEMStandardElementBase {
  * \class CFEMStandardInternalFace
  * \brief Class to define a FEM standard internal face.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CFEMStandardInternalFace : public CFEMStandardElementBase {
  private:
@@ -1434,7 +1434,7 @@ class CFEMStandardInternalFace : public CFEMStandardElementBase {
  * \class CFEMStandardBoundaryFace
  * \brief Class to define a FEM standard boundary face.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CFEMStandardBoundaryFace : public CFEMStandardElementBase {
  private:
diff --git a/Common/include/fem/geometry_structure_fem_part.hpp b/Common/include/fem/geometry_structure_fem_part.hpp
index 0791d9bfe0b..66471908d5a 100644
--- a/Common/include/fem/geometry_structure_fem_part.hpp
+++ b/Common/include/fem/geometry_structure_fem_part.hpp
@@ -2,7 +2,7 @@
  * \file geometry_structure_fem_part.hpp
  * \brief Helper classes for the Fluid FEM solver.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/CDummyGeometry.hpp b/Common/include/geometry/CDummyGeometry.hpp
index 73028f7f957..a7dea357b68 100644
--- a/Common/include/geometry/CDummyGeometry.hpp
+++ b/Common/include/geometry/CDummyGeometry.hpp
@@ -2,7 +2,7 @@
  * \file CDummyGeometry.hpp
  * \brief Headers of the dummy geometry class used in "dry run" mode.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/CGeometry.hpp b/Common/include/geometry/CGeometry.hpp
index 2eb464c7dcd..f8111060725 100644
--- a/Common/include/geometry/CGeometry.hpp
+++ b/Common/include/geometry/CGeometry.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for creating the geometrical structure.
  *        The subroutines and functions are in the <i>CGeometry.cpp</i> file.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/CMultiGridGeometry.hpp b/Common/include/geometry/CMultiGridGeometry.hpp
index 6c875cc6f57..8136859bf64 100644
--- a/Common/include/geometry/CMultiGridGeometry.hpp
+++ b/Common/include/geometry/CMultiGridGeometry.hpp
@@ -2,7 +2,7 @@
  * \file CMultiGridGeometry.hpp
  * \brief Headers of the multigrid geometry class.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/CMultiGridQueue.hpp b/Common/include/geometry/CMultiGridQueue.hpp
index 3e75e80af1a..11995b3492d 100644
--- a/Common/include/geometry/CMultiGridQueue.hpp
+++ b/Common/include/geometry/CMultiGridQueue.hpp
@@ -3,7 +3,7 @@
  * \brief Header of the multigrid queue class for the FVM solver.
  *        The subroutines and functions are in the <i>CMultiGridQueue.cpp</i> file.
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/CPhysicalGeometry.hpp b/Common/include/geometry/CPhysicalGeometry.hpp
index 0f881daeea9..8e10bc2e685 100644
--- a/Common/include/geometry/CPhysicalGeometry.hpp
+++ b/Common/include/geometry/CPhysicalGeometry.hpp
@@ -2,7 +2,7 @@
  * \file CPhysicalGeometry.hpp
  * \brief Headers of the physical geometry class used to read meshes from file.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/dual_grid/CDualGrid.hpp b/Common/include/geometry/dual_grid/CDualGrid.hpp
index 1e96d519e2c..04b0f79dc10 100644
--- a/Common/include/geometry/dual_grid/CDualGrid.hpp
+++ b/Common/include/geometry/dual_grid/CDualGrid.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for doing the complete dual grid structure.
  *        The subroutines and functions are in the <i>CDualGrid.cpp</i> file.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/dual_grid/CEdge.hpp b/Common/include/geometry/dual_grid/CEdge.hpp
index c3fbd76449b..ac40488c5f3 100644
--- a/Common/include/geometry/dual_grid/CEdge.hpp
+++ b/Common/include/geometry/dual_grid/CEdge.hpp
@@ -2,7 +2,7 @@
  * \file CEdge.hpp
  * \brief Declaration of the edge class <i>CEdge.cpp</i> file.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/dual_grid/CPoint.hpp b/Common/include/geometry/dual_grid/CPoint.hpp
index 4e78f588bfa..a6f0ac73870 100644
--- a/Common/include/geometry/dual_grid/CPoint.hpp
+++ b/Common/include/geometry/dual_grid/CPoint.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration of the point class that stores geometric and adjacency
  *        information for dual control volumes.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/dual_grid/CTurboVertex.hpp b/Common/include/geometry/dual_grid/CTurboVertex.hpp
index 47a88bfb5fd..d14d451ea5e 100644
--- a/Common/include/geometry/dual_grid/CTurboVertex.hpp
+++ b/Common/include/geometry/dual_grid/CTurboVertex.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for doing the complete dual grid structure.
  *        The subroutines and functions are in the <i>CTurboVertex.cpp</i> file.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/dual_grid/CVertex.hpp b/Common/include/geometry/dual_grid/CVertex.hpp
index 3d18f439eef..268e8eb278e 100644
--- a/Common/include/geometry/dual_grid/CVertex.hpp
+++ b/Common/include/geometry/dual_grid/CVertex.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for doing the complete dual grid structure.
  *        The subroutines and functions are in the <i>CVertex.cpp</i> file.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/elements/CElement.hpp b/Common/include/geometry/elements/CElement.hpp
index 4c057ba59b2..7c30c56ea97 100644
--- a/Common/include/geometry/elements/CElement.hpp
+++ b/Common/include/geometry/elements/CElement.hpp
@@ -3,7 +3,7 @@
  * \brief Main header of the Finite Element structure declaring the abstract
  *        interface and the available finite element types.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -900,7 +900,7 @@ class CPYRAM5 final : public CElementWithKnownSizes<5, 5, 3> {
  * \ingroup FemAlgos
  * \brief Prism element with 6 Gauss Points
  * \author R. Sanchez, F. Palacios, A. Bueno, T. Economon, S. Padron.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CPRISM6 final : public CElementWithKnownSizes<6, 6, 3> {
  private:
diff --git a/Common/include/geometry/elements/CElementProperty.hpp b/Common/include/geometry/elements/CElementProperty.hpp
index 90efe7194b7..8fc195d964f 100644
--- a/Common/include/geometry/elements/CElementProperty.hpp
+++ b/Common/include/geometry/elements/CElementProperty.hpp
@@ -2,7 +2,7 @@
  * \file CElementProperty.hpp
  * \brief Light classes to define finite element properties.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -32,7 +32,7 @@
  * \ingroup Elasticity_Equations
  * \brief Base class for defining element properties.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CProperty {
  protected:
@@ -106,7 +106,7 @@ class CProperty {
  * \ingroup Elasticity_Equations
  * \brief Class for defining element properties for the structural solver.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CElementProperty final : public CProperty {
  private:
diff --git a/Common/include/geometry/elements/CGaussVariable.hpp b/Common/include/geometry/elements/CGaussVariable.hpp
index 3ce313403b6..78ebcb92683 100644
--- a/Common/include/geometry/elements/CGaussVariable.hpp
+++ b/Common/include/geometry/elements/CGaussVariable.hpp
@@ -2,7 +2,7 @@
  * \file CGaussVariable.hpp
  * \brief Light-weight class to store Gaussian point information.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -33,7 +33,7 @@
  * \class CGaussVariable
  * \ingroup FemAlgos
  * \brief Main class for defining the gaussian points.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CGaussVariable {
  protected:
diff --git a/Common/include/geometry/meshreader/CBoxMeshReaderFVM.hpp b/Common/include/geometry/meshreader/CBoxMeshReaderFVM.hpp
index 58ab28752b4..1c99fe92da8 100644
--- a/Common/include/geometry/meshreader/CBoxMeshReaderFVM.hpp
+++ b/Common/include/geometry/meshreader/CBoxMeshReaderFVM.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CBoxMeshReaderFVM.
  *        The implementations are in the <i>CBoxMeshReaderFVM.cpp</i> file.
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/meshreader/CCGNSMeshReaderFVM.hpp b/Common/include/geometry/meshreader/CCGNSMeshReaderFVM.hpp
index 198589808cf..f655993208a 100644
--- a/Common/include/geometry/meshreader/CCGNSMeshReaderFVM.hpp
+++ b/Common/include/geometry/meshreader/CCGNSMeshReaderFVM.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CCGNSMeshReaderFVM.
  *        The implementations are in the <i>CCGNSMeshReaderFVM.cpp</i> file.
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/meshreader/CMeshReaderFVM.hpp b/Common/include/geometry/meshreader/CMeshReaderFVM.hpp
index f4a46384e3d..d5b934c7de0 100644
--- a/Common/include/geometry/meshreader/CMeshReaderFVM.hpp
+++ b/Common/include/geometry/meshreader/CMeshReaderFVM.hpp
@@ -4,7 +4,7 @@
  * \brief Header file for the class CMeshReaderFVM.
  *        The implementations are in the <i>CMeshReaderFVM.cpp</i> file.
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/meshreader/CRectangularMeshReaderFVM.hpp b/Common/include/geometry/meshreader/CRectangularMeshReaderFVM.hpp
index ed040f4c6b4..cda10fd6b32 100644
--- a/Common/include/geometry/meshreader/CRectangularMeshReaderFVM.hpp
+++ b/Common/include/geometry/meshreader/CRectangularMeshReaderFVM.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CRectangularMeshReaderFVM.
  *        The implementations are in the <i>CRectangularMeshReaderFVM.cpp</i> file.
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/meshreader/CSU2ASCIIMeshReaderFVM.hpp b/Common/include/geometry/meshreader/CSU2ASCIIMeshReaderFVM.hpp
index a63f07a75d4..61a71be8493 100644
--- a/Common/include/geometry/meshreader/CSU2ASCIIMeshReaderFVM.hpp
+++ b/Common/include/geometry/meshreader/CSU2ASCIIMeshReaderFVM.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CSU2ASCIIMeshReaderFVM.
  *        The implementations are in the <i>CSU2ASCIIMeshReaderFVM.cpp</i> file.
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/primal_grid/CHexahedron.hpp b/Common/include/geometry/primal_grid/CHexahedron.hpp
index b6d2da966d1..f2bcc41cf27 100644
--- a/Common/include/geometry/primal_grid/CHexahedron.hpp
+++ b/Common/include/geometry/primal_grid/CHexahedron.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for storing the primal grid structure.
  *        The subroutines and functions are in the <i>CHexahedron.cpp</i> file.
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/primal_grid/CLine.hpp b/Common/include/geometry/primal_grid/CLine.hpp
index 49281694bc1..bafd3e5ea59 100644
--- a/Common/include/geometry/primal_grid/CLine.hpp
+++ b/Common/include/geometry/primal_grid/CLine.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for storing the primal grid structure.
  *        The subroutines and functions are in the <i>CLine.cpp</i> file.
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/primal_grid/CPrimalGrid.hpp b/Common/include/geometry/primal_grid/CPrimalGrid.hpp
index 5b5e2cdf9d3..2a27944b4d4 100644
--- a/Common/include/geometry/primal_grid/CPrimalGrid.hpp
+++ b/Common/include/geometry/primal_grid/CPrimalGrid.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for storing the primal grid structure.
  *        The subroutines and functions are in the <i>primal_grid_structure.cpp</i> file.
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/primal_grid/CPrimalGridBoundFEM.hpp b/Common/include/geometry/primal_grid/CPrimalGridBoundFEM.hpp
index e6dcf964fe9..d08e921b016 100644
--- a/Common/include/geometry/primal_grid/CPrimalGridBoundFEM.hpp
+++ b/Common/include/geometry/primal_grid/CPrimalGridBoundFEM.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for storing the primal grid structure.
  *        The subroutines and functions are in the <i>CPrimalGridBoundFEM.cpp</i> file.
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -33,7 +33,7 @@
 /*!
  * \class CPrimalGridBoundFEM
  * \brief Class to define primal grid boundary element for the FEM solver.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CPrimalGridBoundFEM final : public CPrimalGrid {
  private:
diff --git a/Common/include/geometry/primal_grid/CPrimalGridFEM.hpp b/Common/include/geometry/primal_grid/CPrimalGridFEM.hpp
index 8a12511c2fc..848ed24d890 100644
--- a/Common/include/geometry/primal_grid/CPrimalGridFEM.hpp
+++ b/Common/include/geometry/primal_grid/CPrimalGridFEM.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for storing the primal grid structure.
  *        The subroutines and functions are in the <i>CPrimalGridFEM.cpp</i> file.
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -34,7 +34,7 @@
 /*!
  * \class CPrimalGridFEM
  * \brief Class to define primal grid element for the FEM solver.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CPrimalGridFEM final : public CPrimalGrid {
  private:
diff --git a/Common/include/geometry/primal_grid/CPrism.hpp b/Common/include/geometry/primal_grid/CPrism.hpp
index 75322f6005c..4466c12b468 100644
--- a/Common/include/geometry/primal_grid/CPrism.hpp
+++ b/Common/include/geometry/primal_grid/CPrism.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for storing the primal grid structure.
  *        The subroutines and functions are in the <i>CPrism.cpp</i> file.
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/primal_grid/CPyramid.hpp b/Common/include/geometry/primal_grid/CPyramid.hpp
index d3da90aa269..028136c4f2f 100644
--- a/Common/include/geometry/primal_grid/CPyramid.hpp
+++ b/Common/include/geometry/primal_grid/CPyramid.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for storing the primal grid structure.
  *        The subroutines and functions are in the <i>CPyramid.cpp</i> file.
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/primal_grid/CQuadrilateral.hpp b/Common/include/geometry/primal_grid/CQuadrilateral.hpp
index 8d96240e3d3..435e46e64f2 100644
--- a/Common/include/geometry/primal_grid/CQuadrilateral.hpp
+++ b/Common/include/geometry/primal_grid/CQuadrilateral.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for storing the primal grid structure.
  *        The subroutines and functions are in the <i>CQuadrilateral.cpp</i> file.
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/primal_grid/CTetrahedron.hpp b/Common/include/geometry/primal_grid/CTetrahedron.hpp
index 17eab59670c..447db67d182 100644
--- a/Common/include/geometry/primal_grid/CTetrahedron.hpp
+++ b/Common/include/geometry/primal_grid/CTetrahedron.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for storing the primal grid structure.
  *        The subroutines and functions are in the <i>CTetrahedron.cpp</i> file.
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/primal_grid/CTriangle.hpp b/Common/include/geometry/primal_grid/CTriangle.hpp
index 9518af4c467..e4e785d0ee8 100644
--- a/Common/include/geometry/primal_grid/CTriangle.hpp
+++ b/Common/include/geometry/primal_grid/CTriangle.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for storing the primal grid structure.
  *        The subroutines and functions are in the <i>CTriangle.cpp</i> file.
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/geometry/primal_grid/CVertexMPI.hpp b/Common/include/geometry/primal_grid/CVertexMPI.hpp
index 04d55760940..a61b2dc1f93 100644
--- a/Common/include/geometry/primal_grid/CVertexMPI.hpp
+++ b/Common/include/geometry/primal_grid/CVertexMPI.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for storing the primal grid structure.
  *        The subroutines and functions are in the <i>primal_grid_structure.cpp</i> file.
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/graph_coloring_structure.hpp b/Common/include/graph_coloring_structure.hpp
index 1ad5103cf71..ae428f75554 100644
--- a/Common/include/graph_coloring_structure.hpp
+++ b/Common/include/graph_coloring_structure.hpp
@@ -4,7 +4,7 @@
  *        coloring of a given graph. The functions are in the
  *        <i>graph_coloring_structure.cpp</i> file.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -41,7 +41,7 @@ using namespace std;
  * \ingroup Graph
  * \brief Class, which provides distributed graph coloring algorithms.
  * \author: E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CGraphColoringStructure {
  public:
diff --git a/Common/include/grid_movement/CBSplineBlending.hpp b/Common/include/grid_movement/CBSplineBlending.hpp
index 6965d3d3965..09e2408b430 100644
--- a/Common/include/grid_movement/CBSplineBlending.hpp
+++ b/Common/include/grid_movement/CBSplineBlending.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the CBSplineBlending class.
  *        Defines blending using uniform BSplines
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/grid_movement/CBezierBlending.hpp b/Common/include/grid_movement/CBezierBlending.hpp
index dba2d8a9749..27a03064910 100644
--- a/Common/include/grid_movement/CBezierBlending.hpp
+++ b/Common/include/grid_movement/CBezierBlending.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the CBezierBlending class.
  *        Defines blending using Bernsteinpolynomials (Bezier Curves)
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/grid_movement/CFreeFormBlending.hpp b/Common/include/grid_movement/CFreeFormBlending.hpp
index f8e71ae2e68..7edd70c5724 100644
--- a/Common/include/grid_movement/CFreeFormBlending.hpp
+++ b/Common/include/grid_movement/CFreeFormBlending.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the CFreeFormBlending class.
  *        It is the parent class for the FFD blending function
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/grid_movement/CFreeFormDefBox.hpp b/Common/include/grid_movement/CFreeFormDefBox.hpp
index aca98e7a2ba..2513f067802 100644
--- a/Common/include/grid_movement/CFreeFormDefBox.hpp
+++ b/Common/include/grid_movement/CFreeFormDefBox.hpp
@@ -2,7 +2,7 @@
  * \file CFreeFormDefBox.hpp
  * \brief Headers of the CFreeFormDefBox class.
  * \author F. Palacios & A. Galdran.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/grid_movement/CGridMovement.hpp b/Common/include/grid_movement/CGridMovement.hpp
index e167dd58133..3429c10c6ce 100644
--- a/Common/include/grid_movement/CGridMovement.hpp
+++ b/Common/include/grid_movement/CGridMovement.hpp
@@ -2,7 +2,7 @@
  * \file CGridMovement.hpp
  * \brief Headers of the CGridMovement class
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/grid_movement/CSurfaceMovement.hpp b/Common/include/grid_movement/CSurfaceMovement.hpp
index bcee11a7ec2..0ef697e049d 100644
--- a/Common/include/grid_movement/CSurfaceMovement.hpp
+++ b/Common/include/grid_movement/CSurfaceMovement.hpp
@@ -2,7 +2,7 @@
  * \file CSurfaceMovement.hpp
  * \brief Headers of the CSurfaceMovement class.
  * \author F. Palacios, T. Economon.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/grid_movement/CVolumetricMovement.hpp b/Common/include/grid_movement/CVolumetricMovement.hpp
index 489f330d792..1520cb05829 100644
--- a/Common/include/grid_movement/CVolumetricMovement.hpp
+++ b/Common/include/grid_movement/CVolumetricMovement.hpp
@@ -2,7 +2,7 @@
  * \file CVolumetricMovement.hpp
  * \brief Headers of the CVolumetricMovement class.
  * \author F. Palacios, A. Bueno, T. Economon, S. Padron.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/interface_interpolation/CInterpolator.hpp b/Common/include/interface_interpolation/CInterpolator.hpp
index e3853ae91d9..2bbda6a2636 100644
--- a/Common/include/interface_interpolation/CInterpolator.hpp
+++ b/Common/include/interface_interpolation/CInterpolator.hpp
@@ -2,7 +2,7 @@
  * \file CInterpolator.hpp
  * \brief Base class for multiphysics interpolation.
  * \author H. Kline
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/interface_interpolation/CInterpolatorFactory.hpp b/Common/include/interface_interpolation/CInterpolatorFactory.hpp
index f5382127232..e4ef5850e5e 100644
--- a/Common/include/interface_interpolation/CInterpolatorFactory.hpp
+++ b/Common/include/interface_interpolation/CInterpolatorFactory.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file CInterpolatorFactory.hpp
  * \brief Factory to generate interpolator objects.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/interface_interpolation/CIsoparametric.hpp b/Common/include/interface_interpolation/CIsoparametric.hpp
index 7f1fc5e591a..190cb0a1e4b 100644
--- a/Common/include/interface_interpolation/CIsoparametric.hpp
+++ b/Common/include/interface_interpolation/CIsoparametric.hpp
@@ -2,7 +2,7 @@
  * \file CIsoparametric.hpp
  * \brief Isoparametric interpolation using FE shape functions.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/interface_interpolation/CMirror.hpp b/Common/include/interface_interpolation/CMirror.hpp
index c514d2097a6..46f7487629f 100644
--- a/Common/include/interface_interpolation/CMirror.hpp
+++ b/Common/include/interface_interpolation/CMirror.hpp
@@ -2,7 +2,7 @@
  * \file CMirror.hpp
  * \brief Mirror interpolation for the conservative (work-wise) approach in FSI problems.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/interface_interpolation/CNearestNeighbor.hpp b/Common/include/interface_interpolation/CNearestNeighbor.hpp
index 14c12a08e07..6977cf760a2 100644
--- a/Common/include/interface_interpolation/CNearestNeighbor.hpp
+++ b/Common/include/interface_interpolation/CNearestNeighbor.hpp
@@ -2,7 +2,7 @@
  * \file CNearestNeighbor.hpp
  * \brief Nearest Neighbor interpolation class.
  * \author H. Kline
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/interface_interpolation/CRadialBasisFunction.hpp b/Common/include/interface_interpolation/CRadialBasisFunction.hpp
index 601c96a232e..9b25a800388 100644
--- a/Common/include/interface_interpolation/CRadialBasisFunction.hpp
+++ b/Common/include/interface_interpolation/CRadialBasisFunction.hpp
@@ -2,7 +2,7 @@
  * \file CRadialBasisFunction.hpp
  * \brief Radial basis function interpolation.
  * \author Joel Ho, P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/interface_interpolation/CSlidingMesh.hpp b/Common/include/interface_interpolation/CSlidingMesh.hpp
index 571948870ff..fa9c26ecc8a 100644
--- a/Common/include/interface_interpolation/CSlidingMesh.hpp
+++ b/Common/include/interface_interpolation/CSlidingMesh.hpp
@@ -2,7 +2,7 @@
  * \file CSlidingMesh.hpp
  * \brief Sliding mesh interpolation.
  * \author H. Kline
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/linear_algebra/CMatrixVectorProduct.hpp b/Common/include/linear_algebra/CMatrixVectorProduct.hpp
index a3052d70d9b..bb3561a242b 100644
--- a/Common/include/linear_algebra/CMatrixVectorProduct.hpp
+++ b/Common/include/linear_algebra/CMatrixVectorProduct.hpp
@@ -3,7 +3,7 @@
  * \brief Headers for the classes related to sparse matrix-vector product wrappers.
  *        The actual operations are currently implemented mostly by CSysMatrix.
  * \author F. Palacios, J. Hicken, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/linear_algebra/CPastixWrapper.hpp b/Common/include/linear_algebra/CPastixWrapper.hpp
index 6001ec97e38..2f785315f39 100644
--- a/Common/include/linear_algebra/CPastixWrapper.hpp
+++ b/Common/include/linear_algebra/CPastixWrapper.hpp
@@ -3,7 +3,7 @@
  * \brief An interface to the INRIA solver PaStiX
  *        (http://pastix.gforge.inria.fr/files/README-txt.html)
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/linear_algebra/CPreconditioner.hpp b/Common/include/linear_algebra/CPreconditioner.hpp
index b142645ff1f..415bc90cfa0 100644
--- a/Common/include/linear_algebra/CPreconditioner.hpp
+++ b/Common/include/linear_algebra/CPreconditioner.hpp
@@ -3,7 +3,7 @@
  * \brief Classes related to linear preconditioner wrappers.
  *        The actual operations are currently implemented mostly by CSysMatrix.
  * \author F. Palacios, J. Hicken, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/linear_algebra/CSysMatrix.hpp b/Common/include/linear_algebra/CSysMatrix.hpp
index 3609c260f8f..6c75b487596 100644
--- a/Common/include/linear_algebra/CSysMatrix.hpp
+++ b/Common/include/linear_algebra/CSysMatrix.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration of the block-sparse matrix class.
  *        The implemtation is in <i>CSysMatrix.cpp</i>.
  * \author F. Palacios, A. Bueno, T. Economon, P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/linear_algebra/CSysMatrix.inl b/Common/include/linear_algebra/CSysMatrix.inl
index 9fe0626119c..cbe4b18d6ff 100644
--- a/Common/include/linear_algebra/CSysMatrix.inl
+++ b/Common/include/linear_algebra/CSysMatrix.inl
@@ -5,7 +5,7 @@
  *       of the .cpp file and so they are hidden to avoid triggering
  *       recompilation of other units when changes are made here.
  * \author F. Palacios, A. Bueno, T. Economon, P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/linear_algebra/CSysSolve.hpp b/Common/include/linear_algebra/CSysSolve.hpp
index c38f1bfd9ca..6df8fafa0b4 100644
--- a/Common/include/linear_algebra/CSysSolve.hpp
+++ b/Common/include/linear_algebra/CSysSolve.hpp
@@ -3,7 +3,7 @@
  * \brief Headers for the classes related to linear solvers (CG, FGMRES, etc)
  *        The subroutines and functions are in the <i>CSysSolve.cpp</i> file.
  * \author J. Hicken, F. Palacios, T. Economon, P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/linear_algebra/CSysSolve_b.hpp b/Common/include/linear_algebra/CSysSolve_b.hpp
index 22a91391a32..4abbf8c1ab2 100644
--- a/Common/include/linear_algebra/CSysSolve_b.hpp
+++ b/Common/include/linear_algebra/CSysSolve_b.hpp
@@ -2,7 +2,7 @@
  * \file CSysSolve_b.hpp
  * \brief Routines for the linear solver used in the reverse sweep of AD.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/linear_algebra/CSysVector.hpp b/Common/include/linear_algebra/CSysVector.hpp
index 2c20e1317b6..412f11c4427 100644
--- a/Common/include/linear_algebra/CSysVector.hpp
+++ b/Common/include/linear_algebra/CSysVector.hpp
@@ -3,7 +3,7 @@
  * \brief Declararion and inlines of the vector class used in the
  * solution of large, distributed, sparse linear systems.
  * \author P. Gomes, F. Palacios, J. Hicken, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/linear_algebra/blas_structure.hpp b/Common/include/linear_algebra/blas_structure.hpp
index 3cf8142e184..6e53f304767 100644
--- a/Common/include/linear_algebra/blas_structure.hpp
+++ b/Common/include/linear_algebra/blas_structure.hpp
@@ -4,7 +4,7 @@
           operations, which are typically found in the BLAS libraries.
           The functions are in the <i>blass_structure.cpp</i> file.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -41,7 +41,7 @@ class CConfig;
  * \ingroup BLAS
  * \brief Class, which serves as an interface to the BLAS functionalities needed.
  * \author: E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CBlasStructure {
  public:
diff --git a/Common/include/linear_algebra/vector_expressions.hpp b/Common/include/linear_algebra/vector_expressions.hpp
index e7883c4b5c7..5f0aa103547 100644
--- a/Common/include/linear_algebra/vector_expressions.hpp
+++ b/Common/include/linear_algebra/vector_expressions.hpp
@@ -2,7 +2,7 @@
  * \file vector_expressions.hpp
  * \brief Expression templates for vector types with coefficient-wise operations.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/option_structure.hpp b/Common/include/option_structure.hpp
index 0a5bdfc8205..c8181a3a13f 100644
--- a/Common/include/option_structure.hpp
+++ b/Common/include/option_structure.hpp
@@ -2,7 +2,7 @@
  * \file option_structure.hpp
  * \brief Defines classes for referencing options for easy input in CConfig
  * \author J. Hicken, B. Tracey
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/option_structure.inl b/Common/include/option_structure.inl
index 6cdc29d9656..ce94055fca5 100644
--- a/Common/include/option_structure.inl
+++ b/Common/include/option_structure.inl
@@ -3,7 +3,7 @@
  * \brief Template derived classes from COption, defined here as we
  *        only include them where needed to reduce compilation time.
  * \author J. Hicken, B. Tracey
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/parallelization/mpi_structure.cpp b/Common/include/parallelization/mpi_structure.cpp
index c55dc625eba..bdb92c65db2 100644
--- a/Common/include/parallelization/mpi_structure.cpp
+++ b/Common/include/parallelization/mpi_structure.cpp
@@ -2,7 +2,7 @@
  * \file mpi_structure.cpp
  * \brief Main subroutines for the mpi structures.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/parallelization/mpi_structure.hpp b/Common/include/parallelization/mpi_structure.hpp
index 470b8c4a479..6bce34788b4 100644
--- a/Common/include/parallelization/mpi_structure.hpp
+++ b/Common/include/parallelization/mpi_structure.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the mpi interface for generalized datatypes.
  *        The subroutines and functions are in the <i>mpi_structure.cpp</i> file.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/parallelization/omp_structure.cpp b/Common/include/parallelization/omp_structure.cpp
index f5848ca78e5..6e5161ea426 100644
--- a/Common/include/parallelization/omp_structure.cpp
+++ b/Common/include/parallelization/omp_structure.cpp
@@ -3,7 +3,7 @@
  * \brief Source file counterpart for omp_structure.hpp.
  * \note Contains OpDiLib initialization, finalization and includes the OpDiLib source file.
  * \author J. Blühdorn
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/parallelization/omp_structure.hpp b/Common/include/parallelization/omp_structure.hpp
index 60baa3e44dd..2ba94e99e2a 100644
--- a/Common/include/parallelization/omp_structure.hpp
+++ b/Common/include/parallelization/omp_structure.hpp
@@ -13,7 +13,7 @@
  *       defined here with suitable fallback versions to limit the spread of
  *       compiler tricks in other areas of the code.
  * \author P. Gomes, J. Blühdorn
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/parallelization/special_vectorization.hpp b/Common/include/parallelization/special_vectorization.hpp
index 1c980fd7229..722b6cd1346 100644
--- a/Common/include/parallelization/special_vectorization.hpp
+++ b/Common/include/parallelization/special_vectorization.hpp
@@ -2,7 +2,7 @@
  * \file special_vectorization.hpp
  * \brief Code generator header to create specializations of simd::Array.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/parallelization/vectorization.hpp b/Common/include/parallelization/vectorization.hpp
index eaabce00d41..dd904a5c1e3 100644
--- a/Common/include/parallelization/vectorization.hpp
+++ b/Common/include/parallelization/vectorization.hpp
@@ -2,7 +2,7 @@
  * \file vectorization.hpp
  * \brief Implementation of a portable SIMD type.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/C1DInterpolation.hpp b/Common/include/toolboxes/C1DInterpolation.hpp
index 5625a6f022e..8ca4d5c1b18 100644
--- a/Common/include/toolboxes/C1DInterpolation.hpp
+++ b/Common/include/toolboxes/C1DInterpolation.hpp
@@ -2,7 +2,7 @@
  * \file C1DInterpolation.hpp
  * \brief Classes for 1D interpolation.
  * \author Aman Baig, P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/CLinearPartitioner.hpp b/Common/include/toolboxes/CLinearPartitioner.hpp
index befb327c15a..0ebfb516aae 100644
--- a/Common/include/toolboxes/CLinearPartitioner.hpp
+++ b/Common/include/toolboxes/CLinearPartitioner.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CLinearPartitioner.
  *        The implementations are in the <i>CLinearPartitioner.cpp</i> file.
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/CQuasiNewtonInvLeastSquares.hpp b/Common/include/toolboxes/CQuasiNewtonInvLeastSquares.hpp
index e82b41298b9..e881f4c95bb 100644
--- a/Common/include/toolboxes/CQuasiNewtonInvLeastSquares.hpp
+++ b/Common/include/toolboxes/CQuasiNewtonInvLeastSquares.hpp
@@ -7,7 +7,7 @@
  * \note Based on the IQN-ILS method, see DOI 10.1007/s11831-013-9085-5 and
  * references therein.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/CSquareMatrixCM.hpp b/Common/include/toolboxes/CSquareMatrixCM.hpp
index 178417fe92f..2ba3f60de7c 100644
--- a/Common/include/toolboxes/CSquareMatrixCM.hpp
+++ b/Common/include/toolboxes/CSquareMatrixCM.hpp
@@ -3,7 +3,7 @@
  * \brief Dense general square matrix, used for example in DG standard elements
  *        in Column Major order storage.
  * \author Edwin van der Weide, Pedro Gomes.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/CSymmetricMatrix.hpp b/Common/include/toolboxes/CSymmetricMatrix.hpp
index 2dee2893e34..8b229a4b526 100644
--- a/Common/include/toolboxes/CSymmetricMatrix.hpp
+++ b/Common/include/toolboxes/CSymmetricMatrix.hpp
@@ -2,7 +2,7 @@
  * \file CSymmetricMatrix.hpp
  * \brief Dense symmetric matrix, used for example in RBF interpolation.
  * \author Joel Ho, P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CIncTGVSolution.hpp b/Common/include/toolboxes/MMS/CIncTGVSolution.hpp
index 2885cf863f0..677f78448e9 100644
--- a/Common/include/toolboxes/MMS/CIncTGVSolution.hpp
+++ b/Common/include/toolboxes/MMS/CIncTGVSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CIncTGVSolution.
  *        The implementations are in the <i>CIncTGVSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CInviscidVortexSolution.hpp b/Common/include/toolboxes/MMS/CInviscidVortexSolution.hpp
index f440ad9aac0..e9aaa812e28 100644
--- a/Common/include/toolboxes/MMS/CInviscidVortexSolution.hpp
+++ b/Common/include/toolboxes/MMS/CInviscidVortexSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CInviscidVortexSolution.
  *        The implementations are in the <i>CInviscidVortexSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CMMSIncEulerSolution.hpp b/Common/include/toolboxes/MMS/CMMSIncEulerSolution.hpp
index eb71b4c5a61..69f8906b808 100644
--- a/Common/include/toolboxes/MMS/CMMSIncEulerSolution.hpp
+++ b/Common/include/toolboxes/MMS/CMMSIncEulerSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CMMSIncEulerSolution.
  *        The implementations are in the <i>CMMSIncEulerSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CMMSIncNSSolution.hpp b/Common/include/toolboxes/MMS/CMMSIncNSSolution.hpp
index 51cc3e630d9..3626b9ac6f4 100644
--- a/Common/include/toolboxes/MMS/CMMSIncNSSolution.hpp
+++ b/Common/include/toolboxes/MMS/CMMSIncNSSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CMMSIncNSSolution.
  *        The implementations are in the <i>CMMSIncNSSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.hpp b/Common/include/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.hpp
index acb9fa3a796..f8b5599a193 100644
--- a/Common/include/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.hpp
+++ b/Common/include/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CMMSNSTwoHalfCirclesSolution.
  *        The implementations are in the <i>CMMSNSTwoHalfCirclesSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.hpp b/Common/include/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.hpp
index f879b3dc177..92d03efbe5b 100644
--- a/Common/include/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.hpp
+++ b/Common/include/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CMMSNSTwoHalfSpheresSolution.
  *        The implementations are in the <i>CMMSNSTwoHalfSpheresSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolution.hpp b/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolution.hpp
index 387fa5c78b7..fbdc6a8f82e 100644
--- a/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolution.hpp
+++ b/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CMMSNSUnitQuadSolution.
  *        The implementations are in the <i>CMMSNSUnitQuadSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.hpp b/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.hpp
index ba2135bb343..c3b5a3e508c 100644
--- a/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.hpp
+++ b/Common/include/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CMMSNSUnitQuadSolutionWallBC.
  *        The implementations are in the <i>CMMSNSUnitQuadSolutionWallBC.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CNSUnitQuadSolution.hpp b/Common/include/toolboxes/MMS/CNSUnitQuadSolution.hpp
index 2d5bd8eac48..32f9f2d4263 100644
--- a/Common/include/toolboxes/MMS/CNSUnitQuadSolution.hpp
+++ b/Common/include/toolboxes/MMS/CNSUnitQuadSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CNSUnitQuadSolution.hpp.
  *        The implementations are in the <i>CNSUnitQuadSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CRinglebSolution.hpp b/Common/include/toolboxes/MMS/CRinglebSolution.hpp
index 889b9729801..2c1ede87c0a 100644
--- a/Common/include/toolboxes/MMS/CRinglebSolution.hpp
+++ b/Common/include/toolboxes/MMS/CRinglebSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CRinglebSolution.hpp.
  *        The implementations are in the <i>CRinglebSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CTGVSolution.hpp b/Common/include/toolboxes/MMS/CTGVSolution.hpp
index f40b22fe530..914b34a5e1c 100644
--- a/Common/include/toolboxes/MMS/CTGVSolution.hpp
+++ b/Common/include/toolboxes/MMS/CTGVSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CTGVSolution.
  *        The implementations are in the <i>CTGVSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CUserDefinedSolution.hpp b/Common/include/toolboxes/MMS/CUserDefinedSolution.hpp
index d2b28861e0f..7a6d7c74ecc 100644
--- a/Common/include/toolboxes/MMS/CUserDefinedSolution.hpp
+++ b/Common/include/toolboxes/MMS/CUserDefinedSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CUserDefinedSolution.
  *        The implementations are in the <i>CUserDefinedSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/MMS/CVerificationSolution.hpp b/Common/include/toolboxes/MMS/CVerificationSolution.hpp
index 0802409dbc4..6fe6f849274 100644
--- a/Common/include/toolboxes/MMS/CVerificationSolution.hpp
+++ b/Common/include/toolboxes/MMS/CVerificationSolution.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the base class CVerificationSolution.
  *        The implementations are in the <i>CVerificationSolution.cpp</i> file.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/allocation_toolbox.hpp b/Common/include/toolboxes/allocation_toolbox.hpp
index 2b0adb1f31a..5f88eb3098b 100644
--- a/Common/include/toolboxes/allocation_toolbox.hpp
+++ b/Common/include/toolboxes/allocation_toolbox.hpp
@@ -5,7 +5,7 @@
  * \note  These are "kernel" functions, only to be used with good reason,
  *        always try to use higher level container classes.
  * \author P. Gomes, D. Kavolis
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/geometry_toolbox.hpp b/Common/include/toolboxes/geometry_toolbox.hpp
index c61ba413af0..05cfdbc62fb 100644
--- a/Common/include/toolboxes/geometry_toolbox.hpp
+++ b/Common/include/toolboxes/geometry_toolbox.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file geometry_toolbox.hpp
  * \brief Collection of common lightweight geometry-oriented methods.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/graph_toolbox.hpp b/Common/include/toolboxes/graph_toolbox.hpp
index 0a57ec21fd0..c5929e8f8da 100644
--- a/Common/include/toolboxes/graph_toolbox.hpp
+++ b/Common/include/toolboxes/graph_toolbox.hpp
@@ -2,7 +2,7 @@
  * \file graph_toolbox.hpp
  * \brief Functions and classes to build/represent sparse graphs or sparse patterns.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/ndflattener.hpp b/Common/include/toolboxes/ndflattener.hpp
index 6e9a616a0e2..16d5b1f02e9 100644
--- a/Common/include/toolboxes/ndflattener.hpp
+++ b/Common/include/toolboxes/ndflattener.hpp
@@ -2,7 +2,7 @@
  * \file ndflattener.hpp
  * \brief Flatten pointer-to-pointer-... arrays for MPI communication
  * \author M. Aehle
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/toolboxes/printing_toolbox.hpp b/Common/include/toolboxes/printing_toolbox.hpp
index 47470ccb163..5ede8972166 100644
--- a/Common/include/toolboxes/printing_toolbox.hpp
+++ b/Common/include/toolboxes/printing_toolbox.hpp
@@ -2,7 +2,7 @@
  * \file printing_toolbox.hpp
  * \brief Header file for the printing toolbox.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/include/wall_model.hpp b/Common/include/wall_model.hpp
index b80f9dfcedd..4d7a73224c3 100644
--- a/Common/include/wall_model.hpp
+++ b/Common/include/wall_model.hpp
@@ -2,7 +2,7 @@
  * \file wall_model.hpp
  * \brief Headers for the wall model functions for large eddy simulations.
  * \author E. van der Weide, T. Economon, P. Urbanczyk
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -42,7 +42,7 @@ class CFluidModel;
  * \class CWallModel
  * \brief Base class for defining the LES wall model.
  * \author: E. van der Weide, T. Economon, P. Urbanczyk
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CWallModel {
  public:
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
index 42329dc979d..f660ec5633d 100644
--- a/Common/src/CConfig.cpp
+++ b/Common/src/CConfig.cpp
@@ -2,7 +2,7 @@
  * \file CConfig.cpp
  * \brief Main file for managing the config file
  * \author F. Palacios, T. Economon, B. Tracey, H. Kline
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -3230,7 +3230,7 @@ void CConfig::SetHeader(SU2_COMPONENT val_software) const{
     cout << "\n";
     cout << "-------------------------------------------------------------------------\n";
     cout << "|    ___ _   _ ___                                                      |\n";
-    cout << "|   / __| | | |_  )   Release 7.5.1 \"Blackbird\"                         |\n";
+    cout << "|   / __| | | |_  )   Release 8.0.0 \"Harrier\"                           |\n";
     cout << "|   \\__ \\ |_| |/ /                                                      |\n";
     switch (val_software) {
     case SU2_COMPONENT::SU2_CFD: cout << "|   |___/\\___//___|   Suite (Computational Fluid Dynamics Code)         |\n"; break;
diff --git a/Common/src/adt/CADTBaseClass.cpp b/Common/src/adt/CADTBaseClass.cpp
index 0a063275541..8af4742badf 100644
--- a/Common/src/adt/CADTBaseClass.cpp
+++ b/Common/src/adt/CADTBaseClass.cpp
@@ -2,7 +2,7 @@
  * \file CADTBaseClass.cpp
  * \brief Base class for storing an ADT in an arbitrary number of dimensions.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/adt/CADTElemClass.cpp b/Common/src/adt/CADTElemClass.cpp
index 72659d0fad6..22dba4c5e5e 100644
--- a/Common/src/adt/CADTElemClass.cpp
+++ b/Common/src/adt/CADTElemClass.cpp
@@ -2,7 +2,7 @@
  * \file CADTElemClass.cpp
  * \brief Class for storing an ADT of (linear) elements in an arbitrary number of dimensions.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/adt/CADTPointsOnlyClass.cpp b/Common/src/adt/CADTPointsOnlyClass.cpp
index c03e07dafbf..75062ba722b 100644
--- a/Common/src/adt/CADTPointsOnlyClass.cpp
+++ b/Common/src/adt/CADTPointsOnlyClass.cpp
@@ -2,7 +2,7 @@
  * \file CADTPointsOnlyClass.cpp
  * \brief Class for storing an ADT of only points in an arbitrary number of dimensions.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/basic_types/ad_structure.cpp b/Common/src/basic_types/ad_structure.cpp
index 4da61b9c57b..c5d2ddd34e4 100644
--- a/Common/src/basic_types/ad_structure.cpp
+++ b/Common/src/basic_types/ad_structure.cpp
@@ -2,7 +2,7 @@
  * \file ad_structure.cpp
  * \brief Main subroutines for the algorithmic differentiation (AD) structure.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/containers/CFileReaderLUT.cpp b/Common/src/containers/CFileReaderLUT.cpp
index 31bb8de3338..0e1b6d569c0 100644
--- a/Common/src/containers/CFileReaderLUT.cpp
+++ b/Common/src/containers/CFileReaderLUT.cpp
@@ -2,7 +2,7 @@
  * \file CFileReaderLUT.cpp
  * \brief reading lookup table for tabulated fluid properties
  * \author D. Mayer, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/containers/CLookUpTable.cpp b/Common/src/containers/CLookUpTable.cpp
index bff408de8d0..6ec0ff247f5 100644
--- a/Common/src/containers/CLookUpTable.cpp
+++ b/Common/src/containers/CLookUpTable.cpp
@@ -2,7 +2,7 @@
  * \file CLookupTable.cpp
  * \brief tabulation of fluid properties
  * \author D. Mayer, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/containers/CTrapezoidalMap.cpp b/Common/src/containers/CTrapezoidalMap.cpp
index 4bb943768fd..0f964030748 100644
--- a/Common/src/containers/CTrapezoidalMap.cpp
+++ b/Common/src/containers/CTrapezoidalMap.cpp
@@ -2,7 +2,7 @@
  * \file CTrapezoidalMap.cpp
  * \brief Implementation of the trapezoidal map for tabulation and lookup of fluid properties
  * \author D. Mayer, T. Economon, N. Beishuizen
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/fem/fem_cgns_elements.cpp b/Common/src/fem/fem_cgns_elements.cpp
index 876793af42e..746830ad1c6 100644
--- a/Common/src/fem/fem_cgns_elements.cpp
+++ b/Common/src/fem/fem_cgns_elements.cpp
@@ -2,7 +2,7 @@
  * \file fem_cgns_elements.cpp
  * \brief CGNS element definitions and conversions to the SU2 standard.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/fem/fem_gauss_jacobi_quadrature.cpp b/Common/src/fem/fem_gauss_jacobi_quadrature.cpp
index d7c3c06d74a..f8c1054ea30 100644
--- a/Common/src/fem/fem_gauss_jacobi_quadrature.cpp
+++ b/Common/src/fem/fem_gauss_jacobi_quadrature.cpp
@@ -4,7 +4,7 @@
           quadrature rules. All the functions in this file are based on the
           program JACOBI_RULE of John Burkardt.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/fem/fem_geometry_structure.cpp b/Common/src/fem/fem_geometry_structure.cpp
index 1cc219596f3..a9b92bf0a6d 100644
--- a/Common/src/fem/fem_geometry_structure.cpp
+++ b/Common/src/fem/fem_geometry_structure.cpp
@@ -2,7 +2,7 @@
  * \file fem_geometry_structure.cpp
  * \brief Functions for creating the primal grid for the FEM solver.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/fem/fem_integration_rules.cpp b/Common/src/fem/fem_integration_rules.cpp
index 0766466cad7..ff8bdf19a25 100644
--- a/Common/src/fem/fem_integration_rules.cpp
+++ b/Common/src/fem/fem_integration_rules.cpp
@@ -2,7 +2,7 @@
  * \file fem_integration_rules.cpp
  * \brief FEM integration rules for the standard elements.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/fem/fem_standard_element.cpp b/Common/src/fem/fem_standard_element.cpp
index 4ffc791cfad..e9604a11200 100644
--- a/Common/src/fem/fem_standard_element.cpp
+++ b/Common/src/fem/fem_standard_element.cpp
@@ -2,7 +2,7 @@
  * \file fem_standard_element.cpp
  * \brief Functions for the FEM standard elements.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/fem/fem_wall_distance.cpp b/Common/src/fem/fem_wall_distance.cpp
index cd9920927e3..e95cc8506ff 100644
--- a/Common/src/fem/fem_wall_distance.cpp
+++ b/Common/src/fem/fem_wall_distance.cpp
@@ -2,7 +2,7 @@
  * \file fem_wall_distance.cpp
  * \brief Main subroutines for computing the wall distance for the FEM solver.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/fem/fem_work_estimate_metis.cpp b/Common/src/fem/fem_work_estimate_metis.cpp
index e00f89bf98f..50d50db4d80 100644
--- a/Common/src/fem/fem_work_estimate_metis.cpp
+++ b/Common/src/fem/fem_work_estimate_metis.cpp
@@ -3,7 +3,7 @@
  * \brief This file contains the implementation of the member functions WorkEstimateMetis
           for the FEM standard elements.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/fem/geometry_structure_fem_part.cpp b/Common/src/fem/geometry_structure_fem_part.cpp
index 929abe37abe..ce4fbfa9621 100644
--- a/Common/src/fem/geometry_structure_fem_part.cpp
+++ b/Common/src/fem/geometry_structure_fem_part.cpp
@@ -2,7 +2,7 @@
  * \file geometry_structure_fem_part.cpp
  * \brief Main subroutines for distributin the grid for the Fluid FEM solver.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/CDummyGeometry.cpp b/Common/src/geometry/CDummyGeometry.cpp
index 44f820d8877..1fba711ee64 100644
--- a/Common/src/geometry/CDummyGeometry.cpp
+++ b/Common/src/geometry/CDummyGeometry.cpp
@@ -2,7 +2,7 @@
  * \file CDummyGeometry.hpp
  * \brief Implementation of the dummy geometry class used in "dry run" mode.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/CGeometry.cpp b/Common/src/geometry/CGeometry.cpp
index 9d526f45ebd..9ed1804186a 100644
--- a/Common/src/geometry/CGeometry.cpp
+++ b/Common/src/geometry/CGeometry.cpp
@@ -2,7 +2,7 @@
  * \file CGeometry.cpp
  * \brief Implementation of the base geometry class.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/CMultiGridGeometry.cpp b/Common/src/geometry/CMultiGridGeometry.cpp
index 87b97af6a2f..37b1bd175ba 100644
--- a/Common/src/geometry/CMultiGridGeometry.cpp
+++ b/Common/src/geometry/CMultiGridGeometry.cpp
@@ -2,7 +2,7 @@
  * \file CMultiGridGeometry.cpp
  * \brief Implementation of the multigrid geometry class.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/CMultiGridQueue.cpp b/Common/src/geometry/CMultiGridQueue.cpp
index 8fda68fa507..7ae01c60af3 100644
--- a/Common/src/geometry/CMultiGridQueue.cpp
+++ b/Common/src/geometry/CMultiGridQueue.cpp
@@ -2,7 +2,7 @@
  * \file CMultiGridQueue.cpp
  * \brief Implementation of the multigrid queue class for the FVM solver.
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/CPhysicalGeometry.cpp b/Common/src/geometry/CPhysicalGeometry.cpp
index 917894f4bf3..54d667e0fbd 100644
--- a/Common/src/geometry/CPhysicalGeometry.cpp
+++ b/Common/src/geometry/CPhysicalGeometry.cpp
@@ -2,7 +2,7 @@
  * \file CPhysicalGeometry.cpp
  * \brief Implementation of the physical geometry class.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/dual_grid/CDualGrid.cpp b/Common/src/geometry/dual_grid/CDualGrid.cpp
index 99813fab93f..4019695ed9d 100644
--- a/Common/src/geometry/dual_grid/CDualGrid.cpp
+++ b/Common/src/geometry/dual_grid/CDualGrid.cpp
@@ -2,7 +2,7 @@
  * \file CDualGrid.cpp
  * \brief Main classes for defining the dual grid
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/dual_grid/CEdge.cpp b/Common/src/geometry/dual_grid/CEdge.cpp
index 5b3197d3f2f..92cf493e36f 100644
--- a/Common/src/geometry/dual_grid/CEdge.cpp
+++ b/Common/src/geometry/dual_grid/CEdge.cpp
@@ -2,7 +2,7 @@
  * \file CEdge.cpp
  * \brief Implementation of the edge class.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/dual_grid/CPoint.cpp b/Common/src/geometry/dual_grid/CPoint.cpp
index 190bf7ad69a..e47de05486c 100644
--- a/Common/src/geometry/dual_grid/CPoint.cpp
+++ b/Common/src/geometry/dual_grid/CPoint.cpp
@@ -2,7 +2,7 @@
  * \file CPoint.cpp
  * \brief Main classes for defining the points of the dual grid
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/dual_grid/CTurboVertex.cpp b/Common/src/geometry/dual_grid/CTurboVertex.cpp
index 4c19dd2bf21..8a036cd90aa 100644
--- a/Common/src/geometry/dual_grid/CTurboVertex.cpp
+++ b/Common/src/geometry/dual_grid/CTurboVertex.cpp
@@ -2,7 +2,7 @@
  * \file CTurboVertex.cpp
  * \brief Main classes for defining the turbo vertices of the dual grid
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/dual_grid/CVertex.cpp b/Common/src/geometry/dual_grid/CVertex.cpp
index 844245759ab..1879f66106f 100644
--- a/Common/src/geometry/dual_grid/CVertex.cpp
+++ b/Common/src/geometry/dual_grid/CVertex.cpp
@@ -2,7 +2,7 @@
  * \file CVertex.cpp
  * \brief Main classes for defining the vertices of the dual grid
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/elements/CElement.cpp b/Common/src/geometry/elements/CElement.cpp
index 2c4c5dd38a3..70ef29f8811 100644
--- a/Common/src/geometry/elements/CElement.cpp
+++ b/Common/src/geometry/elements/CElement.cpp
@@ -2,7 +2,7 @@
  * \file CElement.cpp
  * \brief Definition of the Finite Element structure (elements)
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/elements/CHEXA8.cpp b/Common/src/geometry/elements/CHEXA8.cpp
index fee133c71fe..fdc2c8773c8 100644
--- a/Common/src/geometry/elements/CHEXA8.cpp
+++ b/Common/src/geometry/elements/CHEXA8.cpp
@@ -2,7 +2,7 @@
  * \file CHEXA8.cpp
  * \brief Definition of 8-node hexa element with 8 Gauss points.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/elements/CLINE.cpp b/Common/src/geometry/elements/CLINE.cpp
index d2dd6dd66fd..77365707589 100644
--- a/Common/src/geometry/elements/CLINE.cpp
+++ b/Common/src/geometry/elements/CLINE.cpp
@@ -2,7 +2,7 @@
  * \file CLINE.cpp
  * \brief Definition of the 2-node line element with two Gauss points.
  * \author T. Dick
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/elements/CPRISM6.cpp b/Common/src/geometry/elements/CPRISM6.cpp
index 111c771c8b7..6e672a41334 100644
--- a/Common/src/geometry/elements/CPRISM6.cpp
+++ b/Common/src/geometry/elements/CPRISM6.cpp
@@ -2,7 +2,7 @@
  * \file CPRISM6.cpp
  * \brief Definition of the 6-node triangular prism element with 6 Gauss points.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/elements/CPYRAM5.cpp b/Common/src/geometry/elements/CPYRAM5.cpp
index c82d1dbbfeb..9bf8ac96947 100644
--- a/Common/src/geometry/elements/CPYRAM5.cpp
+++ b/Common/src/geometry/elements/CPYRAM5.cpp
@@ -2,7 +2,7 @@
  * \file CPYRAM5.cpp
  * \brief Definition of 5-node pyramid element with 5 Gauss points.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/elements/CPYRAM6.cpp b/Common/src/geometry/elements/CPYRAM6.cpp
index d152598b594..a216fee8dc4 100644
--- a/Common/src/geometry/elements/CPYRAM6.cpp
+++ b/Common/src/geometry/elements/CPYRAM6.cpp
@@ -2,7 +2,7 @@
  * \file CPYRAM6.cpp
  * \brief Definition of 5-node pyramid element with 6 Gauss points.
  * \author T.Dick
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/elements/CQUAD4.cpp b/Common/src/geometry/elements/CQUAD4.cpp
index 628700ed0b7..ab8a2db37bc 100644
--- a/Common/src/geometry/elements/CQUAD4.cpp
+++ b/Common/src/geometry/elements/CQUAD4.cpp
@@ -2,7 +2,7 @@
  * \file CQUAD4.cpp
  * \brief Definition of the 4-node quadrilateral element with 4 Gauss points.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/elements/CTETRA1.cpp b/Common/src/geometry/elements/CTETRA1.cpp
index 1d937ef56ce..e6b5e8ca395 100644
--- a/Common/src/geometry/elements/CTETRA1.cpp
+++ b/Common/src/geometry/elements/CTETRA1.cpp
@@ -2,7 +2,7 @@
  * \file CTETRA1.cpp
  * \brief Definition of 4-node tetra element with 1 Gauss point.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/elements/CTETRA4.cpp b/Common/src/geometry/elements/CTETRA4.cpp
index 614d0352c29..5138a159ebf 100644
--- a/Common/src/geometry/elements/CTETRA4.cpp
+++ b/Common/src/geometry/elements/CTETRA4.cpp
@@ -2,7 +2,7 @@
  * \file CTETRA4.cpp
  * \brief Definition of 4-node tetrahedral element with 4 Gauss point.
  * \author T. Dick
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/elements/CTRIA1.cpp b/Common/src/geometry/elements/CTRIA1.cpp
index f845f2634fb..e21b31e14cd 100644
--- a/Common/src/geometry/elements/CTRIA1.cpp
+++ b/Common/src/geometry/elements/CTRIA1.cpp
@@ -2,7 +2,7 @@
  * \file CTRIA1.cpp
  * \brief Definition of the 3-node triangular element with one Gauss point.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/elements/CTRIA3.cpp b/Common/src/geometry/elements/CTRIA3.cpp
index f9856113e4a..10414b03135 100644
--- a/Common/src/geometry/elements/CTRIA3.cpp
+++ b/Common/src/geometry/elements/CTRIA3.cpp
@@ -2,7 +2,7 @@
  * \file CTRIA3.cpp
  * \brief Definition of the 3-node triangular element with three Gauss points.
  * \author T. Dick
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/meshreader/CBoxMeshReaderFVM.cpp b/Common/src/geometry/meshreader/CBoxMeshReaderFVM.cpp
index 6c14dc3a064..edb0ff5ed6f 100644
--- a/Common/src/geometry/meshreader/CBoxMeshReaderFVM.cpp
+++ b/Common/src/geometry/meshreader/CBoxMeshReaderFVM.cpp
@@ -3,7 +3,7 @@
  * \brief Reads a 3D box grid into linear partitions for the
  *        finite volume solver (FVM).
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/meshreader/CCGNSMeshReaderFVM.cpp b/Common/src/geometry/meshreader/CCGNSMeshReaderFVM.cpp
index 2d8db05e9c8..a4dc472ee99 100644
--- a/Common/src/geometry/meshreader/CCGNSMeshReaderFVM.cpp
+++ b/Common/src/geometry/meshreader/CCGNSMeshReaderFVM.cpp
@@ -3,7 +3,7 @@
  * \brief Class that reads a single zone of a CGNS mesh file from disk into
  *        linear partitions across all ranks.
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/meshreader/CMeshReaderFVM.cpp b/Common/src/geometry/meshreader/CMeshReaderFVM.cpp
index 23a23db1d87..d0d2b3ab243 100644
--- a/Common/src/geometry/meshreader/CMeshReaderFVM.cpp
+++ b/Common/src/geometry/meshreader/CMeshReaderFVM.cpp
@@ -3,7 +3,7 @@
  * \brief Helper class that provides the counts for each rank in a linear
  *        partitioning given the global count as input.
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/meshreader/CRectangularMeshReaderFVM.cpp b/Common/src/geometry/meshreader/CRectangularMeshReaderFVM.cpp
index 5b312489b74..b14a2ded97b 100644
--- a/Common/src/geometry/meshreader/CRectangularMeshReaderFVM.cpp
+++ b/Common/src/geometry/meshreader/CRectangularMeshReaderFVM.cpp
@@ -3,7 +3,7 @@
  * \brief Reads a 2D rectangular grid into linear partitions for the
  *        finite volume solver (FVM).
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/meshreader/CSU2ASCIIMeshReaderFVM.cpp b/Common/src/geometry/meshreader/CSU2ASCIIMeshReaderFVM.cpp
index a32c290c4d9..65daf489737 100644
--- a/Common/src/geometry/meshreader/CSU2ASCIIMeshReaderFVM.cpp
+++ b/Common/src/geometry/meshreader/CSU2ASCIIMeshReaderFVM.cpp
@@ -3,7 +3,7 @@
  * \brief Reads a native SU2 ASCII grid into linear partitions for the
  *        finite volume solver (FVM).
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/primal_grid/CHexahedron.cpp b/Common/src/geometry/primal_grid/CHexahedron.cpp
index a4f7f7cf918..ea428ba4e8e 100644
--- a/Common/src/geometry/primal_grid/CHexahedron.cpp
+++ b/Common/src/geometry/primal_grid/CHexahedron.cpp
@@ -2,7 +2,7 @@
  * \file CHexahedron.cpp
  * \brief Main classes for defining the primal grid elements
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/primal_grid/CLine.cpp b/Common/src/geometry/primal_grid/CLine.cpp
index c3d0d7c26c3..b12156fdb80 100644
--- a/Common/src/geometry/primal_grid/CLine.cpp
+++ b/Common/src/geometry/primal_grid/CLine.cpp
@@ -2,7 +2,7 @@
  * \file CLine.cpp
  * \brief Main classes for defining the primal grid elements
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/primal_grid/CPrimalGrid.cpp b/Common/src/geometry/primal_grid/CPrimalGrid.cpp
index 94269844044..0469f88e002 100644
--- a/Common/src/geometry/primal_grid/CPrimalGrid.cpp
+++ b/Common/src/geometry/primal_grid/CPrimalGrid.cpp
@@ -2,7 +2,7 @@
  * \file CPrimalGrid.cpp
  * \brief Main classes for defining the primal grid elements
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/primal_grid/CPrimalGridBoundFEM.cpp b/Common/src/geometry/primal_grid/CPrimalGridBoundFEM.cpp
index f748cf6b298..7590322ff59 100644
--- a/Common/src/geometry/primal_grid/CPrimalGridBoundFEM.cpp
+++ b/Common/src/geometry/primal_grid/CPrimalGridBoundFEM.cpp
@@ -2,7 +2,7 @@
  * \file CPrimalGridBoundFEM.cpp
  * \brief Main classes for defining the primal grid elements
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/primal_grid/CPrimalGridFEM.cpp b/Common/src/geometry/primal_grid/CPrimalGridFEM.cpp
index 75d12b9067f..fead2a175e7 100644
--- a/Common/src/geometry/primal_grid/CPrimalGridFEM.cpp
+++ b/Common/src/geometry/primal_grid/CPrimalGridFEM.cpp
@@ -2,7 +2,7 @@
  * \file CPrimalGridFEM.cpp
  * \brief Main classes for defining the primal grid elements
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/primal_grid/CPrism.cpp b/Common/src/geometry/primal_grid/CPrism.cpp
index 72726ab08be..4b39798dabb 100644
--- a/Common/src/geometry/primal_grid/CPrism.cpp
+++ b/Common/src/geometry/primal_grid/CPrism.cpp
@@ -2,7 +2,7 @@
  * \file CPrism.cpp
  * \brief Main classes for defining the primal grid elements
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/primal_grid/CPyramid.cpp b/Common/src/geometry/primal_grid/CPyramid.cpp
index 38baeaae45e..76c4b28d77f 100644
--- a/Common/src/geometry/primal_grid/CPyramid.cpp
+++ b/Common/src/geometry/primal_grid/CPyramid.cpp
@@ -2,7 +2,7 @@
  * \file CPyramid.cpp
  * \brief Main classes for defining the primal grid elements
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/primal_grid/CQuadrilateral.cpp b/Common/src/geometry/primal_grid/CQuadrilateral.cpp
index fab0b7a280a..7e3372524fd 100644
--- a/Common/src/geometry/primal_grid/CQuadrilateral.cpp
+++ b/Common/src/geometry/primal_grid/CQuadrilateral.cpp
@@ -2,7 +2,7 @@
  * \file CQuadrilateral.cpp
  * \brief Main classes for defining the primal grid elements
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/primal_grid/CTetrahedron.cpp b/Common/src/geometry/primal_grid/CTetrahedron.cpp
index 78a9ae6de17..83a8c849b11 100644
--- a/Common/src/geometry/primal_grid/CTetrahedron.cpp
+++ b/Common/src/geometry/primal_grid/CTetrahedron.cpp
@@ -2,7 +2,7 @@
  * \file CTetrahedron.cpp
  * \brief Main classes for defining the primal grid elements
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/primal_grid/CTriangle.cpp b/Common/src/geometry/primal_grid/CTriangle.cpp
index 36370731c4d..2228cfc301f 100644
--- a/Common/src/geometry/primal_grid/CTriangle.cpp
+++ b/Common/src/geometry/primal_grid/CTriangle.cpp
@@ -2,7 +2,7 @@
  * \file CTriangle.cpp
  * \brief Main classes for defining the primal grid elements
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/geometry/primal_grid/CVertexMPI.cpp b/Common/src/geometry/primal_grid/CVertexMPI.cpp
index 0de612a88bf..04baff89669 100644
--- a/Common/src/geometry/primal_grid/CVertexMPI.cpp
+++ b/Common/src/geometry/primal_grid/CVertexMPI.cpp
@@ -2,7 +2,7 @@
  * \file CVertexMPI.cpp
  * \brief Main classes for defining the primal grid elements
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/graph_coloring_structure.cpp b/Common/src/graph_coloring_structure.cpp
index 16755851014..bdace7733b4 100644
--- a/Common/src/graph_coloring_structure.cpp
+++ b/Common/src/graph_coloring_structure.cpp
@@ -2,7 +2,7 @@
  * \file graph_coloring_structure.cpp
  * \brief Functions used to carry out the coloring of a given graph.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/grid_movement/CBSplineBlending.cpp b/Common/src/grid_movement/CBSplineBlending.cpp
index 29a1dda3f73..e5b38aab3fa 100644
--- a/Common/src/grid_movement/CBSplineBlending.cpp
+++ b/Common/src/grid_movement/CBSplineBlending.cpp
@@ -2,7 +2,7 @@
  * \file CBSplineBlending.cpp
  * \brief Subroutines for B-Spline blening for FFDs
  * \author F. Palacios, T. Economon, S. Padron
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/grid_movement/CBezierBlending.cpp b/Common/src/grid_movement/CBezierBlending.cpp
index 0d8feebc645..ceabd8eb51f 100644
--- a/Common/src/grid_movement/CBezierBlending.cpp
+++ b/Common/src/grid_movement/CBezierBlending.cpp
@@ -2,7 +2,7 @@
  * \file CBezierBlending.cpp
  * \brief Subroutines for Bezier blending for FFDs
  * \author F. Palacios, T. Economon, S. Padron
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/grid_movement/CFreeFormBlending.cpp b/Common/src/grid_movement/CFreeFormBlending.cpp
index dbac22dc8a6..c71ef32d259 100644
--- a/Common/src/grid_movement/CFreeFormBlending.cpp
+++ b/Common/src/grid_movement/CFreeFormBlending.cpp
@@ -2,7 +2,7 @@
  * \file CFreeFormBlending.cpp
  * \brief Parent class for FFD Blending functions
  * \author F. Palacios, T. Economon, S. Padron
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/grid_movement/CFreeFormDefBox.cpp b/Common/src/grid_movement/CFreeFormDefBox.cpp
index 3757225b133..34c97605797 100644
--- a/Common/src/grid_movement/CFreeFormDefBox.cpp
+++ b/Common/src/grid_movement/CFreeFormDefBox.cpp
@@ -2,7 +2,7 @@
  * \file CFreeFormDefBox.cpp
  * \brief Subroutines for handling Free-Form Deformation Boxes
  * \author F. Palacios, T. Economon, S. Padron
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/grid_movement/CGridMovement.cpp b/Common/src/grid_movement/CGridMovement.cpp
index e11b46b4ae6..f02bb94d552 100644
--- a/Common/src/grid_movement/CGridMovement.cpp
+++ b/Common/src/grid_movement/CGridMovement.cpp
@@ -2,7 +2,7 @@
  * \file CGridMovement.cpp
  * \brief Parent class for grid movement classes
  * \author F. Palacios, T. Economon, S. Padron
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/grid_movement/CSurfaceMovement.cpp b/Common/src/grid_movement/CSurfaceMovement.cpp
index b09631f9836..ea9dc6f374c 100644
--- a/Common/src/grid_movement/CSurfaceMovement.cpp
+++ b/Common/src/grid_movement/CSurfaceMovement.cpp
@@ -2,7 +2,7 @@
  * \file CSurfaceMovement.cpp
  * \brief Subroutines for moving mesh surface elements
  * \author F. Palacios, T. Economon, S. Padron
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/grid_movement/CVolumetricMovement.cpp b/Common/src/grid_movement/CVolumetricMovement.cpp
index abb1e140968..89199a0650b 100644
--- a/Common/src/grid_movement/CVolumetricMovement.cpp
+++ b/Common/src/grid_movement/CVolumetricMovement.cpp
@@ -2,7 +2,7 @@
  * \file CVolumetricMovement.cpp
  * \brief Subroutines for moving mesh volume elements
  * \author F. Palacios, T. Economon, S. Padron
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/interface_interpolation/CInterpolator.cpp b/Common/src/interface_interpolation/CInterpolator.cpp
index 8879287a440..3d903a0e668 100644
--- a/Common/src/interface_interpolation/CInterpolator.cpp
+++ b/Common/src/interface_interpolation/CInterpolator.cpp
@@ -2,7 +2,7 @@
  * \file CInterpolator.cpp
  * \brief Definition of the base class for interface interpolation.
  * \author H. Kline
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/interface_interpolation/CInterpolatorFactory.cpp b/Common/src/interface_interpolation/CInterpolatorFactory.cpp
index be50f5075ce..09c0701aa9c 100644
--- a/Common/src/interface_interpolation/CInterpolatorFactory.cpp
+++ b/Common/src/interface_interpolation/CInterpolatorFactory.cpp
@@ -1,7 +1,7 @@
 /*!
  * \file CInterpolatorFactory.cpp
  * \brief Factory to generate interpolator objects.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/interface_interpolation/CIsoparametric.cpp b/Common/src/interface_interpolation/CIsoparametric.cpp
index 19a68a3b423..54d2397822c 100644
--- a/Common/src/interface_interpolation/CIsoparametric.cpp
+++ b/Common/src/interface_interpolation/CIsoparametric.cpp
@@ -2,7 +2,7 @@
  * \file CIsoparametric.cpp
  * \brief Implementation isoparametric interpolation (using FE shape functions).
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/interface_interpolation/CMirror.cpp b/Common/src/interface_interpolation/CMirror.cpp
index c663af40763..664e0db274f 100644
--- a/Common/src/interface_interpolation/CMirror.cpp
+++ b/Common/src/interface_interpolation/CMirror.cpp
@@ -2,7 +2,7 @@
  * \file CMirror.cpp
  * \brief Implementation of mirror interpolation (conservative approach in FSI problems).
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/interface_interpolation/CNearestNeighbor.cpp b/Common/src/interface_interpolation/CNearestNeighbor.cpp
index 1fba622ef70..96b4b894156 100644
--- a/Common/src/interface_interpolation/CNearestNeighbor.cpp
+++ b/Common/src/interface_interpolation/CNearestNeighbor.cpp
@@ -2,7 +2,7 @@
  * \file CNearestNeighbor.cpp
  * \brief Implementation of nearest neighbor interpolation.
  * \author H. Kline
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/interface_interpolation/CRadialBasisFunction.cpp b/Common/src/interface_interpolation/CRadialBasisFunction.cpp
index 424c227b745..16645017012 100644
--- a/Common/src/interface_interpolation/CRadialBasisFunction.cpp
+++ b/Common/src/interface_interpolation/CRadialBasisFunction.cpp
@@ -2,7 +2,7 @@
  * \file CRadialBasisFunction.cpp
  * \brief Implementation of RBF interpolation.
  * \author Joel Ho, P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/interface_interpolation/CSlidingMesh.cpp b/Common/src/interface_interpolation/CSlidingMesh.cpp
index 9e1cfbef8f5..25e5570fb2f 100644
--- a/Common/src/interface_interpolation/CSlidingMesh.cpp
+++ b/Common/src/interface_interpolation/CSlidingMesh.cpp
@@ -2,7 +2,7 @@
  * \file CSlidingMesh.cpp
  * \brief Implementation of sliding mesh interpolation.
  * \author H. Kline
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/linear_algebra/CPastixWrapper.cpp b/Common/src/linear_algebra/CPastixWrapper.cpp
index 8500c44445a..72c94288ff0 100644
--- a/Common/src/linear_algebra/CPastixWrapper.cpp
+++ b/Common/src/linear_algebra/CPastixWrapper.cpp
@@ -3,7 +3,7 @@
  * \brief An interface to the INRIA solver PaStiX
  *        (http://pastix.gforge.inria.fr/files/README-txt.html)
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/linear_algebra/CSysMatrix.cpp b/Common/src/linear_algebra/CSysMatrix.cpp
index 073fe40cdae..dd02b4152e6 100644
--- a/Common/src/linear_algebra/CSysMatrix.cpp
+++ b/Common/src/linear_algebra/CSysMatrix.cpp
@@ -2,7 +2,7 @@
  * \file CSysMatrix.cpp
  * \brief Implementation of the sparse matrix class.
  * \author F. Palacios, A. Bueno, T. Economon, P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/linear_algebra/CSysSolve.cpp b/Common/src/linear_algebra/CSysSolve.cpp
index 0d50e561ae9..00eef72fdaf 100644
--- a/Common/src/linear_algebra/CSysSolve.cpp
+++ b/Common/src/linear_algebra/CSysSolve.cpp
@@ -2,7 +2,7 @@
  * \file CSysSolve.cpp
  * \brief Main classes required for solving linear systems of equations
  * \author J. Hicken, F. Palacios, T. Economon, P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/linear_algebra/CSysSolve_b.cpp b/Common/src/linear_algebra/CSysSolve_b.cpp
index 000b389b8a5..d02c294e31e 100644
--- a/Common/src/linear_algebra/CSysSolve_b.cpp
+++ b/Common/src/linear_algebra/CSysSolve_b.cpp
@@ -2,7 +2,7 @@
  * \file CSysSolve_b.cpp
  * \brief Routines for the linear solver used in the reverse sweep of AD.
  * \author T. Albring, J. Blühdorn
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/linear_algebra/CSysVector.cpp b/Common/src/linear_algebra/CSysVector.cpp
index 9a43baf070a..353b28ceb34 100644
--- a/Common/src/linear_algebra/CSysVector.cpp
+++ b/Common/src/linear_algebra/CSysVector.cpp
@@ -2,7 +2,7 @@
  * \file CSysVector.cpp
  * \brief Implementation and explicit instantiations of CSysVector.
  * \author P. Gomes, F. Palacios, J. Hicken, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/linear_algebra/blas_structure.cpp b/Common/src/linear_algebra/blas_structure.cpp
index 42313022abc..364d027b806 100644
--- a/Common/src/linear_algebra/blas_structure.cpp
+++ b/Common/src/linear_algebra/blas_structure.cpp
@@ -3,7 +3,7 @@
  * \brief Implementation of the functions that either simulate BLAS functionality
           or interface to an actual BLAS implementation.
  * \author E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/C1DInterpolation.cpp b/Common/src/toolboxes/C1DInterpolation.cpp
index 263c3f1ba57..eefa193f32f 100644
--- a/Common/src/toolboxes/C1DInterpolation.cpp
+++ b/Common/src/toolboxes/C1DInterpolation.cpp
@@ -2,7 +2,7 @@
  * \file C1DInterpolation.cpp
  * \brief Classes for 1D interpolation.
  * \author Aman Baig, P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/CLinearPartitioner.cpp b/Common/src/toolboxes/CLinearPartitioner.cpp
index b148411738c..35bb1ea03d9 100644
--- a/Common/src/toolboxes/CLinearPartitioner.cpp
+++ b/Common/src/toolboxes/CLinearPartitioner.cpp
@@ -3,7 +3,7 @@
  * \brief Helper class that provides the counts for each rank in a linear
  *        partitioning given the global count as input.
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/CSquareMatrixCM.cpp b/Common/src/toolboxes/CSquareMatrixCM.cpp
index b4a33c8b2db..68c5088a8d4 100644
--- a/Common/src/toolboxes/CSquareMatrixCM.cpp
+++ b/Common/src/toolboxes/CSquareMatrixCM.cpp
@@ -2,7 +2,7 @@
  * \file CSquareMatrixCM.cpp
  * \brief Implementation of dense matrix helper class in Column Major order (see hpp).
  * \author Edwin van der Weide, Pedro Gomes.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/CSymmetricMatrix.cpp b/Common/src/toolboxes/CSymmetricMatrix.cpp
index e5f6daa723f..ccb58c03203 100644
--- a/Common/src/toolboxes/CSymmetricMatrix.cpp
+++ b/Common/src/toolboxes/CSymmetricMatrix.cpp
@@ -2,7 +2,7 @@
  * \file CSymmetricMatrix.cpp
  * \brief Implementation of dense symmetric matrix helper class (see hpp).
  * \author Joel Ho, P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CIncTGVSolution.cpp b/Common/src/toolboxes/MMS/CIncTGVSolution.cpp
index 26d2652c0a9..53072c921ff 100644
--- a/Common/src/toolboxes/MMS/CIncTGVSolution.cpp
+++ b/Common/src/toolboxes/MMS/CIncTGVSolution.cpp
@@ -2,7 +2,7 @@
  * \file CIncTGVSolution.cpp
  * \brief Implementations of the member functions of CIncTGVSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CInviscidVortexSolution.cpp b/Common/src/toolboxes/MMS/CInviscidVortexSolution.cpp
index 15cf0943f8c..23edb73aead 100644
--- a/Common/src/toolboxes/MMS/CInviscidVortexSolution.cpp
+++ b/Common/src/toolboxes/MMS/CInviscidVortexSolution.cpp
@@ -2,7 +2,7 @@
  * \file CInviscidVortexSolution.cpp
  * \brief Implementations of the member functions of CInviscidVortexSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CMMSIncEulerSolution.cpp b/Common/src/toolboxes/MMS/CMMSIncEulerSolution.cpp
index a53ca290c6e..ad98ffe6d28 100644
--- a/Common/src/toolboxes/MMS/CMMSIncEulerSolution.cpp
+++ b/Common/src/toolboxes/MMS/CMMSIncEulerSolution.cpp
@@ -2,7 +2,7 @@
  * \file CMMSIncEulerSolution.cpp
  * \brief Implementations of the member functions of CMMSIncEulerSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CMMSIncNSSolution.cpp b/Common/src/toolboxes/MMS/CMMSIncNSSolution.cpp
index b7a4e5dbe52..9dcb68c3ad1 100644
--- a/Common/src/toolboxes/MMS/CMMSIncNSSolution.cpp
+++ b/Common/src/toolboxes/MMS/CMMSIncNSSolution.cpp
@@ -2,7 +2,7 @@
  * \file CMMSIncNSSolution.cpp
  * \brief Implementations of the member functions of CMMSIncNSSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.cpp b/Common/src/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.cpp
index ec53a82b6b0..9743f45250a 100644
--- a/Common/src/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.cpp
+++ b/Common/src/toolboxes/MMS/CMMSNSTwoHalfCirclesSolution.cpp
@@ -2,7 +2,7 @@
  * \file CMMSNSTwoHalfCirclesSolution.cpp
  * \brief Implementations of the member functions of CMMSNSTwoHalfCirclesSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.cpp b/Common/src/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.cpp
index 8497f333a06..6b681598c59 100644
--- a/Common/src/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.cpp
+++ b/Common/src/toolboxes/MMS/CMMSNSTwoHalfSpheresSolution.cpp
@@ -2,7 +2,7 @@
  * \file CMMSNSTwoHalfSpheresSolution.cpp
  * \brief Implementations of the member functions of CMMSNSTwoHalfSpheresSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolution.cpp b/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolution.cpp
index 4e268c5b492..aad62acfa8f 100644
--- a/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolution.cpp
+++ b/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolution.cpp
@@ -2,7 +2,7 @@
  * \file CMMSNSUnitQuadSolution.cpp
  * \brief Implementations of the member functions of CMMSNSUnitQuadSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.cpp b/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.cpp
index 8c5814c3e89..28a760c1949 100644
--- a/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.cpp
+++ b/Common/src/toolboxes/MMS/CMMSNSUnitQuadSolutionWallBC.cpp
@@ -2,7 +2,7 @@
  * \file CMMSNSUnitQuadSolutionWallBC.cpp
  * \brief Implementations of the member functions of CMMSNSUnitQuadSolutionWallBC.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CNSUnitQuadSolution.cpp b/Common/src/toolboxes/MMS/CNSUnitQuadSolution.cpp
index e15253a40c8..be18f90ab88 100644
--- a/Common/src/toolboxes/MMS/CNSUnitQuadSolution.cpp
+++ b/Common/src/toolboxes/MMS/CNSUnitQuadSolution.cpp
@@ -2,7 +2,7 @@
  * \file CNSUnitQuadSolution.cpp
  * \brief Implementations of the member functions of CNSUnitQuadSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CRinglebSolution.cpp b/Common/src/toolboxes/MMS/CRinglebSolution.cpp
index 0ae993520c7..5c3ead31234 100644
--- a/Common/src/toolboxes/MMS/CRinglebSolution.cpp
+++ b/Common/src/toolboxes/MMS/CRinglebSolution.cpp
@@ -2,7 +2,7 @@
  * \file CRinglebSolution.cpp
  * \brief Implementations of the member functions of CRinglebSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CTGVSolution.cpp b/Common/src/toolboxes/MMS/CTGVSolution.cpp
index e30b004e7a4..7393d9156fc 100644
--- a/Common/src/toolboxes/MMS/CTGVSolution.cpp
+++ b/Common/src/toolboxes/MMS/CTGVSolution.cpp
@@ -2,7 +2,7 @@
  * \file CTGVSolution.cpp
  * \brief Implementations of the member functions of CTGVSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CUserDefinedSolution.cpp b/Common/src/toolboxes/MMS/CUserDefinedSolution.cpp
index aee58f83778..330d0b9b405 100644
--- a/Common/src/toolboxes/MMS/CUserDefinedSolution.cpp
+++ b/Common/src/toolboxes/MMS/CUserDefinedSolution.cpp
@@ -2,7 +2,7 @@
  * \file CUserDefinedSolution.cpp
  * \brief Implementations of the member functions of CUserDefinedSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CVerificationSolution.cpp b/Common/src/toolboxes/MMS/CVerificationSolution.cpp
index 23746572e34..e8fb64035c9 100644
--- a/Common/src/toolboxes/MMS/CVerificationSolution.cpp
+++ b/Common/src/toolboxes/MMS/CVerificationSolution.cpp
@@ -2,7 +2,7 @@
  * \file CVerificationSolution.cpp
  * \brief Implementations of the member functions of CVerificationSolution.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncEulerSolution.py b/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncEulerSolution.py
index 4ced7a4efed..2bade94d6ed 100755
--- a/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncEulerSolution.py
+++ b/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncEulerSolution.py
@@ -4,7 +4,7 @@
 #  \brief Python script that generates the source terms for a
 #         manufactured solution for the incompressible Euler eqns.
 #  \author T. Economon
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncNSSolution.py b/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncNSSolution.py
index 457825c8f84..6a89a281d2b 100755
--- a/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncNSSolution.py
+++ b/Common/src/toolboxes/MMS/CreateMMSSourceTerms/CMMSIncNSSolution.py
@@ -4,7 +4,7 @@
 #  \brief Python script that generates the source terms for a
 #         manufactured solution for the incompressible Navier-Stokes eqns.
 #  \author T. Economon
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/Common/src/toolboxes/printing_toolbox.cpp b/Common/src/toolboxes/printing_toolbox.cpp
index daaac9a53e7..1001754a873 100644
--- a/Common/src/toolboxes/printing_toolbox.cpp
+++ b/Common/src/toolboxes/printing_toolbox.cpp
@@ -2,7 +2,7 @@
  * \file printing_toolbox.cpp
  * \brief Printing tools
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Common/src/wall_model.cpp b/Common/src/wall_model.cpp
index 008b3e60999..bbeb0231652 100644
--- a/Common/src/wall_model.cpp
+++ b/Common/src/wall_model.cpp
@@ -3,7 +3,7 @@
  * \brief File, which contains the implementation for the wall model functions
  *        for large eddy simulations.
  * \author E. van der Weide, T. Economon, P. Urbanczyk
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/Docs/docmain.hpp b/Docs/docmain.hpp
index fcda1b961ec..43bcb375f75 100644
--- a/Docs/docmain.hpp
+++ b/Docs/docmain.hpp
@@ -2,7 +2,7 @@
  * \file docmain.hpp
  * \brief This file contains documentation for Doxygen and does not have any significance with respect to C++.
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -26,7 +26,7 @@
  */
 
 /*!
- * \mainpage SU2 version 7.5.1 "Blackbird"
+ * \mainpage SU2 version 8.0.0 "Harrier"
  * SU2 suite is an open-source collection of C++ based software tools
  * to perform PDE analysis and PDE constrained optimization.  The toolset is designed with
  * computational fluid dynamics and aerodynamic shape optimization in mind, but is extensible to
diff --git a/QuickStart/inv_NACA0012.cfg b/QuickStart/inv_NACA0012.cfg
index 6b28535d095..36c100c52ed 100644
--- a/QuickStart/inv_NACA0012.cfg
+++ b/QuickStart/inv_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                                  %
+% File Version 8.0.0 "Harrier"                                                    %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/README.md b/README.md
index 4ad3b1fad6a..6b6db44446e 100644
--- a/README.md
+++ b/README.md
@@ -3,7 +3,7 @@
 </p>
 
 
-# SU2 (ver. 7.5.1 "Blackbird"): The Open-Source CFD Code
+# SU2 (ver. 8.0.0 "Harrier"): The Open-Source CFD Code
 
 Computational analysis tools have revolutionized the way we design engineering systems, but most established codes are proprietary, unavailable, or prohibitively expensive for many users. The SU2 team is changing this, making multiphysics analysis and design optimization freely available as open-source software and involving everyone in its creation and development.
 
diff --git a/SU2_CFD/include/CMarkerProfileReaderFVM.hpp b/SU2_CFD/include/CMarkerProfileReaderFVM.hpp
index 5f1d6c6bcad..f28a0f0b8a0 100644
--- a/SU2_CFD/include/CMarkerProfileReaderFVM.hpp
+++ b/SU2_CFD/include/CMarkerProfileReaderFVM.hpp
@@ -3,7 +3,7 @@
  * \brief Header file for the class CMarkerProfileReaderFVM.
  *        The implementations are in the <i>CMarkerProfileReaderFVM.cpp</i> file.
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/SU2_CFD.hpp b/SU2_CFD/include/SU2_CFD.hpp
index c23920bb9e4..77d13f58dd7 100644
--- a/SU2_CFD/include/SU2_CFD.hpp
+++ b/SU2_CFD/include/SU2_CFD.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines of the code SU2_CFD.
  *        The subroutines and functions are in the <i>SU2_CFD.cpp</i> file.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/definition_structure.hpp b/SU2_CFD/include/definition_structure.hpp
index 0b21e892130..bf826f6338e 100644
--- a/SU2_CFD/include/definition_structure.hpp
+++ b/SU2_CFD/include/definition_structure.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines used by SU2_CFD.
  *        The subroutines and functions are in the <i>definition_structure.cpp</i> file.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/drivers/CDiscAdjMultizoneDriver.hpp b/SU2_CFD/include/drivers/CDiscAdjMultizoneDriver.hpp
index dee86ad3f19..eeac90dcc11 100644
--- a/SU2_CFD/include/drivers/CDiscAdjMultizoneDriver.hpp
+++ b/SU2_CFD/include/drivers/CDiscAdjMultizoneDriver.hpp
@@ -2,7 +2,7 @@
  * \class CDiscAdjMultizoneDriver.hpp
  * \brief Class for driving adjoint multi-zone problems.
  * \author O. Burghardt, P. Gomes, T. Albring, R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp b/SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp
index 8f8a6c19238..d30fc5ac9d2 100644
--- a/SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp
+++ b/SU2_CFD/include/drivers/CDiscAdjSinglezoneDriver.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for driving single or multi-zone problems.
  *        The subroutines and functions are in the <i>driver_structure.cpp</i> file.
  * \author T. Economon, H. Kline, R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -34,7 +34,7 @@
  * \ingroup DiscAdj
  * \brief Class for driving single-zone adjoint solvers.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CDiscAdjSinglezoneDriver : public CSinglezoneDriver {
 protected:
diff --git a/SU2_CFD/include/drivers/CDriver.hpp b/SU2_CFD/include/drivers/CDriver.hpp
index 236c932b630..5ac33896849 100644
--- a/SU2_CFD/include/drivers/CDriver.hpp
+++ b/SU2_CFD/include/drivers/CDriver.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for driving single or multi-zone problems.
  *        The subroutines and functions are in the <i>driver_structure.cpp</i> file.
  * \author T. Economon, H. Kline, R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/drivers/CDriverBase.hpp b/SU2_CFD/include/drivers/CDriverBase.hpp
index 01c3ae7a58d..1aaaed47349 100644
--- a/SU2_CFD/include/drivers/CDriverBase.hpp
+++ b/SU2_CFD/include/drivers/CDriverBase.hpp
@@ -2,7 +2,7 @@
  * \file CDriverBase.hpp
  * \brief Base class for all drivers.
  * \author H. Patel, A. Gastaldi
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/drivers/CDummyDriver.hpp b/SU2_CFD/include/drivers/CDummyDriver.hpp
index 3f1d959f44c..d11c0285e7c 100644
--- a/SU2_CFD/include/drivers/CDummyDriver.hpp
+++ b/SU2_CFD/include/drivers/CDummyDriver.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for driving single or multi-zone problems.
  *        The subroutines and functions are in the <i>driver_structure.cpp</i> file.
  * \author T. Economon, H. Kline, R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/drivers/CMultizoneDriver.hpp b/SU2_CFD/include/drivers/CMultizoneDriver.hpp
index adf9bf9d617..9779f0dc410 100644
--- a/SU2_CFD/include/drivers/CMultizoneDriver.hpp
+++ b/SU2_CFD/include/drivers/CMultizoneDriver.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for driving single or multi-zone problems.
  *        The subroutines and functions are in the <i>driver_structure.cpp</i> file.
  * \author T. Economon, H. Kline, R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -35,7 +35,7 @@
  * \ingroup Drivers
  * \brief Class for driving zone-specific iterations.
  * \author R. Sanchez, O. Burghardt
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CMultizoneDriver : public CDriver {
 protected:
diff --git a/SU2_CFD/include/drivers/CSinglezoneDriver.hpp b/SU2_CFD/include/drivers/CSinglezoneDriver.hpp
index 07cc41c2d51..c1292ea6290 100644
--- a/SU2_CFD/include/drivers/CSinglezoneDriver.hpp
+++ b/SU2_CFD/include/drivers/CSinglezoneDriver.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines for driving single or multi-zone problems.
  *        The subroutines and functions are in the <i>driver_structure.cpp</i> file.
  * \author T. Economon, H. Kline, R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -34,7 +34,7 @@
  * \ingroup Drivers
  * \brief Class for driving single-zone solvers.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CSinglezoneDriver : public CDriver {
 protected:
diff --git a/SU2_CFD/include/fluid/CConductivityModel.hpp b/SU2_CFD/include/fluid/CConductivityModel.hpp
index e22104e3a9b..3267ae86468 100644
--- a/SU2_CFD/include/fluid/CConductivityModel.hpp
+++ b/SU2_CFD/include/fluid/CConductivityModel.hpp
@@ -2,7 +2,7 @@
  * \file CConductivityModel.hpp
  * \brief Defines an interface class for thermal conductivity models.
  * \author S. Vitale, M. Pini, G. Gori, A. Guardone, P. Colonna, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CConstantConductivity.hpp b/SU2_CFD/include/fluid/CConstantConductivity.hpp
index c82f322cd91..4fd94570e7f 100644
--- a/SU2_CFD/include/fluid/CConstantConductivity.hpp
+++ b/SU2_CFD/include/fluid/CConstantConductivity.hpp
@@ -2,7 +2,7 @@
  * \file CConstantConductivity.hpp
  * \brief Defines a constant laminar thermal conductivity model.
  * \author S. Vitale, M. Pini, G. Gori, A. Guardone, P. Colonna, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CConstantConductivityRANS.hpp b/SU2_CFD/include/fluid/CConstantConductivityRANS.hpp
index ce5d2a0f9b2..3a1e2b896c2 100644
--- a/SU2_CFD/include/fluid/CConstantConductivityRANS.hpp
+++ b/SU2_CFD/include/fluid/CConstantConductivityRANS.hpp
@@ -2,7 +2,7 @@
  * \file CConstantConductivityRANS.hpp
  * \brief Defines a constant conductivity model for RANS problems.
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CConstantDensity.hpp b/SU2_CFD/include/fluid/CConstantDensity.hpp
index ed9a1236f22..98cdcd37b59 100644
--- a/SU2_CFD/include/fluid/CConstantDensity.hpp
+++ b/SU2_CFD/include/fluid/CConstantDensity.hpp
@@ -2,7 +2,7 @@
  * \file CConstantDensity.hpp
  * \brief Defines the incompressible constant density model.
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CConstantDiffusivity.hpp b/SU2_CFD/include/fluid/CConstantDiffusivity.hpp
index c4571084c97..8f88d28c881 100644
--- a/SU2_CFD/include/fluid/CConstantDiffusivity.hpp
+++ b/SU2_CFD/include/fluid/CConstantDiffusivity.hpp
@@ -2,7 +2,7 @@
  * \file CConstantDiffusivity.hpp
  * \brief Defines constant mass diffusivity.
  * \author T. Economon, Cristopher Morales Ubal
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CConstantLewisDiffusivity.hpp b/SU2_CFD/include/fluid/CConstantLewisDiffusivity.hpp
index bf7f60598b5..e42c05cbbd0 100644
--- a/SU2_CFD/include/fluid/CConstantLewisDiffusivity.hpp
+++ b/SU2_CFD/include/fluid/CConstantLewisDiffusivity.hpp
@@ -2,7 +2,7 @@
  * \file CConstantLewisDiffusivity.hpp
  * \brief Defines Constant Lewis mass diffusivity.
  * \author M.Heimgartner, C.Morales
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CConstantPrandtl.hpp b/SU2_CFD/include/fluid/CConstantPrandtl.hpp
index d10849a2282..eef1499e4c1 100644
--- a/SU2_CFD/include/fluid/CConstantPrandtl.hpp
+++ b/SU2_CFD/include/fluid/CConstantPrandtl.hpp
@@ -2,7 +2,7 @@
  * \file CConstantPrandtl.hpp
  * \brief Defines a non-constant laminar Prandtl number thermal conductivity model.
  * \author S. Vitale, M. Pini, G. Gori, A. Guardone, P. Colonna, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CConstantPrandtlRANS.hpp b/SU2_CFD/include/fluid/CConstantPrandtlRANS.hpp
index ab1eb2c13c7..2a966a3cc8e 100644
--- a/SU2_CFD/include/fluid/CConstantPrandtlRANS.hpp
+++ b/SU2_CFD/include/fluid/CConstantPrandtlRANS.hpp
@@ -2,7 +2,7 @@
  * \file CConstantPrandtlRANS.hpp
  * \brief Defines a non-constant effective thermal conductivity for RANS problems using Prandtl numbers.
  * \author S. Vitale, M. Pini, G. Gori, A. Guardone, P. Colonna, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CConstantSchmidt.hpp b/SU2_CFD/include/fluid/CConstantSchmidt.hpp
index e76a49cbcf8..a888089ca31 100644
--- a/SU2_CFD/include/fluid/CConstantSchmidt.hpp
+++ b/SU2_CFD/include/fluid/CConstantSchmidt.hpp
@@ -2,7 +2,7 @@
  * \file CConstantSchmidt.hpp
  * \brief Defines a mass diffusivity model with constant Schmidt numbers.
  * \author S. Vitale, M. Pini, G. Gori, A. Guardone, P. Colonna, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CConstantViscosity.hpp b/SU2_CFD/include/fluid/CConstantViscosity.hpp
index 4ceca83970e..187cbae36fc 100644
--- a/SU2_CFD/include/fluid/CConstantViscosity.hpp
+++ b/SU2_CFD/include/fluid/CConstantViscosity.hpp
@@ -2,7 +2,7 @@
  * \file CConstantViscosity.hpp
  * \brief Defines a constant laminar viscosity model.
  * \author S. Vitale, M. Pini, G. Gori, A. Guardone, P. Colonna, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CCoolProp.hpp b/SU2_CFD/include/fluid/CCoolProp.hpp
index c61d82ef0f3..76550e9302c 100644
--- a/SU2_CFD/include/fluid/CCoolProp.hpp
+++ b/SU2_CFD/include/fluid/CCoolProp.hpp
@@ -2,7 +2,7 @@
  * \file CCoolProp.hpp
  * \brief Defines the state-of-the-art fluid model from CoolProp library.
  * \author P. Yan, G. Gori, A. Guardone
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CCoolPropConductivity.hpp b/SU2_CFD/include/fluid/CCoolPropConductivity.hpp
index 416d76759c8..66f8e9d8f5b 100644
--- a/SU2_CFD/include/fluid/CCoolPropConductivity.hpp
+++ b/SU2_CFD/include/fluid/CCoolPropConductivity.hpp
@@ -2,7 +2,7 @@
  * \file CCoolPropConductivity.hpp
  * \brief Defines laminar thermal conductivity model from CoolProp.
  * \author P.YAn, G. Gori, A. Guardone
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CCoolPropViscosity.hpp b/SU2_CFD/include/fluid/CCoolPropViscosity.hpp
index 72f9be4ee0b..89e8a5ef430 100644
--- a/SU2_CFD/include/fluid/CCoolPropViscosity.hpp
+++ b/SU2_CFD/include/fluid/CCoolPropViscosity.hpp
@@ -2,7 +2,7 @@
  * \file CCoolPropViscosity.hpp
  * \brief Defines CoolPropviscosity model.
  * \author P.Yan, G. Gori, A. Guardone,
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
index b888a104307..6c067bc92aa 100644
--- a/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
+++ b/SU2_CFD/include/fluid/CDataDrivenFluid.hpp
@@ -3,7 +3,7 @@
  * \brief Defines a template fluid model class using multilayer perceptrons
  *  for theromodynamic state definition
  * \author E.C.Bunschoten
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CDiffusivityModel.hpp b/SU2_CFD/include/fluid/CDiffusivityModel.hpp
index 0fee7956fd8..b02b7ea95e0 100644
--- a/SU2_CFD/include/fluid/CDiffusivityModel.hpp
+++ b/SU2_CFD/include/fluid/CDiffusivityModel.hpp
@@ -2,7 +2,7 @@
  * \file CDiffusivityModel.hpp
  * \brief Interface class for defining mass diffusivity models.
  * \author T. Economon, C. Morales
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CFluidFlamelet.hpp b/SU2_CFD/include/fluid/CFluidFlamelet.hpp
index 929146baa30..9520a432a44 100644
--- a/SU2_CFD/include/fluid/CFluidFlamelet.hpp
+++ b/SU2_CFD/include/fluid/CFluidFlamelet.hpp
@@ -2,7 +2,7 @@
  * \file CFluidFlamelet.hpp
  * \brief  Defines the flamelet fluid model
  * \author D. Mayer, T. Economon, N. Beishuizen, E. Bunschoten
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CFluidModel.hpp b/SU2_CFD/include/fluid/CFluidModel.hpp
index aa7131f468e..682e4366b49 100644
--- a/SU2_CFD/include/fluid/CFluidModel.hpp
+++ b/SU2_CFD/include/fluid/CFluidModel.hpp
@@ -2,7 +2,7 @@
  * \file CFluidModel.hpp
  * \brief Defines the main fluid model class for thermophysical properties.
  * \author S. Vitale, G. Gori, M. Pini, A. Guardone, P. Colonna, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CFluidScalar.hpp b/SU2_CFD/include/fluid/CFluidScalar.hpp
index f6fc2572db7..d530de01f35 100644
--- a/SU2_CFD/include/fluid/CFluidScalar.hpp
+++ b/SU2_CFD/include/fluid/CFluidScalar.hpp
@@ -2,7 +2,7 @@
  * \file CFluidScalar.hpp
  * \brief  Defines the multicomponent incompressible Ideal Gas model for mixtures.
  * \author T. Economon, Mark Heimgartner, Cristopher Morales Ubal
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CIdealGas.hpp b/SU2_CFD/include/fluid/CIdealGas.hpp
index be28ee4dfd9..de6044961a7 100644
--- a/SU2_CFD/include/fluid/CIdealGas.hpp
+++ b/SU2_CFD/include/fluid/CIdealGas.hpp
@@ -2,7 +2,7 @@
  * \file CIdealGas.hpp
  * \brief Defines the ideal gas model.
  * \author S. Vitale, G. Gori, M. Pini, A. Guardone, P. Colonna
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CIncIdealGas.hpp b/SU2_CFD/include/fluid/CIncIdealGas.hpp
index f7a7bc7c241..2b51afc3f45 100644
--- a/SU2_CFD/include/fluid/CIncIdealGas.hpp
+++ b/SU2_CFD/include/fluid/CIncIdealGas.hpp
@@ -2,7 +2,7 @@
  * \file CIncIdealGas.hpp
  * \brief Defines the incompressible Ideal Gas model.
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CIncIdealGasPolynomial.hpp b/SU2_CFD/include/fluid/CIncIdealGasPolynomial.hpp
index 1d19436c404..8c7ab29bb66 100644
--- a/SU2_CFD/include/fluid/CIncIdealGasPolynomial.hpp
+++ b/SU2_CFD/include/fluid/CIncIdealGasPolynomial.hpp
@@ -2,7 +2,7 @@
  * \file CIncIdealGasPolynomial.hpp
  * \brief Defines the incompressible Ideal Gas model with polynomial Cp.
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CMutationTCLib.hpp b/SU2_CFD/include/fluid/CMutationTCLib.hpp
index 3fb90dd7886..071658e50ce 100644
--- a/SU2_CFD/include/fluid/CMutationTCLib.hpp
+++ b/SU2_CFD/include/fluid/CMutationTCLib.hpp
@@ -2,7 +2,7 @@
  * \file CMutationTCLib.hpp
  * \brief Defines the class for the link to Mutation++ ThermoChemistry library.
  * \author C. Garbacz
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CNEMOGas.hpp b/SU2_CFD/include/fluid/CNEMOGas.hpp
index f8a17a600bf..038ce2ca6b3 100644
--- a/SU2_CFD/include/fluid/CNEMOGas.hpp
+++ b/SU2_CFD/include/fluid/CNEMOGas.hpp
@@ -2,7 +2,7 @@
  * \file CNEMOGas.hpp
  * \brief Defines the nonequilibrium gas model.
  * \author C. Garbacz, W. Maier, S. R. Copeland
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CPengRobinson.hpp b/SU2_CFD/include/fluid/CPengRobinson.hpp
index 5ae07b2cbd6..cdd836d835e 100644
--- a/SU2_CFD/include/fluid/CPengRobinson.hpp
+++ b/SU2_CFD/include/fluid/CPengRobinson.hpp
@@ -2,7 +2,7 @@
  * \file CPengRobinson.hpp
  * \brief Defines the Peng-Robinson model.
  * \author S. Vitale, G. Gori, M. Pini, A. Guardone, P. Colonna
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CPolynomialConductivity.hpp b/SU2_CFD/include/fluid/CPolynomialConductivity.hpp
index 242893818d3..2b016e39f69 100644
--- a/SU2_CFD/include/fluid/CPolynomialConductivity.hpp
+++ b/SU2_CFD/include/fluid/CPolynomialConductivity.hpp
@@ -2,7 +2,7 @@
  * \file CPolynomialConductivity.hpp
  * \brief Defines a non-constant laminar thermal conductivity using a polynomial function of temperature.
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CPolynomialConductivityRANS.hpp b/SU2_CFD/include/fluid/CPolynomialConductivityRANS.hpp
index 1671944faf1..a58587a4a74 100644
--- a/SU2_CFD/include/fluid/CPolynomialConductivityRANS.hpp
+++ b/SU2_CFD/include/fluid/CPolynomialConductivityRANS.hpp
@@ -3,7 +3,7 @@
  * \brief Defines a non-constant thermal conductivity using a polynomial function of temperature
  *        for RANS problems with the addition of a turbulent component based on a turbulent Prandtl number.
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CPolynomialViscosity.hpp b/SU2_CFD/include/fluid/CPolynomialViscosity.hpp
index 6099de8442d..7742458c163 100644
--- a/SU2_CFD/include/fluid/CPolynomialViscosity.hpp
+++ b/SU2_CFD/include/fluid/CPolynomialViscosity.hpp
@@ -2,7 +2,7 @@
  * \file CPolynomialViscosity.hpp
  * \brief Defines a laminar viscosity model as a polynomial function of temperature.
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CSU2TCLib.hpp b/SU2_CFD/include/fluid/CSU2TCLib.hpp
index 7412e6086e9..3200ab9554e 100644
--- a/SU2_CFD/include/fluid/CSU2TCLib.hpp
+++ b/SU2_CFD/include/fluid/CSU2TCLib.hpp
@@ -2,7 +2,7 @@
  * \file CSU2TCLib.hpp
  * \brief Defines the classes for different user defined ThermoChemistry libraries.
  * \author C. Garbacz, W. Maier, S. R. Copeland
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CSutherland.hpp b/SU2_CFD/include/fluid/CSutherland.hpp
index ff9c16f3c3a..74050242138 100644
--- a/SU2_CFD/include/fluid/CSutherland.hpp
+++ b/SU2_CFD/include/fluid/CSutherland.hpp
@@ -2,7 +2,7 @@
  * \file CSutherland.hpp
  * \brief Defines Sutherland's Law for laminar viscosity.
  * \author S. Vitale, M. Pini, G. Gori, A. Guardone, P. Colonna, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CVanDerWaalsGas.hpp b/SU2_CFD/include/fluid/CVanDerWaalsGas.hpp
index 121d5befc10..83279025158 100644
--- a/SU2_CFD/include/fluid/CVanDerWaalsGas.hpp
+++ b/SU2_CFD/include/fluid/CVanDerWaalsGas.hpp
@@ -2,7 +2,7 @@
  * \file CVanDerWaalsGas.hpp
  * \brief Declaration of the Polytropic Van der Waals model.
  * \author S. Vitale, G. Gori, M. Pini, A. Guardone, P. Colonna
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/fluid/CViscosityModel.hpp b/SU2_CFD/include/fluid/CViscosityModel.hpp
index 41fb37164bd..cc5c46541be 100644
--- a/SU2_CFD/include/fluid/CViscosityModel.hpp
+++ b/SU2_CFD/include/fluid/CViscosityModel.hpp
@@ -2,7 +2,7 @@
  * \file CViscosityModel.hpp
  * \brief Interface class for defining laminar viscosity models.
  * \author S. Vitale, M. Pini, G. Gori, A. Guardone, P. Colonna, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/gradients/computeGradientsGreenGauss.hpp b/SU2_CFD/include/gradients/computeGradientsGreenGauss.hpp
index 23543a63e3c..d2e3762997f 100644
--- a/SU2_CFD/include/gradients/computeGradientsGreenGauss.hpp
+++ b/SU2_CFD/include/gradients/computeGradientsGreenGauss.hpp
@@ -4,7 +4,7 @@
  * \note This allows the same implementation to be used for conservative
  *       and primitive variables of any solver.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/gradients/computeGradientsLeastSquares.hpp b/SU2_CFD/include/gradients/computeGradientsLeastSquares.hpp
index 62a46cfab7e..da6b6f08327 100644
--- a/SU2_CFD/include/gradients/computeGradientsLeastSquares.hpp
+++ b/SU2_CFD/include/gradients/computeGradientsLeastSquares.hpp
@@ -3,7 +3,7 @@
  * \brief Generic implementation of Least-Squares gradient computation.
  * \note This allows the same implementation to be used for conservative
  *       and primitive variables of any solver.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/integration/CFEM_DG_Integration.hpp b/SU2_CFD/include/integration/CFEM_DG_Integration.hpp
index ae78b4be5fa..b0679c118b0 100644
--- a/SU2_CFD/include/integration/CFEM_DG_Integration.hpp
+++ b/SU2_CFD/include/integration/CFEM_DG_Integration.hpp
@@ -2,7 +2,7 @@
  * \file CFEM_DG_Integration.hpp
  * \brief Declaration of class for integration with the FEM DG solver.
  * \author E. van der Weide, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -32,7 +32,7 @@
  * \ingroup Drivers
  * \brief Class for integration with the FEM DG solver.
  * \author E. van der Weide, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CFEM_DG_Integration final : public CIntegration {
 public:
diff --git a/SU2_CFD/include/integration/CIntegration.hpp b/SU2_CFD/include/integration/CIntegration.hpp
index 577d908c8d0..29538908d4f 100644
--- a/SU2_CFD/include/integration/CIntegration.hpp
+++ b/SU2_CFD/include/integration/CIntegration.hpp
@@ -2,7 +2,7 @@
  * \file CIntegration.hpp
  * \brief Declaration of the main routines to orchestrate space and time integration.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/integration/CIntegrationFactory.hpp b/SU2_CFD/include/integration/CIntegrationFactory.hpp
index 98e45f4fee1..908b0497aef 100644
--- a/SU2_CFD/include/integration/CIntegrationFactory.hpp
+++ b/SU2_CFD/include/integration/CIntegrationFactory.hpp
@@ -2,7 +2,7 @@
  * \file CIntegrationFactory.hpp
  * \brief Headers of the CIntegrationFactory class
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/integration/CMultiGridIntegration.hpp b/SU2_CFD/include/integration/CMultiGridIntegration.hpp
index e7745f7e563..16499903961 100644
--- a/SU2_CFD/include/integration/CMultiGridIntegration.hpp
+++ b/SU2_CFD/include/integration/CMultiGridIntegration.hpp
@@ -2,7 +2,7 @@
  * \file CMultiGridIntegration.hpp
  * \brief Declaration of class for time integration using a multigrid method.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/integration/CNewtonIntegration.hpp b/SU2_CFD/include/integration/CNewtonIntegration.hpp
index c76a3140743..c55b667b6a0 100644
--- a/SU2_CFD/include/integration/CNewtonIntegration.hpp
+++ b/SU2_CFD/include/integration/CNewtonIntegration.hpp
@@ -2,7 +2,7 @@
  * \file CNewtonIntegration.hpp
  * \brief Newton-Krylov integration.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/integration/CSingleGridIntegration.hpp b/SU2_CFD/include/integration/CSingleGridIntegration.hpp
index ffc6ecfb070..6a51e11bd80 100644
--- a/SU2_CFD/include/integration/CSingleGridIntegration.hpp
+++ b/SU2_CFD/include/integration/CSingleGridIntegration.hpp
@@ -2,7 +2,7 @@
  * \file CSingleGridIntegration.hpp
  * \brief Declaration of class for numerical integration of fine grid-only problems.
  * \author A. Bueno.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/integration/CStructuralIntegration.hpp b/SU2_CFD/include/integration/CStructuralIntegration.hpp
index a0edd77c8df..757ddf583e9 100644
--- a/SU2_CFD/include/integration/CStructuralIntegration.hpp
+++ b/SU2_CFD/include/integration/CStructuralIntegration.hpp
@@ -2,7 +2,7 @@
  * \file CStructuralIntegration.hpp
  * \brief Declaration of class for numerical integration of structural problems.
  * \author R. Sanchez.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/interfaces/CInterface.hpp b/SU2_CFD/include/interfaces/CInterface.hpp
index 49deb7dbe31..7830e091085 100644
--- a/SU2_CFD/include/interfaces/CInterface.hpp
+++ b/SU2_CFD/include/interfaces/CInterface.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations and inlines of the transfer structure.
  *        The subroutines and functions are in the physics folders.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -51,7 +51,7 @@ using namespace std;
  * \ingroup Interfaces
  * \brief Main class for defining the physical transfer of information.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 
 class CInterface {
diff --git a/SU2_CFD/include/interfaces/cfd/CConservativeVarsInterface.hpp b/SU2_CFD/include/interfaces/cfd/CConservativeVarsInterface.hpp
index dfc8523a171..43300f1f336 100644
--- a/SU2_CFD/include/interfaces/cfd/CConservativeVarsInterface.hpp
+++ b/SU2_CFD/include/interfaces/cfd/CConservativeVarsInterface.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer conservative variables
  *        from a generic zone into another one.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/interfaces/cfd/CMixingPlaneInterface.hpp b/SU2_CFD/include/interfaces/cfd/CMixingPlaneInterface.hpp
index de3fe45340a..8eb2ee0aa0f 100644
--- a/SU2_CFD/include/interfaces/cfd/CMixingPlaneInterface.hpp
+++ b/SU2_CFD/include/interfaces/cfd/CMixingPlaneInterface.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer average variables
  *        needed for MixingPlane computation from a generic zone into another one.
  * \author S. Vitale
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/interfaces/cfd/CSlidingInterface.hpp b/SU2_CFD/include/interfaces/cfd/CSlidingInterface.hpp
index 1bf80223ebd..d2adc4f21e4 100644
--- a/SU2_CFD/include/interfaces/cfd/CSlidingInterface.hpp
+++ b/SU2_CFD/include/interfaces/cfd/CSlidingInterface.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer conservative variables
  *        from a generic zone into another
  * \author G. Gori Politecnico di Milano
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/interfaces/cht/CConjugateHeatInterface.hpp b/SU2_CFD/include/interfaces/cht/CConjugateHeatInterface.hpp
index 9cc42f8d20f..093675bb5dc 100644
--- a/SU2_CFD/include/interfaces/cht/CConjugateHeatInterface.hpp
+++ b/SU2_CFD/include/interfaces/cht/CConjugateHeatInterface.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer temperature and heatflux
  *        density for conjugate heat interfaces between structure and fluid zones.
  * \author O. Burghardt
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/interfaces/fsi/CDiscAdjFlowTractionInterface.hpp b/SU2_CFD/include/interfaces/fsi/CDiscAdjFlowTractionInterface.hpp
index d6e86015a83..5959bb91cf2 100644
--- a/SU2_CFD/include/interfaces/fsi/CDiscAdjFlowTractionInterface.hpp
+++ b/SU2_CFD/include/interfaces/fsi/CDiscAdjFlowTractionInterface.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer flow tractions
  *        from a fluid zone into a structural zone in a discrete adjoint simulation.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/interfaces/fsi/CDisplacementsInterface.hpp b/SU2_CFD/include/interfaces/fsi/CDisplacementsInterface.hpp
index f8388331945..1674a6aeca7 100644
--- a/SU2_CFD/include/interfaces/fsi/CDisplacementsInterface.hpp
+++ b/SU2_CFD/include/interfaces/fsi/CDisplacementsInterface.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer boundary displacements
  *        from a structural zone into a fluid zone.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/interfaces/fsi/CFlowTractionInterface.hpp b/SU2_CFD/include/interfaces/fsi/CFlowTractionInterface.hpp
index d3ea4a6a59d..b0d808a5580 100644
--- a/SU2_CFD/include/interfaces/fsi/CFlowTractionInterface.hpp
+++ b/SU2_CFD/include/interfaces/fsi/CFlowTractionInterface.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer flow tractions
  *        from a fluid zone into a structural zone.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/iteration/CAdjFluidIteration.hpp b/SU2_CFD/include/iteration/CAdjFluidIteration.hpp
index 685b86400bf..47dca3c765d 100644
--- a/SU2_CFD/include/iteration/CAdjFluidIteration.hpp
+++ b/SU2_CFD/include/iteration/CAdjFluidIteration.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the iteration classes used by SU2_CFD.
  *        Each CIteration class represents an available physics package.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/iteration/CDiscAdjFEAIteration.hpp b/SU2_CFD/include/iteration/CDiscAdjFEAIteration.hpp
index 86e9073f5ea..9fec0cbd75b 100644
--- a/SU2_CFD/include/iteration/CDiscAdjFEAIteration.hpp
+++ b/SU2_CFD/include/iteration/CDiscAdjFEAIteration.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the iteration classes used by SU2_CFD.
  *        Each CIteration class represents an available physics package.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/iteration/CDiscAdjFluidIteration.hpp b/SU2_CFD/include/iteration/CDiscAdjFluidIteration.hpp
index 6bf38d45af0..1e496031f2e 100644
--- a/SU2_CFD/include/iteration/CDiscAdjFluidIteration.hpp
+++ b/SU2_CFD/include/iteration/CDiscAdjFluidIteration.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the iteration classes used by SU2_CFD.
  *        Each CIteration class represents an available physics package.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/iteration/CDiscAdjHeatIteration.hpp b/SU2_CFD/include/iteration/CDiscAdjHeatIteration.hpp
index 390c5ba6a54..c2d110ade8b 100644
--- a/SU2_CFD/include/iteration/CDiscAdjHeatIteration.hpp
+++ b/SU2_CFD/include/iteration/CDiscAdjHeatIteration.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the iteration classes used by SU2_CFD.
  *        Each CIteration class represents an available physics package.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/iteration/CFEAIteration.hpp b/SU2_CFD/include/iteration/CFEAIteration.hpp
index d5f9a654c45..8a7ff42a40d 100644
--- a/SU2_CFD/include/iteration/CFEAIteration.hpp
+++ b/SU2_CFD/include/iteration/CFEAIteration.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the iteration classes used by SU2_CFD.
  *        Each CIteration class represents an available physics package.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -35,7 +35,7 @@
  * \ingroup Drivers
  * \brief Class for driving an iteration of structural analysis.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CFEAIteration : public CIteration {
  public:
diff --git a/SU2_CFD/include/iteration/CFEMFluidIteration.hpp b/SU2_CFD/include/iteration/CFEMFluidIteration.hpp
index a2f42b6453c..964ca966250 100644
--- a/SU2_CFD/include/iteration/CFEMFluidIteration.hpp
+++ b/SU2_CFD/include/iteration/CFEMFluidIteration.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the iteration classes used by SU2_CFD.
  *        Each CIteration class represents an available physics package.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -35,7 +35,7 @@
  * \ingroup Drivers
  * \brief Class for driving an iteration of the finite element flow system.
  * \author T. Economon, E. van der Weide
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CFEMFluidIteration : public CFluidIteration {
  public:
diff --git a/SU2_CFD/include/iteration/CFluidIteration.hpp b/SU2_CFD/include/iteration/CFluidIteration.hpp
index 6346c716929..c960b635e35 100644
--- a/SU2_CFD/include/iteration/CFluidIteration.hpp
+++ b/SU2_CFD/include/iteration/CFluidIteration.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the iteration classes used by SU2_CFD.
  *        Each CIteration class represents an available physics package.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/iteration/CHeatIteration.hpp b/SU2_CFD/include/iteration/CHeatIteration.hpp
index 6c548788960..b994521267d 100644
--- a/SU2_CFD/include/iteration/CHeatIteration.hpp
+++ b/SU2_CFD/include/iteration/CHeatIteration.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the iteration classes used by SU2_CFD.
  *        Each CIteration class represents an available physics package.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/iteration/CIteration.hpp b/SU2_CFD/include/iteration/CIteration.hpp
index eed41a39a15..da807245967 100644
--- a/SU2_CFD/include/iteration/CIteration.hpp
+++ b/SU2_CFD/include/iteration/CIteration.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the iteration classes used by SU2_CFD.
  *        Each CIteration class represents an available physics package.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/iteration/CIterationFactory.hpp b/SU2_CFD/include/iteration/CIterationFactory.hpp
index 5aa270d0594..271ca8b9e3f 100644
--- a/SU2_CFD/include/iteration/CIterationFactory.hpp
+++ b/SU2_CFD/include/iteration/CIterationFactory.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the iteration classes used by SU2_CFD.
  *        Each CIteration class represents an available physics package.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/iteration/CTurboIteration.hpp b/SU2_CFD/include/iteration/CTurboIteration.hpp
index ad52aaa04b4..438e23bfd1d 100644
--- a/SU2_CFD/include/iteration/CTurboIteration.hpp
+++ b/SU2_CFD/include/iteration/CTurboIteration.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the iteration classes used by SU2_CFD.
  *        Each CIteration class represents an available physics package.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/limiters/CLimiterDetails.hpp b/SU2_CFD/include/limiters/CLimiterDetails.hpp
index 370831eff27..8311bb31697 100644
--- a/SU2_CFD/include/limiters/CLimiterDetails.hpp
+++ b/SU2_CFD/include/limiters/CLimiterDetails.hpp
@@ -3,7 +3,7 @@
  * \brief A class template that allows defining limiters via
  *        specialization of particular details.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/limiters/computeLimiters.hpp b/SU2_CFD/include/limiters/computeLimiters.hpp
index 75918e14702..f33439d5294 100644
--- a/SU2_CFD/include/limiters/computeLimiters.hpp
+++ b/SU2_CFD/include/limiters/computeLimiters.hpp
@@ -2,7 +2,7 @@
  * \file computeLimiters.hpp
  * \brief Compute limiters wrapper function.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/limiters/computeLimiters_impl.hpp b/SU2_CFD/include/limiters/computeLimiters_impl.hpp
index f683bc5ed77..5cc8007eb00 100644
--- a/SU2_CFD/include/limiters/computeLimiters_impl.hpp
+++ b/SU2_CFD/include/limiters/computeLimiters_impl.hpp
@@ -4,7 +4,7 @@
  * \note Common methods are derived by defining small details
  *       via specialization of CLimiterDetails.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/CGradSmoothing.hpp b/SU2_CFD/include/numerics/CGradSmoothing.hpp
index 8213ce959c6..0a07d87ea30 100644
--- a/SU2_CFD/include/numerics/CGradSmoothing.hpp
+++ b/SU2_CFD/include/numerics/CGradSmoothing.hpp
@@ -2,7 +2,7 @@
  * \file CGradSmoothing.hpp
  * \brief Declarations and inlines of the numerics class for gradient smoothing.
  * \author T.Dick
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/CNumerics.hpp b/SU2_CFD/include/numerics/CNumerics.hpp
index c2068ef311b..14088f021cd 100644
--- a/SU2_CFD/include/numerics/CNumerics.hpp
+++ b/SU2_CFD/include/numerics/CNumerics.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration of the base numerics class, the
  *        implementation is in the CNumerics.cpp file.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/NEMO/CNEMONumerics.hpp b/SU2_CFD/include/numerics/NEMO/CNEMONumerics.hpp
index 3cdf113f633..895ffb304f9 100644
--- a/SU2_CFD/include/numerics/NEMO/CNEMONumerics.hpp
+++ b/SU2_CFD/include/numerics/NEMO/CNEMONumerics.hpp
@@ -2,7 +2,7 @@
  * \file CNEMONumerics.hpp
  * \brief Base class template NEMO numerics.
  * \author C. Garbacz, W. Maier, S. R. Copeland
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/NEMO/NEMO_diffusion.hpp b/SU2_CFD/include/numerics/NEMO/NEMO_diffusion.hpp
index 88701d0c79d..9acd5cd9d51 100644
--- a/SU2_CFD/include/numerics/NEMO/NEMO_diffusion.hpp
+++ b/SU2_CFD/include/numerics/NEMO/NEMO_diffusion.hpp
@@ -2,7 +2,7 @@
  * \file NEMO_diffusion.hpp
  * \brief Declarations of numerics classes for viscous flux computation.
  * \author S.R. Copeland, W. Maier, C. Garbacz.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -34,7 +34,7 @@
  * \brief Class for computing viscous term using the average of gradients.
  * \ingroup ViscDiscr
  * \author S.R. Copeland, W. Maier, C. Garbacz
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CAvgGrad_NEMO : public CNEMONumerics {
 private:
@@ -90,7 +90,7 @@ class CAvgGrad_NEMO : public CNEMONumerics {
  * \brief Class for computing viscous term using the average of gradients.
  * \ingroup ViscDiscr
  * \author C. Garbacz, W. Maier, S.R. Copeland.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CAvgGradCorrected_NEMO : public CNEMONumerics {
 private:
diff --git a/SU2_CFD/include/numerics/NEMO/NEMO_sources.hpp b/SU2_CFD/include/numerics/NEMO/NEMO_sources.hpp
index 810be475ef3..df11b67212f 100644
--- a/SU2_CFD/include/numerics/NEMO/NEMO_sources.hpp
+++ b/SU2_CFD/include/numerics/NEMO/NEMO_sources.hpp
@@ -2,7 +2,7 @@
  * \file NEMO_sources.hpp
  * \brief Declarations of numerics classes for source-term integration.
  * \author C. Garbacz, W. Maier, S. Copeland.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -34,7 +34,7 @@
  * \brief Class for two-temperature model source terms.
  * \ingroup SourceDiscr
  * \author C. Garbacz, W. Maier, S. Copeland.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CSource_NEMO : public CNEMONumerics {
 private:
diff --git a/SU2_CFD/include/numerics/NEMO/convection/ausm_slau.hpp b/SU2_CFD/include/numerics/NEMO/convection/ausm_slau.hpp
index ce4216a7ffe..0d01c9a37ad 100644
--- a/SU2_CFD/include/numerics/NEMO/convection/ausm_slau.hpp
+++ b/SU2_CFD/include/numerics/NEMO/convection/ausm_slau.hpp
@@ -2,7 +2,7 @@
  * \file ausm_slau.hpp
  * \brief Declaration of numerics classes for the AUSM and SLAU family of schemes in NEMO.
  * \author F. Palacios, S.R. Copeland, W. Maier, C. Garbacz
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/NEMO/convection/lax.hpp b/SU2_CFD/include/numerics/NEMO/convection/lax.hpp
index 421fa2d58e2..ccf44fbfafd 100644
--- a/SU2_CFD/include/numerics/NEMO/convection/lax.hpp
+++ b/SU2_CFD/include/numerics/NEMO/convection/lax.hpp
@@ -2,7 +2,7 @@
  * \file lax.hpp
  * \brief Declaration of numerics classes for Lax centered scheme.
  * \author F. Palacios, S.R. Copeland, W. Maier, C. Garbacz
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/NEMO/convection/msw.hpp b/SU2_CFD/include/numerics/NEMO/convection/msw.hpp
index 5a20de595e6..8968a27ea0a 100644
--- a/SU2_CFD/include/numerics/NEMO/convection/msw.hpp
+++ b/SU2_CFD/include/numerics/NEMO/convection/msw.hpp
@@ -2,7 +2,7 @@
  * \file msw.hpp
  * \brief Declaration of numerics classes for modified Steger-Warming scheme.
  * \author ADL Stanford, S.R. Copeland, W. Maier, C. Garbacz
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -34,7 +34,7 @@
  * \brief Class for solving a flux-vector splitting method by Steger & Warming, modified version.
  * \ingroup ConvDiscr
  * \author ADL Stanford, S.R. Copeland, W. Maier, C. Garbacz
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CUpwMSW_NEMO : public CNEMONumerics {
 private:
diff --git a/SU2_CFD/include/numerics/NEMO/convection/roe.hpp b/SU2_CFD/include/numerics/NEMO/convection/roe.hpp
index d043354c9be..004e0036e08 100644
--- a/SU2_CFD/include/numerics/NEMO/convection/roe.hpp
+++ b/SU2_CFD/include/numerics/NEMO/convection/roe.hpp
@@ -2,7 +2,7 @@
  * \file roe.hpp
  * \brief Declarations of numerics classes for Roe-type schemes in NEMO.
  * \author S.R. Copeland, W. Maier, C. Garbacz
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -34,7 +34,7 @@
  * \brief Class for evaluating the Riemann problem using Roe's scheme for a two-temperature model.
  * \ingroup ConvDiscr
  * \author S. R. Copeland, W. Maier, C. Garbacz
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CUpwRoe_NEMO : public CNEMONumerics {
 private:
diff --git a/SU2_CFD/include/numerics/continuous_adjoint/adj_convection.hpp b/SU2_CFD/include/numerics/continuous_adjoint/adj_convection.hpp
index 0b439dd9d8e..0f619cc3ec3 100644
--- a/SU2_CFD/include/numerics/continuous_adjoint/adj_convection.hpp
+++ b/SU2_CFD/include/numerics/continuous_adjoint/adj_convection.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for continuous adjoint
  *        convective discretization. Implemented in adj_convection.cpp.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/continuous_adjoint/adj_diffusion.hpp b/SU2_CFD/include/numerics/continuous_adjoint/adj_diffusion.hpp
index 3bd89c5f65e..e236a4e1b8b 100644
--- a/SU2_CFD/include/numerics/continuous_adjoint/adj_diffusion.hpp
+++ b/SU2_CFD/include/numerics/continuous_adjoint/adj_diffusion.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for continuous adjoint
  *        diffusion discretization. Implemented in adj_diffusion.cpp.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/continuous_adjoint/adj_sources.hpp b/SU2_CFD/include/numerics/continuous_adjoint/adj_sources.hpp
index 158d7de27df..24b87d49d1a 100644
--- a/SU2_CFD/include/numerics/continuous_adjoint/adj_sources.hpp
+++ b/SU2_CFD/include/numerics/continuous_adjoint/adj_sources.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for continuous adjoint
  *        source term integration. Implemented in adj_sources.cpp.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/elasticity/CFEAElasticity.hpp b/SU2_CFD/include/numerics/elasticity/CFEAElasticity.hpp
index 61ccff82d17..f0f450af2c1 100644
--- a/SU2_CFD/include/numerics/elasticity/CFEAElasticity.hpp
+++ b/SU2_CFD/include/numerics/elasticity/CFEAElasticity.hpp
@@ -2,7 +2,7 @@
  * \file CFEAElasticity.hpp
  * \brief Declaration and inlines of the base class for elasticity problems.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -38,7 +38,7 @@
  *        The methods we override in this class with an empty implementation are here just to better
  *        document the public interface of this class hierarchy.
  * \author R.Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CFEAElasticity : public CNumerics {
 
diff --git a/SU2_CFD/include/numerics/elasticity/CFEALinearElasticity.hpp b/SU2_CFD/include/numerics/elasticity/CFEALinearElasticity.hpp
index 0b39730e8de..a874286ae21 100644
--- a/SU2_CFD/include/numerics/elasticity/CFEALinearElasticity.hpp
+++ b/SU2_CFD/include/numerics/elasticity/CFEALinearElasticity.hpp
@@ -2,7 +2,7 @@
  * \file CFEALinearElasticity.hpp
  * \brief Declaration and inlines of the linear elasticity FE numerics class.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -35,7 +35,7 @@
  * \brief Class for computing the stiffness matrix of a linear, elastic problem.
  * \ingroup Elasticity_Equations
  * \author R.Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CFEALinearElasticity : public CFEAElasticity {
 protected:
@@ -90,7 +90,7 @@ class CFEALinearElasticity : public CFEAElasticity {
  * \brief Particular case of linear elasticity used for mesh deformation.
  * \ingroup Elasticity_Equations
  * \author R.Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CFEAMeshElasticity final : public CFEALinearElasticity {
 
diff --git a/SU2_CFD/include/numerics/elasticity/CFEANonlinearElasticity.hpp b/SU2_CFD/include/numerics/elasticity/CFEANonlinearElasticity.hpp
index f624abf6bf3..4309d9308c3 100644
--- a/SU2_CFD/include/numerics/elasticity/CFEANonlinearElasticity.hpp
+++ b/SU2_CFD/include/numerics/elasticity/CFEANonlinearElasticity.hpp
@@ -2,7 +2,7 @@
  * \file CFEANonlinearElasticity.hpp
  * \brief Declaration and inlines of the nonlinear elasticity FE numerics class.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -37,7 +37,7 @@
  *        Compute_Plane_Stress_Term and Compute_Stress_Tensor.
  * \ingroup Elasticity_Equations
  * \author R.Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CFEANonlinearElasticity : public CFEAElasticity {
 
diff --git a/SU2_CFD/include/numerics/elasticity/nonlinear_models.hpp b/SU2_CFD/include/numerics/elasticity/nonlinear_models.hpp
index 81fc5a7715a..8ff904987d0 100644
--- a/SU2_CFD/include/numerics/elasticity/nonlinear_models.hpp
+++ b/SU2_CFD/include/numerics/elasticity/nonlinear_models.hpp
@@ -2,7 +2,7 @@
  * \file nonlinear_models.hpp
  * \brief Declarations of nonlinear constitutive models.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -35,7 +35,7 @@
  * \brief Class for computing the constitutive and stress tensors for a neo-Hookean material model, compressible.
  * \ingroup Elasticity_Equations
  * \author R.Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CFEM_NeoHookean_Comp final : public CFEANonlinearElasticity {
 
@@ -83,7 +83,7 @@ class CFEM_NeoHookean_Comp final : public CFEANonlinearElasticity {
  * \brief Constitutive and stress tensors for a Knowles stored-energy function, nearly incompressible.
  * \ingroup Elasticity_Equations
  * \author R.Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CFEM_Knowles_NearInc final : public CFEANonlinearElasticity {
 
@@ -134,7 +134,7 @@ class CFEM_Knowles_NearInc final : public CFEANonlinearElasticity {
  * \brief Class for computing the constitutive and stress tensors for a dielectric elastomer.
  * \ingroup Elasticity_Equations
  * \author R.Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CFEM_DielectricElastomer final : public CFEANonlinearElasticity {
 
@@ -182,7 +182,7 @@ class CFEM_DielectricElastomer final : public CFEANonlinearElasticity {
  * \brief Class for computing the constitutive and stress tensors for a nearly-incompressible ideal DE.
  * \ingroup Elasticity_Equations
  * \author R.Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CFEM_IdealDE final : public CFEANonlinearElasticity {
 
diff --git a/SU2_CFD/include/numerics/flow/convection/ausm_slau.hpp b/SU2_CFD/include/numerics/flow/convection/ausm_slau.hpp
index 1dcefbf237a..5fbc59f5c85 100644
--- a/SU2_CFD/include/numerics/flow/convection/ausm_slau.hpp
+++ b/SU2_CFD/include/numerics/flow/convection/ausm_slau.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration of numerics classes for the AUSM family of schemes,
  *        including SLAU. The implementation is in ausm.cpp.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/flow/convection/centered.hpp b/SU2_CFD/include/numerics/flow/convection/centered.hpp
index 3c890b492ce..808ab86bc06 100644
--- a/SU2_CFD/include/numerics/flow/convection/centered.hpp
+++ b/SU2_CFD/include/numerics/flow/convection/centered.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration of numerics classes for centered schemes,
  *        the implementation is in centered.cpp.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/flow/convection/fds.hpp b/SU2_CFD/include/numerics/flow/convection/fds.hpp
index f5c79c7e648..77d155c8509 100644
--- a/SU2_CFD/include/numerics/flow/convection/fds.hpp
+++ b/SU2_CFD/include/numerics/flow/convection/fds.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of classes for Flux-Difference-Spliting schemes,
  *        the implementations are in fds.cpp
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/flow/convection/fvs.hpp b/SU2_CFD/include/numerics/flow/convection/fvs.hpp
index a509a6fcaea..dd8091fa67b 100644
--- a/SU2_CFD/include/numerics/flow/convection/fvs.hpp
+++ b/SU2_CFD/include/numerics/flow/convection/fvs.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of classes for Flux-Vector-Spliting schemes,
  *        the implementations are in fvs.cpp.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/flow/convection/hllc.hpp b/SU2_CFD/include/numerics/flow/convection/hllc.hpp
index f3e2c6e99ce..5765b566101 100644
--- a/SU2_CFD/include/numerics/flow/convection/hllc.hpp
+++ b/SU2_CFD/include/numerics/flow/convection/hllc.hpp
@@ -2,7 +2,7 @@
  * \file hllc.hpp
  * \brief Declaration of HLLC numerics classes, implemented in hllc.cpp.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -34,7 +34,7 @@
  * \brief Class for solving an approximate Riemann HLLC.
  * \ingroup ConvDiscr
  * \author G. Gori, Politecnico di Milano
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CUpwHLLC_Flow final : public CNumerics {
 private:
@@ -86,7 +86,7 @@ class CUpwHLLC_Flow final : public CNumerics {
  * \brief Class for solving an approximate Riemann HLLC.
  * \ingroup ConvDiscr
  * \author G. Gori, Politecnico di Milano
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CUpwGeneralHLLC_Flow final : public CNumerics {
 private:
diff --git a/SU2_CFD/include/numerics/flow/convection/roe.hpp b/SU2_CFD/include/numerics/flow/convection/roe.hpp
index 7b43d1adac3..02c0d6a4236 100644
--- a/SU2_CFD/include/numerics/flow/convection/roe.hpp
+++ b/SU2_CFD/include/numerics/flow/convection/roe.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for Roe-type schemes,
  *        implemented in roe.cpp.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -119,7 +119,7 @@ class CUpwRoe_Flow final : public CUpwRoeBase_Flow {
  * \brief Class for solving an approximate Riemann solver of L2Roe for the flow equations.
  * \ingroup ConvDiscr
  * \author E. Molina, A. Bueno, F. Palacios, P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CUpwL2Roe_Flow final : public CUpwRoeBase_Flow {
 private:
@@ -149,7 +149,7 @@ class CUpwL2Roe_Flow final : public CUpwRoeBase_Flow {
  * \brief Class for solving an approximate Riemann solver of LMRoe for the flow equations.
  * \ingroup ConvDiscr
  * \author E. Molina, A. Bueno, F. Palacios, P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CUpwLMRoe_Flow final : public CUpwRoeBase_Flow {
 private:
diff --git a/SU2_CFD/include/numerics/flow/flow_diffusion.hpp b/SU2_CFD/include/numerics/flow/flow_diffusion.hpp
index ec5da1248a1..4cdcccac404 100644
--- a/SU2_CFD/include/numerics/flow/flow_diffusion.hpp
+++ b/SU2_CFD/include/numerics/flow/flow_diffusion.hpp
@@ -2,7 +2,7 @@
  * \file flow_diffusion.hpp
  * \brief Declarations of numerics classes for viscous flux computation.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/flow/flow_sources.hpp b/SU2_CFD/include/numerics/flow/flow_sources.hpp
index c8efe27d223..39e6bd25d09 100644
--- a/SU2_CFD/include/numerics/flow/flow_sources.hpp
+++ b/SU2_CFD/include/numerics/flow/flow_sources.hpp
@@ -2,7 +2,7 @@
  * \file flow_sources.hpp
  * \brief Declarations of numerics classes for source-term integration.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -177,7 +177,7 @@ class CSourceBodyForce final : public CSourceBase_Flow {
  * \brief Class for the source term integration of a body force in the incompressible solver.
  * \ingroup SourceDiscr
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CSourceIncBodyForce final : public CSourceBase_Flow {
   su2double Body_Force_Vector[3];
@@ -204,7 +204,7 @@ class CSourceIncBodyForce final : public CSourceBase_Flow {
  * \brief Class for the source term integration of the Boussinesq approximation for incompressible flow.
  * \ingroup SourceDiscr
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CSourceBoussinesq final : public CSourceBase_Flow {
   su2double Gravity_Vector[3];
diff --git a/SU2_CFD/include/numerics/heat.hpp b/SU2_CFD/include/numerics/heat.hpp
index 7578a8cb842..5aff4bed14f 100644
--- a/SU2_CFD/include/numerics/heat.hpp
+++ b/SU2_CFD/include/numerics/heat.hpp
@@ -2,7 +2,7 @@
  * \file heat.hpp
  * \brief Declarations of numerics classes for heat transfer problems.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -36,7 +36,7 @@
  * \brief Class for doing a scalar upwind solver for the heat convection equation.
  * \ingroup ConvDiscr
  * \author O. Burghardt.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CUpwSca_Heat final : public CUpwScalar<typename CIncEulerVariable::template CIndices<unsigned short>> {
  public:
@@ -70,7 +70,7 @@ class CUpwSca_Heat final : public CUpwScalar<typename CIncEulerVariable::templat
  * \brief Class for computing viscous term using average of gradients without correction (heat equation).
  * \ingroup ViscDiscr
  * \author O. Burghardt.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CAvgGrad_Heat final : public CAvgGrad_Scalar<CNoFlowIndices> {
  public:
diff --git a/SU2_CFD/include/numerics/radiation.hpp b/SU2_CFD/include/numerics/radiation.hpp
index 92c66dc1004..08adecd8936 100644
--- a/SU2_CFD/include/numerics/radiation.hpp
+++ b/SU2_CFD/include/numerics/radiation.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the classes used to compute
  *        residual terms in radiation problems.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/scalar/scalar_convection.hpp b/SU2_CFD/include/numerics/scalar/scalar_convection.hpp
index cd629510b13..5c4d7fadf5b 100644
--- a/SU2_CFD/include/numerics/scalar/scalar_convection.hpp
+++ b/SU2_CFD/include/numerics/scalar/scalar_convection.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for discretization of
  *        convective fluxes in scalar problems.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/scalar/scalar_diffusion.hpp b/SU2_CFD/include/numerics/scalar/scalar_diffusion.hpp
index 91b55547251..eb615aed053 100644
--- a/SU2_CFD/include/numerics/scalar/scalar_diffusion.hpp
+++ b/SU2_CFD/include/numerics/scalar/scalar_diffusion.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for discretization of
  *        viscous fluxes in scalar problems.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/scalar/scalar_sources.hpp b/SU2_CFD/include/numerics/scalar/scalar_sources.hpp
index e6caa00b4e2..2505ff6af3b 100644
--- a/SU2_CFD/include/numerics/scalar/scalar_sources.hpp
+++ b/SU2_CFD/include/numerics/scalar/scalar_sources.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file scalar_sources.hpp
  * \brief Declarations of numerics classes for integration of source terms in scalar problems.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/species/species_convection.hpp b/SU2_CFD/include/numerics/species/species_convection.hpp
index 4f44cd9c451..df210050ed3 100644
--- a/SU2_CFD/include/numerics/species/species_convection.hpp
+++ b/SU2_CFD/include/numerics/species/species_convection.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for discretization of
  *        convective fluxes in species problems.
  * \author T. Kattmann
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/species/species_diffusion.hpp b/SU2_CFD/include/numerics/species/species_diffusion.hpp
index 7db4d407cd7..afe9a93e61f 100644
--- a/SU2_CFD/include/numerics/species/species_diffusion.hpp
+++ b/SU2_CFD/include/numerics/species/species_diffusion.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for discretization of
  *        viscous fluxes in species problems.
  * \author T. Kattmann
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/species/species_sources.hpp b/SU2_CFD/include/numerics/species/species_sources.hpp
index 87910f37d37..3c1dd09e596 100644
--- a/SU2_CFD/include/numerics/species/species_sources.hpp
+++ b/SU2_CFD/include/numerics/species/species_sources.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for integration of source
  *        terms in species problems.
  * \author T. Kattmann
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/template.hpp b/SU2_CFD/include/numerics/template.hpp
index e80b696e902..aafe52f0b9e 100644
--- a/SU2_CFD/include/numerics/template.hpp
+++ b/SU2_CFD/include/numerics/template.hpp
@@ -5,7 +5,7 @@
  *        new schemes in SU2, in practice you should look for a similar
  *        scheme and try to re-use functionality (not by copy-paste).
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/turbulent/transition/trans_convection.hpp b/SU2_CFD/include/numerics/turbulent/transition/trans_convection.hpp
index b9328d43f63..c48c7556e32 100644
--- a/SU2_CFD/include/numerics/turbulent/transition/trans_convection.hpp
+++ b/SU2_CFD/include/numerics/turbulent/transition/trans_convection.hpp
@@ -3,7 +3,7 @@
  * \brief Delarations of numerics classes for discretization of
  *        convective fluxes in transition problems.
  * \author S. Kang
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/turbulent/transition/trans_correlations.hpp b/SU2_CFD/include/numerics/turbulent/transition/trans_correlations.hpp
index 253e35c4dc4..c429ab764d9 100644
--- a/SU2_CFD/include/numerics/turbulent/transition/trans_correlations.hpp
+++ b/SU2_CFD/include/numerics/turbulent/transition/trans_correlations.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file trans_correlations.hpp
  * \brief Numerics class for the LM model's correlation functions.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/turbulent/transition/trans_diffusion.hpp b/SU2_CFD/include/numerics/turbulent/transition/trans_diffusion.hpp
index d2155a82e93..9a56ccfb82d 100644
--- a/SU2_CFD/include/numerics/turbulent/transition/trans_diffusion.hpp
+++ b/SU2_CFD/include/numerics/turbulent/transition/trans_diffusion.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for discretization of
  *        viscous fluxes in transition problems.
  * \author S. Kang
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/turbulent/transition/trans_sources.hpp b/SU2_CFD/include/numerics/turbulent/transition/trans_sources.hpp
index 3e47e8172e1..715dbbfdb86 100644
--- a/SU2_CFD/include/numerics/turbulent/transition/trans_sources.hpp
+++ b/SU2_CFD/include/numerics/turbulent/transition/trans_sources.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file trans_sources.hpp
  * \brief Numerics classes for integration of source terms in transition problems.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/turbulent/turb_convection.hpp b/SU2_CFD/include/numerics/turbulent/turb_convection.hpp
index 2a6501ff46f..50bd2ff190d 100644
--- a/SU2_CFD/include/numerics/turbulent/turb_convection.hpp
+++ b/SU2_CFD/include/numerics/turbulent/turb_convection.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for discretization of
  *        convective fluxes in turbulence problems.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/turbulent/turb_diffusion.hpp b/SU2_CFD/include/numerics/turbulent/turb_diffusion.hpp
index e1a009a297a..8e1bad1c3b5 100644
--- a/SU2_CFD/include/numerics/turbulent/turb_diffusion.hpp
+++ b/SU2_CFD/include/numerics/turbulent/turb_diffusion.hpp
@@ -3,7 +3,7 @@
  * \brief Declarations of numerics classes for discretization of
  *        viscous fluxes in turbulence problems.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics/turbulent/turb_sources.hpp b/SU2_CFD/include/numerics/turbulent/turb_sources.hpp
index 541383e6dbd..af920cd34c1 100644
--- a/SU2_CFD/include/numerics/turbulent/turb_sources.hpp
+++ b/SU2_CFD/include/numerics/turbulent/turb_sources.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file turb_sources.hpp
  * \brief Numerics classes for integration of source terms in turbulence problems.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics_simd/CNumericsSIMD.cpp b/SU2_CFD/include/numerics_simd/CNumericsSIMD.cpp
index 9b580c0bfbb..a4b64527892 100644
--- a/SU2_CFD/include/numerics_simd/CNumericsSIMD.cpp
+++ b/SU2_CFD/include/numerics_simd/CNumericsSIMD.cpp
@@ -4,7 +4,7 @@
  * \note This should be the only cpp for this family of classes
  * (which are all templates). All compilation takes place here.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics_simd/CNumericsSIMD.hpp b/SU2_CFD/include/numerics_simd/CNumericsSIMD.hpp
index 23116500854..fc242dd3aea 100644
--- a/SU2_CFD/include/numerics_simd/CNumericsSIMD.hpp
+++ b/SU2_CFD/include/numerics_simd/CNumericsSIMD.hpp
@@ -2,7 +2,7 @@
  * \file CNumericsSIMD.hpp
  * \brief Vectorized (SIMD) numerics classes.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics_simd/flow/convection/centered.hpp b/SU2_CFD/include/numerics_simd/flow/convection/centered.hpp
index d3fef128a18..49e03b333e5 100644
--- a/SU2_CFD/include/numerics_simd/flow/convection/centered.hpp
+++ b/SU2_CFD/include/numerics_simd/flow/convection/centered.hpp
@@ -2,7 +2,7 @@
  * \file centered.hpp
  * \brief Centered convective schemes.
  * \author P. Gomes, F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics_simd/flow/convection/common.hpp b/SU2_CFD/include/numerics_simd/flow/convection/common.hpp
index 52219e305bc..6037e2c15e1 100644
--- a/SU2_CFD/include/numerics_simd/flow/convection/common.hpp
+++ b/SU2_CFD/include/numerics_simd/flow/convection/common.hpp
@@ -2,7 +2,7 @@
  * \file common.hpp
  * \brief Common convection-related methods.
  * \author P. Gomes, F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics_simd/flow/convection/roe.hpp b/SU2_CFD/include/numerics_simd/flow/convection/roe.hpp
index caece76b62b..cdb2e091ed8 100644
--- a/SU2_CFD/include/numerics_simd/flow/convection/roe.hpp
+++ b/SU2_CFD/include/numerics_simd/flow/convection/roe.hpp
@@ -2,7 +2,7 @@
  * \file roe.hpp
  * \brief Roe-family of convective schemes.
  * \author P. Gomes, A. Bueno, F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics_simd/flow/diffusion/common.hpp b/SU2_CFD/include/numerics_simd/flow/diffusion/common.hpp
index bf0cd3b513d..1b8ace29209 100644
--- a/SU2_CFD/include/numerics_simd/flow/diffusion/common.hpp
+++ b/SU2_CFD/include/numerics_simd/flow/diffusion/common.hpp
@@ -2,7 +2,7 @@
  * \file common.hpp
  * \brief Helper functions for viscous methods.
  * \author P. Gomes, C. Pederson, A. Bueno, F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics_simd/flow/diffusion/viscous_fluxes.hpp b/SU2_CFD/include/numerics_simd/flow/diffusion/viscous_fluxes.hpp
index 753deb9e1c0..2de5572555e 100644
--- a/SU2_CFD/include/numerics_simd/flow/diffusion/viscous_fluxes.hpp
+++ b/SU2_CFD/include/numerics_simd/flow/diffusion/viscous_fluxes.hpp
@@ -2,7 +2,7 @@
  * \file viscous_fluxes.hpp
  * \brief Decorator classes for computation of viscous fluxes.
  * \author P. Gomes, C. Pederson, A. Bueno, F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics_simd/flow/variables.hpp b/SU2_CFD/include/numerics_simd/flow/variables.hpp
index 9a41722cc0c..380ee975907 100644
--- a/SU2_CFD/include/numerics_simd/flow/variables.hpp
+++ b/SU2_CFD/include/numerics_simd/flow/variables.hpp
@@ -2,7 +2,7 @@
  * \file variables.hpp
  * \brief Collection of types to store physical variables.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/numerics_simd/util.hpp b/SU2_CFD/include/numerics_simd/util.hpp
index 9698804ef63..3a0f8a68841 100644
--- a/SU2_CFD/include/numerics_simd/util.hpp
+++ b/SU2_CFD/include/numerics_simd/util.hpp
@@ -2,7 +2,7 @@
  * \file util.hpp
  * \brief Generic auxiliary functions.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CAdjElasticityOutput.hpp b/SU2_CFD/include/output/CAdjElasticityOutput.hpp
index ec67f09077b..36f0c63b723 100644
--- a/SU2_CFD/include/output/CAdjElasticityOutput.hpp
+++ b/SU2_CFD/include/output/CAdjElasticityOutput.hpp
@@ -2,7 +2,7 @@
  * \file CAdjElasticityOutput.hpp
  * \brief Headers of the adjoint elasticity output class.
  * \author T. Albring, R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CAdjFlowCompOutput.hpp b/SU2_CFD/include/output/CAdjFlowCompOutput.hpp
index 0474657f6c6..36d6655ad92 100644
--- a/SU2_CFD/include/output/CAdjFlowCompOutput.hpp
+++ b/SU2_CFD/include/output/CAdjFlowCompOutput.hpp
@@ -2,7 +2,7 @@
  * \file CAdjFlowCompOutput.hpp
  * \brief Headers of the adjoint compressible flow output.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CAdjFlowIncOutput.hpp b/SU2_CFD/include/output/CAdjFlowIncOutput.hpp
index 98f2ff1c8a2..6ec4b7b3851 100644
--- a/SU2_CFD/include/output/CAdjFlowIncOutput.hpp
+++ b/SU2_CFD/include/output/CAdjFlowIncOutput.hpp
@@ -2,7 +2,7 @@
  * \file CAdjFlowIncOutput.hpp
  * \brief Headers of the adjoint incompressible flow output.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CAdjFlowOutput.hpp b/SU2_CFD/include/output/CAdjFlowOutput.hpp
index ce1a6958c09..18477f28672 100644
--- a/SU2_CFD/include/output/CAdjFlowOutput.hpp
+++ b/SU2_CFD/include/output/CAdjFlowOutput.hpp
@@ -2,7 +2,7 @@
  * \file CAdjFlowOutput.hpp
  * \brief Headers of the adjoint flow output.
  * \author T. Kattmann
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CAdjHeatOutput.hpp b/SU2_CFD/include/output/CAdjHeatOutput.hpp
index af433e6e438..9b995aec1f0 100644
--- a/SU2_CFD/include/output/CAdjHeatOutput.hpp
+++ b/SU2_CFD/include/output/CAdjHeatOutput.hpp
@@ -2,7 +2,7 @@
  * \file CAdjHeatOutput.hpp
  * \brief Headers of the adjoint heat output.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CBaselineOutput.hpp b/SU2_CFD/include/output/CBaselineOutput.hpp
index 02db86324e6..4134972a73a 100644
--- a/SU2_CFD/include/output/CBaselineOutput.hpp
+++ b/SU2_CFD/include/output/CBaselineOutput.hpp
@@ -2,7 +2,7 @@
  * \file CBaselineOutput.hpp
  * \brief  Headers of the baseline output.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CElasticityOutput.hpp b/SU2_CFD/include/output/CElasticityOutput.hpp
index ad052b009f9..2e6581f59db 100644
--- a/SU2_CFD/include/output/CElasticityOutput.hpp
+++ b/SU2_CFD/include/output/CElasticityOutput.hpp
@@ -2,7 +2,7 @@
  * \file CElasticityOutput.hpp
  * \brief  Headers of the elasticity output.
  * \author F. Palacios, T. Economon, M. Colonno
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CFVMOutput.hpp b/SU2_CFD/include/output/CFVMOutput.hpp
index 8512942aa38..f47790e5a8e 100644
--- a/SU2_CFD/include/output/CFVMOutput.hpp
+++ b/SU2_CFD/include/output/CFVMOutput.hpp
@@ -2,7 +2,7 @@
  * \file CFVMOutput.hpp
  * \brief  Headers of the Finite Volume Method output.
  * \author T. Kattmann
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CFlowCompFEMOutput.hpp b/SU2_CFD/include/output/CFlowCompFEMOutput.hpp
index 3444b3e01f8..657551f0caf 100644
--- a/SU2_CFD/include/output/CFlowCompFEMOutput.hpp
+++ b/SU2_CFD/include/output/CFlowCompFEMOutput.hpp
@@ -2,7 +2,7 @@
  * \file CFlowCompFEMOutput.hpp
  * \brief  Headers of the compressible FEM flow output.
  * \author R. Sanchez, T. Albring.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CFlowCompOutput.hpp b/SU2_CFD/include/output/CFlowCompOutput.hpp
index fbf27d36f43..e458e78b161 100644
--- a/SU2_CFD/include/output/CFlowCompOutput.hpp
+++ b/SU2_CFD/include/output/CFlowCompOutput.hpp
@@ -2,7 +2,7 @@
  * \file CFlowCompOutput.hpp
  * \brief  Headers of the compressible flow output.
  * \author R. Sanchez, T. Albring.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CFlowIncOutput.hpp b/SU2_CFD/include/output/CFlowIncOutput.hpp
index 7a8621f25db..caa3197c8bb 100644
--- a/SU2_CFD/include/output/CFlowIncOutput.hpp
+++ b/SU2_CFD/include/output/CFlowIncOutput.hpp
@@ -2,7 +2,7 @@
  * \file CFlowIncOutput.hpp
  * \brief  Headers of the incompressible flow output.
  * \author T. Albring, R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CFlowOutput.hpp b/SU2_CFD/include/output/CFlowOutput.hpp
index a47cae8de2b..c9b63cb1ed6 100644
--- a/SU2_CFD/include/output/CFlowOutput.hpp
+++ b/SU2_CFD/include/output/CFlowOutput.hpp
@@ -2,7 +2,7 @@
  * \file CFlowOutput.hpp
  * \brief  Headers of the flow output.
  * \author F. Palacios, T. Economon, M. Colonno
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CHeatOutput.hpp b/SU2_CFD/include/output/CHeatOutput.hpp
index c488fcf15fa..7c6276a5df3 100644
--- a/SU2_CFD/include/output/CHeatOutput.hpp
+++ b/SU2_CFD/include/output/CHeatOutput.hpp
@@ -2,7 +2,7 @@
  * \file CHeatOutput.hpp
  * \brief Headers of the heat output.
  * \author R. Sanchez, T. Albring.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CMeshOutput.hpp b/SU2_CFD/include/output/CMeshOutput.hpp
index 023cca0420c..7fe2fc5cef9 100644
--- a/SU2_CFD/include/output/CMeshOutput.hpp
+++ b/SU2_CFD/include/output/CMeshOutput.hpp
@@ -2,7 +2,7 @@
  * \file CMeshOutput.hpp
  * \brief Headers of the mesh output.
  * \author R. Sanchez, T. Albring.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CMultizoneOutput.hpp b/SU2_CFD/include/output/CMultizoneOutput.hpp
index abff2d28af1..1057978fb99 100644
--- a/SU2_CFD/include/output/CMultizoneOutput.hpp
+++ b/SU2_CFD/include/output/CMultizoneOutput.hpp
@@ -2,7 +2,7 @@
  * \file CMultizoneOutput.hpp
  * \brief Headers of the main subroutines for screen and history output in multizone problems.
  * \author R. Sanchez, T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/CNEMOCompOutput.hpp b/SU2_CFD/include/output/CNEMOCompOutput.hpp
index 248dc78ced2..eb7c26e099c 100644
--- a/SU2_CFD/include/output/CNEMOCompOutput.hpp
+++ b/SU2_CFD/include/output/CNEMOCompOutput.hpp
@@ -2,7 +2,7 @@
  * \file CNEMOCompOutput.hpp
  * \brief  Headers of the compressible flow output.
  * \author R. Sanchez, W. Maier.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/COutput.hpp b/SU2_CFD/include/output/COutput.hpp
index 2b41909f254..0060e60501f 100644
--- a/SU2_CFD/include/output/COutput.hpp
+++ b/SU2_CFD/include/output/COutput.hpp
@@ -2,7 +2,7 @@
  * \file COutput.hpp
  * \brief Headers of the output class.
  * \author T.Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/COutputFactory.hpp b/SU2_CFD/include/output/COutputFactory.hpp
index 0bfbeaf60ad..1268ff2161d 100644
--- a/SU2_CFD/include/output/COutputFactory.hpp
+++ b/SU2_CFD/include/output/COutputFactory.hpp
@@ -2,7 +2,7 @@
  * \file COutputFactory.hpp
  * \brief Headers of the output class.
  * \author T.Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CCGNSFileWriter.hpp b/SU2_CFD/include/output/filewriter/CCGNSFileWriter.hpp
index 1bbe79b1aa3..4a8ddfa3b98 100644
--- a/SU2_CFD/include/output/filewriter/CCGNSFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CCGNSFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CCGNSFileWriter.hpp
  * \brief Headers for CGNS file writer class.
  * \author G. Baldan
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CCSVFileWriter.hpp b/SU2_CFD/include/output/filewriter/CCSVFileWriter.hpp
index 5858632e7e0..1ef1b905f65 100644
--- a/SU2_CFD/include/output/filewriter/CCSVFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CCSVFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CCSVFileWriter.hpp
  * \brief Headers fo the CSV file writer class.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CFEMDataSorter.hpp b/SU2_CFD/include/output/filewriter/CFEMDataSorter.hpp
index 90fbbb768c4..152abb97dbf 100644
--- a/SU2_CFD/include/output/filewriter/CFEMDataSorter.hpp
+++ b/SU2_CFD/include/output/filewriter/CFEMDataSorter.hpp
@@ -2,7 +2,7 @@
  * \file CFEMDataSorter.hpp
  * \brief Headers fo the FEM data sorter class.
  * \author T. Albring, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CFVMDataSorter.hpp b/SU2_CFD/include/output/filewriter/CFVMDataSorter.hpp
index a227d35eb3f..9a70396f1ad 100644
--- a/SU2_CFD/include/output/filewriter/CFVMDataSorter.hpp
+++ b/SU2_CFD/include/output/filewriter/CFVMDataSorter.hpp
@@ -2,7 +2,7 @@
  * \file CFVMDataSorter.hpp
  * \brief Headers fo the FVM data sorter class.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CFileWriter.hpp b/SU2_CFD/include/output/filewriter/CFileWriter.hpp
index fa551311791..9349e6dc27b 100644
--- a/SU2_CFD/include/output/filewriter/CFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CFileWriter.hpp
  * \brief Headers fo the file writer class.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CParallelDataSorter.hpp b/SU2_CFD/include/output/filewriter/CParallelDataSorter.hpp
index d9a4f0ba7ff..53a98e7ff8c 100644
--- a/SU2_CFD/include/output/filewriter/CParallelDataSorter.hpp
+++ b/SU2_CFD/include/output/filewriter/CParallelDataSorter.hpp
@@ -2,7 +2,7 @@
  * \file CParallelDataSorter.hpp
  * \brief Headers fo the data sorter class.
  * \author T. Albring, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CParaviewBinaryFileWriter.hpp b/SU2_CFD/include/output/filewriter/CParaviewBinaryFileWriter.hpp
index bf3e93e8879..24fdbfb8c1e 100644
--- a/SU2_CFD/include/output/filewriter/CParaviewBinaryFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CParaviewBinaryFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CParaviewBinaryFileWriter.hpp
  * \brief Headers fo paraview binary file writer class.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CParaviewFileWriter.hpp b/SU2_CFD/include/output/filewriter/CParaviewFileWriter.hpp
index 736812abf88..2d87ab3f6fb 100644
--- a/SU2_CFD/include/output/filewriter/CParaviewFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CParaviewFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CParaviewFileWriter.hpp
  * \brief Headers fo the paraview file writer class.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CParaviewVTMFileWriter.hpp b/SU2_CFD/include/output/filewriter/CParaviewVTMFileWriter.hpp
index 51636622128..f80527bb1b4 100644
--- a/SU2_CFD/include/output/filewriter/CParaviewVTMFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CParaviewVTMFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CParaviewVTMFileWriter.hpp
  * \brief Headers fo paraview binary file writer class.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CParaviewXMLFileWriter.hpp b/SU2_CFD/include/output/filewriter/CParaviewXMLFileWriter.hpp
index ab2368defd8..d411993e880 100644
--- a/SU2_CFD/include/output/filewriter/CParaviewXMLFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CParaviewXMLFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CParaviewXMLFileWriter.hpp
  * \brief Headers fo paraview binary file writer class.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CSTLFileWriter.hpp b/SU2_CFD/include/output/filewriter/CSTLFileWriter.hpp
index 5c639dfe241..072aadc1b45 100644
--- a/SU2_CFD/include/output/filewriter/CSTLFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CSTLFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CSTLFileWriter.hpp
  * \brief Headers fo the STL file writer class.
  * \author T. Kattmann, T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -33,7 +33,7 @@
  * \class CSTLFileWriter
  * \brief Class for writing STL output files.
  * \author T. Kattmann, T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CSTLFileWriter final : public CFileWriter{
 private:
diff --git a/SU2_CFD/include/output/filewriter/CSU2BinaryFileWriter.hpp b/SU2_CFD/include/output/filewriter/CSU2BinaryFileWriter.hpp
index 988da36bbc0..d5ae0b76f10 100644
--- a/SU2_CFD/include/output/filewriter/CSU2BinaryFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CSU2BinaryFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CSU2BinaryFileWriter.hpp
  * \brief Headers fo the SU2 binary file writer class.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CSU2FileWriter.hpp b/SU2_CFD/include/output/filewriter/CSU2FileWriter.hpp
index b3edb0ff0bf..8d360e3f7c3 100644
--- a/SU2_CFD/include/output/filewriter/CSU2FileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CSU2FileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CSU2FileWriter.hpp
  * \brief Headers fo the CSV file writer class.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CSU2MeshFileWriter.hpp b/SU2_CFD/include/output/filewriter/CSU2MeshFileWriter.hpp
index 3967be09a28..87910dd88e4 100644
--- a/SU2_CFD/include/output/filewriter/CSU2MeshFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CSU2MeshFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CSU2MeshFileWriter.hpp
  * \brief Headers fo the CSV file writer class.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CSurfaceFEMDataSorter.hpp b/SU2_CFD/include/output/filewriter/CSurfaceFEMDataSorter.hpp
index 51cc27b33b6..fdda43a2d92 100644
--- a/SU2_CFD/include/output/filewriter/CSurfaceFEMDataSorter.hpp
+++ b/SU2_CFD/include/output/filewriter/CSurfaceFEMDataSorter.hpp
@@ -2,7 +2,7 @@
  * \file CSurfaceFEMDataSorter.hpp
  * \brief Headers fo the surface FEM data sorter class.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CSurfaceFVMDataSorter.hpp b/SU2_CFD/include/output/filewriter/CSurfaceFVMDataSorter.hpp
index 636e15d39c4..99c755699e3 100644
--- a/SU2_CFD/include/output/filewriter/CSurfaceFVMDataSorter.hpp
+++ b/SU2_CFD/include/output/filewriter/CSurfaceFVMDataSorter.hpp
@@ -2,7 +2,7 @@
  * \file CSurfaceFVMDataSorter.hpp
  * \brief Headers for the surface FVM data sorter class.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CTecplotBinaryFileWriter.hpp b/SU2_CFD/include/output/filewriter/CTecplotBinaryFileWriter.hpp
index 532b7728fb5..da464f972ef 100644
--- a/SU2_CFD/include/output/filewriter/CTecplotBinaryFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CTecplotBinaryFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CTecplotBinaryFileWriter.hpp
  * \brief Headers fo the tecplot binary writer class.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/filewriter/CTecplotFileWriter.hpp b/SU2_CFD/include/output/filewriter/CTecplotFileWriter.hpp
index 92f2f729772..27b0506a80b 100644
--- a/SU2_CFD/include/output/filewriter/CTecplotFileWriter.hpp
+++ b/SU2_CFD/include/output/filewriter/CTecplotFileWriter.hpp
@@ -2,7 +2,7 @@
  * \file CTecplotFileWriter.hpp
  * \brief Headers fo the tecplot ASCII writer class.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/output/tools/CWindowingTools.hpp b/SU2_CFD/include/output/tools/CWindowingTools.hpp
index 9a6a2e67b65..d3bcec9d29d 100644
--- a/SU2_CFD/include/output/tools/CWindowingTools.hpp
+++ b/SU2_CFD/include/output/tools/CWindowingTools.hpp
@@ -2,7 +2,7 @@
  * \file signal_processing_toolbox.hpp
  * \brief Header file for the signal processing toolbox.
  * \author S. Schotthöfer
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/sgs_model.hpp b/SU2_CFD/include/sgs_model.hpp
index 34e75bdad35..374a3a14010 100644
--- a/SU2_CFD/include/sgs_model.hpp
+++ b/SU2_CFD/include/sgs_model.hpp
@@ -2,7 +2,7 @@
  * \file sgs_model.hpp
  * \brief Headers of the LES subgrid scale models of the SU2 solvers.
  * \author E. van der Weide, T. Economon, P. Urbanczyk
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -38,7 +38,7 @@ using namespace std;
  * \class CSGSModel
  * \brief Base class for defining the LES subgrid scale model.
  * \author: E. van der Weide, T. Economon, P. Urbanczyk
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CSGSModel {
 
@@ -224,7 +224,7 @@ class CSGSModel {
  * \class CSmagorinskyModel
  * \brief Derived class for defining the Smagorinsky SGS model.
  * \author: E. van der Weide, T. Economon, P. Urbanczyk
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CSmagorinskyModel : public CSGSModel {
 
@@ -413,7 +413,7 @@ class CSmagorinskyModel : public CSGSModel {
  * \class CWALEModel
  * \brief Derived class for defining the WALE SGS model.
  * \author: E. van der Weide, T. Economon, P. Urbanczyk
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CWALEModel : public CSGSModel {
 
@@ -601,7 +601,7 @@ class CWALEModel : public CSGSModel {
  * \class CVremanModel
  * \brief Derived class for defining the WALE SGS model.
  * \author: E. van der Weide, T. Economon, P. Urbanczyk, E. Molina
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CVremanModel : public CSGSModel {
 
diff --git a/SU2_CFD/include/sgs_model.inl b/SU2_CFD/include/sgs_model.inl
index 1c3023782e7..55af9414684 100644
--- a/SU2_CFD/include/sgs_model.inl
+++ b/SU2_CFD/include/sgs_model.inl
@@ -2,7 +2,7 @@
  * \file sgs_model.inl
  * \brief In-Line subroutines of the <i>sgs_model.hpp</i> file.
  * \author E. van der Weide, T. Economon, P. Urbanczyk
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CAdjEulerSolver.hpp b/SU2_CFD/include/solvers/CAdjEulerSolver.hpp
index 79e0dc20701..97e46646b9d 100644
--- a/SU2_CFD/include/solvers/CAdjEulerSolver.hpp
+++ b/SU2_CFD/include/solvers/CAdjEulerSolver.hpp
@@ -2,7 +2,7 @@
  * \file CAdjEulerSolver.hpp
  * \brief Headers of the CAdjEulerSolver class
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CAdjNSSolver.hpp b/SU2_CFD/include/solvers/CAdjNSSolver.hpp
index 9f1ada35c44..22c8246b71b 100644
--- a/SU2_CFD/include/solvers/CAdjNSSolver.hpp
+++ b/SU2_CFD/include/solvers/CAdjNSSolver.hpp
@@ -2,7 +2,7 @@
  * \file CAdjNSSolver.hpp
  * \brief Headers of the CAdjNSSolver class
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CAdjTurbSolver.hpp b/SU2_CFD/include/solvers/CAdjTurbSolver.hpp
index d5eee6c5d39..aa45ea72eee 100644
--- a/SU2_CFD/include/solvers/CAdjTurbSolver.hpp
+++ b/SU2_CFD/include/solvers/CAdjTurbSolver.hpp
@@ -2,7 +2,7 @@
  * \file CAdjTurbSolver.hpp
  * \brief Headers of the CAdjTurbSolver class
  * \author F. Palacios, A. Bueno.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CBaselineSolver.hpp b/SU2_CFD/include/solvers/CBaselineSolver.hpp
index e2747f94af3..45d76a22489 100644
--- a/SU2_CFD/include/solvers/CBaselineSolver.hpp
+++ b/SU2_CFD/include/solvers/CBaselineSolver.hpp
@@ -2,7 +2,7 @@
  * \file CBaslineSolver.hpp
  * \brief Headers of the CBaselineSolver class
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CBaselineSolver_FEM.hpp b/SU2_CFD/include/solvers/CBaselineSolver_FEM.hpp
index 216efa3249d..f831d2cee9d 100644
--- a/SU2_CFD/include/solvers/CBaselineSolver_FEM.hpp
+++ b/SU2_CFD/include/solvers/CBaselineSolver_FEM.hpp
@@ -2,7 +2,7 @@
  * \file CBaslineSolver_FEM.hpp
  * \brief Headers of the CBaselineSolver class
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -31,7 +31,7 @@
  * \class CBaselineSolver_FEM
  * \brief Main class for defining a baseline solution from a restart file for the DG-FEM solver output.
  * \author T. Economon.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CBaselineSolver_FEM final : public CSolver {
 protected:
diff --git a/SU2_CFD/include/solvers/CDiscAdjFEASolver.hpp b/SU2_CFD/include/solvers/CDiscAdjFEASolver.hpp
index 2755731f5a7..296500b6112 100644
--- a/SU2_CFD/include/solvers/CDiscAdjFEASolver.hpp
+++ b/SU2_CFD/include/solvers/CDiscAdjFEASolver.hpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjFEASolver.hpp
  * \brief Headers of the CDiscAdjFEASolver class
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CDiscAdjMeshSolver.hpp b/SU2_CFD/include/solvers/CDiscAdjMeshSolver.hpp
index 20bb3ac28c5..7505ae5275d 100644
--- a/SU2_CFD/include/solvers/CDiscAdjMeshSolver.hpp
+++ b/SU2_CFD/include/solvers/CDiscAdjMeshSolver.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to compute the
  *        the discrete adjoint of the linear-elastic mesh solver.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CDiscAdjSolver.hpp b/SU2_CFD/include/solvers/CDiscAdjSolver.hpp
index 0b4488ba9f3..7ea1653b1f1 100644
--- a/SU2_CFD/include/solvers/CDiscAdjSolver.hpp
+++ b/SU2_CFD/include/solvers/CDiscAdjSolver.hpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjSolver.hpp
  * \brief Headers of the CDiscAdjSolver class
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CEulerSolver.hpp b/SU2_CFD/include/solvers/CEulerSolver.hpp
index eecc7a292a0..04b49d9c523 100644
--- a/SU2_CFD/include/solvers/CEulerSolver.hpp
+++ b/SU2_CFD/include/solvers/CEulerSolver.hpp
@@ -2,7 +2,7 @@
  * \file CEulerSolver.hpp
  * \brief Headers of the CEulerSolver class
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CFEASolver.hpp b/SU2_CFD/include/solvers/CFEASolver.hpp
index 86eb0813e6a..81465f94d01 100644
--- a/SU2_CFD/include/solvers/CFEASolver.hpp
+++ b/SU2_CFD/include/solvers/CFEASolver.hpp
@@ -2,7 +2,7 @@
  * \file CFEASolver.hpp
  * \brief Finite element solver for elasticity problems.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CFEASolverBase.hpp b/SU2_CFD/include/solvers/CFEASolverBase.hpp
index 6a94f8aaa8b..83fe976ffa9 100644
--- a/SU2_CFD/include/solvers/CFEASolverBase.hpp
+++ b/SU2_CFD/include/solvers/CFEASolverBase.hpp
@@ -2,7 +2,7 @@
  * \file CFEASolver.hpp
  * \brief Base class template for all FEA solvers using the SU2 internal finite elements.
  * \author T. Dick
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CFEM_DG_EulerSolver.hpp b/SU2_CFD/include/solvers/CFEM_DG_EulerSolver.hpp
index 87a30af9ce3..48c1e373eeb 100644
--- a/SU2_CFD/include/solvers/CFEM_DG_EulerSolver.hpp
+++ b/SU2_CFD/include/solvers/CFEM_DG_EulerSolver.hpp
@@ -2,7 +2,7 @@
  * \file CFEM_DG_EulerSolver.hpp
  * \brief Headers of the CFEM_DG_EulerSolver class
  * \author E. van der Weide, T. Economon, J. Alonso
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -35,7 +35,7 @@
  * \brief Main class for defining the Euler Discontinuous Galerkin finite element flow solver.
  * \ingroup Euler_Equations
  * \author E. van der Weide, T. Economon, J. Alonso
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CFEM_DG_EulerSolver : public CSolver {
 protected:
diff --git a/SU2_CFD/include/solvers/CFEM_DG_NSSolver.hpp b/SU2_CFD/include/solvers/CFEM_DG_NSSolver.hpp
index da9e533cbbb..4a270d16b76 100644
--- a/SU2_CFD/include/solvers/CFEM_DG_NSSolver.hpp
+++ b/SU2_CFD/include/solvers/CFEM_DG_NSSolver.hpp
@@ -2,7 +2,7 @@
  * \file CFEM_DG_NSSolver.hpp
  * \brief Headers of the CFEM_DG_NSSolver class
  * \author E. van der Weide, T. Economon, J. Alonso
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -35,7 +35,7 @@
  * \brief Main class for defining the Navier-Stokes Discontinuous Galerkin finite element flow solver.
  * \ingroup Navier_Stokes_Equations
  * \author E. van der Weide, T. Economon, J. Alonso
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CFEM_DG_NSSolver final : public CFEM_DG_EulerSolver {
 private:
diff --git a/SU2_CFD/include/solvers/CFVMFlowSolverBase.hpp b/SU2_CFD/include/solvers/CFVMFlowSolverBase.hpp
index b1dc8b8a308..6953dd1bc59 100644
--- a/SU2_CFD/include/solvers/CFVMFlowSolverBase.hpp
+++ b/SU2_CFD/include/solvers/CFVMFlowSolverBase.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file CFVMFlowSolverBase.hpp
  * \brief Base class template for all FVM flow solvers.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CFVMFlowSolverBase.inl b/SU2_CFD/include/solvers/CFVMFlowSolverBase.inl
index bab8f187cae..40af46827be 100644
--- a/SU2_CFD/include/solvers/CFVMFlowSolverBase.inl
+++ b/SU2_CFD/include/solvers/CFVMFlowSolverBase.inl
@@ -1,7 +1,7 @@
 /*!
  * \file CFVMFlowSolverBase.inl
  * \brief Base class template for all FVM flow solvers.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CGradientSmoothingSolver.hpp b/SU2_CFD/include/solvers/CGradientSmoothingSolver.hpp
index a594aef11e7..4ff452ef94e 100644
--- a/SU2_CFD/include/solvers/CGradientSmoothingSolver.hpp
+++ b/SU2_CFD/include/solvers/CGradientSmoothingSolver.hpp
@@ -2,7 +2,7 @@
  * \file CGradientSmoothingSolver.hpp
  * \brief SOlver class for Sobolev smoothing of sensitivities.
  * \author T. Dick
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CHeatSolver.hpp b/SU2_CFD/include/solvers/CHeatSolver.hpp
index ce97728dad6..cbce9cd622e 100644
--- a/SU2_CFD/include/solvers/CHeatSolver.hpp
+++ b/SU2_CFD/include/solvers/CHeatSolver.hpp
@@ -2,7 +2,7 @@
  * \file CHeatSolver.hpp
  * \brief Headers of the CHeatSolver class
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -34,7 +34,7 @@
  * \class CHeatSolver
  * \brief Main class for defining the finite-volume heat solver.
  * \author O. Burghardt
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CHeatSolver final : public CScalarSolver<CHeatVariable> {
 protected:
diff --git a/SU2_CFD/include/solvers/CIncEulerSolver.hpp b/SU2_CFD/include/solvers/CIncEulerSolver.hpp
index 818ffb6bdd2..972d49f6413 100644
--- a/SU2_CFD/include/solvers/CIncEulerSolver.hpp
+++ b/SU2_CFD/include/solvers/CIncEulerSolver.hpp
@@ -2,7 +2,7 @@
  * \file CIncEulerSolver.hpp
  * \brief Headers of the CIncEulerSolver class
  * \author F. Palacios, T. Economon, T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CIncNSSolver.hpp b/SU2_CFD/include/solvers/CIncNSSolver.hpp
index 1c3a3588799..7827458f4dd 100644
--- a/SU2_CFD/include/solvers/CIncNSSolver.hpp
+++ b/SU2_CFD/include/solvers/CIncNSSolver.hpp
@@ -2,7 +2,7 @@
  * \file CIncNSSolver.hpp
  * \brief Headers of the CIncNSSolver class
  * \author F. Palacios, T. Economon, T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CMeshSolver.hpp b/SU2_CFD/include/solvers/CMeshSolver.hpp
index 79876e016c1..852066ad643 100644
--- a/SU2_CFD/include/solvers/CMeshSolver.hpp
+++ b/SU2_CFD/include/solvers/CMeshSolver.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to compute the deformation of
  *        the volumetric numerical grid using the linear elasticity solver.
  * \author Ruben Sanchez, based on CVolumetricMovement developments (F. Palacios, A. Bueno, T. Economon, S. Padron)
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CNEMOEulerSolver.hpp b/SU2_CFD/include/solvers/CNEMOEulerSolver.hpp
index 268b7a9bbc0..5369647e6bf 100644
--- a/SU2_CFD/include/solvers/CNEMOEulerSolver.hpp
+++ b/SU2_CFD/include/solvers/CNEMOEulerSolver.hpp
@@ -2,7 +2,7 @@
  * \file CNEMOEulerSolver.hpp
  * \brief Headers of the CNEMOEulerSolver class
  * \author S. R. Copeland, F. Palacios, W. Maier.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -36,7 +36,7 @@
  * \brief Main class for defining the NEMO Euler's flow solver.
  * \ingroup Euler_Equations
  * \author S. R. Copeland, F. Palacios, W. Maier.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CNEMOEulerSolver : public CFVMFlowSolverBase<CNEMOEulerVariable, ENUM_REGIME::COMPRESSIBLE> {
 protected:
diff --git a/SU2_CFD/include/solvers/CNEMONSSolver.hpp b/SU2_CFD/include/solvers/CNEMONSSolver.hpp
index 4368c20c5cc..0f120901e46 100644
--- a/SU2_CFD/include/solvers/CNEMONSSolver.hpp
+++ b/SU2_CFD/include/solvers/CNEMONSSolver.hpp
@@ -2,7 +2,7 @@
  * \file CNEMONSSolver.hpp
  * \brief Headers of the CNEMONSSolver class
  * \author S. R. Copeland, F. Palacios, W. Maier.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CNSSolver.hpp b/SU2_CFD/include/solvers/CNSSolver.hpp
index 1b1321c4fb6..bea8562388e 100644
--- a/SU2_CFD/include/solvers/CNSSolver.hpp
+++ b/SU2_CFD/include/solvers/CNSSolver.hpp
@@ -2,7 +2,7 @@
  * \file CNSSolver.hpp
  * \brief Headers of the CNSSolver class
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CRadP1Solver.hpp b/SU2_CFD/include/solvers/CRadP1Solver.hpp
index f1130481973..aeea803c4fe 100644
--- a/SU2_CFD/include/solvers/CRadP1Solver.hpp
+++ b/SU2_CFD/include/solvers/CRadP1Solver.hpp
@@ -2,7 +2,7 @@
  * \file CRadP1Solver.hpp
  * \brief Declaration and inlines of the class to compute a P1 radiation problem.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CRadSolver.hpp b/SU2_CFD/include/solvers/CRadSolver.hpp
index 3e41bbdb5d2..034c9a3c9de 100644
--- a/SU2_CFD/include/solvers/CRadSolver.hpp
+++ b/SU2_CFD/include/solvers/CRadSolver.hpp
@@ -2,7 +2,7 @@
  * \file CRadSolver.hpp
  * \brief Declaration and inlines of the class to compute a generic radiation solver.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CScalarSolver.hpp b/SU2_CFD/include/solvers/CScalarSolver.hpp
index fd217446b1e..bd854d4e51c 100644
--- a/SU2_CFD/include/solvers/CScalarSolver.hpp
+++ b/SU2_CFD/include/solvers/CScalarSolver.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file CScalarSolver.hpp
  * \brief Headers of the CScalarSolver class
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CScalarSolver.inl b/SU2_CFD/include/solvers/CScalarSolver.inl
index 0f4ab4baf57..5b6415d65b0 100644
--- a/SU2_CFD/include/solvers/CScalarSolver.inl
+++ b/SU2_CFD/include/solvers/CScalarSolver.inl
@@ -1,7 +1,7 @@
 /*!
  * \file CScalarSolver.inl
  * \brief Main subroutines of CScalarSolver class
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CSolver.hpp b/SU2_CFD/include/solvers/CSolver.hpp
index 06cd950aa13..44eb07c3465 100644
--- a/SU2_CFD/include/solvers/CSolver.hpp
+++ b/SU2_CFD/include/solvers/CSolver.hpp
@@ -2,7 +2,7 @@
  * \file CSolver.hpp
  * \brief Headers of the CSolver class which is inherited by all of the other solvers
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CSolverFactory.hpp b/SU2_CFD/include/solvers/CSolverFactory.hpp
index bdf8300619f..ab8d757c280 100644
--- a/SU2_CFD/include/solvers/CSolverFactory.hpp
+++ b/SU2_CFD/include/solvers/CSolverFactory.hpp
@@ -2,7 +2,7 @@
  * \file CSolverFactory.hpp
  * \brief Headers of the CSolverFactory class
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp b/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp
index 514a3c9a863..f3a957dbc42 100644
--- a/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp
+++ b/SU2_CFD/include/solvers/CSpeciesFlameletSolver.hpp
@@ -2,7 +2,7 @@
  * \file CSpeciesFlameletSolver.hpp
  * \brief Headers of the CSpeciesFlameletSolver class
  * \author D. Mayer, N. Beishuizen, T. Economon, E. Bunschoten
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CSpeciesSolver.hpp b/SU2_CFD/include/solvers/CSpeciesSolver.hpp
index 1d4eef366de..5b78696d9ac 100644
--- a/SU2_CFD/include/solvers/CSpeciesSolver.hpp
+++ b/SU2_CFD/include/solvers/CSpeciesSolver.hpp
@@ -2,7 +2,7 @@
  * \file CSpeciesSolver.hpp
  * \brief Headers of the CSpeciesSolver class
  * \author T. Kattmann.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CTemplateSolver.hpp b/SU2_CFD/include/solvers/CTemplateSolver.hpp
index 4e61f0d55a2..0083cf778fb 100644
--- a/SU2_CFD/include/solvers/CTemplateSolver.hpp
+++ b/SU2_CFD/include/solvers/CTemplateSolver.hpp
@@ -2,7 +2,7 @@
  * \file CTemplateSolver.hpp
  * \brief Headers of the CTemplateSolver class
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CTransLMSolver.hpp b/SU2_CFD/include/solvers/CTransLMSolver.hpp
index 039fb94aa0f..613be3b6da6 100644
--- a/SU2_CFD/include/solvers/CTransLMSolver.hpp
+++ b/SU2_CFD/include/solvers/CTransLMSolver.hpp
@@ -2,7 +2,7 @@
  * \file CTransLMSolver.hpp
  * \brief Headers of the CTransLMSolver class
  * \author A. Aranake
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CTurbSASolver.hpp b/SU2_CFD/include/solvers/CTurbSASolver.hpp
index 9cf498c59aa..35f403b13c1 100644
--- a/SU2_CFD/include/solvers/CTurbSASolver.hpp
+++ b/SU2_CFD/include/solvers/CTurbSASolver.hpp
@@ -2,7 +2,7 @@
  * \file CTurbSASolver.hpp
  * \brief Headers of the CTurbSASolver class
  * \author A. Bueno.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CTurbSSTSolver.hpp b/SU2_CFD/include/solvers/CTurbSSTSolver.hpp
index 23b202a6c10..6dbed05fd9d 100644
--- a/SU2_CFD/include/solvers/CTurbSSTSolver.hpp
+++ b/SU2_CFD/include/solvers/CTurbSSTSolver.hpp
@@ -2,7 +2,7 @@
  * \file CTurbSSTSolver.hpp
  * \brief Headers of the CTurbSSTSolver class
  * \author A. Campos, F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/solvers/CTurbSolver.hpp b/SU2_CFD/include/solvers/CTurbSolver.hpp
index 9a0341a942f..b1a46887617 100644
--- a/SU2_CFD/include/solvers/CTurbSolver.hpp
+++ b/SU2_CFD/include/solvers/CTurbSolver.hpp
@@ -2,7 +2,7 @@
  * \file CTurbSolver.hpp
  * \brief Headers of the CTurbSolver class
  * \author A. Bueno.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/task_definition.hpp b/SU2_CFD/include/task_definition.hpp
index 4706be540be..ee97b080141 100644
--- a/SU2_CFD/include/task_definition.hpp
+++ b/SU2_CFD/include/task_definition.hpp
@@ -2,7 +2,7 @@
  * \file task_definition.hpp
  * \brief Header of the task definition class for the SU2 solvers.
  * \author E. van der Weide, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -37,7 +37,7 @@ using namespace std;
  * \class CTaskDefinition
  * \brief Class for defining a task to be carried out
  * \author: E. van der Weide, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CTaskDefinition {
 
diff --git a/SU2_CFD/include/task_definition.inl b/SU2_CFD/include/task_definition.inl
index 0a50f212f49..5d9d9e939f7 100644
--- a/SU2_CFD/include/task_definition.inl
+++ b/SU2_CFD/include/task_definition.inl
@@ -2,7 +2,7 @@
  * \file task_definition.inl
  * \brief In-Line subroutines of the <i>task_definition.hpp</i> file.
  * \author E. van der Weide, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CAdjEulerVariable.hpp b/SU2_CFD/include/variables/CAdjEulerVariable.hpp
index 9cd33a3d1ef..4d00e9a5b1b 100644
--- a/SU2_CFD/include/variables/CAdjEulerVariable.hpp
+++ b/SU2_CFD/include/variables/CAdjEulerVariable.hpp
@@ -2,7 +2,7 @@
  * \file CAdjEulerVariable.hpp
  * \brief Main class for defining the variables of the adjoint Euler solver.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CAdjNSVariable.hpp b/SU2_CFD/include/variables/CAdjNSVariable.hpp
index 7d0a81e0702..f5f6c996bb6 100644
--- a/SU2_CFD/include/variables/CAdjNSVariable.hpp
+++ b/SU2_CFD/include/variables/CAdjNSVariable.hpp
@@ -2,7 +2,7 @@
  * \file CAdjNSVariable.hpp
  * \brief Main class for defining the variables of the adjoint Navier-Stokes solver.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CAdjTurbVariable.hpp b/SU2_CFD/include/variables/CAdjTurbVariable.hpp
index 9afb2c4550b..30620b8b084 100644
--- a/SU2_CFD/include/variables/CAdjTurbVariable.hpp
+++ b/SU2_CFD/include/variables/CAdjTurbVariable.hpp
@@ -2,7 +2,7 @@
  * \file CAdjTurbVariable.hpp
  * \brief Main class for defining the variables of the adjoint turbulence model.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CBaselineVariable.hpp b/SU2_CFD/include/variables/CBaselineVariable.hpp
index 68912d4b2a3..03c60788972 100644
--- a/SU2_CFD/include/variables/CBaselineVariable.hpp
+++ b/SU2_CFD/include/variables/CBaselineVariable.hpp
@@ -2,7 +2,7 @@
  * \file CBaselineVariable.hpp
  * \brief Main class for defining the variables of a baseline solution from a restart file (for output).
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CDiscAdjFEABoundVariable.hpp b/SU2_CFD/include/variables/CDiscAdjFEABoundVariable.hpp
index 35f8738d951..e77c33d8898 100644
--- a/SU2_CFD/include/variables/CDiscAdjFEABoundVariable.hpp
+++ b/SU2_CFD/include/variables/CDiscAdjFEABoundVariable.hpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjFEABoundVariable.hpp
  * \brief Main class for defining the variables of the adjoint FEA solver at the boundary.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -35,7 +35,7 @@
  * \ingroup DiscAdj
  * \brief Main class for defining the variables on the FEA boundaries for adjoint applications.
  * \author R. Sanchez.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CDiscAdjFEABoundVariable final : public CDiscAdjVariable {
 private:
diff --git a/SU2_CFD/include/variables/CDiscAdjMeshBoundVariable.hpp b/SU2_CFD/include/variables/CDiscAdjMeshBoundVariable.hpp
index 88aa26cf1a0..f889f48c38a 100644
--- a/SU2_CFD/include/variables/CDiscAdjMeshBoundVariable.hpp
+++ b/SU2_CFD/include/variables/CDiscAdjMeshBoundVariable.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class
  *        to define the adjoint variables of the mesh movement.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CDiscAdjVariable.hpp b/SU2_CFD/include/variables/CDiscAdjVariable.hpp
index bc72508de78..5dba843fdfe 100644
--- a/SU2_CFD/include/variables/CDiscAdjVariable.hpp
+++ b/SU2_CFD/include/variables/CDiscAdjVariable.hpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjVariable.hpp
  * \brief Main class for defining the variables of the adjoint solver.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CEulerVariable.hpp b/SU2_CFD/include/variables/CEulerVariable.hpp
index 9f4fef32a82..e9445674273 100644
--- a/SU2_CFD/include/variables/CEulerVariable.hpp
+++ b/SU2_CFD/include/variables/CEulerVariable.hpp
@@ -2,7 +2,7 @@
  * \file CEulerVariable.hpp
  * \brief Class for defining the variables of the compressible Euler solver.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CFEABoundVariable.hpp b/SU2_CFD/include/variables/CFEABoundVariable.hpp
index cdac1cdd476..43f3ca6602e 100644
--- a/SU2_CFD/include/variables/CFEABoundVariable.hpp
+++ b/SU2_CFD/include/variables/CFEABoundVariable.hpp
@@ -2,7 +2,7 @@
  * \file CFEABoundVariable.hpp
  * \brief Class for defining the variables on the FEA boundaries for FSI applications.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -37,7 +37,7 @@
  * A map is constructed so that variables can be referenced by iPoint instead of iVertex.
  * \ingroup Structural Finite Element Analysis Variables
  * \author R. Sanchez.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CFEABoundVariable final : public CFEAVariable {
 protected:
diff --git a/SU2_CFD/include/variables/CFEAVariable.hpp b/SU2_CFD/include/variables/CFEAVariable.hpp
index 6d3ea11a633..0a353a7a04f 100644
--- a/SU2_CFD/include/variables/CFEAVariable.hpp
+++ b/SU2_CFD/include/variables/CFEAVariable.hpp
@@ -2,7 +2,7 @@
  * \file CFEAVariable.hpp
  * \brief Class for defining the variables of the FEM structural problem.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -34,7 +34,7 @@
  * \brief Class for defining the variables of the FEM structural problem.
  * \ingroup Structural Finite Element Analysis Variables
  * \author F. Palacios, R. Sanchez.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CFEAVariable : public CVariable {
 protected:
diff --git a/SU2_CFD/include/variables/CFlowVariable.hpp b/SU2_CFD/include/variables/CFlowVariable.hpp
index a6937fcf586..d13c386456b 100644
--- a/SU2_CFD/include/variables/CFlowVariable.hpp
+++ b/SU2_CFD/include/variables/CFlowVariable.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file CFlowVariable.hpp
  * \brief Class for defining the common variables of flow solvers.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CHeatVariable.hpp b/SU2_CFD/include/variables/CHeatVariable.hpp
index 4bc2d0c1909..4192b85508d 100644
--- a/SU2_CFD/include/variables/CHeatVariable.hpp
+++ b/SU2_CFD/include/variables/CHeatVariable.hpp
@@ -2,7 +2,7 @@
  * \file CHeatVariable.hpp
  * \brief Class for defining the variables of the finite-volume heat equation solver.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -33,7 +33,7 @@
  * \class CHeatVariable
  * \brief Class for defining the variables of the finite-volume heat equation solver.
  * \author O. Burghardt
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  */
 class CHeatVariable final : public CScalarVariable {
 public:
diff --git a/SU2_CFD/include/variables/CIncEulerVariable.hpp b/SU2_CFD/include/variables/CIncEulerVariable.hpp
index 16b33d52e84..f72e2ef9c69 100644
--- a/SU2_CFD/include/variables/CIncEulerVariable.hpp
+++ b/SU2_CFD/include/variables/CIncEulerVariable.hpp
@@ -2,7 +2,7 @@
  * \file CIncEulerVariable.hpp
  * \brief Class for defining the variables of the incompressible Euler solver.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CIncNSVariable.hpp b/SU2_CFD/include/variables/CIncNSVariable.hpp
index 9a561e1e70c..a5b42a512cc 100644
--- a/SU2_CFD/include/variables/CIncNSVariable.hpp
+++ b/SU2_CFD/include/variables/CIncNSVariable.hpp
@@ -3,7 +3,7 @@
  * \brief Class for defining the variables of the incompressible
           Navier-Stokes solver.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CMeshBoundVariable.hpp b/SU2_CFD/include/variables/CMeshBoundVariable.hpp
index b57ce56e6da..3b26d60ac37 100644
--- a/SU2_CFD/include/variables/CMeshBoundVariable.hpp
+++ b/SU2_CFD/include/variables/CMeshBoundVariable.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class
  *        to define the variables of the mesh movement at the moving boundaries.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CMeshElement.hpp b/SU2_CFD/include/variables/CMeshElement.hpp
index c166356c2ce..eda6615ef29 100644
--- a/SU2_CFD/include/variables/CMeshElement.hpp
+++ b/SU2_CFD/include/variables/CMeshElement.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class
  *        to define the variables of the mesh movement.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CMeshVariable.hpp b/SU2_CFD/include/variables/CMeshVariable.hpp
index ce3a807885c..145cbc81968 100644
--- a/SU2_CFD/include/variables/CMeshVariable.hpp
+++ b/SU2_CFD/include/variables/CMeshVariable.hpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class
  *        to define the variables of the mesh movement.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CNEMOEulerVariable.hpp b/SU2_CFD/include/variables/CNEMOEulerVariable.hpp
index 246d24bf7db..d41ae5e73e1 100644
--- a/SU2_CFD/include/variables/CNEMOEulerVariable.hpp
+++ b/SU2_CFD/include/variables/CNEMOEulerVariable.hpp
@@ -2,7 +2,7 @@
  * \file CNEMOEulerVariable.hpp
  * \brief Class for defining the variables of the compressible NEMO Euler solver.
  * \author C. Garbacz, W. Maier, S.R. Copeland
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CNEMONSVariable.hpp b/SU2_CFD/include/variables/CNEMONSVariable.hpp
index 4166590068f..a54291fb0b7 100644
--- a/SU2_CFD/include/variables/CNEMONSVariable.hpp
+++ b/SU2_CFD/include/variables/CNEMONSVariable.hpp
@@ -2,7 +2,7 @@
  * \file CNEMONSVariable.hpp
  * \brief Class for defining the variables of the compressible NEMO Navier-Stokes solver.
  * \author C. Garbacz, W. Maier, S.R. Copeland.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CNSVariable.hpp b/SU2_CFD/include/variables/CNSVariable.hpp
index 116b06ad6d3..d23b7a16eb4 100644
--- a/SU2_CFD/include/variables/CNSVariable.hpp
+++ b/SU2_CFD/include/variables/CNSVariable.hpp
@@ -2,7 +2,7 @@
  * \file CNSVariable.hpp
  * \brief Class for defining the variables of the compressible Navier-Stokes solver.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CPrimitiveIndices.hpp b/SU2_CFD/include/variables/CPrimitiveIndices.hpp
index 77878eff6cb..1ffbaa341f6 100644
--- a/SU2_CFD/include/variables/CPrimitiveIndices.hpp
+++ b/SU2_CFD/include/variables/CPrimitiveIndices.hpp
@@ -1,7 +1,7 @@
 /*!
  * \file CPrimitiveIndices.hpp
  * \brief Abstract representation of flow primitive variable indices that tries to be efficient.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CRadP1Variable.hpp b/SU2_CFD/include/variables/CRadP1Variable.hpp
index 0594e8e29f9..bcfd89f9a31 100644
--- a/SU2_CFD/include/variables/CRadP1Variable.hpp
+++ b/SU2_CFD/include/variables/CRadP1Variable.hpp
@@ -2,7 +2,7 @@
  * \file CRadP1Variable.hpp
  * \brief Class for defining the variables of the P1 radiation model.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CRadVariable.hpp b/SU2_CFD/include/variables/CRadVariable.hpp
index d0c38df88c3..1fa9c735b7c 100644
--- a/SU2_CFD/include/variables/CRadVariable.hpp
+++ b/SU2_CFD/include/variables/CRadVariable.hpp
@@ -2,7 +2,7 @@
  * \file CRadVariable.hpp
  * \brief Class for defining the variables of the radiation solver.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CScalarVariable.hpp b/SU2_CFD/include/variables/CScalarVariable.hpp
index 742596aedda..bd255208c2d 100644
--- a/SU2_CFD/include/variables/CScalarVariable.hpp
+++ b/SU2_CFD/include/variables/CScalarVariable.hpp
@@ -2,7 +2,7 @@
  * \file CScalarVariable.hpp
  * \brief Base class for defining the shared variables of scalar solvers.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CSobolevSmoothingVariable.hpp b/SU2_CFD/include/variables/CSobolevSmoothingVariable.hpp
index ba4d4e1bb1c..cee4cb26ce6 100644
--- a/SU2_CFD/include/variables/CSobolevSmoothingVariable.hpp
+++ b/SU2_CFD/include/variables/CSobolevSmoothingVariable.hpp
@@ -2,7 +2,7 @@
  * \file CSobolevSmoothingVariable.hpp
  * \brief Class for defining the variables of the gradient smoothing.
  * \author T.Dick
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CSpeciesFlameletVariable.hpp b/SU2_CFD/include/variables/CSpeciesFlameletVariable.hpp
index 6f2eb6fe42b..9a569e15c36 100644
--- a/SU2_CFD/include/variables/CSpeciesFlameletVariable.hpp
+++ b/SU2_CFD/include/variables/CSpeciesFlameletVariable.hpp
@@ -2,7 +2,7 @@
  * \file CSpeciesFlameletVariable.hpp
  * \brief Base class for defining the variables of the flamelet transport model.
  * \author D. Mayer, T. Economon, N. Beishuizen
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CSpeciesVariable.hpp b/SU2_CFD/include/variables/CSpeciesVariable.hpp
index a3d254ec30b..2c1b4a25f10 100644
--- a/SU2_CFD/include/variables/CSpeciesVariable.hpp
+++ b/SU2_CFD/include/variables/CSpeciesVariable.hpp
@@ -2,7 +2,7 @@
  * \file CSpeciesVariable.hpp
  * \brief Base class for defining the variables of the species transport model.
  * \author T. Kattmann
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CTransLMVariable.hpp b/SU2_CFD/include/variables/CTransLMVariable.hpp
index 315e03fbba3..cb4cd0d8f97 100644
--- a/SU2_CFD/include/variables/CTransLMVariable.hpp
+++ b/SU2_CFD/include/variables/CTransLMVariable.hpp
@@ -2,7 +2,7 @@
  * \file CTransLMVariable.hpp
  * \brief Declaration of the variables of the transition model.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CTurbSAVariable.hpp b/SU2_CFD/include/variables/CTurbSAVariable.hpp
index 04794ff3622..569e416fa15 100644
--- a/SU2_CFD/include/variables/CTurbSAVariable.hpp
+++ b/SU2_CFD/include/variables/CTurbSAVariable.hpp
@@ -2,7 +2,7 @@
  * \file CTurbSAVariable.hpp
  * \brief Declaration of the variables of the SA turbulence model.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CTurbSSTVariable.hpp b/SU2_CFD/include/variables/CTurbSSTVariable.hpp
index 9abf005f367..0113a0ead3a 100644
--- a/SU2_CFD/include/variables/CTurbSSTVariable.hpp
+++ b/SU2_CFD/include/variables/CTurbSSTVariable.hpp
@@ -2,7 +2,7 @@
  * \file CTurbSSTVariable.hpp
  * \brief Declaration of the variables of the SST turbulence model.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CTurbVariable.hpp b/SU2_CFD/include/variables/CTurbVariable.hpp
index 368fd330824..1a476fdac70 100644
--- a/SU2_CFD/include/variables/CTurbVariable.hpp
+++ b/SU2_CFD/include/variables/CTurbVariable.hpp
@@ -2,7 +2,7 @@
  * \file CTurbVariable.hpp
  * \brief Base class for defining the variables of the turbulence model.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/include/variables/CVariable.hpp b/SU2_CFD/include/variables/CVariable.hpp
index af0d70f2673..050be2b7787 100644
--- a/SU2_CFD/include/variables/CVariable.hpp
+++ b/SU2_CFD/include/variables/CVariable.hpp
@@ -4,7 +4,7 @@
           variables, function definitions in file <i>CVariable.cpp</i>.
           All variables are children of at least this class.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/CMarkerProfileReaderFVM.cpp b/SU2_CFD/src/CMarkerProfileReaderFVM.cpp
index ec31a074f90..485b004be9b 100644
--- a/SU2_CFD/src/CMarkerProfileReaderFVM.cpp
+++ b/SU2_CFD/src/CMarkerProfileReaderFVM.cpp
@@ -2,7 +2,7 @@
  * \file CMarkerProfileReaderFVM.cpp
  * \brief Class that handles the reading of marker profile files.
  * \author T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/SU2_CFD.cpp b/SU2_CFD/src/SU2_CFD.cpp
index fce69de5fd0..8cbd711ec99 100644
--- a/SU2_CFD/src/SU2_CFD.cpp
+++ b/SU2_CFD/src/SU2_CFD.cpp
@@ -2,7 +2,7 @@
  * \file SU2_CFD.cpp
  * \brief Main file of the SU2 Computational Fluid Dynamics code
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -47,7 +47,7 @@ int main(int argc, char *argv[]) {
 
   /*--- Command line parsing ---*/
 
-  CLI::App app{"SU2 v7.5.1 \"Blackbird\", The Open-Source CFD Code"};
+  CLI::App app{"SU2 v8.0.0 \"Harrier\", The Open-Source CFD Code"};
   app.add_flag("-d,--dryrun", dry_run, "Enable dry run mode.\n"
                                        "Only execute preprocessing steps using a dummy geometry.");
   app.add_option("-t,--threads", num_threads, "Number of OpenMP threads per MPI rank.");
diff --git a/SU2_CFD/src/definition_structure.cpp b/SU2_CFD/src/definition_structure.cpp
index 415e36a6421..bc3c4bcc191 100644
--- a/SU2_CFD/src/definition_structure.cpp
+++ b/SU2_CFD/src/definition_structure.cpp
@@ -2,7 +2,7 @@
  * \file definition_structure.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
index b1eafa89ef3..10afe73d7c6 100644
--- a/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjMultizoneDriver.cpp
  * \brief The main subroutines for driving adjoint multi-zone problems
  * \author O. Burghardt, P. Gomes, T. Albring, R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp b/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
index 7731d8899bb..9511f87a7fd 100644
--- a/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CDiscAdjSinglezoneDriver.cpp
@@ -2,7 +2,7 @@
  * \file driver_adjoint_singlezone.cpp
  * \brief The main subroutines for driving adjoint single-zone problems.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/drivers/CDriver.cpp b/SU2_CFD/src/drivers/CDriver.cpp
index c8ead183730..c33977ad33f 100644
--- a/SU2_CFD/src/drivers/CDriver.cpp
+++ b/SU2_CFD/src/drivers/CDriver.cpp
@@ -2,7 +2,7 @@
  * \file CDriver.cpp
  * \brief The main subroutines for driving single or multi-zone problems.
  * \author T. Economon, H. Kline, R. Sanchez, F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/drivers/CDriverBase.cpp b/SU2_CFD/src/drivers/CDriverBase.cpp
index 82bb3c3a477..0a9e02bb8c4 100644
--- a/SU2_CFD/src/drivers/CDriverBase.cpp
+++ b/SU2_CFD/src/drivers/CDriverBase.cpp
@@ -2,7 +2,7 @@
  * \file CDriverBase.hpp
  * \brief Base class template for all drivers.
  * \author H. Patel, A. Gastaldi
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/drivers/CDummyDriver.cpp b/SU2_CFD/src/drivers/CDummyDriver.cpp
index 8f5d68ae15c..fba8430bdc7 100644
--- a/SU2_CFD/src/drivers/CDummyDriver.cpp
+++ b/SU2_CFD/src/drivers/CDummyDriver.cpp
@@ -2,7 +2,7 @@
  * \file CDummyDriver.cpp
  * \brief Dummy driver class for running the preprocessing without geometry preprocessing.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/drivers/CMultizoneDriver.cpp b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
index 14c31aa9ea3..49a9c58e724 100644
--- a/SU2_CFD/src/drivers/CMultizoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CMultizoneDriver.cpp
@@ -2,7 +2,7 @@
  * \file driver_structure.cpp
  * \brief The main subroutines for driving multi-zone problems.
  * \author R. Sanchez, O. Burghardt
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/drivers/CSinglezoneDriver.cpp b/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
index f9fa11e87d6..c35d6b8eac5 100644
--- a/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
+++ b/SU2_CFD/src/drivers/CSinglezoneDriver.cpp
@@ -2,7 +2,7 @@
  * \file driver_direct_singlezone.cpp
  * \brief The main subroutines for driving single-zone problems.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/fluid/CCoolProp.cpp b/SU2_CFD/src/fluid/CCoolProp.cpp
index 40e9dcf48e6..9c48b1da6ba 100644
--- a/SU2_CFD/src/fluid/CCoolProp.cpp
+++ b/SU2_CFD/src/fluid/CCoolProp.cpp
@@ -2,7 +2,7 @@
  * \file CCoolProp.cpp
  * \brief Source of the fluid model from CoolProp.
  * \author P. Yan, G. Gori, A. Guardone
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
index a53601b7f5c..40f8e1234c7 100644
--- a/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
+++ b/SU2_CFD/src/fluid/CDataDrivenFluid.cpp
@@ -2,7 +2,7 @@
  * \file CDataDrivenFluid.cpp
  * \brief Source of the data-driven fluid model class
  * \author E.C.Bunschoten M.Mayer A.Capiello
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/fluid/CFluidFlamelet.cpp b/SU2_CFD/src/fluid/CFluidFlamelet.cpp
index f75a68700a5..0dbdee37c5e 100644
--- a/SU2_CFD/src/fluid/CFluidFlamelet.cpp
+++ b/SU2_CFD/src/fluid/CFluidFlamelet.cpp
@@ -2,7 +2,7 @@
  * \file CfluidFlamelet.cpp
  * \brief Main subroutines of CFluidFlamelet class
  * \author D. Mayer, T. Economon, N. Beishuizen, E. Bunschoten
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/fluid/CFluidModel.cpp b/SU2_CFD/src/fluid/CFluidModel.cpp
index 5aca9e783da..4c199cb117a 100644
--- a/SU2_CFD/src/fluid/CFluidModel.cpp
+++ b/SU2_CFD/src/fluid/CFluidModel.cpp
@@ -2,7 +2,7 @@
  * \file CFluidModel.cpp
  * \brief Source of the fluid model base class containing thermo-physical subroutines.
  * \author S.Vitale, M.Pini, G.Gori, A.Guardone, P.Colonna, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/fluid/CFluidScalar.cpp b/SU2_CFD/src/fluid/CFluidScalar.cpp
index fd439c6bb64..8171e2a515e 100644
--- a/SU2_CFD/src/fluid/CFluidScalar.cpp
+++ b/SU2_CFD/src/fluid/CFluidScalar.cpp
@@ -2,7 +2,7 @@
  * \file CFluidScalar.cpp
  * \brief Defines the multicomponent incompressible Ideal Gas model for mixtures.
  * \author T. Economon, Mark Heimgartner, Cristopher Morales Ubal
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/fluid/CIdealGas.cpp b/SU2_CFD/src/fluid/CIdealGas.cpp
index 2afc1b36e69..433fc059a78 100644
--- a/SU2_CFD/src/fluid/CIdealGas.cpp
+++ b/SU2_CFD/src/fluid/CIdealGas.cpp
@@ -2,7 +2,7 @@
  * \file CIdealGas.cpp
  * \brief Source of the ideal gas model.
  * \author S. Vitale, G. Gori, M. Pini, A. Guardone, P. Colonna
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/fluid/CMutationTCLib.cpp b/SU2_CFD/src/fluid/CMutationTCLib.cpp
index f23aac2b4eb..58629d9f327 100644
--- a/SU2_CFD/src/fluid/CMutationTCLib.cpp
+++ b/SU2_CFD/src/fluid/CMutationTCLib.cpp
@@ -2,7 +2,7 @@
  * \file CMutationTCLib.cpp
  * \brief Source of the Mutation++ 2T nonequilibrium gas model.
  * \author C. Garbacz
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/fluid/CNEMOGas.cpp b/SU2_CFD/src/fluid/CNEMOGas.cpp
index f293726c947..929a09dc63c 100644
--- a/SU2_CFD/src/fluid/CNEMOGas.cpp
+++ b/SU2_CFD/src/fluid/CNEMOGas.cpp
@@ -2,7 +2,7 @@
  * \file CNEMOGas.cpp
  * \brief Source of the nonequilibrium gas model.
  * \author C. Garbacz, W. Maier, S. R. Copeland
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/fluid/CPengRobinson.cpp b/SU2_CFD/src/fluid/CPengRobinson.cpp
index 445854b55cb..4b93a28da70 100644
--- a/SU2_CFD/src/fluid/CPengRobinson.cpp
+++ b/SU2_CFD/src/fluid/CPengRobinson.cpp
@@ -2,7 +2,7 @@
  * \file CPengRobinson.cpp
  * \brief Source of the Peng-Robinson model.
  * \author S. Vitale, G. Gori, M. Pini, A. Guardone, P. Colonna
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/fluid/CSU2TCLib.cpp b/SU2_CFD/src/fluid/CSU2TCLib.cpp
index 67cd77b343e..40b39a449f7 100644
--- a/SU2_CFD/src/fluid/CSU2TCLib.cpp
+++ b/SU2_CFD/src/fluid/CSU2TCLib.cpp
@@ -2,7 +2,7 @@
  * \file CSU2TCLib.cpp
  * \brief Source of user defined 2T nonequilibrium gas model.
  * \author C. Garbacz, W. Maier, S. R. Copeland, J. Needels
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/fluid/CVanDerWaalsGas.cpp b/SU2_CFD/src/fluid/CVanDerWaalsGas.cpp
index 215f8c9a803..790fe87a2fa 100644
--- a/SU2_CFD/src/fluid/CVanDerWaalsGas.cpp
+++ b/SU2_CFD/src/fluid/CVanDerWaalsGas.cpp
@@ -2,7 +2,7 @@
  * \file CVanDerWaalsGas.cpp
  * \brief Source of the Polytropic Van der Waals model.
  * \author S. Vitale, G. Gori, M. Pini, A. Guardone, P. Colonna
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/integration/CFEM_DG_Integration.cpp b/SU2_CFD/src/integration/CFEM_DG_Integration.cpp
index f653c254f94..3378a8aea9e 100644
--- a/SU2_CFD/src/integration/CFEM_DG_Integration.cpp
+++ b/SU2_CFD/src/integration/CFEM_DG_Integration.cpp
@@ -2,7 +2,7 @@
  * \file CFEM_DG_Integration.cpp
  * \brief Definition of time and space integration for the DG solver.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/integration/CIntegration.cpp b/SU2_CFD/src/integration/CIntegration.cpp
index d27be847c53..1ffc29364e2 100644
--- a/SU2_CFD/src/integration/CIntegration.cpp
+++ b/SU2_CFD/src/integration/CIntegration.cpp
@@ -2,7 +2,7 @@
  * \file CIntegration.cpp
  * \brief Implementation of the base class for space and time integration.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/integration/CIntegrationFactory.cpp b/SU2_CFD/src/integration/CIntegrationFactory.cpp
index 0da1709b5d1..9352b75b98c 100644
--- a/SU2_CFD/src/integration/CIntegrationFactory.cpp
+++ b/SU2_CFD/src/integration/CIntegrationFactory.cpp
@@ -2,7 +2,7 @@
  * \file CIntegrationFactory.cpp
  * \brief Main subroutines for CIntegrationFactory .
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/integration/CMultiGridIntegration.cpp b/SU2_CFD/src/integration/CMultiGridIntegration.cpp
index 8460496df5f..8f5b4f01de8 100644
--- a/SU2_CFD/src/integration/CMultiGridIntegration.cpp
+++ b/SU2_CFD/src/integration/CMultiGridIntegration.cpp
@@ -2,7 +2,7 @@
  * \file CMultiGridIntegration.cpp
  * \brief Implementation of the multigrid integration class.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/integration/CNewtonIntegration.cpp b/SU2_CFD/src/integration/CNewtonIntegration.cpp
index 78fd23b2d66..69aaa4d1883 100644
--- a/SU2_CFD/src/integration/CNewtonIntegration.cpp
+++ b/SU2_CFD/src/integration/CNewtonIntegration.cpp
@@ -2,7 +2,7 @@
  * \file CNewtonIntegration.cpp
  * \brief Newton-Krylov integration.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/integration/CSingleGridIntegration.cpp b/SU2_CFD/src/integration/CSingleGridIntegration.cpp
index e43b4518c26..f31493cddb5 100644
--- a/SU2_CFD/src/integration/CSingleGridIntegration.cpp
+++ b/SU2_CFD/src/integration/CSingleGridIntegration.cpp
@@ -2,7 +2,7 @@
  * \file CSingleGridIntegration.cpp
  * \brief Single (fine) grid integration class implementation.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/integration/CStructuralIntegration.cpp b/SU2_CFD/src/integration/CStructuralIntegration.cpp
index 5fc18babb3f..c4a6dd10405 100644
--- a/SU2_CFD/src/integration/CStructuralIntegration.cpp
+++ b/SU2_CFD/src/integration/CStructuralIntegration.cpp
@@ -2,7 +2,7 @@
  * \file CStructuralIntegration.cpp
  * \brief Space and time integration for structural problems.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/interfaces/CInterface.cpp b/SU2_CFD/src/interfaces/CInterface.cpp
index dc068205324..4d8d33b3ecf 100644
--- a/SU2_CFD/src/interfaces/CInterface.cpp
+++ b/SU2_CFD/src/interfaces/CInterface.cpp
@@ -2,7 +2,7 @@
  * \file CInterface.cpp
  * \brief Main subroutines for MPI transfer of information between zones
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/interfaces/cfd/CConservativeVarsInterface.cpp b/SU2_CFD/src/interfaces/cfd/CConservativeVarsInterface.cpp
index 31ca92974d4..85a4a72d4e7 100644
--- a/SU2_CFD/src/interfaces/cfd/CConservativeVarsInterface.cpp
+++ b/SU2_CFD/src/interfaces/cfd/CConservativeVarsInterface.cpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer conservative variables
  *        from a generic zone into another one.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/interfaces/cfd/CMixingPlaneInterface.cpp b/SU2_CFD/src/interfaces/cfd/CMixingPlaneInterface.cpp
index ab7de26be09..76e7509edce 100644
--- a/SU2_CFD/src/interfaces/cfd/CMixingPlaneInterface.cpp
+++ b/SU2_CFD/src/interfaces/cfd/CMixingPlaneInterface.cpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer average variables
  *        needed for MixingPlane computation from a generic zone into another one.
  * \author S. Vitale
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/interfaces/cfd/CSlidingInterface.cpp b/SU2_CFD/src/interfaces/cfd/CSlidingInterface.cpp
index 73a0144c9ee..5eb7437bdfd 100644
--- a/SU2_CFD/src/interfaces/cfd/CSlidingInterface.cpp
+++ b/SU2_CFD/src/interfaces/cfd/CSlidingInterface.cpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer conservative variables
  *        from a generic zone into another
  * \author G. Gori Politecnico di Milano
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/interfaces/cht/CConjugateHeatInterface.cpp b/SU2_CFD/src/interfaces/cht/CConjugateHeatInterface.cpp
index ea9dd7134f7..5aa6772907f 100644
--- a/SU2_CFD/src/interfaces/cht/CConjugateHeatInterface.cpp
+++ b/SU2_CFD/src/interfaces/cht/CConjugateHeatInterface.cpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer temperature and heatflux
  *        density for conjugate heat interfaces between structure and fluid zones.
  * \author O. Burghardt
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/interfaces/fsi/CDiscAdjFlowTractionInterface.cpp b/SU2_CFD/src/interfaces/fsi/CDiscAdjFlowTractionInterface.cpp
index 2db45dd5825..84ddc14f79f 100644
--- a/SU2_CFD/src/interfaces/fsi/CDiscAdjFlowTractionInterface.cpp
+++ b/SU2_CFD/src/interfaces/fsi/CDiscAdjFlowTractionInterface.cpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer flow tractions
  *        from a fluid zone into a structural zone in a discrete adjoint simulation.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/interfaces/fsi/CDisplacementsInterface.cpp b/SU2_CFD/src/interfaces/fsi/CDisplacementsInterface.cpp
index bea9e316c0f..d05fb1f55c0 100644
--- a/SU2_CFD/src/interfaces/fsi/CDisplacementsInterface.cpp
+++ b/SU2_CFD/src/interfaces/fsi/CDisplacementsInterface.cpp
@@ -2,7 +2,7 @@
  * \file CDisplacementsInterface.cpp
  * \brief Main subroutines for transferring boundary displacements.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/interfaces/fsi/CFlowTractionInterface.cpp b/SU2_CFD/src/interfaces/fsi/CFlowTractionInterface.cpp
index 88ee4a5e41f..f3ca34dcbe0 100644
--- a/SU2_CFD/src/interfaces/fsi/CFlowTractionInterface.cpp
+++ b/SU2_CFD/src/interfaces/fsi/CFlowTractionInterface.cpp
@@ -3,7 +3,7 @@
  * \brief Declaration and inlines of the class to transfer flow tractions
  *        from a fluid zone into a structural zone.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/iteration/CAdjFluidIteration.cpp b/SU2_CFD/src/iteration/CAdjFluidIteration.cpp
index c3c0cce8a02..df2be8f0884 100644
--- a/SU2_CFD/src/iteration/CAdjFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CAdjFluidIteration.cpp
@@ -2,7 +2,7 @@
  * \file CAdjFluidIteration.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
index 0ecf23e17fc..2887abf7d8c 100644
--- a/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjFEAIteration.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjFEAIteration.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
index 004d9cabfa4..3e5c8b8d85f 100644
--- a/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjFluidIteration.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjFluidIteration.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp b/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
index 0d220db739e..90d7c5ab85d 100644
--- a/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
+++ b/SU2_CFD/src/iteration/CDiscAdjHeatIteration.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjHeatIteration.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/iteration/CFEAIteration.cpp b/SU2_CFD/src/iteration/CFEAIteration.cpp
index 91b9e715681..3d1b5fd857e 100644
--- a/SU2_CFD/src/iteration/CFEAIteration.cpp
+++ b/SU2_CFD/src/iteration/CFEAIteration.cpp
@@ -2,7 +2,7 @@
  * \file CFEAIteration.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/iteration/CFEMFluidIteration.cpp b/SU2_CFD/src/iteration/CFEMFluidIteration.cpp
index 8fb9b09c420..a599fec41a3 100644
--- a/SU2_CFD/src/iteration/CFEMFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CFEMFluidIteration.cpp
@@ -2,7 +2,7 @@
  * \file CFEMFluidIteration.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/iteration/CFluidIteration.cpp b/SU2_CFD/src/iteration/CFluidIteration.cpp
index cde93a085bb..f879606b66e 100644
--- a/SU2_CFD/src/iteration/CFluidIteration.cpp
+++ b/SU2_CFD/src/iteration/CFluidIteration.cpp
@@ -2,7 +2,7 @@
  * \file CFluidIteration.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/iteration/CHeatIteration.cpp b/SU2_CFD/src/iteration/CHeatIteration.cpp
index 45c8d6f8e68..6ca18523335 100644
--- a/SU2_CFD/src/iteration/CHeatIteration.cpp
+++ b/SU2_CFD/src/iteration/CHeatIteration.cpp
@@ -2,7 +2,7 @@
  * \file CHeatIteration.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/iteration/CIteration.cpp b/SU2_CFD/src/iteration/CIteration.cpp
index 517f3bff2c4..98190ef3972 100644
--- a/SU2_CFD/src/iteration/CIteration.cpp
+++ b/SU2_CFD/src/iteration/CIteration.cpp
@@ -2,7 +2,7 @@
  * \file iteration_structure.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/iteration/CIterationFactory.cpp b/SU2_CFD/src/iteration/CIterationFactory.cpp
index 8e9fd4e86b8..159d8133c51 100644
--- a/SU2_CFD/src/iteration/CIterationFactory.cpp
+++ b/SU2_CFD/src/iteration/CIterationFactory.cpp
@@ -2,7 +2,7 @@
  * \file CAdjFluidIteration.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/iteration/CTurboIteration.cpp b/SU2_CFD/src/iteration/CTurboIteration.cpp
index 464ae8186ea..0028df639f7 100644
--- a/SU2_CFD/src/iteration/CTurboIteration.cpp
+++ b/SU2_CFD/src/iteration/CTurboIteration.cpp
@@ -2,7 +2,7 @@
  * \file CTurboIteration.cpp
  * \brief Main subroutines used by SU2_CFD
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/limiters/CLimiterDetails.cpp b/SU2_CFD/src/limiters/CLimiterDetails.cpp
index 646139d2ff0..22636efe0b8 100644
--- a/SU2_CFD/src/limiters/CLimiterDetails.cpp
+++ b/SU2_CFD/src/limiters/CLimiterDetails.cpp
@@ -3,7 +3,7 @@
  * \brief A class template that allows defining limiters via
  *        specialization of particular details.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/CGradSmoothing.cpp b/SU2_CFD/src/numerics/CGradSmoothing.cpp
index 84685c722ed..7ce9c56d2ab 100644
--- a/SU2_CFD/src/numerics/CGradSmoothing.cpp
+++ b/SU2_CFD/src/numerics/CGradSmoothing.cpp
@@ -2,7 +2,7 @@
  * \file CGradSmoothing.cpp
  * \brief Numerics for gradient smoothing problems.
  * \author T.Dick
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/CNumerics.cpp b/SU2_CFD/src/numerics/CNumerics.cpp
index 1393c14a20a..19a73d8edeb 100644
--- a/SU2_CFD/src/numerics/CNumerics.cpp
+++ b/SU2_CFD/src/numerics/CNumerics.cpp
@@ -4,7 +4,7 @@
  *        Contains methods for common tasks, e.g. compute flux
  *        Jacobians.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp b/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp
index 2f6b5c1712b..f1219a0c7f2 100644
--- a/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp
+++ b/SU2_CFD/src/numerics/NEMO/CNEMONumerics.cpp
@@ -4,7 +4,7 @@
  *        Contains methods for common tasks, e.g. compute flux
  *        Jacobians.
  * \author S.R. Copeland, W. Maier, C. Garbacz
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp b/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
index a72e3f3fb83..8de786c08a9 100644
--- a/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
+++ b/SU2_CFD/src/numerics/NEMO/NEMO_diffusion.cpp
@@ -3,7 +3,7 @@
  * \brief Implementation of numerics classes for discretization
  *        of viscous fluxes in fluid flow NEMO problems.
  * \author S.R. Copeland, W. Maier, C. Garbacz
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp b/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp
index d99ea8702a4..c49dae47bd1 100644
--- a/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp
+++ b/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp
@@ -3,7 +3,7 @@
  * \brief Implementation of numerics classes for integration
  *        of source terms in fluid flow NEMO problems.
  * \author C. Garbacz, W. Maier, S. Copeland.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/NEMO/convection/ausm_slau.cpp b/SU2_CFD/src/numerics/NEMO/convection/ausm_slau.cpp
index 2370183c45d..865cdc268d9 100644
--- a/SU2_CFD/src/numerics/NEMO/convection/ausm_slau.cpp
+++ b/SU2_CFD/src/numerics/NEMO/convection/ausm_slau.cpp
@@ -2,7 +2,7 @@
  * \file ausm_slau.cpp
  * \brief Implementations of the AUSM-family of schemes in NEMO.
  * \author F. Palacios, S.R. Copeland, W. Maier, C. Garbacz
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/NEMO/convection/lax.cpp b/SU2_CFD/src/numerics/NEMO/convection/lax.cpp
index abd7353f714..f7b4922c4c6 100644
--- a/SU2_CFD/src/numerics/NEMO/convection/lax.cpp
+++ b/SU2_CFD/src/numerics/NEMO/convection/lax.cpp
@@ -2,7 +2,7 @@
  * \file lax.cpp
  * \brief Implementations of Lax centered scheme.
  * \author F. Palacios, S.R. Copeland, W. Maier, C. Garbacz
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/NEMO/convection/msw.cpp b/SU2_CFD/src/numerics/NEMO/convection/msw.cpp
index e3cf801a647..5941a4793d3 100644
--- a/SU2_CFD/src/numerics/NEMO/convection/msw.cpp
+++ b/SU2_CFD/src/numerics/NEMO/convection/msw.cpp
@@ -2,7 +2,7 @@
  * \file msw.cpp
  * \brief Implementations of the modified Steger-Warming scheme.
  * \author ADL Stanford, S.R. Copeland, W. Maier, C. Garbacz
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/NEMO/convection/roe.cpp b/SU2_CFD/src/numerics/NEMO/convection/roe.cpp
index 5d8fa7a4813..8ff004f79af 100644
--- a/SU2_CFD/src/numerics/NEMO/convection/roe.cpp
+++ b/SU2_CFD/src/numerics/NEMO/convection/roe.cpp
@@ -2,7 +2,7 @@
  * \file roe.cpp
  * \brief Implementations of Roe-type schemes in NEMO.
  * \author S. R. Copeland, W. Maier, C. Garbacz
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/continuous_adjoint/adj_convection.cpp b/SU2_CFD/src/numerics/continuous_adjoint/adj_convection.cpp
index 6f09425c5c0..2e17ae0db6c 100644
--- a/SU2_CFD/src/numerics/continuous_adjoint/adj_convection.cpp
+++ b/SU2_CFD/src/numerics/continuous_adjoint/adj_convection.cpp
@@ -2,7 +2,7 @@
  * \file adj_convection.cpp
  * \brief Implementation of adjoint convection numerics classes.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/continuous_adjoint/adj_diffusion.cpp b/SU2_CFD/src/numerics/continuous_adjoint/adj_diffusion.cpp
index 55acc909554..8a407c2caa8 100644
--- a/SU2_CFD/src/numerics/continuous_adjoint/adj_diffusion.cpp
+++ b/SU2_CFD/src/numerics/continuous_adjoint/adj_diffusion.cpp
@@ -2,7 +2,7 @@
  * \file adj_diffusion.cpp
  * \brief Implementation of adjoint diffusion numerics classes.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/continuous_adjoint/adj_sources.cpp b/SU2_CFD/src/numerics/continuous_adjoint/adj_sources.cpp
index 379d6125fd1..061772e4ffb 100644
--- a/SU2_CFD/src/numerics/continuous_adjoint/adj_sources.cpp
+++ b/SU2_CFD/src/numerics/continuous_adjoint/adj_sources.cpp
@@ -2,7 +2,7 @@
  * \file adj_sources.cpp
  * \brief Implementation of adjoint source numerics classes.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/elasticity/CFEAElasticity.cpp b/SU2_CFD/src/numerics/elasticity/CFEAElasticity.cpp
index fc87cbc19a5..ac2cd9fef96 100644
--- a/SU2_CFD/src/numerics/elasticity/CFEAElasticity.cpp
+++ b/SU2_CFD/src/numerics/elasticity/CFEAElasticity.cpp
@@ -2,7 +2,7 @@
  * \file CFEAElasticity.cpp
  * \brief Base class for all elasticity problems.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/elasticity/CFEALinearElasticity.cpp b/SU2_CFD/src/numerics/elasticity/CFEALinearElasticity.cpp
index a9ae91c1d12..06dade2a629 100644
--- a/SU2_CFD/src/numerics/elasticity/CFEALinearElasticity.cpp
+++ b/SU2_CFD/src/numerics/elasticity/CFEALinearElasticity.cpp
@@ -2,7 +2,7 @@
  * \file CFEALinearElasticity.cpp
  * \brief Classes for linear elasticity problems.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/elasticity/CFEANonlinearElasticity.cpp b/SU2_CFD/src/numerics/elasticity/CFEANonlinearElasticity.cpp
index 6dea30ef6ee..418566611f9 100644
--- a/SU2_CFD/src/numerics/elasticity/CFEANonlinearElasticity.cpp
+++ b/SU2_CFD/src/numerics/elasticity/CFEANonlinearElasticity.cpp
@@ -3,7 +3,7 @@
  * \brief This file contains the routines for setting the tangent matrix and
  *        residual of a FEM nonlinear elastic structural problem.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/elasticity/nonlinear_models.cpp b/SU2_CFD/src/numerics/elasticity/nonlinear_models.cpp
index 3443e02a424..7e870386678 100644
--- a/SU2_CFD/src/numerics/elasticity/nonlinear_models.cpp
+++ b/SU2_CFD/src/numerics/elasticity/nonlinear_models.cpp
@@ -2,7 +2,7 @@
  * \file nonlinear_models.cpp
  * \brief Definition of nonlinear constitutive models.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/flow/convection/ausm_slau.cpp b/SU2_CFD/src/numerics/flow/convection/ausm_slau.cpp
index 3d0286a0757..525dcaae823 100644
--- a/SU2_CFD/src/numerics/flow/convection/ausm_slau.cpp
+++ b/SU2_CFD/src/numerics/flow/convection/ausm_slau.cpp
@@ -2,7 +2,7 @@
  * \file ausm_slau.cpp
  * \brief Implementations of the AUSM-family of schemes.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/flow/convection/centered.cpp b/SU2_CFD/src/numerics/flow/convection/centered.cpp
index 89a5ec243db..c4568903172 100644
--- a/SU2_CFD/src/numerics/flow/convection/centered.cpp
+++ b/SU2_CFD/src/numerics/flow/convection/centered.cpp
@@ -2,7 +2,7 @@
  * \file centered.cpp
  * \brief Implementations of centered schemes.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/flow/convection/fds.cpp b/SU2_CFD/src/numerics/flow/convection/fds.cpp
index 1fae70b6d9b..358d844e5a2 100644
--- a/SU2_CFD/src/numerics/flow/convection/fds.cpp
+++ b/SU2_CFD/src/numerics/flow/convection/fds.cpp
@@ -2,7 +2,7 @@
  * \file fds.cpp
  * \brief Implementation of Flux-Difference-Splitting schemes.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/flow/convection/fvs.cpp b/SU2_CFD/src/numerics/flow/convection/fvs.cpp
index a156a1b7c31..171a781a54c 100644
--- a/SU2_CFD/src/numerics/flow/convection/fvs.cpp
+++ b/SU2_CFD/src/numerics/flow/convection/fvs.cpp
@@ -2,7 +2,7 @@
  * \file fvs.cpp
  * \brief Implementations of Flux-Vector-Splitting schemes.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/flow/convection/hllc.cpp b/SU2_CFD/src/numerics/flow/convection/hllc.cpp
index 44acc4c806e..e5893bced0d 100644
--- a/SU2_CFD/src/numerics/flow/convection/hllc.cpp
+++ b/SU2_CFD/src/numerics/flow/convection/hllc.cpp
@@ -2,7 +2,7 @@
  * \file hllc.cpp
  * \brief Implementations of HLLC schemes.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/flow/convection/roe.cpp b/SU2_CFD/src/numerics/flow/convection/roe.cpp
index 75cf2fa2bce..67ef74124f3 100644
--- a/SU2_CFD/src/numerics/flow/convection/roe.cpp
+++ b/SU2_CFD/src/numerics/flow/convection/roe.cpp
@@ -2,7 +2,7 @@
  * \file roe.cpp
  * \brief Implementations of Roe-type schemes.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/flow/flow_diffusion.cpp b/SU2_CFD/src/numerics/flow/flow_diffusion.cpp
index 20d49fa469f..d99fcb04b88 100644
--- a/SU2_CFD/src/numerics/flow/flow_diffusion.cpp
+++ b/SU2_CFD/src/numerics/flow/flow_diffusion.cpp
@@ -3,7 +3,7 @@
  * \brief Implementation of numerics classes for discretization
  *        of viscous fluxes in fluid flow problems.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/flow/flow_sources.cpp b/SU2_CFD/src/numerics/flow/flow_sources.cpp
index 95bd3f09e5b..5ebcbf3096e 100644
--- a/SU2_CFD/src/numerics/flow/flow_sources.cpp
+++ b/SU2_CFD/src/numerics/flow/flow_sources.cpp
@@ -3,7 +3,7 @@
  * \brief Implementation of numerics classes for integration
  *        of source terms in fluid flow problems.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/radiation.cpp b/SU2_CFD/src/numerics/radiation.cpp
index fcc036a0e9a..c6f7fc009bd 100644
--- a/SU2_CFD/src/numerics/radiation.cpp
+++ b/SU2_CFD/src/numerics/radiation.cpp
@@ -3,7 +3,7 @@
  * \brief This file contains the implementation of the numerical
  *        methods for radiation.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/scalar/scalar_sources.cpp b/SU2_CFD/src/numerics/scalar/scalar_sources.cpp
index 135cf32f568..b2ab84650a1 100644
--- a/SU2_CFD/src/numerics/scalar/scalar_sources.cpp
+++ b/SU2_CFD/src/numerics/scalar/scalar_sources.cpp
@@ -1,7 +1,7 @@
 /*!
  * \file scalar_sources.cpp
  * \brief Implementation of numerics classes for integration of scalar source-terms.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/species/species_sources.cpp b/SU2_CFD/src/numerics/species/species_sources.cpp
index ab51d4b15e7..7ae364ce941 100644
--- a/SU2_CFD/src/numerics/species/species_sources.cpp
+++ b/SU2_CFD/src/numerics/species/species_sources.cpp
@@ -3,7 +3,7 @@
  * \brief Implementation of numerics classes for integration of
  *        species transport source-terms.
  * \author T. Kattmann
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/numerics/template.cpp b/SU2_CFD/src/numerics/template.cpp
index b0c07932c81..40459ad02d1 100644
--- a/SU2_CFD/src/numerics/template.cpp
+++ b/SU2_CFD/src/numerics/template.cpp
@@ -2,7 +2,7 @@
  * \file template.cpp
  * \brief Empty implementation of numerics templates, see .hpp file.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CAdjElasticityOutput.cpp b/SU2_CFD/src/output/CAdjElasticityOutput.cpp
index b5fc2121968..6b6be57f485 100644
--- a/SU2_CFD/src/output/CAdjElasticityOutput.cpp
+++ b/SU2_CFD/src/output/CAdjElasticityOutput.cpp
@@ -2,7 +2,7 @@
  * \file CAdjElasticityOutput.cpp
  * \brief Main subroutines for elasticity discrete adjoint output
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CAdjFlowCompOutput.cpp b/SU2_CFD/src/output/CAdjFlowCompOutput.cpp
index 8804f203b7f..92c09dd01f4 100644
--- a/SU2_CFD/src/output/CAdjFlowCompOutput.cpp
+++ b/SU2_CFD/src/output/CAdjFlowCompOutput.cpp
@@ -2,7 +2,7 @@
  * \file CAdjFlowCompOutput.cpp
  * \brief Main subroutines for flow discrete adjoint output
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CAdjFlowIncOutput.cpp b/SU2_CFD/src/output/CAdjFlowIncOutput.cpp
index 25ff3365250..b279d0fbfe1 100644
--- a/SU2_CFD/src/output/CAdjFlowIncOutput.cpp
+++ b/SU2_CFD/src/output/CAdjFlowIncOutput.cpp
@@ -2,7 +2,7 @@
  * \file CAdjFlowIncOutput.cpp
  * \brief Main subroutines for flow discrete adjoint output
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CAdjFlowOutput.cpp b/SU2_CFD/src/output/CAdjFlowOutput.cpp
index 7d61021a8d0..f20f9c9bcad 100644
--- a/SU2_CFD/src/output/CAdjFlowOutput.cpp
+++ b/SU2_CFD/src/output/CAdjFlowOutput.cpp
@@ -2,7 +2,7 @@
  * \file CAdjFlowOutput.cpp
  * \brief Main subroutines for flow discrete adjoint output
  * \author T. Kattmann
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CAdjHeatOutput.cpp b/SU2_CFD/src/output/CAdjHeatOutput.cpp
index 2317d0ba738..2b856ef793b 100644
--- a/SU2_CFD/src/output/CAdjHeatOutput.cpp
+++ b/SU2_CFD/src/output/CAdjHeatOutput.cpp
@@ -2,7 +2,7 @@
  * \file CAdjHeatOutput.cpp
  * \brief Main subroutines for flow discrete adjoint output
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CBaselineOutput.cpp b/SU2_CFD/src/output/CBaselineOutput.cpp
index 8493335393e..b17250c29e3 100644
--- a/SU2_CFD/src/output/CBaselineOutput.cpp
+++ b/SU2_CFD/src/output/CBaselineOutput.cpp
@@ -2,7 +2,7 @@
  * \file CBaselineOutput.cpp
  * \brief Main subroutines for flow discrete adjoint output
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CElasticityOutput.cpp b/SU2_CFD/src/output/CElasticityOutput.cpp
index 71726c6ebb3..288fd8adbf8 100644
--- a/SU2_CFD/src/output/CElasticityOutput.cpp
+++ b/SU2_CFD/src/output/CElasticityOutput.cpp
@@ -2,7 +2,7 @@
  * \file CElasticityOutput.cpp
  * \brief Main subroutines for FEA output
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CFVMOutput.cpp b/SU2_CFD/src/output/CFVMOutput.cpp
index 554d6ae5e85..c9c3047aefd 100644
--- a/SU2_CFD/src/output/CFVMOutput.cpp
+++ b/SU2_CFD/src/output/CFVMOutput.cpp
@@ -2,7 +2,7 @@
  * \file CFVMOutput.cpp
  * \brief Main subroutines for Finite Volume Method output
  * \author T. Kattmann
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CFlowCompFEMOutput.cpp b/SU2_CFD/src/output/CFlowCompFEMOutput.cpp
index 4a919c9278b..d6ed5b9dc48 100644
--- a/SU2_CFD/src/output/CFlowCompFEMOutput.cpp
+++ b/SU2_CFD/src/output/CFlowCompFEMOutput.cpp
@@ -2,7 +2,7 @@
  * \file CFlowCompFEMOutput.cpp
  * \brief Main subroutines for compressible flow output
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CFlowCompOutput.cpp b/SU2_CFD/src/output/CFlowCompOutput.cpp
index 30f93e70ea2..8e39772f9c1 100644
--- a/SU2_CFD/src/output/CFlowCompOutput.cpp
+++ b/SU2_CFD/src/output/CFlowCompOutput.cpp
@@ -2,7 +2,7 @@
  * \file CFlowCompOutput.cpp
  * \brief Main subroutines for compressible flow output
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CFlowIncOutput.cpp b/SU2_CFD/src/output/CFlowIncOutput.cpp
index 0a500f187ba..f729dfed82e 100644
--- a/SU2_CFD/src/output/CFlowIncOutput.cpp
+++ b/SU2_CFD/src/output/CFlowIncOutput.cpp
@@ -2,7 +2,7 @@
  * \file CFlowIncOutput.cpp
  * \brief Main subroutines for incompressible flow output
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CFlowOutput.cpp b/SU2_CFD/src/output/CFlowOutput.cpp
index bb3f5c8cd07..75bd80feebb 100644
--- a/SU2_CFD/src/output/CFlowOutput.cpp
+++ b/SU2_CFD/src/output/CFlowOutput.cpp
@@ -2,7 +2,7 @@
  * \file CFlowOutput.cpp
  * \brief Common functions for flow output.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
@@ -2597,7 +2597,7 @@ void CFlowOutput::WriteForcesBreakdown(const CConfig* config, const CSolver* flo
   file << "\n";
   file << "-------------------------------------------------------------------------\n";
   file << "|    ___ _   _ ___                                                      |\n";
-  file << "|   / __| | | |_  )   Release 7.5.1 \"Blackbird\"                         |\n";
+  file << "|   / __| | | |_  )   Release 8.0.0 \"Harrier\"                           |\n";
   file << "|   \\__ \\ |_| |/ /                                                      |\n";
   file << "|   |___/\\___//___|   Suite (Computational Fluid Dynamics Code)         |\n";
   file << "|                                                                       |\n";
diff --git a/SU2_CFD/src/output/CHeatOutput.cpp b/SU2_CFD/src/output/CHeatOutput.cpp
index eccba6e70e9..39d5ee3796f 100644
--- a/SU2_CFD/src/output/CHeatOutput.cpp
+++ b/SU2_CFD/src/output/CHeatOutput.cpp
@@ -2,7 +2,7 @@
  * \file CHeatOutput.cpp
  * \brief Main subroutines for the heat solver output
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CMeshOutput.cpp b/SU2_CFD/src/output/CMeshOutput.cpp
index 4d5c6e1dd1e..eb00dfbe6f9 100644
--- a/SU2_CFD/src/output/CMeshOutput.cpp
+++ b/SU2_CFD/src/output/CMeshOutput.cpp
@@ -2,7 +2,7 @@
  * \file CMeshOutput.cpp
  * \brief Main subroutines for the heat solver output
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CMultizoneOutput.cpp b/SU2_CFD/src/output/CMultizoneOutput.cpp
index 2c63c04ed2b..a30acca6268 100644
--- a/SU2_CFD/src/output/CMultizoneOutput.cpp
+++ b/SU2_CFD/src/output/CMultizoneOutput.cpp
@@ -2,7 +2,7 @@
  * \file CMultizoneOutput.cpp
  * \brief Main subroutines for multizone output
  * \author R. Sanchez, T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/CNEMOCompOutput.cpp b/SU2_CFD/src/output/CNEMOCompOutput.cpp
index d5bb669ec8b..67adfe1559e 100644
--- a/SU2_CFD/src/output/CNEMOCompOutput.cpp
+++ b/SU2_CFD/src/output/CNEMOCompOutput.cpp
@@ -2,7 +2,7 @@
  * \file CNEMOCompOutput.cpp
  * \brief Main subroutines for compressible flow output
  * \author W. Maier, R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/COutput.cpp b/SU2_CFD/src/output/COutput.cpp
index 94d7c0a3cb3..4f52cd64fdb 100644
--- a/SU2_CFD/src/output/COutput.cpp
+++ b/SU2_CFD/src/output/COutput.cpp
@@ -2,7 +2,7 @@
  * \file COutput.cpp
  * \brief Main subroutines for output solver information
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/COutputFactory.cpp b/SU2_CFD/src/output/COutputFactory.cpp
index 4f8892712b6..e0cab769441 100644
--- a/SU2_CFD/src/output/COutputFactory.cpp
+++ b/SU2_CFD/src/output/COutputFactory.cpp
@@ -2,7 +2,7 @@
  * \file COutputFactory.cpp
  * \brief Main subroutines for output solver information
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CCGNSFileWriter.cpp b/SU2_CFD/src/output/filewriter/CCGNSFileWriter.cpp
index 8436698b3c2..34f75473b61 100644
--- a/SU2_CFD/src/output/filewriter/CCGNSFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CCGNSFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CCGNSFileWriter.cpp
  * \brief Filewriter class for CGNS format.
  * \author G. Baldan
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CCSVFileWriter.cpp b/SU2_CFD/src/output/filewriter/CCSVFileWriter.cpp
index 0ec0ba89b9d..254bb48fce3 100644
--- a/SU2_CFD/src/output/filewriter/CCSVFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CCSVFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CCSVFileWriter.cpp
  * \brief CSV Writer output class
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CFEMDataSorter.cpp b/SU2_CFD/src/output/filewriter/CFEMDataSorter.cpp
index 4fd7bdf780d..6d59f44fb71 100644
--- a/SU2_CFD/src/output/filewriter/CFEMDataSorter.cpp
+++ b/SU2_CFD/src/output/filewriter/CFEMDataSorter.cpp
@@ -2,7 +2,7 @@
  * \file CFEMDataSorter.cpp
  * \brief Datasorter class for FEM solvers.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CFVMDataSorter.cpp b/SU2_CFD/src/output/filewriter/CFVMDataSorter.cpp
index 664142e3901..3e0a675eb93 100644
--- a/SU2_CFD/src/output/filewriter/CFVMDataSorter.cpp
+++ b/SU2_CFD/src/output/filewriter/CFVMDataSorter.cpp
@@ -2,7 +2,7 @@
  * \file CFVMDataSorter.cpp
  * \brief Datasorter class for FVM solvers.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CParallelDataSorter.cpp b/SU2_CFD/src/output/filewriter/CParallelDataSorter.cpp
index f4b57b34f3b..69cc4182fb1 100644
--- a/SU2_CFD/src/output/filewriter/CParallelDataSorter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParallelDataSorter.cpp
@@ -2,7 +2,7 @@
  * \file CParallelDataSorter.cpp
  * \brief Datasorter base class.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CParallelFileWriter.cpp b/SU2_CFD/src/output/filewriter/CParallelFileWriter.cpp
index 7f448c880cf..c959a171615 100644
--- a/SU2_CFD/src/output/filewriter/CParallelFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParallelFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CParallelFileWriter.cpp
  * \brief Filewriter base class.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CParaviewBinaryFileWriter.cpp b/SU2_CFD/src/output/filewriter/CParaviewBinaryFileWriter.cpp
index 677bee21961..7675fdb7bd1 100644
--- a/SU2_CFD/src/output/filewriter/CParaviewBinaryFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParaviewBinaryFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CParaviewBinaryFileWriter.cpp
  * \brief Filewriter class for Paraview binary format.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CParaviewFileWriter.cpp b/SU2_CFD/src/output/filewriter/CParaviewFileWriter.cpp
index 9e3c7726ac1..d1d3f78a6bb 100644
--- a/SU2_CFD/src/output/filewriter/CParaviewFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParaviewFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CParaviewFileWriter.cpp
  * \brief Filewriter class for Paraview ASCII format.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CParaviewVTMFileWriter.cpp b/SU2_CFD/src/output/filewriter/CParaviewVTMFileWriter.cpp
index 2b67324b64d..5b4ba4299db 100644
--- a/SU2_CFD/src/output/filewriter/CParaviewVTMFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParaviewVTMFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CParaviewVTMFileWriter.cpp
  * \brief Filewriter class for Paraview binary format.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CParaviewXMLFileWriter.cpp b/SU2_CFD/src/output/filewriter/CParaviewXMLFileWriter.cpp
index 2b453723b08..df4ac46a176 100644
--- a/SU2_CFD/src/output/filewriter/CParaviewXMLFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CParaviewXMLFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CParaviewXMLFileWriter.cpp
  * \brief Filewriter class for Paraview binary format.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CSTLFileWriter.cpp b/SU2_CFD/src/output/filewriter/CSTLFileWriter.cpp
index 3258836e479..f9049f8f2f1 100644
--- a/SU2_CFD/src/output/filewriter/CSTLFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CSTLFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CSTLFileWriter.cpp
  * \brief STL Writer output class
  * \author T. Kattmann, T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CSU2BinaryFileWriter.cpp b/SU2_CFD/src/output/filewriter/CSU2BinaryFileWriter.cpp
index 39ec96fa178..a3183266cd8 100644
--- a/SU2_CFD/src/output/filewriter/CSU2BinaryFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CSU2BinaryFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CSU2BinaryFileWriter.cpp
  * \brief Filewriter class SU2 native binary format.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CSU2FileWriter.cpp b/SU2_CFD/src/output/filewriter/CSU2FileWriter.cpp
index 1c81b799d6a..455f6c7f984 100644
--- a/SU2_CFD/src/output/filewriter/CSU2FileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CSU2FileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CSU2FileWriter.cpp
  * \brief Filewriter class SU2 native ASCII (CSV) format.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CSU2MeshFileWriter.cpp b/SU2_CFD/src/output/filewriter/CSU2MeshFileWriter.cpp
index 13b0798d982..39bc185252a 100644
--- a/SU2_CFD/src/output/filewriter/CSU2MeshFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CSU2MeshFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CSU2MeshFileWriter.cpp
  * \brief Filewriter class SU2 native mesh format.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CSurfaceFEMDataSorter.cpp b/SU2_CFD/src/output/filewriter/CSurfaceFEMDataSorter.cpp
index e92587ae898..ef19eebf145 100644
--- a/SU2_CFD/src/output/filewriter/CSurfaceFEMDataSorter.cpp
+++ b/SU2_CFD/src/output/filewriter/CSurfaceFEMDataSorter.cpp
@@ -2,7 +2,7 @@
  * \file CSurfaceFEMDataSorter.cpp
  * \brief Datasorter for FEM surfaces.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CSurfaceFVMDataSorter.cpp b/SU2_CFD/src/output/filewriter/CSurfaceFVMDataSorter.cpp
index 29c9347880e..77cc2567e90 100644
--- a/SU2_CFD/src/output/filewriter/CSurfaceFVMDataSorter.cpp
+++ b/SU2_CFD/src/output/filewriter/CSurfaceFVMDataSorter.cpp
@@ -2,7 +2,7 @@
  * \file CSurfaceFVMDataSorter.cpp
  * \brief Datasorter for FVM surfaces.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CTecplotBinaryFileWriter.cpp b/SU2_CFD/src/output/filewriter/CTecplotBinaryFileWriter.cpp
index 539191ca1de..ec01ad31428 100644
--- a/SU2_CFD/src/output/filewriter/CTecplotBinaryFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CTecplotBinaryFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CTecplotBinaryFileWriter.cpp
  * \brief Filewriter class for Tecplot binary format.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/filewriter/CTecplotFileWriter.cpp b/SU2_CFD/src/output/filewriter/CTecplotFileWriter.cpp
index 5b04ebd5c15..58a02741f28 100644
--- a/SU2_CFD/src/output/filewriter/CTecplotFileWriter.cpp
+++ b/SU2_CFD/src/output/filewriter/CTecplotFileWriter.cpp
@@ -2,7 +2,7 @@
  * \file CTecplotFileWriter.cpp
  * \brief Filewriter class for Tecplot ASCII format.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/output/tools/CWindowingTools.cpp b/SU2_CFD/src/output/tools/CWindowingTools.cpp
index 98626abfcbb..f3b228fd8f6 100644
--- a/SU2_CFD/src/output/tools/CWindowingTools.cpp
+++ b/SU2_CFD/src/output/tools/CWindowingTools.cpp
@@ -2,7 +2,7 @@
  * \file signal_processing_toolbox.cpp
  * \brief Signal processing tools
  * \author S. Schotthöfer
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/python_wrapper_structure.cpp b/SU2_CFD/src/python_wrapper_structure.cpp
index ac1b774e808..490cc193953 100644
--- a/SU2_CFD/src/python_wrapper_structure.cpp
+++ b/SU2_CFD/src/python_wrapper_structure.cpp
@@ -2,7 +2,7 @@
  * \file python_wrapper_structure.cpp
  * \brief Driver subroutines that are used by the Python wrapper. Those routines are usually called from an external Python environment.
  * \author D. Thomas
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CAdjEulerSolver.cpp b/SU2_CFD/src/solvers/CAdjEulerSolver.cpp
index 034fe16adcc..4e7ff5b2098 100644
--- a/SU2_CFD/src/solvers/CAdjEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CAdjEulerSolver.cpp
@@ -2,7 +2,7 @@
  * \file CAdjEulerSolver.cpp
  * \brief Main subroutines for solving Euler adjoint problems.
  * \author F. Palacios, T. Economon, H. Kline
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CAdjNSSolver.cpp b/SU2_CFD/src/solvers/CAdjNSSolver.cpp
index 42dbce29cdf..50ca5438e92 100644
--- a/SU2_CFD/src/solvers/CAdjNSSolver.cpp
+++ b/SU2_CFD/src/solvers/CAdjNSSolver.cpp
@@ -2,7 +2,7 @@
  * \file CAdjNSSolver.cpp
  * \brief Main subroutines for solving Navier-Stokes adjoint problems.
  * \author F. Palacios, T. Economon, H. Kline
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CAdjTurbSolver.cpp b/SU2_CFD/src/solvers/CAdjTurbSolver.cpp
index 704f4f786d0..33ea1f11841 100644
--- a/SU2_CFD/src/solvers/CAdjTurbSolver.cpp
+++ b/SU2_CFD/src/solvers/CAdjTurbSolver.cpp
@@ -2,7 +2,7 @@
  * \file CAdjTurbVariable.cpp
  * \brief Main subroutines for solving turbulent adjoint problems.
  * \author F. Palacios, A. Bueno, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CBaselineSolver.cpp b/SU2_CFD/src/solvers/CBaselineSolver.cpp
index 97a4c04d15e..7d9e483d633 100644
--- a/SU2_CFD/src/solvers/CBaselineSolver.cpp
+++ b/SU2_CFD/src/solvers/CBaselineSolver.cpp
@@ -2,7 +2,7 @@
  * \file CBaselineSolver.cpp
  * \brief Main subroutines for CBaselineSolver class.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CBaselineSolver_FEM.cpp b/SU2_CFD/src/solvers/CBaselineSolver_FEM.cpp
index bf213f5df36..19247b9ced1 100644
--- a/SU2_CFD/src/solvers/CBaselineSolver_FEM.cpp
+++ b/SU2_CFD/src/solvers/CBaselineSolver_FEM.cpp
@@ -2,7 +2,7 @@
  * \file CBaselineSolver_FEM.cpp
  * \brief Main subroutines for CBaselineSolver_FEM class.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp b/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
index b64d409e5cc..a297039ea3a 100644
--- a/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
+++ b/SU2_CFD/src/solvers/CDiscAdjFEASolver.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjFEASolver.cpp
  * \brief Main subroutines for solving adjoint FEM elasticity problems.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CDiscAdjMeshSolver.cpp b/SU2_CFD/src/solvers/CDiscAdjMeshSolver.cpp
index ff92a04d544..c23df05b762 100644
--- a/SU2_CFD/src/solvers/CDiscAdjMeshSolver.cpp
+++ b/SU2_CFD/src/solvers/CDiscAdjMeshSolver.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjMeshSolver.cpp
  * \brief Main subroutines for solving the discrete adjoint mesh problem.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CDiscAdjSolver.cpp b/SU2_CFD/src/solvers/CDiscAdjSolver.cpp
index e236b19114d..c42e2b4925f 100644
--- a/SU2_CFD/src/solvers/CDiscAdjSolver.cpp
+++ b/SU2_CFD/src/solvers/CDiscAdjSolver.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjSolver.cpp
  * \brief Main subroutines for solving the discrete adjoint problem.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index 1ce06058b5e..e665fbe06e1 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -2,7 +2,7 @@
  * \file CEulerSolver.cpp
  * \brief Main subroutines for solving Finite-Volume Euler flow problems.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CFEASolver.cpp b/SU2_CFD/src/solvers/CFEASolver.cpp
index 858257f094c..507ebbf4d47 100644
--- a/SU2_CFD/src/solvers/CFEASolver.cpp
+++ b/SU2_CFD/src/solvers/CFEASolver.cpp
@@ -2,7 +2,7 @@
  * \file CFEASolver.cpp
  * \brief Main subroutines for solving direct FEM elasticity problems.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CFEASolverBase.cpp b/SU2_CFD/src/solvers/CFEASolverBase.cpp
index 23bd6af4cb8..1280baf9bc6 100644
--- a/SU2_CFD/src/solvers/CFEASolverBase.cpp
+++ b/SU2_CFD/src/solvers/CFEASolverBase.cpp
@@ -2,7 +2,7 @@
  * \file CFEASolverBase.cpp
  * \brief Common class template for FEA solvers
  * \author T. Dick
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp b/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
index ae9da1c7350..42562cf6ba0 100644
--- a/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp
@@ -2,7 +2,7 @@
  * \file CFEM_DG_EulerSolver.cpp
  * \brief Main subroutines for solving finite element Euler flow problems
  * \author J. Alonso, E. van der Weide, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CFEM_DG_NSSolver.cpp b/SU2_CFD/src/solvers/CFEM_DG_NSSolver.cpp
index a84746c83c2..cc8e1a9511e 100644
--- a/SU2_CFD/src/solvers/CFEM_DG_NSSolver.cpp
+++ b/SU2_CFD/src/solvers/CFEM_DG_NSSolver.cpp
@@ -2,7 +2,7 @@
  * \file CFEM_DG_NSSolver.cpp
  * \brief Main subroutines for solving finite element Navier-Stokes flow problems
  * \author J. Alonso, E. van der Weide, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CGradientSmoothingSolver.cpp b/SU2_CFD/src/solvers/CGradientSmoothingSolver.cpp
index 09b391e8505..83e61cb7a9a 100644
--- a/SU2_CFD/src/solvers/CGradientSmoothingSolver.cpp
+++ b/SU2_CFD/src/solvers/CGradientSmoothingSolver.cpp
@@ -2,7 +2,7 @@
  * \file CGradientSmoothing.cpp
  * \brief Main solver routines for the gradient smoothing problem.
  * \author T. Dick
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CHeatSolver.cpp b/SU2_CFD/src/solvers/CHeatSolver.cpp
index 407fa0455cc..c0005bfa792 100644
--- a/SU2_CFD/src/solvers/CHeatSolver.cpp
+++ b/SU2_CFD/src/solvers/CHeatSolver.cpp
@@ -2,7 +2,7 @@
  * \file CHeatSolver.cpp
  * \brief Main subroutines for solving the heat equation
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CIncEulerSolver.cpp b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
index 9c8b67f410e..d8f53845622 100644
--- a/SU2_CFD/src/solvers/CIncEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CIncEulerSolver.cpp
@@ -2,7 +2,7 @@
  * \file CIncEulerSolver.cpp
  * \brief Main subroutines for solving incompressible flow (Euler, Navier-Stokes, etc.).
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CIncNSSolver.cpp b/SU2_CFD/src/solvers/CIncNSSolver.cpp
index 061c8ee02ec..659a3eebef6 100644
--- a/SU2_CFD/src/solvers/CIncNSSolver.cpp
+++ b/SU2_CFD/src/solvers/CIncNSSolver.cpp
@@ -2,7 +2,7 @@
  * \file CIncNSSolver.cpp
  * \brief Main subroutines for solving Navier-Stokes incompressible flow.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CMeshSolver.cpp b/SU2_CFD/src/solvers/CMeshSolver.cpp
index 474112d3c73..20b8269e118 100644
--- a/SU2_CFD/src/solvers/CMeshSolver.cpp
+++ b/SU2_CFD/src/solvers/CMeshSolver.cpp
@@ -2,7 +2,7 @@
  * \file CMeshSolver.cpp
  * \brief Main subroutines to solve moving meshes using a pseudo-linear elastic approach.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp b/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
index cea4549b09e..9b52b1d07b9 100644
--- a/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CNEMOEulerSolver.cpp
@@ -2,7 +2,7 @@
  * \file CNEMOEulerSolver.cpp
  * \brief Headers of the CNEMOEulerSolver class
  * \author S. R. Copeland, F. Palacios, W. Maier, C. Garbacz, J. Needels
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CNEMONSSolver.cpp b/SU2_CFD/src/solvers/CNEMONSSolver.cpp
index 33e04b5f85f..14335d45df9 100644
--- a/SU2_CFD/src/solvers/CNEMONSSolver.cpp
+++ b/SU2_CFD/src/solvers/CNEMONSSolver.cpp
@@ -2,7 +2,7 @@
  * \file CNEMONSSolver.cpp
  * \brief Headers of the CNEMONSSolver class
  * \author S. R. Copeland, F. Palacios, W. Maier.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CNSSolver.cpp b/SU2_CFD/src/solvers/CNSSolver.cpp
index b9b9b698823..b544abccff6 100644
--- a/SU2_CFD/src/solvers/CNSSolver.cpp
+++ b/SU2_CFD/src/solvers/CNSSolver.cpp
@@ -2,7 +2,7 @@
  * \file CNSSolver.cpp
  * \brief Main subroutines for solving Finite-Volume Navier-Stokes flow problems.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CRadP1Solver.cpp b/SU2_CFD/src/solvers/CRadP1Solver.cpp
index 13f6f76a1cf..49611daeb5e 100644
--- a/SU2_CFD/src/solvers/CRadP1Solver.cpp
+++ b/SU2_CFD/src/solvers/CRadP1Solver.cpp
@@ -2,7 +2,7 @@
  * \file CRadP1Solver.cpp
  * \brief Main subroutines for solving P1 radiation problems.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CRadSolver.cpp b/SU2_CFD/src/solvers/CRadSolver.cpp
index 2b5451e5398..26256446773 100644
--- a/SU2_CFD/src/solvers/CRadSolver.cpp
+++ b/SU2_CFD/src/solvers/CRadSolver.cpp
@@ -2,7 +2,7 @@
  * \file CRadP1Solver.cpp
  * \brief Main subroutines for solving generic radiation problems (P1, M1, discrete ordinates...)
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CSolver.cpp b/SU2_CFD/src/solvers/CSolver.cpp
index a7d985811ff..5cd2fd93425 100644
--- a/SU2_CFD/src/solvers/CSolver.cpp
+++ b/SU2_CFD/src/solvers/CSolver.cpp
@@ -2,7 +2,7 @@
  * \file CSolver.cpp
  * \brief Main subroutines for CSolver class.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CSolverFactory.cpp b/SU2_CFD/src/solvers/CSolverFactory.cpp
index af9669fa392..cf252ba018d 100644
--- a/SU2_CFD/src/solvers/CSolverFactory.cpp
+++ b/SU2_CFD/src/solvers/CSolverFactory.cpp
@@ -2,7 +2,7 @@
  * \file CSolverFactory.cpp
  * \brief Main subroutines for CSolverFactoryclass.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
index 2f8297a91a0..58c20ca3cc7 100644
--- a/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
+++ b/SU2_CFD/src/solvers/CSpeciesFlameletSolver.cpp
@@ -2,7 +2,7 @@
  * \file CSpeciesFlameletSolver.cpp
  * \brief Main subroutines of CSpeciesFlameletSolver class
  * \author D. Mayer, T. Economon, N. Beishuizen, E. Bunschoten
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CSpeciesSolver.cpp b/SU2_CFD/src/solvers/CSpeciesSolver.cpp
index 5acebd6164a..3d5c5406a3b 100644
--- a/SU2_CFD/src/solvers/CSpeciesSolver.cpp
+++ b/SU2_CFD/src/solvers/CSpeciesSolver.cpp
@@ -2,7 +2,7 @@
  * \file CSpeciesSolver.cpp
  * \brief Main subroutines of CSpeciesSolver class
  * \author T. Kattmann
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CTemplateSolver.cpp b/SU2_CFD/src/solvers/CTemplateSolver.cpp
index df2dd61085e..df1e6e2946a 100644
--- a/SU2_CFD/src/solvers/CTemplateSolver.cpp
+++ b/SU2_CFD/src/solvers/CTemplateSolver.cpp
@@ -2,7 +2,7 @@
  * \file CTemplateSolver.cpp
  * \brief Subroutines to be implemented for any new solvers
  * \author F. Palacios
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CTransLMSolver.cpp b/SU2_CFD/src/solvers/CTransLMSolver.cpp
index bd412a283a5..7d8fb2485a9 100644
--- a/SU2_CFD/src/solvers/CTransLMSolver.cpp
+++ b/SU2_CFD/src/solvers/CTransLMSolver.cpp
@@ -2,7 +2,7 @@
  * \file CTransLMSolver.cpp
  * \brief Main subroutines for Langtry-Menter Transition model solver.
  * \author A. Aranake, S. Kang.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CTurbSASolver.cpp b/SU2_CFD/src/solvers/CTurbSASolver.cpp
index e1f60cebbb1..2d301dc7722 100644
--- a/SU2_CFD/src/solvers/CTurbSASolver.cpp
+++ b/SU2_CFD/src/solvers/CTurbSASolver.cpp
@@ -2,7 +2,7 @@
  * \file CTurbSASolver.cpp
  * \brief Main subroutines of CTurbSASolver class
  * \author F. Palacios, A. Bueno
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CTurbSSTSolver.cpp b/SU2_CFD/src/solvers/CTurbSSTSolver.cpp
index 3918c07fba4..e1e9ef644c7 100644
--- a/SU2_CFD/src/solvers/CTurbSSTSolver.cpp
+++ b/SU2_CFD/src/solvers/CTurbSSTSolver.cpp
@@ -2,7 +2,7 @@
  * \file CTurbSSTSolver.cpp
  * \brief Main subroutines of CTurbSSTSolver class
  * \author F. Palacios, A. Bueno
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/solvers/CTurbSolver.cpp b/SU2_CFD/src/solvers/CTurbSolver.cpp
index ffd7152346b..3277cd443e0 100644
--- a/SU2_CFD/src/solvers/CTurbSolver.cpp
+++ b/SU2_CFD/src/solvers/CTurbSolver.cpp
@@ -2,7 +2,7 @@
  * \file CTurbSolver.cpp
  * \brief Main subroutines of CTurbSolver class
  * \author F. Palacios, A. Bueno
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CAdjEulerVariable.cpp b/SU2_CFD/src/variables/CAdjEulerVariable.cpp
index b574543155b..48591ed0aa2 100644
--- a/SU2_CFD/src/variables/CAdjEulerVariable.cpp
+++ b/SU2_CFD/src/variables/CAdjEulerVariable.cpp
@@ -2,7 +2,7 @@
  * \file CAdjEulerVariable.cpp
  * \brief Definition of the solution fields.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CAdjNSVariable.cpp b/SU2_CFD/src/variables/CAdjNSVariable.cpp
index f15985ddc67..1753ae9eb4d 100644
--- a/SU2_CFD/src/variables/CAdjNSVariable.cpp
+++ b/SU2_CFD/src/variables/CAdjNSVariable.cpp
@@ -2,7 +2,7 @@
  * \file CAdjNSVariable.cpp
  * \brief Definition of the solution fields.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CAdjTurbVariable.cpp b/SU2_CFD/src/variables/CAdjTurbVariable.cpp
index 73a170b57c0..ff454b08c38 100644
--- a/SU2_CFD/src/variables/CAdjTurbVariable.cpp
+++ b/SU2_CFD/src/variables/CAdjTurbVariable.cpp
@@ -2,7 +2,7 @@
  * \file CAdjTurbVariable.cpp
  * \brief Definition of the solution fields.
  * \author F. Palacios, A. Bueno
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CBaselineVariable.cpp b/SU2_CFD/src/variables/CBaselineVariable.cpp
index 4787d900518..8c8745758b9 100644
--- a/SU2_CFD/src/variables/CBaselineVariable.cpp
+++ b/SU2_CFD/src/variables/CBaselineVariable.cpp
@@ -2,7 +2,7 @@
  * \file CBaselineVariable.cpp
  * \brief Definition of the solution fields.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CDiscAdjFEABoundVariable.cpp b/SU2_CFD/src/variables/CDiscAdjFEABoundVariable.cpp
index 2dbe42cc2fc..d3454b8df60 100644
--- a/SU2_CFD/src/variables/CDiscAdjFEABoundVariable.cpp
+++ b/SU2_CFD/src/variables/CDiscAdjFEABoundVariable.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjFEAVariable.cpp
  * \brief Definition of the variables for FEM adjoint elastic structural problems.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CDiscAdjMeshBoundVariable.cpp b/SU2_CFD/src/variables/CDiscAdjMeshBoundVariable.cpp
index 1fd7a9bdc7d..8c56d503579 100644
--- a/SU2_CFD/src/variables/CDiscAdjMeshBoundVariable.cpp
+++ b/SU2_CFD/src/variables/CDiscAdjMeshBoundVariable.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjMeshVariable.cpp
  * \brief Main subroutines for the discrete adjoint mesh variable structure.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CDiscAdjVariable.cpp b/SU2_CFD/src/variables/CDiscAdjVariable.cpp
index a08a0cf88e0..2a6aa681f3a 100644
--- a/SU2_CFD/src/variables/CDiscAdjVariable.cpp
+++ b/SU2_CFD/src/variables/CDiscAdjVariable.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjVariable.cpp
  * \brief Main subroutines for the discrete adjoint variable structure.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CEulerVariable.cpp b/SU2_CFD/src/variables/CEulerVariable.cpp
index 84a0fa10696..84cb00eb67c 100644
--- a/SU2_CFD/src/variables/CEulerVariable.cpp
+++ b/SU2_CFD/src/variables/CEulerVariable.cpp
@@ -2,7 +2,7 @@
  * \file CEulerVariable.cpp
  * \brief Definition of the solution fields.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CFEABoundVariable.cpp b/SU2_CFD/src/variables/CFEABoundVariable.cpp
index 04d1e676260..a1ab96467d3 100644
--- a/SU2_CFD/src/variables/CFEABoundVariable.cpp
+++ b/SU2_CFD/src/variables/CFEABoundVariable.cpp
@@ -2,7 +2,7 @@
  * \file CFEABoundVariable.cpp
  * \brief Definition of the variables for FEM elastic structural problems.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CFEAVariable.cpp b/SU2_CFD/src/variables/CFEAVariable.cpp
index a49a9d49c66..8e3c32c36fc 100644
--- a/SU2_CFD/src/variables/CFEAVariable.cpp
+++ b/SU2_CFD/src/variables/CFEAVariable.cpp
@@ -2,7 +2,7 @@
  * \file CFEAVariable.cpp
  * \brief Definition of the variables for FEM elastic structural problems.
  * \author R. Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CFlowVariable.cpp b/SU2_CFD/src/variables/CFlowVariable.cpp
index 1fdfd484523..050f3e862d1 100644
--- a/SU2_CFD/src/variables/CFlowVariable.cpp
+++ b/SU2_CFD/src/variables/CFlowVariable.cpp
@@ -1,7 +1,7 @@
 /*!
  * \file CFlowVariable.cpp
  * \brief Definition of common solution fields for flow solvers.
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CHeatVariable.cpp b/SU2_CFD/src/variables/CHeatVariable.cpp
index f87420cea98..158aec9bcc6 100644
--- a/SU2_CFD/src/variables/CHeatVariable.cpp
+++ b/SU2_CFD/src/variables/CHeatVariable.cpp
@@ -2,7 +2,7 @@
  * \file CHeatVariable.cpp
  * \brief Definition of the variables for heat equation problems.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CIncEulerVariable.cpp b/SU2_CFD/src/variables/CIncEulerVariable.cpp
index c1bc702e54a..4fca7f5c357 100644
--- a/SU2_CFD/src/variables/CIncEulerVariable.cpp
+++ b/SU2_CFD/src/variables/CIncEulerVariable.cpp
@@ -2,7 +2,7 @@
  * \file CIncEulerVariable.cpp
  * \brief Definition of the variable classes for incompressible flow.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CIncNSVariable.cpp b/SU2_CFD/src/variables/CIncNSVariable.cpp
index c132cb20efd..e32b8d6dd73 100644
--- a/SU2_CFD/src/variables/CIncNSVariable.cpp
+++ b/SU2_CFD/src/variables/CIncNSVariable.cpp
@@ -2,7 +2,7 @@
  * \file CIncNSVariable.cpp
  * \brief Definition of the variable classes for incompressible flow.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CMeshBoundVariable.cpp b/SU2_CFD/src/variables/CMeshBoundVariable.cpp
index 6095b8c74d0..8a981ef16d1 100644
--- a/SU2_CFD/src/variables/CMeshBoundVariable.cpp
+++ b/SU2_CFD/src/variables/CMeshBoundVariable.cpp
@@ -2,7 +2,7 @@
  * \file CMeshBoundVariable.cpp
  * \brief Definition of the boundary variables for mesh motion using a pseudo-elastic approach.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CMeshElement.cpp b/SU2_CFD/src/variables/CMeshElement.cpp
index f7eb725d329..78794d873fc 100644
--- a/SU2_CFD/src/variables/CMeshElement.cpp
+++ b/SU2_CFD/src/variables/CMeshElement.cpp
@@ -2,7 +2,7 @@
  * \file CMeshElement.cpp
  * \brief Definition of the mesh elements for mesh deformation using a pseudo-elastic approach.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CMeshVariable.cpp b/SU2_CFD/src/variables/CMeshVariable.cpp
index aebd29bbf2e..c494d0447f7 100644
--- a/SU2_CFD/src/variables/CMeshVariable.cpp
+++ b/SU2_CFD/src/variables/CMeshVariable.cpp
@@ -2,7 +2,7 @@
  * \file CMeshVariable.cpp
  * \brief Definition of the variables for mesh motion using a pseudo-elastic approach.
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CNEMOEulerVariable.cpp b/SU2_CFD/src/variables/CNEMOEulerVariable.cpp
index e0a9836034a..2d8690c3ffb 100644
--- a/SU2_CFD/src/variables/CNEMOEulerVariable.cpp
+++ b/SU2_CFD/src/variables/CNEMOEulerVariable.cpp
@@ -2,7 +2,7 @@
  * \file CNEMOEulerVariable.cpp
  * \brief Definition of the solution fields.
  * \author C. Garbacz, W. Maier, S.R. Copeland
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CNEMONSVariable.cpp b/SU2_CFD/src/variables/CNEMONSVariable.cpp
index 05341d2b02a..360d996eb72 100644
--- a/SU2_CFD/src/variables/CNEMONSVariable.cpp
+++ b/SU2_CFD/src/variables/CNEMONSVariable.cpp
@@ -2,7 +2,7 @@
  * \file CNEMONSVariable.cpp
  * \brief Definition of the solution fields.
  * \author C. Garbacz, W. Maier, S.R. Copeland
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CNSVariable.cpp b/SU2_CFD/src/variables/CNSVariable.cpp
index 99b7de10741..b2fe70b35cc 100644
--- a/SU2_CFD/src/variables/CNSVariable.cpp
+++ b/SU2_CFD/src/variables/CNSVariable.cpp
@@ -2,7 +2,7 @@
  * \file CNSVariable.cpp
  * \brief Definition of the solution fields.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CRadP1Variable.cpp b/SU2_CFD/src/variables/CRadP1Variable.cpp
index 7d8a3f7f43c..529fe578dec 100644
--- a/SU2_CFD/src/variables/CRadP1Variable.cpp
+++ b/SU2_CFD/src/variables/CRadP1Variable.cpp
@@ -2,7 +2,7 @@
  * \file CRadP1Variable.cpp
  * \brief Definition of the P1 model variables
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CRadVariable.cpp b/SU2_CFD/src/variables/CRadVariable.cpp
index b50a054c41f..97bcdf1e934 100644
--- a/SU2_CFD/src/variables/CRadVariable.cpp
+++ b/SU2_CFD/src/variables/CRadVariable.cpp
@@ -2,7 +2,7 @@
  * \file CRadVariable.cpp
  * \brief Definition of the radiation variables
  * \author Ruben Sanchez
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CScalarVariable.cpp b/SU2_CFD/src/variables/CScalarVariable.cpp
index e516cfa7c2e..fcb9a491eaa 100644
--- a/SU2_CFD/src/variables/CScalarVariable.cpp
+++ b/SU2_CFD/src/variables/CScalarVariable.cpp
@@ -2,7 +2,7 @@
  * \file CScalarVariable.cpp
  * \brief Definition of the solution fields.
  * \author F. Palacios, A. Bueno
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CSobolevSmoothingVariable.cpp b/SU2_CFD/src/variables/CSobolevSmoothingVariable.cpp
index 523c1dd78a8..d332aa71720 100644
--- a/SU2_CFD/src/variables/CSobolevSmoothingVariable.cpp
+++ b/SU2_CFD/src/variables/CSobolevSmoothingVariable.cpp
@@ -2,7 +2,7 @@
  * \file CSobolevSmoothingVariable.cpp
  * \brief Definition of the variables for gradient smoothing problems.
  * \author T. Dick
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CSpeciesFlameletVariable.cpp b/SU2_CFD/src/variables/CSpeciesFlameletVariable.cpp
index 16536909bee..658d5c85722 100644
--- a/SU2_CFD/src/variables/CSpeciesFlameletVariable.cpp
+++ b/SU2_CFD/src/variables/CSpeciesFlameletVariable.cpp
@@ -2,7 +2,7 @@
  * \file CSpeciesFlameletVariable.cpp
  * \brief Definition of the variable fields for the flamelet class.
  * \author D. Mayer, T. Economon, N. Beishuizen
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CSpeciesVariable.cpp b/SU2_CFD/src/variables/CSpeciesVariable.cpp
index 7f903533499..ddf9f1dd726 100644
--- a/SU2_CFD/src/variables/CSpeciesVariable.cpp
+++ b/SU2_CFD/src/variables/CSpeciesVariable.cpp
@@ -2,7 +2,7 @@
  * \file CSpeciesVariable.cpp
  * \brief Definition of the solution fields.
  * \author T. Kattmann
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CTransLMVariable.cpp b/SU2_CFD/src/variables/CTransLMVariable.cpp
index 31610502131..c5a4a503fa6 100644
--- a/SU2_CFD/src/variables/CTransLMVariable.cpp
+++ b/SU2_CFD/src/variables/CTransLMVariable.cpp
@@ -2,7 +2,7 @@
  * \file CTransLMVariable.cpp
  * \brief Definition of the solution fields.
  * \author A. Aranake, S. Kang
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CTurbSAVariable.cpp b/SU2_CFD/src/variables/CTurbSAVariable.cpp
index c49c261b46d..454ce5734a8 100644
--- a/SU2_CFD/src/variables/CTurbSAVariable.cpp
+++ b/SU2_CFD/src/variables/CTurbSAVariable.cpp
@@ -2,7 +2,7 @@
  * \file CTurbSAVariable.cpp
  * \brief Definition of the solution fields.
  * \author F. Palacios, A. Bueno
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CTurbSSTVariable.cpp b/SU2_CFD/src/variables/CTurbSSTVariable.cpp
index 3a54562e438..9778f1e37cc 100644
--- a/SU2_CFD/src/variables/CTurbSSTVariable.cpp
+++ b/SU2_CFD/src/variables/CTurbSSTVariable.cpp
@@ -2,7 +2,7 @@
  * \file CTurbSSTVariable.cpp
  * \brief Definition of the solution fields.
  * \author F. Palacios, A. Bueno
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CTurbVariable.cpp b/SU2_CFD/src/variables/CTurbVariable.cpp
index 9a139f8490f..54bede5033f 100644
--- a/SU2_CFD/src/variables/CTurbVariable.cpp
+++ b/SU2_CFD/src/variables/CTurbVariable.cpp
@@ -2,7 +2,7 @@
  * \file CTurbVariable.cpp
  * \brief Definition of the solution fields.
  * \author F. Palacios, A. Bueno
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_CFD/src/variables/CVariable.cpp b/SU2_CFD/src/variables/CVariable.cpp
index 01d22d7e0af..601a25f62bc 100644
--- a/SU2_CFD/src/variables/CVariable.cpp
+++ b/SU2_CFD/src/variables/CVariable.cpp
@@ -2,7 +2,7 @@
  * \file CVariable.cpp
  * \brief Definition of the solution fields.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_DEF/include/drivers/CDeformationDriver.hpp b/SU2_DEF/include/drivers/CDeformationDriver.hpp
index cfdd8830d88..ae731d601e7 100644
--- a/SU2_DEF/include/drivers/CDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDeformationDriver.hpp
@@ -2,7 +2,7 @@
  * \file CDeformationDriver.hpp
  * \brief Headers of the main subroutines for driving the mesh deformation.
  * \author A. Gastaldi, H. Patel
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
index 93bf81a55c5..2feddd82224 100644
--- a/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
+++ b/SU2_DEF/include/drivers/CDiscAdjDeformationDriver.hpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjDeformationDriver.cpp
  * \brief Headers of the main subroutines for driving the projection of sensitivities.
  * \author T. Economon, H. Kline, R. Sanchez, A. Gastaldi, H. Patel
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_DEF/src/SU2_DEF.cpp b/SU2_DEF/src/SU2_DEF.cpp
index ccf25daf49e..2597ec778c0 100644
--- a/SU2_DEF/src/SU2_DEF.cpp
+++ b/SU2_DEF/src/SU2_DEF.cpp
@@ -2,7 +2,7 @@
  * \file SU2_DEF.cpp
  * \brief Main file of Mesh Deformation Code (SU2_DEF).
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_DEF/src/drivers/CDeformationDriver.cpp b/SU2_DEF/src/drivers/CDeformationDriver.cpp
index 914eae2f1c2..4a147ff55ac 100644
--- a/SU2_DEF/src/drivers/CDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDeformationDriver.cpp
@@ -2,7 +2,7 @@
  * \file CDeformationDriver.cpp
  * \brief Main subroutines for driving the mesh deformation.
  * \author A. Gastaldi, H. Patel
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
index e37b1bb0c00..99c3546389b 100644
--- a/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
+++ b/SU2_DEF/src/drivers/CDiscAdjDeformationDriver.cpp
@@ -2,7 +2,7 @@
  * \file CDiscAdjDeformationDriver.cpp
  * \brief Main subroutines for driving the projection of sensitivities.
  * \author T. Economon, H. Kline, R. Sanchez, A. Gastaldi, H. Patel
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_DOT/src/SU2_DOT.cpp b/SU2_DOT/src/SU2_DOT.cpp
index cc02b7fb9d5..92b063447f6 100644
--- a/SU2_DOT/src/SU2_DOT.cpp
+++ b/SU2_DOT/src/SU2_DOT.cpp
@@ -2,7 +2,7 @@
  * \file SU2_DOT.cpp
  * \brief Main file of the Gradient Projection Code (SU2_DOT).
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_GEO/include/SU2_GEO.hpp b/SU2_GEO/include/SU2_GEO.hpp
index 223112ba9fc..55e4aa2a3fe 100644
--- a/SU2_GEO/include/SU2_GEO.hpp
+++ b/SU2_GEO/include/SU2_GEO.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines of the code SU2_GEO.
  *        The subroutines and functions are in the <i>SU2_GEO.cpp</i> file.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_GEO/src/SU2_GEO.cpp b/SU2_GEO/src/SU2_GEO.cpp
index 585fa7aec7f..a509fbadac8 100644
--- a/SU2_GEO/src/SU2_GEO.cpp
+++ b/SU2_GEO/src/SU2_GEO.cpp
@@ -2,7 +2,7 @@
  * \file SU2_GEO.cpp
  * \brief Main file of the Geometry Definition Code (SU2_GEO).
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_PY/FSI_tools/FSIInterface.py b/SU2_PY/FSI_tools/FSIInterface.py
index 176f26c394f..4375d53c58d 100644
--- a/SU2_PY/FSI_tools/FSIInterface.py
+++ b/SU2_PY/FSI_tools/FSIInterface.py
@@ -3,7 +3,7 @@
 ## \file FSIInterface.py
 #  \brief FSI interface class that handles fluid/solid solvers synchronisation and communication.
 #  \authors Nicola Fonzi, Vittorio Cavalieri based on the work of David Thomas
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/FSI_tools/FSI_config.py b/SU2_PY/FSI_tools/FSI_config.py
index a0fca32d019..12828d7721a 100644
--- a/SU2_PY/FSI_tools/FSI_config.py
+++ b/SU2_PY/FSI_tools/FSI_config.py
@@ -3,7 +3,7 @@
 ## \file FSI_config.py
 #  \brief Python class for handling configuration file for FSI computation.
 #  \authors Nicola Fonzi, Vittorio Cavalieri based on the work of David Thomas
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/OptimalPropeller.py b/SU2_PY/OptimalPropeller.py
index 388689fb637..fff4202c644 100644
--- a/SU2_PY/OptimalPropeller.py
+++ b/SU2_PY/OptimalPropeller.py
@@ -1,7 +1,7 @@
 ## \file OptimalPropeller.py
 #  \brief Python script for generating the ActuatorDisk.dat file.
 #  \author E. Saetta, L. Russo, R. Tognaccini
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/eval/design.py b/SU2_PY/SU2/eval/design.py
index bac8c91987d..fb7d61b4ad2 100644
--- a/SU2_PY/SU2/eval/design.py
+++ b/SU2_PY/SU2/eval/design.py
@@ -3,7 +3,7 @@
 ## \file design.py
 #  \brief python package for designs
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/eval/functions.py b/SU2_PY/SU2/eval/functions.py
index 08dc2f19692..c215a863426 100644
--- a/SU2_PY/SU2/eval/functions.py
+++ b/SU2_PY/SU2/eval/functions.py
@@ -3,7 +3,7 @@
 ## \file functions.py
 #  \brief python package for functions
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/eval/gradients.py b/SU2_PY/SU2/eval/gradients.py
index da8b76d94c7..f768fa69e90 100644
--- a/SU2_PY/SU2/eval/gradients.py
+++ b/SU2_PY/SU2/eval/gradients.py
@@ -3,7 +3,7 @@
 ## \file gradients.py
 #  \brief python package for gradients
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/io/config.py b/SU2_PY/SU2/io/config.py
index 41cac49d5db..5768b0660f3 100755
--- a/SU2_PY/SU2/io/config.py
+++ b/SU2_PY/SU2/io/config.py
@@ -3,7 +3,7 @@
 ## \file config.py
 #  \brief python package for config
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/io/config_options.py b/SU2_PY/SU2/io/config_options.py
index 512aa9d1f89..dce4261f427 100644
--- a/SU2_PY/SU2/io/config_options.py
+++ b/SU2_PY/SU2/io/config_options.py
@@ -1,7 +1,7 @@
 # \file config_options.py
 #  \brief python package for config
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/io/data.py b/SU2_PY/SU2/io/data.py
index a666b3643e4..850f3eb4eec 100644
--- a/SU2_PY/SU2/io/data.py
+++ b/SU2_PY/SU2/io/data.py
@@ -3,7 +3,7 @@
 ## \file data.py
 #  \brief python package for data utility functions
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/io/filelock.py b/SU2_PY/SU2/io/filelock.py
index 1a6a15b19ae..0bdda9ae390 100644
--- a/SU2_PY/SU2/io/filelock.py
+++ b/SU2_PY/SU2/io/filelock.py
@@ -3,7 +3,7 @@
 ## \file filelock.py
 #  \brief python package for filelocking
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/io/redirect.py b/SU2_PY/SU2/io/redirect.py
index b81a80d2e82..4cf248c7145 100644
--- a/SU2_PY/SU2/io/redirect.py
+++ b/SU2_PY/SU2/io/redirect.py
@@ -3,7 +3,7 @@
 ## \file redirect.py
 #  \brief python package for file redirection
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/io/state.py b/SU2_PY/SU2/io/state.py
index 3203c10a012..584f4ab1f28 100644
--- a/SU2_PY/SU2/io/state.py
+++ b/SU2_PY/SU2/io/state.py
@@ -3,7 +3,7 @@
 ## \file state.py
 #  \brief python package for state
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/io/tools.py b/SU2_PY/SU2/io/tools.py
index 0bf58603942..35a5d2ef45f 100755
--- a/SU2_PY/SU2/io/tools.py
+++ b/SU2_PY/SU2/io/tools.py
@@ -3,7 +3,7 @@
 ## \file tools.py
 #  \brief file i/o functions
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/opt/project.py b/SU2_PY/SU2/opt/project.py
index b5b4c301780..5a26924f481 100644
--- a/SU2_PY/SU2/opt/project.py
+++ b/SU2_PY/SU2/opt/project.py
@@ -3,7 +3,7 @@
 ## \file project.py
 #  \brief package for optimization projects
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/opt/scipy_tools.py b/SU2_PY/SU2/opt/scipy_tools.py
index 3dbe18f83bc..1fdc5d81cca 100644
--- a/SU2_PY/SU2/opt/scipy_tools.py
+++ b/SU2_PY/SU2/opt/scipy_tools.py
@@ -3,7 +3,7 @@
 ## \file scipy_tools.py
 #  \brief tools for interfacing with scipy
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/run/adjoint.py b/SU2_PY/SU2/run/adjoint.py
index a9bd9b32b9a..394bbae7b94 100644
--- a/SU2_PY/SU2/run/adjoint.py
+++ b/SU2_PY/SU2/run/adjoint.py
@@ -3,7 +3,7 @@
 ## \file adjoint.py
 #  \brief python package for running adjoint problems
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/run/deform.py b/SU2_PY/SU2/run/deform.py
index 6f2638672bf..28b033621a1 100644
--- a/SU2_PY/SU2/run/deform.py
+++ b/SU2_PY/SU2/run/deform.py
@@ -3,7 +3,7 @@
 ## \file deform.py
 #  \brief python package for deforming meshes
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/run/direct.py b/SU2_PY/SU2/run/direct.py
index 2bbe23b1884..98ef77ea4e6 100644
--- a/SU2_PY/SU2/run/direct.py
+++ b/SU2_PY/SU2/run/direct.py
@@ -3,7 +3,7 @@
 ## \file direct.py
 #  \brief python package for running direct solutions
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/run/geometry.py b/SU2_PY/SU2/run/geometry.py
index 63ccef8c88f..3257a332f10 100644
--- a/SU2_PY/SU2/run/geometry.py
+++ b/SU2_PY/SU2/run/geometry.py
@@ -3,7 +3,7 @@
 ## \file geometry.py
 #  \brief python package for running geometry analyses
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/run/interface.py b/SU2_PY/SU2/run/interface.py
index 330e66ba93f..796c5977091 100644
--- a/SU2_PY/SU2/run/interface.py
+++ b/SU2_PY/SU2/run/interface.py
@@ -3,7 +3,7 @@
 ## \file interface.py
 #  \brief python package interfacing with the SU2 suite
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/run/merge.py b/SU2_PY/SU2/run/merge.py
index 2e66d14cfc3..39b7a38e181 100644
--- a/SU2_PY/SU2/run/merge.py
+++ b/SU2_PY/SU2/run/merge.py
@@ -1,7 +1,7 @@
 ## \file merge.py
 #  \brief python package for merging meshes
 #  \author T. Economon, T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/run/projection.py b/SU2_PY/SU2/run/projection.py
index fb39aa863a7..4afbc0d6884 100644
--- a/SU2_PY/SU2/run/projection.py
+++ b/SU2_PY/SU2/run/projection.py
@@ -3,7 +3,7 @@
 ## \file projection.py
 #  \brief python package for running gradient projection
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/util/filter_adjoint.py b/SU2_PY/SU2/util/filter_adjoint.py
index a7e1df79247..226f505b6f5 100644
--- a/SU2_PY/SU2/util/filter_adjoint.py
+++ b/SU2_PY/SU2/util/filter_adjoint.py
@@ -3,7 +3,7 @@
 ## \file filter_adjoint.py
 #  \brief Applies various filters to the adjoint surface sensitivities of an airfoil
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/util/plot.py b/SU2_PY/SU2/util/plot.py
index 1591c7849e1..0450f2a96ca 100644
--- a/SU2_PY/SU2/util/plot.py
+++ b/SU2_PY/SU2/util/plot.py
@@ -3,7 +3,7 @@
 ## \file plot.py
 #  \brief python package for plotting
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/util/polarSweepLib.py b/SU2_PY/SU2/util/polarSweepLib.py
index f242769a43a..2114d8c9966 100755
--- a/SU2_PY/SU2/util/polarSweepLib.py
+++ b/SU2_PY/SU2/util/polarSweepLib.py
@@ -1,7 +1,7 @@
 # \file polarSweepLib.py
 #  \brief Functions library for compute_polar.py script.
 #  \author E Arad
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2/util/which.py b/SU2_PY/SU2/util/which.py
index 115b7905a88..e4bb84f889f 100644
--- a/SU2_PY/SU2/util/which.py
+++ b/SU2_PY/SU2/util/which.py
@@ -3,7 +3,7 @@
 ## \file which.py
 #  \brief looks for where a program is
 #  \author T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2_CFD.py b/SU2_PY/SU2_CFD.py
index 0ffe32fc6a7..fe786936fea 100755
--- a/SU2_PY/SU2_CFD.py
+++ b/SU2_PY/SU2_CFD.py
@@ -3,7 +3,7 @@
 ## \file SU2_CFD.py
 #  \brief Python script to launch SU2_CFD through the Python Wrapper.
 #  \author David Thomas
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/SU2_Nastran/pysu2_nastran.py b/SU2_PY/SU2_Nastran/pysu2_nastran.py
index e629d3d6d5a..b0d3b8c6965 100644
--- a/SU2_PY/SU2_Nastran/pysu2_nastran.py
+++ b/SU2_PY/SU2_Nastran/pysu2_nastran.py
@@ -3,7 +3,7 @@
 ## \file pysu2_nastran.py
 #  \brief Structural solver using Nastran models
 #  \authors Nicola Fonzi, Vittorio Cavalieri, based on the work of David Thomas
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/change_version_number.py b/SU2_PY/change_version_number.py
index db448d73173..e6358c8b73e 100755
--- a/SU2_PY/change_version_number.py
+++ b/SU2_PY/change_version_number.py
@@ -3,7 +3,7 @@
 ## \file change_version_number.py
 #  \brief Python script for updating the version number of the SU2 suite.
 #  \author A. Aranake
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
@@ -55,8 +55,8 @@
 if not options.version:
     parser.error("new version number must be provided with -v option")
 
-oldvers = '7.5.1 "Blackbird"'
-oldvers_q = r"7.5.1 \"Blackbird\""
+oldvers = '8.0.0 "Harrier"'
+oldvers_q = r"8.0.0 \"Harrier\""
 newvers = str(options.version) + ' "' + str(options.releasename) + '"'
 newvers_q = str(options.version) + ' \\"' + str(options.releasename) + '\\"'
 # oldvers = 'Copyright 2012-2023, SU2'
diff --git a/SU2_PY/compute_polar.py b/SU2_PY/compute_polar.py
index dd974e37293..102a5eb8bdb 100755
--- a/SU2_PY/compute_polar.py
+++ b/SU2_PY/compute_polar.py
@@ -3,7 +3,7 @@
 ## \file Compute_polar.py
 #  \brief Python script for performing polar sweep.
 #  \author E Arad (based on T. Lukaczyk and  F. Palacios script)
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/compute_uncertainty.py b/SU2_PY/compute_uncertainty.py
index 1184719deef..57fb9b3e598 100755
--- a/SU2_PY/compute_uncertainty.py
+++ b/SU2_PY/compute_uncertainty.py
@@ -3,7 +3,7 @@
 ## \file compute_uncertainty.py
 #  \brief Python script for performing model-form UQ for SST turbulence model
 #  \author J. Mukhopadhaya
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/continuous_adjoint.py b/SU2_PY/continuous_adjoint.py
index bf3358cbe8f..8ec95d2ad31 100755
--- a/SU2_PY/continuous_adjoint.py
+++ b/SU2_PY/continuous_adjoint.py
@@ -3,7 +3,7 @@
 ## \file continuous_adjoint.py
 #  \brief Python script for continuous adjoint computation using the SU2 suite.
 #  \author F. Palacios, T. Economon, T. Lukaczyk
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/direct_differentiation.py b/SU2_PY/direct_differentiation.py
index d81eef0f83a..e5d458ae582 100755
--- a/SU2_PY/direct_differentiation.py
+++ b/SU2_PY/direct_differentiation.py
@@ -3,7 +3,7 @@
 ## \file direct_differentiation.py
 #  \brief Python script for doing the direct differentiation computation using the SU2 suite.
 #  \author F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/discrete_adjoint.py b/SU2_PY/discrete_adjoint.py
index 8afb09b2555..30f07747df4 100755
--- a/SU2_PY/discrete_adjoint.py
+++ b/SU2_PY/discrete_adjoint.py
@@ -3,7 +3,7 @@
 ## \file discrete_adjoint.py
 #  \brief Python script for doing the discrete adjoint computation using the SU2 suite.
 #  \author F. Palacios, T. Economon, T. Lukaczyk
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/finite_differences.py b/SU2_PY/finite_differences.py
index d6684b3706b..589905f7ccc 100755
--- a/SU2_PY/finite_differences.py
+++ b/SU2_PY/finite_differences.py
@@ -3,7 +3,7 @@
 ## \file finite_differences.py
 #  \brief Python script for doing the finite differences computation using the SU2 suite.
 #  \author F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/fsi_computation.py b/SU2_PY/fsi_computation.py
index 9abda6639d4..4f497290332 100755
--- a/SU2_PY/fsi_computation.py
+++ b/SU2_PY/fsi_computation.py
@@ -3,7 +3,7 @@
 ## \file fsi_computation.py
 #  \brief Python wrapper code for FSI computation by coupling a third-party structural solver to SU2.
 #  \authors Nicola Fonzi, Vittorio Cavalieri based on the work of David Thomas
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/merge_solution.py b/SU2_PY/merge_solution.py
index 87f7ae06f1b..94c4ec9ffbb 100755
--- a/SU2_PY/merge_solution.py
+++ b/SU2_PY/merge_solution.py
@@ -3,7 +3,7 @@
 ## \file merge_solution.py
 #  \brief Python script for merging of the solution files.
 #  \author F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/mesh_deformation.py b/SU2_PY/mesh_deformation.py
index b77b0269d0c..5420a6b62c2 100755
--- a/SU2_PY/mesh_deformation.py
+++ b/SU2_PY/mesh_deformation.py
@@ -3,7 +3,7 @@
 ## \file mesh_deformation.py
 #  \brief Python script for doing the parallel deformation using SU2_DEF.
 #  \author F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/parallel_computation.py b/SU2_PY/parallel_computation.py
index a20a5bfb088..0aaa7825c70 100755
--- a/SU2_PY/parallel_computation.py
+++ b/SU2_PY/parallel_computation.py
@@ -3,7 +3,7 @@
 ## \file parallel_computation.py
 #  \brief Python script for doing the continuous adjoint computation using the SU2 suite.
 #  \author T. Economon, T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/parallel_computation_fsi.py b/SU2_PY/parallel_computation_fsi.py
index 20a33338240..e81a32d7ba3 100755
--- a/SU2_PY/parallel_computation_fsi.py
+++ b/SU2_PY/parallel_computation_fsi.py
@@ -3,7 +3,7 @@
 ## \file parallel_computation_fsi.py
 #  \brief Python script for running FSI simulations using the SU2 suite.
 #  \author T. Economon, T. Lukaczyk, F. Palacios, H. Kline, R. Sanchez
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/parse_config.py b/SU2_PY/parse_config.py
index aa57502a683..6157d3985b2 100755
--- a/SU2_PY/parse_config.py
+++ b/SU2_PY/parse_config.py
@@ -3,7 +3,7 @@
 ## \file parse_config.py
 #  \brief Builds a worksheet of all SU2.cpp options
 #  \author A. Aranake, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/profiling.py b/SU2_PY/profiling.py
index a8894197ffd..b14382db8ca 100755
--- a/SU2_PY/profiling.py
+++ b/SU2_PY/profiling.py
@@ -3,7 +3,7 @@
 ## \file profiling.py
 #  \brief Python script for postprocessing the SU2 custom profiling (profiling.csv)
 #  \author T. Economon
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/pySU2/pySU2.i b/SU2_PY/pySU2/pySU2.i
index f783c324335..2fb6e2b058f 100644
--- a/SU2_PY/pySU2/pySU2.i
+++ b/SU2_PY/pySU2/pySU2.i
@@ -4,7 +4,7 @@
 # \file pySU2.i
 # \brief Configuration file for the Swig compilation of the Python wrapper.
 # \author D. Thomas
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/pySU2/pySU2ad.i b/SU2_PY/pySU2/pySU2ad.i
index 8bca85fdd2d..67ce17d7669 100644
--- a/SU2_PY/pySU2/pySU2ad.i
+++ b/SU2_PY/pySU2/pySU2ad.i
@@ -4,7 +4,7 @@
 # \file pySU2ad.i
 # \brief Configuration file for the Swig compilation of the Python wrapper.
 # \author D. Thomas, R. Sanchez
-# \version 7.5.1 "Blackbird"
+# \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/set_ffd_design_var.py b/SU2_PY/set_ffd_design_var.py
index 6c5c798c3ad..ec343c0e75c 100755
--- a/SU2_PY/set_ffd_design_var.py
+++ b/SU2_PY/set_ffd_design_var.py
@@ -3,7 +3,7 @@
 ## \file set_ffd_design_var.py
 #  \brief Python script for automatically generating a list of FFD variables.
 #  \author T. Economon, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/shape_optimization.py b/SU2_PY/shape_optimization.py
index 20cf15d4038..c5edaa09b7d 100755
--- a/SU2_PY/shape_optimization.py
+++ b/SU2_PY/shape_optimization.py
@@ -3,7 +3,7 @@
 ## \file shape_optimization.py
 #  \brief Python script for performing the shape optimization.
 #  \author T. Economon, T. Lukaczyk, F. Palacios
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
@@ -106,7 +106,7 @@ def main():
         "|    ___ _   _ ___                                                      |\n"
     )
     sys.stdout.write(
-        '|   / __| | | |_  )   Release 7.5.1 "Blackbird"                         |\n'
+        '|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |\n'
     )
     sys.stdout.write(
         "|   \\__ \\ |_| |/ /                                                      |\n"
diff --git a/SU2_PY/topology_optimization.py b/SU2_PY/topology_optimization.py
index 45a8818d4ac..f8fcfd38885 100755
--- a/SU2_PY/topology_optimization.py
+++ b/SU2_PY/topology_optimization.py
@@ -2,7 +2,7 @@
 
 ## \file topology_optimization.py
 #  \brief Python script to drive SU2 in topology optimization.
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_PY/updateHistoryMap.py b/SU2_PY/updateHistoryMap.py
index d391dfa9d83..ffd29019261 100644
--- a/SU2_PY/updateHistoryMap.py
+++ b/SU2_PY/updateHistoryMap.py
@@ -3,7 +3,7 @@
 ## \file updateHistoryMap.py
 #  \brief Python script for updating the historyMap.py file.
 #  \author T. Albring
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/SU2_SOL/include/SU2_SOL.hpp b/SU2_SOL/include/SU2_SOL.hpp
index 47e9c842f15..5097dea4154 100644
--- a/SU2_SOL/include/SU2_SOL.hpp
+++ b/SU2_SOL/include/SU2_SOL.hpp
@@ -3,7 +3,7 @@
  * \brief Headers of the main subroutines of the code SU2_SOL.
  *        The subroutines and functions are in the <i>SU2_SOL.cpp</i> file.
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/SU2_SOL/src/SU2_SOL.cpp b/SU2_SOL/src/SU2_SOL.cpp
index a68498b0e07..4d26b1a4844 100644
--- a/SU2_SOL/src/SU2_SOL.cpp
+++ b/SU2_SOL/src/SU2_SOL.cpp
@@ -2,7 +2,7 @@
  * \file SU2_SOL.cpp
  * \brief Main file for the solution export/conversion code (SU2_SOL).
  * \author F. Palacios, T. Economon
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/TestCases/TestCase.py b/TestCases/TestCase.py
index 0d0b39d735a..488865bc936 100644
--- a/TestCases/TestCase.py
+++ b/TestCases/TestCase.py
@@ -3,7 +3,7 @@
 ## \file TestCase.py
 #  \brief Python class for automated regression testing of SU2 examples
 #  \author A. Aranake, A. Campos, T. Economon, T. Lukaczyk, S. Padron
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/aeroelastic/aeroelastic_NACA64A010.cfg b/TestCases/aeroelastic/aeroelastic_NACA64A010.cfg
index cbb53e213ef..883979e23e0 100644
--- a/TestCases/aeroelastic/aeroelastic_NACA64A010.cfg
+++ b/TestCases/aeroelastic/aeroelastic_NACA64A010.cfg
@@ -5,7 +5,7 @@
 % Author: Santiago Padron                                                      %
 % Institution: Stanford University                                             %
 % Date: 07-09-15                                                               %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/axisymmetric_rans/air_nozzle/air_nozzle_restart.cfg b/TestCases/axisymmetric_rans/air_nozzle/air_nozzle_restart.cfg
index effd129b9df..bc6bd05fc6e 100644
--- a/TestCases/axisymmetric_rans/air_nozzle/air_nozzle_restart.cfg
+++ b/TestCases/axisymmetric_rans/air_nozzle/air_nozzle_restart.cfg
@@ -4,7 +4,7 @@
 % Case description: Axisymmetric supersonic converging-diverging air nozzle    %
 % Author: Florian Dittmann                                                     %
 % Date: 2021.12.02                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/cont_adj_euler/naca0012/inv_NACA0012.cfg b/TestCases/cont_adj_euler/naca0012/inv_NACA0012.cfg
index f8ba55367fc..96f0ea2e43d 100644
--- a/TestCases/cont_adj_euler/naca0012/inv_NACA0012.cfg
+++ b/TestCases/cont_adj_euler/naca0012/inv_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_euler/naca0012/inv_NACA0012_FD.cfg b/TestCases/cont_adj_euler/naca0012/inv_NACA0012_FD.cfg
index 32c74d5c1eb..1a9bc3ac798 100644
--- a/TestCases/cont_adj_euler/naca0012/inv_NACA0012_FD.cfg
+++ b/TestCases/cont_adj_euler/naca0012/inv_NACA0012_FD.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg b/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg
index 172fdb8dc6b..e6b16f0575e 100644
--- a/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg
+++ b/TestCases/cont_adj_euler/naca0012/inv_NACA0012_discadj.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_euler/oneram6/inv_ONERAM6.cfg b/TestCases/cont_adj_euler/oneram6/inv_ONERAM6.cfg
index d23b4072609..087457f061c 100644
--- a/TestCases/cont_adj_euler/oneram6/inv_ONERAM6.cfg
+++ b/TestCases/cont_adj_euler/oneram6/inv_ONERAM6.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2015.08.25                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_euler/wedge/inv_wedge_ROE.cfg b/TestCases/cont_adj_euler/wedge/inv_wedge_ROE.cfg
index b659a44e6d2..ea2d11081a4 100644
--- a/TestCases/cont_adj_euler/wedge/inv_wedge_ROE.cfg
+++ b/TestCases/cont_adj_euler/wedge/inv_wedge_ROE.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2012.10.07                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_euler/wedge/inv_wedge_ROE_multiobj.cfg b/TestCases/cont_adj_euler/wedge/inv_wedge_ROE_multiobj.cfg
index 89e84be2421..d31759e32ca 100644
--- a/TestCases/cont_adj_euler/wedge/inv_wedge_ROE_multiobj.cfg
+++ b/TestCases/cont_adj_euler/wedge/inv_wedge_ROE_multiobj.cfg
@@ -6,7 +6,7 @@
 % Author: H.L. Kline, modified from inviscid wedge by Thomas D. Economon       %
 % Institution: Stanford University                                             %
 % Date: 2018.01.07                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_navierstokes/cylinder/lam_cylinder.cfg b/TestCases/cont_adj_navierstokes/cylinder/lam_cylinder.cfg
index a77f8c0fcaf..8ed53e331ac 100644
--- a/TestCases/cont_adj_navierstokes/cylinder/lam_cylinder.cfg
+++ b/TestCases/cont_adj_navierstokes/cylinder/lam_cylinder.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.03.01                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_navierstokes/naca0012_sub/lam_NACA0012.cfg b/TestCases/cont_adj_navierstokes/naca0012_sub/lam_NACA0012.cfg
index 53e3202e8ea..674af9042f3 100644
--- a/TestCases/cont_adj_navierstokes/naca0012_sub/lam_NACA0012.cfg
+++ b/TestCases/cont_adj_navierstokes/naca0012_sub/lam_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: Jul 18th, 2014                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_navierstokes/naca0012_trans/lam_NACA0012.cfg b/TestCases/cont_adj_navierstokes/naca0012_trans/lam_NACA0012.cfg
index 7cb5eee3de7..d2f99966354 100644
--- a/TestCases/cont_adj_navierstokes/naca0012_trans/lam_NACA0012.cfg
+++ b/TestCases/cont_adj_navierstokes/naca0012_trans/lam_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: Jul 18th, 2014                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_rans/naca0012/turb_nasa.cfg b/TestCases/cont_adj_rans/naca0012/turb_nasa.cfg
index 628a4db8a5d..92b3b7189b7 100644
--- a/TestCases/cont_adj_rans/naca0012/turb_nasa.cfg
+++ b/TestCases/cont_adj_rans/naca0012/turb_nasa.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.03.01                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_rans/naca0012/turb_nasa_binary.cfg b/TestCases/cont_adj_rans/naca0012/turb_nasa_binary.cfg
index 0ce12b1f16f..46be0b5f825 100644
--- a/TestCases/cont_adj_rans/naca0012/turb_nasa_binary.cfg
+++ b/TestCases/cont_adj_rans/naca0012/turb_nasa_binary.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.03.01                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_rans/oneram6/turb_ONERAM6.cfg b/TestCases/cont_adj_rans/oneram6/turb_ONERAM6.cfg
index 7a99624cf9e..b82dcf516ca 100644
--- a/TestCases/cont_adj_rans/oneram6/turb_ONERAM6.cfg
+++ b/TestCases/cont_adj_rans/oneram6/turb_ONERAM6.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.03.01                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/cont_adj_rans/rae2822/turb_SA_RAE2822.cfg b/TestCases/cont_adj_rans/rae2822/turb_SA_RAE2822.cfg
index fb2ea6d9e65..e7cad06fd8d 100644
--- a/TestCases/cont_adj_rans/rae2822/turb_SA_RAE2822.cfg
+++ b/TestCases/cont_adj_rans/rae2822/turb_SA_RAE2822.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/control_surface/inv_ONERAM6_moving.cfg b/TestCases/control_surface/inv_ONERAM6_moving.cfg
index 1119269cce6..b698bf27689 100644
--- a/TestCases/control_surface/inv_ONERAM6_moving.cfg
+++ b/TestCases/control_surface/inv_ONERAM6_moving.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 09.07.2011                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/control_surface/inv_ONERAM6_setting.cfg b/TestCases/control_surface/inv_ONERAM6_setting.cfg
index 19e10e6bfef..c48c32c31e0 100644
--- a/TestCases/control_surface/inv_ONERAM6_setting.cfg
+++ b/TestCases/control_surface/inv_ONERAM6_setting.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 09.07.2011                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/coupled_cht/comp_2d/cht_2d_3cylinders.cfg b/TestCases/coupled_cht/comp_2d/cht_2d_3cylinders.cfg
index 01bdcc333fa..a81a7cea3c8 100644
--- a/TestCases/coupled_cht/comp_2d/cht_2d_3cylinders.cfg
+++ b/TestCases/coupled_cht/comp_2d/cht_2d_3cylinders.cfg
@@ -5,7 +5,7 @@
 % Author: O. Burghardt                                                          %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 6, 2020                                                         %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 8.0.0 "Harrier"                                                  %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/coupled_cht/disc_adj_incomp_2d/cht_2d_3cylinders.cfg b/TestCases/coupled_cht/disc_adj_incomp_2d/cht_2d_3cylinders.cfg
index 38eb52af3e8..5c9455c03d4 100644
--- a/TestCases/coupled_cht/disc_adj_incomp_2d/cht_2d_3cylinders.cfg
+++ b/TestCases/coupled_cht/disc_adj_incomp_2d/cht_2d_3cylinders.cfg
@@ -5,7 +5,7 @@
 % Author: O. Burghardt, T. Economon                                             %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: August 8, 2019                                                          %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 8.0.0 "Harrier"                                                  %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/coupled_cht/incomp_2d/cht_2d_3cylinders.cfg b/TestCases/coupled_cht/incomp_2d/cht_2d_3cylinders.cfg
index 0db56062790..71f1d1f2ed0 100644
--- a/TestCases/coupled_cht/incomp_2d/cht_2d_3cylinders.cfg
+++ b/TestCases/coupled_cht/incomp_2d/cht_2d_3cylinders.cfg
@@ -5,7 +5,7 @@
 % Author: O. Burghardt, T. Economon                                             %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: August 8, 2019                                                          %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 8.0.0 "Harrier"                                                  %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/coupled_cht/incomp_2d_unsteady/cht_2d_3cylinders.cfg b/TestCases/coupled_cht/incomp_2d_unsteady/cht_2d_3cylinders.cfg
index bb06f67b7ee..f7192c82a64 100644
--- a/TestCases/coupled_cht/incomp_2d_unsteady/cht_2d_3cylinders.cfg
+++ b/TestCases/coupled_cht/incomp_2d_unsteady/cht_2d_3cylinders.cfg
@@ -5,7 +5,7 @@
 % Author: O. Burghardt, T. Economon                                             %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: August 8, 2019                                                          %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 8.0.0 "Harrier"                                                  %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/ddes/flatplate/ddes_flatplate.cfg b/TestCases/ddes/flatplate/ddes_flatplate.cfg
index 2e6c36b00a5..4fba06c6542 100644
--- a/TestCases/ddes/flatplate/ddes_flatplate.cfg
+++ b/TestCases/ddes/flatplate/ddes_flatplate.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.10                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/deformation/brick_hex/def_brick_hex.cfg b/TestCases/deformation/brick_hex/def_brick_hex.cfg
index 788b7289a06..6b7fd09138b 100755
--- a/TestCases/deformation/brick_hex/def_brick_hex.cfg
+++ b/TestCases/deformation/brick_hex/def_brick_hex.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2016.05.31                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/deformation/brick_hex_rans/def_brick_hex_rans.cfg b/TestCases/deformation/brick_hex_rans/def_brick_hex_rans.cfg
index b84e80b680d..ff84232a6d2 100755
--- a/TestCases/deformation/brick_hex_rans/def_brick_hex_rans.cfg
+++ b/TestCases/deformation/brick_hex_rans/def_brick_hex_rans.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2016.05.31                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/deformation/brick_prism/def_brick_prism.cfg b/TestCases/deformation/brick_prism/def_brick_prism.cfg
index 3f7d78b7d49..9399ba8f391 100755
--- a/TestCases/deformation/brick_prism/def_brick_prism.cfg
+++ b/TestCases/deformation/brick_prism/def_brick_prism.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2016.05.31                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/deformation/brick_prism_rans/def_brick_prism_rans.cfg b/TestCases/deformation/brick_prism_rans/def_brick_prism_rans.cfg
index bfd58255343..cf7a28e8dab 100755
--- a/TestCases/deformation/brick_prism_rans/def_brick_prism_rans.cfg
+++ b/TestCases/deformation/brick_prism_rans/def_brick_prism_rans.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2016.05.31                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/deformation/brick_pyra/def_brick_pyra.cfg b/TestCases/deformation/brick_pyra/def_brick_pyra.cfg
index 0deda077948..00061ed7a40 100755
--- a/TestCases/deformation/brick_pyra/def_brick_pyra.cfg
+++ b/TestCases/deformation/brick_pyra/def_brick_pyra.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2016.05.31                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/deformation/brick_tets/def_brick_tets.cfg b/TestCases/deformation/brick_tets/def_brick_tets.cfg
index 20a95629777..48c8017aa8f 100755
--- a/TestCases/deformation/brick_tets/def_brick_tets.cfg
+++ b/TestCases/deformation/brick_tets/def_brick_tets.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2016.05.31                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/deformation/cylindrical_ffd/def_cylindrical.cfg b/TestCases/deformation/cylindrical_ffd/def_cylindrical.cfg
index 8677ee14b99..129c7ca8761 100644
--- a/TestCases/deformation/cylindrical_ffd/def_cylindrical.cfg
+++ b/TestCases/deformation/cylindrical_ffd/def_cylindrical.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/deformation/intersection_prevention/def_intersect.cfg b/TestCases/deformation/intersection_prevention/def_intersect.cfg
index 8cc980b6792..6df45ec5ce7 100644
--- a/TestCases/deformation/intersection_prevention/def_intersect.cfg
+++ b/TestCases/deformation/intersection_prevention/def_intersect.cfg
@@ -15,7 +15,7 @@
 % Institution:                                                                 %
 %   Technische Universiteit Eindhoven                                          %
 % Date: 2021.01.08                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
diff --git a/TestCases/deformation/naca0012/def_NACA0012.cfg b/TestCases/deformation/naca0012/def_NACA0012.cfg
index a44a8f6aabf..e6675bba06b 100644
--- a/TestCases/deformation/naca0012/def_NACA0012.cfg
+++ b/TestCases/deformation/naca0012/def_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/deformation/naca0012/surface_file_NACA0012.cfg b/TestCases/deformation/naca0012/surface_file_NACA0012.cfg
index 09d7aefa518..b4b8b07f1db 100644
--- a/TestCases/deformation/naca0012/surface_file_NACA0012.cfg
+++ b/TestCases/deformation/naca0012/surface_file_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/deformation/naca4412/def_NACA4412.cfg b/TestCases/deformation/naca4412/def_NACA4412.cfg
index 6ad7b0cc33b..a1ceac5ca8b 100644
--- a/TestCases/deformation/naca4412/def_NACA4412.cfg
+++ b/TestCases/deformation/naca4412/def_NACA4412.cfg
@@ -6,7 +6,7 @@
 % Author: Thomas D. Economon	                                               %
 % Institution: Stanford University                                             %
 % Date: 2016.05.06                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/deformation/rae2822/def_RAE2822.cfg b/TestCases/deformation/rae2822/def_RAE2822.cfg
index a2bffdaac0d..85bb3f0997c 100644
--- a/TestCases/deformation/rae2822/def_RAE2822.cfg
+++ b/TestCases/deformation/rae2822/def_RAE2822.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/deformation/spherical_ffd/def_spherical.cfg b/TestCases/deformation/spherical_ffd/def_spherical.cfg
index aef3ede987d..e959c7026bf 100644
--- a/TestCases/deformation/spherical_ffd/def_spherical.cfg
+++ b/TestCases/deformation/spherical_ffd/def_spherical.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/deformation/spherical_ffd/def_spherical_bspline.cfg b/TestCases/deformation/spherical_ffd/def_spherical_bspline.cfg
index 2a1d1285d64..f1b1b02ca7f 100644
--- a/TestCases/deformation/spherical_ffd/def_spherical_bspline.cfg
+++ b/TestCases/deformation/spherical_ffd/def_spherical_bspline.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/disc_adj_euler/arina2k/Arina2KRS.cfg b/TestCases/disc_adj_euler/arina2k/Arina2KRS.cfg
index a6020dacefc..9a1aacfe9db 100644
--- a/TestCases/disc_adj_euler/arina2k/Arina2KRS.cfg
+++ b/TestCases/disc_adj_euler/arina2k/Arina2KRS.cfg
@@ -6,7 +6,7 @@
 % Author: Jairo Paes Cavalcante Filho [Based on T. Economon & M. Pini work]    %
 % Institution: University of São Paulo                                         %
 % Date: 8-JUL-2018                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/disc_adj_euler/cylinder3D/inv_cylinder3D.cfg b/TestCases/disc_adj_euler/cylinder3D/inv_cylinder3D.cfg
index bb26a568109..b1846a409dc 100644
--- a/TestCases/disc_adj_euler/cylinder3D/inv_cylinder3D.cfg
+++ b/TestCases/disc_adj_euler/cylinder3D/inv_cylinder3D.cfg
@@ -5,7 +5,7 @@
 % Author: ___________________________________________________________________  %
 % Institution: ______________________________________________________________  %
 % Date: __________                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/disc_adj_euler/oneram6/inv_ONERAM6.cfg b/TestCases/disc_adj_euler/oneram6/inv_ONERAM6.cfg
index 2d587524e59..fb67eb36588 100644
--- a/TestCases/disc_adj_euler/oneram6/inv_ONERAM6.cfg
+++ b/TestCases/disc_adj_euler/oneram6/inv_ONERAM6.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios, Heather Kline                                    %
 % Institution: Stanford University                                             %
 % Date: 01.17.2017                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/disc_adj_fea/configAD_fem.cfg b/TestCases/disc_adj_fea/configAD_fem.cfg
index 328e37ebb6b..0303c08aa0b 100644
--- a/TestCases/disc_adj_fea/configAD_fem.cfg
+++ b/TestCases/disc_adj_fea/configAD_fem.cfg
@@ -4,7 +4,7 @@
 % Author: R.Sanchez                                                            %
 % Institution: Imperial College London                                         %
 % Date: 2017.11.29                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 SOLVER= ELASTICITY
diff --git a/TestCases/disc_adj_fsi/configFEA.cfg b/TestCases/disc_adj_fsi/configFEA.cfg
index 12d8a8e5db1..5a81e020ea5 100644
--- a/TestCases/disc_adj_fsi/configFEA.cfg
+++ b/TestCases/disc_adj_fsi/configFEA.cfg
@@ -4,7 +4,7 @@
 % Author: R.Sanchez                                                            %
 % Institution: Imperial College London                                         %
 % Date: 2017.11.29                                                             %
-% File Version 7.5.1 "Blackbird"                                                  %
+% File Version 8.0.0 "Harrier"                                                    %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 SOLVER= ELASTICITY
diff --git a/TestCases/disc_adj_fsi/configFlow.cfg b/TestCases/disc_adj_fsi/configFlow.cfg
index d0269c61ab0..682e7d2a108 100644
--- a/TestCases/disc_adj_fsi/configFlow.cfg
+++ b/TestCases/disc_adj_fsi/configFlow.cfg
@@ -4,7 +4,7 @@
 % Author: R.Sanchez                                                            %
 % Institution: Imperial College London                                         %
 % Date: 2017.11.29                                                             %
-% File Version 7.5.1 "Blackbird"                                                   %
+% File Version 8.0.0 "Harrier"                                                     %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 SOLVER= NAVIER_STOKES
diff --git a/TestCases/disc_adj_heat/disc_adj_heat.cfg b/TestCases/disc_adj_heat/disc_adj_heat.cfg
index 2b3ad200e75..e4989879349 100644
--- a/TestCases/disc_adj_heat/disc_adj_heat.cfg
+++ b/TestCases/disc_adj_heat/disc_adj_heat.cfg
@@ -6,7 +6,7 @@
 % Author: Ole Burghardt                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: November 26th, 2018                                                     %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 8.0.0 "Harrier"                                                  %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/disc_adj_heat/primal.cfg b/TestCases/disc_adj_heat/primal.cfg
index 4fb1d63fbd4..6ada129211c 100644
--- a/TestCases/disc_adj_heat/primal.cfg
+++ b/TestCases/disc_adj_heat/primal.cfg
@@ -5,7 +5,7 @@
 % Author: Ole Burghardt                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: November 26th, 2018                                                     %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 8.0.0 "Harrier"                                                  %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/disc_adj_incomp_euler/naca0012/incomp_NACA0012_disc.cfg b/TestCases/disc_adj_incomp_euler/naca0012/incomp_NACA0012_disc.cfg
index f6d4b5efa5f..d92f2bc75db 100644
--- a/TestCases/disc_adj_incomp_euler/naca0012/incomp_NACA0012_disc.cfg
+++ b/TestCases/disc_adj_incomp_euler/naca0012/incomp_NACA0012_disc.cfg
@@ -4,7 +4,7 @@
 % Case description: Subsonic incompressible inviscid flow around a NACA0012    %
 % Author: Thomas D. Economon                                                   %
 % Date: 2018.10.30                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/disc_adj_incomp_navierstokes/cylinder/heated_cylinder.cfg b/TestCases/disc_adj_incomp_navierstokes/cylinder/heated_cylinder.cfg
index d61038a3126..dc328c88f05 100644
--- a/TestCases/disc_adj_incomp_navierstokes/cylinder/heated_cylinder.cfg
+++ b/TestCases/disc_adj_incomp_navierstokes/cylinder/heated_cylinder.cfg
@@ -4,7 +4,7 @@
 % Case description: Steady incompressible laminar flow past a heated cylinder  %
 % Author: Thomas D. Economon                                                   %
 % Date: 2018.06.10                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/disc_adj_incomp_rans/naca0012/turb_naca0012_sa.cfg b/TestCases/disc_adj_incomp_rans/naca0012/turb_naca0012_sa.cfg
index 82523aefc64..56cb3331551 100755
--- a/TestCases/disc_adj_incomp_rans/naca0012/turb_naca0012_sa.cfg
+++ b/TestCases/disc_adj_incomp_rans/naca0012/turb_naca0012_sa.cfg
@@ -5,7 +5,7 @@
 %                   http://turbmodels.larc.nasa.gov/naca0012_val_sa.html       %
 % Author: Thomas D. Economon & Francisco Palacios                              %
 % Date: 2018.06.10                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/disc_adj_incomp_rans/naca0012/turb_naca0012_sst.cfg b/TestCases/disc_adj_incomp_rans/naca0012/turb_naca0012_sst.cfg
index bde0ff08ebd..aea7942ecef 100755
--- a/TestCases/disc_adj_incomp_rans/naca0012/turb_naca0012_sst.cfg
+++ b/TestCases/disc_adj_incomp_rans/naca0012/turb_naca0012_sst.cfg
@@ -5,7 +5,7 @@
 %                   http://turbmodels.larc.nasa.gov/naca0012_val_sst.html      %
 % Author: Thomas D. Economon & Francisco Palacios                              %
 % Date: 2018.06.10                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/disc_adj_rans/cylinder/cylinder.cfg b/TestCases/disc_adj_rans/cylinder/cylinder.cfg
index 1d3980c9769..b2d4ca0848b 100644
--- a/TestCases/disc_adj_rans/cylinder/cylinder.cfg
+++ b/TestCases/disc_adj_rans/cylinder/cylinder.cfg
@@ -5,7 +5,7 @@
 % Author: Tim Albring                                                          %
 % Institution: TU Kaiserslautern                                               %
 % Date: 2016.06.14                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/disc_adj_rans/cylinder/cylinder_Windowing.cfg b/TestCases/disc_adj_rans/cylinder/cylinder_Windowing.cfg
index dcf0e520307..d89c9e75498 100644
--- a/TestCases/disc_adj_rans/cylinder/cylinder_Windowing.cfg
+++ b/TestCases/disc_adj_rans/cylinder/cylinder_Windowing.cfg
@@ -5,7 +5,7 @@
 % Author: Tim Albring                                                          %
 % Institution: TU Kaiserslautern                                               %
 % Date: 2016.06.14                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/disc_adj_rans/cylinder/cylinder_Windowing_AD.cfg b/TestCases/disc_adj_rans/cylinder/cylinder_Windowing_AD.cfg
index afb023abc94..7ae2770e6f2 100644
--- a/TestCases/disc_adj_rans/cylinder/cylinder_Windowing_AD.cfg
+++ b/TestCases/disc_adj_rans/cylinder/cylinder_Windowing_AD.cfg
@@ -5,7 +5,7 @@
 % Author: Tim Albring                                                          %
 % Institution: TU Kaiserslautern                                               %
 % Date: 2016.06.14                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/disc_adj_rans/cylinder_DT_1ST/cylinder.cfg b/TestCases/disc_adj_rans/cylinder_DT_1ST/cylinder.cfg
index 1d27a5a3022..b204d5b8f4b 100644
--- a/TestCases/disc_adj_rans/cylinder_DT_1ST/cylinder.cfg
+++ b/TestCases/disc_adj_rans/cylinder_DT_1ST/cylinder.cfg
@@ -5,7 +5,7 @@
 % Author: Tim Albring                                                          %
 % Institution: TU Kaiserslautern                                               %
 % Date: 2016.06.14                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/disc_adj_rans/naca0012/naca0012.cfg b/TestCases/disc_adj_rans/naca0012/naca0012.cfg
index 26318392aff..c83765fdd28 100644
--- a/TestCases/disc_adj_rans/naca0012/naca0012.cfg
+++ b/TestCases/disc_adj_rans/naca0012/naca0012.cfg
@@ -5,7 +5,7 @@
 % Author: Steffen Schotthöfer                                                  %
 % Institution: TU Kaiserslautern                                               %
 % Date: Mar 16, 2017                                                           %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sa.cfg b/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sa.cfg
index f8f151f9777..a1b710cb933 100644
--- a/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sa.cfg
+++ b/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sa.cfg
@@ -6,7 +6,7 @@
 % Author: Francisco Palacios	                                               %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sst.cfg b/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sst.cfg
index c9aff3eeea5..7134a4de925 100644
--- a/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sst.cfg
+++ b/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sst.cfg
@@ -6,7 +6,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg b/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg
index 1177b441780..0afb824397b 100644
--- a/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg
+++ b/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg
@@ -5,7 +5,7 @@
 % Author: S. Vitale                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: 2017.03.01                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/euler/CRM/inv_CRM_JST.cfg b/TestCases/euler/CRM/inv_CRM_JST.cfg
index 4e5e9839caa..5472813ad1e 100644
--- a/TestCases/euler/CRM/inv_CRM_JST.cfg
+++ b/TestCases/euler/CRM/inv_CRM_JST.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon	      	      	              	       	       %
 % Institution: Stanford University				                               %
 % Date: 2012.10.07                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/euler/biparabolic/BIPARABOLIC.cfg b/TestCases/euler/biparabolic/BIPARABOLIC.cfg
index 94a1aee34ca..7506bdb98b1 100644
--- a/TestCases/euler/biparabolic/BIPARABOLIC.cfg
+++ b/TestCases/euler/biparabolic/BIPARABOLIC.cfg
@@ -5,7 +5,7 @@
 % Author: Trent W. Lukaczyk                                                    %
 % Institution: Stanford University                                             %
 % Date: 2012.08.16                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/euler/bluntbody/blunt.cfg b/TestCases/euler/bluntbody/blunt.cfg
index dbb4926dc28..c16188707a0 100644
--- a/TestCases/euler/bluntbody/blunt.cfg
+++ b/TestCases/euler/bluntbody/blunt.cfg
@@ -5,7 +5,7 @@
 % Author: Amit Sachdeva                                                        %
 % Institution: ADSG-VSSC                                                       %
 % Date: 2019.01.23                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/euler/channel/inv_channel.cfg b/TestCases/euler/channel/inv_channel.cfg
index 9acd1819ac4..ae7ab80cbc1 100644
--- a/TestCases/euler/channel/inv_channel.cfg
+++ b/TestCases/euler/channel/inv_channel.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2012.09.29                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/euler/channel/inv_channel_RK.cfg b/TestCases/euler/channel/inv_channel_RK.cfg
index edcf30b313c..2a7c72c77f7 100644
--- a/TestCases/euler/channel/inv_channel_RK.cfg
+++ b/TestCases/euler/channel/inv_channel_RK.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2012.10.07                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/euler/naca0012/inv_NACA0012.cfg b/TestCases/euler/naca0012/inv_NACA0012.cfg
index 98af59604f8..a57ff4e4e4d 100644
--- a/TestCases/euler/naca0012/inv_NACA0012.cfg
+++ b/TestCases/euler/naca0012/inv_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/euler/naca0012/inv_NACA0012_Roe.cfg b/TestCases/euler/naca0012/inv_NACA0012_Roe.cfg
index cb5098afa2c..4df2ca7e453 100644
--- a/TestCases/euler/naca0012/inv_NACA0012_Roe.cfg
+++ b/TestCases/euler/naca0012/inv_NACA0012_Roe.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2012.10.07                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/euler/oneram6/inv_ONERAM6.cfg b/TestCases/euler/oneram6/inv_ONERAM6.cfg
index 043a66e1910..f8a5ed2228c 100644
--- a/TestCases/euler/oneram6/inv_ONERAM6.cfg
+++ b/TestCases/euler/oneram6/inv_ONERAM6.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon	      	      	              	       	       %
 % Institution: Stanford University                                             %
 % Date: 2015.08.25                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/euler/ramp/inv_ramp.cfg b/TestCases/euler/ramp/inv_ramp.cfg
index 1ea26b65e2f..2f27ee85973 100644
--- a/TestCases/euler/ramp/inv_ramp.cfg
+++ b/TestCases/euler/ramp/inv_ramp.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon, Amit Sachdeva                                    %
 % Institution: Stanford University                                             %
 % Date: 2023.04.08                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/euler/wedge/inv_wedge_HLLC.cfg b/TestCases/euler/wedge/inv_wedge_HLLC.cfg
index 453ae608577..ebbafb0f624 100644
--- a/TestCases/euler/wedge/inv_wedge_HLLC.cfg
+++ b/TestCases/euler/wedge/inv_wedge_HLLC.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2012.10.07                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/fea_fsi/Airfoil_RBF/config.cfg b/TestCases/fea_fsi/Airfoil_RBF/config.cfg
index eebdfa3d60d..9039bd4519e 100755
--- a/TestCases/fea_fsi/Airfoil_RBF/config.cfg
+++ b/TestCases/fea_fsi/Airfoil_RBF/config.cfg
@@ -3,7 +3,7 @@
 % Case description: 2D airfoil FSI with radial basis function interp.          %
 % Institution: Imperial College London                                         %
 % Date: 2015.08.12                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 SOLVER = MULTIPHYSICS
diff --git a/TestCases/fea_fsi/Airfoil_RBF/configFEA.cfg b/TestCases/fea_fsi/Airfoil_RBF/configFEA.cfg
index 51966af7064..ba53a5cc31a 100644
--- a/TestCases/fea_fsi/Airfoil_RBF/configFEA.cfg
+++ b/TestCases/fea_fsi/Airfoil_RBF/configFEA.cfg
@@ -2,7 +2,7 @@
 % SU2 configuration file                                                 %
 % Case description: 2D airfoil FSI with radial basis function interp.    %
 % Institution: Imperial College London                                   %
-% File Version 7.5.1 "Blackbird"                                         %
+% File Version 8.0.0 "Harrier"                                           %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
 % Interface options ---------------------------------------------------- %
diff --git a/TestCases/fea_fsi/Airfoil_RBF/configFlow.cfg b/TestCases/fea_fsi/Airfoil_RBF/configFlow.cfg
index 9ff342e7b3a..9e2032c5a08 100644
--- a/TestCases/fea_fsi/Airfoil_RBF/configFlow.cfg
+++ b/TestCases/fea_fsi/Airfoil_RBF/configFlow.cfg
@@ -2,7 +2,7 @@
 % SU2 configuration file                                                 %
 % Case description: 2D airfoil FSI with radial basis function interp.    %
 % Institution: Imperial College London                                   %
-% File Version 7.5.1 "Blackbird"                                         %
+% File Version 8.0.0 "Harrier"                                           %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
 % Interface options ---------------------------------------------------- %
diff --git a/TestCases/fea_fsi/DynBeam_2d/configBeam_2d.cfg b/TestCases/fea_fsi/DynBeam_2d/configBeam_2d.cfg
index 1303f5457be..3b9e5f955dd 100644
--- a/TestCases/fea_fsi/DynBeam_2d/configBeam_2d.cfg
+++ b/TestCases/fea_fsi/DynBeam_2d/configBeam_2d.cfg
@@ -4,7 +4,7 @@
 % Author: Ruben Sanchez Fernandez                                              %
 % Institution: Imperial College London                                         %
 % Date: 2016.02.01                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 SOLVER= ELASTICITY
diff --git a/TestCases/fea_fsi/MixElemsKnowles/config.cfg b/TestCases/fea_fsi/MixElemsKnowles/config.cfg
index ffa4573286a..53f943ca738 100644
--- a/TestCases/fea_fsi/MixElemsKnowles/config.cfg
+++ b/TestCases/fea_fsi/MixElemsKnowles/config.cfg
@@ -4,7 +4,7 @@
 % Case description: Tip-loaded 3D cantilever beam, mix of element types,       %
 %                   nonlinear elasticity with Knowles material model.          %
 % Institution: Imperial College London                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/fea_fsi/SquareCyl_Beam/config.cfg b/TestCases/fea_fsi/SquareCyl_Beam/config.cfg
index d4033e5f4b1..361e6a4e5ed 100644
--- a/TestCases/fea_fsi/SquareCyl_Beam/config.cfg
+++ b/TestCases/fea_fsi/SquareCyl_Beam/config.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez Fernandez                                              %
 % Institution: Imperial College London                                         %
 % Date: 2016.06.01                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/fea_fsi/StatBeam_3d/configBeam_3d.cfg b/TestCases/fea_fsi/StatBeam_3d/configBeam_3d.cfg
index e3b82a9e601..c2cc8594e51 100644
--- a/TestCases/fea_fsi/StatBeam_3d/configBeam_3d.cfg
+++ b/TestCases/fea_fsi/StatBeam_3d/configBeam_3d.cfg
@@ -4,7 +4,7 @@
 % Author: Ruben Sanchez Fernandez                                              %
 % Institution: Imperial College London                                         %
 % Date: 2016.02.01                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 SOLVER= ELASTICITY
diff --git a/TestCases/fea_topology/config.cfg b/TestCases/fea_topology/config.cfg
index 021e878895d..a1d6fe63e98 100644
--- a/TestCases/fea_topology/config.cfg
+++ b/TestCases/fea_topology/config.cfg
@@ -2,7 +2,7 @@
 % SU2 configuration file                                                 %
 % Case description: 4 by 1 cantilever optim. for stiff. @ 50% material   %
 % Institution: Imperial College London                                   %
-% File Version 7.5.1 "Blackbird"                                         %
+% File Version 8.0.0 "Harrier"                                           %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
 % Optimization
diff --git a/TestCases/fixed_cl/naca0012/inv_NACA0012.cfg b/TestCases/fixed_cl/naca0012/inv_NACA0012.cfg
index e83ac88b86f..8b42d149a35 100644
--- a/TestCases/fixed_cl/naca0012/inv_NACA0012.cfg
+++ b/TestCases/fixed_cl/naca0012/inv_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg b/TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg
index ba4bb1f9f9a..eecbe2141e1 100644
--- a/TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg
+++ b/TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg b/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg
index 9193f0820ee..d218369f9f7 100644
--- a/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg
+++ b/TestCases/flamelet/01_laminar_premixed_ch4_flame_cfd/lam_prem_ch4_cfd.cfg
@@ -4,7 +4,7 @@
 % Author: Nijso Beishuizen                                                     %
 % Institution: Bosch Thermotechnology                                          %
 % Date: 08/09/2021                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg
index 452bc271b5a..0d9ad8f0331 100644
--- a/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg
+++ b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_ad.cfg
@@ -11,7 +11,7 @@
 % Institution b: Bosch Thermotechnology                                        %
 %                                                                              %
 % Date: 02/21/2023                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg
index acd766cbe84..e24fba9b935 100644
--- a/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg
+++ b/TestCases/flamelet/02_laminar_premixed_ch4_flame_hx_ad/lam_prem_ch4_hx_dot.cfg
@@ -11,7 +11,7 @@
 % Institution b: Bosch Thermotechnology                                        %
 %                                                                              %
 % Date: 02/21/2023                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg b/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg
index 391b49a5d07..d2750fcae1d 100644
--- a/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg
+++ b/TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg
@@ -5,7 +5,7 @@
 % Author: Nijso Beishuizen                                                     %
 % Institution: Bosch Thermotechnology                                          %
 % Date: 08/09/2021                                                             %
-% File Version 7.5.1 "Blackbird",                                              %
+% File Version 8.0.0 "Harrier",                                              %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_prem_ch4_cfd.cfg b/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_prem_ch4_cfd.cfg
index 9092a1ff39d..1ac7c1ebf67 100644
--- a/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_prem_ch4_cfd.cfg
+++ b/TestCases/flamelet/06_laminar_partial_premixed_ch4_flame_cfd/lam_partial_prem_ch4_cfd.cfg
@@ -4,7 +4,7 @@
 % Author: Nijso Beishuizen                                                     %
 % Institution: Bosch Thermotechnology                                          %
 % Date: 16/06/2023                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/grad_smooth/naca0012/inv_NACA0012_gradsmooth.cfg b/TestCases/grad_smooth/naca0012/inv_NACA0012_gradsmooth.cfg
index 902aeab7030..ce3989662c2 100644
--- a/TestCases/grad_smooth/naca0012/inv_NACA0012_gradsmooth.cfg
+++ b/TestCases/grad_smooth/naca0012/inv_NACA0012_gradsmooth.cfg
@@ -4,7 +4,7 @@
 % Case description: Sobolev smoothing for gradient on the NACA 0012 airfoil    %
 % Author: Thomas Dick (TU Kaiserslautern)                                      %
 % Date: 11.11.2021                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/grad_smooth/oneram6/ONERAM6_gradsmooth.cfg b/TestCases/grad_smooth/oneram6/ONERAM6_gradsmooth.cfg
index 0b720e65c58..354c0681020 100644
--- a/TestCases/grad_smooth/oneram6/ONERAM6_gradsmooth.cfg
+++ b/TestCases/grad_smooth/oneram6/ONERAM6_gradsmooth.cfg
@@ -4,7 +4,7 @@
 % Case description: Sobolev smoothing for gradient on the ONERA M6 wing        %
 % Author: Thomas Dick (TU Kaiserslautern)                                      %
 % Date: 11.11.2021                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/gust/cosine_gust_zdir.cfg b/TestCases/gust/cosine_gust_zdir.cfg
index 515a8d44c49..402bd5ca232 100644
--- a/TestCases/gust/cosine_gust_zdir.cfg
+++ b/TestCases/gust/cosine_gust_zdir.cfg
@@ -5,7 +5,7 @@
 % Author: Arne Voß                                                             %
 % Institution: DLR                                                             %
 % Date: 25.05.2023                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/gust/gust_with_mesh_deformation.cfg b/TestCases/gust/gust_with_mesh_deformation.cfg
index 6f208952ac9..b9b956d7721 100644
--- a/TestCases/gust/gust_with_mesh_deformation.cfg
+++ b/TestCases/gust/gust_with_mesh_deformation.cfg
@@ -5,7 +5,7 @@
 % Author: Arne Voß                                                             %
 % Institution: DLR                                                             %
 % Date: 25.05.2023                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/gust/inv_gust_NACA0012.cfg b/TestCases/gust/inv_gust_NACA0012.cfg
index b34aca695d2..f91ffedf7ab 100644
--- a/TestCases/gust/inv_gust_NACA0012.cfg
+++ b/TestCases/gust/inv_gust_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Santiago Padron                                                      %
 % Institution: Stanford University                                             %
 % Date: 06-26-2015                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/harmonic_balance/HB.cfg b/TestCases/harmonic_balance/HB.cfg
index b6d1ce04a81..57b4bd0b9a1 100644
--- a/TestCases/harmonic_balance/HB.cfg
+++ b/TestCases/harmonic_balance/HB.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2016.20.09                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/harmonic_balance/hb_rans_preconditioning/davis.cfg b/TestCases/harmonic_balance/hb_rans_preconditioning/davis.cfg
index af3a7142991..bd52f939081 100644
--- a/TestCases/harmonic_balance/hb_rans_preconditioning/davis.cfg
+++ b/TestCases/harmonic_balance/hb_rans_preconditioning/davis.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2016.20.09                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/hom_euler/NACA0012_3D_Hybrid_4thOrder/fem_NACA0012.cfg b/TestCases/hom_euler/NACA0012_3D_Hybrid_4thOrder/fem_NACA0012.cfg
index c3f156a8aa3..16c0e1dc2c2 100644
--- a/TestCases/hom_euler/NACA0012_3D_Hybrid_4thOrder/fem_NACA0012.cfg
+++ b/TestCases/hom_euler/NACA0012_3D_Hybrid_4thOrder/fem_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/hom_euler/NACA0012_5thOrder/fem_NACA0012.cfg b/TestCases/hom_euler/NACA0012_5thOrder/fem_NACA0012.cfg
index 2ad8def0d80..a52f55b7bdb 100644
--- a/TestCases/hom_euler/NACA0012_5thOrder/fem_NACA0012.cfg
+++ b/TestCases/hom_euler/NACA0012_5thOrder/fem_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/hom_euler/NACA0012_5thOrder/fem_NACA0012_reg.cfg b/TestCases/hom_euler/NACA0012_5thOrder/fem_NACA0012_reg.cfg
index 6cdbad80c93..4308de0c36a 100644
--- a/TestCases/hom_euler/NACA0012_5thOrder/fem_NACA0012_reg.cfg
+++ b/TestCases/hom_euler/NACA0012_5thOrder/fem_NACA0012_reg.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/hom_euler/Sphere_4thOrder_Hexa/fem_Sphere.cfg b/TestCases/hom_euler/Sphere_4thOrder_Hexa/fem_Sphere.cfg
index 367294e3daf..9967a7f393b 100644
--- a/TestCases/hom_euler/Sphere_4thOrder_Hexa/fem_Sphere.cfg
+++ b/TestCases/hom_euler/Sphere_4thOrder_Hexa/fem_Sphere.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/hom_euler/Sphere_4thOrder_Tet/fem_Sphere.cfg b/TestCases/hom_euler/Sphere_4thOrder_Tet/fem_Sphere.cfg
index 75bbfae2904..00ec7aa99ea 100644
--- a/TestCases/hom_euler/Sphere_4thOrder_Tet/fem_Sphere.cfg
+++ b/TestCases/hom_euler/Sphere_4thOrder_Tet/fem_Sphere.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/hom_euler/SubsonicChannel/nPoly1/fem_SubsonicChannel.cfg b/TestCases/hom_euler/SubsonicChannel/nPoly1/fem_SubsonicChannel.cfg
index 64fb4339e6f..29dadb14954 100644
--- a/TestCases/hom_euler/SubsonicChannel/nPoly1/fem_SubsonicChannel.cfg
+++ b/TestCases/hom_euler/SubsonicChannel/nPoly1/fem_SubsonicChannel.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/hom_euler/SubsonicChannel/nPoly1/fem_SubsonicChannel_Farfield.cfg b/TestCases/hom_euler/SubsonicChannel/nPoly1/fem_SubsonicChannel_Farfield.cfg
index cfbfa411984..8748d28aa55 100644
--- a/TestCases/hom_euler/SubsonicChannel/nPoly1/fem_SubsonicChannel_Farfield.cfg
+++ b/TestCases/hom_euler/SubsonicChannel/nPoly1/fem_SubsonicChannel_Farfield.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/hom_euler/SubsonicChannel/nPoly2/fem_SubsonicChannel.cfg b/TestCases/hom_euler/SubsonicChannel/nPoly2/fem_SubsonicChannel.cfg
index 6671d3b91c2..b7401a2720f 100644
--- a/TestCases/hom_euler/SubsonicChannel/nPoly2/fem_SubsonicChannel.cfg
+++ b/TestCases/hom_euler/SubsonicChannel/nPoly2/fem_SubsonicChannel.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/hom_euler/SubsonicChannel/nPoly2/fem_SubsonicChannel_Farfield.cfg b/TestCases/hom_euler/SubsonicChannel/nPoly2/fem_SubsonicChannel_Farfield.cfg
index 3eb44dab96a..2c53edb7869 100644
--- a/TestCases/hom_euler/SubsonicChannel/nPoly2/fem_SubsonicChannel_Farfield.cfg
+++ b/TestCases/hom_euler/SubsonicChannel/nPoly2/fem_SubsonicChannel_Farfield.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/hom_euler/SubsonicChannel/nPoly4/fem_SubsonicChannel.cfg b/TestCases/hom_euler/SubsonicChannel/nPoly4/fem_SubsonicChannel.cfg
index 0107f92a250..a5dcaac6a8e 100644
--- a/TestCases/hom_euler/SubsonicChannel/nPoly4/fem_SubsonicChannel.cfg
+++ b/TestCases/hom_euler/SubsonicChannel/nPoly4/fem_SubsonicChannel.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/hom_euler/SubsonicChannel/nPoly4/fem_SubsonicChannel_Farfield.cfg b/TestCases/hom_euler/SubsonicChannel/nPoly4/fem_SubsonicChannel_Farfield.cfg
index 4a129d7a239..9d19fc688b6 100644
--- a/TestCases/hom_euler/SubsonicChannel/nPoly4/fem_SubsonicChannel_Farfield.cfg
+++ b/TestCases/hom_euler/SubsonicChannel/nPoly4/fem_SubsonicChannel_Farfield.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/hom_navierstokes/CylinderViscous/nPoly3/fem_Cylinder_reg.cfg b/TestCases/hom_navierstokes/CylinderViscous/nPoly3/fem_Cylinder_reg.cfg
index c8495d99c34..2c430c8989c 100644
--- a/TestCases/hom_navierstokes/CylinderViscous/nPoly3/fem_Cylinder_reg.cfg
+++ b/TestCases/hom_navierstokes/CylinderViscous/nPoly3/fem_Cylinder_reg.cfg
@@ -5,7 +5,7 @@
 % Author: Edwin van der Weide                                                  %
 % Institution: University of Twente                                            %
 % Date: 2016.07.15                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/hom_navierstokes/FlatPlate/nPoly4/lam_flatplate_reg.cfg b/TestCases/hom_navierstokes/FlatPlate/nPoly4/lam_flatplate_reg.cfg
index 39f8ddc2f72..99260564e78 100644
--- a/TestCases/hom_navierstokes/FlatPlate/nPoly4/lam_flatplate_reg.cfg
+++ b/TestCases/hom_navierstokes/FlatPlate/nPoly4/lam_flatplate_reg.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon	                                               %
 % Institution: Stanford University                                             %
 % Date: 2013.09.30                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/hom_navierstokes/SphereViscous/nPoly3_QuadDominant/fem_Sphere_reg.cfg b/TestCases/hom_navierstokes/SphereViscous/nPoly3_QuadDominant/fem_Sphere_reg.cfg
index d8daab40b6d..01c13c309dd 100644
--- a/TestCases/hom_navierstokes/SphereViscous/nPoly3_QuadDominant/fem_Sphere_reg.cfg
+++ b/TestCases/hom_navierstokes/SphereViscous/nPoly3_QuadDominant/fem_Sphere_reg.cfg
@@ -5,7 +5,7 @@
 % Author: Edwin van der Weide                                                  %
 % Institution: University of Twente                                            %
 % Date: 2016.07.15                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/hom_navierstokes/SphereViscous/nPoly3_QuadDominant/fem_Sphere_reg_ADER.cfg b/TestCases/hom_navierstokes/SphereViscous/nPoly3_QuadDominant/fem_Sphere_reg_ADER.cfg
index 8f88fd7ff3a..724ed5bedc1 100644
--- a/TestCases/hom_navierstokes/SphereViscous/nPoly3_QuadDominant/fem_Sphere_reg_ADER.cfg
+++ b/TestCases/hom_navierstokes/SphereViscous/nPoly3_QuadDominant/fem_Sphere_reg_ADER.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/hom_navierstokes/UnsteadyCylinder/nPoly4/fem_unst_cylinder.cfg b/TestCases/hom_navierstokes/UnsteadyCylinder/nPoly4/fem_unst_cylinder.cfg
index a121fcb53cb..5f0fb601fca 100644
--- a/TestCases/hom_navierstokes/UnsteadyCylinder/nPoly4/fem_unst_cylinder.cfg
+++ b/TestCases/hom_navierstokes/UnsteadyCylinder/nPoly4/fem_unst_cylinder.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/hom_navierstokes/UnsteadyCylinder/nPoly4/fem_unst_cylinder_ADER.cfg b/TestCases/hom_navierstokes/UnsteadyCylinder/nPoly4/fem_unst_cylinder_ADER.cfg
index 6724df7250c..9bec3e9366c 100644
--- a/TestCases/hom_navierstokes/UnsteadyCylinder/nPoly4/fem_unst_cylinder_ADER.cfg
+++ b/TestCases/hom_navierstokes/UnsteadyCylinder/nPoly4/fem_unst_cylinder_ADER.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index af97193431f..801ca167f31 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -3,7 +3,7 @@
 ## \file hybrid_regression.py
 #  \brief Python script for automated regression testing of SU2 examples
 #  \author A. Aranake, A. Campos, T. Economon, T. Lukaczyk, S. Padron
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/hybrid_regression_AD.py b/TestCases/hybrid_regression_AD.py
index 6da703800f7..a2243e14e24 100644
--- a/TestCases/hybrid_regression_AD.py
+++ b/TestCases/hybrid_regression_AD.py
@@ -3,7 +3,7 @@
 ## \file hybrid_regression_AD.py
 #  \brief Python script for automated regression testing of SU2 examples
 #  \author A. Aranake, A. Campos, T. Economon, T. Lukaczyk, S. Padron
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/incomp_euler/naca0012/incomp_NACA0012.cfg b/TestCases/incomp_euler/naca0012/incomp_NACA0012.cfg
index 398e621ca92..216a1881a31 100644
--- a/TestCases/incomp_euler/naca0012/incomp_NACA0012.cfg
+++ b/TestCases/incomp_euler/naca0012/incomp_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 09/18/2011                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/incomp_euler/nozzle/inv_nozzle.cfg b/TestCases/incomp_euler/nozzle/inv_nozzle.cfg
index b29e9bfdc51..314311408e6 100644
--- a/TestCases/incomp_euler/nozzle/inv_nozzle.cfg
+++ b/TestCases/incomp_euler/nozzle/inv_nozzle.cfg
@@ -4,7 +4,7 @@
 % Case description: Inv. inc. nozzle with pressure inlet and mass flow outlet  %
 % Author: Thomas D. Economon                                                   %
 % Date: 2018.11.30                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/incomp_navierstokes/buoyancy_cavity/lam_buoyancy_cavity.cfg b/TestCases/incomp_navierstokes/buoyancy_cavity/lam_buoyancy_cavity.cfg
index 578b8127f81..96bcd92712b 100644
--- a/TestCases/incomp_navierstokes/buoyancy_cavity/lam_buoyancy_cavity.cfg
+++ b/TestCases/incomp_navierstokes/buoyancy_cavity/lam_buoyancy_cavity.cfg
@@ -4,7 +4,7 @@
 % Case description: Buoyancy-driven flow inside a cavity                       %
 % Author: Thomas D. Economon                                                   %
 % Date: 2018.06.10                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/incomp_navierstokes/cylinder/incomp_cylinder.cfg b/TestCases/incomp_navierstokes/cylinder/incomp_cylinder.cfg
index f292836c8e7..416c10715c5 100644
--- a/TestCases/incomp_navierstokes/cylinder/incomp_cylinder.cfg
+++ b/TestCases/incomp_navierstokes/cylinder/incomp_cylinder.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios						                           %
 % Institution: Stanford University                                             %
 % Date: 2012.03.14                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/incomp_navierstokes/cylinder/poly_cylinder.cfg b/TestCases/incomp_navierstokes/cylinder/poly_cylinder.cfg
index 24bfb194c01..7e12b59731f 100644
--- a/TestCases/incomp_navierstokes/cylinder/poly_cylinder.cfg
+++ b/TestCases/incomp_navierstokes/cylinder/poly_cylinder.cfg
@@ -5,7 +5,7 @@
 %                   custom fluid using polynomial fluid models.                %
 % Author: Thomas D. Economon                                                   %
 % Date: 2018.12.02                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/BC_HeatTransfer.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/BC_HeatTransfer.cfg
index 5005fbaccef..accd40e479a 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/BC_HeatTransfer.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/BC_HeatTransfer.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Robert Bosch GmbH                                               %
 % Date: 2020.12.15                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/DA_configMaster.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/DA_configMaster.cfg
index fb41015dfb7..959a904fd69 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/DA_configMaster.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/DA_configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                           %
 % Institution: Robert Bosch GmbH                                                %
 % Date: 2020.12.15                                                              %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 8.0.0 "Harrier"                                                  %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/FD_configMaster.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/FD_configMaster.cfg
index 42aea7ba914..6fecd5e600a 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/FD_configMaster.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/FD_configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                           %
 % Institution: Robert Bosch GmbH                                                %
 % Date: 2020.12.15                                                              %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 8.0.0 "Harrier"                                                  %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configFluid.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configFluid.cfg
index d2cc26c56f6..23a368fe73d 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configFluid.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configFluid.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Robert Bosch GmbH                                               %
 % Date: 2020.12.15                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configMaster.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configMaster.cfg
index 8e66cb0ab71..04f77424365 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configMaster.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                           %
 % Institution: Robert Bosch GmbH                                                %
 % Date: 2020.12.15                                                              %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 8.0.0 "Harrier"                                                  %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configSolid.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configSolid.cfg
index 8c4a3a1ded4..07f3733229d 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configSolid.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configSolid.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Robert Bosch GmbH                                               %
 % Date: 2020.12.15                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configFluid.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configFluid.cfg
index b8d003a4eca..e6b53711cf2 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configFluid.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configFluid.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Robert Bosch GmbH                                               %
 % Date: 07.06.2019                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configMaster.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configMaster.cfg
index 6fcbc300a41..e4b01538e7e 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configMaster.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                           %
 % Institution: Robert Bosch GmbH                                                %
 % Date: 2020.12.15                                                              %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 8.0.0 "Harrier"                                                  %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configSolid.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configSolid.cfg
index 6c78fb026ed..8db23aa8353 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configSolid.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_3d/configSolid.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Robert Bosch GmbH                                               %
 % Date: 07.06.2019                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configFluid.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configFluid.cfg
index c640520534e..41c4c40e07f 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configFluid.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configFluid.cfg
@@ -4,7 +4,7 @@
 % Case description: Unit Cell flow around pin array (fluid)                    %
 % Author: T. Kattmann                                                          %
 % Date: 2022.02.10                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configMaster.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configMaster.cfg
index 71fb7a2d777..84d81a2b70b 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configMaster.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                           %
 % Institution: None                                                             %
 % Date: 2022.02.10                                                              %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 8.0.0 "Harrier"                                                  %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configSolid.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configSolid.cfg
index 3802e0318e9..20d3b009eb5 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configSolid.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/dp-adjoint_chtPinArray_2d/configSolid.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: None                                                            %
 % Date: 2022.02.10                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/pipeSlice_3d/sp_pipeSlice_3d_dp_hf_tp.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/pipeSlice_3d/sp_pipeSlice_3d_dp_hf_tp.cfg
index b0b2366cf45..5b80170d3f7 100644
--- a/TestCases/incomp_navierstokes/streamwise_periodic/pipeSlice_3d/sp_pipeSlice_3d_dp_hf_tp.cfg
+++ b/TestCases/incomp_navierstokes/streamwise_periodic/pipeSlice_3d/sp_pipeSlice_3d_dp_hf_tp.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Robert Bosch GmbH                                               %
 % Date: 2020.12.14                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/incomp_rans/naca0012/naca0012.cfg b/TestCases/incomp_rans/naca0012/naca0012.cfg
index 7798637c2c4..49bb44fde10 100644
--- a/TestCases/incomp_rans/naca0012/naca0012.cfg
+++ b/TestCases/incomp_rans/naca0012/naca0012.cfg
@@ -6,7 +6,7 @@
 % Author: Francisco Palacios	                                               %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/incomp_rans/naca0012/naca0012_SST_SUST.cfg b/TestCases/incomp_rans/naca0012/naca0012_SST_SUST.cfg
index d5f52a64047..c351edbd375 100644
--- a/TestCases/incomp_rans/naca0012/naca0012_SST_SUST.cfg
+++ b/TestCases/incomp_rans/naca0012/naca0012_SST_SUST.cfg
@@ -6,7 +6,7 @@
 % Author: Francisco Palacios	                                               %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/incomp_rans/rough_flatplate/rough_flatplate_incomp.cfg b/TestCases/incomp_rans/rough_flatplate/rough_flatplate_incomp.cfg
index af9ecc8f023..46d029f7e6d 100644
--- a/TestCases/incomp_rans/rough_flatplate/rough_flatplate_incomp.cfg
+++ b/TestCases/incomp_rans/rough_flatplate/rough_flatplate_incomp.cfg
@@ -5,7 +5,7 @@
 %                   pressure gradient                                          %
 % Author: Akshay Koodly                                                        %
 % Date: 2020.07.07                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/mms/dg_ringleb/ringleb_dg.cfg b/TestCases/mms/dg_ringleb/ringleb_dg.cfg
index 4d9d5108678..f25a4f2d4b3 100644
--- a/TestCases/mms/dg_ringleb/ringleb_dg.cfg
+++ b/TestCases/mms/dg_ringleb/ringleb_dg.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/mms/fvm_incomp_euler/inv_mms_jst.cfg b/TestCases/mms/fvm_incomp_euler/inv_mms_jst.cfg
index 47f57c8a91a..0ca4f269eae 100755
--- a/TestCases/mms/fvm_incomp_euler/inv_mms_jst.cfg
+++ b/TestCases/mms/fvm_incomp_euler/inv_mms_jst.cfg
@@ -4,7 +4,7 @@
 % Case description: Incompressible inviscid MMS test case                      %
 % Author: Thomas D. Economon                                                   %
 % Date: 2019.04.09                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/mms/fvm_incomp_navierstokes/lam_mms_fds.cfg b/TestCases/mms/fvm_incomp_navierstokes/lam_mms_fds.cfg
index 4bac9270cdc..1e77e3c1574 100755
--- a/TestCases/mms/fvm_incomp_navierstokes/lam_mms_fds.cfg
+++ b/TestCases/mms/fvm_incomp_navierstokes/lam_mms_fds.cfg
@@ -4,7 +4,7 @@
 % Case description: Incompressible laminar MMS test case                       %
 % Author: Thomas D. Economon                                                   %
 % Date: 2019.04.09                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/mms/fvm_navierstokes/lam_mms_roe.cfg b/TestCases/mms/fvm_navierstokes/lam_mms_roe.cfg
index 0dfab26bf2f..139e6a4a84e 100755
--- a/TestCases/mms/fvm_navierstokes/lam_mms_roe.cfg
+++ b/TestCases/mms/fvm_navierstokes/lam_mms_roe.cfg
@@ -4,7 +4,7 @@
 % Case description: Compressible laminar MMS test case                         %
 % Author: Thomas D. Economon                                                   %
 % Date: 2019.04.09                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/moving_wall/cavity/lam_cavity.cfg b/TestCases/moving_wall/cavity/lam_cavity.cfg
index 31a541946d6..2fd187e65da 100644
--- a/TestCases/moving_wall/cavity/lam_cavity.cfg
+++ b/TestCases/moving_wall/cavity/lam_cavity.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.10.01                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/moving_wall/spinning_cylinder/spinning_cylinder.cfg b/TestCases/moving_wall/spinning_cylinder/spinning_cylinder.cfg
index 194a46064dd..b28ce99bdc9 100644
--- a/TestCases/moving_wall/spinning_cylinder/spinning_cylinder.cfg
+++ b/TestCases/moving_wall/spinning_cylinder/spinning_cylinder.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.08.21                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/multiple_ffd/naca0012/inv_NACA0012_ffd.cfg b/TestCases/multiple_ffd/naca0012/inv_NACA0012_ffd.cfg
index 8ddf2fd572f..848ecf88acb 100644
--- a/TestCases/multiple_ffd/naca0012/inv_NACA0012_ffd.cfg
+++ b/TestCases/multiple_ffd/naca0012/inv_NACA0012_ffd.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios, Charanya Venkatesan-Crome                        %
 % Institution: Stanford University                                             %
 % Date: 2018.07.23                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/navierstokes/cylinder/cylinder_lowmach.cfg b/TestCases/navierstokes/cylinder/cylinder_lowmach.cfg
index 942f29e8248..ce01b555f79 100644
--- a/TestCases/navierstokes/cylinder/cylinder_lowmach.cfg
+++ b/TestCases/navierstokes/cylinder/cylinder_lowmach.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.09.30                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/navierstokes/cylinder/lam_cylinder.cfg b/TestCases/navierstokes/cylinder/lam_cylinder.cfg
index e69570d421e..1079748199e 100644
--- a/TestCases/navierstokes/cylinder/lam_cylinder.cfg
+++ b/TestCases/navierstokes/cylinder/lam_cylinder.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.09.30                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/navierstokes/flatplate/lam_flatplate.cfg b/TestCases/navierstokes/flatplate/lam_flatplate.cfg
index fe83f857a37..13f3b7db032 100644
--- a/TestCases/navierstokes/flatplate/lam_flatplate.cfg
+++ b/TestCases/navierstokes/flatplate/lam_flatplate.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon						                           %
 % Institution: Stanford University					                           %
 % Date: 2013.09.30                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/navierstokes/flatplate/lam_flatplate_unst.cfg b/TestCases/navierstokes/flatplate/lam_flatplate_unst.cfg
index 26bae83a2f8..89050e0104c 100644
--- a/TestCases/navierstokes/flatplate/lam_flatplate_unst.cfg
+++ b/TestCases/navierstokes/flatplate/lam_flatplate_unst.cfg
@@ -2,7 +2,7 @@
 %                                                                              %
 % SU2 configuration file                                                       %
 % Case description: Test interp. restart, and auto time-step for dual-time     %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/navierstokes/naca0012/lam_NACA0012.cfg b/TestCases/navierstokes/naca0012/lam_NACA0012.cfg
index f64c2ff3956..1c31a0db257 100644
--- a/TestCases/navierstokes/naca0012/lam_NACA0012.cfg
+++ b/TestCases/navierstokes/naca0012/lam_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: Sep 28, 2012                                                           %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/navierstokes/poiseuille/lam_poiseuille.cfg b/TestCases/navierstokes/poiseuille/lam_poiseuille.cfg
index 73459ec133e..ba79d7445f6 100644
--- a/TestCases/navierstokes/poiseuille/lam_poiseuille.cfg
+++ b/TestCases/navierstokes/poiseuille/lam_poiseuille.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2017.02.27                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/navierstokes/poiseuille/profile_poiseuille.cfg b/TestCases/navierstokes/poiseuille/profile_poiseuille.cfg
index 2bc398301d7..d68a89741a1 100644
--- a/TestCases/navierstokes/poiseuille/profile_poiseuille.cfg
+++ b/TestCases/navierstokes/poiseuille/profile_poiseuille.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Robert Bosch LLC                                                %
 % Date: 2018.03.19                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nicf/LS89/turb_SA_PR.cfg b/TestCases/nicf/LS89/turb_SA_PR.cfg
index 4897151ae09..737fdb2f467 100644
--- a/TestCases/nicf/LS89/turb_SA_PR.cfg
+++ b/TestCases/nicf/LS89/turb_SA_PR.cfg
@@ -5,7 +5,7 @@
 % Author: M. Pini, S. Vitale                                                   %
 % Institution: Delft University of Technology                                  %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nicf/LS89/turb_SST_PR.cfg b/TestCases/nicf/LS89/turb_SST_PR.cfg
index e5d6ad55fb1..ff9d057c34c 100644
--- a/TestCases/nicf/LS89/turb_SST_PR.cfg
+++ b/TestCases/nicf/LS89/turb_SST_PR.cfg
@@ -5,7 +5,7 @@
 % Author: M. Pini, S. Vitale                                                   %
 % Institution: Delft University of Technology                                  %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nicf/coolprop/fluidModel.cfg b/TestCases/nicf/coolprop/fluidModel.cfg
index bc4e3c5bb53..89d0c98e03c 100644
--- a/TestCases/nicf/coolprop/fluidModel.cfg
+++ b/TestCases/nicf/coolprop/fluidModel.cfg
@@ -6,7 +6,7 @@
 % Author: Peng Yan, Alberto Guardone                                           %
 % Institution: Politecnico di Milano                                           %
 % Date: 2022.10.8                                                              %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nicf/coolprop/transportModel.cfg b/TestCases/nicf/coolprop/transportModel.cfg
index eecd0cc2790..1e731406a5d 100644
--- a/TestCases/nicf/coolprop/transportModel.cfg
+++ b/TestCases/nicf/coolprop/transportModel.cfg
@@ -6,7 +6,7 @@
 % Author: Peng Yan, Alberto Guardone                                           %
 % Institution: Politecnico di Milano                                           %
 % Date: 2022.11.26                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nicf/datadriven/datadriven_nozzle.cfg b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
index 46e3346ea60..65051295b75 100644
--- a/TestCases/nicf/datadriven/datadriven_nozzle.cfg
+++ b/TestCases/nicf/datadriven/datadriven_nozzle.cfg
@@ -7,7 +7,7 @@
 % Author: Evert Bunschoten                                                     %
 % Institution: Delft University of Technology                                  %
 % Date: 2022.10.8                                                              %
-% File Version  7.5.1 "Blackbird"                                              %
+% File Version  8.0.0 "Harrier"                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nicf/edge/edge_PPR.cfg b/TestCases/nicf/edge/edge_PPR.cfg
index 1da2049b479..06a3c9c7193 100644
--- a/TestCases/nicf/edge/edge_PPR.cfg
+++ b/TestCases/nicf/edge/edge_PPR.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2012.09.29                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nicf/edge/edge_VW.cfg b/TestCases/nicf/edge/edge_VW.cfg
index 48513627b34..91e8803278a 100644
--- a/TestCases/nicf/edge/edge_VW.cfg
+++ b/TestCases/nicf/edge/edge_VW.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2012.09.29                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nonequilibrium/invwedge/invwedge_ausm.cfg b/TestCases/nonequilibrium/invwedge/invwedge_ausm.cfg
index 2a549afcf4e..fcf606ccdf9 100644
--- a/TestCases/nonequilibrium/invwedge/invwedge_ausm.cfg
+++ b/TestCases/nonequilibrium/invwedge/invwedge_ausm.cfg
@@ -5,7 +5,7 @@
 % Author: C. Garbacz                                                           %
 % Institution: Strathclyde University                                          %
 % Date: 2020.11.01                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nonequilibrium/invwedge/invwedge_ausmplusup2.cfg b/TestCases/nonequilibrium/invwedge/invwedge_ausmplusup2.cfg
index d0c09a92926..48399a94fab 100644
--- a/TestCases/nonequilibrium/invwedge/invwedge_ausmplusup2.cfg
+++ b/TestCases/nonequilibrium/invwedge/invwedge_ausmplusup2.cfg
@@ -2,7 +2,7 @@
 %                                                                              %
 % SU2 configuration file                                                       %
 % Case description: Mach 5 inviscid flow over a 10deg wedge- AUSM+-Up2         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nonequilibrium/invwedge/invwedge_lax.cfg b/TestCases/nonequilibrium/invwedge/invwedge_lax.cfg
index d5b025f9ab4..2c5627fc9a2 100644
--- a/TestCases/nonequilibrium/invwedge/invwedge_lax.cfg
+++ b/TestCases/nonequilibrium/invwedge/invwedge_lax.cfg
@@ -2,7 +2,7 @@
 %                                                                              %
 % SU2 configuration file                                                       %
 % Case description: Mach 5 inviscid flow over a 10deg wedge-LAX                %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nonequilibrium/invwedge/invwedge_msw.cfg b/TestCases/nonequilibrium/invwedge/invwedge_msw.cfg
index 73585488a5f..39a7e051035 100644
--- a/TestCases/nonequilibrium/invwedge/invwedge_msw.cfg
+++ b/TestCases/nonequilibrium/invwedge/invwedge_msw.cfg
@@ -2,7 +2,7 @@
 %                                                                              %
 % SU2 configuration file                                                       %
 % Case description: Mach 5 inviscid flow over a 10deg wedge-MSW                %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nonequilibrium/invwedge/invwedge_roe.cfg b/TestCases/nonequilibrium/invwedge/invwedge_roe.cfg
index 6f871316deb..7264f767422 100644
--- a/TestCases/nonequilibrium/invwedge/invwedge_roe.cfg
+++ b/TestCases/nonequilibrium/invwedge/invwedge_roe.cfg
@@ -2,7 +2,7 @@
 %                                                                              %
 % SU2 configuration file                                                       %
 % Case description: Mach 5 inviscid flow over a 10deg wedge-ROE                %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nonequilibrium/invwedge/invwedge_ss_inlet.cfg b/TestCases/nonequilibrium/invwedge/invwedge_ss_inlet.cfg
index 44efe8a4c61..1d9d94eb0c1 100644
--- a/TestCases/nonequilibrium/invwedge/invwedge_ss_inlet.cfg
+++ b/TestCases/nonequilibrium/invwedge/invwedge_ss_inlet.cfg
@@ -5,7 +5,7 @@
 % Author: J. Needels                                                           %
 % Institution: Stanford University                                             %
 % Date: 2022.1.11                                                              %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nonequilibrium/thermalbath/finitechemistry/thermalbath.cfg b/TestCases/nonequilibrium/thermalbath/finitechemistry/thermalbath.cfg
index 171b4ba1140..10d2be9ffa2 100644
--- a/TestCases/nonequilibrium/thermalbath/finitechemistry/thermalbath.cfg
+++ b/TestCases/nonequilibrium/thermalbath/finitechemistry/thermalbath.cfg
@@ -7,7 +7,7 @@
 % Author: C. Garbacz                                                           %
 % Institution: Strathclyde University                                          %
 % Date: 2019.04.10                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nonequilibrium/thermalbath/frozen/thermalbath_frozen.cfg b/TestCases/nonequilibrium/thermalbath/frozen/thermalbath_frozen.cfg
index c2f0cf8e9aa..65e1ae94997 100644
--- a/TestCases/nonequilibrium/thermalbath/frozen/thermalbath_frozen.cfg
+++ b/TestCases/nonequilibrium/thermalbath/frozen/thermalbath_frozen.cfg
@@ -6,7 +6,7 @@
 % Author: C. Garbacz                                                           %
 % Institution: Strathclyde University                                          %
 % Date: 2019.04.10                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nonequilibrium/visc_wedge/axi_visccone.cfg b/TestCases/nonequilibrium/visc_wedge/axi_visccone.cfg
index e9ea9d6d366..9487af19964 100644
--- a/TestCases/nonequilibrium/visc_wedge/axi_visccone.cfg
+++ b/TestCases/nonequilibrium/visc_wedge/axi_visccone.cfg
@@ -4,7 +4,7 @@
 % Case description: Mach 5 viscous flow over a 10deg axisymmetric cone         %
 % Author: C. Garbacz                                                           %
 % Institution: Strathclyde University                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nonequilibrium/visc_wedge/partial_cat.cfg b/TestCases/nonequilibrium/visc_wedge/partial_cat.cfg
index a9677444f83..f139137c5ef 100644
--- a/TestCases/nonequilibrium/visc_wedge/partial_cat.cfg
+++ b/TestCases/nonequilibrium/visc_wedge/partial_cat.cfg
@@ -5,7 +5,7 @@
 %                   catalytic walls - gamma model, effeciency = 0.2            %
 % Author: J. Needels                                                           %
 % Institution: Stanford University                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nonequilibrium/visc_wedge/super_cat.cfg b/TestCases/nonequilibrium/visc_wedge/super_cat.cfg
index cde3c619d0b..a169763992c 100644
--- a/TestCases/nonequilibrium/visc_wedge/super_cat.cfg
+++ b/TestCases/nonequilibrium/visc_wedge/super_cat.cfg
@@ -5,7 +5,7 @@
 %                   catalytic walls - gamma model, effeciency = 0.2            %
 % Author: J. Needels                                                           %
 % Institution: Stanford University                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/nonequilibrium/viscwedge_mpp/viscwedge_mpp.cfg b/TestCases/nonequilibrium/viscwedge_mpp/viscwedge_mpp.cfg
index fb0b3169eb9..0e8a2c5e2c6 100644
--- a/TestCases/nonequilibrium/viscwedge_mpp/viscwedge_mpp.cfg
+++ b/TestCases/nonequilibrium/viscwedge_mpp/viscwedge_mpp.cfg
@@ -5,7 +5,7 @@
 % Author: C. Garbacz                                                           %
 % Institution: Strathclyde University                                          %
 % Date: 2020.11.01                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_euler/equivalentarea_naca64206/NACA64206.cfg b/TestCases/optimization_euler/equivalentarea_naca64206/NACA64206.cfg
index 0f61123ecba..429ea9fa6ea 100644
--- a/TestCases/optimization_euler/equivalentarea_naca64206/NACA64206.cfg
+++ b/TestCases/optimization_euler/equivalentarea_naca64206/NACA64206.cfg
@@ -5,7 +5,7 @@
 % Author: Yuki Utsumi                                                          %
 % Institution: Individual                                                      %
 % Date: 2021.08.07                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_2surf_1obj.cfg b/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_2surf_1obj.cfg
index d00a1493bc2..96bdf7ba4bf 100644
--- a/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_2surf_1obj.cfg
+++ b/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_2surf_1obj.cfg
@@ -7,7 +7,7 @@
 % Author: H.L. Kline, modified from inviscid wedge by Thomas D. Economon       %
 % Institution: Stanford University                                             %
 % Date: 2018.01.07                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj.cfg b/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj.cfg
index a87cfdbdc3a..97dc0cc3f0d 100644
--- a/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj.cfg
+++ b/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj.cfg
@@ -8,7 +8,7 @@
 % Author: H.L. Kline, modified from inviscid wedge by Thomas D. Economon       %
 % Institution: Stanford University                                             %
 % Date: 2018.01.07                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj_1surf.cfg b/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj_1surf.cfg
index 07f45eb5b0f..af75dd2f1e6 100644
--- a/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj_1surf.cfg
+++ b/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj_1surf.cfg
@@ -8,7 +8,7 @@
 % Author: H.L. Kline, modified from inviscid wedge by Thomas D. Economon       %
 % Institution: Stanford University                                             %
 % Date: 2018.01.07                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj_combo.cfg b/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj_combo.cfg
index 77e758b4b99..d36e9cdca3e 100644
--- a/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj_combo.cfg
+++ b/TestCases/optimization_euler/multiobjective_wedge/inv_wedge_ROE_multiobj_combo.cfg
@@ -10,7 +10,7 @@
 % Author: H.L. Kline, modified from inviscid wedge by Thomas D. Economon       %
 % Institution: Stanford University                                             %
 % Date: 2018.01.07                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_euler/multipoint_naca0012/inv_NACA0012_multipoint.cfg b/TestCases/optimization_euler/multipoint_naca0012/inv_NACA0012_multipoint.cfg
index 0774fc5c5e3..1cd29ecab6e 100644
--- a/TestCases/optimization_euler/multipoint_naca0012/inv_NACA0012_multipoint.cfg
+++ b/TestCases/optimization_euler/multipoint_naca0012/inv_NACA0012_multipoint.cfg
@@ -5,7 +5,7 @@
 % Author: Indiana Stokes                                                       %
 % Institution:                                                                 %
 % Date: 2017.07.03                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_euler/pitching_naca64a010/pitching_NACA64A010.cfg b/TestCases/optimization_euler/pitching_naca64a010/pitching_NACA64A010.cfg
index f4e9b0862ed..b48aa059677 100644
--- a/TestCases/optimization_euler/pitching_naca64a010/pitching_NACA64A010.cfg
+++ b/TestCases/optimization_euler/pitching_naca64a010/pitching_NACA64A010.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_euler/pitching_oneram6/pitching_ONERAM6.cfg b/TestCases/optimization_euler/pitching_oneram6/pitching_ONERAM6.cfg
index e056a0664da..5bc53860c7c 100644
--- a/TestCases/optimization_euler/pitching_oneram6/pitching_ONERAM6.cfg
+++ b/TestCases/optimization_euler/pitching_oneram6/pitching_ONERAM6.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon	      	      	              	       	       %
 % Institution: Stanford University				                               %
 % Date: 09.07.2011                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_euler/rotating_naca0012/rotating_NACA0012.cfg b/TestCases/optimization_euler/rotating_naca0012/rotating_NACA0012.cfg
index 4464ff2da1c..e1e8aa5de38 100644
--- a/TestCases/optimization_euler/rotating_naca0012/rotating_NACA0012.cfg
+++ b/TestCases/optimization_euler/rotating_naca0012/rotating_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.03.06                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg b/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg
index b98662f4560..13019e42b2c 100644
--- a/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg
+++ b/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_euler/steady_naca0012/inv_NACA0012_adv.cfg b/TestCases/optimization_euler/steady_naca0012/inv_NACA0012_adv.cfg
index 78250835802..ab5620cc9eb 100644
--- a/TestCases/optimization_euler/steady_naca0012/inv_NACA0012_adv.cfg
+++ b/TestCases/optimization_euler/steady_naca0012/inv_NACA0012_adv.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.09.29                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_euler/steady_naca0012/inv_NACA0012_basic.cfg b/TestCases/optimization_euler/steady_naca0012/inv_NACA0012_basic.cfg
index e0abfe78057..8d733763b2e 100644
--- a/TestCases/optimization_euler/steady_naca0012/inv_NACA0012_basic.cfg
+++ b/TestCases/optimization_euler/steady_naca0012/inv_NACA0012_basic.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 2013.09.29                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_euler/steady_oneram6/inv_ONERAM6_adv.cfg b/TestCases/optimization_euler/steady_oneram6/inv_ONERAM6_adv.cfg
index a0c55da8aed..04c72351cae 100644
--- a/TestCases/optimization_euler/steady_oneram6/inv_ONERAM6_adv.cfg
+++ b/TestCases/optimization_euler/steady_oneram6/inv_ONERAM6_adv.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios, Heather Kline	               	       	           %
 % Institution: Stanford University	                                           %
 % Date: 01.17.2017                                                             %
-% File Version 7.5.1 "Blackbird"                                                   %
+% File Version 8.0.0 "Harrier"                                                     %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_euler/steady_oneram6/inv_ONERAM6_basic.cfg b/TestCases/optimization_euler/steady_oneram6/inv_ONERAM6_basic.cfg
index b2dd3ee5e0f..0a7ac7a1953 100644
--- a/TestCases/optimization_euler/steady_oneram6/inv_ONERAM6_basic.cfg
+++ b/TestCases/optimization_euler/steady_oneram6/inv_ONERAM6_basic.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios, Heather Kline    	              	       	       %
 % Institution: Stanford University	                                           %
 % Date: 01.17.2017                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_rans/naca0012/naca0012.cfg b/TestCases/optimization_rans/naca0012/naca0012.cfg
index ffa7267f40c..e9304f8f4ee 100644
--- a/TestCases/optimization_rans/naca0012/naca0012.cfg
+++ b/TestCases/optimization_rans/naca0012/naca0012.cfg
@@ -5,7 +5,7 @@
 % Author: Steffen Schotthöfer                                                  %
 % Institution: TU Kaiserslautern                                               %
 % Date: Mar 16, 2017                                                           %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_rans/pitching_naca64a010/turb_NACA64A010.cfg b/TestCases/optimization_rans/pitching_naca64a010/turb_NACA64A010.cfg
index 9f42badaa70..389b2793a40 100644
--- a/TestCases/optimization_rans/pitching_naca64a010/turb_NACA64A010.cfg
+++ b/TestCases/optimization_rans/pitching_naca64a010/turb_NACA64A010.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_rans/pitching_oneram6/turb_ONERAM6.cfg b/TestCases/optimization_rans/pitching_oneram6/turb_ONERAM6.cfg
index b8dfed828bf..1ef6403d4ec 100644
--- a/TestCases/optimization_rans/pitching_oneram6/turb_ONERAM6.cfg
+++ b/TestCases/optimization_rans/pitching_oneram6/turb_ONERAM6.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_rans/steady_oneram6/turb_ONERAM6.cfg b/TestCases/optimization_rans/steady_oneram6/turb_ONERAM6.cfg
index 5d343bf53e7..3c625996b40 100644
--- a/TestCases/optimization_rans/steady_oneram6/turb_ONERAM6.cfg
+++ b/TestCases/optimization_rans/steady_oneram6/turb_ONERAM6.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/optimization_rans/steady_rae2822/turb_SA_RAE2822.cfg b/TestCases/optimization_rans/steady_rae2822/turb_SA_RAE2822.cfg
index bcf9093b451..57cd64ad136 100644
--- a/TestCases/optimization_rans/steady_rae2822/turb_SA_RAE2822.cfg
+++ b/TestCases/optimization_rans/steady_rae2822/turb_SA_RAE2822.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index e86bf444a5f..41eb39ba981 100644
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -3,7 +3,7 @@
 ## \file parallel_regression.py
 #  \brief Python script for automated regression testing of SU2 examples
 #  \author A. Aranake, A. Campos, T. Economon, T. Lukaczyk, S. Padron
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index 04f0bea1e73..10a28c974e1 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -3,7 +3,7 @@
 ## \file parallel_regression.py
 #  \brief Python script for automated regression testing of SU2 examples
 #  \author A. Aranake, A. Campos, T. Economon, T. Lukaczyk, S. Padron
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/pastix_support/config.cfg b/TestCases/pastix_support/config.cfg
index 7c19a368716..a715bf34e94 100644
--- a/TestCases/pastix_support/config.cfg
+++ b/TestCases/pastix_support/config.cfg
@@ -2,7 +2,7 @@
 % SU2 configuration file                                                 %
 % PaStiX options (http://pastix.gforge.inria.fr/files/README-txt.html)   %
 % Institution: Imperial College London                                   %
-% File Version 7.5.1 "Blackbird"                                         %
+% File Version 8.0.0 "Harrier"                                           %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
 % Intro:
diff --git a/TestCases/pastix_support/readme.txt b/TestCases/pastix_support/readme.txt
index 96736aeba43..a4eb59a2d3a 100644
--- a/TestCases/pastix_support/readme.txt
+++ b/TestCases/pastix_support/readme.txt
@@ -2,7 +2,7 @@
 % SU2 configuration file                                                 %
 % PaStiX support build instructions.                                     %
 % Institution: Imperial College London                                   %
-% File Version 7.5.1 "Blackbird"                                         %
+% File Version 8.0.0 "Harrier"                                           %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
 % 1 - Download
diff --git a/TestCases/polar/naca0012/inv_NACA0012.cfg b/TestCases/polar/naca0012/inv_NACA0012.cfg
index edf3775394c..1a9275c6ba2 100644
--- a/TestCases/polar/naca0012/inv_NACA0012.cfg
+++ b/TestCases/polar/naca0012/inv_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.11                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/py_wrapper/custom_heat_flux/run_ad.py b/TestCases/py_wrapper/custom_heat_flux/run_ad.py
index 8fa54a0a891..7985e4ff5a2 100644
--- a/TestCases/py_wrapper/custom_heat_flux/run_ad.py
+++ b/TestCases/py_wrapper/custom_heat_flux/run_ad.py
@@ -2,7 +2,7 @@
 
 ## \file run.py
 #  \brief Unsteady adjoint heat transfer case with custom heat flux.
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/py_wrapper/custom_load_fea/config.cfg b/TestCases/py_wrapper/custom_load_fea/config.cfg
index c0352190d77..45d6ef0e2b8 100644
--- a/TestCases/py_wrapper/custom_load_fea/config.cfg
+++ b/TestCases/py_wrapper/custom_load_fea/config.cfg
@@ -1,7 +1,7 @@
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 % SU2 configuration file                                                       %
 % Case description: 2D Beam with custom load via Python wrapper                %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 SOLVER= ELASTICITY
diff --git a/TestCases/py_wrapper/custom_load_fea/run.py b/TestCases/py_wrapper/custom_load_fea/run.py
index 24881ef85df..50567ddfc73 100755
--- a/TestCases/py_wrapper/custom_load_fea/run.py
+++ b/TestCases/py_wrapper/custom_load_fea/run.py
@@ -2,7 +2,7 @@
 
 ## \file run.py
 #  \brief FEA case with custom load.
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/py_wrapper/custom_load_fea/run_ad.py b/TestCases/py_wrapper/custom_load_fea/run_ad.py
index c7b7ebbc48f..907264b39fd 100644
--- a/TestCases/py_wrapper/custom_load_fea/run_ad.py
+++ b/TestCases/py_wrapper/custom_load_fea/run_ad.py
@@ -2,7 +2,7 @@
 
 ## \file run.py
 #  \brief Unsteady adjoint FEA case with custom load.
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/py_wrapper/deforming_bump_in_channel/run.py b/TestCases/py_wrapper/deforming_bump_in_channel/run.py
index 894315baff0..45c6e53b7d3 100755
--- a/TestCases/py_wrapper/deforming_bump_in_channel/run.py
+++ b/TestCases/py_wrapper/deforming_bump_in_channel/run.py
@@ -2,7 +2,7 @@
 
 ## \file run.py
 #  \brief Deforming bump in channel.
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
index 210a1222706..fbdafc0e1ec 100755
--- a/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_fea/flow_load_sens/run_adjoint.py
@@ -3,7 +3,7 @@
 ## \file run_adjoint.py
 #  \brief Python script to launch SU2_CFD_AD and compute the sensitivity of the FEA problem respect to flow loads.
 #  \author Ruben Sanchez
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py b/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
index a613757019d..49c8977a504 100755
--- a/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
+++ b/TestCases/py_wrapper/disc_adj_flow/mesh_disp_sens/run_adjoint.py
@@ -3,7 +3,7 @@
 ## \file run_adjoint.py
 #  \brief Python script to launch SU2_CFD_AD
 #  \author Ruben Sanchez
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/py_wrapper/dyn_fsi/run.py b/TestCases/py_wrapper/dyn_fsi/run.py
index ba6253db6b8..19dce3c8b5a 100644
--- a/TestCases/py_wrapper/dyn_fsi/run.py
+++ b/TestCases/py_wrapper/dyn_fsi/run.py
@@ -2,7 +2,7 @@
 
 ## \file run.py
 #  \brief Unsteady FSI case with custom load.
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/py_wrapper/flatPlate_rigidMotion/flatPlate_rigidMotion_Conf.cfg b/TestCases/py_wrapper/flatPlate_rigidMotion/flatPlate_rigidMotion_Conf.cfg
index 175e61c56a5..8577b5a87ab 100644
--- a/TestCases/py_wrapper/flatPlate_rigidMotion/flatPlate_rigidMotion_Conf.cfg
+++ b/TestCases/py_wrapper/flatPlate_rigidMotion/flatPlate_rigidMotion_Conf.cfg
@@ -5,7 +5,7 @@
 % Author: ___________________________________________________________________  %
 % Institution: ______________________________________________________________  %
 % Date: __________                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
index d5f1cf1a087..4fa464f8d44 100755
--- a/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
+++ b/TestCases/py_wrapper/flatPlate_rigidMotion/launch_flatPlate_rigidMotion.py
@@ -3,7 +3,7 @@
 ## \file flatPlate_rigidMotion.py
 #  \brief Python script to launch SU2_CFD with customized unsteady boundary conditions using the Python wrapper.
 #  \author David Thomas
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py b/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
index 9a96ead26e3..276e37fa520 100755
--- a/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
+++ b/TestCases/py_wrapper/flatPlate_unsteady_CHT/launch_unsteady_CHT_FlatPlate.py
@@ -3,7 +3,7 @@
 ## \file launch_unsteady_CHT_FlatPlate.py
 #  \brief Python script to launch SU2_CFD with customized unsteady boundary conditions using the Python wrapper.
 #  \author David Thomas
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/py_wrapper/flatPlate_unsteady_CHT/unsteady_CHT_FlatPlate_Conf.cfg b/TestCases/py_wrapper/flatPlate_unsteady_CHT/unsteady_CHT_FlatPlate_Conf.cfg
index 04c73f951bf..f7b504e96a7 100644
--- a/TestCases/py_wrapper/flatPlate_unsteady_CHT/unsteady_CHT_FlatPlate_Conf.cfg
+++ b/TestCases/py_wrapper/flatPlate_unsteady_CHT/unsteady_CHT_FlatPlate_Conf.cfg
@@ -5,7 +5,7 @@
 % Author: David THOMAS                                                         %
 % Institution: University of Liège                                             %
 % Date: 12/12/2017                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/py_wrapper/wavy_wall/run_steady.py b/TestCases/py_wrapper/wavy_wall/run_steady.py
index 3f0372cf646..07090c6790b 100644
--- a/TestCases/py_wrapper/wavy_wall/run_steady.py
+++ b/TestCases/py_wrapper/wavy_wall/run_steady.py
@@ -2,7 +2,7 @@
 
 ## \file run.py
 #  \brief Channel with wave-like motion on walls (steady state version).
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/radiation/p1adjoint/configp1adjoint.cfg b/TestCases/radiation/p1adjoint/configp1adjoint.cfg
index cb7178a2aee..bc71c6fdfd3 100644
--- a/TestCases/radiation/p1adjoint/configp1adjoint.cfg
+++ b/TestCases/radiation/p1adjoint/configp1adjoint.cfg
@@ -4,7 +4,7 @@
 % Case description: Coupled CFD-RHT adjoint problem                            %
 % Author: Ruben Sanchez (TU Kaiserslautern)                                    %
 % Date: 2020-02-13                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/radiation/p1model/configp1.cfg b/TestCases/radiation/p1model/configp1.cfg
index f03ab47fe66..49c24ef4813 100644
--- a/TestCases/radiation/p1model/configp1.cfg
+++ b/TestCases/radiation/p1model/configp1.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez                                                        %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern               %
 % Date: 2019-01-29                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/actuatordisk_variable_load/propeller_variable_load.cfg b/TestCases/rans/actuatordisk_variable_load/propeller_variable_load.cfg
index 8fc5c9737e7..6fbd652d6c1 100644
--- a/TestCases/rans/actuatordisk_variable_load/propeller_variable_load.cfg
+++ b/TestCases/rans/actuatordisk_variable_load/propeller_variable_load.cfg
@@ -8,7 +8,7 @@
 % Comments: Grid file and propeller data courtesy of Mauro Minervino,          %
 %           Centro Italiano Ricerche Aerospaziali (CIRA)                       %
 % Date: 07/08/2020                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/flatplate/turb_SA_flatplate.cfg b/TestCases/rans/flatplate/turb_SA_flatplate.cfg
index d62701dd5c4..668de90324a 100644
--- a/TestCases/rans/flatplate/turb_SA_flatplate.cfg
+++ b/TestCases/rans/flatplate/turb_SA_flatplate.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.10                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/flatplate/turb_SA_flatplate_species.cfg b/TestCases/rans/flatplate/turb_SA_flatplate_species.cfg
index e09fe245164..bcf1c84c107 100644
--- a/TestCases/rans/flatplate/turb_SA_flatplate_species.cfg
+++ b/TestCases/rans/flatplate/turb_SA_flatplate_species.cfg
@@ -6,7 +6,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Bosch Thermotechmniek B.V.                                      %
 % Date: 2021.11.30                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/flatplate/turb_SST_flatplate.cfg b/TestCases/rans/flatplate/turb_SST_flatplate.cfg
index 0758224d3d2..c0286b69232 100644
--- a/TestCases/rans/flatplate/turb_SST_flatplate.cfg
+++ b/TestCases/rans/flatplate/turb_SST_flatplate.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.10                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sa.cfg b/TestCases/rans/naca0012/turb_NACA0012_sa.cfg
index c80150a03b6..738a8bec2d2 100644
--- a/TestCases/rans/naca0012/turb_NACA0012_sa.cfg
+++ b/TestCases/rans/naca0012/turb_NACA0012_sa.cfg
@@ -6,7 +6,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst.cfg
index caa8b1bad5b..a36eb3b5b4e 100644
--- a/TestCases/rans/naca0012/turb_NACA0012_sst.cfg
+++ b/TestCases/rans/naca0012/turb_NACA0012_sst.cfg
@@ -6,7 +6,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_1994-KLm.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_1994-KLm.cfg
index 42e5ae174c0..1411fd2c953 100644
--- a/TestCases/rans/naca0012/turb_NACA0012_sst_1994-KLm.cfg
+++ b/TestCases/rans/naca0012/turb_NACA0012_sst_1994-KLm.cfg
@@ -3,7 +3,7 @@
 % SU2 configuration file                                                       %
 % Case description: 2D NACA 0012 Airfoil Validation Case (compressible)        %
 %                   SST-1994-KLm implementation                                %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_2003-Vm.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_2003-Vm.cfg
index c0909cb317e..2dce5941829 100644
--- a/TestCases/rans/naca0012/turb_NACA0012_sst_2003-Vm.cfg
+++ b/TestCases/rans/naca0012/turb_NACA0012_sst_2003-Vm.cfg
@@ -3,7 +3,7 @@
 % SU2 configuration file                                                       %
 % Case description: 2D NACA 0012 Airfoil Validation Case (compressible)        %
 %                   SST-2003-Vm implementation                                 %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_2003m.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_2003m.cfg
index c37bee5d16a..6f056773a76 100644
--- a/TestCases/rans/naca0012/turb_NACA0012_sst_2003m.cfg
+++ b/TestCases/rans/naca0012/turb_NACA0012_sst_2003m.cfg
@@ -1,7 +1,7 @@
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %                                                                              %
 % SU2 configuration file, NACA0012 RANS SST-2003m                              %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_expliciteuler.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_expliciteuler.cfg
index e0043632254..6540e1ae5bb 100644
--- a/TestCases/rans/naca0012/turb_NACA0012_sst_expliciteuler.cfg
+++ b/TestCases/rans/naca0012/turb_NACA0012_sst_expliciteuler.cfg
@@ -5,7 +5,7 @@
 % Author: Max Aehle                                                            %
 % Institution: TU Kaiserslautern                                               %
 % Date: Nov 17th, 2021                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_fixedvalues.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_fixedvalues.cfg
index e461badd1e7..7ff516e2f63 100644
--- a/TestCases/rans/naca0012/turb_NACA0012_sst_fixedvalues.cfg
+++ b/TestCases/rans/naca0012/turb_NACA0012_sst_fixedvalues.cfg
@@ -5,7 +5,7 @@
 % Author: Max Aehle                                                            %
 % Institution: TU Kaiserslautern                                               %
 % Date: Mar 17th, 2021                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_multigrid_restart.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_multigrid_restart.cfg
index 15af3903f87..89e1eb1d810 100644
--- a/TestCases/rans/naca0012/turb_NACA0012_sst_multigrid_restart.cfg
+++ b/TestCases/rans/naca0012/turb_NACA0012_sst_multigrid_restart.cfg
@@ -6,7 +6,7 @@
 % Author: David E. Manosalvas                                                  %
 % Institution: Stanford University                                             %
 % Date: 02.14.2017                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_sust.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_sust.cfg
index 96f1c5a672e..7d0e6ce7092 100644
--- a/TestCases/rans/naca0012/turb_NACA0012_sst_sust.cfg
+++ b/TestCases/rans/naca0012/turb_NACA0012_sst_sust.cfg
@@ -6,7 +6,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/oneram6/turb_ONERAM6.cfg b/TestCases/rans/oneram6/turb_ONERAM6.cfg
index 4dc93e48803..120cb1ca510 100644
--- a/TestCases/rans/oneram6/turb_ONERAM6.cfg
+++ b/TestCases/rans/oneram6/turb_ONERAM6.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.14                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/oneram6/turb_ONERAM6_nk.cfg b/TestCases/rans/oneram6/turb_ONERAM6_nk.cfg
index acd93ebaff7..106487e4170 100644
--- a/TestCases/rans/oneram6/turb_ONERAM6_nk.cfg
+++ b/TestCases/rans/oneram6/turb_ONERAM6_nk.cfg
@@ -2,7 +2,7 @@
 %                                                                              %
 % SU2 configuration file                                                       %
 % Case description: Turbulent flow, ONERA M6, Newton-Krylov solver             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/oneram6/turb_ONERAM6_vc.cfg b/TestCases/rans/oneram6/turb_ONERAM6_vc.cfg
index 16ba7484c52..9a1beb75842 100644
--- a/TestCases/rans/oneram6/turb_ONERAM6_vc.cfg
+++ b/TestCases/rans/oneram6/turb_ONERAM6_vc.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2014.06.14                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/propeller/propeller.cfg b/TestCases/rans/propeller/propeller.cfg
index 2bf449c916a..588c7f5fb1e 100644
--- a/TestCases/rans/propeller/propeller.cfg
+++ b/TestCases/rans/propeller/propeller.cfg
@@ -5,7 +5,7 @@
 % Author:                                                                      %
 % Institution:                                                                 %
 % Date:                                                                        %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/rae2822/turb_SA_RAE2822.cfg b/TestCases/rans/rae2822/turb_SA_RAE2822.cfg
index 73397fe91a1..799744ef8cd 100644
--- a/TestCases/rans/rae2822/turb_SA_RAE2822.cfg
+++ b/TestCases/rans/rae2822/turb_SA_RAE2822.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/rae2822/turb_SST_RAE2822.cfg b/TestCases/rans/rae2822/turb_SST_RAE2822.cfg
index f28e58a14ad..235d69197b5 100644
--- a/TestCases/rans/rae2822/turb_SST_RAE2822.cfg
+++ b/TestCases/rans/rae2822/turb_SST_RAE2822.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/rae2822/turb_SST_SUST_RAE2822.cfg b/TestCases/rans/rae2822/turb_SST_SUST_RAE2822.cfg
index 3d95d9c82b3..18cea09288e 100644
--- a/TestCases/rans/rae2822/turb_SST_SUST_RAE2822.cfg
+++ b/TestCases/rans/rae2822/turb_SST_SUST_RAE2822.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/restart_directdiff_naca/naca0012.cfg b/TestCases/rans/restart_directdiff_naca/naca0012.cfg
index 35d4d38bec5..78d355bd28a 100644
--- a/TestCases/rans/restart_directdiff_naca/naca0012.cfg
+++ b/TestCases/rans/restart_directdiff_naca/naca0012.cfg
@@ -5,7 +5,7 @@
 % Author: Steffen Schotthöfer                                                  %
 % Institution: TU Kaiserslautern                                               %
 % Date: Mar 16, 2017                                                           %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/s809/trans_s809.cfg b/TestCases/rans/s809/trans_s809.cfg
index d807bd0f496..c5e60357c06 100644
--- a/TestCases/rans/s809/trans_s809.cfg
+++ b/TestCases/rans/s809/trans_s809.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/s809/turb_S809.cfg b/TestCases/rans/s809/turb_S809.cfg
index 6691fa178a0..ab0bf685b8b 100644
--- a/TestCases/rans/s809/turb_S809.cfg
+++ b/TestCases/rans/s809/turb_S809.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios                                                   %
 % Institution: Stanford University                                             %
 % Date: 5/15/2013                                                              %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans/vki_turbine/turb_vki.cfg b/TestCases/rans/vki_turbine/turb_vki.cfg
index c808a08bdce..c8c3230da57 100644
--- a/TestCases/rans/vki_turbine/turb_vki.cfg
+++ b/TestCases/rans/vki_turbine/turb_vki.cfg
@@ -5,7 +5,7 @@
 % Author: Francisco Palacios, Thomas D. Economon	                           %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans_uq/naca0012/turb_NACA0012_uq.cfg b/TestCases/rans_uq/naca0012/turb_NACA0012_uq.cfg
index 07cff339ab3..27901dc69af 100644
--- a/TestCases/rans_uq/naca0012/turb_NACA0012_uq.cfg
+++ b/TestCases/rans_uq/naca0012/turb_NACA0012_uq.cfg
@@ -6,7 +6,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_1c.cfg b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_1c.cfg
index e4a2d92ae6f..5cef3fb5437 100644
--- a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_1c.cfg
+++ b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_1c.cfg
@@ -6,7 +6,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_2c.cfg b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_2c.cfg
index e3ed070d761..96cb46e5a0a 100644
--- a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_2c.cfg
+++ b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_2c.cfg
@@ -6,7 +6,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_3c.cfg b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_3c.cfg
index 9a09a1d30b6..f6d157f2d8e 100644
--- a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_3c.cfg
+++ b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_3c.cfg
@@ -6,7 +6,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c1.cfg b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c1.cfg
index d3a0ab603c9..c707ebf78ed 100644
--- a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c1.cfg
+++ b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c1.cfg
@@ -6,7 +6,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c2.cfg b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c2.cfg
index 2dc0002cf58..3a0dafa99c2 100644
--- a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c2.cfg
+++ b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c2.cfg
@@ -6,7 +6,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rotating/caradonna_tung/rot_caradonna_tung.cfg b/TestCases/rotating/caradonna_tung/rot_caradonna_tung.cfg
index 944dc7c99c3..a84b6b28812 100644
--- a/TestCases/rotating/caradonna_tung/rot_caradonna_tung.cfg
+++ b/TestCases/rotating/caradonna_tung/rot_caradonna_tung.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2020.05.24                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/rotating/naca0012/rot_NACA0012.cfg b/TestCases/rotating/naca0012/rot_NACA0012.cfg
index 608002221ad..c90d00bc954 100644
--- a/TestCases/rotating/naca0012/rot_NACA0012.cfg
+++ b/TestCases/rotating/naca0012/rot_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2020.06.06                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/serial_regression.py b/TestCases/serial_regression.py
index 0ca25c6f3c4..a8486bc11ea 100644
--- a/TestCases/serial_regression.py
+++ b/TestCases/serial_regression.py
@@ -3,7 +3,7 @@
 ## \file serial_regression.py
 #  \brief Python script for automated regression testing of SU2 examples
 #  \author A. Aranake, A. Campos, T. Economon, T. Lukaczyk, S. Padron
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/serial_regression_AD.py b/TestCases/serial_regression_AD.py
index 6d0a32046f2..e8300572518 100644
--- a/TestCases/serial_regression_AD.py
+++ b/TestCases/serial_regression_AD.py
@@ -3,7 +3,7 @@
 ## \file serial_regression.py
 #  \brief Python script for automated regression testing of SU2 examples
 #  \author A. Aranake, A. Campos, T. Economon, T. Lukaczyk, S. Padron
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/sliding_interface/bars_SST_2D/bars.cfg b/TestCases/sliding_interface/bars_SST_2D/bars.cfg
index 0f2557b9bfd..bc43e495803 100644
--- a/TestCases/sliding_interface/bars_SST_2D/bars.cfg
+++ b/TestCases/sliding_interface/bars_SST_2D/bars.cfg
@@ -5,7 +5,7 @@
 % Author: A. Rubino                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: Feb 27th, 2017                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/bars_SST_2D/zone_1.cfg b/TestCases/sliding_interface/bars_SST_2D/zone_1.cfg
index c1a65e2f854..7a20c9c665e 100644
--- a/TestCases/sliding_interface/bars_SST_2D/zone_1.cfg
+++ b/TestCases/sliding_interface/bars_SST_2D/zone_1.cfg
@@ -5,7 +5,7 @@
 % Author: A. Rubino                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: Feb 27th, 2017                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/bars_SST_2D/zone_2.cfg b/TestCases/sliding_interface/bars_SST_2D/zone_2.cfg
index 85af3fd372d..10a4e2936c5 100644
--- a/TestCases/sliding_interface/bars_SST_2D/zone_2.cfg
+++ b/TestCases/sliding_interface/bars_SST_2D/zone_2.cfg
@@ -5,7 +5,7 @@
 % Author: A. Rubino                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: Feb 27th, 2017                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/bars_SST_2D/zone_3.cfg b/TestCases/sliding_interface/bars_SST_2D/zone_3.cfg
index bd7e75c4d8d..8f184e207e2 100644
--- a/TestCases/sliding_interface/bars_SST_2D/zone_3.cfg
+++ b/TestCases/sliding_interface/bars_SST_2D/zone_3.cfg
@@ -5,7 +5,7 @@
 % Author: A. Rubino                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: Feb 27th, 2017                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/channel_2D/channel_2D_NN.cfg b/TestCases/sliding_interface/channel_2D/channel_2D_NN.cfg
index e546995168e..c2eb991a72e 100644
--- a/TestCases/sliding_interface/channel_2D/channel_2D_NN.cfg
+++ b/TestCases/sliding_interface/channel_2D/channel_2D_NN.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/channel_2D/channel_2D_WA.cfg b/TestCases/sliding_interface/channel_2D/channel_2D_WA.cfg
index 7c38f87366c..2f1dc19dcf7 100644
--- a/TestCases/sliding_interface/channel_2D/channel_2D_WA.cfg
+++ b/TestCases/sliding_interface/channel_2D/channel_2D_WA.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/channel_2D/zone_2.cfg b/TestCases/sliding_interface/channel_2D/zone_2.cfg
index 81fd7b5a632..6040c078bcf 100644
--- a/TestCases/sliding_interface/channel_2D/zone_2.cfg
+++ b/TestCases/sliding_interface/channel_2D/zone_2.cfg
@@ -5,7 +5,7 @@
 % Author: A. Rubino                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: Feb 27th, 2017                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/channel_2D/zone_3.cfg b/TestCases/sliding_interface/channel_2D/zone_3.cfg
index bd7e75c4d8d..8f184e207e2 100644
--- a/TestCases/sliding_interface/channel_2D/zone_3.cfg
+++ b/TestCases/sliding_interface/channel_2D/zone_3.cfg
@@ -5,7 +5,7 @@
 % Author: A. Rubino                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: Feb 27th, 2017                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/channel_3D/channel_3D_NN.cfg b/TestCases/sliding_interface/channel_3D/channel_3D_NN.cfg
index ff4f2a2c47f..836e18b052e 100644
--- a/TestCases/sliding_interface/channel_3D/channel_3D_NN.cfg
+++ b/TestCases/sliding_interface/channel_3D/channel_3D_NN.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/channel_3D/channel_3D_WA.cfg b/TestCases/sliding_interface/channel_3D/channel_3D_WA.cfg
index c45d7e5b6ab..6e89041dc95 100644
--- a/TestCases/sliding_interface/channel_3D/channel_3D_WA.cfg
+++ b/TestCases/sliding_interface/channel_3D/channel_3D_WA.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/channel_3D/zone_1.cfg b/TestCases/sliding_interface/channel_3D/zone_1.cfg
index 58bf4da96e9..f0863a91ad2 100644
--- a/TestCases/sliding_interface/channel_3D/zone_1.cfg
+++ b/TestCases/sliding_interface/channel_3D/zone_1.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/channel_3D/zone_2.cfg b/TestCases/sliding_interface/channel_3D/zone_2.cfg
index 63c195e9d21..7fd28d0e8a4 100644
--- a/TestCases/sliding_interface/channel_3D/zone_2.cfg
+++ b/TestCases/sliding_interface/channel_3D/zone_2.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/channel_3D/zone_3.cfg b/TestCases/sliding_interface/channel_3D/zone_3.cfg
index 27e586baa60..761a126c09d 100644
--- a/TestCases/sliding_interface/channel_3D/zone_3.cfg
+++ b/TestCases/sliding_interface/channel_3D/zone_3.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/incompressible_steady/config.cfg b/TestCases/sliding_interface/incompressible_steady/config.cfg
index 0abe97efa10..cc19cc09a15 100644
--- a/TestCases/sliding_interface/incompressible_steady/config.cfg
+++ b/TestCases/sliding_interface/incompressible_steady/config.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 8.0.0 "Harrier"                                                  %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/incompressible_steady/configCircle.cfg b/TestCases/sliding_interface/incompressible_steady/configCircle.cfg
index 82943af7b81..757f2469edc 100644
--- a/TestCases/sliding_interface/incompressible_steady/configCircle.cfg
+++ b/TestCases/sliding_interface/incompressible_steady/configCircle.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 8.0.0 "Harrier"                                                  %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/incompressible_steady/configOut.cfg b/TestCases/sliding_interface/incompressible_steady/configOut.cfg
index d19fb2e702c..f9523435cce 100644
--- a/TestCases/sliding_interface/incompressible_steady/configOut.cfg
+++ b/TestCases/sliding_interface/incompressible_steady/configOut.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 8.0.0 "Harrier"                                                  %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/incompressible_unsteady/config.cfg b/TestCases/sliding_interface/incompressible_unsteady/config.cfg
index 4c3221eff70..ea76fd46db9 100644
--- a/TestCases/sliding_interface/incompressible_unsteady/config.cfg
+++ b/TestCases/sliding_interface/incompressible_unsteady/config.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 8.0.0 "Harrier"                                                  %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg b/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg
index 9bc21717854..6640fda6613 100644
--- a/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg
+++ b/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 8.0.0 "Harrier"                                                  %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg b/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg
index 29941635096..7885a977b1e 100644
--- a/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg
+++ b/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg
@@ -5,7 +5,7 @@
 % Author: Ruben Sanchez                                                         %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: January 28th, 2018                                                      %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 8.0.0 "Harrier"                                                  %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/pipe/pipe_NN.cfg b/TestCases/sliding_interface/pipe/pipe_NN.cfg
index 3913e6b54d9..d7b7b982336 100644
--- a/TestCases/sliding_interface/pipe/pipe_NN.cfg
+++ b/TestCases/sliding_interface/pipe/pipe_NN.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/pipe/pipe_WA.cfg b/TestCases/sliding_interface/pipe/pipe_WA.cfg
index f7ec3b6e11d..307ada6e126 100644
--- a/TestCases/sliding_interface/pipe/pipe_WA.cfg
+++ b/TestCases/sliding_interface/pipe/pipe_WA.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/pipe/zone_1.cfg b/TestCases/sliding_interface/pipe/zone_1.cfg
index a5e3c809779..487b236174a 100644
--- a/TestCases/sliding_interface/pipe/zone_1.cfg
+++ b/TestCases/sliding_interface/pipe/zone_1.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/pipe/zone_2.cfg b/TestCases/sliding_interface/pipe/zone_2.cfg
index eecb43bb74d..29e2f7de0d0 100644
--- a/TestCases/sliding_interface/pipe/zone_2.cfg
+++ b/TestCases/sliding_interface/pipe/zone_2.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/pipe/zone_3.cfg b/TestCases/sliding_interface/pipe/zone_3.cfg
index e820acd1080..102d9e56724 100644
--- a/TestCases/sliding_interface/pipe/zone_3.cfg
+++ b/TestCases/sliding_interface/pipe/zone_3.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/pipe/zone_4.cfg b/TestCases/sliding_interface/pipe/zone_4.cfg
index fcb17f1306e..6aff37ad147 100644
--- a/TestCases/sliding_interface/pipe/zone_4.cfg
+++ b/TestCases/sliding_interface/pipe/zone_4.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/pipe/zone_5.cfg b/TestCases/sliding_interface/pipe/zone_5.cfg
index eecb43bb74d..29e2f7de0d0 100644
--- a/TestCases/sliding_interface/pipe/zone_5.cfg
+++ b/TestCases/sliding_interface/pipe/zone_5.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_NN.cfg b/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_NN.cfg
index d87a7ca0380..fde950d8301 100644
--- a/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_NN.cfg
+++ b/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_NN.cfg
@@ -5,7 +5,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_WA.cfg b/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_WA.cfg
index 4175de10251..a41e54fc9df 100644
--- a/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_WA.cfg
+++ b/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_WA.cfg
@@ -5,7 +5,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/single_stage/single_stage_NN.cfg b/TestCases/sliding_interface/single_stage/single_stage_NN.cfg
index 27cd9e3f2ac..ec60565c35c 100644
--- a/TestCases/sliding_interface/single_stage/single_stage_NN.cfg
+++ b/TestCases/sliding_interface/single_stage/single_stage_NN.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/single_stage/single_stage_WA.cfg b/TestCases/sliding_interface/single_stage/single_stage_WA.cfg
index db325d42231..01ac60458d8 100644
--- a/TestCases/sliding_interface/single_stage/single_stage_WA.cfg
+++ b/TestCases/sliding_interface/single_stage/single_stage_WA.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/single_stage/zone_1.cfg b/TestCases/sliding_interface/single_stage/zone_1.cfg
index d9e3562d2f8..2b5a41feccb 100644
--- a/TestCases/sliding_interface/single_stage/zone_1.cfg
+++ b/TestCases/sliding_interface/single_stage/zone_1.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/single_stage/zone_2.cfg b/TestCases/sliding_interface/single_stage/zone_2.cfg
index a1f8e39705f..22481326908 100644
--- a/TestCases/sliding_interface/single_stage/zone_2.cfg
+++ b/TestCases/sliding_interface/single_stage/zone_2.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_NN.cfg b/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_NN.cfg
index 63142b86007..157a43a7124 100644
--- a/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_NN.cfg
+++ b/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_NN.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_WA.cfg b/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_WA.cfg
index 5c5a27cdef5..9e3729a2ade 100644
--- a/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_WA.cfg
+++ b/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_WA.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/supersonic_vortex_shedding/zone_1.cfg b/TestCases/sliding_interface/supersonic_vortex_shedding/zone_1.cfg
index eaec56b6f9d..ef3679f63e4 100644
--- a/TestCases/sliding_interface/supersonic_vortex_shedding/zone_1.cfg
+++ b/TestCases/sliding_interface/supersonic_vortex_shedding/zone_1.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/supersonic_vortex_shedding/zone_2.cfg b/TestCases/sliding_interface/supersonic_vortex_shedding/zone_2.cfg
index 66b6fc00f87..5d9e8b2bbaa 100644
--- a/TestCases/sliding_interface/supersonic_vortex_shedding/zone_2.cfg
+++ b/TestCases/sliding_interface/supersonic_vortex_shedding/zone_2.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/uniform_flow/uniform_NN.cfg b/TestCases/sliding_interface/uniform_flow/uniform_NN.cfg
index a6235e7dfae..2b3c84f7dd5 100644
--- a/TestCases/sliding_interface/uniform_flow/uniform_NN.cfg
+++ b/TestCases/sliding_interface/uniform_flow/uniform_NN.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/uniform_flow/uniform_WA.cfg b/TestCases/sliding_interface/uniform_flow/uniform_WA.cfg
index 55a7a8c2fe4..3dd8981de59 100644
--- a/TestCases/sliding_interface/uniform_flow/uniform_WA.cfg
+++ b/TestCases/sliding_interface/uniform_flow/uniform_WA.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/sliding_interface/uniform_flow/zone_1.cfg b/TestCases/sliding_interface/uniform_flow/zone_1.cfg
index 2caae2c2b18..a49ac681c71 100644
--- a/TestCases/sliding_interface/uniform_flow/zone_1.cfg
+++ b/TestCases/sliding_interface/uniform_flow/zone_1.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/sliding_interface/uniform_flow/zone_2.cfg b/TestCases/sliding_interface/uniform_flow/zone_2.cfg
index 60da4c4a95d..d4b7417f236 100644
--- a/TestCases/sliding_interface/uniform_flow/zone_2.cfg
+++ b/TestCases/sliding_interface/uniform_flow/zone_2.cfg
@@ -6,7 +6,7 @@
 % Author: G. Gori                                                              %
 % Institution: Politecnico di Milano                                           %
 % Date: Oct 5th, 2016                                                          %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/solid_heat_conduction/periodic_pins/configSolid.cfg b/TestCases/solid_heat_conduction/periodic_pins/configSolid.cfg
index 2db8bed2736..f96249130fe 100644
--- a/TestCases/solid_heat_conduction/periodic_pins/configSolid.cfg
+++ b/TestCases/solid_heat_conduction/periodic_pins/configSolid.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Bosch Thermotechniek B.V.                                       %
 % Date: 2021.09.27                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/species_transport/multizone/configMaster.cfg b/TestCases/species_transport/multizone/configMaster.cfg
index 4f4f1ca2cae..6a7c2ba8b2b 100644
--- a/TestCases/species_transport/multizone/configMaster.cfg
+++ b/TestCases/species_transport/multizone/configMaster.cfg
@@ -5,7 +5,7 @@
 % Author: N. Beishuizen                                                         %
 % Institution: Technische Universiteit Eindhoven                                %
 % Date: November 1, 2022                                                        %
-% File Version 7.5.1 "Blackbird"                                                %
+% File Version 8.0.0 "Harrier"                                                  %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/species_transport/passive_transport_validation/passive_transport.cfg b/TestCases/species_transport/passive_transport_validation/passive_transport.cfg
index a618a1e4e1c..fa8becb14b7 100644
--- a/TestCases/species_transport/passive_transport_validation/passive_transport.cfg
+++ b/TestCases/species_transport/passive_transport_validation/passive_transport.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Bosch Thermotechniek B.V                                        %
 % Date: 2021.10.02                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi.cfg
index d39ae5957ac..1b71c6a547c 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Bosch Thermotechniek B.V.                                       %
 % Date: 2021/10/14                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_boundedscalar.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_boundedscalar.cfg
index 4f5a9a62460..203761d77b7 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_boundedscalar.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_boundedscalar.cfg
@@ -5,7 +5,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Bosch Thermotechniek B.V.                                       %
 % Date: 2021/10/14                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel.cfg
index 5ad7433c102..92d226acb9a 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel.cfg
@@ -7,7 +7,7 @@
 % Author: Cristopher Morales Ubal                                              %
 % Institution: Eindhoven University of Technology                              %
 % Date: 2022/06/15                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg
index f49ea42aa8e..370cba307fd 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_TURBULENT_MARKERS.cfg
@@ -8,7 +8,7 @@
 % Author: Cristopher Morales Ubal                                              %
 % Institution: Eindhoven University of Technology                              %
 % Date: 2022/12/05                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_boundedscalar.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_boundedscalar.cfg
index 319ab8e778e..7ecc9f86d17 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_boundedscalar.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_boundedscalar.cfg
@@ -7,7 +7,7 @@
 % Author: Cristopher Morales Ubal                                              %
 % Institution: Eindhoven University of Technology                              %
 % Date: 2022/06/15                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg
index 93ad887d155..d9d8a07ed19 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2.cfg
@@ -8,7 +8,7 @@
 % Author: Cristopher Morales Ubal                                              %
 % Institution: Eindhoven University of Technology                              %
 % Date: 2022/09/12                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg
index 2cd26d57e2d..d8c4b002f53 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_heatcapacity_H2_ND.cfg
@@ -9,7 +9,7 @@
 % Author: Cristopher Morales Ubal                                              %
 % Institution: Eindhoven University of Technology                              %
 % Date: 2022/10/12                                                            %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_viscosity.cfg b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_viscosity.cfg
index 7df939a97d6..22fc0fcb07a 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_viscosity.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_mixingmodel_viscosity.cfg
@@ -8,7 +8,7 @@
 % Author: Cristopher Morales Ubal                                              %
 % Institution: Eindhoven University of Technology                              %
 % Date: 2022/06/27                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/species_transport/venturi_primitive_3species/species3_primitiveVenturi_inletFile.cfg b/TestCases/species_transport/venturi_primitive_3species/species3_primitiveVenturi_inletFile.cfg
index 06b085e6fdf..17488e3af0e 100644
--- a/TestCases/species_transport/venturi_primitive_3species/species3_primitiveVenturi_inletFile.cfg
+++ b/TestCases/species_transport/venturi_primitive_3species/species3_primitiveVenturi_inletFile.cfg
@@ -6,7 +6,7 @@
 % Author: T. Kattmann                                                          %
 % Institution: Bosch Thermotechniek B.V.                                       %
 % Date: 2021/10/14                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/transition/E387_Airfoil/transitional_BC_model_ConfigFile.cfg b/TestCases/transition/E387_Airfoil/transitional_BC_model_ConfigFile.cfg
index c721656a127..7127bdc0915 100644
--- a/TestCases/transition/E387_Airfoil/transitional_BC_model_ConfigFile.cfg
+++ b/TestCases/transition/E387_Airfoil/transitional_BC_model_ConfigFile.cfg
@@ -6,7 +6,7 @@
 % Institution: TOBB University of Economics and Technology                     %	
 %			   TAI-TUSAS Turkish Aerospace Industries                          %
 % Date: Oct 10th, 2016                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/transition/Schubauer_Klebanoff/transitional_BC_model_ConfigFile.cfg b/TestCases/transition/Schubauer_Klebanoff/transitional_BC_model_ConfigFile.cfg
index 9a3769a39b4..3ce91fc9f73 100644
--- a/TestCases/transition/Schubauer_Klebanoff/transitional_BC_model_ConfigFile.cfg
+++ b/TestCases/transition/Schubauer_Klebanoff/transitional_BC_model_ConfigFile.cfg
@@ -6,7 +6,7 @@
 % Institution: TOBB University of Economics and Technology                     %	
 %              TAI-TUSAS Turkish Aerospace Industries                          %
 % Date: Oct 10th, 2016                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/transition/T3A_FlatPlate/transitional_BC_model_ConfigFile.cfg b/TestCases/transition/T3A_FlatPlate/transitional_BC_model_ConfigFile.cfg
index ca01fc108d8..f3ae1289e26 100644
--- a/TestCases/transition/T3A_FlatPlate/transitional_BC_model_ConfigFile.cfg
+++ b/TestCases/transition/T3A_FlatPlate/transitional_BC_model_ConfigFile.cfg
@@ -6,7 +6,7 @@
 % Institution: TOBB University of Economics and Technology                     %	
 %			   TAI-TUSAS Turkish Aerospace Industries                          %
 % Date: Oct 10th, 2016                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/turbomachinery/APU_turbocharger/Jones_restart.cfg b/TestCases/turbomachinery/APU_turbocharger/Jones_restart.cfg
index a766bc072b0..c1a9dec3889 100755
--- a/TestCases/turbomachinery/APU_turbocharger/Jones_restart.cfg
+++ b/TestCases/turbomachinery/APU_turbocharger/Jones_restart.cfg
@@ -5,7 +5,7 @@
 % Author: S. Vitale                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: Jun 28th, 2017                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/turbomachinery/axial_stage_2D/Axial_stage2D.cfg b/TestCases/turbomachinery/axial_stage_2D/Axial_stage2D.cfg
index e1b98aee978..583ec2849eb 100755
--- a/TestCases/turbomachinery/axial_stage_2D/Axial_stage2D.cfg
+++ b/TestCases/turbomachinery/axial_stage_2D/Axial_stage2D.cfg
@@ -5,7 +5,7 @@
 % Author: S. Vitale                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: Feb 28th, 2017                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/turbomachinery/axial_stage_2D/zone_1.cfg b/TestCases/turbomachinery/axial_stage_2D/zone_1.cfg
index 5104dbd1dd7..7f4bdb57fbe 100644
--- a/TestCases/turbomachinery/axial_stage_2D/zone_1.cfg
+++ b/TestCases/turbomachinery/axial_stage_2D/zone_1.cfg
@@ -5,7 +5,7 @@
 % Author: S. Vitale                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: Feb 28th, 2017                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/turbomachinery/axial_stage_2D/zone_2.cfg b/TestCases/turbomachinery/axial_stage_2D/zone_2.cfg
index f8e8677c2d2..2fe06969028 100644
--- a/TestCases/turbomachinery/axial_stage_2D/zone_2.cfg
+++ b/TestCases/turbomachinery/axial_stage_2D/zone_2.cfg
@@ -5,7 +5,7 @@
 % Author: S. Vitale                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: Feb 28th, 2017                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/turbomachinery/centrifugal_blade/centrifugal_blade.cfg b/TestCases/turbomachinery/centrifugal_blade/centrifugal_blade.cfg
index c50f217363e..cd0716b7021 100755
--- a/TestCases/turbomachinery/centrifugal_blade/centrifugal_blade.cfg
+++ b/TestCases/turbomachinery/centrifugal_blade/centrifugal_blade.cfg
@@ -5,7 +5,7 @@
 % Author:S. Vitale                                                             %
 % Institution: Delft University of Technology                                  %
 % Date: Oct 26th, 2015                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/turbomachinery/centrifugal_stage/centrifugal_stage.cfg b/TestCases/turbomachinery/centrifugal_stage/centrifugal_stage.cfg
index 8c4f5ebc038..d3571d77a9b 100755
--- a/TestCases/turbomachinery/centrifugal_stage/centrifugal_stage.cfg
+++ b/TestCases/turbomachinery/centrifugal_stage/centrifugal_stage.cfg
@@ -5,7 +5,7 @@
 % Author: S. Vitale                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: Oct 28th, 2015                                                         %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg b/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg
index 87c0f8abaa8..4d2097fc80f 100644
--- a/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg
+++ b/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg
@@ -5,7 +5,7 @@
 % Author: S. Vitale                                                            %
 % Institution: Delft University of Technology                                  %
 % Date: 2017.03.01                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/tutorials.py b/TestCases/tutorials.py
index d7ea51572bd..71c4319b65c 100644
--- a/TestCases/tutorials.py
+++ b/TestCases/tutorials.py
@@ -3,7 +3,7 @@
 ## \file parallel_regression.py
 #  \brief Python script for automated regression testing of SU2 examples
 #  \author A. Aranake, A. Campos, T. Economon, T. Lukaczyk, S. Padron
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/unsteady/pitching_naca64a010_euler/pitching_NACA64A010.cfg b/TestCases/unsteady/pitching_naca64a010_euler/pitching_NACA64A010.cfg
index f7aefbf144f..0585043774b 100644
--- a/TestCases/unsteady/pitching_naca64a010_euler/pitching_NACA64A010.cfg
+++ b/TestCases/unsteady/pitching_naca64a010_euler/pitching_NACA64A010.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/unsteady/pitching_naca64a010_rans/turb_NACA64A010.cfg b/TestCases/unsteady/pitching_naca64a010_rans/turb_NACA64A010.cfg
index e2a0beda284..83b3e0c46a6 100644
--- a/TestCases/unsteady/pitching_naca64a010_rans/turb_NACA64A010.cfg
+++ b/TestCases/unsteady/pitching_naca64a010_rans/turb_NACA64A010.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: 2011.11.02                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/unsteady/plunging_naca0012/plunging_NACA0012.cfg b/TestCases/unsteady/plunging_naca0012/plunging_NACA0012.cfg
index dcc907f5bca..b1136ad91a0 100644
--- a/TestCases/unsteady/plunging_naca0012/plunging_NACA0012.cfg
+++ b/TestCases/unsteady/plunging_naca0012/plunging_NACA0012.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: Jun 12, 2014                                                           %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/unsteady/square_cylinder/turb_square.cfg b/TestCases/unsteady/square_cylinder/turb_square.cfg
index da3ca2f261f..7b94e4227cc 100644
--- a/TestCases/unsteady/square_cylinder/turb_square.cfg
+++ b/TestCases/unsteady/square_cylinder/turb_square.cfg
@@ -5,7 +5,7 @@
 % Author: Thomas D. Economon						                           %
 % Institution: Stanford University                                             %
 % Date: 2013.02.25                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/user_defined_functions/lam_flatplate.cfg b/TestCases/user_defined_functions/lam_flatplate.cfg
index 457ef91fc10..3f96723da55 100644
--- a/TestCases/user_defined_functions/lam_flatplate.cfg
+++ b/TestCases/user_defined_functions/lam_flatplate.cfg
@@ -4,7 +4,7 @@
 % Case description: Test custom outputs and objective function.                %
 % Author: P. Gomes                                                             %
 % Date: 5th Jan 2022                                                           %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/vandv.py b/TestCases/vandv.py
index a5757cd7043..adcf295916f 100644
--- a/TestCases/vandv.py
+++ b/TestCases/vandv.py
@@ -6,7 +6,7 @@
 #   - Use the SU2 --dry_run mode for configs of large tests.
 #   - Restart from converged results for medium problems.
 #   - Run small cases (<20s) to convergence.
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/TestCases/vandv/species_transport/sandia_jet/validation.cfg b/TestCases/vandv/species_transport/sandia_jet/validation.cfg
index f72e90167ce..6ca77c4ca66 100644
--- a/TestCases/vandv/species_transport/sandia_jet/validation.cfg
+++ b/TestCases/vandv/species_transport/sandia_jet/validation.cfg
@@ -5,7 +5,7 @@
 % Author: S.J.H. Bosmans                                                            %
 % Institution: TU Eindhoven (TU/e)                                                  %
 % Date: 2023/05/04                                                                  %
-% File Version 7.5.1 "Blackbird"                                                    %
+% File Version 8.0.0 "Harrier"                                                      %
 %                                                                                   %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/TestCases/wallfunctions/flatplate/compressible_SA/turb_SA_flatplate.cfg b/TestCases/wallfunctions/flatplate/compressible_SA/turb_SA_flatplate.cfg
index 8d1932d0170..4e437f579a1 100644
--- a/TestCases/wallfunctions/flatplate/compressible_SA/turb_SA_flatplate.cfg
+++ b/TestCases/wallfunctions/flatplate/compressible_SA/turb_SA_flatplate.cfg
@@ -6,7 +6,7 @@
 % Author: Nijso Beishuizen, T. Kattmann                                        %
 % Institution: Bosch Thermotechnology                                          %
 % Date: 2021.09.01                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/wallfunctions/flatplate/compressible_SST/turb_SST_flatplate.cfg b/TestCases/wallfunctions/flatplate/compressible_SST/turb_SST_flatplate.cfg
index 258e11c6081..7565572d097 100644
--- a/TestCases/wallfunctions/flatplate/compressible_SST/turb_SST_flatplate.cfg
+++ b/TestCases/wallfunctions/flatplate/compressible_SST/turb_SST_flatplate.cfg
@@ -6,7 +6,7 @@
 % Author: Nijso Beishuizen, T. Kattmann                                        %
 % Institution: Bosch Thermotechnology                                          %
 % Date: 2021.09.01                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/wallfunctions/flatplate/incompressible_SA/turb_SA_flatplate.cfg b/TestCases/wallfunctions/flatplate/incompressible_SA/turb_SA_flatplate.cfg
index 00ec3704293..6a63d1febd2 100644
--- a/TestCases/wallfunctions/flatplate/incompressible_SA/turb_SA_flatplate.cfg
+++ b/TestCases/wallfunctions/flatplate/incompressible_SA/turb_SA_flatplate.cfg
@@ -6,7 +6,7 @@
 % Author: Nijso Beishuizen, T. Kattmann                                        %
 % Institution: Bosch Thermotechnology                                          %
 % Date: 2021.09.01                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/TestCases/wallfunctions/flatplate/incompressible_SST/turb_SST_flatplate.cfg b/TestCases/wallfunctions/flatplate/incompressible_SST/turb_SST_flatplate.cfg
index aa0e928ac5e..0492f2222a6 100644
--- a/TestCases/wallfunctions/flatplate/incompressible_SST/turb_SST_flatplate.cfg
+++ b/TestCases/wallfunctions/flatplate/incompressible_SST/turb_SST_flatplate.cfg
@@ -6,7 +6,7 @@
 % Author: Nijso Beishuizen, T. Kattmann                                        %
 % Institution: Bosch Thermotechnology                                          %
 % Date: 2021.09.01                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
diff --git a/UnitTests/Common/containers/CLookupTable_tests.cpp b/UnitTests/Common/containers/CLookupTable_tests.cpp
index f17049ec341..5e63f60b149 100644
--- a/UnitTests/Common/containers/CLookupTable_tests.cpp
+++ b/UnitTests/Common/containers/CLookupTable_tests.cpp
@@ -2,7 +2,7 @@
  * \file CLookupTable_tests.cpp
  * \brief Unit tests for the lookup table.
  * \author N. Beishuizen
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/Common/geometry/CGeometry_test.cpp b/UnitTests/Common/geometry/CGeometry_test.cpp
index edd24e82ec0..6bd2dd583df 100644
--- a/UnitTests/Common/geometry/CGeometry_test.cpp
+++ b/UnitTests/Common/geometry/CGeometry_test.cpp
@@ -2,7 +2,7 @@
  * \file CGeometry_tests.cpp
  * \brief Unit tests for CGeometry.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/Common/geometry/dual_grid/CDualGrid_tests.cpp b/UnitTests/Common/geometry/dual_grid/CDualGrid_tests.cpp
index 2193446fe84..0f6dbc38ae8 100644
--- a/UnitTests/Common/geometry/dual_grid/CDualGrid_tests.cpp
+++ b/UnitTests/Common/geometry/dual_grid/CDualGrid_tests.cpp
@@ -2,7 +2,7 @@
  * \file CDualGrid_tests.cpp
  * \brief Unit tests for the dual grid classes
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/Common/geometry/primal_grid/CPrimalGrid_tests.cpp b/UnitTests/Common/geometry/primal_grid/CPrimalGrid_tests.cpp
index 5323fc0da56..0c6596b067a 100644
--- a/UnitTests/Common/geometry/primal_grid/CPrimalGrid_tests.cpp
+++ b/UnitTests/Common/geometry/primal_grid/CPrimalGrid_tests.cpp
@@ -2,7 +2,7 @@
  * \file CPrimalGrid_tests.cpp
  * \brief Unit tests for the primal grid classes
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/Common/simple_ad_test.cpp b/UnitTests/Common/simple_ad_test.cpp
index 32e2b22db83..23dbed55476 100644
--- a/UnitTests/Common/simple_ad_test.cpp
+++ b/UnitTests/Common/simple_ad_test.cpp
@@ -4,7 +4,7 @@
  *        basic functionality, this also serves as a regression test
  *        to make sure that AD works within unit testing.
  * \author C. Pederson
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/Common/simple_directdiff_test.cpp b/UnitTests/Common/simple_directdiff_test.cpp
index 2b97810dd28..f6c7411e97f 100644
--- a/UnitTests/Common/simple_directdiff_test.cpp
+++ b/UnitTests/Common/simple_directdiff_test.cpp
@@ -4,7 +4,7 @@
  *        basic functionality, this also serves as a regression test
  *        to make sure that DD works within unit testing.
  * \author C. Pederson
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/Common/toolboxes/C1DInterpolation_tests.cpp b/UnitTests/Common/toolboxes/C1DInterpolation_tests.cpp
index 026763295fb..b229bd939c8 100644
--- a/UnitTests/Common/toolboxes/C1DInterpolation_tests.cpp
+++ b/UnitTests/Common/toolboxes/C1DInterpolation_tests.cpp
@@ -2,7 +2,7 @@
  * \file C1DInterpolation_tests.cpp
  * \brief Unit tests for splines and what not.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/Common/toolboxes/CQuasiNewtonInvLeastSquares_tests.cpp b/UnitTests/Common/toolboxes/CQuasiNewtonInvLeastSquares_tests.cpp
index 2d336ce7db9..a3e62a932ab 100644
--- a/UnitTests/Common/toolboxes/CQuasiNewtonInvLeastSquares_tests.cpp
+++ b/UnitTests/Common/toolboxes/CQuasiNewtonInvLeastSquares_tests.cpp
@@ -3,7 +3,7 @@
  * \brief Unit tests for the CQuasiNewtonInvLeastSquares class.
  * Which should find the root of a n-d linear problem in n+1 iterations.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
index a495ea3358e..b002fe0a472 100644
--- a/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
+++ b/UnitTests/Common/toolboxes/multilayer_perceptron/CLookUp_ANN_tests.cpp
@@ -2,7 +2,7 @@
  * \file CLookUp_ANN_tests.cpp
  * \brief Unit tests for CLookUp_ANN and CIOMap classes.
  * \author E.C.Bunschoten
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/Common/toolboxes/ndflattener_tests.cpp b/UnitTests/Common/toolboxes/ndflattener_tests.cpp
index 25d2e85d4e8..87d3b1f9e29 100644
--- a/UnitTests/Common/toolboxes/ndflattener_tests.cpp
+++ b/UnitTests/Common/toolboxes/ndflattener_tests.cpp
@@ -2,7 +2,7 @@
  * \file ndflattener_tests.cpp
  * \brief Unit tests for NdFlattener template classes.
  * \author M. Aehle
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/Common/vectorization.cpp b/UnitTests/Common/vectorization.cpp
index 22fa454f961..db53702daba 100644
--- a/UnitTests/Common/vectorization.cpp
+++ b/UnitTests/Common/vectorization.cpp
@@ -2,7 +2,7 @@
  * \file vectorization.cpp
  * \brief Unit tests for the SIMD type and associated expression templates.
  * \author P. Gomes
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/SU2_CFD/gradients.cpp b/UnitTests/SU2_CFD/gradients.cpp
index 0b0beaaf24e..26ac02d8a95 100644
--- a/UnitTests/SU2_CFD/gradients.cpp
+++ b/UnitTests/SU2_CFD/gradients.cpp
@@ -2,7 +2,7 @@
  * \file gradients.cpp
  * \brief Unit tests for gradient calculation.
  * \author P. Gomes, T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/SU2_CFD/numerics/CNumerics_tests.cpp b/UnitTests/SU2_CFD/numerics/CNumerics_tests.cpp
index 0f1110b0c70..c22fc083794 100644
--- a/UnitTests/SU2_CFD/numerics/CNumerics_tests.cpp
+++ b/UnitTests/SU2_CFD/numerics/CNumerics_tests.cpp
@@ -2,7 +2,7 @@
  * \file CNumerics_tests.cpp
  * \brief Unit tests for the numerics classes.
  * \author C. Pederson
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/SU2_CFD/windowing.cpp b/UnitTests/SU2_CFD/windowing.cpp
index 960e28e4fc0..e0e0a03cde6 100644
--- a/UnitTests/SU2_CFD/windowing.cpp
+++ b/UnitTests/SU2_CFD/windowing.cpp
@@ -2,7 +2,7 @@
  * \file windowing.cpp
  * \brief Unit tests for windowed time-averaging.
  * \author C. Bauer
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/UnitQuadTestCase.hpp b/UnitTests/UnitQuadTestCase.hpp
index 9d582291b99..c0eccdc9941 100644
--- a/UnitTests/UnitQuadTestCase.hpp
+++ b/UnitTests/UnitQuadTestCase.hpp
@@ -2,7 +2,7 @@
  * \file UnitQuadTestCase.hpp
  * \brief Simple unit quad test to be used in unit tests.
  * \author T. Albring
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/UnitTests/test_driver.cpp b/UnitTests/test_driver.cpp
index a8ffcd3c8ce..d7299a3827f 100644
--- a/UnitTests/test_driver.cpp
+++ b/UnitTests/test_driver.cpp
@@ -2,7 +2,7 @@
  * \file test_driver.cpp
  * \brief The main entry point for unit tests (the main()).
  * \author C. Pederson
- * \version 7.5.1 "Blackbird"
+ * \version 8.0.0 "Harrier"
  *
  * SU2 Project Website: https://su2code.github.io
  *
diff --git a/config_template.cfg b/config_template.cfg
index 5f4fab871b8..811df18a014 100644
--- a/config_template.cfg
+++ b/config_template.cfg
@@ -5,7 +5,7 @@
 % Author: ___________________________________________________________________  %
 % Institution: ______________________________________________________________  %
 % Date: __________                                                             %
-% File Version 7.5.1 "Blackbird"                                               %
+% File Version 8.0.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
diff --git a/meson.build b/meson.build
index d0c0e4e10e8..5dcd4154fbb 100644
--- a/meson.build
+++ b/meson.build
@@ -1,5 +1,5 @@
 project('SU2', 'c', 'cpp',
-        version: '7.5.1 "Blackbird"',
+        version: '8.0.0 "Harrier"',
         meson_version: '>=0.61.1',
         license: 'LGPL2',
         default_options: ['buildtype=release',
@@ -326,7 +326,7 @@ endif
 
 message('''-------------------------------------------------------------------------
          |    ___ _   _ ___                                                      |
-         |   / __| | | |_  )   Release 7.5.1 "Blackbird"                         |
+         |   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
          |   \__ \ |_| |/ /                                                      |
          |   |___/\___//___|   Meson Configuration Summary                       |
          |                                                                       |
diff --git a/meson.py b/meson.py
index e58b9fa3b09..14c39f67fc6 100755
--- a/meson.py
+++ b/meson.py
@@ -3,7 +3,7 @@
 ## \file meson.py
 #  \brief An extended meson script for setting up the environment and running meson
 #  \author T. Albring and F. Poli
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/meson_scripts/init.py b/meson_scripts/init.py
index 948636d3856..d71785b693f 100755
--- a/meson_scripts/init.py
+++ b/meson_scripts/init.py
@@ -4,7 +4,7 @@
 #  \brief Initializes necessary dependencies for SU2 either using git or it
 #         fetches zip files.
 #  \author T. Albring and F. Poli
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/preconfigure.py b/preconfigure.py
index c6dc0220a5f..a65d1636bd1 100755
--- a/preconfigure.py
+++ b/preconfigure.py
@@ -3,7 +3,7 @@
 ## \file preconfigure.py
 #  \brief An preconfigure script for setting up the build environment
 #  \author T. Albring and F. Poli
-#  \version 7.5.1 "Blackbird"
+#  \version 8.0.0 "Harrier"
 #
 # SU2 Project Website: https://su2code.github.io
 #
diff --git a/su2omp.syntax.json b/su2omp.syntax.json
index 28e22388ccc..72b4dee1a92 100644
--- a/su2omp.syntax.json
+++ b/su2omp.syntax.json
@@ -4,7 +4,7 @@
     "\\file su2omp.syntax.json",
     "\\brief Definitions for the OpDiLib syntax checker",
     "\\author J. Blühdorn",
-    "\\version 7.5.1 \"Blackbird\"",
+    "\\version 8.0.0 \"Harrier\"",
 
     "SU2 Project Website: https://su2code.github.io",